c5 c10 c12 c14 c15 c16 c17 c18 c20 c25 c35 c40 c90 c100 c110 c120 c130 c140 c150 c152 c160 c170 c180 c190 c192 c200 c210 c220 c230 c240 c250 c260 c270 c280 c290 c300 c310a c310b c310c c310d c314a c314b c314c c314d c320a c320b c320c c324a c324b c324c c330 c332 c340 c350 c360 c370 c380 c390 c400 c410 c420 c430 c440 c450 c460 c490 c510a c510b c510c c510d c510e c510f c602 c604 c606 c608 c610 c612 c614 c616 c620 c640 c652 c654 c660 eof 1996010500123 19960105 00123 NM 1996 1 5 96FDEA00001 1 19960102 A 5330 SKIN BOEING 727 7272S2F 1384O81 NM BS 512 DENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 213FE 22935 THE FUSELAGE SKIN IS DENTED AT BS 512 BETWEEN STR 26 TO 27L. REMOVED DENT AND REPAIRED WITH DOUBLER AT BS 512 BETWEEN S TR 26 TO 27L IAW FEDEX SRM 53-30-3. 2 L 7 3 4F A3WE 1996010500125 19960105 00125 NM 1996 1 5 96FDEA00003 1 19960102 A 5522 657278420 SKIN BOEING 727 7272S2F 1384O81 NM RT ELEVATOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 213FE 22935 DUE TO SEVERAL DISCREPANCIES CONSISTING OF CRACKS AND WORN FASTENER HOLES, RT ELEVATOR REQUIRED REPLACEMENT. REMOVED AN D REPLACED RT ELEVATOR PER FEDEX MM 27-30-0, 27-30-01, 27-30-21, 27-30-05, 27-30-11. FUNCTIONAL TEST PER FEDEX MM 27-30 -01 CHECKS GOOD. 2 L 7 3 4F A3WE 1996010500127 19960105 00127 NM 1996 1 5 96FDEA00005 1 19960102 A 5330 SKIN BOEING 727 7272S2F 1384O81 NM BS 1223 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 213FE 22935 CRACK IN CORNER OF SKIN, BS 1223, LBL 16, WL 148. REPAIRED CRACK IN CORNER OF SKIN, BS 1223, LBL 16, WL 148, PER FEDEX EA 7-5330-26829. 2 L 7 3 4F A3WE 1996010500130 19960105 00130 NE 1996 1 5 COMA9630001 3 19960102 A 6114 660714200 HUB SAAB SF340 SF340A 7850100 EU ROTOL R354 R3544123F13 NE PROPELLER DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 941CA 9725 1445 340A021 DRG705886 WHILE PERFORMING DOWTY SB SF340-61-58 SCAN C, SEVERAL FLAW INDICATION WERE DISCOVERED. PROPELLER WAS DISASSEMBLED AND H UB (S/N 110351) WAS REMOVED FROM SERVICE. 2 L 7 2 4T RT A52EU 6 C P61GL 1996010500133 19960105 00133 EA 1996 1 5 COMA9660003 1 19960101 A 2750 601R93001 FLAP CONTROL CNDAIR CL600 CL6002B19 EA INST PANEL DEFECTIVE A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 941CA 6805 2165 7050 FLAPS FAIL MESSAGE ON EICAS. REPLACED THE FLAP POSITION SELECTOR LEVER ASSY. 2 L 7 2 4F RT A21EA 1996010500347 19960105 00347 NM 1996 1 5 95UAL900365 1 19960102 A 3350 LAMP BOEING 767 767322 1385200 NM LT FUSELAGE FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 650UA 25287 THE 6TH EMERGENCY LIGHT ON THE OUTSIDE LEFT SIDE OF THE FUSELAGE WAS INOPERABLE. THE LAMP WAS REPLACED AND THE LIGHT WO RKED NORMALLY DURING AN OPERATIONAL CHECK. 2 L 7 2 4F RT A1NM 1996010500348 19960105 00348 NM 1996 1 5 95UAL900366 1 19960102 A 3350 STRIP BOEING 757 757222 1384956 NM CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 514UA 24839 EMERGENCY ESCAPE LIGHT STRIP INOP ROW 35. REPLACED LIGHT STRIP AND CHECKS OK. 2 L 7 2 4F RT A2NM 1996010500349 19960105 00349 WP 1996 1 5 95UAL900367 1 19960102 A 3244 TIRE DOUG DC10 DC1010 3022110 WP NR 8 FAILED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 WP 29 1841U 46634 RETURNED T0 LAX UNDER AMBER ALERT DUE TO BLOWN NR 8 TIRE ON TAKEOFF AND POSSIBLE DAMAGE. NR 7 TIRE BLEW ON TAXI IN, TOW ED TO GATE AND TRIP CANCELLED. REPLACED NR 1 RT SPOILER, RT INBD FLAP, RT INBD FLAP VANE, NR 7 AND 8 TIRES, RT HORIZ ST AB LEADING EDGE AND NR 7 BRAKE. REPAIRED FUSELAGE AND INSPECTED NR 2 ENGINE FOR FOD. FOD TO THE NR 8 TIRE WAS THE CAUS E OF THE INITIAL TIRE FAILURE. 2 L 7 3 4F A22WE 1996010500350 19960105 00350 1996 1 5 9600019763 4 19960101 A 3442 RADAR SYST DOUG DC9 DC941 302207N WP FWD FUSELAGE MALFUNCTIONED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 763NW 47396 WEATHER RADAR WOULD NOT PAINT GROUND RETURNS AND BEGAN SPOKING AFTER TAKEOFF. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED RADAR TRANSCEIVER AND INDICATOR WITH NO HELP. DEFERRED RADAR SYSTEM PER MEL 34-19 AND AIRCRAFT RET URNED TO SERVICE. 2 L 7 2 4F A6WE 1996010500351 19960105 00351 WP 1996 1 5 9600029607 1 19960101 A 3260 LATCH DOUG DC9 DC932 3022066 WP LT MLG DOOR OUT OF ADJUST A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 607NW 47232 DURING CLIMB, THE LEFT MAIN LANDING GEAR DOOR OPEN LIGHT ILLUMINATED AFTER LANDING GEAR RETRACTION. FOLLOWED COCKPIT OP ERATING MANUAL PROCEDURE AND LIGHT EXTINGUISHED AFTER LANDING GEAR WAS EXTENDED FOR LANDING. AIRCRAFT RETURNED TO DTW A ND LANDED WITHOUT INCIDENT. ADJUSTED LEFT MAIN LANDING GEAR DOOR LATCH AND ROLLER ASSEMBLY, OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996010500352 19960105 00352 WP 1996 1 5 9600039612 1 19960102 A 3260 UNSAFE LIGHT DOUG DC9 DC932 3022066 WP NLG ILLUMINATED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 612NW 47436 DURING CLIMB, THE NOSE LANDING GEAR UNSAFE LIGHT ILLUMINATED DURING UPLATCH CHECK. RECYCLED LANDING GEAR AND LIGHT REMA INED ILLUMINATED. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. INSPECTED AND OPERATIONALLY CHECKED NOSE LANDI NG GEAR SYSTEM. OPERATIONAL CHECK GOOD AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996010500353 19960105 00353 EU 1996 1 5 9600043241 1 19960101 A 3350 321454 POWER SUPPLY AIRBUS 320 A320211 3930320 EU CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 341NW 13530 6277 380 DURING LINE MAINTENANCE, THE LEFT EMERGENCY LIGHTS POWER SUPPLY/BATTERY PACK FAILED SYSTEM TEST. REPLACED THE POWER SUP PLY AND OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996010500354 19960105 00354 EU 1996 1 5 9600053225 1 19960102 A 3350 321430 BATTERY PACK AIRBUS 320 A320211 3930320 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 325US 281 DURING LINE MAINTENANCE, AFT LEFT EMERGENCY LIGHTS BATTERY PACK FAILS COM CHECK. REPLACED BATTERY PACK AND OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996010500355 19960105 00355 EU 1996 1 5 96FDEA00006 1 19960101 A 2910 HYD TUBE AIRBUS 310 A310203 EU NR 2 ENGINE LEAKING A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 413FE 397 SIN - ON CLIMBOUT OF WSSS, LOST YELLOW FLUID TO STAND PIPE AND RETURNED TO WSSS. ON NR 2 ENG TUBE ASSY TO PRESSURE SWIT CH FOUND LEAKING. REMOVED AND REPLACED SAME, (P/N 224-5-12-507). SERVICED YELLOW HYD SYS, LEAK CHECK BY ENG RUN OK. 2 L 7 2 4F RT A35EU 1996010500357 19960105 00357 NM 1996 1 5 DL72L960001 1 19960101 A 3530 PBE BOEING 727 727232 1384082 NM CABIN POPPED INDICATOR A DALA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 27 501DA 21303 FIRST CLASS COAT CLOSET PBE UNSERVICEABLE, INDICATOR POPPED. REPLACED PBE. 2 L 7 3 4F A3WE 1996010500363 19960105 00363 NM 1996 1 5 DL72S960004 1 19960101 A 3350 900835A BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 403DA 21147 RIGHT OVERWING EMERGENCY LIGHT EXIT SIGNS INOP. REPLACED BATTERY PACK AND CHECKS OK. 2 L 7 3 4F A3WE 1996010500364 19960105 00364 NM 1996 1 5 DL72S960005 1 19960101 A 3350 900835A BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 403DA 21147 RIGHT OVERWING CENTER EMERGENCY SLIDE LIGHT INOP. REPLACED BATTERY PACK AND CHECKS OK. 2 L 7 3 4F A3WE 1996010500371 19960105 00371 NM 1996 1 5 DL757960015 1 19960101 A 3350 LIGHT BOEING 757 757232 1384965 NM CABIN MISSING A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 625DL 22915 DURING INSPECTION, FOUND THREE EMERGENCY TRACK LIGHTS MISSING. REPLACED LIGHT ASSEMBLIES AND OPERATION NORMAL. 2 L 7 2 4F RT A2NM 1996010500379 19960105 00379 1996 1 5 DLM88960003 4 19960101 A 3417 CADA DOUG MD88 MD88 3023688 NM RIGHT MALFUNCTIONED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 27 925DL 49712 AT V1, F/O AIRSPEED AND ALT INDICATORS FAILED AND AT LIFT OFF OVERSPEED WARNING CAME ON WITH F/S FAILURE ON BOTH SIDES. GOING TO ALT ON F/O SIDE DID NOT CHANGE OR CADC BOTH ON 1. FLIGHT RETURNED TO EWR. INSTRUMENTS RETURNED TO NORMAL AFT ER LANDING. REPLACED NR 2 CADC (P/N HG28D80) (SN 88111912) AND CADC SWITCH UNIT. 2 L 7 2 4F RT A6WE 1996010500547 19960105 00547 NM 1996 1 5 95UAL900368 1 19960103 A 3350 BATTERY PACK BOEING 727 727222 1384073 NM CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7263U 21410 RAMP PERSONNEL NOTICED EXTERIOR EMERG LIGHTS ON INITIALLY AND THEN WENT OUT. FOUND BOTH ENTRY DOORS AND SERVICE DOORS S LIDE LIGHTS INOPERATIVE. USAIR BATTERY PACK TRIED AND LIGHTS WORKED INITIALLY AND THEN TURNED OFF AND CAME BACK ON. RE PLACED SLIDE BATTERY PACK AND POWER SUPPLY. 2 L 7 3 4F A3WE 1996010500548 19960105 00548 WP 1996 1 5 95UAL900369 1 19960103 A 3350 LIGHT DOUG DC10 DC1010 3022110 WP GALLEY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1830U 46629 GALLEY LIGHT ASSEMBLY INOPERATIVE. REPLACED EEL LIGHT ASSEMBLY. 2 L 7 3 4F A22WE 1996010500549 19960105 00549 NM 1996 1 5 9600066303 1 19960102 A 3350 900835A BATTERY PACK BOEING 747 747451 1384940 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 663US 23818 DURING LINE CHECK, THE LEFT UPPER DECK DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED POWER SUPPLY BATTERY PACK A ND OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996010500550 19960105 00550 WP 1996 1 5 9600079982 1 19960102 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 982US 45790 DURING LINE CHECK, FOUND FORWARD EMERGENCY LIGHTS DIM. REPLACED BATTERIES AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996010500551 19960105 00551 WP 1996 1 5 9600089969 1 19960101 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9333 47246 DURING LINE CHECK, FOUND OVERHEAD EMERGENCY LIGHTS INOPERATIVE FORWARD OF ROW 4. REPLACED BATTERIES AND OPERATIONAL CHE CK GOOD. 2 L 7 2 4F A6WE 1996010500552 19960105 00552 WP 1996 1 5 9600099923 1 19960101 A 2530 OVEN DOUG DC9 DC932 3022066 WP GALLEY DIRTY A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 01 927RC 47469 DURING APPROACH, SMOKE ACCUMULATED IN COCKPIT. DECLARED EMERGENCY WITH ATC AND AIRCRAFT LANDED WITHOUT FURTHER INCIDENT . FIRE DEPARTMENT MET FLIGHT AND VERIFIED SMOKE CAME FROM OVEN. CLEANED, OPERATIONALLY CHECKED OVEN AND OPERATIONAL CH ECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996010500553 19960105 00553 NM 1996 1 5 96UAL900001 1 19960103 A 3230 RETRACT MECH BOEING 747 747238B 1384828 NM NLG MALFUNCTIONED A UALA L ABORTED APPROACH J WARNING INDICATION LD LANDING 1 WP 29 161UA 21352 NOSE GEAR HAD TO BE EXTENDED BY ALTERNATE SYSTEM, HAD A RED GEAR LIGHT AND NO ALTERNATE NOSE GEAR OPEN LIGHT. GPWS SYST EM GAVE AN AURAL GEAR WARNING, CYCLED GEAR. 2 L 7 4 4F A20WE 1996010500554 19960105 00554 NM 1996 1 5 96UAL900002 1 19960103 A 2421 GENERATOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LEFT FAILED A UALA K NONE J H WARNING INDICATION ELECT. POWER LOSS-50 PC NR NOT REPORTED 1 WP 29 772UA 26930 BACKUP ELECTRICAL SYSTEM EICAS MESSAGE DISPLAYED, INDICATING FAILURE OF BACKUP ELECTRICAL SYSTEM. BACKUP CONVERTER AND LEFTHAND BACKUP GENERATOR WERE REPLACED. VENDOR CONFIRMED FAILURE OF THE PMG STATOR WINDINGS IN THE BACKUP GENERATOR. A LSO, THE BACKUP CONVERTER WAS FOUND TO BE DEFECTIVE. 2 L 7 2 4F 4 F RT T0001SE E46NE 1996010500555 19960105 00555 WP 1996 1 5 ABXA9600002 1 19960104 A 3230 LATCH MECH NIHON YS11 YS11A500 6310416 WP NLG ICED UP A ABXA K NONE J WARNING INDICATION DE DESCENT 1 GL 23 919AX 2113 DURING DESCENT CHECKLIST WITH LANDING GEAR HANDLE PLACED TO NEUTRAL, HYDRAULIC LEVER DEPRESSED AND NOSE LANDING GEAR EXT ENDED. TRIED SEVERAL TIMES AND NOSE GEAR EXTENDED EACH TIME. INSPECTED GEAR, FOUND ICE IN LATCHES. REMOVED ICE FROM G EAR AND LATCHES, CLEANED AREA, LUBED GEAR AND CABLES, INSPECTED SWITCHES AND WIRING HARNESS, NO DAMAGE NOTED. 2 L 7 2 4T A1PC 1996010500556 19960105 00556 SW 1996 1 5 COMA9620001 1 19960102 A 2750 850110 POTENTIOMETER SWRNGN SA227 SA227AC 8780603 SW TE FLAPS DEFECTIVE A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 704C AC704 FLAPS WOULD NOT EXTEND DURING LANDING APPROACH. REPLACED THE FLAP POSITION TRANSMITTER. 1 L 7 2 4T A8SW 1996010500557 19960105 00557 EU 1996 1 5 COMA9630002 1 19960101 A 2612 FIRE DETECTOR SAAB SF340 SF340A 7850100 EU LT ENGINE DIRTY A COMA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 SO 01 358CA 340A047 LEFT ENGINE TAIL PIPE HOT WARNING SHORTLY AFTER TAKEOFF. CLEANED TAIL PIPE FIRE DETECTORS AND FOUND NO DEFECTS. ACFT R ETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 1996010500558 19960105 00558 EA 1996 1 5 COMA9660004 1 19960102 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA LT/RT FLAPS DEFECTIVE A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 941CA 7050 FLAPS FAIL CAUTION MESSAGE DURING DESCENT. REPLACED THE LT AND RT FLAPS BRAKE AND POSITION SENSOR. 2 L 7 2 4F RT A21EA 1996010500565 19960105 00565 EU 1996 1 5 QXEA9600001 1 19960101 A 3350 1820 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 803PH 11031 BOI - EMERGENCY EXIT LIGHT AT ROW 8 INOP RIGHTHAND SIDE. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURN ED TO SERVICE. 2 L 7 2 4F RT A20EU 1996010500567 19960105 00567 EU 1996 1 5 QXEA9600004 1 19960101 A 3350 5515800104 CIRCUIT BOARD FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 462AU 11054 PDX - FORWARD CABIN EXIT LIGHT INOP. CIRCUIT BOARD WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVI CE. 2 L 7 2 4F RT A20EU 1996010500569 19960105 00569 NM 1996 1 5 VSTA9601001 1 19960102 A 3231 RETRACT MECH BOEING 737 737247 138448D NM RT MLG DOORS MALFUNCTIONED A VSTA K NONE O OTHER IN INSP/MAINT 1 WP 07 308VA 19613 DURING RETRACT OF MLG PER B737 MM 32-32-0 FOR COMPLIANCE WITH VASI EO NR 32-30-1 RT GEAR OPERATION AND FAIRING WAS SATIS FACTORY. ON DOWN SELECTION THE UPPER FLYING DOOR RUBBED HARD ON THE LOWER DOOR JAMMING BOTH DOORS TOGETHER AND CAUSING DOOR RODS AND FITTINGS TRACK. MALFUNCTION BEING INVESTIGATED. DAMAGE ASSESSMENT, REPAIR AND REPLACEMENT IN PROGRESS. 2 L 7 2 4F A16WE 1996011200001 19960112 00001 NE 1996 1 12 95UAL900370 2 19960104 A 7230 COMPRESSOR BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE NR 1 ENGINE STALLED A UALA C ABORTED TAKEOFF C F.O.D. TO TAKEOFF 1 WP 29 9071U 19952 655822 ON TAKEOFF AT 90 KNOTS, NR ONE ENGINE HAD A COMPRESSOR STALL. A BRIGHT FLASH WAS OBSERVED ON TAKEOFF, ABORTED TAKEOFF. SUPPLEMENTAL DATA UPDATE: ENGINE WAS BORESCOPED AT THE C-6, C-7, AND C-13 BLADES. BORESCOPE REVEALED EVIDENCE OF SMALL BIRD INGESTION WITH NO BLADE OR VANE DAMAGE. CSD COOLER AND PS3 SCREEN WERE CLEANED. 2 L 7 2 4F 4 F A16WE E2EA 1996011200003 19960112 00003 WP 1996 1 12 9600109910 1 19960104 A 3350 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 960N 47256 DURING LINE CHECK, FOUND CEILING EMERGENCY LIGHTS INOPERATIVE FROM ROWS 14 TO 19. REPLACED BATTERIES AND OPERATIONAL CH ECK GOOD. 2 L 7 2 4F A6WE 1996011200004 19960112 00004 NM 1996 1 12 9600112201 1 19960103 A 3150 T/O WARNING BOEING 727 727251 138408H NM FLIGHT DECK SOUNDED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 201US 22154 DURING TAKEOFF ROLL WITH FLAPS AT 5 DEGREES, TAKEOFF WARNING HORN ACTIVATED AND TAKEOFF WAS ABORTED. OPERATIONAL CHECK WAS PERFORMED AND SYSTEM INDICATION CHECKED OK. 2 L 7 3 4F A3WE 1996011200005 19960112 00005 WP 1996 1 12 9600129105 1 19960104 A 3260 UNSAFE LIGHT DOUG DC9 DC915 3022036 WP NLG ILLUMINATED A NWAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 01 95S 47205 DURING APPROACH INTO FAR, NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS EXTENDED. EXECUTED GO-AROUND AND RE CYCLED GEAR. ALL INDICATIONS WERE NORMAL AFTER THIRD CYCLE. AIRCRAFT LANDED WITHOUT INCIDENT. CHECKED NOSE GEAR DOWNL OCK SWITCH AND ALL CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996011200006 19960112 00006 WP 1996 1 12 9600139860 1 19960104 A 3350 60030451 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 768NC 47729 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND OPER ATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996011200007 19960112 00007 NM 1996 1 12 96FDEA00013 1 19960104 A 2781 40174 SWITCH BOEING 727 727277 138408S NM NR 5 LE FLAP INOPERATIVE A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 478FE 21395 AFTER A NORMAL T/O AND FLAP RETRACTION, WE LEVELED AT 5,000 FT AND LEADING EDGE DEVICE LIGHT CAME ON 2 DEGREE SHOWED NR 5 LED UNSAFE. WING ANTI-ICE ON CHECKLIST COMPLETION EXTINGUISHED LIGHT BUT IT CAME ON AGAIN SEVERAL TIMES NO STRUCTURAL LIMITS EXCEEDED. ANTI-ICE CYCLED ON AND OFF WITH NO RESULTS. REPLACED NR 5 L/E KRUEGER FLAP SWITCH. L/E FLAP INDICAT ION OPS CHECK SATISFACTORY ON GROUND TEST. 2 L 7 3 4F RT A3WE 1996011200008 19960112 00008 NM 1996 1 12 96FDEA00014 1 19960105 A 5312 65B07936287 STIFFENER BOEING 747 747245F 1384897 NM BS 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 640FE 20826 BS 400 BULKHEAD STIFFENER FOUND WITH CORROSION CRACK AT BWL 118, ADJACENT TO S 42L. STIFFENER REPLACED AS PER FEDEX B74 7 SRM REV 76 51-30-02. 2 L 7 4 4F A20WE 1996011200009 19960112 00009 NM 1996 1 12 96FDEA00015 1 19960105 A 5312 CHORD BOEING 747 747245F 1384897 NM BS 1000 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 640FE 20826 SIN - BS 1000 BULKHEAD LOWER CHORD FOUND CRACKED AT LBL 9, APPROX 0.75 AND RBL 9, APPROX 0.75. 2 L 7 4 4F A20WE 1996011200010 19960112 00010 NM 1996 1 12 96UAL900003 1 19960104 A 2612 1705 FIRE LOOP BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE NR 1 ENGINE INOPERATIVE A UALA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING NR NOT REPORTED 1 WP 29 9075U 19956 EXPERIENCED NUMBER ONE ENGINE FIRE WARNING, ENGINE WAS SHUTDOWN AND FIRE BOTTLE DISCHARGED. REPLACED NUMBER ONE ENGINE LOWER FIRE DETECTION LOOP, BOTH FIRE BOTTLES AND SQUIBS. 2 L 7 2 4F 4 F A16WE E2EA 1996011200011 19960112 00011 WP 1996 1 12 96UAL900004 1 19960104 A 3350 CONNECTOR DOUG DC10 DC1010 3022110 WP CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1816U 46615 EEL LIGHT INOPERATIVE LT SIDE FORWARD GALLEY. RESEATED LOOSE CONNECTOR. 2 L 7 3 4F A22WE 1996011200012 19960112 00012 NM 1996 1 12 96UAL900005 1 19960104 A 3350 BATTERY BOEING 727 727222 1384073 NM SERVICE DOOR DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7457U 21911 LT AFT SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY DUE TO FAILURE. 2 L 7 3 4F A3WE 1996011200013 19960112 00013 NM 1996 1 12 96UAL900006 1 19960104 A 4900 APU BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN ODOR A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 7457U 21911 WHEN PACKS RAN OFF, APU CABIN HAD BURNT OIL SMELL. 2 L 7 3 4F 4 F A3WE E2EA 1996011200014 19960112 00014 WP 1996 1 12 ABXA9600003 1 19960103 A 3350 1820 BULB DOUG DC8 DC861 3021952 WP OVERHEAD PANEL DEFECTIVE A ABXA K NONE O OTHER CR CRUISE 1 GL 23 849AX 45891 EMERGENCY EXIT DISARM LIGHT ON OVERHEAD PANEL INOP. RELAMPED EMERGENCY EXIT DISARM LIGHT AND OPS CHECK GOOD. 2 L 7 4 4F 4A25 1996011200015 19960112 00015 WP 1996 1 12 ABXA9600004 1 19960103 A 3260 H1410051 DN LOCK SWITCH DOUG DC9 DC933F 302207A WP NLG DEFECTIVE A ABXA O OTHER P NO WARNING INDICATION DE DESCENT 1 GL 23 932AX 47465 NOSE GEAR GREEN DOWN LIGHT WENT OUT WITH GEAR EXTENSION, CYCLED LANDING GEAR, LIGHT FLICKERED OUT AND ON AGAIN. VERIFIE D, FOUND PIN 'C' BROKEN OFF OF NOSE GEAR DOWNLOCK SWITCH. REMOVED BROKEN PIN FROM CONNECTOR PLUG AND REPLACED NOSE GEAR DOWNLOCK SWITCH PER DC-9 MM 32-60-0. SYSTEM GROUND CHECKS GOOD. 2 L 7 2 4F A6WE 1996011200016 19960112 00016 SO 1996 1 12 BIER960029 1 19960104 A 8120 LW18459 ROD SUPPORT PIPER PA31 PA31350 7103110 SO TURBOCHARGER CRACKED B BIEA K NONE O OTHER IN INSP/MAINT 1 EA 21 3521S 317952107 AT UNRELATED MAINTENANCE, FOUND TURBOCHARGER TOP ROD SUPPORT BRACKET BROKEN AT ENGINE. SUBMITTER STATES SUSPECT MISALIG NMENT OF ROD AND SUPPORT AT INSTALLATION. 1 L 7 2 3O A20SO 1996011200017 19960112 00017 SO 1996 1 12 COMA9610002 1 19960104 A 2750 3075001017 CONTROL BOX EMB 120 EMB120RT SO TE FLAPS DEFECTIVE A COMA K NONE O OTHER LD LANDING 1 SO 01 1110J 7530 2275 120110 FLAP ASYMMETRY WARNING DURING LANDING ROLL. REPLACED THE FLAP CONTROL BOX. 2 L 7 2 4T RT A31SO 1996011200019 19960112 00019 EU 1996 1 12 COMA9630003 1 19960102 A 7603 C822249 POWER LEVER SAAB SF340 SF340A 7850100 EU RT ENGINE BINDING A COMA O OTHER O OTHER CR CRUISE 1 SO 01 340SF 340A014 WHEN THE RIGHT ENGINE POWER LEVER WAS ADVANCED DURING CRUISE, THE ENGINE SURGED TO 95 PERCENT. REPLACED BINDING RT ENGI NE POWER LEVER CABLE. 2 L 7 2 4T RT A52EU 1996011200020 19960112 00020 EU 1996 1 12 COMA9630004 1 19960102 A 2613 OVERHEAT WARNING SAAB SF340 SF340A 7850100 EU RT ENGINE ACTIVATED A COMA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 340SF 340A014 RIGHT ENGINE TAIL PIPE HOT WARNING SHORTLY AFTER TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. GROUND RUNS WERE NORMAL AND ACFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 1996011200021 19960112 00021 EU 1996 1 12 COMA9630005 1 19960104 A 3020 9303143005 NOZZLE SAAB SF340 SF340A 7850100 EU LT ENGINE BURNED A COMA K NONE O OTHER CR CRUISE 1 SO 01 347CA 15791 8241 340A028 LEFT ENGINE INLET ANTI-ICE CYCLES ON AND OFF EVERY 15 SECONDS. REPLACED THE INLET PROTECTION DEVICE EXHAUST NOZZLE. 2 L 7 2 4T RT A52EU 1996011200025 19960112 00025 NM 1996 1 12 SWAA960001 1 19960103 A 5610 8300005602 WINDSHIELD BOEING 737 7373H4 1384600 NM RT COCKPIT CRACKED A SWAA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 309SW 22948 EN ROUTE FROM TUS TO SAN, FIRST OFFICER'S WINDSHIELD BEGAN ARCING, THEN CRACKED. AIRCRAFT DIVERTED TO PHX AND MADE AN U NEVENTFUL LANDING. REPLACED WINDOW ASSEMBLY AND HEAT CONTROLLER PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996011200026 19960112 00026 NM 1996 1 12 SWAA960002 1 19960103 A 2730 65445038 ACTUATOR BOEING 737 7372H4 138448C NM ELEV LEAKING A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 94SW 23053 NOTED A-SYSTEM FLUID LOSS EN ROUTE. AIRCRAFT DIVERTED TO PHX AND MADE AN UNEVENTFUL LANDING. INSPECTED TAIL AREA AND P ERFORMED LEAK CHECK. REPLACED ELEVATOR FEEL ACTUATOR PER PER BOEING M/M. TEST FLOWN WITH NO DEFECTS NOTED. 2 L 7 2 4F A16WE 1996011200027 19960112 00027 WP 1996 1 12 UPS805167 1 19960102 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 80 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 WHILE IN FOR C-CHECK, MAINTENANCE FOUND BOLT FRAME HAS .75 INCH LONG CRACK AT FS 80 LONGERON 21R. REPAIRED FRAME PER SR M 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1996011200118 19960112 00118 NM 1996 1 12 9600146301 1 19960104 A 3350 900835A BATTERY PACK BOEING 747 747451 1384940 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 661US 23719 DURING LINE CHECK, TWO EMERGENCY EXIT SIGNS WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996011200119 19960112 00119 WP 1996 1 12 9600159967 1 19960105 A 3260 RELAY DOUG DC9 DC931 3022065 WP RT MLG FAILED A NWAA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 01 9331 47263 DURING APPROACH, THE RIGHT MAIN LANDING GEAR GREEN DOWN LIGHT DID NOT ILLUMINATE AFTER LANDING GEAR EXTENSION. VISUALLY CONFIRMED LANDING GEAR WAS DOWN AND LOCKED. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED RELAY R2-28 AND OPERATIONAL CH ECK GOOD. 2 L 7 2 4F A6WE 1996011200120 19960112 00120 EU 1996 1 12 96FDEA00016 1 19960105 A 3610 DUCT AIRBUS 310 A310203 EU NR 2 ENGINE BLOWN A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 407FE 254 CLIMBING THROUGH 7,000 FT, RECEIVED ECAM AND FIRE HANDLE FIRE WARNING. WHEN THROTTLE MOVED TO IDLE ALL WARNINGS EXTINGU ISHED, TESTED FIRE WARNING SYSTEM AND RETURNED TO EWR, ENG AT IDLE. OPENED UP NR 2 ENG AND FOUND HP RECOUP DUCT BLOWN, (P/N 9345M89-G01) REF IPC 75-00-00 FIG 31 ITEM 150. PERFORMED FIRE WARNING TEST ALL INDICATIONS NORMAL. INSTALLED SERV ICEABLE HP RECOUP AIR DUCT IAW MM 72-00-02. PERFORMED HIGH POWER RUN AS PER JRH, ALL PARAMETERS NORMAL AND A/C OK FOR S ERVICE. 2 L 7 2 4F RT A35EU 1996011200121 19960112 00121 NM 1996 1 12 96FDEA00017 1 19960105 A 3260 H1010153 DN LOCK SWITCH BOEING 727 72722 1384002 NM NLG FAILED A FDEA O OTHER N FALSE WARNING AP APPROACH 1 SO 25 148FE 19086 NOSE GEAR DID NOT SHOW DOWN AND LOCKED. CYCLED IAW CHECKLIST, SUCCESSFUL 3 DOWN. GEAR HORN SOUNDED CONTINUOUSLY WHEN F LAPS EXTENDED TO 30 DEGREES CONFIRMING GEAR UNSAFE CONDITION. REPLACED NOSE LANDING GEAR LOCK SWITCH IAW MM 32-61-21 AN D OPS CHECK GOOD. 2 L 7 3 4F A3WE 1996011200122 19960112 00122 WP 1996 1 12 96FDEA00018 1 19960106 A 5512 PLANK DOUG DC10 DC1010CF 3023502 WP LT HORIZ STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 LT HORIZ STAB FWD UPPER PLANK CRACKED JUST INBOARD OF CLOSING RIB, FROM FWD EDGE AFT THROUGH FASTENER HOLE 1.5 TOTAL CRA CK CONTINUES PAST HOLE. REMOVED FASTENERS AND TRIMMED OUT CRACKED AREA. NDT AT CRACKED AREA AND OPEN HOLES C/W. COLD WORKED HOLES FINAL REAM. INSTALLED CONCOL WASHER, FABRICATED DOUBLER PER SRM 55-20-00. INSTALLED DOUBLER PER SRM 55-20 -22. 2 L 7 3 4F RT A22WE 1996011200123 19960112 00123 NM 1996 1 12 96FDEA00019 1 19960105 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 970 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 487FE 21490 UPPER LOBE, CRACK IN STR 7L STA 970. INSTALLED STR REPAIR PER SRM 53-10-3 PG 5 FIG 3. 2 L 7 3 4F A3WE 1996011200124 19960112 00124 NM 1996 1 12 96FDEA00020 1 19960105 A 5320 DOOR JAMB BOEING 727 727227 1384078 NM BS 416 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 487FE 21490 AFT LWR CORNER OF FWD GALLEY DOOR JAMB, AFT SIDE OF FRAME HEAVY CORROSION FOUND STA 416 ABOVE STR 17R. FOUND WITHIN SRM LIMITS. 2 L 7 3 4F A3WE 1996011200125 19960112 00125 NM 1996 1 12 96FDEA00021 1 19960105 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 344 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 487FE 21490 TOP SURFACE OF FLOORBEAM AT STA 344 CORRODED IN NUMEROUS AREAS FROM LBL 52 TO RBL 38. INSTALLED DOUBLER REPAIR ON TOP C AP OF FLOORBEAM PER DRAWING SR 27-53-007 FROM FEDEX STANDARD REPAIR DRAWING. 2 L 7 3 4F A3WE 1996011200126 19960112 00126 NM 1996 1 12 96FDEA00022 1 19960105 A 5311 BELLFRAME BOEING 727 727227 1384078 NM BS 804.5 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 487FE 21490 CABIN BELL FRAME CRACKED AT RADIUS STA 804.5, JUST ABOVE STA 145. INSTALLED REPAIR PER SRM 51-40-3 PAGE 1 TO 4 REF NR01 41. 2 L 7 3 4F A3WE 1996011200127 19960112 00127 NM 1996 1 12 96FDEA00023 1 19960105 A 5320 ANGLE BOEING 727 727227 1384078 NM BS 804.5 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 487FE 21490 CABIN BELL FRAME ANGLE CRACKED STA 804.5 STR 14R. STOP DRILLED CRACK AND INSTALLED DOUBLER PER 53-10-4 FIG 1. 2 L 7 3 4F A3WE 1996011200128 19960112 00128 NM 1996 1 12 96FDEA00024 1 19960105 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 380 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 487FE 21490 CORROSION ON FLOORBEAM STA 380 RBL 23 TO 51.25 GROUND FASTENER HOLES. FOUND WITHIN SRM LIMITS. 2 L 7 3 4F A3WE 1996011200129 19960112 00129 NM 1996 1 12 96FDEA00025 1 19960108 A 5330 SKIN BOEING 727 7272S2F 1384O81 NM BS 1223 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 213FE 22935 CRACK IN CORNER OF SKIN BS 1223 LBL 16 WL 148. REPAIRED CRACK IN CORNER OF SKIN AT BS 1223 LBL 16 WL 148 PER FEDEX EA 7 -5330-26829. 2 L 7 3 4F A3WE 1996011200130 19960112 00130 NM 1996 1 12 96FDEA00026 1 19960108 A 5320 65453135 STR CLIP BOEING 727 727227 1384078 NM BS 950 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 488FE 21491 DAMAGED STR CLIP, BS 950F STR 7L. REMOVED AND REPLACED STR CLIP BS 950F STR 7L PER FEDEX SRM 51-30-2. 2 L 7 3 4F A3WE 1996011200131 19960112 00131 NM 1996 1 12 96FDEA00027 1 19960108 A 5313 BAC1498144 STRINGER BOEING 727 727227 1384078 NM BS 660 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 488FE 21491 DAMAGED STR AT BS 660 STR 7L. REPAIRED DAMAGED STR 7L BS 660 PER FEDEX SRM 53-10-3, BY REMOVING DAMAGED SECTION AND FAB RICATING REPAIR PARTS AND INSTALLING THEM. 2 L 7 3 4F A3WE 1996011200132 19960112 00132 NM 1996 1 12 96FDEA00028 1 19960108 A 5320 65453135 CLIP BOEING 727 727227 1384078 NM BS 660 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 488FE 21491 CORROSION (C53-224-01) IN STR AND STR CLIP AT BS 660 STR 3R. REMOVED CORROSION AT STR 3 BS 660 RT. ORIGINAL THICKNESS .045, REMOVED .002, 5 INCH BY 1 INCH AREA WITHIN LIMITS PER FEDEX SRM 53-10-1, ALODINED AND PRIMED AREA. REMOVED STR C LIP AT BS 660 RT DUE TO CRACK. REPLACED STR CLIP PER FEDEX SRM 53-10-1. 2 L 7 3 4F A3WE 1996011200133 19960112 00133 NM 1996 1 12 96FDEA00029 1 19960108 A 5311 FRAME BOEING 727 727227 1384078 NM BS 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 488FE 21491 DAMAGED FRAME AND STR CLIP AT BS 600 RT STR 7. REPAIRED FRAME AT BS 600 STR 7 TO 8R IAW FEDEX SRM 53-10-4. REMOVED DAM AGED STR CLIP AND INSTALLED NEW STR CLIP AT BS 600 STR 7R. 2 L 7 3 4F A3WE 1996011200134 19960112 00134 NM 1996 1 12 96FDEA00030 1 19960108 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 360 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 488FE 21491 CORROSION (C53-224-01-1) ON FLOORBEAM AT CLIP NUT HOLE BS 360 RBL 12 WL 208. REMOVED CORROSION ON FLOORBEAM BS 360 RBL 12 WL 208 FOUND TO BE OUT OF LIMITS, ORIGINAL .130 AND REMOVED .032 FROM 1 INCH BY 2 INCH AREA. FABRICATED AND INSTALL ED REPAIR ANGLES FOR FLOORBEAM AT BS 360 RBL 12 WL 208 PER FEDEX SRM 53-10-8, ALODINED AND PRIMED. 2 L 7 3 4F A3WE 1996011200135 19960112 00135 NM 1996 1 12 96FDEA00031 1 19960108 A 5311 FRAME BOEING 727 727227 1384078 NM BS 560 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 488FE 21491 CRACKED IN FRAME BS 560 RT BETWEEN STR 7 AND 8. REPAIRED DAMAGED FRAME BS 560 RT BETWEEN STR 7 AND 8 IAW FEDEX SRM 53-1 0-4. FRAME WAS FOUND NOT TO HAVE INDICATION IAW D6-48875 PT6, 51-00-00 FIG 23. 2 L 7 3 4F A3WE 1996011200137 19960112 00137 NM 1996 1 12 96FDEA00033 1 19960108 A 5313 BAC1498144 STRINGER BOEING 727 727227 1384078 NM BS 757-759 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 488FE 21491 MECH DAMAGE AND FASTENERS MISSING IN STR 7L BS 757 TO 759. ACCOMPLISHED STR REPAIR AT STA 740 TO 770 STR 7L PER FEDEX S RM 53-10-1, 53-10-2 AND 53-10-3. 2 L 7 3 4F A3WE 1996011200138 19960112 00138 NM 1996 1 12 96FDEA00034 1 19960108 A 5311 FRAME BOEING 727 727227 1384078 NM BS 380 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 488FE 21491 FRAME CRACKED AT STA 380 WL 278 RBL 65. REMOVED DAMAGED SECTION OF FRAME AT BS 380 WL 278 RBL 65. FABRICATED REPAIR AN GLE AND DOUBLERS, ALODINED, PRIMED AND INSTALLED WET. ALL WORK DONE PER FEDEX SRM 53-10-4. 2 L 7 3 4F A3WE 1996011200139 19960112 00139 NM 1996 1 12 96FDEA00035 1 19960108 A 5754 65162268A LUG BOEING 727 727227 1384078 NM NR 5 LE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 488FE 21491 NR 5 K-FLAP O/B LUG O/B SIDE UPPER MOUNT BOLT HAS CORROSION UNDER NUT. CORROSION WAS FOUND TO BE OUT OF LIMITS. REMOVE D AND REPLACED NR 5 K-FLAP AND FUNCTIONAL CHECKED IAW FEDEX MM 27-81-1. 2 L 7 3 4F A3WE 1996011200140 19960112 00140 SO 1996 1 12 COMA9610004 1 19960103 A 2752 3203001007 ACTUATOR EMB 120 EMB120RT SO LT TE FLAPS DEFECTIVE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 156CA 1830 120156 RECEIVED TAKEOFF FLAPS AURAL WARNING DURING TAKEOFF AND FLAP DISAGREEMENT WARNING WHEN FLAPS SELECTED UP AFTER TAKEOFF. REPLACED THE LT OUTBD FLAP ACTUATOR. 2 L 7 2 4T RT A31SO 1996011200141 19960112 00141 EU 1996 1 12 COMA9630006 1 19960105 A 3230 RETRACT MECH SAAB SF340 SF340A 7850100 EU LANDING GEAR ICED UP A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 320CA 340A064 LANDING GEAR DID NOT RETRACT FULLY, GEAR CYCLED TWICE WITH SAME RESULT. DE-ICED LANDING GEAR AND RETRACTION CHECK NORMA L. 2 L 7 2 4T RT A52EU 1996011200142 19960112 00142 EU 1996 1 12 COMA9630007 1 19960105 A 2731 DL3827M157 TRIM ACTUATOR SAAB SF340 SF340A 7850100 EU LT ELEVATOR DEFECTIVE A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 356CA 340A034 CONFIGURATION WARNING DURING TAKEOFF ROLL. REPLACED THE LT PITCH TRIM ACTUATOR. 2 L 7 2 4T RT A52EU 1996011200143 19960112 00143 EU 1996 1 12 COMA9630008 1 19960105 A 3350 6104781 BATTERY SAAB SF340 SF340A 7850100 EU CABIN DISCHARGED A COMA K NONE L NO TEST UK UNKNOWN 1 SO 01 380CA 340A012 SEVERAL CABIN EMERGENCY LIGHTS ARE INOP. REPLACED EMERGENCY LIGHTS BATTERY PACKS. 2 L 7 2 4T RT A52EU 1996011200144 19960112 00144 EA 1996 1 12 COMA9660005 1 19960105 A 2150 PACK CNDAIR CL600 CL6002B19 EA RIGHT FAILED A COMA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 924CA 7026 RT COOLING PACK FAULT WARNING. SMOKE IN CABIN AND LAVATORY. SMOKE CLEARED WHEN COOLING PACK SHUTDOWN. PLACED RT COOLI NG PACK ON DEFERRED MAINT LIST. 2 L 7 2 4F RT A21EA 1996011200145 19960112 00145 NM 1996 1 12 DL72K960013 1 19960103 A 5320 FLOOR CHANNEL BOEING 727 727232 1384082 NM BS 1110 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 413DA 21233 FOUND ON MV 1, CORROSION ON FLOOR SUPPORT CHANNEL FWD SIDE TOP LEG STA 1110, LBL 9 AROUND FLOOR PANEL HOLE. REPAIRED PE R M/M 53-20-11. 2 L 7 3 4F A3WE 1996011200146 19960112 00146 NM 1996 1 12 DL72K960014 1 19960103 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 360 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 413DA 21233 CORROSION FOUND ON FLOORBEAM UPPER ANGLE STA 360 LBL 20 TO RBL 14. INSTALLED REPAIR DOUBLERS PER M/M 53-20-11 PG 802 TO 803. 2 L 7 3 4F A3WE 1996011200147 19960112 00147 NM 1996 1 12 DL72L960016 1 19960103 A 2910 65178494061 HYD LINE BOEING 727 727232 1384082 NM B-HYD SYST CRACKED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 509DA 21311 ON T/O, A-SYS HYD QTY DECREASED TO 1.8 GAL. SHORTLY THEREAFTER THE B-SYS STARTED TO DECREASE AND B-HYD PUMPS WERE TURNE D OFF. FOUND THE RIGID HYD LINE FOR THE B-SYS MODULE CRACKED. REPLACED WITH A LIKE LINE, SERVICED SYS AND OPS CK OK. 2 L 7 3 4F A3WE 1996011200155 19960112 00155 NM 1996 1 12 DL72S960027 1 19960104 A 5743 6519296 FITTING BOEING 727 727232 1384082 NM LT WING CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 403DA 21147 AT GEAR CHANGE CORROSION WAS FOUND ON THE LEFT MAIN GEAR FWD TRUNNION ATTACH FITTING O/B LOWER HOLE, O/B UPPER HOLE AND INBD LOWER HOLE. ALL CORROSION WAS REMOVED AND FOUND IN LIMITS. THE AREA WAS REPAIRED PER M/M 57-43-0. 2 L 7 3 4F A3WE 1996011200156 19960112 00156 NM 1996 1 12 DL72S960029 1 19960104 A 5744 FITTING BOEING 727 727232 1384082 NM LEFT WING CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 403DA 21147 AT GEAR CHANGE THE NR 2 FLAP INBD TRACK SUPPORT FITTING WAS FOUND CORRODED ON THE OUTER FACE. THIS FITTING WAS REPAIRED PER M/M 57-42-0 FIG 805, DAMAGE WAS WITHIN LIMITS FOR THIS REPAIR. 2 L 7 3 4F A3WE 1996011200162 19960112 00162 NM 1996 1 12 DL72S960044 1 19960104 A 2760 MOUNT BOLTS BOEING 727 727232 1384082 NM NR 2 SPOILER LOOSE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 495DA 21075 NR 2 SPOILER POWER PACK BOTTOM MOUNT BOLTS ARE LOOSE. REMOVED SPOILER ACTUATOR ATTACH FITTING. REMOVED AND REPLACED AN GLE PER MM 57-42-0 PG 804. INSTALLED POWER PACK, ACTUATOR AND MOUNT FITTING. 2 L 7 3 4F A3WE 1996011200163 19960112 00163 NM 1996 1 12 DL72S960053 1 19960105 A 5240 69562562 HINGE PIN BOEING 727 727232 1384082 NM L 2 SERV DOOR SHEARED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 525DA 21585 FOUND LEFT AFT SERVICE DOOR WITH SHEARED DOOR HINGE PIN. REPLACED HINGE PIN OPERATION NORMAL. 2 L 7 3 4F A3WE 1996011200165 19960112 00165 NE 1996 1 12 DL733960043 2 19960106 A 7200 ENGINE BOEING 737 737347 1384647 NM GE CFM56 CFM563B1 13802 NE NR 2 ENGINE FOD A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 309WA 23442 720673 SHORTLY AFTER T/O, AN ELEC ODOR DEVELOPED IN THE CABIN. COMPLIED WITH CHECKLIST. REMOVED SMALL AMOUNT OF COMPUTER PAPE R FROM NR 2 ENG. RAN ENGINE PER PFHB, NO ODOR PRESENT. RAN ALL ELEC SYS AND A/C PACKS, NO PROBLEM FOUND. INSPECTED EN G PER M/M. 2 L 7 2 4F 4 F RT A16WE E2GL 1996011200166 19960112 00166 NM 1996 1 12 DL73S960031 1 19960104 A 2740 RELAY 91238056 BOEING 737 737232 1384475 NM STAB TRIM INOPERATIVE A DALA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 SO 27 331DL 23103 AT ALTITUDE MAIN STAB TRIM MOTOR WOULD NOT WORK, A/P MOTOR WORKS OK. APPLICABLE C/B WERE CYCLED TO NO AVAIL, RETURNED T O ATL PER DISPATCH. INSPECTED STAB TRIM ACT, CLEANED CONNECTORS, INSPECTED LIMIT SWITHCES, CUTOUT SWITHCES AND ALL CHEC K NORMAL. REPLACED R-66 DUE TO HISTORY AND ALL OPERATION NORMAL. 2 L 7 2 4F RT A16WE 1996011200168 19960112 00168 NM 1996 1 12 DL757960028 1 19960104 A 2622 51211 FIRE BOTTLE BOEING 757 757232 1384965 NM FLIGHT CABIN LEAKING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 636DL 23763 F/C HALON FIRE BOTTLE LEAKING EXTINGUISHING AGENT. 2 L 7 2 4F RT A2NM 1996011200171 19960112 00171 NE 1996 1 12 DL76L960042 2 19960106 A 7261 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 MALFUNCTIONED A DALA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 183DN 27110 724146 NR 2 ENG CHANGE DUE TO HIGH OIL CONSUMPTION. 2 L 7 2 4F 4 F RT A1NM E24NE 1996011200172 19960112 00172 NM 1996 1 12 DL76S960008 1 19960102 A 3350 LAMP 387 BOEING 767 767332 1382001 NM 2L DOOR FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 136DL 00000 23146 SLIDE LIGHT 2L DOOR INOP. RELAMPED, OPN NML. 2 L 7 2 4F RT A1NM 1996011200174 19960112 00174 NM 1996 1 12 DLM11960006 1 19960101 A 2420 WIRE 221W5070511 DOUG MD11 MD11 3023602 NM NR 1 ENGINE DAMAGED A DALA K NONE J WARNING INDICATION CR CRUISE 1 SO 27 805DE 48476 GENERATOR FEEDER CABLES DAMAGED, DUE TO SHORTING IN PYLON. 2 L 7 3 4F RT A22WE 1996011200175 19960112 00175 NM 1996 1 12 DLM11960017 1 19960103 A 3350 TRACK 0105606205 DOUG MD11 MD11 3023602 NM CABIN SHORTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 804DE 48475 EMERGENCY LIGHT TRACK SHORTED. REPLACED TRACK, OPS CHECK GOOD. 2 L 7 3 4F RT A22WE 1996011200176 19960112 00176 NM 1996 1 12 DLM88960018 1 19960103 A 5755 SPOILER DOUG MD88 MD88 3023688 NM RT WING DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 930DL 49717 FOUND DURING A-2 LETTER CHECK, RIGHT I/B FLIGHT SPOILER DELAMINATED AT T/E. REPAIRED PER SRM 51-70-1B. 2 L 7 2 4F RT A6WE 1996011200178 19960112 00178 NM 1996 1 12 DLM88960052 1 19960106 A 3397 WIRE DOUG MD88 MD88 3023688 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 908DL 49539 PN PREFLIGHT, L-1 AND R-1 DOOR EMERGENCY EXIT IDENTIFIER LIGHTS FOUND INOP. MTC REPAIRED BROKEN WIRE IN THE RT SIDE F/C FLOOR TRACK AND OPERATION NORMAL. 2 L 7 2 4F RT A6WE 1996011200180 19960112 00180 EU 1996 1 12 9600163241 1 19960106 A 3260 848401 PROX SENSOR AIRBUS 320 A320211 3930320 EU LT MLG FAILED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 341NW 380 DURING CLIMBOUT AFTER THE LANDING GEAR WAS RETRACTED, THREE LANDING GEAR DISAGREEMENT LIGHTS ILLUMINATED. CYCLED LANDIN G GEAR HANDLE AND ALL INDICATIONS WERE NORMAL. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLA CED THE LEFT MAIN LANDING GEAR PROXIMITY SENSOR (23GA) AND THE NR 2 LANDING GEAR CONTROL INTERFACE UNIT. OPERATIONAL CH ECK OK. 2 L 7 2 4F RT A28NM 1996011200181 19960112 00181 NM 1996 1 12 9600175529 1 19960108 A 7830 TR UNIT BOEING 757 757251 1384970 NM ENGINE MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 529US 23844 DURING CLIMB, REVERSER ISOLATION VALVE STATUS MESSAGE AND REVERSER ISOLATION WARNING LIGHT ILLUMINATED. AIRCRAFT RETURN ED TO DEPARTURE AIRPORT, NO FUEL WAS DUMPED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE DEACTIVATED AND STOWED THR UST REVERSER. THRUST REVERSER WAS PLACED ON MEL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 1996011200182 19960112 00182 NM 1996 1 12 9600186304 1 19960105 A 3350 CONNECTOR BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 664US 23819 DURING LINE CHECK, THE FLOOR PATH EMERGENCY LIGHTS IN THE AFT CABIN LEFT AISLE WERE FOUND INOPERATIVE. RECONNECTED LOOS E CONNECTOR IN FLOOR TRACK AND OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996011200183 19960112 00183 NM 1996 1 12 9600192284 1 19960105 A 5270 DOOR WARNING BOEING 727 727251 138408H NM CARGO DOOR ACTIVATED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 284US 21323 DURING CLIMB, AFT CARGO DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO TPA AND LANDED WITHOUT INCIDENT. AFT CARG O DOOR WAS INSPECTED AND FOUND CLOSED AND LOCKED. AFT CARGO DOOR WAS PLACED ON MEL 52-4. 2 L 7 3 4F A3WE 1996011200184 19960112 00184 NM 1996 1 12 9600202704 1 19960107 A 3350 LIGHT BOEING 727 727225 1384077 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 801EA 22432 DURING PREFLIGHT, FOUND PORTABLE EMERGENCY EXIT LIGHT AT FORWARD GALLEY SERVICE DOOR INOPERATIVE. REPLACED THE LIGHT AS SEMBLY AND BATTERIES, CHECKED OK. 2 L 7 3 4F A3WE 1996011200185 19960112 00185 WP 1996 1 12 9600219923 1 19960108 A 2530 OVEN DOUG DC9 DC932 3022066 WP NR 2 SMOKING A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 01 927RC 47469 DURING FLIGHT, SMOKE ACCUMULATED IN AIRCRAFT FROM NR 2 OVEN. PILOTS WORE SMOKE GOGGLES AND OXYGEN MASKS UNTIL OVEN COOL ED OFF. THE AIRCRAFT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE OVEN AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996011200186 19960112 00186 WP 1996 1 12 9600229916 1 19960108 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 949N 47566 DURING LINE CHECK, FOUND COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996011200187 19960112 00187 WP 1996 1 12 9600239929 1 19960105 A 3350 BATTERY DOUG DC9 DC931 3022065 WP TAILCONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8923E 45838 DURING LINE CHECK, FOUND EMERGENCY LIGHTS IN TAILCONE INOPERATIVE. REPLACED BATTERIES AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996011200188 19960112 00188 WP 1996 1 12 9600249929 1 19960108 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP TAILCONE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8923E 45838 DURING LINE CHECK, FOUND TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERIES, OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996011200189 19960112 00189 WP 1996 1 12 9600259974 1 19960106 A 3350 BATTERY DOUG DC9 DC931 3022065 WP COCKPIT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9338 47347 FOUND COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996011200190 19960112 00190 WP 1996 1 12 9600269967 1 19960106 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9331 47263 WIRING FOR EMERGENCY FLOOR TRACK LIGHTING AT ROW 15 IS LOOSE AND EXPOSED. FOUND WIRE FOR LIGHT AT ROWS 16 AND 18 PULLED OUT OF THE SOCKET. REPAIRED WIRE AND REPLACED SOCKETS, OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996011200191 19960112 00191 WP 1996 1 12 9600279989 1 19960106 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP TAILCONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8945E 47181 DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTING IN TAILCONE AREA INOPERATIVE. REPLACED THE BATTERY PACK AND OPE RATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996011200192 19960112 00192 WP 1996 1 12 9600289952 1 19960105 A 3350 LIGHTS DOUG DC9 DC931 3022065 WP LT/RT NACELLE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 916RW 47144 DURING LINE CHECK, FOUND BOTH NACELLE EMERGENCY LIGHTS INOPERATIVE. REPLACED R2-213 AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996011200193 19960112 00193 WP 1996 1 12 9600299601 1 19960105 A 3231 UPLOCK ASSY DOUG DC9 DC932 3022066 WP LT MLG DOOR LOOSE A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 601NW 47038 DURING APPROACH, THE LEFT MAIN LANDING GEAR DOOR OPEN LIGHT ILLUMINATED AFTER LANDING GEAR EXTENSION. RECYCLED LANDING GEAR AND LIGHT REMAINED ILLUMINATED. EXECUTED GO-AROUND AND AIRCRAFT LANDED WITHOUT INCIDENT. FOUND LEFT MAIN LANDING GEAR DOOR UPLOCK ASSEMBLY LOOSE. RESECURED UPLOCK ASSEMBLY AND RIGGED LANDING GEAR DOOR SPRINGS, OPERATIONAL CHECK GOOD . 2 L 7 2 4F A6WE 1996011200194 19960112 00194 WP 1996 1 12 9600309991 1 19960105 A 3230 UPLATCH ROLLER DOUG DC9 DC932 3022066 WP RT NLG OUT OF ADJUST A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 8957E 47215 DURING CLIMB, THE RIGHT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED AFTER LANDING GEAR RETRACTION. RECYCLED LANDING GEAR AND LIGHT REMAINED ILLUMINATED. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. FOUND RIGHT MAIN LANDING GEAR D OOR UPLATCH ROLLER AND RIGHT MAIN LANDING STRUT TO BUMPER CLEARANCE OUT OF RIG. RIGGED BOTH SYSTEMS AND OPERATIONAL CHE CK GOOD. 2 L 7 2 4F A6WE 1996011200195 19960112 00195 WP 1996 1 12 9600319106 1 19960107 A 2550 CARGO NET DOUG DC9 DC915 3022036 WP CARGO DOOR OUT OF POSITION A NWAA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 GL 01 96S 47206 DURING CLIMB CLE-MSP, FOUND THAT THE AIRCRAFT WOULD NOT PRESSURIZE. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES, NO HE LP. DIVERTED TO DTW WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THAT THE AFT CARGO DOOR WAS NOT FULLY CLOSED AND LATCH ED ON THE AFT SIDE, DUE TO AN UNSECURED CARGO NET AND JAMMED CLIP. THE FORWARD SIDE WAS CLOSED AND LATCHED AND THERE WA S NO ANNUNCIATOR INDICATION. ALSO, FOUND THAT THE DOOR WAS DIFFICULT TO CLOSE. RERIGGED THE DOOR PER 52-31-0, CODE 3. PRESSURE AND OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996011200196 19960112 00196 EU 1996 1 12 96UAL900007 2 19960105 A 7321 SCR501545 ENGINE CONTROL BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU NR 1 ENGINE FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 916UA 25383 726281 NUMBER ONE ENGINE SURGES AT HIGH POWER SETTINGS WITH AUTO THROTTLE ON AND OFF. ALSO, SURGE WAS NOTICEABLE WITH AIRCRAFT IN YAW, BUT NOT NOTICEABLE AT LOWER POWER SETTINGS. REPLACED MAIN ENGINE CONTROL, CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E21EU 1996011200197 19960112 00197 NM 1996 1 12 96UAL900008 1 19960105 A 2910 651784528 HYD LINE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LT ELEV PCU LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 7266U 21413 RETURNED TO LAX UNDER AMBER ALERT DUE TO LOSS OF A-SYSTEM HYDRAULIC QUANTITY AND PRESSURE IN FLIGHT. REPLACED PRESSURE LINE AT LEFT ELEVATOR POWER CONTROL UNIT DUE TO LEAK. 2 L 7 3 4F 4 F A3WE E2EA 1996011200198 19960112 00198 NM 1996 1 12 96UAL900010 1 19960105 A 3340 LIGHT WIRES BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LT WING DAMAGED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 7465U 21919 LEFT WING TRAILING EDGE WHITE LIGHT INOPERATIVE. POWER AND GROUND WIRES FOUND BURNT IN VICINITY OF LIGHT. REPLACED WIR ES. CAUSE UNDETERMINED, POSSIBLE LIGHTNING STRIKE. 2 L 7 3 4F 4 F A3WE E2EA 1996011200199 19960112 00199 WP 1996 1 12 96UAL900011 1 19960105 A 3620 FAIL LIGHTS DOUG DC10 DC1010 3022110 WP NR 2 MANIFOLD ILLUMINATED A UALA O OTHER N FALSE WARNING CL CLIMB 1 WP 29 1844U 48260 NR 2 PNEUMATIC MANIFOLD 'MANIFOLD FAIL' AND 'TEMP HI' LIGHTS ON. PERFORMED EMERGENCY PROCEDURE, NOW OPERATING WITH SYST EMS 1 AND 3. FAILURE OCCURRED CLIMBING THROUGH 20,000 FEET. 2 L 7 3 4F A22WE 1996011200200 19960112 00200 1996 1 12 96UAL900012 4 19960109 A 2565 SEAM BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SLIDE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 769UA 26921 SLIDE REMOVED FROM AIRCRAFT DUE TO INADVERTENT DEPLOYMENT. SLIDE HAS A SEAM LEAK AT THE LT CORNER OF THE SLIDE. REPAIR ED SEAM LEAK, NON-STRUCTURAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 1996011200201 19960112 00201 NM 1996 1 12 96UAL900013 1 19960108 A 2130 7110024 PANEL BOEING 737 737322 1384676 NM COCKPIT DAMAGED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 202UA 24717 PRESSURIZATION AUTO FAIL LIGHT CAME ON, WAS UNABLE TO CONTROL PRESSURIZATION IN STANDBY OR MANUAL MODE. CABIN WAS CLIMB ING AT AN UNCONTROLLABLE RATE. REPLACED MAIN OUTFLOW VALVE AND PRESSURIZATION SELECTOR PANEL. FOUND PIN PUSHED IN ON P ANEL, TESTED PRESSURIZATION SYSTEM AND CHECKED OK. 2 L 7 2 4F RT A16WE 1996011200202 19960112 00202 NM 1996 1 12 96UAL900014 1 19960108 A 3350 LAMP SEGMENT BOEING 747 747422 1384935 NM CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 EMERGENCY EXIT LIGHT INOP AT ROW 1R, LAMP SEGMENT BURNED OUT. REPLACED LAMP SEGMENT AND POWER STRIP. 2 L 7 4 4F RT A20WE 1996011200203 19960112 00203 NM 1996 1 12 96UAL900016 1 19960108 A 2121 36144161 COOLING FAN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU FAILED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 568UA 2272 26674 SMOKE IN AFT AND F0RWARD CABIN AFTER LEVEL OFF AT 37,000 FEET. SMOKE BEGAN TO DISSIPATE AT 24,000 FEET IN DESCENT AND C LEAR AT 10,000 FEET. FLIGHT DIVERTED TO PHX. THE APU HAD A SEVERE COOLING FAN FAILURE WHICH CAUSED OIL TO LEAK INTO TH E INLET PLENUM, CONTAMINATING THE AIR CONDITIONING SYSTEM. THE COOLING FAN HAD THE SHROUDED ROTOR. THE APU ALSO SUSTAI NED FOREIGN OBJECT DAMAGE TO THE COMPRESSOR IMPELLERS. PART TOTAL CYCLES, 2,599. 2 L 7 2 4F 4 F RT A2NM E17NE 1996011200204 19960112 00204 NM 1996 1 12 96UAL900018 1 19960109 A 4900 APU BOEING 727 727222 1384073 NM RT MLG WW FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 7460U 21914 APU AUTO-SHUTDOWN AND SMOKE CAME OUT OF WHEEL WELL AREA. 2 L 7 3 4F A3WE 1996011200205 19960112 00205 SO 1996 1 12 COMA9610005 1 19960107 A 2910 PRESS LINE EMB 120 EMB120RT SO BLUE HYD SYST FROZEN A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 267CA 120259 RT BLUE HYDRAULIC SYSTEM, LOW RESERVOIR PRESSURE, WARNING LIGHT ILLUMINATED. THAWED FROZEN MOISTURE IN RESERVOIR PRESSU RIZATION LINE. 2 L 7 2 4T RT A31SO 1996011200206 19960112 00206 EU 1996 1 12 COMA9630009 1 19960106 A 2432 501122804 POWER SUPPLY SAAB SF340 SF340A 7850100 EU AVIONICS DEFECTIVE A COMA O OTHER J WARNING INDICATION UK UNKNOWN 1 SO 01 320CA 11516 163 340A064 EMERGENCY POWER WARNING LIGHT CAME ON. REPLACED THE EMERGENCY POWER SUPPLY. 2 L 7 2 4T RT A52EU 1996011200207 19960112 00207 EA 1996 1 12 COMA9660006 1 19960106 A 3010 ANTI-ICE DUCT CNDAIR CL600 CL6002B19 EA COCKPIT WARNING A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 912CA 7011 ANTI-ICE DUCT MESSAGE ON EICAS TAKEOFF ABORTED. COULD NOT DUPLICATE DISCREPANCY. SYSTEM CHECKED NORMAL AND ACFT RETURN ED TO SERVICE. 2 L 7 2 4F RT A21EA 1996011200208 19960112 00208 NM 1996 1 12 SCNA96001 1 19960103 A 3350 S106 BATTERY BOEING 727 727225 1384077 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 282SC 22558 THE EMERGENCY EXIT LIGHT LOCATED IN THE AFT CABIN WAS FOUND TO BE DIM. REMOVED AND REPLACED BATTERIES IN LIGHT, OPS CHE CKED GOOD PER MM 33-50-101. 2 L 7 3 4F A3WE 1996011200209 19960112 00209 NM 1996 1 12 SCNA96002 1 19960103 A 3350 1102833 LIGHT ASSY BOEING 727 727225 1384077 NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 282SC 22558 THE EMERGENCY EXIT AREA LIGHT AT SEAT ROW 11 WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY IAW MM 33 -50-81 AND LIGHT OPS CHECKED GOOD. 2 L 7 3 4F A3WE 1996011200210 19960112 00210 NM 1996 1 12 SCNA96003 1 19960105 A 3350 900835A BATTERY BOEING 727 7272J4 1384006 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 285SC 21676 THE FORWARD EMERGENCY EXIT AREA LIGHT COMES ON AND THEN GOES OUT. REMOVED AND REPLACED BATTERY IAW MM 33-50-71 AND LIGH T TESTED NORMAL. 2 L 7 3 4F RT A3WE 1996011200211 19960112 00211 NM 1996 1 12 UPS205179 1 19960108 A 3350 1000679 LIGHT BOEING 727 727247 138408F NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 207UP 21699 YHM - MAINTENANCE REPORTED, L 1 EMERGENCY EXIT LIGHT WILL NOT TEST. LIGHT ASSY REMOVED AND REPLACED AND OPS CHECKED GOO D AS PER MM 33-50-01. 2 L 7 3 4F A3WE 1996011200261 19960112 00261 NM 1996 1 12 9600326304 1 19960107 A 7830 TR SENSOR BOEING 747 747451 1384940 NM NR 2 OUT OF ADJUST A NWAA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CR CRUISE 1 GL 01 664US 23819 DTW - AFTER TAKEOFF, THE NR 2 ENGINE REVERSER AMBER LIGHT ILLUMINATED. NO STATUS, NO EICAS AND NO PRESENT LEG FAULT MES SAGES DISPLAYED. CREW FOLLOWED COCKPIT OPERATING MANUAL, DUMPED 135,000 LBS OF FUEL AND DIVERTED FLIGHT TO MSP. MAINTE NANCE VISUALLY INSPECTED NR 2 REVERSER FOR SECURITY AND ADJUSTED TARGET OF LOCK PROXIMITY SENSOR PER MM 78-30-01 PG 501. OPERATIONAL CHECK WAS NORMAL. 2 L 7 4 4F RT A20WE 1996011200262 19960112 00262 NE 1996 1 12 9600336628 2 19960105 A 7250 TURBINE BOEING 747 747251B 1384892 NM PWA JT9 JT9D7Q 52054 NE NR 2 ENGINE FAILED A NWAA A E F J UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. DUMP FUEL J WARNING INDICATION CL CLIMB 1 GL 01 628US 22389 02037 DURING CLIMB, THE NR 2 ENGINE FIRE WARNING ILLUMINATED. CREW FOLLOWED COCKPIT OPERATING MANUAL, FIRED BOTTLE, IFSD AND SUBSEQUENTLY DUMPED 147,000 LBS OF FUEL AND RETURNED TO LAX. MAINTENANCE FOUND NR 2 ENGINE TURBINE EXHAUST CASE UNCONTA INED FAILURE. REPLACED NR 2 ENGINE AND CHECK WAS NORMAL. 2 L 7 4 4F 4 F A20WE E3NE 1996011200263 19960112 00263 NM 1996 1 12 9600436625 1 19960110 A 3350 POWER SUPPLY BOEING 747 747251B 1384892 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 625US 21707 DURING LINE CHECK, FOUND THE STATE ROOM EMERGENCY TRACK LIGHT INOPERATIVE. REPLACED THE POWER SUPPLY AND BATTERY PACK A ND FUNCTIONAL CHECK WAS NORMAL. 2 L 7 4 4F A20WE 1996011200264 19960112 00264 EU 1996 1 12 96FDEA00036 1 19960109 A 2750 SOLENOID VALVE AIRBUS 310 A310203 EU FLAP SYST FAILED A FDEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 25 414FE 400 TPE - AFTER T/O, FLAPS WERE VERY SLOW TO RETRACT, FLAPS/SLATS STUCK AT ZERO DEGREES. FOLLOWED EMERGENCY/ABNORMAL PROCED URE AND RETURNED TO TPE. FLAPS RETRACTED TO ZERO DEGREE DETENT ON THE GROUND AND THE FLAP SYS NR 1 FAULT LIGHT ILLUMINA TED. REMOVED AND REPLACED HIGH SPEED SOLENOID VALVE, WORKS OK (P/N 500A000-03), OFF (S/N 03601). BITE TEST ON SFCC NR 1, ALL OK PLACARD REMOVED AND NOTIFIED MOCC. 2 L 7 2 4F RT A35EU 1996011200265 19960112 00265 NM 1996 1 12 96UAL900019 1 19960109 A 3350 BATTERY BOEING 737 737222 1384473 NM COCKPIT DISCHARGED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 9045U 19551 FLIGHT DECK EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY AND CHECKS OK. 2 L 7 2 4F A16WE 1996011200266 19960112 00266 NM 1996 1 12 96UAL900020 1 19960109 A 2820 FUEL BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUEL SYSTEM IMBALANCE A UALA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 WP 29 7274U 21421 AIRCRAFT REQUIRES 3 UNITS OF AILERON TRIM FOR LEVEL FLIGHT. FLIGHT DIVERTED TO RAP DUE TO AIRCRAFT DEVELOPED FUEL IMBAL ANCE EN ROUTE. CAUSE OF UNBALANCE UNDETERMINED. MAINTENANCE CHECKED FUEL TANKS WITH DRIPSTICKS AND FOUND A DIFFERENCE OF ONLY 1,000 POUNDS. 2 L 7 3 4F 4 F A3WE E2EA 1996011200267 19960112 00267 WP 1996 1 12 96UAL900021 1 19960109 A 2170 COALESCER BAG DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN DIRTY A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 1813U 46612 WHEN BOARDING AIRCRAFT GOT ACRID ODOR APPARENTLY FROM AIR CONDITIONING SYSTEM. WORSE AFTER ENGINE START AND TAKEOFF. A LL GAUGE INDICATIONS NORMAL, COULD NOT DUPLICATE. BURNED OUT PACKS AND REPLACED ALL COALESCER BAGS. 2 L 7 3 4F 4 F A22WE E23EA 1996011200268 19960112 00268 1996 1 12 MWEA96003 4 19960110 A 2565 13621225 EVAC SLIDE DOUG DC9 DC932 3022066 WP TAIL COMPT LOW PRESSURE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING SERVICE CHECK, FOUND TAIL COMPARTMENT EVAC SLIDE PRESSURE LOW. REMOVED AND REPLACED EVAC SLIDE. 2 L 7 2 4F A6WE 1996011200269 19960112 00269 EU 1996 1 12 QXEA9600007 1 19960103 A 3350 1820 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 803PH 11031 GEG - TWO OVERHEAD EMERGENCY LIGHTS ARE INOP. BULBS WERE REPLACED AND LIGHTS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SE RVICE. 2 L 7 2 4F RT A20EU 1996011200270 19960112 00270 EU 1996 1 12 QXEA9600008 1 19960103 A 3350 1820 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 801PH 11097 GEG - TWO 28V CABIN OVERHEAD EMERGENCY LIGHTS ARE INOP. BULBS WERE REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETUR NED TO SERVICE. 2 L 7 2 4F RT A20EU 1996011200273 19960112 00273 NM 1996 1 12 QXEA9600011 1 19960105 A 3260 864202 SENSOR ELDEC DHAV DHC8 DHC8102 2809003 NM NLG INTERMITTENT A QXEA K NONE N FALSE WARNING CR CRUISE 1 NM 09 825PH 213 SEA - NOSE GEAR RED UNSAFE ADVISORY LIGHT AND GEAR HANDLE LIGHT CYCLED ON AND OFF FOR VARYING LENGTHS OF TIME IN CRUISE. AIRCRAFT LANDED IN SEA WITHOUT FURTHER PROBLEM. AIRCRAFT INSPECTED AND FERRIED TO PDX. NLG DRAG STRUT PROX SENSOR FA ILED AIR/GRO TEST. DRAG STRUT PROX SENSOR REPLACED AND CHECKED GOOD IAW MAINT MANUAL ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1996011200275 19960112 00275 EU 1996 1 12 QXEA9600013 1 19960106 A 3397 WIRE FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN BROKEN A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 802PH 11017 BOI - FLOOR PROXIMITY LIGHTING BETWEEN 6 C, D, E AND 9 C, D, E INOP. REPAIRED BROKEN WIRE AT BATTERY PACK CANNON PLUG. 2 L 7 2 4F RT A20EU 1996011200276 19960112 00276 EU 1996 1 12 QXEA9600014 1 19960107 A 3350 1820 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 802PH 11017 SEA - LIGHT ON EMERGENCY EXIT HANDLE ROW 8 RIGHT IS INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996011200277 19960112 00277 NM 1996 1 12 QXEA9600015 1 19960107 A 3350 321430 BATTERY PACK DORNER DORNER DO32 DO328100 2996000 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 330PH 3008 PDX - EXIT SIGN ABOVE SEAT 11A AND RIGHT SIDE AFT EXTERIOR INOP. REPLACED AND LIGHT OPS CHECKED GOOD. 2 H 7 2 4T RT A45NM 1996011200279 19960112 00279 SW 1996 1 12 SWIA95704 1 19960101 A 5210 PRESSURE LINE SWRNGN SA227 SA227AC 8780603 SW PAX DOOR CUT A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 27220 AC718 A/C WOULD NOT PRESSURIZE, CABIN DOOR WAS LEAKING. CABIN DOOR SUPPLY LINE CUT. REMOVED AND REPLACED SUPPLY LINE WITH NE W ONE, OPS CHECKS GOOD. 1 L 7 2 4T A8SW 1996011200280 19960112 00280 SO 1996 1 12 SWIA95705 1 19960104 A 2750 CONNECTORS EMB 120 EMB120ER 3260203 SO LT TE FLAPS LOOSE A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 199SW 120237 AFTER TAKEOFF, TRIED TO RETRACT FLAPS AND THEY ONLY WENT UP TO ABOUT 7 DEGREES, RECEIVED A FLAP DISAGREEMENT WARNING. W E THEN RETURNED FOR LANDING AT SLC. AFTER TOUCHDOWN THE FLAPS RETRACTED. BEFORE TAKEOFF WE GOT DE-ICED WITH FLAPS DOWN 45 DEGREES AS 50P. FOUND DE-ICE FLUID IN CANNON PLUGS ON LT OUTBOARD FLAP ACTUATOR. CLEANED AND SECURED PLUGS, CYCLED FLAPS NUMEROUS TIMES, NO DEFECTS NOTED AND OPS GOOD. 2 L 7 2 4T RT A31SO 1996011200281 19960112 00281 EA 1996 1 12 SWIA95706 1 19960107 A 2421 IDG CNDAIR CL600 CL6002B19 EA RT ENGINE FAILED A SWIA K NONE O OTHER CR CRUISE 1 NM 07 409SW 7056 NR 1 IDG CAUTION MESSAGE ILLUMINATED IN FLIGHT. IDG DISCONNECTED PER CHECKLIST. REMOVED AND REPLACED NR 2 IDG ON RIGHT HAND ENGINE. RAN ENGINE, OPS CHECK AND LEAK CHECK GOOD. 2 L 7 2 4F RT A21EA 1996011200282 19960112 00282 NM 1996 1 12 UPS205183 1 19960109 A 3350 LIGHT BOEING 727 727247 138408F NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 209UP 21698 YHM - MAINTENANCE REPORTED, L-1 EMERGENCY LIGHT IS INOP. RESERVED L-1 EMERGENCY LIGHT ASSY AND ASSY CHECKED SERVICEABLE . 2 L 7 3 4F A3WE 1996011200428 19960112 00428 WP 1996 1 12 IXXA95134 1 19960103 A 3230 GRND SHIFT MECH DOUG DC8 DC862 3021970 WP NLG OUT OF RIG A IXXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 51CX 46027 ON DEPARTURE OUT OF EWR, THE LANDING GEAR HANDLE WOULD NOT MOVE TO THE 'RETRACT' POSITION. THE AIRCRAFT APPEARED TO BE STUCK IN THE 'GROUND' MODE. THE AIRCRAFT RETURNED TO EWR FOR MAINTENANCE. THE AIRCRAFT WAS FERRIED TO A MAINTENANCE FA CILITY WHERE THE NOSE LANDING GEAR WAS DISASSEMBLED, INSPECTED, AND RESEALED, AND THE GROUND SHIFT MECHANISM WAS RIGGED. THE LANDING GEAR WAS OPERATIONALLY CHECKED AND DETERMINED TO BE OPERATING NORMALLY FOLLOWING THE RE-RIG. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 4 4F 4A25 1996011200518 19960112 00518 WP 1996 1 12 9600349101 1 19960103 A 5320 FITTING DOUG DC9 DC915 3022036 WP PAX DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 91S 47063 DURING H-CHECK, FOUND CRACKS IN THE AFT ENTRY DOOR UPPER LEFT AND RIGHT STOP FITTINGS. REPLACED FITTINGS. 2 L 7 2 4F A6WE 1996011200519 19960112 00519 WP 1996 1 12 9600359610 1 19960103 A 5720 FITTING DOUG DC9 DC932 3022066 WP CTR WING CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 610NW 47432 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE CENTER WING END FITTING (SECOND STRINGER FROM THE FOR WARD END). REPLACED END FITTING (P/N 3920326-501N) PER SRM 51-30-2. 2 L 7 2 4F A6WE 1996011200520 19960112 00520 WP 1996 1 12 9600369941 1 19960103 A 5720 FITTING DOUG DC9 DC932 3022066 WP WS 69 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3324L 47103 DURING SPECIAL MAINTENANCE VISIT, FOUND CORROSION ON THE RIGHT WING LOWER AFT FLANGE FOOT OUTBOARD OF XRS 69 AT STR 18. REPLACED FITTING PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996011200521 19960112 00521 WP 1996 1 12 9600371154 1 19960104 A 5320 SPLICE FITTING DOUG DC10 DC1040 3023508 WP FS 1718 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 154US 46763 DURING T-CHECK, FOUND CORROSION ON THE STR 52 SPLICE FITTING AT FS 1718. FABRICATED AND INSTALLED PER AFA 7102-1 AND SR M 53-10-00. 2 L 7 3 4F A22WE 1996011200522 19960112 00522 WP 1996 1 12 9600389605 1 19960104 A 5341 FITTING DOUG DC9 DC932 3022066 WP FS 598-620 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 605NW 47223 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE LEFT WING TO FUSELAGE ATTACH FITTING BETWEEN STR 22L - 23L, FS 598 - 620. REPLACED FITTING PER SRM 51-30. 2 L 7 2 4F A6WE 1996011200523 19960112 00523 WP 1996 1 12 9600399938 1 19960106 A 5320 FITTING DOUG DC9 DC931 3022065 WP DOOR STOP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 1798U 47369 DURING M-CHECK, FOUND A CRACK IN THE AFT ENTRY DOOR RIGHT SIDE STOP FITTING. REPLACED FITTING PER SRM 51-30-0. 2 L 7 2 4F A6WE 1996011200524 19960112 00524 WP 1996 1 12 9600409870 1 19960106 A 5320 FITTING DOUG DC9 DC951 3022051 WP FS 701-708 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 779NC 48101 DURING H-CHECK, FOUND CORROSION ON THE LONGERON 29L KEEL FITTING BETWEEN FS 701 - 708. REPLACED FITTING PER SRM 51-10-4 . 2 L 7 2 4F A6WE 1996011200525 19960112 00525 WP 1996 1 12 9600419602 1 19960106 A 5320 FITTINGS DOUG DC9 DC932 3022066 WP FS 996 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 602NW 47046 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACKS IN THE INTERCOSTAL SUPPORT FITTINGS FS 996, BETWEEN LONGERONS 27L - 28L AND BETWEEN 27R - 28R. REPLACED FITTINGS PER SRM 51-30-2. 2 L 7 2 4F A6WE 1996011200526 19960112 00526 WP 1996 1 12 9600429602 1 19960106 A 5320 FITTING DOUG DC9 DC932 3022066 WP FS 598-639 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 602NW 47046 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LONGERON 24R KEEL BEAM FITTING BETWEEN FS 598 - 639 . REPLACED FITTING PER SRM 51-00. 2 L 7 2 4F A6WE 1996011200527 19960112 00527 NM 1996 1 12 9600446307 1 19960110 A 3350 CONNECTOR BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 667US 24222 DURING LINE CHECK, THE FLOOR MOUNTED EMERGENCY PATH LIGHTS BETWEEN SEAT ROWS 52L TO 58L WERE FOUND INOPERATIVE. RECONNE CTED LIGHT PIN IN FLOOR TRACK. OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996011200528 19960112 00528 EU 1996 1 12 96FDEA00037 1 19960110 A 5101 STRUCTURE AIRBUS 310 A310221 3930310 EU AIR FRAME VIBRATION A FDEA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 25 416FE 288 AFTER TAKEOFF WITH GEAR UP, A/C STARTED VIBRATING. GEAR WAS CYC DOWN & UP WITH NO PROBLEMS. VIB CONTD. LEVEL OFF AT 5 000 FEET. FLAPS/SLATS RETRACTED, VIBRATION STOPPED AT PWR REDUCTION (VIB WAS MOD). RETND FOR LANDING WITH NORMAL SLAT/ FLAP EXTENSION & NO VIB AT REDUCED PWR. PERFORMED WALKAROUND INSP OF RUDDER, LANDING GEAR, STABILIZER, FLAPS AND SLATS, AILERONS, SPOILERS, ELEVATORS ALL CK'D OK FROM GROUND. PERFORMED HI-PWR ENG RUN PER MM 71-00-00, PG A588 IN CONJUNCTIO N WITH A300 FLT MANUAL, REF 5-3-2. PARAM CK'D WITH PUBLISHED LIMITS FOR WEATHER CONDITIONS. 1.489 NR 1 ENG N1=1.2, N2= .6, NR 2 ENG N1=.4, N2=6. VISUALLY INSP ENG SHROUDS, BLADE TIPS, & RUB STRIPS PER MM 72-23-01, PG 601-606, CK'D GOOD. 2 L 7 2 4F RT A35EU 1996011200529 19960112 00529 WP 1996 1 12 ABXA9600005 1 19960104 A 3350 60030431 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 905AX 6864 47147 DURING SERVICE CHECK, IT WAS NOTED EMERGENCY EXIT LIGHTS DO NOT EXTINGUISH WITH SWITCH IN OFF POSITION WHEN AIRCRAFT POW ER IS TURNED OFF. REPLACED EMERGENCY LIGHT'S BATTERY POWER SUPPLY IAW DC-9 MM 33-53-0. 2 L 7 2 4F A6WE 1996011200530 19960112 00530 WP 1996 1 12 ABXA9600006 1 19960103 A 5280 5616307501 DOOR DOUG DC8 DC862 3021970 WP LT MG DAMAGED A ABXA O OTHER J WARNING INDICATION TO TAKEOFF 1 GL 23 803AX 46077 THE GEAR UNSAFE LIGHT ILLUMINATED IN-FLIGHT. RECYCLED GEAR WITH NO EFFECT. DOWN INDICATIONS NORMAL. GEAR DOOR LATCH L IGHTS WERE CHECKED AND LEFT DOOR INDICATED UNLATCHED. FOUND LEFT LANDING GEAR DOOR DAMAGED DUE TO ICE ACCUMULATION. RE PAIRED DOOR IAW ABX REA D825-13919. PERFORMED GEAR SWING, OPS CHECKED GOOD IAW DC-8 MM 32-30-0. 2 L 7 4 4F 4A25 1996011200531 19960112 00531 WP 1996 1 12 ABXA9600007 1 19960109 A 3240 305323001 CONTROL VALVE DOUG DC8 DC861 3021952 WP BRAKE SYST BROKEN A ABXA K NONE O OTHER TX TAXI/GRND HDL 1 GL 23 847AX 6892 46031 LEFT BRAKES GO FULL TRAVEL WITH NO BRAKING ACTION. BRAKE PRESSURE AND FLUID QUANTITY ARE NORMAL. REPLACED BROKEN BRAKE CONTROL VALVE IAW DC8 MM. OPS CHECK GOOD. 2 L 7 4 4F 4A25 1996011200532 19960112 00532 WP 1996 1 12 ABXA9600008 1 19960110 A 3040 TERMINAL DOUG DC8 DC863 302198A WP WINDSHIELD HEAT DIRTY A ABXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 816AX 46093 DURING CRUISE, ELECTRICAL TYPE FUMES WERE NOTED FROM AREA OF CAPTAIN'S GLARESHIELD. TURNED OFF WINDSHIELD HEAT AND SMEL L SEEMED TO DISSIPATE, BUT THERE WAS A RESIDUAL SMELL LATER. PULLED CIRCUIT BREAKERS FOR FLOOR HEATERS AND SMELL SEEMED TO GO AWAY. INSPECTED THE FLOOR HEATERS AND ELECTRICAL CONNECTORS AND NO DEFECTS WERE NOTED. INSPECTED CAPTAIN'S WIND SHIELD AND TERMINAL BLOCK. FOUND DIRT ON MATING SURFACE BETWEEN WINDSHIELD AND TERMINAL BLOCK THAT CAUSED THE TERMINAL BLOCK TO BECOME HOT. CLEANED MATING SURFACE AND INSTALLED NEW HARDWARE. OPS CHECK GOOD. 2 L 7 4 4F 4A25 1996011200533 19960112 00533 1996 1 12 COMA9610006 4 19960109 A 3413 066500011801 VSI EMB 120 EMB120RT SO LEFT DEFECTIVE A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 255CA 275 120238 PILOTS VSI TUBE BLANK. REPLACED THE 1VA-81A TA/VS1. 2 L 7 2 4T RT A31SO 1996011200534 19960112 00534 SO 1996 1 12 COMA9610007 1 19960108 A 2751 INDICATION EMB 120 EMB120RT SO TE FLAPS MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 256CA 120245 FLAP DISAGREEMENT INDICATION AFTER TAKEOFF. COULD NOT DUPLICATE DISCREPANCY - ACFT RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 1996011200535 19960112 00535 SO 1996 1 12 COMA9610008 1 19960108 A 5753 KRP138112VT ROLLER EMB 120 EMB120RT SO LT FLAP WORN A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 256CA 120245 FLAP DISAGREEMENT INDICATION AFTER TAKEOFF. REPLACED WORN ROLLERS ON LT OUTBOARD FLAP. 2 L 7 2 4T RT A31SO 1996011200536 19960112 00536 SO 1996 1 12 COMA9610009 1 19960109 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST UK UNKNOWN 1 SO 01 269CA 14680 2007 120263 EMERGENCY FLOOR PATH LIGHTING AFT OF ROW 5 IS INOPERATIVE. REPLACED EMERGENCY LIGHTING BATTERY. 2 L 7 2 4T RT A31SO 1996011200537 19960112 00537 SO 1996 1 12 COMA9610010 1 19960106 A 5753 KRP138112VT ROLLERS EMB 120 EMB120RT SO LT FLAP WORN A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 266CA 120258 FLAP DISAGREEMENT WARNING AFTER TAKEOFF. REPLACED LT OUTBOARD FLAP ROLLERS. 2 L 7 2 4T RT A31SO 1996011200538 19960112 00538 SO 1996 1 12 COMA9610011 1 19960106 A 5753 TRACKS EMB 120 EMB120RT SO TE FLAPS DIRTY A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 179CA 120179 FLAP DISAGREEMENT WARNING AFTER TAKEOFF. COULD NOT DUPLICATE - CLEANED FLAP TRACKS AND ROLLERS AND RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 1996011200539 19960112 00539 SO 1996 1 12 COMA9610013 1 19960109 A 5753 KRP138112VT ROLLERS EMB 120 EMB120RT SO RT FLAP WORN A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 267CA 120259 FLAP DISAGREEMENT WARNING AFTER TAKEOFF. REPLACED WORN ROLLERS ON RT OUTBOARD FLAP. 2 L 7 2 4T RT A31SO 1996011200541 19960112 00541 EU 1996 1 12 COMA9630010 1 19960108 A 3246 5009237 RACE LORAL 5010488 SAAB SF340 SF340A 7850100 EU LT MLG WHEEL SPUN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 344CA 405 OCT910062 340A025 MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO MATE FOUND FLAT. DURING INSPECTION, FOUND INNER RACE SPUN. SUB-ASSY HAS BE EN REMOVED FROM SERVICE AND SENT TO ABS FOR REPAIR AND OVERHAUL. 2 L 7 2 4T RT A52EU 1996011200542 19960112 00542 EU 1996 1 12 COMA9630011 1 19960109 A 3020 NH2466881 INLET SAAB SF340 SF340A 7850100 EU RT ENGINE BURNED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 347CA 5314 4737 340A028 RIGHT ENGINE INLET HEAT FAILED AND LOWER INLET SECTION IS BURNED. REPLACED THE FORWARD LOWER INLET. 2 L 7 2 4T RT A52EU 1996011200543 19960112 00543 EA 1996 1 12 COMA9660007 1 19960109 A 2613 356024310 ELEMENT CNDAIR CL600 CL6002B19 EA LT PYLON DEFECTIVE A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 924CA 7026 LEFT 14TH STAGE DUCT OVERHEAT WARNING IS ON INTERMITTENTLY DURING FLIGHT. REPLACED THE PYLON SECTION OF THE 14TH STAGE BLEED LEAK DETECTION SYSTEM. 2 L 7 2 4F RT A21EA 1996011200544 19960112 00544 EA 1996 1 12 COMA9660008 1 19960110 A 2750 RETRACT MECH CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 932CA 7038 FLAPS ARE STUCK AT ZERO DEGREES. COULD NOT DUPLICATE DISCREPANCY, SYSTEM FUNCTION CHECK NORMAL. ACFT RETURNED TO SERVI CE. 2 L 7 2 4F RT A21EA 1996011200545 19960112 00545 EA 1996 1 12 COMA9660009 1 19960110 A 3220 16400105 DRAG BRACE CNDAIR CL600 CL6002B19 EA NLG DEFECTIVE A COMA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 929CA 882 882 7035 NOSE LANDING GEAR DID NOT RETRACT. REPLACED THE NLG DRAG BRACE ASSY. 2 L 7 2 4F RT A21EA 1996011200546 19960112 00546 EA 1996 1 12 COMA9660010 1 19960110 A 3220 16400105 DRAG BRACE CNDAIR CL600 CL6002B19 EA NLG DEFECTIVE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 946CA 471 471 7072 THE NOSE LANDING GEAR DID NOT RETRACT. REPLACED THE NLG DRAG BRACE ASSY. 2 L 7 2 4F RT A21EA 1996011200547 19960112 00547 NM 1996 1 12 DHLA720007 1 19960109 A 2780 106081917 SWITCH BOEING 727 727228 NM NR 2 LE FLAP FAILED A T DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 720DH 19544 DURING CLIMB, FLAPS UP LEADING EDGE LIGHT INTERMITTENTLY ON. DURING FLAP EXTENSION, NR 2 L/E FLAP DID NOT LOCK UP. YEL LOW AND GREEN L/E FLAP LIGHTS ON FORWARD PANEL WERE ALTERNATING. CHRISTMAS TREE INDICATED INTERMITTENT YELLOW LIGHT FOR NR 2 L/E FLAP. AT FLAPS 5 DEGREES, ALL GREEN INDICATION. INSPECTED FLAPS. NO DEFECT NOTED. REMOVED AND REPLACED FLA P INDICATING SWITCH. OPS CHECK OK. REF 27-82-1. 2 L 7 3 4F A3WE 1996011200548 19960112 00548 WP 1996 1 12 SCNA96004 1 19960108 A 3234 580500 CONTROL CABLE DOUG DC10 DC1015 3022118 WP COCKPIT OUT OF ADJ A SCNA O OTHER O OTHER CL CLIMB 1 GL 15 152SC 48289 AFTER TAKEOFF, LANDING GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. RETRACTED GEAR WITH HANDLE RELEASE BUTTON AND GEA R RETRACTED NORMALLY. ADJUSTED PUSH/PULL CABLE ROD END PER MM 32-21-01, ANTI-RETRACTION OPS CHECKED NORMAL ON GROUND. 2 L 7 3 4F A22WE 1996011200549 19960112 00549 WP 1996 1 12 UPS805189 1 19960110 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 8 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 WHILE IN FOR B-CHECK, MAINTENANCE REPORTED LONGERON 34R ATTACH FITTING AT STA 8.00 CRACKED, EVIDENCE OF CORROSION. WILL REPAIR/REPLACE FITTING PER UPS E.O. DC8 SRM. 2 L 7 4 4F RT 4A25 1996011900001 19960119 00001 WP 1996 1 19 9600451158 1 19960102 A 3350 POWER SUPPLY DOUG DC10 DC1040 3023508 WP FUSELAGE FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 158US 46767 DURING LINE CHECK, FOUND THE AFT EMERGENCY LIGHT POWER SUPPLY FAILED BITE TEST. REPLACED THE AFT POWER SUPPLY AND BATTE RY PACK. 2 L 7 3 4F A22WE 1996011900002 19960119 00002 WP 1996 1 19 9600469998 1 19960111 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8934E 47143 DURING LINE CHECK, EMERGENCY FLOOR PATH LIGHT AT REAR OF CABIN INOPERATIVE. REPAIRED BROKEN WIRE AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996011900003 19960119 00003 WP 1996 1 19 9600479935 1 19960110 A 3222 SCHRADER VLV DOUG DC9 DC931 3022065 WP NLG STRUT FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 1332U 47404 DURING CLIMB, THE AIRCRAFT DID NOT SHIFT INTO FLIGHT MODE AND THE LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. SERVICED NOSE STRUT AND REPLACED SCHRADER VALVE, OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996011900004 19960119 00004 EU 1996 1 19 9600483208 1 19960109 A 2611 SMOKE ALARM AIRBUS 320 A320211 3930320 EU CARGO COMPT ACTIVATED A NWAA D F RETURN TO BLOCK ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 GL 01 308US 107 DURING TAXI AFT CARGO SMOKE ECAM INDICATION ILLUMINATED AND DISCHARGED EXTINGUISHING AGENT. AIRCRAFT RETURNED TO THE GA TE AND FIRE DEPARTMENT INVESTIGATED SOURCE OF INDICATION. NO DETECTION OF FIRE OR SMOKE NOTED. MAINTENANCE VERIFIED NO EVIDENCE OF FIRE OR SMOKE AND REPLACED THE FIRE EXTINGUISHING BOTTLE. SYSTEM OPERATION CHECKED NORMAL. 2 L 7 2 4F RT A28NM 1996011900005 19960119 00005 NE 1996 1 19 9600492295 2 19960103 A 7230 COMPRESSOR BOEING 727 727251 138408H NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE STALLED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 01 295US 21506 696495 NR 2 ENGINE COMPRESSOR STALLED ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTEN ANCE INSPECTED THE ENGINE AND NO DISCREPANCIES WERE NOTED. AIRCRAFT CONTINUED IN SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 1996011900006 19960119 00006 NE 1996 1 19 9600509878 2 19960101 A 7320 FUEL CONTL SYST DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE NR 1 ENGINE OUT OF ADJUST A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 01 787NC 48149 688767 NR 1 ENGINE WOULD NOT DEVELOP TARGET EPR FOR TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. M AINTENANCE TRIMMED THE ENGINE AND SUBSEQUENT RUNUP WAS SATISFACTORY. 2 L 7 2 4F 4 F A6WE E2EA 1996011900007 19960119 00007 EU 1996 1 19 9600513245 1 19960111 A 3350 321454 POWER SUPPLY AIRBUS 320 A320211 3930320 EU PIT PANEL INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 345NW 10254 5008 399 DURING SYSTEM TEST, THE EMERGENCY LIGHT FAILED AT PTT PANEL, COM EMER L FAULT. REPLACED THE POWER SUPPLY AND BATTERY PA CK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A28NM 1996011900008 19960119 00008 EU 1996 1 19 9600523245 1 19960109 A 2913 4205400 HYD PUMP AIRBUS 320 A320211 3930320 EU NR 2 ENGINE FAILED A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 345NW 9683 399 DURING CLIMB UPON FLAP RETRACTION, LOST YELLOW SYSTEM HYDRAULIC FLUID. FLIGHT RETURNED TO MIA WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE YELLOW PTU PLUG BLOWN OUT AND THE NBR 2 ENGINE DRIVEN HYDRAULIC PUMP INOPERATIVE. REPLACED THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP, 2-WAY HYDRAULIC VALVE, PTU MANIFOLD, AND PRIORITY VALVE. LEAK AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A28NM 1996011900009 19960119 00009 WP 1996 1 19 9600531211 1 19960111 A 4900 TSCP7004B APU DOUG DC10 DC1030 3023501 WP TAIL FAILED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 211NW 54569 2234 46868 DURING CLIMB, A STRONG OIL SMELL WAS PRESENT THROUGH OUT THE AIRCRAFT. FLIGHT CREW FOLLOWED SMOKE REMOVAL PROCEDURES, B UT ODOR COULD NOT BE ISOLATED. FLIGHT RETURNED TO DEPARTURE AIRPORT LANDING WITHOUT FURTHER INCIDENT. GROUND PERSONNEL REMOVED AND REPLACED ALL THREE WATER SEPARATOR BAGS AND DETERMINED THAT APU WAS SOURCE OF ODOR. APU PLACED ON MEL. 2 L 7 3 4F A22WE 1996011900012 19960119 00012 1996 1 19 9600569163 4 19960109 A 3454 5224280102 NAV RECEIVER DOUG DC9 DC914 3022034 WP NR 1 MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 8906E 42076 45747 CAPTAIN'S NAV RECEIVER FAILED SHORTLY AFTER TAKEOFF. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED NR 1 NAV RECEIVER. OPERATIONAL CHECK OK AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996011900013 19960119 00013 WP 1996 1 19 9600579139 1 19960110 A 3350 60030451 BATTERY PACK DOUG DC9 DC914 3022034 WP RT EXTERIOR DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 948L 47049 DURING PERIODIC CHECK, RIGHT EXTERIOR EMERGENCY LIGHT FAILED TEN MINUTE TEST. REPLACED BATTERY PACK AND OPERATIONAL CHE CK OK. 2 L 7 2 4F A6WE 1996011900014 19960119 00014 WP 1996 1 19 9600589180 1 19960108 A 3350 6011779 BATTERY PACK DOUG DC9 DC914 3022034 WP RT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 3312L 45707 DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AND OPERATIO NAL CHECK OK. 2 L 7 2 4F A6WE 1996011900015 19960119 00015 NM 1996 1 19 9600599311 1 19960111 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 314RC 49110 DURING LINE MAINTENANCE INSPECTION, FOUND AFT TWO ROWS OF OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996011900016 19960119 00016 WP 1996 1 19 9600609851 1 19960108 A 3350 CONNECTOR DOUG DC9 DC951 3022051 WP BATTERY PACK CONTAMINATED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 760NC 47708 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. CLEANED CANNON PLUG ON BATTE RY PACK. 2 L 7 2 4F A6WE 1996011900017 19960119 00017 NM 1996 1 19 96FDEA00049 1 19960113 A 2780 656021211 MODULE BOEING 727 727225 1384077 NM LE FLAPS FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 467FE 21449 NR 1 LED SLAT, LT WING DID NOT RETRACT WHILE GOING FROM FLAP 5 TO FLAP 2. AMBER LIGHT ON FRONT PANEL WAS ON AND S/O PAN EL IND AMBER, INTRANSIT RED TABS COMPLETED WITH SAME IND. ALSO, WING ANTI-ICE ATTEMPTED. NR 1 SLAT FUNCTIONS NORMAL, P OSITION SWITCH INOPERATIVE. APPLIED HEAT TO NR 1 RETRACT SWITCH, NO HELP. INSTALLED SWITCH CONTACT JUMPER, NO HELP. R EPLACED L/E POS CONTROL MODULE, RAN FLAPS THROUGH NUMEROUS CYCLES AND ALL IND NORMAL. 2 L 7 3 4F A3WE 1996011900018 19960119 00018 NM 1996 1 19 96FDEA00050 1 19960111 A 5320 WEB BOEING 747 747245F 1384897 NM BS 1241 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 640FE 20826 SIN - CENTER SECTION TANK AFT FACE WEB EXTERIOR FOUND EXFOLIATED AT BS 1241 WL 172, BETWEEN LBL 5 TO 80 AS MARKED. 2 L 7 4 4F A20WE 1996011900019 19960119 00019 NM 1996 1 19 96FDEA00051 1 19960111 A 5320 WEB BOEING 747 747245F 1384897 NM BS 1241 EXFOLIATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 640FE 20826 CENTER SECTION TANK AFT FACE WEB EXTERIOR FOUND EXFOLIATED AT BS 1241 WL 172 BETWEEN RBL 80 TO 104. REPAIR CARRIED OUT AS PER ERA B57-10-94. 2 L 7 4 4F A20WE 1996011900020 19960119 00020 NM 1996 1 19 96FDEA00052 1 19960112 A 5280 DOOR DOUG MD11 MD11F 3023600 NM LT MLG DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 LT MLG DOOR HAS 2 INCH CRACK AT UPPER MID HINGE AREA, LWR SKIN. 2 L 7 3 4F RT A22WE 1996011900021 19960119 00021 NM 1996 1 19 96FDEA00053 1 19960112 A 5280 DOOR DOUG MD11 MD11F 3023600 NM CTR GEAR DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 CENTERLINE LANDING GEAR DOOR, LT FWD DOOR IS CRACKED AT LOWER FWD CORNER AT RADIUS. REMOVED LOWER CORNER SECTION LOCATE D NEW FRAME, INSTALLED NEW FRAME PER SRM 51-00-01. 2 L 7 3 4F RT A22WE 1996011900022 19960119 00022 NM 1996 1 19 96FDEA00054 1 19960112 A 5280 ANB73872 FRAME DOUG MD11 MD11F 3023600 NM CTR GEAR DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 CENTERLINE LANDING GEAR DOOR, RT FWD DOOR IS CRACKED AT LOWER FWD CORNER AT RADIUS. REMOVED CRACKED FRAME AND INSTALLED NEW FRAME PER SRM 51-00-01. 2 L 7 3 4F RT A22WE 1996011900024 19960119 00024 NM 1996 1 19 96FDEA00056 1 19960115 A 5320 65453133 STRINGER CLIP BOEING 727 727227 1384078 NM BS 440 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 488FE 21491 CRACKED STR CLIP AT BS 440 STR 1L. UPON REMOVAL OF CRACKED STR CLIP FOUND STR NR 1 TO BE DAMAGED AT BS 441. PERFORMED STR REPAIR BS 436 TO 446 STR NR 1 IAW FEDEX SRM 53-10-3 AND INSTALLED NEW STR CLIP BS 440 STR NR 1. 2 L 7 3 4F A3WE 1996011900025 19960119 00025 NM 1996 1 19 96FDEA00057 1 19960115 A 5314 KEEL BEAM BOEING 727 727227 1384078 NM BS 950 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 488FE 21491 CORROSION ON LT KEEL BEAM OUTBOARD FLANGE AT BS 950D PLUS 3, LBL 10. REMOVED CORROSION ON LT KEEL BEAM OUTBOARD FLANGE AND REPAIRED PER FEDEX EA 7-5310-26837. 2 L 7 3 4F A3WE 1996011900026 19960119 00026 NM 1996 1 19 96UAL900022 1 19960110 A 3350 BATTERY BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE GALLEY DISCHARGED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 9013U 19051 AFT GALLEY EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES AND CHECKS OK. 2 L 7 2 4F 4 F A16WE E2EA 1996011900027 19960119 00027 EU 1996 1 19 96UAL900023 2 19960110 A 7230 COMPRESSOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563B2 13802 EU NR 1 ENGINE BIRD STRIKE A UALA A E UNSCHED LANDING ENGINE SHUTDOWN C Y F.O.D. ENGINE STOPPAGE CL CLIMB 1 WP 29 350UA 24301 721649 NUMBER ONE ENGINE FAILED DURING ROTATION. HEAVY FIRST STAGE FAN DAMAGE. A BIRD STRIKE WAS THE CAUSE OF THE ENGINE FAIL URE. ENGINE WAS REMOVED AND SENT TO THE SHOP FOR REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 1996011900028 19960119 00028 EU 1996 1 19 96UAL900024 2 19960110 A 7200 ENGINE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563B2 13802 EU NR 2 FAILED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 29 312UA 23673 720804 NUMBER TWO ENGINE WENT TO 935 DEGREES, ABORTED TAKEOFF AT 90 KNOTS. THE ENGINE EXPERIENCED AN EXHAUST GAS TEMPERATURE E XCEEDENCE, DUE TO NORMAL ENGINE PERFORMANCE DETERIORATION. ENGINE WAS REMOVED AND SENT TO THE SHOP FOR REPAIR. HIGH PR ESSURE TURBINE HARDWARE DID NOT REVEAL ANY OUT OF THE ORDINARY CONDITIONS. THIS ENGINE ACCUMULATED 9049 HOURS SINCE LAS T SHOP VISIT. 2 L 7 2 4F 4 F RT A16WE E21EU 1996011900029 19960119 00029 NM 1996 1 19 96UAL900025 1 19960110 A 3350 BATTERY PACK BOEING 727 727222 1384073 NM AFT ENTRY DOOR DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7444U 21898 AFT ENTRY DOOR EMERGENCY EXIT SLIDE LIGHT INOPERATIVE. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1996011900030 19960119 00030 NM 1996 1 19 96UAL900026 1 19960111 A 3350 LIGHT BOEING 727 727222 1384073 NM CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7255U 21402 1 LEFT EMERGENCY LIGHT DOES NOT ILLUMINATE WITH LOSS OF ESS POWER. REPLACED LIGHT ASSEMBLY. 2 L 7 3 4F A3WE 1996011900031 19960119 00031 NE 1996 1 19 96UAL900027 2 19960111 A 7200 ENGINE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE NR 2 VIBRATION A UALA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 WP 29 610UA 21871 707515 HIGH VIBRATION, NUMBER TWO ENGINE. TROUBLESHOT PROBLEM PER 767-200 MM 71-05-00, PAGES 120 TO 121. REPLACED OIL FILTER, LOOKED AT MAGNETIC CHIP DETECTORS, CHECKED ENGINE INLET AND EXHAUST FOR DAMAGE OR METAL FRAGMENTS. PERFORMED A HIGH PO WER ENGINE RUN AND NO PROBLEMS FOUND. MAXIMUM VIBRATION DURING HIGH POWER RUN WAS 0.5 MILS AT 1.4 EPR, LIMIT IS 5.0 MIL S. PROBLEM HAS NOT BEEN DUPLICATED SINCE ORIGINAL WRITE-UP. 2 L 7 2 4F 4 F RT A1NM E3NE 1996011900032 19960119 00032 NM 1996 1 19 96UAL900028 1 19960111 A 3350 BATTERY PACK BOEING 727 727222 1384073 NM CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7277U 21424 THE AFT CABIN DOOR EXTERIOR EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1996011900033 19960119 00033 NM 1996 1 19 96UAL900029 1 19960112 A 3350 LAMP BOEING 737 737222 1384473 NM CABIN FAILED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 9017U 19055 EMERGENCY ESCAPE PATH LIGHTING INOP AT ROW 12. RELAMPED AND REPLACED COVER, CHECKS OK. 2 L 7 2 4F A16WE 1996011900039 19960119 00039 WP 1996 1 19 ABXA9600013 1 19960109 A 5330 592032339 SKIN DOUG DC9 DC932 3022066 WP BS 436 PUNCTURED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 ONE INCH HOLE IN FUSELAGE BETWEEN REAR OF FORWARD BELLY DOOR AREA AND STATIC PORT. THE HOLE WAS CAUSED BY SNOW PLOW MAK ING CONTACT WITH FUSELAGE. FABRICATED AND INSTALLED REPAIR IAW REPAIR ENGINEERING AUTHORIZATION D953-14048-MR. 2 L 7 2 4F A6WE 1996011900047 19960119 00047 SO 1996 1 19 COMA9610014 1 19960111 A 3246 3006041 WHEEL 314461 EMB 120 EMB120RT SO RT MLG DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 244CA 4441 226 1217 MECHANIC REMOVED TIRE FROM A/C DUE TO TIRE WORN TO LIMITS. DURING INSPECTION IN WHEEL SHOP, FOUND DAMAGE TO SUB ASSY AN D KEY INSERTS ANTICIPATE BRAKE FAILURE. SUB ASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO BFG FOR FURTHER INSPECTION A ND EVALUATION. 2 L 7 2 4T RT A31SO 1996011900048 19960119 00048 SO 1996 1 19 COMA9610015 1 19960111 A 3246 3006041 WHEEL 314461 EMB 120 EMB120RT SO RT MLG DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 264CA 4467 497 1256 MECHANIC REMOVED TIRE FROM AIRCRAFT DUE TO TIRE WORN TO LIMITS. DURING INSPECTION OF WHEEL IN WHEEL SHOP, FOUND DAMAGED KEYS DUE TO BRAKE FAILURE. SUB ASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO BFG FOR INSPECTION AND EVALUATION. 2 L 7 2 4T RT A31SO 1996011900049 19960119 00049 SO 1996 1 19 COMA9610016 1 19960112 A 5753 FLAP TRACKS EMB 120 EMB120RT SO TE FLAPS DIRTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 196CA 120196 FLAP DISAGREEMENT WARNING WHEN FLAPS SELECTED UP AFTER TAKEOFF. CLEANED THE FLAP TRACKS AND ACFT RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 1996011900050 19960119 00050 SO 1996 1 19 COMA9610017 1 19960111 A 3230 12038594001 CONTROL BOX EMB 120 EMB120RT SO LANDING GEAR DEFECTIVE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 247CA 9843 120225 LANDING GEAR WILL NOT RETRACT. REPLACED THE LANDING GEAR CONTROL BOX. 2 L 7 2 4T RT A31SO 1996011900051 19960119 00051 SO 1996 1 19 COMA9610018 1 19960111 A 6120 30005000052 SCU 3000500005 EMB 120 EMB120RT SO LT\RT ENGINE MALFUNCTIONED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 263CA 1572 745 2120 120255 AUTO-FEATHER SYSTEM WILL NOT ARM INTERMITTENTLY. REPLACED THE LT AND RT ENGINE TORQUE SIGNAL CONDITIONER UNITS. 2 L 7 2 4T RT A31SO 1996011900052 19960119 00052 1996 1 19 COMA9610019 4 19960110 A 3418 C818171 AOA EMB 120 EMB120RT SO LEFT DEFECTIVE A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 1110J 13204 4617 120110 STICK SHAKER CAME ON DURING TAKEOFF ROLL. REPLACED THE LT ANGLE OF ATTACK VANE. 2 L 7 2 4T RT A31SO 1996011900053 19960119 00053 EU 1996 1 19 COMA9630012 1 19960111 A 2731 DL3827M157 ACTUATOR SAAB SF340 SF340A 7850100 EU LT ELEV TRIM DEFECTIVE A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 359CA 11175 2364 340A053 THE LT ELEVATOR TRIM INDICATION IS INOP. REPLACED THE LT ELEVATOR TRIM ACTUATOR. 2 L 7 2 4T RT A52EU 1996011900054 19960119 00054 EU 1996 1 19 COMA9630013 1 19960111 A 5270 DOOR WARNING SAAB SF340 SF340A 7850100 EU CARGO COMPT ACTIVATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 356CA 340A034 CARGO DOOR WARNING CAME ON AFTER TAKEOFF. INSPECTED CARGO DOOR MECHANISM AND WARNING SYSTEM, NO DEFECTS FOUND. ACFT RE TURNED TO SERVICE. 2 L 7 2 4T RT A52EU 1996011900055 19960119 00055 EU 1996 1 19 COMA9630014 1 19960112 A 3260 D494050001 CONTROL BOX SAAB SF340 SF340A 7850100 EU LANDING GEAR DEFECTIVE A COMA K NONE N FALSE WARNING CL CLIMB 1 SO 01 158CA 21835 372 340A158 LANDING GEAR INTRANSIT LIGHT DOES NOT ILLUMINATE DURING GEAR RETRACTION. REPLACED THE LAND GEAR CONTROL BOX. 2 L 7 2 4T RT A52EU 1996011900056 19960119 00056 EA 1996 1 19 COMA9660011 1 19960111 A 4900 38004882 APU CNDAIR CL600 CL6002B19 EA CABIN SMOKING A COMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 924CA 3539 820 7026 WHILE APU WAS OPERATING AND AC PACKS IN OPERATION, THE CABIN BEGAN TO FILL WITH SMOKE. SEVERAL SECONDS LATER THE APU AU TO-SHUTDOWN OCCURRED. 2 L 7 2 4F RT A21EA 1996011900057 19960119 00057 EA 1996 1 19 COMA9660012 1 19960111 A 5610 NP1393211 WINDSHIELD CNDAIR CL600 CL6002B19 EA LT COCKPIT CRACKED A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 940CA 7048 PILOTS WINDSHIELD CRACKED DURING TAXI. REPLACED PILOTS WINDSHIELD. 2 L 7 2 4F RT A21EA 1996011900059 19960119 00059 1996 1 19 MWEA96004 4 19960112 A 2565 13621225 EVAC SLIDE DOUG DC9 DC914 3022034 WP TAILCONE LOW PRESSURE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 DURING A-CHECK, FOUND TAIL EVAC SLIDE PRESSURE LOW. REPLACED TAIL EVAC SLIDE. 2 L 7 2 4F A6WE 1996011900060 19960119 00060 WP 1996 1 19 MWEA96005 1 19960114 A 2560 3952273501 GIRT BAR LATCH DOUG DC9 DC915 3022036 WP FWD ENTRY DOOR LACK OF LUBE A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 300ME 45718 CREW REPORTS, FWD ENTRY DOOR EVAC SLIDE GIRT BAR LATCH SPRING IS WEAK. CLEANED AND LUBED GIRT BAR LATCHES AND OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996011900061 19960119 00061 NM 1996 1 19 MWEA96006 1 19960114 A 2560 5956953503 SLIDE COVER DOUG MD88 MD88 3023688 NM FWD GALLEY DOOR LOOSE A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 701ME 49760 CREW REPORTS, FWD GALLEY DOOR SLIDE COVER IS LOOSE. RESECURED FWD GALLEY DOOR SLIDE COVER. 2 L 7 2 4F RT A6WE 1996011900062 19960119 00062 1996 1 19 SWAA960003 2 19960109 A 7200 ENGINE BOEING 737 737317 138447P NM NR 2 BIRD STRIKE A SWAA A UNSCHED LANDING C F.O.D. CL CLIMB 1 SW 07 693SW 23174 AFTER TAKEOFF, EXPERIENCED BIRD STRIKE TO NUMBER 2 ENGINE. AIRCRAFT RETURNED TO SMF AND MADE AN UNEVENTFUL LANDING. RE PLACED NUMBER 2 ENGINE PER PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996011900063 19960119 00063 NM 1996 1 19 SWAA960004 1 19960108 A 3230 BACR13CG2AB RELAY BOEING 737 7373H4 1384600 NM E/E COMPT FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 608SW 27928 AFTER TAKEOFF, UNABLE TO RAISE GEAR HANDLE. OVERRIDE TRIGGER WAS USED TO RAISE GEAR, CYCLED GEAR NORMALLY. AIRCRAFT RE TURNED TO MDW AND MADE AN UNEVENTFUL LANDING. REPLACED RELAY R276, CHECKED AIR SAFETY SENSOR, AND OPS CHECKED PER BOEIN G M/M. 2 L 7 2 4F RT A16WE 1996011900064 19960119 00064 NM 1996 1 19 SWAA960005 1 19960108 A 5320 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 1121 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 1121, BETWEEN S12 AND 13L. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996011900065 19960119 00065 NM 1996 1 19 SWAA960006 1 19960108 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 258/875-883 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 875 TO 883, BETWEEN S1 AND 2L, BETWEEN S1 AND 2R, AT BS 258, S21L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996011900066 19960119 00066 NM 1996 1 19 SWAA960007 1 19960108 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 1019, BS 340 BETWEEN S17 AND 18L, BS 256 BETWEEN S22 TO 23R A ND AT BS 310, S21R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996011900067 19960119 00067 NM 1996 1 19 SWAA960008 1 19960108 A 5312 BLKHD WEB BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178 BBL 0 WL 185. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996011900068 19960119 00068 NM 1996 1 19 SWAA960009 1 19960108 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND BULKHEAD CRACKED 2 PLACES AT BS 178, LBL 5 TO 12 AT WL 201 TO 205, LBL 5.7. REPAIRED PE R BOEING SRM. 2 L 7 2 4F RT A16WE 1996011900069 19960119 00069 NM 1996 1 19 SWAA960010 1 19960108 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 986 WL 208 RBL 5, 24, 32 AND 43. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996011900070 19960119 00070 NM 1996 1 19 SWAA960011 1 19960108 A 5320 STIFFENER BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 178 LBL 5 WL 184. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996011900071 19960119 00071 NM 1996 1 19 SWAA960012 1 19960108 A 5320 CHORD BOEING 737 7373H4 1384600 NM BS 1156 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND O/B CHORD CRACKED AT BS 1156 RBL 23 S4R. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996011900072 19960119 00072 NM 1996 1 19 SWAA960013 1 19960108 A 5320 SPLICE BOEING 737 7373H4 1384600 NM BS 360/907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE AND SHEAR TIE AT S15 CRACKED AT BS 360 AND BS 907 S4R. REPLACED PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1996011900073 19960119 00073 NM 1996 1 19 SWAA960014 1 19960108 A 5320 CLIP BOEING 737 7373H4 1384600 NM BS 787 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 787, S1L. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996011900074 19960119 00074 NM 1996 1 19 SWAA960015 1 19960108 A 5320 DOOR FRAME BOEING 737 7373H4 1384600 NM BS 492 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT BS 492 RBL 37 WL 161. REPAIRED PER TRAMCO EWO 95-0789. 2 L 7 2 4F RT A16WE 1996011900075 19960119 00075 NM 1996 1 19 UPS205187 1 19960101 A 5230 ANGLE BOEING 727 72730C 1384009 NM AFT CARGO DR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 917UP 19310 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED AFT CARGO DOOR NR 1 BEAM UPPER I/B L-ANGLE IS CRACKED 1 INCH ON FWD END IN RA DIUS. FABRICATED BEAM L-ANGLE IAW SRM 51-40-3, 52-30-1 AND INSTALLED REPAIR ANGLE IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996011900076 19960119 00076 WP 1996 1 19 RRXA960001 1 19960110 A 3230 47713921 ACTUATOR PIN DOUG DC8 DC871F 302199D WP LT MLG BROKEN A RRXA K NONE J WARNING INDICATION CL CLIMB 1 WP 15 500MH 16396 45812 KPIA-KDAY - FLT 525 - UPLATCH CHECK FAILED ON GEAR RETRACTION OUT OF KPIA. CYCLED GEAR NUMEROUS TIMES AND GEAR UNSAFE A ND GEAR DOOR WARNING LIGHTS ILLUMINATED, N500MH FERRIED TO KMCN. MAINTENANCE FOUND THE LT MLG RETRACT CYLINDER PIN BROK EN. MAINTENANCE INSPECTED THE BOSS AND PIN HOLE AND FOUND SERVICABLE. MAINTENANCE INSTALLED A NEW BOSS PIN IAW SB 32-1 02. THE LEFT HAND MLG OPERATED NORMALLY ON GEAR SWING IAW 32-10-1. 2 L 7 4 4F RT 4A25 1996011900077 19960119 00077 NM 1996 1 19 UPS405206 1 19960113 A 3350 LIGHT BOEING 747 747SR46 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 688UP 20784 MAINTENANCE REPORTED, EMERGENCY LIGHTS UNARMED, LIGHT INOP. RELAMPED, NO HELP. ADJUSTED SOCKET TO MAKE PROPER CONTACT, RELAMPED AND OPS CHECK GOOD. 2 L 7 4 4F A20WE 1996011900078 19960119 00078 EU 1996 1 19 WWMA9600003 1 19960111 A 3222 STRUT SAAB SF340 340B 7860101 EU NLG REQ'D SERVICE A WWMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 15 306AE 340B306 THE LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF, THE HANDLE WOULD NOT MOVE. THE AIRCRAFT RETURNED TO FIELD WITHOUT INC IDENT. MAINTENANCE REPACKED THE LANDING GEAR STRUT DUE TO A FLUID LEAK AND POSSIBLE IMPROPER REPACK OF THE GEAR FROM TH E PREVIOUS NIGHT. THE GEAR WAS SWUNG AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 1996011900137 19960119 00137 EU 1996 1 19 VTZA96059 1 19960103 A 7722 HTMAS6F2821SW CONNECTOR BAG JETSTM JETSTM3201 1500217 EU RT ENGINE DIRTY A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 493UE 7573 1266 805 IAD/WI - FLT 6181 - DURING TAKEOFF AT 0653 HOURS ON 1-3-96, ABORTED TAKEOFF DUE TO RT EGT FLUCTUATING PLUS OR MINUS 50 D EGREES ON THE TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 03523 IAW M EL 76-2 ON THE RT TTL. MAINTENANCE LATER CLEARED DMI NR 03523 ON 1-4-96 BY CLEANING THE RT ENGINE ZONE 2 CANNON PLUG. A IRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1996011900138 19960119 00138 EU 1996 1 19 VTZA96060 1 19960104 A 3260 ATG135022 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU RT MLG FAILED A VTZA A UNSCHED LANDING O N OTHER FALSE WARNING CL CLIMB 1 EA 27 303UE 41015 IAD/MHT - FLT 6207 - DURING CLIMB-OUT AT 2200 HOURS ON 1-4-96, RETURNED TO IAD DUE TO THE RT MLG INTRANSIT LIGHT REMAINI NG ILLUMINATED AFTER GEAR SELECTED UP. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED RT MAIN GEAR UPLOCK SWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1996011900177 19960119 00177 WP 1996 1 19 9600611154 1 19960102 A 5320 WEB DOUG DC10 DC1040 3023508 WP FS 1908-1921 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 154US 46763 DURING T-CHECK, FOUND CORROSION IN THE FLOOR WEB AND DOUBLER AT FS 1908 TO 1921 LBL 88. REPAIRED WEB (P/N AGA 3807-5) P ER EA 11-104450. 2 L 7 3 4F A22WE 1996011900178 19960119 00178 WP 1996 1 19 9600621154 1 19960102 A 5347 SEAT TRACK DOUG DC10 DC1040 3023508 WP FS 1878-1908 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 154US 46763 DURING T-CHECK, FOUND CORROSION IN THE MAIN CABIN SEAT TRACK FS 1878 TO 1908 AT LBL 100. REPAIRED TRACK (P/N AFA 7789-5 03) PER EA 11-104452. 2 L 7 3 4F A22WE 1996011900179 19960119 00179 WP 1996 1 19 9600639101 1 19960104 A 5347 SEAT TRACK DOUG DC9 DC915 3022036 WP FS 200-274 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 91S 47063 DURING H-CHECK, FOUND CORROSION ON THE RIGHT INBOARD SEAT TRACK FROM FS 200 TO 274. REPAIRED TRACK (P/N 5910143) PER EA 91-102023. 2 L 7 2 4F A6WE 1996011900180 19960119 00180 WP 1996 1 19 9600649101 1 19960104 A 5315 FLOORBEAM DOUG DC9 DC915 3022036 WP FS 786 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 91S 47063 DURING H-CHECK, FOUND CORROSION ON THE FS 786 FLOORBEAM UPPER SIDE. REPAIRED BEAM (P/N 9912243) PER EA 91-102634. 2 L 7 2 4F A6WE 1996011900181 19960119 00181 WP 1996 1 19 9600651154 1 19960105 A 5312 BULKHEAD DOUG DC10 DC1040 3023508 WP FS 1787 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 154US 46763 DURING T-CHECK, FOUND VERTICAL CRACKS IN A FS 1787 BULKHEAD STANCHION AT LBL 9, 10 INCHES ABOVE THE CARGO FLOOR LINE. R EPAIRED STANCHION PER EA 11-104463. 2 L 7 3 4F A22WE 1996011900182 19960119 00182 WP 1996 1 19 9600669302 1 19960105 A 5311 FRAME DOUG DC9 DC982 3022082 WP FS 237-446 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 302RC 48055 DURING H-CHECK, FOUND CORROSION ON THE FOLLOWING FUSELAGE FRAMES; FS 237 AT LONGERON 30, FS 332 AT LONGERON 30 AND FS 44 6 AT LONGERON 29R. REPAIRED ALL FRAMES (P/N 27777930-5) PER EA 93-103399. 2 L 7 2 4F A6WE 1996011900183 19960119 00183 WP 1996 1 19 9600679905 1 19960108 A 5330 SKIN DOUG DC9 DC931 3022065 WP FS 775 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 955N 47160 DURING A SPECIAL MAINTENANCE VISIT, FOUND CORROSION IN THE FUSELAGE SKIN AT FS 775 AT LONERON 18R. REPAIRED SKIN PER EA 99-104044. 2 L 7 2 4F A6WE 1996011900184 19960119 00184 WP 1996 1 19 9600681225 1 19960108 A 5320 FITTING DOUG DC10 DC1030 3023501 WP FS 1509-1521 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 225NW 46582 DURING T-CHECK, FOUND CORROSION ON THE CENTER GEAR WELL STRINGER FITTINGS AT LBL 21, 14, 7, BL 0, AND RBL 21 FROM BS 150 9 TO 1521. REPLACED STRINGER FITTINGS. 2 L 7 3 4F A22WE 1996011900185 19960119 00185 WP 1996 1 19 9600699601 1 19960109 A 5320 DOOR JAMB DOUG DC9 DC932 3022066 WP AFT CABIN DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 601NW 47038 DURING LINE CHECK, FOUND A CRACK IN THE AFT CABIN DOOR JAMB IN THE UPPER LEFT CORNER. REPAIRED JAMB (P/N 5917463-7) PER EA 96-103427. 2 L 7 2 4F A6WE 1996011900186 19960119 00186 WP 1996 1 19 9600709302 1 19960109 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FS 600-675 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 302RC 48055 DURING H-CHECK, FOUND CORROSION ON LONGERON 26L AT FS 600 TO 675. REPAIRED LONGERON (P/N 5936051-501) PER EA 93-103423. 2 L 7 2 4F A6WE 1996011900187 19960119 00187 WP 1996 1 19 9600711154 1 19960110 A 5330 SKIN DOUG DC10 DC1040 3023508 WP FS 1661-1681 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 154US 46763 DURING T-CHECK, FOUND CORROSION ON THE FUSELAGE SKIN FS 1661 TO 1681, LONGERONS 51L AND 51R BENEATH THE ANTI-COLLISION B EACON. REPAIRED SKIN (P/N NFA 6214) PER EA 11-99375. 2 L 7 3 4F A22WE 1996011900188 19960119 00188 WP 1996 1 19 9600721154 1 19960110 A 5313 LONGERON DOUG DC10 DC1040 3023508 WP FS 1401-1521 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 154US 46763 DURING T-CHECK, FOUND CORROSION ON LONGERONS 29R TO 31R BETWEEN FS 1401 TO 1521. REPAIRED LONGERONS PER EA 11-104451. 2 L 7 3 4F A22WE 1996011900189 19960119 00189 NM 1996 1 19 9600732298 1 19960110 A 5312 BULKHEAD BOEING 727 727251 138408H NM FS 1183 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 298US 22152 DURING PERIODIC CHECK, FOUND CORROSION ON THE BS 1183 BULKHEAD TO STRINGER 30 JACK PAD FITTING. REPLACED THE FITTING PE R SRM 51-10-1. 2 L 7 3 4F A3WE 1996011900190 19960119 00190 WP 1996 1 19 9600749870 1 19960111 A 5320 FITTING DOUG DC9 DC951 3022051 WP DOOR STOP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 779NC 48101 DURING H-CHECK, FOUND TWO CRACKS, 2 INCHES AND 2.25 INCHES IN THE AFT ENTRY DOOR UPPER LEFT AND RIGHT DOOR STOP FITTINGS . REPLACED FITTINGS PER EM 5270-01005 AND DWG J060229. 2 L 7 2 4F A6WE 1996011900191 19960119 00191 WP 1996 1 19 9600759605 1 19960111 A 5320 FITTING DOUG DC9 DC932 3022066 WP FS 370 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 605NW 47223 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A .5 INCH CRACK IN THE FORWARD CARGO FLOOR SUPPORT FITTING AT FS 370 , LONGERON 28L. REPLACED FITTING PER SRM 51-01. 2 L 7 2 4F A6WE 1996011900192 19960119 00192 WP 1996 1 19 9600769605 1 19960111 A 5320 FITTING DOUG DC9 DC932 3022066 WP FS 756-805 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 605NW 47223 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE LONGERON 30 END FITTING AT FS 756 TO 805. REPLACED FITTING PER SRM 51-01. 2 L 7 2 4F A6WE 1996011900193 19960119 00193 WP 1996 1 19 9600771154 1 19960112 A 5530 FITTING DOUG DC10 DC1040 3023508 WP VERT STAB CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 154US 46763 DURING T-CHECK, FOUND A CRACK IN THE NR 4 BANJO FITTING, FORWARD RIGHT FLANGE IN THE RADIUS. REPAIRED PER SRM 55-20-00, SHEETS 1-17. 2 L 7 3 4F A22WE 1996011900194 19960119 00194 NM 1996 1 19 9600786302 1 19960111 A 3350 LIGHT BOEING 747 747451 1384940 NM DOOR 5R INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 662US 23720 DURING LINE CHECK, THE DOOR 5R EMERGENCY SLIDE LIGHT WAS FOUND INOPERATIVE. REPLACED THE DOOR 5R SLIDE LIGHT ASSEMBLY A ND OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996011900195 19960119 00195 NM 1996 1 19 9600796302 1 19960112 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 662US 23720 DURING LINE CHECK, THE OVERHEAD EMERGENCY LIGHTS AT BOTH DOOR 2L AND 2R WERE FOUND INOPERATIVE. REPLACED EMERGENCY LIGH T BATTERY PACK AND CHARGE, OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996011900196 19960119 00196 NM 1996 1 19 9600806309 1 19960111 A 3350 POWER SUPPLY BOEING 747 747451 1384940 NM EXTERIOR INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 669US 24224 DURING LINE CHECK, THE AFT TWO EXTERIOR EMERGENCY LIGHTS LOCATED ON THE RIGHT WING TO BODY FAIRING WERE FOUND INOPERATIV E. REPLACED THE EXTERIOR EMERGENCY LIGHT POWER SUPPLY, OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996011900197 19960119 00197 WP 1996 1 19 9600819854 1 19960111 A 5350 RELEASE MECH DOUG DC9 DC951 3022051 WP TAILCONE MALFUNCTIONED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 763NC 47716 DURING LINE CHECK, FOUND THAT THE TAILCONE DID NOT RELEASE USING THE INTERIOR HANDLE. REPLACED CABLE 301A AND THE UPPER LEFT LATCH SPRING. RERIGGED THE RELEASE SYSTEM PER MM 53-50-3 PG 301 AND OPERATIONAL CHECKS OK. 2 L 7 2 4F A6WE 1996011900198 19960119 00198 WP 1996 1 19 9600829908 1 19960111 A 5350 RELEASE MECH DOUG DC9 DC931 3022065 WP TAILCONE MALFUNCTIONED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 958N 47254 DURING 'B' CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE HANDLE FROM THE CLIPS AND DROP THE TAILCONE. REPL ACED THE HANDLE AND CLIPS PER EO 5350-01049. 2 L 7 2 4F A6WE 1996011900199 19960119 00199 NM 1996 1 19 9600832703 1 19960112 A 3350 BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8878Z 21451 DURING PREFLIGHT, FOUND AFT AIRSTAIR EMERGENCY LIGHT INOPERATIVE. REPLACED THE BATTERY PACK AND CHECKED OK. 2 L 7 3 4F A3WE 1996011900200 19960119 00200 NM 1996 1 19 9600842289 1 19960114 A 3350 BATTERY PACK BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 289US 21377 DURING PREFLIGHT, FOUND THE RIGHT OVERWING MIDDLE EMERGENCY LIGHT INOPERATIVE. REPLACED THE BATTERY PACK AND CHECKED OK . 2 L 7 3 4F A3WE 1996011900201 19960119 00201 WP 1996 1 19 9600859756 1 19960113 A 3010 PRESS SWITCH DOUG DC9 DC941 302207N WP ANTI-ICE MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 GL 01 756NW 47180 EN ROUTE DTW-YHZ, AIRFOIL ICE PROTECTION PRESSURE ABNORMAL LIGHT REMAINED ON DURING WING ANTI-ICE OPERATION. FLIGHT RET URNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED THE TAIL ANTI-ICE VALVE, NO HELP. REPLACED THE PRESSURE SWITCH AND OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996011900202 19960119 00202 WP 1996 1 19 9600869755 1 19960113 A 3260 GEAR LIGHT DOUG DC9 DC941 302207N WP NLG MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 755NW 47179 NOSE LANDING GEAR RED UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDEN T. INSPECTED AND CYCLED NOSE GEAR. OPERATIONAL CHECK WAS NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996011900203 19960119 00203 WP 1996 1 19 9600879861 1 19960112 A 3520 90000200712 REGULATOR DOUG DC9 DC951 3022051 WP PASS OXY SYST MALFUNCTIONED A NWAA G O2 MASK DEPLOYED J WARNING INDICATION UK UNKNOWN 1 GL 01 770NC 47758 DURING CHECK OF PASSENGER OXYGEN SYSTEM IN MANUAL POSITION, PRESSURE ROSE TO 60 PSI AND OXYGEN MASKS WERE DEPLOYED THROU GHOUT THE CABIN. REPLACED THE PASSENGER OXYGEN BOTTLE AND REGULATOR, RE-STOWED ALL MASKS. OPERATIONAL CHECK NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996011900204 19960119 00204 WP 1996 1 19 9600889101 1 19960113 A 3350 6011779 BATTERY PACK DOUG DC9 DC915 3022036 WP LT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 91S 47063 DURING LINE MAINTENANCE INSPECTION, FOUND THE LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED THE BATTERY PACK AND O PERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996011900205 19960119 00205 NE 1996 1 19 9600891160 2 19960112 A 7230 COMPRESSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 1 ENGINE STALLED A NWAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS LD LANDING 1 GL 01 168US 46769 86185 DURING LANDING WITH REVERSER DEPLOYED, THE NR 1 ENGINE EXPERIENCED A REVERSE STALL. EGT WENT TO 950 DEGREES AND THE ENG INE WAS SHUTDOWN. PERFORMED INSPECTION ON THE INLET AND EXHAUST, INSPECTION WAS NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A22WE E20EA 1996011900206 19960119 00206 WP 1996 1 19 9600909902 1 19960111 A 7711 EPR INDICATOR DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9 52048 NE NR 2 MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 952N 47073 666305 NR 2 EPR INDICATION WAS BELOW TARGET WITH THE POWER LEVER AGAINST THE FORWARD STOPS. THE TAKEOFF WAS ABORTED AND THE AI RCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE EPR INDICATOR WITH A SERVICEABLE UNIT. 2 L 7 2 4F 4 F A6WE E2EA 1996011900207 19960119 00207 WP 1996 1 19 9600919943 1 19960114 A 3350 LIGHT DOUG DC9 DC931 3022065 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 1308T 47615 DURING LINE CHECK, FOUND EMERGENCY LIGHT EXIT SIGN BROKEN AT AFT EXIT DOOR. REPLACED THE LIGHT ASSEMBLY. 2 L 7 2 4F A6WE 1996011900208 19960119 00208 WP 1996 1 19 9600929975 1 19960112 A 3260 SWITCH DOUG DC9 DC931 3022065 WP LT MLG FAILED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 9339 47382 DURING APPROACH, THE LEFT MAIN LANDING GEAR GREEN SAFE LIGHT DID NOT ILLUMINATE AFTER LANDING GEAR EXTENSION. RECYCLED LANDING GEAR AND LIGHT ILLUMINATED. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE LEFT MAIN LANDING GEAR DOWN LIMIT S WITCH AND CANNON PLUG, OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996011900209 19960119 00209 1996 1 19 9600939613 4 19960113 A 3418 9650041027 COMPUTER DOUG DC9 DC932 3022066 WP E/E COMPT FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 613NW 1456 539 47438 DURING CLIMB, THE STALL INDICATION FAILURE LIGHT ILLUMINATED. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. RE PLACED THE STALL WARNING COMPUTER AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996011900210 19960119 00210 WP 1996 1 19 9600949935 1 19960112 A 3222 STRUT DOUG DC9 DC931 3022065 WP NLG REQ'D SERVICE A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 1332U 47404 DURING CLIMB, THE AIRCRAFT DID NOT SHIFT INTO FLIGHT MODE AFTER LANDING GEAR RETRACTION. PULLED CIRCUIT BREAKERS TO PUT AIRCRAFT INTO FLIGHT MODE. AIRCRAFT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. SERVICED NOSE STRUT AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996011900211 19960119 00211 NE 1996 1 19 9600959902 2 19960114 A 7321 FUEL CONTROL DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7B 52053 NE NR 2 ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 952N 47073 666305 NR 2 ENGINE EPR INDICATION FAILED TO REACH TARGET ON TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO MAIN TENANCE. THE FUEL CONTROL ASSEMBLY AND THE PT2 PROBE AND NOSE DOME ASSEMBLY WERE REPLACED. THE AIRCRAFT RETURNED TO SE RVICE. 2 L 7 2 4F 4 F A6WE E2EA 1996011900212 19960119 00212 WP 1996 1 19 9600969902 1 19960112 A 7711 EPR IND DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7B 52053 NE NR 2 ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 952N 47073 666305 NR 2 ENGINE EPR INDICATION FAILED TO REACH TARGET ON TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE EPR TRANSMITTER, INDICATOR AND A CRACKED FITTING IN THE PT7 SYSTEM. IN ADDITION, THE EN GINE WAS FIELD TRIMMED PER PWA'S JT8D MAINTENANCE MANUAL. 2 L 7 2 4F 4 F A6WE E2EA 1996011900213 19960119 00213 NE 1996 1 19 9600979852 2 19960110 A 7200 ENGINE DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE NR 2 FAILED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 GL 01 761NC 47116 688802 NR 2 ENGINE FAILED ON CLIMBOUT. THE ENGINE WAS SHUTDOWN AND THE FLIGHT RETURNED MAKING AN UNEVENTFUL OVERWEIGHT LANDING IN DTW. MAINTENANCE REPLACED THE ENGINE WITH A SERVICEABLE UNIT. 2 L 7 2 4F 4 F A6WE E2EA 1996011900214 19960119 00214 WP 1996 1 19 9600989977 1 19960115 A 3350 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9341 47390 DURING LINE CHECK, FOUND CEILING EMERGENCY LIGHTS INOPERATIVE FROM ROWS 5 TO 12. REPLACED THE BATTERIES AND OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996011900215 19960119 00215 NM 1996 1 19 96FDEA00040 1 19960112 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 488FE 21491 CORROSION (C53-224-01), ON STR FLANGE AT BS 720 STR 4L. REMOVED DAMAGED SECTION OF STR, FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 53-10-3. 2 L 7 3 4F A3WE 1996011900216 19960119 00216 NM 1996 1 19 96FDEA00058 1 19960112 A 5347 SEAT TRACK BOEING 727 727227 1384078 NM BS 804-848 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 487FE 21490 UPPER LOBE FLOOR, OVER WING AREA CORR ON O/B FLANGE FLOOR TRACK LBL 45 STA 804 TO 848 LT. INSTALLED NEW SEAT TRACK AND CHORD PER SRM 51-10-1. INSTALLATION OF FLOATING SEAT TRACK FROM STA 740 TO 760 COVERED ON NR 1415 LBL 45. 2 L 7 3 4F A3WE 1996011900217 19960119 00217 SO 1996 1 19 COMA9610020 1 19960115 A 5270 DOOR WARNING EMB 120 EMB120RT SO CARGO COMPT MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 248CA 120228 CARGO DOOR WARNING SHORTLY AFTER TAKEOFF. PLACED CARGO DOOR WARNING SYSTEM ON DEFERRED MAINTENANCE LIST AND ACFT CONTIN UED SERVICE. 2 L 7 2 4T RT A31SO 1996011900218 19960119 00218 SO 1996 1 19 COMA9610021 1 19960115 A 3150 CIRCUIT BREAKER EMB 120 EMB120RT SO AURAL WARNING TRIPPED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 161CA 120143 TAKEOFF TRIM WARNING DURING TAKEOFF ROLL. FOUND THE AURAL WARNING CIRCUIT BREAKER TRIPPED. RESET BREAKER AND ACFT CONT INUED SERVICE. 2 L 7 2 4T RT A31SO 1996011900219 19960119 00219 SO 1996 1 19 COMA9610022 1 19960114 A 2431 40769 BATTERY EMB 120 EMB120RT SO FUSELAGE FALSE WARNING A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 196CA 8101 301 120196 BATTERY AURAL WARNING SOUNDED AFTER TAKEOFF. BATTERY TEMP GAUGE INDICATED NORMAL. REPLACED THE BATTERY. 2 L 7 2 4T RT A31SO 1996011900220 19960119 00220 SO 1996 1 19 COMA9610023 1 19960112 A 7603 CIRCUIT BREAKERS EMB 120 EMB120RT SO POWER LEVERS TRIPPED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 1110J 120110 THE LT AND RT POWER LEVER FLIGHT IDLE STOP SOLENOIDS CIRCUIT BREAKERS WERE TRIPPED. RESET CIRCUIT BREAKERS AND SYSTEM T EST NORMAL. 2 L 7 2 4T RT A31SO 1996011900221 19960119 00221 SO 1996 1 19 COMA9610024 1 19960111 A 3246 118143 BEARING COVER EMB 120 EMB120RT SO LT MLG MISSING A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 269CA 110 120263 RT ANTI-SKID INOP WARNING DURING TAKEOFF ROLL. REPLACED MISSING BEARING COVER ON LT MLG WHEEL. 2 L 7 2 4T RT A31SO 1996011900222 19960119 00222 EU 1996 1 19 COMA9630015 1 19960115 A 3246 5009237 INNER RACE LORAL 5010488 SAAB SF340 SF340A 7850100 EU RT MLG SPUN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 158CA 11714 527 JAN920214 340A158 MECHANIC REMOVED WHEEL FROM A/C DUE TO TIRE WORN TO LIMITS. DURING VISUAL INSPECTION FOUND INNER RACE SPUN. SUBASSY HA S BEEN REMOVED FROM SERVICE AND SENT TO ABS. 2 L 7 2 4T RT A52EU 1996011900223 19960119 00223 EA 1996 1 19 COMA9660013 1 19960114 A 3260 DISAGREE MESSAGE CNDAIR CL600 CL6002B19 EA NLG ACTIVATED A COMA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 01 948CA 7079 NOSE LANDING GEAR DISAGREE MESSAGE, WHEN GEAR SELECTED DOWN. COULD NOT DUPLICATE AND NO FAULTS FOUND WITH NLG. 2 L 7 2 4F RT A21EA 1996011900224 19960119 00224 EA 1996 1 19 COMA9660014 1 19960115 A 2120 601R952111 DUCT CNDAIR CL600 CL6002B19 EA AFT EQUIP BAY FAILED A COMA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 01 949CA 7080 AT 31,000 FEET CABIN STARTED DEPRESSURIZING RAPIDLY. FOUND AIR CONDITIONING DUCT SEPARATED FROM THE WATER SEPARATOR. R EPLACED DUCT. 2 L 7 2 4F RT A21EA 1996011900225 19960119 00225 WP 1996 1 19 MWEA95010 1 19960110 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 1076 CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 DURING C-CHECK, FOUND FRAME AT STA 1076 LONGERON 20R IS CHAFED FROM LOOSE STANDOFF BRACKET. INSTALLED DOUBLER REPAIR IA W SRM 53-03 FIG 4. 2 L 7 2 4F A6WE 1996011900226 19960119 00226 WP 1996 1 19 MWEA96009 1 19960110 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 389/408 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 DURING C-CHECK, FOUND FWD CARGO BIN FLOORBEAMS DAMAGED FROM CARGO DOOR AT STA 389 AND 408. INSTALLED ANGLE REPAIR IAW S RM 53-05 PG 289. 2 L 7 2 4F A6WE 1996011900227 19960119 00227 WP 1996 1 19 MWEA96011 1 19960113 A 5320 991556133 DOUBLER DOUG DC9 DC932 3022066 WP BS 996 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 DURING C-CHECK, FOUND JACKPAD DOUBLER INSIDE AFT CARGO BIN AT STA 996 CORRODED BEYOND LIMITS. INSTALLED NEW DOUGLAS PAR T IAW SRM 53-01 PG 1 AND 2. 2 L 7 2 4F A6WE 1996011900228 19960119 00228 WP 1996 1 19 MWEA96012 1 19960116 A 3350 6011775 BATTERY PACK DOUG DC9 DC932 3022066 WP LT NACELLE DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 602ME 48133 DURING C-CHECK, FOUND LEFT EMERGENCY NACELLE LIGHT INOP. REPLACED NACELLE LIGHT BATTERY PACK AND OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996011900229 19960119 00229 NM 1996 1 19 SWAA960016 1 19960112 A 5260 T-STRIP BOEING 737 7372H4 138448C NM AIRSTAIR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 51SW 21448 DURING SCHEDULED MAINT CHECK, FOUND T-STRIP CRACKED ABOVE FWD UPPER AIRSTAIR DOORWAY STOP IN SEVERAL PLACES. REPAIRED T -STRIP PER BOEING SRM. 2 L 7 2 4F A16WE 1996011900230 19960119 00230 NM 1996 1 19 SWAA960017 1 19960114 A 5230 FRAME BOEING 737 7375H4 138449D NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 DURING SCHEDULED MAINT CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT FWD LOWER AFT DOOR STOP. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996011900231 19960119 00231 NM 1996 1 19 SWAA960018 1 19960114 A 5320 PANEL BOEING 737 7373H4 1384600 NM NLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED MAINT CHECK, FOUND WHEEL WELL LOWER FIXED PANEL BELOW KEEL BEAM CRACKED 1 INCH ON RIGHT SIDE ACROSS FRO M PREVIOUS REPAIR. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996011900232 19960119 00232 NM 1996 1 19 SWAA960019 1 19960114 A 5240 SKIN BOEING 737 7372T4 1384492 NM SERVICE DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED MAINT CHECK, FOUND FWD SERVICE DOOR LOWER HINGE CUTOUT CRACKED AT PREVIOUS REPAIR. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996011900233 19960119 00233 NM 1996 1 19 SWAA960020 1 19960114 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 772 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED MAINT CHECK, FOUND FLOORBEAM CORROSION AT BS 772 LBL 12.25 RBL 3, RBL 7.5, RBL 8.25 AND RBL 13.25. REP AIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996011900234 19960119 00234 NM 1996 1 19 SWAA960021 1 19960114 A 5315 FLOORBEAM BOEING 737 7372T4 1384492 NM BS 986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED MAINT CHECK, FOUND AFT GALLEY FLOORBEAM CORRODED AROUND FASTENER HOLE AT BS 986.5 RBL 4. REPAIRED PER SWA RA 1-253-1420. 2 L 7 2 4F A16WE 1996011900235 19960119 00235 NM 1996 1 19 SWAA960022 1 19960114 A 5315 FLOORBEAM BOEING 737 7372T4 1384492 NM BS 986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED MAINT CHECK, FOUND AFT GALLEY FLOORBEAM CORRODED AROUND FASTENER HOLE AT BS 986.5 LBL 10. REPAIRED PER SWA RA 1-253-1419. 2 L 7 2 4F A16WE 1996011900236 19960119 00236 NM 1996 1 19 SWAA960023 1 19960114 A 5315 FLOORBEAM BOEING 737 7372T4 1384492 NM BS 1006 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED MAINT CHECK, FOUND AFT GALLEY FLOORBEAM CORRODED AROUND FASTENER HOLE AT BS 1006 AFT FLANGE, LBL 15 TO 28. REPAIRED PER SWA RA 1-253-1417. 2 L 7 2 4F A16WE 1996011900237 19960119 00237 NM 1996 1 19 SWAA960024 1 19960114 A 5315 FLOORBEAM BOEING 737 7372T4 1384492 NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED MAINT CHECK, FOUND AFT GALLEY FLOORBEAM CORROSION AROUND FASTENER HOLE AND MIGRATING UNDER WEB AT BS 10 16, FWD FLANGE LBL 0 TO 39. REPAIRED PER SWA RA 1-253-1415. 2 L 7 2 4F A16WE 1996011900238 19960119 00238 NM 1996 1 19 SWAA960025 1 19960114 A 5347 SEAT TRACK BOEING 737 7372T4 1384492 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED MAINT CHECK, FOUND CABIN SEAT TRACK CRACKED AT SCREW HOLE. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996011900239 19960119 00239 NM 1996 1 19 SWAA960026 1 19960114 A 5315 FLOORBEAM BOEING 737 7372T4 1384492 NM BS 294 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED MAINT CHECK, FOUND FWD GALLEY FLOORBEAM CORROSION UPPER TEE CAP FASTENER BS 294 LBL 11. REPAIRED PER B OEING SRM. 2 L 7 2 4F A16WE 1996011900240 19960119 00240 NM 1996 1 19 SWAA960027 1 19960114 A 5320 BRACKET BOEING 737 7372T4 1384492 NM BS 294 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED MAINT CHECK, FOUND FWD ENTRY DOOR WEB TO FRAME ATTACH BRACKET CRACKED AT BS 294 S11L. REPAIRED PER BOE ING SRM. 2 L 7 2 4F A16WE 1996011900241 19960119 00241 NM 1996 1 19 SWAA960028 1 19960114 A 5330 SKIN BOEING 737 7372T4 1384492 NM BS 910 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED MAINT CHECK, FOUND FUSELAGE SKIN LAP CORRODED AT BS 910 S27L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996011900242 19960119 00242 NM 1996 1 19 SWAA960029 1 19960114 A 5230 SKIN BOEING 737 7372T4 1384492 NM AFT CARGO DOOR DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED MAINT CHECK, FOUND AFT CARGO DOOR WEB DAMAGED AT CUTOUT LOWER AFT SIDE. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996011900243 19960119 00243 WP 1996 1 19 UPS805216 1 19960113 A 5320 FITTING DOUG DC8 DC871 302199A WP AFT BLKHD CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 WHILE IN FOR B-CHECK, FOUND FITTING ON STRINGER 32R AT AFT BULKHEAD OF AIRCON COMP IS CORRODED. REMOVED AND REPLACED FI TTING. 2 L 7 4 4F 4A25 1996011900244 19960119 00244 EU 1996 1 19 WWMA9600004 1 19960113 A 2611 SMOKE LIGHT SAAB SF340 340B 7860101 EU CARGO COMPT ILLUMINATED A WWMA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 15 320AE 340B320 THE CARGO SMOKE LIGHT ILLUMINATED AND THE CREW DISCHARGED THE NR 1 FIRE BOTTLE. THE AIRCRAFT DIVERTED TO MLU AND LANDED WITHOUT INCIDENT. UPON INVESTIGATION MAINTENANCE FOUND NO EVIDENCE OF FIRE OR SMOKE. THE DETECTOR OPTIC SENSORS WERE CLEANED AND THE CARGO FIRE EXTINGUISHER SYSTEM WAS DEFERED IAW MEL 26-4. THE AIRCAFT WAS RETURNED TO SERVICE, THE FIRE BOTTLE WAS REPLACED AND THE MEL WAS CLEARED AT THE EARLIEST OPPORTUNITY. 2 L 7 2 4T RT A52EU 1996011900245 19960119 00245 EU 1996 1 19 WWMA9600005 1 19960114 A 2611 SMOKE LIGHT SAAB SF340 340B 7860101 EU CARGO COMPT ILLUMINATED A WWMA O OTHER N FALSE WARNING IN INSP/MAINT 1 WP 15 320AE 340B320 THE CARGO SMOKE LIGHT ILLUMINATED WHILE THE FLIGHT CREW WAS PREFLIGHTING THE AIRCRAFT. MAINTENANCE FOUND NO INDICATION OF SMOKE OR FIRE. THE DETECTOR ELECTRICAL CONNECTORS WERE DISCONNECTED AND THE SMOKE LIGHT STAYED ON. THE CONNECTORS W ERE RECONNECTED AND THE WEU WAS RERACKED. ALL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED. 2 L 7 2 4T RT A52EU 1996011900310 19960119 00310 WP 1996 1 19 9600999969 1 19960116 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9333 47246 DURING LINE CHECK, FOUND COCKPIT AND FORWARD ENTRANCE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND OPERATION AL CHECK GOOD. 2 L 7 2 4F A6WE 1996011900311 19960119 00311 WP 1996 1 19 9601009937 1 19960116 A 3350 LIGHT DOUG DC9 DC931 3022065 WP TAIL COMPT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 908H 47517 DURING LINE CHECK, AFT LEFT EMERGENCY LIGHT INOPERATIVE IN TAIL COMPARTMENT. REPOSITIONED LIGHT AND OPERATIONAL CHECK G OOD. 2 L 7 2 4F A6WE 1996011900312 19960119 00312 WP 1996 1 19 9601019945 1 19960116 A 3010 PRESS REG VLV DOUG DC9 DC931 3022065 WP AIRFOIL DE-ICE MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 GL 01 8925E 45840 DURING FLIGHT, THE AIRFOIL ICE PROTECTION PRESSURE ABNORMAL LIGHT ILLUMINATED DURING WING ANTI-ICE. FOLLOWED COCKPIT OP ERATING MANUAL PROCEDURES AND LIGHT REMAINED ILLUMINATED. AIRCRAFT DIVERTED TO CLE AND LANDED WITHOUT INCIDENT. REPLACE D ICE PROTECTION PRESSURE REGULATOR VALVE, OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996011900313 19960119 00313 WP 1996 1 19 9601029933 1 19960116 A 3222 STRUT DOUG DC9 DC931 3022065 WP NLG REQD SERVICE A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 1334U 47280 DURING CLIMB, THE NOSE LANDING GEAR WOULD NOT RETRACT AND THE AIRCRAFT DID NOT SHIFT INTO FLIGHT MODE. AIRCRAFT RETURNE D TO YUL AND LANDED WITHOUT INCIDENT. SERVICED NOSE LANDING GEAR STRUT AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996011900315 19960119 00315 NM 1996 1 19 96FDEA00060 1 19960117 A 5753 SKIN BOEING 727 72722 1384002 NM RT TE FOREFLAP GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 THERE'S A GOUGE ON THE RT WING FOREFLAP UPPER SURFACE ABOVE THE NR 8 FLAP TRACK. REMOVED AND REPLACED DAMAGE ON O/B RT WING FOREFLAP IAW FEDEX SRM 51-40-6. 2 L 7 3 4F A3WE 1996011900316 19960119 00316 NM 1996 1 19 96FDEA00061 1 19960117 A 5311 FRAME BOEING 727 727233 138408A NM BS 720 GOUGE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 GOUGE IN FRAME AT BS 720B LT BETWEEN STR NR 14 TO NR 15, WAS FOUND TO BE OUT OF LIMITS PER FEDEX SRM 51-40-3. REMOVED A ND REPLACED FABRICATED DOUBLER AND INSTALLED PER SRM 51-40-3. 2 L 7 3 4F RT A3WE 1996011900317 19960119 00317 NM 1996 1 19 96FDEA00062 1 19960117 A 5311 FRAME BOEING 727 727233 138408A NM BS 600 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 DENTS IN FRAME BS 600 LBL 34 TO 46 WL 160. REPAIRED DENTS IN FRAME BS 600 LBL 34 TO 46 WL 160 PER FEDEX SRM 51-40-3. 2 L 7 3 4F RT A3WE 1996011900318 19960119 00318 NM 1996 1 19 96FDEA00063 1 19960116 A 5311 FRAME BOEING 727 727233 138408A NM BS 660 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 DENTS IN FRAME BS 660 LBL 34 TO 46 WL 160. REPAIRED DENTED FRAME BS 660 LBL 34 TO 46 WL 160 IAW FEDEX SRM 51-40-3. 2 L 7 3 4F RT A3WE 1996011900319 19960119 00319 WP 1996 1 19 96UAL900031 1 19960115 A 3350 CIRCUIT BREAKER DOUG DC10 DC1030 3023501 WP COCKPIT DEFECTIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1859U 47819 EMERGENCY LIGHTS FLASH ON, THEN OFF INTERMITTENTLY WITH COCKPIT SWITCH IN THE ARMED POSITION. ALL BUSES POWERED. REPLA CED EMERGENCY LIGHTS CONTROL CIRCUIT BREAKER DUE TO DEFECT. 2 L 7 3 4F A22WE 1996011900320 19960119 00320 NM 1996 1 19 96UAL900032 1 19960115 A 3350 BATTERY PACK BOEING 727 727222 1384073 NM CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7444U 21898 EMERGENCY LIGHT JUST FORWARD OF FORWARD GALLEY ON THE CEILING OVER THE AISLE IS INOPERATIVE. REPLACED WEAK BATTERY PACK . 2 L 7 3 4F A3WE 1996011900321 19960119 00321 NM 1996 1 19 96UAL900033 1 19960115 A 3350 LIGHT STRIP BOEING 757 757222 1384956 NM CABIN DISCONNECTED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 563UA 26665 EMERGENCY LIGHT STRIP INOP AT 13A. DISCOVERED EMERGENCY LIGHT STRIP DISCONNECTED. RECONNECTED, TESTS NORMAL. 2 L 7 2 4F RT A2NM 1996011900322 19960119 00322 NE 1996 1 19 96UAL900037 2 19960116 A 7321 MEC BOEING 737 737322 1384676 NM GE CFM56 CFM563B1 13802 NE NR 1 ENGINE MALFUNCTIONED A UALA K NONE O OTHER CL CLIMB 1 WP 29 365UA 24534 722317 NUMBER ONE ENGINE SURGED DURING CLIMB, N1 WENT FROM A TARGET OF 92 PERCENT TO 94.3 PERCENT. ALSO, HAD A 1,000 POUND INC REASE IN FUEL FLOW, THROTTLE WAS RETARDED AND ENGINE SURGED TWO MORE TIMES BEFORE IT STABILIZED. ENGINE SURGING WAS CAU SED BY AN INTERMITTENT FAILURE OF THE MAIN ENGINE CONTROL ROTARY VARIABLE DIFFERENTIAL TRANSDUCER. THE MAIN ENGINE CONT ROL WAS REPLACED AND CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1996011900328 19960119 00328 WP 1996 1 19 ABXA9600026 1 19960111 A 5347 291491311M SEAT TRACK DOUG DC9 DC932 3022066 WP FS 783/872 FAILED A ABXA K NONE O OTHER TO TAKEOFF 1 GL 23 901AX 47426 DURING TAKEOFF ROLL, FS 694 SEAT TRACK FAILED PUSHING THE 'C' CONTAINER LOCK OUT OF THE SEAT TRACK. TWO BALLAST PALLETS AND ONE 'C' CONTAINER. TORE THE SEAT TRACK LOCKS FROM THE SEAT TRACKS AT FS 783 AND 872, WHICH WERE IN LOCKING POSITIO N. THE RIGHT PYLON BULKHEAD ABSORBED THE IMPACT, CONTAINERS CAME TO REST AT FS 965. THE CREW SECURED THE FREIGHT AND T HE FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. INSPECTED PER REA D953-14079. REPAIRED PER REA D953-14153, D953-14159, D 953-14079 AND THE DC-9 SRM. REFERENCE WORK ORDER NR DMG 454. REA'S D925-14089 THROUGH 14152 WERE ISSUED TO THE DC-9 FL EET TO PROVIDE INCREASED SUPPORT. 2 L 7 2 4F A6WE 1996011900329 19960119 00329 WP 1996 1 19 ABXA9600027 1 19960115 A 3260 7000010101 DNLOCK SW DOUG DC9 DC932 3022066 WP NLG DEFECTIVE A ABXA K NONE P NO WARNING INDICATION CR CRUISE 1 GL 23 900AX 47380 ON GEAR EXTENSION, NOSE WHEEL GREEN LIGHT DID NOT ILLUMINATE. RECYCLED GEAR, NORMAL INDICATIONS. REPLACED NOSE LANDING GEAR DOWN LOCK SWITCH IAW DC-9 MM 32-60-0. 2 L 7 2 4F A6WE 1996011900330 19960119 00330 WP 1996 1 19 ABXA9600028 1 19960116 A 3260 80801 UPLOCK SW DOUG DC9 DC941 302207N WP MLG DEFECTIVE A ABXA K NONE N FALSE WARNING TO TAKEOFF 1 GL 23 952AX 47615 LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER TAKEOFF. RECYCLED GEAR, LIGHT WENT OUT AFTER TWO MINUTES, THEN ILLUMI NATED BRIEFLY AGAIN. REPLACED LEFT MAIN LANDING GEAR UPLOCK SWITCH IAW DC-9 SUPPLEMENTIAL MM 32-60-1. 2 L 7 2 4F A6WE 1996011900331 19960119 00331 WP 1996 1 19 ABXA9600029 1 19960115 A 7603 406175 BOLT DOUG DC8 DC863 302198A WP PWA JT3D JT3D7 52039 NE NR 3 ENGINE LOOSE A ABXA E ENGINE SHUTDOWN O OTHER CL CLIMB 1 GL 23 823AX 46122 669769 DURING CLIMB, NR 3 ENGINE COULD NOT BE CONTROLLED WITH THROTTLE INPUTS. ENGINE REMAINED AT MAX CONTINUOUS THRUST WITH T HE THROTTLE LEVER PULLED BACK TO IDLE. ENGINE WAS SHUTDOWN AND MAINTAINED A POSITIVE OIL PRESSURE DURING SHUTDOWN PROCE DURES. SECURED AND SAFETIED THE NR 3 ENGINE POWER LEVER LINKAGE AT THE FCU INPUT CLEVIS. GROUND RAN ENGINE, ALL CONTRO LS AND PARAMETERS CHECKED GOOD. 2 L 7 4 4F 4 F 4A25 1E8 1996011900332 19960119 00332 NE 1996 1 19 ABXA9600030 2 19960114 A 7230 739201ABX7 C1 DISK DOUG DC8 DC863 302198A WP PWA JT3D JT3D7 52039 NE NR 2 ENGINE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 823AX 46122 671397 DURING COMPLIANCE OF AD 80-12-51, PRATT AND WHITNEY SB 5136, FOUND CRACK INDICATIONS IN C-1 DISK, FIRST STAGE FAN BLADES . REPLACED C-1 DISK, FIRST STAGE FAN BLADES IAW ABX TEST AND MAINTENANCE RECORD WORK SHEETS, BS374A, BS375A, BS376A AND BS377A. 2 L 7 4 4F 4 F 4A25 1E8 1996011900336 19960119 00336 SO 1996 1 19 BIER960030 1 19960117 A 3297 WIRE PIPER PA31 PA31350 7103110 SO LANDING GEAR BROKEN B BIEA O OTHER J WARNING INDICATION CL CLIMB 1 EA 21 27508 317852031 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. INVESTIGATION REVEALED BROKEN WIRE GOING TO LEFT GEAR SAFETY SWITCH THERE BY NOT ALLOWING ANTI-RETRACT SOLENOID FROM WORKING. 1 L 7 2 3O A20SO 1996011900337 19960119 00337 NM 1996 1 19 DL72E960069 1 19960111 A 2130 39608831 VALVE BOEING 727 727247 138408F NM RIGHT MALFUNCTIONED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 282WA 21484 ON CLIMBOUT THROUGH 29,000 FT, THE CABIN CONTINUED TO CLIMB THROUGH THE PRESET 4,800 CABIN ALITITUDE. DESENCED TO 18,00 0 WHERE THE CABIN STABLIZED AT 10,000. PACK BLEEDS AND OUTFLOW APPEARED OK. REPLACED RT FLOW CONTROL VALVE, LEAK CKS G OOD. PRESSURIZED A/C TO 7 PSI DIFF, ALL SYS NORMAL. 2 L 7 3 4F A3WE 1996011900340 19960119 00340 NM 1996 1 19 DL72E960086 1 19960114 A 5754 651622296 RIB BOEING 727 727247 138408F NM NR 6 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2829W 21481 SLAT NR 6, RIB NR 10 AND 12 CRACKED. REPAIRED PER M/M 57-54-0 FIG 814. 2 L 7 3 4F A3WE 1996011900341 19960119 00341 1996 1 19 DL72L960059 4 19960109 A 2565 SLIDE 146110015 BOEING 727 727232 1384082 NM R1 DOOR LOW PRESSURE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 503DA 1992 21305 DURING INSPECTION, R-1 DOOR SLIDE PRESSURE FOUND LOW 500 LBS. REPLACED SLIDE. 2 L 7 3 4F A3WE 1996011900342 19960119 00342 NM 1996 1 19 DL72S960054 1 19960109 A 5751 657273434 SKIN BOEING 727 727232 1384082 NM AILERON DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 408DA 21152 DURING SHOP INSPECTION, AILERON PANEL UPPER SKIN WAS FOUND DENTED. SPLICED UPPER SKIN PER SRM 57-53-5 FIG 3. 2 L 7 3 4F A3WE 1996011900344 19960119 00344 NM 1996 1 19 DL72S960068 1 19960105 A 5311 FRAME BOEING 727 727232 1384082 NM BS 1110 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 495DA 21075 AT MID VISIT 2, FOUND FRAME CRACKED AT STA 1110 ABOVE STR 27L. REMOVED LT FIXED FLOOR PNL FROM 1070 TO 1130 FOR ACCESS. CUT OUT DAMAGE PER SRM 53-10-4 FIG 27 AND INSTALLED REPAIR PER SRM 53-10-4 FIG 27. 2 L 7 3 4F A3WE 1996011900345 19960119 00345 NM 1996 1 19 DL72S960081 1 19960112 A 2780 BRACKET BOEING 727 727232 1384082 NM NR 2 LE FLAP ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 525DA 21585 SETUP TO INSPECT THE ATTACH BRACKET FOR THE NR 2 LEADING EDGE FLAP ACTUATOR FOR CONDITION. FOUND ATTACH BRACKET CRACKE D AND REPAIRED PER MM 27-81-22. 2 L 7 3 4F A3WE 1996011900346 19960119 00346 NM 1996 1 19 DL72S960093 1 19960115 A 3350 BATTERY PACK 900835A BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 522DA 21582 AFT DOORS SLIDE EMERGENCY LTS INOP. ALSO, FWD CABIN AISLE EXIT SIGN EMERGENCY LIGHT INOP. FWD ENTRY EMERGENCY SLIDE LI GHT INOP. REPLACED BATTERY PACK AT M983, M1085 AND OPN NORMAL. REPLACED L-1 SLIDE REFLECTOR ASSY, OPN NORMAL. 2 L 7 3 4F A3WE 1996011900347 19960119 00347 NM 1996 1 19 DL72W960092 1 19960115 A 5754 ANGLE BOEING 727 727247 138408F NM NR 2 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2811W 20649 DURING C-1 LETTER CHECK, FOUND .5 INCH CRACK AT NR 2 L/E SLAT COVE SKIN ATTACH ANGLE BELOW I/B UPSTOP PAD. REPAIRED PER M/M 57-54-0. 2 L 7 3 4F A3WE 1996011900348 19960119 00348 NM 1996 1 19 DL72W960109 1 19960113 A 3220 BUSHING BOEING 727 727247 138408F NM NLG DOOR WORN A DALA O OTHER O OTHER CL CLIMB 1 SO 27 2807W 20579 ON CLIMBOUT FROM RIC AT 360 KTS, THE NOSE WHEEL DOORS WERE SLAMMING OPEN AND SHUT REPEATEDLY. FOUND NLG DOOR OUT OF RIG AND BUSHINGS WORN IN ROD ON FWD QUAD. REPLACED ROD AND RIGGED NLG DOORS. 2 L 7 3 4F A3WE 1996011900349 19960119 00349 NM 1996 1 19 DL72W960112 1 19960109 A 2560 LANYARD BOEING 727 727247 138408F NM R1 DOOR BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 295WA 22532 ON PREFLIGHT, FOUND R-1 DOOR SLIDE GIRT BAR LANYARD BROKEN. REPLACED LANYARD, OPERATION NORMAL. 2 L 7 3 4F A3WE 1996011900350 19960119 00350 NM 1996 1 19 DL733960062 1 19960110 A 3230 CONTROL CABLE BOEING 737 737347 1384647 NM GEAR HANDLE LOOSE A DALA O OTHER J WARNING INDICATION LD LANDING 1 SO 27 302WA 23182 GEAR DOWN 3 RED AND 3 GREEN LIGHTS. RECYCLED OK 3 GREEN, HAPPENED ON 2 APPROACHS. CORRECTED CABLE TENSION FOR LANDING GEAR ACTUATOR, GEAR SWING NORMAL. 2 L 7 2 4F RT A16WE 1996011900352 19960119 00352 NM 1996 1 19 DL73E960094 1 19960109 A 5330 654688257 SKIN BOEING 737 737247 138448D NM FS 1027 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 243WA 23517 DURING OVERHAUL INSPECTION, MAINTENANCE FOUND A 2.5 CRACK UNDER AN EXISTING REPAIR DOUBLER AT APPROXIMATELY FS 1027, BET WEEN S-7L AND S-8L. THE CRACK PROPAGATED IN THE SKIN FROM THE LOWER FORWARD CORNER OF THE DOUBLER. IN ACCORDANCE WITH B737-200 SRM 53-30-3 FIG 6, THE PREVIOUS CUTOUT UNDER THE REPAIR DOUBLER AND THE NEW DAMAGE WERE INCORPORATED INTO A SIN GLE REPAIR. 2 L 7 2 4F A16WE 1996011900353 19960119 00353 NM 1996 1 19 DL73S960100 1 19960113 A 3230 UPLOCK ACT 654482518 BOEING 737 737232 1384475 NM LT MLG FAILED A DALA K NONE J WARNING INDICATION TO TAKEOFF 1 SO 27 303DL 2392 23075 LT MLG UNSAFE LIGHT ON IN FLT WITH LT GEAR VIB ALONG WITH UNSAFE INDICATION. JACKED A/C, RAN GEAR AND FOUND UNLOCK ACTU ATOR BYPASSING FLUID. REPLACED SAME, GEAR CKS OK. 2 L 7 2 4F RT A16WE 1996011900354 19960119 00354 NM 1996 1 19 DL757960055 1 19960109 A 3350 BPS73 PWR SUPPLY BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 643DL 23997 EMERGENCY LIGHTS INOP AFT LT DOOR AND AFT LT OVERHEAD. REPLACED BATTERY PACK AND PWR SUPPLY. 2 L 7 2 4F RT A2NM 1996011900355 19960119 00355 NM 1996 1 19 DL757960056 1 19960109 A 3350 20131A BATTERY PACK BOEING 757 757232 1384965 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 643DL 23997 EMERGENCY LIGHTS INOP AFT LT FLOOR PATH LIGHTS. REPLACED BATT PACK. 2 L 7 2 4F RT A2NM 1996011900356 19960119 00356 NM 1996 1 19 DL757960075 1 19960112 A 3230 257T110314 LEVER MODULE BOEING 757 757232 1384965 NM FLT CABIN MALFUNCTIONED A DALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 27 673DL 25978 ON APPROACH TO ATL, NOSE GEAR DID NOT EXTEND, EXTENDED NORMALLY ON SECOND ATTEMPT. FOUND ACCUMULATION OF ICE ON NOSE GE AR AND HYD LINES ON AIRCRAFT ARRIVAL. INSPECTED W/W AREA, NOSE GEAR AND MECHANSM FOR DAMAGE AND NONE FOUND. JACKED AIR CRAFT, CYCLED GEAR AND OPS NORMAL. REPLACED LEVER MODULE PER MM, OPS NORMAL. 2 L 7 2 4F RT A2NM 1996011900357 19960119 00357 NM 1996 1 19 DL757960085 1 19960114 A 2530 COFFEE MAKER 811150417 BOEING 757 757232 1384965 NM CABIN SMOKING A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 674DL 188 25979 ELECTRICAL SMOKE CAME OUT OF NR 1 F/C COFFEE MAKER. C/B PULLED TO STOP SMOKE. REPLACED DISPENSER, OPN NML. 2 L 7 2 4F RT A2NM 1996011900358 19960119 00358 NM 1996 1 19 DL757960090 1 19960115 A 5754 114N300219 TE WEDGE BOEING 757 757232 1384965 NM NR 5 LE SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 607DL 22814 T/E WEDGE WAS FOUND TO BE DELAMINATED DURING SHOP INSPECTION FOR NR 5 L/E SLAT. THE NOTED T/E WEDGE WAS REPLACED PER SR M 57-43-02. 2 L 7 2 4F RT A2NM 1996011900359 19960119 00359 NM 1996 1 19 DL76S960106 1 19960115 A 2910 LINE BOEING 767 767332 1382001 NM WING ROOT CRACKED A DALA O OTHER K J B FLUID LOSS WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 120DL 23279 ON APPROACH TO ATL, HAD SMOKE OR BURNING ODOR IN AFT AND MID CABIN. FOUND SLAT PRESSURE HYD LINE CRACKED AT WING ROOT F USELAGE FITTING. REPLACED HYD LINE, NO LEAKS NOTED. REPLACED PRECOOLER FILTERS DUE TO SKYDROL CONTAMINATION. 2 L 7 2 4F RT A1NM 1996011900360 19960119 00360 WP 1996 1 19 DLL10960048 1 19960107 A 3350 079123 LIGHT LKHEED 1011 10113851 5265010 WP CABIN MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 721DA 193C1139 EMERGENCY LIGHT MISSING AT SEAT 1CD. RELAMPED AND REPLACED, CHECKS GOOD. 2 L 7 3 4F A23WE 1996011900361 19960119 00361 WP 1996 1 19 DLL10960076 1 19960112 A 3397 WIRE LKHEED 1011 10113851 5265010 WP CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 723DA 193C1150 EMERGENCY FLOOR TRACK LIGHT OUT AT SEAT 27 H, J. REPAIRED BROKEN WIRE IN FLOOR TRACK. 2 L 7 3 4F A23WE 1996011900362 19960119 00362 WP 1996 1 19 DLL10960082 1 19960113 A 3230 1516207122 CONTROL VALVE LKHEED 1011 10113851 5265010 WP LEFT W/W MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 733DS 193C1224 AFTER T/O RAISED GEAR HANDLE, ON PILOTS PANEL RSD DOOR AND INTRANSIT LIGHT ON, ALL GREEN LIGHTS OUT. ON S/O PANEL LT GE AR OR DOOR LIGHT ON. CYCLED GEAR, NO CHANGE AND RETURNED TO LAX. REPLACED RT PHASE CONTROL VALVE, OPERATION NORMAL. 2 L 7 3 4F A23WE 1996011900363 19960119 00363 WP 1996 1 19 DLL10960084 1 19960113 A 2750 SCREW JACK 1796062 LKHEED 1011 10113851 5265010 WP RT TE FLAP BROKEN A A DALA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 SO 27 722DA 193C1147 ON CLIMBOUT FLAPS EXTENDED 4 TO 6 DEGREES, SLATS UP WITH NO ACTUATION OF FLAP HANDLE. FLAPS WOULD NOT EXTEND BEYOND 10 DEGREES FOR LANDING. GPWS INHIBITED AS PER PROCEDURE. REPLACED RT INBRD FLAP SCREW JACK AND BEARINGS. RIGGED AND OPS CKD GOOD. 2 L 7 3 4F A23WE 1996011900364 19960119 00364 WP 1996 1 19 DLL10960088 1 19960114 A 3350 POWER SUPPLY 5165741 LKHEED 1011 10113851 5265010 WP PWA JT8 JT8D219 52053 NE CABIN INOPERATIVE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 717DA 62887 193C1096 725754 EMERGENCY LIGHTS IN FIRST CLASS FAILED TO ILLUMINATE DURING LAYOVER TEST. REPLACED POWER SUPPLY. 2 L 7 3 4F 4 F A23WE E9NE 1996011900365 19960119 00365 WP 1996 1 19 DLL13960057 1 19960108 A 5743 1591922 FITTING LKHEED 1011 10113851 5265010 WP LT MLG ACTUATOR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 790DL 193A1143 AT HMV, THE LT MLG ACTUATOR ATTACH FITTING WAS FOUND CORRODED ON THE UPPER FLANGE. TO REMOVE THE CORROSION THE FASTENER HOLE WAS OVERSIZED AND SPOTFACED IN ACCORDANCE WITH INSTRUCTIONS OF THE L1011 SRM FIG 808. THE FITTING WILL BE REPAIRE D PER L1011 SRM 57-14-00 FIG 808. 2 L 7 3 4F A23WE 1996011900366 19960119 00366 WP 1996 1 19 DLL15960067 1 19960110 A 3350 5165741 POWER SUPPLY LKHEED 1011 10113853 5265020 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 752DA 193W1172 ON LAYOVER, FOUND MID CABIN EMERGENCY LIGHTS INOP. REPLACED EMERGENCY LIGHT POWER SUPPLY, CHECKS GOOD. 2 L 7 3 4F A23WE 1996011900367 19960119 00367 WP 1996 1 19 DLL17960058 1 19960108 A 5330 1503536 SKIN LKHEED 1011 10113853 5265020 WP FS 1438 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 768DL 193H1216 AT HMV IN ATL, THE FUSELAGE SKIN AT FS 1438, LBL 14 WAS FOUND CORRODED. THE REPAIR CONSISTED OF TRIMMING THE FUSELAGE S KIN AND INSTALLING A REPAIR DOUBLER AND TRIPLER PER DL ERA 272995 REV A. 2 L 7 3 4F A23WE 1996011900369 19960119 00369 NM 1996 1 19 DLM88960060 1 19960109 A 5320 THRESHOLD DOUG MD88 MD88 3023688 NM CARGO DOOR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 902DL 49533 FOUND ON D1 LTR CHECK, CORROSION AT MID CARGO DOOR THRESHOLD. REPAIRED PER SRM 53-05 FIG 63. 2 L 7 2 4F RT A6WE 1996011900370 19960119 00370 NM 1996 1 19 DLM88960066 1 19960110 A 5320 JAMB DOUG MD88 MD88 3023688 NM C1 CARGO DOOR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DL 49538 FOUND ON C2 LTR CHECK, CORROSION C1 CARGO DOOR LWR JAMB LONGERON HAS CORROSION. REPAIRED PER SRM 53-05 FIG 44. 2 L 7 2 4F RT A6WE 1996011900371 19960119 00371 NM 1996 1 19 DLM88960070 1 19960112 A 2750 5935973501 DRIVE ARM DOUG MD88 MD88 3023688 NM LT TE FLAP BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 967DL 53116 LEFT TRAILING EDGE FLAP REPORTED WITH EXCESSIVE DROOP. FOUND BROKEN LINK ON LT FLAP ACTUATOR. REMOVED LINK AND ACTUATO R. INSTALLED AFT END OF ARM ASSEMBLY, LINK AND ROD. INSTALLED ACTUATOR AND RECONNECTED LINKS, OPERATION NORMAL. 2 L 7 2 4F RT A6WE 1996011900372 19960119 00372 NM 1996 1 19 DLM88960108 1 19960115 A 3244 TIRE DOUG MD88 MD88 3023688 NM LT MLG BLOWN A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 911DE 49967 AFTER TAKEOFF, RECEIVED LEFT MAIN GEAR UNSAFE LIGHT AND RETURNED FLL. FOUND NR 2 MAIN TIRE BLOWN, WITH WIRING TO SENSOR DAMAGED AND FLAP DAMAGED. REPLACED NR 1, NR 2 WHEELS AND REPAIRED WIRING. FERRIED TO ATL FOR REPAIRS. 2 L 7 2 4F RT A6WE 1996011900373 19960119 00373 NM 1996 1 19 DLM88960111 1 19960114 A 2910 HYD LINE DOUG MD88 MD88 3023688 NM TAIL COMP LEAKING A DALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 939DL 49812 AFTER TAKEOFF, HAD FAINT BURNING ODOR IN CABIN AND LAV SMOKE DETECTOR WENT OFF. FOUND HYDRAULIC LINE LEAKING AT RT THRU ST REV MODULE. INSTALLED APPROVED FLEX LINE FWD TO MCO. 2 L 7 2 4F RT A6WE 1996011900374 19960119 00374 NM 1996 1 19 DLM88960113 1 19960108 A 3231 RETRACT MECH DOUG MD88 MD88 3023688 NM LT MLG DOOR MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 999DN 53371 ON LANDING GEAR RETRACTION, LEFT MAIN GEAR UNSAFE LIGHT REMAINED ILLUMINATED WITH GEAR DOOR OPEN LIGHT. AIRCRAFT RETURN ED ATL. CYCLED GEAR, ALL VISUAL NORMAL AND INDICATIONS NORMAL. BLED HYDRAULIC SYSTEM OF AIR, INSPECTED GEAR DOORS AND AREA, OPERATION NORMAL. 2 L 7 2 4F RT A6WE 1996011900375 19960119 00375 WP 1996 1 19 MWEA96013 1 19960116 A 3222 591009505105 STRUT DOUG DC9 DC914 3022034 WP NLG REQD SERVICE A MWEA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 GL 31 400ME 45727 MCI - AFTER TAKEOFF, LOST PRESSURIZATION AND TAKEOFF WARNING CAME ON AND AUTO SPOILER DO NOT USE LIGHT ILLUMINATED. AIR CRAFT RETURNED TO MCI. FOUND NOSE GEAR STRUT DEFLATED KEEPING THE A/C IN GROUND MODE. SERVICED STRUT WITH AIR, FOUND N O LEAKS. 2 L 7 2 4F A6WE 1996011900376 19960119 00376 NE 1996 1 19 SWIA95707 2 19960112 A 7261 O-RING EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT ENGINE FAILED A SWIA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 07 196SW 120151 LOSS OF OIL PRESSURE EN ROUTE, SHUTDOWN LEFT ENGINE. REPLACED O-RING ON LEFT AUXILIARY GENERATOR AND REPLACED CLAMP. R AN ENGINE, OPS AND LEAK CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1996011900377 19960119 00377 SW 1996 1 19 SWIA95708 1 19960113 A 2910 HYD LINE SWRNGN SA227 SA227AC 8780603 SW RIGHT CRACKED A SWIA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 NM 07 3117S AC603 TOTAL LOSS OF HYDRAULIC PRESSURE. FOUND RIGHT HYDRAULIC PRESSURE LINE CRACKED. REPLACED LINE AND SERVICED HYDRAULIC SY STEM. RAN ENGINES AND OPS, LEAK CHECK GOOD. 1 L 7 2 4T A8SW 1996011900378 19960119 00378 1996 1 19 SWIA95709 4 19960116 A 3425 AHRS COMPUTER EMB 120 EMB120ER 3260203 SO RIGHT LOOSE A SWIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 NM 07 189SW 120048 FIRST OFFICER'S COMPUTER FLAG COMES ON AND GOES OFF CONTINIOUSLY WHILE AIRBORNE. REPLACED FIRST OFFICER'S AHC-85 AHRS C OMPUTER RETAINING SCREW/NUT. OPS CHECK OF AHC-85 AHRS COMPUTER CHECKS GOOD. 2 L 7 2 4T RT A31SO 1996011900379 19960119 00379 NM 1996 1 19 VSTA9601011 1 19960110 A 5320 65C3372247 CHORD BOEING 737 737247 138448D NM FS 727 CRACKED A VSTA K NONE O OTHER IN INSP/MAINT 1 WP 07 302VA 20126 CRACKED FAIL-SAFE CHORD FS 727 LEFT HAND SIDE. REPAIRED IAW BOEING SB 737-53-1088. REPLACED REPAIRED CHORD IAW EO 53-1 0-3 R1 11/13/95. COMPLETION TERMINATES INSPECTION PER WORK CARD 5364 FOR SIDE REPLACED. MAINTENANCE PERFORMED BY SOUTH WEST AERO TECH NR S5WR702J. 2 L 7 2 4F A16WE 1996011900518 19960119 00518 NE 1996 1 19 9601035514 2 19960117 A 7530 STATOR VANE ACT BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE NR 1 ENGINE FAILED A NWAA E D ENGINE SHUTDOWN RETURN TO BLOCK J X WARNING INDICATION ENGINE FLAMEOUT TX TAXI/GRND HDL 1 GL 01 514US 23202 716370 DURING TAXI OUT, EICAS MESSAGE ENGINE CONTROLS DISPLAYED. THIRTY SECONDS LATER, NR 1 ENGINE SHUT DOWN. AIRCRAFT RETURNE D TO GATE. GROUND MAINTENANCE REPLACED NR 1 ENGINE STATOR VANE ACTUATOR. OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F RT A2NM E17NE 1996011900519 19960119 00519 NM 1996 1 19 9601046305 1 19960116 A 3350 CONNECTOR BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 665US 23820 DURING LINE CHECK, THE FLOOR EMERGENCY PATH LIGHTS BETWEEN SEAT ROWS 35R TO 42R WERE FOUND INOPERATIVE. RECONNECTED EME RGENCY LIGHT CONNECTOR PIN. OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996011900520 19960119 00520 NM 1996 1 19 9601056625 1 19960117 A 2150 PACK BOEING 747 747251B 1384892 NM NR 1 MALFUNCTIONED A NWAA A J UNSCHED LANDING DUMP FUEL B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 625US 21707 AFTER TAKEOFF AND SUBSEQUENTLY TURNING OFF PACKS, SMOKE FILLED THE ENTIRE AIRCRAFT. WITH ALL PACKS SHOWING NORMAL OPERA TING TEMPERATURE, THE SMOKE DISSIPATED WITHIN A MINUTE. CREW FOLLOWED COCKPIT OPERATING PROCEDURE, DUMPED 177,000 POUND S OF FUEL, AND RETURNED TO LAX. FOUND NR 1 PACK FILTER WITH OIL SMELL. NR 2 AND NR 3 PACKS CHECKED OK. DEFERRED NR 1 PACK PER MEL 21-1A. 2 L 7 4 4F A20WE 1996011900521 19960119 00521 NM 1996 1 19 96FDEA00065 1 19960117 A 5320 STIFFENER BOEING 727 72722 1384002 NM BS 319 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 CORROSION (C53-111-03-1/2), ON VERTICAL STIFFENER BS 319 WL 181 RBL 15. REMOVED CORROSION AND INSTALLED REPAIR IAW FEDE X SRM 51-40-4. 2 L 7 3 4F A3WE 1996011900522 19960119 00522 NM 1996 1 19 96FDEA00066 1 19960118 A 5313 STRINGER BOEING 727 72722 1384002 NM BS 396 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 CORROSION (C53-224-03-1/2) ON STR 22R, BS 396. REMOVED CORROSION AT BS 396, STR 22R. REMOVED IN A 1 INCH BY 2 INCH ARE A. ORIGINAL METAL THICKNESS IS .040 INCH. REMOVED .009 INCH, FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. FABRICA TED AND INSTALLED REPAIR PARTS PER FEDEX SRM 53-10-3, FIG 2. APPLIED PROTECTIVE FINISHERS. 2 L 7 3 4F A3WE 1996011900523 19960119 00523 NM 1996 1 19 96FDEA00067 1 19960118 A 5753 TE SKIN BOEING 727 72722 1384002 NM RT TE FORE FLAP DISBONDED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 RIGHT WING INBD FORE FLAP UPPER SURFACE HAS DISBOND ON T/E AREA MARKED. REPAIRED RT WING INBOARD FORE FLAP IAW SRM 51-4 0-6. 2 L 7 3 4F A3WE 1996011900524 19960119 00524 NM 1996 1 19 96FDEA00068 1 19960118 A 5311 FRAME BOEING 727 727233 138408A NM BS 720 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 GOUGE IN FRAME AT BS 720B, LT BETWEEN STR 15 AND STR 14. GOUGE IN FRAME AT BS 720B, LT BETWEEN STR 15 AND STR 14 WAS FO UND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1 AND WAS REPAIRED PER FEDEX SRM 51-40-3. 2 L 7 3 4F RT A3WE 1996011900525 19960119 00525 NM 1996 1 19 96FDEA00069 1 19960118 A 5311 FRAME BOEING 727 727233 138408A NM BS 700 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22088 DENTS IN FRAME BS 700 RBL 34 TO 44 WL 160. REPAIRED DENTED FRAME AT BS 700 RBL 34 TO RBL 44 WL 160 IAW FEDEX SRM 51-40- 3. 2 L 7 3 4F RT A3WE 1996011900526 19960119 00526 NM 1996 1 19 96FDEA00070 1 19960118 A 5311 FRAME BOEING 727 727233 138408A NM BS 580 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 DENTS IN FRAME BS 580, LBL 37 - LBL 46, WL 160. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR DOUBLER AT BS 58 0, LB 37 - LB 46, WL 160 PER FEDEX SRM 51-40-3. 2 L 7 3 4F RT A3WE 1996011900527 19960119 00527 NM 1996 1 19 96FDEA00071 1 19960115 A 5313 STRINGER DOUG MD11 MD11F 3023600 NM FS 545 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 FORWARD END OF STRINGER 35L CRACKED FROM RIVET HOLE TO FWD END LENGTH. APPROXIMATELY .1250 INCH FS 545 CONFIRMED BY HFE C. FABRICATED STRINGER 35L PER SAMPLE AND INSTALLED STRINGER PER SRM 51-00-01. 2 L 7 3 4F RT A22WE 1996011900528 19960119 00528 NM 1996 1 19 96FDEA00073 1 19960115 A 5313 STRINGER DOUG MD11 MD11F 3023600 NM FS 545 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 602FE 48402 FOUND STRINGER 34L SEVERED FWD OF PREVIOUS SKIN CRACK STATION FS 545. FABRICATED STRINGER 34L PER SAMPLE AND INSTALLED PER SRM 51-00-01. 2 L 7 3 4F RT A22WE 1996011900529 19960119 00529 NE 1996 1 19 96UAL900038 2 19960117 A 7200 50G631 BEARING BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 4 ENGINE FAILED A UALA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 WP 29 183UA 25379 717694 NR 4 ENGINE FAILURE SHORTLY AFTER TAKEOFF. DUMPED FUEL AND RETURNED TO FIELD. REPLACED ENGINE. ANGLE GEARBOX AB-1 BEA RING FAILURE. 2 L 7 4 4F 4 F RT A20WE E24NE 1996011900530 19960119 00530 NM 1996 1 19 96UAL900039 1 19960117 A 2560 25860304 ASPIRATOR ASSY BFGOODRICH 7A110424 BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE CREW SLIDE INOPERATIVE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 4729U G129 19926 CREW SLIDE FOUND WITH LARGE WAD OF PACKING PAPER BLOCKING ASPIRATOR FLAPPER DOORS. REMOVED ASPIRATOR FROM SLIDE AND REM OVED PAPER WAD. PAPER WAS INSTALLED IN THE ASPIRATOR AFTER MANUFACTURE TO PREVENT DOORS FROM OPENING/CLOSING DURING SHI PPING. PAPER NOT REMOVED DURING ORIGINAL INSTALLATION INTO THE SLIDE ASSEMBLY. 2 L 7 4 4F 4 F A20WE E20EA 1996011900531 19960119 00531 NM 1996 1 19 96UAL900040 1 19960117 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT DOOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 566UA 26670 NR 1 LEFT DOOR OUTER EMERGENCY LIGHT INOP. ACCOMPLISHED LIGHT SYSTEM TEST PER MAINTENANCE MANUAL 33-51-00 AND DETERMINE D LIGHT OPERATION NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996011900532 19960119 00532 SO 1996 1 19 COMA9610025 1 19960115 A 3244 314461 TIRE 314461 EMB 120 EMB120RT SO MLG WHEEL SEPARATED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 268CA 9388 225 120262 MECHANIC REMOVED TIRE FROM A/C DUE TO TIRE FLAT AND MATE TO BLOWN TIRE. DURING INSPECTION FOUND TIRE BEAD SEPARATION WI TH WIRE OFF BEAD EXPOSED. REMOVED WHEEL ASSY FROM SERVICE AND SENT WHEEL AND TIRE TO BFG. 2 L 7 2 4T RT A31SO 1996011900533 19960119 00533 SO 1996 1 19 COMA9610026 1 19960115 A 3246 3006031 WHEEL 314461 EMB 120 EMB120RT SO MLG CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 268CA 8701 2406 120262 MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE BLOWN AND WHEEL DAMAGE. WHEEL SHOP INSPECTED AND FOUND OUTBOARD HALF A SSY P/N 300-603-1 WAS CRACKED. CRACK IN FLANGE APPROXIMATELY 6 INCHES LONG. WHEEL ASSY HAS BEEN REMOVED FROM SERVICE A ND SENT TO BFG. 2 L 7 2 4T RT A31SO 1996011900534 19960119 00534 SO 1996 1 19 COMA9610027 1 19960116 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 268CA 14448 1285 120262 EMERGENCY ESCAPE PATH LIGHTING FROM ROW 8 THROUGH ROW 10 ARE INOPERATIVE. REPLACED EMERGENCY BATTERY. 2 L 7 2 4T RT A31SO 1996011900535 19960119 00535 EU 1996 1 19 COMA9630016 1 19960116 A 3020 NH2466881 INLET HEAT SAAB SF340 SF340A 7850100 EU LT ENGINE FAILED A COMA K NONE O OTHER CR CRUISE 1 SO 01 358CA 6742 1168 340A047 LEFT ENGINE INLET HEAT FAIL LIGHT ILLUMINATED. RED GLOW SEEN IN INTAKE. REPLACED THE LEFT LOWER INLET DUCT. 2 L 7 2 4T RT A52EU 1996011900536 19960119 00536 EU 1996 1 19 COMA9630017 1 19960116 A 2720 CONNECTORS SAAB SF340 SF340A 7850100 EU RUDDER LIMITER DIRTY A COMA K NONE F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 01 347CA 340A028 RUDDER LIMITER OVERRIDE CIRCUIT BREAKER TRIPPED AND WILL NOT RESET. CLEANED WATER FROM WIRING CONNECTIONS AT RUDDER LIM ITER. ACFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 1996011900537 19960119 00537 EA 1996 1 19 COMA9660015 1 19960116 A 7732 6233M30A ACCELEROMETER CNDAIR CL600 CL6002B19 1900309 EA LT ENG DEFECTIVE A COMA K NONE N FALSE WARNING CL CLIMB 1 SO 01 916CA 6411 7014 LEFT ENGINE N2 VIBRATION CAUTION COMES ON AT 87 PERCENT TO 88 PERCENT N2. REPLACED THE LT ENGINE N2 ACCELEROMETER. 2 L 7 2 4F RT A21EA 1996011900538 19960119 00538 NM 1996 1 19 P5CA9600001 1 19960117 A 3241 421897 CONTROL BOX BOEING 747 747123 1384873 NM ANTI SKID SYST FAILED A P5CA K NONE O OTHER LD LANDING 1 WP 23 859FT 20326 DEPARTING KHV, TOWER ADVISED RUBBER LEFT ON RUNWAY. ON ARRIVAL ANC, DISCOVERED NR 11 TIRE BLOWN, HOLE IN WING-BODY FAIR ING, 18 OF CONDUIT MISSING FROM RT BG STRUT. REPLACED ANTI-SKID BOX DUE TO FAILED BITE CHECK IAW MM 32-42-00, 3 TIRES I AW MM 32-45-01. PERFORMED INTERIM REPAIR ON PANEL IAW MA5350-02:01. 2 L 7 4 4F A20WE 1996011900539 19960119 00539 NM 1996 1 19 UPS205219 1 19960116 A 3260 2314152 SWITCH MECH BOEING 727 727185C 138406N NM RT MLG DOOR MISSING A IPXA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 940UP 19826 CREW REPORTED, AFTER TAKEOFF, GEAR IN OFF POSITION, GEAR DOOR LIGHT ILLUMINATED, GEAR CYCLED LIGHT REMAINED ON, CONTACTE D MAINTENANCE. REMAINDER OF FLIGHT FLOWN WITH GEAR HANDLE UP, LIGHT GIBSON WAS OFF. FOUND BUSHING, RT MAIN LANDING DOO R SWITCH MECHANISM MISSING. INSTALLED SAME PER 727-MM 32-62-11. 2 L 7 3 4F A3WE 1996012600051 19960126 00051 WP 1996 1 26 USAA960004 1 19960119 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 101 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 820US 37700 49119 PIT - DURING Q-6 CHECK INSPECTION, FOUND A .25 INCH CRACK COMING FROM RIVET AT STA 101, LEFT AFT OF STRAKE IN SKIN. REM OVED DAMAGED AREA AND INSTALLED DOUBLER AND FILLER REPAIR PER USAIR TYPICAL REPAIR 53-30-11. (X) 2 L 7 2 4F A6WE 1996012600060 19960126 00060 NM 1996 1 26 USAASB96003 1 19960108 A 2133 10612097 OUTFLOW VALVE BOEING 737 7372B7 1384560 NM CABIN STUCK A USAA A UNSCHED LANDING O OTHER TO TAKEOFF 1 EA 19 280AU 22892 CLT - FLT 521 - AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. STOPPED AT 8,000 FEET ABOVE AGL, THEN RETURNED TO CLT. ON DESCENT AT 2,000 FEET, AIRCRAFT STARTED TO PRESSURIZE. MAINTENANCE REPLACED OUTFLOW VALVE DUE TO STICKING. OPS CHECKE D OK. (X) 2 L 7 2 4F A16WE 1996012600062 19960126 00062 WP 1996 1 26 9601069967 1 19960118 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9331 47263 DURING LINE CHECK, FOUND EMERGENCY FLOOR LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600063 19960126 00063 WP 1996 1 26 9601079909 1 19960118 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 959N 47255 DURING LINE CHECK, FOUND FORWARD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600064 19960126 00064 WP 1996 1 26 9601089608 1 19960118 A 3010 39271011 VALVE DOUG DC9 DC932 3022066 WP RT ENGINE FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 608NW 47233 DURING CLIMB, THE RIGHT ICE PROTECTION TEMPERATURE HIGH LIGHT ILLUMINATED. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND LIGHT REMAINED ILLUMINATED. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE PNEUMATIC AUGMENTA TION VALVE AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600065 19960126 00065 WP 1996 1 26 9601099949 1 19960118 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP TAILCONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8928E 45865 DURING LINE CHECK, FOUND EMERGENCY PATH LIGHTS IN TAILCONE INOPERATIVE. REPLACED BATTERY PACK AND POWER SUPPLY, OPERATI ONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600066 19960126 00066 WP 1996 1 26 9601109604 1 19960117 A 3244 TIRES DOUG DC9 DC932 3022066 WP NR 1/2 MLG DAMAGED A NWAA A UNSCHED LANDING B E SMOKE/FUMES/ODORS/SPARKS VIBRATION/BUFFET CL CLIMB 1 GL 01 604NW 47222 DURING TAKEOFF, THE AIRCRAFT WAS SLOW TO ACCELERATE AND A SLIGHT VIBRATION WAS EXPERIENCED. DURING CLIMB, A RUBBER SMOK E SMELL WAS DETECTED AFTER LANDING GEAR RETRACTION. AIRCRAFT DIVERTED TO ORD AND LANDED WITHOUT INCIDENT. FOUND NR 2 M AIN LANDING GEAR TIRE FLAT-SPOTTED AND FLAT, NR 1 MAIN LANDING GEAR TIRE FLAT-SPOTTED. REPLACED NR 1, NR 2 MAIN LANDING GEAR TIRES AND ANTI-SKID CONTROL BOX. OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600067 19960126 00067 WP 1996 1 26 9601119921 1 19960117 A 3010 39271011 VALVE DOUG DC9 DC932 3022066 WP LT ENGINE FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 943N 51182 4761 47647 DURING CLIMB, THE LEFT ICE PROTECTION TEMPERATURE HIGH LIGHT ILLUMINATED. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND LIGHT EXTINGUISHED. AIRCRAFT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. REPLACED THE PNEUMATIC AUGMENTATION VALV E AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600068 19960126 00068 WP 1996 1 26 9601129906 1 19960116 A 3260 CONNECTOR DOUG DC9 DC932 3022066 WP NLG DIRTY A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 956N 47252 GCM - DURING CLIMB, THE NOSE LANDING GEAR UNSAFE LIGHT ILLUMINATED AFTER LANDING GEAR RETRACTION. RECYCLED LANDING GEAR AND LIGHT EXTINGUISHED. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. LUBRICATED NOSE LANDING GEAR, CLEANED CANNON PLUG AND SWITCH ON NOSE LANDING GEAR INDICATION SYSTEM. OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600069 19960126 00069 NM 1996 1 26 9601132710 1 19960112 A 2910 CIRCUIT BREAKER BOEING 727 727225 1384077 NM B-HYD SYST TRIPPED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 820EA 22557 DURING TAKEOFF ROLL, TAKEOFF ABORTED UNDER 80 KTS DUE LOW 'B' SYSTEM PRESSURE 2,000 PSI. RESET 'B' SYSTEM CIRCUIT BREAK ER AND SYSTEM CHECKED NORMAL. 2 L 7 3 4F A3WE 1996012600070 19960126 00070 WP 1996 1 26 9601141161 1 19960119 A 2820 2720121 CONTROLLER DOUG DC10 DC1040 3023508 WP FUSELAGE FAILED A A NWAA A J UNSCHED LANDING DUMP FUEL K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 161US 46770 DURING CRUISE, THE TANK OVER FILLED LIGHT ILLUMINATED AND FUEL WAS STREAMING FROM THE LEFT DUMP NOZZLE. DUMPED 92,500 L BS OF FUEL AND RETURNED TO DTW. REPLACED FUEL CONTROLLER. 2 L 7 3 4F A22WE 1996012600071 19960126 00071 WP 1996 1 26 9601159178 1 19960117 A 3222 5910096 STRUT DOUG DC9 DC914 3022034 WP NLG REQD SERVICE A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 3310L 45705 AIRCRAFT FAILED TO SHIFT FROM GROUND MODE TO FLIGHT MODE AFTER TAKEOFF. LANDING GEAR RETRACTED NORMALLY. FLIGHT RETURN ED TO MSP AND LANDED WITHOUT INCIDENT. REPACKED AND SERVICED NOSE LANDING GEAR STRUT TO PROPER LEVELS. OPERATIONAL CHE CK NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996012600072 19960126 00072 NM 1996 1 26 96FDEA00074 1 19960119 A 5753 SKIN BOEING 727 72722 1384002 NM RT TE FOREFLAP CHAFING A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 RT WING I/B FOREFLAP IS CHAFING APPROX 24 INCHES O/B FROM I/B LEADING EDGE. REPAIRED DAMAGE AREA ON RT WING I/B FOREFL AP APPROX 24 INCHES O/B FROM I/B LEADING EDGE. 2 L 7 3 4F A3WE 1996012600073 19960126 00073 NM 1996 1 26 96FDEA00075 1 19960119 A 5330 SKIN BOEING 727 72722 1384002 NM FUSELAGE LIGHTNING STRIKE A FDEA K NONE C F.O.D. IN INSP/MAINT 1 SO 25 169FE 18866 LIGHTNING STRIKES AT BS 706, 793, 824 AND 888 BETWEEN STR 4 AND 5. REPAIRED LIGHTNING STRIKES AT BS 750, 793, 824 BY IN STALLING NEW FASTENERS. REPAIRED BS 888 BY CUTTING OUT DAMAGED AREA AND FABRICATING REPAIR PARTS. INSTALLED IAW 53-30- 3. 2 L 7 3 4F A3WE 1996012600074 19960126 00074 NM 1996 1 26 96FDEA00076 1 19960119 A 5320 FITTING BOEING 727 72722 1384002 NM BS 870 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 CRACK IN AFT FLANGE OF TERMINAL FITTING AT BS 870 STR 13R. HFEC DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED PER EWO N R 96-2043. 2 L 7 3 4F A3WE 1996012600076 19960126 00076 NM 1996 1 26 96FDEA00078 1 19960118 A 5330 SKIN BOEING 727 72722 1384002 NM BS 875-878 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 CORROSION ON SKIN INTERIOR AT BS 875 TO 878 BELOW STR 9R. REPAIRED CORROSION ON INTERIOR SKIN AT BS 875 TO 878 BELOW ST R 9R PER FEDEX EA 7-5310-26957. 2 L 7 3 4F A3WE 1996012600077 19960126 00077 NM 1996 1 26 96FDEA00079 1 19960123 A 5330 SKIN BOEING 727 727233 138408A NM BS 1073 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 BS 1073 STR 19 TO 20L THERE IS A SHARP CREASE IN SKIN. REMOVED DAMAGE AT BS 1073 STR 19 TO 20L IN SKIN. FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 53-30-3. 2 L 7 3 4F RT A3WE 1996012600078 19960126 00078 NM 1996 1 26 96FDEA00080 1 19960119 A 5330 SKIN BOEING 727 727233 138408A NM BS 1030-1050 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 BS 1030 TO 1050 STR 20 TO 21L SKIN IS CREASED. REMOVED DAMAGE AT BS 1030 TO 1050 STR 20 TO 21L IN SKIN. FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 53-30-3. 2 L 7 3 4F RT A3WE 1996012600079 19960126 00079 NM 1996 1 26 96FDEA00081 1 19960119 A 5311 FRAME BOEING 727 727233 138408A NM BS 680 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 DENTS IN FRAME BS 680 LBL 34 TO 45 WL 160. CUT OUT DAMAGE ON FRAME BS 680 LBL 34 TO 45 WL 160, FABRICATED AND INSTALLED REPAIR PER FEDEX SRM 51-40-3. 2 L 7 3 4F RT A3WE 1996012600080 19960126 00080 NM 1996 1 26 96FDEA00082 1 19960119 A 5311 FRAME BOEING 727 727233 138408A NM BS 700 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 DENTS IN FRAME BS 700 LBL 34 TO 44 WL 160. REMOVED DAMAGE AND FABRICATED REPAIR PARTS PER SRM 51-40-3. 2 L 7 3 4F RT A3WE 1996012600081 19960126 00081 NM 1996 1 26 96FDEA00083 1 19960119 A 5311 FRAME BOEING 727 727233 138408A NM BS 500 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 DENTS IN FRAME BS 500 RBL 34 TO 44 WL 160. CUT OUT DAMAGE REPAIRED FRAME BS 500 RBL 34 TO 44 WL 160 PER FEDEX SRM 51-40 -3. 2 L 7 3 4F RT A3WE 1996012600082 19960126 00082 NM 1996 1 26 96FDEA00084 1 19960123 A 5330 SKIN BOEING 727 727233 138408A NM BS 1050-1056 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 FIVE DENTS IN SKIN 1050 TO 1056 STR 28 TO 29R. REPAIRED SKIN IAW FEDEX SRM 53-30-3. 2 L 7 3 4F RT A3WE 1996012600083 19960126 00083 NM 1996 1 26 96FDEA00085 1 19960119 A 5320 651758866 BEAM BOEING 727 727233 138408A NM BS 268 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 CORROSION (C53-221-01), ON 25G BEAM AT BS 268 LBL 7 WL 08.1. REMOVED AND REPLACED 25G BEAM PER SRM 53-10-01. 2 L 7 3 4F RT A3WE 1996012600084 19960126 00084 NM 1996 1 26 96FDEA00086 1 19960119 A 5313 STRINGER BOEING 727 727233 138408A NM BS 720 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 CORROSION (53-111-01-2), ON STR 28L BS 720 PLUS 4 WL 149. REMOVED, FABRICATED AND REPLACED STR 28L BS 720 PLUS 4 WL 149 IAW FEDEX SRM 53-10-2 AND 53-10-3. 2 L 7 3 4F RT A3WE 1996012600086 19960126 00086 NM 1996 1 26 96FDEA00088 1 19960118 A 5311 FRAME BOEING 727 727233 138408A NM BS 500 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 DENT IN FRAME BS 500 LBL 34 TO 46 WL 160. CUT OUT DENT, FABRICATED REPAIR DOUBLER, CLEANED, TREATED PART AND FRAME. IN STALLED REPAIR DOUBLER PER FEDEX SRM 51-40-3. 2 L 7 3 4F RT A3WE 1996012600087 19960126 00087 NM 1996 1 26 96FDEA00089 1 19960119 A 5753 SKIN BOEING 727 727233 138408A NM RT TE FOREFLAP DISBONDED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 RT WING I/B FOREFLAP I/B END HAS DISBONDED RUBSTRIP UPPER SURFACE. REPAIRED PER SRM 51-40-06. 2 L 7 3 4F RT A3WE 1996012600088 19960126 00088 NM 1996 1 26 96FDEA00090 1 19960119 A 5751 TE WEDGE BOEING 727 727233 138408A NM RT AILERON DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 RT WING O/B AILERON T/E WEDGE DELAMINATED AT O/B END. REPAIRED PER SRM 51-40-6. 2 L 7 3 4F RT A3WE 1996012600089 19960126 00089 NM 1996 1 26 96FDEA00093 1 19960119 A 5311 FRAME BOEING 727 727233 138408A NM BS 360 GOUGE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 FOUND GOUGE IN FRAME STA 360 WL 156 LBL 40, BETWEEN STR 24 TO 25 LT, E-BAY. REMOVED DAMAGE AND FABRICATED PART. REPAIR ED PER SRM 51-40-3 AND 53-10-2. 2 L 7 3 4F RT A3WE 1996012600090 19960126 00090 NM 1996 1 26 96FDEA00094 1 19960119 A 5330 SKIN BOEING 727 727233 138408A NM BS 480-560 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 AREA OF SKIN DAMAGE STA 480 TO 560 STR 26 LT TO RT LOWER SKIN PANEL INCLUDING 2 DENTS STA 496 AND 503 BETWEEN STR 26-27R , MARKED. BLENDED AREA OF SKIN DAMAGE STA 480 TO 560 STR 26 LT AND RT LOWER SKIN PANEL. FOUND TO BE WITHIN LIMITS EXCL UDING 2 AREAS. ONE AT STA 500 RBL 14 AND 1 AT STA 490 RBL 22 PER FEDEX SRM 53-30-1, REPAIRED BOTH AREAS PER FEDEX SRM 5 3-30-3. 2 L 7 3 4F RT A3WE 1996012600091 19960126 00091 NM 1996 1 26 96FDEA00095 1 19960119 A 5347 SEAT TRACK BOEING 727 727233 138408A NM BS 480 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 CORROSION (C53-224-01), ON SEAT TRACK BS 480 RBL 25 WL 208. REMOVED SECTION OF TRACK, FABRICATED NEW SECTION AND INSTAL LED PER SRM 53-10-5. 2 L 7 3 4F RT A3WE 1996012600092 19960126 00092 NM 1996 1 26 96FDEA00096 1 19960113 A 5320 FITTING BOEING 747 747245F 1384897 NM BS 1020 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 640FE 20826 SIN - MAIN DECK ATTACH FITTING AT BS 1020 BETWEEN FLOORBEAMS LBBL 72 TO 92 AND 98.58 FOUND 8 INCH CRACK. 2 L 7 4 4F A20WE 1996012600093 19960126 00093 NM 1996 1 26 96FDEA00097 1 19960113 A 5315 FLOOR BEAM BOEING 747 747245F 1384897 NM BS 1000 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 640FE 20826 MAIN DECK LBBL 33 TO 99 FLOOR BEAM AT 1000 FOUND CRACKED AT FLOOR BOARD ATTACHMENT HOLE, NOTE PREVIOUS CORROSION BLEND O UT AREA. REPAIR CARRIED OUT AS PER REF SNRM 1654 FOR DETAILS ERA B53-40-27. 2 L 7 4 4F A20WE 1996012600094 19960126 00094 NM 1996 1 26 96FDEA00098 1 19960113 A 5320 INTERCOSTAL BOEING 747 747245F 1384897 NM BS 1020 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 640FE 20826 SIN - MAIN DECK LATERAL INTERCOSTAL AT BS 1020 BETWEEN FLOORBEAMS LBBL 72.92 AND 98.58, FOUND CRACKED ON UPPER SURFACE. 2 L 7 4 4F A20WE 1996012600095 19960126 00095 NM 1996 1 26 96FDEA00099 1 19960113 A 5320 STIFFENER BOEING 747 747245F 1384897 NM BS 1100 MISSING FASTENER A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 640FE 20826 SIN - MAIN DECK LBBL 57 TO 50 FLOORBEAM VERTICAL STIFFENER AT BS 1100, FOUND 4 EA HI-LOK COLLARS MISSING. 2 L 7 4 4F A20WE 1996012600096 19960126 00096 NM 1996 1 26 96FDEA00100 1 19960113 A 5320 BRACKET BOEING 747 747245F 1384897 NM BS 1200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 640FE 20826 SIN - MAIN DECK RBBL 57 TO 50 FLOORBEAM AT BS 1200, FOUND ANGLE BRACKET TO VERTICAL STIFFENER CRACKED. 2 L 7 4 4F A20WE 1996012600097 19960126 00097 NM 1996 1 26 96FDEA00101 1 19960119 A 5754 65162268A K-FLAP BOEING 727 727227 1384078 NM NR 5 LE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 488FE 21491 NR 5 K-FLAP O/B LUB O/B SIDE UPPER MOUNT BOLT HAS CORROSION UNDER NUT. CORROSION WAS FOUND TO BE OUT OF LIMITS. REMOVE D AND REPLACED NR 5 K-FLAP AND FUNCTIONAL CHECK IAW FEDEX MM 27-81-1. 2 L 7 3 4F A3WE 1996012600098 19960126 00098 NM 1996 1 26 96UAL900041 1 19960118 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 509UA 24763 EMERGENCY ESCAPE LIGHTING INOP AT OVERWING EXIT ROW 17 ABC. RELAMPED DEFECTIVE EMERGENCY ESCAPE LIGHT AT OVERWING EXIT ROW 17 ABC AND OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996012600100 19960126 00100 WP 1996 1 26 96UAL900044 1 19960118 A 2820 ARLO627511 TEE ASSY DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL FUEL MANIFOLD RUPTURED A A UALA K NONE O OTHER NR NOT REPORTED 1 WP 29 1834U 47966 UNWANTED FUEL TRANSFER INTO NR 2 MAIN TANK WITH FILL VALVE SWITCH IN CLOSED POSITION AND NR 2 MAIN FILL VALVE LIGHT INDI CATING FILL VALVE IS IN CLOSED POSITTION. A WELD FAILED ALLOWING A PRESSURE RELIEF VALVE TO COME OFF THE FUEL MANIFOLD. REPLACED RUPTURED FUEL PUMP TEE ASSEMBLY. 2 L 7 3 4F 4 F A22WE E23EA 1996012600101 19960126 00101 NM 1996 1 26 96UAL900045 1 19960118 A 3350 LEADER LINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE AFT LAV FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 509UA 24763 FLOOR EMERGENCY ESCAPE LIGHTING INOP AFT LAVATORY AREA. REPLACED LEADER LINE FLOOR EMERGENCY ESCAPE LIGHTING AT AFT LAV ATORY AREA AND OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996012600102 19960126 00102 NM 1996 1 26 96UAL900046 1 19960119 A 4900 APU BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE APU COMPT SMOKING A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 7289U 21567 CREW REPORTED SMOKE AND FIRE COMING FROM APU ON ARRIVAL. RESET CB AND APU STARTED, NO SMOKE. COULD NOT DUPLICATE. 2 L 7 3 4F 4 F A3WE E2EA 1996012600103 19960126 00103 NM 1996 1 26 96UAL900047 1 19960119 A 2820 69186122 VENT TUBE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 FUEL TANK BROKEN A UALA O OTHER O OTHER CR CRUISE 1 WP 29 7286U 21564 WHILE OPERATING ALL OUT OF NR 2 FUEL TANK, THE NR 3 TANK DECREASED SLOWLY IN QUANTITY WITH ONLY THE AFT PUMP OPERATING. LEAKED 1,200 LBS OVER 1 HOUR 15 MINUTES. TURNING OFF BOTH BOOST PUMPS QUANTITY DECREASE STOPPED. FOUND BROKEN VENT TU BE AND REPLACED TUBE. 2 L 7 3 4F 4 F A3WE E2EA 1996012600104 19960126 00104 WP 1996 1 26 96UAL900048 1 19960119 A 2760 APH7201 SPRING DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL SPEEDBRAKE DRUM FAILED A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 1837U 47969 SPOILERS FAILED TO RETRACT AFTER LANDING. HELICAL RETURN SPRING ON SPEEDBRAKE DRUM FOUND BROKEN. REPLACED SPRING. 2 L 7 3 4F 4 F A22WE E23EA 1996012600105 19960126 00105 1996 1 26 96UAL900049 4 19960119 A 2565 SEAM PICO D29835193 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 2L SLIDE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7441U 16970877 21895 NR 2L EVACUATION SLIDE REMOVED FOR EXPIRATION OF TIME. SHOP FOUND MINOR SEAM LEAK ON THE TUBE DIRECTLY UNDER THE GIRT. REPAIRED SEAM LEAK, NON-STRUCTUAL. 2 L 7 3 4F 4 F A3WE E2EA 1996012600106 19960126 00106 NM 1996 1 26 96UAL900050 1 19960119 A 3350 CONNECTOR BOEING 737 737522 138449F NM CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 904UA 25004 EMERGENCY FLOOR MOUNTED ESCAPE LIGHTING INOP ROWS 15 TO 20. RECONNECTED FLOOR MOUNTED EMERGENCY ESCAPE LIGHTING AT ROWS 15 THROUGH 20 TO POWER SOURCE AND OPERATION CHECKS NORMAL. 2 L 7 2 4F RT A16WE 1996012600107 19960126 00107 WP 1996 1 26 MWEA96014 1 19960116 A 2560 5917689103 SLIDE COVER DOUG DC9 DC932 3022066 WP FWD GALLEY DOOR FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 203ME 47673 CREW REPORTS, FWD GALLEY DOOR EVACUATION SLIDE COVER CAME OFF. RESECURED GALLEY DOOR SLIDE COVER. 2 L 7 2 4F A6WE 1996012600108 19960126 00108 WP 1996 1 26 MWEA96015 1 19960118 A 7711 EPR SENSE LINE DOUG DC9 DC914 3022034 WP RIGHT ICED UP A MWEA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 31 600ME 45725 PILOT REPORTS LESS THAN MAX POWER INDICATION, RT ENG WENT TO 1.7 EPR WHILE LT ENGINE JUMPED TO 2.0 EPR AFTER A LAG IN SP OOL UP ON TAKEOFF. THE TAKEOFF WAS ABORTED. INSPECTED ALL EPR SENSE LINES, NO DISCREPANCIES NOTED. RAN BOTH ENGINES T O TAKEOFF POWER. FOUND BOTH INDICATIONS NORMAL WITH ANTI-ICE ON AND OFF. SUSPECT TEMPORARY ICING IN PT2 LINE. RETURNE D A/C TO SERVICE AND NO FURTHER PROBLEMS ON SUBSEQUENT FLIGHTS. 2 L 7 2 4F A6WE 1996012600109 19960126 00109 WP 1996 1 26 MWEA96016 1 19960118 A 4900 GRCP8598D APU DOUG DC9 DC932 3022066 WP AFT ACCESSORY INJESTED SPRAY A MWEA K NONE J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 31 204ME 47680 MKE - CREW REPORTS, AFTER LANDING THE LT LAV SMOKE DETECTOR SOUNDED. FLIGHT ATTENDANTS REPORT SMELLING FUEL FUMES AND T HE CABIN SLIGHTLY CLOUDED. RAN BOTH PACKS ON GROUND AND COULD NOT DUPLICATE SMOKE OR FUMES IN CABIN. SMOKE DETECTOR O PS CHECK GOOD. SUBMITTER SUSPECTS SPRAY FROM TAXI INJESTED IN APU. RETURNED A/C TO SERVICE. 2 L 7 2 4F A6WE 1996012600110 19960126 00110 NM 1996 1 26 P5CA9600002 1 19960118 A 5320 ANGLE BOEING 747 747124 1384874 NM BS 840 BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND BROKEN ANGLE AT CONNECTING POINT TO CEILING SUPPORT CHANNEL BS 840 NEAR LBL 33. FABRICATED NEW ANGLE IAW SRM 53-1 0-21 AND INSTALLED IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996012600111 19960126 00111 NM 1996 1 26 P5CA9600003 1 19960118 A 5320 DOOR SILL BOEING 747 747124 1384874 NM CARGO DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND CRACK IN MAIN DECK SIDE CARGO DOOR SILL AT LOWER AFT END. REPAIRED CRACK IAW SRM 51-40-02. 2 L 7 4 4F A20WE 1996012600112 19960126 00112 NM 1996 1 26 P5CA9600004 1 19960118 A 5754 LE FLAP BOEING 747 747124 1384874 NM LT WING BENT A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEADING EDGE FLAP NR 10 OUTBOARD CORNER FOLDED AND BENT. REPAIRED IAW SRM 57-50-03 AND INSTALLED PER SRM 51-30-02 . 2 L 7 4 4F A20WE 1996012600113 19960126 00113 NM 1996 1 26 P5CA9600005 1 19960118 A 5730 SKIN BOEING 747 747124 1384874 NM WS 1336/1364 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL ONE CORROSION ON RIGHT WING UPPER SURFACE ABOVE WING FRONT SPAR BETWEEN STA WS 1336 AND 1364. CORROSION REM OVED IAW SRM 51-10-01 AND FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600114 19960126 00114 NM 1996 1 26 P5CA9600006 1 19960118 A 5730 SKIN BOEING 747 747124 1384874 NM WS 1392 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL ONE CORROSION ON RIGHT WING UPPER SURFACE ABOVE WING CENTER SPAR AROUND WS 1392. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600115 19960126 00115 NM 1996 1 26 P5CA9600007 1 19960118 A 5730 SKIN BOEING 747 747124 1384874 NM WS 1308/1336 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL ONE CORROSION ON RIGHT WING UPPER SURFACE ABOVE REAR SPAR BETWEEN WS 1308 AND 1336. REMOVED CORROSION IAW S RM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600116 19960126 00116 NM 1996 1 26 P5CA9600008 1 19960118 A 5730 SKIN BOEING 747 747124 1384874 NM WS 862-1000 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL ONE CORROSION ON RIGHT WING UPPER SURFACE ABOVE REAR SPAR BETWEEN WS 862 AND 1000. REMOVED CORROSION IAW SR M 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600117 19960126 00117 NM 1996 1 26 P5CA9600009 1 19960118 A 5730 SKIN BOEING 747 747124 1384874 NM WS 469.82 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL ONE CORROSION ON RIGHT WING UPPER SURFACE ABOVE REAR SPAR AT WS 469.82. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600118 19960126 00118 NM 1996 1 26 P5CA9600010 1 19960118 A 5730 SKIN BOEING 747 747124 1384874 NM WS 586.62 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL ONE CORROSION ON RIGHT WING UPPER SURFACE AROUND WING CENTER SPAR AT WS 586.62. REMOVED CORROSION IAW SRM 5 1-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600119 19960126 00119 NM 1996 1 26 P5CA9600011 1 19960118 A 5730 SKIN BOEING 747 747124 1384874 NM WS 323.82 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL ONE CORROSION ON RIGHT WING UPPER SURFACE BETWEEN STR 26 AND WING CENTER SPAR NEAR WING ROOT, WS 323.82. RE MOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600120 19960126 00120 NM 1996 1 26 P5CA9600012 1 19960118 A 5730 SKIN BOEING 747 747124 1384874 NM WS 1516-1548 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL ONE CORROSION ON RIGHT WING LOWER SURFACE NEAR FUEL TANK ACCESS BETWEEN WS 1548.20 AND 1516.60. REMOVED COR ROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600121 19960126 00121 NM 1996 1 26 P5CA9600013 1 19960118 A 5730 SKIN BOEING 747 747124 1384874 NM WS 917-1140 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL ONE CORROSION ON LEFT LOWER WING SURFACE AT FUEL TANK ACCESS BETWEEN WS 917 AND 1140. REMOVED CORROSION IAW SRM 51-10-01, TREATED IAW SRM 51-10-02. 2 L 7 4 4F A20WE 1996012600122 19960126 00122 NM 1996 1 26 P5CA9600014 1 19960118 A 5730 SKIN BOEING 747 747124 1384874 NM WS 642-669.5 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL ONE CORROSION ON LEFT WING LOWER SURFACE AROUND FUEL TANK ACCESS BETWEEN WS 642 AND 669.50. REMOVED CORROSI ON IAW SRM 51-10-01, TREATED AREA IAW SRM 51-10-02. 2 L 7 4 4F A20WE 1996012600123 19960126 00123 NM 1996 1 26 P5CA9600015 1 19960118 A 5330 SKIN BOEING 747 747124 1384874 NM FS 1840-1880 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL ONE CORROSION ON LEFT LOWER FUSELAGE BETWEEN BS 1840 AND 1880, STR 49. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600124 19960126 00124 NM 1996 1 26 P5CA9600016 1 19960118 A 5330 PANEL BOEING 747 747124 1384874 NM BS 1780 LOOSE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND BENT AND LOOSE RIVETS ON AFT CARGO DOOR SWITCH ACCESS PANEL, BS 1780 STR 35 TO 36. FABRICATED AND INSTALLED NEW P ANELS AND FASTENERS IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996012600125 19960126 00125 NM 1996 1 26 P5CA9600017 1 19960118 A 5230 HINGE BOEING 747 747124 1384874 NM CARGO DOOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL ONE CORROSION ON FWD DOOR UPPER HINGE CONNECTING TO FUS SKIN BS 560 TO 660. REMOVED CORROSION IAW SRM 51-10 -01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600126 19960126 00126 NM 1996 1 26 P5CA9600018 1 19960118 A 5230 HINGE BOEING 747 747124 1384874 NM CARGO DOOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL ONE CORROSION ON AFT CARGO DOOR UPPER HINGE CONNECTING TO FUS SKIN BS 1820 TO 1960. REMOVED CORROSION IAW S RM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600127 19960126 00127 NM 1996 1 26 P5CA9600019 1 19960118 A 5730 SKIN BOEING 747 747124 1384874 NM WS 917-1364 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL ONE CORROSION ON RIGHT WING LOWER SURFACE AROUND WING FUEL TANK ACCESS BETWEEN WS 917 AND 1364. REMOVED COR ROSION IAW SRM 51-10-01, TREATED AREA IAW SRM 51-10-02. 2 L 7 4 4F A20WE 1996012600128 19960126 00128 WP 1996 1 26 RRXA9600002 1 19960118 A 3260 RETRACT MECH DOUG DC8 DC863 302198A WP NLG DOORS MALFUNCTIONED A RRXA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 15 964R 46000 KDEN-KADY - FLT 109 - AFTER TAKEOFF, ON GEAR RETRACTION EXCESSIVE VIBRATION WAS FELT FROM NOSE AREA AND LOUD SOUND HEARD . AIRCRAFT RETURNED TO KDEN. MAINTENANCE FOUND THE NOSE GEAR DOORS DOWN. MAINTENANCE SECURED NOSE GEAR DOORS AND NO D EFECTS NOTED. 2 L 7 4 4F 4A25 1996012600129 19960126 00129 NE 1996 1 26 UPS505225 2 19960118 A 7200 ENGINE BOEING 757 75724APF 1384969 NM PWA 2037 PW2040 NE RIGHT FLAME-OUT A IPXA E ENGINE SHUTDOWN X ENGINE FLAMEOUT AP APPROACH 1 SO 01 434UP 25465 CREW REPORTED, RT ENGINE FLAMED-OUT ON APPROACH. REMOVED AND REPLACED RT ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 1996012600130 19960126 00130 NM 1996 1 26 96ZZZX302 1 19960102 A 3610 10610652 DUCT SEAL BOEING 727 727231 1384079 NM NR 3 STRUT FAILED A TWAA O OTHER J WARNING INDICATION CR CRUISE 1 CE 05 54354 21986 MCI - FLT 469 - DURING CRUISE, NR 3 STRUT OVERHEAT LIGHT ILLUMINATED. REMOVED AND REPLACED NR 3 STRUT DUCT SEAL, MFG PN 10-61065-2. OPERATIONAL CHECK NORMAL. CHECK C-1 - 4-28-95 - MCI. 2 L 7 3 4F A3WE 1996012600133 19960126 00133 WP 1996 1 26 96ZZZX305 1 19960104 A 3350 58222 BATTERY PACK DOUG DC9 DC941 302207N WP CABIN DISCHARGED A TWAA K NONE L NO TEST TX TAXI/GRND HDL 1 CE 05 935L 47603 STL - FLT 141 - DURING LANDING AND TAXI, THE EGRESS LIGHTS FLICKERED ON AND OFF. FOUND BATTERY PACK, MFG PN 5822-2, WEA K. REPLACED BATTERY PACK AND EGRESS LIGHT, OPERATION CHECKED NORMAL. CHECK C - 8-27-95 - STL. 2 L 7 2 4F A6WE 1996012600134 19960126 00134 WP 1996 1 26 96ZZZX306 1 19960104 A 2170 17946081 COALESCER BAG DOUG DC9 DC982 3022082 WP CABIN CONTAMINATED A TWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 CE 05 955U 49427 STL - FLT 99 - DURING APPROACH, SMOKE EMITTED INTO AFT CABIN AND COCKPIT. FOUND LEFT AND RIGHT COALESCER ELEMENTS, MFG PN 179460-8-1, CONTAMINATED. REPLACED LEFT AND RIGHT COALESCER ELEMENTS AND AIR CONDITIONING SYSTEM OPERATION CHECKED N ORMAL. CHECK C-2D - 10-17-95 - MCI. 2 L 7 2 4F A6WE 1996012600135 19960126 00135 WP 1996 1 26 96ZZZX307 1 19960108 A 3610 DUCT DOUG DC9 DC931 3022065 WP NR 1 ENGINE CRACKED A TWAA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 988Z 47134 STL - FLT 568 - AFTER TAKEOFF, NR 1 ENGINE FIREWARNING LIGHT ILLUMINATED. REMOVED AND REPLACED CRACKED 8TH STAGE DUCT. OPERATIONAL LEAK CHECK ACCOMPLISHED, NO LEAKS FOUND. OP-15 - 8-21-95 - STL. 2 L 7 2 4F A6WE 1996012600136 19960126 00136 WP 1996 1 26 96ZZZX308 1 19960107 A 2160 BAC18R2A CIRCUIT BREAKER DOUG DC9 DC931 3022065 WP TEMP CONTROL MALFUNCTIONED A TWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 992Z 47095 STL - FLT 298 - DURING CRUISE, HAD AN ELECTRICAL FLASH AND ODOR EMITTED FROM CIRCUIT BREAKER PANEL. FOUND CIRCUIT BREAK ER FOR FLIGHT DECK TEMPERATURE CONTROL WITH INTERNAL MALFUNCTION. REPLACED TEMPERATURE CONTROL CIRCUIT BREAKER, MFG PN BAC18R2A. FLIGHT DECK TEMPERATURE CONTROL CHECKED NORMAL. CHECK C - 6-19-95 - STL. 2 L 7 2 4F A6WE 1996012600137 19960126 00137 WP 1996 1 26 96ZZZX309 1 19960107 A 3260 CONNECTOR DOUG DC9 DC931 3022065 WP RT MLG DOOR SW LOOSE A TWAA O OTHER N FALSE WARNING AP APPROACH 1 CE 05 993Z 47082 STL - FLT 394 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, LANDING GEAR DOOR OPEN LIGHT REMAINED ON. VISUAL CHECK SHOWED LANDING GEAR DOORS TO BE CLOSED. FOUND PIN PUSHED BACK IN RIGHT GEAR DOOR SWITCH CONNECTOR. SECURED PIN IN RIGH T GEAR DOOR SWITCH CONNECTOR. LANDING GEAR DOOR OPERATION AND INDICATION CHECKED NORMAL. CHECK C - 8-11-95 - STL. 2 L 7 2 4F A6WE 1996012600138 19960126 00138 WP 1996 1 26 96ZZZX310 1 19960107 A 3231 LATCH DOUG DC9 DC931 3022065 WP LT MLG DOOR NOT LATCHED A TWAA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 993Z 47082 STL - FLT 541 - AFTER TAKEOFF, LANDING GEAR RETRACTION LEFT MLG UNSAFE LIGHT REMAINED ON. CYCLED LANDING GEAR AND LANDI NG GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED. FOUND LEFT MLG DOOR LATCH HOOK NOT LATCHING INTO POSITION. RIGGED DOOR L ATCH ROLLER ASSY. LANDING GEAR AND DOOR OPERATION AND INDICATION CHECKED NORMAL. CHECK C - 8-11-95 - STL. 2 L 7 2 4F A6WE 1996012600139 19960126 00139 EU 1996 1 26 96ZZZX311 1 19960110 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 414WF 9 414 DFW - FLT 3543 - FORWARD CABIN EMERGENCY FLOOR LIGHTS INOPERABLE. REPLACED BATTERY PACK AND POWER SUPPLY CHECKED GOOD. RETURNED TO SERVICE. REFERENCE OPERATOR CONTROL NR SIMA960103. 2 H 7 2 4T RT A53EU 1996012600147 19960126 00147 WP 1996 1 26 96ZZZX319 1 19960104 A 3150 SWITCH DOUG DC9 DC932 3022066 WP TAKEOFF WARNING DIRTY A VJ6A C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 11 904VJ 47377 PHL/PHL - FLT 545, CREW ADVANCED THROTTLES ON TAKEOFF AND GOT A TAKEOFF WARNING HORN AT APPROXIMATELY 15 KNOTS. CYCLED FLAPS AFTER CLEANING THE TAKEOFF WARNING SWITCH. NO DEFECTS NOTED. 2 L 7 2 4F A6WE 1996012600152 19960126 00152 NM 1996 1 26 BJNA96101 1 19960111 A 3350 SPLICE BOEING 737 737214 138446R NM CABIN FAILED A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 457TM 20156 OVERWING SEAT EMERGENCY LIGHT LEFT, INOPERATIVE. REPAIRED SPLICE AND OPS CHECK OK IAW 20-30-12 AND 30-51-0. (X) 2 L 7 2 4F A16WE 1996012600154 19960126 00154 WP 1996 1 26 HAL9601 1 19960102 A 3610 39271012 AUGMENTATION VLV DOUG DC9 DC951 3022051 WP LEFT LEAKING A HALA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 WP 13 669HA 10119 P2011 47654 INFORMATION FROM LOG PAGE 126945, 126946. HNL - FLT 534 - AFTER TAKEOFF, TAIL COMP. TEMP HI-LIGHT ON. PERFORMED ABNORM AL CHECK, LIGHT WENT OFF, RETURNED TO HNL. RAN ENGINES AT TAKEOFF POWER, FOUND LEFT AUGMENTATION VALVE LEAKING. NO LEA KS NOTED AT RIGHT AUGMENTATION VALVE. REPLACED LEFT AUGMENTATION VALVE AND CLAMPS. GROUND RUN AT TAKEOFF AND CLIMB POW ER SETTINGS. NO ABNORMAL WARNING LIGHTS ILLUMINATED. NO LEAKS FOUND. OK FOR SERVICE. OPERATIONS CHECK OK. (X) 2 L 7 2 4F A6WE 1996012600163 19960126 00163 WP 1996 1 26 ORJA96001 1 19960101 A 3246 26088911 WHEEL DOUG DC9 DC982 3022082 WP NR 3 MLG BROKEN A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 840RA 5202 49424 REMOVED NR 3 MAIN WHEEL ASSY DUE TO BROKEN TIE BOLT. REPLACED IAW MM 32. (X) 2 L 7 2 4F A6WE 1996012600165 19960126 00165 EU 1996 1 26 SIMA960082 1 19960108 A 3246 5009237 INNER WHEEL HUB 5010488 SAAB SF340 340B 7860101 EU NR 2 WHEEL CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 594MA 175 MAY931232 340B212 LAW - LAW SHOP - MAIN WHEEL ASSY, PN N5010488, SN MAY 93-1232, WAS REMOVED FROM AIRCRAFT FOR TIRE REPLACEMENT. DURING S HOP INSPECTION, 2 CRACKS (APPROX .50 INCH) WERE FOUND RUNNING ACROSS THE TIRE BEAD FLANGE AREA OF INNER HUB ASSY. PN 50 09237, SN AUG89-0900, INNER WHEEL HUB ASSY WAS REMOVED FROM SERVICE. (X) 2 L 7 2 4T RT A52EU 1996012600166 19960126 00166 EU 1996 1 26 SIMA960101 1 19960109 A 2612 899253 FIRE LOOP SAAB SF340 SF340A 7850100 EU NR 2 ENGINE MALFUNCTIONED A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 112AE 340A112 DFW - FLT 3511 - AFTER TAKEOFF, NR 2 ENGINE GIVES FALSE WARNINGS ON BOTH HANDLE AND CAPTAIN'S WARNING PANEL. AIRCRAFT T URNED BACK. MAINTENANCE INSPECTED AND REPLACED ENGINE FIRE LOOP. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1996012600167 19960126 00167 EU 1996 1 26 SIMA960102 1 19960109 A 2612 89905202 FIRE CNTRL UNIT SAAB SF340 SF340A 7850100 EU NR 2 ENGINE MALFUNCTIONED A SIMA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 112AE 0300 340A112 DFW - FLT 3633 - AFTER TAKEOFF, NR 2 ENGINE WARNING ACTIVATED. CREW RESPONDED BY PULLING THE T-HANDLE AND BLOWING A FIR E BOTTLE, THEY DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. THE FIRE LIGHT HAD EXTINGUISHED AND NO EMERGE NCY EVACUATION WAS PERFORMED. MAINTENANCE INITIAL INSPECTION SHOWED NO SIGN OF FIRE. REPLACED FIRE BOTTLE AND SQUIBB A ND FIRE CONTROL UNIT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1996012600168 19960126 00168 EU 1996 1 26 SIMA960103 1 19960110 A 3350 3012001 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 414WF 0853 414 DFW - FLT 3543 - FORWARD CABIN EMERGENCY FLOOR LIGHTS INOPERABLE. REPLACED BATTERY PACK AND POWER SUPPLY CHECKED GOOD. RETURNED TO SERVICE. REFERENCE OPERATOR CONTROL NR 96ZZZX311. (X) 2 H 7 2 4T RT A53EU 1996012600169 19960126 00169 EU 1996 1 26 SIMA960111 1 19960111 A 3350 3012001 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 270AT 811 270 OKC - EMERGENCY FLOOR PATH LIGHTING PORTIONS REMAIN ILUMINATED WHEN SYSTEM IS DISARMED. REPLACED EMERGENCY BATTERY PACK 73WL IAW MM 33-50-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1996012600170 19960126 00170 NM 1996 1 26 TWRA9601 1 19960104 A 4930 MA11A1173 FUEL VALVE ACT BOEING 747 747212B 1384886 NM APU INOPERATIVE A TWRA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 EA 15 616FF 21939 DURING FLIGHT, FUEL VALVE LIGHT ILLUMINATED FOR APU. FLIGHT ATTENDANT AT L5 DOOR NOTICED A FUEL SMELL. UPON LANDING, T HE FUEL VALVE WAS LOCKED OUT. THE ITEM WAS DEFERRED PER DDPG. RETURN FLIGHT TO MIAMI, NO FUEL SMELL WAS NOTICED. ON A RRIVAL AT JFK, INSPECTION CHECKED APU FUEL SHROUD FOR LEAKS, NONE FOUND. MAINTENANCE REPLACED FUEL VALVE ACTUATOR. OPS CHECK AND LEAK CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 4 4F A20WE 1996012600171 19960126 00171 NM 1996 1 26 W8PA960001 1 19960109 A 2740 AR7077M1 TRIM MOTOR BOEING 737 7373L9 1384470 NM EMPENNAGE DEFECTIVE A W8PA H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED AP APPROACH 1 NM 03 960WP 23331 CREW REPORTED ON APPROACH IN PATTERN AT 400 FEET, HORIZONTAL STABILIZER TRIM CONTINUED TO RUN IN NOSE DOWN POSITION, HAD TO DISCONNECT. MAINTENANCE REPLACED STABILIZER TRIM MOTOR PER MM 27-41-51. OPS CHECKED SYSTEM OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1996012600172 19960126 00172 NM 1996 1 26 W8PA960002 1 19960116 A 2797 WIRE BOEING 737 7373B7 1384580 NM E 3-2 RACK FAILED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 509AU 23384 FOUND CHAFED WIRE, W084-508-24 WHICH HAD ARCED ON 3-2 SHELF RACK. WIRE IS 2B VAC TO AUTOSTAT COMPUTER. REPAIRED WIRE W O84-508-24 AND ADDED ANTI-CHAFE MATERIAL TO WIRE BUNDLE AND EDGE OF E 3-2 RACK. (X) 2 L 7 2 4F RT A16WE 1996012600173 19960126 00173 WP 1996 1 26 9601169759 1 19960116 A 3350 21 BATTERYQXEA96000 DOUG DC9 DC941 302207N WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 759NW 47287 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES AND O PERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996012600174 19960126 00174 WP 1996 1 26 9601179868 1 19960115 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 777NC 47787 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 11 AND 15 INOPERATIVE. REPLACED BATTER IES AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996012600175 19960126 00175 WP 1996 1 26 9601189868 1 19960117 A 3350 SOCKET DOUG DC9 DC951 3022051 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 777NC 47787 DURING LINE MAINTENANCE INSPECTION, FOUND FIRST CLASS SECTION FOR FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. REPLACE D LIGHT SOCKET AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996012600176 19960126 00176 WP 1996 1 26 9601199151 1 19960116 A 3350 60030451 BATTERY PACK DOUG DC9 DC914 3022034 WP TAILCONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8909E 45770 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS ABOVE TAILCONE SLIDE INOPERATIVE. REPLACED BATTERY PACK AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996012600177 19960126 00177 NM 1996 1 26 9601202710 1 19960117 A 3350 LIGHT BOEING 727 727225 1384077 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 820EA 22557 DURING PREFLIGHT, FOUND RED EXIT CUE LIGHT INOPERATIVE AT ROW 17. REPLACED LIGHT MODULE 17D AND CHECKED OK. 2 L 7 3 4F A3WE 1996012600178 19960126 00178 WP 1996 1 26 9601219139 1 19960116 A 3350 113317 BATTERY PACK DOUG DC9 DC914 3022034 WP PAX DOOR SLIDE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 948L 38440 3275 47049 DURING PERIODIC CHECK, EMERGENCY BATTERY PACK FOR MAIN CABIN DOOR EVACUATION SLIDE FAILED TEST. REPLACED SLIDE. 2 L 7 2 4F A6WE 1996012600179 19960126 00179 WP 1996 1 26 9601229753 1 19960117 A 3260 DOOR SWITCHES DOUG DC9 DC941 302207N WP MAIN GEAR DIRTY A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 753NW 47117 MEM-PHL - DURING CLIMBOUT, LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. RECYCLED GEAR AND NORMAL INDICATIONS WERE ACHIEVED. FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. CLEANED MAIN LANDING GEAR DOOR SWITCHES. OPERATIONAL CHECK NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996012600180 19960126 00180 WP 1996 1 26 9601239967 1 19960120 A 7711 EPR INDICATION DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9A 52048 NE NR 1 ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 9331 47263 657496 AS TAKEOFF POWER WAS APPLIED, THE NR 1 ENGINE EPR INDICATION STARTED DECREASING. THE TAKEOFF WAS ABORTED AND THE AIRCRA FT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE ENGINE AND WARMED THE FUEL CONTROL UNIT WITH AN EXTERNAL HEAT SOURCE . NO DISCREPANCIES WERE NOTED AND AIRCRAFT CONTINUED IN SERVICE. 2 L 7 2 4F 4 F A6WE E2EA 1996012600181 19960126 00181 WP 1996 1 26 96FDEA00103 1 19960120 A 5512 SKIN DOUG DC10 DC1010 3022110 WP HORIZ STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68049 47803 TWO CRACKS FOUND AT L/E OF LT STABILIZER UPPER SKIN PANEL, AT CLOSING RIB AREA STA XE = 28.426, XFS = 86.616. CRACKS AR E APPROX .25 INCH AND 2.0 INCH IN LENGTH. REPAIRED AS PER EO 8-5510-7-3312 PART 4 AND SRM 55-20-00. 2 L 7 3 4F A22WE 1996012600182 19960126 00182 WP 1996 1 26 96FDEA00104 1 19960118 A 5720 APB70801 ANGLE DOUG DC10 DC1010 3022110 WP WING CENTER SECT CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 L/LT WW FWD BULKHEAD TOP OF WING CENTER BOX SECTION, REMOVABLE PANEL HAS HEAVY CORROSION, APPROX 10 INCHES O/B OF VERTIC AL KEEL BEAM WEB. REMOVED CORRODED ANGLE, CLEANED, TREATED AND PRIMED UPPER WING SURFACE THAT MATES WITH ANGLES REF 51- 00 VOL 11 SRM, OK TO INSTALL ANGLE. INSTALLATION COMPLETED AS PER SRM 53-00-01. 2 L 7 3 4F A22WE 1996012600183 19960126 00183 WP 1996 1 26 96FDEA00105 1 19960120 A 5511 SPAR CAP DOUG DC10 DC1010 3022110 WP HORIZ STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 CRACK IN HORIZONTAL STABILIZER OUTER RT SECTION, UPPER AFT SPAR CAP AFT BARREL NUT HOLE ADJACENT TO OPERATING BULKHEAD. CRACK MEASURES .3125 INCH INTO HOLE AND THEN PROGRESSES FWD .3750 INCH LONG. CRACK WAS REWORKED PER AN ELLIPTICAL SHAP E AND CALCULATED, AREA EQUALS .387 SQ PER S/B A55118 A MAXIMUM OF .92 IS ALLOWED. 2 L 7 3 4F A22WE 1996012600185 19960126 00185 NM 1996 1 26 96FDEA00107 1 19960117 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 440 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 487FE 21490 UPPER LOBE STR 3L STA 440 CRACKED. INSTALLED REPAIR ON STR 3L STA 440 PER MM 53-10-3 PG 5 WITH FAB PARTS ON SHOP ORDER FE7X, FM7K, FM69. 2 L 7 3 4F A3WE 1996012600186 19960126 00186 NM 1996 1 26 96FDEA00108 1 19960116 A 5330 SKIN BOEING 727 727227 1384078 NM BS 720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 487FE 21490 FWD CARGO FUSELAGE SKIN CORRODED BETWEEN STR 28 LT AND RT STA 720C PLUS 5. CUT OUT CORRODED AREA AND INSTALLED DOUBLER PER SRM 53-30-3. 2 L 7 3 4F A3WE 1996012600187 19960126 00187 NM 1996 1 26 96FDEA00109 1 19960122 A 5347 BAC1510190 SEAT TRACK BOEING 727 727227 1384078 NM BS 950 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 488FE 21491 CORROSION (C53-224-04), ON SEAT TRACK AT CLIP NUTHOLES BS 950E PLUS 18 RBL 1. REPLACED SEAT TRACK AND INSTALLED REPAIR STRAP IAW FEDEX SRM 53-10-05. 2 L 7 3 4F A3WE 1996012600188 19960126 00188 WP 1996 1 26 ABXA9600036 1 19960119 A 3260 MS25231313 BULB DOUG DC8 DC863 302198A WP GEAR INDICATOR FAILED A ABXA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 23 820AX 46155 DURING LANDING GEAR EXTENSION, LEFT MAIN LANDING GEAR LIGHT DID NOT ILLUMINATE. ABNORMAL LANDING GEAR PROCEDURES WERE C OMPLETED. REPLACED LIGHT BULBS FOR THE LEFT MAIN LANDING GEAR INDICATOR AND THE BULBS ILLUMINATED DURING NEXT LANDING G EAR EXTENSION. 2 L 7 4 4F 4A25 1996012600189 19960126 00189 SO 1996 1 26 COMA9610028 1 19960115 A 2750 3471001001 ANNUNICATOR PNL EMB 120 EMB120RT SO TE FLAPS MALFUNCTIONED A COMA O OTHER N FALSE WARNING TO TAKEOFF 1 SO 01 162CA 7659 2083 120150 DURING TAKEOFF, RECEIVED FLAP CONTROL FAULT WARNING. REPLACED THE FLAP ANNUNCIATOR PANEL. 2 L 7 2 4T RT A31SO 1996012600190 19960126 00190 SO 1996 1 26 COMA9610029 1 19960116 A 3230 20885 UPLOCK ACTUATOR EMB 120 EMB120RT SO LT MLG FAILED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 259CA 10790 768 120252 LT MAIN LANDING GEAR A-SYSTEM INTRANSIT INDICATOR REMAINED ON WHEN GEAR SELECTED DOWN. CYCLED GEAR WITH SAME RESULTS. R EPLACED THE LT MLG UPLOCK ACTUATOR. 2 L 7 2 4T RT A31SO 1996012600191 19960126 00191 SO 1996 1 26 COMA9610030 1 19960114 A 6120 8210181 PUMP EMB 120 EMB120RT SO LT PROP DEFECTIVE A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 256CA 4639 1673 120245 LEFT ENGINE PROPELLER WILL NOT UNFEATHER. REPLACED THE PROPELLER OVERSPEED GOVERNOR OIL PUMP. 2 L 7 2 4T RT A31SO 1996012600192 19960126 00192 SO 1996 1 26 COMA9610031 1 19960118 A 5230 12023348005 DOOR SEAL EMB 120 EMB120RT SO CARGO COMPT LOOSE A COMA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 01 244CA 120217 CABIN PRESSURIZATION FAILED DURING FLIGHT. REPLACED CARGO DOOR SEAL WHICH HAD COME LOOSE. 2 L 7 2 4T RT A31SO 1996012600193 19960126 00193 SO 1996 1 26 COMA9610032 1 19960118 A 2730 ATG120TR PROX SENSOR EMB 120 EMB120RT SO ELEVATOR DEFECTIVE A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 267CA 120259 TRIM AURAL WARNING SOUNDS WHEN POWER LEVERS ADVANCED. REPLACED THE ELEVATOR TRIM PROXIMITY SENSORS. 2 L 7 2 4T RT A31SO 1996012600194 19960126 00194 EU 1996 1 26 COMA9630018 1 19960117 A 2613 004WS00 WEU SAAB SF340 SF340A 7850100 EU AVIONICS MALFUNCTIONED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 358CA 12117 223 340A047 DURING TAKEOFF, LEFT ENGINE TAIL PIPE HOT WARNING CAME ON. REPLACED THE WARNING ELECTRONIC UNIT. 2 L 7 2 4T RT A52EU 1996012600195 19960126 00195 EA 1996 1 26 COMA9660016 1 19960117 A 3230 16600101 UPLOCK ASSY CNDAIR CL600 CL6002B19 EA NLG MALFUNCTIONED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 948CA 853 7079 DURING APPROACH, WHEN LANDING GEAR SELECTED DOWN, THE NLG INDICATED UNSAFE. COULD NOT DUPLICATE DISCREPANCY. REPLACED THE NLG UPLOCK ASSY FOR TROUBLESHOOTING. 2 L 7 2 4F RT A21EA 1996012600196 19960126 00196 WP 1996 1 26 DHL96801007 1 19960118 A 2710 H654 PRESS SWITCH DOUG DC8 DC873 302199C WP AILERON PCU INTERMITTENT A T DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 801DH 46033 AILERON MANUAL CONTROL LIGHT ILLUMINATED AFTER TAKEOFF. ABNORMAL PROCEDURES FOLLOWED. REPLACED AILERON PCU PRESSURE SW ITCH PER M/M 27-10 AND OPS CHECK OK. 2 L 7 4 4F RT 4A25 1996012600197 19960126 00197 WP 1996 1 26 MWEA96017 1 19960119 A 2560 3952273501 GIRT BAR LATCH DOUG DC9 DC915 3022036 WP PAX DOOR LACK OF LUBE A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 300ME 45718 CREW REPORTS, AMIN ENTRANCE DOOR GIRT BAR LATCH VERY DIFFICULT TO OPERATE. CLEANED, LUBED LATCHES AND RESHIMMED FOR MOR E CARPET CLEARANCE. 2 L 7 2 4F A6WE 1996012600198 19960126 00198 WP 1996 1 26 MWEA96018 1 19960119 A 2530 50226 OVEN DOUG DC9 DC932 3022066 WP FWD GALLEY MALFUNCTIONED A MWEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 31 203ME 47673 CREW REPORTS, CIRCUIT BREAKER FOR LEFT OVEN POPPED. RESET CB, POPPED AGAIN. F/A REPORTS, SMELLING ELECTRICAL SMOKE. R EPLACED OVEN AND OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996012600199 19960126 00199 NM 1996 1 26 P5CA9600020 1 19960117 A 2730 CONTROL RODS BOEING 747 747122 1384872 NM ELEVATOR DISCONNECT A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 DURING GROUND CHECK, FOUND BOTH OUTBOARD ELEVATOR RODS DISCONNECTED. RECONNECTED AND PERFORMED OPERATIONAL CHECK IAW MM 27-31-02. INVESTIGATING TO DETERMINE WHY DISCONNECTED. 2 L 7 4 4F A20WE 1996012600200 19960126 00200 NM 1996 1 26 P5CA9600021 1 19960120 A 3610 69B401186 DUCT BOEING 747 747122 1384872 NM NR 2 PYLON CRACKED A P5CA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 854FT 19754 AFTER ENGINE START, WING LEADING EDGE OVERHEAT LIGHT ILLUMINATED. FLIGHT RETURNED TO BLOCKS. FOUND LEADING EDGE PNEUMA TIC DUCT INBOARD OF NR 2 ENGINE CRACKED. REPLACED DUCT ASSEMBLY, INSPECTED AND LEAK CHECKED IAW MM 36-10-00. 2 L 7 4 4F A20WE 1996012600201 19960126 00201 NE 1996 1 26 P5CA9600022 2 19960120 A 7321 FUEL CONTROL BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 4 ENGINE MALFUNCTIONED A P5CA A E UNSCHED LANDING ENGINE SHUTDOWN X ENGINE FLAMEOUT CL CLIMB 1 WP 23 852FT 19757 662276 NR 4 ENGINE FLAME-OUT AT 29,000 FT, ATTEMPTED ENGINE RESTART, UNSUCCESSFUL. FLIGHT RETURNED TO MIAMI. REPLACED FCU, FU EL PUMP, TT2 SENSOR IAW MM 73-11 01 AND 73-21 01. LEAK CHECK AND RUNUP OK. 2 L 7 4 4F 4 F A20WE E20EA 1996012600203 19960126 00203 NM 1996 1 26 SWAA960031 1 19960114 A 3241 39353 ANTI-SKID VALVE BOEING 737 7372H4 138448C NM RT MLG MALFUNCTIONED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 81SW 22730 AFTER GEAR RETRACTION, UPON GEAR HANDLE BEING POSITIONED TO OFF, INBOARD GEAR ANTI-SKID LIGHT ILLUMINATED. LIGHT EXTING UISHES WITH HANDLE IN UP OR DOWN POSITIONS. AIRCRAFT DIVERTED TO BNA AND MADE AN UNEVENTFUL LANDING. AT HOU, REPLACED RT INBOARD ANTI-SKID VALVE PER BOEING M/M. 2 L 7 2 4F A16WE 1996012600204 19960126 00204 NM 1996 1 26 SWAA960032 1 19960117 A 5312 BRACKET BOEING 737 7372T4 1384492 NM BS 351.2 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED MAINT CHECK, FOUND BULKHEAD AT BS 351.2 ATTACH BRACKET CRACKED ON LEFT SIDE. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996012600205 19960126 00205 NM 1996 1 26 SWAA960033 1 19960117 A 5320 SPLICE BOEING 737 7372T4 1384492 NM BS 947.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED MAINT CHECK, FOUND STRINGER SPLICE AT S27L CORRODED AT BS 947.5 AND 967. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996012600206 19960126 00206 NM 1996 1 26 SWAA960034 1 19960117 A 5320 WEB BOEING 737 7372T4 1384492 NM BS 294 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED MAINT CHECK, FOUND WEB FWD FLANGE TO FRAME CRACKED AT S7L AT BS 294. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996012600207 19960126 00207 NM 1996 1 26 UPS405244 1 19960119 A 3350 LIGHT BOEING 747 747123 1384873 NM CABIN DOOR INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 675UP 20390 MAINTENANCE REPORTED, CABIN DOOR EMERGENCY LIGHT INOP. CLEANED CONTACTS, OPS CHECK OK. 2 L 7 4 4F A20WE 1996012600277 19960126 00277 NE 1996 1 26 96ZZZX324 2 19960105 A 7200 ENGINE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE RIGHT MALFUNCTIONED A MASA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 01 432AW 7374 286 PCE123226 AIRCRAFT DEPARTED GJT. WHEN THE ENGINE BLEEDS WERE SELECTED ON, THE CABIN AND COCKPIT BEGAN TO FILL WITH SMOKE. THE AI RCRAFT RETURNED TO GJT. AFTER TROUBLESHOOTING AND A TEST FLIGHT, IT WAS DETERMINED THE NR 2 ENGINE WAS LEAKING OIL INTE RNALLY INTO THE BLEED AIR SYSTEM. THE TURBOMACHINE WAS REPLACED. GROUND RUNS AND ANOTHER TEST FLIGHT WERE PERFORMED WI TH NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 1996012600287 19960126 00287 EU 1996 1 26 96ZZZX334 1 19960103 A 3260 INTRANSIT LIGHT BAG JETSTM JETSTM3101 1500215 EU LT MLG MALFUNCTIONED A VNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 838JS 741 FLT 4091 - AFTER TAKEOFF, AFTER LANDING GEAR WAS RETRACTED, LEFT MLG INTRANSIT LIGHT REMAINED ILLUMINATED. AIRCRAFT RET URNED TO FIELD, LANDED WITHUT FURTHER INCIDENT. PIT MAINTENANCE JACKED THE AIRCRAFT, CONDUCTED A GEAR SWING, UNABLE TO DUPLICATE THE PROBLEM. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A21EU 1996012600293 19960126 00293 EU 1996 1 26 96ZZZX340 1 19960105 A 3350 321454 BATTERY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 634AW 0585 091 PHX - FLT 0815 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS INOP AT LT MID-SHIP. PER T.S.M., REPLACED POW ER SUPPLY. FIRST UNIT BAD FROM STOCK AND THEN BATTERY WAS DEAD. SWAPPED BATTERY PACK FROM RT SIDE WITH NEW POWER SUPPL Y. LIGHTS OPERATE NORMALLY. MID-LEFT EMERGENCY LIGHT BATTERY, 3214-54. MID-RIGHT EMERGENCY LIGHT BATTERY, 3214-54. M ID-RIGHT EMERGENCY LIGHT BATTERY, 3214-54. STC SA 3432NM. REFERENCE OPERATOR CONTROL NR AWXA96003, AND NR 96ZZZX341. ( X) 2 L 7 2 4F RT A28NM 1996012600294 19960126 00294 EU 1996 1 26 96ZZZX341 1 19960105 A 3350 321454 BATTERY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 634AW 6155 091 PHX - FLT 0815 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS INOP AT LT MID-SHIP. PER T.S.M., REPLACED POW ER SUPPLY. FIRST UNIT BAD FROM STOCK AND THEN BATTERY WAS DEAD. SWAPPED BATTERY PACK FROM RT SIDE WITH NEW POWER SUPPL Y. LIGHTS OPERATE NORMALLY. MID-LEFT EMERGENCY LIGHT BATTERY, 3214-54. MID-RIGHT EMERGENCY LIGHT BATTERY, 3214-54. M ID-RIGHT EMERGENCY LIGHT BATTERY, 3214-54. STC SA 3432NM. REFERENCE OPERATOR CONTROL NR AWXA96003, AND NR 96ZZZX340. ( X) 2 L 7 2 4F RT A28NM 1996012600308 19960126 00308 EU 1996 1 26 AWXA96003 1 19960105 A 3350 321454 BATTERY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 634AW 3414 091 PHX - FLT 0815 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS INOP AT LT MID-SHIP. PER T.S.M., REPLACED POW ER SUPPLY. FIRST UNIT BAD FROM STOCK AND THEN BATTERY WAS DEAD. SWAPPED BATTERY PACK FROM RT SIDE WITH NEW POWER SUPPL Y. LIGHTS OPERATE NORMALLY. MID-LEFT EMERGENCY LIGHT BATTERY, 3214-54. MID-RIGHT EMERGENCY LIGHT BATTERY, 3214-54. M ID-RIGHT EMERGENCY LIGHT BATTERY, 3214-54. STC SA 3432NM. REFERENCE OPERATOR CONTROL NR 96ZZZX340, AND NR 96ZZZX341. ( X) 2 L 7 2 4F RT A28NM 1996012600321 19960126 00321 NM 1996 1 26 IXKA960001 1 19960102 A 5753 TORQUE TUBE BOEING 727 727251 138408H NM TE FLAPS LOOSE A A IXKA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 25 259US 19978 ATL/MDW - FLT 59 - INBOARD FLAPS WOULD NOT RETRACT ABOVE 15 DEGREES. AIR TURN BACK TO ATL. ON SYSTEM OPS AND INSPECTIO N, FOUND FLAPS IN BYPASS MODE. RESET ASSYMETRY. FOUND LOOSE TORQUE TUBE COUPLING AT OUTBOARD FLAP POWER CONTROL UNIT. SECURED LOOSE TORQUE TUBE COUPLING, RETORQUED SCREWS. OPS CHECK OK PER 27-51-01. (X) 2 L 7 3 4F A3WE 1996012600322 19960126 00322 NM 1996 1 26 P9IA096002 1 19960117 A 4980 4353919M EXHAUST CLAMP BOEING 727 727231 1384079 NM APU FAILED A P9IA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 03 12305 63828 19562 DURING GROUND OPERATION OF APU, THE FIRE WARNING ACTIVATED AND THE APU AUTO SHUT DOWN WITH SMOKE COMING OUT OF THE APU S HROUD. INSPECTION FOUND CLAMP BROKEN FOR INNER EXHAUST DUCT AT SPOT WELD. INSPECTED APU, NO OTHER DAMAGE NOTED. REPLA CED O-RING AND CLAMP. RUN AND OPS CHECKS GOOD, MM 49-00. (X) 2 L 7 3 4F A3WE 1996012600325 19960126 00325 EU 1996 1 26 SIMA960051 1 19960104 A 3350 BATTERY PACK SAAB SF340 SF340A 7850100 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 107AE 340A107 ACT - FLT 3906 - FORWARD EMERGENCY SIGN LIGHTS INOPERABLE. FOUND ON CREW PREFLIGHT INSPECTION. REPLACED BATTERY PACK. SYSTEM OPS CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1996012600326 19960126 00326 EU 1996 1 26 SIMA960091 1 19960108 A 3350 3012007 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 377AT 210 377 DFW - FLT 3819 - CENTER AIRCRAFT EMERGENCY LIGHTS STAYED ON ALL THE TIME. MAINTENANCE REPLACED THE NR 2 BATTERY PACK. O PS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1996012600329 19960126 00329 NE 1996 1 26 UIEA9601 2 19960107 A 7261 RR34150G SCAVENGE PUMP BOEING 747 747230B 1384889 NM GE CF6 CF650E2 30018 NE NR 1 ENGINE FAILED A UIEA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 EA 15 508MC 57603 11373 21644 530288 BANKOK/TAIPEI, CI346/07 - EN ROUTE, INCURRED NR 1 ENGINE SHUT DOWN IN FLIGHT-DESCENT PHASE FOR LOSS OF OIL PRESSURE AND N2 RPM. ON ARRIVAL, CHECKED MAIN OIL SCREEN AND CHIP DETECTORS ALL OK. FOUND LUBE AND OIL SCAVENGE PUMP DRIVE SHAFT SH EARED. DRAINED ENGINE OIL, REPLACED SCAVENGE PUMP, SERVICED ENGINE. ENGINE RUN-UP, OPS CHECK OK. (X) 2 L 7 4 4F 4 F A20WE E23EA 1996012600330 19960126 00330 WP 1996 1 26 9601259933 1 19960121 A 3222 STRUT DOUG DC9 DC931 3022065 WP NLG REQD SERVICE A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 133U 47280 DURING CLIMB, THE AIRCRAFT DID NOT SHIFT INTO FLIGHT MODE. RECYCLED LANDING GEAR AND AIRCRAFT SHIFTED INTO FLIGHT MODE. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. SERVICED NOSE GEAR STRUT, CLEANED GROUND SENSING SWITC HES AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600331 19960126 00331 WP 1996 1 26 9601269967 1 19960120 A 2421 GENERATOR DOUG DC9 DC931 3022065 WP LT ENGINE FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 GL 01 9331 47263 DURING TAKEOFF, THE GLIDESCOPE, SPEED COMMAND AND COMPASS FLAGS CAME ON. ALSO, THE NR 1 EPR GAUGE INDICATOR STARTED TO DECREASE. ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACED THE LEFT ENGINE GENERATOR, CONSTANT SPEED DRIVE AND CONST ANT SPEED DRIVE OIL COOLER. FLUSHED AND CLEANED LINES AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600332 19960126 00332 1996 1 26 9601279982 4 19960119 A 3418 80098717 AOA TRANSDUCER DOUG DC9 DC932 3022066 WP NR 2 FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 982US 39501 210 45790 DURING CLIMB, THE STALL INDICATION WARNING LIGHT ILLUMINATED. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND LIGHT RE MAINED ILLUMINATED MOMENTARILY, THEN EXTINGUISHED. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE NR 2 ANGLE OF ATTACK TRANSDUCER AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600333 19960126 00333 WP 1996 1 26 9601289911 1 19960119 A 3231 RETRACT MECH DOUG DC9 DC931 3022065 WP NLG DOOR MALFUNCTIONED A NWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 01 961N 47405 DURING TAKEOFF, A VIBRATION WAS DETECTED FROM THE NOSE WHEEL. AIRCRAFT CONTINUED TAKEOFF AND RETURNED TO MSP LANDING WI THOUT INCIDENT. FOUND RIGHT NOSE LANDING GEAR DOOR OPEN. SECURED DOOR AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600334 19960126 00334 WP 1996 1 26 9601299954 1 19960119 A 3230 CONTROL VALVE DOUG DC9 DC931 3022065 WP LANDING GEAR ICED UP A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 921RW 47164 DURING CLIMB, THE LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO DAY AND LANDED WITHOUT INCIDENT. FOUND ICE ON L ANDING GEAR CONTROL VALVE. REMOVED ICE AND OPERATIONAL CHECK OF LANDING GEAR SYSTEM GOOD. 2 L 7 2 4F A6WE 1996012600335 19960126 00335 WP 1996 1 26 9601309954 1 19960119 A 3230 SHIFT MECH DOUG DC9 DC931 3022065 WP LANDING GEAR ICED UP A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 921RW 47164 DURING CLIMB, THE LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO DAY AND LANDED WITHOUT INCIDENT. FOUND ICE AND SNOW ON GROUND SHIFT MECHANISM. REMOVED SNOW AND ICE, OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600336 19960126 00336 WP 1996 1 26 9601319994 1 19960121 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP TAILCONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8979E 47328 DURING LINE CHECK, FOUND TAILCONE EMERGENCY LIGHT INOPERATIVE. REPLACED THE BATTERY PACK AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600337 19960126 00337 WP 1996 1 26 9601329986 1 19960121 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 986US 47480 DURING LINE CHECK, FOUND OVERHEAD EMERGENCY LIGHTS INOPERATIVE AT ROWS 5 TO 11. REPLACED BATTERIES AND OPERATIONAL CHEC K GOOD. 2 L 7 2 4F A6WE 1996012600338 19960126 00338 WP 1996 1 26 9601339972 1 19960121 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9336 47338 DURING LINE CHECK, FOUND CEILING AND MID CABIN EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES AND OPERATIONAL CH ECK GOOD. 2 L 7 2 4F A6WE 1996012600339 19960126 00339 WP 1996 1 26 9601349957 1 19960121 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP LT/RT NACELLE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 915RW 47139 DURING LINE CHECK, FOUND LEFT AND RIGHT NACELLE EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY, OPERAT IONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600340 19960126 00340 WP 1996 1 26 9601359917 1 19960121 A 3350 LIGHT DOUG DC9 DC932 3022066 WP DOOR 1L INTERMITTENT A NWAA K NONE L NO TEST CR CRUISE 1 GL 01 967N 47573 DURING CRUISE, THE FORWARD EMERGENCY LIGHTS ILLUMINATED INTERMITTENTLY. REPLACED THE POWER SUPPLY, BATTERIES AND THE EM ERGENCY EXIT SIGN AT DOOR 1L. OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600341 19960126 00341 WP 1996 1 26 9601369907 1 19960121 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 957N 47253 DURING LINE CHECK, FOUND AFT INTERIOR OVERWING EMERGENCY LIGHTS INOPERATIVE. RESET BATTERY PACK AND OPERATIONAL CHECK G OOD. 2 L 7 2 4F A6WE 1996012600342 19960126 00342 WP 1996 1 26 9601379902 1 19960121 A 3350 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 952N 47073 DURING LINE CHECK, FOUND AFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERIES AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600343 19960126 00343 WP 1996 1 26 9601389998 1 19960120 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8934E 47143 DURING LINE CHECK, FOUND AFT CENTER CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND OPERATIONAL CHECK G OOD. 2 L 7 2 4F A6WE 1996012600344 19960126 00344 NM 1996 1 26 9601396601 1 19960119 A 2910 HYD SWIVEL BOEING 747 747151 1384891 NM RT MLG BROKEN A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 601US 19778 DURING CLIMB, AIRCRAFT LOST HYDRAULIC QUANTITY ON THE NR 4 HYDRAULIC SYSTEM, WHEN THE LANDING GEAR WAS RETRACTED. AIRCR AFT RETURNED TO NRT AND LANDED WITHOUT INCIDENT. FOUND BROKEN SWIVEL JOINT ON THE RIGHT WING LANDING GEAR DOWNLOCK ACTU ATOR. REPLACED ADP AND EDP ASSEMBLIES. REPLACED CASE DRAIN AND PRESSURE FILTER FOR ADP/EDP. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996012600345 19960126 00345 WP 1996 1 26 9601409876 1 19960118 A 3231 DOOR LINKS DOUG DC9 DC951 3022051 WP NLG FAILED A NWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 01 785NC 48110 DURING CLIMB, A VIBRATION WAS FELT FROM THE NOSE LANDING GEAR AREA ON GEAR RETRACTION. FLIGHT RETURNED TO MSP AND LANDE D WITHOUT INCIDENT. REPLACED BOTH NOSE GEAR DOOR LINKS. OPERATIONAL CHECK NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996012600346 19960126 00346 WP 1996 1 26 9601419856 1 19960120 A 3350 60030451 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 765NC 47718 DURING LINE MAINTENANCE INSPECTION, FOUND AFT OVERWING EMERGENCY EXIT SIGN LIGHT INOPERATIVE. REPLACED BATTERY PACK AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996012600347 19960126 00347 NM 1996 1 26 9601422761 1 19960120 A 2131 CONTROLLER BOEING 727 7272M7 138407S NM CABIN FAILED A NWAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 01 721RW 21200 DURING FLIGHT, LOST CABIN PRESSURE AT FL 350. AN EMERGENCY DESCENT TO 8,000 FEET WAS MADE, LAST 150 MILES FLOWN AT 8,00 0 FEET. AIRCRAFT LANDED WITHOUT INCIDENT AT MSP. PERFORMED PRESSURIZATION LEAK CHECK. REPLACED AUTO PRESSURE CONTROLL ER AND CONTROL PANEL. PERFORMED FUNCTIONAL CHECK AND SYSTEM OK FOR SERVICE. 2 L 7 3 4F A3WE 1996012600348 19960126 00348 NM 1996 1 26 96FDEA00111 1 19960120 A 5330 SKIN BOEING 727 727233 138408A NM BS 1073 CREASED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 BS 1973 STR 19 TO 20L, THERE IS A SHARP CREASE IN SKIN. REMOVED DAMAGE AT BS 1073 STR 19 TO 20L IN SKIN. FABRICATED AN D INSTALLED REPAIR PARTS PER FEDEX SRM 53-30-3. 2 L 7 3 4F RT A3WE 1996012600349 19960126 00349 NM 1996 1 26 96FDEA00112 1 19960120 A 5330 SKIN BOEING 727 727233 138408A NM BS 1030-1050 CREASED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 BS 1030 TO 1050, STR 20 TO 21L SKIN IS CREASED. REMOVED DAMAGE AT BS 1030 TO 1050, STR 20 TO 21L IN SKIN. FABRICATED A ND INSTALLED REPAIR PARTS PER FEDEX SRM 53-30-3. 2 L 7 3 4F RT A3WE 1996012600350 19960126 00350 NM 1996 1 26 96FDEA00113 1 19960122 A 5330 SKIN BOEING 727 727233 138408A NM BS 1050-1056 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 FIVE DENTS IN SKIN STA 1050 TO 1056, STR 28 TO 29R. REPAIRED SKIN IAW FEDEX SRM 53-30-3. 2 L 7 3 4F RT A3WE 1996012600351 19960126 00351 NM 1996 1 26 96FDEA00114 1 19960120 A 5313 BAC1498138 STRINGER BOEING 727 727233 138408A NM BS 620 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 MECHANICAL DAMAGE IN HAT SECTION OF STRINGER, AT BS 620 STR 4R. REMOVED DAMAGED SECTION STRINGER 4R BS 620, FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 53-10-3. 2 L 7 3 4F RT A3WE 1996012600352 19960126 00352 NM 1996 1 26 96FDEA00115 1 19960120 A 5313 BAC1498138 STRINGER BOEING 727 727233 138408A NM BS 460 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 GOUGE ON STRINGER AT BS 460 STR 3R. REMOVED DAMAGED SECTION STR 3R BS 460, FABRICATED AND INSTALLED REPAIR PARTS PER FE DEX SRM 53-10-3. 2 L 7 3 4F RT A3WE 1996012600353 19960126 00353 NM 1996 1 26 96FDEA00116 1 19960123 A 3610 322861001 VALVE BOEING 727 72725C 138400H NM LT/RT DAMAGED A FDEA K NONE O OTHER UK UNKNOWN 1 SO 25 116FE 19298 BOTH LT AND RT PURGE SHUTOFF VALVES PHYSICALLY DAMAGED, ENDS BLOWN OFF. REMOVED AND REPLACED VALVES, LT-12231, RT-C6419 8. 2 L 7 3 4F A3WE 1996012600354 19960126 00354 NM 1996 1 26 96FDEA00117 1 19960108 A 5711 SPAR BOEING 747 747245F 1384897 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 640FE 20826 RT WING ROOT ON REAR SPAR LOCATION ATTACHMENT TO CENTER TANK, 4 HOLES IN THE REAR SPAR COMMON TO SPLICE PLATE AND 3 HOLE S IN THE SPLICE PLATE COMMON TO THE REAR SPAR FOUND CRACKED. SPLICE PLATE PLACED AND CRACKED FASTENER HOLES OVERSIZED A ND BUSHING INSTALLED AS PER FEDEX ERA NR B57-10-92 REV 1 65B14528-6, 65B15275-12, 1 EACH 15-5PH-1.250 INCH DIA 1 FT. 2 L 7 4 4F A20WE 1996012600355 19960126 00355 NM 1996 1 26 96UAL900051 1 19960122 A 2781 FLAP INDICATION BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LE FLAPS MALFUNCTIONED A UALA O OTHER N FALSE WARNING DE DESCENT 1 WP 29 608UA 21869 LANDED UNDER AMBER ALERT DUE TO IRREGULAR FLAP CONFIGURATION. EICAS MESSAGE LEADING EDGE SLAT ASSYMMETRY DISPLAYED, LEA DING EDGE ILLUMINATED WITH FLAP LEVER, ONE UNIT. PERFORMED PSEU BITE TEST AND NO FAULT. LEADING EDGE AND TRAILING EDGE FLAPS OPERATED NORMAL. UNABLE TO DETECT ANY DEFECTS. 2 L 7 2 4F 4 F RT A1NM E3NE 1996012600356 19960126 00356 NM 1996 1 26 96UAL900052 1 19960122 A 3350 BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7272U 21419 EMERGENCY EXIT ABOVE DOOR 1L IS INOPERATIVE. REPLACED BATTERIES AND GROUND CHECKS GOOD. 2 L 7 3 4F 4 F A3WE E2EA 1996012600357 19960126 00357 NM 1996 1 26 96UAL900053 1 19960122 A 3350 SIGN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN MALFUNCTIONED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7467U 21921 EMERGENCY EXIT LIGHT ABOVE DOOR 1 ILLUMINATES WITH POWER, SWITCH AND BATTERY OFF. REPLACED EXIT SIGN LIGHT ASSEMBLY AT DOOR 1L. 2 L 7 3 4F 4 F A3WE E2EA 1996012600358 19960126 00358 NM 1996 1 26 96UAL900054 1 19960122 A 3350 STRIP BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 9051U 19932 EMERGENCY ESCAPE PATH LIGHTING IN FIRST CLASS INOP. REPLACED LIGHT STRIP. 2 L 7 2 4F 4 F A16WE E2EA 1996012600359 19960126 00359 NM 1996 1 26 96UAL900055 1 19960122 A 3350 BATTERY BOEING 737 737322 1384676 NM CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 367UA 24536 EMERGENCY LIGHTS INOP AT ROWS 1, 10 TO 16, 18 AND DOOR 2 LEFT. REPLACED BATTERY PACK AND CHECKS OK. 2 L 7 2 4F RT A16WE 1996012600360 19960126 00360 NM 1996 1 26 96UAL900056 1 19960122 A 3350 STRIP BOEING 737 737522 138449F NM CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 912UA 25290 FORWARD GALLEY EMERGENCY ESCAPE PATH LIGHT STRIP INOP. REPLACED GALLEY LIGHT STRIP AND CHECKS OK. 2 L 7 2 4F RT A16WE 1996012600361 19960126 00361 SO 1996 1 26 COMA9610033 1 19960119 A 3230 2094500102 UPLOCK HOOK EMB 120 EMB120RT SO LT MLG LACK OF LUBE A COMA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 200CD 16985 4467 120200 LT MLG WILL NOT RETRACT. FOUND UPLOCK HOOK ASSY TO BE BINDING. CLEANED AND LUBED UPLOCK ASSY AND SYSTEM OPERATES NORMA LLY. 2 L 7 2 4T RT A31SO 1996012600362 19960126 00362 SO 1996 1 26 COMA9610034 1 19960120 A 5753 FLAP TRACKS EMB 120 EMB120RT SO TE FLAPS DIRTY A COMA K NONE O OTHER CL CLIMB 1 SO 01 248CA 120228 RECEIVED FLAP DISAGREEMENT WARNING SHORTLY AFTER TAKEOFF. CLEANED FLAP TRACKS AND SYSTEM OPERATION NORMAL. 2 L 7 2 4T RT A31SO 1996012600363 19960126 00363 SO 1996 1 26 COMA9610035 1 19960121 A 3231 12012347001 LATCH EMB 120 EMB120RT SO LT MLG DOOR BROKEN A COMA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 243CA 120212 WHEN LANDING GEAR RETRACTED, LT MLG INTRANSIT INDICATION REMAINED ON. REPLACED BROKEN LATCH ASSY ON INBD GEAR DOOR. 2 L 7 2 4T RT A31SO 1996012600364 19960126 00364 EU 1996 1 26 COMA9630019 1 19960118 A 3020 NH2466881 INLET HEAT SAAB SF340 SF340A 7850100 EU RT ENGINE FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 146CA 8365 2132 340A146 RT ENGINE INTAKE HEAT FAILED. REPLACED THE UNDER TEMP THERMISTOR WITH THE SPARE THERMISTOR AND SYSTEM OPERATES NORMAL. 2 L 7 2 4T RT A52EU 1996012600365 19960126 00365 EU 1996 1 26 COMA9630020 1 19960119 A 2910 7229152675 HYD TUBE SAAB SF340 SF340A 7850100 EU RT MLG LEAKING A COMA K NONE K FLUID LOSS UK UNKNOWN 1 SO 01 320CA 340A064 HYDRAULIC FLUID LEAKING FROM RT WHEEL WELL. REPLACED LEAKING BRAKE LINE WHICH WAS CHAFED THROUGH BY WOW HARNESS WIRING. 2 L 7 2 4T RT A52EU 1996012600366 19960126 00366 EU 1996 1 26 COMA9630021 1 19960121 A 5610 7256100502 WINDSHIELD SAAB SF340 SF340A 7850100 EU RT COCKPIT NOT SEALED A COMA K NONE O OTHER CR CRUISE 1 SO 01 358CA 12136 9613 340A047 COPILOTS WINDSHIELD SQUEALS DURING FLIGHT. REPLACED COPILOTS WINDSHIELD. 2 L 7 2 4T RT A52EU 1996012600367 19960126 00367 EA 1996 1 26 COMA9660017 1 19960121 A 3030 102AH2AG TAT PROBE HEAT CNDAIR CL600 CL6002B19 EA FUSELAGE FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 933CA 7040 TAT PROBE HEAT CAUTION MESSAGE ON EICAS. REPLACED THE TAT PROBE. 2 L 7 2 4F RT A21EA 1996012600368 19960126 00368 EA 1996 1 26 COMA9660018 1 19960121 A 3222 16040101 STRUT CNDAIR CL600 CL6002B19 EA NLG LEAKING A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 914CA 7012 NOSE LANDING GEAR STRUT BOTTOMS DURING TAXI. REPLACED THE NLG SHOCK STRUT. 2 L 7 2 4F RT A21EA 1996012600369 19960126 00369 EA 1996 1 26 COMA9660019 1 19960120 A 7714 5071T98P01 AMPLIFIER CNDAIR CL600 CL6002B19 EA RT ENGINE DEFECTIVE A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 933CA 7040 RT ENGINE WILL NOT ACHIEVE TAKEOFF THRUST. REPLACED THE N1 AMPLIFIER AND ENGINE RUNS NORMAL, ACFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1996012600370 19960126 00370 1996 1 26 COMA9660020 4 19960119 A 3418 864806 PSEU CNDAIR CL600 CL6002B19 EA AVIONICS DEFECTIVE A COMA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 952CA 1931 7092 WOW OUTPUT AND WOW INPUT CAUTION MESSAGE ON EICAS. REPLACED THE PROXIMITY SENSOR ELECTRONIC UNIT. 2 L 7 2 4F RT A21EA 1996012600371 19960126 00371 NM 1996 1 26 DHL96717005 1 19960119 A 3310 106075213 BALLAST BOEING 727 72723 1384004 NM COCKPIT FAILED A T DHLA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 717DH 19389 MEDIUM AMOUNT OF SMOKE IN COCKPIT FROM UNDER FRONT PANEL RIGHT SIDE. FOUND BALLAST FOR PANEL FLUORESCENT LIGHTS CAUSING SMOKE. DEACTIVATED SYSTEM, DEFERRED PER MEL 33-1. 2 L 7 3 4F A3WE 1996012600372 19960126 00372 NM 1996 1 26 DL72K960128 1 19960105 A 5330 6554590 SKIN BOEING 727 727232 1384082 NM BS 720 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 413DA 21233 CORROSION WAS FOUND ON THE RAM AIR ACTUATOR ACCESS DOOR CUTOUT AT THE FWD LT CORNER. THE CORROSION WAS CUTOUT AND REPAI RED WITH AN EXTERNAL AND AN INTERNAL DOUBLER PER FAA/DER FORM 8110-3, DATED 1-5-96. 2 L 7 3 4F A3WE 1996012600373 19960126 00373 NM 1996 1 26 DL72L960115 1 19960116 A 5330 65C20489 SKIN BOEING 727 727232 1384082 NM BS 1005 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 511DA 21313 BELLY SKIN WAS CORRODED REQUIRING A 1 INCH BY 4 INCH CUTOUT OF THE SKIN. THE STA 1009 BUTT SPLICE IS AFT OF THE CUTOUT AND FORWARD OF AN EXISTING REPAIR. REPAIRED PER SRM 53-30-3 FIG 3A. 2 L 7 3 4F A3WE 1996012600374 19960126 00374 NM 1996 1 26 DL72L960134 1 19960117 A 5330 6554590 SKIN BOEING 727 727232 1384082 NM FS 720 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 511DA 21313 DURING INSPECTION, THE RAM AIR ACTUATOR ACCESS DOOR CUTOUT WAS FOUND TO HAVE CORROSION ON THE ATTACH FLANGE IN THE LT AF T CORNER. IN ACCORDANCE WITH FAA/DER FORM 8110-3, DATED 1-17-96, THE DAMAGE HAS BEEN BLENDED TO 0.59 MINIMUM FLANGE THI CKNESS. 2 L 7 3 4F A3WE 1996012600375 19960126 00375 NM 1996 1 26 DL72S960104 1 19960116 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 4 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 408DA 21152 FOUND DURING E-2 LETTER CHECK, .375 INCH CRACK NR 4 L/E SLAT COVE SKIN LWR ATTACH ANGLE AT O/B END. REPAIRED PER M/M 57 -54-0 PAR 5A. 2 L 7 3 4F A3WE 1996012600376 19960126 00376 NM 1996 1 26 DL72S960105 1 19960116 A 5312 BLKHD WEB BOEING 727 727232 1384082 NM BS 870 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 408DA 21152 FOUND ON E2 LETTER CHECK, STA 870 BULKHEAD WEB CRACKED 3 INCHES AT APU LOAD CONTROL VALVE CUTOUT, LWR END IN RT W/W. RE PAIR PER SRM 53-10-9, TIME LIMITED INST. 2 L 7 3 4F A3WE 1996012600377 19960126 00377 NM 1996 1 26 DL72S960110 1 19960116 A 5320 ANGLE BOEING 727 727232 1384082 NM RT WW CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 408DA 21152 FOUND ON E2 LETTER CHECK, KEEL BEAM VERT STIFFENER CRACKED .5 INCH FWD INBD RT W/W. TIME LIMITED REPAIR PER SRM 53-10-9 . 2 L 7 3 4F A3WE 1996012600378 19960126 00378 NM 1996 1 26 DL72S960118 1 19960106 A 5320 HINGES BOEING 727 727232 1384082 NM ACCESS DOOR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 495DA 21075 FROM MV2 ATL ITEM, CORROSION BEHIND HINGES ON ACCESS DOOR 3448R, LOC RT A/C COMP. REMOVED ACCESS DOOR 3448R, DAMAGE SEC TION OFF ANGLE AND INSTALLED REPAIR PER MM 53-30-1 PG 807. 2 L 7 3 4F A3WE 1996012600379 19960126 00379 NM 1996 1 26 DL72S960129 1 19960111 A 5321 FLOOR PAN BOEING 727 727232 1384082 NM BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 419DA 21272 FOUND ON MV1 CHECK, LT AND RT LAV FLOOR PAN DITCHING SEAL PANEL CRACKED, VIEWED FROM BAG BIN FWD OF 1183. REPAIRED PER M/M 53-0-11. 2 L 7 3 4F A3WE 1996012600380 19960126 00380 NM 1996 1 26 DL72S960143 1 19960121 A 3350 334701745 LIGHT BOEING 727 727232 1384082 NM LT OVERWING INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 408DA 21152 ON INSPECTION, LEFT OVERWING EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY, OPN CKS NORMAL. 2 L 7 3 4F A3WE 1996012600381 19960126 00381 NM 1996 1 26 DL72S960147 1 19960121 A 3350 BATTERY PACK 20131A BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 475DA 6800 20752 ON L/O CHECK, FOUND EMERGENCY LIGHTS OUT FROM ROW 27 AFT TO F/A SEAT. REPLACED BATTERY PACK M9027 AND OPS CHECKS NORMAL . 2 L 7 3 4F A3WE 1996012600382 19960126 00382 NM 1996 1 26 DL72S960152 1 19960119 A 2780 BRACKET BOEING 727 727232 1384082 NM NR 5 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 517DA 21433 FROM HMV ATL, NR 5 KRUEGER FLAP ACTUATOR ATTACH BRACKET CRACKED. INSTALLED REPAIR PER MM 57-20-21 PG 811. 2 L 7 3 4F A3WE 1996012600383 19960126 00383 NM 1996 1 26 DL72S960157 1 19960117 A 3260 H1010154 DNLOCK SWITCH BOEING 727 727232 1384082 NM NLG FAILED A DALA O OTHER N FALSE WARNING AP APPROACH 1 SO 27 496DA 21076 ON GEAR EXTENSION RECEIVED RED NOSE GEAR LIGHT, VISUALLY VERIFIED DOWN AND LOCKED. REPLACED NOSE GEAR DOWNLOCK SWITCH A ND NOSE GEAR POSITION SWITCH. ALSO, AS PRECAUTION REPLACED LANDING GEAR ACCESORY UNIT AND OPERATION NORMAL. 2 L 7 3 4F A3WE 1996012600384 19960126 00384 NM 1996 1 26 DL72S960160 1 19960116 A 3397 WIRE BOEING 727 727232 1384082 NM CABIN BROKEN A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 401DA 21145 ON PREDEPARTURE, EMERGENCY TRACK LIGHTS IN FWD CABIN INOP. REPAIRED BROKEN WIRE AT ROW 14 AND OPERATION NORMAL. 2 L 7 3 4F A3WE 1996012600385 19960126 00385 NM 1996 1 26 DL72W960116 1 19960114 A 5521 SPAR BOEING 727 7272Q8 138407W NM RT ELEVATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831L 21826 THE RIGHT HAND ELEVATOR REAR SPAR HAD A CRACK EMANATING .25 INCH FROM THE INBOARD SIDE OF THE SHEAR PLATE, AT THE THIRD FROM INBOARD TAB HINGE FITTING-TO-REAR SPAR ATTACHMENT. CRACK WAS WITHIN THE S/B 55-0087 INTERIM REPAIR 0.250 ALLOWABLE LIMIT ON CRACK LENGTH BEYOND THE END OF THE SHEAR PLATE. THE CRACK WAS STOP DRILLED PER THE S/B 55-0087 REV 1. THE S/ B INITIATED THE REQUIRED REPETITIVE INSPECTION AND PERMANENT REPAIR. 2 L 7 3 4F A3WE 1996012600386 19960126 00386 NM 1996 1 26 DL72W960119 1 19960117 A 5754 ANGLE BOEING 727 727247 138408F NM NR 2 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 292WA 22110 FOUND ON A1 LETTER CHECK, TWO .5 INCH CRACKS AT NR 2 L/E SLAT COVE SKIN ANGLE, BELOW TIA DUCT. REPAIRED PER MM 57-50-0. 2 L 7 3 4F A3WE 1996012600387 19960126 00387 NM 1996 1 26 DL72W960127 1 19960119 A 3350 334701744 BATTERY PACK BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 292WA 22110 DURING INSPECTION, AFT CABIN BULLNOSE EMERGENCY LIGHT INOP. REPLACED BATT RACK, OPS NORMAL. 2 L 7 3 4F A3WE 1996012600389 19960126 00389 NM 1996 1 26 DL73E960145 1 19960121 A 3350 081691 SOCKET BOEING 737 737247 138448D NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 382DL 23609 EMERGENCY FLOOR LIGHT AT ROW 2 IS INOP. REPLACED SOCKET, DL (P/N 337201959), (MFG 08169-1), OPS GOOD. 2 L 7 2 4F A16WE 1996012600390 19960126 00390 NM 1996 1 26 DL73E960159 1 19960114 A 3260 DN SWITCH BOEING 737 737247 138448D NM LANDING GEAR FAILED A DALA O OTHER N FALSE WARNING AP APPROACH 1 SO 27 376DL 23603 WHEN LANDING GEAR WAS PLACED DOWN, ALL 3 GREEN AND ALL 3 RED LIGHTS ILLUMINATED. REPLACED GEAR HANDLE DOWN SWITCH (S-78 ), OPERATION NORMAL. 2 L 7 2 4F A16WE 1996012600391 19960126 00391 NM 1996 1 26 DL73S960158 1 19960120 A 3240 AV24E1144 VALVE BOEING 737 737232 1384475 NM PARKING BRAKE LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 329DL 23101 ON CLIMBOUT, LOST A/B HYDRAULIC SYSTEM PRESSURE. FLIGHT RETURNED MSP. FOUND PARKING BRAKE VALVE LEAKING. REPLACED VAL VE, SERVICED SYSTEM AND OPERATION NORMAL. 2 L 7 2 4F RT A16WE 1996012600392 19960126 00392 NM 1996 1 26 DL757960120 1 19960117 A 3350 767 BULB BOEING 757 757232 1384965 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 620DL 22910 DURING INSPECTION, FOUND EMERGENCY LIGHT AT R-2 DOOR INOP. RELAMPED AND CHECKS GOOD. 2 L 7 2 4F RT A2NM 1996012600393 19960126 00393 NM 1996 1 26 DL757960121 1 19960117 A 3350 BULB BOEING 757 757232 1384965 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 646DL 24217 R2 DOOR OUTSIDE EMERGENCY LIGHT INOP. EMERGENCY TRACK LIGHT AT ROW 1, 28 INOP. RELAMPED AND OPERATION NORMAL. 2 L 7 2 4F RT A2NM 1996012600394 19960126 00394 NM 1996 1 26 DL757960124 1 19960118 A 5754 114N4004166A TE WEDGE BOEING 757 757232 1384965 NM NR 8 LE FLAP DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 634DL 23615 DURING INSPECTION, NR 8 L/E SLAT TRAILING EDGE WEDGE WAS FOUND DELAMINATED. REPLACED WEDGE PER SRM 57-43-07. 2 L 7 2 4F RT A2NM 1996012600395 19960126 00395 NM 1996 1 26 DL757960125 1 19960118 A 3350 POWER SUPPLY BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 669DN 25142 R2 DOOR EXIT LIGHT DID NOT ILLUMINATE DURING LIGHT TEST. REPLACED POWER SUPPLY AND OPERATION NORMAL. 2 L 7 2 4F RT A2NM 1996012600396 19960126 00396 NM 1996 1 26 DL757960132 1 19960119 A 5610 141T480120 WINDSHIELD BOEING 757 757232 1384965 NM LT FLT DECK FAILED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 680DA 26956 COPILOT WINDSHIELD OUTER PANE SHATTERED, CLIMBING THROUGH 10,000 FT. FLIGHT RETURNED JFK. REPLACED WINDSHIELD. 2 L 7 2 4F RT A2NM 1996012600397 19960126 00397 NM 1996 1 26 DL757960136 1 19960118 A 5754 114N4005157 TE WEDGE BOEING 757 757232 1384965 NM NR 4 LE SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 646DL 24217 DURING INSPECTION, FOUND THE TRAILING EDGE WEDGE ON THE NR 4 SLAT DELAMINATED IN THE UPPER SKIN. THERE IS A PREVIOUS RE PAIR DOUBLER THAT MEASURES 2 INCHES FORE/AFT AND 10 INCHES WIDE, INSTALLED IN THE DAMAGED REGION. REPAIRED TRAILING EDG E WEDGE IN ACCORDANCE WITH B757 SRM 51-70-10. 2 L 7 2 4F RT A2NM 1996012600398 19960126 00398 NM 1996 1 26 DL767960139 1 19960120 A 3350 BULB BOEING 767 767232 1385132 NM RT OVERWING FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 106DA 22218 RT OVERWING EMERGENCY LIGHT INOP. RELAMPED AND CLEANED CONTACT. 2 L 7 2 4F RT A1NM 1996012600399 19960126 00399 WP 1996 1 26 DLL10960137 1 19960118 A 2150 ACTUATOR 75010304 LKHEED 1011 10113851 5265010 WP NR 2 PACK FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 722DA 2204 193C1147 AFTER TAKEOFF HAD BURNING ODOR AND VISIBLE SMOKE, RETURNED HNL. RAN ALL ENGINES, COULD NOT DUPLICATE. RAN PACKS, ALL N ORMAL. REPLACED NR 3 WATER SEPARATOR BAG. DUE TO HISTORY SUBSEQUENT MAINTENANCE FOUND FAULTY NR 2 PACK RAMA AIR DOOR A CTUATOR. REPLACED ACTUATOR. 2 L 7 3 4F A23WE 1996012600400 19960126 00400 WP 1996 1 26 DLL10960146 1 19960121 A 3350 BULB LKHEED 1011 10113851 5265010 WP CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 716DA 193C1095 FOUND EMERGENCY TRACK LIGHT AT SEAT 43GH INOP. REPLACED BULB AND EMERGENCY TRACK LIGHT OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A23WE 1996012600401 19960126 00401 WP 1996 1 26 DLL13960095 1 19960116 A 3233 327003309 ACTUATOR LKHEED 1011 10113851 5265010 WP LT MLG CRACKED A DALA K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 SO 27 790DL 193A1143 LEFT MLG ACTUATOR CYLINDER LOWER END CRACKED COMPLETELY AND FAILED DURING PREFLIGHT OPERATIONS POST HMV. CAUSED COMPLET E LOSS OF C-SYSTEM HYD FLUID. CYLINDER APPEARS TO NOT HAVE BEEN IDENTIFIED AS BEING MODIFIED PER SB. REPLACED CYLINDER . 2 L 7 3 4F A23WE 1996012600402 19960126 00402 WP 1996 1 26 DLL13960122 1 19960117 A 5330 SKIN LKHEED 1011 10113851 5265010 WP FS 1765 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 790DL 193A1143 DURING HMV INSPECTION, THE FUSELAGE SKIN WAS FOUND SEVERELY CORRODED AT FS 1765, STR 39. THE DAMAGE WAS TRIMMED OUT AND FINAL CUT OUT DIMENSIONS ARE 8.5 INCH BY 7.5 INCH. AN EXTERNAL DOUBLER WILL BE INSTALLED AS A PERMANENT REPAIR PER DL ERA 272931 REV C. 2 L 7 3 4F A23WE 1996012600403 19960126 00403 WP 1996 1 26 DLL13960123 1 19960117 A 5320 1542395 PRESS DECK LKHEED 1011 10113851 5265010 WP BS 359 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 790DL 193A1143 THE NLG PRESSURE DECK CONTAINED CORROSION THAT WAS CUT OUT AT STA 359, LBL 26. THE FINAL CUT OUT DIMENSIONS ARE 4 INCH BY 8 INCH. INSTALLED REPAIR PER DL ERA 273038 R B. 2 L 7 3 4F A23WE 1996012600404 19960126 00404 WP 1996 1 26 DLL15960103 1 19960116 A 3350 BATTERY PACK 5165741 LKHEED 1011 10113853 5265020 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 755DL 54040 193Y1184 OVERHEAD EMERGENCY LIGHTS AT 20AB INOP. REPLACED DEFECTIVE BATTERY PACK AT 22AB OVERHEAD AND LIGHTS CHECK GOOD. 2 L 7 3 4F A23WE 1996012600405 19960126 00405 WP 1996 1 26 DLL17960102 1 19960116 A 3350 POWER SUPPLY 5165741 LKHEED 1011 10113853 5265020 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 764DA 56640 193H1202 EMERGENCY LIGHTS AT L-3 DOOR INOP. REPLACED POWER SUPPLY AND EMERGENCY LIGHTS CHECK GOOD. 2 L 7 3 4F A23WE 1996012600406 19960126 00406 NM 1996 1 26 DLM11960140 1 19960120 A 5610 NBA6045501 WINDSHIELD DOUG MD11 MD11 3023602 NM LT COCKPIT CRACKED A DALA K NONE O OTHER DE DESCENT 1 SO 27 801DE 48472 CAPT WINDSHIELD BROKE ON DESCENT THROUGH FL 310. REPLACED CAPT WINDSHIELD PER M/M 56-11-01. ALSO, REPLACED ANTI-ICE CO NTROLLER ON LOG 790446/002. 2 L 7 3 4F RT A22WE 1996012600407 19960126 00407 NM 1996 1 26 DLM11960141 1 19960120 A 3040 9615046004 CONTROLLER DOUG MD11 MD11 3023602 NM LT WINDSHIELD FAILED A DALA K NONE O OTHER DE DESCENT 1 SO 27 801DE 48472 DUE TO CAPT WINDSHIELD CRACK, REPLACING CAPT/LEFT WINDSHIELD ANTI-ICE CONTROLLER. REPLACED LEFT WINDSHIELD ANTI-ICE CON TROLLER. WINDSHIELD REPLACED ON LOG 790446/001. 2 L 7 3 4F RT A22WE 1996012600408 19960126 00408 NM 1996 1 26 DLM88960096 1 19960116 A 3260 BULB DOUG MD88 MD88 3023688 NM RT MLG FAILED A DALA L ABORTED APPROACH P NO WARNING INDICATION LD LANDING 1 SO 27 920DE 53423 ON APPROACH TO CVG, RIGHT MLG DOWNLOCK IND GREEN LIGHT FAILED TO ILLUMINATE. ALL OTHER IND WERE NORMAL, NO HORN AND NO RED LIGHT. CHECKED SENSORS RT GEAR AND PERFORMED BITE CHECK OF PSEV, NO FAULTS. RELAMPED RT GEAR POS IND AND CHECKS GO OD. 2 L 7 2 4F RT A6WE 1996012600409 19960126 00409 1996 1 26 DLM88960126 4 19960118 A 3425 AHARS 4608000307 DOUG MD88 MD88 3023688 NM LT/RT COCKPIT FAILED A DALA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 SO 27 946DL 696 49819 IN FLIGHT BOTH CAPTS AND F/O COMPASSES TUMBLE. AIRCRAFT RETURNED TO DFW. REPLACED BOTH AHARS UNITS AND SYS OPNS NORMAL . 2 L 7 2 4F RT A6WE 1996012600411 19960126 00411 NM 1996 1 26 DLM88960155 1 19960102 A 3232 5939710502 ACTUATOR DOUG MD88 MD88 3023688 NM LT MLG DOOR FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 949DL 49880 ON GEAR RETRACTIONS RED LIGHT RT MAIN GEAR EXTENDED 3 GREEN BUT GEAR DOOR OPEN LT ON. FLIGHT RETURNED TO BOS. FOUND BR OKEN TORQUE SHAFT. REPLACED RT GEAR DOOR AND DOOR ACTUATOR. 2 L 7 2 4F RT A6WE 1996012600412 19960126 00412 WP 1996 1 26 MWEA96019 1 19960120 A 5530 ANGLE DOUG DC9 DC932 3022066 WP VERT STAB CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 DURING C-CHECK, FOUND VERTICAL STAB TO FUSELAGE EXTERIOR ATTACH ANGLE CRACKED ON LT SIDE APPROX 8 INCH FROM AFT END. IN STALLED DOUBLER REPAIR IAW SRM 53-05 FIG 23. 2 L 7 2 4F A6WE 1996012600413 19960126 00413 WP 1996 1 26 MWEA96020 1 19960120 A 5320 ANGLE DOUG DC9 DC932 3022066 WP FS 1076 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 DURING C-CHECK, FOUND ANGLE AT FS 1076 IN AFT ACCESSORY COMPT CRACKED AT LONGERON 16R. FABRICATED AND INSTALLED ANGLE I AW SRM 53-01. 2 L 7 2 4F A6WE 1996012600414 19960126 00414 NM 1996 1 26 P5CA9600023 1 19960123 A 5755 SKIN BOEING 747 747122 1384872 NM NR 9 SPOILER CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND CORROSION AND SLIGHT BULGING OF PAINT AROUND RIVET HEAD FORWARD OF NR 9 SPOILER. CLEANED AND TREATED PER SRM 51-1 0-01. 2 L 7 4 4F A20WE 1996012600415 19960126 00415 NE 1996 1 26 P5CA9600024 2 19960123 A 7250 SLEEVE BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 2 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND TURBINE REVERSER SLEEVE CRACKED BETWEEN TWO PREVIOUS REPAIRS. REPAIRED IAW SRM 54-30-03. REPAIR INCLUDES BOTH PR EVIOUS REPAIRS. 2 L 7 4 4F 4 F A20WE E20EA 1996012600416 19960126 00416 NM 1996 1 26 P5CA9600025 1 19960123 A 5330 SKIN BOEING 747 747122 1384872 NM BS 2658 CHAFED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND APU COMPT FORWARD BULKHEAD FWD SIDE CHAFED THROUGH AT STA 2658, CAUSED BY IMPROPERLY INSTALLED SHROUD AT BULKHEAD. REPAIRED DAMAGED AREA IAW SRM 53-10-04. 2 L 7 4 4F A20WE 1996012600417 19960126 00417 NM 1996 1 26 P5CA9600026 1 19960122 A 2710 ACTUATOR BOEING 747 747121 1384871 NM RT AILERON INOPERATIVE A P5CA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 WP 23 831FT 19648 DURING TAXI OUT, ON FLIGHT CONTROL CHECK, FOUND RT AILERON WOULD NOT UNLOCK FROM HIGH SPEED MODE WITH FLAPS IN TAKEOFF P OSITION. RETURNED TO BLOCKS, APPLIED HEAT TO AILERON LOCKOUT ACTUATOR AND SYSTEM BECAME OPERATIVE. OPERATIONAL CHECK G OOD IAW MM 27-11-00. 2 L 7 4 4F A20WE 1996012600419 19960126 00419 NM 1996 1 26 VSTA9601012 1 19960106 A 5523 6573799501 TAB BOEING 737 737247 138448D NM LT ELEVATOR CRACKED A VSTA K NONE E VIBRATION/BUFFET NR NOT REPORTED 1 WP 07 303VA 20125 INTERMITTENT AIRFRAME VIBRATION. LOOSE FASTENERS AT LT ELEVATOR INBOARD HINGE LUG. REPLACED LT ELEVATOR TAB. 2 L 7 2 4F A16WE 1996012600420 19960126 00420 NM 1996 1 26 VSTA9601013 1 19960120 A 5230 57094 SEAL BOEING 737 737204 1384458 NM CARGO DOOR LEAKING A VSTA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 07 312VA 20236 UNABLE TO HOLD PRESSURIZATION IN AIRCRAFT CABIN. AFT CARGO DOOR SEAL LEAKING. REMOVED AND REPLACED DOOR SEAL. 2 L 7 2 4F A16WE 1996012600463 19960126 00463 WP 1996 1 26 HAL9602 1 19960107 A 3260 0080004003 PROX CONTL BOX DOUG DC9 DC951 3022051 WP RT MLG/NLG MALFUNCTIONED A HALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 13 2FOR 460 47796 HNL - FLT 516 - INFORMATION FROM LOG PAGE 149767-1. RED NOSE AND RT MAIN UNSAFE LIGHTS AFTER GEAR RETRACTION. RECYCLED , UNABLE TO EXTINGUISH ONE OR BOTH. CHECKED WIRING ON RT MAIN AND NOSE GEAR. FOUND OK. REPLACED PROXIMITY CONTROL BOX . RETRACTION CHECK OK. (X) 2 L 7 2 4F A6WE 1996012600464 19960126 00464 WP 1996 1 26 9601439912 1 19960120 A 5350 RELEASE MECH DOUG DC9 DC931 3022065 WP TAILCONE OUT OF ADJUST A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 962N 47406 DURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL BOTH THE INTERIOR AND EXTERIOR TAILCONE HANDLES. REPLAC ED THE CLIPS AND HANDLES PER EO 5350-01049. 2 L 7 2 4F A6WE 1996012600465 19960126 00465 WP 1996 1 26 9601449754 1 19960115 A 5210 CLOSING MECH DOUG DC9 DC941 302207N WP CABIN DOOR MALFUNCTIONED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 754NW 47178 MBS-DTW - UPON ARRIVAL, FOUND THAT THE MAIN CABIN DOOR WOULD NOT OPEN. MAINTENANCE RERIGGED THE DOOR PER MM 52-11-0 PG 501 TO 514. REPLACED LOCK ADJUSTMENT AND CRANK ROD ENDS. PRESSURE AND OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996012600466 19960126 00466 WP 1996 1 26 9601459754 1 19960119 A 5210 BAYONET DOUG DC9 DC941 302207N WP PAX DOOR OUT OF RIG A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 754NW 47178 RST-MSP - AFTER ARRIVAL, FOUND THAT THE MAIN CABIN DOOR WOULD NOT OPEN FROM THE INSIDE. MAINTENANCE RERIGGED THE MAIN C ABIN DOOR PER MM 52-11-00. 2 L 7 2 4F A6WE 1996012600467 19960126 00467 NE 1996 1 26 9601461148 2 19960119 A 7532 SOLENOID DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 1 ENGINE FAILED A NWAA E ENGINE SHUTDOWN J WARNING INDICATION LD LANDING 1 GL 01 148US 46757 86181 DURING LANDING, THE NR 1 ENGINE EXPERIENCED COMPRESSOR STALL. EGT INCREASED TO TOP OF SCALE. CREW FOLLOWED COCKPIT OPE RATING PROCEDURE, SHUT NR 1 ENGINE DOWN AND MOTORED UNTIL EGT IS BELOW 100C. BORESCOPED NR 1 ENGINE AND INSPECTED PER M M 71-00-00. REPLACED RABS SOLENOID AND ALL CHECKS WERE NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A22WE E20EA 1996012600468 19960126 00468 NM 1996 1 26 9601476601 1 19960120 A 3240 SELECTOR VALVE BOEING 747 747151 1384891 NM BRAKE SYST FAILED A NWAA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CL CLIMB 1 GL 01 601US 19778 AFTER TAKEOFF, GEAR AND FLAPS CHECKED UP, NR 4 HYDRAULIC SYSTEM QUANTITY INDICATION ILLUMINATED. CREW FOLLOWED COCKPIT OPERATING PROCEDURE AND RETURNED TO NRT. REPLACED RESERVE BRAKE SELECTOR VALVE AND PERFORMED LEAK CHECK. CHECK WAS NOR MAL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F A20WE 1996012600469 19960126 00469 WP 1996 1 26 9601489608 1 19960122 A 3260 BULB DOUG DC9 DC932 3022066 WP NLG MISINSTALLED A NWAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 01 608NW 47233 DURING APPROACH, THE NOSE LANDING GEAR GREEN LIGHT ILLUMINATED. PERFORMED GO-AROUND AND AIRCRAFT LANDED WITHOUT INCIDEN T. INSTALLED CORRECT BULB FOR NOSE LANDING GEAR INDICATION AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600470 19960126 00470 NM 1996 1 26 9601492292 1 19960120 A 3234 CONTROL VALVE BOEING 727 727251 138408H NM LANDING GEAR FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 292US 21503 AFTER TAKEOFF, GEAR WOULD NOT RETRACT AND GEAR HANDLE WOULD NOT RAISE TO THE 'UP' POSITION. AIRCRAFT RETURNED TO MSP AN D LANDED WITHOUT INCIDENT. REPLACED THE LANDING CONTROL VALVE AND OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996012600471 19960126 00471 NM 1996 1 26 9601506302 1 19960121 A 3350 CONNECTOR BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 662US 23720 DURING LINE CHECK, THE FLOOR PATH EMERGENCY LIGHTS BETWEEN SEAT ROWS 35 TO 43 WERE FOUND INOPERATIVE. RECONNECTED EMERG ENCY LIGHT CONNECTOR AT SEAT ROW 43 AND OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996012600472 19960126 00472 NM 1996 1 26 9601512771 1 19960121 A 2150 MIX VALVE BOEING 727 7272M7 138407S NM RT PACK FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 01 742RW 21952 DURING FLIGHT, LOSE RIGHT AIR CONDITIONING PACK WITH LOSS OF PRESSURIZATION. AIRCRAFT DROPPED TO 10,000 FEET AND RETURN ED TO MSP. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE RIGHT HAND PACK MIX VALVE AND OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996012600473 19960126 00473 WP 1996 1 26 9601529601 1 19960121 A 3260 PUSH ROD DOUG DC9 DC932 3022066 WP LT MLG DOOR OUT OF ADJUST A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 601NW 47038 DURING APPROACH, THE LEFT MAIN LANDING GEAR DOOR OPEN LIGHT ILLUMINATED AFTER LANDING GEAR EXTENSION. RECYCLED LANDING GEAR AND LIGHT EXTINGUISHED. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND LEFT MAIN LANDING GEAR DOOR SEQUENCE DRIVE ARM PU SH ROD OUT OF RIG. RIGGED PUSH ROD AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600474 19960126 00474 NM 1996 1 26 9601532771 1 19960123 A 3350 POWER SUPPLY BOEING 727 7272M7 138407S NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 742RW 21952 DURING PREFLIGHT, FOUND SECTION OF FLOOR PATH EMERGENCY LIGHTS LEFT SIDE OF CABIN INOPERATIVE. REPLACED POWER SUPPLY AN D BATTERY, CHECKED OK. 2 L 7 3 4F A3WE 1996012600475 19960126 00475 NM 1996 1 26 9601542202 1 19960121 A 3350 BATTERY PACK BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 202US 22155 DURING PREFLIGHT, FOUND BOTH OVERWING EXIT SIGN EMERGENCY LIGHTS INOPERATIVE ON RIGHT SIDE OF AIRCRAFT. REPLACED BATTER IES IN POWER SUPPLY AND CHECKED OK. 2 L 7 3 4F A3WE 1996012600476 19960126 00476 NM 1996 1 26 96FDEA00119 1 19960116 A 5510 STRINGER BOEING 747 747245F 1384897 NM STA 152.4-184.80 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 640FE 20826 RT HORIZ STAB COMP STR 10 BETWEEN STAB STA 152.4 AND 184.80 FOUND CORRODED. MINOR SURFACE CORROSION REMOVED AND AREA RE PROTECTED AS PER SRM FEDEX 51-10-01 AND 51-10-02 REV 76 WITHIN LIMITS AS PER SRM FEDEX 55-10-01 REV 76. 2 L 7 4 4F A20WE 1996012600477 19960126 00477 NM 1996 1 26 96UAL900057 1 19960123 A 3350 BATTERY BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE CABIN DISCHARGED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 153UA 20102 EMERGENCY LIGHTS INOP IN THE CEILING AT ROW 38 AND LAVATORY 117. REPLACED BATTERY PACK AND CHECKS OK. 2 L 7 4 4F 4 F A20WE E20EA 1996012600478 19960126 00478 NM 1996 1 26 96UAL900058 1 19960123 A 3350 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 549UA 25397 FLOOR EMERGENCY ESCAPE LIGHTING INOP AT ROW 13. RECONNECTED FLOOR EMERGENCY ESCAPE LIGHTING AT ROW 13 AND OPERATION CHE CKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996012600479 19960126 00479 NM 1996 1 26 96UAL900059 1 19960123 A 2612 1061096115 FIRE DETECTOR BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE ENGINE INOPERATIVE A UALA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 WP 29 986UA 21748 CREW REPORTS NR TWO ENGINE FIRE WARNING WENT OFF IN CLIMB-OUT. FIRED BOTTLE AND SHUT DOWN ENGINE. REPLACED LOWER FIRE LOOP DETECTOR. TESTED ENGINE FIRE DETECTION SYSTEM. CHECKS O.K. 2 L 7 2 4F 4 F A16WE E2EA 1996012600480 19960126 00480 WP 1996 1 26 ARWA9601001 1 19960117 A 5341 3613917 FITTING DOUG DC8 DC863F 302198F WP LT MLG WW CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LEFT WHEEL WELL FWD BULKHEAD, UPPER OUTER WING ATTACH FORGING AND ADJACENT SKIN HAS LEVEL II CORROSION. CLEANED CORRODE D AREA, CORROSION FOUND TO BE OUT OF LIMITS. CUT OUT CORRODED AREA, FABRICATED DOUBLER, TWO REPAIR STRAPS AND PLUG. IN STALLED IAW DER EO ARW 950173-082, FAA FORM 8110-3 ATTACHED. 2 L 7 4 4F 4A25 1996012600481 19960126 00481 WP 1996 1 26 ARWA9601002 1 19960117 A 5730 SKIN DOUG DC8 DC863F 302198F WP WS 454 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LEFT WING STA 454 NEAR CENTER SPAR HAS 5 INCH CRACK INBOARD AND AFT OF HI-LOCK. REMOVED CRACK, FABRICATED PLUG AND DOUB LER. INSTALLED SAME IAW AVITAS ENGINEERING EO 96AROW002D-1, FAA FORM 8110-3 ATTACHED. 2 L 7 4 4F 4A25 1996012600483 19960126 00483 NM 1996 1 26 DL72S960169 1 19960119 A 5313 65564415 STRINGER BOEING 727 727232 1384082 NM FS 950-990 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 419DA 21272 DURING INSPECTION, CORROSION WAS REMOVED BY BLENDING AND SPOT FACING IN SEVERAL LOCATIONS ON THE UPPER SURFACE OF THE O/ B AND I/B SKIN FLANGES, STRINGER 29L BETWEEN STA 950 AND STA 970. MINIMUM REMAINING FLANGE THICKNESS WAS .100. ALL COR ROSION BLENDS ARE CONSIDERED ACCEPTABLE AS PERMANENT REPAIRS. ALSO, THE STRINGER REQUIRES SPLICING BETWEEN STA 950F AND 970, DUE TO CRACKING AND EXTENSIVE CORROSION BETWEEN STA 970 AND 990. THERE IS AN EXISTING SPLICE LOCATED AT STA 990 P LUS 10. THIS REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH FAA/DER FORM 8110-3, DL ERA 303010 REV A. 2 L 7 3 4F A3WE 1996012600484 19960126 00484 NM 1996 1 26 DL72S960170 1 19960119 A 5314 65454414 KEEL BEAM BOEING 727 727232 1384082 NM BS 950 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 419DA 21272 DURING INSPECTION, THE OUTBD FLANGE OF THE RT KEEL BEAM, STR 29R WAS FOUND WITH CORROSION AT STA 950. DUE TO INTERFEREN CE ITEMS IT WAS NECESSARY TO CUT THE FUSELAGE SKIN TO REMOVE THE CORRODED FLANGE. REPAIR DOUBLERS AND STRAPS WERE INSTA LLED IN ACCORDANCE WITH FAA/DER FORM 8110-3, DER DESIGNATION SO-831, DATED 01-19-96. 2 L 7 3 4F A3WE 1996012600485 19960126 00485 NM 1996 1 26 DL72S960171 1 19960105 A 5754 651622199 SKIN BOEING 727 727232 1384082 NM NR 4 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 495DA 21075 DURING INSP, THE FOLLOWING DAMAGE WAS FOUND REQUIRING MRR'S N/R 0058 CRACKS FOUND IN NR 9 AND NR 18 RIB. REPAIRED PER M /M 57-54-0 FIG 805. N/R 0059 CRACKS FOUND IN REPAIR DOUBLERS ON NR 11 AND 12 RIBS. REPAIRED PER M/M 57-54-00. N/R 006 2 CRACK FOUND IN UPPER SKIN AT FENCE MOUNTING HOLE. REPAIRED PER M/M 57-54-0 FIG 813 FOR NR 4 L/E SLAT. 2 L 7 3 4F A3WE 1996012600486 19960126 00486 NM 1996 1 26 DL72S960172 1 19960105 A 5754 651622199 ANGLE BOEING 727 727232 1384082 NM NR 4 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 495DA 21075 CRACK FOUND IN LWR AFT ATTACH ANGLE. REPAIRED PER M/M 57-54-00 FOR NR 4 L/E SLAT. 2 L 7 3 4F A3WE 1996012600488 19960126 00488 1996 1 26 DL72S960178 4 19960123 A 2565 CABLE BOEING 727 727232 1384082 NM L2 DOOR SLIDE BROKEN A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 499DA 21143 LEFT SERVICE DOOR EVACUATION SLIDE FAILED TO DEPLOY AND PULL HANDLE CAME OFF WHEN PULLED. CABLE ON PULL HANDLE BROKE. R EPLACED DOOR SLIDE PER M/M 25-60-15. 2 L 7 3 4F A3WE 1996012600489 19960126 00489 NM 1996 1 26 DL73E960156 1 19960112 A 5321 FLOOR PANEL BOEING 737 737247 138448D NM FS 777 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 243WA 23517 DURING HMV, LT FIXED FLOOR PANEL AT FS 777 FOUND CORRODED BEYOND LIMITS. REPAIRED PER MM 53-21-04 PG 801. 2 L 7 2 4F A16WE 1996012600490 19960126 00490 1996 1 26 DL73S960144 4 19960121 A 3425 DG BOEING 737 737232 1384475 NM NR 1 INOPERATIVE A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 327DL 23099 AIR TURNBACK, NR 1 COMPASS SYSTEM INTERMITTENTLY INOP, HGD FLAG IN CAPT HSI AND F/O RMI. REPLACED NR 1 DG AND OPS CKS O K. 2 L 7 2 4F RT A16WE 1996012600491 19960126 00491 NM 1996 1 26 DL767960149 1 19960122 A 3260 SENSOR BOEING 767 767232 1385132 NM NLG MALFUNCTIONED A A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 106DA 22218 RETRACTING FLAPS TO UP POSITION AFTER T/O, THE FLAPS AND CONF LIGHT ILLUM WITH ASSOCIATED WARNING. STATUS MSG NOSE A/G DISAGREE STATUS MSG APPEARED. A/C WAS A ATB DUE TO STATUS MSG, NOSE A/G DISAGREE. REPLACED S266 NOSE GEAR COMPRESSED SENSOR. 2 L 7 2 4F RT A1NM 1996012600492 19960126 00492 WP 1996 1 26 DLL10960148 1 19960122 A 5312 1504400 CANTED BLKHD LKHEED 1011 10113851 5265010 WP FS 1212 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 715DA 193C1092 WHILE PERFORMING INSPECTIONS PER SI 7-70645-12, THE FS 1212 CANTED BULKHEAD WAS FOUND WITH CRAL\CKS IN THE TYPICAL MANNE R AT LBL 10, RBL 22.5, RBL 22.5 AND RBL 42.5. THE CRACKS WERE CUT OUT AND REPAIR DOUBLERS WERE INSTALLED PER DL ERA 273 149. 2 L 7 3 4F A23WE 1996012600493 19960126 00493 WP 1996 1 26 DLL10960168 1 19960122 A 5312 1504400113 BULKHEAD LKHEED 1011 10113851 5265010 WP FS 1212 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 713DA 193C1089 WHILE PERFORMING THE SI 7-70645-12 FS 1212 CANTED BULKHEAD INSPECTION, CRACKS WERE FOUND AT FOUR LOCATIONS. REPAIRED PE R DL ERA 273100 RA. 2 L 7 3 4F A23WE 1996012600494 19960126 00494 WP 1996 1 26 DLL15960151 1 19960122 A 3232 ACTUATOR LKHEED 1011 10113853 5265020 WP RT MLG FAILED A DALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 27 753DA 193W1189 ON APPROACH INTO ATL, WHEN THE GEAR WAS EXTENDED THE ACFT LOST C-SYST HYD PRESS. ON INSPECTION FOUND RT MLG RETRACT ACT UATOR LOWER END BLOWN OUT AND THE GEAR DOOR WAS TORN OUT AT THE DOOR ACTUATOR ATTACH STRUCTURE. REPLACED DOOR AND ACTUA TOR. 2 L 7 3 4F A23WE 1996012600495 19960126 00495 WP 1996 1 26 DLL17960163 1 19960122 A 5711 1605415101 SPAR CAP LKHEED 1011 10113853 5265020 WP WS 315/329 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 768DL 193H1216 CRACKS WERE DISCOVERED EMANATING FROM TWO EXISTING FASTENER HOLES AT IWS 329 AND IWS 315. THE CRACKS WERE FOUND IN THE REAR SPAR UPPER CAP AND UPPER WING SKIN. THE SUBJECT HOLES WERE OVERSIZED TO REMOVE THE CRACKS IN THE DAMAGED MEMBERS O NLY. REPAIRS ACCOMPLISHED PER DL ERA 273032AD RB. 2 L 7 3 4F A23WE 1996012600496 19960126 00496 WP 1996 1 26 DLL17960164 1 19960122 A 5330 1608990 SKIN LKHEED 1011 10113853 5265020 WP FS 1677/1685 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 768DL 193H1216 THE FUSELAGE SKIN BETWEEN FS 1677 AND FS 1685 WAS BADLY GOUGED/DENTED BELOW THE C3 DOOR FROM S-27 TO S-33. THE REPAIR H AD BEEN PREVIOUSLY REPAIRED ON A TIME LIMITED BASIS. THIS REVISION PROVIDES PERMANENT REPAIR INSTRUCTIONS. ACCOMPLISHE D REPAIRS PER DL ERA 272973 RB. 2 L 7 3 4F A23WE 1996012600497 19960126 00497 NM 1996 1 26 DLM88960165 1 19960122 A 5330 5924802133 SKIN DOUG MD88 MD88 3023688 NM FS 237 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 943DL 49816 THE FUSELAGE SKIN IS DENTED AFT OF FS 237, 5 INCHES ABOVE THE L-18L CUSP. THE DENT IS APPROXIMATELY .125 INCH BY 3 INCH BY 2.5 INCH. A TIME LIMITED REPAIR WAS ORIGINALLY INSTALLED. THIS REVISION PROVIDES PERMANENT REPAIR INSTRUCTIONS TO THE REPAIR PER DL ERA 272073 REV B. 2 L 7 2 4F RT A6WE 1996012600498 19960126 00498 NM 1996 1 26 DLM88960166 1 19960122 A 5330 5936003 SKIN DOUG MD88 MD88 3023688 NM FS 636 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 943DL 49816 THE FUSELAGE SKIN WAS FOUND WITH EDGE DAMAGE FWD OF THE C2 DOOR. THE DAMAGE WAS TO THE OUTER SKIN ONLY AND AFTER CLEANU P MEASURED APPROX 2 INCH BY 5 INCH. THE PERMANENT REPAIR WILL BE ACCOMPLISHED PER MD88 SRM 53-05 FIG 80 CONFIG 7003. 2 L 7 2 4F RT A6WE 1996012600499 19960126 00499 NM 1996 1 26 DLM88960167 1 19960122 A 5330 5936046 SKIN DOUG MD88 MD88 3023688 NM FS 779-807 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 943DL 49816 CORROSION WAS FOUND UNDERNEATH THE FAIRING RUB STRIP BETWEEN FS 779 AND 807. THE CORROSION WAS REMOVED AND BLENDED OUT WITH THE MAXIMUM DEPTH OF DAMAGE .130 OCCURRING AT FS 807. REPAIRED PER DL ERA 273091 RC. 2 L 7 2 4F RT A6WE 1996012600500 19960126 00500 WP 1996 1 26 MWEA96021 1 19960120 A 5312 WEB DOUG DC9 DC932 3022066 WP BS 996 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 DURING INSPECTION, FOUND WEB AT STA 996 AFT PRESSURE BULKHEAD HAD MODERATE CORROSION FROM LONGERON 28L TO 28R AT 6 O'CLO CK POSITION. INSTALLED REPAIR IAW SRM 53-01 FIG 2 AND RETURNED A/C TO SERVICE. 2 L 7 2 4F A6WE 1996012600501 19960126 00501 WP 1996 1 26 MWEA96022 1 19960120 A 5312 TEE DOUG DC9 DC932 3022066 WP BS 996 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 DURING INSPECTION, FOUND AFT CARGO COMPARTMENT AFT BULKHEAD STA 996 LOWER CENTER SUPPORT TEE ANGLE CORRODED TO EXCESS AT CENTER NUTPLATE LOCATIONS. REMOVED CORROSION AND INSTALLED DOUBLER ANGLE REPAIR IAW SRM 53-01 FIG 2. ACFT RETURNED A/ C TO SERVICE. 2 L 7 2 4F A6WE 1996012600502 19960126 00502 WP 1996 1 26 MWEA96023 1 19960122 A 5320 5917497501 FITTING DOUG DC9 DC932 3022066 WP JACK PAD CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 DURING INSPECTION, FOUND AFT JACK PAD SUPPORT FITTING HAS MODERATE CORROSION. MAINTENANCE REPLACED AFT JACK PAD FITTING IAW SRM 51-30-5. 2 L 7 2 4F A6WE 1996012600503 19960126 00503 NM 1996 1 26 P5CA9600027 1 19960122 A 5730 SKIN BOEING 747 747122 1384872 NM WS 570-590 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND ONE INCH CRACK ON LOWER FLANGE, MIDPOINT ON LEFT WING LEADING EDGE BETWEEN STA 570 TO 590. REPAIRED CRACK PER SRM 57-40-03. 2 L 7 4 4F A20WE 1996012600504 19960126 00504 NM 1996 1 26 P5CA9600028 1 19960124 A 5730 SKIN BOEING 747 747124 1384874 NM WS 585/807 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL 1 CORROSION ON LEFT WING UPPER SURFACE ABOVE THE CENTER WING SPAR AROUND WS 585.62 AND WS 807. REMOVED CORR OSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600505 19960126 00505 NM 1996 1 26 P5CA9600029 1 19960124 A 5730 SKIN BOEING 747 747124 1384874 NM WS 1084 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL 1 CORROSION ON LEFT WING UPPER SURFACE BETWEEN MID AND REAR SPARS AROUND WS 1084. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600506 19960126 00506 NM 1996 1 26 P5CA9600030 1 19960124 A 5330 PANEL BOEING 747 747124 1384874 NM BS 1000 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL 1 CORROSION ON FAIRING SUPPORT AND PANEL ON LOWER FUSELAGE BS 1000 BETWEEN BL 0 AND RBL 25. REMOVED CORROSI ON IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600507 19960126 00507 NM 1996 1 26 P5CA9600031 1 19960124 A 5730 SKIN BOEING 747 747124 1384874 NM WS 1280-1485 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL 1 CORROSION ON LEFT WING LOWER SURFACE AROUND FUEL TANK ACCESS BETWEEN WS 1280 TO 1485. REMOVED CORROSION I AW SRM 51-10-01, VERIFIED WITHIN LIMITS OF SRM 57-10-01. 2 L 7 4 4F A20WE 1996012600508 19960126 00508 NM 1996 1 26 P5CA9600032 1 19960124 A 5730 PANEL BOEING 747 747124 1384874 NM RT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND DELAMINATION ON RT WING LEADING EDGE FIBERGLASS PANEL TOP OF WING, NEAR NR 18 AND NR 19 LEADING EDGE. REPAIRED IA W SRM 51-40-09. 2 L 7 4 4F A20WE 1996012600509 19960126 00509 NM 1996 1 26 P5CA9600033 1 19960124 A 5730 PANEL BOEING 747 747124 1384874 NM RT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND DELAMINATED TOP PANEL ON RIGHT WING FORWARD OF NR 8 SPOILER. REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996012600510 19960126 00510 NM 1996 1 26 P5CA9600034 1 19960124 A 5730 PANEL BOEING 747 747124 1384874 NM LT WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND FIBERGLASS PANEL ON LOWER LEFT WING NEAR NR 3 CANOE CRACKED. REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996012600511 19960126 00511 NM 1996 1 26 P5CA9600035 1 19960124 A 5532 PANEL BOEING 747 747124 1384874 NM VERT STAB DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEFT SIDE PANEL NR 324AL ON VERTICAL STABILIZER DELAMINATED. REPAIRED IAW SRM 51-40-06. 2 L 7 4 4F A20WE 1996012600512 19960126 00512 NM 1996 1 26 P5CA9600036 1 19960124 A 5532 SKIN BOEING 747 747124 1384874 NM RT HORIZ STAB DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND DELAMINATED AREA ON RIGHT STABILIZER UPPER SURFACE AHEAD OF OUTBOARD ELEVATOR AND BEHIND REAR SPAR. REPAIRED IAW SRM 51-40-06. 2 L 7 4 4F A20WE 1996012600513 19960126 00513 NM 1996 1 26 P5CA9600037 1 19960124 A 5520 ELEVATOR BOEING 747 747124 1384874 NM LEFT CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND INBOARD AFT CORNER OF LEFT HAND INBOARD ELEVATOR CRACKED. REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996012600514 19960126 00514 NM 1996 1 26 P5CA9600038 1 19960124 A 5730 PANEL BOEING 747 747124 1384874 NM RT WING PUNCTURED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND HOLE ON INBOARD SURFACE OF LOWER FIXED PANEL, RT WING T/E CAVITY. REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996012600515 19960126 00515 NM 1996 1 26 P5CA9600039 1 19960124 A 5751 PANEL BOEING 747 747124 1384874 NM RT OUTBD AILERON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND CRACKED PANEL BETWEEN TWO INBOARD BALANCE WEIGHTS OF RT OUTBOARD AILERON. REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996012600516 19960126 00516 NM 1996 1 26 P5CA9600040 1 19960124 A 5754 SKIN BOEING 747 747124 1384874 NM RT LE FLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND TOP EDGE CRACKED ON LEADING EDGE FLAPS 19, 23 AND 25 RT WING. REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996012600517 19960126 00517 NM 1996 1 26 P5CA9600041 1 19960124 A 5754 PANEL BOEING 747 747124 1384874 NM LT LE FLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND CRACK ON LEADING EDGE FIBERGLASS PANEL ON LEADING EDGE FLAPS 6, 7, 10, 11. REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996012600518 19960126 00518 NM 1996 1 26 P5CA9600042 1 19960124 A 5754 FLAP BOEING 747 747124 1384874 NM NR 6/7 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND CRACK ON LOWER EDGE OF LEADING EDGE FLAPS 6 AND 7. REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996012600519 19960126 00519 NM 1996 1 26 P5CA9600043 1 19960124 A 5730 SKIN BOEING 747 747124 1384874 NM WS 807 DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND DELAMINATED AREA OVER UPPER WING LEADING EDGE SURFACE ON RT WING APPROX WS 807. REPAIRED SAME IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996012600520 19960126 00520 NM 1996 1 26 P5CA9600044 1 19960124 A 5730 PANEL BOEING 747 747124 1384874 NM RT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND DELAMINATED PANEL ON RT WING UPPER SURFACE NEAR NR 2 SPEED BRAKE. REPAIRED SAME IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996012600521 19960126 00521 NM 1996 1 26 P5CA9600045 1 19960124 A 5753 SKIN BOEING 747 747124 1384874 NM LT TE FLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND CRACK IN LOWER EDGE ON INBOARD EDGE, AFT T/E FLAP LEFT WING. REPAIRED SAME IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996012600522 19960126 00522 NM 1996 1 26 P5CA9600046 1 19960124 A 5240 ACCESS DOOR BOEING 747 747124 1384874 NM NLG CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND NOSE LANDING GEAR SERVICE INTERPHONE ACCESS DOOR CRACKED. REPAIRED SAME IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996012600523 19960126 00523 NM 1996 1 26 P5CA9600047 1 19960124 A 5320 SUPPORT BOEING 747 747124 1384874 NM BS 860 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL 1 CORROSION ON FAIRING SUPPORT LOWER FUSELAGE, BS 860 BETWEEN LBL 40 AND RBL 25. CORROSION REMOVED IAW SRM 51-10-01, FOUND WITHIN LIMITS OF 53-10-01. 2 L 7 4 4F A20WE 1996012600524 19960126 00524 NM 1996 1 26 P5CA9600048 1 19960124 A 5320 SUPPORT BOEING 747 747124 1384874 NM BS 900 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL 1 CORROSION AND CRACKED AIR LOCKS ON FAIRING SUPPORT, LOWER FUSELAGE AT BS 900 BETWEEN BL 0 AND LBL 50. REM OVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF 53-10-01. INSTALLED NEW AIR LOCKS IAW SRM 57-30-02. 2 L 7 4 4F A20WE 1996012600525 19960126 00525 NM 1996 1 26 P5CA9600049 1 19960124 A 5330 PANEL BOEING 747 747124 1384874 NM BS 760-780 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL 1 CORROSION AROUND FASTENERS ON LAV SERVICE PANEL, LOWER FUSELAGE BETWEEN BS 760 TO 780. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. INSTALLED NEW FASTENERS/RIVETS. 2 L 7 4 4F A20WE 1996012600526 19960126 00526 NM 1996 1 26 P5CA9600050 1 19960124 A 5320 SUPPORT BOEING 747 747124 1384874 NM BS 840 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL 1 CORROSION ON FAIRING SUPPORT LOWER FUSELAGE AT BS 840 RIGHT SIDE NEAR STR 37. REMOVED CORROSION IAW SRM 5 1-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600527 19960126 00527 NM 1996 1 26 P5CA9600051 1 19960124 A 5411 FRAME BOEING 747 747124 1384874 NM NR 2 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND RIGHT SIDE FORWARD CORNER ON SLOT SEAL INST FRAME CRACKED. CRACK REMOVED, PATCH FABRICATED FROM 301 1/2 HARD STAI NLESS STEEL AND INSTALLED IAW SRM 54-12-02. 2 L 7 4 4F A20WE 1996012600528 19960126 00528 NM 1996 1 26 P5CA9600052 1 19960124 A 5414 SKIN BOEING 747 747124 1384874 NM NR 2 PYLON CHAFED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND RT INTERIOR SKIN LOWER EDGE CHAFED ON NR 2 PYLON, NS 222. PATCHED AND RIVETED IAW SRM 54-12-02. 2 L 7 4 4F A20WE 1996012600529 19960126 00529 NM 1996 1 26 P5CA9600053 1 19960124 A 5411 FRAME BOEING 747 747124 1384874 NM NR 2 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND CRACKED FRAME AND IMPROPERLY INSTALLED REPAIR DOUBLER ON LEFT HAND SIDE SKIN UPPER MOST OVAL HOLE. OLD REPAIR REM OVED, NEW DOUBLER MANUFACTURED FROM STAINLESS STEEL AND INSTALLED IAW SRM 54-12-02. 2 L 7 4 4F A20WE 1996012600530 19960126 00530 NM 1996 1 26 P5CA9600054 1 19960124 A 5414 SKIN BOEING 747 747124 1384874 NM NR 2 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEFT HAND SIDE SKIN NS 180 LOWER CORNER CRACKED ON INTERIOR SIDE. NEW STRAP FIRE SHIELD MANUFACTURED AND INSTALLE D IAW SRM 54-12-02. 2 L 7 4 4F A20WE 1996012600531 19960126 00531 NM 1996 1 26 P5CA9600055 1 19960124 A 5400 STRAP BOEING 747 747124 1384874 NM NR 3 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND CRACKED STRAP ON BOTH SIDES OF NR 3 SKIRT FORWARD EDGE. REPAIRED IAW SRM 54-12-02. 2 L 7 4 4F A20WE 1996012600532 19960126 00532 NM 1996 1 26 P5CA9600056 1 19960124 A 5414 SKIN BOEING 747 747124 1384874 NM NR 4 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND CRACK IN SKIN FRONT SPAR NS 128.5 AT NR 4 PYLON. REPAIRED IAW SRM 54-12-02. 2 L 7 4 4F A20WE 1996012600533 19960126 00533 NM 1996 1 26 P5CA9600057 1 19960124 A 5411 RIB BOEING 747 747124 1384874 NM NR 4 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND CRACK IN NR 4 PYLON INTERIOR CAVITY RIB NS 163. DEFECTIVE AREA REMOVED AND REPAIRED IAW SRM 54-12-02. 2 L 7 4 4F A20WE 1996012600534 19960126 00534 NE 1996 1 26 P5CA9600058 2 19960124 A 7530 65B975171 VANE BOEING 747 747124 1384874 NM PWA JT9 JT9D7A 52054 NE NR 4 ENG CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 662591 FOUND CRACK ON NR 4 ENGINE CASCADE VANE. CRACK TREATED IAW SRM 51-10-02. 2 L 7 4 4F 4 F A20WE E20EA 1996012600535 19960126 00535 NM 1996 1 26 P5CA9600059 1 19960124 A 5730 SKIN BOEING 747 747124 1384874 NM BS 1000 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL 1 CORROSION ON SKIN ON LOWER CHORD OF FRONT SPAR IN WING CENTER SECTION AT ACCESS TO DRY BAY, BS 1000 APPROX RBL 98. CORROSION REMOVED IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600536 19960126 00536 NM 1996 1 26 P5CA9600060 1 19960124 A 5330 SKIN BOEING 747 747124 1384874 NM BS 2200 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL 1 CORROSION AND SKIN SWELLING ON LOWER FUSELAGE NEAR BS 2200 STR 33. REMOVED CORROSION IAW SRM 51-10-01, FO UND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600537 19960126 00537 NM 1996 1 26 P5CA9600061 1 19960124 A 5730 SPAR CHORD BOEING 747 747124 1384874 NM WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL 1 CORROSION ON FRONT SPAR UPPER CHORD IN WING CENTER SECTION DRY BAY BS 1000 BETWEEN LBL TO RBL 120. REMOVE D CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600538 19960126 00538 NM 1996 1 26 P5CA9600062 1 19960124 A 5730 SKIN BOEING 747 747124 1384874 NM WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL 1 CORROSION ON CEILING SKIN OF WING CENTER SECTION DRY BAY, BETWEEN FRONT SPAR AND S-28C BETWEEN RBL TO LBL 128. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600539 19960126 00539 NM 1996 1 26 P5CA9600063 1 19960124 A 5713 STRINGER BOEING 747 747124 1384874 NM WING CTR SECT CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL 1 CORROSION ON HORIZONTAL STRINGERS IN CEILING OF WING CENTER SECTION DRY BAY, BETWEEN S-23C AND S-29C BETWE EN RBL TO LBL 128. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600540 19960126 00540 NM 1996 1 26 P5CA9600064 1 19960124 A 5711 SPAR CHORD BOEING 747 747124 1384874 NM WING CTR SECT CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL 1 CORROSION AROUND RIVET ON LOWER CHORD OF FRONT SPAR IN WING CENTER SECTION DRY BAY, BS 1000 LBL 57. REMOV ED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600541 19960126 00541 NM 1996 1 26 P5CA9600065 1 19960124 A 5730 SKIN BOEING 747 747124 1384874 NM WING CTR SECT CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL 1 CORROSION ON SKIN ABOVE LOWER CHORD OF FRONT SPAR IN WING CENTER SECTION DRY BAY, BS 1000 LBL 33. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-1. 2 L 7 4 4F A20WE 1996012600543 19960126 00543 NM 1996 1 26 P5CA9600067 1 19960124 A 7110 COWL BOEING 747 747124 1384874 NM PWA JT9 JT9D7A 52054 NE NR 4 ENGINE CHAFED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 662591 FOUND UPPER EDGE CHAFED ON 4R ENGINE SIDE COWL. FABRICATED STRAP AND REPAIRED IAW SRM 51-40-02. 2 L 7 4 4F 4 F A20WE E20EA 1996012600544 19960126 00544 NM 1996 1 26 P5CA9600068 1 19960124 A 5720 BRACKET BOEING 747 747124 1384874 NM LT WING GEAR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND CRACKED BRACKET IN LT WLG DOOR CUTOUT ON LG SUPPORT BEAM. FABRICATED AND INSTALLED NEW BRACKED IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996012600545 19960126 00545 NM 1996 1 26 P5CA9600069 1 19960124 A 5720 BEAM BOEING 747 747124 1384874 NM LT WING GEAR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL 1 CORROSION ON LT WING L/G BEAM AFT SIDE STA 1350. CORROSION REMOVED IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996012600546 19960126 00546 NM 1996 1 26 P5CA9600070 1 19960124 A 5720 BEAM BOEING 747 747124 1384874 NM LT WING GEAR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEVEL 1 CORROSION ON UPPER CHORD OF LT WING L/G BEAM STA 1350. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN L IMITS OF SRM 53-30-01. 2 L 7 4 4F A20WE 1996012600547 19960126 00547 NM 1996 1 26 P5CA9600071 1 19960124 A 5512 PANEL BOEING 747 747124 1384874 NM RT HORIZ STAB DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND RT STABILIZER PANELS 344HB, 344QB, 344JB DELAMINATED. REPAIRED IAW SRM 51-40-06. 2 L 7 4 4F A20WE 1996012600548 19960126 00548 NM 1996 1 26 P5CA9600072 1 19960124 A 5350 FAIRING BOEING 747 747124 1384874 NM BS 1475-1540 DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND DELAMINATED AREAS AND HOLES ON FUSELAGE WING BODY FAIRINGS, BS 1475 TO 1540. REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996012600549 19960126 00549 NM 1996 1 26 P5CA9600073 1 19960124 A 5350 FAIRINGS BOEING 747 747124 1384874 NM BS 1475-1540 DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND DELAMINATED AREAS AND HOLES LT UPPER FUSELAGE AT OVERWING FAIRING, BS 1475 TO 1540. 2 L 7 4 4F A20WE 1996012600550 19960126 00550 NM 1996 1 26 P5CA9600074 1 19960124 A 7110 COWL BOEING 747 747124 1384874 NM PWA JT9 JT9D7A 52054 NE NR 3 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 695757 FOUND LOWER AFT CORNER OF NR 3 LT FAN COWL CRACKED, NR 3 RT FAN COWL CRACKED AT OLD REPAIR. REPAIRED IAW SRM 51-40-06. 2 L 7 4 4F 4 F A20WE E20EA 1996012600551 19960126 00551 NM 1996 1 26 P5CA9600075 1 19960124 A 7110 COWL BOEING 747 747124 1384874 NM PWA JT9 JT9D7A 52054 NE NR 1 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 662320 FOUND CRACK IN OLD REPAIR OF NR 1 RT FAN COWL. REPAIRED IAW SRM 51-40-06. 2 L 7 4 4F 4 F A20WE E20EA 1996012600552 19960126 00552 NM 1996 1 26 P5CA9600076 1 19960124 A 5730 PANEL BOEING 747 747124 1384874 NM LT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND DELAMINATED AREAS ON LEFT WING UPPER SKIN AT T/E BETWEEN SPOILER NR 4 AND INBOARD AILERON AND ON TRIANGLE PANEL IN BOARD TO GATE FITTING. REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996012600553 19960126 00553 NM 1996 1 26 P5CA9600077 1 19960124 A 5730 SKIN BOEING 747 747124 1384874 NM LT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND DELAMINATED AREAS ON LEFT WING L/E UPPER SKIN BEHIND INBOARD SIDE OF L/E FLAP NR 8 AND NR 10. REPAIRED SAME IAW S RM 51-40-09. 2 L 7 4 4F A20WE 1996012600554 19960126 00554 NM 1996 1 26 P5CA9600078 1 19960124 A 5330 SKIN BOEING 747 747124 1384874 NM BS 1475-1540 DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND DELAMINATED AREA AND HOLES ON RT UPPER FUSELAGE AT OVERWING FAIRINGS, BS 1475 TO 1540. REPAIRED SAME IAW SRM 51-4 0-09. 2 L 7 4 4F A20WE 1996012600555 19960126 00555 NM 1996 1 26 P5CA9600079 1 19960124 A 5280 FAIRING BOEING 747 747124 1384874 NM LT MLG DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LT WLG STRUT DOOR FAIRING CRACKED ON FWD AND AFT CORNERS. REPAIRED SAME IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996012600556 19960126 00556 NM 1996 1 26 P5CA9600080 1 19960124 A 5720 TIP BOEING 747 747124 1384874 NM RT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND PANEL DELAMINATED ON RT WING TIP UPPER SURFACE. REPAIRED SAME IAW SRM 51-40-06. 2 L 7 4 4F A20WE 1996012600557 19960126 00557 NM 1996 1 26 P5CA9600081 1 19960124 A 5311 FRAME BOEING 747 747124 1384874 NM BS 2200 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND FRAME LOWER CHORD STA 2200 STR 44 RT SIDE CRACKED. REINFORCED AND REPAIRED SAME IAW SRM 53-10-04. 2 L 7 4 4F A20WE 1996012600558 19960126 00558 NM 1996 1 26 P5CA9600082 1 19960124 A 5512 PANEL BOEING 747 747124 1384874 NM HORIZ STAB DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND DELAMINATED PANELS 334DB, 334HB, 334KB ON LEFT HORIZONTAL STABILIZER. REPAIRED SAME IAW SRM 51-40-06. 2 L 7 4 4F A20WE 1996012600559 19960126 00559 NM 1996 1 26 P5CA9600083 1 19960124 A 2710 EYE BOLTS BOEING 747 747124 1384874 NM CCA ASSY CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND ALL EYE BOLTS ON PUSH-PULL RODS ON CCA PROGRAMMER CORRODED, RT W/G WHEEL WELL. REMOVED CORROSION IAW SRM 53-10-01 , PAINTED IAW CP 20-40-00. 2 L 7 4 4F A20WE 1996012600560 19960126 00560 NE 1996 1 26 SCNA96005 2 19960119 A 7200 ENGINE BOEING 727 727227 1384078 NM PWA JT8 JT8D9 52048 NE NR 3 ENGINE MALFUNCTIONED A SCNA E ENGINE SHUTDOWN O OTHER CL CLIMB 1 GL 15 275AF 22092 DURING CLIMBOUT, THE NUMBER 3 ENGINE FAILED AT FL 210. NO ATTEMPT TO RESTART ENGINE IN FLIGHT WAS MADE. MAINTENANCE EN GINE RUN WAS ACCOMPLISHED PER MM 71-00-30 PAGE 216 AND NO DEFECTS WERE NOTED. 2 L 7 3 4F 4 F A3WE E2EA 1996012600561 19960126 00561 NE 1996 1 26 SCNA96006 2 19960120 A 7260 GEARBOX BOEING 727 727227 1384078 NM PWA JT8 JT8D17R 52049 NE NR 3 ENGINE MALFUNCTIONED A SCNA E ENGINE SHUTDOWN J WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 275AF 22092 700821 THE NR 3 ENGINE SHUT DOWN ON TAXI OUT. FOUND NR 3 ENGINE TO HAVE A GEARBOX PROBLEM, SUN COUNTRY WILL UPDATE THIS REPORT WHEN SHOP FINDINGS ARE AVAILABLE. 2 L 7 3 4F 4 F A3WE E2EA 1996012600562 19960126 00562 NM 1996 1 26 SCNA96007 1 19960121 A 3260 H1010153 SWITCH BOEING 727 727259 138408J NM NLG FAILED A SCNA K NONE N FALSE WARNING CL CLIMB 1 GL 15 289SC 22475 AFTER GEAR RETRACTION, NOSE GEAR INDICATION WAS RED AND GREEN AT THE SAME TIME. REPLACED THE NOSE GEAR LOCK SWITCH PER MM 32-61-01 PAGE 404. PERFORMED NOSE GEAR LOCK AND POSITION SWITCH ADJUSTMENT AND TEST PER MM 32-61-71 PAGE 501. 2 L 7 3 4F A3WE 1996012600563 19960126 00563 NM 1996 1 26 SCNA96008 1 19960121 A 3260 MS2500111 SWITCH BOEING 727 727259 138408J NM NLG LACK OF LUBE A SCNA K NONE N FALSE WARNING CL CLIMB 1 GL 15 289SC 22475 AFTER GEAR RETRACTION, NOSE GEAR INDICATION WAS RED AND GREEN AT THE SAME TIME. JACKED NOSE OF THE AIRCRAFT, SWUNG GEAR , LUBED AND CLEANED THE DOWNLOCK SWITCH. INDICATION CHECKED NORMAL. 2 L 7 3 4F A3WE 1996012600564 19960126 00564 NM 1996 1 26 SCNA96009 1 19960122 A 3260 H1010154 SWITCH BOEING 727 727259 138408J NM NLG CORRODED A SCNA O OTHER N FALSE WARNING CL CLIMB 1 GL 15 289SC 22475 AFTER GEAR RETRACTION NOSE GEAR INDICATION WAS RED AND GREEN AT THE SAME TIME. FOUND THE LANDING GEAR POSITION SWITCH ( S93) CORRODED AND HANGING UP. REMOVED AND REPLACED SWITCH AND CANNON PLUG (D300). INDICATION CHECKED GOOD PER B727, MM 32-61-71. 2 L 7 3 4F A3WE 1996012600565 19960126 00565 NM 1996 1 26 UPS405284 1 19960109 A 5711 SPAR BOEING 747 747123 1384873 NM WS 1000 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 AMS - WHILE IN FOR C-CHECK, CORROSION ON LWR FRONT SPAR CHORD BBSTA 1000 NEAR STA 38L. REMOVED CORROSION PER SRM 57-10- 01 FIG 1, OUT OF LIMIT. REWORKED CORROSION SPOT PER KLM DFX 96-001 BOEING APPROVAL. 2 L 7 4 4F A20WE 1996012600628 19960126 00628 SO 1996 1 26 C2XA96IA001 1 19960104 A 5347 12015997003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 31711 120107 IAH - DURING 1C INSPECTION, FOUND RIGHT FORWARD UPPER SEAT TRACK CORRODED IN SEVERAL AREAS. MAINTENANCE REMOVED AND REP LACED THE SEAT TRACK, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996012600629 19960126 00629 SO 1996 1 26 C2XA96IA002 1 19960104 A 5347 12015994003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 31711 120107 IAH - DURING 1C INSPECTION, FOUND LEFT FORWRAD UPPER SEAT TRACK CORRODED AT FWD END. MAINTENANCE REMOVED AND REPLACED T HE SEAT TRACK, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996012600630 19960126 00630 SO 1996 1 26 C2XA96IA003 1 19960104 A 5347 12015995003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 31711 120107 IAH - DURING 1C INSPECTION, FOUND LEFT FORWARD LOWER SEAT TRACK CORRODED IN SEVERAL AREAS. MAINTENANCE REMOVED AND REPL ACED THE SEAT TRACK, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996012600631 19960126 00631 SO 1996 1 26 C2XA96IA004 1 19960104 A 5347 12026864007 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 31711 120107 IAH - DURING 1C INSPECTION, FOUND LEFT AFT LOWER SEAT TRACK CORRODED IN SEVERAL AREAS. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996012600634 19960126 00634 SO 1996 1 26 C2XA96IA007 1 19960105 A 5720 12061341607 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 31711 120107 IAH - DURING 1C INSPECTION, FOUND LEFT WING UPPER SURFACE SKIN SUPPORT CRACKED AT RIB NR 15. THE SKIN SUPPORT IS LOCATE D 3RD AFT OF AUXILIARY SPAR. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE . (M) 2 L 7 2 4T RT A31SO 1996012600635 19960126 00635 SO 1996 1 26 C2XA96IA008 1 19960105 A 5720 12061341607 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 31711 120107 IAH - DURING 1C INSPECTION, FOUND LEFT WING UPPER SURFACE SKIN SUPPORT CRACKED AT RIB NR 15. THE SKIN SUPPORT IS LOCATE D 4TH AFT OF AUXILIARY SPAR. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE . (M) 2 L 7 2 4T RT A31SO 1996012600636 19960126 00636 SO 1996 1 26 C2XA96IA009 1 19960105 A 5720 12061341611 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 31711 120107 IAH - DURING 1C INSPECTION, FOUND RIGHT WING LOWER SURFACE SKIN SUPPORT CRACKED AT RIB NR 15. THE SKIN SUPPORT IS LOCAT ED 5TH AFT OF AUXILIARY SPAR. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRFT APPROVED FOR RETURN TO SERVICE. (M ) 2 L 7 2 4T RT A31SO 1996012600637 19960126 00637 SO 1996 1 26 C2XA96IA010 1 19960105 A 5720 12061341613 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 31711 120107 IAH - DURING 1C INSPECTION, FOUND RIGHT WING LOWER SURFACE SKIN SUPPORT CRACKED AT RIB NR 15. THE SKIN SUPPORT IS LOCAT ED 4TH AFT OF AUXILIARY SPAR. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVIC E. (M) 2 L 7 2 4T RT A31SO 1996012600638 19960126 00638 SO 1996 1 26 C2XA96IA011 1 19960105 A 5720 12061341615 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 31711 120107 IAH - DURING 1C INSPECTION, FOUND RIGHT WING LOWER SURFACE SKIN SUPPORT CRACKED AT RIB NR 15. THE SKIN SUPPORT IS LOCAT ED 3RD AFT OF AUXILIARY SPAR. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVIC E. (M) 2 L 7 2 4T RT A31SO 1996012600639 19960126 00639 SO 1996 1 26 C2XA96IA012 1 19960105 A 5720 12061341617 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 31711 120107 IAH - DURING 1C CHECK INSPECTION, FOUND RIGHT WING LOWER SURFACE SKIN SUPPORT CRACKED AT RIB NR 15. THE SKIN SUPPORT IS LOCATED 2ND AFT OF AUXILIARY SPAR. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996012600640 19960126 00640 SO 1996 1 26 C2XA96IA013 1 19960105 A 5720 12017056015 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 31711 120107 IAH - DURING 1C CHECK INSPECTION, FOUND RIGHT WING LOWER SURFACE SKIN SUPPORT CRACKED AT RIB NR 16. THE SKIN SUPPORT IS LOCATED 3RD AFT OF AUXILIARY SPAR. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996012600670 19960126 00670 WP 1996 1 26 IXXA9569 1 19960103 A 3040 CONNECTOR DOUG DC8 DC863F 302198F WP RT WINDSHIELD LOOSE A IXXA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 23 784AL 46135 BETWEEN KNGU AND BIKF, AN ELECTRICAL SMELL AND A SMALL AMOUNT OF SMOKE WERE NOTED COMING FROM THE FIRST OFFICERS WINDSHI ELD AREA. IN KNGU, NO SOURCE COULD BE IDENTIFIED FOR THE SMELL. THE WINDSHIELD HEAT WAS PRECAUTIONARILY DEFERRED FOR F URTHER TROUBLESHOOTING. FURTHER TROUBLESHOOTING REVEALED A LOOSE ELECTRICAL CONNECTOR AT THE FIRST OFFICERS WINDOW HEAT SENSOR. THE LOOSE CONNECTION WAS SECURED, AND THE WINDSHIELD HEAT WAS RETURNED TO SERVICE. (M) 2 L 7 4 4F 4A25 1996012600672 19960126 00672 WP 1996 1 26 IXXA9594 1 19960103 A 3230 UPLATCH CABLE DOUG DC8 DC871 302199A WP LT MLG DOOR OUT OF ADJUST A IXXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 824BX 45946 ON TAKEOFF FROM TOL TO ONT, THE CREW REPORTED AN UNSAFE GEAR AND DOOR LIGHT AFTER GEAR RETRACTION. THE AIRCRAFT RETURNE D TO TOL FOR MAINTENANCE. THE AIRCRAFT WAS FERRIED TO A MAINTENANCE FACILITY FOR LANDING GEAR SYSTEM INSPECTION AND RI G CHECK. A RIG CHECK OF THE LANDING GEAR MECHANICAL CONTROL SYSTEM WAS ACCOMPLISHED. AN INITIAL GEAR TEST SHOWED THE L EFT MLG DOOR UPLATCH OUT OF RIG. THE LEFT MLG DOOR UPLATCH CABLE AND DOOR ROLLER MECHANISM WERE RIGGED. FINAL LANDING GEAR OPERATIONAL CHECK WAS NORMAL, AND THE AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 4 4F 4A25 1996012600744 19960126 00744 EU 1996 1 26 SIMA960021 1 19960102 A 2620 E0052R8B3ASWE CONNECTOR AEROSP ATR42 ATR42300 8680920 EU NR 1 ENGINE DIRTY A SIMA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SW 21 424MQ 045 ORD - FLT NR 4100 - ENGINE FIRE BOTTLE DISCHARGE LIGHTS ILLUMINATED DURING TAXI, RETURNED TO GATE. RAI'D CANNON PLUG ON FIRE BOTTLE NR 1 SQUIB ON THE NR 1 ENGINE, OPS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996012600755 19960126 00755 NM 1996 1 26 9601702291 1 19960120 A 2780 RETRACT MECH BOEING 727 727251 138408H NM LE FLAPS OUT OF ADJUST A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 GL 01 291US 21379 DURING TAKEOFF ROLL, TAKEOFF WARNING HORN SOUNDED. TAKEOFF WAS ABORTED WITHOUT INCIDENT. RESET FLAP TRIM. SECOND TAKE OFF WAS SUCCESSFUL. REPLACED THE LEADING EDGE SWITCHES S311 AND S312 AND RIGGED FOLLOW-UP DRUM. PERFORMED TAKEOFF WARN ING TEST. CHECKED OK. 2 L 7 3 4F A3WE 1996012600756 19960126 00756 NM 1996 1 26 9601712286 1 19960120 A 3260 BULB BOEING 727 727251 138408H NM RT MLG FAILED A NWAA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 GL 01 286US 21325 DURING APPROACH INTO MSP, NO GEAR DOWN AND LOCKED ON RIGHT LANDING GEAR. AIRCRAFT MADE A GO-AROUND AND LANDED ON SECOND APPROACH WITHOUT INCIDENT. REPLACED THE LIGHT BULB. CHECKED OK. 2 L 7 3 4F A3WE 1996012600757 19960126 00757 WP 1996 1 26 9601729871 1 19960123 A 3397 WIRE DOUG DC9 DC951 3022051 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 780NC 48102 DURING LINE CHECK, FOUND WIRING FOR RIGHT OVERHEAD EMERGENCY EXIT LIGHTS BROKEN. REPAIRED WIRES. OPERATIONAL CHECK GOO D. 2 L 7 2 4F RT A6WE 1996012600758 19960126 00758 WP 1996 1 26 9601739866 1 19960124 A 3260 PROX SWITCH DOUG DC9 DC951 3022051 WP NLG MALFUNCTIONED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 775NC 47785 DURING CLIMB, THE NOSE LANDING GEAR UNSAFE LIGHT ILLUMINATED. PERFORMED COCKPIT OPERATING MANUAL PROCEDURE AND THE LIGH T REMAINED ILLUMINATED. AIRCRAFT CONTINUED TO DESTINATION AND ACCOMPLISHED TOWER FLYBY AND LANDED WITHOUT INCIDENT. RE PLACED THE NOSE LANDING GEAR DOWNLOCK PROXIMITY SWITCH. OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600759 19960126 00759 WP 1996 1 26 9601749912 1 19960120 A 3230 UPLOCK HOOK DOUG DC9 DC931 3022065 WP LT MLG OUT OF ADJUST A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 962N 47406 DURING CLIMB, THE LEFT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED AFTER LANDING GEAR RETRACTION. RECYCLED LANDING GEAR AND LIGHT EXTINGUISHED. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. FOUND RIGHT MAIN LANDING GEAR U PLOCK HOOK HINGE BOLT TOO TIGHT. RETORQUED BOLT. OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996012600760 19960126 00760 NE 1996 1 26 9601751162 2 19960122 A 7260 GEAR BOX DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 2 ENGINE LEAKING A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 162US 46771 86168 AFTER TAKEOFF, THE NR 2 ENGINE OIL DECREASED RAPIDLY. CREW FOLLOWED COCKPIT OPERATING PROCEDURE AND RETURNED TO MSP. R EPLACED STARTER DRIVE SEAL, BOTH HYDRAULIC PUMP DRIVE SEALS, GEAR BOX, AND BREATHER VALVE. PERFORMED LEAK CHECK. ENGIN E RUN-UP WAS NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A22WE E20EA 1996012600761 19960126 00761 NM 1996 1 26 9601762703 1 19960124 A 3350 POWER SUPPLY BOEING 727 727225 1384077 NM DOOR 1L INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8878Z 21451 DURING PRE-FLIGHT, FOUND EMERGENCY LIGHT AT DOOR 1L INOPERATIVE. REPLACED THE POWER SUPPLY. CHECKED OK. 2 L 7 3 4F A3WE 1996012600762 19960126 00762 NM 1996 1 26 9601775513 1 19960124 A 3350 BPS73 POWER SUPPLY BOEING 757 757251 1384970 NM DOOR 3R INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 513US 23201 DURING OVERNIGHT MAINTENANCE, FOUND DOOR 3R EMERGENCY LIGHT INOPERATIVE. REPLACED THE POWER SUPPLY. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A2NM 1996012600763 19960126 00763 EU 1996 1 26 9601783223 1 19960122 A 3260 INDICATION AIRBUS 320 A320211 3930320 EU LANDING GEAR MALFUNCTIONED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 323US 272 DURING APPROACH INTO LAS AFTER LANDING GEAR EXTENSION, RECEIVED L/G GEAR NOT DOWN LOCKED MESSAGE. CYCLED LANDING GEAR H ANDLE AND ALL INDICATIONS WERE NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTION REVEALED NO DISCREPANC IES. 2 L 7 2 4F RT A28NM 1996012600764 19960126 00764 WP 1996 1 26 9601799601 1 19960123 A 3231 59164605509 SELECTOR VALVE DOUG DC9 DC932 3022066 WP MLG DOOR MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 GL 01 601NW 451 47038 DURING APPROACH INTO DSM, LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS EXTENDED. RECYCLED GEAR WITH NO HELP. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE LEFT MAIN GEAR DOOR ACTUATOR WITH NO HELP. REPLACE D THE MAIN LANDING GEAR SELECTOR VALVE. OPERATIONAL CHECK NORMAL ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996012600765 19960126 00765 WP 1996 1 26 9601809154 1 19960122 A 3350 BATTERY DOUG DC9 DC914 3022034 WP COCKPIT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8913E 45830 DURING PRE-FLIGHT CHECK, COCKPIT EMERGENCY LIGHTS WOULD NOT ILLUMINATE. REPLACED THE EMERGENCY LIGHT BATTERIES. OPERAT IONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996012600766 19960126 00766 NM 1996 1 26 9601816301 1 19960124 A 3350 CONNECTOR BOEING 747 747451 1384940 NM UPPER DECK LOOSE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 661US 23719 DURING LINE CHECK, THE UPPER DECK FLOOR PATH EMERGENCY LIGHTS AT SEAT ROWS 77 TO 79 WERE FOUND INOPERATIVE. RECONNECT ED LIGHT ASSEMBLY PIN AT SEAT 77. OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996012600767 19960126 00767 NM 1996 1 26 9601826308 1 19960124 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 668US 24223 DURING PRE-FLIGHT CHECK, THE CEILING MOUNTED EMERGENCY LIGHTS ILLUMINATED AND WOULD NOT EXTINGUISH. REPLACED THE BATTER Y PACK. OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996012600768 19960126 00768 NM 1996 1 26 9601836310 1 19960124 A 3350 LIGHT BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 670US 24225 DURING LINE CHECK (TPE), THE FLOOR PATH EMERGENCY LIGHTS BETWEEN SEAT ROWS 24R TO 31R WERE FOUND INOPERATIVE. RECONNECT ED LOOSE LIGHT ASSEMBLY. OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996012600769 19960126 00769 NM 1996 1 26 9601846301 1 19960124 A 3350 CONNECTOR BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 661US 23719 DURING LINE CHECK, THE FLOOR PATH EMERGENCY LIGHTS BETWEEN SEAT ROWS 25L TO 35L WERE FOUND INOPERATIVE. RECONNECTED LIG HTS ASSEMBLY PIN AT SEAT 25. OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996012600770 19960126 00770 NM 1996 1 26 96FDEA00120 1 19960124 A 2750 163087 TRANSMITTER BOEING 727 72722 1384002 NM TE FLAPS WORN A A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 191FE 19084 AFTER TAKEOFF DURING FLAP RETRACTION. THE OUTBOARD FLAPS BECAME ASYMMETRICAL BETWEEN THE ZERO AND 2 DEGREE INDICATOR, R EPEAT WRITE UP. FOUND RT OUTBOARD TRANSMITTER SECURING COLLAR LOOSE, ADJUSTED TRANSMITTER AND TIGHTENED COLLAR PER MM 2 7-52-12. RAN FLAPS SEVERAL TIMES, OPS CK GOOD. SUGGEST REPLACING RT OUTBOARD FLAP TRANSMITTER AND LOCKING COLLAR DUE T O POSSIBILITY OF COLLAR AND/OR TRANSMITTER SHAFT WORN. 2 L 7 3 4F A3WE 1996012600771 19960126 00771 NE 1996 1 26 96FDEA00121 2 19960124 A 7200 ENGINE BOEING 727 727227 1384078 NM PWA JT8 JT8D17 52049 NE NR 3 OIL LOSS A FDEA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION UK UNKNOWN 1 SO 25 482FE 21464 AT APPROXIMATELY FLIGHT LEVEL 220, NR 3 LOW OIL PRESSURE/FILTER BYPASS LIGHT FLASHED ON AND OFF. CONFIRMING LOW PRESSUR E ZERO QUANTITY AND RED LINE OIL TEMPERATURE. ENGINE WAS SHUT DOWN, LANDING ACCOMPLISHED DFW. REPLACED NR 3 ENGINE PER WORK CARDS 70T0001, 70T0003, 70T0301, AND C/W FEC-M-0485 ENGINE RUN FORM, ALL OPS AND LEAK CKS GOOD. 2 L 7 3 4F 4 F A3WE E2EA 1996012600772 19960126 00772 WP 1996 1 26 96FDEA00122 1 19960124 A 5512 SKIN DOUG DC10 DC1010 3022110 WP LT STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 CRACK INDICATION ON LT STAB L/E AT UPPER FWD TANG. CRACK EXTENDS ITSELF ACROSS FASTENER HOLE APPROX 1.25 INCH IN LENGTH . CRACK LOCATION IS 5 INCHES I/B OF CLOSURE RIB AREA. REPAIRED CRACK IN REF TO SRM 55-20-00 FIG 9 AND 10. ALSO, PER E A 8-5510-21035A. 2 L 7 3 4F A22WE 1996012600804 19960126 00804 WP 1996 1 26 ABXA9600071 1 19960123 A 2910 AE2460001J0630 HYD HOSE DOUG DC8 DC861 3021952 WP NR 2 ENGINE FAILED A ABXA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 23 843AX 46017 DURING CRUISE, HYDRAULIC QUANTITY DROPPED TO STANDPIPE LEVEL. FOUND HYDRAULIC PRESSURE LINE BLOWN ON NR 2 ENGINE. REPL ACED PRESSURE LINE AND THE NR 2/NR 3 HYDRAULIC PUMPS IAW DC8 MM, CHAPTER 29-10-12. OPS CHECK AND LEAK CHECK WERE GOOD. 2 L 7 4 4F 4A25 1996012600805 19960126 00805 SO 1996 1 26 COMA9610036 1 19960124 A 3260 PROX SENSOR EMB 120 EMB120RT SO LANDING GEAR MALFUNCTIONED A COMA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 01 268CA 120262 LANDING GEAR DID NOT EXTEND WHEN SELECTED TO DOWN. PLACED THE B-SYSTEM PROXIMITY SENSOR ON DEFERRED MAINTENANCE LIST AN D ACFT CONTINUED SERVICE. 2 L 7 2 4T RT A31SO 1996012600806 19960126 00806 SO 1996 1 26 COMA9610037 1 19960123 A 3411 PITOT SYST EMB 120 EMB120RT SO RIGHT CONTAMINATED A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 156CA 120156 COPILOT'S AIR SPEED INDICATOR FAILED DURING FLIGHT. CLEANED MOISTURE FROM COPILOT'S PITOT SYSTEM. ACFT RETURNED TO SER VICE. 2 L 7 2 4T RT A31SO 1996012600807 19960126 00807 SO 1996 1 26 COMA9610038 1 19960123 A 7931 SEDLOC4BC OIL PRESS GAUGE EMB 120 EMB120RT SO RT ENGINE DEFECTIVE A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 462CA 12382 4164 120264 RIGHT ENGINE OIL PRESSURE INDICATES ZERO. REPLACED THE RT ENGINE OIL PRESSURE GAUGE. PART TOTAL CYCLES, 12,823. 2 L 7 2 4T RT A31SO 1996012600808 19960126 00808 EU 1996 1 26 COMA9630022 1 19960124 A 3020 ND00752200 CONTROLLER SAAB SF340 SF340A 7850100 EU RT ENGINE FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 359CA 3886 226 340A053 RIGHT ENGINE INLET HEAT FAILED. REPLACED THE INLET HEAT CONTROLLER AND LOAD MONITOR. PART TOTAL CYCLES, 4566. 2 L 7 2 4T RT A52EU 1996012600809 19960126 00809 NE 1996 1 26 COMA9630023 2 19960123 A 7320 7086M60G11 ECU SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LT ENGINE MALFUNCTIONED A A COMA E A ENGINE SHUTDOWN UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 SO 01 340SF 13783 340A014 367108 LEFT ENGINE SHUT DOWN IN-FLIGHT. TORQUE WAS ERRATIC FOR 3 SECONDS AND THEN SHUT DOWN BY ITSELF. PROBLEM COULD NOT BE D UPLICATED. ENGINE WAS INSPECTED AND NO DEFECTS NOTED. THE ELECTRONIC CONTROL UNIT WAS REPLACED AS A PRECAUTIONARY MEAS URE. PART TOTAL CYCLES, 15,108. 2 L 7 2 4T 4 T RT A52EU E8NE6 1996012600810 19960126 00810 EU 1996 1 26 COMA9630024 1 19960124 A 3060 666000094 BRUSH BLOCK SAAB SF340 SF340A 7850100 EU LT PROP WORN A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 361CA 340A056 LEFT PROPELLER DEICE IS INOPERATIVE. REPLACED THE PROPELLER DEICE BRUSH BLOCK ASSY. 2 L 7 2 4T RT A52EU 1996012600811 19960126 00811 EA 1996 1 26 COMA9660021 1 19960119 A 5270 WARNING CNDAIR CL600 CL6002B19 EA PAX DOOR MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 924CA 7026 PASSENGER DOOR OUTER HANDLE WARNING MESSAGE ON EICAS. PROBLEM COULD NOT BE DUPLICATED. OPERATION OF CABIN DOOR AND IND ICATION SYSTEM WERE NORMAL. 2 L 7 2 4F RT A21EA 1996012600812 19960126 00812 NM 1996 1 26 P5CA9600084 1 19960124 A 2820 COUPLING BOEING 747 747122 1384872 NM NR 1 PYLON LOOSE A A P5CA F ACTIVATE FIRE EXT. A FLAME/FIRE IN INSP/MAINT 1 WP 23 851FT 19756 ON BLOCK IN, GROUND PERSONNEL SAW TAILPIPE FIRE, NR 1 ENGINE. CREW DISCHARGED FIRE BOTTLE AND MOTORED ENGINE, PUT OUT F IRE. INSPECTED ENGINE AND PYLON FOR DAMAGE, NO STRUCTURES FOUND DAMAGED. FOUND AFT-MOST FUEL FEED LINE COUPLING LOOSE AND FUEL LEAK IN NR 1 PYLON. FOUND SAFETY WIRE BROKEN AT PIG TAIL. REPLACED O-RING AND TIGHTENED COUPLING IAW MM 28-22 -07, OPS AND LEAK CHECK OK. PYLON CONDUCTIVITY INSPECTION OK. 2 L 7 4 4F A20WE 1996012600813 19960126 00813 NM 1996 1 26 P5CA9600085 1 19960123 A 5320 65B108651 SUPPORT BEAM BOEING 747 747122 1384872 NM WS 432.65 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND SUPPORT BEAM CRACKED IN PREVIOUS REPAIR. REPAIRED PER SRM 51-40-03, WEB REPLACED WITH 2024-T3.040 MATERIAL. 2 L 7 4 4F A20WE 1996012600814 19960126 00814 NM 1996 1 26 P5CA9600086 1 19960123 A 5743 SUPPORT FTG BOEING 747 747122 1384872 NM LT WING MLG CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 DURING SSID INSPECTION, NOTED INDICATION OF CRACK ON OUTBOARD WING GEAR SUPPORT FITTING. REMOVED FITTING AND REPAIRED P ER S/B 747-57-2244. BORED TO FIRST OVERSIZE, MAG PART INSP COMPLETED, FITTING REINSTALLED. 2 L 7 4 4F A20WE 1996012600815 19960126 00815 NM 1996 1 26 P5CA9600087 1 19960123 A 5751 65B022332 FITTING BOEING 747 747122 1384872 NM RT INBD AILERON WORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND BOTH FORWARD AND AFT INBOARD FAIL-SAFE FITTINGS ON RT INBOARD AILERON DUE TO LOOSE RIVETS IN PREVIOUS REPAIR. REM OVED FITTINGS, REPAIRED WEB, REINSTALLED NEW BUSHINGS AND FITTINGS IAW SRM 57-51 02A-001A AND 57-42-14-001. 2 L 7 4 4F A20WE 1996012600816 19960126 00816 SO 1996 1 26 SWIA95710 1 19960118 A 3230 RETRACT MECH EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LANDING GEAR MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 196SW 120151 LANDING GEAR COULD NOT COME UP. INSTALLED TWO NEW HARNESSES ON RIGHT MAIN GEAR FOR A+ AND B+ INTRANSIT LIGHT. SET GAP TO PROPER SETTING PER MAINTENANCE MANUAL. SWUNG GEAR SEVERAL TURNS AND OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1996012600817 19960126 00817 NM 1996 1 26 UPS205300 1 19960119 A 5320 INTERCOSTAL BOEING 727 72721C 138400M NM BS 682 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON INTERCOSTAL STA 682, RBL 10 - LBL 10, WL 152. REPLACED STRUCTUR E LBL 10 - RBL 10, STA 682, WL 152 I/A/W SRM 51-29-1. 2 L 7 3 4F A3WE 1996020200001 19960202 00001 WP 1996 2 2 9601551225 1 19960103 A 5330 SKIN DOUG DC10 DC1030 3023501 WP RADIO ALT MOUNT CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 225NW 46582 DURING T-CHECK, FOUND CORROSION ON THE MOUNTING RINGS FOR ALL 4 RADIO ALTIMETER MOUNTING RINGS. REPAIRED RINGS (P/N AYB 7022-1; AYB 7053-1, -501) PER EA 12-103877. 2 L 7 3 4F A22WE 1996020200002 19960202 00002 WP 1996 2 2 9601569139 1 19960108 A 5311 FRAME DOUG DC9 DC914 3022034 WP FS 58 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 948L 47049 DURING H-CHECK, FOUND A 4 INCH CRACK IN THE FS 58 FRAME AT THE 12 O'CLOCK POSITION. REPAIRED FRAME (P/N 9911502-3) PER EA 91-102024. 2 L 7 2 4F A6WE 1996020200003 19960202 00003 WP 1996 2 2 9601579139 1 19960108 A 5320 SUPPORT DOUG DC9 DC914 3022034 WP FS 230-260 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 948L 47049 DURING H-CHECK, FOUND CORROSION ON THE CENTERLINE FLOOR SUPPORT FS 230 TO 260. REPAIRED SUPPORT (P/N 5910137-7) PER EA 91-102025. 2 L 7 2 4F A6WE 1996020200004 19960202 00004 NM 1996 2 2 9601585506 1 19960109 A 5320 SILL BOEING 757 757251 1384970 NM CARGO DOOR CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 506US 23195 DURING T-CHECK, FOUND CORROSION ON THE AFT CARGO DOOR LOWER SILL INNER CHORD. REPAIRED CHORD (P/N 146N8522-51), PER EA 55-104364. 2 L 7 2 4F RT A2NM 1996020200005 19960202 00005 WP 1996 2 2 9601599139 1 19960109 A 5240 DOUBLER DOUG DC9 DC914 3022034 WP FWD SERV DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 948L 47049 DURING H-CHECK, FOUND A CRACK ON THE FORWARD SERVICE DOOR JAMB, LOWER AFT CORNER. REPAIRED DOUBLER (P/N 5911407-33), PE R EA 91-104980. 2 L 7 2 4F A6WE 1996020200006 19960202 00006 WP 1996 2 2 9601601225 1 19960110 A 5330 SKIN DOUG DC10 DC1030 3023501 WP FS 1950-1958 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 225NW 46582 DURING T-CHECK, FOUND CORROSION ON THE FUSELAGE SKIN FS 1950 TO 1958, LONGERON 50L TO 52. REPAIRED SKIN (P/N AGA 7418-1 ) PER EA 12-104396. 2 L 7 3 4F A22WE 1996020200007 19960202 00007 NM 1996 2 2 9601612298 1 19960112 A 5320 ANGLE BOEING 727 727251 138408H NM FS 1263 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 298US 22152 DURING H-CHECK, FOUND A CRACK IN THE VERTICAL STAIRWELL TORQUE BOX, RIGHT SIDE BS 1263 FRAME CHORD ANGLE. REPAIRED ANGL E PER EA 22-103436. 2 L 7 3 4F A3WE 1996020200008 19960202 00008 EU 1996 2 2 9601623214 1 19960112 A 5313 LONGERON AIRBUS 320 A320211 3930320 EU FS 14300-14834 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 314US 160 DURING 1C1 CHECK, FOUND CORROSION ON FUSELAGE STRINGERS 41R, 43R AND 44 EACH BETWEEN FRAMES 33 TO 34. REPAIRED STRINGER S PER EA 32-105085, -105086 AND -105087. 2 L 7 2 4F RT A28NM 1996020200009 19960202 00009 NM 1996 2 2 9601632298 1 19960115 A 5313 LONGERON BOEING 727 727251 138408H NM FS 1000 CORROSION A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 298US 22152 DURING H-CHECK, FOUND CORROSION ON STR 29L AT BS 1000. REPAIRED STRINGER (P/N 65-56144-3), PER EA 22-103431. 2 L 7 3 4F A3WE 1996020200010 19960202 00010 NM 1996 2 2 9601642298 1 19960115 A 5210 FRAME BOEING 727 727251 138408H NM PAX DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 298US 22152 DURING P-CHECK, FOUND A CRACK IN THE MAIN CABIN DOOR FRAME AT THE UPPER HINGE RELIEF. REPAIRED DOOR (P/N 50-7945-177), PER EA 22-103435. 2 L 7 3 4F A3WE 1996020200011 19960202 00011 NM 1996 2 2 9601652298 1 19960116 A 5313 LONGERON BOEING 727 727251 138408H NM FS 623 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 298US 22152 DURING H-CHECK, FOUND CORROSION ON STR 27R AT BS 623. REPAIRED STRINGER (P/N 65-56236), PER EA 22-103428. 2 L 7 3 4F A3WE 1996020200012 19960202 00012 WP 1996 2 2 9601661157 1 19960118 A 5313 LONGERON DOUG DC10 DC1040 3023508 WP FS 1509-1521 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 157US 46766 DURING L-CHECK, FOUND CORROSION ON THE RBL 7 LONGERON FITTING FROM FS 1509 TO 1521 IN THE CENTER GEAR WHEEL WELL. REPLA CED THE FITTING PER SRM 51-00-00 FIG 2. 2 L 7 3 4F A22WE 1996020200013 19960202 00013 WP 1996 2 2 9601679606 1 19960118 A 5320 CASTING DOUG DC9 DC932 3022066 WP FS 70 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 606NW 47225 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE LEFT DIAGONAL WEB ATTACH CASTING IN THE NOSE LANDING GEAR WHEEL WELL FS 70. REPLACED CASTING PER SRM 51-01. 2 L 7 2 4F A6WE 1996020200014 19960202 00014 NM 1996 2 2 9601686719 1 19960119 A 5320 FITTING BOEING 747 747251F 1384898 NM FS 1264-1268 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 619US 21321 DURING P-CHECK, FOUND CORROSION ON THE INNER KEEL BEAM BOX FITTING BS 1264 TO 1268 RBL 4 TO RBL 8. REPLACED FITTING PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996020200015 19960202 00015 WP 1996 2 2 9601699154 1 19960121 A 5755 FITTING DOUG DC9 DC914 3022034 WP SPOILER CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8913E 45830 DURING LINE CHECK, FOUND A CRACK IN THE RIGHT WING INBOARD SPOILER CENTER HINGE FITTING. REPLACED SPOILER (P/N 591055-5 16), PER MM 27-61-1 PG 401 TO 406. 2 L 7 2 4F A6WE 1996020200016 19960202 00016 WP 1996 2 2 9601859865 1 19960122 A 5320 FITTING DOUG DC9 DC951 3022051 WP FS 674 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 774NC 47776 DURING H-CHECK, FOUND A CRACK IN THE FS 674 FLOORBEAM RIGHT SIDE END FITTING. REPLACED FITTING (P/N 3912075-2N), PER SR M 51-30-1 AND -5. 2 L 7 2 4F A6WE 1996020200017 19960202 00017 NM 1996 2 2 9601866730 1 19960122 A 5320 FITTING BOEING 747 7472J9F 1384806 NM FS 400 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 630US 21668 DURING PERIODIC CHECK, FOUND A CRACK IN THE SEAT TRACK SUPPORT FITTING AT BS 400, RBL 11. REPLACED FITTING (P/N 65B1483 1-2). 2 L 7 4 4F RT A20WE 1996020200018 19960202 00018 WP 1996 2 2 9601879871 1 19960123 A 5313 LONGERON DOUG DC9 DC951 3022051 WP FS 1167 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 780NC 48102 DURING H-CHECK, FOUND CORROSION ON THE LONGERON 21R END FITTING AT FS 1167. REPLACED FITTING PER SRM 51-30-2. 2 L 7 2 4F A6WE 1996020200019 19960202 00019 WP 1996 2 2 9601889871 1 19960123 A 5320 FITTING DOUG DC9 DC951 3022051 WP FS 225 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 780NC 48102 DURING H-CHECK, FOUND A CRACK AND CORROSION IN THE LONGERON 25R SPLICE FITTING AT FS 225. REPLACED FITTING PER SRM 51-1 0-3. 2 L 7 2 4F A6WE 1996020200020 19960202 00020 NM 1996 2 2 9601896719 1 19960119 A 5320 SPLICE PLATE BOEING 747 747251F 1384898 NM FS 1920 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 619US 21321 DURING PERIODIC CHECK, FOUND CORROSION ON THE BS 1920 FLOORBEAM SPLICE PLATE FROM LBL 98 TO LBL 105. REPLACED PLATE (P/ N 65B17953-2), PER SRM 51-10-01 PG 18. 2 L 7 4 4F A20WE 1996020200021 19960202 00021 WP 1996 2 2 9601909151 1 19960125 A 7711 EPR INDICATOR DOUG DC9 DC914 3022034 WP PWA JT8 JT8D7B 52053 NE NR 2 ENGINE FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 8909E 45749 666810 NR 2 ENGINE EPR INDICATION WAS LOW ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAI NTENANCE REPLACED THE EPR INDICATOR WITH A SERVICEABLE UNIT. 2 L 7 2 4F 4 F A6WE E2EA 1996020200022 19960202 00022 NM 1996 2 2 9601915503 1 19960125 A 3350 BPS73 POWER SUPPLY BOEING 757 757251 1384970 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 503US 23192 DURING MAINTENANCE, FOUND AFT RIGHT SECTION OF CABIN EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED POWER SUPPLY M736 AND B ATTERY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A2NM 1996020200023 19960202 00023 WP 1996 2 2 9601929930 1 19960124 A 3260 BULB DOUG DC9 DC931 3022065 WP RT MLG FAILED A NWAA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 01 89S 47042 YEG - DURING APPROACH, RIGHT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE ON GEAR EXTENSION. CREW CONFIRMED VISUALL Y THROUGH PERISCOPE THAT GEAR WAS DOWN AND LOCKED. AIRCRAFT LANDED WITHOUT INCIDENT. EMERGENCY EQUIPMENT WAS CALLED OU T ON STANDBY AS A PRECAUTION. CLEANED RIGHT MAIN GEAR DOWNLOCK SWITCH CONNECTOR AND RELAMPED INDICATOR LIGHTS. OPERATI ONAL CHECK NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996020200024 19960202 00024 WP 1996 2 2 9601939975 1 19960124 A 3260 DN/UPLOCK SW DOUG DC9 DC931 3022065 WP RT MLG MALFUNCTIONED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 9339 47382 DURING CLIMBOUT FROM CMH, RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. RECYCLED GEAR AND NORMAL INDICATIONS WERE ACHIEVED. FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED RIGHT MAIN GEA R UPLOCK AND DOWNLOCK SWITCHES. OPERATIONAL CHECK NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996020200025 19960202 00025 WP 1996 2 2 9601949601 1 19960125 A 3350 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 601NW 47038 DURING LINE MAINTENANCE INSPECTION, FOUND CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN POWER SUPP LY AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996020200026 19960202 00026 WP 1996 2 2 9601959986 1 19960124 A 3350 6011779 BATTERY PACK DOUG DC9 DC932 3022066 WP LT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 986US 47480 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AND OPERATION AL CHECK NORMAL. 2 L 7 2 4F A6WE 1996020200027 19960202 00027 WP 1996 2 2 9601969917 1 19960124 A 3350 FUSE DOUG DC9 DC932 3022066 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 967N 47573 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS INOPERATIVE IN FORWARD CABIN AND AT LEFT FORWARD DOOR EMERGEN CY EXIT. REPLACED BLOWN FUSE AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996020200028 19960202 00028 NM 1996 2 2 96FDEA00124 1 19960125 A 3270 1U1169 ACTUATOR BOEING 727 727227 1384078 NM TAIL SKID FAILED A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 485FE 21488 AFTER T/O, THE LANDING GEAR HAD TO BE RECYCLED TO EXTINGUISH THE TAIL SKID LIGHT. DURING THE SECOND ATTEMPT IT TOOK 10 SECONDS FOR THE LIGHT TO GO OUT. REPLACED TAIL SKID ACTUATOR PER MM 32-71-12 AND ADJ PER MM 32-71-01, GROUND CHECKS OK. 2 L 7 3 4F A3WE 1996020200029 19960202 00029 NM 1996 2 2 96FDEA00126 1 19960126 A 3230 SPINDLE/ARM BOEING 727 7272D4 138407U NM LT MLG BROKEN A FDEA A UNSCHED LANDING O OTHER UK UNKNOWN 1 SO 25 288FE 21850 WHEN MANUALLY CRANKING THE L/GEAR A SNAP WAS HEARD AND THE MECHANICAL POINTER STOPPED MOVING. THE SNAP WAS HEARD BEFORE REACHING THE MECHANICAL STOP, GEAR DID EXTEND BUT NO FURTHER POINTER MOVEMENT WAS VISIBLE. FOUND MANUAL EXTENSION INDI CATOR SPINDLE BROKEN AND FOLLOWER ARM BENT. REPLACED SPINDLE AND ARM AS PER MM 32-34-71. PERFORMED ADJ AND TEST LANDIN G GEAR MANUAL EXTENSION SYSTEM AS PER MM 32-34-81. ALL CHECKED GOOD, OK FOR SERVICE AND REQUIRED ITEM INSPECTION COMPLI ED WITH. 2 L 7 3 4F A3WE 1996020200030 19960202 00030 NM 1996 2 2 96FDEA00127 1 19960122 A 5311 FRAME BOEING 727 727233 138408A NM BS 700 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 DENTS IN FRAME BS 700 RBL 34 TO 44 WL 160. REPAIRED DENTED FRAME AT BS 700 RBL 34 TO 44 WL 160 IAW FEDEX SRM 51-40-3. 2 L 7 3 4F RT A3WE 1996020200031 19960202 00031 NM 1996 2 2 96FDEA00128 1 19960126 A 5313 STRINGER BOEING 727 727233 138408A NM BS 720 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 CORROSION (C53-111-01-2), ON STR 28L BS 720 PLUS 4 WL 149. REMOVED, FABRICATED AND REPLACED STR 28L BS 720 PLUS 4 WL 14 9 IAW FEDEX SRM 53-10-2 AND 53-10-3. 2 L 7 3 4F RT A3WE 1996020200032 19960202 00032 NM 1996 2 2 96FDEA00129 1 19960119 A 5330 SKIN BOEING 727 727233 138408A NM BS 480-560 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 AREA OF SKIN DAMAGE STA 480 TO 560 STR 26 LT AND RT LOWER SKIN PANEL INCLUDING 2 DENTS STA 498 AND 503 BETWEEN STR 26 TO 27R, MARKED. BLENDED AREA OF SKIN DAMAGE STA 480 TO 560 STR 26 LT AND RT LOWER SKIN PANEL. FOUND TO BE WITH LIMITS EX CLUDING TWO AREAS. ONE AT STA 500 RBL 14 AND ONE AT STA 490 RBL 22 PER FEDEX SRM 53-30-1. REPAIRED BOTH AREAS PER FEDE X SRM 53-30-3. 2 L 7 3 4F RT A3WE 1996020200033 19960202 00033 NM 1996 2 2 96FDEA00130 1 19960125 A 5530 STRINGER BOEING 727 727233 138408A NM VERT FIN CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 VERTICAL FIN STA 110, STR 8L IS CRACKED, BAY NR 6. REPAIRED CRACKED STRINGER PER SRM 55-30-4. 2 L 7 3 4F RT A3WE 1996020200034 19960202 00034 NM 1996 2 2 96FDEA00131 1 19960118 A 5311 FRAME BOEING 727 727233 138408A NM BS 520 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 DENTS IN FRAME BS 520 LBL 37 TO 46 WL 160. DENTS IN FRAME AT BS 520 LBL 37 TO 46 WL 160 WERE FOUND TO BE OUT OF LIMITS PER FEDEX SRM 51-10-1. REPAIRED FRAME PER FEDEX SRM 51-40-3. 2 L 7 3 4F RT A3WE 1996020200035 19960202 00035 NM 1996 2 2 96FDEA00132 1 19960126 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 1130 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 CORROSION (C53-11-01 AND -3), ON LOWER CHORD OF FLOORBEAM AT NUTPLATE HOLES BS 1130 FROM RBL 50 TO LBL 38 WL 200. REMOV ED CORROSION, FABRICATED REPAIR ANGLE PER EA 7-5310-26949. 2 L 7 3 4F RT A3WE 1996020200036 19960202 00036 NM 1996 2 2 96FDEA00133 1 19960126 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 460 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 CORROSION ON FLOORBEAM BS 460 RBL 10 AND 15 WL 208. REPAIRED FLOORBEAM AT BS 460 RBL 10 TO 15 WL 208. ALL WORK DONE IA W FEDEX EA 7-5310-26943. 2 L 7 3 4F RT A3WE 1996020200037 19960202 00037 NM 1996 2 2 96FDEA00134 1 19960125 A 5330 SKIN BOEING 727 727233 138408A NM BS 710 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 BS 710 LBL 6 WL 149 FOUND DEEP GOUGE AT FASTENER HOLE ON EXTERIOR SKIN WHILE WORKING NR 0413. REMOVED DAMAGE, FABRICATE D REPAIR PARTS AND INSTALLED PER SRM 53-30-3. 2 L 7 3 4F RT A3WE 1996020200038 19960202 00038 NM 1996 2 2 96FDEA00135 1 19960126 A 5313 STRINGER BOEING 727 72722 1384002 NM BS 360-368 DELAMINATION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 DELAMINATION OF SKIN LAP STRINGER 19L BS 360 TO 368. REMOVED FASTENERS IN SKIN LAP AT STR 19L. UPON REMOVAL OF FASTENE RS FOUND NO FURTHER INDICATIONS OF DELAMINATION. INSTALLED NEW STR TIE AND INSTALLED STR 19 SPLICE. ALL WORK DONE IAW FEDEX SRM 53-10-3. 2 L 7 3 4F A3WE 1996020200039 19960202 00039 NM 1996 2 2 96FDEA00136 1 19960126 A 5530 65678961 FITTING BOEING 727 72722 1384002 NM VERT FIN CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 LT VERTICAL FIN FRONT SPAR TERMINAL FITTING FWD O/B FLANGE IS CRACKED. REPAIRED LT VERTICAL FIN FRONT SPAR TERMINAL FIT TING FWD O/B FLANGE IAW FEDEX EA 7-5510-26907. 2 L 7 3 4F A3WE 1996020200040 19960202 00040 NM 1996 2 2 96FDEA00137 1 19960126 A 5320 69239022 FITTING BOEING 727 72722 1384002 NM BS 360 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 CORROSION ON STR TO FRAME TIE AT BS 360 STR 20L. REMOVED AND REPLACED STR TIE AT BS 360 20L, DUE TO CORROSION OUT OF LI MITS. 2 L 7 3 4F A3WE 1996020200041 19960202 00041 NM 1996 2 2 96UAL900060 1 19960124 A 3350 STRIP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE MID LAV INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 556UA 26650 EMERGENCY EVACUATION LIGHTING AT FORWARD MID LAVATORY AREA INOP. REPLACED EMERGENCY EVACUATION LIGHTING STRIP AT MID LA VATORY AREA AND OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996020200042 19960202 00042 NE 1996 2 2 96UAL900061 2 19960124 A 7250 2810194 VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ENGINE LEAKING A UALA D RETURN TO BLOCK K FLUID LOSS IN INSP/MAINT 1 WP 29 512UA 24809 FUEL LEAK ON NR 2 ENGINE COMING FROM CORE ACCESSORY DRAIN DURING ENGINE OPERATION. NO FUEL LEAK AFTER SHUTDOWN. *S/D* REPLACED THE LPT CASE COOLING VALVE AND THE HPT CASE COOLING VALVE, CHECKS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 1996020200043 19960202 00043 NM 1996 2 2 96UAL900062 1 19960124 A 2760 PCA TRANSFORMER GM69375600 BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 4 SPOILER MALFUNCTIONED A UALA K NONE O OTHER UK UNKNOWN 1 WP 29 542UA 25276 SPOILER HANDLE GOES TO FULL EXTEND AS SOON AS HANDLE IS ARMED. SUPPLEMENTAL DATA UPDATE: NR 3 FAULT ON THE SPOILER CON TROL MODULE. REPLACED NR 4 SPOILER PCA TRANSFORMER (RVDT). CLEARED FAULT, OPERATION NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996020200044 19960202 00044 NM 1996 2 2 96UAL900063 1 19960125 A 2131 PRESS CONTROLLER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN MALFUNCTIONED A UALA O OTHER O OTHER CL CLIMB 1 WP 29 7461U 21915 AT 31,000 FT CABIN ALT OBSERVED AT 9,000 FT SWITCHED TO STANDBY AND CABIN CONTINUED TO CLIMB. WENT TO MANUAL AND FLIGHT RETURNED TO DEN. MAINTENANCE REPLACED PRESSURE CONTROLLER. 2 L 7 3 4F 4 F A3WE E2EA 1996020200045 19960202 00045 NM 1996 2 2 96UAL900064 1 19960125 A 2420 IDG CABLE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE RT ENGINE SHORTED A UALA O OTHER B H SMOKE/FUMES/ODORS/SPARKS ELECT. POWER LOSS-50 PC DE DESCENT 1 WP 29 605UA 21866 DESCENDING THROUGH 18,000 FEET, LOST RIGHT MAIN AC BUS, GENERATOR WOULD NOT RESET. BUS REMAINED OFF FOR REMAINDER OF FL IGHT. APU GENERATOR WOULD NOT POWER BUS. PASSENGERS REPORTED SPARKS FROM RIGHT ENGINE WHEN LIGHTS WENT OUT. A SHORTED IDG FEEDER CABLE ON THE RIGHT ENGINE CAUSED THE RIGHT MAIN AC BUS TO SHORT THE CIRCUIT BREAKER. THE FEEDER CABLE WAS R EPAIRED AND REPOSITIONED TO PREVENT FURTHER CHAFING. 2 L 7 2 4F 4 F RT A1NM E3NE 1996020200046 19960202 00046 NM 1996 2 2 96UAL900065 1 19960125 A 3232 S273N1016 ACTUATOR DOWTY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NLG WORN A UALA O OTHER J E WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 WP 29 534UA 25129 EICAS LANDING GEAR DISAGREE INDICATION. LANDING GEAR DOORS AND LANDING GEAR LIGHTS ON SIMULTANEOUSLY. CONDITION OCCURR ED AFTER TAKEOFF WITH GEAR HANDLE UP. VIBRATION ACCOMPANIED OCCURRENCE. APPROXIMATELY 45 SECONDS LATER ABNORMALITIES C LEARED. SUPPLEMENTAL DATA UPDATE: NOSE LANDING GEAR DOOR ACTUATOR RETRACTION CYCLE WAS NOT OPERATING NORMALLY WHICH CA USED THE EICAS MESSAGE. REPLACED NOSE GEAR DOOR ACTUATOR. REMOVED ACTUATOR WAS FOUND TO HAVE WORN SEALS. ACTUATOR WAS OVERHAULED, TESTED AND RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A2NM E17NE 1996020200047 19960202 00047 WP 1996 2 2 MWEA96024 1 19960124 A 2120 AIR DISTR DOUG DC9 DC932 3022066 WP CABIN ODOR A MWEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 31 502ME 48132 F/A REPORTS, AN ELECTRICAL SMELL NEAR THE EMERGENCY EXIT ROWS. NO SMOKE REPORTED AND IT DISAPPEARED AFTER 10 MIN. LOWE RED PSU DOORS AT EMERGENCY EXIT ROWS, NO DEFECTS NOTED AND COULD NOT DUPLICATE. RETURNED A/C TO FLIGHT AND NO FURTHER D ISCREPANCIES ON THIS OR SUBSEQUENT FLIGHTS. 2 L 7 2 4F A6WE 1996020200048 19960202 00048 NM 1996 2 2 P5CA9600088 1 19960123 A 5320 CHORD BOEING 747 747122 1384872 NM BS 1351 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND LEVEL 1 CORROSION AT STATION 1350 PRESSURE DECK TOP CHORD. CORROSION REMOVED, FOUND WITHIN LIMITS IAW SRM 53-10-0 1. 2 L 7 4 4F A20WE 1996020200049 19960202 00049 NM 1996 2 2 UPS205316 1 19960126 A 3260 INDICATION SYST BOEING 727 727247 138408F NM LANDING GEAR MALFUNCTIONED A IPXA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 208UP 21701 CREW REPORTED, ON GEAR RETRACTION RED NOSE GEAR LIGHT REMAINED ILLUMINATED. CYCLED GEAR, NORMAL DOOR INDICATION EXTENSI ON AND RETRACTION. THREE GROUND LIGHTS ON EXTENSION AND NO RED LIGHT ON RETRACTION. RED NOSE LIGHT CAME BACK ON AND FL UCTUATED IN INTENSITY. OCCASIONALLY GROUND NOSE LIGHT CAME ON DIM AND WENT OUT WHILE RED LIGHT STAYED ON. 2 L 7 3 4F A3WE 1996020200050 19960202 00050 WP 1996 2 2 UPS805315 1 19960125 A 3230 TRIGGER DOUG DC8 DC871F 302199D WP NLG NOT LOCKED A IPXA O OTHER E VIBRATION/BUFFET CL CLIMB 1 SO 01 798UP 45895 CLIMBING THROUGH 25K AT 340IAS, NOSE GEAR DOOR POSSIBLY FELL OPEN, CONFIRMED BY LOUD COCKPIT NOISE AND VIBRATION. IMMED IATELY DECLARED AN EMERGENCY AND RAN GEAR DOOR UNLOCKED CHECKLIST IN THE QRH. RECTIFIED THE PROBLEM. NOSE GEAR LINK RE LEASE TRIGGER WAS NOT FULLY LOCKED. 2 L 7 4 4F RT 4A25 1996020200051 19960202 00051 WP 1996 2 2 UPS805317 1 19960126 A 3260 DNLOCK SWITCH DOUG DC8 DC871F 302199D WP NLG FAILED A IPXA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 SO 01 703UP 45939 CREW REPORTED, NOSE LANDING GEAR DID NOT GIVE A GROUND INDICATION. COMPLETED CHECKLIST DID FLYBY AND DECLARED EMERGENCY . LANDED AFTER MAINTENANCE AND TOWER VISUALLY CHECKED GEAR DOWN. 2 L 7 4 4F RT 4A25 1996020200062 19960202 00062 CE 1996 2 2 96ZZZX397 1 19960105 A 3213 161500L STRUT LEAR 24 24 5170302 CE LT MLG GROOVE FAILED A VLLA K NONE O OTHER IN INSP/MAINT 1 GL 05 710TV 8381 4863 78020 24159 LEFT LANDING GEAR STRUT SNAP-RING GROOVE FAILED. SUSPECT CAUSE - EXTREME ROUGHNESS ON RUNWAY. 2 L 7 2 4J A10CE 1996020200087 19960202 00087 NE 1996 2 2 96ZZZX454 2 19960104 A 7314 706800 FUEL PUMP BOEING 767 767231 1385131 NM PWA JT9 JT9D7R4D 52054 NE LT ENGINE MALFUNCTIONED A TWAA O OTHER O OTHER AP APPROACH 1 CE 05 603TW 22566 STL - FLT 721 - DURING APPROACH, LEFT ENGINE WOULD NOT RESPOND TO THROTTLE MOVEMENT. COMPLETED APPROACH AND LANDING. F OUND FUEL PUMP, MFG PN 706800, MALFUNCTION. REPLACED ENGINE FUEL PUMP AND ENGINE FUEL CONTROL, MFG PN 773333-21. ENGIN E OPERATION THEN CHECKED NORMAL. CHECK C-1C - 12-28-95 - LAX. 2 L 7 2 4F 4 F RT A1NM E3NE 1996020200088 19960202 00088 NE 1996 2 2 96ZZZX455 2 19960108 A 7310 3035681 FUEL FILTER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE LT ENGINE DIRTY A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 425JS 3037 FLT 4194 - DURING CRUISE, THE FLIGHT CREW WAS ALERTED BY AN AMBER FUEL FILTER BYPASS CAS MESSAGE. EICAS FUEL SYSTEM PAG E INDICATED THE LEFT ENGINE HP FUEL FILTER IMPENDING BYPASS INDICATION. AIRCRAFT RETURNED TO PIT, LANDED WITHOUT FURTHE R INCIDENT. PIT MAINTENANCE REMOVED AND REPLACED LEFT ENGINE HP FUEL PUMP FILTER IAW MM 73-10-00. GROUND CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 1996020200089 19960202 00089 EU 1996 2 2 96ZZZX456 1 19960106 A 3260 622800200 UPLOCK SWITCH ROTOL BAG JETSTM JETSTM3101 1500215 EU LT/RT MLG DIRTY A VNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 854JS 735 FLT 4178 - AFTER LANDING GEAR WAS RETRACTED, THE LEFT MLG INTRANSIT LIGHT REMAINED ILLUMINATED. CREW CYCLED GEAR SEVERA L TIMES WITH NO SUCCESS. AIRCRAFT RETURNED TO FIELD, AND LANDED WITHOUT FURTHER INCIDENT. OUT STATION MAINTENANCE CLEA NED THE LEFT AND RIGHT UPLOCK MICROSWITCHES IAW STD MAINTENANCE PRACTICES. GROUND CHECKED GOOD, AIRCRAFT RETURNED TO SE RVICE. 2 L 7 2 4T RT A21EU 1996020200090 19960202 00090 NM 1996 2 2 96ZZZX457 1 19960110 A 3250 2304000001 SERVO VALVE MESSIER DORNER DO32 DO328100 2996000 NM NLG STEERING DEFECTIVE A VNAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 424JS 3033 FLT 4194 - WHILE TAXIING ON THE RUNWAY IN PREPARATION FOR TAKEOFF, CREW WAS ALERTED BY A NOSE WHEEL STEERING FAIL CAS ME SSAGE. DAY MAINTENANCE UNABLE TO CORRECT DISCREPANCY IN CMH. AIRCRAFT WAS FERRIED FROM CMH TO CAK. CAK MAINTENANCE RE MOVED AND REPLACED NOSE WHEEL STEERING SERVO VALVE IAW MM 32-51-00. GROUND CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A45NM 1996020200091 19960202 00091 NE 1996 2 2 96ZZZX458 2 19960112 A 7210 PT61916B GEARBOX FOKKER F27 F27MK500 4990629 EU RROYCE DART DART5327R 54509 NE LT ENGINE FAILED A MTNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 33 722FE 1202 10472 13307 RIC - ON CLIMB-OUT, THE LEFT ENGINE INDICATED A POWER LOSS (RPM DROPPED TO 13,800 AT MAX). THE CREW DECLARED AN EMERGEN CY AND RETURNED TO RIC. DURING DESCENT, LEFT GENERATOR LIGHT, LEFT ALTERNATOR LIGHT, AND LEFT GEARBOX OIL PRESSURE LIGH T CAME ON. ALL TEMPERATURES WERE NORMAL. THE AIRCRAFT LANDED WITHOUT ANY OTHER PROBLEMS. AFTER TROUBLESHOOTING, MECHA NIC FOUND INTERNAL FAILURE IN THE LEFT GEARBOX. 2 H 7 2 4T 4 T A817 E297 1996020200092 19960202 00092 CE 1996 2 2 96ZZZX459 1 19960102 A 7120 12991003279 TRUSS BEECH 1900 1900C 1154161 CE RT ENGINE CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 CE 01 130UE 1678 UC130 SPI - DURING VISUAL INSPECTION OF AREA 'A' AS REQUIRED BY AD 95-12-18, A CRACK WAS FOUND. THE RIGHT ENGINE TRUSS WAS R EPLACED WITH SERVICEABLE. 2 L 7 2 4T RT A24CE 1996020200094 19960202 00094 SW 1996 2 2 MALA964791 1 19960101 A 2460 JGZA RELAY SWRNGN SA227 SA227AC 8780603 SW RT CONSOLE SHORTED A MALA O OTHER O OTHER AP APPROACH 1 GL 15 433MA AC714 MSP - FLT 3230 - INBOUND, CREW NOTED ALL OF THE RT ENGINE INSTRUMENTS WERE INOPERATIVE. THE AIRCRAFT CONTINUED TO MSP A ND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE RT BUS TIE RELAY. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 1 L 7 2 4T A8SW 1996020200095 19960202 00095 NE 1996 2 2 MALA964794 2 19960102 A 7320 7863916 HMU DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE NR 2 ENGINE FAILED A MALA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 GL 15 865MA 364 BEH - FLT 3488 - AFTER TAKEOFF, THE NR 2 ENGINE BEGAN TO SURGE IN RPM AND TORQUE. THE CREW REDUCED POWER, BUT THE ENGIN E CONTINUED TO SURGE. THE CREW ELECTED TO PERFORM A PRECAUTIONARY SHUT DOWN AND RETURNED TO BEH WITHOUT INCIDENT. THE PROBLEM COULD NOT BE DUPLICATED IN BEH, SO THE AIRCRAFT WAS FERRIED TO DTW FOR FURTHER TROUBLESHOOTING. MAINTENANCE PER SONNEL REPLACED THE HMU. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 2 H 7 2 4T 4 T RT A13NM E20NE 1996020200096 19960202 00096 SW 1996 2 2 MALA964795 1 19960107 A 5400 2735112 ATTACH ANGLE SWRNGN SA227 SA227AC 8780603 SW RT NACELLE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 63NE AC763B MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE PERSONNEL NOTED A CRACK IN THE RIGHT INBOARD LOWER WING TO NACELLE ATTA CH ANGLE. THEY STOP DRILLED A CRACK AND INSTALLED A REPAIR DOUBLER IAW FAC ARP 54-20-9101. (X) 1 L 7 2 4T A8SW 1996020200097 19960202 00097 SW 1996 2 2 MALA964796 1 19960107 A 5753 2731141001 DOUBLER SWRNGN SA227 SA227AC 8780603 SW LT TE FLAP WORN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 63NE AC763B MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE PERSONNEL NOTED EXCESSIVE WEAR ON THE LEFT FLAP WALKING BEAM ROLLER DOU BLER. THEY REPLACED THE DOUBLER AND INSTALLED A REINFORCEMENT IAW FAC SRM 57-90-10. (X) 1 L 7 2 4T A8SW 1996020200098 19960202 00098 SW 1996 2 2 MALA964797 1 19960107 A 5753 2731141001 DOUBLER SWRNGN SA227 SA227AC 8780603 SW RT TE FLAP WORN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 63NE AC763B MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE PERSONNEL NOTED EXCESSIVE WEAR ON THE RIGHT FLAP WALKING BEAM ROLLER DO UBLER. THEY REPLACED THE DOUBLER AND INSTALLED A REINFORCEMENT IAW FAC SRM 57-90-10. (X) 1 L 7 2 4T A8SW 1996020200099 19960202 00099 SW 1996 2 2 MALA964798 1 19960107 A 2730 2744026007 TORQUE TUBE SWRNGN SA227 SA227AC 8780603 SW RT HORIZ STAB CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 63NE AC763B MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE PERSONNEL NOTED CORROSION IN THE RIGHT ELEVATOR TORQUE TUBE. THEY REPL ACED THE TORQUE TUBE IAW WITH FAC SRM 51-00-00. (X) 1 L 7 2 4T A8SW 1996020200100 19960202 00100 SW 1996 2 2 MALA964799 1 19960107 A 2730 2744026007 TORQUE TUBE SWRNGN SA227 SA227AC 8780603 SW LT HORIZ STAB CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 63NE AC763B MSP - DURING A SCHEUDLED INSPECTION, MAINTENANCE PERSONNEL NOTED CORROSION IN THE LT ELEVATOR TORQUE TUBE. THEY REPLACE D THE TORQUE TUBE IAW FAC SRM 51-00-00. (X) 1 L 7 2 4T A8SW 1996020200101 19960202 00101 SW 1996 2 2 MALA964800 1 19960107 A 5400 2735112 ANGLE SWRNGN SA227 SA227AC 8780603 SW LT NACELLE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 63NE AC763B MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE PERSONNEL NOTED A CRACK IN THE LT LOWER INBOARD WING TO NACELLE ATTACH ANGLE. THEY STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW FAC ARP 54-20-9101. (X) 1 L 7 2 4T A8SW 1996020200102 19960202 00102 SW 1996 2 2 MALA964801 1 19960106 A 3260 1EN516 SWITCH SWRNGN SA227 SA227AC 8780603 SW LT NLG FAILED A MALA O OTHER P NO WARNING INDICATION CL CLIMB 1 GL 15 445MA AC687 BRD - FLT 3236 - AFTER TAKEOFF, THE NLG RED INTRANSIT LIGHT DID NOT ILLUMINATE UPON GEAR RETRACTION. THE AIRCRAFT CONTI NUED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE LT NLG UPLOCK SWITCH. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 1 L 7 2 4T A8SW 1996020200103 19960202 00103 SW 1996 2 2 MALA964802 1 19960105 A 3230 SWITCHES SWRNGN SA227 SA227AC 8780603 SW NLG OUT OF ADJUST A MALA O OTHER O OTHER CL CLIMB 1 GL 15 445MA AC687 GFK - FLT 3253 - AFTER DEPARTURE, THE NOSE GEAR WOULD CYCLE IN THE GEAR WELL AFTER RETRACTION. THE CREW CYCLED THE GEAR SEVERAL TIMES AND THE CYCLING STOPPED. THE AIRCRAFT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONN EL ADJUSTED THE RIGGING OF THE NLG POSITION SWITCHES. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 1 L 7 2 4T A8SW 1996020200104 19960202 00104 NM 1996 2 2 MALA964803 1 19960105 A 3350 LIGHTS DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 832MA 341 MSP - FLT 3231 - DURING PRE-FLIGHT INSPECTION, CREW NOTED THE FLOOR TRACK EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANC E PERSONNEL REPLACED ALL SIX BATTERY PACKS, PN 61-078-1 AND DASH 9. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 2 H 7 2 4T RT A13NM 1996020200105 19960202 00105 NM 1996 2 2 MALA964804 1 19960106 A 3350 6104781 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 822MA 326 DTW - FLT 3120 - DURING A POST-FLIGHT INSPECTION, CREW NOTED THE CABIN EMERGENCY LIGHTS WOULD SHUT OFF AFTER ONLY FIVE S ECONDS OF OPERATION. MAINTENANCE PERSONNEL REPLACED THREE EMERGENCY LIGHT BATTERY PACKS. ALL SYSTEMS OPERATED SATISFAC TORILY. (X) 2 H 7 2 4T RT A13NM 1996020200106 19960202 00106 SW 1996 2 2 MALA964805 1 19960105 A 3260 1EN516 SWITCH SWRNGN SA227 SA227AC 8780603 SW LT NLG FAILED A MALA O OTHER P NO WARNING INDICATION CL CLIMB 1 GL 15 26906 AC654B BRD - FLT 3462 - AFTER TAKEOFF, THE RED NOSE GEAR INTRANSIT LIGHT DID NOT ILLUMINATE DURING GEAR RETRACTION. THE AIRCRA FT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE LT NOSE LANDING GEAR UPLOCK SWITCH. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 1 L 7 2 4T A8SW 1996020200107 19960202 00107 NM 1996 2 2 MALA964806 1 19960105 A 3260 82410315001 SOCKET ASSY DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 827MA 331 DTW - FLT 3432 - DURING A PRE-FLIGHT INSPECTION, CREW NOTED THE NOSE GEAR AND LT MAIN GEAR ALTERNATE DOWN AND LOCKED LIG HTS WERE INOPERATIVE. MAINTENANCE PERSONNEL REPLACED THE MAIN GEAR EMERGENCY DOWNLOCK INDICATOR SOCKET AND REPAIRED A B ROKEN WIRE FOR THE NOSE GEAR LIGHT. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 2 H 7 2 4T RT A13NM 1996020200108 19960202 00108 SW 1996 2 2 MALA964807 1 19960104 A 3233 2751016003 ACTUATOR SWRNGN SA227 SA227AC 8780603 SW RT MLG MALFUNCTION A MALA O OTHER J WARNING INDICATION AP APPROACH 1 GL 15 426MA AC645 BEH - FLT 3485 - DURING APPROACH, THE RT MAIN GEAR DOWN AND LOCKED LIGHT DID NOT ILLUMINATE. THE CREW RECYCLED THE GEAR AND THE LIGHT ILLUMINATED NORMALLY. THE AIRCRAFT CONTINUED TO BEH AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE RT MLG ACTUATOR, PN 27-51016-003. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 1 L 7 2 4T A8SW 1996020200113 19960202 00113 WP 1996 2 2 9601979941 1 19960108 A 5713 LONGERON DOUG DC9 DC932 3022066 WP WS 69-91 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3324L 47103 DURING SPECIAL MAINTENANCE VISIT, FOUND CORROSION ON THE LEFT WING STRINGER 15 BETWEEN XRS 69 TO 91. REPAIRED STRINGER PER EA 99-104039. 2 L 7 2 4F A6WE 1996020200114 19960202 00114 WP 1996 2 2 9601989941 1 19960108 A 5713 LONGERON DOUG DC9 DC932 3022066 WP WS 58-137 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3324L 47103 DURING SPECIAL MAINTENANCE VISIT, FOUND CORROSION ON RIGHT WING STRINGERS 14 AND 15, XRS 58 TO 137 AND ON 20 AND 21, XRS 69 TO 91. REPAIRED STRINGERS PER EA 99-104038. 2 L 7 2 4F A6WE 1996020200115 19960202 00115 WP 1996 2 2 9601999941 1 19960109 A 5330 SKIN DOUG DC9 DC932 3022066 WP FS 200 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3324L 47103 DURING SPECIAL MAINTENANCE VISIT, FOUND A .75 INCH CRACK IN THE FUSELAGE SKIN AT FS 200, LONGERON 13L. REPAIRED SKIN (P /N 5911406-59) PER EA 99-104036. 2 L 7 2 4F A6WE 1996020200116 19960202 00116 WP 1996 2 2 9602009155 1 19960124 A 5320 FITTING DOUG DC9 DC914 3022034 WP FS 200 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8914E 45831 DURING H-CHECK, FOUND CORROSION IN THE FORWARD SERVICE DOOR JAMB FLOOR TO FRAME SUPPORT FITTING, FS 200. REPLACED FITTI NG PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996020200117 19960202 00117 WP 1996 2 2 9602019962 1 19960125 A 5320 FITTING DOUG DC9 DC931 3022065 WP FS 155 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 914RW 47362 DURING SPECIAL MAINTENANCE VISIT, FOUND A CRACK IN THE LONGERON 11R END FITTING AT FS 155. REPLACED FITTING ANGLES PER SRM 53-05 FIG 100. 2 L 7 2 4F A6WE 1996020200118 19960202 00118 1996 2 2 9602029760 4 19960126 A 3416 2050011RC ALTIMETER DOUG DC9 DC941 302207N WP LT COCKPIT FAILED A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 760NW 30723 28147 47288 DURING CLIMB, CAPTAIN'S ALTIMETER OFF FLAG CAME ON. RESET CIRCUIT BREAKER AND ALTIMETER CAME ON MOMENTARILY, THEN OFF F LAG RETURNED. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED CAPTAIN'S ALTIMETER AND OPERATIO NAL CHECK GOOD. 2 L 7 2 4F A6WE 1996020200119 19960202 00119 WP 1996 2 2 9602039153 1 19960121 A 5350 CLIPS DOUG DC9 DC914 3022034 WP TAILCONE OUT OF ADJUST A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8912E 45829 DURING EO 5350-01032 TAILCONE FUNCTIONAL CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR RELEASE HAN DLE FROM THE CLIPS AND DROP THE TAILCONE. ALSO, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO PULL THE EXTERIOR RELEASE H ANDLE FROM THE CLIPS. ADJUSTED THE INTERIOR AND EXTERIOR CLIPS. 2 L 7 2 4F A6WE 1996020200120 19960202 00120 WP 1996 2 2 9602049877 1 19960123 A 5350 RELEASE MECH DOUG DC9 DC951 3022051 WP TAIL CONE MALFUNCTIONED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 786NC 48148 DURING EO 5350-01032 TAIL CONE FUNCTION CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR RELEASE HAND LE FROM THE CLIPS. ALSO, FOUND THAT THE TAIL CONE DID NOT DROP FROM THE AIRCRAFT, BUT HUNG UP ON THE UPPER LOCKPINS. R ERIGGED THE TAIL CONE PER MM 53-50-3, PAR 4 AND CITEXT 09-5350-1-0024, CHECKED OK. 2 L 7 2 4F A6WE 1996020200121 19960202 00121 WP 1996 2 2 9602059880 1 19960125 A 7711 PT2 PROBE DOUG DC9 DC951 3022051 WP LT/RT ENGINES ICED UP A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 675MC 47651 EPR INDICATION LOW ON BOTH ENGINES DURING TAKEOFF. THE TAKEOFF WAS ABORTED AND THE FLIGHT RETURNED TO THE GATE. MAINTE NANCE CLEARED ICE DEPOSITS FROM BOTH PT2 PROBES. ENGINE INDICATION RETURNED TO NORMAL ON SUBSEQUENT RUNUP. 2 L 7 2 4F A6WE 1996020200122 19960202 00122 NM 1996 2 2 96FDEA00138 1 19960119 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 1072-1090 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 492FE 21530 UPPER LOBE BS 1072 TO 1090 STR 7R DAMAGE TO STRINGER INSIDE U-CHANNEL ABOVE SKIN RIVETS. INSTALLED REPAIR DOUBLER IAW B OEING SRM 53-10-3. 2 L 7 3 4F A3WE 1996020200123 19960202 00123 NM 1996 2 2 96FDEA00139 1 19960119 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 757-759 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 492FE 21530 BS 757 TO 759 STR 7L DAMAGE INSIDE STRINGER ABOVE RIVETS THROUGH SKIN. REPLACED STR PER SRM 53-10-3. 2 L 7 3 4F A3WE 1996020200124 19960202 00124 NM 1996 2 2 96FDEA00140 1 19960118 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 882-889 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 492FE 21530 UPPER LOBE BS 882 TO 889 STR 7R DAMAGED TO STR INSIDE U-CHANNEL ABOVE SKIN RIVETS. REMOVE DAMAGED STR 7R FROM BS 872 TO 898, FABRICATED PARTS 1, 2, 3 AND 4. DRILLED AND INSTALLED PER SRM 53-10-3 FIG 3. 2 L 7 3 4F A3WE 1996020200125 19960202 00125 NM 1996 2 2 96FDEA00141 1 19960118 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 885-888 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 492FE 21530 UPPER LOBE BS 885 TO 888 STR 7L, DAMAGE TO STRINGER INSIDE U-CHANNEL. REMOVED FASTENERS, CUT OUT DAMAGED AREA, FABRICA TED FILLER, REPAIRED PARTS 1, 2, 3. LOCATED AND DRILLED ALL HOLES, TREATED AND PRIMED ALL PARTS AND INSTALLED PER SRM 5 3-10-3 PAGES 5 TO 8 FIG 3. 2 L 7 3 4F A3WE 1996020200127 19960202 00127 NM 1996 2 2 96UAL900067 1 19960126 A 2460 26930017 CIRCUIT BREAKER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563B2 13802 EU E/E COMPT DEFECTIVE A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 338UA 24242 LOST CAPTAIN'S AND FIRST OFFICER'S INSTRUMENTS. RESTORED POWER TO FIRST OFFICER'S INSTRUMENTS BUT NEVER REGAINED CAPTAI N'S INSTRUMENTS. THE NUMBER ONE ELECTRICAL BUS CIRCUIT BREAKER AND THE NUMBER TWO GENERATOR BREAKER AUXILIARY CONTACTS WERE FOUND DEFECTIVE. BOTH PARTS WERE REPLACED AND WIRING CHECKS ACCOMPLISHED AS A PRECAUTIONARY. TWO VERIFICATION FLI GHTS WERE ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E21EU 1996020200129 19960202 00129 WP 1996 2 2 ABXA9600072 1 19960104 A 3231 522103 BUSHING DOUG DC9 DC933F 302207A WP RT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND RIGHT MAIN LANDING GEAR DOOR ARTICULATING DOOR LINKAGE WORN. REPLAC ED BUSHINGS IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1996020200130 19960202 00130 WP 1996 2 2 ABXA9600073 1 19960104 A 3231 3923166501 FITTING DOUG DC9 DC933F 302207A WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR ARTICULATING DOOR LINKAGE WORN. REPLACED FITTING IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1996020200131 19960202 00131 WP 1996 2 2 ABXA9600074 1 19960104 A 3231 NB3218600 BUSHING DOUG DC9 DC933F 302207A WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR HINGES WORN. REPLACED BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1996020200132 19960202 00132 WP 1996 2 2 ABXA9600075 1 19960111 A 5610 575468827 DOUBLER DOUG DC9 DC932 3022066 WP LT EYEBROW CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 DURING COMPLIANCE OF AD 90-18-03; SB 56-11 REV 3; EAAD 56-3956MA, FOUND DOUBLER CRACKED AT UPPER AFT CORNER OF LEFT EYEB ROW WINDOW FRAME. REPLACED DOUBLER IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 1996020200153 19960202 00153 WP 1996 2 2 ABXA9600096 1 19960111 A 5280 5913433504 HINGE DOUG DC9 DC941 302207N WP RT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 91-22-07, ASB 32-244, FOUND THE RIGHT MAIN LANDING GEAR OUTBOARD DOOR H INGE WORN. REPLACED HINGE IAW DC-9 SRM 51-10-3. 2 L 7 2 4F A6WE 1996020200155 19960202 00155 WP 1996 2 2 ABXA9600098 1 19960104 A 5330 591141622 SKIN DOUG DC9 DC932 3022066 WP BS 617 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 900AX 47380 DURING C-CHECK INSPECTION, FOUND A 1.4 INCH CRACK IN THE SKIN AT STA 617, AT LONGERON 18R. REPAIRED IAW ABX REA D953-13 873-MR. 2 L 7 2 4F A6WE 1996020200156 19960202 00156 WP 1996 2 2 ABXA9600099 1 19960103 A 5311 9919613502 FRAME DOUG DC9 DC932 3022066 WP BS 617 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 900AX 47380 DURING C-CHECK INSPECTION, FOUND FRAME 617 CRACKED BETWEEN LONGERONS 18R AND 19R. REPAIRED IAW ABX REA D953-13907-MR. 2 L 7 2 4F A6WE 1996020200157 19960202 00157 WP 1996 2 2 ABXA9600100 1 19960105 A 5753 5912168502 VANE DOUG DC9 DC932 3022066 WP RT TE FLAP DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 900AX 47380 DURING C-CHECK INSPECTION, FOUND THE RIGHT WING FORWARD MOVEABLE VANE DELAMINATED. REPLACED VANE IAW DC-9 MM 27-51-02. 2 L 7 2 4F A6WE 1996020200158 19960202 00158 WP 1996 2 2 ABXA9600101 1 19960103 A 5753 5910042504 VANE DOUG DC9 DC932 3022066 WP RT TE FLAP DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 900AX 47380 DURING C-CHECK INSPECTION, FOUND RIGHT FLAP CENTER FIXED VANE DELAMINATED. REPLACED VANE IAW DC-9 MM 27-51-3. 2 L 7 2 4F A6WE 1996020200163 19960202 00163 WP 1996 2 2 ABXA9600106 1 19960125 A 3260 7000010101 SWITCH DOUG DC8 DC863 302198A WP LT MLG DEFECTIVE A ABXA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 23 820AX 46155 ON GEAR EXTENSION LEFT MAIN GEAR DOWNLOCK LIGHT DID NOT ILLUMINATE. RECYCLED LANDING GEAR AND DOWNLOCK LIGHT DID NOT IL LUMINATE. DOWNLOCK LIGHT CAME ON DURING LANDING. CLEANED LEFT MAIN GEAR DOWNLOCK SWITCH CANNON PLUG AND REPLACED DOWNL OCK SWITCH. GEAR RETRACTION AND GEAR INDICATION CHECK WAS GOOD IAW DC-8 MM. 2 L 7 4 4F 4A25 1996020200164 19960202 00164 WP 1996 2 2 ABXA9600107 1 19960125 A 3231 DOOR DOUG DC8 DC863 302198A WP RT MLG OUT OF ADJUST A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 818AX 46075 ON GEAR RETRACTION, RED GEAR UNSAFE LIGHT REMAINED ILLUMINATED. ALSO, RIGHT GEAR DOOR UNLATCH LIGHT ILLUMINATED. RECYC LED GEAR AND HAD NO CHANGE. ADJUSTED DOOR LATCH ASSEMBLY TO OBTAIN PROPER CLEARANCE AND OPS CHECKED GOOD IAW DC-8 MM CH APTER 32-31-4. 2 L 7 4 4F 4A25 1996020200165 19960202 00165 WP 1996 2 2 ABXA9600108 1 19960126 A 3350 60030431 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 905AX 47147 EMERGENCY BATTERY PACK INTERMITTENT OPERATION. REPLACED EMERGENCY BATTERY PACK. 2 L 7 2 4F A6WE 1996020200167 19960202 00167 WP 1996 2 2 ARWA9601003 1 19960127 A 5330 SKIN DOUG DC8 DC862 3021970 WP BS 288-297 CRACKED A ARWA K NONE O OTHER UK UNKNOWN 1 SO 19 802BN 45909 DURING POST FLIGHT INSPECTION, AN 8.5 FUSELAGE SKIN PUNCTURE WAS NOTED AT FS 288.00 TO 297.00 AT LONGERON 32R. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER I/A/W SRM 53-2-1 FIG 7. SEALED AREA I/A/W SRM 51-1-11. 2 L 7 4 4F 4A25 1996020200168 19960202 00168 SO 1996 2 2 COMA9610039 1 19960125 A 6120 711JOMRL731P8 SEAL EMB 120 EMB120RT SO RT ENGINE DEFECTIVE A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 162CA 120150 RIGHT ENGINE NP FLUCTUATES. REPLACED PROPELLER TRANSFER TUBE SEALS. 2 L 7 2 4T RT A31SO 1996020200169 19960202 00169 SO 1996 2 2 COMA9610040 1 19960125 A 2913 MPEV30082B PUMP HYD EMB 120 EMB120RT SO RIGHT FAILED A COMA K NONE O OTHER CR CRUISE 1 SO 01 255CA 16470 231 120238 RT ELECTRIC HYDRAULIC PUMP IS INOP. REPLACED THE RT ELECTRIC MOTOR DRIVEN HYDRAULIC PUMP. 2 L 7 2 4T RT A31SO 1996020200170 19960202 00170 SO 1996 2 2 COMA9610041 1 19960125 A 2752 3203001011 ACTUATOR EMB 120 EMB120RT SO RT TE FLAP DEFECTIVE A COMA O OTHER J WARNING INDICATION LD LANDING 1 SO 01 164D 256 120164 FLAP ASYMMETRY WARNING AFTER LANDING. REPLACED THE RT OUTBD FLAP ACTUATOR. 2 L 7 2 4T RT A31SO 1996020200171 19960202 00171 SO 1996 2 2 COMA9610042 1 19960127 A 3260 922AA2YA6P2722 SENSOR EMB 120 EMB120RT SO LT MLG DEFECTIVE A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 196CA 120196 AFTER LANDING GEAR RETRACTED, A RUMBLING SOUND WAS HEARD AS IF GEAR DOORS WERE OPEN. FOUND LT MLG UPLOCK PROXIMITY SENS OR, SYSTEM-A DEFECTIVE. DEFERRED SYSTEM PER EMB SNL 32-015 AND ACFT RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 1996020200172 19960202 00172 SO 1996 2 2 COMA9610043 1 19960128 A 3060 78614423 LEAD WIRE EMB 120 EMB120RT SO LT PROP BROKEN A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 259CA 120252 LEFT PROPELLER DE-ICE IS INOP. REPLACED BROKEN DE-ICE LEAD WIRE AND ACFT RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 1996020200173 19960202 00173 EU 1996 2 2 COMA9630025 1 19960125 A 3620 M2001542 SWITCH 211C119136A SAAB SF340 SF340A 7850100 EU RT BLEED AIR FAILED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 357CA 11888 4889 M236 340A044 RT BLEED AIR FAULT CAUTION LIGHT ILLUMINATED DURING CLIMB. REPLACED THE BLEED AIR PRESSURE SWITCH AND THE BLEED AIR OVE RTEMP SWITCH FOR TROUBLESHOOTING. PROBLEM DID NOT DUPLICATE IN MAINTENANCE. 2 L 7 2 4T RT A52EU 1996020200174 19960202 00174 WP 1996 2 2 MWEA96025 1 19960126 A 3350 1001191 PIN DOUG DC9 DC932 3022066 WP FWD GALLEY LOOSE A MWEA K NONE L NO TEST NR NOT REPORTED 1 GL 31 502ME 48132 CREW REPORTS, EMERGENCY FLASHLIGHT RETAINING PIN WILL NOT STAY IN SOCKET. REPLACED FLASHLIGHT ASSEMBLY AND RETURNED A/C TO SERVICE. 2 L 7 2 4F A6WE 1996020200175 19960202 00175 WP 1996 2 2 MWEA96026 1 19960126 A 5730 SKIN DOUG DC9 DC914 3022034 WP WS 80 LE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 LT WING LEADING EDGE DENTED STA XRS 80. INSTALLED DOUBLER REPAIR IAW SRM 57-06 FIG 2 AND RETURNED A/C TO SERVICE. 2 L 7 2 4F A6WE 1996020200176 19960202 00176 WP 1996 2 2 MWEA96027 1 19960127 A 3350 SOCKET DOUG DC9 DC914 3022034 WP CABIN DIRTY A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 700ME 45696 DURING C-CHECK, SEVERAL OVERHEAD CENTER AISLE EMERGENCY LIGHTS DID NOT ILLUMINATE DURING TEST. CLEANED AND TIGHTENED SO CKET. OPS CHECK GOOD AND RETURNED A/C TO SERVICE. 2 L 7 2 4F A6WE 1996020200177 19960202 00177 NM 1996 2 2 P5CA9600089 1 19960125 A 7711 613116 PT7 LINE BOEING 747 747122 1384872 NM NR 4 ENGINE BROKEN A P5CA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 23 851FT 19756 ON TAKEOFF, LOST NR 1 AND NR 4 EPR INDICATION AND NR 3 AND NR 4 GENERATOR. TAKEOFF WAS ABORTED. REPLACED NR 3 GCU, GRO UND CHECK OK. FOUND NR 4 GCR RACK PLUG LOOSE, SECURED AND GROUND RUN CHECK OK. FOUND NR 4 ENGINE PT7 LOOP LINE BROKEN AT ONE O'CLOCK POSITION. REPLACED LINE, GROUND RUN OK IAW MM 77-11-15. DEFERRED REPAIR OF NR 1 EPR. 2 L 7 4 4F A20WE 1996020200178 19960202 00178 NM 1996 2 2 P5CA9600090 1 19960127 A 2710 INDICATOR BOEING 747 747121 1384871 NM RT AILERON INOPERATIVE A P5CA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 WP 23 830FT 19642 RETURNED TO RAMP DUE TO IMPROPER RT OUTBOARD AILERON INDICATION. FUNCTIONAL CHECK OF ALL CONTROL SURFACES NORMAL, ALL C OCKPIT INDICATIONS NORMAL IAW MM 27-00-00. 2 L 7 4 4F A20WE 1996020200179 19960202 00179 NM 1996 2 2 P5CA9600091 1 19960127 A 3244 TIRE BOEING 747 747122 1384872 NM NR 10 BLOWN A P5CA A UNSCHED LANDING O OTHER TO TAKEOFF 1 WP 23 854FT 19754 BLEW NR 10 TIRE ON TAKEOFF FROM HONG KONG. RETURNED TO HONG KONG, MADE UNEVENTFUL LANDING. REMOVED AND REPLACED TIRE I AW MM 32-45-01. 2 L 7 4 4F A20WE 1996020200180 19960202 00180 NM 1996 2 2 UPS205319 1 19960124 A 5753 652466858 WEDGE BOEING 727 72721C 138400M NM RT TE MIDFLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, REMOVED AND REPLACED RT I/B MIDFLAP T/E WEDGE. REPLACED AS REQUIRED PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996020200181 19960202 00181 NM 1996 2 2 UPS205320 1 19960119 A 5753 652163327 MID SPAR BOEING 727 72721C 138400M NM LT TE MIDFLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON LT O/B MIDFLAP MID SPAR AFT SIDE 54 AND 58 O/B OF THE I/B END OF MID SPAR. REPLACED ON NRC 368443. 2 L 7 3 4F A3WE 1996020200182 19960202 00182 NM 1996 2 2 UPS205321 1 19960119 A 5753 652163327 MID SPAR BOEING 727 72721C 138400M NM LT TE MIDFLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON LT O/B MIDFLAP MID SPAR UPPER INTERIOR SURFACE AFT SIDE 49 AND 5 5 I/B OF THE O/B END OF MID SPAR. REPLACED ON NRC 368443. 2 L 7 3 4F A3WE 1996020200183 19960202 00183 NM 1996 2 2 UPS205322 1 19960119 A 2750 652163327 FITTING BOEING 727 72721C 138400M NM LT TE MIDFLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON LT O/B MIDFLAP I/B ACTUATING MECHANISM AFT SMALL PULLY SUPPORT F ITTING. REPLACED ENTIRE MIDFLAP ON NRC 368443. 2 L 7 3 4F A3WE 1996020200184 19960202 00184 NM 1996 2 2 UPS205323 1 19960119 A 2750 652163327 FITTING BOEING 727 72721C 138400M NM LT TE MIDFLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON LT O/B MIDFLAP I/B ACTUATING MECHANISM AFT SMALL PULLY SUPPORT F ITTING. REPLACED ENTIRE MIDFLAP ON NRC 368443. 2 L 7 3 4F A3WE 1996020200185 19960202 00185 NM 1996 2 2 UPS205324 1 19960119 A 2711 6521773501 FITTING BOEING 727 72721C 138400M NM LT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT I/B AILERON TAB HINGE FITTINGS CORRODED, 3 EA. REMOVED AND REPLACED LT AI LERON TAB FITTINGS IAW SRM 51-30-2 AND MM 27-10-0. 2 L 7 3 4F A3WE 1996020200186 19960202 00186 NM 1996 2 2 UPS205325 1 19960119 A 2710 6524646501 HINGE ARM BOEING 727 72721C 138400M NM LT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT I/B AILERON CENTER HINGE ARM IS CORRODED AROUND BOLT HOLE. REMOVED AND RE PLACED HINGE ARM IAW MM 27-10-01 AND 27-10-0. 2 L 7 3 4F A3WE 1996020200187 19960202 00187 NM 1996 2 2 UPS205326 1 19960123 A 2711 6521773501 HINGE TAB BOEING 727 72721C 138400M NM RT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING I/B AILERON TAB HINGES ARE CORRODED. REMOVED AND REPLACED RT WING I/ B AILERON TAB HINGES IAW SRM 51-30-02 AND MM 51-10-0. 2 L 7 3 4F A3WE 1996020200188 19960202 00188 NM 1996 2 2 UPS205327 1 19960123 A 2710 65849505 ROD END BOEING 727 72721C 138400M NM RT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING O/B ROD END CLEVIS IS PITTED. REMOVED AND REPLACED RT WING O/B AILER ON ROD END CLEVISES IAW MM 57-50-11 AND 27-10-00. 2 L 7 3 4F A3WE 1996020200189 19960202 00189 NM 1996 2 2 UPS205328 1 19960122 A 2710 6593155264 HINGE FITTING BOEING 727 72721C 138400M NM RT INBD AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING O/B AILERON CENTER HINGE FITTING PITTED AILERON SIDE. REMOVED AND RE PLACED CENTER HINGE FITTING IAW 51-30-2 AND MM 27-10-31. ALSO, FOUND CRACKED RIB SUPPORT BRACKET. REMOVED AND REPLACED BRACKET IAW SRM 51-20-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996020200190 19960202 00190 NM 1996 2 2 UPS205329 1 19960123 A 5754 ANGLE BOEING 727 72721C 138400M NM NR 7 SLAT TRACK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, NR 7 SLAT I/B TRACK I/B RIB SUPPORT ANGLE CRACKED. REPAIRED IAW 57-50-03, 51 -30-2, OHM 57-51-41, MM 27-81-11 AND SRM 51-20-1. 2 L 7 3 4F A3WE 1996020200191 19960202 00191 NM 1996 2 2 UPS205330 1 19960123 A 5754 BONDING JUMPER BOEING 727 72721C 138400M NM NR 6 K-FLAP CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, NR 6 FLAP O/B LOWER BONDING JUMPER HAS CORROSION AROUND ATTACH BOLT UPPER END LOWER SURFACE. REMOVED AND REPLACED NR 6 K-FLAP IAW MM 27-81-01 AND 27-81-00. 2 L 7 3 4F A3WE 1996020200192 19960202 00192 NM 1996 2 2 UPS205331 1 19960123 A 5754 SLAT BOEING 727 72721C 138400M NM NR 5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, NR 5 SLAT AFT LOWER CHORD O/B END CRACKED. REMOVED AND REPLACED NR 5 SLAT IA W MM 27-81-11. 2 L 7 3 4F A3WE 1996020200193 19960202 00193 NM 1996 2 2 UPS205332 1 19960123 A 5511 650174313 RIB BOEING 727 72721C 138400M NM HORZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT NR 2 ELEVATOR HINGE SUPPORT RIB IS CRACKED ON I/B UPPER FLANGE NEAR AFT EN D. REMOVED RT NR 2 ELEVATOR HINGE SUPPORT RIB IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996020200194 19960202 00194 NM 1996 2 2 UPS205333 1 19960125 A 5530 MID SPAR BOEING 727 72721C 138400M NM VERT FIN CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT VENT FIN MID SPAR CHORD IS CHAFED AT ACCESS PNL 9601. REPAIRED AS REQUIRE D PER UPS EO 727-55-0309. 2 L 7 3 4F A3WE 1996020200195 19960202 00195 NM 1996 2 2 UPS405318 1 19960125 A 5315 FLOORBEAM BOEING 747 747123 1384873 NM BS 1060 CORRODED A IPXA O OTHER O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 WHILE IN FOR C-CHECK AMS MAINTENANCE REPORTED, FLOORBEAM UPPER CHORD CORRODED AT BS 1580 LBL 0. REMOVED AND REPLACED FL OORBEAM IAW SRM 51-40-04. 2 L 7 4 4F A20WE 1996020200196 19960202 00196 NM 1996 2 2 UPS405334 1 19960112 A 5314 KEEL BEAM BOEING 747 747123 1384873 NM BS 1242 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 WHILE IN FOR C CHECK AT AMS, MAINTENANCE, FOUND CORROSION ON CENTERLINE KEELBEAM WEB INSIDE BSTA 1242. REPAIRED AS REQU IRED PER SRM 51-10-01, AND KLM DTZ 96-011. 2 L 7 4 4F A20WE 1996020200197 19960202 00197 NM 1996 2 2 UPS405342 1 19960126 A 2560 69B515751 RELEASE HANDLE BOEING 747 747121 1384871 NM ESCAPE SLIDE BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 MAINTENANCE REPORTED, ESCAPE SLIDE RELEASE HANDLE CLIP BROKEN AND PAWL BROKEN MAKING ESCAPE SLIDE ARMED AND NOT SAFE. R EMOVED AND REPLACED RELEASE HANDLE CLIP AND PAWL. SLIDE SECURED AND OPERATES FROM SAFE TO ARM NORMALLY. 2 L 7 4 4F A20WE 1996020200198 19960202 00198 WP 1996 2 2 UPS805335 1 19960104 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FS 760 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CRACK AT FLOORBEAM TO WING L-ATTACH ANGLE LBL 40 FS 760. REPLACED ANGLE PER SRM 51-2-20D. 2 L 7 4 4F RT 4A25 1996020200199 19960202 00199 WP 1996 2 2 UPS805336 1 19960103 A 5510 5654500 ANGLE DOUG DC8 DC873F 302199F WP HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT HORIZ STAB LEADING EDGE I/B SUPPORT ANGLE CRACKED. REPLACED ANGLE PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996020200202 19960202 00202 WP 1996 2 2 UPS805339 1 19960109 A 5713 STRINGER DOUG DC8 DC871F 302199D WP WS 485 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT WING, STRINGER 54 LOWER CRACKED AT STA XW 485. REPAIRED IAW UPS EO DC8-57 10-7184. 2 L 7 4 4F RT 4A25 1996020200203 19960202 00203 WP 1996 2 2 UPS805340 1 19960109 A 5711 SPAR DOUG DC8 DC871F 302199D WP NR 1 MAIN TANK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT WING, NR 1 MAIN TANK O/B SECTION CRACKED LOWER CENTER SPAR AND WEB THROUGH ACCESS PNL 506A. REPAIRED IAW UPS EO DC8-5710-7895A. 2 L 7 4 4F RT 4A25 1996020200204 19960202 00204 WP 1996 2 2 UPS805341 1 19960109 A 5311 FRAME DOUG DC8 DC871F 302199D WP FS 781 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT FRAME STA 781 BETWEEN LONG 18 AND 19 CRACKED. REPAIRED IAW UPS EO DC8-53- 1553 AND TIMCO REO 01764. 2 L 7 4 4F RT 4A25 1996020200205 19960202 00205 WP 1996 2 2 UPS805343 1 19960128 A 5754 5751184505 FITTING DOUG DC8 DC871F 302199D WP LT TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 MAINTENANCE REPORTED, FLAP FITTING CRACKED ON O/B FLAP I/B FITTING. REMOVED AND REPLACED FITTING. 2 L 7 4 4F RT 4A25 1996020200206 19960202 00206 WP 1996 2 2 UPS805344 1 19960104 A 5320 SUBFLOOR WEB DOUG DC8 DC873F 302199F WP FS 45 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION BULGE ON SUBFLOOR WEB FWD ENTRY DOOR FS 45. REPAIRED PER SRM 53-2- 0 AND SRM 51-1-2. 2 L 7 4 4F RT 4A25 1996020200207 19960202 00207 WP 1996 2 2 UPS805345 1 19960108 A 5315 3774605C01 FLOORBEAM DOUG DC8 DC873F 302199F WP FS 55 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON FLOORBEAM FS 55 LBL 37. REPLACED PER UPS EO DC8-53-1547. 2 L 7 4 4F RT 4A25 1996020200210 19960202 00210 WP 1996 2 2 9602069301 1 19960124 A 2910 HYD LINE DOUG DC9 DC982 3022082 WP ELEC HYD PUMP FAILED A NWAA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 01 301RC 48054 ON APPROACH INTO BIL, THE RIGHT HYDRAULIC PRESSURE AND QUANTITY WENT TO ZERO. ACTUATED EMERGENCY GEAR EXTENSION HANDLE, NO HELP. LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED. INITIATED LEFT HIGH G-TURN, SECURED DOWN AND LOCKED INDICATION. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE SERVICED HYDRAULIC SYSTEM AND FOUND BAD HYDRAULIC LINE AT ELECT RIC PUMP. REPLACED LEFT MAIN LANDING GEAR EMERGENCY EXTENSION CABLE AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996020200211 19960202 00211 NM 1996 2 2 9602076719 1 19960127 A 3240 SHUTTLE VALVE BOEING 747 747251F 1384898 NM NR 15 BRAKE FAILED A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 619US 21321 DURING CLIMB AFTER LANDING GEAR RETRACTION, THE NR 4 HYDRAULIC QUANTITY WENT FROM 8 GALLONS TO 2 GALLONS AND THE LOW QUA NTITY LIGHT ILLUMINATED. THE NR 2 HYDRAULIC QUANTITY WENT FROM 5 GALLONS TO 8 GALLONS. AIRCRAFT DIVERTED TO SEA AND LA NDED WITHOUT INCIDENT. REPLACED THE NR 15 BRAKE SHUTTLE VALVE AND OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996020200212 19960202 00212 NM 1996 2 2 9602086627 1 19960126 A 3830 DRAIN BOEING 747 747251B 1384892 NM FS 800 CLOGGED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 627US 21709 DURING CLIMB, WATER OVERFLOWED FROM THE FIRST CLASS LAVATORY AND NR 2 GALLEY. AIRCRAFT RETURNED TO NRT AND LANDED WITHO UT INCIDENT. CLEANED AND PURGED CLOGGED DRAIN AT STATION 800 AND OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996020200213 19960202 00213 EU 1996 2 2 9602093245 1 19960127 A 3230 664700500A4B CONTROL UNIT AIRBUS 320 A320211 3930320 EU LANDING GEAR MALFUNCTIONED A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 345NW 13299 9444 399 DURING CLIMBOUT, THE LANDING GEAR DID NOT RETRACT. CYCLED THE LANDING GEAR HANDLE AND GEAR RETRACTED NORMALLY. FLIGHT CONTINUED TO ORIGINAL DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR CONTROL INTERFACE UNIT AND SYSTEM TESTED OK. 2 L 7 2 4F RT A28NM 1996020200214 19960202 00214 WP 1996 2 2 9602109953 1 19960128 A 2822 O-RING DOUG DC9 DC931 3022065 WP RT BOOST PUMP SPLIT A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 918RW 47158 DURING CLIMB AFTER CENTER TANK WAS EMPTY, THE RIGHT FUEL PRESSURE LOW LIGHT ILLUMINATED. RIGHT FUEL INDICATION DID NOT DECREASE AND THE LEFT FUEL INDICATION WAS DECREASING AT THE RATE OF EQUAL TO BOTH ENGINE BURNS. ACCOMPLISHED COCKPIT OP ERATING MANUAL PROCEDURES AND FUEL LOW PRESSURE LIGHT EXTINGUISHED WITH CROSSFEED ON. FLIGHT RETURNED TO PHX AND LANDED WITHOUT INCIDENT. RIGHT FUEL INDICATION DID DECREASE ON DESCENT. REPLACED O-RING AT RIGHT AFT FUEL BOOST PUMP PRESSUR E LINE. ALSO, REPLACED THE LEFT ENGINE LOW PRESSURE FUEL FILTERS. OPERATIONAL CHECK NORMAL AND AIRCRAFT RETURNED TO SE RVICE. 2 L 7 2 4F A6WE 1996020200215 19960202 00215 WP 1996 2 2 9602119989 1 19960127 A 2923 405016 AUX HYD PUMP DOUG DC9 DC931 3022065 WP LANDING GEAR MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 8945E 47181 LANDING GEAR WAS VERY SLOW TO RETRACT AFTER TAKEOFF. NOSE GEAR RED UNSAFE LIGHT EXTINGUISHED AT 3,500 FEET AND BOTH MAI NS AT 4,500 FEET. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE LANDING GEAR ALTERNATE HYDRAULIC PU MP DUE TO INTERNAL BYPASSING. OPERATIONAL CHECK NORMAL ON GEAR SWING AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996020200216 19960202 00216 NE 1996 2 2 9602129984 2 19960125 A 7220 NOSE BULLET DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE NR 1 ENGINE ICED UP A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 677MC 47756 688231 NR 1 ENGINE EPR INDICATION WAS ABNORMALLY HIGH DURING POWER APPLICATION ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND TH E AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REMOVED ICE DEPOSITS FROM THE ENGINE NOSE BULLET AND PT2 PROBE. ENGINE IN DICATIONS RETURNED TO NORMAL ON SUBSEQUENT RUNUP. 2 L 7 2 4F 4 F A6WE E2EA 1996020200217 19960202 00217 EU 1996 2 2 9602133215 1 19960128 A 3260 INDICATION AIRBUS 320 A320211 3930320 EU LANDING GEAR MALFUNCTIONED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 315US 171 DURING CLIMBOUT AFTER LANDING GEAR RETRACTION, RECEIVED 'L/G GEAR NOT UPLOCKED' AND 'L/G DOORS NOT CLOSED' MESSAGES. CY CLED LANDING GEAR HANDLE AND ALL INDICATIONS NORMAL. AIRCRAFT CONTINUED TO ORIGINAL DESTINATION AND LANDED WITHOUT INCI DENT. CORRECTIVE ACTION WILL BE ACCOMPLISHED DURING 'C' CHECK. 2 L 7 2 4F RT A28NM 1996020200218 19960202 00218 EU 1996 2 2 9602143223 1 19960128 A 3231 RETRACT MECH AIRBUS 320 A320211 3930320 EU NLG DOORS OUT OF RIG A NWAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 01 323US 272 DURING APPROACH, THE LANDING GEAR DID NOT EXTEND. CYCLED THE LANDING GEAR HANDLE AND GEAR EXTENDED NORMALLY. ACCOMPLIS HED A MISSED APPROACH. DURING SECOND APPROACH ATTEMPT, LANDING GEAR FUNCTIONED NORMALLY. AIRCRAFT LANDED WITHOUT INCID ENT. MAINTENANCE RIGGED THE NOSE LANDING GEAR DOORS AND OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996020200219 19960202 00219 WP 1996 2 2 9602151154 1 19960128 A 3234 HANDLE DOUG DC10 DC1040 3023508 WP LANDING GEAR LACK OF LUBE A NWAA O OTHER J WARNING INDICATION LD LANDING 1 GL 01 154US 46763 DURING GEAR EXTENSION, THE GEAR HANDLE BUTTON STUCK IN PLACE IN DOWN POSITION WITH AN UNSAFE GEAR INDICATION. RECYCLED GEAR AND MANUALLY PUSHED HANDLE IN AND GOT NORMAL GEAR INDICATIONS. LUBED GEAR HANDLE RELEASE BUTTON AND GEAR HANDLE PI VOTS. 2 L 7 3 4F A22WE 1996020200220 19960202 00220 WP 1996 2 2 9602169967 1 19960127 A 3260 GEAR LIGHT DOUG DC9 DC931 3022065 WP RT MLG MALFUNCTIONED A NWAA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 01 9331 47263 DURING APPROACH INTO MSP, THE RIGHT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR WAS EXTENDED. RECYCLED GEAR AND NORMAL INDICATIONS WERE ACHIEVED. JACKED AIRCRAFT AND CYCLED GEAR SEVERAL TIMES AND ALL INDICATIONS CHECKED NO RMAL. DISCREPANCY COULD NOT BE DUPLICATED. CLEANED SWITCHES AS A PRECAUTION AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996020200221 19960202 00221 WP 1996 2 2 9602179917 1 19960128 A 3350 FUSE DOUG DC9 DC932 3022066 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 967N 47573 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. REPLACED FUSE AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996020200222 19960202 00222 NM 1996 2 2 9602182275 1 19960126 A 2133 OUTFLOW VALVE BOEING 727 727251 138408H NM CABIN DIRTY A NWAA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 GL 01 275US 21154 AFTER TAKEOFF, COULD NOT PRESSURIZE AIRCRAFT. FUEL WAS DUMPED AND THE AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCID ENT. FOUND OUTFLOW VALVES VERY DIRTY. CLEANED OUTFLOW VALVES AND INSPECTED PLUMBING TO CONTROLLER. PERFORMED PRESSURI ZATION TEST, CHECKED OK. 2 L 7 3 4F A3WE 1996020200223 19960202 00223 NM 1996 2 2 9602192769 1 19960128 A 2612 FIRE LOOP BOEING 727 7272M7 138407S NM NR 2 ENGINE MALFUNCTIONED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 GL 01 729RW 21742 DURING CLIMB, THE NR 2 ENGINE FIRE BELL AND LIGHT ACTIVATED. ENGINE SHUT DOWN, AIRCRAFT RETURNED TO ORD AND LANDED WITH OUT INCIDENT. REPLACED THE NR 2 FIRE DETECTION UNIT AND ENGINE FIRE LOOP. 2 L 7 3 4F A3WE 1996020200224 19960202 00224 WP 1996 2 2 9602209913 1 19960130 A 5350 RELEASE HANDLE DOUG DC9 DC931 3022065 WP TAILCONE OUT OF ADJUST A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 963N 47415 DURING EO 5350-01032 TAILCONE FUNCTIONAL CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE EXTERIOR TAILCONE HA NDLE FROM THE CLIPS DURING THE FIRST TWO ATTEMPTS. THE FORCE REQUIRED DURING THE THIRD ATTEMPT WAS WITHIN LIMITS. NO F URTHER ACTION WAS TAKEN. 2 L 7 2 4F A6WE 1996020200225 19960202 00225 NM 1996 2 2 96UAL900068 1 19960129 A 2780 RETRACT MECH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LE FLAPS MALFUNCTIONED A UALA O OTHER F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 WP 29 516UA 24860 UNABLE TO MOVE FLAPS NORMALLY, LEADING EDGE LIGHT ON AND FLAP ASYMMETRY MESSAGE. FLAPS RECYCLED IN ALT OK, BUT STILL LO CKED OUT IN NORMAL. BITE CHECK ON NR 1 FSEU SHOWS SLAT LOSS. 2 L 7 2 4F 4 F RT A2NM E17NE 1996020200226 19960202 00226 NM 1996 2 2 96UAL900069 1 19960129 A 3350 TRACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 535UA 25130 EMERGENCY EXIT LIGHTS FLOOR TRACK LENS AT ROWS 1 THROUGH 2 ARE DAMAGED. REPLACED EMERGENCY EXIT LIGHTS FLOOR TRACK COVE R. 2 L 7 2 4F 4 F RT A2NM E17NE 1996020200227 19960202 00227 NM 1996 2 2 96UAL900070 1 19960129 A 3350 STRIP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 566UA 26670 EMERGENCY EXIT LIGHT STRIP DAMAGED AND LOOSE. SECURED THE EMERGENCY EXIT LIGHT STRIP TRACK TO FLOOR USING TAPE AND LEAV ING THE EMERGENCY EXIT LIGHT STRIP ELEMENT VISIBLE. NEEDS TO BE CLEANED UNDERNEATH TRACK AND RESECURED. 2 L 7 2 4F 4 F RT A2NM E17NE 1996020200228 19960202 00228 NM 1996 2 2 96UAL900071 1 19960129 A 2780 FSEU BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LE FLAPS MALFUNCTIONED A UALA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 WP 29 527UA 24995 ON APPROACH, EICAS MESSAGE DISPLAYED, LEADING EDGE ASYMMETRY MESSAGE AND LEADING EDGE WARNING LIGHT. FLAPS STUCK AT 25 DEGREES AND NO ADVERSE CONTROL WHEEL FORCES - LANDED WITH FLAPS AT 25 DEGREES. REPLACED NR 1 FSEU AND SWITCHES S10338 AND S10340 PER MM. CYCLED FLAPS SEVERAL TIMES AND OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996020200229 19960202 00229 NM 1996 2 2 96UAL900072 1 19960129 A 3231 27464 ACTUATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NLG DOOR MALFUNCTIONED A UALA O OTHER E J VIBRATION/BUFFET WARNING INDICATION TO TAKEOFF 1 WP 29 534UA 25129 ON TAKEOFF, NOSE GEAR RETRACTION DOORS LIGHT REMAINED ON WITH NOTICEABLE VIBRATION AND WIND NOISE. GEAR DISAGREE LIGHT ON EICAS. NOSE GEAR DOORS WOULD NOT FULLY CLOSE DUE TO A MALFUNCTIONING NOSE GEAR DOOR ACTUATOR. REPLACED NOSE GEAR AC TUATOR, SYSTEM CHECKS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 1996020200230 19960202 00230 NM 1996 2 2 96UAL900073 1 19960129 A 2781 285T004953 FSEU BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LE FLAPS MALFUNCTIONED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 608UA 21869 AFTER TAKEOFF WITH FLAP RETRACTION, LEADING EDGE FLAP ASYMMETRY EICAS MESSAGE APPEARS AND AMBER WARNING PRESENT. FLAPS APPEAR TO BE VISUALLY RETRACTED. AIRCRAFT RETURNED TO MIA. SUPPLEMENTAL DATA UPDATE: THE LEADING EDGE FLAP ASYMMETRY EICAS MESSAGE AND AMBER WARNING WERE FALSE FLAP SLAT ELECTRONIC UNIT (FSEU) INDICATIONS. THE FSEU WAS REPLACED PER MM 2 7-51-01. 2 L 7 2 4F 4 F RT A1NM E3NE 1996020200231 19960202 00231 NM 1996 2 2 96UAL900074 1 19960129 A 2560 3A34991 VALVE FLANGE BFGOODRICH 7A14793 BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ESCAPE SLIDE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 179UA G421 25158 DURING SLIDE OVERHAUL, FOUND RIGHT HAND INFLATE/DEFLATE RUBBER MOUNTING FLANGE CRACKED. PROBABLE CAUSE WAS BENDING OF T HE VALVE DURING SLIDE PACKING. REPLACED RUBBER INFLATE/DEFLATE VALVE FLANGE. 2 L 7 4 4F 4 F RT A20WE E24NE 1996020200233 19960202 00233 WP 1996 2 2 96UAL900076 1 19960129 A 2120 AIR DISTR DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 1831U 46630 NOXIOUS OILY FUMES FROM AIR CONDITIONING SYSTEM ON GROUND AND IN THE AIR. SOME PASSENGERS AND FLIGHT ATTENDANTS WERE NA USEATED. FUMES REALLY STRONG WHEN IN RAINY CONDITIONS. SUPPLEMENTAL DATA UPDATE COULD NOT FIND SOURCE OF ODOR OR DUPLI CATE PROBLEM. REPLACED COALESCER BAGS AS A PRECAUTIONARY ACTION. 2 L 7 3 4F 4 F A22WE E23EA 1996020200234 19960202 00234 WP 1996 2 2 96UAL900077 1 19960129 A 5620 9F122891 SEAL DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN WINDOW SEPARATED A UALA K NONE D INFLIGHT SEPARATION IN INSP/MAINT 1 WP 29 1810U 46609 WINDOW AT 12J, ANACOUSTICAL PANE AND RETAINER FOR PANE MISSING. SUPPLEMENTAL DATA UPDATE REPLACED ANACOUSTICAL PANE AT 12J. ON 1/16/96 1T WAS REPORTED THAT WINDOW 12J SEAL WAS COMING OFF. RESET THE SEAL IN THE WINDOW TRACK. SUBMITTER SU GGEST, THE PROBABLE CAUSE OF THE PANE SEPARATION IS THAT THE SEAL MAY HAVE BEEN INSTALLED INCORRECTLY. 2 L 7 3 4F 4 F A22WE E23EA 1996020200235 19960202 00235 1996 2 2 96UAL900078 4 19960129 A 3417 4061100901 ADC BOEING 737 737322 1384676 NM LEFT INOPERATIVE A UALA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 WP 29 310UA 23671 ON TAKEOFF, CAPTAIN'S AIRSPEED INDICATOR AND BOTH FLIGHT MANAGEMENT COMPUTERS INOP. NUMBER ONE AIR DATA COMPUTER SHOWED BARO REFERENCE NUMBER TWO, OUT OF LIMIT IN FAULT MEMORY. REPLACED NUMBER ONE AIR DATA COMPUTER, CHECKS OK. 2 L 7 2 4F RT A16WE 1996020200236 19960202 00236 NM 1996 2 2 96UAL900079 1 19960129 A 2740 69394131 BRAKE PLATE BOEING 737 737322 1384676 NM HORIZ STAB CHIPPED A UALA A UNSCHED LANDING F FLT CONT AFFECTED TO TAKEOFF 1 WP 29 203UA 24718 CREW REPORTS THAT THE HORIZONTAL STABILIZER TRIM IS JAMMED AND CANNOT BE TRIMMED MANUALLY OR ELECTRONICALLY. JACKSCREW ASSEMBLY WAS JAMMED, ASSEMBLY WAS REMOVED FROM AIRCRAFT AND ROUTED TO THE SHOP. DURING DISASSEMBLY A BRAKE PLATE WAS FO UND CHIPPED. CHIP SHOWED SIGNS OF WEAR AND AN IMPACT MARK. 2 L 7 2 4F RT A16WE 1996020200237 19960202 00237 NM 1996 2 2 96UAL900080 1 19960129 A 3350 CONNECTOR BOEING 737 737322 1384676 NM CABIN LOOSE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 320UA 23952 EMERGENCY ESCAPE PATH LIGHTING INOP FROM ROW 12 TO ROW 18. RESEATED CONNECTOR ON POWER CABLE, CHECKS OK. 2 L 7 2 4F RT A16WE 1996020200238 19960202 00238 SO 1996 2 2 COMA9610044 1 19960126 A 2435 23080013 STARTER GEN EMB 120 EMB120RT SO LT ENGINE FAILED A COMA E D ENGINE SHUTDOWN RETURN TO BLOCK M Y OVER TEMP ENGINE STOPPAGE TX TAXI/GRND HDL 1 SO 01 189CA 5986 118 120189 DURING LEFT ENGINE START, T6 EXCEEDED 900 DEGREE CELSIUS. START WAS ABORTED AND DURING DRY MOTOR, THE STARTER FAILED. R EPLACED THE STARTER/GENERATOR AND START CONTACTOR. 2 L 7 2 4T RT A31SO 1996020200239 19960202 00239 SO 1996 2 2 COMA9610045 1 19960128 A 3150 80055711 AURAL WARN UNIT EMB 120 EMB120RT SO AVIONICS MALFUNCTIONED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 255CA 11394 2242 120238 TAKEOFF AURAL WARNING SOUNDED DURING TAKEOFF ROLL. REPLACED THE AURAL WARNING UNIT. 2 L 7 2 4T RT A31SO 1996020200240 19960202 00240 SO 1996 2 2 COMA9610046 1 19960128 A 2750 3471001001 ANNUNCIATOR EMB 120 EMB120RT SO INST PANEL DEFECTIVE A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 205CA 7650 491 120205 TAKEOFF FLAPS AURAL WARNING SOUNDED DURING TAKEOFF ROLL. REPLACED THE FLAP ANNUNCIATOR UNIT. 2 L 7 2 4T RT A31SO 1996020200241 19960202 00241 EU 1996 2 2 COMA9630026 1 19960129 A 7712 TQ INDICATION SAAB SF340 SF340A 7850100 EU RT ENGINE MALFUNCTIONED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 358CA 340A047 THE RT ENGINE TORQUE INDICATOR WENT FULL DEFLECTION DURING TAKEOFF. COULD NOT DUPLICATE DISCREPANCY DURING MAINTENANCE RUNS AND ACFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 1996020200242 19960202 00242 NM 1996 2 2 DHL96742005 1 19960130 A 2611 302842 SMOKE DETECTOR BOEING 727 727225 1384077 NM NR 3 MALFUNCTIONED A T DHLA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 742DH 21290 CARGO SMOKE LIGHT ILLUMINATED DURING CRUISE FLT. INSPECTED CARGO AREA FOR SMOKE AND INSPECTED NR 1, 2 AND 3 SMOKE DETEC TORS AND AMP. OPS CHECKED 3 TIMES, TEST OK. RAN PROVISION CHECK AND AIR CONDITION CK PER JRH, NO FAULT FOUND. 2 L 7 3 4F A3WE 1996020200244 19960202 00244 NM 1996 2 2 DL72S960173 1 19960123 A 3320 036405 BALLAST BOEING 727 727232 1384082 NM CABIN FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 536DA 22049 CEILING POWER FWD C/B ON P18-3 PNL POPPED FOLLOWED BY AN ACRID ELECTRICAL SMELL IN THE FWD PART OF THE AIRCRAFT. PULLED AND COLLARED FWD CONT C/B AND FWD CEILING PWR C/B. PULLED C/P ON CEILING LIGHT AT RT ROW 24 AND LT 17. FOUND BURNED B ALLAST, REPLACED BALLAST AND OPERATION NORMAL. 2 L 7 3 4F A3WE 1996020200245 19960202 00245 NM 1996 2 2 DL72S960176 1 19960123 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 2 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 405DA 21149 FOUND DURING E-2 LETTER CHECK, NR 2 L/E SLAT COVE SKIN ATTACH ANGLE CRACKED BELOW TAI DUCT. REPAIRED PER M/M 57-54-0 FIG 805. 2 L 7 3 4F A3WE 1996020200246 19960202 00246 NM 1996 2 2 DL72S960177 1 19960123 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 7 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 405DA 21149 FOUND DURING E-2 LETTER CHECK, NR 7 L/E SLAT COVE SKIN ATTACH ANGLE CRACKED .375 INCH BELOW TAI DUCT. REPAIRED PER M /M 57-54-0 FIG 805. 2 L 7 3 4F A3WE 1996020200247 19960202 00247 NM 1996 2 2 DL72S960180 1 19960124 A 2120 BOEING 727 727232 1384082 NM CABIN ODOR A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 420DA 39986 21273 ON TAKEOFF, COCKPIT AND CABIN FILLED WITH SMOKE, DID NOT SMELL LIKE ELECTRICAL. FLIGHT RETURNED TO SEA. MAINT INSPECTE D ENGINES INLETS AND EXHAUST APU AREA AND RAM AIR DOORS, NO DISCREPANCY FOUND. RAN APU WITH A/C PACKS AND ENGS WITH PAC KS. SUSPECT ANTI-ICE FLUID FUMES CAUSED TROUBLE. ALL ELECT SYSTEMS OPERATED NORMAL AND ACFT RETURNED TO SERVICE. 2 L 7 3 4F A3WE 1996020200248 19960202 00248 NM 1996 2 2 DL72S960187 1 19960119 A 5512 SKIN BOEING 727 727232 1384082 NM LT HORIZ STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 517DA 21433 FROM HMV ATL, THE LOWER SKIN ON THE LT HORIZ STAB IS GOUGED AND CRACKED I/B END. ACCOMPLISHED REPAIRS PER SRM 55-10-3 F IG 3. 2 L 7 3 4F A3WE 1996020200249 19960202 00249 NM 1996 2 2 DL72S960198 1 19960125 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 2 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 489DA 21019 FOUND DURING A-1 LETTER CHECK, .5 INCH CRACK NR 2 L/E SLAT COVE SKIN ATTACH ANGLE, ADJACENT TO O/B TRACK. REPAIRED P ER M/M 57-54-0. 2 L 7 3 4F A3WE 1996020200251 19960202 00251 NM 1996 2 2 DL72S960202 1 19960125 A 5320 DECK BOEING 727 727232 1384082 NM BS 940-950 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 495DA 21075 DURING MIDVISIT, TWO 1 INCH CRACKS WERE FOUND IN THE LT MAIN LANDING GEAR WHEEL WELL PRESSURE DECK BETWEEN STATIONS 940 AND 950, BETWEEN LBL 50 AND 60. MODIFICATION INSTALLED IN ACCORDANCE WITH BOEING SERVICE BULLETIN 727-53-0149, REVISION 4. 2 L 7 3 4F A3WE 1996020200252 19960202 00252 NM 1996 2 2 DL72S960204 1 19960126 A 5320 WEB BOEING 727 727232 1384082 NM BS 1303 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 542DA 22391 FOUND ON A-2 LETTER CHECK, .375 INCH CRACK IN TORQUE BOX LIGHTENING HOLE AT STA 1303 RIGHT SIDE 48 SECTION. REPAIRED PE R MM 53-11-0. 2 L 7 3 4F A3WE 1996020200253 19960202 00253 NM 1996 2 2 DL72S960206 1 19960126 A 5330 SKIN BOEING 727 727232 1384082 NM L1 DOOR AREA CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 542DA 22391 FOUND DURING A-2 LETTER CHECK, .75 INCH CRACK IN FUSELAGE SKIN AT L-1 DOOR LWR HINGE CUTOUT. REPAIRED PER ERA 303079-1 4 AND M/M 53-30-0. 2 L 7 3 4F A3WE 1996020200254 19960202 00254 NM 1996 2 2 DL72W960212 1 19960127 A 2160 COOLING VALVE BOEING 727 727247 138408F NM PWA 2037 PW2037 NE EE COMP FAILED A DALA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 2817W 20873 716548 DISPATCHED WITH ONE PACK, MIX VLV INOP. ACFT WOULD NOT HOLD THE CABIN WITH CARGO HEAT OUTFLOW CLOSED AND OUTFLOW VLV FU LL CLOSED. REPLACED EQUIP COOLING VLV IN E/E COMP, PRESS ACFT TO 3 PSI AND OPERATION CKS OK. 2 L 7 3 4F 4 F A3WE E17NE 1996020200255 19960202 00255 NM 1996 2 2 DL73E960188 1 19960123 A 2460 TRANS RELAY BOEING 737 737247 138448D NM EE COMPT FAILED A DALA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 SO 27 238WA 23186 AT CRUISE 33,000 FT, ALT LOST ALL ELECT POWER AND CAPT INSTRUMENTS WERE COMPLETELY OUT FOR APPROX 20 MIN. RECOVERED F/O INSTR AND EVENTUALLY CAPT INSTRUMENTS RETURNED. REPLACED NR 1 TXFR RLY R-3 CPN 243201020. FOUND NR 2 ALT TXFR BUS C/B POPPED AND WOULD NOT RESET. REPLACED SAME. REPLACED NR 1 GEN BRKR CPN 243001013 S/N TF7130. ALSO, REPLACED NR 1 BTB S/N 172A CPN 243001008 AND BUS PROT PANEL S/N 6836 CPN 243001013. OPERATION NOW NORMAL. 2 L 7 2 4F A16WE 1996020200256 19960202 00256 NM 1996 2 2 DL757960161 1 19960123 A 3231 SOLENOID 96005011 BOEING 757 757232 1384965 NM RT MLG DOOR FAILED A DALA O OTHER J WARNING INDICATION LD LANDING 1 SO 27 642DL FAH0504 23996 RIGHT MAIN GEAR WOULD NOT EXTEND NORMALLY, USED ALT EXTENSION AND GOT NORMAL INDICATION. REPLACED RT GEAR DOOR INTERLOC K SOLENOID AND OPS NORMAL. 2 L 7 2 4F RT A2NM 1996020200258 19960202 00258 NM 1996 2 2 DL757960214 1 19960128 A 3350 BPS73 POWER SUPPLY BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 673DL 25978 POWER SUPPLY FUSES OPEN, TRACK LIGHTS INOP IN AFT CABIN. REPLACED POWER SUPPLY AND OPS CHECK NORMAL. 2 L 7 2 4F RT A2NM 1996020200259 19960202 00259 NE 1996 2 2 DL76L960185 2 19960124 A 7230 COMPRESSOR BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE STALLED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 27 180DN 25985 724685 ENGINE COMPRESSOR STALLED AS POWER WAS ADDED FOR T/O. BELIEVED TO BE LT ENGINE, NO EXCEEDENCE, ENGINE WAS REPLACED AND ROUTED TO SHOP. 2 L 7 2 4F 4 F RT A1NM E24NE 1996020200260 19960202 00260 NM 1996 2 2 DL76L960186 1 19960124 A 2560 SLIDE RELAY BOEING 767 767332 1382001 NM E4 RACK DEFECTIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 173DN 24800 ON ALL CABIN SERVICE AND ENTRY DOORS, THE SLIDE ARMED LIGHT WILL NOT FLASH IN ARMED MODE WITH THE HANDLE SLIGHTLY PULLED . REPLACED DEFECTIVE RELAY, OPERATION NORMAL. 2 L 7 2 4F RT A1NM 1996020200261 19960202 00261 NM 1996 2 2 DL76L960192 1 19960125 A 5754 114T310022A SLAT BOEING 767 767332 1382001 NM NR 7 LE SLAT DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 172DN 24775 THE NR 7 SLAT TRAILING EDGE WEDGE LOWER SKIN WAS FOUND WITH A HOLE. THE HOLE IS .5 INCH IN DIAMETER AND IS LOCATED 42 I NCHES INBOARD FROM THE OUTBOARD EDGE AND 4 INCHES FOWARD OF THE AFT EDGE. THE TRAILING EDGE WEDGE IS MANUFACTURED WITH 0.016 5052-H38 FACE SHEETS WITH A METALLIC HONEYCOMB CORE PER BMS 4-6, TYPE 4.1-25. ACCOMPLISHED REPAIRS PER DL ERA 273 086-14AD. 2 L 7 2 4F RT A1NM 1996020200262 19960202 00262 WP 1996 2 2 DLL10960101 1 19960116 A 3230 BUSHING LS100203A7 LKHEED 1011 10113851 5265010 WP LT GEAR NOT INSTALLED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 733DS 193C1224 ON GEAR RETRACTION, RED DOOR AND INTRANS WITH LEFT GEAR OR DOOR ON S/O PANEL. CYCLED GEAR, SAME INDICATIONS. FOUND PHA SE CONTROL VALVE INCORRECTLY INSTALLED DUE TO OMITTED BUSHING ON THE TWO ACTUATING ROD/S TWO LUGS. INSTALLED MISSING BU SHING, OPERATION NORMAL. 2 L 7 3 4F A23WE 1996020200263 19960202 00263 WP 1996 2 2 DLL10960190 1 19960123 A 5312 1504400 BULKHEAD LKHEED 1011 10113851 5265010 WP FS 1212 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 712DA 193C1088 WHILE PERFORMING INSPECTION SI 7-70645-12, THE FS 1212 CANTED BULKHEAD WAS FOUND WITH A 12 INCH LONG VERTICAL CRACK AT R BL 22.5. THE SUBJECT WEB IS M/F .050 7075 T6 CLAD SHEET. ACCOMPLISHED REPAIRS PER DL ERA 273152-14. 2 L 7 3 4F A23WE 1996020200264 19960202 00264 WP 1996 2 2 DLL10960191 1 19960125 A 5320 1553017 FITTING LKHEED 1011 10113851 5265010 WP FS 792 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 733DS 193C1224 BOTH THE FWD AND AFT FITTINGS ON THE FWD FRAME FS 792 ARE REQUIRED TO BE MFG'D TO ACCOMMODATE A FRAME REPAIR INSTALLED B Y ER/A 271917-14. SUBJECT FITTINGS ARE M/F 7075-T6 DIE FORGINGS, APPROVAL PER DL ERA 271918-14 REV B. 2 L 7 3 4F A23WE 1996020200265 19960202 00265 WP 1996 2 2 DLL10960195 1 19960125 A 5312 1505220 WATERLINE LKHEED 1011 10113851 5265010 WP FS 1363 ELONGATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 714DA 193C1090 WHILE ACCOMPLISHING THE CENTER WEB SPLICE ON THE FS 1363 BKHD PER SI 7-69959-14AD, OPN 0319, THE POTABLE WATER LINE CUTO UT WAS DAMAGED AND ELONGATED THROUGH THE WEB AND FWD MOD SPLICE STRAP. THE ORIGINAL CUTOUT WAS A 1.25 DIA HOLE. THE EL ONGATED CUTOUT HAS A MAX WIDTH OF 1.5 AND CAUSES A SHORT EDGE DISTANCE CONDITION OF .22 MIN ON 4 ADJACENT FASTENERS. TH E ORIGINAL WEB IS MADE FROM .065 THICK 7075-T6 CLAD SHEET. THE FWD MOD SPLICE STRAP IS MADE FROM .080 THICK 7075-T6CLAD SHEET. ACCOMPLISHED REPAIRS PER DL ERA 272019-14 REV A. 2 L 7 3 4F A23WE 1996020200266 19960202 00266 WP 1996 2 2 DLL13960193 1 19960125 A 5312 STRAP LKHEED 1011 10113851 5265010 WP FS 1363 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 790DL 193A1143 THE BULKHEAD SPLICE STRAP AT FS 1363 LBL 42.5 WAS FOUND CRACKED. THE SUBJECT STRAP IS M/F 0.100 7075-T6 CLAD. ACCOM PLISHED REPAIRS PER DL ERA 272789-14AD. 2 L 7 3 4F A23WE 1996020200267 19960202 00267 NM 1996 2 2 DLM88960179 1 19960123 A 3340 LIGHT LENS DOUG MD88 MD88 3023688 NM RT WING LIGHTNING STRIKE A DALA O OTHER C B F.O.D. SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 905DL 49536 AIRCRAFT INCURRED LIGHTNING STRIKE ON APPROACH AND SMOKE WAS SMELLED IN CABIN AND COCKPIT. THE SMOKE OCCURED 5 TO 8 MIN AFTER STRIKE AND DISSIPATED AFTER 10 MIN. INSPECTED AIRCRAFT PER M/M 05-53-00 PG 601. FOUND RT AFT TAIL LIGHT LENS SH ATTERED AND NO OTHER DAMAGE NOTED. REPLACED LENS, RAN PACKS AND NO ODORS OR SMOKE. 2 L 7 2 4F RT A6WE 1996020200268 19960202 00268 NM 1996 2 2 DLM88960182 1 19960124 A 3222 STRUT DOUG MD88 MD88 3023688 NM NLG REQD SERVICE A DALA K NONE J WARNING INDICATION LD LANDING 1 SO 27 919DE 53422 NOSE GEAR UNSAFE LIGHT ON RETRACTION, CYCLED SAME LIGHT WITH CORRESPONDING NOISE. SERVICED NOSE STRUT PER JIC OP 4703, JACKED A/C, CYCLED NOSE GEAR AND ALL IND NORMAL. A/C OK FOR SERVICE. 2 L 7 2 4F RT A6WE 1996020200269 19960202 00269 NM 1996 2 2 DLM88960189 1 19960124 A 3220 STRUT DOUG MD88 MD88 3023688 NM NLG REQD SERVICE A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 919DE 53422 NOSE GEAR UNSAFE LIGHT ON RETRACTION, CYCLED SAME LIGHT WITH CORRESPONDING NOISE. SERVICED NOSE STRUT PER JIC OPN 4703, JACKED AN CYCLED NOSE GEAR AND ALL INDICATIONS NORMAL. A/C OK FOR SERVICE. 2 L 7 2 4F RT A6WE 1996020200270 19960202 00270 NM 1996 2 2 DLM88960205 1 19960126 A 2913 PUMP DOUG MD88 MD88 3023688 NM LT MLG WW FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 923DL 49705 AFTER T/O, SMOKE IN CABIN AND COCKPIT WITH SMOKE ALARMS ON FURTHER INSP FOUND HYD TRANSFER PUMP CASE DRAIN LINE HAD FILL ED ITS OVERFLOW CONTAINER. WHICH IN TURN HAD BEEN RUNNING INTO THE APU INTAKE. REPLACED HYD TRANSFER PUMP, DUMPED AND CLEANED DRAIN CAN. APU WILL HAVE TO BE CLEANED TO PREVENT FURTHER CONTAMINATION OF AIR CONDITIONER SYSTEMS. 2 L 7 2 4F RT A6WE 1996020200271 19960202 00271 WP 1996 2 2 MWEA96028 1 19960126 A 5311 FRAME DOUG DC9 DC914 3022034 WP LT MLG WW GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 DURING D-CHECK, FOUND FWD FRAME OF LT WHEEL WELL OPENING HAS A DEEP GOUGE 4 INCHES LONG. INSTALLED DOUBLER REPAIR IAW S RM 53-01 FIG 2 SHEET 4. RETURNED A/C TO SERVICE. 2 L 7 2 4F A6WE 1996020200272 19960202 00272 NM 1996 2 2 VSTA9601014 1 19960128 A 2810 106121061N FUEL CELL BOEING 737 737204 1384458 NM NR 2 DAMAGED A VSTA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 07 312VA 20236 FUEL LEAKING FROM CENTER DRAIN MAST. REPLACED CENTER TANK NR 2 FUEL BLADDER AND REPAIRED VENT BOX. LEAK CHECKS NORMAL. 2 L 7 2 4F A16WE 1996020200273 19960202 00273 NM 1996 2 2 VSTA9601015 1 19960128 A 5610 BAC008632 WINDOW BOEING 737 737247 138448D NM R1 WINDOW CRACKED A VSTA K NONE O OTHER IN INSP/MAINT 1 WP 07 302VA 20126 R1 WINDOWS OUTER PANE CRACKED. REMOVED AND REPLACED R1 WINDOW AND HEAT CONTROLLER. 2 L 7 2 4F A16WE 1996020200346 19960202 00346 NM 1996 2 2 96ZZZM102 1 19960103 A 3350 3314030 LIGHT BOEING 727 727227 1384078 NM CABIN INOP A AMTA K NONE L NO TEST CR CRUISE 1 GL 11 769AT 028715 21998 EMERGENCY EXIT LIGHT ABOVE RIGHT FORWARD SERVICE DOOR INOP. REMOVED AND REPLACED FORWARD EMERGENCY EXIT LIGHT. 2 L 7 3 4F A3WE 1996020200350 19960202 00350 NE 1996 2 2 96ZZZM106 2 19960103 A 7261 ENGINE OIL 2380 DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE RIGHT REQ'D SERV A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 429JS 3043 FLT NR 4005 - EN ROUTE FROM CVG TO PHL, CAPTAIN NOTICED A FLUCTUATION IN THE RIGHT ENGINE OIL PRESSURE INDICATION. AIRC RAFT DIVERTED TO PIT WHERE MX SERVICED THE RIGHT ENGINE WITH FOUR QUARTS OF TURBINE OIL. GROUND CHECKED GOOD AIRCRAFT T O SERVICE. (M) 2 H 7 2 4T 4 T RT A45NM E20NE 1996020200428 19960202 00428 NM 1996 2 2 AALA960002 1 19960101 A 3350 A3060720101 CONDUCTOR DOUG MD11 MD11 3023602 NM CABIN CORRODED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1763 48553 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT LEFT AISLE FROM L2 DOOR TO PAX SEAT ROW 15B INOPERATIVE. REPLAC ED EMERGENCY FLOOR LIGHT FLAT CONDUCTOR AFT OF L2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1996020200429 19960202 00429 EU 1996 2 2 AALA960010 1 19960103 A 3260 200392605 BUFFER FOKKER F28 F28MK0100 4990807 EU LT MLG NEED ADJUST A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 1431B 11416 BNA - FLT 2079 - AFTER TAKEOFF BNA, WHEN LANDING GEAR RETRACTED, LEFT MAIN LANDING GEAR MFDU WARNING DISPLAYED. RECYCLE D LANDING GEAR WITH SAME RESULTS. AIRCRAFT RETURNED TO BNA AND LANDED WITHOUT INCIDENT. ADJUSTED LEFT MAIN LANDING GEA R DOOR BUMPER AND INSTALLED LOCK PIN AND SAFETY WIRE. ACCOMPLISHED LANDING GEAR RETRACTON CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1996020200430 19960202 00430 WP 1996 2 2 AALA960017 1 19960107 A 3350 A3030398101 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 76201 53291 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 1 THROUGH 4 IN FIRST CLASS CABIN INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR BY PAX SEAT ROW 1. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 1996020200431 19960202 00431 WP 1996 2 2 AALA960018 1 19960107 A 3350 STRIP DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 210AA 49161 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FIRST CLASS GALLEY INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BY FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996020200443 19960202 00443 EU 1996 2 2 C2XA96IA014 1 19960111 A 2820 1153000 PRESS SWITCH AEROSP ATR42 ATR42320 8680930 EU RT NACELLE LEAKING A C2XA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 09 17810 093 IAH - DURING 4A CHECK INSPECTION, FOUND RT FUEL SHUTOFF VALVE PRESSURE SWITCH LEAKING, LOCATED BEHIND RIGHT ENGINE AFT U PPER COWLING, FORWARD OF FRONT WING SPAR. MAINTENANCE REMOVED AND REPLACED THE PRESSURE SWITCH. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996020200444 19960202 00444 EU 1996 2 2 C2XA96IA015 1 19960112 A 2710 2S711009100200 BELLCRANK BRG AEROSP ATR42 ATR42320 8680930 EU LT AILERON RUSTY A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14832 187 IAH - DURING 1A CHECK INSPECTION, FOUND LEFT AILERON CONTROL SYSTEM BELLCRANK BEARING BINDING AND RUSTY. BELLCRANK LOCA TED AT LEFT WING RIB 24, ACCESS THROUGH LOWER WING PANEL 523AB. MAINTENANCE REMOVED AND REPLACED THE BELLCRANK ASSEMBLY . AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996020200445 19960202 00445 EU 1996 2 2 C2XA96IA016 1 19960112 A 3350 44 BULB AEROSP ATR42 ATR42320 8680930 EU PAX DOOR FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14832 187 IAH - DURING 1A CHECK INSPECTION, THE PASSENGER DOOR/STAIR EMERGENCY FLOOR LIGHT WAS FOUND TO BE INOPERATIVE. LOCATED O N THE INTERIOR OF THE DOOR, LOWER SIDE OF THE SECOND STEP. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULB. AIRCRAFT A PPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996020200446 19960202 00446 EU 1996 2 2 C2XA96IA017 1 19960112 A 5320 ANGLE AEROSP ATR42 ATR42320 8680930 EU WING/FUS CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 97841 280 IAH - DURING 4C CHECK INSPECTION, FOUND A CRACKED ATTACHMENT ANGLE ON RIGHT WING TO FUSELAGE FAIRING SUPPORT FRAME NR 29 . MAINTENANCE REMOVED AND REPLACED ATTACHMENT ANGLE. (M) 2 H 7 2 4T RT A53EU 1996020200447 19960202 00447 EU 1996 2 2 C2XA96IA018 1 19960112 A 5730 S5241053600000 ACCESS PANEL AEROSP ATR42 ATR42320 8680930 EU LT WING CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 97841 280 IAH - DURING 4C CHECK INSPECTION, FOUND LEFT WING ACCESS PANEL NR 522CT TO HAVE CORROSION ON MATING SURFACES. MAINTENAN CE REMOVED AND REPLACED THE PANEL. (M) 2 H 7 2 4T RT A53EU 1996020200448 19960202 00448 SO 1996 2 2 C2XA96IA019 1 19960114 A 2550 PE710261 TIE DOWNS EMB 120 EMB120RT SO CARGO FLOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 34712 120111 IAH - DURING C1 CHECK INSPECTION, FOUND CARGO NET TIE DOWN PADS IN AFT CARGO TO BE CORRODED. THE TIE DOWN PADS ARE INST ALLED ONTO THE BUTTSTRAPS OF THE AFT CARGO FLOOR. MAINTENANCE REMOVED AND REPLACED THE TIE DOWN PADS. (M) 2 L 7 2 4T RT A31SO 1996020200449 19960202 00449 SO 1996 2 2 C2XA96IA020 1 19960115 A 5320 12015374002 ATTACH ANGLE EMB 120 EMB120RT SO RT AFT FUSE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 34712 120111 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT FIN TO FUSELAGE ATTACH ANGLE CRACKED, AT FASTENER HOLE. MAINTENANCE REMOVE D AND REPLACED THE ANGLE, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996020200450 19960202 00450 SO 1996 2 2 C2XA96IA021 1 19960115 A 5320 12020235005 BRACKET EMB 120 EMB120RT SO CABIN CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 34712 120111 IAH - DURING C-CHECK INSPECTION, FOUND FORWARD CARGO DOOR TORSION BAR BRACKET CRACKED. MAINTENANCE REMOVED AND REPLACED THE BRACKET. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996020200451 19960202 00451 SO 1996 2 2 C2XA96IA022 1 19960115 A 5400 12030995001 ANGLE EMB 120 EMB120RT SO LT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 34712 120111 IAH - DURING C-CHECK INSPECTION, FOUND LEFT NACELLE FRAME NR 2 UPPER ANGLE CRACKED. MAINTENANCE REMOVED AND REPLACED TH E ANGLE. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996020200452 19960202 00452 SO 1996 2 2 C2XA96IA023 1 19960115 A 5400 12030995001 ANGLE EMB 120 EMB120RT SO RT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 34712 120111 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT NACELLE FRAME NR 2 UPPER ANGLE CRACKED. MAINTENANCE REMOVED AND REPLACED T HE ANGLE. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996020200453 19960202 00453 SO 1996 2 2 C2XA96IA024 1 19960116 A 5347 12016000003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 34712 120111 IAH - DURING C-CHECK INSPECTION, FOUND THE RIGHT FORWARD FLOOR SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED TH E SEAT TRACK, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996020200454 19960202 00454 SO 1996 2 2 C2XA96IA025 1 19960116 A 5347 12026864007 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 34712 120111 IAH - DURING C-CHECK INSPECTION, FOUND THE LEFT AFT FLOOR SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEA T TRACK, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996020200455 19960202 00455 EU 1996 2 2 C2XA96IA026 1 19960116 A 2721 NTA14115005A BEARING AEROSP ATR42 ATR42320 8680930 EU RUDDER TAB WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 97841 280 IAH - DURING C-CHECK INSPECTION, FOUND RUDDER TAB CONTROL BELLCRANK MIDDLE BEARING WORN. MAINTENANCE REMOVED AND REPLAC ED THE BEARING. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996020200456 19960202 00456 EU 1996 2 2 C2XA96IA027 1 19960116 A 2721 MS276416 BEARING AEROSP ATR42 ATR42320 8680930 EU RUDDER TAB RUSTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 97841 280 IAH - DURING C-CHECK INSPECTION, FOUND RUDDER TAB CONTROL BELLCRANK PIVOT POINT BRACKET NR 7, BOTTOM BEARING RUSTED. M AINTENANCE REMOVED AND REPLACED THE BEARING. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996020200490 19960202 00490 WP 1996 2 2 CAL960001 1 19960101 A 2150 DUCT DOUG DC9 DC981 3022081 WP LT PACK LOOSE A CALA G O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 SW 09 13881 48045 FLT 1875 - THE CABIN PRESS BEGAN TO CLIMB SLOWLY WHILE AT CRUISE ALT FL 310 AND WAS ACCOMPANIED BY FLOW LIGHT COMING ON, WHILE EN ROUTE. SYS WAS SWITCHED TO STANDBY W/O REMEDY. WHILE DESCENDING TO 10,000 FT THE CABIN RATE OF CLIMB INCREAS ED AND THE 02 MASKS DEPLOYED. THE A/C WAS DIVERTED TO TPA WHERE IT LANDED SAFELY. MX FOUND RUBBER DUCT TO DISCHARGE SI DE OF LT PACK HAD PARTIALLY SLID OFF DUE TO LOOSE CLAMP. NEITHER THE DUCT OR CLAMP WERE DAMAGED. THE RUBBER DUCT WAS R EPOSITIONED AND RESECURED. THE A/C WAS PRESS AND NO LEAKS FOUND. THE O2 MASKS DID NOT DEPLOY AT ROWS 2, 4, 31, AND 32 LT, 31 RT, OR FWD F/A STA. ALL PAX AND F/A 02 GENS REPLACED. PSU DROP CK PERFORMED IAW MM 35-00-00 AND OPS CK GOOD.(M) 2 L 7 2 4F A6WE 1996020200498 19960202 00498 WP 1996 2 2 IXXA9601 1 19960103 A 3231 CONNECTOR DOUG DC8 DC871F 302199D WP RT MLG DOOR LOOSE A IXXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 828BX 45993 ON TAKEOFF OUT OF ONT, THE FLT CREW OBSERVED A LANDING GEAR DOOR UNSAFE INDICATION AFTER GEAR RETRACTION. THE LANDING G EAR WAS CYCLED, AND THE WARNING LIGHT EXTINGUISHED. TOL MAINTENANCE INSPECTED THE LANDING GEAR DOOR WARNING SYSTEM AND FOUND THE ELECTRICAL CONNECTOR ON THE RIGHT DOOR UPLATCH SWITCH LOOSE. THE CONNECTOR WAS SECURED AND THE INDICATION SYS TEM OPS CHECKED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 4 4F RT 4A25 1996020200499 19960202 00499 SW 1996 2 2 MALA964792 1 19960103 A 3260 POSITION IND SWRNGN SA227 SA227AC 8780603 SW LANDING GEAR MALFUNCTIONED A MALA O OTHER N FALSE WARNING DE DESCENT 1 GL 15 426MA AC645 FLT NR 3156 - INBOUND TO DTW, THE RIGHT MAIN GEAR DID NOT EXTEND WHEN THE GEAR HANDLE WAS SELECTED DOWN. THE CREW RECYC LED THE GEAR AND IT EXTENDED NORMALLY. THE AIRCRAFT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNE L FUNCTIONALLY TESTED THE LANDING GEAR SYSTEM, BUT WERE UNABLE TO DUPLICATE THIS DISCREPANCY. THE LANDING GEAR POSITION INDICATOR WAS REPLACED AS A PRECAUTION. (M) 1 L 7 2 4T A8SW 1996020200500 19960202 00500 SW 1996 2 2 MALA964793 1 19960104 A 3230 RETRACT MECH SWRNGN SA227 SA227AC 8780603 SW NLG MALFUNCTIONED A MALA O OTHER J WARNING INDICATION DE DESCENT 1 GL 15 438MA AC721B FLT NR 3078 - INBOUND TO MSP, THE NOSE GEAR STARTED CYCLING UP AND DOWN. THE AIRCRAFT CONTINUED TO MSP AND LANDED WITHO UT INCIDENT. MAINTENANCE PERSONNEL FUNCTIONALLY TESTED THE LANDING GEAR AND PERFORMED RIGGING CHECKS BUT WERE UNABLE TO DUPLICATE THIS DISCREPANCY. (M) 1 L 7 2 4T A8SW 1996020200506 19960202 00506 EU 1996 2 2 VTZA96065 1 19960124 A 2150 1379211L403 ACM BAG JETSTM JETSTM3201 1500217 EU LT WING ROOT OVERSERVICED A VTZA G H O2 MASK DEPLOYED DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 27 495UE 818 PHF/IAD - FLT 6242 AT 1848 HOURS ON 1-24-96, THE FLIGHT CREW REPORTED NOXIOUS FUMES FROM THE FLOWS IN-FLIGHT. CREW DEAC TIVATED SYSTEM AND DEPLOYED OXYGEN MASKS. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED THE EX CESS OIL FROM THE LT ACM. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1996020200507 19960202 00507 1996 2 2 VTZA96061 4 19960111 A 3454 069102505 TRANSCEIVER BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 478UE 892 FLT NR 6200 - IAD-ROA - DURING CRUISE, RETURNED TO IAD DUE TO BOTH NAVIGATION RADIOS WERE INTERMITTENT. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED BOTH NAVIGATION RECEIVERS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996020200508 19960202 00508 EU 1996 2 2 VTZA96062 1 19960112 A 3240 91SE16 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU PARKING BRAKE OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 316UE 41055 FLT NR 6490 - JFK-IAD - ABORTED TAKEOFF DUE TO THE TAKEOFF CONFIG WARNING SYSTEM SOUNDING ON THE TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. AIRCRAFT THEN WAS FERRIED TO IAD AND LANDED WITH NO FURTHER INCIDENTS. MA INTENANCE ADJUSTED THE PARKING BRAKE MICROSWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996020200509 19960202 00509 EU 1996 2 2 VTZA96063 1 19960105 A 2435 23095002 START GEN JETAIR JETSTM JETSTM4101 1500501 EU LEFT FAILED A VTZA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 27 320UE 41043 FLT NR 6207 - IAD-MHT - MADE AN UNSCHEDULED LANDING DUE TO LEFT GENERATOR FAILURE. AIRCRAFT RETURNED TO GATE WITH NO FU RTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED STARTER/GENERATOR AND PERFORMED GROUND RUNS. AIRCRAFT WAS RELEASED A ND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996020200545 19960202 00545 NM 1996 2 2 96UAL900081 1 19960130 A 3350 BATTERY PACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 533UA 25073 EEL LIGHTING GOES OFF AFTER 7 SECONDS WITH MASTER SWITCH IN FLIGHT DECK AND AGAIN WITH AFT ATTENDANT PANEL TURNED ON. R EPLACED BATTERY PACK AND LIGHTS CHECK NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996020200546 19960202 00546 NM 1996 2 2 96UAL900082 1 19960130 A 2133 39606411 OUT FLOW VALVE BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE FUSELAGE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 9060U 19941 CREW REPORTS, UNABLE TO PRESSURIZE AIRPLANE AFTER TAKEOFF. CAN CONTROL OUTFLOW VALVE OPEN AND CLOSE. THE RIGHT FLOW CO NTROL VALVE WOULD NOT TURN ON. REPLACED FLOW CONTROL VALVE AND CONNECTOR PINS. THE SHOP FOUND THE FLOW CONTROL VALVE H AD LOW AIR FLOW CAUSED BY A FAILED BUTTERFLY SEAL, A SENSE LINE WITH A HOLE IN IT, A BAD FILTER CIRCUIT AND FROZEN MOTOR BEARINGS. 2 L 7 2 4F 4 F A16WE E2EA 1996020200547 19960202 00547 NM 1996 2 2 DHL727005 1 19960131 A 2150 39854021 SHUTOFF VALVE BOEING 727 727228 NM LT PACK FAILED A DHLA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 727DH 20204 AIRCRAFT COULD NOT PRESSURIZE IN AUTO/MANUAL OR STANDBY. FLEW AT 10,000 MSL UNPRESSURIZED, REQUIRED FUEL STOP IN MCI. R EMOVED AND REPLACED LEFT HAND PACK SHUTOFF VALVE, OPS CHECKED OK. 2 L 7 3 4F A3WE 1996020200548 19960202 00548 NM 1996 2 2 DL72L960208 1 19960119 A 5754 651622296 RIBS BOEING 727 727232 1384082 NM NR 6 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 504DA 21306 DURING INSPECTION, NR 6 L/E SLAT WAS FOUND WITH RIBS NR 12, 13, 14 AND 15 CRACKED. ACCOMPLISHED REPAIRS PER MM 57-54-0. 2 L 7 3 4F A3WE 1996020200549 19960202 00549 NM 1996 2 2 DL72L960210 1 19960118 A 5754 651622296 ANGLE BOEING 727 727232 1384082 NM NR 6 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 504DA 21306 LOWER FWD ANGLE CRACKED AT NR 13 RIB. REPAIRED PER MM 57-54-0 PG 807A. ALSO, WIND EROSION FWD OUTER SKIN. REPAIRED L/ E WIND EROSION PER SRM 57-50-3 FIG 8 FOR L/E SLAT NR 6. 2 L 7 3 4F A3WE 1996020200550 19960202 00550 NM 1996 2 2 DL72L960229 1 19960129 A 2780 BRACKET BOEING 727 727232 1384082 NM NR 1 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 508DA 21310 NR 1 SLAT ACTUATOR I/B BRACKET BROKEN OUT AROUND FWD ATTACH BOLT. FOUND DURING C-1 LTR CK TPAMM. REPAIRED PER M/M 57-2 0-21. 2 L 7 3 4F A3WE 1996020200551 19960202 00551 NM 1996 2 2 DL72S960216 1 19960128 A 5754 6516221100 RIB BOEING 727 727232 1384082 NM NR 5 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 408DA 21152 RIB WAS FOUND TO BE CRACKED ON INSPECTION. RIB WAS REPAIRED PER M/M 57-54-00. FOUND DURING SHOP INSPECTION OF NR 5 L/E SLAT. 2 L 7 3 4F A3WE 1996020200552 19960202 00552 NM 1996 2 2 DL72S960217 1 19960128 A 5754 6516221100 SKIN BOEING 727 727232 1384082 NM NR 5 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 408DA 21152 OUTER SKIN CRACKED AT FENCE ATTACH HOLE AND GROOVED AT REMAINING ATTACH HOLES. SKIN WAS REPAIRED PER M/M 57-54-0. FOUN D DURING SHOP INSPECTION OF NR 5 L/E SLAT. 2 L 7 3 4F A3WE 1996020200553 19960202 00553 NM 1996 2 2 DL72S960218 1 19960128 A 5754 6516221100 SKIN BOEING 727 727232 1384082 NM NR 5 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 408DA 21152 LOWER L/E SKIN CRACKED AND WORN AT FENCE ATTACH HOLE. SKIN WAS REPAIRED PER M/M 57-54-0. FOUND DURING SHOP INSPECTION OF NR 5 LE SLAT. 2 L 7 3 4F A3WE 1996020200554 19960202 00554 NM 1996 2 2 DL72S960219 1 19960128 A 5754 65162256A SKIN BOEING 727 727232 1384082 NM NR 4 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 517DA 21433 NR 4 KRUEGER FLAP HAS TWO 1 INCH CRACKS AT O/B CUTOUT FOR LWR LIP ATTACH FITTING. REPAIRED PER SRM 57-50-3. 2 L 7 3 4F A3WE 1996020200555 19960202 00555 NM 1996 2 2 DL72S960221 1 19960129 A 3350 1060091102 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 485DA 20865 EMERGENCY LIGHTS OVER DOOR INOP AT R1 AND R2. REPLACED LIGHT ASSYS. 2 L 7 3 4F A3WE 1996020200556 19960202 00556 NM 1996 2 2 DL72S960227 1 19960119 A 5347 GALLEY TRACK BOEING 727 727232 1384082 NM BS 380-440 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 517DA 21433 ATL HMV, STA 380 TO 440 CENTER RT GALLEY TRACK HAS CORROSION IN AND ON LEGS OF TRACK. REMOVED TRACKS FROM STA 380 TO 44 0. INSTALLED NEW TRACK PER MM 53-20-11. 2 L 7 3 4F A3WE 1996020200557 19960202 00557 NM 1996 2 2 DL72S960231 1 19960119 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 1090-1110 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 517DA 21433 HMV ATL, CORROSION STA 1090 TO 1110. BULGED BETWEEN STRINGER AND SKIN APPROX 6 INCHES FWD OF 1090 TO 4 INCHES AFT OF 1 110. REPAIRED DAMAGE PER SRM 53-12-0 FIG 807. 2 L 7 3 4F A3WE 1996020200558 19960202 00558 NM 1996 2 2 DL72S960233 1 19960126 A 5330 65545902 SKIN BOEING 727 727232 1384082 NM FS 720 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 405DA 21149 DURING INSPECTION, CORROSION WAS FOUND ON THE BELLY SKIN ABOVE THE RAM AIR INLET. THE DAMAGE CUTOUT MEASURES 12 INCHES FWD AND AFT BY 10 INCHES INBD AND OUTBD AT FS 720C. IN ACCORDANCE WITH 8110-3 DATED 1/26/96, AN EXTERNAL DOUBLER AND TR IPLER WERE INSTALLED AROUND THE CUTOUT. AN PREEXISTING TI DOUBLER WAS REPLACED BY THIS REPAIR. 2 L 7 3 4F A3WE 1996020200559 19960202 00559 NM 1996 2 2 DL73S960223 1 19960129 A 3260 189929 SENSOR BOEING 737 737232 1384475 NM RT MLG FAILED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 321DL 23093 SHIP 321 WAS OFF AND RETURNED WITH RT GEAR UNSAFE LIGHT. FOUND RT MAIN GEAR SENSOR S73 BAD. REPLACED SAME AND OPS NORM AL. 2 L 7 2 4F RT A16WE 1996020200560 19960202 00560 NM 1996 2 2 DL757960224 1 19960128 A 2910 BACH8A04EE0232K HYD HOSE BOEING 757 757232 1384965 NM LT MLG WW FAILED A DALA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 656DL 24396 AFTER LANDING, LEFT HYD QTY WENT TO ZERO, FLAPS STOPPED AT 1 DEGREE DURING RETRACTION, SET HANDLE TO MATCH FLAPS. FOUND HYD LINE GOING TO THE DOWN AND LOCK ACTUATOR IN THE LEFT WHEEL WELL WITH PUNCTURE. INSTALLED APPROVED HYD LINE. ATL A DVISED, NO LEAKS FOUND ON TEST. 2 L 7 2 4F RT A2NM 1996020200561 19960202 00561 NM 1996 2 2 DL76E960222 1 19960128 A 3230 LOCK ACTUATOR BOEING 767 767232 1385132 NM RT MLG FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 112DL 22224 FRA - RIGHT GEAR DID NOT RETRACT ON DEPARTURE. CHECKED RIGHT GEAR FOR OBVIOUS DAMGE AND NONE FOUND. RESET RIGHT GEAR U P FUSE PER MM 32-32-19. CHECKED GEAR OPS WITH LG PINS INSTALLED AND FOUND ALL HYD AVAILABLE TO RETRACT GEAR. ALSO, REP LACED PROX BOX DUE FAILED CARD 014. THEN HAD 2ND ATB DUE TO RT MAIN GEAR DID NOT RETRACT ON DEPARTURE. FOUND DRAG BRAC E LOCK ACTUATOR FAILED. 2 L 7 2 4F RT A1NM 1996020200562 19960202 00562 NM 1996 2 2 DL76L960239 1 19960125 A 5414 SKIN BOEING 767 767332 1382001 NM NR 2 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 173DN 24800 AT LETTER CHECK IN DFW, A .5 INCH CRACK WAS FOUND IN THE NR 2 ENGINE PYLON OUTBOARD STRUT SKIN. THE CRACK EMANATES FROM THE FORWARD TORQUE BOX ACCESS HOLE AT THE UPPER FORWARD CORNER AT APPROXIMATELY NAC STA 158 AND EXTENDS DIAGONALLY UPWA RD AND FWD TO A FASTENER HOLE. BOTH SHEETS OF 0.080 2024-T3 BONDED ASSY ARE CRACKED. REPAIRED PER DL ERA 273175-14. 2 L 7 2 4F RT A1NM 1996020200563 19960202 00563 NM 1996 2 2 DL76S960203 1 19960126 A 2910 CHECK VALVE BOEING 767 767332 1382001 NM LT MLG WW CRACKED A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 123DN 23437 INFLIGHT GOT EICAS FOR LT SYS HYDRAULIC'S, FOLLOWED IMMEDIATELY BY LEFT HYDRAULIC SYS PRESSURE MESSAGE. STATUS PAGE SHO WS LT QTY AT 0.04. FOUND CHECK VALVE AT GROUND HYD SERV QUICK DISCONNECT LEAKING. 2 L 7 2 4F RT A1NM 1996020200564 19960202 00564 WP 1996 2 2 DLL10960240 1 19960123 A 5312 1504400 WEB LKHEED 1011 10113851 5265010 WP FS 1212 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 720DA 193C1136 AT LAYOVER IN ATL WHILE PERFORMING SI 7-70645-12, THE FS 1212 CANTED BULKHEAD WAS FOUND WITH VERTICAL CRACKS AT RBL 22.5 LBL 10 AND LBL 30. THEY MEASURE 9, 8 AND 9 INCHES RESPECTIVELY. ALSO, WHILE ACCOMPLISHING REPAIR, ONE HOLE AT LBL 30 WAS DRILLED WITH SHORT EDGE DISTANCE AND AN ADJACENT HOLE WAS DAMAGED RESULTING IN A SMALL CRACK. ACCOMPLISHED REPAIRS PER DL ERA 273157-14C. 2 L 7 3 4F A23WE 1996020200565 19960202 00565 WP 1996 2 2 DLL13960230 1 19960129 A 2120 DUCT LKHEED 1011 10113851 5265010 WP NR 3 PACK LOOSE A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 782DL 193A1006 AT FL 330, FLT CREW HEARD A LOUD BANG AND CABIN STARTED TO CLIMB AT 2,000 FPM UNABLE TO HOLD MORE THEN 4 PSID. DIVERTED TO SLC, FOUND DUCT BLOWN LOOSE FROM FITTING ON NR THREE PACK. REATTACHED DUCT AND RAN NR 3 PACK OPS OK. 2 L 7 3 4F A23WE 1996020200566 19960202 00566 1996 2 2 DLM88960220 4 19960128 A 2210 26ET59T SWITCH 4034242972 DOUG MD88 MD88 3023688 NM AUTO FLT CONTL FAILED A DALA L ABORTED APPROACH F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 27 996DL 91111537 53363 ON FINAL APPROACH A/P WOULD NOT DISCONNECT WITH THE YOKE DISCONNECT SWITCHES OR THE ON/OFF SWITCH ON THE AUTO FLIGHT CON TROL PANEL. IT WAS NECESSARY TO PULL C/BS TO DISCONNECT A/P. REPLACED MODE CONTROL PANEL OPERATION NORMAL. ANALYSIS R EVEALED THAT THE FGCP FAILURE WAS CAUSED BY A DEFECTIVE AUTOPILOT ENGAGE TOGGLE SWITCH. MICROSWITCH, DIVISION OF HONEYW ELL INC HAS IDENTIFIED AN INFERIOR SWITCH MANUFACTURING PROCESS FOR SWITCHES PROCUCED FROM MAR 1991 TO MAY 1993. DELTA ISSUED A SPECIAL INSPECTION TO FIND AND REMOVE FROM SERVICE ALL SUSPECT UNITS. 2 L 7 2 4F RT A6WE 1996020200567 19960202 00567 WP 1996 2 2 SCNA96010 1 19960125 A 2560 14111101 BATTERY DOUG DC10 DC1015 3022118 WP L1 DOOR SLIDE DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 152SY 48289 L-1 PASSENGER DOOR SLIDE LOW PRESSURE LIGHT DOES NOT PRESS TO TEST. REMOVED AND REPLACED BATTERIES IN L-1 DOOR SLIDE AN D SLIDE TESTED GOOD. 2 L 7 3 4F A22WE 1996020200568 19960202 00568 NM 1996 2 2 SCNA96011 1 19960120 A 3350 10617837 TERMINAL BOEING 727 727225 1384077 NM CABIN SHORTED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 282SC 22558 EMERGENCY EXIT CIRCUIT BREAKER WOULD NOT RESET. FOUND SHORTED BULB TERMINAL AT RIGHT FORWARD OVERWING EMERGENCY EXIT LI GHT. REPOSITIONED TERMINAL AND OPS CHECKED NORMAL. 2 L 7 3 4F A3WE 1996020200569 19960202 00569 NM 1996 2 2 UPS205348 1 19960130 A 3350 BATTERY BOEING 727 72727C 138400J NM MAIN ENTRY DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 910UP 19117 MAINTENANCE REPORTED, EMERGENCY EXIT LIGHT ASSY AT MAIN ENTRY AND CABIN ENTRANCE WEAK AND WILL NOT ILLUMINATE. REMOVED AND REPLACED BATTERIES, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1996020200570 19960202 00570 NM 1996 2 2 UPS205349 1 19960131 A 3350 LIGHT BOEING 727 72727C 138400J NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 914UP 19246 MAINTENANCE REPORTED, FWD COCKPIT EMERGENCY EXIT LIGHT INOP. RESET EMERGENCY EXIT LIGHT, BATT RECHARGED AND OPS CHECK O F LIGHT GOOD, NO DEFECTS SEEN. 2 L 7 3 4F A3WE 1996020200572 19960202 00572 WP 1996 2 2 UPS805350 1 19960106 A 5730 TE WEDGE DOUG DC8 DC871F 302199D WP RT WING CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 710UP 45938 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING T/E EDGE O/B WEDGE HAS CORROSION ON INNER LOWER SURFACE. REPAIRED PE R 51-1-21. 2 L 7 4 4F RT 4A25 1996020200573 19960202 00573 WP 1996 2 2 UPS805351 1 19960106 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 608-614 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 710UP 45938 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, MODERATE CORROSION ON RT WING L/E BETWEEN XFS 608 TO XFS 614, LOWER SURFACE. REPLACED DOUBLER SECTION PER DOUGLAS PRINT 5769600. 2 L 7 4 4F RT 4A25 1996020200574 19960202 00574 WP 1996 2 2 UPS805352 1 19960105 A 5753 FLAP TRACK DOUG DC8 DC871F 302199D WP RT TE FLAP CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 710UP 45938 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, BOTH I/B AND O/B FLAP TRACK ASSYS HAVE CORROSION PITS, LOWER SIDE RT AFT I/B FLAP ASSY STA XW 98. REPLACED TRACKS PER MM 27-51-03. 2 L 7 4 4F RT 4A25 1996020200575 19960202 00575 WP 1996 2 2 UPS805353 1 19960103 A 5311 FRAME DOUG DC8 DC871F 302199D WP FS 80 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 710UP 45938 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, MODERATE CORROSION ON AFT SIDE OF BOLT FRAME FS 80, LONGERON 26R. REPAIRED B OLT FRAME PER SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1996020200576 19960202 00576 WP 1996 2 2 UPS805354 1 19960102 A 5320 FITTING DOUG DC8 DC871F 302199D WP FS 802 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 45938 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, HEAVY CORROSION ON MAIN CABIN VERTICAL ATTACH FITTING, FS 802, RBL 40. REPLA CED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996020200577 19960202 00577 WP 1996 2 2 UPS805355 1 19960102 A 5320 ANGLE DOUG DC8 DC871F 302199D WP FS 798 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 45938 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION BULGE ON VERTICAL ATTACH ANGLE AND WEB FS 798, RBL 40. REPLACED AN GLE PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1996020200578 19960202 00578 WP 1996 2 2 UPS805356 1 19960130 A 2710 AILERON LIGHT DOUG DC8 DC871F 302199D WP COCKPIT ILLUMINATED A IPXA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 730UP 46030 CREW REPORTED, AILERON CONTROL MANUAL LIGHT ILLUMINATED IN FLIGHT, NO LOSS OF HYD CHECKLIST COMPLETED AND LANDING UNEVEN TFUL. INSPECTED AIL CABLES, PWR PACKS AND ALL ASSOCIATED SYSTEMS AND NO VISUAL DEFECTS NOTED. AIL HYD PWR SYSTEMS CHEC KS NORMAL PER MM 27-10-00. 2 L 7 4 4F RT 4A25 1996020200579 19960202 00579 NM 1996 2 2 9602216303 1 19960125 A 2710 550030017 ACTUATOR BOEING 747 747451 1384940 NM RT AILERON FAILED A NWAA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CR CRUISE 1 GL 01 663US 17189 17090 23818 DURING CRUISE, AN AILERON LOCKOUT STATUS MESSAGE APPREARED ON EICAS. AIRCRAFT DUMPED 161,000 POUNDS OF FUEL, RETURNED T O DTW, AND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT OUTBOARD AILERON ACTUATOR. OPERATIONAL CHECK OK. PART TOTAL CYCLES, 2,069. 2 L 7 4 4F RT A20WE 1996020200580 19960202 00580 NM 1996 2 2 9602222299 1 19960129 A 3350 BATTERY PACK BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 299US 22153 DURING PRE-FLIGHT, FOUND EMERGENCY TRACK LIGHTING INOPERATIVE AT ROW 16. REPLACED THE POWER SUPPLY AND BATTERY PACK. C HECKED OK. 2 L 7 3 4F A3WE 1996020200581 19960202 00581 1996 2 2 9602232201 4 19960130 A 3444 GROUND PROX WARN BOEING 727 727251 138408H NM COCKPIT SOUNDED A NWAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 01 201US 22154 DURING SHORT FINAL, GROUND PROXIMITY WARNING SOUNDED PULL-UP COMMAND. AIRCRAFT MADE A GO-AROUND AND LANDED WITHOUT INCI DENT. RIGGED BODY CABLE SYSTEM. CHECKED OK. 2 L 7 3 4F A3WE 1996020200582 19960202 00582 NM 1996 2 2 9602242287 1 19960130 A 5270 SWITCH BOEING 727 727251 138408H NM AIRSTAIR MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 287US 21375 DURING TAKEOFF ROLL, AMBER AIRSTAIR WARNING LIGHT ILLUMINATED. REJECTED TAKEOFF AT LESS THAN 60 KNOTS. AIRCRAFT STOPPE D WITHOUT INCIDENT. REPLACED SWITCH S394 AND GREASED PLUNGER. AIRSTAIR INDICATION CHECKED OK. 2 L 7 3 4F A3WE 1996020200583 19960202 00583 WP 1996 2 2 9602259154 1 19960130 A 3350 1001191 LIGHT DOUG DC9 DC914 3022034 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8913E 2845 2845 45830 DURING LINE CHECK, FOUND FORWARD ENTRY PORTABLE EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY. 2 L 7 2 4F A6WE 1996020200584 19960202 00584 NE 1996 2 2 9602266612 2 19960127 A 7200 ENGINE BOEING 747 747251B 1384892 NM PWA JT9 JT9D7F 52054 NE NR 1 FAILED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 01 612US 20357 62880 EN ROUTE NRT-SFO, THE NR 1 ENGINE OIL PRESSURE AND QUANTITY DECREASED TO ZERO. CREW FOLLOWED COCKPIT OPERATING PROCEDUR E, SHUT ENGINE DOWN, DECLARED EMERGENCY, AND DESCENDED TO FL 250. FLIGHT DIVERTED TO HNL AND LANDED WITHOUT FURTHER INC IDENT. AIRCRAFT WAS FERRIED TO MSP WHERE THE NR 1 ENGINE WAS CHANGED. 2 L 7 4 4F 4 F A20WE E20EA 1996020200585 19960202 00585 NE 1996 2 2 9602271141 2 19960126 A 7230 COMPRESSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20J 52054 NE NR 3 ENGINE STALLED A NWAA O OTHER R PARTIAL RPM/PWR LOSS LD LANDING 1 GL 01 141US 46750 86160 DURING LANDING ROLL-OUT (CDG), THE NR 3 ENGINE EXPERIENCED A SLIGHT REVERSE STALL. CREW FOLLOWED COCKPIT OPERATING PROC EDURE BY SHUTTING THE ENGINE DOWN AND PROCEEDED WITH LANDING WITHOUT FURTHER INCIDENT. REPLACED THE NR 3 ENGINE AND CHE CK WAS NORMAL. 2 L 7 3 4F 4 F A22WE E20EA 1996020200586 19960202 00586 NM 1996 2 2 9602286308 1 19960129 A 3350 CONNECTOR BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 668US 24223 DURING LINE CHECK (TPE), THE FLOOR PATH EMERGENCY LIGHTS BETWEEN SEAT ROWS 51R TO 59R WERE FOUND INOPERATIVE. RECONNECT ED LIGHT ASSEMBLY CONNECTOR AT ROW 59R. OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996020200588 19960202 00588 WP 1996 2 2 9602309609 1 19960130 A 3260 DNLOCK SWITCH DOUG DC9 DC932 3022066 WP NLG MALFUNCTIONED A NWAA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 01 609NW 47234 ON DESCENT INTO DSM, NOSE LANDING GEAR RED UNSAFE LIGHT DID NOT ILLUMINATE WHEN THROTTLES WERE BROUGHT TO IDLE. AFTER G EAR EXTENSION, NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE. COCKPIT MANUAL OPERATING PROCEDURES WERE PERFORMED AND CREW CO NFIRMED VISUALLY THROUGH PERISCOPE THAT THE NOSE GEAR WAS DOWN AND LOCKED. AIRCRAFT LANDED WITHOUT INCIDENT. NOTE: EM ERGENCY EQUIPMENT WAS CALLED STANDBY AS A PRECAUTION. REPLACED NOSE GEAR DOWNLOCK SWITCH. OPERATIONAL CHECK NORMAL. A IRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996020200589 19960202 00589 WP 1996 2 2 9602319874 1 19960125 A 5350 CLIPS DOUG DC9 DC951 3022051 WP TAILCONE OUT OF ADJUST A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 783NC 48108 DURING EO 5350-01032 TAILCONE FUNCTIONAL CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO BOTH PULL THE EXTERIOR HANDLE FROM THE CLIPS AS WELL AS TO DROP THE TAILCONE USING THE INTERIOR HANDLE. ADJUSTED THE CLIPS AND UPPER LATCHES. CHECK ED OK. 2 L 7 2 4F A6WE 1996020200590 19960202 00590 WP 1996 2 2 9602329851 1 19960126 A 5350 RELEASE MECH DOUG DC9 DC951 3022051 WP TAILCONE WORN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 47708 47708 DURING LINE MAINTENANCE, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR TAILCONE HANDLE AND THAT THE TAILC ONE DID NOT DROP. ALSO, FOUND WORN BEARING PLATES AND GUIDE PINS. REPLACED THE PLATES, PINS, AND UPPER RIGHT LATCH. R ERIGGED THE SYSTEM PER EO 5350-01049. CHECKED OK. 2 L 7 2 4F A6WE 1996020200591 19960202 00591 WP 1996 2 2 9602339957 1 19960127 A 5350 RELEASE MECH DOUG DC9 DC931 3022065 WP TAILCONE WORN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 915RW 47139 DURING LINE MAINTENANCE, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR TAILCONE HANDLE. ALSO, FOUND WORN BEARING PLATES AND GUIDE PINS. REPLACED THE PLATES AND PINS. CHECKED OK. 2 L 7 2 4F A6WE 1996020200592 19960202 00592 EU 1996 2 2 9602343221 1 19960130 A 3350 321430 BATTERY PACK AIRBUS 320 A320211 3930320 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 321US 262 DURING LINE MAINTENANCE, THE EMERGENCY LIGHTS FAILED TEST. FOUND LEFT BATTERY FAULT LIGHT ILLUMINATED (11WL). REPLACED BATTERY PACK AND RESET FUSES. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996020200593 19960202 00593 WP 1996 2 2 9602359957 1 19960130 A 2781 SWITCH DOUG DC9 DC931 3022065 WP LE FLAPS MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 915RW 47139 AFTER TAKEOFF AND DURING FLAP/SLAT RETRACTION, SLAT DISAGREEMENT LIGHT ILLUMINATED AND BLUE SLAT EXTEND LIGHT REMAINED O N. HANDLE FELT LIKE IT WAS BINDING IN THE RETRACT POSITION. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLA CED THE LEFT AND RIGHT SLAT RETRACT SWITCHES. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996020200595 19960202 00595 NM 1996 2 2 96FDEA00153 1 19960131 A 5610 WINDOW BOEING 727 727233 138408A NM RT COCKPIT LEAKING A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 258FE 20940 COPILOT WINDOW HAD LOUD WIND RUSH NOISE PASSING APPROX 4000 - 4500 FEET. LEVELED AT 5600 TO INSPECT. WINDOW APPEARED T O BE LEAKING EXCESSIVELY. RETURNED TO DFW. VERIFIED TORQUE. RESEALED AERODYNAMIC SEALANT IAW MM 56-11-0 AND MM SUPPLE MENT. APPLIED SPEED TAPE IAW E.A. 7-5610-26983. 2 L 7 3 4F RT A3WE 1996020200596 19960202 00596 NM 1996 2 2 96FDEA00154 1 19960125 A 5313 STRINGER BOEING 727 727227 1384078 NM FS 720 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 494FE 21532 FORWARD CARGO STA 720, STR 28R, HAS CORROSION ON STRINGER. REPLACED CORRODED STRINGER PER SRM 53-10-3 WITH NEW STRINGER , 3 FEET, AND SPLICE. 2 L 7 3 4F A3WE 1996020200597 19960202 00597 NM 1996 2 2 96FDEA00155 1 19960131 A 5330 M497209 SKIN BOEING 727 72722 1384002 NM BS 1083 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 DENT TO SKIN DUE TO TOOL BOX AT STA 1083 AND BETWEEN STR 28 - 29L. REPAIRED DAMAGED SKIN AT BS 1083, BETWEEN STR 28 - 2 9L PER FEDEX SRM 53-30-3 PER ENGINE REPAIR REQUEST REPLY. MFG PART NUMBER M502776. 2 L 7 3 4F A3WE 1996020200598 19960202 00598 NM 1996 2 2 96FDEA00156 1 19960131 A 5751 651926010 HINGE BOEING 727 72722 1384002 NM RT AILERION CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 RIGHT WING OUTBOARD AILERON INBOARD HINGE FITTING IS CORRODED (NR 2 HINGE FITTING). REMOVED CORROSION, FABRICATED REPAI R ANGLE ON FLANGE ON RIGHT WING OUTBOARD AILERON HINGE FITTING IAW FEDEX EA 7-5750-26969. 2 L 7 3 4F A3WE 1996020200599 19960202 00599 NM 1996 2 2 96FDEA00157 1 19960131 A 5754 RIB BOEING 727 72722 1384002 NM LE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 CORROSION ON NR 6 K-FLAP MOST OUTBOARD RIB WHERE LANDING LIGHT CONDUIT ATTACHES TO RIB UPPER BOLT HOLE. REMOVED CORROSI ON, REPAIRED PER EWO NR 96-2025. 2 L 7 3 4F A3WE 1996020200600 19960202 00600 NM 1996 2 2 96FDEA00158 1 19960201 A 5315 BAC14902865 FLOOR BEAM BOEING 727 72722 1384002 NM BS 312 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CORROSION ON FLOOR BEAM (C53-224-01 (1)) BS 312, WL 208 LBL 46. REMOVED CORROSION ON FLOOR BEAM AT BS 312, WL 208, LBL 46, OUT OF LIMITS PER FEDEX SRM 53-10-1. REPAIRED FLOOR BEAM PER FEDEX SRM 53-10-8. 2 L 7 3 4F A3WE 1996020200601 19960202 00601 NM 1996 2 2 96FDEA00159 1 19960201 A 5330 SKIN BOEING 727 72722 1384002 NM BS 411 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 EXTERIOR SKIN HAS A GOUGE IN THE SKIN AT BS 411, 3 INCHES BELOW STR 19R. REMOVED DAMAGE AT BS 411 BELOW STR 19R, FABRIC ATED FILLER AND DOUBLER DRILLED, DEBURRED, ALODINED, AND PRIMED, AND INSTALLED PER FEDEX SRM 53-30-3. 2 L 7 3 4F A3WE 1996020200602 19960202 00602 NM 1996 2 2 96FDEA00160 1 19960201 A 5330 SKIN BOEING 727 72722 1384002 NM BS 426 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 EXTERIOR SKIN, COUNTERSINK MISDRILLED AT FASTENER HEAD, BS 426, RBL 12.75 ON BOTTOM OF BELLY SKIN AT (RIGHT) FORWARD CO RNER OF DOOR CUT-OUT. REMOVED DAMAGED AREA AT BS 426, RBL 12.75 ON BOTTOM OF BELLY SKIN. FABRICATED AND INSTALLED SKIN DOUBLER PER FEDEX SRM 53-30-3. 2 L 7 3 4F A3WE 1996020200603 19960202 00603 NM 1996 2 2 96FDEA00161 1 19960201 A 5311 FRAME BOEING 727 72722 1384002 NM BS 440 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 DAMAGE TO FRAME AT BS 440, STR 2R. ORIGINAL MATERIAL THICKNESS WAS .055 INCH. MECHANICALLY BLENDED OUT GOUGE IN AN ARE A OF 1.25 INCH BY .50 INCH. REMOVED .010 INCH AND REMAINING THICKNESS WAS .045 INCH FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. CUT OUT DAMAGE AND DID REPAIR PER FEDEX SRM 53-10-4. 2 L 7 3 4F A3WE 1996020200604 19960202 00604 NM 1996 2 2 96FDEA00162 1 19960201 A 5754 65185338 HINGE FITTING BOEING 727 72722 1384002 NM NR 1 LE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 FIXED L/E FITTING FOR NR 1 K-FLAP CENTER LUG IS CORRODED. REPLACED CENTER HINGE FITTING WITH NEW. 2 L 7 3 4F A3WE 1996020200607 19960202 00607 WP 1996 2 2 ABXA9600110 1 19960129 A 3260 7000010101 SWITCH DOUG DC9 DC932 3022066 WP RT MLG DEFECTIVE A ABXA K NONE P NO WARNING INDICATION LD LANDING 1 GL 23 900AX 47380 NO GREEN LIGHT FOR RIGHT MAIN WHEN GEAR EXTENDED AT ILN, RECYCLED GEAR, CHANGED BULBS, NO GREEN, ALTERNATE GEAR SHOWS DO WN AND LOCKED. REPLACED RIGHT MAIN LANDING GEAR DOWNLOCK SWITCH. OPS CHECKS GOOD. 2 L 7 2 4F A6WE 1996020200608 19960202 00608 WP 1996 2 2 ABXA9600111 1 19960130 A 3350 5708458503 BATTERY PACK DOUG DC8 DC863 302198A WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 816AX 46093 DURING PRE-DEPARTURE CHECK, EMERGENCY LIGHT DISARM LIGHT ILLUMINATED WHEN THE EMERGENCY LIGHT SWITCH WAS ARMED. REPLACE D EMERGENCY LIGHT BATTERY PACK IAW DC8 MM, CHAPTER 33-50-1. OPS CHECK WAS GOOD. 2 L 7 4 4F 4A25 1996020200609 19960202 00609 WP 1996 2 2 ABXA9600112 1 19960130 A 3231 DOOR DOUG DC8 DC863 302198A WP RT MLG OUT OF ADJUST A ABXA K NONE J WARNING INDICATION CL CLIMB 1 GL 23 818AX 46075 AFTER LANDING GEAR WAS RETRACTED AND DURING THE UPLATCH CHECK, THE LANDING GEAR UNSAFE LIGHT ILLUMINATED AND THE RIGHT M AIN LANDING GEAR DOOR NOT LATCHED LIGHT ILLUMINATED. RECYCLED THE LANDING GEAR TWICE WITH NO CHANGE IN THE INDICATION. FOUND RIGHT MAIN LANDING GEAR DOOR OUT-OF-ADJUSTMENT. RIGGED THE RIGHT GEAR DOOR AND FOLLOW-UP MECHANISM PER DC8 MM, C HAPTER 32-31-5. OPS CHECK WAS GOOD. 2 L 7 4 4F 4A25 1996020200610 19960202 00610 SO 1996 2 2 COMA9610047 1 19960130 A 3230 RETRACT MECH EMB 120 EMB120RT SO NLG ICED UP A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 200CD 120200 NOSE LANDING, GEAR INTRANSIT LIGHTS REMAINED ON AFTER GEAR RETRACTION. REMOVED ICE FROM LANDING GEAR, RETRACT CHECKS NO RMAL, AND ACFT RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 1996020200611 19960202 00611 SO 1996 2 2 COMA9610048 1 19960131 A 2750 3075001017 FLAP CONTL UNIT EMB 120 EMB120RT SO TE FLAPS DEFECTIVE A COMA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 179CA 2264 120179 FLAP CONTROL FAULT WARNING WHEN FLAPS SELECTED TO 15 DEGREES. REPLACED THE FLAP CONTROL UNIT. PART TOTAL CYCLES, 10,65 8. 2 L 7 2 4T RT A31SO 1996020200612 19960202 00612 SO 1996 2 2 COMA9610049 1 19960131 A 5753 12018503614 SKIN EMB 120 EMB120RT SO RT TE FLAP DELAMINATED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 1117H 17531 31 120117 RIGHT INBOARD WING FLAP IS DELAMINATING ON THE TRAILING EDGE. REPAIRED FLAP. PART TOTAL CYCLES, 20,031. 2 L 7 2 4T RT A31SO 1996020200613 19960202 00613 SO 1996 2 2 COMA9610050 1 19960131 A 5280 AN4 BOLT EMB 120 EMB120RT SO LT MLG DOOR MISSING A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 130G 120130 LEFT MLG INTRANSIT INDICATOR REMAINED ON AFTER LANDING GEAR RETRACTED. REPLACED MISSING BOLT ON INBOARD FORWARD GEAR DO OR LATCH HANDLE. ACFT RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 1996020200614 19960202 00614 EU 1996 2 2 COMA9630027 1 19960130 A 6120 8542M2 COMPUTER SAAB SF340 SF340A 7850100 EU E/E COMPT FAILED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 356CA 8339 8213 340A034 AUTO-COARSEN SYSTEM FAILED DURING TAKEOFF. REPLACED THE AUTO-COARSEN COMPUTER. PART TOTAL CYCLES, 9,434. 2 L 7 2 4T RT A52EU 1996020200615 19960202 00615 NE 1996 2 2 MWEA96029 2 19960131 A 7200 ENGINE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7 52053 NE RIGHT FAILED A MWEA O OTHER J WARNING INDICATION CR CRUISE 1 GL 31 202ME 47672 667101 PILOT REPORTS OIL STRAINER CLOGGING LIGHT ILLUMINATED DURING FLIGHT. PULLED BACK POWER. LIGHT EXTINGUISHED. A/C DIVER TED TO DENVER AS PRECAUTION. CHANGED MAIN OIL FILTER. RAN ENGINE. FOUND METAL. ENGINE CHANGE SCHEDULED IN DEN 2/2/96 . 2 L 7 2 4F 4 F A6WE E2EA 1996020200616 19960202 00616 SO 1996 2 2 SWIA95711 1 19960130 A 2750 TRACKS EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT TE FLAP WORN A SWIA D RETURN TO BLOCK O OTHER TO TAKEOFF 1 NM 07 213SW 120277 AFTER TAKEOFF, FLAPS WOULD NOT RETRACT, RECEIVED FLAP DISAGREEMENT. REPLACED BOTH MOVEABLE FLAP TRACKS ON LEFT OUTBOARD FLAP. REPLACED FOUR TRACK ROLLERS. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1996020200617 19960202 00617 SW 1996 2 2 SWIA95712 1 19960130 A 2910 HYD LINE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP LT ENGINE FAILED A SWIA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 07 2702Z AC669 TOTAL HYDRAULIC FAILURE OVER SMO. REPLACED NR 6 FLEX LINE FOR LEFT ENGINE HYDRAULIC PRESSURE WITH PRE-FABRICATED STAINL ESS STEEL LINE. SERVICED RESERVOIR BLEED AIR FROM SYSTEM. RUN-UP AND LEAK CHECKS GOOD. 1 L 7 2 4T 4 T A8SW E4WE 1996020200618 19960202 00618 NM 1996 2 2 UPS205368 1 19960130 A 5313 STRINGER BOEING 727 72762C 138402C NM FS 740 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 912UP 19244 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, F.S. 740 STRINGER SKIN HAS CORROSION. REPAIRED I.A.W. DHC SK 912-788. 2 L 7 3 4F A3WE 1996020200619 19960202 00619 WP 1996 2 2 UPS805357 1 19960131 A 3260 DNLOCK SWITCH DOUG DC8 DC871F 302199D WP LT MLG DIRTY A IPXA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 755UP 46055 CREW REPORTED, LOWERED LANDING AT BDC AND DID NOT GET GREEN LIGHT FOR LEFT MLG. CYCLED GEAR, NO CHANGE. CHANGED BULBS, NO CHANGE. CYCLED GEAR AGAIN AND GOT NORMAL INDICATION. CLEANED GEAR DOWNLOCK SWITCH, CLEANED TERMINALS. 2 L 7 4 4F RT 4A25 1996020200620 19960202 00620 WP 1996 2 2 UPS805358 1 19960201 A 7331 MS2719824 FF TRANSMITTER DOUG DC8 DC873F 302199F WP NR 2 ENGINE DEFECTIVE A IPXA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 SO 01 807UP 46007 CREW REPORTED, NR 2 ENGINE INFLIGHT SHUT-DOWN - FLAMEOUT - TOP OF DESCENT FL 360, UNABLE TO RESTART. NR 2 ENG F/F TRANS MITTER SEAL DEFECTIVE. REPLACED SEAL. 2 L 7 4 4F RT 4A25 1996020200621 19960202 00621 WP 1996 2 2 UPS805359 1 19960201 A 3260 MS2719824 UPLATCH LIGHT DOUG DC8 DC873F 302199F WP LANDING GEAR DEFECTIVE A IPXA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 811UP 46089 CREW REPORTED DURING UPLATCH CHECK OBTAINED GEAR NOT LATCHED LIGHT. PERFORMED CHECKLIST AND CONTINUED FLIGHT. ACCOMPLI SHED E.O. DC8-3230-7910, A/C O.K. TO CONTINUE PER D-105486 BY MMOC FOR ONE FLIGHT ONLY TO SDF. 2 L 7 4 4F RT 4A25 1996020200624 19960202 00624 WP 1996 2 2 UPS805362 1 19960103 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FS 490-510 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, HEAVY CORROSION ON OUTBOARD SIDE OF LONGERON 31L F.S. 490 - 510. REPAIRED P ER UPS E.O. 2 L 7 4 4F RT 4A25 1996020200625 19960202 00625 WP 1996 2 2 UPS805363 1 19960102 A 5320 STIFFENER DOUG DC8 DC873F 302199F WP BS 280-290 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MODERATE CORROSION ON STIFFENER BETWEEN STA 280 - 290, LONGERON 31R. REPLACE D FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996020200626 19960202 00626 WP 1996 2 2 UPS805364 1 19960102 A 5320 ATTACH ANGLE DOUG DC8 DC873F 302199F WP FS 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON ATTACH ANGLE, F.S. 300, LONGERON 27R. REPLACED ANGLE PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996020200627 19960202 00627 WP 1996 2 2 UPS805365 1 19960102 A 5320 FITTING DOUG DC8 DC873F 302199F WP FS 330-360 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MODERATE CORROSION ON LONGERONS 36 AND 35 AND FITTINGS F.S. 330-360. REPAIRE D LONGERONS PER SRM 53-2-2, FIG. 10, AND REPLACED FITTINGS PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996020200628 19960202 00628 WP 1996 2 2 UPS805366 1 19960104 A 5320 FITTING DOUG DC8 DC873F 302199F WP FS 1220 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED B/T FITTING HEAVY CORROSION ON LONGERON 33R, F.S. 1220. REPLACED FITTING PER SRM 53-2-0. 2 L 7 4 4F RT 4A25 1996020200629 19960202 00629 WP 1996 2 2 UPS805367 1 19960109 A 5320 FITTING DOUG DC8 DC873F 302199F WP FS 1220 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MODERATE CORROSION ON B/T FITTING LONGERON 33R-34R, F.S. 1220. REPLACED FITT ING PER SRM 53-2-0. 2 L 7 4 4F RT 4A25 1996020900033 19960209 00033 NM 1996 2 9 96FDEA00145 1 19960202 A 5330 SKIN BOEING 727 72722 1384002 NM BS 339.5 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 EXTERIOR, SKIN HAS SHARP DENT AT BS 339.5, 2 INCHES BELOW STR 19R. REMOVED DAMAGED AREA ON SKIN, FABRICATED AND INSTALL ED THE FILLER AND DOUBLER PER FEDEX SRM 53-30-3. 2 L 7 3 4F A3WE 1996020900034 19960209 00034 NM 1996 2 9 96FDEA00163 1 19960128 A 5330 SKIN BOEING 727 72722 1384002 NM BS 255.5 MECH DAMAGE A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 193FE 19142 SKIN HAS TWO DRILL STARTS AT BS 255.5 WL 169 RT SIDE. FABRICATED SKIN DOUBLER PER FEDEX 53-30-1 AT BS 255.5 WL 169 RT S IDE. 2 L 7 3 4F A3WE 1996020900035 19960209 00035 NM 1996 2 9 96FDEA00164 1 19960129 A 5313 BAC1498140050 STRINGER BOEING 727 72722 1384002 NM BS 410 MISDRILLED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 TRAMCO RESPONSIBILITY 9601-59 WHILE WORKING NR0048 SKIN REPAIR MISDRILLED STR AT BS 410 STR 20R. REMOVED DAMAGED STR S ECTION BS 410 STR 20R, FABRICATED REPAIR PARTS AND INSTALLED PER FEDEX SRM 53-10-3. 2 L 7 3 4F A3WE 1996020900036 19960209 00036 NM 1996 2 9 96FDEA00165 1 19960129 A 5313 BAC1498132 STRINGER BOEING 727 72722 1384002 NM BS 590 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CORROSION (C53-111-01-2), ON STR 27L BS 590 WL 152. CUT OUT CORRODED AREA, FABRICATED AND INSTALLED REPAIR SPLICE AND S HIM AT BS 590 STR 27L WL 152 PER FEDEX SRM 53-10-3. 2 L 7 3 4F A3WE 1996020900037 19960209 00037 WP 1996 2 9 96FDEA00166 1 19960130 A 5511 SPAR CAP DOUG DC10 DC1010 3022110 WP LT HORIZ STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68051 47805 LT HORIZONTAL STABILIZER, UPPER FWD SPAR CAP AFT TANG HAS CRACK INDICATION IN FASTENER HOLE AT EXISTING FILLER LOCATION, THAT BEING THE O/B FASTENER. REPAIRED CRACK IN REFERENCE TO SRM 55-20-00 FIG 9 AND 10, PER EA 8-5510-27035A. 2 L 7 3 4F A22WE 1996020900038 19960209 00038 NM 1996 2 9 96FDEA00167 1 19960201 A 5320 FITTING BOEING 727 72722 1384002 NM BS 870 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 CRACK IN AFT FLANGE OF TERMINAL FITTING AT BS 870 STR 13R. HFEC DAMAGE FABRICATED REPAIR PARTS AND INSTALLED PER EWO NR 96-2-43. 2 L 7 3 4F A3WE 1996020900039 19960209 00039 NM 1996 2 9 96FDEA00168 1 19960201 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM BS 640 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CORROSION (C53-224-06), AROUND NUTPLATE HOLE ON LOWER SURFACE OF BS 640 FLOORBEAM RBL 19 WL 208. REPAIRED CORROSION ARO UND NUTPLATE HOLES ON LOWER SURFACE OF BS 640 FLOORBEAM RBL 19 WL 208 PER FEDEX SRM 53-10-8. 2 L 7 3 4F A3WE 1996020900040 19960209 00040 NM 1996 2 9 96FDEA00169 1 19960201 A 5320 65453136 STR CLIP BOEING 727 72722 1384002 NM BS 600 MECH DAMAGE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 MECH DAMAGE TO STR CLIP AT BS 600 STR 7R. REMOVED AND REPLACED STR CLIP AT BS 600 STR 7R. 2 L 7 3 4F A3WE 1996020900041 19960209 00041 NM 1996 2 9 96FDEA00170 1 19960201 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM BS 1030 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CORROSION (C53-224-01,3), AROUND NUTPLATE HOLE ON FLOORBEAM AT BS 1030 RBL 21 WL 208.1. REMOVED DAMAGED SECTION OF FLOO RBEAM OUT OF LIMITS PER FEDEX SRM 53-10-1. REPAIRED FLOORBEAM PER FEDEX SRM 53-10-8. 2 L 7 3 4F A3WE 1996020900042 19960209 00042 NM 1996 2 9 96FDEA00171 1 19960202 A 5320 FAIL-SAFE CHORD BOEING 727 72722 1384002 NM BS 804.5 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CRACK IN FAIL-SAFE CHORD BS 804.5 AT FASTENERS THROUGH STR 14L. CUT OUT DAMAGED, FABRICATED PART, DRILLED, DEBURRED, AL ODINED, PRIMED AND FASTENED INTO PLACE PER FEDEX SRM 51-40-3. 2 L 7 3 4F A3WE 1996020900043 19960209 00043 NM 1996 2 9 96FDEA00172 1 19960202 A 5330 SKIN BOEING 727 72722 1384002 NM BS 276 DAMAGED A FDEA K NONE C F.O.D. IN INSP/MAINT 1 SO 25 193FE 19142 EXTERIOR SKIN, 2 LIGHTNING STRIKES AT BS 276 ON CROWN SKIN LBL 11 AND 15. REPAIRED LIGHTNING STRIKE AT BS 276 LBL 11 IA W FEDEX SRM 53-30-3 FIG 20 PAR 2. REPAIRED LIGHTNING STRIKE AT BS 276 LBL 15 IAW FEDEX SRM 53-30-3 FIG 3. 2 L 7 3 4F A3WE 1996020900044 19960209 00044 NM 1996 2 9 96FDEA00173 1 19960202 A 5313 BAC1498132 STRINGER BOEING 727 72722 1384002 NM BS 445 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CRACK STR AND STR SPLICE AT BS 445 STR 23R. REMOVED CRACKED STR SPLICE AT BS 440 STR 23R, CUT OFF 10 INCHES OF CRACKED STR. REPLACED STR SPLICE, FABRICATED AND INSTALLED STR REPAIR PER FEDEX SRM 53-10-3 AT BS 445 STR 23R. 2 L 7 3 4F A3WE 1996020900045 19960209 00045 NM 1996 2 9 96FDEA00174 1 19960202 A 5320 CLIP BOEING 727 72722 1384002 NM BS 650-700 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CORROSION (C53-224-00), ON STR CLIP BS 650 TO 700 STR 7R. REMOVED CORROSION ON STR CLIP, FOUND TO BE OUT OF LIMITS. RE MOVED AND REPLACED STR CLIP, CORROSION ON STR WAS FOUND TO BE IN LIMITS PER FEDEX SRM 53-10-1. 2 L 7 3 4F A3WE 1996020900046 19960209 00046 NM 1996 2 9 96FDEA00175 1 19960202 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM BS 1030 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CORROSION AROUND NUTPLATE HOLE ON FLOORBEAM AT BS 1030 LBL 70.5 WL 208. CUT OUT DAMAGE ON FLOORBEAM, FABRICATED REPAIR ANGLES AND INSTALLED ALL WORK DONE PER FEDEX SRM 53-10-8. 2 L 7 3 4F A3WE 1996020900047 19960209 00047 NM 1996 2 9 96FDEA00176 1 19960202 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM BS 580 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 TRAMCO RESPONSIBILITY 9601-62, WHILE REMOVING SEAT TRACK NR 0381, DAMAGED FOUR HOLES IN TOP OF FLOORBEAM BS 580 BL 0 WL 208. REMOVED DAMAGED AREA, FOUR HOLES IN TOP OF FLOORBEAM BS 580 BL 0 WL 208, FABRICATED REPAIR PARTS, ALODINED, PRIMED AND INSTALLED PER FEDEX SRM 51-10-8. 2 L 7 3 4F A3WE 1996020900048 19960209 00048 NM 1996 2 9 96FDEA00177 1 19960202 A 5320 M165960 CLIP BOEING 727 72722 1384002 NM BS 328 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CRACKED STR CLIP AT BS 328 STR 19L. REMOVED CRACKED STR CLIP AT BS 328 STR 19L AND REPLACED WITH NEW ONE. 2 L 7 3 4F A3WE 1996020900049 19960209 00049 NM 1996 2 9 96FDEA00178 1 19960202 A 5315 BAC1505100617 FLOOR BEAM BOEING 727 72722 1384002 NM BS 560 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 TRAMCO RESPONSIBILITY 9601-61, WHILE REMOVING SEAT TRACK NR0381 DAMAGED TWO HOLES IN TOP OF FLOOR BEAM BS 560 BL 0 WL 20 8. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PARTS AND FASTENERS PER FEDEX SRM 53-10-8, BS 560 BL 0 WL 208. 2 L 7 3 4F A3WE 1996020900050 19960209 00050 NM 1996 2 9 96UAL900083 1 19960201 A 2410 7324284E IDG BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT ENGINE FAILED A UALA D RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 WP 29 647UA 25284 DURING TAXI OUT, THE RIGHT INTEGRATED DRIVE GENERATOR FAILED. AIRCRAFT RETURNED TO GATE. SUPPLEMENTAL DATA UPDATE: RI GHT INTEGRATED DRIVE GENERATOR REPLACED FOR FAILED DIODES. 2 L 7 2 4F 4 F RT A1NM E24NE 1996020900051 19960209 00051 1996 2 9 96UAL900084 4 19960201 A 2565 D31591462 SCHRADER VALVE BOEING 737 737522 138449F NM SLIDE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 948UA 26691 SLIDE REMOVED FOR TIME CONTROLLED OVERHAUL. SLIDE HAS SCHRADER VALVE SEPARATION FROM THE SLIDE MATERIAL. REINSTALLED T HE SCHRADER VALVE TO THE LATEST MODEL ASPIRATOR AND PATCHED THE SLIDE PER VENDOR MANUAL. 2 L 7 2 4F RT A16WE 1996020900052 19960209 00052 WP 1996 2 9 96UAL900085 1 19960201 A 2170 21D10011 COALESCER BAGS DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN DIRTY A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 1815U 46614 STRONG ODOR OF GLYCOL AFTER TAKEOFF. SUBMITTER SUGGEST, GLYCOL INJESTED IN PACKS DURING DE-ICING. REPLACED ALL 3 COALE SCER BAGS. 2 L 7 3 4F 4 F A22WE E23EA 1996020900053 19960209 00053 NE 1996 2 9 RRXA9600004 2 19960201 A 7420 IGNITION LEAD DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C1 13802 NE NR 4 ENGINE FAILED A RRXA O OTHER X ENGINE FLAMEOUT DE DESCENT 1 WP 15 8087U 45977 692350 FLT 28 - KDAY-KRDU, THE NR 4 ENGINE FLAMED-OUT AT THE TOP OF DECENT. THE ENGINE FLAME-OUT CHECKLIST WAS PERFORMED AND T HE ENGINE RESTARTED WITH IN 10 SEC. MAINTENANCE INSPECTED THE IGNITION SYSTEM AND FOUND THE A-SYSTEM IGNITION LEAD HAD SIGNS OF ARCING. 2 L 7 4 4F 4 F RT 4A25 E2GL 1996020900056 19960209 00056 NM 1996 2 9 96ZZZX565 1 19960109 A 2131 7638101 CONTROLLER BOEING 737 7373G7 1384595 NM CABIN FAILED A AWXA K NONE O OTHER CL CLIMB 1 WP 28 304AW 79J7158 24011 PHX/BUR - FLT 0484 - AUTOPRESSURE INOPERATIVE AT 280 FEET CABIN ALTITUDE AT 3,000 FEET, DIFFERENTIAL PRESSURE 8.4. REMO VED AND REPLACED REAR OUTFLOW VALVE. OPS CHECKED GOOD. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER. OPS CHECKED GO OD. REFERENCE CONTROL NR AWXA960011. 2 L 7 2 4F RT A16WE 1996020900057 19960209 00057 EU 1996 2 9 96ZZZX566 1 19960120 A 3234 SELECTOR VALVE AIRBUS 320 A320231 3930325 EU LANDING GEAR MALFUNCTIONED A AWXA K NONE J WARNING INDICATION DE DESCENT 1 WP 28 633AW CWDDR62489 082 LAS/ORD - FLT 0701 - WHEN LANDING GEAR SELECTED DOWN, GEAR DOORS AMBER, GEAR DID NOT EXTEND. CYCLED SELECTOR GEAR, GEAR DOWN NORMAL. NO FAULTS FOUND RECORDED ON L.G.C.I.U. BOTH L.G.C.I.U'S CHECK GOOD. REMOVED AND REPLACED NR 1 L.G.C.I.U . TO UPGRADE TO MOD 4B. INTERROGATED C.F.D.S. POST-FLIGHT FAULTS ON L.G.C.I.U., NR 1 AND NR 2. NO FAULTS FOUND. CHECK ED UPLOCK CIRCUIT CONTINUITY FROM SELECTOR TO L.G.C.I.U.'S. CHECKED GOOD. REMOVED AND REPLACED WING GEAR DOOR ACTUATOR PER 32-31-11. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE PER 32-31-12. FUNCTION CHECK GOOD. REFERENCE CONTROL NR AWXA960019. 2 L 7 2 4F RT A28NM 1996020900060 19960209 00060 NM 1996 2 9 96ZZZX569 1 19960128 A 2160 39606411 VALVE BOEING 737 737201 1384454 NM LT PACK MALFUNCTIONED A F3LA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 NM 03 212US 28949 1044 P2298 20212 DEN - FLT 233 - UPON ARRIVAL, FLIGHT CREW REPORTED THE LEFT PACK TEMPERATURE CONTROL WENT TO FULL HOT IN AUTOMATIC MODE CAUSING SMOKE IN THE CABIN. SMOKE DISSIPATED WHEN CONTROL WAS REPOSITIONED TO MANUAL. REPLACED THE LEFT PACK VALVE, AN D SYSTEM CHECKED OKAY. 2 L 7 2 4F A16WE 1996020900061 19960209 00061 NM 1996 2 9 96ZZZX570 1 19960129 A 2161 5483766 CONTROL MODULE BOEING 737 737201 1384454 NM CABIN FAILED A F3LA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 NM 03 212US 20212 MSP - FLT 417 - UPON ARRIVAL, FLIGHT CREW REPORTED AN ACRID ODOR AND SMOKE IN THE CABIN. ODOR AND SMOKE CLEARED WHEN LE FT PACK WAS TURNED OFF. MAINTENANCE REPLACED THE CABIN TEMPERATURE MODULE AND SYSTEM CHECKED OKAY. 2 L 7 2 4F A16WE 1996020900062 19960209 00062 NM 1996 2 9 96ZZZX571 1 19960121 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 922TS UA5194 20415 AFT ENTRY OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. (X) 2 L 7 3 4F A3WE 1996020900068 19960209 00068 NM 1996 2 9 AWXA960010 1 19960108 A 2131 7638101 PRESS CONTROLLER BOEING 737 737277 1384570 NM CABIN FAILED A AWXA A UNSCHED LANDING J O WARNING INDICATION OTHER CR CRUISE 1 WP 28 185AW 86112107 22652 FLT NR 780 - OMA/LAS - AIR TURN BACK, CREW REPORTS THAT THEY ARE NOT ABLE TO PRESSURIZE AIRCRAFT IN AUTO OR MANUAL MODE. AIRCRAFT MAINTENANCE FERRIED TO PHX STATION. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER. AIRCRAFT OPERATES NORMA LLY AT THIS TIME. (M) 2 L 7 2 4F RT A16WE 1996020900069 19960209 00069 NM 1996 2 9 AWXA960011 1 19960109 A 2133 7110033 OUTFLOW VALVE BOEING 737 7373G7 1384595 NM CABIN FAILED A AWXA K NONE O OTHER CL CLIMB 1 WP 28 304AW 152827 24011 PHX/BUR - FLT 0484 - AUTOPRESSURE INOPERATIVE AT 280 FEET CABIN ALTITUDE AT 3,000 FEET, DIFFERENTIAL PRESSURE 8.4. REMO VED AND REPLACED REAR OUTFLOW VALVE. OPS CHECKED GOOD. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER. OPS CHECKED GO OD. REFERENCE CONTROL NR 96ZZZX565. (X) 2 L 7 2 4F RT A16WE 1996020900070 19960209 00070 NM 1996 2 9 AWXA960012 1 19960109 A 3397 WIRE BOEING 737 7373S3 1384711 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 313AW 23712 PHX - FLT 0226 - DURING ROUTINE MAINTENANCE CHECK, FOUND INTERIOR EMERGENCY LIGHTING FOR AFT DOOR EXIT PATHWAYS INOPERAT IVE. REPAIRED AND REPINNED WIRE AT PIN 2. SYSTEM OPS CHECKED GOOD. (X) 2 L 7 2 4F RT A16WE 1996020900071 19960209 00071 NM 1996 2 9 AWXA960013 1 19960111 A 2612 FIRE DETECTOR BOEING 757 7572S7 1384962 NM CARGO COMPT DIRTY A AWXA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 28 901AW 23321 ATL/PHX - FLT 0610 - ABORTED TAKEOFF. CREW ABORTED TAKEOFF AT 135 KNOTS WHEN THE AFT CARGO FIRE WARNING WENT OFF WITH A SSOCIATED WARNING BELL. INSPECTED AFT PIT BAGGAGE PIT AND PERFORMED SYSTEM TEST OF CARGO WARNING FIRE DETECTION SYSTEM. FOUND DETECTORS AND DUCTS DIRTY. CLEANED DETECTORS AND DUCTS. (X) 2 L 7 2 4F RT A2NM 1996020900072 19960209 00072 NM 1996 2 9 AWXA960015 1 19960206 A 2612 894481 FIRE LOOP BOEING 737 7373G7 1384595 NM APU FAILED A AWXA F ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 WP 28 307AW 3634 24634 LAS - FLT NR 72 - APU SHUTDOWN WITH FIRE WARNING. CAPTAIN BLEW FIRE BOTTLE. FIRE WARNING CONTINUED. PULLED TUB, NO IN DICATION OF FIRE. SHOOK WIRES AT TAIL PIPE CONNECTINO. D982 FORWARD OF TAILPIPE FIRE WARNING WENT OFF. COLLARED APU F IRE DETECTION C/B. PLACED ON MEL 49-01, 26-07 AND 26-22. APU FIRE LOOP SHORTED. PLACED ON MEL 26-08. CLEARED MEL 26- 07 ON 3/10. REMOVED AND REPLACED FIRE BOTTLE. CLEARED MEL 26-08 ON 3/8. REMOVED AND REPLACED FORWARD LOOP. CLEARED M EL 49-01 ON 3/8. APU OPS NORMAL AFTER R/R OF FORWARD LOOP. MEL 26-22 WAS ENTERED IN ERROR. (M) 2 L 7 2 4F RT A16WE 1996020900073 19960209 00073 NM 1996 2 9 AWXA960016 1 19960118 A 5315 BAC150510067 FLOORBEAM BOEING 737 737277 1384570 NM BS 987 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 PAE - FLT 3887 - DURING C-9 INSPECTION, FOUND CORROSION ON BS 987 UPPER CHORD OF FLOORBEAM WL 208, RBL 45 TO RBL 50. RE MOVED CORRODED UPPER CHORD OF BS 987 FROM LBL 27 TO LBL 53, WL 208. FABRICATED NEW UPPER CHORD. SPLICE ANGLES AND FILL ERS PER SRM 53-10-09. ANODIZED, PRIMED, AND INSTALLED REPAIR PARTS. (X) 2 L 7 2 4F RT A16WE 1996020900074 19960209 00074 EU 1996 2 9 AWXA960019 1 19960120 A 3232 ACTUATOR AIRBUS 320 A320231 3930325 EU WING GEAR DOOR MALFUNCTIONED A AWXA O OTHER J WARNING INDICATION DE DESCENT 1 WP 28 633AW 488 082 LAS/ORD - FLT 0701 - WHEN LANDING GEAR SELECTED DOWN, GEAR DOORS AMBER, GEAR DID NOT EXTEND. CYCLED SELECTOR GEAR, GEAR DOWN NORMAL. NO FAULTS FOUND RECORDED ON L.G.C.I.U. BOTH L.G.C.I.U'S CHECK GOOD. REMOVED AND REPLACED NR 1 L.G.C.I.U . TO UPGRADE TO MOD 4B. INTERROGATED C.F.D.S. POST-FLIGHT FAULTS ON L.G.C.I.U., NR 1 AND NR 2. NO FAULTS FOUND. CHECK ED UPLOCK CIRCUIT CONTINUITY FROM SELECTOR TO L.G.C.I.U.'S. CHECKED GOOD. REMOVED AND REPLACED WING GEAR DOOR ACTUATOR PER 32-31-11. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE PER 32-31-12. FUNCTION CHECK GOOD. REFERENCE OPERATOR CONTROL NR 96ZZZX566. (X) 2 L 7 2 4F RT A28NM 1996020900075 19960209 00075 NM 1996 2 9 AWXA96008 1 19960107 A 3350 1012623 LIGHT BOEING 737 7373G7 1384595 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 160AW 23782 PHX - FLT 0160 - DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 8, A, B, C, EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EM ERGENCY LIGHT ON SEAT 8L. SYSTEM OPS CHECKED GOOD. STC SA3432NM. (X) 2 L 7 2 4F RT A16WE 1996020900076 19960209 00076 NM 1996 2 9 AWXA96009 1 19960108 A 3397 WIRE BOEING 737 73733A 1384673 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 164AW 23625 PHX - FLT 0536 - DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 3 SEAT EMERGENCY LIGHT INOPERATIVE. REPAIRED WIRING AS NEE DED. STC BOEING STANDARD. (X) 2 L 7 2 4F RT A16WE 1996020900078 19960209 00078 NM 1996 2 9 CAL960003 1 19960104 A 3260 CIRCUIT BREAKER BOEING 737 7373T0 1384582 NM NLG IND SYSTEM TRIPPED A CALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SW 09 14336 23574 CLE - FLT 1108 - WHEN LANDING GEAR WAS EXTENDED ON APPROACH TO CLE, THE NOSE GEAR INDICATED UNSAFE AND THE MAIN GEAR HAD NO INDICATION. CHECK LIST PROCEDURES WERE FOLLOWED AND DURING A TOWER FLYBY, THE AIR/GROUND RELAY CIRCUIT BREAKER WAS OBSERVED TO BE TRIPPED. THE CIRCUIT BREAKER WAS RESET AND ALL INDICATIONS WERE NORMAL. THE AIRCRAFT LANDED WITHOUT INC IDENT. MAINTENANCE PINNED THE GEAR AND CYCLED THE GEAR HANDLE SEVERAL TIMES WITH NORMAL INDICATIONS. THE CIRCUIT BREAK ER REMAINED SET. IN ADDITION, THE E-11 SHELF WAS INSPECTED AND NO DISCREPANCIES WERE FOUND. (X) 2 L 7 2 4F RT A16WE 1996020900079 19960209 00079 WP 1996 2 9 CAL960007 1 19960109 A 2612 FIRE LOOP DOUG DC9 DC983 3022083 WP NR 1 ENGINE INOPERATIVE A CALA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING DE DESCENT 1 SW 09 938MC 49525 IAH - FLT 1949 - THE NR 1 ENGINE FIRE WARNING LIGHT AND BELL ACTIVATED WHILE ON DESCENT INTO IAH. THE NR 1 ENGINE WAS S HUT DOWN, BOTH FIRE BOTTLES WERE DISCHARGED, AND THE FIRE WARNING CEASED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTE NANCE FOUND NO EVIDENCE OF FIRE. TROUBLESHOOTING FOUND THE NR 1 ENGINE UPPER BARRIER FIRE LOOP CONNECTOR AT FAULT. THE CONNECTOR WAS REMOVED AND REPLACED. THE FIRE DETECTION SYSTEM CHECKED GOOD. IN ADDITION, BOTH FIRE BOTTLES WERE REMOV ED AND REPLACED. (X) 2 L 7 2 4F RT A6WE 1996020900080 19960209 00080 WP 1996 2 9 CAL960033 1 19960116 A 5730 SKIN DOUG DC9 DC982 3022082 WP WS 242 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12811 35042 49265 IAH - FLT 1707 - INSPECTION FOUND A 5.25 INCH CRACK IN LEFT WING LEADING EDGE SKIN AT STA 242. A DOUBLER REPAIR WAS INS TALLED IAW ECRA 5730-01428. (X) 2 L 7 2 4F A6WE 1996020900081 19960209 00081 NM 1996 2 9 CAL960043 1 19960108 A 5344 65575342 FITTING BOEING 727 727224 1384076 NM R-2 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 66099 20655 IAH - INSPECTION FOUND A 1.5 INCH CRACK IN R-2 DOOR UPPER HINGE FITTING. THE FITTING WAS REMOVED AND REPLACED IAW SRM 5 1-10-1. (X) 2 L 7 3 4F A3WE 1996020900082 19960209 00082 NM 1996 2 9 EIAA9601 1 19960122 A 3244 26156114 TIRE BOEING 747 747273C 1384896 NM NR 9 FAILED A EIAA C D ABORTED TAKEOFF RETURN TO BLOCK E VIBRATION/BUFFET TO TAKEOFF 1 NM 09 470EV 20653 LAX - LOG PAGE F00612 - ON TAKEOFF ROLL, FELT SEVERE VIBRATION THROUGH AIRFRAME, ABORTED TAKEOFF, NR 9 TIRE BLOWN ON TAK EOFF. REPLACED NR 9 TIRE PER MM 32-41-15, PERFORMED AXLE INSPECTION PER MM 32-41-15, PERFORMED 'TIRE TREAD LOSS' INSPEC TION PER MM 5-51-34 AND 'HIGH ENERGY STOP' INSPECTION PER MM 5-51-01. (X) 2 L 7 4 4F A20WE 1996020900084 19960209 00084 NM 1996 2 9 IXKA960002 1 19960103 A 2197 WIRE BOEING 727 727224 1384076 NM LT PACK FAILED A IXKA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 25 32719 20388 ATL/TPA - FLT 17 - DURING CLIMB-OUT, UNABLE TO CONTROL CABIN PRESSURIZATION. AIRCRAFT RETURNED TO ATL DUE ONE PACK OUT. FOUND WIRES BAD ON 210 DEGREE SENSOR BULB WHICH CAUSED PACK TEMP OVERHEAT LIGHT AND TRIPPED OFF LEFT PACK. REPAIRED W IRES AND PERFORMED PRESSURIZATION AND OPS CHECK OK PER MM 21-30-0. (X) 2 L 7 3 4F A3WE 1996020900085 19960209 00085 NM 1996 2 9 TAOA19601 1 19960115 A 3350 900835A BATTERY PACK BOEING 727 727294 1384088 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 921TS 8585 22043 AFT FUSELAGE EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. (X) 0 4 A3WE 1996020900086 19960209 00086 NM 1996 2 9 TWRA9602 1 19960110 A 2530 812020401 COFFEE MAKER BOEING 747 747121 1384871 NM GALLEY FAILED A TWRA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 604FF 19659 JFK/LAX - DURING FLIGHT, MID-GALLEY COFFEE MAKER TRIPPED CIRCUIT BREAKER. WHEN CIRCUIT BREAKER WAS RESET, A STRONG ODOR OF ELECTRICAL SMOKE WAS NOTICED FOLLOWED BY VISUAL SMOKE. THE GALLEY WAS ISOLATED BY SHUTTING OFF GALLEY POWER. THE G ALLEY WAS PLACARDED, 'DO NOT USE' AND CIRCUIT BREAKER COLLARED. ELECTRICAL WIRING WAS CHECKED, NO FAULT WAS FOUND. ALL CANNON PLUGS WERE CHECKED FOR SECURITY, ALL OK. COFFEE MAKER WAS SENT TO VENDOR FOR REPAIR. (X) 2 L 7 4 4F A20WE 1996020900088 19960209 00088 NE 1996 2 9 TWRA9605 2 19960116 A 7230 COMPRESSOR BOEING 747 747121 1384871 NM PWA JT9 JT9D7A 52054 NE NR 3 ENGINE STALLED A A TWRA A E UNSCHED LANDING ENGINE SHUTDOWN E VIBRATION/BUFFET CL CLIMB 1 EA 15 613FF 19647 662962 GYC - DURING CLIMB AT FL 270, NR 3 ENGINE HAD A COMPRESSOR STALL (LOUD BANG) AND EGT WENT TO 1,000 DEGREES FOR 8 SECONDS . ENGINE WAS SHUT DOWN IAW CHECK LIST. UPON LANDING, MAINTENANCE FOUND METAL IN THE TAILPIPE. AIRCRAFT WAS SET UP FOR 3-ENGINE FERRY PER GMM 3-25-3-26. ENGINE REPLACED. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 4 4F 4 F A20WE E20EA 1996020900127 19960209 00127 WP 1996 2 9 9602379605 1 19960126 A 5320 FITTING DOUG DC9 DC932 3022066 WP FS 718 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 605NW 47223 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE KEEL WEB TO FLOORBEAM ATTACH FITTING AT FS 718. REPL ACED FITTING PER SRM 51-01. 2 L 7 2 4F A6WE 1996020900128 19960209 00128 WP 1996 2 9 9602389606 1 19960126 A 5320 FITTING DOUG DC9 DC932 3022066 WP FS 1095 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 606NW 47225 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE LONGERON 5L TO FS 1095 FRAME ATTACH FITTING. REPLACE D FITTING PER SRM 51-01. 2 L 7 2 4F A6WE 1996020900129 19960209 00129 WP 1996 2 9 9602391150 1 19960126 A 5320 FITTING DOUG DC10 DC1040 3023508 WP FS 1513-1517 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 150US 46759 DURING L-CHECK, FOUND CORROSION ON THE LONGITUDINAL FITTING AT FS 1513 TO 1517, LBL 29 IN THE CENTER LANDING GEAR WHEEL WELL AFT SHELF. REPLACED FITTING PER SRM 51-00-00 PG 2. 2 L 7 3 4F A22WE 1996020900130 19960209 00130 WP 1996 2 9 9602409970 1 19960127 A 5712 RIB DOUG DC9 DC931 3022065 WP WS 69 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9334 47247 DURING M-CHECK, FOUND A CRACK IN THE LEFT WING FUEL TANK RIB TO LOWER WING ATTACH FITTING, XRS 69 AT STR 11. REPLACED F ITTING PER SRM 51-30-2. 2 L 7 2 4F A6WE 1996020900131 19960209 00131 WP 1996 2 9 9602419871 1 19960129 A 5320 FITTING DOUG DC9 DC951 3022051 WP FS 1167 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 780NC 48102 DURING H-CHECK, FOUND CORROSION ON BOTH THE LEFT AND RIGHT FS 1167 FLOORBEAM TO FRAME ATTACH FITTINGS. REPLACED BOTH FI TTINGS. 2 L 7 2 4F A6WE 1996020900132 19960209 00132 WP 1996 2 9 9602429871 1 19960129 A 5743 FITTING DOUG DC9 DC951 3022051 WP MLG CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 780NC 48102 DURING H-CHECK, FOUND CORROSION ON THE RIGHT MAIN LANDING GEAR FITTING SIDE BRACE ATTACH LUGS. REPLACED FITTING PER CIT EXT 09-5740-1-0007. 2 L 7 2 4F A6WE 1996020900133 19960209 00133 WP 1996 2 9 9602439605 1 19960129 A 5320 FITTING DOUG DC9 DC932 3022066 WP FS 744-756 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 605NW 47223 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE KEEL WEB ATTACH FITTING FS 744 TO 756, IN THE LOWER I NBOARD AFT CORNER OF THE LEFT MAIN LANDING GEAR WHEEL WELL. REPLACED FITTING PER SRM 51-01. 2 L 7 2 4F A6WE 1996020900134 19960209 00134 NM 1996 2 9 9602446730 1 19960130 A 5230 FITTING BOEING 747 7472J9F 1384806 NM CARGO DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 630US 21668 DURING P-CHECK, FOUND A CRACK IN THE AFT CARGO DOOR LATCH HOOK FITTING, LOWER FORWARD CORNER. REPLACED FITTING. 2 L 7 4 4F RT A20WE 1996020900135 19960209 00135 NM 1996 2 9 9602456730 1 19960130 A 5320 FITTING BOEING 747 7472J9F 1384806 NM EE DOOR HINGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 630US 21668 DURING P-CHECK, FOUND CORROSION ON THE FITTINGS BELOW BOTH THE FORWARD AND AFT E/E DOOR HINGES. REPLACED BOTH FITTINGS PER SRM 51-30-5. 2 L 7 4 4F RT A20WE 1996020900136 19960209 00136 WP 1996 2 9 9602469871 1 19960130 A 5744 FITTING DOUG DC9 DC951 3022051 WP RT TE FLAP BROKEN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 780NC 48102 DURING H-CHECK, FOUND THAT THE RIGHT WING FLAP FITTING INSIDE PANEL 1647A IS BROKEN AND HAS A ROW OF SHEARED FASTENERS. REPLACED FITTING PER SRM 51-30-1. 2 L 7 2 4F A6WE 1996020900137 19960209 00137 WP 1996 2 9 9602479606 1 19960130 A 5343 FITTING DOUG DC9 DC932 3022066 WP FS 756 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 606NW 47225 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN BOTH THE LEFT AND RIGHT MAIN LANDING GEAR WHEEL WELL FI TTINGS AT FS 756, LONGERON 30. REPLACED FITTINGS PER SRM 51-30-5 AND 51-01. 2 L 7 2 4F A6WE 1996020900138 19960209 00138 WP 1996 2 9 9602489944 1 19960130 A 5320 FITTING DOUG DC9 DC931 3022065 WP FS 150 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 1309T 47316 DURING SVI CHECK, FOUND CORROSION ON THE CUSP FITTING AT FS 150, LONGERON 18R. REPLACED FITTING PER SRM 51-30-1, -2. 2 L 7 2 4F A6WE 1996020900139 19960209 00139 WP 1996 2 9 9602499606 1 19960131 A 5320 FITTING DOUG DC9 DC932 3022066 WP FS 1095 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 606NW 47225 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE FS 1095 FRAME TO LONGERON 25L ATTACH FITTING. REPLAC ED FITTING PER SRM 51-01 AND 51-30-5. 2 L 7 2 4F A6WE 1996020900140 19960209 00140 WP 1996 2 9 9602509753 1 19960201 A 3231 UPLATCH ROLLER DOUG DC9 DC941 302207N WP RT MLG DOOR FROZEN A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 753NW 47117 DURING DEPARTURE CLIMB UPON LANDING GEAR RETRACTION, GEAR DOOR INDICATION REMAINED ILLUMINATED. RECYCLED GEAR PER MAINT ENANCE CONTROL, INDICATION CEASED. DTW MAINTENANCE FOUND THE RIGHT GEAR DOOR UPLATCH ROLLER FROZEN. FREED UPLATCH ROLL ER AND LUBRICATED, OPERATIONAL CHECK WAS NORMAL. 2 L 7 2 4F A6WE 1996020900141 19960209 00141 WP 1996 2 9 9602519750 1 19960201 A 3222 STRUT DOUG DC9 DC941 302207N WP NLG REQD SERVICE A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 750NW 47114 DURING CLIMB, THE AIRCRAFT DID NOT SHIFT INTO FLIGHT MODE. UTILIZED OVERRIDE BUTTON TO RETRACT LANDING GEAR. AFTER LAN DING GEAR RETRACTION, THE NOSE GEAR DOORS DID NOT CLOSE AND THE NOSE LANDING GEAR UNSAFE LIGHT ILLUMINATED. AIRCRAFT RE TURNED TO DTW AND LANDED WITHOUT INCIDENT. SERVICED STRUT ON NOSE LANDING GEAR AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996020900142 19960209 00142 WP 1996 2 9 9602529139 1 19960201 A 3260 SI288 SWITCH DOUG DC9 DC914 3022034 WP RT MLG DOOR FAILED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 948L 47049 DURING APPROACH, THE RIGHT MAIN LANDING GEAR DOOR OPEN LIGHT ILLUMINATED AFTER LANDING GEAR EXTENSION. PERFORMED COCKPI T OPERATING MANUAL PROCEDURES AND PERFORMED EMERGENCY LANDING GEAR EXTENSION. AIRCRAFT LANDED WITHOUT INCIDENT. REPLAC ED THE RIGHT MAIN LANDING GEAR DOOR POSITION SWITCH AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996020900143 19960209 00143 1996 2 9 9602539103 4 19960202 A 3421 258733511 VERTICAL GYRO DOUG DC9 DC915 3022036 WP FUSELAGE MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 93S 21608 3294 47078 DURING CLIMB, THE VERTICAL GYRO FLAG APPEARED. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED THE NR 2 VERTICAL GYRO AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996020900144 19960209 00144 NM 1996 2 9 9602546626 1 19960131 A 3234 GEAR HANDLE BOEING 747 747251B 1384892 NM COCKPIT LACK OF LUBE A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 626US 21708 DURING APPROACH, THE LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER LANDING GEAR EXTENSION. EXECUTED GO-AROUND AN D RECYCLED THE LANDING GEAR AND THE LIGHT EXTINGUISHED. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND LANDING GEAR CONTROL H ANDLE STICKING. LUBRICATED LANDING GEAR CONTROL HANDLE, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996020900145 19960209 00145 NM 1996 2 9 9602552286 1 19960127 A 3350 POWER SUPPLY BOEING 727 727251 138408H NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 286US 21325 DURING PREFLIGHT, FOUND THE EMERGENCY LIGHT AT DOOR 2R INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY PACK, CHECKED OK. 2 L 7 3 4F A3WE 1996020900146 19960209 00146 NM 1996 2 9 9602562298 1 19960125 A 3350 POWER SUPPLY BOEING 727 727251 138408H NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 298US 22152 DURING PREFLIGHT, FOUND AFT SECTION OF FLOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY PACK, CHEC KED OK. 2 L 7 3 4F A3WE 1996020900147 19960209 00147 NM 1996 2 9 9602572286 1 19960201 A 3350 BATTERY PACK BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 286US 21325 DURING PREFLIGHT, FOUND FORWARD SECTION OF EMERGENCY LIGHT TRACK INOPERATIVE. REPLACED BATTERY PACK AND CHECKED OK. 2 L 7 3 4F A3WE 1996020900148 19960209 00148 NM 1996 2 9 9602582298 1 19960129 A 3231 RETRACT MECH BOEING 727 727251 138408H NM RT MLG DOOR MALFUNCTIONED A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 298US 22152 DURING CLIMB AND LANDING GEAR RETRACTION, THE RIGHT MAIN GEAR DOOR DID NOT FULLY CLOSE. LANDING GEAR RECYCLED AND ALL I NDICATIONS WERE NORMAL. AIRCRAFT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. PERFORMED LANDING GEAR DOOR FUNCTIONAL CHECK AND SYSTEM CHECKED OK. 2 L 7 3 4F A3WE 1996020900149 19960209 00149 NM 1996 2 9 9602592298 1 19960127 A 3350 SIGN BOEING 727 727251 138408H NM CABIN SHORTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 298US 22152 DURING PREFLIGHT, FOUND LAST SECTION OF FLOOR EMERGENCY LIGHTS INOPERATIVE. ALSO, FOUND RIGHT AFT DOOR EMERGENCY EXIT S IGN SHORTING. REPLACED SIGN WITH A SERVICEABLE UNIT, CHECKED OK. 2 L 7 3 4F A3WE 1996020900150 19960209 00150 NM 1996 2 9 9602602202 1 19960127 A 3350 BATTERY PACK BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 202US 22155 DURING PREFLIGHT, FOUND THE RIGHT OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED THE BATTERY CHARGER AND BATTERY PACK. 2 L 7 3 4F A3WE 1996020900151 19960209 00151 NM 1996 2 9 9602612704 1 19960201 A 3350 BATTERY BOEING 727 727225 1384077 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 801EA 22432 DURING PREFLIGHT, FOUND AFT SECTION OF FLOOR PATH EMERGENCY LIGHTING INOPERATIVE. REPLACED BATTERY AND CHECKED OK. 2 L 7 3 4F A3WE 1996020900152 19960209 00152 NM 1996 2 9 9602622705 1 19960202 A 3350 BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 802EA 22433 DURING PREFLIGHT, FOUND AFT ENTRY EXIT EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AND CHECKED OK. 2 L 7 3 4F A3WE 1996020900153 19960209 00153 NM 1996 2 9 9602632298 1 19960130 A 3350 BATTERY PACK BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 298US 22152 DURING PREFLIGHT, FOUND AFT SECTION OF FLOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND CHECKED OK. 2 L 7 3 4F A3WE 1996020900154 19960209 00154 WP 1996 2 9 9602649988 1 19960127 A 7711 EPR INDICATOR DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9A 52048 NE NR 1 ENGINE ERRATIC A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 8944E 47167 666297 THE NR 1 ENGINE EPR INDICATION WAS ERRATIC ON TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. M AINTENANCE REPLACED THE INDICATOR WITH A SERVICEABLE UNIT. 2 L 7 2 4F 4 F A6WE E2EA 1996020900155 19960209 00155 WP 1996 2 9 9602659305 1 19960201 A 7711 PT7 LINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE NR 2 ENGINE MOISTURE CONTAM A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 307RC 48086 708425 THE NR 2 ENGINE EPR INOPERATIVE ON TAKEOFF. ABORTED TAKEOFF AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE CLEARED MOISTURE FROM THE PT7 LINE. SYSTEM OPERATION RETURNED TO NORMAL. 2 L 7 2 4F 4 F A6WE E9NE 1996020900156 19960209 00156 WP 1996 2 9 9602669990 1 19960128 A 7711 EPR INDICATOR DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9 52048 NE NR 2 ENGINE FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 8950E 47186 657252 THE NR 2 ENGINE EPR INDICATION UNRELIABLE ON TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. M AINTENANCE REPLACED THE EPR INDICATOR WITH A SERVICEABLE UNIT. 2 L 7 2 4F 4 F A6WE E2EA 1996020900157 19960209 00157 WP 1996 2 9 9602679607 1 19960201 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 607NW 47232 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS IN FIRST CLASS SECTION AND AT GALLEY SERVICE DOOR INOPERATIVE. REPLACED BATTERIES AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996020900158 19960209 00158 WP 1996 2 9 9602689983 1 19960201 A 3350 6011779 BATTERY PACK DOUG DC9 DC932 3022066 WP RT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 983US 47282 DURING LINE MAINTENANCE INSPECTION, FOUND THE RIGHT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AND OPER ATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996020900159 19960209 00159 1996 2 9 9602699902 4 19960201 A 2565 13621224 SLIDE DOUG DC9 DC931 3022065 WP TAIL SECTION LOW PRESSURE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 952N 27673 287 47073 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL EVACUATION SLIDE LOW ON PRESSURE. REPLACED SLIDE. 2 L 7 2 4F A6WE 1996020900160 19960209 00160 WP 1996 2 9 9602709913 1 19960201 A 3222 5910448 STRUT DOUG DC9 DC931 3022065 WP NLG REQD SERVICE A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 963N 47415 AIRCRAFT FAILED TO SHIFT FROM GROUND MODE TO FLIGHT MODE AFTER TAKEOFF. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCID ENT. INSPECTED GROUND SHIFT MECHANISM AND NO PROBLEMS WERE FOUND. RESERVICED NOSE LANDING GEAR STRUT TO PROPER LEVELS. OPERATIONAL CHECK NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996020900161 19960209 00161 WP 1996 2 9 9602719859 1 19960201 A 5350 CLIPS DOUG DC9 DC951 3022051 WP TAILCONE OUT OF ADJUST A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 768NC 47729 DURING EO 5350-01032 TAILCONE FUNCTION CHECK, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO PULL THE EXTERIOR TAILCONE HAN DLE FROM THE CLIPS. ADJUSTED THE CLIPS AND CHECKED OK. 2 L 7 2 4F A6WE 1996020900162 19960209 00162 WP 1996 2 9 9602729755 1 19960201 A 3240 SPIN BRAKES DOUG DC9 DC941 302207N WP NOSE GEAR INOPERATIVE A NWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 01 755NW 47179 AFTER TAKEOFF AND GEAR RETRACTION MSP-YEG, EXPERIENCED VIBRATION. UPLATCH CHECK AND GEAR DOOR INDICATION LIGHTS ALL OK. RETURNED TO MSP WITHOUT FURTHER INCIDENT. FOUND THE NOSE GEAR SPIN BRAKES INOPERATIVE. REPLACED BRAKES. ALSO, FOUND THE E/E COMPARTMENT DOOR LOOSE. ADJUSTED LATCH. NO OTHER DISCREPANCIES WERE NOTED. 2 L 7 2 4F A6WE 1996020900163 19960209 00163 WP 1996 2 9 9602739865 1 19960201 A 3260 SENSOR DOUG DC9 DC951 3022051 WP NOSE GEAR INOPERATIVE A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 774NC 47776 AFTER TAKEOFF, FOUND THAT THE NOSE GEAR UNSAFE LIGHT DID NOT EXTINGUISH. CYCLED THE GEAR, NO HELP. FOLLOWED THE COCKPI T OPERATING MANUAL AND RETURNED TO MSP WITHOUT FURTHER INCIDENT. GEAR INDICATIONS NORMAL FOR LANDING, BUT CALLED OUT EM ERGENCY EQUIPMENT AS A PRECAUTIONARY MEASURE. REPLACED THE NOSE GEAR PROXIMITY SENSOR, ADJUSTED THE GAP AND GEAR SWING CHECKED OK. 2 L 7 2 4F A6WE 1996020900164 19960209 00164 WP 1996 2 9 9602749865 1 19960201 A 3260 SENSOR DOUG DC9 DC951 3022051 WP NLG OUT OF ADJUST A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 774NC 47776 AFTER TAKEOFF, FOUND THAT THE NOSE GEAR UNSAFE LIGHT DID NOT EXTINGUISH. ACFT RETURNED TO MSP WITHOUT FURTHER INCIDENT. ADJUSTED THE NOSE GEAR WARNING SWITCH AND SWUNG THE GEAR SEVERAL TIMES PER MM 32-60-01 PG 208, CHECKED OK. 2 L 7 2 4F A6WE 1996020900165 19960209 00165 NM 1996 2 9 9602756307 1 19960201 A 3350 LIGHTS BOEING 747 747451 1384940 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 667US 24222 DURING LINE CHECK, THE FLOOR MOUNTED EMERGENCY PATH LIGHTS AT DOOR 2L AND SEAT ROW 21L WERE FOUND INOPERATIVE. REPLACED THE FLOOR MOUNTED EMERGENCY LIGHT ASSEMBLY AT ROW 21L AND OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996020900166 19960209 00166 NM 1996 2 9 9602766309 1 19960201 A 3350 CONNECTOR BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 669US 24224 DURING LINE CHECK, THE AFT CABIN FLOOR MOUNTED EMERGENCY LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRE AT SEAT ROW 65 L AND OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996020900167 19960209 00167 NE 1996 2 9 9602776612 2 19960201 A 7320 FUEL CONTROL BOEING 747 747251B 1384892 NM PWA JT9 JT9D7F 52054 NE NR 1 ENGINE FROZE UP A A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 612US 20357 62678 CREW ABORTED TAKEOFF DUE TO NR 1 ENGINE UNABLE TO REACH TAKEOFF POWER. MAINTENANCE APPLIED HEAT TO THE FUEL CONTROL PS4 LINE AND ALL INDICATIONS WERE NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4 F A20WE E20EA 1996020900169 19960209 00169 NM 1996 2 9 9602795523 1 19960201 A 2410 IDG BOEING 757 757251 1384970 NM RT ENGINE REQD SERVICE A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 GL 01 523US 23617 DURING START OF TAKEOFF ROLL, LOST RIGHT GENERATOR. ABORTED TAKEOFF AND CLEARED RUNWAY. CREW RESET RIGHT GENERATOR AND FLIGHT DEPARTED WITHOUT FURTHER INCIDENT. DTW MAINTENANCE SERVICED RIGHT IDG. 2 L 7 2 4F RT A2NM 1996020900170 19960209 00170 1996 2 9 9602801146 4 19960204 A 3418 STALL TRANSDUCER DOUG DC10 DC1040 3023508 WP NR 1 MALFUNCTIONED A NWAA A J UNSCHED LANDING DUMP FUEL N FALSE WARNING TO TAKEOFF 1 GL 01 146US 46755 DURING TAKEOFF, AUTO SLAT WOULD NOT RETRACT AND STICK SHAKER ACTIVATED. DUMPED 16,000 LBS OF FUEL AND RETURNED TO DTW. REPLACED AT/SC COMPUTER (11-2232-9-0001, SN 10201) AND THE NR 1 STALL TRANSDUCER (11-3418-9-0001, SN 00438). 2 L 7 3 4F A22WE 1996020900171 19960209 00171 EU 1996 2 9 9602813221 1 19960203 A 3230 RETRACT MECH AIRBUS 320 A320211 3930320 EU LANDING GEAR MALFUNCTIONED A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 321US 262 DURING CLIMBOUT, THE LANDING GEAR DID NOT RETRACT. CYCLED THE LANDING GEAR HANDLE AND ALL INDICATIONS NORMAL. LANDING GEAR EXTENDED NORMALLY AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING REVEALED NO DISCREPANCIES. REPLACED EXTEND SENSOR (24GA), AS PRECAUTIONARY AND OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996020900172 19960209 00172 GL 1996 2 9 9602821221 2 19960202 A 7230 COMPRESSOR DOUG DC10 DC1030 3023501 WP GE CF6 CF650C 30018 GL NR 1 ENGINE STALLED A NWAA O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 GL 01 221NW 46579 17469 EN ROUTE, THE NR 1 ENGINE EXPERIENCED SEVERAL COMPRESSOR STALLS. EGT WAS CLIMBING TO MAX AND SUBSEQUENT VIBRATION, POWE R LEVER WAS PULLED BACK FOR THE REMAINDER OF THE FLIGHT. FOUND METAL IN TAILPIPE OF NR 1 ENGINE. ENGINE IS SCHEDULED F OR CHANGE IN MSP. 2 L 7 3 4F 4 F A22WE A23EA 1996020900173 19960209 00173 NM 1996 2 9 9602836302 1 19960204 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 662US 23720 DURING LINE CHECK, THE DOOR 3L AND LEFT OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE EMERGENCY LIGHTS BATTERY PACK AND OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996020900174 19960209 00174 WP 1996 2 9 9602849971 1 19960202 A 2780 RETRACT MECH DOUG DC9 DC931 3022065 WP LE FLAPS MALFUNCTIONED A NWAA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 01 93359 47337 DURING APPROACH, SLAT ASYMMETRY OCCURRED AND AIRCRAFT ROLLED LEFT. SLAT DISAGREEMENT LIGHT ILLUMINATED WITH NO BLUE SLA T EXTEND LIGHT. CAPTAIN DECLARED A YELLOW EMERGENCY AND EMERGENCY EQUIPMENT WAS CALLED OUT AS A PRECAUTION. AIRCRAFT L ANDED WITHOUT INCIDENT. OPERATED SLATS, INSPECTED T-DUCTS AND ALL CHECKED OK. DISCREPANCY COULD NOT BE DUPLICATED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996020900175 19960209 00175 WP 1996 2 9 9602859968 1 19960204 A 3222 5910448 STRUT DOUG DC9 DC931 3022065 WP NLG REQD SERVICE A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 9332 47264 AFTER TAKEOFF, LANDING GEAR HANDLE WOULD NOT RAISE ON GEAR RETRACTION, NOSE WHEEL WAS STEERABLE. THIS CAUSED THE AIRCRA FT TO REMAIN IN GROUND MODE. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. EMERGENCY EQUIPMENT WAS CALLED OUT ON STANDBY AS A PRECAUTION. REPACKED NOSE LANDING GEAR STRUT AND SERVICED TO PROPER LEVELS. OPERATIONAL CHECK NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996020900176 19960209 00176 WP 1996 2 9 9602869607 1 19960203 A 3242 SPIN BRAKES DOUG DC9 DC932 3022066 WP NLG MALFUNCTIONED A NWAA A UNSCHED LANDING E B VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 607NW 47232 DURING GEAR RETRACTION AFTER TAKEOFF, A LOUD GRINDING WAS HEARD COMING FROM NOSE GEAR AREA FOLLOWED BY A BURNING RUBBER ODOR. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. NORMAL GEAR INDICATIONS WERE NOTED ON GEAR RETRACTION AND EX TENSION. REPLACED BOTH SPIN BRAKES. ALSO, REPLACED BOTH NOSE TIRES AS A PRECAUTION AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996020900177 19960209 00177 WP 1996 2 9 9602879607 1 19960203 A 3230 RETRACT MECH DOUG DC9 DC932 3022066 WP NLG LACK OF LUBE A NWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 01 607NW 47232 DURING GEAR RETRACTION, A LOUD VIBRATION WAS COMING FROM NOSE GEAR AREA. FLIGHT RETURNED TO BNA AND LANDED WITHOUT INCI DENT. LUBRICATED ALL NOSE GEAR GREASE FITTINGS AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996020900178 19960209 00178 NM 1996 2 9 9602885523 1 19960202 A 2421 729825C IDG BOEING 757 757251 1384970 NM NR 2 ENGINE FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 GL 01 523US 22114 3608 23617 DURING APPLICATION OF TAKEOFF THRUST, RIGHT GENERATOR CONTROL TRIPPED. ABORTED TAKEOFF AT 20 KNOTS AND CLEARED RUNWAY. CREW RESET GENERATOR CONTROL PER COCKPIT OPERATING MANUAL AND DEPARTED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND OVE R FREQUENCY AND PMG WIRING MESSAGES LOGGED. PLACED RIGHT GENERATOR AND IDG ON MEL 24-00-1 FOR REPLACEMENT OF IDG PER FI M. MAINTENANCE REPLACED THE IDG, LEAK AND OPERATIONAL CHECK WAS NORMAL. 2 L 7 2 4F RT A2NM 1996020900179 19960209 00179 EU 1996 2 9 9602893232 1 19960203 A 3260 SENSOR AIRBUS 320 A320211 3930320 EU RT MLG DOOR FAILED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 332NW 319 DURING CLIMBOUT AFTER LANDING GEAR RETRACTION, LANDING GEAR DOOR INDICATED UNLOCKED. CYCLED LANDING GEAR HANDLE AND ALL INDICATIONS WERE NORMAL. AIRCRAFT CONTINUED TO ORIGINAL DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT MAIN LANDING GEAR DOOR PROXIMITY SENSOR AND OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996020900180 19960209 00180 EU 1996 2 9 9602903236 1 19960204 A 2421 740119E IDG AIRBUS 320 A320211 3930320 EU NR 2 ENGINE MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 336NW 11325 3627 355 DURING CLIMBOUT, THE NR 2 ENGINE INTEGRATED DRIVE GENERATOR LOW OIL PRESSURE LIGHT ILLUMINATED. AIRCRAFT RETURNED TO DT W AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 ENGINE INTEGRATED DRIVE GENERATOR, LEAK AND OPERATIONAL CH ECK OK. 2 L 7 2 4F RT A28NM 1996020900181 19960209 00181 NM 1996 2 9 9602912296 1 19960203 A 2781 LINKAGE ARM BOEING 727 727251 138408H NM NR 5 LE FLAP LOOSE A NWAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 01 296US 21788 DURING CLIMB AFTER FLAP RETRACTION, NR 5 LEADING EDGE FLAP INDICATOR REMAINED ILLUMINATED. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. INSPECTED FLAP POSITION INDICATION LINKAGE TO SWITCH. FOUND LINKAGE ARM LOOSE, TIGHTENED AND ADJUSTED LINKAGE LEADING EDGE KRUEGER FLAP OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996020900182 19960209 00182 NM 1996 2 9 96FDEA00179 1 19960201 A 3260 189915 UPLOCK SENSOR BOEING 727 727233 138408A NM RT MLG MALFUNCTIONED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 271FE 22036 RT GEAR UNSAFE RED LIGHT ON AFTER GEAR RETRACTION. RECYCLED GEAR, LIGHT REMAINED ON WITH DOOR LIGHT OUT. INSTALLED RT MAIN GEAR UPLOCK SENSOR PER MM 32-61-81, OPS CHECK NORMAL. REPLACED LANDING GEAR ACCESSORY UNIT, MODULE TESTED NORMAL P ER 32-09-121. 2 L 7 3 4F RT A3WE 1996020900183 19960209 00183 NM 1996 2 9 96FDEA00180 1 19960203 A 2750 BYPASS VALVE BOEING 727 727233 138408A NM TE FLAP FAILED A FDEA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 25 272FE 22037 ON LANDING APPROACH, O/B FLAPS DIDN'T EXTEND WITH FLAP HANDLE, I/B FLAPS OKAY. SUBSEQUENT SYSTEM-A HYD HAD TOTAL LOSS. CHECKLIST, M/GAR EXTENSION AND LANDED OKAY. FOUND O/B TRAILING EDGE BYPASS VALVE BODY SEPARATED. REMOVED AND REPLACED VALVE, LEAK CHECKS OKAY. OPS CHECK FLAP SYSTEM, HYD AND ELECTRICAL, ALL CHECK OKAY PER MM 27-51-151. DUE TO LOSS OF A -SYSTEM FLUID, PERFORMED MM 29-11-0 PAGE 102, ALL FILTERS ARE CLEAN AND REPLACED. A/C OKAY FOR SERVICE. 2 L 7 3 4F RT A3WE 1996020900184 19960209 00184 NE 1996 2 9 96FDEA00181 2 19960204 A 7310 FUEL FILTER AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680C2A5 NE NR 1 ENGINE CONTAMINATED A FDEA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 25 651FE 728 ON TAKEOFF, NR 1 ENG FUEL CLOG LIGHT WITH AMBER WARNING ILLUMINATED, ENGINE ANTI-ICE WAS ON. REMOVED AND REPLACED NR 1 ENG FUEL FILTER. SUSPECT WATER AND ICE IN SYSTEM. LEAK CHECK GOOD, OK FOR SERVICE. 2 L 7 2 4F 4 F RT A35EU E13NE 1996020900185 19960209 00185 NM 1996 2 9 96FDEA00182 1 19960202 A 5320 STIFFENER BOEING 727 72722 1384002 NM BS 319 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 CORROSION (C53-111-03-1/2), ON VERTICAL STIFFENER BS 319 WL 181 RBL 15. REMOVED CORROSION AND INSTALLED REPAIR IAW FEDE X SRM 51-40-4. 2 L 7 3 4F A3WE 1996020900186 19960209 00186 NM 1996 2 9 96FDEA00183 1 19960202 A 5320 STIFFENER BOEING 727 72722 1384002 NM BS 336 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 CORROSION (C53-224-03-1/2), ON VERTICAL STIFFENER BS 336 WL 181 RBL 15. REMOVED CORROSION AND INSTALLED REPAIR IAW FEDE X SRM 51-40-4. 2 L 7 3 4F A3WE 1996020900187 19960209 00187 NM 1996 2 9 96FDEA00184 1 19960205 A 3260 SWITCH BOEING 727 7272S2F 1384O81 NM MLG LACK OF LUBE A FDEA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 SO 25 215FE 22936 LT GEAR GREEN LIGHT DID NOT COME ON WHEN LANDING GEAR WAS EXTENDED, RED LIGHT REMAINED ON. AFTER CYCLING GEAR AND MISSE D APPROACH, GREEN LIGHT CAME ON AND A/C LANDED. LUBRICATED NOSE LANDING GEAR WITH AEROSHELL NR 5, CLEANED CANNON PLUG A T MICRO SWITCH AND ALL LIGHTS INDICATED DOWN AND LOCKED ON GROUND. 2 L 7 3 4F A3WE 1996020900188 19960209 00188 NM 1996 2 9 96FDEA00185 1 19960205 A 5315 BAC1505100617 FLOORBEAM BOEING 727 72722 1384002 NM BS 560 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 TRAMCO RESPONSIBILITY 9601-61, WHILE REMOVING SEAT TRACK NR 0381 DAMAGED TWO HOLES IN TOP OF FLOORBEAM, BS 560 BL 0 WL 2 08. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PARTS AND FASTENERS PER FEDEX SRM 53-10-8 BS 560 BL 0 WL 208. 2 L 7 3 4F A3WE 1996020900189 19960209 00189 NM 1996 2 9 96FDEA00186 1 19960205 A 5330 SKIN BOEING 727 72722 1384002 NM BS 306 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 EXTERIOR SKIN IS CUT, DUE TO TOOLING MARK AROUND RIVET HEAD AT BS 306 IN LOWER ROW OF SKIN LAP STR 24L. ACCOMP SKIN REP AIR AT BS 306 IN LOWER ROW OF SKIN LAP, STR 24L IAW FEDEX SRM 53-30-3. 2 L 7 3 4F A3WE 1996020900190 19960209 00190 NM 1996 2 9 96FDEA00187 1 19960205 A 5320 651862222 INTERCOSTAL BOEING 727 72722 1384002 NM CARGO DOOR AREA CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 AFT CARGO AFT HINGE ARM INTERCOSTAL IS CRACKED WHERE HINGE PIN MOUNTS TO INTERCOSTAL. REMOVED CRACKED HINGE ARM INTERCO STAL AND INSTALLED NEW INTERCOSTAL AT AFT HINGE SRM LOCATION IAW FEDEX SRM 51-10-1. 2 L 7 3 4F A3WE 1996020900191 19960209 00191 NM 1996 2 9 96FDEA00188 1 19960205 A 5330 SKIN BOEING 727 72722 1384002 NM BS 1108 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 EXTERIOR SKIN BULGE AND RIVET HEAD DISHED AT BS 1108, 4.5 INCHES UP FROM BOTTOM OF SKIN LAP, STR 26R AT AFT CARGO DOOR C UT OUT LWR AFT CORNER. 2 L 7 3 4F A3WE 1996020900192 19960209 00192 NM 1996 2 9 96FDEA00189 1 19960205 A 5313 STRINGER BOEING 727 72722 1384002 NM BS 890 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CRACK THROUGH FASTENER HOLE AT FAIL-SAFE STR INTERSECTION BS 890 STR 14R. REPAIRED CRACK THROUGH FASTENER HOLE AT FAIL- SAFE STR INTERSECTION BS 890 STR 14R AS PER FEDEX SRM 51-40-3. 2 L 7 3 4F A3WE 1996020900193 19960209 00193 NM 1996 2 9 96FDEA00190 1 19960128 A 5315 BAC1505100617 FLOOR BEAM BOEING 727 72722 1384002 NM BS 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CORROSION (C53-224-06), ON FLOOR BEAM AT BS 600 RBL 10 WL 208. REMOVED CORRODED SECTION FLOOR BEAM, FABRICATED REPAIR A NGLES AND INSTALLED ALL WORK DONE PER FEDEX SRM 53-10-8. 2 L 7 3 4F A3WE 1996020900194 19960209 00194 NM 1996 2 9 96FDEA00191 1 19960205 A 5330 SKIN BOEING 727 72722 1384002 NM BS 358-362 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 LFEC INSP INDICATED A GREATER THAN 20 PERCENT MATERIAL LOSS AT BS 360, 2 INCHES BELOW STR 17L WL 203 TO 206. AREA MARKE D IN RED AND IS VISIBLE ON THE SURFACE OF THE SKIN. REPAIRED AREA FROM BS 358 TO 360, BS 360 TO 362 AT STR 17L TO 18L I AW FEDEX EO 7-5330-7-23196. 2 L 7 3 4F A3WE 1996020900195 19960209 00195 SO 1996 2 9 COMA9610051 1 19960202 A 3230 12038594001 BOX CONTROL EMB 120 EMB120RT SO LANDING GEAR DEFECTIVE A COMA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 243CA 10624 2531 120212 WHEN LANDING GEAR SELECTED VP, NO RETRACTION. CYCLED SELECTOR 3 TIMES BEFORE LANDING GEAR RETRACTED. REPLACED THE LAND ING GEAR CONTROL BOX. 2 L 7 2 4T RT A31SO 1996020900196 19960209 00196 SO 1996 2 9 COMA9610052 1 19960202 A 2750 KRP138112VT ROLLERS EMB 120 EMB120RT SO RT TE FLAP WORN A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 269CA 120263 AFTER TAKEOFF, FLAP DISAGREEMENT WHEN FLAPS SELECTED UP. REPLACED THE RT OUTBD FLAP ROLLERS. 2 L 7 2 4T RT A31SO 1996020900197 19960209 00197 SO 1996 2 9 COMA9610053 1 19960202 A 2750 KRP138112VT ROLLERS EMB 120 EMB120RT SO LT TE FLAP WORN A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 267CA 120259 AFTER TAKEOFF, FLAP DISAGREEMENT WHEN FLAPS SELECTED UP. REPLACED ROLLERS ON LT OUTBD FLAP. 2 L 7 2 4T RT A31SO 1996020900198 19960209 00198 SO 1996 2 9 COMA9610054 1 19960201 A 2750 RETRACT MECH EMB 120 EMB120RT SO TE FLAPS LACK OF LUBE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 267CA 120259 AFTER TAKEOFF, FLAP DISAGREEMENT WHEN FLAPS SELECTED UP. CLEANED, LUBRICATED FLAP TRACKS AND ROLLERS, ACFT RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 1996020900199 19960209 00199 SO 1996 2 9 COMA9610055 1 19960201 A 2750 KRP138112VT ROLLERS EMB 120 EMB120RT SO LT TE FLAPS WORN A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 264CA 120256 AFTER TAKEOFF, FLAP DISAGREEMENT WHEN FLAPS SELECTED UP. REPLACED WORN ROLLERS ON LT WING FLAP. 2 L 7 2 4T RT A31SO 1996020900200 19960209 00200 SO 1996 2 9 COMA9610056 1 19960202 A 2750 KRP138112VT ROLLERS EMB 120 EMB120RT SO RT TE FLAPS CONTAMINATED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 196CA 120196 AFTER TAKEOFF, FLAP DISAGREEMENT WHEN FLAPS SELECTED UP. FOUND RT WING FLAP ROLLERS CONTAMINATED WITH ANTI-SEIZE COMPOU ND. REPLACED ROLLERS. 2 L 7 2 4T RT A31SO 1996020900201 19960209 00201 SO 1996 2 9 COMA9610057 1 19960201 A 2750 KRP138112VT ROLLERS EMB 120 EMB120RT SO RT TE FLAPS WORN A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 196CA 120196 AFTER TAKEOFF, FLAP DISAGREEMENT WHEN FLAPS SELECTED UP. REPLACED WORN ROLLERS ON RT WING FLAPS. 2 L 7 2 4T RT A31SO 1996020900202 19960209 00202 EU 1996 2 9 COMA9630028 1 19960201 A 3040 MS2774318 RELAY SAAB SF340 SF340A 7850100 EU WINDSHIELD WIPER DEFECTIVE A COMA H DEACTIVATE SYST/CIRCUITS O OTHER CR CRUISE 1 SO 01 343CA 340A024 COPILOTS WINDSHIELD WIPER OPERATES WHEN SWITCH IS OFF. REPLACED THE WINDSHIELD WIPER RELAY. 2 L 7 2 4T RT A52EU 1996020900203 19960209 00203 EA 1996 2 9 COMA9660022 1 19960201 A 3010 14463101 DUCT CNDAIR CL600 CL6002B19 EA RT WING CRACKED A COMA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 SO 01 936CA 7043 ANTI-ICE DUCT WARNING MESSAGE ON EICAS. REPLACED CRACKED PICOLLO TUBE AT RT OUTBD WING. 2 L 7 2 4F RT A21EA 1996020900204 19960209 00204 1996 2 9 COMA9660023 4 19960201 A 3416 6222855011 RADIO ALT CNDAIR CL600 CL6002B19 EA AVIONICS DEFECTIVE A COMA K NONE O OTHER LD LANDING 1 SO 01 937CA 7044 DURING LANDING, GROUND LIFT DUMP DID NOT AUTO DEPLOY. REPLACED THE NR 1 RADIO ALTIMETER. 2 L 7 2 4F RT A21EA 1996020900205 19960209 00205 NM 1996 2 9 DHL96703001 1 19960201 A 3030 851CM2 PITOT HEAT BOEING 727 72730C 1384009 NM RIGHT INOPERATIVE A T DHLA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 703DH 19010 RIGHT HAND PITOT HEAT INOP LIGHT ON, NO AMP READING. REMOVED AND REPLACED RIGHT HAND PROBE. 2 L 7 3 4F A3WE 1996020900206 19960209 00206 NM 1996 2 9 DL72K960244 1 19960107 A 5754 6516224101 SLAT BOEING 727 727232 1384082 NM NR 1 POSITION CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 481DA 20861 UPON INSPECTION FOR NR 1 LEADING EDGE SLAT, GROUND DAMAGE WAS FOUND. REPAIRED PER SRM 57-50-3. 2 L 7 3 4F A3WE 1996020900207 19960209 00207 NM 1996 2 9 DL72K960245 1 19960131 A 5754 6516224101 RIB BOEING 727 727232 1384082 NM NR 1 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 481DA 20861 UPON INSPECTION FOR NR 1 LEADING EDGE SLAT, RIB NR 15 WAS FOUND CRACKED. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1996020900208 19960209 00208 NE 1996 2 9 DL72L960238 2 19960130 A 7532 754001351 PRBC BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE FAILED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 27 504DA 21306 700576 ON TAKEOFF, GOT COMPRESSOR STALL NR 2 ENGINE. INSPECTED INLET AND EXHAUST, ALL OK. RAN ENGINE TO TAKEOFF POWER, ALL CK S NORMAL, BUT ON DECEL GOT COMPRESSOR STALL AT 80 TO 85 N2. REPLACED PRBC, RAN ENGINE PER PFHB TEST-E AND ALL CKS GOOD. 2 L 7 3 4F 4 F A3WE E2EA 1996020900209 19960209 00209 NM 1996 2 9 DL72L960257 1 19960201 A 5530 STRINGER BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 510DA 21312 STRINGERS CRACKED 3RD BAY UP IN VERT STAB ON LT AND RT SIDE UPPER END AND 3RD BAY UP RT LOWER. FOUND DURING A-2 LTR CK TPAMM AND REPAIRED PER SRM 55-30-0. 2 L 7 3 4F A3WE 1996020900210 19960209 00210 NE 1996 2 9 DL72S960236 2 19960130 A 7310 37820113 FUEL PUMP BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE FAILED A A DALA C D ABORTED TAKEOFF RETURN TO BLOCK X ENGINE FLAMEOUT TO TAKEOFF 1 SO 27 521DA 21472 687428 ON TAKEOFF ROLL CVG AT 78 KTS, NR 2 ENGINE APPEARED TO FLAME, ALL ENGINE INST ROLLED BACK. REJECTED TAKEOFF AND RETURNE D TO GATE. INSPECTED INTAKE AND EXHAUST, PULLED OIL FILTER, ALL CHECKS OK. FOUND NO FUEL FLOW TO ENGINE. REPLACED FUE L CONTROL AND FUEL PUMP. 2 L 7 3 4F 4 F A3WE E2EA 1996020900211 19960209 00211 NM 1996 2 9 DL72S960242 1 19960130 A 3350 BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 470DA 20747 FWD OVERHEAD EMERGENCY LIGHT INOP IN COACH CABIN. REPLACED BATTERIES, CKS GOOD. 2 L 7 3 4F A3WE 1996020900212 19960209 00212 NM 1996 2 9 DL72S960243 1 19960131 A 3350 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 485DA 20865 EMERGENCY EXIT LIGHT AT R1 AND R2 DOOR INOP. REPLACED EMERGENCY LIGHTS OVER R1 AND R2 DOORS AND OPERATION NORMAL. 2 L 7 3 4F A3WE 1996020900213 19960209 00213 NM 1996 2 9 DL72S960247 1 19960131 A 5754 BRACKET BOEING 727 727232 1384082 NM LE FLAP ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 418DA 21271 FOUND DURING C-1 LETTER CHECK, .5 INCH CRACK NR 1 L/E FLAP ACTUATOR ATTACH BRACKET I/B LWR SIDE. REPAIRED PER M/M 57 -20-21 PAR 12. 2 L 7 3 4F A3WE 1996020900214 19960209 00214 NM 1996 2 9 DL72S960248 1 19960131 A 5754 BRACKET BOEING 727 727232 1384082 NM LE FLAP ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 418DA 21271 FOUND DURING C-1 LETTER CHECK, .375 INCH CRACK NR 2 L/E FLAP ACTUATOR ATTACH BRACKET AT I/B LWR END. REPAIRED PER M/M 5 7-20-21 PAR 12. 2 L 7 3 4F A3WE 1996020900215 19960209 00215 NM 1996 2 9 DL72S960249 1 19960131 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 7 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 418DA 21271 FOUND DURING C-1 LETTER CHECK, .5 INCH CRACK NR 7 L/E SLAT LWR COVE SKIN ATTACH ANGLE BELOW I/B TRACK. REPAIRED PER M/M 57-54-0. 2 L 7 3 4F A3WE 1996020900218 19960209 00218 NM 1996 2 9 DL72S960255 1 19960201 A 2613 WIRE BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE NR 3 ENG STRUT BROKEN A DALA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 SO 27 517DA 21433 700710 ON CLIMBOUT, NR 3 ENGINE STRUT OVERHEAT LIGHT CAME ON, WING ANTI-ICE NOT ON, BUT DUCT TEMP SHOWED 200 DEGREES. FOUND ST RUT WING ANTI-ICE VALVE STUCK OPEN. REMOVED AND REPLACED RELAY R32 AND FOUND BROKEN WIRES IN CANNON PLUG ON STRUT VALVE . REMOVED AND REPLACED CANNON PLUG VALVE, OPERATION NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1996020900219 19960209 00219 NM 1996 2 9 DL72S960256 1 19960122 A 5320 ACCESS DOOR BOEING 727 727232 1384082 NM LT RAM AIR ACT CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 517DA 21433 CORROSION WAS FOUND ON THE RAM AIR ACTUATOR ACCESS DOOR ON THE LT SIDE. THE CORROSION WAS CUT OUT AND STRUCTURAL INTEGR ITY WAS RETURNED PER AN INTERNAL AND EXTERNAL DOUBLER REPAIR PER DL ERA 303056-14. 2 L 7 3 4F A3WE 1996020900220 19960209 00220 NM 1996 2 9 DL72S960264 1 19960202 A 5754 PANEL BOEING 727 727232 1384082 NM NR 4 TE FLAP WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 518DA 21469 HMV, LEADING EDGE O/B END WORN, NR 4 TRAILING EDGE FLAP. REPLACED WORN SEAL ON TRAILING EDGE PANEL, CUT OUT DAMAGE AND REPAIRED PER M/M 57-52-0 FIG 803. 2 L 7 3 4F A3WE 1996020900221 19960209 00221 NM 1996 2 9 DL72S960265 1 19960130 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 344 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 469DA 20746 FOUND ON MV-1 CHECK, CORROSION ON FLOORBEAM STA 344 RBL 45. REPAIRED PER SRM 53-10-8 FIG 10. 2 L 7 3 4F A3WE 1996020900222 19960209 00222 NM 1996 2 9 DL72S960266 1 19960203 A 5754 651622359 SLAT BOEING 727 727232 1384082 NM NR 2 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 489DA 21019 ON CREW WALK-AROUND, NR 2 LEADING EDGE SLAT DAMAGE. ANTI-ICE TELESCOPING DUCT DAMAGED SLAT AND WING. REPLACED SLAT, FE RRIED TO ATL FOR FURTHER MAINTENANCE. 2 L 7 3 4F A3WE 1996020900223 19960209 00223 NM 1996 2 9 DL73S960252 1 19960130 A 5312 BLKHD WEB BOEING 737 737232 1384475 NM FS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 304DL 23076 REF. E.O. 03-069482-12 ME-04 OPN. 0445.1, 2 INCH CRACK AND 1 INCH CRACK IN BS 178 BULKHEAD WEB AT RT BL 5.7 INBOARD OF V ERTICAL STIFFENER. .50 INCH CRACK IN 178 BULKHEAD WEB AT RT BL 5.7 OUTBOARD OF VERTICAL STIFFENER. TWO .25 INCH CRACKS AND 1 INCH CRACK IN 178 BULKHEAD WEB AT LT BL 5.7 INBOARD OF VERTICAL STIFFENER. ACCOMPLISHED REPAIRS PER SRM 53-10-11 , REF S/B 737-53-1173. 2 L 7 2 4F RT A16WE 1996020900224 19960209 00224 NM 1996 2 9 DL73S960254 1 19960129 A 5312 BLKHD WEB BOEING 737 737232 1384475 NM FS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 312DL 23084 REF. E.O. 03-069482-12 OPN. 445. WEB IS CRACKED AT TWO LOCATIONS JUST INBOARD AND ONE LOCATION JUST OUTBOARD OF THE VER TICAL STIFFENER AT LBL 5.7 BETWEEN WL 207 AND WL 184. WEB IS CRACKED AT TWO LOCATIONS JUST INBOARD OF VERTICAL STIFFENE R AT RBL 5.7 BETWEEN WL 207 AND WL 184. REPAIRED PER SRM 53-10-11. REF. E.O. 03-069482-12 OPN. 430. CRACK AT FASTENER AT RBL 15, WL 234, F.S. 178 BULKHEAD WEB. REPAIRED PER SRM 53-10-11, AND DL ERA 303106-14. REF. S/B 737-53-1173. 2 L 7 2 4F RT A16WE 1996020900225 19960209 00225 NM 1996 2 9 DL73S960261 1 19960202 A 8012 START VALVE BOEING 737 737232 1384475 NM NR 1 ENGINE STICKING A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 320DL 23092 NR 1 ENGINE START VALVE OPEN LIGHT CAME ON AFTER TAKEOFF, WENT OUT AFTER NR 1 BLEED WAS TURNED OFF. REPLACED NR 1 ENGIN E START VALVE AND BLEED SWITCH. RAN ENGINE AT TAKEOFF POWER, ALL INDICATIONS CHECKS GOOD AND LEAK CHECK OK. 2 L 7 2 4F RT A16WE 1996020900226 19960209 00226 WP 1996 2 9 DLL10960250 1 19960131 A 7714 N2 INDICATOR LKHEED 1011 10113851 5265010 WP NR 2 ENG INTERMITTENT A DALA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 27 728DA 193C1173 DURING TAKEOFF, EPR AT 1.522 THE N2 GAUGE WAS PEGGED OUT HIGH ABOVE 120 PERCENT ON NR 1 ENGINE FOR 4 SECONDS. REPLACED NR 1 ENG N2 INDICATOR AS PRECAUTIONARY. SWAPPED N2 PROBE TO ALTERNATE PICK UPS. RAN ENGINE TO TAKEOFF POWER, CKS OK. 2 L 7 3 4F A23WE 1996020900227 19960209 00227 WP 1996 2 9 DLL14960258 1 19960201 A 3350 20131A BATTERY PACK LKHEED 1011 1011385115 5265015 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 736DY 193C1227 FLOOR TRACK LIGHTING INOP IN AFT CABIN. REPLACED BATTERY PACK, OPERATION NORMAL. 2 L 7 3 4F A23WE 1996020900228 19960209 00228 WP 1996 2 9 DLL15960259 1 19960202 A 5753 SKIN LKHEED 1011 10113853 5265020 WP NR 3 TE VANE WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 753DA 193W1189 NUMBER 3 RT FLAP VANE CAME IN WITH WORN UPPER SKIN 15 TO 57 FROM INBOARD END. REPLACED SKIN SECTION PER SRM CHAPTER 57- 53-00 FIG 815. 2 L 7 3 4F A23WE 1996020900230 19960209 00230 NM 1996 2 9 DLM90960269 1 19960203 A 3222 STRUT DOUG MD90 MD9030 3023690 NM NLG REQD SERVICE A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 905DA 53385 ON TAKEOFF, NOSE LANDING GEAR FAILED TO RETRACT. FOUND NOSE GEAR STRUT FLUID LOW. SERVICED STRUT AND GEAR CYCLED, OPS NORMAL. 2 L 7 2 4F RT A6WE 1996020900231 19960209 00231 WP 1996 2 9 MWEA96030 1 19960130 A 5542 SKIN DOUG DC9 DC932 3022066 WP RUDDER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 DURING C-CHECK, FOUND RUDDER SKIN CRACKED .875 INCH AT TOP CLOSEOUT RIB MIDPOINT OF RUDDER. INSTALLED FLUSH REPAIR IAW SRM 55-03 FIG 8A. 2 L 7 2 4F A6WE 1996020900232 19960209 00232 WP 1996 2 9 MWEA96031 1 19960201 A 5712 99193017 RIB DOUG DC9 DC932 3022066 WP WS 134.9/137 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 DURING C-CHECK, FOUND TWO LEADING EDGE RIBS AT STA XIS 134.9 AND 137.0 ON LT WING CRACKED. REPLACED LEADING EDGE RIBS I AW SRM 51-30-2 AND RETURNED A/C TO SERVICE. 2 L 7 2 4F A6WE 1996020900233 19960209 00233 WP 1996 2 9 MWEA96032 1 19960202 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 775 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 DURING C-CHECK, FOUND FRAME CRACKED STA 775 AT LONGERON 28L IN AFT CARGO COMPT. FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 53-03 FIG 5. 2 L 7 2 4F A6WE 1996020900234 19960209 00234 WP 1996 2 9 MWEA96033 1 19960202 A 5313 5920319 LONGERON DOUG DC9 DC932 3022066 WP BS 418 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 DURING C-CHECK, FOUND CRACKED LONGERON IN FWD CARGO COMPT STA 418, LONGERON 29L. MAINTENANCE SPLICED IN NEW SECTION OF LONGERON IAW SRM 53-02 FIG 14. 2 L 7 2 4F A6WE 1996020900235 19960209 00235 WP 1996 2 9 MWEA96034 1 19960202 A 5320 SPLICE DOUG DC9 DC932 3022066 WP BS 897-910 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 DURING C-CHECK, FOUND CORRODED LONGERON SPLICE BETWEEN STA 897 AND 910 LT SIDE LONGERON 22. FABRICATED AND INSTALLED LO NGERON SPLICE IAW DAC DRAWING 3914675 AND SRM 53-01 PG 1. 2 L 7 2 4F A6WE 1996020900236 19960209 00236 WP 1996 2 9 MWEA96035 1 19960202 A 5350 LATCH DOUG DC9 DC932 3022066 WP TAILCONE LACK OF LUBE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 DURING C-CHECK, THE TAILCONE DID NOT RELEASE PROPERLY. FOUND UPPER RT LATCH CAUSING RELEASE HANDLE TO PULL HARD. CLEAN ED AND LUBED ALL TAILCONE LATCHES. 2 L 7 2 4F A6WE 1996020900237 19960209 00237 NM 1996 2 9 P5CA9600094 1 19960109 A 5730 PANEL BOEING 747 747122 1384872 NM LT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 ON LEFT WING OUTBOARD MIDFLAP LEADING EDGE, FOUND TWO DELAMINATED AREAS BETWEEN NR 1 AND NR 2 FLAP TRACKS. FIBERGLASS R EPAIR CARRIED OUT IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996020900238 19960209 00238 NM 1996 2 9 P5CA9600095 1 19960109 A 5730 SKIN BOEING 747 747122 1384872 NM LT WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 FOUND LEVEL 1 CORROSION ON LEFT WING UPPER SURFACE AT WBL 579, WBL 565, WLB 370, CENTER SPAR AREA. CORROSION REMOVED, F OUND WITHIN SRM 57-30-01. 2 L 7 4 4F A20WE 1996020900239 19960209 00239 NM 1996 2 9 P5CA9600096 1 19960112 A 2760 BEARING BOEING 747 747122 1384872 NM LT SPOILER CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 FOUND LEVEL 1 CORROSION ON LEFT WING SPOILER POSITION TRANSMITTER FINE ADJUSTMENT ROD BEARING. END ASSEMBLY REPLACED, F UNCTION CHECK SATISFACTORY IAW SRM 27-68-00. 2 L 7 4 4F A20WE 1996020900240 19960209 00240 NM 1996 2 9 P5CA9600097 1 19960108 A 5730 PANEL BOEING 747 747122 1384872 NM RT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 FOUND TWO DELAMINATED AREAS NEAR AFT EDGE OF FIXED T/E PANEL FORWARD OF INBOARD AILERON, RIGHT WING. FIBERGLASS REPAIR CARRIED OUT IAW MM 51-40-09. 2 L 7 4 4F A20WE 1996020900241 19960209 00241 NE 1996 2 9 P5CA9600098 2 19960105 A 7250 BRACKET BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 3 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 FOUND CRACKED BRACKET AT FLANGE 'P' AT APPROX 1 O'CLOCK OF NR 3 ENGINE. CRACKED BRACKET REPLACED IAW MM 72-50-00. 2 L 7 4 4F 4 F A20WE E20EA 1996020900242 19960209 00242 NM 1996 2 9 P5CA9600099 1 19960107 A 5730 SKIN BOEING 747 747122 1384872 NM LT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 FOUND DELAMINATED AREA ON INBOARD FOREFLAP LOWER SKIN BETWEEN NR 4 AND NR 5 FLAP TRACKS ON LEFT WING. FIBERGLASS REPAIR CARRIED OUT IAW SRM 51-51-00. 2 L 7 4 4F A20WE 1996020900243 19960209 00243 NM 1996 2 9 P5CA9600100 1 19960107 A 5720 STIFFENER BOEING 747 747122 1384872 NM LT WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 FOUND LEFT WING STIFFENER CRACKED AFT OF NR 11 L/E FLAP. STIFFENER REPAIRED AND REINSTALLED IAW SRM 51-40-03. 2 L 7 4 4F A20WE 1996020900244 19960209 00244 NE 1996 2 9 P5CA9600101 2 19960104 A 7320 BRACKET BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 3 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 NR 3 ENGINE TT2 SENSOR SUPPORT BRACKET AND MOUNTING PLATE FOUND CRACKED. REPAIRED AND REINSTALLED IAW MM 73-21-04. 2 L 7 4 4F 4 F A20WE E20EA 1996020900245 19960209 00245 NM 1996 2 9 P5CA9600102 1 19960104 A 5730 PANEL BOEING 747 747122 1384872 NM LT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LEFT WING FIXED TRAILING EDGE FOUND DELAMINATED OUTBOARD OF OUTBOARD FLAPS. FIBERGLASS REPAIR CARRIED OUT IAW SRM 51-40 -09. 2 L 7 4 4F A20WE 1996020900246 19960209 00246 NM 1996 2 9 P5CA9600103 1 19960103 A 3610 69B91104600 DUCT LINK BOEING 747 747122 1384872 NM NR 1 ENGINE BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 NR 1 ENGINE PNEUMATIC DUCT LINK AT PYLON HORIZONTAL FIREWALL FOUND BROKEN ON LEFT SIDE. LINK ASSY REPLACED AND SECURED IAW MM 36-11-01. 2 L 7 4 4F A20WE 1996020900247 19960209 00247 NE 1996 2 9 P5CA9600104 2 19960103 A 7320 69B902821 BRACKET BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 2 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 NR 2 PYLON TT2 SENSOR BRACKET FOUND CRACKED. BRACKET REPLACED PER MM 73-22-02. 2 L 7 4 4F 4 F A20WE E20EA 1996020900248 19960209 00248 NM 1996 2 9 P5CA9600105 1 19960103 A 7830 65B9751918 VANE BOEING 747 747122 1384872 NM NR 2 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 FOUND NR 2 ENGINE CASCADE VANE CRACKED AT 8 O'CLOCK POSITION BELOW JACKSCREW. REPAIRED IAW OHM 78-31-51. 2 L 7 4 4F A20WE 1996020900249 19960209 00249 NM 1996 2 9 P5CA9600106 1 19960103 A 7830 65B97513 VANE BOEING 747 747122 1384872 NM NR 3 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 NR 3 ENGINE CASCADE VANE ASSY 2ND FROM TOP, LT SIDE FOUND CRACKED. REPAIRED AND REINSTALLED AS PER MM 78-31-07. 2 L 7 4 4F A20WE 1996020900250 19960209 00250 NM 1996 2 9 P5CA9600107 1 19960103 A 3600 PRECOOLER MOUNT BOEING 747 747122 1384872 NM NR 3 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 NR 3 ENGINE PRE-COOLER FORWARD LOWER MOUNT FOUND CRACKED. REPAIRED AND REINSTALLED IAW MM 36-12-01. 2 L 7 4 4F A20WE 1996020900251 19960209 00251 NE 1996 2 9 P5CA9600108 2 19960102 A 7250 S FLANGE BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 2 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 NR 2 ENGINE S-FLANGE FOUND CRACKED AT 5:30 O'CLOCK POSITION. REPAIRED IAW MM 72-53-02. 2 L 7 4 4F 4 F A20WE E20EA 1996020900252 19960209 00252 NM 1996 2 9 P5CA9600109 1 19960103 A 5400 65B915161 FAIRING BOEING 747 747122 1384872 NM NR 3 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 FOUND NR 3 ENGINE FORWARD FAIRING CRACKED AT FRAME. REPAIRED IAW MM 51-40-03 AND REINSTALLED PER MM 71-40-08. 2 L 7 4 4F A20WE 1996020900253 19960209 00253 NM 1996 2 9 P5CA9600110 1 19960108 A 5720 69B113427 BRACKET BOEING 747 747122 1384872 NM RT WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 FOUND RT WING ANGLE BRACKET CRACKED AT ILGS 949.5. REMOVED AND REPLACED IAW MM 57-31-17. 2 L 7 4 4F A20WE 1996020900254 19960209 00254 NM 1996 2 9 P5CA9600111 1 19960103 A 5312 BRACKET BOEING 747 747122 1384872 NM BS 1480 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 FOUND 4 BRACKETS ATTACHED TO BS 1480 BULKHEAD CRACKED AND BENT. REPAIRED AND REPLACED AS REQUIRED IAW SRM 53-10-22. 2 L 7 4 4F A20WE 1996020900255 19960209 00255 NM 1996 2 9 P5CA9600112 1 19960107 A 5720 69B411575 BRACKET BOEING 747 747122 1384872 NM RT WING DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 FOUND SUPPORT BRACKET FOR LEADING EDGE MIDSECTION DUCT DAMAGED. NEW BRACKET INSTALLED IAW SRM 36-11-12. 2 L 7 4 4F A20WE 1996020900256 19960209 00256 NM 1996 2 9 P5CA9600113 1 19960107 A 5720 65B12725634 SUPPORT BOEING 747 747122 1384872 NM RT WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 FOUND SUPPORT TUBE ASSY AT ILES 949.5 FOR WING L/E LOWER SURFACE PANEL CRACKED. REPLACED IAW MM 57-31-17. 2 L 7 4 4F A20WE 1996020900257 19960209 00257 NM 1996 2 9 P5CA9600114 1 19960107 A 5400 65B9309882 BRACKET BOEING 747 747122 1384872 NM NR 4 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 NR 4 PYLON AFT FAIRING DOOR FOURTH BRACKET ANGLES CRACKED. ANGLES REPLACED AND BRACKET ASSY REINSTALLED IAW MM 54-32-01 . 2 L 7 4 4F A20WE 1996020900258 19960209 00258 NM 1996 2 9 P5CA9600115 1 19960104 A 5400 65B90727612 BRACKET BOEING 747 747122 1384872 NM NR 3 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 NR 3 PYLON LT AFT FAIRING DOOR, AFT MOST BRACKET ANGLES FOUND CRACKED. ANGLE REPLACED IAW MM 54-32-01. 2 L 7 4 4F A20WE 1996020900259 19960209 00259 NM 1996 2 9 P5CA9600116 1 19960105 A 3810 BRACKET BOEING 747 747122 1384872 NM BS 1000 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 FOUND BS 1000 SUPPORT BRACKET FOR POTABLE WATER TANK LOWER SUPPORT BRACE CRACKED. NEW SUPPORT BRACKET INSTALLED IAW SRM 53-11-22. 2 L 7 4 4F A20WE 1996020900260 19960209 00260 NM 1996 2 9 P5CA9600117 1 19960105 A 3810 65B5472510 BRACES BOEING 747 747122 1384872 NM WATER TANK BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 POTABLE WATER TANK LOWER SUPPORT BRACES LEFT AND RIGHT BROKEN. NEW SUPPORT BRACES INSTALLED PER IPC 38-11-02. 2 L 7 4 4F A20WE 1996020900261 19960209 00261 NM 1996 2 9 P5CA9600118 1 19960105 A 2612 BRACKET BOEING 747 747122 1384872 NM NR 2 ENGINE BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 FOUND NR 2 ENGINE UPPER RIGHT FIRE DETECTOR MOUNTING BRACKET BROKEN OFF. REPAIRED AND REINSTALLED IAW MM 26-11-02. 2 L 7 4 4F A20WE 1996020900262 19960209 00262 NM 1996 2 9 P5CA9600119 1 19960105 A 5330 SKIN BOEING 747 747122 1384872 NM FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 FOUND LOWER SKIN CORRODED NEAR VHF ANTENNA NR 2 MOUNTING POINT. LEVEL ONE CORROSION REMOVED, WITHIN SRM 53-30-01 LIMITS . 2 L 7 4 4F A20WE 1996020900263 19960209 00263 NM 1996 2 9 P5CA9600120 1 19960104 A 5400 RIB BOEING 747 747122 1384872 NM NR 4 ENGINE BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 RIGHT LOWER SLOT SEAL FAIRING SUPPORT RIB ON NR 4 ENGINE FOUND BROKEN OFF. REPLACED IAW SRM 54-30-01. 2 L 7 4 4F A20WE 1996020900264 19960209 00264 NE 1996 2 9 P5CA9600121 2 19960105 A 7250 S FLANGE BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE 3 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 FOUND NR 3 ENGINE S-FLANGE CRACKED AT 1:30 O'CLOCK POSITION. WELDING CARRIED OUT IAW AMS 58-17. 2 L 7 4 4F 4 F A20WE E20EA 1996020900265 19960209 00265 NM 1996 2 9 P5CA9600122 1 19960105 A 5751 SKIN BOEING 747 747122 1384872 NM LT AILERON DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 FOUND LEFT WING INBOARD AILERON UPPER SKIN DELAMINATED. FIBERGLASS REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996020900266 19960209 00266 NE 1996 2 9 P5CA9600123 2 19960104 A 7250 R-FLANGE BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 4 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 FOUND NR 4 ENGINE RIGHT HAND R-FLANGE CRACKED AT 3:30 POSITION. WELDED IAW AMS 58-17 IAW P/W 72-53-01. 2 L 7 4 4F 4 F A20WE E20EA 1996020900267 19960209 00267 NM 1996 2 9 P5CA9600124 1 19960104 A 3610 69B911042 TIE DUCT BOEING 747 747122 1384872 NM NR 4 ENGINE BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 FOUND NR 4 ENGINE RIGHT HAND PNEUMATIC DUCT TIE LINK BROKEN. REMOVED AND REPLACED TIE LINK IAW 36-11-01. 2 L 7 4 4F A20WE 1996020900268 19960209 00268 NM 1996 2 9 P5CA9600125 1 19960105 A 3610 PNEU DUCT BOEING 747 747122 1384872 NM NR 3 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 FOUND NR 3 ENGINE PNEUMATIC DUCT CRACKED. REPAIRED PER MM 36-10-02. 2 L 7 4 4F A20WE 1996020900269 19960209 00269 NM 1996 2 9 P5CA9600126 1 19960104 A 5310 STRUCTURE BOEING 747 747122 1384872 NM BS 736 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 FOUND PDU SUPPORT STRUCTURE AT BS 736 CRACKED. REPAIRED IAW SRM 53-10-07. 2 L 7 4 4F A20WE 1996020900270 19960209 00270 NM 1996 2 9 P5CA9600127 1 19960104 A 5720 65B12725629 TUBE ASSY BOEING 747 747122 1384872 NM RIGHT WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 FOUND CRACK IN RIGHT WING SUPPORT TUBE ASSY FOR WING LEADING EDGE LOWER SURFACE. REMOVED AND REPLACED TUBE ASSY IAW IPC 57-31-17. 2 L 7 4 4F A20WE 1996020900271 19960209 00271 NM 1996 2 9 P5CA9600128 1 19960104 A 4970 36002102 EGT HARNESS BOEING 747 747122 1384872 NM APU BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 FOUND APU EGT HARNESS BROKEN AT 8 O'CLOCK AND 9 O'CLOCK POSITIONS. LEFT AND RIGHT EGT HARNESS ASSY'S REPLACED IAW MM 49 -61-04. 2 L 7 4 4F A20WE 1996020900272 19960209 00272 NM 1996 2 9 P5CA9600129 1 19960104 A 5730 SKIN BOEING 747 747122 1384872 NM RT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 FOUND SKIN DELAMINATION ON INBOARD T/E AFT FLAP LOWER SURFACE BETWEEN FLAP CANOE NR 5 AND NR 6. FIBERGLASS REPAIR CARRI ED OUT IAW SRM 51-50-09. 2 L 7 4 4F A20WE 1996020900273 19960209 00273 NM 1996 2 9 P5CA9600130 1 19960104 A 5753 SKIN BOEING 747 747122 1384872 NM RT TE FOREFLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 FOUND CRACK AT RIGHT WING OUTBOARD T/E FOREFLAP BETWEEN FLAP TRACKS NR 7 AND NR 8. FIBERGLASS REPAIRED IAW SRM 51-40-09 . 2 L 7 4 4F A20WE 1996020900274 19960209 00274 NM 1996 2 9 P5CA9600131 1 19960104 A 5753 SKIN BOEING 747 747122 1384872 NM RT TE FLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 FOUND RIGHT WING OUTBOARD T/E AFT FLAP LOWER SURFACE DELAMINATED. REPAIRED AS PER SRM 51-40-09. 2 L 7 4 4F A20WE 1996020900275 19960209 00275 NM 1996 2 9 P5CA9600132 1 19960104 A 5730 PANEL BOEING 747 747122 1384872 NM RT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 FOUND RIGHT WING FIXED T/E PANEL ASSY BL 128.47 TO 263.94 DELAMINATED. REPAIRED IAW SRM 57-30-04. 2 L 7 4 4F A20WE 1996020900276 19960209 00276 NM 1996 2 9 SCNA96012 1 19960201 A 5315 651758866 FLOORBEAM BOEING 727 727225 1384077 NM BS 259.5-277 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING SCHEDULED INSPECTION, FOUND LEVEL 2 CORROSION ON THE UPPER CAP OF THE THIRD CREWMANS SEAT FLOORBEAM INSTALLATION. REMOVED AND REPLACED THE UPPER CAP STA 266.75 LBL 8.5 TO RBL 21 AND INTERCOSTAL STA 259.5 TO 277 LBL 13.5. 2 L 7 3 4F A3WE 1996020900277 19960209 00277 NM 1996 2 9 UPS205372 1 19960202 A 3222 STRUT BOEING 727 7272A1 138407F NM NLG FLAT A IPXA O OTHER J WARNING INDICATION TO TAKEOFF 1 SO 01 213UP 21341 CREW REPORTED, AFTER TAKEOFF NOSE GEAR INDICATED OPEN. ON RECYCLE ALL DOORS WERE OPEN WHEN HANDLE PLACED OFF, MAIN INDI CATED DOWN. ALL 3 OPEN WHEN HANDLE PLACED DOWN, ALL INDICATIONS NORMAL. REPLACED NLS SHOCK STRUT SEALS IAW 12-15-24 AN D OPS CHECKED GOOD. 2 L 7 3 4F A3WE 1996020900278 19960209 00278 NM 1996 2 9 UPS505369 1 19960201 A 2150 3964961 SHUTOFF VALVE BOEING 757 75724APF 1384969 NM RT PACK INOPERATIVE A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 01 404UP 23726 CREW REPORTED, RT PACK SURGE, OIL SMELL IN COCKPIT. REPLACED RT PACK FLOW CONTROL AND SHUTOFF VALVE PER MM 21-51-01. 2 L 7 2 4F RT A2NM 1996020900279 19960209 00279 NM 1996 2 9 UPS505371 1 19960130 A 5753 BRACKET BOEING 757 75724APF 1384969 NM LT TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 439UP 25470 WHILE IN FOR AN SI CHECK, MAINTENANCE REPORTED, LEFT O/B MAIN FLAP, O/B CLOSURE RIB EXTERNAL AFT BRACKET CRACKED. FABRI CATED AND INSTALLED NEW BRACKET IAW SRM 51-40-02, 51-30-01. 2 L 7 2 4F RT A2NM 1996020900280 19960209 00280 WP 1996 2 9 UPS805368 1 19960201 A 3260 DNLOCK SWITCH DOUG DC8 DC871F 302199D WP LT MLG INOPERATIVE A IPXA O OTHER P NO WARNING INDICATION AP APPROACH 1 SO 01 755UP 46055 CREW REPORTED, GEAR LOWERED ON APPROACH, MAIN GREEN LIGHT DID NOT ILLUMINATE. GEAR HAD TO BE CYCLED TWO TIMES TO GET IL LUMINATION. REPLACED LEFT MLG DOWNLOCK SWITCH, SWUNG GEAR SEVERAL TIMES, OPERATED NORMAL MM 32-60-00. 2 L 7 4 4F RT 4A25 1996020900281 19960209 00281 WP 1996 2 9 UPS805370 1 19960203 A 2560 CONTAINER DOUG DC8 DC873F 302199F WP ESCAPE SLIDE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 CREW REPORTED, ESCAPE SLIDE NEEDS TO BE REPACKED THE OUTER COATING CRACKED. REPACKED SLIDE IN CONTAINER, CONTAINER ASSY ON ORDER. 2 L 7 4 4F RT 4A25 1996020900302 19960209 00302 CE 1996 2 9 96ZZZX592 1 19960112 A 7921 6526601 COOLER CESSNA 206 U206G 2073356 CE ENGINE OIL LEAKS A IUJA K NONE K FLUID LOSS IN INSP/MAINT 1 AL 03 4975U 108 D951990275 U2060179 SUBMITTER STATED THIS IS THE EIGHTH OIL COOLER OF THIS TYPE TO LEAK BETWEEN 100-HOUR AND 200-HOUR TT'S. 1 H 7 1 3O A4CE 1996020900320 19960209 00320 WP 1996 2 9 9602921159 1 19960204 A 3350 BATTERY DOUG DC10 DC1040 3023508 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 159US 46768 DURING LINE CHECK, FOUND THE FORWARD SECTION OF THE EMERGENCY FLOOR LIGHT INOPERATIVE. REPLACED THE FORWARD BATTERY PAC K. 2 L 7 3 4F A22WE 1996020900321 19960209 00321 NM 1996 2 9 9602932292 1 19960204 A 2913 HYD PUMPS BOEING 727 727251 138408H NM A-HYD PUMPS FAILED A NWAA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 01 292US 21503 DURING LANDING GEAR EXTENSION HYDRAULIC SYSTEM-A DROPPED TO ZERO PRESSURE AND ZERO QUANTITY. AIRCRAFT LANDED WITHOUT IN CIDENT. REPLACED BOTH A-SYSTEM ENGINE HYDRAULIC PUMPS, SYSTEM FILTERS AND RIGHT GEAR DOOR OPEN HYDRAULIC LINE. OPERATI ONAL CHECK OF SYSTEM OK. 2 L 7 3 4F A3WE 1996020900322 19960209 00322 WP 1996 2 9 9602949304 1 19960201 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 931MC 48057 DURING LINE CHECK, MAINTENANCE FOUND FORWARD OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERY P ACK AND CHECKED GOOD. 2 L 7 2 4F A6WE 1996020900323 19960209 00323 WP 1996 2 9 9602959885 1 19960203 A 3222 STRUT DOUG DC9 DC951 3022051 WP NLG REQD SERVICE A NWAA K NONE O OTHER AP APPROACH 1 GL 01 401EA 47682 DURING TAKEOFF, PILOT REPORTED NOSE GEAR BOTTOMS OUT. UPON EXTENDING GEAR FOR LANDING, CABIN PRESSURE COULD NOT BE MAIN TAINED. MAINTENANCE REPACKED NOSE GEAR STRUT AND RECYCLED GEAR THREE TIMES. OPERATIONALLY CHECKED GROUND SHIFT MECHANI SM AND ALL CHECKED GOOD. 2 L 7 2 4F A6WE 1996020900324 19960209 00324 NM 1996 2 9 9602962291 1 19960205 A 3350 BATTERY PACK BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 291US 21379 DURING PREFLIGHT, FOUND EMERGENCY EXIT LIGHT AT DOOR 2R INOPERATIVE. REPLACED BATTERY PACK AND POWER SUPPLY, CHECKED OK . 2 L 7 3 4F A3WE 1996020900325 19960209 00325 NM 1996 2 9 9602972298 1 19960204 A 3350 BATTERY CHARGER BOEING 727 727251 138408H NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 298US 22152 DURING PREFLIGHT, FOUND EMERGENCY LIGHT AT DOOR R2 INOPERATIVE. REPLACED BATTERY CHARGER AND BATTERY, CHECKED OK. 2 L 7 3 4F A3WE 1996020900326 19960209 00326 WP 1996 2 9 9602989925 1 19960205 A 3222 5910448 STRUT DOUG DC9 DC932 3022066 WP NLG REQD SERVICE A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 925US 47472 AFTER TAKEOFF, LANDING GEAR HANDLE WOULD NOT RAISE DURING GEAR RETRACTION AND AIRCRAFT FAILED TO SHIFT FROM GROUND MODE TO FLIGHT MODE. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NOSE LANDING GEAR STRUT LOW ON F LUID. RESERVICED STRUT TO PROPER LEVELS AND OPERATIONAL CHECK NORMAL ON GEAR SWING. 2 L 7 2 4F A6WE 1996020900327 19960209 00327 NM 1996 2 9 96FDEA00192 1 19960206 A 5320 FITTING BOEING 727 72722 1384002 NM BS 870 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 DURING UT INSPECTION, CRACK INDICATION FOUND AT FUSE BS 870 TERMINAL FITTING RT AFT OF ROW 2, BELOW FASTENER 6. REPAIRE D CRACK AT BS 870 TERMINAL FITTING RT AFT OF ROW 2, BELOW FASTENER 6 PER FEDEX EA'S 7-5310-26957 AND 7-5310-26913. 2 L 7 3 4F A3WE 1996020900328 19960209 00328 NM 1996 2 9 96FDEA00193 1 19960206 A 5330 SKIN BOEING 727 72722 1384002 NM BS 875-878 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 CORROSION ON SKIN INTERIOR AT BS 875 TO 878 BELOW STR 9R. REPAIRED CORROSION ON INTERIOR SKIN AT BS 875 TO 878 BELOW ST R 9R PER FEDEX EA 7-5310-26957. 2 L 7 3 4F A3WE 1996020900329 19960209 00329 WP 1996 2 9 ABXA9600113 1 19960201 A 5610 2701093 LINK DOUG DC9 DC932 3022066 WP RT COCKPIT NOT SECURED A ABXA K NONE O OTHER TX TAXI/GRND HDL 1 GL 23 904AX 47040 FIRST OFFICERS CLEARVIEW WINDOW BROKEN. RESCURED AFT LOCK BAR, LOWER AFT LINKAGE ROD BY REPLACING THE RETAINING PIN. T HE WINDOW WAS NOT BROKEN. 2 L 7 2 4F A6WE 1996020900330 19960209 00330 WP 1996 2 9 ABXA9600114 1 19960201 A 3260 7000010101 SWITCH DOUG DC9 DC932 3022066 WP RIGHT DEFECTIVE A ABXA K NONE N FALSE WARNING AP APPROACH 1 GL 23 983AX 47257 GEAR DOOR OPEN LIGHT REMAINED ON WHEN GEAR WAS SELECTED DOWN. CYCLED GEAR, NO HELP. REPLACED RIGHT GEAR DOOR CLOSE SWI TCH IAW DC-9 MM 32-10-00. LUBED BYPASS DRUM AND CABLE. 2 L 7 2 4F A6WE 1996020900331 19960209 00331 SO 1996 2 9 COMA9610058 1 19960203 A 5246 DOOR EMB 120 EMB120RT SO FUEL SERVICE UNLATCHED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 259CA 120252 DURING TAKEOFF ROLL, SERVICE DOOR WARNING LIGHT ILLUMINATED. FOUND FUEL SERVICE DOOR UNLATCHED. SECURED DOOR AND ACFT CONTINUED SERVICE. 2 L 7 2 4T RT A31SO 1996020900332 19960209 00332 NE 1996 2 9 COMA9610059 2 19960203 A 7200 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE RIGHT FAILED A COMA E ENGINE SHUTDOWN Y ENGINE STOPPAGE CL CLIMB 1 SO 01 1110J 120110 115312 DURING FLIGHT, RT ENGINE FAILED. REPLACED THE RT ENGINE. 2 L 7 2 4T 4 T RT A31SO E20NE 1996020900333 19960209 00333 SO 1996 2 9 COMA9610060 1 19960204 A 5753 KRP138112VT ROLLERS EMB 120 EMB120RT SO RT TE FLAP WORN A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 152CA 120152 AFTER TAKEOFF, FLAP DISAGREEMENT WARNING WHEN FLAPS SELECTED UP. REPLACED WORN ROLLERS AT RT OUTBD FLAP. 2 L 7 2 4T RT A31SO 1996020900334 19960209 00334 SO 1996 2 9 COMA9610061 1 19960204 A 2750 RETRACT MECH EMB 120 EMB120RT SO TE FLAPS MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 254CA 120233 AFTER TAKEOFF, FLAP DISAGREEMENT WHEN FLAPS SELECTED UP. COULD NOT DUPLICATE. INSPECTED FLAP SYSTEM AND NO DEFECTS NOT ED. 2 L 7 2 4T RT A31SO 1996020900335 19960209 00335 SO 1996 2 9 COMA9610062 1 19960204 A 7110 12025600611 COWLING EMB 120 EMB120RT SO RT ENGINE DAMAGED A COMA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 SO 01 258CA 120247 RT ENGINE OUTBD COWLING DOOR OPENED IN FLIGHT. REPLACED COWLING AND REPAIRED SURROUNDING DAMAGE. 2 L 7 2 4T RT A31SO 1996020900336 19960209 00336 1996 2 9 COMA9630029 4 19960204 A 3413 066500011801 VSI SAAB SF340 SF340A 7850100 EU RT COCKPIT FAILED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 359CA 340A053 COPILOTS VERTICAL SPEED INDICATOR WENT BLANK. REPLACED COPILOTS IVA-81A. 2 L 7 2 4T RT A52EU 1996020900337 19960209 00337 NE 1996 2 9 COMA9660024 2 19960203 A 7230 6018T30P06 FAN BLADE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RT ENGINE DAMAGED A COMA A UNSCHED LANDING E C VIBRATION/BUFFET F.O.D. CR CRUISE 1 SO 01 936CA 7043 807038 SEVERE VIBRATION FROM THE RT ENGINE. FOUND RT ENGINE FAN BLADES DAMAGED BY APPARENT ICE INGESTION. REPLACED 18 DAMAGED BLADES. 2 L 7 2 4F 4 F RT A21EA E15NE 1996020900338 19960209 00338 NE 1996 2 9 DL72L960246 2 19960130 A 7240 COMB CHAMBER BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE FAILED A A DALA E A ENGINE SHUTDOWN UNSCHED LANDING T J ENGINE CASE PENETRATION WARNING INDICATION TO TAKEOFF 1 SO 27 513DA 21315 700010 ON TAKEOFF, THE NR 1 ENGINE SHUTDOWN WITH FIRE WARNING IND FOLLOWING. AFTER A/C RETURNED, MAINTENANCE FOUND THE NR 1 EN GINE HAD A UNCONTAINED FAILURE. ALSO, AFTER FURTHER INSPECTION A/C SUBSTAINED MORE DAMAGE TO THE TAIL, FUSELAGE AND S-D UCT DUE TO PARTS COMING FROM THE NR 1 ENGINE. FURTHER INSPECTION SHOWED THAT THE OUTER CASE OF THE COMBUSTION CHAMBER H AD COME APART. 2 L 7 3 4F 4 F A3WE E2EA 1996020900340 19960209 00340 NM 1996 2 9 DL72S960174 1 19960124 A 5754 651622497 SPAR BOEING 727 727232 1384082 NM LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 536DA 22049 DURING SHOP INSPECTION FOR WING SLAT PANEL, FOUND LEADING EDGE SPAR HAD A TEMPORARY REPAIR. REPAIRED SPAR PER MM 7-54-0 FIG 802 A. 2 L 7 3 4F A3WE 1996020900341 19960209 00341 NM 1996 2 9 DL72S960274 1 19960204 A 3232 DOOR ACTUATOR BOEING 727 727232 1384082 NM RT MLG ICED UP A DALA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 SO 27 467DA 20744 ON DEPARTURE, RT MAIN GEAR WOULD NOT RETRACT, TRANSIT LIGHT ON AND SECOND OFFICER'S PANEL NEVER ILLUMINATED. REMOVED IC E BUILD-UP ON RT GEAR DOOR ACTUATOR, LUBED GEAR AND DOORS, PERFORMED GEAR SWING AND OPS NORMAL. 2 L 7 3 4F A3WE 1996020900342 19960209 00342 NM 1996 2 9 DL72S960275 1 19960122 A 3350 FUSE BOEING 727 727232 1384082 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 497DA 21077 ON PREFLIGHT, EMERGENCY TRACK LIGHTS FOUND INOP. REPLACED FUSES AT EMERGENCY EXIT PATH BATTERY PACKS. CHECKED WIRING S YSTEM AND OPERATION NORMAL. 2 L 7 3 4F A3WE 1996020900344 19960209 00344 NM 1996 2 9 DL757960199 1 19960104 A 7830 315N300138SP THRUST REVERSER BOEING 757 757232 1384965 NM NR 2 ENGINE DAMAGED A A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 618DL 22908 757 NR 2 ENGINE HIGH PRESSURE AIR LINE NOT CONNECTED AT FIREWALL, BLEW HOLE IN THRUST REVERSER INNER CORE (315N3101 ASSY ) AT NAC STA 110, APPOX 3 INCH BY 8 INCH AT 1 O'CLOCK POSITION. REQUIRES REPAIR AT NORDAM PER LIASON ENGINEERING. ERA PENDING, SENT TO OUTSIDE REPAIR 01-26-96. 2 L 7 2 4F RT A2NM 1996020900345 19960209 00345 1996 2 9 DLL10960197 4 19960125 A 2220 MACH FEEL WIRE LKHEED 1011 10113851 5265010 WP NR 2 ENGINE BROKEN A DALA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 718DA 193C1097 DURING CLIMB, NR 1 MACH FEEL FAIL LIGHT CAME ON, WOULD NOT RESET. THEN 30 MINS LATER, DURING CRUISE THE NR 2 MACH FEEL FAIL LIGHT CAME ON AND WOULD NOT RESET. REPLACED NR 1 MACH TRIM MOTOR, FOUND BROKEN WIRE ON CONNECTOR TO NR 2 TRIM MOTO R. 2 L 7 3 4F A23WE 1996020900346 19960209 00346 WP 1996 2 9 DLL10960232 1 19960129 A 2750 PDU LKHEED 1011 10113851 5265010 WP RT TE FLAP FAILED A DALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 27 735D 193C1226 ON TAKEOFF AT FLAP RETRACTION FROM 10 DEGREES TO 4 DEGREES, RT FLAP INDICATION STAYED AT 10 DEGREES WHILE LEFT WING INDI CATION WENT TO 4 DEGREES. REPLACING FLAP PDU AS PRECAUTIONARY. REPLACED RT TRAINING EDGE FLAP POSITION TRANSMITTER. 2 L 7 3 4F A23WE 1996020900348 19960209 00348 WP 1996 2 9 DLL15960267 1 19960204 A 3350 POWER SUPPLY LKHEED 1011 10113853 5265020 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 754DL 193Y1181 EMERGENCY LIGHT INOP AT 2L DOOR. REPLACED POWER SUPPLY, CHECKS OK. 2 L 7 3 4F A23WE 1996020900349 19960209 00349 NM 1996 2 9 DLM88960263 1 19960204 A 4990 38005041 TURBINE DOUG MD88 MD88 3023688 NM APU OIL LEAK A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 912DL 3308 49543 CLIMBING THROUGH 11.0 TURNED ENG A/I ON, SMOKE IN CABIN AND COCKPIT. APU NOTICED TO HAVE EXCESSIVE OIL LEAKAGE. PUT AP U ON MCO, BURNED BOTH PACKS OUT. 2 L 7 2 4F RT A6WE 1996020900350 19960209 00350 WP 1996 2 9 SCNA96013 1 19960201 A 2597 119821001 WIRE DOUG DC10 DC1015 3022118 WP L1 DOOR SLIDE BROKEN A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 THE L-1 DOOR SLIDE PUSH TO TEST DOES NOT ILLUMINATE WHEN PRESSED. REPAIRED BROKEN WIRE AT BATTERY HOLDER AND SLIDE TEST ED GOOD. 2 L 7 3 4F A22WE 1996020900351 19960209 00351 NM 1996 2 9 SCNA96014 1 19960130 A 3350 900835A BATTERY PACK BOEING 727 727259 138408J NM AFT CARGO DOOR DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 THE EXTERIOR EMERGENCY EXIT LIGHT ON THE AFT RIGHT CARGO DOOR TESTED DIMLY. REMOVED AND REPLACED BATTERY PACK AND LIGHT TESTED GOOD. 2 L 7 3 4F A3WE 1996020900352 19960209 00352 NM 1996 2 9 SCNA96015 1 19960202 A 2611 PU90421S SMOKE DETECTOR BOEING 727 7272A1 138407F NM LT AFT LAV INOPERATIVE A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 286SC 21601 THE AFT LEFT LAVATORY SMOKE DETECTOR WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED SMOKE DETECTOR AND UNIT CHECKED GOOD. 2 L 7 3 4F A3WE 1996020900353 19960209 00353 WP 1996 2 9 SCNA96016 1 19960130 A 3230 AEH70721 INTERLOCK CRANK DOUG DC10 DC1010 3022110 WP MLG WW FROZEN A SCNA O OTHER J WARNING INDICATION CL CLIMB 1 GL 15 573SC 46905 DURING CLIMB HAD TO USE THE OVERRIDE GEAR RELEASE TO RAISE LANDING GEAR. THE MAIN GEAR HYDRAULIC INTERLOCK CYLINDER CRA NK WAS FOUND FROZEN WITH ICE IN THE ANTI-RETRACT POSITION. APPLIED HEAT, CRANK OPERATED FREELY AND ANTI-RETRACT BUTTON IS NOT NEEDED TO RAISE HANDLE. HYDRAULIC INTERLOCK CYLINDER OPS CHECKED GOOD PER MM 32-31-05. 2 L 7 3 4F A22WE 1996020900354 19960209 00354 WP 1996 2 9 SCNA96017 1 19960202 A 3350 A3060719103 TRACK DOUG DC10 DC1010 3022110 WP CABIN FAILED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 573SC 46905 EMERGENCY TRACK LIGHTING FROM SEATS 11ABC TO 13ABC WAS FOUND TO BE INOPERATIVE. FOUND BROKEN WIRE. REPAIRED WIRE AND L IGHTS OPS CHECKED NORMAL. 2 L 7 3 4F A22WE 1996020900355 19960209 00355 NM 1996 2 9 SWAA960040 1 19960117 A 5312 BULKHEAD BOEING 737 7372T4 1384492 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED MAINT CHECK, FOUND BS 178 BULKHEAD CRACK INDICATIONS AROUND RIVET HEAD FWD SIDE, WL 234, RBL 0. REPAIR ED PER BOEING SRM. 2 L 7 2 4F A16WE 1996020900356 19960209 00356 NM 1996 2 9 SWAA960041 1 19960130 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 312 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 53SW 21534 DURING SCHEDULED MAINT CHECK, FOUND TRANSVERSE FLOORBEAM AT BS 312 CRACKED ON LOWER CHORD AFT FLANGE, LBL 62. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996020900357 19960209 00357 NM 1996 2 9 SWAA960042 1 19960130 A 5320 INTERCOSTAL BOEING 737 7372H4 138448C NM AIRSTAIR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 53SW 21534 DURING SCHEDULED MAINT CHECK, FOUND AIRSTAIR DOORWAY UPPER STOP SUPPORT INTERCOSTAL CRACKED AROUND UPPER/FWD STOP FITTIN G. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996020900358 19960209 00358 NM 1996 2 9 SWAA960043 1 19960130 A 5210 DOOR FRAME BOEING 737 7372H4 138448C NM AFT ENTRY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 53SW 21534 DURING SCHEDULED MAINT CHECK, FOUND AFT ENTRY DOOR HINGE CUTOUT CRACKED AT UPPER HINGE. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996020900359 19960209 00359 NM 1996 2 9 SWAA960044 1 19960130 A 5210 DOOR FRAME BOEING 737 7372H4 138448C NM AFT ENTRY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21722 DURING SCHEDULED MAINT CHECK, FOUND AFT ENTRY DOOR LOWER HINGE CUTOUT CRACKED AT BOTTOM RADIUS. REPAIRED PER BOEING SRM . 2 L 7 2 4F A16WE 1996020900360 19960209 00360 NM 1996 2 9 SWAA960045 1 19960130 A 5230 DOOR FRAME BOEING 737 7372H4 138448C NM CARGO COMPT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21722 DURING SCHEDULED MAINT CHECK, FOUND FWD CARGO DOOR FRAME CRACKED ABOVE FWD I/B DOOR STOP. REPAIRED PER SWA ACO 577-52. 2 L 7 2 4F A16WE 1996020900361 19960209 00361 NM 1996 2 9 SWAA960046 1 19960130 A 5315 FLOORBEAM STRAP BOEING 737 7373A4 1384585 NM E/E COMPT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 674SW 23252 DURING SCHEDULED MAINT CHECK, FOUND CENTER FLOORBEAM STRAP BROKEN IN E AND E COMPARTMENT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996020900362 19960209 00362 NM 1996 2 9 SWAA960047 1 19960131 A 2751 TRANSIT LIGHT BOEING 737 7373Q8 1384670 NM FLAP INDICATION MALFUNCTIONED A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 670SW 23784 AFTER FLAP RETRACTION, TRANSIT INDICATION LIGHT REMAINED ILLUMINATED ON FWD AND OVERHEAD PANELS. CYCLED FLAPS TWICE, NO HELP. AIRCRAFT RETURNED TO MDW AND MADE AN UNEVENTFUL LANDING. CYCLED SLATS/FLAPS PER BOEING M/M, VERIFIED PROBLEM TO BE INDICATION, DEFERRED AND CONTINUED PER MEL 27-3. 2 L 7 2 4F RT A16WE 1996020900363 19960209 00363 NM 1996 2 9 SWAA960048 1 19960130 A 5313 STRINGER BOEING 737 7372T4 1384492 NM BS 1088 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED MAINT CHECK, FOUND S17L CRACKED AT END, BS 1088. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996020900364 19960209 00364 NM 1996 2 9 SWAA960049 1 19960130 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 316SW 23338 DURING SCHEDULED D-CHECK, FOUND FUSE SKIN CRACKS AT BS 178 WL 217 LBL 11 TO 12, AT WL 218 RBL 10 TO 12, AT WL 212 TO 213 RBL 5, AT WL 200 TO 201 RBL 5, AT WL 197 TO 199 LBL 5 AND WL 201 TO 202.5 LBL 5. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996020900365 19960209 00365 NM 1996 2 9 SWAA960050 1 19960130 A 5320 SPLICE BOEING 737 7373H4 1384600 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 316SW 23338 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, S15L. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996020900366 19960209 00366 NM 1996 2 9 SWAA960051 1 19960130 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 333 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 316SW 23338 DURING SCHEDULED D-CHECK, FOUND CRACKED WEB AND STRINGER AT BS 333, S8R. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996020900367 19960209 00367 NM 1996 2 9 SWAA960052 1 19960130 A 5320 CLIP BOEING 737 7373H4 1384600 NM BS 616/277 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 316SW 23338 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED BS 616, S5L, S8R AND AT BS 277, S10 AND 11R. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996020900368 19960209 00368 NM 1996 2 9 SWAA960053 1 19960130 A 5320 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 316SW 23338 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED BETWEEN S15L AND 14L, BS 360, WL 228. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996020900369 19960209 00369 NM 1996 2 9 SWAA960054 1 19960130 A 5240 DOOR FRAME BOEING 737 7373H4 1384600 NM BS 294.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 316SW 23338 DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOOR FRAME CRACKED, BS 294.5, WL 208, RBL 54. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996020900370 19960209 00370 EU 1996 2 9 WWMA9600013 1 19960202 A 3230 RETRACT MECH SAAB SF340 340B 7860101 EU LANDING GEAR ICED UP A WWMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 15 354SB 340B354 THE LANDING GEAR INTRANSIT LIGHT STAYED ON AFTER GEAR RETRACTION. THE AIRCRAFT RETURNED TO FIELD WITHOUT INCIDENT. UPO N INVESTIGATION MAINTENANCE FOUND A LARGE ICE BUILD-UP ON THE LANDING GEAR. THE ICE WAS REMOVED AND A GEAR SWING WAS PE RFORMED. 2 L 7 2 4T RT A52EU 1996020900371 19960209 00371 EU 1996 2 9 WWMA9600014 1 19960202 A 3230 RETRACT MECH SAAB SF340 340B 7860101 EU LANDING GEAR ICED UP A WWMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 15 352SB 340B352 THE LANDING GEAR INTRANSIT LIGHT STAYED ON AFTER GEAR RETRACTION. THE AIRCRAFT RETURNED TO FIELD WITHOUT INCIDENT. UPO N INVESTIGATION MAINTENANCE FOUND A LARGE ICE BUILD-UP ON THE LANDING GEAR. THE ICE WAS REMOVED AND A GEAR SWING WAS PE RFORMED. 2 L 7 2 4T RT A52EU 1996020900372 19960209 00372 EU 1996 2 9 WWMA9600015 1 19960203 A 3230 RETRACT MECH SAAB SF340 340B 7860101 EU LANDING GEAR ICED UP A WWMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 15 345SB 340B345 AFTER TAKEOFF, THE LANDING GEAR FAILED TO RETRACT. THE AIRCRAFT RETURNED TO FIELD WITHOUT INCIDENT. UPON INVESTIGATION MAINTENANCE FOUND A LARGE ICE BUILD-UP ON THE LANDING GEAR. THE ICE WAS REMOVED, THE GEAR WAS SWUNG AND THE AIRCRAFT W AS RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 1996020900373 19960209 00373 EU 1996 2 9 WWMA9600016 1 19960203 A 3230 RETRACT MECH SAAB SF340 340B 7860101 EU LANDING GEAR ICED UP A WWMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 15 245AE 340B245 AFTER TAKEOFF, THE LANDING GEAR FAILED TO RETRACT. THE AIRCRAFT RETURNED TO FIELD WITHOUT INCIDENT. UPON INVESTIGATION MAINTENANCE FOUND A LARGE ICE BUILD-UP ON THE LANDING GEAR. THE ICE WAS REMOVED, THE GEAR WAS SWUNG AND THE AIRCRAFT W AS RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 1996020900374 19960209 00374 EU 1996 2 9 WWMA9600017 1 19960203 A 3230 RETRACT MECH SAAB SF340 340B 7860101 EU LANDING GEAR ICED UP A WWMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 15 254AE 340B254 AFTER TAKEOFF, THE LANDING GEAR FAILED TO RETRACT. THE AIRCRAFT RETURNED TO FIELD WITHOUT INCIDENT. UPON INVESTIGATION MAINTENANCE FOUND A LARGE ICE BUILD-UP ON THE LANDING GEAR. THE ICE WAS REMOVED, THE GEAR WAS SWUNG AND THE AIRCRAFT W AS RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 1996020900375 19960209 00375 NM 1996 2 9 9602992712 1 19960102 A 7711 EPR INDICATOR BOEING 727 7272S7 138407Z NM PWA JT8 JT8D17R 52049 NE NR 3 ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 712RC 22020 689864 NR 3 EPR INDICATION WAS ABNORMALLY LOW ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. THE NR 3 EPR SYSTEM WAS PLACED ON MEL AND THE FLIGHT CONTINUED AS SCHEDULED. MAINTENANCE SUBSEQUENTLY REPLACED THE EPR INDICATOR AND TRANSMITTER WITH SERVICEABLE UNITS. 2 L 7 3 4F 4 F A3WE E2EA 1996020900376 19960209 00376 WP 1996 2 9 9603009601 1 19960202 A 3150 SWITCH DOUG DC9 DC932 3022066 WP T/O WARNING FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 601NW 47038 TAKEOFF WARNING HORN SOUNDED WHEN ADVANCING THROTTLES TO TAKEOFF POWER. ABORTED TAKEOFF AND RETURNED TO THE GATE. REPL ACED FLAP TAKEOFF WARNING SWITCH AND CANNON PLUG, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996020900377 19960209 00377 WP 1996 2 9 9603019914 1 19960206 A 2910 LINE DOUG DC9 DC931 3022065 WP RT HYD SYST LOOSE A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 964N 47416 DURING CLIMB THROUGH 22,000 FEET, LOSS OF RIGHT HYDRAULIC SYSTEM QUANTITY OCCURRED. FLIGHT DIVERTED TO DTW AND LANDED W ITHOUT INCIDENT. FOUND HYDRAULIC LINE GOING TO AFT SIDE OF AUXILIARY PUMP LEAKING. TIGHTENED LINE AND RESERVICED SYSTE M TO PROPER LEVELS. 2 L 7 2 4F A6WE 1996020900378 19960209 00378 WP 1996 2 9 9603021226 1 19960203 A 3230 RETRACT MECH DOUG DC10 DC1030 3023501 WP NLG MALFUNCTIONED A NWAA A J UNSCHED LANDING DUMP FUEL J E WARNING INDICATION VIBRATION/BUFFET TO TAKEOFF 1 GL 01 226NW 46583 DURING TAKEOFF, A LOUD BANG, AIRFRAME VIBRATION, AND A NOSE GEAR UNSAFE LIGHT OCCURRED. DUMPED 130,000 LBS OF FUEL AND RETURNED TO HNL. REPLACED THE UPPER AND LOWER LOCK LINKS, NOSE UNLOCK CYLINDER, RETRACT CYLINDER, AND LEFT AND RIGHT DO OR LINKS. OPERATION OF NOSE GEAR RETRACT NORMAL. 2 L 7 3 4F A22WE 1996020900379 19960209 00379 WP 1996 2 9 9603039876 1 19960206 A 3230 RETRACT MECH DOUG DC9 DC951 3022051 WP LT MLG MALFUNCTIONED A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 785NC 48110 LEFT MAIN LANDING GEAR EXTENDED ON UPLATCH CHECK. CREW CHECKED ACCORDING TO COCKPIT OPERATING MANUAL AND LIGHT WENT OUT . ON APPROACH, PUT HANDLE IN UPLATCH POSITION AND GEAR CHECKED NORMAL. MAINTENANCE JACKED AIRCRAFT AND SWUNG GEAR SEVE RAL TIMES, OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996020900380 19960209 00380 NM 1996 2 9 9603042276 1 19960206 A 3350 LIGHTS BOEING 727 727251 138408H NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 276US 21155 DURING LINE CHECK, FOUND THAT THE MAIN CABIN DOOR EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND BA TTERIES, CHECKED OK. 2 L 7 3 4F A3WE 1996020900381 19960209 00381 1996 2 9 9603059967 4 19960203 A 2565 113317 SLIDE DOUG DC9 DC931 3022065 WP MAIN CABIN DOOR LOW PRESSURE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9331 38611 47263 DURING LINE MAINTENANCE INSPECTION, FOUND MAIN CABIN DOOR EVACUATION SLIDE LOW ON PRESSURE. REPLACED SLIDE. 2 L 7 2 4F A6WE 1996020900382 19960209 00382 WP 1996 2 9 9603069907 1 19960202 A 3350 60030451 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 957N 47253 DURING LINE MAINTENANCE INSPECTION, FOUND OVERWING EMERGENCY EXIT LIGHTS AT ROW 13 INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996020900383 19960209 00383 WP 1996 2 9 9603079983 1 19960204 A 3350 6011779 BATTERY PACK DOUG DC9 DC932 3022066 WP RT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 983US 47282 DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AND OPERATIO NAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996020900384 19960209 00384 WP 1996 2 9 9603089933 1 19960202 A 2780 RETRACT MECH DOUG DC9 DC931 3022065 WP LE SLAT LACK OF LUBE A NWAA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 01 1334U 47280 ON APPROACH, SLAT DISAGREEMENT LIGHT ILLUMINATED AND ROLL WAS EXPERIENCED. A SUCCESSFUL LANDING WAS ACCOMPLISHED WITH S PLIT FLAP/SLAT HANDLE. CHECKED SLAT RIGGING AND RETRACT/EXTEND SWITCHES, ALL CHECKED GOOD. LUBED ANTI-ICE TELESCOPING DUCTS. 2 L 7 2 4F A6WE 1996020900385 19960209 00385 WP 1996 2 9 9603099876 1 19960206 A 3230 UPLOCK MECH DOUG DC9 DC951 3022051 WP LT MLG LACK OF LUBE A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 785NC 48110 DURING CLIMBOUT ON INITIAL UPLATCH CHECK, RECEIVED GEAR DOOR OPEN AND LEFT MAIN GEAR UNSAFE INDICATION. CREW FOLLOWED C OCKPIT OPERATING PROCEDURE AND RECEIVED GREEN INDICATION. FLIGHT RETURNED TO MSP. MAINTENANCE LUBED UPLOCK MECHANISM A ND ADJUSTED DOOR. SWUNG GEAR SEVERAL TIMES AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996020900386 19960209 00386 WP 1996 2 9 9603109876 1 19960206 A 3230 UPLOCK ASSY DOUG DC9 DC951 3022051 WP MLG FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 785NC 48110 DURING CLIMBOUT AT GEAR UPLATCH CHECK, MAIN LANDING GEAR UNSAFE LIGHT AND GEAR DOOR LIGHT CAME ON. GEAR UNSAFE LIGHT DI D NOT GO OUT WHEN GEAR HANDLE WAS MOVED TO UP POSITION. FLIGHT RETURNED TO MSP AND LANDED NORMALLY. MAINTENANCE REPLAC ED GEAR UPLOCK ASSEMBLY. JACKED AIRCRAFT AND RAN GEAR, OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996020900387 19960209 00387 NM 1996 2 9 96FDEA00194 1 19960207 A 5320 FITTING BOEING 727 72722 1384002 NM BS 870 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 CRACK IN HOLES NR 2 AND NR 4 OF ROW 2, FWD O/B FLANGE, AT BS 870 JUST BELOW STR 9R. REPAIRED CRACK IN HOLES NR 2 AND NR 4 OF ROW 2 FWD O/B FLANGE, AT BS 870 JUST BELOW STR 9R PER FEDEX EA 7-5310-26957. 2 L 7 3 4F A3WE 1996020900388 19960209 00388 WP 1996 2 9 ABXA9600115 1 19960206 A 3260 7000010101 DNLOCK SWITCH DOUG DC9 DC933F 302207A WP NLG DEFECTIVE A ABXA O OTHER N FALSE WARNING AP APPROACH 1 GL 23 933AX 47291 NOSE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED AND NO NOSE GEAR GREEN LIGHT. RECYCLED GEAR AND COMPLETED GEAR ABNORMAL CHECKLIST. REPLACED NOSE LANDING GEAR DOWNLOCK SWITCH AND REMOVED OVERCENTER LINKAGE SHIMS AS PER MM SUPP 32-60-01 AND MM 32-21-3. OPS CHECKED GOOD ON GROUND AND GEAR SWING. 2 L 7 2 4F A6WE 1996020900389 19960209 00389 WP 1996 2 9 ABXA9600116 1 19960206 A 2612 FIRE WIRING DOUG DC8 DC861 3021952 WP PWA JT3D JT3D7 52039 NE NR 2 ENGINE CHAFED A ABXA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 GL 23 851AX 45940 669528 DURING APPROACH, INTERMITTENT FIRE WARNING INDICATIONS OCCURRED ON THE NR 2 ENGINE. SHUTDOWN THE NR 2 ENGINE AT 1445Z A ND DISCHARGED THE LEFT WING INBOARD FIRE EXTINGUISHER. REPAIRED CHAFED WIRE ON THE LOWER FIRE LOOP OF THE NR 2 ENGINE. REPLACED THE LEFT WING INBOARD FIRE EXTINGUISHER AND SQUIBS. 2 L 7 4 4F 4 F 4A25 1E8 1996020900390 19960209 00390 NM 1996 2 9 DL72E960285 1 19960205 A 3350 RPS1 POWER SUPPLY BOEING 727 727247 138408F NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 831WA 21483 ON PREFLIGHT, EMERGENCY TRACK LIGHTS INOP IN FWD CABIN. REPLACED POWER SUPPLY, OPS NORMAL. 2 L 7 3 4F A3WE 1996020900391 19960209 00391 NM 1996 2 9 DL72S960268 1 19960124 A 5230 65569271 SKIN BOEING 727 727232 1384082 NM C-3 CARGO DOOR DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 405DA 21149 DURING INSPECTION, C-3 CARGO DOOR OUTER SKIN WAS FOUND WITH THREE DENTS BEYOND ALLOWBLE LIMITS. REPAIRED SKIN PER SRM 5 2-30-1 FIG 9. 2 L 7 3 4F A3WE 1996020900392 19960209 00392 NM 1996 2 9 DL72S960273 1 19960203 A 5330 65545902 SKIN BOEING 727 727232 1384082 NM FS 680-720 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 469DA 20746 DURING INSPECTION, CORROSION WAS FOUND ON THE FUSELAGE SKIN AT STA 700 TO 720F FROM STR 26R TO 27R. THE SKIN PANEL WILL BE REPLACED IN ACCORDANCE WITH B727 SRM 51-10-1. 2 L 7 3 4F A3WE 1996020900394 19960209 00394 NM 1996 2 9 DL72S960278 1 19960120 A 5530 STRINGER BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 517DA 21433 STRINGER 8 ON LT SIDE OF VERT STAB AT FIN STA 180.6 IS CRACKED. FABRICATED REPAIR ANGLE IAW MM 55-30-0 PG 803. 2 L 7 3 4F A3WE 1996020900395 19960209 00395 NM 1996 2 9 DL72W960270 1 19960205 A 5754 ANGLE BOEING 727 727247 138408F NM NR 7 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2807W 20579 FOUND ON C-2 LETTER CHECK, COVE SKIN SUPPORT ANGLE CRACKED .0625 INCH BELOW NR 7 SLAT ANTI-ICE DUCT. REPAIRED PER MM 57 -54-0. 2 L 7 3 4F A3WE 1996020900396 19960209 00396 NM 1996 2 9 DL73E960272 1 19960202 A 5315 654541026 FLOORBEAM BOEING 737 7372S3 NM BS 675 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 369DL 21776 DURING INSPECTION, THE LONGITUDINAL FLOORBEAM AT APPROXIMATELY STA 675 AND RBL 45 WAS FOUND WITH A 2.5 INCH CRACK IN THE LOWER CHORD. DAMAGE REMOVAL RESULTED IN TRIMMING OUT THE LOWER HORIZONTAL FLANGE OF THE CHORD IN ACCORDANCE WITH FORM 8110-3, DATED 2-2-96. 2 L 7 2 4F RT A16WE 1996020900397 19960209 00397 NM 1996 2 9 DL757960271 1 19960205 A 2622 FIRE BOTTLE BOEING 757 757232 1384965 NM CABIN EMPTY A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 681DA 26957 DURING LAYOVER, FOUND FWD CABIN HALO FIRE BOTTLE EMPTY. REPLACED BOTTLE. 2 L 7 2 4F RT A2NM 1996020900398 19960209 00398 NM 1996 2 9 DL767960286 1 19960205 A 2710 KP4R16FS428 BEARING BOEING 767 767232 1385132 NM AILERON CONTROL FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 106DA 22218 ON PREFLIGHT FLIGHT CONTROL CHECK, AILERON VERY STIFF TO MOVE ON BOTH PILOT CONTROL COLUMNS. FOUND BAD BEARING IN CENTE RING MECHANISIM IN LEFT WHEEL WELL. REPLACED BEARING, OPERATION CHECK NORMAL. 2 L 7 2 4F RT A1NM 1996020900399 19960209 00399 WP 1996 2 9 DLL10960276 1 19960206 A 5312 1504400 BLKHD WEB LKHEED 1011 10113851 5265010 WP FS 1212 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 730DA 193C1199 WHILE PERFORMING INSPECTIONS PER SI 7-70645-12, THE FS 1212 CANTED BULKHEAD WAS FOUND WITH CRACKS IN THE TYPICAL LOCATIO N AT LBL 30, LBL 10, RBL 22.5 AND RBL 42.5. THE SUBJECT WEB IS M/F FROM .050 7075-T6 SHEET AND WILL BE REPAIRED PER DL ERA 273246 REV A. 2 L 7 3 4F A23WE 1996020900400 19960209 00400 NM 1996 2 9 DLM88960260 1 19960202 A 2432 BATTERY CHARGER DOUG MD88 MD88 3023688 NM E/E COMP FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 976DL 53257 ON PREDEPARTURE SAW SMOKE COMING FROM 2 VENTS BELOW E AND E COMPARTMENT. REPLACED BATTERIES AND CHARGER, OPS NORMAL. S HOP INSPECTION DETERMINED CHARGER FAILED. PROVIDED CONTINUOUS FULL CHARGE, OVERHEATING THE BATTERY. 2 L 7 2 4F RT A6WE 1996020900401 19960209 00401 NM 1996 2 9 DLM88960284 1 19960205 A 3260 833703 LOCK SWITCH DOUG MD88 MD88 3023688 NM NLG FAILED A DALA O OTHER N FALSE WARNING CL CLIMB 1 SO 27 917DL 49573 AFTER GEAR RETRACTION ON TAKEOFF, PBI NOSE GEAR UNSAFE RED INDICATOR LIGHT REMAINED ON. CYCLED GEAR, NO HELP. C/B P38 PULLED TO SILENCE WARNING. REPLACED NOSE LOCK SWITCH, CYCLED GEAR AND OPERATION NORMAL. 2 L 7 2 4F RT A6WE 1996020900402 19960209 00402 NM 1996 2 9 DLM88960287 1 19960106 A 3350 RPS1 POWER SUPPLY DOUG MD88 MD88 3023688 NM AFT CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 957DL 49976 ON PREFLIGHT, AFT CABIN EMERGENCY FLOOR TRACK LIGHTS INOP. REPLACED POWER SUPPLY AND OPERATION NORMAL. 2 L 7 2 4F RT A6WE 1996020900403 19960209 00403 1996 2 9 MWEA96036 4 19960206 A 2565 13621225 SLIDE DOUG DC9 DC914 3022034 WP TAILCONE LOW PRESS A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 DURING SERVICE CHECK, FOUND TAIL EVACUATION SLIDE PRESSURE LOW. INSTALLED SERVICEABLE TAIL SLIDE. 2 L 7 2 4F A6WE 1996020900404 19960209 00404 WP 1996 2 9 MWEA96037 1 19960206 A 2560 5917689103 SLIDE COVER DOUG DC9 DC915 3022036 WP FWD GALLEY DOOR FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 300ME 45718 CREW REPORTS, GALLEY SERVICE DOOR EVACUATION SLIDE COVER CAME OFF. MAINTENANCE REINSTALLED SLIDE COVER. 2 L 7 2 4F A6WE 1996020900405 19960209 00405 WP 1996 2 9 RRXA9600005 1 19960201 A 3260 SWITCH DOUG DC8 DC871F 302199D WP LT MLG DOOR MALFUNCTIONED A RRXA O OTHER N FALSE WARNING CL CLIMB 1 WP 15 801GP 46039 FLT 2 - KDAY-KOAK - ON GEAR RETRACTION, RED GEAR DOOR PLUS AMBER GEAR DOOR LIGHTS REMAINED ON AFTER CYCLING GEAR. SELEC TED FLAPS TO 25 DEGREES, LIGHT WENT OUT. MAINTENANCE REMOVED AND REPLACED THE LEFT PRIMARY DOOR LIGHT SWITCH, AND LUBED THE MLG. AN OPERATIONAL CHECK OF THE MLG WARNING SYSTEM WAS GOOD. (M) 2 L 7 4 4F RT 4A25 1996020900406 19960209 00406 WP 1996 2 9 RRXA9600006 1 19960202 A 3260 CABLES DOUG DC8 DC871F 302199D WP MLG DOOR LACK OF LUBE A RRXA O OTHER J WARNING INDICATION CL CLIMB 1 WP 15 801GP 46039 KDAY-KATL - FLT NR 38 - ON GEAR RETRACTION THE RED GEAR DOORS LIGHT REMAINED ON. AFTER CYCLING GEAR AND FLAPS SELECTED TO 25 DEGREES LIGHT WENT OUT. MAINTENANCE RIGGED MLG DOOR FOLLOW UP CABLES IAW MM 32-31-5. AN OPERATIONAL CHECK OF THE MLG POSITION WARNING SYSTEM WAS GOOD ON GEAR SWING. (M) 2 L 7 4 4F RT 4A25 1996020900407 19960209 00407 NM 1996 2 9 SWAA960055 1 19960205 A 5720 SUPPORT BOEING 737 7373H4 1384600 NM WS 571 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 601WN 27695 DURING SCHEDULED D-CHECK, FOUND LEFT WING L/E RIB LOWER SURFACE PANEL SUPPORT AT STA 571 CRACKED. REPLACED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1996020900408 19960209 00408 NM 1996 2 9 SWAA960056 1 19960205 A 5730 SKIN BOEING 737 7373H4 1384600 NM LT WING DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 601WN 27695 DURING SCHEDULED D-CHECK, FOUND LEFT WING FIXED L/E HAS VEHICLE STRIKE DAMAGE AT STA 567. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996020900409 19960209 00409 NM 1996 2 9 SWAA960057 1 19960205 A 5730 SKIN BOEING 737 7373H4 1384600 NM WS 571.1 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 601WN 27695 DURING SCHEDULED D-CHECK, FOUND LEFT WING FIXED L/E RIB HAS VEHICLE STRIKE DAMAGE AT STA 571. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996020900410 19960209 00410 NM 1996 2 9 SWAA960058 1 19960205 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED 1/4 D-CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD UPPER RADIUS OF TORQUE TUBE CUTOUT AT AFT SERVICE DOOR. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996020900411 19960209 00411 NM 1996 2 9 SWAA960059 1 19960205 A 5510 ANGLE BOEING 737 7373H4 1384600 NM HORZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 316SW 23338 DURING SCHEDULED D-CHECK, FOUND HORIZONTAL STAB CENTER SECTION RT THRUST BEAM UPPER I/B ATTACH ANGLE CRACKED AT BS 1113. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996020900412 19960209 00412 NM 1996 2 9 SWAA960060 1 19960205 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 312 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 316SW 23338 DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL CRACKED AT BS 312, S4L. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996020900413 19960209 00413 NM 1996 2 9 SWAA960061 1 19960205 A 5330 SKIN BOEING 737 7372H4 138448C NM AFT ENTRY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 DURING SCHEDULED B2 CHECK, FOUND AFT ENTRY DOOR UPPER HINGE CUTOUT ON OUTER SKIN CRACKED IN BOTTOM RADIUS. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996020900414 19960209 00414 NM 1996 2 9 SWAA960062 1 19960205 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 420-440 DAMAGE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 80SW 22675 DURING SCHEDULED CHECK, FOUND LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN BETWEEN BS 420 AND 440, BETWEEN S14 AND 15L. REP AIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996020900415 19960209 00415 NM 1996 2 9 SWAA960063 1 19960205 A 5320 DOUBLER BOEING 737 7372H4 138448C NM VHF ANTENNA ELONGATED HOLES A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 80SW 22675 DURING SCHEDULED CHECK, FOUND EGG SHAPED HOLES ON NR 2 VHF ANTENNA DOUBLER. REPAIRED PER SWA ACO 6470-53. 2 L 7 2 4F A16WE 1996020900416 19960209 00416 NM 1996 2 9 SWAA960064 1 19960205 A 5320 SUPPORT BOEING 737 7372H4 138448C NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 80SW 22675 DURING SCHEDULED CHECK, FOUND FLOORBEAM SUPPORT AT BS 540, BL 0 TO LBL 25, WL 208 CRACKED. REPLACED PER SWA ACO 6470-53 . 2 L 7 2 4F A16WE 1996020900417 19960209 00417 NM 1996 2 9 SWAA960065 1 19960205 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 312 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 53SW 21534 DURING SCHEDULED C1 CHECK, FOUND TRANSVERSE FLOORBEAM AT BS 312 CRACKED ON LOWER CHORD AFT FLANGE, LBL 62.0. REPAIRED P ER BOEING SRM. 2 L 7 2 4F A16WE 1996020900418 19960209 00418 NM 1996 2 9 SWAA960066 1 19960205 A 3350 6104781 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 50SW 21447 DURING SCHEDULED CHECK, FOUND LT AND RT FWD OUTSIDE EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F A16WE 1996020900419 19960209 00419 NM 1996 2 9 SWAA960067 1 19960205 A 5330 SKIN BOEING 737 7373H4 1384600 NM AFT GALLEY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED BC1 CHECK, FOUND AFT GALLEY DOOR UPPER HINGE CUTOUT ON FUSELAGE TOP FWD CORNER CRACKED. REPAIRED PER S WA RA 1-353-909. 2 L 7 2 4F RT A16WE 1996020900420 19960209 00420 NM 1996 2 9 SWAA960068 1 19960205 A 5320 DOOR FRAME BOEING 737 7373H4 1384600 NM FWD SERVICE DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/4 D-CHECK, FOUND FWD SERVICE DOOR FRAME CRACKED AT FWD UPPER LOCK CAM PLATE. REPLACED PER BOEING SRM . 2 L 7 2 4F RT A16WE 1996020900421 19960209 00421 NE 1996 2 9 SWAA960069 2 19960206 A 7230 COMP BLADES BOEING 737 7373H4 1384600 NM GE CFM56 CFM563B1 13802 NE NR 1 ENGINE BENT A SWAA A UNSCHED LANDING C F.O.D. CR CRUISE 1 SW 07 389SW 26592 AFTER TAKEOFF, EXPERIENCED BIRD STRIKE TO NUMBER 1 ENGINE. AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. PE RFORMED BIRD STRIKE INSPECTION, FOUND SEVERAL BENT BLADES ON NUMBER 1 ENGINE. COMPLIED WITH BORESCOPE INSPECTION AND RE PLACED BENT BLADES PER BOEING M/M. 2 L 7 2 4F 4 F RT A16WE E2GL 1996020900423 19960209 00423 WP 1996 2 9 96ZZZM109 1 19960101 A 5347 SEAT TRACK DOUG DC8 DC863 302198A WP BS 1520-1620 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 4935C 45931 FOUND LEVEL 2 CORROSION ON CABIN FLOOR STATION 1520-1620 LEFT SIDE OUTBOARD SEAT TRACK. REMOVED DAMAGED AREA AND SPLICE D IN NEW SEAT TRACK PER SRM 51-2-3. (M) 2 L 7 4 4F 4A25 1996020900424 19960209 00424 WP 1996 2 9 96ZZZM110 1 19960101 A 5512 565174762 PANELS DOUG DC8 DC863 302198A WP RT HORIZ STAB CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 4935C 45931 FOUND LEVEL 2 CORROSION ON RIGHT HORIZONTAL STABILIZER OUTBOARD UPPER SURFACE PANELS AREA CORRODED BETWEEN RIVETS AT TRA ILING EDGE. REPLACED PANEL WITH NEW PANELS. (M) 2 L 7 4 4F 4A25 1996020900425 19960209 00425 WP 1996 2 9 96ZZZM111 1 19960101 A 5512 565174764 PANELS DOUG DC8 DC863 302198A WP RT HORIZ STAB CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 4935C 45931 FOUND LEVEL 2 CORROSION ON RIGHT HORIZONTAL STABILIZER OUTBOARD UPPER SURFACE PANELS AREA CORRODED BETWEEN RIVETS AT TRA ILING EDGE. REPLACED PANEL WITH NEW PANELS. (M) 2 L 7 4 4F 4A25 1996020900426 19960209 00426 WP 1996 2 9 96ZZZM112 1 19960101 A 5730 SKIN DOUG DC8 DC863 302198A WP RIGHT WING CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 4935C 45931 FOUND LEVEL 2 CORROSION, RIGHT WING UPPER SKIN AT XW 0.000 CENTER SPAR AREA SKIN HAS SURFACE CORROSION AT FUSELAGE STATI ON 781.500. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER RICH DRAWING 95-10-06-001. (M) 2 L 7 4 4F 4A25 1996020900427 19960209 00427 WP 1996 2 9 96ZZZM113 1 19960101 A 5311 FRAME DOUG DC8 DC863 302198A WP BS 1220 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 4935C 45931 LEVEL 2 CORROSION, HEAVY CORROSION ON CARGO TRACK SUPPORT FRAME AT STATION 1220 BETWEEN STRINGERS 26L AND 27L. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 51-2-0. (M) 2 L 7 4 4F 4A25 1996020900428 19960209 00428 WP 1996 2 9 96ZZZM114 1 19960101 A 5540 DOUBLER DOUG DC8 DC863 302198A WP RUDDER CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 4935C 45931 LEVEL 2 CORROSION, RUDDER SURFACE IS CORRODED ON RIGHT SIDE ABOVE TAB CUTOUT. REMOVED DAMAGED AREA, FABRICATED AND INST ALLED REPAIR PER SRM 55-2-0. (M) 2 L 7 4 4F 4A25 1996020900429 19960209 00429 WP 1996 2 9 96ZZZM115 1 19960101 A 5730 SKIN DOUG DC8 DC863 302198A WP WS 311 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 4935C 45931 LEVEL 2 CORROSION, RIGHT WING STATION 311 STRINGER 8 UPPER SKIN HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED AND INS TALLED REPAIR PER RICH DRAWING 45931-6. (M) 2 L 7 4 4F 4A25 1996020900478 19960209 00478 WP 1996 2 9 96ZZZM164 1 19960101 A 5320 HAT SECTION DOUG DC8 DC863 302198A WP BS 1600-1560 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 4935C 45931 LEVEL 2 CORROSION, CABIN FLOOR STATION 1600L TO 1560L HAT INBOARD OF INBOARD SEAT TRACK IS BROKEN AND CORRODED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 51-01-00. (M) 2 L 7 4 4F 4A25 1996020900483 19960209 00483 WP 1996 2 9 ASAA9680001 1 19960102 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 950AS 53023 SEA - DURING MAINTENANCE CHECK, THE OVERWING EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND O PERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996020900484 19960209 00484 WP 1996 2 9 ASAA9680003 1 19960103 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 950AS 53023 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHT WIRING AT ROW 1 WAS FOUND BROKEN. REPLACED WIRE SECTION AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996020900485 19960209 00485 WP 1996 2 9 ASAA9680004 1 19960103 A 3350 60030431 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 966AS 49104 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 8 TO 13 WERE FOUND INOPERATIVE. REPLACED THE BA TTERY PACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996020900486 19960209 00486 WP 1996 2 9 ASAA9680005 1 19960103 A 5320 S2652479 SUPPORT DOUG DC9 DC982 3022082 WP BS 200 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 936AS 28441 49363 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FLOOR BOARD SUPPORT AT Y200, X PLUS 56, Z0. REMOVED DAMAGED AREA AND INS TALLED NEW PIECES IAW DC-9 SRM 53-10-01. (M) 2 L 7 2 4F A6WE 1996020900487 19960209 00487 WP 1996 2 9 ASAA9680006 1 19960103 A 5320 S2652479 SUPPORT DOUG DC9 DC982 3022082 WP FS 200-220 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 936AS 28441 49363 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FLOOR BOARD SUPPORT AT Y200 TO Y220, X PLUS 15, Z0. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 53-10-01. (M) 2 L 7 2 4F A6WE 1996020900488 19960209 00488 WP 1996 2 9 ASAA9680007 1 19960103 A 5347 TMS6022044 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 239 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 936AS 28441 49363 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON SEAT TRACK AT Y239, X-22, Z0. REMOVED DAMAGED AREA AND INSTALLED NEW PIE CES IAW DC-9 SRM 51-10-03 AND 53-05. (M) 2 L 7 2 4F A6WE 1996020900489 19960209 00489 WP 1996 2 9 ASAA9680008 1 19960103 A 5320 3932140 HAT CHANNEL DOUG DC9 DC982 3022082 WP BS 1129/1138 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 936AS 28441 49363 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON HAT CHANNEL AT Y1129 AND Y1138, X PLUS 3, Z0. REMOVED DAMAGED AREA AND I NSTALLED NEW PIECES IAW DC-9 SRM 51-10-03, 53-14-03 AND 53-01. (M) 2 L 7 2 4F A6WE 1996020900516 19960209 00516 NM 1996 2 9 F3LA96001 1 19960111 A 3242 214747 BRAKE ASSY BOEING 737 737301 1384611 NM LT MLG FROZE UP A F3LA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 NM 03 578US 23257 FLT NR 443 - DURING TAKEOFF ROLL, FLIGHT CREW REPORTED THE AIRCRAFT PULLED TO THE LEFT. ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE FOUND THE NR 1 BRAKE FROZEN UP DUE TO WEATHER CONDITIONS. FREED BRAKE, PERFORMED ENGINE POWER RUN A ND HIGH SPEED TAXI AND CHECKED OK. UPON ARRIVAL IN DEN, MAINTENANCE REPLACED THE NR 1 BRAKE ASSEMBLY AS PRECAUTIONARY. (M) 2 L 7 2 4F RT A16WE 1996020900549 19960209 00549 EU 1996 2 9 USAA960000 1 19960103 A 5414 SKIN FOKKER F28 F28MK0100 4990807 EU RT STUB WING DELAMINATION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 856US 14405 11286 PIT - DURING Q-1 INSPECTION, FOUND SKIN DELAMINATION RIGHT STUB WING TO FUSELAGE AT STATION 24011-26011. INSTALLED DOUB LER REPAIR PER USAIR EA NR 29492B AND EA NR 31703. (M) 2 L 7 2 4F RT 1996020900550 19960209 00550 EU 1996 2 9 USAA960001 1 19960103 A 5315 FLOOR BEAM FOKKER F28 F28MK0100 4990807 EU BS 3845-5315 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 856US 11286 PIT - DURING Q-1 INSPECTION, FOUND CORROSION ON FLOOR BEAM BLO AT STATION 3845 T-CAP. REMOVED SECTION OF CORRODED T-CAP FROM STATION 3845 TO 5315 AND SPLICED IN NEW SECTION PER SRM 53-21-10. (M) 2 L 7 2 4F RT 1996020900551 19960209 00551 EU 1996 2 9 USAA960002 1 19960103 A 5330 SKIN FOKKER F28 F28MK0100 4990807 EU FWD FUSELAGE LIGHTNING STRIKE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 856US 14405 11286 PIT - DURING Q-1 INSPECTION, FOUND LIGHTNING STRIKE DAMAGE ABOVE CO-PILOTS SLIDING WINDOW IN FUSELAGE SKIN PITTED. INST ALLED FLUSH REPAIR PER USIAR EA NR 31049. (M) 2 L 7 2 4F RT 1996020900552 19960209 00552 EU 1996 2 9 USAA960003 1 19960103 A 5414 SKIN FOKKER F28 F28MK0100 4990807 EU LT STUB WING DELAMINATION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 856US 14405 11286 PIT - DURING Q-1 INSPECTION, FOUND SKIN DELAMINATION LEFT STUB WING TO FUSELAGE AT STATION 24011 TO 26011. INSTALLED DO UBLER REPAIR PER USAIR EA NR 29492B AND EA NR 31703. (M) 2 L 7 2 4F RT 1996020900553 19960209 00553 EU 1996 2 9 USAA960005 1 19960103 A 5315 FLOOR BEAM FOKKER F28 F28MK0100 4990807 EU BS 1127 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 856US 14405 11286 PIT - DURING Q-1 INSPECTION, FOUND CORROSION .005 INCH TO .053 INCH ON FLOOR BEAM AT STATION 1127R FWD OF FRAME 4850. R EPLACED SECTION OF BEAM FROM STATION 4850 TO 5305 PER SRM 53-21-10. (M) 2 L 7 2 4F RT 1996020900554 19960209 00554 NM 1996 2 9 USAA960007 1 19960108 A 5414 SKIN BOEING 757 757225 1384959 NM NR 1 PYLON CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 609AU 35206 22205 CLT - INSPECTION VISUALLY FOUND EXFOLIATION LEVEL 2 CORROSION BETWEEN SKIN AND DOUBLER INBOARD PYLON SKIN IN AREA OF HEA T SHIELD NR 1 PYLON. REPLACED SKIN IN NR 1 PYLON INBOARD SIDE AS PER EA NR 40605. (M) 2 L 7 2 4F RT A2NM 1996020900555 19960209 00555 NM 1996 2 9 USAA960008 1 19960108 A 5414 SKIN BOEING 757 757225 1384959 NM NR 1 PYLON CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 609AU 35206 22205 CLT - INSPECTION VISUALLY FOUND EXFOLIATION LEVEL 2 CORROSION BETWEEN SKIN AND DOUBLER OUTBOARD PYLON SKIN IN AREA OF HE AT SHIELD NR 1 PYLON. REPLACED SKIN NR 1 PYLON OUTBOARD SIDE PER USAIR EA NR 40605. (M) 2 L 7 2 4F RT A2NM 1996020900556 19960209 00556 NM 1996 2 9 USAA960009 1 19960108 A 5330 SKIN BOEING 757 757225 1384959 NM BS 480-500 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 609AU 35206 22205 CLT - INSPECTION VISUALLY FOUND A .0531 INCH DEEP DENT WITH .0065 GOUGE LOCATED AT FUSELAGE SKIN AT STRINGER 52R-55R, BE TWEEN STATION 480-500. INSTALLED EXTERNAL DOUBLER AS PER USAIR EA NR 40595. (M) 2 L 7 2 4F RT A2NM 1996020900557 19960209 00557 NM 1996 2 9 USAA960010 1 19960108 A 5330 SKIN BOEING 757 757225 1384959 NM BS 231.5 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 609AU 35206 22205 CLT - INSPECTION VISUALLY AND BY HFEC FOUND AT FUSELAGE SKIN A DENT 5.5 INCH BY 3.75 INCH, .130 DEEP LOCATED AT BS 231.5 , OUTBOARD CHORD ABOVE VANE. REPLACED CHORD ANGLES AND REPAIRED SKIN WITH FILLER AND DOUBLER AS PER USAIR EA NR 40596. (M) 2 L 7 2 4F RT A2NM 1996020900558 19960209 00558 NM 1996 2 9 USAA960012 1 19960108 A 5330 SKIN BOEING 737 737201 1384454 NM BS 480 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 245US 35206 22751 CLT - INSPECTION VISUALLY FOUND A DENT 8 INCHES BY 4 INCHES IMPACT DAMAGE LOCATED AT BS 480 BETWEEN STRINGER 25R AND STR INGER 26R OF FUSELAGE SKIN. INSTALLED DOUBLER PER USA EA NR 40585. (M) 2 L 7 2 4F A16WE 1996020900559 19960209 00559 NM 1996 2 9 USAA960047 1 19960105 A 5311 65C25211125 FRAME BOEING 737 7372B7 1384560 NM BS 597 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 34396 22888 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK STATION 597 RIGHT FRAME OUTBOARD FLANGE RADIUS JUST ABOVE C ENTER WING. REMOVED AND REPLACED FRAME PER DRAWING 65-46538. NO WEIGHT CHANGE. (M) 2 L 7 2 4F A16WE 1996020900560 19960209 00560 NM 1996 2 9 USAA960048 1 19960105 A 5311 FRAME BOEING 737 7372B7 1384560 NM BS 400 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 34396 22888 INT - DURING Q-5 CHECK, EDDY CURRENT FOUND .5 INCH CRACK AT BS 400 STRINGER 25L TO STRINGER 26L. INSTALLED DOUBLER, REP AIRED PER EA 40544. (M) 2 L 7 2 4F A16WE 1996020900561 19960209 00561 NM 1996 2 9 USAA960049 1 19960105 A 5320 69353214 CLIP BOEING 737 7372B7 1384560 NM BS 639 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 34396 22888 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK IN STRINGER CLIP, AT BS 639 STRINGER 6R. REPLACED CLIP, REPAIRED PER EO 5393G227. (M) 2 L 7 2 4F A16WE 1996020900562 19960209 00562 NM 1996 2 9 USAA960050 1 19960105 A 5320 693535214 TIE CLIP BOEING 737 7372B7 1384560 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 34396 22888 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK STATION 616, STRINGER 2L TIE CLIP. INSTALLED NEW TIE CLI P. REPAIRED PER EO 5393G227. (M) 2 L 7 2 4F A16WE 1996020900563 19960209 00563 NM 1996 2 9 USAA960051 1 19960105 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 986.5 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 34396 22888 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND SPOTS OF CORROSION AT FLOOR BOARD BEAM ATTACH HOLES BS 986.5 LBL 18 TO R IGHT END. INSTALLED REPLACEMENT T-CAP. REPAIRED PER TR 53-10-05C. CORROSION TASK NR C53-107-02. CORROSION LEVEL 1. ( M) 2 L 7 2 4F A16WE 1996020900564 19960209 00564 NM 1996 2 9 USAA960052 1 19960105 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 967 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 34396 22888 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORRODED AREA 38 INCHES IN LENGTH UPPER FLANGE CABIN FLOOR BEAM BS 967 L BL 10-RBL 28. INSTALLED T-CAP REPAIR. REPAIRED PER TR 53-10-05C. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. ( M) 2 L 7 2 4F A16WE 1996020900565 19960209 00565 NM 1996 2 9 USAA960053 1 19960105 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 947 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 34396 22888 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 21 INCHES CORRODED AREA AT FLOOR BEAM BS 947 RBL 10 TO LBL 11. REPAIRED T-CAP. REPAIRED PER SRM 53-10-9. CORROSION TASK NR C53-107-02. CORROSION LEVEL 1. (M) 2 L 7 2 4F A16WE 1996020900566 19960209 00566 NM 1996 2 9 USAA960054 1 19960105 A 5320 1121963 INTERCOSTAL BOEING 737 7372B7 1384560 NM BS 986-1006 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 34396 22888 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND THREE CORRODED AREA ON INTERCOSTAL .5 INCH BY .25 INCH AT BS 986 TO BS 1 006 APPROXIMATELY LBL 18 INCHES. REPLACED WITH IDENTICAL PART NR 1121963. REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996020900568 19960209 00568 NM 1996 2 9 USAABB96002 1 19960104 A 2121 6054578 FAN BOEING 767 767201 1385125 NM FWD CARGO FAILED A USAA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 649US 31879 23901 LAX - FL 7 - EN ROUTE PIT-LAX - PASSENGER SMELLED AND SAW SMOKE IN THE CABIN. CREW DESCENDED FROM FL390 TO FL310 AND SH UT DOWN THE RIGHT PACK. SMOKE ABATED, FLIGHT CONTINUED TO LAX AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACE D THE LEFT RECIRCULATION FAN AND FILTER. (M) 2 L 7 2 4F RT A1NM 1996020900569 19960209 00569 WP 1996 2 9 USAAD96001 1 19960102 A 3231 7000010101 DOOR SWITCH DOUG DC9 DC931 3022065 WP LT MLG INOPERATIVE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 942VJ 47057 CLT - FL 551 - AFTER TAKEOFF, CREW HAD GEAR DOOR OPEN INDICATION. FLIGHT RETURNED TO CLT AND LANDED WITH BOTH MAIN LAND ING GEAR DOORS OPEN. THE LEFT GEAR DOOR WAS DAMAGED. MAINTENANCE REPLACED THE LEFT LANDING GEAR DOOR SWITCH AND THE LE FT MAIN LANDING GEAR DOOR. (M) 2 L 7 2 4F A6WE 1996020900570 19960209 00570 WP 1996 2 9 USAAD96002 1 19960106 A 3244 TIRE DOUG DC9 DC931 3022065 WP NR 3 MLG FAILED A USAA A UNSCHED LANDING O OTHER TO TAKEOFF 1 EA 19 929VJ 48118 FLT NR 328 - CLT - UPON TAKEOFF AT CLT, THE NR 3 MAIN TIRE LOST THE RECAP. GEAR WAS NOT RETRACTED. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT INCIDENT. (M) 2 L 7 2 4F A6WE 1996020900571 19960209 00571 WP 1996 2 9 USAAD96003 1 19960106 A 3230 RETRACT MECH DOUG DC9 DC931 3022065 WP LT MLG/NLG MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 986VJ 47209 FLT NR 1281 - SYR - ON TAKEOFF CLIMB FROM SYR CAPTAIN REPORTED A GEAR INDICATION PROBLEM AND RETURNED TO THE FIELD AT SY R. THE NOSE AND LEFT MAIN GEAR WOULD NOT RETRACT. (M) 2 L 7 2 4F A6WE 1996020900572 19960209 00572 WP 1996 2 9 USAAD96004 1 19960105 A 3260 H146 DOWNLOCK SWITCH DOUG DC9 DC931 3022065 WP LT MLG INOPERATIVE A USAA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 EA 19 967VJ 47375 SYR - FL 1146 - ON APPROACH, CREW SELECTED GEAR DOWN AND THE LEFT MAIN GEAR GREEN LIGHT DID NOT ILLUMINATE. CREW RECYCL ED GEAR WITH SAME RESULT. NO WARNING HORN SOUNDED AND NO RED LIGHT ILLUMINATED. GEAR WAS VERIFIED DOWN AND LOCKED THRO UGH VIEW PORT. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR DOWNLOCK SWITCH AND PRO GRAMMED THE GEAR HARNESS FOR REPLACEMENT. (M) 2 L 7 2 4F A6WE 1996020900575 19960209 00575 EU 1996 2 9 USAAF96001 1 19960101 A 3260 858202 PROX SWITCH FOKKER F28 F28MK0100 4990807 EU LANDING GEAR FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 898US 8787 11398 PIT - FL 317 - AFTER TAKEOFF AND UPON GEAR RETRACTION, CREW RECEIVED 'GND/FLT' MESSAGE ON MFDU, FOLLOWED BY SEVERAL AURA L AND VISUAL WARNINGS. FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE PROXIMITY SWITCH ELECTRONICS UNIT. (M) 2 L 7 2 4F RT 1996020900576 19960209 00576 EU 1996 2 9 USAAF96002 1 19960103 A 3246 WHEEL FOKKER F28 F28MK0100 4990807 EU LT MLG LOST A USAA A UNSCHED LANDING D INFLIGHT SEPARATION TO TAKEOFF 1 EA 19 890US 11365 PIT - FL 1095, DURING TAKEOFF AT PIT, THE LEFT OUTBOARD MAIN WHEEL DEPARTED THE AIRCRAFT. CREW WAS ADVISED BY THE PIT T OWER. FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE WHEEL. INVESTIGATION PROCE EDING, REVEALED THE POSSIBILITY EXISTS OF A FALSE TORQUE ON THE WHEEL NUT. (M) 2 L 7 2 4F RT 1996020900577 19960209 00577 EU 1996 2 9 USAAF96004 1 19960105 A 3260 GROUND SENSE FOKKER F28 F28MK0100 4990807 EU LANDING GEAR MALFUNCTIONED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 886US 11346 FLT NR 1007 - CLT - THE FLIGHT RETURNED TO FIELD DUE TO A GROUND SENSE PROBLEM. (M) 2 L 7 2 4F RT 1996020900578 19960209 00578 EU 1996 2 9 USAAF96005 1 19960108 A 4920 GTCP36150RR APU FOKKER F28 F28MK0100 4990807 EU APU COMPARTMENT FAILED A USAA A B UNSCHED LANDING EMER. DESCENT O T OTHER ENGINE CASE PENETRATION CR CRUISE 1 EA 19 850US 3957 11276 CRW - FL 7007 - EN ROUTE TYS-PIT - CABIN ALTITUDE BEGAN CLIMBING AND WAS UNCONTROLLABLE. CREW DESCENDED AND DIVERTED TO CRW. BOTH PACKS WERE REPORTED AS OPERATING SATISFACTORILY. MAINTENANCE FOUND A HOLE IN THE AFT PRESSURE BULKHEAD DUE TO AN UNCONTAINED APU FAILURE. THE APU HAD FAILED ON THE GROUND IN TYS. THE FACT THAT THE FAILURE WAS UNCONTAINED WAS NOT RECOGNIZED PRIOR TO FLIGHT. THIS IS THE FIRST REPORTED UNCONTAINED FAILURE OF THIS MODEL APU. (M) 2 L 7 2 4F RT 1996020900579 19960209 00579 EU 1996 2 9 USAAF96006 1 19960108 A 3260 BULB FOKKER F28 F28MK0100 4990807 EU COCKPIT FAILED A USAA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 EA 19 851US 11278 GRR - FL 400 - CREW REPORTED, THAT THE LEFT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE ON GEAR EXTENSION. CREW PE RFORMED A TOWER FLY-BY AND DECLARED AN EMERGENCY. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED A BURNE D OUT LIGHT BULB. (M) 2 L 7 2 4F RT 1996020900580 19960209 00580 EU 1996 2 9 USAAF96008 1 19960112 A 3010 32186211 SHUTOFF VALVE FOKKER F28 F28MK0100 4990807 EU TAIL ANTI-ICE INOPERATIVE A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 882US 11340 11334 CLT - FL 1295 - EN ROUTE PIT - LGA, CREW RECEIVED TAIL ANTI-ICING FAULT SHORTLY AFTER SELECTING TAIL ANTI-ICE. FLIGHT D IVERTED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE TAIL ANTI-ICE SHUTOFF VALVE. (M) 2 L 7 2 4F RT 1996020900581 19960209 00581 EU 1996 2 9 USAAF96009 1 19960116 A 3350 2LA00557300 DOME LIGHT FOKKER F28 F28MK0100 4990807 EU COCKPIT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 885US 11345 PIT - COCKPIT EMERGENCY LIGHT DID NOT ILLUMINATE WITH THE EMERGENCY SWITCH IN THE ON POSITION. MAINTENANCE REPLACED THE DOME LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT 1996020900584 19960209 00584 NM 1996 2 9 USAASB96001 1 19960103 A 2613 355724255 ELEMENT BOEING 737 7372B7 1384560 NM LT ENG SHORTED A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 277AU 22889 FLT NR 1244 - CLT - LEFT WING BODY OVERHEAT ILLUMINATED IN FLT. ISOLATED LEFT BLEED AIR DUCT BUT OVERHEAT LIGHT REMAINE D ON. MAINTENANCE FOUND OVERHEAT ELEMENT SHORTED. REPLACED ELEMENT. OPS CHECKS SAT. (M) 2 L 7 2 4F A16WE 1996020900585 19960209 00585 NM 1996 2 9 USAASB96002 1 19960105 A 2130 7110025 PRESS SELECTOR BOEING 737 737301 1384611 NM P-5 PANEL FAILED A USAA A UNSCHED LANDING O OTHER TO TAKEOFF 1 EA 19 350US 23553 FLT NR 1440 - MCO - ON TAKEOFF FROM PBI, AIRCRAFT WOULD NOT PRESSURIZE. SELECTED STANDBY THEN MANUAL, NO HELP, OUTFLOW VALVE FULL CLOSED. MAINTENANCE REPLACED PRESSURIZATION SELECTOR PANEL. PRESSURIZED AIRCRAFT ON GROUND AT MCO. OPS CHE CKS OK. (M) 2 L 7 2 4F RT A16WE 1996020900586 19960209 00586 NM 1996 2 9 USAASB96004 1 19960105 A 2750 RETRACT MECH BOEING 737 7374B7 1384702 NM TE FLAPS LACK OF LUBE A USAA L ABORTED APPROACH F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 EA 19 426US 24548 FLT NR 2339 - FLL - ON APPROACH TO FLL, COULD NOT GET FLAPS TO EXTEND BEYOND 18 DEGREES INDICATED. INITIATED GO AROUND, RESET BREAKERS, FLAPS EXTENDED NORMALLY SECOND TIME, NO ASYMMETRY. MAINTENANCE LUBRICATED BALL NUT RESERVOIR AND JACKS CREWS. (M) 2 L 7 2 4F RT A16WE 1996020900587 19960209 00587 NM 1996 2 9 USAASB96005 1 19960109 A 3260 6552811113 ACCY UNIT BOEING 737 737201 1384454 NM LANDING GEAR FAILED A USAA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 EA 19 257AU 22799 FLT NR 1530 - PHL - GREEN 'NOSE GREEN' REMAINED ON ENTIRE LIGHT. RED 'NOSE GEAR' LIGHT NEVER CAME ON IN FLIGHT. FLEW B Y TOWER. MAINTENANCE REPLACED THE LANDING GEAR ACCY UNIT. ALL INDICATIONS NORMAL. (M) 2 L 7 2 4F A16WE 1996020900588 19960209 00588 NM 1996 2 9 USAASB96006 1 19960109 A 3397 WIRE BOEING 737 7372B7 1384560 NM CABIN BROKEN A USAA K NONE L NO TEST NR NOT REPORTED 1 EA 19 284AU 23131 FLT NR 1635 - PHL - UNSCHEDULED MAINTENANCE FOR CEILING EMERGENCY LIGHTS INOP. MAINTENANCE REPAIRED WIRE ON CENTER OVER HEAD CEILING LIGHT. EMERGENCY LIGHTS OPS CHECK NORMAL. (M) 2 L 7 2 4F A16WE 1996020900644 19960209 00644 EA 1996 2 9 96ZZZX625 1 19960123 A 5610 17180001 WINDOW SIERRACIN DHAV DHC8 DHC8311 1386006 EA PILOT'S LT SIDE CRACKED A MASA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 01 436AW 8454 021 336 GRAND JUNCTION, COLORADO - AIRCRAFT DEPARTED AT SCHEDULED DEPARTURE TIME WHEN ABOUT 10 MINUTES OUT, THE PILOT'S LEFT SID E WINDOW CRACKED FROM TOP TO BOTTOM ABOUT HALF WAY BACK. AIRCRAFT RETURNED TO GRAND JUNCTION WHERE WINDOW WAS REPLACED AND RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1996020900645 19960209 00645 WP 1996 2 9 C1HA960001 1 19960102 A 2133 A3138000003 OUTFLOW VALVE DOUG DC8 DC862 3021970 WP CABIN FROZE UP A A C1HA B EMER. DESCENT O OTHER DE DESCENT 1 WP 23 802MG 46098 AT TOP OF DESCENT, PRESSURIZATION STARTED TO CLIMB THAT WAS UNCONTROLLABLE IN MAN. AND AUTOMATIC. LEVER FELT CABLES WER E BOUND. FOUND OUTFLOW VALVE COMPARTMENT WET. REPAIRED AFT LAV. PLUMBING DRIED OUT LPS3 OUTFLOW COMPARTMENT. DRIED A ND LUBED OUTFLOW VALVE PRESS. CK OPS, CK OK ON GROUND IN MANUAL ONLY. AUTO PRESS. INOPERATIVE, TRANSFERRED TO DMI 510. (X) 2 L 7 4 4F 4A25 1996020900646 19960209 00646 NE 1996 2 9 C1HA960004 2 19960103 A 7220 BULLET DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3B 52039 NE NR 2 ENGINE SNOW PACKED A C1HA C D ABORTED TAKEOFF RETURN TO BLOCK C F.O.D. TO TAKEOFF 1 WP 23 802MG 46098 669726 PRIOR TO REACHING V1, NR 2 ENGINE COMPRESSOR STALLED. VISUALLY INSPECTED NR 2 ENGINE INTAKE. FOUND SNOW ON NOSE BULLET . REMOVED SNOW, INSPECTED COMPRESSOR, TAIL PIPE, NO DEFECTS NOTED. RAN ENGINES 2 AND 3 ON TAKEOFF POWER. IAW CHAPTER 71, NO DEFECTS NOTED. (X) 2 L 7 4 4F 4 F 4A25 1E8 1996020900647 19960209 00647 WP 1996 2 9 C1HA960005 1 19960103 A 2130 W307EG SWITCH DOUG DC8 DC862 3021970 WP F/E PANEL FAILED A C1HA O OTHER P NO WARNING INDICATION DE DESCENT 1 WP 23 802MG 46098 CABIN ALT. WARNING HORN FAILED TO COME ON DURING ENTIRE LOSS OF PRESSURIZATION. FOUND CABIN LOW PRESSURE WARNING HORN S ILENCE SWITCH FAILED OPEN AND BAD CONNECTION ON CABIN LOW PRESSURE SWITCH. REMOVED AND REPLACED SILENCE SWITCH AND REPA IRED CONNECTION SYSTEM. OPS CHECK GOOD. (X) 2 L 7 4 4F 4A25 1996020900648 19960209 00648 WP 1996 2 9 C1HA96002 1 19960102 A 3520 40774415020 OXYGEN LINE DOUG DC8 DC862 3021970 WP CABIN BROKEN A C1HA B EMER. DESCENT O OTHER DE DESCENT 1 WP 23 802MG 46098 DEPLOYED MASK IAW RAPID CABIN DEPRESSURIZATION CHECK LIST AND MASK DID NOT DEPLOY. CABIN CLIMBED THROUGH 16,000 FEET AN D DID NOT DEPLOY AUTOMATICALLY. FOUND OXYGEN LINE BROKEN. REMOVED AND REPLACED. OPS CHECK GOOD. (X) 2 L 7 4 4F 4A25 1996020900672 19960209 00672 NM 1996 2 9 96UAL900086 1 19960202 A 2120 AIR DISTR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN SMOKE A UALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 775UA 26947 INBOUND CREW REPORTS SMOKE ABOVE SEAT 8AB. 2 L 7 2 4F 4 F RT T0001SE E46NE 1996020900673 19960209 00673 NM 1996 2 9 96UAL900087 1 19960202 A 2722 33215208 ACTUATOR 33152218S BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RUDDER WORN A UALA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 WP 29 547UA 25368 CREW REPORTED LEFT HYDRAULIC FLUID LEVEL WENT DOWN ON LANDING. FOUND HYDRAULIC FLUID LEAKING FROM TAIL OF AIRCRAFT. SU PPLEMENTAL DATA UPDATE: REPLACED RUDDER CENTER PCA. PCA WAS FOUND TO HAVE WORN PISTON ROD SEALS CAUSING THE LEAKAGE. O VERHAULED ACTUATOR WAS TESTED AND RETURNED TO SERVICEABLE CONDITION. 2 L 7 2 4F 4 F RT A2NM E17NE 1996020900674 19960209 00674 WP 1996 2 9 96UAL900088 1 19960202 A 2150 PACK DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN ODOR A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 1814U 46613 UPON ARRIVAL LAX, APU STARTED AND PACKS FILLED CABIN WITH OILY SMELL. RAN PACKS WITH GROUND SOURCE AND NO SMELL NOTED. INOPED APU. 2 L 7 3 4F 4 F A22WE E23EA 1996020900675 19960209 00675 NM 1996 2 9 96UAL900089 1 19960205 A 2131 7638101 CONTROLLER BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE E/E COMPT FAILED A UALA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 WP 29 997UA 22457 CABIN PRESSURE CONTROL FAILED AT FL 350, STANDBY HELD FOR 2 MINUTES THEN FAILED. MANUAL AC AND DC FAILED TO CONTROL AT ALL. SUPPLEMENTAL DATA UPDATE: THE CABIN PRESSURE CONTROLLER WAS REPLACED. PRESSURIZATION SYSTEM CHECKS O.K. 2 L 7 2 4F 4 F A16WE E2EA 1996020900676 19960209 00676 NM 1996 2 9 96UAL900090 1 19960205 A 3260 PROX CARD BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE E/E COMPT BAD A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 9015U 19053 AFTER TAKEOFF, GEAR LEVER WOULD NOT GO PAST NEUTRAL POSITION, RETURNED TO ORD. *S/D* THE A-1 AND A-2 LANDING GEAR POSI TION INDICATING SYSTEM PROXIMITY CARDS IN THE LANDING GEAR ACCESSORY UNIT WERE FOUND BAD. REPLACED CARDS, SYSTEM CHECKS OK. 2 L 7 2 4F 4 F A16WE E2EA 1996020900677 19960209 00677 NM 1996 2 9 96UAL900091 1 19960206 A 3350 BATTERY CHARGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7945U 21899 LEFT AFT OVER WING EMERGENCY LIGHT INOPERATIVE. RELAMPED. NO HELP. REPLACED BATTERY CHARGER. OPERATIONALLY CHECKED O KAY. 2 L 7 2 4F 4 F RT A2NM E17NE 1996020900678 19960209 00678 NM 1996 2 9 96UAL900092 1 19960206 A 3350 STRIP BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 4717U 19878 EMERGENCY ESCAPE LIGHTING INOP AT ROWS 37-49, RIGHT AISLE. REPLACED LIGHT STRIP. 2 L 7 4 4F 4 F A20WE E20EA 1996020900679 19960209 00679 NM 1996 2 9 96UAL900093 1 19960206 A 4920 38220803 COMPRESSOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU DAMAGED A UALA A UNSCHED LANDING C B J F.O.D. SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 WP 29 547UA 5838 25368 REPORTED SMOKE IN CABIN. FLIGHT DIVERTED TO SPOKANE. FOREIGN OBJECT DAMAGE IN THE APU DRIVEN COMPRESSOR. REPLACED APU . 2 L 7 2 4F 4 F RT A2NM E17NE 1996020900680 19960209 00680 WP 1996 2 9 96UAL900094 1 19960206 A 7830 9007M62G16 BLOCKER DOOR GE DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 2 TR UNIT FAILED A A UALA O OTHER O OTHER LD LANDING 1 WP 29 1839U 58000 46633 UPON DEPLOYING REVERSERS AT LAX ON 1/9/96, LOST NR 2 RT REV. TRANSLATING COWL. FOUND BROKEN IN SEVERAL PIECES. UPPER B LOCKER DOOR FAILED CAUSING DOOR TO JAM BETWEEN COWL AND CORE STRUCTURE. THIS CAUSED ACTUATOR ATTACH FITTINGS TO SHEAR, LIBERATING THE COWL. COWL SPLIT AT FWD BONDMENT. REPLACED NR 2 RT REVERSER. FAIL-SAFE FASTENERS WILL BE ADDED AT THE FITTING TO BLOCKER DOOR ATTACHMENT ON ALL OLD STYLE DOORS, AT SHOP VISIT. THE INSPECTION DOCUMENT WILL BE REVISED TO SP ECIFICALLY CHECK THE FITTING FOR LOOSENESS OR BOND FAILURE AT EACH C-CHECK. 2 L 7 3 4F 4 F A22WE E23EA 1996020900681 19960209 00681 NM 1996 2 9 96UAL900095 1 19960206 A 2780 RETRACT MECH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LE FLAPS LOCKED OUT A A UALA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 WP 29 541UA 25253 LEADING EDGE SLAT ASYMMETRY MESSAGE DISPLAYED ON STATUS PANEL OF THE ENGINE INDICATING AND CREW ALERT SYSTEM (EICAS) AND FLAPS LOCKED OUT ELECTRICALLY DURING CRUISE. ASYMMETRY MESSAGE OCCURRED AT 17,000 FEET, 320 IAS, WITH FLAPS UP. USED ALTERNATE FLAPS FOR LANDING. 2 L 7 2 4F 4 F RT A2NM E17NE 1996020900682 19960209 00682 NM 1996 2 9 96UAL900096 1 19960208 A 2752 ACE UNIT LEAR ASTRONI 4885500901 BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LT FLAPERON MALFUNCTIONED A UALA K NONE F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 WP 29 775UA 26947 LEFT OUTBOARD FLAPERON DOES NOT FOLLOW COMMANDS AND RAM TRANSDUCER HAS FEEDBACK FAULT. REPLACED ACTUATOR CONTROL ELECTR ONICS L2. UNIT RETURNED TO MANUFACTURER FOR ANALYSIS. 2 L 7 2 4F 4 F RT T0001SE E46NE 1996020900683 19960209 00683 NM 1996 2 9 96UAL900097 1 19960208 A 2750 ALT DRIVE MOTOR TALLEY CORP 2473T1001 BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE TE FLAPS FAILED A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 602UA 139 21863 LANDED IN SFO UNDER AMBER ALERT BECAUSE FLAPS WOULD NOT EXTEND. REPLACED ALT FLAP DRIVE MOTOR. DURING SHOP VISIT FOUND ROTOR RUSTED TO STATOR. CLEANED ROTOR AND REPLACED MOTOR BEARINGS. MOTOR WAS TESTED AND MADE SERVICEABLE. 2 L 7 2 4F 4 F RT A1NM E3NE 1996020900684 19960209 00684 NM 1996 2 9 DL72S960281 1 19960206 A 5720 STIFFENER BOEING 727 727232 1384082 NM WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 484DA 20864 FOUND ON B1 LETTER CHECK, 2 INCH CRACK IN WING L/E SPAR STIFFENER AT NR 6 SLAT INBD TRACK. REPLACED STIFFENER PER MM 57 -20-21. 2 L 7 3 4F A3WE 1996020900685 19960209 00685 NM 1996 2 9 DL72S960282 1 19960206 A 5720 ANGLE BOEING 727 727232 1384082 NM SPAR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 484DA 20864 FOUND ON B-1 LETTER CHECK, TWO L/E SPAR STIFFENERS CRACKED .50 INCH, ONE AT NR 3 SLAT INBD TRACK, THE OTHER AT NR 2 SLAT OUTBD TRACK. REPLACED ANGLES PER MM 57-20-21. 2 L 7 3 4F A3WE 1996020900686 19960209 00686 NM 1996 2 9 DL72S960289 1 19960203 A 5230 6556927102 SKIN BOEING 727 727232 1384082 NM CARGO DOOR GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 518DA 21469 DURING INSPECTION OF C-3 CARGO DOOR, A SMALL GOUGE WAS FOUND IN THE EXTERIOR SKIN. THE DAMAGE WAS REPAIRED PER SRM 52-0 0-3. 2 L 7 3 4F A3WE 1996020900687 19960209 00687 NM 1996 2 9 DL72S960291 1 19960206 A 3260 SENSOR BOEING 727 727232 1384082 NM RT MLG DIRTY A DALA O OTHER N FALSE WARNING CL CLIMB 1 SO 27 407DA 21151 ON GEAR RETRACTION, RED RT GEAR AND GREEN RT GEAR LIGHTS REMAINED ON. COMPLETED LDG GEAR RETRACTION MALFUNCTION CHECK L IST, BOTH LIGHTS REMAINED ON. ABOUT 40 SECONDS LATER, BOTH LIGHTS OUT. CHECKED AND CLEANED RIGHT MAIN LANDING GEAR DOW NLOCK, SENSOR OPERATION NORMAL. 2 L 7 3 4F A3WE 1996020900688 19960209 00688 WP 1996 2 9 DLL15960292 1 19960206 A 2720 CONTROL CABLE LKHEED 1011 10113853 5265020 WP RUDDER PEDAL JAMMED A DALA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 27 755DL 193Y1184 ON TAXI OUT - RUDDER PEDAL WOULD NOT MOVE LEFT - RIGHT MOVEMENT OK. FOUND CAPTAIN'S FORE/AFT RUDDER POSITION HAND CRANK MECHANISM JAMMED. FREED CABLE. OPERATION NORMAL. 2 L 7 3 4F A23WE 1996020900689 19960209 00689 1996 2 9 DLM88960279 4 19960206 A 2565 LANYARD D29982125 DOUG MD88 MD88 3023688 NM L1 DOOR SLIDE DETACHED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 904DE 2056 53409 L1 DOOR GIRT BAR HARD TO OPERATE. FOUND SLIDE PACK LANYARD DETACHED FROM SLIDE. REMOVED AND REPLACED SLIDE ASSY. 2 L 7 2 4F RT A6WE 1996020900690 19960209 00690 NM 1996 2 9 DLM88960280 1 19960206 A 3260 DNLOCK SWITCH H141016 DOUG MD88 MD88 3023688 NM NLG FAILED A DALA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 SO 27 984DL 53311 NLG GREEN LIGHT DID NOT ILLUMINATE WITH GEAR HANDLE EXTENDED. NLG WAS UP AND RED LIGHT WAS NOT ON. AFTER 2 ANNUN/OIG L IGHT TESTS, GREEN LIGHT ILLUMINATED NORMALLY. REMOVED AND REPLACED S1-412 NLG DOWN AND LOCKED SWITCH. JACKED AND SWUNG NLG SEVERAL TIMES, ALL INDICATIONS NORMAL. 2 L 7 2 4F RT A6WE 1996020900691 19960209 00691 WP 1996 2 9 MWEA96038 1 19960207 A 2560 5917689103 SLIDE COVER DOUG DC9 DC932 3022066 WP FWD ENTRY DOOR FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 602ME 48133 CREW REPORTS MAIN ENTRANCE DOOR EVACUATION SLIDE COVER FELL OFF. REINSTALLED SLIDE COVER. RETURNED A/C TO SERVICE. 2 L 7 2 4F A6WE 1996020900692 19960209 00692 NM 1996 2 9 UPS405373 1 19960131 A 5330 SKIN BOEING 747 747121 1384871 NM BS 1720 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN FOR C-CHECK IN AMS, MAINTENANCE REPORTED, CORROSION AT B.S. 1720 LT STR 34 AT LAP SPLICE. OUT OF LIMITS I.A.W. 53-30-01, REPAIRED PER SRM 53-30-03, FIG. 17. 2 L 7 4 4F A20WE 1996020900693 19960209 00693 NM 1996 2 9 UPS405386 1 19960202 A 5320 SHEAR TIE BOEING 747 747121 1384871 NM BS 1840 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN FOR C-CHECK, AT AMS, MAINTENANCE REPORTED, FOUND CRACK IN SHEAR-TIE AT B.S. 1840 BETWEEN STR 48-47 LT. REPAIRE D PER SRM 53-10-04, FIG. 3. 2 L 7 4 4F A20WE 1996020900694 19960209 00694 NM 1996 2 9 UPS405387 1 19960202 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 980 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN FOR C-CHECK, AT AMS, MAINTENANCE REPORTED, CORROSION IN STR 42 RT, STA 980. OUT OF LIMITS, REPLACED STR 42 I.A .W. SRM 53-10-03, FIG. 1. 2 L 7 4 4F A20WE 1996020900695 19960209 00695 NM 1996 2 9 UPS405388 1 19960202 A 5344 HINGES BOEING 747 747121 1384871 NM BS 820/840 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN FOR C-CHECK, AT AMS, MAINTENANCE REPORTED, CORROSION ON CEC DR. HINGE FITTINGS STA 820/840, LBL 15. REPLACED F ITTINGS PER SRM 51-40-04. 2 L 7 4 4F A20WE 1996020900696 19960209 00696 NM 1996 2 9 UPS405389 1 19960201 A 5347 CARGO TRACK BOEING 747 747121 1384871 NM BS 1750-1770 OUT OF LIMITS A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN FOR C-CHECK, AT AMS, MAINTENANCE REPORTED, FOUND EXISTING BLEND-OUTS IN CARGO TRACK OUT OF LIMITS PER SRM 51-10 -01 AT LBL 25 BETWEEN B.S. 1750 AND 1770. REPAIRED PER SRM 53-10-05, FIG. 5. 2 L 7 4 4F A20WE 1996020900697 19960209 00697 NM 1996 2 9 UPS405390 1 19960202 A 5320 STIFFENERS BOEING 747 747121 1384871 NM BS 1780/1740 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN FOR C-CHECK, AT AMS, MAINTENANCE REPORTED, FOUND CRACKS IN STIFFENERS OF FRAME WEB UPPER CHORD AT B.S 1780 RBL AND LBL 14, AND B.S. 1740, RBL AND LBL 14. REPLACED STIFFENERS PER SRM 53-30-02. 2 L 7 4 4F A20WE 1996020900698 19960209 00698 NM 1996 2 9 UPS605374 1 19960205 A 2432 BATTERY CHARGER BOEING 767 76734AF 1385212 NM APU INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 301UP 27239 MAINTENANCE REPORTED, APU BATTERY CHARGER INOPERATIVE. TRIPS CIRCUIT BREAKER AT P33 PNL. DEFERRED PER MEL I.A.W. 24-31 -2. 2 L 7 2 4F RT A1NM 1996020900700 19960209 00700 WP 1996 2 9 UPS805376 1 19960108 A 5320 DOUBLER DOUG DC8 DC871F 302199D WP FS 72 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, F.S. 72 JACK PAD DOUBLER HAS CORROSION. REPLACED DOUBLER PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996020900701 19960209 00701 WP 1996 2 9 UPS805377 1 19960108 A 5320 ANGLE DOUG DC8 DC871F 302199D WP FS 1040 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, HEAVY CORROSION ON VERT. SUPPORT ANGLE FORWARD SIDE, F.S. 1040 LONGERON 27R. REPLACED ANGLE PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996020900702 19960209 00702 WP 1996 2 9 UPS805378 1 19960103 A 5320 FITTING DOUG DC8 DC871F 302199D WP FS 1220/1260 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, 2 EACH FITTINGS CRACKED AT FORWARD END, F.S. 1220, LONGERON 17R, AND F.S. 12 60, LONGERON 18R. REPLACED FITTINGS PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996020900703 19960209 00703 WP 1996 2 9 UPS805379 1 19960114 A 5712 RIBS DOUG DC8 DC871F 302199D WP WS 138/328 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, RT WING L/E 2 EACH RIBS CRACKED AT STA XFS138, XFS 328. REPAIRED RIBS PER M M 27-00-00, FIG. 801. 2 L 7 4 4F RT 4A25 1996020900704 19960209 00704 WP 1996 2 9 UPS805380 1 19960109 A 5712 RIBS DOUG DC8 DC871F 302199D WP RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, RT WING L/E ASSY, 8 EACH, RIBS CRACKED AT STA XFS 841, 836, 817, 797, 771, 6 52, 620, AND 626. REPAIRED RIBS PER MM 57-00-00, FIG. 801. 2 L 7 4 4F RT 4A25 1996020900705 19960209 00705 WP 1996 2 9 UPS805381 1 19960109 A 5712 RIBS DOUG DC8 DC871F 302199D WP RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, RT WING L/E ASSY, 8 EACH, RIBS CRACKED AT STA. XFS 608, 596, 871, 827, 803, 785, 779, AND 749. REPAIRED RIBS PER MM 57-00-00, FIG. 801. 2 L 7 4 4F RT 4A25 1996020900706 19960209 00706 WP 1996 2 9 UPS805382 1 19960114 A 5320 FITTING DOUG DC8 DC871F 302199D WP FS 1230 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, B/T FITTING CRACKED AT F.S. 1230, BETWEEN LONGERONS 33R-34R. REPLACED FITTI NG PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996020900707 19960209 00707 WP 1996 2 9 UPS805383 1 19960114 A 5720 WEB DOUG DC8 DC871F 302199D WP RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, RT WING L/E LOWER SURFACE CRACKED IN WEB BETWEEN STA. XFS 608-614. REPAIRED WEB PER SRM 57-2-0. 2 L 7 4 4F RT 4A25 1996020900708 19960209 00708 WP 1996 2 9 UPS805384 1 19960114 A 5712 RIBS DOUG DC8 DC871F 302199D WP LT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, LT WING L/E, 3 EACH, RIBS CRACKED AT STA. XFS 767, 846, 679. REPAIRED RIBS PER MM 57-00-00, FIG. 801. 2 L 7 4 4F RT 4A25 1996020900709 19960209 00709 WP 1996 2 9 UPS805385 1 19960110 A 5320 FITTINGS DOUG DC8 DC871F 302199D WP FS 940/960 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, T-FITTINGS, 2 EACH, CRACKED AT KEEL BEAM, CRACKED F.S. 940 AND 960. REPLACE D FITTINGS PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1996020900710 19960209 00710 WP 1996 2 9 UPS805391 1 19960109 A 5311 BELT FRAME DOUG DC8 DC871F 302199D WP FS 1440 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, BELT FRAME CRACKED ON FORWARD SIDE F.S. 1440, LONGERON 23R. REPAIRED PER SR M 53-2-0. 2 L 7 4 4F RT 4A25 1996020900711 19960209 00711 WP 1996 2 9 UPS805392 1 19960114 A 5320 FITTING DOUG DC8 DC871F 302199D WP FS 1200 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CRACKED FITTING F.S. 1200, BETWEEN LONGERONS 33R AND 34R. REPLACED FITTING P ER SRM 53-1-0. 2 L 7 4 4F RT 4A25 1996020900712 19960209 00712 WP 1996 2 9 UPS805393 1 19960121 A 5313 LONGERONS DOUG DC8 DC871F 302199D WP FS 250-310 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, LONGERONS CRACKED TOP O/B FLANGE, F.S 260. REPLACED LONGERON, SECTION F.S. 250-310, PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996020900713 19960209 00713 WP 1996 2 9 UPS805394 1 19960114 A 5313 LONGERONS DOUG DC8 DC871F 302199D WP FS 1230 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, B/T FITTING CRACKED F.S. 1230, BETWEEN LONGERONS 33R-34R. REPLACED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996020900714 19960209 00714 WP 1996 2 9 UPS805395 1 19960108 A 5753 CANOE FITTING DOUG DC8 DC871F 302199D WP WS 428 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, RT WING NR 5 FLAP SUPPORT CANOE FITTING CRACKED UPPER FORWARD FASTENER HOLE, STA 428. REPLACED FITTING PER MM 27-51-12. 2 L 7 4 4F RT 4A25 1996020900715 19960209 00715 WP 1996 2 9 UPS805396 1 19960110 A 5314 KEEL BEAM DOUG DC8 DC871F 302199D WP FS 940 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, KEEL BEAM SPLICED RT SIDE CRACKED AT F.S. 940. REPLACED SPLICE PER SRM 51-3 -0. 2 L 7 4 4F RT 4A25 1996020900716 19960209 00716 WP 1996 2 9 UPS805397 1 19960108 A 5313 LONGERONS DOUG DC8 DC871F 302199D WP FS 260-270 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, LONGERONS CRACKED 35L, F.S. 260-270. REPLACED LONGERON SECTION F.S. 250-310 PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996021300001 19960213 00001 NM 1996 2 13 96FDEA00091 1 19960119 A 5753 SKIN BOEING 727 727233 138408A NM LT TE AFT FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 LT WING O/B AFT FLAP DELAMINATED 14 INCHES FROM O/B END T/E. REPAIRED PER SRM 51-40-06. 2 L 7 3 4F RT A3WE 1996021300002 19960213 00002 NM 1996 2 13 96FDEA00092 1 19960119 A 5753 TE SKIN BOEING 727 727233 138408A NM LT TE FOREFLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 LT WING I/B FOREFLAP I/B TRAILING EDGE HAS DELAMINATED AREA, MARKED. REPAIRED PER SRM 51-40-6. 2 L 7 3 4F RT A3WE 1996021300006 19960213 00006 NM 1996 2 13 DL72S960283 1 19960206 A 5755 ANGLE BOEING 727 727232 1384082 NM NR 7 SPOILER CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 484DA 20864 FOUND ON B1 LETTER CHECK, NR 7 SPOILER ATTACH CASTING CRACKED AT LOWER WING ATTACH. REPAIRED PER MM 57-20-22. 2 L 7 3 4F A3WE 1996021600007 19960216 00007 WP 1996 2 16 ASAA9680039 1 19960127 A 5210 MECHANISM DOUG DC9 DC983 3022083 WP L1 DOOR LACK OF LUBE A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 974AS 53450 ANC - FLT 112 - AFTER ARRIVAL, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN. CLEANED AND LUBRICATED DOOR MECHANISM A ND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 1996021600008 19960216 00008 WP 1996 2 16 ASAA9680040 1 19960129 A 5210 49157461 TUBE ASSY DOUG DC9 DC982 3022082 WP R1 DOOR BROKEN A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 957AS 49126 SEA - FLT 92 - AFTER ARRIVAL, CREW REPORTED THE R1 DOOR WOULD NOT OPEN. FOUND LOWER SEAL ACTUATOR TUBE ROD END BROKEN. REPLACED TUBE ASSEMBLY AND ADJUSTED ROD END AND OPERATED NORMALLY. (X) 2 L 7 2 4F A6WE 1996021600009 19960216 00009 EA 1996 2 16 HNAA9690304 1 19960113 A 3230 155507 LOCK ACTUATOR MENASCO DHAV DHC7 DHC7102 2802708 EA LT MLG FAILED A HNAA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 EA 07 903HA 7729 MC094 061 DCA/PHL - FLT 3098 - AFTER TAKEOFF WHEN LANDING GEAR WAS SELECTED UP, THE LEFT MAIN GEAR WOULD NOT FULLY RETRACT. THE A IRCRAFT TURNED BACK TO DCA AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE LEFT MLG LOCK ACTUATOR. (X) 2 H 7 4 4T A20EA 1996021600010 19960216 00010 NM 1996 2 16 HNAA9691406 1 19960117 A 3260 SENSOR TARGET DHAV DHC8 DHC8102 2809003 NM NLG DETACHED A HNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 07 914HA 53 MIA/EYW - FLT 3042 - AFTER TAKEOFF, THE NOSE GEAR DOOR AMBER LIGHT REMAINS ON AFTER GEAR RETRACTION. THE CREW CYCLED TH E GEAR, LIGHT REMAINED ILLUMINATED. THE AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT INCIDENT. THE NOSE GEAR DOOR POSIT ION SENSOR TARGET WAS FOUND DETACHED. REINSTALLED SAME. OPS CHECK GOOD. (X) 2 H 7 2 4T RT A13NM 1996021600011 19960216 00011 NM 1996 2 16 HNAA9693802 1 19960110 A 2910 HYD RESERVOIR DHAV DHC8 DHC8102 2809003 NM NR 2 SYSTEM REQUIRED SERVICE A HNAA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 EA 07 938HA 152 SBY/LYN - FLT EN14 - AFTER TAKEOFF WHEN LANDING GEAR WAS SELECTED UP, THE NR 2 HYDRAULIC PUMP CAUTION LIGHT ILLUMINATED THEN WENT OUT. UPON GEAR DOWN SELECTION, THE GEAR WOULD NOT EXTEND AND THE RIGHT FORWARD DOOR ONLY OPENED HALF WAY. PE RFORMED ALTERNATE GEAR EXTENSION AND RETURNED TO SBY WITHOUT INCIDENT. BLED NR 2 HYDRAULIC SYSTEM RESERVOIR AND SWUNG T HE GEAR. (X) 2 H 7 2 4T RT A13NM 1996021600012 19960216 00012 NM 1996 2 16 HNAA9697505 1 19960112 A 3231 RETRACT MECH DHAV DHC8 DHC8102 2809003 NM LANDING GEAR OUT OF ADJUST A HNAA K NONE J WARNING INDICATION CL CLIMB 1 EA 07 975HA 176 ORF\PHF - FLT 71 - AFTER TAKEOFF, LEFT REAR AND CENTER MLG DOORS WILL NOT CLOSE COMPLETELY FOLLOWING GEAR RETRACTION. T HE AIRCRAFT CONTINUED ON TO PHF AND LANDED WITHOUT INCIDENT. FOUND GEAR DOORS OUT OF RIG, RIGGED AS REQUIRED. (X) 2 H 7 2 4T RT A13NM 1996021600013 19960216 00013 WP 1996 2 16 IXXA9602 1 19960114 A 7933 WIRE DOUG DC8 DC863 302198A WP NR 3 ENGINE DAMAGED A IXXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 788AL 45999 SJU - ON CLIMB-OUT, NOTED THE NR 3 ENGINE WAS DISPLAYING AN ABNORMALLY HIGH OIL TEMPERATURE. THE NR 3 ENGINE WAS PRECAU TIONARILY SHUT DOWN, AND THE AIRCRAFT RETURNED TO SJU FOR MAINTENANCE. SJU MAINTENANCE DETERMINED A WIRING DEFECT AT TH E NR 3 OIL TEMP INDICATOR WAS CAUSING AN ERRONEOUSLY HIGH OIL TEMPERATURE INDICATION. THE DAMAGED WIRE WAS REPLACED, AN D THE ENGINE RUN TO CONFIRM NORMAL OIL TEMP INDICATION. (X) 2 L 7 4 4F 4A25 1996021600018 19960216 00018 SW 1996 2 16 MALA964790 1 19960101 A 3260 2782186057 POSITION IND SWRNGN SA227 SA227AC 8780603 SW RT MLG MALFUNCTIONED A MALA O OTHER O OTHER AP APPROACH 1 GL 15 2692P AC658B MSP - FLT 3448 - DURING APPROACH TO MSP, CREW NOTED RT MAIN GEAR DOWN AND LOCKED LIGHT WAS INTERMITTENTLY INOPERATIVE. T HE AIRCRAFT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE LANDING GEAR POSITION INDI CATOR. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 1 L 7 2 4T A8SW 1996021600019 19960216 00019 NM 1996 2 16 MALA964808 1 19960106 A 2913 570347 HYDRAULIC PUMP DHAV DHC8 DHC8102 2809003 NM LT ENGINE FAILED A MALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 15 816MA 231 FLT 3341 - IN CRUISE FLIGHT, THE NR 1 ENGINE HYDRAULIC PUMP CAUTION LIGHT ILLUMINATED. THE CREW PERFORMED QUICK REFEREN CE PROCEDURES AND CONTINUED TO DTW. MAINTENANCE REPLACED THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP. SYSTEM OPERATED SATISF ACTORILY. (X) 2 H 7 2 4T RT A13NM 1996021600020 19960216 00020 NM 1996 2 16 MALA964809 1 19960107 A 3610 7821004 SWITCH DHAV DHC8 DHC8102 2809003 NM LT WING FAILED A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 846MA 344 FLT 3127 - IN CRUISE FLIGHT, THE NR 1 AND NR 2 BLEED HOT LIGHTS CAME ON INTERMITTENTLY. THE AIRCRAFT RETURNED TO DTW. M AINTENANCE REPLACED THE LEFT PRESSURE SWITCH. SYSTEM OPERATED SATISFACTORILY. (X) 2 H 7 2 4T RT A13NM 1996021600021 19960216 00021 SW 1996 2 16 MALA964810 1 19960107 A 5753 2736003001 RIB SWRNGN SA227 SA227AC 8780603 SW LT TE FLAP CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 63NE AC763B MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE PERSONNEL NOTED A CRACK IN THE LT FLAP END RIB. THEY REPLACED THE END RIB IAW FAC SRM 51-00-00. (X) 1 L 7 2 4T A8SW 1996021600022 19960216 00022 SW 1996 2 16 MALA964811 1 19960107 A 5320 2722085 DOOR FRAME SWRNGN SA227 SA227AC 8780603 SW CARGO COMPT CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 63NE AC763B MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE PERSONNEL NOTED A CRACK IN THE FUSELAGE FORWARD CARGO DOOR FRAME. THEY REPAIRED THE CRACK BY REMOVING THE CRACKED AREA AND INSTALLING DOUBLERS IAW FAC ARP 53-20-9503. (X) 1 L 7 2 4T A8SW 1996021600023 19960216 00023 1996 2 16 MALA964812 4 19960108 A 3416 28702502 ALTIMETER SWRNGN SA227 SA227AC 8780603 SW LT COCKPIT INOPERATIVE A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 442MA AC725 MSP - FLT 3002 - AFTER TAKEOFF FROM MSP, THE CAPTAIN'S ALTIMETER, ALTITUDE ALERTER, TCAS, AND TRANSPONDER MODE 'C' FLAGG ED INOPERATIVE. THE AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE NR 1 ALTI METER. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 1 L 7 2 4T A8SW 1996021600024 19960216 00024 SW 1996 2 16 MALA964813 1 19960108 A 3230 RETRACT MECH SWRNGN SA227 SA227AC 8780603 SW NLG MALFUNCTIONED A MALA K NONE O OTHER CL CLIMB 1 GL 15 2692P AC658B MQT/MSP - FLT 3487 - AFTER DEPARTURE FROM MQT, THE NOSE GEAR WOULD CYCLE UP AND DOWN AFTER GEAR WAS RETRACTED. THE AIRC RAFT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL INSPECTED THE RIGGING OF THE LANDING GEAR SWIT CHES, BUT WERE UNABLE TO DUPLICATE THIS DISCREPANCY. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 1 L 7 2 4T A8SW 1996021600025 19960216 00025 NM 1996 2 16 MALA964814 1 19960110 A 3350 10005511 LAMP EMERG EXIT DHAV DHC8 DHC8102 2809003 NM COCKPIT INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 865MA 364 DTW - FLT 3152 - DURING PRE-FLIGHT INSPECTION IN DTW, CREW NOTED THE COCKPIT EMERGENCY LIGHT WAS INOPERATIVE. MAINTENAN CE PERSONNEL REPLACED THE LIGHT. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 2 H 7 2 4T RT A13NM 1996021600026 19960216 00026 SW 1996 2 16 MALA964816 1 19960108 A 2820 VENT LINE SWRNGN SA227 SA227AC 8780603 SW LEFT KINKED A MALA K NONE O OTHER DE DESCENT 1 GL 15 436MA AC719B DTW - FLT 3359 - INBOUND TO DTW, THE CREW NOTED FUEL WOULD NOT TRANSFER FROM LEFT TO RIGHT. THE AIRCRAFT CONTINUED TO D TW AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED A KINKED VENT LINE AT THE LT NACA VENT. ALL SYSTEMS OPE RATED SATISFACTORILY. (X) 1 L 7 2 4T A8SW 1996021600027 19960216 00027 NM 1996 2 16 MALA964817 1 19960110 A 7722 10168N01T00 ITT INDICATOR DHAV DHC8 DHC8102 2809003 NM NR 1 ENGINE INTERNAL FAULT A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 854MA 357 DTW - FLT 3106 - AFTER DEPARTURE FROM DTW, THE NR 1 ITT GAUGE BEGAN FLUCTUATING AND READ 300 DEGREES LESS THAN NR 2. TH E AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE NR 1 ITT INDICATOR. ALL SYS TEMS OPERATED SATISFACTORILY. (X) 2 H 7 2 4T RT A13NM 1996021600029 19960216 00029 EU 1996 2 16 RAIA960102 1 19960109 A 5270 91SE13 SWITCH BAG JETSTM JETSTM3201 1500217 EU PAX DOOR DIRTY A RAIA O OTHER J WARNING INDICATION CR CRUISE 1 CE 03 340TE 7726 939 STL - FLT 7075 - PASSENGER DOOR WARNING ILLUMINATED. MAINTENANCE DEFERRED PASSENGER DOOR WARNING LIGHT PER MEL 52-2 CAT C. MAINTENANCE CLEANED PASSENGER DOOR HANDLE MICROSWITCH, OPERATIONAL CHECK GOOD, DMI CLEARED. (X) 2 L 7 2 4T RT A56EU 1996021600030 19960216 00030 EU 1996 2 16 RAIA960103 1 19960103 A 3260 9005EN38 SWITCH BAG JETSTM JETSTM3201 1500217 EU RT MLG OUT OF ADJUST A RAIA O OTHER N FALSE WARNING CL CLIMB 1 CE 03 432AM 10247 883 STL - FLT 7082 - RIGHT MAIN GEAR INTRANSIT LIGHT WOULD NOT EXTINGUISH AFTER GEAR RETRACTION. MAINTENANCE ADJUSTED RIGHT MAIN GEAR UPLOCK SWITCH AND SERVICED RT MLG STRUT, GEAR SWING OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4T RT A56EU 1996021600031 19960216 00031 EU 1996 2 16 RAIA960104 1 19960104 A 3222 B00A70356A STRUT BAG JETSTM JETSTM3201 1500217 EU NLG REQUIRED SERVICE A RAIA O OTHER J WARNING INDICATION CL CLIMB 1 CE 03 338TE 8038 2199 932 STL - FLT 7054 - LANDING GEAR HANDLE LOCKED IN DOWN POSITION. MAINTENANCE SERVICED NOSE STRUT, GEAR SWING OPERATIONAL C HECK GOOD. (X) 2 L 7 2 4T RT A56EU 1996021600032 19960216 00032 EU 1996 2 16 RAIA960106 1 19960105 A 2612 51224127 FIRE LOOP BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA F ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 343TE 7198 955 STL - FLT 7442 - RIGHT ENGINE FIRE WARNING ON RUNWAY BEFORE TAKEOFF, FLIGHT CREW FIRED FIRE BOTTLES AND EVACUATED AIRCRA FT. MAINTENANCE INSPECTED ENGINE AND FOUND NO EVIDENCE OF FIRE, MAINTENANCE THEN REMOVED AND REPLACED ZONE 1 FIRE LOOP, OPERATONAL CHECK GOOD. (X) 2 L 7 2 4T RT A56EU 1996021600033 19960216 00033 NE 1996 2 16 RAIA960109 2 19960107 A 7260 31044158 GARLOCK SEAL JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE LT STARTER FAILED A RAIA E ENGINE SHUTDOWN Y K J ENGINE STOPPAGE FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 03 551HK 4521 41040 76100 STL - FLT 7535 - LOST OIL PRESSURE ON LEFT ENGINE. ENGINE SHUT DOWN. REPLACED STARTER GARLOCK SEAL. LEAK CHECKED GOOD . ENGINE TT, 4,520.7 HOURS. (X) 2 L 7 2 4T 4 T RT A41NM E18NE 1996021600034 19960216 00034 EU 1996 2 16 RAIA960110 1 19960107 A 3260 9005EN38 UPLOCK SWITCH BAG JETSTM JETSTM3201 1500217 EU LT MLG FAILED A RAIA O OTHER N FALSE WARNING CL CLIMB 1 CE 03 423AM 10685 858 STL - FLT 7372 - LEFT MAIN GEAR INTRANSIT LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. REPLACED UPLOCK SWITCH. (X ) 2 L 7 2 4T RT A56EU 1996021600035 19960216 00035 EU 1996 2 16 RAIA960111 1 19960108 A 3411 1379260L420 PITOT LINE BAG JETSTM JETSTM3201 1500217 EU RT FWD FUSE ICED UP A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 430AM 10313 880 STL - FLT 7098 - FIRST OFFICER'S AIRSPEED INDICATOR INOPERATIVE, READS ZERO. MAINTENANCE REMOVED ICE FROM PITOT LINE, O PERATIONAL CHECK GOOD. (X) 2 L 7 2 4T RT A56EU 1996021600036 19960216 00036 EU 1996 2 16 RAIA960113 1 19960111 A 7931 S7931000600000 LINE AEROSP ATR42 ATR42300 8680920 EU RT ENGINE CRACKED A RAIA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 03 426TE 11112 228 STL - FLT 7232 - LOW OIL PRESSURE INDICATION RIGHT ENGINE, SHUT DOWN ENGINE. AIRCRAFT LANDED WITHOUT INCIDENT IN PIA. M AINTENANCE REFLARED LINE AT OIL PRESSURE MANIFOLD BLOCK, PERFORMED GROUND RUNS, OPERATIONAL AND LEAK CHECKS GOOD, AIRCRA FT RELEASED. (X) 2 H 7 2 4T RT A53EU 1996021600037 19960216 00037 WP 1996 2 16 RAIA960114 2 19960110 A 7510 31998061 ANTI-ICE VALVE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UAR 01514 WP RT ENGINE FAULTY A RAIA O OTHER O OTHER CR CRUISE 1 CE 03 428AM 11616 28 877 66139 STL - FLT 7492 - RIGHT ENGINE ANTI-ICE FAILED IN-FLIGHT. CIRCUIT BREAKER WOULD NOT RESET. MAINTENANCE REPLACED RIGHT E NGINE ANTI-ICE VALVE, OPERATION CHECK GOOD. ENGINE TT, 8,557.8 HOURS. (X) 2 L 7 2 4T 4 T RT A56EU E4WE 1996021600038 19960216 00038 NE 1996 2 16 RAIA960115 2 19960111 A 7320 31059005 FUEL CONTROL JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE LT ENGINE OUT OF ADJUST A RAIA D C RETURN TO BLOCK ABORTED TAKEOFF O OTHER CL CLIMB 1 CE 03 553HK 1333 41066 75081 STL - FLT 7458 - LEFT ENGINE ACHIEVED ONLY 95 PERCENT TORQUE ON TAKEOFF. FLOWS SET TO 3, ENGINE ANTI-ICE ON. MAINTENAN CE ADJUSTED MAXIMUM FUEL FLOW. GROUND RUNS GOOD. ENGINE TT, 1,332.7 HOURS. (X) 2 L 7 2 4T 4 T RT A41NM E18NE 1996021600039 19960216 00039 EU 1996 2 16 RAIA960116 1 19960111 A 3213 B00A703031A STRUT BAG JETSTM JETSTM3201 1500217 EU LT MLG REQUIRED SERVICE A RAIA O OTHER J WARNING INDICATION CL CLIMB 1 CE 03 430AM 10169 4259 880 STL - FLT 7374 - LEFT MAIN GEAR WOULD NOT RETRACT. MAINTENANCE SERVICED LEFT MAIN STRUT. GEAR SWING OPERATION CHECKED GOOD. (X) 2 L 7 2 4T RT A56EU 1996021600040 19960216 00040 1996 2 16 RAIA960117 4 19960111 A 3418 C771075 LIFT TRANSDUCER BAG JETSTM JETSTM3201 1500217 EU RT WING FAILED A RAIA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 424AM 8566 865 STL - FLT 7300 - DURING TAXI OUT, STICK SHAKER ACTIVATED. MAINTENANCE REPLACED RIGHT LIFT TRANSDUCER. SYSTEM OPERATION AL CHECK GOOD. (X) 2 L 7 2 4T RT A56EU 1996021600041 19960216 00041 EU 1996 2 16 RAIA960118 1 19960113 A 2150 ASNA214407 CLAMP AEROSP ATR72 ATR72202 8680940 EU LT PACK VALVE FAULTY A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 721TE 217 PIA - FLT 7121 - ELECTRIC SMOKE WARNING IN AIR, RETURNED TO PIA AND EVACUATED AIRCRAFT. AIRCRAFT FERRY FLIGHT TO STL. M AINTENANCE REPLACED DEFECTIVE CLAMP ON PACK VALVE, OPERATIONAL CHECK OF SYSTEM GOOD. (X) 2 H 7 2 4T RT A53EU 1996021600042 19960216 00042 EU 1996 2 16 RAIA960119 1 19960114 A 7500 8961153 GASKET BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UAR 01514 WP LT ENGINE FAILED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 429AM 879 66321 STL - FLT 7260 - LEFT ENGINE WOULD NOT MAKE TARGET TORQUE. MAINTENANCE REPLACED P3 GASKETS, GROUND RUNS GOOD. ENGINE T T, 5,973.2 HOURS. (X) 2 L 7 2 4T 4 T RT A56EU E4WE 1996021600043 19960216 00043 NE 1996 2 16 RAIA960120 2 19960114 A 7320 32448554 HMU AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW124B NE LT ENGINE FAILED A A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 721TE 6149 217 STL - FLT 7166 - DURING TAKEOFF ROLL, NR 1 ENGINE WOULD NOT MAKE MORE THAN 39 PERCENT TORQUE. ALSO, LOAD SQUEAL FROM NR 1 ENGINE. MAINTENANCE REPLACED HMU, GROUND RUNS GOOD. ENGINE TT, 7,409.8 HOURS. (X) 2 H 7 2 4T 4 T RT A53EU E2ONE 1996021600044 19960216 00044 EU 1996 2 16 RAIA960123 1 19960115 A 3350 311701 POWER SUPPLY BAG JETSTM JETSTM3201 1500217 EU CABIN DIRTY A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 429AM 10315 879 STL - MX-2 - EMERGENCY LIGHTS IN CABIN INOPERATIVE. MAINTENANCE CLEANED CONNECTION ON FORWARD EMERGENCY LIGHTS POWER SU PPLY, SYSTEM OPERATION CHECK GOOD. (X) 2 L 7 2 4T RT A56EU 1996021600045 19960216 00045 EU 1996 2 16 RAIA960124 1 19960116 A 3350 311701 BATTERY PACK BAG JETSTM JETSTM3201 1500217 EU CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 425AM 10533 870 STL - MX - ALL CENTER ISLE EMERGENCY LIGHTS ARE OUT. MAINTENANCE REPLACED NR 3 EMERGENCY LIGHT BATTERY PACK, SYSTEM OPE RATION CHECK GOOD. (X) 2 L 7 2 4T RT A56EU 1996021600046 19960216 00046 NE 1996 2 16 RAIA960125 2 19960114 A 7320 6945059010 TT2 SENSOR JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE RT ENGINE FAILED A RAIA O OTHER J WARNING INDICATION CL CLIMB 1 CE 03 552HK 1660 41057 76077 JFK - FLT 7731 - IEC CAPTION ILLUMINATED IN-FLIGHT, WOULD NOT RESET. MAINTENANCE REPLACED TT2 SENSOR, GROUND RUN GOOD. ENGINE TT, 1,659.7 HOURS. (X) 2 L 7 2 4T 4 T RT A41NM E18NE 1996021600047 19960216 00047 EU 1996 2 16 RAIA960126 1 19960116 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 426TE 228 STL - MX - TWO SECTIONS OF ESCAPE PATH LIGHTING INOPERABLE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES AT THE NR 1 AND NR 4 LOCATIONS. NR 1 AND NR 4 LOCATIONS, TT: 11,149.5 HOURS. (X) 2 H 7 2 4T RT A53EU 1996021600048 19960216 00048 EU 1996 2 16 RAIA960127 1 19960116 A 5270 DOOR LIGHT BAG JETSTM JETSTM3201 1500217 EU BAGG COMPT ILLUMINATED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 435AM 889 STL - FLT 7178 - ABORTED TAKEOFF DUE TO POD DOOR LIGHT ILLUMINATING. MAINTENANCE CYCLED POD DOOR, COULD NOT DUPLICATE D ISCREPANCY. OPERATION CHECK GOOD. (X) 2 L 7 2 4T RT A56EU 1996021600049 19960216 00049 EU 1996 2 16 RAIA960128 1 19960117 A 2150 6411343 SWITCH AEROSP ATR42 ATR42300 8680920 EU RT PACK FAILED A RAIA O OTHER O OTHER CL CLIMB 1 CE 03 426TE 9606 228 STL - FLT 7400 - RIGHT PACK VALVE FAULTED AND WOULD NOT RESET. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE THERMAL SW ITCH. OPERATIONAL CHECK GOOD. (X) 2 H 7 2 4T RT A53EU 1996021600050 19960216 00050 EU 1996 2 16 RAIA960129 1 19960117 A 7712 31024766 TQ SIGNAL COND BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 429AM 5466 4266 879 STL - FLT 7072 - LEFT ENGINE ONLY MADE 80 PERCENT TORQUE. MAINTENANCE REPLACED LEFT TORQUE SIGNAL CONDITIONER, GROUND R UNS GOOD. (X) 2 L 7 2 4T RT A56EU 1996021600051 19960216 00051 EU 1996 2 16 RAIA960130 1 19960118 A 2731 S2738197100400 TRIM ROD AEROSP ATR42 ATR42300 8680920 EU ELEV TRIM ICED UP A RAIA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 CE 03 426TE 11160 228 FYV - FLT 7407 - AFTER TAKEOFF, NOSE PITCHED UP. TRIMMED NOSE TO FULL DOWN LIMITS, AIRCRAFT WAS SLOW TO CLIMB OUT. MAI NTENANCE INSPECTED TAIL AND FOUND ICE ON ELEVATOR TRIM RODS. DEICED AIRCRAFT, RAN TRIM FULL TRAVEL, AND INSPECTED CABLE S, OPERATIONAL CHECK NORMAL. (X) 2 H 7 2 4T RT A53EU 1996021600052 19960216 00052 EU 1996 2 16 RAIA960131 1 19960120 A 7332 1153000 SWITCH AEROSP ATR72 ATR72202 8680940 EU RT ENGINE DIRTY A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 721TE 2750 217 SGF - FLT 7018 - RIGHT ENGINE FEED 'LOW' LIGHT ILLUMINATED. MAINTENANCE REMOVED, CLEANED, AND REINSTALLED RIGHT LOW PRE SSURE SWITCH. OPERATIONAL CHECK GOOD ON GROUND RUNS. (X) 2 H 7 2 4T RT A53EU 1996021600053 19960216 00053 WP 1996 2 16 RAIA960133 2 19960119 A 7320 89778025 FUEL CONTROL BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UAR 01514 WP LT ENGINE OUT OF ADJUST A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 434AM 7851 3609 887 66295 BMI - FLT 7325 - LEFT ENGINE RPM WOULD NOT COME ABOVE 98.5 PERCENT - 99 PERCENT ON TAKEOFF. FERRY FLIGHT TO STL. MAINT ENANCE ADJUSTED RPM, GROUND RUNS GOOD. ENGINE TT, 6,994.1 HOURS. (X) 2 L 7 2 4T 4 T RT A56EU E4WE 1996021600054 19960216 00054 1996 2 16 RAIA960134 4 19960120 A 3414 39948132236 AIRSPEED IND BAG JETSTM JETSTM3201 1500217 EU RT COCKPIT FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 433AM 7893 885 ALO - FLT 7414 - FIRST OFFICER'S AIRSPEED INDICATOR INOPERATIVE. FERRY FLIGHT TO STL. MAINTENANCE REPLACED AIRSPEED IN DICATOR, OPERATION CHECK GOOD. (X) 2 L 7 2 4T RT A56EU 1996021600055 19960216 00055 1996 2 16 RAIA960135 3 19960121 A 6140 CAP LIGHT BAG JETSTM JETSTM3201 1500217 EU LEFT MALFUNCTIONED A RAIA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 CE 03 875JX 875 STL - FLT 7372 - LEFT REVERSE CAP LIGHT WOULD NOT EXTINGUISH. MAINTENANCE DEFERRED REV CAP LIGHT PER MEL. MAINTENANCE CLEARED DMI, PERFORMED OPERATIONAL CHECK REVERSE CAP LIGHT, OPS CHECKED GOOD DURING ROUND RUN. (X) 2 L 7 2 4T RT A56EU 1996021600056 19960216 00056 WP 1996 2 16 RAIA960136 2 19960121 A 7321 89778025 FUEL CONTROL BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UAR 01514 WP LT ENGINE OUT OF ADJUST A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 428AM 7612 3579 877 66170 STL - FLT 7058 - LEFT ENGINE WOULD ONLY ACHIEVE 97.5 PERCENT RPM. MAINTENANCE ADJUSTED SCREW 'X', PERFORMED GROUND RUNS , OPERATIONAL CHECK GOOD. ENGINE TT, 9,060.6 HOURS. (X) 2 L 7 2 4T 4 T RT A56EU E4WE 1996021600057 19960216 00057 EU 1996 2 16 RAIA960138 1 19960121 A 7332 FUEL PRESS LIGHT BAG JETSTM JETSTM3201 1500217 EU RIGHT ILLUMINATED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 03 425AM 870 STL - FLT 7308 - RIGHT FUEL RPESSURE LIGHT ILLUMINATED DURING TAKEOFF ROLL. MAINTENANCE ISSUED DMI 73-2. MAINTNANCE LA TER PRESSURE CHECKED SYSTEM AND CND, GROUND RUNS GOOD - CLEARED DMI. (X) 2 L 7 2 4T RT A56EU 1996021600058 19960216 00058 EU 1996 2 16 RAIA960139 1 19960124 A 5270 MS161065 SWITCH BAG JETSTM JETSTM3201 1500217 EU BAGG DOOR DIRTY A RAIA D RETURN TO BLOCK N FALSE WARNING CL CLIMB 1 CE 03 435AM 10181 889 STL - FLT 7506 - POD DOOR LIGHT ILLUMINATED IN-FLIGHT. MAINTENANCE CLEANED POD DOOR MICROSWITCH, POD DOOR WARNING SYSTE M OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A56EU 1996021600059 19960216 00059 EU 1996 2 16 RAIA960140 1 19960125 A 2420 10200311 GEN CONTL UNIT AEROSP ATR42 ATR42300 8680920 EU RT AVONICS LOOSE A RAIA D RETURN TO BLOCK O OTHER CR CRUISE 1 CE 03 426TE 12009 8460 228 STL - FLT 7180 - RIGHT GENERATOR FAULTED IN-FLIGHT, WILL NOT RESET. MAINTENANCE RERACKED RIGHT GENERATOR CONTROL UNIT, PERFORMED GROUND RUNS, OPERATIONAL CHECK GOOD. (X) 2 H 7 2 4T RT A53EU 1996021600060 19960216 00060 EU 1996 2 16 RAIA960141 1 19960123 A 3350 3011151 BATTERY AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 422TE 106 STL - MX - ALL EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES, OPS CHECK GOOD. TOP FWD TT: 16,645.5. BOTTOM FWD TT: 16,645.5. MID-TOP TT: 16,645.5. TOP AFT TT: 16,645.5. BOTTOM AFT TT: 16,645.5. MID-BOT TT: 16,645.5. (X) 2 H 7 2 4T RT A53EU 1996021600061 19960216 00061 EU 1996 2 16 RAIA960142 1 19960124 A 7332 1103P0645 PRESS SWITCH BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 03 425AM 2298 870 STL- FLT 7454 - RIGHT FUEL CAPTION ILLUMINATED ON TAKEOFF ROLL. MAINTENANCE PLACED ON DMI 73-2. MAINTENANCE LATER CLEA RED DMI BY REPLACING LOW FUEL PRESSURE SWITCH, GROUND RUNS GOOD. (X) 2 L 7 2 4T RT A56EU 1996021600064 19960216 00064 NM 1996 2 16 9503156309 1 19960207 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 669US 24224 DURING LINE CHECK, THE RIGHT BODY FAIRING EXTERIOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED POWER SUPPLY AND B ATTERY PACK, OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996021600065 19960216 00065 WP 1996 2 16 9603139307 1 19960206 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP TAIL CONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 309RC 48088 DURING LINE CHECK, FOUND TAIL CONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY AND CHECKS GOOD. 2 L 7 2 4F A6WE 1996021600066 19960216 00066 WP 1996 2 16 9603149966 1 19960207 A 2450 CIRCUIT BREAKER DOUG DC9 DC931 3022065 WP LT AC BUS DAMAGED A A NWAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 GL 01 9330 47138 DURING CLIMB, LEFT AC BUS CIRCUIT BREAKER POPPED. CREW RESET ALL THREE BREAKERS AND ONE POPPED AGAIN FIVE MINUTES LATER . POWER COULD NOT BE RESTORED TO LEFT AC BUS. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND L EFT AC BUS B-PHASE CIRCUIT BREAKER DAMAGED. REPLACED CIRCUIT BREAKER AND OPERATIONAL CHECK NORMAL ON ALL SYSTEMS DURING POWER CHECK. 2 L 7 2 4F A6WE 1996021600067 19960216 00067 NM 1996 2 16 9603162276 1 19960206 A 3350 BATTERY BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 276US 21155 DURING LINE CHECK, FOUND DOOR 1 LEFT EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY AND BATTERY, OPERATIONAL CHEC K OK. 2 L 7 3 4F A3WE 1996021600068 19960216 00068 NM 1996 2 16 9603172296 1 19960207 A 3350 BATTERY PACK BOEING 757 757251 1384970 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 296US 21788 DURING LINE CHECK, FOUND AFT GALLEY DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AND POWER SUPPLY, OPERATION AL CHECK OK. 2 L 7 2 4F RT A2NM 1996021600069 19960216 00069 NM 1996 2 16 9603185503 1 19960208 A 7334 FUEL PRESS SW BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE NR 2 ENGINE FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 503US 23192 716476 DURING TAKEOFF ROLL, NR 2 ENGINE FUEL FILTER MESSAGE APPEARED. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO GATE. MAIN TENANCE PERSONNEL REPLACED FUEL FILTER PRESSURE DIFFERENTIAL SWITCH AND OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F RT A2NM E17NE 1996021600070 19960216 00070 WP 1996 2 16 9603199882 1 19960207 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 670MC 47659 DURING LINE CHECK, AFT CABIN DOOR AND TAIL CONE EMERGENCY LIGHTS REPORTED DIM. REPLACED BATTERY POWER SUPPLY ASSEMBLY A ND OPERATIONAL CHECKS GOOD. 2 L 7 2 4F A6WE 1996021600071 19960216 00071 NE 1996 2 16 96FDEA00195 2 19960208 A 7321 7436025 FUEL CONTROL BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE FAILED A FDEA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 SO 25 220FE 20934 AT IDLE POWER NR 3 ENGINE FAILED TO RESPOND TO THROTTLE MOVEMENT. CONTINUED OPERATION UNTIL NR 3 GEN FAILED. ACCOMP EN GINE SHUTDOWN PROCEDURES IAW CHECKLIST PROCEDURES AND LANDING UNEVENTFUL. REMOVED AND REPLACED MAIN FUEL PUMP AND FUEL CONTROL UNITS AS PER MM 73-11-1 AND 73-21-1. TRIM RUN AND LEAK CHECK GOOD. RII COMPLIED WITH E/E NR 1208 FUEL PUMP (P/ N 378200) (S/N NR OFF 1201M). 2 L 7 3 4F 4 F RT A3WE E2EA 1996021600072 19960216 00072 NM 1996 2 16 96FDEA00196 1 19960209 A 2780 RETRACT MECH BOEING 727 72722 1384002 NM LE FLAPS FAILED A FDEA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 25 189FE 19082 DURING FLAP RETRACTION, L/E DEVICES FAILED TO RETRACT PROPERLY. ARRIVED WITH THE L/E DEVICES AND FLAP HANDLE IN THE 2 D EGREE POSITION AMBER LIGHT WAS STILL ON, NO GREEN LIGHT. CYCLED FLAPS AND OPS CHECK NORMAL. 2 L 7 3 4F A3WE 1996021600138 19960216 00138 WP 1996 2 16 ABXA9600185 1 19960207 A 3350 5708458503 BATTERY PACK DOUG DC8 DC862 3021970 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 805AX 45906 DURING PREFLIGHT INSPECTION, FOUND EMERGENCY EXIT LIGHT CONTROL CIRCUIT BREAKER POPPED. REPLACED EMERGENCY EXIT LIGHT B ATTERY PACK. EMERGENCY LIGHT SYSTEM OPS CHECKED GOOD IAW DC-8 MM. 2 L 7 4 4F 4A25 1996021600139 19960216 00139 SO 1996 2 16 COMA9610063 1 19960206 A 5720 120271450003 BRACKET EMB 120 EMB120RT SO LT WING CRACKED A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 161CA 120143 THE LEFT AILERON WAS STRUCK BY A GROUND VEHICLE. NO DAMAGE WAS FOUND ON THE AILERON. HOWEVER, THE BRACKET ON THE WING REAR SPAR, THAT THE AILERON SERVO TAB RODS ARE CONNECTED TO, WAS FOUND CRACKED. THE BRACKET WAS REPAIRED PER AERODESIGN REPORT NR 1783-1 REV IR, DATED 2-6-96. 2 L 7 2 4T RT A31SO 1996021600140 19960216 00140 SO 1996 2 16 COMA9610064 1 19960204 A 3260 INTRANSIT LIGHT EMB 120 EMB120RT SO LT MLG MALFUNCTIONED A COMA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 01 263CA 120255 LEFT MLG INTRANSIT LIGHT REMAINED ON WHEN LANDING GEAR EXTENDED. COULD NOT DUPLICTE DISCREPANCY. SUSPECT ICE ON LANDIN G GEAR. CLEANED LANDING GEAR. 2 L 7 2 4T RT A31SO 1996021600141 19960216 00141 SO 1996 2 16 COMA9610065 1 19960204 A 3230 12038594001 CONTROL BOX EMB 120 EMB120RT SO NLG DEFECTIVE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 200CD 11812 300 120200 NOSE LANDING GEAR INTRANSIT LIGHT REMAINED ON AFTER GEAR RETRACTION. REPLACED THE LANDING GEAR CONTROL ASSY. 2 L 7 2 4T RT A31SO 1996021600142 19960216 00142 SO 1996 2 16 COMA9610066 1 19960204 A 2750 RETRACT MECH EMB 120 EMB120RT SO TE FLAPS MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 257CA 120248 FLAP DISAGREEMENT WARNING WHEN FLAPS SELECTED UP AFTER TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. CLEANED FLAP TRACKS A ND ROLLER. 2 L 7 2 4T RT A31SO 1996021600143 19960216 00143 SO 1996 2 16 COMA9610067 1 19960205 A 6120 78249024 PCU EMB 120 EMB120RT SO LT PROP DEFECTIVE A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 247CA 9968 1757 120225 LEFT PROPELLER TAKES 15 SECONDS TO UNFEATHER. REPLACED THE PITCH CONTROL UNIT. 2 L 7 2 4T RT A31SO 1996021600144 19960216 00144 SO 1996 2 16 COMA9610068 1 19960205 A 3260 922AA2YA6PZ722 SENSOR EMB 120 EMB120RT SO NLG MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 200CD 120200 NOSE LANDING GEAR INTRANSIT LIGHT REMAINED ON AFTER RETRACTION. COUD NOT DUPLICATE DISCREPANCY. REPLACED A-SYSTEM PROX IMITY SENSOR, WHILE TROUBLESHOOTING. 2 L 7 2 4T RT A31SO 1996021600145 19960216 00145 SO 1996 2 16 COMA9610069 1 19960205 A 2752 3430001003 ACTUATOR EMB 120 EMB120RT SO RT TE FLAP DEFECTIVE A A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 254CA 120233 FLAP DISAGREEMENT WARNING WHEN FLAPS SELECTED UP AFTER TAKEOFF. REPLACED THE RT OUTBD FLAP ACTUATOR. 2 L 7 2 4T RT A31SO 1996021600146 19960216 00146 SO 1996 2 16 COMA9610070 1 19960207 A 3150 ATG120TR PROX SENSOR EMB 120 EMB120RT SO ELEV TRIM DEFECTIVE A COMA K NONE N FALSE WARNING TO TAKEOFF 1 SO 01 255CA 120238 TAKEOFF TRIM AURAL WARNING SOUNDED DURING TAKEOFF. TRIM WAS CONFIRMED IN THE GREEN BAND. REPLACED THE LT ELEVATOR TRIM PROXIMITY SENSOR. 2 L 7 2 4T RT A31SO 1996021600147 19960216 00147 NE 1996 2 16 COMA9610071 2 19960207 A 7311 10718D HEAT EXCHANGER EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE LEAKING A COMA K NONE K FLUID LOSS UK UNKNOWN 1 SO 01 267CA 12698 882 120259 LEFT ENGINE LEAKING FUEL. REPLACED THE FUEL TO OIL HEAT EXCHANGER. 2 L 7 2 4T 4 T RT A31SO E20NE 1996021600148 19960216 00148 NE 1996 2 16 COMA9610072 2 19960206 A 7310 12018198005 HOSE ASSY EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE LEAKING A COMA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 255CA 120238 RT ENGINE IS LEAKING FUEL. REPLACED THE MOTIVE FLOW FUEL RETURN HOSE AND FITTING AT THE ENGINE HMU, DUE TO DAMAGED THRE ADS. 2 L 7 2 4T 4 T RT A31SO E20NE 1996021600149 19960216 00149 SO 1996 2 16 COMA9610073 1 19960206 A 3150 CONNECTOR EMB 120 EMB120RT SO ELEV TRIM LOOSE A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 168CA 120168 TAKEOFF TRIM AURAL WARNING SOUNDED WHEN POWER ADVANCED FOR TAKEOFF. REPLACED LOOSE WIRING CONNECTIONS AT ELEVATOR TRIM PROXIMITY SENSORS. 2 L 7 2 4T RT A31SO 1996021600150 19960216 00150 NE 1996 2 16 COMA9630030 3 19960208 A 6114 660714200 PROP HUB R3544123F13 SAAB SF340 SF340A 7850100 EU ROTOL R354 R3544123F13 NE MOUNTING FLANGE DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 8352 2874 DRG828288 340A047 DRG828288 DURING AD93-19-01 INSPECTION, FLAW INDICATIONS WERE FOUND IN HUB REAR FACT MOUNTING FLANGE. PROPELLER WAS DISASSEMBLED AND HUB REMOVED FROM SERIVCE. 2 L 7 2 4T RT A52EU 6 C P61GL 1996021600151 19960216 00151 EU 1996 2 16 COMA9630031 1 19960206 A 3246 5006227 WHEEL SAAB SF340 SF340A 7850100 EU RT NLG DEPARTED A COMA K NONE D INFLIGHT SEPARATION LD LANDING 1 SO 01 320CA 5271 421 340A064 GRINDING NOISE COMING FROM NLG DURING TAKEOFF, LANDING, AND TAXI. THE RT NLG WHEEL ASSY DEPARTED AIRCRAFT DURING LANDIN G. PROBABLE CAUSE WAS BEARING FAILURE. REPLACED THE NLG WHEEL ASSY. 2 L 7 2 4T RT A52EU 1996021600152 19960216 00152 NE 1996 2 16 COMA9630032 2 19960207 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LEFT LOW POWER A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 359CA 2303 340A053 367205 LEFT ENGINE WILL NOT ACHIEVE TAKEOFF TORQUE. REPLACED THE LEFT ENGINE. 2 L 7 2 4T 4 T RT A52EU E8NE6 1996021600153 19960216 00153 EU 1996 2 16 COMA9630033 1 19960207 A 3150 004WS00 WEU SAAB SF340 SF340A 7850100 EU AVIONICS DEFECTIVE A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 358CA 14472 340A047 LEFT ENGINE INTAKE HEAT FAIL LIGHT CAME ON DURING FLIGHT. REPLACED DEFECTIVE WARNING ELECTRONIC UNIT. 2 L 7 2 4T RT A52EU 1996021600154 19960216 00154 1996 2 16 COMA9660025 4 19960201 A 3418 45150340 SENSOR CNDAIR CL600 CL6002B19 EA RIGHT DEFECTIVE A COMA K NONE O OTHER CR CRUISE 1 SO 01 951CA 7091 THERE IS A 25 KNOT DIFFERENCE BETWEEN THE GREEN LINE ON LT AND RT AIRSPEED INDICATORS. REPLACED THE RT AOA VANE. 2 L 7 2 4F RT A21EA 1996021600155 19960216 00155 EA 1996 2 16 COMA9660026 1 19960207 A 5610 601R332242 STRAP CNDAIR CL600 CL6002B19 EA RT WINDSHIELD LEAKING A COMA K NONE O OTHER CR CRUISE 1 SO 01 940CA 7048 COPILOTS WINDSHIELD IS LEAKING AIR. LOUD SQUEAL IS HEARD WHEN AIRCRAFT PRESSURIZED. RESEALED AND RETORQUED THE RT WIND SHIELD CONNECTING STRAP BETWEEN FRONT AND SIDE WINDSHIELD. 2 L 7 2 4F RT A21EA 1996021600156 19960216 00156 EA 1996 2 16 COMA9660027 1 19960207 A 2710 CONTROL CABLE CNDAIR CL600 CL6002B19 1900309 EA AILERON CONTL LACK OF LUBE A COMA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SO 01 945CA 7069 PILOTS AILERON CONTROLS SEEM TO BE EITHER LOOSE OR BINDING. INSPECTED AILERON CONTROL PATH AND FOUND NO DEFECTS. CLEAN ED AND LUBED AILERON CABLE PATH. 2 L 7 2 4F RT A21EA 1996021600157 19960216 00157 NM 1996 2 16 DL72S960290 1 19960207 A 5330 SKIN BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 495DA 21075 A .375 INCH CRACK AT F/O EYEBROW WINDOW LOWER FWD CORNER CUTOUT. FOUND DURING F-2 LTR CHECK TPAMM. REPAIRED PER SRM 53 -30-3. 2 L 7 3 4F A3WE 1996021600158 19960216 00158 1996 2 16 DL757960288 4 19960207 A 2320 ACARS PRINTER 700300000 BOEING 757 757232 1384965 NM COCKPIT SMOKING A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 685DA 330 27588 COCKPIT PRINTER STARTED TO SMOKE IN FLIGHT. PULLED CIRCUIT BREAKER S-5 AND SMOKE STOPPED. REPLACED ACARS PRINTER, CHEC KED OK AND ADDED NEW PAPER. 2 L 7 2 4F RT A2NM 1996021600162 19960216 00162 NM 1996 2 16 DLM88960299 1 19960207 A 5610 5912290505 WINDOW DOUG MD88 MD88 3023688 NM FLT DECK SHORTED A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 913DE 49956 CAPTAIN RECEIVED ELECTRIC SHOCK WHEN TOUCHING FRAME OF LEFT WINDSCREEN. REPLACED WINDOW AND CONTROLLER. 2 L 7 2 4F RT A6WE 1996021600163 19960216 00163 NM 1996 2 16 UPS205399 1 19960203 A 5320 ANGLE BOEING 727 72725C 138400H NM FS 804 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CRACK ON WEB TIE ANGLE AT STA 804 STR 10 RT. REPAIRED WEB AND FABRICATED TIE ANGLE. 2 L 7 3 4F A3WE 1996021600164 19960216 00164 NM 1996 2 16 UPS205400 1 19960205 A 5751 HINGE FITTING BOEING 727 72725C 138400H NM RT AILERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING O/B AILERON O/B HINGE FITTING IS CORRODED. REMOVED AND REPLACED AILE RON HINGE FITTING IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996021600165 19960216 00165 NM 1996 2 16 UPS205401 1 19960204 A 5751 HINGE FITTING BOEING 727 72725C 138400H NM RT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING O/B AILERON CENTER O/B HINGE FITTING IS CORRODED. REMOVED AND REPLAC ED AILERON HINGE FITTING IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996021600166 19960216 00166 NM 1996 2 16 UPS405402 1 19960203 A 5313 STRINGER BOEING 747 747121 1384871 NM FS 800 SCRATCHED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN FOR C-CHECK AT AMS MAINTENANCE REPORTED, FOUND SCRATCHES ON O/B TOP FLANGE STR 45 LT STA 800. REPLACED STR 45 FROM STA 790 TO 810 IAW SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 1996021600167 19960216 00167 NM 1996 2 16 UPS405403 1 19960202 A 5320 SHEAR TIE BOEING 747 747121 1384871 NM BS 1800 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN FOR C-CHECK AT AMS MAINTENANCE REPORTED, FOUND CRACK IN SHEAR TIE AT B-STA 1800 BETWEEN STR 48 TO 47 LT. REPAI RED AS REQUIRED PER SRM 53-10-04 FIG 3. 2 L 7 4 4F A20WE 1996021600168 19960216 00168 NM 1996 2 16 UPS405404 1 19960202 A 5320 SHEAR TIE BOEING 747 747121 1384871 NM BS 1820 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN FOR C-CHECK AT AMS MAINTENANCE REPORTED, CRACKED SHEAR TIE STA 1820 BETWEEN STR 50 TO 49 RT. REPAIRED AS REQUI RED PER SRM 53-10-04 FIG 3. 2 L 7 4 4F A20WE 1996021600169 19960216 00169 WP 1996 2 16 UPS805405 1 19960131 A 5320 FITTINGS DOUG DC8 DC871F 302199D WP FS 940/960 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, 2 FITTINGS ABOVE LONGERON 24 CRACKED FS 940 AND 960. REPLACED FITTINGS PER S RM 51-1-20D. 2 L 7 4 4F RT 4A25 1996021600170 19960216 00170 WP 1996 2 16 UPS805406 1 19960128 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 501 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING L/E UPPER RIBS CRACKED AT STA XFS 501. REPAIRED PER MM 57-00-00 FIG 801. 2 L 7 4 4F RT 4A25 1996021600171 19960216 00171 WP 1996 2 16 UPS805407 1 19960127 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT WING L/E ASSY HAS 8 RIBS CRACKED AT STA XFS 691, 672, 666, 660, 647, 641, 635 AND 629. REPAIRED PER MM 57-00-00 FIG 801. 2 L 7 4 4F RT 4A25 1996021600172 19960216 00172 WP 1996 2 16 UPS805408 1 19960112 A 5730 SKIN DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING I/B SLOT CUTOUT AFT O/B CORNER HAS A 1.0625 INCH CRACK. INSTALLED NE W PANEL SECTION PER SRM 51-3-0. 2 L 7 4 4F RT 4A25 1996021600173 19960216 00173 WP 1996 2 16 UPS805409 1 19960116 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FS 260 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, LONGERON 35L CRACKED FS 260. REPLACED LONGERON SECTION PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996021600174 19960216 00174 WP 1996 2 16 UPS805410 1 19960112 A 5320 FITTING DOUG DC8 DC871F 302199D WP FS 70 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, FS 70 LONGERON 21R END FITTING CRACKED. REPLACED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996021600175 19960216 00175 WP 1996 2 16 UPS805411 1 19960110 A 5510 FITTING DOUG DC8 DC871F 302199D WP LT HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT HORIZ STAB CRACKED ON T-FITTING LOWER FWD I/B. REPLACED FITTING PER SRM 5 1-1-20D. 2 L 7 4 4F RT 4A25 1996021600176 19960216 00176 WP 1996 2 16 UPS805412 1 19960108 A 5330 SKIN DOUG DC8 DC871F 302199D WP FS 160 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, 2 CRACKS ON SKIN FS 160 FWD UPPER CORNER OF FWD SERVICE DOOR. REPAIRED SKIN PER SRM 53-0 FIG 14. 2 L 7 4 4F RT 4A25 1996021600177 19960216 00177 WP 1996 2 16 UPS805413 1 19960121 A 5320 FITTING DOUG DC8 DC871F 302199D WP FS 1152 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, FITTING ON LONGERON 31R CRACKED FS 1152. REPLACED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996021600178 19960216 00178 WP 1996 2 16 UPS805414 1 19960116 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FS 340-348 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, 4 CRACKS IN O/B LOWER FLANGE OF LONGERON 35L 340 TO 348. REPLACED LONGERON S ECTION FS 190 TO 390 PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996021600179 19960216 00179 EU 1996 2 16 WWMA9600019 1 19960206 A 2150 5419C000 ACM BAG JETSTM JETSTM3201 1500217 EU LEFT OVERSERVICED A WWMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 15 959AE 959 THE FLIGHT CREW REPORTED, OIL FUMES IN THE CABIN WHEN THE LEFT ENGINE FLOW IS TURNED ON. UPON INVESTIGATION MAINTENANCE FOUND THE LEFT COOLING TURBINE OVERSERVICED. EXCESSIVE OIL WAS DRAINED FROM THE ACM AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT A56EU 1996021600181 19960216 00181 NM 1996 2 16 96ZZZX635 1 19960108 A 3260 327 BULB DORNER DO32 DO328100 2996000 NM GEAR HANDLE DEFECTIVE A VNAA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 07 434JS 3051 FLT 4016 - WHILE SELECTING GEAR DOWN FOR LANDING, CREW DID NOT GET A GEAR DOWN INDICATION FOR THE LEFT MAIN LANDING GEAR . CREW CYCLED THE GEAR SEVERAL TIMES, WITHOUT SUCCESS. CREW ELECTED TO DO AN EMERGENCY LANDING GEAR EXTENSION, STILL D OWN INDICATION FOR THE LT MLG. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. PIT MAINTENANCE REMOVED AND REPLACED LIGHT BU LB IN THE LANDING GEAR SELECT HANDLE. GROUND RUN CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A45NM 1996021600182 19960216 00182 NM 1996 2 16 96ZZZX636 1 19960109 A 3260 870003 PSEU ELDEC DORNER DO32 DO328100 2996000 NM AVIONICS RACK MALFUNCTIONED A VNAA O OTHER N FALSE WARNING CR CRUISE 1 GL 07 434JS 3051 FLT 4058 - DURING CRUISE AT FL 200, CREW NOTICED SEVERAL AMBER CAS MESSAGES (HYD AT FAIL, STANDBY PUMP FAIL, AND PROXI F AIL). CREW CONSULTED QUICK REFERENCE HANDBOOK TO DETERMINE IF THEY WERE EXPERIENCING A SYSTEM FAILURE OR AN INDICATION PROBLEM. ONCE THEY DETERMINED THE FAILURE MODE WAS A RESULT OF THE INDICATION SYSTEM, THEY CONTINUED ON TO PIT. UPON L ANDING, CREW EXPERIENCED A NOSE WHEEL STEERING AND ANTI-SKID FAIL INDICATION. THE AIRCRAFT CONTINUED TO THE GATE WITH N O FURTHER PROBLEMS. PIT MAINTENANCE RESET PSEU, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A45NM 1996021600184 19960216 00184 NM 1996 2 16 96ZZZX638 1 19960105 A 3260 870003 PSEU DORNER DO32 DO328100 2996000 NM AVIONIC RACK MALFUNCTIONED A VNAA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 07 434JS 3051 FLT 4008 - DURING PREPARATION FOR TAKEOFF, CREW NOTICED 4 AMBER CAS MESSAGES RELATED TO THE AIRCRAFT HYDRAULIC SYSTEM. A IRCRAFT RETURNED TO THE GATE. OUT-STATION MAINTENANCE RE-RACKED THE PSEU (PROXIMITY SENSOR ELECTRONIC UNIT). GROUND RU N CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A45NM 1996021600185 19960216 00185 NM 1996 2 16 96ZZZX639 1 19960109 A 3060 A56362 BRUSH BLOCK DORNER DO32 DO328100 2996000 NM ENGINE GEARCASE DIRTY A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 437JS 3055 FLT 4033 - RIGHT PROPELLER HEAT FAILED SHORTLY AFTER TAKEOFF, CREW WAS INSTRUCTED TO RETURN TO FIELD. AIRCRAFT LANDED W ITHOUT FURTHER INCIDENT. PIT MAINTENANCE INSPECTED AND CLEANED BOTH LEFT AND RIGHT PROPELLER DE-ICE BRUSH BLOCK ASSEMBL IES IAW STD MAINTENANCE PRACTICES. GROUND RUN CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A45NM 1996021600191 19960216 00191 WP 1996 2 16 96ZZZX645 1 19960105 A 7603 BOLT DOUG DC9 DC951 3022051 WP THRUST LEVER MISSING A TWAA E ENGINE SHUTDOWN O OTHER CL CLIMB 1 CE 05 415EA 47749 MCI - FLT 1435 - DURING CLIMB, SHUT DOWN RIGHT ENGINE, SN 1716, DUE TO NO THRUST LEVER RESPONSE. FOUND BOLT MISSING FRO M CROSS-SHAFT TO THRUST LEVER CABLE. INSTALLED NEW BOLT, NUT, AND COTTER PIN. ENGINE THRUST LEVER RESPONSE AND ENGINE OPERATION CHECKED NORMAL. CHECK C-12 - 12-27-95 - STL. 2 L 7 2 4F A6WE 1996021600194 19960216 00194 WP 1996 2 16 96ZZZX648 1 19960104 A 2421 976J2528 GENERATOR DOUG DC9 DC932 3022066 WP NR 1 ENGINE FAILED A A VJ6A O OTHER H ELECT. POWER LOSS-50 PC CR CRUISE 1 SO 11 942VV 47648 TPA/ATL - ON FLT 210 - THE CAPTAIN DECLARED AN EMERGENCY FOR THE LEFT GENERATOR FAILURE. RIGHT GENERATOR DID NOT CROSS- TIE. NO POWER TO LEFT BUS AND LOST RADIO COMMUNCATIONS. REMOVED AND REPLACED LEFT GENERATOR, RESECURED CONNECTOR AT PY LON AND FOUND PHASE 'B' AT PYLON LOOSE. RAN ENGINE AND X-TIED, ALL SYSTEMS OPS CHECKED OK. 2 L 7 2 4F A6WE 1996021600200 19960216 00200 NM 1996 2 16 96ZZZX654 1 19960111 A 3242 214747 BRAKE ASSY BOEING 737 737301 1384611 NM LT MLG FROZE UP A F3LA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 NM 03 578US 1644 658 1496 23257 MDW - DURING TAKEOFF ROLL, FLIGHT CREW REPORTED THE AIRCRAFT PULLED TO THE LEFT. ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE FOUND NR 1 BRAKE FROZEN UP DUE TO WEATHER CONDITIONS (SNOWING AND FREEZING COLD). FREED BRAKE, PERFORMED E NGINE POWER RUN AND HIGH SPEED TAXI AND CHECKED OKAY. UPON ARRIVAL IN DEN, MAINTENANCE REPLACED THE NR 1 BRAKE ASSEMBLY AS PRECAUTIONARY. PART TOTAL CYCLES, 1,267. 2 L 7 2 4F RT A16WE 1996021600204 19960216 00204 SO 1996 2 16 C2XA96IA032 1 19960129 A 5720 12061344607 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 34712 120111 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING LOWER NR 3 SKIN SUPPORT CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. A/C TT, 13,396.7. CYCLES, 18,250. (X) 2 L 7 2 4T RT A31SO 1996021600205 19960216 00205 SO 1996 2 16 C2XA96IA033 1 19960129 A 5720 12061341611 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 34712 120111 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING LOWER NR 2 SKIN SUPPORT CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. A/C TT, 13,396.7. CYCLES, 18,250. (X) 2 L 7 2 4T RT A31SO 1996021600206 19960216 00206 SO 1996 2 16 C2XA96IA034 1 19960129 A 5720 12061341615 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 34712 120111 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING UPPER NR 2 SKIN SUPPORT CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. A/C TT, 13,396.7. CYCLES, 18,250. (X) 2 L 7 2 4T RT A31SO 1996021600207 19960216 00207 SO 1996 2 16 C2XA96IA035 1 19960129 A 5720 12017057017 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 34712 120111 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER NR 2 SKIN SUPPORT CRACKED AT RIB NR 18. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. A/C TT, 13,396.7. CYCLES, 18,250. (X) 2 L 7 2 4T RT A31SO 1996021600208 19960216 00208 SO 1996 2 16 C2XA96IA037 1 19960129 A 5720 12017059009 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 34712 120111 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING UPPER NR 4 SKIN SUPPORT CRACKED AT RIB NR 18. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. A/C TT, 13,396.7. CYCLES, 18,250. (X) 2 L 7 2 4T RT A31SO 1996021600209 19960216 00209 SO 1996 2 16 C2XA96IA038 1 19960129 A 5720 12017063009 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 34712 120111 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING UPPER NR 3 SKIN SUPPORT CRACKED AT RIB NR 21. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. A/C TT, 13,396.7 HOURS. CYCLES, 18,250. (X) 2 L 7 2 4T RT A31SO 1996021600210 19960216 00210 SO 1996 2 16 C2XAIA036 1 19960129 A 5720 12017059020 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 34712 120111 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER NR 1 SKIN SUPPORT CRACKED AT RIB NR 18. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. A/C TT, 13,396.7. CYCLES, 18,250. (X) 2 L 7 2 4T RT A31SO 1996021600211 19960216 00211 NM 1996 2 16 CAL960005 1 19960106 A 2910 FILTER BOEING 737 7373T0 1384582 NM A-HYD SYSTEM LEAKING A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 301AL 23841 MEX - FLT 0789 - FLIGHT CREW RECEIVED HYDRAULIC A-SYSTEM LOW QUANTITY INDICATION WHILE EN ROUTE FROM IAH TO ACA. THE AI RCRAFT WAS DIVERTED TO MEX WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE A-HYDRAULIC SYSTEM ELECTRIC MOTOR DR IVEN PUMP ACOUSTIC FILTER LEAKING. THE FILTER AND PACKING WERE REMOVED AND REPLACED. THE HYDRAULIC SYSTEM WAS SERVICED AND LEAK CHECKS WERE GOOD. (X) 2 L 7 2 4F RT A16WE 1996021600212 19960216 00212 NM 1996 2 16 CAL960006 1 19960107 A 2913 6507606 HYD PUMP BOEING 737 737291 138448W NM NR 2 ENGINE LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 17252 19542 4059 20362 IAH - FLT 1607 - THE A-HYDRAULIC SYSTEM WAS LOST WHILE EN ROUTE TO IAH. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. M AINTENANCE FOUND THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP LEAKING. THE NR 2 PUMP WAS REMOVED AND REPLACED. IN ADDITION, T HE NR 1 ENGINE DRIVEN PUMP WAS REMOVED AND REPLACED. ALL SYSTEMS CHECKED GOOD. (X) 2 L 7 2 4F A16WE 1996021600214 19960216 00214 NM 1996 2 16 CAL960011 1 19960102 A 5315 FLOOR BEAM BOEING 737 737130 1384435 NM BS 663 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14212 65664 19029 HOU - INSPECTION FOUND A 1.5 INCH CRACK IN FLOOR BEAM AT STA 663, BL ZERO, WING CENTER BOX. A REPAIR WAS INSTALLED IAW ECRA 5710-01708. (X) 2 L 7 2 4F A16WE 1996021600217 19960216 00217 NM 1996 2 16 CAL960032 1 19960114 A 3350 3004183 LIGHT BOEING 747 747230B 1384889 NM L-5 DOOR INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 78019 20527 LAX - FLT 0006 - THE A-ZONE LIGHTS ILLUMINATED WITH THE EMERGENCY EXIT LIGHT SWITCH IN THE ARM POSITION. ONLY THE A-ZON E DOOR EMERGENCY LIGHTS ILLUMINATED WITH THE SWITCH IN THE 'ON' POSITION. MAINTENANCE FOUND THE L-5 DOOR EMERGENCY LIGH T ASSEMBLY AT FAULT. THE L-5 DOOR EMERGENCY LIGHT WAS REPLACED. (X) 2 L 7 4 4F A20WE 1996021600233 19960216 00233 NM 1996 2 16 USAA960011 1 19960108 A 5330 SKIN BOEING 757 7572B7 1384964 NM BS 278 DENT A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 633AU 1604 27811 CLT - INSPECTION VISUALLY FOUND A DENT 5 INCHES BY 4 INCHES, .280 INCH DEEP AT EXTERIOR SKIN STA 278, 2 INCHES BELOW STR 17L FUSELAGE SKIN. INSTALLED DOUBLER PER BOEING SRM 53-00-01, FIG 203, WITH BLIND RIVETS. (X) 2 L 7 2 4F RT A2NM 1996021600234 19960216 00234 NM 1996 2 16 9603202298 1 19960117 A 5311 FRAME BOEING 727 727251 138408H NM FS 1090 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 298US 22152 DURING PERIODIC CHECK, FOUND A CRACK IN THE NR 3 CARGO DOOR FRAME BS 1090 ABOVE STRINGER 26R. REPAIRED FRAME (P/N 65-56 131-41) PER EA 22-103425. 2 L 7 3 4F A3WE 1996021600235 19960216 00235 NM 1996 2 16 9603216719 1 19960117 A 5320 BEAM BOEING 747 747251F 1384898 NM FS 1420 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 619US 21321 DURING PERIODIC CHECK, FOUND CORROSION ON THE LEFT LONGERON CHORD CREASE BEAM BS 1420 WL 152. REPAIRED BEAM (P/N 65B150 32-3) PER EA 67-99376. 2 L 7 4 4F A20WE 1996021600236 19960216 00236 NM 1996 2 16 9603226719 1 19960120 A 5230 BEAM BOEING 747 747251F 1384898 NM FS 585-610 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 619US 21321 DURING PERIODIC CHECK, FOUND CORROSION ON THE FORWARD CARGO DOOR LOWER BEAM AT BS 585, 590 AND 610. REPAIRED BEAM (P/N 65B04697-2) PER EA 67-99406 AND -99378. 2 L 7 4 4F A20WE 1996021600237 19960216 00237 NM 1996 2 16 9603236719 1 19960124 A 5230 WEB BOEING 747 747251F 1384898 NM FS 1880 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 619US 21321 DURING PERIODIC CHECK, FOUND CORROSION ON THE AFT CARGO DOOR LOWER BEAM WEB BS 1880. REPAIRED WEB (P/N 65B04721-1) PER EA 67-99380. 2 L 7 4 4F A20WE 1996021600238 19960216 00238 WP 1996 2 16 9603249865 1 19960124 A 5320 CUSP DOUG DC9 DC951 3022051 WP FS 1167 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 774NC 47776 DURING H-CHECK, FOUND CORROSION IN THE FS 1167 CUSP, LEFT SIDE. REPAIRED CUSP (P/N 9910503-3) PER EA 98-103369. 2 L 7 2 4F A6WE 1996021600239 19960216 00239 WP 1996 2 16 9603259606 1 19960201 A 5320 FITTINGS DOUG DC9 DC932 3022066 WP FS 756 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 606NW 47225 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FS 756 ATTACH FITTINGS AT LONGERONS 29L AND 29R. R EPLACED BOTH FITTINGS PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996021600240 19960216 00240 WP 1996 2 16 9603269606 1 19960201 A 5320 FITTING DOUG DC9 DC932 3022066 WP FS 996 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 606NW 47225 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE FS 996 FLOORBEAM FITTING AT RBL 58. REPLACED FITTING PER SRM 51-01. 2 L 7 2 4F A6WE 1996021600241 19960216 00241 NM 1996 2 16 9603276730 1 19960201 A 5312 BLKHD FITTING BOEING 747 7472J9F 1384806 NM FS 1480 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 630US 21668 DURING PERIODIC CHECK, FOUND A .5 INCH CRACK IN THE FS 1480 BULKHEAD HORIZONTAL BEAM TIE FITTING LEFT OUTBOARD END, ABOV E STRINGER 36L. REPLACED TIE FITTING PER SRM 51-10-01, PAR 9. 2 L 7 4 4F RT A20WE 1996021600242 19960216 00242 WP 1996 2 16 9603289605 1 19960206 A 5415 FITTING DOUG DC9 DC932 3022066 WP FS 1038 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 605NW 47223 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE RIGHT PYLON AFT SPAR UPPER FORWARD INBOARD FITTING AP PROXIMATELY FS 1038. REPLACED FITTING PER SRM 51-30-25. 2 L 7 2 4F A6WE 1996021600243 19960216 00243 WP 1996 2 16 9603299606 1 19960207 A 5320 FITTING DOUG DC9 DC932 3022066 WP FS 794 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 606NW 47225 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE FS 794 TO LONGERON 30 SPLICE FITTING. REPLACED FITTI NG PER SRM 51-01. 2 L 7 2 4F A6WE 1996021600244 19960216 00244 WP 1996 2 16 9603309867 1 19960207 A 5350 RELEASE MECH DOUG DC9 DC951 3022051 WP TAIL CONE MALFUNCTIONED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 776NC 47786 DURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO ACTIVATE THE RELEASE SYSTEM USING THE INTERIOR HANDLE. AL SO, THE TAIL CONE DID NOT DROP. FOUND THAT THE TAIL CONE HUNG UP ON THE RAIN GUTTER SEALANT. REMOVED THE SEALANT AND A CCOMPLISHED TAIL CONE MODIFICATION PER EO 5350-01049. 2 L 7 2 4F A6WE 1996021600245 19960216 00245 NM 1996 2 16 9603312703 1 19960208 A 2400 ELECTRICAL POWER BOEING 727 727225 1384077 NM E/E COMPT FAILED A A NWAA O OTHER B H SMOKE/FUMES/ODORS/SPARKS ELECT. POWER LOSS-50 PC UK UNKNOWN 1 GL 01 8878Z 21451 AFTER ARRIVING AT THE GATE AND WHILE TRANSFERRING ELECTRICAL POWER FROM ENGINE NR 3 GENERATOR TO GROUND, LOST ALL ELECTR ICAL POWER, APU WAS ON MEL. CABIN FILLED WITH SMOKE. CREW INITIATED AN EMERGENCY EVACUATION THROUGH THE MAIN CABIN DOO R, AFT AIRSTAIR AND OVERWING EXITS. FIRE RESCUE WAS CALLED AND HELPED DEPLANE PASSENGERS OFF THE WING. MAINTENANCE DET ERMINED THAT THE SMOKE IN THE CABIN WAS DUE TO ELECTRICAL POWER FAILURE AND AIR CONDITIONING PACKS BEING ON. PACKS OVER HEATED DUE TO COOLING FANS SHUTTING DOWN. INSPECTED ELECTRICAL SYSTEM AND PACKS. INSPECTION AND OPERATIONAL CHECKS WER E NORMAL. 2 L 7 3 4F A3WE 1996021600246 19960216 00246 NE 1996 2 16 9603326603 2 19960209 A 7250 TURBINE BOEING 747 747151 1384891 NM PWA JT9 JT9D7A 52054 NE NR 1 ENGINE DAMAGED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 01 603US 19780 62693 EN ROUTE, THE NR 1 ENGINE STALLED AND IFSD WAS ACCOMPLISHED. RESTART WAS ATTEMPTED, BUT FAILED. CREW FOLLOWED COCKPIT OPERATING PROCEDURE AND RETURNED TO NRT. VISUAL INSPECTION REVEALED METAL IN THE TAILPIPE AND A 6TH STAGE TURBINE DAMAG E. REPLACED NR 1 ENGINE AND CHECK WAS NORMAL. 2 L 7 4 4F 4 F A20WE E20EA 1996021600247 19960216 00247 NE 1996 2 16 9603331143 2 19960208 A 7230 COMPRESSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 2 ENGINE STALLED A NWAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DE DESCENT 1 GL 01 133JC 46752 86117 DURING DESCENT, THE NR 2 ENGINE COMPRESSOR STALLED. THE ENGINE WAS SHUTDOWN AND RESTARTED. CREW FOLLOWED COCKPIT OPERA TING PROCEDURE AND CONTINUED TO LAX WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED NR 2 ENGINE AND CHECK WAS NORMAL. 2 L 7 3 4F 4 F A22WE E20EA 1996021600248 19960216 00248 WP 1996 2 16 9603349853 1 19960208 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 762NC 47710 DURING LINE CHECK, FOUND CEILING LIGHTS INOPERATIVE ROWS 15 THROUGH 19. MAINTENANCE REPLACED BATTERIES AND POWER PACK, OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996021600249 19960216 00249 WP 1996 2 16 9603359178 1 19960208 A 3350 BATTERY PACK DOUG DC9 DC914 3022034 WP CATWALK DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 3310L 45705 DURING LINE CHECK, FOUND CATWALK EMERGENCY LIGHTS WOULD NOT ILLUMINATE. REPLACED THE BATTERY AND BATTERY PACK, OPERATIO NAL CHECK GOOD. 2 L 7 2 4F A6WE 1996021600250 19960216 00250 1996 2 16 9603369610 4 19960205 A 2565 13621224 SLIDE DOUG DC9 DC932 3022066 WP TAIL SECTION LOW PRESSURE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 610NW 47432 DURING PERIODIC CHECK, FOUND AFT TAIL SECTION EMERGENCY EVACUATION SLIDE WITH LOW PRESSURE. REPLACED SLIDE. 2 L 7 2 4F A6WE 1996021600251 19960216 00251 WP 1996 2 16 9603379910 1 19960206 A 3350 60030451 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 960N 47256 DURING LINE MAINTENANCE INSPECTION, FOUND CENTER CABIN SECTION OF OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED THE B ATTERY PACK AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996021600252 19960216 00252 WP 1996 2 16 9603389613 1 19960208 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 613NW 47438 DURING LINE MAINTENANCE INSPECTION, FOUND AFT CABIN SECTION EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES AND OPERAT IONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996021600253 19960216 00253 NM 1996 2 16 9603392769 1 19960209 A 2782 269002910 ACTUATOR BOEING 727 7272M7 138407S NM RT LE SLAT LEAKING A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 729RW 21742 AFTER TAKEOFF, HYDRAULIC SYSTEM 'A' FLUID DEPLETED. CREW CALLED FOR CFR AND RETURNED TO MEM WITHOUT FURTHER INCIDENT. M AINTENANCE FOUND RIGHT WING SLAT ACTUATOR LEAKING. REPLACED NR 8 SLAT ACTUATOR AND OPERATIONAL CHECK NORMAL. 2 L 7 3 4F A3WE 1996021600254 19960216 00254 WP 1996 2 16 9603409139 1 19960118 A 5311 FRAME DOUG DC9 DC914 3022034 WP FS 737 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 948L 47049 DURING H-CHECK, FOUND A CRACK IN THE FS 737 FRAME AT LONGERON 17R. REPAIRED THE FRAME (P/N 5911447) PER EA 91-103364. 2 L 7 2 4F A6WE 1996021600255 19960216 00255 NM 1996 2 16 9603426638 1 19960210 A 3397 WIRE BOEING 747 747251B 1384892 NM CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 638US 23549 DURING LINE CHECK, FOUND EMERGENCY FLOOR PATH LIGHTS INOPERATIVE AT DOOR 3R. REPAIRED BROKEN WIRES AND OPERATIONAL CHEC K GOOD. 2 L 7 4 4F A20WE 1996021600256 19960216 00256 WP 1996 2 16 9603431220 1 19960209 A 2780 ACTUATOR DOUG DC10 DC1030 3023501 WP LE SLATS MALFUNCTIONED A NWAA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 GL 01 122NW 46577 DURING FLAP RETRACTION FROM FLAPS 1, THE OUTBOARD SLATS STUCK IN THE EXTENDED POSITION AND THE SLAT DISAGREE LIGHT ILLUM INATED. AIRCRAFT RETURNED TO SEA. RESET THE AUTO SLAT ACTUATOR AND THE AIRCRAFT RETURNED TO SERVICE. A PRECAUTIONARY CHANGE OF THE PROXIMITY CONTROL BOX WAS ACCOMPLISHED AT KIX. 2 L 7 3 4F A22WE 1996021600257 19960216 00257 NM 1996 2 16 9603442712 1 19960209 A 2750 FLAP BOEING 727 7272S7 138407Z NM RT OUTBD TE LOOSE A A NWAA O OTHER E VIBRATION/BUFFET CR CRUISE 1 GL 01 712RC 22020 EN ROUTE AT 25,000 FEET AND 310 KNOTS, RIGHT OUTBOARD FLAP BEGAN TO VIBRATE VIGOROUSLY. CREW SLOWED AIRCRAFT AND PERFOR MED A FLIGHT CONTROL CHECK. AIRCRAFT BANKED QUICKER TO THE RIGHT AND SLOWER TO THE LEFT. CONTINUED TO DTW, DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND RIGHT OUTBOARD AFT FLAP LOOSE AND ADJUSTED FLAP ECCEN TRICS. 2 L 7 3 4F A3WE 1996021600258 19960216 00258 NM 1996 2 16 9603456309 1 19960211 A 3350 LIGHT BOEING 747 747451 1384940 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 669US 24224 DURING LINE CHECK, THE FLOOR MOUNTED EMERGENCY PATH LIGHTS AT SEAT ROWS 35L TO 42L WERE FOUND INOPERATIVE. RECONNECTED THE CONNECTOR PIN IN FLOOR TRACK AT SEAT ROW 42L AND OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996021600259 19960216 00259 NM 1996 2 16 9603462710 1 19960211 A 2130 AUTO PACK TRIP BOEING 727 727225 1384077 NM CABIN MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 820EA 22557 DURING TAKEOFF ROLL, AUTO PACK TRIP NO ARM LIGHT ILLUMINATED. AIRCRAFT ABORTED TAKEOFF WITH NO INCIDENT. AUTO PACK TRI P SYSTEM WAS PLACED ON MEL 21-30. 2 L 7 3 4F A3WE 1996021600260 19960216 00260 NM 1996 2 16 9603472717 1 19960211 A 3350 BATTERY PACK BOEING 727 7272S7 138407Z NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 721RC 22492 DURING PREFLIGHT, FOUND EMERGENCY FLOOR LIGHTS INOPERATIVE IN AFT OF AIRCRAFT. REPLACED BATTERY PACK AND CHECKED OK. 2 L 7 3 4F A3WE 1996021600261 19960216 00261 WP 1996 2 16 9603489945 1 19960211 A 3222 SCHRADER VALVE DOUG DC9 DC931 3022065 WP NLG STRUT FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 8925E 45840 DURING CLIMBOUT, THE AIRCRAFT WOULD NOT SHIFT FROM GROUND MODE TO FLIGHT MODE. AIRCRAFT WAS UNABLE TO PRESSURIZE AND NO SE WHEEL WAS STEERABLE. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NOSE LANDING GEAR STRUT FLAT. REPLACED SCHRADER VALVE AND SERVICED STRUT TO PROPER LEVELS. 2 L 7 2 4F A6WE 1996021600262 19960216 00262 WP 1996 2 16 9603499958 1 19960210 A 3230 UPLATCH SPRING DOUG DC9 DC931 3022065 WP RT MLG BROKEN A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 917RW 47145 DURING CLIMBOUT, THE RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BROKEN SPRING TO UPLATCH MECHANISM AND REPLACED SPRING. 2 L 7 2 4F A6WE 1996021600263 19960216 00263 WP 1996 2 16 96FDEA00197 1 19960207 A 3222 STRUT DOUG DC10 DC1010F 3022111 WP NLG REQD SERVICE A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 68059 46907 ON TAKEOFF, GEAR OVERRIDE WAS USED TO RETRACT LT GEAR PER CHECKLIST. ON EXTENSION, DOWN AND LOCK IND NORMAL, INTERMITTE NT WARNING HORN SOUNDED UNTIL FLAPS RETRACTED TO 22 DEGREES, THEN HORN SILENCED. SUSPECT NOSE STRUT NOT EXTENDING FULLY , RESULTING IN GROUND SENSING STILL HOLDING LATCH. DISASSEMBLED PER 32-21-03, SERVICED AND LEAK CHECKED OK. 2 L 7 3 4F A22WE 1996021600264 19960216 00264 NM 1996 2 16 96FDEA00198 1 19960209 A 5320 SHEAR TIE BOEING 727 72722 1384002 NM BS 1050 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CORROSION ON BOTTOM SIDE OF SHEAR TIE BS 1050 WL 146 LBL 7 TO 13, FOUND TO BE OUT OF LIMITS WHILE WORKING NR O0053. ACC OMPLISHED SHEAR TIE REPAIR AT BS 1050 WL 146 LBL 7 TO 13 PER FEDEX SRM 53-10-4. 2 L 7 3 4F A3WE 1996021600265 19960216 00265 NM 1996 2 16 96FDEA00199 1 19960209 A 5320 SHEAR TIE BOEING 727 72722 1384002 NM BS 1050 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CORROSION ON BOTTOM SIDE OF SHEAR TIE BS 1050 WL 146 RBL 16 TO 22, FOUND WHILE WORKING NR OO53, OUT OF LIMITS. CUT OFF DAMAGED SHEAR TIE, FABRICATED NEW SHEAR TIE FROM HEAT TREATED MATERIAL, BACK DRILLED, ALODINED, PRIMED, PAINTED AND INST ALLED FASTENERS PER FEDEX SRM 53-10-4. 2 L 7 3 4F A3WE 1996021600266 19960216 00266 NM 1996 2 16 96FDEA00201 1 19960209 A 5320 SHEAR TIE BOEING 727 72722 1384002 NM BS 1050 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CORROSION FOUND ON BOTTOM SIDE OF SHEAR TIE BS 1050 WL 146 LBL 1 TO 6, FOUND TO BE OUT OF LIMITS WHILE WORKING NR 0053. REPAIRED CORRODED SHEAR TIE PER FEDEX SRM 51-10-4. 2 L 7 3 4F A3WE 1996021600267 19960216 00267 NM 1996 2 16 96FDEA00202 1 19960209 A 5320 SHEAR TIE BOEING 727 72722 1384002 NM BS 1050 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CORROSION FOUND ON BOTTOM SIDE OF SHEAR TIE BS 1050 LBL 32 TO 38, FOUND TO BE OUT OF LIMITS WHILE WORKING NR 0053. CUT OUT DAMAGE AND REPAIRED PER FEDEX SRM 53-10-4. 2 L 7 3 4F A3WE 1996021600268 19960216 00268 NM 1996 2 16 96FDEA00203 1 19960209 A 5320 SHEAR TIE BOEING 727 72722 1384002 NM BS 1030 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CORROSION ON BOTTOM SIDE OF SHEAR TIE BS 1030 RBL 8 TO 13 WL 146, FOUND WHILE WORKING NR 0053. ACCOMPLISHED REPAIR ON S HEAR TIE BS 1030 RBL 8 TO 13 WL 146 IAW FEDEX SRM 53-10-4. 2 L 7 3 4F A3WE 1996021600269 19960216 00269 NM 1996 2 16 96FDEA00204 1 19960209 A 5320 SHEAR TIE BOEING 727 72722 1384002 NM BS 1030 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 199FE 19142 CORROSION ON BOTTOM SIDE OF SHEAR TIE BS 1030 LBL 17 TO 22, FOUND WHILE WORKING NR 0053 WL 146. 2 L 7 3 4F A3WE 1996021600270 19960216 00270 NM 1996 2 16 96FDEA00205 1 19960209 A 5320 SHEAR TIE BOEING 727 72722 1384002 NM BS 1030 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CORROSION ON BOTTOM SIDE OF SHEAR TIE BS 1030 RBL 17 TO 22 WL 146, FOUND WHILE WORKING NR0053. REMOVED SHEAR TIE AND CO RROSION, TREATED AND REINSTALLED IAW FEDEX SRM 53-10-1 AND 53-10-4. 2 L 7 3 4F A3WE 1996021600271 19960216 00271 NM 1996 2 16 96FDEA00206 1 19960209 A 5320 SHEAR TIE BOEING 727 72722 1384002 NM BS 970 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CORROSION ON BOTTOM SIDE OF SHEAR TIE BS 970 LBL 2 TO 6 WL 146, FOUND WHILE WORKING NR 0053. ACCOMPLISHED SHEAR TIE REP AIR AT BS 970 LBL 2 TO 6 WL 146 IAW FEDEX SRM 53-10-4 FIG 15. REMAINING FASTENERS ON FLOOR SUPPORT BRACKET WILL BE INS TALLED ON NR 0053. 2 L 7 3 4F A3WE 1996021600272 19960216 00272 NM 1996 2 16 96FDEA00207 1 19960209 A 5320 SHEAR TIE BOEING 727 72722 1384002 NM BS 970 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CORROSION ON BOTTOM OF SHEAR TIE BS 970 LBL 8 TO 13 WL 146, FOUND WHILE WORKING NR 0053. ACCOMPLISHED SHEAR TIE REPAIR BS 970 LBL 8 TO 13 WL 146 IAW FEDEX SRM 53-10-4 FIG 15. REMAINING FASTENERS ON FLOOR SUPPORT BRACKET WILL BE INSTALLED ON NR 0053. 2 L 7 3 4F A3WE 1996021600273 19960216 00273 NM 1996 2 16 96FDEA00208 1 19960209 A 5320 SHEAR TIE BOEING 727 72722 1384002 NM BS 970 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CORROSION ON BOTTOM OF SHEAR TIE BS 970 RBL 8 TO 13 WL 146, FOUND WHILE WORKING NR 0053. 2 L 7 3 4F A3WE 1996021600274 19960216 00274 NM 1996 2 16 96FDEA00209 1 19960209 A 5320 SHEAR TIE BOEING 727 72722 1384002 NM BS 970 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CORROSION ON BOTTOM SIDE OF SHEAR TIE BS 990 LBL 2 TO 4 WL 146, FOUND WHILE WORKING NR 0053. ACCOMPLISHED SHEAR TIE REP AIR AT BS 990 LBL 2 TO 4 WL 146 PER FEDEX SRM 53-10-4. 2 L 7 3 4F A3WE 1996021600275 19960216 00275 NM 1996 2 16 96FDEA00210 1 19960209 A 5320 SHEAR TIE BOEING 727 72722 1384002 NM BS 990 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CORROSION ON BOTTOM OF SHEAR TIE BS 990 LBL 9 TO 13 WL 146, FOUND WHILE WORKING NR 0053. 2 L 7 3 4F A3WE 1996021600276 19960216 00276 NM 1996 2 16 96FDEA00211 1 19960209 A 5320 FAIL-SAFE CHORD BOEING 727 72722 1384002 NM BS 1010 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 BS 1010 CRACKED FAIL-SAFE CHORD AT RBL 45 WL 149, FOUND WHILE WORKING NR 0053. 2 L 7 3 4F A3WE 1996021600277 19960216 00277 NM 1996 2 16 96FDEA00212 1 19960209 A 5320 SHEAR TIE BOEING 727 72722 1384002 NM BS 1050 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CORROSION ON BOTTOM SIDE OF SHEAR TIE BS 1050 WL 146 RBL 1 TO 6, FOUND TO BE OUT OF LIMITS WHILE WORKING NR 0053. 2 L 7 3 4F A3WE 1996021600278 19960216 00278 NM 1996 2 16 96FDEA00213 1 19960209 A 5330 6518220 SKIN BOEING 727 72722 1384002 NM BS 366 CREASED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 BS 366 STR 20R THERE IS A CREASE IN SKIN. *S/D* REPAIRED CREASE PER FEDEX SRM 53-03-3. 2 L 7 3 4F A3WE 1996021600279 19960216 00279 NM 1996 2 16 96FDEA00214 1 19960209 A 5311 6516314 FRAME BOEING 727 72722 1384002 NM BS 310 GOUGE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 FWD ENTRY DOOR LATCH ROLLER RIBS ON DOOR STRUCTURE. *S/D* REMOVED AND REPLACED FORWARD SIDE FRAME PER SRM 53-10-1. 2 L 7 3 4F A3WE 1996021600280 19960216 00280 NM 1996 2 16 96FDEA00215 1 19960209 A 5320 SHEAR TIE BOEING 727 72722 1384002 NM BS 970 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION (C53-111-01,3) ON SHEAR TIE AT BS 970 RBL 10. 2 L 7 3 4F A3WE 1996021600281 19960216 00281 NM 1996 2 16 96FDEA00216 1 19960209 A 5320 SHEAR TIE BOEING 727 72722 1384002 NM BS 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 MECHANISM DAMAGE ON SHEAR TIE AT BS 600 BETWEEN STR 16 TO 17R. 2 L 7 3 4F A3WE 1996021600282 19960216 00282 NM 1996 2 16 96FDEA00217 1 19960209 A 5315 BAC1505100617 FLOORBEAM BOEING 727 72722 1384002 NM BS 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CORROSION (C53-224-06), ON FLOORBEAM OF BS 600 RBL 10 TO 30 WL 208. REMOVED CORRODED SECTION OF FLOORBEAM FABRICATED RE PAIR ANGLES AND INSTALLED ALL WORK DONE PER FEDEX SRM 53-10-8. 2 L 7 3 4F A3WE 1996021600283 19960216 00283 NM 1996 2 16 96FDEA00218 1 19960209 A 5314 65184071 KEEL BEAM BOEING 727 72722 1384002 NM BS 1030-1050 CORROSIOIN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 EXTERIOR SKIN BULGE IN SKIN AT KEEL BEAM STR 29L BS 1050 TO 1030. 2 L 7 3 4F A3WE 1996021600284 19960216 00284 NM 1996 2 16 96FDEA00219 1 19960209 A 5313 STRINGER BOEING 727 72722 1384002 NM BS 1130-1149 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 INTERCOSTAL BETWEEN BS 1130 AND 1149 HAS FASTENER PULLED THROUGH STR 6R. CUT OUT STR DAMAGE AREA FABRICATED STR SPLICES REPAIR AND INSTALLED REPAIR PARTS WITH FASTENERS PER FEDEX SRM 53-10-3 FIG 3 AT BS 1130 AND 1149 STR 6R. 2 L 7 3 4F A3WE 1996021600285 19960216 00285 NM 1996 2 16 96FDEA00220 1 19960209 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM BS 344 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CORROSION ON FLOORBEAM (C53-224-01(1), BS 344 WL 208 RBL 15 TO 50 AROUND NUT CLIP HOLES UPPER AND LOWER SURFACE. REMOVE D UPPER CHORD OF FLOORBEAM BS 344 FABRICATED AND INSTALLED NEW UPPER CHORD OF FLOORBEAM PER FEDEX SR 27-53-007. 2 L 7 3 4F A3WE 1996021600286 19960216 00286 NM 1996 2 16 96FDEA00221 1 19960209 A 5751 65192596 HINGE BOEING 727 72722 1384002 NM RT AILERON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CORROSION ON RT WING O/B AILERON NR 3 HINGE. REMOVED CORRODED NR 3 HINGE, INSTALLED A NEW HINGE AND REINSTALLED RT WING O/B AILERON IAW FEDEX MM 27-10-31, FUNCTIONAL TESTED IAW FEDEX MM 27-10-00. 2 L 7 3 4F A3WE 1996021600287 19960216 00287 NM 1996 2 16 96FDEA00222 1 19960206 A 5320 DOOR FRAME BOEING 727 72722 1384002 NM BS 1057.5 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CORROSION FOUND ON DOOR FRAME BS 1057.5 WL 162 RBL 25, WHILE WORKING NR 0053. 2 L 7 3 4F A3WE 1996021600288 19960216 00288 NM 1996 2 16 96FDEA00223 1 19960209 A 5311 FRAME BOEING 727 72722 1384002 NM BS 1070 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 BS 1070 FRAME CRACK EMITTING FROM STOP DRILL HOLE AT BL 0 TO BL 10 WL 150, FOUND WHILE WORKING CUSTOMER CARD NR 0053. R EMOVED DAMAGE FROM FRAME BS 1070 AT BL 0 AND LBL 10 WL 150, FABRICATED FILLERS AND INSTALLED IAW SRM 51-40-3 AND PREVIOU S REPAIR DOUBLER REINSTALLED. 2 L 7 3 4F A3WE 1996021600289 19960216 00289 NM 1996 2 16 96FDEA00224 1 19960209 A 5320 SHEAR TIE BOEING 727 72722 1384002 NM BS 1030 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CORROSION ON BOTTOM OF SHEAR TIE BS 1030 LBL 3 TO 4 WL 146, FOUND TO BE OUT OF LIMITS WHILE WORKING NR 0053. ACCOMPLISH ED SHEAR TIE REPAIR AT BS 1030 LBL 3 TO 4 WL 146 IAW FEDEX SRM 53-10-4 FIG 15. 2 L 7 3 4F A3WE 1996021600290 19960216 00290 NM 1996 2 16 96FDEA00225 1 19960209 A 5330 SKIN BOEING 727 72722 1384002 NM BS 1120 CREASE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 BS 1120 BETWEEN STR 17 TO 19L, THERE IS A CREASE IN SKIN. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND REPAIRED PER SRM 53-30-3. 2 L 7 3 4F A3WE 1996021600291 19960216 00291 NM 1996 2 16 96FDEA00226 1 19960212 A 5320 6516343 CHANNEL BOEING 727 72722 1384002 NM BS 1157-1110 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION (C-53-111-01, -3) ON NR 2 CARGO DOORWAY C-CHANNEL BS 1057 TO 1110 RBL 27, WL 147. *S/D* REMOVED AND REPLACED C-CHANNEL AT DOORWAY. 2 L 7 3 4F A3WE 1996021600292 19960216 00292 NM 1996 2 16 96FDEA00227 1 19960209 A 5315 6540145 FLOOR BEAM BOEING 727 72722 1384002 NM BS 1110 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION (C53-111-01, -3) ON LOWER CHORD OF 1110 FLOOR BEAM WL 200 LBL 2 TO 30 AT NUTPLATE HOLES. *S/D* REMOVED AND R EPLACED CORRODED LOWER CHORD AT BS 1110 FLOOR BEAM AT WL 200, RBL TO LBL 19.75 WITH FABRICATED REPAIR PARTS PER SRM 53-1 0-8 FIG 2 PER FEDEX EA 75310-27491. 2 L 7 3 4F A3WE 1996021600293 19960216 00293 NM 1996 2 16 96FDEA00228 1 19960212 A 5311 FRAME BOEING 727 72722 1384002 NM BS 1050 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 DENT IN FRAME BS 1050 BETWEEN STR 25 TO 26L LBL 30 WL 153. REPAIRED DENT IN FRAME AT BS 1050 BETWEEN STR 25 TO 26L LBL 30 WL 153 PER FEDEX SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 1996021600294 19960216 00294 NM 1996 2 16 96FDEA00229 1 19960209 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM BS 540 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION AT BS 540 FLOORBEAM LOWER CHORD FROM LBL 16 TO RBL 28 WL 200. 2 L 7 3 4F A3WE 1996021600295 19960216 00295 NM 1996 2 16 96FDEA00230 1 19960216 A 5315 65208279 FLOOR BEAM BOEING 727 72722 1384002 NM BS 640 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION (C53-111-01, -2) ON LOWER FLANGE OF FLOOR BEAM AT BS 640 LBL 23 TO RBL 26.7 WL 200. *(S/D)* REMOVED AND COR RODED ON LOWER FLANGE OF FLOOR BEAM IN NUTPLATE HOLES AT BS 640 LBL 23 TO RBL 26.7 WL 200. REPAIR PARTS PER FDE SRM 53- 10-8. 2 L 7 3 4F A3WE 1996021600296 19960216 00296 NM 1996 2 16 96FDEA00231 1 19960209 A 5753 652163254 TIE WEDGE BOEING 727 72722 1384002 NM RT TE MIDFLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 RT WING I/B MIDFLAP TIE WEDGE HAS AN AREA OF DELAMINATION ON O/B END 12 INCHES BY 3 INCHES. 2 L 7 3 4F A3WE 1996021600297 19960216 00297 NM 1996 2 16 96FDEA00232 1 19960209 A 5753 MR57579185 SKIN BOEING 727 72722 1384002 NM LT TE AFT FLAP DELAMINATION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 LEFT WING I/B AFT FLAP HAS AREA OF DELAMINATION ON I/B UPPER AND LOWER SKIN 18 INCHES BY 18 INCHES. REPAIRED DELAMINATI ON PER SRM 51-40-06. 2 L 7 3 4F A3WE 1996021600298 19960216 00298 NM 1996 2 16 96FDEA00233 1 19960209 A 5754 6556119 BONDING STRAP BOEING 727 72722 1384002 NM NR 4 LE FLAP CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION (097-562-01-2) NR 4 RT FLAP BULLNOSE OB BONDING JUMPER UPPER ATTACH POINT AND TOOLING MARKS BS 950A, STR 7 RT AFT SIDE OF FRAME. *S/D* REMOVED CORROSION PER FEDEX SRM 57-50-3 AND 27-57-010. 2 L 7 3 4F A3WE 1996021600299 19960216 00299 NM 1996 2 16 96FDEA00234 1 19960212 A 5315 BAC1505100617 FLOORBEAM BOEING 727 72722 1384002 NM BS 620 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CORROSION (C53-224-06) ON FLOORBEAM AT BS 620 RBL 10 TO 43 WL 208. REMOVED DAMAGED SECTION OF FLOORBEAM, FABRICATED REP AIR PARTS, CLEANED, TREATED AND INSTALLED PARTS. ALL WORK ACCOMPLISHED IAW FEDEX SRM 53-10-8 AT BS 620 RBL 10 TO 43 WL 208. 2 L 7 3 4F A3WE 1996021600300 19960216 00300 NM 1996 2 16 96FDEA00235 1 19960212 A 5320 SHEAR TIE BOEING 727 72722 1384002 NM BS 1030 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CORROSION (C53-111-01,-3) AFT CARGO BAY, ON SHEAR TIE AT BS 1030 RBL 4 WL 138.5. REPAIRED SHEAR TIE AT BS 1030 RBL 4 WL 138.5 AS PER FEDEX SRM 53-10-4. 2 L 7 3 4F A3WE 1996021600301 19960216 00301 NM 1996 2 16 96FDEA00236 1 19960212 A 5320 SHEAR TIE BOEING 727 72722 1384002 NM BS 1030 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 OBLONGED HOLE ON SHEAR TIE AT BS 1030 RBL 42 WL 165, FOUND WHILE WORKING NR 0053. CUT OFF DAMAGED SHEAR TIE, FABRICATED AND INSTALLED NEW SHEAR TIE AT BS 1030 RBL 42 WL 165 PER FEDEX SRM 53-10-4. 2 L 7 3 4F A3WE 1996021600302 19960216 00302 NM 1996 2 16 96UAL900098 1 19960209 A 2750 ALT DRIVE MOTOR TALLEY CORP 243T1001 BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE TE FLAPS OUT OF ADJUST A UALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 602UA 21863 ON TAXI OUT, RECEIVED TRAILING EDGE FLAP DISAGREE MESSAGE. THE FLAPS LOCKED OUT AT POSITION 5. REPLACED ALTERNATE FLAP DRIVE MOTOR. SHOP FINDINGS DETERMINED THAT THE CLUTCH WOULD NOT RELEASE. THE MOTOR WAS ADJUSTED BY RESETTING THE TORS ION SPRINGS AND ADJUSTING THE CABLE COLLARS. THE MOTOR WAS RETURNED TO STOCK. 2 L 7 2 4F 4 F RT A1NM E3NE 1996021600304 19960216 00304 1996 2 16 96UAL900100 4 19960209 A 2565 D31042118 SLIDE BOEING 757 757222 1384956 NM DOOR 4R LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 DOOR 4 RT, RETURNED TO SHOP FOR TIME CONTROLLED OVERHAUL. THE LOWER INFLATION TUBE IS LEAKING AT THE SEAMS. ALSO, THER E IS CORROSION IN BOTH ASPIRATORS AND ON THE CHECK VALVES. RETURNED TO VENDOR FOR REPAIR. 2 L 7 2 4F RT A2NM 1996021600305 19960216 00305 NM 1996 2 16 96UAL900101 1 19960209 A 5742 AR7077M2MOD1 ACTUATOR BOEING 737 737322 1384676 NM STAB TRIM FAILED A UALA O OTHER J F WARNING INDICATION FLT CONT AFFECTED CR CRUISE 1 WP 29 353UA 21620 24321 WHEN AUTOPILOT 'B' SELECTED, THE STABILIZER OUT OF TRIM LIGHT DISPLAYED. AIRCRAFT STARTED DESCENT AND WOULD NOT HOLD AL TITUDE, THE AIRCRAFT CLIMBED SEVERAL TIMES. AFTER DISCONNECTING AUTOPILOT, COULD NOT TRIM FWD USING YOKE SWITCH OR MANU ALLY TRIM FWD PAST 4.5 UNITS. FOUND MAIN STABILIZER TRIM ACTUATOR INOP. REPLACED THE ACTUATOR, CHECKS OK. 2 L 7 2 4F RT A16WE 1996021600307 19960216 00307 WP 1996 2 16 ABXA9600186 1 19960209 A 3350 60030431 POWER SUPPLY DOUG DC9 DC933F 302207A WP CABIN INOPERATIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 933AX 7391 4548 47291 EMERGENCY LIGHTS INOPERATIVE. FOUND CIRCUIT BREAKER POPPED. REPLACED EMERGENCY LIGHT POWER SUPPLY. 2 L 7 2 4F A6WE 1996021600308 19960216 00308 SO 1996 2 16 COMA9610074 1 19960208 A 3260 922AA2YAGPZ722 SENSOR EMB 120 EMB120RT SO RT MLG DEFECTIVE A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 264CA 120256 LANDING GEAR DID NOT INDICATE RETRACT WHEN CONTROL WAS SELECTED UP. FOUND DEFECTIVE A-SYSTEM PROXIMITY SENSOR RT MLG SW APPED 'A' AND 'B' SYSTEM SENSORS AND DEFERRED SYSTEM PER EMB SERVICE LETTER. 2 L 7 2 4T RT A31SO 1996021600309 19960216 00309 SO 1996 2 16 COMA9610075 1 19960206 A 2910 LINES EMB 120 EMB120RT SO LT/RT ENGINE FROZEN A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 200CD 120200 LEFT AND RIGHT HYDRAULIC RESERVOIR LOW PRESS WARNINGS ILLUMINATED. THAWED THE FROZEN MOISTURE THAT WAS BLOCKING THE HYD RAULIC RESERVOIR BLEED AIR PRESSURIZATION LINES. 2 L 7 2 4T RT A31SO 1996021600310 19960216 00310 SO 1996 2 16 COMA9610076 1 19960209 A 3150 80055711 WARNING UNIT EMB 120 EMB120RT SO AVIONICS DEFECTIVE A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 268CA 11114 3065 120262 PITCH TRIM AURAL WARNING SOUNDED DURING TAKEOFF. TRIM WAS CONFIRMED IN THE TAKEOFF RANGE. REPLACED THE AUDIO WARNING U NIT. 2 L 7 2 4T RT A31SO 1996021600311 19960216 00311 SO 1996 2 16 COMA9610077 1 19960209 A 2797 WIRE EMB 120 EMB120RT SO ELEV TRIM BROKEN A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 268CA 120262 TAKEOFF TRIM WARNING WHEN POWER ADVANCED FOR TAKEOFF. REPAIRED BROKEN WIRE SPLICE AT ELEVATOR TRIM PROXIMITY SENSOR. 2 L 7 2 4T RT A31SO 1996021600312 19960216 00312 EU 1996 2 16 COMA9630034 1 19960209 A 3230 AIR126076 DNLOCK ROLLER SAAB SF340 SF340A 7850100 EU NLG SEIZED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 358CA 340A047 WHEN LANDING GEAR SELECTED DOWN, THE NLG INTRANSIT LIGHT REMAINED ON. REPLACED SEIZED DOWN LOCK ROLLER ON NLG. 2 L 7 2 4T RT A52EU 1996021600313 19960216 00313 NE 1996 2 16 COMA9630035 2 19960209 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LEFT FAILED A COMA O OTHER J WARNING INDICATION UK UNKNOWN 1 SO 01 359CA 340A053 367215 LEFT ENGINE CHIP DETECTOR WARNING ACTIVATED. REPLACED THE LEFT ENGINE. 2 L 7 2 4T 4 T RT A52EU E8NE6 1996021600314 19960216 00314 NE 1996 2 16 P5CA9600133 2 19960209 A 7310 225166 FUEL FILTER BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE NR 2 ENGINE CONTAMINATED A P5CA E D ENGINE SHUTDOWN RETURN TO BLOCK X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 WP 23 858FT 20109 662336 AFTER LEAVING BLOCKS, WHILE ADVANCING POWER, NR 2 ENGINE FLAMED OUT. INSPECTED ENGINE, FOUND MAIN FUEL FILTER CONTAMINA TED WITH DIRT, PAINT AND DEBRIS. REPLACED FUEL FILTER IAW MM 73-21-02, FUEL PUMP AND FCU IAW MM 73-11-01, OPS CHECK NOR MAL. AS PRECAUTIONARY CHANGED FILTERS ON NR 1, NR 3, NR 4 ENGINES, SCHEDULED REPLACEMENT OF ALL 4 FILTERS IN 50 FLIGHT HOURS. 2 L 7 4 4F 4 F A20WE E20EA 1996021600315 19960216 00315 NE 1996 2 16 P5CA9600134 2 19960211 A 7200 ENGINE BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE NR 4 FAILED A A P5CA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 23 858FT 20109 662652 ON CLIMBOUT, NR 4 FILTER BYPASS LIGHT CAME ON LEAVING 5,000 FEET. THE NR 4 THROTTLE RETARDED TO IDLE, OIL QTY WENT TO Z ERO, OIL TEMP TO 150, SHUTDOWN ENGINE, DUMPED FUEL AND RETURNED TO CALI. ENGINE DID NOT SURGE, TAKEOFF EGT WAS NORMAL, ZERO OIL PRESSURE DURING 45 MINUTES WINDMILL. ENGINE DETERMINED UNSERVICEABLE SINCE RESERVICED OIL EXITED ENGINE IMMEDI ATELY VIA TAILPIPE ON GROUND MOTORING. ENGINE REPLACED IAW WORK CARDS MA7100-001 AND MA7100-002. 2 L 7 4 4F 4 F A20WE E20EA 1996021600316 19960216 00316 NM 1996 2 16 SCNA96018 1 19960208 A 3350 582214 CONNECTOR BOEING 727 727259 138408J NM CABIN CORRODED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 SECOND SECTION OF EMERGENCY PATH LIGHTING FROM THE FRONT WAS FOUND TO BE INTERMITTENT. CLEANED CORROSION FROM CANNON PL UG AT THE POWER SUPPLY AND LIGHTING TESTED GOOD. 2 L 7 3 4F A3WE 1996021600317 19960216 00317 WP 1996 2 16 SCNA96019 1 19960209 A 2611 72130000011 SMOKE DETECTOR DOUG DC10 DC1010 3022110 WP NR 3 LAV FAILED A SCNA K NONE N FALSE WARNING UK UNKNOWN 1 GL 15 573SC 46905 THE NUMBER 3 LAVATORY SMOKE DETECTOR SOUNDED CONTINUOUSLY FOR NO APPARENT REASON. REMOVED AND REPLACED NUMBER 3 LAVATOR Y SMOKE DETECTOR AND DETECTOR TESTED GOOD. 2 L 7 3 4F A22WE 1996021600318 19960216 00318 NM 1996 2 16 UPS405416 1 19960202 A 5320 STIFFENER BOEING 747 747121 1384871 NM BS 1800 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK IN UPPER STIFFENER AND DEFORMATION ON LOWER STIFFENER OF FRAME AT BS 1800 LBL 14, AFT CARGO COMPARTMENT. REPLACED STIFFENERS PER SRM 51-30-02. 2 L 7 4 4F A20WE 1996021600319 19960216 00319 NM 1996 2 16 UPS405417 1 19960202 A 5311 FRAME WEB BOEING 747 747121 1384871 NM BS 1760 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK IN FRAME WEB UNDER UPPER CHORD AT BS 1760 LBL 25. REMOVED DAMAGE AND REPA IRED WEB IAW SRM 51-40-02. 2 L 7 4 4F A20WE 1996021600320 19960216 00320 NM 1996 2 16 UPS405418 1 19960201 A 5312 FRAME WEB BOEING 747 747121 1384871 NM BS 1760 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN FOR C-CHECK, MAINTENANCE FOUND DENT IN FRAME WEB UNDER UPPER CHORD AT BS 1760 LBL 52, DAMAGE OUT OF LIMITS PER SRM 53-10-01. REMOVED DAMAGED SECTION OF FRAME WEB AND REPAIRED IAW SRM 51-40-02. 2 L 7 4 4F A20WE 1996021600321 19960216 00321 NM 1996 2 16 UPS405419 1 19960209 A 5311 FRAME FITTING BOEING 747 747121 1384871 NM BS 1960 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FRAME FITTING AT BS 1960 RBL 54. REPLACED FITTING IAW SRM 51-20-01 AND 51-30-02. 2 L 7 4 4F A20WE 1996021600322 19960216 00322 NM 1996 2 16 UPS405420 1 19960201 A 5311 FRAME WEB BOEING 747 747121 1384871 NM BS 1700 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK IN LOWER FRAME WEB BLANKET HOLE AT BS 1700 S-46 LT. STOP DRILLED CRACK, R EPAIRED WEB IAW SRM 53-10-04 FIG 41. 2 L 7 4 4F A20WE 1996021600323 19960216 00323 NM 1996 2 16 UPS405421 1 19960201 A 5311 FRAME WEB BOEING 747 747121 1384871 NM BS 1600 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK IN LOWER FRAME WEB UNDER FRAME UPPER CHORD AT BS 1600 RBL 40. REMOVED DAM AGED SECTION OF FRAME WEB AND REPAIRED IAW SRM 51-40-02 FIG 1. 2 L 7 4 4F A20WE 1996021600324 19960216 00324 NM 1996 2 16 UPS405422 1 19960201 A 5311 FRAME WEB BOEING 747 747121 1384871 NM BS 1620 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK IN LOWER FRAME WEB AT BS 1620 NEAR S-49/48 RT. REMOVED DAMAGED SECTION OF FRAME WEB AND REPAIRED IAW SRM 51-40-02 FIG 1. 2 L 7 4 4F A20WE 1996021600325 19960216 00325 NM 1996 2 16 UPS405424 1 19960210 A 5712 RIB BOEING 747 747121 1384871 NM LE WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK IN UPPER CHORD FLANGE L/E RIB AT I/B LEADING EDGE STATION 802.5, 852.45 AN D 886.5. REPAIRED IAW SRM 57-20-03 FIG 1. 2 L 7 4 4F A20WE 1996021600326 19960216 00326 NM 1996 2 16 UPS405425 1 19960210 A 5712 RIB BOEING 747 747121 1384871 NM LE WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN FOR C-CHECK, MAINTENANCE FOUND 2 CRACKS IN UPPER CHORD OF L/E RIB AT O/B LEADING EDGE STATION 1534.95, 1462.85, 14653.35, 1309.15, 1237.05, 1195.55 AND 1483.95. REPAIRED PER SRM 57-20-03 FIG 1. 2 L 7 4 4F A20WE 1996021600327 19960216 00327 NM 1996 2 16 UPS405426 1 19960210 A 5320 ATTACH BEAM BOEING 747 747121 1384871 NM NR 3 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN FOR C-CHECK, MAINTENANCE FOUND AFT PDU ATTACHMENT BEAM NR 3 CRACKED. REPAIRED PER SRM 51-40-03. 2 L 7 4 4F A20WE 1996021600328 19960216 00328 WP 1996 2 16 UPS805415 1 19960208 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 WHILE IN FOR B-CHECK, MAINTENANCE REPORTED CORROSION 4.375 CRACK COMING FROM RIVET AT LOWER RT SIDE OF FUSELAGE AFT OF N OSE W/W. REPAIR PENDING. 2 L 7 4 4F RT 4A25 1996021600329 19960216 00329 WP 1996 2 16 UPS805423 1 19960123 A 2450 PANEL DOUG DC8 DC873F 302199F WP COCKPIT MALFUNCTIONED A IPXA O OTHER H ELECT. POWER LOSS-50 PC CR CRUISE 1 SO 01 804UP 46004 CREW REPORTED, LOSS OF ALL GENS IN FLIGHT, ACCOMPLISHED QRH CHECKLIST AND GOT ALL 4 BACK ON LINE. REMOVED AND REPLACED BUSS PROTECTION PANEL. RAN ALL 4 ENG AND ACCOM PREF CHECK, ALL OPS CHECK OK. 2 L 7 4 4F RT 4A25 1996021600330 19960216 00330 EU 1996 2 16 WWMA9600020 1 19960212 A 3230 RETRACT MECH SAAB SF340 340B 7860101 EU LANDING GEAR MALFUNCTIONED A WWMA O OTHER J WARNING INDICATION CR CRUISE 1 WP 15 307AE 340B307 THE FLIGHT CREW REPORTED, THE LANDING GEAR FAILED TO COME DOWN. CIRCUIT BREAKER F7 WAS POPPED, CB WAS RESET, THE GEAR C AME DOWN AND WAS LEFT DOWN FOR THE REMAINDER OF THE FLIGHT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORME D LANDING GEAR SWINGS AND COULD NOT DUPLICATE ANY PROBLEMS. 2 L 7 2 4T RT A52EU 1996021600333 19960216 00333 1996 2 16 96ZZZX657 3 19960117 A 6140 CONNECTOR BAG JETSTM JETSTM3101 1500215 EU BETA SWITCH DIRTY A SABA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 05 163PC 678 FLT 5090 - ON 1-17-96 DURING TAKEOFF ROLL, THE BETA LIGHT ILLUMINATED. THE CAPTAIN ABORTED THE TAKEOFF AND RETURNED TO GATE. CANNON PLUGS WERE CLEANED AND THE RESISTANCE OF THE BETA SWITCH AND CANNON PLUGS WERE CHECKED. THE AIRCRAFT WAS THEN GROUND RUN AND A FUNCTION CHECK OF THE BETA SWITCH WAS PERFORMED. ALL INDICATIONS WERE NORMAL. THE AIRCRAFT WAS R ETURNED TO SERVICE. (X) 2 L 7 2 4T RT A21EU 1996021600334 19960216 00334 1996 2 16 96ZZZX658 3 19960117 A 6140 8659566 BETA SWITCH BAG JETSTM JETSTM3101 1500215 EU LT ENGINE INTERMITTENT A SABA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 05 163PC 678 AHN/CLT - FLT 5082 - ON 1-17-96, AIRCRAFT WAS IN PROCESS OF TAKING OFF WHEN THE LT ENGINE BETA LIGHT ILLUMINATED. THE C APTAIN ABORTED TAKEOFF AND RETURNED TO GATE. THE CAPTAIN CONTACTED MAINTENANCE CONTROL AND NOTIFIED THEM OF THE PROBLEM . A MECHANIC WAS SENT TO AHN. THE LT BETA SWITCH WAS REMOVED AND REPLACED AND THE SYSTEM WAS LEAK CHECKED AND THEN FUN CTION TESTED. THE AIRCRAFT WAS THEN FERRIED BACK TO CLT SO THE RII ON THE LEAK CHECK COULD BE C/W. ONCE IN CLT, AN RII INSPECTOR LEAK-CHECKED THE AIRCRAFT AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A21EU 1996021600335 19960216 00335 NM 1996 2 16 96ZZZX659 1 19960125 A 2611 SMOKE LIGHT BOEING 727 727222 1384073 NM CARGO COMPT MALFUNCTIONED A RYNA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 07 7643U 20037 CARGO SMOKE DETECTOR LIGHT ILLUMINATED CLIMBING THROUGH 12,000 FEET. MADE AIR TURN-BACK FOR LANDING AT DAYTON. LIGHT E XTINGUISHED AT 500 FEET AGL AND REMAINED OUT. NO SMOKE NOTED. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED MAIN CARGO COMPARTMENT FOR EVIDENCE OF FIRE WITH NONE NOTED. INSPECTED AND OPERATIONALLY TESTED SMOKE DETECTOR SYSTEM. OPS CHECKS NORMAL. 2 L 7 3 4F A3WE 1996021600336 19960216 00336 NM 1996 2 16 96ZZZX660 1 19960120 A 3411 BACH30B PITOT LINES BOEING 727 727225 1384077 NM E E COMPARTMENT NOT CONNECTED A A MYWA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 803MA 22434 LOG REPORT: F-GL1316 AT MIA - OMEGA'S ARE UNRELIABLE, NO TROUBLE CODES SHOW. BOTH TRANSPONDERS ARE INOP, AUTOPILOT IS OVER-SENSITIVE. CAPTAIN'S PRIMARY AND ALT ALTIMETERS ARE INOP. FOUND PITOT-STATIC LINES DISCONNECTED AT THE ADC. THE LINES WERE RE-CONNECTED. ALL SYSTEMS CHECKED NORMAL. GROUND CHECK OF AUTOPILOT SYSTEM WAS NORMAL. SELF-TEST OF ADC WA S NORMAL. LEAK CHECKED. ALL OK. NOTE: RETURNED FROM FLIGHT. A MAINTENANCE DELAY OF 2 HRS 30 MINUTES WAS INCURRED. 2 L 7 3 4F A3WE 1996021600337 19960216 00337 NM 1996 2 16 96ZZZX661 1 19960118 A 4900 CONNECTOR BOEING 727 727151C 138404V NM APU CONTAMINATED A A RYNA F H ACTIVATE FIRE EXT. DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 CE 07 432EX 19867 NOTE: THIS IS CLOSING ACTION FOR SDR SUBMITTED 1-18-96, SAME AIRCRAFT. PROBLEM: IN CRUISE AT FL 310, APU CRANK LIGHT ILLUMINATED FOLLOWED BY APU EGT RISE TO 300 DEGREES. PULLED THE APU FIRE HANDLE AND APU CONTROL BUS CIRCUIT BREAKER AT WHICH TIME THE APU SHUT DOWN. THE AIRCRAFT WAS LANDED AT IND WITHOUT INCIDENT. CORRECTIVE ACTION: DETERMINED MOISTURE ACCUMULATION IN CONNECTION D1398 LOCATED NEAR APU WAS CAUSE. CLEANED AND RE-SEATED CONNECTION, OPS CHECK GOOD. ALSO, REPLACED THE APU START RELAY, AND THE APU MASTER SWITCH DURING TROUBLESHOOTING. 2 L 7 3 4F A3WE 1996021600338 19960216 00338 NE 1996 2 16 96ZZZX662 2 19960105 A 7200 001A711E1110203 ENGINE COWL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE LT NACELLE BIRD STRIKE A VNAA O OTHER C F.O.D. AP APPROACH 1 GL 07 422JS 3018 PIT - FLT 4041 - DURING APPROACH, THE FLIGHT CREW HEARD SEVERAL AUDIBLE THUMPS FROM THE LEFT SIDE OF THE AIRCRAFT. THE AIRCRAFT LANDED WITH NO FURTHER INCIDENT. PIT MX CONDUCTED A BIRD STRIKE INSPECTION IAW MM 05-57-07. ALSO REMOVED AND REPLACED THE LT ENGINE COWL IAW MM 71-01-00 WHICH WAS DAMAGED AS A RESULT OF THE BIRD STRIKE. AIRCRAFT WAS THEN RETURNE D TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 1996021600339 19960216 00339 NM 1996 2 16 96ZZZX663 1 19960111 A 5610 001A561A0000205 WINDSHIELD DORNER DO32 DO328100 2996000 NM RT COCKPIT FAILED A VNAA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 GL 07 424JS 120 3033 PHI/CVG - FLT BS1003 - EN ROUTE, FLIGHT CREW HEARD A LOUD 'POP' ASSOCIATED WITH THE SHATTERING OF THE FIRST OFFICER'S WI NDSHIELD. CREW WAS ADVISED TO DIVERT TO CAK. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. CAK MAINTENANCE REMOVED AND RE PLACED THE FIRST OFFICER'S WINDSHIELD IAW MM 56-10-00. AIRCRAFT RETURED TO SERVICE. 2 H 7 2 4T RT A45NM 1996021600340 19960216 00340 NM 1996 2 16 C1HA960007 1 19960128 A 2612 CONNECTOR BOEING 727 727191 1384063 NM NR 2 ENGINE DIRTY A C1HA K NONE N FALSE WARNING CL CLIMB 1 WP 23 502MG 19391 NR 2 ENGINE FIRE WARNING CAME ON BRIEFLY ON TAKEOFF AND DURING T/R ON LANDING. ACCOMPLISHED VISUAL AND SHAKE CHECK OF W IRING. CLEANED OIL OUT OF CANNON PLUG. SYSTEM OPS CHECK NORMAL. NO DEFECTS NOTED. PRIOR TO T/S GROUND CHECK ACCOMPLI SHMENT OF SYSTEM AND TEST NORMAL. DURING SHAKE CHECK, UNABLE TO FAULT SYSTEM. NOTE, TAIL CONNECTION FOR LOWER LOOP ON ENGINE WAS VERY OILY AND WAS CLEANED. RE-CHECK OF SYSTEM DURING RUN-UP. NO DEFECTS NOTED. (X) 2 L 7 3 4F A3WE 1996021600341 19960216 00341 WP 1996 2 16 CAL960045 1 19960104 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 83 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 27522 67005 47524 HOU - INSPECTION FOUND A 4 INCH CRACK IN PRESSURE PANEL WEB OF LEFT NOSE WHEELWELL TUNNEL AT STA 83. REPAIRED PER ECRA 5310-03031. (X) 2 L 7 2 4F A6WE 1996021600342 19960216 00342 WP 1996 2 16 CAL960046 1 19960108 A 5210 SB095201385 PAN DOUG DC9 DC932 3022066 WP MAIN CABIN DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 27522 67005 47524 HOU - INSPECTION FOUND A 5 INCH CRACK IN DOOR PAN AT UPPER FORWARD CORNER OF MAIN CABIN DOOR. THE CRACK WAS STOP DRILLE D AND A DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 18A. (X) 2 L 7 2 4F A6WE 1996021600343 19960216 00343 NM 1996 2 16 CAL960047 1 19960120 A 2130 7110025 CONTROL PANEL BOEING 737 7372C0 1384488 NM COCKPIT INOPERATIVE A CALA G O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 SW 09 10242 24552 20071 BDL - FLT 1064 - THE CABIN PRESSURE BEGAN TO FLUCTUATE AT FL 270 WHILE EN ROUTE FROM CLE TO BDL, AND SHORTLY AFTER, BEGA N TO CLIMB RAPIDLY. PRESSURE CONTROL WAS SWITCHED TO STANDBY, BUT CABIN PRESSURE COULD NOT BE MAINTAINED. A DESCENT WA S STARTED, THE OXYGEN MASKS DEPLOYED, AND UNEVENTFUL LANDING MADE AT BDL. MX REMOVED AND REPLACED CABIN PRESSURE CONTRO L PANEL. PRESS CONTROLLER WAS ALSO REPLACED AS PRECAUTIONARY MEASURE. ALL DOOR SEALS AND THE OUTFLOW VALVE WERE INSPEC TED AND FND IN GOOD CONDITION. THE ACFT WAS PRESSURIZED TO 5 PSI, AND ALL SYSTEMS CHECKED GOOD. THE OXYGEN SYSTEM WAS SERVICED AND LEAK CHECK WAS GOOD. (X) 2 L 7 2 4F A16WE 1996021600344 19960216 00344 WP 1996 2 16 CAL960058 1 19960123 A 3610 34H40550 CLAMP DOUG DC10 DC1010 3022110 WP NR 2 ENGINE WORN A CALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 68042 46901 GUM - FLT 0977 - NR 2 ENGINE A-FIRE LOOP LIGHT ILLUMINATED DURING CLIMB OUT OF GUM WITH B-LOOP ON PLACARD. THE B-LOOP H AD BEEN PLACARDED PREVIOUSLY FOR BEING INTERMITTENLY INOPERABLE. LATER, BOTH LOOP LIGHTS AND FIRE LIGHT WERE ON. ENGIN E POWER REDUCED AND ALL FIRE WARNING LIGHTS EXTINGUISHED. ACFT RETURNED TO GUM WHERE IT LANDED WITHOUT INCIDENT. MX FN D NO EVIDENCE OF FIRE. MX FND A HEAVY AIR LEAK AT THE HIGH STAGE BLEED VALVE DUE TO A WORN UPPER CLAMP. LEAK SOURCE LO CATED CLOSE TO PYLON A & B SENSING FIRE WARNING ELEMENT. BLEED VALVE CLAMP REPLACED. A HIGH POWER RUN PERFORMED FOR 20 MINUTES WITH BOTH THE 'A' AND 'B' FIRE WARNING SYSTEMS TESTING AND OPERATING NORMAL. (X) 2 L 7 3 4F A22WE 1996021600345 19960216 00345 NM 1996 2 16 CAL960060 1 19960122 A 3340 HARNESS BOEING 727 727227 1384078 NM NLG WW OUT OF POSITION A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 99763 20772 IAH - FLT 8950 - THE 'NOSE GEAR DOOR' ANNUNCIATOR LIGHT ON SECOND OFFICER'S PANEL AND THE FORWARD PANEL DOOR WARNING LIG HT ILLUMINATED AFTER GEAR WAS RETRACTED DEPARTING IAH. THE AIRCRAFT HAD A HISTORY OF PROBLEMS WITH THE NOSE GEAR DOOR W ARNING LIGHT. GEAR WAS CYCLED, BUT THE LIGHT REMAINED ILLUMINATED. ACFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDE NT. MAINTENANCE FOUND THE NLG TAXI LIGHT HARNESS INTERFERING WITH THE DOORS. THE HARNESS WAS REPOSITIONED. IN ADDITIO N, THE DOORS AND CABLES WERE ADJUSTED IAW MM 32-21-1, PAGE 501. THE GEAR WAS OPERATED SEVERAL TIMES WITH NO DEFECTS NOT ED. (X) 2 L 7 3 4F A3WE 1996021600346 19960216 00346 NM 1996 2 16 CAL960061 1 19960122 A 4990 388019010 OIL PUMP BOEING 757 757224 1384958 NM APU INOPERATIVE A CALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 09 58101 6632 27291 IAH - FLT 0602 - WHILE OPERATING THE APU WITH THE NR 2 GENERATOR PLACARDED INOPERATIVE, THE APU OIL QUANTITY STATUS ADD MESSAGE CAME ON EN ROUTE TO IAH. THE APU SHUT DOWN AUTOMATICALLY SHORTLY BEFORE LANDING. MAINTENANCE FOUND THE APU OIL PUMP AT FAULT. THE APU OIL PUMP WAS REMOVED AND REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD. (X) 2 L 7 2 4F RT A2NM 1996021600347 19960216 00347 WP 1996 2 16 HAL96005 1 19960125 A 2720 59140665519 POWER PACK DOUG DC9 DC951 3022051 WP RUDDER CONTROL FAILED A HALA K NONE J F WARNING INDICATION FLT CONT AFFECTED LD LANDING 1 WP 13 709HA 8531 N1496 47764 HNL - FLT 167 - RUDDER BIND WHEN PUSHING RIGHT RUDDER. LEFT RUDDER IS NORMAL. REMOVED AND REPLACED THE RUDDER POWER PA CKAGE DUE TO BYPASSING HYDRAULIC FLUID. (X) 2 L 7 2 4F A6WE 1996021600348 19960216 00348 WP 1996 2 16 HAL96006 1 19960124 A 3350 60030431 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 709HA 47764 HNL - INFORMATION FROM LOG PAGE 150530. PORTION OF CENTER CABIN EMERGENCY FLOOR LIGHTS COME ON WHEN THE BATTERY SWITCH IS TURNED ON. REPLACED THE BATTERY PACK AND THE OPERATIONAL CHECK WAS GOOD. (X) 2 L 7 2 4F A6WE 1996021600349 19960216 00349 NM 1996 2 16 IXKA960003 1 19960103 A 3310 69482723 TEST MODULE BOEING 727 727251 138408H NM INST PANEL FAILED A IXKA E H ENGINE SHUTDOWN DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 25 258US CAR5034 19977 TPA/ATL - FLT 72 - WHILE PARKING AT GATE, ELECTRICAL SMOKE STARTED TO COME FROM GLARE SHIELD AND INSTRUMENT PANEL. SHU T DOWN ENGINES AND APU. FOUND MASTER DIM AND TEST MODULE M833 BURNED. REMOVED AND REPLACED MASTER TEST AND DIM MODULE. OPS CHECK PER MM 33-15-01. (X) 2 L 7 3 4F A3WE 1996021600350 19960216 00350 NM 1996 2 16 IXKA960004 1 19960122 A 7997 WIRE BOEING 727 727225 1384077 NM NR 3 ENGINE CHAFED A IXKA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 EA 25 356PA 20626 TPA/ATL - FLT 12 - LOW OIL FILTER BYPASS LIGHT CAME ON IN-FLIGHT. IN-FLIGHT SHUT DOWN NR 3 ENGINE PRECAUTIONARY. REMOV ED AND REPLACED NR 3 ENGINE OIL SCREEN, NO CLOGGING FOUND. FOUND CHAFED WIRE 6 INCHES FROM BYPASS PRESSURE SWITCH, D140 2, PIN NR 1. WIRE REPAIRED, OPS CHECK OK PER MM 79-34-01. (X) 2 L 7 3 4F A3WE 1996021600351 19960216 00351 1996 2 16 MZZA96004 4 19960124 A 3425 5222782004 CDI BOEING 727 727227 1384078 NM NR 2 POSITION FAILED A MZZA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 WP 13 86426 0412 21364 GUM - FLT 977 - NR 2 OMEGA WARNING LIGHT ON AND DISPLAY BLANK. RESET CIRCUIT BREAKER, WORKED FOR 15 MINUTES, THEN SAME. AIR RETURN BACK TO GUAM AFTER DUMPING 9,000 POUNDS OF FUEL. MAINTENANCE REPLACED NR 2 OMEGA CDU AND RPU, WITH NO HELP . FURTHER TROUBLESHOOTING FOUND PROBLEM WITH NR 2 CDI ASSEMBLY. REMOVED AND REPLACED NR 2 CDI, AND SYSTEM OPERATION CH ECK GOOD. (X) 2 L 7 3 4F A3WE 1996021600353 19960216 00353 WP 1996 2 16 ORJA96002 1 19960107 A 3350 41B004AD073 BATTERY PACK EA1D13D3 DOUG DC9 DC987 3022087 WP EMPENNAGE DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 752RA 49780 EMERGENCY LIGHTS IN EMPENNAGE INOP. REPLACED BATTERY PACK. (X) 2 L 7 2 4F RT A6WE 1996021600354 19960216 00354 EU 1996 2 16 P2RA960001 1 19960118 A 3240 BRAKES AIRBUS 300 A300B4203 3930306 EU LANDING GEAR FAILED A P2RA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 14975 W270 261 BRAKES SPONGY - GO ALL THE WAY TO FLOOR. BRAKES GRAB IN 'NORMAL'. INSUFFICIENT BRAKE PRESSURE IN 'ALTERNATE'. REPLACE D LT AND RT BRAKE MOTORS. REPLACED STANDBY BRAKE RESERVOIR, REPLACED EMERGENCY BRAKE DISTRIBUTION VALVE, FLUSHED BRAKE SYSTEM, SERVICED BRAKE SYSTEM. OPS CHECK, LEAK CHECK, HI-SPEED TAXI CHECK, GOOD IN ALL MODES OF OPERATION. (X) 2 L 7 2 4F A35EU 1996021600355 19960216 00355 EU 1996 2 16 P2RA960002 1 19960122 A 3240 NAS16126 O-RING C232670011 AIRBUS 300 A300B4203 3930306 EU MLG WW LEAKING A P2RA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 23 14975 261 IN 'NORMAL', BRAKES GRAB EITHER LEFT OR RIGHT. PEDAL OK IN 'ALTERNATE'. TOWER REPORTED A LITLE SMOKE ON TAXI OUT IAH. AIRCRAFT RETURNED TO RAMP - NR 5 TIRE ON INSPECTION SHOWED RUBBER RIBBONS ON CASE. BRAKE TEMPS NORMAL. INSPECTED ALL BRAKES IAW MM 32-42-00 - SYSTEM LEAK AND OPS CHECK GOOD. ROLLED NR 5 TIRE WHILE ON JACK - CHECKED GOOD. REMOVED AND REP LACED O-RING ON SWIVEL UNDER SERVO VALVE. LEAK CHECKED GOOD. (X) 2 L 7 2 4F A35EU 1996021600359 19960216 00359 1996 2 16 RAIA960101 4 19960103 A 3418 C771075 LIFT TRANSDUCER BAG JETSTM JETSTM3201 1500217 EU LEFT WING FAILED A RAIA O OTHER J WARNING INDICATION CL CLIMB 1 CE 03 430AM 9139 1211 880 STL - FLT 7326 - ON CLIMB-OUT AT 2,000 FEET, LEFT STALL SYSTEM ACTIVATED AND WOULD NOT STOP. HAD TO TURN OFF STALL SYST EM TO DEACTIVATE STICK SHAKER. MAINTENANCE REMOVED AND REPLACED LEFT LIFT TRANSDUCER. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4T RT A56EU 1996021600360 19960216 00360 EU 1996 2 16 RAIA960105 1 19960107 A 3222 B00A703056A STRUT BAG JETSTM JETSTM3201 1500217 EU NOSE GEAR REQUIRED SERVICE A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 341TE 7666 1962 950 JLN - FLT 7068 - UNABLE TO RAISE GEAR. USED OVERRIDE NOSE GEAR, INDICATED RED. LOWERED GEAR AND RETURNED TO JLN. MAIN TENANCE SERVICED NOSE STRUT, GEAR SWING OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4T RT A56EU 1996021600361 19960216 00361 EU 1996 2 16 RAIA960107 1 19960104 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 425TE 125 STL - MAINTENANCE - EMERGENCY TRACK LIGHTING INOP. MAINTENANCE REMOVED AND REPLACED BATTERY PACKS AT LOCATIONS 2A AND 2 B, 5C AND 5D. BATTERY PACKS 2A AND 2B, TT: 15,271.0, TSO: 2,000.0. BATTERY PACKS 5C AND 5D, TT: 15,271.0, TSO: 2,0 00.0. (X) 2 H 7 2 4T RT A53EU 1996021600362 19960216 00362 EU 1996 2 16 RAIA960112 1 19960107 A 3222 B00A70356A STRUT BAG JETSTM JETSTM3201 1500217 EU NLG REQUIRED SERVICE A RAIA O OTHER J WARNING INDICATION CL CLIMB 1 CE 03 430AM 10145 4235 880 STL - FLT 7440 - LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. MAINTENANCE SERVICED NOSE STRUT, GEAR SWING OPERATION CH ECKS GOOD. (X) 2 L 7 2 4T RT A56EU 1996021600363 19960216 00363 EU 1996 2 16 SIMA960261 1 19960126 A 3350 3011151 POWER SUPPLY AEROSP ATR42 ATR42300 8680920 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 422MQ 7919 028 CMI - EMERGENCY LIGHT POWER PACK AT 30WL INOP. REMOVED AND INSPECTED POWER PACK AND BATTERY AT 30WL. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1996021600364 19960216 00364 NM 1996 2 16 TAOA019603 1 19960122 A 3350 900835A BATTERY PACK BOEING 727 727294 1384088 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 921TS UA4442 22043 AFT CABIN OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERY PACK AND BASE. OPERATIONAL CHECK OK. (X) 0 4 A3WE 1996021600365 19960216 00365 NM 1996 2 16 TAOA019604 1 19960122 A 2910 BACH30AX157 HOSE BOEING 727 727227 1384078 NM RT ELEVATOR LEAKING A TAOA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 EA 15 925TS 21244 SYSTEM A-HYDRAULIC QUANTITY LOW ON LANDING. BRAKE PRESSURE FAILED, THEN RECOVERED. REPLACED LEAKING RT ELEVATOR MODULE PRESSURE HOSE. LEAK CHECK AND OPERATIONAL CHECK OK. (X) 2 L 7 3 4F A3WE 1996021600366 19960216 00366 NM 1996 2 16 WRLA96004 1 19960120 A 7931 DC6210SLK3SN TRANSMITTER DOUG MD11 MD11 3023602 NM NR 2 ENGINE LOOSE WIRING A WRLA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 273WA 48519 ON TAXIING OUT, FLIGHT CREW NOTED NR 2 ENGINE OIL PRESSURE DROPPED TO 'ZERO' IN ENGINE START. FLIGHT CREW ELECTED TO RE TURN TO GATE FOR CORRECTIVE ACTION. AIRCRAFT RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE PERSONNEL FOUND CONNECTORS LOOSE ON NR 2 OIL PRESSURE TRANSMITTER. TIGHTENED CONNECTORS ON NR 2 OIL PRESSURE TRANSMITTER. CHECKED GOOD ON ENGINE RUN. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 3 4F RT A22WE 1996021600367 19960216 00367 EU 1996 2 16 9603503204 1 19960212 A 2740 42049 MOTOR AIRBUS 320 A320211 3930320 EU HORIZ STAB LEAKING A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 304US 40 DURING CLIMBOUT, NOTICED AN ACCUMULATION OF NOXIOUS FUMES IN THE COCKPIT AND CABIN. CREW DONNED THE OXYGEN MASKS AND TH E AIRCRAFT RETURNED TO MIA WITH EMERGENCY EQUIPMENT STANDING BY. AN UNEVENTFUL OVERWEIGHT LANDING WAS ACCOMPLISHED. MA INTENANCE FOUND THE GREEN HYDRAULIC SYSTEM TRIMMABLE HORIZONTAL STABILIZER HYDRAULIC MOTOR LEAKING THROUGH THE CASE DRAI N. THE FLUID WAS INGESTED INTO THE APU INLET. REPLACED THE HYDRAULIC MOTOR, LEAK AND OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996021600368 19960216 00368 1996 2 16 9603512298 4 19960212 A 3418 2566A30 TRANSDUCER BOEING 727 727251 138408H NM E/E COMPT MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 298US 33550 5507 22152 DURING ROTATION ON A 5 DEGREE FLAP TAKEOFF, THE STALL WARNING CONTROL COLUMN SHAKER INITIATED. SHAKER CONTINUED THROUGH CLIMB DURING FLAP RETRACTION AT NORMAL SPEEDS. VISUAL SCAN OF THE WINGS WAS NORMAL. AN EMERGENCY LANDING WAS DECLARED AND THE AIRCRAFT RETURNED TO MSP WITHOUT INCIDENT. MAINTENANCE REPLACED THE STALL WARNING COMPUTER AND TRANSDUCER, OPE RATIONAL CHECK NORMAL. 2 L 7 3 4F A3WE 1996021600369 19960216 00369 NM 1996 2 16 9603522298 1 19960212 A 3231 LINKAGE BOEING 727 727251 138408H NM NLG DOOR OUT OF ADJUST A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 298US 22152 DURING APPROACH UPON GEAR EXTENSION, NOSE LANDING GEAR DOOR INDICATION REMAINED ILLUMINATED. RECYCLED GEAR, INDICATION CEASED UPON RETRACTION AND REMAINED ILLUMINATED FOR APPROXIMATELY 20 SECONDS AFTER EXTENSION. ALL GEAR LIGHT INDICATED DOWN AND LOCKED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED THE DOOR CLOSED TENSION AND LUBRICATED THE ACTIVATION LINKAGE. OPERATIONAL CHECK WAS NORMAL. 2 L 7 3 4F A3WE 1996021600370 19960216 00370 WP 1996 2 16 9603531161 1 19960210 A 3350 POWER SUPPLY DOUG DC10 DC1040 3023508 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 161US 46770 DURING LINE CHECK, THE EMERGENCY LIGHT TEST LIGHT WOULD NOT ILLUMINATE. REPLACED POWER SUPPLY AND BATTERY. 2 L 7 3 4F A22WE 1996021600371 19960216 00371 WP 1996 2 16 9603549753 1 19960209 A 3297 WIRE DOUG DC9 DC941 302207N WP LT MLG DOOR SW LOOSE A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 753NW 47117 AFTER GEAR RETRACTION, GEAR DOOR OPEN LIGHT STAYED ON. FLIGHT CREW FOLLOWED COCKPIT OPERATING PROCEDURE AND RECYCLED GE AR, LIGHT REMAINED ON. FLIGHT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LOOSE WIRE ON LEFT MAIN LANDING GEAR DOOR SWTICH. REPLACED THE MAIN LANDNG GEAR DOOR SWITCH AND LEFT AND RIGHT MAIN LANDING GEAR DOOR SWITCHES. OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996021600372 19960216 00372 1996 2 16 9603551157 4 19960212 A 3417 HG280D5 COMPUTER DOUG DC10 DC1040 3023508 WP LEFT FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 157US 13667 5846 46766 DURING TAKEOFF, CAPTAIN'S AIRSPEED INDICATOR FROZE AT 100 KNOTS WHILE THE FIRST OFFICER'S INDICATOR READ 60 KNOTS. TAKE OFF WAS ABORTED. THE CAPTAIN'S AIR DATA COMPUTER WAS SWAPPED WITH THE NR 3 COMPUTER AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A22WE 1996021600373 19960216 00373 NE 1996 2 16 9603569305 2 19960205 A 7250 TURBINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE NR 1 ENGINE FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 01 307RC 48086 708426 NR 1 ENGINE EXPERIENCED A CONTAINED TURBINE FAILURE ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE ENGINE WITH A SERVICEABLE UNIT. 2 L 7 2 4F 4 F A6WE E9NE 1996021600374 19960216 00374 WP 1996 2 16 9603579914 1 19960210 A 3260 UPLATCH MECH DOUG DC9 DC931 3022065 WP LT MLG ICED UP A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 964N 47416 DURING CLIMBOUT, THE LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. RECYCLED GEAR AND NORMAL INDICATIONS WERE ACHIEVED. FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LEFT MAIN G EAR UPLATCH MECHANISM PACKED WITH SNOW AND ICE. CLEANED AND LUBED MECHANISM AND OPERATIONAL CHECK NORMAL ON GEAR CYCLE. 2 L 7 2 4F A6WE 1996021600375 19960216 00375 EU 1996 2 16 9603583234 1 19960205 A 3350 321430 BATTERY PACK AIRBUS 320 A320211 3930320 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 334NW 339 DURING LINE MAINTENANCE, THE FORWARD LEFT EPSU 10 WL FAILED THE EMERGENCY LIGHTS TEST. REPLACED THE BATTERY PACK AND OP ERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996021600376 19960216 00376 NE 1996 2 16 9603599853 2 19960209 A 7230 COMPRESSOR DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE NR 2 ENGINE STALLED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 01 762NC 47117 696766 THE NR 2 ENGINE COMPRESSOR STALLED ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAI NTENANCE REMOVED A PIECE OF CARDBOARD FROM THE INLET AND INSPECTED THE ENGINE. NO DISCREPANCIES WERE NOTED. ENGINE PER FORMANCE RETURNED TO NORMAL. 2 L 7 2 4F 4 F A6WE E2EA 1996021600377 19960216 00377 WP 1996 2 16 9603601150 1 19960211 A 7830 TR UNLOCK LIGHT DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 1 ENGINE ILLUMINATED A NWAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 01 150US 46759 86178 DURING TAKEOFF, THE NR 1 REVERSER UNLOCK LIGHT ILLUMINATED. TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE NR 1 REVERSER AND FOUND NORMAL. PLACARD NR 1 REVERSER INDICATION PER MEL 78-2A. 2 L 7 3 4F 4 F A22WE E20EA 1996021600378 19960216 00378 NE 1996 2 16 9603616740 2 19960211 A 7200 ENGINE BOEING 747 747251F 1384898 NM PWA JT9 JT9D7Q 52054 NE NR 3 LOW POWER A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 640US 23888 02025 DURING TAKEOFF ROLL, THE NR 3 ENGINE FAILED TO OBTAIN TAKEOFF POWER. TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO T HE GATE. MAINTENANCE CHECKED INLET, EXHAUST, AND PS4 LINES TO CONTROL FOR SECURITY. ALSO, CHECKED EVC FEEDBACK CABLE T O 3.0 BLEED AND RAN ENGINE AT TAKEOFF POWER, ALL PARAMETERS WERE NORMAL. 2 L 7 4 4F 4 F A20WE E3NE 1996021600379 19960216 00379 NM 1996 2 16 96UAL900103 1 19960212 A 3350 LIGHT BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 620UA 21880 AFT CROSS AISLE FLOOR EMERGENCY EEL LIGHT INOP. REPLACED LAMP, OPERATIONS CHECK IS NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 1996021600380 19960216 00380 WP 1996 2 16 96UAL900104 1 19960212 A 3350 BATTERY PACK DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1854U 47813 AFT EMERGENCY LIGHT FAILED BATTERY TEST. REPLACED AFT EMERGENCY LIGHT BATTERY (P/N EMSE299A). 2 L 7 3 4F 4 F A22WE E23EA 1996021600382 19960216 00382 NM 1996 2 16 96UAL900106 1 19960212 A 2782 ACTUATOR DOWTY 269002910 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LE SLAT FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 7464U 13759 21918 DURING FLAP RETRACTION ON DEPARTURE, LED NR 6 REMAINED FULLY EXTENDED AFTER MOVING FLAP HANDLE FROM POSITION 2 TO ZERO. FLIGHT RETURNED TO ORD. NR 6 LEADING EDGE SLAT ACTUATOR FAILED IN THE EXTENDED POSITION. ACTUATOR WAS REPLACED AND OP ERATION WAS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1996021600383 19960216 00383 NM 1996 2 16 96UAL900107 1 19960212 A 3350 CONNECTORS BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DIRTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7443U 21897 TWO EMERGENCY EXIT LIGHTS INOPERATIVE AT LEFT OVERWING WINDOWS. CLEANED CONNECTIONS, CHECKS OKAY. 2 L 7 3 4F 4 F A3WE E2EA 1996021600384 19960216 00384 NM 1996 2 16 96UAL900108 1 19960212 A 3350 POWER SUPPLY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7463U 21917 EXTERIOR LEFT FWD OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY ASSEMBLY (P/N M654). 2 L 7 3 4F 4 F A3WE E2EA 1996021600385 19960216 00385 NM 1996 2 16 96UAL900109 1 19960212 A 2120 AIR DISTR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN SMOKE A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 7257U 21404 WHILE OPERATING PACKS ON GROUND WITH APU AIR, CABIN FILLED WITH SMOKE. OPERATED PACKS FROM APU FOR OVER AN HOUR AND NO ODOR NOTED. SUSPECT DE-ICING FLUID. CHECKED APU AND FLOW MULTIPLIER INLETS, NO RESIDUAL FLUID NOTED. 2 L 7 3 4F 4 F A3WE E2EA 1996021600386 19960216 00386 NM 1996 2 16 96UAL900110 1 19960212 A 5240 651759612 DOOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE EXTERNAL PWR MISSING A UALA A UNSCHED LANDING D INFLIGHT SEPARATION NR NOT REPORTED 1 WP 29 7273U 21420 CREW REPORTS, LOUD NOISE FROM NOSE GEAR AREA. GROUND CREW FOUND EXTERNAL POWER DOOR MISSING. NEW DOOR AND ATTACHMENTS INSTALLED. 2 L 7 3 4F 4 F A3WE E2EA 1996021600387 19960216 00387 WP 1996 2 16 ABXA9600187 1 19960209 A 3350 60030431 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 980AX 4141 47176 WITH A/C POWER OFF, BATTERY OFF AND EMERGENCY LIGHT SWITCH OFF, EMERGENCY LIGHTS REMAIN ON. REPLACED EMERGENCY LIGHT PO WER SUPPLY IAW DC9 MM 33-56. 2 L 7 2 4F A6WE 1996021600388 19960216 00388 WP 1996 2 16 ABXA9600188 1 19960211 A 3230 FOLLOW-UP MECH DOUG DC8 DC863 302198A WP LT MLG OUT OF ADJUST A ABXA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 817AX 45928 DURING CLIMB, RED GEAR UNSAFE LIGHT ILLUMINATED AFTER GEAR RETRACTION. RECYCLED LANDING GEAR TWICE AND RED UNSAFE LIGHT REMAINED ILLUMINATED. RIGGED LEFT MAIN GEAR FOLLOW-UP MECHANISM IAW DC8 MM, CHAPTER 32-31-5. OPS CHECK GOOD DURING GE AR RETRACTION CHECK. 2 L 7 4 4F 4A25 1996021600389 19960216 00389 SO 1996 2 16 COMA9610078 1 19960209 A 3411 0856NB1 PITOT TUBE EMB 120 EMB120RT SO NR 1 DEFECTIVE A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 168CA 120168 PILOTS AIR SPEED INDICATOR FAILED DURING FLIGHT. REPLACED THE NR 1 PITOT TUBE. 2 L 7 2 4T RT A31SO 1996021600390 19960216 00390 EU 1996 2 16 COMA9630036 1 19960211 A 2710 7227150623 BELL CRANK SAAB SF340 SF340A 7850100 EU LT AILERON SEIZED BEARING A COMA K NONE F FLT CONT AFFECTED UK UNKNOWN 1 SO 01 347CA 340A028 CREW REPORTS, THAT AILERONS ARE STIFF AND HARD TO MOVE. REPLACED THE LT INBD AILERON BELL CRANK ASSY. 2 L 7 2 4T RT A52EU 1996021600391 19960216 00391 EU 1996 2 16 COMA9630037 1 19960211 A 2460 FU1540200 FUSE SAAB SF340 SF340A 7850100 EU RIGHT FAILED A COMA K NONE H ELECT. POWER LOSS-50 PC UK UNKNOWN 1 SO 01 358CA 340A047 RT BATTERY BUS IS INOP. REPLACED 200 AMP FUSE AT RT POWER DISTRIBUTION UNIT. 2 L 7 2 4T RT A52EU 1996021600392 19960216 00392 EA 1996 2 16 COMA9660028 1 19960212 A 2760 SECU CNDAIR CL600 CL6002B19 EA COCKPIT TRIPPED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 954CA 7100 DURING TAKEOFF, FLIGHT SPOILER CAUTION MESSAGE ON EICAS. RESET THE SPOILER ELECTRONIC CONTROL UNITS. NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 1996021600393 19960216 00393 EA 1996 2 16 COMA9660029 1 19960211 A 3350 362624 LAMP CNDAIR CL600 CL6002B19 EA CABIN INOP A COMA K NONE L NO TEST UK UNKNOWN 1 SO 01 924CA 7026 FORWARD AMBER AISLE EMERGENCY LIGHTS ARE INOP. REPLACED FLEXIBLE LAMP ASSY. 2 L 7 2 4F RT A21EA 1996021600395 19960216 00395 NM 1996 2 16 DL72K960295 1 19960107 A 5754 6516224101 SKIN BOEING 727 727232 1384082 NM NR 1 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 481DA 20861 UPON ROUTINE INSPECTION, THE TAI DUCT SKIN CUTOUT WAS CRACKED. REPAIRED AS PER MM 57-54-0, FOR NR 1 L/E SLAT. 2 L 7 3 4F A3WE 1996021600396 19960216 00396 NM 1996 2 16 DL72L960313 1 19960210 A 3350 1102833 LIGHT BOEING 727 727232 1384082 NM AIRSTAIR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 507DA 21309 OVERHEAD EMERGENCY LIGHT AT BOTTOM OF AIRSTAIRS IS INOP. REPLACED LIGHT ASSEMBLY. 2 L 7 3 4F A3WE 1996021600397 19960216 00397 NM 1996 2 16 DL72S960297 1 19960208 A 5522 SKIN BOEING 727 727232 1384082 NM RT ELEV TORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 411DA 21223 FOUND DURING E-1 LETTER CHECK, .75 INCH TEAR RIGHT ELEVATOR LWR SKIN 15 INCHES AFT OF HINGE CENTERLINE AND 6 FEET O/B OF I/B END. REPAIRED PER SRM 55-20-3 FIG 4. 2 L 7 3 4F A3WE 1996021600398 19960216 00398 NM 1996 2 16 DL72S960298 1 19960208 A 5320 WEB BOEING 727 727232 1384082 NM BS 1243 CRACK A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 411DA 21223 FOUND DURING E-1 LETTER CHECK, .25 INCH CRACK LWR TORQUE BOX VERTICAL WEB LIGHTENING HOLE FWD OF BS 1243 LEFT SIDE. R EPAIRED PER M/M 53-11-0 PAR 15. 2 L 7 3 4F A3WE 1996021600399 19960216 00399 NM 1996 2 16 DL72S960300 1 19960203 A 5312 BLKHD CHANNEL BOEING 727 727232 1384082 NM BS 720 WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 518DA 21469 AT MID VISIT 2, FOUND VERT SUPPORT CHANNEL WORN AT TOP STA 720D ABOVE STR 26 LT. REMOVED DAMAGED SECTION PER SRM 53-10- 9 FIG 9. DRILLED NEW DOUBLER AND INSTALLED PER SRM 53-10-9 FIG 9. 2 L 7 3 4F A3WE 1996021600400 19960216 00400 NM 1996 2 16 DL72S960310 1 19960209 A 3350 900542 BATTERY PACK BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 531DA 21814 DURING LAYOVER CHECK, FOUND FWD AND AFT BULLNOSE EMERGENCY LIGHTS WOULD NOT TEST. REPLACED BATTERY PACK AT FWD 1088 AND REPLACED BATTERY PACK AT AFT 1089, NOW CHECKS OK. 2 L 7 3 4F A3WE 1996021600401 19960216 00401 NM 1996 2 16 DL72S960311 1 19960209 A 3350 IDENTIFIER BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 531DA 21814 DURING LAYOVER CHECK, AFT CABIN DOOR EMERGENCY EXIT IDENTIFIER INOP ON TEST. REPLACED AFT CABIN DOOR IDENTIFIER AND REP AIRED BROKEN WIRE AT D9069P. 2 L 7 3 4F A3WE 1996021600402 19960216 00402 NM 1996 2 16 DL72S960312 1 19960210 A 3230 RETRACT MECH BOEING 727 727232 1384082 NM RT MLG LACK OF LUBE A DALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 27 517DA 21433 RT MAIN GEAR DID NOT RETRACT AFTER TAKEOFF. INSPECTED, LUBRICATED RT MAIN GEAR. JACKED A/C CYCLED GEAR SEVERAL TIMES, OPERATION NORMAL. 2 L 7 3 4F A3WE 1996021600403 19960216 00403 NM 1996 2 16 DL72S960316 1 19960211 A 3350 LIGHT BOEING 727 727232 1384082 NM AIRSTAIR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 421DA 21274 AIRSTAIR COMPARTMENT EMERGENCY LIGHT IS INOP DURING TEST. REPLACED LIGHT ASSY, CHECKS GOOD. 2 L 7 3 4F A3WE 1996021600404 19960216 00404 NM 1996 2 16 DL72S960323 1 19960122 A 3350 RPS1 POWER SUPPLY BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 489DA 21019 ON PREFLIGHT CHECK, EMERGENCY TRACK LIGHTING INOP AT MID CABIN. REPLACED AFT BATTERY PACK AND BASE FOR FLOOR TRACK SYS, OPS NORMAL. 2 L 7 3 4F A3WE 1996021600405 19960216 00405 NM 1996 2 16 DL72S960326 1 19960210 A 3231 RETRACT MECH BOEING 727 727232 1384082 NM NLG DOOR OUT OF RIG A DALA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 516DA 21432 AFTER TAKEOFF WITH GEAR HANDLE IN OFF POS, FELT AND HEARD LOUD THUMP 4 OR 5 TIMES AT APPROX 2 MIN INTERVALS. PROBLEM WE NT AWAY WITH HANDLE IN UP POSITION. RIGGED AND ADJUSTED NOSE GEAR DOORS PER MM, OPERATION NORMAL. 2 L 7 3 4F A3WE 1996021600406 19960216 00406 NM 1996 2 16 DL72W960302 1 19960109 A 5210 SEAL BOEING 727 727247 138408F NM L1 DOOR OUT OF POSITION A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 293WA 22111 AFTER TAKEOFF, EXPERIENCED EXTREMELY LOUD NOISE FROM FWD ENTRY DOOR. ACFT RTN TO BLK AT 1331. FOUND L1 DOOR LOWER HING E FLAPPER SEAL OUT OF POSITION. CYCLE DOOR, SEAL POSITION NORMAL. 2 L 7 3 4F A3WE 1996021600407 19960216 00407 NM 1996 2 16 DL72W960306 1 19960209 A 5754 ANGLE BOEING 727 727247 138408F NM NR 7 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2809W 20581 SLAT ANGLE CRACKED UNDER NR 7 SLAT I/B STOP PAD AREA. FOUND DURING LETTER CHECK, NR 7 L/E SLAT. INSTALLED REPAIR PER M M 57-54-0. 2 L 7 3 4F A3WE 1996021600408 19960216 00408 NM 1996 2 16 DL72W960307 1 19960209 A 5313 STRINGER BOEING 727 727247 138408F NM BS 850 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2809W 20581 A 1 INCH CRACK THROUGH HORIZ LEG OF STR 18A AND STA 950. REPAIRED PER MM 53-12-0, FOUND AT LETTER CHECK. 2 L 7 3 4F A3WE 1996021600409 19960216 00409 NM 1996 2 16 DL72W960308 1 19960209 A 2780 BRACKET BOEING 727 727247 138408F NM NR 6 LE FLAP ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2809W 20581 FOUND AT LETTER CHECK, NR 6 L/E FLAP ACTUATOR MOUNT BOX CRACKED, I/B SIDE UPPER AND LWR CORNERS. REPAIRED PER MM 57-20- 21. 2 L 7 3 4F A3WE 1996021600410 19960216 00410 NM 1996 2 16 DL72W960309 1 19960209 A 2780 ANGLE BOEING 727 727247 138408F NM NR 1 SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2809W 20581 A 1.5 INCH CRACK AT NR 1 SLAT ACTUATOR O/B ATTACH ANGLE. REPAIRED PER MM 57 20-21. 2 L 7 3 4F A3WE 1996021600411 19960216 00411 NM 1996 2 16 DL72W960318 1 19960206 A 5320 WEB BOEING 727 727247 138408F NM BS 285.5-294.5 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2807W 20579 DURING INSPECTION, THE LT SIDEWALL WEB OF THE NOSE WHEEL WELL HAS A 1.25 INCH CRACK BETWEEN STA 294.5 AND 285.5, APPROXI MATELY AT WL 170. THE REPAIR IS ACCOMPLISHED IN ACCORDANCE WITH S/B 727-53-145. 2 L 7 3 4F A3WE 1996021600412 19960216 00412 NM 1996 2 16 DL72W960320 1 19960210 A 5320 651841483 WEB BOEING 727 727247 138408F NM FS 294.5 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2809W 20581 DURING INSPECTION, THE LT SIDEWALL WEB OF THE NOSE WHEEL WELL HAD A 1.25 INCH CRACK AT STA 294.5, APPROXIMATELY AT WL 17 0. THE DAMAGED PORTION WAS TRIMMED OUT AND A REPAIR DOUBLER AND STRAPS WAS INSTALLED IN ACCORDANCE WITH B727-53-145. 2 L 7 3 4F A3WE 1996021600413 19960216 00413 NM 1996 2 16 DL73E960325 1 19960210 A 3350 BATTERY BOEING 737 7372S3 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 369DL 21776 ON PREFLIGHT, EMERGENCY EXIT LIGHT AT FWD SERVICE DOOR INOP. REPLACED BATTERIES, BULBS AND SECURED WIRE TERMINAL, OPERA TION NORMAL. 2 L 7 2 4F RT A16WE 1996021600414 19960216 00414 NM 1996 2 16 DL757960301 1 19960209 A 3230 BACB10Y6 ROD END BOEING 757 757232 1384965 NM NLG BROKEN A DALA O OTHER E VIBRATION/BUFFET CL CLIMB 1 SO 27 608DA 22815 JUST AFTER TAKEOFF, A THUD WAS HEARD IN THE FWD FUSELAGE AREA. EXTREME VIBRATION FOLLOWED GEAR RETRACTION IN NOSE WHEEL AREA. FOUND ROD END BROKEN ON FWD NOSE GEAR OPERATING ROD. REPLACED RT FWD OPERATION ROD ASSEMBLY, PERFORMED ADJ AND TEST. 2 L 7 2 4F RT A2NM 1996021600415 19960216 00415 NM 1996 2 16 DL757960322 1 19960208 A 2910 AS11506K0451 HYD HOSE BOEING 757 757232 1384965 NM LT MLG LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SO 27 623DL 22913 ON TAKOFF, LANDING GEAR WOULD NOT RETRACT. FOUND LEFT SHUTTLE VALVE FUSE SET. FOUND LEFT TRUCK POSITION PRESSURE LINE BLOWN. REPLACED LEFT SHUTTLE VALVE FUSE AND LEFT TRUCK POSITION ACTUATOR. ALSO, REPLACED BLOWN LINE AND OPERATION NORM AL. 2 L 7 2 4F RT A2NM 1996021600416 19960216 00416 NE 1996 2 16 DL76L960317 2 19960209 A 7230 COMPRESSOR BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE DAMAGED A DALA K NONE C F.O.D. IN INSP/MAINT 1 SO 27 184DN 27111 724148 DURING INSPECTION, FOUND FOD TO 2ND, 3RD, 5TH AND 6TH STAGE COMPRESSOR. REPLACED ENGINE, ROUTED TO SHOP. 2 L 7 2 4F 4 F RT A1NM E24NE 1996021600417 19960216 00417 NM 1996 2 16 DL76S960305 1 19960210 A 3230 ACTUATOR 273T63008 BOEING 767 767332 1382001 NM LT MLG FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 116DL 00040 23275 FAILURE OF LEFT MLG TO RETRACT AFTER T/O. FOUND LEFT MLG DRAG BRACE ACTUATOR FAILED INTERNALLY, PISTON FELL OUT OF ACT BODY UPON REMOVAL. REPLACED ACTUATOR, OPERATION NORMAL. 2 L 7 2 4F RT A1NM 1996021600418 19960216 00418 WP 1996 2 16 DLL13960303 1 19960208 A 3350 BATTERY CHARGER LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 789DL 193A1142 L4 EMERGENCY SLIDE LIGHT INOP. REPLACED BATTERY/CHARGER, OPERATION NORMAL. 2 L 7 3 4F A23WE 1996021600419 19960216 00419 WP 1996 2 16 DLL17960319 1 19960211 A 3350 LIGHT LKHEED 1011 10113853 5265020 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 768DL 193H1216 EMERGENCY TRACK LIGHTS INOP AT 37C AND 39F. RELAMPED, CKS OK. 2 L 7 3 4F A23WE 1996021600420 19960216 00420 NM 1996 2 16 DLM88960314 1 19960210 A 2530 OVEN DOUG MD88 MD88 3023688 NM FWD GALLEY SMOKING A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 900DE 53372 FIRST CLASS GALLEY OVEN SMOKES, NO EVIDENCE OF FOOD SPILLAGE REPORTED. INSPECTED F/C OVEN, OPN NORMAL. 2 L 7 2 4F RT A6WE 1996021600421 19960216 00421 NM 1996 2 16 DLM90960324 1 19960122 A 3397 WIRE DOUG MD90 MD9030 3023690 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 904DA 53384 ON PREFLIGHT, FLOOR EMERGENCY PATH LIGHTS INOP IN FWD CABIN. FOUND BROKEN WIRE AT SEAT ROW 10. REPAIRED WIRE, OPERATIO N NORMAL. 2 L 7 2 4F RT A6WE 1996021600422 19960216 00422 NM 1996 2 16 P5CA9600135 1 19960206 A 5330 SKIN BOEING 747 747122 1384872 NM CARGO DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 ON PREDEPARTURE CHECK, FOUND SKIN DAMAGE AT FORWARD EDGE OF OPENING FOR REAR LOWER CARGO DOOR. DOOR FRAME TEAR STRIP AN D OUTER SKIN DISTORTED AND CRACKED. REPAIRED PER DOCUMENT R747-5310-28-1/1. 2 L 7 4 4F A20WE 1996021600423 19960216 00423 NM 1996 2 16 UPS205427 1 19960212 A 3350 1000679 LIGHT BOEING 727 72725C 138400H NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 933UP 19857 MAINTENANCE REPORTED, FWD ENTRY EMERGENCY LIGHT INOP. REMOVED AND REPLACED FWD ENTRY LIGHT ASSY, CK NORMAL. 2 L 7 3 4F A3WE 1996021600424 19960216 00424 NM 1996 2 16 UPS205439 1 19960202 A 5320 SHEAR TIE BOEING 727 72725C 138400H NM BS 277 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED UPPER SHEAR TIE CRACKED AT BS 277, STR 16 RT, ACCESSING REQ. REPAIRED IAW 51 -40-02 FIG 1. 2 L 7 3 4F A3WE 1996021600425 19960216 00425 NM 1996 2 16 UPS205440 1 19960206 A 5220 HANDLE BOEING 727 72725C 138400H NM OVERWING EXIT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION OF RT AFT EXTERNAL HANDLE SEAL CASTING ON OVERWING EXIT. REMOVED A ND REPLACED CASTING IAW SRM 51-30-02, 51-10-05 AND 51-10-08. 2 L 7 3 4F A3WE 1996021600426 19960216 00426 NM 1996 2 16 UPS205441 1 19960203 A 5753 THRUST SHAFT BOEING 727 72725C 138400H NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON THE NR 7 FLAP CARRIAGE LOCATER ON THE THRUST SHAFT FWD OF THE TH RUST NUT. RECEIVED NEW FLAP CARRIAGE. 2 L 7 3 4F A3WE 1996021600427 19960216 00427 NM 1996 2 16 UPS205442 1 19960206 A 2780 BULLNOSE BOEING 727 72725C 138400H NM NR 3 LE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON THE L/W NR 3 K-FLAP BULLNOSE CENTER HINGE LOWER ATTACH POINT. R EPLACED NR 3 K-FLAP PER MM 27-81-00. 2 L 7 3 4F A3WE 1996021600428 19960216 00428 NM 1996 2 16 UPS205443 1 19960206 A 5751 HINGE BOEING 727 72725C 138400H NM RT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON THE RT WING O/B AILERON CENTER O/B HINGE AILERON SIDE. REPLACED PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996021600429 19960216 00429 NM 1996 2 16 UPS205444 1 19960206 A 5751 HINGE FITTING BOEING 727 72725C 138400H NM RT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON THE RT WING I/B AILERON HINGE FITTINGS O/B AND CENTER FITTINGS. REPLACED FITTINGS PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996021600430 19960216 00430 NM 1996 2 16 UPS205445 1 19960206 A 5752 HINGE FITTING BOEING 727 72725C 138400H NM AILERON TAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON THE LT I/B AILERON TAB HINGE FITTINGS, AILERON SIDE. REPLACED I AW 727 SRM 51-30-2. 2 L 7 3 4F A3WE 1996021600431 19960216 00431 NM 1996 2 16 UPS405429 1 19960201 A 5312 BLKHD WEB BOEING 747 747121 1384871 NM BS 145 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CRACK IN BULKHEAD WEB AT BSTA 2160 LBL 35. REPLACED WEB BETWEEN RBL 8 TO LBL 58, ALL TO SRM 51-40-02. 2 L 7 4 4F A20WE 1996021600432 19960216 00432 NM 1996 2 16 UPS405430 1 19960212 A 5320 SHEAR TIE BOEING 747 747121 1384871 NM BS 2060 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, 3 SHEAR TIES ARE CRACKED AT BS 2060 BETWEEN STR 48 TO 51 LBL. REPAIRED PER S RM 53-10-04 FIG 41. 2 L 7 4 4F A20WE 1996021600433 19960216 00433 NM 1996 2 16 UPS405431 1 19960212 A 5320 SHEAR TIE BOEING 747 747121 1384871 NM BS 2100 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, 3 SHEAR TIES CRACKED AT BS 2100 BETWEEN STR 4 TO 50 LBL. REPAIRED PER SRM 53 -10-04 FIG 41. 2 L 7 4 4F A20WE 1996021600434 19960216 00434 NM 1996 2 16 UPS405432 1 19960202 A 5320 BRACKET BOEING 747 747121 1384871 NM BS 1840 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CRACK IN INTERCOSTAL BRACKET UNDER FRAME UPPER CHORD AT BS 1840 LBL 5. REPLA CED BRACKET PER SRM 51-30-02. 2 L 7 4 4F A20WE 1996021600435 19960216 00435 NM 1996 2 16 UPS405433 1 19960201 A 5320 SHEAR TIE BOEING 747 747121 1384871 NM BS 1780 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CRACK ON SHEAR TIES AT BS 1780 BETWEEN S-50/49 LT AND BETWEEN S-43 RT AND DOO R SILL BEAM. REPAIRED IAW SRM 53-10-04 FIG 3. 2 L 7 4 4F A20WE 1996021600436 19960216 00436 NM 1996 2 16 UPS405434 1 19960201 A 5320 SHEAR TIE BOEING 747 747121 1384871 NM BS 1760 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CRACK ON SHEAR TIE AT BS 1760 BETWEEN S-51/50 LT. REPAIRED IAW SRM 53-10-04 FIG 3. 2 L 7 4 4F A20WE 1996021600437 19960216 00437 NM 1996 2 16 UPS405435 1 19960201 A 5312 BLKHD WEB BOEING 747 747121 1384871 NM BS 2160 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CRACK IN BULKHEAD WEB AT BS 2160 RBL 30. REPAIRED AS PER SRM 51-40-02. 2 L 7 4 4F A20WE 1996021600438 19960216 00438 NM 1996 2 16 UPS405436 1 19960206 A 5320 INTERCOSTAL BOEING 747 747121 1384871 NM BS 1900-1915 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CRACK IN INTERCOSTAL UNDER CARGO TRACK AT LBL 25 BETWEEN BS 1900/1915. STOP DRILLED IAW SRM 51-40-02. 2 L 7 4 4F A20WE 1996021600439 19960216 00439 NM 1996 2 16 UPS405437 1 19960212 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 2150-2170 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, FOUND IN BULK CARGO COMP AT BS 2156 STR 46 RBL CORROSION IN STRINGER. REPLAC ED STR BETWEEN BS 2150 AND 2170 IAW SRM 53-10-03 FIG 1 AND SRM 51-30-02. 2 L 7 4 4F A20WE 1996021600440 19960216 00440 NM 1996 2 16 UPS405438 1 19960201 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1740-1780 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, FOUND CRACK DUE TO CORROSION ON STR FLANGE AT BS 1757, S-43 RT. REPLACED STR FROM BS 1740 TO 1780 IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996021600442 19960216 00442 WP 1996 2 16 UPS805447 1 19960104 A 5330 SKIN DOUG DC8 DC871F 302199D WP FS 1060/1070 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, HEAVY CORROSION AT FUSELAGE EXTERNAL SKIN PANEL FS 1060 AND FS 1070 UNDER KEE L PLATE. REPAIRED SKIN PER UPS EO. 2 L 7 4 4F RT 4A25 1996021600443 19960216 00443 WP 1996 2 16 UPS805448 1 19960130 A 5320 GUSSET DOUG DC8 DC871F 302199D WP FS 156 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, MODERATE CORROSION AT GUSSET ANGLE RBL 35 UNDER COPILOT RUDDER PEDALS AND BUL KHEAD. REPLACED GUSSET PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996021600444 19960216 00444 WP 1996 2 16 UPS805449 1 19960130 A 5330 SKIN DOUG DC8 DC871F 302199D WP SLIDE DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, SKIN CRACKED ON A-X-SLIDE DOOR AT FASTENER ON AFT END OF RAMP. REPAIRED SKIN PER SRM 52-2-0. 2 L 7 4 4F RT 4A25 1996021600445 19960216 00445 WP 1996 2 16 UPS805450 1 19960127 A 5753 VANE DOUG DC8 DC871F 302199D WP NR 5 TE FLAP DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT WING O/B NR 5 FLAP VANE DEL ON UPPER SIDE. REPLACED VANE ASSY PER MM 27-5 1-14. 2 L 7 4 4F RT 4A25 1996021600446 19960216 00446 WP 1996 2 16 UPS805451 1 19960127 A 5753 VANE DOUG DC8 DC871F 302199D WP NR 1 TE FLAP DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT AND RT WING NR 1 FLAP VANES DELAMINATED ON BOTTOM SIDES. REPLACED VANES P ER MM 27-51-14. 2 L 7 4 4F RT 4A25 1996021600447 19960216 00447 WP 1996 2 16 UPS805452 1 19960127 A 5755 SKIN DOUG DC8 DC871F 302199D WP RT SPOILER DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 WHILE IN FOR C-CHECK MAINTENANCE REPORTED RT WING NR 2 SPOILER DELAMINATED ON BOTTOM SIDE. REPLACED SPOILER PER MM 27-6 1-00. 2 L 7 4 4F RT 4A25 1996021600448 19960216 00448 WP 1996 2 16 UPS805453 1 19960131 A 5720 TRAP FITTING DOUG DC8 DC871F 302199D WP LT/RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT AND RT TRAP FITTINGS CRACKED AT LOWER ENDS. REPLACED FITTINGS PER SRM 57- 2-7. 2 L 7 4 4F RT 4A25 1996021600449 19960216 00449 WP 1996 2 16 UPS805454 1 19960130 A 5320 SHEAR TIE DOUG DC8 DC871F 302199D WP FS 640 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, 1 INCH LONG CRACK ON LOWER SIDE OF SHEAR TIE FS 640 BETWEEN LONGERONS 26L TO 27L. REPLACED SHEAR TIE PER SRM 53-2-0 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996021600450 19960216 00450 WP 1996 2 16 UPS805455 1 19960130 A 5320 DOOR FRAME DOUG DC8 DC871F 302199D WP SLIDE DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, A-X-SLIDE FRAME CRACKED ON BOTTOM SIDE THROUGH LIGHTENING HOLE. REPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996021600451 19960216 00451 NM 1996 2 16 VSTA9602001 1 19960209 A 2731 6573799501 TRIM TAB BOEING 737 737247 138448D NM LT ELEVATOR LOOSE A VSTA K NONE D INFLIGHT SEPARATION NR NOT REPORTED 1 WP 07 303VA 20125 AIRCRAFT RETURNED TO DEPARTURE AIRPORT, DUE TO AIRFRAME VIBRATION. REPLACED LT ELEVATOR TRIM TAB. 2 L 7 2 4F A16WE 1996021600452 19960216 00452 EU 1996 2 16 HEEA966539 1 19960126 A 7712 305731365 INDICATOR SNIAS 350 AS350B2 8680813 EU ENG TORQUE DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 6097Z 2820 POINTER GOING ALL OVER WITH VOLTAGE ALSO MAKES CLICKING SOUND. POINTS AT FLOOR WHEN OFF. POINTER DOES NOT SPIN. READS NO TORQUE. 1 G 7 1 3U H9EU 1996021600453 19960216 00453 EU 1996 2 16 HEEA966542 1 19960126 A 6220 827S115X140X12FP SHAFT SEAL 105141081 BOLKMS 105 BO105S 5626006 EU M/R LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 4302G 1726 050065 S853 INBOARD AND OUTBOARD SEALS LEAKING, BEARINGS BREAKING DOWN, 3 EACH RETAINERS CORRODED, 8 EACH SECONDARY BUSHING SCARRED, 4 EACH PRIMARY BUSHING SCARRED AND CORRODED. SEE MMIR# 6543 FOR ADDITIONAL PART INFORMATION. 1 G 7 2 3U H3EU 1996021600454 19960216 00454 EU 1996 2 16 HEEA966543 1 19960126 A 6220 827N85X105X13FP7 SHAFT SEAL 105141081 BOLKMS 105 BO105S 5626006 EU M/R LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 4302G 1726 050065 S853 INBOARD AND OUTBOARD SEALS LEAKING, BEARINGS BREAKING DOWN, 3 EACH RETAINERS CORRODED, 8 EACH SECONDARY BUSHING SCARRED, 4 EACH PRIMARY BUSHING SCARRED AND CORRODED. SEE MMIR# 6542 FOR ADDITIONAL PART INFORMATION. 1 G 7 2 3U H3EU 1996021600455 19960216 00455 NE 1996 2 16 HEEA966544 1 19960129 A 2820 6531703006109 VALVE SKRSKY S76 S76A 8143006 NE FUEL SYS DEFECTIVE E HEEA K NONE J WARNING INDICATION NR NOT REPORTED 1 SW 03 4253S 760035 VALVE CAUSING LOW PRESSURE FUEL LIGHT TO COME ON. 1 G 7 2 3U H1NE 1996021600456 19960216 00456 EU 1996 2 16 HEEA966545 1 19960129 A 2435 150SG1064 ARMATURE AEROSP AS355 AS355F2 8680812 EU STARTER/GEN SHORTED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6040U 5474 INSTALLED ARMATURE IN STARTER GEN. WHEN PUT ON TEST, BRUSHES WERE ARCHING EXCESSIVELY. FOUND ARMATURE COMMENTATOR SHOR TED OUT. 1 G 7 2 3U H11EU 1996021600457 19960216 00457 1996 2 16 HEEA966546 4 19960129 A 2210 7000298901 COMPUTER BELL 412 412 1182202 SW AFCS DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893N 33010 WITH BOTH HELIPILOTS ENGAGED, IN A TURN A SLIGHT TAP IS FELT IN THE CYCLIC STICK. 1 G 7 2 4U H4SW 1996021600458 19960216 00458 EU 1996 2 16 HEEA966547 1 19960129 A 6240 2360016901 INDICATOR SNIAS 350 AS350B2 8680813 EU ROTOR NOISY E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 60951 2771 ROTOR INDICATOR BEARING NOISY. 1 G 7 1 3U H9EU 1996021600459 19960216 00459 1996 2 16 HEEA966548 4 19960129 A 3421 7660002113103 GYRO SKRSKY S76 S76A 8143006 NE COCKPIT VG DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1545X 760050 VERT GYRO KEEPS IN ROLL. 1 G 7 2 3U H1NE 1996021600460 19960216 00460 1996 2 16 HEEA966549 4 19960129 A 3421 7660002113103 GYRO SKRSKY S76 S76A 8143006 NE COCKPIT VG DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1545X 760050 VERT GYRO KEEPS IN ROLL. 1 G 7 2 3U H1NE 1996021600461 19960216 00461 EU 1996 2 16 HEEA966550 4 19960129 A 2562 DK100 DATA TAG BOLKMS 105 BO105S 5626006 EU LOCATOR BEACON TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7171A 5975 S838 BEACON DATA TAG TORN AND ILLEGIBLE. 1 G 7 2 3U H3EU 1996021600462 19960216 00462 EU 1996 2 16 HEEA966551 1 19960129 A 7930 6607190A PRESSURE SWITCH BOLKMS 105 BO105S 5626006 EU XMSN FAILED E HEEA K NONE N FALSE WARNING IN INSP/MAINT 1 SW 03 50293 160 S677 SWITCH CONTACTS WILL NOT OPEN OR CLOSE. T-OIL LIGHT ILLUMINATED IN FLIGHT. 1 G 7 2 3U H3EU 1996021600463 19960216 00463 SW 1996 2 16 HEEA966552 1 19960131 A 2422 ASH4501 INVERTER BELL 412 412 1182202 SW AC SYS INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2298Z 33077 INVERTER INOPERATIVE. TIME SINCE REPAIR 14:25. 1 G 7 2 4U H4SW 1996021600464 19960216 00464 1996 2 16 HEEA966553 4 19960131 A 2200 2593996333 TARSYN 333 BELL 412 412 1182202 SW AUTO FLT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2298Z 33077 ADI ROLLS VERTICAL "SPINNING". TIME SINCE REPAIR 590:35. 1 G 7 2 4U H4SW 1996021600465 19960216 00465 SW 1996 2 16 HEEA966554 1 19960131 A 6710 214001347005 ACTUATOR BELL 412 412 1182202 SW M/R DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 7128R 36007 ROTARY ACTUATOR DEFECTIVE. BINDING IN CONTROLS. TIME SINCE REPAIR 107:05. 1 G 7 2 4U H4SW 1996021600466 19960216 00466 SW 1996 2 16 HEEA966555 1 19960131 A 7923 209072433105 VALVE BELL 412 412 1182202 SW DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 22608 33075 VALVE FLUTTERING; CAUSES ENGINE ITT TO FLUCTUATE WITH HEATER TURNED OFF. 1 G 7 2 4U H4SW 1996021600467 19960216 00467 SW 1996 2 16 HEEA966556 1 19960131 A 2730 214001970107 ACTUATOR ASSY BELL 214 214ST 1182106 SW ELEV DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3897N 28106 #1 ELEVATOR GOES OFF LINE, WILL NOT COME BACK ON LINE. 2 G 7 2 4U H10SW 1996021600468 19960216 00468 SW 1996 2 16 HEEA966557 1 19960131 A 2510 412070843105 RESTRAIN SYS BELL 412 412 1182202 SW SHOULDER STRAP DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 SHOULDER STRAPS ABOVE ADJUSTMENT BUCKLE APPROX. 1 1/2 INCH DIFFERENCE. 1 G 7 2 4U H4SW 1996021600469 19960216 00469 SW 1996 2 16 HEEA966558 1 19960131 A 2435 36B510954G2 CLUTCH BELL 214 214ST 1182106 SW STARTER/GEN FAIL TEST E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 CLUTCH FAILS BREAK AWAY AND CLUTCH SLIPPAGE TORQUE TEST PER LELAND S/B 2CM272B1-80-08. CLUTCH SLIPPAGE IS AT 290 INCH POUNDS. 2 G 7 2 4U H10SW 1996021600470 19960216 00470 NE 1996 2 16 HEEA966559 1 19960131 A 3210 7625001000109 LANDING GEAR SKRSKY S76 S76A 8143006 NE SHRADER VALVE DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 792CH 14655 760193 TOP LOCK AND NUT SPINNING UNDER SHRADER VALVE. 1 G 7 2 3U H1NE 1996021600481 19960216 00481 SW 1996 2 16 HEEA966570 1 19960131 A 6330 206033554101 LINK ASSY BELL 206 206L3 1182108 SW XMSN MOUNT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8587X 51464 ELASTOMER BEARING DETERIORATED. 1 G 7 1 3U H2SW 1996021600482 19960216 00482 SW 1996 2 16 HEEA966571 1 19960131 A 6330 206033554101 LINK ASSY BELL 206 206L3 1182108 SW XMSN MOUNT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8587X 51464 ELASTOMER BEARING DETERIORATED. 1 G 7 1 3U H2SW 1996021600483 19960216 00483 SW 1996 2 16 HEEA966572 1 19960131 A 6330 206033554101 LINK ASSY BELL 206 206L3 1182108 SW XMSN MOUNT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8587X 51464 ELASTOMER BEARING DETERIORATED. 1 G 7 1 3U H2SW 1996021600484 19960216 00484 SW 1996 2 16 HEEA966573 1 19960131 A 7714 412075010109 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH STICKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7128R 36007 TACH DOES NOT READ RIGHT. ALL NEEDLES STICK EXCESSIVELY. TIME SINCE REPAIR 742:35. 1 G 7 2 4U H4SW 1996021600485 19960216 00485 SW 1996 2 16 HEEA966574 1 19960131 A 6720 206010793101 CONNECTING LINK BELL 206 206B 1181511 SW T/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3181J 3771 TAIL ROTOR P/C LINK IS CRACKED ON BOTH ENDS WHERE BEARINGS PRESSED INTO LINK. REPLACED P/C LINK WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 1996021600486 19960216 00486 EU 1996 2 16 HEEA966575 1 19960131 A 6410 355A12004008 BLADE SNIAS 350 AS350B2 8680813 EU T/R DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100U 345 2863 HIGH FREQUENCY VIBRATION. T/R BLADE DEFECTIVE 1 G 7 1 3U H9EU 1996021600487 19960216 00487 NE 1996 2 16 HEEA966576 2 19960131 A 7210 3024780 GEARBOX BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE COMBINING MAKING METAL E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893P 13346 33012 COMBINING GEARBOX MAKING METAL. 1 G 7 2 4U 4 U H4SW E22EA 1996021600488 19960216 00488 EU 1996 2 16 HEEA966577 1 19960131 A 6410 355A12004008 BLADE SNIAS 350 AS350B2 8680813 EU T/R ERODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 2732 2771 T/R BLADE IS ERODED. (EROSION AT BLADE TIPS) 1 G 7 1 3U H9EU 1996021600489 19960216 00489 EU 1996 2 16 HEEA966578 1 19960131 A 6730 SC50811 SERVO SNIAS 350 AS350B2 8680813 EU M/R LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 1313 2771 SERVO LEAKING. 1 G 7 1 3U H9EU 1996021600490 19960216 00490 1996 2 16 HEEA966579 4 19960131 A 2312 069102525 DISPLAY KX165 BOLKMS 105 BO105S 5626006 EU COCKPIT VHF FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 135AE S838 NO DISPLAY. FOUND BROKEN DISPLAY. REPLACED DISPLAY DS901. APPLIED DC4 COMPOUND. REPAIRED. 1 G 7 2 3U H3EU 1996021600491 19960216 00491 1996 2 16 HEEA966580 4 19960131 A 3452 066106200 TRANSCEIVER KT76 BELL 206 206L1 1182107 SW COCKPIT ATC DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2245Y 45751 UNIT NOT REPORTING ALTITUDE. VERIFIED UNIT TO HAVE VERY WEAK POWER OUT. TRIED ADJUSTING POWER TO SPECS. NO HELP. REPL ACED CAVITY OSCILLATOR V101. REPAIRED. ADJUSTED FREQUENCY. BENCH CHECK GOOD. 1 G 7 1 3U H2SW 1996021600492 19960216 00492 1996 2 16 HEEA966581 4 19960131 A 3452 066106200 TRANSCEIVER KT76 SNIAS 350 AS350B2 8680813 EU COCKPIT ATC DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 6097Z 2820 DOES NOT RESPOND. VERIFIED UNIT TO HAVE LOW POWER OUT AND INTERMITTENT RECEIVE. REPLACED CAVITY OSCILLATOR V101. REPAI RED LOW POWER. RESOLDERED GROUND CONNECTIONS ON PRE-SELECTOR. REPAIRED INTERMITTENT RECEIVE. ADJUSTED FREQUENCY AND P ULSE WIDTH. BENCH CHECKGOOD. 1 G 7 1 3U H9EU 1996021600493 19960216 00493 1996 2 16 HEEA966582 4 19960131 A 3452 066106200 TRANSCEIVER KT76 BELL 206 206L1 1182107 SW COCKPIT ATC INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2124Z 45646 INOPERATIVE. REPLACED WEAK V101 CAVITY OSCILLATOR AND WEAK V301 PHOTODETECTOR. ADJUSTED FREQUENCY. BENCH CHECK GOOD. 1 G 7 1 3U H2SW 1996021600494 19960216 00494 1996 2 16 HEEA966583 4 19960131 A 3454 071121627 CONTROL BELL 412 412 1182202 SW COCKPIT NAV INTERMITTENT E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2148K 36001 LED DISPLAY IS INTERMITTENT. REPLACED PHOTOCELL V101. REPAIRED. BENCH CHECK GOOD. 1 G 7 2 4U H4SW 1996021600495 19960216 00495 1996 2 16 HEEA966584 4 19960131 A 3454 071121627 CONTROL SWITCH BELL 214 214ST 1182106 SW COCKPIT NAV DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 8045T 28101 STANDBY SWITCH HAS NO SPRING TENSION. INSTALLED SWITCH S102. REPAIRED PROBLEM. ALSO INSTALLED HEADER P201. UNIT BENCH CHECK GOOD. 2 G 7 2 4U H10SW 1996021600496 19960216 00496 1996 2 16 HEEA966585 4 19960131 A 3444 066104800 ALTIMETER KRA405 BELL 214 214ST 1182106 SW COCKPIT RAD ALT READS LOW E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3897N 28106 RADAR ALTIMETER READS 500 FEET LOW AND VARIABLE. PERFORMED COMPLETE CALIBRATION AND ALIGNMENT. REPLACED RESISTORS R518, R519, R534 AND R260 TO INCORPORATE MOD 10. BENCH CHECK GOOD. 2 G 7 2 4U H10SW 1996021600497 19960216 00497 NE 1996 2 16 HEEA966586 1 19960131 A 6410 7610105101041 BLADE SKRSKY S76 S76A 8143006 NE T/R SPLIT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545X 6478 760050 PADDLE "A" SPLIT OPEN ON THE TRAILING EDGE AT THE ATTACHMENT AREA. 1 G 7 2 3U H1NE 1996021600499 19960216 00499 WP 1996 2 16 96ZZZM166 1 19960113 A 3230 RETRACT MECH DOUG DC9 DC932 3022066 WP LANDING GEAR LACK OF LUBE A VJ6A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 938VV 47442 FLT NR 559 - BNA-ATL - ON TAKEOFF THE LANDING GEAR WOULD NOT RETRACT. AIR RETURN TO BNA. LUBED RELEASES SWITCH AND CYC LED GEAR LEVER WITH PINS INSTALLED. NO DEFECTS NOTED, AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F A6WE 1996021600500 19960216 00500 WP 1996 2 16 96ZZZM167 1 19960113 A 7930 4201091A PRESS SWITCH DOUG DC9 DC932 3022066 WP NR 2 ENGINE STUCK A VJ6A A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 11 930VV 47723 ON FLT NR 530 - ATL- AIR RETURN, NR 2 ENGINE OIL FILTER CLOG LIGHT CAME ON IN FLIGHT. REPLACED NR 2 ENGINE OIL FILTER. INSPECTED FILTER FOR METAL AND OTHER DEBRIS, NO DEFECTS NOTED, FOUND DIFFERENTIAL PRESSURE SWITCH STUCK CLOSED. REMOVE D AND REPLACED SWITCH, RAN NR 2 ENGINE. OPS CHECK NORMAL, LEAK CHECK OK. (M) 2 L 7 2 4F A6WE 1996021600501 19960216 00501 WP 1996 2 16 96ZZZM168 1 19960113 A 2150 DUCT DOUG DC9 DC932 3022066 WP LT PACK LOOSE A VJ6A A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 11 936VV 47397 ON FLT NR 283 - IAD-FLL - AT FL 350 PRESSURIZATION FAILED. CABIN CLIMBED TO 11,000 FEET. THE CREW COULD NOT CONTROL MA NUALLY. CREW PERFORMED EMERGENCY DESCENT AS PER VJ EMERGENCY PROCEDURES. MANUAL PRESSURE REGAINED AT 12,000 FEET. FLI GHT DIVERTED TO ATL FOR MAINTENANCE. UPON INSPECTION OF TAIL COMPARTMENT MX FOUND LEFT PACK DUCT BLOWN OFF THE WATER SE PARATOR. RESECURED DUCT AND TIGHTENED CLAMPS. RAN LEFT PACK. NO LEAKS NOTED. SYSTEM CHECKS GOOD PER MM 21-30. (M) 2 L 7 2 4F A6WE 1996021600506 19960216 00506 EU 1996 2 16 96ZZZM173 1 19960103 A 3411 PITOT TUBE BAG JETSTM JETSTM3101 1500215 EU LEFT ICED UP A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 07 853JS 730 FLT NR 4111 - ON TAKEOFF ROLL, CAPTAIN NOTICED HIS AIRSPEED INDICATOR WAS READING LOW. CREW ABORTED TAKEOFF, AND RETURN ED TO THE GATE. PIT MX ACTIVATED PITOT HEAT TO REMOVE ICE ACCUMULATION IN THE PITOT HEAD. AIRCRAFT RETURNED TO SERVICE . (M) 2 L 7 2 4T RT A21EU 1996021600507 19960216 00507 NE 1996 2 16 96ZZZM174 2 19960109 A 7320 7863916 HYDRO MECH UNIT HAMSTD DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 ENG MALFUNCTIONED A HNAA A UNSCHED LANDING J R WARNING INDICATION PARTIAL RPM/PWR LOSS CL CLIMB 1 EA 07 934HA 1119 F3784 139 FLT 7106 - PHF-ROA - AFTER TAKEOFF, THE NR 2 ENGINE HAD A SEVERE REDUCTION IN POWER. THE PILOT FEATHERED THE ENGINE. T HE AIRCRAFT RETURNED TO PHF AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND MOISTURE IN THE ELECTRICAL CON TROL UNIT CONNECTORS. REMOVED AND REPLACED THE NR 2 ELECTRICAL CONTROL UNIT. ALSO, REMOVED AND REPLACED THE NR 2 HYDRO MECHANICAL UNIT AS A PRECAUTION. (M) 2 H 7 2 4T 4 T RT A13NM E20NE 1996021600513 19960216 00513 NM 1996 2 16 ASAA9610002 1 19960107 A 3230 65446916 MODULE BOEING 737 737290C 138448V NM NLG FAILED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 12738 23136 ANC - FLT NR 65 - DURING APPROACH CREW REPORTED, THE NOSE LANDING GEAR FAILED TO EXTEND ON FIRST ATTEMPT. RECYCLED AND GEAR EXTENDED NORMALLY. LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR MODULE, PERFORMED GEAR RETRACTION AND OPER ATED NORMALLY. (M) 2 L 7 2 4F A16WE 1996021600514 19960216 00514 NM 1996 2 16 ASAA9610003 1 19960108 A 3350 86210151 BATTERY BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS ON SEVERAL PALLETS WERE FOUND INOPERATIVE. REPLAC ED BATTERIES AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1996021600515 19960216 00515 NM 1996 2 16 ASAA9610004 1 19960109 A 3350 BR9279106 EXIT IDENTIFIER BOEING 737 737298C 1384490 NM CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING MAINTENANCE CHECK, THE RIGHT OVERWING EMERGENCY EXIT IDENTIFIER WAS FOUND BROKEN. REPLACED EXIT IDENTIFIER . REPLACED EXIT IDENTIFIER LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996021600516 19960216 00516 NM 1996 2 16 ASAA9610005 1 19960111 A 5521 65C1611915 SPAR BOEING 737 7372Q8C 138448S NM LT ELEV CRACKED A ASAA O OTHER O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 SEA - DURING C-CHECK, THE REAR SPAR AT THE INBOARD HINGE FITTING FOR THE LEFT ELEVATOR TAB WAS FOUND CRACKED. REPAIRED PER EA 5520-01031. (M) 2 L 7 2 4F A16WE 1996021600517 19960216 00517 NM 1996 2 16 ASAA9610006 1 19960111 A 5320 65C3372211 ANGLE BOEING 737 7372Q8C 138448S NM BS 727 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 SEA - DURING C-CHECK, A 1 INCH CRACK WAS FOUND ON THE BS 727 FORMED ANGLE COMPRESSION CHORD AT RBL 25. REPAIRED PER EA 5310-01390. (M) 2 L 7 2 4F A16WE 1996021600518 19960216 00518 NM 1996 2 16 ASAA9610008 1 19960112 A 5753 6571909114 MIDFLAP BOEING 737 7372Q8C 138448S NM WS 254 WORN SKIN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 SEA - DURING C-CHECK, A WEAR MARK WAS FOUND ON THE RIGHT MIDFLAP LOWER WING SKIN AS A RESULT OF RUBBING ON THE NR 7 FLAP TRACK FAIRING WHEN THE FLAPS ARE RETRACTED. REPAIRED PER EA 5750-01195 AND BOEING TELEX ASA-SEA-96-0008RR DATED 1/8/96 . (M) 2 L 7 2 4F A16WE 1996021600519 19960216 00519 NM 1996 2 16 ASAA9610009 1 19960115 A 2530 80674040 COFFEE MAKER BOEING 737 737290C 138448V NM AFT GALLEY SMOKING A ASAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 01 730AS 37474 22577 ANC - FLT NR 23 - CREW REPORTED, AFT GALLEY COFFEE MAKER STARTED SMOKING. TURNED OFF GALLEY POWER AND SMOKE SUBSIDED. R EPLACED AFT GALLEY COFFEE MAKER AND OPERATED NORMALLY, NO ODORS DETECTED. (M) 2 L 7 2 4F A16WE 1996021600520 19960216 00520 NM 1996 2 16 ASAA9610010 1 19960116 A 3260 65653527 UPLOCK SENSOR BOEING 737 7372Q8C 138448S NM NLG OUT OF ADJUST A ASAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 01 741AS 21959 SEA - AIR TURN BACK OF FLT 65 - CREW REPORTED, THE NOSE LANDING GEAR UNSAFE LIGHT ON WITH GEAR HANDLE IN OFF POSITION, E XTINGUISHES WITH GEAR HANDLE IN UP POSITION. CYCLED GEAR AND GOT SAME RESULTS. FOUND NOSE LANDING GEAR UPLOCK SENSOR A DJUSTED TO MAXIMUM LIMIT. ADJUSTED SENSOR TO MINIMUM LIMIT AND ACCOMPLISHED GEAR SWING, OPERATION AND INDICATION NORMAL . (M) 2 L 7 2 4F A16WE 1996021600521 19960216 00521 NM 1996 2 16 ASAA9640001 1 19960102 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 782AS 25113 SEA - DURING MAINTENANCE CHECK, THE AFT FIVE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED TRAC K WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996021600522 19960216 00522 NM 1996 2 16 ASAA9640002 1 19960110 A 2530 8609020000 OVEN BOEING 737 7374Q8 NM RT GALLEY DEFECTIVE A ASAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 01 783AS 10842 25114 ANC - FLT 197 - CREW REPORTED, AN ELECTRICAL SMELLING SMOKE WAS EMITTING FROM GRILL LABLELED 'CIRCUIT BREAKER BEHIND' ON AFT NR 2 RIGHT GALLEY OVEN. PULLED CIRCUIT BREAKER AND SMOKE SUBSIDED. RELEASED PER MEL 25-10 AND SUBSEQUENTLY REPLAC ED OVEN, OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996021600523 19960216 00523 1996 2 16 ASAA9640003 4 19960112 A 2565 61621469 SLIDE BOEING 737 7374Q8 NM L-2 DOOR FAILED TO DEPLOY A ASAA O OTHER O OTHER IN INSP/MAINT 1 NM 01 773AS 8134 25106 SEA - THE L-2 EMERGENCY EVACUATION ESCAPE SLIDE FAILED TO DEPLOY FULLY DURING TESTING. REPLACED SLIDE ASSEMBLY. THOROU GH INVESTIGATION AND FUNCTIONAL EVALUATION BY AIRCRUISERS COMPANY SHOWED NO ABNORMALITIES IN THE HARDWARE OR FUNCTIONING OF THE SLIDE. NO REASON FOR THE DEPLOYMENT PROBLEM COULD BE FOUND. (M) 2 L 7 2 4F RT A16WE 1996021600524 19960216 00524 NM 1996 2 16 ASAA9640004 1 19960112 A 3397 WIRE BOEING 737 7374Q8 NM CABIN DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 773AS 25106 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 15-17 WERE FOUND INOPERATIVE. REPLACED DA MAGED WIRE HARNESS AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996021600525 19960216 00525 NM 1996 2 16 ASAA9640005 1 19960112 A 3397 WIRE BOEING 737 7374Q8 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 782AS 25113 LAX - FLT NR 157 - CREW REPORTED, THE AFT 5 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE INOPERATIVE. RESECURED LOOSE WIRING AT ROW 25 AND THE LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996021600526 19960216 00526 WP 1996 2 16 ASAA9680009 1 19960104 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 935AS 49236 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 13 TO 18 WERE FOUND INOPERATIVE. REPLACED THE B ATTERY PACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996021600527 19960216 00527 WP 1996 2 16 ASAA9680010 1 19960106 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 967AS 49103 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN FORWARD CABIN WERE FOUND INOPERATIVE. REPLACED THE BAT TERIES AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996021600528 19960216 00528 WP 1996 2 16 ASAA9680011 1 19960107 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 943AS 53018 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 9 TO 11 WERE FOUND INOPERATIVE. REPLACED THE BA TTERIES AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996021600529 19960216 00529 1996 2 16 ASAA9680012 4 19960107 A 2565 D29982121 SLIDE DOUG DC9 DC982 3022082 WP R1 DOOR FAILED TEST A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 954AS 49387 OAK - DURING C-CHECK, THE R1 DOOR EMERGENCY EVACUATION SLIDE EMERGENCY LIGHTS FAILED TEST. REPLACED THE R1 DOOR EMERGEN CY EVACUATION SLIDE. (M) 2 L 7 2 4F A6WE 1996021600530 19960216 00530 WP 1996 2 16 ASAA9680013 1 19960113 A 2560 D37013109 BOTTLE DOUG DC9 DC983 3022083 WP L1 DOOR LOW PRESS A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 PDX - DURING MAINTENANCE CHECK, THE L1 DOOR EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. REPLACE D THE L1 DOOR EMERGENCY EVACUATION SLIDE. (M) 2 L 7 2 4F RT A6WE 1996021600531 19960216 00531 WP 1996 2 16 ASAA9680014 1 19960115 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 935AS 49236 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 29 TO 31 WERE FOUND INOPERATIVE. REPLACED THE B ATTERIES AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996021600532 19960216 00532 WP 1996 2 16 ASAA9680015 1 19960115 A 5313 2777922425000 LONGERON DOUG DC9 DC982 3022082 WP BS 210-236 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 936AS 28441 49363 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON LONGERON 29L AT Y210 TO Y236. REMOVED DAMAGED AREA AND INSTALLED NEW PIE CES IAW DC9-SRM 51-10-03, 51-30-02 AND 53-14-01. (M) 2 L 7 2 4F A6WE 1996021600533 19960216 00533 WP 1996 2 16 ASAA9680016 1 19960115 A 5313 59365631 LONGERON DOUG DC9 DC982 3022082 WP BS 769-788 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 936AS 28441 49363 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON LONGERON 30L AT Y769 TO Y788. REMOVED DAMAGED AREA AND INSTALLED NEW PIE CES IAW DC-9 SRM 51-30-05. (M) 2 L 7 2 4F A6WE 1996021600534 19960216 00534 WP 1996 2 16 ASAA9680017 1 19960115 A 5320 5932731501 SPLICE DOUG DC9 DC982 3022082 WP BS 598 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 936AS 28441 49363 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON LONGERON 28L SPLICE AT Y598. REMOVED DAMAGED AREA AND INSTALLED NEW PIEC ES IAW DC-9 SRM 51-30-05 AND 53-01. (M) 2 L 7 2 4F A6WE 1996021600535 19960216 00535 WP 1996 2 16 ASAA9680018 1 19960115 A 5347 TMS6022044 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1174 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 936AS 28441 49363 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON SEAT TRACK AT Y1174, X PLUS 22, Z0. REMOVED DAMAGED AREA AND INSTALLED N EW PIECES IAW DC-9 SRM 51-30-01 AND 53-05. (M) 2 L 7 2 4F A6WE 1996021600536 19960216 00536 WP 1996 2 16 ASAA9680019 1 19960115 A 5347 TMS6019943 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 232-239 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 936AS 28441 49363 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON SEAT TRACK AT Y232 TO Y239, X MINUS 44, Z0. REMOVED DAMAGED AREA AND INS TALLED NEW PIECES IAW DC-9 SRM 53-05. (M) 2 L 7 2 4F A6WE 1996021600537 19960216 00537 WP 1996 2 16 ASAA9680020 1 19960115 A 5320 TMS6015609 SUPPORT DOUG DC9 DC982 3022082 WP BS 169-174 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 936AS 28441 49363 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FLOOR SUPPORT AT Y169 TO Y174, X MINUS 52, Z PLUS 1. REMOVED DAMAGED ARE A AND INSTALLED NEW PIECES IAW DC-9 SRM 51-30-02, 53-10-01 AND 53-01. (M) 2 L 7 2 4F A6WE 1996021600538 19960216 00538 WP 1996 2 16 ASAA9680021 1 19960115 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 1287-1307 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 936AS 28441 49363 PAE - DURING 30K CHECK, CRACK WAS FOUND ON FLOOR SUPPORT AT Y1287 TO Y1307, X0, Z0. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-10-03, 51-30-02 AND 53-14-03. (M) 2 L 7 2 4F A6WE 1996021600539 19960216 00539 WP 1996 2 16 ASAA9680022 1 19960116 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 958AS 8308 53024 SEAT - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBL Y AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996021600540 19960216 00540 WP 1996 2 16 ASAA9680023 1 19960110 A 4920 38420723 TURBINE WHEEL DOUG DC9 DC983 3022083 WP AUX POWER UNIT FAILED A A ASAA O OTHER T ENGINE CASE PENETRATION TX TAXI/GRND HDL 1 NM 01 949AS 53022 SEA - DURING TAXI TO GATE AFTER LANDING OF FLT 85 - CREW REPORTED THE AIRBORNE AUXILIARY POWER UNIT SHUTDOWN. THE AIRBO RNE AUXILIARY POWER UNIT HAD TURBINE WHEEL MATERIAL FAILURE WHICH RESULTED IN PIECES PENETRATING THE PLENUM. THERE WAS NO DAMAGE TO THE ENCLOSURE OR TO THE AIRCRAFT STRUCTURE. REPLACED THE AIRBORNE AUXILIARY POWER UNIT AND OPERATED NORMAL LY. (M) 2 L 7 2 4F RT A6WE 1996021600541 19960216 00541 1996 2 16 ASAA9680025 4 19960120 A 2565 D37013109 SLIDE BOTTLE DOUG DC9 DC982 3022082 WP R1 DOOR LOW PRESSURE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 930AS 49231 SEA - DURING MAINTENANCE CHECK, THE R1 DOOR EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. REPLACE D THE R1 DOOR EMERGENCY EVACUATION SLIDE. (M) 2 L 7 2 4F A6WE 1996021600542 19960216 00542 WP 1996 2 16 ASAA9680026 1 19960120 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1271 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 936AS 28441 49363 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FRAME AT Y1271, Z-50, LONGERON 26L TO 27R. REMOVED DAMAGED AREA AND INST ALLED NEW PIECES IAW DC-9 SRM 51-10-03, 51-30-02 AND 53-03. (M) 2 L 7 2 4F A6WE 1996021600543 19960216 00543 WP 1996 2 16 ASAA9680027 1 19960120 A 5313 5936667 LONGERON DOUG DC9 DC982 3022082 WP BS 1245-1271 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 936AS 49363 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON LONGERON 30 FROM Y1245 TO Y1271, X-0, Z-50. REMOVED DAMAGED AREA AND INS TALLED NEW PIECES IAW DC-9 SRM 51-10-03, 51-30-02, 53-14-03 AND 53-02. (M) 2 L 7 2 4F A6WE 1996021600544 19960216 00544 WP 1996 2 16 ASAA9680028 1 19960120 A 5313 5936027501 LONGERON DOUG DC9 DC982 3022082 WP BS 1117-1136 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 936AS 28441 49363 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON LONGERON 29R FROM Y1117 TO Y1136. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW ASA EA 5310-01396. (M) 2 L 7 2 4F A6WE 1996021600545 19960216 00545 WP 1996 2 16 ASAA9680029 1 19960120 A 5320 99367184 INTERCOSTAL DOUG DC9 DC982 3022082 WP BS 1307-1322 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 936AS 28441 49363 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON INTERCOSTAL FROM Y1307 TO Y1322. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-30-02 AND 51-30-05. (M) 2 L 7 2 4F A6WE 1996021600546 19960216 00546 WP 1996 2 16 ASAA9680030 1 19960120 A 5320 CUSP DOUG DC9 DC982 3022082 WP BS 200 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 936AS 28441 49363 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON CUSP AT Y200, X-56, Z-0. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES I AW DC-9 SRM 51-10-03, 51-30-03, 51-30-05 AND 53-05. (M) 2 L 7 2 4F A6WE 1996021600547 19960216 00547 NM 1996 2 16 AWXA960020 1 19960120 A 5330 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 304AW 24011 PHX - FLT NR 842 - DURING ROUTINE MAINTENANCE CHECK, FOUND FUSELAGE SKIN DENTED ACROSS STRINGER 25R, 4 FEET FORWARD OF A FT CARGO DOOR CUTOUT. OPENED UP INTERIOR FOR INSPECTION AND NO DAMAGE NOTED. FUSELAGE SKIN WITHIN LIMITS PER SRM 53-00 -01, FIGURE 101. NDT INSPECTION COMPLIED WITH ON W/O NR 7516-01-A336. (M) 2 L 7 2 4F RT A16WE 1996021600548 19960216 00548 WP 1996 2 16 CAL960009 1 19960109 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG REQ'D SERVICE A CALA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SW 09 93875 49125 FLT NR 1862 - DEN - THE NOSE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION AND WAS ACCOMPANIED BY NOS E GEAR VIBRATION. THE GEAR WAS EXTENDED FOR RETURN TO DEN AND THERE WAS A LOUD THUMP WHEN NOSE GEAR LOCKED DOWN. A TOW ER FLY-BY WAS CONDUCTED AND THE GEAR WAS CONFIRMED DOWN AND LOCKED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPACKED AND SERVICED THE NLG IAW MM 32-21-02. THE UPPER AND LOWER BEARINGS AND INNER AND OUTER CYLINDERS WERE INSPECTE D WITH NO ABNORMALITIES FOUND. A GEAR SWING WAS PERFORMED AND OPERATION AND INDICATIONS WERE GOOD. (M) 2 L 7 2 4F A6WE 1996021600549 19960216 00549 WP 1996 2 16 CAL960042 1 19960114 A 2780 5920257515 DRIVE MECHANISM DOUG DC9 DC932 3022066 WP LT LE SLAT BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15525 10275 47531 FLT NR 1787 - IAH - LEFT LEADING EDGE SLAT WOULD NOT RETRACT AFTER LANDING AT IAH. NO IN FLIGHT ABNORMALITIES WERE OBSE RVED. MAINTENANCE FOUND THE LEFT OUTBOARD SLAT DRIVE MECHANISM BROKEN. THE SLAT DRIVE MECHANISM WAS REMOVED AND REPLAC ED IAW MM 27-80-4. THE LEFT SLAT CABLES WERE RIGGED IAW MM 27-80-2 AND OPERATION CHECKED GOOD. IN ADDITION, BOTH THE U PPER AND LOWER LEFT SLAT DRIVE ACTUATORS WERE REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. (M) 2 L 7 2 4F A6WE 1996021600552 19960216 00552 WP 1996 2 16 CKSA96001 1 19960107 A 2612 FIRE WARNING DOUG DC8 DC8F55 3021928 WP NR 2 ENGINE MALFUNCTIONED A CKSA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 6161M 71304 45762 MSLP - FIRE INDICATION ON NR 2 ENGINE, AIR ABORT RETURNED TO MSLP. FIRE WARNING CEASED ONCE FIRE HANDLE WAS PULLED. OP ENED COWLING AND INSPECTED ENGINE, NO FIRE INDICATION NOTED. RAN ENGINE AT IDLE, NO AIR LEAKS NOTED. CLOSED COWLING, R AN ENGINE AT TAKEOFF POWER, NO FIRE INDICATION NOTED. COULD NOT DUPLICATE PROBLEM. (M) 2 L 7 4 4F 4A25 1996021600554 19960216 00554 WP 1996 2 16 GRAA9601 1 19960116 A 3350 6011775 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A GRAA K NONE L NO TEST IN INSP/MAINT 1 WP 11 500TR 49144 LINE MAINTENANCE AT MYRTLE BEACH, SC, DISCOVERED THAT THE OVERWING EMERGENCY LIGHT HAD FAILED. MAINTENANCE REMOVED AND REPLACED THE OVERWING EMERGENCY LIGHT SYSTEM. OPERATIONALLY CEHCKED NORMAL. (M) 2 L 7 2 4F A6WE 1996021600555 19960216 00555 WP 1996 2 16 HALA9604 1 19960111 A 3397 WIRE DOUG DC9 DC951 3022051 WP CABIN LOOSE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 679HA 47662 HNL - FLT 112 - EMERGENCY FLOOR LIGHTS IN FRONT OF CABIN DO NOT ILLUMINATED. CHECKED AND FOUND LOOSE WIRE, RESECURED. ( M) 2 L 7 2 4F RT A6WE 1996021600558 19960216 00558 NE 1996 2 16 HNAA9693401 2 19960109 A 7321 7898426009 ELEC CONTROL UNI HAMSTD DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 ENG FAILED A HNAA A UNSCHED LANDING J R WARNING INDICATION PARTIAL RPM/PWR LOSS CL CLIMB 1 EA 07 934HA 11702 89104169 139 FLT 7106 - PHF-ROA - AFTER TAKEOFF, THE NR 2 ENGINE HAD A SEVERE REDUCTION IN POWER. THE PILOT FEATHERED THE ENGINE. T HE AIRCRAFT RETURNED TO PHF AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND MOISTURE IN THE ELECTRICAL CON TROL UNIT CONNECTORS. REMOVED AND REPLACED THE NR 2 ELECTRICAL CONTROL UNIT. ALSO, REMOVED AND REPLACED THE NR 2 HYDRO MECHANICAL UNIT AS A PRECAUTION. (M) 2 H 7 2 4T 4 T RT A13NM E20NE 1996021600563 19960216 00563 NM 1996 2 16 MZZA96002 1 19960116 A 2121 5007024620 FAN BOEING 727 727227 1384078 NM LT PACK FAILED A MZZA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 13 86426 AA31148 21364 FLT NR 926 - SPN - ON DESCENT, SMOKE AND ELECTRICAL SMELL COMING FROM GASPER SYSTEM. STRONGEST AROUND MID CABIN. TURNE D OFF RIGHT PACK AND GASPER FAN. PULLED CIRCUIT BREAKER FOR GASPER FAN. MAINTENANCE FOUND GASPER FAN FROZEN. ALSO, CH ECKED WIRING AND FOUND ALL GOOD. DUE GASPER FAN NON STOCK ITEM IN SAIPAN, SYSTEM DEACTIVATED AND PLACARDED INOPERATIVE PER MRL 21-24. (M) 2 L 7 3 4F A3WE 1996021600564 19960216 00564 EA 1996 2 16 NNAA9690103 1 19960112 A 3260 805310 PROXIMITY ELDEC DHAV DHC7 DHC7102 2802708 EA NR 3 MLG WW FAILED A HNAA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 EA 07 901HA 27208 180 042 FLT EN29 - ORF-DCA - AFTER TAKEOFF, GOT RIGHT MAIN GEAR INDICATION 'RED UNSAFE LIGHT', AND THE GEAR HANDLE LIGHT STAYED ON AFTER THE GEAR WAS SELECTED UP. THE AIRCRAFT RETURNED TO ORF AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE RIGHT HAND PROXIMITY BOX. (M) 2 H 7 4 4T A20EA 1996021600568 19960216 00568 EU 1996 2 16 SIMA960121 1 19960112 A 3350 3012001 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 414WF 599 414 DFW - FLT NR 3350 - EMERGENCY LIGHTS STILL ILLUMINATED WITH SWITCH OFF. RAI'D BATTERY PACK IN POWER SUPPLY 61WL. (M) 2 H 7 2 4T RT A53EU 1996021600569 19960216 00569 EU 1996 2 16 SIMA960151 1 19960115 A 3350 3012001 BATTERY PACK 629 AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 407AT 407 DFW - FLT NR 3749 - EMERGENCY LIGHTS ON AIRSTAIRS WON'T SHUT OFF AFTER BEING TESTED. RAI'D EMERGENCY BATTERY PACK, OPS CHECKED GOOD, RETURNED AIRCRAFT TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996021600570 19960216 00570 NM 1996 2 16 USAA960043 1 19960105 A 5311 INNER CHORD BOEING 737 7372B7 1384560 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 34396 22888 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK STATION 616 LEFT FRAME INBOARD INNER CHORD ANGLE FIRST FA STENER ABOVE CENTER WING. INSTALLED FILLER AND ANGLE. REPAIRED PER EA 40570. (M) 2 L 7 2 4F A16WE 1996021600571 19960216 00571 NM 1996 2 16 USAA960044 1 19960105 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 707 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 34396 22888 INT -DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK BL 0 LONGITUDINAL FLOOR BEAM LOWER WEB STATION 707 WL 203 AT FASTENER HOLE. INSTALLED DOUBLER, REPAIRED PER BOEING REF DRAWING 65C34537. (M) 2 L 7 2 4F A16WE 1996021600572 19960216 00572 NM 1996 2 16 USAA960045 1 19960105 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 707-708 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 34396 22888 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND TWO .25 INCH CRACKS RBL 25 LONGITUDINAL FLOOR BEAM LOWER WEB STATION 707 -708, WL 203 AT FASTENER HOLES. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2. (M) 2 L 7 2 4F A16WE 1996021600573 19960216 00573 NM 1996 2 16 USAA960046 1 19960105 A 5311 FRAME BOEING 737 7372B7 1384560 NM STA 616R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 34396 22888 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK STATION 616 RIGHT FRAME INBOARD INNER CHORD ANGLE FIRST F ASTENER ABOVE CENTER WING. INSTALLED FILLER AND REPAIR ANGLE. REPAIRED PER EA 40570. (M) 2 L 7 2 4F A16WE 1996021600574 19960216 00574 NM 1996 2 16 USAA960055 1 19960117 A 5320 WEB BOEING 737 7373B7 1384580 NM BS 1016 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 23314 22950 CLT - INSPECTION VISUALLY FOUND LEVEL 2 CORROSION, 3 INCHES BY 3 INCHES ON WEB, LOCATED AT BS 1016 THROUGH BL0. INSTALL ED DOUBLERS, FILLERS AND STIFFENERS AS PER USAIR SRM 53-80-08, 51-70-11 AND 53-80-01. (M) 2 L 7 2 4F RT A16WE 1996021600575 19960216 00575 NM 1996 2 16 USAA960059 1 19960117 A 5320 INTERCOSTAL BOEING 737 7373B7 1384580 NM BS 986.5-1006 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 32314 22950 CLT - INSPECTION VISUALLY FOUND A LEVEL 2 CORROSION, 3 INCHES BY 6 INCHES, LOCATED ON INTERCOSTAL AT S21L, BS 986.5 THRO UGH BS 1006. FABRICATED AND INSTALLED NEW PARTS AS PER USAIR SRM 53-60-15, FIG 1 SHEET 4 DETAIL II-A. (M) 2 L 7 2 4F RT A16WE 1996021600576 19960216 00576 NM 1996 2 16 USAA960060 1 19960117 A 5311 FRAME BOEING 737 7373B7 1384580 NM FS 967 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 32414 22950 CLT - INSPECTION VISUALLY FOUND AN LEVEL 2 CORRODED AREA 3 INCHES ON FRAME, LOCATED FS 967 AT S-27L. FABRICATED NEW PAR TS AND INSTALLED FAIL/SAFE CHORD AS PER BOEING 51-70-11, 51-30-01 FIG 2, PG 14 AND BOEING DRAWING 65-46563-7. (M) 2 L 7 2 4F RT A16WE 1996021600577 19960216 00577 NM 1996 2 16 USAA960061 1 19960117 A 5320 DOUBLER BOEING 737 7373B7 1384580 NM BS 986.5 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 32314 22950 CLT - INSPECTION VISUALLY FOUND LEVEL 2 CORRODED AREA, 6 INCHES BY 6 INCHES, ON DOUBLER LOCATED AT BS 986.5 THROUGH 527L , 527R. (M) 2 L 7 2 4F RT A16WE 1996021600578 19960216 00578 NM 1996 2 16 USAA960062 1 19960117 A 5313 STRINGER BOEING 737 7373B7 1384580 NM FS 967 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 32314 22950 CLT - INSPECTION VISUALLY FOUND LEVEL 2 CORROSION, 6 INCHES LOCATED ON STRINGER 27L AT FS 967. INSTALLED REPAIR CHANNEL AND ANGLES AS PER BOEING SRM 53-00-03 FIGURE 201, DETAIL VII. (M) 2 L 7 2 4F RT A16WE 1996021600579 19960216 00579 NM 1996 2 16 USAA960064 1 19960117 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 967-987 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 371US 32314 22950 CLT - INSPECTION VISUALLY FOUND A LEVEL 2 CORRODED AREA, 10 INCHES BY 6 INCHES, LOCATED ON SKIN AT BS 967 THROUGH BS 987 , BL 0. CUT OUT CORRODED SKIN AND INSTALLED DOUBLER AS PER BOEING SRM 53-00-01 AND USAIR EO 40687. (M) 2 L 7 2 4F RT A16WE 1996021600580 19960216 00580 NM 1996 2 16 USAA960097 1 19960117 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 927-967 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 35889 22756 INT - DURING CX-6 CHECK VISUAL INSPECTION, FOUND TWO LOCATIONS 2 INCHES BY 4 INCHES CORRODED AND 2 INCHES BY 8 INCHES CO RRODED AT STRINGER 27L, BS 927 TO 967. INSTALLED STRINGER AND DOUBLERS. REPAIRED PER SRM 53-10-3, FIG 1. (M) 2 L 7 2 4F A16WE 1996021600581 19960216 00581 NM 1996 2 16 USAA960098 1 19960123 A 5522 SKIN BOEING 737 737301 1384611 NM RT ELEVATOR DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 346US 25889 23515 CLT - INSPECTION VISUALLY FOUND A .25 INCH IMPACT DAMAGE TO COMPOSITE SKIN THROUGH COMPOSITE LAYERS LOCATED RIGHT ELEVAT OR SKIN 15 INCHES OUTBOARD FROM INBOARD END, MIDDLE OF ELEVATOR. ACCOMPLISHED WET LAYUP COMPOSITE REPAIR AS PER BOEING SRM 51-70-17 AND USAIR EA NR 40618. (M) 2 L 7 2 4F RT A16WE 1996021600582 19960216 00582 NM 1996 2 16 USAA960099 1 19960123 A 5320 DOUBLER BOEING 737 737301 1384611 NM FS 1006-1016 MISINSTALLED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 346US 25889 23515 CLT - INSPECTION VISUALLY FOUND AN 8 INCH BY 8 INCH EXTERNAL DOUBLER WITH BLIND FASTENERS, LOCATED AT FS 1006 TO 1016 BE TWEEN STRINGER 23R THROUGH STRINGER 25R. REINSTALLED WITH SOLID RIVETS AS USAIR EA NR 40533. (M) 2 L 7 2 4F RT A16WE 1996021600583 19960216 00583 NM 1996 2 16 USAA960100 1 19960123 A 5315 FLOOR BEAM BOEING 737 737301 1384611 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 346US 25889 23515 CLT - INSPECTION BY HFEC, FOUND A CRACK APPROXIMATELY 1 INCH, LOCATED AT THE FLOOR BEAM, STATION 520, LBL 25. INSTALLED DOUBLER AND RADIUS BLOCK AS PER USA EO NR 40604. (M) 2 L 7 2 4F RT A16WE 1996021600584 19960216 00584 NM 1996 2 16 USAA960101 1 19960123 A 5315 FLOOR BEAM BOEING 737 737301 1384611 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 346US 25889 23515 CLT - INSPECTION BY HFEC, FOUND A CRACK APPROXIMATELY 1 INCH LOCATED AT THE FLOOR BEAM, STATION 520, RBL 45. FABRICATED AND INSTALLED DOUBLERS AND FILLERS AS PER USAIR 40604. (M) 2 L 7 2 4F RT A16WE 1996021600585 19960216 00585 NM 1996 2 16 USAA960102 1 19960123 A 5315 FLOOR BEAM BOEING 737 737301 1384611 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 346US 25889 23515 CLT - INSPECTION FOUND BY HFEC, A CRACK APPROXIMATELY 1 INCH LOCATED AT FLOOR BEAM STATION 520, LBL 45. FABRICATED AND INSTALLED DOUBLERS AND FILLERS AS PER USAIR EA NR 40604. (M) 2 L 7 2 4F RT A16WE 1996021600586 19960216 00586 NM 1996 2 16 USAA960103 1 19960123 A 5330 SKIN BOEING 737 737301 1384611 NM FS 530 TORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 346US 25889 23515 CLT - INSPECTION VISUALLY FOUND 2 INCHES OF TORN SKIN AT EDGE OF CUTOUT, GND AIR/COND LOCATED APPROXIMATELY FS 530 BL0. INSTALLED REPAIR STRAP AS PER USAIR EO NR 40532. (M) 2 L 7 2 4F RT A16WE 1996021600587 19960216 00587 NM 1996 2 16 USAASB96009 1 19960117 A 5610 5893543110 WINDSHIELD BOEING 737 7372B7 1384560 NM FLIGHT DECK CRACKED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 282AU 23115 FLT NR 1080 - PIT - DIVERTED TO PIT, FLIGHT OFFICERS WINDSHIELD CRACKED IN FLIGHT. MAINTENANCE REPLACED FLIGHT OFFICERS COCKPIT WINDSHIELD. (M) 2 L 7 2 4F A16WE 1996021600588 19960216 00588 NM 1996 2 16 USAASB96011 1 19960119 A 2130 7207375 VALVE BOEING 737 7373B7 1384580 NM AFT CARGO COMPT FAILED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 520AU 23706 FLT NR 1111 - PIT - RAPID DEPRESSURIZATION AT FL 370. CABIN CLIMBED AT 2000 FT/MINUTE. PRESS CONTROLLER WOULD NOT CONT ROL CABIN IN STANDBY, MANUAL AC, OR MANUAL DC. MAINTENANCE REPLACED RIGHT SAFETY RELIEF VALVE. (M) 2 L 7 2 4F RT A16WE 1996021600589 19960216 00589 NM 1996 2 16 USAASB96012 1 19960119 A 2130 PRESSURIZATION BOEING 737 737201 1384454 NM CABIN LOST A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 242US 22444 FLT NR 818 - PIT - FLIGHT DIVERTED DUE TO LOSS OF PRESSURIZATION. (M) 2 L 7 2 4F A16WE 1996021600590 19960216 00590 NM 1996 2 16 USAASB96013 1 19960119 A 3230 UPLOCK BOEING 737 737301 1384611 NM RT MLG LACK OF LUBE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 300AU 23228 FLT NR 1551 - MCO - RIGHT GEAR INDICATED UNSAFE (NOT LOCKED) AFTER GEAR RETRACTION. GEAR WAS RECYCLED WITH SAME RESULT. MAINTENANCE CHECKED LANDING GEAR SENSORS AND INDICATIONS IAW MM. ALL CHECKED NORMAL. PERFORMED RETRACTION CHECK IAW MM. ALL SYSTEMS AND INDICATIONS CHECKED NORMAL. CLEANED AND LUBED RT GEAR UPLOCK. (M) 2 L 7 2 4F RT A16WE 1996021600591 19960216 00591 NM 1996 2 16 USAASB96014 1 19960119 A 2622 892480 EXTINGUISHER BOEING 737 737301 1384611 NM RT BAG BIN LEAKING A USAA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 19 350US 23553 FLT NR 1974 - CLT - AFT WATER FIRE EXTINGUISHER SEAL MISSING AND IS LEAKING. MAINTENANCE REPLACED EXTINGUISHER. (M) 2 L 7 2 4F RT A16WE 1996021600592 19960216 00592 NM 1996 2 16 USAASB96015 1 19960119 A 8012 START VLV LIGHT BOEING 737 737296 1384486 NM COCKPIT ILLUMINATED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 238US 22398 FLT NR 1951 - BOS - START VALVE OPEN LIGHT CAME ON IN FLIGHT. RETURNED TO FIELD. (M) 2 L 7 2 4F RT A16WE 1996021600593 19960216 00593 NM 1996 2 16 USAASB96016 1 19960120 A 8012 START VLV LIGHT BOEING 737 737296 1384486 NM NR 2 ENGINE ILLUMINATED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 238US 22398 FLT NR 388 - JAX - DIVERTED TO JAX, DUE TO START VALVE OPEN LIGHT ILLUMINATED AND NR 2 ENGINE OVERHEAT. (M) 2 L 7 2 4F RT A16WE 1996021600594 19960216 00594 NM 1996 2 16 USAASB96019 1 19960124 A 3350 20131 BATTERY PACK BOEING 737 737301 1384611 NM BS 634 DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334US 23231 FLT NR 1191 - PHL - MAINTENANCE FOUND L2 DOOR EMERGENCY ESCAPE SLIDE LIGHT INOP. MAINTENANCE REPLACED THE BATTERY PACK. (M) 2 L 7 2 4F RT A16WE 1996021600595 19960216 00595 1996 2 16 VTZA96057 4 19960103 A 3417 7000700953 AIR DATA JETAIR JETSTM JETSTM4101 1500501 EU NR 1 FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 305UE 41019 FLT NR 6211 - IAD-PVD - DURING CRUISE, RETURNED TO IAD DUE TO THE AIRSPEED INDICATION SPLIT OF 100 KNOTS, WITH THE CAPTA INS AIRSPEED INDICATING 30 KNOTS OVER THE OVERSPEED WARNING. AIRCRFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENA NCE REPLACED THE NR 1 AIR DATA COMPUTER. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996021600596 19960216 00596 EU 1996 2 16 VTZA96058 1 19960103 A 3411 Q50AB1 CURRENT SENSOR BAG JETSTM JETSTM3201 1500217 EU FORWARD FUSELAGE FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 495UE 818 FLT NR 6218 - IAD-ELM - DURING CLIMB-OUT, RETURNED TO IAD DUE TO THE NR 1 PITOT HEAT FAILING. AIRCRAFT LANDED AT IAD WI TH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE CURRENT SENSOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SER VICE. (M) 2 L 7 2 4T RT A56EU 1996021600600 19960216 00600 EU 1996 2 16 WTAA960001 1 19960101 A 3240 AC63740 MAXARETTE BAG JETSTM JETSTM3101 1500215 EU RT MLG INOPERATIVE A WTAA O OTHER O OTHER LD LANDING 1 WP 17 107XV 723 SBP - RIGHT BRAKE REPORTED INOPERATIVE ON LANDING ROLL OUT. MAINTENANCE REPLACED RIGHT WHEEL BRAKE MAXARETTE. BRAKE SY STEM OPERATION NORMAL DURING TAXI CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996021600601 19960216 00601 EU 1996 2 16 WTAA960002 1 19960103 A 2612 D2370120 FIRE DETECTOR BAG JETSTM JETSTM3101 1500215 EU RT ENGINE INTERMITTENT A WTAA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 17 418UE 780 MOD - RIGHT ENGINE FIRE BELL ACTIVATES INTERMITTENTLY. MAINTENANCE WAS UNABLE TO DUPLICATE DISCREPANCY. REPLACED RIGHT ENGINE FIRE DETECTOR FOR PRECAUTIONARY PURPOSES. DETECTION SYSTEM FUNCTIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 2 4T RT A21EU 1996021600602 19960216 00602 EU 1996 2 16 WTAA960003 1 19960105 A 3230 1860 UPLOCK BAG JETSTM JETSTM3101 1500215 EU RT MLG FAILED A WTAA O OTHER J WARNING INDICATION LD LANDING 1 WP 17 426UE 774 LAX - MAIN LANDING GEAR FAILED TO INDICATE DOWN AND LOCKED AFTER GEAR EXTENSION PRIOR TO LANDING. CREW ACCOMPLISHED EME RGENCY GEAR EXTENSION PROCEDURES. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT MAIN LANDING GEAR UPLOC K. LANDING GEAR EXTENSION AND RETRACTION OPERATION NORMAL DURING GEAR SWING. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996021600603 19960216 00603 SO 1996 2 16 WTAA960004 1 19960105 A 3230 922AA2YA6P PROX SENSOR EMB 120 EMB120RT SO LT MLG OUT OF ADJUST A WTAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 17 250YV 120250 RDD - LEFT FORWARD GEAR DOORS REMAINED OPEN AND LEFT 'A' RED INTRANSIT LIGHT REMAINED ILLUMINATED FOLLOWING GEAR RETRACT ION ON DEPARTURE FROM STATION. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. AIRCRAFT FERRIED TO FAT FOR REPAIRS. MA INTENANCE ADJUSTED LEFT MAIN LANDNIG GEAR UPLOCK 'A' PROXIMITY SWITCH. LANDING GEAR SYSTEM OPERATIONAL CHECK NORMAL DUR ING GEAR SWING. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996021600604 19960216 00604 SO 1996 2 16 WTAA960005 1 19960110 A 3234 12038594001 GEAR SELECTOR EMB 120 EMB120RT SO COCKPIT FAILED A WTAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 17 201YW 120201 CIC - DURING REPOSITION FLIGHT CIC TO RDD, LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION W ITHOUT INCIDENT. AIRCRAFT RELEASED FOR FERRY FLIGHT TO FAT FOR REPAIRS. MAINTENANCE REMOVED AND REPLACED LANDING GEAR SELECTOR UNIT. GEAR RETRACTION SYSTEM OPERATIONAL CHECK NORMAL DURING GROUND RETRACTION CHECK. AIRCRAFT RETURNED TO SE RVICE. (M) 2 L 7 2 4T RT A31SO 1996021600606 19960216 00606 SO 1996 2 16 WTAA960007 1 19960112 A 5230 1202317001 SEAL EMB 120 EMB120RT SO CARGO DOOR LOOSE A WTAA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 17 284UE 120145 SFO - CREW REPORTED, UNABLE TO PRESSURIZE AIRCRAFT AFTER DEPARTURE. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAI NTENANCE RESECURED LOOSE CARGO DOOR SEAL. AIRCRAFT PRESSURIZATION SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED T O SERVICE. (M) 2 L 7 2 4T RT A31SO 1996021600607 19960216 00607 EU 1996 2 16 WTAA960008 1 19960112 A 2130 2648A000 EMER SAFETY VLV BAG JETSTM JETSTM3101 1500215 EU FWD PRESS BLKHD CLOGGED FILTER A WTAA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 17 107XV 723 LAX - CREW REPORTED, UNABLE TO PRESSURIZE AIRCRAFT IN AUTO MANUAL MODE AFTER DEPARTURE. AIRCRAFT RETURNED TO STATION WI THOUT INCIDENT. MAINTENANCE CLEANED DIFFERENTIAL FILTER ON EMERGENCY SAFETY 'DUMP' VALVE. PRESSURIZATION SYSTEM OPERAT IONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996021600608 19960216 00608 SO 1996 2 16 WTAA960009 1 19960114 A 2752 3203001005 ACTUATOR EMB 120 EMB120RT SO RT TE FLAP FAILED A A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 17 280UE 120090 SFO - TAKEOFF ABORTED WITHOUT INCIDENT. FLAP ASYMMETRY AND FAULT REPORTED DURING TAKEOFF ROLL. AIRCRAFT FERRIED TO FAT FOR REPAIRS. MAINTENANCE REMOVED AND REPLACED RIGHT INBOARD FLAP ACTUATOR. FLAP SYSTEM OPERATIONAL CHECK NORMAL. AIR CRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996021600609 19960216 00609 EU 1996 2 16 WTAA960010 1 19960116 A 2612 51224127 FIRE LOOP BAG JETSTM JETSTM3101 1500215 EU RT ENGINE SHORTED A WTAA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 17 418UE 780 ACV - RIGHT ENGINE FIRE DETECTION LIGHT WILL NOT EXTINGUISH. AIRCRAFT FERRIED TO FAT FOR REPAIRS. MAINTENANCE REPLACED RIGHT ENGINE FIRE DETECTION LOOP. DETECTION SYSTEM FUNCTIONAL CHECK NORMAL. AIRCRAFT RETURNED SERVICE. (M) 2 L 7 2 4T RT A21EU 1996021600610 19960216 00610 SO 1996 2 16 WTAA960011 1 19960116 A 7712 SEDLOC2R TQ INDICATOR EMB 120 EMB120RT SO LT ENGINE FAILED A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 17 278UE 120083 FAT - LEFT ENGINE TORQUE INDICATION FAILED ON TAKEOFF ROLL PRIOR TO V1. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE REPLACED LEFT TORQUE INDICATOR. ENGINE INDICATIONS NORMAL DURING GROUND RUN. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996021600611 19960216 00611 SO 1996 2 16 WTAA960012 1 19960116 A 3150 AURAL WARNING EMB 120 EMB120RT SO COCKPIT ACTIVATED A WTAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 17 280UE 120090 FAT - TAKEOFF ABORTED WITHOUT INCIDENT. AURAL WARNING ACTIVATED DURING TAKEOFF ROLL. UNABLE TO DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996021600612 19960216 00612 NE 1996 2 16 9603116613 2 19960212 A 7261 ENGINE BOEING 747 747251B 1384892 NM PWA JT9 JT9D7F 52054 NE NR 1 HIGH OIL USE A NWAA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CR CRUISE 1 GL 01 613US 20358 89633 EN ROUTE, THE NR 1 ENGINE HAD HIGH OIL CONSUMPTION. CREW DUMPED 15,000 LBS OF FUEL AND DIVERTED TO SFO WITHOUT FURTHER INCIDENT. AIRCRAFT IS SCHEDULED FOR NR 1 ENGINE CHANGE. 2 L 7 4 4F 4 F A20WE E20EA 1996021600613 19960216 00613 NE 1996 2 16 9603121156 2 19960210 A 7530 BLEED CONVERTER DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20J 52054 NE NR 3 ENGINE MALFUNCTIONED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DE DESCENT 1 GL 01 156US 46765 86164 AT TOP OF DESCENT, THE NR 3 ENGINE EXPERIENCED COMPRESSOR STALL. THE NR 3 ENGINE WAS SHUTDOWN AND RESTARTED. FLIGHT CO NTINUED TO LGW WITHOUT FURTHER INCIDENT. REPLACED BLEED CONVERTER AND PS4 RESTRICTOR. PERFORMED ENGINE RUNUP AND ALL P ARAMETERS WERE NORMAL. 2 L 7 3 4F 4 F A22WE E20EA 1996021600614 19960216 00614 WP 1996 2 16 9603629925 1 19960209 A 3350 92274517 RELAY DOUG DC9 DC932 3022066 WP LT NACELLE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 925US 47472 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK WITH NO HELP. REPLACED RELAY R2-213 AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996021600615 19960216 00615 WP 1996 2 16 9603639989 1 19960209 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP TAIL CONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8945E 47181 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL CONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996021600616 19960216 00616 WP 1996 2 16 9603649960 1 19960211 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 920RW 47163 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD GALLEY EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERIES AND OPERATIONA L CHECK NORMAL. 2 L 7 2 4F A6WE 1996021600617 19960216 00617 WP 1996 2 16 96FDEA00237 1 19960213 A 2781 CONNECTOR DOUG DC10 DC1010F 3022111 WP LE SLAT LOOSE A FDEA O OTHER N FALSE WARNING AP APPROACH 1 SO 25 68057 48264 RECEIVED SLAT DISAGREE LIGHT, AIRBORNE AT FLAPS 15 DEGREES, NO FLAP LANDING ACCOMP EWR. FOUND SLAT HANDLE LAND LIMIT SW ITCH S1-380 PLUG LOOSE. RESECURED SAME, OPERATED SLATS/FLAPS SEVERAL TIMES AND ALL OPS CKS NORMAL. 2 L 7 3 4F A22WE 1996021600618 19960216 00618 WP 1996 2 16 96FDEA00238 1 19960213 A 2781 H024B SLAT HANDLE DOUG DC10 DC1010F 3022111 WP LE FLAPS WORN A FDEA O OTHER N FALSE WARNING AP APPROACH 1 SO 25 68057 48264 SLAT DISAGREE LIGHT AIRBORNE PAST FLAPS 0 EXT APPROACH AND LANDING IN 0 EXT SLAT. SEVERAL DISAGREE LIGHTS EVEN AT SLAT EXTEND. WIGGLING SLAT HANDLE FIXED THIS EACH TIME. CHECKED LEADING EDGE SLATS PER TAFI 27-80-00 FAULTS CODE AD. BITE CHECKED PROXIMITY ELECTRONIC UNIT CHANNELS 1-6, CHECKED NORMAL. T/S TO SLAT HANDLE T/O LIMIT SWITCH. REMOVED AND REPLA CED BOTH SLAT HANDLE, T/O RETRACT (S1-379) AND SLAT HANDLE LIMIT (S1-380) IAW MM 27-84-02. OPS CHECKED SLAT LIGHTS, OPS NORMAL. 2 L 7 3 4F A22WE 1996021600619 19960216 00619 NM 1996 2 16 96FDEA00239 1 19960214 A 5320 SHEAR TIE BOEING 727 72722 1384002 NM BS 970 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CORROSION ON BOTTOM OF SHEAR TIE BS 970 RBL 8 TO 13 WL 146, FOUND WHILE WORKING NR0053. REMOVED DAMAGED SHEAR TIE, FABR ICATED NEW SHEAR TIE IAW FEDEX SRM 53-10-4, CLEANED UP AREA AND INSTALLED SHEAR TIE. 2 L 7 3 4F A3WE 1996021600620 19960216 00620 NM 1996 2 16 96FDEA00240 1 19960214 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM BS 950 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CORROSION (C53-224-01) ON UPPER CHORD OF BS 950 FLOORBEAM AT RBL 21 WL 208. CLEANED AND TREATED CORROSION ON UPPER CHOR D OF BS 950 FLOORBEAM AT RBL 21 WL 208, FOUND TO BE WITHIN LIMITS PER FEDEX EA 7-5310-27447. 2 L 7 3 4F A3WE 1996021600621 19960216 00621 NM 1996 2 16 96FDEA00241 1 19960213 A 3251 AC67402550JL CYLINDER DOUG MD11 MD11F 3023600 NM NLG STEERING FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 612FE 48605 DURING OPS CK OF NOSE WHEEL STEERING, THE RT STEERING CYLINDER BLEW APART (LITERALLY). ** (S/D) ** REMOVED AND REPLACED RT NOSE WHEEL STEERING CYLINDER PER MM 32-52-30. S/N OFF AP214, S/N ON FEC101. 2 L 7 3 4F RT A22WE 1996021600622 19960216 00622 NM 1996 2 16 96FDEA00242 1 19960201 A 5330 SKIN BOEING 727 72727 138400K NM BS 720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 494FE 21532 BS 720 O/B SIDE OF STR 28 RT, FUSELAGE SKIN IS BULGING. CUT OUT DAMAGE AREA 1 INCH BY 2 INCH AND INSTALLED DOUBLER PER SRM 51-0-6. 2 L 7 3 4F A3WE 1996021600623 19960216 00623 NM 1996 2 16 96FDEA00243 1 19960201 A 5320 SHEAR TIE BOEING 727 727227 1384078 NM BS 590 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 494FE 21532 AFT LEG OF SHEAR TIE ON BELL FRAME STA 590 IS DEEPLY CORRORED BETWEEN STR 26 TO 27L. CORROSION WAS FOUND BEYOND LIMITS. REMOVED SHEAR TIE AND REPLACES WITH SERVICEABLE SHEAR TIE PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996021600624 19960216 00624 NM 1996 2 16 96FDEA00244 1 19960214 A 5313 BAC1498139 STRINGER BOEING 727 72722 1384002 NM BS 400 GOUGE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 GOUGE IN STR BS 400 STR 16R. REPAIRED GOUGE IN STR BS 400 STR 16R PER FEDEX SRM 53-10-03 FIG 2. 2 L 7 3 4F A3WE 1996021600625 19960216 00625 NM 1996 2 16 96FDEA00245 1 19960214 A 5311 6515932 FRAME BOEING 727 72722 1384002 NM BS 580 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 THE FRAME AT BS 580 IS CRACKED ON I/B FLANGE AT RBL 67, WL 210. *S/D* THE FRAME AT BS 580, RBL 67, WL 210, WAS FOUND T O BE DAMAGED BEYOND LIMITS PER SRM 53-10-1. REPAIRED FRAME PER FEDEX SRM 51-40-3. 2 L 7 3 4F A3WE 1996021600626 19960216 00626 NM 1996 2 16 96FDEA00246 1 19960214 A 5320 WEB BOEING 727 72722 1384002 NM BS 560-580 MECH DAMAGE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 MECHANICAL DAMAGE AND MISDRILLED HOLES IN WEB AT BS 560 TO 580 LBL 41 WL 200. 2 L 7 3 4F A3WE 1996021600627 19960216 00627 NM 1996 2 16 96FDEA00247 1 19960214 A 5313 STRINGER BOEING 727 72722 1384002 NM BS 640 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 WHILE WORKING NR0429, FOUND GOUGE ON STR NR 3 BS 640 RT. 2 L 7 3 4F A3WE 1996021600628 19960216 00628 NM 1996 2 16 96FDEA00248 1 19960214 A 5320 6516350 SHEAR WEB BOEING 727 72722 1384002 NM BS 1174 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION EMANATING FROM UNDER NUTPLATES ON BOTTOM SIDE OF SHEAR WEB AT BS 1174 RBL 5, LBL 20 WL 208. *S/D* FABRICATED NEW WEB AND INSTALLED PER SRM 53-10-1. 2 L 7 3 4F A3WE 1996021600629 19960216 00629 NM 1996 2 16 96FDEA00249 1 19960216 A 5320 6517684 SHEAR WEB BOEING 727 72722 1384002 NM BS 1173 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 WHILE WORKING CARD NR 0583, FOUND BS 540 FLOOR BEAM, BL 0 WL 208 TO HAVE DOUBLE HOLE. *S/D* REPAIRED FLOOR BEAM AT BS 540, BL 0, WL 208 IAW FEDEX SRM 53-10-8. 2 L 7 3 4F A3WE 1996021600630 19960216 00630 NM 1996 2 16 96FDEA00250 1 19960214 A 5315 6540145 FLOOR BEAM BOEING 727 72722 1384002 NM BS 580 DOUBLE HOLE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 WHILE WORKING CARD NR 0685, FOUND BS 580 FLOOR BEAM, BL 0 WL 208 TO HAVE DOUBLE HOLE. *S/D* REPAIRED DOUBLE HOLE PER S RM 53-10-8 SRM 53-10-8. 2 L 7 3 4F A3WE 1996021600631 19960216 00631 NM 1996 2 16 96FDEA00251 1 19960214 A 5315 6540145 FLOOR BEAM BOEING 727 72722 1384002 NM BS 600 DOUBLE DRILLED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 194FE 19143 WHILE WORKING CARD NR 0683, FOUND BS 600 FLOOR BEAM, BL 0 WL 208 TO HAVE DOUBLE HOLE. *S/D* REPAIRED FLOOR BEAM BS 600 , BL 0, WL 208 IAW FEDEX SRM 53-10-8, HOLE PER SRM 53-10-8. 2 L 7 3 4F A3WE 1996021600632 19960216 00632 NM 1996 2 16 96FDEA00252 1 19960214 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM BS 970 MISDRILLED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 WHILE WORKING NR0754, FOUND DOUBLE HOLE IN BS 970 FLOORBEAM AT BL 0 WL 208. 2 L 7 3 4F A3WE 1996021600633 19960216 00633 NM 1996 2 16 96FDEA00253 1 19960214 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM BS 990 MISDRILLED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 WHILE WORKING NR0754, FOUND DOUBLE HOLE IN BS 990 FLOORBEAM AT BL 0 WL 208. 2 L 7 3 4F A3WE 1996021600634 19960216 00634 NM 1996 2 16 96FDEA00254 1 19960214 A 2910 HYD TUBE BOEING 727 727227 1384078 NM A HYD SYST FAILED A FDEA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 25 485FE 21488 HYD SYS 'A' LOSS ON DESCENT INTO TYS. ** (S/D) ** REMOVED AND REPLACED NR 1 ENG TO 'A' SYS MODULE PRESSURE TUBE ASSY. S ERVICED HYD - AND RAN NR 1 ENG. OPS AND LEAK CHECKS GOOD. 2 L 7 3 4F A3WE 1996021600635 19960216 00635 NM 1996 2 16 96UAL900111 1 19960213 A 2131 39268631 REGULATOR BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE E/E COMPT LEAKING A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 9024U 19062 SMOKE IN CABIN, THE RIGHT PACK WAS OFF AND THE OVERHEAT LIGHT CAME ON. THE TURBOFAN WAS RUNNING ALL THE TIME. REPLACED THE PRESSURE REGULATOR, CHECKS OK. THE SHOP FOUND AN INTERNAL DIAPHRAGM WAS LEAKING. 2 L 7 2 4F 4 F A16WE E2EA 1996021600636 19960216 00636 NM 1996 2 16 DHL96715001 1 19960211 A 2751 18129932 POSITION IND BOEING 727 727155C 138404Z NM TE FLAPS MALFUNCTIONED A T DHLA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 715DH 19618 UPON APPROACH, WHEN FLAPS 2 WERE SELECTED INBOARD FLAPS WENT TO 2 DEGREES OUTBOARD SHOWED 0 DEGREES WORKED ALTERNATE PRO CEDURE, ABNORMAL PROCEDURE AND LANDED AFTER LANDING OUTBOARD FLAPS SHOWED 2 DEGREES. TROUBLESHOT PER MM 27-51-00, FOUND FLAP POSITION INDICATOR OUTBOARD DEFECTIVE. REPLACED OUTBOARD FLAP POSITION INDICATOR, OPERATION CHECKS OKAY. 2 L 7 3 4F A3WE 1996021600637 19960216 00637 NM 1996 2 16 SWAA960070 1 19960206 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21722 DURING SCHEDULED CHECK, FOUND AFT SERVICE DOORWAY SKIN AT LOWER HINGE CUTOUT CRACKED UNDER REINFORCEMENT TAB. REPAIRED P ER BOEING DRAWING 65C27269 AND SWA ACO 649-53. 2 L 7 2 4F A16WE 1996021600638 19960216 00638 NM 1996 2 16 SWAA960071 1 19960206 A 5320 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 807 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED CHECK, FOUND AFT CARGO BELT FRAME AT BS 807 HAS CORRODED SHEAR TIE BETWEEN S27 AND 26R. REPLACED PER B OEING SRM. 2 L 7 2 4F RT A16WE 1996021600639 19960216 00639 NM 1996 2 16 SWAA960072 1 19960206 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 747 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 314SW 23336 DURING SCHEDULED CHECK, FOUND A 3 INCH CRACK AT S18R AT BS 747. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996021600640 19960216 00640 NM 1996 2 16 SWAA960073 1 19960206 A 2150 20405011 ACM BOEING 737 7373Y0 1384671 NM RIGHT MALFUNCTIONED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 664SW 23495 PASSENGER COMPLAINED OF STRONG OIL ODOR IN CABIN. ALSO, FLIGHT CREW EXPERIENCED SAME IN COCKPIT, SEEM TO BE STONGER AT OVERWING EXIT AREA. REPLACED AIR MACHINE, WATER SEPARATOR BAG AND OPS CHECKED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996021600641 19960216 00641 NM 1996 2 16 SWAA960074 1 19960213 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED 1/4 D-CHECK, FOUND A .75 INCH CRACK IN FUSELAGE SKIN AT FWD UPPER RADIUS OF DOOR TORQUE TUBE CUTOUT, AT AFT SERVICE DOOR CUTOUT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996021600642 19960216 00642 NM 1996 2 16 SWAA960075 1 19960213 A 5412 BLKHD ANGLE BOEING 737 7372T4 1384492 NM NR 2 ENGINE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED 1/2 D-CHECK, FOUND NUMBER 2 ENGINE PYLON, UPPER FWD BULKHEAD WEB TO SKIN ATTACH ANGLE CRACKED AT FWD FA STENER STA 222.7. REPAIRED PER SWA RA 1-257-030. 2 L 7 2 4F A16WE 1996021600643 19960216 00643 NM 1996 2 16 SWAA960076 1 19960213 A 5512 SKIN BOEING 737 7373H4 1384600 NM RT HORZI STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 350SW 24409 DURING SCHEDULED 1/4 D-CHECK, FOUND LOWER SKIN OF RIGHT HORZI STAB CRACKED BETWEEN STA 120 AND 129. REPAIRED PER SWA RA 1-355-0215. 2 L 7 2 4F RT A16WE 1996021600644 19960216 00644 NM 1996 2 16 SWAA960077 1 19960213 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND FUSELAGE BULKHEAD CRACKED AT BS 727 BBL 0. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996021600645 19960216 00645 NM 1996 2 16 SWAA960078 1 19960213 A 5312 BLKHD ANGLE BOEING 737 7373H4 1384600 NM BS 727 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND FUSELAGE BULKHEAD SUPPORT ANGLE CRUSHED AND DENTED AT BS 727, BBL 0. REPAIRED PER BOEIN G SRM. 2 L 7 2 4F RT A16WE 1996021600646 19960216 00646 NM 1996 2 16 SWAA960079 1 19960213 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 526 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND WEB CRACKED IN RADIUS AT BS 526 LBL 44 WL 160. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996021600647 19960216 00647 NM 1996 2 16 SWAA960080 1 19960213 A 5320 BRACKET BOEING 737 7373H4 1384600 NM BS 887 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME HAT SECTION ATTACH BRACKET AT BS 887 S9R, BS 847 S9R, BS 827 S9R, BS 787 S9R, BS 787 S9R, BS 767 S9R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996021600648 19960216 00648 NM 1996 2 16 SWAA960081 1 19960213 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 327 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND FORWARD GALLEY DOORWAY LOWER AFT CORNER SKIN CRACKED 1 INCH AT BS 327 WL 206 RBL 65. RE PAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996021600649 19960216 00649 NM 1996 2 16 SWAA960082 1 19960213 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND BULKHEAD AT BS 178 CRACKED 2 PLACES WL 219, LBL 5 TO 12. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996021600650 19960216 00650 NM 1996 2 16 SWAA960083 1 19960213 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND BULKHEAD AT BS 178 CRACKED 2 PLACES WL 210 TO 213, RBL 5.7. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996021600692 19960216 00692 SO 1996 2 16 96ZZZX705 2 19960123 A 8530 649317CEA6 CYLINDER CESSNA 210 T210M 2073451 CE CONT O520 TSIO520R 17040 SO ENGINE FAILED A A CFCA K NONE O OTHER IN INSP/MAINT 1 GL 03 7398M 1044 21062018 511444 THE NORMAL LIFE OF THIS CYLINDER IS AT 1,500 HOURS TCO. THIS ONE LASTED 1,043 HOURS. THIS PREMATURE WEAR FAILURE SEEMS TO BE AN UNFORTUNATE TREND FOR CERMICHROME CYLINDERS. SUBMITTER RECOMMENDS NORMAL OPERATIONS WATCHING ENGINE PARAMETER S AND FREQUENT OIL CHANGE INTERVALS. 1 H 7 1 3O 3 O 3A21 E8CE 1996021600693 19960216 00693 SO 1996 2 16 96ZZZX706 1 19960101 A 3260 487869 SWITCH PIPER PA23 PA23250 7102308 SO NLG DOWNLOCK OUT OF ADJUST A CFCA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 03 3260 277554025 PILOT COULD NOT GET DOWN AND LOCKED INDICATION OF THE NOSE GEAR. UPON SUCCESSFUL LANDING (GEAR WAS IN FACT DOWN AND LOC KED), NOTED THE SWITCH AND BRACKET ASEMBLY WERE NOT MAKING CONTACT. SWITCH IS ADJUSTABLE AND SUBMITTER SUGGESTS CAREFUL INSPECTION BE MADE AT SCHEDULED INSPECTIONS TO VERIFY SWITCH IS MAKING POSITIVE CONTACT. 1 L 7 2 3O 1A10 1996021600694 19960216 00694 CE 1996 2 16 96ZZZX707 1 19960101 A 3230 12430192 BRACKET CESSNA 210 T210M 2073451 CE NLG BENT A CFCA K NONE O OTHER IN INSP/MAINT 1 GL 03 6611C 21063930 DURING CERTAIN LOADING CONDITIONS, THE T210 CAN PRODUCE A NOSE WHEEL SHIMMEY THAT ALLOWS THIS BRACKET TO BEND OUT OF POS ITION. SUBMITTER RECOMMENDS A PRE-FLIGHT INSPECTION FOR PROPER ENGAGEMENT OF SWITCH. 1 H 7 1 3O 3A21 1996021600695 19960216 00695 EU 1996 2 16 RAIA960121 1 19960114 A 2150 32145602 PACK VALVE AEROSP ATR42 ATR42300 8680920 EU LT ENGINE DIRTY A RAIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 2FOR 10120 8974 199 STL - FLT 7180 - NR 1 PACK FAULTED WITH STRONG ELECTRICAL SMOKE SMELL ASSOCIATED, RETURNED TO GATE. MAINTENANCE CLEANED PACK VALVE CONNECTION SURFACE, GROUND RUN GOOD. (X) 2 H 7 2 4T RT A53EU 1996021600696 19960216 00696 NE 1996 2 16 RAIA960122 2 19960114 A 7321 789843 ECU AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE RT ENGINE FAILED A RAIA O OTHER J WARNING INDICATION CL CLIMB 1 CE 03 2FOR 12319 10432 199 120561 STL - FLT 7180 - NR 2 ECU FAULTED, COULD NOT RESET. MAINTENANCE REPLACED ECU, GROUND RUNS GOOD. ENGINE TT 14,383.1 HOU RS. (X) 2 H 7 2 4T 4 T RT A53EU E20NE 1996021600697 19960216 00697 WP 1996 2 16 WRLA96002 1 19960116 A 2130 CONNECTOR DOUG DC10 DC1030 3023501 WP ISOLATION VALVE DIRTY A WRLA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 27 2FOR 46933 ON TAXIING, AFTER ENGINE START, FLIGHT CREW NOTED NR 1 AND NR 2 ISOLATION VALVES, PN DC26F14155, WOULD NOT CLOSE. FLIGH T CREW ELECTED TO RETURN TO GATE FOR CORRECTIVE ACTION. AIRCRAFT RETURNED TO GATE WITHOUT INCIDENT. DURING TROUBLESHOO TING, MAINTENANCE CREW IDENTIFIED INTERMITTENT CONTACT BETWEEN WIRING HARNESSES AND ISOLATION VALVES. CLEANED CANNON PL UG NR 1 AND NR 2 ISOLATION VALVES. OPS CHECKED BOTH ISOLATION VALVES. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 3 4F A22WE 1996021600698 19960216 00698 WP 1996 2 16 9603659979 1 19960209 A 5350 RELEASE MECH DOUG DC9 DC931 3022065 WP TAILCONE OUT OF ADJUST A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9343 47439 DURING EO 5350-01032 TAILCONE FUNCTIONAL CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO DROP THE TAILCONE USING THE I NTERIOR HANDLE. REPLACED ALL 4 LATCH SPRINGS AND INTERIOR FUNCTIONAL RECHECK OK. THEN FOUND THAT EXCESSIVE FORCE WAS R EQUIRED TO DROP THE TAILCONE USING THE EXTERIOR HANDLE. TAILCONE WAS REINSTALLED WITH NO ADDITIONAL ACTION. EXTERIOR F UNCTIONAL RECHECK WAS OK. 2 L 7 2 4F A6WE 1996021600699 19960216 00699 WP 1996 2 16 9603669610 1 19960212 A 7711 EPR TRANSMITTER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9 52048 NE NR 2 ENGINE MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 01 610NW 47432 657568 NR 2 ENGINE EPR INDICATION FAILED IN CRUISE FLIGHT. THE AIRCRAFT DIVERTED TO DCA AND LANDED WITHOUT INCIDENT. MAINTENA NCE PURGED THE SYSTEM OF MOISTURE AND REPLACED THE EPR TRANSMITTER. SYSTEM OPERATION RETURNED TO NORMAL. 2 L 7 2 4F 4 F A6WE E2EA 1996021600700 19960216 00700 NM 1996 2 16 9603676305 1 19960214 A 3350 CONNECTOR BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 665US 23820 DURING LINE CHECK (TPE), THE FLOOR MOUNTED EMERGENCY LIGHT AT SEAT ROWS 24 TO 31 WERE FOUND INOPERATIVE. RECONNECTED LI GHT ASSEMBLY AT SEAT 24. OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996021600701 19960216 00701 WP 1996 2 16 9603689912 1 19960214 A 3260 H146 DNLOCK SWITCH DOUG DC9 DC931 3022065 WP LT MLG INTERMITTENT A NWAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 01 962N 47406 DURING FINAL APPROACH INTO HOU, THE LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR EXTENSION. GREEN LIGHT W AS NOT ILLUMINATED. EXECUTED GO-AROUND PROCEDURES AND SUCCESSFUL LANDING WAS ACCOMPLISHED ON SECOND ATTEMPT. FOUND THE LEFT MAIN GEAR DOWNLOCK SWITCH WITH INTERMITTENT GROUND AND NO OVERTRAVEL. REPLACED THE SWITCH. OPERATIONAL CHECK NOR MAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996021600702 19960216 00702 NM 1996 2 16 9603692204 1 19960214 A 2780 RETRACT MECH BOEING 727 727251 138408H NM NR 2 LE SLAT MALFUNCTIONED A A NWAA A J UNSCHED LANDING DUMP FUEL F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 01 204US 22544 AFTER TAKEOFF DURING FLAP RETRACTION, THE NR 2 LEADING EDGE SLAT WOULD NOT RETRACT. RECYCLED FLAPS TO NO AVAIL. VISUAL INSPECTION AND INDICATION SYSTEM SHOWED NR 2 LEADING EDGE SLAT FULLY EXTENDED. FLIGHT CREW DECLARED A YELLOW EMERGENCY AND JETTISONED 22,000 POUNDS OF FUEL. FLIGHT RETURNED TO TPA WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED A TEST H OP AND COULD NOT DUPLICATE MALFUNCTION. INVESTIGATION CONTINUES. 2 L 7 3 4F A3WE 1996021600703 19960216 00703 NM 1996 2 16 9603702204 1 19960214 A 2782 1U10955 ACTUATOR BOEING 727 727251 138408H NM NR 2 LE SLAT MALFUNCTIONED A A NWAA A J UNSCHED LANDING DUMP FUEL F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 01 204US 46585 5217 22544 DURING CLIMB UPON FLAP RETRACTION, THE NR 2 LEADING EDGE FLAP WOULD NOT RETRACT. CYCLED FLAPS TO NO AVAIL. CREW DECLAR ED A YELLOW EMERGENCY AND JETTISONED 20,000 POUNDS OF FUEL. AIRCRAFT RETURNED TO TPA WITHOUT FURTHER INCIDENT. MAINTEN ANCE REPLACED THE NR 2 LEADING EDGE SLAT VALVE AND ACTUATOR. LEAK AND OPERATIONAL CHECK WERE SATISFACTORY. PART TOTAL CYCLES, 32,960. 2 L 7 3 4F A3WE 1996021600704 19960216 00704 WP 1996 2 16 9603719178 1 19960213 A 3350 BATTERY PACK DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 3310L 45705 DURING LINE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE IN AFT CABIN. REPLACED POWER PACK AND BATTERY. OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996021600705 19960216 00705 WP 1996 2 16 9603729886 1 19960213 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 600TR 47783 DURING LINE CHECK, FOUND OVERHEAD EMERGENCY LIGHT AT ROW 22 INOPERATIVE. MAINTENANCE FOUND TWO LOOSE CONNECTIONS. TIGH TENED CONNECTIONS, REPLACED BULB AND BATTERY PACK. OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996021600706 19960216 00706 WP 1996 2 16 9603739868 1 19960211 A 3350 LIGHT DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 777NC 47787 DURING LINE CHECK, FOUND ENTRANCE DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEM BLY WITH A SERVICEABLE UNIT. CHECKED GOOD. 2 L 7 2 4F A6WE 1996021600707 19960216 00707 WP 1996 2 16 9603749886 1 19960213 A 2133 OUT FLOW VALVE DOUG DC9 DC951 3022051 WP CABIN CONTAMINATED A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 600TR 47783 ON CLIMB OUT OF DTW, CABIN PRESSURE CLIMBED UNCONTROLLABLY. FLIGHT DESCENDED TO 1000 FEET AND OPERATED PRESSURIZATION I N MANUAL CONTROL FLIGHT, CONTINUED TO DESTINATION WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND SIDEWALL INSULATION STUCK IN OUTFLOW AIR NOZZLE. REMOVED INSULATION AND PRESSURIZED AIRCRAFT. VALVES OPERATED NORMALLY AND PRESSURIZATION CHECK ED GOOD. 2 L 7 2 4F A6WE 1996021600708 19960216 00708 WP 1996 2 16 9603759868 1 19960212 A 3260 INDICATOR BULB DOUG DC9 DC951 3022051 WP RT MLG FAILED A NWAA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 GL 01 777NC 47787 ON APPROACH TO BNA, GREEN LIGHT ON RIGHT MAIN GEAR DID NOT ILLUMINATE. EXECUTED MISSED APPROACH. JARRED LIGHT SEVERAL TIMES AND GREEN LIGHT CAME ON INDICATING GEAR DOWN. LANDED WITHOUT INCIDENT. FOUND FILLAMENT BURNED ON ONE BULB AND ON E BULB WAS INOPERATIVE. CHECKED SOCKETS AND REPLACED LAMPS. CHECKED GOOD. 2 L 7 2 4F A6WE 1996021600709 19960216 00709 WP 1996 2 16 9603769877 1 19960209 A 5350 RELEASE MECH DOUG DC9 DC951 3022051 WP TAILCONE OUT OF ADJUST A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 786NC 48148 DURING EO 5350-01032 TAILCONE FUNCTION RECHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR HANDLE FROM THE CLIPS AND THAT INADEQUATE FORCE WAS REQUIRED TO DROP THE TAILCONE. ALSO, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO DROP THE TAILCONE USING THE EXTERIOR HANDLE. ADJUSTED CLIPS AND LATCHES. CHECKED OK. 2 L 7 2 4F A6WE 1996021600711 19960216 00711 WP 1996 2 16 9603789908 1 19960212 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 958N 47254 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD ENTRY OVERHEAD EMERGENCY LIGHTS VERY DIM. REPLACED BATTERIES. OPERAT IONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996021600712 19960216 00712 WP 1996 2 16 9603799955 1 19960214 A 3231 5914984 LINKAGE DOUG DC9 DC931 3022065 WP NLG DOOR OUT OF ADJUST A NWAA O OTHER E VIBRATION/BUFFET CL CLIMB 1 GL 01 922RW 47182 AFTER DEPARTURE FROM HPN, A VIBRATION WAS FELT COMING FROM NOSE GEAR AREA. FLIGHT CONTINUED TO DESTINATION (DTW) AT RED UCED SPEED AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LEFT NOSE GEAR DOOR NOT PROPERLY RIGGED. ADJUSTED DOOR LINK. OPERATIONAL CHECK NORMAL ON GEAR CYCLE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996021600713 19960216 00713 WP 1996 2 16 9603809956 1 19960211 A 5350 BEARING PLATES DOUG DC9 DC931 3022065 WP TAILCONE WORN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 923RW 47183 DURING LINE CHECK, FOUND THAT THE TAILCONE FAILED TO DROP USING THE EXTERIOR HANDLE. ALSO, FOUND FOUR LOOSE/WORN GUIDE PINS, TWO WORN BEARING PLATES, AND INADEQUATE CONDUIT TO CLAMP BLOCK CLEARANCE. TIGHTENED/REPLACED THE GUIDE PINS, REPL ACED THE BEARING PLATES, TRIMMED THE CONDUIT, AND RERIGGED THE TAILCONE PER MM 53-50-3, PG. 201, SUPP. 1. 2 L 7 2 4F A6WE 1996021600714 19960216 00714 NM 1996 2 16 96UAL900112 1 19960214 A 2760 CONTROL MECH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT SPOILER OUT OF ADJUST A UALA O OTHER O OTHER CR CRUISE 1 WP 29 587UA 26713 GROUND SPOILER ON THE LEFT WING IS FLOATING IN CRUISE, ESPECIALLY THE OUTBOARD AFT EDGE. 2 L 7 2 4F 4 F RT A2NM E17NE 1996021600715 19960216 00715 NM 1996 2 16 96UAL900113 1 19960214 A 2560 SLIDE BF GOODRICH 7A14371 BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE DOOR 2R FAILED TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 4718U G1071 19879 DURING OVERHAUL, DOOR 2 RIGHT SLIDE FAILED AIR RETENTION TEST DUE TO POROSITY ON BOTH FILL TUBES. PATCHED AREAS OF PORO SITY. 2 L 7 4 4F 4 F A20WE E20EA 1996021600716 19960216 00716 NM 1996 2 16 96UAL900114 1 19960214 A 2560 SLIDE BF GOODRICH 7A14371 BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE DOOR R2 FAILED TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 153UA G1041 20102 DURING OVERHAUL, DOOR 2 RIGHT SLIDE FAILED AIR RETENTION TEST DUE TO POROSITY ON BOTH FILL TUBES, TOP PUSHER TUBE AND CR OSS TUBE. PATCHED AREAS OF POROSITY. 2 L 7 4 4F 4 F A20WE E20EA 1996021600717 19960216 00717 NM 1996 2 16 96UAL900115 1 19960214 A 2560 PUSHER TUBE BF GOODRICH 7A14371 BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE DOOR SLIDE FAILED TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 154UA G1091 20103 DURING OVERHAUL, DOOR 2 SLIDE FAILED AIR RETENTION TEST DUE TO POROSITY ON THE TOP PUSHER TUBE. PUSHER TUBE REPLACED BY OEM. 2 L 7 4 4F 4 F A20WE E20EA 1996021600718 19960216 00718 WP 1996 2 16 ABXA9600189 1 19960214 A 3260 7000010101 UPLIMIT SWITCH DOUG DC9 DC932 3022066 WP NLG DEFECTIVE A ABXA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 23 987AX 47364 CREW REPORTS NOSE GEAR DOWNLOCK INDICATOR DID NOT ILLUMINATE INITIALLY INTO TRI. HAD TO CYCLE GEAR THEN WORKED OK, ALSO CHECKED GOOD ONTO GSP. REPLACED NOSE GEAR UP LIMIT SWITCH PER SUPPLEMENTAL MM 32-60-01. OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996021600719 19960216 00719 SO 1996 2 16 COMA9610079 1 19960214 A 5270 DOOR WARNING EMB 120 EMB120RT SO CARCO COMPT ACTIVATED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 247CA 120225 CARGO DOOR WARNING CAME ON DURING TAKEOFF. COULD NOT DUPLICATE - INSPECTED DOOR SYSTEM AND OPERATIONAL CHECK SATISFACTO RY. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 1996021600720 19960216 00720 SO 1996 2 16 COMA9610080 1 19960213 A 3060 78614423 DEICE LEAD EMB 120 EMB120RT SO LT PROP BROKEN A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 179CA 120179 LEFT PROPELLER DEICE IS INOP. REPLACED DEICE LEAD WIRE ON LT PROPELLER. 2 L 7 2 4T RT A31SO 1996021600721 19960216 00721 SO 1996 2 16 COMA9610081 1 19960213 A 3250 2050000002 POTENTIOMETER EMB 120 EMB120RT SO NLG STEERING MALFUNCTION A COMA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SO 01 254CA 120233 NOSE WHEEL STEERING DISCONNECT TEST DID NOT FUNCTION. REPLACED THE N.W.S. FEED-BACK POTENTIOMETER. 2 L 7 2 4T RT A31SO 1996021600722 19960216 00722 SO 1996 2 16 COMA9610082 1 19960213 A 2752 3203001007 ACTUATOR EMB 120 EMB120RT SO RT TE FLAP DEFECTIVE A A COMA K NONE J WARNING INDICATION UK UNKNOWN 1 SO 01 162CA 2351 120150 FLAP CONTROL FAULT WARNING. REPLACED THE RT OUTBD FLAP ACTUATOR. PART TOTAL CYCLES, 2,517. 2 L 7 2 4T RT A31SO 1996021600723 19960216 00723 SO 1996 2 16 COMA9610083 1 19960213 A 2913 PV302229 HYD PUMP EMB 120 EMB120RT SO RT ENGINE LEAKING A COMA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 256CA 7368 6830 120245 HYDRAULIC FLUID LEAKING FROM RT ENGINE NACELLE. REPLACED THE ENGINE DRIVEN HYDRAULIC PUMP. PART TOTAL CYCLES, 7,269. 2 L 7 2 4T RT A31SO 1996021600724 19960216 00724 EU 1996 2 16 COMA9630038 1 19960213 A 3020 6058T80P03 ANTI ICE VALVE SAAB SF340 SF340A 7850100 EU RT ENGINE DEFECTIVE A COMA K NONE O OTHER CR CRUISE 1 SO 01 341CA 6994 2259 340A021 RT ENGINE INDICATED NO TORQUE DROP WHEN ANTI-ICE SELECTED ON. REPLACED THE ANTI-ICE VALVE. PART TOTAL CYCLES, 7,921. 2 L 7 2 4T RT A52EU 1996021600725 19960216 00725 EA 1996 2 16 COMA9660030 1 19960213 A 5610 NP1393211 WINDSHIELD CNDAIR CL600 CL6002B19 EA LT COCKPIT CRACKED A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 920CA 349 349 7022 PILOT'S WINDSHIELD CRACKED. REPLACED WINDSHIELD. PART TOTAL CYCLES, 321. 2 L 7 2 4F RT A21EA 1996021600727 19960216 00727 NM 1996 2 16 DL72K960334 1 19960211 A 5312 BLKHD STIFFENER BOEING 727 727232 1384082 NM FS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 472DA 20749 FOUND ON MV1 1183 BULKHEAD VERTICAL STIFFENER CRACKED 1 INCH AT LOWER END, BL 8L WL 185. REPAIR: REPAIRED PER M/M 55-1 1-0, PAR 9. 2 L 7 3 4F A3WE 1996021600728 19960216 00728 NM 1996 2 16 DL72L960330 1 19960213 A 2750 ANGLE BOEING 727 727232 1384082 NM NR1 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 511DA 21313 ATTACH ANGLE BROKEN NR 1 L.E. FLAP ACTUATOR BOX. FOUND DURING B-1 LTR CK TPAMM. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1996021600729 19960216 00729 NM 1996 2 16 DL72L960331 1 19960213 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 2 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 511DA 21313 FOUND DURING B-1 LETTER CHECK - .50 INCH CRACK NR 2 L/E SLAT COVE SKIN ATTATCH ANGLE BELOW I/B UPSTOP PAD. REPAIRED PER M/M 57-54-0. 2 L 7 3 4F A3WE 1996021600730 19960216 00730 NM 1996 2 16 DL72L960332 1 19960213 A 5720 STIFFENER BOEING 727 727232 1384082 NM RT WING FWD SPAR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 511DA 21313 FOUND DURING B-1 LETTER CHECK - 1 INCH CRACK LWR END SPAR STIFFENER AT NR 6 L/E SLAT I/B TRACK I/B ANGLE. REPLACED PE R MM 57-20-21. 2 L 7 3 4F A3WE 1996021600731 19960216 00731 NM 1996 2 16 DL72W960321 1 19960213 A 5751 657273421 SKIN BOEING 727 727247 138408F NM LT AILERON WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2809W 20581 DURING INSPECTION, LEFT WING AILERON LOWER OUTBOARD SKIN HAD SEVERAL OVERSIZED AND WORN FASTENER HOLES DUE TO FATIGUE. S PLICED IN NEW SECTION OF SKIN PER MM 57-51-00, FIG 801. 2 L 7 3 4F A3WE 1996021600732 19960216 00732 WP 1996 2 16 DLL10960335 1 19960213 A 3350 456 BULB LKHEED 1011 10113851 5265010 WP CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 718DA 193C1097 FLIGHT ATTENDENT REPORTED IN CDL THAT THE EXIT SIGN BETWEEN FIRST CLASS AND COACH ON RIGHT SIDE OF CABIN INOP. RELAMPED , OPERATION NORMAL. 2 L 7 3 4F A23WE 1996021600733 19960216 00733 NM 1996 2 16 DLM88960329 1 19960213 A 2161 TEMP CONTROLLER DOUG MD88 MD88 3023688 NM E/E COMP MALFUNCTIONED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 945DL 49818 ON TAKEOFF, A STRONG ACRID SMELL FILLED THE CABIN IMMEDIATELY FOR APPROX 4-5 MINUTES. BEFORE CLEARING ODOR, RETURNED WH EN GEAR EXTENDED FOR LANDING. TEMP IN COCKPIT INCREASED, SMOKE DET. ACTIVATED. FOUND RT AUTO TEMP CONT HAD VALVE FULL OPEN, RAN FULL COLD IN MANUAL, RAN BOTH ENGINES AND OPERATED BOTH PACKS. NO PROBLEMS FOUND. FWD. RT. AUTO TEMP. CONTRO LLER TO MCO AND PLAC. PER. MEL 21-00-30A. 2 L 7 2 4F RT A6WE 1996021600734 19960216 00734 NM 1996 2 16 DLM90960341 1 19960209 A 2410 41320691 FILTER BOWL DOUG MD90 MD9030 3023690 NM RT ENGINE CRACKED A DALA O OTHER K FLUID LOSS CR CRUISE 1 SO 27 908DA 53388 RIGHT AC FAULT CAME ON DURING CRUISE, ALONG WITH STATUS MSG RT GEN OIL PRESS. STARTED APU AND PICKED UP RT AC LOAD. TH EN RTI GEN OFF ILLUMINATED. FOUND RT VSCF GEN OIL LOW WITH FILTER HOUSING CRACKED AND LEAKING. REPLACED FILTER BOWL. S ERVICED, OPERATION NORMAL. 2 L 7 2 4F RT A6WE 1996021600735 19960216 00735 NM 1996 2 16 SCNA96020 1 19960210 A 3350 58791 RIBBON LEAD BOEING 727 727259 138408J NM CABIN CHAFED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 THE EMERGENCY TRACK LIGHTING FROM SEAT 7 ABC TO 14 ABC FLICKERS ON AND OFF. FOUND CHAFED RIBBON SUPPLY LINE FROM BATTER Y. REPLACED CHAFED RIBBON LEAD AND OPS CHECKED EMERGENCY LIGHTS IAW MM 33-50-00. 2 L 7 3 4F A3WE 1996021600736 19960216 00736 NM 1996 2 16 SCNA96021 1 19960213 A 3350 1000677 LIGHT BOEING 727 727225 1384077 NM L 1 DOOR FAILED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 282SC 22558 THE L-1 EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY AND LIGHT TESTED GOOD. 2 L 7 3 4F A3WE 1996021600737 19960216 00737 NM 1996 2 16 UPS205482 1 19960209 A 5311 FRAME BOEING 727 72725C 138400H NM BS 320 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C CHECK, MAINTENANCE REPORTED CRACKED FRAME BS 320, LBL 45. INSTALLED DOUBLER IAW SRM 51-30-2 AND 51-40-3. 2 L 7 3 4F A3WE 1996021600738 19960216 00738 NM 1996 2 16 UPS205483 1 19960209 A 5320 STIFFENER BOEING 727 72725C 138400H NM BS 308 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION ON HOR. STIFFENER TOP NOSE WW AROUND FASTENER HEADS BS 308, WL 181, LBL 10, RBL 10. REPAIRED PER SRM 53-10-1, 53-10-2, 51-10-6. 2 L 7 3 4F A3WE 1996021600739 19960216 00739 NM 1996 2 16 UPS205484 1 19960209 A 5320 STIFFENER BOEING 727 72725C 138400H NM BS 295 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION REINFORCING ANGLE AT BS 295, WL 181, RBL 12. REPLACED ANGLE PER SR M 51-10-6, 53-10-6, 53-10-2, 53-10-1, 51-30-5. 2 L 7 3 4F A3WE 1996021600740 19960216 00740 NM 1996 2 16 UPS205485 1 19960209 A 5320 HAT CHANNEL BOEING 727 72725C 138400H NM BS 324-340 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION ON HAT CHANNEL AT STA 324-340, RBL 20, WL 208. REPLACED HAT CHANNE L PER SRM 51-20-1, 51-10-2, 51-30-2. 2 L 7 3 4F A3WE 1996021600741 19960216 00741 NM 1996 2 16 UPS205486 1 19960109 A 5315 FLOOR BEAM BOEING 727 72725C 138400H NM BS 344 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION ON FLOOR BEAM AT STA 344, RBL 17-20, WL 208. REPAIRED FLOOR BEAM P ER SRM 53-10-8, FIG. 7 AND E.R. NR 020696CD3, 53-10-10. 2 L 7 3 4F A3WE 1996021600742 19960216 00742 NM 1996 2 16 UPS205488 1 19960208 A 5751 FITTING BOEING 727 72725C 138400H NM AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION R/W AILERON O/B HINGE FITTING. REPLACED FITTING PER SRM 51-30-2 AN D 51-10-1. 2 L 7 3 4F A3WE 1996021600743 19960216 00743 NM 1996 2 16 UPS205489 1 19960209 A 5751 HINGE ARM BOEING 727 72725C 138400H NM RT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION R/W I/B AILERON HINGE ARM. REPLACED HINGE PER UPS MM 27-10-01. 2 L 7 3 4F A3WE 1996021600744 19960216 00744 NM 1996 2 16 UPS205490 1 19960210 A 5347 SEAT TRACK BOEING 727 72725C 138400H NM BS 360-520 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION ON SEAT TRACK STA 360-520, RBL 60, WL 208. REPLACED SEAT TRACK PER SRM 51-10-6, 53-10-5, AND 51-30-2. 2 L 7 3 4F A3WE 1996021600745 19960216 00745 NM 1996 2 16 UPS205491 1 19960208 A 5347 SEAT TRACK BOEING 727 72725C 138400H NM BS 760-848 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON SEAT TRACK STA 760-848, RBL 60, WL 208. REPLACED SEAT TRACK PER SRM 51-10-6, 53-10-5, AND 51-30-2. 2 L 7 3 4F A3WE 1996021600746 19960216 00746 NM 1996 2 16 UPS205492 1 19960209 A 5315 FLOOR BEAM BOEING 727 72725C 138400H NM BS 312 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON FLOOR BEAM STA 312, LBL 48, BL ZERO, WL 208, AROUND NUTPLATE HOL ES. REPLACED FLOORBEAM PER SRM 53-10-8. 2 L 7 3 4F A3WE 1996021600747 19960216 00747 NM 1996 2 16 UPS205493 1 19960209 A 5751 FITTING BOEING 727 72725C 138400H NM LT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION LT O/B AILERON HINGE FITTING. REPLACED FITTING PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996021600748 19960216 00748 NM 1996 2 16 UPS205494 1 19960209 A 5751 FITTING BOEING 727 72725C 138400H NM LT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION LT O/B AILERON HINGE FITTING. REPLACED FITTING PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996021600749 19960216 00749 NM 1996 2 16 UPS205495 1 19960209 A 5751 FITTING BOEING 727 72725C 138400H NM LT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION LT O/B AILERON HINGE FITTING. REPLACED FITTING PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996021600750 19960216 00750 NM 1996 2 16 UPS205496 1 19960209 A 5752 FITTING BOEING 727 72725C 138400H NM LT AILERON TAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION LT O/B AILERON TAB FITTINGS, TAB SIDE. REPLACED FITTINGS PER SRM 5 1-30-2. 2 L 7 3 4F A3WE 1996021600751 19960216 00751 NM 1996 2 16 UPS205497 1 19960208 A 5311 FRAME BOEING 727 72725C 138400H NM BS 284.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C CHECK, MAINTENANCE REPORTED FRAME CRACKED AT BS 284.5 AT STR 24R, RBL 20. REPAIRED PER SRM 51-30-2 AND 5 3-10-2. 2 L 7 3 4F A3WE 1996021600752 19960216 00752 NM 1996 2 16 UPS205498 1 19960209 A 5320 INTERCOSTAL BOEING 727 72725C 138400H NM FS 211-219 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION ON INTERCOSTAL STA 211-219, RBL 25, WL 174. REPLACED INTERCOSTAL P ER SRM 53-10-1, 51- 20-1, AND 51-10-22. 2 L 7 3 4F A3WE 1996021600753 19960216 00753 NM 1996 2 16 UPS205499 1 19960209 A 5320 STIFFENERS BOEING 727 72725C 138400H NM BS 203 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION ON STIFFENERS AT STA 203, LBL 18 AND 22, WL 180. REPLACED STIFFENE RS PER SRM 51-40-4. 2 L 7 3 4F A3WE 1996021600754 19960216 00754 NM 1996 2 16 UPS205501 1 19960202 A 5755 SPOILER BOEING 727 72725C 138400H NM NR 3 SPOILER WATER ENTRAPMENT A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C CHECK, MAINTENANCE REPORTED POSSIBLE WATER ENTRAPMENT IN VIEW X-RAY NR 3 SPOILER. REPAIRED PER SRM 51-40 -6. 2 L 7 3 4F A3WE 1996021600755 19960216 00755 NM 1996 2 16 UPS205502 1 19960201 A 5755 SPOILER BOEING 727 72725C 138400H NM NR 7 SPOILER WATER ENTRAPMENT A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C CHECK, MAINTENANCE REPORTED POSSIBLE WATER ENTRAPMENT IN VIEW 5 X-RAY NR 7 SPOILER. REPAIRED PER SRM 51- 40-6. 2 L 7 3 4F A3WE 1996021600756 19960216 00756 NM 1996 2 16 UPS205503 1 19960210 A 5347 SEAT TRACK BOEING 727 72725C 138400H NM BS 344-360 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C CHECK, MAINTENANCE REPORTED CORROSION ON SEAT TRACK FLANGE AROUND NUTPLATE HOLES AT STA 344-360, LBL 65, WL 208. REPAIRED PER SRM 53-10-1, 51-10-6, 51-30-2, 51-10-2, AND OHM 20-41-02. 2 L 7 3 4F A3WE 1996021600757 19960216 00757 NM 1996 2 16 UPS205504 1 19960201 A 5755 SPOILER BOEING 727 72725C 138400H NM NR 9 SPOILER WATER ENTRAPMENT A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C CHECK, MAINTENANCE REPORTED POSSIBLE WATER ENTRAPMENT IN VIEW 8 OF X-RAY OF SPOILER NR 9. REPAIRED PER S RM 57-50-6. 2 L 7 3 4F A3WE 1996021600758 19960216 00758 NM 1996 2 16 UPS205505 1 19960201 A 5755 SPOILER BOEING 727 72725C 138400H NM NR 14 SPOILER WATER ENTRAPMENT A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C CHECK, MAINTENANCE REPORTED POSSIBLE WATER ENTRAPMENT IN VIEW 6 OF X-RAY OF SPOILER NR 14. REPAIRED PER SRM 57-50-6. 2 L 7 3 4F A3WE 1996021600759 19960216 00759 NM 1996 2 16 UPS205506 1 19960201 A 5755 SPOILER BOEING 727 72725C 138400H NM NR 14 SPOILER WATER ENTRAPMENT A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C CHECK, MAINTENANCE REPORTED POSSIBLE WATER ENTRAPMENT IN VIEW 4 OF X-RAY OF SPOILER NR 14. REPAIRED PER SRM 57-50-6. 2 L 7 3 4F A3WE 1996021600760 19960216 00760 NM 1996 2 16 UPS205507 1 19960201 A 5755 SPOILER BOEING 727 72725C 138400H NM NR 14 SPOILER WATER ENTRAPMENT A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C CHECK, MAINTENANCE REPORTED POSSIBLE WATER ENTRAPMENT IN VIEW 5 OF X-RAY OF SPOILER NR 14. REPAIRED PER SRM 57-50-6. 2 L 7 3 4F A3WE 1996021600761 19960216 00761 NM 1996 2 16 UPS405456 1 19960213 A 3350 S13560A BATTERY PACK BOEING 747 747SR46 NM UPPER DECK DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 680UP 20923 MAINTENANCE REPORTED EMERGENCY AISLE EXIT LIGHT INOP UPPER DECK RT SIDE. REMOVED AND REPLACED BATT. PACK. OP CK GOOD. 2 L 7 4 4F A20WE 1996021600762 19960216 00762 NM 1996 2 16 UPS405457 1 19960213 A 5320 SHEAR TIE BOEING 747 747121 1384871 NM BS 2140 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN AMS FOR C CHECK, MAINTENANCE REPORTED CRACKED SHEAR TIE AT B.S. 2140, STR. 49-50 LT. REPAIRED CRACK PER SRM 53 -10-04,, FIG. 1. 2 L 7 4 4F A20WE 1996021600763 19960216 00763 NM 1996 2 16 UPS405458 1 19960209 A 5311 FRAME WEB BOEING 747 747121 1384871 NM BS 1840 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN AMS FOR C CHECK, MAINTENANCE REPORTED CRACKED FRAME WEB UNDER UPPER CHORD AT B.S. 1840 LBL 6. REPAIRED WEB PER SRM 51-40-02. 2 L 7 4 4F A20WE 1996021600764 19960216 00764 NM 1996 2 16 UPS405459 1 19960201 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1740 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN AMS FOR C CHECK, MAINTENANCE REPORTED THEY FOUND CORROSION ON STRINGER-END UNDER STRINGER SPLICE AT BS 1740 S45 R. CORROSION REMOVED PER SRM 51-10-01. REPLACED STRINGER PER SRM 51-30-02. 2 L 7 4 4F A20WE 1996021600765 19960216 00765 NM 1996 2 16 UPS405460 1 19960201 A 5312 BULKHEAD BOEING 747 747121 1384871 NM BS 2160 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN AMS FOR C CHECK, MAINTENANCE REPORTED BULK CARGO COMP. T-CHORD ON BULKHEAD FOR CARGO FLOOR STRUCTURE IS CORRODE D AND CRACKED ON HORIZ. FLANGE AT STA 2160, RBL 2, 23, AND 29. REPLACED UPPER CHORD PER SRM 51-30-02. 2 L 7 4 4F A20WE 1996021600766 19960216 00766 NM 1996 2 16 UPS405461 1 19960213 A 5320 SHEAR TIE BOEING 747 747121 1384871 NM BS 2080 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN AMS FOR C CHECK, MAINTENANCE REPORTED 3 CRACKED SHEAR TIES IN BULK CARGO COMP. AT BS 2080 BETWEEN STR 50 TO 48 LBL AND RBL BETWEEN STR 49-50. REPAIRED PER SRM 53-10-04, FIG. 41. 2 L 7 4 4F A20WE 1996021600767 19960216 00767 NM 1996 2 16 UPS405462 1 19960131 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 460-480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN AMS FOR C CHECK, MAINTENANCE REPORTED FWD. CARGO COMP. STR. 39 RT BETWEEN STA 460-480, STRINGER IS CRACKED. RE PAIRED PER SRM 53-10-03, FIG. 3. 2 L 7 4 4F A20WE 1996021600768 19960216 00768 NM 1996 2 16 UPS405463 1 19960214 A 5751 FITTING BOEING 747 747121 1384871 NM LT AILERON ELONGATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN AMS FOR C CHECK, MAINTENANCE REPORTED LT WING O/B AILERON ATTACH FITTINGS HAVE ELONGATED HOLES AT W/S 1308, 142 3, 1485, AND 1548. REPLACED FITTINGS PER SRM 51-30-02. 2 L 7 4 4F A20WE 1996021600769 19960216 00769 NM 1996 2 16 UPS605464 1 19960213 A 4930 APU BOEING 767 76734AF 1385212 NM APU DRAIN MAST FUEL LEAK A IPXA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 305UP 27243 MAINTENANCE REPORTED FUEL RUNNING OUT OF THE DRAIN MAST APU RUNNING. PLACARD PER MEL 49-11-1. 2 L 7 2 4F RT A1NM 1996021600770 19960216 00770 WP 1996 2 16 UPS805465 1 19960105 A 5320 CUSP FITTING DOUG DC8 DC871F 302199D WP FS 1580 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON CUSP FITTING FS 1580 LONGERON 21R. REPLACED FITTING PER S RM 51-3-0. 2 L 7 4 4F RT 4A25 1996021600771 19960216 00771 WP 1996 2 16 UPS805466 1 19960105 A 5311 BELT FRAME DOUG DC8 DC871F 302199D WP FS 200 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON BELT FRAME LWR. LIP. LONGERON 36, FS 200. REPAIRED FRAME PER SRM 53-2-0 AND 51-1-20D. 2 L 7 4 4F RT 4A25 1996021600772 19960216 00772 WP 1996 2 16 UPS805467 1 19960106 A 5320 DOUBLER DOUG DC8 DC871F 302199D WP FS 620 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON INNER DOUBLER, FS 620 LONGERON 35R. REPAIRED PER UPS E.O. 2 L 7 4 4F RT 4A25 1996021600773 19960216 00773 WP 1996 2 16 UPS805468 1 19960104 A 5320 FITTING DOUG DC8 DC871F 302199D WP FS 70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON END FITTING FS 70 LONGERON 30L. REPLACED END FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996021600774 19960216 00774 WP 1996 2 16 UPS805469 1 19960103 A 5320 SHEAR TIE DOUG DC8 DC871F 302199D WP FS 1060 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON SHEAR TIE, FS 1060 LONGERON 35R - 36R. REPLACED SHEAR TIE PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996021600775 19960216 00775 WP 1996 2 16 UPS805470 1 19960108 A 5320 WEB DOUG DC8 DC871F 302199D WP FS 70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C CHECK, MAINTENANCE REPORTED MODERATE CORROSION LWR. SIDE WEB FS 70 LONGERON 21R. REPAIRED WEB PER SRM 53 -2-0. 2 L 7 4 4F RT 4A25 1996021600776 19960216 00776 WP 1996 2 16 UPS805471 1 19960115 A 5320 DOUBLER DOUG DC8 DC871F 302199D WP FS 220-260 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION INNER DOUBLER FS 220-260 LONGERON 35L-31R. REPLACED DOUBLER PER SRM 51-1-20D AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1996021600777 19960216 00777 WP 1996 2 16 UPS805472 1 19960115 A 5330 SKIN DOUG DC8 DC871F 302199D WP FS 190-450 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION AT FUSE. SKIN FS 190-450. REPLACED SKIN PER DAC DRAWING NR 5 755271. 2 L 7 4 4F RT 4A25 1996021600778 19960216 00778 WP 1996 2 16 UPS805473 1 19960104 A 5320 FITTING DOUG DC8 DC871F 302199D WP FS 1220/1175 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C CHECK, MAINTENANCE REPORTED 2 EACH FITTINGS HAVE HEAVY CORROSION AT FS 1220 LONGERON 35R, AND FS 1175 LON GERON 33R. REPLACED FITTINGS PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996021600779 19960216 00779 WP 1996 2 16 UPS805474 1 19960103 A 5320 FITTING DOUG DC8 DC871F 302199D WP FS 1150 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION AND CRACKED FITTINGS, FS 1150 LONGERON 34R-33R. REPLACED FIT TINGS PER SRM 51-1-20D AND 51-1-8. 2 L 7 4 4F RT 4A25 1996021600780 19960216 00780 WP 1996 2 16 UPS805475 1 19960104 A 5320 DOUBLER DOUG DC8 DC871F 302199D WP FS 1050-1350 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON INNER DOUBLER FS 1050-1350 LONGERON 31L-31R. REPLACED DOU BLER PER SRM 50-2-0 AND 51-1-20D AND UPS E.O. 2 L 7 4 4F RT 4A25 1996021600781 19960216 00781 WP 1996 2 16 UPS805476 1 19960103 A 5311 BOLT FRAME DOUG DC8 DC871F 302199D WP FS 1120 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION UPPER FLANGE BOLT FRAME, FS 1120 LONGERON 36. REPAIRED PER S RM 53-2-0. 2 L 7 4 4F RT 4A25 1996021600782 19960216 00782 WP 1996 2 16 UPS805477 1 19960103 A 5311 FRAME DOUG DC8 DC871F 302199D WP FS 1140 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION UPPER FLANGE OF FRAME FS 1140 LONGERON 34L-35L. REPAIRED PER UPS E.O. 2 L 7 4 4F RT 4A25 1996021600783 19960216 00783 WP 1996 2 16 UPS805478 1 19960102 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FS 1018 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION LONGERON 35R, FS 1018. REPLACED SECTION PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996021600784 19960216 00784 WP 1996 2 16 UPS805479 1 19960102 A 5311 FRAME DOUG DC8 DC871F 302199D WP FS 1280 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON BELT FRAME FS 1280 LONGERON 22R. REPAIRED FRAME PER SRM 5 3-2-0, FIG. 2 2 L 7 4 4F RT 4A25 1996021600785 19960216 00785 WP 1996 2 16 UPS805480 1 19960102 A 5312 BLKHD CAP DOUG DC8 DC871F 302199D WP FS 980 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON BULKHEAD CAP FS 980 LONGERON 34R-35R. REPAIRED PER UPS E. O. 2 L 7 4 4F RT 4A25 1996021600786 19960216 00786 WP 1996 2 16 UPS805481 1 19960102 A 5315 FLOOR BEAM DOUG DC8 DC871F 302199D WP FS 55 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 WHILE IN FOR C CHECK, MAINTENANCE REPORTED EXFOLIATION CORROSION ON UPPER FLANGE OF FLOOR BEAM, FS 55 RBL 45. REPAIRED PER UPS E.O. 2 L 7 4 4F RT 4A25 1996022300002 19960223 00002 NE 1996 2 23 96ZZZX709 2 19960102 A 7230 COMPRESSOR BOEING 767 7673Y0 NM PWA 4060 PW4060 52119 NE LT ENGINE DAMAGED A TWAA O OTHER R PARTIAL RPM/PWR LOSS CL CLIMB 1 CE 05 632TW 24953 JFK - FLT 880 - AFTER TAKEOFF, LT ENGINE S/N 4703 SURGED WITH ACCOMPANYING COMPRESSOR STALL AND HIGH EGT. REDUCED POWER TO IDLE. FOUND HIGH PRESSURE COMPRESSOR DETERIORATION. ENGINE TOTAL TIME: 10,716 HOURS, 2,083 CYCLES. INVESTIGATION REVEALED INCREASED BLADE TIP CLEARANCE TO THE STATOR RUB STRIPS IN THE HIGH PRESSURE COMPRESSOR. THE HIGH RPESSURE COM PRESSOR MODULE WAS REPAIRED AND ENGINE S/N 4703 WAS RETURNED TO SERVICE. (X) 2 L 7 2 4F 4 F RT A1NM E24NE 1996022300014 19960223 00014 SO 1996 2 23 96ZZZX721 2 19960125 A 8540 539800 CLUTCH SPRING L42085A4 CESSNA 402 402A 207590M CE CONT O520 TSIO520E 17040 SO STARTER/ADAPTER FAILED A VUMA O OTHER K FLUID LOSS CR CRUISE 1 WP 13 7816Q 26 76307 401A0116 183356 DURING CRUISE, PILOT NOTICED OIL COMING OUT OF THE TURBOCHARGER VENT AND ENGINE COWLING ON THE RIGHT ENGINE. THE STARTE R/ADAPTER SPRING CLUTCH WAS FOUND TO HAVE APPARENTLY FAILED AND AT LEAST ONE PIECE OF THE SPRING CAME INTO CONTINUOUS CO NTACT WITH THE STARTER SHAFT GEAR ASSY CAUSING STARTER SHAFT GEAR TO FAIL. 1 L 7 2 3O 3 O A7CE E8CE 1996022300025 19960223 00025 NM 1996 2 23 9603815514 1 19960125 A 5315 CHORD BOEING 757 757251 1384970 NM FS 345 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 514US 23202 DURING PERIODIC CHECK, FOUND CORROSION ON THE BS 345 FLOORBEAM UPPER CHORD FROM LBL 8 TO BL 0. REPAIRED CHORD PER EA 55 -13905. 2 L 7 2 4F RT A2NM 1996022300026 19960223 00026 WP 1996 2 23 9603829102 1 19960202 A 5320 FITTINGS DOUG DC9 DC915 3022036 WP FS 642 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 92S 47064 DURING H-CHECK, FOUND CORROSION ON THE FS 642 T-CAP END FITTINGS IN BOTH THE LEFT AND RIGHT MAIN LANDING GEAR WHEEL WELL KEEL. REPLACED BOTH FITTINGS PER SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 1996022300027 19960223 00027 WP 1996 2 23 9603839997 1 19960207 A 5313 LONGERON DOUG DC9 DC931 3022065 WP FS 155 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8933E 47142 DURING SPECIAL MAINTENANCE VISIT, FOUND CRACKS IN THE LONGERON 10R AND 11R END FITTINGS AT FS 155. REPAIRED BOTH PER SR M 53-05 FIG 100. 2 L 7 2 4F A6WE 1996022300028 19960223 00028 WP 1996 2 23 9603849762 1 19960207 A 5320 FITTING DOUG DC9 DC941 302207N WP AFT OF LAV DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 762NW 47395 DURING H-CHECK, FOUND A CRACK IN THE HORIZONTAL FITTING JUST AFT OF THE LEFT LAVATORY LOWER DOOR LATCH ROLLER. REPLACED FITTING PER SRM 51-30-2. 2 L 7 2 4F A6WE 1996022300029 19960223 00029 WP 1996 2 23 9603859605 1 19960209 A 5320 FITTING DOUG DC9 DC932 3022066 WP FS 996 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 605NW 47223 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LONGERON 19L END FITTING AT FS 996. REPLACED FITTI NG PER SRM 51-01. 2 L 7 2 4F A6WE 1996022300030 19960223 00030 WP 1996 2 23 9603869605 1 19960209 A 5320 FITTING DOUG DC9 DC932 3022066 WP FS 863 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 605NW 47223 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LONGERON 22L SPLICE AT FS 863. REPLACED SPLICE FIT TING PER SRM 51-01. 2 L 7 2 4F A6WE 1996022300031 19960223 00031 WP 1996 2 23 9603879152 1 19960209 A 5320 FITTING DOUG DC9 DC914 3022034 WP FS 470 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8911E 45825 DURING H-CHECK, FOUND A CRACK IN THE LONGERON 28R END FITTING AT FS 470. REPLACED FITTING PER SRM 51-30-2. 2 L 7 2 4F A6WE 1996022300032 19960223 00032 WP 1996 2 23 9603889762 1 19960210 A 5320 FITTING DOUG DC9 DC941 302207N WP FS 1072 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 762NW 47395 DURING H-CHECK, FOUND CORROSION ON THE FS 1072 FLOOR FITTING RIGHT LAV SIDE. REPLACED FITTING PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996022300033 19960223 00033 EU 1996 2 23 9603893241 1 19960214 A 3350 321454 BATTERY PACK AIRBUS 320 A320211 3930320 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 341NW 19119 6185 380 DURING LINE MAINTENANCE, THE EMERGENCY LIGHTS TEST FAULTED THE RIGHT EPSU. REPLACED EPSU AND BATTERY PACK AND OPERATION AL CHECK OK. 2 L 7 2 4F RT A28NM 1996022300034 19960223 00034 NM 1996 2 23 9603906304 1 19960215 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 664US 23819 DURING LINE CHECK, THE FLOOR AMOUNTED EMERGENCY PATH LIGHTS AFT OF DOOR 4L WERE FOUND INOPERATIVE. REPAIRED BROKEN WIRE AND OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996022300035 19960223 00035 WP 1996 2 23 9603919606 1 19960212 A 5320 FITTING DOUG DC9 DC932 3022066 WP FS 996 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 606NW 47225 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE LONGERON 28R END FITTING AT FS 996. REPLACED FITTING PER SRM 51-01. 2 L 7 2 4F A6WE 1996022300036 19960223 00036 WP 1996 2 23 9603929606 1 19960213 A 5320 FITTING DOUG DC9 DC932 3022066 WP FS 579-604 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 606NW 47225 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE LONGERON 29L END FITTING AT FS 579 TO 604. REPLACE D FITTING PER SRM 51-01, 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1996022300037 19960223 00037 WP 1996 2 23 9603939152 1 19960213 A 5320 FITTING DOUG DC9 DC914 3022034 WP FS 484 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8911E 45825 DURING H-CHECK, FOUND CORROSION ON THE INTERCOSTAL END FITTING LOCATED IN THE FORWARD CARGO BIN FS 484 OUTBOARD OF LONGE RON 28R. REPLACED FITTING PER SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1996022300038 19960223 00038 NE 1996 2 23 9603941162 2 19960214 A 7261 SEAL DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 2 ENGINE LEAKING A NWAA E ENGINE SHUTDOWN J K WARNING INDICATION FLUID LOSS DE DESCENT 1 GL 01 162US 46771 86168 DURING DESCENT, THE NR 2 ENGINE WAS SHUTDOWN DUE TO OIL PRESSURE DROPPING BELOW 35 PSI AND OIL QUANTITY DROPPING TO 1 GA LLON. CREW FOLLOWED COCKPIT OPERATING PROCEDURE AND CONTINUED FLIGHT TO HNL WITHOUT FURTHER INCIDENT. REPLACED THE RIG HT GARLOCK SEAL THAT WAS LEAKING. ALSO, REPLACED THE BROKEN O-RING ON INPUT SHAFT. RAN THE NR 2 ENGINE AT TAKEOFF POWE R AND NO LEAK WAS DETECTED. 2 L 7 3 4F 4 F A22WE E20EA 1996022300039 19960223 00039 WP 1996 2 23 9603959914 1 19960212 A 2910 HYD LINE DOUG DC9 DC931 3022065 WP CARGO COMPT LEAKING A NWAA L ABORTED APPROACH J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 GL 01 964N 47416 DURING FINAL APPROACH, FLAP POSITION INDICATED 25 DEGREES AND NEVER MOVED WHEN FLAPS WERE SELECTED TO 40 DEGREES. EXECU TED GO-AROUND AND FLAPS MOVED SLOWLY, BUT DID ACHIEVE 40 DEGREES ON SECOND ATTEMPT AND A SUCCESSFUL LANDING WAS ACCOMPLI SHED. MAINTENANCE FOUND HYDRAULIC LINE IN FORWARD CARGO AREA LEAKING THROUGH PIN HOLE. REPLACED LINE AND THE LEAK AND OPERATIONAL CHECK OF FLAP SYSTEM WAS NORMAL. 2 L 7 2 4F A6WE 1996022300041 19960223 00041 WP 1996 2 23 9603979989 1 19960217 A 4990 OIL SYST DOUG DC9 DC931 3022065 WP APU REQD SERVICE A NWAA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 GL 01 8945E 47181 PREVIOUS TO DEPARTURE, ENGINE NR 2 GENERATOR PLACED ON MEL AND APU WAS USED FOR GENERATOR POWER. DURING CRUISE FLIGHT, THE APU LOW OIL LIGHT ILLUMINATED AND SHORTLY THERE AFTER, THE APU AUTO SHUTDOWN. CAPTAIN DECLARED AN EMERGENCY AND DIV ERTED TO FAR. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL SERVICED APU WITH OIL, GROUND RUN AND LEAK CHECK ED, NO LEAK NOTICED. 2 L 7 2 4F A6WE 1996022300042 19960223 00042 WP 1996 2 23 9603989755 1 19960216 A 2450 BUS CONTL PNL DOUG DC9 DC941 302207N WP COCKPIT MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 755NW 47179 ON TAKEOFF ROLL, MASTER CAUTION ILLUMINATED AND SEVERAL LIGHTS STARTED BLINKING. TAKEOFF WAS ABORTED AND RETURNED TO TH E GATE. INSPECTED CROSSTIE RELAY, LEFT AND RIGHT GENERATOR RELAYS AND NO DEFECTS FOUND. REPLACED THE LEFT GENERATOR CO NTROL PANEL AND VOLTAGE REGULATOR. REPLACED BUS CONTROL PANEL AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996022300043 19960223 00043 WP 1996 2 23 9603999963 1 19960215 A 3241 ANTI-SKID DOUG DC9 DC931 3022065 WP LT MLG MALFUNCTIONED A NWAA O OTHER O OTHER LD LANDING 1 GL 01 913RW 47171 BOTH THE LEFT MAIN GEAR TIRES BLEW ON LANDING INTO GRR. AIRCRAFT REMAINED ON RUNWAY AND PASSENGERS WERE DEPLANED VIA ST AIRS. AIRCRAFT WAS TOWED TO THE GATE WITH BOTH TIRES FLAT. MAINTENANCE REPLACED BOTH LEFT MAIN ANTI-SKID VALVES, ALL F OUR ANTI-SKID TRANSDUCERS, NR 1 AND NR 2 BRAKE AND WHEEL ASSEMBLIES AND ANTI-SKID CONTROL BOX, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996022300044 19960223 00044 WP 1996 2 23 9604009994 1 19960216 A 3350 6011779 BATTERY PACK DOUG DC9 DC931 3022065 WP LT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8979E 47328 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AND OPERATION AL CHECK NORMAL. 2 L 7 2 4F A6WE 1996022300045 19960223 00045 WP 1996 2 23 9604019944 1 19960218 A 3350 6011779 BATTERY PACK DOUG DC9 DC931 3022065 WP LT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 1309T 47316 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AND OPERATION AL CHECK NORMAL. 2 L 7 2 4F A6WE 1996022300046 19960223 00046 WP 1996 2 23 9604029974 1 19960217 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9338 47347 DURING PERIODIC CHECK, FOUND AFT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996022300047 19960223 00047 WP 1996 2 23 9604039940 1 19960216 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 3322L 47031 DURING LINE MAINTENANCE INSPECTION, FOUND AFT CEILING EMERGENCY LIGHTS DIM. REPLACED BATTERIES AND OPERATIONAL CHECK NO RMAL. 2 L 7 2 4F A6WE 1996022300048 19960223 00048 WP 1996 2 23 9604049923 1 19960217 A 3350 60030451 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 927RC 47469 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN SECTION OF OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATT ERY PACK AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996022300049 19960223 00049 NM 1996 2 23 96FDEA00255 1 19960215 A 3231 RETRACT MECH BOEING 727 7272S2F 1384O81 NM NLG DOORS MALFUNCTIONED A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 211FE 22933 NOSE GEAR DOOR WARNING LIGHT ON SECOND OFFICER'S PANEL AND RED DOOR WARNING LIGHT ON FRONT PANEL REMAINED ON AFTER GEAR RETRACTION. THE ABNORMAL PROCEDURE WAS ATTEMPTED. DURING RECYCLE, DOORS OPERATED NORMAL BUT LIGHT REMAINED ON DURING R ETRACTION. ALSO, LOUD RUMBLING NOISE LIKE DOORS WERE OPEN WAS EVIDENT THROUGHOUT FLIGHT. REPEAT WRITE-UP, DEFERRED LIG HT PER MEL 32-1 EXP 2-25-95 CAT C CONT NR 0215039, NOSE GEAR DOOR WARNING SYSTEM INOP. NOSE STRUT WAS FOUND FLAT AGAIN AFTER RESERVICING STRUT. RECHECKED NOSE GEAR DOORS PER MM 32-21, NO DEFECTS NOTED. SWUNG GEAR SEVERAL TIMES WITH NO DE FECTS. 2 L 7 3 4F A3WE 1996022300050 19960223 00050 NM 1996 2 23 96FDEA00256 1 19960216 A 5314 65184071 KEEL BEAM BOEING 727 72722 1384002 NM BS 1030-1050 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 EXTERIOR SKIN, BULGE IN SKIN AT KEEL BEAM STR 29L BS 1050 TO 1030. REMOVED CORROSION ON KEEL BEAM BS 1030 TO 1050 STR 29L, FOUND TO BE OUT LIMITS PER FEDEX SRM 53-10-1. REMOVED FRAMES BS 970, 990, 1010, 1050, 1070 AND 1030. REMOVED KEEL BEAM, INSTALLED NEW KEEL BEAMS AND REINSTALLED FRAMES BS 970, 990, 1010, 1050, 1070 AND 1030 IAW FEDEX EO 7-5310-7-2356 0 PART 1 AND 7-5310-7-23560 PART 6. 2 L 7 3 4F A3WE 1996022300051 19960223 00051 NM 1996 2 23 96FDEA00257 1 19960216 A 5311 65C100844 FRAME BOEING 727 72722 1384002 NM BS 930 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CRACK AND MULTIPLE STOP DRILLS ON UNDERSIDE OF FRAME AT BS 930 BETWEEN STR 15 TO 14R. REPAIRED CRACK AND MULTIPLE STOP DRILLS ON UNDERSIDE OF FRAME AT BS 930, BETWEEN STR 15 TO 14R IAW FEDEX EA 7-5310-27450. 2 L 7 3 4F A3WE 1996022300052 19960223 00052 NM 1996 2 23 96FDEA00258 1 19960216 A 5320 FRAME SPLICE BOEING 727 72722 1384002 NM BS 1010 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 FRAME SPLICE DAMAGE AT BS 1010 RT WL 157 RBL 41 BETWEEN STR 24 TO 25R. REMOVED DAMAGED FRAME SPLICE AT BS 1010 RT WL 15 7 RBL 14. FABRICATED NEW FRAME SPLICE AND INSTALLED. 2 L 7 3 4F A3WE 1996022300053 19960223 00053 NM 1996 2 23 96FDEA00259 1 19960213 A 5753 652163254 TIE WEDGE BOEING 727 72722 1384002 NM RT TE MIDFLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 RT WING I/B MIDFLAP TIE WEDGE HAS AN AREA OF DELAMINATION ON O/B END 12 INCHES BY 3 INCHES. REPAIRED DELAMINATION PER S RM 51-40-6. 2 L 7 3 4F A3WE 1996022300054 19960223 00054 NM 1996 2 23 96FDEA00260 1 19960216 A 5320 65453132 STRINGER CLIP BOEING 727 72722 1384002 NM BS 420 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 DAMAGED STR CLIP BS 420 STR NR 4 LT. REMOVED AND REPLACED DAMAGED STR CLIP AT BS 420 STR 4 LT. 2 L 7 3 4F A3WE 1996022300055 19960223 00055 NM 1996 2 23 96FDEA00261 1 19960213 A 5311 FRAME BOEING 727 72722 1384002 NM BS 1010 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 DENT IN FRAME AT BS 1010 LBL 39 WL 153. FABRICATED PART AND REPAIRED FROM PER SRM 51-40-03. 2 L 7 3 4F A3WE 1996022300056 19960223 00056 NM 1996 2 23 96FDEA00262 1 19960216 A 5311 FRAME BOEING 727 72722 1384002 NM BS 1090 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 DENT IN FRAME BS 1090 BETWEEN STR 23 TO 24L LBL 47 WL 169. REMOVED DAMAGE, FABRICATED REPAIR ANGLE AND INSTALLED PER SR M 51-40-3. 2 L 7 3 4F A3WE 1996022300057 19960223 00057 NM 1996 2 23 96FDEA00263 1 19960216 A 5751 TE WEDGE BOEING 727 72722 1384002 NM LT AILERON DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 LT WING O/B AILERON T/E WEDGE HAS AN AREA OF DELAMINATION ON I/B LOWER SURFACE 6 INCHES BY 4 INCHES. REPAIRED LT WING O /B AILERON T/E WEDGE PER FEDEX SRM 51-80-04 SRM 51-40-06. 2 L 7 3 4F A3WE 1996022300058 19960223 00058 NM 1996 2 23 96FDEA00264 1 19960216 A 5753 SKIN BOEING 727 72722 1384002 NM LT TE AFT FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 LT WING O/B AFT FLAP HAS A 6 INCH BY 3 INCH DELAMINATED DENT ON LOWER SURFACE 30 INCHES FROM I/B END. REPAIRED DELAMINA TION PER SRM 51-40-6. 2 L 7 3 4F A3WE 1996022300059 19960223 00059 NM 1996 2 23 96FDEA00265 1 19960216 A 5330 SKIN BOEING 727 72722 1384002 NM BS 688 GOUGE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 GOUGE IN SKIN AT STA 688 RBL 30 BETWEEN STR 24 AND 25R. REPAIRED GOUGE IN SKIN AT STA 688 RBL 30 BETWEEN STR 24 AND 25R IAW FEDEX SRM 53-30-3, 53-30-1. 2 L 7 3 4F A3WE 1996022300060 19960223 00060 NM 1996 2 23 96FDEA00267 1 19960216 A 5754 65185338 HINGE BOEING 727 72722 1384002 NM NR 1 K-FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 FIXED L/E FITTING PER NR 1 K-FLAP CENTER LUG IS CORRODED. REPAIRED CENTER HINGE FITTING WITH NEW. 2 L 7 3 4F A3WE 1996022300061 19960223 00061 NM 1996 2 23 96FDEA00268 1 19960216 A 5330 SKIN BOEING 727 72722 1384002 NM BS 1108 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 EXTERIOR SKIN BULGE AND RIVET HEAD DISHED AT BS 1108, 4.5 INCHES UP FROM BOTTOM OF SKIN LAP STR 26R, AT AFT CARGO DOOR C UTOUT LOWER AFT CORNER. REPAIRED DAMAGED SKIN AT BS 1108 STR 26 RT SKIN LAP PER FEDEX EA 7-5330-27406. 2 L 7 3 4F A3WE 1996022300062 19960223 00062 NM 1996 2 23 96FDEA00269 1 19960216 A 5311 65207822 FRAME BOEING 727 72722 1384002 NM BS 1057.5 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CORROSION FOUND ON DOOR FRAME BS 1057.5 WL 162 RBL 25, WHILE WORKING NR0053. REMOVED AND REPLACED FRAME IAW DRAWING 65- 20728. 2 L 7 3 4F A3WE 1996022300063 19960223 00063 NM 1996 2 23 96FDEA00270 1 19960216 A 5320 SHEAR TIE BOEING 727 72722 1384002 NM BS 1030 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CORROSION ON BOTTOM SIDE OF SHEAR TIE BS 1030 LBL 17 TO 22, FOUND WHILE WORKING NR0053 WL 146. REMOVED SHEAR TIE, REMOV ED CORROSION, TREATED AND REINSTALLED IAW FEDEX SRM 53-10-1, 53-10-4. 2 L 7 3 4F A3WE 1996022300064 19960223 00064 NM 1996 2 23 96FDEA00271 1 19960209 A 5320 SHEAR TIE BOEING 727 72722 1384002 NM BS 1030 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CORROSION ON BOTTOM SIDE OF SHEAR TIE BS 1030 RBL 17 TO 22 WL 146, FOUND WHILE WORKING NR0053. REMOVED SHEAR TIE, REMOV ED CORROSION, TREATED AND REINSTALLED SHEAR TIE FEDEX SRM 53-10-1. 2 L 7 3 4F A3WE 1996022300065 19960223 00065 NM 1996 2 23 96FDEA00272 1 19960216 A 5320 SHEAR TIE BOEING 727 72722 1384002 NM BS 990 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CORROSION ON BOTTOM OF SHEAR TIE BS 990 LBL 9 TO 13 WL 146, FOUND WHILE WORKING NR0053. REPAIRED SHEAR TIE WITH DOUBLER IAW FEDEX SRM 53-10-4. 2 L 7 3 4F A3WE 1996022300066 19960223 00066 NM 1996 2 23 96FDEA00273 1 19960216 A 5320 FAIL-SAFE CHORD BOEING 727 72722 1384002 NM BS 1010 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 BS 1010 CRACKED FAIL-SAFE CHORD AT RBL 45 WL 149, FOUND WHILE WORKING NR0053. REMOVED CRACKED FAIL-SAFE CHORD, INSTALL ED NEW CHORD AND SPLICE IAW FEDEX SRM 51-40-3. 2 L 7 3 4F A3WE 1996022300067 19960223 00067 NM 1996 2 23 96FDEA00274 1 19960216 A 5320 SHEAR TIE BOEING 727 72722 1384002 NM BS 1050 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CORROSION ON BOTTOM SIDE OF SHEAR TIE BS 1050 WL 146 RBL 1 TO 6, FOUND TO BE OUT OF LIMITS WHILE WORKING NR0053. REMOV ED DAMAGED AREA AND INSTALLED REPAIR IAW FEDEX SRM 53-10-4. 2 L 7 3 4F A3WE 1996022300068 19960223 00068 NM 1996 2 23 96FDEA00275 1 19960216 A 5330 SKIN BOEING 727 72722 1384002 NM BS 1090 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 FOUND CRACK IN UPPER SKIN BS 1090 WL 140 RBL 25. REPAIRED DAMAGE SKIN BS 1090 WL 140 RBL 25 PER FEDEX EA 7-5330-27406. 2 L 7 3 4F A3WE 1996022300069 19960223 00069 NM 1996 2 23 96FDEA00283 1 19960219 A 5311 FRAME BOEING 727 72722 1384002 NM BS 1090 DOUBLE DRILLED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 193FE 19142 BS 1090 FRAME HAS A DOUBLE HOLE BETWEEN STR 8 TO 9L. REPAIRED FRAME IAW FEDEX SRM 53-10-4. 2 L 7 3 4F A3WE 1996022300070 19960223 00070 NM 1996 2 23 96FDEA00284 1 19960209 A 5330 SKIN BOEING 727 72722 1384002 NM BS 1080-1110 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION (C53-100-01-4), BS 1080 TO 1110 STR 26 LT AND RT. ALSO, DEEP GOUGES ON EXTERIOR SKIN. MECHANICALLY REMOVED C ORROSION FROM EXTERIOR SKIN, BS 1080 TO 1110 STR 26 LT AND RT. FOUND A 1.5 INCH BY 1.5 INCH AREA AT STR 27L BS 1090 TO BE OUT OF LIMITS PER FEDEX SRM 53-30-1. ALL OTHER AREAS TO BE WITHIN LIMITS. REPAIRED SKIN AT BS 1091 STR 27L PER FEDE X SRM 53-30-3. 2 L 7 3 4F A3WE 1996022300071 19960223 00071 NM 1996 2 23 96UAL900116 1 19960215 A 3260 PSEU BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LANDING GEAR FAILED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 609UA 21870 RETURNED TO LAX DUE TO FLAP CONFIGURATION MESSAGE AND WARNING HORN DURING GEAR RETRACTION. SUPPLEMENTAL DATA UPDATE: R EPLACED PSEU AS PRECAUTIONARY AND NOSE GEAR-NOT COMPRESSED SENSOR S266. 2 L 7 2 4F 4 F RT A1NM E3NE 1996022300072 19960223 00072 NM 1996 2 23 96UAL900117 1 19960215 A 3350 LIGHT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE GALLEY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7252U 21399 AFT GALLEY EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY. 2 L 7 3 4F 4 F A3WE E2EA 1996022300074 19960223 00074 NM 1996 2 23 96UAL900119 1 19960215 A 3350 BATTERY PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE DOOR 2R INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7299U 21894 EMERGENCY EXIT LIGHT ABOVE DOOR 2R AT AFT GALLEY INOPERATIVE. REPLACED BATTERIES. 2 L 7 3 4F 4 F A3WE E2EA 1996022300075 19960223 00075 WP 1996 2 23 ABXA9600190 1 19960130 A 5330 57503223 SKIN DOUG DC8 DC861 3021952 WP FS 1114 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 843AX 46017 DURING C-CHECK INSPECTION, DISCOVERED FUSELAGE SKIN CORRODED AT FUSELAGE STATION 1114 OUTBOARD OF LONGERON 36, JUST FORW ARD OF EXISTING REPAIR. REPAIRED FUSELAGE CORRODED LOWER SKIN AT FUSELAGE STATION 1114, LONGERON 34L TO 34R IAW ABX REA -D853-13488. 2 L 7 4 4F 4A25 1996022300076 19960223 00076 WP 1996 2 23 ABXA9600191 1 19960130 A 5730 5641253502 PANEL DOUG DC8 DC861 3021952 WP RT WING LE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 843AX 46017 DURING C-CHECK INSPECTION, DISCOVERED RIGHT WING LEADING EDGE ALONG FORWARD RIB CORRODED AND SKIN PULLING UP OVER RIVETS AT STATION 329 INSIDE LEADING EDGE PANEL 522B. REPAIRED RIGHT WING LEADING EDGE LOWER ACCESS PANEL 522B IAW ABX REA-D8 57-13489-MR. 2 L 7 4 4F 4A25 1996022300077 19960223 00077 WP 1996 2 23 ABXA9600192 1 19960130 A 5230 9754100121 BEAM DOUG DC8 DC861 3021952 WP CROSS-SLIDE DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 843AX 46017 DURING C-CHECK INSPECTION, DISCOVERED FORWARD CROSS-SLIDE DOOR AT NR 1 PIT LOCKING HOOK FITTING, 4TH HOOK FROM FORWARD E ND, FRAME BEAM IS CRACKED. REPAIRED BEAM AT FORWARD CROSS-SLIDE DOOR IAW ABX REA-D852-13484-MR. 2 L 7 4 4F 4A25 1996022300078 19960223 00078 WP 1996 2 23 ABXA9600193 1 19960130 A 5720 3648747 DOUBLER DOUG DC8 DC861 3021952 WP WS 845 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 843AX 46017 DURING C-CHECK INSPECTION, DISCOVERED RIGHT WING LEADING EDGE HAS CORROSION UNDER RETAINER RING INSIDE PANEL 517B. REPA IRED RIGHT WING OUTBOARD LEADING EDGE INTERNAL DOUBLER ACCESS PANEL 517B, AT XFS 845 IAW ABX REA-D857-13486-MR. 2 L 7 4 4F 4A25 1996022300079 19960223 00079 WP 1996 2 23 ABXA9600194 1 19960130 A 5320 5750092 TRAP FITTING DOUG DC8 DC861 3021952 WP RT MLG CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 843AX 46017 DURING C-CHECK INSPECTION, DISCOVERED RIGHT HAND TRAP FITTING HAS CRACK EXCEEDING LAST STOP DRILL. REPAIRED RIGHT MAIN LANDING GEAR SUPPORT FITTING IAW ABX REA-D853-13487-MR. 2 L 7 4 4F 4A25 1996022300080 19960223 00080 SO 1996 2 23 COMA9610084 1 19960217 A 2750 FLAP TRACKS EMB 120 EMB120RT SO TE FLAPS DIRTY A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 205CA 120205 FLAP DISAGREEMENT WARNING WHEN FLAPS RETRACTED AFTER TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. CLEANED AND INSPECTED F LAP TRACKS AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4T RT A31SO 1996022300081 19960223 00081 SO 1996 2 23 COMA9610085 1 19960216 A 7931 APT79RT110008OP OIL PRESS TRANS EMB 120 EMB120RT SO RT ENG DEFECTIVE A COMA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 1117H 9988 356 120117 RT ENGINE OIL PRESSURE INDICATES 80 PSI AT CRUISE POWER SETTING. WHEN POWER WAS REDUCED, OIL PRESSURE DECREASED TO NORM AL. REPLACED THE OIL PRESSURE TRANSDUCER. 2 L 7 2 4T RT A31SO 1996022300082 19960223 00082 SO 1996 2 23 COMA9610086 1 19960215 A 2750 3471001001 FLAP AND PANEL EMB 120 EMB120RT SO COCKPIT MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 189CA 7601 3718 120189 FLAP DISAGREEMENT WARNING WHEN FLAPS RETRACTED AFTER TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. REPLACED THE FLAP ANNUN CIATOR FOR TROUBLESHOOTING. 2 L 7 2 4T RT A31SO 1996022300083 19960223 00083 NE 1996 2 23 COMA9630039 3 19960215 A 6111 ERROSION GUARD SAAB SF340 SF340A 7850100 EU ROTOL R389 R3894123F25 NE RT PROP DEBONDING A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 357CA 340A044 180185 RT PROPELLER BLADE, ERROSION GUARD, IS DEBONDING ON BLADE NR 4. REPLACED THE PROPELLER ASSY. 2 L 7 2 4T RT A52EU 6 C P30NE 1996022300084 19960223 00084 EU 1996 2 23 COMA9630040 1 19960215 A 2612 89905201 FIRE DETECTOR SAAB SF340 SF340A 7850100 EU RT ENGINE FAILED A COMA K NONE N FALSE WARNING UK UNKNOWN 1 SO 01 356CA 340A034 INTERMITTENT RIGHT ENGINE FIRE DETECTOR FAIL WARNING. REPLACED THE FIRE DETECTION CONTROL UNIT. 2 L 7 2 4T RT A52EU 1996022300085 19960223 00085 WP 1996 2 23 MWEA96040 1 19960215 A 2560 113317 SLIDE COVER DOUG DC9 DC932 3022066 WP SERVICE DOOR FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 401ME 47133 CREW REPORTS, FWD GALLEY SERVICE DOOR SLIDE COVER FELL OFF. REINSTALLED GALLEY DOOR EVAC SLIDE COVER. 2 L 7 2 4F A6WE 1996022300086 19960223 00086 WP 1996 2 23 MWEA96041 1 19960215 A 3810 WATER SERV CAP DOUG DC9 DC932 3022066 WP FWD FUS NOT INSTALLED A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 300ME 45718 A LARGE PIECE OF ICE HAD FORMED AROUND THE FWD WATER SERVICE PANEL. REMOVED ICE AND FOUND WATER SERVICE CAP NOT PROPERL Y INSTALLED AND OVERFLOW VALVE PARTIALLY OPEN. INSPECTED FUSELAGE, NO DAMAGE. ALSO, ENGINE FOR INGESTION AND FOUND 2 C -1 BLADES WITH MINOR DENTS. BLENDED DENTS PER PRATT AND WHITNEY MM 72-00, FIG 601. 2 L 7 2 4F A6WE 1996022300087 19960223 00087 WP 1996 2 23 MWEA96042 1 19960217 A 3350 CONNECTOR DOUG DC9 DC914 3022034 WP CABIN DIRTY A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 600ME 45725 DURING INSPECTION, FOUND TWO EMERGENCY LIGHTS ABOVE AFT F/A SEAT WERE VERY DIM. CLEANED THE GROUND CONNECTION AND OPS C HECKED GOOD. 2 L 7 2 4F A6WE 1996022300088 19960223 00088 NM 1996 2 23 P5CA9600136 1 19960215 A 5753 SKIN BOEING 747 747121 1384871 NM RT TE FOREFLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 830FT 19642 FOUND RIGHT WING O/B FOREFLAP LOWER SURFACE DELAMINATED, 6 INCHES BY 6 INCHES. REMOVED DAMAGE, FABRICATED FIBERGLASS RE PAIR IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1996022300089 19960223 00089 NM 1996 2 23 P5CA9600137 1 19960215 A 5711 SPAR BOEING 747 747121 1384871 NM LT WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 830FT 19642 FOUND LEVEL ONE SURFACE CORROSION ON LEFT WING FRONT SPAR UPPER CHORD CAP LOWER SURFACE, AT FS 1395 AFT OF NR 3 LED. RE MOVED CORROSION IAW SRM 51-10-01. 2 L 7 4 4F A20WE 1996022300090 19960223 00090 NM 1996 2 23 P5CA9600138 1 19960215 A 7800 EXHAUST SLEEVE BOEING 747 747121 1384871 NM NR 2 ENGINE WORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 830FT 19642 FOUND NR 2 ENGINE EXHAUST SLEEVE OUTER SKIN LEADING EDGE WORN AT 7 O'CLOCK POSITION. REMOVED OLD DOUBLER, MANUFACTURED AND INSTALLED NEW DOUBLER IAW SRM 51-10-01. 2 L 7 4 4F A20WE 1996022300091 19960223 00091 NM 1996 2 23 P5CA9600139 1 19960215 A 7800 EXHAUST SLEEVE BOEING 747 747121 1384871 NM NR 1 ENGINE BENT A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 830FT 19642 FOUND NR 1 ENGINE EXHAUST SLEEVE INNER T/E SKIN BENT AT 8 O'CLOCK POSITION. STRAIGHTENED AS NEEDED IAW SRM 54-10-02. 2 L 7 4 4F A20WE 1996022300092 19960223 00092 NM 1996 2 23 P5CA9600140 1 19960215 A 5522 SKIN BOEING 747 747121 1384871 NM LEFT ELEVATOR DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 830FT 19642 FOUND LEFT INBOARD ELEVATOR, INBOARD T/E CORNER DELAMINATED. REPAIRED IAW SRM 51-40-12. 2 L 7 4 4F A20WE 1996022300093 19960223 00093 NM 1996 2 23 P5CA9600141 1 19960215 A 5522 SKIN BOEING 747 747121 1384871 NM LEFT ELEVATOR DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 830FT 19642 FOUND SMALL AREA OF LEFT OUTBOARD ELEVATOR T/E DELAMINATED. REPAIRED BOTH TOP AND BOTTOM ELEVATOR T/E IAW SRM 51-40-12. 2 L 7 4 4F A20WE 1996022300094 19960223 00094 NM 1996 2 23 UPS405508 1 19960202 A 5320 65B105645 SPLICE BOEING 747 747121 1384871 NM BS 1355 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED SPLICE FITTING INSIDE LEFT BLG WW ON O/W LONGERON NEARLY CRACKED IN TWO, SUSPECT CORROSION CRACK. REPLACED SPLICE ACC SRM 53-10-02. 2 L 7 4 4F A20WE 1996022300095 19960223 00095 NM 1996 2 23 UPS405509 1 19960214 A 5320 SHEAR TIE BOEING 747 747121 1384871 NM BS 2180 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED CORRODED SHEAR TIE PROFILE ON AFT SIDE OF SHEAR TIE, AT BS 2180 LBL BETWE EN STR 42 AND 43. REPLACED SHEAR TIE PROFILE ACC SRM 51-20-01 AND 51-30-02. 2 L 7 4 4F A20WE 1996022300096 19960223 00096 NM 1996 2 23 UPS405510 1 19960205 A 5320 SHEAR TIE BOEING 747 747121 1384871 NM BS 2180 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED SHEAR TIE CRACKED AT BS 2180 LBL BETWEEN 43 AND 44. REPLACED SHEAR TIE A T BS 2180 LBL ACC SRM 51-20-01 AND 51-30-02. 2 L 7 4 4F A20WE 1996022300097 19960223 00097 NM 1996 2 23 UPS405511 1 19960215 A 5320 ANGLE BOEING 747 747121 1384871 NM BS 1960 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED CRACKS IN REINFORCEMENT ANGLE IN TOP OF FRAME AT BS 1960 LBL 53. REPLACE D REINFORCEMENT ANGLE AT BS 1960 LBL 53 ACC SRM 51-20-01 AND 51-30-02. 2 L 7 4 4F A20WE 1996022300098 19960223 00098 NM 1996 2 23 UPS405512 1 19960215 A 5320 SHEAR TIES BOEING 747 747121 1384871 NM BS 2240 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED SHEAR TIES ARE CRACKED AT BS 2240 BETWEEN STR 47 AND 48 RBL AND BETWEEN S TR 47 AND 48 LBL. REPAIRED SHEAR TIES AT BS 2240 ACC SRM 53-10-04. 2 L 7 4 4F A20WE 1996022300099 19960223 00099 NM 1996 2 23 UPS405513 1 19960215 A 5311 FRAME BOEING 747 747121 1384871 NM BS 2000 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON UPPER CHORD OF FRAME AT BS 2000 RBL 45. REMOVED CORROSION F ROM UPPER CHORD OF FRAME ACC SRM 51-10-01, WITHIN LIMITS OF SRM 53-10-09. 2 L 7 4 4F A20WE 1996022300100 19960223 00100 NM 1996 2 23 UPS405514 1 19960131 A 5311 FRAME BOEING 747 747121 1384871 NM BS 1860 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED CRACK AND CORROSION ON FRAME AT BS 1860, JUST UNDER SIDE GUIDE. REMOVED DAMAGED SECTION FROM FRAME UPPER CHORD AND REPAIRED FRAME ACC TO SRM 51-40-03 FIG 1. 2 L 7 4 4F A20WE 1996022300101 19960223 00101 NM 1996 2 23 UPS405515 1 19960201 A 5311 FRAME BOEING 747 747121 1384871 NM BS 1780 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED CRACK IN OWER FRAME WEB IN BLANKET HOLE AT BS 1780, LBL 40. REMOVED DAMA GED SECTION FROM FRAME WEB AND REPAIRED WEB ACC TO SRM 51-40-02 FIG 1. 2 L 7 4 4F A20WE 1996022300102 19960223 00102 NM 1996 2 23 UPS405516 1 19960206 A 5311 FRAME BOEING 747 747121 1384871 NM BS 1900 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED CRACK IN FRAME UPPER FLANGE AT BS 1900, LBL 60 TO 63. STOP DRILLED CRACK AND REPAIRED FRAME UPPER FLANGE ACC TO SRM 51-40-03, FIG 1. 2 L 7 4 4F A20WE 1996022300103 19960223 00103 NM 1996 2 23 UPS405517 1 19960215 A 5720 CHORD BOEING 747 747121 1384871 NM WS 1520 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED RT WING L/E STRIP OF RABBET AREA IS BULGED AT WS 1520, CORROSION FOUND ON UPPER CHORD. REWORKED CORROSION ON UPPER CHORD AND REPAIRED UPPER CHORD ACC TO KLM DFX 96-034 APPROVEL PER UPS EFN 747 -57-0307. 2 L 7 4 4F A20WE 1996022300104 19960223 00104 NM 1996 2 23 UPS405518 1 19960201 A 5330 SKIN BOEING 747 747121 1384871 NM WS 1280 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN FOR C-CHECK AT AMS, MAINTENANCE REPORTED RT WING L/E LOWER SKIN AND LOWER CHORD WS 1280 FOUND CORRODED. REPAIR ED CHORD AND SKIN ACC KLM DFX 96-027R1 ISSUE NR 3 REPAIR APPROVED PER UPS EFN 747-57-0308. 2 L 7 4 4F A20WE 1996022300105 19960223 00105 NM 1996 2 23 UPS405519 1 19960202 A 5311 FRAME BOEING 747 747121 1384871 NM BS 1960 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN FOR C-CHECK AT AMS, MAINTENANCE REPORTED BULK CARGO COMPARTMENT FOUND CRACK IN WEB OF FRAME AROUND BLANKET HOLE AT BS 1960, LBL 4. REPAIRED CRACK IN WEB AT BS 1960 ACC TO SRM 51-40-02. 2 L 7 4 4F A20WE 1996022300106 19960223 00106 NM 1996 2 23 UPS405520 1 19960202 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1965 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN FOR C-CHECK AT AMS, MAINTENANCE REPORTED BULK CARGO COMPARTMENT FOUND CORRODED, STRINGER END AT BS 1965 S-49 LT UNDER STRINGER SPLICE. REMOVED CORROSION FROM STRINGER END ACC SRM 51-10-01, OUT OF LIMITS PER SRM 53-10-01. REPAIRED STRINGER PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 1996022300107 19960223 00107 NM 1996 2 23 UPS405521 1 19960201 A 5320 SHEAR TIES BOEING 747 747121 1384871 NM BS 1960 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN FOR C-CHECK AT AMS, MAINTENANCE REPORTED BULK CARGO COMPARTMENT FOUND 4 SHEAR TIES CRACKED AT BS 1960 BETWEEN S -46 50 LT. REPAIRED CRACKED SHEAR TIES AT BS 1960 ACC TO SRM 53-10-04, FIG 41. 2 L 7 4 4F A20WE 1996022300108 19960223 00108 NM 1996 2 23 UPS405522 1 19960201 A 5311 FRAME BOEING 747 747121 1384871 NM BS 1960 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN FOR C-CHECK AT AMS, MAINTENANCE REPORTED BULK CARGO COMPARTMENT FOUND CRACKED WEB AT BS 1960, RBL 2 AROUND BLAN KET ATTACHMENT HOLE. REPAIRED FRAME WEB AT BS 1960 RBL 2 AROUND BLANKET ATTACHMENT PER SRM 51-40-02. 2 L 7 4 4F A20WE 1996022300109 19960223 00109 NM 1996 2 23 UPS405523 1 19960201 A 5320 SHEAR TIE BOEING 747 747121 1384871 NM BS 1940 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN FOR C-CHECK AT AMS, MAINTENANCE REPORTED BULK CARGO COMPARTMENT SHEAR TIE CRACKED AT BS 1940 BETWEEN STR 46 TO 47 LT. REPAIRED SHEAR TIE AT BS 1640 BETWEEN STR 46 TO 47 LT ACC TO SRM 53-10-04 FIG 41. 2 L 7 4 4F A20WE 1996022300110 19960223 00110 NM 1996 2 23 UPS405524 1 19960201 A 5320 SHEAR TIE BOEING 747 747121 1384871 NM BS 2040 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN FOR C-CHECK AT AMS, MAINTENANCE REPORTED BULK CARGO COMPARTMENT HAS 2 SHEAR TIES CRACKED AT BS 2040 BETWEEN STR 47 TO 48 AND STR 49 AND 50 LT. REPAIRED SHEAR TIE AT BS 2040 LT ACC TO SRM 53-10-4 FIG 41. 2 L 7 4 4F A20WE 1996022300111 19960223 00111 WP 1996 2 23 UPS8005526 1 19960128 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FS 902 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY INTERGRANNULAR CORROSION FS 902, LONGERON 24R NEEDS REPLACEMENT. REPLA CED LONGERON PER DOUGLAS DRAWING NR 5750196. 2 L 7 4 4F RT 4A25 1996022300112 19960223 00112 WP 1996 2 23 UPS8005527 1 19960130 A 5543 TAB DOUG DC8 DC871F 302199D WP RUDDER DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RUDDER TRIM TAB DELAMINATION RT SIDE 30 INCHES FROM BOTTOM. REPLACED TAB ASS Y FOR MM 27-21-02. 2 L 7 4 4F RT 4A25 1996022300113 19960223 00113 WP 1996 2 23 UPS8005528 1 19960127 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FS 880 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT LONGERON 24 CRACKED IN FISH MOUTH BOTTLE BOLT HOLE FS 880. REPLACED LONGE RON PER DOUGLAS DRAWING NR 5750188. 2 L 7 4 4F RT 4A25 1996022300114 19960223 00114 WP 1996 2 23 UPS8005529 1 19960131 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP FS 920 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION LT PRESSURE DECK PANEL AND FLOORBEAM FS 920 ABOVE LONGERON 24 L. REPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996022300115 19960223 00115 EU 1996 2 23 WWMA9600021 1 19960218 A 2730 5331139 PITCH TRIM SW SAAB SF340 340B 7860101 EU LT COCKPIT DEFECTIVE A WWMA O OTHER O OTHER CR CRUISE 1 WP 15 349SB 340B349 THE CREW REPORTED, AN UNCOMMANDED ELEVATOR TRIM IN FLIGHT, PRECEEDED BY THE CAPTAINS ELEVATOR TRIM BEING INTERMITTENT. M AINTENANCE REPLACED THE CAPTAINS PITCH TRIM SWITCH AND RELEASED THE AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 1996022300143 19960223 00143 NE 1996 2 23 AALA960016 2 19960105 A 7250 9304M93G04 ELBOW AIRBUS 300 A300B4605R 3930308 EU GE CF6 CF680C2A5 NE NR 2 ENGINE BROKEN A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 50051 459 JFK - FLT 0587 - AFTER TAKEOFF JFK DURING CLIMB-OUT AT FL 270, NR 2 ENGINE ECAM ADVISORY ON ENGINE PAGE FOLLOWED BY FIRE WARNING BOTH LOOPS. RETARDED NR 2 ENGINE TO IDLE AND ENGINE FIRE WARNING WENT OUT. ACCOMPLISHED ABNORMAL PROCEDURE AN D AIRCRAFT RETURNED TO JFK LANDING WITHOUT INCIDENT. REPLACED BROKEN HPT ELBOW AT REAR TURBINE CASE FRAME ON NR 2 ENGIN E. ACCOMPLISHED LEAK AND GROUND ENGINE RUN CHECK AT HIGH POWER WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPE RATION. (X) 2 L 7 2 4F 4 F RT A35EU E13NE 1996022300144 19960223 00144 NM 1996 2 23 AALA960021 1 19960109 A 5522 SKIN BOEING 727 727223 1384074 NM ELEVATOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 706AA 22463 CORROSION AROUND RT OUTBOARD STATIC WICK MOUNT BRACKET. CUT OUT DELAMINATED AREA, APPLIED REPAIR PER SRM 55-20-3, PAGE 3, AND REINSTALLED STATIC BASE AND WICK. (X) 2 L 7 3 4F A3WE 1996022300145 19960223 00145 NM 1996 2 23 9604056739 1 19960216 A 3246 26070812 WHEEL BOEING 747 747251F 1384898 NM LANDING GEAR CRACKED A NWAA A J UNSCHED LANDING DUMP FUEL K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 639US 79 23887 DURING CLIMB, THE NR 4 HYDRAULIC QUANTITY AND PRESSURE WENT TO ZERO AND A VIBRATION WAS FELT DURING LANDING GEAR RETRACT ION. AIRCRAFT DUMPED 200,000 LBS OF FUEL AND RETURNED TO ANC AND LANDED WITHOUT INCIDENT. FOUND NR 11 WHEEL ASSEMBLY C RACKED AND BRAKE DAMAGED. REPLACED NR 11 WHEEL AND BRAKE. ALSO, REPLACED ASSOCIATED PARTS THAT WERE DAMAGED. INSPECTE D FUSELAGE AND WHEEL WELL AREA FOR DAMAGE, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996022300146 19960223 00146 WP 1996 2 23 9604069852 1 19960217 A 3397 WIRE DOUG DC9 DC951 3022051 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 761NC 47709 DURING LINE CHECK, FOUND FIRST CLASS CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERIES, FOUND B ROKEN GROUND WIRE. REPAIRED GROUND WIRE AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A6WE 1996022300147 19960223 00147 WP 1996 2 23 9604079758 1 19960217 A 3350 BATTERY PACK DOUG DC9 DC941 302207N WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 758NW 47286 DURING LINE CHECK, FOUND OVERWING AFT LIGHT VERY DIM. REPLACED BATTERIES AND POWER SUPPLY, OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996022300148 19960223 00148 WP 1996 2 23 9604089860 1 19960216 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 769NC 47757 DURING LINE CHECK, FOUND AFT OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996022300149 19960223 00149 NM 1996 2 23 9604095532 1 19960218 A 2530 OVEN BOEING 757 757251 1384970 NM AFT GALLEY DIRTY A NWAA A E F UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 532US 24263 DURING CLIMB WHILE PREPARING MEALS, FLIGHT ATTENDANT REPORTED SMOKE COMING FROM AFT GALLEY LT OVEN. FIRE BOTTLE WAS USE D TO EXTINGUISH SMOKE. DECLARED AN EMERGENCY, RETURNED TO DTW, LANDING WAS UNEVENTFUL. UPON AIRCRAFT COMING TO A STOP ON TAXIWAY, CREW INITIATED AN EMERG EVAC ENGINES AND APU WERE SHUTDOWN PER EMERG PROC AND FIRE EXTINGUISHING AGENTS DISC HARGED. AFTER FIRE DEP, RELEASED AIRCRAFT, MAINT BEGAN INVESTIGATION. SMOKE WAS DUE TO HAMBURGER GREASE DURING MEAL PR EPARATION. REPLACED AFT GALLEY OVENS AND CONTROLLERS. DURING EMERGENCY EVACUATION, DOORS 1R, 2L AND 4R DID NOT DEPLOY, INVESTIGATION CONTINUES. 2 L 7 2 4F RT A2NM 1996022300150 19960223 00150 1996 2 23 9604109604 4 19960218 A 2565 113317 SLIDE DOUG DC9 DC932 3022066 WP FWD GALLEY DOOR LOW PRESSURE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 604NW 34587 467 47222 DURING PERIODIC CHECK, FOUND FORWARD GALLEY SERVICE DOOR EVACUATION SLIDE LOW ON PRESSURE. REPLACED SLIDE. 2 L 7 2 4F A6WE 1996022300151 19960223 00151 1996 2 23 9604119989 4 19960218 A 2565 13621228 SLIDE DOUG DC9 DC931 3022065 WP TAIL SECTION LOW PRESSURE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8945E 1244 1228 47181 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL EVACUATION SLIDE LOW ON PRESSURE. REPLACED SLIDE. 2 L 7 2 4F A6WE 1996022300152 19960223 00152 NM 1996 2 23 9604126636 1 19960217 A 3150 T/O WARNING BOEING 747 747251B 1384892 NM COCKPIT ACTIVATED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 636US 23547 DURING TAKEOFF, THE TAKEOFF WARNING HORN ACTIVATED. ABORTED TAKEOFF AND RETURNED TO THE GATE. OPERATIONALLY CHECKED SY STEM, COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F A20WE 1996022300153 19960223 00153 NM 1996 2 23 9604135636 1 19960219 A 3610 DUCT BOEING 757 757251 1384970 NM RT PYLON SEPARATED A NWAA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 GL 01 536US 26483 DURING CLIMBOUT THROUGH FL 260, AN AIRFRAME VIBRATION BEGAN. SHORTLY THEREAFTER, A RIGHT DUCT LEAK INDICATION ILLUMINAT ED. THE RIGHT DUCT PRESSURE INDICATION DECREASED BELOW THE LEFT DUCT PRESSURE INDICATION. CREW ISOLATED THE RIGHT PNEU MATIC DUCT SYSTEM AND RETURNED TO DTW WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED THE FORWARD PYLON PANEL AND FOUND T HE DUCT SEPARATED 2 OR 3 FEET AFT OF PANEL OPENING. INSTALLED A NEW FUSED COUPLING AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A2NM 1996022300154 19960223 00154 1996 2 23 9604149948 4 19960216 A 2565 13621225 SLIDE DOUG DC9 DC931 3022065 WP TAIL CONE LOW PRESSURE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8929E 1786 1781 45866 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL CONE EVACUATION SLIDE LOW ON PRESSURE. REPLACED SLIDE. 2 L 7 2 4F A6WE 1996022300155 19960223 00155 EU 1996 2 23 9604163210 1 19960215 A 7120 LH7461T144D NUT AIRBUS 320 A320211 3930320 EU LT ENG FWD MOUNT IMPROPER CONFIG A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 310NW 121 DURING LINE CHECK DIRECTED INSPECTION, FOUND ONE IMPROPER CONFIGURATION NUT ON THE LEFT ENGINE FORWARD ENGINE MOUNT, FOR WARD OUTBOARD ATTACH BOLT (P/N LH7461T144D). REPLACED NUT WITH (P/N VN401B144) PER MM 71-00-00 PG 436. 2 L 7 2 4F RT A28NM 1996022300156 19960223 00156 EU 1996 2 23 9604173207 1 19960214 A 7120 LH7461T144D NUT AIRBUS 320 A320211 3930320 EU LT ENG FWD MOUNT CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 307US 106 DURING '1C1' CHECK, LEFT ENGINE CHANGE FOUND THE FORWARD ENGINE MOUNT FORWARD ATTACH NUTS CRACKED. FURTHER INVESTIGATIO N REVEALED THAT IMPROPER CONFIGURATION NUTS WERE PREVIOUSLY INSTALLED (P/N LH7461T144D) PROPER CONFIGURATION IS (VN401B1 44). REPLACED ENGINE (P/N CMF56-5), (S/N 731569; 11692 T50) AND ASSOCIATED MOUNTING HARDWARE. 2 L 7 2 4F RT A28NM 1996022300157 19960223 00157 WP 1996 2 23 96FDEA00288 1 19960217 A 2700 FLT CONT CABLES DOUG DC10 DC1030 3023501 WP CTR GEAR WW BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 317FE 46835 DURING REPLACEMENT OF HYD REVERSABLE MOTOR PUMP SHUTOFF VALVE, BROKEN FLIGHT CONTROL CABLES WERE FOUND IN CENTER GEAR WE LL. REMOVED AND REPLACED BOTH FLAP INPUT AILERON LOCKOUT CABLE RUNS. ADJUSTED AS PER 27-10-00 PAGE 515, RII REQUIRED. OPS CK GOOD, (P/N S4913810AS13117), (S4913801AS112404), (S4916997AS04808). 2 L 7 3 4F A22WE 1996022300158 19960223 00158 WP 1996 2 23 96UAL900120 1 19960216 A 3350 BATTERY DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1816U 46615 EMERGENCY LIGHT SYSTEM DID NOT TEST. MID FWD AND MID AFT FAILURE LIGHTS ON. REPLACED BATTERY SUPPLIES AT MID FWD AND M ID AFT POSITIONS, TESTS NORMAL. 2 L 7 3 4F 4 F A22WE E23EA 1996022300159 19960223 00159 NM 1996 2 23 96UAL900121 1 19960216 A 2612 105080037525 FIRE DET LOOP BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE INOPERATIVE A UALA O OTHER L NO TEST IN INSP/MAINT 1 WP 29 7277U 21424 NR 2 ENGINE FIRE TEST INOPERATIVE, FIRE DETECTION LOOP WOULD NOT GROUND TEST. REPLACED FIRE DETECTION LOOP FOR NR 2 ENG INE AND GROUND TEST NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1996022300160 19960223 00160 NM 1996 2 23 96UAL900122 1 19960216 A 2150 PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE COCKPIT ODOR A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 7451U 21905 FUMES IN COCKPIT WITH PACKS RUNNING. SUPPLEMENTAL DATA UPDATE: OPERATED BOTH PACKS FOR 1 HOUR AND NO FUMES NOTICED. 2 L 7 3 4F 4 F A3WE E2EA 1996022300161 19960223 00161 NM 1996 2 23 96UAL900123 1 19960216 A 3350 BATTERY PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7293U 21571 EMERGENCY EXIT LIGHT AT CENTER AISLE CEILING ADJACENT TO AFT GALLEY WOULD NOT GO OUT. REPLACED BATTERY PACK AND CIRCUIT BOARD BASE, CHECKS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1996022300162 19960223 00162 NM 1996 2 23 96UAL900124 1 19960219 A 3350 LAMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 6 SLIDE INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 663UA 27160 THE RIGHT NR 6 SLIDE LIGHT IS INOP. REPLACED LAMP, OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 1996022300163 19960223 00163 NM 1996 2 23 96UAL900125 1 19960219 A 2612 FIRE BELL BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE COCKPIT MALFUNCTIONED A UALA O OTHER L NO TEST IN INSP/MAINT 1 WP 29 7260U 21407 FLIGHT CREW ADVISED FIRE WARNING SYSTEM BELL DOES NOT RING WHEN SYSTEM IS TESTED. SUPPLEMENTAL DATA UPDATE: REPLACED A URAL WARNING BOX ASSEMBLY. OPERATIONALLY, CHECKS OK. 2 L 7 3 4F 4 F A3WE E2EA 1996022300164 19960223 00164 NM 1996 2 23 96UAL900126 1 19960219 A 2612 FIRE TEST BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7277U 21424 NR 2 ENGINE FIRE TEST INOPERATIVE. 2 L 7 3 4F 4 F A3WE E2EA 1996022300165 19960223 00165 NM 1996 2 23 96UAL900127 1 19960219 A 5521 RIB BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE RT ELEVATOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7465U 21919 RIGHT ELEVATOR LOWER SURFACE INBD END HAD POPPED AND HAD LOOSE RIVETS. AFTER REMOVAL OF ACCESS PANEL FOUND STIFFENER RI B CRACKED. MANUFACTURED AND INSTALLED NEW RIB, REPLACED POPPED AND LOOSE RIVETS. 2 L 7 3 4F 4 F A3WE E2EA 1996022300166 19960223 00166 NM 1996 2 23 96UAL900128 1 19960219 A 3350 BATTERY PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7461U 21915 FOUND SEVERAL INOPERATIVE EEL STRIP LIGHTS IN MAIN CABIN, INCLUDING BOTH OVERWING EMERGENCY EXITS. REPLACED BATTERY PAC K AND GROUND CHECKED NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1996022300167 19960223 00167 NM 1996 2 23 96UAL900129 1 19960219 A 3250 4129RA9 VALVE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU NLG STEERING LEAKING A UALA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 907UA 14544 25007 CREW REPORTS, SEVERAL PASSENGERS AND FLIGHT ATTENDANTS COMPLAIN OF HEAVY FUMES IN PASSENGER CABIN. NOSE STEERING METERI NG VALVE WAS FOUND LEAKING HYDRAULIC FLUID AND IT WAS INGESTED INTO THE PACKS. REPLACED METERING VALVE AND COALESCER BA GS. 2 L 7 2 4F 4 F RT A16WE E21EU 1996022300168 19960223 00168 NM 1996 2 23 96UAL900130 1 19960219 A 2170 COALESCER BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE CABIN CONTAMINATED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 9032U 19070 DURING CLIMB, KEROSENE LIKE SMELL IN PASSENGER CABIN. BOTH PACKS AND BLEEDS ON AT THE TIME. FUEL SMELL ORIGINATED FROM THE GROUND PNEUMATIC CONNECTOR, WHICH WAS CONTAMINATED FROM A GROUND TRUCK USED FOR STARTING THE ENGINES. THE DUCTING WAS CLEANED, COALESCER BAGS WERE REPLACED AND SYSTEM CHECKS OK. 2 L 7 2 4F 4 F A16WE E2EA 1996022300169 19960223 00169 NM 1996 2 23 96UAL900131 1 19960219 A 3350 BATTERY PACK BOEING 737 737291 138448W NM PWA JT8 JT8D9A 52048 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 982UA 21640 EMERGENCY PATHWAY LIGHTING DIM FROM LEFT WING EXIT DOOR FORWARD. REPLACED BATTERY PACK FOR THE EEL LIGHT ASSEMBLY. 2 L 7 2 4F 4 F A16WE E2EA 1996022300170 19960223 00170 NM 1996 2 23 DHL9670801 1 19960203 A 5320 FRAME BOEING 727 72725 1384006 NM FWD CARGO DR CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 64052 18275 FWD CARGO DOOR CUTOUT, FWD UPPER FRAME CRACKED AT UPPER STOP FITTING. STOP DRILLED CRACK IN FRAME PER SRM 51-10-1. FAB RICATED DOUBLER REPAIR PER SRM 53-10-4, FIG 10. HEAT TREATED DOUBLER REPAIR PER BAC 5602. INSTALLED DOUBLER REPAIR PER SRM 53-10-4 FIG 10. 2 L 7 3 4F A3WE 1996022300171 19960223 00171 NM 1996 2 23 DL72K960337 1 19960214 A 5754 65162249092 RIB BOEING 727 727232 1384082 NM NR 8 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 480DA 20860 DURING SHOP INSPECTION, NR 8 L/E SLAT WAS FOUND WITH CRACKED RIB. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1996022300172 19960223 00172 NM 1996 2 23 DL72K960338 1 19960214 A 5754 65162249092 SKIN BOEING 727 727232 1384082 NM NR 8 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 480DA 20860 DURING SHOP INSPECTION, NR 8 L/E SLAT WAS FOUND WITH CRACKED TAI SKIN. REPAIRED SKIN PER MM 57-54-0 FIG 803. 2 L 7 3 4F A3WE 1996022300173 19960223 00173 NM 1996 2 23 DL72K960342 1 19960212 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 344 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 472DA 20749 FOUND ON MV1 CHECK, CORROSION SEVERAL PLACES FLOORBEAM STA 344. REPAIRED PER SRM 53-10-8 FIG 11. 2 L 7 3 4F A3WE 1996022300174 19960223 00174 NM 1996 2 23 DL72K960345 1 19960215 A 5754 651622373 SKIN BOEING 727 727232 1384082 NM NR 2 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 481DA 20861 DURING SHOP VISIT, INNER TAI SKIN CRACKED BETWEEN RIBS NR 11 AND NR 12 AT AFT RIVET TAIL. REPAIRED PER MM 57-54-0 FIG 8 03A, FOR NR 2 L/E SLAT. 2 L 7 3 4F A3WE 1996022300175 19960223 00175 NM 1996 2 23 DL72K960371 1 19960111 A 5330 651842010 SKIN BOEING 727 727232 1384082 NM FS 259.5-294.5 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 471DA 20748 DURING INSPECTION, THE LOWER RT FUSELAGE SKIN BETWEEN STA 259.5 AND STA 294.5 WAS FOUND DENTED JUST ABOVE STR 19R. THE FRAME SHEAR TIE AT STA 277 BETWEEN S-19R AND S-18R WAS DAMAGED AND BEING REPAIRED IN ACCORDANCE WITH B727 SRM. THE SKIN WAS REPAIRED PER A TIME-LIMITED REPAIR PER FAA/DER FORM8110-3, DTD 01-11-96 DL ERA 302990 REV A. 2 L 7 3 4F A3WE 1996022300176 19960223 00176 NM 1996 2 23 DL72L960344 1 19960213 A 5330 651752786 SKIN BOEING 727 727232 1384082 NM FS 1183-1263 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 513DA 21315 DAMAGE WAS FOUND ON THE UPPER TORQUE BOX SKIN DUE TO AN UNCONTAINED ENGINE FAILURE. THE DAMAGED SKIN SECTIONS WERE REMA NUFACTURED AND REPLACED IN ACCORDANCE WITH FAA/DER FORM 8110-3, DATED 12 FEB 96. 2 L 7 3 4F A3WE 1996022300177 19960223 00177 NE 1996 2 23 DL72P960336 2 19960214 A 7261 528174A PACKING BOEING 727 727225 1384077 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE LEAKING A DALA E ENGINE SHUTDOWN J K WARNING INDICATION FLUID LOSS CL CLIMB 1 SO 27 8890Z 21859 700310 NR 1 ENGINE SHUTDOWN IN FLIGHT DUE TO LOSS OF OIL PRESSURE AND QUANTITY. QUANTITY WENT TO ZERO AFTER SHUTDOWN. FOUND P ACKING LEAKING ON N1 ACCESSORY HOUSING REF PW JT8D,IPC 72-21-00 FIG 3A ITEM 110 (P/N 528174). CHECKED MOS, FOUND CLEAN. REPLACED PACKING, PERFORMED HIGH POWER RUNUP AND LEAK CHECK OK. 2 L 7 3 4F 4 F A3WE E2EA 1996022300178 19960223 00178 1996 2 23 DL72S960340 4 19960214 A 3417 CADC HG180U270 BOEING 727 727232 1384082 NM E/E COMP FAILED A DALA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 SO 27 402DA Q3169 21146 AFTER TAKEOFF, TCAS DISPLAYED ALL FAILED AND MAIN TCAS SCREEN SHOWED NR 1 XPONDER DATA BUS AND ALT DATA. CENTER ADVISED THEY RECEIVED SQUAWK, BUT NO ALT READOUT. AT FL 310 LEVEL OFF AND CRUISE MACH .80, A/C BEGAN MILD DUTCH ROLL. ROLL CE ASED WHEN SPEED SLOWED TO 270/260 KIAS. BOTH FLT DIR INOP, YAW DAMPER FLAGS NOT IN VIEW AND DIVERTED TO CVG PER DISPATCH ER AND MAINT CONTROL. REPLACED CADC, CAPT ALT FLAG OUT, TCAS OPS OK, NORMAL NO FLAGS. 2 L 7 3 4F A3WE 1996022300179 19960223 00179 NM 1996 2 23 DL72S960351 1 19960216 A 2150 39854021 VALVE BOEING 727 727232 1384082 NM RT PACK STICKING A DALA B EMER. DESCENT O OTHER CL CLIMB 1 SO 27 469DA 20746 AT 18,000 FT CABIN CLIMB 1000 FPM, STANDBY AND MANUAL NO HELP. MADE EMERGENCY DESCENT TO 11,000 FT. FOUND RT PACK VALV E STICKING CLOSED. REPLACED SAME, OPS CKS. REMOVED BOTH WATER SEP BAGS, NO OBSTRUCTIONS FOUND. REINSTALLED PRESSURIZA TION, CHECK NORMAL. 2 L 7 3 4F A3WE 1996022300180 19960223 00180 NM 1996 2 23 DL72S960352 1 19960212 A 5754 TE WEDGE 652678868A BOEING 727 727232 1384082 NM NR 5 LE SLAT DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 411DA A10259 21223 NR 5 L/E SLAT T/E WEDGE UPPER SURFACE DENTED. REPLACED WEDGE PER SRM 57-43-02. 2 L 7 3 4F A3WE 1996022300181 19960223 00181 NM 1996 2 23 DL72S960364 1 19960218 A 2530 OVEN 254005170 BOEING 727 727232 1384082 NM AFT GALLEY FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 522DA 002 21582 ALL 3 FWD FACING OVENS IN AFT GALLEY WERE SMOKING AND EMITTING AN ELECTRICAL/CHEMICAL ODOR. THEY WERE NOT USEABLE. 2 L 7 3 4F A3WE 1996022300182 19960223 00182 NM 1996 2 23 DL72S960367 1 19960218 A 2710 652844812 BELL CRANK BOEING 727 727232 1384082 NM RT AILERON TAB WORN A DALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 27 408DA 21152 PILOT REPORTS, AT 230 KTS A LOUD VIBRATION WAS HEARD FROM THE F/O WINDOW AREA DURING CLIMBOUT AND AT 220 KTS DURING DECE L THE VIBRATION STOPPED. REPLACED THE RIGHT HAND OUTBOARD AILERON TRIM TAB BELL CRANK, WHICH WAS FOUND TO HAVE OBLONGED MOUNT HOLES. RIG CHECK OK. 2 L 7 3 4F A3WE 1996022300183 19960223 00183 NM 1996 2 23 DL72S960369 1 19960218 A 2120 AIR DISTR BOEING 727 727232 1384082 NM AFT GALLEY ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 543DA 22392 DURING FINAL APPROACH, FLT ATTN NOTICED BURNING SMELL LIKE FIREWORKS, AROUND LT AFT LAV AREA. MTC POWERED A/C, TURNED O N ALL GALLEY AND LAV EQUIPMENT AND WAS UNABLE TO REPRODUCE ANY NOTICEABLE SMELL. 2 L 7 3 4F A3WE 1996022300184 19960223 00184 NM 1996 2 23 DL72S960370 1 19960218 A 2150 HPRSOV 39271611 BOEING 727 727232 1384082 NM NR 2 PACK MALFUNCTIONED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 543DA P1946 22392 ON DECENT AT ABOUT 9K, STRONG DUSTY ELEC SMELL IN AFT ENTRY AREA. THE WING AND ENGINE HEAT OFF. DEACTIVATED GALLEY PO WER AND LAV FLUSH MOTORS AS PRECAUTION. INSPECTED AND OPERATED SYSTEMS, UNABLE TO DUPLICATE. SUBSEQUENT OCCURENCE ISOL ATED PROBLEM TO HIGH BLEED PRESSURE TO NR 2 PACK. REPLACED HPRSOV, LEAK AND OPERATION CHECK NORMAL. NO ODOR NOTED. 2 L 7 3 4F A3WE 1996022300188 19960223 00188 NM 1996 2 23 DL72W960347 1 19960215 A 5754 RIB BOEING 727 727247 138408F NM NR 8 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 296WA 22533 FOUND DURING F-1 LETTER CHECK, 2 INCH CRACK NR 8 L/E SLAT NOSE RIB AT I/B SIDE OF ACTUATOR ATTACH FITTING. REPAIRED PER M/M 57-54-00 PAR 9. 2 L 7 3 4F A3WE 1996022300189 19960223 00189 NM 1996 2 23 DL72W960348 1 19960215 A 2780 ATTACH BOX BOEING 727 727247 138408F NM NR 1 LE FLAP ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 296WA 22533 FOUND DURING F-1 LETTER CHECK, .25 INCH CRACK NR 1 L/E FLAP ACTUATOR ATTACH BOX O/B SIDE. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1996022300190 19960223 00190 NM 1996 2 23 DL72W960349 1 19960215 A 5754 ANGLE BOEING 727 727247 138408F NM NR 2 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 296WA 22533 FOUND DURING F-1 LETTER CHECK, .375 INCH CRACK NR 2 L/E SLAT COVE SKIN ATTACH ANGLE BELOW TAI DUCT. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1996022300191 19960223 00191 NM 1996 2 23 DL72W960363 1 19960216 A 5713 STRINGER BOEING 727 727247 138408F NM WS 656.5 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 295WA 22532 FROM MV-2 ATL, LT WING INSIDE WS 656.5 FWD STRINGER NR 14 FWD ATTACH TAB CRACKED. VIEWED WITH MIRROR TOP SURFACE OF TAB AT ATTACH HOLE. REPAIRED PER MM 57-13-0 PG 811. 2 L 7 3 4F A3WE 1996022300192 19960223 00192 NM 1996 2 23 DL72W960366 1 19960214 A 5542 SKIN BOEING 727 727247 138408F NM RUDDER GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 295WA 22532 SKIN GOUGED LOWER RUDDER EXT SKIN LT SIDE HAS SEVERAL NICKS AND GOUGES AT AREA OF LETTER 'A' L/E. BLENDED DAMAGE, CHECK ED ALLOWABLE LIMITS OF GOUGE, FOUND DEPTH TO BE .019. DRILLED UP DOUBLER, INSTALLED REPAIR PER SRM 55-20-3. 2 L 7 3 4F A3WE 1996022300193 19960223 00193 NM 1996 2 23 DL73E960381 1 19960122 A 5330 654576988 SKIN BOEING 737 737247 138448D NM FS 379 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 243WA 23517 DURING INSPECTION, A 1 INCH CRACK WAS FOUND JUST LEFT OF BL 0 AT STA 379 IN THE SKIN AFT OF THE E/E AIR DUCT CUTOUT. TH E CRACK IS TYPICAL OF THOSE COVERED BY BOEING S/B 737-53-1117, REV 1. DURING REMOVAL OF THE EXHAUST DUCT, THE INTERNAL SURROUND DOUBLER WAS TORN RESULTING IN A 1 INCH BY 1.25 INCH CUTOUT. REPAIRED AS REQUIRED BY BOEING SERVICE BULLETIN 73 7-53-1117, WHICH INSTALLS A DOUBLER REF DL ERA 303053-14. 2 L 7 2 4F A16WE 1996022300194 19960223 00194 NM 1996 2 23 DL73S960373 1 19960128 A 5330 DOOR CUTOUT BOEING 737 737232 1384475 NM CABIN CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 305DL 23077 DURING INSPECTION, BOTH THE L1 AND R1 DOOR CUTOUTS HAD CRACKS RUNNING FROM THE LOWER AFT CORNER EDGES AND TERMINATING IN FASTENER HOLES. BOTH CRACKS EXTEND THROUGH THE SKIN, BONDED DOUBLER AND UNDERLYING BEAR STRAP. THE R1 DOOR CUTOUT WAS REPAIRED IN ACCORDANCE WITH B737-200 SRM 53-30-3, FIG 26. THE L1 DOOR WAS IN ACCORDANCE WITH BAC S/B 737-53-1083. 2 L 7 2 4F RT A16WE 1996022300195 19960223 00195 NM 1996 2 23 DL757960339 1 19960214 A 2910 312N310024 TUBE BOEING 757 757232 1384965 NM RT PYLON CRACKED A DALA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 637DL 23760 EN ROUTE, RECEIVED EICAS RT HYD SYS PRESS AND EICAS ADVISORY RT HYD QTY. RT HYD QTY READ .65 AND RF WAS DISPLAYED. BOT H RT SIDE PUMPS TURNED OFF IAW POM (2003Z). FOUND RT ENG HYD PRESSURE LINE (312N3100-24) IN PYLON CRACKED. REPLACED TU BE, OPERATION NORMAL. 2 L 7 2 4F RT A2NM 1996022300196 19960223 00196 NM 1996 2 23 DL757960353 1 19960212 A 5754 TE WEDGE 114N4004165 BOEING 757 757232 1384965 NM NR 3 LE SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 658DL A10259 24420 DURING INSPECTION, NR 3 L/E SLAT T/E WEDGE WAS FOUND DELAMINATED. REPLACED WEDGE PER SRM 57-43-02. 2 L 7 2 4F RT A2NM 1996022300198 19960223 00198 WP 1996 2 23 DLL10960356 1 19960217 A 3350 LIGHT 305 LKHEED 1011 10113851 5265010 WP L4 SLIDE INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 717DA 193C1096 DURING INSPECTION, L-4 DOOR SLIDE LIGHT INOP. RELAMED, OPERATION NORMAL. 2 L 7 3 4F A23WE 1996022300199 19960223 00199 WP 1996 2 23 DLL10960358 1 19960217 A 3245 TIRE CAP 1547903101 LKHEED 1011 10113851 5265010 WP NR 3R WHEEL MISSING A DALA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 SO 27 719DA 41790529 193C1135 AT ROTATION, LOUD ENGINE VIBRATION AUDIBLE. CHECKED ENGINE VIBRATION LIGHT ON PILOT ANN ON CHANNELS A AND B, SHOWED 5.0 UNITS STEADY AND AT LEVEL OFF THROTTLE BACK VIBRATIONS DROPPED TO 3.8 BOTH CNLS, SHUTDOWN ENGINE. TOWER INSPECTED RUNW AY AND FOUND LARGE PIECES OF TIRE TREAD. NR 3 ENGINE SHUTDOWN, NR 3 REAR TIRE FLAT AND CAP MISSING/DAMAGE TO RT INBD FL AP VANE AND HYD LINES RT W/W AREA. ALSO, DAMAGE TO 1ST STAGE FAN NR 3 ENGINE. 2 L 7 3 4F A23WE 1996022300200 19960223 00200 WP 1996 2 23 DLL13960343 1 19960215 A 3350 POWER SUPPLY 5165741 LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 785DL 60815 193A1121 FLOOR TRACK LIGHTS INOP IN D-ZONE. REPLACED POWER SUPPLY (P/N 337001090), OPS CHECK NORMAL. 2 L 7 3 4F A23WE 1996022300201 19960223 00201 WP 1996 2 23 DLL13960378 1 19960216 A 5712 RIB CAP LKHEED 1011 10113851 5265010 WP WS 529 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 790DL 193A1143 THE RT WING IWS 529 UPPER CAP IS CRACKED IN TYPICAL LOCATIONS. THE REF ERA AUTHORIZES REPLACEMENT OF THE SUBJECT CAP CO NTAINING CRACKS PER LAC L1011 S/B 093-57-207, REF DL ERA 272877 AD REV A. 2 L 7 3 4F A23WE 1996022300202 19960223 00202 WP 1996 2 23 DLL17960346 1 19960130 A 3230 1591922 FITTING LKHEED 1011 10113853 5265020 WP LT MLG ACT CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 769DL 193H1218 LT MLG ACTUATOR ATTACH FITTING WAS FOUND CORRODED ON THE UPPER FLANGE. IN ORDER TO REMOVE THE CORROSION THE FASTENER HO LES WERE OVERSIZED AND SPOT FACED IN ACCORDANCE WITH THE INSTRUCTIONS OF THE L1011 SRM FIG 808. FASTENER HOLE 1 TO 4 AN D 6 REQUIRED SPOT FACING DEEPER THAN THE LIMIT ALLOWED PER SRM REPAIR AND HOLE 5 HAS NOT BEEN SPOTFACED BEYOND ALLOWABLE LIMITS. ALL HOLES WERE OVERSIZED WITHIN ALLOWABLE LIMITS AS SET FORTH BY THE SUBJECT SRM REPAIR. REPAIRS ACCOMPLISHED PER DL ERA 273186 REV A. 2 L 7 3 4F A23WE 1996022300203 19960223 00203 WP 1996 2 23 DLL17960372 1 19960216 A 5711 1605415 SPAR CAP LKHEED 1011 10113853 5265020 WP WS 293-343 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 769DL 193H1218 CRACKS WERE FOUND EMANATING FROM EXISTING FASTENER HOLES BETWEEN IWS 293.5 AND IWS 343. THE CRACKS WERE FOUND IN THE RE AR SPAR UPPER SKIN AND CAP. THE SUBJECT FASTENER HOLES WERE OVERSIZED TO REMOVE THE CRACKS IN THE DAMAGED MEMBERS ONLY WITH INSURANCE CUTS TAKEN. REPAIRED PER DL ERA 273234 AD REV A. 2 L 7 3 4F A23WE 1996022300204 19960223 00204 WP 1996 2 23 DLL17960374 1 19960216 A 5312 BLKHD BEAM LKHEED 1011 10113853 5265020 WP BS 449 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 769DL 193H1218 THE NLG W/W SIDEWALL BULKHEAD UPPER BEAM IS CRACKED IN ITS UPPER BEND RADIUS AT ITS AFT MOST END, STA 449. THE CRACK RU NS FWD APPROX 1.5 INCH AND HAS BEEN STOP DRILLED WITH A .25 INCH HOLE. THE BEAM WILL BE REPAIRED WITH TWO REPAIR ANGLES , PER DL ERA 273196 REV A. 2 L 7 3 4F A23WE 1996022300205 19960223 00205 WP 1996 2 23 DLL17960379 1 19960216 A 5730 1617189102 SKIN LKHEED 1011 10113853 5265020 WP WS 346 OVERSIZED HOLE A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 769DL 193H1218 TWO EXISTING FASTENER HOLES AT IWS 346 ON THE RT WING WERE FOUND TO HAVE UNDOCUMENTED BUSHINGS INSTALLED THROUGH THE WIN G SKIN ONLY. NO CRACK INDICATIONS WERE FOUND AFTER EDDY CURRENT INSPECTION. BOTH HOLES WERE MEASURED AT .440 DIA. REP AIR APPROVAL PER DL ERA 273208 AD REV A. 2 L 7 3 4F A23WE 1996022300206 19960223 00206 NM 1996 2 23 DLM11960354 1 19960216 A 2560 PRESS INDICATOR 3512438900 DOUG MD11 MD11 3023602 NM 4R DOOR SLIDE FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 811DE 48566 PRESS TO TEST FUNCTION DID NOT WORK ON 4R DOOR PRESSURE INDICATOR LIGHT. LIGHT ILLUMINATED WHEN JACK CONNECTING IT TO S LIDE WAS DISCONNECTED. REPLACED INDICATOR ASSY, CHECKS GOOD. 2 L 7 3 4F RT A22WE 1996022300207 19960223 00207 NM 1996 2 23 DLM88960350 1 19960216 A 2910 OVERFLOW CAN DOUG MD88 MD88 3023688 NM HYD SYST OVERFLOWING A DALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 SO 27 920DL 49644 ON APPROACH WITH ENGINE ANTI-ICE ON, AFT SMOKE DETECTORS WENT OFF AND THERE WAS SMOKE IN THE CABIN. REPLACED WATER SEPA RATOR BAGS AND LEAK CHECK OK. CHECKED ACM OIL, FOUND OK. FOUND HYD OVERFLOW CAN OVERFLOWING, EMPTIED SAME AND RAN ENGI NES PACKS ANTI-ICE, APU COULD NOT DUPLICATE. 2 L 7 2 4F RT A6WE 1996022300208 19960223 00208 NM 1996 2 23 DLM88960362 1 19960218 A 2150 PACK 68347811 DOUG MD88 MD88 3023688 NM LEFT INOPERATIVE A DALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 27 938DL 49811 AFTER TAKEOFF, A/C WOULD NOT PRESSURIZE, LEFT PACK SUPPLY WAS ZERO. FLT ATTENDANT REPORTED LOUD SOUND LEFT AFT DOOR, OA P SHOWED NO DOOR LIGHTS. PERFORMED POM PROCEDURE, NO EFFECT. FOUND BOTH PACKS INOP, RT PACK INTERMITTENT OPERATION. F WD RT PACK TO MCO/PLAC REF MEL 21-00-01A, REPLACED THERMAL SWT 190F FOR LEFT A/C SYS, PACK CHECKS GOOD. BORROWED SWT FR OM RT SYS (P/N 219101528). 2 L 7 2 4F RT A6WE 1996022300209 19960223 00209 WP 1996 2 23 MWEA96043 1 19960219 A 2560 113313 EVAC SLIDE DOUG DC9 DC932 3022066 WP FWD GALLEY DOOR LOOSE A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 302ME 47102 CREW REPORTS, GALLEY SERVICE DOOR EVAC SLIDE AND GIRT BAR IS LOOSE. RESECURED GALLEY DOOR SLIDE AND GIRT BAR. 2 L 7 2 4F A6WE 1996022300210 19960223 00210 NM 1996 2 23 P5CA9600143 1 19960219 A 7722 EGT INDICATION BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE NR 3 ENGINE HIGH A P5CA O OTHER J WARNING INDICATION TO TAKEOFF 1 WP 23 858FT 20109 662763 ON TAKEOFF, NR 3 EGT WENT TO 920 DEGREES FOR APPROX 45 SECONDS. ALL OTHER INDICATIONS NORMAL AND NO ABNORMAL PERFORMANC E FOR REST OF FLIGHT. PERFORMED REQUIRED INSPECTIONS FOR CATEGORY A ITEMS PER MM 72-00-00 PG 680L 3 B, SATISFACTORY. 2 L 7 4 4F 4 F A20WE E20EA 1996022300211 19960223 00211 NM 1996 2 23 P5CA9600144 1 19960219 A 5730 SKIN BOEING 747 747123 1384873 NM WS 300 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 FOUND LOWER LEFT HAND WING SKIN WITH LEVEL ONE CORROSION AT APPROX STATION 300. REMOVED CORROSION IAW SRM 51-10-01. 2 L 7 4 4F A20WE 1996022300212 19960223 00212 EU 1996 2 23 QXEA9600019 1 19960115 A 3350 23531 POWER SUPPLY FOKKER F28 F28MK1000 4990808 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 450US 11101 FORWARD EMERGENCY EXIT LIGHT INOP. ENTRANCE CENTER POWER SUPPLY REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996022300213 19960223 00213 NM 1996 2 23 QXEA9600020 1 19960116 A 3350 82410162007 CONTROL BOX DHAV DHC8 DHC8102 2809003 NM CABIN MALFUNCTIONED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 830PH 314 EMERGENCY LIGHTS DO NOT GO OFF WHEN SELECTED OFF. EMERGENCY LIGHT CONTROL BOX REPLACED AND LIGHTS OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 1996022300214 19960223 00214 NE 1996 2 23 QXEA9600021 2 19960117 A 7261 3037233 SEAL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE NR 2 ENGINE CRACKED A QXEA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 NM 09 338PH 3029 PCE116066 NR 2 ENGINE OIL PRESS CAUTION CAS MESSAGE AFTER DEPARTURE. FLIGHT CREW MONITORED PRESS TO 40 PSI WHEN PROP WAS FEATHERE D. OIL PRESS RECOVERED TO 50 PSI AFTER PROP WAS FEATHERED. AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT FURTHER PROBL EM. NR 2 ENGINE WAS 14 PTS LOW ON OIL. SERVICED OIL AND ON GROUND HIGH OIL CONSUMPTION WAS NOTED, 1PT IN 15 MIN. CENT RIFUGAL BREATHER CARBON SEAL WAS REPLACED AND FILTERS INSPECTED IAW MAINT MANUAL. ENGINE OPS CHECKED GOOD ON GROUND RUN . 2 H 7 2 4T 4 T RT A45NM E20NE 1996022300215 19960223 00215 SW 1996 2 23 QXEA9600022 1 19960117 A 2150 20475541 COOLING TURBINE SWRNGN SWRNGN SA227 SA227AC 8780603 SW NR 2 SYS FAILED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 NM 09 385PH 13649 AC595 SMOKE IN THE CABIN ON FINAL APPROACH. SMOKE ISOLATED TO NR 2 BLEED. AIRCRAFT LANDED IN BZN WITHOUT FURTHER PROBLEM. N R 2 COOLING TURBINE REPLACED IAW MAINT MANUAL, OPS CHECKED GOOD ON GROUND RUN. 1 L 7 2 4T A8SW 1996022300216 19960223 00216 EU 1996 2 23 QXEA9600023 1 19960118 A 3350 6008903 BATTERY PACK FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 468US 11095 PDX - EVACUATION LIGHTS AT EXIT ROW 8 C/D/E INOP. BATTERY PACK REPLACED AT ROW 8 C/D/E AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996022300217 19960223 00217 EU 1996 2 23 QXEA9600024 1 19960118 A 5210 LOCK MECHANISM FOKKER FOKKER F28 F28MK1000 4990808 EU PAX DOOR FROZEN A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 468US 11095 YEG - CREW COULD NOT OPEN MAIN CABIN DOOR VIA NORMAL OR EMERGENCY MODE FROM INSIDE. DOOR OPERATION WAS NORMAL FROM EXTE RIOR. LOCK MECHANISM FOUND FROZEN. FREED UPLOCK MECHANISM WITH HEAT AND LUBE WITH SILICONE SPRAY. MCD OPS CHECKED GOO D. 2 L 7 2 4F RT A20EU 1996022300218 19960223 00218 EU 1996 2 23 QXEA9600025 1 19960118 A 3350 MGG1280 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 469US 11096 GEG - FORWARD EMERGENCY EXIT SIGN HAS SEVERAL 28V BULBS INOP. BULBS WERE REPLACED AND SIGN OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996022300219 19960223 00219 EU 1996 2 23 QXEA9600026 1 19960121 A 3350 1312 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 469US 11096 SEA - RIGHT HAND OVERWING EMERGENCY LIGHT INOP. BULB WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996022300220 19960223 00220 EU 1996 2 23 QXEA9600027 1 19960123 A 3350 MGG1280 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 802PH 11017 SEA - LIGHT IN OVERHEAD EXIT LIGHT SIGN AT ROW 8 INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996022300221 19960223 00221 NM 1996 2 23 QXEA9600028 1 19960123 A 2121 011390500 FAN DORNER DORNER DO32 DO328100 2996000 NM CABIN SMOKING A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 09 338PH 3029 GEG - ELECTRICAL SMOKE SMELL SEEMS TO BE LOCATED IN GALLEY. SMELL LOCATED TO RECIRCULATION SYSTEM. AFT RECIRCULATION F AN REPLACED IAW MAINT MANUAL. FAN OPS CHECKED GOOD. 2 H 7 2 4T RT A45NM 1996022300222 19960223 00222 NM 1996 2 23 QXEA9600029 1 19960124 A 3350 MS274081A SWITCH PANEL DHAV 4972062001 DHAV DHC8 DHC8102 2809003 NM FA PANEL MALFUNCTIONED A QXEA K NONE L NO TEST CR CRUISE 1 NM 09 813PH 32 PDX - ALL EMERGENCY LIGHTS IN CABIN FLICKER DURING FLIGHT. FLIGHT ATTENDANTS SWITCH PANEL REPLACED AND LIGHTS OPS CHECK ED GOOD. 2 H 7 2 4T RT A13NM 1996022300223 19960223 00223 EU 1996 2 23 QXEA9600030 1 19960124 A 3350 MGG1280 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 464US 11063 GEG - CABIN OVERHEAD EMERGENCY EXIT SIGN AT ROW 8 FACING FORWARD IS INOP. BULBS WERE REPLACED AND SIGN OPS CHECKED GOOD . 2 L 7 2 4F RT A20EU 1996022300224 19960223 00224 EU 1996 2 23 QXEA9600031 1 19960127 A 3350 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 801PH 11097 PDX - RIGHT HAND EXIT LIGHT INOP ON FORWARD CABIN BULKHEAD. LEFT HAND EXIT LIGHT DIM ON FORWARD CABIN BULKHEAD. BULBS REPLACED IN LEFT RIGHT EXIT LIGHTS AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996022300225 19960223 00225 EU 1996 2 23 QXEA9600032 1 19960128 A 3397 WIRE DHAV FOKKER F28 F28MK1000 4990808 EU CABIN SHORTED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 464US 11063 SEA - FLOOR PROXIMITY LIGHTS AT ROW 1 TO 8 ILLUMINATE WITHOUT CAUSE. AIRCRAFT FERRIED TO PDX FOR REPAIR. WIRE AT SEAT 8 A/B REPAIRED AND BATTERY PACK REPLACED. LIGHTS OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996022300226 19960223 00226 NM 1996 2 23 QXEA9600033 1 19960129 A 3350 MS33205 CIRCUIT BREAKER DHAV DHAV DHC8 DHC8102 2809003 NM COCKPIT INTERMITTENT A QXEA K NONE L NO TEST TO TAKEOFF 1 NM 09 813PH 32 PDX - EMERGENCY LIGHTS FLICKER ON TAKEOFF ABOUT THE SAME TIME STANDBY HYDRAULIC SWITCHES ARE TURNED OFF. POWER SUPPLY P S1 AND PS2, CONTROL BOX AND CIRCUIT BREAKER 1 AND 2 REPLACED. LIGHTS OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 1996022300227 19960223 00227 EU 1996 2 23 QXEA9600034 1 19960129 A 3350 MGG1280 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 457US 11036 PDX - EXIT SIGN AT ROW 8 IS DIM ON BOTH SIDES. BULBS WERE REPLACED AND SIGN OPS CHECKED GOOD. AIRCRAFT RETURNED TO SER VICE. 2 L 7 2 4F RT A20EU 1996022300228 19960223 00228 NE 1996 2 23 QXEA9600035 2 19960129 A 7261 3037223 CARBON SEAL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE NR 1 ENGINE CRACKED A QXEA A E UNSCHED LANDING ENGINE SHUTDOWN J Y WARNING INDICATION ENGINE STOPPAGE CR CRUISE 1 NM 09 332PH 3010 116032 NR 1 ENGINE OIL PRESS DROPPED TO 30 PSI, LEFT ENGINE LIGHT ILLUMINATED. NR 1 ENGINE SHUTDOWN IN FLIGHT. AIRCRAFT LANDE D WITHOUT FURTHER PROBLEM. NR 1 ENGINE CENTRIFUGAL CARBON SEAL FOUND CRACKED. CARBON SEAL REPLACED AND ENGINE OPS CHEC KED GOOD. NO LEAKS OR OIL LOSS NOTED. 2 H 7 2 4T 4 T RT A45NM E20NE 1996022300229 19960223 00229 NM 1996 2 23 QXEA9600036 1 19960130 A 3350 6038443 PWR SUPPLY DHAV DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 831PH 328 SEA - LEFT HAND UNDERWING AND ROW 6 OVERHEAD EMERGENCY LIGHTS INOP. POWER SUPPLY AND BATTERY REPLACED, LIGHTS OPS CHECK ED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1996022300230 19960223 00230 EU 1996 2 23 QXEA9600037 1 19960131 A 3350 1312 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 454US 11107 BOI - RIGHT OVERWING 28V EXIT LIGHT INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996022300231 19960223 00231 EU 1996 2 23 QXEA9600038 1 19960131 A 3350 1312 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 802PH 11017 PDX - EMERGENCY EXIT LIGHT OVER LEFT HAND WINDOW EXIT INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996022300232 19960223 00232 EU 1996 2 23 QXEA9600039 1 19960131 A 3350 MGG1280 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 462AU 11054 PDX - EXIT SIGN BETWEEN OVERWING EXITS ARE INOP. BULBS WERE REPLACED AND SIGN OPS CHECKED GOOD. AIRCRAFT RETURNED TO S ERVICE. 2 L 7 2 4F RT A20EU 1996022300233 19960223 00233 EU 1996 2 23 QXEA9600040 1 19960131 A 3350 608905 POWER SUPPLY FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 462AU 2751 11054 PDX - LEFT AND RIGHT WING ROOT EMERGENCY LIGHTS ARE INOP. BATTERY POWER SUPPLY REPLACED AND LIGHTS OPS CHECKED GOOD. A IRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996022300234 19960223 00234 SW 1996 2 23 QXEA9600041 1 19960201 A 3260 602EN6026 UP LIMIT SWITCH SWRNGN SWRNGN SA227 SA227AC 8780603 SW NLG OUT OF ADJUST A QXEA K NONE N FALSE WARNING CL CLIMB 1 NM 09 3114H AC584 LWS - NOSE GEAR CYCLES CONTINOUSLY AFTER GEAR RETRACTION. AIRCRAFT LANDED IN LWS WITHOUT FURTHER PROBLEM. AIRCRAFT FER RIED TO BOI FOR REPAIR. NOSE GEAR SWITCHES ADJUSTED IAW MAINT MANUAL. NOSE GEAR OPS CHECKED GOOD ON GEAR SWING. AIRCR AFT RETURNED TO SERVICE. 1 L 7 2 4T A8SW 1996022300235 19960223 00235 EU 1996 2 23 QXEA9600042 1 19960201 A 3350 1820 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 450US 11101 PDX - EMERGENCY LIGHTS IN PULL DOWN COVERS ROW 8 OVERWING EXITS ARE INOP. BULBS WERE REPLACED AND LIGHTS OPS CHECKED GO OD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996022300236 19960223 00236 EU 1996 2 23 QXEA9600043 1 19960201 A 3350 1012721 LIGHT FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 468US 11095 SEA - EMERGENCY LIGHT AT SEAT 2A INOP. LIGHT ASSY REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996022300237 19960223 00237 EU 1996 2 23 QXEA9600044 1 19960201 A 3350 5515800104 CIRCUIT BOARD FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN MALFUNCTIONED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 803PH 11031 PDX - EXIT SIGN LIGHT DIM IN PAX CABIN CEILING ROW 8. SIGN CIRCUIT BOARD REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996022300238 19960223 00238 NM 1996 2 23 QXEA9600045 1 19960204 A 3350 6104781 BATTERY PACK DHAV DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 829PH 339 304 SEA - AFT INSIDE AND RIGHT HAND AFT OUTSIDE EMERGENCY LIGHTS INOP. BATTERY PACK REPLACED AND LIGHTS OPS CHECKED GOOD. A IRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1996022300239 19960223 00239 SW 1996 2 23 QXEA9600046 1 19960205 A 3250 2753057059 TILLER SWRNGN SWRNGN SA227 SA227AC 8780603 SW COCKPIT SHORTED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 09 26877 AC652 BOI - SMOKE IN COCKPIT. NWS TILLER OVERLAY FOUND SHORTED. TILLER ASSY REPLACED AND TILLER OPS CHECKED GOOD. 1 L 7 2 4T A8SW 1996022300240 19960223 00240 EU 1996 2 23 QXEA9600047 1 19960205 A 3350 1312 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 454US 11107 GEG - EMERGENCY EXIT LIGHT INOP AT 8A. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996022300241 19960223 00241 1996 2 23 QXEA9600048 2 19960204 A 7200 ENGINE FOKKER F28 F28MK1000 4990808 EU RROYCE STC STCSPEY NR 2 BIRD STRIKE A QXEA E ENGINE SHUTDOWN C X F.O.D. ENGINE FLAMEOUT AP APPROACH 1 NM 09 464US 11063 9227 SMF - NR 2 ENGINE INGESTED SEVERAL BIRDS ON APPROACH TO SMF. ENGINE FLAMED OUT AS A RESULT OF BIRD INGESTION. AIRCRAFT LANDED IN SMF WITHOUT FURTHER INCIDENT. NR 2 ENGINE REPLACED IAW MAINT MANUAL AND ENGINE OPS CHECKED GOOD ON GROUND RU N. 2 L 7 2 4F 4 F RT A20EU E2EU 1996022300242 19960223 00242 EU 1996 2 23 QXEA9600049 1 19960206 A 3350 1312 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 469US 11096 PDX - EXIT LIGHT AT ROW 8A INOP. BULB REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996022300243 19960223 00243 NM 1996 2 23 QXEA9600050 1 19960206 A 2120 AIR DISTR DORNER DO32 DO328100 2996000 NM CABIN ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 09 338PH 3029 RDD - SMOKE ODOR IN COCKPIT AND CABIN. RECIRCULATION FANS INSPECTED, UNDER FLOOR AREA INSPECTED AND NO DEFECTS NOTED. F ANS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. AIRCRAFT REINSPECTED AT QX MAINT FACILITY AND NO DEFECTS WERE NOTE D. NO FURTHER PIREPS THROUGH 2-7. 2 H 7 2 4T RT A45NM 1996022300244 19960223 00244 NE 1996 2 23 QXEA9600051 2 19960206 A 7200 ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 FAILED A QXEA A E UNSCHED LANDING ENGINE SHUTDOWN Y ENGINE STOPPAGE CL CLIMB 1 NM 09 840PH 74 SEA - NR 1 ENGINE SHUTDOWN ON CLIMB WHEN NR 1 ENGINE INTAKE WAS SWITCHED ON. AIRCRAFT RETURNED TO FIELD AND LANDED WITH OUT INCIDENT. MAINTENANCE COULD DUPLICATE PROBLEM, WHEN THE NR 1 ENGINE INTAKE HEAT IS SWITCHED ON THE NR 1 FUEL SHUTOF F VALVE CLOSES. AIRCRAFT DOWN FOR REPAIR. 2 H 7 2 4T 4 T RT A13NM E20NE 1996022300245 19960223 00245 EU 1996 2 23 QXEA9600052 1 19960207 A 3350 1312 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU GALLEY FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 452US 11105 SEA - LOWER EMERGENCY EXIT LIGHT INOP IN RIGHT SIDE FORWARD GALLEY. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996022300246 19960223 00246 NM 1996 2 23 QXEA9600053 1 19960207 A 3350 6104781 BATTERY PACK DHAV DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 828PH 175 287 PDX - AFT RIGHT HAND EMERGENCY EGRESS LIGHT AND AFT OVERHEAD CENTER CEILING ASILE LIGHT INOP. BATTERY PACK AT 3351-PH R EPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1996022300247 19960223 00247 SW 1996 2 23 QXEA9600054 1 19960208 A 3310 PS401 POWER SUPPLY SWRNGN SWRNGN SA227 SA227AC 8780603 SW COCKPIT MALFUNCTIONED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 09 26952 AC661 PDX - ELECTRICAL SMELL IN COCKPIT, SMELL BEGAN ON CLIMBOUT. BOTH SIDE PANELS REMOVED, WIRING INSPECTED AND NO CHAFES OR BURNS NOTED. POWER SUPPLY PS189 REPLACED AND OPS CHECKED FOR 30 MINUTES, NO REPEAT OF PROBLEM. AIRCRAFT RETURNED TO S ERVICE. 1 L 7 2 4T A8SW 1996022300248 19960223 00248 NM 1996 2 23 QXEA9600055 1 19960209 A 3350 6104781 BATTERY PACKS DHAV DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 814PH 43 PDX - EMERGENCY LIGHTS INOP. BATTERY PACKS REPLACED AND LIGHTS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1996022300249 19960223 00249 1996 2 23 QXEA9600056 4 19960209 A 3442 071131313 RADAR UNIT BENDIX DHAV DHC8 DHC8102 2809003 NM COCKPIT MALFUNCTIONED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 09 812PH 7846 26 SEA - BURNT WIRE ODOR COMING FROM COCKPIT. RADAR GRAPHICS UNIT REPLACED FOR BURNT SMELL. RADAR GRAPHICS UNIT OPS CHECK ED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1996022300250 19960223 00250 EU 1996 2 23 QXEA9600057 1 19960210 A 3350 MGG1280 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU GALLEY FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 464US 11063 GEG - OVERHEAD EXIT SIGN IN GALLEY INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCARFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996022300252 19960223 00252 NM 1996 2 23 QXEA9600059 1 19960213 A 3350 321473 PWR SUPPLY FOKKER DORNER DO32 DO328100 2996000 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 330PH 3008 PDX - AFT EXIT SIGN INOP 9 AND 10, FLOOR PROXIMITY LIGHTS INOP AFT RIGHT HAND EXIT LIGHT INOP. BATTERY AND POWER SUPPLY 7LK REPLACED. DAMAGED PIN FOUND ON REMOVED UNIT AND AIRCRAFT CONNECTOR. LIGHTS OPS CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A45NM 1996022300253 19960223 00253 EU 1996 2 23 QXEA9600060 1 19960213 A 3397 WIRE FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN BROKEN A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 457US 11036 PDX - EVACUATION LIGHT AT ROW 3A INOP. BROKEN WIRE REPAIRED AT SEAT 2B. LIGHT OPS CHECKED GOOD AND AIRCRAFT RETURNED T O SERVICE. 2 L 7 2 4F RT A20EU 1996022300254 19960223 00254 EU 1996 2 23 QXEA9600061 1 19960213 A 3350 1315 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU GALLEY FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 466US 11075 SEA - GALLEY SERVICE DOOR LOWER EMERGENCY EXIT LIGHT INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETU RNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996022300255 19960223 00255 NM 1996 2 23 QXEA9600062 1 19960212 A 2120 AIR DISTR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE CABIN ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 09 102AV 091 10036 BOI - OIL SMELL IN CABIN ON DESCENT. AIRCRAFT LANDED IN BOI WITHOUT FURTHER PROBLEM. AIRCRAFT FERRIED TO PDX FOR REPAI R. NR 1 ENGINE REPLACED IAW MAINT MANUAL. ENGINE AND BLEED AIR OPS CHECKED GOOD ON GROUND RUN. AIRCRAFT RETURNED TO S ERVICE. AWAITING ENGINE TEARDOWN FOR CAUSE. 2 H 7 2 4T 4 T RT A13NM E20NE 1996022300256 19960223 00256 EU 1996 2 23 QXEA9600063 1 19960214 A 3350 6008903 BATTERY PACK FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 454US 11107 PDX - ENTRYWAY EVAC LIGHTS INOP. BATTERY PACK REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996022300257 19960223 00257 EU 1996 2 23 QXEA9600064 1 19960216 A 3350 1315 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU GALLEY FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 452US 11105 BOI - GALLEY SERVICE DOOR LOWER EMERGENCY EXIT LIGHT INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETU RNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996022300258 19960223 00258 EU 1996 2 23 QXEA9600065 1 19960216 A 3350 1315 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 450US 11101 PDX - EMERGENCY LIGHT IN CABIN CEILING AT ROW 2 INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996022300259 19960223 00259 EU 1996 2 23 QXEA9600066 1 19960216 A 3350 1315 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU GALLEY FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 452US 11105 BOI - GALLEY SERVICE DOOR LOWER EMERGENCY LIGHT INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996022300260 19960223 00260 EU 1996 2 23 QXEA9600067 1 19960217 A 3350 1312 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 803PH 11031 GEG - LEFT HAND LIGHT FLICKERS. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996022300261 19960223 00261 NM 1996 2 23 QXEA9600068 1 19960217 A 2611 824PTY SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM LAVATORY MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 102AV 091 SEA - LAV SMOKE DETECTOR CAME ON IN FLIGHT, NO SMOKE WAS OBSERVED. AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT FURTHE R PROBLEM. LAV SMOKE DETECTOR REPLACED AND DETECTOR OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1996022300262 19960223 00262 NM 1996 2 23 AALA960032 1 19960110 A 3260 63200036 DOOR SWITCH BOEING 727 727223 1384074 NM RT MLG DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 862AA 21089 DFW - FLT 0296 - AFTER TAKEOFF DFW WHEN LANDING GEAR RETRACTED, MLG DOOR WARNING REMAINED ILLUMINATED WITH ASSOCIATED RT MLG DOOR WARNING INDICATION ON F/E PANEL. EXTENDED LANDING GEAR AND ALL INDICATIONS RETURNED TO NORMAL. AIRCRAFT RETU RNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED RT MLG DOOR SWITCH. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1996022300263 19960223 00263 WP 1996 2 23 AALA960042 1 19960220 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP BS 837-859 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 130AA 46989 TUL - NR 6 SEAT TRACK HAS CORROSION DAMAGE UNDER RIGHT AFT SERVICE CENTER JUST OUTBOARD OF 'P' LIFT. REPLACED 93 INCHES OF SEAT TRACK UNDER RIGHT AFT SERVICE CENTER AND JUST FORWARD OF SERVICE CENTER PER SRM 53-70-00. (M) 2 L 7 3 4F A22WE 1996022300264 19960223 00264 NE 1996 2 23 AALA960045 2 19960111 A 7314 378200 FUEL PUMP BOEING 727 727223 1384074 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE DEFECTIVE A AALA E ENGINE SHUTDOWN X ENGINE FLAMEOUT DE DESCENT 1 SW 07 703AA 22461 MEX - FLT 2087 - DURING DESCENT INTO MEX, FUEL HEAT APPLIED PER PROCEDURES. UPON LEVEL OFF WHEN POWER LEVERS INCREASED, NOTED NR 3 ENGINE HAD EXPERIENCED FLAME-OUT. ATTEMPTED NR 3 ENGINE RESTART. ACCOMPLISHED ENGINE SHUT-DOWN PROCEDURE A ND AIRCRAFT PROCEEDED TO MEX, LANDING WITHOUT INCIDENT. REPLACED NR 3 ENGINE FUEL PUMP AND FUEL CONTROL. ACCOMPLISHED LEAK CHECK AND GROUND ENGINE RUN WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2 L 7 3 4F 4 F A3WE E2EA 1996022300265 19960223 00265 NM 1996 2 23 AALA960051 1 19960113 A 2810 SCREWS BOEING 727 727227 1384078 NM LT WING LOOSE A AALA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SW 07 716AA 20608 IAD - FLT 1267 - AFTER TAKEOFF IAD DURING CLIMB-OUT, FLUID NOTED LEAKING FROM AREA OF LT OUTBOARD AILERON. AIRCRAFT RET URNED TO IAD AND LANDED WITHOUT INCIDENT. RETORQUED LOOSE SCREWS AT THIRD FROM WING TIP UNDERWING FUEL TANK ACCESS PLAT E. SYSTEM GROUND CHECKED NORMAL OPERATION WITH NO LEAKS OR SEEPAGE NOTED. (X) 2 L 7 3 4F A3WE 1996022300266 19960223 00266 NM 1996 2 23 AALA960053 1 19960113 A 3260 WIRE BOEING 727 727227 1384078 NM RT MLG LOOSE A AALA K NONE N FALSE WARNING CR CRUISE 1 SW 07 728AA 20735 SJU - FLT 0450 - EN ROUTE MIA/SJU DURING CRUISE AT FL 330, RT MLG RED AND GREEN LIGHTS ILLUMINATED WITH LANDING GEAR HAN DLE IN THE OFF POSITION. NO OTHER ABNORMAL INDICATIONS NOTED. DESCENDING THROUGH FL 280 INTO SJU, THE LIGHTS EXTINGUIS HED AND THE AIRCRAFT LANDED SJU WITHOUT INCIDENT. RE-SPLICED TWO LOOSE WIRES ON THE RT MLG DOWNLOCK SENSOR. SYSTEM GRO UND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1996022300267 19960223 00267 EU 1996 2 23 AALA960061 1 19960116 A 3350 LIGHT STRIP FOKKER F28 F28MK0100 4990807 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1427A 11412 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY HAD ONE BULB INOPERATIVE. REPLACED EMERGENCY FLO OR LIGHT STRIP BY FORWARD GALLEY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT 1996022300268 19960223 00268 WP 1996 2 23 AALA960064 1 19960110 A 5320 5852105 ROLLER TRAY DOUG DC10 DC1010 3022110 WP BS 1631-1661 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 TUL - CORROSION IN ROLLER TRAY BETWEEN STA 1631 TO STA 1661. REPLACED ROLLER TRAY PER SRM 53-70-00. TST: 54,115.43 HO URS. CYCLES, 18,537. (X) 2 L 7 3 4F A22WE 1996022300269 19960223 00269 NM 1996 2 23 AALA960067 1 19960116 A 3231 AYG7378504N DOOR FITTING DOUG MD11 MD11 3023602 NM CENTER GEAR BROKEN A AALA O OTHER E VIBRATION/BUFFET CL CLIMB 1 SW 07 1759 48481 JFK - FLT 0050 - AFTER TAKEOFF DFW DURING CLIMB-OUT THROUGH FL 250, VIBRATION NOTED BY F/A'S IN AREA OF PASSENGER SEAT R OWS 25 TO 34. NO OTHER ABNORMAL INDICATIONS AND AIRCRAFT PROCEEDED TO JFK LANDING WITHOUT INCIDENT. REPLACED CENTER LA NDING GEAR RT DOOR AFT TRIPOD FITTING. ACCOMPLISHED CENTER LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F RT A22WE 1996022300270 19960223 00270 WP 1996 2 23 AALA960068 1 19960116 A 5741 FITTING DOUG DC10 DC1010 3022110 WP BS 1156 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 TUL - CAST FITTING BETWEEN LONGERONS 28 AND 29 AT STA 1156 ARE CRACKED FROM TOP AFT HOLE THROUGH FASTENER TO RADIUS. CU T OUT CRACKED AREA PER 53-30-00, PAGE 27. DRILLED REPAIR PARTS PER SRM 53-30-00, PAGE 27 AND PRIMED AND TREATED PARTS P ER SRM 51-21-01 AND INSTALLED REPAIR PER SRM 53-30-00, PAGE NR 7P27. TST: 54,115 HOURS. CYCLES, 18,537. (X) 2 L 7 3 4F A22WE 1996022300271 19960223 00271 WP 1996 2 23 AALA960069 1 19960116 A 5311 BELL FRAME DOUG DC10 DC1010 3022110 WP BS 959 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 TUL - CORROSION AT BELL FRAME LOWER FLANGE STA 959 NEAR STRINGER ATTACH POINT. MANUFACTURED AND INSTALLED DOUBLER PER R EPAIR SRM 53-30-00, PAGE 31, FIGURE 8, SHEET NR 1 AND 51-21-01. TST: 54,115. CYCLES, 18,537. (X) 2 L 7 3 4F A22WE 1996022300272 19960223 00272 WP 1996 2 23 AALA960093 1 19960109 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 795 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 TUL - SUPPORT UNDER MID-GALLEY BETWEEN SEAT TRACKS HAS CORROSION ON LAST INCH OF SUPPORT. BLENDED, ALODINED, PAINTED PE R FSO 7349. TST: 54,175. CYCLES, 18,535. (X) 2 L 7 3 4F A22WE 1996022300273 19960223 00273 NM 1996 2 23 AALA96010 1 19960121 A 5210 BOLT BOEING 757 757223 1384957 NM L1 DOOR MISSING A A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 628AA 24586 SAN - FLT 0509 - AT THE GATE AFTER ARRIVAL, UNABLE TO OPEN L1 DOOR. PASSENGERS DEPLANED THROUGH R1 DOOR. REPLACED BOLT AND BUSHING FOUND MISSING FROM UPPER END OF L1 DOOR HANDLE LINKAGE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1996022300274 19960223 00274 WP 1996 2 23 AALA960115 1 19960119 A 3350 A3030398101 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 494AA 49732 DFW - DURING OVERNIGHT CHECK, DISCOVERED EMERGENCY FLOOR LIGHTS IN FIRST CLASS CABIN INOPERATIVE. RESECURED LOOSE EMERG ENCY FLOOR LIGHT CONNECTOR AT FORWARD PART OF FIRST CLASS CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1996022300275 19960223 00275 WP 1996 2 23 AALA960116 1 19960120 A 3350 LIGHT STRIP DOUG DC9 DC982 3022082 WP CABIN MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 476AA 49651 ATL - DURING OVERNIGHT CHECK, DISCOVERED EMERGENCY FLOOR LIGHT STRIP BETWEEN PASSENGER SEAT ROWS 28 AND 32 MISSING. REP LACED EMERGENCY FLOOR LIGHT STRIP BETWEEN PASSENGER SEAT ROWS 28 AND 32. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1996022300276 19960223 00276 WP 1996 2 23 AALA960118 1 19960121 A 3397 WIRE DOUG DC9 DC983 3022083 WP TAIL CONE SHORTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 571AA 49353 SFO - DURING OVERNIGHT CHECK, DISCOVERED EMERGENCY LIGHT ABOVE TAIL CONE SLIDE INOPERATIVE. REPAIRED SHORTED WIRES AT A FT RT UPPER AIR CONDITIONING BAY WIRE CLAMP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A6WE 1996022300277 19960223 00277 EU 1996 2 23 AALA960119 1 19960121 A 3230 D226550002 DAMPER ASSY MENASCO AIRBUS 300 A300B4605R 3930308 EU LT MLG DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 7083A B313 645 SJU - FLT 0699 - AFTER TAKEOFF SJU, UNABLE TO RETRACT LANDING GEAR USING EITHER SYSTEM 1 OR SYSTEM 2. AIRCRAFT RETURNED TO SJU AND LANDED WITHOUT INCIDENT. REPLACED LT MLG PITCH DAMPER ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. ( X) 2 L 7 2 4F RT A35EU 1996022300278 19960223 00278 WP 1996 2 23 AALA960123 1 19960123 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 833 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 TUL - TWO INCHES OF SUPPORT CORRODED, NO PREVIOUS MODS. REPLACED SECTION OF TRACK PER FS07349. TST: 54,115.43 HOURS. CYCLES, 18,537. (X) 2 L 7 3 4F A22WE 1996022300279 19960223 00279 EU 1996 2 23 AALA960125 1 19960124 A 3234 715391 SEQUENCE VALVE FOKKER F28 F28MK0100 4990807 EU NLG DEFECTIVE A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 07 1440A 11435 DFW - FLT 1175 - DURING APPROACH TO DFW WHEN LANDING GEAR EXTENDED, NLG DID NOT EXTEND. RECYCLED LANDING GEAR WITH SAME RESULTS. ACCOMPLISHED ALTERNATE LANDING GEAR EXTENSION PROCEDURE AND AIRCRAFT LANDED DFW WITHOUT INCIDENT. REPLACED N LG SEQUENCE VALVE. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED, NORMAL OPE RATION. (X) 2 L 7 2 4F RT 1996022300280 19960223 00280 WP 1996 2 23 AALA960126 1 19960124 A 3350 A3030398101 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 434AA 49452 DFW - DURING OVERNIGHT CHECK, DISCOVERED EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY INOPERATIVE. RESECURED LOOSE EMERGENC Y FLOOR LIGHT CONNECTOR AT FORWARD END OF FIRST CLASS CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1996022300281 19960223 00281 WP 1996 2 23 AALA960128 1 19960123 A 3222 ACG7002503 INNER CYLINDER DOUG DC10 DC1010 3022110 WP NLG STRUT CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 160AA 24679 46710 LAX - DURING B-CHECK, CRACK FOUND ON NLG INNER CYLINDER AT AFT SIDE OF GEAR NEAR LOWER TORQUE LINK. REPLACED NLG INNER CYLINDER. SERVICED NLG STRUT WITH OIL AND NITROGEN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A22WE 1996022300282 19960223 00282 WP 1996 2 23 AALA960134 1 19960125 A 3350 L201011 LIGHT DOUG DC9 DC982 3022082 WP L1 DOOR DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 559AA 53089 MIA - DURING OVERNIGHT CHECK, DISCOVERED EMERGENCY LIGHT AT L1 DOOR INOPERATIVE. REPLACED EMERGENCY LIGHT AT L1 DOOR. S YSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1996022300283 19960223 00283 WP 1996 2 23 AALA960135 1 19960125 A 2121 WIRE DOUG DC9 DC982 3022082 WP LT ACM BAY SHORTED A A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 553AA 53083 ORD - DURING MAINTENANCE TO REPAIR AN INOPERATIVE LT AIR CYCLE MACHINE COOLING FAN PREVIOUSLY PLACARDED INOP AT DFW/24, FOUND COOLING FAN WIRE BUNDLE SHORTED AND BURNED DUE TO CHAFING AT FIRST CLAMP AND BRACKET. REPLACED LT ACM COOLING FAN , REPLACED ELECTRICAL CONNECTOR AND REPAIRED WIRE BUNDLE BY REPLACING WIRE FROM P1-173 CONNECTOR TO FIRST SPLICE. OPERA TED LT ACM WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1996022300284 19960223 00284 NM 1996 2 23 AALA960136 1 19960125 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 824-919 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1750B 48419 AT STA 824 - STA 919, NR 4 SEAT TRACK HAS CORROSION AT LAV\GALLEY TIE-DOWN AREAS AND FLOORBOARD SUPPORT EARS. INSTALLED NEW SEAT TRACK SECTION PER SRM 53-70-00, PAGES 3-4, FIGURE 1, SHEETS 1-2. (X) 2 L 7 3 4F RT A22WE 1996022300285 19960223 00285 NM 1996 2 23 AALA960146 1 19960126 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 358-361 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1750B 48419 CORRODED AT STA 358 TO STA 361 WHERE LAV 'B' ATTACHES TO TRACK AT OUTBOARD FORWARD CORNER OF NR 8 SEAT TRACK. REPAIRED SEAT TRACK PER SRM 53-70-00, FIGURE 4, PAGES 8 AND 9. (X) 2 L 7 3 4F RT A22WE 1996022300286 19960223 00286 WP 1996 2 23 AALA960151 1 19960129 A 3222 5920629519 PISTON DOUG DC9 DC982 3022082 WP NLG STRUT DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 457AA 49562 DFW - FLT 1116 - AFTER TAKEOFF DFW WHEN LANDING GEAR RETRACTED, NLG FAILED TO RETRACT. AIRCRAFT RETURNED TO DFW AND LAN DED WITHOUT INCIDENT. REPLACED NLG STRUT INNER CYLINDER. ALSO, REPLACED NLG RETRACTION ACTUATOR. SERVICED NLG STRUT W ITH OIL AND NITROGEN. ACCOMPLISHED LEAK AND GROUND CHECKS WITH NO DEFECTS FOUND. ACCOMPLISHED FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS FOUND. SYSTEM OPERATIONAL CHECKED NORMAL. (X) 2 L 7 2 4F A6WE 1996022300287 19960223 00287 WP 1996 2 23 AALA960152 1 19960128 A 2170 COALESCER BAG DOUG DC9 DC982 3022082 WP CABIN CONTAMINATED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 437AA 49455 BNA - FLT 2075 - AFTER TAKEOFF BNA WITH APU PLACARDED INOPERATIVE DUE TO OIL LOSS, SMOKE NOTED IN CABIN AND COCKPIT. AI RCRAFT RETURNED TO BNA AND LANDED WITHOUT INCIDENT. REPLACED ALL COALESCER BAGS AND ACCOMPLISHED GROUND ENGINE RUN AND PACK BURN-OUT PROCEDURE WITH NO SMOKE NOTED. AIRCRAFT RETURNED TO SERVICE AND APU SUBSEQUENTLY REPLACED AT ORD/29. (X) 2 L 7 2 4F A6WE 1996022300288 19960223 00288 WP 1996 2 23 AALA960155 1 19960129 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG REQUIRED SERVICE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 479AA 49654 ORD - FLT 1387 - AFTER TAKEOFF ORD WHEN LANDING GEAR RETRACTED, NLG DID NOT LOCK UP AND RED LIGHT REMAINED ILLUMINATED. RECYCLED LANDING GEAR MULTIPLE TIMES WITH SAME RESULT. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. SERVICED NLG STRUT WITH OIL AND NITROGEN. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHEC KED NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1996022300289 19960223 00289 WP 1996 2 23 AALA960160 1 19960130 A 3260 833703 SENSOR ELDEC DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA K NONE N FALSE WARNING CL CLIMB 1 SW 07 70404 49315 DFW - FLT T0264 - AFTER TAKEOFF PHX DURING CLIMB-OUT AT 310 KNOTS, RED NLG LIGHT ILLUMINATED BRIEFLY AND THEN EXTINGUISH ED. NO OTHER ABNORMAL INDICATIONS AND AIRCRAFT PROCEEDED TO DFW LANDING WITHOUT INCIDENT. REPLACED NLG UPLOCK SENSOR. ACCOMPLISHED NLG RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1996022300290 19960223 00290 WP 1996 2 23 AALA960162 1 19960129 A 3220 59104475071 GEAR ASSY DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 431AA CP1206 49343 MCO - FLT 1183 - AFTER TAKEOFF MCO WHEN LANDING GEAR RETRACTED, NLG FAILED TO RETRACT. AIRCRAFT RETURNED MCO AND LANDED WITHOUT INCIDENT. AIRCRAFT GEAR DOWN MAINTENANCE FERRY MCO/TUL. REPLACED NLG ASSY. ACCOMPLISHED LANDING GEAR RETRACT ION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1996022300291 19960223 00291 EU 1996 2 23 AWXA950043 1 19960203 A 5347 ASNA2495 SEAT TRACK AIRBUS 320 A320231 3930325 EU BS 8077 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 635AW 092 PAE - FLT 3851 - DURING SCHEDULED C-4 MAINTENANCE CHECK, FOUND SPOT CORROSION AT SEAT TRACK BS 8077, IFR 20 Y-765. FABR ICATED AND REPAIRED PER SRM 53-11-15. AIRCRAFT TT, 15,138 HOURS. AIRCRAFT TC, 7,863. (X) 2 L 7 2 4F RT A28NM 1996022300292 19960223 00292 NM 1996 2 23 AWXA960027 1 19960122 A 5230 10608214 SEAL BOEING 737 7373S3 1384711 NM AFT CARGO DOOR LOOSE A AWXA O OTHER O OTHER DE DESCENT 1 WP 28 315AW 23734 SJC-PHX - FLT NR 202 - DURING DESCENT THROUGH 5000 FEET, LOST PRESSURE IN CABIN. DESCENDED AT 2000 FPM, CABIN WAS CONTR OLLABLE IN MANUAL. FOUND AFT CARGO DOOR SEAL PULLED LOOSE, SECURED. LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996022300293 19960223 00293 NM 1996 2 23 AWXA960031 1 19960124 A 3213 654610021 STRUT BOEING 737 7372M8 1384483 NM RT MLG LOW PRESSURE A AWXA C D ABORTED TAKEOFF RETURN TO BLOCK E VIBRATION/BUFFET TO TAKEOFF 1 WP 28 141AW MC01258P667 21955 DEN/PHX - FLT 0491 - ABORTED TAKEOFF. ON TAKEOFF ROLL, FELT LIKE AIRCRAFT HAD FLAT TIRE AND AIRCRAFT NEEDED LEFT RUDDER TO STAY STRAIGHT. CONTRACT MAINTENANCE CHECKED ALL MAIN TIRES AND BRAKES. SPIN CHECK GOOD. ADJUSTED STRUT PRESSURE 5 0 PSI. CHECKED FLIGHT CONTROL MOVEMENT. ALL TIRE PRESSURES GOOD. (X) 2 L 7 2 4F A16WE 1996022300294 19960223 00294 NM 1996 2 23 AWXA960037 1 19960131 A 5230 6547952524 SKIN BOEING 737 7373G7 1384595 NM AFT CARGO DOOR GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 1265 23778 PAE - FLT 3846 - DURING SCHEDULED C-10 MAINTENANCE CHECK, FOUND GOUGE IN AFT CARGO DOOR SKIN AT STA 810, WL 246 (.012 IN CH BY 6 INCHES). REPLACED AFT CARGO DOOR SKIN ON WORK ORDER 212404 Z-4. AIRCRAFT TT, 27,949 HOURS. AIRCRAFT TC, 21,76 4. (X) 2 L 7 2 4F RT A16WE 1996022300295 19960223 00295 NM 1996 2 23 AWXA960038 1 19960131 A 5330 SKIN BOEING 737 7373G7 1384595 NM BS 304 DAMAGED A AWXA K NONE C F.O.D. IN INSP/MAINT 1 WP 28 156AW 23778 PAE - FLT 3846 - DURING SCHEDULED C-10 MAINTENANCE CHECK, FOUND LIGHTNING STRIKE IN SKIN AT STA 304, ABOVE STR 22 RT. R EMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, ALODINED, PRIMED, AND INSTALLED DOUBLER AT BS 304 BETWEEN STR 21 AND STR 2 2 RT, IAW SRM 53-00-01, FIGURE 202. AIRCRAFT TT, 27,949 HOURS. AIRCRAFT TC, 21,764. (X) 2 L 7 2 4F RT A16WE 1996022300296 19960223 00296 NM 1996 2 23 AWXA960039 1 19960130 A 5330 SKIN BOEING 737 7373G7 1384595 NM BS 307 GOUGE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 PAE - FLT 3846 - DURING SCHEDULED C-10 MAINTENANCE CHECK, FOUND GOUGE IN SKIN AT STA 307 BETWEEN STR 18 AND STR 19 RT, ( .070 INCH BY .25 INCH). REMOVED DAMAGED AREA 1.2 INCHES BY 1.5 INCHES. FABRICATED AND INSTALLED REPAIR PER SRM 53-00-0 1, FIGURE 202. AIRCRAFT TT, 27,949 HOURS. AIRCRAFT TC, 21,764. (X) 2 L 7 2 4F RT A16WE 1996022300297 19960223 00297 EU 1996 2 23 AWXA960044 1 19960203 A 5347 SEAT TRACK AIRBUS 320 A320231 3930325 EU BS 6877-7177 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 635AW 092 PAE - FLT 3851 - DURING SCHEDULED C-4 MAINTENANCE CHECK, FOUND CORROSION ON TOP SURFACE OF RAIL STA 6877 TO STA 7177 Y+ 500-2240. FABRICATED AND INSTALLED REPAIR PER SRM 53-00-14, FIGURE 204. AIRCRAFT TT, 15,138 HOURS. AIRCRAFT TC, 7,863 . (X) 2 L 7 2 4F RT A28NM 1996022300298 19960223 00298 EU 1996 2 23 AWXA960045 1 19960203 A 5347 ASNA2495 SEAT TRACK AIRBUS 320 A320231 3930325 EU BS 8077 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 635AW 092 PAE - FLT 3851 - DURING SCHEDULED C-4 MAINTENANCE CHECK, FOUND CORROSION AT SEAT TRACK BS 8077, IFR 20Y - 1292 - 2489. S PLICED REPAIR PER SRM 53-11-15. AIRCRAFT TT, 15,138 HOURS. AIRCRAFT TC, 7,863. (X) 2 L 7 2 4F RT A28NM 1996022300299 19960223 00299 EU 1996 2 23 AWXA960051 1 19960205 A 5347 SEAT TRACK AIRBUS 320 A320231 3930325 EU BS 8077-8277 CORROSION A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 636AW 098 PAE - FLT 3841 - DURING SCHEDULED C-4, S-1 MAINTENANCE CHECK, FOUND CORROSION ON SEAT RAIL, STA 8077 TO STA 8227, Y-765, Z-240. REMOVED CORROSION ON SEAT RAIL AT BS 8077 - BS 8227, Y-765, Z-240. FABRICATED REPAIR PARTS IAW SRM 53-11-15, F IGURE 204. ALODINED, PRIMED, AND INSTALLED REPAIR PARTS IAW SRM 53-11-15, FIGURE 204. AIRCRAFT TT, 15,146 HOURS. AIRCR AFT TC,7,702. (X) 2 L 7 2 4F RT A28NM 1996022300300 19960223 00300 EU 1996 2 23 AWXA960052 1 19960206 A 5320 TRACK AIRBUS 320 A320231 3930325 EU BS 7830 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 636AW 098 PAE - FLT 3851 - DURING SCHEDULED C-4, S-1 MAINTENANCE CHECK, FOUND CORROSION ON RT SIDE OF FLIGHT DECK DOOR STA 7830, Y -254, Z-240. REPAIRED TRACK PER SRM 53-11-14, FIGURE 201. AIRCRAFT TT, 15,138 HOURS. AIRCRAFT TC, 7,863. (X) 2 L 7 2 4F RT A28NM 1996022300301 19960223 00301 NE 1996 2 23 TWRA9606 2 19960203 A 7261 OIL SYSTEM BOEING 747 747238B 1384828 NM PWA JT9 JT9D7F 52054 NE NR 3 ENGINE LOW SERVICE A TWRA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 614FF 20534 663041 GRU - FLT 60 - DURING CLIMB-OUT OF GRU, FLIGHT CREW REPORTED IFSD OF NR 3 ENGINE DUE TO LOW OIL PRESSURE (ZERO). AIRCRA FT RETURNED TO GRU. MCC WAS NOTIFIED. WHILE ON THE GROUND AT GRU, MAINTENANCE CHECKED CHIP DETECTORS AND ADDED 6 GALLO NS OF OIL. HIGH POWER RUN-UP WAS PERFORMED AND NO LEAKS FOUND. OIL QUANTITY OK. OIL PRESSURE AND TEMP OK. AIRCRAFT W AS RELEASED FOR FLIGHT. (X) 2 L 7 4 4F 4 F A20WE E20EA 1996022300302 19960223 00302 NE 1996 2 23 HEEA966589 1 19960131 A 6210 7615009043051 TIP CAP SKRSKY S76 S76A 8143006 NE M/R BLADE SEPARATION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22342 760096 FIBERGLASS BROKEN BETWEEN INNER DOUBLER AND OUTER DOUBLER, WITH SOME SEPARATION ON THE LEADING EDGE ABRASION STRIP ON TH E UPPER SURFACE. 1 G 7 2 3U H1NE 1996022300303 19960223 00303 1996 2 23 HEEA966590 4 19960131 A 2370 9806019001 CVR BELL 212 212 1181420 SW COCKPIT WONT TEST E HEEA K NONE L NO TEST NR NOT REPORTED 1 SW 03 102PH 2757 30899 CVR WILL NOT TEST. 1 G 7 1 4U H4SW 1996022300304 19960223 00304 SW 1996 2 23 HEEA966595 1 19960202 A 6210 206010200133 BLADE BELL 206 206B 1181511 SW M/R CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2276B 3257 3628 BLADE HAS EXCESSIVE AMOUNT OF EXFOLIATION OF THE LEADING EDGE. 1 G 7 1 3U H2SW 1996022300305 19960223 00305 SW 1996 2 23 HEEA966597 1 19960202 A 3212 214073929105 FLOAT VALVE BELL 214 214ST 1182106 SW FITTING LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 FLOAT VALVE LEAKING OUT OF OUTPORT FITTING AFTER MANUAL INFLATION. S/N 1 &S/N 9 2 G 7 2 4U H10SW 1996022300306 19960223 00306 1996 2 23 HEEA966598 4 19960202 A 3452 066106200 TRANSCEIVER KT76 BELL 206 206L 1181522 SW COCKPIT ATC DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 62127 52023 INTERMITTENT SIGNAL. FOUND V101 CAVITY OSCILLATOR WEAK. REPLACED V101 CAVITY OSCILLATOR. ADJUSTED POWER OUT AND FREQUE NCY TO SPECS. BENCH CHECK GOOD. 1 G 7 1 3U H2SW 1996022300307 19960223 00307 1996 2 23 HEEA966599 4 19960202 A 3452 066106200 TRANSCEIVER KT76 BELL 206 206L1 1182107 SW CCOCKPIT ATC INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1078G 45398 TRANSPONDER INOPERATIVE. REPLACED DETERIORATED RESISTOR R477. REPLACED PHOTOCELL V301 DUE TO WEAK REPLY LIGHT. REPAIRE D. COOKED UNIT. FOUND MTL TO BE BELOW SPECS. ALIGNED RECEIVER. REPAIRED. BENCH CHECK GOOD. 1 G 7 1 3U H2SW 1996022300308 19960223 00308 SW 1996 2 23 HEEA966600 1 19960202 A 7714 206075681117 INDICATOR BELL 206 206L 1181522 SW DUAL TACH DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 21497 51518 TURBINE NEEDLE HAS NO INDICATION. TIME SINCE REPAIR 10:55. 1 G 7 1 3U H2SW 1996022300309 19960223 00309 1996 2 23 HEEA966601 4 19960202 A 3453 25410036 LORAN 7000RCU BELL 412 412 1182202 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2261D 33076 LORAN FLASHES ADVISORY WARNING LIGHT. 1 G 7 2 4U H4SW 1996022300310 19960223 00310 1996 2 23 HEEA966602 4 19960202 A 2370 9806019001 CVR BELL 214 214ST 1182106 SW COCKPIT WONT TEST E HEEA K NONE L NO TEST NR NOT REPORTED 1 SW 03 5748M 3545 28102 CVR WILL NOT TEST. 2 G 7 2 4U H10SW 1996022300311 19960223 00311 NE 1996 2 23 HEEA966603 1 19960202 A 2435 230811011 ARMATURE 23081018 SKRSKY S76 S76A 8143006 NE START/GEN DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 528 ARMATURE CAUSES EXCESSIVE ARCHING WHEN TESTING. 1 G 7 2 3U H1NE 1996022300312 19960223 00312 SW 1996 2 23 HEEA966604 1 19960202 A 2435 230811010 ARMATURE 23081018 BELL 206 206L1 1182107 SW START/GEN DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 997 ARMATURE CAUSES EXCESSIVE ARCHING WHEN TESTING. 1 G 7 1 3U H2SW 1996022300313 19960223 00313 SW 1996 2 23 HEEA966605 1 19960202 A 6230 206010450113 SWASHPLATE BELL 206 206L1 1182107 SW M/R SEAL SPUN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5737T 15038 45454 SEAL SPUN IN OUTER CAP (WORN) 1 EACH 206-010-444-001 OUTER CAP, T.T. UNKNOWN 1 EACH 206-010-460-001 SEAL, T.T. 38:15. REPLACED WITH SERVICEABLE PARTS. 1 G 7 1 3U H2SW 1996022300314 19960223 00314 1996 2 23 HEEA966606 4 19960205 A 2312 069102525 TRANSCEIVER KX165 BOLKMS 105 BO105S 5626006 EU COCKPIT INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 135AE 36 S838 RADIO INOPERATIVE. 1 G 7 2 3U H3EU 1996022300315 19960223 00315 1996 2 23 HEEA966607 4 19960205 A 2312 064105430 TRANSCEIVER SNIAS 350 AS350B2 8680813 EU COCKPIT VHF DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 6100R 527 2862 VHF RADIO TRANSMITTER HAS LOUD BACKGROUND NOISE, RECEIVER IS GOOD. 1 G 7 1 3U H9EU 1996022300316 19960223 00316 SW 1996 2 23 HEEA966608 1 19960205 A 6220 412010124109 BOLT 412010100193 BELL 412 412 1182202 SW M/R FLAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7128R 3431 AAD50028 36007 BOLT TUNGSTEN CARBIDE COATING FLAKING. S/N A557 & A60 1 G 7 2 4U H4SW 1996022300317 19960223 00317 SW 1996 2 23 HEEA966609 1 19960205 A 6220 412010124109 BOLT 412010100193 BELL 412 412 1182202 SW M/R DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z 2846 AAD50026 36019 BOLT COATING CHIPPING. 1 G 7 2 4U H4SW 1996022300318 19960223 00318 1996 2 23 HEEA966610 4 19960205 A 2312 064105430 TRANSCEIVER BOLKMS 105 BO105S 5626006 EU COCKPIT INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 205UC S668 ON FIRST FLIGHT OF THE DAY, UNIT WENT INOPERATIVE. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1996022300319 19960223 00319 EU 1996 2 23 HEEA966611 1 19960205 A 7722 56265550011 INDICATOR AEROSP AS355 AS355F1 8680810 EU COCKPIT T4 ERROR E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5793Y 5141 CHECKED INDICATOR USING BARFIELD T-1000 AND FOUND INDICATOR 40 DEGREES OFF. INDICATOR COULD NOT BE ADJUSTED. ADJUSTME NT SCREW IS STRIPPED OUT AND PUSHED IN. 1 G 7 2 3U H11EU 1996022300320 19960223 00320 EU 1996 2 23 HEEA966612 1 19960205 A 2844 81141010010 TRANSMITTER AEROSP AS355 AS355F2 8680812 EU FUEL SYS FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 6040U 5474 FUEL PRESSURE TRANSMITTER DROPS TO ZERO PRESSURE. 1 G 7 2 3U H11EU 1996022300321 19960223 00321 EU 1996 2 23 HEEA966613 1 19960205 A 6400 AE99296F COUPLING O-RING BOLKMS 117 BK117B1 5626012 EU T/R LEAK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 117BK 7229 T/R COUPLING HALF O-RING OUT OF CENTER HOLE, LEAKS. 1 G 7 2 3U H13EU 1996022300322 19960223 00322 EU 1996 2 23 HEEA966614 1 19960205 A 3213 350A41108700 CROSSTUBE SNIAS 350 AS350B2 8680813 EU LT AFT SKID CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4000L 12 2873 BOLT HOLE CRACKED AT L/H AFT MOUNTING HOLE TO SKIDTUBE AT AFT CROSSTUBE. 1 G 7 1 3U H9EU 1996022300323 19960223 00323 SW 1996 2 23 HEEA966615 1 19960205 A 3212 214052200105 FLOAT BELL 214 214ST 1182106 SW FWD LT TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 FLOAT UNIT TORN. SENT TO A/C FUEL CELLS FOR GIRT PATTERN FOR P/N 214-052-200-102 2 G 7 2 4U H10SW 1996022300324 19960223 00324 1996 2 23 HEEA966616 4 19960205 A 3413 7160 INDICATOR BOLKMS 117 BK117B1 5626012 EU COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 117BK 7229 VSI INDICATOR LEAKING. 1 G 7 2 3U H13EU 1996022300325 19960223 00325 1996 2 23 HEEA966617 4 19960205 A 3416 B4553110104 ALTIMETER BOLKMS 117 BK117B1 5626012 EU COCKPIT LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 117BK 7229 ALTIMETER LEAKING. 1 G 7 2 3U H13EU 1996022300326 19960223 00326 EU 1996 2 23 HEEA966618 1 19960205 A 6420 350A33211905 HUB SNIAS 350 AS350B2 8680813 EU T/R BEARING FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100U 345 2863 LAMINATE BEARING SEPARATED. HIGH FREQUENCY VIBERATION. 1 G 7 1 3U H9EU 1996022300327 19960223 00327 NE 1996 2 23 HEEA966619 1 19960205 A 7931 7645001078119 TRANSMITTER SKRSKY S76 S76A 8143006 NE ENG OIL LEAKING E HEEA K NONE K FLUID LOSS NR NOT REPORTED 1 SW 03 22342 760096 PRESS TRANSMITTER SEEPING OIL AT CONNECTORS. 1 G 7 2 3U H1NE 1996022300328 19960223 00328 NE 1996 2 23 HEEA966620 1 19960205 A 7931 7645001078119 TRANSMITTER SKRSKY S76 S76A 8143006 NE ENG OIL OIL SEEP E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 22342 760096 OIL SEEPING OUT OF WEEP HOLE. 1 G 7 2 3U H1NE 1996022300329 19960223 00329 NE 1996 2 23 HEEA966621 1 19960205 A 6322 7630807902106 BLOWER SKRSKY S76 S76A 8143006 NE OIL COOLER DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22342 760096 ENGINE OIL TEMP HIGH. OIL COOLER DIRTY AND SCORED. 1 G 7 2 3U H1NE 1996022300330 19960223 00330 1996 2 23 HEEA966622 4 19960205 A 3444 54025100034 ALERTER BEECH 200 200CBEECH 1152926 CE COCKPIT DAMAGED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 39PH BL3 HARD SPOTS DURING RUN UP AND RUN DOWN. FACEPLATE IS CRACKED. 1 L 7 2 4T A24CE 1996022300331 19960223 00331 EU 1996 2 23 HEEA966623 1 19960205 A 6520 350A33020005 GEAR BOX SNIAS 350 AS350B2 8680813 EU T/R YOKE SEIZED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6097Z 1464 2820 COULD NOT REMOVE T/R YOKE ASSEMBLY FROM GEARBOX ASSEMBLY. 1 G 7 1 3U H9EU 1996022300332 19960223 00332 1996 2 23 HEEA966624 4 19960205 A 3422 5208100001 GYRO BOLKMS 105 BO105S 5626006 EU COCKPIT DG DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 90752 S156 DG GYRO SLAVE INDICATOR DOESN'T WORK PROPERLY; IT FLUCTUATES. 1 G 7 2 3U H3EU 1996022300333 19960223 00333 NE 1996 2 23 HEEA966625 1 19960205 A 7810 7630507003044 EJECTOR SKRSKY S76 S76A 8143006 NE EXHAUST CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 792CH 760193 EXH EJECTOR IS CRACKED. 1 G 7 2 3U H1NE 1996022300334 19960223 00334 1996 2 23 HEEA966626 4 19960205 A 3444 7001840913 TRANSCEIVER BELL 212 212 1181420 SW COCKPIT INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5736J 31140 TRANSCEIVER INOPERATIVE AFTER 2 MINUTES TIME; DROPS OFF. 1 G 7 1 4U H4SW 1996022300335 19960223 00335 1996 2 23 HEEA966627 4 19960205 A 3416 8140BS20LW5V ALTIMETER SKRSKY S76 S76A 8143006 NE COCKPIT ENCODER ERRATIC E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1547D 760077 ENCODER OUTPUT BECOMES ERRATIC AFTER UNIT WARMS UP. 1 G 7 2 3U H1NE 1996022300336 19960223 00336 SW 1996 2 23 HEEA966628 1 19960205 A 6240 206075681105 INDICATOR BELL 206 206L1 1182107 SW DUAL TACH FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1072T 45385 INDICATOR FAILED NO ROTOR OR TURBINE INDICATION. 1 G 7 1 3U H2SW 1996022300337 19960223 00337 SW 1996 2 23 HEEA966629 1 19960205 A 2436 206075447007 REGULATOR BELL 206 206L3 1182108 SW DC SYS FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3108E 51498 INTERMITTENTLY FALLS OFF LINE AFTER UNIT WARMS UP. IF TURNED OFF IT WILL NOT COME ON LINE. VOLTAGE KEPT GOING UP TO 3 0 VOLTS. 1 G 7 1 3U H2SW 1996022300338 19960223 00338 EU 1996 2 23 HEEA966630 1 19960205 A 7931 81071010012 TRANSMITTER AEROSP AS355 AS355F1 8680810 EU ENG OIL FLUCTUATES E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5774M 5009 TRANSMITTER FLUCTUATES AT IDLE SPEED. 1 G 7 2 3U H11EU 1996022300339 19960223 00339 SW 1996 2 23 HEEA966631 1 19960205 A 7931 222375077111 TRANSMITTER BELL 214 214ST 1182106 SW ENG OIL DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3897N 28106 OIL PRESSURE GAUGE FLUCTUATING. 2 G 7 2 4U H10SW 1996022300340 19960223 00340 SW 1996 2 23 HEEA966632 1 19960205 A 6240 2360016901 INDICATOR BELL 206 206L3 1182108 SW M/R DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 31821 51076 INDICATOR ROTOR WILL NOT SPIN AND BEARING IS BAD. 1 G 7 1 3U H2SW 1996022300341 19960223 00341 SW 1996 2 23 HEEA966633 1 19960205 A 5260 FYLM735023 MOTOR ASSY BELL 412 412 1182202 SW STEP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893P 33012 MOTOR ARMATURE HAS A DEAD SPOT. 1 G 7 2 4U H4SW 1996022300342 19960223 00342 SW 1996 2 23 HEEA966634 1 19960205 A 2430 51509002R CONTROL UNIT BELL 212 212 1181420 SW DC SYS DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1079U 31122 #2 GENERATOR KICKS OFF LINE WHEN ANY INVERTER IS TURNED ON. 1 G 7 1 4U H4SW 1996022300343 19960223 00343 SW 1996 2 23 HEEA966635 1 19960205 A 2430 51509002R CONTROL UNIT BELL 412 412 1182202 SW DC SYS DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 7128R 36007 CONTROL UNIT DEFECTIVE. UNABLE TO PARALLEL. 1 G 7 2 4U H4SW 1996022300344 19960223 00344 SW 1996 2 23 HEEA966636 1 19960205 A 2430 51509002R CONTROL UNIT BELL 212 212 1181420 SW DC SYS DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1079U 31122 CONTROL UNIT DEFECTIVE. GENERATOR WOULD NOT COME ON LINE. 1 G 7 1 4U H4SW 1996022300345 19960223 00345 SW 1996 2 23 HEEA966637 1 19960205 A 2430 51509002R CONTROL UNIT BELL 212 212 1181420 SW DC SYS DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 102PH 30899 CONTROL UNIT VOLT ADJUSTMENT SCREW BROKEN. 1 G 7 1 4U H4SW 1996022300346 19960223 00346 SW 1996 2 23 HEEA966638 1 19960205 A 2430 51509002R CONTROL UNIT BELL 412 412 1182202 SW DC SYS FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2014K 33020 CONTROL UNIT FAILED. #2 DC GENERATOR INOPERATIVE. 1 G 7 2 4U H4SW 1996022300347 19960223 00347 NE 1996 2 23 HEEA966639 1 19960205 A 2430 7655009006105 CONTROL UNIT SKRSKY S76 S76A 8143006 NE DC SYS DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1545X 760050 CONTROL UNIT DEFECTIVE. #2 D.C. GENERATOR WOULD NOT COME ON LINE. 1 G 7 2 3U H1NE 1996022300348 19960223 00348 EU 1996 2 23 HEEA966640 1 19960205 A 7931 10593975 SWITCH BOLKMS 105 BO105S 5626006 EU OIL COOLER DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 4302G S853 PRESSURE SWITCH DEFECTIVE. OIL COOLER LIGHT DOESN'T COME ON WHEN SHUT DOWN. 1 G 7 2 3U H3EU 1996022300349 19960223 00349 EU 1996 2 23 HEEA966641 2 19960205 A 7510 1092T1002W SERVOMOTOR BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENGINE INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 SERVO MOTOR INOPERATIVE. 1 G 7 2 3U 3 U H3EU E4CE 1996022300350 19960223 00350 SW 1996 2 23 HEEA966643 1 19960206 A 2100 222325009101 BLOWER BELL 230 230 1182149 SW RAM AIR DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 2765 23009 RAM AIR BLOWER INTERMITTENT OPERATION. 1 G 7 2 3U NC H9SW 1996022300351 19960223 00351 NE 1996 2 23 HEEA966644 1 19960206 A 6220 7610608000047 DAMPER SKRSKY S76 S76A 8143006 NE M/R WORN EXCESSIVELY E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22342 760096 DAMPER IS WORN EXCESSIVELY. (CYLINDER HAS WEAR) 1 G 7 2 3U H1NE 1996022300352 19960223 00352 NE 1996 2 23 HEEA966645 1 19960206 A 6320 7635109082105 CHIP DETECTOR SKRSKY S76 S76A 8143006 NE TRANSMISSION DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546G 760076 NO CONTINUITY BETWEEN PINS A AND B WHEN BRIDGING CHIP GAP AND CHECK FOR LEAKS AT ELECTRICAL CONNECTOR 1 G 7 2 3U H1NE 1996022300357 19960223 00357 1996 2 23 HEEA966650 4 19960206 A 3416 1003511424 ALTIMETER SKRSKY S76 S76A 8143006 NE COCKPIT STICKS E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3122H 760233 ALTIMETER INTERMITTENTLY STICKS WHEN DECREASING ALTITUDE. 1 G 7 2 3U H1NE 1996022300358 19960223 00358 NE 1996 2 23 HEEA966651 1 19960206 A 7810 7630507003044 EJECTOR SKRSKY S76 S76A 8143006 NE EXHAUST CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911MJ 760231 EXH EJECTOR IS CRACKED. 1 G 7 2 3U H1NE 1996022300359 19960223 00359 EU 1996 2 23 HEEA966652 1 19960206 A 2842 647511011 TRANSMITTER AEROSP AS355 AS355F2 8680812 EU FUEL QTY FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 6040U 5474 FUEL GAUGE READS "0". 1 G 7 2 3U H11EU 1996022300360 19960223 00360 1996 2 23 HEEA966653 4 19960206 A 3414 412075009105 INDICATOR BELL 412 412 1182202 SW COCKPIT AIRSPEED READS LOW E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3893P 33012 INDICATES 5 KNOTS LOW THROUGHOUT SCALE. SENT TO MASCO FOR INSPECTION AND REPAIR. 1 G 7 2 4U H4SW 1996022300361 19960223 00361 EU 1996 2 23 HEEA966654 1 19960206 A 2430 480GC01Y03 ELEC. BOX AEROSP AS355 AS355F1 8680810 EU DC SYS DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5793Y 5141 R/H GENERATOR WILL NOT COME ON LINE. 1 G 7 2 3U H11EU 1996022300362 19960223 00362 1996 2 23 HEEA966655 4 19960206 A 2210 2593996333 TARSYN 333 BELL 412 412 1182202 SW AUTO FLIGHT FAIL TEST E HEEA K NONE L NO TEST NR NOT REPORTED 1 SW 03 3893P 33012 FAILED FAST MCHRONIZATION RATE TEST #8.4 ON SST. 1 G 7 2 4U H4SW 1996022300363 19960223 00363 1996 2 23 HEEA966656 4 19960206 A 3416 A30 ENCODER ACK BOLKMS 105 BO105S 5626006 EU COCKPIT ERRATIC E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 54197 23 S805 ENCODER HAS ERRATIC OUTPUT. 1 G 7 2 3U H3EU 1996022300364 19960223 00364 1996 2 23 HEEA966657 4 19960206 A 2210 7000299901 CONTROL BELL 412 412 1182202 SW AUTOPILOT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 108X 33115 CPL LIGHT WILL NOT COME ON WHEN CPL SWITCH IS PUSHED. 1 G 7 2 4U H4SW 1996022300367 19960223 00367 SW 1996 2 23 HEEA966662 1 19960206 A 6330 206033506101 RESTRAINT BELL 206 206L1 1182107 SW TRANSMISSION WORN EXCESS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5742H 45476 RESTRAINT IS WORN EXCESSIVELY. (BEARING WORN) 1 G 7 1 3U H2SW 1996022300368 19960223 00368 1996 2 23 HEEA966663 4 19960206 A 2370 9806019001 CVR BELL 412 412 1182202 SW COCKPIT INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 2910 36002 CVR INOPERATIVE. 1 G 7 2 4U H4SW 1996022300369 19960223 00369 EU 1996 2 23 HEEA966664 1 19960206 A 7714 DL43638 INDICATOR BOLKMS 105 BO105S 5626006 EU TRIPLE TACH DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 911EB S812 #1 AND #2 NEEDLES HAVE A 10% TORQUE SPLIT. 1 G 7 2 3U H3EU 1996022300370 19960223 00370 NE 1996 2 23 HEEA966665 1 19960206 A 3610 7650007903102 VALVE SKRSKY S76 S76A 8143006 NE BLEED SOV DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 31219 493 760230 BLEED AIR ADVISORY LIGHT COMES ON WITH #1 ENGINE RUNNING AND #2 SHUTDOWN. VALVE LEAKING. 1 G 7 2 3U H1NE 1996022300371 19960223 00371 NM 1996 2 23 HEEA966666 1 19960206 A 6710 900900C301000810 COLLECTIVE STICK DOUG MD900 MD900 3027375 NM COPILOT GRIP DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 9214U 246 90000014 THROTTLE GRIPS ON PILOT AND COPILOTS COLLECTIVE STICKS ARE CRACKED AROUND SET SCREW AREA AND THE LOWER GRIP ON PILOTS ST ICK IS BROKEN COMPLETELY FREE. THROTTLE GRIP MOVES BUT FMV LINKAGE DOES NOT. PARTS NEEDED 2 UPPER GRIP ASSEMBLIES 1 LO WER GRIPASSEMBLY. 1 G 7 2 3U NC H19NM 1996022300372 19960223 00372 NM 1996 2 23 HEEA966667 1 19960206 A 6710 900C3010007109 COLLECTIVE STICK DOUG MD900 MD900 3027375 NM PILOT GRIP CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 9214U 246 90000014 THROTTLE GRIPS ON PILOT AND COPILOTS COLLECTIVE STICKS ARE CRACKED AROUND SET SCREW AREA AND THE LOWER GRIP ON PILOTS ST ICK IS BROKEN COMPLETELY FREE. THROTTLE GRIP MOVES BUT FMV LINKAGE DOES NOT. PARTS NEEDED 2 UPPER GRIP ASSEMBLIES 1 LO WER GRIPASSEMBLY. 1 G 7 2 3U NC H19NM 1996022300373 19960223 00373 NM 1996 2 23 HEEA966668 1 19960206 A 6710 900C3010007109 COLLECTIVE STICK DOUG MD900 MD900 3027375 NM GRIP CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 9214U 23 90000014 THROTTLE GRIPS ON COPILOTS COLLECTIVE STICKS ARE CRACKED AROUND SET SCREW AREA. PARTS NEEDED 1 UPPER GRIP ASSEMBLIES 1 LOWER GRIP ASSEMBLY. SENT TO MCDONNELL DOUGLAS...THEIR PROPERTY BEING RETURNED. 1 G 7 2 3U NC H19NM 1996022300374 19960223 00374 SW 1996 2 23 HEEA966669 1 19960208 A 6420 212011707103 RACE BELL 212 212 1181420 SW T/R CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 BEARING RACE IS CORRODED. 1 G 7 1 4U H4SW 1996022300375 19960223 00375 SW 1996 2 23 HEEA966674 1 19960208 A 6410 222016001111 BLADE 222012701117 BELL 230 230 1182149 SW T/R ERRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 236X 1074 A313 23015 T/R BLADE PAINT EROSION. S/N A542 &A547 1 G 7 2 3U NC H9SW 1996022300376 19960223 00376 SW 1996 2 23 HEEA966675 1 19960208 A 6410 206016201127 BLADE BELL 206 206L1 1182107 SW T/R PAINT PEEL E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2251A 483 45755 T/R BLADE PAINT PEELING. 1 G 7 1 3U H2SW 1996022300377 19960223 00377 SW 1996 2 23 HEEA966676 1 19960208 A 6410 212010750105 BLADE BELL 412 412 1182202 SW T/R PAINT PEEL E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911FD 942 33056 T/R BLADE PAINT PEELING AND FILLER MISSING. 1 G 7 2 4U H4SW 1996022300378 19960223 00378 NE 1996 2 23 HEEA966677 1 19960208 A 6210 7615009100049A BLADE SKRSKY S76 S76A 8143006 NE M/R STRAP SEPARATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31217 9509 760229 M/R BLADE TIP ATTACHMENT STRAP SEPARATED ON THE LOWER SIDE. 1 G 7 2 3U H1NE 1996022300379 19960223 00379 SW 1996 2 23 HEEA966678 1 19960209 A 6220 206011132113A GRIP 206011100159 BELL 206 206L 1181522 SW M/R HUB DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7074W 532 A1419 52033 M/R HUB REMOVED DUE TO GREASE LEAKAGE. AT DISASSEMBLY FOUND SEAL RETAINER P/N 206-011-129-003 UNBONDED CAUSING LEAK IN GRIP. FOUND RETAINER SEAT WORN. ALSO FOUND TRUNNION EXCESSIVELY TIGHT. FOUND THRUST PLUGS BREAKING DOWN. 1 G 7 1 3U H2SW 1996022300380 19960223 00380 SW 1996 2 23 HEEA966679 1 19960209 A 6320 204040386001 CASE ASSY 212040001191 BELL 212 212 1181420 SW TRANSMISSION CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2384 A1085 TRANSMISSION IS CORRODED. (CORROSION BEYOND LIMITS ON FLANGE) 1 G 7 1 4U H4SW 1996022300381 19960223 00381 GL 1996 2 23 HEEA966680 2 19960209 A 7250 6892828 SHIELD 23035128 BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL NR 1 NOZZLE DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8591X CAT97847 51495 CAE895558 UPON INSPECTION PER CEBA-72-3208 OF DALLAS AIRMOTIVE OH #1 NOZZLE SHIELD, NOTED THE FOLLOWING: DOME FAILED CHEMICAL CHE CK. 1 G 7 1 3U 3 U H2SW E1GL 1996022300382 19960223 00382 1996 2 23 HEEA966683 4 19960209 A 2312 064105430 TRANSCEIVER BELL 206 206B 1181511 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 39122 3312 TRANSCEIVER GOES OFF AND ON INTERMITTENTLY. 1 G 7 1 3U H2SW 1996022300392 19960223 00392 SW 1996 2 23 96ZZZX756 1 19960119 A 3231 LIMIT SWITCH MTSBSI MU2 MU2B30 5780410 SW WIRE DIAGRAM MISWIRED A H2OA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 05 617BB 5854 522 DURING TROUBLESHOOTING THE GEAR EXTENSION SYSTEM, AN ERROR WAS FOUND IN THE WIRING DIAGRAM ON PAGE 10-2 OF MITSUBISHI MM , YET 69016. WIRE LABELED 'G125D20' ON NR 10 PIN OF TB 302 IS ACTUALLY WIRE 'G174AS0'. THIS ERROR WAS FOUND BY LOOKING AT THE ACTUAL WIRE NUMBER ON THE AIRPLANE. SUBMITTER SUGGESTS CORRECTING THIS WIRNG DIAGRAM APPROPRIATELY WITH MITSUBI SH AND BEECH. 1 H 7 2 3T A2PC 1996022300400 19960223 00400 CE 1996 2 23 96ZZZX764 1 19960119 A 3233 231710012 ACTUATOR LEAR 35 35A 5170602 CE NLG DEFECTIVE A AOQA O OTHER P NO WARNING INDICATION AP APPROACH 1 EA 11 717JB B117 646 DURING APPROACH TO HUF, NOSE GEAR WOULD NOT INDICATE DOWN AND LOCKED. CYCLED GEAR SEVERAL TIMES TO OBTAIN DOWN AND LOCK ED INDICATION. AIRCRAFT LANDED WITHOUT INCIDENT. DUE TO THE NATURE OF THE RECENT MECHANICAL RELIABILITY OF THE NOSE GE AR OPERATION IN LEARJET N717JB, NOSE GEAR ACTUATOR PN 2317100-12, SN B117, HAS BEEN REMOVED FROM SERVICE. PART TT: 279 2.8 HOURS. LANDINGS, 2,266. 2 L 7 2 4F A10CE 1996022300401 19960223 00401 CE 1996 2 23 96ZZZX765 1 19960201 A 7331 FUEL FLOW LINE CESSNA 210 210L 2073448 CE INSTRUMENT PANEL CHAFED A A FPIA K NONE H ELECT. POWER LOSS-50 PC CR CRUISE 1 SO 15 93111 35433 21060266 AIRCRAFT EXPERIENCED ELECTRICAL FAILURE ON 1-26-96. MX FOUND FUEL FLOW LINE CHAFED THROUGH, SPRAYING A FUEL MIST ON CHA FED ELECTRICAL WIRES. ON 2-1-96, FLIGHT EXPRESS (FPIA) REPORTED THAT AN INSPECTION ON THE FUEL PRESSURE LINE TO THE FUE L FLOW INDICATOR BEHIND THE INSTRUMENT PANEL HAS RESULTED IN APPROXIMATELY 70 PERCENT OF THE LINES WERE FOUND CHAFED; AL SO, CHAFING WIRE BUNDLES. THE LINES WERE CHAFED PRIMARILY BY THE DEFROSTER CABLE. FLIGHT EXPRESS IS REMOVING ALL FUEL LINES ON ITS ENTIRE FLEET OF CE-210'S AND REPLACING THE LINES WITH STRATOFLEX III HOSE AND FITTING. AN SDR WAS PREPARED BY ORLANDO FSDO ON 2-2-96. REPORT WAS TELEPHONED IN TO AFS 643, 2-2-96. P/N'S 1200106193, 1200106216, AND 1200106263. 1 H 7 1 3O 3A21 1996022300405 19960223 00405 CE 1996 2 23 96ZZZX769 1 19960101 A 2750 9952402S1 MOTOR BEECH 100 100BEECH 1152916 CE FLAP FAILED A RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 524SC 523 B37 INTERNAL FAILURE OF FLAP MOTOR. 1 L 7 2 3T A14CE 1996022300407 19960223 00407 WP 1996 2 23 96ZZZX771 2 19960103 A 7261 30715647 REGULATOR LEAR 35 35LEAR 5170600 CE GARRTT TFE731 TFE73122B 01518 WP LT ENG BREATHER DEFECTIVE A BSYA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 8040A 7202 048 P74237 LEFT ENGINE LOST OIL PRESSURE ON APPROACH. FOUND DEFECTIVE OIL BREATHER REGULATOR. INSTALLED SB 79-3055. 2 L 7 2 4F 4 F A10CE E6WE 1996022300416 19960223 00416 NE 1996 2 23 UIEA9603 2 19960131 A 7530 7479555 VANE CONTROL BOEING 747 747228F 1384895 NM PWA JT9 JT9D7J 52054 NE NR 1 ENGINE INOPERATIVE A UIEA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 EA 15 2FOR 547 20887 662904 ENGINE REPAIRED BY LUFTHANSA, FIRST FLIGHT AFTER INSTALLATION. NR 1 ENGINE STALL WHILE CLIMBING THROUGH 10,000 FEET. F LT NR GTI900/31, LUXEMBOURG-TURIN-ENGINE SHUT-DOWN. ENGINE RE-START ATTEMPT UNSUCCESSFUL. AIRCRAFT RETURNED TO LUXEMBO URG BORESCOPE HPC/HRT NORMAL, MAGNETIC PLUGS, OIL FILTERS, FUEL FILTER, INLET, EXHAUST - OK. INSPECT PT2/TT2 LINES, FUE L PUMP FP12, 3-WAY VALVE - OK. INSPECT VSV UNISON RINGS SPACERS - OK. REPLACE ENGINE VANE CONTROL, ACCOMPLISH TRIM RUN , POWER RUN - ENGINE OPS NORMAL. 2 L 7 4 4F 4 F A20WE E20EA 1996022300417 19960223 00417 WP 1996 2 23 9602789860 1 19960220 A 3260 PROX CONTL UNIT DOUG DC9 DC951 3022051 WP LANDING GEAR MALFUNCTIONED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 769NC 47757 ON CLIMBOUT, GEAR DOOR OPEN LIGHT DID NOT GO OUT WHEN GEAR WAS RETRACTED. RECYCLED GEAR 3 TIMES, LIGHT REMAINED ON. LI GHT EXTINGUISHED NORMALLY WHEN GEAR EXTENDED FOR LANDING AT DTW. REPLACED THE PROXIMITY SWITCH CONTROL UNIT AND OPERATI ONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996022300418 19960223 00418 NM 1996 2 23 9604152706 1 19960219 A 2120 AIR DISTR BOEING 727 727225 1384077 NM CABIN ODOR A NWAA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 815EA 22552 DURING CLIMB AND AFTER GEAR RETRACTION, CREW OBSERVED A RUBBER SMELL IN THE CABIN. EMERGENCY WAS DECLARED FOR LANDING A T DTW AND AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT WHEELS, TIRES AND WHEEL WELLS WERE INSPECTED, NO DAMAGE OR DEFECTS WERE FOUND. 2 L 7 3 4F A3WE 1996022300419 19960223 00419 NM 1996 2 23 9604182298 1 19960219 A 3260 GEAR WARNING BOEING 727 727251 138408H NM LT MLG DOOR MALFUNCTIONED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 298US 22152 DURING TAKEOFF, THE LEFT GEAR DOOR LIGHT REMAINED ON AFTER GEAR RETRACTION. CYCLED GEAR ON SECOND RETRACTION, LIGHT EXT INGUISHED. LEFT GEAR WARNING SYSTEM WAS PLACED ON MEL 32-1, PLACARD NR 474710. 2 L 7 3 4F A3WE 1996022300420 19960223 00420 NM 1996 2 23 9604192705 1 19960220 A 3260 DN LOCK SENSOR BOEING 727 727225 1384077 NM LT MLG FAILED A NWAA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 01 802EA 22433 DURING GEAR EXTENSION, THE LEFT MAIN LANDING GEAR HAD NO INDICATION WARNING LIGHTS. ON THIRD GEAR EXTENSION, GEAR WARNI NG OPERATED NORMALLY, THREE GREEN LIGHTS. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED DAMAGED GEAR DOWNLOCK SENSOR. OP ERATIONAL CHECK OF WARNING LIGHT AND LOCK CHECKED OK. 2 L 7 3 4F A3WE 1996022300421 19960223 00421 NM 1996 2 23 9604205508 1 19960218 A 2722 3800022104 ACTUATOR BOEING 757 757251 1384970 NM RUDDER FAILED A NWAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 01 508US 23167 DURING CLIMB, RUDDER RATIO LIGHT ILLUMINATED SEVERAL TIMES ACCOMPANIED BY ACTUAL RUDDER INPUT, CAUSING ABOUT 5 UNITS OF AILERON TO HOLD WINGS LEVEL. FLIGHT RETURNED TO MSP. REPLACED THE RUDDER RATIO ACTUATOR. 2 L 7 2 4F RT A2NM 1996022300422 19960223 00422 WP 1996 2 23 9604219908 1 19960220 A 2131 10256861 CONTROLLER DOUG DC9 DC931 3022065 WP COCKPIT PANEL FAILED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 958N 29198 47254 AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. CABIN PRESSURIZATION WENT INTO FULL NEGATIVE RATE OF CLIMB. FLIGHT RETURN ED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND FAULT WITH CABIN PRESSURE CONTROLLER. REPLACED CONTROLLER AND REPLACED CABIN PRESSURE AMPLIFIER AS A PRECAUTION. OPERATIONAL CHECK NORMAL ON GROUND. 2 L 7 2 4F A6WE 1996022300423 19960223 00423 WP 1996 2 23 9604229763 1 19960216 A 3350 BATTERY PACK DOUG DC9 DC941 302207N WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 763NW 47396 DURING LINE CHECK, FOUND ONE SECTION OF EMERGENCY LIGHTS INOPERATIVE AT SECTION 886. REPLACED BATTERY PACK AND OPERATIO NAL CHECK GOOD. 2 L 7 2 4F A6WE 1996022300424 19960223 00424 WP 1996 2 23 9604239854 1 19960214 A 5350 RELEASE MECH DOUG DC9 DC951 3022051 WP TAIL CONE MALFUNCTIONED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 763NC 47716 DURING LINE CHECK, FOUND THAT THE TAIL CONE FAILED TO DROP. CLEANED PAINT AND DE-ICING FLUID FROM THE TAIL CONE SEAL. A LSO, FOUND AND REPLACED 13 WORN GUIDE PINS AND 12 WORN BEARING PLATES. 2 L 7 2 4F A6WE 1996022300425 19960223 00425 NM 1996 2 23 96FDEA00276 1 19960216 A 5330 SKIN BOEING 727 72722 1384002 NM BS 365-390 CREASE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 LARGE CREASE IN EXTERIOR SKIN BS 365 TO 390 STR 23R. 2 L 7 3 4F A3WE 1996022300426 19960223 00426 NM 1996 2 23 96FDEA00277 1 19960216 A 5320 6516349 SHEAR WEB BOEING 727 72722 1384002 NM BS 1173 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION (C53-224-01) ON SHEAR WEB AT BS 1173 RBL 27 WL 208. *S/D* REPAIRED SHEAR WEB PER SRM 51-40-2. 2 L 7 3 4F A3WE 1996022300427 19960223 00427 NM 1996 2 23 96FDEA00278 1 19960216 A 5320 6517684 SHEAR WEB BOEING 727 72722 1384002 NM BS 1173 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION ON NOSE WHEEL WELL VERTICAL WEB BS 303 TO 309, WL 177, LBL 15 ON SHEAR WEB AT BS 1173 RBL 27 WL 208. *S/D* R EMOVED CORROSION FOUND MATERIAL LOSS WAS WITHIN LIMITS PER SRM 53-10. TREATED AREA, PRIMED AND REINSTALLED FASTENERS RE MOVED. 2 L 7 3 4F A3WE 1996022300428 19960223 00428 NM 1996 2 23 96FDEA00279 1 19960216 A 5320 65184152 NOSE CHORD BOEING 727 72722 1384002 NM BS 312-324 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION (C53-111-01) ON UPPER NOSE CHORD BS 312 TO 324 RBL 15 WL 169. *S/D* REMOVED AND REPLACED UPPER NOSE CHORDS 2 94.5 TO BS 355 RBL 15 WL 169 IAW DRAWING NR 65-18415. WEB TO BE INSTALLED ON NR 0834 AT BS 294.5. 2 L 7 3 4F A3WE 1996022300429 19960223 00429 NM 1996 2 23 96FDEA00280 1 19960216 A 5315 FLOOR BEAM BOEING 727 72722 1384002 NM BS 600 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION (C53-111-01, -2) ON LOWER FLANGE OF FLOOR BEAM IN NUTPLATE HOLES AT BS 600 LBL 20 TO RBL 26 WL 200. *S/D* RE MOVED AND CORRODED AREA FROM LBL 17 TO RT SKIN FABRICATED AND INSTALLED REPAIR PARTS PER FDE SRM 53-10-18 FIG 2. 2 L 7 3 4F A3WE 1996022300430 19960223 00430 NM 1996 2 23 96FDEA00281 1 19960216 A 5320 65207264 THRESHOLD WEB BOEING 727 72722 1384002 NM BS 527 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION (C53-111-01-2) ON DOOR THRESHOLD VERTICAL WEB AT BS 527 RBL 22 WL 156. WILL REQUIRE PARTIAL REMOVAL OF HORIZO NTAL WEB AND STRAP. *S/D* REMOVED, FABRICATED AND INSTALLED VERTICAL AND HORIZONTAL WEB PER SRM 53-10-1. 2 L 7 3 4F A3WE 1996022300431 19960223 00431 NM 1996 2 23 96FDEA00282 1 19960216 A 5330 6554583 SKIN PANEL BOEING 727 72722 1384002 NM BS 1108-1130 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 BS 1110 STR 26 THERE IS BULGE IN SKIN TRIPLER DAMAGED OUT OF LIMITS. *S/D* REPLACED BONDED DOUBLER AT BS 1148 TO 1166 STR 25 TO 26 RIGHT. REPLACED BONDED TRIPLER FROM BS 1108 TO 1130 STR 25R TO 26R. REPAIRED REMAINING DEBONDED SKIN USIN G FIXED PATTERN PER FEDEX SRM 53-30-4 FROM BS 1110 TO 1183. 2 L 7 3 4F A3WE 1996022300432 19960223 00432 NM 1996 2 23 96FDEA00285 1 19960219 A 5521 65174403 HINGE RIB BOEING 727 72722 1384002 NM RT ELEVATOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 RT ELEVATOR HINGE RIB AT HORIZONTAL STAB STATION 136.50 IS CRACKED ON THE I/B UPPER FLANGE. *S/D* REMOVED AND REPLACED ELEVATOR HINGE RIB SRM 27-30-0. 2 L 7 3 4F A3WE 1996022300433 19960223 00433 NM 1996 2 23 96FDEA00286 1 19960219 A 5320 6517508 CHORD BOEING 727 72722 1384002 NM BS 1342 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 AREA OF CORROSION ON BS 1342 CHORD UPPER FWD RT FLANGE RBL 20. *S/D* REMOVED AND REPLACED UPPER CHORD IAW FEDEX DRAWIN G 65-17508. 2 L 7 3 4F A3WE 1996022300434 19960223 00434 NM 1996 2 23 96FDEA00287 1 19960219 A 5315 6540145 FLOOR BEAM BOEING 727 72722 1384002 NM BS 500 DOUBLE HOLE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 DOUBLE HOLE IN FLOORBEAM BS 500 BL 0 WL 208.1. *S/D* REPAIRED DOUBLE HOLE AT BS 500, BL 0 WL 208.1 IAW FEDEX SRM 57-1 0-8. 2 L 7 3 4F A3WE 1996022300435 19960223 00435 WP 1996 2 23 ABXA9600195 1 19960219 A 2612 5775631 FIRE LOOP DOUG DC8 DC861 3021952 WP PWA JT3D JT3D3B 52039 NE NR 4 ENGINE DEFECTIVE A ABXA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 GL 23 842AX 46015 645729 DURING CLIMB, FIRE WARNING INDICATION OCCURRED ON THE NR 4 ENGINE. DISCHARGED BOTH FIRE EXTINGUISHERS, BUT FIRE WARNING INDICATION REMAINED. COMPLETED INFLIGHT SHUTDOWN OF THE NR 4 ENGINE. REPLACED LOWER FIRE LOOP ASSEMBLY AND UPPER AFT FIRE LOOP ASSEMBLY ON THE NR 4 ENGINE. REPLACED BOTH FIRE EXTINGUISHERS ON THE RIGHT WING. COMPLETED PNEUMATIC LEAK CH ECK OF THE NR 4 ENGINE AND NO LEAKS WERE NOTED. NO INDICATIONS OF A FIRE ON THE NR 4 ENGINE WERE NOTED. 2 L 7 4 4F 4 F 4A25 1E8 1996022300439 19960223 00439 NM 1996 2 23 DL757960365 1 19960219 A 5754 114N4003177A TE WEDGE BOEING 757 757232 1384965 NM NR 2 LE SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 658DL 24420 DURING INSPECTION, LEFT WING NR 2 SLAT T/E WEDGE WAS FOUND DELAMINATED. REPLACED WEDGE PER SRM 57-43-02 FIG 202. 2 L 7 2 4F RT A2NM 1996022300440 19960223 00440 NE 1996 2 23 DL757960406 2 19960217 A 7310 5010224 HOUSING CAP BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE LT FUEL FILTER CRACKED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 633DL 23614 ON CLIMBOUT NOTICED EXCESSIVE FUEL CONSUMPTION ON LEFT ENGINE. FUEL IMBALANCE BECAME EXCESSIVE AND UNCONTROLLABLE, SHUT DOWN LEFT ENGINE AND FUEL CONSUMPTION BECAME NORMAL. FOUND LEFT ENGINE FUEL PUMP MAIN FILTER HOUSING CAP AND FILTER HAD BEEN BLOWN OFF. REPLACED FUEL PUMP AND FUEL CONTROL, OPERATION NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996022300441 19960223 00441 WP 1996 2 23 DLL10960395 1 19960127 A 5312 1641601102 BLKHD ANGLE LKHEED 1011 10113851 5265010 WP FS 1363 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 719DA 193C1135 THE 1641601-102 ANGLE INSTALLED AS PART OF THE FS 1363 BULKHEAD MODIFICATION PER DAL EO 7-47702-3AD WAS FOUND CRACKED AT A FASTENER HOLE DURING ROUTINE LAYOVER INSPECTIONS AND OPERATIONS. THE CRACK APPEARS TO HAVE BEEN THE RESULT OF PRELOA D, CAUSED BY A GAP BETWEEN THE ANGLE AND THE ADJACENT STIFFENER. ACCOMPLISHED REPAIRS PER DL ERA 2 73193-14AD. 2 L 7 3 4F A23WE 1996022300442 19960223 00442 WP 1996 2 23 DLL10960403 1 19960217 A 2710 FLT CONTROLS LKHEED 1011 10113851 5265010 WP LT AILERON LACK OF LUBE A DALA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SO 27 721DA 193C1139 AIRCRAFT HARD TO ROLL RIGHT, BUT ROLLS NORMAL BACK TO THE LEFT. TURNING OFF B-AILERON SERVO INBD, CAUSED UNCOMMANDED HA RD LEFT ROLL. INSPECTION OF FLT CONTROL SYSTEM FOUND EXTREME BINDING IN LINKAGE BETWEEN LEFT INBD AILERON AND WHEEL WE LL. LUBED LINKAGE BEARINGS UNTIL FREE, OPERATION NORMAL. 2 L 7 3 4F A23WE 1996022300443 19960223 00443 WP 1996 2 23 MWEA96044 1 19960220 A 2560 52102122 ESCAPE ROPE DOUG DC9 DC915 3022036 WP FLT COMPT DEPLOYED A MWEA K NONE O OTHER LD LANDING 1 GL 31 900ME 45841 PILOT REPORTS, UPON LANDING IN MKE THE F/O'S ESCAPE ROPE DEPLOYED AND UNRAVELED. MAINTENANCE RESECURED ESCAPE ROPE. 2 L 7 2 4F A6WE 1996022300444 19960223 00444 NM 1996 2 23 SCNA96022 1 19960218 A 3350 S106 BATTERIES BOEING 727 7272J4 1384006 NM AFT ENTRY DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 284SC 21438 THE AFT ENTRY EMERGENCY AREA LIGHT FOUND TO BE INOPERATIVE. REMOVED AND REPLACED BATTERIES IAW 33-50-101, LIGHT OPS CHE CKED NORMAL. 2 L 7 3 4F RT A3WE 1996022300445 19960223 00445 NM 1996 2 23 SWAA960084 1 19960212 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 740 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED SERVICE CHECK, FOUND LEFT FUSELAGE SKIN CRACKED AT BS 740, S17L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996022300446 19960223 00446 NM 1996 2 23 SWAA960085 1 19960213 A 3350 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 67SW 22356 EMERGENCY EXIT LIGHTS WILL NOT TURN OFF AFTER AIRCRAFT SHUTDOWN. REWIRED REAR SWITCH, REPLACED AFT ENTRY DOOR LIGHT ASS EMBLY AND SECURED AFT FLOOR TRACK LIGHTING BATTERY PACK PER BOEING SRM. 2 L 7 2 4F A16WE 1996022300447 19960223 00447 NM 1996 2 23 SWAA960086 1 19960216 A 5320 INTERCOSTAL BOEING 737 7372H4 138448C NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 82SW 22731 DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL CRACKED AT BS 727, LBL 35 TO 44, WL 180. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996022300448 19960223 00448 NM 1996 2 23 SWAA960087 1 19960216 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 725 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 82SW 22731 DURING SCHEDULED D-CHECK, FOUND ANGLE CRACKED AT BS 725, LBL 17 WL 230. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996022300449 19960223 00449 NM 1996 2 23 SWAA960088 1 19960216 A 5320 CLIP BOEING 737 7372H4 138448C NM BS 787 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 82SW 22731 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, S2R. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996022300450 19960223 00450 NM 1996 2 23 SWAA960089 1 19960216 A 5320 SPLICE BOEING 737 7372H4 138448C NM BS 907 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 82SW 22731 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CORRODED AT BS 907, S25R. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996022300451 19960223 00451 NM 1996 2 23 SWAA960090 1 19960216 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 757 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 82SW 22731 DURING SCHEDULED D-CHECK, FOUND STRINGER 24R CORRODED AT BS 757. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996022300452 19960223 00452 NM 1996 2 23 SWAA960091 1 19960216 A 5240 SKIN BOEING 737 7372H4 138448C NM SERVICE DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 82SW 22731 DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOOR INNER SKIN CRACKED AT OUTER EDGE CORNER LWR CONTROL BOX CAVITY. REPAIR ED PER BOEING SRM. 2 L 7 2 4F A16WE 1996022300453 19960223 00453 NM 1996 2 23 SWAA960092 1 19960216 A 5320 WEB BOEING 737 7372H4 138448C NM BS 695/709 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 82SW 22731 DURING SCHEDULED D-CHECK, FOUND WEBS CRACKED AT BS 695 LBL 61 WL 206 AND AT BS 709 RBL 25 WL 205. REPLACED PER BOEING S RM. 2 L 7 2 4F A16WE 1996022300454 19960223 00454 NM 1996 2 23 SWAA960093 1 19960216 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 384 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 82SW 22731 DURING SCHEDULED D-CHECK, FOUND CRACKED UPPER ANGLE ON SHEAR WEB AT BS 384 BL 0 WL 208. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996022300455 19960223 00455 NM 1996 2 23 SWAA960094 1 19960218 A 5320 CHORD BOEING 737 7373H4 1384600 NM BS 1138/1156 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND CRACKED LOWER CHORDS AT S5L AND S5R, BS 1138 AND AT BS 1156, LBL 23 AND RBL 23. REPLACE D PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996022300456 19960223 00456 NM 1996 2 23 SWAA960095 1 19960218 A 5320 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 1121 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND SHEAR TIES CRACKED AT BS 1121 BETWEEN S12 AND 13L AND AT BS 360, S13L AND S15L. REPLACE D PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996022300457 19960223 00457 NM 1996 2 23 SWAA960096 1 19960218 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 328/986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND FLOORBEAMS CORRODED AT BS 986 LBL 30 TO RBL 51, BS 328 RBL 14 AND 15 WL 208 AND BS 986 W L 208 RBL 5, 24, 32, 43 AND LBL 43. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996022300458 19960223 00458 NM 1996 2 23 SWAA960097 1 19960218 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORTS CORRODED AT BS 957.5 WL 208 RBL 49, BS 1006 TO 1016 WL 208 LBL 6 TO 8 AND AT BS 540 LBL 2 WL 208. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996022300459 19960223 00459 NM 1996 2 23 SWAA960098 1 19960218 A 5320 SPLICE BOEING 737 7373H4 1384600 NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907 S4L AND S4R. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996022300460 19960223 00460 NM 1996 2 23 SWAA960099 1 19960218 A 5320 CLIPS BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 787 S11L, BS 947 S25R AND S21L AND AT BS 663 S10R AND S10L. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996022300461 19960223 00461 NM 1996 2 23 SWAA960100 1 19960218 A 5320 DOOR FRAME BOEING 737 7373H4 1384600 NM BS 296 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR FRAME CRACKED AT BS 296 RBL 40 WL 274. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996022300462 19960223 00462 NM 1996 2 23 SWAA960101 1 19960218 A 5320 DOOR FRAME BOEING 737 7373H4 1384600 NM FWD CARGO CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT BS 492 RBL 37 WL 161. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996022300463 19960223 00463 NM 1996 2 23 SWAA960102 1 19960218 A 5320 CHORD BOEING 737 7373H4 1384600 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM CRACKED AT BS 663 RBL 65 WL 208. REPLACED CREASE BEAM CHORD PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996022300464 19960223 00464 NM 1996 2 23 SWAA960103 1 19960218 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 987 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND STRINGER CRACKED AT BS 987, S20R. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996022300465 19960223 00465 NM 1996 2 23 SWAA960104 1 19960218 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED D-CHECK, FOUND 3 CRACKS ON BS 178 BULKHEAD ADJACENT TO 2 FASTENERS AT WL 234 RBL 10. REPAIRED PER BOEI NG SRM. 2 L 7 2 4F RT A16WE 1996022300466 19960223 00466 NM 1996 2 23 SWAA960105 1 19960218 A 5241 DOOR SKIN BOEING 737 7373H4 1384600 NM AFT GALLEY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 331SW 23695 DURING SCHEDULED B/C1 CHECK, FOUND AFT GALLEY DOOR UPPER HINGE CUTOUT TOP FWD CORNER CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996022300467 19960223 00467 NM 1996 2 23 SWAA960106 1 19960218 A 5311 BELT FRAME BOEING 737 7373H4 1384600 NM BS 807 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED 1/4 D-CHECK, FOUND BELT FRAME CRACKED AT BS 807 BL 0. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996022300468 19960223 00468 NM 1996 2 23 SWAA960107 1 19960218 A 5230 DOOR BOEING 737 7375H4 138449D NM FWD CARGO CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 523SW 26565 DURING SCHEDULED B-CHECK, FOUND FWD CARGO DOOR CRACKED ON FWD LOWER CORNER ADJACENT TO UPLOCK HOOK. REPAIRED PER SWA TY PICAL REPAIR T1-A25-005. 2 L 7 2 4F RT A16WE 1996022300469 19960223 00469 NE 1996 2 23 SWAA960108 2 19960219 A 7230 COMPRESSOR BOEING 737 7373H4 1384600 NM GE CFM56 CFM563B1 13802 NE NR 2 ENGINE STALLED A SWAA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 07 323SW 23344 721375 INITIATED AIR TURNBACK DUE TO NUMBER 2 ENGINE COMPRESSOR STALL. AIRCRAFT LANDED AT LAS WITHOUT INCIDENT. INSPECTED, EN GINE CHANGE UNDERWAY PER BOEING M/M. 2 L 7 2 4F 4 F RT A16WE E2GL 1996022300470 19960223 00470 SO 1996 2 23 SWIA95713 1 19960201 A 3260 UPLOCK ROLLER EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE NLG LACK OF LUBE A SWIA O OTHER N FALSE WARNING CL CLIMB 1 NM 07 205SW 120260 AFTER SELECTING GEAR UP ON TAKEOFF, NOSE GEAR INDICATED UNSAFE, TWO RED LIGHTS. CYCLED GEAR TWICE AND GOT SAME INDICATI ON. JACKED AIRCRAFT AND CYCLED GEAR, ALL INDICATIONS AND RETRACTION NORMAL. CHECKED UPLOCK HOOK RIGGING PER MAINTENANC E MANUAL, CHECKED GOOD. FOUND UPLOCK ROLLER DRY, LUBED UPLOCK ROLLER AND HOOK. ALSO, SERVICED NOSE STRUT WITH HYD FLUI D AND N2. CYCLED GEAR SEVERAL TIMES, GEAR RETRACTION AND DOOR OPERATION NORMAL. 2 L 7 2 4T 4 T RT A31SO E20NE 1996022300471 19960223 00471 SO 1996 2 23 SWIA95714 1 19960206 A 3260 CONNECTOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT MLG MISWIRED A SWIA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 NM 07 190SW 120050 RIGHT MAIN GEAR -A+ LIGHT DIDN'T EXTINGUISH AND NO OTHER GEAR LIGHTS WOULD ILLUMINATE WITH GEAR HANDLE DOWN. USED EMERG ENCY GEAR EXTENSION PRECEDURE TO PUT GEAR DOWN. REPLACED RIGHT GEAR -A+ SYSTEM PROX WIRE HARNESS. AFTER CONNECTING PRO X SENSOR, RIGHT RED -A+ LIGHT STAYS ON. TROUBLESHOT TO RIGHT UPLOCK CAM CANNON PLUG FOR PROX SENSOR WIRED INCORRECTLY. SWAPPED WIRES IN CANNON PLUG FOR -A+ SYSTEM AND -B+ SYSTEMS IN RIGHT WHEEL WELL FOR A LIGHT INDICATIONS. GROUND OPS CH ECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1996022300472 19960223 00472 WP 1996 2 23 SWIA95715 2 19960210 A 7210 8546922 RED GEAR BOX SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP LT ENGINE FAILED A SWIA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 NM 07 2698C AC665 LEFT ENGINE FAILED IN FLIGHT, NO ABNORMAL INDICATIONS NOTED PRIOR TO EVENT. HOOKED UP FUEL GAUGE TO LEFT FUEL PUMP OUTP UT AND MONITORED ENGINE, NO FUEL PRESSURE REGISTERED. PULLED CHIP DETECTOR PLUG AND FOUND METAL ON PLUG. REMOVED OIL F ILTER AND FOUND SUBSTANTIAL METAL IN OIL. REMOVED LEFT ENGINE FOR GEAR BOX REPAIRS. REMOVED AND REPLACED OIL COOLER WI TH OVERHAULED UNIT AND OPS CHECKS GOOD. 1 L 7 2 4T 4 T A8SW E4WE 1996022300473 19960223 00473 SO 1996 2 23 SWIA95717 1 19960214 A 3230 SEQUENCE VALVE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT MLG FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 212SW 120276 AFTER TAKEOFF, RIGHT MAIN GEAR WOULD NOT RETRACT AND RED LIGHT STAYED ON. TOWER VERIFIED THAT GEAR DID NOT RETRACT. RE PLACED RIGHT MAIN LANDING GEAR OUTBOARD SEQUENCE VALVE. CYCLED GEAR SEVERAL TIMES, OPS CHECK GOOD AND TEST FLIGHT SATIS FACTORY. 2 L 7 2 4T 4 T RT A31SO E20NE 1996022300474 19960223 00474 SW 1996 2 23 SWIA95718 1 19960215 A 2910 LINE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP LT ENGINE FAILED A SWIA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 07 2724S AC720 COMPLETE HYDRAULIC FAILURE, LEFT SYSTEM FIRST THEN COMPLETE PRESSURE LOSS. REPLACED DEFECTIVE HYDRAULIC PRESSURE LINE A T LEFT ENGINE FIREWALL AND SERVICED SYSTEM. SPRAYED DOWN SURROUNDING AREA AND RAN LEFT ENGINE TWICE, NO LEAKS NOTED. R ESERVICED RESERVOIR TO FULL LEVEL. 1 L 7 2 4T 4 T A8SW E4WE 1996022300478 19960223 00478 WP 1996 2 23 96ZZZM178 1 19960112 A 3240 27056512 BRACKET DOUG DC8 DC8F55 3021928 WP NLG WW CRACKED A CKSA O OTHER E VIBRATION/BUFFET CL CLIMB 1 GL 23 6161M 71329 45762 KMIA - AFTER TAKEOFF HEARD LOUD NOISE AND VIBRATION COMING FROM NOSE GEAR AREA. CYCLED GEAR TWICE WITH NO CHANGE. ON T HIRD CYCLE NOISE AND VIBRATION STOPPED. EXTENDED GEAR FOR LANDING, NO NOISE OR VIBRATION NOTED. INSPECTED NOSE WHEEL W ELL, FOUND NOSE TIRE BRAKE PAD BRACKET CRACKED. REMOVED AND REPLACED NOSE TIRE BRAKE PAD BRACKET. NO OTHER DEFECTS NOT ED. AIRCRAFT GOOD FOR FLIGHT. REFERENCE CKSA96002. 2 L 7 4 4F 4A25 1996022300479 19960223 00479 WP 1996 2 23 96ZZZM179 1 19960112 A 3240 37038375 BRACKET DOUG DC8 DC8F55 3021928 WP NLG WW CRACKED A CKSA O OTHER E VIBRATION/BUFFET CL CLIMB 1 GL 23 6161M 71329 45762 KMIA - AFTER TAKEOFF HEARD LOUD NOISE AND VIBRATION COMING FROM NOSE GEAR AREA. CYCLED GEAR TWICE WITH NO CHANGE. ON T HIRD CYCLE NOISE AND VIBRATION STOPPED. EXTENDED GEAR FOR LANDING NO NOISE OR VIBRATION NOTED. INSPECTED NOSE WHEEL WE LL, FOUND NOSE TIRE BRAKE PAD BRACKET CRACKED. REMOVED AND REPLACED NOSE TIRE BRAKE PAD BRACKET. NO OTHER DEFECTS NOTE D. AIRCRAFT GOOD FOR FLIGHT. REFERENCE CKSA96002. 2 L 7 4 4F 4A25 1996022300482 19960223 00482 WP 1996 2 23 96ZZZM182 1 19960118 A 2612 892809040002 FIRE CNTRL UNIT DOUG DC9 DC983 3022083 WP NR 2 ENGINE MALFUNCTIONED A TWAA E ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 CE 05 9302B 49528 STL - DURING DESCENT, NR 2 ENGINE, S/N 3231, WAS SHUT DOWN DUE TO FIRE INDICATION LIGHT ILLUMINATION AND FIRE BELL SOUND ED. BOTH FIRE EXTINGUISHER BOTTLES WERE DISCHARGED. REMOVED AND REPLACED NR 2 ENGINE FIRE DETECTION CONTROL UNIT, MFG P/N 892809-0400-02. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1996022300492 19960223 00492 NM 1996 2 23 96ZZZM192 1 19960105 A 5720 CHORD BOEING 727 727231 1384079 NM RT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 64319 20052 MCI - DURING C-CHECK, FOUND CRACK ON LOWER CHORD ATTACH BOLT HEAD FLANGE ABOVE EXCESS HOLE, RIGHT WING, W.5738.5. REPAI RED PER SRM 57-10-05, PAGE 3-5, AND TWA STANDARD PRACTICES. (M) 2 L 7 3 4F A3WE 1996022300493 19960223 00493 NM 1996 2 23 96ZZZM193 1 19960105 A 5712 RIB BOEING 727 727231 1384079 NM WS 629 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 64319 20052 MCI - DURING C-CHECK, FOUND A CRACK AT WS 629 RIB LOWER HOLE, STRINGER 2. STOP DRILLED PER SRM 57-10-5 AND REPAIRED PER SRM 57-10-5, FIGURE 2 AND TWA STANDARD PRACTICES. (M) 2 L 7 3 4F A3WE 1996022300495 19960223 00495 NM 1996 2 23 96ZZZM195 1 19960111 A 5311 FRAME BOEING 747 747131 1384881 NM BS 380 BROKEN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 93108 19674 MCI - DURING OP-16, FOUND RIGHT FRAME BROKEN AT STRINGER 24A, STATION 380. REPAIRED PER ARA 8913 AND TWA STANDARD PRACT ICES. (M) 2 L 7 4 4F A20WE 1996022300496 19960223 00496 WP 1996 2 23 96ZZZM196 1 19960121 A 3222 A00314 SCHRADER VALVE DOUG DC9 DC982 3022082 WP NLG STRUT CRACKED A TWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 05 950U 49230 TPA - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, NOSE LANDING GEAR WOULD NOT RETRACT. FOUND NOSE LANDING GEAR INFLA TION LOW DUE TO CRACKED SCHRADER VALVE. REPLACED SCHRADER VALVE, MFG P/N A00314, AND SERVICED NOSE LANDING GEAR, OPERAT ION THEN CHECKED NORMAL. 2 L 7 2 4F A6WE 1996022300498 19960223 00498 NM 1996 2 23 96ZZZM198 1 19960111 A 5330 SKIN BOEING 747 747131 1384881 NM BS 1830-1840 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 93108 19674 MCI - DURING OP-16, FOUND CORROSION ON INNER SKIN AND DOUBLER, BETWEEN STRINGERS 45R AND 46R, STATION 1830 TO 1840. CUT OUT CORROSION AND REPAIRED PER ARA 9822. 2 L 7 4 4F A20WE 1996022300499 19960223 00499 NM 1996 2 23 96ZZZM199 1 19960122 A 2750 285T004953 FSEU BOEING 767 767231 1385131 NM FLAP SYSTEM FAILED A TWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 05 602TW 22565 JFK - DURING CLIMB, THE FLAPS WOULD NOT FULLY RETRACT. REMOVED AND REPLACED THE FLAP/SLAT ELECTRONICS UNIT (FSEU), MFG P/N 285T0049-53. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A1NM 1996022300500 19960223 00500 WP 1996 2 23 96ZZZM200 1 19960119 A 3230 39140165505 CYLINDER DOUG DC9 DC932 3022066 WP RT MLG MALFUNCTIONED A TWAA O OTHER J WARNING INDICATION AP APPROACH 1 CE 05 926L 47172 STL - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, RIGHT MAIN LANDING GEAR DID NOT SHOW DOWN AND LOCKED. CYCLED LAND ING GEAR. FOUND RIGHT MAIN LANDING GEAR BUNGEE CYLINDER MALFUNCTION. REPLACED RIGHT MAIN LANDING GEAR BUNGEE CYLINDER, MFG P/N 3914016-5505. LANDING GEAR OPERATION AND INDICATION THEN CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 1996022300501 19960223 00501 NM 1996 2 23 96ZZZM201 1 19960111 A 5730 SKIN BOEING 747 747131 1384881 NM WS 398 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 93108 19674 MCI - DURING OP-16, FOUND CORROSION BETWEEN UPPER SKIN AND REAR SPAR CAP, WS 398. REMOVED CORROSION AND INSTALLED DOUBL ER REPAIR PER ARA 8915 AND SRM 57-30-03, FIGURE 9. (M) 2 L 7 4 4F A20WE 1996022300502 19960223 00502 NM 1996 2 23 96ZZZM202 1 19960111 A 5330 SKIN BOEING 747 747131 1384881 NM FS 800-820 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 93108 19674 MCI - DURING OP-16, FOUND POPPED RIVETS AND BULGING SKIN IN FORWARD CARGO BIN CUTOUT FOR E/E DOOR, BETWEEN FS 800 AND FS 820, INBOARD OF STRINGER 46L. INSTALLED NEW SKIN SECTION PER ARA 9807. (M) 2 L 7 4 4F A20WE 1996022300503 19960223 00503 NM 1996 2 23 96ZZZM203 1 19960111 A 5330 SKIN BOEING 747 747131 1384881 NM FS 740-850 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 93108 19674 DURING OP-16, FOUND CORROSION ON FORWARD FUSELAGE SKIN PANEL FS 740 TO FS 850, STRINGER 44L TO 44R. INSTALLED NEW SKIN PANEL PER ARA 9807. (M) 2 L 7 4 4F A20WE 1996022300504 19960223 00504 NM 1996 2 23 96ZZZM204 1 19960111 A 5330 SKIN BOEING 747 747131 1384881 NM FS 780-800 DISBONDED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 93108 19674 MCI - DURING OP-16, FOUND DOUBLER DISBONDED BETWEEN FS 780 AND FS 800, INBOARD OF STRINGER 45R. INSTALLED NEW SKIN PANE L PER TWA ARA 9807. (M) 2 L 7 4 4F A20WE 1996022300505 19960223 00505 NM 1996 2 23 96ZZZM205 1 19960111 A 5311 FRAME BOEING 747 747131 1384881 NM FS 240 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 93108 19674 MCI - DURING OP-16, FOUND LEFT STRINGER 13A FRAME WEB CRACKED, FS 240. REPAIRED WEB PER ARA 9626 AND ARA 9629A. 2 L 7 4 4F A20WE 1996022300506 19960223 00506 NM 1996 2 23 96ZZZM206 1 19960111 A 5320 ANGLE BOEING 747 747131 1384881 NM BS 467 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 93108 19674 MCI - DURING OP-16, FOUND 1.5 INCH CRACK IN 1-L DOOR INBOARD SUPPORT ANGLE FOR THRESHOLD PLATE, STATION 467, LBL 90. CU T UPPER FLANGE OFF 'U' CHANNEL AND REPLACED WITH REPAIR PER ARA 9627. (M) 2 L 7 4 4F A20WE 1996022300507 19960223 00507 NM 1996 2 23 96ZZZM207 1 19960125 A 2530 SERVING CART BOEING 767 767231 1385131 NM NR 2 GALLEY SMOKING A TWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 607TW 22570 JFK - DURING CRUISE, NR 2 AFT GALLEY SERVING CART EMITTED SMOKE WHEN TURNED ON. REMOVED AND REPLACED SERVING CART. OPE RATIONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A1NM 1996022300508 19960223 00508 1996 2 23 96ZZZM208 4 19960126 A 2210 2589445933 ACTUATOR DOUG DC9 DC951 3022051 WP YAW DAMPER FAILED A TWAA O OTHER O OTHER CL CLIMB 1 CE 05 410EA 47731 STL - DURING CLIMB, UNCOMMANDED RUDDER MOVEMENT WAS DETECTED. REMOVED AND REPLACED YAW DAMPER ACTUATOR DUE TO INTERNAL FAILURE, MFG P/N 2589445-933. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F A6WE 1996022300509 19960223 00509 WP 1996 2 23 96ZZZM209 1 19960127 A 2780 RETRACT MECH LKHEED 1011 10113851 5265010 WP LE SLATS FROZEN A TWAA O OTHER J WARNING INDICATION LD LANDING 1 CE 05 31019 193B1066 STL - DURING LANDING THE LEADING EDGE SLATS WERE FROZEN AND WOULD NOT DEPLOY. LEADING EDGE SLAT ACTUATORS AND JACKSCREW S WERE THAWED, LUBRICATED AND SERVICED. LEADING EDGE SLATS WERE CYCLED NUMEROUS TIMES, OPERATION NORMAL. 2 L 7 3 4F A23WE 1996022300510 19960223 00510 WP 1996 2 23 96ZZZM210 1 19960123 A 2612 5938323505 FIRE LOOP DOUG DC9 DC983 3022083 WP RT ENGINE CHAFED A TWAA O OTHER N FALSE WARNING CL CLIMB 1 CE 05 9302B 49528 MCI - DURING CLIMB RIGHT ENGINE 'B' FIRE WARNING LOOP FLICKERED ON, SWITCHED TO 'A' LOOP. AFTER LEVEL OFF AT CRUISE. ' A' LOOP WARNING CAME ON AND WENT OFF. FOUND LOWER APRON 'A' AND 'B' LOOPS CHAFED. REPLACED 'A' AND 'B' APRON LOOPS, MF G P/N 5938323-505 AND 5938323-506, AND FIRE WARNING SYSTEM OPERATION CHECKED NORMAL. 2 L 7 2 4F RT A6WE 1996022300511 19960223 00511 WP 1996 2 23 96ZZZM211 1 19960123 A 2612 5938323506 FIRE LOOP DOUG DC9 DC983 3022083 WP RT ENGINE CHAFED A TWAA O OTHER N FALSE WARNING CL CLIMB 1 CE 05 9302B 49528 MCI - DURING CLIMB RIGHT ENGINE 'B' FIRE WARNING LOOP FLICKERED ON, SWITCHED TO 'A' LOOP. AFTER LEVEL OFF AT CRUISE. ' A' LOOP WARNING CAME ON AND WENT OFF. FOUND LOWER APRON 'A' AND 'B' LOOPS CHAFED. REPLACED 'A' AND 'B' APRON LOOPS, MF G P/N 5938323-505 AND 5938323-506, AND FIRE WARNING SYSTEM OPERATION CHECKED NORMAL. 2 L 7 2 4F RT A6WE 1996022300514 19960223 00514 WP 1996 2 23 96ZZZM214 1 19960114 A 3350 58531 POWER WIRE DOUG DC9 DC932 3022066 WP CABIN FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 926L 47172 STL - EMERGENCY EXIT LIGHT INOPERATIVE AT SEAT 12A. REMOVED AND REPLACED POWER WIRE, MFG P/N 5853-1. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996022300515 19960223 00515 WP 1996 2 23 ASAA9680031 1 19960120 A 5230 J0602283 DOOR FRAME DOUG DC9 DC982 3022082 WP CARGO COMPT CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 936AS 28441 49363 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FORWARD CARGO COMPARTMENT DOOR FRAME PAN AT Y370 TO Y427, X-15 TO X-18, Z -18. REPLACED DOOR FRAME PAN IAW DC-9 SRM 51-30-02, AND 53-05. (M) 2 L 7 2 4F A6WE 1996022300516 19960223 00516 WP 1996 2 23 CKSA96002 1 19960112 A 3240 27056511 BRACKET DOUG DC8 DC8F55 3021928 WP NLG WW CRACKED A CKSA O OTHER E VIBRATION/BUFFET CL CLIMB 1 GL 23 6161M 71329 45762 KMIA - AFTER TAKEOFF, HEARD LOUD NOISE AND VIBRATION COMING FROM NOSE GEAR AREA. CYCLED GEAR TWICE WITH NO CHANGE. ON THIRD CYCLE NOISE AND VIBRATION STOPPED. EXTENDED GEAR FOR LANDING, NO NOISE OR VIBRATION NOTED. INSPECTED NOSE WHEEL WELL, FOUND NOSE TIRE BRAKE PAD BRACKET CRACKED. REMOVED AND REPLACED NOSE TIRE BRAKE PAD BRACKET. NO OTHER DEFECTS NO TED. AIRCRAFT GOOD FOR FLIGHT. (M) 2 L 7 4 4F 4A25 1996022300517 19960223 00517 WP 1996 2 23 RRXA9600001 1 19960110 A 3233 47713921 ACTUATOR PIN DOUG DC8 DC871F 302199D WP LT MLG FAILED A RRXA O OTHER J WARNING INDICATION CL CLIMB 1 WP 15 500MH 45812 KDAY - FLT 525 - UPLATCH CHECK FAILED ON GEAR RETRACTION OUT OF KPIA. CYCLED GEAR NUMEROUS TIMES. GEAR UNSAFE AND GEAR DOOR WARNING LIGHTS ILLUMINATED. FERRIED A/C TO KMCN. MX FOUND THE LEFT MLG RETRACT CYCLINDER PIN BROKEN. MAINTENANC E INSPECTED THE BOSS AND PIN HOLE AND FOUND SERVICEABLE. MAINTENANCE INSTALLED A NEW BOSS PIN IAW SB 32-102. THE LEFT MLG OPERATED NORMALLY ON GEAR SWING IAW 32-10-1. (M) 2 L 7 4 4F RT 4A25 1996022300522 19960223 00522 NM 1996 2 23 USAA960013 1 19960104 A 5320 SHEAR BEAM BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 228US 43760 21817 ROA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND ONE .375 INCH CRACK STRINGER 18A LEFT SHEAR BEAM AT BS 727. INSTALLED DOUBLER. REPAIRED PER EO 5393G256 REV 'A' 11/01/95. (M) 2 L 7 2 4F A16WE 1996022300523 19960223 00523 NM 1996 2 23 USAA960014 1 19960104 A 5320 SHEAR BEAM BOEING 737 737201 1384454 NM BS 706 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 228US 43760 21817 ROA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND .375 INCH CRACK STRINGER 18A LEFT SHEAR BEAM WEB AT BS 706. INSTALLED DOUBLER. REPAIRED PER EO 5393G259 REV 'A' 11/01/95. (M) 2 L 7 2 4F A16WE 1996022300524 19960223 00524 NM 1996 2 23 USAA960015 1 19960105 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 34396 22888 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 CRACKS IN UPPER RADIUS OF FLOOR BEAM AND .5 INCH LONGITUDINAL CRACK BS 520 2 INCH CRACK AT LBL 24 AND RBL 24, AND .5 INCH CRACK AT LBL 45. INSTALLED REPAIRS AND PREVENTIVE MODIFICATION ON B S 520 FLOOR BEAM PER SB 727-53-1120 REV 1. REPAIRED PER EA 40569. (M) 2 L 7 2 4F A16WE 1996022300526 19960223 00526 NM 1996 2 23 USAA960017 1 19960105 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 328 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 34396 22888 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 12 CORRODED AREAS APPROX 1 INCH BY 1 INCH EACH AT FLOOR BEAM, BS 328 RBL 48 AND LBL 48. SPLICED IN NEW T-CAP. REPAIRED PER TR 53-10-13. CORROSION TASK NR C53-107-01, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996022300527 19960223 00527 NM 1996 2 23 USAA960018 1 19960105 A 5320 69353214 CLIP BOEING 737 7372B7 1384560 NM BS 597 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 34396 22888 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK IN STRINGER CLIP, BS 597 S-9 R. REPLACED CLIP, REPAIRED PER EO 5393G227. (M) 2 L 7 2 4F A16WE 1996022300528 19960223 00528 NM 1996 2 23 USAA960019 1 19960105 A 5320 6545834551 INTERCOSTAL BOEING 737 7372B7 1384560 NM BS 328-344 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 34396 22888 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK IN INTERCOSTAL BS 328 TO 344 LBL 17 INCHES. INSTALLED NEW INTERCOSTAL. (M) 2 L 7 2 4F A16WE 1996022300529 19960223 00529 NM 1996 2 23 USAA960020 1 19960105 A 5312 69389331 FITTING BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 34396 34396 22888 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK AT STATION 727 BULKHEAD STIFFENER FITTING IN LOWER FORWAR D RADIUS, BL 0 WL 202.5. REPAIRED PER EO 5394G176. (M) 2 L 7 2 4F A16WE 1996022300530 19960223 00530 NM 1996 2 23 USAA960021 1 19960105 A 5320 DOUBLER BOEING 737 7372B7 1384560 NM BS 500 DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 34396 22888 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND DAMAGE ON UNKNOWN DOUBLER 12 INCHES BY 18 INCHES STATION 500B BETWEEN ST RINGER 27R AND 26R. PREVIOUS INSTALLED EXT DOUBLER. REPAIRED PER SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1996022300531 19960223 00531 NM 1996 2 23 USAA960023 1 19960105 A 5313 65457768 STRINGER BOEING 737 7372B7 1384560 NM BS 1006 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 34396 22888 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION AT STRINGER 27R STATION 1006, 2 INCH BY 1 INCH. REPAIRED AND REPLACED SHORT STRINGER SECTION WITH NEW COMPLETE STRINGER. REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-208-01, CO RROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996022300532 19960223 00532 NM 1996 2 23 USAA960024 1 19960105 A 5320 65457768 SUPPORT BOEING 737 7372B7 1384560 NM BS 947 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 34396 22888 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCH BY 1 INCH AT FLOOR SUPPORT 10 PERCENT DEEP AT STRINGER 28L STATION 947. REPAIRED AND REPLACED STR SECTION AND REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-202-01, CORROSI ON LEVEL 2. (M) 2 L 7 2 4F A16WE 1996022300533 19960223 00533 NM 1996 2 23 USAA960025 1 19960105 A 5320 693535214 CLIP BOEING 737 7372B7 1384560 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 34396 22888 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK STRINGER TIE CLIP BS 787 STRINGER 10R. REPLACED CLIP, RE PAIRED PER EO 5393G227. (M) 2 L 7 2 4F A16WE 1996022300534 19960223 00534 NM 1996 2 23 USAA960026 1 19960105 A 5320 693535214 CLIP BOEING 737 7372B7 1384560 NM BS 767 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 34396 22888 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACKED STRINGER TIE CLIP BS 767 STRINGER 10R. REPLACED TIE CL IP, REPAIRED PER EO 5393G227. (M) 2 L 7 2 4F A16WE 1996022300535 19960223 00535 NM 1996 2 23 USAA960027 1 19960105 A 5320 693535214 CLIP BOEING 737 7372B7 1384560 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 34396 22888 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACKED STRINGER TIE CLIP BS 787 STRINGER 4R. REPLACED CLIP, R EPAIRED PER EO 5393G227. (M) 2 L 7 2 4F A16WE 1996022300536 19960223 00536 NM 1996 2 23 USAA960028 1 19960105 A 5320 693535214 CLIP BOEING 737 7372B7 1384560 NM BS 8007 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 34396 22888 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACKED TIE CLIP, BS 807, STRINGER 10R. REPLACED TIE CLIP, REP AIRED PER EO 5393G227. (M) 2 L 7 2 4F A16WE 1996022300537 19960223 00537 NM 1996 2 23 USAA960029 1 19960105 A 5320 693535214 CLIP BOEING 737 7372B7 1384560 NM BS 827 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 34396 22888 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACKED TIE CLIP, BS 827 STRINGER 10R. REPLACED TIE CLIP, REPA IRED PER EO 5393G227. (M) 2 L 7 2 4F A16WE 1996022300538 19960223 00538 NM 1996 2 23 USAA960030 1 19960105 A 5320 693535214 CLIP BOEING 737 7372B7 1384560 NM BS 685 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 34396 22888 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK IN STRINGER 3L TIE CLIP, AT BS 685. REPLACED TIE CLIP, R EPAIRED PER EO 5393G227. (M) 2 L 7 2 4F A16WE 1996022300539 19960223 00539 NM 1996 2 23 USAA960031 1 19960105 A 5320 693535214 CLIP BOEING 737 7372B7 1384560 NM BS 685 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 34396 22888 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .1250 INCH CRACK IN STRINGER 5L TIE CIP, BS 685. REPLACED TIE CLIP. RE PAIRED PER EO 5393G227. (M) 2 L 7 2 4F A16WE 1996022300540 19960223 00540 NM 1996 2 23 USAA960032 1 19960105 A 5320 693535214 CLIP BOEING 737 7372B7 1384560 NM BS 685 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 34396 22888 INT - DURING Q-5 CHECK VISUAL INSPECTION, .1250 INCH CRACK IN STRINGER 2R TIE CLIP, AT BS 685. REPLACED TIE CLIP, REPAI RED PER EO 5393G227. (M) 2 L 7 2 4F A16WE 1996022300541 19960223 00541 NM 1996 2 23 USAA960033 1 19960105 A 5320 5393G277 CLIP BOEING 737 7372B7 1384560 NM BS 685 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 22888 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .1250 INCH CRACK STRINGER 3R TIE CLIP, AT BS 685. REPLACED TIE CLIP, RE PAIRED PER EO 5393G227. (M) 2 L 7 2 4F A16WE 1996022300542 19960223 00542 NM 1996 2 23 USAA960034 1 19960105 A 5320 693535214 CLIP BOEING 737 7372B7 1384560 NM BS 685 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 34396 22888 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .1250 INCH CRACK IN STRINGER 4R TIE CLIP BS 685. REPLACED TIE CLIP, REP AIRED PER EO 5393G227. (M) 2 L 7 2 4F A16WE 1996022300543 19960223 00543 NM 1996 2 23 USAA960035 1 19960105 A 5320 693535214 CLIP BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 34396 22888 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .1250 INCH CRACK IN STRINGER 4R TIE CLIP, BS 727 B. REPLACED TIE CLIP, REPAIRED PER EO NR 5393G227. (M) 2 L 7 2 4F A16WE 1996022300544 19960223 00544 NM 1996 2 23 USAA960036 1 19960105 A 5320 693535214 CLIP BOEING 737 7372B7 1384560 NM BS 706 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 34396 22888 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK IN STRINGER 3R TIE CLIP AT BS 706. REPLACED CLIP, REPAIR ED PER EO 5393G227. (M) 2 L 7 2 4F A16WE 1996022300545 19960223 00545 NM 1996 2 23 USAA960037 1 19960105 A 5320 693535214 CLIP BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 34396 22888 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .1250 INCH CRACK IN STRINGER 5L TIE CLIP AT BS 727A. REPLACED CLIP, REP AIRED PER EO NR 5394G227. (M) 2 L 7 2 4F A16WE 1996022300546 19960223 00546 NM 1996 2 23 USAA960038 1 19960105 A 5320 693535214 CLIP BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 34396 22888 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK IN STRINGER 6L TIE CLIP, BS 727B. REPLACED CLIP, REPAIRE D PER EO NR 5393G227. (M) 2 L 7 2 4F A16WE 1996022300547 19960223 00547 NM 1996 2 23 USAA960039 1 19960105 A 5320 693535214 CLIP BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 34396 22888 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .1250 INCH CRACK IN STRINGER 7R TIE CLIP, BS 727B. REPLACED CLIP, REPAI RED PER EO NR 5393G227. (M) 2 L 7 2 4F A16WE 1996022300548 19960223 00548 NM 1996 2 23 USAA960040 1 19960105 A 5320 693535214 CLIP BOEING 737 7372B7 1384560 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 34396 22888 DURING Q-5 CHECK VISUAL INSPECTION, FOUND .1250 INCH CRACK IN STRINGER 3L, BS 747 AT STRINGER TIE CLIP. REPLACED CLIP, REPAIRED PER EO NR 5393G227. (M) 2 L 7 2 4F A16WE 1996022300549 19960223 00549 NM 1996 2 23 USAA960041 1 19960105 A 5320 693535214 CLIP BOEING 737 7372B7 1384560 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 34396 22888 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .1250 INCH CRACK IN STRINGER 10R TIE CLIP AT BS 747. REPLACED CLIP, REP AIRED PER EO NR 5393G227. (M) 2 L 7 2 4F A16WE 1996022300550 19960223 00550 NM 1996 2 23 USAA960042 1 19960105 A 5320 693535214 CLIP BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 34396 22888 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .1250 INCH CRACK IN STRINGER 5R TIE CLIP, BS 727 B. REPLACED CLIP, REPA IRED PER EO NR 5393G227. (M) 2 L 7 2 4F A16WE 1996022300551 19960223 00551 WP 1996 2 23 USAA960056 1 19960119 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 101 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 820US 37700 49119 PIT - DURING Q-6 INSPECTION, FOUND A .5 INCH CRACK STATION 101 RIGHT SIDE LEADING EDGE OF STROBE IN SKIN. REMOVED DAMAG ED AREA AND INSTALLED FILLER AND DOUBLER REPAIR PER USAIR TYPICAL REPAIR 53-30-11. (M) 2 L 7 2 4F A6WE 1996022300552 19960223 00552 WP 1996 2 23 USAA960057 1 19960119 A 5312 BULKHEAD DOUG DC9 DC982 3022082 WP FS 1338 CHAFFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 820US 37700 49119 PIT - DURING Q-6 INSPECTION, FOUND TWO CHAFFED 4 INCH RADIUS AREAS FROM LEFT ENGINE THRUST REVERSER CABLE DRUM SHAFT BOL T HEADS IN STATION 1338 AFT PRESSURE BULKHEAD AFT SIDE. INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 78-30-14. (M ) 2 L 7 2 4F A6WE 1996022300553 19960223 00553 WP 1996 2 23 USAA960058 1 19960119 A 5312 BULKHEAD DOUG DC9 DC982 3022082 WP BS 1338 CHAFFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 820US 37700 49119 PIT - DURING Q-6 INSPECTION, FOUND TWO CHAFFED 4 INCH RADIUS AREAS FROM RIGHT ENGINE THRUST REVERSER CABLE DRUM SHAFT BO LT HEADS IN STATION 1338 AFT PRESSURE BULKHEAD AFT SIDE. INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 78-30-14. ( M) 2 L 7 2 4F A6WE 1996022300554 19960223 00554 NM 1996 2 23 USAA960065 1 19960117 A 5320 DOOR FRAME BOEING 737 737401 1384701 NM BS 295 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 19812 23990 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK FORWARD SERVICE DOOR, FORWARD CUTOUT FRAME AT STATION 295, WL 209. CUTOUT DAMAGE AND INSTALLED A FLUSH REPAIR. (M) 2 L 7 2 4F RT A16WE 1996022300555 19960223 00555 NM 1996 2 23 USAA960066 1 19960117 A 5315 FLOOR BEAM BOEING 737 737401 1384701 NM BS 947 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 19812 23990 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER AREA OF CORROSION STATION 947 FLOOR BEAM UPPER FLANGE RB L 4, WL 208. CUTOUT DAMAGED FLOOR BEAM AND INSTALLED FILLER AND REPAIR ANGLES. REPAIRED PER SRM 53-60-51. CORROSION T ASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996022300556 19960223 00556 NM 1996 2 23 USAA960067 1 19960117 A 5320 65C333701 INTERCOSTAL BOEING 737 737401 1384701 NM BS 947-967 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 19812 23990 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH AREA OF CORROSION INTERCOSTAL UPPER FLANGE STATION 947 TO 967, LBL 25, WL 208. REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996022300557 19960223 00557 NM 1996 2 23 USAA960068 1 19960117 A 5315 FLOOR BEAM BOEING 737 737401 1384701 NM BS 344 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 19812 23990 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 53 INCHES CORROSION FLOOR BEAM, BS 344 LBL 37 TO RBL 16. INS TALLED T-CAP AND REPAIR ANGLE AND STRAPS. REPAIRED PER TR 53-10-03. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. ( M) 2 L 7 2 4F RT A16WE 1996022300558 19960223 00558 NM 1996 2 23 USAA960069 1 19960117 A 5320 BEAM BOEING 737 737401 1384701 NM BS 312 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 19812 23990 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 5 INCHES BY 40 INCHES CORRODED BEAM, BS 312 LBL 18 TO RBL 22. FABRICATE D AND INSTALLED T-CAP AND REPAIR ANGLES. REPAIRED PER TR 53-10-3. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M ) 2 L 7 2 4F RT A16WE 1996022300559 19960223 00559 NM 1996 2 23 USAA960070 1 19960117 A 5320 6545834255 INTERCOSTAL BOEING 737 737401 1384701 NM BS 294-312 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 19812 23990 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 1 INCH CORRODED INTERCOSTAL BETWEEN BS 294 THROUGH 312 RBL 11 . REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996022300560 19960223 00560 NM 1996 2 23 USAA960071 1 19960117 A 5315 FLOOR BEAM BOEING 737 737401 1384701 NM BS 294.5 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 19812 23990 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 50 INCHES CORRODED FLOOR BEAM BS 294.5 RBL 6, RBL 56. INSTAL LED T-CAP AND REPAIR ANGLES AND FILLER, REPAIRED PER SRM 53-10-51. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M ) 2 L 7 2 4F RT A16WE 1996022300561 19960223 00561 NM 1996 2 23 USAA960072 1 19960117 A 5330 SKIN BOEING 737 737401 1384701 NM BS 475 DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 19812 23990 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND UNKNOWN 4 INCH DIAMETER PREVIOUSLY INSTALLED SKIN DOUBLER, NO SDA ON FIL E BS 475 BETWEEN STRINGER 15R AND STRINGER 16R. DOUBLER INSTALLED PER SRM 53-00-01 FIG 208. (M) 2 L 7 2 4F RT A16WE 1996022300562 19960223 00562 NM 1996 2 23 USAA960073 1 19960117 A 5320 65C333671 INTERCOSTAL BOEING 737 737401 1384701 NM BS 947-967 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 19812 23990 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 3 INCH AREA OF CORROSION INTERCOSTAL UPPER FLANGE STATION 947 TO 967, LBL 51 WL 208. REPLACED WITH IDENTICAL PART NR 65C333671. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M ) 2 L 7 2 4F RT A16WE 1996022300563 19960223 00563 NM 1996 2 23 USAA960074 1 19960117 A 5315 FLOOR BEAM BOEING 737 737401 1384701 NM BS 328 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 19812 23990 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND SEVERAL AREAS .75 INCH BY .75 INCH CORROSION ON FLOOR BEAM STATION 328 R BL 11 TO RBL 57. SPLICED IN NEW UPPER CHORD SECTION. REPAIRED PER SRM 53-10-51. CORROSION TASK NR C53-107-02, CORROSI ON LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996022300564 19960223 00564 NM 1996 2 23 USAA960075 1 19960117 A 5320 65C80735116 ANGLE BOEING 737 737401 1384701 NM BS 947-1006 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 19812 23990 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY 2 INCH CORRODED AREAS LEFT Z-ANGLE BS 947 TO BS 1006. REPLACED WITH IDENTICAL PART NR 65C80735-116. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996022300565 19960223 00565 NM 1996 2 23 USAA960076 1 19960117 A 5320 6546812169 INTERCOSTAL BOEING 737 737401 1384701 NM BS 967-986 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 19812 23990 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA AT INTERCOSTAL BS 967 TO BS 986 LBL 16. R EPLACED WITH IDENTICAL PART NR 65-46812-169. REMOVED DEFECTIVE PART COMPLETED INSTALLATION OF INTERCOSTAL. REPAIRED PE R SRM 51-10-02. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996022300566 19960223 00566 NM 1996 2 23 USAA960077 1 19960117 A 5320 6546812169 INTERCOSTAL BOEING 737 737401 1384701 NM BS 967-986 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 19812 23990 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA INTERCOSTAL BS 967 TO BS 986 RBL 16 INCHE S. REPLACED WITH IDENTICAL PART NR 65-46812-169. REMOVED DAMAGED PART COMPLETED INSTALLATION OF INTERCOSTAL. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996022300567 19960223 00567 NM 1996 2 23 USAA960078 1 19960117 A 5320 654587545 ANGLE BOEING 737 737401 1384701 NM BS 285-355 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 19812 23990 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORROSION IN SEVERAL AREAS (NUTPLATES HOLES) BS 285 TO BS 355 RIGHT SIDE Z-ANGLE. REMOVED DAMAGED ANGLE COMPLETED INSTALLATION OF Z-ANGLE AND REPAIR PARTS. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C52-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996022300568 19960223 00568 NM 1996 2 23 USAA960079 1 19960117 A 5347 BAC1520792 SEAT TRACK BOEING 737 737401 1384701 NM BS 336 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 19812 23990 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND TWO 1 INCH DIAMETER SPOTS OF CORROSION (APPROX 25 PERCENT METAL LOSS), R BL 54.5 SEAT TRACK AT BS 336 AT SCREW HOLES. REMOVED SEAT TRACK, REPLACED SEAT TRACK COMPLETED REPAIR. REPAIRED PER SR M 53-00-52 FIG 202. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996022300569 19960223 00569 NM 1996 2 23 USAA960080 1 19960117 A 5320 6545834256 INTERCOSTAL BOEING 737 737401 1384701 NM BS 328-344 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 19812 23990 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH BY .5 INCH CORROSION AT INTERCOSTAL RBL 11 BETWEEN BS 328 THROUG H 344. REPLACED INTERCOSTAL. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996022300570 19960223 00570 NM 1996 2 23 USAA960081 1 19960117 A 5320 6545834260 INTERCOSTAL BOEING 737 737401 1384701 NM BS 312-328 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 19812 23990 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH BY.5 INCH CORROSION AT INTERCOSTAL LBL 11 BETWEEN BS 312-328. R EPLACED INTERCOSTAL. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996022300571 19960223 00571 NM 1996 2 23 USAA960082 1 19960117 A 5320 6545834259 INTERCOSTAL BOEING 737 737401 1384701 NM BS 328-344 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 19812 23990 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH BY .5 INCH CORROSION AT INTERCOSTAL LBL 11 BETWEEN BS 328-344. R EPLACED INTERCOSTAL. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996022300572 19960223 00572 NM 1996 2 23 USAA960083 1 19960117 A 5320 BAC150643 INTERCOSTAL BOEING 737 737401 1384701 NM BS 947-967 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 19812 23990 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH AREA OF CORROSION AT INTERCOSTAL UPPER FLANGE STATION 9 47 TO 967 LBL 16, WL 208. REPLACED WITH IDENTICAL P/N BAC1506-43. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107 -02, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996022300573 19960223 00573 NM 1996 2 23 USAA960084 1 19960117 A 5320 65C807351 ANGLE BOEING 737 737401 1384701 NM BS 947-1006 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 19812 23990 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND SEVERAL 2 INCH BY 2 INCH CORRODED AREAS AT BS 947 TO BS 1006 RIGHT SIDE Z-ANGLE. REMOVED RIGHT SIDE Z-ANGLE, COMPLETED INSTALLATION OF RIGHT SIDE Z-ANGLE. REPAIRED PER SRM 51-10-02, CORROSIO N TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996022300574 19960223 00574 NM 1996 2 23 USAA960085 1 19960117 A 5315 FLOOR BEAM BOEING 737 737401 1384701 NM BS 986 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 19812 23990 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY 1 INCH CORRODED NUT PLATE HOLES FLOOR BEAM, BS 986 LBL 45 INCHES TO RBL 45 INCHES. MODIFIED PART NR INSTALLED, EXT BAC1505-100703, 7075-T65, BAC1490-2887 AND 2886. REMOVED DAMAGED T-CAP. COMPLETED INSTALLATION OF T-CAP ON FLOOR SEAL AT BS 986.5. REPAIRED PER EA 40627. CORROSION TASK NR C5 3-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996022300575 19960223 00575 NM 1996 2 23 USAA960086 1 19960117 A 5320 6545834610 INTERCOSTAL BOEING 737 737401 1384701 NM BS 336 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 19812 23990 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 2 INCH AREA SURFACE CORROSION AT INTERCOSTAL, BS 336, RBL 59, WL 208. REPLACED CORRODED INTERCOSTAL WITH NEW PART. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSIO N LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996022300576 19960223 00576 NM 1996 2 23 USAA960087 1 19960117 A 5313 BAC15201357 STRINGER BOEING 737 737401 1384701 NM BS 787-847 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 19812 23990 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 2 INCH CORRODED AREA AT FLOOR STRINGER, BS 787 TO BS 847 RBL 1 4 INCHES. REMOVED DAMAGED FLOOR STRINGER, COMPLETED INSTALLATION AND REPAIR OF FLOOR STRINGER. REPAIRED PER SRM 53-00- 53 FIG 202 ALSO, SRM 51-10-2. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996022300577 19960223 00577 NM 1996 2 23 USAA960088 1 19960117 A 5315 FLOOR BEAM BOEING 737 737401 1384701 NM BS 360 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 19812 23990 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 2 INCH CORRODED AREA BL 0 BS 360, FLOOR BEAM. FABRICATED AND INSTALLED REPAIR ANGLE. REPAIRED PER SRM 53-30-51. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996022300578 19960223 00578 NM 1996 2 23 USAA960089 1 19960117 A 5312 SKIN BOEING 737 737401 1384701 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 19812 19812 23990 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK STATION 178 BULKHEAD SKIN LBL 4.75, WL 198. INSTALLED DOU BLER, REPAIRED PER EA 40743. (M) 2 L 7 2 4F RT A16WE 1996022300579 19960223 00579 NM 1996 2 23 USAA960090 1 19960117 A 5312 SKIN BOEING 737 737401 1384701 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 19812 19812 23990 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK STATION 178 BULKHEAD SKIN LBL 4.75, WL 201. INSTALLED DOU BLER, REPAIRED PER EA 40743. (M) 2 L 7 2 4F RT A16WE 1996022300580 19960223 00580 NM 1996 2 23 USAA960091 1 19960117 A 5320 65C3468824 BEAM BOEING 737 737401 1384701 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 19812 23990 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK UPPER T-CAP IN RADIUS BS 520 RBL 45.5, BEAM. CONTAINED CRA CK INSTALLED U-CHANNEL AND RADIUS BLOCKS AND COMPLETED REPAIR, EA 40649. (M) 2 L 7 2 4F RT A16WE 1996022300581 19960223 00581 NM 1996 2 23 USAA960092 1 19960117 A 5312 SKIN BOEING 737 737401 1384701 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 19812 19812 23990 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .1875 INCH CRACK STATION 178 BULKHEAD SKIN RBL 4.75 WL 201. INSTALLED D OUBLER, REPAIRED PER EA 40743. (M) 2 L 7 2 4F RT A16WE 1996022300582 19960223 00582 NM 1996 2 23 USAA960093 1 19960117 A 5315 FLOOR BEAM BOEING 737 737401 1384701 NM BS 520 WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 19812 23990 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH GROOVE WORN INTO CHANNEL ON CABIN FLOOR BEAM AT BS 520 AT BBL 0 . INSTALLED REPAIR PER SB AND EA. REPAIRED PER SB 737-53-1120 REV 1 AND REV 2 AND EA 40548. (M) 2 L 7 2 4F RT A16WE 1996022300583 19960223 00583 NM 1996 2 23 USAA960095 1 19960117 A 5315 FLOOR BEAM BOEING 737 737401 1384701 NM BS 520 WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 19812 23990 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .1875 GROOVE WORN IN CHANNEL ON CABIN FLOOR BEAM, BS 520 AT LBL 24.75. I NSTALLED REPAIR PER SB AND EA, REPAIRED PER SB 737-53-1120 REV 1 AND EA 40649. (M) 2 L 7 2 4F RT A16WE 1996022300584 19960223 00584 NM 1996 2 23 USAA960096 1 19960117 A 5315 FLOOR BEAM BOEING 737 737401 1384701 NM BS 520 WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 19812 23990 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .1875 INCH GROOVE WORN INTO CHANNEL ON CABIN FLOOR BEAM, BS 520 AT RBL 2 4.75. INSTALLED REPAIR PER SB AND EA. REPAIRED PER SB 737-53-1120 REV 1 AND EA 40649. (M) 2 L 7 2 4F RT A16WE 1996022300585 19960223 00585 NM 1996 2 23 USAA960105 1 19960125 A 5330 FUSELAGE SKIN BOEING 767 7672B7 1385107 NM BS 390 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 652US 24329 24765 CLT - INSPECTION VISUALLY FOUND A 12 INCH LONG BY 2 INCH WIDE BY .250 INCH DEEP DENT IN THE FUSELAGE SKIN LOCATED AT STA TION 390 BETWEEN STRINGER 28R AND STRINGER 24R. INSTALLED DOUBLER (TIME LIMITED REPAIR) AS PER USAIR EA NR 40719. (M) 2 L 7 2 4F RT A1NM 1996022300586 19960223 00586 NM 1996 2 23 USAA960107 1 19960125 A 5320 6545834261 ANGLE BOEING 737 7372B7 1384560 NM BS 292-300 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 8 INCH CORROSION AT CABIN FLOOR SUPPORT ANGLE, STATION 292 TO STATION 300 LBL 12. REPLACED ANGLE, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996022300587 19960223 00587 NM 1996 2 23 USAA960108 1 19960125 A 5320 6545834252 BEAM BOEING 737 7372B7 1384560 NM BS 277-294.5 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 3 INCH CORROSION ON BEAM AT BS 277-294.5 LBBL 12. REPLACED ANGLE, REPAI RED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996022300588 19960223 00588 NM 1996 2 23 USAA960109 1 19960125 A 5320 6940276 TIE CLIP BOEING 737 7372B7 1384560 NM BS 1064 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK IN STRINGER TIE CLIP, STATION 1064 STRINGER 17L. INSTALL ED NEW TIE CLIP MFG PER BOEING DRAWING 69-40276. REPAIRED PER BOEING ASSEMBLY DRAWING 69-40276. (M) 2 L 7 2 4F A16WE 1996022300589 19960223 00589 NM 1996 2 23 USAA960110 1 19960125 A 5320 INTERCOSTAL BOEING 737 7372B7 1384560 NM BS 927-947 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 2 INCH CORROSION INTERCOSTAL STATION 927 TO STATION 947 RBL 8 INCH. INSTALLED NEW INTERCOSTAL. REPAIRED PER DRAWING 65-67316. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996022300590 19960223 00590 NM 1996 2 23 USAA960111 1 19960125 A 5320 693535214 TIE CLIP BOEING 737 7372B7 1384560 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP BS 747 STRINGER 6R. REPLACED TIE CLIP . REPAIRED PER EA 5393G227. MODIFIED PART NR INSTALLED 69-35352-14. (M) 2 L 7 2 4F A16WE 1996022300591 19960223 00591 NM 1996 2 23 USAA960112 1 19960125 A 5320 693535214 TIE CLIP BOEING 737 7372B7 1384560 NM BS 827 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .1250 INCH CRACK STRINGER TIE CLIP BS 827 STRINGER 47. REPLACED TIE CLI P. REPAIRED PER EA 5393G227. MODIFIED PART NR INSTALLED 69-35353-14. (M) 2 L 7 2 4F A16WE 1996022300592 19960223 00592 NM 1996 2 23 USAA960113 1 19960125 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK BS 520 LBL 25 WL 207.75 UPPER CHORD FLOOR BEAM. STOP DRI LLED CRACK .25 INCH. INSTALLED REPAIR DOUBLER AND FLOOR BEAM MOD. REPAIRED PER EA 40741. (M) 2 L 7 2 4F A16WE 1996022300593 19960223 00593 NM 1996 2 23 USAA960114 1 19960125 A 5320 6545834252 ANGLE BOEING 737 7372B7 1384560 NM BS 292-300 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .1875 INCH BY 3 INCH AND .1875 INCH BY 2 INCH CORROSION AT CABIN FLOOR S UPPORT ANGLE, BS 292 THROUGH BS 300. REPLACED SUPPORT ANGLE, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, C ORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996022300594 19960223 00594 NM 1996 2 23 USAA960115 1 19960125 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 328 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER CORROSION PIT, TOP CAP FLOOR BEAM, STATION 328 AT RBL 20 . REMOVED TOP 'T' OF FLOOR BEAM AND INSTALLED NEW T-CAP. REPAIRED PER TYPICAL REPAIR 53-10-13. CORROSION TASK NR C53- 107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996022300595 19960223 00595 NM 1996 2 23 USAA960117 1 19960125 A 5320 6940276 TIE CLIP BOEING 737 7372B7 1384560 NM BS 1064 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK AT TIE CLIP, STATION 1064 STR 9 L. REPLACED CRACKED TIE CLIP WITH ONE FABRICATED PER ORIG DRAWING. REPAIRED PER BOEING DRAWING 69-40276. (M) 2 L 7 2 4F A16WE 1996022300596 19960223 00596 NM 1996 2 23 USAA960118 1 19960125 A 5311 FRAME BOEING 737 7372B7 1384560 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK AT FRAME BS 616, 5 INCHES BELOW FLOOR LEVEL LEFT SIDE. CUT OUT DAMAGE, INSTALLED ANGLE AND FILLER. REPAIRED PER EA 40740. (M) 2 L 7 2 4F A16WE 1996022300597 19960223 00597 NM 1996 2 23 USAA960119 1 19960125 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM FS 328 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER CORROSION FLOOR BEAM FS 328 RBL 20 1/2. REMOVED DAMAGED 'T' CHORD FROM LBL 29 TO RBL 65. REPAIRED PER TYPICAL REPAIR NR 53-10-13 AND SRM CHAPTER 51-40-2 FIG 1. CORROSION TAS K NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996022300598 19960223 00598 NM 1996 2 23 USAA960120 1 19960125 A 5320 ANGLE BOEING 737 7372B7 1384560 NM BS 308 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 3 INCH CORROSION STATION 308 LBL 24 TO LBL 30 ANGLE AT BULKHEA D. REPLACED ANGLE, REPAIRED PER SRM 51-10-01. (M) 2 L 7 2 4F A16WE 1996022300599 19960223 00599 NM 1996 2 23 USAA960121 1 19960125 A 5311 65465394950 FRAME BOEING 737 7372B7 1384560 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT -DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 616, 5 INCHES FLOOR LEVEL RIGHT SIDE FRAME. CUT OUT DAMA GE INSTALLED ANGLE AND FILLER. REPAIRED PER EA 40740. (M) 2 L 7 2 4F A16WE 1996022300600 19960223 00600 NM 1996 2 23 USAA960122 1 19960125 A 5320 CHORD BOEING 737 7372B7 1384560 NM BS 710 CHAFFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 17 INCHES BY 2 INCHES CHAFFED AND FRETTING LEFT CHORD BS 710 TO BS 727. FABRICATED WASHERS AND STRAP AND INSTALLED. REPAIRED PER EA 40745. (M) 2 L 7 2 4F A16WE 1996022300601 19960223 00601 NM 1996 2 23 USAA960123 1 19960125 A 5320 1123053 CHANNEL BOEING 737 7372B7 1384560 NM BS 307 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCH BY 2 INCH STATION 307 LBL 11 TO LBL 42 AT CHANNEL. REP LACED CHANNEL. REPAIRED PER SRM 51-10-01. (M) 2 L 7 2 4F A16WE 1996022300602 19960223 00602 NM 1996 2 23 USAA960124 1 19960125 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 706-710 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CRACK IN WEB 4 INCHES AT FLOOR BEAM, BL O, STATION 706-710. CUTOUT CRAC KED WEB AND INSTALLED FILLER AND DOUBLER. REPAIRED PER BOEING REPAIR DRAWING NR 65C34537. (M) 2 L 7 2 4F A16WE 1996022300603 19960223 00603 NM 1996 2 23 USAA960125 1 19960125 A 5311 FRAME BOEING 737 7372B7 1384560 NM BS 794 DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH BLEND OUT AFT CARGO FORWARD FRAME BS 794 STRINGER 19R THROUGH STR INGER 20R. INSTALLED DOUBLER. REPAIRED PER SRM 51-40-3. (M) 2 L 7 2 4F A16WE 1996022300604 19960223 00604 NM 1996 2 23 USAA960126 1 19960125 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 312 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 20 INCH CORROSION FLOOR BEAM STATION 312, LBL 11 TO RBL 11. R EPLACED T-CAP. REPAIRED PER TR 53-10-13. (M) 2 L 7 2 4F A16WE 1996022300605 19960223 00605 NM 1996 2 23 USAA960127 1 19960125 A 5315 6545410 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 680 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CRACK IN WEB CUT OUT FOR LEFT AILERON BELLCRANK (1 INCH CRACK), BS 680 L BL 24 AND RBL 24 WEB OF FLOOR BEAM AT AILERON CUTOUT. INSTALLED REINFORCEMENT. REPAIRED PER EA 40739 AND SB 737-53-113 0, R 4 FIG 5. (M) 2 L 7 2 4F A16WE 1996022300606 19960223 00606 NM 1996 2 23 USAA960128 1 19960125 A 5320 TIE CLIP BOEING 737 7372B7 1384560 NM BS 706 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK BS 706 STRINGER 4L TIE CLIP. INSTALLED NEW TIE CLIP. REP AIRED PER EA 5393G227. (M) 2 L 7 2 4F A16WE 1996022300607 19960223 00607 NM 1996 2 23 USAA960129 1 19960125 A 5320 693585214 TIE CLIP BOEING 737 7372B7 1384560 NM BS 685 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP, STRINGER 4R, BS 685. INSTALLED NEW T IE CLIP. REPAIRED PER EA 5393G227. MODIFIED PART NR INSTALLED 69-35852-14. (M) 2 L 7 2 4F A16WE 1996022300608 19960223 00608 NM 1996 2 23 USAA960130 1 19960125 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 344 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 2 PLACES 3 INCHES BY 8 INCHES AND 3 INCHES BY 20 INCHES FLOOR BEAM T-CAP, BS 344 LBL 55 AND RBL 8 TO LBL 14. REPLACED 4 FEET OF T-CAP. REPAIRED PER TR 53-10-13. (M) 2 L 7 2 4F A16WE 1996022300609 19960223 00609 NM 1996 2 23 USAA960131 1 19960125 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK HIGH FREQUENCY EDDY CURRENT, FOUND .0625 INCH CRACK BS 520 LBBL 45.50 FLOOR BEAM. INSTALLED DOUB LER. REPAIRED PER EA 40741 SB 737-53-1120. (M) 2 L 7 2 4F A16WE 1996022300610 19960223 00610 NM 1996 2 23 USAA960132 1 19960125 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 EDDY CURRENT INSPECTION, FOUND .5 INCH CRACK BS 520 RBBL 45.50 FLOOR BEAM. INSTALLED DOUBLER. REPAIRE D PER EA 40741 SB 737-53-1120. (M) 2 L 7 2 4F A16WE 1996022300611 19960223 00611 NM 1996 2 23 USAA960133 1 19960125 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK BS 520 RBBL 25 FLOOR BEAM. INSTALLED DOUBLER. REPAIRED PE R EA 40741 SB 737-53-1120. (M) 2 L 7 2 4F A16WE 1996022300612 19960223 00612 NM 1996 2 23 USAA960135 1 19960125 A 5320 693535214 TIE CLIP BOEING 737 7372B7 1384560 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP BS 787 STRINGER 6 RT. REPLACED TIE CL IP. REPAIRED PER EA 5393G227. MODIFIED PART NR INSTALLED 693535214. (M) 2 L 7 2 4F A16WE 1996022300613 19960223 00613 NM 1996 2 23 USAA960136 1 19960125 A 5320 693535214 TIE CLIP BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP BS 727 A STRINGER 7A. REPLACED TIE CL IP. REPAIRED PER EA 5393G227. MODIFIED PART NR INSTALLED 69-35352-14. (M) 2 L 7 2 4F A16WE 1996022300614 19960223 00614 NM 1996 2 23 USAA960137 1 19960125 A 5320 693535214 TIE CLIP BOEING 737 7372B7 1384560 NM BS 827 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP BS 827 STRINGER 6R. REPLACED TIE CLIP . REPAIRED PER EA 5393G227. MODIFIED PART NR INSTALLED 69-35352-14. (M) 2 L 7 2 4F A16WE 1996022300615 19960223 00615 NM 1996 2 23 USAA960138 1 19960125 A 5320 693535214 TIE CLIP BOEING 737 7372B7 1384560 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP STRINGER 7R BS 747. REPLACED TIE CLIP . REPAIRED PER EA 5393G227. MODIFIED PART NR INSTALLED 69-35352-14. (M) 2 L 7 2 4F A16WE 1996022300616 19960223 00616 NM 1996 2 23 USAA960139 1 19960125 A 5320 693535214 TIE CLIP BOEING 737 7372B7 1384560 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP BS 787, STRINGER 5R. REPLACED TIE CLI P. REPAIRED PER EA 5393G227. MODIFIED PART NR INSTALLED 69-35352-14. (M) 2 L 7 2 4F A16WE 1996022300617 19960223 00617 NM 1996 2 23 USAA960140 1 19960125 A 5320 693535214 TIE CLIP BOEING 737 7372B7 1384560 NM BS 767 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK AT TIE CLIP BS 767, STRINGER 7L. REPLACED TIE CLIP. REP AIRED PER EA 5393G227. MODIFIED PART NR INSTALLED 69-35352-14. (M) 2 L 7 2 4F A16WE 1996022300618 19960223 00618 NM 1996 2 23 USAA960141 1 19960125 A 5320 69414606 FITTING BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK BS 727 RBL 6.5 KEEL BEAM VERTICAL STIFFENER FITTING. REPL ACED FITTING, REPAIRED PER BOEING DRAWING 65-46547. (M) 2 L 7 2 4F A16WE 1996022300619 19960223 00619 NM 1996 2 23 USAA960142 1 19960125 A 5320 693535214 TIE CLIP BOEING 737 7372B7 1384560 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK AT TIE CLIP BS 787, STRINGER 8L. REPLACED TIE CLIP. REPA IRED PER EO 5393G227. MODIFIED PART NR INSTALLED 6935352-14. (M) 2 L 7 2 4F A16WE 1996022300620 19960223 00620 NM 1996 2 23 USAA960143 1 19960125 A 5320 693535214 TIE CLIP BOEING 737 7372B7 1384560 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK AT TIE CLIP, BS 616 STRINGER 2L. REPLACED TIE CLIP. REP AIRED PER EA 5393G227. MODIFIED PART NR INSTALLED 69-35352-14. (M) 2 L 7 2 4F A16WE 1996022300621 19960223 00621 NM 1996 2 23 USAA960144 1 19960125 A 5320 693535214 TIE CLIP BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER 2R BS 727A, AT STRINGER TIE CLIP. REPLACED TIE CLIP. REPAIRED PER EA 5393G227. MODIFIED PART NR INSTALLED 69-35352-14. (M) 2 L 7 2 4F A16WE 1996022300622 19960223 00622 NM 1996 2 23 USAA960145 1 19960125 A 5320 693535214 TIE CLIP BOEING 737 7372B7 1384560 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP STRINGER 2R, BS 616. REPLACED TIE CLI P. REPAIRED PER EA 5393G227. MODIFIED PART NR INSTALLED 6935352-14. (M) 2 L 7 2 4F A16WE 1996022300623 19960223 00623 NM 1996 2 23 USAA960146 1 19960125 A 5320 653535214 TIE CLIP BOEING 737 7372B7 1384560 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK STRINGER 3R BS 616 STRINGER TIE CLIP. REMOVED AND REPLAC ED TIE CLIP. REPAIRED PER EA 5393G227. MODIFIED PART NR INSTALLED 653535214. (M) 2 L 7 2 4F A16WE 1996022300624 19960223 00624 NM 1996 2 23 USAA960147 1 19960125 A 5320 TIE CLIP BOEING 737 7372B7 1384560 NM BS 807 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT -DURING Q-4 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK BS 807 STRINGER 4L AT TIE CLIP. INSTALLED NEW CLIP. REPAI RED PER EA 5393G227. (M) 2 L 7 2 4F A16WE 1996022300625 19960223 00625 NM 1996 2 23 USAA960148 1 19960125 A 5320 693535214 TIE CLIP BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER 5R BS 727B AT STRINGER TIE CLIP. INSTALLED NEW MODIFIED TIE CLIP PER EO 5393G227. REPAIRED PER EO 5393G227. MODIFIED PART NR INSTALLED 6935352-14. (M) 2 L 7 2 4F A16WE 1996022300626 19960223 00626 NM 1996 2 23 USAA960149 1 19960125 A 5320 69353214 TIE CLIP BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP STRINGER 4R, BS 727B. INSTALLED NEW T IE CLIP PER EO 5393G227, REPAIRED PER EO 5393G227. MODIFIED PART NR INSTALLED 69-3532-14. (M) 2 L 7 2 4F A16WE 1996022300627 19960223 00627 NM 1996 2 23 USAA960150 1 19960125 A 5320 TIE CLIP BOEING 737 7372B7 1384560 NM BS 807 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK BS 807 STRINGER 5L TIE CLIP. INSTALLED NEW CLIP. REPAIRE D PER EA 5393G227. (M) 2 L 7 2 4F A16WE 1996022300628 19960223 00628 NM 1996 2 23 USAA960151 1 19960125 A 5320 TIE CLIP BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER 6R BS 727B AT STRINGER TIE CLIP. INSTALLED NEW CLIP. REPAIRED PER EA 5393G227. (M) 2 L 7 2 4F A16WE 1996022300629 19960223 00629 NM 1996 2 23 USAA960152 1 19960125 A 5320 693535214 TIE CLIP BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP STRINGER 4R BS 727A. REMOVED DAMAGED TIE CLIP, REPLACED AND COMPLETED INSTALLATION OF TIE CLIP. REPAIRED PER EA 53936227. DEFECTIVE PART REPLACED WITH IDEN TICAL PART NR 69-35352-14. (M) 2 L 7 2 4F A16WE 1996022300630 19960223 00630 NM 1996 2 23 USAA960153 1 19960125 A 5320 693535214 TIE CLIP BOEING 737 7372B7 1384560 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK AT STRINGER TIE CLIP STRINGER 4R BS 616. REPLACED TIE C LIP. REPAIRED PER EA 5393G227. MODIFIED PART NR INSTALLED 69-35-352-14. (M) 2 L 7 2 4F A16WE 1996022300631 19960223 00631 NM 1996 2 23 USAA960154 1 19960125 A 5330 693535214 TIE CLIP BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK TIE CLIP BS 727B S-1 L. REPLACED TIE CLIP. REPAIRED PER EO 5393G227. MODIFIED PART NR INSTALLED 69-35352-14. (M) 2 L 7 2 4F A16WE 1996022300632 19960223 00632 NM 1996 2 23 USAA960155 1 19960125 A 5320 693535214 TIE CLIP BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK TIE CLIP BS 727B STRINGER 8L. REPLACED TIE CLIP. REPAIRE D PER EO 5393G227. MODIFIED PART NR INSTALLED 69-35352-14. (M) 2 L 7 2 4F A16WE 1996022300633 19960223 00633 NM 1996 2 23 USAA960156 1 19960125 A 5320 693535214 TIE CLIP BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK AT STRINGER TIE CLIP STRINGER 6R BS 727A. REPLACED TIE CLIP. REPAIRED PER EA 5393G227. MODIFIED PART NR INSTALLED 69-35352-14. (M) 2 L 7 2 4F A16WE 1996022300634 19960223 00634 NM 1996 2 23 USAA960157 1 19960125 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 947 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 24 INCH CORROSION AT CABIN FLOOR BEAM STATION 947 LBL 12 INCHE S TO RBL 12 INCHES. INSTALLED T-CAP AND REPAIRED DOUBLERS. REPAIRED PER TR 53-10-13. CORROSION TASK NR C53-107-02, CO RROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996022300635 19960223 00635 NM 1996 2 23 USAA960158 1 19960125 A 5320 INTERCOSTAL BOEING 737 7372B7 1384560 NM BS 947-967 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 35219 22885 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA INTERCOSTAL STATION 947 TO 967 LBL 17 INC HES. REMOVED AND REPLACED WITH NEW INTERCOSTAL. REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEV EL 2. (M) 2 L 7 2 4F A16WE 1996022300636 19960223 00636 NM 1996 2 23 USAA960159 1 19960127 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 947 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 223US 46301 21665 ROA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND 17 INCH STR 27L CORRODED AT STATION 947 STRINGER 27L. REPAIRED STRINGE R STR SPLICE, REPAIRED PER SRM 53-10-3, PG 3. (M) 2 L 7 2 4F A16WE 1996022300637 19960223 00637 NM 1996 2 23 USAA960160 1 19960127 A 5330 SKIN BOEING 737 737201 1384454 NM ENTRY DOOR AREA CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 223US 46301 21665 ROA - DURING CX-5 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND HINGE CUTOUT AFT ENTRY DOOR SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-03 FIG 34. (M) 2 L 7 2 4F A16WE 1996022300638 19960223 00638 NM 1996 2 23 USAA960161 1 19960127 A 5320 SHEAR BEAM BOEING 737 737201 1384454 NM BS 706 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 223US 46301 21665 INT - DURING CX-5 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND .75 INCH CRACK AT SHEAR BEAM STRINGER 18A, STATION 706 . INSTALLED REPAIR ANGLES AND DOUBLERS. REPAIRED PER EO 5393G256 PART 3 SECTION IV. (M) 2 L 7 2 4F A16WE 1996022300639 19960223 00639 NM 1996 2 23 USAA960162 1 19960129 A 5330 SKIN BOEING 757 757225 1384959 NM FS 1681.8-1701 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 609AU 35206 22205 CLT - INSPECTION VISUALLY FOUND AN 8 INCH BY 8 INCH CORROSION EXTERNAL DOUBLER NOT PER SRM LOCATED AT FS 1681.8 THROUGH 1701 BETWEEN STRINGER 17 AND STRINGER 19L. FABRICATED AND INSTALLED EXTERIOR DOUBLER AS PER USAIR EA 40578 AND BOEING S RM 53-60-10. (M) 2 L 7 2 4F RT A2NM 1996022300640 19960223 00640 NM 1996 2 23 USAA960163 1 19960220 A 5311 65025229 FRAME BOEING 737 7373B7 1384580 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 504AU 35827 23379 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .300 INCH CRACK AFT CARGO BELOW FLOOR BS 727D BETWEEN STRINGER 27L AND STRINGER 27R ON FRAME. INSTALLED DOUBLER AND REPAIR FILLER AND REPAIR ANGLE PER REPAIR DOCUMENT EA 61538 AND SRM 53-00 -07 FIG 201. (M) 2 L 7 2 4F RT A16WE 1996022300641 19960223 00641 NM 1996 2 23 USAA960164 1 19960220 A 5400 301A3109 DOUBLER BOEING 737 7373B7 1384580 NM NR 1 PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 504AU 35827 23379 CLT - DURING Q-6 CHECK EDDY CURRENT INSPECTION, FOUND A 3 INCH CRACK AT NR 1 ENGINE PYLON PANEL 5724L DOUBLER. INSTALLE D DOUBLER PER SRM TYPICAL REPAIR 54-50-04D. (M) 2 L 7 2 4F RT A16WE 1996022300642 19960223 00642 NM 1996 2 23 USAA960165 1 19960129 A 5414 SKIN BOEING 757 757225 1384959 NM NR 2 PYLON CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 609AU 35206 22205 CLT - INSPECTION VISUALLY FOUND EXFOLIATION LEVEL 2 CORROSION BETWEEN SKIN AND DOUBLER, 2 INCHES LOCATED INBOARD PYLON I N AREA OF HEAT SHIELD NR 2 PYLON. REPLACED PYLON SKIN INBOARD AS PER USAIR 40605 AND USAIR EO 5492R274. (M) 2 L 7 2 4F RT A2NM 1996022300643 19960223 00643 NM 1996 2 23 USAA960166 1 19960129 A 5414 SKIN BOEING 757 757225 1384959 NM NR 2 PYLON CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 609AU 35206 22205 CLT - INSPECTION VISUALLY FOUND AN EXFOLIATION LEVEL 2 CORROSION BETWEEN SKIN AND DOUBLER 4 INCHES OUTBOARD PYLON SKIN I N AREA OF HEAT SHIELD NR 2 PYLON. REPLACED PYLON SKIN OUTBOARD AS PER USAIR EA 40605, EA 40669 AND USAIR EO 05492R274. (M) 2 L 7 2 4F RT A2NM 1996022300644 19960223 00644 NM 1996 2 23 USAA960167 1 19960129 A 5330 SKIN BOEING 757 757225 1384959 NM BS 1280 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 609AU 35206 22205 CLT - INSPECTION VISUALLY FOUND A SHARP DENT 1 INCH DIAMETER .145 INCH DEEP, 3 INCHES FORWARD BS 1280 BETWEEN STRINGER 1 280 BETWEEN STRINGER 24L AND STRINGER 25L. INSTALLED FLUSH PATCH REPAIR AS PER BOEING SRM 53-00-01. (M) 2 L 7 2 4F RT A2NM 1996022300645 19960223 00645 NM 1996 2 23 USAA960168 1 19960129 A 5330 SKIN BOEING 757 757225 1384959 NM BS 1738 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 609AU 35206 22205 CLT - INSPECTION VISUALLY FOUND A DENT 1 INCH DIAMETER BY .50 INCH DEEP (APPROXIMATELY 1.25 INCH BY .75 INCH) LOCATED AT BS 1738, S27L. INSTALLED DOUBLER AS PER USAIR EA 58015 AND BOEING SRM 53-00-01. (M) 2 L 7 2 4F RT A2NM 1996022300646 19960223 00646 NM 1996 2 23 USAA960169 1 19960129 A 5330 SKIN BOEING 757 757225 1384959 NM BS 231.5 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 609AU 35206 22205 CLT - INSPECTION VISUALLY AND BY HFEC, FOUND A DENT 5.5 INCH BY 3.75 INCH BY .130 INCH DEEP IN THE FUSELAGE SKIN LOCATED AT BS 231.5, OUTBOARD CHORD ABOVE AOA VANE. REPLACED CHORD ANGLES AND REPAIRED W/SKIN FILLER AND DOUBLER AS PER EA 405 96. (M) 2 L 7 2 4F RT A2NM 1996022300647 19960223 00647 EU 1996 2 23 USAA960196 1 19960201 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 482US 21531 11231 PIT - DURING SIP INSPECTION, FOUND .25 INCH CRACK IN THE LOWER AFT APERTURE FRAME CORNER SIP REF 53-10-20 EDDY CURRENT. REMOVED DAMAGED AREA AND INSTALLED FILLER PLUG AND 2 DOUBLERS PER SRM 53-02-16. (M) 2 L 7 2 4F RT A20EU 1996022300648 19960223 00648 EU 1996 2 23 USAA960197 1 19960201 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 482US 21531 11231 PIT - DURING SIP INSPECTION, FOUND 2 CRACKS, .25 INCH FWD AND .25 INCH AFT SED UPPER APERTURE FRAME CORNERS, SIP REF 53- 10-20 EDDY CURRENT. REMOVED DAMAGED AREAS AND INSTALLED DOUBLER REPAIR AND FILLER PLUGS PER USAIR TYPICAL REPAIR 53-10- 04. (M) 2 L 7 2 4F RT A20EU 1996022300649 19960223 00649 EU 1996 2 23 USAA960198 1 19960201 A 5312 BLKHD ANGLE FOKKER F28 F28MK4000 4990810 EU FWD PRESS BLKHD CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 482US 21531 11231 PIT - DURING SIP INSPECTION, FOUND 2 CRACKS, 3 INCHES AND 1.5 INCHES A REPAIR DOUBLER AT THE FORWARD PRESSURE BULKHEAD F S 1550 AFT SIDE OF LOWER CONNECTION ANGLE SIP REF 53-10-06 VISUAL/EDDY CURRENT. REMOVED DOUBLERS, STOP DRILLED CRACKS A ND INSTALLED NEW DOUBLERS PER SRM 53-02-18. (M) 2 L 7 2 4F RT A20EU 1996022300650 19960223 00650 WP 1996 2 23 USAAD96002A 1 19960106 A 3244 TIRE DOUG DC9 DC931 3022065 WP NR 3 MLG FAILED A USAA A UNSCHED LANDING D INFLIGHT SEPARATION TO TAKEOFF 1 EA 19 929VJ 9973 6921 48118 CLT - FLIGHT NR 328 - UPON TAKEOFF AT CLT, THE NR 3 MAIN TIRE LOST THE RECAP. GEAR WAS NOT RETRACTED. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 3 AND NR 4 (P/N 3910063507) WHEELS, A MAIN LAN DING GEAR SENSOR (DAMAGED), A RIGHT INBOARD TRAILING EDGE FLAP PANEL (DAMAGED), AND THE C1 FAN ASSEMBLY ON THE RIGHT ENG INE (DAMAGE). (M) 2 L 7 2 4F A6WE 1996022300651 19960223 00651 WP 1996 2 23 USAAD96003A 1 19960106 A 3230 RETRACT MECH DOUG DC9 DC931 3022065 WP NLG/LT MLG LACK OF LUBE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 986VJ 47209 SYR - UPON TAKEOFF FROM SYR, CREW RECEIVED NOSE AND LEFT MAIN GEARS UNSAFE LIGHTS. NEITHER GEARED RETRACTED. FLIGHT RE TURNED TO SYR AND LANDED WITH NO FURTHER INCIDENT. THE AIRCRAFT WAS FERRIED TO PHL, WHERE IT WAS JACKED AND THE GEAR SW UNG. NO DEFECTS WERE NOTED. MAINTENANCE LUBED THE GEAR AND RELEASED THE AIRCRAFT FOR SERVICE. (M) 2 L 7 2 4F A6WE 1996022300652 19960223 00652 WP 1996 2 23 USAAD96005 1 19960120 A 3230 RETRACT MECH DOUG DC9 DC982 3022082 WP NLG MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 823US 49142 MCO - AFTER TAKEOFF FROM MCO, NOSE GEAR WOULD NOT RETRACT. FLIGHT RETURNED TO MCO AND LANDED WITH NO FURTHER INCIDENT. (M) 2 L 7 2 4F A6WE 1996022300653 19960223 00653 WP 1996 2 23 USAAD96005A 1 19960110 A 3230 BOLTS DOUG DC9 DC982 3022082 WP NLG MISSING A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 823US 49142 MCO - AFTER TAKEOFF FROM MCO, NOSE GEAR WOULD NOT RETRACT. CREW TRIED TO CYCLE THE GEAR TO NO AVAIL. FLIGHT RETURNED T O MCO AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED BOLTS IN THE NOSE GEAR SPRAY DEFLECTOR AND LUBED THE GE AR. (M) 2 L 7 2 4F A6WE 1996022300654 19960223 00654 WP 1996 2 23 USAAD96006 1 19960112 A 2150 39613011 CONTROL VLV DOUG DC9 DC981 3022081 WP LT PACK FAILED A USAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 19 805US 16101 48053 PIT - FLIGHT WAS HOLDING FOR LANDING AT PHL WHEN BOTH AUTO PRESSURE CONTROLLERS FAILED AND CABIN ALTITUDE BEGAN TO CLIMB . CREW DECLARED AN EMERGENCY. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT PACK CONTROL VALV E DUE TO LOW FLOW. (M) 2 L 7 2 4F A6WE 1996022300655 19960223 00655 WP 1996 2 23 USAAD96007 1 19960107 A 3222 STRUT DOUG DC9 DC931 3022065 WP NLG REQ'D SERVICE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 986VJ 47209 ALB - AFTER TAKEOFF, THE NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. EXTENDED GEAR, NORMAL INDIC ATIONS WERE RECEIVED. ATTEMPTED SECOND RETRACTION AND GEAR LEVER WOULD NOT MOVE. FLIGHT RETURNED TO ALB AND LANDED WIT H NO FURTHER INCIDENT. MAINTENANCE INSPECTED THE GEAR AND FOUND THE NITROGEN CHARGE IN THE NOSE GEAR LOW. GEAR WAS SER VICED AND RELEASED FOR SERVICE. (M) 2 L 7 2 4F A6WE 1996022300656 19960223 00656 WP 1996 2 23 USAAD96008 1 19960117 A 2170 COALESCER BAG DOUG DC9 DC931 3022065 WP CABIN CONTAMINATED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 977VJ 48155 BHM - ON MAINTENANCE FERRY FLIGHT, AFTER TAKEOFF, CREW NOTED RANCID BURNING SMELL. CREW DECLARED AND EMERGENCY AND THE FLIGHT RETURNED TO BHM. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THAT A BIRD HAD BEEN INJESTED CAUSIN G THE SMELL. ALL APPROPRIATE INSPECTIONS WERE COMPLETED AND THE WATER SEPARATOR BAG CHANGED. (M) 2 L 7 2 4F A6WE 1996022300657 19960223 00657 WP 1996 2 23 USAAD96009 1 19960118 A 3350 60030431 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 939VJ 48120 PIT - EMERGENCY LIGHT WERE ILLUMINATED WITH THE SWITCH IN THE OFF POSITION. MAINTENANCE REPLACED TWO EMERGENCY LIGHT PO WER SUPPLIES. (M) 2 L 7 2 4F A6WE 1996022300658 19960223 00658 WP 1996 2 23 USAAD96010 1 19960123 A 3234 92743643 RELAY DOUG DC9 DC931 3022065 WP GEAR LEVER FAILED A USAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 19 982VJ 48158 PIT - ON GEAR EXTENSION CREW RECEIVED THREE UNSAFE GEAR INDICATIONS. CREW CYCLED THE GEAR AND RECEIVED THREE SAFE INDIC ATIONS. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE R2-28 LANDING GEAR LEVER RELAY, AND SWUNG THE GEAR. (M) 2 L 7 2 4F A6WE 1996022300659 19960223 00659 WP 1996 2 23 USAAD96012A 1 19960125 A 2421 976J2526 GENERATOR DOUG DC9 DC981 3022081 WP LEFT ENGINE FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 807US 16679 5141 48039 CLT - CREW RECEIVED FAULT LIGHT ON LEFT ELECTRIC BUS. RESET WOULD NOT CURE PROBLEM. APU STARTED, BUT IT WOULD NOT POWE R THE BUS. FLIGHT DIVERTED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT GENERATOR. (M) 2 L 7 2 4F A6WE 1996022300660 19960223 00660 WP 1996 2 23 USAAD96014 1 19960131 A 2560 SLIDE COVER DOUG DC9 DC931 3022065 WP TAILCONE NOT RELEASED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 935VJ 48115 PIT - DURING ANNUAL OPERATIONAL CHECK OF THE TAIL CONE EVACUATION SYSTEM, TAIL CONE WAS DROPPED BUT THE HARD COVER WHICH PROTECTS THE SLIDE WAS NOT RELEASED. THIS PREVENTED THE SLIDE FROM BEING DEPLOYED. MAINTENANCE WAS NOT ABLE TO DETERM INE WHY THE COVER REMOVAL WAS NOT INITATED. THE TAILCONE WAS REINSTALLED AND RIGGED, AND REDEPLOYED. THE SYSTEM PERFOR MED CORRECTLY, RESULTING IN A GOOD SLIDE DEPLOYMENT. PER USAIR STANDARD PRACTICES, TWO MORE OPERATIONAL CHECKS WILL BE PERFORMED ON THIS SYSTEM, AND AN INVESTIGATION INITIATED. (M) 2 L 7 2 4F A6WE 1996022300661 19960223 00661 WP 1996 2 23 USAAD96015 1 19960201 A 3230 RETRACT MECH DOUG DC9 DC981 3022081 WP NLG MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 812US 48092 ORD - AFTER TAKEOFF AND ON GEAR RETRACTION, CREW RECEIVED THREE RED LIGHTS. GEAR WAS CYCLED, CREW RECEIVED GREEN INDICA TIONS FOR THE MAINS BUT A RED FOR THE NOSE GEAR. FLIGHT RETURNED TO ORD AND LANDED WITH NO FURTHER INCIDENT. MAINTENAN ACE ACTION PENDING. (M) 2 L 7 2 4F A6WE 1996022300662 19960223 00662 WP 1996 2 23 USAAD96016 1 19960201 A 3230 RETRACT MECH DOUG DC9 DC981 3022081 WP NLG MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 812US 48092 ORD - AFTER TAKEOFF AND ON GEAR RETRACTION, CREW COULD NOT RETRACT THE NOSE GEAR. THIS IS THE SECOND RETURN TO FIELD OF THIS FLIGHT ON THIS DAY. MAINTENANCE ACTION PENDING. (M) 2 L 7 2 4F A6WE 1996022300663 19960223 00663 EU 1996 2 23 USAAF96003A 1 19960105 A 3260 PROX SENSOR FOKKER F28 F28MK0100 4990807 EU LT MLG OUT OF ADJUST A USAA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 EA 19 886US 11346 FLT NR 1488 - RIC - SHORTLY AFTER GEAR RETRACTION THE FOLLOWING ALERTS, 'LD FAULT', 'STAB TRIM CONFIG' AND 'TCAS'. WHEN GEAR EXTENDED, LOUD RELAY CLICKING FOLLOWED BY ALL MESSAGES CLEARING. MAINTENANCE ADJUSTED THE LEFT MAIN GEAR NR 3 PRO XIMITY SENSOR AND SWUNG THE GEAR. (M) 2 L 7 2 4F RT 1996022300664 19960223 00664 EU 1996 2 23 USAAF96004A 1 19960105 A 3260 HARNESS FOKKER F28 F28MK0100 4990807 EU LT MLG FAULTY A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 886US 11346 CLT - AFTER TAKEOFF, CREW RECEIVED GND/FLT FAULT, LIFT DUMPER FAULT, TCAS FAULT AND PROX SW SYS INOP. FLIGHT RETURNED T O CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR HARNESS AND THE SENSOR. (M) 2 L 7 2 4F RT 1996022300665 19960223 00665 EU 1996 2 23 USAAF96010 1 19960118 A 2133 OUTFLOW VALVE FOKKER F28 F28MK0100 4990807 EU CABIN DEACTIVATED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 850US 11276 PIT - AFTER TAKEOFF, AIRCRAFT WOULD NOT PRESSURIZE IN AUTOMATIC OR MANUAL MODES. FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REACTIVATED THE OUTFLOW VALVE WHICH WAS DEACTIVATED DUE TO PREVIOUS WORK. (M) 2 L 7 2 4F RT 1996022300666 19960223 00666 EU 1996 2 23 USAAF96011 1 19960122 A 3260 UPLOCK BRACKET FOKKER F28 F28MK4000 4990810 EU RT MLG OUT OF ADJUST A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 477AU 11226 GSO - AFTER TAKEOFF, CREW RECEIVED THE RED WARNING LIGHT FOR THE RIGHT MAIN LANDING GEAR. CREW COULD NOT GET THE LIGHT TO EXTINGUISH. FLIGHT RETURNED FILED AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE ADJUSTED THE RIGHT GEAR UPLOCK B RACKET. (M) 2 L 7 2 4F RT A20EU 1996022300667 19960223 00667 EU 1996 2 23 USAAF96012 1 19960123 A 3230 TEST VALVE FOKKER F28 F28MK0100 4990807 EU MLG OUT OF POSITION A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 895US 11380 PIT - AFTER TAKEOFF, CREW RECEIVED LEFT AND RIGHT MAIN LANDING GEAR WARNING ON THE MFDU. THE GEAR WAS CYCLED WITH THE S AME RESULT. FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE LANDING GEAR TEST VALVE IN THE TEST POSITION. THE SWITCH WAS SAFETIED AND THE AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT 1996022300668 19960223 00668 EU 1996 2 23 USAAF96013 1 19960124 A 2750 A83132409 FLEX SHAFT FOKKER F28 F28MK4000 4990810 EU TE FLAPS BROKEN A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 484US 11234 CLT - CREW RECEIVED 'WING FLAP ASYMMETRY' WARNING LIGHT, AFTER TAKEOFF. FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTH ER INCIDENT. MAINTENANCE FOUND THE SQUIRREL CAGE DRIVE COUPLING BROKEN AND REPLACED IT. (M) 2 L 7 2 4F RT A20EU 1996022300669 19960223 00669 EU 1996 2 23 USAAF96014 1 19960124 A 3231 71541 SEQUENCING VLV FOKKER F28 F28MK0100 4990807 EU RT MLG DOR FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 856US 14498 11286 CHS - AFTER TAKEOFF, CREW WOULD NOT GET THE MAIN GEAR TO RETRACT. THE GEAR WAS CYCLED TWICE. FLIGHT RETURNED TO CHS AN D LANDED WITH NO FURTHER INCIDENT. AIRCRAFT FERRIED TO CLT FOR REPAIR. MAINTENANCE REPLACED THE RIGHT GEAR DOOR SEQUEN CING 'A' VALVE. GEAR SWING COMPLETED. (M) 2 L 7 2 4F RT 1996022300670 19960223 00670 EU 1996 2 23 USAAF96016 1 19960126 A 4990 38075412 APU FOKKER F28 F28MK4000 4990810 EU APU COMPT OIL LEAK A USAA A UNSCHED LANDING B K SMOKE/FUMES/ODORS/SPARKS FLUID LOSS CL CLIMB 1 EA 19 483US 20105 11233 CLT - AFTER TAKEOFF, THE CABIN AND COCKPIT BEGAN TO FILL WITH SMOKE. THE CREW DECLARED AN EMERGENCY. THE FLIGHT RETURN ED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. THIS INCIDENT WAS SIMILAR TO A PREVIOUS INCIDENT OCCURING ON 1/25/96. M AINTENANCE REPLACED BOTH PACK WATER SEPARATOR BAGS DUE TO OIL CONTAMINATION FROM THE APU. THE APU WAS REPLACED. (M) 2 L 7 2 4F RT A20EU 1996022300671 19960223 00671 EU 1996 2 23 USAAF96019A 1 19960205 A 8011 38349621 STARTER FOKKER F28 F28MK4000 4990810 EU RIGHT ENGINE FAILED A USAA A E UNSCHED LANDING ENGINE SHUTDOWN J M WARNING INDICATION OVER TEMP CL CLIMB 1 EA 19 494US 17585 11167 CAE - UPON TAKEOFF FROM CAE, CREW RECEIVED AURAL AND VISUAL FIRE WARNINGS ON THE NR 2 ENGINE AND THE START VALVE LIGHT. CREW SECURED THE ENGINE AND THE WARNINGS STOPPED. FLIGHT RETURNED TO CAE AND LANDED WITH NO FURTHER INCIDENT. SET 20 MINUTES. HEAT FROM THE STARTER CAUSED THE FIRE WARNING. MAINTENANCE REPLACED THE STARTER AND THE RIGHT ENGINE OUTBOARD FIRE DETECTION LOOP. (M) 2 L 7 2 4F RT A20EU 1996022300673 19960223 00673 NM 1996 2 23 USAASB96018 1 19960122 A 4900 3804286242 AUX POWER UNIT BOEING 737 737201 1384454 NM APU COMPARTMENT FAILED A USAA F ACTIVATE FIRE EXT. J WARNING INDICATION AP APPROACH 1 EA 19 234US 54190 22274 FLT NR 1184 - BWI - ON FINAL APPROACH APU FIRE WARNING MOMENTARILY WENT OFF. FIRED FIRE BOTTLE. MAINTENANCE REPLACED T HE APU. (M) 2 L 7 2 4F A16WE 1996022300674 19960223 00674 NM 1996 2 23 USAASB96020 1 19960126 A 2121 215201 GASPER FAN BOEING 737 737201 1384454 NM FWD CARGO COMPT FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 224US 22301 21666 CHS - EN ROUTE MCO-IAD - CREW NOTED ELECTRICAL IN SMELL IN CABIN. FLIGHT DIVERTED TO CHS AND LANDED WITH NO FURTHER INC IDENT. MAINTENANCE REPLACED THE GASPER FAN. (M) 2 L 7 2 4F A16WE 1996022300675 19960223 00675 WP 1996 2 23 Y2PA96001 1 19960118 A 2910 791586380320 HYD LINE DOUG DC9 DC915F 3022037 WP RT MLG WW BROKEN A Y2PA K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 GL 23 197US 47154 MCI - LOST ALL HYDRAULIC FLUID FROM RIGHT SYSTEM AND SUBSEQUENT PRESSURE. FURTHER INVESTIGATION SHOWED A HYDRAULIC LINE FAILURE IN THE RIGHT WHEEL WELL. REMOVED AND REPLACED LINE WITH A SERVICEABLE UNIT. (M) 2 L 7 2 4F A6WE 1996022300676 19960223 00676 WP 1996 2 23 Y2PA96002 1 19960119 A 2720 5914387507 ACT BELLOWS DOUG DC9 DC915F 3022037 WP RUDDER CONTROL LEAKING A Y2PA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 23 197US 47154 DFW - UNSCHEDULED LANDING AT DFW FOR RUDDER TRAVEL UNRESTRICTED LIGHT ILLUMINATED AT CRUISE. DRAINED ACCUMULATED FLUID FROM SYSTEM SUMPS, OPS CHECK GOOD AS PER MM 27-20-3. (M) 2 L 7 2 4F A6WE 1996022300677 19960223 00677 WP 1996 2 23 Y2PA96003 1 19960119 A 3234 GEAR HANDLE DOUG DC9 DC915F 3022037 WP LANDING GEAR MALFUNCTIONED A Y2PA O OTHER J WARNING INDICATION AP APPROACH 1 GL 23 197US 47154 DFW - ON FINAL APPROACH INTO DFW, GEAR HANDLE WOULD NOT GO DOWN, AFTER SEVERAL ATTEMPTS THE GEAR HANDLE DID GO DOWN AND THE GEAR EXTENDED NORMALLY. PERFORMED GEAR RETRACTION AND EXTENSION, OPS CHECKS GOOD PER DC-9 MM 32-30-0, NO DEFECTS NO TED. (M) 2 L 7 2 4F A6WE 1996022300678 19960223 00678 1996 2 23 Y2PA96004 4 19960131 A 3417 25874003733 AIR DATA COMP DOUG DC9 DC915F 3022037 WP COMPT MALFUNCTIONED A Y2PA O OTHER O OTHER CR CRUISE 1 GL 23 196US 47155 ORD - IN FLIGHT AT HIGH ALTITUDE AND HIGH SPEEDS HORIZ STABILIZER RUNS FULL FORWARD (NOSE DOWN TRIM). CREW MUST PLACE F ORWARD PRESSURE ON YOKE TO MAINTAIN LEVEL FLIGHT. FOUND PITOT STATIC LEAK IN DRAIN BEHIND CADC COMPUTER TEST FLEW AIRCR AFT. MACH TRIM COMPENSATOR APPEARS TO OPERATE EARLY. ADJUSTED AND TESTED HORIZONTAL STABILIZER TRIM INDICATING AND SHU T OFF CONTROL CABLES FOUND LOW CABLE TENSION ON SHUT OFF CABLES RIGGED PER MM 27-40-0. MACH TRIM STILL ACTUATES EARLY. DEFERRED MACH TRIM, DMI NR 0047. REMOVED AND REPLACED AIR DATA COMPUTER. SYSTEM OPERATIONAL CHECKED GOOD PER DC9MM 22 -10-0 AND 22-10-1. DMI CLEARED. (M) 2 L 7 2 4F A6WE 1996022300705 19960223 00705 SO 1996 2 23 96ZZZX799 2 19960123 A 8530 649317CEA6 CYLINDER CESSNA 210 T210M 2073451 CE CONT O520 TSIO520R 17040 SO ENGINE EXCESS WEAR A CFCA K NONE O OTHER IN INSP/MAINT 1 GL 03 7398M 1044 21062018 511444 FOUND CYLINDER EXCESS WEAR. THE NORMAL LIFE OF THIS CYLINDER IS AT 1,500 HOURS TBO. THIS CYLINDER LASTED 1,043 HOURS. PREMATURE WEAR FAILURE SEEMS TO BE AN UNFORTUNATE TREND FOR CERMICHROME CYLINDERS. SUBMITTER RECOMMENDS NORMAL OPERATI ONS WATCHING ENGINE PARAMETERS AND FREQUENT OIL CHANGE INTERVALS. 1 H 7 1 3O 3 O 3A21 E8CE 1996022300706 19960223 00706 CE 1996 2 23 96ZZZX800 1 19960123 A 3260 12430192 BRACKET CESSNA 210 T210N 2073456 CE NLG SWITCH BENT A CFCA K NONE O OTHER IN INSP/MAINT 1 GL 03 6611C 21063930 DURING CERTAIN LANDING CONDITIONS, THE AIRCRAFT CAN PRODUCE A NOSE WHEEL SHIMMEY THAT CAUSES NLG SWITCH BRACKET TO BEND OUT OF POSITION. SUBMITTER RECOMMENDS A PRE-FLIGHT INSPECTION FOR PROPER ENGAGEMENT OF SWITCH. SUBMITTER RECOMMENDS CE SSNA BUILD A STRONGER OR HEAVIER BRACKET. 1 H 7 1 3O 3A21 1996022700001 19960227 00001 1996 2 27 VTZA96087 4 19960109 A 6113 SPINNER JETAIR JETSTM JETSTM4101 1500501 EU ENGINE ICED UP A VTZA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 EA 27 324UE 41017 FLT NR 6486 - JFK-IAD - DURING CRUISE, MADE UNSCHEDULED LANDING DUE TO PROP VIBRATION. AIRCRAFT RETURNED TO GATE WITH N O FURTHER INCIDENT. MAINTENANCE REMOVED ICE FROM SPINNER AND PERFORMED GROUND RUNS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996030100020 19960301 00020 NM 1996 3 1 AALA960011 1 19960102 A 5730 SKIN BOEING 727 727223 1384074 NM CENTER WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 871AA 21383 TUL - INTERGRANULAR CORROSION BOTTOM CENTER WING SKIN ABOVE LT PRIMARY HEAT EXCHANGER, AND ABOVE RT PRIMARY HEAT EXCHANG ER. CORROSION REMOVED. FLAP PEENED, ALODINED, AND PRIMED PER ESO 11697. TST, 49,700 HOURS. CYCLES, 30,826. (X) 2 L 7 3 4F A3WE 1996030100021 19960301 00021 EU 1996 3 1 AALA960019 1 19960105 A 5310 STRUCTURE AIRBUS 300 A300B4605R 3930308 EU BS 1605-1658 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 70054 461 TUL - FROM FRAMES 23-24 AT STR 55, CORROSION AROUND SEVERAL RIVET BUTTS IN FORWARD MANHOLE WERE FOUND. REMOVED ALL CORR OSION PER SRM 51-74-10 AND MADE REPAIR PER ESO 30595, DATED 1-5-96. TST, 21,454.49 HOURS. CYCLES, 8,568. (X) 2 L 7 2 4F RT A35EU 1996030100022 19960301 00022 EU 1996 3 1 AALA960029 1 19960108 A 2420 224W4710513 CABLES AIRBUS 300 A300B4605R 3930308 EU NR 1 ENGINE CHAFED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 25071 514 TUL - GROUND CABLE AND C-PHASE CABLE OF NR 1 IDG, CHAFING AT HYDRUALIC MODULE LINE, LEFT SIDE OF ENGINE. REPAIRED GROUN D AND C-PHASE CABLES AND REPOSITIONED FOR CLEARANCE. TST, 19,154.41 HOURS. CYCLES, 7,633. (X) 2 L 7 2 4F RT A35EU 1996030100023 19960301 00023 EU 1996 3 1 AALA960052 1 19960112 A 5330 SKIN AIRBUS 300 A300B4605R 3930308 EU FS 432-446 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80057 465 TUL - DENT IN FUSELAGE SKIN AT FORWARD LOWER CORNER OF FORWARD CARGO CUT-OUT. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-10-12. TST, 20,955 HOURS. CYCLES, 8,316. (X) 2 L 7 2 4F RT A35EU 1996030100024 19960301 00024 NM 1996 3 1 AALA960057 1 19960115 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 791 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1761R 48551 TUL - DURING C-CHECK, FOUND CORROSION ON NR 7 SEAT TRACK AT AFT LAVATORY TIE-DOWN AT STA 791 IN MID-CABIN. INSTALLED SE AT TRACK PLUG REPAIR PER SRM 53-70-00, PAGE 8, FIGURE 4. TST, 10,829.41 HOURS. CYCLES, 1,916. (X) 2 L 7 3 4F RT A22WE 1996030100025 19960301 00025 NM 1996 3 1 AALA960058 1 19960111 A 5320 SUPPORT DOUG MD11 MD11 3023602 NM BS 824 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1761R 48551 TUL - FLOORBOARD SUPPORT CORRODED BETWEEN FLOORBOARD 241BF AND FLOORBOARD 241HF. INSTALLED FLOORBOARD SUPPORT PER AARD 51-10-00-1, PAGE 1 AT STA 824. TST, 10,829 HOURS. CYCLES, 1,916. (X) 2 L 7 3 4F RT A22WE 1996030100026 19960301 00026 NM 1996 3 1 AALA960059 1 19960111 A 5320 SUPPORT DOUG MD11 MD11 3023602 NM BS 806-840 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1761R 48551 TUL - LEFT GALLEY SUPPORT-FLOORBOARD SUPPORT EARS CORRODED. INSTALLED NEW TRACK SECTION (GALLEY SUPPORT) PER SRM 53-70- 00, FIGURE 1, PAGES 3 AND 4, FROM STA 806 TO STA 840. TST, 10,829 HOURS, CYCLES, 1,916. (X) 2 L 7 3 4F RT A22WE 1996030100027 19960301 00027 WP 1996 3 1 AALA960065 1 19960115 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP BS 825-840 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 TUL - SEAT TRACK CORROSION OUT OF LIMITS. REPLACED 35 INCHES OF NR 6 SEAT TRACK BY SPLICING IN NEW MATERIAL. TST, 54,1 15.43 HOURS. CYCLES, 18,537. (X) 2 L 7 3 4F A22WE 1996030100028 19960301 00028 EU 1996 3 1 AALA960091 1 19960118 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80057 465 TUL - CORROSION ON FLOOR SUPPORT 'A', RT SIDE AT R-4 DOOR FROM FRAME 73A TO FRAME 75A. INSTALLED FABRICATED PART PER AA RD 51-10-00-3. ALODINED, PRIMED, AND PAINTED. TST, 20,955 HOURS. CYCLES, 8,316. (X) 2 L 7 2 4F RT A35EU 1996030100029 19960301 00029 WP 1996 3 1 AALA960092 1 19960118 A 5315 5588613 FLOORBEAM DOUG DC10 DC1010 3022110 WP BS 1841 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 TUL - CORROSION ON UPPER FLOORBEAM FLANGE TOP AND BOTTOM AT NUTPLATE HOLES AT STA 1841, LONGERONS 43L TO 43R. MANUFACTU RED AND INSTALLED NEW FLOORBEAM PER AARD 51-01-00-05, PAGE 1. TST, 54,115.43 HOURS. CYCLES, 18,537. (X) 2 L 7 3 4F A22WE 1996030100030 19960301 00030 EU 1996 3 1 AALA960094 1 19960119 A 5320 A53970197200 FLOOR SUPPORT AIRBUS 300 A300B4605R 3930308 EU FS 3619 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80057 465 TUL - CORROSION ON T-ANGLE SUPPORT FOR FLOOR/CARGO ROLLER TRACK/TRAY AT FRAME NR 56 AT NR 6 TRAY. INSTALLED NEW T-ANGLE , AND SPLICE SUPPORT DOUBLER PER SRM 53-10-15 AND SRM 51-71-50. TST, 20,955.4 HOURS. CYCLES, 8,316. (X) 2 L 7 2 4F RT A35EU 1996030100031 19960301 00031 WP 1996 3 1 AALA960124 1 19960123 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 865-830 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 TUL - CORROSION HOLES IN TRACK SIDE WALL SUPPORT IN AREA JUST FORWARD OF CARGO DOOR (MKD). REPLACED WITH NEW RAIL SEGME NT PER SRM 51-00-01, PAGE 5. TREATED, PRIMED, AND PAINTED. TST, 54,115 HOURS. CYCLES, 18,537. (X) 2 L 7 3 4F A22WE 1996030100032 19960301 00032 WP 1996 3 1 AALA960131 1 19960124 A 5320 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP BS 825-840 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 TUL - A 15 INCH SECTION OF FLOOR SUPPORT CORRODED. A SECTION APPROXIMATELY 15 INCHES LONG WAS REPLACED PER ESO 7349. T ST, 54,115.43 HOURS. CYCLES, 18,537. (X) 2 L 7 3 4F A22WE 1996030100033 19960301 00033 EU 1996 3 1 AALA960132 1 19960118 A 5315 FLOOR BEAM AIRBUS 300 A300B4605R 3930308 EU BS 63 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80057 465 TUL - CORROSION BEAM LT SIDE OUTBOARD END AT THE ROLLER TRAY, FRAME STA 63. INSTALLED NEW SECTION OF FLOORBEAM PER SRM 53-10-15 AT FRAME 63 AND TREATED, PRIMED, AND PAINTED PER SRM 51-74-10. TST, 20,955 HOURS. CYCLES, 8,316. (X) 2 L 7 2 4F RT A35EU 1996030100034 19960301 00034 EU 1996 3 1 AALA960145 1 19960126 A 7120 A54612062601 ENG MOUNT AIRBUS 300 A300B4605R 3930308 EU LT ENGINE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80057 465 TUL - FORWARD PYLON TRUSS ENGINE MOUNT, RT AFT HOLE HAS PITTING ON INNER WALL. HOLE REAMED BUSHING AND REPAIRED WASHER. INSTALLED PER ESO 30595, DATED 1-23-96. TST, 20,955 HOURS. CYCLES, 8,316. (X) 2 L 7 2 4F RT A35EU 1996030100035 19960301 00035 NM 1996 3 1 AALA960148 1 19960127 A 5320 SUPPORT DOUG MD11 MD11 3023602 NM BS 495 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1750B 48419 TUL - AT STA 495 JUST INBOARD OF SEAT TRACK NR 2, INBOARD EDGE OF LAV-A, FLOOR SUPPORT IS CORRODED. REPLACED SUPPORT PE R SRM 53-00-01. TXT, 18,391 HOURS. CYCLES, 3,272. (X) 2 L 7 3 4F RT A22WE 1996030100036 19960301 00036 NM 1996 3 1 AALA960149 1 19960126 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 824-899 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1750B 48419 TUL - STA 824 TO STA 899, NR 3 SEAT TRACK IN LAV/GALLEY, MOUNT AREAS AND FLOOR SUPPORT EARS HAVE CORROSION. INSTALLED S EAT TRACK SECTION PER SRM 53-70-00, PAGES 3 AND 4, FIGURE 1. TST, 18,391.33 HOURS. CYCLES, 3,272. (X) 2 L 7 3 4F RT A22WE 1996030100037 19960301 00037 NM 1996 3 1 AALA960150 1 19960126 A 5320 SUPPORT DOUG MD11 MD11 3023602 NM BS 824 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1750B 48419 TUL - STA 824 BETWEEN SEAT TRACKS 3 AND 4, FLOOR SUPPORT HAS CORROSION. INSTALLED FLOOR SUPPORT PER AARD 51-10-00-1, PA GE 1. TST, 18,391.33 HOURS. CYCLES, 3,272. (X) 2 L 7 3 4F RT A22WE 1996030100038 19960301 00038 NM 1996 3 1 AALA960153 1 19960129 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 824-899 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1750B 48419 TUL - STA 824-STA 899 AT SEAT TRACK NR 6 IN LAV/GALLEY, MOUNT AREAS HAVE CORROSION. INSTALLED NEW SECTION OF TRACK PER SRM 53-70-00, PAGES 3-4, FIGURE 1. TST, 18,391.33 HOURS, CYCLES, 3,272. (X) 2 L 7 3 4F RT A22WE 1996030100039 19960301 00039 NM 1996 3 1 AALA960154 1 19960129 A 5320 SUPPORT DOUG MD11 MD11 3023602 NM BS 457 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1750B 48419 TUL - STA 457 BETWEEN SEAT TRACK NR 5 AND SEAT TRACK NR 6, FLOOR SUPPORT HAS CORROSION. REPLACED FLOOR SUPPORT PER SRM 53-00-01, PAGE 1. TST, 18,391.33 HOURS. CYCLES, 3,272. (X) 2 L 7 3 4F RT A22WE 1996030100040 19960301 00040 NM 1996 3 1 AALA960157 1 19960129 A 5320 INTERCOSTAL DOUG MD11 MD11 3023602 NM BS 320 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1750B 48419 TUL - STA 320, G2 GALLEY, SUPPORT INTERCOSTAL HAS CORROSION. REMOVED AND REPLACED INTERCOSTAL SUPPORT PER SRM 53-00-1, PAGE 1. TST, 18,391.33 HOURS. CYCLES, 3,272. (X) 2 L 7 3 4F RT A22WE 1996030100041 19960301 00041 NM 1996 3 1 AALA960158 1 19960129 A 5320 SUPPORT DOUG MD11 MD11 3023602 NM BS 366-392 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1750B 48419 TUL - STA 366 TO STA 392, G-2 INBOARD GALLEY SUPPORT HAS CORROSION. REMOVED AND REPLACED G2 INBOARD GALLEY SUPPORT PER SRM 53-00-01. TST, 18,391.33 HOURS. CYCLES, 3,272. (X) 2 L 7 3 4F RT A22WE 1996030100042 19960301 00042 NM 1996 3 1 AALA960165 1 19960127 A 5315 146N5180 FLOOR BEAM BOEING 757 757223 1384957 NM FS 1640 MISDRILLED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 643AA 24601 AFW - FLOOR BEAM AT STA 1640, RBL 24, WAS DRILLED IN RADIUS OF THE LOWER FLANGE, AFT SIDE PER MRB 757-714 TST, 15,723.2 2 HOURS. CYCLES, 5,740. (X) 2 L 7 2 4F RT A2NM 1996030100043 19960301 00043 NM 1996 3 1 AALA960166 1 19960127 A 5210 146N62016 DOOR PAN BOEING 757 757223 1384957 NM R4 DOOR GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 643AA 24601 AFW - R-4 DOOR PAN HAS A GOUGE BEYOND SRM LIMITS. PER MRB 757-709. TST, 15,723.22 HOURS. CYCLES, 5,740. (X) 2 L 7 2 4F RT A2NM 1996030100044 19960301 00044 NM 1996 3 1 AALA960167 1 19960127 A 5310 146N8522 STRUCTURE BOEING 757 757223 1384957 NM BS 1434 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 643AA 24601 AFW - AFT CARGO LOWER SILL SURROUND STRUCTURE HAS CORROSION REMOVED ON THE LOWER SURFACE OF THE INNER CHORD. PER MRB 75 7-706. TST, 15,723.22 HOURS. CYCLES, 5,740. (X) 2 L 7 2 4F RT A2NM 1996030100045 19960301 00045 NM 1996 3 1 AALA960168 1 19960127 A 5315 141N5113 FLOOR BEAM BOEING 757 757223 1384957 NM BS 377 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 643AA 24601 AFW - FLOOR BEAM AT STA 377 HAS CORROSION REMOVED ON UPPER SURFACE BEYOND SRM LIMITS. PER MRB 757-703. TOTAL CYCLES, 1 5,723.22 HOURS. CYCLES, 5,740. (X) 2 L 7 2 4F RT A2NM 1996030100046 19960301 00046 NM 1996 3 1 AALA960169 1 19960127 A 5315 141N5112 FLOOR BEAM BOEING 757 757223 1384957 NM BS 365 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 643AA 24601 AFW - FLOOR BEAM AT STA 365, RBL 25, HAS CORROSION BLENDED BEYOND SRM LIMITS. PER MRB 757-702. TST, 15,723.22 HOURS. C YCLES, 5740. (X) 2 L 7 2 4F RT A2NM 1996030100047 19960301 00047 NM 1996 3 1 AALA960170 1 19960127 A 5315 141N2800 FLOOR BEAM BOEING 757 757223 1384957 NM FS 324 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 643AA 24601 AFW - FLOOR BEAM AT STA 324 HAS CORROSION ON UPPER SURFACE REMOVED BEYOND SRM LIMITS. PER MRB 757-700. TST, 15,723.22 HOURS. CYCLES, 5,740. (X) 2 L 7 2 4F RT A2NM 1996030100048 19960301 00048 NM 1996 3 1 AALA960171 1 19960127 A 5321 146N5300 DECK PLATE BOEING 757 757223 1384957 NM BS 1720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 643AA 24601 AFW - DECK PLATE HAS CORROSION REMOVED ON UPPER SURFACE AT SEVERAL LOCATIONS. CORROSION REMOVED IS BEYOND SRM LIMITS. P ER MRB 757-699. TST, 15,723.22 HOURS, CYCLES, 5,740. (X) 2 L 7 2 4F RT A2NM 1996030100050 19960301 00050 NM 1996 3 1 9604242286 1 19960222 A 2121 FAN BOEING 727 727251 138408H NM CABIN OVERHEATED A NWAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 01 286US 21325 DURING TAXI OUT, A VERY STRONG ODOR WAS OBSERVED WITH SMOKE AT ROW 15A. GASPER FAN CIRCUIT BREAKER POPPED. AIRCRAFT RE TURNED TO BLOCKS WITHOUT INCIDENT. VERIFIED GASPER FAN OVERHEATED, DISCONNECTED CANNON PLUG. PLACED ON MEL 21-24, PLAC ARD NR 411586. 2 L 7 3 4F A3WE 1996030100051 19960301 00051 NE 1996 3 1 9604256615 2 19960219 A 7321 FUEL CONTROL BOEING 747 747251B 1384892 NM PWA JT9 JT9D7Q 52054 NE NR 2 ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 616US 20360 02275 DURING TAKEOFF, THE NR 2 ENGINE FAILED TO REACH TAKEOFF POWER. CREW ABORTED TAKEOFF AT 60 KNOTS AND RETURNED TO THE GAT E. FOUND HYDRAULIC STAGE PRESSURE TO BE ZERO. REPLACED FUEL CONTROL AND FUEL PUMP. THE NR 2 ENGINE HIGH POWER RUNUP C HECK WAS NORMAL AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4 F A20WE E3NE 1996030100052 19960301 00052 WP 1996 3 1 9604269948 1 19960216 A 5350 RELEASE MECH DOUG DC9 DC931 3022065 WP TAIL CONE WORN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8929E 45866 DURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO DROP THE TAIL CONE USING THE INTERIOR HANDLE. ALSO, FOUND WORN GUIDE PINS, GUIDE PIN BEARING PLATES AND 2 MISSING PHENOLIC BLOCKS. REPLACED PINS, PLATES, BLOCKS AND ACCOMPLISHE D EO 5350-01049, CHECKED OK. 2 L 7 2 4F A6WE 1996030100053 19960301 00053 WP 1996 3 1 9604279925 1 19960221 A 3350 FUSE DOUG DC9 DC932 3022066 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 925US 47472 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD SERVICE DOOR AND FORWARD CABIN FLOOR PROXIMITY EMERGENCY LIGHTS INOPER ATIVE. REPLACED BATTERIES WITH NO HELP. REPLACED BLOWN FUSE AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996030100054 19960301 00054 WP 1996 3 1 9604289953 1 19960222 A 3350 016624001 BATTERIES DOUG DC9 DC931 3022065 WP COCKPIT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 918RW 47158 DURING PREFLIGHT CHECK, FOUND COCKPIT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES AND OPERATIONAL CHECK N ORMAL. 2 L 7 2 4F A6WE 1996030100055 19960301 00055 WP 1996 3 1 9604299301 1 19960222 A 3231 ROLLER DOUG DC9 DC982 3022082 WP LT MLG DOOR OUT OF ADJUST A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 301RC 48054 LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INC IDENT. ADJUSTED GEAR DOOR UPLATCH ROLLER AND OPERATIONAL CHECK NORMAL ON GEAR CYCLE. 2 L 7 2 4F A6WE 1996030100056 19960301 00056 NM 1996 3 1 9604302276 1 19960221 A 3350 BATTERY PACK BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 276US 21155 DURING PREFLIGHT, FOUND EMERGENCY EXIT LIGHT ABOVE GALLEY DOOR 1R INOPERATIVE. REPLACED BATTERIES AND CHECKED OK. 2 L 7 3 4F A3WE 1996030100057 19960301 00057 WP 1996 3 1 9604319152 1 19960220 A 3260 INDICATION DOUG DC9 DC914 3022034 WP LT MLG MALFUNCTIONED A NWAA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 01 8911E 45825 ON APPROACH INTO MSP, THE LEFT MAIN GEAR SHOWED NO GREEN LIGHT UPON EXTENSION. RECYCLED GEAR AND INDICATIONS WERE NORMA L. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING REVEALED NO DISCREPANCIES. 2 L 7 2 4F A6WE 1996030100058 19960301 00058 WP 1996 3 1 9604329882 1 19960221 A 3397 WIRE DOUG DC9 DC951 3022051 WP TAIL CONE CHAFED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 670MC 47659 DURING LINE CHECK, FOUND AFT TAIL CONE SLIDE EMERGENCY LIGHTS DIM. FOUND WIRE IN AFT TAIL CONE SLIDE EMERGENCY LIGHTS I NOPERATIVE, AFT EMERGENCY SLIDE LIGHTS DIM AND VENTRAL STAIR EMERGENCY LIGHTS DIM. FOUND WIRE IN AFT TAIL CONE EMERGENC Y SLIDE LIGHT CHAFED AGAINST THE REFLECTOR. REPLACED WIRE AND BATTERY PACK, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A6WE 1996030100059 19960301 00059 EU 1996 3 1 9604333221 1 19960221 A 3260 848401 SENSOR AIRBUS 320 A320211 3930320 EU NLG MALFUNCTIONED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 321NW 262 DURING CLIMBOUT, THE LANDING GEAR DID NOT RETRACT, THREE GREEN AND THREE RED GEAR INDICAITON LIGHTS WERE ILLUMINATED. C YCLED THE LANDING GEAR HANDLE AND ALL INDICATIONS NORMAL. AIRCRAFT CONTINUED TO ORIGINAL DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING WAS ABLE TO DUPLICATE THE DISCREPANCY. THE RIGHT NOSE LANDING GEAR DOOR DID NOT INDICATE FULLY OPEN. REPLACED THE RIGHT NOSE LANDING GEAR DOOR PROXIMITY SENSOR (39GA), OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996030100060 19960301 00060 NM 1996 3 1 96FDEA00289 1 19960222 A 5320 SHEAR TIE BOEING 727 72722 1384002 NM BS 970 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION (C53-111-01, 3) ON SHEAR TIE AT BS 970 RBL 10 WL 138.5. REMOVED AND REPLACED SHEAR TIE AT BS 970 RBL 10 WL 13 8.5. 2 L 7 3 4F A3WE 1996030100061 19960301 00061 NM 1996 3 1 96FDEA00290 1 19960222 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM BS 540 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION AT BS 540 FLOORBEAM LOWER CHORD FROM LBL 16 TO RBL 28 WL 200. REPAIRED LOWER CHORD OF FLOORBEAM AT BS 540 WL 200 FROM LBL 16 TO RBL 28 IAW FEDEX SRM 53-10-08. 2 L 7 3 4F A3WE 1996030100062 19960301 00062 NM 1996 3 1 96FDEA00291 1 19960222 A 5320 WEB BOEING 727 72722 1384002 NM BS 560-580 MECH DAMAGE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 MECHANICAL DAMAGE AND MISDRILLED HOLES IN WEB AT BS 560 TO 580 LBL 41 WL 200. REMOVED DAMAGE, FABRICATED REPAIR PARTS A ND INSTALLED PER SRM 51-40-2. 2 L 7 3 4F A3WE 1996030100063 19960301 00063 NM 1996 3 1 96FDEA00292 1 19960222 A 5313 STRINGER BOEING 727 72722 1384002 NM BS 640 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 WHILE WORKING NR0429, FOUND GOUGE ON STR NR 3 BS 640 RT. REPAIRED STR NR 3 BS 640 IAW FEDEX SRM 53-10-3. 2 L 7 3 4F A3WE 1996030100064 19960301 00064 NM 1996 3 1 96FDEA00293 1 19960222 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM BS 970 DOUBLE DRILLED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 194FE 19143 WHILE WORKING NR0754, FOUND DOUBLE HOLE IN BS 970 FLOORBEAM AT BL 0 WL 208. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-10-8. 2 L 7 3 4F A3WE 1996030100065 19960301 00065 NM 1996 3 1 96FDEA00294 1 19960222 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM BS 990 DOUBLE DRILLED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 WHILE WORKING NR0754, FOUND DOUBLE HOLE IN BS 990 FLOORBEAM AT BL 0 WL 208. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-10-8. 2 L 7 3 4F A3WE 1996030100066 19960301 00066 NM 1996 3 1 96FDEA00295 1 19960222 A 5320 65184152 NOSE CHORD BOEING 727 72722 1384002 NM NLG WW CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION (C53-111-01) ON UPPER NOSE CHORD, BS 312 TO 324 RBL 15 WL 169. REMOVED AND REPLACED UPPER NOSE CHORD STA 294 .5 TO 355 RBL 15 WL 169 IAW BAC DRAWING NR 65-18415. WEB TO BE INSTALLED ON NR0834 AT STA 294.5 TO 355 RBL 15 TO 25 WL 169. 2 L 7 3 4F A3WE 1996030100067 19960301 00067 NM 1996 3 1 96FDEA00296 1 19960222 A 5330 SKIN BOEING 727 72722 1384002 NM BS 365-390 CREASE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 LARGE CREASE IN EXTERIOR SKIN BS 365 TO 390 STR 23R. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-3 0-3. 2 L 7 3 4F A3WE 1996030100068 19960301 00068 NM 1996 3 1 96FDEA00297 1 19960222 A 5315 45838 FLOORBEAM BOEING 727 72722 1384002 NM BS 620 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION (C53-111-01, 2) ON LOWER FLANGE OF FLOORBEAM IN NUTPLATE HOLES AT BS 620 LBL 20 TO RBL 26 WL 200. REPAIRED FL OORBEAM BS 620 LBL 20 TO RBL 26 WL 200 IAW FEDEX SRM 53-10-8. 2 L 7 3 4F A3WE 1996030100069 19960301 00069 NM 1996 3 1 96FDEA00298 1 19960222 A 5313 BAC1498141 STRINGER BOEING 727 72722 1384002 NM BS 680-700 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 MECH DAMAGE ON STR NR 3 BS 680 TO 700 LT. REMOVED MECH DAMAGE ON STR NR 3 BS 680 TO 700 LT, FOUND TO BE OUT OF LIMITS P ER FEDEX SRM 53-10-1. REMOVED DAMAGED SECTION OF STR BS 670 TO 710, FABRICATED REPAIR PARTS AND INSTALLED PER FEDEX SRM 53-10-3 FIG 3. 2 L 7 3 4F A3WE 1996030100070 19960301 00070 NM 1996 3 1 96FDEA00299 1 19960222 A 5320 65189552 FITTING BOEING 727 72722 1384002 NM BS 360 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION ON STR 26R FITTING BS 360. REMOVED T-FITTING BS 360 STR 26R, INSTALLED NEW T-FITTING AT BS 360 STR 26R. 2 L 7 3 4F A3WE 1996030100071 19960301 00071 NM 1996 3 1 96FDEA00300 1 19960222 A 5315 BAC14902285 FLOORBEAM BOEING 727 72722 1384002 NM BS 560 DOUBLE DRILLED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 WHILE WORKING CARD NR0683, FOUND BS 560 FLOORBEAM BL 0 WL 208 TO HAVE 3 DOUBLE HOLES. REPAIRED FLOORBEAM AT BS 560 BL 0 WL 208 IAW FEDEX SRM 53-10-8, (P/N BAC 1505-100617). 2 L 7 3 4F A3WE 1996030100072 19960301 00072 NM 1996 3 1 96FDEA00301 1 19960222 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM BS 1010 DOUBLE DRILLED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 WHILE WORKING NRO754, FOUND DOUBLE HOLE IN BS 1010 FLOORBEAM AT BL 0 WL 208. REPAIRED FLOORBEAM BS 1010 BL 0 WL 208 IAW FEDEX SRM 53-10-8. 2 L 7 3 4F A3WE 1996030100073 19960301 00073 NM 1996 3 1 96FDEA00302 1 19960222 A 5751 652172719 HINGE FITTING BOEING 727 72722 1384002 NM LT AILERON ELONGATED HOLES A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 O/B LT WING AILERON HINGE FITTING MOST I/B ON AILERON SIDE BOLT HOLES ARE ELONGATED. REMOVED AND REPLACED O/B LT WING A ILERON I/B HINGE FITTING. REINSTALLED AND TORQUED ATTACH BOLTS IAW FEDEX MM 27-10-31. 2 L 7 3 4F A3WE 1996030100074 19960301 00074 NM 1996 3 1 96FDEA00303 1 19960222 A 5320 65175551622 SUPPORT BOEING 727 72722 1384002 NM BS 1362 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 WHILE WORKING NR0122, FOUND RIB SUPPORT WEB TO BE CRACKED AT THREE FASTENER LOCATIONS BS 1362 WL 281 RBL 11. REMOVED AN D REPLACED WEB BS 1362 WL 181 RBL 11. 2 L 7 3 4F A3WE 1996030100075 19960301 00075 NM 1996 3 1 96FDEA00304 1 19960222 A 2910 BACH8R04NN0157 HYDRAULIC LINE BOEING 727 727233 138408A NM LT ELEVATOR LEAKING A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 281FE 22348 DURING FLAP RETRACTION FOLLOWING TAKEOFF, A-SYS HYD QTY AND PRESS WENT TO 0. ALL CHECKLIST PROCEDURES WERE FOLLOWED, GE AR WAS MANUALLY CRANKED DOWN, 1 AND 2 FLUID SHUTOFFS WERE CLOSED AND ALTERNATE FLAP WAS TURNED ON. GROUND PROXIMITY SYS TEM INHIBITED, FLUID SHUTOFF SWITCH WAS OFF 25 MINUTES. ENG RUNNING +0 PRESS. REPLACED LT ELEVATOR ACTUATOR PRESS LINE , LEAK CHECK GOOD. REPLACED NR 1 AND NR 2 ENG HYD PUMPS PER MM 29-11-96, LEAK CHECK GOOD. SERVICED HYD RESERVOIR, COMP LIED WITH MM 29-11 PER INSTALLATION AND CHECK. 2 L 7 3 4F RT A3WE 1996030100076 19960301 00076 NM 1996 3 1 96FDEA00305 1 19960221 A 2613 OVERHEAT DET BOEING 727 727223 1384074 NM NR 2 ENGINE SHORTED A FDEA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CL CLIMB 1 SO 25 278FE 22345 LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED DURING CLIMBOUT WITH ENG ANTI-ICE ON. FOLLOWED PUBLISHED ABNORMAL PROCEDURES AND DETERMINED ENG NR 2 INLET ANTI-ICE SYS TO BE THE SOURCE OF THE OVERHEAT TEMP ON ENG NR 2 INLET. LEFT ENG NR 3 ANTI- ICE OFF FOR REMAINDER OF FLIGHT. FOUND DETECTOR M322 SHORTED. REPLACED SAME AND CHECKED GOOD. FOUND CONNECTOR BAD FWD END OF OVERHEAT DETECTOR AND REPLACED CONNECTOR. 2 L 7 3 4F A3WE 1996030100077 19960301 00077 NM 1996 3 1 96FDEA00306 1 19960223 A 3610 DUCT BOEING 727 727233 138408A NM PRECOOLER LOOSE A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 254FE 20936 THREE MINUTES AFTER TAKEOFF WITH CLIMB POWER SELECTED 90 PERCENT, ENG NR 1 STRUT OVERHEAT LIGHT ILLUMINATED. ACCOMP RED TAB PROCEDURES AND LIGHT EXTINGUISHED, SYS TESTS GOOD AND NO FURTHER PROBLEMS. INSP STUB WING TEMP SENSORS VALVES AND DUCTS. FOUND LOOSE CLAMP ON DUCT FROM PRECOOLER TO OVER BOARD DUCT. SECURED SAME, RAN ENG AT HIGH RPM, NO LEAKAGE. 2 L 7 3 4F RT A3WE 1996030100078 19960301 00078 NM 1996 3 1 96UAL900132 1 19960220 A 2560 4A31211 ASPIRATOR BF GOODRICH 7A14391 BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 5 DOOR SLIDE SHEARED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 4728U G1278 19925 DURING TEST INFLATION OF DOOR 5 RT SLIDE, AT OVERHAUL ONE ASPIRATOR SHEARED IN TWO. SHEAR POINT IS LOCATED BELOW THE RE TAINING BANDS WHICH HOLD THE ASPIRATOR IN PLACE. REPLACED ASPIRATOR, RETURNED DAMAGED ASPIRATOR TO OEM FOR ANALYSIS. 2 L 7 4 4F 4 F A20WE E20EA 1996030100079 19960301 00079 NM 1996 3 1 96UAL900133 1 19960220 A 2410 CSD BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 7276U 21423 AFTER NR 1 ENGINE WAS STARTED THE LEFT PACK SMOKED UP CABIN. REPLACED CONSTANT SPEED DRIVE DUE TO INOPERATIVE GENERATOR . NO SUBSEQUENT COMMENTS ON SMOKE IN CABIN. 2 L 7 3 4F 4 F A3WE E2EA 1996030100080 19960301 00080 NM 1996 3 1 96UAL900134 1 19960220 A 3350 LIGHT BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 4729U 19926 OVERWING EMERGENCY LIGHT ON LEFT SIDE INOP. REPLACED LIGHT. 2 L 7 4 4F 4 F A20WE E20EA 1996030100081 19960301 00081 EU 1996 3 1 96UAL900135 2 19960220 A 7230 335014511 DISK BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU ENG COMPRESSOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 722353 DURING SHOP VISIT, FLUORESCENT PENETRATE INSPECTION OF THE FAN DISK, TWO DOVETAIL CRACKS WERE FOUND. ONE CRACK WAS FOUN D AT THE BOTTOM OF THE DOVETAIL SLOT NR 6 RIGHT PRESSURE FACE. THE SECOND CRACK WAS FOUND AT THE BOTTOM OF THE DOVETAIL SLOT NR 22 LEFT PRESSURE FACE. 2 L 7 2 4F 4 F RT A16WE E21EU 1996030100082 19960301 00082 1996 3 1 96UAL900136 4 19960220 A 2564 D23940117 VALVE BODY AIR CRUISES C17638109 BOEING 757 757222 1384956 NM CYLINDER ASSY LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 588UA 371181 26717 FIRST TIME OVERHAUL ON THE 46 MAN RAFT REVEALED THAT THE VALVE BODY WAS LOOSE FROM THE PRESSURIZATION CYLINDER. CYLINDE R PRESSURE WAS ACCEPTABLE, RETORQUED VALVE BODY TO CYLINDER PRIOR TO RECHARGE. 2 L 7 2 4F RT A2NM 1996030100083 19960301 00083 NM 1996 3 1 96UAL900137 1 19960220 A 2120 AIR DISTR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 WP 29 508UA 24744 RUBBER ODOR IN COCKPIT AND CABIN AFTER ANTI-ICE ACTIVATED. APPROXIMATELY FIVE MINUTES AFTER ANTI-ICE ACTIVATION ODOR BE GINS. 2 L 7 2 4F 4 F RT A2NM E17NE 1996030100084 19960301 00084 NM 1996 3 1 96UAL900138 1 19960221 A 2170 21B37C011 COALESCER BAG BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE CABIN CONTAMINATED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 9001U 19039 CREW REPORTS, HEAVY SMOKE IN COCKPIT AND CABIN. TURNED RIGHT PACK OFF AND THEN LEFT PACK, NO HELP. CREW TURNED OFF SOM E ELECTRICAL FUNCTIONS AND SMOKE WAS SOMEWHAT BETTER ON APPROACH. SOURCE OF SMOKE MAYBE OIL OR ELECTRICAL. OIL WAS FOU ND IN THE LEFT PACK SYSTEM. THE COALESCER BAG WAS REPLACED AND A PACK BURNOUT WAS ACCOMPLISHED. 2 L 7 2 4F 4 F A16WE E2EA 1996030100085 19960301 00085 NE 1996 3 1 96UAL900139 2 19960221 A 7530 ACTUATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE FAILED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 29 549UA 25397 726582 LEFT ENGINE FAILED TO DEVELOP TAKEOFF POWER DURING TAKEOFF. *S/D* REPLACED LEFT BLEED VALVE ACTUATOR, OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996030100086 19960301 00086 NM 1996 3 1 96UAL900140 1 19960221 A 3350 STRIP BOEING 737 737322 1384676 NM CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 373UA 24638 AFT CABIN EMERGENCY ESCAPE PATH LIGHTING INOP. REPLACED POWER STRIP, CHECKS OK. 2 L 7 2 4F RT A16WE 1996030100087 19960301 00087 NM 1996 3 1 96UAL900142 1 19960222 A 3610 773288 PRSOV HAMILTON STA PCN6439026 BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT ENGINE DIRTY FILTER A UALA D RETURN TO BLOCK J WARNING INDICATION NR NOT REPORTED 1 WP 29 655UA 92 25393 AIRCRAFT RETURNED TO BLOCKS DUE TO RIGHT ENGINE PRSOV FAILURE. REPLACED PRSOV, THE FILTER ASSEMBLY WAS CLOGGED. 2 L 7 2 4F 4 F RT A1NM E24NE 1996030100088 19960301 00088 NM 1996 3 1 96UAL900143 1 19960222 A 3350 BATTERY PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7467U 21921 ALL EMERGENCY EXIT LIGHTS IN THE AIRCRAFT ARE OUT, INSIDE AND OUT, FERRIED TO DEN. DEN REPLACED BATTERIES AND AFT STAIR LIGHT UNIT. 2 L 7 3 4F 4 F A3WE E2EA 1996030100089 19960301 00089 WP 1996 3 1 96UAL900144 1 19960222 A 5400 AUB70763 SPAR WEB DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 3 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 1858U 46987 DURING ENGINE CHANGE THE NR 3 PYLON CENTER SPAR WEB WAS FOUND TO BE CRACKED. THE CRACK IS AT STATION 416 AND PROPAGATES 2 INCHES FROM LIGHTENING HOLE TO EDGE OF WEB. A PERMANENT REPAIR WAS MADE PER DC-10-30 STRUCTURAL REPAIR MANUAL. 2 L 7 3 4F 4 F A22WE E23EA 1996030100090 19960301 00090 SO 1996 3 1 COMA9610087 1 19960220 A 2150 12042863003 SEAL EMB 120 EMB120RT SO LEFT WORN A COMA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 SO 01 137H 120137 LEFT DUCT LEAK WARNING ILLUMINATED DURING FLIGHT. REPLACED WORN HEAT EXCHANGER SEAL. 2 L 7 2 4T RT A31SO 1996030100091 19960301 00091 SO 1996 3 1 COMA9610088 1 19960221 A 3260 922FS2A6NZ735 PROX SENSOR EMB 120 EMB120RT SO RT MLG DEFECTIVE A COMA O OTHER N FALSE WARNING LD LANDING 1 SO 01 264CA 120256 NOSE WHEEL STEERING FAILED DURING LANDING. REPLACED DEFECTIVE WEIGHT ON WHEELS PROXIMITY SENSOR IN RT MLG. 2 L 7 2 4T RT A31SO 1996030100092 19960301 00092 SO 1996 3 1 COMA9610089 1 19960221 A 2752 3203001005 ACTUATOR EMB 120 EMB120RT SO LT TE FLAP DEFECTIVE A COMA K NONE J WARNING INDICATION UK UNKNOWN 1 SO 01 162CA 3319 120150 LEFT INBD FLAP WILL NOT RETRACT. REPLACED THE LT INBD FLAP ACTUATOR. 2 L 7 2 4T RT A31SO 1996030100093 19960301 00093 1996 3 1 COMA9630041 4 19960220 A 3425 6226190113 COMPUTER SAAB SF340 SF340A 7850100 EU AVIONICS FAILED A COMA K NONE J WARNING INDICATION UK UNKNOWN 1 SO 01 320CA 18538 2438 340A064 COPILOTS ATTITUDE AND HEADING RED FLAGGED. CIRCUIT BREAKER TRIPPED. REPLACED THE AHC-85 COMPUTER. 2 L 7 2 4T RT A52EU 1996030100094 19960301 00094 EU 1996 3 1 COMA9630042 1 19960219 A 3350 6104781 BATTERY SAAB SF340 SF340A 7850100 EU CABIN DISCHARGED A COMA K NONE L NO TEST UK UNKNOWN 1 SO 01 380CA 340A012 EMERGENCY LIGHTS ARE INOP. RECHARGED EMERGENCY LIGHTS BATTERY PACKS. 2 L 7 2 4T RT A52EU 1996030100095 19960301 00095 NM 1996 3 1 DL72E960412 1 19960221 A 3350 BATTERIES S106 BOEING 727 727247 138408F NM AIRSTAIRS DISCHARGED A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 2826W NONE 21331 EMERGENCY EXIT LIGHT OVER THE BOTTOM STEP OF THE AIR STAIRS IS INOP. REPLACED BATTERIES, OPS NORMAL. 2 L 7 3 4F A3WE 1996030100097 19960301 00097 NM 1996 3 1 DL72L960390 1 19960220 A 5751 652176634 SKIN BOEING 727 727232 1384082 NM LT AILERON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 511DA 21313 DURING INSPECTION, LEFT WING O/B AILERON WAS FOUND WITH LOWER OUTBOARD SKIN CRACKED. REPAIRED PER MM 57-51-0 PG 801. 2 L 7 3 4F A3WE 1996030100098 19960301 00098 NM 1996 3 1 DL72L960400 1 19960221 A 5320 WEB BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 507DA 21309 FOUND DURING D-1 LETTER CHECK, .125 INCH CRACK IN TORQUE BOX WEB AT AFT LT LIGHTENING HOLE. REPAIRED PER MM 53-11-0 PG 828. 2 L 7 3 4F A3WE 1996030100099 19960301 00099 NM 1996 3 1 DL72L960401 1 19960221 A 5720 BRACKET BOEING 727 727232 1384082 NM NR 5 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 507DA 21309 FOUND DURING D-1 LETTER CHECK, NR 5 L/E FLAP ACTUATOR MOUNT BRACKET CRACKED AT LOWER I/B CORNER. REPAIRED PER MM 57 -20-21. 2 L 7 3 4F A3WE 1996030100100 19960301 00100 NM 1996 3 1 DL72L960404 1 19960220 A 5320 WEB BOEING 727 727232 1384082 NM LEFT TQ BOX CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 507DA 21309 FOUND ON D-1 LETTER CHECK, .125 INCH CRACK IN TORQUE BOX WEB AT AFT LT LIGHTENING HOLE. REPAIRED PER M/M 53-11-0 PG 828 . 2 L 7 3 4F A3WE 1996030100101 19960301 00101 NM 1996 3 1 DL72L960405 1 19960220 A 5700 BRACKET BOEING 727 727232 1384082 NM NR 5 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 507DA 21309 FOUND ON D-1 LETTER CHECK, NR 5 L/E FLAP ACTUATOR MOUNT BRACKET CRACKED AT LOWER I/B CORNER. REPAIRED PER M/M 57-0-21 PG 811. 2 L 7 3 4F A3WE 1996030100102 19960301 00102 NM 1996 3 1 DL72L960414 1 19960221 A 5330 65545952 SKIN BOEING 727 727232 1384082 NM BS 870 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 503DA 21305 DURING INSPECTION, CORROSION WAS FOUND ON THE FUSELAGE SKIN AT STA 870 AND STR 9R. THE CUT OUT MEASURES 5 INCHES BY 3 I NCHES, IN ACCORDANCE WITH B727 SRM 53-30-3 FIG 3A, A DOUBLER AND TRIPLER WERE INSTALLED. 2 L 7 3 4F A3WE 1996030100103 19960301 00103 NM 1996 3 1 DL72S960385 1 19960220 A 5754 651622199 SKIN BOEING 727 727232 1384082 NM NR 4 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 419DA 21272 DURING INSPECTION, NR 4 L/E SLAT OUTER SKIN WAS FOUND CRACKED AT FENCE ATTACH MOUNT HOLE. REPAIRED SKIN PER MM 57-54-0 FIG 813. 2 L 7 3 4F A3WE 1996030100104 19960301 00104 NM 1996 3 1 DL72S960389 1 19960220 A 5754 651622199 RIB BOEING 727 727232 1384082 NM NR 4 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 419DA 21272 DURING INSPECTION, NR 4 L/E SLAT WAS FOUND WITH FOUR CRACKED/DAMAGED LEADING EDGE SUPPORT RIBS. REPAIRED PER MM 57-54-0 . 2 L 7 3 4F A3WE 1996030100105 19960301 00105 NM 1996 3 1 DL72S960396 1 19960221 A 5532 SKIN BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 493DA 21062 A 1 INCH CRACK AT CENTER ENGINE INLET HOUSING OUTER SKIN BELOW PANEL 9523. REPAIRED PER MM 54-30-0. 2 L 7 3 4F A3WE 1996030100106 19960301 00106 NM 1996 3 1 DL72S960397 1 19960221 A 5720 BRACKET BOEING 727 727232 1384082 NM RT WING LE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 493DA 21062 A .4375 INCH CRACK AT NR 5 L/E FLAP ACTUATOR MOUNT BRACKET I/B UPPER CORNER. REPAIRED PER MM 57-20-21 PAR 12. 2 L 7 3 4F A3WE 1996030100107 19960301 00107 NM 1996 3 1 DL72S960398 1 19960221 A 5754 RIB BOEING 727 727232 1384082 NM NR 4 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 493DA 21062 A .5 INCH CRACK PAST PREVIOUS STOP DRILL, LOWER O/B SIDE OF NR 4 SLAT NOSE RIB AT ACTUATOR ATTACH. A .375 INCH CRACK UP PER O/B SIDE OF NR 4 L/E SLAT NOSE RIB AT ACTUATOR ATTACH. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1996030100108 19960301 00108 NM 1996 3 1 DL72S960399 1 19960221 A 5311 FRAME BOEING 727 727232 1384082 NM LT MLG WW CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 493DA 21062 FOUND DURING A-1 LETTER CHECK, .5 INCH CRACK IN LT MLG UPLOCK FRAME O/B FLANGE AT STA 910 UPPER END OF RADIUS BLOCK. RE PAIRED PER MM 53-11-0. 2 L 7 3 4F A3WE 1996030100109 19960301 00109 NM 1996 3 1 DL72S960402 1 19960221 A 5720 ANGLE BOEING 727 727232 1384082 NM RT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 493DA 21062 FOUND DURING A-1 LETTER CHECK, ANGLE CRACKED NR 7 SLAT O/B TRACK SUPPORT BOX I/B ANGLE. ANGLE CRACKED NR 6 SLAT I /B TRACK SUPPORT BOX I/B ANGLE. REPLACED ANGLES PER M/M 57-20-21 PG 813. 2 L 7 3 4F A3WE 1996030100110 19960301 00110 NM 1996 3 1 DL733960416 1 19960213 A 5230 DOOR BOEING 737 737347 1384647 NM FWD CARGO CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 302WA 23182 DURING OVERHAUL, THE AFT LOWER FRAME ON THE C1 DOOR WAS DISCOVERED TO HAVE A 1.5 INCH CRACK IN THE RADIUS. IN ACCORDANC E WITH BACO S/B 737-52-1100 REV 2, THE CROSS BEAM WAS MODIFIED AND THE FRAME WAS REPLACED. 2 L 7 2 4F RT A16WE 1996030100112 19960301 00112 NE 1996 3 1 DL76L960421 2 19960217 A 7230 FAN BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE DAMAGED A DALA K NONE C F.O.D. IN INSP/MAINT 1 SO 27 183DN 27110 724681 DURING LAYOVER, ENGINE FAN BLADES WERE FOUND WITH FOD EROSION DAMAGE. BORESCOPED ENGINE, NO DAMAGE FOUND. REPLACED ENGI NE FAN BLADE SET. 2 L 7 2 4F 4 F RT A1NM E24NE 1996030100113 19960301 00113 NE 1996 3 1 DL76L960422 2 19960217 A 7230 FAN BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE DAMAGED A DALA K NONE C F.O.D. IN INSP/MAINT 1 SO 27 183DN 27110 724165 DURING LAYOVER, FOUND NR 2 ENGINE WAS FOUND WITH FOD EROSION DAMAGE TO FAN BLADES. BORESCOPED ENGINE, NO DAMAGE FOUND. REPLACED ENGINE FAN BLADE SET. 2 L 7 2 4F 4 F RT A1NM E24NE 1996030100114 19960301 00114 NM 1996 3 1 DL76S960391 1 19960220 A 4900 380029816 APU BOEING 767 767332 1382001 NM AFT FUSELAGE MALFUNCTIONED A DALA F ACTIVATE FIRE EXT. P NO WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 125DL 14464 24075 ON TAXI OUT, TOWER NOTIFIED OF APU FIRE, NO COCKPIT INDICATION. DISCHARGED BOTTLE, INSPECTED APU AREA AND EXHAUST FOR D AMAGE AND SMOKE, NONE FOUND. INSPECTED TAIL SECTION AREA FOR DAMAGE, NONE FOUND. APU DEFFERED PER MEL 49-11-01A. SUSP ECT TAIL PIPE FIRE, FERRIED TO LAX. REPLACED APU, ROUTED TO SHOP. 2 L 7 2 4F RT A1NM 1996030100115 19960301 00115 NM 1996 3 1 DL76S960411 1 19960221 A 5330 143T3211 SKIN BOEING 767 767332 1382001 NM BS 456 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 117DL 23276 THE FUSELAGE SKIN IN THE VICINITY OF BS 456 AND CENTERED OVER THE S-36L LAP SPLICE WAS DAMAGED DUE TO CONTACT WITH GROUN D EQUIPMENT. AS A RESULT, THE SKIN IN THIS AREA WAS DENTED IN SEVERAL PLACES. THE SKIN WILL BE REPAIRED IN ACCORDANCE WITH DL ERA 273259 REV C. 2 L 7 2 4F RT A1NM 1996030100116 19960301 00116 WP 1996 3 1 DLL14960383 1 19960220 A 3230 RETAINING RING 1523153115 LKHEED 1011 1011385115 5265015 WP LT MLG SHEARED A DALA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 SO 27 741DA DL3 193C1245 LT LANDING GEAR TRUCK POSITION CYLINDER PISTON RETAINING RING HAD SHEARED FROM THE THREADED PORTION. LOST C-SYSTEM HY DRAULICS ON LANDING, CAUSED AUTO GROUND SPOILERS FAIL. REPLACED ACTUATOR, OPERATION NORMAL. 2 L 7 3 4F A23WE 1996030100117 19960301 00117 WP 1996 3 1 MWEA96045 1 19960221 A 3260 801801 PROXIMITY SENSOR DOUG DC9 DC932 3022066 WP LT MLG DAMAGED A MWEA D RETURN TO BLOCK N FALSE WARNING CL CLIMB 1 GL 31 602ME 48133 PILOT REPORTS, LT GEAR UNSAFE LIGHT ILLUMINATED AFTER GEAR RETRACTION. PERFORMED QRH, NO CHANGE. REPLACED DAMAGED LT G EAR UPLIMIT PROXIMITY SENSOR AND PLUG CONNECTOR. PERFORMED GEAR SWING, OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996030100118 19960301 00118 WP 1996 3 1 MWEA96046 1 19960221 A 5542 59102561 SKIN DOUG DC9 DC932 3022066 WP RUDDER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 DURING INSPECTION, FOUND CRACK IN RUDDER SKIN APPROX .875 INCH IN LENGTH FROM RIVET TO RIVET TOP CLOSE OUT RIB MID POINT OF RUDDER. INSTALLED FLUSH REPAIR IAW SRM 55-03 FIG 8A. 2 L 7 2 4F A6WE 1996030100119 19960301 00119 NM 1996 3 1 P5CA9600145 1 19960221 A 7110 NOSE COWL BOEING 747 747123 1384873 NM NR 1 ENGINE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 FOUND NR 1 ENGINE NOSE COWL INLET ACOUSTICAL PANEL AT THE 8 O'CLOCK POSITION IS DELAMINATING AT THE CORNER OF OUTER PANE L. FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 54-30-03 AND 51-10-01. 2 L 7 4 4F A20WE 1996030100120 19960301 00120 NM 1996 3 1 P5CA9600146 1 19960222 A 5522 65B0808161 SKIN BOEING 747 747123 1384873 NM RT ELEVATOR DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 FOUND TEMPORARY COMPOSITE REPAIR DELAMINATED AT RIGHT OUTBOARD ELEVATOR INBOARD TRAILING EDGE. REMOVED AND REPLACED SKI N FROM RIGHT OUTBOARD ELEVATOR IAW SRM 51-40-12. 2 L 7 4 4F A20WE 1996030100121 19960301 00121 NM 1996 3 1 P5CA9600147 1 19960222 A 5730 65B0808161 PANEL BOEING 747 747123 1384873 NM LT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 FOUND UPPER LEFT WING COMPOSITE PANEL AT ROOT DELAMINATED AT LEADING EDGE. REMOVED AND REPLACED PANEL IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996030100122 19960301 00122 EU 1996 3 1 QXEA9600073 1 19960222 A 3350 MGG1280 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 801PH 11097 FORWARD PASSENGER CABIN EXIT, BOTH SIGNS 28V LAMPS ARE INOP. BULBS WERE REPLACED AND SIGNS OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996030100123 19960301 00123 WP 1996 3 1 SCNA96023 1 19960219 A 2611 PU90499 SMOKE DETECTOR DOUG DC10 DC1015 3022118 WP LAVATORY-B FAILED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 LAVATORY B-SMOKE DETECTOR WILL NOT RESET. REMOVED AND REPLACED SMOKE DETECTOR AND PREFORMED SELF TEST, OPS CHECKED OK. 2 L 7 3 4F A22WE 1996030100124 19960301 00124 NM 1996 3 1 SCNA96024 1 19960220 A 3350 900814 BATTERY PACK BOEING 727 727225 1384077 NM RT OVERWING DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 282SC 22558 THE RIGHT EXTERIOR FORWARD OVERWING EMERGENCY LIGHT WAS FOUND STROBING. REMOVED AND REPLACED BATTERY PACK AND LIGHT CHE CKED NORMAL. 2 L 7 3 4F A3WE 1996030100125 19960301 00125 NM 1996 3 1 SCNA96025 1 19960221 A 3350 S106 BATTERIES BOEING 727 727225 1384077 NM AFT ENTRY DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 282SC 22558 THE AFT ENTRY EMERGENCY AREA LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED BATTERIES IAW MM 33-50-101 AND SYSTEM OP CHECKED GOOD. 2 L 7 3 4F A3WE 1996030100126 19960301 00126 WP 1996 3 1 SCNA96026 1 19960221 A 3350 A3060733101 TRACK DOUG DC10 DC1010 3022110 WP CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 573SC 46905 THE AFT CABIN, LEFT SIDE, REAR HALF OF EMERGENCY PATH LIGHTING WAS FOUND TO BE INOPERATIVE. REPLACED DAMAGED SECTION OF FLOOR TRACK LIGHTING AND FLOOR TRACK LIGHTING OPS CHECKED GOOD. 2 L 7 3 4F A22WE 1996030100127 19960301 00127 NM 1996 3 1 UPS2005546 1 19960220 A 2910 LINE BOEING 727 727247 138408F NM B-HYD SYSTEM FAILED A IPXA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 207UP 21699 CREW REPORTED, AFTER GEAR EXT, LOSS OF B-SYSTEM PRESSURE AND LOW PRESSURE LIGHTS CAME ON. B-SYS PRESS ZERO AND QUANTITY DECREASED FROM 3 TO 1.9, RAN APPROVED CHECKLIST, LOST B-SYS. REPLACED NR 2 PUMP PRESSURE LINE WITH TEMPORARY FLEX LINE BETWEEN B-PUMP AND B-SYS MODULE PACKAGE. NO LEAKS NOTED, OPS CHECK OK (DEFFERAL NR D-106432). 2 L 7 3 4F A3WE 1996030100128 19960301 00128 NM 1996 3 1 UPS2005547 1 19960221 A 3020 567618 ANTI-ICE TUBE BOEING 727 72725C 138400H NM NR 2 ENGINE BROKEN A IPXA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 01 947UP 19722 CREW REPORTED, NR 2 FIRE WARN LIGHT AND BELL WITH CLIMB THRUST, CLIMBING TO ALTITUDE OUT OF ROA. ENGINE NR 2 SHUTDOWN A T 0927Z PER CHECKLIST, FIRE LIGHT WENT OUT AND ALL ENGINE INDICATIONS NORMAL. ENGINE HEAT WAS ON IN THE ICING CONDITION S. REMOVED AND REPLACED BROKEN LT REAR A/I TUBE ASSY. REMOVED AND REPLACED CRACKED HIGH PRESSURE SUPPLY WYE DUCT. ALL IAW MM 75-10, LEAK CHECK GOOD. 2 L 7 3 4F A3WE 1996030100129 19960301 00129 NM 1996 3 1 UPS205534 1 19960213 A 5241 5708458503 UPPER GATE BOEING 727 72725C 138400H NM MID GALLEY DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, MID GALLEY DOOR UPPER GATE HAS AREAS OF CORROSION. REMOVED AND REPLACED MID GALLEY DOOR GATE IAW SRM 51-10-1, 51-20-4, 51-30-8 AND MM 52-12-11. 2 L 7 3 4F A3WE 1996030100130 19960301 00130 NM 1996 3 1 UPS205535 1 19960212 A 5230 FRAME BOEING 727 72725C 138400H NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK MAINTENANCE REPORTED WHILE WORKING NRC 432263 DOOR 74, FOUND THE UPPER FLANGE ON THE LOWER AFT FRAM E TO BE CRACKED. REPAIRED UPPER FLANGE ON THE LOWER AFT FRAME ON AFT CARGO DOOR IAW SRM 51-40-3. 2 L 7 3 4F A3WE 1996030100131 19960301 00131 NM 1996 3 1 UPS205536 1 19960214 A 5320 WEB BOEING 727 72725C 138400H NM BS 227 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, VERTICAL WEB FOUND TO BE CORRODED OUT OF LIMITS PER SRM 53-10-2 AT STA 227 LB L 41 TO 44 WL 209 TO 218, CORROSION (C53-221-01,03, 01). REMOVED DAMAGED AREA OF VERTICAL WEB, FABRICATED REPAIR PARTS AND INSTALLED PER 53-10-2 AND 51-20-4. 2 L 7 3 4F A3WE 1996030100132 19960301 00132 NM 1996 3 1 UPS205537 1 19960210 A 5330 SKIN BOEING 727 72725C 138400H NM BS 310 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON FUSELAGE SKIN AFT OF FWD TOILET SERVICE PANEL BS 310 RBL 68 WL 1 86. CORROSION OUT OF LIMITS, REMOVED DAMAGED SKIN, FABRICATED REPAIR PARTS AND INSTALLED. ALL WORK DONE PER SRM 53-30- 3 AND 53-30-2. 2 L 7 3 4F A3WE 1996030100133 19960301 00133 NM 1996 3 1 UPS205538 1 19960212 A 5330 SKIN BOEING 727 72725C 138400H NM BS 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON INSIDE OF FUSELAGE SKIN BELOW FWD TOILET SERVICE PANEL AT BS 300 RBL 54 WL 182. REMOVED DAMAGED AREA AND REPAIRED PER SRM 53-30-3 AND 53-30-2. 2 L 7 3 4F A3WE 1996030100134 19960301 00134 NM 1996 3 1 UPS205539 1 19960213 A 5755 SKIN BOEING 727 72725C 138400H NM NR 1 SPOILER DELAMINATION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, NR 1 SPOILER HAS AN AREA OF DELAMINATION AT HINGE AREA FWD EDGE CENTER OF SPO ILER UPPER SURFACE. REPAIRED NR 1 SPOILER IAW SRM 51-40-6. 2 L 7 3 4F A3WE 1996030100135 19960301 00135 NM 1996 3 1 UPS205540 1 19960213 A 5755 SPOILER BOEING 727 72725C 138400H NM LT WING WATER ENTRAPED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, NR 1 SPOILER HAS POSSIBLE WATER ENTRAPMENT IN VIEW 4 OF X-RAY. REPAIRED NR 1 SPOILER IAW SRM 51-40-6. 2 L 7 3 4F A3WE 1996030100136 19960301 00136 NM 1996 3 1 UPS205541 1 19960213 A 5755 SPOILER BOEING 727 72725C 138400H NM LT WING WATER ENTRAPED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, NR 1 SPOILER HAS POSSIBLE WATER ENTRAPMENT IN VIEW 6 OF X-RAY. REPAIRED NR 1 SPOILER IAW SRM 51-40-6. 2 L 7 3 4F A3WE 1996030100137 19960301 00137 NM 1996 3 1 UPS205542 1 19960214 A 5754 65217505A BULLNOSE BOEING 727 72725C 138400H NM NR 2 K-FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, L/W NR 2 K-FLAP BULLNOSE IS CORRODED AT O/B HINGE LOWER ATTACH POINT. REMOVE D AND REPLACED BULLNOSE IAW MM 27-81-01 AND SRM 57-50-1. 2 L 7 3 4F A3WE 1996030100138 19960301 00138 NM 1996 3 1 UPS205543 1 19960214 A 5751 CENTER HINGE BOEING 727 72725C 138400H NM LT INBD AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT I/B AILERON CENTER HINGE IS CORRODED AT PANEL ATTACH POINT. REPLACED HING E FITTING IAW MM 27-10-01. 2 L 7 3 4F A3WE 1996030100139 19960301 00139 NM 1996 3 1 UPS205544 1 19960213 A 5755 FITTING BOEING 727 72725C 138400H NM NR 3 SPOILER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, I/B CENTER HINGE BOLT HOLE CORRODED, NR 3 SPOILER. REMOVED AND REPLACED NR 3 SPOILER ACT HINGE FITTING IAW MM 27-61-81. 2 L 7 3 4F A3WE 1996030100140 19960301 00140 NM 1996 3 1 UPS205558 1 19960216 A 5320 CHORD BOEING 727 72725C 138400H NM BS 330-346 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON MID CHORD BETWEEN DOG HOUSE FLOOR AND CHORD BS 330 AND 346 RBL 1 5 WL 170. REMOVED AND REPLACED MID CHORD IAW SRM 51-30-2 AND 51-20-4. 2 L 7 3 4F A3WE 1996030100141 19960301 00141 NM 1996 3 1 UPS205559 1 19960216 A 5320 STIFFENER BOEING 727 72725C 138400H NM BS 344 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON NOSE GEAR W/W VERT STIFFENER AT BS 344 LBL 14 WL 173 AND 180. R EMOVED AND REPLACED STIFFENER IAW SRM 51-30-2 AND 51-20-4. 2 L 7 3 4F A3WE 1996030100142 19960301 00142 NM 1996 3 1 UPS205560 1 19960216 A 5320 STIFFENER BOEING 727 72725C 138400H NM BS 344 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON VERT STIFFENER AT BS 344 LBL 14 WL 180. REMOVED AND REPLACED ST IFFENER IAW SRM 51-30-2 AND 51-20-4. 2 L 7 3 4F A3WE 1996030100143 19960301 00143 NM 1996 3 1 UPS205561 1 19960217 A 5754 UPPER LUG BOEING 727 72725C 138400H NM NR 5 K-FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, NR 5 K-FLAP O/B UPPER LUG CORRODED AT BONDING POINT. REMOVED AND REPLACED NR 5 K-FLAP IAW UPS MM 27-81-01. 2 L 7 3 4F A3WE 1996030100144 19960301 00144 NM 1996 3 1 UPS205562 1 19960216 A 5751 FITTING BOEING 727 72725C 138400H NM RT INBD AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING O/B AILERON I/B CENTER HINGE FITTING AILERON SIDE IS CORRODED AND BEA RING BLOCK HAS BLOWN DUST COVER. REPLACED CENTER HINGE FITTING IAW UPS OHM 57-50-111 AND MM 27-10-41. 2 L 7 3 4F A3WE 1996030100145 19960301 00145 NM 1996 3 1 UPS205563 1 19960214 A 5347 SEAT TRACK BOEING 727 72725C 138400H NM BS 550-650 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, SEAT TRACK STA 480 TO 650 RBL 45 WL 208 HAS MECHANICAL DAMAGE AND CORROSION. REPLACED SECTION OF SEAT TRACK FROM BS 550 TO 650 RBL 45 WL 208. WORK DONE PER SRM 53-10-5 AND 51-30-8. 2 L 7 3 4F A3WE 1996030100146 19960301 00146 NM 1996 3 1 UPS205564 1 19960214 A 5347 SEAT TRACK BOEING 727 72725C 138400H NM BS 650-740 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION IN WELL OF SEAT TRACK AT STA 680 TO 730, LBL 45, WL 208. REMOVED C ORRODED SEAT TRACK FROM BS 650 TO 740, WL 208, LBL 45, FABRICATED NEW SECTION AND INSTALLED. ALL WORK DONE PER SRM 53-1 0-1 AND 53-10-5. 2 L 7 3 4F A3WE 1996030100147 19960301 00147 NM 1996 3 1 UPS205565 1 19960202 A 5755 SUPPORT FITTING BOEING 727 72725C 138400H NM NR 11 SPOILER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, FLUORESCENT PENETRANT INSPECTION OF THE NR 11 O/B FLT SPOILER ACT SUPPORT FIT TING, EXHIBITS CORROSION INDICATIONS AROUND THE HOLE ON BOTH THE I/B AND O/B LOWER LUGS. REMOVED AND INSTALLED NEW FITT ING. WORK DONE PER SRM 51-30-2, MM 27-51-131, AND 27-61-81. 2 L 7 3 4F A3WE 1996030100148 19960301 00148 NM 1996 3 1 UPS205566 1 19960216 A 5320 WEB BOEING 727 72725C 138400H NM BS 203-219 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION ON WEB AND ANGLES AT STA 203 TO 219 LBL 15 WL 159. REPLACED WEB IA W SRM 51-40-2, 51-30-2, 51-10-6, 51-10-2, 51-10-1, 53-10-1, 51-20-4, AND 51-20-1. 2 L 7 3 4F A3WE 1996030100149 19960301 00149 NM 1996 3 1 UPS405530 1 19960216 A 5751 FITTINGS BOEING 747 747121 1384871 NM LT AILERON ELONGATED HOLES A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN AMS FOR C-CHECK MAINTENANCE REPORTED, LT WING O/B AILERON, 4 ATTACHMENT FITTINGS HOLES ARE ELONGATED AT WS 1308 , 1423, 1485 AND 1548. REPLACED HINGE FITTINGS IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996030100150 19960301 00150 NM 1996 3 1 UPS405531 1 19960216 A 5320 SHEAR TIES BOEING 747 747121 1384871 NM BS 1980 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN AMS FOR C-CHECK MAINTENANCE REPORTED, FOUND 3 CRACKED SHEAR TIES AT BS 1980 BETWEEN STR 46 TO 50 LBL. REPAIRED SHEAR TIES IAW SRM 53-10-4 FIG 41. 2 L 7 4 4F A20WE 1996030100151 19960301 00151 NM 1996 3 1 UPS405532 1 19960201 A 5320 SHEAR TIE BOEING 747 747121 1384871 NM BS 2120 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN AMS FOR C-CHECK MAINTENANCE REPORTED, FOUND 2 CRACKED SHEAR TIES AT BS 2120 BETWEEN STR 45 TO 50 LBL AND BETWEE N STRINGER 49 TO 50 RBL. REPAIRED PER SRM 53-10-4 FIG 41. 2 L 7 4 4F A20WE 1996030100152 19960301 00152 NM 1996 3 1 UPS405533 1 19960218 A 2560 RELEASE MECH BOEING 747 747121 1384871 NM ESCAPE HATCH INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 MAINTENANCE REPORTED, FLIGHT DECK OVERHEAD ESCAPE HATCH WILL NOT UNLOCK AND OPEN. RESECURED LOOSE LINKAGE IN FLIGHT DEC K OVERHEAD ESCAPE HATCH DOOR, OPS CHECKS NORMAL. 2 L 7 4 4F A20WE 1996030100153 19960301 00153 NM 1996 3 1 UPS405548 1 19960208 A 5730 SKIN BOEING 747 747121 1384871 NM WS 1160 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN AMS FOR C-CHECK, DURING RIVET INSTALLATION FOUND RT WING CORROSION ON LOWER SIDE OF UPPER WING SKIN O/B OF PYL ON 4 AT WS 1160. REPAIRED IAW KLM DFX 96-040 ISSUE NR 3 APPROVED PER UPS 747-57-0309. 2 L 7 4 4F A20WE 1996030100154 19960301 00154 NM 1996 3 1 UPS405549 1 19960207 A 5311 FRAME BOEING 747 747121 1384871 NM BS 1840 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN AMS FOR C-CHECK, FOUND CRACK IN FRAME UPPER CHORD BS 1840 RT BL 32 NEAR EXISTING SPLICE. REMOVED DAMAGE UPPER CHORD AND REPAIRED CHORD ACC TO KLM DFX 96-035, ISSUE NR 4, APPROVED PER UPS EFN 747-53-0751. 2 L 7 4 4F A20WE 1996030100155 19960301 00155 NM 1996 3 1 UPS405550 1 19960205 A 5320 WEB BOEING 747 747121 1384871 NM BS 1840-1860 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN AMS FOR C-CHECK MAINTENANCE REPORTED, DENT IN UPPER WEB OF TORQUE BOX BS 1840 TO 1860 RBL 20. REPLACED UPPER W EB AND BLIND FASTENERS FOR SOLID FASTENERS PER SRM 51-30-02. 2 L 7 4 4F A20WE 1996030100156 19960301 00156 NM 1996 3 1 UPS405551 1 19960206 A 5320 SHEAR TIE BOEING 747 747121 1384871 NM BS 1880 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN AMS FOR C-CHECK MAINTENANCE REPORTED, SHEAR TIES CRACKED AT FRAME BS 1880 BETWEEN S-48/47 RT S-51/50 RT AND S-4 5/44 LT. REPAIRED SHEAR TIES IAW SRM 53-10-04 FIG 3. 2 L 7 4 4F A20WE 1996030100157 19960301 00157 NM 1996 3 1 UPS405552 1 19960205 A 5320 FASTENERS BOEING 747 747121 1384871 NM BS 1840-1860 LOOSE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN AMS FOR C-CHECK MAINTENANCE REPORTED, LOOSE FASTENERS IN UPPER WEB OF TORQUE BOX BS 1840 TO 1860 BETWEEN RBL 25 TO 45. REPLACED UPPER WEB AND REPLACED BLIND FASTENERS FOR SOLID FASTENERS PER SRM 51-30-02. 2 L 7 4 4F A20WE 1996030100158 19960301 00158 NM 1996 3 1 UPS405553 1 19960206 A 5320 SHEAR TIE BOEING 747 747121 1384871 NM BS 1900 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN AMS FOR C-CHECK MAINTENANCE REPORTED, CRACKS IN FRAME SHEAR TIES AT BS 1900 BETWEEN S-46/45 LT AND S-45/44 LT. REPAIRED SHEAR TIES IAW SRM 53-10-04 FIG 3. 2 L 7 4 4F A20WE 1996030100159 19960301 00159 NM 1996 3 1 UPS405554 1 19960206 A 5347 CARGO TRACK BOEING 747 747121 1384871 NM BS 1910 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN AMS FOR C-CHECK MAINTENANCE REPORTED, CRACK IN CARGO TRACK LOWER SIDE UNDER END-STOP FITTING, BS 1910 RBL 45. S TOP DRILLED CRACK AND REPAIRED TRACK IAW SRM 53-10-05 FIG 2. 2 L 7 4 4F A20WE 1996030100160 19960301 00160 NM 1996 3 1 UPS405555 1 19960201 A 5320 SHEAR TIE BOEING 747 747121 1384871 NM BS 1700 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN AMS FOR C-CHECK MAINTENANCE REPORTED, CRACKS IN SHEAR TIES AT BS 1700 BETWEEN S-51 LT/RT, S-48/47 AND S-47/46 R T. REPAIRED SHEAR TIES AT BS 1700 IAW SRM 53-10-04 FIG 3. 2 L 7 4 4F A20WE 1996030100161 19960301 00161 NM 1996 3 1 UPS405556 1 19960202 A 5313 LONGERON BOEING 747 747121 1384871 NM BS 1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN AMS FOR C-CHECK MAINTENANCE REPORTED, RT BLG WW OVERWING LONGERON CRACKED FROM BS 1480. REPAIRED IAW SRM 53-1 0-01 FIG 1 AND AS PER BOEING TELEX UPS- AMS -96-0038RE. 2 L 7 4 4F A20WE 1996030100162 19960301 00162 NM 1996 3 1 UPS405557 1 19960201 A 5330 SKIN BOEING 747 747121 1384871 NM BS 1700-1720 DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN AMS FOR C-CHECK MAINTENANCE REPORTED, FOUND DELAMINATION DUE TO CORROSION ON SKIN LAP SPLICE UNDER S-46 RT BETW EEN BS 1700/1720. REMOVED EXISTING REPAIR PER SRM 51-30-02, REMOVED DELAMINATED PART OF OVERLAPPED SKIN BY EXTENDING CU TOUT TO BS 1695 AND REPAIRED LAP SPLICE IAW SRM 53-30-03 FIG 18. 2 L 7 4 4F A20WE 1996030100163 19960301 00163 1996 3 1 UPS5005545 4 19960221 A 3442 WXR CONTL PNL BOEING 757 75724APF 1384969 NM COCKPIT SHORTED A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 435UP 25466 CREW REPORTED, WXR FAIL DISPLAYED ON HSI DURING INFLIGHT WXR TEST. ELECTRICAL FUMES NOTED, TEST SECURED. FUMES DISSAPA TED, ASSIGNED M-106357 PER MEL 34-43-1 AND INSTALLED PLACARD PER MEL. 2 L 7 2 4F RT A2NM 1996030100164 19960301 00164 WP 1996 3 1 UPS805567 1 19960220 A 3350 5708458503 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 818UP 46108 ON PREDEPARTURE, EMERGENCY LIGHT FAILED. REPLACED BATTERY PACK. 2 L 7 4 4F RT 4A25 1996030100165 19960301 00165 EU 1996 3 1 WWMA9600022 1 19960220 A 2611 7211121000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU LAV DEFECTIVE A WWMA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 WP 15 339SB 340B339 DURING ENGINE START THE LAV SMOKE LIGHT ILLUMINATED, THE FLIGHT ATTENDENT CONFIRMED IT WAS A FALSE INDICATION. MAINTENA NCE REPLACED THE LAV SMOKE DETECTOR AND RELEASED THE AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 1996030100166 19960301 00166 1996 3 1 WWMA9600023 4 19960221 A 3416 6223975001 ALTIMETER SAAB SF340 340B 7860101 EU LEFT DEFECTIVE A WWMA O OTHER J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 15 349SB 340B349 LEFT ALTIMETER FLAG CAME ON 15 MINUTES AFTER TAKEOFF, IT WAS FOLLOWED BY AN ELECTRICAL SMOKE ODOR. THE LEFT ALTIMETER C IRCUIT BREAKER WAS PULLED AND THE FLIGHT CONTINUED TO PSP WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT ALTIMETER AND RETURNED THE AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 1996030100167 19960301 00167 WP 1996 3 1 9604579868 1 19960217 A 7332 WARNING LIGHT DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE FUEL PRESSURE ILLUMINATED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 777NC 47787 696709 MASTER CAUTION AND LOW FUEL PRESSURE WARNING ILLUMINATED ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETU RNED TO THE GATE. THE FLIGHT CREW APPLIED FUEL HEAT WHILE RETURNING TO THE GATE AND CLEARED THE WARNING. THE ENGINE WA S INSPECTED AND RUNUP, NO DISCREPANCIES WERE NOTED. 2 L 7 2 4F 4 F A6WE E2EA 1996030100168 19960301 00168 NM 1996 3 1 9604586628 1 19960224 A 3241 421897 CONTROL UNIT BOEING 747 747251B 1384892 NM LT/RT ANTI-SKID FAILED A NWAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 01 628US 14698 8055 22389 DURING TAKEOFF, ANTI-SKID LIGHTS ILLUMINATED ON BOTH THE PILOTS AND SECOND OFFICER'S PANEL. ABORTED TAKEOFF AND RETURNE D TO THE GATE. REPLACED THE ANTI-SKID CONTROL UNIT AND OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996030100169 19960301 00169 WP 1996 3 1 9604599992 1 19960118 A 2822 CIRCUIT BREAKER DOUG DC9 DC931 3022065 WP FUEL BOOST PUMP TRIPPED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 8960E 45869 AFT CENTER FUEL BOOST PUMP CIRCUIT BREAKERS POPPED DURING CLIMBOUT. CREW PERFORMED COCKPIT OPERATING MANUAL PROCEDURES AND BREAKERS POPPED AGAIN. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET AFT CENTER FUEL BOOST PUMP CIRCUIT BREAKERS AND RAN PUMPS FOR OVER ONE HOUR WITH NO PROBLEMS. 2 L 7 2 4F A6WE 1996030100170 19960301 00170 WP 1996 3 1 9604609975 1 19960225 A 3297 WIRE DOUG DC9 DC931 3022065 WP LT MLG BROKEN A NWAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 01 9339 47382 DURING APPROACH INTO FAR, THE LEFT MAIN GEAR GREEN INDICATION LIGHT FAILED TO ILLUMINATE AFTER GEAR WAS EXTENDED FOR LAN DING. EXECUTED GO-AROUND PROCEDURES AND CREW VISUALLY CONFIRMED THROUGH PERISCOPE THAT GEAR WAS DOWN AND LOCKED. CAPTA IN DECLARED AN EMERGENCY AND AIRCRAFT LANDED WITHOUT INCIDENT ON SECOND ATTEMPT. MAINTENANCE FOUND FAULTY WIRE AT LEFT MAIN GEAR DOWNLOCK SWITCH. REPAIRED BROKEN WIRE AT SWITCH CONNECTOR AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996030100171 19960301 00171 WP 1996 3 1 9604619931 1 19960223 A 3260 DOOR SWITCH DOUG DC9 DC931 3022065 WP LT MLG FAILED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 90S 47244 LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE LEFT MAIN GEAR DOOR SWITCH AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996030100172 19960301 00172 NM 1996 3 1 9604622203 1 19960224 A 2781 GROUND WIRE BOEING 727 727251 138408H NM NR 8 LE FLAP BROKEN A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 203US 22543 DURING TAKEOFF ROLL, THE LEADING EDGE INDICATOR WENT AMBER AND TAKEOFF WAS ABORTED AT 30 KNOTS. AIRCRAFT RETURNED TO BL OCKS WITHOUT INCIDENT. BROKEN GROUND WIRE WAS FOUND ON THE NR 8 LEADING EDGE SLAT EXTEND SWITCH. REPAIRED WIRE AND OPE RATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996030100173 19960301 00173 NE 1996 3 1 9604631150 2 19960225 A 7230 COMPRESSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 2 ENGINE STALLED A NWAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DE DESCENT 1 GL 01 150US 46759 86144 DURING DESCENT, THE NR 2 ENGINE COMPRESSOR STALLED AND INFLIGHT SHUTDOWN WAS ACCOMPLISHED. CREW FOLLOWED COCKPIT OPERAT ING PROCEDURE AND CONTINUED FLIGHT TO PHX. INSPECTION AND RUNUP OF NR 2 ENGINE ON GROUND WAS NORMAL. 2 L 7 3 4F 4 F A22WE E20EA 1996030100174 19960301 00174 WP 1996 3 1 9604641220 1 19960226 A 2780 RETRACT MECH DOUG DC10 DC1030 3023501 WP LE FLAPS MALFUNCTIONED A NWAA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION TO TAKEOFF 1 GL 01 220NW 46577 DURING TAKEOFF, THE SLATS WOULD NOT RETRACT. THE FLIGHT DUMPED FUEL AND RETURNED TO LGW. MAINTENANCE RESET THE AUTO SL AT SYSTEM AND OPERATIONAL CHECK OK. 2 L 7 3 4F A22WE 1996030100175 19960301 00175 WP 1996 3 1 9604659966 1 19960224 A 3350 6011779 BATTERY PACK DOUG DC9 DC931 3022065 WP LT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9330 47138 DURING LINE MAINTENANCE INSPECTION, FOUND THE LEFT ENGINE NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AN D OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996030100176 19960301 00176 WP 1996 3 1 9604669966 1 19960224 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9330 47138 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD OVERWING EXIT EMERGENCY LIGHTS WEAK. REPLACED BATTERIES AND OPERATION AL CHECK NORMAL. 2 L 7 2 4F A6WE 1996030100177 19960301 00177 NM 1996 3 1 96FDEA00307 1 19960206 A 5313 STRINGER BOEING 727 72725C 138400H NM BS 676 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 118FE 19300 UPPER LOBE MAIN CARGO INTERIOR STRUCTURE, STR 15L CRACKED AT FS 676. REMOVED DAMAGED SECTION OF STR 15L AND INSTALLED S TR SPLICE REPAIR PER SRM 53-10-3 FIG 1 PG 3 TO 48. 2 L 7 3 4F A3WE 1996030100178 19960301 00178 NM 1996 3 1 96FDEA00308 1 19960207 A 5320 STIFFENER BOEING 727 72725C 138400H NM BS 870 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 118 19300 CENTER TANK STA 870 BL 0 VERTICAL STIFFENER HAS POPPED FASTENERS AND WEB IS BULDGED. INSTALLED NEW CENTER TANK VERTICAL STIFFENER AND WEB REPAIR PER SRM 51-10-1 AND EA 7-5710-27462. 2 L 7 3 4F A3WE 1996030100179 19960301 00179 NM 1996 3 1 96FDEA00309 1 19960213 A 5320 WEB BOEING 727 72725C 138400H NM CENTER TANK CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 118FE 19300 LOWER FUSE CENTER TANK REAR SPAR UPPER CHORD, 3 RIVETS HAD POPPED 2 RIVETS WORKING, SKIN WARP BULGE LBL 18 TO 30. INSTA LLED DOUBLER AND TRIPLER TO CENTER TANK UPPER WEB PER ESO 11782 DATED 2-13-96, AWAITING FEDEX EA. 2 L 7 3 4F A3WE 1996030100180 19960301 00180 NM 1996 3 1 96FDEA00310 1 19960213 A 5311 BELLFRAME BOEING 727 72725C 138400H NM BS 990 PLUGGED HOLE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 118FE 19300 STR 27L BELLFRAME 990 PLUGGED HOLE TOP NEAR EXISTING FASTENER HOLE. INSTALLED DOUBLER PER SRM 51-40-3. 2 L 7 3 4F A3WE 1996030100181 19960301 00181 NM 1996 3 1 96FDEA00311 1 19960220 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 950 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 118FE 19300 CABIN FLOORBEAM AT STA 950 IS CORRODED AROUND SCREW HOLES TOP AND BOTTOM OF BEAM FROM SEAT TRACK NR 3 TO NR 5. REMOVED CORROSION PER 51-10-06, OUT OF LIMITS. REPAIRED PER ESO 11782 AND FEDEX EA 7-5310-27477. 2 L 7 3 4F A3WE 1996030100182 19960301 00182 NM 1996 3 1 96FDEA00312 1 19960223 A 5320 FORGING BOEING 727 72725C 138400H NM BS 870 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 118FE 1930 HFEC IND A CRACK IN LT STA 870 FORGING AT INTEGRAL RIB, BELOW CABIN FLOOR WL 190 ON TOP SIDE AT LOWER AFT FASTENER CRACK . ALSO, RUNNING UNDER RIB EXTENDING AFT. REMOVED INTEGRAL RIB FLUSH WITH WEB, PER ESO 11782. HFEC CONFIRMED NO CRACKS AFTER DAMAGE REMOVAL. FABRICATED BATH TUBE FITTING PER ESO 11782 DATED 2-15-96 AND BOEING S/B 53-0116 DATED 10-31-91. INSTALLED REPAIR FITTING AND EXTERNAL STRAP PER ESO 11782 AND FEDEX EA 7-5310-27474A. 2 L 7 3 4F A3WE 1996030100183 19960301 00183 NM 1996 3 1 96FDEA00313 1 19960222 A 5530 65195316 RT FITTING BOEING 727 72722 1384002 NM BS 1342 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION (C53-137-01) BS 1342 RBL 17 STR 5R ON FITTING ANGLE. REMOVED CORROSION TERMINAL FITTING AND INSTALLED NEW RT SPAR FITTING AT BS 1342 IAW BOEING SB 727-55-088. 2 L 7 3 4F A3WE 1996030100184 19960301 00184 NM 1996 3 1 96FDEA00314 1 19960222 A 5530 65195315 LT FITTING BOEING 727 72722 1384002 NM BS 1342 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION (C53-137-01) BS 1342 LBL 17 STR 5L ON FITTING ANGLE. REMOVED AND REPLACED FITTING AT 1342, LBL 17 AT S5L PER. 2 L 7 3 4F A3WE 1996030100185 19960301 00185 NM 1996 3 1 96FDEA00315 1 19960222 A 5320 6515929 WEB BOEING 727 72722 1384002 NM BS 520 CRACK A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CRACK IN WEB AT BS 520 WL 198 RBL 58. *S/D* REMOVED AND FABRICATED NEW WEB AND INSTALLED THE WEB AT BS 500 TO 580, RBL 58, WL 198 AS PER BOEING DRAWING 65-19309. 2 L 7 3 4F A3WE 1996030100186 19960301 00186 NM 1996 3 1 96FDEA00316 1 19960222 A 5315 45838 FLOOR BEAM BOEING 727 72722 1384002 NM BS 620 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION (C53-111-01, -2) ON LOWER FLANGE OF FLOORBEAM IN NUTPLATE HOLES AT BS 620 LBL 20 TO RBL 26 WL 200. *S/D* REP AIRED FLOOR BS 620, LBL 20 TO RBL 26, WL 200 IAW FEDEX SRM 53-10-8. 2 L 7 3 4F A3WE 1996030100187 19960301 00187 NM 1996 3 1 96FDEA00317 1 19960222 A 5320 65317731 CHORD BOEING 727 72722 1384002 NM BS 1176 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION (C53-224-08) ON BS 1176 CHORD AT LBL 20 AND RBL 65 WL 208. REMOVED AND REPLACED BS 1176 CHORD PER SRM 51-30-2 . 2 L 7 3 4F A3WE 1996030100188 19960301 00188 NM 1996 3 1 96FDEA00318 1 19960222 A 5330 6554573 SKIN BOEING 727 72722 1384002 NM BS 640-650 GOUGE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 GOUGES IN SKIN AT BS 590 TO 620 BETWEEN STR 21 TO 22R. *S/D* REPAIRED 3 GOUGES IN THE SKIN AT BS 590 TO 620 BETWEEN ST R 21 TO 22 RT PER FEDEX SRM 53-30-3. 2 L 7 3 4F A3WE 1996030100189 19960301 00189 NM 1996 3 1 96FDEA00319 1 19960222 A 5320 65189552 FITTING BOEING 727 72722 1384002 NM BS 360 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION ON STR 26R FITTING BS 360. REMOVED T-FITTING AT BS 360, STR 26R, INSTALLED NEW T-FITTING AT BS 360 STR 26R PE R SRM 53-10-1 AND SRM 53-10-3. 2 L 7 3 4F A3WE 1996030100190 19960301 00190 NM 1996 3 1 96FDEA00320 1 19960222 A 5320 65189553 FITTING BOEING 727 72722 1384002 NM BS 360 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION (C53-111-01-1) STR 26L FITTING BS 360. REPAIRED STRINGER TE FITTING AT S26L, BS 360 AND MADE STRINGER REPAIR ON S26L FROM BS 360 TO 390, DAMAGE ON THAT PORTION OF STRINGER FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 AND SRM 53-10-3 . 2 L 7 3 4F A3WE 1996030100191 19960301 00191 NM 1996 3 1 96FDEA00321 1 19960222 A 5315 6540145 FLOOR BEAM BOEING 727 72722 1384002 NM BS 1010 DOUBLE DRILLED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 194FE 19143 WHILE WORKING NR0754, FOUND DOUBLE HOLE IN BS 1010 FLOOR BEAM AT BL 0 WL 208. *S/D* REMOVED DAMAGED, FABRICATED REPAI R PARTS AND INSTALLED PER SRM 53-10-8. 2 L 7 3 4F A3WE 1996030100192 19960301 00192 NM 1996 3 1 96FDEA00322 1 19960222 A 5320 69239021 FITTING BOEING 727 72722 1384002 NM BS 360-367 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION ON STR 20L FITTING BS 360 TO 367. REMOVED AND REPLACED CORRODED FITTING PER SB 727-53-0209. 2 L 7 3 4F A3WE 1996030100193 19960301 00193 NM 1996 3 1 96FDEA00324 1 19960222 A 5320 65175551622 WEB BOEING 727 72722 1384002 NM BS 1362 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 WHILE WORKING NR0122, FOUND RIB SUPPORT WEB TO BE CRACKED AT 3 FASTENER LOCATIONS BS 1662 WL 281 RBL 11. 2 L 7 3 4F A3WE 1996030100194 19960301 00194 NM 1996 3 1 96FDEA00325 1 19960222 A 5320 6516312 WEB BOEING 727 72722 1384002 NM BS 294-355 CORROSIOIN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION ON WEB AT BS 294.5 TO 355 RBL 10 TO 35 WL 169. CORROSION FOUND TO BE OUT OF LIMITS. *S/D* REMOVED AND REPLA CED WEB PER SRM 51-40-02. 2 L 7 3 4F A3WE 1996030100195 19960301 00195 WP 1996 3 1 96FDEA00326 1 19960222 A 5754 BRACKET DOUG DC10 DC1030 3023501 WP LT LE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 320FE 47835 LEFT O/B SLAT DRIVE OUTER BRACKET CRACKED .187 LONG IN FILLET RADIUS OF FWD FLANGE. 2 L 7 3 4F A22WE 1996030100196 19960301 00196 NM 1996 3 1 96FEA00323 1 19960222 A 5330 SKIN BOEING 727 72722 1384002 NM BS 945 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 GOUGE IN EXTERIOR SKIN BS 945 STR 9R. 2 L 7 3 4F A3WE 1996030100197 19960301 00197 WP 1996 3 1 ABXA9600196 1 19960221 A 7120 99581545 MOUNT STRAP DOUG DC9 DC932 3022066 WP NR 1 ENGINE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 NR 1 ENGINE, REAR ENGINE MOUNT CRACKED OFF BETWEEN VIBRATION ISOLATOR AND FUSELAGE. REPLACED CRACKED MOUNT STRAP PER SR M 51-50-1 AND 51-30-5. 2 L 7 2 4F A6WE 1996030100198 19960301 00198 1996 3 1 ARWA9602001 4 19960224 A 2211 2588787904 COMPUTER DOUG DC8 DC862 3021970 WP COCKPIT MALFUNCTIONED A ARWA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 SO 19 1803 45895 YAW DAMPER SWERVED AIRCRAFT, RETURNED TO MIAMI. YAW DAMPER AT 37,000, SEVERE INFLIGHT UPSET, LEFT DEFLECTION. ACCOMPLI SHED WIRING CONTINUITY AND INTEGRITY CHECK OF THE TRANSFER VALVE AND POSITION SENSOR FROM YAW CHANNEL TO RUDDER PACKAGE. REPLACED YAW COMPUTER AND ACCOMPLISHED A/P BITE TEST IAW MM 22-1-00, OPS CHECKED NORMAL. 2 L 7 4 4F 4A25 1996030100199 19960301 00199 NM 1996 3 1 DL72L960417 1 19960222 A 5330 SKIN BOEING 727 727232 1384082 NM PAX DOOR CUTOUT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 514DA 21430 A 1.5 INCH CRACK AT MAIN ENTRY DOOR CUTOUT, OUTER SKIN AT UPPER HINGE CUTOUT. FOUND AT A-2 LTR CHECK. REPAIRED PER MM 53-30-0 PG 11. 2 L 7 3 4F A3WE 1996030100200 19960301 00200 NM 1996 3 1 DL72L960418 1 19960222 A 5720 MOUNT BRACKET BOEING 727 727232 1384082 NM RT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 503DA 21305 FOUND DURING D-1 LETTER CHECK, .375 INCH CRACK AT NR 6 L/E FLAP ACTUATOR MOUNT BOX UPPER O/B CORNER. REPAIRED PER M/M 5 7-20-21 PG 811. 2 L 7 3 4F A3WE 1996030100202 19960301 00202 NM 1996 3 1 DL72S960427 1 19960223 A 5320 ANGLE BOEING 727 727232 1384082 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 517DA 21433 CORROSION AT UPSTOP ANGLE FWD OF FWD HINGE ACCESS PNL 3348L. REPAIRED BEAM PER M/M 53-30-1. 2 L 7 3 4F A3WE 1996030100203 19960301 00203 NM 1996 3 1 DL72S960428 1 19960223 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 2 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 517DA 21433 NR 2 L/E SLAT COVE SKIN ANGLE IS CRACKED UNDER TAI DUCT. REPAIRED PER MM 57-54-0 PAR 5A. 2 L 7 3 4F A3WE 1996030100204 19960301 00204 NM 1996 3 1 DL72S960429 1 19960223 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 3 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 517DA 21433 NR 3 L/E SLAT COVE SKIN ANGLE CRACKED UNDER TAI DUCT. REPAIRED PER MM 57-54-0 PAR 5A. 2 L 7 3 4F A3WE 1996030100205 19960301 00205 NE 1996 3 1 DL72S960431 2 19960224 A 7320 714810 P/D VALVE BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE LEAKING A DALA O OTHER X ENGINE FLAMEOUT AP APPROACH 1 SO 27 495DA 21075 696642 DESCENDING INTO ROC, NR 2 ENG FAILED/FLAME-OUT. ATTEMPTED RESTART NOT SUCCESSFUL. PRIOR TO DESCENT NR 2 FUEL FLOW 1,00 0 LBS HIGHER THAN OTHERS AND IT USED 1,000 LBS MORE DURING FLT. FOUND FUEL LEAK AT P AND D VLV. REPLACED PACKING, RAN ENGINE AND LEAK CHECK GOOD. 2 L 7 3 4F 4 F A3WE E2EA 1996030100206 19960301 00206 NM 1996 3 1 DL733960430 1 19960224 A 3260 TARGET BOEING 737 737347 1384647 NM NLG RUSTED A DALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 27 3301 23181 NOSE GEAR DOWN AND LOCKED LIGHT WOULD NOT IND GREEN ON EXT OF GEAR. FOUND LOCK SENSOR TARGET BENT UP ABOVE SENSOR. REP LACED RUSTED SPRING RETAINER BOLTS, PERFORMED NLG RETRACTION AND GEAR OPS NORMAL. 2 L 7 2 4F RT A16WE 1996030100207 19960301 00207 NM 1996 3 1 DL767960423 1 19960223 A 2130 PRESS SYST BOEING 767 767232 1385132 NM GE CF6 CF680A 30025 NE CABIN MALFUNCTIONED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 111DN 22223 725403 AIRCRAFT WOULD NOT PRESSURIZE ON CLIMBOUT. INSPECTED AIRCRAFT ON ARRIVAL, NO DOORS OR SERVICE DOORS OPEN. FOUND EQUIPM ENT COOLING VALVES OPEN, RESEQUENCED EQUIPMENT COOLING VALVES AND LOCKED OUT PER MEL 21-58-06. AIRCRAFT PRESSURIZED NOR MALLY. 2 L 7 2 4F 4 F RT A1NM E13NE 1996030100208 19960301 00208 NE 1996 3 1 DLM88960419 2 19960222 A 7200 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE FAILED A DALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 27 909DL 49540 718154 DURING CLIMBOUT, 15,000 FT IN CLEAR SMOOTH AIR AND STEADY CLIMB POWER SETTING LT ENG POPPED LOUDLY AND VIBRAT ED. POWER WAS REDUCED, RETURNED TO DFW. A BURNT OIL SMELL WAS REPORTED IN CABIN AFTER THE COMPRESSOR STALL. ENGINE WA S REPLACED AND ROUTED TO SHOP. 2 L 7 2 4F 4 F RT A6WE E9NE 1996030100209 19960301 00209 NM 1996 3 1 DLM88960420 1 19960223 A 2910 HYD LINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE CHAFED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 962DL 49981 725403 LOST RIGHT HYD PRESSURE IN FLIGHT, THEN QTY SYSTEM TURNED OFF AND ALT GEAR EXT USED. FOUND RIGHT ENGINE HYD PRESSURE L INE CHAFED AT PLYON ATTACH ANGLE. REPLACED SAME. 2 L 7 2 4F 4 F RT A6WE E9NE 1996030100210 19960301 00210 NM 1996 3 1 DLM88960425 1 19960223 A 2910 PACKING 31914912 DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE LT HYD SYST LEAKING A DALA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 955DL 49886 718225 LEFT HYD SYS FAILURE, QTY DECREASED TO 4 QTS. COMPLIED WITH PROCEDURES, LEFT ENG HYD PUMP OFF, QTY TO 17 QTS BUT NO LEF T HYD PRESS. FOUND LEFT SYSTEM HYD FWD FILTER UNION OF ENG HIGH PRESS MOD LEAKING. REPLACED UNION PACKING, LEAK CHECK OK. 2 L 7 2 4F 4 F RT A6WE E9NE 1996030100211 19960301 00211 NM 1996 3 1 MWEA96047 1 19960224 A 5230 SKIN DOUG MD88 MD88 3023688 NM AFT CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 DURING C-CHECK, FOUND AFT CARGO DOOR SKIN CRACKED NEXT TO DOOR HANDLE CUTOUT. MAINTENANCE INSTALLED DOUBLER REPAIR IAW SRM 52-05 FIG 30. 2 L 7 2 4F RT A6WE 1996030100212 19960301 00212 NM 1996 3 1 P5CA9600148 1 19960223 A 5730 65B1534017 PANEL BOEING 747 747124 1384874 NM WS 1116 MISSING A P5CA K NONE O OTHER CR CRUISE 1 WP 23 855FT 19733 UPPER WING PANEL DEPARTED IN FLIGHT, CONTINUED WITHOUT ANY DIFFICULTIES. MISSING PANEL LOCATION, INBOARD OF LEADING EDG E STA 1116, APPROX 3 FT BY 4 FT. ALL FASTENERS STILL INSTALLED. TEMPORARY PANEL FABRICATED FOR FERRY FLIGHT TO NEW YOR K. PANEL REPLACED IN NEW YORK IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996030100213 19960301 00213 NM 1996 3 1 P5CA9600149 1 19960224 A 5730 65B115004 PANEL BOEING 747 747122 1384872 NM WS 294.62 DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 ON WALKAROUND FOUND RT PANEL LOWER WING MOST FORWARD BETWEEN WBL1500 WS 294.620 DELAMINATED. APPEARS TO HAVE BEEN CAUSE D BY POWER UNIT PLACED UNDER WING. REPLACED PANEL IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996030100214 19960301 00214 NM 1996 3 1 UPS205568 1 19960224 A 5210 507945152 SUPPORT BOEING 727 727247 138408F NM PAX DOOR CRACKED A IPXA K NONE O OTHER CL CLIMB 1 SO 01 210UP 21687 CREW REPORTED, AFTER TAKEOFF LOUD AIR LEAK COMING FROM FWD ENT DOOR. FOUND CRACK AROUND A LIGHTENING HOLE SUPPORT AREA FOR TORQUE TUBE LATCH ARM FWD UPPER CORNER OF DOOR. NO TYPICAL SRM REPAIR ADDRESSING EITHER REPLACING THE DOOR OR AN EO FOR REPAIR. 2 L 7 3 4F A3WE 1996030100215 19960301 00215 WP 1996 3 1 UPS205570 1 19960222 A 3350 LIGHT DOUG DC8 DC871F 302199D WP COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 213UP 45950 MAINTENANCE REPORTED, COCKPIT EMERGENCY EXIT LIGHT LOOSE. COCKPIT EMERGENCY EXIT LIGHT SECURING CLAMPS ADJUSTED ASSY RE SECURED AND TESTED SERVICEABLE AS PER MM 33-50-01. 2 L 7 4 4F RT 4A25 1996030100216 19960301 00216 WP 1996 3 1 UPS805569 1 19960223 A 3350 LIGHT DOUG DC8 DC871F 302199D WP CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 750UP 45950 MAINTENANCE REPORTED, EMERGENCY EXIT LIGHT SWITCH LEFT ON, LOW VOLTAGE. REPLACED BATTERY PACK, OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 1996030100217 19960301 00217 EU 1996 3 1 WWMA9600024 1 19960225 A 2611 7211121000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU LAVATORY DEFECTIVE A WWMA O OTHER N FALSE WARNING CR CRUISE 1 WP 15 339SB 340B339 THE LAV SMOKE LIGHT ILLUMINATED, NO SMOKE WAS DETECTED. MAINTENANCE REPLACED THE LAV SMOKE DETECTOR AND RELEASED THE AI RCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 1996030100232 19960301 00232 EU 1996 3 1 9604713237 1 19960226 A 3350 321454 EPSU AIRBUS 320 A320211 3930320 EU CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 337NW 12406 7316 358 DURING LINE CHECK, THE EPSU FAILED INT LOAD TEST. REPLACED EPSU AND OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996030100233 19960301 00233 NM 1996 3 1 9604726307 1 19960223 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 667US 24222 DURING LINE CHECK, FOUND EMERGENCY FLOOR PATH LIGHTS INOPERATIVE ON THE LEFT SIDE FROM ROWS 51 TO 55. RECONNECTED WIRE AND OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1996030100234 19960301 00234 NM 1996 3 1 9604736622 1 19960224 A 3350 BATTERY PACK BOEING 747 747251B 1384892 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 622US 21704 DURING LINE CHECK, FOUND EMERGENCY FLOOR PATH LIGHTS INOPERATIVE IN ALL ZONES. REPLACED FIVE BATTERIES AND OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996030100235 19960301 00235 NM 1996 3 1 9604746611 1 19960223 A 3350 POWER SUPPLY BOEING 747 747251B 1384892 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 611US 20356 DURING LINE CHECK, FOUND 'A' ZONE EMERGENCY FLOOR PATH LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERIES. 2 L 7 4 4F A20WE 1996030100236 19960301 00236 NE 1996 3 1 9604759753 2 19960223 A 7261 OIL FILTER DOUG DC9 DC941 302207N WP PWA JT8 JT8D11 52044 NE NR 2 ENGINE DIRTY A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 753NW 47117 676250 NR 2 ENGINE OIL FILTER CLOG WARNING LIGHT ILLUMINATED ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNE D TO THE GATE. CARBON CONTAMINATION WAS FOUND IN THE OIL FILTER. MAINTENANCE REPLACED THE FILTER AND SUBSEQUENT RUNUP WAS SATISFACTORY. 2 L 7 2 4F 4 F A6WE E2EA 1996030100237 19960301 00237 NE 1996 3 1 9604769924 2 19960222 A 7321 FUEL CONTROL DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9 52048 NE NR 1 ENGINE FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 926RC 47473 666323 NR 1 ENGINE EPR INDICATION WAS BELOW TARGET ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE G ATE. MAINTENANCE REPLACED THE FUEL CONTROL UNIT WITH A SERVICEABLE COMPONENT. SUBSEQUENT RUNUP WAS SATISFACTORY. 2 L 7 2 4F 4 F A6WE E2EA 1996030100238 19960301 00238 NE 1996 3 1 9604779908 2 19960222 A 7320 PT2 PROBE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7B 52053 NE NR 1 ENGINE MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 01 958N 47254 657610 NR 1 EPR INDICATION WAS ERRATIC DURING CLIMB AND CRUISE. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENAN CE REPLACED THE INLET NOSE BULLET/PT2 PROBE WITH A SERVICEABLE UNIT AND SYSTEM OPERATION RETURNED TO NORMAL. 2 L 7 2 4F 4 F A6WE E2EA 1996030100239 19960301 00239 1996 3 1 9604789938 4 19960223 A 2565 113317 SLIDE DOUG DC9 DC931 3022065 WP SVC DOOR LOW PRESSURE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 1798U 26006 6158 47369 DURING PERIODIC CHECK, FOUND FORWARD SERVICE DOOR EVACUATION SLIDE LOW ON PRESSURE. REPLACED SLIDE. 2 L 7 2 4F A6WE 1996030100240 19960301 00240 WP 1996 3 1 9604799942 1 19960226 A 3350 6014113 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 3991C 47175 DURING LINE MAINTENANCE INSPECTION, FOUND MID TO AFT CABIN EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE. REPLACED BATTERY PACKS AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996030100241 19960301 00241 WP 1996 3 1 9604809958 1 19960226 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP TAILCONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 917RW 47145 DURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE CATWALK EMERGENCY LIGHTS INOPERATIVE. REPAIRED BROKEN WIRE AND OPERA TIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996030100242 19960301 00242 WP 1996 3 1 9604819912 1 19960226 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP TAILCONE DISCHARGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 962N 47406 DURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE EMERGENCY EVACUATION LIGHTS INOPERATIVE. REPLACED BATTERIES AND OPER ATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996030100243 19960301 00243 WP 1996 3 1 9604829178 1 19960223 A 3350 LIGHT DOUG DC9 DC914 3022034 WP TAILCONE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 331OL 45705 DURING LINE CHECK, FOUND AFT TAILCONE EMERGENCY FLOOR PROXIMITY LIGHTS INOPERATIVE. REPLACED AFT TAILCONE FLOOR PROXIMI TY LIGHT ASSEMBLY AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996030100244 19960301 00244 WP 1996 3 1 9604839851 1 19960223 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 760NC 47708 DURING LINE CHECK, FOUND CABIN OVERHEAD EMERGENCY LIGHTS STA 400 TO 550 INOPERATIVE. REPLACED POWER SUPPLY AND OPERATIO NAL CHECK GOOD. 2 L 7 2 4F A6WE 1996030100245 19960301 00245 WP 1996 3 1 ARWA9602002 1 19960227 A 5330 SKIN DOUG DC8 DC863F 302198F WP FS 1783 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 DURING PREFLIGHT INSPECTION, FOUND LEVEL 2 CORROSION ON FUSELAGE TAIL SECTION PLATING AT FS 1783, L17L. CUT OUT DAMAGED AREA, FABRICATED, INSTALLED FILLER AND DOUBLER IAW SRM 53-2-1 FIG 7, PG 115 AND 116. CLASS 3 REPAIR TO BE REPLACED BEF ORE 6,000 LANDINGS. 2 L 7 4 4F 4A25 1996030100246 19960301 00246 NM 1996 3 1 VSTA9602002 1 19960222 A 8010 MS250081 SWITCH BOEING 737 737284 138448R NM START LEVER FAILED A VSTA K NONE O OTHER NR NOT REPORTED 1 WP 07 310VA 21501 NR 1 ENGINE WOULD NOT START. FOUND BAD SWITCH IN THROTTLE QUAD. REMOVED AND REPLACED START SWITCH IN QUAD. 2 L 7 2 4F A16WE 1996030100248 19960301 00248 WP 1996 3 1 96ZZZM216 1 19960124 A 5311 BELT RING DOUG DC9 DC931 3022065 WP BS 718 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 991Z 47096 STL - DURING C-CHECK, FOUND .5 INCH CRACK AT BOTH ATTACH POINTS TO BELTRING, LONGERON 6R, STATION 718. REPAIRED PER SRM 53-02, FIGURE 2A. 2 L 7 2 4F A6WE 1996030100249 19960301 00249 WP 1996 3 1 96ZZZM217 1 19960124 A 5313 LONGERON DOUG DC9 DC931 3022065 WP FS 737 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 991Z 47096 STL - DURING C-CHECK, FOUND ONE 2 INCH CRACK IN LONGERON 4L, LOWER LEG, STATION 737. REPAIRED PER SRM 53-02, FIGURE 2A. 2 L 7 2 4F A6WE 1996030100251 19960301 00251 WP 1996 3 1 96ZZZM219 1 19960124 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 699 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 991Z 47096 STL - DURING C-CHECK, FOUND .5 INCH CRACK IN LOWER FLANGE OF LONGERON 7L, STATION 699. REPAIRED PER SRM 53-02, FIGURE 2 A. 2 L 7 2 4F A6WE 1996030100253 19960301 00253 NM 1996 3 1 96ZZZM221 1 19960114 A 5755 651734781A SPOILER BOEING 727 727231 1384079 NM NR 12 DELAMINATED A TWAA O OTHER E VIBRATION/BUFFET CR CRUISE 1 CE 05 54331 20309 STL - DURING CRUISE, NR 12 FLIGHT SPOILER, MFG P/N 65-17347-81A, DELAMINATED CAUSING EXTREME AIRFRAME BUFFETING. REMOVE D AND REPLACED NR 12 FLIGHT SPOILER AND RIGGED. OPERATIONAL CHECK NORMAL. 2 L 7 3 4F A3WE 1996030100259 19960301 00259 WP 1996 3 1 96ZZZM227 1 19960122 A 2913 314195 HYDRAULIC PUMP DOUG DC9 DC932 3022066 WP NR 2 ENGINE FAILED A VJ6A A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 11 915VV 47443 ON FLT NR 511 - ATL-ATL - AIR RETURN, THE RIGHT HYDRAULIC PRESSURE INDICATED ZERO IN FLIGHT. THE RIGHT ENGINE DRIVEN HY DRAULIC PUMP SHAFT WAS SHEARED. THE PUMP WAS REPLACED. (M) 2 L 7 2 4F A6WE 1996030100260 19960301 00260 WP 1996 3 1 96ZZZM228 1 19960131 A 3231 39552501 SEQUENCE ARM DOUG DC9 DC932 3022066 WP MLG DOOR BROKEN A VJ6A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 919VV 47260 ON FLT 549 - ATL-ATL - AIR RETURN, ON TAKEOFF THE LEFT GEAR UNSAFE AND GEAR DOOR WARNING LIGHTS ON. RECYCLED GEAR AND G OT THREE GREEN WITH GEAR DOORS CLOSED. FOUND LEFT MLG DOOR SEQUENCE ARM BROKEN, REPLACED ARM AND PERFORMED MLG MECHANIC AL CONTROL PUSH PULL CABLE RIG CHECK PER MM 52-31-0 PARA 3B. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1996030100261 19960301 00261 WP 1996 3 1 96ZZZM229 1 19960119 A 2150 WWD148 CLAMP DOUG DC9 DC932 3022066 WP RT ACM BROKEN A VJ6A A UNSCHED LANDING O OTHER CL CLIMB 1 SO 11 904VJ 47377 ON FLT NR 116 - ATL-ATL - AIR RETURN, RIGHT PACK INOP AFTER TAKEOFF, NO PRESSURE INDICATION OR AIR FLOW. FOUND CLAMP LO OSE ON RIGHT ACM AND BROKEN CLAMP ON RIGHT WATER SEPARATOR. SECURED LOOSE CLAMP ON ACM AND INSTALLED CLAMP ON WATER SEP ARATOR. PRESSURIZATION AND AIR CONDITIONING OPS CHECK NORMAL. (M) 2 L 7 2 4F A6WE 1996030100272 19960301 00272 NM 1996 3 1 96ZZZM240 1 19960111 A 5315 FLOOR BEAM BOEING 747 747131 1384881 NM FS 480 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 93108 19674 MCI - DURING OP-16, FOUND CORROSION ON FLOOR BEAM CAP, FS 480, RIGHT SIDE. REMOVED CORROSION PER SRM 51-10-01 AND REPAI RED PER ARA 9622. 2 L 7 4 4F A20WE 1996030100273 19960301 00273 WP 1996 3 1 96ZZZM241 1 19960128 A 3222 A03772REVH SEAL DOUG DC9 DC982 3022082 WP NLG FAILED A TWAA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 950U 49230 STL - AFTER TAKEOFF, NOSE GEAR FAILED TO RETRACT, IT WAS DETERMINED THAT THE NOSE GEAR WAS DOWN AND LOCKED. REMOVED AND REPLACED NOSE GEAR SEAL KIT, MFG P/N A03772REVH. GEAR SWING CHECKED NORMAL. 2 L 7 2 4F A6WE 1996030100274 19960301 00274 WP 1996 3 1 96ZZZM242 1 19960109 A 2820 4TL623 SWITCH DOUG DC9 DC982 3022082 WP CTR FUEL TANK FAILED A TWAA O OTHER J WARNING INDICATION CR CRUISE 1 CE 05 956U 49701 MCI - DURING CRUISE, CREW WAS UNABLE TO TRANSFER FUEL OUT OF THE CENTER TANK. REMOVED AND REPLACED WORN CENTER BOOST PU MP ON-OFF SWITCH, MFG P/N 4TL62-3. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996030100275 19960301 00275 NM 1996 3 1 96ZZZM243 1 19960116 A 5270 AIRSTAIR LIGHT BOEING 727 727231 1384079 NM COCKPIT ILLUMINATED A TWAA O OTHER N FALSE WARNING CR CRUISE 1 CE 05 64320 20053 SAT - FLT 199 - DURING CRUISE, AFT AIRSTAIR LIGHT ILLUMINATED IN COCKPIT. REMOVED UPLOCK OVERCENTER BUNGEE, CLEANED AND LUBRICATED AND REINSTALLED, CHECKED CABLE RIG, ADJUSTED SWITCH STRIKERS AND PERFORMED UPLATCH MECHANISM CHECK. OPERATI ON NORMAL. CHECK C-4 - 10-25-95 - MCI. 2 L 7 3 4F A3WE 1996030100280 19960301 00280 WP 1996 3 1 96ZZZM248 1 19960110 A 2612 898005 FIRELOOP LKHEED 1011 10113851 5265010 WP NR 2 ENGINE FAILED A TWAA E ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 CE 05 31008 193B1028 BOS - DURING DESCENT SHUT DOWN NR 2 ENGINE, S/N 4422, DUE TO FIREWARNING. FOUND LOWER ZONE 1 AFT DETECTOR LOOP, MFG P/N 898005, SHORTED. REPLACED DETECTOR LOOP AND PERFORMED HIGH POWER ENGINE RUN AND OPERATION CHECKED NORMAL. 2 L 7 3 4F A23WE 1996030100281 19960301 00281 NM 1996 3 1 96ZZZM249 1 19960127 A 3234 574205 SELECTOR VALVE DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A MALA O OTHER O OTHER AP APPROACH 1 GL 15 817MA 249 FLT NR 3231 - DURING APPROACH TO BJI, THE GEAR WAS VERY SLOW TO EXTEND WHEN SELECTED DOWN. THE AIRCRAFT CONTINUED TO BJ I AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE LANDING GEAR SELECTOR, P/N 535201-1, AND THE SELECTOR VALVE, P/N 57420-5. ALL SYSTEMS OPERATED SATISFACTORILY. REFERENCE MALA964845. 2 H 7 2 4T RT A13NM 1996030100305 19960301 00305 WP 1996 3 1 AALA960003 1 19960102 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1139 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 161AA 46942 FOUND CORROSION UNDER S/S STRAP AND SKIN AT STATION 1139 BETWEEN LONGERON 43L AND 46L. MANUFACTURED AND INSTALLED PER S RM 53-20-00 PG 81-82-71-72 CLASS 3 REPAIR. (M) 2 L 7 3 4F A22WE 1996030100308 19960301 00308 WP 1996 3 1 AALA960006 1 19960102 A 5320 CUSP DOUG DC9 DC982 3022082 WP BS 1174 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 276AA 49273 TULE - FOUND CORROSION ON BOTTOM OF CUSP. INSTALLED DOUBLER PER SRM 53-01 FIG 4 SHEET 3 PAGE 17. (M) 2 L 7 2 4F A6WE 1996030100309 19960301 00309 WP 1996 3 1 AALA960007 1 19960102 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 203 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 276AA 49273 TUL - FOUND NR 5 SEAT TRACK HAS CORROSION ON LUG. SPLICED IN NEW SECTION OF SEAT TRACK FROM STATION 200 TO STATION 323, PER SRM 53-05 FIG 4 AND 1. (M) 2 L 7 2 4F A6WE 1996030100311 19960301 00311 NM 1996 3 1 AALA960009 1 19960103 A 3397 WIRE BOEING 767 767223 1385123 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 339AA 22336 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT FORWARD CROSS AISLE INOPERATIVE. REPAIRED BROKEN EMERGENCY EXIT LIGHT WIRE AT FORWARD CROSS AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1996030100312 19960301 00312 NM 1996 3 1 AALA960012 1 19960102 A 5711 FITTING BOEING 727 727223 1384074 NM RT REAR SPAR OVERSIZED HOLES A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 864AA 21369 TULE - FOUND FITTING RIGHT WING REAR SPAR CENTER SECTION TO OUTBOARD SPLICE TWO FASTENER HOLES. OVERSIZED HOLES INSTALL ED BUSHINGS REINSTALLED BOLTS ESO116797 DATED 12-22-95 TO BE COMPLETED PER AA REQUEST FOR SERVICE WITHIN 6000 CYCLES OR NEXT N/C. (M) 2 L 7 3 4F A3WE 1996030100313 19960301 00313 NM 1996 3 1 AALA960013 1 19960102 A 5320 STIFFENER BOEING 727 727223 1384074 NM FS 1183 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 864AA 21369 TULE - FOUND VERTICAL STIFFENER CRACKED IN RADIUS AT LOWER END FORWARD SIDE OF STATION 1183 WEB RBL 8 WL 188. STOP DRIL LED CRACK AND INSTALLED DOUBLER PER SIB 727-53-0175 DATED 10-22-87 REVISED 3-25-93. (M) 2 L 7 3 4F A3WE 1996030100316 19960301 00316 EU 1996 3 1 AALA960025 1 19960109 A 2913 862536 PUMP VICKERS FOKKER F28 F28MK0100 4990807 EU NR 1 ENGINE DEFECTIVE A AALA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 1436A HG24230 11426 JFK - FLT NR 1072 - EN ROUTE YYZ/JFK - DURING CRUISE, LOST SYSTEM 1 HYDRAULIC QUANTITY WITH PRESSURE DROPPING TO 500 PSI AND QUANTITY AT 35. SYSTEM 2 PRESSURE AND QUANTITY NORMAL. ACCOMPLISHED QRH PROCEDURES FOR NR 1 HYDRAULIC SYSTEM AND AIRCRAFT PROCEEDED TO JFK. ACCOMPLISHED ALTERNATE LANDING GEAR EXTENSION AND ALTERNATE FLAP EXTENSION AND AIRCRAFT LAND ED JFK WITHOUT INCIDENT. REPLACED NR 1 ENGINE HYDRAULIC PUMP AND SERVICED SYSTEM. ACCOMPLISHED LEAK AND GROUND CHECK W ITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1996030100317 19960301 00317 EU 1996 3 1 AALA960026 1 19960109 A 3350 A3060719102 STRIP AIRBUS 300 A300B4605R 3930308 EU CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 70072 515 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT STRIP MISSING AT RIGHT AISLE FROM PAX SEAT ROW 29H AFT. REPLACED EM ERGENCY FLOOR LIGHT STRIP AT RIGHT AISLE FROM PAX SEAT ROW 29H AFT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996030100318 19960301 00318 WP 1996 3 1 AALA960027 1 19960109 A 3350 A3060719102 STRIP DOUG DC10 DC1010 3022110 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 160AA 46710 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PAX SEAT ROW 18C INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT ST RIP BY PAX SEAT ROW 18C. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A22WE 1996030100319 19960301 00319 WP 1996 3 1 AALA960028 1 19960109 A 3350 A3030398101 CONNECTOR DOUG DC10 DC1010 3022110 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 160AA 46710 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PAX SEAT ROW 11C INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR L IGHT CONNECTOR BY PAX SEAT ROW 11C. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A22WE 1996030100320 19960301 00320 NM 1996 3 1 AALA960033 1 19960110 A 3350 A3030398101 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 652AA 24610 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 10 THROUGH 18 INOPERATIVE. RESECURED LOOSE E MERGENCY FLOOR LIGHT CONNECTOR BY PAX SEAT ROW 10. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1996030100327 19960301 00327 EU 1996 3 1 AALA960043 1 19960111 A 3350 STRIP AIRBUS 300 A300B4605R 3930308 EU CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 3075A 606 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT STRIP BETWEEN PAX SEAT ROWS 8B THROUGH 13B MISSING. REPLACED EMERGE NCY FLOOR LIGHT STRIP BETWEEN PASSENGER SEAT ROWS 8B THROUGH 13B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996030100328 19960301 00328 NM 1996 3 1 AALA960046 1 19960108 A 5314 145T8611 KEEL BEAM BOEING 767 767223 1385123 NM BS 795 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 301AA 22307 AFW - FOUND CORROSION ON KEEL BEAM BEYOND SRM LIMITS AFTER BLEND OUT. FLAP PEENED AND REFINISHED AREA. KEEL BEAM IS SA TISFACTORY FOR CONTINUED SERVICE WITH NOTED CONDITION PER MRB 767-1105. (M) 2 L 7 2 4F RT A1NM 1996030100329 19960301 00329 EU 1996 3 1 AALA960049 1 19960112 A 3350 STRIP AIRBUS 300 A300B4605R 3930308 EU CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14056 463 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT STRIP BETWEEN PAX SEAT ROWS 15B THROUGH 21B MISSING. REPLACED MISSI NG EMERGENCY FLOOR LIGHT STRIP BETWEEN PAX SEAT ROWS 15B THROUGH 21B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996030100330 19960301 00330 WP 1996 3 1 AALA960054 1 19960115 A 5312 591013061 BLKHD DOUBLER DOUG DC9 DC982 3022082 WP BS 1338 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 258AA 49288 TUL - FOUND CORROSION ON SPADE PLATE, FORWARD FACE OF PRESSURE BULKHEAD STRINGER 1338 LONGERON 30. INSTALLED NEW SPADE PLATE ON FORWARD FACE OF AFT PRESSURE BULKHEAD. (M) 2 L 7 2 4F A6WE 1996030100331 19960301 00331 WP 1996 3 1 AALA960060 1 19960115 A 5320 5936597509 SUPPORT DOUG DC9 DC982 3022082 WP BS 1212 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 285AA 49297 TULE - FOUND CORROSION ON FLOOR BOARD SUPPORT IN AFT CARGO COMPARTMENT AT STATION 1212, WHERE BOLTED TO RIGHT FRAME. IN STALLED NEW FLOOR BOARD SUPPORT. (M) 2 L 7 2 4F A6WE 1996030100332 19960301 00332 WP 1996 3 1 AALA960066 1 19960116 A 3231 RETRACT MECH DOUG DC9 DC982 3022082 WP NLG DOOR MALFUNCTIONED A AALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 07 203AA 49145 SJC - FLT NR 812 - AFTER TAKEOFF AND LANDING GEAR RETRACTION OUT OF SJC, NOISE AND VIBRATION NOTED IN COCKPIT FROM NOSE WHEEL AREA. NOISE AND VIBRATION CEASED WHEN LANDING GEAR EXTENDED AND AIRCRAFT RETURNED TO SJC, LANDING WITHOUT INCIDEN T. CHECK OF AIRCRAFT AFTER RETURN TO GATE REVEALED RIGHT NOSE LANDING GEAR DOOR OPEN. CHECKED NOSE LANDING GEAR DOOR H INGES, LATCH MECHANISM AND LINKAGES WITH NO DEFECTS FOUND. ACCOMPLISHED NOSE LANDING GEAR RETRACTION CHECK WITH NO DEFE CTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996030100333 19960301 00333 WP 1996 3 1 AALA960072 1 19960116 A 5320 BRACKET DOUG DC9 DC982 3022082 WP BS 636 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 258AA 49288 TUL - FOUND ANGLE FORWARD BOTTOM CORNER HAS CORROSION MID CARGO DOOR CUTOUT. INSTALLED NEW CORNER BRACKET IN FORWARD BO TTOM CORNER OF MID CARGO DOOR CUTOUT. (M0 2 L 7 2 4F A6WE 1996030100334 19960301 00334 WP 1996 3 1 AALA960073 1 19960116 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 1212-1231 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 258AA 49288 TUL - FOUND LONGERON 25R IS CORRODED FROM STATION 1212-1231. CUT OUT 19 INCHES OF CORRODED LONGERON. INSTALLED NEW PIE CE OF LONGERON AND LONGERON SPLICE PER SRM 53-02 FIG 5. (M) 2 L 7 2 4F A6WE 1996030100335 19960301 00335 WP 1996 3 1 AALA960074 1 19960116 A 5320 DOOR JAMB DOUG DC9 DC982 3022082 WP BS 1155-1212 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 258AA 49288 TUL - FOUND CORROSION LOWER DOOR JAMB, STATION 1155 TO STATION 1212. REPAIRED PER ESO 80559, DATED 1-11-96 AND AARD 53- 10-00-3. (M) 2 L 7 2 4F A6WE 1996030100336 19960301 00336 NM 1996 3 1 AALA960075 1 19960108 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM FS 600 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 898AA 22014 TUL - FOUND CORROSION ON SHEAR TIE STATION 600 BETWEEN STRINGER 26L AND 27L. REMOVED CORROSION ON SHEAR TIE BEYOND LIMI TS. REPLACED SHEAR TIE PER SRM 53-10-1. (M) 2 L 7 3 4F A3WE 1996030100337 19960301 00337 NM 1996 3 1 AALA960076 1 19960118 A 5313 STRINGER BOEING 727 727223 1384074 NM FS 590-600 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 898AA 22014 FOUND CORROSION IN STRINGER 27 LEFT STATION 590 - 600. REMOVED CORROSION, CUT OUT BAD SECTION OF STRINGER AND INSTALLED STRINGER REPAIR PER SRM 53-10-3 PG 3-43. (M) 2 L 7 3 4F A3WE 1996030100338 19960301 00338 NM 1996 3 1 AALA960077 1 19960118 A 5330 SKIN BOEING 727 727223 1384074 NM FS 590-602 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 898AA 22014 TULE - FOUND CORROSION ON SKIN FS 590-602 STRINGER 26L TO 27L. REMOVED CORROSION, FOUND BEYOND LIMITS, INSTALLED REPAIR DOUBLER PER SRM 53-30-3 PGS 12-14A. (M) 2 L 7 3 4F A3WE 1996030100339 19960301 00339 WP 1996 3 1 AALA960085 1 19960117 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 258AA 49288 TUL - FOUND CORROSION ON NR 2 SEAT TRACK AT STATION 1200. INSTALLED NEW SEAT TRACK PER SRM 53-05 FIG 43, STATION 1185 T O STATION 1305. (M) 2 L 7 2 4F A6WE 1996030100341 19960301 00341 WP 1996 3 1 AALA960087 1 19960119 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 256-797 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 258AA 49288 TULE - FOUND CORROSION AT SEAT TRACK NR 6, STATION 256 TO STATION 797. REMOVED AND REPLACED SEAT TRACK NR 6 BETWEEN STA TION 256 AND STATION 797. (M) 2 L 7 2 4F A6WE 1996030100342 19960301 00342 NM 1996 3 1 AALA960095 1 19960122 A 5713 STRINGER BOEING 727 727223 1384074 NM WS 629 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 6819 19494 TULE - FOUND NR 2 STRINGER AFT RIB ATTACH ANGLE (STRINGER NR 13) STATION WS 629 CRACKED. REPAIRED STRINGER PER SB 727-5 7A159. (M) 2 L 7 3 4F A3WE 1996030100343 19960301 00343 NM 1996 3 1 AALA960096 1 19960122 A 5712 6516253951 RIB BOEING 727 727223 1384074 NM WS 601.5 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 6819 19494 TULE - FOUND LOWER RIB CHORD CRACKED AT STRINGER 5 AT STATION 601.5 INSIDE RIGHT WING FUEL TANK. REMOVED RIB AND INSTAL LED NEW BUILT UP RIB PER SB 727-57-0127 FOR STATION 601.5R. COVER PLATE ON ES8 1517971. (M) 2 L 7 3 4F A3WE 1996030100344 19960301 00344 NM 1996 3 1 AALA960097 1 19960122 A 5712 RIB BOEING 727 727223 1384074 NM WS 738.5 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 6819 19494 TULE - FOUND CRACK IN RADIUS OF LOWER RIB CHORD WING STATION 738.5 RIGHT WING (FWD CHORD) IN FUEL TANK. STOP DRILLED BO TH ENDS OF CRACK, NDT CHECKED BOTH STOP DRILLS. INSTALLED DOUBLER PER SRM 57-10-5 PAGE NR 4. (M) 2 L 7 3 4F A3WE 1996030100345 19960301 00345 WP 1996 3 1 AALA960098 1 19960118 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP BS 1022-1155 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 258AA 49288 TULE - FOUND RIGHT TIEDOWN TRACK CORRODED AT EACH MOUNT SCREW HEAD. REMOVED CORRODED RIGHT TIEDOWN TRACK AND INSTALLED NEW TRACK FROM STATION 1022-1155. (M) 2 L 7 2 4F A6WE 1996030100346 19960301 00346 WP 1996 3 1 AALA960099 1 19960118 A 5320 59360263 INTERCOSTAL DOUG DC9 DC982 3022082 WP BS 1184 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 258AA 49288 TULE - FOUND INTERCOSTAL CORROSION BEYOND REPAIR LIMITS BELOW AFT CARGO DOOR SILL. REPLACED INTERCOSTAL AT STATION 1184 OF DOOR JAMB UNDER PLATE. (M) 2 L 7 2 4F A6WE 1996030100347 19960301 00347 WP 1996 3 1 AALA960100 1 19960118 A 5320 59360263 INTERCOSTAL DOUG DC9 DC982 3022082 WP BS 1193 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 258AA 49288 TULE - INTERCOSTAL CORROSION BEYOND REPAIR LIMITS BELOW AFT CARGO DOOR SILL. REPLACED INTERCOSTAL AT STATION 1193 OF DO OR JAMB UNDR PLATE. (M) 2 L 7 2 4F A6WE 1996030100348 19960301 00348 WP 1996 3 1 AALA960101 1 19960118 A 5320 991007813 ANGLE DOUG DC9 DC982 3022082 WP BS 190 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 258AA 49288 TULE - FOUND CORROSION UNDER SCUFF PLATE OF FORWARD SERVICE DOOR OF CUSP ANGLE BEYOND REPAIR LIMITS. INSTALLED DOOR JAM B PAN AND CUSP REPAIR PER SRM 53-05 FIG 55 PG 139-145 REFER TO E58 1484568. (M) 2 L 7 2 4F A6WE 1996030100349 19960301 00349 WP 1996 3 1 AALA960102 1 19960120 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 1212 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 258AA 49288 TULE - FOUND CORROSION ON FLOOR BOARD ATTACH ANGLE FRAME STATION 1212, LONGERON 28L TO LONGERON 29R. REPLACED WITH NEW ANGLE. (M) 2 L 7 2 4F A6WE 1996030100350 19960301 00350 WP 1996 3 1 AALA960103 1 19960120 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 1271 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 258AA 49288 TULE - FOUND TEMPORARY DOUBLER INSTALLED AT STATION 1271 LONGERON 28L. INSTALLED FLASH REPAIR AND INTERNAL DOUBLER PER SRM 53-04 FIG 38 AND ESO NR 80559 DATED 1-18-96. (M) 2 L 7 2 4F A6WE 1996030100351 19960301 00351 WP 1996 3 1 AALA960104 1 19960119 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 1155-1212 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 258AA 49288 TUL - FOUND FLOOR BOARD ATTACH ANGLE CORRODED, STATION 1155 - STATION 1212. INSTALLED NEW FLOOR BOARD ATTACH ANGLE, STA TION 1136 - 1212. (M) 2 L 7 2 4F A6WE 1996030100352 19960301 00352 WP 1996 3 1 AALA960105 1 19960119 A 5313 5000675 LONGERON DOUG DC9 DC982 3022082 WP BS 1212-1231 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 258AA 49288 TUL - FOUND CORROSION STATION 1212 TO STATION 1231 LONGERON 26R AND LONGERON END FITTING. INSTALLED LONGERON SECTION AN D SPLICED PER ESO 80559 DATED 1-18-96. (M) 2 L 7 2 4F A6WE 1996030100353 19960301 00353 WP 1996 3 1 AALA960106 1 19960119 A 5320 593607022 GUSSETT DOUG DC9 DC982 3022082 WP BS 1155 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 258AA 49288 TUL - FOUND CORROSION ON GUSSET AT FORWARD CORNER OF DOOR JAMB STATION 1155. REPLACED GUSSET (SUPPORT) AT FORWARD CORNE R OF DOOR JAMB STATION 1155. (M) 2 L 7 2 4F A6WE 1996030100354 19960301 00354 WP 1996 3 1 AALA960107 1 19960119 A 5320 593607021 GUSSET DOUG DC9 DC982 3022082 WP BS 1212 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 258AA 49288 TUL - FOUND CORROSION ON GUSSET AT DOOR JAMB STATION 1212. REPLACED GUSSET (SUPPORT) AT AFT CORNER OF DOOR JAMB STATION 1212. (M) 2 L 7 2 4F A6WE 1996030100355 19960301 00355 WP 1996 3 1 AALA960108 1 19960119 A 5347 59366631 CARGO TRACK DOUG DC9 DC982 3022082 WP BS 1007-1231 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 258AA 49288 TUL - FOUND LEFT TIEDOWN TRACK CORRODED FROM STATION 1079 TO STATION 1212 WHERE IT MOUNTS TO BELL FRAMES. INSTALLED NEW TIEDOWN TRACK. (M) 2 L 7 2 4F A6WE 1996030100356 19960301 00356 WP 1996 3 1 AALA960109 1 19960121 A 5320 CUSP DOUG DC9 DC982 3022082 WP BS 1175 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 285AA 49297 TULE - FOUND CUSP CORRODED LOWER SURFACE, STATION 1175 UNDER NR 1 SEAT TRACK. INSTALLED DOUBLER PER SRM 53-01 PAGE 7 FI GURE 2 SHEET 2. (M) 2 L 7 2 4F A6WE 1996030100357 19960301 00357 WP 1996 3 1 AALA960110 1 19960122 A 5320 FLOOR CUSP DOUG DC9 DC982 3022082 WP FS 179-200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 258AA 49288 TUL - FOUND CORROSION ON FLOOR CUSP INSIDE FORWARD RIGHT SERVICE DOOR BETWEEN STATION 179 TO STATION 200. INSTALLED NEW SECTION OF CUSP AND DOUBLER PER SRM 51-01 FIG 2. (M) 2 L 7 2 4F A6WE 1996030100358 19960301 00358 WP 1996 3 1 AALA960111 1 19960122 A 5320 FLOOR CUSP DOUG DC9 DC982 3022082 WP BS 167-179 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 258AA 49288 TUL - FOUND CORROSION ON FLOOR CUSP INSIDE FORWARD RIGHT SERVICE DOOR BETWEEN STATION 167 TO 179. INSTALLED NEW SECTION OF CUSP AND DOUBLER PER SRM 53-01 FIG 2. (M) 2 L 7 2 4F A6WE 1996030100359 19960301 00359 WP 1996 3 1 AALA960122 1 19960123 A 2121 6054578 FAN DOUG DC9 DC982 3022082 WP ACM BAY DEFECTIVE A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 07 298AA 544995 49310 DFW - FLT NR 1439 - DURING APPROACH TO DFW, SMOKE WITH ELECTRICAL SMELL NOTED IN CABIN. ACCOMPLISHED CHECKLIST AND AIRC RAFT LANDED DFW WITHOUT INCIDENT. REPLACED GASPER RECIRCULATION FAN. ALSO, CHANGED ALL ACM COALESCER BAGS. ACCOMPLISH ED GROUND ENGINE RUN AND OPERATED ALL PACKS AND FANS WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M ) 2 L 7 2 4F A6WE 1996030100360 19960301 00360 WP 1996 3 1 AALA960130 1 19960124 A 3222 5920629519 STRUT PISTON DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 431AA 49343 IAD - FLT NR 151 - AFTER TAKEOFF DCA WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR DID NOT RETRACT. RECYCLED LANDING G EAR WITH SAME RESULTS. AIRCRAFT DIVERTED TO IAD AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR STRUT PISTON. SERVICED NOSE LANDING GEAR WITH OIL AND NITROGEN AND ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996030100361 19960301 00361 NM 1996 3 1 AALA960137 1 19960125 A 5320 SUPPORT DOUG MD11 MD11 3023602 NM BS 421-459 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1750B 48419 TULE - FOUND CORROSION FROM STATION 421 TO STATION 459, AT LAVATORY 3 FLOOR SUPPPORT INBOARD OF SEAT TRACK NR 7. REMOVE D AND REPLACED FLOOR BOARD SUPPORT PER SRM 53-00-01. (M) 2 L 7 3 4F RT A22WE 1996030100362 19960301 00362 WP 1996 3 1 AALA960143 1 19960128 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG REQ'D SERVICE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 457AA 49562 DFW - FLT NR 1067 - AFTER TAKEOFF DFW WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR FAILED TO RETRACT. RECYCLED LANDIN G GEAR WITH SAME RESULT. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. SERVICED NOSE LANDING GEAR STRUT WITH O IL AND NITROGEN. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERAT ION. (M) 2 L 7 2 4F A6WE 1996030100363 19960301 00363 WP 1996 3 1 AALA960147 1 19960126 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG REQ'D SERVICE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 431AA 49343 ORD - FLT NR 1046 - AFTER TAKEOFF ORD WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR FAILED TO RETRACT. RECYCLED LANDIN G GEAR WITH SAME RESULT. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. SERVICED NOSE LANDING GEAR STRUT WITH O IL AND NITROGEN AND REPLACED SCHRADER VALVE. ACCOMPLISHED NOSE LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SY STEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996030100364 19960301 00364 SO 1996 3 1 C2XA96CL002 1 19960118 A 3230 20885 UPLOCK ACTUATOR EMB 120 EMB120RT SO NLG OUT OF ADJUST A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 16719 13451 486 120138 ABE - FLT NR 3321 - AFTER TAKEOFF AND GEAR RETRACTION, THE CREW REPORTED THAT THE GEAR DOOR REMAINED OPEN. MAINTENANCE INSPECTED AIRCRAFT AND ADJUSTED THE NOSE GEAR UPLOCK ACTUATOR, MAINTENANCE ALSO CLEANED THE NOSE AND MAIN GEAR UPLOCK HO OKS. THE OPERATIONAL CHECKS WERE GOOD IAW EMB120 MM 32-32-00. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1996030100365 19960301 00365 SO 1996 3 1 C2XA96CL003 1 19960119 A 3231 12043270501 RELAY BOX EMB 120 EMB120RT SO MLG DOORS FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 16719 8760 120107 120138 CLE - FLT NR 3388 - THE CREW REPORTED THAT UPON GEAR RETRACTION THE MAIN LANDING GEAR FORWARD DOORS REMAINED OPEN. MAIN TENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE LANDING GEAR CONTROL RELAY BOX IAW EMB120MM 32-31-02. ALL O PERATIONAL CHECKS WERE GOOD IAW EMB120 MM 32-32-00. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1996030100366 19960301 00366 SO 1996 3 1 C2XA96CL004 1 19960122 A 3233 1959500007 ACTUATOR EMB 120 EMB120RT SO LT MLG OUT OF ADJUST A C2XA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 09 59708 13345 13330 281 120098 CLE - FLT NR 3338 - THE CREW REPORTED THAT AFTER TAKEOFF THE LEFT MAIN LANDING GEAR WOULD NOT RETRACT, THE GEAR WAS CYCL ED THREE TIMES WITH THE SAME RESULTS. MAINTENANCE INSPECTED AIRCRAFT AND ADJUSTED THE LEFT MAIN GEAR ACTUATOR IAW EMB 1 20MM 32-32-10, ALL OPERATIONAL CHECKS WERE GOOD IAW EMB120 MM 32-32-00. AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1996030100367 19960301 00367 SO 1996 3 1 C2XA96CL005 1 19960125 A 2750 3075001017 CONTROL UNIT EMB 120 EMB120RT SO NOSE ELEC BAY FAILED A A C2XA O OTHER F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 SW 09 47722 120166 ROC - FLT NR 3113 - CREW REPORTED THAT DURING LANDING WHEN THE FLAPS WERE SELECTED TO 15 DEGREES, THE RIGHT OUTBOARD EXT ENDED TO 10 DEGREES AND THE LEFT OUTBOARD EXTENDED TO 45 DEGREES CAUSING A FLAP ASYMMETRY. MAINTENANCE INSPECTED AIRCRA FT AND REMOVED AND REPLACED THE FLAP CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD IAW EMB120 MM 27-50-00. AIRCRAFT RELEA SED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1996030100368 19960301 00368 SO 1996 3 1 C2XA96CL006 1 19960128 A 2750 3075001017 CONTROL UNIT EMB 120 EMB120RT SO TE FLAPS FAILED A C2XA K NONE J WARNING INDICATION AP APPROACH 1 SW 09 47722 11932 120166 CLT - FLT NR 3372 - CREW REPORTED, THAT DURING APPROACH THEY RECEIVED A FLAP CONTROL FAULT, THE CREW RESET THE SYSTEM BU T RECEIVED ANOTHER FLAP CONTROL FAULTY WHEN FLAPS WERE EXTENDED TO 25 DEGREES. MAINTENANCE INSPECTED AIRCRAFT AND REMOV ED AND REPLACED THE FLAP CONTROL UNIT IAW EMB-120 MM 27-50-06. OPERATIONAL CHECKS WERE GOOD IAW EMB-120 MM 27-50-00. A IRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996030100369 19960301 00369 SO 1996 3 1 C2XA96CL007 1 19960130 A 2752 3203001007 ACTUATOR EMB 120 EMB120RT SO LT TE FLAP LINKAGE BINDING A C2XA K NONE J WARNING INDICATION AP APPROACH 1 SW 09 47722 10913 475 120166 ROC - FLIGHT NR 3113 - CREW REPORTED THAT ON APPROACH WITH FLAPS SELECTED TO 15 DEGREES, A FLAP ASYMMETRY OCCURRED THEN CHANGED TO A FLAP DISAGREEMENT. THE CREW ALSO REPORTED THAT THEY DID NOT RECEIVE A FLAP LIGHT ON THE MAP OR A DISAGREEM ENT LIGHT ON THE FLAP PANEL. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED THE LEFT OUTBOARD FLAP ACTUATOR IA W EMB-120 MM 27-50-09. OPERATIONAL AND LEAK CHECKS WERE GOOD IAW EMB-120 MM 27-50-00. AIRCRAFT RELEASED FOR SERVICE. ( M) 2 L 7 2 4T RT A31SO 1996030100370 19960301 00370 SO 1996 3 1 C2XA96CL008 1 19960130 A 2750 3075001017 CONTROL UNIT EMB 120 EMB120RT SO TE FLAPS FAILED A C2XA O OTHER J WARNING INDICATION AP APPROACH 1 SW 09 47722 7002 212 120166 CLE - FLIGHT NR 3286 - CREW REPORTED THAT ON APPROACH WHEN THE FLAPS WERE SELECTED TO 25 DEGREES FROM 15 DEGREES, THE LE FT AND RIGHT OUTBOARD FLAPS STAYED AT 15 DEGREES AND THE NACELLE AND INBOARD FLAPS WENT TO 25 DEGREES WITHOUT A WARNING INDICATION ON THE MAP OR OVERHEAD PANELS. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED THE FLAP CONTROL UNIT , IAW EMB-120 MM 27-50-06. OPERATIONAL CHECKS WERE GOOD IAW EMB-120 MM 27-50-00. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1996030100371 19960301 00371 SO 1996 3 1 C2XA96CL009 1 19960131 A 2750 3203001007 ACTUATOR EMB 120 EMB120RT SO RT TE FLAP STICKING A C2XA K NONE P NO WARNING INDICATION TO TAKEOFF 1 SW 09 47722 8442 525 120166 CLT - FLT NR 3340 - CREW REPORTED, THAT AFTER TAKEOFF AND FLAP RETRACTION, THE LEFT AND RIGHT OUTBOARD FLAPS STAYED AT 1 5 DEGREES WITHOUT RECEIVING A DISAGREEMENT INDICATION. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED THE RIGH T OUTBOARD FLAP ACTUATOR. MAINTENANCE ALSO REPLACED THE RIGHT OUTBOARD FLAP ACTUATOR CANNON PLUG NR PO 807. ALL WORK W AS ACCOMPLISHED IAW EMB-120 MM 27-50-00, OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1996030100372 19960301 00372 SO 1996 3 1 C2XA96CL010 1 19960201 A 2750 3069001017 FLAP ANNUNCIATOR EMB 120 EMB120RT SO COCKPIT FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 59708 10272 120098 CLE - FLT 3138 - CREW REPORTED THAT AFTER TAKEOFF AND FLAP RETRACTION, THEY RECEIVED A FLAP DISAGREEMENT. MAINTENANCE I NSPECTED AIRCRAFT AND REMOVED AND REPLACED THE FLAP ANNUNCIATOR IAW EMB-120 MM 27-50-05. OPERATIONAL CHECKS WERE GOOD I AW EMB-120 MM 27-50-00. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1996030100373 19960301 00373 SO 1996 3 1 C2XA96CL011 1 19960201 A 2752 3203001005 ACTUATOR EMB 120 EMB120RT SO RT TE FLAP FAULTED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 59708 11380 918 120098 CLE - FLT NR 3237 - CREW REPORTED THAT AFTER TAKEOFF AND FLAP RETRACTION THEY RECEIVED A FLAP DISAGREEMENT. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED THE RIGHT INBOARD FLAP ACTUATOR IAW EMB-120 MM 27-50-02. OPERATIONAL CHECK S WERE GOOD IAW EMB-120 MM 27-50-00. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1996030100374 19960301 00374 SO 1996 3 1 C2XA96CL012 1 19960205 A 6120 7902013 PROP ACTUATOR EMB 120 EMB120RT SO LT ENGINE LEAKING A C2XA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 09 15721 8848 5582 563 120160 GRR - FLIGHT NR 3378 - CREW REPORTED THAT AFTER TAKEOFF THEY HAD NO OIL PRESSURE IN THE LEFT ENGINE. MAINTENANCE INSPEC TED AIRCRAFT AND REMOVED AND REPLACED THE LEFT ENGINE PROP ACTUATOR IAW HAMILTON STANDARD MM 61-13-04. OPERATIONAL AND LEAK CHECKS WERE GOOD IAW EMB120 MM 61-00-00. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1996030100375 19960301 00375 SO 1996 3 1 C2XA96CL013 1 19960205 A 2750 3075001017 CONTROL UNIT EMB 120 EMB120RT SO TE FLAPS FAILED A C2XA K NONE J WARNING INDICATION AP APPROACH 1 SW 09 15713 10087 279 120114 CLE - FLIGHT NR 3933 - CREW REPORTED THAT ON APPROACH WHEN THE FLAPS WERE SELECTED TO 15 DEGREES A FLAP DISAGREEMENT OCC URRED. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED THE FLAP CONTROL UNIT IAW EMB-120 MM 27-50-06. OPERATIO NAL CHECKS WERE GOOD IAW EMB-120 MM 27-50-00. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1996030100376 19960301 00376 SO 1996 3 1 C2XA96CL014 1 19960205 A 5753 DRP138112VT FLAP ROLLER EMB 120 EMB120RT SO TE FLAPS BINDING A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 59708 120098 CLE - FLIGHT NR 3357 - CREW REPORTED THAT AFTER TAKEOFF WHEN FLAPS WERE SELECTED TO 0 DEGREES, A FLAP DISAGREEMENT OCCUR RED. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED THE RIGHT AND LEFT OUTBOARD FLAP ROLLERS IAW EMB-120 MM 27 -50-12. OPERATIONAL CHECKS WERE GOOD IAW EMB-120 MM 27-50-00. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1996030100377 19960301 00377 SO 1996 3 1 C2XA96CL015 1 19960203 A 5753 KRP138112VT FLAP ROLLERS EMB 120 EMB120RT SO TE FLAP BINDING A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 16724 120171 CVG - FLIGHT NR 3260 - CREW REPORTED THAT AFTER TAKEOFF AND FLAP RETRACTION THEY RECEIVED A FLAP DISAGREEMENT. MAINTENA NCE INSPECTED AIRCRAFT AND CLEANED THE FLAP TRACKS AND ROLLERS. THE SUBSEQUENT FLIGHT, ALSO FLIGHT NR 3260 REPORTED A F LAP DISAGREEMENT AFTER TAKEOFF AND FLAP RETRACTION. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED THE LEFT AN D RIGHT OUTBOARD FLAP ROLLERS IAW EMB-120 MM 27-50-12. OPERATIONAL CHECKS WERE GOOD IAW EMB-120 MM 27-50-00. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1996030100378 19960301 00378 EU 1996 3 1 C2XA96IA028 1 19960121 A 5610 NP1588013 WINDSHIELD AEROSP ATR42 ATR42320 8680930 EU LT COCKPIT CRACKED A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 09 14828 179 FLT NR 2729 - CAPTAINS FORWARD WINDSHIELD CRACKED IN FLIGHT, RETURNED TO STATION. AIRCRAFT FERRIED TO IAH WHERE WINDSHI ELD WAS REMOVED AND REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996030100379 19960301 00379 SO 1996 3 1 C2XA96IA029 1 19960125 A 5712 12017060005 RIB EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 34712 120111 IAH - DURING 1C CHECK INSPECTION, FOUND RIGHT WING RIB NR 19 (NOSE RIB WEB) TO BE CRACKED. MAINTENANCE INSTALLED L-PROF ILE. (M) 2 L 7 2 4T RT A31SO 1996030100380 19960301 00380 SO 1996 3 1 C2XA96IA030 1 19960125 A 5720 12017063009 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 34712 120111 IAH - DURING 1C CHECK INSPECTION, FOUND RIGHT WING RIB NR 20 UPPER SURFACE SKIN SUPPORT NR 4 CRACKED. MAINTENANCE REMOV ED AND REPLACED THE SKIN SUPPORT BRACKET. (M) 2 L 7 2 4T RT A31SO 1996030100381 19960301 00381 SO 1996 3 1 C2XA96IA031 1 19960125 A 5720 12017063009 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 34712 120111 IAH - DURING 1C CHECK INSPECTION, FOUND RIGHT WING RIB NR 21 UPPER SURFACE SKIN SUPPORT BRACKET NR 2 TO BE CRACKED. MAI NTENANCE REMOVED AND REPLACED THE SKIN SUPPORT BRACKET. (M) 2 L 7 2 4T RT A31SO 1996030100382 19960301 00382 SO 1996 3 1 C2XA96IA039 1 19960129 A 5712 12017058002 RIB EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 34712 120111 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING NOSE RIB NR 17 WEB CRACKED AT UPPER SURFACE ATTACHMENT. MAINTENANCE R EMOVED AND REPAIRED THE UPPER FLANGE WITH 'L' ANGLE PER FAX NR EST 023/96. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M ) 2 L 7 2 4T RT A31SO 1996030100383 19960301 00383 EU 1996 3 1 C2XA96IA040 1 19960129 A 5720 S5701007200640 STRUT AEROSP ATR42 ATR42320 8680930 EU RT WING BEARINGS WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14828 179 IAH - DURING 6C CHECK INSPECTION, FOUND RIGHT WING STRUT ASSEMBLY AT RIB NR 8 FLAP SUPPORT BEAM TO HAVE PLAY AT FORWARD AND AFT BEARINGS. MAINTENANCE REMOVED AND REPLACED THE STRUT ASSEMBLY, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996030100384 19960301 00384 EU 1996 3 1 C2XA96IA042 1 19960206 A 5320 S53973202210 ANGLE AEROSP ATR72 ATR72212 EU FS 27 CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 69902 385 IAH - DURING C-CHECK INSPECTION, FOUND LOWER RIGHT ATTACH ANGLE CRACKED UNDER PANEL 196 ES FORWARD SIDE FRAME 27. NEW A TTACH ANGLE WERE FABRICATED AND INSTALLED. (M) 2 H 7 2 4T RT A53EU 1996030100385 19960301 00385 EU 1996 3 1 C2XA96IA043 1 19960206 A 5347 S53678001228 SEAT TRACK AEROSP ATR72 ATR72212 EU FS 36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 69902 385 IAH - DURING C-CHECK INSPECTION, RIGHT FLIGHT ATTENDANTS SEAT TRACK AT FRAME 36 FOUND TO HAVE CORROSION BEYOND ACCEPTABL E LIMITS. SEAT TRACK WAS REMOVED AND REPLACED. (M) 2 H 7 2 4T RT A53EU 1996030100386 19960301 00386 NE 1996 3 1 C2XA96IA044 2 19960206 A 7421 IGNITER AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE LT ENGINE LOOSE A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 09 17831 185 120518 CRP - FLT NR 2590 - DURING CRUISE, THE PILOT REPORTED THAT THE LEFT ENGINE FIRE INDICATION ILLUMINATED. THE ORIGINAL FL IGHT PLAN WAS FROM IAH TO BRO, BUT THE AIRCRAFT DIVERTED AND LANDED AT CRP WITHOUT FURTHER INCIDENT. MAINTENANCE INSPEC TED THE LEFT ENGINE AND FOUND THE INBOARD IGNITER TO BE UNSECURE. MAINTENANCE REINSTALLED THE IGNITER, AND RAN THE LEFT ENGINE WITH NO FURTHER FIRE INDICATIONS. THE AIRCRAFT WAS THEN APPROVED FOR RETURNED TO SERVICE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1996030100387 19960301 00387 WP 1996 3 1 CAL960052 1 19960124 A 2910 7936907590 HYD LINE DOUG DC9 DC982 3022082 WP RT MLG WW CRACKED A CALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 72830 49490 FLT NR 268 - EWR - THE RT HYD FLUID QTY DROPPED TO TWO QTS WHILE EN ROUTE FROM FLL TO EWR. THE AIRCRAFT LANDED AT EWR W ITH THE GEAR DOORS OPEN. MAINTENANCE FOUND THE GROUND SPOILER HYD PRESSURE LINE IN THE RT WHEEL WELL CRACKED AT FITTING . A FLEX LINE WAS INSTALLED AND A DIP WAS ISSUED TO REPLACE THE FLEX LINE WITHIN 1200 FLIGHT HOURS OR 500 CYCLES, WHICH EVER OCCURS FIRST. THE RIGHT HYD SYSTEM WAS SERVICED TO FULL AND ALL CONTROL SURFACES WERE CYCLED WITH NO LEAKS OR OTHE R DEFECTS NOTED. THE LEFT AND RIGHT MLG DOORS WERE INSPECTED AND NO DEFECTS WERE FOUND. (M) 2 L 7 2 4F A6WE 1996030100388 19960301 00388 WP 1996 3 1 CAL960053 1 19960111 A 5712 RIB DOUG DC9 DC981 3022081 WP LT WING LE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14880 34534 48044 HOU - INSPECTION FOUND A .625 INCH CRACK IN LOWER RADIUS OF LEFT WING LEADING EDGE RIB, LOCATED OUTBOARD OF NR 8 SLAT TR ACK. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-04. (M) 2 L 7 2 4F A6WE 1996030100389 19960301 00389 WP 1996 3 1 CAL960054 1 19960111 A 5720 BRACKET DOUG DC9 DC981 3022081 WP RT WING BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14880 34534 48044 HOU - INSPECTION FOUND RIGHT WING LEADING EDGE RIB LOWER ATTACH BRACKET BROKEN OUTBOARD OF NR 2 SLAT TRACK. A NEW BRACK ET WAS FABRICATED AND INSTALLED IAW SRM 51-60-0 AND 51-30-2. (M) 2 L 7 2 4F A6WE 1996030100390 19960301 00390 WP 1996 3 1 CAL960055 1 19960111 A 5720 BRACKET DOUG DC9 DC981 3022081 WP RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14880 34534 48044 HOU - INSPECTION FOUND A.75 INCH CRACK IN RIGHT WING LEADING EDGE RIB AFT BRACKET, LOCATED AT FORWARD SPAR UPPER CAP OUT BOARD OF NR 8 SLAT TRACK. A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-60-0 AND 51-30-2. (M) 2 L 7 2 4F A6WE 1996030100391 19960301 00391 WP 1996 3 1 CAL960056 1 19960110 A 5210 RIB DOUG DC9 DC981 3022081 WP CABIN DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14880 34534 48044 HOU - INSPECTION FOUND A 1.5 INCH CRACK IN RIB OF MAIN CABIN DOOR. A DOUBLER WAS INSTALLED IAW SRM 52-05. (M) 2 L 7 2 4F A6WE 1996030100392 19960301 00392 WP 1996 3 1 CAL960057 1 19960123 A 2612 FIRE DETECT DOUG DC9 DC932 3022066 WP NR 2 ENGINE MALFUNCTIONED A CALA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 09 12508 47797 FLT NR 1787 - SDF - THE NR 1 ENG FIRE WARNING LIGHT ILLUMINATED IN FLT. THE ENGINE FIRE BOTTLE WAS DISCHARGED AND THE L IGHT WENT OUT. THE LIGHT ILLUMINATED AGAIN AND THE SECOND FIRE BOTTLE WAS DISCHARGED, BUT THE LIGHT REMAINED ON. THE A IRCRAFT WAS DIVERTED TO SDF WHERE IT LANDED WITHOUT INCIDENT. MX FOUND NO EVIDENCE OF FIRE. THE NR 2 ENGINE 'A' FIRE D ETECTION LOOP WAS FOUND 'OPEN' AND THE 'B' LOOP WAS CONTACTING THE COWLING. THE 'B' LOOP WAS REPOSITIONED. THE 'A' LOO P WAS REMOVED AND REPLACED IAW MM 26-10-4, CODE 1. BOTH THE 'A' AND 'B' FIRE DETECTION SYSTEMS CHECKED GOOD. BOTH ENGI NE FIRE BOTTLES WERE REMOVED AND REPLACED. (M) 2 L 7 2 4F A6WE 1996030100393 19960301 00393 WP 1996 3 1 CAL960059 1 19960120 A 2612 892809040002 FIRE DET MODULE DOUG DC9 DC982 3022082 WP NR 1 ENGINE INOPERATIVE A CALA O OTHER N FALSE WARNING CL CLIMB 1 SW 09 14814 15979 49112 FLT NR 421 - IAH - THE NR 1 ENGINE LOOP 'B' FIRE DETECTOR LIGHT AND MASTER CAUTION LIGHT ILLUMINATED DURING CLIMB-OUT AT 18,000 FEET. THE NR 1 ENGINE LOOP SWITCH WAS MOVED TO LOOP 'A' AND TEST WAS NORMAL. THE NR 1 ENGINE FIRE DETECTION MO DULE WAS REMOVED AND REPLACED. THE NR 1 ENGINE FIRE DETECTION SYSTEM CHECKED GOOD. (M) 2 L 7 2 4F A6WE 1996030100394 19960301 00394 NM 1996 3 1 CAL960062 1 19960124 A 2910 65445101472 HYD LINE BOEING 737 737130 1384435 NM 'A' HYD SYSTEM CHAFED A CALA O OTHER K FLUID LOSS CR CRUISE 1 SW 09 44214 19031 FLT NR 1069 - TPA - AIRCRAFT LOST THE 'A' SYSTEM HYDRAULICS WHILE EN ROUTE FROM GSO TO TPA. QRH CHECKLIST PROCEDURES WE RE ACCOMPLISHED AND THE AIRCRAFT LANDED AT TPA WITHOUT INCIDENT. MAINTENANCE FOUND 'A' SYSTEM HYDRAULIC PRESSURE LINE A BOVE LEFT MLG CHAFED THROUGH. A FLEX LINE WAS INSTALLED AND A DIP WAS ISSUED TO REPLACE THE FLEX LINE WITHIN 500 FLIGHT S OR 1200 HOURS, WHICHEVER COMES FIRST. LEAK CHECK OF THE HYDRAULIC SYSTEM CHECKED GOOD. (M) 2 L 7 2 4F A16WE 1996030100395 19960301 00395 WP 1996 3 1 CAL960063 1 19960124 A 3260 DNLOCK SENSOR DOUG DC9 DC982 3022082 WP NLG INOPERATIVE A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 819NY 49479 FLT NR 1821 - SEA - THE NLG RED LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION ON TAKEOFF FROM SEA. THE COCKPIT NLG I NDICATOR PIN INDICATED THE GEAR WAS IN TRANSIT. CYCLING THE GEAR DID NOT HELP. THE AIRCRAFT WAS RETURNED TO SEA WHERE IT LANDED WITHOUT INCIDENT. THE NOSE GEAR STRUT WAS SERVICED. A NOSE GEAR RETRACT WAS PERFORMED, BUT THE PROBLEM REMAI NED. MAINTENANCE FOUND THE NOSE GEAR DOWNLOCK SENSOR AT FAULT DURING A GEAR PROXIMITY SENSOR BITE CHECK. THE SENSOR WA S REMOVED AND REPLACED. A NOSE GEAR RETRACTION WAS PERFORMED WITH OPERATION AND INDICATIONS CHECKING GOOD. (M) 2 L 7 2 4F A6WE 1996030100396 19960301 00396 NM 1996 3 1 CAL960064 1 19960125 A 3222 STRUT BOEING 737 7373T0 1384582 NM NLG LEAKING A CALA O OTHER J WARNING INDICATION CL CLIMB 1 SW 09 70330 23460 FLT NR 0295 - IAH - THE LANDING GEAR LEVER WOULD NOT RAISE BEYOND THE OFF POSITION AFTER TAKEOFF FROM ORD. THE LOCK OVE RRIDE WAS USED TO RETRACT THE GEAR. THE FLIGHT WAS CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. THE CONTROL LEVE R LOCK SYSTEM WAS TROUBLESHOT PER MM 32-31-21 AND NO FAULTS WERE NOTED. MAINTENANCE FOUND THE NLG STRUT LEAKING. THE N LG STRUT WAS REPACKED IAW MM 32-21-11 AND SERVICED PER MM 12-15-41. A DIP WAS ISSUED TO CHECK STRUT PRESSURE AND X-DIME NSION AFTER 4, BUT PRIOR TO 20 LANDINGS. (M) 2 L 7 2 4F RT A16WE 1996030100397 19960301 00397 NM 1996 3 1 CAL960065 1 19960125 A 2612 FIRELOOP BOEING 737 7373T0 1384582 NM NR 2 ENGINE INOPERATIVE A CALA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SW 09 17326 23456 FLT NR 1827 - IAH - THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED WHILE ON APPROACH TO IAH. THE THROTTLES WERE BROUGHT TO IDLE, BUT THE LIGHT DID NOT EXTINGUISH. BOTH FIRE BOTTLES WERE DISCHARGED, BUT THE LIGHT REMAINED ON. THE NR 2 ENGINE WAS SHUT DOWN AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE NR 2 ENGINE CORE FIRE DETECTION LOOP WAS FOUND AT FAULT AND THE OUTBOARD CORE LOOP CONNECTORS WERE FOUND BROKEN. THE CORE LOOP ASSE MBLY AND BOTH CONNECTORS WERE REMOVED AND REPLACED. THE NR 2 ENGINE WAS RUN AT VARIOUS POWER SETTINGS AND ALL INDICATIO NS CHECKED NORMAL. (M) 2 L 7 2 4F RT A16WE 1996030100398 19960301 00398 NM 1996 3 1 CAL960067 1 19960130 A 2910 HYD LINE BOEING 737 737130 1384435 NM 'A' HYD SYSTEM LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 44214 19031 FLT NR 1069 - TPA - THE 'A' HYDRAULIC SYSTEM WAS LOST WHILE IN FLIGHT WITH THE QUANTITY GAUGE INDICATING ZERO. THE AIRC RAFT LANDED AT TPA WITHOUT INCIDENT. MAINTENANCE FOUND FLEX LINE TO 'A' HYDRAULIC SYSTEM PRESSURE MODULE LEAKING. THE LINE WAS REPLACED USING ORIGINAL EQUIPMENT RIGID LINE. THE HYDRAULIC SYSTEM WAS SERVICED TO FULL AND LEAK CHECKS WERE G OOD. (M) 2 L 7 2 4F A16WE 1996030100399 19960301 00399 SW 1996 3 1 MALA964822 1 19960116 A 5320 2724087901 CORNER SWRNGN SA227 SA227AC 8780603 SW FS 133.87 PUNCTURED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 27465 AC755B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE FORWARD LOWER PASSENGER DOOR FUSELAGE AT FS 133.87 TO BE DAM AGED. REPAIRS WERE COMPLETED BY REPLACING THE FORWARD LOWER CORNER, P/N 27-24087-901, IAW FAC SRM 51-00-00 PAGE 4, 51-4 0-02 AND 51-30-04. (M) 1 L 7 2 4T A8SW 1996030100400 19960301 00400 NM 1996 3 1 MALA964823 1 19960116 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM FS 330 DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 849MA 347 DURING A C-CHECK INSPECTION IN FFV, A DENT WAS NOTED IN THE FUSELAGE AT STATION X330.0 BELOW STRINGER 18P ON THE LEFT SI DE. REPAIRS WERE COMPLETED BY INSTALLING A DOUBLER IAW DEHAVILLAND RD8-53-1867. (M) 2 H 7 2 4T RT A13NM 1996030100401 19960301 00401 1996 3 1 MALA964824 4 19960118 A 3442 071131900 RADAR DHAV DHC8 DHC8102 2809003 NM RADOME FAILED A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 846MA 344 FLT NR 3130 - ON CLIMB-OUT FROM DTW, THE WEATHER RADAR BECAME INOPERATIVE. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE R EPLACED THE WEATHER RADAR, P/N 071-1319-00. SYSTEM OPERATED SATISFACTORILY. (M) 2 H 7 2 4T RT A13NM 1996030100402 19960301 00402 NM 1996 3 1 MALA964825 1 19960118 A 3060 7826893 BRUSH BLOCK DHAV DHC8 DHC8102 2809003 NM LT PROP FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 833MA 343 FLT NR 3006 - DURING CLIMB-OUT FROM DTW, THE LEFT ELEVATOR HORN HEAT CAUTION LIGHT ILLUMINATED AND THE LEFT TRU CIRCUIT BREAKER POPPED. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE LEFT PROP DE-ICE BRUSH BLOCK AND C PHASE CIRCUI T BREAKER FUSE. SYSTEM OPERATED SATISFACTORILY. (M) 2 H 7 2 4T RT A13NM 1996030100403 19960301 00403 SW 1996 3 1 MALA964826 1 19960120 A 3260 1EN516 UPLOCK SWITCH SWRNGN SA227 SA227AC 8780603 SW NLG FAILED A MALA O OTHER N FALSE WARNING CL CLIMB 1 GL 15 63NE AC763B FLIGHT NR 3087 - ON CLIMB-OUT FROM YQT, NO NOSE GEAR INTRANSIT LIGHT WAS NOTED DURING GEAR RETRACTION. THE AIRCRAFT CON TINUED TO MSP WITH THE GEAR DOWN. MAINTENANCE REPLACED THE NOSE GEAR UPLOCK POSITION SWITCH. SYSTEM OPERATED SATISFACT ORILY. (M) 1 L 7 2 4T A8SW 1996030100404 19960301 00404 SW 1996 3 1 MALA964827 1 19960121 A 3020 31998061 VALVE SWRNGN SA227 SA227AC 8780603 SW RT ENGINE FAILED A MALA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 158MC AC762B FLT NR 3226 - IN CRUISE FLIGHT, THE RIGHT INTAKE HEAT CIRCUIT BREAKER POPPED. THE AIRCRFT RETURNED TO MSP. MAINTENANCE REPLACED THE RIGHT ENGINE INTAKE HEAT ANTI-ICE SOLENOID VALVE. SYSTEM OPERATED SATISFACTORILY. (M) 1 L 7 2 4T A8SW 1996030100405 19960301 00405 SW 1996 3 1 MALA964828 1 19960119 A 5320 DOOR FRAME SWRNGN SA227 SA227AC 8780603 SW FS 438.06 CRACKED A MALA O OTHER O OTHER IN INSP/MAINT 1 GL 15 428MA AC646 DURING A SCHEDULED INSPECTION IN MSP, THE CARGO DOOR FRAME, AT FS 438.060, WAS FOUND TO BE CRACKED. REPAIRS WERE COMPLE TED BY INSTALLING A REPAIR ANGLE, PLATE AND FILLER IAW FAC ARM 53-20-9503. (M) 1 L 7 2 4T A8SW 1996030100406 19960301 00406 SW 1996 3 1 MALA964829 1 19960120 A 5311 FRAME SWRNGN SA227 SA227AC 8780603 SW FS 174 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 159MC AC728B DURING A SCHEDULED INSPECTION MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE FUSELAGE FRAME AT FS 174. THEY STOP DRILL ED THE CRACK AND FABRICATED AND INSTALLED A REPAIR DOUBLER IAW FAC SRM 53-90-20. (M) 1 L 7 2 4T A8SW 1996030100407 19960301 00407 SW 1996 3 1 MALA964830 1 19960121 A 3310 LIGHT PANEL SWRNGN SA227 SA227AC 8780603 SW COCKPIT SMOKING A MALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 15 438MA AC721B FLT 3347 - IN CRUISE FLIGHT TO DTW, THE CREW NOTED A SMOKE SMELL FROM THE RT CIRCUIT BREAKER SIDE CONSOLE. THE CREW TUR NED OFF THE SIDE PANEL LIGHTS AND PULLED THE CIRCUIT BREAKER. THE SMELL DISSIPATED. THE AIRCRAFT CONTINUED TO DTW. TH E SYSTEM WAS DEFERRED PER MEL 33-1 (C). MAINTENANCE PERSONNEL REPAIRED A FAULTY CIRCUIT BREAKER LIGHTING PANEL. ALL SY STEMS OPERATED SATISFACTORILY. (X) 2 L 7 2 4T RT A8SW 1996030100408 19960301 00408 SW 1996 3 1 MALA964837 1 19960122 A 3260 1EN516 POSITION SW SWRNGN SA227 SA227AC 8780603 SW NLG FAILED A MALA O OTHER P NO WARNING INDICATION CL CLIMB 1 GL 15 60NE AC760B FLT NR 3027 - ON CLIMB-OUT FROM GPS, THE NOSE GEAR INTRANSIT LIGHT FAILED TO ILLUMINATE UPON GEAR RETRACTION. ALL OTHER INDICATIONS WERE NORMAL. THE LIGHT ALSO FAILED TO ILLUMINATE ON APPROACH TO MSP. MAINTENANCE REPLACED THE LEFT UP POS ITION SWITCH. SYSTEM OPERATED SATISFACTORILY. (M) 1 L 7 2 4T A8SW 1996030100409 19960301 00409 NM 1996 3 1 MALA964838 1 19960106 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN LOOSE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 865MA 364 FLT NR 3166 - DURING THE POST FLIGHT INSPECTION IN DTW, THE CREW NOTED AN EMERGENCY LIGHT WAS INOP ON THE LEFT SIDE AT R OW 4. MAINTENANCE RESECURED A LOOSE CONNECTOR. SYSTEM OPERATED SATISFACTORILY. (M) 2 H 7 2 4T RT A13NM 1996030100410 19960301 00410 NM 1996 3 1 MALA964839 1 19960107 A 3350 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 865MA 364 DURING MAINTENANCE WALKAROUND IN DTW, THE EMERGENCY ESCAPE PATH LIGHTS, THE TWO MOST FORWARD, WERE FOUND TO BE INOPERATI VE. THE SYSTEM WAS DEFERRED PER MEL 33-13. THE WRITE-UP WAS UNABLE TO BE DUPLICATED. THE SYSTEM OPERATED SATISFACTORI LY. (M) 2 H 7 2 4T RT A13NM 1996030100411 19960301 00411 SW 1996 3 1 MALA964840 1 19960124 A 5210 2724045013 FRAME SWRNGN SA227 SA227AC 8780603 SW PASSENGER DOOR CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 423MA AC636 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE PASSENGER DOOR AFT FRAME. THEY REPAIRE D THE CRACK BY REMOVING 7 INCHES OF THE FRAME AND INSTALLING A FILLER AND DOUBLER IAW FAC SRM 52-90-10. (M) 1 L 7 2 4T A8SW 1996030100412 19960301 00412 NM 1996 3 1 MALA964841 1 19960125 A 3350 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 831MA 339 FLT NR 3125 - DURING PREFLIGHT INSPECTION IN DTW, THE CREW NOTED THE RED FLOOR TRACK LIGHTS WERE BURNED OUT. MAINTENANC E PERSONNEL FUNCTIONALLY TESTED THE SYSTEM BUT WERE UNABLE TO DUPLICATE THIS DISCREPANCY. ALL SYSTEMS OPERATED SATISFAC TORILY. (M) 2 H 7 2 4T RT A13NM 1996030100413 19960301 00413 NM 1996 3 1 MALA964842 1 19960126 A 3350 1005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 833MA 343 FLT NR 3372 - DURING PREFLIGHT INSPECTION IN MSP, THE CREW NOTED THE COCKPIT OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. M AINTENANCE PERSONNEL REPLACED THE LIGHT ASSEMBLY. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2 H 7 2 4T RT A13NM 1996030100414 19960301 00414 SW 1996 3 1 MALA964843 1 19960126 A 5210 SEAL SWRNGN SA227 SA227AC 8780603 SW PAX DOOR OUT OF ADJUST A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 434MA AC717 FLT NR 3354 - AFTER DEPARTURE FROM DTW, THE CREW NOTED A LOUD SQUEAL FROM THE PASSENGER DOOR. THE CREW ELECTED TO RETUR N TO DTW AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL SHIMMED THE PASSENGER DOOR SEAL. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 1 L 7 2 4T A8SW 1996030100415 19960301 00415 NM 1996 3 1 MALA964844 1 19960127 A 2420 51608002 CONTROL UNIT DHAV DHC8 DHC8102 2809003 NM LT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 865MA 364 FLT NR 3410 - AFTER DEPARTURE FROM DTW, THE NR 1 AC GENERATOR CAUTION LIGHT ILLUMINATED. THE AIRCRAFT RETURED TO DTW AN D LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE NR 1 AC GENERATOR CONTROL UNIT. ALL SYSTEMS OPERATED SAT ISFACTORILY. (M) 2 H 7 2 4T RT A13NM 1996030100416 19960301 00416 NM 1996 3 1 MALA964845 1 19960127 A 3234 5352011 SELECTOR VALVE DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A MALA O OTHER O OTHER AP APPROACH 1 GL 15 817MA 249 FLT NR 3231 - DURING APPROACH TO BJI, THE GEAR WAS VERY SLOW TO EXTEND WHEN SELECTED DOWN. THE AIRCRAFT CONTINUED TO BJ I AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE LANDING GEAR SELECTOR, P/N 535201-1, AND THE SELECTOR VALVE, P/N 57420-5. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2 H 7 2 4T RT A13NM 1996030100417 19960301 00417 EU 1996 3 1 RAIA960145 1 19960126 A 5610 WINDOW SEALANT AEROSP ATR42 ATR42300 8680920 EU RT COCKPIT FAILED A RAIA O OTHER O OTHER CR CRUISE 1 CE 03 423TE 119 STL - FLT NR 7408 - HISSING SOUND FROM FIRST OFFICERS SIDE WINDOW, ALSO NOTICED SEALER TRAILING FROM WINDOW. MAINTENANC E RESEALED FIRST OFFICERS SIDE WINDOW. (M) 2 H 7 2 4T RT A53EU 1996030100418 19960301 00418 EU 1996 3 1 RAIA960146 1 19960125 A 5270 MS161065 SWITCH BAG JETSTM JETSTM3201 1500217 EU POD DOOR DIRTY A RAIA D RETURN TO BLOCK N FALSE WARNING CL CLIMB 1 CE 03 875JX 8944 875 MSN - FLT NR 7171 - POD DOOR LIGHT ILLUMINATED AFTER TAKEOFF. MAINTENANCE PLACED ON DMI 52-1. MAINTENANCE LATER CLEARE D DMI BY CLEANING MICRO-SWITCH, OPERATION CHECK GOOD. (M) 2 L 7 2 4T RT A56EU 1996030100419 19960301 00419 EU 1996 3 1 RAIA960147 1 19960126 A 2430 1030032 SENSOR AEROSP ATR42 ATR42300 8680920 EU RIGHT WING FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION CR CRUISE 1 CE 03 426TE 11211 228 STL - FLT NR 7240 - NR 2 DC GENERATOR FAULT. MAINTENANCE REMOVED AND REPLACED RIGHT HALL EFFECT SENSOR. OPERATIONAL CH ECK GOOD. (M) 2 H 7 2 4T RT A53EU 1996030100420 19960301 00420 1996 3 1 RAIA960149 3 19960126 A 6140 8659562 BETA SWITCH BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 429AM 8696 6230 879 STL - FLT NR 7350 - RIGHT BETA LIGHT ILLUMINATED ON TAKEOFF ROLL. MAINTENANCE REMOVED AND REPLACED RIGHT BETA SWITCH, P ERFORMED GROUND RUNS OPS CHECK GOOD. (M) 2 L 7 2 4T RT A56EU 1996030100421 19960301 00421 1996 3 1 RAIA960155 4 19960130 A 3417 7000700951 AIR DATA COMP AEROSP ATR72 ATR72202 8680940 EU LT AV RACK MALFUNCTIONED A RAIA D RETURN TO BLOCK O OTHER CL CLIMB 1 CE 03 723TE 9297 1843 283 STL - FLT NR 7003 - CAPTAIN VERTICAL SPEED INDICATOR INTERMITTENTLY DISPLAYS THE BOOT UP SCREEN. MAINTENANCE RERACKED N R 1 AIR DATA COMPUTER, OPERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1996030100422 19960301 00422 EU 1996 3 1 RAIA960157 1 19960130 A 2612 D2370120 FIRE LOOP BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 343TE 955 DEC - FLT NR 7301 - RIGHT ENGINE FIRE DETECTION SYSTEM SOUNDED, CREW FIRED BOTH FIRE BOTTLES AND SHUT DOWN ENGINE. MAIN TENANCE FOUND NO EVIDENCE OF FIRE. RIGHT ENGINE FORWARD FIRE LOOP REPLACED, BOTTLES REPLACED, OPERATION CHECK GOOD. (M ) 2 L 7 2 4T RT A56EU 1996030100423 19960301 00423 EU 1996 3 1 RAIA960158 1 19960131 A 2611 72111211000 SMOKE DETECTOR BAG JETSTM JETSTM3201 1500217 EU AFT BAGGAGE FAILED A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 435AM 889 STL - FLT NR 7440 - ON TAKEOFF 'SMOKE' ILLUMINATED ON CAP, TAKEOFF ABORTED. MAINTENANCE REMOVED AND REPLACED AFT BAGGAG E COMPARTMENT SMOKE DETECTOR, OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A56EU 1996030100424 19960301 00424 EU 1996 3 1 RAIA960159 1 19960131 A 3222 B00A703056A STRUT BAG JETSTM JETSTM3201 1500217 EU NLG REQ'D SERVICE A RAIA D RETURN TO BLOCK O OTHER CL CLIMB 1 CE 03 429AM 10491 4553 879 STL - FLT NR 7284 - GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION AFTER TAKEOFF. MAINTENANCE REPACKED THE NLG STRUT, GE AR SWING OPERATION CHECK GOOD. (M) 2 L 7 2 4T RT A56EU 1996030100425 19960301 00425 EU 1996 3 1 RAIA960201 1 19960201 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN LOW VOLTS A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 421TE 102 STL - MX - EMERGENCY TRACK LIGHTING INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS, OPS CHECK GOO D. (M) 2 H 7 2 4T RT A53EU 1996030100426 19960301 00426 NE 1996 3 1 SIMA960262 3 19960130 A 6114 66714200 HUB SAAB SF340 SF340A 7850100 EU ROTOL R354 R3544123F13 NE LT PROP CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 112AE 108603 340A112 LAW - DURING NDT HUB INSPECTION IN SHOP, PROPELLER (S/N DRG/1538/88) THE HUB (P/N 66714200 S/N 108603) INDICATED A CRACK IN THE MOUNTING FACE AREA OUTBOARD OF NR 9 BOLT INSERT. THE HUB WAS REMOVED FROM SERVICE. (M) 2 L 7 2 4T RT A52EU 6 C P61GL 1996030100427 19960301 00427 EU 1996 3 1 SIMA960263 1 19960126 A 6130 3037784 PROP BRAKE AEROSP ATR42 ATR42300 8680920 EU RT ENG FAILED A SIMA F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 SW 21 430MQ 10408 0136 GRB - FLT NR 4240 - AFTER ENGINE START AND PROP BRAKE ON, PILOT NOTED PROP BRAKE UNLOCK WARNING ON CAP PANEL. UPON VIEW ING THE ENGINE CREW NOTED FIRE FROM THE FORWARD ENGINE COWLING AREA. FIRE BOTTLES WERE DISCHARGED AND CFR WAS CALLED TO ENSURE FIRE WAS EXTINGUISHED. MAINTENANCE REMOVED AND DEFERRED THE PROP BRAKE PER MEL PROCEDURES. ENGINE AND COWLS IN SPECTED FOR OVERHEAT DAMAGE AND NONE FOUND. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996030100442 19960301 00442 NM 1996 3 1 TSAA9653003 1 19960118 A 5330 SKIN BOEING 737 7372Q9 138448M NM BS 764 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 804AL 21719 DURING OVERNIGHT CHECK DISCOVERED FUSELAGE SKIN CRACK 1 INCH LONG AT BS 764, STRINGER 16L. VERIFIED ENDS OF CRACK WITH HFEC. REPAIRED PER SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1996030100444 19960301 00444 1996 3 1 VTZA96068 3 19960201 A 6140 KPT06F83S CONNECTOR BAG JETSTM JETSTM3201 1500217 EU LT ENG DIRTY A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 492UE 790 FLT NR 6250 - ABE-IAD - ABORTED TAKEOFF DUE TO THE LEFT ENGINE BETA CAPTION LIGHT WOULD NOT EXTINGHISH. AIRCRAFT RETURN ED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE CLEANED THE BETA SWITCH CANNON PLUG. AIRCRAFT WAS RELEASED AND APPRO VED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996030100445 19960301 00445 EU 1996 3 1 VTZA96069 1 19960201 A 3411 PITOT BAG JETSTM JETSTM3201 1500217 EU FWD FUS FROZE UP A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 27 495UE 818 FLT NR 6302 - ISP-IAD - ABORTED TAKEOFF DUE TO THE CAPTAINS AIRSPEED INDICATOR REMAINING AT ZERO DURING THE TAKEOFF ROLL . AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE THAWED THE PITOT STATIC LINES TO THE NR 1 AIRSPEED INDICATOR. (M) 2 L 7 2 4T RT A56EU 1996030100446 19960301 00446 1996 3 1 VTZA96070 4 19960202 A 3425 7003360948 AHRS JETAIR JETSTM JETSTM4101 1500501 EU AVIONICS BAY FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 303UE 41015 FLT NR 6150 - IAD-EWR - DURING CLIMB-OUT, RETURNED TO IAD DUE TO THE AHRS FAILING. AIRCRAFT LANDED AT IAD WITH NO FURTH ER INCIDENTS. MAINTENANCE REPLACED AHRS COMPUTER NR 1. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996030100447 19960301 00447 EU 1996 3 1 VTZA96073 1 19960203 A 3250 CONTROL BOX JETAIR JETSTM JETSTM4101 1500501 EU NLG STEERING FAILED A VTZA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 27 305UE 41019 FLT NR 6191 - IAD-BOS - AFTER LANDING, THE NOSEWHEEL STEERING LOCKED UP EXITING RUNWAY. BLEW BOTH NOSE TIRES ATTEMPTING TO LEAVE THE RUNWAY. AIRCRAFT WAS THEN TOWED TO GATE AND NOSEWHEEL STEERING BOX WAS LUBED AND REMOVED AND REPLACED BOT H N/G TIRES. OPS CHECK OK. AIRCRAFT WAS THEN RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996030100448 19960301 00448 EU 1996 3 1 WTAA960013A 1 19960121 A 3260 9005EN38 SWITCH BAG JETSTM JETSTM3101 1500215 EU NOSE GEAR DIRTY A WTAA O OTHER N FALSE WARNING AP APPROACH 1 WP 17 401UE 729 LAX - GEAR HORN SOUNDED AND NOSE GEAR INTRANSIT LIGHT REPORTED INTERMITTENT DURING GEAR EXTENSION WITH FLAPS SET AT 10 D EGREES. WARNING STOPPED WITH GEAR DOWN AND LOCKED. GEAR WARNING SYSTEM OPERATIONAL CHECK NORMAL DURING GEAR RETRACTION CHECK WITH FLAPS UP AND AT THE 10 DEGREE POSITIONS. UNABLE TO DUPLICATE REPORTED DISCREPANCY. CLEANED AND INSPECTED N OSE GEAR UPLOCK, DOWNLOCK AND POWER LEVER QUANDRANT MICROSWITCHES. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996030100449 19960301 00449 EU 1996 3 1 WTAA960013B 1 19960121 A 3260 91SE16 SWITCH BAG JETSTM JETSTM3101 1500215 EU NLG DIRTY A WTAA O OTHER N FALSE WARNING AP APPROACH 1 WP 17 401UE 729 LAX - GEAR HORN SOUNDED AND NOSE GEAR INTRANSIT LIGHT REPORTED INTERMITTENT DURING GEAR EXTENSION WITH FLAPS SET AT 10 D EGREES. WARNING STOPPED WITH GEAR DOWN AND LOCKED. GEAR WARNING SYSTEM OPERATIONAL CHECK NORMAL DURING GEAR RETRACTION CHECK WITH FLAPS UP AND AT THE 10 DEGREE POSITIONS. UNABLE TO DUPLICATE REPORTED DISCREPANCY. CLEANED AND INSPECTED N OSE GEAR UPLOCK, DOWNLOCK AND POWER LEVER QUADRANT MICROSWITCHES. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996030100450 19960301 00450 EU 1996 3 1 WTAA960014 1 19960121 A 7722 6100116 EGT INDICATOR BAG JETSTM JETSTM3101 1500215 EU RT ENGINE FAILED A WTAA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 17 331CA 793 SFO - RIGHT ENGINE EGT GAUGE INDICATION DROPPED TO 450 DEGREES AND STUCK DURING CLIMB-OUT. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT EGT GAUGE. SYSTEM OPERATIONAL CHECK NORMAL, AIRCRAFT RETURNED TO SERVICE . (M) 2 L 7 2 4T RT A21EU 1996030100451 19960301 00451 SO 1996 3 1 WTAA960015 1 19960121 A 2731 12038650001 TRIM ACTUATOR EMB 120 EMB120RT SO HORIZ STAB FROZE UP A WTAA K NONE F FLT CONT AFFECTED CR CRUISE 1 WP 17 275UE 120058 FAT - ELEVATOR TRIM REPORTED INOPERATIVE 'FROZEN' AT ALTITUDE. SYSTEM OPERATION REPORTED NORMAL AT LOWER ALTITUDES. MA INTENANCE REMOVED AND REPLACED LEFT AND RT ELEVATOR TRIM ACTUATORS DUE TO WATER INGRESS, CAUSING UNITS TO FREEZE AT ALTI TUDE. OPERATIONAL CHECK OF ELEVATOR TRIM SYSTEM GOOD. TEST AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996030100452 19960301 00452 SO 1996 3 1 WTAA960016 1 19960121 A 2731 12038650001 TRIM ACTUATOR EMB 120 EMB120RT SO HORIZ STAB LACK OF LUBE A WTAA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 WP 17 201YW 120201 SFO - PITCH TRIM SYSTEM REPORTED INOPERATIVE 'FROZEN' AT ALTITUDE. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. NOTE , SYSTEM BEGAN TO OPERATE NORMALLY ON DESCENT AT MINUS 5 DEGREE CELSIUS. MAINTENANCE INSPECTED AND LUBRICATED ELEVATOR TRIM ACTUATORS. TRIM SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996030100453 19960301 00453 SO 1996 3 1 WTAA960017 1 19960123 A 5270 MS250851 SWITCH EMB 120 EMB120RT SO CARGO DOOR BROKEN WIRE A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 17 276UE 120067 LAX - CARGO DOOR WARNING ACTIVATED ON TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE ACCOMPLISHED DEFERRA L MAINTENANCE PROCEDURE 52-70-1. AIRCRAFT RETURNED TO SERVICE. NOTE, CARGO DOOR WARNING SYSTEM REACTIVATED AFTER THE R EPAIR OF WIRES ON CARGO DOOR MICROSWITCH AT AIRCRAFT RON. (M) 2 L 7 2 4T RT A31SO 1996030100454 19960301 00454 EU 1996 3 1 WTAA960018 1 19960113 A 7712 31034391 CONNECTOR BAG JETSTM JETSTM3101 1500215 EU LT ENGINE DIRTY A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 WP 17 422UE 782 ACV - LEFT ENGINE TORQUE AND EGT INDICATION DROPPED WITH ENGINE SURGE DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCI DENT. MAINTENANCE CLEANED CANNON PLUG AT LEFT ENGINE TORQUE RING CABLE ASSEMBLY. LEFT ENGINE OPERATIONAL CHECK NORMAL DURING GROUND RUN. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996030100455 19960301 00455 SO 1996 3 1 WTAA960019 1 19960127 A 5270 DOOR WARNING EMB 120 EMB120RT SO CARGO DOOR ACTIVATED A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 17 122AM 120013 ACV - CARGO DOOR 'AURAL' WARNING ACTIVATED DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. OPENED CARGO DOOR AN D INSPECTED. NO DEFECTS NOTED. RESECURED DOOR AND PERFORMED AURAL WARNING CHECK. SYSTEM OPERATIONAL CHECK NORMAL. UN ABLE TO DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996030100456 19960301 00456 EU 1996 3 1 WTAA960020 1 19960129 A 3260 9005EN38 SWITCH BAG JETSTM JETSTM3101 1500215 EU NLG DIRTY A WTAA O OTHER N FALSE WARNING AP APPROACH 1 WP 17 401UE 729 SFO - INTERMITTENT NOSE LANDING GEAR INTRANSIT LIGHT INDICATION REPORTED. MAINTENANCE INSPECTED, CLEANED AND LUBRICATED NOSE LANDING GEAR DOWNLOCK MICROSWITCH. GEAR INDICATION OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996030100457 19960301 00457 EU 1996 3 1 WTAA960021 1 19960129 A 3260 9005EN38 SWITCH BAG JETSTM JETSTM3101 1500215 EU LT MLG INTERMITTENT A WTAA K NONE N FALSE WARNING AP APPROACH 1 WP 17 427UE 811 SEAT - INTERMITTENT LEFT MAIN LANDING GEAR INTRANSIT LIGHT INDICATIONS REPORTED. MAINTENANCE REMOVED AND REPLACED LEFT MAIN LANDING GEAR DOWNLOCK MICROSWITCH. GEAR INDICATIONS NORMAL DURING OPERATIONAL CHECK. AIRCRAFT RETURNED TO SERVICE . (M) 2 L 7 2 4T RT A21EU 1996030100458 19960301 00458 SO 1996 3 1 WTAA960022 1 19960129 A 3260 922AA2YA6P PROX SENSOR EMB 120 EMB120RT SO RT MLG FAILED A WTAA O OTHER N FALSE WARNING AP APPROACH 1 WP 17 216YV 120216 FAT - RIGHT MAIN LANDING GEAR 'A' SYSTEM INTRANSIT LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION AND EXTENSION. CREW USED EMERGENCY GEAR EXTENSION PROCEDURES TO ASSURE PROPER GEAR EXTENSION PRIOR TO LANDING. AIRCRAFT LANDED WITHOUT INC IDENT. MAINTENANCE REPLACED RIGHT MAIN LANDING GEAR 'A' SYSTEM DOWNLOCK PROXIMITY SENSOR. LANDING GEAR POSITION INDICA TION SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996030100459 19960301 00459 SO 1996 3 1 WTAA960023 1 19960130 A 3260 922AA2YA6P PROX SENSORS EMB 120 EMB120RT SO RT MLG DIRTY CONNECTION A WTAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 17 201YW 120201 LAX - RIGHT MAIN LANDING GEAR 'A' SYSTEM RED INTRANSIT LIGHT REMAINED ILLUMINATED FOLLOWING GEAR RETRACTION. AIRCRAFT R ETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE SWAPPED 'A' AND 'B' SYSTEM ELECTRICAL CONNECTORS. DEFERRED 'A' SYSTEM PROXIMITY INDICATION PER MEL 32-60-1. AIRCRAFT RETURNED TO SERVICE. NOTE, MAINTENANCE CLEARED PREVIOUSLY DEFERRED ITE M BY CLEANING THE ELECTRICAL CONNECTORS AT THE RIGHT MAIN GEAR 'A' SYSTEM PROXIMITY SENSORS. (M) 2 L 7 2 4T RT A31SO 1996030100460 19960301 00460 SO 1996 3 1 WTAA960024 1 19960203 A 2750 3075001017 FLAP CONTL UNIT EMB 120 EMB120RT SO COCKPIT FAILED A WTAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 17 454UE 120155 FAT - EN ROUTE SFO TO SBA, FLAP ASYMMETRY REPORTED IN LEVEL FLIGHT AT FL 230. LEFT NACELLE FLAP AT 15 DEGREES. AIRCRAF T DIVERTED TO FAT, LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED FLAP CONTROL UNIT. FLAP SYSTEM OPERATIONAL CHECK NOR MAL ON GROUND. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996030100461 19960301 00461 EU 1996 3 1 WTAA960025 1 19960202 A 5242 137328C414 E/E DOOR BAG JETSTM JETSTM3101 1500215 EU FWD FUSELAGE DAMAGED A WTAA K NONE C F.O.D. AP APPROACH 1 WP 17 431UE 813 SJC - BIRD STRIKE REPORTED ON FINAL APPROACH FOR LANDING. MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECTION ON AIRCRAFT. DAMAGE LIMITED TO RIGHT AVIONICS BAY DOOR. ACCOMPLISHED TEMPORARY REPAIR TO DOOR AND FERRIED AIRCRAFT TO FAT FOR FINAL REPAIRS. FAT MAINTENANCE REMOVED AND REPLACED RIGHT AVIONICS BAY DOOR. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996030100462 19960301 00462 EU 1996 3 1 WTAA960026 1 19960204 A 2611 72111211000 SMOKE DETECTOR BAG JETSTM JETSTM3101 1500215 EU BAGGAGE COMPT MOISTURE A WTAA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 WP 17 422UE 782 SFO - SMOKE DETECTION LIGHT ACTIVATED ON TAXI-OUT. AIRCRAFT RETURNED TO GATE. LIGHT EXTINGUISHED UPON ENGINE SHUTDOWN. NO SMOKE OR FIRE DETECTED. DETERMINED TO BE FALSE INDICATION. CLEANED MOISTURE FROM SMOKE DETECTOR CANNON PLUG. SMO KE DETECTION SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996030100463 19960301 00463 EU 1996 3 1 WTAA960027 1 19960128 A 5350 RADOME BAG JETSTM JETSTM3101 1500215 EU FWD FUS BIRD STRIKE A WTAA K NONE C F.O.D. NR NOT REPORTED 1 WP 17 422UE 782 SFO - BIRD STRIKE REPORTED AT NOSE AREA OF AIRCRAFT. MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECTION ON AIRCRAFT. NO D EFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996030100464 19960301 00464 EU 1996 3 1 WTAA960028 1 19960131 A 2611 72111211000 SMOKE DETECTOR BAG JETSTM JETSTM3101 1500215 EU BAGGAGE COMPT DIRTY A WTAA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 WP 17 422UE 782 SFO - SMOKE DETECTION LIGHT ACTIVATED ON TAXI-OUT. AIRCRAFT RETURNED TO GATE. NO SMOKE OR FIRE DETECTED. DETERMINED T O BE FALSE INDICATION. CLEANED SMOKE DETECTOR. SMOKE DETECTION SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996030100465 19960301 00465 NE 1996 3 1 96ZZZX827 2 19960112 A 7200 ENGINE BOEING 767 767205 1385121 NM PWA JT9 JT9D7R4D 52054 NE NR 1 SURGED A TWAA O OTHER O OTHER CL CLIMB 1 CE 05 650TW 23057 SEA - FLT 740 - DURING CLIMB, NR 1 ENGINE, S/N 4603, SURGED. POWER WAS REDUCED TO IDLE. CHANGED NR 1 ENGINE. ENGINE T OTAL TIME: 29,752 HOURS; 8,040 CYCLES. CHECK C-4C - 10-25-95 - LAX. 2 L 7 2 4F 4 F RT A1NM E3NE 1996030100468 19960301 00468 NE 1996 3 1 MZZA96001 2 19960110 A 7260 NAS5514H UNION BOEING 727 727224 1384076 NM PWA JT8 JT8D17 52049 NE NR 1 ENGINE WORN A MZZA J A E DUMP FUEL UNSCHED LANDING ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 13 79744 22253 GUM - FLT 956 - NR 1 ENGINE ON CLIMB-OUT STARTED WITH 4 GALLONS OF OIL AND THEN DEPLETED TO 1 GALLON. OIL TEMPERATURE R OSE TO 120 DEGREES. PRECAUTIONARY SHUT ENGINE DOWN AND AIR RETURN TO GUAM. MAINTENANCE FOUND OIL LINE GEARBOX UNION FI TTING LOOSE LOCATED ABOVE THE MAIN OIL FILTER HOUSING. MAINTENANCE REPLACED THE UNION FITTING. ENGINE RUN-UP CHECK AT 90 PERCENT N2 FOR 5 MINUTES AT 55 PSI OIL PRESSURE AND NO LEAK FOUND. (X) 2 L 7 3 4F 4 F A3WE E2EA 1996030100469 19960301 00469 EU 1996 3 1 USAA960063 1 19960226 A 5312 BULKHEAD ANGLE FOKKER F28 F28MK0100 4990807 EU BS 14911 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 865US 15805 11308 PIT - DURING Q- CHECK, FOUND 1 INCH CRACK IN ANGLE AT CTR PRESSURE BULKHEAD ANGLE CRACK, STRINGER 64 RHS, STATION 14911. VISUALLY DETECTED AND VERIFIED BY NDT. INSTALLED REPAIR ANGLES PER USAIR EA NR 46216. (M) 2 L 7 2 4F RT 1996030100502 19960301 00502 CE 1996 3 1 96ZZZX861 1 19960126 A 5751 122005211 HINGE CESSNA 206 TU206G 2073357 CE LT OTBD AILERON CRACKED E A SQPA K NONE O OTHER IN INSP/MAINT 1 NM 11 756WZ U20604427 THE LT AND RT OUTBOARD AILERON HINGES WERE FOUND CRACKED AT THE LOWER MOUNTING FLANGE AREA. SUBMITTER ASSUMES FATIGUE A S CAUSE AND RECOMMENDS CAREFUL INSPECTION OF HINGE THROUGH THE TRAILING EDGE FALSE SPAR. 1 H 7 1 3O A4CE 1996030100503 19960301 00503 CE 1996 3 1 96ZZZX862 1 19960126 A 5751 122005212 HINGE CESSNA 206 TU206G 2073357 CE RT OTBD AILERON CRACKED E SQPA K NONE O OTHER IN INSP/MAINT 1 NM 11 756WZ U20604427 THE LT AND RT OUTBOARD AILERON HINGES WERE FOUND CRACKED AT THE LOWER MOUNTING FLANGE AREA. SUBMITTER ASSUMES FATIGUE A S CAUSE AND RECOMMENDS CAREFUL INSPECTION OF HINGE THROUGH THE TRAILING EDGE FALSE SPAR. 1 H 7 1 3O A4CE 1996030100534 19960301 00534 WP 1996 3 1 9604349155 1 19960114 A 5320 DOUBLER DOUG DC9 DC914 3022034 WP PAX DOOR JAMB CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8914E 458314 DURING H-CHECK, FOUND CRACKS IN THE FORWARD ENTRY DOOR JAMB, SID PSE 53.09.031 DOOR STOP DOUBLERS AFT SIDE, 4TH AND 5TH STOPS FROM THE BOTTOM. REPAIRED JAMB PER EA 91-103367. 2 L 7 2 4F A6WE 1996030100535 19960301 00535 WP 1996 3 1 9604359155 1 19960124 A 5311 FRAME DOUG DC9 DC914 3022034 WP FS 817 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8914E 45831 DURING H-CHECK, FOUND CORROSION IN THE FS 817 FRAME AT THE RIGHT CUSP. REPAIRED FRAME (P/N 5910163-73) PER EA 91-102643 . 2 L 7 2 4F A6WE 1996030100536 19960301 00536 WP 1996 3 1 9604369155 1 19960125 A 5320 SUPPORT DOUG DC9 DC914 3022034 WP FS 160-164 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8914E 45831 DURING H-CHECK, FOUND CORROSION ON THE FLOOR SUPPORTS AT FS 160, LBL 12 TO 56 AND AT LBL 12, FS 160 TO 164. REPAIRED SU PPORTS PER EA 91-106634. 2 L 7 2 4F A6WE 1996030100537 19960301 00537 WP 1996 3 1 9604379155 1 19960125 A 5312 BULKHEAD DOUG DC9 DC914 3022034 WP FS 110 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8914E 45831 DURING H-CHECK, FOUND CORROSION ON THE HORIZONTAL PRESSURE PANEL AT FS 110, RIGHT SIDE BETWEEN THE TWO VERTICAL FITTINGS . REPAIRED PANEL PER EA 91-106633. 2 L 7 2 4F A6WE 1996030100538 19960301 00538 WP 1996 3 1 9604389865 1 19960126 A 5315 FLOORBEAM DOUG DC9 DC951 3022051 WP FS 1136 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 774NC 47776 DURING H-CHECK, FOUND CORROSION ON THE FS 1136 FLOORBEAM AT APPROXIMATELY RBL 18. REPAIRED BEAM PER EA 98-106626. 2 L 7 2 4F A6WE 1996030100539 19960301 00539 NM 1996 3 1 9604396730 1 19960127 A 5320 ANGLE BOEING 747 7472J9F 1384806 NM FS 490 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 630US 21668 DURING P-CHECK, FOUND CORROSION ON THE MAIN DECK FLOOR LEFT SIDE WALL ANGLE BS 490. REPAIRED ANGLE PER EA 67-99390. 2 L 7 4 4F RT A20WE 1996030100540 19960301 00540 WP 1996 3 1 9604409102 1 19960131 A 5315 FLOORBEAM DOUG DC9 DC915 3022036 WP FS 237 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 92S 47064 DURING H-CHECK, FOUND A TWO INCH CRACK IN THE FS 237 FLOORBEAM AT LBL 6. REPAIRED BEAM (P/N 9911544-5) PER EA 99-102644 . 2 L 7 2 4F A6WE 1996030100541 19960301 00541 NM 1996 3 1 9604416730 1 19960131 A 5347 SEAT TRACK BOEING 747 7472J9F 1384806 NM FS 2240 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 630US 21668 DURING P-CHECK, FOUND CORROSION ON THE MAIN DECK SEAT TRACK AT BS 2240, LBL 11. REPAIRED TRACK PER EA 67-99392. 2 L 7 4 4F RT A20WE 1996030100542 19960301 00542 NM 1996 3 1 9604426730 1 19960201 A 5711 SPAR WEB BOEING 747 7472J9F 1384806 NM WS 1488-1500 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 630US 21668 DURING P-CHECK, FOUND CORROSION ON THE RIGHT WING FRONT SPAR WEB AT FS 1488 AND 1500. REPAIRED WEB (P/N 65B22749-3) PER EA 67-99419. 2 L 7 4 4F RT A20WE 1996030100543 19960301 00543 NM 1996 3 1 9604436730 1 19960203 A 5711 SPAR WEB BOEING 747 7472J9F 1384806 NM WS 1022 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 630US 21668 DURING P-CHECK, FOUND CORROSION ON THE LEFT WING FRONT SPAR WEB AT FS 1022. REPAIRED WEB (P/N 65B22851-1) PER EA 67-993 91. 2 L 7 4 4F RT A20WE 1996030100544 19960301 00544 NM 1996 3 1 9604446730 1 19960205 A 5315 FLOORBEAM BOEING 747 7472J9F 1384806 NM FS 460 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 630US 21668 DURING P-CHECK, FOUND CORROSION ON THE MAIN DECK FLOORBEAM UPPER CHORD AT BS 460, RBL 86. REPAIRED CHORD (P/N 65B10342- 538) PER EA 67-99394. 2 L 7 4 4F RT A20WE 1996030100545 19960301 00545 WP 1996 3 1 9604459102 1 19960206 A 5313 LONGERON DOUG DC9 DC915 3022036 WP FS 897 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 92S 47064 DURING H-CHECK, FOUND A .5 INCH CRACK IN LONGERON 2R AT FS 897. REPAIRED LONGERON (P/N 5911432-3) PER EA 91-102046. 2 L 7 2 4F A6WE 1996030100546 19960301 00546 WP 1996 3 1 9604469152 1 19960208 A 5341 FITTING DOUG DC9 DC914 3022034 WP FS 494 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8911E 45825 DURING H-CHECK, FOUND A CRACK IN THE LOWER WING TO FUSELAGE ATTACH FITTING AT FS 494 BETWEEN LONGERONS 22L TO 23L. REPL ACED FITTING (P/N 5910006-43) PER EA 91-109372. 2 L 7 2 4F A6WE 1996030100547 19960301 00547 NM 1996 3 1 9604472762 1 19960208 A 5313 LONGERON BOEING 727 7272M7 138407S NM FS 970-990 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 722RW 21201 DURING H-CHECK, FOUND CORROSION ON STR 29L FROM BS 970 TO 990. REPAIRED STRINGER (P/N 65-56441) PER EA 27-103457. 2 L 7 3 4F A3WE 1996030100548 19960301 00548 NM 1996 3 1 9604482762 1 19960209 A 5313 LONGERON BOEING 727 7272M7 138407S NM FS 950 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 722RW 21201 DURING H-CHECK, FOUND CORROSION ON STR 27L FROM BS 950E TO 950F. REPAIRED STRINGER (P/N 65-56245-39) PER EA 27-103456. 2 L 7 3 4F A3WE 1996030100549 19960301 00549 WP 1996 3 1 9604499762 1 19960210 A 5311 FRAME DOUG DC9 DC941 302207N WP FS 1072 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 762NW 47395 DURING H-CHECK, FOUND CORROSION IN THE FS 1072 FRAME AT THE AFT PRESSURE BULKHEAD LOWER LEFT SIDE. REPAIRED FRAME (P/N 5910163-73) PER EA 97-102648. 2 L 7 2 4F A6WE 1996030100550 19960301 00550 NM 1996 3 1 9604502762 1 19960213 A 5315 FLOORBEAM BOEING 727 7272M7 138407S NM FS 1130 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 722RW 21201 DURING H-CHECK, FOUND CORROSION ON THE BS 1130 FLOORBEAM UPPER AND LOWER CHORDS BETWEEN LBL 39 AND RBL 51. REPAIRED CHO RDS (P/N 65-20821) UPPER, (P/N 65-20838-17) LOWER, PER EA 27-103458 AND -103454 RESPECTIVELY. 2 L 7 3 4F A3WE 1996030100551 19960301 00551 WP 1996 3 1 9604519762 1 19960214 A 5320 SUPPORT DOUG DC9 DC941 302207N WP FS 237-256 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 762NW 47395 DURING H-HECK, FOUND CORROSION ON THE FLOOR SUPPORT FROM FS 237 TO 256, BL 0. REPAIRED SUPPORT (P/N 5910760-11) PER EA 97-109375. 2 L 7 2 4F A6WE 1996030100552 19960301 00552 WP 1996 3 1 9604529605 1 19960215 A 5320 FITTING DOUG DC9 DC932 3022066 WP FS 996 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 605NW 47223 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LONGERON 26R END FITTING AT FS 996. REPLACED FITTI NG PER SRM 51-01. 2 L 7 2 4F A6WE 1996030100553 19960301 00553 WP 1996 3 1 9604539152 1 19960215 A 5312 BLKHD DOOR JAMB DOUG DC9 DC914 3022034 WP AFT CABIN CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8911E 45825 DURING H-CHECK, FOUND TWO CRACKS IN THE AFT CABIN DOOR JAMB SEAL RETAINER RING LEFT AND RIGHT SIDES AT APPROXIMATELY THE 3 AND 9 O'CLOCK POSITIONS. REPAIRED JAMB PER EA 91-109376. 2 L 7 2 4F A6WE 1996030100554 19960301 00554 WP 1996 3 1 9604549152 1 19960216 A 5320 DOUBLER DOUG DC9 DC914 3022034 WP FS 536 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8911E 45825 DURING H-CHECK, FOUND CORROSION ON THE LEFT FUSELAGE WINDOW BELT DOUBLER AT FS 536 BETWEEN THE SKIN AND THE WINDOW RETAI NER. REPAIRED DOUBLER (P/N 9911535) PER EA 91-109376. 2 L 7 2 4F A6WE 1996030100555 19960301 00555 WP 1996 3 1 9604559152 1 19960216 A 5330 SKIN DOUG DC9 DC914 3022034 WP FS 199 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8911E 45825 DURING H-CHECK, FOUND A .375 INCH CRACK IN THE FORWARD ENTRY DOOR JAMB FS 199 AT THE 5TH STOP HOLE FROM THE BOTTOM. REP AIRED JAMB SKIN (P/N 5911406-59) PER EA 91-109374. 2 L 7 2 4F A6WE 1996030100556 19960301 00556 WP 1996 3 1 9604569152 1 19960216 A 5713 LONGERON DOUG DC9 DC914 3022034 WP WS 69-91 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8911E 45825 DURING H-CHECK, FOUND CORROSION IN THE RIGHT WING STRINGERS 18, 21 AND 22 APPROXIMATELY STA 69 TO 91. REPAIRED PER EA 9 1-109380. 2 L 7 2 4F A6WE 1996030100557 19960301 00557 NM 1996 3 1 9604672716 1 19960209 A 5712 RIB CHORD BOEING 727 7272S7 138407Z NM FS 760 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 720RC 22491 DURING PERIODIC CHECK, FOUND CRACKS IN THE BS 760 WING TO BODY UPPER RIB CHORD, UPPER AND LOWER FORWARD FASTENER HOLES. REPAIRED CHORD (P/N 65-18522-16) PER EA 27-103441. 2 L 7 3 4F A3WE 1996030100558 19960301 00558 WP 1996 3 1 9604689758 1 19960215 A 5744 FITTING DOUG DC9 DC941 302207N WP SPOILER CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 758NW 47286 DURING SPECIAL MAINTENANCE VISIT, FOUND A CRACK IN THE SPOILER SUPPORT FITTING BETWEEN THE INBOARD AND OUTBOARD SPOILERS . REPLACED FITTING PER SRM 51-30-2. 2 L 7 2 4F A6WE 1996030100559 19960301 00559 WP 1996 3 1 9604699853 1 19960217 A 5412 BULKHEAD DOUG DC9 DC951 3022051 WP NR 2 PYLON CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 762NC 47710 DURING LINE CHECK, FOUND A CRACK IN THE NR 2 ENGINE PYLON OUTER BULKHEAD. REPAIRED BULKHEAD (P/N 9958159-62) PER EA 98- 099525. 2 L 7 2 4F A6WE 1996030100560 19960301 00560 NM 1996 3 1 9604706601 1 19960219 A 5320 FITTING BOEING 747 747151 1384891 NM FS 1480 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 601US 19778 DURING P-CHECK, FOUND CORROSION ON THE BS 1480 BULKHEAD TO THE KEEL BEAM TORQUE BOX DRAG FITTING IN THE RIGHT BODY LANDI NG GEAR WHEEL WELL. REPLACED FITTING. 2 L 7 4 4F A20WE 1996030100561 19960301 00561 EU 1996 3 1 9604843221 1 19960222 A 2700 3945122502 COMPUTER AIRBUS 320 A320211 3930320 EU NR 2 ELEV/AIL MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 321US 262 DURING TAKEOFF ROLL, RECEIVED F/CTL ELAC 2 PITCH FAULT MESSAGE. TAKEOFF WAS ABORTED AT APPROXIMATELY 80 KNOTS. AIRCRAF T RETURNED TO THE GATE WHERE MAINTENANCE REPLACED THE NR 2 ELEVATOR AILERON COMPUTER, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996030100562 19960301 00562 WP 1996 3 1 9604859160 1 19960215 A 3260 DOOR LIGHT DOUG DC9 DC914 3022034 WP LANDING GEAR ILLUMINATED A NWAA L ABORTED APPROACH N FALSE WARNING DE DESCENT 1 GL 01 8903E 45744 DURING DESCENT, LANDING GEAR EXTENDED BUT DOOR OPEN LIGHT REMAINED ILLUMINATED. PERFORMED GO-AROUND AND LIGHT EXTINGUIS HED. TOWER INDICATED ALL LOOKED OK AND AIRCRAFT LANDED WITHOUT INCIDENT. TROUBLESHOOTING FOUND NO TROUBLE, DOOR OPERAT IONALLY CHECKED GOOD. 2 L 7 2 4F A6WE 1996030100563 19960301 00563 WP 1996 3 1 9604869860 1 19960227 A 3222 STRUT DOUG DC9 DC951 3022051 WP NLG REQD SERVICE A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 769NC 47757 DURING CLIMBOUT, UNABLE TO RETRACT LANDING GEAR AND AIRCRAFT PLACED IN FLIGHT MODE MANUALLY. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. NOSE STRUT WAS FOUND FLAT ON RETURN TO GATE. SERVICED NOSE STRUT AND CHECKED GOOD. 2 L 7 2 4F A6WE 1996030100564 19960301 00564 WP 1996 3 1 9604879160 1 19960226 A 3230 RETRACT MECH DOUG DC9 DC914 3022034 WP LANDING GEAR LACK OF LUBE A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 8903E 45744 DURING CLIMBOUT UPON FLAP RETRACTION, TAKEOFF WARNING SOUNDED, PRESSURIZATION FAILED AND SPOILER DO NOT USE LIGHT ILLUMI NATED. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPACKED STRUT, CLEANED AND LUBRICATED GROUND SHIFT LINKAGE . GEAR OPERATIONALLY CHECKED GOOD. 2 L 7 2 4F A6WE 1996030100565 19960301 00565 WP 1996 3 1 96DHL804002 1 19960127 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 940 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 DURING C-CHECK, FLOORBEAM AT STA 940, RIGHT HAND LIGHTENING HOLE CRACKED. REMOVED FASTENER AT END OF CRACK, OVERSIZED H OLE TO .248, FABRICATED DOUBLER ALODINED AND PRIMED. INSTALLED DOUBLER PER SRM 51-01-08 AND EO 25260-5108. 2 L 7 4 4F RT 4A25 1996030100566 19960301 00566 NM 1996 3 1 96FDEA00266 1 19960216 A 5320 CLIP BOEING 727 72722 1384002 NM BS 380 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION (C53-111-01-1), STRINGER CLIP STR 24L BS 380. REMOVED AND REPLACED STR CLIP AT STR 24L BS 380. 2 L 7 3 4F A3WE 1996030100567 19960301 00567 NM 1996 3 1 96FDEA00327 1 19960227 A 7931 7900030 PRESS SWITCH BOEING 727 727233 138408A NM NR 2 ENGINE FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 258FE 20940 DURING CLIMB, THE NR 2 LOW OIL PRESSURE FILTER BYPASS LIGHT ILLUMINATED. THE THRUST LEVER WAS RETARDED AND THE LIGHT WE NT OUT AT EPR BUT AFTER A FEW MINUTES THE LIGHT CAME ON AGAIN AND REMAINED ON. THE ENGINE WAS SHUTDOWN, ALL ENGINE READ INGS WERE NORMAL, NR 2 OIL PRESS AT 45 PSI. REMOVED AND REPLACED NR 2 MAIN OIL FILTER, LOP SWITCH NR 2 ENGINE AND NR 2 ENGINE FILTER BYPASS SWITCH. RAN NR 2 ENGINE OPS AND LEAK OK. 2 L 7 3 4F RT A3WE 1996030100568 19960301 00568 NM 1996 3 1 96FDEA00328 1 19960226 A 5320 CHANNEL BOEING 727 72722 1384002 NM BS 1057-1110 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION (C53-111-01, -3), ON NR 2 CARGO DOORWAY C-CHANNEL BS 1057 TO 1110 RBL 27 WL 147. REMOVED AND REPLACED C-CHANN EL AT DOORWAY. 2 L 7 3 4F A3WE 1996030100569 19960301 00569 NM 1996 3 1 96FDEA00329 1 19960226 A 5315 65208279 FLOORBEAM BOEING 727 72722 1384002 NM BS 640 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION (C53-111-01, -2), ON LOWER FLANGE OF FLOORBEAM BS 640 RBL 23 TO 26.7 WL 200. REMOVED CORROSION ON LOWER FLANG E OF FLOORBEAM IN NUTPLATE HOLES AT BS 640 LBL 20 TO RBL 26 WL 200. FOUND TO BE OUT OF LIMITS AT RBL 23 TO RBL 26.5, RE PAIRED IT AS PER FEDEX SRM 53-10-8. 2 L 7 3 4F A3WE 1996030100570 19960301 00570 NM 1996 3 1 96FDEA00330 1 19960226 A 5311 FRAME BOEING 727 72722 1384002 NM BS 580 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 THE FRAME AT BS 580 IS CRACKED ON I/B FLANGE AT RBL 67 WL 210. THE FRAME AT BS 580 RBL 67 WL 210 WAS FOUND TO BE DAMAGE D BEYOND LIMITS PER FEDEX SRM 53-10-1. REPAIRED FRAME PER FEDEX SRM 51-40-3. 2 L 7 3 4F A3WE 1996030100571 19960301 00571 NM 1996 3 1 96FDEA00331 1 19960228 A 2740 R1631M1 TRIM MOTOR BOEING 727 72722 1384002 NM VERT STAB FAILED A FDEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 25 147FE 19080 AFTER TAKEOFF, MAIN STABILIZER TRIM FAILED. RESET CIRCUIT BREAKER TO NO AVAIL, CRUISE TRIM WORKED NORMALLY. REPLACED M AIN ELECTRIC STABILIZER TRIM MOTOR PER MM 27-40-31 PAGE 201, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1996030100572 19960301 00572 NM 1996 3 1 96FDEA00332 1 19960226 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM BS 540 DOUBLE DRILLED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 WHILE WORKING CARD NR0683, FOUND BS 540 FLOORBEAM BL 0 WL 208 TO HAVE DOUBLE HOLE. REPAIRED FLOORBEAM AT BS 540 BL 0 WL 208 IAW FEDEX SRM 53-10-8. 2 L 7 3 4F A3WE 1996030100573 19960301 00573 NM 1996 3 1 96FDEA00333 1 19960226 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM BS 580 DOUBLE DRILLED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 WHILE WORKING CARD NR0683, FOUND BS 580 FLOORBEAM BL 0 WL 208 TO HAVE DOUBLE HOLE. REPAIRED DOUBLE HOLE PER FEDEX SRM 5 3-10-8. 2 L 7 3 4F A3WE 1996030100574 19960301 00574 NM 1996 3 1 96FDEA00334 1 19960226 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM BS 600 DOUBLE DRILLED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 WHILE WORKING CARD NR0683, FOUND BS 600 FLOORBEAM BL 0 WL 208 TO HAVE DOUBLE HOLE. REPAIRED FLOORBEAM BS 600 BL 0 WL 20 8 IAW FEDEX SRM 53-10-8. 2 L 7 3 4F A3WE 1996030100575 19960301 00575 NM 1996 3 1 96FDEA00335 1 19960226 A 5330 SKIN BOEING 727 72722 1384002 NM FUSELAGE CORROSIOIN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 BS 1110 STR 26, THERE IS BULGE IN SKIN TRIPLER DAMAGED OUT OF LIMITS. REPLACED BONDED DOUBLER AT BS 1148 TO 1166 STR 25 TO 26R. REPLACED BONDED TRIPLER FROM BS 1108 TO 1130 STR 25 TO 26R. REPAIRED REMAINING DEBONDED SKIN USING FIXED PAT TERN PER FEDEX SRM 53-30-4, FROM BS 1110 TO 1183. 2 L 7 3 4F A3WE 1996030100576 19960301 00576 NM 1996 3 1 96FDEA00336 1 19960226 A 5320 WEB BOEING 727 72722 1384002 NM BS 303-309 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION (C53-111-01-1), ON DOGHOUSE WEB STA 303 TO 309 LT LBL 15 WL 177. REMOVED CORROSION FOUND MATERIAL LOSS WAS WI THIN LIMITS PER SRM 53-10-1. TREATED AREA, PRIMED AND REINSTALLED FASTENERS. 2 L 7 3 4F A3WE 1996030100577 19960301 00577 NM 1996 3 1 96FDEA00337 1 19960226 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM BS 500 DOUBLE DRILLED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 DOUBLE HOLE IN FLOORBEAM BS 500 BL 0 WL 208.1. REPAIRED DOUBLER HOLE AT BS 500 BL 0 WL 208 IAW FEDEX SRM 53-10-8. 2 L 7 3 4F A3WE 1996030100578 19960301 00578 NM 1996 3 1 96FDEA00338 1 19960226 A 5330 SKIN BOEING 727 72722 1384002 NM BS 945 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 GOUGE IN EXTERIOR SKIN BS 945 STR 9R. REMOVED DAMAGED SKIN, BS 945 STR 9R. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FEDEX SRM 53-30-3. 2 L 7 3 4F A3WE 1996030100579 19960301 00579 NM 1996 3 1 96FDEA00339 1 19960226 A 5320 WEB BOEING 727 72722 1384002 NM BS 294-355 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION ON WEB AT BS 294.5 TO 355 RBL 10 TO 35 WL 169. CORROSION FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED WEB PER SRM 51-40-02. 2 L 7 3 4F A3WE 1996030100580 19960301 00580 NM 1996 3 1 96FDEA00340 1 19960226 A 5313 STRINGER BOEING 727 72722 1384002 NM BS 930 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION (C53-224-01, -2), ON STR 9R BS 930 PLUS 7 RT AREA IS OUT OF LIMITS. REPAIRED STR 9R IAW FEDEX SRM 53-10-3. 2 L 7 3 4F A3WE 1996030100581 19960301 00581 NM 1996 3 1 96FDEA00341 1 19960226 A 5312 BLKHD WEB BOEING 727 72722 1384002 NM BS 950 CUT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 WHILE WORKING NR0788, FOUND A CUT IN 950 BULKHEAD VERTICAL WEB BL 0 WL 208 AFT SIDE. REPAIRED CUT IN 950 BULKHEAD VERTI CAL WEB AT BL 0 WL 208 AFT SIDE PER FEDEX SRM 53-10-9 FIG 2. 2 L 7 3 4F A3WE 1996030100582 19960301 00582 NM 1996 3 1 96FDEA00342 1 19960226 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM BS 1110 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION (C53-111-01, -3), ON LOWER CHORD OF 1110 FLOORBEAM WL 200 LBL 2 TO 30 AT NUTPLATE HOLES. REMOVED AND REPLACED CORRODED LOWER CHORD OF BS 1110 FLOORBEAM AT WL 200 RBL 4 TO LBL 19.75 WITH FABRICATED REPAIR PARTS PER SRM 53-10-8 FIG 2. 2 L 7 3 4F A3WE 1996030100583 19960301 00583 WP 1996 3 1 96FDEA00343 1 19960224 A 5753 SKIN DOUG DC10 DC1030 3023501 WP LT TE FLAP CRACK A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 320FE 47835 LT WING O/B FLAP, I/B UPPER SURFACE T/E SKIN HAS 5 INCH CRACK. REPAIRED PER SRM 57-10-00 PG 10 FIG 7. 2 L 7 3 4F A22WE 1996030100584 19960301 00584 NM 1996 3 1 96FDEA00344 1 19960226 A 5330 6554572 SKIN BOEING 727 727233 138408A NM BS 480 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 266FE 21672 DENT IN SKIN BS 480 BETWEEN STR 22 TO 23R. *S/D* TRIMMED OUT DENT IN SKIN AT BS 480 BETWEEN STRINGER, 22 TO 23R, FABRI CATED AND INSTALLED EXTERNAL REPAIR DOUBLER PER FEDEX SRM 53-30-3. 2 L 7 3 4F RT A3WE 1996030100585 19960301 00585 NM 1996 3 1 96FDEA00345 1 19960226 A 5320 6518915 CHORD BOEING 727 727233 138408A NM BS 360-344 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 266FE 21672 CORROSION (C53-100-01-1) ON UPPER I/B FLANGE OF LOWER RT NOSE CHORD BS 360 TO 344 RBL 16 WL 145, ACCESS IS REQUIRED. *S /D* REMOVED RT LOWER NOSE CHORD AT BS 360 TO 275 RBL 16, WL 145 AND REPLACED CHORD, REINSTALLED ALL ITEMS REMOVED FOR A CCESS. 2 L 7 3 4F RT A3WE 1996030100586 19960301 00586 NM 1996 3 1 96FDEA00346 1 19960226 A 5314 6518636 KEEL BEAM BOEING 727 727233 138408A NM BS 950 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 266FE 21672 CORROSION ON KEEL BEAM (STR 29L) AROUND FASTENERS COMMON TO THE SKIN AT BS 950. *S/D* REMOVED CORROSION FROM S-29L LEF THAND KEEL BEAM AT BS 950 AND REPAIRED AREAS IAW SRM 27-53-13. 2 L 7 3 4F RT A3WE 1996030100587 19960301 00587 NM 1996 3 1 96FDEA00347 1 19960226 A 5311 6516335 FRAME BOEING 727 727233 138408A NM BS 920 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 266FE 21672 CREASED DENT IN FRAME AT BS 920 BETWEEN STR 26 TO 25L. *S/D* REMOVED DAMAGE FRAME SECTION, INSTALLED REPAIR DOUBLER IA W FEDEX SRM 51-40-3. 2 L 7 3 4F RT A3WE 1996030100588 19960301 00588 NM 1996 3 1 96FDEA00348 1 19960226 A 5313 6515931 STRINGER BOEING 727 72722 1384002 NM BS 560 DAMAGE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 MECHANICAL DAMAGE ON STR 25L BS 560, WL 154. *S/D* REPAIRED DAMAGE STRINGER AT BS 560, STR 25L WL 154 PER FEDEX EA 7-5 310-27491. 2 L 7 3 4F A3WE 1996030100589 19960301 00589 NM 1996 3 1 96FDEA00349 1 19960228 A 2780 POSITION SWITCH BOEING 727 72725 1384006 NM NR 3 LE FLAP MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 156FE 18289 LEFT I/B LEADING EDGE DEVICE NR 3 WOULD NOT RETRACT AFTER TAKEOFF. RECYCLED TO 5 DEGREES AND BACK TO 2 DEGREES WITH NO RETRACTION. REPLACED NR 3 KREUGER FLAP POSITION SWITCH PER MM 27-82-1, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1996030100590 19960301 00590 NE 1996 3 1 96UAL900141 2 19960221 A 7530 1B1775 STATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE FAILED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 WP 29 555UA 26647 726636 DURING TAKEOFF, THE LEFT ENGINE FAILED AND SHUTDOWN. AIRCRAFT RETURNED TO FIELD. A CLUSTER OF VANES LIBERATED FROM THE .9375 STATOR ASSEMBLY, RESULTING IN SECONDARY DAMAGE CAUSING THE EGT TO RISE ABOVE LIMITS FORCING THE FLIGHT CREW TO SH UTDOWN THE ENGINE IN FLIGHT. NEW STYLE .9375 STATOR ASSEMBLIES WILL BE INSTALLED PER PWA SB 72-250 IN THE ENGINE AND AL L ADDITIONAL DAMAGE REPAIRED. 2 L 7 2 4F 4 F RT A2NM E17NE 1996030100591 19960301 00591 NM 1996 3 1 96UAL900145 1 19960223 A 3350 LIGHT BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOP A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 953UA 26700 AFT OVERWING EMERGENCY EXIT LIGHT ON LEFT SIDE OF AIRCRAFT INOP. RELAMPED, CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E21EU 1996030100592 19960301 00592 NE 1996 3 1 96UAL900146 2 19960226 A 7250 735903 BLADE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE FRACTURED A UALA E ENGINE SHUTDOWN E VIBRATION/BUFFET CL CLIMB 1 WP 29 7289U 21567 700021 DURING CLIMBOUT, HEARD LOUD SQUEAL AND VIBRATION FROM NR 2 ENGINE. EPR DROPPED OFF FROM 2.17 TO APPROXIMATELY 1.6 AND T HEN EGT BEGAN TO CLIMB RAPIDLY. PERFORMED ENGINE SHUTDOWN. ORIGIN OF FAILURE NOT DETERMINED DUE TO THE ENGINE OPERATIO N AFTER THE FAILURE. PROBABLE CAUSE IS STRESS RUPTURE OF T-3 BLADE DUE TO EXCESSIVE NOTCH WEAR AND ACCUMULATIVE CREEP D AMAGE. OVER TEMP ANALYSIS ON T-2 BLADES VERIFIED NO OVERTEMP EXISTED. A FULL REPAIR WAS ACCOMPLISHED. 2 L 7 3 4F 4 F A3WE E2EA 1996030100593 19960301 00593 NM 1996 3 1 96UAL900147 1 19960226 A 3350 POWER SUPPLY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7262U 21409 LT OVERWING EMERGENCY EXIT HATCH EXTERNAL LIGHT INOPERATIVE. REPLACED POWER SUPPLY DUE TO BATTERY CONNECTION TERMINAL B ROKEN OFF. 2 L 7 3 4F 4 F A3WE E2EA 1996030100594 19960301 00594 NM 1996 3 1 96UAL900148 1 19960227 A 5270 MR32033 SENSOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CARGO DOOR DIRTY A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 647UA 25284 AFTER TAKEOFF, RETURNED TO JFK DUE TO A FORWARD CARGO DOOR WARNING LIGHT. SUPPLEMENTAL DATA UPDATE: SENSORS S214 AND S 215 WERE DIRTY AND OUT OF ADJUSTMENT. CLEANED AND ADJUSTED SENSORS AND REPLACED PSEU DRIVER CARD (A3). ALL INDICATIONS NORMAL AFTER BITE CHECK. 2 L 7 2 4F 4 F RT A1NM E24NE 1996030100595 19960301 00595 NM 1996 3 1 96UAL900149 1 19960227 A 2410 735511A CSD BOEING 737 737322 1384676 NM NR 2 ENGINE FAILED A UALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 WP 29 343UA 24247 NUMBER TWO GENERATOR TRIPPED OFF LINE ON TAKEOFF AND UNABLE TO RESET. REPLACED NUMBER TWO ENGINE CONSTANT SPEED DRIVE A ND GENERATOR. RAN ENGINE, CHECKS OK. SHOP FINDINGS SHOWED THE CONSTANT SPEED DRIVE GOVERNOR TRIM HEAD AND BUSHING WAS LOOSE WHICH WOULD CAUSE IT TO LOCKUP. 2 L 7 2 4F RT A16WE 1996030100596 19960301 00596 NE 1996 3 1 96UAL900151 2 19960227 A 7261 BREATHER TUBE BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 3 BEARING CRACKED A UALA F E A ACTIVATE FIRE EXT. ENGINE SHUTDOWN UNSCHED LANDING A T FLAME/FIRE ENGINE CASE PENETRATION CL CLIMB 1 WP 29 4719U 19880 662778 FIRE WARNING IN NR 1 ENGINE. NR 3 BEARING BREATHER TUBE AT 1 O'CLOCK WAS FOUND TO BE CRACKED FORWARD OF SEAL RING GROOV ES. THIS CRACKED TUBE ALLOWED 15TH STAGE HOT AIR TO ENTER THE 7TH STAGE BUFFER AIR COMPARTMENT. 2 L 7 4 4F 4 F A20WE E20EA 1996030100597 19960301 00597 NM 1996 3 1 DL72K960443 1 19960221 A 5754 65162249092 RIB BOEING 727 727232 1384082 NM NR 8 RT SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 480DA 20860 UPON ROUTINE INSPECTION, THE I/B ACTUATOR RIB WAS FOUND TO BE DAMAGED. REPAIR WAS ACCOMPLISHED PER THE 727 M/M 57-54-0 FIG 804, FOR NR 8 L/E SLAT. 2 L 7 3 4F A3WE 1996030100598 19960301 00598 NM 1996 3 1 DL72L960434 1 19960223 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM R 1 DOOR CUTOUT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 514DA 21430 DURING INSPECTION, THE FUSELAGE SKIN, DOUBLER AND TRIPLER WERE FOUND CRACKED IN THE UPPER FWD CORNER OF THE R-1 DOOR CUT OUT. THE CRACK IS 0.5 LONG AND RAN FROM THE EDGE OF THE CUTOUT TO A LOCAL RIVET HOLE. IN ACCORDANCE WITH FAA 8110-3 FO RM, A TIME-LIMITED REPAIR DOUBLER WAS INSTALLED, PERMANENT REPAIRS TO BE ACCOMPLISHED AT MV-1 REF DL ERA 303210-14. 2 L 7 3 4F A3WE 1996030100600 19960301 00600 NM 1996 3 1 DL72S960437 1 19960226 A 5320 WEB BOEING 727 727232 1384082 NM TORQUE BOX CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 476DA 20753 TWO LIGHTENING HOLES IN RT VERT WEB OF AFT AIR STAIR TORQUE BOX WERE FOUND WITH CRACKS ROUTED PAST LIMITS. FOUND AT D-2 LTR CHECK AND REPAIRED PER MM 53-11-0. 2 L 7 3 4F A3WE 1996030100601 19960301 00601 NM 1996 3 1 DL72S960441 1 19960226 A 5754 651622295 RIB BOEING 727 727232 1384082 NM NR 3 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 477DA 20754 DURING INSPECTION, NR 3 L/E SLAT WAS FOUND WITH CRACKED RIB AT THE ANTI-ICE T-DUCT. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1996030100602 19960301 00602 NM 1996 3 1 DL72S960442 1 19960226 A 5754 651622295 RIB BOEING 727 727232 1384082 NM NR 3 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 477DA 20754 DURING INSPECTION, NR 3 L/E SLAT WAS FOUND WITH CRACKED RIB JUST O/B OF THE ACTUATOR ATTACH FITTING. REPAIRED PER MM 57 -54-0. 2 L 7 3 4F A3WE 1996030100603 19960301 00603 NM 1996 3 1 DL73E960433 1 19960131 A 5330 SKIN BOEING 737 737247 138448D NM FS 937 TORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 245WA 23519 A/C 372 WAS STRUCK BY A SERVICE VEHICLE RESULTING IN A 6 INCH TEAR AND GOUGE IN THE SKIN AT STA 937, BETWEEN S-21R AND S -22R. IN ACCORDANCE WITH B737-200 SRM 53-30-3 FIG 3, THE SKIN WAS REPAIRED. 2 L 7 2 4F A16WE 1996030100604 19960301 00604 NM 1996 3 1 DL73S960448 1 19960225 A 3260 189929 UPLOCK SENSOR BOEING 737 737232 1384475 NM RT MLG FAILED A DALA O OTHER N FALSE WARNING CR CRUISE 1 SO 27 327DL 23099 DURING CRUISE, RT MLG UNSAFE LIGHT ILLUMINATED WITH GEAR UP, ALL INDICATIONS NORMAL WITH GEAR DOWN. FERRIED TO SLC, REP LACED RT MLG UPLOCK SENSOR, SWUNG GEAR AND OPERATION NORMAL. 2 L 7 2 4F RT A16WE 1996030100605 19960301 00605 NM 1996 3 1 DL757960447 1 19960225 A 2920 6510 SWITCH BOEING 757 757232 1384965 NM RAT SYSTEM FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 614DL 22821 DURING INSPECTION, CONDUCTING RAM AIR TURBINE DEPLOYMENT TEST, TURBINE FAILED TO DEPLOY. REPLACED RAT DEPLOY PRESSURE S WITCH AND OPERATION NORMAL. 2 L 7 2 4F RT A2NM 1996030100606 19960301 00606 WP 1996 3 1 DLL10960438 1 19960226 A 3397 WIRE LKHEED 1011 10113851 5265010 WP CABIN BROKEN A DALA O OTHER L NO TEST CR CRUISE 1 SO 27 723DA 193C1150 LEFT FLOOR TRACK LIGHTS JUST AFT OF 2L DOOR, ROWS 20 TO 26 INOP. REPAIRED BROKEN WIRE IN FLOOR TRACK AT SEAT 27B AND OP ERATION NORMAL. 2 L 7 3 4F A23WE 1996030100607 19960301 00607 WP 1996 3 1 DLL17960444 1 19960216 A 5320 1512371105 DOUBLER LKHEED 1011 10113853 5265020 WP BS 620 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 766DA 193H1207 AT HMV, THE FWD OUTFLOW VALVE DOUBLER (P/N 1512371) WAS REPLACED DUE TO CORROSION AT THE FWD AND AFT CORNERS OF THE OUTF LOW VALVE CUTOUT. ACCOMPLISHED REPAIRS PER SRM 53-31-00. 2 L 7 3 4F A23WE 1996030100608 19960301 00608 NM 1996 3 1 DLM88960435 1 19960226 A 5330 5953050517 SKIN DOUG MD88 MD88 3023688 NM BS 256 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 THE FUSELAGE SKIN AT STA 256 BETWEEN STR 19L AND 20L WAS FOUND DENTED. THE DENT IS 6 INCH BY 6 INCH BY .25 DEEP AND DOE S NOT AFFECT THE UNDERLYING STRUCTURE. THE DENT WILL BE TRIMMED OUT AND REPAIRED IN ACCORDANCE WITH ERA 266789-14. 2 L 7 2 4F RT A6WE 1996030100609 19960301 00609 NM 1996 3 1 DLM90960450 1 19960225 A 2420 1B1901 TRANSFORMER DOUG MD90 MD9030 3023690 NM LT ELECT SYS FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 910DN 53390 ON FINAL APPROACH GEAR LOWERED, ENTIRE ELECTRICAL SYSTEM BEGAN TO CHATTER AND LIGHTS FLICKER. FLIGHT INSTRUMENT CRT'S B LANKED. SELECTED EMERGENCY POWER FLIGHT INSTRUMENTS AND OPERATION RETURNED. REMOVED LEFT CONVERTER UNIT AND LEFT TRANS FORMER. CLEANED LARGE AMOUNT OF DE-ICING FLUID FROM THE EQUIPMENT BAY. REPLACED CEU AND TRANSFORMER, NO HELP. FWD LEF T GEN TO MCO. EPCU FAULTS LT CONVERTER EU FAILED AND LT CONVERTER POWER FEEDER. REPLACED CEU AND FOUND CONV TRANSFORME R ASSEMBLY TO HAVE A BURNT ELECTRICAL SMELL. REPLACED SAME AND OPERATION NORMAL. 2 L 7 2 4F RT A6WE 1996030100610 19960301 00610 NM 1996 3 1 P5CA9600151 1 19960228 A 7931 60B001317 PRESS INDICATOR BOEING 747 747122 1384872 NM NR 3 ENGINE INOPERATIVE A P5CA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 853FT 19753 AFTER PUSHBACK, NR 3 ENGINE WAS STARTED AND OIL PRESSURE INDICATOR DID NOT INDICATE. REMOVED AND REPLACED OIL PRESSURE INDICATOR IAW MM 79-32-03, OPS CHECKS GOOD. 2 L 7 4 4F A20WE 1996030100611 19960301 00611 NM 1996 3 1 P5CA9600152 1 19960219 A 5730 SKIN BOEING 747 747123 1384873 NM WS 300 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 FOUND LEVEL ONE CORROSION ON LOWER LEFT WING SKIN AT APPROX STATION 300. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITH IN LIMITS. 2 L 7 4 4F A20WE 1996030100612 19960301 00612 NM 1996 3 1 QXEA9600076 1 19960226 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 841PH 82 COCKPIT PORTABLE LIGHT IS INOP. LIGHT AND HOLDER REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1996030100613 19960301 00613 EU 1996 3 1 QXEA9600077 1 19960226 A 5220 A26500701 DOOR FOKKER F28 F28MK1000 4990808 EU FWD FUSELAGE CRACKED CORNER A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 802PH 11017 PDX - SERVICE/EMERGENCY DOOR FRAME CRACKED AT LOWER FORWARD CORNER OUTER RADIUS. CRACK FOUND DURING C-CHECK. CRACK REP AIRED I/A/W EA 28-52-98. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996030100614 19960301 00614 EU 1996 3 1 QXEA9600078 1 19960226 A 5311 10305 FRAME FOKKER F28 F28MK1000 4990808 EU BS 10305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 802PH 42764 11017 PDX - LEFT FUSELAGE FRAME 10305 IS CRACKED AT RADIUS JUST ABOVE FLOOR LEVEL. CRACK FOUND DURING C-CHECK. CRACK REPAIRE D I/A/W EA 28-53-319. AIRCRAFT RETURNED TO SERVICE. AIRCRAFT TOTAL CYCLES, 46,017. 2 L 7 2 4F RT A20EU 1996030100615 19960301 00615 1996 3 1 QXEA9600079 4 19960226 A 2565 S130508 SLIDE FOKKER F28 F28MK1000 4990808 EU GALLEY LOW PRESS A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 802PH 2012 11017 PDX - FORWARD GALLEY EMERGENCY ESCAPE SLIDE BOTTLE PRESS FOUND LOW, 25 PSI. ITEM FOUND DURING C-CHECK. SLIDE REPLACED I/A/W MAINT MANUAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996030100616 19960301 00616 EU 1996 3 1 QXEA9600080 1 19960226 A 5312 BLKHD WEB FOKKER F28 F28MK1000 4990808 EU FWD PRESS BLKHD CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 802PH 11017 PDX - FRONT PRESSURE BULKHEAD CRACK IN AFT SIDE OF WEB AT HORIZONTAL BEAM NR VI. CRACK FOUND DURING C-CHECK. CRACK REP AIRED I/A/W SRM. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996030100617 19960301 00617 EU 1996 3 1 QXEA9600081 1 19960226 A 5541 RIB A06000401 FOKKER F28 F28MK1000 4990808 EU RUDDER CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 802PH 11017 PDX - RUDDER RIB BELOW PANEL 57Y HAS A 1.25 CRACK. CRACK FOUND DURING C-CHECK. CRACK REPAIRED I/A/W EA 28-55-45. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996030100618 19960301 00618 NM 1996 3 1 QXEA9600082 1 19960226 A 5347 85320490135 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM RT MID FWD CORROSION A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 12619 275 PDX - P/N 85320490135 SEAT TRACK FOUND CORRODED BEYOND LIMITS DURING C-CHECK. NEW TRACK INSTALLED I/A/W SRM. AIRCRAFT RETURNED TO SERVICE. AIRCRAFT TOTAL CYCLES, 17,630. 2 H 7 2 4T RT A13NM 1996030100619 19960301 00619 NM 1996 3 1 QXEA9600083 1 19960226 A 5347 85330217001 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM LT MID AFT CORRODED A QXEA K NONE N FALSE WARNING IN INSP/MAINT 1 NM 09 827PH 12619 275 PDX - P/N 85330217001 SEAT TRACK FOUND CORRODED DURING C-CHECK. NEW TRACK INSTALLED I/A/W SRM. AIRCRAFT RETURNED TO SE RVICE. AIRCRAFT TOTAL CYCLES, 17,630. 2 H 7 2 4T RT A13NM 1996030100620 19960301 00620 NM 1996 3 1 QXEA9600084 1 19960226 A 5347 85330469001 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM RT MID AFT CORROSION A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 12619 275 PDX - P/N 85330469001 SEAT TRACK FOUND CORRODED BEYOND LIMITS DURING C-CHECK. NEW TRACK INSTALLED I/A/W SRM. AIRCRAFT RETURNED TO SERVICE. AIRCRAFT TOTAL CYCLES, 17,630. 2 H 7 2 4T RT A13NM 1996030100621 19960301 00621 NM 1996 3 1 QXEA9600085 1 19960226 A 5347 85331040109 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM RT OTBD AFT CORROSION A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 12619 275 PDX - P/N 85331040109 SEAT TRACK FOUND CORRODED BEYOND LIMITS DURING C-CHECK. NEW TRACK INSTALLED I/A/W SRM. AIRCRAFT RETURNED TO SERVICE. AIRCRAFT TOTAL CYCLES, 17,630. 2 H 7 2 4T RT A13NM 1996030100622 19960301 00622 NM 1996 3 1 QXEA9600086 1 19960226 A 5347 85331039101 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM LT OTBD AFT CORROSION A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 827PH 12619 275 PDX - P/N 85331039101 SEAT TRACK FOUND CORRODED BEYOND LIMITS DURING C-CHECK. NEW TRACK INSTALLED I/A/W SRM. AIRCRAFT RETURNED TO SERVICE. AIRCRAFT TOTAL CYCLES, 17,630. 2 H 7 2 4T RT A13NM 1996030100623 19960301 00623 NM 1996 3 1 QXEA9600087 1 19960228 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 841PH 82 PDX - COCKPIT EMERGENCY LIGHT IS INOPERATIVE. LIGHT REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1996030100624 19960301 00624 NM 1996 3 1 UPS205573 1 19960219 A 5230 FRAME BOEING 727 72725C 138400H NM CARGO DOOR GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MAIN CARGO DOOR HAS TOOLING MARKS/GOUGES IN Z-FRAME STA 590 WL 302. GOUGE OU T OF LIMITS, FABRICATED REPAIR ANGLE AND HEAT TREATED. INSTALLED PART IAW SRM 51-40-3, 51-10-2, 51-30-2, AND 53-10-1. 2 L 7 3 4F A3WE 1996030100625 19960301 00625 NM 1996 3 1 UPS205574 1 19960220 A 5220 65210818 HANDLE CASTING BOEING 727 72725C 138400H NM LT EMER EXIT CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON LT AFT OVERWING EXIT EXTERNAL HANDLE SEAL CASTING. REMOVED AND REPLACED SEAL CASTING IAW SRM 51-30-02 AND UPS OHM 52-26-01. 2 L 7 3 4F A3WE 1996030100626 19960301 00626 NM 1996 3 1 UPS205575 1 19960220 A 5220 65210818 HANDLE CASTING BOEING 727 72725C 138400H NM LT EMER EXIT CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON LT FWD OVERWING EXIT EXTERIOR HANDLE SEAL CASTING. REMOVED AND REPLACED SEAL CASTING IAW SRM 51-30-02 AND UPS OHM 52-26-01. 2 L 7 3 4F A3WE 1996030100627 19960301 00627 NM 1996 3 1 UPS205576 1 19960220 A 5220 65210818 HANDLE CASTING BOEING 727 72725C 138400H NM RT EMER EXIT CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON RT FWD OVERWING EXIT EXTERIOR HANDLE SEAL CASTING. REMOVED AND REPLACED SEAL CASTING IAW SRM 51-30-02 AND UPS OHM 52-26-01. 2 L 7 3 4F A3WE 1996030100628 19960301 00628 NM 1996 3 1 UPS205577 1 19960215 A 5755 651734857 SKIN BOEING 727 72725C 138400H NM NR 5 SPOILER DELAMINATION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED SPOILER NR 5 HAS DELAMINATION AT THE ACTUATOR FITTING AT FWD EDGE CENTER OF S POILER BOTH UPPER AND LOWER SURFACE. REPAIRED SPOILER IAW SRM 51-40-6 AND 57-50-6. 2 L 7 3 4F A3WE 1996030100629 19960301 00629 NM 1996 3 1 UPS205578 1 19960220 A 5320 651986219 MID CHORD BOEING 727 72725C 138400H NM BS 302 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON LT MID CHORD BETWEEN DOGHOUSE FLOOR AND BS 302 LBL 15 WL 170. C ORROSION REMOVED OUT OF LIMITS IAW SRM 53-10-1. REMOVED AND REPLACED LT MID CHORD IAW SRM 51-30-2, 51-30-4 AND MM 51-20 -151. 2 L 7 3 4F A3WE 1996030100630 19960301 00630 NM 1996 3 1 UPS205579 1 19960220 A 5320 BAC1518352 STIFFENER BOEING 727 72725C 138400H NM BS 358 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON HORIZONTAL STIFFENER BS 358 LBL 6 AND WL 149. CORROSION OUT OF LIMITS, REMOVED DAMAGED STIFFENER, FABRICATED AND INSTALLED NEW PARTS PER SRM 51-30-2, 51-10-1 AND DWG-18417. 2 L 7 3 4F A3WE 1996030100631 19960301 00631 NM 1996 3 1 UPS205580 1 19960220 A 5320 BAC1518352 STIFFENER BOEING 727 72725C 138400H NM BS 357 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON HORIZONTAL STIFFENER BS 357 LBL 16 AND WL 1498. CORROSION OUT O F LIMITS, REMOVED DAMAGED STIFFENER, FABRICATED AND INSTALLED NEW PARTS PER SRM 51-30-2, 51-10-1 AND DWG-18417. 2 L 7 3 4F A3WE 1996030100632 19960301 00632 NM 1996 3 1 UPS205581 1 19960215 A 5755 6517347048 SKIN BOEING 727 72725C 138400H NM NR 4 SPOILER DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED NR 4 SPOILER HAS AN AREA OF DELAMINATION AROUND CENTER DOUBLER ON THE LOWER S URFACE. REPAIRED NR 4 SPOILER AROUND CENTER DOUBLER IAW SRM 51-40-6 AND 57-50-6. 2 L 7 3 4F A3WE 1996030100633 19960301 00633 NM 1996 3 1 UPS205582 1 19960220 A 5754 65217495 ATTACH LUG BOEING 727 72725C 138400H NM NR 1 LE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT WING NR 1 K-FLAP BULLNOSE I/B ROD ATTACH LUG IS CORRODED. REMOVED AND REP LACED NR 1 K-FLAP BULLNOSE IAW UPS OHM 57-51-01. 2 L 7 3 4F A3WE 1996030100634 19960301 00634 NM 1996 3 1 UPS205583 1 19960131 A 5347 SEAT TRACK BOEING 727 72725C 138400H NM BS 680-700 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MECHANICAL DAMAGE ON SEAT TRACK AT STATION 680 TO 700 LBL 65 WL 208. FOUND D AMAGE TO BE OUT OF LIMITS, REMOVED DAMAGED SEAT TRACK AND REINSTALLED FABRICATED SEAT TRACK WITH FASTENERS AT STA 683 TO 740 IAW SRM 51-30-02, 51-10-02, AND 53-10-1. 2 L 7 3 4F A3WE 1996030100635 19960301 00635 NM 1996 3 1 UPS205590 1 19960222 A 5311 65224978 FRAME BOEING 727 72725C 138400H NM BS 930 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT 930 FRAME CRACKED AT TOP OF FORGED SECTION STR 14 BETWEEN RIVETS ON FACE O F FRAME. REPAIRED RT 930 FRAME AT STR 14R PER UPS EO NR B727-5310-2580-B APPENDIX 8.1 AND 8.2. 2 L 7 3 4F A3WE 1996030100636 19960301 00636 NM 1996 3 1 UPS205591 1 19960222 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 1030 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION (C53-224-01-05-03), ON FLOORBEAM UPPER FLANGE BS 1030, RBL 10 AND L BL 0 TO 58, WL 208. CORROSION REMOVAL ON FLOORBEAM UPPER FLANGE WAS OUT OF LIMITS. REMOVED DAMAGED SECTION, FABRICATED REPAIR PARTS AND INSTALLED PER TRAMCO EWO NR 96-2079, EO NR 727-53-1729. 2 L 7 3 4F A3WE 1996030100637 19960301 00637 NM 1996 3 1 UPS205592 1 19960221 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 660 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION (C53-224-01.05-01) ON FLOORBEAM UPPER CHORD AROUND NUTPLATE HOLES S TA 660 RBL 10 TO RBL 55. MECHANICALLY REMOVED CORROSION FROM 660 FLOORBEAM UPPER CHORD RBL 10 TO 58. FOUND REWORK FROM RBL 54 TO 58 TO BE OUT OF LIMITS IAW SRM 53-10-1. REPAIRED AREA IAW UPS EO NR 727-53-1726. 2 L 7 3 4F A3WE 1996030100638 19960301 00638 NM 1996 3 1 UPS205593 1 19960221 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 600 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION (C53-224-01.05-01) ON FLOORBEAM UPPER CHORD STA 600 RBL 45 TO RBL 6 5 WL 208, AROUND NUTPLATE HOLES. CORROSION REMOVAL ON UPPER CHORD OF FLOORBEAM WAS OUT OF LIMITS. BLENDED AREA, FABRIC ATED AND INSTALLED REPAIR PARTS, ALL WORK DONE PER TRAMCO EWO 96-2080, EO NR 727-53-1730. 2 L 7 3 4F A3WE 1996030100639 19960301 00639 NM 1996 3 1 UPS205594 1 19960222 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 640 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION (C53-224-01.05-01), ON FLOORBEAM UPPER CHORD STA 640, LBL 60 TO RBL 60, WL 208 AROUND NUTPLATE HOLES. CORROSION REMOVAL WAS OUT OF LIMITS. REMOVED DAMAGED SECTION, FABRICATED REPAIR PAR TS AND INSTALLED PER TRAMCO EWO 96-2071, EO 727-53-1727. 2 L 7 3 4F A3WE 1996030100640 19960301 00640 NM 1996 3 1 UPS205595 1 19960221 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 680 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON FLOORBEAM UPPER CHORD AROUND NUTPLATE HOLES STA 680 LBL 60 TO RB L 60, WL 208. CORROSION REMOVAL ON FLOORBEAM UPPER CHORD WAS OUT OF LIMITS PER SRM 53-10-1. BLENDED AREA, FABRICATED R EPAIR ANGLES, REPAIR PARTS AND INSTALLED PER TRAMCO EWO 96-2086 AND EO NR 727-53-1731. 2 L 7 3 4F A3WE 1996030100641 19960301 00641 NM 1996 3 1 UPS205597 1 19960224 A 5210 6516479 GATE BOEING 727 72725C 138400H NM BS 328 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FWD ENTRY DOOR UPPER GATE CORRODED AROUND LOWER RIV-NUTS AND EXTERNAL EDGES C ORROSION (C53-224-01.06-01). REMOVED AND REPLACED FWD ENTRY DOOR UPPER GATE IAW UPS SRM 51-10-1, 51-10-2, 51-10-3 AND U PS MM 52-11-00. 2 L 7 3 4F A3WE 1996030100642 19960301 00642 NM 1996 3 1 UPS205598 1 19960224 A 5210 65164810 GATE BOEING 727 72725C 138400H NM BS 328 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FORWARD ENTRY DOOR LOWER GATE EXTERNAL SURFACE CORRODED CORROSION (C53-224-01 .06-01). REMOVED AND REPLACED FWD ENTRY DOOR LOWER GATE IAW UPS SRM 51-30-2, 51-10-1, 51-10-2 AND UPS MM 52-11-00. 2 L 7 3 4F A3WE 1996030100643 19960301 00643 NM 1996 3 1 UPS205599 1 19960210 A 5312 BULKHEAD BOEING 727 72725C 138400H NM BS 178 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED SUSPECTED CRACK AT FASTENER HOLE ON BS 178 BULKHEAD LBL 9, WL 236. REMOVED 2 FASTENERS, CLEANED AREA, NDT INSPECTED FOUND CRACK. TRIMMED OUT AREA THAT WAS CRACKED. NDT VERIFIED CRACK CONTAINMENT FABRICATED REPAIR FILLER AND DOUBLER AND INSTALLED ON AIRCRAFT IAW SRM 53-10-9, SRM 51-30-2. 2 L 7 3 4F A3WE 1996030100644 19960301 00644 NM 1996 3 1 UPS205600 1 19960129 A 5311 FRAME BOEING 727 72725C 138400H NM BS 930 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT STA 930 FRAME CRACKED ON ZEE FRAME T-FORGED FRAME AT SPLICE ON STRINGER NR 14. REMOVED CRACKED FRAME, POSITIONED AND INSTALLED NEW FRAME, LOCATED ALL HOLES AND SECURED WITH FASTENERS IAW EO B74 7-5310-2580-B ER 020596JM1, ER 0214964D1 SRM 51-40-04, 53-10-3. 2 L 7 3 4F A3WE 1996030100645 19960301 00645 NM 1996 3 1 UPS205601 1 19960223 A 5347 SEAT TRACK BOEING 727 72725C 138400H NM BS 870-1000 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION (4-25-02) AND MECHANICAL DAMAGE ON SEAT TRACK AT STA 870 TO 1000 LB L 45 WL 208. REMOVED AND REPLACED SEAT TRACK FROM STA 870 TO 1060 LBL 45 IAW UPS SRM 51-30-2. 2 L 7 3 4F A3WE 1996030100646 19960301 00646 NM 1996 3 1 UPS205602 1 19960223 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 312 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION (C53-224-01.05-01), ON FLOORBEAM STA 312 LBL 48 TO LBL 0 WL 208 ARO UND NUTPLATE HOLES. REMOVED AND REPLACED FLOORBEAM IAW UPS SRM 53-10-8, 51-10-6, 53-10-1. 2 L 7 3 4F A3WE 1996030100647 19960301 00647 NM 1996 3 1 UPS205603 1 19960223 A 5754 65162262 BONDING JUMPER BOEING 727 72725C 138400H NM NR 5 LE FLAP CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED NR 5 K-FLAP I/B UPPER LUG CORRODED AT BONDING JUMPER. REMOVED AND REPLACED N R 5 K-FLAP NRC 432723. 2 L 7 3 4F A3WE 1996030100648 19960301 00648 NM 1996 3 1 UPS205604 1 19960227 A 5320 4130 FORGING BOEING 727 72725C 138400H NM BS 870 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT AFT 870 TERMINAL FORGING IS CRACKED AT BS 870 WL 188 LBL 67. REMOVED CRAC KED AREA AND NDT VERIFIED CRACK CONTAINMENT, REPAIRED IAW EO 96-2060. 2 L 7 3 4F A3WE 1996030100649 19960301 00649 NM 1996 3 1 UPS205605 1 19960227 A 5330 SKIN BOEING 727 72725C 138400H NM BS 640-660 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON INNER SKIN BS 640 TO 660 BETWEEN STR 2 TO 3 LT. REMOVED CORROSI ON, OUT OF LIMITS PER SRM 53-30-2 FABRICATED REPAIR PARTS AND INSTALLED IAW 96-2089. 2 L 7 3 4F A3WE 1996030100650 19960301 00650 NM 1996 3 1 UPS205606 1 19960227 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 1110 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON FLOORBEAM UPPER FLANGE BS 1110 RBL 50 TO 56 LBL 3 TO 20 AND 40 T O 44. REMOVED CORROSION, OUT OF LIMITS REPAIRED PER EWO 96-2087. 2 L 7 3 4F A3WE 1996030100651 19960301 00651 NM 1996 3 1 UPS205607 1 19960227 A 5320 FORGING BOEING 727 72725C 138400H NM BS 950 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED WHILE WORKING FUSELAGE CUST NR 433165, FOUND A CRACK ON THE BS 950 FORGING AT THE FWD SIDE OF PRESSURE WEB ATTACH FITTING. DRILLED CRACK AND VERIFIED CRACK CONTAINMENT, INSTALLED NEW FITTING AND R EPAIRED IAW EO 96-2098. 2 L 7 3 4F A3WE 1996030100652 19960301 00652 NM 1996 3 1 UPS205608 1 19960227 A 5313 STRINGER BOEING 727 72725C 138400H NM BS 940 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STRINGER 18A LT HAS NO EDGE DISTANCE AT STA 940, DUE TO CORROSION IN FASTENER HOLES. REMOVED CORROSION, FABRICATED REPAIR PARTS AND INSTALLED IAW EWO 96-2090. 2 L 7 3 4F A3WE 1996030100653 19960301 00653 NM 1996 3 1 UPS205609 1 19960223 A 5610 SEAL BOEING 727 72751C 1384015 NM LT WINDSHIELD LOOSE A IPXA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 904UP 18946 CREW REPORTED, LOUD FLAPPING SOUND HEARD AT 15,000 FT MSL 280 KTS AT TOP OF CAPT'S WINDSHIELD. REQUESTED PRIORITY LANDI NG, DECLARED EMERGENCY AND LANDED. AFTER SLOWING ASAP, FLAPPING SOUND WAS TOP OUTSIDE SEAL ON NEW WINDOW INSTALLED ON 2 /20 IN SDF, DEFERRED AERO DYNAMIC SEAL. INSTALLED MYLAR TAPE. 2 L 7 3 4F A3WE 1996030100654 19960301 00654 NM 1996 3 1 UPS505571 1 19960222 A 5320 SUPPORT BOEING 757 75724APF 1384969 NM BS 1465 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 441UP 27386 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED AFT BULK CARGO COMP LT FLOOR TO SIDEWALL SUPPORT CRACKED AT BS 1465. REPAIRE D CRACK IAW SRM 51-70-13. 2 L 7 2 4F RT A2NM 1996030100655 19960301 00655 NM 1996 3 1 UPS505572 1 19960225 A 5753 113N200348H SKIN BOEING 757 75724APF 1384969 NM RT TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 441UP 27386 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT I/B MAIN FLAP HAS 5 CRACK'S 6 INCHES LONG ON UPPER SURFACE OF I/B TRAILING EDGE. REMOVED AND REPLACED MAIN FLAP IAW MM 27-51-02, 27-51-12, AND 27-51-13. 2 L 7 2 4F RT A2NM 1996030100656 19960301 00656 WP 1996 3 1 UPS805584 1 19960221 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FS 1776 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 783UP 45973 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED BOLT FRAME SHEAR TIE CRACKED AT FS 1776 LONGERON 9R. PROFILED CRACKED AREA F OR SRM 53-2-0. 2 L 7 4 4F RT 4A25 1996030100657 19960301 00657 WP 1996 3 1 UPS805585 1 19960219 A 5320 FITTING DOUG DC8 DC871F 302199D WP FS 1600 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 783UP 45973 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 1600 NEAR LONGERON 21L FLOORBEAM FITTING CRACKED. REPLACED FITTING PER SR M 51-1-20D. 2 L 7 4 4F RT 4A25 1996030100658 19960301 00658 WP 1996 3 1 UPS805586 1 19960221 A 5414 SKIN DOUG DC8 DC871F 302199D WP NR 1 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 783UP 45973 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED NR 1 PYLON T/E HAS A .5 INCH CRACK AT LOWER AFT END. REPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996030100659 19960301 00659 WP 1996 3 1 UPS805587 1 19960221 A 5414 SKIN DOUG DC8 DC871F 302199D WP NR 2 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 783UP 45973 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED NR 2 PYLON T/E HAS A 2.5 INCH CRACK AT LOWER AFT END. REPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996030100660 19960301 00660 WP 1996 3 1 UPS805588 1 19960219 A 5753 57011525010 SKIN DOUG DC8 DC871F 302199D WP NR 3 TE VANE DEALAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 783UP 45973 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT WING NR 3 FLAP VANE DELAMINATED AT LOWER SURFACE. REPLACED FLAP VANE ASSY PER MM 27-51-14. 2 L 7 4 4F RT 4A25 1996030100661 19960301 00661 WP 1996 3 1 UPS805589 1 19960219 A 5755 56551602 SKIN DOUG DC8 DC871F 302199D WP NR 2 SPOILER DEALAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 783UP 45973 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT WING NR 2 SPOILER DELAMINATED AT LOWER SURFACE. REPLACED SPOILER PANEL PE R MM 27-61-01. 2 L 7 4 4F RT 4A25 1996030100662 19960301 00662 WP 1996 3 1 UPS805596 1 19960227 A 2560 EXC ROPE COVER DOUG DC8 DC871F 302199D WP COCKPIT OUT OF ADJUST A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 MAINTENANCE REPORTED, CAPTAINS ESCAPE ROPE WILL NOT REMAIN SECURE IN STOWED POSITION. PERFORMED INTERIM REPAIR TO CAPT' S ESCAPE ROPE COVER AND DEFERRED PER EO DC8-2510-7055 A FINAL REPAIR REQUIRED PRIOR TO FIRST FLIGHT ON 3-4-96. 2 L 7 4 4F RT 4A25 1996030100663 19960301 00663 WP 1996 3 1 9604889951 1 19960228 A 3230 UPLOCK LATCH DOUG DC9 DC932 3022066 WP RT MLG BINDING A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 9347 45827 DURING CLIMBOUT, RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. FLIGHT CONTINUED TO MSP AND LA NDED WITHOUT INCIDENT. MAINTENANCE FREED MOVEMENT TO RIGHT MAIN GEAR UPLOCK LATCH. OPERATIONAL CHECK NORMAL, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996030100664 19960301 00664 1996 3 1 9604892762 4 19960216 A 3454 CONNECTOR BOEING 727 7272M7 138407S NM NAV SWITCHING DIRTY A NWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 01 722RW 21201 DURING CRUISE, THE VHF NR 1, NR 2 AND AUXILIARY HAD NO BEARING SIGNAL OR LOCALIZER AND ALL NAV FLAGS ILLUMINATED. FLIGH T RETURNED TO MSP. CLEANED NAV SWITCHING UNIT CONNECTOR. 2 L 7 3 4F A3WE 1996030100665 19960301 00665 1996 3 1 9604909150 4 19960110 A 3416 ALTIMETER DOUG DC9 DC914 3022034 WP LT/RT COCKPIT FAILED A NWAA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 01 8908E 45749 DURING CRUISE, CAPTAIN'S AND FIRST OFFICER'S ALTIMETERS WOULD NOT AGREE. DIVERTED TO MEM AND LANDED WITHOUT INCIDENT. R EPLACED CAPTAIN'S AND FIRST OFFICER'S ALTIMITERS. REROUTED STATIC LINE TO FIRST OFFICER'S INDICATOR. PERFORMED BARFIEL D TEST, CHECKED STATIC PORTS, AND ALL CHECKED GOOD. 2 L 7 2 4F A6WE 1996030100666 19960301 00666 NM 1996 3 1 96FDEA00350 1 19960111 A 5311 BELL FRAME BOEING 727 727227 1384078 NM BS 804.5 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 487FE 21490 CABIN, BELL FRAME CRACKED STA 804.5 STR 14R. STOP DRILLED CRACK AND INSTALLED DOUBLER 7075T6.090 PER 53-30-4 FIG 1. 2 L 7 3 4F A3WE 1996030100667 19960301 00667 NM 1996 3 1 96FDEA00351 1 19960228 A 5312 BLKHD WEB BOEING 727 72722 1384002 NM BS 870 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 ON REMOVAL OF THE REAR, UPPER AND LOWER SPAR CHORDS, FOUND 870 BULKHEAD WEB HAS CORROSION, LBL TO RBL 70 WL 174 TO 140. REMOVED AND REPLACED 870 BULKHEAD WEB. 2 L 7 3 4F A3WE 1996030100668 19960301 00668 NM 1996 3 1 96FDEA00352 1 19960228 A 5330 SKIN BOEING 727 727233 138408A NM BS 1223 GOUGE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 266FE 21672 GOUGE IN FUSELAGE SKIN AT BS 1223 WL 290 STR 19R, ACCESSING OF THE TORQUE BOX REQUIRED. REMOVED DAMAGE IN FUSELAGE SKIN AT BS 1223 WL 290 STR 19R AND INSTALLED REPAIR DOUBLER PER SRM 53-30-3. 2 L 7 3 4F RT A3WE 1996030100669 19960301 00669 NM 1996 3 1 96FDEA00353 1 19960228 A 5330 SKIN BOEING 727 72722 1384002 NM BS 1142-1148 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 WHILE WORKING NR0007, FOUND CORROSION IN UPPER SKIN LAP BS 1142 TO 1148 STR 26R. REPAIRED SKIN PER SRM 53-30-3 AND SB 7 27-53-0072. 2 L 7 3 4F A3WE 1996030100670 19960301 00670 NM 1996 3 1 96FDEA00354 1 19960228 A 5330 SKIN BOEING 727 72722 1384002 NM BS 227.8 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 BULGING AROUND FASTENERS ON EXTERIOR SKIN BS 227.8 RBL TO LBL 5. REPAIRED BULGING SKIN AT BS 227.8 RBL TO LBL 5 AS PER FEDEX SRM 53-30-3. 2 L 7 3 4F A3WE 1996030100671 19960301 00671 NM 1996 3 1 96FDEA00355 1 19960228 A 5320 SHEAR TIE BOEING 727 72722 1384002 NM BS 1166 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 SHEAR TIE IS CRACKED AT FASTENER HOLE, BS 1166 BETWEEN STR 25 TO 26R. REPAIRED CRACKED SHEAR TIE PER FEDEX SRM 53-10-4 FIG 14. 2 L 7 3 4F A3WE 1996030100672 19960301 00672 NM 1996 3 1 96FDEA00356 1 19960228 A 5330 SKIN BOEING 727 72722 1384002 NM BS 590-620 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 THREE GOUGES IN SKIN AT BS 590 TO 620, BETWEEN STR 21 TO 22R. REPAIRED 3 GOUGES IN THE SKIN AT BS 590 TO 620, BETWEEN S TR 21 TO 22R PER FEDEX SRM 53-30-3. 2 L 7 3 4F A3WE 1996030100673 19960301 00673 NM 1996 3 1 96FDEA00357 1 19960228 A 5320 SHEAR WEB BOEING 727 72722 1384002 NM BS 1173 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION (C53-224-02), ON SHEAR WEB AT BS 1173 RBL 27 WL 208. REPAIRED SHEAR WEB PER SRM 51-40-2. 2 L 7 3 4F A3WE 1996030100674 19960301 00674 NM 1996 3 1 96FDEA00358 1 19960228 A 5315 BAC1505100797 FLOOR BEAM BOEING 727 72722 1384002 NM BS 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION (C53-111-01, -2) ON LOWER FLANGE OF FLOORBEAM IN NUTPLATE HOLES AT BS 600 LBL 20 TO RBL 26 WL 200. REMOVED CO RRODED AREA FROM LBL 17 TO RT SKIN. FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 53-10-8 FIG 2. 2 L 7 3 4F A3WE 1996030100675 19960301 00675 NM 1996 3 1 96FDEA00359 1 19960225 A 5521 65174403 HINGE RIB BOEING 727 72722 1384002 NM RT ELEVATOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 RT ELEVATOR HINGE RIB AT HORIZONTAL STAB STATION 136.50 IS CRACKED ON THE I/B UPPER FLANGE. REMOVED AND REPLACED ELEVAT OR HINGE RIB PER SRM 27-30-0. 2 L 7 3 4F A3WE 1996030100676 19960301 00676 NM 1996 3 1 96FDEA00360 1 19960228 A 5320 65317731 CHORD BOEING 727 72722 1384002 NM BS 1176 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION (C53-224-08), ON BS 1176 CHORD AT LBL 20 AND RBL 65 WL 208. REMOVED AND REPLACED 1176 CHORD PER 51-30-2. 2 L 7 3 4F A3WE 1996030100677 19960301 00677 NM 1996 3 1 96FDEA00361 1 19960111 A 5311 BELL FRAME BOEING 727 727227 1384078 NM BS 804.5 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 487FE 21490 CABIN BELL FRAME ANGLE CRACKED STA 804.5 STR 14R. INSTALLED REPAIR PER 51-40-3 PG 1 TO 4. 2 L 7 3 4F A3WE 1996030100678 19960301 00678 NM 1996 3 1 96UAL900152 1 19960228 A 3350 BATTERIES BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE CABIN DISCHARGED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 986UA 21748 LEFT HAND OUTSIDE OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERIES AND CHECKS OK. 2 L 7 2 4F 4 F A16WE E2EA 1996030100679 19960301 00679 NM 1996 3 1 96UAL900153 1 19960228 A 2612 18252 SENSOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7266U 21413 NO FIRE TEST ON NR 1 ENGINE. SUPPLEMENTAL DATA UPDATE: REPLACED NR 1 ENGINE LOWER SENSOR. CHECKS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1996030100680 19960301 00680 NM 1996 3 1 96UAL900154 1 19960228 A 7711 511749 PT7 TUBE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE LEAKING A UALA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 WP 29 7271U 6907 21418 ABORTED TAKEOFF AT 60 KNOTS DUE TO NR 3 ENGINE LOW POWER INDICATION. RETURN TO BLOCKS AT ORD. INTERMEDIATE PT7 MANIFOL D TUBE WAS FOUND TO BE LEAKING DURING PRESSURE CHECK. ENGINE PRESSURE RATIO TRANSMITTER AND INDICATOR WERE REPLACED PER PRECAUTIONARY. 2 L 7 3 4F 4 F A3WE E2EA 1996030100681 19960301 00681 EU 1996 3 1 COMA9630043 1 19960226 A 2730 531137 PITCH TRIM SW SAAB SF340 SF340A 7850100 EU CONTROL YOKE FAILED A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 344CA 340A025 PILOTS PITCH TRIM IS INTERMITTENT. REPLACED THE PILOTS PITCH TRIM SWITCH. 2 L 7 2 4T RT A52EU 1996030100682 19960301 00682 NE 1996 3 1 COMA9630044 3 19960227 A 6114 660714200 HUB SAAB SF340 SF340A 7850100 EU ROTOL R354 R3544123F13 NE PROPELLER CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 140N 7733 1480 340A140 DRG440988 FOUND MULTIPLE CRACK INDICATIONS AROUND BOLT HOLES DURING ULTRASONIC INSPECTION SB 61-58. PROPELLER WAS DISASSEMBLED AN D HUB REMOVED FROM SERVICE. 2 L 7 2 4T RT A52EU 6 C P61GL 1996030100683 19960301 00683 EU 1996 3 1 COMA9630045 1 19960228 A 2710 7227150624 BEARING SAAB SF340 SF340A 7850100 EU RT AILERON SEIZED A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 358CA 340A047 AILERON CONTROL MOVEMENT IS EXTREMELY STIFF ON GROUND AND IN FLIGHT. FOUND THE RT INBD AILERON BELL CRANK TO HAVE FROZE N BEARINGS. REPLACED THE CRANK ASSY. 2 L 7 2 4T RT A52EU 1996030100684 19960301 00684 EU 1996 3 1 COMA9630046 1 19960227 A 3020 9303143005 NOZZLE SAAB SF340 SF340A 7850100 EU LT INLET HEAT BURNED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 342CA 340A023 LEFT ENGINE INLET HEAT FAILED. REPLACED THE INLET PROTECTION DEVICE EXHAUST NOZZLE. 2 L 7 2 4T RT A52EU 1996030100685 19960301 00685 EU 1996 3 1 COMA9630047 1 19960227 A 2613 1734362450 HEAT SENSOR SAAB SF340 SF340A 7850100 EU RT TAILPIPE WET A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 340SF 340A014 RT TAIL PIPE HOT WARNING ILLUMINATED DURING TAKEOFF. DRIED MOISTURE ON THE TAIL PIPE HEAT SENSORS. ACFT RETURNED TO SE RVICE. 2 L 7 2 4T RT A52EU 1996030100686 19960301 00686 EA 1996 3 1 COMA9660032 1 19960228 A 2752 853D10010 ACTUATOR CNDAIR CL600 CL6002B19 EA RT TE FLAP FAILED A COMA K NONE O OTHER CL CLIMB 1 SO 01 943CA 7062 FLAPS FAIL CAUTION MESSAGE ON EICAS WHEN FLAPS SELECTED FROM 20 DEGREES TO 0 DEGREES AFTER TAKEOFF. MAINTENANCE FOUND T HE RT OUTBD FLAP ACTUATOR TO BE FAILED INTERNALLY, WHICH IN TURN CAUSED SUBSTANTIAL DAMAGE TO THE FLAP, FLAP DRIVE CABLE S AND POWER DRIVE UNIT. REPLACED ACTUATOR, FLAPS, DRIVE CABLES AND PDU. 2 L 7 2 4F RT A21EA 1996030100687 19960301 00687 NM 1996 3 1 DHL96721001 1 19960226 A 3260 SWITCH BOEING 727 727228 NM LANDING GEAR MALFUNCTIONED A T DHLA O OTHER N FALSE WARNING DE DESCENT 1 SO 01 721DH 19545 AFTER GEAR RETRACTION AT PAP ALL 3 GEAR SHOWED RED AND GREEN LIGHTS ILLUMINATED ON FORWARD PANEL, DOOR LIGHTS WERE NOT I LLUMINATED. ON S/O PANEL SECONDARY MAIN GEAR LIGHTS WERE ILLUMINATED, TAIL SKID LIGHT WAS ILLUMINATED AND NO GEAR DOOR LIGHTS. CYCLED GEAR 2 TIMES WITH NO PROBLEMS. CHECK CONDITION AND SECURED MAIN GEAR AND NOSE GEAR SWITCH. RERACKED TH E LANDING GEAR ACCESSORY BOX. OPERATED GEAR TO UP AND DOWN POSITIONS AND LIGHT CHECKS NORMAL PER MM 32-60. 2 L 7 3 4F A3WE 1996030100688 19960301 00688 WP 1996 3 1 MWEA96048 1 19960228 A 3350 60030431 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 302ME 47102 MAINTENANCE REPORTS, SEVERAL A/C INTERIOR EMERGENCY LIGHTS REMAINED ILLUMINATED WHEN A/C WAS POWERED DOWN. REPLACED TWO BATTERY POWER SUPPLIES AND OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996030100689 19960301 00689 WP 1996 3 1 RRXA9600008 1 19960229 A 2612 FIRE WIRE DOUG DC8 DC871 302199A WP NR 4 ENGINE CHAFED A RRXA E ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 WP 15 8177U 45983 KLRD/KDAY - FLT 019 - ON DESCENT, NR 4 ENGINE SHORT CIRCUIT LIGHT ILLUMINATED FOLLOWED BY AN INTERMITTENT FIRE BELL. PR ECAUTIONARY SHUT DOWN OF NR 4 ENGINE WAS ACCOMPLISHED. MAINTENANCE REPAIRED A CHAFED WIRE AT THE FORWARD END OF RT AFT FIRE LOOP. AN OPERATIONAL CHECK OF THE NR 4 ENGINE FIRE WARNING SYSTEM WAS GOOD. (X) 2 L 7 4 4F 4A25 1996030800001 19960308 00001 NM 1996 3 8 96ZZZX891 1 19960130 A 7711 AN6289D4 PT7 JAM NUT BOEING 737 737277 1384570 NM NR 2 ENGINE LOOSE A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 181AW 22648 MDW/CMH - FLT 0282 - NR 2 EPR INDICATION WAS LOW AND FLUCTUATING. MAINTENANCE INSPECTED AND FOUND P2 TEST CAP AT EPR TR ANSMITTER LOOSE AND THE JAM NUT AT PT7 TEE FITTING TO TRANSMITTER LOOSE. RESECURED. RAN ENGINES TO TAKEOFF POWER. EPR MADE ALL PARAMETERS PER MM 71-11-01 AND MM 71-09-236. REFERENCE: OPERATOR CONTROL NR AWXA960035. (X) 2 L 7 2 4F RT A16WE 1996030800002 19960308 00002 NM 1996 3 8 96ZZZX892 1 19960126 A 3230 2431600000 UPLOCK ROLLER DORNER DO32 DO328100 2996000 NM LT MLG WW DIRTY A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 423JS 3032 FLT 4014 - LEFT MLG WOULD NOT LOCK IN THE 'UP' POSITION WHEN GEAR WAS RETRACTED AFTER TAKEOFF. AIRCRAFT RETURNED TO THE FIELD, LANDED WITHOUT FURTHER INCIDENT. PIT MX CLEANED AND LUBRICATED THE MLG 'UP' LOCK ROLLERS IAW MM 32-00-00 AND ST D MX PRACTICES. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A45NM 1996030800003 19960308 00003 1996 3 8 96ZZZX893 3 19960127 A 6112 E62127 DEICE BOOT DORNER DO32 DO328100 2996000 NM LT PROPELLER FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 424JS 3033 FLT 7160 - LEFT PROPELLER HEAT FAILED SHORTLY AFTER TAKEOFF. AIRCRAFT RETURNED TO FIELD, LANDED WITHOUT FURTHER INCIDEN T. PIT MX REMOVED AND REPLACED LT PROPELLER ASSEMBLY IAW MM 61-10-00. GROUND CHECKED GOOD, AIRCRAFT RETURNED TO SERVIC E. (X) 2 H 7 2 4T RT A45NM 1996030800004 19960308 00004 NM 1996 3 8 96ZZZX894 1 19960127 A 3411 PITOT TUBE DORNER DO32 DO328100 2996000 NM RIGHT ICED UP A VNAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 424JS 3033 FLT 4158 - SHORTLY AFTER TAKEOFF, THE FIRST OFFICER NOTICED AIR SPEED AND ALTIMETER INDICATORS WERE FLUCTUATING APPROXIM ATELY 100 KNOTS. AIRCRAFT RETURNED TO FIELD, LANDED WITHOUT FURTHER INCIDENT. PIT MX ACTIVATED PITOT STATIC HEAT SYSTE M TO MELT ICE ACCUMULATION. GROUND CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A45NM 1996030800005 19960308 00005 NM 1996 3 8 96ZZZX895 1 19960124 A 5220 001A522A10312204 ACRYLIC COVER DORNER DO32 DO328100 2996000 NM COCKPIT HATCH MISSING A VNAA O OTHER O OTHER CR CRUISE 1 GL 07 427JS 3039 FLT 4024 - DURING CRUISE, CREW HEARD A LOUD NOISE COMING FROM THE COCKPIT EMERGENCY ESCAPE HATCH. AIRCRAFT LANDED IN PI T WITHOUT FURTHER INCIDENT. PIT MX INSPECTED AIRCRAFT AND NOTICED THE ACRYLIC EMERGENCY ESCAPE HATCH HANDLE COVER WAS M ISSING. PIT MX REPLACED THE ACRYLIC COVER IAW MM 52-20-00 AND RETURNED AIRCRAFT TO SERVICE. (X) 2 H 7 2 4T RT A45NM 1996030800006 19960308 00006 NM 1996 3 8 96ZZZX896 1 19960116 A 5610 17300009 DV WINDOW DORNER DO32 DO328100 2996000 NM LT COCKPIT CRACKED A VNAA A UNSCHED LANDING O OTHER IN INSP/MAINT 1 GL 07 430JS 217 3044 FLT 4149 - DURING CRUISE AT FL 230, CAPTAIN'S DV WINDOW FAILED. CRACKED FROM TOP TO BOTTOM. AIRCRAFT DIVERTED TO CAK W HERE MX REMOVED AND REPLACED LEFT DV WINDOW IAW MM 56-10-00. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A45NM 1996030800007 19960308 00007 NM 1996 3 8 96ZZZX897 1 19960115 A 5610 SPSD0328131 WINDSHIELD DORNER DO32 DO328100 2996000 NM RIGHT DEFECTIVE A VNAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 434JS 200 3051 FLT 4081 - DURING CRUISE AT FL 210, THE FIRST OFFICER'S WINDSHIELD BEGAN TO ARC. SHORTLY THEREAFTER, THE OUTER PANE OF THE WINDSHIELD SHATTERED. AIRCRAFT RETURNED TO FIELD, LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT WAS LATER FERRIED FROM CLT TO CAK WHERE MX REPLACED THE FIRST OFFICER'S (RIGHT) WINDSHIELD IAW MM TR56-10-00 AND MM TR56-11-00. GROUND CHECKE D GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A45NM 1996030800008 19960308 00008 NE 1996 3 8 96ZZZX898 2 19960120 A 7310 3035681 FUEL FILTER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE RT ENGINE CLOGGED A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 07 434JS 3051 FLT 4029 - PRIOR TO TAKEOFF AS ENGINES WERE BROUGHT UP TO POWER, THE CREW WAS ALERTED BY A CAS MESSAGE (RT FUEL FILTER B YPASS). AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. PIT MX REMOVED AND REPLACED RT ENGINE HIGH PRESSURE FUEL F ILTER IAW MM 73-00-00. GROUND RUNS CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T 4 T RT A45NM E20NE 1996030800009 19960308 00009 WP 1996 3 8 96ZZZX899 1 19960205 A 5330 SKIN DOUG DC8 DC862 3021970 WP FS 1290 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 8974U 46110 LEVEL 2 CORROSION/2 SMALL SKIN BULGES JUST AFT OF NR 4 PIT DOOR FS 1290, STR 28R. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-1. 2 L 7 4 4F 4A25 1996030800010 19960308 00010 WP 1996 3 8 96ZZZX900 1 19960205 A 5330 SKIN DOUG DC8 DC862 3021970 WP FS 540 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 8974U 46110 LEVEL 2 CORROSION/LOWER FUSELAGE IS BULGED WITH CORROSION AT FS 540R BETWEEN LONGERONS 35R AND 34R BELOW FORWARD CARGO D OOR SILL PLATE. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 52-2-1. 2 L 7 4 4F 4A25 1996030800011 19960308 00011 WP 1996 3 8 96ZZZX901 1 19960205 A 5320 DOUBLER DOUG DC8 DC862 3021970 WP BS 1240-1260 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 8974U 46110 LEVEL 2 CORROSION/AFT CARGO COMPARTMENT, LT SIDE STR 21L, BETWEEN STA 1240 AND STA 1260, FLOOR SUPPORT CORRODED. REMOVE D DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR PER RICH DRAWING D85310-6124. (X) 2 L 7 4 4F 4A25 1996030800012 19960308 00012 WP 1996 3 8 96ZZZX902 1 19960205 A 5320 DOUBLER DOUG DC8 DC862 3021970 WP BS 1240-1260 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 8974U 46110 LEVEL 2 CORROSION/AFT CARGO COMPARTMENT, LT SIDE STR 21L BETWEEN STA 1240 AND STA 1260, FUSELAGE SKIN HAS CORROSION. RE MOVED DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR PER RICH E.O. D85310-6124, REV 1. 2 L 7 4 4F 4A25 1996030800013 19960308 00013 WP 1996 3 8 96ZZZX903 1 19960205 A 5320 DOUBLER DOUG DC8 DC862 3021970 WP BS 1160-1180 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 8974U 46110 LEVEL 2 CORROSION/AFT CARGO COMPARTMENT STR 21R BETWEEN STA 1160 AND STA 1180, FLOOR SUPPORT HAS CORROSION. REMOVED DAM AGED AREA, FABRICATED, AND INSTALLED REPAIR PER SRM 53-2-5. (X) 2 L 7 4 4F 4A25 1996030800014 19960308 00014 WP 1996 3 8 96ZZZX904 1 19960205 A 5320 DOUBLER DOUG DC8 DC862 3021970 WP BS 1160-1180 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 8974U 46110 LEVEL 2 CORROSION/AFT CARGO COMPARTMENT, STR 21R BETWEEN STA 1160 AND STA 1180, FLOOR SUPPORT HAS CORROSION. REMOVED DA MAGED AREA, FABRICATED, AND INSTALLED REPAIR PER RICH E.O. NR RCH D85310-6124. (X) 2 L 7 4 4F 4A25 1996030800015 19960308 00015 WP 1996 3 8 96ZZZX905 1 19960205 A 5330 SKIN DOUG DC8 DC862 3021970 WP BS 1220-1240 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 8974U 46110 LEVEL 2 CORROSION/AFT CARGO COMPARTMENT LOWER AREA, STR 34R BETWEEN STA 1220 AND STA 1240, FUSELAGE SKIN HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR PER SRM 51-1-0. (X) 2 L 7 4 4F 4A25 1996030800016 19960308 00016 NM 1996 3 8 ASAA9610016 1 19960211 A 3397 WIRE BOEING 737 737298C 1384490 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 ANC - FLT 20 - EMERGENCY EXIT LIGHTS ILLUMINATE IN THE ARMED POSITION. REPAIRED DEFECTIVE WIRING SPLICE CONNECTION AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1996030800017 19960308 00017 NM 1996 3 8 ASAA9610017 1 19960212 A 3350 MS2452423 SWITCH BOEING 737 737298C 1384490 NM F/A PANEL DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 ANC - FLT 51 - EMERGENCY EXIT LIGHTS ILLUMINATE IN THE ARMED POSITION (WING EXIT AND PART OF EMERGENCY EXIT FLOOR TRACK LIGHTS). REPLACED F/A EMERGENCY LIGHT SWITCH AND FOUND PIN D4250 PUSHED BACK; RESET PIN AND LIGHTS OPERATED NORMALLY. ( X) 2 L 7 2 4F RT A16WE 1996030800018 19960308 00018 NM 1996 3 8 ASAA9640007 1 19960206 A 3350 SOCKET BOEING 737 7374Q8 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 776AS 25109 SEA - DURING MAINTENANCE CHECK, FOUND AFT MOST SECTION OF EMERGENCY EXIT FLOOR TRACK LIGHTING INOPERATIVE. RECONNECTED TRACK LIGHT SOCKET; LIGHTS OPERATED NORMALLY. (X 2 L 7 2 4F RT A16WE 1996030800019 19960308 00019 NM 1996 3 8 ASAA9640008 1 19960208 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 776AS 25109 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS FOUND INOPERATIVE FROM ROW 26 AFT. RECONNECTED TR ACK WIRING AT ROW 26. LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1996030800020 19960308 00020 WP 1996 3 8 ASAA9680046 1 19960208 A 3350 60030431 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 935AS 49236 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 8 TO 12 FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND OPERATED NORMALLY. (X) 2 L 7 2 4F A6WE 1996030800021 19960308 00021 WP 1996 3 8 ASAA9680047 1 19960210 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 943AS 53018 SEA - DURING MAINTENANCE CHECK, EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 24 TO 27 FOUND INOPERATIVE. TIGHTENED LOOSE CONN ECTOR AT ROW 24 AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 1996030800022 19960308 00022 WP 1996 3 8 ASAA9680048 1 19960210 A 3350 41B004AD07G3 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 951AS 49111 SEA - DURING MAINTENANCE CHECK, THE LT AND RT AFT OVERWING EMERGENCY EXIT IDENTIFIER SIGNS WERE FOUND INOPERATIVE. REPL ACED THE BATTERIES AND OPERATED NORMALLY. (X) 2 L 7 2 4F A6WE 1996030800023 19960308 00023 WP 1996 3 8 ASAA9680049 1 19960210 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 953AS 49386 SEA - DURING MAINTENANCE CHECK, THE FORWARD TWO RED EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPAIRED WIRE TO TRACK LIGHTS AND OPERATED NORMALLY. (X) 2 L 7 2 4F A6WE 1996030800024 19960308 00024 WP 1996 3 8 ASAA9680050 1 19960212 A 3350 SOCKET DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 943AS 53018 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 27 TO 29 FOUND INOPERATIVE. RESET LIGHT SOCK ET AT ROW 27 AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 1996030800027 19960308 00027 NM 1996 3 8 AWXA960014 1 19960111 A 3020 655812310 DUCT ASSY BOEING 737 737297 1384480 NM NR 1 ENG COWL CRACKED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 147AW 22630 PHX/SJC - FLT 0870 - DURING CLIMB-OUT, NR 1 ENGINE FIRE LIGHT CAME ON. (NR 1 OVHT DET CURRENTLY ON MEL 26-02.) THE FIR E DET SYSTEM WOULD NOT TEST IN EITHER NORM OR FIRE. THE FIRE OVERHEAT SYSTEM DID START TO TEST IN NORM AND FIRE. AIRCR AFT RETURN TO PHX NO OVERWEIGHT LANDING INSPECTION REQUIRED. FOUND EXPANSION JOINT CRACKED ON DUCT AT TOP OF ENGINE FOR COWL ANTI-ICE VALVE. REPLACED DUCT, LEAK CHECK OK. REF MEL 26-02 FOUND CHAFED WIRE AT CONNECTOR D978 SPRING SUPPORT. REPLACED CONNECTOR, OPS OK MEL REMOVED. (X) 2 L 7 2 4F A16WE 1996030800029 19960308 00029 NE 1996 3 8 AWXA960054 2 19960206 A 7200 ENGINE BOEING 737 737277 1384570 NM PWA JT8 JT8D15 52051 NE NR 2 FAILED A AWXA A E UNSCHED LANDING ENGINE SHUTDOWN J K WARNING INDICATION FLUID LOSS CR CRUISE 1 WP 28 179AW 22646 P708321B CMH/BOS - FLT 1620 - AIR TURNBACK, IN-FLIGHT SHUTDOWN. ENGINE 2 LOW OIL PRESSURE LIGHT ILLUMINATED WITH PRESSURE ERRATI C. OIL TEMPERATURE AROUND 10. SHUT DOWN ENGINE. FOUND FERROS METAL IN THE MAIN ENGINE OIL FILTERS. REMOVED AND REPLA CED ENGINE. (X) 2 L 7 2 4F 4 F RT A16WE E2EA 1996030800030 19960308 00030 WP 1996 3 8 CAL960083 1 19960130 A 5280 SB093201893 SKIN DOUG DC9 DC981 3022081 WP LT MLG DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37882 39547 48027 HOU - INSPECTION FOUND SEVERAL CRACKS IN THE EXTERIOR SKIN OF LT INBOARD MLG DOOR. THE CRACKS WERE LOCATED UNDER GROUND SKID ATTACH POINTS. THE LONGEST CRACK WAS 2 INCHES. NEW SKIN WAS INSTALLED IAW SRM 51-30-2. (X) 2 L 7 2 4F A6WE 1996030800031 19960308 00031 WP 1996 3 8 CAL960084 1 19960129 A 5320 ANGLE DOUG DC9 DC981 3022081 WP DOOR CUTOUT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37882 39547 48027 HOU - INSPECTION FOUND ANGLE FITTING AT LOWER AFT CORNER OF AFT BAGGAGE BIN DOOR JAMB CUT-OUT CORRODED. THE CORRODED AN GLE FITTING WAS REMOVED AND A NEW ONE WAS INSTALLED IAW SRM 51-30-1. (X) 2 L 7 2 4F A6WE 1996030800032 19960308 00032 WP 1996 3 8 CAL960085 1 19960129 A 5511 RIB DOUG DC9 DC981 3022081 WP LT HORIZ STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37882 48027 HOU - INSPECTION FOUND LT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED. THE CRACK WAS LOCATED IN AREA WHERE SIDE ROLL ER BRACKET ATTACHES AND MEASURED 1 INCH LONG. THE AREA REPAIRED IAW SRM 55-01. (X) 2 L 7 2 4F A6WE 1996030800033 19960308 00033 WP 1996 3 8 CAL960086 1 19960124 A 5350 CABLES DOUG DC9 DC981 3022081 WP TAILCONES OUT OF RIG A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37882 48027 HOU - TAILCONE FAILED DROP TEST FROM INTERIOR HANDLE. A FORCE OVER 35 POUNDS WAS REQUIRED. THE TAILCONE CABLE SYSTEM W AS RIGGED AND TESTED IAW MM 53-53-00. (X) 2 L 7 2 4F A6WE 1996030800034 19960308 00034 WP 1996 3 8 CAL960087 1 19960125 A 5755 5910055519 PANEL DOUG DC9 DC981 3022081 WP LT SPOILER BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37882 17871 48027 HOU - INSPECTION FOUND THE LT WING INBOARD FLIGHT SPOILER PANEL NEARLY BROKEN IN HALF. THE SPOILER PANEL WAS REMOVED AN D REPLACED IAW MM 27-61-01. (X) 2 L 7 2 4F A6WE 1996030800035 19960308 00035 NM 1996 3 8 CAL960088 1 19960206 A 2612 CONNECTORS BOEING 737 737217 1384464 NM APU FIRE DET LOOSE A CALA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 SW 09 12231 19885 FLT NR 1517 - MDW - THE APU FIRE WARNING LIGHT ILLUMINATED AFTER TAKEOFF FROM MDW. THE APU FIRE BOTTLE WAS DISCHARGED, BUT THE LIGHT REMAINED ON. THE AIRCRAFT WAS RETURNED TO MDW WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED TH E APU AREA AND FOUND NO EVIDENCE OF FIRE. THE APU FIRE DETECTION SYSTEM AND APU FIRE EXTINGUISHING SYSTEM WERE PLACARDE D INOPERATIVE. LOOSE CONNECTORS WERE FOUND AT SHROUD DISCONNECT. THE CONNECTORS WERE CLEANED AND TIGHTENED. THE DETEC TION SYSTEM CHECKED GOOD. IN ADDITION, THE APU FIRE BOTTLE WAS REPLACED. BOTH PLACARDS WERE REMOVED. THE AIRCRAFT HAS COMPLETED OVER 25 FLTS SINCE THIS ANOMALY WAS FIRST REPORTED, WITHOUT A REPEAT OF THE PROBLEM. (M) 2 L 7 2 4F A16WE 1996030800036 19960308 00036 NM 1996 3 8 CAL960090 1 19960125 A 5314 KEEL BEAM BOEING 737 7373T0 1384582 NM BS 727 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14320 32810 23371 GSO - INSPECTION FOUND A 1.5 INCH CRACK AND CORROSION ON LT KEEL BEAM AT BS 727. AN ANGLE AND EXTERNAL STRAP REPAIR WAS INSTALLED IAW ECRA 5310-03224. (X) 2 L 7 2 4F RT A16WE 1996030800037 19960308 00037 NM 1996 3 8 CAL960091 1 19960121 A 5230 SKIN BOEING 737 7373T0 1384582 NM C-2 DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14320 32810 23371 GSO - INSPECTION FOUND C-2 DOOR EXTERIOR SKIN HAD DENTS, GOUGES, AND NICKS. THE DAMAGED SECTION OF SKIN WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 52-00-01. (X) 2 L 7 2 4F RT A16WE 1996030800038 19960308 00038 WP 1996 3 8 CKSA96008 1 19960123 A 2910 477633611 O-RINGS DOUG DC8 DC861 3021952 WP STAB LOCKOUT DETERIORATED A CKSA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 GL 23 812CK 49595 45890 KSEA - FLT 71431 - EN ROUTE TO KSEA LOST HYDRAULIC QUANTITY AND PRESSURE. RESEALED STABILIZER LOCK-OUT SWIVEL. OPS AND PRESSURE CHECK OK IAW 27-11-7. (X) 2 L 7 4 4F 4A25 1996030800039 19960308 00039 1996 3 8 CKSA96009 4 19960130 A 3418 C267072 TRANSDUCER DOUG DC8 DC863F 302198F WP RT WING SHORTED A CKSA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 23 870BX 54753 46036 KLAX - FLT 71573 - AFTER TAKEOFF, STALL WARNING AND STICK SHAKER STAYS ON FROM FLAP 12 DEGREE TO FLAP ZERO DEGREE POSITI ON. REMOVED AND REPLACED LIFT TRANSDUCER. OPS CHECKS NORMAL IAW MM 34-16-1. (X) 2 L 7 4 4F 4A25 1996030800040 19960308 00040 WP 1996 3 8 ORJA96004 1 19960126 A 3350 41B994AD073 BATTERY EA1D13D3 DOUG DC9 DC987 3022087 WP EMPENNAGE DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 751RA 49779 EMPENNAGE EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY. OPS CHECKS GOOD. (X) 2 L 7 2 4F RT A6WE 1996030800041 19960308 00041 NM 1996 3 8 PCAA9600260 1 19960106 A 7921 28E997 OIL COOLER DHAV DHC8 DHC8102 2809003 NM NR 1 ENGINE LEAKS A PCAA E ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 EA 13 416AW 10403 900056 282 LOW OIL PRESSURE ON NR 1 ENGINE REQUIRED PRECAUTIONARY SHUT-DOWN. (OIL LIGHT ILLUMINATED AND PRESSURE DROPPED SLOWLY TO 40 PSI AND SHUT-DOWN WAS INITIATED.) MASTER WARNING FLASHED WITHOUT CAPTION. REMOVED AND REPLACED OIL COOLER IAW MM. GROUND RAN AIRCRAFT. OPS CHECK AND LEAK CHECK GOOD, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. AIRCRAFT TOTAL C YCLES, 12,113. (X) 2 H 7 2 4T RT A13NM 1996030800042 19960308 00042 NM 1996 3 8 PCAA9600261 1 19960110 A 3350 82410162007 CONTROL BOX DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 819EX 016 EMERGENCY LIGHTS ILLUMINATED DURING FLIGHT. REMOVED AND REPLACED EMERGENCY LIGHTS CONTROL BOX, SYSTEM OPERATIONAL CHECK ED GOOD. AIRCRAFT RETURNED TO SERVICE. ACTT: 17,473 HOURS. ACTC: 18,580. (X) 2 H 7 2 4T RT A13NM 1996030800043 19960308 00043 NM 1996 3 8 PCAA9600262 1 19960110 A 2913 570347001 HYD PUMP DHAV DHC8 DHC8102 2809003 NM NR 2 ENGINE FAILED A PCAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 13 820EX 12865 5122 485721 019 UPON GEAR SELECTION DOWN, NR 2 ENGINE HYDRAULIC LIGHT ILLUMINATED, GEAR DID NOT OPERATE. CREW COMPLETED EMERGENCY CHECK LIST, GEAR OPERATED NORMALLY, SYSTEM PRESSURE RETURNED TO NORMAL. REMOVED AND REPLACED NR 2 ENGINE DRIVEN HYDRAULIC PU MP. RETRACTION TEST CHECKED GOOD. AROUND RAN AIRCRAFT, LEAK AND OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVIC E. ACTT: 17,539:42 HOURS. ACTC: 18,668. (X) 2 H 7 2 4T RT A13NM 1996030800044 19960308 00044 NM 1996 3 8 PCAA9600263 1 19960113 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM PASSENGER DOOR FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 810EX 001669 308 PASSENGER DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT POWER PACK. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. ACTT: 10,211:48 HOURS. ACTC: 11,411. (X) 2 H 7 2 4T RT A13NM 1996030800045 19960308 00045 NM 1996 3 8 PCAA9600264 1 19960129 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN LOOSE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 415AW 280 CABIN EMERGENCY LIGHTS ARE COMING ON FROM CLIMB-OUT TO CRUISE. INSPECTED AC CONTACTOR BOXES. SECURED LOOSE WIRES ON LI NE CONTACTOR. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. ACTT: 10,995:18. ACTC: 12,688. (X) 2 H 7 2 4T RT A13NM 1996030800046 19960308 00046 NM 1996 3 8 PCAA9600265 1 19960129 A 2611 473054 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM BAGG COMPT FAILED A PCAA O OTHER N FALSE WARNING NR NOT REPORTED 1 EA 13 827EX 000104 390 AFT BAG SMOKE DETECTOR WARNING ILLUMINATED IN-FLIGHT. PERFORMED SMOKE DETECTOR TEST, FOUND NR 1 SMOKE DETECTOR NOT TEST ING PROPERLY. ISOLATED NR 1 SMOKE DETECTOR IAW MEL PROCEDURE 26-8. AIRCRAFT RETURNED TO SERVICE. ACTT: 3,169:18. AC TC: 3,667. (X) 2 H 7 2 4T RT A13NM 1996030800047 19960308 00047 SO 1996 3 8 SRAA19602 1 19960119 A 3230 RETRACT MECH LKHEED 382 382E 526413U SO RT MLG LACK OF LUBE A SRAA O OTHER N FALSE WARNING CL CLIMB 1 SO 19 910SJ 4383 CYWG - FLT 1002 - OUT OF CYWG ON LANDING GEAR RETRACTION (OAT MINUS 35 DEGREES CELSIUS), RT MLG INDICATED FULL DOWN. ON DESCENT TO LAX, RT MLG INDICATED UP - (OAT PLUS 15 DEGREES CELSIUS), CYCLED GEAR. OPS CHECKS NORMAL, UNABLE TO DUPLICA TE INDICATIONS. POST-FLIGHT INSPECTED RT MLG FOR PROPER LUBRICATION, INSTALLATION AND CONDITION OF POSITION INDICATOR S WITCHES - ALL FOUND NORMAL IAW MM CHAPTER 32. (X) 2 H 7 4 4T A1SO 1996030800048 19960308 00048 SO 1996 3 8 SRAA29601 1 19960201 A 2613 1734316700 DETECTOR LKHEED 382 382G 526414U SO NR 3 ENGINE MALFUNCTIONED A SRAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 19 920SJ 4561 FLT ADT07 - ON TAKEOFF ROLL FROM MHZ, MASTER TURBINE OVERHEAT ILLUMINATED, ABORTED TAKEOFF AND RETURNED TO BLOCK. FOUND NR 3 ENGINE AT 7 O'CLOCK OVERHEAT DETECTOR DID NOT FUNCTION PROPERLY, REPLACED NR 7 DETECTOR. SYSTEM OPS CHECKED GOOD PER MM, CHAPTER 26. (X) 2 H 7 4 4T A1SO 1996030800049 19960308 00049 GL 1996 3 8 SRAA29602 2 19960202 A 7230 VENT TUBE LKHEED 382 382E 526413U SO ALLSN 501D 501D22A 03006 GL NR 3 ENGINE CRACKED A SRAA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 19 908SJ 4300 FLT UPA3060 - ON CLIMB-OUT FROM LTN, NR 3 ENGINE NACELLE OVEHEAT LIGHT ILLUMINATED, SHUT DOWN NR 3 ENGINE AND ACCOMPLISH ED AIR TURN BACK TO LTN. FOUND COMPRESSOR VENT TUBE CRACKED, REPLACED LINE AND PERFORMED ENGINE RUN-UP, LEAK CHECKED GO OD PER MM CHAPTER 75-00. (X) 2 H 7 4 4T 4 T A1SO E282 1996030800050 19960308 00050 WP 1996 3 8 TC8A96001 1 19960125 A 3610 PNEUMATIC LINE DOUG DC8 DC8F54 3021926 WP NR 1 ENGINE LOOSE A TC8A O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 802CK 45679 SBGR/SBGR - FLT 2405 - NR 1 ENGINE FIRE ALARM CAME 'ON' DURING CLIMB, SHORTLY AFTER TAKEOFF. TIGHTENED PNEUMATIC LINE A T AFT REVERSER SYSTEM. CHECK OPS OK IAW MM 78-02. (X) 2 L 7 4 4F 4A25 1996030800051 19960308 00051 WP 1996 3 8 TC8A96002 1 19960127 A 2612 FIRE LOOP DOUG DC8 DC8F54 3021926 WP ENGINE MALFUNCTIONED A TC8A O OTHER N FALSE WARNING TO TAKEOFF 1 GL 23 802CK 45679 SBGR - FL 02604 - FALSE FIRE ALARM ON NR 3 ENGINE ON MCT (MAXIMUM CONTINUOUS TAKEOFF). ISOLATED ENGINE FIRE LOOP. CHEC KED PER MM 26-2-0. (X) 2 L 7 4 4F 4A25 1996030800052 19960308 00052 WP 1996 3 8 TC8A96003 1 19960203 A 8012 CLAMP DOUG DC8 DC8F54 3021926 WP NR 3 START VLV LOOSE A TC8A O OTHER N FALSE WARNING CR CRUISE 1 GL 23 802CK 45679 SBCF/SBGR - FLT 03301 - FALSE ENGINE FIRE ALARM NR 3. TIGHTENED CLAMP AT STARTER VALVE, CHECKED IAW 80-1-0, NORMAL. (X ) 2 L 7 4 4F 4A25 1996030800053 19960308 00053 NM 1996 3 8 WRLA96005 1 19960127 A 2460 750866C ELECT PCU DOUG MD11 MD11 3023602 NM E/E COMPT TRIPPED A WRLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 273WA 48519 ON PUSHBACK, FLIGHT CREW NOTED A LEVEL 2 ALERT 'NR 2 ENGINE OIL PRESSURE LOW'. FLIGHT CREW ELECTED TO RETURN TO GATE FO R CORRECTIVE ACTION. AIRCRAFT RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE FOUND NO OIL LEAKS ON NR 2 ENGINE. RESET ELECTRICAL POWER CONTROL UNIT IN CFDS. RESTART NR 2 ENGINE. NO ALERTS FOUND, CHECKED NORMAL. AIRCRAFT RETURNED TO SE RVICE. (X) 2 L 7 3 4F RT A22WE 1996030800054 19960308 00054 NM 1996 3 8 WRLA96006 1 19960201 A 3210 TRANSDUCER WIRE DOUG MD11 MD11 3023602 NM NR 3 MLG WHEEL BROKEN A WRLA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 280WA 48458 ON TAXIING OUT, FLIGHT CREW RECEIVED A NR 3 TIRE PRESSURE/WHEEL TRANSDUCER ALERT. LEVEL 2. AIRCRAFT RETURNED TO GATE W ITHOUT FURTHER INCIDENT. MAINTENANCE DISCOVERED THE NR 3 MAIN WHEEL ASSY WHEEL TRANSDUCER RETAINING BOLT BROKEN, P/N NA S 640413. BOLT WAS REPLACED AND NR 3 TIRE PRESSURE INDICATION PLACED ON MEL 32-45-2 DUE TO BROKEN WIRE IN AXLE. AIRCRA FT RETURNED TO SERVICE. (X) 2 L 7 3 4F RT A22WE 1996030800055 19960308 00055 NE 1996 3 8 YIEA96002 2 19960118 A 7200 ENGINE AMD FALC20 FALCON 2720302 EU GE CF700 CF7002D2 30010 NE LEFT FLAME OUT A YIEA O OTHER X ENGINE FLAMEOUT CL CLIMB 1 GL 23 816AA 11905 6013 290 245U122 PILOT REPORTED WHILE IN A STEADY STATE CLIMB-OUT OF FL 310, LT ENG FLAMED OUT AT 31,400 FEET. ACFT FLYING AT .68 MACH. THERE WERE NO CLOUDS AND NO TURBULENCE. CREW DESCENDED AND TRIED RESTARTS AT FL 290, FL 250, AND FL 150 WITHOUT SUCCES S. ENG RELIGHT FINALLY ACHIEVED AT 11,000 FEET. ACFT CONTINUED TO DESTINATION WITHOUT INCIDENT. ENG GIVEN A THOROUGH INSPECTION OF INLET AND EXHAUST FOR EVIDENCE OF FOD, BUT NONE FOUND. FUEL SYS CHECKED. A FULL GRND POWER RUN PERFORMED ON ENG IAW GE MM AND ALL PARAMETERS CHECKED WITHIN LIMITS. NO MECHANICAL CAUSE COULD BE FOUND FOR FLAME-OUT. THIS SAM E FLIGHT CREW SUFFERED A FLAME-OUT OF LT ENG ON ANOTHER ACFT WITHIN PREVIOUS 24 HRS. ENG RETURNED TO SERVICE. (X) 2 L 7 2 4F 4 F A7EU E7EA 1996030800056 19960308 00056 EU 1996 3 8 9604913224 1 19960227 A 3350 100865 EPSU AIRBUS 320 A320211 3930320 EU CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 324US 273 DURING LINE MAINTENANCE, THE AFT SECTION OF EMERGENCY FLOOR PATH LIGHTS WERE INOPERATIVE. REPLACED EPSU 11O WL 3, OPERA TIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996030800057 19960308 00057 WP 1996 3 8 9604929966 1 19960229 A 2422 3980001 BOOST PUMP DOUG DC9 DC931 3022065 WP FUEL TANKS FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 9330 35217 4017 47138 CAPTAIN'S NAV FLAGGED ON HSI AFTER TAKEOFF. THIS WAS FOLLOWED BY NUMEROUS CIRCUIT BREAKERS POPPING INCLUDING THE LEFT A C BUS C-PHASE. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED BOTH A AND C PHASE CIRCUIT BRE AKERS FOR LEFT AC BUS. FOUND ALL PHASES OF CENTER FORWARD FUEL BOOST PUMP CIRCUIT BREAKERS POPPED. THIS IS THE SUSPECT ED CAUSE FOR THE LEFT AC BUS CIRCUIT BREAKER POPPED. REPLACED CENTER FORWARD FUEL BOOST PUMP. LEAK AND OPERATIONAL CHE CK NORMAL. 2 L 7 2 4F A6WE 1996030800058 19960308 00058 WP 1996 3 8 9604939998 1 19960229 A 3350 6011779 BATTERY PACK DOUG DC9 DC931 3022065 WP LT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8934E 47143 DURING LINE MAINTENANCE INSPECTION, FOUND THE LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIO NAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996030800059 19960308 00059 WP 1996 3 8 9604949998 1 19960229 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8934E 47143 DURING LINE MAINTENANCE INSPECTION, FOUND MULTIPLE OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATION AL CHECK NORMAL. 2 L 7 2 4F A6WE 1996030800060 19960308 00060 WP 1996 3 8 9604959908 1 19960228 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 958N 47254 DURING LINE MAINTENANCE INSPECTION, FOUND CEILING EMERGENCY LIGHTS INOPERATIVE IN COCKPIT, GALLEY AND ENTRY. REPLACED B ATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996030800061 19960308 00061 WP 1996 3 8 9604969919 1 19960222 A 5350 GUIDE PINS DOUG DC9 DC932 3022066 WP TAIL CONE WORN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 941N 47450 DURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE TAIL CONE HANDLE AND THAT THE TAIL CONE DID NOT D ROP. ALSO, FOUND 16 WORN GUIDE PINS AND 7 WORN PLATES. REPLACED THE PINS, PLATES AND ACCOMPLISHED EO 5350-01049, CHECK ED OK. 2 L 7 2 4F A6WE 1996030800062 19960308 00062 NM 1996 3 8 9604976633 1 19960217 A 5730 PANEL BOEING 747 747227B 1384888 NM TE WING SEPARATED A NWAA K NONE D INFLIGHT SEPARATION UK UNKNOWN 1 GL 01 633US 21991 EN ROUTE, THE LEFT WING TRAILING EDGE PANEL INBOARD OF NR 6 SPOILER BEGAN FLUTTERING WITH SUBSEQUENT INFLIGHT SEPARATION OF APPROXIMATELY A 30 INCH BY 50 INCH SECTION. CONTINUED TO NRT WITHOUT FURTHER INCIDENT. REPLACED THE TRAILING EDGE PANEL AND THE INBOARD FOREFLAP (P/N 65B39011-13) AND REPAIRED THE INBOARD MID FLAP, UPPER INBOARD SURFACE PER SRM 51-10- 01 PARA 9 PG 18. 2 L 7 4 4F A20WE 1996030800063 19960308 00063 NM 1996 3 8 9604985501 1 19960229 A 2741 POSITION TRANS BOEING 757 757251 1384970 NM HORIZ STAB FAILED A NWAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 01 501US 23190 DURING APPLICATION OF TAKEOFF POWER, STABILIZER WARNING MESSAGE ILLUMINATED AND TAKEOFF WAS ABORTED. VERIFIED STABILIZE R TRIM SETTING WAS WITHIN GREEN BAND AND MESSAGE REMAINED. MAINTENANCE REPLACED THE CENTER STABILIZER TRIM POSITION TRA NSMITTER AND OPERATIONAL CHECK WAS NORMAL. 2 L 7 2 4F RT A2NM 1996030800064 19960308 00064 NM 1996 3 8 96FDEA00010 1 19960104 A 5313 BAC1498113 STRINGER BOEING 727 727227 1384078 NM BS 720 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 488FE 21491 CORROSION (C53-224-01), ON STR FLANGE AT BS 720 LT STR 4. REMOVED DAMAGED SECTION OF STR, FABRICATED AND INSTALLED REPA IR PARTS PER FEDEX SRM 53-10-3. 2 L 7 3 4F A3WE 1996030800065 19960308 00065 NM 1996 3 8 96FDEA00011 1 19960104 A 5347 BAC1510190 SEAT TRACK BOEING 727 727227 1384078 NM BS 950 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 488FE 21491 CORROSION (C53-224-04), ON SEAT TRACK AT CLIP NUT HOLES BS 950E PLUS 18 RBL 1. REPLACED SEAT TRACK AND INSTALLED REPAIR STRAP IAW FEDEX SRM 53-10-05. 2 L 7 3 4F A3WE 1996030800066 19960308 00066 NM 1996 3 8 96FDEA00012 1 19960104 A 5315 FLOOR BEAM BOEING 727 727227 1384078 NM BS 720 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 488FE 21491 CORROSION ON LOWER FLANGE OF FLOOR BEAM AT BS 720 WL 200 LBL 45 TO RBL 45. REPAIRED FLOOR BEAM AT BS 720 WL 200 LBL 4 5 TO RBL 45. 2 L 7 3 4F A3WE 1996030800067 19960308 00067 NM 1996 3 8 96FDEA00064 1 19960115 A 5320 STIFFENER BOEING 727 72722 1384002 NM BS 336 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 CORROSION (C53-224-03-1/2), ON VERTICAL STIFFENER, BS 336 WL 181 RBL 15. REMOVED CORROSION AND INSTALLED REPAIR IAW FED EX SRM 51-40-4. 2 L 7 3 4F A3WE 1996030800068 19960308 00068 NM 1996 3 8 96FDEA00147 1 19960130 A 5315 BAC14902865 FLOOR BEAM BOEING 727 72722 1384002 NM BS 312 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CORROSION ON FLOOR BEAM (C 53-224-01, -1), BS 312 WL 208 LBL 46. REMOVED CORROSION ON FLOOR BEAM AT BS 312 WL 208 LBL 46 OUT OF LIMITS PER FEDEX SRM 53-10-1. REPAIRED FLOOR BEAM PER FEDEX SRM 53-10-8. 2 L 7 3 4F A3WE 1996030800069 19960308 00069 NM 1996 3 8 96FDEA00148 1 19960130 A 5320 SHEAR TIE BOEING 727 72722 1384002 NM BS 1030 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CORROSION (C53-111-01, -3), AFT CARGO ON SHEAR TIE AT BS 1030 RBL 4 WL 138.5. REPAIRED SHEAR TIE AT BS 1030 RBL 4 WL 13 8.5 AS PER FEDEX SRM 53-10-4. 2 L 7 3 4F A3WE 1996030800070 19960308 00070 NM 1996 3 8 96UAL900155 1 19960229 A 2751 2061141 INDICATOR BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE TE FLAP SHORTED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 905UA 25005 AFTER TAKEOFF, FLAP INDICATOR FAILED AT POSITION NR 1. FLAPS EXTENDED NORMALLY. SUPPLEMENTAL DATA UPDATE: FOUND AN OP EN CIRCUIT IN THE FLAP ASYMMETRY PROTECTION CIRCUIT WITHIN THE TRAILING EDGE FLAP POSITION INDICATOR. 2 L 7 2 4F 4 F RT A16WE E2GL 1996030800071 19960308 00071 NM 1996 3 8 96UAL900156 1 19960229 A 2130 PRESSURIZATION BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 7264U 21411 DIVERTED TO CID DUE TO LOSS OF PRESSURIZATION. SUPPLEMENTAL DATA UPDATE: AIRCRAFT CHECKED FOR OBVIOUS DEFECTS. NONE F OUND. AIRCRAFT PRESSURE CHECKED OKAY. VERIFIED FORWARD CARGO HEAT OUTFLOW WORKING. NO SUBSEQUENT COMMENTS ON PRESSURI ZATION. 2 L 7 3 4F 4 F A3WE E2EA 1996030800072 19960308 00072 SO 1996 3 8 COMA9610090 1 19960224 A 5270 WARNING LIGHT EMB 120 EMB120RT SO SERVICE DOOR ILLUMINATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 161CA 120143 SERVICE DOOR WARNING LIGHT ILLUMINATED DURING TAKEOFF. ALL DOORS CONFIRMED CLOSED, COULD NOT DUPLICATE DISCREPANCY. AL L DOORS INSPECTED FOR SECURITY AND FUNCTION. 2 L 7 2 4T RT A31SO 1996030800073 19960308 00073 SO 1996 3 8 COMA9610091 1 19960222 A 6120 AURAL WARNING EMB 120 EMB120RT SO AUTOFEATHER SYS ACTIVATED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 263CA 120255 AUTOFEATHER AURAL WARNING DURING TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. CLEANED AND TIGHTENED WIRING CONNECTORS AT THE TORQUE SIGNAL CONDITIONERS. 2 L 7 2 4T RT A31SO 1996030800074 19960308 00074 EA 1996 3 8 COMA9660031 1 19960225 A 3231 601R751461 CONTROL VALVE CNDAIR CL600 CL6002B19 EA NLG DOORS MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 927CA 7031 NOSE LANDING GEAR DOOR OPEN MESSAGE ON EICAS AFTER GEAR RETRACTED. REPLACED THE NLG DOORS CONTROL VALVE. 2 L 7 2 4F RT A21EA 1996030800075 19960308 00075 NM 1996 3 8 DL72S960436 1 19960227 A 3350 1000677 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 532DA 22045 FOUND EMERGENCY EXIT LIGHT INOP AT AFT LT DOOR IN EMERGENCY. REPLACED LIGHT ASSY. 2 L 7 3 4F A3WE 1996030800076 19960308 00076 NM 1996 3 8 DL72S960445 1 19960227 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 1 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 526DA 21586 FOUND DURING E-1 LETTER CHECK, .1875 INCH CRACK IN COVE ANGLE NR 1 SLAT BELOW TAI DUCT. REPAIRED PER MM 57-54-0 PG 5A. 2 L 7 3 4F A3WE 1996030800077 19960308 00077 NM 1996 3 8 DL72S960446 1 19960227 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 7 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 526DA 21586 FOUND DURING E-1 LETTER CHECK, NR 7 SLAT ANGLE CRACKED AT ANTI-ICE DUCT CUTOUT. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1996030800078 19960308 00078 NM 1996 3 8 DL72S960452 1 19960228 A 5751 652176624 SPAR BOEING 727 727232 1384082 NM AILERON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 467DA 20744 SPAR WAS FOUND CRACKED NEAR TAB FITTING. SPLICED SPAR SECTION PER SRM 51-40-3 FIG 1. FOUND DURING SHOP INSPECTION OF A ILERON ASSEMBLY. 2 L 7 3 4F A3WE 1996030800079 19960308 00079 NM 1996 3 8 DL72S960453 1 19960228 A 5751 652176624 SKIN BOEING 727 727232 1384082 NM AILERON WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 467DA 20744 LOWER SKIN WAS FOUND WITH OVERSIZED HOLES. SPLICED SKIN SECTION PER M/M 57-51-0 FIG 801. FOUND DURING SHOP INSPECTION OF AILERON ASSEMBLY. 2 L 7 3 4F A3WE 1996030800080 19960308 00080 NM 1996 3 8 DL72S960456 1 19960228 A 5210 SKIN BOEING 727 727232 1384082 NM MAIN ENT DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 468DA 20745 MAIN ENTRY DOOR OUTER SKIN CRACKED .25 INCH AT RIVET TOP AFT CORNER. FOUND AT D-2 LTR CHECK. REPAIRED PER MM 52-11-01 FIG 804. 2 L 7 3 4F A3WE 1996030800081 19960308 00081 NM 1996 3 8 DL72S960461 1 19960228 A 5330 6518420482 SKIN BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 476DA 20753 THE FUSELAGE SKIN AND UNDERLYING DOUBLER WAS FOUND TO HAVE A .25 INCH CRACK IN THE UPPER FORWARD CORNER OF THE L-1 DOOR CUTOUT. A TIME LIMITED REPAIR HAS BEEN INSTALLED AND A PERMANENT REPAIR WILL BE INSTALLED PER SB 727-53-0186, REV 1. 2 L 7 3 4F A3WE 1996030800082 19960308 00082 NM 1996 3 8 DL72S960466 1 19960228 A 5320 BEAR STRAP BOEING 727 727232 1384082 NM FS 1070 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 467DA 20744 DURING INSPECTION, CORROSION WAS FOUND ON THE INTERNAL SKIN DOUBLER OF THE R-2 DOOR CUTOUT AT STATION 1070. IN ACCORDAN CE WITH FAA/DER FORM 8110-3 DATED 2-8-96, THE DAMAGE WAS CUT OUT AND A DOUBLER AND TRIPLER INSTALLED. 2 L 7 3 4F A3WE 1996030800083 19960308 00083 NM 1996 3 8 DL72S960467 1 19960228 A 5330 6518420282 SKIN BOEING 727 727232 1384082 NM FS 345 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 467DA 20744 DURING INSPECTION, THREE CRACKS WERE FOUND IN THE SKIN AND DOOR SURROUND STRUCTURE IN THE LOWER AFT CORNER OF THE L1 DOO R CUTOUT. ALL CRACKS GO THROUGH THE SKIN, BONDED DOUBLER AND THE BEAR STRAP. CRACK LENGTH VARIED FROM 1 TO 2 INCH LENG TH. IN ACCORDANCE WITH FAA/DER FORM 8110-3 DATED 02-28-96, THE DAMAGED AREA WAS CUT OUT AND A DOUBLER AND TRIPLER WERE INSTALLED. 2 L 7 3 4F A3WE 1996030800084 19960308 00084 NM 1996 3 8 DL757960449 1 19960215 A 5754 114N4003171 SKIN BOEING 757 757232 1384965 NM NR 2 LE SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 632DL 23613 DURING SHOP INSPECTION FOR NR 2 L/E SLAT, FOUND T/E WEDGE DELAMINATED. REPAIRED PER SRM 57-43-02. 2 L 7 2 4F RT A2NM 1996030800085 19960308 00085 NM 1996 3 8 DL757960451 1 19960227 A 5330 5924802 SKIN BOEING 757 757232 1384965 NM FS 237-262 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 652DL 24392 LT FUSELAGE SKIN WAS FOUND WITH DENTS BETWEEN FS 237 AND FS 255 ABOVE STR 18. SINCE VARIOUS DENTS REQUIRE CUT OUT, THE FORWARD SECTION OF THE SKIN PANEL IS CUT VERTICALLY AT FS 262 FROM THE LOWER EDGE OF THE PANEL AT THE CUSP STR 18L UP TO THE PANEL UPPER EDGE BELOW STR 15L. THE FORWARD SECTION OF THE PANEL WAS REPLACED AND A REPAIR SPLICE ADDED AT FS 262. THE SUBJECT SKIN PANEL IS MADE FROM 0.050 THICK 2024-T3 AL CLAD MATERIAL. ACCOMPLISHED REPAIRS PER DL ERA 273375 REV A. 2 L 7 2 4F RT A2NM 1996030800086 19960308 00086 NM 1996 3 8 DL757960474 1 19960228 A 2820 312N310019 FUEL LINE BOEING 757 757232 1384965 NM NR 1 PYLON CRACKED A DALA O OTHER K FLUID LOSS IN INSP/MAINT 1 SO 27 625DL 22915 ON PREFLIGHT, FOUND FUEL LEAK IN PYLON AREA OF NR 1 ENGINE. FOUND FUEL FEED LINE LEAKING DUE TO CRACK AT FLANGE, FWD EN D OF LINE. REPLACED FUEL FEED LINE. 2 L 7 2 4F RT A2NM 1996030800087 19960308 00087 WP 1996 3 8 DLL15960454 1 19960228 A 3350 BATTERY PACK 5165741 LKHEED 1011 10113853 5265020 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 751DA 38241 193W1166 DURING PREFLIGHT, FOUND AFT CABIN EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK, OPERATION NORMAL. 2 L 7 3 4F A23WE 1996030800088 19960308 00088 WP 1996 3 8 DLL15960459 1 19960206 A 5753 1529112109AD SKIN LKHEED 1011 10113853 5265020 WP NR 1 FLAP VANE GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 756DR 193Y1185 UPON ROUTINE INSPECTION, A 12 INCH GOUGE WAS FOUND ON I/B END TOP SKIN. REPAIRED AS PER SRM 57-53-00, FOR LT NR 1 FLAP VANE. 2 L 7 3 4F A23WE 1996030800089 19960308 00089 WP 1996 3 8 DLL17960455 1 19960218 A 5753 1529112110AD SKIN LKHEED 1011 10113853 5265020 WP NR 1 FLAP VANE WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 766DA 193H1207 GROOVE WORN THROUGH UPPER SKIN, I/B END. INSTALLED EXTERNAL REPAIR DOUBLER PER SRM 57-53-00. FOUND DURING INSPECTION O F NR 1 RT FLAP VANE. 2 L 7 3 4F A23WE 1996030800090 19960308 00090 EU 1996 3 8 QXEA9600088 1 19960229 A 3350 6008905 BATTERY FOKKER F28 F28MK1000 4990808 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 801PH 11097 BOI - RIGHT OVERWING EXIT LIGHT IS INOPERATIVE. BATTERY R31 WAS REPLACED I/A/W MAINT MANUAL. LIGHT OPS CHECKED GOOD. A IRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996030800091 19960308 00091 EU 1996 3 8 QXEA9600089 1 19960228 A 3350 1315 BULB FOKKER F28 F28MK1000 4990808 EU GALLEY FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 802PH 11017 GEG - EMERGENCY EXIT LIGHT ABOVE GALLEY IS INOPERATIVE AND SIGN NEXT TO GALLEY IS INOPERATIVE. BULBS WERE REPLACED AND LIGHTS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996030800092 19960308 00092 EU 1996 3 8 QXEA9600090 1 19960229 A 3350 1012721 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 468US 11095 PDX - ROW 8CDE EXIT LIGHT IS INOPERATIVE. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996030800094 19960308 00094 NM 1996 3 8 9604996310 1 19960303 A 3350 CONNECTOR PIN BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 670US 24225 DURING LINE CHECK, THE FLOOR MOUNTED EMERGENCY PATH LIGHTS BETWEEN UPPER DECK SEAT ROWS 77 TO 79 WERE FOUND INOPERATIVE. RECONNECTED LOOSE LIGHT ASSEMBLY PIN FOUND AT SEAT 79 AND OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996030800095 19960308 00095 EU 1996 3 8 9605003236 1 19960301 A 3260 INTERFACE UNITS AIRBUS 320 A320211 3930320 EU NR 1/2 MALFUNCTIONED A NWAA O OTHER N FALSE WARNING UK UNKNOWN 1 GL 01 336NW 355 ON THE WHEEL PAGE OF THE ECAM, THE NOSE LANDING GEAR TRIANGLE INDICATED RED WITH THE GEAR DOWN. CYCLED THE LANDING GEAR HANDLE AND ALL INDICATIONS WERE NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 AND NR 2 LAND ING GEAR CONTROL INTERFACE UNITS AND OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996030800096 19960308 00096 NE 1996 3 8 9605011144 2 19960301 A 7230 COMPRESSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 3 ENGINE STALLED A NWAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS LD LANDING 1 GL 01 144JC 46753 86149 DURING LANDING ROLLOUT, THE NR 3 ENGINE EXPERIENCED REVERSE STALL. CREW FOLLOWED COCKPIT OPERATING PROCEDURE AND NR 3 E NGINE SHUTDOWN WAS ACCOMPLISHED WITHOUT FURTHER INCIDENT. BORESCOPE INSPECTION OF NR 3 ENGINE HPC 13TH AND 15TH STATOR STAGES REVEALED NO DISCREPANCIES. 2 L 7 3 4F 4 F A22WE E20EA 1996030800097 19960308 00097 EU 1996 3 8 9605023212 1 19960303 A 2120 87292325V04 COMPUTER AIRBUS 320 A320211 3930320 EU AVIONICS COMPT MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 312US 8708 8438 152 DURING CLIMBOUT, RECEIVED VENT AVIONICS SYS FAULT, FOLLOWED SHORTLY BY VENT EXTRACT FAULT. SEVERAL MINUTES LATER, RECEI VED AVIONICS SMOKE MESSAGE AND GEN 1 LINE SMOKE LIGHT ILLUMINATED. AIRCRAFT DIVERTED TO CLE AND LANDED WITHOUT INCIDENT WITH EMERGENCY EQUIPMENT STANDING BY. MAINTENANCE REPLACED THE AVIONICS EQUIPMENT VENTILATION COMPUTER AND OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996030800098 19960308 00098 EU 1996 3 8 9605033236 1 19960302 A 3260 848401 PROX SENSOR AIRBUS 320 A320211 3930320 EU NLG MALFUNCTIONED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 336NW 355 DURING APPROACH, RECEIVED L/G DOORS NOT CLOSED MESSAGE AFTER LOWERING THE LANDING GEAR. ALSO, THE WHEEL PAGE ON ECAM DI SPLAYED ONE RED GEAR TRIANGLE. CYCLED LANDING GEAR HANDLE AND ALL INDICATIONS WERE NORMAL. AIRCRAFT LANDED WITHOUT INC IDENT. MAINTENANCE REPLACED BOTH NOSE LANDING GEAR UPLOCK PROXIMITY SENSORS 18GA AND 19GA, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996030800099 19960308 00099 WP 1996 3 8 9605049876 1 19960303 A 3222 STRUT DOUG DC9 DC951 3022051 WP NLG REQD SERVICE A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 785NC 48110 DURING CLIMBOUT, GEAR UNSAFE LIGHT ILLUMINATED UPON GEAR RETRACTION. RECYCLED GEAR AND RETRACTED NORMALLY. FLIGHT RETU RNED TO MSP AND LANDED WITHOUT INCIDENT. FOUND NOSE STRUT LOW. REPLACED NOSE LANDING GEAR STRUT SERVICING VALVE. SERV ICED STRUT AND CHECKED GOOD. 2 L 7 2 4F A6WE 1996030800100 19960308 00100 NM 1996 3 8 96FDEA00363 1 19960301 A 5320 651758866 G-BEAM BOEING 727 727233 138408A NM BS 267 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 266FE 21672 CORROSION BS 267 BL 0 LBL 5 WL 208 ON G-BEAM. REMOVED G-BEAM, DRILLED UP AND INSTALLED NEW G-BEAM. INSTALLED ALL ACCES S PANELS. REMOVED FOR ACCESS TO G-BEAM. 2 L 7 3 4F RT A3WE 1996030800101 19960308 00101 NM 1996 3 8 96FDEA00364 1 19960301 A 5311 FRAME BOEING 727 727233 138408A NM BS 970 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 266FE 21672 CORROSION (C53-113-01, -2) ON FRAME JUST O/B OF STR 29L AROUND FASTENERS COMMON TO SKIN AND KEEL BEAM, BS 970 WL 138.5 L BL 8. CORROSION WAS OUT OF LIMITS PER SRM 53-10-1. REMOVED CORRODED SHEAR TIE, BS 970 WL 138.5 LBL 8L AND REPAIRED PER SRM 53-10-4. 2 L 7 3 4F RT A3WE 1996030800102 19960308 00102 NM 1996 3 8 96FDEA00365 1 19960301 A 5320 65198618 CHORD BOEING 727 727233 138408A NM BS 275-360 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 266FE 21672 CORROSION (C53-100-01-1) ON UPPER I/B FLANGE OF LOWER RT NOSE CHORD BS 360 TO 344 RBL 16 WL 145 BELLY AREA, ACCESS IS RE QUIRED. REMOVED RT LOWER NOSE CHORD AT BS 360 TO 275 RBL 16 WL 145, REPLACED CHORD AND REINSTALLED ALL ITEMS REMOVED FO R ACCESS. 2 L 7 3 4F RT A3WE 1996030800103 19960308 00103 NM 1996 3 8 96FDEA00366 1 19960301 A 5320 CHORD BOEING 727 72722 1384002 NM BS 1342 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 AREA OF CORROSION ON BS 1342 CHORD UPPER FWD RT FLANGE RBL 20. REMOVED AND REPLACED UPPER CHORD IAW FEDEX DRAWING 65-17 508. 2 L 7 3 4F A3WE 1996030800104 19960308 00104 NM 1996 3 8 96FDEA00367 1 19960301 A 5320 WEB BOEING 727 72722 1384002 NM BS 520 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 104FE 19143 CRACK IN WEB AT BS 520 WL 198 RBL 58. REMOVED, FABRICATED NEW WEB AND INSTALLED THE WEB AT BS 500 TO 560 RBL 58 WL 198, AS PER BOEING DRAWING 65-19309. 2 L 7 3 4F A3WE 1996030800105 19960308 00105 NM 1996 3 8 96FDEA00368 1 19960228 A 5320 65242581 STRAP BOEING 727 72722 1384002 NM BS 520 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION (C53-111-01-2), ON FWD CARGO BAY THRESHOLD STRAP, BS 520 RBL 24 WL 156. REMOVED AND REPLACED THE FWD CARGO BA Y THRESHOLD STRAP BS 500 TO 580 RBL 24 WL 156. 2 L 7 3 4F A3WE 1996030800106 19960308 00106 NM 1996 3 8 96FDEA00369 1 19960228 A 5320 BAC14902763 FAIL-SAFE BOEING 727 72722 1384002 NM BS 380 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION (53-111-01-1) ON THE FAIL-SAFE AT BS 380 STR 26L WL 150 AROUND I/B FASTENER HOLE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-40-3. 2 L 7 3 4F A3WE 1996030800107 19960308 00107 NM 1996 3 8 96FDEA00370 1 19960301 A 5313 STRINGER BOEING 727 72722 1384002 NM BS 560 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 MECH DAMAGE ON STR 25L BS 560 WL 154. REPAIRED DAMAGED STR AT BS 560 STR 25L WL 154 PER FEDEX EA 7-5310-27491. 2 L 7 3 4F A3WE 1996030800108 19960308 00108 NM 1996 3 8 96FDEA00371 1 19960301 A 5320 STIFFENER BOEING 727 72722 1384002 NM BS 740 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 WHILE WORKING 7-5310-7-3367B PT 1, DISCOVERED A CRACK IN THE FWD PRESSURE PAN STIFFENER AT BS 740 WL 208 LT. ALSO, FOUN D FWD PRESSURE PAN DAMAGED, FABRICATED NEW STIFFENER AND RIVETED TOGETHER NEW PAN. ALL WORK ACCOMPLISHED PER FEDEX SRM 51-20-1 AND BOEING DRAWING NR 65-38294. 2 L 7 3 4F A3WE 1996030800109 19960308 00109 NM 1996 3 8 96FDEA00372 1 19960228 A 5320 65207264 THRESHOLD WEB BOEING 727 72722 1384002 NM BS 527 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION (C53-111-01-1) ON DOOR THRESHOLD VERTICAL WEB, BS 527 RBL 22 WL 156. REMOVED, FABRICATED AND INSTALLED VERTIC AL AND HORIZONTAL WEB PER SRM 53-10-1. 2 L 7 3 4F A3WE 1996030800110 19960308 00110 NM 1996 3 8 96FDEA00373 1 19960304 A 5320 65189553 FITTING BOEING 727 72722 1384002 NM BS 360 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION 26L BS 360 FITTING. REPLACED STR TIE FITTING AT STR 26L, BS 360 AND MADE STR REPAIR ON STR 26L FROM BS 360 TO 390. DAMAGE ON THAT PORTION OF STR WAS FOUND TO BE OUT OF LIMITS AS PER FEDEX SRM 53-10-1 FEDEX SRM 53-10-3. 2 L 7 3 4F A3WE 1996030800111 19960308 00111 NM 1996 3 8 96FDEA00374 1 19960301 A 5311 FRAME BOEING 727 727233 138408A NM BS 970 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 266FE 21672 CREASED DENT IN FRAME AT BS 970 BETWEEN STR 26 TO 25L. REMOVED DAMAGED FRAME SECTION, INSTALLED REPAIR DOUBLER IAW FEDE X SRM 51-40-3. 2 L 7 3 4F RT A3WE 1996030800112 19960308 00112 WP 1996 3 8 96FDEA00375 1 19960228 A 5512 SKIN DOUG DC10 DC1030 3023501 WP RT HORIZ STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 320FE 47835 RT HORIZ STAB UPPER AFT SKIN PANEL HAS .5625 INCH CRACK AT K/B AFT CORNER APPROX 1 INCH FROM PANEL AFT EDGE, ADJACENT TO WORKING BULKHEAD. 2 L 7 3 4F A22WE 1996030800113 19960308 00113 NM 1996 3 8 96FDEA00376 1 19960228 A 5711 6516330 SPAR CHORD BOEING 727 72722 1384002 NM BS 870 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION (C53-132-02) ON THE WING CENTER SECTION REAR UPPER SPAR CHORD, STA 870 LBL 30 RBL 30 WL 174. *S/D* REMOVE D AND REPLACED UPPER CHORD PER FEDEX EA 7-5710-27481. 2 L 7 3 4F A3WE 1996030800114 19960308 00114 NM 1996 3 8 96FDEA00377 1 19960228 A 5521 6516815 VERT MID SPAR BOEING 727 72722 1384002 NM FS 225.707 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 VERTICAL FIN MID SPAR, STR 7 AND PANEL SUPPORT HAS WORN FASTENER HOLE AT FIN STA 225.707 LEFTSIDE. *S/D* REPAIRED PER FEDEX EA 75510-27728. 2 L 7 3 4F A3WE 1996030800115 19960308 00115 NM 1996 3 8 96FDEA00378 1 19960228 A 5531 MID SPAR BOEING 727 72722 1384002 NM VERT STAB WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 VERTICAL FIN MID SPAR, STR 7 AND PANEL SUPPORT HAS WORN FASTENER HOLE AT FIN STA 225.707 LT. REPAIRED PER FEDEX EA 7-55 10-27728. 2 L 7 3 4F A3WE 1996030800116 19960308 00116 SO 1996 3 8 COMA9610092 1 19960302 A 6120 MS252531 AUTOFEATHER SW EMB 120 EMB120RT SO CONTROL QUADRANT FAILED A COMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 263CA 120255 AUTOFEATHER SYSTEM DID NOT ARM DURING TAKEOFF. REPLACED THE AUTOFEATHER ARM MICRO SWITCH IN THE POWER LEVER QUADRANT. 2 L 7 2 4T RT A31SO 1996030800117 19960308 00117 SO 1996 3 8 COMA9610093 1 19960229 A 3233 1959500007 ACTUATOR EMB 120 EMB120RT SO LT MLG DEFECTIVE A COMA K NONE O OTHER DE DESCENT 1 SO 01 263CA 120255 LT MLG INDICATED UNSAFE. LANDING GEAR CYCLED TWICE WITH SAME RESULTS. USED EMERGENCY SYSTEM TO EXTEND LANDING GEAR AND ALL GEAR INDICATED SAFE. REPLACED THE LT MLG HYDRAULIC ACTUATOR. 2 L 7 2 4T RT A31SO 1996030800118 19960308 00118 SW 1996 3 8 COMA9620003 1 19960229 A 7722 8974763 EGT COMPENSATOR SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP RT ENGINE OUT OF ADJUST A COMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 702M AC702 44577 RT ENGINE TORQUE ROLLBACK FROM 87 PERCENT TO 82 PERCENT DURING TAKEOFF. RECALIBRATED THE EGT COMPENSATOR. 1 L 7 2 4T 4 T A8SW E4WE 1996030800119 19960308 00119 EU 1996 3 8 COMA9630048 1 19960228 A 3020 ND00751940 INTAKE ANTI-ICE ND00752200 SAAB SF340 SF340A 7850100 EU LT ENGINE MALFUNCTION A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 343CA 4227 2663 L242315 340A024 LEFT ENGINE INTAKE ANTI-ICE FAILED. REPLACED THE INTAKE LOAD MONITOR AND THERMAL CONTROLLER. 2 L 7 2 4T RT A52EU 1996030800120 19960308 00120 EA 1996 3 8 COMA9660033 1 19960229 A 2611 473052 SMOKE DETECTOR CNDAIR CL600 CL6002B19 EA CARGO COMPT FALSE WARNING A COMA F ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 941CA 7050 CARGO SMOKE WARNING ACTIVATED DURING TAXI, FIRE BOTTLES DISCHARGED. FOUND NO EVIDENCE OF SMOKE OR FIRE. CLEANED SMOKE DETECTORS AND REPLACED FIRE BOTTLES. 2 L 7 2 4F RT A21EA 1996030800121 19960308 00121 EA 1996 3 8 COMA9660034 1 19960303 A 5240 DOOR CNDAIR CL600 CL6002B19 EA OXYGEN SERVICE NOT LATCHED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 929CA 7035 OXYGEN SERVICE DOOR OPEN IN FLIGHT. CLOSED AND SECURED DOOR. 2 L 7 2 4F RT A21EA 1996030800122 19960308 00122 WP 1996 3 8 MWEA96049 1 19960302 A 2560 113313 EVAC SLIDE DOUG DC9 DC932 3022066 WP GALLEY SERV DOOR FELL OFF A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 MAINT REPORTS, WHEN GALLEY SERVICE DOOR WAS OPENED THE EVACUATION SLIDE FELL OFF. REINSTALLED GALLEY DOOR EVAC SLIDE. 2 L 7 2 4F A6WE 1996030800123 19960308 00123 WP 1996 3 8 MWEA96050 1 19960302 A 3397 WIRE DOUG DC9 DC932 3022066 WP CABIN CHAFED A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 401ME 47133 CREW REPORTS, ABOVE ROW 5 C AND D OVERHEAD BIN THERE WAS A FLASH AND SUBSEQUENT SMOKE. REPLACED SIDEWALL LIGHT DISCONNE CT DUE TO CHAFED WIRES AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1996030800124 19960308 00124 1996 3 8 QXEA9600092 4 19960303 A 2210 7015327901 PANEL HONEYWELL DORNER DO32 DO328100 2996000 NM COCKPIT SMOKING A QXEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 09 332PH 3380 3010 EN ROUTE, SMOKE WITH ASSOCIATED SMELL COMING FROM NOSE UP/ NOSE DOWN THUMB WHEEL ON FGC. AIRCRAFT DIVERTED TO EUG AND L ANDED WITHOUT FURTHER PROBLEMS. FGC AND NR 1 IAC WERE REPLACED AND AUTOPILOT OPS CHECKED GOOD. 2 H 7 2 4T RT A45NM 1996030800125 19960308 00125 EU 1996 3 8 QXEA9600093 1 19960302 A 3350 1315 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 450US 11101 SEVERAL OVERHEAD EMERGENCY LIGHTS INOP. BULBS WERE REPLACED AND LIGHTS OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996030800126 19960308 00126 NE 1996 3 8 RRXA9600009 2 19960229 A 7200 ENGINE DOUG DC8 DC871 302199A WP GE CFM56 CFM562C1 13802 NE NR 1 LOST POWER A RRXA E ENGINE SHUTDOWN X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 WP 15 8177U 45983 692197 KPDX/KSJC - FLT 502 - NR 1 ENGINE LOST POWER DURING CLIMB. OIL PRESSURE WENT TO ZERO WHILE ENGINE STILL ROTATING AT 20 PERCENT N2. SHUT-DOWN PROCEDURES ACCOMPLISHED. MAINTENANCE INSPECTED THE NR 1 ENGINE INLET AND EXHAUST, NO DEFECTS NOT ED. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE FUEL FILTERS. CHECKED THE OIL CHIP DETECTORS, NO CONTAMINATION FO UND. NR 1 ENGINE OPERATED NORMALLY ON GROUND RUN. (X) 2 L 7 4 4F 4 F 4A25 E2GL 1996030800130 19960308 00130 EU 1996 3 8 96ZZZX909 1 19960114 A 3350 300150 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 370AM 771 1034 340B370 TYR - FLT 3773 - DURING WALK-AROUND, FOUND ALL EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED ALL FOUR POWER SUPPLI ES. OPERATION CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. PART TOTAL CYCLES, 774. REFERENCE OPERATOR CONTROL N R SIMA960141, NR 96ZZZX910, AND NR 96ZZZX911. 2 L 7 2 4T RT A52EU 1996030800131 19960308 00131 EU 1996 3 8 96ZZZX910 1 19960114 A 3350 300150 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 370AM 771 1079 340B370 TYR - FLT 3773 - DURING WALK-AROUND, FOUND ALL EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED ALL FOUR POWER SUPPLI ES. OPERATION CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. PART TOTAL CYCLES, 774. REFERENCE OPERATOR CONTROL N R SIMA960141, NR 96ZZZX909, AND NR 96ZZZX911. 2 L 7 2 4T RT A52EU 1996030800132 19960308 00132 EU 1996 3 8 96ZZZX911 1 19960114 A 3350 300150 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 370AM 771 1083 340B370 TYR - FLT 3773 - DURING WALK-AROUND, FOUND ALL EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED ALL FOUR POWER SUPPLI ES. OPERATION CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. PART TOTAL CYCLES, 774. REFERENCE OPERATOR CONTROL N R SIMA960141, NR 96ZZZX909, AND NR 96ZZZX910. 2 L 7 2 4T RT A52EU 1996030800133 19960308 00133 SO 1996 3 8 96ZZZX912 1 19960103 A 2913 PV302229 HYDRUALIC PUMP EMB 120 EMB120RT SO RT ENGINE FAILED A MASA O OTHER J WARNING INDICATION LD LANDING 1 SW 01 270YV 120270 AIRCRAFT LOST GREEN SYSTEM PRESSURE AND QUANTITY ON APPROACH TO JAC. EMERGENCY GEAR EXTENSION AND NO FLAPS LANDING WAS ACCOMPLISHED WITH NO INCIDENT. 2 L 7 2 4T RT A31SO 1996030800135 19960308 00135 SO 1996 3 8 96ZZZX914 1 19960130 A 3231 12012347001 LATCH EMB 120 EMB120ER 3260203 SO MLG DOOR UNLATCHED A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 01 298YV 120298 AIRCRAFT DEPARTED FROM GRAND JUNCTION, CO. WHEN AIRCRAFT GEAR WAS SELECTED UP AND PILOTS GOT NO NOSE GEAR DOOR INDICATI ON, PILOT RETURNED AIRCRAFT TO THE GATE WHERE MAINTENANCE DETERMINED THE NOSE LANDING GEAR DOORS WERE NOT LATCHED. MAIN TENANCE THEN RE-LATCHED THE DOORS AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 1996030800137 19960308 00137 WP 1996 3 8 96ZZZX916 1 19960130 A 2130 5924030523 VALVE DOUG DC9 DC932 3022066 WP CABIN FAILED A VJ6A A G UNSCHED LANDING O2 MASK DEPLOYED O OTHER CL CLIMB 1 SO 11 921VV 47284 ATL/ATL - FLT 509 - AIR RETURN, CABIN WOULD NOT PRESSURIZE IN MANUAL OR AUTO, ALL MASKS DEPLOYED. FOUND LT DIVERTER VAL VE ASSY BROKEN. AFT INBOARD HEAT EXCHANGER FRAME SEAL REPLACED WITH HINGE REPLACEMENT. RESTOWED MASKS. 2 L 7 2 4F A6WE 1996030800138 19960308 00138 EU 1996 3 8 96ZZZX917 1 19960101 A 2460 WIRE BAG JETSTM JETSTM3101 1500215 EU TERM BLOCK T2AJ CHAFED A SABA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 05 693JX 693 CLT/ISO - FLT 5234 - ON 1-1-96, FLIGHT HAD JUST TAKEN OFF WHEN THE CIRCUIT BREAKER FOR THE LEFT FUEL AND OIL PRESSURE GA UGE TRIPPED. THE CAPTAIN TRIED TO RESET THE BREAKER, BUT IT IMMEDIATELY TRIPPED AGAIN. THE CAPTAIN RETURNED TO THE FIE LD WHERE HE MADE AN UNEVENTFUL LANDING. MAINTENANCE PERSONNEL WERE DISPATCHED TO TROUBLESHOOT THE PROBLEM. A CHAFED WI RE AT TERMINAL BLOCK T2AJ WAS FOUND TO BE CAUSING THE PROBLEM. THE WIRE WAS REPAIRED AND THE AIRCRAFT RETURNED TO SERVI CE. 2 L 7 2 4T RT A21EU 1996030800142 19960308 00142 EU 1996 3 8 96ZZZX921 1 19960114 A 3297 200877943 WIRE HARNESS ELDEC BAC 146 146200A 1500266 EU LT MLG WORN A TIXA O OTHER N FALSE WARNING CL CLIMB 1 WP 19 138TR E2138 EUG - FLT 121 - AIRCRAFT DEPARTED OUT OF EUG AT 0645 LOCAL TIME. DURING LANDING GEAR RETRACTION, LT MAIN INTRANSIT LIGH T REMAINED ON. THE LANDING GEAR WAS CYCLED AGAIN WITH NO CHANGE IN INDICATION. THE AIRCRAFT RETURNED TO EUG AIRPORT WI THOUT FURTHER INCIDENT, LANDING AT 0704 LOCAL TIME. AFTER INSPECTION OF LANDING GEAR FOR OBVIOUS DEFECTS, THE DECISION TO FERRY AIRCRAFT TO LAS MAINTENANCE BASE WAS MADE. THE LMLG UPLOCK SWITCH WIRE HARNESS WAS FOUND LOOSE AT ONE END AND WAS REPLACED. 2 H 7 4 4F A49EU 1996030800143 19960308 00143 EU 1996 3 8 96ZZZX922 1 19960115 A 2120 AIR DIST BAG JETSTM JETSTM3201 1500217 EU CABIN ODOR A S4XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 27 846JX 846 CLIMBING OUT OF 2,000 FEET, SMOKE APPEARED THROUGHOUT CABIN ACCOMPANIED BY A 'BURNING ELECTRICAL' SMELL. AN EMERGENCY W AS DECLARED AS THE CAPTAIN SHUT OFF THE RECIRCULATION FAN AND BLEW OUT THE CABIN. THE EMERGENCY CHECK LIST WAS CONDUCTE D AND THE RECIRCULATION FAN CIRCUIT BREAKER PULLED. AIRCRAFT RETURNED TO OAKLAND. MAINTENANCE ACTION - PERFORMED GROU ND RUN ON AIRCRAFT TESTING ALL SYSTEMS. NO DEFECTS OR ABNORMAL CONDITIONS NOTED. FOUND LOOSE MAIN TERMINAL ON ESSENTIA L DC BUSBAR AND RE-TORQUED. ALL PARAMETERS NORMAL AT FULL POWER AS WELL. 2 L 7 2 4T RT A56EU 1996030800153 19960308 00153 WP 1996 3 8 AALA960020 1 19960104 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 313 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 579AA 53156 TUL - SKIN DAMAGED, INSTALLED TEMPORARY DOUBLER AT FS 313 BETWEEN LONGERONS 21L AND 22L. INSTALLED PERMANENT CLASS 'I' REPAIR. TST, 13,177.38 HOURS. CYCLES, 7,275. (X) 2 L 7 2 4F A6WE 1996030800154 19960308 00154 WP 1996 3 8 AALA960070 1 19960116 A 5230 EDK18518 ANGLE DOUG DC9 DC982 3022082 WP BS 1155 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 402A 43313 TUL - CORROSION STA 1155, LOWER FORWARD CORNER OF CARGO DOOR ANGLE CASTING, SAME AREA FASTENER RUSTY. REMOVED AND REPLA CED ANGLE. TST, 30,058.4 HOURS. CYCLES, 17,497. (X) 2 L 7 2 4F A6WE 1996030800155 19960308 00155 WP 1996 3 8 AALA960071 1 19960116 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 1155 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 402A 43313 TUL - CORROSION STA 1155, LOWER FORWARD CORNER OF CARGO DOOR JAMB ANGLE. REMOVED AND REPLACED JAMB ANGLE. TST, 30,058. 4 HOURS. CYCLES, 17,497. (X) 2 L 7 2 4F A6WE 1996030800156 19960308 00156 NM 1996 3 8 AALA960078 1 19960112 A 5321 146N5300 DECK PLATE BOEING 757 757223 1384957 NM BS 1681 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 640A 24598 AFW - DECK PLATE HAS CORROSION REMOVED ON UPPER SURFACE AT VARIOUS LOCATIONS, PER MRB 757-685. TST, 15,514.52 HOURS. C YCLES, 5,884. (X) 2 L 7 2 4F RT A2NM 1996030800157 19960308 00157 NM 1996 3 8 AALA960079 1 19960112 A 5315 146N5136 FLOOR BEAM BOEING 757 757223 1384957 NM BS 1640 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 640A 24598 AFW - CORROSION BLENDED ON TOP SURFACE OF FLOOR BEAM AT STA 1640, LBL 57, LBL 53, BL ZERO, AND RBL 57. BLENDS ARE BEYON D SRM LIMITS, PER MRB 757-686. TST, 15,514.52. CYCLES, 5,884. (X) 2 L 7 2 4F RT A2NM 1996030800158 19960308 00158 NM 1996 3 8 AALA960080 1 19960112 A 5315 141N5112 FLOOR BEAM BOEING 757 757223 1384957 NM BS 365 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 640A 24598 AFW - FLOOR BEAM AT STA 365 HAS CORROSION BLENDED BEYOND SRM LIMITS, PER MRB 757-687. TST, 15,514.52 HOURS. CYCLES, 5, 884. (X) 2 L 7 2 4F RT A2NM 1996030800159 19960308 00159 NM 1996 3 8 AALA960081 1 19960112 A 5210 146N62015 DOOR PAN BOEING 757 757223 1384957 NM L4 DOOR GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 640A 24598 AFW - L-4 DOOR HANDLE PAN HAS A GOUGE BEYOND SRM LIMITS, PER MRB 757-692. TST, 15,514.52 HOURS. CYCLES, 5,884. (X) 2 L 7 2 4F RT A2NM 1996030800160 19960308 00160 NM 1996 3 8 AALA960082 1 19960112 A 5315 146N5092 FLOOR BEAM BOEING 757 757223 1384957 NM BS 1701 MISDRILLED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 640A 24598 AFW - FLOOR BEAM AT STA 1701, RBL 50, HAD TWO HOLES MISDRILLED, PER MRB 757-693. TST, 15,514.52 HOURS. CYCLES, 5,884. ( X) 2 L 7 2 4F RT A2NM 1996030800161 19960308 00161 NM 1996 3 8 AALA960083 1 19960112 A 5220 146N63T0 DOOR FRAME BOEING 757 757223 1384957 NM OVERWING GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 640A 24598 AFW - AFT LT OVERWING EXIT DOOR FRAME LOWER SIDE HAD DEEP GOUGE. GOUGE IS BLENDED BEYOND SRM LIMITS, PER MRB 757-200. T ST, 15,512.52. CYCLES, 5,884. (X) 2 L 7 2 4F RT A2NM 1996030800162 19960308 00162 NM 1996 3 8 AALA960084 1 19960112 A 5210 146N62016 DOOR PAN BOEING 757 757223 1384957 NM R4 DOOR GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 640A 24598 AFW - R-4 DOOR HANDLE PAN HAS GOUGE BEYOND SRM LIMITS, PER MRB 757-200. TST, 15,514.52 HOURS. CYCLES, 5,884. (X) 2 L 7 2 4F RT A2NM 1996030800163 19960308 00163 WP 1996 3 8 AALA960117 1 19960121 A 3350 A3030398101 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7550 53032 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 3E AND 6E FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR BY PASSENGER SEAT ROW 3E. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1996030800164 19960308 00164 NM 1996 3 8 AALA960161 1 19960129 A 4920 NHL6050507 APU DOUG MD11 MD11 3023602 NM APU COMPT LEAKING OIL A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 1756 P107 48491 JFK - FLT 0735 - AFTER TAKEOFF JFK DURING CLIMB-OUT, ACRID BURNING ODOR NOTED THROUGHOUT AIRCRAFT WITH NO OTHER ABNORMAL INDICATIONS. ACCOMPLISHED CHK LIST AND ACFT RETURNED TO JFK LANDING WITHOUT INCIDENT. ACCOMPLISHED BORESCOPE OF NR 1 ENG COMPR, NO DEFECTS FOUND. CHECKED ALL ENG BLEED DUCTS FOR PRESENCE OF OIL WITH NO DEFECTS FOUND. REPLACED ALL COALE SCER BAGS AND ACCOMPLISHED GROUND ENG RUN AND PACK BURN-OUT PROCEDURE WITH NO DEFECTS FND. SYSTEM GROUND CHECKED, NORM AL OPERATION. ACCOMPLISHED CHK FLT, PROBLEM REPEATED. REPLACED APU DUE TO OIL DISCOVERED IN BLEED DUCTS. ACCOMPLISHED PACK BURN-OUT PROCEDURE AND REPLACED ALL COALESCER BAGS. SYSTEM GROUND CHK NORMAL OPER. (X) 2 L 7 3 4F RT A22WE 1996030800165 19960308 00165 NM 1996 3 8 AALA960164 1 19960130 A 5315 146N5089 FLOOR BEAM BOEING 757 757223 1384957 NM BS 1640 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 653A 24611 AFW - FLOOR BEAM AT STA 1640, RBL 55 AND RBL 58 HAS CORROSION BLENDED BEYOND SRM LIMITS, PER MRB 757-718. TST, 13,759 H OURS. CYCLES, 4,865. (X) 2 L 7 2 4F RT A2NM 1996030800166 19960308 00166 NM 1996 3 8 AWXA96007 1 19960105 A 2121 6454051 FAN BOEING 737 7373B7 1384580 NM CABIN FAILED A AWXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 28 328AW 75179 23377 CMH/MCO - FLT 3105 - PILOT REPORTED NOISE AND SMOKE IN CABIN. FOUND A BAD RECIRCULATION FAN. REMOVED AND REPLACED RECI RCULATION FAN. OPS CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1996030800167 19960308 00167 NM 1996 3 8 C1HA960003 1 19960102 A 3320 9781 BALLAST AVTECH BOEING 727 727223 1384074 NM CABIN OVERHEATED A C1HA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 23 705CA 19479 DURING THIS FLIGHT, FLIGHT ATTENDANT REPORTED SMELL OF ELECTRICAL SMOKE TYPE. IT WAS INVESTIGATED AND SMELL WAS COMING FROM MID-CABIN CEILING FLUORESCENT LIGHT. PULLED CIRCUIT BREAKERS, SMOKE SMELL STOPPED. UNABLE TO ISOLATE A PARTICULAR AREA. C/A FOUND DEFECTIVE FLUORESCENT BALLAST ABOVE SEAT 12C. REMOVED AND REPLACED BALLAST AND OPS CHECK OK. (X) 2 L 7 3 4F A3WE 1996030800168 19960308 00168 NM 1996 3 8 C1HA960006 1 19960119 A 3222 1AN6227 SEAL BOEING 727 727223 1384074 NM NLG STRUT DAMAGED A C1HA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 23 705CA 19479 ON GEAR RETRACTION, DOOR RED LIGHT REMAINED ON FORWARD PANEL AND NOSE GEAR DOOR LIGHT ON F.E. PANEL. RECYCLING THE GEAR HAD NO EFFECT. LANDED AT PVR FOR INVESTIGATING. REPLACED METERING VALVE GLAND NUT SEALS, SERVICED STRUT FLUID AND CHA RGED WITH NITROGEN TO CORRECT X DIMENSION PER MM 32-21-1. CHECKED N.W.W. AND N STRUT DOOR MECHANISMS FOR CORRECT DIMENS ION PER MM 32-22-1. OPERATED NLG AND DOORS ON GEAR SWING. NO DEFECTS NOTED AND INDICATOR CHECKED GOOD. (X) 2 L 7 3 4F A3WE 1996030800169 19960308 00169 EU 1996 3 8 C2XA96IA041 1 19960130 A 5720 S5701208600800 BEAM AEROSP ATR72 ATR72212 EU LT WING INBD CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 69901 379 IAH - DURING C-CHECK INSPECTION, FOUND LT WING RIB 13 FORWARD INBOARD FLAP HINGE BEAM CHAFED FROM PANEL 552AB. MAINTENA NCE REMOVED AND REPLACED THE BEAM ASSEMBLY, AIRCRAFT APPROVED FOR RETURN TO SERVICE. AIRCRAFT TT, 4,819.7 HOURS. CYCLE S, 5,199. (X) 2 H 7 2 4T RT A53EU 1996030800170 19960308 00170 NM 1996 3 8 CAL960004 1 19960105 A 3231 1U1085 SEQUENCE VALVE BOEING 727 727224 1384076 NM RT MLG LEAKING A CALA O OTHER K FLUID LOSS CL CLIMB 1 SW 09 69736 32291 16149 20665 EWR - FLT 0358 - THE RT MLG DOOR WOULD OPEN WHEN GEAR HANDLE WAS PLACED FROM UP TO OFF. MAINTENANCE FOUND THE RT MLG LO CK OPERATED SEQUENCE VALVE LEAKING. THE VALVE WAS REMOVED AND REPLACED IAW MM 32-32-41, PAGES 401-403. (X) 2 L 7 3 4F A3WE 1996030800171 19960308 00171 NE 1996 3 8 CAL960071 2 19960129 A 7230 K157G02 HPC BLADE DOUG DC10 DC1030 3023501 WP GE CF6 CF650* 30018 NE NR 2 ENG DAMAGE A CALA A J UNSCHED LANDING DUMP FUEL O OTHER TO TAKEOFF 1 SW 09 41068 56397 247 47867 455127 FLT NR 56 - EWR - THE NR 2 ENGINE FAILED ON TAKEOFF FROM EWR. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO EWR WHER E IT LANDED WITHOUT INCIDENT. THE NR 2 ENGINE WAS REMOVED AND REPLACED. INVESTIGATION REVEALED THAT THE PRIMARY CAUSE OF ENGINE FAILURE WAS DUE TO IMPACT DAMAGE TO A FIRST STAGE HPC BLADE CAUSED BY FOD. (M) 2 L 7 3 4F 4 F A22WE E23EA 1996030800172 19960308 00172 EU 1996 3 8 DKAA96001 1 19960112 A 3260 A238021015 DOWNLOCK SWITCH AMD FALC20 FALCOND 2720304 EU MLG FAILED A DKAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 23 226R 226 MAIN LANDING GEAR UNSAFE LIGHT STAYED ON AFTER GEAR EXTENSION. CHECKED AND ADJUSTED MLG DOWNLOCK SWITCHES. OPERATIONAL CHECKED GOOD DURING RETRACTION AND EXTENSION CHECK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F A7EU 1996030800173 19960308 00173 EU 1996 3 8 DKAA96002 1 19960112 A 3230 A123802 SQUAT SWITCH MESSIER AMD FALC20 FALCON20C5 2730107 EU LT MLG FAILED A DKAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 980R 823 98 COULD NOT RAISE GEAR HANDLE AFTER TAKEOFF, NOSE WHEEL WAS CENTERED. REPLACED 17G1 WITH SERVICEABLE UNIT IAW AMD MM 32. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A7EU 1996030800174 19960308 00174 EU 1996 3 8 RAIA960108 1 19960103 A 2761 TY176001C ACTUATOR JETAIR JETSTM JETSTM4101 1500501 EU RT SPOILER FAILED A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 559HK 220 41075 JFK - FLT 7733 - TAKEOFF CONFIGURATION LIGHT ILLUMINATED. MAINTENANCE REPLACED RIGHT SPOILER ACTUATOR. OPERATIONAL CHE CKED GOOD. AIRCRAFT TT, 219.7 HOURS. (X) 2 L 7 2 4T RT A41NM 1996030800175 19960308 00175 EU 1996 3 8 RAIA960137 1 19960121 A 5270 SP4594 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU CABIN DOOR DIRTY A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 561HK 69 41077 JFK - FLT 7759 - MAIN BAGGAGE DOOR LIGHT CAME ON DURING TAKEOFF ROLL. MAINTENANCE CLEANED BAGGAGE DOOR LIGHT MICROSWITC H, OPERATION CHECK GOOD. AIRCRAFT TT, 69.4 HOURS. (X) 2 L 7 2 4T RT A41NM 1996030800176 19960308 00176 EU 1996 3 8 RAIA960148 1 19960127 A 3241 140149 TRANSDUCER JETAIR JETSTM JETSTM4101 1500501 EU RT OTBD WHEEL FAULTY A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 556HK 759 41073 SUX - FLT 7213 - ANTI-SKID LIGHT ILLUMINATED ON TAKEOFF ROLL. MAINTENANCE REPLACED RIGHT OUTBOARD WHEEL TRANSDUCER. (X ) 2 L 7 2 4T RT A41NM 1996030800177 19960308 00177 NE 1996 3 8 RAIA960150 3 19960127 A 6111 7895881 SEAL AEROSP ATR42 ATR42300 8680920 EU HAMSTD 14SF 14SF5 NE LT PROPELLER LEAKING A RAIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 426TE 228 900558 STL - FLT 7234 - ELECTRIC SMOKE WARNING DURING TAXI EVIDENCE OF SMOKE IN CABIN AND COCKPIT. MAINTENANCE DETERMINED OIL LEAK FROM PROPELLER CAUSED SMOKE, MAINTENANCE REMOVED AND REPLACED LEFT PROP BLADE SEAL. GROUND OPS CHECK GOOD. AIRCRA FT TT, 11,204.9 HOURS. (X) 2 H 7 2 4T RT A53EU 6 C P7NE 1996030800178 19960308 00178 EU 1996 3 8 RAIA960151 1 19960126 A 5270 SP4594 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGGAGE DOOR DIRTY A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 557HK 597 41074 DCA - FLT 7746 - BAGGAGE DOOR LIGHT ILLUMINATED DURING TAKEOFF. MAINTENANCE CLEANED MICROSWITCH, OPERATION CHECK GOOD. (X) 2 L 7 2 4T RT A41NM 1996030800179 19960308 00179 EU 1996 3 8 RAIA960152 1 19960129 A 2913 PV304426 HYDRAULIC PUMP BAG JETSTM JETSTM3201 1500217 EU RT ENGINE LEAKING A RAIA O OTHER K FLUID LOSS AP APPROACH 1 CE 03 872JX 5534 872 SFO - FLT 4738 - WHILE SELECTING GEAR DOWN, EXPERIENCED TOTAL HYDRAULIC FAILURE. AIRCRAFT LANDED WITHOUT INCIDENT. MAI NTENANCE FOUND RT HYDRAULIC FAILED. MAINTENANCE REPLACED RT HYDRAULIC PUMP. OPERATIONAL CHECK OF HYDRAULIC SYSTEM GOOD . (X) 2 L 7 2 4T RT A56EU 1996030800180 19960308 00180 EU 1996 3 8 RAIA960156 1 19960130 A 2760 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU SPOILER ACT CONTAMINATED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 556HK 785 41073 STL - FLT 7460 - TOCW ILLUMINATED DURING TAKEOFF. MAINTENANCE CLEANED GYLCOL FROM CANNON PLUGS ON BOTH SPOILER ACTUATOR S, PN TY176301C. OPERATION CHECK GOOD. (X) 2 L 7 2 4T RT A41NM 1996030800181 19960308 00181 NE 1996 3 8 RRXA960003 2 19960130 A 7310 FILTER DOUG DC8 DC871 302199A WP GE CFM56 CFM562C1 13802 NE NR 1 ENGINE DIRTY A RRXA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 WP 15 811AL 46099 693124 KOAK/KDAY - FLT 002 - 380 MILES OUT OF KOAK, NR 1 ENGINE FLAMED OUT. RESTART WAS NOT SUCCESSFUL. NR 1 ENGINE RESTART A CCOMPLISHED AT 10,000 FEET. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE FUEL FILTER, INSPECTED NR 1 ENGINE IGNITION SY STEM, AND PERFORMED AN ENGINE GROUND RUN. NO DEFECTS NOTED. (X) 2 L 7 4 4F 4 F 4A25 E2GL 1996030800182 19960308 00182 EU 1996 3 8 SIMA960081 1 19960107 A 3230 C2458900 UPLOCK BOX AEROSP ATR42 ATR42300 8680920 EU RT MLG FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 12MQ M024 012 CVG - FLT 4020 - RIGHT MAIN GEAR WILL NOT LOCK UP TO THE RETRACT POSITION DURING CLIMB. CONTINUED FLIGHT WITHOUT FURTHE R MECHANICAL INCIDENT - DIVERTED TO RFD PER WEATHER. RFD MAINTENANCE REPLACED RIGHT MLG UPLOCK BOX. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1996030800183 19960308 00183 EU 1996 3 8 SIMA960141 1 19960114 A 3350 300150 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 370AM 771 1070 340B370 TYR - FLT 3773 - DURING WALK-AROUND, FOUND ALL EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED ALL FOUR POWER SUPPLI ES. OPERATION CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. PART TOTAL CYCLES, 774. REFERENCE OPERATOR CONTROL N R 96ZZZX909, NR 96ZZZX910, AND NR 96ZZZX911. (X) 2 L 7 2 4T RT A52EU 1996030800185 19960308 00185 NM 1996 3 8 USAASB96008 1 19960112 A 7830 3810056101 CONTROL VALVE BOEING 737 7374B7 1384702 NM LT ENGINE FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 446US 24873 TPA - FLT 202 - NR 2 ENGINE REVERSER LIGHT ON OVERHEAD PANEL ILLUMINATED DURING FLIGHT, THROTTLE OPERATED NORMALLY AND R EVERSER OPERATED NORMALLY ON GROUND. MAINTENANCE REPLACED THRUST REVERSER CONTROL VALVE. NO LEAKS NOTED. OK FOR SERVI CE. (X) 2 L 7 2 4F RT A16WE 1996030800186 19960308 00186 NM 1996 3 8 W8PA960003 1 19960115 A 3350 20131A BATTERY PACK BOEING 737 7373Y0 1384671 NM CABIN DISCHARGED A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 962WP 6760 23748 ON SERVICE CHECK, FOUND RIGHT AND LEFT OUTSIDE EMERGENCY EXIT LIGHTS INOPERATIVE. FOUND BATTERY PACK WEAK. REPLACED BA TTERY PACK. OPS CHECK OK. (X) 2 L 7 2 4F RT A16WE 1996030800187 19960308 00187 NE 1996 3 8 96ZZZX925 2 19960119 A 7200 ENGINE LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B02 54555 NE NR 1 FAILED A RIAA A E J UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SO 19 764BE 24760 1423 193P1113 10598 SFO/HNL - FLT 1113 - DURING CRUISE, NR 1 ENGINE WAS SHUT DOWN AT 1726, AIRCRAFT DUMPED FUEL, AND RETURNED TO SFO DUE TO HIGH VIB'S, BOTH CHANNELS. UPON LANDING AT SFO, FOUND METAL ON ALL 3 CHIP DETECTORS. AIRCRAFT FERRIED TO MIA ON TWO EN GINES ON 1-20-96 FOR NR 1 ENGINE CHANGE. 2 L 7 3 4F 4 F A23WE E12EU 1996030800188 19960308 00188 WP 1996 3 8 96ZZZX926 1 19960122 A 2410 707388H IDG LKHEED 1011 10113851 5265010 WP NR 1 ENGINE FAILED A RIAA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 19 764BE 193P1113 FT. MYERS/LAS - FLT 1682 - DURING CRUISE 65 MINUTES OUT, NR 1 ENGINE LOST OIL QUANTITY, ENGINE WAS SHUT DOWN. UPON ARRI VAL AT LAS, MAINTENANCE DETERMINED OIL LOSS FROM IDG. IDG REPLACED. 2 L 7 3 4F A23WE 1996030800189 19960308 00189 NM 1996 3 8 96ZZZX928 1 19960215 A 2612 106087713 FIRE LOOP BOEING 727 727225 1384077 NM NR 2 ENGINE FAILED A MYWA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SO 19 804MA 22435 HUF - FIRE WARNING BELL SOUNDS ON TAKEOFF. NO LIGHTS. CANNOT SILENCE EXCEPT BY PULLING NR 2 ENGINE DETECTOR CIRCUIT BR EAKER. FOUND LOWER LOOP ON NR 2 ENGINE TO BE FAILING. REMOVED AND REPLACED LOOP. SYSTEM CHECKS GOOD IAW 26-10-00. NO TE: THE INCIDENT HAPPENED ON A FLIGHT OPERATED BY U. S. MARSHALL SERVICES AND RESULTED IN A FLIGHT RETURN. 2 L 7 3 4F A3WE 1996030800191 19960308 00191 NE 1996 3 8 96ZZZX930 2 19960217 A 7314 378200 FUEL PUMP BOEING 727 727225 1384077 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE FAILED A MYWA O OTHER X ENGINE FLAMEOUT DE DESCENT 1 SO 19 887MA 21857 0781M BOS - FLT GL501 - WHILE DESCENDING THROUGH 16,000 FEET WITH NR 1 ENGINE AT IDLE, GB ILLUMINATED. CHECKED ALL PARAMETERS . ENGINE FLAMED OUT. SHUT DOWN IAW EMERGENCY PROCEDURES. ATTEMPTED IN-FLIGHT RESTART IAW ABNORMAL PROCEDURES. NO FUE L FLOW. COMPLETE ENGINE SHUTDOWN EMERGENCY PROCEDURES. REPLACED NR 1 ENGINE FUEL CONTROL AND FUEL PUMP. NOTE: THE OU TBOUND FLIGHT, GL612, WAS CANCELLED (OPERATIONAL DECISION) AND RESCHEDULED TO 0730 LOCAL TIME ON 2-19-96. 2 L 7 3 4F 4 F A3WE E2EA 1996030800192 19960308 00192 NM 1996 3 8 AALA960055 1 19960115 A 3350 24003 TEST SWITCH HONEYWELL BOEING 767 767223 1385123 NM AFT F/A PANEL DEFECTIVE A AALA K NONE O OTHER CR CRUISE 1 SW 07 327AA 22327 ORD - FLT 0037 - EN ROUTE ZRH/ORD DURING CRUISE, PASSENGER EMERGENCY EXIT LIGHTING ILLUMINATED AND COULD NOT BE EXTINGUI SHED. NO OTHER ABNORMAL INDICATIONS AND AIRCRAFT PROCEEDED TO ORD, LANDING WITHOUT INCIDENT. REPLACED EMERGENCY EXIT L IGHTING TEST SWITCH 528 AT AFT F/A PANEL. REPLACED BATTERY PACKS. SYSTEM GROUND CHECKED, NORMAL OPERATIONAL. (X) 2 L 7 2 4F RT A1NM 1996030800193 19960308 00193 NM 1996 3 8 AALA960112 1 19960117 A 3350 A3030398101 CONNECTOR BOEING 727 727227 1384078 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 723AA 20731 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FIRST CLASS CABIN FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1996030800194 19960308 00194 NM 1996 3 8 AALA960113 1 19960118 A 3350 A303098101 CONNECTOR BOEING 727 727223 1384074 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 890AA 22006 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 10D AND 16D FOUND INOPERATIVE. RESECUR ED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR BY PASSENGER SEAT ROW 10D. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1996030800195 19960308 00195 NM 1996 3 8 AALA960127 1 19960124 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 369AA 25196 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT PASSENGER SEATS 8B TO 12B FOUND INOPERATIVE. RESECURED LOOSE EME RGENCY EXIT LIGHT SIDEWALL CONNECTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1996030800196 19960308 00196 NM 1996 3 8 AALA960138 1 19960126 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 328AA 22328 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 37H FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY E XIT LIGHT HARNESS CONNECTOR AT PASSENGER SEAT 37H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1996030800197 19960308 00197 WP 1996 3 8 AALA960140 1 19960126 A 3350 STRIP DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 242AA 49255 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY FOUND INOPERATIVE. REPLACED EMERGENCY LIGHT STRI P BY FORWARD GALLEY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1996030800198 19960308 00198 NM 1996 3 8 AALA960142 1 19960128 A 3350 STRIP BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 894AA 22010 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT AFT SECTION OF MAIN CABIN FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP AT AFT SECTION OF MAIN CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1996030800199 19960308 00199 NM 1996 3 8 AALA960144 1 19960128 A 3350 1722331 CONNECTOR BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 359AA 24040 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 22AB FOUND INOPERATIVE. REPLACED EMERGENCY EXIT LI GHT CONNECTOR AT PASSENGER SEAT 22AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1996030800200 19960308 00200 NM 1996 3 8 AALA960159 1 19960130 A 3350 LP8095001 LIGHT BOEING 767 767223 1385123 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 316AA 22318 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 26H FOUND INOPERATIVE. REPLACED EMERGENCY EXIT LAM P ASSEMBLY AT PASSENGER SEAT 26H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1996030800201 19960308 00201 WP 1996 3 8 AALA960172 1 19960201 A 3350 STRIP DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 70504 49798 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT AFT SECTION OF MAIN CABIN FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP AT AFT SECTION OF MAIN CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1996030800202 19960308 00202 WP 1996 3 8 AALA960176 1 19960204 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 454AA 49559 LGA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT AFT SECTION OF MAIN CABIN FOUND INOPERATIVE. REPAIRED BROKEN/SH ORTED EMERGENCY FLOOR LIGHT WIRES AT AFT SECTION OF MAIN CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1996030800203 19960308 00203 WP 1996 3 8 AALA960178 1 19960202 A 3230 RETRACT MECH DOUG DC9 DC982 3022082 WP LT MLG LACK OF LUBE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 7533A 49987 ORD - FLT 0037 - AFTER TAKEOFF ORD WHEN LANDING GEAR RETRACTED, LT MLG WOULD NOT RETRACT. RECYCLED LANDING GEAR WITH SA ME RESULTS. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. LUBRICATED ALL LANDING GEARS AND SERVICED WITH OIL A ND NITROGEN. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. ACCOMPLISHED FUNCTIONAL CHECK FLIGHT WI TH NO DEFECTS FOUND. SYSTEM OPERATIONAL CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1996030800204 19960308 00204 EU 1996 3 8 AALA960209 1 19960206 A 3350 LAMP FOKKER F28 F28MK0100 4990807 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1426A 11411 ORD - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT EXIT LIGHT AT FORWARD SERVICE DOOR FOUND BROKEN AND INOPERATIVE. RE PLACED EMERGENCY FLOOR LIGHT EXIT LIGHT AT FORWARD SERVICE DOOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT 1996030800205 19960308 00205 NM 1996 3 8 AALA960212 1 19960206 A 3350 PINS BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 383AN 26995 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT PASSENGER SEATS 10B AND 11B FOUND INOPERATIVE. RESEATED LOOSE EM ERGENCY EXIT LIGHT PINS AT PASSENGER SEATS 10B AND 11B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1996030800206 19960308 00206 NM 1996 3 8 AALA960244 1 19960210 A 3397 WIRE BOEING 727 727223 1384074 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 878AA 21390 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT FORWARD SECTION OF FIRST CLASS CABIN FOUND INOPERATIVE. REPAIRE D BROKEN WIRE TO EMERGENCY FLOOR LIGHT STRIP AT FORWARD SECTION OF FIRST CLASS CABIN. SYSTEM GROUND CHECKED, NORMAL OPE RATION. (X) 2 L 7 3 4F A3WE 1996030800207 19960308 00207 WP 1996 3 8 AALA960249 1 19960212 A 3350 A3030398101 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 505AA 49799 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AFT OF PASSENGER SEAT ROW 21 FOUND INOPERATIVE. RESECURED LOOSE EM ERGENCY FLOOR LIGHT CONNECTOR BY PASSENGER SEAT ROW 21. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1996030800208 19960308 00208 NE 1996 3 8 GRAA9610 2 19960217 A 7261 7578678 OIL FILTER DOUG DC9 DC915 3022036 WP PWA JT8 JT8D7B 52053 NE NR 2 ENGINE DIRTY A GRAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 11 1070T 45784 655415 RNO - ON TAKEOFF ROLL, AIRCRAFT HAD A NR 2 ENGINE OIL STRAINER CLOGGING LIGHT ILLUMINATE. AIRCRAFT ABORTED TAKEOFF AT 6 0 KIAS. AIRCRAFT RETURNED TO THE RAMP WITHOUT FURTHER OCCURRENCE. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE MAI N OIL FILTER ASSEMBLY. MAINTENANCE RAN THE NR 2 ENGINE FOR AN OPERATIONAL AND LEAK CHECK. NR 2 ENGINE OPERATIONALLY CH ECKED NORMAL, NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F 4 F A6WE E2EA 1996030800209 19960308 00209 EA 1996 3 8 HNAA9690512 1 19960219 A 3230 155507 ACTUATOR DHAV DHC7 DHC7102 2802708 EA LT MLG FAILED A HNAA K NONE J WARNING INDICATION AP APPROACH 1 EA 07 905HA 31529 471 MC146 070 DCA/PHL - FLT 3169 - UPON APPROACH TO PHL, THE LT MLG WOULD NOT EXTEND. CREW PERFORMED ALTERNATE GEAR EXTENSION AND LAN DED WITHOUT INCIDENT. REMOVED AND REPLACED THE LT MLG LOCK ACTUATOR. (X) 2 H 7 4 4T A20EA 1996030800210 19960308 00210 NM 1996 3 8 HNAA9692011 1 19960213 A 3350 6013211X BATTERY PACK DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 920HA 14821 ORF175 084 PHF/DCA - FLT 3091 - DURING PREFLIGHT WALK-AROUND, FOUND LEFT AND RIGHT UNDERWING INTERIOR AND EXTERIOR EEL LIGHTS INOPE RATIVE. REMOVED AND REPLACED PS3 AND PS6 BATTERY PACKS. (X) 2 H 7 2 4T RT A13NM 1996030800211 19960308 00211 NM 1996 3 8 HNAA9697510 1 19960205 A 3231 ACTUATOR ROD DHAV DHC8 DHC8102 2809003 NM LT MLG DOOR OUT OF ADJUST A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 975HA 176 SBY/PHL - FLT 3081 - AFTER TAKEOFF, THE LEFT GEAR DOOR ADVISORY LIGHT REMAINED ON. THE AIRCRAFT RETURNED TO SBY AND LAN DED WITHOUT INCIDENT. REMOVED ICE FROM THE GEAR DOOR AND THE GEAR DOOR PROXIMITY SENSOR BRACKET ASSEMBLY. EVALUATION F LIGHT FOUND UNSATISFACTORY. UPON RETURN, ADJUSTED LEFT FORWARD GEAR DOOR ACTUATOR ROD. GEAR SWING OPERATIONAL CHECK GO OD. (X) 2 H 7 2 4T RT A13NM 1996030800212 19960308 00212 EU 1996 3 8 P2RA960004 1 19960213 A 3350 311701 BATTERY PACK AIRBUS 300 A300B4203 3930306 EU R-2 DOOR DISCHARGED A P2RA K NONE L NO TEST IN INSP/MAINT 1 WP 23 14975 0390 261 FOUND R-2 AND L-2 EMERGENCY 'EXIT' LIGHTS INOPERATIVE. CLEANED CONTACTS ON BATTERY PACK FOR L-2 DOOR LIGHT, OPS CHECK O K. REPLACED BATTERY PACK FOR R-2 'EXIT' LIGHT, OPS CHECK OK. (X) 2 L 7 2 4F A35EU 1996030800213 19960308 00213 EU 1996 3 8 PLG2196E1 1 19960201 A 2612 72PEF910129 FIRE CONTROL BOX SAAB SF340 SF340A 7850100 EU RT ENGINE MALFUNCTIONED A PLGA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NE 05 745BA 0237 340A111 BOS - FLT 4304 - AFTER DEPARTURE, RIGHT ENGINE FIRE WARNING CAME ON INTERMITTENTLY. THE AIRCRAFT RETURNED TO BOS AND LA NDED WITHOUT INCIDENT. MAINTENANCE DETERMINED PROBLEM TO BE INDICATION ONLY. THE RIGHT FIRE DETECT CONTROL BOX REMOVED AND REPLACED FOR TROUBLESHOOTING. MAINTENANCE PERFORMED OPERATIONAL CHECK OF FIRE DETECT SYSTEM. NO FAULT FOUND. SYS TEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1996030800214 19960308 00214 CE 1996 3 8 PLG2196E2 1 19960201 A 3260 308607084300X INDICATOR BEECH 1900 1900C 1154161 CE LANDING GEAR BROKEN A PLGA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NE 05 3068M UB69 BOS - FLT 4868 - DURING CLIMB-OUT, CREW NOTED AFTER GEAR RETRACTION, THE DOWN AND LOCKED INDICATORS WERE STILL LIT. THE AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. THE AIRCRAFT FERRIED TO PSM FOR REPAIRS. MAINTENANCE REPLACED T HE DOWN AND LOCKED INDICATOR AND SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1996030800215 19960308 00215 EU 1996 3 8 PLG2196E3 1 19960201 A 2612 899253 FIRE LOOP SAAB SF340 SF340A 7850100 EU RT ENGINE INTERMITTENT A PLGA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NE 05 745BA 340A111 BOS - FLT 4304 - AFTER DEPARTURE, RIGHT ENGINE FIRE WARNING CAME ON INTERMITTENTLY. AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE VERIFIED THE PROBLEM WAS ONLY INDICATION. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE FIRE LOOP. SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1996030800216 19960308 00216 CE 1996 3 8 PLG2796E1 1 19960204 A 3230 RETRACT MECH BEECH 1900 1900C 1154161 CE NLG LACK OF LUBE A PLGA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 NE 05 820BE UB64 ACK - FLT 4947 - DURING DESCENT INTO ACK, CREW NOTED THE NOSE GEAR DID NOT FULLY EXTEND. AIRCRAFT DIVERTED TO BOS. CRE W PUMPED GEAR DOWN AND OBTAINED THREE GREEN DOWN AND LOCK INDICATIONS. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE I NSPECTED THE GEAR SYSTEM, CLEANED, AND LUBED ALL INDICATION SWITCHES. THE GEAR WAS SWUNG NUMEROUS TIMES WITH NO FAULTY INDICATIONS. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1996030800217 19960308 00217 EU 1996 3 8 PLG2896E1 1 19960208 A 2421 31342001 AC GENERATOR SAAB SF340 340B 7860101 EU LEFT FAILED A PLGA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CR CRUISE 1 NE 05 365BE 10906 1789 726 340B299 FLT NR 4910 - CLOSE OUT WITH THE REMOVAL AND REPLACEMENT OF THE LEFT AC GNERATOR. THE LEFT AC GENERATOR SYSTEM OPS CHEC KED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1996030800218 19960308 00218 CE 1996 3 8 PLG2996E1 1 19960209 A 5210 SEAL BEECH 1900 1900C 1154161 CE PASSENGER DOOR LOOSE A PLGA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NE 05 15394 UC63 BTV/LGA - FLT 4693 - DURING FLIGHT AT 16,000 FEET, CREW NOTICED AIRCRAFT STARTING TO DEPRESSURIZE. AT THE SAME TIME, TH EY HEARD A LOUD SQUEAL COMING FROM THE MAIN CABIN DOOR. THE AIRCRAFT DIVERTED TO ALB AND LANDED WITHOUT INCIDENT. MAIN TENANCE INSPECTED DOOR AND FOUND THE DOOR SEAL HAD COME LOOSE. MAINTENANCE REINSTALLED THE SEAL AND DEFERRED THE PRESSU RIZATION UNTIL THE SEAL CAN BE REPLACED. AIRCRAFT WAS RELEASED TO SERVICE. THIS SDR WILL REMAIN OPEN UNTIL SEAL IS REM OVED AND REPLACED. (X) 2 L 7 2 4T RT A24CE 1996030800219 19960308 00219 EU 1996 3 8 RAIA960153 1 19960126 A 5270 SP4594 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGGAGE DOOR OUT OF ADJUST A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 557HK 597 41074 DCA - FLT 7748 - BAGGAGE DOOR LIGHT ILLUMINATED DURING TAKEOFF. MAINTENANCE PLACED SYSTEM ON DMI 52-2. MAINTENANCE LAT ER CLEARED DMI BY ADJUSTING MICROSWITCH, OPERATION CHECK GOOD. (X) 2 L 7 2 4T RT A41NM 1996030800220 19960308 00220 EU 1996 3 8 RAIA960202 1 19960201 A 3240 C24646070 BRAKE VALVE AEROSP ATR42 ATR42300 8680920 EU RT MLG ACT LEAKING A RAIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CE 03 423TE 16110 119 STL - FLT 7174 - HYDRAULIC PRESSURE ON GREEN SYSTEM LOST AT GEAR RETRACTION, GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED FROM FLIGHT WITHOUT INCIDENT. MAINTENANCE FOUND RT MLG ACTUATOR BRAKE VALVE CRACKED REPLACED VALVE, GEAR SWING OPS CHEC K GOOD. (X) 2 H 7 2 4T RT A53EU 1996030800221 19960308 00221 EU 1996 3 8 RAIA960203 1 19960201 A 3230 NTA11155 ACTUATOR BOLT AEROSP ATR42 ATR42300 8680920 EU LT MLG ACT FAILED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 16110 119 STL - DURING MAINTENANCE CHECK GEAR SWING, THE LT MLG ACTUATOR FUSELAGE MOUNTING BRACKET HARDWARE WAS FOUND BROKEN LOOSE . MAINTENANCE REPLACED BRACKET HARDWARE AND REPAIRED ATTACH FITTINGS, GEAR WINGS OPS CHECK GOOD. (X) 2 H 7 2 4T RT A53EU 1996030800222 19960308 00222 EU 1996 3 8 RAIA960204 1 19960203 A 3222 B00A703056A STRUT BAG JETSTM JETSTM3201 1500217 EU NOSE GEAR REQ'D SERVICE A RAIA O OTHER J WARNING INDICATION CL CLIMB 1 CE 03 425AM 10665 5828 870 CMI - FLT 7443 - GEAR WOULD NOT COME UP WHEN SELECTED UP. MAINTENANCE REPACKED NOSE STRUT, PERFORMED GEAR SWING, OPERAT IONAL CHECK GOOD. (X) 2 L 7 2 4T RT A56EU 1996030800223 19960308 00223 EU 1996 3 8 RAIA960205 1 19960204 A 3260 5EN16N95 SWITCH BAG JETSTM JETSTM3201 1500217 EU NOSE GEAR OUT OF ADJUST A RAIA O OTHER N FALSE WARNING CL CLIMB 1 CE 03 425AM 10636 870 STL - FLT 7326 - LANDING GEAR HANDLE WOULD NOT MOVE TO 'UP' POSITION AFTER TAKEOFF. MAINTENANCE ADJUSTED NOSE SQUAT SWI TCH, PERFORMED GEAR SWING, OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4T RT A56EU 1996030800224 19960308 00224 EU 1996 3 8 RAIA960206 1 19960201 A 3411 PITOT SYSTEM BAG JETSTM JETSTM3201 1500217 EU LT/RT FROZEN A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 432AM 883 STL - FLT 7455 - BOTH AIRSPEED INDICATORS STUCK AT 80 KNOTS ON TAKEOFF ROLL. MAINTENANCE THAWED AIRCRAFT PITOT SYSTEM, OPERATION CHECK GOOD ON HIGH-SPEED TAXI. (X) 2 L 7 2 4T RT A56EU 1996030800225 19960308 00225 1996 3 8 RAIA960207 4 19960201 A 3414 39948B2236 AIRSPEED IND BAG JETSTM JETSTM3201 1500217 EU LT COCKPIT FAILED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 338TE 8141 932 STL - FLT 7318 - CAPTAIN'S AIRSPEED INDICATOR INOPERATIVE. MAINTENANCE REPLACED AIRSPEED INDICATOR, OPERATION CHECK AND LEAK CHECK GOOD. (X) 2 L 7 2 4T RT A56EU 1996030800226 19960308 00226 EU 1996 3 8 RAIA960208 1 19960202 A 3411 PITOT SYSTEM BAG JETSTM JETSTM3201 1500217 EU RIGHT CONTAMINATED A RAIA O OTHER N FALSE WARNING CL CLIMB 1 CE 03 338TE 932 STL - FLT 7410 - FIRST OFFICER'S AIRSPEED INDICATOR GIVING FALSE INDICATION, AIRSPEED INCREASES WITH ALTITUDE. MAINTENA NCE PURGED AND LEAK TESTED PITOT STATIC SYSTEM, OPERATION CHECK GOOD. (X) 2 L 7 2 4T RT A56EU 1996030800227 19960308 00227 EU 1996 3 8 RAIA960209 1 19960203 A 3222 B00A703056A STRUT BAG JETSTM JETSTM3201 1500217 EU NOSE GEAR REQ'D SERVICE A RAIA O OTHER J WARNING INDICATION CL CLIMB 1 CE 03 436AM 10304 4145 891 STL - FLT 7477 - NOSE GEAR INTRANSIT LIGHT REMAINED ILLUMINATED WHEN GEAR SELECTED UP. MAINTENANCE RE-PACKED NLG STRUT, NOSE WHEEL STEERING, AND GEAR SWING CHECK GOOD. (X) 2 L 7 2 4T RT A56EU 1996030800228 19960308 00228 WP 1996 3 8 RAIA960210 2 19960206 A 7321 89778025 FUEL CONTROL BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT ENGINE OUT OF ADJUST A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 423AM 9250 2288 858 66345 STL - FLT 7332 - AFTER TAKEOFF, LT RPM WOULD ONLY MAKE 97 PERCENT. MAINTENANCE ADJUSTED SCREW 'X'. PERFORMED GROUND RU NS, OPERATIONAL CHECK GOOD. ENGINE TT, 4,598.7 HOURS. (X) 2 L 7 2 4T 4 T RT A56EU E4WE 1996030800229 19960308 00229 NE 1996 3 8 RAIA960211 2 19960206 A 7200 ENGINE AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW124B NE LEFT OIL LEAK A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 03 721TE 7550 5254 217 124172 PIA - FLT 7121 - ELECTRIC SMOKE INDICATION ON CCAS ACCOMPANIED BY SMOKE IN FORWARD CABIN AND FORWARD CARGO. MAINTENANCE DEFERRED LEFT PACK SYSTEM. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE. PERFORMED GROUND RUNS, OPERATIONAL CHECK GOO D, DMI CLEARED. (X) 2 H 7 2 4T 4 T RT A53EU E2ONE 1996030800230 19960308 00230 EU 1996 3 8 RAIA960212 1 19960206 A 5210 S52176001008 DOOR AEROSP ATR42 ATR42300 8680920 EU PASSENGER CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 421TE 16869 102 STL - DURING A MAINTENANCE INSPECTION, PASSENGER DOOR WAS FOUND TO HAVE CORROSION ON SEVERAL STRUCTURAL MEMBERS. MAINTE NANCE REPLACED PASSENGER DOOR. (X) 2 H 7 2 4T RT A53EU 1996030800231 19960308 00231 EU 1996 3 8 RAIA960213 1 19960206 A 3260 9005EN38 SWITCH BAG JETSTM JETSTM3201 1500217 EU LT MLG FAILED A RAIA O OTHER N FALSE WARNING DE DESCENT 1 CE 03 428AM 10607 877 STL - FLT 7068 - LT MAIN GEAR DOWN AND LOCKED GREEN INDICATOR REMAINS ILLUMINATED AT ALL TIMES. MAINTENANCE REPLACED LE FT DOWNLOCK SWITCH, GEAR SWING GOOD. (X) 2 L 7 2 4T RT A56EU 1996030800232 19960308 00232 WP 1996 3 8 RAIA960214 2 19960207 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RIGHT LOW POWER A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CE 03 425AM 870 66075 BMI - FLT 7325 - ON TAKEOFF AFTER THE POWER WAS SET ON RIGHT ENGINE 100 PERCENT, THE TORQUE DROPPED BELOW 40 PERCENT. T HE TAKEOFF WAS ABORTED. MAINTENANCE INSPECTED RIGHT ENGINE FOR BLEED LEAKS. NONE FOUND. GROUND RAN AIRCRAFT, OPS CHEC K GOOD. ENGINE TT, 9,162.5 HOURS. (X) 2 L 7 2 4T 4 T RT A56EU E4WE 1996030800233 19960308 00233 EU 1996 3 8 RAIA960215 1 19960208 A 2120 AIR DISTRIBUTOR AEROSP ATR72 ATR72202 8680940 EU COCKPIT SMOKE A RAIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 721TE 217 STL - FLT 7170 - DURING TAXI, SMOKE IN COCKPIT AND FRONT CABIN. MAINTENANCE PERFORMED GROUND RUNS WITH PACKS ON. FOUND NO VISUAL INDICATIONS OF SMOKE. (X) 2 H 7 2 4T RT A53EU 1996030800234 19960308 00234 EU 1996 3 8 RAIA960216 1 19960208 A 3260 9005EN38 SWITCH BAG JETSTM JETSTM3201 1500217 EU RT MLG DIRTY A RAIA O OTHER N FALSE WARNING CL CLIMB 1 CE 03 971JX 5526 971 LAX - FLT 4784 - RIGHT GREEN DOWN AND LOCKED LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. MAINTENANCE CLEANED RIGH T MLG DOWNLOCK SWITCH, GEAR SWING GOOD. (X) 2 L 7 2 4T RT A56EU 1996030800235 19960308 00235 CE 1996 3 8 S2YA950030 1 19960126 A 5270 MS2250081 SWITCH BEECH 1900 1900D 1154162 CE PASSENGER DOOR LOOSE WIRE A S2YA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 13 79SK 4776 UE79 THE CABIN DOOR WARNING ANNUNCIATOR ILLUMINATED IN FLIGHT, THE LIGHT EXTINGUISHED WHEN THE CABIN DIFFERENTIAL PRESSURE DR OPPED TO 1.0 PSI. THE CREW DIVERTED TO SBN FROM THE INTENDED DESTINATION OF MKE, FLIGHT NR 1053.1. THE AIRCRAFT WAS TH EN FERRIED FROM SBN TO MKE. MAINTENANCE CLEANED AND LUBED THE SENSE SWITCH. THEY ALSO TIGHTENED A LOOSE WIRE TERMINAL TO THE SWITCH. OPERATIONALLY CHECKED THE SYSTEM AND FOUND NORMAL. (X) 2 L 7 2 4T RT A24CE 1996030800236 19960308 00236 EU 1996 3 8 SABA960001 1 19960204 A 7603 SWITCH ROLLER BAG JETSTM JETSTM3101 1500215 EU RT POWER LEVER WORN A SABA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 05 156PC 728 CLT/AHN - FLT 5125 - ON 2-4-96, HAD JUST ROTATED WHEN THE BETA HORN STARTED BLOWING. THE CAPTAIN CIRCLED AROUND AND MAD E AN UNEVENTFUL LANDING. UPON LANDING, THE BETA HORN WENT SILENT. AFTER THE PASSENGERS WERE DEPLANED, MAINTENANCE PERS ONNEL INSPECTED THE AIRCRAFT. THE ROLLER FOR THE RIGHT POWER LEVER MICROSWITCH WAS FOUND FLAT SPOTTED. THE ROLLER WAS REPLACED AND BETA HORN SYSTEM FUNCTION CHECKED. ALL INDICATIONS NORMAL. THE AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A21EU 1996030800237 19960308 00237 EU 1996 3 8 SABA960002 1 19960212 A 3260 SWITCH WIRE BAG JETSTM JETSTM3101 1500215 EU LT MLG BROKEN A SABA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 05 159PC 768 CLT/HTS - FLT 5112 - ON 2-12-96, SELECTED GEAR UP, ALL 3 INTRANSIT LIGHTS ILLUMINATED. TWO INTRANSIT LIGHTS EXTINGUISHE D, LT MAIN LIGHT REMAINED ILLUMINATED. MAINTENANCE CONTROL CONTACTED AND SUPERVISOR NOTIFIED OF THE PROBLEM. CAPTAIN W AS INFORMED TO RETURN TO CLT SO PROBLEM COULD BE CORRECTED. CAPTAIN INFORMED AIR TRAFFIC CONTROL OF HIS NEED TO RETURN TO CLT. HE DID NOT DECLARE EMERGENCY. LANDING GEAR EXTENDED AND CAPTAIN HAD 3 GREEN LIGHTS ILLUMINATED. ACFT MADE UNE VENTFUL LANDING IN CLT, AND AFTER PASSENGERS DEPLANED, MX INSPECTED LT MAIN GEAR AND FND BROKEN WIRE ON UPLOCK MICROSWIT CH. BROKEN WIRE REPAIRED. EXTENSION AND RETRACTION SYSTEMS WERE FUNCTION TESTED, AND ACFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A21EU 1996030800238 19960308 00238 NE 1996 3 8 SABA960003 2 19960213 A 7230 COMPRESSOR STBROS SD3 SD360 8100606 EU PWA PT6 PT6A67R 52043 NE NR 1 ENGINE SEIZED A SABA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 05 742CC 14491 4579 SH3742 106035 CLT/OAJ - FLT 5006 - ON 2-13-96, HAD ROTATED AND JUST SELECTED GEAR UP WHEN NR 1 ENGINE PRODUCED 'LOUD BOOM' AND SHUT IT SELF DOWN. CAPTAIN DECLARED EMERGENCY, PERFORMED EMERG CHECKLIST ITEMS, AND RETURNED TO FIELD FOR UNEVENTFUL LANDING. A FTER PASSENGERS DEPLANED, MX INSPECTED NR 1 ENGINE. OIL FOUND AROUND INTAKE AREA. OIL FILTER WAS PULLED AND FND CONTAM INATED WITH FINE METAL PARTICLES. COMPRESSOR SCREEN PULLED AND COMPRESSOR COULD NOT BE TURNED BY HAND. BASED ON THESE FINDINGS, DECISION MADE TO REPLACE ENGINE. NO ENGINE IN STOCK, ONE ORDERED AOG. ACFT CURRENTLY IN HANGAR WITH NR 1 ENG INE REMOVED AWAITING ARRIVAL OF A SERVICEABLE ENGINE. (X) 2 H 7 2 4T 4 T A41EU E26NE 1996030800239 19960308 00239 SO 1996 3 8 WTAA960034 1 19960215 A 3230 922FSZA6NZ735 PROX SENSOR EMB 120 EMB120RT SO NOSE GEAR FAILED A WTAA O OTHER J WARNING INDICATION CL CLIMB 1 WP 17 251YV 120251 SFO - LANDING GEAR FAILED TO RETRACT AFTER DEPARTURE. CREW USED OVER-RIDE SYSTEM TO COMPLETE GEAR RETRACTION. AIRCRAFT FERRIED TO FAT FOR REPAIRS. FAT MAINTENANCE REMOVED AND REPLACED NOSE GEAR WEIGHT ON WHEELS PROXIMITY SENSOR. LANDING GEAR RETRACTION CHECK NORMAL DURING GEAR SWING. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1996030800240 19960308 00240 1996 3 8 HEEA966684 4 19960212 A 3452 066106200 TRANSCEIVER KT76 BELL 206 206L1 1182107 SW COCKPIT ATC DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2761X 45283 FIRST DIGIT KNOB BROKEN. REPLACED KNOB. ALSO REPLACED V101 CAVITY THAT WAS WEAK. INSPECTED AND UNIT BENCH CHECK GOOD. 1 G 7 1 3U H2SW 1996030800241 19960308 00241 1996 3 8 HEEA966685 4 19960212 A 3452 066106200 TRANSCEIVER KT76 AEROSP AS355 AS355F2 8680812 EU COCKPIT ATC DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 6040U 5474 2 YEAR INSPECTION DUE. REPLACED WEAK V101 CAVITY OSCILLATOR, WEAK V301 PHOTO DETECTOR AND DETERIORATED R477 RESISTOR. A DJUSTED AND BENCH CHECK GOOD. 1 G 7 2 3U H11EU 1996030800242 19960308 00242 1996 3 8 HEEA966686 4 19960212 A 2312 40001452502 TRANSCEIVER RT138F BOLKMS 105 BO105S 5626006 EU COCKPIT VHF FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 131AE S787 GUARD LIGHT STAYS ON, CAN'T TRANSMIT OR RECEIVE ON GUARD FREQUENCY WHEN CONTROL UNIT SWITCHED ON CHANNEL 2-15. VERIFIED GUARD RECEIVER VERY INTERMITTENT. TROUBLESHOT AND REPAIRED COLD SOLDIER JOINT ON J11 OF GUARD RECEIVER BOARD. ADJUSTED FREQUENCY AND MIC GAIN. UNIT BENCH CHECK GOOD. 1 G 7 2 3U H3EU 1996030800243 19960308 00243 1996 3 8 HEEA966687 4 19960212 A 3453 25410038 LORAN 7000CDU BELL 412 412 1182202 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 22608 33075 CDU BLANKS OUT ON BRG/DIST. SELECTION - GIVES NO DATA. 1 G 7 2 4U H4SW 1996030800244 19960308 00244 SW 1996 3 8 HEEA966688 1 19960212 A 6720 214001540117 ACTUATOR ASSY BELL 214 214ST 1182106 SW SAS YAW DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 SAS YAW CHANNEL WOULD NOT COME ON LINE UNTIL ACTUATOR LOCK WAS PUSHED INTO OPEN POSITION. WITH ACTUATOR INSTALLED IN AI RCRAFT, LOCK SOLENOID WOULD NOT OPEN LOCK WITHOUT BEING PUSHED. LOCK WOULD STAY OPEN ONCE IT WAS PUSHED THERE. 2 G 7 2 4U H10SW 1996030800245 19960308 00245 GL 1996 3 8 HEEA966689 2 19960212 A 7314 3881005 FUEL PUMP BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL ENG WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 41128 1766 51134 CAE895384 FUEL PUMP WORN INTERNAL SPLINES. 1 G 7 1 3U 3 U H2SW E1GL 1996030800246 19960308 00246 SW 1996 3 8 HEEA966695 1 19960215 A 6410 205012710001 BEARING 212011701003 BELL 412 412 1182202 SW T/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911FD 942 A714 33056 BLADE BEARINGS WORN BEYOND LIMITS. ( 1 G 7 2 4U H4SW 1996030800247 19960308 00247 SW 1996 3 8 HEEA966697 1 19960215 A 3340 214175127103 POWER SUPPLY BELL 214 214ST 1182106 SW STROBE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5748M 30 28102 DOES NOT SUPPLY POWER TO STROBE LIGHT. 2 G 7 2 4U H10SW 1996030800248 19960308 00248 EU 1996 3 8 HEEA966698 1 19960220 A 6210 10515141 BLADE BOLKMS 105 BO105S 5626006 EU M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 624MB 9198 S751 M/R BLADE NOSE AND NECK SHELLS CRACKED AND SEPARATED AT ROOT END AREA. 1 G 7 2 3U H3EU 1996030800249 19960308 00249 EU 1996 3 8 HEEA966699 1 19960220 A 6210 10515141 BLADE BOLKMS 105 BO105S 5626006 EU M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 624MB 8726 S751 M/R BLADE NOSE AND NECK SHELLS CRACKED AND SEPARATED AT ROOT END AREA. 1 G 7 2 3U H3EU 1996030800250 19960308 00250 EU 1996 3 8 HEEA966700 1 19960220 A 7722 56265550011 INDICATOR AEROSP AS355 AS355F1 8680810 EU COCKPIT T4 ERRATIC E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5793Y 5141 T4 INDICATOR NEEDLE HAS A ERRATIC INDICATION. TIME SINCE REPAIR 0:00. 1 G 7 2 3U H11EU 1996030800251 19960308 00251 1996 3 8 HEEA966703 4 19960220 A 3442 MI5851345 INDICATOR P40 SKRSKY S76 S76A 8143006 NE COCKPIT RADAR DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 31219 760230 INDICATOR INTERMITTENT UNSTABLE PICTURE. UNIT HAS BAD CRT, BAD REFRESH MEMORY BOARD AND BAD VIDEO BOARD. 1 G 7 2 3U H1NE 1996030800252 19960308 00252 1996 3 8 HEEA966704 4 19960220 A 3444 066305401 INDICATOR KI250 BOLKMS 105 BO105S 5626006 EU COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 911EB S812 WILL NOT TEST. REPLACED CRACKED LENS AND RUBBER GASKET. ALIGNED AND CALIBRATED TO SPECS. BENCH CHECK GOOD. 1 G 7 2 3U H3EU 1996030800253 19960308 00253 EU 1996 3 8 HEEA966706 1 19960220 A 6410 355A09103600 BEARING SNIAS 350 AS350B2 8680813 EU T/R HALF SHELL WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 2510 2771 BEARING DETERIORATED. 1 G 7 1 3U H9EU 1996030800254 19960308 00254 SW 1996 3 8 HEEA966707 1 19960220 A 5320 206031314083S CHANNEL BELL 206 206L3 1182108 SW FUSELAGE MIS MFG E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 41128 51134 CHANNEL FORWARD UPPER FLANGE HAS NO EDGE DISTANCE FOR RIVET INSTALLATION. 1 G 7 1 3U H2SW 1996030800255 19960308 00255 SW 1996 3 8 HEEA966708 1 19960220 A 6220 206010121005 LATCH BELL 206 206L3 1182108 SW M/R MIS MFG E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 41128 51134 BEVEL FOR LATCH BOLT NUT MACHINED WRONG (TOO SHALLOW) 1 G 7 1 3U H2SW 1996030800256 19960308 00256 EU 1996 3 8 HEEA966709 1 19960220 A 6210 10515150 BLADE BOLKMS 105 BO105S 5626006 EU M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 54191 3582 S804 BLADE NOSE AND NECK SHELLS CRACKED AT THE CUFF AREA) 1 G 7 2 3U H3EU 1996030800258 19960308 00258 1996 3 8 HEEA966711 4 19960220 A 3451 066106600 TRANSCEIVER BELL 412 412 1182202 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 108X 33115 TRANSCEIVER INOPERATIVE; WEAK RECEIVE ON SOME CHANNELS. 1 G 7 2 4U H4SW 1996030800259 19960308 00259 1996 3 8 HEEA966712 4 19960220 A 3453 4530103 LORAN ARNAV21 BELL 206 206L3 1182108 SW COCKPIT WEAK E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3108E 51498 LORAN DISPLAY WEAK. 1 G 7 1 3U H2SW 1996030800260 19960308 00260 1996 3 8 HEEA966713 4 19960220 A 3442 MI5851352 R/T UNIT P40 SKRSKY S76 S76A 8143006 NE RADAR DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545X 760050 R/T UNIT HAS BAD IF BOARD AND BAD MODULATOR BOARD CAUSING UNIT TO DROP OFF LINE IN MAP MODE. ALSO GAIN VOLTAGE IS OUT O F SPECS. AT MAXIMUM GAIN, UNABLE TO ADJUST. 1 G 7 2 3U H1NE 1996030800261 19960308 00261 1996 3 8 HEEA966714 4 19960220 A 3422 5050010902 GYRO SNIAS 350 AS350B2 8680813 EU COCKPIT ERRATIC E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 6100R 2862 GYRO UNIT WILL NOT MAINTAIN HEADING (ERRATIC) 1 G 7 1 3U H9EU 1996030800262 19960308 00262 1996 3 8 HEEA966715 4 19960220 A 3442 MI5851345 INDICATOR P40 SKRSKY S76 S76A 8143006 NE COCKPIT FAULTY E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1545X 760050 INDICATOR DROPS OFF LINE AND HAS INTERMITTENT GLICK ON SCREEN. 1 G 7 2 3U H1NE 1996030800263 19960308 00263 SW 1996 3 8 HEEA966716 1 19960222 A 2910 AE1009102G0174 HOSE ASSY BELL 230 230 1182149 SW HYD SYS CHAFED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 825 23009 HOSE CHAFED 1 G 7 2 3U NC H9SW 1996030800264 19960308 00264 SW 1996 3 8 HEEA966717 1 19960222 A 2430 A772XTA RELAY BELL 230 230 1182149 SW DC SYS FAULTY E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 2789 23009 TROUBLESHOOTING GENERATORS COMING OFF LINE, AFTER ENGINE START. FOUND RELAY FAULTY. 1 G 7 2 3U NC H9SW 1996030800265 19960308 00265 SW 1996 3 8 HEEA966718 1 19960222 A 2430 A772XTA RELAY BELL 230 230 1182149 SW DC SYS FAULTY E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 61 23009 WHEN STARTING EITHER #1 OR #2 ENGINES FIRST, RESPECTIVE STARTER GENERATOR WOULD NOT COME ON LINE. (INTERMITTENT PROBLEM ) 1 G 7 2 3U NC H9SW 1996030800266 19960308 00266 SW 1996 3 8 HEEA966719 1 19960222 A 6330 222331618105 ISOLATION MOUNT BELL 230 230 1182149 SW M/R XMSN BEARING WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 506 23009 MOUNT BEARING WORN. 1 G 7 2 3U NC H9SW 1996030800267 19960308 00267 EU 1996 3 8 HEEA966720 1 19960222 A 2822 704A37721081 SWITCH SNIAS 350 AS350B2 8680813 EU FUEL BOOST FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 246 2771 BOOST PUMP DOES NOT ILLUMINATE "FUEL PUMP" LIGHT WHEN TURNED OFF. SWITCH FAILED. 1 G 7 1 3U H9EU 1996030800268 19960308 00268 SW 1996 3 8 HEEA966721 1 19960222 A 6710 206062721105 ACTUATOR BELL 230 230 1182149 SW M/R DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 23009 STROKE ADJUSTMENT WAS NOT CONSTANT AND WOULD NOT ADJUST TO MINIMUM RANGE. 1 G 7 2 3U NC H9SW 1996030800269 19960308 00269 SW 1996 3 8 HEEA966722 1 19960226 A 6720 230312001101 LINK BELL 230 230 1182149 SW T/R WORN EXCESS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 272 23009 LINK IS WORN EXCESSIVELY. (SPHERICAL BEARINGS WORN) 1 G 7 2 3U NC H9SW 1996030800270 19960308 00270 SW 1996 3 8 HEEA966724 1 19960226 A 6720 222312702101 PITCH LINKS BELL 230 230 1182149 SW T/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 418 23009 PITCH LINK BEARINGS WORN. 1 G 7 2 3U NC H9SW 1996030800271 19960308 00271 EU 1996 3 8 HEEA966726 1 19960226 A 6220 704A33633109 BEARING SNIAS 350 AS350B2 8680813 EU M/R BLISTERED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 1803 2771 BEARING IS BLISTERED AND SEPARATING. 1 G 7 1 3U H9EU 1996030800272 19960308 00272 1996 3 8 HEEA966727 4 19960226 A 3452 066106200 TRANSCEIVER KT76 BELL 206 206B 1181511 SW COCKPIT ATC DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2278V 3632 TRANSCEIVER OFF FREQUENCY. REPLACED DEFECTIVE V101 CAVITY OSCILLATOR. ALSO REPLACED DETERIORATED R477 RESISTOR AND REPL ACED WEAK V301 PHOTOCELL. ADJUSTED AND BENCH CHECK GOOD. 1 G 7 1 3U H2SW 1996030800273 19960308 00273 1996 3 8 HEEA966728 4 19960226 A 3452 066106200 TRANSCEIVER KT76 BELL 206 206L1 1182107 SW COCKPIT ATC WEAK E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2759U 45267 TRANSMITS WEAK. REPLACED WEAK V101 CAVITY OSCILLATOR. ALSO REPLACED WEAK V301 PHOTODETECTOR. ADJUSTED FREQUENCY AND BE NCH CHECK GOOD. 1 G 7 1 3U H2SW 1996030800274 19960308 00274 1996 3 8 HEEA966729 4 19960226 A 3444 066304400 ALTIMETER. BELL 214 214ST 1182106 SW COCKPIT RAD ALT READS LOW E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3897N 28106 RADAR ALT READS 500 FEET LOW AND VARIABLE. VERIFIED INDICATOR TO READ LOW. PERFORMED TOTAL ALIGNMENT. REPAIRED. FOUND DH BULB TO INTERMITTENTLY LIGHT. REPLACED DH PUSH BUTTON SWITCH DS101 AND BULB DS101A. REPAIRED. BENCH CHECK GOOD. 2 G 7 2 4U H10SW 1996030800275 19960308 00275 1996 3 8 HEEA966730 4 19960226 A 2312 4000106010 CONTROL UNIT C10 BOLKMS 105 BO105S 5626006 EU COCKPIT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 911EB S812 DISPLAY WILL NOT COME ON. REPLACED FUSE F1 AND DIODE CR5. REPAIRED. DISPLAY DOES NOT DIM. REPLACED PHOTOCELL RT1. RE PAIRED. REPLACED INTERMITTENT THUMBWHEEL ASSY. BENCH CHECK GOOD. 1 G 7 2 3U H3EU 1996030800276 19960308 00276 1996 3 8 HEEA966731 4 19960226 A 3452 066106200 TRANSCEIVER KT76 BELL 206 206L 1181522 SW COCKPIT ATC DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 62127 52023 ATC NOT RECEIVING CODE 0461. VERIFIED UNIT HAD NO POWER OUT. REPLACED V101 P/N C2080A. REPAIRED. ADJUSTED POWER AND F REQUENCY. BENCH CHECK GOOD. 1 G 7 1 3U H2SW 1996030800277 19960308 00277 1996 3 8 HEEA966732 4 19960226 A 3450 071106603 RECEIVER KFS580B SKRSKY S76 S76A 8143006 NE COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5426U 760167 NO AUDIO AND WILL NOT TEST. ALSO FACEPLATE DAMAGED AND CRACKED. 1 G 7 2 3U H1NE 1996030800278 19960308 00278 SW 1996 3 8 HEEA966733 1 19960226 A 6320 206040032011 BEARING 206040004111 BELL 206 206L1 1182107 SW XMSN FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5007Q 1079 BMC45212 45187 BEARING BALLS AND RACER SPALLED CAUSING TRANSMISSION METAL IN OIL. REPLACED WITH SERVICEABLE BEARING. 1 G 7 1 3U H2SW 1996030800279 19960308 00279 1996 3 8 HEEA966736 4 19960228 A 2210 214074303115 AMPLIFIER ASSY BELL 214 214ST 1182106 SW AUTO FLT DEFECTIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 3897N 28106 AMPLIFIER WILL NOT TEST OR ENGAGE. 2 G 7 2 4U H10SW 1996030800280 19960308 00280 EU 1996 3 8 HEEA966737 1 19960228 A 6420 350A33211905 BODY SNIAS 350 AS350B2 8680813 EU T/R WORN BEARING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 668 2771 T/R BODY HAS WORN BEARING. 1 G 7 1 3U H9EU 1996030800281 19960308 00281 EU 1996 3 8 HEEA966738 1 19960228 A 7931 642790041 TRANSMITTER SNIAS 350 AS350B2 8680813 EU ENG OIL DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 2686 2771 CANNON PLUG END OF TRANSMITTER COMING LOOSE AND INDICATOR PEGS OUT. 1 G 7 1 3U H9EU 1996030800282 19960308 00282 EU 1996 3 8 HEEA966739 1 19960228 A 7933 646600251 TEMP PROBE SNIAS 350 AS350B2 8680813 EU ENG OIL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6097Z 1522 2820 ENGINE OIL TEMP PROBE FAILED CAUSING TEMP GAUGE TO GO TO HIGH STOP. 1 G 7 1 3U H9EU 1996030800283 19960308 00283 EU 1996 3 8 HEEA966740 1 19960228 A 5610 04011341990 WINDOW SNIAS 350 AS350B2 8680813 EU LT SLIDER CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100R 502 2862 WINDOW IS CRACKED. (LOWER TRACK ON SLIDE WINDOW CRACKED) 1 G 7 1 3U H9EU 1996030800284 19960308 00284 EU 1996 3 8 HEEA966743 1 19960228 A 2822 D107318D1 PUMP BOLKMS 105 BO105S 5626006 EU FUEL INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7062X S793 PUMP COMPLETELY INOPERATIVE. 1 G 7 2 3U H3EU 1996030800285 19960308 00285 EU 1996 3 8 HEEA966744 1 19960228 A 2844 DK042 TRANSMITTER BOLKMS 105 BO105S 5626006 EU FUEL PRESSURE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7062X 233 S793 FUEL PRESSURE GAUGE STICKS. 1 G 7 2 3U H3EU 1996030800286 19960308 00286 SW 1996 3 8 HEEA966745 1 19960228 A 2841 206075189001 INDICATOR BELL 206 206B 1181511 SW FUEL QTY FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 21431 3452 FUEL QTY INDICATOR WILL NOT INDICATE. 1 G 7 1 3U H2SW 1996030800287 19960308 00287 1996 3 8 HEEA966746 4 19960228 A 3453 25410036 LORAN 7000RCU BELL 412 412 1182202 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 22608 33075 ADVISORY LIGHT STAYS ON AT ALL TIMES. 1 G 7 2 4U H4SW 1996030800288 19960308 00288 SW 1996 3 8 HEEA966747 1 19960228 A 5311 206032308103S FRAME BELL 206 206L3 1182108 SW UPPER RT CRACKED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 31821 51076 CRACKED UPPER R/H. REPLACED WITH SERVICEABLE FRAME. 1 G 7 1 3U H2SW 1996030800289 19960308 00289 SW 1996 3 8 HEEA966748 1 19960228 A 6310 289051098 SEAL 206040270101 BELL 206 206L3 1182108 SW FREEWHEEL FELL OUT E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 6161A B127967 51611 SEAL FELL OUT OF SUPPORT ASSEMBLY. REPLACED WITH SERVICEABLE SEAL. 1 G 7 1 3U H2SW 1996030800290 19960308 00290 SW 1996 3 8 HEEA966749 1 19960228 A 5320 206031200076 STRAP BELL 206 206B 1181511 SW RT BOX BEAM CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2753F 2729 R/H BOX BEAM STRAP CRACKED AT UPPER AFT RADIUS JUST BELOW HIGH SHEER RIVETS. REPLACED STRAP AND RETURNED TO SERVICE. 1 G 7 1 3U H2SW 1996030800291 19960308 00291 SW 1996 3 8 HEEA966750 1 19960228 A 6510 327211 DISC SET BELL 206 206L3 1182108 SW T/R DRIVE CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 41128 51134 DISC SETS ARE CORRODED BEYOND LIMITS. REPLACED WITH SERVICEABLE DISC SETS. 1 G 7 1 3U H2SW 1996030800292 19960308 00292 SW 1996 3 8 HEEA966751 1 19960228 A 2435 214060056103 STARTER BELL 214 214ST 1182106 SW ENGINE DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 904 28101 STARTER DRAGGING. KICKS GENERATOR OFF LINE. COMMUTATOR PITTED. 2 G 7 2 4U H10SW 1996030800293 19960308 00293 1996 3 8 HEEA966752 4 19960228 A 3421 214175241101 GYROSCOPE BELL 214 214ST 1182106 SW COCKPIT FAULTY E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 GYRO WOULD NOT PUT OUT SIGNAL FOR ROLL CHANNEL TO THE AARS AMP. 2 G 7 2 4U H10SW 1996030800294 19960308 00294 EU 1996 3 8 HEEA966753 1 19960228 A 6320 704A37721089 SWITCH SNIAS 350 AS350B2 8680813 EU MGB PRESS DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100U 371 2863 CAUSES MGBP LIGHT TO COME ON INTERMITTENTLY. 1 G 7 1 3U H9EU 1996030800295 19960308 00295 WP 1996 3 8 HEEA966754 1 19960228 A 6520 369D25303 GEARBOX HUGHES 369 369D 4470706 WP T/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 CRACKED CORE. INVESTIGATE AND ANALYZE CASE. 1 G 7 1 3U H3WE 1996030800296 19960308 00296 EU 1996 3 8 HEEA966755 1 19960228 A 6520 350A33109100 GEAR SET SNIAS 350 AS350B2 8680813 EU T/R MAKING METAL E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 112 GEARS WERE INSTALLED ON GEARBOX S/N M-811 AT T.S.O. -0-. AFTER 112 HOURS METAL PARTICLES WERE FOUND ON CHIP DETECTOR. U PON DISASSEMBLY, FOUND UNUSUAL SCUFFING ON GEAR TEETH, NO OTHER DEFECTS WERE FOUND ON GEARBOX. 1 G 7 1 3U H9EU 1996030800297 19960308 00297 EU 1996 3 8 HEEA966756 1 19960228 A 6730 SC5081 SERVO SNIAS 350 AS350B2 8680813 EU M/R LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 6097Z 1234 2820 R/H FORWARD SERVO ON MAIN ROTOR WAS LEAKING AT UPPER BARREL TO BODY. (SERVO SENT WITH AIRCRAFT ON 11-4-94 AND INSTALLED 1-28-95. 1 G 7 1 3U H9EU 1996030800298 19960308 00298 WP 1996 3 8 9605059753 1 19960301 A 3350 BATTERIES DOUG DC9 DC941 302207N WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 753NW 47117 DURING LINE CHECK, FOUND ONE SECTION OF CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996030800299 19960308 00299 WP 1996 3 8 9605069865 1 19960301 A 2913 HYD PUMP DOUG DC9 DC951 3022051 WP LT ENGINE FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 01 774NC 47776 DURING CRUISE, THE LEFT ENGINE DRIVEN HYDRAULIC PUMP FAILED. FLIGHT DIVERTED TO ORD AND LANDED NORMALLY. FOUND PUMP SH AFT SHEARED. REPLACED PUMP, LEAK AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996030800300 19960308 00300 NM 1996 3 8 9605072276 1 19960303 A 3350 BATTERY PACK BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 276US 21155 DURING PREFLIGHT, FOUND FORWARD ENTRY DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT BATTERY PACK UNIT AND OPERATIONA L CHECK OK. 2 L 7 3 4F A3WE 1996030800301 19960308 00301 NM 1996 3 8 9605082284 1 19960301 A 2150 39854021 VALVE BOEING 727 727251 138408H NM RT PACK MALFUNCTIONED A NWAA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 GL 01 284US 29888 21127 21323 AFTER TAKEOFF DURING CLIMB, COULD NOT CONTROL AIRCRAFT CABIN PRESSURIZATION IN AUTO OR MANUAL MODES. AIRCRAFT RETURNED TO DTW DUMPING 20,000 LBS OF FUEL BEFORE LANDING WITHOUT INCIDENT. REPLACED THE RIGHT PACK VALVE AND CLEANED BOTH OUTFL OW VALVE SHAFTS. AIRCRAFT PRESSURIZED TO 3 PSI, LEAK CHECKED IN BOTH AUTO AND MANUAL MODES, SYSTEM CHECKED OK. 2 L 7 3 4F A3WE 1996030800302 19960308 00302 WP 1996 3 8 9605099952 1 19960304 A 2130 10256852 CONTROLLER DOUG DC9 DC931 3022065 WP COCKPIT PANEL LOOSE WIRE A NWAA G B O2 MASK DEPLOYED EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 01 916RW 9120 1284 47144 LOSS OF CABIN PRESSURIZATION OCCURRED DURING CRUISE FLIGHT AT 33,000 FEET. OXYGEN MASKS WERE DEPLOYED THROUGHOUT CABIN AND DESCENT WAS MADE TO 10,000 FEET. FLIGHT WAS CONTINUED TO DESTINATION AND AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND LOOSE ELECTRICAL CONNECTION ON PRESSURIZATION CONTROLLER. REPLACED CONTROLLER AND REPLACED AMPLIFIER AS A PRECAUTION. OPERATIONAL CHECK NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996030800303 19960308 00303 WP 1996 3 8 9605109983 1 19960303 A 2923 AS19593 PUMP DOUG DC9 DC932 3022066 WP RT AUX HYD SYS MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 983US 480 468 47282 DURING CLIMBOUT, COCKPIT LIGHTS BEGAN FLICKERING AND LEFT AC GENERATOR LOAD METER INTERMITTENTLY PEGGED TO MAXIMUM. RIG HT HYDRAULIC PRESSURE WENT TO 3,000 PSI WITH ENGINE PUMPS AT LOW AND AUXILIARY PUMP SWITCH OFF. AUXILIARY PUMP CIRCUIT BREAKER ON LEFT GENERATOR BUS WAS PULLED AND ALL SYSTEMS RETURNED TO NORMAL. FLIGHT DIVERTED TO MSO AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT AUXILIARY HYDRAULIC PUMP AND CONTROL RELAY R2-15. OPERATIONAL CHECK NORMAL AND AI RCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996030800304 19960308 00304 1996 3 8 9605119152 4 19960304 A 3420 258733511 VERT GYRO DOUG DC9 DC914 3022034 WP NR 2 FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 8911E 45825 DURING CLIMBOUT, FIRST OFFICER'S VERTICAL GYRO FAILED. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED TH E NR 2 VERTICAL GYRO AND CHECKED OK. 2 L 7 2 4F A6WE 1996030800305 19960308 00305 NM 1996 3 8 9605126631 1 19960303 A 5230 SEAL BOEING 747 747251B 1384892 NM CARGO DOOR DAMAGED A NWAA A B UNSCHED LANDING EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 01 631US 23111 DURING CRUISE, PRESSURIZATION AUTO FAIL LIGHT ILLUMINATED ACCOMPANIED BY A LOSS OF PRESSURIZATION. AIRCRAFT DIVERTED TO MNL AND LANDED WITHOUT INCIDENT. REPLACED AIR/GROUND RELAY R229, RIGHT OUTFLOW VALVE ACTUATOR AND AUTO PRESSURE CONTRO LLER. REPAIRED DENT IN FORWARD CARGO DOOR DEPRESSOR SEAL AND OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996030800306 19960308 00306 NE 1996 3 8 9605269867 2 19960229 A 7261 GEARBOX DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE NR 2 ENGINE DAMAGED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 776NC 47786 696743 CLIMBING THROUGH FL190, NR 2 ENGINE OIL PRESSURE AND QUANTITY DROPPED TO ZERO. THE ENGINE WAS SHUTDOWN AND THE FLIGHT R ETURNED TO DTW WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LP5 FITTING AND THREADS PULLED FROM THEIR BOSS ON THE GE ARBOX. THE ENGINE WAS REPLACED WITH A SERVICEABLE UNIT. 2 L 7 2 4F 4 F A6WE E2EA 1996030800307 19960308 00307 NM 1996 3 8 96FDEA00385 1 19960216 A 5315 FLOOR BEAM BOEING 727 727227 1384078 NM BS 360 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 UPPER LOBE CORROSION ON FLOOR BEAM STA 360 TOP CHORD, AFT FLANGE, BOTTOM SIDE LBL 8. INSTALLED REPAIR PER SRM 53-10-2 FIG 3. 2 L 7 3 4F A3WE 1996030800308 19960308 00308 NM 1996 3 8 96FDEA00386 1 19960221 A 5311 FRAME BOEING 727 727227 1384078 NM BS 720 BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 FWD LOWER CARGO COMPT STA 720 FRAME BENT BETWEEN STR 23 TO 24L. INSTALLED DOUBLER PER SRM 53-10-4. 2 L 7 3 4F A3WE 1996030800309 19960308 00309 NM 1996 3 8 96FDEA00387 1 19960223 A 5320 FLANGE BOEING 727 727227 1384078 NM BS 950 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 CORROSION ON O/B FLANGE OF STR 29R AFT SIDE STA 950E. CUT OUT DAMAGED AREA AND INSTALLED STR SPLICE AND SKIN DOUBLER PE R ESO 11782 DATED 2-21-96, AUTHORIZED BY FEDEX EA 7-5310-27736 DATED 2-29-96. 2 L 7 3 4F A3WE 1996030800310 19960308 00310 NM 1996 3 8 96FDEA00388 1 19960226 A 5330 SKIN BOEING 727 727227 1384078 NM FS 683 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 LOWER FWD CARGO COMPT FUSE BELLY SKIN CORRODED AT STA 683 O/B OF STR 28L. CUT OUT DAMAGED SECTION OF SKIN. INSTALLED REPAIR DOUBLER PER SRM 53-30-3 FIG 3A SHEET 3A. 2 L 7 3 4F A3WE 1996030800311 19960308 00311 NM 1996 3 8 96FDEA00389 1 19960227 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 1040-1050 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 CORROSION LT SIDE OF STR 28L STA 1040 TO 1050 IN AFT CARGO. CORROSION REMOVED, DAMAGE BEYOND MM LIMITS. REMOVED DAMAGE D MATERIAL, INSTALLED DOUBLER AND STR REPAIR PER SRM 53-10-3. 2 L 7 3 4F A3WE 1996030800312 19960308 00312 NM 1996 3 8 96FDEA00390 1 19960229 A 5320 ANGLE BOEING 727 727227 1384078 NM FLIGHT DECK CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 FLOOR PLATE BULGING 36 FWD OF FLIGHT DECK ENTRY DOOR AT BL 0. REPLACED CORRODED CHORD ANGLE FROM LBL 6 TO RBL 18 PER SR M 51-40-4. 2 L 7 3 4F A3WE 1996030800313 19960308 00313 NM 1996 3 8 96FDEA00391 1 19960229 A 5320 RIB CHORD BOEING 727 727227 1384078 NM BS 760 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 RT 760 RIB CHORD AT BL 70.5 TOP FWD HOLE IS CRACKED. ENLARGED TOP FWD HOLE TO REMOVE CRACK, HOLE ENLARGED TO .5 INCH DI A. CRACK REMOVED, INSTALLED 7075-T6 FREEZE PLUG PER SRM 51-10-7. INSTALLED SECOND OVERSIZED HI-LOK AT PLUG LOCATIONS P ER ESO 11782. 2 L 7 3 4F A3WE 1996030800314 19960308 00314 NM 1996 3 8 96FDEA00392 1 19960229 A 5330 SKIN BOEING 727 727227 1384078 NM BS 723 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 LOWER FWD CARGO COMPT FUSE SKIN CORRODED STA 723 BETWEEN STR 28 LT AND RT. REMOVED CORROSION, SKIN THICKNESS BEYOND LIM ITS. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-30-3. 2 L 7 3 4F A3WE 1996030800315 19960308 00315 EU 1996 3 8 96FDEA00393 1 19960302 A 5270 SWITCH AIRBUS 310 A310203 EU CARGO DOOR LACK OF LUBE A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 413FE 397 CARGO DOOR OPEN WARNING WITH ASSOCIATED ECAM EVERY 5 SECONDS. CLEANED AND LUBED SWITCHES 14 AND 16WS, CKS OK. 2 L 7 2 4F RT A35EU 1996030800316 19960308 00316 NM 1996 3 8 96FDEA00394 1 19960303 A 5313 STRINGER BOEING 727 72725C 138400H NM FS 1045 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 CABIN UPPER LOBE STRINGER NR 1 CRACKED THROUGH AT FS 1045. CUT OUT DAMAGE AND INSTALLED SPLICE PER SRM 51-10-3. 2 L 7 3 4F A3WE 1996030800317 19960308 00317 NM 1996 3 8 96FDEA00395 1 19960215 A 5315 FLOOR BEAM BOEING 727 727227 1384078 NM BS 344 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 FLOOR BEAM UPPER CHORD LWR SURFACE CORRODED STA 344 LBL 50 TO RBL 10 WL 200. *S/D* INSTALLED FLOOR BEAM REPAIR PER STA NDARD REPAIR DRAWING MANUAL SRM 27-53-007, NR0346. 2 L 7 3 4F A3WE 1996030800318 19960308 00318 NM 1996 3 8 96FDEA00396 1 19960226 A 5320 SKATE ANGLE BOEING 727 72725C 138400H NM NOSE COMPT CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 RT FWD SKATE ANGLE NOSE COMPARTMENT HAS CORROSION ON FWD END. *S/D* REMOVED AND REPLACED RT FWD SKATE ANGLE PER SRM 51 -10-1. 2 L 7 3 4F A3WE 1996030800319 19960308 00319 NM 1996 3 8 96FDEA00397 1 19960229 A 5711 SPAR CHORD BOEING 727 72725C 138400H NM WS 304 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 WS 304 RT WING 3RD STR AFT OF FWD UPPER SPAR CHORD CRACKED. *S/D* REPAIRED STRINGER AT WS 304 RT WING 3RD TOP FRONT SP AR CHORD PER SRM 7-10-4. 2 L 7 3 4F A3WE 1996030800320 19960308 00320 NM 1996 3 8 96UAL900157 1 19960304 A 3350 LIGHT BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 610UA 21871 EXIT EMERGENCY LIGHT OVER DOOR 2R IS INOP. REPLACED LAMP, OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 1996030800321 19960308 00321 NM 1996 3 8 96UAL900158 1 19960304 A 3213 69394654 GLAND NUT BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE LT MLG FRACTURED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 9069U 19950 ON GEAR RETRACTION LEFT MAIN GEAR RED LIGHT STAYED ON WITH GEAR HANDLE IN THE UP POSITION. RECYCLED GEAR AND GOT 3 GREE N LIGHTS IN DOWN POSITION. RED LIGHT REMAINED ON WITH GEAR HANDLE IN THE UP POSITION, HAD HEAVY DRAG IN CRUISE. *S/D* LEFT MAIN GEAR GLAND NUT WAS FOUND FRACTURED AT THE LUBE FITTING AND OFFSET IN THE OUTER CYLINDER. GLAND NUT WAS REPLA CED AND SENT TO LAB FOR ANALYSIS. 2 L 7 2 4F 4 F A16WE E2EA 1996030800322 19960308 00322 WP 1996 3 8 96UAL900159 1 19960304 A 2530 OVENS DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL GALLEY DIRTY A UALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 1811U 46610 POSSIBLE SMOKE IN GALLEY ON PUSH BACK, RETURNED TO BLOCKS. OVEN VENT SCREENS WERE PLUGGED WITH DIRT AND GRIM. CLEANED OVEN SCREENS. 2 L 7 3 4F 4 F A22WE E23EA 1996030800323 19960308 00323 NM 1996 3 8 96UAL900160 1 19960304 A 3610 PRSOV BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT ENGINE MALFUNCTIONED A UALA O OTHER E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CR CRUISE 1 WP 29 521UA 24891 726678 DURING FLIGHT, THE RIGHT ENGINE COMPRESSOR STALLED AND RECOVERED WITHOUT EXCEEDING LIMITS. THIRTY MINUTES LATER COMPRE SSOR STALL REOCCURRED, EGT STARTED TO RISE AND THROTTLE WAS PULLED TO IDLE. ENGINE STABILIZED AND POWER WAS RESTORED. E NGINE INSPECTED AND BORESCOPED AT MCO, NOTHING FOUND. SUSPECT 14TH STAGE STABILITY BLEED VALVE MALFUNCTION. REPLACED 1 4TH STAGE BLEED CONVERTER VALVE, REVERSE FLOW AIR VALVE, HIGH STAGE PILOT CONTROL, HIGH STAGE VALVE, PRSOV AND PRSOV REG ULATOR. NO REOCCURANCES OF PROBLEM. 2 L 7 2 4F 4 F RT A2NM E17NE 1996030800325 19960308 00325 NM 1996 3 8 96UPS20561 1 19960226 A 5320 65176923 FORGING BOEING 727 72725C 138400H NM BS 940 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 931UP 19858 DURING 'C' CHECK MAINTENANCE REPORTED, BS 940 FORGING CRACKED AT STRINGER 18A, WL 208. REPLACED FORGING IAW EO B727-531 0-4501C. 2 L 7 3 4F A3WE 1996030800327 19960308 00327 WP 1996 3 8 ABXA9600232 1 19960301 A 5610 27010933 HINGE PIN DOUG DC8 DC861 3021952 WP COCKPIT MISALIGNED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 FIRST OFFICER'S SLIDING WINDOW WILL NOT OPEN. FOUND FIRST OFFICER'S SLIDING WINDOW AFT HINGE PIN MISALIGNED AT LINKAGE. REINSTALLED HINGE PIN IN PROPER POSITION ON CLEVIS. OPS CHECK OF FIRST OFFICER'S SLIDING WINDOW WAS GOOD. 2 L 7 4 4F 4A25 1996030800328 19960308 00328 WP 1996 3 8 ARWA9603002 1 19960305 A 5730 56113601295754 SKIN DOUG DC8 DC862 3021970 WP WS 624-693 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 810BN 45905 LT WING UPPER SURFACE BETWEEN WING STA XRS 624.000 AND XRS 693.000 CENTER SKIN AREA HAS CORROSION. BLENDED OUT CORROSIO N, INSTALLED DOUBLER IAW DAC FAX 96-02-29-010 AND 96-02-06-004. 2 L 7 4 4F 4A25 1996030800329 19960308 00329 WP 1996 3 8 ARWA9603003 1 19960305 A 5730 56113601301375 PANEL DOUG DC8 DC862 3021970 WP WS 695-727 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 810BN 45905 RT WING UPPER SURFACE BETWEEN WING STA XRS 659.000 AND XRS 727.000 HAS CORROSION AROUND FASTENERS' HEADS. CUT OUT DAMAG ED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW DAC 96-02-26-003 AND 96-03-01-002. 2 L 7 4 4F 4A25 1996030800330 19960308 00330 WP 1996 3 8 ARWA9603004 1 19960305 A 5730 57695892 SKIN DOUG DC8 DC862 3021970 WP WS 472.75 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 810BN 45905 CORROSION ON RT WING LOWER SURFACE AT WING STA XFS 472.750. REMOVED CORRODED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW DER JOSSAIR, CO EO ARW 960051-0024. 2 L 7 4 4F 4A25 1996030800331 19960308 00331 WP 1996 3 8 ARWA9603005 1 19960305 A 5542 570125141 SKIN DOUG DC8 DC862 3021970 WP RUDDER CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 810BN 45905 RUDDER BOTTOM SURFACE, INSPECTION PANEL CUT OUT SKIN IS CRACKED. REMOVED AND REPLACED CRACKED SECTION IAW DER JOSSAIR, CO DRAWING ARW 950163-0014. 2 L 7 4 4F 4A25 1996030800332 19960308 00332 EU 1996 3 8 COMA9630049 1 19960302 A 6120 8542M2 COMPUTER SAAB SF340 SF340A 7850100 EU AUTO COARSEN SYS FAILED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 356CA 8484 220 340A034 AUTO COARSEN FAIL WARNING DURING TAKEOFF. REPLACED THE AUTO COARSEN COMPUTER. 2 L 7 2 4T RT A52EU 1996030800333 19960308 00333 EU 1996 3 8 COMA9630050 1 19960303 A 2910 3268 DUMP VALVE SAAB SF340 SF340A 7850100 EU NLG LEAKING A COMA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 347CA 340A028 HYDRAULIC SYSTEM PUMP CYCLES EVERY 90 SECONDS. REPLACED MAIN ACCUMULATOR DUMP VALVES. 2 L 7 2 4T RT A52EU 1996030800334 19960308 00334 NM 1996 3 8 DL72E960490 1 19960229 A 3240 BRAKES BOEING 727 727247 138408F NM LEFT REQD SERVICE A DALA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 2826W 21331 AFTER INITIAL BREAK APPLICATION ON RUNWAY, BRAKES WERE NORMAL. BUT ON SUBSEQUENT APPLICATION TO TURN OFF RUNWAY LEFT BR AKES WERE SOFT AND INEFFECTIVE. BLED NR 3 AND NR 4 BRAKES, ANTI-SKID TEST WAS NORMAL, RESET DEBOOST ON LEFT GEAR AND OP ERATION NORMAL. 2 L 7 3 4F A3WE 1996030800335 19960308 00335 NM 1996 3 8 DL72K960468 1 19960229 A 2782 269002911 ACTUATOR BOEING 727 727232 1384082 NM NR 4 LE SLAT CRACKED A DALA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 27 479DA 20756 NR 4 L/E SLAT ACTUATOR CRACKED IN FLT CAUSING A-SYSTEM HYD FLUID LOSS. REPLACED ACTUATOR. 2 L 7 3 4F A3WE 1996030800336 19960308 00336 NM 1996 3 8 DL72S960463 1 19960129 A 5754 651622296 RIB BOEING 727 727232 1384082 NM NR 6 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 419DA 21272 DURING INSPECTION, NR 6 L/E SLAT WAS FOUND WITH NR 1 L/E SUPPORT RIB CRACKED. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1996030800337 19960308 00337 NM 1996 3 8 DL72S960464 1 19960229 A 5330 651842011 SKIN BOEING 727 727232 1384082 NM FS 312 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 468DA 20745 DURING INSPECTION, THE SKIN AT STA 312 AND S-22R WAS FOUND TO HAVE TWO CRACKS EMANATING FROM FASTENERS. ALSO, A PREVIOU S REPAIR WAS INSTALLED JUST BELOW THE TWO CRACKS. IN ACCORDANCE WITH B727 SRM 53-30-3 FIG 3, BOTH DAMAGE LOCATIONS WERE INCORPORATED UNDER ONE REPAIR. 2 L 7 3 4F A3WE 1996030800338 19960308 00338 NM 1996 3 8 DL72S960465 1 19960229 A 5330 65545889 SKIN BOEING 727 727232 1384082 NM FS 700 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 468DA 20745 DURING INSPECTION, THE FUSELAGE SKIN WAS FOUND CORRODED ALONG THE S-26L LAP JOINT AT STA 700. REMOVAL OF THE CORROSION RESULTED IN A 3 INCH WIDE BY 10 INCH LONG CUT OUT IN THE OVERLAPPING SKIN ONLY. A PREVIOUS REPAIR DOUBLER IS LOCATED WI THIN 2 INCHES OF THIS REPAIR. IN ACCORDANCE WITH B727 SRM 53-30-3 FIG 14, THE SKIN WAS REPAIRED. 2 L 7 3 4F A3WE 1996030800339 19960308 00339 NM 1996 3 8 DL72S960470 1 19960229 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 2 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 421DA 21274 A .25 INCH CRACK AT NR 2 SLAT COVE SKIN ANGLE BELOW I/B TRACK. FOUND DURING C-1 LTR CK TPAMM AND REPAIRED PER MM 57-54- 0. 2 L 7 3 4F A3WE 1996030800340 19960308 00340 NM 1996 3 8 DL72S960475 1 19960109 A 5754 651622296 RIB BOEING 727 727232 1384082 NM NR 6 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 419DA 21272 UPON ROUTINE INSPECTION, A CRACK WAS FOUND ON 2ND RIB FROM I/B END. REPAIRED AS PER SRM 57-50-3 FIG 9, FOR NR L/E SLAT. 2 L 7 3 4F A3WE 1996030800341 19960308 00341 NM 1996 3 8 DL72S960478 1 19960301 A 3830 CHECK VALVE BOEING 727 727225 1384077 NM FWD FILL LINE DIRTY A DALA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SO 27 8875Z 21293 AFTER TAKEOFF, NOTICED BLUE FLUID STREAKING WINDOWS ON RIGHT SIDE OF AIRCRAFT. RETURNED TO LAX WHERE MECHANICS PRESSURI ZED A/C AND FOUND FLUID LEAKING FROM FWD LAV FILL LINE. CLEANED FILL LINE CHECK VALVE AND SYS CHECKS NORMAL. 2 L 7 3 4F A3WE 1996030800342 19960308 00342 NM 1996 3 8 DL72S960480 1 19960101 A 7797 WIRE HARNESS BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE BURNED A DALA E ENGINE SHUTDOWN H ELECT. POWER LOSS-50 PC CL CLIMB 1 SO 27 408DA 21152 700703 A/C LOST N-1 INDICATION, FUEL HEAT LIGHT AND START VALVE LIGHT 'ON'. F/F STUCK ON 4800 PPH, ENGINE SHUTDOWN. FOUND WIR E HARNESS MELTED IN FWD PYLON SPLICED IN NEW ENG WIRING AT PLUGS D374J, D356J, D350J, D386P AND D362J, PERFORMED CK OUT PER PFHB AND CKS GOOD. 2 L 7 3 4F 4 F A3WE E2EA 1996030800343 19960308 00343 NM 1996 3 8 DL72S960491 1 19960303 A 3397 WIRE BOEING 727 727232 1384082 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 401DA 21145 ON PREFLIGHT, EMERGENCY TRACK LIGHTING ON RT SIDE AT SEAT ROW 12 TO FIRST CLASS DIVIDER INOP. REPAIRED BROKEN WIRE AT S EAT ROW 12. 2 L 7 3 4F A3WE 1996030800344 19960308 00344 NM 1996 3 8 DL72W960469 1 19960229 A 5754 ANGLE BOEING 727 727247 138408F NM NR 2 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 291WA 22109 NR 2 SLAT COVE SKIN ANGLE AT TAI DUCT CRACKED .5 INCH. FOUND DURING A-2 LTR CK, REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1996030800345 19960308 00345 NM 1996 3 8 DL73S960472 1 19960229 A 3350 OL3071BPEGPL BULB BOEING 737 737232 1384475 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 320DL 23092 ON CHECK, FOUND FOUR EMERGENCY TRACK LIGHTS INOP. REPLACED BULBS AND OPERATION NORMAL. 2 L 7 2 4F RT A16WE 1996030800346 19960308 00346 NM 1996 3 8 DL757960457 1 19960229 A 3350 LENSE BOEING 757 757232 1384965 NM CABIN CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 607DL 22814 EMERGENCY LIGHT/EXIT SIGN AT R-1 DOOR FOUND WITH CRACKED LENS. REPLACED EXIT SIGN LIGHT ASSEMBLY AND LENS, OPERATION NO RMAL. 2 L 7 2 4F RT A2NM 1996030800347 19960308 00347 NM 1996 3 8 DL757960458 1 19960229 A 3350 BATTERY PACK 2G131A BOEING 757 757232 1384965 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 607DL 32205 22814 ON LAYOVER, FOUND AFT 3 LT AISLE EMERGENCY LIGHT INOP. REPLACED M737 BATTERY PACK EMERGENCY LIGHTS AND CK NORMAL. 2 L 7 2 4F RT A2NM 1996030800348 19960308 00348 NM 1996 3 8 DL757960462 1 19960229 A 5754 114N3002120A TE WEDGE BOEING 757 757232 1384965 NM NR 6 TE FLAP DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 658DL 24420 DURING INSPECTION, NR 6 SLAT T/E WEDGE WAS FOUND DENTED. REPLACED WEDGE PER SRM 57-43-02. 2 L 7 2 4F RT A2NM 1996030800349 19960308 00349 NM 1996 3 8 DL757960476 1 19960301 A 5754 114N4004145 SKIN BOEING 757 757232 1384965 NM NR 3 TE SLAT GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 650DL 24390 DURING ROUTINE INSPECTIONS OF THE NR 3 SLAT, THE TRAILING EDGE WEDGE WAS FOUND DAMAGED. THE DAMAGE WAS A .25 INCH PUNCT URE THROUGH BOTH UPPER AND LOWER SKINS OF THE NR 3 SLAT TRAILING EDGE WEDGE. IN ACCORDANCE WITH B757 SRM 51-70-10, THE DAMAGE WAS REPAIRED PER B757 SRM 57-43-02 FIG 201. 2 L 7 2 4F RT A2NM 1996030800350 19960308 00350 NM 1996 3 8 DL757960481 1 19960301 A 2560 654N001041 SLIDE BOTTLE BOEING 757 757232 1384965 NM LT SLIDE FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 680DA 26956 LEFT OVERWING SLIDE BOTTLE WOULD NOT TEST. DISARMED/REARMED LEFT OFFWING ESCAPE SYSTEM PER MM 25-65-00. VISUALLY VERIF IED ROUND CRANK HANDLE IN LOCKING POSITION AND VENT HANDLE IN THE OPERATE POSITION. ALSO, VERIFIED PRESSURE BOTTLE SAFE TY PIN AND CAPS REMOVED. PRESSURE AND SQUIB TEST OPERATION NORMAL. 2 L 7 2 4F RT A2NM 1996030800351 19960308 00351 NM 1996 3 8 DL757960494 1 19960302 A 5210 MECHANISM BOEING 757 757232 1384965 NM R 4 DOOR OUT OF ADJUST A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 619DL 22909 ON DEPARTURE, R-4 DOOR SLIDE WOULD NOT ARM AND FERRIED TO ATL. ADJUSTED DOOR RIGGING PER MM 52-11-0 AND OPERATION NORMA L. 2 L 7 2 4F RT A2NM 1996030800352 19960308 00352 NM 1996 3 8 DL76S960484 1 19960303 A 2560 POWER SUPPLY S283T0143 BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 116DL 24732 23275 NO SQUIB TEST ON EMERGENCY ESCAPE SLIDE/SPOILER. REPLACED M391 POWER SUPPLY AND BATTERY PACK OPERATION NORMAL. 2 L 7 2 4F RT A1NM 1996030800353 19960308 00353 NM 1996 3 8 DL76S960485 1 19960303 A 2560 BATTERY PACK 20131A BOEING 767 767332 1382001 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 116DL 25737 23275 NO SQUIB TEST ON EMERGENCY ESCAPE SLIDE/SPOILER. BATTERY PACK LOW VOLTS FROM MODULE 961, REPLACED SAME. 2 L 7 2 4F RT A1NM 1996030800355 19960308 00355 NE 1996 3 8 DLL10960495 2 19960302 A 7261 727706605 SCAVENGE PUMP LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B02 54555 NE NR 2 ENGINE FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 713DA 193C1089 DURING CRUISE HAD STRONG ENGINE EXHAUST TYPE ODOR. PERFORMED INSPECTION OF ENGINES, FOUND NR 2 ENGINE OIL SCAVENGE PUMP FAULTY. REPLACED PUMP AND PERFORMED DUCT BURNOUT. 2 L 7 3 4F 4 F A23WE E12EU 1996030800356 19960308 00356 WP 1996 3 8 DLL16960482 1 19960303 A 3350 269002911 POWER SUPPLY 5165741 LKHEED 1011 10113853 5265020 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 759DA 193Y1176 TWO EMERGENCY LIGHT POWER SUPPLIES HAVE CHARGE LIGHT INOP. REPLACED POWER SUPPLIES. 2 L 7 3 4F A23WE 1996030800357 19960308 00357 NM 1996 3 8 DLM88960479 1 19960301 A 3020 DE-ICE FLUID DOUG MD88 MD88 3023688 NM AIR FOIL DE-ICE OVER FILLED A DALA K NONE W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 946DL 49819 LIGHT SMOKE IN CABIN WHEN AIRFOIL DE-ICE SELECTED. FOUND RES OVER FILLED BOTTLES FULL, HYD FLUID LEAKING INTO KEEL BEAM AREA THEN ON SKIN INTO APU INTAKE. CLEANED BOTTLES, RAN AC SYSTEM AND NO SMOKE NOTED. 2 L 7 2 4F RT A6WE 1996030800358 19960308 00358 NM 1996 3 8 DLM88960496 1 19960301 A 3220 STRUT DOUG MD88 MD88 3023688 NM NLG REQD SERVICE A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 911DL 49542 AFTER TAKEOFF, NOSE GEAR UNSAFE LIGHT ILLUMINATED, AIR NOISE FROM NOSE GEAR AREA. DISASSEMBLED NOSE STRUT, FOUND THREE PINTS OF WATER AND ICE INSIDE STRUT. CLEANED STRUT, INSTALLED NEW SEALS, SERVICED PER MM AND OPERATION NORMAL. 2 L 7 2 4F RT A6WE 1996030800359 19960308 00359 WP 1996 3 8 MWEA96051 1 19960305 A 2560 5917689103 EVAC SLIDE COVER DOUG DC9 DC932 3022066 WP FWD ENTRY FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 401ME 47133 CREW REPORTS, FWD ENTRY DOOR EVACUATION SLIDE COVER FELL OFF. MAINT REINSTALLED EVACUATION SLIDE COVER. 2 L 7 2 4F A6WE 1996030800360 19960308 00360 WP 1996 3 8 MWEA96052 1 19960305 A 5542 SKIN DOUG DC9 DC932 3022066 WP RUDDER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 DURING INSPECTION, FOUND CRACK IN RUDDER SKIN .5 INCH LENGTH ON LT SIDE 4 AFT OF CENTERLINE STA ZR 26.043. MAINTENANCE INSTALLED DOUBLER REPAIR IAW SRM 55-01 FIG 2. RECALCULATED BALANCE AND RETURNED A/C TO SERVICE. 2 L 7 2 4F A6WE 1996030800361 19960308 00361 EU 1996 3 8 QXEA9600094 1 19960304 A 2613 FDBA562461SNK CONNECTOR FOKKER FOKKER F28 F28MK1000 4990808 EU NR 2 ENG DIRTY A QXEA A E UNSCHED LANDING ENGINE SHUTDOWN J Y WARNING INDICATION ENGINE STOPPAGE CL CLIMB 1 NM 09 468US 11095 NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED IN FLIGHT WITH ASSOCIATED MASTER WARNING LIGHT. NR 2 ENGINE SHUTDOWN PER CHECKLI ST PROCEDURES AND WARNING LIGHT REMAINED ON AFTER ENGINE SHUTDOWN. AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT FURTHE R PROBLEM. CANNON PLUG NR 4 IN STUBWING WAS FOUND OIL SOAKED. CANNON PLUG CLEANED AND ENGINE OVERHEAT INDICATION OPS C HECKED GOOD ON GROUND RUN. 2 L 7 2 4F RT A20EU 1996030800362 19960308 00362 NM 1996 3 8 SCNA96027 1 19960229 A 2612 894120 ELEMENT BOEING 727 7272A1 138407F NM NR 1 ENGINE FAILED A SCNA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 GL 15 287SC 21345 DURING CRUISE, THE NUMBER ONE FIRE WARNING LIGHT ILLUMINATED AND THE AURAL WARNING SOUNDED. SHUTDOWN ENGINE AND BLEW ON E BOTTLE AND THE FIRE INDICATION EXTINGUISHED. REMOVED AND REPLACED THE NUMBER 1 FIRE DETECTION ELEMENT PER MM 26-00-00 AND THE SYSTEM TESTED GOOD. REMOVED AND REPLACED BLOWN FIRE BOTTLE, RAN NUMBER 1 ENGINE AND RECEIVED NO FIRE INDICATIO NS. 2 L 7 3 4F A3WE 1996030800363 19960308 00363 NM 1996 3 8 SCNA96028 1 19960228 A 3350 S106 BATTERIES BOEING 727 727227 1384078 NM AFT AIRSTAIR DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 275AF 22092 THE AFT AIRSTAIR EMERGENCY LIGHT WAS FOUND TO BE DIM. REPLACED BATTERIES IN LIGHT AND UNIT TESTED GOOD. 2 L 7 3 4F A3WE 1996030800364 19960308 00364 NM 1996 3 8 SWAA960123 1 19960226 A 5320 WEB BOEING 737 7372H4 138448C NM BS 182 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED D-CHECK, FOUND CRACKED VERTICAL STIFFENER WEB AT BS 182 LBL 18 WL 184. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996030800365 19960308 00365 NM 1996 3 8 SWAA960124 1 19960226 A 5312 BULKHEAD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED D-CHECK, FOUND BS 178 PRESSURE BULKHEAD CRACKED 2 PLACES, ONE AT LBL 10 AND AT LBL 11, WL 219. REPAIRE D PER BOEING SRM. 2 L 7 2 4F A16WE 1996030800366 19960308 00366 NM 1996 3 8 SWAA960125 1 19960226 A 5312 BULKHEAD BOEING 737 7372H4 138448C NM APU COMPT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED D-CHECK, FOUND APU COMPARTMENT UPPER BULKHEAD CRACKED AT LIGHTENING HOLE BETWEEN BS 1136 AND 1121 RIGHT SIDE AND BETWEEN BS 1121 AND 1104 LEFT SIDE. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996030800367 19960308 00367 NM 1996 3 8 SWAA960126 1 19960226 A 5312 BULKHEAD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED D-CHECK, FOUND BULKHEAD SKIN CRACKED AT BS 178 WL 235 APPROX LBL 13. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996030800368 19960308 00368 NM 1996 3 8 SWAA960127 1 19960226 A 5320 INTERCOSTAL BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL CRACKED AT BS 178 WL 195 LBL 24. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996030800369 19960308 00369 NM 1996 3 8 SWAA960128 1 19960226 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED D-CHECK, FOUND SUPPORT ANGLE CRACK AT BS 178 WL 194 LBL 23. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996030800370 19960308 00370 NM 1996 3 8 SWAA960129 1 19960226 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 495 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED D-CHECK, FOUND STRINGERS CRACKED AT BS 495, S23 AND 22R AND AT BS 1012, S7L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996030800371 19960308 00371 NM 1996 3 8 SWAA960130 1 19960226 A 5320 CLIPS BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 747 S22R AT BS 727A S19R AND AT BS 520 S19L. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996030800372 19960308 00372 NM 1996 3 8 SWAA960131 1 19960226 A 5312 BULKHEAD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED D-CHECK, FOUND BULKHEAD BS 178 CRACK ON LEFT SIDE AT WL 194 IN RADIUS OF SIDE CHORD. REPAIRED PER SWA ACO 96-0017. 2 L 7 2 4F A16WE 1996030800373 19960308 00373 NM 1996 3 8 SWAA960132 1 19960226 A 5320 STRAP BOEING 737 7372H4 138448C NM BS 492 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED D-CHECK, FOUND DOOR FRAME STRAP CRACKED AT BS 492 RBL 54 WL 180. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996030800374 19960308 00374 NM 1996 3 8 SWAA960133 1 19960226 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 179 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AND FAIL-SAFE CHORD CRACKED AT BS 179 LBL 55. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996030800375 19960308 00375 NM 1996 3 8 SWAA960134 1 19960226 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 440 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440 RBL 37 WL 160. REPAIRED PER TRAMCO EWO 96-0041. 2 L 7 2 4F A16WE 1996030800376 19960308 00376 NM 1996 3 8 SWAA960135 1 19960226 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 440 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED 2 PLACES AT BS 440 LBL 55 AND 57 WL 177 AND 175. REPAIRED PER BO EING SRM. 2 L 7 2 4F A16WE 1996030800377 19960308 00377 NM 1996 3 8 SWAA960136 1 19960226 A 5313 STRINGERS BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED D-CHECK, FOUND STRINGERS CORRODED BS 907 LBL 21 WL 168, BS 903 RBL 21 WL 168 AND BS 908 TO 906 RBL 19 W L 165. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996030800378 19960308 00378 EU 1996 3 8 WWMA9600025 1 19960301 A 2120 AIR DIST SAAB SF340 340B 7860101 EU COCKPIT ODOR A WWMA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 15 261AE 340B261 CREW REPORTED, TOXIC FUMES IN THE COCKPIT DURING DECENT, AN EMERGENCY WAS DECLARED. THEY REPORTED THERE WERE NO WARNING S OR ABNORMAL AIRCRAFT INDICATIONS. MAINTENANCE RAN THE AIRCRAFT WITH BLEEDS, AVIONICS AND ALL SYSTEMS ON IN DIFFERENT CONFIGURATIONS AND COULD NOT DUPLICATE THE PROBLEM. THE AVIONICS RACK FAN FILTER WAS CHANGED AND THE AIRCRAFT WAS RELEA SED FOR SERVICE. 2 L 7 2 4T RT A52EU 1996030800379 19960308 00379 EU 1996 3 8 WWMA9600026 1 19960304 A 3610 1379731L407 DUCT BAG JETSTM JETSTM3201 1500217 EU LT ACM RUPTURED A WWMA O OTHER J WARNING INDICATION CR CRUISE 1 WP 15 952AE 952 CREW REPORTED, IN FLIGHT BOTH BLEEDS FAILED CAUSING THE CABIN TO DEPRESSURIZE. UPON INVESTIGATION MAINTENANCE FOUND THE DUCT CONNECTING THE WATER SOCK TO THE ACM RUPTURED AND THE SAME DUCT ON THE RIGHT SIDE PARTICALLY DISCONNECTED, CAUSING A DECREASE IN AIR FLOW. THE LEFT DUCT WAS REPLACED AND THE RIGHT DUCT WAS RECONNECTED. THE AIRCRAFT WAS RETURNED TO S ERVICE WITHOUT FURTHER PROBLEMS. 2 L 7 2 4T RT A56EU 1996030800380 19960308 00380 NM 1996 3 8 96ZZZM250 1 19960202 A 2781 H1010261 SWITCH BOEING 727 72751C 1384015 NM NR 4 LE FLAP FAILED A RYNA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 07 413EX 19206 AFTER TAKEOFF DURING CLIMB, AS THE FLAPS WERE RETRACTED THE NR 4 LEADING EDGE FLAP INTRANSIT LIGHTS REMAINED ILLUMINATED . EXECUTED AIR TURN BACK TO IND. AIRCRAFT WAS LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE NR 4 LEADING EDGE FLA P POSITION SWITCH PER MM 27-80-00. OPS CHECK GOOD. (M) 2 L 7 3 4F A3WE 1996030800381 19960308 00381 NM 1996 3 8 96ZZZM251 1 19960202 A 2781 H1010261 SWITCH EATON BOEING 727 727212 138407G NM NR 4 LE FLAP FAILED A UHVA O OTHER N FALSE WARNING CL CLIMB 1 SO 17 293AS 0576 21348 FKYC NR 9170 - KFLL-KMIA - AFTER TAKEOFF ON FLAP RETRACTION NR 4 KRUEGER FLAP INDICATION REMAINED AMBER. CYCLED FLAPS, NO HELP. RETURNED AIRCRAFT TO DFLL. MAINTENANCE REPLACED NR 4 LEADING EDGE FLAP POSITION SWITCH PER MAINTENANCE MANUAL CHAPTER 27. CYCLED LEADING EDGE FLAPS SEVERAL TIMES, OPS CHECKS GOOD. RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1996030800382 19960308 00382 NM 1996 3 8 96ZZZM252 1 19960129 A 2913 371380 HYDRAULIC PUMP VICKERS BOEING 727 727225 1384077 NM NR 1 ENG MALFUNCTIONED A MYWA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SO 19 803MA MX346380 22434 IN FLIGHT FROM PUNTA CANA, THE CREW NOTICED A SLIGHT VIBRATION AND ERRATIC SYSTEM 'A' PRESSURE FROM NR 1 ENGINE. TURNED OFF NR 1 'A' SYSTEM PUMP. VIBRATION AND ERRATIC PRESSURE CEASED. FLIGHT WENT TO MIAMI FOR REPAIR. REPLACED NR 1 ENGI NE HYDRAULIC PUMP PER MM REFERENCE. OPS CHECKED AND LEAK CHECKED OK. FLIGHT DIVERTED TO MIAMI FOR REPAIR BEFORE CONTIN UING TO NAS AS SCHEDULED. 2 L 7 3 4F A3WE 1996030800384 19960308 00384 EU 1996 3 8 96ZZZM254 1 19960125 A 2760 NAS16125 O-RING AIRBUS 320 A320231 3930325 EU NR 2 SPOILER EXTRUDED A AWXA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 WP 28 636AW 098 FLT NR 860 - PHX/SAN - EMERGENCY LANDING AT SAN, YELLOW HYDRAULIC SYSTEM LEAK AND ALL FLUID LOST ON APPROACH. HYDRAULIC LEAK IN WHEEL WELL AREA. FOUND UNION ON AUTO BRAKE MODULE LOOSE. SECURED AND OPS CHECK NORMAL. ALSO, FOUND O-RING EX TRUDED FROM NR 2 SPOILER ACTUATOR SWIVEL. REPLACED O-RING. LEAK AND OPS CHECK NORMAL. REFERENCE AWXA960033. 2 L 7 2 4F RT A28NM 1996030800385 19960308 00385 NM 1996 3 8 96ZZZM255 1 19960130 A 7711 AN6289D4 PT7 JAM NUT BOEING 737 737277 1384570 NM PWA JT8 JT8D15 52051 NE NR 2 ENG LOOSE A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 181AW 22648 FLT NR 282 - MDW-CMH - ABORTED TAKEOFF, NR 2 EPR INDICATION WAS LOW AND FLUCTUATING. MAINTENANCE INSPECTION AND FOUND T HE P2 TEST CAP AT EPR TRANSMITTER LOOSE AND THE JAM NUT AT PT7 TEE FITTING TO TRANMITTER LOOSE, RESECURED. RAN ENGINES TO TAKEOFF POWER. EPR MADE ALL PARAMETERS PER MM 71-11-01 AND 71-09-236. REFERENCE AWXA960035. 2 L 7 2 4F 4 F RT A16WE E2EA 1996030800386 19960308 00386 NM 1996 3 8 96ZZZM256 1 19960124 A 2731 65C2577313 MOUNT FITTING BOEING 737 7373G7 1384595 NM RT ELEVATOR WORN A AWXA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 WP 28 305AW 24012 LAS-ABQ - FLT NR 720 - AIRCRAFT DIVERETED TO PHOENIX FOR FLIGHT CONTROL VIBRATION. CREW REPORTED VIBRATION FELT THROUGH OUT AIRCRAFT. MORE NOTICEABLE IN THE REAR. DID NOT FEEL VIBRATION IN POWER LEVERS BUT FELT IN YOKE. VIBRATION FREQUEN CY INCREASED WITH AIRSPEED AND FELT IN ALL PHASES OF FLIGHT. REMOVED AND REPLACED RIGHT ELEVATOR TAB INBOARD BUSHING AN D MOUNT FITTING FOR WEAR. REFERENCE AWXA960028. 2 L 7 2 4F RT A16WE 1996030800387 19960308 00387 EU 1996 3 8 96ZZZM257 1 19960202 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 421MQ 2983 014 CMI - EMERGENCY LIGHTS FOR BATTERY PACK POSITION 10WL INOPERATIVE AND EMERGENCY LIGHTS AT POSITION 3WL WILL NOT GO OUT. RAI'D BATTERY PACKS AT 10WL AND 3WL. AIRCRAFT WAS RETURNED TO SERVICE. REFERENCE SIMA960332. 2 H 7 2 4T RT A53EU 1996030800389 19960308 00389 NM 1996 3 8 96ZZZM259 1 19960202 A 2910 65178229 HYD MODULE BOEING 737 7372P6 NM NLG WW LEAKING A ZZDA A UNSCHED LANDING K FLUID LOSS TO TAKEOFF 1 SO 15 2FOR 21355 AFTER TAKEOFF FROM OMA, LANDING GEARS WOULD NOT RETRACT RESULTING IN AN AIR TURN BACK. FOUND 'B' HYD SYSTEM MODULE UNIT (HOUSING) FAILED AT THE NR 5 PUMP PRESSURE SUPPLY PORT. REMOVED AND REPLACED MODULE PER MM 29-12-31. OPS AND LEAK CHE CK GOOD. ALSO, FOUND NR 2 ENGINE DRIVEN HYD PUMP LEAKING. REMOVED AND REPLACED PUMP PER MM 29-12-00. REMOVED AND REPL ACED NR 1 ENGINE DRIVER HYD PUMP FOR PRECAUTIONARY MEASURE. OPS AND LEAK GOOD. 2 L 7 2 4F RT A16WE 1996030800390 19960308 00390 WP 1996 3 8 96ZZZM260 1 19960206 A 3246 BEAD SEAT 95608597 DOUG DC9 DC931 3022065 WP NR 4 WHEEL CRACKED A A4JA K NONE O OTHER IN INSP/MAINT 1 SO 15 8924E 45839 DURING SHOP VISIT, DISCOVERED THAT NR 4 MAIN WHEEL ASSY BEAD SEAT AREA WAS CRACKED. SCRAPPED THE WHEEL HALF. 2 L 7 2 4F A6WE 1996030800391 19960308 00391 WP 1996 3 8 96ZZZM261 1 19960206 A 3246 GSY189C48 BOLT 9560892 DOUG DC9 DC931 3022065 WP NR 2 MLG WHEEL BROKEN A A4JA K NONE O OTHER IN INSP/MAINT 1 SO 15 8924E 45839 FOUND NR 2 MAIN WHEEL ASSY WITH A BROKEN THROUGH BOLT. REPLACED NR 2 WHEEL ASSY. 2 L 7 2 4F A6WE 1996030800392 19960308 00392 CE 1996 3 8 96ZZZM262 1 19960125 A 5210 SEAL BEECH 1900 1900C 1154161 CE PAX DOOR OUT OF POSITION A AMWA A B UNSCHED LANDING EMER. DESCENT J WARNING INDICATION CL CLIMB 1 CE 07 134YV UC134 FLT NR 5637 - FORWARD CABIN DOOR OPEN LIGHT CAME ON DURING CLIMB-OUT. LIGHT WENT OUT WHEN PRESSURE WENT BELOW 1 PSI. M AINTENANCE FOUND DOOR SEAL OUT OF TRACK, REINSTALLED SEAL. OPS CHECKED NORMAL. (M) 2 L 7 2 4T RT A24CE 1996030800394 19960308 00394 NM 1996 3 8 96ZZZM264 1 19960118 A 7931 APS3D10001000A TRANSDUCER DORNER DO32 DO328100 2996000 NM LT ENG GEAR BOX FAILED A EQGA E ENGINE SHUTDOWN J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SW 19 340LS 565 45664303 3040 AIRCRAFT DEPARTED RIL, FLIGHT NR 100, EN ROUTE TO DFW WHEN THE LEFT ENGINE OIL PRESSURE STARTED FLUCTUATING EXCESSIVELY. THE PILOT SHUTDOWN THE LEFT ENGINE AND RETURNED TO RIL WITHOUT FURTHER INCIDENT. UPON TROUBLESHOOTING, FOUND THE LEFT GEARBOX PRESSURE TRANSDUCER WAS BAD. REPLACED TRANSDUCER, GROUND RAN, ALL SYSTEMS CHECKED NORMAL. AIRCRAFT WAS RETURN ED TO SERVICE. (M) 2 H 7 2 4T RT A45NM 1996030800398 19960308 00398 NM 1996 3 8 ASAA9610011 1 19960124 A 3350 8821004 BATTERY PACK BOEING 737 737210C 1384459 NM PALLET 3-8 DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE ON PALLET 3-8. REPLACED BA TTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1996030800399 19960308 00399 NM 1996 3 8 ASAA9610012 1 19960128 A 3350 8821004 BATTERY BOEING 737 737210C 1384459 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 744AS 21822 JNU - DURING MAINTENANCE CHECK, FOUND ONE SEAT PALLET TRACK LIGHTS INOPERATIVE. REPLACED BATTERY AND LIGHTS OPERATED NO RMALLY. (M) 2 L 7 2 4F A16WE 1996030800400 19960308 00400 NM 1996 3 8 ASAA9610013 1 19960202 A 3350 883200312 RECEIVER BOEING 737 737290C 138448V NM CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 18 WOULD NOT EXTINGUISH. REPLACED EMERGENC Y EXIT LIGHT RECEIVER AT ROW 18 AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1996030800401 19960308 00401 NM 1996 3 8 ASAA9610014 1 19960204 A 3350 8821004 BATTERY PACK BOEING 737 7372Q8C 138448S NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 5 WERE FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1996030800402 19960308 00402 NM 1996 3 8 ASAA9610015 1 19960205 A 3397 WIRE BOEING 737 737290C 138448V NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING MAINTENANCE CHECK, TWO WHITE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE IN THE AFT CABIN. RE PAIRED FLOOR TRACK WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1996030800403 19960308 00403 NM 1996 3 8 ASAA9640006 1 19960125 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 771AS 25104 ANC - DURING MAINTENANCE CHECK, THE AFT THREE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED TRA CK WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996030800404 19960308 00404 WP 1996 3 8 ASAA9680032 1 19960121 A 5210 5910081167 DOOR DOUG DC9 DC982 3022082 WP L1 OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 936AS 49363 SEA - DURING MAINTENANCE CHECK, THE L1 DOOR GUST LOCK WAS FOUND INOPERATIVE. RERIGGED DOOR PER MAINTENANCE MANUAL AND O PERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996030800405 19960308 00405 WP 1996 3 8 ASAA9680033 1 19960121 A 5210 5956538 SEAL DOUG DC9 DC982 3022082 WP R1 DOOR RUBBING A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 936AS 49363 SEA - DURING MAINTENANCE CHECK, THE R1 DOOR WAS FOUND DIFFICULT TO OPEN. REMOVED EXCESS INTERIOR TRIM SEAL FROM FORWARD UPPER CORNER OF FRAME AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996030800406 19960308 00406 WP 1996 3 8 ASAA9680034 1 19960123 A 5210 MECHANISM DOUG DC9 DC982 3022082 WP L1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 936AS 49363 SEA - PRIOR TO DEPARTURE OF FLIGHT 370, CREW REPORTED THE L1 DOOR WOULD NOT CLOSE AND LOCK NORMALLY. ADJUSTED DOOR MECH ANISM PER MAINTENANCE MANUAL AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996030800407 19960308 00407 WP 1996 3 8 ASAA9680035 1 19960124 A 3350 60030431 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 936AS 49363 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 2 TO 6 WERE FOUND INOPERATIVE. REPLACED THE BAT TERY PACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996030800408 19960308 00408 WP 1996 3 8 ASAA9680037 1 19960126 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 967AS 49103 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 2 TO 7 WERE FOUND INOPERATIVE. REPLACED THE BAT TERIES AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996030800409 19960308 00409 WP 1996 3 8 ASAA9680038 1 19960127 A 5210 MECHANISM DOUG DC9 DC982 3022082 WP L1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 934AS 49235 SEA - DURING MAINTENANCE CHECK, THE L-1 DOOR GUST LOCK WAS FOUND NOT OPERATING PROPERLY. RERIGGED DOOR PER MM AND ADJUS TED GUST LOCK MECHANISM AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996030800410 19960308 00410 WP 1996 3 8 ASAA9680041 1 19960130 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 934AS 10264 49235 PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED. (M) 2 L 7 2 4F A6WE 1996030800411 19960308 00411 WP 1996 3 8 ASAA9680043 1 19960202 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 950AS 53023 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 4 TO 8 WERE FOUND INOPERATIVE. FOUND BROKEN WIRE AT LAMP MODULE, P/N 0105606003. REPLACED LAMP MODULE AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996030800412 19960308 00412 WP 1996 3 8 ASAA9680044 1 19960204 A 3350 014597101 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 935AS 49236 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 9 TO 12 WERE FOUND INOPERATIVE. REPLACED THE BA TTERIES AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996030800416 19960308 00416 NM 1996 3 8 AWXA96001 1 19960101 A 2820 FUEL SUMP DRAIN BOEING 737 7373S3 1384711 NM RT WING LEAKING A AWXA O OTHER K FLUID LOSS IN INSP/MAINT 1 WP 28 316AW 23713 CMH/MDS - FLT NR 403 - FLIGHT CREW REPORTED, FUEL LEAK FROM RIGHT WING. POST FLIGHT INSPECTION REVEALED FUEL RUNNING OU T OF RIGHT TANK SUMP DRAIN AFT OF INBOARD LEADING EDGE. CONTRACT MAINTENANCE RESEATED WING SUMP DRAIN. NO FURTHER LEAK S NOTED. (M) 2 L 7 2 4F RT A16WE 1996030800417 19960308 00417 NM 1996 3 8 AWXA960017 1 19960119 A 5315 BAC1505100617 FLOOR BEAM BOEING 737 737277 1384570 NM BS 967 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 PAE - FLT 3877 - DURING SCHEDULED C-CHECK, FOUND CORROSION ON UPPER CHORD OF FLOOR BEAM BS 967, WL 208, RBL 14 TO 50. R EMOVED CORRODED UPPER FLOOR BEAM FROM BS 967, RBL 14 TO 50. FABRICATED NEW UPPER CHORD, BACK DRILLED CHORD, FABRICATED REPAIR ANGLES, ALODINED, PRIMED, SEALED AND INSTALLED PER SRM 53-10-9. (M) 2 L 7 2 4F RT A16WE 1996030800418 19960308 00418 NM 1996 3 8 AWXA960018 1 19960120 A 3397 WIRE BOEING 737 73733A 1384673 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 166AW 23627 FLT NR 808 - PHX-SLC - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS AROUND ROW 18 SEAT INOP. REPAIRED WIRIN G AT ROW 18. OPS CHECK GOOD. (M0 2 L 7 2 4F RT A16WE 1996030800419 19960308 00419 NM 1996 3 8 AWXA960022 1 19960120 A 5313 STRINGER BOEING 737 737277 1384570 NM BS 1066 CHAFFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 PAE - FLT NR 3877 - DURING C-CHECK INSPECTION, FOUND DAMAGE TO STRINGER S12L AT STATION 1066 FROM WIRING BRACKET CHAFFIN G. CUT OUT DAMAGED AREA AND REPAIRED. REFERENCE SRM 53-10-03, FIGURE 1. (M) 2 L 7 2 4F RT A16WE 1996030800420 19960308 00420 EU 1996 3 8 AWXA960023 1 19960120 A 5320 RAIL AIRBUS 320 A320231 3930325 EU BS 2087-8077 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 634AW 091 PAE - FLT NR 3888 - DURNG C-CHECK INSPECTION, FOUND SURFACE CORROSION AT DUMMY RAIL STATION 2087, FR 16 TO STATION 8077, FR 20 Y-765. CORROSION REPLACED SEAT TRACK DUMMY RAIL PER SRM 51-42-11. (M) 2 L 7 2 4F RT A28NM 1996030800421 19960308 00421 EU 1996 3 8 AWXA960024 1 19960120 A 5320 RAIL AIRBUS 320 A320231 3930325 EU BS 7087-8077 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 634AW 091 PAE - FLT NR 3488 - DURING C-CHECK INSPECTION, FOUND SEVERAL SPOT CORROSION AT DUMMY RAILS STATION 7087, FR 16, STATION 8077, FR 10, Y254. REPAIRED CHORD PER SRM 53-11-14. (M) 2 L 7 2 4F RT A28NM 1996030800422 19960308 00422 EU 1996 3 8 AWXA960026 1 19960122 A 3230 E0052R8B3ASNE CONNECTOR AIRBUS 320 A320231 3930325 EU LANDING GEAR DIRTY A AWXA O OTHER J WARNING INDICATION DE DESCENT 1 WP 28 633AW 082 MKE/LAS - FLT NR 935 - LANDING GEAR WOULD NOT EXTEND WHEN COMMANDED. CYCLED GEAR PER ECAM, GEAR EXTENDED. REPLACED CON NECTOR 26GA AND CLEANED CONNECTOR 27GA AND 29GA. REINSTALLED BACK SHELL ON 31GA. LGCIU'S BITE GOOD. NO FAULTS NOTED. (M) 2 L 7 2 4F RT A28NM 1996030800423 19960308 00423 NM 1996 3 8 AWXA960028 1 19960124 A 2731 BACB28AP04P013 BUSHING BOEING 737 7373G7 1384595 NM RT ELEVATOR WORN A AWXA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 WP 28 305AW 24012 LAS-ABQ - FLT NR 720 - AIRCRAFT DIVERETED TO PHOENIX FOR FLIGHT CONTROL VIBRATION. CREW REPORTED VIBRATION FELT THROUGH OUT AIRCRAFT. MORE NOTICEABLE IN THE REAR. DID NOT FEEL VIBRATION IN POWER LEVERS BUT FELT IN YOKE. VIBRATION FREQUEN CY INCREASED WITH AIRSPEED AND FELT IN ALL PHASES OF FLIGHT. REMOVED AND REPLACED RIGHT ELEVATOR TAB INBOARD BUSHING AN D MOUNT FITTING FOR WEAR. (M) 2 L 7 2 4F RT A16WE 1996030800424 19960308 00424 EU 1996 3 8 AWXA960029 1 19960124 A 2910 S43500272 SERVICE MANIFOLD AIRBUS 320 A320231 3930325 EU YELLOW HYD SYS FAILED A AWXA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CL CLIMB 1 WP 28 636AW 098 FLT 258 - LAS/CMH - AIR TURN BACK, ON TAKEOFF LEG AFTER POWER REDUCTION TO CLIMB POWER, ECAM HYDRAULIC YELLOW RESERVOIR LOW LEVEL QUANTITY INDICATION SHOWED LOSS OF ALL FLUID PTU EMG 2 YELLOW PUMP SHUT OFF WITHIN SECONDS. REMOVED AND REPLA CED GROUND SERVICE MANIFOLD PER AMM 29-19-41 AND LEAK CHECKED GOOD. SERVICED YELLOW HYDRAULIC SYSTEM, RAN NR 1 AND NR 2 ENGINES AND NO LEAKS NOTED. (M) 2 L 7 2 4F RT A28NM 1996030800425 19960308 00425 EU 1996 3 8 AWXA960030 1 19960124 A 3260 ABS012110 PROX SENSOR AIRBUS 320 A320231 3930325 EU NLG FAILED A AWXA O OTHER N FALSE WARNING AP APPROACH 1 WP 28 633AW 082 FLT NR 264 - PHX-CMH - ON APPROACH, HAD TO RECYCLE GEAR HANDLE TO GET GEAR DOWN AND THREE GREEN. FOUND PROXIMITY SENSOR 36GS NOSE GEAR DOOR DOWN SENSOR INOP. REMOVED AND REPLACED SENSOR PER 32-31-73. GROUND AND OPS CHECKS GOOD. (M) 2 L 7 2 4F RT A28NM 1996030800426 19960308 00426 EU 1996 3 8 AWXA960033 1 19960125 A 3240 MS21902J6 UNION AIRBUS 320 A320231 3930325 EU BRAKE MODULE LOOSE A AWXA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 WP 28 636AW 098 FLT NR 860 - PHX/SAN - EMERGENCY LANDING AT SAN, YELLOW HYDRAULIC SYSTEM LEAK AND ALL FLUID LOST ON APPROACH. HYDRAULIC LEAK IN WHEEL WELL AREA. FOUND UNION ON AUTO BRAKE MODULE LOOSE. SECURED AND OPS CHECK NORMAL. ALSO, FOUND O-RING EX TRUDED FROM NR 2 SPOILER ACTUATOR SWIVEL. REPLACED O-RING. LEAK AND OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A28NM 1996030800427 19960308 00427 EU 1996 3 8 AWXA960034 1 19960126 A 5230 D5237134000200 HANDLE AIRBUS 320 A320231 3930325 EU CARGO DOOR OUT OF ADJUST A AWXA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 28 624AW 55 FLT NR 657 - SNA - ABORTED TAKEOFF, AFT CARGO DOOR ECAM WARNING. FOUND CARGO DOOR HANDLE BEING PUSHED OUT OF PROX SWITC H RANGE, PERFORMED PER 32-52-30-06. HANDLE NOW CLOSES NORMALLY WITH NO INTERFERENCE AND INDICATION IS NORMAL. (M) 2 L 7 2 4F RT A28NM 1996030800428 19960308 00428 NM 1996 3 8 AWXA960036 1 19960131 A 5320 DOOR FRAME BOEING 737 7373G7 1384595 NM BS 787 GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 PAE - FLT NR 3846 - DURING SCHEDULED C-10 MAINTENANCE CHECK, FOUND GOUGE IN THE AFT CARGO DOOR FRAME LOWER FORWARD CORNE R AT BS 787, WL 160. BLENDED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 51-70-11, 53-60-15 AND 51-20-01. (M ) 2 L 7 2 4F RT A16WE 1996030800429 19960308 00429 NM 1996 3 8 AWXA96004 1 19960105 A 5512 657378337 SKIN BOEING 737 7373G7 1384595 NM HORIZ STAB DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 LAS-PHX - FLT NR 1229 - CREW FOUND MULTIPLE DENTS IN LE OF HORIZONTAL STABILIZER OUT OF LIMITS. INTERIM REPAIR PER SRM 55-10-01, FILLED 1 DENT PER PARAGRAPH 'P' AND INSTALLED DMI 57834. ON 01/07, REMOVED AND REPLACED AND RESEALED LEFT HOR IZONTAL STABILIZER LEADING EDGE, DMI CLEARED. (M) 2 L 7 2 4F RT A16WE 1996030800430 19960308 00430 NM 1996 3 8 AWXA96005 1 19960106 A 4950 BACC10DU400C CLAMP BOEING 737 73733A 1384673 NM APU BLEED DUCT LOOSE A AWXA K NONE O OTHER UK UNKNOWN 1 WP 28 175AW 23634 PHX-LAS - FLT 367 - CREW REPORTED, RATTLING NOISE UNDER SINK IN AFT LAV. MAINTENANCE FOUND APU BLEED DUCT CLAMP AND STA NDOFF LOOSE. TIGHTENED CLAMP AND REPOSITIONED STANDOFF. (M) 2 L 7 2 4F RT A16WE 1996030800431 19960308 00431 SO 1996 3 8 C2XA96CL017 1 19960212 A 2750 3075001017 FLAP CONTL UNIT EMB 120 EMB120RT SO E/E BAY FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 15725 1702 303 120173 LAN - FLIGHT NR 3120 - CREW REPORTED, THAT AFTER TAKEOFF THEY HAD AN OUTBOARD FLAP DISAGREEMENT. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED THE FLAP CONTROL UNIT IAW EMB-120 MM 27-50-06. OPERATIONAL CHECKS WERE GOOD IAW EMB-1 20 MM 27-50-00. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1996030800432 19960308 00432 NM 1996 3 8 CAL960066 1 19960129 A 3260 LIGHT MODULE BOEING 727 727224 1384076 NM COCKPIT SHORTED A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 69736 69736 FLT NR 1422 - ATL - THE NOSE GEAR DOOR LIGHT ON SECOND OFFICERS PANEL AND THE DOOR LIGHT ON FORWARD PANEL REMAINED ILLUM INATED AFTER GEAR RETRACTION. THE GEAR WAS CYCLED, BUT THE LIGHT REMAINED ON. THE AIRCRAFT WAS RETURNED TO ATL WHERE I T LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE COCKPIT 'DOORS' LIGHT MODULE SHORTED. THE LIGHT MODULE WAS REMOVED AN D REPLACED. A DOOR WARNING SYSTEM TEST WAS PERFORMED IAW MM 32-62-0 AND OPERATION CHECKED GOOD. (M) 2 L 7 3 4F A3WE 1996030800433 19960308 00433 WP 1996 3 8 CAL960068 1 19960130 A 2913 AS66411LS666 HYD PUMP DOUG DC9 DC982 3022082 WP NR 1 ENGINE CRACKED A CALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 71828 21275 49488 FLT NR 431 - MSY - THE LEFT HYDRAULIC SYSTEM FLUID QUANTITY AND PRESSURE DROPPED TO ZERO WHILE IN FLIGHT. THE AIRCRAFT LANDED AT MSY WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP CASE CRACKED. THE PUMP WAS REM OVED AND REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD. (M) 2 L 7 2 4F A6WE 1996030800434 19960308 00434 NM 1996 3 8 CAL960069 1 19960130 A 3350 LIGHT BOEING 737 737291 138448W NM CABIN WIRE BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17252 20362 FLT NR 1630 - EWR - THE AFT CABIN RIGHT EMERGENCY EXIT LIGHT NEAR BACK WALL ON FLOOR WOULD NOT ILLUMINATE. MAINTENANCE FOUND A WIRE TO THE EXIT LIGHT BROKEN. THE WIRE WAS REPAIRED AND THE LIGHT WAS RELAMPED. (M) 2 L 7 2 4F A16WE 1996030800435 19960308 00435 WP 1996 3 8 CAL960070 1 19960130 A 4900 3812761 APU DOUG DC9 DC982 3022082 WP AC TAIL MALFUNCTIONED A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 16893 49392 FLT NR 483 - DCA - OPERATING THE APU WITH THE NR 1 GENERATOR PLACARDED INOPERATIVE. THE APU SHUT DOWN DURING CLIMB-OUT OF BWI. AN APU RESTART ATTEMPT WAS UNSUCCESSFUL. THE AIRCRAFT WAS DIVERTED TO DCA WHERE IT MADE A NORMAL LANDING. MAI NTENANCE STARTED THE APU SEVERAL TIMES WHILE ON THE GROUND AT DCA. THE FAULT COULD NOT BE DUPICATED. (M) 2 L 7 2 4F A6WE 1996030800436 19960308 00436 WP 1996 3 8 CAL960072 1 19960131 A 3260 833703 PROX SENSOR DOUG DC9 DC982 3022082 WP RT MLG DOOR INOPERATIVE A CALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 14840 49580 FLT NR 1896 - IAH - THE GEAR DOOR OPEN LIGHT ILLUMINATED WHEN GEAR WAS RETRACTED AFTER TAKEOFF FROM PHX. THE AIRCRAFT W AS RETURNED TO PHX WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT MLG DOOR PROXIMITY SENS OR IAW MM 32-60-05, PAGE 212. OPERATION OF THE GEAR DOOR OPEN LIGHT WAS RESTORED TO NORMAL. (M) 2 L 7 2 4F A6WE 1996030800437 19960308 00437 WP 1996 3 8 CAL960075 1 19960203 A 3233 59370365001 RETRACT CYLINDER DOUG DC9 DC982 3022082 WP RT MLG LEAKING A CALA O OTHER B K J SMOKE/FUMES/ODORS/SPARKS FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 16815 36347 19900 49113 FLT NR 1951 - LAS - THE RIGHT HYDRAULIC SYSTEM QUANTITY AND PRESSURE DROPPED WHILE EN ROUTE TO LAS. SMOKE WAS OBSERVED IN THE CABIN AFTER LANDING AT LAS. ALL 3 SLIDES WERE DEPLOYED AND THE PASSENGERS WERE EVACUATED. MAINTENANCE FOUND THE RIGHT MLG ACTUATOR LEAKING CAUSING HYDRAULIC FLUID TO ENTER THE APU INLET WHICH RESULTED IN SMOKE. THE RIGHT MLG ACTUA TOR WAS REMOVED AND REPLACED. THE HYDRAULIC SYSTEM WAS SERVICED. THE APU WAS RUN WITH BOTH PACKS AND ENGINES OPERATING AND NO SMOKE WAS OBSERVED IN THE CABIN. IN ADDITION, ALL THREE EMERGENCY EVACUATION SLIDES WERE REMOVED AND REPLACED. (M) 2 L 7 2 4F A6WE 1996030800438 19960308 00438 NE 1996 3 8 CAL960076 2 19960203 A 7260 CARBON SEAL BOEING 727 727243 138408D NM PWA JT8 JT8D9 52048 NE NR 2 GEAR BOX LEAKING A CALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 17410 21663 665234 FLT NR 6834 - TPA - THE NR 2 ENGINE WAS SHUT DOWN WHILE EN ROUTE TO TPA DUE TO LOSS OF OIL QUANTITY. THE AIRCRAFT LANDE D AT TPA WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE STARTER DRIVE SPLINE ADAPTER CARBON SEAL LEAKING. THE SEA L WAS REPLACED IAW MM 72-61-0. THE ENGINE WAS RUN AND NO LEAKS WERE NOTED. (M) 2 L 7 3 4F 4 F RT A3WE E2EA 1996030800439 19960308 00439 WP 1996 3 8 CAL960077 1 19960204 A 3230 580205158 CONTROL CABLE DOUG DC9 DC981 3022081 WP RT MLG BENT A CALA O OTHER J WARNING INDICATION CL CLIMB 1 SW 09 37882 48027 FLT NR 1170 - EWR - THE RIGHT MLG UNSAFE LIGHT AND GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. 'AB NORMAL' PROCEDURES WERE COMPLIED WITH, BUT THE LIGHTS STAYED ON FOR REMAINDER OF FLIGHT. THE AIRCRAFT LANDED AT EWR WIT H GEAR DOORS OPEN. MAINTENANCE RESET THE DOORS AND THE AIRCRAFT TAXIIED TO GATE. MAINTENANCE FOUND THE RIGHT MLG MECHA NICAL CONTROL CABLE BENT AND BINDING. THE CONTROL CABLE WAS REMOVED AND REPLACED IAW MM 32-31-00. THE CABLE WAS ADJUST ED AND TESTED IAW MM 32-31-00, PAGE 501-509. THE GEAR WAS SWUNG SEVERAL TIMES WITH OPERATION AND INDICATIONS CHECKING G OOD. (M) 2 L 7 2 4F A6WE 1996030800440 19960308 00440 NM 1996 3 8 CAL960079 1 19960121 A 3350 BATTERY PACK BOEING 737 7373T0 1384582 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14341 23579 HOU - THE LEFT AFT EMERGENCY CEILING LIGHT BATTERY PACK FAILED CAPACITY TEST. THE BATTERY PACK WAS REMOVED AND REPLACED . (M) 2 L 7 2 4F RT A16WE 1996030800441 19960308 00441 WP 1996 3 8 CAL960080 1 19960118 A 5350 CABLES DOUG DC9 DC932 3022066 WP TAILCONE OUT OF RIG A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18513 48112 HOU - THE TAILCONE INTERIOR RELEASE HANDLE PULLED AT 45 POUNDS AND THE TAILCONE DID NOT DROP. THE TAILCONE WAS ADJUSTED AND RIGGED IAW WORK CARD 08-5350-1-0007. (M) 2 L 7 2 4F A6WE 1996030800442 19960308 00442 WP 1996 3 8 CAL960081 1 19960118 A 5350 CABLES DOUG DC9 DC932 3022066 WP TAILCONE OUT OF RIG A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18513 48112 HOU - THE TAILCONE EXTERIOR HANDLE FAILED TEST PULLING AT 50 POUNDS AND THE TAILCONE DID NOT PROP. THE TAILCONE WAS RIG GED AND ADJUSTED IAW WORK CARD 08-5350-1-0007. (M) 2 L 7 2 4F A6WE 1996030800443 19960308 00443 NM 1996 3 8 CAL960082 1 19960205 A 3350 BATTERY PACK BOEING 727 727224 1384076 NM AFT AIRSTAIR DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 79746 22449 FLT NR 232 - EWR - THE EMERGENCY OVERHEAD LIGHTING IN AFT AIRSTAIR WAS FOUND INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED AND OPERATION OF THE LIGHTING WAS RESTORED. (M) 2 L 7 3 4F A3WE 1996030800444 19960308 00444 WP 1996 3 8 CKSA96003 1 19960118 A 2910 5393397161108 HYD HOSE DOUG DC8 DC851 3021920 WP NR 3 ENG HOLE A CKSA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 23 804CK 53104 45689 KHUF - IN FLIGHT AT 0505Z, HYDRAULIC RESERVOIR LOW PRESSURE LIGHT CAME ON AT 0530. LOST ALL HYDRAULIC PRESSURE, PERFORM ED CHECKLIST PROCEDURES. FOUND HYDRAULIC SUCTION LINE AT PUMP ON NR 3 ENGINE LEAKING. REPLACED LINE AND SERVICED HYDRA ULICS, LEAK CHECK GOOD. (M) 2 L 7 4 4F 4A25 1996030800445 19960308 00445 WP 1996 3 8 CKSA96006 1 19960118 A 3260 7000010101 DNLOCK SWITCH DOUG DC8 DC861 3021952 WP LT MLG INTERMITTENT A CKSA O OTHER N FALSE WARNING AP APPROACH 1 GL 23 812CK 49562 45890 KSEA - ON APPROACH TO KSEA, HAD UNSAFE LANDING LEFT GEAR LIGHT INDICATION. RECYCLED GEAR SEVERAL TIMES. LEFT MAIN GEAR DOWNLOCK LIGHT ILLUMINATED, LANDED WITHOUT INCIDENT. VISUALLY INSPECTED LEFT MAIN LANDING GEAR UPLATCH ASSEMBLY, AND A LL MECHANICAL COMPONENTS, NO DEFECTS NOTED. CHECKED WIRING TO DOWNLOCK SWITCH, NO DEFECTS NOTED. FOUND MAIN LANDING GE AR DOWNLOCK SWITCH TO BE INTERMITTENT. REMOVED AND REPLACED SAME PER DC-8 MM 32-60-0 PARAGRAPH 1A, B, AND C PG 201. (M) 2 L 7 4 4F 4A25 1996030800446 19960308 00446 WP 1996 3 8 CKSA96007 1 19960119 A 3260 WIRE DOUG DC8 DC863 302198A WP LANDING GEAR CHAFED A CKSA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 869BX 55282 46035 KYIP - GEAR NOT LATCHED LIGHT AND GEAR HORN REMAINED ON AFTER GEAR RETRACTION, RECYCLED GEAR NO HELP. REPAIRED CHAFED W IRING AT PIN E AND F, ON PLUG P1-2199 ON SECONDARY LANDING GEAR. GEAR WARNING SWITCH SYSTEM, OPS CHECKS GOOD ON GROUND. (M) 2 L 7 4 4F 4A25 1996030800448 19960308 00448 NE 1996 3 8 EIAA9603 2 19960131 A 7200 ENGINE BOEING 747 747212B 1384886 NM PWA JT9 JT9D7J 52054 NE NR 1 FLAMED OUT A EIAA O OTHER X ENGINE FLAMEOUT AP APPROACH 1 NM 09 485EV 20712 662254 NR 1 ENGINE FLAMED OUT ON APPROACH, ATTEMPTED TO RESTART. SUBMITTER STATES, SUSPECT HIGH STAGE FUEL PUMP FAILURE. 2 L 7 4 4F 4 F A20WE E20EA 1996030800449 19960308 00449 NM 1996 3 8 F3LA96008 1 19960214 A 3260 WARNING HORN BOEING 737 737201 1384454 NM LANDING GEAR SOUNDED A F3LA O OTHER N FALSE WARNING AP APPROACH 1 NM 03 217US 20215 FLT NR 546 - DEN - UPON ARRIVAL, FLIGHT CREW REPORTED THE LANDING GEAR WARNING HORN SOUNDED WITH THROTTLES RETARDED TO I DLE AND FLAPS UP. WARNING HORN DID NOT SOUND AT FLAP SETTINGS 1 OR 5 WITH THROTTLES RETARDED TO IDLE. LANDING GEAR WAS UP IN BOTH CASES. MAINTENANCE PEFORMED LANDING GEAR WARNING TEST PER MM 31-26-0 AND FLAP SETTINGS 1 AND 5 CHECKED NORM AL. LUBED FLAP SWITCH AS PRECAUTIONARY. (M) 2 L 7 2 4F A16WE 1996030800450 19960308 00450 SO 1996 3 8 GLBA96001 1 19960105 A 2750 CONNECTOR EMB 120 EMB120RT SO TE FLAPS WET A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 281UE 19123 120092 ORD - AFTER TAKEOFF, THE CREW NOTED A DISAGREEMENT FAULT WHEN THE FLAPS WERE SELECTED UP. THE CREW ELECTED AN AIR TURN BACK WHICH WAS FOLLOWED BY AN UNEVENTFUL LANDING. MAINTENANCE FOUND CANNON PLUGS WET WITH GLYCOL. THE PLUGS WERE DRIED AND THEN THE FLAPS WERE SUCCESSFULLY CYCLED 4 TIMES. (M) 2 L 7 2 4T RT A31SO 1996030800451 19960308 00451 1996 3 8 GLBA96003 4 19960115 A 6122 PROP GOVERNOR BEECH 1900 1900C 1154161 CE RT ENGINE MALFUNCTIONED A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 01 84GL UC84 BIS - THE CREW OBSERVED AFTER TAKEOFF THAT THE RIGHT PROP WOULD NOT GO BEYOND 1400 RPM. THEY ELECTED AN AIR TURN BACK F OLLOWED BY AN UNEVENTFUL LANDING. MAINTENANCE COULD NOT DUPLICATE THE PROBLEM ON THE GROUND. A TEST FLIGHT WAS REQUEST ED AN WAS SUCCESSFUL. (M) 2 L 7 2 4T RT A24CE 1996030800452 19960308 00452 WP 1996 3 8 GRAA9602 1 19960102 A 3350 6100928 LAMP DOUG DC9 DC987 3022087 WP CABIN INOPERATIVE A GRAA K NONE L NO TEST IN INSP/MAINT 1 WP 11 1074T 49727 PILOT ENTERED IN LOG THAT THE CABIN EMERGENCY FLOOR TRACK LIGHT PULLED LOOSE. MAINTENANCE REPLACED THE LAMP AND LENS, P /N 079123. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE LIGHTING SYSTEM. OPERATIONAL CHECKED NORMAL. AIRCRAFT RE TURNED TO SERVICE. (M) 2 L 7 2 4F RT A6WE 1996030800453 19960308 00453 WP 1996 3 8 GRAA9603 1 19960131 A 3222 59403381 STRUT DOUG DC9 DC987 3022087 WP NLG REQ'D SERV A GRAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 11 1075T 49724 UPON TAKEOFF AT FAR, NLG WOULD NOT RETRACT. AIRCRAFT RETURNED TO FAR WITHOUT FURTHER INCIDENT. MX WAS NOTIFIED AND A F ERRY PERMIT WAS GENERATED. THE AIRCRAFT DEPARTED TO MKE WITH THE GEAR DOWN AND PINNED. MX DISCOVERED THAT THE NLG TORQ UE LINK SCISSORS WERE STIFF, DISASSEMBLED THE TORQUE LINK SCISSORS AND REAMED THE BUSHINGS TO PROPER FIT, IAW 32-21-03, AND DC OHM 32-21-00. MX DRAINED THE 5606 HYD FLUID IN THE NLG STRUT AND REPLACED THE FLUID WITH 3 GALLONS ROYED LGF. J ACKED THE AIRCRAFT AND CYCLED THE NLG. OPERATIONAL CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A6WE 1996030800454 19960308 00454 WP 1996 3 8 GRAA9604 1 19960209 A 7711 MR701DC8 CIRCUIT BREAKER DOUG DC9 DC987 3022087 WP COCKPIT TRIPPED A GRAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 WP 11 1074T 49727 AT RNO, AIRCRAFT BEGAN TAKEOFF ROLL AND CIRCUIT BREAKER L-33 POPPED. THIS CIRCUIT BREAKER PROVIDES POWER TO THE NR 1 EP R SYSTEM. AIRCRAFT ABORTED TAKEOFF AT 60 KIAS. AIRCRAFT RETURNED TO THE GATE WITHOUT ANY FURTHER OCCURANCE. MAINTENAN CE RESET CIRCUIT BREAKER L-33. AIRCRAFT WAS RUN TO TAKEOFF POWER FOR 2 MINUTES AND COULD NOT DUPLICATE THE PROBLEM. AI RCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A6WE 1996030800455 19960308 00455 WP 1996 3 8 GRAA9605 1 19960123 A 3350 TRACK LIGHT DOUG DC9 DC982 3022082 WP CABIN DIM A GRAA K NONE L NO TEST IN INSP/MAINT 1 WP 11 500TR 49144 LINE MAINTENANCE AT MYR, DISCOVERED THE AFT EMERGENCY TRACK LIGHTS DIM WHILE PERFORMING AND OPERATIONAL CHECK OF THE SYS TEM. MAINTENANCE REPLACED THE FOUNDATION STRIP, P/N 37781, AND 5 FLEXIBLE LIGHT SEGMENTS, P/N 362624, AND TRACK COVER P /N 5878. MAINTENANCE PERFORMED AND OPERATIONAL CHECK OF THE SYSTEM. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4F A6WE 1996030800456 19960308 00456 WP 1996 3 8 GRAA9606 1 19960206 A 3350 100865 POWER SUPPLY DOUG DC9 DC987 3022087 WP CABIN INOPERATIVE A GRAA K NONE L NO TEST IN INSP/MAINT 1 WP 11 1074T 49727 LINE MAINTENANCE AT RNO, DISCOVERED THE FWD AND AFT EMERGENCY FLOOR TRACK LIGHT TRACK INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FWD AND AFT POWER SUPPLIES. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM. THE SYSTEM OPERATIONAL CHECKED NORMAL. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A6WE 1996030800457 19960308 00457 WP 1996 3 8 GRAA9607 1 19960205 A 3350 DC26E1065 CONNECTOR DOUG DC9 DC987 3022087 WP CABIN FAILED A GRAA K NONE L NO TEST IN INSP/MAINT 1 WP 11 1075T 49724 LINE MAINTENANCE AT ENV, DISCOVERED THAT THE FORWARD FLIGHT ATTENDANT ENTRY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CANNON PLUG. OPERATIONALLY CHECKED NORMAL, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A6WE 1996030800458 19960308 00458 WP 1996 3 8 HALA9607 1 19960203 A 4900 381015P109 APU DOUG DC9 DC951 3022051 WP EMPENNAGE FAILURE A HALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 13 2FOR 47742 OGG - PRIOR TO TAKEOFF, UNKNOWN SMOKE FILLED THE COCKPIT AND PASSENGER CABIN. CONDUCTED EMERGENCY EVACUATION. MAINTENA NCE INSPECTION DISCLOSED APU FAILURE RESULTED IN APU OIL TO ENTER BLEED AIR SYSTEM CAUSING SMOKE. APU WAS REPLACED AND ALL SYSTEM CHECK NORMAL. 2 L 7 2 4F A6WE 1996030800459 19960308 00459 WP 1996 3 8 HALA9609 1 19960207 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 2FOR 47796 HNL - AFT CABIN EMERGENCY LIGHTS INOP. REPLACED BATTERIES. OPS CHECK OK. (M) 2 L 7 2 4F A6WE 1996030800460 19960308 00460 NM 1996 3 8 IXKA960005 1 19960227 A 2780 BOLTS BOEING 727 727251 138408H NM LE SLAT ACT LOOSE A IXKA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 25 267US 20289 AT EWR - FLT NR 39 - NR 4 LEADING SLAT LIGHT CAME ON, AIRCRAFT RETURNED TO EWR. FOUND NR 4 LEADING EDGE ACTUATOR REAR M OUNT BOLTS LOOSE, TIGHTENED LOOSE MOUNT BOLTS AND OPS CHECK FLAPS PER MM 27-80. OPS OK. (M) 2 L 7 3 4F A3WE 1996030800461 19960308 00461 WP 1996 3 8 IXXA9604 1 19960127 A 3320 02741 BALLAST DOUG DC8 DC862 3021970 WP COCKPIT FAILED A IXXA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 23 735PL 46153 EN ROUTE BETWEEN PDX, AND OAK, THE FLIGHT CREW NOTED THE SMELL OF SMOKE COMING FROM THE ENGINE INDICATION PANEL. IN OAK , MAINTENANCE INSPECTED THE AIRCRAFT AND DETERMINED THAT A FLUORESCENT LIGHTING BALLAST HAD FAILED, EMITTING THE SMELL. THE FLUORESCENT LIGHTS POWERED BY THAT BALLAST WERE DEFERRED, AND THE AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 4 4F 4A25 1996030800462 19960308 00462 WP 1996 3 8 IXXA9605 1 19960131 A 2120 AIR DISTR DOUG DC8 DC871 302199A WP CABIN ODOR A IXXA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 23 824BX 45946 EN ROUTE BETWEEN MKE AND DEN, THE AIR CONDITIONING PACKS WERE PRODUCING A STRONG, UNIDENTIFIED ODOR. ON THE GROUND IN D EN, THE PACKS WERE OPERATIONALLY CHECKED AND FOUND NOT TO BE PRODUCING AND ODOR AT THAT TIME. A REVIEW OF THE FLIGHT SU GGESTED THAT A SMALL AMOUNT OF DE-ICE FLUID MAY HAVE BEEN PULLED INTO THE BLEED AIR SYSTEM, PRODUCING A RESIDUAL ODOR. ( M) 2 L 7 4 4F 4A25 1996030800463 19960308 00463 WP 1996 3 8 IXXA9606 1 19960131 A 2120 AIR DISTR DOUG DC8 DC862 3021970 WP CABIN ODOR A IXXA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 23 21CX 45955 EN ROUTE BETWEEN LPLA AND KWRT, THE AIR CONDITIONING SYSTEM INTERMITTENTLY PRODUCED THE STRONG SMELL OF OIL IN THE COCKP IT. THE FLIGHT CREW SUSPECTED A TURBOCOMPRESSOR OIL SEAL FAILURE. INSPECTION ON THE GROUND IN KWRT SHOWED THE TC'S TO BE NORMAL, WITH NO LEAKAGE OF LOSS OF OIL. NO OTHER SOURCE COULD BE IDENTIFIED FOR THE INTERMITTENT SMELL. (M) 2 L 7 4 4F 4A25 1996030800464 19960308 00464 WP 1996 3 8 IXXA9607 1 19960131 A 2730 CONTROL DOUG DC8 DC871F 302199D WP ELEVATOR NOT EFFECTIVE A IXXA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 23 821BX 45811 TAKEOFF OUT OF OAK WAS ABORTED AT 80 KT DUE TO AN ABNORMAL ELEVATOR EFFECTIVENESS CHECK. (M) 2 L 7 4 4F RT 4A25 1996030800465 19960308 00465 NE 1996 3 8 IXXA9608 2 19960102 A 7200 ENGINE DOUG DC8 DC871 302199A WP GE CFM56 CFM562C1 13802 NE NR 4 FLAMED OUT A IXXA O OTHER X ENGINE FLAMEOUT NR NOT REPORTED 1 GL 23 824BX 45946 692290 EN ROUTE FROM TOL TO SEA, THE NR 4 ENGINE FLAMED OUT AT 35,000 FEET. TWO UNSUCCESSFUL RESTART ATTEMPTS WERE MADE. THE ENGINE WAS SECURED AND THE AIRCRAFT DIVERETED TO MSO FOR MAINTENANCE. UPON ARRIVAL IN MSO, THE FLIGHT CREW REPORTED THE Y SUMPED TANKS AND REMOVING SOME WATER FROM THE SUMPS. IN MSO, MAINTENANCE ACCOMPLISHED A FLAMEOUT CHECK PER THE CFM56M M. NO DEFECTS FOUND. THE NR 4 MAIN FUEL TANK WAS ENTERED AND FOUND TO BE NORMAL AND UNCONTAMINATED. THE FUEL FILTER W AS FOUND CLEAN BUT PRECAUTIONARILY CHANGED. MAINTENANCE SUMPED ALL TANKS. (M) 2 L 7 4 4F 4 F 4A25 E2GL 1996030800466 19960308 00466 WP 1996 3 8 IXXA9609 1 19960202 A 3260 H141003 DNLOCK SWITCH DOUG DC8 DC863F 302198F WP RT MLG FAILED A IXXA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 23 906R 46087 IN PREPARATION FOR LANDING AT DAY, THE LANDING GEAR WAS EXTENDED, BUT NO SAFE INDICATION WAS PRESENT FOR THE RIGHT MLG. THE AIRCRAFT ACCOMPLISHED A FLY-BY OF THE CONTROL TOWER AND OBTAINED VISUAL VERIFICATION THAT THE RIGHT MLG WAS EXTENDE D. A NORMAL LANDING WAS ACCOMPLISHED. MAINTENANCE DETERMINED THAT THE RIGHT MLG DOWNLOCK SWITCH HAD FAILED INTERNALLY, CAUSING AND INDICATION PROBLEM. THE RIGHT MLG DOWNLOCK SWITCH WAS REPLACED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 4 4F 4A25 1996030800467 19960308 00467 NM 1996 3 8 MALA964818 1 19960114 A 2611 3023143 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM CARGO COMPT FAILED A MALA O OTHER N FALSE WARNING CR CRUISE 1 GL 15 826MA 330 FLT NR 3394 - EN ROUTE FROM AZO TO MSP, THE CARGO SMOKE WARNING LLIGHT WOULD INTERMITTENTLY ILLUMINATE. THE AIRCRAFT CO NTINUED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE NR 2 SMOKE DETECTOR. ALL SYSTEMS OPERAT ED SATISFACTORILY. (M) 2 H 7 2 4T RT A13NM 1996030800468 19960308 00468 SW 1996 3 8 MALA964819 1 19960114 A 3230 ML345 SWITCH SWRNGN SA227 SA227AC 8780603 SW RT MLG FAILED A MALA K NONE O OTHER CL CLIMB 1 GL 15 26863 AC650B FLT NR 3462 - AFTER DEPARTURE FROM BJI, THE NOSE GEAR BEGAN TO CYCLE AFTER LANDING GEAR RETRACTION. THE AIRCRAFT CONTIN UED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE RIGHT INBOARD MLG POSITION SWITCH. ALL SYST EMS OPERATED SATISFACTORILY. (M) 1 L 7 2 4T A8SW 1996030800469 19960308 00469 SW 1996 3 8 MALA964820 1 19960114 A 2431 MS3126E835 CONNECTOR SWRNGN SA227 SA227AC 8780603 SW LT WING ROOT CORRODED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 26906 AC654B FLT NR 3222 - AFTER DEPARTING DSM, THE LEFT BATT WARM LIGHT ILLUMINATED. SHORTLY AFTER, THE LEFT BATTERY HOT LIGHT ILLU MINATED. THE CREW ELECTED TO RETURN TO DSM AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED TH E LEFT BATTERY TEMP CANNON PLUG. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 1 L 7 2 4T A8SW 1996030800470 19960308 00470 SW 1996 3 8 MALA964821 1 19960115 A 3260 1EN516 UPLIMIT SWITCH SWRNGN SA227 SA227AC 8780603 SW RT MLG OUT OF ADJUST A MALA K NONE O OTHER CR CRUISE 1 GL 15 26863 AC650B FLT NR 3233 - EN ROUTE FROM MSP TO BRD, THE NOSE LANDING GEAR CONTINUED TO CYCLE AFTER RETRACTION. THE AIRCRAFT CONTINU ED TO BRD AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL ADJUSTED THE RIGGING OF THE RIGHT LANDING GEAR UP LIMIT SW ITCHES. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 1 L 7 2 4T A8SW 1996030800471 19960308 00471 EU 1996 3 8 P2RA960003 1 19960128 A 7830 9105M20G05 THRUST REVERSER AIRBUS 300 A300B4203 3930306 EU NR 1 ENG DELAMINATED A P2RA K NONE O OTHER IN INSP/MAINT 1 WP 23 14975 261 DAMAGE ON CORE SECTION OF NR 1 ENGINE LEFT THRUST REVERSER. REMOVED AND REPLACED NR 1 ENGINE LEFT THRUST REVERSER PER A 300MM, OPERATIONAL CHECK OK. (M) 2 L 7 2 4F A35EU 1996030800472 19960308 00472 EU 1996 3 8 PLG2596E1 1 19960205 A 3230 UPSTOP PAD SAAB SF340 340B 7860101 EU LT MLG OUT OF ADJUST A PLGA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NE 05 358BE 340B279 PSM - FLT 4471 - ON CLIMB-OUT, THE LANDING GEAR INTRANSIT LIGHT STAYED ILLUMINATED, AND THE HYDRAULIC PUMP CONTINUED TO RUN. THE AIRCRAFT RETURNED TO PSM AND LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE UPSTOP PAD ON THE LEFT HAND MA IN GEAR. TEST FLIGHT WAS PERFORMED AND GEAR OPERATED NORMALLY. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1996030800473 19960308 00473 1996 3 8 PLG2796G1 4 19960127 A 3444 54022722034 ALTITUDE ALERTER BEECH 1900 1900C 1154161 CE CABIN DEFECTIVE A PLGA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NE 05 819BE 1772 UB62 FLT NR 3819 - PSM-PWM - AFTER TAKEOFF, THE CREW NOTICED A ONE AMP CIRCUIT BREAKER POPPED WITH SMOKE EMITTING FROM THE CI RCUIT BREAKER PANEL. THE AIRCRAFT RETURNED TO PSM LANDING WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT AND FOUND THE ALTITUDE ALERTER TO BE DEFECTIVE. MAINTENANCE REMOVED AND REPLACED THE ALTITUDE ALERTER AND THE CIRCUIT BREAKER AND RETURNED THE AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1996030800474 19960308 00474 EU 1996 3 8 SIMA960301 1 19960130 A 3350 3012001 POWER PACK AEROSP ATR72 ATR72212 EU CABIN INOPERATIVE A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 414WF 356 414 ORD - FLT NR 4029 - DURING TAXI, THE FLOOR EMERGENCY LIGHTS ILLUMINATED. MAINTENANCE REPLACED THE FORWARD NR 1 POWER SU PPLY, CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996030800475 19960308 00475 EU 1996 3 8 SIMA960332 1 19960202 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 421MQ 3373 014 CMI - EMERGENCY LIGHTS FOR BATTERY PACK POSITION 10WL INOPERATIVE AND EMERGENCY LIGHTS AT POSITION 3WL WILL NOT GO OUT. RAI'D BATTERY PACKS AT 10WL AND 3WL. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996030800476 19960308 00476 NM 1996 3 8 TAOA029603 1 19960207 A 3350 OL3071BPEGL LAMP BOEING 727 727254 138408L NM CABIN INOPERATIVE A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 916TS 20437 EPL ROW 11 HAS 1 LAMP INOP. RELAMPED, OPERATIONAL CHECK OK. (M) 2 L 7 3 4F A3WE 1996030800477 19960308 00477 NM 1996 3 8 TAOA029606 1 19960210 A 3350 RPSIB CHARGER BOEING 727 727225 1384077 NM CABIN INOP A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 919TS 6299 20447 EPL DOES NOT ILLUMINATE FROM ROW 26 TO AFT ENTRY. REPLACED BATTERY CHARGER. OPERATIONAL CHECK OK. (M) 2 L 7 3 4F A3WE 1996030800478 19960308 00478 NM 1996 3 8 TAOA029607 1 19960210 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 925TS 3899 21244 CEILING EMERGENCY LIGHT AT ROW 3 INOP. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. (M) 2 L 7 3 4F A3WE 1996030800479 19960308 00479 NM 1996 3 8 USAA960170 1 19960130 A 5320 693535214 TIE CLIP BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 237US 39557 22353 INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK BS 727 B S-1, STRINGER TIE CLIP. REPAIRED PER EO 53 93G227. MODIFIED PART NR INSTALLED 69-35352-14. (M) 2 L 7 2 4F A16WE 1996030800480 19960308 00480 NM 1996 3 8 USAA960171 1 19960130 A 5320 693535214 TIE CLIP BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 237US 39557 22353 INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK AT STRINGER TIE CLIP BS 727A STRINGER 4 RIGHT. REPA IRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M) 2 L 7 2 4F A16WE 1996030800481 19960308 00481 NM 1996 3 8 USAA960172 1 19960130 A 5320 693535214 TIE CLIP BOEING 737 737201 1384454 NM BS 639 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 237US 39557 22353 INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP BS 639 STRINGER 4 RIGHT. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M) 2 L 7 2 4F A16WE 1996030800482 19960308 00482 NM 1996 3 8 USAA960173 1 19960130 A 5320 693535214 TIE CLIP BOEING 737 737201 1384454 NM BS 578 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 237US 39557 22353 INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP BS 578 STRINGER 3 RIGHT. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M) 2 L 7 2 4F A16WE 1996030800483 19960308 00483 NM 1996 3 8 USAA960174 1 19960130 A 5320 693535214 TIE CLIP BOEING 727 727251 138408H NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273US 39557 20295 INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP BS 616 STRINGER 2 RIGHT. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M) 2 L 7 3 4F A3WE 1996030800484 19960308 00484 NM 1996 3 8 USAA960175 1 19960130 A 5320 693535214 TIE CLIP BOEING 737 737201 1384454 NM BS 827 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 237US 39557 22353 INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP BS 827 STRINGER 5 LEFT. REPAIRED PER EO 5393G227. MODIFIED PER NR 69-35352-14. (M) 2 L 7 2 4F A16WE 1996030800485 19960308 00485 NM 1996 3 8 USAA960176 1 19960130 A 5320 693535214 TIE CLIP BOEING 737 737201 1384454 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 237US 39557 22353 INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP BS 787 STRINGER 10L. REPAIRED PER EO 5353G227. MODIFIED PART NR 69-35352-14. (M) 2 L 7 2 4F A16WE 1996030800486 19960308 00486 NM 1996 3 8 USAA960177 1 19960130 A 5320 693535214 TIE CLIP BOEING 737 737201 1384454 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 237US 39557 22353 INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP BS 747 STRINGER 7L AND STRINGER 10 L. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M) 2 L 7 2 4F A16WE 1996030800487 19960308 00487 NM 1996 3 8 USAA960178 1 19960130 A 5320 693535214 TIE CLIP BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 237US 39557 22353 INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP STATION 727 A STRINGERS 3L, STRING ER 4L, STRINGER 5L. REPAIRED PER EO 5393G227. MODIFIED PER NR 69-35352-14. (M) 2 L 7 2 4F A16WE 1996030800488 19960308 00488 NM 1996 3 8 USAA960179 1 19960130 A 5320 693535214 TIE CLIP BOEING 737 737201 1384454 NM BS 706 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 237US 39557 22353 INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP BS 706, STRINGER 10L. REPAIRED PE R EO 5393G227. MODIFIED PART NR 69-35352-14. (M) 2 L 7 2 4F A16WE 1996030800489 19960308 00489 NM 1996 3 8 USAA960180 1 19960130 A 5320 693535214 TIE CLIP BOEING 737 737201 1384454 NM BS 685 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 237US 39557 22353 INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP STATION 685, STRINGER 2L AND STRIN GER 5L. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M) 2 L 7 2 4F A16WE 1996030800490 19960308 00490 NM 1996 3 8 USAA960181 1 19960130 A 5320 693535214 TIE CLIP BOEING 737 737201 1384454 NM BS 639 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 237US 39557 22353 INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK STRINGER TIE CLIP STATION 639 STRINGERS 4L, 6L. REP AIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M) 2 L 7 2 4F A16WE 1996030800491 19960308 00491 NM 1996 3 8 USAA960182 1 19960130 A 5320 693535214 TIE CLIP BOEING 737 737201 1384454 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 237US 39557 22353 INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK IN 2 STRINGER TIE CLIPS BS 616 AT STRINGER 2L AND ST RINGER 4L. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M) 2 L 7 2 4F A16WE 1996030800492 19960308 00492 NM 1996 3 8 USAA960183 1 19960130 A 5320 693535214 TIE CLIP BOEING 737 737201 1384454 NM BS 578 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 237US 39557 22353 INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK BS 578 AT STRINGER 3 LEFT STRINGER TIE CLIP. REPAIR ED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M) 2 L 7 2 4F A16WE 1996030800493 19960308 00493 NM 1996 3 8 USAA960184 1 19960130 A 5320 693535214 TIE CLIP BOEING 737 737201 1384454 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 237US 39557 22353 INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK BS 747 STRINGER 5 RIGHT, STRINGER TIE CLIP. REPAIRE D PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M) 2 L 7 2 4F A16WE 1996030800494 19960308 00494 NM 1996 3 8 USAA960185 1 19960130 A 5320 693535214 TIE CLIP BOEING 737 737201 1384454 NM BS 767 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 237US 39557 22353 INT - DURING DROP IN VISUAL INSPECTION, FOUND .125 INCH CRACK BS 767 AT STRINGER 6 RIGHT STRINGER TIE CLIP. REPAIRED PE R EO 5393G227. MODIFIED PART NR 69-35352-14. (M) 2 L 7 2 4F A16WE 1996030800495 19960308 00495 NM 1996 3 8 USAA960186 1 19960130 A 5320 693535214 TIE CLIP BOEING 737 737201 1384454 NM BS 767 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 237US 39557 22353 INT - DURING DROP IN VISUAL INSPECTION, FOUND .125 INCH CRACK BS 767 AT STRINGER 10 RIGHT, STRINGER TIE CLIP. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-3535214. (M) 2 L 7 2 4F A16WE 1996030800496 19960308 00496 NM 1996 3 8 USAA960187 1 19960130 A 5320 693535214 TIE CLIP BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 237US 39557 22353 INT - DURING DROP IN VISUAL INSPECTION, FOUND .125 INCH CRACK IN EACH OF 2 CLIPS, BS 727B AT STRINGER 2L AND STRINGER 7L , STRINGER TIE CLIPS. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M) 2 L 7 2 4F A16WE 1996030800497 19960308 00497 NM 1996 3 8 USAA960188 1 19960130 A 5320 693535214 TIE CLIP BOEING 737 737201 1384454 NM BS 685 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 237US 22353 INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK BS 685 STRINGER 3 RIGHT STRINGER TIE CLIP. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M) 2 L 7 2 4F A16WE 1996030800498 19960308 00498 NM 1996 3 8 USAA960189 1 19960130 A 5320 693535214 TIE CLIP BOEING 737 737201 1384454 NM BS 767 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 237US 39227 22353 INT - DURING DROP IN VISUAL INSPECTION, FOUND .125 INCH CRACK IN EACH OF 2 CLIPS BS 767 AT STRINGER 5L AND STRINGER 10L, STRINGER TIE CLIPS. REPAIRED PER EO 5393G227. MODIFIED PART NR 69-35352-14. (M) 2 L 7 2 4F A16WE 1996030800499 19960308 00499 NM 1996 3 8 USAA960190 1 19960130 A 5320 693535214 TIE CLIP BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 237US 39695 22353 INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK TIE CLIP, STRINGER 3R, BS 727. REPAIRED PER EO 5393 G227. MODIFIED PART NR 69-35352-14. (M) 2 L 7 2 4F A16WE 1996030800500 19960308 00500 NM 1996 3 8 USAA960191 1 19960130 A 5330 SKIN BOEING 737 737201 1384454 NM BS 347 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 237US 39695 22353 INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK SKIN BS 347 AT STRINGER 17L. INSTALLED DOUBLERS. R EPAIRED PER EO 5391G-694. (M) 2 L 7 2 4F A16WE 1996030800501 19960308 00501 WP 1996 3 8 USAA960192 1 19960205 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 943VJ 47058 BOS - DURING INSPECTION OF PCI 1366 (FUSELAGE AREA BELOW MED) FOUND .125 INCH CRACK IN THE SKIN AT STATION 200 LONGERON 22L. FERRIED AIRCRAFT TO PIT FOR REPAIRS. INSTALLED CLASS 3 DOUBLER PER SRM 53-04 FIG 12B. (M) 2 L 7 2 4F A6WE 1996030800502 19960308 00502 WP 1996 3 8 USAA960193 1 19960205 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 680 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 943VJ 71351 47058 BOS - DURING INSPECTION OF PCI 949 (UPPER FUSELAGE CROWN INSPECTION) FOUND .5 INCH CRACK IN LONGERON 5R AT STATION 680. AIRCRAFT WAS FERRIED TO PIT FOR REPAIR. REPAIRED LONGERON BY SPLICING PER SRM 53-02 FIG 2 IN PIT. (M) 2 L 7 2 4F A6WE 1996030800503 19960308 00503 WP 1996 3 8 USAA960194 1 19960205 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 180 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 941VJ 71005 47054 BOS - DURING INSPECTION FOR PCI 959 A .125 INCH CRACK IN SKIN COMING FROM RIVET STATION 180 LONGERON 22L. FERRIED AIRCR AFT TO PIT FOR REPAIRS. ACCOMPLISHED EXTERNAL CLASS 3 REPAIR DOUBLER PER SRM 53-04 FIG 12B IN PIT. (M) 2 L 7 2 4F A6WE 1996030800504 19960308 00504 NM 1996 3 8 USAA960195 1 19960103 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 786.5-1016 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 234US 41362 22274 ROA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND CORROSION ON STRINGER 27L, BS 786.5 TO BS 1016. INSTALLED STRINGER SPL ICES, REPAIRED PER SRM 53-10-3. (M) 2 L 7 2 4F A16WE 1996030800505 19960308 00505 WP 1996 3 8 USAA960199 1 19960202 A 5330 SKIN DOUG DC9 DC981 3022081 WP BS 140-160 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 826US 39281 48026 PIT - DURING C-6 INSPECTION, FOUND CORROSION AT LONGERON 22R STATION 140 TO STATION 160 BETWEEN SKIN AND LONGERON. REMO VED DAMAGED AREA AND ACCOMPLISHED LONGERON SPLICE REPAIR AND SKIN DOUBLER REPAIR PER SRM 53-04-12B AND 53-02 FIG 2. (M) 2 L 7 2 4F A6WE 1996030800506 19960308 00506 WP 1996 3 8 USAA960200 1 19960202 A 5330 SKIN DOUG DC9 DC981 3022081 WP BS 1437 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 802US 37838 48036 PIT - DURING Q-4 INSPECTION, FOUND 1 INCH CRACK AT STATION 1437 LONGERON 3R IN FUSELAGE SKIN. INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 27. (M) 2 L 7 2 4F A6WE 1996030800507 19960308 00507 WP 1996 3 8 USAA960201 1 19960202 A 5313 59360501 LONGERON DOUG DC9 DC981 3022081 WP BS 1285-1295 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 802US 37838 48036 PIT - DURING Q-4 INSPECTION, FOUND LEVEL 1 CORROSION ON LONGERON 30 FROM STATION 1285 TO STATION 1295. CORROSION TASK N R C57-53300. CUT OUT CORRODED SECTION OF LONGERON AND ACCOMPLISHED SPLICE REPAIR PER DACO DWG 5936667. (M) 2 L 7 2 4F A6WE 1996030800508 19960308 00508 WP 1996 3 8 USAA960202 1 19960202 A 5313 LONGERON DOUG DC9 DC981 3022081 WP BS 1231-1250 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 802US 37838 48036 PIT - DURING Q-4 INSPECTION, FOUND LEVEL 1 CORROSION AT LONGERON 29L STATION 1231-1250 AROUND AND AT RIVETS. CORROSION TASK NR C57-53300. SPLICED IN NEW SECTION OF LONGERON PER USAIR EA 31905. (M) 2 L 7 2 4F A6WE 1996030800509 19960308 00509 WP 1996 3 8 USAA960203 1 19960202 A 5311 FRAME DOUG DC9 DC981 3022081 WP BS 1154-1211 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 802US 37838 48036 PIT - DURING Q-4 INSPECTION, FOUND CORROSION 3 FEET BY 2 INCHES WIDE ON PREVIOUS REPAIR DOUBLER BETWEEN STATION 1154 - S TATION 1211 AFT CARGO DOOR LOWER FRAME. CORROSION LEVEL 1 TASK NR C57-53300. MANUALLY INSTALLED REPAIR DOUBLERS PER US AIR EO NR 5390M251. (M) 2 L 7 2 4F A6WE 1996030800510 19960308 00510 EU 1996 3 8 USAA960204 1 19960207 A 5315 FLOOR BEAM FOKKER F28 F28MK0100 4990807 EU BS 5305 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 892US 10204 11372 PIT - DURING SCHEDULED CORROSION TRACK VISIT FOUND A CORRODED AREA 1 INCH BY 1.5 INCH AT BL 0 TOP T-EXTRUSION STATION 53 05 FLOOR BEAM. REMOVED T-EXTRUSION FROM FORWARD FACTORY SPLICE OF FLOOR BEAM. INSTALLED NEW SECTION ANS SPLICED AFT EN D WITH 2 EACH DOUBLERS PER USAIR EA NR 32099. (M) 2 L 7 2 4F RT 1996030800511 19960308 00511 NM 1996 3 8 USAA960205 1 19960207 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 967 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 35486 22886 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 45 INCHES CORROSION STATION 967 BL 0 TO RBL 45 FLOOR BEAM. CU TOFF TOP CAP, FABRICATED AND REPAIRED SPLICE AND INSTALLED PER SRM 53-10-9 FIG 2. CORROSION TASK NR C53-107-02, CORROSI ON LEVEL 2. (M) 2 L 7 2 4F A16WE 1996030800512 19960308 00512 NM 1996 3 8 USAA960206 1 19960207 A 5320 6546812170 ANGLE BOEING 737 7372B7 1384560 NM BS 967-947 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 35486 22886 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 20 INCH BY 1 INCH CORROSION AT FLOOR BEAM SUPPORT ANGLE STATION 967 TO 9 47 LBL 12. REPLACED WITH IDENTICAL PART NR 65-46812-170 AND ANGLE, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107 -02, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996030800513 19960308 00513 NM 1996 3 8 USAA960230 1 19960207 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 1006 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 35486 22886 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORROSION FLOOR BEAM STATION 1006, LBL 11 INCHES. SPLI CED IN NEW SECTION OF FLOOR BEAM, REPAIRED PER SRM 53-10-9. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996030800514 19960308 00514 NM 1996 3 8 USAA960231 1 19960207 A 5320 6546812191 FLOOR SUPPORT BOEING 737 7372B7 1384560 NM BS 986.5 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 35486 22886 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 2 INCH CORROSION 8 INCH FLOOR SUPPORT INTERCOSTAL STATION 986. 5 LNL 15 INCHES. REPLACED WITH IDENTICAL PART NR 65-46812-191, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996030800515 19960308 00515 NM 1996 3 8 USAA960232 1 19960207 A 5347 SEAT TRACK BOEING 737 7372B7 1384560 NM BS 1016/986.5 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 35486 22886 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORROSION FLOOR SEAT TRACK BETWEEN STATION 1016 AND STA TION 986.5. INSTALLED NEW SEAT TRACK SECTION, REPAIRED PER SRM 51-10-3. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996030800516 19960308 00516 NM 1996 3 8 USAA960233 1 19960207 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 1016 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 35486 22886 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA FLOOR BEAM UPPER T-CAP BS 1016 LBL 3 INCH ES. INSTALLED T-CAP, REPAIR PLUS 2.6 LB WT CHANGE, REPAIRED PER SRM 53-10-9. CORROSION TASK NR C53-107-02, CORROSION L EVEL 2. (M) 2 L 7 2 4F A16WE 1996030800517 19960308 00517 NM 1996 3 8 USAA960234 1 19960207 A 5313 STRINGER BOEING 737 7372B7 1384560 NM BS 351.2-380 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 35486 22886 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 8 INCH CORRODED AREA ON SIDE OF STRINGER BS 351.2 - BS 380, ST RINGER 28L. REPLACED STRINGER SECTION REPAIRED PER SRM 51-10-1, PAGE 5, STEP 4. CORROSION TASK NR C53-202-01, CORROSIO N LEVEL 2. (M) 2 L 7 2 4F A16WE 1996030800518 19960308 00518 NM 1996 3 8 USAA960235 1 19960207 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 312 GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 35486 22886 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND GOUGE APPROXIMATELY 22 INCHES FLOOR BEAM BS 312, LBL 12 INCHES TO RBL 10 INCHES. CUT OUT DAMAGED AREA AND INSTALLED NEW SECTION WITH REPAIR ANGLES. REPAIRED PER TR 53-10-13. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996030800519 19960308 00519 NM 1996 3 8 USAA960236 1 19960207 A 5320 6546812 ANGLE BOEING 737 7372B7 1384560 NM BS 967-947 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 35486 22886 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 20 INCH BY 1 INCH CORROSION FLOOR SUPPORT ANGLE AT STATIO N967 TO 947 RB L 20. REPAIRED PER SRM 51-10-1. REPLACED WITH IDENTICAL PART NR 65-46812. CORROSION TASK NR C53-107-02. CORROSION LE VEL 2. (M) 2 L 7 2 4F A16WE 1996030800520 19960308 00520 NM 1996 3 8 USAA960237 1 19960207 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 986.5 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 35486 22886 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 1 INCH CORRODED NUT PLATE HOLES 3 FLOOR BEAM, STATION 986.5 R BL 36, LBL 5, RBL 5. INSTALLED DOUBLERS, REPAIR PER SRM 53-10-9 FIG 7. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2 . (M) 2 L 7 2 4F A16WE 1996030800521 19960308 00521 NM 1996 3 8 USAA960238 1 19960207 A 5320 6552878533 ANGLE BOEING 737 7372B7 1384560 NM AFT ENTRY DOOR CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 35486 22886 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 24 INCH CORROSION Z-ANGLE AFT ENTRY DOOR. REPLACED WITH IDENT ICAL PART NR 65-52878-533, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996030800522 19960308 00522 NM 1996 3 8 USAA960239 1 19960207 A 5320 ANGLE BOEING 737 7372B7 1384560 NM AFT ENTRY DOOR CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 35486 22886 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 4 INCH BY 4 INCH CORRODED WEB AFT ENTRY DOOR Z-ANGLE THRESHOLD WEB. FAB RICATED NEW WEB, REPAIRED PER SRM 51-10-1 AND BOEING DRAWING 65-52878. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2 . (M) 2 L 7 2 4F A16WE 1996030800523 19960308 00523 NM 1996 3 8 USAA960240 1 19960207 A 5320 FITTING BOEING 737 7372B7 1384560 NM BS 695 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 35486 22886 INT - DURING Q-6 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND 1.5 INCH CRACK IN FORWARD INBOARD CHORD ANGLE BS 695 FI TTING, WL 202, JUST ABOVE STRINGER 18A RIGHT. INSTALLED PERMANENT ANGLE REPAIR, LESS THAN 1 POUND. REPAIRED PER EA 406 44. (M) 2 L 7 2 4F A16WE 1996030800524 19960308 00524 EU 1996 3 8 USAA960241 1 19960212 A 5311 D31108001 FRAME FOKKER F28 F28MK0100 4990807 EU BS 1491 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 855US 14269 11283 PIT - DURING Q-1 CHECK INSPECTION, FOUND 3 INCH CRACK FRAME STATION 1491 BL 883L HIGH FREQUENCY EDDY CURRENT INSPECTION. STOP DRILLED CRACK AND INSTALLED DOUBLERS PER USAIR EA NR 32077. (M) 2 L 7 2 4F RT 1996030800525 19960308 00525 NM 1996 3 8 USAA960245 1 19960213 A 5330 SKIN BOEING 737 737301 1384611 NM BS 510 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 591US 25451 23936 GSO - DURING DE-ICING VISUALLY FROM DE-ICING BUCKET (DE-ICER DID NTO STRIKE A/C) FOUND 4 INCH CRACK IN SKIN, STATION 510 AT STRINGER 12L. INSTALLED DOUBLER WITH BLIND FASTENERS, REPAIRED PER SRM 53-00-01, 51-40-00. DEFERRED OM-7, NR 32811 . (M) 2 L 7 2 4F RT A16WE 1996030800526 19960308 00526 WP 1996 3 8 USAAD96011A 1 19960125 A 2612 FIRE LOOPS DOUG DC9 DC981 3022081 WP RT ENGINE MALFUNCTIONED A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 807US 48039 TYS - FL 285 - EN ROUTE BNA-BWI, CREW RECEIVED RIGHT ENGINE 'B' LOOP FIRE WARNING. CREW FOLLOWED PILOT HANDBOOK PROCEDU RES. SHORTLY THEREAFTER, THE CREW RECEIVED THE RIGHT AND LEFT 'A' LOOP AND LEFT 'B' LOOP WARNINGS. FLIGHT DIVERTED TO TYS AND LANDED WITHOUT NO FURTHER INCIDENT. MAINTENANCE REPLACED TWO GASKETS ON THE LEFT ENGINE ANTI-ICE DUCTS AND ONE ON THE RIGHT ENGINE DUCT. ALSO, FOUND POSSIBLE SHORT BETWEEN THE RIGHT 'A' AND 'B' LOOPS. BOTH LOOPS WERE REPLACED AS A PRECAUTION. (M) 2 L 7 2 4F A6WE 1996030800527 19960308 00527 WP 1996 3 8 USAAD96013A 1 19960127 A 3040 WINDSHIELD DOUG DC9 DC931 3022065 WP RT COCKPIT MALFUNCTIONED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 921VJ 48141 PHL - FL 2526 - FLIGHT RETURNED TO PHL DUE TO THE FIRST OFFICERS WINDSHIELD HEAT BEING INOPERATIVE. MAINTENANCE COULD N OT FIND A PROBLEM. THE WINDSHIELD HEAT WORKED PROPERLY. (M) 2 L 7 2 4F A6WE 1996030800528 19960308 00528 WP 1996 3 8 USAAD96015A 1 19960201 A 3222 STRUT DOUG DC9 DC981 3022081 WP NLG REQ'D SERVICE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 812US 48092 ORD - FL 904 - AFTER TAKEOFF AND ON GEAR RETRACTION, CREW RECEIVED THREE RED LIGHTS. GEAR WAS CYCLED, CREW RECEIVED GRE EN INDICATIONS FOR THE MAINS BUT A RED FOR THE NOSE GEAR. FLIGHT RETURNED TO ORD AND LANDED WITH NO FURTHER INCIDENT. M AINTENANCE ACCOMPLISHED A STRUT SERVICING PER THE MAINTENANCE MANUAL. (M) 2 L 7 2 4F A6WE 1996030800529 19960308 00529 WP 1996 3 8 USAAD96016A 1 19960201 A 3222 STRUT DOUG DC9 DC981 3022081 WP NLG REQ'D SERVICE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 812US 48092 ORD - FLT 904 - AFTER TAKEOFF AND ON GEAR RETRACTION, CREW COULD NOT RETRACT THE NOSE GEAR. THIS IS THE SECOND RETURN T O FIELD OF THIS FLIGHT ON THIS DAY. MAINTENANCE SERVICED THE NOSE STRUT WHILE ON JACKS, AND THEN SWUNG THE GEAR. AIRCR AFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F A6WE 1996030800530 19960308 00530 WP 1996 3 8 USAAD96017 1 19960202 A 5610 WINDSHIELD DOUG DC9 DC931 3022065 WP RT COCKPIT CRACKED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 922VJ 48142 ORD - FL 979 - FIRST OFFICERS WINDSHIELD CRACKED. FLIGHT RETURNED TO FIELD AND LANDED WITH NO FURTHER INCIDENT. (M) 2 L 7 2 4F A6WE 1996030800531 19960308 00531 WP 1996 3 8 USAAD96017A 1 19960202 A 5610 WINDSHIELD DOUG DC9 DC931 3022065 WP RT COCKPIT CRACKED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 922VJ 34339 48142 ORD FLI 979 - FIRST OFFICERS WINDSHIELD CRACKED. FLIGHT RETURNED TO FIELD AND LANDED WITH NO FURTHER INCIDENT. MAINTEN ANCE REPLACED THE WINDOW HEAT CONTROLLER, P/N 9615059002, AND THE WINDOW. (M) 2 L 7 2 4F A6WE 1996030800532 19960308 00532 WP 1996 3 8 USAAD96018 1 19960204 A 2822 6550934 BOOST PUMP DOUG DC9 DC981 3022081 WP CENTER FUEL TANK FAILED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 814US 39244 5379 48094 CLT - FLT 259 - EN ROUTE LGA-MCO - THE CENTER FUEL TANK BOOST PUMP CIRCUIT BREAKERS FWD 'A' AND 'B' POPPED AND COULD NOT BE RESET. FLIGHT DIVERTED TO CLT DUE TO FUEL CONSIDERATIONS. MAINTENANCE REPLACED THE CENTER FUEL BOOST PUMP. (M) 2 L 7 2 4F A6WE 1996030800533 19960308 00533 WP 1996 3 8 USAAD96019 1 19960204 A 2130 PRESSURIZATION DOUG DC9 DC931 3022065 WP CABIN MALFUNCTIONED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 933VJ 47216 LGA - FLT 8002 - CREW REPORTED, THAT THE AIRCRAFT WOULD NOT PRESSURIZE ABOVE 10,000 FT. FLIGHT DIVERTED TO LGA AND LAND ED WITH NO FURTHER INCIDENT. (M) 2 L 7 2 4F A6WE 1996030800534 19960308 00534 WP 1996 3 8 USAAD96020 1 19960204 A 3230 RETRACT MECH DOUG DC9 DC981 3022081 WP NLG MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 812US 48092 DCA - FLT 2287 - AFTER TAKEOFF AND ON GEAR RETRACTION, CREW COULD NOT RETRACT THE NOSE GEAR. CREW CYCLED THE GEAR TWICE WITH THE SAME RESULT. FLIGHT RETURNED TO DCA AND LANDED WITH NO FURTHER INCIDENT. (M) 2 L 7 2 4F A6WE 1996030800535 19960308 00535 EU 1996 3 8 USAAF96017 1 19960130 A 3260 GEAR WARNING FOKKER F28 F28MK0100 4990807 EU LT MLG ACTIVATED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 862US 11300 STL - FL 1254 - AFTER TAKEOFF FROM STL AND GEAR RETRACTION, CREW RECEIVED MFDU MESSAGE THAT THE LEFT LANDING GEAR WAS NO T UP. GEAR WAS CYCLED WITH THE SAME RESULT. FLIGHT RETURNED TO STL AND LANDED WITH NO FURTHER INCIDENT. AIRCRAFT WAS FERRIED TO PIT. MAINTENANCE CHECKED THE GEAR DOOR SWITCHES AND FOUND NO PROBLEMS. AIRCRAFT WAS JACKED AND GEAR SWUNG T EN TIMES WITH NO FAULTS. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT 1996030800537 19960308 00537 EU 1996 3 8 USAAF96019 1 19960205 A 2612 FIRE LOOP FOKKER F28 F28MK4000 4990810 EU NR 2 ENGINE FAILED A USAA A E UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 EA 19 494US 11167 CAE - FL 0854 - UPON TAKEOFF FROM CAE, CREW RECEIVED AURAL AND VISUAL FIRE WARNINGS ON THE NR 2 ENGINE. CREW SECURED TH E ENGINE AND THE WARNINGS STOPPED. FLIGHT RETURNED TO CAE AND LANDED WITH NO FURTHER INCIDENT. SET 20 MINUTES. REMOVE D AND REPLACED NR 2 OUTBOARD ENGINE DETECTION LOOP. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A20EU 1996030800538 19960308 00538 NM 1996 3 8 USAASB96021 1 19960127 A 3260 106122629 UPLOCK SENSOR BOEING 737 737301 1384611 NM RT MLG WW FAILED A USAA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 EA 19 300AU 23228 MCO - FL 2226 - AFTER TAKEOFF FROM MCO, THE RIGHT MAIN LANDING GEAR RED LIGHT REMAINED ON. FLIGHT RETURNED TO MCO AND L ANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT GEAR UPLOCK SENSOR AND MAIN GEAR RED GEAR CARD. (M) 2 L 7 2 4F RT A16WE 1996030800539 19960308 00539 NM 1996 3 8 USAASB96026 1 19960207 A 5230 6546921199 SEAL BOEING 737 7373B7 1384580 NM CARGO DOOR FAILED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 376US 22955 FLT NR 1075 - PHL - UNABLE TO PRESSURIZE AIRCRAFT IN ANY MODE. OUTFLOW VALVE WAS CONTROLLABLE IN FLIGHT. BUT EVEN WITH OUTFLOW VALVE FULL CLOSED, AIRCRAFT WOULD NOT PRESSURIZE. MAINTENANCE REPAIRED FORWARD CARGO DOOR SEAL PRESSURIZED AIR CRAFT TO 7.6 DIFF. OPS NORMAL. (M) 2 L 7 2 4F RT A16WE 1996030800540 19960308 00540 NM 1996 3 8 USAASB96027 1 19960209 A 5610 PPG5893543109 WINDSHIELD BOEING 737 737401 1384701 NM LT COCKPIT SHATTERED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 407US 12872 23877 TPA - FL 1798 - EN ROUTE CLT-SRQ - THE CAPTAINS OUTER WINDOW PANE SHATTERED. THE FLIGHT DIVERTED TO TPA AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE WINDSHIELD. (M) 2 L 7 2 4F RT A16WE 1996030800541 19960308 00541 WP 1996 3 8 Y2PA96005 1 19960131 A 7711 L680A2 EPR TRANSMITTER DOUG DC9 DC915F 3022037 WP NR 2 ENG FAILED A Y2PA O OTHER O OTHER TO TAKEOFF 1 GL 23 198US 47045 YIP - ON TAKEOFF, THE NR 2 ENGINE WOULD NOT ACCELERATE BEYOND 1.4 EPR. FOUND TO BE AN INDICATION PROBLEM ONLY. REMOVED AND REPLACED EPR TRANSMITTER. SYSTEM OPERATIONAL CHECKED GOOD. (M) 2 L 7 2 4F A6WE 1996030800542 19960308 00542 WP 1996 3 8 Y2PA96006 1 19960202 A 4990 CONNECTOR DOUG DC9 DC915F 3022037 WP APU DEFECTIVE A Y2PA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC NR NOT REPORTED 1 GL 23 198US 47045 YIP - AUXILIARY POWER UNIT (APU) SHUT DOWN AT FLIGHT LEVEL 350, AND WOULD NOT RE-START. LEFT ENGINE GENERATOR INOP (DEF ERRED ITEM NR 0043), APU REQUIRED FOR FLIGHT OPERATION. AIRCRAFT TO YIP. TROUBLESHOT AND FOUND SHORTED PIN (PIN NR F) IN THE APU SPEED SENSE CANNON PLUG. REPLACED DEFECTIVE PIN IN CANNON PLUG, APU OPERATIONAL CHECKED GOOD. PIN NR F IS F OR THE APU LOW OIL PRESSURE TRANSMITTER. LOW OIL PRESSURE WILL SHUT THE APU DOWN. (M) 2 L 7 2 4F A6WE 1996030800545 19960308 00545 SO 1996 3 8 96ZZZX933 1 19960129 A 3231 8401226 HOSE PIPER PA46 PA46310P 7104605 SO DOOR ACTUATOR LEAKING A A BVHA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 07 121RF 2877 4608034 STRATOFLEX, PN 111F4174S0152, DATED 1-8-95 PT 2355. HOSE INSTALLED ON NLG DOOR ACTUATOR. HOSE LEAKING THROUGH SIDEWALL . 1 L 7 1 3O A25SO 1996030800546 19960308 00546 CE 1996 3 8 96ZZZX934 1 19960131 A 5743 5127201 FITTING CESSNA 402 402C 207590R CE LT MLG SUPPORT CRACKED A A APIA K NONE O OTHER IN INSP/MAINT 1 WP 13 6878L 11549 402C0602 FOUND LEFT MAIN GEAR FORWARD SUPPORT CRACKED IN CASTING AT WEB ABOVE TRUNNION BEARING HOLE. THIS ISSUE IS ADDRESSED BY CESSNA SB MEB. SUSPECT THIS CRACK IS CAUSED BY REPEATED HARD LANDINGS. 1 L 7 2 3O A7CE 1996030800568 19960308 00568 CE 1996 3 8 96ZZZX957 1 19960213 A 3244 TIRE GOODYEARAERO LEAR 24 24B 5170306 CE MLG BULGED A DRUA K NONE O OTHER IN INSP/MAINT 1 GL 25 119MA 20 51542211 200 TIRE DEVELOPED A BULGE IN SIDEWALL AFTER A SHORT TIME IN SERVICE. 2 L 7 2 4J A10CE 1996030800569 19960308 00569 CE 1996 3 8 96ZZZX958 1 19960213 A 3244 TIRE GOODYEARAERO LEAR 24 24B 5170306 CE SIDEWALL BULGED A DRUA K NONE O OTHER IN INSP/MAINT 1 GL 25 740EJ 21 52091421 222 TIRE DEVELOPED A BULGE IN THE SIDEWALL AFTER A SHORT TIME IN SERVICE. 2 L 7 2 4J A10CE 1996030800578 19960308 00578 EA 1996 3 8 96ZZZX967 1 19960111 A 5510 C2TP159A BRACKET DHAV DHC2 DHC2MK1 2800102 EA LT H STAB SPAR CRACKED A ERHA K NONE O OTHER IN INSP/MAINT 1 AL 03 4444Z 1307 LEFT HORIZONTAL STABILIZER ATTACH FITTING ON STABILIZER SPAR FOUND CRACKED. INTERGRANULAR CORROSION EVIDENT ON THE COMP LETE LENGTH OF CRACK. PART IS HIGHLY LOADED AND SUBJECT TO STRESS CORROSION. SUBMITTER STATED THIS FITTING SHOULD BE E XAMINED CAREFULLY DURING THE REPETITIVE INSPECTIONS REQUIRED BY AD 92-24-02. THESE FITTINGS ARE REMOVED FOR THE INSPECT ION OF SPAR. 1 H 7 1 3R A806 1996030800582 19960308 00582 NE 1996 3 8 96ZZZX971 2 19960213 A 7200 ENGINE LEAR 25 25 5170506 CE GE CJ610 CJ6106 30006 NE RIGHT ENGINE BIRD STRIKE A ECAA C D ABORTED TAKEOFF RETURN TO BLOCK R C PARTIAL RPM/PWR LOSS F.O.D. TO TAKEOFF 1 EA 11 25EC 026 FLT 1 - AIRCRAFT EXPERIENCED A LOSS OF POWER IN RIGHT ENGINE ON TAKEOFF ROLL FROM FRG. TAKEOFF ABORTED AND AIRCRAFT RET URNED TO MAINTENANCE HANGAR. VISUALLY INSPECTED NR 2 ENGINE. EVIDENCE FOUND OF BIRD STRIKE AND INGESTION. VISUAL DAMA GE TO COMPRESSOR FIRST STAGE. ENGINE TO BE REMOVED FOR REPAIR. 2 L 7 2 4J 4 J A10CE 1E16 1996030800583 19960308 00583 EU 1996 3 8 96ZZZX972 1 19960207 A 7712 311996901 FITTING PILATS PC12 PC12 7090550 EU TORQ SENSE TUBE NOT WELDED A BVHA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 07 263AL 178 112 FOUND LOOSE TORQUE SENSING FITTING WHILE PERFORMING ANNUAL INSPECTION. CLOSE INSPECTION OF TUBE ASSY SHOWED FLARED FITT ING NOT WELDED TO TUBE ASSY. TUBE ASSY INSTALLED IAW P & W SB NR 14185. 1 L 7 1 3T RT A78EU 1996030800585 19960308 00585 NM 1996 3 8 HNAA9695009 1 19960205 A 6123 M817142AC1 TERMINAL BLOCK DHAV DHC8 DHC8102 2809003 NM DC CONTACTOR BOX FAILED A HNAA K NONE J WARNING INDICATION IN INSP/MAINT 1 EA 07 2FOR 23567 070 TPA/TLH - FLT 3448 - DURING AUTOFEATHER TEST, THE LEFT AND RIGHT ALTERNATE FEATHER ADVISORY LIGHTS WOULD NOT ILLUMINATE. REPLACED 2431-TB7 TERMINAL BLOCK IN DC CONTACTOR BOX. (X) 2 H 7 2 4T RT A13NM 1996030800586 19960308 00586 WP 1996 3 8 9605139858 1 19960220 A 5240 FITTING DOUG DC9 DC951 3022051 WP SERVICE DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 767NC 47724 DURING H-CHECK, FOUND A CRACK IN THE FORWARD SERVICE DOOR NR 3 BEAM AFT END FITTING. REPLACED THE FITTING PER SRM 51-30 -2 AND 51-30-5. 2 L 7 2 4F A6WE 1996030800587 19960308 00587 WP 1996 3 8 9605149105 1 19960220 A 5320 FITTING DOUG DC9 DC915 3022036 WP FS 817 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 95S 47205 DURING H-CHECK, FOUND CORROSION ON THE LEFT LAVATORY FITTING ON THE AFT SIDE OF THE FS 817 FRAME. REPLACED FITTING PER SRM 51-30-3. 2 L 7 2 4F A6WE 1996030800588 19960308 00588 NM 1996 3 8 9605155505 1 19960222 A 5320 FITTING BOEING 757 757251 1384970 NM CARGO THRESHOLD CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 505US 23194 DURING T-CHECK, FOUND CORROSION IN AN AFT CARGO DOOR THRESHOLD FITTING, FORWARD FITTING. REPLACED FITTING. 2 L 7 2 4F RT A2NM 1996030800589 19960308 00589 WP 1996 3 8 9605169866 1 19960224 A 5320 STOP FITTING DOUG DC9 DC951 3022051 WP ENTRY DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 775NC 47785 DURING H-CHECK, FOUND A CRACK IN THE AFT ENTRY DOOR STOP FITTING APPROXIMATELY 18 INCHES ABOVE THE FLOOR. REPLACED FITT ING PER SRM 51-30-2. 2 L 7 2 4F A6WE 1996030800590 19960308 00590 WP 1996 3 8 9605179105 1 19960225 A 5320 FITTINGS DOUG DC9 DC915 3022036 WP FS 642 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 95S 47205 DURING H-CHECK, FOUND CORROSION ON THE FS 642 LEFT KEEL FITTINGS AT LONGERON 30 AND OUTBOARD OF LONGERON 29L. REPLACED BOTH FITTINGS PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996030800591 19960308 00591 WP 1996 3 8 9605189105 1 19960226 A 5320 FITTING DOUG DC9 DC915 3022036 WP FS 642 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 95S 47205 DURING H-CHECK, FOUND A CRACK IN THE RIGHT KEEL FITTING FS 642 OUTBOARD OF LONGERON 29R. REPLACED FITTING REF 51-30. 2 L 7 2 4F A6WE 1996030800592 19960308 00592 NM 1996 3 8 9605196601 1 19960226 A 5320 FITTING BOEING 747 747151 1384891 NM FS 1668 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 601US 19778 DURING P-CHECK, FOUND A 2.125 INCH CRACK IN THE NR 4 RIGHT DOOR FORWARD SIDE CUTOUT FITTING BS 1668, 8 INCHES ABOVE THE THRESHOLD. REPLACED FITTING PER SRM 51-10-01 PAR 9. 2 L 7 4 4F A20WE 1996030800593 19960308 00593 WP 1996 3 8 9605209151 1 19960227 A 5320 FITTING DOUG DC9 DC914 3022034 WP FS 200 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8909E 45770 DURING H-CHECK, FOUND CORROSION ON THE CUSP T-FITTING AFT OF THE RIGHT SIDE SERVICE DOOR CUTOUT FS 200. REPLACED FITTIN G PER SRM 51-30-1, 30-5. 2 L 7 2 4F A6WE 1996030800594 19960308 00594 NM 1996 3 8 9605212297 1 19960227 A 5320 FITTING BOEING 727 727251 138408H NM FS 560-600 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 297US 21789 DURING H-CHECK, FOUND CORROSION ON THREE FORWARD CARGO THRESHOLD FITTINGS BS 560, 580 AND 600. REPLACED FITTINGS PER SR M 51-10-01 PG 4 PAR 4A. 2 L 7 3 4F A3WE 1996030800595 19960308 00595 NM 1996 3 8 9605225505 1 19960227 A 5320 FITTING BOEING 757 757251 1384970 NM FS 566 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 505US 23194 DURING T-CHECK, FOUND CORROSION IN A FORWARD CARGO DOOR THRESHOLD FITTING, BS 566. REPLACED FITTING. 2 L 7 2 4F RT A2NM 1996030800596 19960308 00596 NM 1996 3 8 9605232297 1 19960228 A 5320 ATTACH PLATE BOEING 727 727251 138408H NM NLG CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 297US 21789 DURING H-CHECK, FOUND CORROSION ON THE DRAG BRACE SUPPORT BEAM ATTACH PLATE. REPLACED PLATE (P/N 69-45947-1), PER SRM 5 1-10-1 PG 4 PAR 4A. 2 L 7 3 4F A3WE 1996030800597 19960308 00597 WP 1996 3 8 9605249923 1 19960229 A 5330 SKIN DOUG DC9 DC932 3022066 WP FS 237-241 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 927RC 47469 DURING LINE CHECK, FOUND A 3 INCH CRACK IN THE LEFT SIDE WINDOW BELT FS 237 TO 241, 10 O'CLOCK POSITION. REPLACED BELT (P/N 9911531-1), PER SRM 51-01 SEC 1 ITEM C. 2 L 7 2 4F A6WE 1996030800598 19960308 00598 WP 1996 3 8 9605259611 1 19960229 A 5320 FITTING DOUG DC9 DC932 3022066 WP FS 996 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 611NA 47435 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK AND CORROSION IN THE FLOOR SUPPORT CORNER FITTING AT FS 996, LONGERON 18L LBL 50. REPLACED FITTING (P/N 5913100-1), PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996030800599 19960308 00599 WP 1996 3 8 9605279610 1 19960305 A 7711 LG80A2 EPR TRANSMITTER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9 52048 NE NR 2 ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 610NW 33792 980 47432 657568 NR 2 ENGINE EPR INDICATION DID NOT REACH TARGET ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE FLIGHT RETURNED TO THE GATE. MAINTENANCE REPLACED THE EPR TRANSMITTER WITH A SERVICEABLE UNIT. 2 L 7 2 4F 4 F A6WE E2EA 1996030800600 19960308 00600 NM 1996 3 8 9605286718 1 19960304 A 7603 POWER LEVER BOEING 747 747251F 1384898 NM PWA JT9 JT9D7F 52054 NE NR 3 ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 618US 21122 62640 DURING TAKEOFF ROLL, THE NR 3 ENGINE THROTTLE WOULD NOT ADVANCE PAST 80 PERCENT N2. TAKEOFF WAS ABORTED AND THE AIRCRAF T RETURNED TO THE GATE. MAINTENANCE INSPECTED THE NR 3 THROTTLE CABLE AT FUEL CONTROL AND FOUND OK. SEQUENCE MECHANISM AND THRUST LEVER AT FULL TRAVEL, FOUND NORMAL. 2 L 7 4 4F 4 F A20WE E20EA 1996030800601 19960308 00601 WP 1996 3 8 9605299752 1 19960304 A 3350 BATTERIES DOUG DC9 DC941 302207N WP TAIL COMPT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 752NW 47116 DURING LINE CHECK, FOUND ALL TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE OR VERY DIM. REPLACED LAMPS, BATTERIES, POWE R PACKS AND ALL CHECKED GOOD. 2 L 7 2 4F A6WE 1996030800602 19960308 00602 NM 1996 3 8 96FDEA00381 1 19960301 A 5312 6517508224 BLKHD SUPPORT BOEING 727 72722 1384002 NM BS 1342 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 REMOVED VERTICAL CHORD TO ACCESS TERMINAL FITTING AND DISCOVERED CORROSION ON BULKHEAD SUPPORT CHANNEL, BS 1342 WL 238 T O 246 RBL 24. REMOVED AND REPLACED BS 1342 BULKHEAD SUPPORT CHANNEL OF BS 1342 RBL 24 WL 193 TO 258. 2 L 7 3 4F A3WE 1996030800603 19960308 00603 NM 1996 3 8 96FDEA00398 1 19960303 A 5315 FLOOR BEAM BOEING 727 72725C 138400H NM BS 640 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 CABIN FLOOR BEAM CORRODED ON UPPER SURFACE STA 640 BL 0 TO RBL 65. *S/D* REPAIRED IAW SRM 53-10-8 NR0781. 2 L 7 3 4F A3WE 1996030800604 19960308 00604 NM 1996 3 8 96FDEA00399 1 19960303 A 5315 FLOOR BEAM BOEING 727 72725C 138400H NM BS 420 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 CABIN FLOOR BEAM TOP AFT FLANGE CORRODED ON UPPER AND LWR SURFACE STA 420 LBL 0 TO 24. *S/D* REMOVED CORRODED SECTION FAB AND INSTALLED REPAIR PER SRM 53-10-8 FIG 8. 2 L 7 3 4F A3WE 1996030800605 19960308 00605 NM 1996 3 8 96FDEA00400 1 19960303 A 5315 FLOOR BEAM BOEING 727 72725C 138400H NM BS 480 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 CABIN FLOOR BEAM CORRODED ON UPPER FLANGE STA 480 LBL 28. *S/D* REPAIRED CRACKED/CORRODED FLOOR BEAM STA 480 LBL 28 FI G 5. 2 L 7 3 4F A3WE 1996030800606 19960308 00606 NM 1996 3 8 96FDEA00401 1 19960304 A 5230 ACT SUPT FTG BOEING 727 727233 138408A NM CARGO DOOR GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 MCD AFT ACTUATOR SUPT FITTING IS GOUGED IN THREE PLACES. MCD AFT ACTUATOR SUPT FITTING BLENDED WITHIN LIMITS PER DRW NR 65-48200 AND FEDEX SRM 51-10-6 AND 51-10-2. 2 L 7 3 4F RT A3WE 1996030800607 19960308 00607 NM 1996 3 8 96FDEA00402 1 19960304 A 5230 INNER SKIN BOEING 727 727233 138408A NM NR 3 CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 NR 3 CARGO DOOR INNER SKIN HAS A 3 INCH CRACK AFT OF THE FWD EDGE 14 INCHES FROM THE BOTTOM. REMOVED DAMAGED AREA, INST ALLED REPAIR DOUBLER IAW FEDEX SRM 51-40-2. 2 L 7 3 4F RT A3WE 1996030800608 19960308 00608 NM 1996 3 8 96FDEA00403 1 19960304 A 5311 FRAME BOEING 727 727223 1384074 NM BS 520 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 DENT ON UPPER FLANGE OF FRAME AT BS 520 LBL 34 WL 161. 2 L 7 3 4F A3WE 1996030800609 19960308 00609 NM 1996 3 8 96FDEA00404 1 19960304 A 5230 FWD FRAME BOEING 727 727223 1384074 NM CARGO DOOR NICKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 MCD FWD FRAME AND INNER SKIN ARE NICKED AT CENTER OF DOOR. REPAIRED MCD FWD FRAME IAW FEDEX EA NR 7-5230-27785. 2 L 7 3 4F A3WE 1996030800610 19960308 00610 NM 1996 3 8 96FDEA00405 1 19960304 A 5230 AFT FRAME BOEING 727 727223 1384074 NM CARGO DOOR NICKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 MCD AFT FRAME IS NICKED IN TWO PLACES. REPAIRED MCD AFT FRAME IAW FEDEX EA NR 7-5230-27785. 2 L 7 3 4F A3WE 1996030800611 19960308 00611 NM 1996 3 8 96FDEA00406 1 19960304 A 5230 SKIN BOEING 727 727223 1384074 NM CARGO DOOR NICKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 MCD INNER SKIN IS NICKED AT THE AFT EDGE 46 INCHES FROM THE BOTTOM. 2 L 7 3 4F A3WE 1996030800612 19960308 00612 NM 1996 3 8 96FDEA00407 1 19960305 A 5531 MID SPAR BOEING 727 72722 1384002 NM VERT STAB WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 VERTICAL FIN MID SPAR, STR 7 AND PANEL SUPPORT HAS WORN FASTENER HOLE AT FIN STA 225.707 RT. REPAIRED PER FEDEX EA 7-55 10-27728. 2 L 7 3 4F A3WE 1996030800613 19960308 00613 NM 1996 3 8 96FDEA00408 1 19960305 A 5320 651757011 MOPSILL BOEING 727 727233 138408A NM BS 295-304 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 FOUND MOPSILL AT WL 208 BS 295 TO 304 LBL 50 IS CRACKED. REMOVED AND REPLACED MOPSILL WL 208 BS 295 TO 304 LBL 50. 2 L 7 3 4F RT A3WE 1996030800630 19960308 00630 WP 1996 3 8 ABXA9600242 1 19960305 A 2510 5641031533 SEAT DOUG DC8 DC863 302198A WP RT COCKPIT LACK OF LUBE A ABXA K NONE O OTHER CR CRUISE 1 GL 23 819AX 45927 FIRST OFFICER'S SEAT WILL NOT STAY IN A LOCKED POSITION. LUBRICATED FIRST OFFICER'S SEAT, OPS CHECK GOOD IN ALL POSITIO NS. 2 L 7 4 4F 4A25 1996030800631 19960308 00631 WP 1996 3 8 ARWA9603001 1 19960306 A 2910 B-NUT DOUG DC8 DC863 302198A WP LT MLG WW LEAKING A ARWA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 19 345JW 46042 AFTER TAKEOFF GOT SLOW LOSS OF HYD FLUID, QTY ALMOST TO STANDPIPE. TROUBLESHOT FOUND LINE LEAKING AT PRESSURE SERVICING CHECK VALVE B-NUT LOOSE. TIGHTENED B-NUT, SERVICE MAIN SYSTEM AND NO LEAKS NOTED. 2 L 7 4 4F 4A25 1996030800632 19960308 00632 WP 1996 3 8 MWEA96053 1 19960302 A 5312 BLKHD STIFFENER DOUG DC9 DC914 3022034 WP AFT PRESS BLHKD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING INSPECTION, FOUND RADIAL STIFFENER CRACKED AT 9 O'CLOCK POSITION ON AFT PRESSSURE BULKHEAD. INSTALLED DOUBLE ANG LE REPAIR IAW SRM 53-01 FIG 2 SHT 4. 2 L 7 2 4F A6WE 1996030800633 19960308 00633 WP 1996 3 8 MWEA96054 1 19960305 A 2560 5917689103 SLIDE COVER DOUG DC9 DC932 3022066 WP FWD ENTRY DOOR FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 401ME 47133 CREW REPORTS, FWD ENTRY DOOR EVAC SLIDE COVER FELL OFF. REINSTALLED EVAC SLIDE COVER. 2 L 7 2 4F A6WE 1996030800634 19960308 00634 NM 1996 3 8 P5CA00155 1 19960306 A 2840 BAC12CF2A RELAY BOEING 747 747122 1384872 NM FUELING PANEL INOP A P5CA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 23 853FT 19753 ON CLIMBOUT FL 20.0, LOST ALL POWER TO ENGINE FUEL PANEL, WITH NO GAUGE MOVEMENT AND NO GAUGE PRESSURE TO TEST. ON LAND ING, AFTER APPROX 4 MINUTES TAXI, ALL POWER CAME BACK AND FUEL QUANTITY GAUGES RAN DOWN TO ACTUAL FUEL. FOUND FAULTY R9 96 RELAY AND REPLACED RELAY IAW WPM 28-21-01. ALL INDICATIONS CHECKED OK ON ENGINE GROUND RUN AND WITH AIRCRAFT IN FLIG HT MODE. 2 L 7 4 4F A20WE 1996030800635 19960308 00635 NM 1996 3 8 P5CA9600154 1 19960303 A 2450 10608061025 CIRCUIT BREAKER BOEING 747 747123 1384873 NM COCKPIT FAILED A P5CA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 23 859FT 20326 AIRCRAFT RETURNED TO BLOCKS DUE TO FAILURE OF ALL RADIO/AIR DATA INSTRUMENTS ON CAPTAIN'S SIDE. FOUND ESSENTIAL RADIO B US C/B OPEN, DUE TO HISTORY OF C/B OPENING REPLACED C/B. CHECKED SYSTEM PER MM 34-13-00 AND 24-50-02. 2 L 7 4 4F A20WE 1996030800636 19960308 00636 WP 1996 3 8 SCNA96029 1 19960303 A 2611 72130001010 SMOKE DETECTOR DOUG DC10 DC1010 3022110 WP NR 8 LAV FAILED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 573SC 46905 THE SMOKE DETECTOR IN LAVATORY NUMBER 8 WAS FOUND TO SOUND INTERMITTENTLY. CLEANED OPTICAL LENS AND DETECTOR, OPS CHECK ED GOOD. 2 L 7 3 4F A22WE 1996030800637 19960308 00637 NE 1996 3 8 9605301157 2 19960204 A 7230 COMPRESSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 3 ENGINE STALLED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 01 157US 46766 86170 DURING TAKEOFF, THE NR 3 ENGINE STALLED AND TAKEOFF WAS ABORTED. AIRCRAFT RETURNED TO GATE AND BORESCOPE OF NR 3 ENGINE REVEALED NO TROUBLE. REPLACED THE NR 3 EVC AND PRECISION TRIMMED. OPERATIONAL CHECK WAS NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A22WE E20EA 1996030800638 19960308 00638 WP 1996 3 8 9605319959 1 19960304 A 3350 6014113 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 919RW 47162 DURING LINE MAINTENANCE INSPECTION, FOUND AFT SECTION OF FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996030800639 19960308 00639 WP 1996 3 8 9605329938 1 19960305 A 3350 60030451 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 1798U 47369 DURING LINE MAINTENANCE INSPECTION, FOUND AFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERA TIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996030800640 19960308 00640 WP 1996 3 8 9605339967 1 19960305 A 3350 60030451 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9331 47263 DURING LINE MAINTENANCE INSPECTION, FOUND MAIN CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE AT ROWS 12 AND 14. REPLACE D BATTERY PACK. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996030800641 19960308 00641 EU 1996 3 8 96UAL900162 1 19960305 A 3350 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2500 V2527A5 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 406UA 454 EMERGENCY LIGHT TEST FAILED. REPLACED FWD EMERGENCY POWER SUPPLY UNIT. 2 L 7 2 4F RT A28NM E40NE 1996030800642 19960308 00642 WP 1996 3 8 96UAL900163 1 19960305 A 3350 BATTERY PACK DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1811U 46610 EEL LIGHTS WOULD NOT TEST PER NR 2 SERVICE. REPLACED BOTH MID FWD AND AFT BATTERY PACKS. 2 L 7 3 4F 4 F A22WE E23EA 1996030800643 19960308 00643 NM 1996 3 8 96UAL900164 1 19960305 A 2121 FAN JOY MANUFACT 5007024620MO BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 7294U OM847 21572 ELECTRICAL FUMES NOTICED IN CENTER OF CABIN, COULD NOT ISOLATE CAUSE. FOUND GASPER FAN POPPING CIRCUIT BREAKER. REPLAC ED GASPER FAN. OPERATIONALLY CHECKED OKAY AND NO ODOR NOTICED. 2 L 7 3 4F 4 F A3WE E2EA 1996030800644 19960308 00644 NM 1996 3 8 96UAL900165 1 19960305 A 3350 BATTERY PACK BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN DISCHARGED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 392UA 24667 NR TWO LEFT DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK. CHECKS O.K. 2 L 7 2 4F 4 F RT A16WE E2GL 1996030800645 19960308 00645 NM 1996 3 8 96UAL900166 1 19960305 A 3350 LIGHT BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE CABIN DISCONNECTED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 9004U 19042 NR ONE LEFT DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REINSTALLED EXIT LIGHT AT DOOR ONE LEFT. CHECKS O.K. 2 L 7 2 4F 4 F A16WE E2EA 1996030800646 19960308 00646 1996 3 8 96UAL900167 4 19960305 A 2565 SLIDE BF GOODRICH 7A14401 BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE ALL TUBES FAILED TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 4727U G1043 19883 SLIDE FAILED AIR RETENTION TEST DURING OVERHAUL. AIR RETENTION FAILED DUE TO SLIDE POROSITY. SLIDE SCRAPPED. 2 L 7 4 4F 4 F A20WE E20EA 1996030800647 19960308 00647 1996 3 8 96UAL900168 4 19960305 A 2565 SLIDE BF GOODRICH 7A14381 BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE ALL TUBES FAILED TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 4717U G1030 19878 SLIDE FAILED AIR RETENTION TEST DURING OVERHAUL. AIR RETENTION FAILED DUE TO SLIDE POROSITY. SLIDE SCRAPPED. 2 L 7 4 4F 4 F A20WE E20EA 1996030800648 19960308 00648 1996 3 8 96UAL900169 4 19960305 A 2565 SLIDE BF GOODRICH 7A14381 BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE ALL TUBES FAILED TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 4735U G1043 19928 SLIDE FAILED AIR RETENTION TEST DURING OVERHAUL. FAILED DUE TO POROSITY. SLIDE SCRAPPED. 2 L 7 4 4F 4 F A20WE E20EA 1996030800649 19960308 00649 NM 1996 3 8 96UAL900170 1 19960306 A 2612 FIRE LOOP BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE OUT OF POSITION A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7281U 21559 NR 1 ENGINE FIRE DETECTION SYSTEM INOPERATIVE. SQUIB TEST REMAINS ON FOR A SHORT TIME AFTER TEST. FOUND LOWER LOOP RUB BING AGAINST ENGINE COWLING. REPOSITIONED LOOP, FIRE DETECTION SYSTEM CHECKS OKAY. 2 L 7 3 4F 4 F A3WE E2EA 1996030800650 19960308 00650 1996 3 8 96UAL900171 4 19960306 A 2565 SLIDE/RAFT AIR CRUISER 24D30051101 DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 3 FAILED TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1834U 1573 47966 NR 3 RT SLIDE/RAFT REMOVED FOR TIME EXPIRATION. UNIT FAILED THE AIR RETENTION TEST DUE TO LEAKING AROUND THE COMMUNICAT OR TUBE. RETURNED UNIT TO MANUFACTURER FOR REPAIR. 2 L 7 3 4F 4 F A22WE E23EA 1996030800651 19960308 00651 SO 1996 3 8 COMA9610094 1 19960306 A 2910 7588717 FILTER EMB 120 EMB120RT SO LT HYD SYST DIRTY A COMA K NONE J WARNING INDICATION UK UNKNOWN 1 SO 01 256CA 120245 LEFT HYDRAULIC SYSTEM FILTER BYPASS WARNING ILLUMINATED. REPLACED HYDRAULIC SYSTEM FILTER. 2 L 7 2 4T RT A31SO 1996030800652 19960308 00652 WP 1996 3 8 COMA9620004 2 19960303 A 7313 3103235 NOZZLE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP RT ENGINE DIRTY A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 704C AC704 RT ENGINE WILL NOT ACHIEVE CHARTED TAKEOFF TORQUE. REPLACED THE ENGINE FUEL NOZZLES. POWER ASSURANCE RUNS NORMAL AND A CFT RETURNED TO SERVICE. 1 L 7 2 4T 4 T A8SW E4WE 1996030800653 19960308 00653 EU 1996 3 8 COMA9630051 1 19960305 A 3020 NH24668073 INLET DUCT SAAB SF340 SF340A 7850100 EU LT ENGINE BURNED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 344CA 37 340A025 LEFT ENGINE INLET ANTI-ICE IS INOPERATIVE. REPLACED LOWER INLET ASSY. PART TOTAL CYCLES, 45. 2 L 7 2 4T RT A52EU 1996030800654 19960308 00654 EU 1996 3 8 COMA9630052 1 19960305 A 2613 OVERHEAT WARNING SAAB SF340 SF340A 7850100 EU RT ENGINE ACTIVATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 343CA 340A024 RIGHT ENGINE TAIL PIPE HOT WARNING CAME ON SHORTLY AFTER TAKEOFF. FOUND NO DEFECTS WITH FIRE DETECTION SYSTEM. AIRCRAF T WAS IN HEAVY RAIN. MOISTURE WAS SUSPSECTED CAUSE OF FALSE WARNING. 2 L 7 2 4T RT A52EU 1996030800655 19960308 00655 NE 1996 3 8 COMA9630053 2 19960306 A 7260 CHIP LIGHT SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RT ENGINE ILLUMINATED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 146CA 21 340A146 367470 RT ENGINE CHIP DETECTOR WARNING ILLUMINATED. DEBRIS ON CHIP DETECTOR WAS DETERMINED TO BE WITHIN M/M LIMIITATIONS. ACF T RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE6 1996030800656 19960308 00656 EU 1996 3 8 COMA9630054 1 19960306 A 2613 OVERHEAT LIGHT SAAB SF340 SF340A 7850100 EU LT ENGINE ILLUMINATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 358CA 340A047 LEFT ENGINE TAIL PIPE HOT WARNING LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF. FOUND NO DEFECTS WITH AIRCRAFT OR TAIL PIPE HOT WARNING SYSTEM. SUBMITTER STATED CAUSE OF FALSE WARNING IS MOISTURE. ACFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 1996030800657 19960308 00657 EU 1996 3 8 COMA9630055 1 19960306 A 7712 CTOT SAAB SF340 SF340A 7850100 EU LT ENGINE FAILED A COMA C ABORTED TAKEOFF M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 SO 01 356CA 340A034 LEFT ENGINE ITT REACHED 934 DEGREES DURING TAKEOFF. FOUND CONSTANT TORQUE ON TAKEOFF SYSTEM DEFECTIVE. PLACED CTOT SYS TEM ON DEFERRED MAINTENANCE LIST. ACFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 1996030800658 19960308 00658 EU 1996 3 8 COMA9630056 1 19960306 A 3020 NH24668081 INLET SAAB SF340 SF340A 7850100 EU RT ENGINE BURNED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 341CA 11531 957 340A021 RT ENGINE INLET HEAT FAILED. REPLACED THE LOWER INLET ASSY. PART TOTAL CYCLES, 12,972. 2 L 7 2 4T RT A52EU 1996030800659 19960308 00659 EA 1996 3 8 COMA9660035 1 19960306 A 3010 124112450 SWITCH CNDAIR CL600 CL6002B19 EA RT WING SHORTED WIRE A COMA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 918CA 7018 RT WING ANTI-ICE DUCT WARNING COMES ON INTERMITTENTLY. INSTALLED INSULATION BOOT OVER BARE WIRE TERMINALS ON DUCT LEAK SENSOR 28 WK. THESE SENSORS HAVE BARE WIRE TERMINALS AND ARE INSTALLED IN EXTREMELY CLOSE PROXIMITY TO STRUCTURE AND WI RE BUNDLES WHICH CAN COVER SHORTS TO GROUND. 2 L 7 2 4F RT A21EA 1996030800660 19960308 00660 EA 1996 3 8 COMA9660036 1 19960306 A 3260 GEAR INDICATION CNDAIR CL600 CL6002B19 EA NLG MALFUNCTIONED A COMA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 01 948CA 7079 NOSE LANDING GEAR DISAGREE MESSAGE ON EICAS WHEN GEAR SELECTED DOWN. COULD NOT DUPLICATE DISCREPANCY. CLEANED NLG AND ACFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1996030800661 19960308 00661 NM 1996 3 8 DL72K960488 1 19960228 A 5754 RIB BOEING 727 727232 1384082 NM NR 4 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 415DA 21257 NA FOUND ON MV1 CHECK, REFERENCE EO 04-05512-12 OPN 0304, WHILE BORESCOPING SLAT TRACK BOLT HOLES, FOUND .75 INCH CRACK IN L/E RIB NR 4 SLAT AT I/B TRACK I/B RIB. REPAIR: REPAIRED PER M/M 57-54-00, FIG 813A. 2 L 7 3 4F A3WE 1996030800662 19960308 00662 NM 1996 3 8 DL72K960489 1 19960222 A 5240 FRAME BOEING 727 727232 1384082 NM L 2 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 415DA 21257 NA FOUND ON MV1 CHK L-2 DOOR S/N 1097 HAS .50 INCH CRACK AT FWD FRAME UPPER HINGE CUTOUT. REPAIR: REPAIRED PER SRM 52-40- 2, FIG 4. 2 L 7 3 4F A3WE 1996030800663 19960308 00663 NM 1996 3 8 DL72L960498 1 19960305 A 2782 CASTING BOEING 727 727232 1384082 NM NR 2 SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 505DA 21307 FOUND ON D1 LETTER CK, NR 2 SLAT ACTUATOR MOUNT CASTING/ANGLE CRACKED O/B UPPER EAR. REPAIRED PER MM 57-42-0. 2 L 7 3 4F A3WE 1996030800664 19960308 00664 NM 1996 3 8 DL72L960499 1 19960305 A 2782 ANGLE BOEING 727 727232 1384082 NM NR 6 FLAP ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 505DA 21307 FOUND ON D1 LETTER CK, NR 6 L/E FLAP ACTUATOR SUPPORT BOX CRACKED INBD END. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1996030800665 19960308 00665 NM 1996 3 8 DL72L960500 1 19960305 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 7 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 505DA 21307 FOUND ON D1 LETTER CK, NR 7 SLAT LOWER ANGLE CRACKED AT THE ANTI-ICE DUCT CUTOUT. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1996030800666 19960308 00666 NM 1996 3 8 DL72S960440 1 19960227 A 8010 SWITCH BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE DEFECTIVE A DALA D RETURN TO BLOCK X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 SO 27 496DA 21076 688660 WITH NR 1 AND NR 2 ENGINES RUNNING, STARTED NR 3 ENG AND THEN NR 2 FLAMED OUT. RESET FUEL SHUTOFF VALVE CIRCUIT BREAKER AND STARTED ENG, CONTRACT MTC CKD FUEL S/O VLV OPERATION. CKD ENG FOR FUEL LEAKS. CKD INTAKE/EXHAUST. ALL OK. START ED ENG SEVERAL TIMES, ALL WAS NORMAL. SUBSEQUENT OCCURRENCE, MTC FOUND DEFECTIVE START LEVER SWITCH. REPLACED SWITCH O PERATION NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1996030800667 19960308 00667 NM 1996 3 8 DL72S960501 1 19960301 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 7 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 416DA 21258 FOUND ON C1 LETTER CK, FOUND 1.25 INCH CRACK AT NR 7 SLAT I/B TRACK BOX INBD ANGLE. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1996030800668 19960308 00668 NM 1996 3 8 DL72S960502 1 19960301 A 5320 WEB BOEING 727 727232 1384082 NM BS 1235/1263 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 416DA 21258 FOUND ON C1 LETTER CK, TORQUE BOX WEB CRACKED .50 INCH AT STA 1235, LT, AND .1250 INCH AT STA 1263 RT. REPAIRED PER MM 53-11-0. 2 L 7 3 4F A3WE 1996030800669 19960308 00669 NM 1996 3 8 DL72S960509 1 19960305 A 5311 6556124 FRAME BOEING 727 727232 1384082 NM FS 950 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 546DA 22677 DURING A MID-VISIT, THE FRAME AT STATION 950F WAS FOUND WITH A DENT LOCATED NEAR STRINGER 25L AND A .25 INCH CRACK EMANA TING FROM A TOOLING HOLE OUTBOARD OF STRINGER 27L. FRAME WAS SPLICED FROM THE FACTORY SPLICE AT STRINGER 25L TO JUST OU TBOARD OF STRINGER 27L. PER DL ERA 303258-14AD. 2 L 7 3 4F A3WE 1996030800670 19960308 00670 NM 1996 3 8 DL72S960512 1 19960304 A 3350 LIGHT BOEING 727 727232 1384082 NM CABIN LOOSE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 407DA 21151 ON PRE-FLIGHT, FOUND SECTION OF TRACK LIGHTING LOOSE WITH EXPOSED WIRING. REPAIRED WIRING SECURED TRACK, OPERATION NORM AL. 2 L 7 3 4F A3WE 1996030800671 19960308 00671 NM 1996 3 8 DL73E960493 1 19960302 A 3350 TRACK 081691 BOEING 737 737247 138448D NM CABIN MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 381DL 23608 NA EMERGENCY FLOOR TRACK LIGHT AT ROW 26 MISSING. REPLACED SOCKET, BULB AND MODULE OPERATIONAL TEST NORMAL. 2 L 7 2 4F A16WE 1996030800672 19960308 00672 NM 1996 3 8 DL73S960492 1 19960302 A 3350 LIGHT 081691 BOEING 737 737232 1384475 NM CABIN MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 306DL 23078 NA EMERGENCY TRACK LIGHT AT 19DEF INOPERATIVE. LIGHT SOCKET AND BULB MISSING. REPLACED SOCKET AND BULB OPERATIONAL TEST N ORMAL. 2 L 7 2 4F RT A16WE 1996030800673 19960308 00673 NM 1996 3 8 DL767960487 1 19960304 A 2910 PRESS LINE AE70577778 BOEING 767 767232 1385132 NM NR 2 ENGINE LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 104DA 22216 LEFT HYDRAULIC SYSTEM FAILURE IN-FLIGHT. RETURNED DFW. FOUND ENGINE PRESSURE LINE WITH HOLE IN IT. REPLACED LINE. 2 L 7 2 4F RT A1NM 1996030800674 19960308 00674 NM 1996 3 8 DL76L960505 1 19960305 A 5414 311T3450 SKIN BOEING 767 767332 1382001 NM PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 173DN 24800 TWO ADDITIONAL CRACKS WERE FOUND AT HMV, 2/96. ONE CRACK IS IN THE NR 2 PYLON, RT SKIN AND DOUBLER, AND IS 1.38 INCHES LONG, RUNNING DIAGONALLY UP AND AFT FROM THE UPPER AFT CORNER OF THE FWD TORQUE BOX ACCESS OPENING AT NAC STA 170. THE SECOND CRACK IS IN THE NR 1 PYLON RT SKIN ONLY AND IS 1.63 INCHES LONG, RUNNING DIAGONALLY UP AND AFT FROM THE AFT UPPER CORNER OF THE FORWARD TORQUE BOX ACCESS HOLE AT NAC STA 170. ACCOMPLISHED REPAIRS PER DL ERA 273175-14 REV D. 2 L 7 2 4F RT A1NM 1996030800675 19960308 00675 NE 1996 3 8 MWEA96055 2 19960306 A 7320 PT 2 LINE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7B 52053 NE NR 1 ENG ICE BUILDUP A MWEA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 31 202ME 47672 649674 PILOT REPORTS UPON SPOOLING UP FOR TAKEOFF, THE NR 1 ENGINE EPR WOULD NOT RISE ABOVE 1.4 INDICATED. ALL OTHER PARAMETER S NORMAL. RETURN TO GATE. FOUND ICE IMBEDDED IN PT2 INLET. CLEANED ICE. RAN ENGINE TO TAKEOFF POWER. OPS CHECK GOOD . 2 L 7 2 4F 4 F A6WE E2EA 1996030800676 19960308 00676 NM 1996 3 8 SCNA96030 1 19960304 A 2612 656020911 FIRE DET UNIT BOEING 727 7272A1 138407F NM NR 1 ENGINE FAILED A SCNA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 GL 15 287SC 21345 THE NR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED AND BELL SOUNDED. SHUT DOWN NR 1 ENGINE AND BLEW ONE FIRE BOTTLE. REMOV ED AND REPLACED NR 1 ENGINE FIRE B-LOOP AND FIRE DETECTION UNIT. FIRE DETECTION SYSTEM TESTED GOOD. 2 L 7 3 4F A3WE 1996030800677 19960308 00677 SO 1996 3 8 SWIA95719 1 19960223 A 3260 PROX SENSOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT MLG MALFUNCTIONED A SWIA O OTHER N FALSE WARNING CR CRUISE 1 NM 07 203SW 120240 HAD TO USE THE ABNORMAL LANDING GEAR EXTENSION TO GET THE GEAR DOWN. REMOVED AND REPLACED RIGHT MAIN DOWNLOCK PROXIMITY SENSOR. CYCLED GEAR NINE TIMES. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1996030800678 19960308 00678 SO 1996 3 8 SWIA95720 1 19960226 A 2910 PRESS LINE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE GREEN HYD SYST FAILED A SWIA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 07 232SW 120306 GREEN HYDRAULIC SYSTEM FAILED IN-FLIGHT. WHEN EMERGENCY GEAR EXTENSION PROCEDURE WAS ATTEMPTED, GEAR WOULD NOT LOWER. G EAR DOORS WOULD NOT OPEN. ABNORMAL LANDING GEAR SEQUENCE WAS PERFORMED IN ORDER NUMEROUS TIMES. GEAR DOORS WERE NOTED CLOSED. REPLACED HYDRAULIC PRESSURE LINE AT GREEN SYSTEM PACK. SERVICED GREEN HYDRAULIC SYSTEM. OPERATED ELECTRIC AND ENGINE DRIVEN PUMPS. FOUND PRESSURE GOOD. REMOVED ALL FOUR FILTERS AT GREEN RESERVOIR. FOUND NO METAL CONTAMINATION ON FILTERS OR IN FLUID. CYCLED GEAR IN NORMAL CONDITION. ALL CHECKS GOOD. PERFORMED NUMEROUS EMERGENCY EXTENSIONS AND ALL CHECKD GOOD. NO LEAKS NOTED FROM LINE. 2 L 7 2 4T 4 T RT A31SO E20NE 1996030800679 19960308 00679 SW 1996 3 8 SWIA95721 1 19960302 A 2720 CONTROL CABLE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP RUDDER FAILED A SWIA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 685AV AC685 ON TAXI IN FELT POP IN RUDDER PEDALS. ON FURTHER INSPECTION, FOUND THE RUDDER PEDALS NO LONGER MOVE THE RUDDER. REPLAC ED RIGHT AFT RUDDER CABLE. ADJUSTED TENSION, CHECKED RIGGING. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A8SW E4WE 1996031200001 19960312 00001 WP 1996 3 12 96UPS805611 1 19960219 A 5752 5717798502 AILERON TAB DOUG DC8 DC871F 302199D WP RT AILERON DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 783UP 45973 DURING 'C' CHECK MAINTENANCE REPORTED, RT AILERON TRIM IS DELAMINATED. REPLACED TAB ASSY PER MM 27-12-01-4. 2 L 7 4 4F RT 4A25 1996031200002 19960312 00002 WP 1996 3 12 96UPS805610 1 19960221 A 5320 47752621 ANGLE DOUG DC8 DC871F 302199D WP FS 902 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 783UP 45973 DURING 'C' CHECK MAINTENANCE REPORTED, KEEL BEAM LOWER ATTACH ANGLE CRACKED ON BOTH SIDES AT FS 902. REPLACED ANGLE PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996031500001 19960315 00001 WP 1996 3 15 9605349971 1 19960306 A 5220 591015931 EMER EXIT DOOR DOUG DC9 DC931 3022065 WP CABIN OUT OF RIG A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9335 47337 DURING M-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE LEFT AFT OVERWING EMERGENCY DOOR AND THAT INADEQU ATE FORCE WAS REQUIRED TO RELEASE THE LEFT FORWARD, RIGHT FORWARD, AND RIGHT AFT OVERWING EMERGENCY EXITS. RERIGGED ALL DOORS PER MM 52-21-0. CHECKED OK. 2 L 7 2 4F A6WE 1996031500002 19960315 00002 NM 1996 3 15 9605356628 1 19960306 A 2612 FIRE WARNING BOEING 747 747251B 1384892 NM PWA JT9 JT9D7R4G2 52054 NE NR 4 ENGINE ILLUMINATED A NWAA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 GL 01 628US 22389 15257 THE NR 4 ENGINE EXPERIENCED HIGH NACELLE TEMPERATURE. THE FORWARD PANEL FIRE DETECTOR ILLUMINATED, BUT THE FIRE WARNING BELL DID NOT ACTIVATE. CREW FOLLOWED COCKPIT OPERATING PROCEDURE, SHUT ENGINE DOWN, DUMPED 170,000 POUNDS OF FUEL, AND DIVERTED TO MSP WITHOUT FURTHER INCIDENT. FOUND BLOW-OUT DOORS MISSING ON LEFT COWL OF THE NR 4 ENGINE. AIRCRAFT WAS S CHEDULED FOR NR 4 ENGINE CHANGE. 2 L 7 4 4F 4 F A20WE E3NE 1996031500003 19960315 00003 EU 1996 3 15 9605363235 1 19960306 A 3240 C20216332292C BSCU AIRBUS 320 A320211 3930320 EU AVIONICS COMPT. MALFUNCTIONED A NWAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 01 335NW 6604 1555 340 DURING TAXI IN AT THE GATE, THE BRAKES DID NOT RESPOND. USED ENGINE THRUST REVERSE TO STOP AIRCRAFT SAFELY AT THE GATE. THE BRAKES GRABBED AS THE AIRCRAFT CAME TO A STOP. MAINTENANCE REPLACED THE BRAKE STEERING CONTROL UNIT. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996031500004 19960315 00004 NM 1996 3 15 9605376719 1 19960308 A 3244 260356113 TIRE RECAP BOEING 747 747251F 1384898 NM BODY LAND GEAR SEPARATED A NWAA K NONE O OTHER LD LANDING 1 GL 01 619US 12943 157 21321 DURING LANDING, THE NR 7 BODY LANDING TIRE RECAP SEPARATED CAUSING DAMAGE TO SECTION 46 BODY FAIRING, OUTBOARD BODY GEAR DOOR ROD, AND THE LEFT BODY GEAR BRAKE LINE. INSTALLED NEW TIRE, BRAKE LINE, DOOR ROD, AND REPAIRED BODY FAIRING. OPE RATIONAL CHECK GOOD. TOTAL CYCLES, 2,045. 2 L 7 4 4F A20WE 1996031500005 19960315 00005 NM 1996 3 15 96FDEA00461 1 19960308 A 2780 POSITION SWITCH BOEING 727 727233 138408A NM NR 2 LE FLAP OUT OF ADJUST A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 271FE 22036 ON DEPARTURE WHEN FLAPS RETRACTED TO 2 DEGREES, THE NR 2 LEADING EDGE DEVICE REMAINED EXTENDED. WHEN FLAPS WERE RETURNE D TO 5 DEGREES THE LEADING EDGE DEVICES WERE NORMAL. C/A: FOUND NR 2 LEADING EDGE FLAP POSITION SWITCH OUT OF ADJUSTME NT. ADJUSTED NR 2 FLAP SWITCH IN ACCORDANCE WITH MAINTENANCE MANUAL 27-82-1, PAGES 402-403. OPERATIONAL CHECK NORMAL, REQUIRED ITEMS INSPECTED. 2 L 7 3 4F RT A3WE 1996031500006 19960315 00006 NM 1996 3 15 96FDEA00462 1 19960307 A 5320 6516338 WEB BOEING 727 727233 138408A NM BS 950 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CRACK IN WEB AT BS 950A + 17, BL ZERO, WL 203.5. ****S/D***** AT BS 950A + 17, BL ZERO, WL 203.5, REMOVED DAMAGED AREA. FABRICATED REPAIR WEB AND INSTALLED PER FEDEX SRM 51-40-2. 2 L 7 3 4F RT A3WE 1996031500007 19960315 00007 NM 1996 3 15 96FDEA00463 1 19960112 A 5311 65B3F0666 FRAME BOEING 747 747245F 1384897 NM BS 1660 CRACKED A FDEA K NONE O OTHER CL CLIMB 1 SO 25 640FE 20826 MAIN DECK CRACK FOUND PROPAGATED BEYOND THE STOP DRILL ON THE FRAME AT BS 1660 AT S13R. C/A: FRAME REPLACED PER DWG 65 B00146. 2 L 7 4 4F A20WE 1996031500008 19960315 00008 NM 1996 3 15 96UAL900172 1 19960307 A 5230 DOOR HANDLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO DOOR NOT SECURED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 312UA 23673 UNABLE TO CONTROL CABIN PRESSURE IN ANY MODE. AFT PIT DOOR RELEASE HANDLE UNDER PIT DOOR SEAL. SECURED HANDLE, PRESSUR IZED AIRCRAFT, CHECKS NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 1996031500036 19960315 00036 EU 1996 3 15 ABXA9600243 2 19960305 A 7200 ENGINE NIHON YS11 YS11A500 6310416 WP RROYCE DART DART54210K 54522 EU NR 2 FAILED A ABXA E ENGINE SHUTDOWN J Y WARNING INDICATION ENGINE STOPPAGE CR CRUISE 1 GL 23 919AX 11217 5277 2113 21348 NR 2 ENGINE FAILED IN-FLIGHT. REPLACED NR 2 ENGINE. NOTE: NO TEAR-DOWN FINDINGS AVAILABLE AT THIS TIME ON FAILED ENGIN E. 2 L 7 2 4T 4 T A1PC E5EU 1996031500037 19960315 00037 NM 1996 3 15 DL72K960520 1 19960306 A 5315 FLOOR BEAM BOEING 727 727232 1384082 NM BS 380 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 412DA 21232 FOUND ON CV-1 CHECK CORROSION ON FLOOR BEAM STA 380 RBL 55. REPAIR: REPAIRED PER M/M 53-20-11. 2 L 7 3 4F A3WE 1996031500038 19960315 00038 NM 1996 3 15 DL72L960524 1 19960306 A 3260 656021132M0DA ACCESSORY UNIT BOEING 727 727232 1384082 NM LANDING GEAR MALFUNCTIONED A DALA O OTHER N FALSE WARNING CL CLIMB 1 SO 27 511DA 21313 ON GEAR RETRACTION, THE RIGHT GEAR RED LANDING GEAR DISAGREEMENT LIGHT REMAINED ILLUMINATED AND REMAINED ILLUMINATED UNT IL GEAR EXTENDED FOR LANDING. PERFORMED OPERATION TEST OF UPLOCK SENSORS PER MM 32-61-811, REPLACED LANDING GEAR ACCESS SORY UNIT PER 32-09-121, CLEANED ALL SENSORS, OPERATION NORMAL. 2 L 7 3 4F A3WE 1996031500039 19960315 00039 NM 1996 3 15 DL72S960508 1 19960306 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 4 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 531DA 21814 FOUND DURING C-2 LETTER CHECK - 2 INCH CRACK NR 4 L/E SLAT COVE SKIN ATTACH ANGLE BELOW TAI DUCT. REPAIRED PER MM 57-54 -0 PAR 5A. 2 L 7 3 4F A3WE 1996031500040 19960315 00040 NM 1996 3 15 DL72W960511 1 19960306 A 3350 900835A BATTERY PACK BOEING 727 727247 138408F NM LT EXTERIOR DISCHARGED A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 293WA 22111 LEFT OVER WING EXTERIOR FWD EMERG ESCAPE PATH ILLUMINATION LIGHT INOPERATIVE. REPLACED BOTH BULBS - NO HELP. REPLACED BATTERY PACK - OPERATION NOW NORMAL. 2 L 7 3 4F A3WE 1996031500041 19960315 00041 NM 1996 3 15 DL73S960510 1 19960303 A 5312 BLKHD WEB BOEING 737 737232 1384475 NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 326DL 23098 DURING ACCOMPLISHMENT OF S.I. 3-69482-12, A 1 INCH CRACK WAS FOUND IN THE RADIUS OF THE VERTICAL CHORD OF THE LBL 5.7 VE RTICAL STIFFENER AT BS 178. THE BULKHEAD WEB WAS ALSO FOUND CRACKED AT SEVERAL LOCATIONS BETWEEN WL 184.5 AND 207 AND L BL 5.7 TO RBL 5.7. THE DAMAGE WAS TRIMMED OUT OF THE CHORD AND REPAIRED WITH A REPAIR ANGLE AND A STRAP. THE DAMAGE WA S ALSO TRIMMED OUT OF THE BULKHEAD AND REPAIRED WITH A FILLER AND A DOUBLER. REPAIRS ACCOMPLISHED PER DL ERA 303240-14. 2 L 7 2 4F RT A16WE 1996031500042 19960315 00042 NE 1996 3 15 DLL10960497 2 19960305 A 7260 VB3503 CHIP DETECTOR LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B02 54555 NE NR 1 ENGINE LEAKING A DALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 718DA 193C1097 10659 NR 1 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED - GAUGE SHOWED LOW OIL QUANTITY. ENGINE NR 1 SHUT DOWN IAW POM AND EMERG PROCEDURES ON FINAL APPROACH. N3 WENT TO ZERO. FOUND EVIDENCE OF LEAKING AT MASTER CHIP DETECTOR HOUSING. REPLACED F INE SCAVANGE FILTER. REMOVED DETECTOR AND HOUSING. REPLACED DETECTOR ASSY. SERVICED ENGINE OIL. RAN ENG AT T.O. PER PFHB. NO LEAKS FOUND. 2 L 7 3 4F 4 F A23WE E12EU 1996031500043 19960315 00043 WP 1996 3 15 DLL13960506 1 19960306 A 5320 1504420101 FITTING LKHEED 1011 10113851 5265010 WP FS 1212 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 783DL 193A1009 CRACK FOUND AT FS 1212, WL 174 O/B KEEL BEAM AFT LEG FITTING. AT REV A, AN UNIDENTIFIED BLEND TO THE OPPOSITE FLANGE WA S FOUND. THE BLEND MEASURES .75 INCH BY .3750 INCH BY .080 INCH DEEP. AT REV B, A PREVIOUSLY UNDETECTED .0937 INCH LON G CRACK AND A SMALL AREA OF CORROSION WERE FOUND IN THE SAME VERTICAL FLANGE ABOVE. THE CRACK ELIMINATES VERTICALLY FRO M THE LOWER EDGE OF THE VERTICAL FLANCE AT A LOCATION .3750 INCH FWD FROM THE AFT EDGE OF THE FITTING. THE CORROSION DA MAGE EXTENDS AFT FROM THE CRACK TO THE END OF THE FITTING AND DOWN FROM THE CRACK TIP TO THE VERTICAL FLANGE LOWER EDGE. REPAIRED PER ERA 273414-14. 2 L 7 3 4F A23WE 1996031500044 19960315 00044 WP 1996 3 15 DLL13960525 1 19960306 A 5210 1281T10033 ACTUATOR LKHEED 1011 10113851 5265010 WP L 2 DOOR INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 784DA 193A1038 2L DOOR ELECTRIC ACTUATION INOPERATIVE. UNABLE TO CLOSE DOOR MANUALLY. REPLACED 2L DOOR ACTUATOR ASSEMBLY, OPERATION N ORMAL. 2 L 7 3 4F A23WE 1996031500045 19960315 00045 WP 1996 3 15 DLL17960507 1 19960306 A 5330 1542244101 SKIN LKHEED 1011 10113853 5265020 WP FS 1795-1745 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 766DA 193H1207 FUSELAGE SKIN WAS FOUND DAMAGED FROM STR 41 TO STR 44. ERA 268511-14. REPAIRED A PREVIOUS PUNCTURE IN THE SKIN, STR, A ND FUSELAGE SKIN LOCATED FROM STR 44 TO STR 46 AT THE TEAR STRAP. ERA 268517-14 COVERED A DENT LOCATED BETWEEN STR 41 A ND STR 42 AT STA 1725. ADDITIONAL DAMAGE WAS FOUND BETWEEN THESE TWO PREVIOUSLY DAMAGED LOCATIONS. REPAIRED PER DL ERA 273344-14, REV B. 2 L 7 3 4F A23WE 1996031500046 19960315 00046 NM 1996 3 15 DLM88960513 1 19960305 A 5320 59124921 JAMB PAN DOUG MD88 MD88 3023688 NM SERVICE DOOR PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 938DL 49811 THE FUSELAGE FORWARD SERVICE DOOR SURROUND STRUCTURE LOWER JAMB PAN WAS DAMAGED FROM TOOLING. THE PAN HAS SEVERAL PUNCT URES. REPLACEMENT PAN IS NOT AVAILABLE, SO FABRICATED SECTION WAS SPLICED IN PER THE MD-88 SRM, REFERENCE DL ERA 273424 -14. 2 L 7 2 4F RT A6WE 1996031500047 19960315 00047 NM 1996 3 15 DLM90960523 1 19960304 A 3010 59650831 DE ICE DOUG MD90 MD9030 3023690 NM LT STRAKE FAILED A DALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 27 901DA 53381 ANTI-ICE FAULT ILLUMINATES ON O.A.P. WITH ACFT IN AIR MODE AND ENG A/I ON...LEFT STRAKE LOWER SURFACE NOT HEATING AND A RCING. REPLACED STRAKE ASSEMBLY OPERATION NORMAL. 2 L 7 2 4F RT A6WE 1996031500048 19960315 00048 WP 1996 3 15 MWEA96056 1 19960307 A 2530 50226 OVEN DOUG DC9 DC932 3022066 WP GALLEY DIRTY A MWEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 31 401ME 47133 CREW REPORTS A/C RT OVEN PUTS OUT FOUL ODOR. DEFERRED OVEN UNTIL RETURN TO MKE. MAINTENANCE IN MKE CLEANED OVEN. NO F URTHER ODOR. 2 L 7 2 4F A6WE 1996031500049 19960315 00049 EU 1996 3 15 QXEA9600097 1 19960306 A 3350 MGG1280 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 469US 11096 GEG - CENTER AISLE EXIT SIGN IS INOPERATIVE. 28V BULBS WERE REPLACED AND SIGN OPS CHECKED GOOD. AIRCRAFT RETURNED TO S ERVICE. 2 L 7 2 4F RT A20EU 1996031500050 19960315 00050 EU 1996 3 15 QXEA9600098 1 19960306 A 3350 6008905 BATTERY PACK FOKKER F28 F28MK1000 4990808 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 452US 1034 11105 PDX - EMERGENCY LIGHT BATTERY PACK FOR LEFT OVERWING EXIT AND SIDE WALL SIGN IS INOPERATIVE. REPLACED BATTERY PACK NR 6 , EXIT SIGN AND SIDE WALL SIGN OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996031500051 19960315 00051 NM 1996 3 15 QXEA9600099 1 19960307 A 3350 1013075 BULB DHAV DHC8 DHC8102 2809003 NM FWD EXIT FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 825PH 213 PDX - ONE FLOOR PROXIMITY LIGHT IS INOPERATIVE AT THE FORWARD EXIT, 3RD BULB BACK. BULB WAS REPLACED AND BULB OPS CHECK ED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1996031500102 19960315 00102 WP 1996 3 15 9605679991 1 19960307 A 2170 COALESCER BAG DOUG DC9 DC932 3022066 WP CABIN DIRTY A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 8957E 47215 SHORTLY AFTER TAKEOFF, THE LAVATORY SMOKE DETECTORS WERE ACTIVATED BY SMOKE ENTERING THE CABIN FROM THE AIR CONDITIONING SYSTEM. THE FLIGHT RETURNED TO ATL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND CHANGED THE AI R CONDITIONING COALESCER BAGS. NO OTHER DISCREPANCIES NOTED. 2 L 7 2 4F A6WE 1996031500103 19960315 00103 NM 1996 3 15 9605682297 1 19960307 A 5280 SEAL BOEING 727 727251 138408H NM NLG DOOR OUT OF ADJUST A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 297US 21789 DURING APPROACH UPON GEAR EXTENSION, NOSE LANDING GEAR DOOR REMAINED OPEN. RECYCLED LANDING GEAR TO NO AVAIL. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE FORWARD NOSE LANDING GEAR DOOR SEAL RUBBING AND RESTRICTING PRO PER DOOR MOVEMENT. ADJUSTED AND LUBRICATED DOOR SEAL. OPERATIONAL CHECK WAS NORMAL. 2 L 7 3 4F A3WE 1996031500104 19960315 00104 WP 1996 3 15 9605699919 1 19960307 A 3260 SWITCH DOUG DC9 DC932 3022066 WP GEAR DOOR DIRTY A NWAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 01 941N 47450 DURING APPROACH INTO SLC, AMBER GEAR DOOR LIGHT CAME ON AFTER GEAR WAS EXTENDED. CREW DID GO-AROUND DURING WHICH GEAR D OOR LIGHT EXTINGUISHED. EMERGENCY EQUIPMENT REQUESTED AS A PRECAUTION. FLIGHT LANDED WITHOUT INCIDENT. CLEANED DOOR S WITCH AND OPERATION CHECKED GOOD. 2 L 7 2 4F A6WE 1996031500105 19960315 00105 NE 1996 3 15 9605701150 2 19960306 A 7230 COMPRESSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 3 ENGINE STALLED A NWAA O OTHER R PARTIAL RPM/PWR LOSS DE DESCENT 1 GL 01 150US 46759 86145 AT TOP OF DESCENT, THE NR 3 ENGINE COMPRESSOR STALLED AND EGT ROSE TO 750 DEGREES. THE ENGINE WAS SHUT DOWN AND A SUCCE SSFUL RESTART WAS ACCOMPLISHED. FLIGHT CONTINUED TO DTW WITHOUT FURTHER INCIDENT. VISUAL INSPECTION AND BORESCOPE OF N R 3 ENGINE HIGH PRESSURE COMPRESSOR (HPC), COMBUSTION CHAMBER, AND HIGH PRESSURE TURBINE (HPT) REVEALED NO DISCREPANCIES . REPLACED FUEL CONTROL, PRESSURE RATIO BLEED CONTROL (PRBC), AND BLEED CONVERTER VALVE. OPERATIONAL CHECK NORMAL. AI RCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A22WE E20EA 1996031500106 19960315 00106 WP 1996 3 15 9605719604 1 19960306 A 3231 RETRACT MECH DOUG DC9 DC932 3022066 WP NLG DOOR MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 604NW 47222 DURING ALTERNATE FUELING PROCEDURE, NOSE GEAR DOORS WERE OPENED ACCORDING TO MANUAL PROCEDURES. AFTER TAKEOFF, THE GEAR DOORS WOULD NOT CLOSE. THE AIRCRAFT RETURNED TO OMA AND LANDED WITHOUT INCIDENT. INSPECTED AND CLOSED NOSE GEAR DOORS MANUALLY. AIRCRAFT DEPARTED WITH NO PROBLEM. 2 L 7 2 4F A6WE 1996031500107 19960315 00107 NM 1996 3 15 9605722767 1 19960309 A 2752 MS93911302E4C DRIVE MOTOR BOEING 727 7272M7 138407S NM TE FLAPS FAILED A NWAA A J UNSCHED LANDING DUMP FUEL F K J FLT CONT AFFECTED FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 727RW 45956 9315 21656 DURING FIRST 20 MINUTES OF FLIGHT, AIRCRAFT EXPERIENCED TOTAL LOSS OF 'A' SYSTEM HYDRAULICS. FUEL WAS DUMPED AND AIRCRA FT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED OUTBOARD FLAP DRIVE MOTOR AND NR 1 AND NR 2 ENGINE DRIVE HYD RAULIC PUMPS AND CASE AND MAIN DRAIN HYDRAULIC FILTERS. LEAK AND PRESSURE CHECKED 'A' HYDRAULIC SYSTEM. CHECKED OK. 2 L 7 3 4F A3WE 1996031500108 19960315 00108 NM 1996 3 15 9605736718 1 19960309 A 7722 8DJ200LWN1 EGT INDICATOR BOEING 747 747251F 1384898 NM PWA JT9 JT9D7F 52054 NE NR 1 MALFUNCTIONED A NWAA C E D ABORTED TAKEOFF ENGINE SHUTDOWN RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 618US 17352 1039 21122 89564 DURING TAKEOFF ROLL, THE NR 1 ENGINE EGT EXCEEDED 1,000 DEGREES WITH NO INDICATOR LIGHT. CREW ABORTED TAKEOFF; SUBSEQUE NT ENGINE SHUT-DOWN AND RETURNED TO GATE. REPLACED THE NR 1 EGT INDICATOR AND PERFORMED INSTALLATION RESISTANCE CHECK I NCLUDING EGT INDICATING ACCURACY TEST. AIRCRAFT IS SCHEDULED FOR NR 1 ENGINE CHANGE IN MSP. 2 L 7 4 4F 4 F A20WE E20EA 1996031500109 19960315 00109 NM 1996 3 15 9605746631 1 19960309 A 3350 BATTERY PACK BOEING 747 747251B 1384892 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 631US 23111 DURING LINE CHECK, FOUND ZONE 'E' FLOOR PATH EMERGENCY LIGHTS AND OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTE RY PACKS. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996031500110 19960315 00110 NE 1996 3 15 9605759991 2 19960308 A 7261 OIL FILTER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7 52053 NE NR 2 ENGINE CONTAMINATED A NWAA O OTHER J WARNING INDICATION CR CRUISE 1 GL 01 8957E 47215 653677 EN ROUTE TO MCI, NR 2 ENGINE OIL FILTER CLOG WARNING LIGHT ILLUMINATED. THE ENGINE WAS REDUCED TO IDLE THRUST AND THE F LIGHT CONTINUED AS SCHEDULED WITHOUT INCIDENT. MAINTENANCE REPLACED THE OIL FILTER AND OIL FILTER PRESSURE DIFFERENTIAL SWITCH. SYSTEM OPERATION CHECKED NORMAL ON SUBSEQUENT RUN-UP. 2 L 7 2 4F 4 F A6WE E2EA 1996031500111 19960315 00111 WP 1996 3 15 9605769851 1 19960310 A 3222 STRUT DOUG DC9 DC951 3022051 WP NLG REQD SERVICE A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 760NC 47708 DURING CLIMB-OUT OF LGA, LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO LGA AND LANDED WITHOUT INCIDENT. INSPECT ED GROUND SHIFT MECHANISM AND GROUND SENSING FUNCTIONS. SERVICED NOSE GEAR STRUT TO PROPER LEVEL AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996031500112 19960315 00112 NM 1996 3 15 96FDEA00451 1 19960305 A 5754 65162256 FLAP BOEING 727 727233 138408A NM NR 4 LE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 NR 4 K-FLAP OUTBOARD LOWER BONDING JUMPER IS CORRODED AT UPPER ATTACH POINT. MATERIAL REMOVED DURING REWORK EXCEEDS LIM ITS PER FEDEX SR 27-57-010, REV B. ****S/D*** COMING. C/A REMOVED CORRODED AREA AND REPAIRED OUTBOARD LOWER BONDING JUMPER ATTACH POINT PER FEDEX SRM 57-50-3. 2 L 7 3 4F RT A3WE 1996031500113 19960315 00113 NM 1996 3 15 96FDEA00464 1 19960115 A 5311 FRAME BOEING 747 747245F 1384897 NM BS 1980 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 640FE 20826 (STATION SIN). SNRM 1246. MAIN DECK FRAME FOUND CRACKED AT BS 1980 S13L AS MARKED. C/A REPAIR CARRIED OUT PER FEDEX E RA NR B53-10-324. 2 L 7 4 4F A20WE 1996031500114 19960315 00114 NM 1996 3 15 96FDEA00465 1 19960115 A 5320 65B02803 SHEAR TIE BOEING 747 747245F 1384897 NM BS 1800 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 640FE 20826 STATION (SIN) SNRM (1258). MAIN DECK CROWN AREA INTERIOR BS 1800 BETWEEN 54R AND 55R SHEAR-TIE FOUND CRACKED AS MARKED. C/A SHEAR-TIE REPLACED PER DWG 65B00146. 2 L 7 4 4F A20WE 1996031500115 19960315 00115 NM 1996 3 15 96FDEA00466 1 19960115 A 5320 65B3860015 CLIP BOEING 747 747245F 1384897 NM BS 1860 BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 640FE 20826 STATION (SIN) SNRM (1236). MAIN DECK STRINGER CLIP FOUND BENT AT BS 1860 AT S11R AS MARKED. C/A STRINGER CLIP REPLACED PER DWG 65B00146. 2 L 7 4 4F A20WE 1996031500116 19960315 00116 NM 1996 3 15 96FDEA00467 1 19960115 A 5313 BAC167513 STRINGER BOEING 747 747245F 1384897 NM BS 1980 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 640FE 20826 STATION (SIN) SNRM (1248). MAIN DECK STRINGER FOUND CRACKED AT BS 1980, AT S12L AS MARKED. C/A STRINGER REPAIRED PER F EDEX SRM REV 76-53-10-03, PAGE 2. 2 L 7 4 4F A20WE 1996031500117 19960315 00117 WP 1996 3 15 96FDEA00468 1 19960310 A 5320 WEB DOUG DC10 DC1010F 3022111 WP BS 1500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 LEFT WHEEL INBOARD VERTICAL WALL AT STA 1500 NEAR UPPER TEE CHORD, THERE IS A 3 INCH CRACK IN WEB SKIN JUST FORWARD OF V ERTICAL STIFFENER; ALSO, ON CENTER GEAR WELL, 3 EACH FASTENER HOLES ARE CRACKED ATTACHING WEB TO TEE CHORD STA 1500. ** *S/D*** COMING. 2 L 7 3 4F A22WE 1996031500118 19960315 00118 GL 1996 3 15 96FDEA00469 2 19960310 A 7200 ENGINE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C GL NR 1 FAILED A FDEA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 25 602FE 48402 DURING CLIMB OUT, NR 1 ENGINE COMPRESSOR STALLS. THROTTLE WAS RETARDED, ENGINE CONTINUED TO STALL, FLIGHT CREW SHUT DOW N NR 1 ENGINE. THE AIRCRAFT RETURNED TO MEMPHIS. POWER PLANT LINE FOUND METAL IN THE TAIL PIPE. C/A FOUND METAL IN TA ILPIPE. BOPED HPT CONFIRMED NR 1 ENGINE CHANGE DUE. REMOVED AND REPLACED NR 1 ENGINE PER W/C 71T0101 AND W/C 71T0701. ENGINE RUN AND LEAK CHK GOOD. PART 7100191 OFF 702757 POS 01 RSN 02. 2 L 7 3 4F 4 F RT A22WE E23EA 1996031500119 19960315 00119 NM 1996 3 15 96FDEA00470 1 19960115 A 5320 69B070034 SHEAR TIE BOEING 747 747245F 1384897 NM BS 1760 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 640FE 20826 STATION (SIN) SNRM (1232). MAIN DECK SHEAR TIE FOUND CRACKED AT BS 1760 BETWEEN 54R AND 55R AS MARKED. C/A SHEAR TIE REPLACED PER DWG 65B01783. 2 L 7 4 4F A20WE 1996031500120 19960315 00120 NM 1996 3 15 96FDEA00471 1 19960308 A 5350 65397349 FAIRING BOEING 727 727233 138408A NM PANEL 3340 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 SNRM (0509). GOUGE ON FAIRING 3340, 22 INCHES FROM BOTTOM AND 12 INCHES AFT OF PANEL. C/A REMOVED DAMAGED AREA 3 INCHE S BY 5 INCHES, .040 INCH, AND REPAIRED PER FEDEX SRM 51-40-2. 2 L 7 3 4F RT A3WE 1996031500121 19960315 00121 NM 1996 3 15 96FDEA00472 1 19960308 A 5610 WINDOW BOEING 727 727233 138408A NM RT COCKPIT HEAT DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 SNRM (0133). FIRST OFFICER'S NR 5 WINDOW IS DAMAGED BEYOND LIMITS (HEAT DAMAGED). *** S/D *** REMOVED AND REPLACED TH E F/O'S NR 5 WINDOW PER FEDEX MM 56-11-41. 2 L 7 3 4F RT A3WE 1996031500122 19960315 00122 NM 1996 3 15 96FDEA00473 1 19960308 A 5610 WINDOW BOEING 727 727233 138408A NM LT COCKPIT HEAT DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 SNRM (0139). CAPTAIN'S NR 4 WINDOW MIDDLE PANE IS HEAT DAMAGED. *** S/D *** REMOVED AND REPLACED THE CAPT'S NR 4 WIND OW PER FEDEX MM 56-11-31. 2 L 7 3 4F RT A3WE 1996031500123 19960315 00123 NM 1996 3 15 96FDEA00474 1 19960308 A 5610 WINDOW BOEING 727 727233 138408A NM LT COCKPIT DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 SNRM (0139). CAPTAIN'S NR 5 WINDOW IS DAMAGED BEYOND LIMITS, DELAMINATED. *** S/D *** REMOVED DAMAGED NR 5 WINDOW AND REPLACED WITH NEW PER FEDEX MM 56-11-41. SEAL WILL BE APPLIED ON CARD NR NR0134. PERFORMED FUNCTIONAL TEST OF CAPT'S WINDOW IAW FEDEX MM 30-41-02. 2 L 7 3 4F RT A3WE 1996031500124 19960315 00124 NM 1996 3 15 96FDEA00475 1 19960308 A 5610 WINDOW BOEING 727 727233 138408A NM RT NR 3 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 SNRM (0141). F/O'S NR 3 WINDOW IS DAMAGED BEYOND LIMITS, GOUGED. *** S/D *** COMING. 2 L 7 3 4F RT A3WE 1996031500125 19960315 00125 NM 1996 3 15 96FDEA00476 1 19960308 A 5610 WINDOW BOEING 727 727233 138408A NM RT COCKPIT HEAT DAMAGE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 FIRST OFFICER'S NR 4 WINDOW IS DAMAGED BEYOND LIMITS (HEAT DAMAGE). *****S/D **** REMOVED AND REPLACED THE F/O'S NR 4 W INDOW PER FEDEX MM 56-11-31. 2 L 7 3 4F RT A3WE 1996031500126 19960315 00126 NM 1996 3 15 96FDEA00477 1 19960308 A 5754 SKIN BOEING 727 727233 138408A NM NR 4 SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 SNRM (0270). NR 4 SLAT, 01B GUIDE HOOK CUT-OUT, CRACKED. C/A STOP DRILLED CRACK AND FABRICATED AND INSTALLED REPAIR PA RTS PER FEDEX SRM 57-30-4. 2 L 7 3 4F RT A3WE 1996031500127 19960315 00127 NM 1996 3 15 96FDEA00479 1 19960308 A 5320 65453132 CLIP BOEING 727 727233 138408A NM BS 380 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 SNRM (0649). BS 380, STRINGER 7L, STRINGER CLIP IS DAMAGED. ***S/D** COMING. 2 L 7 3 4F RT A3WE 1996031500128 19960315 00128 NM 1996 3 15 96FDEA00480 1 19960308 A 5320 65463132 STRINGER CLIP BOEING 727 727233 138408A NM BS 700 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 SNRM 0663, BS 700 STRINGER CLIP NR 5 HAS CORROSION. *S/D* REMOVED STRINGER CLIP AT BS 700 STRINGER CLIP NR 5 LT, REPLA CED WITH NEW CLIP PER SRM 51-30-2. 2 L 7 3 4F RT A3WE 1996031500129 19960315 00129 NM 1996 3 15 96FDEA00481 1 19960308 A 5320 65453132 CLIP BOEING 727 727233 138408A NM BS 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 SNRM (0663). BS 700, STRINGER 7R IS CRACKED (CLIP). ***S/D** COMING. 2 L 7 3 4F RT A3WE 1996031500130 19960315 00130 NM 1996 3 15 96FDEA00482 1 19960308 A 5230 52FX16513 CENTERING BLOCK BOEING 727 727233 138408A NM CARGO DOOR GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 SNRM (0690). MAIN CARGO DOOR AFT CENTERING IS GOUGED. C/A REMOVED GOUGED MAIN CARGO DOOR AFT CENTERING BLOCK, INSTALL ED ONE EACH NEW BLOCK IAW FEDEX 727 SRM 51-10-1. 2 L 7 3 4F RT A3WE 1996031500131 19960315 00131 NM 1996 3 15 96FDEA00483 1 19960308 A 5320 65607124 SUPPORT BOEING 727 727233 138408A NM BS 1065 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 SNRM (0709). CORROSION (53-224-01 (3), (53-224-04) FLOOR BOARD SUPPORT B.S. 1068, LBL 25, WL 208. ORIGINAL THICKNESS, .091 INCH. REMAINING .072 INCH OUT OF LIMITS PER FEDEX SRM 53-10-1, FIG 1 DETAIL VI. *** S/D *** COMING. 2 L 7 3 4F RT A3WE 1996031500132 19960315 00132 NM 1996 3 15 96FDEA00484 1 19960308 A 5330 SKIN BOEING 727 727233 138408A NM BS 349 LIGHTNING STRIKE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 SNRM (0709). LIGHTNING STRIKER AT BS 349 (BETWEEN STR 3 AND STR 4 LT). BS 360 (BETWEEN STR 3 AND STR 4 LT), BS 376, ST R 3 LT, BS 374 LT, BS 439, STR 4 LT. *** S/D *** COMING. 2 L 7 3 4F RT A3WE 1996031500133 19960315 00133 NM 1996 3 15 96FDEA00485 1 19960308 A 5320 THRESHOLD PLATE BOEING 727 72722 1384002 NM BS 1176 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 SNRM 0087, CORROSION (C53-224-04) AFT ENTRY DOOR THRESHOLD SUPPORT PLATE BS 1176, WL 209 LBL 11 TO RBL11. *S/D* REPLAC ED THRESHOLD SUPPORT PLATE. 2 L 7 3 4F A3WE 1996031500134 19960315 00134 NM 1996 3 15 96FDEA00486 1 19960308 A 5712 RIB BOEING 727 72722 1384002 NM WS 772 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 SNRM (0109), FIXED LEADING EDGE LEFT WING HAS GOUGES JUST O/B OF NR 1 SLAT ON VERTICAL RIB. REMOVED AND REPLACED VERTIC AL RIB. 2 L 7 3 4F A3WE 1996031500135 19960315 00135 NM 1996 3 15 96FDEA00487 1 19960308 A 5753 TRACK BOEING 727 72722 1384002 NM TE MIDFLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 SNRM (0384), RT WING OB MIDFLAP HAS A 2 INCH CRACK ON LOWER SURFACE T/E JUST BELOW I/B OF OB AFT FLAP TRACK ASSY. REMOV ED, FABRICATED AND INSTALLED NEW U-CHANNEL AND INSTALLED NEW TRACK ASSEMBLY MM 27-51-56. 2 L 7 3 4F A3WE 1996031500136 19960315 00136 NM 1996 3 15 96FDEA00488 1 19960115 A 5320 CLIP BOEING 747 747245F 1384897 NM BS 1780 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 640FE 20826 MAIN DECK STRINGER CLIP FOUND CRACKED AT BS 1780 STR 12R AND 12L AS MARKED. STRINGER CLIP REPLACED AS DWR 65B01703. 2 L 7 4 4F A20WE 1996031500137 19960315 00137 NM 1996 3 15 96UAL900173 1 19960308 A 3260 387 BULB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT MLG FAILED A UALA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 WP 29 526UA 24994 RIGHT LANDING GEAR HAD NO INDICATION WITH GEAR DOWN AND FLAPS AT 30 DEGREES. WITH GEAR DOWN AND THROTTLES AT IDLE NO HO RN. COMPLETED TOWER FLYBY FOR GEAR DOWN VERIFICATION. LANDED UNDER AMBER ALERT. SUPPLEMENTAL DATA UPDATE: RIGHT MAIN LANDING GEAR INDICATOR LIGHT HAD A BURNED OUT BULB. RELAMPED OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996031500138 19960315 00138 NM 1996 3 15 96UAL900174 1 19960308 A 2130 CIRCUIT BREAKER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE PRESSUR SYST MALFUNCTIONED A UALA A UNSCHED LANDING L NO TEST CL CLIMB 1 WP 29 7266U 21413 RETURNED TO DEN, DUE TO PRESSURIZATION PROBLEMS. FAILED STANDBY TEST. PULLED AND RESET ALL CIRCUIT BREAKERS. 2 L 7 3 4F 4 F A3WE E2EA 1996031500139 19960315 00139 NM 1996 3 15 96UAL900175 1 19960308 A 3350 STRIP BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 949UA 26692 FORWARD GALLEY EMERGENCY ESCAPE PATH LIGHTING INOP. REPLACED FORWARD GALLEY LIGHT STRIP. 2 L 7 2 4F 4 F RT A16WE E2GL 1996031500140 19960315 00140 NM 1996 3 15 96UAL900176 1 19960308 A 3350 LAMP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN FAILED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 382UA 24657 EMERGENCY EXIT SLIDE LIGHT INOP. CLEANED SOCKET AND REPLACED LAMP. CHECKS O.K. 2 L 7 2 4F 4 F RT A16WE E2GL 1996031500141 19960315 00141 NM 1996 3 15 96UAL900177 1 19960308 A 3350 BATTERY BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563B2 13802 EU CABIN DISCHARGED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 334UA 24229 EMERGENCY ESCAPE PATH LIGHTING INOP AT ROWS ONE AND TWO. REPLACED BATTERY PACK, CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E21EU 1996031500142 19960315 00142 WP 1996 3 15 ABXA9600244 1 19960307 A 3260 7000010101 UPLOCK SWITCH DOUG DC9 DC931 3022065 WP LT MLG DEFECTIVE A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 936AX 47269 AFTER GEAR RETRACTION, LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED, RECYCLED GEAR, NO HELP. LIGHT EXTINGUISHED AFTER 2- 3 MINUTES UPON ENTERING TURBULENCE. REPLACED LEFT GEAR UPLOCK SWITCH S1-79. 2 L 7 2 4F A6WE 1996031500143 19960315 00143 WP 1996 3 15 ABXA9600245 1 19960308 A 3350 60030431 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 936AX 47269 DURING PRE-DEPARTURE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY. 2 L 7 2 4F A6WE 1996031500144 19960315 00144 WP 1996 3 15 ABXA9600246 1 19960309 A 3260 0080004003 PROX CONTL BOX DOUG DC9 DC941 302207N WP RT MLG WW DEFECTIVE A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 954AX 47612 DURING THE GEAR UPLATCH CHECK, THE LANDING GEAR HANDLE WAS BINDING. RECYCLED THE GEAR AND BINDING WAS STILL THERE. APP ROXIMATELY 1 HOUR AFTER TAKEOFF, THE LEFT GEAR UNSAFE LIGHT ILLUMINATED. THE GEAR OPERATED NORMALLY WHEN EXTENDED FOR L ANDING. RE-ROUTED SAFETY WIRE ON LANDING GEAR CONTROL DRUM IN THE RIGHT WHEELWELL. REPLACED THE PROXIMITY CONTROL BOX FOR THE INDICATION PROBLEM. 2 L 7 2 4F A6WE 1996031500145 19960315 00145 WP 1996 3 15 ABXA9600247 1 19960311 A 3350 60030431 POWER SUPPLY DOUG DC9 DC941 302207N WP CABIN INOPERATIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 990AX 47493 EMERGENCY LIGHTS COME ON AFTER AIRCRAFT POWER IS REMOVED. REPLACED EMERGENCY LIGHT POWER SUPPLY. 2 L 7 2 4F A6WE 1996031500146 19960315 00146 WP 1996 3 15 ABXA9600248 1 19960308 A 5610 SLIDING WINDOW DOUG DC8 DC861 3021952 WP RT COCKPIT LACK OF LUBE A ABXA K NONE O OTHER TX TAXI/GRND HDL 1 GL 23 849AX 45891 CHECKED FIRST OFFICER'S SLIDING WINDOW DURING TAXI OUT AND WINDOW WOULD NOT OPEN. HANDLE OPENS (RELEASES FROM HOOK) BUT WINDOW FAILS TO SLIDE BACK. CLEANED AND LUBED WINDOW TRACK AND ROD ENDS IAW DC8 MM. OPS CHECK GOOD. 2 L 7 4 4F 4A25 1996031500147 19960315 00147 SO 1996 3 15 COMA9610095 1 19960307 A 3260 12038594001 CONTROL BOX EMB 120 EMB120RT SO LANDING GEAR MALFUNCTION A COMA K NONE N FALSE WARNING CL CLIMB 1 SO 01 205CA 10865 5771 120205 LANDING GEAR INTRANSIT LIGHTS REMAINED ON WITH GEAR RETRACTED. REPLACED THE LANDING GEAR CONTROL BOX. 2 L 7 2 4T RT A31SO 1996031500148 19960315 00148 SO 1996 3 15 COMA9610096 1 19960307 A 3000 102AU1AF OAT PROBE HEAT EMB 120 EMB120RT SO NOSE FAILED A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 200CD 11962 5521 120200 OUTSIDE AIR TEMPERATURE PROBE HEAT IS INOPERATIVE. REPLACED THE TRUE AIR TEMP PROBE. PART TOTAL CYCLES, 12,082. 2 L 7 2 4T RT A31SO 1996031500149 19960315 00149 EU 1996 3 15 COMA9630057 1 19960307 A 2450 A2042C PDU SAAB SF340 SF340A 7850100 EU LEFT DEFECTIVE A COMA K NONE H ELECT. POWER LOSS-50 PC UK UNKNOWN 1 SO 01 140N 5334 477 340A140 LEFT MAIN ELECTRIC BUS DROPS OFF LINE. REPLACED THE LT POWER DISTRIBUTION UNIT. PART TOTAL CYCLES, 5,920. 2 L 7 2 4T RT A52EU 1996031500150 19960315 00150 EU 1996 3 15 COMA9630058 1 19960308 A 2436 51539007A GCU SAAB SF340 SF340A 7850100 EU LT DC GEN DEFECTIVE A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 341CA 5859 4631 340A021 LEFT ENGINE WILL NOT START (NO ROTATION) USING CROSS GENERATOR PROCEDURE. REPLACED THE LT GENERATOR CONTROL UNIT. PART TOTAL CYCLES, 6,629. 2 L 7 2 4T RT A52EU 1996031500151 19960315 00151 EU 1996 3 15 COMA9630059 1 19960307 A 3213 AIR8302212 STRUT SAAB SF340 SF340A 7850100 EU RT MLG FAILED A COMA K NONE K FLUID LOSS TX TAXI/GRND HDL 1 SO 01 356CA 2084 340A034 RIGHT MLG STRUT IS LEAKING. ATTEMPTED RESEAL OF STRUT AND FOUND IT TO BE DAMAGED INTERNALLY. REPLACED SHOCK STRUT. PA RT TOTAL CYLES, 2,360. 2 L 7 2 4T RT A52EU 1996031500152 19960315 00152 EA 1996 3 15 COMA9660037 1 19960307 A 2740 70604 TRIM CONTL UNIT CNDAIR CL600 CL6002B19 EA STAB TRIM DEFECTIVE A COMA K NONE F FLT CONT AFFECTED UK UNKNOWN 1 SO 01 931CA 4804 178 7037 STABILIZER TRIM CHANNEL 2 IS INOPERATIVE. REPLACED THE HORIZONTAL TRIM CONTROL UNIT. PART TOTAL CYCLES, 4,048. 2 L 7 2 4F RT A21EA 1996031500153 19960315 00153 EA 1996 3 15 COMA9660038 1 19960306 A 2750 860D10014 FECU CNDAIR CL600 CL6002B19 EA FLAP SYST DEFECTIVE A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 915CA 2412 1014 7013 FLAPS FAILED WHEN SELECTED TO TAKEOFF RANGE. REPLACED THE FLAP ELECTRONIC CONTROL UNIT. PART TOTAL CYCLES, 2,172. 2 L 7 2 4F RT A21EA 1996031500154 19960315 00154 WP 1996 3 15 MWEA96057 1 19960309 A 5330 SKIN DOUG DC9 DC914 3022034 WP FS 718 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 DURING INSPECTION, FOUND SKIN CRACK .75 INCH IN LENGTH AT STA 718, LONGERON 15R. INSTALLED DOUBLER REPAIR IAW SRM 53-04 , FIG. 12B. 2 L 7 2 4F A6WE 1996031500155 19960315 00155 NM 1996 3 15 P5CA9600156 1 19960308 A 2781 WIRE BOEING 747 747123 1384873 NM NR 2 LED SWITCH SHORTED A P5CA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 858FT 20109 WHEN LEADING EDGE DEVICES WERE EXTENDED, THE NR 2 INDICATED AMBER. AIRCRAFT RETURNED TO BLOCKS. FOUND WIRING AT THE NR 2 POSITION SWITCH WAS SHORTING TO GROUND. REPAIRED IAW STANDARD WIRING PRACTICES 20-10-13. 2 L 7 4 4F A20WE 1996031500156 19960315 00156 NM 1996 3 15 P5CA9600157 1 19960307 A 2751 98010903 POSITION IND BOEING 747 747122 1384872 NM TE FLAPS FAILED A P5CA O OTHER N FALSE WARNING DE DESCENT 1 WP 23 851FT 19756 WHEN EXTENDING FLAPS FOR APPROACH, OUTBOARD TRAILING FLAPS SPLIT: LEFT STAYED AT 1 DEGREE, RIGHT WENT TO 5 DEGREES. EX TENDED FLAPS BY ALTERNATE SYSTEM, FLAPS EXTENDED NORMALLY. FLAP TRANSMISSION SERVICED IAW MM 12-13-13. CHECKED FLAP PO SITION INDICATION SYSTEM CABLE TENSIONS AND FOUND NORMAL IAW MM 27-58-02. REPLACED OUTBOARD FLAP POSITION INDICATOR AND OPS CHECK NORMAL IAW MM 27-58-00. 2 L 7 4 4F A20WE 1996031500157 19960315 00157 GL 1996 3 15 QXEA9600100 3 19960308 A 6114 750350AF O-RING SWRNGN SA227 SA227AC 8780603 SW ROTOL R321 R321482F8 GL NR 2 PROP DOME CUT A QXEA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 09 26877 AC652 DRG360786 MWH - NR 2 ENGINE SHUTDOWN IN-FLIGHT DUE TO LOW OIL PRESSURE INDICATION. AIRCRAFT LANDED IN MWH WITHOUT FURTHER PROBLEM S. NR 2 PROPELLER LEAKING OIL BECAUSE OF CUT PROP DOME O-RING. O-RING REPLACED I/A/W MAINT. MANUAL AND PROP OPS CHECKE D GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A8SW 6 C P61GL 1996031500158 19960315 00158 EU 1996 3 15 QXEA9600101 1 19960310 A 3350 5515800104 CIRCUIT BOARD FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 802PH 11017 PSC - EXIT SIGN ON FORWARD CABIN BULKHEAD IS INOPERATIVE. LIGHT CIRCUIT BOARD REPLACED AND SIGN OPS CHECKED GOOD. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996031500159 19960315 00159 EU 1996 3 15 QXEA9600102 1 19960310 A 3350 1312 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 469US 11096 GEG - LEFT EMERGENCY EXIT SIGN AT ROW 8AB IS INOPERATIVE. BULBS WERE REPLACED AND SIGN OPS CHECKED GOOD. AIRCRAFT RETU RNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996031500160 19960315 00160 EU 1996 3 15 QXEA9600103 1 19960310 A 3350 MGG1280 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 469US 11096 GEG - AISLE OVERHEAD EMERGENCY EXIT SIGN AT ROW 8 IS INOPERATIVE ON FORWARD AND AFT SIDE (28V). BULBS WERE REPLACED AND SIGN OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996031500161 19960315 00161 NE 1996 3 15 SWAA960137 2 19960303 A 7261 OIL PUMP BOEING 737 7372H4 138448C NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE MALFUNCTIONED A SWAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 63SW 22061 DURING CLIMBOUT, EXPERIENCED NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATING AND ASSOCIATED OIL PRESSURE DROP. CREW PER FORMED ENGINE SHUT-DOWN CHECKLIST. AIRCRAFT RETURNED TO MDW AND MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED NR 2 ENGINE OIL PRESSURE PUMP, TRANSMITTER, AND MAIN OIL SCREEN PER BOEING M/M. 2 L 7 2 4F 4 F A16WE E2EA 1996031500162 19960315 00162 NM 1996 3 15 SWAA960138 1 19960303 A 5610 5893543109RPR WINDOW BOEING 737 7372H4 138448C NM L1 SHATTERED A SWAA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 105SW 23249 CAPTAIN'S NR 1 WINDOW OUTER PANE SHATTERED ACROSS ENTIRE LENGTH. DIVERTED TO TUL AND MADE AN UNEVENTFUL LANDING. REMOV ED AND REPLACED WINDOW ASSEMBLY PER BOEING M/M. 2 L 7 2 4F A16WE 1996031500185 19960315 00185 WP 1996 3 15 9605389162 1 19960209 A 5720 CLIPS DOUG DC9 DC914 3022034 WP WS 69 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8907E 45748 DURING A SPECIAL MAINTENANCE VISIT, FOUND CORROSION IN THE RIGHT WING REAR SPAR STR 15 - 16 CLIPS AT STA 69. REPLACED CLIPS (P/N 4192009-2, P/N 4911499-520) PER EA 91-104054. 2 L 7 2 4F A6WE 1996031500186 19960315 00186 WP 1996 3 15 9605399162 1 19960211 A 5713 LONGERON DOUG DC9 DC914 3022034 WP WS 92-107 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8907E 45748 DURING A SPECIAL MAINTENANCE VISIT, FOUND CORROSION ON THE LEFT WING STR 14 FROM XRS 92-107. REPAIRED STRINGER (P/N 591 1277-501) PER EA 91-106787. 2 L 7 2 4F A6WE 1996031500187 19960315 00187 WP 1996 3 15 9605409162 1 19960213 A 5720 SPLICE DOUG DC9 DC914 3022034 WP RT FWD SPAR CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8907E 45748 DURING A SPECIAL MAINTENANCE VISIT, FOUND CORROSION IN THE RIGHT WING FORWARD SPAR SPLICE PLATE AND SPLICE ANGLE DOUBLER . REPLACED PLATE (P/N 3912208-1) AND DOUBLER (P/N 4913572-1) PER EA 91-106788. 2 L 7 2 4F A6WE 1996031500188 19960315 00188 NM 1996 3 15 9605412297 1 19960214 A 5711 SPAR CHORD BOEING 727 727251 138408H NM LT WING CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 297US 21789 DURING H-CHECK, FOUND A CRACK IN THE LEFT AUXILIARY SPAR LOWER CHORD AT THE NR 7 SPOILER ACTUATOR. REPAIRED CHORD PER E A 22-105174. 2 L 7 3 4F A3WE 1996031500189 19960315 00189 NM 1996 3 15 9605426601 1 19960215 A 5312 BLKHD WEB BOEING 747 747151 1384891 NM FS 400 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 601US 19778 DURING P-CHECK, FOUND A CRACK IN THE BS 400 BULKHEAD WEB LBL 41 AT THE UPPER INBOARD CORNER OF THE LEFT CUTOUT. REPAIRE D THE WEB (P/N 65B07936) PER EA 66-99395. 2 L 7 4 4F A20WE 1996031500190 19960315 00190 NM 1996 3 15 9605435505 1 19960217 A 5312 BLKHD CHORD BOEING 757 757251 1384970 NM FS 324 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 505US 23194 DURING T-CHECK, FOUND CORROSION ON THE BS 324 BULKHEAD CHORD AT RBL 34, WATER LINE 208. REPAIRED CHORD (P/N 141N2932-1) PER EA 55-99494. 2 L 7 2 4F RT A2NM 1996031500191 19960315 00191 WP 1996 3 15 9605441149 1 19960217 A 5313 LONGERON DOUG DC10 DC1040 3023508 WP FS 1156 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 149US 46758 DURING T-CHECK, FOUND CORROSION ON LONGERON 47R AT FS 1156. REPAIRED LONGERON (P/N ADA7308-502) PER EA 11-103951. 2 L 7 3 4F A22WE 1996031500192 19960315 00192 NM 1996 3 15 9605452297 1 19960219 A 5530 STRINGER BOEING 727 727251 138408H NM VERT STAB CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 297US 21789 DURING H-CHECK, FOUND CRACKS IN THE VERTICAL STABILIZER STR 8 AT STA 110 AND IN STR 11 AT STA 134. REPAIRED STRINGERS ( P/N 65-16811-3, P/N 65-16810) PER EA 22-103467. 2 L 7 3 4F A3WE 1996031500193 19960315 00193 NM 1996 3 15 9605465505 1 19960220 A 5315 FLOOR BEAM BOEING 757 757251 1384970 NM FS 345 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 505US 23194 DURING T-CHECK, FOUND CORROSION ON THE BS 345 FLOOR BEAM UPPER CHORD AT LBL 10. REPAIRED CHORD (P/N 141N5111) PER EA 55 -99492. 2 L 7 2 4F RT A2NM 1996031500194 19960315 00194 NM 1996 3 15 9605472297 1 19960222 A 5313 LONGERON BOEING 727 727251 138408H NM FS 950 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 297US 21789 DURING H-CHECK, FOUND CORROSION ON STR 29R FROM BS 950D - BS 950E. REPAIRED STRINGER (P/N 65-56441-4) PER EA 22-99523. 2 L 7 3 4F A3WE 1996031500195 19960315 00195 WP 1996 3 15 9605489858 1 19960222 A 5315 FLOOR BEAM DOUG DC9 DC951 3022051 WP FS 237 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 767NC 47724 DURING H-CHECK, FOUND A TWO-INCH CRACK IN THE FS 237 FLOOR BEAM, LBL 6. REPAIRED BEAM (P/N 9911544-5) PER EA 98-102654. 2 L 7 2 4F A6WE 1996031500196 19960315 00196 WP 1996 3 15 9605491149 1 19960222 A 5312 BLKHD WEB DOUG DC10 DC1040 3023508 WP FS 2007 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 149US 46758 DURING T-CHECK, FOUND CORROSION ON THE FS 2007 AFT PRESSURE BULKHEAD WEB AND STIFFENER AT LBL 32, Z = -40. REPAIRED W EB (P/N NJC6040-501) AND STIFFENER (P/N NJC6040-109) PER EA 11-99304. 2 L 7 3 4F A22WE 1996031500197 19960315 00197 WP 1996 3 15 9605509858 1 19960223 A 5311 FRAME DOUG DC9 DC951 3022051 WP FS 693 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 767NC 47724 DURING H-CHECK, FOUND A .50 INCH CRACK IN THE FS 693 FRAME AT LONGERON 24L. REPAIRED FRAME (P/N 9919621) PER EA 98-1026 55. 2 L 7 2 4F A6WE 1996031500198 19960315 00198 WP 1996 3 15 9605519858 1 19960223 A 5320 FLOOR CAP DOUG DC9 DC951 3022051 WP FS 237-265 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 767NC 47724 DURING H-CHECK, FOUND CORROSION IN THE CENTER LINE FLOOR CAP FROM BS 237 - BS 265. REPAIRED CAP (P/N 5910760-11) PER EA 98-109386. 2 L 7 2 4F A6WE 1996031500199 19960315 00199 NM 1996 3 15 9605526729 1 19960223 A 5414 SKIN BOEING 747 747251F 1384898 NM NR 2 PYLON CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 629US 22388 DURING P-CHECK, FOUND A .50 INCH CRACK IN THE NR 2 PYLON INBOARD SKIN OUTER LAYER AT NACELLE STA 175, WATER LINE 151. R EPAIRED SKIN PER EA 67-99442. 2 L 7 4 4F A20WE 1996031500200 19960315 00200 NM 1996 3 15 9605536729 1 19960226 A 5311 FRAME BOEING 747 747251F 1384898 NM FS 281 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 629US 22388 DURING PERIODIC CHECK, FOUND A CRACK IN THE BS 281 UPPER CLOSURE FRAME AT LBL 44, WATER LINE 312. REPAIRED FRAME (P/N 6 5B12888-3) PER EA 67-99438. 2 L 7 4 4F A20WE 1996031500201 19960315 00201 NM 1996 3 15 9605542297 1 19960227 A 5330 SKIN BOEING 727 727251 138408H NM FS 682-688 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 297US 21789 DURING H-CHECK, FOUND CORROSION ON THE INNER FUSELAGE SKIN AT BS 682 - BS 688, STR 26L - STR 27L. REPAIRED SKIN (P/N 65 -54590-6) PER EA 22-99540. 2 L 7 3 4F A3WE 1996031500202 19960315 00202 WP 1996 3 15 9605551149 1 19960227 A 5320 JAMB DOUG DC10 DC1040 3023508 WP FS 999 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 149US 46758 DURING T-CHECK, FOUND CORROSION IN THE FORWARD CARGO DOOR JAMB AT FS 999, LONGERON 43L. REPAIRED JAMB (P/N S2929817) PE R EA 11-103895. 2 L 7 3 4F A22WE 1996031500203 19960315 00203 WP 1996 3 15 9605561149 1 19960227 A 5320 SPLICE DOUG DC10 DC1040 3023508 WP FS 1156 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 149US 46758 DURING T-CHECK, FOUND CORROSION ON THE LONGERON 50L SPLICE AT FS 1156. REPAIRED SPLICE (P/N ADA 7313) PER EA 11-103956. 2 L 7 3 4F A22WE 1996031500204 19960315 00204 WP 1996 3 15 9605571149 1 19960228 A 5313 LONGERON DOUG DC10 DC1040 3023508 WP FS 1964 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 149US 46758 DURING T-CHECK, FOUND CORROSION ON LONGERON 48L AT FS 1964. REPAIRED LONGERON (P/N AGA 7047-1) PER EA 11-103940. 2 L 7 3 4F A22WE 1996031500205 19960315 00205 NM 1996 3 15 9605586729 1 19960228 A 5720 SUPPORT BEAM BOEING 747 747251F 1384898 NM WS 684 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 629US 22388 DURING P-CHECK, FOUND CORROSION ON THE RIGHT WING SPOILER SUPPORT BEAM UPPER CHORD AT WS 684. REPAIRED CHORD (P/N 65B11 614-6) PER EA 67-99439. 2 L 7 4 4F A20WE 1996031500206 19960315 00206 NM 1996 3 15 9605596601 1 19960228 A 5320 SILL BOEING 747 747151 1384891 NM FS 2280 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 601US 19778 DURING P-CHECK, FOUND A CRACK AND CORROSION IN THE DOOR 5R LOWER SILL CHORD BS 2280. REPAIRED CHORD (P/N 65B04423-2) PE R EA 66-99546. 2 L 7 4 4F A20WE 1996031500207 19960315 00207 NM 1996 3 15 9605606601 1 19960229 A 5230 FRAME BOEING 747 747151 1384891 NM CARGO DOOR CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 601US 19778 DURING P-CHECK, FOUND CORROSION ON THE BULK CARGO DOOR FORWARD LOWER CORNER FRAME. REPAIRED FRAME (P/N 65B07094-1) PER EA 66-99453. 2 L 7 4 4F A20WE 1996031500208 19960315 00208 WP 1996 3 15 9605611149 1 19960229 A 5313 LONGERON DOUG DC10 DC1040 3023508 WP FS 1781 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 149US 46758 DURING T-CHECK, FOUND CORROSION ON LONGERON 46R AT FS 1781. REPAIRED LONGERON (P/N AFA 7098-1) PER EA 11-103255. 2 L 7 3 4F A22WE 1996031500209 19960315 00209 NM 1996 3 15 9605626601 1 19960301 A 5320 FITTING BOEING 747 747151 1384891 NM FS 1416 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 601US 19778 DURING P-CHECK, FOUND CORROSION ON THE BS 1416 FRAME TO STRINGER TIE FITTING, 28 INCHES BELOW THE CEILING IN THE LEFT BO DY GEAR WHEELWELL. REPLACED FITTING. 2 L 7 4 4F A20WE 1996031500210 19960315 00210 NM 1996 3 15 9605636601 1 19960302 A 5330 SKIN BOEING 747 747151 1384891 NM FS 1960 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 601US 19778 DURING P-CHECK, FOUND CORROSION ON THE FUSELAGE SKIN AT BS 1960, STR 29R - STR 42R. REPAIRED SKIN (P/N 65B07000-9) PER EA 66-99465. 2 L 7 4 4F A20WE 1996031500211 19960315 00211 WP 1996 3 15 9605649992 1 19960304 A 5210 FITTING DOUG DC9 DC931 3022065 WP AFT ENTRY DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8960E 45869 DURING A SPECIAL MAINTENANCE VISIT, FOUND A CRACK IN THE AFT ENTRY DOOR NR 3 ALIGNMENT FITTING. REPLACED FITTING. 2 L 7 2 4F A6WE 1996031500212 19960315 00212 WP 1996 3 15 9605659611 1 19960305 A 5552 FITTING DOUG DC9 DC932 3022066 WP LT ELEVATOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 611NA 47435 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN A LEFT ELEVATOR GEARED TAB HINGE FITTING. REPLACED FITTI NG (P/N 3918075-509) PER SRM 51-30-2. 2 L 7 2 4F A6WE 1996031500213 19960315 00213 WP 1996 3 15 9605669611 1 19960305 A 5320 FITTING DOUG DC9 DC932 3022066 WP FS 996 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 611NA 47435 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE INTERCOSTAL ATTACH FITTING AT FS 996, LONGERON 28R. R EPLACED FITTING PER SRM 51-30-02. 2 L 7 2 4F A6WE 1996031500214 19960315 00214 NM 1996 3 15 9605776739 1 19960309 A 5315 FLOOR BEAM BOEING 747 747251F 1384898 NM FS 1210-1260 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 639US 23887 DURING PERIODIC CHECK, FOUND FLOOR BEAM FLANGE AT STA 1210 - STA 1260 CORRODED BEYOND SRM LIMITS. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-10-01 AND EA 67-99581. 2 L 7 4 4F A20WE 1996031500215 19960315 00215 NE 1996 3 15 9605781149 2 19960309 A 7200 ENGINE DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20J 52054 NE NR 3 FOD A NWAA E D ENGINE SHUTDOWN RETURN TO BLOCK C J F.O.D. WARNING INDICATION TX TAXI/GRND HDL 1 GL 01 149US 46758 86146 DURING TAXIING, THE NR 3 ENGINE GENERATOR CAME OFF-LINE FOLLOWED BY HIGH EGT OF 840 DEGREES. THE ENGINE WAS SHUT DOWN A ND THE AIRCRAFT RETURNED TO THE GATE. GROUND CREW AND SEVERAL PASSENGERS NOTED WHAT APPEARED LIKE A PIECE OF PLASTIC BE ING SUCKED INTO THE ENGINE FOLLOWED BY BLACK SMOKE. PERFORMED FOD INSPECTION AND RUN-UP AT TAKEOFF POWER. CHECKS WERE NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A22WE E20EA 1996031500216 19960315 00216 NM 1996 3 15 9605796304 1 19960311 A 3350 LIGHTS BOEING 747 747451 1384940 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 664US 23819 DURING LINE CHECK, THE FLOOR MOUNTED EMERGENCY PATCH LIGHTS AT SEAT ROWS 32R THROUGH 42R WERE FOUND INOPERATIVE. RECONN ECTED EMERGENCY LIGHT CONNECTOR PIN AT SEAT ROW 32R. OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996031500217 19960315 00217 WP 1996 3 15 9605809993 1 19960310 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP LT NACELLE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8986E 47402 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996031500218 19960315 00218 WP 1996 3 15 9605819969 1 19960308 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9333 47246 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND BULB S. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996031500219 19960315 00219 WP 1996 3 15 9605829976 1 19960309 A 5350 HANDLE DOUG DC9 DC931 3022065 WP TAILCONE MALFUNCTIONED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9340 47389 DURING FUNCTIONAL CHECK OF TAILCONE RELEASE SYSTEM, EXCESSIVE FORCE WAS REQUIRED TO DROP THE TAILCONE USING THE INTERIOR HANDLE. REPLACED THE INTERIOR HANDLE AND SUPPORT PLATE. SYSTEM CHECKED NORMAL. 2 L 7 2 4F A6WE 1996031500220 19960315 00220 WP 1996 3 15 9605839980 1 19960309 A 5350 CLIPS DOUG DC9 DC931 3022065 WP TAILCONE MALFUNCTIONED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9344 47440 DURING FUNCTIONAL CHECK OF TAILCONE RELEASE SYSTEM, EXCESSIVE FORCE WAS REQUIRED TO RELEASE INTERIOR HANDLE FROM CLIPS. REPLACED CLIPS PER EO 5350-01049. 2 L 7 2 4F A6WE 1996031500221 19960315 00221 WP 1996 3 15 9605849933 1 19960309 A 3010 ANTI ICE DUCT DOUG DC9 DC931 3022065 WP LT LE FLAPS BINDING A NWAA O OTHER F P FLT CONT AFFECTED NO WARNING INDICATION AP APPROACH 1 GL 01 1334U 47280 SLAT DISAGREEMENT LIGHT ILLUMINATED WITH NOTICEABLE ROLL TO THE RIGHT WHEN SLATS WERE EXTENDED FOR LANDING INTO DTW. CYC LED SLATS WITH SAME RESULTS. SUCCESSFUL LANDING WAS ACCOMPLISHED USING FLAPS ONLY. NOTE: BLUE SLAT EXTEND LIGHT NEVER ILLUMINATED. MAINTENANCE FOUND LEFT ANTI-ICE T-DUCT BINDING. REPLACED DUCT. ALSO, LUBED SLAT ROLLERS. OPERATIONAL C HECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996031500222 19960315 00222 WP 1996 3 15 9605859955 1 19960311 A 2910 1474252 VALVE DOUG DC9 DC931 3022065 WP RT HYD SYSTEM LEAKING A NWAA O OTHER K FLUID LOSS CL CLIMB 1 GL 01 922RW 39169 47182 LOSS OF RIGHT HYDRAULIC SYSTEM QUANTITY OCCURRED DURING CLIMBOUT FROM YWG. FLIGHT CONTINUED TO DESTINATION (MSP). CAPTA IN DECLARED YELLOW EMERGENCY AND AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED BRAKE/SPOILER VALVE. ALSO, REPLACED CASE D RAIN FILTERS. LEAK AND OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996031500223 19960315 00223 WP 1996 3 15 9605869940 1 19960311 A 2432 BATTERY DOUG DC9 DC932 3022066 WP BATTERY COMPT MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 3322L 47031 A STEADY BATTERY CHARGE RATE OF 15 TO 18 AMPS WAS OBSERVED DURING CLIMBOUT. FLIGHT RETURNED TO DTW AND LANDED WITHOUT I NCIDENT. REPLACED THE BATTERY CHARGER, MAIN BATTERY, AND SENSOR. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVI CE. 2 L 7 2 4F A6WE 1996031500224 19960315 00224 EU 1996 3 15 9605873201 1 19960308 A 5210 MECHANISM AIRBUS 320 A320211 3930320 EU R1 DOOR FROZEN A NWAA O OTHER O OTHER IN INSP/MAINT 1 GL 01 301US 031 DURING GROUND OPERATIONS, THE DOOR 1R WOULD NOT DISARM DUE TO BEING FROZEN. LUBRICATED GIRT BAR AND MECHANISM. OPERATI ONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996031500225 19960315 00225 WP 1996 3 15 9605889161 1 19960308 A 3350 BATTERY PACK DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8905E 45746 DURING LINE CHECK, FOUND COCKPIT EMERGENCY LIGHTS WOULD NOT ILLUMINATE. REPLACED BATTERY PACK AND OPERATIONAL CHECK GOO D. 2 L 7 2 4F A6WE 1996031500226 19960315 00226 WP 1996 3 15 9605899851 1 19960310 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 760NC 47708 DURING LINE CHECK, FOUND LEFT WING EMERGENCY LIGHT OUT. REPLACED POWER SUPPLY. CHECKED GOOD. 2 L 7 2 4F A6WE 1996031500227 19960315 00227 WP 1996 3 15 9605909991 1 19960310 A 7930 CLOG LIGHT DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7 52053 NE NR 2 ENGINE ILLUMINATED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 8957E 47215 653677 NR 2 ENGINE OIL FILTER CLOG WARNING LIGHT ILLUMINATED ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNE D TO THE GATE. MAINTENANCE INSPECTED THE OIL FILTER; NO CONTAMINANTS NOTED. THE OIL FILTER WAS REPLACED AND THE ENGINE WAS RUN-UP. NO FURTHER DISCREPANCIES NOTED. 2 L 7 2 4F 4 F A6WE E2EA 1996031500228 19960315 00228 WP 1996 3 15 ABXA9600249 1 19960311 A 3231 RETRACT MECH DOUG DC8 DC862 3021970 WP NLG DOOR LACK OF LUBE A ABXA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 23 805AX 45906 DURING GEAR RETRACTION AFTER TAKEOFF, A LOUD NOISE WAS HEARD FROM THE NOSE GEAR AREA. THE LANDING GEAR RETRACTED AND TH E LIGHTS WENT OUT. RECYCLED GEAR AND CONDITION REMAINED. FOUND LEFT NOSE LANDING GEAR DOOR UNLATCHED. CLEANED AND LUB ED THE ACTUATOR MECHANICAL RELEASE AND PISTON. VERIFIED DOOR LOCKING OPERATION. 2 L 7 4 4F 4A25 1996031500229 19960315 00229 NE 1996 3 15 ARWA9603006 2 19960308 A 7261 B NUT DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE TURBINE CASE LOOSE A ARWA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 19 441J 45988 AIRCRAFT RETURNED TO MIA DUE TO LOSS OF OIL QUANTITY, NR 3 ENGINE. FOUND NR 6 BEARING FILTER B-NUT LOOSE, RESECURED AND SAFETIED. NO LEAKS NOTED ON RUN-UP -- RESERVICED OIL TANK AS REQUIRED IAW MM 79-20-00 AND MM 72-50-00. 2 L 7 4 4F 4 F 4A25 1E8 1996031500230 19960315 00230 SO 1996 3 15 COMA9610097 1 19960308 A 3231 12012347001 LATCH ASSY EMB 120 EMB120RT SO RT MLG DOOR BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 1110J 120110 RIGHT MLG DOOR FOUND IN THE OPEN POSITION DURING PREFLIGHT. REPLACED BROKEN DOOR LATCH ASSY. 2 L 7 2 4T RT A31SO 1996031500231 19960315 00231 SO 1996 3 15 COMA9610098 1 19960308 A 3150 CIRCUIT BREAKER EMB 120 EMB120RT SO AURAL WARNING TRIPPED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 265CA 120257 TRIM AURAL WARNING SOUNDED DURING TAKEOFF ROLL. FOUND AURAL WARNING CIRCUIT BREAKER TRIPPED. RESET BREAKER AND SYSTEM TEST NORMAL. 2 L 7 2 4T RT A31SO 1996031500232 19960315 00232 SO 1996 3 15 COMA9610099 1 19960308 A 2910 2025000002 SWIVEL EMB 120 EMB120RT SO LT MLG LEAKING A COMA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 162CA 120150 HYDRAULIC FLUID LEAKAGE ON LEFT MLG STRUT. REPLACED BROKEN LINE SWIVEL FITTING. 2 L 7 2 4T RT A31SO 1996031500233 19960315 00233 SO 1996 3 15 COMA9610100 1 19960309 A 3230 INTRANSIT LIGHT EMB 120 EMB120RT SO LT MLG MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 256CA 120245 LEFT MLG INTRANSIT LIGHTS REMAIN ON AFTER LANDING GEAR RETRACTED. COULD NOT DUPLICATE DISCREPANCY. FOUND ALL ADJUSTMEN TS AND CLEARANCES WITHIN LIMITS. ACFT RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 1996031500234 19960315 00234 SO 1996 3 15 COMA9610101 1 19960309 A 5753 12033048001 TRACK EMB 120 EMB120RT SO LT TE FLAP WORN A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 179CA 120179 FLAP DISAGREEMENT WARNING SHORTLY AFTER TAKEOFF. REPLACED WORN FLAP TRACKS ON LEFT OUTBOARD FLAP. 2 L 7 2 4T RT A31SO 1996031500235 19960315 00235 EU 1996 3 15 COMA9630060 1 19960310 A 2450 M83726291002P RELAY SAAB SF340 SF340A 7850100 EU E/E COMPT DEFECTIVE A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 140N 340A140 LEFT MAIN BUS FAILED 4 TIMES AND RESET ITSELF EACH TIME AFTER 4 MINUTES. REPLACED THE TIME DELAY RELAY 71PC. 2 L 7 2 4T RT A52EU 1996031500236 19960315 00236 EU 1996 3 15 COMA9630061 1 19960309 A 2622 892480 FIRE EXT SAAB SF340 SF340A 7850100 EU CABIN CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 320CA 19530 660 340A064 CABIN FIRE EXTINGUISHER HANDLE IS HARD TO ROTATE. CLEANED AND REASSEMBLED FIRE EXTINGUISHER AND RETURNED TO SERVICE. P ART TOTAL CYCLES, 22,156. 2 L 7 2 4T RT A52EU 1996031500237 19960315 00237 EU 1996 3 15 COMA9630062 1 19960308 A 3240 BRAKES SAAB SF340 SF340A 7850100 EU RIGHT REQD SERVICE A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 342CA 340A023 WHEN AIRCRAFT HYDRAULIC PUMP CYCLES ON, THE RT BRAKES GRAB. COULD NOT DUPLICATE DISCREPANCY. BLED BRAKE HYDRAULIC SYST EM AND ACFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 1996031500238 19960315 00238 EA 1996 3 15 COMA9660039 1 19960308 A 2750 857SD100 FLEX SHAFT CNDAIR CL600 CL6002B19 EA TE FLAPS DAMAGED A COMA K NONE O OTHER LD LANDING 1 SO 01 915CA 7013 FLAPS FAILED AT ZERO DEGREES. REPLACED DAMAGED FLAP FLEX DRIVE CABLE. 2 L 7 2 4F RT A21EA 1996031500239 19960315 00239 NM 1996 3 15 DL72E960549 1 19960227 A 5744 FITTING BOEING 727 727247 138408F NM NR 4 FLAP TRACK PITTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831WA 21483 LT MLG NR 4 FLAP TRACK PORKCHOP FITTING HAS PITTED BUSHING. FORWARD HOLE BORED TO 1.7068 INCH PER MM 57-42-0, PAGE 814. MPI PER PS 900-6-2, NR 01. OK. TURNED O/D OF BUSHING BRUSH CAD FITTING IN STRIKE CAD PLATE BUSHING, PAINTED FITTING PE R MM 57-42-0. INSTALLED BUSHING. OK TO INSTALL BUSHING TOP COATED REF MM 57-42-0. 2 L 7 3 4F A3WE 1996031500240 19960315 00240 NM 1996 3 15 DL72K960517 1 19960307 A 3260 POSITION SWITCH BOEING 727 727232 1384082 NM PWA 2037 PW2037 NE NLG MALFUNCTIONED A DALA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 SO 27 471DA 20748 716323 UPON NOSE GEAR EXTENSION, HAD AN UNSAFE NOSE GEAR INDICATION. INDICATED WERE TWO GREEN MAIN GEAR LIGHTS AND ONE RED NOS E GEAR LIGHT. NO DOOR LIGHTS WERE ILLUMUMINATED. PERFORMED EMERG CK LIST IAW POM INCLUDING AN ATTEMPT AT MANUAL GEAR E XTENSION TO NO AVAIL. VISUAL INSP OF GEAR THROUGH VIEWING PORT SHOWED NOSE DOWN AND LOCKED. UPON FLAP SELECTION TO 30 DEGREES, HAD AN AURAL GEAR WARNING. SILENCED WARNING AND HAD NORMAL LANDING. PIN GEAR AND TAXI TO GATE. REMOVED AND R EPLACED NOSE GEAR POSITION SWITCH 93, ADJUSTED. OPS CK OK MM 32-61-71, PAGE 501. 2 L 7 3 4F 4 F A3WE E17NE 1996031500241 19960315 00241 NM 1996 3 15 DL72K960531 1 19960308 A 5312 BLKHD BEAM BOEING 727 727232 1384082 NM BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 491DA 21060 FOUND DURING A-2 LETTER CHECK - 1.50 INCH CRACK VERTICAL BEAM BS 1183 BLKHD AT RBL 8. REPAIRED PER MM 53-11-0, PG 811 . 2 L 7 3 4F A3WE 1996031500242 19960315 00242 NE 1996 3 15 DL72K960541 2 19960310 A 7321 FUEL CONTROL 37820113 BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE FAILED A DALA O OTHER X ENGINE FLAMEOUT TO TAKEOFF 1 SO 27 491DA 1901 21060 687434 ENGINE FAILURE, NR 3, AT LIFT-OFF - FUEL TO ZERO WITH NORMAL WIND DOWN INDICATIONS. REPLACED FCU AND ENGINE DRIVEN FUEL PUMP. 2 L 7 3 4F 4 F A3WE E2EA 1996031500243 19960315 00243 NM 1996 3 15 DL72K960545 1 19960307 A 5330 651753062 SKIN BOEING 727 727232 1384082 NM BS 1250 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 412DA 21232 DURING A MID-VISIT, A CRACK WAS FOUND IN THE FUSELAGE SKIN AT STA 1250 NEAR STRINGER 23R. THERE WAS AN EXISTING REPAIR DOUBLER IMMEDIATELY FORWARD OF THE DAMAGE. INSTALLED PER ER/A 233656-14. AFT TERMINATION POINT OF THE EXISTING DOUBLER IS ROUGHLY AT STA 1243. EXISTING REPAIR DOUBLER WAS REMOVED AND A SINGLE DOUBLER WAS INSTALLED TO INCLUDE THE THREE CU T-OUTS PER DL ERA 303265-14. 2 L 7 3 4F A3WE 1996031500244 19960315 00244 NM 1996 3 15 DL72P960537 1 19960310 A 2782 ACTUATOR 10605582 BOEING 727 727225 1384077 NM NR 4 LE FLAP FAILED A DALA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 SO 27 8891Z 1417DEFGK 21860 POSITION NR 4 LE FLAP WENT UNLOCK FL 270 IN CLIMB. RECYCLED, UNABLE TO GET RETRACT INDICATION. CORRECTIVE ACTION....RE PLACED LE ACTUATOR POS NR 4 PER MM 27-81-27. ADJUSTED SWITCH PER MM 27-82-1. GROUND CHECK NORMAL. INDICATION OK. LEA K CHECK OK. 2 L 7 3 4F A3WE 1996031500245 19960315 00245 NM 1996 3 15 DL72S960522 1 19960306 A 2782 BRACKET BOEING 727 727232 1384082 NM NR 2/7 SLAT MISINSTALLED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 546DA 22677 DURING MID-VISIT, THE NR 2 AND NR 7 SLAT ACTUATOR MOUNT BRACKETS WERE FOUND WITH GAPS EXCEEDING THE 0.01 INCH LIMIT SET BY S.I. 4-59271-12. GAPS ARE SUBJECT OF S/B 727-57-1030. SHIMS WERE INSTALLED IN ACCORDANCE WITH THE SERVICE BULLETIN. BRACKETS WERE NOT FOUND TO BE CRACKED. 2 L 7 3 4F A3WE 1996031500246 19960315 00246 NM 1996 3 15 DL72S960530 1 19960301 A 5754 651622194 SKIN BOEING 727 727232 1384082 NM NR 5 LE SLAT WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 546DA 22677 DURING A ROUTINE HANGAR INSPECTION, NR 637 WAS WRITTEN DUE TO A GROOVE WORN IN INNER SKIN OF NR 5 SLAT. THE DAMAGE WAS REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1996031500248 19960315 00248 NM 1996 3 15 DL72S960542 1 19960303 A 5754 SKIN BOEING 727 727232 1384082 NM NR 4 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 546DA 22677 HMV/ATL - NR 4 SLAT TOP SKIN - CRACK AT OUTBOARD SIDE OF STALL FENCE MID-AREA SCREW ATTACH POINT. CORRECTION: REMOVED F ENCE. INSTALLED DOUBLER REPAIR PER MM 57-40-0. 2 L 7 3 4F A3WE 1996031500249 19960315 00249 NM 1996 3 15 DL72W960518 1 19960307 A 5754 ANGLE BOEING 727 727247 138408F NM NR 1 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2821W 21059 FOUND DURING B-2 LETTER CHECK - 1 INCH CRACK NR 1 L/E SLAT COVE SKIN ATTACH ANGLE BELOW TAI DUCT. REPAIRED PER M/M 57-5 4-0 PAR 12. 2 L 7 3 4F A3WE 1996031500250 19960315 00250 NM 1996 3 15 DL72W960519 1 19960307 A 5754 ANGLE BOEING 727 727247 138408F NM NR 8 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2821W 21059 FOUND DURING B-2 LETTER CHECK - NR 8 L/E SLAT COVE SKIN ATTACH ANGLE CRACKED AT OUTBOARD UPSTOP PAD. REPAIRED PER M/ M 57-54-0, PAR 5A. 2 L 7 3 4F A3WE 1996031500251 19960315 00251 NM 1996 3 15 DL72W960535 1 19960309 A 3350 LIGHT 1000677 BOEING 727 727247 138408F NM COCKPIT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2811W 24727 20649 COCKPIT EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSY. OPS CHECKS GOOD. 2 L 7 3 4F A3WE 1996031500252 19960315 00252 NE 1996 3 15 DL73S960534 2 19960309 A 7200 ENGINE BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE NR 2 FAILED A DALA E A ENGINE SHUTDOWN UNSCHED LANDING E J Y VIBRATION/BUFFET WARNING INDICATION ENGINE STOPPAGE CL CLIMB 1 SO 27 318DL 23367 23090 717150 EXPERIENCED MULTIPLE COMPRESSOR STALLS ON NR 2 ENGINE AT APPROXIMATELY 6,000 FEET MSL ON DEP CVG INSTANTEOUS OVERTEMP AS SOCIATED WITH MODERATE VIBRATION ACCOMPANIED STALLS. VISUAL FLAMES ALSO ACCOMPANIED BACKFIRES. NO EXTERNAL DAMAGE OR EV IDENCE OF OTHER ABNORMAL COMPLICATIONS AFTER SHUT DOWN. EMERGENCY RETURN RUNWAY 18L. ACCOMPLISHED AT CVG. REPLACED NR 2 ENGINE AND ROUTED TO SHOP. ENGINE TOTAL CYCLES, 20,393. 2 L 7 2 4F 4 F RT A16WE E2EA 1996031500253 19960315 00253 NE 1996 3 15 DL757960516 2 19960305 A 7321 78360014068 EEC BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 ENGINE FAILED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 613DL 22820 716323 DURING CLIMB-OUT THROUGH 7,000 FEET, LEFT ENGINE BEGAN TO SURGE REDUCING POWER. CORRECTED SURGING, BUT WHEN CLIMB POWER WAS AGAIN APPLIED, THE SURGING RESUMED. RETURNED LAX. REPLACED LT EEC. REPLACED LT PMA STATOR. REPLACED 14 STG CONV ERTER VALVE AND 14 STG VALVE. ALL CKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996031500254 19960315 00254 NM 1996 3 15 DL76L960544 1 19960222 A 2840 HG1057LR02 PROCESSOR BOEING 767 767332 1382001 NM FUEL IND SYSTEM MALFUNCTIONED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 174DN 24802 DIVERTED BDL DUE WEATHER, DURING DIVERSION HAD EICAS STATUS MESSAGE FUEL QUANTITY CHANNEL. PERFORMED BITE, FAULTS PROCE SSOR CHANNELS 1 AND 2. COULD NOT DISPATCH. REPLACED PROCESSOR PER M/M. PERFORMED BITE, OPERATION NORMAL. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK 2 L 7 2 4F RT A1NM 1996031500255 19960315 00255 NM 1996 3 15 DL76S960503 1 19960305 A 2560 ARMED LIGHT B417T65132 BOEING 767 767332 1382001 NM 2 L DOOR FAILED A DALA K NONE P NO WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 136DL 23146 2L DOOR SLIDE ARMED LIGHT NOT ILLUMINATING WHEN THE SLIDE IS ARMED. LIGHT ASSY PRESS-TO-TESTS NORMALLY. CORRECTIVE ACT ION - FORWARD TO MCO AND PLACED PER MEL. REPLACED LIGHT ASSEMBLY OPERATION NORMAL. 2 L 7 2 4F RT A1NM 1996031500256 19960315 00256 WP 1996 3 15 DLL13960514 1 19960307 A 5312 1504400 BLKHD WEB LKHEED 1011 10113851 5265010 WP FS 1212 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 786DL 193A1123 THE FS 1212 BLKHD WAS FOUND WITH A 7 INCH VERTICAL CRACK AT RBL 22.5. THE CRACK WAS CUT OUT AND A REPAIR FILLER AND DOU BLER WERE INSTALLED PER DL ERA 273431-14A. 2 L 7 3 4F A23WE 1996031500257 19960315 00257 NM 1996 3 15 DLM88960526 1 19960307 A 3222 STRUT DOUG MD88 MD88 3023688 NM NLG REQD SERVICE A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 982DL 53273 NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED DFW. C/A - FOUND NOSE GEAR FROZEN WITH WATER IN STRUT. DRAINED A ND RESERVICED. SWUNG GEAR, OPERATION NORMAL. 2 L 7 2 4F RT A6WE 1996031500258 19960315 00258 NM 1996 3 15 DLM88960527 1 19960307 A 3222 STRUT DOUG MD88 MD88 3023688 NM NLG REQD SERVICE A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 989DL 53341 NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. FOUND WATER IN NOSE STRUT FLUID RESERVICED. CHECKED NORMAL DURING RETRACTIO N. 2 L 7 2 4F RT A6WE 1996031500259 19960315 00259 NM 1996 3 15 DLM88960529 1 19960308 A 3222 STRUT DOUG MD88 MD88 3023688 NM NLG REQD SERVICE A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 905DE 53410 AFTER TAKEOFF, GEAR WOULD NOT RETRACT, USED REL, GOT MAINS UP, NOT NOSE GEAR, A/C STAYED IN GROUND MODE. RETURNED PHL. LANDED UNEVENTFULLY, NOSE GEAR STEERABLE. SERVICED NOSE STRUT PER MM 32 21 02. CYCLED NOSE GEAR, OPS NORMAL. 2 L 7 2 4F RT A6WE 1996031500260 19960315 00260 NM 1996 3 15 DLM88960532 1 19960308 A 3222 STRUT DOUG MD88 MD88 3023688 NM NLG REQD SERVICE A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 982DL 53273 ON TAKEOFF, GEAR RETRACTION LANDING GEAR LIGHTS INDICATED AN UNSAFE NOSE GEAR. EXTENDED GEAR, GOT THREE DOWN AND LOCKED . RETURNED TO AIRPORT. LOUD NOISE ACCOMPANIED UNSAFE INDICATION AS THOUGH GEAR DOOR NOT CLOSED. SWUNG NOSE GEAR. ALL INDICATION IS GOOD. FOUND NOSE STRUT PNEUMATIC CHRG UNDERSERVICED. VERIFIED PROPER FLUID LEVEL. SERVICED PNEUMATIC C HRG PROPERLY. RAN STRUT ENTIRE LENGTH SEVERAL TIMES. SWUNG GEAR. RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 1996031500261 19960315 00261 NM 1996 3 15 UPS96205621 1 19960213 A 5320 672492 CLIP BOEING 727 727185C 138406N NM BS 360 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 WHILE IN FOR D-CHECK, MAINTENANCE REPORTED STRINGER CLIP AT BS 360 AND STRINGER 1 IS CORRODED. REMOVED AND REPLACED CLI P I.A.W. SRM 51-30-2. 2 L 7 3 4F A3WE 1996031500262 19960315 00262 NM 1996 3 15 UPS96205622 1 19960214 A 5313 STRINGER BOEING 727 727185C 138406N NM BS 1030-1060 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 WHILE IN FOR D-CHECK, MAINTENANCE REPORTED CORROSION ON STR 20R, STA 1030-1060. CUT OUT DAMAGED AREA PER SRM 53-10-3. R EPLACED STR 20R FROM STA 1040-1060 AND INSTALLED SPLICE AT STA 1020-1030, STR 20R I.A.W. SRM 53-10-3, FIG. 4, AND SRM 51 -30-2. 2 L 7 3 4F A3WE 1996031500263 19960315 00263 NM 1996 3 15 UPS96205623 1 19960221 A 5330 SKIN BOEING 727 727185C 138406N NM FS 1080 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 WHILE IN FOR D-CHECK, MAINTENANCE REPORTED FUSELAGE SKIN UPPER LAP CORRODED BEYOND LIMITS AT STR 10R, FROM FS 1080-1122. REMOVED DAMAGE PER SRM 53-30-03 AND INSTALLED CONICAL WASHERS PER SRM 51-30-5 AND INSTALLED REPAIR PARTS PER SRM 51-30 -5. 2 L 7 3 4F A3WE 1996031500264 19960315 00264 NM 1996 3 15 UPS96205624 1 19960214 A 5330 SKIN BOEING 727 727185C 138406N NM BS 520 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 WHILE IN FOR D-CHECK, MAINTENANCE REPORTED FS 520, STR 23R, LOWER FORWARD CARGO DOOR SKIN CRACKED. REMOVED DAMAGED AREA AND INSTALLED REPAIR PARTS I.A.W. DHC SK-940-271 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996031500265 19960315 00265 NM 1996 3 15 UPS96205625 1 19960215 A 5313 STRINGER BOEING 727 727185C 138406N NM BS 1050 CORROSION A IPXA O OTHER O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 WHILE IN FOR D-CHECK, MAINTENANCE REPORTED CORROSION ON STR 19L, STA 1050. CORROSION OUT OF LIMITS. INSTALLED REPAIR P ARTS PER BOEING SRM 53-10-3. CORROSION REMOVED PER SRM 57-10-6. 2 L 7 3 4F A3WE 1996031500266 19960315 00266 NM 1996 3 15 UPS96205626 1 19960220 A 5313 STRINGER BOEING 727 727185C 138406N NM BS 440 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 WHILE IN FOR D-CHECK, MAINTENANCE REPORTED FS 420-440, STR 9L, HAS CORROSION UNDER EDGE OF LAP AND FS 440, STR 8L-10L HA S CORROSION UNDER CIRCUMFERENTIAL JOINT ON FORWARD SIDE. REPAIRED PER SRM 51-30-2, 51-10-6, 51-20-4 AND DWG NR 69-62161 . 2 L 7 3 4F A3WE 1996031500267 19960315 00267 NM 1996 3 15 UPS96205627 1 19960220 A 5347 SEAT TRACK BOEING 727 727185C 138406N NM BS 929 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 WHILE IN FOR D-CHECK, MAINTENANCE REPORTED MAIN CABIN SEAT TRACK AT RBL 62, BS 929 TO 932 HAS EXFOLIATION CORROSION. RE MOVED DAMAGED SECTION OF TRACK, ALODINED AND PRIMED AND FASTENED PER SRM 51-10-2, 51-30-2, AND 53-10-5. 2 L 7 3 4F A3WE 1996031500268 19960315 00268 NM 1996 3 15 UPS96205628 1 19960214 A 5320 SPLICE BOEING 727 727185C 138406N NM BS 1070 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 WHILE IN FOR D-CHECK, MAINTENANCE REPORTED CORROSION ON STR SPLICE 20L, STA 1070-1090. FABRICATED AND INSTALLED STR SEC TION AND SPLICES PER BOEING SRM 53-10-3 AND 51-30-2. 2 L 7 3 4F A3WE 1996031500269 19960315 00269 NM 1996 3 15 UPS96205629 1 19960215 A 5330 SKIN BOEING 727 727185C 138406N NM BS 580 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 WHILE IN FOR D-CHECK, MAINTENANCE REPORTED CORROSION ON SKIN BELOW FLOOR STA 580, STR 17R. REMOVED DAMAGED AREA, FABRIC ATED AND INSTALLED DOUBLER PER BOEING SRM 51-40-2 AND 51-30-2. 2 L 7 3 4F A3WE 1996031500270 19960315 00270 NM 1996 3 15 UPS96205630 1 19960228 A 5313 STRINGER BOEING 727 727185C 138406N NM BS 1166-1183 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 WHILE IN FOR D-CHECK, MAINTENANCE REPORTED LAP AT STA 1166-1183 AT STR 10R OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICA TED REPAIR PARTS, AND INSTALLED REPAIR PER SRM 53-30-3 AND SRM 51-30-5. 2 L 7 3 4F A3WE 1996031500271 19960315 00271 NM 1996 3 15 UPS96205631 1 19960209 A 5711 SPAR BOEING 727 727185C 138406N NM WS 304 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 WHILE IN FOR D-CHECK, MAINTENANCE REPORTED RT WING REAR SPAR UPPER CHORD CRACKED AT W.S. 304 ABOVE MLG SUPPORT BEAM ATTA CH FITTING. CUT OUT DAMAGE AREA, FABRICATED REPAIR PARTS PER BOEING DWG 65C21546, 65-16233 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996031500272 19960315 00272 NM 1996 3 15 UPS96205632 1 19960301 A 5313 STRINGER BOEING 727 727185C 138406N NM BS 455-460 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 WHILE IN FOR D-CHECK, MAINTENANCE REPORTED STR 22L CORRODED FROM STA 440 TO STA 460 REMOVED BEYOND LIMITS. CORROSION RE PAIRED AT STRINGER FROM STA 443-468 I.A.W. SRM 53-10-3. 2 L 7 3 4F A3WE 1996031500273 19960315 00273 NM 1996 3 15 UPS96205633 1 19960219 A 5320 INTERCOSTAL BOEING 727 727185C 138406N NM BS 1148-1160 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 WHILE IN FOR D-CHECK, MAINTENANCE REPORTED INTERCOSTAL CRACKED AT STA 1148-1166 AND STR 22R. REMOVED, FABRICATED, AND I NSTALLED INTERCOSTAL PER SRM 53-10-2 AND SRM 53-30-2. 2 L 7 3 4F A3WE 1996031500274 19960315 00274 NM 1996 3 15 UPS96205634 1 19960213 A 5720 FITTING BOEING 727 727185C 138406N NM RT REAR SPAR CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 WHILE IN FOR D-CHECK, MAINTENANCE REPORTED CORROSION AROUND BUSHING IN FITTING, FORWARD SIDE OF RT WING REAR SPAR FOR AT TACHMENT OF MLG SUPPORT BEAM. REMOVED AND REPAIRED FITTING NR 65-16290 PER BOEING DWG NR 65-16290 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996031500275 19960315 00275 NM 1996 3 15 UPS96205635 1 19960208 A 5230 FITTING BOEING 727 727185C 138406N NM MAIN CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 WHILE IN FOR D-CHECK, MAINTENANCE REPORTED MAIN DOOR LATCH SUPPORT FITTING CRACKED B/S 560, REF N/R 428722. REMOVED AND REPLACED CARGO DOOR LATCH SUPPORT FITTING PER DHC SK-940-769 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996031500276 19960315 00276 NM 1996 3 15 UPS96205636 1 19960215 A 5313 STRINGER BOEING 727 727185C 138406N NM BS 440-460 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 WHILE IN FOR D-CHECK, MAINTENANCE REPORTED STA 440-460, STR 18L HAS CORROSION. REMOVED DAMAGED AREA AND INSTALLED REPAI R PARTS PER SRM 53-10-3 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996031500277 19960315 00277 NM 1996 3 15 UPS96205637 1 19960214 A 5320 ANGLE BOEING 727 727185C 138406N NM BS 295.5-267 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 WHILE IN FOR D-CHECK, MAINTENANCE REPORTED NLG LT TUNNEL, STA 295.5 TO STA 267 C/P SUB-FLOOR SUPPORT ANGLE HAS SEVERE CO RROSION. REMOVED DAMAGED AREA, FABRICATED, AND INSTALLED T-ANGLE REPAIR PER BOEING SRM 51-40-2, 51-40-4, AND 51-30-2. 2 L 7 3 4F A3WE 1996031500278 19960315 00278 NM 1996 3 15 UPS96205638 1 19960214 A 5320 INTERCOSTAL BOEING 727 727185C 138406N NM BS 304 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 WHILE IN FOR D-CHECK, MAINTENANCE REPORTED CABIN FLOOR INTERCOSTAL UPPER OUTBOARD FLANGE HAS A 1.5 INCH CRACK AT RBL 44 AND BS 304 UNDER FORWARD LAV. REMOVED DAMAGED AREA PER SRM 51-40-3, FABRICATED AND INSTALLED FILLER AND REPAIR ANGLE PE R SRM 51-10-2, 51-30-2, AND 51-40-3. 2 L 7 3 4F A3WE 1996031500279 19960315 00279 NM 1996 3 15 UPS96205639 1 19960215 A 5320 INTERCOSTAL BOEING 727 727185C 138406N NM BS 294.5 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 WHILE IN FOR D-CHECK, MAINTENANCE REPORTED INTERCOSTAL HAS CORROSION ABOVE LAV SERVICE PANEL TO FRAME 294.5 AND 518R. R EMOVED, FABRICATED, AND INSTALLED REPLACEMENT LATCH CHANNEL PER SRM 51-10-1 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996031500280 19960315 00280 NM 1996 3 15 UPS96205640 1 19960215 A 5320 SHEAR TIE BOEING 727 727185C 138406N NM BS 294.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 WHILE IN FOR D-CHECK, MAINTENANCE REPORTED FUSELAGE FRAME SHEAR TIE IS CRACKED NEAR THE RADIUS UPPER END BETWEEN S20R AN D S21R, BS 294.5. REMOVED DAMAGED AREA PER SRM 51-40-3. FABRICATED ANGLE AND REPAIRED PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996031500281 19960315 00281 NM 1996 3 15 UPS96205641 1 19960117 A 5531 SPAR BOEING 727 72725C 138400H NM VERT STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 WHILE IN FOR MOD WORK, MAINTENANCE REPORTED FS 1342, THE VERTICAL FIN REAR SPAR CHORD CRACKED. REPAIRED I.A.W. BOEING D WG 69-70556. 2 L 7 3 4F A3WE 1996031500282 19960315 00282 NM 1996 3 15 UPS96205642 1 19960110 A 5531 RIB BOEING 727 72725C 138400H NM VERT STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 WHILE IN FOR MOD WORK, MAINTENANCE REPORTED RT RIB CRACKED BS 1367 FIN STA 22.5. CUT OUT DAMAGE AND REPAIRED WEB I.A.W. SRM 51-40-2. 2 L 7 3 4F A3WE 1996031500283 19960315 00283 NM 1996 3 15 UPS96205643 1 19960104 A 5313 STRINGER BOEING 727 72725C 138400H NM BS 294.5 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 WHILE IN FOR MOD WORK, MAINTENANCE REPORTED STR 26L AT BS 294.5 HAS HEAVY CORROSION. INSTALLED REPLACEMENT ANGLE PER SR M 51-30-2 AND SRM 53-10-2. 2 L 7 3 4F A3WE 1996031500284 19960315 00284 NM 1996 3 15 UPS96205644 1 19960128 A 5330 SKIN BOEING 727 72725C 138400H NM BS 1243-1342 GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 WHILE IN FOR MOD WORK, MAINTENANCE REPORTED SKIN PANEL STA 1243-1342, STR 11R-14R HAS GOUGE. REMOVED SKIN, FABRICATED, AND INSTALLED STRINGER PER BOEING DWG 65-17558 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996031500285 19960315 00285 NM 1996 3 15 UPS96205645 1 19960128 A 5330 SKIN BOEING 727 72725C 138400H NM BS 1243-1342 GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 WHILE IN FOR MOD WORK, MAINTENANCE REPORTED SKIN PANEL STA 1243-1342, STR 11L-14L HAS GOUGE. REMOVED SKIN, FABRICATED A ND INSTALLED STRINGER PER BOEING DWG 65-17528 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996031500286 19960315 00286 NM 1996 3 15 UPS96205646 1 19960119 A 5320 WINDOW FRAME BOEING 727 72725C 138400H NM BS 590 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 WHILE IN FOR MOD WORK, MAINTENANCE REPORTED RT WINDOW FRAME FS 590 AFTER CORROSION REMOVAL. LOWER FLANGE FOUND BEYOND L IMITS PER SRM 56-20-1 ON NR 408510. FABRICATED DOUBLER AND INSTALLED CONICAL WASHERS PER SRM 56-20-3, FIG. 1. INSTALLE D REPAIR DOUBLER PER SRM 56-20-3, FIG.1. 2 L 7 3 4F A3WE 1996031500287 19960315 00287 NM 1996 3 15 UPS96205647 1 19960119 A 5320 WINDOW FRAME BOEING 727 72725C 138400H NM BS 530 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 WHILE IN FOR MOD WORK, MAINTENANCE REPORTED RT WINDOW FRAME FS 530 AFTER CORROSION REMOVAL, FLANGE FOUND BEYOND LIMITS P ER SRM 56-20-1 ON NR 408505. FABRICATED DOUBLER AND INSTALLED CONICAL WASHERS PER SRM 56-20-3, FIG 1. INSTALLED REPAIR DOUBLER PER SRM 56-20-3, FIG 1. 2 L 7 3 4F A3WE 1996031500288 19960315 00288 NM 1996 3 15 UPS96205648 1 19960204 A 5530 CHORD BOEING 727 72725C 138400H NM VERT STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 WHILE IN FOR MOD WORK, MAINTENANCE REPORTED LT INNER CHORD FIN STA 22.5 IS CRACKED. REMOVED DAMAGED AREA I.A.W. BOEING DWG 65C20296. INSTALLED REPAIR DOUBLER PER BOEING DWG 65C20296 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996031500289 19960315 00289 NM 1996 3 15 UPS96205649 1 19960119 A 5753 SPAR CHORD BOEING 727 72725C 138400H NM LT TE MIDFLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 WHILE IN FOR MOD WORK, MAINTENANCE REPORTED LT INBOARD MID-FLAP WBL 124.2 REAR SPAR 4TH FASTENER HOLE REVEALED A CRACK O N SPAR CAP BELOW SKIN AT 3 O'CLOCK POSITION. LOWER PANEL WAS OPENED, 10 EACH FASTENERS REMOVED. REPAIRED HOLE AREA I.A .W. DHC SK 949-436 AND E.O. B727-5750-3582 APP AND C-5750-7667A. 2 L 7 3 4F A3WE 1996031500290 19960315 00290 NM 1996 3 15 UPS96205661 1 19960310 A 3350 LIGHT BOEING 727 72725C 138400H NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 931UP 19858 MAINTENANCE REPORTED EMERGENCY LIGHT IN COCKPIT FAILED. REMOVED AND REPLACED LIGHT ASSY. OPS NORMAL. 2 L 7 3 4F A3WE 1996031500291 19960315 00291 NE 1996 3 15 UPS96405614 2 19960306 A 7200 ENGINE BOEING 747 747121 1384871 NM PWA JT9 JT9D7A 52054 NE NR 2 FAILED A IPXA E ENGINE SHUTDOWN Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SO 01 682UP 20349 CREW REPORTED EN ROUTE TO YQX, NR 2 ENGINE FAILED AT 16:21Z. N2 SEIZED, EGT PEAKED AT 935 DEGREES. CREW ACCOMPLISHED A LL APPLICABLE CHECKLIST PROCEDURES PER AOM. PERFORMED UNEVENTFUL LANDING AT GANDER, NEWFOUNDLAND, 17:47Z. 2 L 7 4 4F 4 F A20WE E20EA 1996031500292 19960315 00292 NM 1996 3 15 UPS96405650 1 19960308 A 2140 DECK HEATER BOEING 747 747123 1384873 NM COCKPIT MALFUNCTIONED A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 01 672UP 20324 CREW REPORTED STRONG ELECTRICAL SMELL BEGAN DURING DESCENT. ISOLATED TO RT UPPER DECK HEATER. NO ABNORMAL INDICATIONS, BUT BURNING SMELL RECURRED WITH RT UPPER DECK HEATER ON. DEFFERED RT UPPER DECK HEATER, M 10789 ASSIGNED PER MEL SEQ N R 21-18-2. 2 L 7 4 4F A20WE 1996031500293 19960315 00293 NM 1996 3 15 UPS96405659 1 19960308 A 3350 LIGHT BOEING 747 747SR46 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 680UP 20923 MAINTENANCE REPORTED EMERGENCY LIGHT OUT IN CEILING INBOARD 5L DOOR. REMOVED AND REPLACED LIGHT ASSY. OPS NORMAL. 2 L 7 4 4F A20WE 1996031500294 19960315 00294 WP 1996 3 15 UPS96805613 1 19960305 A 2560 GIRT BAR DOUG DC8 DC873F 302199F WP ESCAPE SLIDE OUT OF ADJUST A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 MAINTENANCE REPORTED ESCAPE SLIDE CONTAINER INSECURE. SLIDE BAR WOULD NOT ENGAGE IN CLIPS. SECURED AND RE-POSITIONED. 2 L 7 4 4F RT 4A25 1996031500295 19960315 00295 WP 1996 3 15 UPS96805615 1 19960215 A 5320 SHEARTIE DOUG DC8 DC873F 302199F WP BS 55 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED SHEARTIE CRACKED AT F.S. 55, BETWEEN LONGERONS 28L-30L. REPLACED SHEARTIE SE CTION PER SRM 53-2-0. 2 L 7 4 4F RT 4A25 1996031500296 19960315 00296 WP 1996 3 15 UPS96805616 1 19960212 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 80 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED BOLT FRAME SUPPORT ANGLE CRACKED AT F.S. 80, LONGERON 33L. REPAIRED ANGLE PE R DPS 10.225. 2 L 7 4 4F RT 4A25 1996031500297 19960315 00297 WP 1996 3 15 UPS96805617 1 19960215 A 5320 SHEARTIE DOUG DC8 DC873F 302199F WP BS 35 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED SHEARTIE CRACKED AT F.S. 35 BETWEEN LONGERONS 28L-30L. REPLACED SHEARTIE SEC TION PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996031500298 19960315 00298 WP 1996 3 15 UPS96805618 1 19960213 A 5320 SUPPORT DOUG DC8 DC873F 302199F WP BS 80 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED BOLT FRAME SUPPORT ANGLE CRACKED AT F.S. 80, LONGERON 33R. REPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996031500299 19960315 00299 WP 1996 3 15 UPS96805619 1 19960208 A 5530 5651927 ANGLE DOUG DC8 DC873F 302199F WP VERT STAB CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON VERTICAL STABILIZER TO FUSELAGE RT ATTACH ANGLE. REPAIRED ANGLE PER SRM 53-2-5, FIG. 16A. 2 L 7 4 4F RT 4A25 1996031500300 19960315 00300 WP 1996 3 15 UPS96805620 1 19960208 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP BS 67 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FUSELAGE SKIN DOUBLER CRACKED AT LOWER FORWARD CORNER OF LT PRIMARY HEAT EXCH ANGER. REPAIRED PER UPS E.O. 2 L 7 4 4F RT 4A25 1996031500301 19960315 00301 NE 1996 3 15 HEEA966758 2 19960228 A 7210 3024780 GEARBOX BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE NR 1 POWER SECT MAKING METAL E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D 5089 33076 METAL GENERATION FROM #1 POWER SECTION COMBINING GR BOX. 1 G 7 2 4U 4 U H4SW E22EA 1996031500302 19960315 00302 GL 1996 3 15 HEEA966759 2 19960228 A 7314 3881005 PUMP BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL FUEL SYS WORN EXCESS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 41128 3142 51134 FUEL PUMP IS WORN EXCESSIVELY. (WORN INTERNAL SPLINES) 1 G 7 1 3U 3 U H2SW E1GL 1996031500304 19960315 00304 1996 3 15 HEEA966761 4 19960228 A 3416 A30 ENCODER BELL 206 206L1 1182107 SW COCKPIT ERROR E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1077A 45382 ALTIMETER ENCODER REPORTS 100 FEET HIGH AND WILL NOT CALIBRATE. 1 G 7 1 3U H2SW 1996031500305 19960315 00305 1996 3 15 HEEA966762 4 19960228 A 3444 4004437901 ALTIMETER RT220 BELL 412 412 1182202 SW COCKPIT ERRATIC E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 108X 33115 ERRATIC FROM 500 FEET AND UPWARDS. 1 G 7 2 4U H4SW 1996031500306 19960315 00306 SW 1996 3 15 HEEA966763 1 19960228 A 6330 206033554101 LINK ASSY BELL 206 206L1 1182107 SW XMSN MOUNT BEARING WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5006F 45181 LINK ASSY LOWER BEARING WORN. S/N LK6747 & LK11088 1 G 7 1 3U H2SW 1996031500307 19960315 00307 SW 1996 3 15 HEEA966764 1 19960228 A 7810 212061201012 EJECTOR ASSY BELL 412 412 1182202 SW RT EXHAUST DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D 33076 RT EJECTOR DRAIN FITTING BROKEN. 1 G 7 2 4U H4SW 1996031500308 19960315 00308 SW 1996 3 15 HEEA966765 1 19960228 A 2844 BSE20630G TRANSDUCER BELL 206 206L1 1182107 SW FUEL PRESSURE DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 27766 45312 INDICATES "0" PRESSURE. 1 G 7 1 3U H2SW 1996031500309 19960315 00309 EU 1996 3 15 HEEA966766 1 19960228 A 2840 81141010010 TRANSMITTER AEROSP AS355 AS355F1 8680810 EU FUEL SYS DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5793Y 5141 CONTACTS OPEN FROM 1.2 TO 1.4 BARS THEN CLOSES. 1 G 7 2 3U H11EU 1996031500310 19960315 00310 1996 3 15 HEEA966767 4 19960228 A 2562 DK100 BATTERY BOLKMS 105 BO105S 5626006 EU LOCATOR BEACON LOW VOLTS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 BEACON DC VOLTAGE TOO LOW. 1 G 7 2 3U H3EU 1996031500311 19960315 00311 1996 3 15 HEEA966768 4 19960228 A 3421 1113034 INDICATOR BELL 412 412 1182202 SW COCKPIT ATTITUDE STUCK E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 7128R 36007 INDICATOR STUCK AT 15 DEGREES IN ROLL. 1 G 7 2 4U H4SW 1996031500312 19960315 00312 1996 3 15 HEEA966771 4 19960228 A 3416 37500220 ALTIMETER BELL 206 206L1 1182107 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2124Z 45646 ALTIMETER INDICATES 200 FEET LOW; EXCESSIVE CASE LEAK. 1 G 7 1 3U H2SW 1996031500314 19960315 00314 1996 3 15 HEEA966773 4 19960228 A 2210 214074303115 AMPLIFIER ASSY BELL 214 214ST 1182106 SW AUTO FLIGHT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 8045T 28101 ROLL NETWORK VOLTAGES ARE ERRATIC. TIME SINCE REPAIR 470:50. 2 G 7 2 4U H10SW 1996031500315 19960315 00315 SW 1996 3 15 HEEA966774 1 19960228 A 6330 206033506101 RESTRAINT BELL 206 206L1 1182107 SW TRANSMISSION BEARING DEFECT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1078D 45397 TRANS RESTRAINT BEARING UNSTAKED. 1 G 7 1 3U H2SW 1996031500316 19960315 00316 SW 1996 3 15 HEEA966775 1 19960228 A 6330 206033506101 RESTRAINT BELL 206 206L1 1182107 SW TRANSMISSION BEARING WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2249Z 45753 RESTRAINT HAS WORN BEARINGS. 1 G 7 1 3U H2SW 1996031500317 19960315 00317 SW 1996 3 15 HEEA966776 1 19960228 A 6330 206033506101 RESTRAINT BELL 206 206L1 1182107 SW TRANSMISSION BEARING WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5012V 45200 RESTRAINT HAS BEARING PLAY. 1 G 7 1 3U H2SW 1996031500319 19960315 00319 SW 1996 3 15 HEEA966781 1 19960228 A 2120 205072277009 VALVE BELL 412 412 1182202 SW AIR DIST DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 107X 33113 VALVE WILL NOT OPEN, OVERHEATS AND POPS CIRCUIT BREAKER. 1 G 7 2 4U H4SW 1996031500320 19960315 00320 SW 1996 3 15 HEEA966782 1 19960228 A 6220 2020H9 DAMPER BELL 212 212 1181420 SW M/R OIL DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5736J 31140 DAMPER HYDRAULIC FLUID DARK, UNABLE TO SEE PIN. 1 G 7 1 4U H4SW 1996031500321 19960315 00321 SW 1996 3 15 HEEA966783 1 19960228 A 6330 206033516101 FLEXURE BELL 206 206L1 1182107 SW XMSN DETERIORATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5007Y 45192 FLEXURE HAS DETERIORATED ELASTOMER. 1 G 7 1 3U H2SW 1996031500323 19960315 00323 SW 1996 3 15 HEEA966785 1 19960228 A 6330 214031615105 CLEVIS ARM BELL 214 214ST 1182106 SW MR XMSN MT WORN E HEEA K NONE E VIBRATION/BUFFET IN INSP/MAINT 1 SW 03 3897N 28106 CLEVIS ASSY CAUSING VIBRATION, SUSPECT WORN RUBBER. 2 G 7 2 4U H10SW 1996031500324 19960315 00324 1996 3 15 HEEA966786 4 19960228 A 3416 A30 ENCODER AEROSP AS355 AS355F2 8680812 EU COCKPIT ALTIMETE ERROR E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 6040U 5474 ENCODER 200 FEET OFF AND WILL NOT CALIBRATE. 1 G 7 2 3U H11EU 1996031500325 19960315 00325 SW 1996 3 15 HEEA966787 1 19960228 A 6330 206033554101 LINK ASSY BELL 206 206L3 1182108 SW XMSN MT BEARING GALLED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 8587X 51464 LINK ASSY ID OF TOP BEARING GALLED. 1 G 7 1 3U H2SW 1996031500326 19960315 00326 1996 3 15 HEEA966788 4 19960228 A 2562 ELT910 ELT NARCO BELL 206 206L1 1182107 SW COCKPIT MALFUNCTION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3178K 45765 ELT CAME ON THREE TIMES IN FLIGHT. 1 G 7 1 3U H2SW 1996031500327 19960315 00327 1996 3 15 HEEA966789 4 19960228 A 3421 7660002113103 GYRO SKRSKY S76 S76A 8143006 NE COCKPIT VG PRECESSES E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1546K 760082 VERT GYRO PRECESSING. 1 G 7 2 3U H1NE 1996031500328 19960315 00328 SW 1996 3 15 HEEA966790 1 19960228 A 2824 L88010491 VALVE BELL 412 412 1182202 SW FUEL XFER INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2261D 33076 VALVE INOPERATIVE. WILL NOT ACTUATE. 1 G 7 2 4U H4SW 1996031500329 19960315 00329 1996 3 15 HEEA966792 4 19960228 A 3421 4021541671 HORIZON GYRO BOLKMS 117 BK117A3 5626015 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 401PH 7050 GYRO TUMBLES WHILE CAGING, FLAG PULL IS SLOW, CAUSES PITCH/ROLL CSAS TO BE UNRELIABLE. 1 G 7 2 3U H13EU 1996031500330 19960315 00330 1996 3 15 HEEA966793 4 19960228 A 3453 066402600 LORAN KLN88 BELL 206 206L3 1182108 SW COCKPIT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 6610Y 51419 LORAN LOCKS UP AND WILL NOT SELF TEST OR FUNCTION WHEN POWER IS RESET AND UNIT DROPS USER WAYPOINTS. 1 G 7 1 3U H2SW 1996031500331 19960315 00331 1996 3 15 HEEA966794 4 19960228 A 3457 0845000000 SKYNAV 5000 BELL 206 206L1 1182107 SW COCKPIT GPS DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2775A 45297 GPS WILL NOT RECEIVE SATELLITES AND LOSES WAYPOINTS, ALSO DISPLAYS FOREIGN CHARACTERS. 1 G 7 1 3U H2SW 1996031500332 19960315 00332 1996 3 15 HEEA966795 4 19960228 A 3442 MI5851352 RADAR P40 BELL 212 212 1181420 SW RT UNIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5736J 31140 RADAR SCREEN INTERMITTENTLY FLASHES SOLID GREEN. ALSO UNIT HAS NO VOLTAGE GAIN AND NO RECEIVER SENSITIVITY. 1 G 7 1 4U H4SW 1996031500333 19960315 00333 SW 1996 3 15 HEEA966796 1 19960228 A 5320 206033410021 INTERCOSTAL BELL 206 206L3 1182108 SW FUSELAGE DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6610Y 51419 IMPROPER RIVETS INSTALLED IN INTERCOSTAL. REPLACED WITH SERVICEABLE INTERCOSTAL. 1 G 7 1 3U H2SW 1996031500334 19960315 00334 1996 3 15 HEEA966797 4 19960228 A 2312 4000106010 CONTROL UNIT C10 BELL 206 206L1 1182107 SW COCKPIT VHF DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 513EH 45421 THUMBWHEELS DON'T AGREE WITH DISPLAY. TRIED CLEANING THUMBWHEEL. NO HELP. REPLACED THUMBWHEEL S1. REPAIRED. BENCH CH ECK GOOD. 1 G 7 1 3U H2SW 1996031500335 19960315 00335 NE 1996 3 15 HEEA966798 1 19960228 A 6210 7615009100048A BLADE SKRSKY S76 S76A 8143006 NE M/R UNBONDED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3122G 11684 760232 TIP RIB UNBONDED, AND TIME EXTENSION IS ALSO DUE. 1 G 7 2 3U H1NE 1996031500336 19960315 00336 1996 3 15 HEEA966799 4 19960228 A 3453 4530103 LORAN ARNAV21 BOLKMS 105 BO105S 5626006 EU COCKPIT INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 721MB S752 LORAN WILL NOT COME ON - INOPERATIVE. 1 G 7 2 3U H3EU 1996031500337 19960315 00337 1996 3 15 HEEA966800 4 19960228 A 3444 071111400 ANTENNA BOLKMS 105 BO105S 5626006 EU RADAR ALTIMETER WONT TEST E HEEA K NONE L NO TEST NR NOT REPORTED 1 SW 03 911EB S812 ANTENNA WILL NOT TEST. 1 G 7 2 3U H3EU 1996031500338 19960315 00338 NE 1996 3 15 HEEA966801 2 19960228 A 7200 0292005220 ENGINE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE COMPRESSOR OIL LOSS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 2771 LOSS OF OIL OUT OF TAIL PIPE, BLEED VALVE AND COMPRESSOR. 1 G 7 1 3U 3 U H9EU E19EU 1996031500339 19960315 00339 EU 1996 3 15 HEEA966802 1 19960228 A 7170 0174126090 DRAIN VALVE SNIAS 350 AS350B2 8680813 EU ENGINE FUEL LEAK E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 6095S 1153 2777 FUEL LEAKING AT UPPER MATING SURFACE ON SHUTDOWN. 1 G 7 1 3U H9EU 1996031500340 19960315 00340 GL 1996 3 15 HEEA966803 1 19960228 A 6710 206062721105 ACTUATOR BELL 230 230 1182149 SW ALLSN 250C 250C30G2 03013 GL ENG CONTROL DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 230UN 215 23009 UNABLE TO BEEP DUAL ENGINE RPM UP OR DOWN. 1 G 7 2 3U 3 U NC H9SW E1GL 1996031500341 19960315 00341 1996 3 15 HEEA966804 4 19960228 A 3453 27010045 ANTENNA BELL 412 412 1182202 SW LORAN DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 22608 33075 LORAN SLOW TO ACQUIRE STATIONS AND GIVE READOUTS. 1 G 7 2 4U H4SW 1996031500342 19960315 00342 1996 3 15 HEEA966805 4 19960228 A 3453 4520183 ANTENNA ARNAV SKRSKY S76 S76A 8143006 NE LORAN DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1545X 760050 WILL NOT LOCK ON TO SIGNAL. 1 G 7 2 3U H1NE 1996031500343 19960315 00343 SW 1996 3 15 HEEA966807 1 19960301 A 6321 206076049001 HOUSING 206076047101 BELL 206 206L3 1182108 SW ROTOR BRAKE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4180F 7073 FEB1391 51469 HOUSING CRACKED BETWEEN FLUID RESERVOIR AND PISTON HOUSING. WOULD NOT HOLD PRESS. 1 G 7 1 3U H2SW 1996031500344 19960315 00344 1996 3 15 HEEA966812 4 19960301 A 3416 8503S20LW5V ALTIMETER SKRSKY S76 S76A 8143006 NE COCKPIT READS LOW E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5435V 760158 ALTIMETER NEEDLE INDICATES 180 FEET LOW AT 20K. 1 G 7 2 3U H1NE 1996031500345 19960315 00345 SW 1996 3 15 HEEA966822 1 19960304 A 6510 204040623003 BEARING 212040600005 BELL 412 412 1182202 SW T/R DRIVE DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893P 988 A2008782 33012 BEARING SHIELD ROTATING. 1 G 7 2 4U H4SW 1996031500346 19960315 00346 SW 1996 3 15 HEEA966823 1 19960304 A 6410 206010765001 BEARING 206016201127 BELL 206 206L3 1182108 SW T/R BLADE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 363BH 511 CS1838 51345 BEARINGS CRACKED. ALSO REPLACED 2 EACH SLEEVES P/N 206-010-733-003 AND 4 EACH SPACERS P/N 206-011-742-101. 1 G 7 1 3U H2SW 1996031500347 19960315 00347 SW 1996 3 15 HEEA966824 1 19960304 A 6410 206010765001 BEARING 206016201127 BELL 206 206L3 1182108 SW T/R BLADE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 363BH 449 CS7262 51345 BEARINGS CRACKED. ALSO REPLACED 2 EACH SLEEVES P/N 206-010-733-003 AND 4 EACH SPACERS P/N 206-011-742-101. HELD AT PHI FOR CSR SIGNATURE. NOTE: SEE MMIR# HEEA0006823 FOR 2 EACH ADDITIONAL BEARINGS REMOVED. 1 G 7 1 3U H2SW 1996031500348 19960315 00348 SW 1996 3 15 HEEA966825 1 19960304 A 6410 206010765001 BEARING 206011810135 BELL 206 206L3 1182108 SW T/R BLADE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 41128 771 A463 51134 DISASSEMBLED T/R HUB AND BLADE ASSEMBLY FOR OVERHAUL. FOUND INBOARD BEARINGS CRACKED ON BLADE S/N CS4037 AND BLADE S/N CS4316. ALSO REPLACED 4 EACH SLEEVES P/N 206-010-733-003 AND 8 EACH SPACERS P/N 206-011-742-101. 1 G 7 1 3U H2SW 1996031500349 19960315 00349 SW 1996 3 15 HEEA966826 1 19960304 A 6410 206010765001 BEARING 206016201127 BELL 206 206B 1181511 SW T/R BLADE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 39122 1046 CS60786045 3312 BEARINGS CRACKED. ALSO REPLACED 4 EACH SLEEVES, P/N 206-010-733-003 AND 8 EACH SPACERS, P/N 206-011-742-101.NOTE: SEE MMIR #6826 THROUGH #6835 FOR ADDITIONAL BEARINGS REPLACED. 1 G 7 1 3U H2SW 1996031500350 19960315 00350 SW 1996 3 15 HEEA966827 1 19960304 A 6410 206010765001 BEARING 206016201127 BELL 206 206L1 1182107 SW T/R BLADE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 20898 788 CS65416447 45721 BEARINGS CRACKED. ALSO REPLACED 4 EACH SLEEVES, P/N 206-010-733-003 AND 8 EACH SPACERS, P/N 206-011-742-101. NOTE: SE E MMIR'S # 6826 THROUGH #6835 FOR ADDITIONAL BEARING REPLACEMENTS. 1 G 7 1 3U H2SW 1996031500351 19960315 00351 SW 1996 3 15 HEEA966828 1 19960304 A 6410 206010765001 BEARING 206016201127 BELL 206 206L3 1182108 SW T/R BLADE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6161A 1991 CS58825500 51611 BEARINGS CRACKED. ALSO REPLACED 4 EACH SLEEVES, P/N 206-010-733-003 AND 8 EACH SPACERS, P/N 206-011-742-101. NOTE: SE E MMIR'S # 6826 THROUGH #6835 FOR ADDITIONAL BEARING REPLACEMENTS. 1 G 7 1 3U H2SW 1996031500352 19960315 00352 SW 1996 3 15 HEEA966829 1 19960304 A 6410 206010765001 BEARING 206016201127 BELL 206 206L1 1182107 SW T/R BLADE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 10814 972 CS52015169 45415 BEARINGS CRACKED. ALSO REPLACED 4 EACH SLEEVES, P/N 206-010-733-003 AND 8 EACH SPACERS, P/N 206-011-742-101. NOTE: S EE MMIR # 6826 THROUGH #6835 FOR ADDITIONAL BEARINGS REPLACED. 1 G 7 1 3U H2SW 1996031500353 19960315 00353 SW 1996 3 15 HEEA966830 1 19960304 A 6410 206010765001 BEARING 206016201127 BELL 206 206L3 1182108 SW T/R BLADE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3116P 746 CS68316826 51530 BEARINGS CRACKED. ALSO REPLACED 4 EACH SLEEVES, P/N 206-010-733-003 AND 8 EACH SPACERS, P/N 206-011-742-101. NOTE: SE E MMIR'S # 6826 THROUGH #6835 FOR ADDITIONAL BEARING REPLACEMENTS. 1 G 7 1 3U H2SW 1996031500354 19960315 00354 SW 1996 3 15 HEEA966831 1 19960304 A 6410 206010765001 BEARING 206016201127 BELL 206 206L3 1182108 SW T/R BLADE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6160Y 1576 CS63426490 51609 BEARINGS CRACKED. ALSO REPLACED 4 EACH SLEEVES, P/N 206-010-733-003 AND 8 EACH SPACERS, P/N 206-011-742-101. NOTE: SE E MMIR'S # 6826 THROUGH #6835 FOR ADDITIONAL BEARING REPLACEMENTS. 1 G 7 1 3U H2SW 1996031500355 19960315 00355 SW 1996 3 15 HEEA966832 1 19960304 A 6410 206010765001 BEARING 206016201127 BELL 206 206L 1181522 SW T/R BLADE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7077F 905 CS53146309 52038 BEARINGS CRACKED. ALSO REPLACED 4 EACH SLEEVES, P/N 206-010-733-003 AND 8 EACH SPACERS, P/N 206-011-742-101. NOTE: SE E MMIR'S # 6826 THROUGH #6835 FOR ADDITIONAL BEARING REPLACEMENTS. 1 G 7 1 3U H2SW 1996031500356 19960315 00356 SW 1996 3 15 HEEA966833 1 19960304 A 6410 206010765001 BEARING 206016201127 BELL 206 206L 1181522 SW T/R BLADE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7077B 800 CS48905049 52037 BEARINGS CRACKED. ALSO REPLACED 4 EACH SLEEVES, P/N 206-010-733-003 AND 8 EACH SPACERS, P/N 206-011-742-101. NOTE: S EE MMIR'S # 6826 THROUGH #6835 FOR ADDITIONAL BEARING REPLACEMENTS. 1 G 7 1 3U H2SW 1996031500357 19960315 00357 SW 1996 3 15 HEEA966834 1 19960304 A 6410 206010765001 BEARING 206016201127 BELL 206 206L1 1182107 SW T/R BLADE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 10761 432 CS60466062 45381 BEARINGS CRACKED. ALSO REPLACED 4 EACH SLEEVES, P/N 206-010-733-003 AND 8 EACH SPACERS, P/N 206-011-742-101. NOTE: SE E MMIR'S # 6826 THROUGH #6835 FOR ADDITIONAL BEARING REPLACEMENTS. 1 G 7 1 3U H2SW 1996031500358 19960315 00358 SW 1996 3 15 HEEA966835 1 19960304 A 6410 206010765001 BEARING 206016201127 BELL 206 206L3 1182108 SW T/R BLADE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31801 2266 CS4819 51074 BEARINGS CRACKED. ALSO REPLACED 2 EACH SLEEVES, P/N 206-010-733-003 AND 4 EACH SPACERS, P/N 206-011-742-101. NOTE: SE E MMIR'S # 6826 THROUGH #6835 FOR ADDITIONAL BEARING REPLACEMENTS. 1 G 7 1 3U H2SW 1996031500359 19960315 00359 SW 1996 3 15 HEEA966837 1 19960308 A 3213 214052004101 SHOE ASSY BELL 214 214ST 1182106 SW SKID MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 5748M 28102 SHOE ASSY BOLT HOLES DO NOT LINE UP DURING INSTALLATION. 2 G 7 2 4U H10SW 1996031500360 19960315 00360 1996 3 15 HEEA966838 4 19960308 A 3416 5934P1 ALTIMETER SNIAS 350 AS350B2 8680813 EU COCKPIT READS LOW E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 2690 2771 ALTIMETER READS 200 FEET LOW. 1 G 7 1 3U H9EU 1996031500361 19960315 00361 EU 1996 3 15 HEEA966839 1 19960308 A 6240 DL43638 INDICATOR BOLKMS 105 BO105S 5626006 EU TRIPLE TACH STICKS E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 911EB S812 ROTOR NEEDLE INTERMITTENTLY STICKS. 1 G 7 2 3U H3EU 1996031500362 19960315 00362 1996 3 15 HEEA966840 4 19960308 A 3444 066104800 ALTIMETER KRA405 BELL 412 412 1182202 SW RADAR ALT FLUCTUATES E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2149S 36002 NEEDLE FLUCTUATES. REPLACED RESISTOR R518,R519,R534 AND R260 TO INCORPORATE MOD 10 AS PER KING SERVICE BULLETIN KRA-405- 10. BENCH CHECK GOOD. 1 G 7 2 4U H4SW 1996031500363 19960315 00363 1996 3 15 HEEA966841 4 19960308 A 3444 066104802 ALTIMETER KRA405 BELL 412 412 1182202 SW RADAR ALT FLUCTUATES E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 21498 36003 IN FLIGHT 200 FEET NEEDLE FLUCTUATES. INSTALLED MOD 10 AS PER SERVICE BULLETIN KING KRA-405-10. PERFORMED COMPLETE CALI BRATION AND ALIGNMENT. BENCH CHECK GOOD. 1 G 7 2 4U H4SW 1996031500364 19960315 00364 1996 3 15 HEEA966842 4 19960308 A 3444 066304400 ALTIMETER BELL 412 412 1182202 SW RADAR AL;T DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 21498 36003 BENCH CHECK REQUIRED. FOUND PH LIGHT DOES NOT DIM. REPLACED PHOTOCELL V101. REPAIRED. PERFORMED COMPLETE CALIBRATION AND ALIGNMENT. BENCH CHECK GOOD. 1 G 7 2 4U H4SW 1996031500403 19960315 00403 NM 1996 3 15 9605916635 1 19960312 A 2913 350880 HYD PUMP BOEING 747 747227B 1384888 NM NR 1 ENGINE FAILED A NWAA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 01 635US 25035 49 21682 DURING APPROACH, THE NR 1 HYDRAULIC SYSTEM LOST HYDRAULIC FLUID. DECLARED EMERGENCY AND ALTERNATELY EXTENDED LANDING GE AR AND FLAPS. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP AND OPERATIONAL CHECK G OOD. 2 L 7 4 4F A20WE 1996031500404 19960315 00404 NM 1996 3 15 9605922285 1 19960312 A 2932 ST7R HYD PRESS TRANS BOEING 727 727251 138408H NM A-HYD SYST FAILED A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 285US 116 55 21324 DURING CRUISE FLIGHT, SYSTEM-A HYDRAULICS HAD A RAPID LOSS OF FLUID. AIRCRAFT DIVERTED TO MEM AND LANDED WITHOUT INCIDE NT. REPLACED THE SYSTEM-A HYDRAULIC TRANSMITTER AND LEAK CHECK OK. 2 L 7 3 4F A3WE 1996031500405 19960315 00405 WP 1996 3 15 9605939979 1 19960309 A 5330 SKIN DOUG DC9 DC931 3022065 WP CARGO DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9343 47439 DURING LINE MAINTENANCE INSPECTION, FOUND CRACK IN FUSELAGE SKIN AT FORWARD UPPER CORNER OF FORWARD CARGO DOOR CUTOUT. F ABRICATED DOUBLER FROM 2024-TC, .160 AL. INSTALLED PER EA 99-099563. 2 L 7 2 4F A6WE 1996031500406 19960315 00406 WP 1996 3 15 9605949927 1 19960306 A 5311 FRAME DOUG DC9 DC931 3022065 WP TAIL CONE AREA WORN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8920E 45835 DURING LINE MAINTENANCE INSPECTION, FOUND FUSELAGE FRAMES WORN AT UPPER AND LOWER RIGHT AND LEFT TAIL CONE LATCH BAYONET HOLES. REPAIRED PER EA 99-109443 AND REPLACED LOWER FRAME SECTIONS. 2 L 7 2 4F A6WE 1996031500407 19960315 00407 NM 1996 3 15 9605956739 1 19960311 A 5720 BEAM BOEING 747 747251F 1384898 NM LT WING CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 639US 23887 DURING PERIODIC CHECK, FOUND UPPER FLANGE ON THE LEFT WING OUTBOARD LEADING EDGE BEAM CRACKED IN RADIUS. STOP DRILLED C RACK AND CUT OUT DAMAGED AREA. FABRICATED DOUBLER AND FILLER FROM 7075 AND HEAT TREATED TO T6. REPAIR WAS ACCOMPLISHED PER EA 67-103263, SEC 1. 2 L 7 4 4F A20WE 1996031500408 19960315 00408 EU 1996 3 15 9605963216 1 19960307 A 5320 WEB AIRBUS 320 A320211 3930320 EU FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 316US 192 DURING PERIODIC CHECK, THE TRIANGLE WEB PANEL AFT OF FRAME 68, NEAR THE FUSELAGE SKIN WAS FOUND CRACKED. STOP DRILLED C RACK AND SEALED PER EA 32-106827. 2 L 7 2 4F RT A28NM 1996031500409 19960315 00409 EU 1996 3 15 9605973213 1 19960217 A 7830 TR UNIT AIRBUS 320 A320211 3930320 EU NR 1 ENGINE MALFUNCTIONED A NWAA E ENGINE SHUTDOWN X ENGINE FLAMEOUT LD LANDING 1 GL 01 313US 153 DURING LANDING, THE NR 1 ENGINE FLAMED OUT AFTER COMING OUT OF SECOND THRUST REVERSER ENGAGEMENT AND ENGINE RESTARTED DU RING TAXI INTO GATE. GROUND MAINTENANCE INSPECTED, RAN AND OPERATED NR 1 ENGINE THRUST REVERSER SEVERAL TIMES, NO PROBL EMS FOUND. 2 L 7 2 4F RT A28NM 1996031500410 19960315 00410 NM 1996 3 15 9605982708 1 19960305 A 3244 TIRE CAP BOEING 727 727225 1384077 NM NR 2 SEPARATED A NWAA O OTHER C E F.O.D. VIBRATION/BUFFET LD LANDING 1 GL 01 817EA 22554 ON LANDING ROLLOUT, CREW EXPERIENCED VIBRATION FROM THE MAIN LANDING GEAR. ON POST FLIGHT INSPECTION, FOUND NR 2 TIRE C AP HAD SEPARATED FROM THE TIRE AND HAD DAMAGE TO FLAPS AND UNDERSIDE OF WING. THE TRAILING EDGE FLAP, MIDFLAP AND FOREF LAP WERE REMOVED, REPAIRED AND REINSTALLED. REPLACED THE LEFT INBOARD GROUND SPOILER PANEL AND NR 2 TIRE. THE NR 1 ENG INE WAS BORESCOPED FOR FOREIGN OBJECT DAMAGE. OPERATIONAL CHECK OF FLAPS AND SPOILERS CHECKED OK. 2 L 7 3 4F A3WE 1996031500411 19960315 00411 NM 1996 3 15 96FDEA00518 1 19960313 A 5350 RADOME BOEING 727 72722 1384002 NM BS 175 CHIPPED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 WHILE WORKING CARD 71C102-01, FOUND RADOME TO BE MISALIGNED AT BS 178 ALLOWING RADOME TO CATCH DOUBLER WHICH CRACKED DOU BLER AND CHIPPED RADOME WL 285, LBL 4. REPAIRED RADOME WL 285 LBL 4, PER SRM 53-50-4 AND REPAIRED SKIN DOUBLER AT BS 17 8 WL 235 LBL 4 PER EA 7-5310-27737. 2 L 7 3 4F A3WE 1996031500412 19960315 00412 NM 1996 3 15 96FDEA00519 1 19960312 A 5330 SKIN BOEING 727 72722 1384002 NM BS 423 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 WHILE PERFORMING PRESSURIZATION DISCOVERED CRACK IN EXTERIOR SKIN BS 423, JUST BELOW STR 23 RT. REPAIRED EXTERIOR SKIN IAW SRM 53-30-3 FIG 2. 2 L 7 3 4F A3WE 1996031500413 19960315 00413 NM 1996 3 15 96UAL900178 1 19960311 A 2450 AUTO BUSS BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE RT AC SYST MALFUNCTIONED A UALA O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 WP 29 618UA 21878 RIGHT AC AUTO BUS TIE DID NOT PICK UP LOAD WHEN RIGHT GENERATOR TRIPPED. AT CRUISE TRIED TURNING OFF RIGHT BUS WITH APU GEN ON LINE. RIGHT BUS TIE BREAKER WOULD NOT PICK UP POWER FROM OTHER SOURCE WITH BTB SWITCH IN AUTO. 2 L 7 2 4F 4 F RT A1NM E3NE 1996031500414 19960315 00414 NM 1996 3 15 96UAL900179 1 19960311 A 3350 BATTERY PACK BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 618UA 21878 THREE EXTERIOR EMERGENCY LIGHTS ON RIGHT SIDE INOP. TWO OVER THE WING AND ONE BY THE RIGHT FORWARD ENTRY DOOR. REPLACE D BATTERY PACK. 2 L 7 2 4F 4 F RT A1NM E3NE 1996031500415 19960315 00415 NM 1996 3 15 96UAL900180 1 19960311 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 520UA 24890 SEAT 34C OVERHEAD EMERGENCY LAMP INOP. RELAMPED. 2 L 7 2 4F 4 F RT A2NM E17NE 1996031500416 19960315 00416 NM 1996 3 15 96UAL900181 1 19960311 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 562UA 26664 RIGHT SIDE EXTERNAL EMERGENCY LIGHT INOP FORWARD OF DOOR 4. RELAMPED. 2 L 7 2 4F 4 F RT A2NM E17NE 1996031500417 19960315 00417 NM 1996 3 15 96UAL900182 1 19960311 A 2781 655280739 ACCESSORY UNIT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LE FLAPS FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 337UA 24241 NR 4 LEADING EDGE FLAP WOULD NOT RETRACT. SUPPLEMENTAL DATA UPDATE: REPLACED FLAP/SLAT POSITION SWITCH ACCESSORY UNIT. SYSTEM CHECKED GOOD. FAILURE OF THE ACCESSORY UNIT COULD NOT BE VERIFIED BY THE HOME SHOP. 2 L 7 2 4F 4 F RT A16WE E2GL 1996031500418 19960315 00418 NM 1996 3 15 96UAL900183 1 19960311 A 3397 WIRE BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 160UA 21237 EMERGENCY EXIT LIGHT FROM DOOR 2R TO SEAT 17GH INOP. REPLACED FEEDER CABLE. 2 L 7 4 4F 4 F A20WE E20EA 1996031500420 19960315 00420 NM 1996 3 15 96UAL900185 1 19960312 A 3350 LIGHT STRIP BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE CABIN DAMAGED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 9068U 19949 EMERGENCY ESCAPE PATH LIGHTING INOP FROM ROW 15 TO ROW 18. REPLACED DAMAGED LIGHT STRIP AND CHECKS OK. 2 L 7 2 4F 4 F A16WE E2EA 1996031500421 19960315 00421 EU 1996 3 15 96UAL900186 1 19960312 A 3350 POWER SUPPLY AIRBUS 320 A320232 3930326 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 430UA 568 EMERGENCY EXIT LIGHT SYSTEM INOP FROM FORWARD MAIN DOOR TO ROW 6. REPLACED POWER SUPPLY. 2 L 7 2 4F RT A28NM 1996031500424 19960315 00424 NM 1996 3 15 96ZZZM269 1 19960131 A 2910 HYD LINE BOEING 757 75723N 1384973 NM NLG DOOR MISINSTALLED A AMTA O OTHER J W WARNING INDICATION INADEQUATE Q C CL CLIMB 1 GL 11 515AT 27598 IND- FLT 468 - GEAR DOOR LIGHT REMAINED ON FOR ABOUT ONE MINUTE AFTER GEAR RETRACTION. OPEN DOOR NOISE WAS AUDIBLE. NO EICAS MSG. AFTER ONE MINUTE LIGHT OUT AND NO GEAR NOISE. NLG DOOR LOCK RELEASE ACT HYD LINES INSTALLED BACKWARDS. RE POSITIONED LINES AND REPLACED ACT IAW 32-35-22. AIRCRAFT ADDED TO OPS SPEC 10/95, BOEING MANUFACTURE NOTIFIED OF POSSIB LE INSTALLATION ERROR AT FACTORY. 2 L 7 2 4F RT A2NM 1996031500425 19960315 00425 NM 1996 3 15 96ZZZM270 1 19960202 A 2421 976J4491 APU GENERATOR BOEING 737 73733A 1384673 NM NR 2 FAILED A AWXA O OTHER J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 28 173AW TZ4397M 23632 STL-LAS - FLT NR 940 - NR 2 BUS OFF LIGHT AT GATE WITH APU RUNNING AND BAD ELECTRICAL SMELL IN FLIGHT DECK. STANDBY POW ER OFF LIGHT ILLUMINATED ON GROUND. REMOVED AND REPLACED APU GENERATOR PER R6D49005. OPS CHECK GOOD. REFERENCE AWXA96 0041. 2 L 7 2 4F RT A16WE 1996031500426 19960315 00426 NE 1996 3 15 96ZZZM271 2 19960203 A 7200 ENGINE LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122* 54555 NE NR 1 VIBRATION A RIAA A J UNSCHED LANDING DUMP FUEL E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 19 305GB 193P1127 10523 ON RIA FLT 858, FROM ORD TO JSJ AT 2500 FEET AT CLIMB POWER NR 1 ENGINE VIBRATION INCREASED TO 4.0, ENGINE THRUST WAS RE DUCED, AVM ALSO DECREASED. AIRCRAFT DUMPED 17,000 LBS OF FUEL AND AIR RETURNED TO ORD WITH NR 1 ENGINE AT IDLE. AFTER LANDING ACCOMPLISHED TROUBLESHOOTING PER 71-91-00, INSPECTION INLET, EXHAUST, MCD'S AND MAIN OIL SCREEN FOUND OK. LUBED CLAPPERS AND ACCOMPLISHED AVM SURVEY PER 71-00-00, ENGINE RUNUP NORMAL MAX AVM 1.2 AT TAKEOFF, EPR 537. AIRCRAFT OK FO R SERVICE. 2 L 7 3 4F 4 F A23WE A12EU 1996031500427 19960315 00427 WP 1996 3 15 96ZZZM272 1 19960211 A 3260 UNSAFE LIGHT DOUG DC8 DC862 3021970 WP LT MLG DOOR ILLUMINATED A RIAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 19 8974U 46110 RIA FLT NR 7700 MIA - DOVER AIRCRAFT RETURNED TO MIA AFTER TAKEOFF WHEN MLG DOOR UNSAFE LIGHT ILLUMINATED. IN MIA, AIRC RAFT JACKED AND RIGGED LEFT DOOR ACTUATOR. OPS CHECK OK, AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 4 4F 4A25 1996031500428 19960315 00428 NM 1996 3 15 96ZZZM273 1 19960216 A 2820 BACK20G3 KNOB BOEING 727 727172C 1384058 NM NR 3 CROSSFEED OUT OF INDEX A RYNA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 07 527PC 19665 EN ROUTE FROM SEA TO MSP AIRCRAFT MADE UNSCHEDULED LANDING AT BIL. NR 3 FUEL TANK UNABLE TO CROSS-FEED FROM NR 1 OR NR 2 FUEL TANKS. FOUND NR 3 FUEL TANK CROSS-FEED SELECTOR SWITCH KNOB DEFECTIVE. KNOB WAS INDEXED 90 DEGREE OFF, WHEN SET TANK TO ENGINE X-FEED VALVE OPEN. WHEN SET TO X-FEED VALVE WAS CLOSED. REPLACED CROSSFEED SWITCH KNOB, VALVE OPERATES NORMALLY. OPS CHECKS GOOD PER MM 28-22-11. (M) 2 L 7 3 4F A3WE 1996031500429 19960315 00429 NM 1996 3 15 96ZZZM274 1 19960203 A 3260 001A321A3000000 UPLOCK DORNER DO32 DO328100 2996000 NM LT MLG ICED UP A EQGA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 19 340LS 3040 AFTER DEPARTING DFW, THE FLIGHT CREW SELECTED GEAR UP, NEITHER MAIN GEAR WOULD SHOW UP AND LOCKED. THE CREW THEN SELECT ED GEAR DOWN WITH NO PROBLEM. THEY THEN RETURNED TO DFW AND LANDED WITHOUT FURTHER INCIDENT. INSPECTION REVEALED THAT THE MAIN GEAR UPLOCK ROLLERS AND HOOKS HAD ICED OVER. DE-ICED THE GEAR SYSTEMS, NO FURTHER PROBLEMS NOTED. THIS IS A P OST SB-328-30-132 (SLUSH GUARDS) AIRCRAFT. (M) 2 H 7 2 4T RT A45NM 1996031500430 19960315 00430 NM 1996 3 15 96ZZZM275 1 19960203 A 3260 001A321A3000001 UPLOCK DORNER DO32 DO328100 2996000 NM RT MLG ICED UP A EQGA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 19 340LS 674 3040 AFTER DEPARTING DFW, THE FLIGHT CREW SELECTED GEAR UP, NEITHER MAIN GEAR WOULD SHOW UP AND LOCKED. THE CREW THEN SELECT ED GEAR DOWN WITH NO PROBLEM. THEY THEN RETURNED TO DFW AND LANDED WITHOUT FURTHER INCIDENT. INSPECTION REVEALED THAT THE MAIN GEAR UPLOCK ROLLERS AND HOOKS HAD ICED OVER. DE-ICED THE GEAR SYSTEMS, NO FURTHER PROBLEMS NOTED. THIS IS A P OST SB-328-30-132 (SLUSH GUARDS) AIRCRAFT. (M) 2 H 7 2 4T RT A45NM 1996031500431 19960315 00431 NM 1996 3 15 96ZZZM276 1 19960203 A 3260 001A321A3000000 UPLOCK DORNER DO32 DO328100 2996000 NM LT MLG ICED UP A EQGA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 19 328LS 270 3025 AFTER DEPARTING DFW, THE FLIGHT CREW SELECTED GEAR UP, NEITHER MAIN GEAR WOULD SHOW UP AND LOCKED. THE CREW THEN SELECT ED GEAR DOWN WITH NO PROBLEM. THEY THEN RETURNED TO DFW AND LANDED WITHOUT FURTHER INCIDENT. INSPECTION REVEALED THAT THE MAIN GEAR UPLOCK ROLLERS AND HOOKS HAD ICED OVER. DE-ICED THE GEAR SYSTEMS, NO FURTHER PROBLEMS NOTED. THIS IS A P OST SB-328-30-132 (SLUSH GUARDS) AIRCRAFT. (M) 2 H 7 2 4T RT A45NM 1996031500432 19960315 00432 NM 1996 3 15 96ZZZM277 1 19960203 A 3260 001A321A3000001 UPLOCK DORNER DO32 DO328100 2996000 NM RT MLG ICED UP A EQGA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 19 328LS 270 3025 AFTER DEPARTING DFW, THE FLIGHT CREW SELECTED GEAR UP, NEITHER MAIN GEAR WOULD SHOW UP AND LOCKED. THE CREW THEN SELECT ED GEAR DOWN WITH NO PROBLEM. THEY THEN RETURNED TO DFW AND LANDED WITHOUT FURTHER INCIDENT. INSPECTION REVEALED THAT THE MAIN GEAR UPLOCK ROLLERS AND HOOKS HAD ICED OVER. DE-ICED THE GEAR SYSTEMS, NO FURTHER PROBLEMS NOTED. THIS IS A P OST SB-328-30-132 (SLUSH GUARDS) AIRCRAFT. 2 H 7 2 4T RT A45NM 1996031500433 19960315 00433 SW 1996 3 15 96ZZZM278 1 19960208 A 3411 93B0100004D0300 PITOT LINE FRCHLD SA227 SA227DC 3377521 SW COCKPIT LOOSE A EQGA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 19 850LS 3506 DC850B SHORTLY AFTER TAKEOFF FROM DFW EN ROUTE TO HOT, THE FIRST OFFICERS PITOT SYSTEMS INSTRUMENTS FAILED. THE PILOT RETURNED TO DFW WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS THEN FERRIED TO HOT MAINTENANCE. UPON INSPECTION, THE PITOT LINE GO ING INTO THE FDR WAS FOUND TO BE LOOSE. THE LINE WAS RESECURED AND ALL TESTS COMPLETED CHECKED NORMAL. AIRCRAFT WAS RE TURNED TO SERVICE. 1 L 7 2 4T RT A18SW 1996031500434 19960315 00434 NM 1996 3 15 96ZZZM279 1 19960207 A 3260 870003 PSEU BOX ELDEC DORNER DO32 DO328100 2996000 NM E/E COMPT FAILED A EQGA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 19 340LS 698 55 3040 AFTER DEPARTING DFW EN ROUTE TO ASE, PROXIMITY SYSTEM FAIL LIGHT CAME ON ALONG WITH HYDRAULIC SYSTEM FAIL. PILOT RETURN ED TO DFW AND LANDED WITHOUT FURTHER INCIDENT. UPON INSPECTION, THE PSEU BOX WAS FOUND TO BE FAULTY. REPLACED THE PSEU BOX. ALL SYSTEMS CHECKED NORMAL. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. 2 H 7 2 4T RT A45NM 1996031500435 19960315 00435 NM 1996 3 15 96ZZZM280 1 19960107 A 5320 STRAPS BOEING 727 727259 138408J NM BS 1065-1075 CORRODED A UHVA K NONE O OTHER IN INSP/MAINT 1 SO 17 203AV 22474 FLOORBEAM STABILIZER STRAPS HAVE LEVEL 2 CORROSION STATION 1065-1075 RBL 24. REMOVED CARGO CEILING PANELS, INSTALLED SP LICE REPAIR AND REINSTALLED CARGO CEILING PANEL PER SRM 51-40-2 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1996031500436 19960315 00436 WP 1996 3 15 96ZZZM281 1 19960207 A 2750 5751152503 FLAP LINK DOUG DC8 DC861 3021952 WP WS 97 CRACKED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 27UA 44349 40510 45942 DURING MAINTENANCE CHECK, FOUND RIGHT WING INBOARD FLAP, OUTBOARD HINGE DRIVE LINK CRACKED AT STATION 97. REMOVED AND R EPLACED RIGHT WING INBOARD FLAP, OUTBOARD HINGE DRIVE LINK AND PERFORMED OPERATIONAL CHECK IAW MAINTENANCE MANUAL 27-51- 1. (M) 2 L 7 4 4F 4A25 1996031500437 19960315 00437 EU 1996 3 15 96ZZZM282 1 19960201 A 5610 7256100501 WINDSHIELD SAAB SF340 340B 7860101 EU LT COCKPIT CRACKED A NVEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 SO 03 323AE 340B323 FLT NR 4867 - YOW - DURNG CRUISE, THE CAPTAINS FORWARD WINDSHIELD HEAT FAILED. THE HEATING ELEMENT ARCED CAUSING THE OU TER PANE OF THE WINDOW TO CRACK ACROSS THE BOTTOM. THE INNER PANE CRACKED AT THE LEFT AND THE RIGHT EDGES OF THE WINDOW , ABOUT 2 INCHES IN ON BOTH SIDES. THE CAPTAINS VISION WAS IMPAIRED SO THE FIRST OFFICER FINISHED THE LEG. THE AIRCRAF T LANDED WITHOUT INCIDENT. REPLACED CAPTAINS FORWARD WINDSHIELD. (M) 2 L 7 2 4T RT A52EU 1996031500438 19960315 00438 WP 1996 3 15 96ZZZM283 1 19960204 A 2131 ED7244365 PRESS CTLR LKHEED 1011 10113851 5265010 WP CABIN FAILED A WRNA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 05 311EA 193A1012 AIRCRAFT DEPARTED BQN EN ROUTE TO GSO, CREW EXPERIENCED DIFFICULTY WITH CABIN PRESSURIZATION. C/B 3X14 PULLED AND RESET TO NO AVAIL. AIRCRAFT RETURNED TO BQN. LANDING NORMAL. AFT OUTFLOW VALVE OK IN ALL MODES, FORWARD VALVE INOP IN ALL MODES. T/S PER 21-50-00. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVIC E. (M) 2 L 7 3 4F A23WE 1996031500440 19960315 00440 NM 1996 3 15 96ZZZM285 1 19960107 A 5320 INTERCOSTAL BOEING 727 727259 138408J NM BS 1030 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 203AV 22474 AFT CABIN 1130 RBL 48-65 LEVEL 2 EXFOLIATING CORROSION ON TOP OF INTERCOSTAL. REMOVED OLD ANGLE AT STATION 1030 RBL 48- 65 FABRICATED NEW ONE, TREATED, PRIMED AND INSTALLED PER SRM 51-40. (M) 2 L 7 3 4F A3WE 1996031500441 19960315 00441 NM 1996 3 15 96ZZZM286 1 19960105 A 5315 FLOOR BEAM BOEING 727 727259 138408J NM BS 1110 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 203AV 22474 STATION 1110 FLOOR BEAM UPPER SURFACE HAS LEVEL 2 CORROSION AT RBL 10 TO RBL 65. REMOVED CORROSION CAT OUT OF LIMITS SE CTION. FABRICATED FLOOR BEAM AND SPLICE ANGLES PER SRM 51-40-3 FIG 1 ALODINE, PRIME AND INSTALLED PER SRM 51-40-3. (M) 2 L 7 3 4F A3WE 1996031500442 19960315 00442 NM 1996 3 15 96ZZZM287 1 19960106 A 5347 SEAT TRACK BOEING 727 727259 138408J NM BS 1060-1140 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 203AV 22474 SEAT TRACK RL 25 STATION 1060 TO 1140 HAS LEVEL 2 CORROSION ALONG TOP AND FLANGE OF TRACK. REMOVED DAMAGED SEAT TRACK A ND FABRICATED A NEW SEAT TRACK RE-INSTALLED COMP AT STATION 1060 TO 1140 RBL 25 PER SRM 51-10-1, SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1996031500443 19960315 00443 NM 1996 3 15 96ZZZM288 1 19960106 A 5347 SEAT TRACK BOEING 727 727259 138408J NM BS 340-480 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 203AV 22474 SEAT TRACK RL STATION 1060 TO 1140 HAS LEVEL 2 CORROSION ALONG TOP OF FLANGE AND TRACK. REMOVED AND FABRICATED NEW SEAT TRACK AND INSTALLED PER SRM 51-10-4, 53-10-5 AND 51-30-02. (M) 2 L 7 3 4F A3WE 1996031500444 19960315 00444 NM 1996 3 15 96ZZZM289 1 19960107 A 5315 FLOOR BEAM BOEING 727 727259 138408J NM BS 460-480 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 203AV 22474 STATION 460 FLOOR BEAM UPPER SURFACE HAS LEVEL 2 CORROSION FROM RBL 10 TO 60. COMPLETED INSTALLATION OF FABRICATED FLOO R BEAM REPAIR IAW SRM 53-10-8. (M) 2 L 7 3 4F A3WE 1996031500445 19960315 00445 NM 1996 3 15 96ZZZM290 1 19960105 A 5347 SEAT TRACK BOEING 727 727259 138408J NM BS 340-380 CORROSION B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 203AV 22474 SEAT TRACK RBL 54 FROM STATION 340 TO 380 HAS LEVEL 2 CORROSION ON SCALLOP AREA. REMOVED AND REPLACED SEAT TRACK PER SR M 51-10-1 AND 51-30-2 FROM STATION 340 TO 380 53-10-1. (M) 2 L 7 3 4F A3WE 1996031500446 19960315 00446 NM 1996 3 15 96ZZZM291 1 19960107 A 5320 ANGLE BOEING 727 727259 138408J NM BS 1110-1130 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 203AV 22474 AFT CABIN FLOOR STATION 1110-1130 INTERCOSTAL AT BL 0 HAS LEVEL 2 CORROSION AROUND FASTENER HOLES AND CRACK IN RADIUS. F ABRICATED ANGLE, TREATED AND INSTALLED PER SRM 51-10-1, 51-10-02 AND 51-20-1. (M) 2 L 7 3 4F A3WE 1996031500447 19960315 00447 NM 1996 3 15 96ZZZM292 1 19960108 A 5320 WEB BOEING 727 727259 138408J NM BS 1136-1160 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 203AV 22474 AFT CABIN GALLEY AREA LEVEL 2 CORROSION ON HAT SECTION AND FLOOR WEB AT STATION 1136-1160 RBL 16-22. REPAIRED FLOOR WEB PER SRM 51-30-02 AND REINSTALLED PER SRM 51-10-02 AND SRM 51-40-02. (M) 2 L 7 3 4F A3WE 1996031500448 19960315 00448 NM 1996 3 15 96ZZZM293 1 19960109 A 5347 SEAT TRACK BOEING 727 727259 138408J NM BS 1060-1140 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 203AV 22474 SEAT TRACK RBL 54 STATION 1060 TO 1140 HAS LEVEL 2 CORROSION AT NUMEROUS AREAS ALONG TOP AND FLANGE OF TRACK. REMOVED O LD SEAT TRACK, FABRICATED AND INSTALLED NEW SEAT TRACK PER SRM 53-10-5, 51-10-1 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1996031500449 19960315 00449 NM 1996 3 15 96ZZZM294 1 19960105 A 5347 SEAT TRACK BOEING 727 727259 138408J NM BS 420-460 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 203AV 22474 SEAT TRACK RBL 54 STATION 420-460 HAS ONE AREA OF LEVEL 2 CORROSION INSIDE AND ALONG OUTSIDE OF SEAT TRACK. REPLACED AN D INSTALLED SEAT TRACK PER SRM 51-10-5 AND 51-10-2. (M) 2 L 7 3 4F A3WE 1996031500450 19960315 00450 NM 1996 3 15 96ZZZM295 1 19960106 A 5320 65649502 SUPPORTS BOEING 727 727259 138408J NM BS 420 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 203AV 22474 STATION 420 RBL 10 INCHES TO 60 INCHES OF LEVEL 2 CORROSION ON UPPER SURFACE OF FLOOR SUPPORT. ALSO, SMALL SECTION OF R 1 GALLEY DOOR FLOOR STRUCTURE AT STA 420 HAS LEVEL 2. REMOVED AND REPLACED FLOOR SUPPORTS PER SRM 53-10-2, 51-10-2, 51- 30-2. (M) 2 L 7 3 4F A3WE 1996031500451 19960315 00451 NM 1996 3 15 96ZZZM296 1 19960106 A 5347 TRACK BOEING 727 727259 138408J NM BS 1020-1140 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 203AV 22474 SEAT TRACK RBL 42 STATION 1020 TO 1140 HAS LEVEL 2 CORROSION ALONG TOP AND FLANGE OF SEAT TRACK. REMOVED AND REPLACED S EAT TRACKS FROM STATION 1030 TO 1140 RBL 42 PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1996031500452 19960315 00452 NM 1996 3 15 96ZZZM297 1 19960107 A 5320 SUPPORT BOEING 727 727259 138408J NM BS 312 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 203AV 22474 LEVEL 2 EXFOLIATING CORROSION OF FLOOR SUPPORT AT STATION 312 CBL TO LBL 20 INCHES. CUT OUT DAMAGED AREA ON AFT SIDE OF 'T', FABRICATED AND INSTALLED REPAIR ANGLES, STRAPS AND FILLERS IAW SRM 51-40-4 FIG 1. (M) 2 L 7 3 4F A3WE 1996031500453 19960315 00453 NM 1996 3 15 96ZZZM298 1 19960109 A 5320 SUPPORT BOEING 727 727259 138408J NM BS 1010-1030 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 203AV 22474 FLOOR SUPPORTS AT STATION 1010-1030, RBL 10 HAS LEVEL 2 CORROSION. REMOVED AND INSTALLED NEW SUPPORT PER SRM 51-10-1, 5 1-20-2, AND 51-30-2. (M) 2 L 7 3 4F A3WE 1996031500454 19960315 00454 NM 1996 3 15 96ZZZM299 1 19960109 A 5320 SUPPORT BOEING 727 727259 138408J NM BS 990-998 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 203AV 22474 FLOOR SUPPORTS AT 998 RBL 24 AND STATION 990-998 RBL 10 HAVE LEVEL 2 CORROSION. FABRICATED AND INSTALLED FLOOR SUPPORT PER SRM 51-10-1, 53-10-8, 51-10-6. (M) 2 L 7 3 4F A3WE 1996031500455 19960315 00455 NM 1996 3 15 96ZZZM300 1 19960107 A 5321 FLOOR BOEING 727 72723 1384004 NM BS 1138-1148 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 1993 18449 LEVEL 2 EXFOLIATING CORROSION UNDER STAINLESS STEEL PLATE AT STA 1130-1148, RBL 26 AT RIGHT AFT LAV. FABRICATED DOUBLER AND FILLER, LOCATED AND DRILLED AND INSTALLED COMPLETE PER SRM 51-10-6, 51-40-2 AND TREATED. (M) 2 L 7 3 4F A3WE 1996031500456 19960315 00456 NM 1996 3 15 96ZZZM301 1 19960105 A 5320 FLOOR STABILIZER BOEING 727 72723 1384004 NM BS 600-640 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 1993 18449 LEVEL 2 EXFOLIATING CORROSION, STATION 600-640 RBL 12, UPPER AND LOWER SURFACES OF FLOOR STABILIZER GROUND NUTPLATE HOLE S. REMOVED CORROSION, TREATED, PRIMED PER SRM 51-10-6 AND 51-10-2. (M) 2 L 7 3 4F A3WE 1996031500457 19960315 00457 NM 1996 3 15 96ZZZM302 1 19960105 A 5315 FLOOR BEAM BOEING 727 72723 1384004 NM BS 640 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 1993 18449 LEVEL 2 EXFOLIATING CORROSION, STATION 640 RBL 12-64, UPPER SURFACE, FORWARD HORIZONTAL. FLANGE OF FLOOR BEAM, AROUND C LIP NUT HOLES. REMOVED CORROSION TREATED, PRIMED PER SRM 51-10-6, 51-10-2. (M) 2 L 7 3 4F A3WE 1996031500459 19960315 00459 NM 1996 3 15 96ZZZM304 1 19960102 A 5321 FLOOR BOEING 727 72723 1384004 NM STA 600-640 CORROSION B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 1993 18449 LEVEL 2 EXFOLIATING CORROSION, STATION 600-640 RBL 64, UPPER HORIZONTAL SURFACE, OUTBOARD FLOOR STABILIZER. REMOVED COR ROSION AND TREATED AND PRIMED PER SRM 51-10-6, 51-10-2. (M) 2 L 7 3 4F A3WE 1996031500460 19960315 00460 NE 1996 3 15 96ZZZM305 2 19960116 A 7250 TURBINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D217C 52053 NE NR 2 ENGINE FAILED A TWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 05 931TW 49527 STL - DURING TAKEOFF, NR 2 ENGINE SUFFERED A TURBINE FAILURE. REMOVED AND REPLACED NR 2 ENGINE. OPERATIONAL AND TRIM C HECKS NORMAL. 2 L 7 2 4F 4 F RT A6WE E9NE 1996031500461 19960315 00461 NE 1996 3 15 96ZZZM306 2 19960111 A 7230 COMPRESSOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE LT ENGINE STALLED A TWAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 CE 05 907TW 49165 SAN - DURING CLIMB SHUT DOWN LEFT ENGINE DUE TO COMPRESSOR STALL. FOUND METAL PARTICLES IN TAILPIPE. REPLACED ENGINE A ND ENGINE OPERATION CHECKED NORMAL. 2 L 7 2 4F 4 F A6WE E9NE 1996031500462 19960315 00462 NE 1996 3 15 96ZZZM307 2 19960111 A 7230 TURBINE BLADE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE LT ENGINE FAILED A TWAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 CE 05 958U 49703 3258 STL - DURING CLIMB SHUT DOWN LEFT ENGINE DUE TO COMPRESSOR STALL. FOUND METAL PARTICLES IN TAILPIPE. REPLACED ENGINE A ND ENGINE OPERATION CHECKED NORMAL. INVESTIGATION OF ENGINE, S/N 3258, COMPRESSOR STALL REVEALED THE AIRFOIL OF ONE TUR BINE BLADE FAILED DUE TO A FATIGUE CRACK CAUSING THE COMPRESSOR STALL, WHICH LEAD TO THE ENGINE SHUT DOWN. THE ENGINE W AS REPAIRED AND RETURNED TO SERVICE. 2 L 7 2 4F 4 F A6WE E9NE 1996031500463 19960315 00463 WP 1996 3 15 AALA960139 1 19960126 A 3350 CONDUCTOR DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7550 53032 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FIRST CLASS CABIN INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT F LAT CONDUCTOR IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996031500464 19960315 00464 WP 1996 3 15 AALA960141 1 19960127 A 3350 STRIP DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 485AA 49678 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT AFT SECTION OF MAIN CABIN INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP AT AFT SECTION OF MAIN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996031500465 19960315 00465 WP 1996 3 15 AALA960173 1 19960131 A 5320 SHEAR TIE DOUG DC9 DC982 3022082 WP BS 1307 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 275AA 49272 TUL - FOUND SHEAR TIE CRACKED IN 2 PLACES AT STATION 1307 BULKHEAD BETWEEN LONGERONS 14 AND 15 LEFT. (M) 2 L 7 2 4F A6WE 1996031500466 19960315 00466 NM 1996 3 15 AALA960208 1 19960206 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 560 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 863AA 21090 TULE - FOUND CORROSION ON STRINGER 27R, AFT OF STATION 560. CUT OUT CORRODED AREA, INSTALLED REPAIR PER SRM 53-10-3, FI G 1. (M) 2 L 7 3 4F A3WE 1996031500467 19960315 00467 WP 1996 3 15 AALA960216 1 19960206 A 5311 27779305 FRAME DOUG DC9 DC982 3022082 WP BS 1322 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 275AA 49272 FOUND HEAVY CORROSION ON FRAME 1322. CUT OUT CORRODED AREA AND REPAIRED PER SRM CHAP 53-03 FIG 2A SHEET 1. (M) 2 L 7 2 4F A6WE 1996031500468 19960315 00468 WP 1996 3 15 AALA960217 1 19960206 A 5321 FLOOR WEB DOUG DC9 DC982 3022082 WP BS 162-198 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 275AA 49272 TUL - FLOOR WEB CORRODED, INBOARD OF FORWARD SERVICE DOOR. SPLICED IN NEW SECTION OF WEB. (M) 2 L 7 2 4F A6WE 1996031500469 19960315 00469 WP 1996 3 15 AALA960218 1 19960206 A 5321 FLOOR WEB DOUG DC9 DC982 3022082 WP BS 196-200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 246AA 49238 TULE - FOUND FLOOR WEB CORRODED UNDER THRESHOLD STRIP AT AFT END OF FORWARD GALLEY DOOR OPENING. INSTALLED CUSP DOUBLER AS PER SRM 53-01 FIG 2. (M) 2 L 7 2 4F A6WE 1996031500470 19960315 00470 WP 1996 3 15 AALA960219 1 19960207 A 5320 GUSSET DOUG DC9 DC982 3022082 WP BS 1211 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 275AA 49272 TUL - GUSSET HAS CORROSION. REMOVED OLD PART, INSTALLED NEW SERVICEABLE PART. (M) 2 L 7 2 4F A6WE 1996031500471 19960315 00471 WP 1996 3 15 AALA960245 1 19960209 A 2120 116961 DUCT DOUG DC9 DC982 3022082 WP BS 351 FAILED A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 292AA 49304 TULE - DURING CARGO HEAT CHECK SMELLED SMOKE IN FORWARD CARGO, FOUND HEATER DUCT BURNED. REPLACED CARGO HEATER DUCT (FO RWARD CARGO) AND RELAYS R2-211 CARGO HEATER RELAY AND R2-212 GROUND SENSE RELAY. OPENED UP FORWARD CARGO SIDEWALL PANEL S AND CEILING PANELS LOOKED FOR EVIDENCE OF BURNED WIRES, NONE FOUND. OPERATION CHECKS GOOD. (M) 2 L 7 2 4F A6WE 1996031500472 19960315 00472 WP 1996 3 15 AALA960246 1 19960209 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1287 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 275AA 49272 TULE - FOUND FRAME CORRODED. INSTALLED DOUBLER PER ESO 80559 REPAIR NR 1 DATED 2/9/96. (M) 2 L 7 2 4F A6WE 1996031500473 19960315 00473 WP 1996 3 15 AALA960247 1 19960209 A 5320 SHEAR TIE DOUG DC9 DC982 3022082 WP BS 1287 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 275AA 49272 TULE - FOUND SHEAR TIE CORRODED. REMOVED AND REPLACED SHEAR TIE PER SRM 53-03 FIG 5. (M) 2 L 7 2 4F A6WE 1996031500474 19960315 00474 WP 1996 3 15 AALA960248 1 19960209 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP BS 693-712 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 275AA 49272 TULE - FOUND INTERCOSTAL CORRODED. REPLACED INTERCOSTAL. (M) 2 L 7 2 4F A6WE 1996031500475 19960315 00475 WP 1996 3 15 AALA960255 1 19960210 A 5320 CUSP DOUG DC9 DC982 3022082 WP BS 200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 275AA 49272 TULE - CORROSION ON CUSP, UNDER MOST FORWARD END OF SEAT TRACK NR 5, STATION 200-220. REMOVED CORROSION AND INSTALLED D OUBLER PER SRM 53-01 FIG 2 SH 2. (M) 2 L 7 2 4F A6WE 1996031500476 19960315 00476 WP 1996 3 15 AALA960256 1 19960210 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 275AA 49272 TULE - FOUND HEAVY CORROSION, NR 5 SEAT TRACK STATION 200. REPLACED SEAT TRACK SECTION STATION 200. (M) 2 L 7 2 4F A6WE 1996031500477 19960315 00477 WP 1996 3 15 AALA960258 1 19960206 A 5311 27779305 FRAME DOUG DC9 DC982 3022082 WP BS 1287 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 275AA 49272 TULE - FRAME 1287 HAS CORROSION FROM L29L TO L29R. INSTALLED DOUBLER PER ESO 80559 REPAIR 13 DATE 2-9-96. (M) 2 L 7 2 4F A6WE 1996031500478 19960315 00478 WP 1996 3 15 AALA960259 1 19960206 A 5320 SHEAR TIE DOUG DC9 DC982 3022082 WP BS 1287 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 275AA 49272 TULE - SHEAR TIE AT STATION 1287 HAS CORROSION FROM L29R TO L30. REMOVED AND REPLACED SHEAR TIE PER SRM 53-03 FIG 3. ( M) 2 L 7 2 4F A6WE 1996031500479 19960315 00479 WP 1996 3 15 AALA960260 1 19960213 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 1287-1309 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 275AA 49272 TUL - FOUND CORROSION ON LONGERON. SPLICE LONGERON PER SRM 53-02 FIG 1 AND PER ESO 80559 DATED 2-12-96. (M) 2 L 7 2 4F A6WE 1996031500480 19960315 00480 NM 1996 3 15 AWXA960041 1 19960202 A 2450 915F2133 BUS PROTECT PNL BOEING 737 73733A 1384673 NM FLT DECK FAILED A AWXA O OTHER J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 28 173AW SI1898 23632 STL-LAS - FLT NR 940 - NR 2 BUS OFF LIGHT AT GATE WITH APU RUNNING AND BAD ELECTRICAL SMELL IN FLIGHT DECK. STANDBY POW ER OFF LIGHT ILLUMINATED ON GROUND. REMOVED AND REPLACED BUS PROTECTION PANEL. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996031500481 19960315 00481 1996 3 15 AWXA960042 4 19960203 A 3454 6223257001 VHF NAV RECEIVER BOEING 737 7372E3 NM NR 1 FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 138AW 3689 22792 PHX-SFO - FLT NR 607 - AIR TURN BACK, NR 1 VHF NAVIGATION FAILING ON CLIMB-OUT. FLAG IN VIEW ON RMI AND CDI. REMOVED A ND REPLACED NR 1 VHF NAVIGATION RECEIVER. OPS TESTED GOOD WITH TIC TESTER. (M) 2 L 7 2 4F RT A16WE 1996031500482 19960315 00482 NM 1996 3 15 AWXA960053 1 19960206 A 3350 20121 BATTERY PACK BOEING 737 73733A 1384673 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 175AW 23634 PHX - FLT NR 1406 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT INOP OVER L-1 DOOR. REPLACED DOOR BATTERY P ACK. (M) 2 L 7 2 4F RT A16WE 1996031500483 19960315 00483 EU 1996 3 15 AWXA960055 1 19960207 A 5347 DS311278220001 SEAT TRACK AIRBUS 320 A320231 3930325 EU BS 1202 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 636AW 098 FLT NR 3841 - PAE - DURING SCHEDULED C-4, S-1 MAINTENANCE CHECK, FOUND CORROSION ON SEAT RAIL, SIA 7081 TO 8377, Y-1202, Z-240. REPLACED SEAT RAIL PER SRM 57-40-11. (M) 2 L 7 2 4F RT A28NM 1996031500484 19960315 00484 NE 1996 3 15 AWXA960058 2 19960208 A 7321 79830015046 EEC AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE NR 1 ENGINE FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 637AW 25000140 099 PHX/SAN - FLT NR 860 - AIR TURN BACK, ENGINE 1 SENSOR FAULT, ECAM MESSAGE ENGINE SURGED AFTER TAKEOFF AND THEN STABILIZE D. REMOVED AND REPLACED NR 1 ENGINE EEC PER CARD R9E73301. (M) 2 L 7 2 4F 4 F RT A28NM E311NE 1996031500485 19960315 00485 SW 1996 3 15 BDHA0005 1 19960124 A 7722 8974696 EGT LEAD SWRNGN SA226 SA226TC 8780404 SW RIGHT OPEN A BDHA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 15 328BA TC253 MSP - FLT NR 421 - THE CREW REPORTED THE RIGHT EGT WAS ERRATIC ON TAXI AND RETURNED. THE LEAD WAS REPLACED FROM THE COM P TO THE RAKE AND ENGINE RUN PERFORMED. ALL INDICATIONS WERE NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 1 L 7 2 4T A8SW 1996031500486 19960315 00486 SW 1996 3 15 BDHA960002 1 19960103 A 2910 2781006681 HYD LINE SWRNGN SA226 SA226TC 8780404 SW COCKPIT CRACKED A BDHA O OTHER J K WARNING INDICATION FLUID LOSS TX TAXI/GRND HDL 1 GL 15 229AM TC305 PIR - FLT 421 - WHILE TAXIING, THE PILOT NOTICED FLUCTUATIONS OF THE HYDRAULIC PRESSURE INDICATOR. MAINTENANCE INSPECTI ON REVEALED A BROKEN LINE UNDER THE PILOTS SEAT GOING TO THE HAND PUMP PRESSURE RELEIF VALVE. THE LINE WAS REPAIRED, LE AK CHECKED AND THE AIRCRAFT RETURNED TO SERVICE. (M) 1 L 7 2 4T A8SW 1996031500487 19960315 00487 SW 1996 3 15 BDHA96003 1 19960118 A 3260 MS250261 GEAR SWITCH SWRNGN SA226 SA226TC 8780404 SW MLG FROZE A BDHA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 328BA TC253 MSP - FLT 475 - AFTER TAKEOFF, THE LEFT AND RIGHT MLG DOWN LIGHTS STAYED ON WITH THE GEAR RETRACTED. THE AIRCRAFT RETUR NED AND GEAR RETRACTION PERFORMED. ALL GEAR SWITCHES WERE CLEANED AND OPERATION WAS NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 1 L 7 2 4T A8SW 1996031500488 19960315 00488 SO 1996 3 15 C2XA96IA045 1 19960214 A 3231 NAS5135 WASHER EMB 120 EMB120RT SO LT MLG DOOR BROKEN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 57734 120199 SHV - FLT 2519 - DURING A PREFLIGHT INSPECTION, THE PILOT NOTICED THAT THE LEFT MAIN GEAR AFT OUTBOARD DOOR HAD COME LOO SE AT THE ACTUATING ROD. THE GEAR DOOR WAS REMOVED AND THE AIRCRAFT WAS FERRIED TO IAH, WHERE MAINTENANCE REMOVED AND R EPLACED A BROKEN SAFETY TANG WASHER ON THE ACTUATING ROD. THE MAIN GEAR AFT DOOR WAS REINSTALLED AND THE AIRCRAFT WAS R ETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996031500489 19960315 00489 EU 1996 3 15 C2XA96IA046 1 19960217 A 3350 44 LAMP 3011210 AEROSP ATR42 ATR42320 8680930 EU CABIN FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14829 181 IAH - DURING ROUTINE CHECK OF EMERGENCY LIGHTING SYSTEM, PASSENGER DOOR GROUND ILLUMINATION LIGHT FAILED TO OPERATE. RE MOVED AND REPLACED LIGHT BULB, OPERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1996031500490 19960315 00490 EU 1996 3 15 C2XA96IA047 1 19960217 A 3350 3011210 LIGHT AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14829 181 IAH - DURING ROUTINE CHECK OF EMERGENCY LIGHTING SYSTEM, AFT RIGHT GROUND ILLUMINATION LIGHT FAILED TO OPERATE. REMOVED AND REPLACED EXTERNAL EMERGENCY LIGHT ASSEMBLY, OPERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1996031500491 19960315 00491 EU 1996 3 15 C2XA96IA048 1 19960217 A 3350 44 LAMP 3011210 AEROSP ATR42 ATR42320 8680930 EU CABIN FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14829 181 IAH - DURING ROUTINE CHECK OF EMERGENCY LIGHTING SYSTEM, FORWARD RIGHT GROUND ILLUMINATION LIGHT FAILED TO OPERATE. REM OVED AND REPLACED LIGHT BULB, OPERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1996031500492 19960315 00492 EU 1996 3 15 C2XA96IA049 1 19960218 A 3350 0341516 FUSE AEROSP ATR42 ATR42300 8680920 EU CABIN BLOWN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16824 166 IAH - DURING ROUTINE CHECK OF EMERGENCY LIGHTING SYSTEM, PASSENGER DOOR GROUND ILLUMINATION LIGHT FAILED TO OPERATE. IN SPECTED AND FOUND BROKEN WIRE AT LIGHT ASSY PIN CONNECTOR, ALSO FOUND BLOWN FUSE AT LIGHT POWER SUPPLY. REPAIRED WIRE A ND REPLACED FUSE, OPERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1996031500493 19960315 00493 EU 1996 3 15 C2XA96IA050 1 19960216 A 5320 S53971402204 ANGLE AEROSP ATR42 ATR42300 8680920 EU FRAME CRACKED A C2XA O OTHER O OTHER IN INSP/MAINT 1 SW 09 16824 166 IAH - DURING C-CHECK INSPECTION, FOUND BELLY FAIRING SUPPORT ANGLE CRACKED JUST FORWARD OF HYDRAULIC TANK FRAME 27. MAI NTENANCE STOP DRILLED CRACK AND INSTALLED DOUBLER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996031500494 19960315 00494 EU 1996 3 15 C2XA96IA051 1 19960216 A 5312 S53572601206 BULKHEAD AEROSP ATR42 ATR42300 8680920 EU FRAME 25 CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16824 166 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT REAR SPAR BULKHEAD CRACKED AT STRINGER 10 FRAME 25 TOP AFT HI-LOK COLLER SI DE. MAINTENANCE REMOVED HI-LOK, DRILLED HOLE TO NEXT OVER SIZE. PERFORMED EDDY CURRENT AND FOUND NO CRACK INDICATION A ND REINSTALLED HI-LOK. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996031500495 19960315 00495 EU 1996 3 15 C2XA96IA052 1 19960216 A 5320 S53970901226 ANGLE AEROSP ATR42 ATR42300 8680920 EU FRAME 24 LT CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16824 166 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING TO FUSELAGE FAIRING FRAME 24 THIRD ATTACH ANGLE FROM OUTBOARD CRACKED. MAINTENANCE REMOVED AND REPLACED ATTACH ANGLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996031500496 19960315 00496 EU 1996 3 15 C2XA96IA053 1 19960216 A 5320 S53970901300 ANGLE AEROSP ATR42 ATR42300 8680920 EU FRAME CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16824 166 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING TO FUSELAGE FAIRING FRAME 24 HAS TWO CRACKS AROUND LOWER TWO RIVETS ON LOWER ATTACH ANGLE. MAINTENANCE REMOVED AND REPLACED ATTACH ANGLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE . (M) 2 H 7 2 4T RT A53EU 1996031500497 19960315 00497 EU 1996 3 15 C2XA96IA054 1 19960216 A 5320 S53970901226 ANGLE AEROSP ATR42 ATR42300 8680920 EU FRAME 24 CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16824 166 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING TO FUSELAGE FAIRING FRAME 24 HAS CRACKED LOWER ATTACH ANGLE. MAINTENAN CE REMOVED AND REPLACED ATTACH ANGLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996031500498 19960315 00498 EU 1996 3 15 C2XA96IA055 1 19960216 A 5320 S53970901300 ANGLE AEROSP ATR42 ATR42300 8680920 EU FRAME 24 CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16824 166 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING TO FUSELAGE FAIRING FRAME 24 THIRD ATTACH ANGLE FROM OUTBOARD CRACKED. MAINTENANCE REMOVED AND REPLACED ATTACH ANGLE, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996031500499 19960315 00499 EU 1996 3 15 C2XA96IA057 1 19960218 A 6130 FE1595006 PROPELLER BRAKE AEROSP ATR42 ATR42320 8680930 EU NR 2 ENG BURNED A C2XA C D F ABORTED TAKEOFF RETURN TO BLOCK ACTIVATE FIRE EXT. B P SMOKE/FUMES/ODORS/SPARKS NO WARNING INDICATION TX TAXI/GRND HDL 1 SW 09 14828 5795 3640 179 IAH - FLT NR 2661 - AFTER AN ABORTED TAKEOFF DUE TO ERRATIC AIRSPEED INDICATION, THE CO-PILOT NOTICED SMOKE EMITTING FRO M THE RIGHT NACELLE ON TAXI BACK TO THE GATE. NO FIRE WARNING WAS INDICATED, BUT THE CREW ELECTED TO BLOW THE NR 2 ENGI NE FIRE BOTTLE AS A PRECAUTIONARY MEASURE. MAINTENANCE INSPECTED THE NR 2 ENGINE AND FOUND THE PROPELLER BRAKE TO BE BU RNED. MAINTENANCE REMOVED THE PROP BRAKE AND PLACED THE SYSTEM UNDER MEL 61-50-1C, AND THE AIRCRAFT WAS APPROVED FOR RE TURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996031500501 19960315 00501 NM 1996 3 15 CAL960014 1 19960110 A 3350 1001141 LIGHT BOEING 727 727232 1384082 NM AFT AIRSTAIR INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 45793 20647 FLT NR 700 - EWR - INSPECTION FOUND THE EMERGENCY EXIT OVERHEAD LIGHTS IN AFT AIRSTAIR INOPERATIVE. THE LIGHT ASSEMBLY WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. (M) 2 L 7 3 4F A3WE 1996031500502 19960315 00502 WP 1996 3 15 CAL960073 1 19960201 A 3350 EMBS1392 CHARGER DOUG DC10 DC1030 3023501 WP CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15069 69788 46584 FLT NR 51 - EWR - THE EMERGENCY LIGHTS WOULD NOT TEST DURING A PREFLIGHT CHECK. MAINTENANCE FOUND A FAULTY POWER SUPPLY AT MID CABIN. THE EMERGENCY LIGHT CHARGER AND BATTERY WERE REMOVED AND REPLACED AND OPERATION CHECKED GOOD. (M) 2 L 7 3 4F A22WE 1996031500503 19960315 00503 NE 1996 3 15 CAL960074 2 19960202 A 7250 TURB BLADE BOEING 727 727224 1384076 NM PWA JT8 JT8D9 52048 NE NR 2 ENGINE BROKEN A CALA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 SW 09 93738 62175 10640 20666 665995 EWR - FLT 2000 - THE NR 2 ENGINE GAVE OFF A LOUD BANG ON CLIMB-OUT OF EWR. ENGINE POWER WAS REDUCED AND THE AIRCRAFT WA S RETURNED TO EWR. MAINTENANCE FOUND METAL IN THE NR 2 ENGINE TAILPIPE. THE NR 2 ENGINE WAS REMOVED AND REPLACED. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION. SUPPLEMENT - THE ENGINE FAILED DUE TO A BROKEN FIRST STAGE TURBINE BLADE. THE BLADE BROKE NEAR THE ROOT AND INVESTIGATION INDICATED THE FAILURE INITIATED AT THE TRAILING ED GE. (X) 2 L 7 3 4F 4 F A3WE E2EA 1996031500504 19960315 00504 NM 1996 3 15 CAL960078 1 19960204 A 2170 COALSCER BAG BOEING 727 727243 138408D NM RT A/C PACK DIRTY A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 09 17410 21663 FLT NR 566 - EWR - THE RIGHT AIR CONDITIONING PACK BEGAN TO PRODUCE SMOKE IN THE CABIN WHILE ON DESCENT INTO EWR. THE C OOLING DOOR WAS OPENED TO BRING TEMPERATURE DOWN AND THE SMOKE STOPPED. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. T HE RIGHT PACK WATER SEPARATOR BAG WAS REMOVED AND REPLACED. THE ENGINES WERE RUN AT VARIOUS POWER SETTINGS WITH THE PAC KS OPERATING AND NO SMOKE WAS OBSERVED. (M) 2 L 7 3 4F RT A3WE 1996031500505 19960315 00505 NM 1996 3 15 CAL960092 1 19960202 A 3350 BATTERY PACK BOEING 737 7373T0 1384582 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14320 23371 GSO - THE R-2 DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE R-2 DOOR EMERGENCY LIGHT BATTERY PACK WAS REMOVED AND REP LACED IAW MM 33-51-51 AND OPERATION OF THE EMERGENCY LIGHT WAS RESTORED. (M) 2 L 7 2 4F RT A16WE 1996031500506 19960315 00506 WP 1996 3 15 CAL960093 1 19960115 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 1165 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16808 36783 49262 MIA - INSPECTION FOUND FLOOR BOARD SUPPORT HAT CHANNEL CORRODED IN MAIN CABIN AT STATION 1165. A NEW FLOOR BOARD SUPPOR T HAT CHANNEL WAS FABRICATED AND INSTALLED IAW SRM 51-30-1. (M) 2 L 7 2 4F A6WE 1996031500507 19960315 00507 WP 1996 3 15 CAL960094 1 19960119 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 570-695 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16808 36783 49262 MIA - INSPECTION FOUND CORROSION ON FLOOR SUPPORT TRACK IN CENTER CARGO COMPARTMENT BETWEEN BS 570-695, LBL 20. THE COR RODED AREA WAS CUT OUT AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-1-0. (M) 2 L 7 2 4F A6WE 1996031500508 19960315 00508 WP 1996 3 15 CAL960095 1 19960114 A 5753 VANE DOUG DC9 DC982 3022082 WP RT TE FLAP GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16808 36783 49262 MIA - INSPECTION FOUND TOP INBOARD END OF RIGHT WING 5TH FOREFLAP VANE HAD GOUGES. THE DAMAGED AREA WAS CUT OUT AND A H OT BOND REPAIR WAS INSTALLED IAW SRM 51-1-9A. (M) 2 L 7 2 4F A6WE 1996031500509 19960315 00509 WP 1996 3 15 CAL960096 1 19960113 A 5753 VANE DOUG DC9 DC982 3022082 WP LT TE FLAP DINGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16808 36783 49262 MIA - INSPECTION FOUND LOWER SURFACE OF INBOARD LEFT FLAP VANE DINGED AND ERODED DUE TO IMPACT DAMAGE CAUSED BY TIRE DEB RIS. A HOT BOND REPAIR WAS PERFORMED IAW SRM 51-1-9A. (M) 2 L 7 2 4F A6WE 1996031500510 19960315 00510 WP 1996 3 15 CAL960097 1 19960113 A 5730 SKIN DOUG DC9 DC982 3022082 WP LT WING TE DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16808 36783 49262 MIA - INSPECTION FOUND LEFT WING LOWER TRAILING EDGE SKIN PANEL DELAMINATED AROUND MOUNT SCREWS FOR INBOARD AND OUTBOARD ANTI-SKID VALVES. THE PANEL WAS REPAIRED WITH FIBERGLASS OVERLAY IAW SRM 51-70-1. (M) 2 L 7 2 4F A6WE 1996031500511 19960315 00511 WP 1996 3 15 CAL960098 1 19960121 A 5730 SKIN DOUG DC9 DC982 3022082 WP RT WING TE DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16808 36783 49262 MIA - INSPECTION FOUND RIGHT WING CENTER SPAR TRAILING EDGE LOWER PANEL BELOW INBOARD AND OUTBOARD ANTI-SKID VALVES DELA MINATED. THE DELAMINATED AREA WAS CUT OUT. A NEW CORE WAS INSTALLED AND FIBERGLASS OVERLAY WAS APPLIED IAW SRM 51-70-2 . (M) 2 L 7 2 4F A6WE 1996031500512 19960315 00512 WP 1996 3 15 CAL960099 1 19960113 A 5753 SKIN DOUG DC9 DC982 3022082 WP LT TE FLAP CHAFED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16808 36783 49262 MIA - INSPECTION FOUND LEFT WING INBOARD FLAP UPPER SURFACE CHAFED INTO TWENTY INCHES FROM OUTBOARD END. THE CHAFED ARE A WAS CUT OUT. AN INTERNAL DOUBLER AND FILLER WERE FABRICATED IAW SRM 51-01, FIGURE 4 AND INSTALLED IAW SRM 51-30-0. ( M) 2 L 7 2 4F A6WE 1996031500513 19960315 00513 WP 1996 3 15 CAL960100 1 19960115 A 5755 SKIN DOUG DC9 DC982 3022082 WP RT SPOILER DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16808 36783 49262 MIA - INSPECTION FOUND RIGHT WING INBOARD SPOILER UPPER SKIN DELAMINATED AT FORWARD INBOARD AREA. THE DAMAGED CORE WAS CUT OUT AND A HOT BOND REPAIR WAS DONE IAW SRM 51-70-1A. (M) 2 L 7 2 4F A6WE 1996031500514 19960315 00514 WP 1996 3 15 CAL960101 1 19960113 A 5753 VANE DOUG DC9 DC982 3022082 WP LT TE FLAP CHAFED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16808 36783 49262 MIA - INSPECTION FOUND LEFT WING OUTBOARD FLAP OUTBOARD VANE SEGMENT CHAFED WITH METAL CURLED AT INBOARD UPPER END. THE CHAFED AREA WAS CUT OUT. FILLER AND DOUBLER WERE FABRICATED AND HOT BONDED IAW SRM 51-1-40A. (M) 2 L 7 2 4F A6WE 1996031500515 19960315 00515 WP 1996 3 15 CAL960102 1 19960111 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP FWD GALLEY DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16808 49262 MIA - INSPECTION FOUND FORWARD GALLEY EMERGENCY LIGHT DIM. THE BATTERY PACK WAS REPLACED AND A LAMP WAS INSTALLED PER M M 33-50-0. (M) 2 L 7 2 4F A6WE 1996031500516 19960315 00516 WP 1996 3 15 CAL960103 1 19960111 A 3350 BATTERY DOUG DC9 DC982 3022082 WP AFT GALLEY DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16808 49262 MIA - INSPECTION FOUND AFT GALLEY EMEREGNCY LIGHT DIM. THE BATTERIES FOR THE LIGHT WERE REMOVED, CHARGED AND REINSTALLE D. (M) 2 L 7 2 4F A6WE 1996031500517 19960315 00517 WP 1996 3 15 CAL960105 1 19960111 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP AFT GALLEY DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16808 49262 MIA - INSPECTION FOUND THE AISLE OVERHEAD EMERGENCY LIGHT AT AFT GALLEY TO LAV INOPERATIVE. THE BATTERIES FOR THE EMERG ENCY LIGHT WERE REMOVED, CHARGED, AND REINSTALLED. (M) 2 L 7 2 4F A6WE 1996031500518 19960315 00518 WP 1996 3 15 CAL960106 1 19960111 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16808 49262 MIA - INSPECTION FOUND THE FORWARD ENTRY EMERGENCY LIGHT DIM. THE BATTERIES FOR THE EMERGENCY LIGHT WERE REMOVED, RECHA RGED, AND REINSTALLED. (M) 2 L 7 2 4F A6WE 1996031500519 19960315 00519 WP 1996 3 15 CAL960109 1 19960208 A 2750 HANDLE DOUG DC9 DC981 3022081 WP FLAP SYSTEM LACK OF LUBE A CALA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 SW 09 37882 48027 FLT NR 1490 - CLE - THE FLAP/SLAT HANDLE WOULD NOT LOCK INTO THE SLAT RETRACT POSITION. WHEN HOLDING FLAP/SLAT HANDLE T O SLAT RETRACT POSITION THE SLAT DISAGREE LIGHT CAME ON AND BOTH LEFT AND RIGHT HYDRAULIC GAUGES DROPPED. THE DIAL-A-FL AP WAS MOVED SEVERAL TIMES. A SNAP WAS HEARD, AND THEN SLATS WERE RAISED. THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LA NDED WITHOUT INCIDENT. MAINTENANCE FOUND THE DIAL-A-FLAP STOP MECHANISM AND FLAP/SLAT HANDLE DIRTY AND GUMMED UP. THE STOP MECHANISM AND HANDLE WERE CLEANED AND LUBRICATED. OPERATION WAS SMOOTH AND NO DEFECTS WERE NOTED. (M) 2 L 7 2 4F A6WE 1996031500520 19960315 00520 NE 1996 3 15 CAL960110 2 19960208 A 7250 TURB BLADE BOEING 737 7372C0 1384488 NM PWA JT8 JT8D9 52048 NE NR 2 ENGINE BROKE A CALA E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SW 09 73243 48830 1760 20072 666083 FLT NR 1930 - IAH - THE NR 2 ENGINE SHUDDERED AND THEN BEGAN TO LOSE POWER DURING CLIMB-OUT OF IAH. THE NR 2 ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. THE NR 2 ENGINE WAS REMOVED AND REPLA CED. INVESTIGATION REVEALED A FIRST STAGE TURBINE BROKEN ABOOUT .5 INCH FROM THE TIP. (M) 2 L 7 2 4F 4 F A16WE E2EA 1996031500521 19960315 00521 NM 1996 3 15 CAL960111 1 19960209 A 2121 6454051 FAN BOEING 737 7373T0 1384582 NM CABIN INOPERATIVE A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 71314 33169 5421 23365 FLT NR 1082 - CLE - A SMOKEY ODOR IN REAR OF CABIN WAS REPORTED TWICE DURING FLIGHT. THE AIR WAS CLEARED BOTH TIMES BY USING HIGH POSITION ON BOTH PACKS. MAINTENANCE RAN BOTH PACKS AND INSPECTED THE WATER SEPARATOR BAGS. MAINTENANCE WAS UNABLE TO REPRODUCE THE ODOR AND NO DEFECTS WERE FOUND. SUBSEQUENTLY, WHILE THE AIRCRAFT WAS IN SERVICE CHECK, THE AIR DISTRIBUTION FAN WAS FOUND AT FAULT. THE AIR DISTRIBUTION FAN WAS REMOVED AND REPLACED. (M) 2 L 7 2 4F RT A16WE 1996031500522 19960315 00522 WP 1996 3 15 CAL960112 1 19960121 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 1287 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 34838 26291 49634 MIA - INSPECTION FOUND ANGLE UNDER LEFT FLOOR TRACK IN AFT PIT CORRODED AT STATION 1287. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-05-4 AND 51-30-02. (M) 2 L 7 2 4F A6WE 1996031500523 19960315 00523 WP 1996 3 15 CAL960113 1 19960116 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP FS 1142 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 34838 26291 49634 MIA - INSPECTION FOUND CORROSION ON WEB AND FLOOR SUPPORT STRUCTURE UNDER BRACKET AT AFT SERVICE DOOR AREA, FS 1142. TH E CORRODED AREAS WERE REMOVED AND REPAIRS WERE INSTALLED IAW SRM 53-01, FIGURE 2, SHEET 3 AND 4. (M) 2 L 7 2 4F A6WE 1996031500524 19960315 00524 WP 1996 3 15 CAL960114 1 19960121 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 34838 26291 49634 MIA - INSPECTION FOUND FLOORBOARD SUPPORT AT FORWARD SERVICE DOOR, STATION 200 CORRODED. A NEW FLOOR SUPPORT WAS FABRIC ATED AND INSTALLED IAW SRM 51-30-2. (M) 2 L 7 2 4F A6WE 1996031500525 19960315 00525 WP 1996 3 15 CAL960115 1 19960111 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 1150 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 34838 26291 49634 MIA - INSPECTION FOUND FORWARD ANGLE UNDER PANEL AT AFT SERVICE DOOR ENTRY, STATION 1150 CORRODED. A NEW ANGLE WAS FABR ICATED AND INSTALLED IAW SRM 51-10-2A AND 51-30-2. (M) 2 L 7 2 4F A6WE 1996031500526 19960315 00526 WP 1996 3 15 CAL960117 1 19960120 A 5753 SKIN DOUG DC9 DC982 3022082 WP RT TE FLAP DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 34838 26291 49634 MAI - THE SECOND FROM INBOARD SECTION OF RIGHT WING TRAILING EDGE FLAP WAS FOUND DELAMINATED. A FIBERGLASS OVERLAY WAS APPLIED IAW SRM 51-70-2. (M) 2 L 7 2 4F A6WE 1996031500527 19960315 00527 WP 1996 3 15 CAL960118 1 19960120 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 1287 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 34838 26291 49634 MIA - INSPECTION FOUND LONGERON 28L CORRODED AT STATION 1287 IN AFT CARGO COMPARTMENT. THE CORROSION WAS REMOVED IAW SR M 51-10-3. A SECTION OF LONGERON WAS REMOVED AND A NEW SECTION WAS SPLICED IN IAW SRM 53-02, FIGURE 1. (M) 2 L 7 2 4F A6WE 1996031500528 19960315 00528 WP 1996 3 15 CAL960119 1 19960121 A 5330 SKIN DOUG DC9 DC982 3022082 WP FS 350 GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 34838 26291 49634 MIA - INSPECTION FOUND FUSELAGE BELLY SKIN DENTED AND GOUGED AT FS 350 BETWEEN LONGERON 28R AND 29R. THE GOUGE WAS BURN ISHED. THE SMALL DENT WAS DRILLED OUT, AND FLUSH FASTENERS WERE INSTALLED IAW SRM 53-01, FIGURE 38, SHEET 1. (M) 2 L 7 2 4F A6WE 1996031500529 19960315 00529 NM 1996 3 15 CAL960120 1 19960109 A 5320 SUPPORT BOEING 727 727227 1384078 NM BS 312-328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 49249 21247 STATION 31J - INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT BS 312 TO 328, LBL 28. THE CORRODED AREA WAS REMOVED. A NEW PART WAS FABRICATED, TREATED, AND INSTALLED IAW SRM 51-10-1, 51-10-2, AND MM 51-20-11. (M) 2 L 7 3 4F A3WE 1996031500530 19960315 00530 NM 1996 3 15 CAL960121 1 19960109 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 380 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 49249 21247 STATION 31J - INSPECTION FOUND FLOORBEAM CORRODED AT BS 380, RBL 10 TO 60. THE CORRODED AREA WAS CUT OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8. (M) 2 L 7 3 4F A3WE 1996031500531 19960315 00531 NM 1996 3 15 CAL960122 1 19960109 A 5320 SUPPORT BOEING 727 727227 1384078 NM BS 360-380 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 49249 21247 STATION 31J - INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT BS 360 TO 380, RBL 10. THE FLOOR SUPPORT WAS REMOVED. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-2, AND 51-40-4. (M) 2 L 7 3 4F A3WE 1996031500532 19960315 00532 NM 1996 3 15 CAL960123 1 19960116 A 5320 FITTING BOEING 727 727227 1384078 NM BS 420-460 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 49249 21247 STATION 31J - INSPECTION FOUND FLOOR SUPPORT FITTING AT BS 420 TO 440, RBL 10 AND AT BS 440 TO 460, RBL 10 CORRODED. TH E FLOOR SUPPORT FITTINGS WERE REMOVED. NEW FLOOR SUPPORT FITTINGS AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-2 0-2 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1996031500533 19960315 00533 NM 1996 3 15 CAL960124 1 19960110 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 440 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 49249 21247 STATION 31J - INSPECTION FOUND CABIN FLOORBEAM CORRODED AT BS 440, LBL 20 TO RBL 20. THE CORRODED SECTION WAS CUT OUT. A REPAIR BEAM SECTION WAS FABRICATED AND INSTALLED IAW SRM 53-10-8, FIGURE 3, 51-30-2, 51-20-4, 51-10-1, 51-30-8, 51-10 -2, AND MM 51-20-0. (M) 2 L 7 3 4F A3WE 1996031500534 19960315 00534 NM 1996 3 15 CAL960125 1 19960107 A 5315 FLOOR BEAM BOEING 727 727227 1384078 NM BS 460 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 49249 21247 STATION 31J - INSPECTION FOUND CABIN FLOORBEAAM CORRODED AT BS 460, RBL 60. THE CORRODED AREA WAS TRIMMED OUT. A FLOOR BEAM REPAIR SECTION WAS FABRICATED AND INSTALLED IAW SRM 53-10-8. (M) 2 L 7 3 4F A3WE 1996031500535 19960315 00535 NM 1996 3 15 CAL960126 1 19960110 A 5315 FLOOR BEAM BOEING 727 727227 1384078 NM BS 480 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 49249 21247 STATION 31J - INSPECTION FOUND CABIN FLOOR BEAM CORRODED AT BS 480, RBL 0 TO 60. THE CORRODED CAP WAS REMOVED FROM RBL 0 TO 60. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-8, FIGURE 3, 51-10-1, 51-10-2, AND 51-20-0. (M) 2 L 7 3 4F A3WE 1996031500536 19960315 00536 NM 1996 3 15 CAL960127 1 19960109 A 5320 ANGLE BOEING 727 727227 1384078 NM BS 720-740 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 49249 21247 STATION 31J - INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT BS 720F TO 740, BL 0. THE SUPPORT ANGLE WAS REMOVED. A NEW SUPPORT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2, AND MM 51-20-0. (M) 2 L 7 3 4F A3WE 1996031500537 19960315 00537 NM 1996 3 15 CAL960128 1 19960106 A 5315 FLOOR BEAM BOEING 727 727227 1384078 NM BS 825.95 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 49249 21247 STATION 31J - INSPECTION FOUND FLOORBEAM WEB CRACKED APPROXIMATELY 12 INCHES AT BS 825.95, LBL 59, FROM WL 208 TO 220. T HE CRACK WAS CUT OUT. A WEB REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-30-2, AND 51-10-2. (M) 2 L 7 3 4F A3WE 1996031500538 19960315 00538 NM 1996 3 15 CAL960129 1 19960111 A 5330 SKIN BOEING 727 727227 1384078 NM FS 1010 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 49249 21247 STATION 31J - INSPECTION FOUND SKIN CORRODED AT FS 1010, STRINGER 28L. THE CORRODED SECTION OF SKIN WAS CUT OUT. A DOUB LER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-2, 53-30-3, AND 51-10-2. A STRINGER SECTION AND TWO CA P SPLICES WERE FABRICATED AND INSTALLED IAW SRM 53-10-3 AND 51-10-2. (M) 2 L 7 3 4F A3WE 1996031500539 19960315 00539 NM 1996 3 15 CAL960130 1 19960107 A 5320 SUPPORT BOEING 727 727227 1384078 NM BS 1033 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 49249 21247 STATION 31J - INSPECTION FOUND CORROSION UNDER FLOOR SUPPORT ANGLE STRAP AT STATION 1033, LBL 12 TO RBL 12. THE FLOOR S UPPORT WAS REPLACED AND THE AREA WAS PRIMED IAW SRM 51-10-6, 51-10-2, 51-30-3, 51-30-2, AND 53-10-1. (M) 2 L 7 3 4F A3WE 1996031500540 19960315 00540 NM 1996 3 15 CAL960131 1 19960115 A 5320 SUPPORT BOEING 727 727227 1384078 NM BS 1070 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 49249 21247 STATION 31J - INSPECTION FOUND FLOOR SUPPORT OVER PULLEY CORRODED AT BS 1070, RBL 20. THE FLOOR SUPPORT WAS REMOVED. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW MM 51-20-2 AND 51-20-11. (M) 2 L 7 3 4F A3WE 1996031500541 19960315 00541 NM 1996 3 15 CAL960132 1 19960110 A 5315 FLOOR BEAM BOEING 727 727227 1384078 NM BS 1110 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 49249 21247 STATION 31J - INSPECTION FOUND FLOOR BEAM CORRODED AT BS 1110, RBL 25. THE FLOOR BEAM UPPER CHORD WAS REMOVED IAW SRM 5 3-10-8. A NEW FLOOR BEAM UPPER CAP, STRAPS, SUPPORT ANGLES, L-ANGLES, AND STIFFENERS WERE FABRICATED AND INSTALLED IAW SRM 51-10-2. (M) 2 L 7 3 4F A3WE 1996031500542 19960315 00542 NM 1996 3 15 CAL960133 1 19960108 A 5320 SUPPORT BOEING 727 727227 1384078 NM BS 1070-1090 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 49249 21247 STATION 31J - INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 1070-1090, RBL 10. THE FLOOR SUPPORT WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-4 AND MM 51-10-2. (M) 2 L 7 3 4F A3WE 1996031500543 19960315 00543 NM 1996 3 15 CAL960134 1 19960111 A 5315 FLOOR BEAM BOEING 727 727227 1384078 NM BS 1130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 49249 21247 STATION 31J - INSPECTION FOUND FLOOR BEAM LOWER CHORD CORRODED AT FASTENER HOLES, BS 1130, RBL O TO 56. A NEW REPAIR ST RAP WAS FABRICATED. THE REPAIR WAS INSTALLED IAW AERO CORP ENGINEERING ORDER 96-250. (M) 2 L 7 3 4F A3WE 1996031500544 19960315 00544 NM 1996 3 15 CAL960135 1 19960108 A 5312 BLKHD CHORD BOEING 727 727227 1384078 NM BS 1176.9 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 49249 21247 STATION 31J - INSPECTION FOUND BULKHEAD REINFORCEMENT CHORD CORRODED ON RIGHT OUTBOARD END AT BS 1176.9. THE CORRODED S ECTION OF CHORD WAS REMOVED. A NEW CHORD ANGLE BRACKET REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-6, 51-40-3, 51 -40-4, 51-10-1, 51-10-2, AND MM 51-20-0. (M) 2 L 7 3 4F A3WE 1996031500546 19960315 00546 NM 1996 3 15 CAL960137 1 19960108 A 5320 HAT SECTIONS BOEING 727 727227 1384078 NM LT/RT LAV CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 49249 21247 STATION 31J - INSPECTION FOUND FLOOR HAT SECTIONS AT LEFT AND RIGHT AFT LAV SIDEWALLS CORRODED. THE FLOOR HAT SECTIONS WERE REMOVED AND REPLACED IAW SRM 51-10-2, 51-30-2, AND 51-20-4. (M) 2 L 7 3 4F A3WE 1996031500547 19960315 00547 NM 1996 3 15 CAL960138 1 19960107 A 5320 HAT SECTION BOEING 727 727227 1384078 NM LAV FLOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 49249 21247 STATION 31J - INSPECTION FOUND FORWARD LAV FLOOR HAT SECTION CORRODED UNDER LAV DOOR AND INBOARD WALL. THE HAT SECTION WAS REMOVED. A NEW HAT SECTION WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, PAGE 4, 51-30-5, 51-30-8, 51-30-3, 51-30-2 , 51-30-4, 51-10-2, AND MM 51-20-0. (M) 2 L 7 3 4F A3WE 1996031500548 19960315 00548 NM 1996 3 15 CAL960139 1 19960111 A 5321 FLOOR BOEING 727 727227 1384078 NM FWD LAVATORY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 49249 21247 STATION 31J - INSPECTION FOUND FORWARD LAV FLOOR PANEL CORRODED. A NEW WEB SECTION AND L-ANGLE REPAIR WAS FABRICATED AN D INSTALLED IAW SRM 51-40-2, 51-10-1, 51-10-2, AND 51-40-3. (M) 2 L 7 3 4F A3WE 1996031500549 19960315 00549 NM 1996 3 15 CAL960140 1 19960109 A 7110 FLANGE BOEING 727 727227 1384078 NM NR 1 ENGINE COWL CRUSHED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 49249 21247 STATION 31J - INSPECTION FOUND NR 1 ENGINE LOWER COWL FLANGE ON UPPER INBOARD LONGERON CRUSHED. A 3.5 INCH SECTION OF L ONGERON WAS REMOVED. A Z-ANGLE, REPAIR DOUBLER, AND COVER PLATE WERE FABRICATED AND INSTALLED IAW SRM 51-40-3. (M) 2 L 7 3 4F A3WE 1996031500550 19960315 00550 NM 1996 3 15 CAL960141 1 19960111 A 5320 69455964 GUSSET BOEING 727 727227 1384078 NM BS 825.96 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 49249 21247 STATION 31J - INSPECTION FOUND A 1.5 INCH CRACK IN RIGHT OVERWING EXIT GUSSET AT BS 825.95, RBL 50, WL 215 TO 220. A NE W GUSSET WAS DRILLED AND INSTALLED IAW EA SA001-5310-01870. (M) 2 L 7 3 4F A3WE 1996031500551 19960315 00551 NM 1996 3 15 CAL960144 1 19960106 A 5712 RIB BOEING 727 727227 1384078 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 49249 21247 STATION 31J - INSPECTION FOUND TWO .5 INCH CRACKS AT THE TWO MOST AFT SCREW HOLES IN RIGHT WING LEADING EDGE RIB UPPER C HORD. THE CHORD WAS REMOVED. AN ANGLE WAS FABRICATED AND INSTALLED IAW SRM 57-20-2, 51-10-2, 51-30-2, AND MM 51-20-2. (M) 2 L 7 3 4F A3WE 1996031500552 19960315 00552 NM 1996 3 15 CAL960145 1 19960106 A 5720 STIFFENER BOEING 727 727227 1384078 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 49249 21247 STATION 31J - INSPECTION FOUND A .75 INCH CRACK ON LOWER END OF THE THIRD VERTICAL STIFFENER OF RIGHT WING LEADING EDGE INBOARD RIB AT WS 75. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40- 3, 51-10-2, AND 51-30-2. (M) 2 L 7 3 4F A3WE 1996031500553 19960315 00553 NM 1996 3 15 CAL960146 1 19960108 A 5210 SKIN BOEING 727 727227 1384078 NM R-1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 49249 21247 STATION 31J - INSPECTION FOUND A 1 INCH CRACK AT RIVET HOLE OF R-1 DOOR AFT LOWER CORNER EXTERNAL SKIN. THE CRACKED ARE A OF DOOR WAS REMOVED. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-00-3 AND 52-00-3. (M) 2 L 7 3 4F A3WE 1996031500554 19960315 00554 NM 1996 3 15 CAL960147 1 19960108 A 5210 SKIN BOEING 727 727227 1384078 NM R-1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 49249 21247 STATION 31J - INSPECTION FOUND A .5 INCH CRACK THROUGH RIVET HOLE OF R-1 DOOR EXTERNAL SKIN ABOVE LOWER HINGE CUTOUT. T HE CRACKED AREA WAS REMOVED. A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 52-00-3, 51-30-2, 51-10- 2, AND MM 51-20-2. (M) 2 L 7 3 4F A3WE 1996031500555 19960315 00555 NM 1996 3 15 CAL960148 1 19960106 A 5754 ATTACHMENT BOEING 727 727227 1384078 NM NR 4 LE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 49249 21247 STATION 31J - INSPECTION FOUND A 1 INCH CRACK AT OUTBOARD BULL NOSE AFT LINKAGE ATTACHMENT OF RIGHT WING NR 4 KRUEGER FL AP. THE CRACK WAS STOP DRILLED. DOUBLERS AND ANGLES WERE FABRICATED AND INSTALLED IAW SRM 57-30-3, 51-10-2, AND 51-30- 8. (M) 2 L 7 3 4F A3WE 1996031500556 19960315 00556 NM 1996 3 15 CAL960149 1 19960127 A 5321 FLOOR SKIN BOEING 727 727227 1384078 NM G2 GALLEY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 49249 21247 STATION 31J - INSPECTION FOUND G2 GALLEY FLOOR AND MOUNT BRACKET CORRODED. THE MOUNT BRACKET AND FLOOR SKIN WERE REMOVE D. A NEW FLOOR SKIN WAS FABRICATED AND INSTALLED. THE CORROSION WAS CLEANED FROM BLOCK TIE DOWN AND REBONDED AND A NEW UPPER SHELF WAS INSTALLED IAW MM 25-32-0 AND SRM 51-40-9 AND 51-10-2. (M) 2 L 7 3 4F A3WE 1996031500557 19960315 00557 NM 1996 3 15 CAL960150 1 19960103 A 5311 FRAME BOEING 727 727227 1384078 NM BS 1263 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 49249 21247 STATION 31J - INSPECTION FOUND BS 1263 TORQUE BOX FRAME AT VENTRAL STAIR AREA HAD A 2 INCH CRACK IN RADIUS OF REPAIR DOU BLER AFT FLANGE AND A 4 INCH CRACK BEYOND CONTAINMENT OF ONE DOUBLER AND STOP DRILL ON FORWARD FLANGE. REPAIRS WERE PER FORMED IAW CAL WORK CARD NR MFG JA5310-0246004001. FASTENERS WERE INSTALLED IAW SRM 51-30-2. PARTS CHANNEL AND FRAME S UPPORT WERE INSTALLED IAW SRM 51-10-4. (M) 2 L 7 3 4F A3WE 1996031500558 19960315 00558 NM 1996 3 15 CAL960151 1 19960109 A 5320 SUPPORT BOEING 727 727227 1384078 NM BS 418 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 49249 21247 STATION 31J - INSPECTION FOUND CORROSION ON CABIN FLOOR SUPPORT AT BS 418, RBL 20 TO 40. THE CORROSION WAS REMOVED AND TREATED IAW SRM 51-10-6. (M) 2 L 7 3 4F A3WE 1996031500559 19960315 00559 NM 1996 3 15 CAL960152 1 19960214 A 2910 HYD LINE BOEING 737 737130 1384435 NM 'A' HYD SYSTEM LEAKING A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77215 19032 FLT NR 1446 - EWR - THE 'A' SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO WHEN GEAR WAS EXTENDED FOR LANDING AT EWR. THE AI RCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NR 1 ENGINE 'A' SYSTEM HYDRAULIC PRESSURE LINE LEAKING AT CLAMP. THE PRESSURE LINE WAS REMOVED AND REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD. (M) 2 L 7 2 4F A16WE 1996031500560 19960315 00560 NM 1996 3 15 CAL960154 1 19960209 A 5412 65574808 FIREWALL BOEING 737 7372C0 1384488 NM NR 2 ENGINE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73243 20072 IAH - INSPECTION FOUND THE NR 2 ENGINE PYLON FIREWALL PAN HAD A 2.5 INCH CRACK THROUGH FOUR FASTENERS AT NAC STATION 144 . A DOUBLER WAS INSTALLED IAW ECRA 5450-01139. A DIP WAS ISSUED TO REINSPECT THE AREA AT LPV CHECKS AND PERMANENTLY RE PAIR PAN AT NEXT 1/4D-CHECK. (M) 2 L 7 2 4F A16WE 1996031500561 19960315 00561 NM 1996 3 15 CAL960157 1 19960216 A 3397 WIRE BOEING 737 7373Q8 1384670 NM CABIN BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14381 26310 FLT NR 1979 - EWR - INSPECTION FOUND ALL EMERGENCY AISLE PATH LIGHTS INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AND P IN PULLED OUT OF PLUG AT ROW 11. THE PIN WAS REINSTALLED AND THE WIRE WAS REPAIRED. IN ADDITION, A BLOWN BATTERY PACK FUSE WAS REPLACED. OPERATIONAL CHECKS WERE GOOD. (M) 2 L 7 2 4F RT A16WE 1996031500562 19960315 00562 WP 1996 3 15 CAL960158 1 19960218 A 2740 AJG70415533 VALVE DOUG DC10 DC1030 3023501 WP HORIZ STAB LEAKING A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 14062 16060 7874 47863 FLT NR 10 - EWR - THE NR 1 HYDRAULIC SYSTEM BEGAN TO LOSE FLUID WHILE EN ROUTE FROM IAH TO ORY. THE QUANTITY DROPPED ST EADILY. THE AIRCRAFT WAS DIVERTED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LOWER PRIMARY TRIM CO NTROL VALVE LEAKING. THE LOWER PRIMARY TRIM CONTROL VALVE WAS REMOVED AND REPLACED IAW MM 27-43-03, PAGE 501. LEAK AND OPERATIONAL CHECKS WERE GOOD. (M) 2 L 7 3 4F A22WE 1996031500563 19960315 00563 WP 1996 3 15 CAL960159 1 19960115 A 5320 FLOOR WEB DOUG DC9 DC982 3022082 WP BS 1300 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16808 36783 49262 MIA - INSPECTION FOUND AN 8 INCH CRACK IN SUB FLOOR WEB ON RIGHT SIDE, STATION 1300, STRINGER 18. A NEW DOUBLER WAS FAB RICATED AND INSTALLED IAW SRM 53-01, FIGURE 2. (M) 2 L 7 2 4F A6WE 1996031500564 19960315 00564 WP 1996 3 15 CAL960160 1 19960117 A 5312 BULKHEAD DOUG DC9 DC982 3022082 WP FS 1490 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16808 36783 36783 49262 MIA - INSPECTION FOUND A .5 INCH CRACK IN CANTED BULKHEAD WEB JUST FORWARD OF RUDDER TRIM ACTUATOR DRUM AT FS 1490, RIGH T SIDE. THE CRACKED WEB WAS REMOVED AND A BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-30-02. (M) 2 L 7 2 4F A6WE 1996031500565 19960315 00565 WP 1996 3 15 CAL960162 1 19960115 A 5530 5939711501 ANGLE DOUG DC9 DC982 3022082 WP BS 1401-1429 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16808 36783 49262 MIA - INSPECTION FOUND A .5 INCH CRACK IN LEFT AND RIGHT VERTICAL STABILIZER TO FUSELAGE EXTERNAL ATTACH ANGLES LOCATED BETWEEN BS 1401 TO 1429. THE ANGLES WERE REMOVED AND REPLACED IAW SRM 51-30-2. (M) 2 L 7 2 4F A6WE 1996031500566 19960315 00566 WP 1996 3 15 CAL960163 1 19960120 A 5330 SKIN DOUG DC9 DC982 3022082 WP FWD FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 34838 26291 49634 MIA - INSPECTION FOUND A .5 INCH CRACK IN SKIN AT AFT HINGE CUTOUT FOR RIGHT NLG STRUT DOOR. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 62. (M) 2 L 7 2 4F A6WE 1996031500567 19960315 00567 WP 1996 3 15 CAL960164 1 19960120 A 5510 CHORD DOUG DC9 DC982 3022082 WP HORIZ STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 34838 26291 49634 MIA - INSPECTION FOUND A 1 INCH CRACK IN INBOARD LOWER CHORD OF INBOARD LEFT HORIZONTAL STABILIZER LEADING EDGE FLANGE. THE CRACK WAS LOCATED AT ROLLER FITTING. THE CHORD WAS REMOVED AND REPLACED IAW SRM 51-30-2. (M) 2 L 7 2 4F A6WE 1996031500568 19960315 00568 WP 1996 3 15 CAL960165 1 19960117 A 5311 FRAME DOUG DC10 DC1030 3023501 WP BS 1841 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13067 77547 47866 KUL - INSPECTION FOUND CAP CORRODED AT FRAME, STATION 1841 BETWEEN LONGERONS 50L AND 51R. THE AREA WAS REPAIRED IAW ECR A 5310-03214. (M) 2 L 7 3 4F A22WE 1996031500569 19960315 00569 WP 1996 3 15 CAL960166 1 19960117 A 5313 LONGERON DOUG DC10 DC1030 3023501 WP BS 1409 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13067 77547 47866 KUL - INSPECTION FOUND CORROSION IN FLANGE OF LONGERON 32L AT STATION 1409. REPAIRED IAW ECRA 5310-03215. (M) 2 L 7 3 4F A22WE 1996031500570 19960315 00570 WP 1996 3 15 CAL960167 1 19960118 A 5313 LONGERON DOUG DC10 DC1030 3023501 WP BS 1406 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13067 77547 47866 KUL - INSPECTION FOUND CORROSION IN THE FLANGE OF LONGERON 37L AT STATION 1406. REPAIRED IAW ECRA 5310-03217. (M) 2 L 7 3 4F A22WE 1996031500571 19960315 00571 WP 1996 3 15 CAL960168 1 19960118 A 5313 LONGERON DOUG DC10 DC1030 3023501 WP BS 1412 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13067 77547 47866 KUL - INSPECTION FOUND CORROSION IN RIGHT FLANGE OF LONGERON 30L AT STATION 1412. REPAIRED IAW ECRA 5310-03219. (M) 2 L 7 3 4F A22WE 1996031500572 19960315 00572 WP 1996 3 15 CAL960169 1 19960122 A 5313 LONGERON DOUG DC10 DC1030 3023501 WP BS 1811 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13067 77547 47866 KUL - INSPECTION FOUND CORROSION ON BOTH SIDES OF LONGERON 46L AT STATION 1811. REPAIRED IAW ECRA 5310-03221. (M) 2 L 7 3 4F A22WE 1996031500573 19960315 00573 WP 1996 3 15 CAL960170 1 19960122 A 5313 LONGERON DOUG DC10 DC1030 3023501 WP BS 1536/1545 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13067 77547 47866 KUL - INSPECTION FOUND CORROSION IN LONGERON SPLICE 37R AT STATION 1536 AND 1545. REPAIRED IAW ECRA 5310-03223. (M) 2 L 7 3 4F A22WE 1996031500574 19960315 00574 WP 1996 3 15 CAL960171 1 19960122 A 5313 LONGERON DOUG DC10 DC1030 3023501 WP BS 1561 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13067 77547 47866 KUL - INSPECTION FOUND CORROSION IN LONGERON SPLICE 32R AT STATION 1561. REPAIRED PER ECRA 5310-03222. (M0 2 L 7 3 4F A22WE 1996031500575 19960315 00575 WP 1996 3 15 CAL960172 1 19960124 A 5315 FLOOR BEAM DOUG DC10 DC1030 3023501 WP BS 1701 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13067 77547 47866 KUL - INSPECTION FOUND CORROSION ON FLOOR BEAM AT STATION 1701. REPAIRED IAW ECRA 5310-03225. (M) 2 L 7 3 4F A22WE 1996031500576 19960315 00576 WP 1996 3 15 CAL960173 1 19960117 A 5753 ARC2906504 FAIRING DOUG DC10 DC1030 3023501 WP RT TE FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13067 77547 47866 KUL - INSPECTION FOUND CORROSION IN SKIN AND DOUBLER OF THE RIGHT PANEL ASSEMBLY OF RIGHT WING INBOARD FLAP OUTER HINGE FAIRING. REPAIRED IAW ECRA 5752-01017. (M) 2 L 7 3 4F A22WE 1996031500577 19960315 00577 WP 1996 3 15 CAL960174 1 19960219 A 2740 AJG70415535 VALVE DOUG DC10 DC1030 3023501 WP HORIZ STAB LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 68060 19616 47850 FLT NR 41 - EWR - THE NR 1 HYDRAULIC SYSTEM QUANTITY DROPPED SLOWLY WHILE EN ROUTE FROM FCO TO EWR. THE SYSTEM WAS SHUT DOWN IN FLIGHT AND RESTARTED PRIOR TO LANDING. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LOWER PRIMA RY TRIM CONTROL VALVE LEAKING. THE VALVE WAS REMOVED AND REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD. (M) 2 L 7 3 4F A22WE 1996031500578 19960315 00578 NM 1996 3 15 CAL960175 1 19960219 A 2750 RESERVOIR BOEING 737 737130 1384435 NM FLAP DRIVE MOTOR LOW FLUID A CALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 09 14206 19023 FLT NR 1627 - EWR - THE FLAPS WOULD NOT RETRACT FROM 5 DEGREE POSITION AFTER DEPARTURE FROM EWR. ALTERNATE FLAP EXTENSI ON WAS USED PER 'ABNORMAL' PROCEDURES AND THE FLAPS EXTENDED TO 15 DEGREES. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT L ANDED WITHOUT INCIDENT. THE FLAPS WERE EXTENDED AND THE TORQUE TUBES, TRANSMISSION, CARRIAGES, AND TOGGLES WERE INSPECT ED WITH NO DEFECTS NOTED. THE FLAP DRIVE MOTOR RESERVOIR WAS FOUND LOW ON FLUID. THE RESERVOIR WAS SERVICED AND THE FL APS WERE SUCCESSFULLY CYCLED SEVERAL TIMES. IN ADDITION, THE FLAP POSITION INDICATOR WAS REPLACED AS A PRECAUTIONARY ME ASURE. (M) 2 L 7 2 4F A16WE 1996031500579 19960315 00579 NM 1996 3 15 CAL960177 1 19960204 A 5330 SKIN BOEING 737 737247 138448D NM BS 847-927 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14246 67915 20129 GSO - INSPECTION FOUND FUSELAGE SKIN DELAMINATED AT STATION 847-927, STRINGER 20R-25R. THE DELAMINATED SECTION OF SKIN WAS CUT OUT. THE AREA WAS REPAIRED IAW SRM 53-30-2 AND 53-30-3, FIGURE 7. (M) 2 L 7 2 4F A16WE 1996031500580 19960315 00580 NM 1996 3 15 CAL960178 1 19960209 A 5320 CHORD BOEING 737 737247 138448D NM BS 727 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14246 67915 20129 INSPECTION FOUND A 3 INCH CRACK FROM FORWARD FASTENER HOLE TO AFT HOLE OF RIGHT OUTBOARD CHORD AT STRINGER 18A, STATION 727. THE CHORD SEGMENT WAS REMOVED AND REPLACED IAW BOEING DRAWING NR 65C33722 AND CONTINENTAL WORK CARD JA5310-0163804 001. (M) 2 L 7 2 4F A16WE 1996031500581 19960315 00581 NM 1996 3 15 CAL960179 1 19960204 A 5315 FLOOR BEAM BOEING 737 737247 138448D NM BS 675 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14246 67915 20129 GSO - INSPECTION FOUND A 3 INCH CRACK IN LOWER 'T' CHORD OF FLOOR BEAM AT STATION 675, BBL 0, REPAIRED IAW ECRA 5710-017 15. (M) 2 L 7 2 4F A16WE 1996031500582 19960315 00582 NM 1996 3 15 CAL960180 1 19960211 A 5312 BULKHEAD BOEING 737 737247 138448D NM STA 178 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14246 67915 20129 GSO - INSPECTION FOUND A 7 INCH CRACK IN PRESSURE BULKHEAD ON RIGHT SIDE JUST ABOVE HORIZONTAL STIFFENER AT STATION 178. THE CRACKED AREA WAS REMOVED AND A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-10-11. (M) 2 L 7 2 4F A16WE 1996031500583 19960315 00583 NM 1996 3 15 CAL960181 1 19960211 A 5312 BULKHEAD BOEING 737 737247 138448D NM BS 178 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14246 67915 20129 GSO - INSPECTION FOUND AN 8 INCH CRACK IN PRESSURE BULKHEAD AT PRESSURE FEED THROUGH FOR RADAR WIRING AT STATION 178. T HE CRACKED SECTION WAS REMOVED. A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-10-11. (M) 2 L 7 2 4F A16WE 1996031500584 19960315 00584 NM 1996 3 15 CAL961076 1 19960130 A 5330 SKIN BOEING 737 737247 138448D NM E/E DOOR CUTOUT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14246 67915 20129 GSO - INSPECTION FOUND E/E COMPARTMENT DOOR CUTOUT CORRODED AT STATION 328-370, RBL 15.7. A SECTION OF T-ANGLE WAS REMO VED AND REPLACED. EXTERNAL DOUBLERS WERE FABRICATED AND INSTALLED IAW EC 5310-01233 AND BAC DRAWING 65-45829. (M) 2 L 7 2 4F A16WE 1996031500585 19960315 00585 EU 1996 3 15 COEA9670101 1 19960130 A 3250 SEALS DUNLOP FOKKER F27 F27MK600 4990706 EU NLG STEERING LEAKING A COEA C D ABORTED TAKEOFF RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 NM 01 701FE 10419 DURING TAKEOFF ROLL OF FLGHT 7826 FROM RAPID CITY, NORTH DAKOTA, THE NOSE WHEEL CENTERING FAIL LIGHT ILLUMINATED AND CRE W ELECTED TO ABORT. AIRCRAFT RETURNED TO RAMP WITHOUT INCIDENT. INSPECTION REVEALED THAT THE SEALS ON THE LEFT SIDE OF THE STEERING MOTOR WERE LEAKING FLUID. MAINTENANCE REPLACED THE NOSE WHEEL STEERING MOTOR AND SEALS. SYSTEM OPERATION AND LEAK CHECKED GOOD. (M) 2 H 7 2 4T A817 1996031500586 19960315 00586 EA 1996 3 15 GLBA96002 2 19960110 A 7310 3032791 FUEL TUBE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA LT ENGINE CHAFED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 60UE 17611 UC60 PIR - AFTER TAKEOFF, THE CREW OBSERVED A TORQUE DROP TO 1300 LBS. THE CREW ELECTED AND AIR TURN BACK AND COMPLETED AN U NEVENTFUL LANDING. MAINTENANCE FOUND A CHAFED FUEL TUBE AT THE LEFT FUEL CONTROL UNIT. THE TUBE WAS REPLACED AND LEAK CHECKED. (M) 2 L 7 2 4T 4 T RT A24CE E4EA 1996031500587 19960315 00587 WP 1996 3 15 GRAA9608 1 19960215 A 2460 MP1501B0C8 CIRCUIT BREAKER DOUG DC9 DC987 3022087 WP COCKPIT FAILED A GRAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 WP 11 1074T 49727 AT RNO - AIRCRAFT BLOCKED OUT OF GATE B-10. AIRCRAFT HAD THE DC BUS OFF LIGHT ILLUMINATE ON TAXI OUT. AIRCRAFT TAXIED TO THE NORTH RAMP WITHOUT FURTHER OCCURENCE. MAINTENANCE RECYCLED THE DC BUS SYSTEM CIRCUIT BREAKERS. OPERATIONAL CHEC K OF THE DC BUS SYSTEM CHECKED NORMAL. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A6WE 1996031500588 19960315 00588 1996 3 15 GRAA9609 4 19960215 A 3425 4608000806 AHRS DOUG DC9 DC987 3022087 WP E/E BAY FAILED A GRAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 11 1074T 49727 EN ROUTE BLI-IAS AIRCRAFT DIVERTED INTO RNO DUE TO NR 2 AHRS FAILED, NR 2 VERTICAL GYRO FAILED, AND NR 1 FLIGHT MANAGEME NT ANNUNCIATOR AND FLIGHT DIRECTOR FAILED. MAINTENANCE REMOVED AND REPLACED THE NR 2 AHRS UNIT. OPERATIONAL TEST OF TH E NAVIGATION SYSTEM CHECKED NORMAL, NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A6WE 1996031500589 19960315 00589 EU 1996 3 15 RAIA960144 1 19960125 A 7334 1103P0645 SWITCH BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 973JX 10360 973 SMF - FLT NR 4718 - DURING TAKEOFF ROLL LEFT LOW FUEL PRESSURE CAPTION ILLUMINATED, TAKEOFF WAS ABORTED. MAINTENANCE DE FERRED THE LEFT LOW PRESSURE CAPTION PER MEL 73-2. MAINTENANCE CLEARED MEL ON 1-29-96. REMOVED AND REPLACED LEFT FUEL PRESSURE SWITCH, OPS CHECK GOOD. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996031500590 19960315 00590 WP 1996 3 15 RRXA9600007 1 19960213 A 2612 CONNECTOR PIN DOUG DC8 DC871 302199A WP NR 2 FIRE DET PUSHED BACK A RRXA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 WP 15 8079U 45947 FLT EB329 - KDAY-KICT - IN FLIGHT NR 2 ENGINE FIRE WARNING SOUNDED. DISCHARGED 1 BOTTLE AND WARNING STOPPED. APPROXIMA TELY 5 MINUTES LATER FIRE WARNING SOUNDED AGAIN, DISCHARGED 2ND BOTTLE FIRE WARNING REMAINED ON. NR 2 ENGINE SHUT DOWN. MAINTENANCE FOUND PIN NR F PUSHED BACK ON FIRE DETECTION AMP. RESEATED PIN, NR 2 ENGINE FIRE DETECTION SYSTEM CHECKS GOOD ON GROUND RUN. (M) 2 L 7 4 4F 4A25 1996031500591 19960315 00591 NE 1996 3 15 SRAA19601 2 19960129 A 7310 FILTERS BOEING 747 747212B 1384886 NM PWA JT9 JT9D7A 52054 NE FUEL SYSTEM DIRTY A SRAA K NONE J WARNING INDICATION CR CRUISE 1 SO 19 745SJ 20888 FLT 6216 - LOS-JNB - DURING FLIGHT ALL FOUR ENGINE ICING LIGHTS ILLUMINATED AND WOULD NOT EXTINGUISH WITH FUEL HEAT ON. CONTINUED FLIGHT TO JNB AND LANDED WITHOUT INCIDENTS. INITIAL INSPECTION OF ENGINE FUEL FILTERS SHOW EVIDENCE OF RUST COLORED DEPOSITS. DRAINED AND SUMPED FUEL FROM ALL TANKS, ENTERED TANKS AND CHECKED FOR COMTAMINATION, NONE FOUND. REP LACED FINE AND COARSE FILTERS AT ALL FCU'S MAIN FUEL FILTERS, APU FUEL FILTER, PERFORMED ENGINE RUN ALL ENGINES PERFORME D SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 4 4F 4 F A20WE E20EA 1996031500592 19960315 00592 NE 1996 3 15 TWRA9607 2 19960203 A 7230 SCAVENGE LINE BOEING 747 747238B 1384828 NM PWA JT9 JT9D7F 52054 NE NR BRG COMPT CLOGGED A TWRA A E UNSCHED LANDING ENGINE SHUTDOWN K FLUID LOSS CL CLIMB 1 EA 15 614FF 20534 663041 FLT 60 - DURING CLIMB-OUT FROM GRU, FLIGHT CREW AGAIN SHUT NR 3 ENGINE DOWN DUE TO LOW OIL PRESSURE AND LOSS OF OIL QUAN TITY. SAME ITEM AS PREVIOUSLY REPORTED. AIRCRAFT RETURNED ONCE AGAIN TO GRU. THE FLIGHT WAS CANCELLED AND THE ENGINE WAS PREPARED FOR 3 ENGINE FERRY TO SJU THEN TO JFK. UPON ARRIVAL AT JFK, AFTER FURTHER INVESTIGATION THE NR 3 ENGINE WA S REPLACED DUE TO SUSPECTED NR 3 BRG COMPT SCAVENGE CLOG ENG RUNUP PERFORMED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 4 4F 4 F A20WE E20EA 1996031500593 19960315 00593 NM 1996 3 15 USAA960207 1 19960207 A 5320 65C105924 ANGLE BOEING 737 7372B7 1384560 NM BS 967-947 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 35486 22886 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 20 INCH BY 1 INCH CORROSION FLOOR SUPPORT ANGLE, STATION 967 TO STATION 947 RBL 45, REPAIRED PER SRM 51-10-1. REPLACED WITH IDENTICAL PART NR 65C10592-4. CORROSION TASK NR C53-107-02, CORROS ION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996031500594 19960315 00594 NM 1996 3 15 USAA960208 1 19960207 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 328 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 35486 22886 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 6 INCH BY 2 INCH CORRODED FLOOR BEAM AREA AND AT ALL CLIPNUT HOLES BS 32 8 RBL 6 TO RBL 56. INSTALLED NEW T-CAP AND DOUBLERS, REPAIRED PER TR 53-10-13. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996031500595 19960315 00595 NM 1996 3 15 USAA960209 1 19960207 A 5320 ANGLE BOEING 737 7372B7 1384560 NM BS 695 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 35486 22886 INT - DURING Q-6 CHECK VISUAL EDDY CURRENT INSPECTION, FOUND 1 INCH CRACK IN FORWARD INBOARD CHORD ANGLE BS 695 FITTING, WL 202, JUST ABOVE STRINGER 18A LEFT. INSTALLED PERMANENT ANGLE REPAIR, LESS THAN 1 LB, REPAIRED PER EA 40644. (M) 2 L 7 2 4F A16WE 1996031500596 19960315 00596 NM 1996 3 15 USAA960210 1 19960207 A 5320 65C105925 ANGLE BOEING 737 7372B7 1384560 NM BS 957 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 35486 22886 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 11 INCH BY 40 INCH CORROSION FLOOR SUPPORT ANGLE AT STATION 957 RBL 6 TO RBL 45. REPAIRED PER SRM 51-10-1. REPLACED WITH IDENTICAL PART NR 65-C10592-5 OR 6. CORROSION TASK NR C53-107-02, COR ROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996031500597 19960315 00597 NM 1996 3 15 USAA960211 1 19960207 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 967 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 35486 22886 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 45 INCH CORROSION FLOOR BEAM STATION 967 BL 0 TO LBL 45. INST ALLED ONE DUOBLER AT LBL 42, REPAIRED PER TR 53-10-01A. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996031500598 19960315 00598 NM 1996 3 15 USAA960213 1 19960207 A 5320 6546812198 ANGLE BOEING 737 7372B7 1384560 NM BS 986.5-967 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 35486 22886 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 20 INCH CORRODED FLOOR SUPPORT ANGLE STATION 986.5 TO 967 LBL 12. REPLACED ANGLE, REPAIRED PER SRM 51-10-1. CORROSION TASK NR 53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996031500599 19960315 00599 NM 1996 3 15 USAA960216 1 19960207 A 5311 FRAME BOEING 737 7372B7 1384560 NM BS 807 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 35486 22886 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK TOP FLANGE OF FRAME STATION 807 LEFT BETWEEN STRINGER 24 A ND STRINGER 25. CUT OUT CRACK, FABRICATED FILLER AND REPAIRED DOUBLER PER SRM 51-40-3. (M) 2 L 7 2 4F A16WE 1996031500600 19960315 00600 NM 1996 3 15 USAA960217 1 19960207 A 5312 BLKHD FITTING BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 35486 22886 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK STATION 727 BULKHEAD STIFFENER FITTING AT BL 0 WL 202.5. R EMOVED CRACKED FITTING, INSTALLED NEW ONE, REPAIRED PER EO 5394G176. (M) 2 L 7 2 4F A16WE 1996031500601 19960315 00601 NM 1996 3 15 USAA960218 1 19960207 A 5320 1137215 INTERCOSTAL BOEING 737 7372B7 1384560 NM BS 312-328 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 35486 22886 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND FOUR 1 INCH BY 1 INCH CORRODED AREAS AT CLIP NUT HOLES BS 312 TO BS 328 RBL 11 INTERCOSTAL. REMOVED AND INSTALLED NEW INTERCOSTAL, REPAIRED PER SRM 51-10-1 PAGE 5. CORROSION TASK NR C53-107- 02, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996031500602 19960315 00602 NM 1996 3 15 USAA960219 1 19960207 A 5320 ANGLE BOEING 737 7372B7 1384560 NM BS 306-345 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 35486 22886 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 6 CORRODED AREAS AT CLIP NUT HOLES APPROXIMATELY 1 INCH BY 1 INCH BS 306 TO BS 345 LBL 48 'A' ANGLE LEFT ENTRANCE DOOR. REMOVED AND INSTALLED NEW PART, REPAIRED PER SRM 51-10-1 PAGE 5. CORRO SION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996031500603 19960315 00603 NM 1996 3 15 USAA960220 1 19960207 A 5320 654587545 ANGLE BOEING 737 7372B7 1384560 NM BS 294.5-344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 35486 22886 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY 1 INCH CORRODED AREAS AT CLIP NUT HOLES 'Z' ANGLE BS 2 94.5 TO BS 344 RBL 56. REPAIRED PER SRM 51-10-1 AND BOEING DRAWING 65-45875. CORROSION TASK NR C53-107-02, CORROSION L EVEL 2. (M) 2 L 7 2 4F A16WE 1996031500604 19960315 00604 NM 1996 3 15 USAA960221 1 19960207 A 5320 INTERCOSTAL BOEING 737 7372B7 1384560 NM BS 294.5/312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 35486 22886 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 3 CORRODED AREAS APPROXIMATELY 1 INCH BY 1 INCH ON INTERCOSTAL, RBL 10 I NCHES BETWEEN BS 294.5 AND BS 312. REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-1 AND BOEING DRAWING 65-45834. CORROSI ON TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996031500605 19960315 00605 NM 1996 3 15 USAA960222 1 19960207 A 5320 6545834261 INTERCOSTAL BOEING 737 7372B7 1384560 NM BS 292 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 35486 22886 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 1 INCH CORRODED AREA AT INTERCOSTAL BS 292 LBL 12 INCHES. REP LACED INTERCOSTAL, REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996031500606 19960315 00606 NM 1996 3 15 USAA960223 1 19960207 A 5320 6545834258 INTERCOSTAL BOEING 737 7372B7 1384560 NM BS 344-360 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 35486 22886 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORRODED AREA 4 PLACES INTERCOSTAL, BS 344 TO BS 360 RB L 11. REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996031500607 19960315 00607 NM 1996 3 15 USAA960224 1 19960207 A 5320 6545824252 INTERCOSTAL BOEING 737 7372B7 1384560 NM BS 297/303 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 35486 22886 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 CORRODED AREAS APPROXIMATELY 2 INCHES BY 2 INCHES INTERCOSTAL, BS 297 AND BS 303 LBL 12. INSTALLED NEW INTERCOSTAL, REPAIRED PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 1996031500608 19960315 00608 NM 1996 3 15 USAA960225 1 19960207 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 294.5 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 35486 22886 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA FLOOR BEAM 'T' CAP CABIN BS 294.5 LBL 10 INCHES, RBL 20. CUT AND REPLACED T-CAP, LESS THAN 1 LB WEIGHT CHANGE, REPAIRED PER TR 53-10-04B. CORROSION TASK NR C53 -107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996031500609 19960315 00609 NM 1996 3 15 USAA960226 1 19960207 A 5320 1137215 INTERCOSTAL BOEING 737 7372B7 1384560 NM BS 312/328 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 35486 22886 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND THREE CORRODED AREAS, APPROXIMATELY 1 INCH BY 1 INCH AT INTERCOSTAL, RBL 10 INCH BETWEEN BS 312 AND BS 328. REPLACED WITH IDENTICAL PART NR 1137215, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996031500610 19960315 00610 NM 1996 3 15 USAA960227 1 19960207 A 5320 6545834260 INTERCOSTAL BOEING 737 7372B7 1384560 NM BS 312/328 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 35486 22886 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 2 INCH CORRODED AREA INTERCOSTAL LBL 11 INCHES BETWEEN BS 312 AND BS 328. REPLACED WITH IDENTICAL PART NR 65-45834-260, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, COR ROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996031500611 19960315 00611 NM 1996 3 15 USAA960228 1 19960207 A 5320 6545834259 INTERCOSTAL BOEING 737 7372B7 1384560 NM BS 328/344 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 35486 22886 INT - DURING Q-6 CHCK VISUAL INSPECTION, FOUND TWO CORRODED AREAS APPROXIMATELY 1 INCH BY 1 INCH, INTERCOSTAL LBL 10 INC HES BETWEEN BS 328 AND BS 344. REPLACED WITH IDENTICAL PART NR 65-45834-259, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996031500612 19960315 00612 NM 1996 3 15 USAA960229 1 19960207 A 5320 6546812170 INTERCOSTAL BOEING 737 7372B7 1384560 NM BS 1006-986.5 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 35486 22886 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 3 INCH CORROSION INTERCOSTAL STATION 1006 - 986.5 '0' BL. REP LACED WITH INDENTICAL PART NR 65-46812-170, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996031500613 19960315 00613 EU 1996 3 15 USAA960242 1 19960212 A 5311 D31108001 FRAME FOKKER F28 F28MK0100 4990807 EU BS 14911 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 855US 14269 11283 PIT - DURING Q-1 CHECK INSPECTION, FOUND 1 INCH CRACK, FRAME STATION 14911 BL 883 R (HFEC INSPECTION). STOP DRILLED CRA CK AND INSTALLED DOUBLERS PER USAIR EA NR 32077. (M) 2 L 7 2 4F RT 1996031500614 19960315 00614 EU 1996 3 15 USAA960243 1 19960212 A 5730 SKIN FOKKER F28 F28MK0100 4990807 EU WS 2301 DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 855US 14269 11283 PIT - DURING Q-1 CHECK INSPECTION, FOUND FUSELAGE SKIN DELAMINATION RIGHT SIDE STUB WING LAY AREA AT FRAME STATION 23011 . INSTALLED DOUBLER REPAIR PER USAIR EA NR 31894. (M) 2 L 7 2 4F RT 1996031500615 19960315 00615 EU 1996 3 15 USAA960244 1 19960212 A 5730 SKIN FOKKER F28 F28MK0100 4990807 EU WS 2401 DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 855US 14269 11283 PIT - DURING Q-1 CHECK INSPECTION, FOUND FUSELAGE SKIN DELAMINATION LEFT SIDE STUB WING LAY AREA AT FRAME STATION 24011. INSTALLED DOUBLER REPAIR PER USAIR EA NR 31894. (M) 2 L 7 2 4F RT 1996031500616 19960315 00616 NM 1996 3 15 USAA960249 1 19960216 A 5320 INTERCOSTAL BOEING 737 737401 1384701 NM BS 500-520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 19822 23991 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO 2 INCH CRACKS AT NUT PLATE HOLES BS 500 G TO BS 520 BL 0 INTERCOSTAL . REPAIRED PER S/B 737-53-1120 AND EA 40888. (M) 2 L 7 2 4F RT A16WE 1996031500617 19960315 00617 NM 1996 3 15 USAA960250 1 19960216 A 5512 SKIN BOEING 737 737401 1384701 NM BS 184.6-193.9 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 19822 23991 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND FIVE 1 INCH BY 1 INCH BY .050 INCH DENTS, RIGHT HORIZONTAL STABILIZER LO WER INTERSPAR SKIN STABILIZER STATION 184.7 TO 193.9 AT MID CHORD. CUT OUT DAMAGE PLUS INSTALLED DOUBLER PER SRM 55-10- 01 FIG 206. (M) 2 L 7 2 4F RT A16WE 1996031500618 19960315 00618 NM 1996 3 15 USAA960251 1 19960216 A 5315 FLOOR BEAM BOEING 737 737401 1384701 NM BS 794 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 19822 23991 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 4 INCH CORRODED AREA AND SEVERAL 1 INCH BY 1 INCH AREAS AT BS 794 RBL 14 INCHES CARGO FLOOR BEAM. CUT OUT CORRODED SECTION (BS 779-877) FABRICATED AND INSTALLED NEW BEAM SECTION PER BOEING DRAWING 65-53844 AND SRM 53-00-53 FIG 202. CORROSION TASK NR C53-108-01, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996031500619 19960315 00619 NM 1996 3 15 USAA960252 1 19960216 A 5315 FLOOR BEAM BOEING 737 737401 1384701 NM BS 312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 19822 23991 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 5 INCHES OF SCRATCHES AND CORROSION ON FLOOR BEAM BS 312 LBL 15 TO 20. S PLICED 'T' SECTION PER TR 53-10-03. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996031500620 19960315 00620 NM 1996 3 15 USAA960253 1 19960216 A 5320 FITTING BOEING 737 737401 1384701 NM BS 521 GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 23991 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO .25 INCH GOUGES LBL 45 SEAT TRACK SUPPORT CHANNEL FITTING STATION 52 1, WL 207. REPAIRED PER EA 40888 STEP 3. (M) 2 L 7 2 4F RT A16WE 1996031500621 19960315 00621 NM 1996 3 15 USAA960254 1 19960216 A 5315 FLOOR BEAM BOEING 737 737401 1384701 NM BS 947 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 19822 23991 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 4 INCH BY .5 INCH CORRODED FLOOR BEAM BS 947 LBL 5 AND RBL 6, LBL 16. I NSTALLED T-CAP PER EA 40816. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996031500622 19960315 00622 NM 1996 3 15 USAA960255 1 19960216 A 5320 FITTING BOEING 737 737401 1384701 NM BS 521 GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 19822 23991 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO .25 INCH GOUGES SEAT TRACK SUPPORT CHANNEL FITTING STATION 521, LBL 25, WL 207. REPAIRED PER EA 40888 STEP 3. (M) 2 L 7 2 4F RT A16WE 1996031500623 19960315 00623 NM 1996 3 15 USAA960256 1 19960216 A 5320 CHANNEL BOEING 737 737401 1384701 NM BS 521 GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 19822 23991 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO .25 INCH GOUGES SEAT TRACK SUPPORT CHANNEL FITTINGS STATION 521, BL 0 WL 207. REPAIRED PER EA 40888 STEP 3. (M) 2 L 7 2 4F RT A16WE 1996031500624 19960315 00624 NM 1996 3 15 USAA960257 1 19960216 A 5320 FITTINGS BOEING 737 737401 1384701 NM BS 521 GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 19822 23991 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO .25 INCH GOUGES SEAT TRACK SUPPORT CHANNEL FITTING STATION 521, RBL 25, WL 207. REPAIRED PER EA 40888 STEP 3. (M) 2 L 7 2 4F RT A16WE 1996031500625 19960315 00625 NM 1996 3 15 USAA960258 1 19960216 A 5315 FLOOR BEAM BOEING 737 737401 1384701 NM BS 294 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 19822 23991 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 BY 32 INCH CORROSION FLOOR BEAM BS 294 RBL 7 - RBL 60. INSTALLED T-C AP AND REPAIRED ANGLES PER SRM 53-10-51. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996031500626 19960315 00626 NM 1996 3 15 USAA960259 1 19960216 A 5315 FLOOR BEAM BOEING 737 737401 1384701 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 19822 23991 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK IN RADIUS BS 520 RBL 45 INCHES INBOARD SIDE OF SEAT TRACK F LOOR BEAM. REPAIRED PER EA 40888 STEPS 1 AND 2. (M) 2 L 7 2 4F RT A16WE 1996031500627 19960315 00627 EU 1996 3 15 USAAF96022 1 19960213 A 2740 2310011SB2719 STAB CONTRL UNIT FOKKER F28 F28MK0100 4990807 EU VERT STAB FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 855US 14278 11283 PIT - FL 862 - CREW RECEIVED HYDRAULIC STAB CHANNEL 2 FAULT. AFTER PERFORMING APPLICABLE PROCEDURE, RECEIVED CHANNEL 1 FAULT ALSO. MAINTENANCE REPLACED THE HORIZONTAL STABILIZER ACTUATOR AND THE STABILIZER SERVOS. (M) 2 L 7 2 4F RT 1996031500628 19960315 00628 NM 1996 3 15 USAASB96010 1 19960118 A 3260 106122619 SENSOR BOEING 737 7373B7 1384580 NM NOSE GEAR FAILED A USAA O OTHER N FALSE WARNING LD LANDING 1 EA 19 510AU 23385 FLT NR 7015 - PIT - AFTER EXTENSION, RED NOSE GEAR LIGHT FAILED TO EXTINGUISH. MAINTENANCE REPLACED THE NOSE GEAR LOCK SENSOR. INDICATIONS NORMAL. (M) 2 L 7 2 4F RT A16WE 1996031500629 19960315 00629 NM 1996 3 15 USAASB96022 1 19960129 A 3260 189915 PROX SW BOEING 737 7373B7 1384580 NM NLG FAILED A USAA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 EA 19 376US 22955 FLT NR 1215 - PIT - RED NOSE GEAR LIGHT ON TAKEOFF WHEN HANDLE IN UP AND OFF POSITION. RECYCLED GEAR THREE GREEN LIGHTS , RED REMAINED ON. MAINTENANCE REPLACED NOSE GEAR LOCK SENSOR. SWUNG GEAR, OPS CHECK OK. (M) 2 L 7 2 4F RT A16WE 1996031500630 19960315 00630 NM 1996 3 15 USAASB96023 1 19960130 A 3397 WIRE BOEING 737 7373B7 1384580 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 373US 22952 FLT NR 592 - BWI - MAINTENANCE FOUND AISLE EMERGENCY LIGHT AT 7D INOP. MAINTENANCE REPAIRED BROKEN WIRE AT 7D. OPS CHE CK SATISFACTORY. (M) 2 L 7 2 4F RT A16WE 1996031500631 19960315 00631 NM 1996 3 15 USAASB96030 1 19960212 A 2613 OVERHEAT DET BOEING 737 737201 1384454 NM RT WING MALFUNCTIONED A USAA A UNSCHED LANDING M OVER TEMP CR CRUISE 1 EA 19 262AU 22868 FLT 771 - PIT - DIVERTED TO PIT DUE TO RIGHT WING AND BODY OVERHEAT. RIGHT WING BODY OVERHEAT LIGHT ILLUMINATED IN FLIG HT. WENT OUT SHORTLY AFTER RIGHT ENGINE BLEED VALVE WAS CLOSED ACCORDING TO FLIGHT MANUAL PROCEDURE. MAINTENANCE CHECK ED WIRING RESISTANCE PER MM, CHECKS OK. PRESSURIZED, NO LEAKS FOUND. REPLACED OVERHEAT DETECTOR PRECAUTIONARY, CHECKS OK. (M) 2 L 7 2 4F A16WE 1996031500635 19960315 00635 NE 1996 3 15 96ZZZX1086 2 19960202 A 8530 48183 PUSHROD 114649 DOUG DC3 DC3C 3021457 WP PWA R1830 R183090D 52020 NE NR 6 CYL EXHAUST BROKEN A VLLA O OTHER E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 GL 05 9923S 232 25964 CP351777 ENGINE STARTED RUNNING ROUGH. FOUND NR 6 CYLINDER EXHAUST PUSHROD BROKEN IN TWO. THIS CAUSED EXHAUST VALVE IN NR 6 CYL INDER NOT TO OPEN. 2 L 7 2 4R 4 R A669 5E4 1996031500649 19960315 00649 CE 1996 3 15 96ZZZX1100 1 19960220 A 2820 S22184 CHECK VALVE CESSNA 402 402B 207590P CE LT AUX FUEL STUCK A OEZA K NONE O OTHER IN INSP/MAINT 1 WP 19 767EA 7017 402B1244 PILOT REPORTED THE LAST 10 GALLONS OF FUEL WAS NOT BEING SUCKED UP BY THE ENGINE DRIVEN FUEL PUMP. MAINTENANCE FOUND VE NT CHECK VALVE WAS STUCK OPEN. REPLACEMENT OF VALVE CURED THE PROBLEM. 1 L 7 2 3O A7CE 1996031500653 19960315 00653 SO 1996 3 15 96ZZZX1104 1 19960205 A 7922 SL53E19600 VERNATHERM PIPER PA31 PA31350 7103110 SO ENGINE OIL FAILED A LVAA K NONE O OTHER IN INSP/MAINT 1 WP 19 27196 694 317752095 VERNATHERM BROKE AT ROLL PIN HOLE. ALL PARTS RECOVERED. TOTAL TIME ON VERNATHERM 693.7 HOURS SINCE NEW. 1 L 7 2 3O A20SO 1996031500657 19960315 00657 1996 3 15 96ZZZX1108 4 19960115 A 6122 G210659 GOVERNOR WOODWARD BNORM BN2 BN2A3 1520215 EU RT PROP SHAFT BROKE A VLIA O OTHER Y ENGINE STOPPAGE CR CRUISE 1 SO 21 906GD 2700 504 1444822K 1060 DURING CRUISE FLIGHT, RIGHT ENGINE QUIT AND PROPELLER FEATHERED. RIGHT GOVERNOR REMOVED AND FOUND BROKEN SHAFT. GOVERN OR REPLACED AND AIRCRAFT RETURNED TO SERVICE. 1 H 7 2 3O A17EU 1996031500677 19960315 00677 WP 1996 3 15 9605989610 1 19960313 A 3350 RELAY DOUG DC9 DC932 3022066 WP LT/RT NACELLE MALFUNCTIONED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 610NW 47432 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT AND RIGHT NACELLE EMERGENCY LIGHTS INOPERATIVE. REPLACED RELAY R2-213, O PERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996031500678 19960315 00678 WP 1996 3 15 9605999855 1 19960313 A 3231 NW29568461 CONTROL CABLE DOUG DC9 DC951 3022051 WP RT NLG DOOR BROKEN A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 764NC 47717 DURING CLIMBOUT, EXPERIENCED A LOUD NOISE AND VIBRATION ON NOSE GEAR AT GEAR RETRACTION. RETURNED TO TPA AND LANDED WIT HOUT INCIDENT. FOUND RIGHT NOSE GEAR DOOR STOP UPPER CABLE BROKEN. REMOVED BROKEN HARDWARE AND DOOR OPERATION CHECKED GOOD. 2 L 7 2 4F RT A6WE 1996031500679 19960315 00679 NE 1996 3 15 9606006612 2 19960216 A 7320 ENGINE BOEING 747 747251B 1384892 NM PWA JT9 JT9D7F 52054 NE NR 4 OUT OF RIG A NWAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS LD LANDING 1 GL 01 612US 20357 62706 DURING LANDING ROLLOUT, THE NR 4 ENGINE STALLED IN REVERSE. THE ENGINE WAS SHUTDOWN WHILE STILL IN REVERSE AND WITH EGT CLIMBING THROUGH 750 DEGREES. PERFORMED STATIC BLEED CHECK, CHECKED RABS, RAN ENGINE IN REVERSE AND ALL CHECKS WERE NO RMAL. FOUND NR 1 ENGINE WAS OUT OF RIG. RIGGED NR 1 ENGINE, PERFORMED RUNUP, RETRIMMED NR 1 ENGINE AND TEST WAS NORMAL . 2 L 7 4 4F 4 F A20WE E20EA 1996031500680 19960315 00680 WP 1996 3 15 9606019978 1 19960312 A 3350 60030451 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9342 47391 DURING PREFLIGHT CHECK, FOUND FORWARD OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS AND OPERATIONAL CHE CK NORMAL. 2 L 7 2 4F A6WE 1996031500681 19960315 00681 NM 1996 3 15 9606022714 1 19960313 A 3234 GEAR HANDLE BOEING 727 7272S7 138407Z NM FLIGHT DECK LACK OF LUBE A NWAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 01 718RC 22344 DURING GEAR EXTENSION, GEAR UNSAFE WAS INDICATED ON ALL THREE GEARS. ON SECOND GEAR RECYCLE ALL INDICATIONS WERE NORMAL . AIRCRAFT LANDED WITHOUT INCIDENT. CLEANED AND LUBRICATED GEAR HANDLE, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996031500682 19960315 00682 NM 1996 3 15 9606032203 1 19960312 A 3150 WARNING HORN BOEING 727 727251 138408H NM SPEED BRAKE SOUNDED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 203US 22543 DURING TAKEOFF ROLL, SPEED BRAKE DEPLOYED AND WARNING HORN SOUNDED. TAKEOFF WAS ABORTED WITHOUT INCIDENT. INSPECTED SW ITCHES AND OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996031500683 19960315 00683 WP 1996 3 15 9606049930 1 19960312 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 89S 47042 DURING LINE MAINTENANCE INSPECTION, FOUND AFT OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES AND OPERAT IONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996031500684 19960315 00684 WP 1996 3 15 9606059930 1 19960311 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP EMERGENCY EXIT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 89S 47042 DURING LINE MAINTENANCE INSPECTION, FOUND MID CABIN OVERHEAD EMERGENCY EXIT LIGHTS DIM. REPLACED BATTERIES AND OPERATIO NAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996031500685 19960315 00685 NM 1996 3 15 96DHL70901A 1 19960302 A 5330 SKIN BOEING 727 72782C 1384026 NM FS 1390 BULGED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 DURING A11 CHECK, FUSELAGE SKIN BULGED UNDER RAIN GUTTER FS 1390 APPROXIMATELY JUST ABOVE NR 2 ENGINE LEFT FORWARD COWL. REMOVED FASTENERS, CUTOUT DAMAGED AREA, FABRICATED REPAIR PARTS 3.5 INCHES BY 5 INCHES. INSTALLED DOUBLER 8.5 INCHES BY 9.5 INCHES PER SRM 53-30-3. REINSTALLED RAIN GUTTER PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996031500686 19960315 00686 WP 1996 3 15 96FDEA00520 1 19960313 A 2750 BOLT DOUG DC10 DC1010 3022110 WP RT TE FLAP SHEARED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 052FE 97806 SNRM 6021, RIGHT O/B FLAP I/B HINGE ATTACH FITTING TO FLAP O/B LOWER .5625 BOLT SHEARED, AS SEEN IN AREA OF 635 ACCESS P ANEL. INSTALLED NEW RIGHT O/B FLAP BOLT PER GMM 57-52-04. 2 L 7 3 4F A22WE 1996031500687 19960315 00687 NM 1996 3 15 96UAL900187 1 19960313 A 3244 40X14 TIRE BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE RT MLG SEPARATED A UALA K NONE O OTHER LD LANDING 1 WP 29 9066U 19947 RIGHT OUTBOARD MAIN TIRE SEPARATED AND DAMAGED THE FLAP AND NUMBER ONE SPOILER. *S/D* REPLACED NUMBER THREE AND FOUR M AIN TIRE. REPAIRED FLAP AND SPOILER. TIRE CAP COMPLETELY GONE. 2 L 7 2 4F 4 F A16WE E2EA 1996031500688 19960315 00688 NM 1996 3 15 96UAL900188 1 19960313 A 2410 BACH5R0116DUF CSD HOSE BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE ENGINE LEAKING A UALA C D ABORTED TAKEOFF RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 WP 29 9007U 19045 ABORTED TAKEOFF DUE TO LOW OIL PRESSURE LIGHT CAME ON AT 90 KNOTS. SUPPLEMENTAL DATA UPDATE: CONSTANT SPEED DRIVE OIL SERVICE LINE WAS LEAKING. REPLACED TWO SHORT HOSES ON THE ELBOW FITTING AND ASSOCIATED "O" RINGS. CHECKS O.K. 2 L 7 2 4F 4 F A16WE E2EA 1996031500689 19960315 00689 NM 1996 3 15 96UAL900189 1 19960313 A 3350 STRIP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 661UA 27158 AFT CROSS AISLE EMERGENCY ESCAPE PATH LIGHTING INOP. REPLACED LIGHT STRIP AND CHECKS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 1996031500690 19960315 00690 WP 1996 3 15 ABXA9600272 1 19960312 A 3231 RETRACT MECH DOUG DC8 DC862 3021970 WP RT MLG DOOR MALFUNCTIONED A ABXA K NONE J WARNING INDICATION CL CLIMB 1 GL 23 804AX 45987 LANDING GEAR UNSAFE LIGHT ILLUMINATED WHEN LANDING GEAR RETRACTED DURING CLIMBOUT. INDICATION CONFIRMED THAT THE RIGHT MAIN LANDING GEAR DOOR WAS NOT LATCHED. RECYCLED LANDING GEAR TWICE WITHOUT CHANGE. CHECKED WIRING FROM RIGHT PROXIMIT Y SWITCH TO PROXIMITY BOX AND WIRING CHECKED GOOD. COMPLETED MAB DC832-6 AND INDICATIONS CHECKED GOOD. 2 L 7 4 4F 4A25 1996031500691 19960315 00691 1996 3 15 COMA9610102 2 19960312 A 7320 CIRCUIT BREAKER EMB 120 EMB120RT SO FLIGHT IDLE TRIPPED A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 164D 120164 FLIGHT IDLE STOP SOLENOID CIRCUIT BREAKER IS TRIPPED. RESET BREAKER, SYSTEM TEST NORMAL. 2 L 7 2 4T RT A31SO 1996031500692 19960315 00692 SO 1996 3 15 COMA9610103 1 19960311 A 7710 DOOR LATCH EMB 120 EMB120RT SO ENGINE COWL BROKEN A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 200CD 120200 OIL INSPECTION DOOR ON ENGINE COWLING WILL NOT STAY CLOSED. REPAIRED BROKEN SHEET METAL LATCH RETAINER. 2 L 7 2 4T RT A31SO 1996031500693 19960315 00693 EU 1996 3 15 COMA9630063 1 19960312 A 3350 6104781 BATTERY SAAB SF340 SF340A 7850100 EU CABIN DISCHARGED A COMA K NONE L NO TEST UK UNKNOWN 1 SO 01 380CA 340A012 EMERGENCY LIGHTING BATTERIES ARE DISCHARGED. REPLACED EMERGENCY LIGHTS BATTERY. 2 L 7 2 4T RT A52EU 1996031500694 19960315 00694 EU 1996 3 15 COMA9630064 1 19960312 A 3350 MS1557081 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A COMA K NONE L NO TEST UK UNKNOWN 1 SO 01 140N 340A140 CABIN DOOR EMERGENCY LIGHT IS INOP. REPLACED BULB IN EMERGENCY LIGHT. 2 L 7 2 4T RT A52EU 1996031500695 19960315 00695 EU 1996 3 15 COMA9630065 1 19960311 A 2711 MS276456A BEARING SAAB SF340 SF340A 7850100 EU AILERON TRIM WORN A COMA K NONE E VIBRATION/BUFFET AP APPROACH 1 SO 01 344CA 340A025 WHEN FLAPS ARE SET TO 15 DEGREES THERE IS A FLUTTER FELT IN THE CONTROL YOKE. REPLACED WORN BEARINGS AT AILERON TRIM TA BS. 2 L 7 2 4T RT A52EU 1996031500696 19960315 00696 EU 1996 3 15 COMA9630066 1 19960310 A 3150 004WS00 WEU SAAB SF340 SF340A 7850100 EU AVIONICS MALFUNCTIONED A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 357CA 19989 340A044 LEFT AIR VALVE LIGHT STAYS ON WITH SWITCH IN OFF POSITION. REPLACED THE WARNING ELECTRONIC UNIT. 2 L 7 2 4T RT A52EU 1996031500697 19960315 00697 EU 1996 3 15 COMA9630067 1 19960310 A 2750 HP14161005 CONTROL VALVE SAAB SF340 SF340A 7850100 EU TE FLAPS FAILED A COMA O OTHER J WARNING INDICATION UK UNKNOWN 1 SO 01 342CA 340A023 FLAPS FAIL WARNING ON, FLAPS DO NOT RESPOND TO SELECTED COMMANDS. REPLACED THE FLAP CONTROL VALVE. 2 L 7 2 4T RT A52EU 1996031500698 19960315 00698 EA 1996 3 15 COMA9660040 1 19960310 A 3411 PITOT SYS CNDAIR CL600 CL6002B19 EA NR 1 WATER CONTAM A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 937CA 7044 ADC NR 1 IS NOT FUNCTIONING PROPERLY. DRAINED WATER FROM NR 1 PITOT SYSTEM. 2 L 7 2 4F RT A21EA 1996031500699 19960315 00699 EA 1996 3 15 COMA9660041 1 19960311 A 2130 21197644 PRESS SELECT PNL CNDAIR CL600 CL6002B19 EA COCKPIT MALFUNCTION A COMA K NONE O OTHER CL CLIMB 1 SO 01 927CA 5140 844 7031 CABIN PRESSURE CLIMBS AT 2,000 RPM AFTER TAKEOFF AND DESENDS BELOW FIELD ELEVATION DURING DESENT. REPLACED THE PRESSURE SELECT PANEL. 2 L 7 2 4F RT A21EA 1996031500700 19960315 00700 EA 1996 3 15 COMA9660042 1 19960312 A 2742 83963 ACTUATOR CNDAIR CL600 CL6002B19 EA HORZ STAB FAILED A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 931CA 3620 1199 7037 STABILIZER TRIM CHANNEL ONE IS INOP. REPLACED THE STABILIZER TRIM ACTUATOR. 2 L 7 2 4F RT A21EA 1996031500701 19960315 00701 1996 3 15 COMA9660043 4 19960312 A 3410 6229819004 AIR DATA PANEL CNDAIR CL600 CL6002B19 EA AVIONICS MALFUNCTION A COMA K NONE O OTHER CR CRUISE 1 SO 01 926CA 6457 4615 7027 NR 2 ALTIMETER BARROMETRIC SETTING CHANGES WITH POWER CHANGES. REPLACED THE AIR DATA PANEL. 2 L 7 2 4F RT A21EA 1996031500702 19960315 00702 1996 3 15 COMA9660044 4 19960313 A 3410 6229819004 AIR DATA PANEL CNDAIR CL600 CL6002B19 EA AVIONICS MALFUNCTION A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 932CA 7038 PILOTS ALTIMETER SETTING JUMPS EVERY 2 MINUTES. REPLACED THE AIR DATA PANEL. 2 L 7 2 4F RT A21EA 1996031500703 19960315 00703 EA 1996 3 15 COMA9660045 1 19960313 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA LT TE FLAP FAILED A COMA K NONE O OTHER CR CRUISE 1 SO 01 915CA 3084 41 7013 FLAPS FAIL MESSAGE ON EICAS. REPLACED THE LT FLAP BRAKE AND POSITION SENSOR. 2 L 7 2 4F RT A21EA 1996031500704 19960315 00704 NM 1996 3 15 DL72K960561 1 19960312 A 3350 1000677 BATTERY BOEING 727 727232 1384082 NM R1 DOOR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 414DA 21256 ON PREFLIGHT, R-1 DOOR EMERGENCY LIGHT INOP. REPLACED BATTERY PACK AND OPERATION NORMAL. 2 L 7 3 4F A3WE 1996031500705 19960315 00705 NM 1996 3 15 DL72S960546 1 19960311 A 5530 FORMER BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 470DA 20747 FOUND DURING C-2 LETTER CHECK, 1.25 INCH CRACK VERT STAB FORMER AT STRINGER ATTACH POINT, FIN STATION 110.4 AND STR 9 L EFT. REPAIRED PER M/M 55-30-3 PG 802. 2 L 7 3 4F A3WE 1996031500706 19960315 00706 NM 1996 3 15 DL72S960548 1 19960311 A 5320 WEB BOEING 727 727232 1384082 NM BS 870 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 470DA 20747 VISIBLE CRACK IN STA 870 BULKHEAD WEB BELOW LOAD CONTROL VALVE BOX INSIDE PANEL 3455R. CRACK MEASURES 3 INCHES LONG ON AFT SIDE OF WEB FROM LOAD CONTROL VALVE BOX CUTOUT, EXTENDING DOWN AND OUTBOARD. REPAIRED PER SRM 53-10-9 FIG 13. 2 L 7 3 4F A3WE 1996031500707 19960315 00707 NM 1996 3 15 DL72S960551 1 19960220 A 5754 651622199 SKIN BOEING 727 727232 1384082 NM NR 4 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 478DA 20755 DURING INSPECTION, NR 4 L/E SLAT UPPER SKIN WAS FOUND CRACKED SEVERAL PLACES UNDER THE WING FENCE. REPAIRED SKIN PER MM 57-54-0. 2 L 7 3 4F A3WE 1996031500708 19960315 00708 NM 1996 3 15 DL72S960552 1 19960220 A 5754 651622199 RIB BOEING 727 727232 1384082 NM NR 4 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 478DA 20755 DURING INSPECTION, NR 4 L/E SLAT INTERNAL SUPPORT RIB NR 5 AND NR 17 WERE FOUND CRACKED. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1996031500709 19960315 00709 NM 1996 3 15 DL72S960553 1 19960229 A 5754 651622296 RIB BOEING 727 727232 1384082 NM NR 6 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 419DA 21272 THE O/B ACTUATOR RIB WAS FOUND TO BE CRACKED IN 2 PLACES. REPAIRED PER M/M 57-54-0 FIGS 804 AND 814, FOR NR 6 L/E SLAT PANEL. 2 L 7 3 4F A3WE 1996031500710 19960315 00710 NM 1996 3 15 DL72S960554 1 19960229 A 5754 651622296 RIB BOEING 727 727232 1384082 NM NR 6 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 419DA 21272 THE NR 9 RIB WAS FOUND TO BE CRACKED. REPAIRED PER M/M 57-54-0 FIG 804, FOR NR 6 L/E SLAT PANEL. 2 L 7 3 4F A3WE 1996031500711 19960315 00711 NM 1996 3 15 DL72S960555 1 19960229 A 5754 651622296 RIB BOEING 727 727232 1384082 NM NR 6 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 419DA 21272 THE I/B ACTUATOR RIB WAS FOUND TO BE CRACKED. REPAIRED PER M/M 57-54-0 FIG 804, FOR NR 6 L/E SLAT PANEL. 2 L 7 3 4F A3WE 1996031500712 19960315 00712 NM 1996 3 15 DL72S960557 1 19960312 A 5720 BRACKET BOEING 727 727232 1384082 NM LT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 478DA 20755 FOUND DURING E-1 LETTER CHECK, NR 1 SLAT ACTUATOR SUPPORT BRACKET CRACKED I/B SIDE. REPAIRED PER MM 57-20-21 PG 812. 2 L 7 3 4F A3WE 1996031500713 19960315 00713 NM 1996 3 15 DL72S960558 1 19960312 A 5720 BRACKET BOEING 727 727232 1384082 NM LT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 403DA 21147 FOUND DURING F-1 LETTER CHECK, 1 INCH CRACK AT NR 2 L/E FLAP ACTUATOR MOUNT BRACKET. REPAIRED PER MM 57-54-21. 2 L 7 3 4F A3WE 1996031500714 19960315 00714 NM 1996 3 15 DL72S960559 1 19960312 A 5320 WEB BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 478DA 20755 FOUND DURING E-1 LETTER CHECK, LIGHTENING HOLE AT RT FWD TORQUE BOX WEB CRACKED .1875 INCH. REPAIRED PER MM 53-11-0. 2 L 7 3 4F A3WE 1996031500715 19960315 00715 NM 1996 3 15 DL72S960560 1 19960312 A 5720 BRACKET BOEING 727 727232 1384082 NM LT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 403DA 21147 FOUND DURING F-1 LETTER CHECK, CRACK EXTENDING FROM NR 2 SLAT ACTUATOR MOUNT BRACKET UPPER I/B BOLT HOLE. REPAIRED PER M/M 57-42-0. 2 L 7 3 4F A3WE 1996031500716 19960315 00716 NM 1996 3 15 DL72S960562 1 19960312 A 5754 SKIN BOEING 727 727232 1384082 NM NR 4 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 478DA 20755 FOUND ON E1 LETTER CHECK, 2 CRACKS IN OUTBD SURFACE OF NR 4 L/E FLAP, 1.5 INCH AND 2 INCH. REPAIRED AND REPLACED L/E FL AP. 2 L 7 3 4F A3WE 1996031500717 19960315 00717 NM 1996 3 15 DL72S960563 1 19960312 A 2782 BRACKET BOEING 727 727232 1384082 NM NR 1 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 478DA 20755 FOUND ON E1 LETTER CHECK, NR 1 SLAT ACTUATOR MOUNT BRACKET CRACKED ON O/B SIDE. REPAIRED PER M/M 57-20-21. 2 L 7 3 4F A3WE 1996031500718 19960315 00718 NM 1996 3 15 DL73E960556 1 19960312 A 2121 6068502 FAN BOEING 737 737247 138448D NM COCKPIT FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 242WA 23516 SMOKE IN THE COCKPIT AFTER LDG IN ICT, ABOUT THE SAME TIME THE CONTROL CABIN AUG FAN C/B POPPED. CONTRACT MTC INSPECTED FAN AND TESTED A/C SYS, PLACED THE AUG FAN ON MCO. FAN WAS LATER REPLACED. 2 L 7 2 4F A16WE 1996031500719 19960315 00719 NM 1996 3 15 DLM88960528 1 19960308 A 2910 HYD LINE DOUG MD88 MD88 3023688 NM NR 2 PYLON BROKEN A DALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 27 983DL 53247 R-RT HYDRAULIC SYSTEM FAILED IN FLT, PRESS 0 ATY-1 CONFIG FLAPS SLATS 23, LANDING GEAR UP 160 KTS. MANUAL GEAR LOWERING ACCOMPLISHED IAW CHECKLIST. FOUND BROKEN HYDRAULIC LINE IN RT PYLON. REPLACED LINE AND NR 2 PUMP SERVICED, OPERATION NORMAL. 2 L 7 2 4F RT A6WE 1996031500720 19960315 00720 NM 1996 3 15 DLM88960533 1 19960309 A 3222 STRUT DOUG MD88 MD88 3023688 NM NLG WATER CONTAM A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 955DL 49886 ON T/O ROLL, LOUD NOISE FROM NOSE GEAR AREA, MULTIPLE FLAGS NOTED ON FMA, A/S INDICATOR ETC, CAPTS INSTRUMENTS FAILED . FOUND STRUT FLAT. SERVICED STRUT PER OPN 4703 AND PERFORMED BITE CHECK ON INSTRUMENTS, ALL OK. A/C DEPARTED A SECON D TIME, AFTER GEAR RETRACTION NOSE GEAR RED LIGHT REMAINED ILLUMINATED. RETURNED JFK, FERRIED ATL. REPACKED STRUT, FOU ND FLUID CONTAMINATED WITH WATER. SERVICED STRUT AND OPERATION NORMAL. 2 L 7 2 4F RT A6WE 1996031500721 19960315 00721 NM 1996 3 15 DLM88960538 1 19960310 A 3222 STRUT DOUG MD88 MD88 3023688 NM NLG REQD SERVICED A DALA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 905DE 53410 NOSE GEAR UNSAFE LIGHT ON WITH GEAR HANDLE UP, EXCESSIVE WIND NOISE FROM GEAR PROBLEM. RESERVICED NOSE GEAR, JACKED A/C , RAN GEAR 10 TIMES AND GEAR OPERATION NORMAL. 2 L 7 2 4F RT A6WE 1996031500722 19960315 00722 NM 1996 3 15 UPS96205660 1 19960110 A 5320 6517555720 ANGLE BOEING 727 72725C 138400H NM FS 1345 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT SKIN SUPPORT ANGLE CRACKED FS 1345 FIN STA 22.5. REMOVED, FABRICATED AND INSTALLED NEW ANGLE SECTION IAW SRM 51-40-3 AND 51-30-2. 2 L 7 3 4F A3WE 1996031500723 19960315 00723 1996 3 15 UPS96205665 4 19960313 A 3120 CLOCK BOEING 727 7272A1 138407F NM COCKPIT F/E BAD GROUND A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 213UP 21341 DURING TAKEOFF AND FLIGHT, WHEN F/O O2 MASK METAL COMES IN CONTACT WITH F/E CLOCK ON F/E'S PNL, SPARKS FLY OFF OF MASK A ND CLOCK. FOUND BAD GROUND. WIRE RETERMINATED, NEW GROUND LUG AND OP'S CHECK OK. 2 L 7 3 4F A3WE 1996031500724 19960315 00724 NM 1996 3 15 UPS96405668 1 19960307 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 980 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED CRACKED STRINGER AT BS 980 5-38 LT. REPAIRED STRINGER IAW SRM 53-10-03. 2 L 7 4 4F A20WE 1996031500725 19960315 00725 NM 1996 3 15 UPS96505669 1 19960313 A 2497 WIRE BOEING 757 75724APF 1384969 NM P11 PNL BROKEN A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 01 426UP 25457 PRIOR TO T/D, SPARKS AND SMOKE CAME FROM STANDBY POWER SECTION OF P11 PNL. THE STANDBY BUS ON P6 POPPED, ALL STANDBY A/ C POWERED ITEMS WERE LOST. FOUND WIRE BROKEN CAUSED BY INTERFERENCE WITH GROUND STD AT AP .0011. REPAIRED AS REQUIRED . 2 L 7 2 4F RT A2NM 1996031500726 19960315 00726 NM 1996 3 15 UPS96505671 1 19960312 A 5240 ACCESS DOOR BOEING 757 75724APF 1384969 NM LT AC BAY DAMAGED A IPXA O OTHER E VIBRATION/BUFFET CL CLIMB 1 SO 01 428UP 25459 UPON DEPARTURE, EXPERIENCED VIBRATION ABOUT THE SAME TIME FLAPS WERE RETRACTED. VIBRATION CONTINUED UNTIL SEVERAL MINUT ES LATER, THEN STOPPED. REMOVED AND REPLACED PNUE ACCESS DOOR IN LT A/C BAY DOOR. 2 L 7 2 4F RT A2NM 1996031500727 19960315 00727 NM 1996 3 15 UPS96505672 1 19960313 A 5315 FLOOR BEAM BOEING 757 75724APF 1384969 NM BS 278 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 402UP 23724 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION FOUND ON FLOOR BEAM BS 278 WL 200 RBL 3 AND LBL 11. REPAIRED FLOOR BEAM UPPER CHORD PER UPS EO 757-53-0030. 2 L 7 2 4F RT A2NM 1996031500728 19960315 00728 WP 1996 3 15 UPS96805651 1 19960129 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FS 665 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 783UP 45973 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON LONGERON 36 FS 665. REPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996031500729 19960315 00729 WP 1996 3 15 UPS96805652 1 19960216 A 5320 WEB DOUG DC8 DC873F 302199F WP FS 55 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CABIN SUBFLOOR WEB HAS A 4 INCH CRACK AT FS 55 LBL 6. REPLACED WEB SECTION P ER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1996031500730 19960315 00730 WP 1996 3 15 UPS96805653 1 19960217 A 5342 3641125502N FITTING DOUG DC8 DC873F 302199F WP FS 759 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED VERTICAL ATTACH FITTING IS CRACKED AT FS 759 RBL 48. REPLACED FITTING PER SR M 51-1-21. 2 L 7 4 4F RT 4A25 1996031500731 19960315 00731 WP 1996 3 15 UPS96805654 1 19960216 A 5320 FITTING DOUG DC8 DC873F 302199F WP FS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FLOOR BEAM SUPPORT FITTING IS CRACKED AT FS 689 RBL 26. REPLACED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996031500732 19960315 00732 WP 1996 3 15 UPS96805655 1 19960216 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED AFT ENTRY DOOR LOWER FWD CORNER FUSELAGE SKIN CUTOUT AND DOUBLER HAVE A 4 INC H LONG CRACK. REPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996031500733 19960315 00733 WP 1996 3 15 UPS96805656 1 19960208 A 5342 5651927 ATTACH ANGLE DOUG DC8 DC873F 302199F WP FS 1766 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED VERTICAL STAB TO FUSELAGE ATTACH ANGLE HAS A 1 INCH CRACK ON AFT END. REPAIR ED PER UPS EO. 2 L 7 4 4F RT 4A25 1996031500734 19960315 00734 WP 1996 3 15 UPS96805657 1 19960206 A 5755 56851661 SKIN DOUG DC8 DC873F 302199F WP LT SPOILER DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT WING SPOILER DELAMINATED TOP AFT O/B EDGE. REPLACED SPOILER ASSY REP MM 2 7-61-01. 2 L 7 4 4F RT 4A25 1996031500735 19960315 00735 WP 1996 3 15 UPS96805658 1 19960208 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP FS 67 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FUSELAGE SEAM DOUBLER CRACKED LOWER FWD CORNER OF RT PRIMARY HEAT EXCHANGER. REPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996031500736 19960315 00736 WP 1996 3 15 UPS96805662 1 19960219 A 5320 12454993N STIFFENER DOUG DC8 DC873F 302199F WP FS 1737 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT STIFFENER TO BOLT FRAME STA 1737 CRACKED LONGERON 22R. REPLACED STIFFENER PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996031500737 19960315 00737 WP 1996 3 15 UPS96805663 1 19960207 A 5752 5642831503 CONTROL TAB DOUG DC8 DC873F 302199F WP LT AILERON DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LEFT I/B AILERON CONTROL TAB DELAMINATED I/B AFT EDGE, TOP AND BOTTOM SIDE. R EPLACED TAB PER MM 27-13-01. 2 L 7 4 4F RT 4A25 1996031500738 19960315 00738 WP 1996 3 15 UPS96805664 1 19960206 A 5330 501386215 SKIN DOUG DC8 DC873F 302199F WP FS 21.92 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED 2 CRACK'S IN FUSELAGE SKIN, FS 21.92 LONGERONS 31 LT AND RT. REPAIRED SKIN P ER UPS EO. 2 L 7 4 4F RT 4A25 1996031500739 19960315 00739 WP 1996 3 15 UPS96805666 1 19960226 A 5522 SKIN DOUG DC8 DC871F 302199D WP RT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 783UP 45973 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT ELEVATOR UPPER SKIN HAS 2 CRACK'S AT STA 77.67 NEAR T/E. REPAIRED SKIN PE R UPS EO. 2 L 7 4 4F RT 4A25 1996031500740 19960315 00740 WP 1996 3 15 UPS96805667 1 19960301 A 5743 5611440 FITTING DOUG DC8 DC871F 302199D WP LT WING MLG CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 783UP 45973 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT MLG ATTACH FITTING RETRACT BRACKET ATTACH LUG, AFT LUG UPPER ATTACH HOLE H AS CORROSION DAMAGE INSIDE HOLE AND FWD LUG SURFACE. REPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996031500741 19960315 00741 WP 1996 3 15 UPS96805670 1 19960313 A 3230 ACTUATOR DOUG DC8 DC873F 302199F WP RT MLG DAMAGED A IPXA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 810UP 46001 CREW REPORTED, UPON LOWERING GEAR NO DOWN AND LOCKED INDICATION ON RT MAIN GEAR WITH ASSOCIATED GEAR INDICATION AND DOOR NOT LATCH LIGHTS. CYCLED GEAR AND CHECKED LIGHTS WITH NO HELP. COMPLETED FLY-BY AND ALL PERTINANT CHECKLISTS NORMAL L ANDING AND ROLLOUT. REMOVED AND REPLACED RT MAIN GEAR BUNGEE ACT, OPS CK OK. 2 L 7 4 4F RT 4A25 1996031500742 19960315 00742 WP 1996 3 15 UPS96805673 1 19960309 A 5240 DOUBLER DOUG DC8 DC873F 302199F WP AIR ACCESS DR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 WHILE IN FOR B-CHECK, MAINTENANCE REPORTED AIR ACCESS DOOR SUPPORT DOUBLER LOWER EDGE CORROSION REPAIR. REPAIRED PER EO DC8-5310-8016A. 2 L 7 4 4F RT 4A25 1996031500743 19960315 00743 WP 1996 3 15 UPS96805674 1 19960311 A 5320 T-CHORD DOUG DC8 DC873F 302199F WP BS 8 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 WHILE IN FOR B-CHECK, MAINTENANCE REPORTED STATION 8 T-CHORD CORROSION REPAIR. BLENDED CORROSION INSTALLED 2 REPAIR STR APS EQUALING 100 MATERIAL USING 7075-T6 MATERIAL PER EO DC8-5310-8015A. 2 L 7 4 4F RT 4A25 1996031500744 19960315 00744 WP 1996 3 15 UPS96805675 1 19960313 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 WHILE IN FOR B-CHECK, MAINTENANCE REPORTED CORROSION IN BELLY AND CRACKED LONGERONS. REPAIRED PER EO DC8-5330-8018. 2 L 7 4 4F RT 4A25 1996032100001 19960321 00001 NE 1996 3 21 96FDEA00125 2 19960126 A 7260 779600 GEARBOX BOEING 747 747245F 1384897 NM PWA JT9 JT9D7A 52054 NE NR 4 ENG FAILED A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 638FE 21841 SYD - DURING CLIMBOUT, SHUT NR 4 ENG DOWN DUE TO LOSS OF OIL QTY LOW PRESS AND ILLUM OF OIL PRESS LIGHT. FLIGHT RETURNE D TO SYDNEY. WINDMILL TIME PER CREW SAFETY REPORT 24 MIN. FOUND DE-AERATOR BROKEN. REPLACED MAIN GEARBOX ASSY AS PER PRATT AND WHITNEY JT9D ENG MANUAL 72-00-00, GEARBOX INSTALLATION ENG RII C/W. 2 L 7 4 4F 4 F A20WE E20EA 1996032100003 19960321 00003 NE 1996 3 21 DLL17960296 2 19960208 A 7314 FUEL PUMP PAC102MK4 LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE NR 2 ENGINE FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 766DA B1135 193H1207 014882 DURING CLIMBOUT, NR 2 ENG FUEL PRESS LIGHT BLINKED AND CAME ON STEADY. AT 25,000 FT COULD NOT ADVANCE ENG PAST 5,000 PP H F/F. ALSO, DECREASE IN N1 FROM 90 PERCENT TO 80. REPLACED NR 2 FUEL PUMP, OPERATION NORMAL. 2 L 7 3 4F 4 F A23WE E12EU 1996032100004 19960321 00004 NM 1996 3 21 UPS405428 1 19960210 A 5720 SUPPORT TUBE BOEING 747 747121 1384871 NM ILES 788 PUNCTURED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, HOLE IN SUPPORT TUBE AT I/B LEADING EDGE STATION 788. REPLACED SUPPORT IAW S RM 51-30-05 AND MM 20-10-13. 2 L 7 4 4F A20WE 1996032100005 19960321 00005 EU 1996 3 21 HEEA966701 1 19960220 A 6240 10594575 TRANSMITTER BOLKMS 105 BO105S 5626006 EU ROTOR RPM ERRATIC E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 86CH S557 TRANSMITTER UNIT WILL NOT TEST PROPERLY AND NEEDLE HAS A ERRATIC INDICATION. TIME SINCE REPAIR 0:00. 1 G 7 2 3U H3EU 1996032100006 19960321 00006 EU 1996 3 21 HEEA966702 1 19960220 A 6240 10594565 INDICATOR BOLKMS 105 BO105S 5626006 EU MAST MOMENT ERRATIC E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 86CH S557 UNIT WILL NOT TEST PROPERLY AND NEEDLE HAS A ERRATIC INDICATION. TIME SINCE REPAIR 0:00. 1 G 7 2 3U H3EU 1996032200009 19960322 00009 CE 1996 3 22 96ZZZX1136 1 19960205 A 2435 15809111 SHAFT BENDIX 30B3749BT LEAR 25 25D 5170514 CE RT ENG STARTER SHEARED A VNRA K NONE O OTHER IN INSP/MAINT 1 SW 05 347AC 396 828 347 WHILE AT MSP UNDER EXTREME COLD CONDITIONS (MINUS 12 DEGREES FAHRENHEIT), RIGHT STARTER GENERATOR SHAFT SHEARED DURING S TART ATTEMPT. CAUSE FOR FAILING UNKNOWN. SUSPECTED COMBINATION OF TEMPS AND AGE OF SHAFT, THESE ARE NOT NORMALLY REPLA CED AT OVERHAUL. INSTALLED OVERHAULED UNIT. 2 L 7 2 4J A10CE 1996032200035 19960322 00035 NE 1996 3 22 9606066603 2 19960313 A 7310 FILTER BOEING 747 747151 1384891 NM PWA JT9 JT9D7A 52054 NE ENGINE DIRTY A NWAA B EMER. DESCENT X ENGINE FLAMEOUT CR CRUISE 1 GL 01 603US 19780 62452 DURING CRUISE AT FL330, THE NR 1 AND NR 4 ENGINES FLAMED OUT SIMULTANEOUSLY. RESTART WAS SUCCESSFUL AND THE FLIGHT CONT INUED TO NRT WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED CROSS FEED VALVE OPERATIONAL CHECK, FUEL TRANSFER VALVE CR OSS FEED MANIFOLD IN FUEL FLOW CHECK AND FOD CHECK. CHECKS WERE NORMAL AND RUNUP OF ALL FOUR ENGINES REVEALED NO DISCRE PANCIES. REPLACED ALL FOUR ENGINE FILTERS AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4 F A20WE E20EA 1996032200036 19960322 00036 1996 3 22 9606075507 4 19960313 A 3425 SWITCH BOEING 757 757251 1384970 NM FLIGHT DECK FAILED A NWAA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION LD LANDING 1 GL 01 507US 23196 AFTER TOUCHDOWN AT MSP, THE AIRCRAFT WENT INTO A GO-AROUND MODE WITHOUT HITTING GA SWITCHES AND SPEED BRAKES WENT DOWN A ND THROTTLES MOVED FORWARD. CAPTAIN WAS FLYING MANUALLY AT THE TIME OF THE OCCURRENCE. THE AIRCRAFT CONTINUED LANDING WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 AND NR 2 GA SWITCHES, S7 AND S8. OPERATIONAL CHECKS NORMAL, LR C FCC'S AND TMC CHECK OK. 2 L 7 2 4F RT A2NM 1996032200037 19960322 00037 WP 1996 3 22 9606089929 1 19960313 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8923E 45838 DURING LINE MAINTENANCE INSPECTION, FOUND ALL OVERWING EXIT EMERGENCY LIGHTS DIM. REPLACED BATTERIES AND OPERATIONAL CH ECK NORMAL. 2 L 7 2 4F A6WE 1996032200038 19960322 00038 WP 1996 3 22 9606099962 1 19960313 A 3350 60030451 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 914RW 47362 DURING LINE MAINTENANCE INSPECTION, FOUND AFT OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND OPE RATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996032200039 19960322 00039 WP 1996 3 22 9606109970 1 19960313 A 3350 60030451 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9334 47247 DURING LINE MAINTENANCE INSPECTION, FOUND BOTH AFT OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AN D OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996032200040 19960322 00040 NE 1996 3 22 9606119925 2 19960314 A 7230 COMPRESSOR DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9 52048 NE RT ENGINE STALLED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 925US 47472 665868 RIGHT ENGINE COMPRESSOR STALL OCCURRED DURING TAKEOFF ROLL AT 70 KNOTS. ABORTED TAKEOFF AND RETURNED TO THE GATE. A .5 INCH LAYER OF SLUSH WAS REPORTED TO BE ON RUNWAY AT TIME OF INCIDENT. MAINTENANCE BORESCOPED 6TH, 7TH AND 13TH STAGE C OMPRESSOR, ALL CHECKED NORMAL. ALSO, ENGINE RUN CHECKED GOOD. 2 L 7 2 4F 4 F A6WE E2EA 1996032200041 19960322 00041 WP 1996 3 22 96FDEA00523 1 19960314 A 5210 DRIVE CHAIN DOUG DC10 DC1010 3022110 WP L-1 DOOR SHEARED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 052FE 47806 SNRM 2146, UPON EMERGENCY AIR OPERATION OF L-1 DOOR, DOOR DID NOT MOVE TO OPEN POSITION. UPON INSPECTION FOUND EMERGENC Y AIR MOTOR DRIVE CHAIN SHEARED. 2 L 7 3 4F A22WE 1996032200042 19960322 00042 WP 1996 3 22 96FDEA00524 1 19960311 A 5320 FITTING DOUG DC10 DC1010 3022110 WP BS 17.81 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 052FE 47806 SNRM 0773, SHEAR TIE FITTING HAS INTERGRANULAR CORROSION AT STA 17.81 BETWEEN LONGERON 47R TO 45R. 2 L 7 3 4F A22WE 1996032200043 19960322 00043 NM 1996 3 22 96FDEA00525 1 19960314 A 5270 UNLOCK LIGHT BOEING 727 7272D4 138407U NM CARGO DOOR MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 287FE 21849 MAIN CARGO DOOR LIGHT CAME ON IN FLIGHT ON CLIMBOUT. DEFERRED PER MEL 52-4 (A) MAIN CARGO DOOR VISUALLY CHECKED LOCKED EXPIRES 3/16/96 CONTROL0314030. REMOVED AND REPLACED AFT CARGO DOOR UNLOCKED LIGHT RECEPTACLE, OPS CHECKED GOOD. 2 L 7 3 4F A3WE 1996032200044 19960322 00044 NM 1996 3 22 96UAL900190 1 19960314 A 2820 FUEL TRANSFER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 FUEL TANK FAILED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 7283U 21561 UNWANTED FUEL TRANSFER OUT OF NR 1 MAIN FUEL TANK. REPORTED 1000 POUND LOSS WITH NO PUMPS ON. 2 L 7 3 4F 4 F A3WE E2EA 1996032200045 19960322 00045 NE 1996 3 22 96UAL900191 2 19960314 A 7200 ENGINE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE AIRFRAME POWER LOSS A UALA O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 WP 29 7278U 21425 CREW REPORTED LOSING POWER IN CLIMB, CRUISE, AND DESCENT. FRICTION LOCK WORKS NORMAL AND NO THROTTLE MOVEMENT IS EVIDEN T. ALL INDICATIONS SHOW LOSS OF POWER. ACCOMPLISHED ENGINE POWER RUN. ENGINE PARAMETERS NORMAL AND STEADY DURING TAKE OFF AND PART POWER SETTINGS. NO CAUSE FOUND FOR WRITE-UP. NO CORRECTIVE ACTION REQUIRED. 2 L 7 3 4F 4 F A3WE E2EA 1996032200046 19960322 00046 GL 1996 3 22 96UAL900192 2 19960314 A 7250 TURBIN MID FRAME DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 3 ENGINE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 1823U 46622 NR 3 ENGINE TURBINE MID FRAME HAS CRACK 1.5 INCHES LONG AT 6 O'CLOCK POSITION. 2 L 7 3 4F 4 F A22WE E23EA 1996032200047 19960322 00047 WP 1996 3 22 ABXA9600250 1 19960131 A 5320 49125391 FITTING DOUG DC9 DC941 302207N WP BS 1042 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 DURING C-CHECK INSPECTION, FOUND CRACKED FITTING AT LOWER INBOARD PYLON BULKHEAD AT STA 1042. REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 1996032200048 19960322 00048 WP 1996 3 22 ABXA9600251 1 19960202 A 5730 9951631 PANEL DOUG DC9 DC941 302207N WP WS 509 DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 DURING C-CHECK INSPECTION, FOUND HOLE AT TRAILING EDGE OF PANEL 1512, LEFT WING. REPLACED PANEL IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 1996032200049 19960322 00049 WP 1996 3 22 ABXA9600252 1 19960131 A 5320 591016397 SHEAR TIE DOUG DC9 DC941 302207N WP BS 1072 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 DURING C-CHECK INSPECTION, FOUND SHEAR TIE STA 1072 CRACKED AT LONGERON 18L. SHEAR TIE REPLACED IAW DC-9 SRM 51-30-2 AN D 51-30-5. 2 L 7 2 4F A6WE 1996032200050 19960322 00050 WP 1996 3 22 ABXA9600253 1 19960203 A 5315 1242520 FLOOR BEAM DOUG DC9 DC941 302207N WP BS 962 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 DURING C-CHECK INSPECTION, FOUND FLOOR BEAM AT STA 962 HAD A CRACK WHICH EXTENDED PAST STOP DRILL. REPAIRED IAW DC-9 SU PPLEMENTAL SRM DRAWING K05159. 2 L 7 2 4F A6WE 1996032200051 19960322 00051 WP 1996 3 22 ABXA9600254 1 19960205 A 5280 3923159505 ARM DOUG DC9 DC941 302207N WP RT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 DURING C-CHECK INSPECTION AND COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND RIGHT MAIN LANDING GEAR FLYING DOOR PIVOT ARM WORN. REPLACED ARM ASSEMBLY IAW DC-9 MM 20-16-0. 2 L 7 2 4F A6WE 1996032200052 19960322 00052 WP 1996 3 22 ABXA9600255 1 19960203 A 5280 5913433504 HINGE LOBES DOUG DC9 DC941 302207N WP RT MLG DOOR MISSING A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 91-22-07; ASB 32-244, FOUND RIGHT MAIN LANDING GEAR FLYING DOOR AFT ATT ACH HINGE LOBES MISSING BUSHINGS. REPLACED HINGE IAW DC-9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1996032200053 19960322 00053 WP 1996 3 22 ABXA9600256 1 19960206 A 3231 3923167507 ROD DOUG DC9 DC941 302207N WP RT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 91-22-07; ASB 32-244, FOUND RIGHT MAIN LANDING GEAR FLYING DOOR ACTUATI NG RODS WORN. REPLACED ROD IAW DC-9 MM 20-16-0. 2 L 7 2 4F A6WE 1996032200054 19960322 00054 WP 1996 3 22 ABXA9600257 1 19960206 A 3231 3923161503 ROD DOUG DC9 DC941 302207N WP RT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 91-22-07; ASB 32-244, FOUND RIGHT MAIN LANDING GEAR FLYING DOOR ACTUATI NG RODS WORN. REPLACED ROD IAW DC-9 MM 20-16-0. 2 L 7 2 4F A6WE 1996032200055 19960322 00055 WP 1996 3 22 ABXA9600258 1 19960212 A 5713 9919369502 STRINGER CAP DOUG DC9 DC941 302207N WP WS 58 GOUGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 90-18-03, SB 57-98 REV 8, FOUND RIGHT WING TENSION BOLT HOLE AT STRINGE R NR 23 GOUGED. REPAIRED IAW ABX REA D957-14318-MR. 2 L 7 2 4F A6WE 1996032200056 19960322 00056 WP 1996 3 22 ABXA9600259 1 19960212 A 5713 991934822 STRINGER WEB DOUG DC9 DC941 302207N WP WS 58 GOUGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 90-18-03; SB 57-98 REV 8, FOUND RIGHT WING TENSION BOLT HOLE AT STRINGE R NR 23 GOUGED. REPAIRED IAW ABX REA D957-14318-MR. 2 L 7 2 4F A6WE 1996032200057 19960322 00057 WP 1996 3 22 ABXA9600260 1 19960212 A 5720 991934834 STRINGER DOUBLER DOUG DC9 DC941 302207N WP WS 58 GOUGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 90-18-03; SB 57-98 REV 8, FOUND RIGHT WING TENSION BOLT HOLE AT STRINGE R NR 23 GOUGED. REPAIRED IAW ABX REA D957-14318-MR. 2 L 7 2 4F A6WE 1996032200058 19960322 00058 WP 1996 3 22 ABXA9600261 1 19960212 A 5720 991934836 STRINGER DOUBLER DOUG DC9 DC941 302207N WP WS 58 GOUGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 90-18-03; SB 57-98 REV 8, FOUND RIGHT WING TENSION BOLT HOLE AT STRINGE R NR 23 GOUGED. REPAIRED IAW ABX REA D957-14318-MR. 2 L 7 2 4F A6WE 1996032200059 19960322 00059 WP 1996 3 22 ABXA9600262 1 19960211 A 5330 591142739 SKIN DOUG DC9 DC941 302207N WP BS 1056 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 DURING C-CHECK INSPECTION, FOUND SKIN CRACKED AT STA 1056, BETWEEN LONGERONS 15R AND 16R. REPAIRED IAW ABX REA D953-142 81-MR. 2 L 7 2 4F A6WE 1996032200060 19960322 00060 WP 1996 3 22 ABXA9600263 1 19960206 A 5330 592032379 SKIN DOUG DC9 DC941 302207N WP BS 448 DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 DURING C-CHECK INSPECTION, THE FUSELAGE SKIN WAS DAMAGED WHILE A REPAIR WAS BEING ACCOMPLISHED AT STA 448, BETWEEN LONGE RONS 23R AND 25R. REPAIRED IAW ABX REA D953-14302-MR. 2 L 7 2 4F A6WE 1996032200061 19960322 00061 WP 1996 3 22 ABXA9600264 1 19960202 A 5713 3911238509 STRINGER CAP DOUG DC9 DC941 302207N WP WS 58 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 90-18-03; SB 57-98 REV 8, FOUND STRINGER 19L CORRODED AT SPOT FACE FOR TENSION BOLT AT T-CAP. REPAIRED IAW DC-9 SRM 51-10-3. 2 L 7 2 4F A6WE 1996032200062 19960322 00062 WP 1996 3 22 ABXA9600265 1 19960202 A 5713 3911238507 STRINGER CAP DOUG DC9 DC941 302207N WP WS 58 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 957AX 47509 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 90-18-03; SB 57-98 REV 8, FOUND CORROSION IN STRINGER 20L AT T-CAP. RE PAIRED IAW DC-9 SRM 51-10-3. 2 L 7 2 4F A6WE 1996032200063 19960322 00063 WP 1996 3 22 ABXA9600266 1 19960202 A 5713 3911238505 STRINGER CAP DOUG DC9 DC941 302207N WP WS 58 GOUGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 90-18-03; SB 57-98 REV 8, FOUND STRINGER 21L GOUGED INSIDE TENSION BOLT HOLE AT T-CAP. REPAIRED IAW DC-9 SRM 57-03. 2 L 7 2 4F A6WE 1996032200064 19960322 00064 WP 1996 3 22 ABXA9600267 1 19960202 A 5713 3911238501 STRINGER CAP DOUG DC9 DC941 302207N WP WS 58 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 90-18-03; SB 57-98 REV 8, FOUND STRINGER 23L CORRODED AND GOUGED INSIDE TENSION BOLT HOLE AT T-CAP. REPAIRED IAW DC-9 SRM 51-10 AND 57-03. 2 L 7 2 4F A6WE 1996032200065 19960322 00065 WP 1996 3 22 ABXA9600268 1 19960201 A 5713 99193691 STRINGER CAP DOUG DC9 DC941 302207N WP WS 58 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 90-18-03; SB 57-98 REV 8, FOUND LEFT WING T-CAP CORRODED INSIDE BARREL NUT HOLES, STRINGERS 12, 20, 21 AND 23. REPAIRED IAW DC-9 SRM 51-10-3 AND DC-9 SB 57-98. 2 L 7 2 4F A6WE 1996032200066 19960322 00066 WP 1996 3 22 ABXA9600269 1 19960131 A 5713 99193692 STRINGER CAP DOUG DC9 DC941 302207N WP XRS 58 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 90-18-03; SB 57-98 REV 8, FOUND T-CAP CORRODED INSIDE BARREL NUT HOLES AT STRINGERS 12, 18, 19, 20, 21, 22 AND 23 ON THE RIGHT WING. REPAIRED IAW DC-9 SRM 51-10-3 AND DC-9 SB 57-98. 2 L 7 2 4F A6WE 1996032200073 19960322 00073 WP 1996 3 22 ABXA9600277 1 19960224 A 5280 52210370P4109 BUSHING DOUG DC9 DC931 3022065 WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 907AX 47203 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND LEFT MAIN LANDING GEAR DOOR ATTACHING LINK WORN AT ATTACHMENT POINT TO DOOR. REPLACED BUSHING AW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1996032200074 19960322 00074 WP 1996 3 22 ABXA9600278 1 19960224 A 3231 3923159505 ARM DOUG DC9 DC931 3022065 WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 907AX 47203 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND LEFT MAIN LANDING GEAR DOOR ATTACHING LINK WORN AT ATTACHMENT POINT TO DOOR. REPLACED ARM ASSEMBLY IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1996032200075 19960322 00075 WP 1996 3 22 ABXA9600279 1 19960224 A 5280 52210370P4109 BUSHING DOUG DC9 DC931 3022065 WP RT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 907AX 47203 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND RIGHT MAIN LANDING GEAR DOOR ATTACHING LINK WORN AT ATTACHMENT POINT TO DOOR. REPLACED BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1996032200076 19960322 00076 WP 1996 3 22 ABXA9600280 1 19960224 A 3231 3923159505 ARM DOUG DC9 DC931 3022065 WP RT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 907AX 47203 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND THE RIGHT MAIN LANDING GEAR DOOR ATTACHING LINK WORN AT ATTACHMENT P OINT TO DOOR. REPLACED ARM ASSEMBLY IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1996032200091 19960322 00091 WP 1996 3 22 ABXA9600295 1 19960111 A 5320 575468828 DOUBLER DOUG DC9 DC932 3022066 WP RT COCKPIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 DURING COMPLIANCE OF AD 90-18-03; SB 56-11 REV 3, EAAD 56-3956-MA, FOUND STEEL DOUBLER CRACKED AT UPPER AFT CORNER OF TH E RIGHT EYEBROW WINDOW FRAME. REPLACED DOUBLER IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 1996032200092 19960322 00092 WP 1996 3 22 ABXA9600296 1 19960127 A 3231 392316507 DRIVER ROD DOUG DC9 DC931 3022065 WP BS 111 WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND THE RIGHT MAIN LANDING GEAR OUTBOARD DOOR DRIVER ROD HAD EXCESSIVE P LAY. REPLACED DRIVER ROD IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1996032200093 19960322 00093 WP 1996 3 22 ABXA9600297 1 19960209 A 5280 29242891 BUSHING DOUG DC9 DC932 3022066 WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 986AX 47543 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND WING MOUNTED HINGE ON THE LEFT OUTBOARD MAIN LANDING GEAR DOOR HAD E XCESSIVE SIDE PLAY. REPAIRED IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1996032200094 19960322 00094 WP 1996 3 22 ABXA9600298 1 19960221 A 5280 3923159505 LINK DOUG DC9 DC931 3022065 WP RT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND THE RIGHT MAIN LANDING GEAR OUTBOARD DOOR LINK ATTACHING POINT AT TH E DOOR HAD EXCESSIVE SIDE TO SIDE PLAY. REPLACED LINK ON RIGHT MAIN LANDING GEAR OUTBOARD DOOR IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1996032200095 19960322 00095 WP 1996 3 22 ABXA9600299 1 19960229 A 2760 3923250503 DRIVE LINK DOUG DC9 DC941 302207N WP RT INBD SPOILER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47497 DURING COMPLIANCE OF AD 85-01-03; SB 27-228 REV 4, DURING EDDY CURRENT INSPECTION, FOUND THAT THE RIGHT INBOARD SPOILER DRIVE LINK HAD A CRACK INDICATION. REPLACED LINK IAW DC-9 SUPP MM 27-61-01. 2 L 7 2 4F A6WE 1996032200096 19960322 00096 WP 1996 3 22 ABXA9600300 1 19960206 A 5311 99196192 FRAME DOUG DC9 DC931 3022065 WP BS 737 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 943AX 47528 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 78-07-05; SB 53-131, FOUND THE FUSELAGE FRAME AT STA 737 CRACKED. REPL ACED FRAME IAW DC-9 SB 53-13-1. 2 L 7 2 4F A6WE 1996032200097 19960322 00097 WP 1996 3 22 ABXA9600301 1 19960206 A 5311 99196172 FRAME DOUG DC9 DC931 3022065 WP BS 699 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 943AX 47528 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 78-07-05; SB 53-131, FOUND THE FUSELAGE FRAME AT STA 699R CRACKED. REP LACED THE FRAME IAW DC-9 SB 53-131. 2 L 7 2 4F A6WE 1996032200098 19960322 00098 WP 1996 3 22 ABXA9600302 1 19960206 A 5311 9919619503N FRAME DOUG DC9 DC931 3022065 WP BS 737 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 943AX 47528 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 78-07-058; SB 53-131, THE FUSELAGE FRAME AT STA 737L WAS FOUND CRACKED. REPLACED FRAME IAW DC-9 SB 53-131. 2 L 7 2 4F A6WE 1996032200099 19960322 00099 WP 1996 3 22 ABXA9600303 1 19960206 A 5311 99196271 FRAME DOUG DC9 DC931 3022065 WP BS 699 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 943AX 47528 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 78-07-05; SB 53-131, THE FUSELAGE FRAME AT STA 699L WAS FOUND CRACKED. REPLACED FRAME IAW DC-9 SB 53-131. 2 L 7 2 4F A6WE 1996032200100 19960322 00100 WP 1996 3 22 ABXA9600304 1 19960202 A 5720 99193082 FITTING DOUG DC9 DC931 3022065 WP WS 334 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 943AX 47528 DURING C-CHECK INSPECTION, FOUND THE RIGHT WING LEADING EDGE FITTING AT STA XOS 334 CRACKED. REPAIRED FITTING IAW ABX R EA D957-14255-MR. 2 L 7 2 4F A6WE 1996032200101 19960322 00101 WP 1996 3 22 ABXA9600305 1 19960202 A 5320 3916209501 SUPPORT DOUG DC9 DC931 3022065 WP BS 680 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 943AX 47528 DURING C-CHECK INSPECTION, FOUND A VERTICAL FLOOR SUPPORT CRACKED AT STA 680, RBL 44. REPLACED SUPPORT IAW DC-9 SRM 51- 30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1996032200102 19960322 00102 WP 1996 3 22 ABXA9600306 1 19960202 A 5320 3916209501 SUPPORT DOUG DC9 DC931 3022065 WP BS 680 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 943AX 47528 DURING C-CHECK INSPECTION, FOUND A VERTICAL FLOOR SUPPORT CRACKED AT STA 680, LBL 44. REPLACED SUPPORT IAW DC-9 SRM 51- 30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1996032200103 19960322 00103 WP 1996 3 22 ABXA9600307 1 19960205 A 5311 9919613502 FRAME DOUG DC9 DC931 3022065 WP BS 617 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 943AX 47528 DURING C-CHECK INSPECTION, FOUND FUSELAGE FRAME 617 CRACKED BETWEEN LONGERON 18 AND 19R. REPAIRED FRAME IAW ABX REA D95 3-14294-MR. 2 L 7 2 4F A6WE 1996032200104 19960322 00104 WP 1996 3 22 ABXA9600308 1 19960122 A 5330 SKIN DOUG DC9 DC941 302207N WP BS 623 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 956AX 47620 DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON FUSELAGE SKIN AT STA 623 BETWEEN LONGERONS 25L AND 25R. REPAIRED IAW DC-9 SRM 53-04, FIGURE 43. 2 L 7 2 4F A6WE 1996032200105 19960322 00105 1996 3 22 DHL96706003 4 19960310 A 3417 HG180V2 AIR DATA COMP 5222703000 BOEING 727 72722C 138400F NM NR 2 MALFUNCTIONED A T DHLA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 SO 01 706DH 4094 19192 BOTH TRANSPONDERS FAILED THROUGH 6,000 FEET. CYCLED TRANSPONDERS, PULLED AND RESET C/B. REMOVED AND REPLACED AIR DATA COMPUTER FOR NO ALT REPORTING. REMOVED AND REPLACED NR 2 ATC DUE TO WEAK REPLY AND LEAK CHECKED PER 34-11-0. 2 L 7 3 4F A3WE 1996032200106 19960322 00106 NM 1996 3 22 DL72L960580 1 19960308 A 5210 SNAP RING BOEING 727 727232 1384082 NM L 1 DOOR FAILED A DALA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 502DA 21304 FWD 1L DOOR WOULD NOT OPEN AT GATE, REPEATED ATTEMPS DOOR FINALLY OPENED. FOUND SNAP RING MISSING ON UPPER ARM OF DOOR GUIDE PIN. INSTALLED SNAP RING AND OPERATION NORMAL. 2 L 7 3 4F A3WE 1996032200107 19960322 00107 NM 1996 3 22 DL72S960567 1 19960313 A 5320 WEB BOEING 727 727232 1384082 NM BS 1243 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 532DA 22045 FOUND ON B2 LETTER CHECK, LOWER RT TORQUE BOX LIGHTENING HOLE WEB CRACKED FS 1243. REPAIRED PER MM 53-11-0. 2 L 7 3 4F A3WE 1996032200108 19960322 00108 NM 1996 3 22 DL72W960576 1 19960308 A 5330 SKIN BOEING 727 727247 138408F NM BS 1098 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2821W 21059 DURING LETTER CHECK AT TAMPA, A .5 INCH CRACK IN THE FUSELAGE SKIN AT STA 1098 ALONG S-1. CRACK WAS REPAIRED PER B727 S RM 53-30-3, FIGURE 3. 2 L 7 3 4F A3WE 1996032200109 19960322 00109 NM 1996 3 22 DL757960564 1 19960313 A 3230 HOSE BOEING 757 757232 1384965 NM LT MLG GEAR CRACKED A DALA A UNSCHED LANDING K FLUID LOSS TO TAKEOFF 1 SO 27 605DL 22812 ON TAKEOFF, GEAR HANDLE WOULD NOT GO TO THE UP POSITION, USED LOCK OVERIDE TO GET GEAR UP AND FLIGHT RETURNED ATL. FOUN D LEFT TRUCK POS HYD HOSE CRACKED. REPLACED HOSE AND OPERATION NORMAL. 2 L 7 2 4F RT A2NM 1996032200110 19960322 00110 NM 1996 3 22 DL757960579 1 19960313 A 2750 FSEU COMPUTERS 285N001140 BOEING 757 757232 1384965 NM LE FLAPS MALFUNCTIONED A DALA O OTHER J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 SO 27 682DA D01512 26958 CLIMBING THROUGH FL390 FLAP UP, L/E SLAT ASYMMETRICAL EICAS MSG AND L/E CAUTION LIGHT. CYCLING ALTN L/E SLAT SWITCH HA D NO EFFECT. PERFORMED 20 DEGREE FLAP LANDING PER PILOTS OPS MANUAL. LIGHT AND MSG EXTINGUISHED ON TAXI IN WITH FLAPS UP AND BOTH CAME BACK ON AT GATE. REPLACED ALL 3 FSEU COMPUTERS. ALSO, REPLACED BOTH SLAT SWITCHES. CYCLED FLAPS SEVE RAL TIMES AND OPS NORMAL. 2 L 7 2 4F RT A2NM 1996032200111 19960322 00111 NM 1996 3 22 DL76S960569 1 19960313 A 5754 144T410427A SKIN BOEING 767 767332 1382001 NM NR 4 LE SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 126DL 24076 THE NR 4 LEADING EDGE SLAT WAS FOUND WITH THE UPPER SKIN DELAMINATED AT THE T/E WEDGE. THE DAMAGE IS ON THE LT WING WIT H THE LOCATION OF THE DAMAGE 4 INCHES FROM TE, 81 FROM I/B EDGE AND 3 INCHES IN DIA. ACCOMPLISHED REPAIRS PER DL ERA 27 3469-14 RA. 2 L 7 2 4F RT A1NM 1996032200112 19960322 00112 NM 1996 3 22 DL76S960570 1 19960313 A 5754 144T410529A TE WEDGE BOEING 767 767332 1382001 NM NR 5 LE SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 126DL 24076 THE NR 5 LEADING EDGE SLAT ON THE LT WING WAS DELAMINATED ON THE T/E WEDGE. THE DAMAGE IS AT THE AFT, I/B CORNER WITH 3 .5 INCH DIA COVERAGE. IN ADDITION, THE NR 5 SLAT WAS FOUND WITH AN UNIDENTIFIED PREVIOUS REPAIR EXTENDING FROM THE I/B EDGE OF THE TRAILING EDGE WEDGE TO THE EDGE OF THE NEW DAMAGE LOCATION. THIS REPAIR WILL BE REMOVED AND INCORPORATED IN TO THE CURRENT REPAIR SCHEME PER DL ERA 273469-14 REV A. 2 L 7 2 4F RT A1NM 1996032200113 19960322 00113 NM 1996 3 22 DL76S960572 1 19960313 A 5754 144T410132A TE WEDGE BOEING 767 767332 1382001 NM NR 12 LE SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 128DL 24078 THE RT WING NR 12 SLAT TE WEDGE WAS FOUND WITH THE UPPER SKIN DELAMINATED. THE DAMAGE LOCATION IS 3.5 INCHES FROM THE T E EDGE, 10 INCHES FROM THE I/B EDGE COVERING 3.5 DIA. ACCOMPLISHED REPAIRS PER DL ERA 273469-14 REV A. 2 L 7 2 4F RT A1NM 1996032200114 19960322 00114 NM 1996 3 22 DLM88960566 1 19960313 A 3260 SWITCH DOUG MD88 MD88 3023688 NM NLG INOPERATIVE A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 901DE 53378 RED NOSE GEAR UNSAFE LIGHT ON WITH GEAR HANDLE UP, PREFORMED POM PROCEDURES INCLUDING CYCLING GEAR. REPLACED NOSE GEAR INTERLOCK SWITCH, SWUNG NOSE GEAR AND CHECKS OK. 2 L 7 2 4F RT A6WE 1996032200115 19960322 00115 NM 1996 3 22 DLM88960568 1 19960313 A 5320 59124921 DOOR JAMB DOUG MD88 MD88 3023688 NM FWD SERVICE DOOR DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 938DL 49811 FUSELAGE FWD SERVICE DOOR SURROUND STRUCTURE LOWER JAMB PAN WAS DAMAGED BY TOOLING. THE DAMAGE CONSISTS OF PUNCTURES CO MPLETELY THROUGH THE PAN AT BOTH THE FWD AND AFT LOWER CORNERS, REQUIRING REPLACEMENT. A REPLACEMENT PAN IS NOT IMMEDIA TELY AVAILABLE, SO THE REPAIR CONSISTS OF SPLICING IN REFABRICATED REPLACEMENT SECTIONS PER THE MD-88 SRM WILL BE ACCOMP LISHED REF DL ERA 273424-14 REV B. 2 L 7 2 4F RT A6WE 1996032200116 19960322 00116 NM 1996 3 22 DLM88960581 1 19960308 A 3240 BOLT DOUG MD88 MD88 3023688 NM BRAKE PEDALS LOOSE A DALA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 962DL 49981 AFTER LANDING, BRAKES ARE SPONGY AND INEFFECTIVE AND PARKING BRAKE WILL NOT SET. SECURED LOOSE BOLT ON BRAKE SWITCH BRA CKET TO ALLOW FULL TRAVEL OF BRAKE PEDAL AND OPERATION NORMAL. 2 L 7 2 4F RT A6WE 1996032200117 19960322 00117 WP 1996 3 22 MWEA96059 1 19960315 A 3350 60030431 POWER SUPPLY DOUG DC9 DC914 3022034 WP CABIN INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 500ME 45711 DURING SERVICE CHECK, FOUND AFT CABIN OVERHEAD EMERGENCY LIGHTS ILLUMINATE WITH A/C POWER OFF. REPLACED BATTERY POWER S UPPLY AND OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996032200118 19960322 00118 WP 1996 3 22 SCNA96031 1 19960308 A 2611 30231R17 SMOKE DETECTOR DOUG DC10 DC1030 3023501 WP CARGO COMPT FAILED TEST A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 600GC 46965 THE NUMBER 2 LOWER AFT CARGO SMOKE DETECTOR FAILED TO TEST. RELAMPED AND CHECKED SMOKE DETECTOR PER DC10 MM 26-14-00 AN D DETECTOR CHECKED NORMAL. 2 L 7 3 4F A22WE 1996032200119 19960322 00119 WP 1996 3 22 SCNA96032 1 19960309 A 2611 72130000008 SMOKE DETECTOR DOUG DC10 DC1010 3022110 WP NR 1 LAV MALFUNCTIONED A SCNA K NONE O OTHER UK UNKNOWN 1 GL 15 571SC 46645 THE NUMBER 1 LAV WAS FOUND TO BE INOPERATIVE. OPS CHECKED NUMBER 1 LAV SMOKE DETECTOR PER DC10 MM 26-00 AND NO DEFECTS WERE NOTED. 2 L 7 3 4F A22WE 1996032200120 19960322 00120 1996 3 22 SCNA96033 2 19960308 A 7261 EXXON2380 OIL SYST DOUG DC10 DC1010 3022110 WP NR 2 ENGINE LOW A SCNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 572SC 46977 THE NUMBER 2 ENGINE OIL QUANTITY INDICATION DROPPED TO ZERO AND OIL PRESSURE FLUCTUATED DURING CLIMB. REDUCED NUMBER 2 ENGINE POWER TO IDLE AND AIRCRAFT RETURNED TO STATION. SERVICED OIL TO FULL AND ACCOMPLISHED LEAK CHECK PER DC10 MM 79- 00-00, NO LEAKS WERE NOTED. 2 L 7 3 4F A22WE 1996032200121 19960322 00121 WP 1996 3 22 SCNA96034 1 19960312 A 2611 72130000008 SMOKE DETECTOR DOUG DC10 DC1010 3022110 WP NR 1 LAV FAILED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 571SC 46645 THE NUMBER 1 LAVATORY SMOKE DETECTOR WOULD NOT TEST. REMOVED AND REPLACED THE NUMBER 1 LAVATORY SMOKE DETECTOR AND NEW DETECTOR OPS CHECKED GOOD. 2 L 7 3 4F A22WE 1996032200135 19960322 00135 WP 1996 3 22 96ZZZX1174 1 19960226 A 5320 TEAR STRAP LKHEED 1011 10113851 5265010 WP BS 1555 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 300AW 193P1134 LEVEL 2 CORROSION, C2 CARGO TEAR STRAP LIFTING AT FS 1555 BETWEEN STR 39 AND STR 40. REMOVED CORROSION AND REPAIRED PER SRM 53-31-00. 2 L 7 3 4F A23WE 1996032200136 19960322 00136 WP 1996 3 22 96ZZZX1175 1 19960226 A 5330 SKIN LKHEED 1011 10113851 5265010 WP BS 1536 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 300AW 193P1134 LEVEL 2 CORROSION, LOWER AFT FUSELAGE SKIN HAS INTERNAL CORROSION WITH BULGING SKIN AND CRACKED RIVET HEADS AT ST1536 FR OM STR 33 TO STR 35L. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-31-00. 2 L 7 3 4F A23WE 1996032200137 19960322 00137 WP 1996 3 22 96ZZZX1176 1 19960227 A 5330 SKIN LKHEED 1011 10113851 5265010 WP BS 639-886 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 300AW 193P1134 LEVEL 2 CORROSION, BELLY SKIN HAS SEVERAL AREAS OF CORROSION FROM STA 639 TO STA 886 BETWEEN STR 31R AND STR 35L. REMOV ED DAMAGED AREAS, FABRICATED AND INSTALLED REPAIRS PER SRM 53-31-00. 2 L 7 3 4F A23WE 1996032200138 19960322 00138 WP 1996 3 22 96ZZZX1177 1 19960227 A 5330 SKIN LKHEED 1011 10113851 5265010 WP BS 639-883 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 300AW 193P1134 LEVEL 2 CORROSION, SEVERAL AREAS OF CORROSION ALONG BELLY SKIN FROM STA 639 TO STA 883 BETWEEN STR 31R AND 35L. REMOVED AND REPLACED DAMAGED AREAS PER SRM 51-33-00. 2 L 7 3 4F A23WE 1996032200139 19960322 00139 WP 1996 3 22 96ZZZX1178 1 19960227 A 5320 TEAR STRAP LKHEED 1011 10113851 5265010 WP BS 1555 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 300AW 193P1134 LEVEL 2 CORROSION, C2 CARGO TEAR STRAP LIFTING AT FS 1555 BETWEEN STR 39 AND STR 40. REMOVED CORROSION AND REPAIRED PER SRM 53-31-00. 2 L 7 3 4F A23WE 1996032200140 19960322 00140 WP 1996 3 22 96ZZZX1179 1 19960227 A 5313 STRINGER LKHEED 1011 10113851 5265010 WP BS 643 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 300AW 193P1134 LEVEL 2 CORROSION, C1 CARGO COMPARTMENT AT STA 643, STR 31, HAS CORROSION. REMOVED AND REPLACED DAMAGED SECTION OF STRI NGER. 2 L 7 3 4F A23WE 1996032200141 19960322 00141 WP 1996 3 22 96ZZZX1180 1 19960227 A 5313 STRINGER LKHEED 1011 10113851 5265010 WP BS 629-649 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 300AW 193P1134 LEVEL 2 CORROSION, C1 CARGO COMPARTMENT HAS CORROSION ON STR 32 BETWEEN FS 629 AND FS 649. REMOVED AND REPLACED SECTION OF STRINGER. 2 L 7 3 4F A23WE 1996032200142 19960322 00142 WP 1996 3 22 96ZZZX1181 1 19960227 A 5320 SUPPORT LKHEED 1011 10113851 5265010 WP BS 1463-1480 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 300AW 193P1134 LEVEL 2 CORROSION, C2 CARGO FLOOR SUPPORT BETWEEN FS 1463 AND FS 1480, LEFT SIDE AT LBL 48 HAS CORROSION. REMOVED DAMAG ED AREA, FABRICATIONED AND INSTALLED REPAIR PER SRM 51-50-0. 2 L 7 3 4F A23WE 1996032200143 19960322 00143 WP 1996 3 22 96ZZZX1182 1 19960227 A 5320 SUPPORT LKHEED 1011 10113851 5265010 WP BS 1525 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 300AW 193P1134 LEVEL 2 CORROSION, CENTER CARGO COMPARTMENT HAS CORROSION AROUND NUTPLATE AT LONGITUDINAL FLOOR SUPPORT AT RBL, 36 INCHE S FORWARD OF FLOOR SUPPORT BEAM AT STA 1525. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 51-50-02. 2 L 7 3 4F A23WE 1996032200144 19960322 00144 WP 1996 3 22 96ZZZX1183 1 19960227 A 5320 STRAP LKHEED 1011 10113851 5265010 WP BS 1625 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 300AW 193P1134 LEVEL 2 CORROSION, C3 CARGO COMPARTMENT FORWARD BULKHEAD AT STA 1625. STRAP ALONG LOWER SIDE AT FLOOR LEVEL CORRODED. R EMOVED AND REPLACED LOWER STRAP PER SRM 51-50-00. 2 L 7 3 4F A23WE 1996032200152 19960322 00152 NM 1996 3 22 96ZZZX1191 1 19960208 A 5320 GUSSET BOEING 727 727231 1384079 NM FS 825.95 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 64339 20844 JFK - DURING CHECK C-4D, FOUND A 1.25 INCH VERTICAL CRACK IN LT SIDE OF FUSELAGE FRAME GUSSET, STA 825.95. REPAIRED PER SB 727-53-0197. AIRCRAFT TT: 53,646 HRS; 35,058 CYCLES. 2 L 7 3 4F A3WE 1996032200153 19960322 00153 NM 1996 3 22 96ZZZX1192 1 19960203 A 3350 3350002541 LIGHT TRACK BOEING 727 727231 1384079 NM CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 54337 20491 STL - FLT 123 - DURING PREFLIGHT, FOUND FIRST CLASS EGRESS LIGHTS INOPERATIVE. FOUND CAP STRIP, MFG PN 3350-0025-40, CA ME LOOSE FROM LIGHT TRACK. REINSTALLED CAP STRIP IN TRACK AND EGRESS LIGHTS. OPERATION CHECKED NORMAL. CHECK C-2 - 9- 13-95 - MCI. 2 L 7 3 4F A3WE 1996032200154 19960322 00154 WP 1996 3 22 96ZZZX1193 1 19960123 A 2612 5938323505 FIRE LOOP A DOUG DC9 DC983 3022083 WP RT ENGINE CHAFED WIRE A TWAA O OTHER N FALSE WARNING CL CLIMB 1 CE 05 9302B 49528 MCI - FLT 1159 - DURING CLIMB, RT ENGINE 'B' FIREWARNING LOOP FLICKERED ON, SWITCHED TO 'A' LOOP. AFTER LEVEL-OFF AT CR UISE, 'A' LOOP WARNING CAME ON AND WENT OFF. FOUND LOWER APRON 'A' AND 'B' LOOPS CHAFED. REPLACED 'A' AND 'B' APRON LO OPS, MFG PN 5938323-505 AND PN 5938323-506, AND FIREWARNING SYSTEM OPERATION CHECKED NORMAL. CHECK C-2D - 11-15-95 - MC I. REFERENCE: OPERATOR CONTROL NR 96ZZZX1194. 2 L 7 2 4F RT A6WE 1996032200155 19960322 00155 WP 1996 3 22 96ZZZX1194 1 19960123 A 2612 5938323506 FIRE LOOP B DOUG DC9 DC983 3022083 WP RT ENGINE CHAFED WIRE A TWAA O OTHER N FALSE WARNING CL CLIMB 1 CE 05 9302B 49528 MCI - FLT 1159 - DURING CLIMB, RT ENGINE 'B' FIREWARNING LOOP FLICKERED ON, SWITCHED TO 'A' LOOP. AFTER LEVEL-OFF AT CR UISE, 'A' LOOP WARNING CAME ON AND WENT OFF. FOUND LOWER APRON 'A' AND 'B' LOOPS CHAFED. REPLACED 'A' AND 'B' APRON LO OPS, MFG PN 5938323-505 AND PN 5938323-506, AND FIREWARNING SYSTEM OPERATION CHECKED NORMAL. CHECK C-2D - 11-15-95 - MC I. REFERENCE: OPERATOR CONTROL NR 96ZZZX1193. 2 L 7 2 4F RT A6WE 1996032200156 19960322 00156 NM 1996 3 22 96ZZZX1195 1 19960224 A 3230 69141065 TRANSFER CYL BOEING 727 727231 1384079 NM NLG MALFUNCTIONED A TWAA O OTHER J WARNING INDICATION AP APPROACH 1 CE 05 64319 20052 LGA - FLT 460 - DURING APPROACH WHEN LANDING GEAR EXTENDED, NLG DID NOT EXTEND. CYCLED LANDING GEAR. FOUND NLG HYDRAUL IC TRANSFER CYLINDER NOT OPERATING PROPERLY. REPLACED NLG HYDRAULIC TRANSFER CYLINDER, MFG PN 69-14106-5. NLG OPERATIO N THEN CHECKED NORMAL. CHECK C-2 - 1-18-96. MCI. 2 L 7 3 4F A3WE 1996032200157 19960322 00157 NM 1996 3 22 96ZZZX1196 1 19960224 A 3260 DOOR SWITCH BOEING 727 727231 1384079 NM RT MLG DIRTY A TWAA O OTHER N FALSE WARNING CL CLIMB 1 CE 05 54352 21984 DTW - FLT 220 - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, RT MLG AND DOOR LIGHTS REMAINED ILLUMINATED. CYCLED LAND ING GEAR. FOUND RT MLG DOOR SWITCH AND TARGET DIRTY. CLEANED DOOR SWITCH AND TARGET. DOOR LIGHT INDICATION THEN CHECK ED NORMAL. CHECK C - 4-9-95 - MCI. 2 L 7 3 4F A3WE 1996032200158 19960322 00158 NM 1996 3 22 96ZZZX1197 1 19960223 A 3230 RETRACT MECH BOEING 727 727231 1384079 NM NLG LACK OF LUBE A TWAA O OTHER J WARNING INDICATION AP APPROACH 1 CE 05 64319 20052 LGA - FLT 300 - DURING APPROACH WHEN LANDING GEAR EXTENDED, NLG DID NOT EXTEND. CYCLED LANDING GEAR. LUBRICATED NLG TR UNNION, BEARINGS AND DRAG BRACE. NLG OPERATION THEN CHECKED NORMAL. CHECK C-2 - 1-18-96 - MCI. 2 L 7 3 4F A3WE 1996032200159 19960322 00159 NM 1996 3 22 96ZZZX1198 1 19960225 A 3230 65404676 RELEASE ACTUATOR BOEING 727 727231 1384079 NM NLG FAILED A TWAA O OTHER J WARNING INDICATION AP APPROACH 1 CE 05 64319 20052 LGA - FLT 396 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, NLG DID NOT EXTEND. CYCLED LANDING GEAR. FOUND NLG LOC K RELEASE ACTUATOR BYPASSING HYDRAULIC PRESSURE. REPLACED NLG HYDRAULIC LOCK RELEASE ACTUATOR, MFG PN 65-40467-6. NLG OPERATION THEN CHECKED NORMAL. CHECK C-2 - 1-18-96 - MCI. 2 L 7 3 4F A3WE 1996032200160 19960322 00160 WP 1996 3 22 96ZZZX1199 1 19960224 A 2530 958000119 SERVING CART LKHEED 1011 10113851 5265010 WP CABIN FAILED A TWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 31023 193B1080 JFK - FLT 148 - DURING CRUISE, SERVING CART, SN 1482, EMITTED AN ELECTRICAL ODOR. DISCONNECTED SERVING CART. FOUND BAD HEATING PADS. REPLACED SERVING CART, MFG PN 958000-119. NEW SERVING CART OPERATION CHECKED NORMAL. CHECK C-11A - 11- 29-95 - LAX. 2 L 7 3 4F A23WE 1996032200161 19960322 00161 NM 1996 3 22 96ZZZX1200 1 19960225 A 3233 651783013 ACTUATOR BOEING 727 727231 1384079 NM RT MLG FAILED A TWAA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 54352 21984 STL - FLT 385 - AFTER TAKEOFF WHEN LANDING GEAR RETRACTED, RT MLG AND DOOR LIGHTS REMAINED ILLUMINATED. CYCLED LANDING GEAR. FOUND RT MLG HYDRAULIC ACTUATOR MALFUNCTION. REPLACED RT MLG ACTUATOR, MFG PN 65-17830-13. RT MLG OPERATION AND INDICATION THEN CHECKED NORMAL. CHECK C - 4-9-95 - MCI. 2 L 7 3 4F A3WE 1996032200162 19960322 00162 NM 1996 3 22 96ZZZX1201 1 19960223 A 3260 43410332203 IND LIGHT SOCKET BOEING 767 767231 1385131 NM RT MLG BROKEN A TWAA O OTHER P NO WARNING INDICATION AP APPROACH 1 CE 05 610TW 22573 MXP - FLT 843 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, RT MLG DID NOT INDICATE DOWN AND LOCKED. CYCLED LANDING GEAR. FOUND RT MLG GREEN INDICATOR LIGHT SOCKET, MFG PN 434-1033-2203, BROKEN. REPLACED LIGHT SOCKET AND LANDING GEAR INDCATION CHECKED NORMAL. CHECK C-5A - 1-24-96 - LAX. 2 L 7 2 4F RT A1NM 1996032200163 19960322 00163 WP 1996 3 22 96ZZZX1202 1 19960220 A 5320 JAMB DOUG DC9 DC982 3022082 WP CARGO DOOR CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 902TW 49153 MCI - DURING OP-15, FOUND CORROSION ON AFT CARGO DOOR JAMB LOWER BEAM. REPLACED BEAM PER SRM 51-01, PAGE 1, ITEM C. AI RCRAFT TT: 39,822 HRS; 20,932 CYCLES. 2 L 7 2 4F A6WE 1996032200164 19960322 00164 NE 1996 3 22 96ZZZX1203 2 19960217 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE LEFT FAILED A TWAA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 CE 05 952U 49266 STL - FLT 414 - DURING CLIMB, LT ENGINE SURGED ACCOMPANIED WITH A DROP IN EPR. SHUT DOWN LT ENGINE, SN 3201. FOUND MET AL PARTICLES IN TAILPIPE AND TURBINE BLADE DAMAGE. CHANGED LT ENGINE AND ENGINE OPERATION CHECKED NORMAL. ENGINE TOTAL TIME: 31,874 HRS; 16,491 CYCLES. CHECK C-1D - 8-21-95 - MCI. 2 L 7 2 4F 4 F A6WE E9NE 1996032200165 19960322 00165 WP 1996 3 22 96ZZZX1204 1 19960217 A 3350 58541 CONNECTOR DOUG DC9 DC931 3022065 WP CABIN DIRTY A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 991Z 47096 STL - DURING ROUTINE MAINTENANCE, FOUND EGRESS LIGHTS SEAT ROWS 21 TO 23 AND TAILCONE PATHWAY, INOPERATIVE. FOUND EGRES S LIGHT CABLE CONNECTOR, MFG PN 5854-1, DIRTY. CLEANED CABLE CONNECTOR AND LIGHT OPERATION CHECKED NORMAL. CHECK C - 9 -2-95 - STL. 2 L 7 2 4F A6WE 1996032200166 19960322 00166 WP 1996 3 22 96ZZZX1205 1 19960211 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 639 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 986Z 47589 STL - DURING OP-15, FOUND .3750 INCH CRACK ON TOP LIP OF LONGERON 7L, STA 639. REPLACED LONGERON SECTION PER SRM 53-02, PAGE 2A, FIGURE 2. AIRCRAFT TT: 54,237 HRS; 59,836 CYCLES. 2 L 7 2 4F A6WE 1996032200168 19960322 00168 SW 1996 3 22 MALA964894 1 19960229 A 3230 RETRACT MECH SWRNGN SA227 SA227AC 8780603 SW NLG LACK OF LUBE A MALA O OTHER J WARNING INDICATION AP APPROACH 1 GL 15 423MA AC636 DTW - FLT 3386 - ON APPROACH TO DTW THE NOSE GEAR WAS SLOW TO SHOW DOWN AND LOCKED AFTER GEAR EXTENSION. MAINTENANCE WA S UNABLE TO DUPLICATE THE DISCREPANCY. AS A PRECAUTION, THE NOSE GEAR AND POSITION SWITCHES WERE CLEANED AND LUBED. (X ) 1 L 7 2 4T A8SW 1996032200169 19960322 00169 WP 1996 3 22 VTZA96096 2 19960227 A 7321 89778025 FUEL CONTL UNIT BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE331* 01514 WP RT ENGINE FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 482UE 8919 2704 897 P66205 IAD/PIT - FLT 36332 - DURING TAKEOFF AT 1730 HRS ON 2-27-96, ABORTED TAKEOFF DUE TO RT ENGINE TORQUE FLUCTUATING FROM 90 PERCENT TO 100 PERCENT. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED RT FUEL CONTROL UNI T. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T 3 T RT A56EU E2WE 1996032200170 19960322 00170 EU 1996 3 22 VTZA96098 1 19960227 A 3610 1379254L402 DUCTING BAG JETSTM JETSTM3201 1500217 EU RT STUB WING DISCONNECTED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 471UE 821 IAD/CRW - FLT 6378 - DURING CRUISE, AT 1845 HRS ON 2-27-96, RETURNED TO IAD DUE TO CABIN DEPRESSURIZING. AIRCRAFT LANDE D AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE RESECURED THE LOOSE ACM DUCTING ON THE RT ACM. AIRCRAFT RELEASED AND A PPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1996032200171 19960322 00171 WP 1996 3 22 9606129962 1 19960311 A 5711 SPAR CAP DOUG DC9 DC931 3022065 WP WS 530 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 914RW 47362 DURING PERIODIC CHECK, FOUND LEFT WING OUTBOARD AFT TOP SPAR CAP CORRODED AT WS XFS 530. INSTALLED REPAIR PER EA 99-109 480. 2 L 7 2 4F A6WE 1996032200172 19960322 00172 WP 1996 3 22 9606131220 1 19960315 A 2424 976J86215 GEN CONTL UNIT DOUG DC10 DC1030 3023501 WP NR 2 FAILED A NWAA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 GL 01 220NW 46577 DURING CRUISE, LOST THE NR 2 AC BUS AND DC BUS, FOLLOWED COM PROCEDURES AND DIVERTED TO KIX. MAINTENANCE REPLACED THE N R 2 GENERATOR CONTROL UNIT. 2 L 7 3 4F A22WE 1996032200173 19960322 00173 NM 1996 3 22 9606145507 1 19960317 A 3350 20131A BATTERY PACK BOEING 757 757251 1384970 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 507US 23196 DURING LINE CHECK, FOUND OVERHEAD EMERGENCY LIGHTS AT ROW 1 THROUGH 14 AND EXTERIOR LIGHT AT DOOR 1R AND 1L INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACKS M730 AND M731, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A2NM 1996032200174 19960322 00174 1996 3 22 9606159947 4 19960315 A 3418 STALL WARN COMP DOUG DC9 DC931 3022065 WP NR 2 FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 8938E 47161 STALL WARNING INDICATION FAILURE LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. R EPLACED NR 2 STALL WARNING COMPUTER AND TONE GENERATOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996032200175 19960322 00175 WP 1996 3 22 9606169102 1 19960317 A 3260 SWITCH DOUG DC9 DC915 3022036 WP NLG FAILED A NWAA O OTHER P NO WARNING INDICATION DE DESCENT 1 GL 01 92S 47064 DURING DESCENT INTO MSP, NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE. RECYCLED GEAR AND GREEN LIGHT INDICATED NORMAL. AIR CRAFT LANDED WITHOUT INCIDENT. REPLACED UP-LIMIT AND DOWN AND LOCKED SWITCHES, GEAR OPERATIONAL CHECKED GOOD. 2 L 7 2 4F A6WE 1996032200176 19960322 00176 WP 1996 3 22 9606179605 1 19960315 A 3260 SOCKET DOUG DC9 DC932 3022066 WP LT MLG SHORTED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 605NW 47223 DURING CLIMBOUT AT APPROXIMATELY 28,000 FEET, THE LEFT MAIN LANDING GEAR GREEN LIGHT ILLUMINATED. NO VIBRATION OR YAW W AS FELT. HYDRAULIC PUMP WAS SWITCHED TO HIGH WITH NO CHANGE. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. LIGH T REMAINED ON THROUGHOUT GEAR EXTENSION WITH NO FLICKERING. MAINTENANCE FOUND LEFT MAIN GEAR GREEN LIGHT SOCKET SHORTIN G TO GROUND. REPLACED SOCKET AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996032200177 19960322 00177 NM 1996 3 22 9606186739 1 19960313 A 5347 SEAT TRACK BOEING 747 747251F 1384898 NM FS 1260-1300 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 639US 23887 DURING PERIODIC CHECK, FOUND CORROSION ON INBOARD FLANGE OF SEAT TRACK AT BS 1260 TO 1300, RBL 11. CUT OUT DAMAGED AREA S AND INSTALLED .125 7075-T6 ANGLE REPAIR PER EA 67-99582. 2 L 7 4 4F A20WE 1996032200178 19960322 00178 WP 1996 3 22 9606199607 1 19960317 A 3260 DNLOCK SWITCH DOUG DC9 DC932 3022066 WP NLG MALFUNCTIONED A NWAA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 01 607NW 47232 NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE ON APPROACH INTO GFK. RECYCLED GEAR AND NORMAL INDICATIONS WERE ACHIEV ED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSE LANDING GEAR DOWNLOCK SWITCH, OPERATIONAL CHECK NO RMAL ON GEAR SWING. 2 L 7 2 4F A6WE 1996032200179 19960322 00179 WP 1996 3 22 ABXA9600309 1 19960313 A 2910 4765599 BULKHEAD FITTING DOUG DC8 DC862 3021970 WP NR 2 ENGINE LEAKING A ABXA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 GL 23 801AX 46077 HYDRAULIC QUANTITY GAUGE INDICATION BEGAN DECREASING DURING DESCENT. EMERGENCY CHECKLIST WAS ACCOMPLISHED. HYDRAULIC FLUID QUANTITY STABILIZED AT THE STANDPIPE LEVEL. REPLACED NR 2 ENGINE HYDRAULIC PRESSURE LINE BULKHEAD FITTING. GROUN D RAN ENGINE AND LEAK CHECK WAS GOOD. SERVICED HYDRAULIC RESERVOIR. 2 L 7 4 4F 4A25 1996032200180 19960322 00180 WP 1996 3 22 ABXA9600310 1 19960314 A 3040 WB0340 TERMINAL BLOCK DOUG DC9 DC932 3022066 WP RT WINDSHIELD DIRTY A ABXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 23 987AX 47364 AFTER TAKEOFF, A BRIGHT FLASH AND POPPING SOUND OCCURED ON FIRST OFFICERS SIDE OF COCKPIT. ELECTRICAL SMOKE WAS SMELLED . AFTER LANDING, RIGHT WINDSHIELD HEAT CIRCUIT BREAKER WAS POPPED. CLEANED THE DIRTY TERMINAL BLOCK AT THE FIRST OFFI CERS WINDSHIELD. 2 L 7 2 4F A6WE 1996032200181 19960322 00181 WP 1996 3 22 ARWA9603007 1 19960317 A 7931 42D491C DIFF OIL SWITCH DOUG DC8 DC863F 302198F WP NR 4 ENGINE CRACKED A ARWA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 19 661AV 45969 AIRCRAFT DEPARTED MAO 1200Z, AT 1412Z PRECAUTIONARY INFLIGHT SHUTDOWN OF NR 4 ENGINE DUE TO FLUCTUATING OIL PRESSURE BEL OW 35 PSI, OIL PRESSURE LIGHT ILLUMINATED AND OIL QUANTITY DECREASED TO ONE GALLON. CONTINUED ON TO MIAMI. FOUND DIFFE RENTIAL OIL PRESSURE SWITCH CRACKED. REMOVED AND REPLACED PRESSURE SWITCH AS PER MM 79-30-00, OPS AND LEAK CHECKED NORM AL. 2 L 7 4 4F 4A25 1996032200182 19960322 00182 NE 1996 3 22 DHL96802001 2 19960307 A 7320 FLIGHT IDLE DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C1 13802 NE NR 1 ENGINE OUT OF ADJUST A T DHLA O OTHER X ENGINE FLAMEOUT DE DESCENT 1 SO 01 802DH 46076 692403 NUMBER ONE ENGINE FLAMED OUT ON DESCENT INTO BRUSSELS, NO FUEL FLOW INDICATED AND NO ATTEMPT WAS MADE TO RESTART. ADJUS TED FLIGHT IDLE PER 73-21-10 TO 74.5 N2, RAN ENGINE AND OPERATIONS CHECKED OKAY PER 71-00-00. 2 L 7 4 4F 4 F RT 4A25 E2GL 1996032200183 19960322 00183 NE 1996 3 22 P5CA9600160 2 19960316 A 7530 BACH7A01363AR PRBC LINE BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE NR 4 ENGINE LEAKING A P5CA E ENGINE SHUTDOWN Y J ENGINE STOPPAGE WARNING INDICATION DE DESCENT 1 WP 23 858FT 20109 662964 AT TOP OF DESCENT, NR 4 ENGINE COMPRESSOR STALLED WITH EGT RISE, SHUTDOWN ENGINE AND RESTARTED. ENGINE STARTED AND STAB ILIZED NORMALLY, USED ENGINE FOR REMAINDER OF FLIGHT, OPS NORMAL. PERFORMED BLEED CHECK, BORESCOPE AND PT2 LEAK CHECK, FOUND FLEX LINE FROM PRBC LEAKING. REPLACED SAME IAW MM 77-11-03, OPS CHECK NORMAL. 2 L 7 4 4F 4 F A20WE E20EA 1996032200184 19960322 00184 NM 1996 3 22 P5CA9600161 1 19960317 A 7830 TR UNIT BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE NR 3 ENGINE MALFUNCTIONED A P5CA K NONE J WARNING INDICATION LD LANDING 1 WP 23 859FT 20326 662258 NR 3 ENGINE OVERTEMPED IN REVERSE, EGT REACHED 920 DEGREES. VISUALLY INSPECTED ENGINE INTAKE AND TAILPIPE, NO DAMAGE FO UND. REVERSER DEACTIVATED, PENDING RABS SYSTEM CHECK AT JFK. 2 L 7 4 4F 4 F A20WE E20EA 1996032200185 19960322 00185 NM 1996 3 22 P5CA9600162 1 19960317 A 3246 260356116I RETENTION SCREWS BOEING 747 747122 1384872 NM NR 10 WHEEL LOOSE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 FOUND NR 10 WHEEL ASSEMBLY ALIGNMENT KEYS MIGRATED DUE TO LOOSE/MISSING RETENTION SCREWS, CAUSED DAMAGE TO BRAKE ASSEMBL Y. REMOVED AND REPLACED NR 10 WHEEL ASSEMBLY PER MM 32-45-01. REMOVED AND REPLACED BRAKE ASSEMBLY PER MM 32-41-15. BR AKE ASSEMBLY (P/N 2601902-60) (S/N B0903). 2 L 7 4 4F A20WE 1996032200186 19960322 00186 EU 1996 3 22 QXEA9600104 1 19960312 A 3310 56140BVL2 BALLAST FOKKER F28 F28MK1000 4990808 EU COCKPIT SHORTED A QXEA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 801PH 11097 STRONG ELECTRICAL BURNT SMELL IN COCKPIT. MAIN INSTRUMENT LIGHTING CIRCUIT BREAKER PULLED AND COLLARED. REPLACED BALLA ST LG-16D, ALL BULBS AND LIGHTING OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996032200187 19960322 00187 EU 1996 3 22 QXEA9600105 1 19960312 A 2560 0598011003 SLIDE COVER FOKKER F28 F28MK1000 4990808 EU EMER EXIT OUT OF POSITION A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 452US 11105 FORWARD EMERGENCY EXIT SLIDE PINS PULLED AND STOWED IMPROPERLY. WATER PUMP COVER FOUND IN UP POSITION. CLOSED COVER AN D RESTOWED SLIDE. 2 L 7 2 4F RT A20EU 1996032200188 19960322 00188 EU 1996 3 22 QXEA9600106 1 19960313 A 3350 1312 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 801PH 11097 EXIT LIGHTS ON THE OVERWING EXIT ARE INOP. BULBS WERE REPLACED AND LIGHTS OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996032200189 19960322 00189 NM 1996 3 22 QXEA9600107 1 19960313 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT MISINSTALLED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 841PH 82 COCKPIT OVERHEAD EMERGENCY LIGHT IS ON BRIGHT WHEN IN THE MOUNTING BRACKET AND ENGINES ARE RUNNING. LIGHT DOESN'T COME ON WHEN EMERGENCY LIGHTS ARE TURNED ON. LIGHT REMOVED AND REINSTALLED CORRECTLY, LIGHT OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 1996032200190 19960322 00190 EU 1996 3 22 QXEA9600108 1 19960317 A 3350 1820 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 464US 11063 THE 28V EMERGENCY LIGHT AT LEFT OVERWING EXIT INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996032200191 19960322 00191 EU 1996 3 22 QXEA9600109 1 19960317 A 3350 5515800104 CIRCUIT BOARD FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 468US 11095 EXIT SIGN ON FORWARD CABIN BULKHEAD IS DIM. CIRCUIT BOARD REPLACED AND SIGN OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996032200192 19960322 00192 NM 1996 3 22 QXEA9600110 1 19960317 A 5347 85331040109 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORROSION A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 831PH 328 SEAT TRACK (P/N 85331040109), FOUND CORRODED DURING C-CHECK. NEW SEAT TRACK INSTALLED IAW SRM. 2 H 7 2 4T RT A13NM 1996032200193 19960322 00193 NM 1996 3 22 QXEA9600111 1 19960317 A 5347 85320490133 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORROSION A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 831PH 328 LEFT FORWARD CENTER SEAT TRACK HAS CORROSION UNDER WARDROBE FLOOR, CORROSION NOTED DURING C-CHECK. NEW SEAT TRACK INSTA LLED IAW SRM. 2 H 7 2 4T RT A13NM 1996032200194 19960322 00194 NM 1996 3 22 96ZZZX1226 1 19960125 A 2530 SERVING CART BOEING 767 767231 1385131 NM NR 2 GALLEY SMOKING A TWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 607TW 22570 JFK - FLT 903 - DURING CRUISE, NR 2 AFT GALLEY SERVING CART EMITTED SMOKE WHEN TURNED ON. REMOVED AND REPLACED SERVING CART. OPERATIONAL CHECK NORMAL. CHECK C-6A - 12-7-95 - LAX. 2 L 7 2 4F RT A1NM 1996032200195 19960322 00195 WP 1996 3 22 96ZZZX1227 1 19960127 A 2782 ACTUATORS LKHEED 1011 10113851 5265010 WP LE SLATS FROZEN A TWAA O OTHER J F WARNING INDICATION FLT CONT AFFECTED LD LANDING 1 CE 05 31019 193B1066 STL - DURING LANDING, THE LEADING EDGE SLATS WERE FROZEN AND WOULD NOT DEPLOY. LEADING EDGE SLAT ACTUATORS AND JACKSCRE WS WERE THAWED, LUBRICATED AND SERVICED. LEADING EDGE SLATS WERE CYCLED NUMEROUS TIMES, OPERATION NORMAL. 2 L 7 3 4F A23WE 1996032200196 19960322 00196 WP 1996 3 22 96ZZZX1228 1 19960128 A 3222 A03772REVH STRUT SEAL DOUG DC9 DC982 3022082 WP NLG FAILED A TWAA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 950U 49230 STL - AFTER TAKEOFF, NOSE GEAR FAILED TO RETRACT. IT WAS DETERMINED THE NOSE GEAR WAS DOWN ALND LOCKED. REMOVED AND RE PLACED NOSE GEAR SEAL KIT, MFG PN A03772REVH. GEAR SWING CHECKED NORMAL. CHECK C-1D - 4-13-95 - MCI. 2 L 7 2 4F A6WE 1996032200197 19960322 00197 WP 1996 3 22 96ZZZX1229 1 19960127 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 242 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 956U 49701 STL - DURING CHECK 'C', FOUND SCRAPE ON FUSELAGE, STA 242, LONGERON 17L. REPAIRED FUSELAGE DAMAGE PER SRM 53-04, FIGURE 38, SHEET 20 AND SRM 53-02, FIGURE 2. AIRCRAFT TT: 24,501 HRS; 12,379 CYCLES. 2 L 7 2 4F A6WE 1996032200199 19960322 00199 WP 1996 3 22 96ZZZX1231 1 19960203 A 3222 B050762 SCHRADER VALVE DOUG DC9 DC931 3022065 WP NLG ICED UP A TWAA O OTHER N FALSE WARNING CL CLIMB 1 CE 05 978Z 47250 STL - FLT 585 - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, NLG UNSAFE RED LIGHT REMAINED ILLUMINATED WITH INTERMITTE NT WARNING HORN. CYCLED LANDING GEAR. FOUND ICE IN NLG STRUT SCHRADER VALVE, MFG PN B05076-2. REPLACED SCHRADER VALVE , SERVICED NOSE STRUT WITH OIL AND NITROGEN AND LANDING GEAR INDICATION CHECKED NORMAL. CHECK C - 12-22-95 - STL. 2 L 7 2 4F A6WE 1996032200200 19960322 00200 NM 1996 3 22 96ZZZX1232 1 19960202 A 7830 R1409M131 ACTUATOR BOEING 747 747131 1384881 NM NR 3 ENGINE FAILED A TWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 05 93104 19670 JFK - FLT 12 - DURING TAKEOFF ROLL, NR 3 ENGINE THROTTLE WOULD NOT ADVANCE. REMOVED AND REPLACED THRUST REVERSER SEQUEN CE ACTUATOR, MFG PN R1409M13-1. OPERATIONAL CHECK NORMAL. CHECK C-2 - 10-23-95 - JFK. 2 L 7 4 4F A20WE 1996032200201 19960322 00201 WP 1996 3 22 96ZZZX1233 1 19960206 A 3222 SCHRADER VALVE DOUG DC9 DC982 3022082 WP NLG STRUT MALFUNCTIONED A TWAA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 915TW 49186 PKX - FLT 205 - AFTER TAKEOFF, NLG DID NOT RETRACT. FOUND NLG INFLATION LOW. REPLACED SHRADER VALVE, MFG PN B05076-2, AND SERVICED NLG. NLG INDICATION AND OPERATION THEN CHECKED NORMAL. CHECK C-1D - 2-27-95 - MCI. 2 L 7 2 4F A6WE 1996032200202 19960322 00202 NM 1996 3 22 96ZZZX1234 1 19960206 A 7920 OIL LINE SEAL BOEING 727 727231 1384079 NM NR 2 ENGINE LEAKING A TWAA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 05 54325 20232 MCI - FLT 475 - DURING CRUISE, SHUT DOWN NR 2 ENGINE, SN 3921, DUE TO LOSS OF OIL QUANTITY. FOUND OIL LEAK AT FUEL OIL COOLER LINE. REPLACED OIL LINE SEAL, MFG PN 443330, AND RETAINER, MFG PN 354117; ENGINE LEAK CHECK AND OPERATION WAS NO RMAL. ENGINE TT: 57,657 HRS; 38,613 CYCLES. CHECK C-3 - 4-8-95 - MCI. 2 L 7 3 4F A3WE 1996032200203 19960322 00203 NE 1996 3 22 96ZZZX1235 2 19960209 A 7230 COMPRESSOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE NR 1 ENGINE STALLED A TWAA E ENGINE SHUTDOWN E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 CE 05 959U 49704 IND - FLT 160 - DURING CLIMB, SHUT DOWN NR 1 ENGINE, SN 3245, DUE TO VIBRATION AND COMPRESSOR STALLS. DURING GROUND RUN , ENGINE HAD OFF IDLE STALLS. REPLACED ENGINE AND OPERATONAL CHECKS WERE NORMAL. ENGINE TT: 26,119 HOURS; 13,618 CYCL ES. CHECK C-1D - 7-28-95 - MCI. 2 L 7 2 4F 4 F A6WE E9NE 1996032200204 19960322 00204 NE 1996 3 22 96ZZZX1236 2 19960203 A 7321 76960616 FUEL CONTROL DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 2 ENGINE FAILED A TWAA E ENGINE SHUTDOWN Y J ENGINE STOPPAGE WARNING INDICATION AP APPROACH 1 CE 05 912TW 49183 STL - FLT 296 - DURING APPROACH, NR 2 ENGINE, SN 3232, SPUN DOWN. COMPLETED SHUTDOWN CHECKLIST. FOUND INTERNAL MALFUNC TION IN FUEL CONTROL, MFG PN 769606-16. REPLACED FUEL CONTROL AND ENGINE OPERATION CHECKED NORMAL. ENGINE TT: 31,831 HOURS; 16,687 CYCLES CHECK C-1 - 10-12-95 - MCI. 2 L 7 2 4F 4 F A6WE E9NE 1996032200205 19960322 00205 WP 1996 3 22 96ZZZX1237 1 19960124 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 699 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 991Z 47096 STL - DURING CHECK 'C', FOUND .50 INCH CRACK IN LOWER FLANGE OF LONGERON 7L, STA 699. REPAIRED PER SRM 53-02, FIGURE 2A . AIRCRAFT TT: 63,390 HOURS; 75,098 CYCLES. 2 L 7 2 4F A6WE 1996032200206 19960322 00206 WP 1996 3 22 96ZZZX1238 1 19960124 A 5320 BELT RING DOUG DC9 DC931 3022065 WP FS 718 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 991Z 47096 STL - DURING CHECK 'C', FOUND .50 INCH CRACK AT BOTH ATTACH POINTS TO BELT RING, LONGERON 6R, STA 718. REPAIRED PER SRM 53-02, FIGURE 2A. AIRCRAFT TT: 68,390 HRS; 75,098 CYCLES. 2 L 7 2 4F A6WE 1996032200207 19960322 00207 WP 1996 3 22 96ZZZX1239 1 19960124 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 737 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 991Z 47096 STL - DURING CHECK 'C', FOUND .50 INCH CRACK IN LONGERON 4L, LOWER LEG, STA 737. REPAIRED PER SRM 53-02, FIGURE 2A. AI RCRAFT TT: 63,390 HOURS; 75,098 CYCLES. 2 L 7 2 4F A6WE 1996032200208 19960322 00208 1996 3 22 96ZZZX1240 4 19960126 A 2210 2589445933 ACTUATOR DOUG DC9 DC951 3022051 WP YAW DAMPER FAILED A TWAA O OTHER O OTHER CL CLIMB 1 CE 05 410EA 47731 STL - FLT 503 - DURING CLIMB, UNCOMMANDED RUDDER MOVEMENT WAS DETECTED. REMOVED AND REPLACED YAW DAMPER ACTUATOR DUE TO INTERNAL FAILURE, MFG PN 2589445-933. OPERATIONAL CHECK NORMAL. CHECK C-12 - 1-11-95 - STL. 2 L 7 2 4F A6WE 1996032200209 19960322 00209 NM 1996 3 22 96ZZZX1241 1 19960131 A 3350 6104783 BATTERY PACK BOEING 727 727231 1384079 NM CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 54348 21967 STL - DURING LAYOVER MAINTENANCE, LT OVERWING EMERGENCY EXIT LIGHT FOUND INOPERATIVE. REMOVED AND REPLACED EMERGENCY LI GHT BATTERY PACK, MFG PN 61-0478-3. OPERATIONAL CHECK NORMAL. CHECK C - 7-20-95 - MCI. 2 L 7 3 4F A3WE 1996032200210 19960322 00210 NE 1996 3 22 96ZZZX1242 2 19960208 A 7200 ENGINE BOEING 747 747156 1384884 NM PWA JT9 JT9D7A 52054 NE NR 1 FAILED A TWAA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 CE 05 134TW 19958 JFK - FLT 884 - DURING CLIMB, SHUT DOWN NR 1 ENGINE, SN 4187, DUE TO COMPRESSOR STALL ACCOMPANIED BY INCREASING EGT AND DECREASING RPM. FOUND METAL PARTICLES IN TAILPIPE. REPLACED ENGINE AND ENGINE OPERATION CHECKED NORMAL. ENGINE TT: 8 0,615 HRS; 14,493 CYCLES. CHECK C-2 - 1-15-96 - JFK. 2 L 7 4 4F 4 F A20WE E20EA 1996032200211 19960322 00211 NM 1996 3 22 96ZZZX1243 1 19960207 A 3260 656021134 WARNING MODULE BOEING 727 727231 1384079 NM LANDING GEAR FAILED A TWAA O OTHER N FALSE WARNING AP APPROACH 1 CE 05 52312 19831 MCI - FLT 117 - DURING APPROACH, LANDING GEAR WARNING HORN SOUNDED; CYCLED GEAR. REMOVED AND REPLACED LANDING GEAR POSI TION WARNING MODULE, MFG PN 65-60211-34. OPERATION NORMAL. CHECK C-3 - 3-24-95 - MCI. 2 L 7 3 4F A3WE 1996032200212 19960322 00212 WP 1996 3 22 96ZZZX1244 1 19960229 A 3222 B050762 SCHRADER VALVE DOUG DC9 DC982 3022082 WP NLG LEAKING A TWAA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 909TW 49170 CMH - FLT 211 - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, NLG DID NOT RETRACT. CYCLED LANDING GEAR. FOUND NLG SCH RADER VALVE LEAKING. REPLACED SCHRADER VALVE, MFG PN B05076-2, AND SERVICED LANDING GEAR. NLG OPERATION CHECKED NORMAL . CHECK C-2D - 4-10-95 - MCI. 2 L 7 2 4F A6WE 1996032200213 19960322 00213 NM 1996 3 22 96ZZZX1245 1 19960114 A 5320 WEB BOEING 727 72723 1384004 NM BS 241 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 59690 19389 DURING C-CHECK, NOSE WHEELWELL, RT SIDE PRESSURE WEB, FOUND CRACKED BELOW ACCESS PANEL, STA 241. CUT OUT DAMAGED AREA A ND INSTALLED EXTERNAL DOUBLER 17 INCHES BY 21 INCHES AT STA 241 PER BOEING SRM 51-40-2. TAT: 59,690.0 HRS. TAC: 43,7 08. 2 L 7 3 4F A3WE 1996032200214 19960322 00214 EU 1996 3 22 AALA960179 2 19960202 A 7310 CASC509 REGULATOR LUCAS FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAYMK65015 EU LT/RT ENGINES DEFECTIVE A A AALA O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 SW 07 1443A 11446 17571 ATL - FLT 0752 - EN ROUTE DFW/ATL DURING CRUISE AT FL 300, NR 1 ENGINE EXPERIENCED TEMPORARY LOSS OF POWER (ROLLBACK) AN D UPON RECOVERY OF POWER TO NR 1 ENGINE, NR 2 ENGINE EXPERIENCED THE SAME EVENT. ENGINE POWER WAS RECOVERED AND AIRCRAF T PROCEEDED TO ATL, LANDING WITHOUT INCIDENT. REPLACED FUEL FLOW REGULATORS ON LT AND RT ENGINES. SYSTEM LEAK AND GROU ND CHECKED, NORMAL OPERATION. ACCOMPLISHED FUNCTIONAL CHECK FLIGHT/FERRY FLIGHT ATL/DFW WITH NO DEFECTS FOUND. SYSTEMS OPERATIONAL CHECKED NORMAL. ENGINE S/N 17571 AND ENGINE S/N 17572. (X) 2 L 7 2 4F 4 F RT 1996032200215 19960322 00215 NM 1996 3 22 AALA960180 1 19960124 A 5312 145T8750 BULKHEAD BOEING 767 767223 1385123 NM BS 957 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 313AA 22316 AFW - FOUND AND BLENDED OUT CORROSION ON THE UPPER SURFACE OF THE MAIN CABIN PRESSURE DECK. BLEND-OUTS EXCEEDED SRM MAX IMUM LIMITS. REMOVED CORROSION, ROTO-PEENED. ALODINED, PRIMED, AND PAINTED. APPROVED BY ENGINEERING WITH NOTED CONDIT ION PER MRB 767-1115. TST: 42,562.49 HRS. CYCLES, 10,821. (X) 2 L 7 2 4F RT A1NM 1996032200216 19960322 00216 NM 1996 3 22 AALA960181 1 19960124 A 5320 146T20031 CHORD BOEING 767 767223 1385123 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 313AA 22316 AFW - OVERSIZED EXISITNG HOLE ON CHORD TO ELIMINATE INNER GRANULAR CORROSION. INSTALLED FREEZE PLUG IN HOLE AFTER DRILL ING. DRILLED NEW HOLE THROUGH FREEZE PLUG. CHORD TO BE REPLACED AT NEXT MBV. APPROVED BY ENGINEERING PER MRB 767-1132 . TST: 42,562.49 HRS. CYCLES, 10,821. (X) 2 L 7 2 4F RT A1NM 1996032200217 19960322 00217 NM 1996 3 22 AALA960182 1 19960124 A 5320 CHORD BOEING 767 767223 1385123 NM BS 1087 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 313AA 22316 AFW - FOUND AND BLENDED OUT CORROSION ON THE UPPER SURFACE OF THE INNER CHORD IN AFT CARGO. PRIMED AND FILLED BLENDED A REA. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1131. TST: 42,562.49 HRS. CYCLES , 10,821. (X) 2 L 7 2 4F RT A1NM 1996032200218 19960322 00218 NM 1996 3 22 AALA960183 1 19960124 A 5315 111T5008 FLOOR BEAM BOEING 767 767223 1385123 NM BS 845 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 313AA 22316 AFW - FLOOR BEAM WEB GOUGED. DAMAGE BLENDED AND FOUND BEYOND SRM LIMITS. FABRICATED AND INSTALLED .071 INCH THICK 7075 -T6 DOUBLER. APPROVED BY ENGINEERING PER MRB 767-1126. TST: 42,562.49 HRS. CYCLES, 10,821. (X) 2 L 7 2 4F RT A1NM 1996032200219 19960322 00219 NM 1996 3 22 AALA960184 1 19960124 A 5320 146T121311 CHORD BOEING 767 767223 1385123 NM BS 1351 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 313AA 22316 AFW - FOUND AND BLENDED OUT CORROSION ON THE UPPER SURFACE OF THE 146T1213-11 INNER CHORD. THE BLEND-OUT EXCEEDS SRM MA XIMUM LIMITS. REFINISHED BLENDED AREA PER SRM. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1123. TST: 42,562 HRS. CYCLES, 10,821. (X) 2 L 7 2 4F RT A1NM 1996032200220 19960322 00220 NM 1996 3 22 AALA960185 1 19960124 A 5315 146T5141 FLOOR BEAM BOEING 767 767223 1385123 NM BS 1480 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 313AA 22316 AFW - FLOOR BEAM CORRODED. AFTER BLENDING, FOUND DAMAGE BEYOND SRM LIMITS. ALODINED BLENDED AREA. FABRICATED AND INST ALLED REPAIR STOP USING .050 INCH 301 1/2 HARD STAINLESS STEEL. APPLIED TWO COATS OF PRIMER. APPROVED BY ENGINEERING P ER MRB 767-1124. TST: 42,562.49 HRS. CYCLES, 10,821. (X) 2 L 7 2 4F RT A1NM 1996032200221 19960322 00221 NM 1996 3 22 AALA960186 1 19960124 A 5315 111T5008 FLOOR BEAM BOEING 767 767223 1385123 NM BS 850-870 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 313AA 22316 AFW - FLOOR BEAM CORRODED AND BLENDED ON THE UPPER OUTER SURFACE. FOUND THE BLEND-OUT EXCEEDED SRM LIMITS. REMOVED FLO OR BEAM SECTION FROM STA 849 TO STA 878. SPLICED IN NEW SECTION. APPROVED BY ENGINEERING PER MRB 767-1119. TST: 42,5 62.49 HRS. CYCLES, 10,821. (X) 2 L 7 2 4F RT A1NM 1996032200222 19960322 00222 NM 1996 3 22 AALA960187 1 19960124 A 5315 111T5007 FLOOR BEAM BOEING 767 767223 1385123 NM BS 859 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 313AA 22316 AFW - FOUND AND REMOVED CORROSION ON FLOOR BEAM. AFTER BLENDING, FOUND BEYOND SRM LIMITS. EDDY CHECKED BLEND-OUTS. RO TO-PEENED AND REFINISHED BLENDED AREAS. APPROVED BY ENGINEERING PER MRB 767-1118. TST: 42,562.49 HRS. CYCLES, 10,821 . (X) 2 L 7 2 4F RT A1NM 1996032200223 19960322 00223 NM 1996 3 22 AALA960188 1 19960124 A 5730 111T3013 SKIN BOEING 767 767223 1385123 NM WING CTR SECTION CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 313AA 22316 AFW - CORROSION REMOVED FROM CENTER WING UPPER SKIN AT AFT DRAINS LOCATIONS. APPROVED AND REPAIRED PER INSTRUCTIONS OF MRB 767-1117. TST: 42,562.49 HRS. CYCLES, 10,821. (X) 2 L 7 2 4F RT A1NM 1996032200224 19960322 00224 NM 1996 3 22 AALA960189 1 19960124 A 5313 140T011516 STRINGER BOEING 767 767223 1385123 NM BS 434 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 313AA 22316 AFW - STRINGER CORRODED. DAMAGE REQUIRED THE REMOVAL OF 2.5 INCHES OF STRINGER AT AFT END OF SPLICE. REMOVED CORROSION . FABRICATED AND INSTALLED NEW REPAIR SPLICE. APPROVED BY ENGINEERING PER MRB 767-1112. TST: 42,562.49 HRS. CYCLES, 10,821. (X) 2 L 7 2 4F RT A1NM 1996032200225 19960322 00225 NM 1996 3 22 AALA960191 1 19960124 A 5320 140T01516 SPLICE BOEING 767 767223 1385123 NM BS 434 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 313AA 22316 AFW - STRINGER CORRODED. DAMAGE REQUIRED REMOVAL OF .90 INCH OF STRINGER AT AFT END OF SPLICE. REMOVED CORROSION. FAB RICATED AND INSTALLED NEW REPAIR SPLICE. APPROVED BY ENINEERING PER MRB 767-1113. TST: 42,562.49 HRS. CYCLES, 10,8 21. (X) 2 L 7 2 4F RT A1NM 1996032200226 19960322 00226 NM 1996 3 22 AALA960192 1 19960124 A 5320 143T15902 CHORD BOEING 767 767223 1385123 NM BS 539.5 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 313AA 22316 AFW - FOUND AND BLENDED CORROSION IN TWO LOCATIONS ON INNER SURFACE OF FAIL-SAFE CHORD. REMOVED CORROSION. ROTO-PEENE D TREATED AND PAINTED. APPROVED BY ENGINEERING PER MRB 767-1111. TST: 42,562.49 HRS. CYCLES, 10,821. (X) 2 L 7 2 4F RT A1NM 1996032200227 19960322 00227 NM 1996 3 22 AALA960193 1 19960124 A 5313 140T01156 STRINGER BOEING 767 767223 1385123 NM BS 434 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 313AA 22316 AFW - STRINGER CORRODED. DAMAGE REQUIRED REMOVAL OF .70 INCH OF STRINGER FORWARD OF SPLICE. REMOVED ALL CORROSION. FA BRICATED AND INSTALLED REPAIR SPLICE. REPAIR APPROVED BY ENGINEERING PER MRB 767-1109. TST: 42,562.49 HRS. CYCLES, 10,821. (X) 2 L 7 2 4F RT A1NM 1996032200228 19960322 00228 NM 1996 3 22 AALA960194 1 19960124 A 5330 143T3520 SKIN BOEING 767 767223 1385123 NM FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 313AA 22316 AFW - FUSELAGE SKIN GOUGED FORWARD OF LOWER FORWARD CORNER OF FORWARD CARGO DOOR CUT-OUT. BLENDED GOUGE, PARENT MATERIA L .202 INCH THICK. LOW POINT OF BLEND .143 INCH THICK. APPROVED FOR CONTINUED SERVICE IN NOTED CONDITION BY ENGINEERIN G PER MRB 767-1110. TST: 42,562.49 HRS. CYCLES, 10,821. (X) 2 L 7 2 4F RT A1NM 1996032200229 19960322 00229 NM 1996 3 22 AALA960195 1 19960120 A 5315 111T5007 FLOOR BEAM BOEING 767 767323 1385205 NM BS 786-848 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 39365 24046 AFW - CORROSION ON THE UPPER SURFACE OF TWO MAIN CABIN FLOOR BEAMS. BLEND, SHIM, AND REFINISH PER MRB 767-1120. TST: 32,231.54 HRS. CYCLES, 5,446. (X) 2 L 7 2 4F RT A1NM 1996032200230 19960322 00230 NM 1996 3 22 AALA960196 1 19960120 A 5315 111T5007 FLOOR BEAM BOEING 767 767323 1385205 NM BS 941 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 39365 24046 AFW - FLOOR BEAMS HAVE DEEP GOUGES. BLEND AND REFINISH PER MRB 767-1130. TST: 32,231.54 HRS. CYCLES, 5,446. (X) 2 L 7 2 4F RT A1NM 1996032200231 19960322 00231 NM 1996 3 22 AALA960197 1 19960120 A 5315 111T5008 FLOOR BEAM BOEING 767 767323 1385205 NM BS 871-928/786 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 39365 24046 AFW - CORROSION ON THE UPPER SURFACE OF THE CABIN FLOOR BEAM. BLEND, SHIM, AND PAINT PER MRB 767-1122. TST: 32,231.5 4 HRS. CYCLES, 5,446. (X) 2 L 7 2 4F RT A1NM 1996032200232 19960322 00232 NM 1996 3 22 AALA960220 1 19960208 A 5315 FLOOR BEAM BOEING 727 727223 1384074 NM BS 381 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 897AA 22013 TUL - CORROSION ON FLOOR BEAM AT STA 381, RBL 24 TO RBL 65. REMOVED CORROSION PER SRM 51-10-6. REPAIRED FLOOR BEAM IAW SRM 53-10-8. TST: 42,813 HRS. CYCLES, 21,496. (X) 2 L 7 3 4F A3WE 1996032200233 19960322 00233 NM 1996 3 22 AALA960221 1 19960208 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 683 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 897AA 22013 TUL - STR 25L HAS HEAVY CORROSION INSIDE AT STA 683. REMOVED AND SPLICED IAW 53-10-3. TST: 42,813 HRS. CYCLES, 21,4 96. (X) 2 L 7 3 4F A3WE 1996032200234 19960322 00234 NM 1996 3 22 AALA960222 1 19960208 A 5320 FITTING BOEING 727 727223 1384074 NM BS 950 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 897AA 22013 TUL - TIE-IN FITTING BETWEEN 29R-29L ON AFT SIDE OF STA 950 CHORD HAS CORROSION. REMOVED CORROSION PER SRM 51-10-6 AND REPLACED TIE-IN FITTING PER SRM 51-10-1, PAGE 4. TST: 42,813 HRS. CYCLES, 21,496. (X) 2 L 7 3 4F A3WE 1996032200235 19960322 00235 NM 1996 3 22 AALA960223 1 19960208 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 700-708 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 897AA 22013 TUL - CORROSION ON STR 28L, STA 700 - STA 708. INSTALLED 28L REPAIR FROM STA 680 - STA 725 PER SRM 53-10-3. TST: 42, 813 HRS. CYCLES, 21,496. (X) 2 L 7 3 4F A3WE 1996032200236 19960322 00236 NM 1996 3 22 AALA960224 1 19960208 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 950 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 897AA 22013 TUL - CORROSION ON T-CHORD ANGLE AT STA 950 AT STR 30 IN AFT CARGO AREA. REMOVED OLD T-CHORD ANGLE AND REPLACED WITH NE W T-CHORD ANGLE IAW SRM 51-10-1, PAGE 4. TST: 42,813 HRS. CYCLES, 21,496. (X) 2 L 7 3 4F A3WE 1996032200237 19960322 00237 NM 1996 3 22 AALA960225 1 19960208 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 344-420 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 897AA 22013 TUL - RIGHT CREASE ANGLE HAS CORROSION FROM STA 344 TO STA 420. REMOVED AND REPLACED RT CREASE ANGLE FROM STA 355 TO ST A 445 PER SRM 51-10-01. REMOVED CORROSION FROM STA 344 TO STA 355 PER SRM 51-10-06. TREATED AND PRIMED PER SRM 51-10-0 6. TST: 42,813 HRS. CYCLES, 21,496. (X) 2 L 7 3 4F A3WE 1996032200238 19960322 00238 NM 1996 3 22 AALA960226 1 19960208 A 5330 SKIN BOEING 727 727223 1384074 NM FS 584-593 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 897AA 22013 TUL - CORROSION ON FUSELAGE SKIN, FS 584 TO FS 593 UNDER AND OUTBOARD OF STR 28L. CUT OUT DAMAGED AREA OF SKIN AND INST ALLED FILLER AND DOUBLER PER SRM 53-30-3, FIGURE 3. TST: 42,813 HRS. CYCLES, 21,496. (X) 2 L 7 3 4F A3WE 1996032200239 19960322 00239 NM 1996 3 22 AALA960227 1 19960208 A 5711 SPAR WEB BOEING 727 727223 1384074 NM WS 515 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 897AA 22013 TUL - CORROSION ON AFT SIDE OF FRONT SPAR WEB AT NR 3 SLAT ACT DOG HOUSE. INSTALLED DOUBLER IAW ESO 11697 DATED 1-17-96 . SELAED REPAIR AREA INSIDE TANK. TST: 42,813 HRS. CYCLES, 21,496. (X) 2 L 7 3 4F A3WE 1996032200240 19960322 00240 NM 1996 3 22 AALA960228 1 19960208 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1008-1011 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 897AA 22013 TUL - CORROSION ON STR 29R, STA 1008 TO STA 1011, INBOARD AND OUTBOARD SIDES. REMOVED CORROSION PER SRM 51-10-6. REMOV ED AND REPLACED FACTORY STRINGER SPLICE WITH A NEW PART PER SRM 53-10-3. TST: 42,813 HRS. CYCLES, 21,496. (X) 2 L 7 3 4F A3WE 1996032200241 19960322 00241 NM 1996 3 22 AALA960229 1 19960208 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1000-1002 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 897AA 22013 TUL - CORROSION ON STR 29R AROUND HILOK COLLARS, STA 1000 TO STA 1002. REPLACED STRINGER SPLICE PER SRM 53-10-3. TST: 42,813 HRS. CYCLES, 21,496. (X) 2 L 7 3 4F A3WE 1996032200242 19960322 00242 NM 1996 3 22 AALA960230 1 19960208 A 5311 FRAME BOEING 727 727223 1384074 NM FS 804 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 897AA 22013 TUL - OUTBOARD FLANGE OF STUB FRAME CRACKED IN RADIUS AT STA 804, STR 14L. REMOVED FASTENER AND STOPPED DRILLED CRACK W ITH .25 INCH DRILL. DYE CHECK FOUND NO CRACK OUTSIDE OF STOP-DRILL. INSTALLED STAINLESS REPAIR ANGLE PER SRM 51-40-3. TST: 42,813 HRS. CYCLES, 21,496. (X) 2 L 7 3 4F A3WE 1996032200243 19960322 00243 NM 1996 3 22 AALA960231 1 19960208 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 897AA 22013 TUL - STR 15L, STRINGER END FORWARD OF ICE LIGHT BETWEEN STA 720B AND STA 720C IS CRACKED. REMOVED DAMAGED STRINGER END AND SPLICED IN A NEW SECTION PER SRM 53-10-3, FIGURE 1. TST: 42,813 HRS. CYCLES, 21,496. (X) 2 L 7 3 4F A3WE 1996032200244 19960322 00244 NM 1996 3 22 AALA960232 1 19960208 A 5320 6575259 INTERCOSTAL BOEING 727 727223 1384074 NM FS 580-600 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 897AA 22013 TUL - CORROSION ON INTERCOSTAL OUTBOARD SIDE OF STRINGER 28L BETWEEN FS 500 - FS 600. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-10-1, PAGE 4. TST: 42,813 HRS. CYCLES, 21,496. (X) 2 L 7 3 4F A3WE 1996032200245 19960322 00245 NM 1996 3 22 AALA960233 1 19960208 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 897AA 22013 TUL - STR 15R, STRINGER END FORWARD OF ICE LIGHT BETWEEN STA 720B AND STA 720C IS CRACKED. REPAIRED CRACKED STR 15R AT FORWARD SIDE OF ICE LIGHT BETWEEN STA 720B AND STA 720C PER SRM 53-10-3, FIGURE 1. TST: 42,813 HRS. CYCLES, 21,496. ( X) 2 L 7 3 4F A3WE 1996032200246 19960322 00246 NM 1996 3 22 AALA960234 1 19960208 A 5315 FLOOR BEAM BOEING 727 727223 1384074 NM BS 359 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 897AA 22013 TUL - GOUGE IN UNDER SIDE OF FLOOR BEAM UPPER FLANGE, .50 INCH BY .040 INCH, STA 359, BL 25R. BLENDED GOUGE, INSTALLED DOUBLER PER SRM 53-10-8, PAGE 9E. TST: 42,813 HRS. CYCLES, 21,496. (X) 2 L 7 3 4F A3WE 1996032200247 19960322 00247 NM 1996 3 22 AALA960235 1 19960208 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 897AA 22013 TUL - STR 15L, STRINGER END AFT OF ICE LIGHT BETWEEN STA 720B AND STA 720C IS CRACKED. REMOVED DAMAGED STRINGER END AND SPLICED IN NEW SECTION PER SRM 53-10-3, FIGURE 1, STA 720C, STR 15L. TST: 42,813 HRS. CYCLES, 21,496. (X) 2 L 7 3 4F A3WE 1996032200248 19960322 00248 NM 1996 3 22 AALA960236 1 19960208 A 5313 BAC1498133 STRINGER BOEING 727 727223 1384074 NM BS 589 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 897AA 22013 TUL - CORROSION ON STR 28L AT STA 587. CUT OUT CORROSION AREA OF STR 28L AND INSTALLED STRINGER REPAIR PER SRM 53-10-3, FIGURE 1, DETAIL 2. TST: 42,813 HRS. CYCLES, 21,496. (X) 2 L 7 3 4F A3WE 1996032200249 19960322 00249 NM 1996 3 22 AALA960237 1 19960208 A 5315 FLOOR BEAM BOEING 727 727223 1384074 NM FS 1110 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 897AA 22013 TUL - FS 1110 FLOOR BEAM, BL ZERO HAS CORROSION. FLOOR BEAM REPAIRED PER SRM 53-10-8, PAGE 9A. TST: 42,813 HRS. CYCL ES, 21,496. (X) 2 L 7 3 4F A3WE 1996032200250 19960322 00250 NM 1996 3 22 AALA960238 1 19960208 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 309-350 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 897AA 22013 TUL - FLOORBOARD ANGLE NEXT TO FWD ENTRY DOOR THRESHOLD, CORROSION ON UPPER SURFACE FROM STA 309 TO STA 350, ENTIRE LENG TH. INSTALLED LT CREASE ANGLE PER 51-10-1, PAGE 4. TST: 42,813 HRS. CYCLES, 21,496. (X) 2 L 7 3 4F A3WE 1996032200251 19960322 00251 EU 1996 3 22 AALA960239 1 19960207 A 5310 A53981929203 ATTACH SECTION AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14053 420 TUL - ATTACH SECTION CORRODED BEYOND MM (SRM) LIMITS. REPLACED ATTACH SECTION PER SRM 51-72-10. TST: 21,713 HRS. CYCL ES, 8,831. (X) 2 L 7 2 4F RT A35EU 1996032200252 19960322 00252 EU 1996 3 22 AALA960253 1 19960212 A 5310 A53981929202 ATTACH SECTION AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14053 420 TUL - CORRODED ALONG LENGTH. REPLACED ATTACH SECTION PER SRM 51-72-10. TST: 21,713 HRS. CYCLES, 8,831. (X) 2 L 7 2 4F RT A35EU 1996032200253 19960322 00253 NM 1996 3 22 AALA960261 1 19960213 A 5320 DOUBLER BOEING 727 727223 1384074 NM BS 1068 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 896AA 22012 TUL - CORROSION ON SKIN DOUBLER AND TRIPPLER AROUND AFT LAV SERVICE PAN STA 1068-1183, STR 21-23. INSTALLED DOUBLER PER SRM 53-30-4, PAGE 40 AND SRM 53-30-3. TST: 43,002 HRS. CYCLES, 21,381. (X) 2 L 7 3 4F A3WE 1996032200254 19960322 00254 EU 1996 3 22 AALA960262 1 19960214 A 5311 FRAME FOKKER F28 F28MK0100 4990807 EU TAIL CONE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1417D 11396 TUL - CRACK AT VERTICAL CUT-OUT AUXILIARY FRAME, LT SIDE. INSTALLED REPAIR CLIP DOUBLER PER SRM 53-00-02 - R71, PAGE 20 3. TAT: 8,372.3 HRS; CYCLES 6,604. (X) 2 L 7 2 4F RT 1996032200255 19960322 00255 EU 1996 3 22 AALA960263 1 19960214 A 5311 FRAME FOKKER F28 F28MK0100 4990807 EU TAIL CONE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1417D 11396 TUL - CRACK AT VERTICAL CUT-OUT AUXILIARY FRAME, RT SIDE. INSTALLED REPAIR CLIP DOUBLER PER 53-00-02-R71, PAGE 203. TS T: 8,372.3 HRS. CYCLES, 6,604. (X) 2 L 7 2 4F RT 1996032200256 19960322 00256 NM 1996 3 22 AALA960282 1 19960206 A 5754 114T418022 TRACK BOEING 767 767223 1385123 NM NR 11 SLAT WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 303AA 22309 AFW - FOUND NR 11 SLAT TRACKS WORN BEYOND MM LIMITS. INBOARD TRACK WORN TO .011 INCH. OUTBOARD TRACK WORN TO .013 INCH . BLENDED WORN AREAS. EDDY CURRENT CHECKED. NO CRACKS FOUND. ROTO-PEENED, PRIMED, AND COATED WITH AEROSHELL 7. APPR OVED BY ENGINEERING PER MRB 767-1146. TRACKS WILL BE REPLACED AT NEXT MBV. TST: 43,462.33 HRS. CYCLES, 13,660. (X) 2 L 7 2 4F RT A1NM 1996032200257 19960322 00257 NM 1996 3 22 AALA960283 1 19960206 A 5754 114T418021 TRACK BOEING 767 767223 1385123 NM NR 1/12 SLAT WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 303AA 22309 AFW - NR 1 AND NR 12 SLAT TRACKS FOUND WORN BEYOND MM LIMITS. NR 1 WORN TO .011 INCH AND NR 12 WORN TO .014 INCH. BLEN DED WORN AREAS. EDDY CURRENT CHECKED. NO CRACKS FOUND. ROTO-PEENED, PRIMED, AND LUBED. APPROVED BY ENGINEERING PER M RB 767-1147. TRACKS WILL BE REPLACED NEXT MBV. TST: 43,462.33 HRS. CYCLES, 13,660. (X) 2 L 7 2 4F RT A1NM 1996032200258 19960322 00258 NM 1996 3 22 AALA960284 1 19960206 A 5414 311T1400 SKIN BOEING 767 767223 1385123 NM RT PYLON CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 303AA 22309 AFW - FOUND AND BLENDED DAMAGE ON THE RT PYLON INBOARD SIDE SKIN. FOUND THE BLEND EXCEEDED SRM LIMITS. REFINISHED BLEN DED AREA PER SRM. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1141. TST: 43,462. 33 HRS. CYCLES, 13,660. (X) 2 L 7 2 4F RT A1NM 1996032200259 19960322 00259 NM 1996 3 22 AALA960288 1 19960214 A 5320 146T122327 SHEAR TIE BOEING 767 767223 1385123 NM BS 1562 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 322AA 22323 AFW - FOUND AND BLENDED OUT CORROSION ON THE AFT SIDE OF THE SHEAR-TIE. FOUND BLEND-OUT EXCEEDS SRM LIMITS. ALODINED A ND PRIMED AREA. REPLACED FASTENERS. APPROVED FOR CONTINUED SERVICE BY ENGINEERING PER MRB 767-1152. TST: 41,252.20 HRS. CYCLES, 7,600. (X) 2 L 7 2 4F RT A1NM 1996032200260 19960322 00260 NM 1996 3 22 AALA960289 1 19960214 A 5343 161T11126 TRUNNION BOEING 767 767223 1385123 NM RT MLG CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 322AA 22323 AFW - DURING REINSTALLATION OF THE RT MLG AFTER REWORK AT THE AFT TRUNNION, REMOVED THE FWD TRUNNION HOUSING DUE TO LOOS ENESS. AFTER REMOVAL, FOUND AND BLENDED OUT CORROSION IN THE CHAMFER ON THE THRUST FACE IN QUADRANT 2. APPLIED PRIMER AND REINSTALLED HOUSING WITHOUT SHOT-PEENING OR CAD PLATING THE BLENDED AREA. APPROVED FOR CONTINUED SERVICE BY ENGINEE RING WITH NOTED CONDITION UNTIL NEXT SCHEDULED LANDING GEAR OVERHAUL PER MRB 767-1156. TST: 41,252.20 HRS. CYCLES, 7, 600. (X) 2 L 7 2 4F RT A1NM 1996032200261 19960322 00261 NM 1996 3 22 AALA960290 1 19960214 A 5343 161T11126 TRUNNION TAB BOEING 767 767223 1385123 NM RT MLG CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 322AA 22323 AFW - DURING REINSTALLATION OF THE RT MLG AFTER REWORK OF THE AFT TRUNNION, REMOVED THE FWD TRUNNION HOUSING DUE TO LOOS ENESS. AFTER REMOVAL, FOUND AND BLENDED CORROSION ON THE INNER SURFACE OF THE 3 O'CLOCK POSITION TAB. AFTER BLENDED, A PPLIED PRIMER AND REINSTALLED HOUSING WITHOUT SHOT-PEENING OR CAD PLATING THE BLENDED AREA. APROVED BY ENGINEERING WITH NOTED CONDITION UNTIL NEXT SCHEDULED LANDING GEAR OVERHAUL PER MRB 767-1159. TST: 41,252.20 HRS. CYCLES, 7,600. (X) 2 L 7 2 4F RT A1NM 1996032200262 19960322 00262 NM 1996 3 22 AALA960291 1 19960214 A 5320 143T15902 CHORD BOEING 767 767223 1385123 NM BS 539.5 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 322AA 22323 AFW - BLENDED OUT CORROSION ON THE INNER SURFACE OF THE FAIL-SAFE CHORD. BLENDED OUT IS BEYOND SRM LIMITS. INSTALLED N EW FASTENERS, ROTO-PEENED, ALODINED, AND PRIMED. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1151. TST: 41,252.20 HRS. CYCLES, 7,600. (X) 2 L 7 2 4F RT A1NM 1996032200263 19960322 00263 NM 1996 3 22 AALA960292 1 19960214 A 5730 111T3013 SKIN BOEING 767 767223 1385123 NM WS 955 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 322AA 22323 AFW - CENTER WING UPPER SKIN PREVIOUSLY BLENDED. LIGHT CORROSION AGAIN. BLEND-OUT WAS PREVIOUSLY BEYOND SRM LIMITS AND ADDRESSED ON MRB 767-424. SHOT-PEENED BLEND OUT PER SRM. TREATED, PRIMED, AND APPLIED FUEL BARRIER COMPOUND SEALED WI TH BM55-95. APPLIED DINOLTROL. APPROVED FOR CONTINUED SERVICE BY ENGINEERING PER MRB 767-1140. TST: 41,252.20 HRS. C YCLES, 7,600. (X) 2 L 7 2 4F RT A1NM 1996032200264 19960322 00264 NM 1996 3 22 AALA960293 1 19960214 A 5512 185T2001 SKIN BOEING 767 767223 1385123 NM RT HORIZ STAB DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 322AA 22323 AFW - DAMAGE ON THE LOWER SURFACE AT FS 127 WAS REPAIRED PER SMM/AFW 1371 AND ESO 9196 13DEC95. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1138. TST: 41,252.20 HRS. CYCLES, 7,600. (X) 2 L 7 2 4F RT A1NM 1996032200265 19960322 00265 NM 1996 3 22 AALA960294 1 19960214 A 5315 111T5007 FLOOR BEAM BOEING 767 767223 1385123 NM BS 814-955 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 322AA 22323 AFW - FOUND AND BLENDED OUT GOUGES ON THE UPPER SURFACE OF THE MAIN CABIN FLOORBEAM. THE BLEND-OUT EXCEEDS SRM LIMITS. ROTO-PEENED, DYE CHECKED, ALODINED, PRIMED, AND PAINTED DAMAGED AREAS. APPROVED FOR CONTINUED SERVICE BY ENGINEERING P ER SRB 767-1142. TST: 41,252.20 HRS. CYCLES, 7,600. (X) 2 L 7 2 4F RT A1NM 1996032200266 19960322 00266 NM 1996 3 22 AALA960295 1 19960212 A 5730 111T3013 SKIN BOEING 767 767223 1385123 NM WS 955 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 322AA 22323 AFW - AREA PREVIOUSLY BLENDED. LIGHT CORROSION FOUND AGAIN IN THIS LOCATION. BLENDED, FLAP PEENED, REFINISHED AND FILL ED WITH BM55-55 PER ENGINEERING MRB 767-1140. TST: 41,252.20 HRS. CYCLES, 7,600. (X) 2 L 7 2 4F RT A1NM 1996032200267 19960322 00267 NM 1996 3 22 AALA960296 1 19960216 A 5315 111T5008 FLOOR BEAM BOEING 767 767323 1385205 NM BS 865 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 380AN 25449 AFW - FLOOR BEAM AT LBL 33, STA 865, HAS CORROSION. REPAIRED PER MRB 767-1136. TST: 12,783.33 HRS. CYCLES, 2,028. ( X) 2 L 7 2 4F RT A1NM 1996032200268 19960322 00268 WP 1996 3 22 AALA960300 1 19960222 A 5320 CUSP DOUG DC9 DC982 3022082 WP BS 254-256 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 253AA 49286 TUL - 3 INCH BY 4 INCH AREA OF CUSP MEMBRANE TOTALLY CORRODED THROUGH. REMOVED CORRODED SECTION AND INSTALLED OVERLAY P ATCH PER SRM 53-01, PAGE 8, FIGURE 2. TST: 34,543.23 HRS. CYCLES, 19,744. (X) 2 L 7 2 4F A6WE 1996032200269 19960322 00269 SO 1996 3 22 ASOA96006 1 19960309 A 5230 12023348005 SEAL EMB 120 EMB120RT SO CARGO DOOR DEFECTIVE A ASOA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 11 233AS 120031 MEI/ATL - INBOUND, LOST CABIN PRESSURIZATION IN CRUISE FLIGHT AT 22,000 FEET. CREW PERFORMED AN EMERGENCY DESCENT TO 5, 000 FEET AND REGAINED CONTROL OF PRESSURIZATION. THE FLIGHT CONTINUED TO ATL WHERE LANDING WAS MADE SAFELY AND WITHOUT INCIDENT. REMOVED AND REPLACED CARGO DOOR SEAL. OPERATIONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1996032200270 19960322 00270 NM 1996 3 22 IXKA9600008 1 19960229 A 5270 SWITCH BOEING 727 727251 138408H NM CARGO DOOR OUT OF ADJUST A IXKA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 25 264US 19983 EWR/ATL - FLT 25 - AT EWR, AFT CARGO DOOR OPEN LIGHT CAME ON DURING TAKEOFF ROLL. ABORTED TAKEOFF. ADJUSTED CARGO DOOR SWITCH PER MM 52-70-01. OPS CHECK OK. (X) 2 L 7 3 4F A3WE 1996032200271 19960322 00271 EU 1996 3 22 VTZA96099 1 19960303 A 2770 137515F427 GUST LOCK JETAIR JETSTM JETSTM4101 1500501 EU CENTER CONSOLE NOT LATCHED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 301UE 41012 BOS/IAD - FLT 6157 - DURING TAKEOFF AT 1130 HRS ON 3-3-96, ABORTED TAKEOFF DUE TO TAKEOFF CONFIGURATION WARNING SYSTEM A CTIVATING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE CYCLED THE GUST LOCK. AIRCRAFT RELEASED A ND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1996032200303 19960322 00303 WP 1996 3 22 96ZZZW38 1 19960101 A 5320 HAT SECTION DOUG DC8 DC863 302198A WP BS 1560-1600 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 4935C 45931 LEVEL 2 CORROSION - CABIN FLOOR STATION 1600L TO 1569L HAT INBOARD OF INBOARD SEAT TRACK IS BROKEN AND CORRODED. REMOVE D DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 51-01-00. 2 L 7 4 4F 4A25 1996032200304 19960322 00304 WP 1996 3 22 96ZZZW39 1 19960101 A 5347 SEAT TRACK DOUG DC8 DC863 302198A WP BS 1520-1620 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 4935C 45931 LEVEL 2 CORROSION - CABIN FLOOR STATION 1520 TO 1620 LEFT SIDE OUTBOARD SEAT TRACK HAS CORROSION. REMOVED DAMAGED AREA AND SPLICED IN NEW SEAT TRACK PER SRM 51-2-3. 2 L 7 4 4F 4A25 1996032200306 19960322 00306 WP 1996 3 22 96ZZZW40 1 19960101 A 5512 56517476264 PANELS DOUG DC8 DC863 302198A WP HORIZ STAB CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 4935C 45931 LEVEL 2 CORROSION - RIGHT HORIZONTAL STABILIZER OUTBOARD UPPER SURFACE PANELS ARE CORRODED BETWEEN RIVETS AT TRAILING ED GE. REPLACED PANEL WITH NEW PANELS. 2 L 7 4 4F 4A25 1996032200312 19960322 00312 EU 1996 3 22 9606203222 1 19960316 A 3830 14400359 FLUSH CONTL UNIT AIRBUS 320 A320211 3930320 EU FWD LAV MALFUNCTIONED A NWAA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 01 322US 263 DURING CRUISE, THE FORWARD LAVATORY TOILET OVERFLOWED SPILLING FLUID INTO THE FIRST CLASS CABIN. AIRCRAFT DIVERTED TO D FW AND LANDED WITHOUT INCIDENT. THE FORWARD LAV WAS PLACED ON MEL AND THE FLUSH CONTROL UNIT LATER WAS REPLACED, OPERAT IONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996032200313 19960322 00313 WP 1996 3 22 9606219601 1 19960317 A 3350 LIGHTS DOUG DC9 DC932 3022066 WP CABIN MALFUNCTIONED A NWAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 01 601NW 47038 DURING TAXI OUT, FLIGHT ATTENDANT REPORTED EMERGENCY LIGHTS ON WITH SWITCH IN ARMED POSITION. RECYCLED SWITCH AND LIGHT S EXTINGUISHED. CIRCUIT BREAKER WAS POPPED AND RESET. MAINTENANCE CHECKED EMERGENCY LIGHTING SYSTEM AND NO PROBLEMS WE RE FOUND. 2 L 7 2 4F A6WE 1996032200314 19960322 00314 WP 1996 3 22 9606229990 1 19960315 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP COCKPIT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8950E 47186 DURING LINE MAINTENANCE INSPECTION, FOUND COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN BATTERY PACK, OPE RATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996032200315 19960322 00315 NM 1996 3 22 96FDEA00526 1 19960318 A 3230 RETRACT MECH DOUG MD11 MD11 3023602 NM LANDING GEAR SLOW A FDEA O OTHER J WARNING INDICATION DE DESCENT 1 SO 25 617FE 48748 ARRIVAL, GEAR HANDLE DOWN AND IN-GEAR DID NOT EXTEND ALL RED LIGHT, CONFIRMED GEAR WAS STILL UP ON CONFIG PAGE. CYCLE G EAR, GEAR CAME DOWN MUCH SLOWER THAN NORMAL, NOSE FIRST, CENTER, THEN MAIN. HYDRO PRESS NORMAL. 2 L 7 3 4F RT A22WE 1996032200316 19960322 00316 NM 1996 3 22 96FDEA00527 1 19960315 A 5754 65162256A BULLNOSE BOEING 727 72725 1384006 NM NR 4 LE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 CORROSION ON NR 4 K-FLAP O/B BONDING JUMPER LOWER ATTACH POINT. REMOVED CORROSION ON NR 4 K-FLAP BULLNOSE O/B BONDING J UMPER, FOUND TUBE OUT OF LIMITS PER SRM 57-50-1. BLENDED TO LIMITS PER DRAWING SR 27-57-010. CLEANED AND TREATED AREA AND REINSTALLED BONDING JUMPER. 2 L 7 3 4F A3WE 1996032200317 19960322 00317 NM 1996 3 22 96FDEA00528 1 19960315 A 5753 SKIN BOEING 727 727233 138408A NM LT TE AFT FLAP DISBONDED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 LEFT WING I/B AFT FLAP HAS DISBONDED DENT UPPER SURFACE AT 18 INCHES FROM I/B END. REPAIRED LEFT WING I/B AFT FLAP AT 1 8 INCHES FROM I/B END IAW FEDEX 51-40-6. 2 L 7 3 4F RT A3WE 1996032200318 19960322 00318 NM 1996 3 22 96FDEA00529 1 19960311 A 5347 SEAT TRACK BOEING 727 727233 138408A NM BS 950 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CORROSION ON SEAT TRACK FLANGE AT BS 950C TO 950E PLUS 5 RBL 25 WL 208. REPLACED SEAT TRACK FROM BS 950 TO 950E PLUS 10 RBL 25 WL 208. 2 L 7 3 4F RT A3WE 1996032200319 19960322 00319 NM 1996 3 22 96FDEA00530 1 19960314 A 5311 FRAME BOEING 727 727233 138408A NM BS 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 AT FRAME 500 ABOVE STR 24L HAS A 1 INCH BY .5 INCH HOLE TORN THROUGH TOP OF FRAME. REPAIRED PER FEDEX SRM 51-40-03. 2 L 7 3 4F RT A3WE 1996032200320 19960322 00320 NM 1996 3 22 96FDEA00531 1 19960314 A 5314 65564416 KEEL BEAM BOEING 727 727233 138408A NM BS 990 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 RT KEEL BEAM CRACKED AT BS 990 STR 29R, SPLICED IN NEW SECTION OF AFT RT KEEL BEAM. REPAIRED RT KEEL BEAM PER FEDEX CAR D 7-5310-7-2356C PT 5 AND FEDEX EA NR 7-5310-27778. 2 L 7 3 4F RT A3WE 1996032200321 19960322 00321 NM 1996 3 22 96FDEA00532 1 19960315 A 5753 SKIN BOEING 727 727233 138408A NM RT TE AFT FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 RT WING I/B AFT FLAP HAS A 2 INCH DELAMINATED DENT 14 INCHES FROM I/B END UPPER SURFACE. REPAIRED RT WING I/B AFT FLAP 14 INCHES FROM I/B END UPPER SURFACE IAW FEDEX SRM 51-40-6. 2 L 7 3 4F RT A3WE 1996032200322 19960322 00322 NM 1996 3 22 96FDEA00533 1 19960315 A 5320 DOUBLER BOEING 727 72722 1384002 NM BS 875 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 CORROSION (C53-132-02, 1) ON ACCESS HOLE DOUBLER BS 875 WL 184 LBL 63. FOUND CORROSION TO BE OUT OF LIMITS PER FEDEX SR M 53-10-01. FABRICATED AND REPLACED ACCESS HOLE DOUBLER AT BS 875 WL 184 LBL 63. 2 L 7 3 4F A3WE 1996032200323 19960322 00323 NM 1996 3 22 96FDEA00534 1 19960311 A 5711 65185371 SPAR CHORD BOEING 727 72722 1384002 NM WS 870 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 CORROSION (C53-132-02, 1) ON THE WING CENTER LOWER SPAR CHORD STA 870 LBL 36 TO 40 WL 138. REMOVED AND REPLACED LOWER S PAR CHORD. 2 L 7 3 4F A3WE 1996032200324 19960322 00324 NM 1996 3 22 96FDEA00535 1 19960311 A 5711 65185381 SPAR CHORD BOEING 727 72722 1384002 NM WS 870 UPPER CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 CORROSION (C53-132-02, 1) ON THE WING CENTER SECTION UPPER SPAR CHORD STA 870 LBL TO RBL 60 WL 178. REMOVED AND REPLACE D UPPER SPAR CHORD. 2 L 7 3 4F A3WE 1996032200325 19960322 00325 NM 1996 3 22 96FDEA00536 1 19960315 A 5230 651862578 ANGLE BOEING 727 72722 1384002 NM CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 WHILE WORKING NR0254, FOUND AFT CARGO DOOR NR 3 FROM BOTTOM, O/B L-ANGLE TO BE CRACKED IN RADIUS. REMOVED AND REPLACED AFT CARGO DOOR NR 3 O/B L-ANGLE. 2 L 7 3 4F A3WE 1996032200326 19960322 00326 NM 1996 3 22 96FDEA00537 1 19960318 A 5311 FRAME BOEING 727 72722 1384002 NM BS 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 WHILE WORKING NR0177, FOUND CRACK IN FRAME AT BS 500 LBL 8 WL 156. REMOVED AND REPLACED ANGLE PER SRM 51-40-3. 2 L 7 3 4F A3WE 1996032200327 19960322 00327 NM 1996 3 22 96FDEA00538 1 19960318 A 5311 FRAME BOEING 727 72722 1384002 NM BS 1070 DOUBLE DRILLED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 187FE 19079 DOUBLE DRILLED HOLES ON FRAME AT BS 1070 LBL 20 WL 149. TRIMMED DAMAGE AND INSTALLED DOUBLER PER SRM 51-40-3. 2 L 7 3 4F A3WE 1996032200328 19960322 00328 NM 1996 3 22 96FDEA00540 1 19960318 A 5311 FRAME BOEING 727 72722 1384002 NM BS 1130 DOUBLE DRILLED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 DOUBLE DRILLED HOLES ON THE NESTLED FLANGE OF A-FRAME AT 1130 LBL 19 WL 154. TRIMMED AND REPAIRED DOUBLE DRILLED HOLES ON NESTLED FLANGE OF A-FRAME AT 1130 LBL 19 WL 154 PER FEDEX SRM 51-40-3. 2 L 7 3 4F A3WE 1996032200329 19960322 00329 NM 1996 3 22 96FDEA00541 1 19960318 A 5320 65242581 STRAP BOEING 727 72722 1384002 NM BS 540/560 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 CORROSION (C53-113-01) ON THRESHOLD VERTICAL WEB, BS 540 AND 560 RBL 21 WL 156. REMOVED AND REPLACED VERTICAL WEB SRM 5 3-10-1. 2 L 7 3 4F A3WE 1996032200330 19960322 00330 NM 1996 3 22 96FDEA00542 1 19960318 A 5210 DOOR SKIN BOEING 727 72722 1384002 NM BS 340 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 FWD ENTRY DOOR HAS 2 DENTS BY LOWER HINGE CUTOUT AFT SIDE OF DOOR ON EXTERNAL SKIN. REMOVED DAMAGE AND INSTALLED DOUBLE R PER SRM 52-00-3. 2 L 7 3 4F A3WE 1996032200331 19960322 00331 NM 1996 3 22 96FDEA00543 1 19960318 A 5311 FRAME BOEING 727 72722 1384002 NM BS 1050 DOUBLE DRILLED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 DOUBLE DRILLED HOLES ON FRAME AT BS 1050 LBL 20 WL 147. TRIMMED DAMAGED AREA AND REPAIRED FRAME PER FEDEX SRM 51-40-3 F IG 1. 2 L 7 3 4F A3WE 1996032200332 19960322 00332 NM 1996 3 22 96FDEA00544 1 19960318 A 5311 FRAME BOEING 727 72722 1384002 NM BS 870 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 CRACK INDICATION NOTED HOLE 2 ROW 2 BS 870 LT. REMOVED ANGLE, STOP DRILLED CRACK, INSTALLED ANGLE PER SB 727-53-194 AND ER 031496LD2. 2 L 7 3 4F A3WE 1996032200333 19960322 00333 NM 1996 3 22 96FDEA00545 1 19960311 A 5330 SKIN BOEING 727 72722 1384002 NM BS 366 CREASED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 BS 366 STR 20R THERE IS A CREASE IN SKIN. REPAIRED CREASE PER FEDEX SRM 53-03-3. 2 L 7 3 4F A3WE 1996032200334 19960322 00334 NM 1996 3 22 96FDEA00546 1 19960311 A 5210 DOOR FRAME BOEING 727 72722 1384002 NM BS 310 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 FWD ENTRY DOOR LATCH ROLLER RUBS ON DOOR STRUCTURE. REMOVED AND REPLACED FWD SIDE FRAME SRM 53-10-1. 2 L 7 3 4F A3WE 1996032200335 19960322 00335 NM 1996 3 22 96FDEA00547 1 19960311 A 5320 SHEAR TIE BOEING 727 72722 1384002 NM BS 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 MECH DAMAGE ON SHEAR TIE AT BS 600 BETWEEN STR 16 AND 17R. REMOVED AND REPLACED SHEAR TIE SRM 53-10-1. 2 L 7 3 4F A3WE 1996032200336 19960322 00336 NM 1996 3 22 96FDEA00548 1 19960311 A 5754 BULLNOSE BOEING 727 72722 1384002 NM NR 4 LE FLAP CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION (097-562-01-2) NR 4 K-FLAP BULLNOSE O/B BONDING JUMPER, UPPER ATTACH POINT. REMOVED CORROSION PER FEDEX SRM 5 7-50-03 AND 27-57-010. 2 L 7 3 4F A3WE 1996032200337 19960322 00337 NM 1996 3 22 96FDEA00549 1 19960311 A 5320 SHEAR WEB BOEING 727 72722 1384002 NM BS 1174 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION EMANATING FROM UNDER NUTPLATES ON BOTTOM SIDE OF SHEAR WEB AT BS 1174 RBL 6 TO LBL 20 WL 208. FABRICATED NEW WEB AND INSTALLED PER SRM 53-10-1. 2 L 7 3 4F A3WE 1996032200338 19960322 00338 NM 1996 3 22 96FDEA00550 1 19960311 A 5531 65195316 FITTING BOEING 727 72722 1384002 NM BS 1342 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION (C53-137-01) BS 1342 RBL 17 STR 5R ON FITTING ANGLE. REMOVED CORRODED TERMINAL FITTING AND INSTALLED NEW RT S PAR TERMINAL FITTING ON VERTICAL STABILIZER AT BS 1342 IAW BOEING SB 727-55-088. 2 L 7 3 4F A3WE 1996032200339 19960322 00339 NM 1996 3 22 96FDEA00551 1 19960310 A 5530 FITTING BOEING 727 72722 1384002 NM BS 1342 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION (C53-137-01) BS 1342 LBL 17 STR 5L ON FITTING ANGLE. REMOVED AND REPLACED FITTING ON VERTICAL STABILIZER AT B S 1342 LBL 17 AT STR 5L PER SB 727-55-00. 2 L 7 3 4F A3WE 1996032200340 19960322 00340 NM 1996 3 22 96FDEA00552 1 19960311 A 5320 69239021 FITTING BOEING 727 72722 1384002 NM BS 360 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION ON STR 20L FITTING BS 360 TO 367. REMOVED AND REPLACED CORRODED FITTING PER SB 727-53-0209. 2 L 7 3 4F A3WE 1996032200341 19960322 00341 NM 1996 3 22 96FDEA00553 1 19960311 A 5320 INTERCOSTAL BOEING 727 72722 1384002 NM BS 1055 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 DENTED INTERCOSTAL BS 1055 BETWEEN STR 23L TO 25L LBL 36 TO 48 WL 156. REMOVED AND REPLACED OUT OF LIMITS INTERCOSTAL P ER FEDEX SRM 53-10-1. 2 L 7 3 4F A3WE 1996032200342 19960322 00342 NM 1996 3 22 96FDEA00554 1 19960311 A 5711 SPAR CHORD BOEING 727 72722 1384002 NM BS 870 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION (C53-132-02) ON THE WING CENTER SECTION REAR UPPER SPAR CHORD, STA 870 LBL 30 RBL 30 WL 174. REMOVED AND REPL ACED UPPER CHORD PER FEDEX EA 7-5710-27481. 2 L 7 3 4F A3WE 1996032200343 19960322 00343 NM 1996 3 22 96FDEA00555 1 19960311 A 5711 SPAR CHORD BOEING 727 72722 1384002 NM BS 870 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 CORROSION (C53-132-02) ON THE WING CENTER SECTION REAR LOWER CHORD, STA 870 LBL 20 TO 26 WL 140. REMOVED AND REPLACED L OWER CHORD PER FEDEX EA 7-5710-27481. 2 L 7 3 4F A3WE 1996032200344 19960322 00344 NM 1996 3 22 96FDEA00556 1 19960318 A 5311 FRAME BOEING 727 727233 138408A NM BS 1030 DOUBLE DRILLED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 DOUBLE AND TRIPLE HOLES IN FRAME STA 1030 BETWEEN STR 8 AND 9 RT. ACCESSED AREA, TRIMMED OUT DAMAGED AREA, FABRICATED D OUBLER AND INSTALLED FASTENERS AT BS 1030 BETWEEN STR 8 AND 9 RT PER EWO NR 96-2135. 2 L 7 3 4F RT A3WE 1996032200345 19960322 00345 NM 1996 3 22 96FDEA00557 1 19960318 A 5311 BAC15171080 FRAME BOEING 727 727233 138408A NM BS 760 DOUBLE DRILLED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 DOUBLE HOLE IN BS 760 FRAME BELOW STR 6L. REMOVED DAMAGE, FABRICATED REPAIR PART AND INSTALLED AT BS 760 FRAME BELOW ST R 6L PER FEDEX SRM 53-10-4. 2 L 7 3 4F RT A3WE 1996032200346 19960322 00346 NM 1996 3 22 96FDEA00558 1 19960318 A 5347 BAC1520793 SEAT TRACK BOEING 727 727233 138408A NM BS 760-848 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CORROSION AROUND FASTENER HOLES IN SEAT TRACK WELL FROM BS 760 TO 848 RBL 25 WL 208. REMOVED CORRODED SEAT TRACK WELL F ROM BS 760 TO 848 RBL 25 WL 208 FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. INSTALLED NEW SEAT TRACK WELL AT BS 76 0 TO 848 RBL 25 WL 208, WET WITH SEALANT AND INSTALLED FASTENERS. 2 L 7 3 4F RT A3WE 1996032200347 19960322 00347 NM 1996 3 22 96FDEA00559 1 19960318 A 5347 BAC1520792 SEAT TRACK BOEING 727 727233 138408A NM BS 344 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CORROSION (C53-224-01, 1) AROUND FASTENER THROUGH FLANGE OF SEAT TRACK AT BS 344 LBL 24 WL 208. REMOVED CORROSION ON UP PER SEAT TRACK FLANGE BS 344 LBL 24 WL 208 IN AN AREA 1 INCH BY .5 INCH BY .0135 INCH. ORIGINAL THICKNESS WAS .070, REM AINING MATERIAL THICKNESS IS .0565 AND WAS FOUND TO BE WITHIN LIMITS IAW FEDEX SRM 53-10-1. 2 L 7 3 4F RT A3WE 1996032200348 19960322 00348 NM 1996 3 22 96FDEA00560 1 19960318 A 5320 SHEAR WEB BOEING 727 727233 138408A NM BS 1139 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CORROSION (C53-224-04) ON SHEAR WEB BS 1139 RBL 25 TO 45 WL 208. REPAIRED SHEAR WEB AT BS 1139. 2 L 7 3 4F RT A3WE 1996032200349 19960322 00349 NM 1996 3 22 96FDEA0539 1 19960318 A 5311 FRAME BOEING 727 72722 1384002 NM BS 1110 DOUBLE DRILLED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 DOUBLE DRILLED HOLES ON THE NESTLED FLANGE OF FRAME AT BS 1110 LBL 19 WL 152. TRIMMED DAMAGE AND INSTALLED DOUBLER PER FEDEX SRM 51-40-3. 2 L 7 3 4F A3WE 1996032200350 19960322 00350 WP 1996 3 22 ABXA9600312 1 19960213 A 5280 24312157A06 BUSHING DOUG DC9 DC941 302207N WP BS 111 WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 47511 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR ATTACH LINK HAD EXCESSIVE PLAY. REPLACED BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1996032200351 19960322 00351 WP 1996 3 22 ABXA9600313 1 19960213 A 5280 S221037014109 BUSHING DOUG DC9 DC941 302207N WP BS 111 WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 46534 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND THE LEFT MAIN LANDING GEAR OUTBOARD DOOR ATTACHING LINK HAD EXCESSIV E PLAY. REPLACED BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1996032200352 19960322 00352 WP 1996 3 22 ABXA9600314 1 19960216 A 5280 29244721 HINGE DOUG DC9 DC932 3022066 WP BS 111 WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 984AX 47258 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND RIGHT MAIN LANDING GEAR OUTBOARD DOOR HINGE HAD EXCESSIVE PLAY. REP AIRED IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1996032200353 19960322 00353 WP 1996 3 22 ABXA9600315 1 19960216 A 5280 29244721 HINGE DOUG DC9 DC932 3022066 WP BS 111 WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 984AX 47258 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND THE LEFT MAIN LANDING GEAR OUTBOARD DOOR HINGE HAD EXCESSIVE PLAY. R EPAIRED IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1996032200354 19960322 00354 WP 1996 3 22 ABXA9600316 1 19960216 A 5280 S2210370P4101 BUSHING DOUG DC9 DC932 3022066 WP BS 111 WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 984AX 47258 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR LINK ASSEMBLY HAD EXCESSIVE PLA Y. REPLACED BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1996032200355 19960322 00355 WP 1996 3 22 ABXA9600317 1 19960216 A 5280 5910557503 DOOR DOUG DC9 DC932 3022066 WP BS 111 DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 984AX 47258 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND THE LEFT MAIN LANDING GEAR OUTBOARD DOOR DELAMINATED. REPLACED DOOR IAW DC-9 OVERHAUL MANUAL. 2 L 7 2 4F A6WE 1996032200356 19960322 00356 WP 1996 3 22 ABXA9600318 1 19960306 A 3231 3923159505 LINK DOUG DC9 DC932 3022066 WP BS 111 WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 42176 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND THE RIGHT MAIN LANDING GEAR OUTBOARD DOOR LINK WORN. REPLACED LINK IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1996032200357 19960322 00357 WP 1996 3 22 ABXA9600319 1 19960228 A 3231 3923167507 ROD DOUG DC9 DC941 302207N WP RT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47497 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND THE RIGHT MAIN LANDING GEAR OUTBOARD DOOR ROD END BEARING WORN AT UP PER ATTACH POINT OF FORWARD DOOR SECTION. REPLACED RIGHT MAIN LANDING GEAR OUTBOARD DOOR ROD END ASSEMBLY IAW DC-9 OVER HAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1996032200358 19960322 00358 WP 1996 3 22 ABXA9600320 1 19960228 A 3231 3923159505 ARM DOUG DC9 DC941 302207N WP RT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47497 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND THE RIGHT MAIN LANDING GEAR OUTBOARD DOOR ARM ASSEMBLY HAD EXCESSIVE PLAY. REPLACED RIGHT MAIN LANDING GEAR DOOR ARM IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1996032200359 19960322 00359 WP 1996 3 22 ABXA9600321 1 19960228 A 5280 HB218600 BUSHING DOUG DC9 DC941 302207N WP RT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47497 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND THE RIGHT MAIN LANDING GEAR OUTBOARD DOOR HAD EXCESSIVE PLAY AT THE ATTACH HINGE. REPLACED BUSHINGS IN THE DOOR HINGE IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1996032200360 19960322 00360 WP 1996 3 22 ABXA9600322 1 19960228 A 5280 HB218600 BUSHING DOUG DC9 DC941 302207N WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47497 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND THE LEFT MAIN LANDING GEAR OUTBOARD DOOR TO WING ATTACHING HINGE HAD EXCESSIVE PLAY. REPLACED BUSHINGS IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1996032200361 19960322 00361 WP 1996 3 22 ABXA9600323 1 19960228 A 5280 S221037084109 BUSHING DOUG DC9 DC941 302207N WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47497 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND THE LEFT MAIN LANDING GEAR OUTBOARD DOOR ATTACHING LINK HAD EXCESSIV E PLAY. REPLACED BUSHING ON ARM IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1996032200362 19960322 00362 WP 1996 3 22 ABXA9600324 1 19960111 A 2710 B538DD BEARING DOUG DC9 DC931 3022065 WP RT AILERON WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 DURING C-CHECK INSPECTION, FOUND THE RIGHT AILERON TRIM TAB LINKAGE WORN. REPLACED TRIM TAB LINKAGE BEARINGS IAW DC-9 M M 20-10-1. 2 L 7 2 4F A6WE 1996032200363 19960322 00363 WP 1996 3 22 ABXA9600325 1 19960118 A 5753 5912158501 ANGLE DOUG DC9 DC931 3022065 WP LT FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 DURING C-CHECK INSPECTION, FOUND THE LEFT WING OUTBOARD FLAP HINGE ATTACH ANGLE INSIDE THE FLAP CRACKED. REPLACED ANGLE IAW DC-9 SRM 51-30-1. 2 L 7 2 4F A6WE 1996032200364 19960322 00364 WP 1996 3 22 ABXA9600326 1 19960112 A 5730 59205212 TRAILING EDGE DOUG DC9 DC931 3022065 WP RT WING DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 DURING C-CHECK INSPECTION, FOUND THE RIGHT WING OUTBAORD TRAILING EDGE ASSEMBLY DELAMINATED. REPAIRED IAW DC-9 SRM 51-7 0-2. 2 L 7 2 4F A6WE 1996032200365 19960322 00365 WP 1996 3 22 ABXA9600327 1 19960117 A 5753 995760010 ANGLE DOUG DC9 DC931 3022065 WP RT FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 DURING C-CHECK INSPECTION, FOUND THE RIGHT WING OUTBOARD FLAP ATTACH ANGLE INSIDE FLAP CRACKED. REPLACED ANGLE IAW DC-9 SRM 51-30-1. 2 L 7 2 4F A6WE 1996032200366 19960322 00366 WP 1996 3 22 ABXA9600328 1 19960115 A 5753 49135661 FITTING DOUG DC9 DC931 3022065 WP RT FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 DURING C-CHECK INSPECTION, FOUND THE UPPER FITTING INSIDE OUTBOARD EXPANSION JOINT ON THE RIGHT FLAP CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-2 AND 51-30-1. 2 L 7 2 4F A6WE 1996032200367 19960322 00367 WP 1996 3 22 ABXA9600329 1 19960114 A 5400 5913262 ANGLE DOUG DC9 DC931 3022065 WP RT PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 DURING C-CHECK INSPECTION, FOUND THE RIGHT PYLON UPPER ATTACH ANGLE CRACKED NEAR THE FORWARD END. REPAIRED IAW DC-9 SRM 54-04, FIGURE 10. 2 L 7 2 4F A6WE 1996032200368 19960322 00368 WP 1996 3 22 ABXA9600330 1 19960115 A 5400 5913262 ANGLE DOUG DC9 DC931 3022065 WP RT PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 DURING C-CHECK INSPECTION, FOUND THE RIGHT PYLON UPPER ATTACH ANGLE CRACKED NEAR THE CENTER. REPAIRED IAW DC-9 SRM 54-0 4, FIGURE 10. 2 L 7 2 4F A6WE 1996032200369 19960322 00369 WP 1996 3 22 ABXA9600331 1 19960121 A 5347 S2914913 SEAT TRACK DOUG DC9 DC931 3022065 WP BS 278-872 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 DURING C-CHECK INSPECTION, FOUND THE MAIN CABIN SEAT TRACKS CRACKED, WORN AND CORRODED AT PERMANENT LOCK ATTACH POINTS. REPAIRED IAW ABX REA RE-14184-MR. 2 L 7 2 4F A6WE 1996032200370 19960322 00370 WP 1996 3 22 ABXA9600332 1 19960115 A 5230 59101413 SKIN DOUG DC9 DC931 3022065 WP CARGO DOOR BLENDED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 DURING C-CHECK INSPECTION, FOUND DEEP BLEND OUT ON AFT EDGE OF THE FORWARD LOWER CARGO DOOR SKIN. REPAIRED IAW ABX REA D952-14076-MR. 2 L 7 2 4F A6WE 1996032200371 19960322 00371 WP 1996 3 22 ABXA9600333 1 19960120 A 5320 5956879501 JAMB DOUG DC9 DC931 3022065 WP BS 200 DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 DURING C-CHECK INSPECTION, FOUND THE ENTRY DOOR AFT JAMB INNER SKIN AT STA 200 DENTED AND TORN. REPAIRED IAW ABX REA D9 53-14173-MR. 2 L 7 2 4F A6WE 1996032200372 19960322 00372 WP 1996 3 22 ABXA9600334 1 19960121 A 5320 99101553 PRESSURE PANEL DOUG DC9 DC931 3022065 WP BS 737-756 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 DURING C-CHECK INSPECTION, FOUND CORROSION ON THE PRESSURE PANEL BETWEEN RBL 37 AND LBL 37 STA 737 TO 756. REPAIRED IAW ABX REA D953-14154-MR. 2 L 7 2 4F A6WE 1996032200373 19960322 00373 WP 1996 3 22 ABXA9600335 1 19960116 A 5711 5911301502 SPAR CAP DOUG DC9 DC931 3022065 WP WS 530 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 DURING C-CHECK INSPECTION, FOUND CORROSION ON THE RIGHT WING LOWER SPAR CAP AT XW-530. REPAIRED IAW ABX REA D957-14078- MR. 2 L 7 2 4F A6WE 1996032200374 19960322 00374 WP 1996 3 22 ABXA9600336 1 19960125 A 5711 5911301502 SPAR CAP DOUG DC9 DC931 3022065 WP WS 530 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 DURING C-CHECK INSPECTION, FOUND RIGHT WING AFT SPAR LOWER CAP CORRODED 12 INCHES FROM THE OUTBOARD AILERON HINGE. REPA IRED IAW DC-9 SRM 57-09, FIGURE 11 AND ABX REA D957-14179. 2 L 7 2 4F A6WE 1996032200375 19960322 00375 WP 1996 3 22 ABXA9600337 1 19960229 A 5753 5910042503 VANE DOUG DC9 DC931 3022065 WP LT TE FLAP DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 DURING C-CHECK INSPECTION, FOUND LEADING EDGE OF THE LEFT WING NR 2 FIXED VANE DELAMINATED. REPLACED VANE IAW DC-9 MM 2 7-51-3. 2 L 7 2 4F A6WE 1996032200376 19960322 00376 WP 1996 3 22 ABXA9600338 1 19960302 A 5752 59104141 TAB DOUG DC9 DC931 3022065 WP LT ELEVATOR DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 DURING C-CHECK INSPECTION, FOUND LEFT ELEVATOR OUTBOARD TAB DENTED AND DELAMINATED. REPLACED TAB IAW DC-9 MM 27-30-4. 2 L 7 2 4F A6WE 1996032200377 19960322 00377 WP 1996 3 22 ABXA9600339 1 19960227 A 5511 5918000530 SPAR CAP DOUG DC9 DC931 3022065 WP LT HORIZ STAB CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON THE LEFT HORIZONTAL STABILIZER SPAR UPPER CAP. REPAIRED IAW ABX R EA D955-14656-MR. 2 L 7 2 4F A6WE 1996032200378 19960322 00378 WP 1996 3 22 ABXA9600340 1 19960227 A 5511 5918000530 SPAR CAP DOUG DC9 DC931 3022065 WP RT HORIZ STAB CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON THE RIGHT HORIZONTAL STABILIZER SPAR UPPER CAP. REPAIRED IAW ABX REA D955-14630-MR. 2 L 7 2 4F A6WE 1996032200379 19960322 00379 WP 1996 3 22 ABXA9600341 1 19960227 A 5511 5918000529 SPAR CAP DOUG DC9 DC931 3022065 WP RT HORIZ STAB CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON THE RIGHT HORIZONTAL STABILIZER SPAR, UPPER CAP. REPAIRED IAW ABX REA D955-14630-MR. 2 L 7 2 4F A6WE 1996032200380 19960322 00380 WP 1996 3 22 ABXA9600342 1 19960218 A 5400 5913262 ANGLE DOUG DC9 DC931 3022065 WP LT PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 DURING C-CHECK INSPECTION, FOUND A CRACK AROUND FASTENER ON THE LEFT PYLON UPPER ATTACH ANGLE. REPAIRED IAW DC-9 SRM 54 -04, FIG 10. 2 L 7 2 4F A6WE 1996032200381 19960322 00381 WP 1996 3 22 ABXA9600343 1 19960221 A 5330 591140659 SKIN DOUG DC9 DC931 3022065 WP BS 180 GOUGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 DURING C-CHECK INSPECTION, FOUND DEEP GOUGES IN THE FUSELAGE SKIN AT THE EDGE OF THE ENTRANCE DOOR. REPAIRED IAW ABX RE A D953-14638-MR. 2 L 7 2 4F A6WE 1996032200382 19960322 00382 WP 1996 3 22 ABXA9600344 1 19960219 A 5320 3916209502 BRACKET DOUG DC9 DC931 3022065 WP BS 680 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 DURING C-CHECK INSPECTION, FOUND FLOOR SUPPORT BRACKET CRACKED AT STA 680, RBL 45. REPLACED IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 1996032200383 19960322 00383 WP 1996 3 22 ABXA9600345 1 19960222 A 5320 991968914 BRACKET DOUG DC9 DC931 3022065 WP BS 658 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 DURING C-CHECK INSPECTION, FOUND FLOOR SUPPORT BRACKET ATTACH ANGLE CRACKED AT STA 658. REPLACED BRACKET IAW DC-9 SRM 5 1-30-5. 2 L 7 2 4F A6WE 1996032200384 19960322 00384 WP 1996 3 22 ABXA9600346 1 19960222 A 5311 99581982 FRAME DOUG DC9 DC931 3022065 WP BS 617 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 DURING C-CHECK INSPECTION, FOUND FRAME AT STA 617 RIGHT CRACKED. REPAIRED IAW DC-9 SRM 53-03, FIGURE 16. 2 L 7 2 4F A6WE 1996032200385 19960322 00385 WP 1996 3 22 ABXA9600347 1 19960220 A 5320 3916209501 FITTING DOUG DC9 DC931 3022065 WP BS 680 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 DURING C-CHECK INSPECTION, FOUND A CRACK IN THE SEAT TRACK TO BEAM SUPPORT FITTING AT STA 680, LBL 44. REPLACED FITTING IAW DC-9 SRM 51-30-2 AND 51-30-1. 2 L 7 2 4F A6WE 1996032200386 19960322 00386 WP 1996 3 22 ABXA9600348 1 19960219 A 5531 99118227 RIB DOUG DC9 DC931 3022065 WP VERT STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 DURING C-CHECK INSPECTION, FOUND VERTICAL STABILIZER LEADING EDGE RIB CRACKED. REPAIRED IAW DC-9 SUPP SRM DRAWING K0549 8. 2 L 7 2 4F A6WE 1996032200387 19960322 00387 WP 1996 3 22 ABXA9600349 1 19960219 A 5531 99118215 RIB DOUG DC9 DC931 3022065 WP VERT STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 DURING C-CHECK INSPECTION, FOUND VERTICAL STABILIZER LEADING EDGE RIB CRACKED. REPAIRED IAW DC-9 SUPP SRM DRAWING K0515 9. 2 L 7 2 4F A6WE 1996032200388 19960322 00388 WP 1996 3 22 ABXA9600350 1 19960219 A 5531 99118316 RIB DOUG DC9 DC931 3022065 WP VERT STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 DURING C-CHECK INSPECTION, FOUND VERTICAL STABILIZER LEADING EDGE RIB CRACKED. REPAIRED IAW DC-9 SUPP SRM DRAWING K0549 8. 2 L 7 2 4F A6WE 1996032200389 19960322 00389 WP 1996 3 22 ABXA9600351 1 19960226 A 5531 99118306 RIB DOUG DC9 DC931 3022065 WP VERT STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 DURING C-CHECK INSPECTION, FOUND THE VERTICAL STABILIZER TOP LEADING EDGE HAD A CRACKED LEFT RIB BELOW PANEL 6307. REPA IRED IAW DC-9 SUPP SRM DRAWING K05159. 2 L 7 2 4F A6WE 1996032200390 19960322 00390 WP 1996 3 22 ABXA9600352 1 19960223 A 5531 991188310 RIB DOUG DC9 DC931 3022065 WP VERT STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 DURING C-CHECK INSPECTION, FOUND THE VERTICAL STABILIZER LEADING EDGE RIB CRACKED. REPAIRED IAW DC-9 SUPPLEMENTAL SRM D RAWING K05159. 2 L 7 2 4F A6WE 1996032200391 19960322 00391 WP 1996 3 22 ABXA9600353 1 19960223 A 5531 99118849 RIB DOUG DC9 DC931 3022065 WP VERT STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 DURING C-CHECK INSPECTION, FOUND THE VERTICAL STABILIZER LEADING EDGE RIB CRACKED. REPAIRED IAW DC-9 SUPP SRM DRAWING K 05159. 2 L 7 2 4F A6WE 1996032200392 19960322 00392 SO 1996 3 22 COMA9610104 1 19960228 A 3244 0286780 TIRE EMB 120 EMB120RT SO RT MLG FAILED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 247CA 120225 RT MLG TIRE FAILED DURING TAKEOFF ROLL. REPLACED RT WHEEL TIRE ASSY. 2 L 7 2 4T RT A31SO 1996032200393 19960322 00393 SO 1996 3 22 COMA9610105 1 19960201 A 5270 SWITCH EMB 120 EMB120RT SO CARGO DOOR OUT OF ADJUST A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 243CA 120212 CARGO DOOR WARNING LIGHT ILLUMINATED DURING TAKEOFF ROLL. ADJUSTED CARGO DOOR MICRO SWITCH. 2 L 7 2 4T RT A31SO 1996032200394 19960322 00394 SO 1996 3 22 COMA9610106 1 19960318 A 5230 12020773001 ROLLER EMB 120 EMB120RT SO CARGO DOOR WORN A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 130G 120130 CARGO DOOR WILL NOT OPEN. FORWARD LOWER ROLLER CAME OUT OF THE TRACK. REPLACED DOOR ROLLER, OPERATES NORMAL. 2 L 7 2 4T RT A31SO 1996032200395 19960322 00395 SW 1996 3 22 COMA9620005 1 19960313 A 2720 27420519011 TORQUE TUBE SWRNGN SA227 SA227AC 8780603 SW RUDDER BENT A COMA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 703CA AC703 RUDDER PEDALS ARE OFFSET IN FLIGHT. FOUND RUDDER TORQUE TUBE BENT. REPLACED TORQUE TUBE. 1 L 7 2 4T A8SW 1996032200396 19960322 00396 EU 1996 3 22 COMA9630068 1 19960313 A 2730 DL3827M157 ACTUATOR SAAB SF340 SF340A 7850100 EU LT ELEV FAILED A COMA K NONE F FLT CONT AFFECTED UK UNKNOWN 1 SO 01 356CA 16152 220 340A034 MAIN PITCH TRIM IS INOP. REPLACED LT PITCH TRIM ACTUATOR. 2 L 7 2 4T RT A52EU 1996032200397 19960322 00397 EU 1996 3 22 COMA9630069 1 19960318 A 2510 010890053 SHOULDER HARNESS SAAB SF340 SF340A 7850100 EU COPILOTS MALFUNCTIONED A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 158CA 340A158 COPILOTS SHOULDER HARNESS LOCK DOES NOT WORK. REPLACED SHOULDER HARNESS. 2 L 7 2 4T RT A52EU 1996032200398 19960322 00398 NE 1996 3 22 COMA9630070 3 19960318 A 6114 7503503AG O-RING SAAB SF340 SF340A 7850100 EU ROTOL R389 R3894123F25 NE RT PROP WORN A COMA O OTHER O OTHER LD LANDING 1 SO 01 340SF 2624 340A014 176385 RT PROPELLER RPM DROPPED TO 1340 DURING LANDING. REPLACED THE PROPELLER PISTON DOME O-RING. 2 L 7 2 4T RT A52EU 6 C P30NE 1996032200399 19960322 00399 EA 1996 3 22 COMA9660046 1 19960314 A 2750 855D1005 BPSU CNDAIR CL600 CL6002B19 EA LT TE FLAP MALFUNCTION A COMA K NONE O OTHER CL CLIMB 1 SO 01 933CA 4359 1678 7040 FLAPS FAILED AT 8 DEGREES, WHEN SELECTED UP AFTER TAKEOFF. REPLACED THE LT FLAP BRAKE AND POSITION SENSOR. 2 L 7 2 4F RT A21EA 1996032200400 19960322 00400 EA 1996 3 22 COMA9660047 1 19960312 A 2823 B9731653 SHUT OFF VALVE CNDAIR CL600 CL6002B19 EA RT ENGINE FAILED A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 920CA 7022 RT ENGINE FUEL SHUT OFF VALVE FAILED. REPLACED VALVE. 2 L 7 2 4F RT A21EA 1996032200401 19960322 00401 EA 1996 3 22 COMA9660048 1 19960318 A 5270 840534 PROX SWITCH CNDAIR CL600 CL6002B19 EA CABIN DOOR DEFECTIVE A COMA K NONE N FALSE WARNING CR CRUISE 1 SO 01 947CA 7077 PASSENGER DOOR WARNING ON EICAS DURING FLIGHT. REPLACED THE DOOR HANDLE PROXIMITY SWITCH. 2 L 7 2 4F RT A21EA 1996032200402 19960322 00402 1996 3 22 MWEA96060 4 19960318 A 2565 13621225 EVAC SLIDE DOUG DC9 DC932 3022066 WP TAIL CONE LOW PRESSURE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 AFT ACCESSORY COMPARTMENT TAIL EVAC SLIDE PRESSURE READS BELOW MINIMUM. REPLACED TAIL EVACUATION SLIDE ASSY. 2 L 7 2 4F A6WE 1996032200403 19960322 00403 WP 1996 3 22 MWEA96061 1 19960318 A 5330 SKIN DOUG DC9 DC915 3022036 WP FS 737/786 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 AFT FUS UPPER SKIN CRACKS, FS 786, LONG 7L, 1 INCH AND .75 INCH IN LENGTH, ONE AT FS 737, LONG 7L, .75 INCH IN LENGTH. R EPAIRED CRACKS IAW DC9 SRM 53-04, FIG 38. 2 L 7 2 4F A6WE 1996032200404 19960322 00404 WP 1996 3 22 MWEA96062 1 19960316 A 5330 SKIN DOUG DC9 DC915 3022036 WP FS 859 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 DURING C-CHECK, FOUND SKIN CRACK AT FS 859, .25 INCH IN LENGTH EMANATING FROM FASTENER HOLE LONGERON 13R. INSTALLED DOU BLER REPAIR IAW SRM 53-01, FIG 2 SHEET 3. 2 L 7 2 4F A6WE 1996032200405 19960322 00405 NM 1996 3 22 UPS96205691 1 19960311 A 5311 FRAME BOEING 727 72727C 138400J NM BS 212 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON LOWER END OF FRAME AT BS 212 LBL 16 WL 168. REMOVED CORROSION, FABRICATED NEW WEB AND INSTALLED PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996032200406 19960322 00406 NM 1996 3 22 UPS96205692 1 19960310 A 5313 STRINGER BOEING 727 72727C 138400J NM BS 993 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED STR AT STA 993 CRACKED. STOP DRILLED AND SPLICED IN REPAIR IAW MM 51-20-31 SRM 53-10-3, 51-30-2, AND 51-20-4. 2 L 7 3 4F A3WE 1996032200407 19960322 00407 NM 1996 3 22 UPS96205693 1 19960309 A 5754 RIB BOEING 727 72727C 138400J NM NR 6 LE SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED NR 6 SLAT HAS CRACK ON FIRST RIB I/B FROM O/B END. REMOVED AND REPLACED RIB IAW SRM 57-50-3. 2 L 7 3 4F A3WE 1996032200408 19960322 00408 NM 1996 3 22 UPS96205694 1 19960305 A 5741 106051616 BUSHING BOEING 727 72727C 138400J NM LT WING/FUS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION LEFT FRONT BOTTLE PIN BUSHING, ON FWD FACE. REMOVED AND REPLACED BUSHING IAW MM 57-41-11 AND 57-10-7. 2 L 7 3 4F A3WE 1996032200409 19960322 00409 NM 1996 3 22 UPS96205695 1 19960310 A 5752 652172630 SKIN BOEING 727 72727C 138400J NM RT AILERON TAB DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED RT WING O/B AILERON TAB I/B AND SKIN IS DELAMINATED UPPER SURFACE. REPAIRED RIGHT WING OUTBOARD AILERON TAB IAW SRM 51-40-6 AND 51-80-6. 2 L 7 3 4F A3WE 1996032200410 19960322 00410 NM 1996 3 22 UPS96205696 1 19960217 A 5315 FLOOR BEAM BOEING 727 727185C 138406N NM FS 680 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 680 RBL 3 TO 10, FLOOR BEAM UPPER FLANGE IS CORRODED BEYOND LIMITS. REMOV ED DAMAGED SECTION FROM LBL 9 TO RBL 65.0 IAW SRM 53-10-8 FIG 5, REPAIRED IAW SRM 53-10-8 AND 51-30-3. 2 L 7 3 4F A3WE 1996032200411 19960322 00411 NM 1996 3 22 UPS96205697 1 19960226 A 5320 ATTACH CHANNEL BOEING 727 727185C 138406N NM BS 312 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FUS STA 312 STR 19R, STRINGER TO FRAME ATTACH CHANNEL IS CRACKED. REMOVED, F ABRICATED AND INSTALLED ATTACH CHANNEL PER SRM 53-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 1996032200412 19960322 00412 NM 1996 3 22 UPS96205698 1 19960214 A 5320 FRAME CLIP BOEING 727 727185C 138406N NM FS 328 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FRAME CLIP CRACKED AT STA 328 STR 13R. CUT OUT DAMAGED FRAME SECTION IAW SRM 53-10-4, FABRICATED NEW FRAME/SPLICES IAW SRM 53-10-4 AND INSTALLED IAW SRM 53-10-4 AND 51-30-2. 2 L 7 3 4F A3WE 1996032200413 19960322 00413 NM 1996 3 22 UPS96205699 1 19960221 A 5313 STRINGER BOEING 727 727185C 138406N NM FS 1160 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION BEYOND LIMITS AT STR 22R FS 1160 REF N/R 429045 FOR CORROSION REMOV AL. CUT OUT WAS MADE FROM STA 1158 TO STA 1173 STR 22R. FABRICATED SPLICE SECTION PER SRM 53-10-3 FIG 1 AND INSTALLED PARTS PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996032200414 19960322 00414 NM 1996 3 22 UPS96205700 1 19960310 A 5330 SKIN BOEING 727 727185C 138406N NM STA 304 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON SKIN AT STA 304 STR 14R, OUT OF LIMITS. REMOVED DAMAGED AREA IA W SRM 53-30-3. FABRICATED AND INSTALLED REPAIR IAW SRM 53-30-3 FIG 5. 2 L 7 3 4F A3WE 1996032200415 19960322 00415 NM 1996 3 22 UPS96205701 1 19960306 A 5315 FLOOR BEAM BOEING 727 727185C 138406N NM FS 640 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FWD LOWER CARGO STA 640 BETWEEN LBL 44 TO 62. FLOOR BEAM UPPER FLANGE AFT SI DE HAS HEAVY EXFOLIATION CORROSION IN SEVERAL PLACES. REPAIRED DAMAGE AREA OF FLOOR BEAM LBL 8 TO LBL 62 IAW SRM 53-10- 8 FIG 5, SRM 51-30-2. 2 L 7 3 4F A3WE 1996032200416 19960322 00416 NM 1996 3 22 UPS96205702 1 19960209 A 5720 STIFFENER BOEING 727 727185C 138406N NM WS 171 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT FRONT SPAR VERTICAL STIFFENER INB OF NR 3 TANK FUELING VALVE HAS CORROSION AT BONDING WIRE. REMOVED DAMAGED STIFFENER, FABRICATED REPLACEMENT STIFFENER IAW SRM 51-10-1 AND INSTALLED IAW SRM 51- 30-2. 2 L 7 3 4F A3WE 1996032200417 19960322 00417 NM 1996 3 22 UPS96205703 1 19960316 A 3350 BATTERIES BOEING 727 727180C 138406G NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 920UP 19873 WHILE ON GROUND, MAINTENANCE REPORTED BOTH EMERGENCY EXIT LIGHTS ARE INOP. INSTALLED S-106 BATTERIES IN BOTH EMERGENCY EXIT LIGHTS, MODULES AND FUNCTION CHECKED SERVICEABLE. 2 L 7 3 4F A3WE 1996032200418 19960322 00418 NM 1996 3 22 UPS96405676 1 19960314 A 5730 SKIN BOEING 747 747121 1384871 NM RT WING LE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 WHILE IN FOR C-CHECK AT AMS, MAINTENANCE REPORTED RT WING UPPER SIDE FOUND CORROSION ROUND FASTENER HEADS AT WS 550. RE WORKED CORROSION PER SRM 51-10-01. REWORKED AREA OUT OF LIMITS PER SRM 57-30-01. REWORKED WING NOSE PER SRM 57-30-04 F IG 2. 2 L 7 4 4F A20WE 1996032200419 19960322 00419 NM 1996 3 22 UPS96405677 1 19960314 A 5730 SKIN BOEING 747 747121 1384871 NM WS 500 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 WHILE IN FOR C-CHECK AT AMS, MAINTENANCE REPORTED RT WING UPPER SIDE FOUND CORROSION ROUND FASTENER HEADS AT WS 500. RE WORKED CORROSION PER SRM 51-10-01. REWORKED AREA OUT OF LIMITS PER SRM 57-30-01 FIG 4. REWORKED WING NOSE PER SRM 57-3 0-04 FIG 2. 2 L 7 4 4F A20WE 1996032200420 19960322 00420 NM 1996 3 22 UPS96405678 1 19960314 A 5730 SKIN BOEING 747 747121 1384871 NM WS 460 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 WHILE IN FOR C-CHECK AT AMS, MAINTENANCE REPORTED RT WING UPPER SIDE FOUND CORROSION AROUND FASTENER HEADS AT WS 460. R EWORKED CORROSION PER SRM 51-10-01. REWORKED AREA OUT OF LIMITS PER SRM 57-30-01 FIG 4. REWORKED WING NOSE PER SRM 57- 30-04 FIG 2. 2 L 7 4 4F A20WE 1996032200421 19960322 00421 NM 1996 3 22 UPS96405679 1 19960313 A 3350 1000679 LIGHT BOEING 727 727180C 138406G NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 921UP 19874 MAINTENANCE REPORTED, COCKPIT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY PER MM 33-50-10 1. 2 L 7 3 4F A3WE 1996032200422 19960322 00422 NM 1996 3 22 UPS96405704 1 19960306 A 5320 ANGLE BOEING 747 747121 1384871 NM BS 2200 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED AREA AFT OF BULK CARGO COMP, CRACKS WERE FOUND IN INNER ANGLE OF FRAME UP PER FLANGE, DUE TO CORROSION AT BS 2200, NEAR S-36 RT. REPLACED INNER ANGLE OF FRAME UPPER FLANGE AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 1996032200423 19960322 00423 NM 1996 3 22 UPS96405705 1 19960307 A 5320 HINGE PLATES BOEING 747 747121 1384871 NM BS 1010/1033 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED WING TO BODY FAIRING SUPP STRU/ACFT BAY DOORS, FOUND HINGE POINT ATTACH P LATES CRACKED DUE TO DELAMINATION OF SHIMS BETWEEN ATTACH PLATES AND KEEL BEAM STRUCTURE LBL 8 BS 1010 AND BS 1033. REP LACED HINGE POINT ATTACH PLATES AND SHIMS PER SRM 51-30-02. 2 L 7 4 4F A20WE 1996032200424 19960322 00424 WP 1996 3 22 UPS96805680 1 19960313 A 5400 5753054 ANGLE DOUG DC8 DC873F 302199F WP PYLON DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED WING FRONT SPAR PYLON SUPPORT FITTING REPLACEMENT. REWORKED NR 2 AND NR 3 PY LON FOOTSTOOL FITTING T-DOUBLER/SKATE ANGLE IAW UPS EO DC8-57-061. 2 L 7 4 4F RT 4A25 1996032200425 19960322 00425 WP 1996 3 22 UPS96805681 1 19960313 A 5742 5753054 FITTING DOUG DC8 DC873F 302199F WP PYLON DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED WING FRONT SPAR PYLON SUPPORT FITTING REPLACEMENT. REWORKED NR 2 AND NR 3 PY LON FOOTSTOOL FITTING IAW UPS EO DC8-57-0641. 2 L 7 4 4F RT 4A25 1996032200426 19960322 00426 WP 1996 3 22 UPS96805682 1 19960313 A 5330 SKIN DOUG DC8 DC873F 302199F WP C4 DOOR CUTOUT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED C-4 DOOR CUTOUT, FWD UPPER CORNER CRACKED APPROX .25 INCH LONG. FABRICATED R EPAIR USING 7075-T6 AND INSTALLED IAW DC-8 SRM 53-2-0, 51-1-21, AND 51-1-20D. 2 L 7 4 4F RT 4A25 1996032200427 19960322 00427 WP 1996 3 22 UPS96805683 1 19960313 A 5210 SKIN DOUG DC8 DC873F 302199F WP R 1 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED R-1 DOOR FRAME FUSELAGE SKIN CRACKED ON LOWER AFT CORNER. FABRICATED FILLER, DOUBLER, TRIPLER AND INSTALLED IAW DC-8 SRM 53-2-0, 51-1-21, AND 51-1-21D. 2 L 7 4 4F RT 4A25 1996032200428 19960322 00428 WP 1996 3 22 UPS96805684 1 19960205 A 5754 SKIN DOUG DC8 DC873F 302199F WP RT TE SLAT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT I/B SLAT UPPER SURFACE PITTED AND MODERATE CORROSION. REPLACED SLAT PANEL PER SRM 51-3-0. 2 L 7 4 4F RT 4A25 1996032200429 19960322 00429 WP 1996 3 22 UPS96805685 1 19960214 A 5320 52597266 ANGLE DOUG DC8 DC873F 302199F WP FS 70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON CHORD ANGLE AT FS 70 BETWEEN LONGERONS 31R TO 32R. WILL B E REPAIRED ON TASK CARD NR 423121 PENDING APPROVAL. 2 L 7 4 4F RT 4A25 1996032200430 19960322 00430 WP 1996 3 22 UPS96805686 1 19960212 A 5330 SKIN DOUG DC8 DC873F 302199F WP FS 120 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MAIN CARGO DOOR FWD UPPER CORNER OF CUTOUT HAS CRACKED FUSELAGE SKIN. REPAIR ED PER UPS EO DC8-5330-7812A. 2 L 7 4 4F RT 4A25 1996032200431 19960322 00431 WP 1996 3 22 UPS96805687 1 19960215 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP FS 930 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED 6 SHEARED FASTENERS DUE TO CORROSION DAMAGE ON WHEEL WELL COILING DOUBLER, FS 930 BL 0. REPLACED DOUBLER SECTION PER SRM 51-1-20D AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1996032200432 19960322 00432 WP 1996 3 22 UPS96805688 1 19960215 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP FS 912 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED 1 SHEARED FASTENER DUE TO CORROSION DAMAGE ON WHEEL WELL COILING DOUBLER FS 9 12 RBL 1. REPLACED DOUBLER SECTION PER SRM 51-1-20D AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1996032200433 19960322 00433 WP 1996 3 22 UPS96805689 1 19960215 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP FS 875 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED 2 SHEARED FASTENERS DUE TO CORROSION DAMAGE ON WHEEL WELL COILING DOUBLER FS 875 LBL 1. REPLACED DOUBLER SECTION PER SRM 51-1-20D AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1996032200434 19960322 00434 WP 1996 3 22 UPS96805690 1 19960215 A 5412 BLKHD LWR CAP DOUG DC8 DC873F 302199F WP NR 3 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED NR 3 PYLON I/B SUPPORT BULKHEAD FWD LOWER CAP HAS A 17 INCH LONG CRACK. REPA IRED PER UPS EO DC8-57-0647. 2 L 7 4 4F RT 4A25 1996032200435 19960322 00435 NE 1996 3 22 VNAA9600001 2 19960318 A 7310 3035861 HP FUEL FILTER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE RT ENGINE DIRTY A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 07 439JS 3057 PCE116123 HP FUEL FILTER BYPASS WARNING ON TAKEOFF. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MX REPLACED THE RT ENGINE HP FUEL FILTER IAW MM 73-00-00, GROUND CHECKED GOOD. 2 H 7 2 4T 4 T RT A45NM E20NE 1996032200479 19960322 00479 NM 1996 3 22 96ZZZX1289 1 19960130 A 3150 CONNECTOR BOEING 767 7673Y0 NM NR 2 TRANSDUCER DIRTY A TWAA O OTHER N FALSE WARNING CR CRUISE 1 CE 05 EICAL 24952 JFK - FLT 901 - DURING CRUISE, BOTH EICAS ANTI-SKID LIGHTS ILLUMINATED. CLEANED AND RESEATED NR 2 TRANSDUCER CONNECTOR. PERFORMED BITE CHECK, SYSTEM TESTED NORMAL, NO FAULTS NOTED. CHECK C-C4A - 11-15-95 - LAX. (IRELAND) 2 L 7 2 4F RT A1NM 1996032200480 19960322 00480 WP 1996 3 22 96ZZZX1290 1 19960130 A 3222 STRUT DOUG DC9 DC983 3022083 WP NLG REQ'D SERVICE A TWAA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 EICIW 49785 TPA - FLT 427 - DURING CLIMB, NLG DOOR FAILED TO RETRACT. SERVICED NLG STRUT. OPERATIONAL CHECK NORMAL. CHECK C-01 - 6-27-95 - MCI. (IRELAND) 2 L 7 2 4F RT A6WE 1996032200481 19960322 00481 EU 1996 3 22 HEEA966843 1 19960313 A 6520 350A33200403 SPIDER SNIAS 350 AS350B2 8680813 EU TAIL ROTOR WORN BEARING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 350BZ 1562 2653 PART IS WORN EXCESSIVELY. (WORN BEARINGS) 1 G 7 1 3U H9EU 1996032200482 19960322 00482 SW 1996 3 22 HEEA966844 1 19960313 A 6220 206011149105 YOKE 206011100159 BELL 206 206L1 1182107 SW M/R BEARING FAIL E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2133X 955 A2416 45634 ASSEMBLY CAME IN DUE TO TRUNNION PIN RETIREMENT. FOUND TRUNNION BEARINGS BREAKING DOWN AND THRUST PLUGS BREAKING DOWN. REMOVED GRIPS DUE TO SEAL LEAK AND FOUND OUTBOARD BEARING JOURNALS BREAKING DOWN. REPLACEMENT PART INFORMATION LISTED B ELOW: 2 EACH, BEARING P/N 206-011-111-001, 2 EACH, SCREWS P/N 206-010-111-105, 4 EACH, BEARINGS P/N 206-011-118-001, 2 EACH, THRUST WASHER P/N 206-010-110-105, 1 G 7 1 3U H2SW 1996032200483 19960322 00483 NE 1996 3 22 HEEA966845 1 19960313 A 6210 7615009100051A BLADE SKRSKY S76 S76A 8143006 NE M/R UNBONDED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22342 11694 760096 INSPECTION DUE FOR TIME EXTENSION. THE TIP RIB IS UNBONDED, THE NICKEL STRIP HAS NUMEROUS CRACKS WITH SMALL AREAS UNBON DED. 1 G 7 2 3U H1NE 1996032200484 19960322 00484 1996 3 22 HEEA966846 4 19960313 A 2312 4000103000 TRANSCEIVER RT450 BOLKMS 117 BK117B2 5626013 EU COCKPIT VHF DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 132AE 7238 TRANSMITTER CUTS OUT AFTER ABOUT 5 SECONDS. 1 G 7 2 3U NC H13EU 1996032200485 19960322 00485 1996 3 22 HEEA966847 4 19960313 A 2312 4000098000 TRANSCEIVER BOLKMS 117 BK117B1 5626012 EU COCKPIT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 217UC 7152 WILL NOT RECEIVE OR TRANSMIT, PROBLEM ON SYNTHESIZER BOARD. 1 G 7 2 3U H13EU 1996032200486 19960322 00486 1996 3 22 HEEA966848 4 19960313 A 2312 4000106010 CONTROL UNIT C10 BOLKMS 105 BO105CBS 5626008 EU COCKPIT VHF FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5418A S800 UNABLE TO PROGRAM IN MANUAL POSITION. 1 G 7 2 3U NC H3EU 1996032200487 19960322 00487 1996 3 22 HEEA966849 4 19960313 A 3442 MI5851352 R/T UNIT BELL 412 412 1182202 SW RADAR DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2149S 36002 NO NOISE BAND IN TEST, ALSO FOUND RECEIVER SENSITIVITY VERY WEAK. 1 G 7 2 4U H4SW 1996032200488 19960322 00488 1996 3 22 HEEA966850 4 19960313 A 3444 066104802 ALTIMETER KRA405 BELL 412 412 1182202 SW RADAR ALT ERROR E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 21498 36003 READS LOWER THAN ACTUAL ALTITUDE AND ERRATIC. FOUND PRECISION EQUIPMENT VOLTAGE TO EITHER DOUBLE OR HALF WHEN AMPLITUDE IS CHANGED. FOUND PROBLEM TO BE ON CAL/LOOP BOARD. REPLACED INTEGRATED CIRCUITS I501,I502,I503,I504,I505,I507,I508, TR ANSISTORS Q501 THROUGH Q512; DIODES CR503,CR521,CR508;CAPACITORS C506 AND C520. REPLACED CAL/LOOP BOARD. REPAIRED. RE PLACED RESISTORS R518,R519,R534 AND R260 TO INCORPORATE MOD 10 AS PER KING SERVICE BULLETIN KRA-405-10. BENCH CHECK GOO D. 1 G 7 2 4U H4SW 1996032200489 19960322 00489 1996 3 22 HEEA966851 4 19960313 A 3453 25410038 LORAN 7000CDU BELL 412 412 1182202 SW LORAN CDU DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 22608 33075 SEVERAL LED'S ARE INOPERATIVE. 1 G 7 2 4U H4SW 1996032200490 19960322 00490 1996 3 22 HEEA966852 4 19960313 A 3453 25410036 LORAN 7000RCU BELL 412 412 1182202 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 22608 33075 LOCKS UP AND DISPLAYS WARNING CODES. 1 G 7 2 4U H4SW 1996032200491 19960322 00491 1996 3 22 HEEA966853 4 19960313 A 2312 069102525 TRANSCEIVER KX165 BOLKMS 105 BO105S 5626006 EU COCKPIT VHF FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 50293 S677 WOULD NOT RECEIVE OR TRANSMIT. FOUND CONNECTION ON E136 HAD A BURNT HOLE WITH CARBON BUILD UP ON IT. CLEANED BURNT HOLE AND HUMISEALED. REPAIRED. REPLACED BAD DISPLAY DS101. VOR BEARING OUT OF TOLERANCE. PERFORMED VOR/LOC CONVERTER ALI GNMENT, REPAIRED. BENCH CHECK GOOD. 1 G 7 2 3U H3EU 1996032200492 19960322 00492 1996 3 22 HEEA966854 4 19960313 A 2312 40001278500 TRANSCEIVER BOLKMS 117 BK117B2 5626013 EU COCKPIT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 134AE 7237 WILL NOT TRANSMIT. FOUND NO 29V ON POWER SUPPLY. REPLACED U2 (IC), U1 (IC),VR1 (DIODE) AND REPAIRED POWER SUPPLY. SYNT HESIZER BOARD HAS BAD TUNING VOLTAGE. REPLACED U11 (IC), U12 (IC), U13 (IC), U9 (IC), U10 (IC). REPAIRED. FOUND WEAK RECEIVER SENSE AT 406MHZ.ALIGNED THE RECEIVER AND ADJUSTED SYNTHESIZER PRESELECTOR VOLTAGE TO SPECS, REPAIRED. FOUND TR ANSMIT TONE SET A CODE 11 FOR A TONE OF 91.5HZ DRIFTING OFF FREQUENCY. REPLACED U14 (IC) ON AUDIO BOARD. REPAIRED. BE NCH CHECK GOOD. 1 G 7 2 3U NC H13EU 1996032200493 19960322 00493 EU 1996 3 22 HEEA966855 1 19960313 A 6210 10515141 BLADE BOLKMS 105 BO105S 5626006 EU M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5368F 4903 S718 PART IS CRACKED. (NOSE AND NECK SHELL CRACKED AND SEPARATED THERE ARE SEPARATION ALSO PRESENT ON THE THREE INBOARD LEAD ING EDGE ABRASION STRIP. 1 G 7 2 3U H3EU 1996032200494 19960322 00494 EU 1996 3 22 HEEA966856 1 19960313 A 6210 10515141 BLADE BOLKMS 105 BO105S 5626006 EU M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5368F 4904 S718 PART IS CRACKED. (NOSE AND NECK SHELL CRACKED AND. THE INBOARD STRIP HAS SEPARATION AT JOINT. 1 G 7 2 3U H3EU 1996032200495 19960322 00495 SW 1996 3 22 HEEA966857 1 19960313 A 6230 412040101127 MAST ASSY 412040366105 BELL 412 412 1182202 SW M/R CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893N 1460 A900050 33010 CORROSION BEYOND LIMITS IN BORE IN AREA "T". REPLACED MAST ASSEMBLY. 1 G 7 2 4U H4SW 1996032200496 19960322 00496 1996 3 22 HEEA966858 4 19960313 A 2312 064105430 TRANSCEIVER BELL 206 206L3 1182108 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 4282Z 51499 NO LED AFTER 20 MINUTES OF FLIGHT. ALSO WENT DEAD, AFTER SHUTOFF FOR 5 MINUTES NO LED BUT COULD T/R ON LOST SET FREQUEN CY. FOUND DISPLAY BOARD BURNT. REPLACED DISPLAY BOARD. NO HELP. REPLACED TRANSISTOR Q507. NO HELP. REPAIRED OPEN RU N FROM COLLECTOR OF Q503 TO LEG 1 OF TRANSFORMER T501. STILL NO DISPLAY. REPLACED DIODES CR504 AND CR505 AND TRANSFORM ER T501.REPAIRED. ADJUSTED SQUELCH AND SIDETONE. TOUCHED UP FACEPLATE WITH BLACK PAINT. BENCH CHECK GOOD. 1 G 7 1 3U H2SW 1996032200497 19960322 00497 SW 1996 3 22 HEEA966859 1 19960315 A 6710 222040061105 CASE ASSY BELL 230 230 1182149 SW M/R LINK BUSHING WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 2561 23009 WORN INBOARD IDLER LINK LUG BUSHINGS. 1 G 7 2 3U NC H9SW 1996032200498 19960322 00498 WP 1996 3 22 9606239925 1 19960315 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP CABIN NOT SEATED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 925US 47472 DURING LINE MAINTENANCE INSPECTION, FOUND OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. RESEATED BATTERIES IN PACKS, OPER ATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996032200499 19960322 00499 WP 1996 3 22 9606249929 1 19960317 A 3350 60030451 BATTERY PACK DOUG DC9 DC931 3022065 WP TAIL CONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8923E 45838 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL CONE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHE CK NORMAL. 2 L 7 2 4F A6WE 1996032200500 19960322 00500 WP 1996 3 22 9606259937 1 19960315 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 908H 47517 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS IN FORWARD CABIN AND AT GALLEY SERVICE DOOR INOPERATIVE. REP LACED BATTERIES AT GALLEY DOOR POWER SUPPLY AND REPAIRED SHORTED WIRE AT ROW 20D, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996032200501 19960322 00501 WP 1996 3 22 9606269912 1 19960319 A 3260 DNLOCK SWITCH DOUG DC9 DC931 3022065 WP LT MLG MALFUNCTIONED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 962N 47406 DURING APPROACH, THE LEFT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. RECYCLED GEAR TWICE BE FORE NORMAL INDICATIONS WERE ACHIEVED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A BAD SOCKET ON THE LEFT MA IN GEAR DOWNLOCK SWITCH. REPLACED SWITCH, OPERATIONAL CHECK NORMAL ON GEAR SWING. 2 L 7 2 4F A6WE 1996032200502 19960322 00502 WP 1996 3 22 9606279951 1 19960318 A 3350 6011779 BATTERY PACK DOUG DC9 DC932 3022066 WP RT NACELLE DISCHARGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9347 45827 DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT ENGINE NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPER ATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996032200503 19960322 00503 WP 1996 3 22 9606289979 1 19960318 A 3350 FUSE DOUG DC9 DC931 3022065 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9343 47439 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. REPLACED FORWARD ENTRY DOOR FUSE, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996032200504 19960322 00504 1996 3 22 9606292705 4 19960317 A 3454 RMI BOEING 727 727225 1384077 NM NR 2 MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 01 802EA 22433 DURING CRUISE FLIGHT, THE INSTRUMENT COMPARATOR LIGHT CAME ON IN FLIGHT WITH A 10 DEGREE SPLIT BETWEEN RMI'S. WHEN SWIT CHING TO CAPTAIN'S OR FIRST OFFICER'S RMI HAD A 90 DEGREE SPLIT. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE INSTRUMENT SWITCHING UNIT, CONNECTOR D4883, SLAVING AMPLIFIER AND NR 2 RMI AND NR 1 DIRECTIONAL GYRO. OPE RATIONALLY CHECKED NR 1 AND NR 2 COMPASS SYSTEMS, CHECKED OK. 2 L 7 3 4F A3WE 1996032200505 19960322 00505 NM 1996 3 22 9606302203 1 19960314 A 3150 T/O WARNING SYST BOEING 727 727251 138408H NM COCKPIT ACTIVATED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 GL 01 203US 22543 ABORTED TAKEOFF DUE TO FLIGHT CONTROL TAKEOFF WARNING HORN SOUNDED. RESET FLIGHT CONTROL. SECOND TAKEOFF ROLL WAS NORM AL, PERFORMED TAKEOFF WARNING SYSTEM CHECK AND CHECKED OK. 2 L 7 3 4F A3WE 1996032200506 19960322 00506 WP 1996 3 22 9606319139 1 19960314 A 5720 FENCE DOUG DC9 DC914 3022034 WP WING SEPARATION A NWAA K NONE D INFLIGHT SEPARATION UK UNKNOWN 1 GL 01 9481 47049 DURING LINE CHECK, FOUND THAT THE RIGHT WING LEADING EDGE FENCE WAS MISSING AFTER FLIGHT 1704, CVG-DTW. REPAIRED THE WI NG LEADING EDGE PER SRM 57-06, FIG 2 AND REPLACED THE FENCE. 2 L 7 2 4F A6WE 1996032200507 19960322 00507 NM 1996 3 22 96FDEA00563 1 19960315 A 5320 65185385 CHORD BOEING 727 72725 1384006 NM BS 870 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 NR0329 AND 005, CORROSION (C53-132-02, 1) BS 870 UPPER CHORD FASTENER HEAD SHEARED AND SKIN BULGING AT RBL 52 RBL 25 TO 41 AND AT LBL 5 ON VERTICAL FLANGE. 2 L 7 3 4F A3WE 1996032200508 19960322 00508 NM 1996 3 22 96FDEA00564 1 19960315 A 5754 65162256A BULLNOSE BOEING 727 72725 1384006 NM NR 4 LE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 NR0323 AND 004, CORROSION ON NR 4 K-FLAP O/B BONDING JUMPER LOWER ATTACH POINT. 2 L 7 3 4F A3WE 1996032200509 19960322 00509 NM 1996 3 22 96FDEA00565 1 19960315 A 5753 65216352 SKIN BOEING 727 72725 1384006 NM RT TE AFT FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 NR0248 AND 003, RT WING O/B TRAILING EDGE AFT FLAP IS DELAMINATED APPROX 96 INCHES FROM I/B EDGE. 2 L 7 3 4F A3WE 1996032200510 19960322 00510 NM 1996 3 22 96FDEA00566 1 19960315 A 5751 HINGE FITTING BOEING 727 72725 1384006 NM LT AILERON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 NR0196 AND 002, LEFT O/B AILERON NR 1 HINGE FITTING IS CORRODED ON LOWER SURFACE. 2 L 7 3 4F A3WE 1996032200511 19960322 00511 NM 1996 3 22 96FDEA00567 1 19960315 A 5330 SKIN BOEING 727 72725 1384006 NM BS 316 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 NR0097 AND 001, LIGHTNING STRIKE ON FASTENER HEAD BS 316 LBL 55 WL 178. 2 L 7 3 4F A3WE 1996032200512 19960322 00512 NM 1996 3 22 96FDEA00568 1 19960318 A 5315 FLOOR BEAM BOEING 727 72725 1384006 NM BS 1030 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 NR0542 AND 016, CORROSION (C53-224-01) ON LOWER SURFACE OF UPPER FLANGE OF FLOORBEAM AROUND NUTPLATE AND FASTENER HOLES, BS 1030 RBL 48 TO 60 WL 208. 2 L 7 3 4F A3WE 1996032200513 19960322 00513 NM 1996 3 22 96FDEA00569 1 19960318 A 5315 60208 FLOOR BEAM BOEING 727 72725 1384006 NM BS 480 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 CORROSION (C53-224-01) ON FLOOR BEAM BS 480 LBL 39 WL 208. PERFORMED FLOOR BEAM REPAIR AT BS 480 LBL 39 WL 208 IAW 53- 10-8 FEDEX 727 SRM AND ENGINEERING REQUEST. 2 L 7 3 4F A3WE 1996032200514 19960322 00514 NM 1996 3 22 96FDEA00570 1 19960318 A 5753 TE WEDGE BOEING 727 72725 1384006 NM RT TE MIDFLAP DELAMINATION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 NR0480 AND 014, RT WING O/B MIDFLAP TRAILING EDGE WEDGE HAS A DISBOND 88 FROM I/B END ON UPPER SKIN. 2 L 7 3 4F A3WE 1996032200515 19960322 00515 NM 1996 3 22 96FDEA00571 1 19960318 A 5315 651627910 FLOOR BEAM BOEING 727 72725 1384006 NM BS 760-848 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 NR 0474 AND 013, CORROSION (C53-224-01) AND OR BARE METAL AROUND ALL NUT CLIP HOLES LOWER SURFACE BS 760 TO 848 RBL 25 W L 208 ON LONGITUDINAL FLOOR BEAM. CORROSION DAMAGE ON LONGITUDINAL FLOOR BEAM WAS FOUND OUT OF LIMITS. REMOVED DAMAGED BEAM AND INSTALLED NEW BEAM AT BS 760 TO 848 RBL 25 WL 208 REF FEDEX SRM 53-10-1. 2 L 7 3 4F A3WE 1996032200516 19960322 00516 NM 1996 3 22 96FDEA00572 1 19960318 A 5311 FRAME BOEING 727 72725 1384006 NM BS 700 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 NR0452 AND 012, CORROSION ON FRAME BS 700 WL 149 RBL 4. 2 L 7 3 4F A3WE 1996032200517 19960322 00517 NM 1996 3 22 96FDEA00573 1 19960318 A 5311 FRAME BOEING 727 72725 1384006 NM BS 700 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 NR0451 AND 011, CORROSION ON FRAME BS 700 WL 155 RBL TO LBL 11. 2 L 7 3 4F A3WE 1996032200518 19960322 00518 NM 1996 3 22 96FDEA00574 1 19960318 A 5320 SHEAR TIE BOEING 727 72725 1384006 NM BS 990 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 NR0235 AND 010, CORROSION (C53-113-01, 2) ON SHEAR TIE BS 990 WL 158 STR 29R. REMOVED DAMAGED SHEAR TIE BS 990 WL 158 S TR 29R AND INSTALLED REPAIR PER FEDEX SRM 53-10-4. 2 L 7 3 4F A3WE 1996032200519 19960322 00519 NM 1996 3 22 96FDEA00575 1 19960317 A 5320 FORGING BOEING 727 72725 1384006 NM BS 950 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 (NR 0230 AND NR 009). CORROSION (C53-111-01 (3)) ON THE BS 950 FORGING WL 208, RBL 50. **** S/D **** REMOVED CORR OSION ON THE BS 950 FORGING, WL 280, RBL 50. BLENDED DAMAGED AREA, CLEANED, TREATED AND RE-INSTALLED FASTENERS PER FEDE X EA 7-5310-28062. 2 L 7 3 4F A3WE 1996032200520 19960322 00520 NM 1996 3 22 96FDEA00576 1 19960318 A 5311 FRAME BOEING 727 72725 1384006 NM BS 1130 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 NR0168 AND 008, DAMAGED FRAME BS 1130 RBL 50 WL 188 UNDER FLANGE. 2 L 7 3 4F A3WE 1996032200521 19960322 00521 NM 1996 3 22 96FDEA00577 1 19960318 A 5330 SKIN BOEING 727 72725 1384006 NM BS 1108 CREASED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 NR0098 AND 007, CREASE IN SKIN BS 1108 WL 208 LBL 60. REMOVED DAMAGE IN SKIN BS 1108 WL 208 LBL 60 FABRICATED AND INST ALLED REPAIR DOUBLER PER FEDEX SRM 53-30-3. 2 L 7 3 4F A3WE 1996032200522 19960322 00522 NM 1996 3 22 96FDEA00578 1 19960318 A 5312 6516300 BULKHEAD WEB BOEING 727 72725 1384006 NM BS 178 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 NR0079 AND 006, CORROSION (C53-100-0164) ON FWD SIDE OF 178 BULKHEAD RBL 21 TO 26 WL 218. *S/D* CORROSION WAS REMOVED WITHIN LIMITS ON BULKHEAD PER SRM 53-10-1, WEB WAS REPLACED. 2 L 7 3 4F A3WE 1996032200523 19960322 00523 NM 1996 3 22 96FDEA00579 1 19960315 A 5320 65453132 STRINGER CLIP BOEING 727 727233 138408A NM BS 700 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 NR0663 AND 076, CORROSION BS 700 STR CLIP NR 5L HAS CORROSION. *S/D* REMOVED STRINGER CLIP AT BS 700, STR CLIP 5L, REP LACED WITH NEW CLIP PER SRM 51-30-2. 2 L 7 3 4F RT A3WE 1996032200524 19960322 00524 NM 1996 3 22 96FDEA00580 1 19960315 A 5347 BAC1520793 SEAT TRACK BOEING 727 727233 138408A NM BS 1130-1173 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 (NR 0388 AND NR 075). CORROSION ON THE RIGHT SIDE OF SEAT TRACK AT BS 1160, RBL 45, WL 208. ****S/D**** REMOVED AND R EPLACED SEAT TRACK FROM BS 1130 - 1173, RBL 45, WL 208 IAW FEDEX SRM 53-10-5. 2 L 7 3 4F RT A3WE 1996032200525 19960322 00525 NM 1996 3 22 96FDEA00581 1 19960315 A 5320 FILLER BOEING 727 72722 1384002 NM BS 1057-1097 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 NR 0543 AND 026, WHILE WORKING NR 0221, DISCOVERED CORROSION ON SKIN FROM BS 1059 TO 1097 BETWEEN STR 25 AND 26R RBL 32 TO 39 WL 149. REMOVED CORROSION, FABRICATED FILLER AND INSTALLED, SRM 53-30-1. 2 L 7 3 4F A3WE 1996032200526 19960322 00526 NM 1996 3 22 96FDEA00582 1 19960315 A 5320 DOUBLER BOEING 727 72722 1384002 NM BS 875 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 NR 0527 AND 025, CORROSION (C53-132-02, 1) ON ACCESS HOLE DOUBLER BS 875 WL 184 RBL 63. FABRICATED AND REPLACED DOUBLER ON ACCESS DOOR, SRM 53-10-1. 2 L 7 3 4F A3WE 1996032200527 19960322 00527 NM 1996 3 22 96FDEA00583 1 19960315 A 5320 WEB BOEING 727 72722 1384002 NM BS 212-221 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 NR0496 AND 023, CORROSION (C53-224-03-1/2) NOSE E-BAY WEB IS CORRODED STA 212 TO 221 RBL 26 WL 178. 2 L 7 3 4F A3WE 1996032200528 19960322 00528 NM 1996 3 22 96FDEA00584 1 19960315 A 5320 65184151 CHORD BOEING 727 72722 1384002 NM BS 318/336/344 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 NR0399 AND 021, CORROSION (C53-113-03) ON LT MID NOSE CHORD VERTICAL FLANGE EMANATING FROM BENEATH VERTICAL STIFFENER AT BS 318, 336 AND 344. TWO BULGES IN FLOOR WEB ON CHORD HORIZONTAL FLANGE AT BS 318 AND 336 LBL 15 WL 169, ACCESS REQUIR ED. 2 L 7 3 4F A3WE 1996032200529 19960322 00529 NM 1996 3 22 96FDEA00585 1 19960315 A 5320 FLOOR SUPPORT BOEING 727 72722 1384002 NM BS 515 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 NR 0209 AND 020) CORROSION ON FLOOR SUPPORT AT BS 515 RBL 9 WL 156. REPAIRED FLOOR SUPPORT SRM 53-10-5. 2 L 7 3 4F A3WE 1996032200530 19960322 00530 NM 1996 3 22 96FDEA00586 1 19960315 A 5330 SKIN BOEING 727 72722 1384002 NM BS 1183/1188 LIGHTNING STRIKE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 NR0491 AND 022, TWO LIGHTNING STRIKES AT BS 1188 STR 27R AND BS 1183 STR 27R. REPAIRED DAMAGE PER SRM 53-30-3. 2 L 7 3 4F A3WE 1996032200531 19960322 00531 NM 1996 3 22 96FDEA00587 1 19960315 A 5330 SKIN BOEING 727 72722 1384002 NM BS 219 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 NR 0072 AND 019, BS 219-3 LBL 15 WL 163 THERE IS A DEEP GOUGE IN SKIN. REPAIRED GOUGE IN SKIN SRM 53-30-3 AND 53-30-1. 2 L 7 3 4F A3WE 1996032200532 19960322 00532 NM 1996 3 22 96FDEA00588 1 19960315 A 5330 SKIN BOEING 727 72722 1384002 NM BS 660 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 REMOVED GOUGE IN SKIN AT BS 660 TO 3 STR 20R WL 181, FABRICATED REPAIR DOUBLER IAW 53-30-3. 2 L 7 3 4F A3WE 1996032200533 19960322 00533 NM 1996 3 22 96FDEA00589 1 19960318 A 5320 WEB BOEING 727 72722 1384002 NM BS 294-344 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 NR 0558 AND 047, UPON REMOVAL OF LT I/B DOGHOUSE WEB, FOUND IT TO BE OUT OF LIMITS AT BS 294 TO 344 LBL 15 TO 23 WL 159. REMOVED AND REPLACED LT I/B DOGHOUSE WEB AND REINSTALLED ALL DUCTS AND BRACKETS THAT WERE REMOVED FOR INSTALLATION AT BS 294 TO 351 LBL 15 TO 13 WL 169. ALL WORK IAW FEDEX SRM 53-10-9 AND BAC DRW NR 65-18915. 2 L 7 3 4F A3WE 1996032200534 19960322 00534 NM 1996 3 22 96FDEA00590 1 19960318 A 5230 651862588 ANGLE BOEING 727 72722 1384002 NM BS 1082 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 NR 0540 AND 045, WHILE WORKING NR 0254 FOUND AFT CARGO DOOR NR 2 FROM BOTTOM, I/B L-ANGLE TO BE CRACKED IN RADIUS. REMO VED AND REPLACED L-ANGLE SRM 52-30-1. 2 L 7 3 4F A3WE 1996032200535 19960322 00535 NM 1996 3 22 96FDEA00606 1 19960318 A 5260 6526211177 RISER BOEING 727 727233 138408A NM AFT AIRSTAIR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 FOUND CORROSION ON NR 2 AIRSTAIR RISER WHILE REMOVING TREAD. REMOVED AND REPLACED NR 2 AIRSTAIR RISER, ALODINED, PRIMED AND PAINTED. 2 L 7 3 4F RT A3WE 1996032200536 19960322 00536 NM 1996 3 22 96FDEA00607 1 19960313 A 5400 651957243 RIB BOEING 727 727233 138408A NM NR 3 ENG CHAFING A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 NR 3 ENG LOWER COWL HAS TWO AREAS OF CHAFING ON NR 5 RIB. REMOVED AND REPLACED NR 3 ENGINE LOWER COWL NR 5 RIB. 2 L 7 3 4F RT A3WE 1996032200537 19960322 00537 NM 1996 3 22 96FDEA00608 1 19960315 A 5240 65184424 DEPRESSOR SEAL BOEING 727 727233 138408A NM SERVICE DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 FOUND CRACK IN DEPRESSOR SEAL RT AFT SERVICE DOOR UPPER FWD CORNER REVEAL. REPLACED DEPRESSOR SEAL. 2 L 7 3 4F RT A3WE 1996032200538 19960322 00538 NM 1996 3 22 96FDEA00609 1 19960315 A 5230 SKIN BOEING 727 727233 138408A NM NR 3 CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 NR 3 CARGO DOOR INNER SKIN HAS A RIVNUT HOLE WITH THREE CRACKS EMANATING FROM IT 12 INCHES AFT OF THE FWD EDGE, 1.5 INCH FROM THE BOTTOM. FABRICATED AND INSTALLED EXTERNAL DOUBLER AFTER DAMAGED AREA WAS REMOVED. 2 L 7 3 4F RT A3WE 1996032200539 19960322 00539 NM 1996 3 22 96FDEA00610 1 19960315 A 5210 69223239 SUPPORT ASSY BOEING 727 727233 138408A NM FWD ENTRY DOOR DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 TRAMCO RESPONSIBILITY 9603-12, UPON REMOVAL OF FWD ENTRY DOOR UPPER HINGE CASTING IN DOOR, LOWER SUPPORT, UPPER HINGE SU PPORT ASSY WAS DAMAGED. REMOVED AND REPLACED DAMAGED UPPER HINGE SUPPORT ASSY. 2 L 7 3 4F RT A3WE 1996032200540 19960322 00540 NM 1996 3 22 96FDEA00611 1 19960315 A 5210 50794543 WEB BOEING 727 727233 138408A NM FWD ENTRY DOOR GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 FWD ENTRY DOOR UPPER HINGE CASTING IN DOOR, LOWER SUPPORT WEB IS GOUGED REQUIRING REPLACEMENT. REMOVED AND REPLACED LOW ER SUPPORT WEB ON UPPER HINGE CASTING, FWD ENTRY DOOR. 2 L 7 3 4F RT A3WE 1996032200541 19960322 00541 NM 1996 3 22 96FDEA00612 1 19960318 A 5330 SKIN BOEING 727 727233 138408A NM BS 710 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CORROSION ON SKIN AROUND BLIND FASTENERS UNDER FAIRING STRUCTURE AT BS 720A PLUS 10, 1 INCH BELOW STR 29L. REPAIRED SKI N AROUND BLIND FASTENERS UNDER FAIRING STRUCTURE AT BS 710, 1 INCH BELOW STR 28L PER FEDEX SRM 53-30-1, 53-10-1, 53-10-3 AND 51-20-1. 2 L 7 3 4F RT A3WE 1996032200542 19960322 00542 NM 1996 3 22 96FDEA00613 1 19960318 A 5260 6526211176 RISER ASSY BOEING 727 727233 138408A NM AFT AIRSTAIR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 WHILE WORKING ON TREAD REMOVAL FOUND CORROSION ON NR 1 RISER BEYOND LIMITS. REMOVED AND REPLACED NR 1 AIRSTAIR RISER, A LODINED, PRIMED AND PAINTED. 2 L 7 3 4F RT A3WE 1996032200543 19960322 00543 NM 1996 3 22 96FDEA00614 1 19960318 A 5330 SKIN BOEING 727 727233 138408A NM BS 400 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 TWO DENTS IN FUSELAGE SKIN BS 400 STR 17L. REPAIRED DENTS PER FEDEX SRM 53-30-03 FIG 1. 2 L 7 3 4F RT A3WE 1996032200544 19960322 00544 NM 1996 3 22 96FDEA00615 1 19960318 A 5315 FLOOR BEAM BOEING 727 727233 138408A NM BS 1030 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CORROSION ON FLOOR BEAM UPPER CHORD BS 1030 LBL 9 RBL 10 AND RBL 21 WL 208. REMOVED DAMAGE FABRICATED AND INSTALLED REP AIR PARTS ON FLOOR BEAM UPPER CHORD BS 1030 RBL 10 WL 208 PER FEDEX SRM 53-10-8 FIG 8. REMOVED .011 OF ORIGINAL .125 AT LBL 9 AND .006 AT RBL 21 OF ORIGINAL .125. BOTH WITHIN LIMITS PER FEDEX SRM 53-10-1. ALODINED AND PRIMED AREAS. 2 L 7 3 4F RT A3WE 1996032200545 19960322 00545 NM 1996 3 22 96FDEA00616 1 19960318 A 5311 FRAME BOEING 727 727233 138408A NM BS 660 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 DENT ON TOP FLANGE OF FRAME BS 660 LBL 42 WL 165. REPAIRED DENTED FRAME AT BS 660 LBL 42 WL 165 IAW FEDEX SRM 51-40-3. 2 L 7 3 4F RT A3WE 1996032200546 19960322 00546 NM 1996 3 22 96FDEA00617 1 19960319 A 5347 TMS6010452 SEAT TRACK BOEING 727 727233 138408A NM BS 1130-1175 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 SEAT TRACK CORRODED (C53-224-01, 3, 4) OUT OF LIMITS ALONG FLANGE AT BS 1158 RBL 25 WL 208. REMOVED SECTION OF SEAT TRA CK FROM BS 1130 TO 1175 RBL 25 WL 208 AND INSTALLED NEW SEAT TRACK. 2 L 7 3 4F RT A3WE 1996032200547 19960322 00547 NM 1996 3 22 96FDEA00618 1 19960320 A 5347 BAC1520841 SEAT TRACK BOEING 727 727233 138408A NM BS 760-845 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CORROSION AROUND FASTENER HOLES IN SEAT TRACK WELL FROM BS 760 TO 845 LBL 45 WL 208. SEAT TRACK CORRODED BEYOND LIMITS PER SRM 53-10-1. REMOVED AND REPLACED SEAT TRACK BS 760 TO 848 LBL 45 WL 208. 2 L 7 3 4F RT A3WE 1996032200548 19960322 00548 NM 1996 3 22 96FDEA00620 1 19960320 A 5311 FRAME BOEING 727 727233 138408A NM BS 660 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 DENT ON TOP FLANGE OF FRAME AT BS 660 RBL 33 WL 160. REPAIRED DENT ON TOP FLANGE PER FEDEX SRM 53-40-03. 2 L 7 3 4F RT A3WE 1996032200549 19960322 00549 NM 1996 3 22 96FDEA00621 1 19960320 A 5311 FRAME BOEING 727 727233 138408A NM BS 680 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 DENT ON TOP FLANGE OF FRAME AT BS 680 RBL 39 WL 163. REPAIRED DENT ON FRAME AT BS 680 RBL 39 WL 163 IAW FEDEX SRM 51-40 -3. 2 L 7 3 4F RT A3WE 1996032200550 19960322 00550 NM 1996 3 22 96FDEA00622 1 19960320 A 5347 652363736 SEAT TRACK BOEING 727 727233 138408A NM BS 480-680 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CORROSION (C53-224-01) ALONG SEAT TRACK FLANGE AND AROUND FASTENERS IS OUT OF LIMITS BS 480 TO 680 LBL 45 WL 208. REMOV ED AND REPLACED SEAT TRACK AT BS 480 TO 680 LBL 45 WL 208 PER FEDEX SRM 53-10-5. 2 L 7 3 4F RT A3WE 1996032200551 19960322 00551 NM 1996 3 22 96FDEA00623 1 19960320 A 5320 ANGLE BOEING 727 727233 138408A NM BS 720 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CRACKED L-ANGLE ON FLOOR SUPPORT AT BS 720B PLUS 10 RBL 14 WL 155. REMOVED CRACKED L-ANGLE ON FLOOR SUPPORT AT BS 720B PLUS 10 RBL 14 WL 155, FABRICATED REPAIR PART, DRILLED, ALODINED, PRIMED AND INSTALLED IAW FEDEX SRM 51-20-1. 2 L 7 3 4F RT A3WE 1996032200552 19960322 00552 NM 1996 3 22 96FDEA00624 1 19960320 A 5320 WEB BOEING 727 727233 138408A NM BS 950 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CRACK IN WEB AT BS 950A PLUS 17 BL 0 WL 203.5. REMOVED DAMAGED AREA, FABRICATED REPAIR WEB AND INSTALLED PER FEDEX SRM 51-10-2. 2 L 7 3 4F RT A3WE 1996032200553 19960322 00553 NM 1996 3 22 96FDEA00625 1 19960320 A 5320 65453132 CLIP BOEING 727 727233 138408A NM BS 700 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CORROSION BS 700 STR CLIP NR 5L HAS CORROSION ON IT. REMOVED STR CLIP AT BS 700 STR CLIP NR 5L. REPLACED WITH NEW STR CLIP PER FEDEX SRM 51-30-2. 2 L 7 3 4F RT A3WE 1996032200554 19960322 00554 NM 1996 3 22 96FDEA00626 1 19960320 A 5347 BAC1520793 SEAT TRACK BOEING 727 727233 138408A NM BS 1130-1173 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CORROSION ON THE RIGHT SIDE OF SEAT TRACK AT BS 1160 RBL 45 WL 208. REMOVED SECTION OF SEAT TRACK FROM BS 1130 TO 1173 RBL 45 AND REPLACED WITH NEW SEAT TRACK. 2 L 7 3 4F RT A3WE 1996032200555 19960322 00555 NM 1996 3 22 96FDEA00627 1 19960320 A 5320 65255775 ANGLE BOEING 727 727233 138408A NM BS 920 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CORROSION ON FAIRING FORMER BS 920E WL 138.5 LBL TO RBL 10. REMOVED AND REPLACED T-ANGLE AT BS 920E WL 138.5 LBL TO RBL 10 PER FEDEX SRM 51-30-2. 2 L 7 3 4F RT A3WE 1996032200556 19960322 00556 NM 1996 3 22 96FDEA00629 1 19960320 A 5320 6A5453132 CLIP BOEING 727 727233 138408A NM BS 720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CORROSION BS 720E STR CLIPS 3 AND 4 RT HAVE CORROSION. REMOVED AND REPLACED STR CLIP AT BS 720E 3 RT PER FEDEX 51-10-1. STR CLIP 4 AT BS 720E RT FOUND TO BE WITHIN LIMITS PER FEDEX SRM 53-10-1. 2 L 7 3 4F RT A3WE 1996032200557 19960322 00557 NM 1996 3 22 96FDEA00630 1 19960320 A 5347 658624533 SEAT TRACK BOEING 727 727233 138408A NM BS 950-1070 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 SEAT TRACK CORRODED OUT OF LIMITS AND CRACKED ALONG FLANGE BS 950D TO 1070 LBL 45 WL 208. REMOVED AND REPLACED SEAT TRA CK AT BS 950D TO 1070. DRILLED HOLES, ALODINED, PRIMED AND INSTALLED. 2 L 7 3 4F RT A3WE 1996032200558 19960322 00558 NM 1996 3 22 96FDEA00631 1 19960320 A 5315 BAC14902888 FLOOR BEAM BOEING 727 727233 138408A NM BS 1070 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CORROSION (C53-224-01, 3, 4) AND BARE METAL ON UPPER CHORD OF FLOOR BEAM BS 1070 RBL 25 TO 55 WL 208. REMOVED DAMAGE OF UPPER CHORD OF FLOOR BEAM BS 1070 RBL 10 TO SKIN RT, REPAIRED PER FEDEX SRM 53-10-8 FIG 3. 2 L 7 3 4F RT A3WE 1996032200559 19960322 00559 NM 1996 3 22 96FDEA00632 1 19960320 A 5350 FAIRING FORMER BOEING 727 727233 138408A NM BS 740 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CORROSION (C53-122-01) ON FAIRING FORMER AROUND NUTPLATES AT BS 740 WL 138.5 RBL TO LBL 11 TO 32 PER FEDEX SRM 51-40-3. 2 L 7 3 4F RT A3WE 1996032200560 19960322 00560 NM 1996 3 22 96FDEA00633 1 19960320 A 5347 BAC1520793 SEAT TRACK BOEING 727 727233 138408A NM BS 760-848 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CORROSION AROUND FASTENER HOLES IN SEAT TRACK WELL FROM BS 760 TO 848 LBL 25 WL 208. SEAT TRACK CORRODED OUT OF LIMITS PER FEDEX SRM 53-10-1. REMOVED AND REPLACED SEAT TRACK BS 760 TO 848 LBL 25 WL 208. 2 L 7 3 4F RT A3WE 1996032200561 19960322 00561 NM 1996 3 22 96FDEA00634 1 19960320 A 5311 FRAME BOEING 727 727233 138408A NM BS 460 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CORROSION (C53-224-01) BS 460 BETWEEN STR 4 AND 5R FRAME HAS CORROSION. REMOVED CORROSION AND REPAIRED FRAME BS 460 BET WEEN STR 4 AND 5R PER FEDEX EA 7-5310-27747. 2 L 7 3 4F RT A3WE 1996032200562 19960322 00562 NM 1996 3 22 96FDEA00635 1 19960320 A 5313 65271322 STRINGER BOEING 727 72725 1384006 NM BS 482 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 MECH DAMAGE ON STR 23L AT STA 482. REMOVED DAMAGED STR BS 482 STR 23L AND INSTALLED REPAIR PER FEDEX SRM 53-10-3. 2 L 7 3 4F A3WE 1996032200563 19960322 00563 NM 1996 3 22 96FDEA00636 1 19960320 A 5320 65453132 CLIP BOEING 727 72725 1384006 NM BS 420 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 CRACKED STR CLIP BS 420 STR 4L. REMOVED CRACKED STR CLIP, DRILLED NEW STR CLIP AND INSTALLED AT BS 420 STR 4L. 2 L 7 3 4F A3WE 1996032200564 19960322 00564 NM 1996 3 22 QXEA9600112 1 19960319 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 841PH 82 COCKPIT OVERHEAD EMERGENCY LIGHT IS INOP. COCKPIT OVERHEAD LIGHT REPLACED AND LIGHT OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 1996032200565 19960322 00565 NM 1996 3 22 SWAA960139 1 19960311 A 5320 CLIP BOEING 737 7372H4 138448C NM BS 787/747/947 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 787 S24R AND S20R, BS 727A S25L, BS 747 S20L AND S22L AND A T BS 947, S25R. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996032200566 19960322 00566 NM 1996 3 22 SWAA960140 1 19960311 A 5320 CHORD BOEING 737 7372H4 138448C NM BS 726 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED D-CHECK, FOUND CHORD CRACKED AT BS 726, RBL 9 WL 202. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996032200567 19960322 00567 NM 1996 3 22 SWAA960141 1 19960311 A 5315 FLOOR BEAM BOEING 737 7372H4 138448C NM BS 999/1002/1005 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORROSION AT BS 999 LBL 13 WL 208, BS 1002 LBL 12 WL 208 AND BS 1005 LBL 10 W L 208. REPLACED CORRODED SECTION PER BOEING SRM. 2 L 7 2 4F A16WE 1996032200568 19960322 00568 NM 1996 3 22 SWAA960142 1 19960311 A 5315 FLOOR BEAM BOEING 737 7372H4 138448C NM BS 987/947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORROSION AT BS 987 LBL 3 TO 19 WL 208 AND BS 947 RBL 10 WL 208 AND LBL 4, 12 , 22, WL 208. REPLACED CORRODED SECTION PER BOEING SRM. 2 L 7 2 4F A16WE 1996032200569 19960322 00569 NM 1996 3 22 SWAA960143 1 19960311 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 344 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 344 LBL 45 WL 170. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996032200570 19960322 00570 NM 1996 3 22 SWAA960144 1 19960311 A 5320 SPLICE BOEING 737 7372H4 138448C NM BS 907 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CORRODED AT BS 907, S20R. REPLACED WITH NEW PER BOEING SRM. 2 L 7 2 4F A16WE 1996032200571 19960322 00571 NM 1996 3 22 SWAA960145 1 19960311 A 5320 SPLICE BOEING 737 7372H4 138448C NM BS 909 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED D-CHECK, FOUND STRINGER AND STRINGER SPLICE CORRODED AT BS 909 LBL171 WL 171. REPLACED WITH NEW PER BO EING SRM. 2 L 7 2 4F A16WE 1996032200572 19960322 00572 NM 1996 3 22 SWAA960146 1 19960311 A 5320 SHEAR TIE BOEING 737 7372H4 138448C NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN S14 AND 15L. REPLACED WITH NEW PER BOEING SRM. 2 L 7 2 4F A16WE 1996032200573 19960322 00573 NM 1996 3 22 SWAA960147 1 19960311 A 3350 20121 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 607SW 27927 DURING SCHEDULED A1-CHECK, FOUND RT EMERGENCY EXIT LIGHTS INOP. REPLACED LIGHT HOUSING PER BOEING MM. 2 L 7 2 4F RT A16WE 1996032200574 19960322 00574 NM 1996 3 22 SWAA960148 1 19960311 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 947.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED SV-CHECK, FOUND FUSE SKIN CRACKED AT BS 947.5, ABOVE S25L AND FWD 4 INCHES. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996032200575 19960322 00575 NM 1996 3 22 SWAA960149 1 19960311 A 5315 FLOOR BEAM BOEING 737 7372H4 138448C NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CRACKS AT BS 500B LT IN RADIUS OF UPPER FLANGE. REPAIRED PER SWA ACO 595-53. 2 L 7 2 4F A16WE 1996032200576 19960322 00576 NM 1996 3 22 SWAA960150 1 19960228 A 7931 ST104Z OIL PRESS TRANSM BOEING 737 7372T4 1384492 NM NR 2 ENGINE INOP A SWAA E ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 SW 07 722WN 22698 BETWEEN 75 AND 100 MILES FROM OMA, NUMBER 2 ENGINE OIL PRESSURE DROPPED TO 20 PSI, ALL OTHER INDICATIONS READ NORMAL. P ERFORMED ENGINE SHUTDOWN CHECKLIST, AIRCRAFT MADE AN UNEVENTFUL LANDING AT OMA. REMOVED AND REPLACED OIL PRESSURE TRANS MITTER PER BOEING MM. 2 L 7 2 4F A16WE 1996032200577 19960322 00577 NM 1996 3 22 SWAA960151 1 19960311 A 3230 RETRACT MECH BOEING 737 7372H4 138448C NM LANDING GEAR MALFUNCTIONED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 26SW 21117 AFTER TAKEOFF, CREW WAS UNABLE TO RAISE GEAR WITHOUT USING OVERRIDE TRIGGER. AIRCRAFT RETURNED TO DAL AND MADE AN UNEVE NTFUL LANDING. CYCLED GEAR SEVERAL TIMES, NO DEFECTS NOTED. RESET LANDING GEAR POSITION LIGHTS C/B. 2 L 7 2 4F A16WE 1996032200578 19960322 00578 NM 1996 3 22 VSTA9603001 1 19960318 A 5230 9040073009 SEAL BOEING 737 737247 138448D NM AFT BAGGAGE DOOR OUT OF POSITION A VSTA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 07 303VA 20125 COULD NOT CONTROL CABIN ALTITUDE, CABIN CLIMB TO 12,000 FEET. FOUND DOOR SEAL OUT OF CHANNEL, REINSTALLED AND SECURED. GROUND CHECKS NORMAL. 2 L 7 2 4F A16WE 1996032200579 19960322 00579 EU 1996 3 22 WWMA9600027 1 19960316 A 2150 5419C000 ACM BAG JETSTM JETSTM3201 1500217 EU LEFT/RIGHT OVERSERVICED A WWMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 15 959AE 959 THE CREW REPORTED, A STRONG OIL/HYDRAULIC SMELL COMING FROM THE BLEED AIR. MAINTENANCE DRAINED EXCESS OIL FROM BOTH THE LEFT AND RIGHT COOLING TURBINES, PERFORMED GROUND RUNS AND RELEASED THE AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A56EU 1996032200580 19960322 00580 EU 1996 3 22 WWMA9600028 1 19960314 A 3260 D49412001 IND SOCKET SAAB SF340 340B 7860101 EU RT MLG BROKEN A WWMA O OTHER P NO WARNING INDICATION LD LANDING 1 WP 15 306AE 340B306 CREW REPORTED, THE RIGHT MAIN LANDING GEAR DID NOT INDICATE DOWN AND LOCKED, AFTER 10 SECONDS THE GEAR WAS RECYCLED AND THEN INDICATED DOWN AND LOCKED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE GEAR HANDLE PANEL RIGHT IN DICATOR SOCKET BROKEN. THE PANEL WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE WITHOUT FURTHER PROBLEMS. 2 L 7 2 4T RT A52EU 1996032200581 19960322 00581 NE 1996 3 22 96ZZZM308 2 19960210 A 7310 48333 FUEL PUMP FILTER 37E501242P10 AMD FALC20 FALCON 2720302 EU GE CF700 CF7002D2 30010 NE LT ENG CRUSHED A YIEA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 GL 23 814AA 698064 31 245U139 YIP - LEFT ENGINE FLAMED OUT DURING STEADY STATE CLIMB AT 36,000 FEET. AIRCRAFT DESCENDED AND THE ENGINE WAS AIRSTARTED PER THE CHECK LIST. AIRCRAFT RETURNED TO YIP AND MADE A NORMAL TWO ENGINE LANDING. LEFT ENGINE WAS INSPECTED FOR FOD IN THE INLET, EXHAUST AND BY BOROSCOPE METHODS WITH NO DEFECTS NOTED. LOW PRESSURE AND ENGINE FUEL FILTERS INSPECTED. F OUND LOW PRESSURE AND FUEL PUMP FILTERS CRUSHED UPON INSPECTION. REPLACED FILTERS WITH SERVICEABLE. AIRCRAFT RELEASED FOR TEST FLIGHT. REFERENCE YIEA96007. 2 L 7 2 4F 4 F A7EU E7EA 1996032200582 19960322 00582 EU 1996 3 22 96ZZZM309 1 19960208 A 3350 321430 BATTERY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 622AW 3767 054 LAS - FLT NR 85 - DURING ROUTINE MAINTENANCE CHECK, FOUND MISCELLANEOUS EMERGENCY LIGHTS IN AFT INOP. REMOVED AND REPLA CED EMERGENCY PACK, PACK CHECKS GOOD. REMOVED AND REPLACED BATTERY ON AFT POWER SUPPLY, CHECKS GOOD. REFERENCE AWXA960 057. 2 L 7 2 4F RT A28NM 1996032200583 19960322 00583 1996 3 22 96ZZZM310 4 19960218 A 3414 CONNECTOR DOUG DC9 DC932 3022066 WP LT COCKPIT LOOSE A VJ6A C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 11 931VV 47674 ON TAKEOFF ROLL AT 100 KTS, ON CROSS CHECK OF AIRSPEED INDICATORS, THE CAPTAINS WAS AT ZERO KTS AND THE FIRST OFFICERS W AS 100 KTS, TAKEOFF WAS ABORTED. RESEATED CANNON PLUG AND PERFORMED INSTRUMENT PITOT STATIC LEAKAGE CHECK, OPS CHECK GO OD IAW MM 31-10. (M) 2 L 7 2 4F A6WE 1996032200584 19960322 00584 WP 1996 3 22 96ZZZM311 1 19960217 A 2150 AYLF97141 SENSOR DOUG DC9 DC932 3022066 WP RT PACK INOP A VJ6A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 11 921VV 47284 ON FLT NR 166, SAV-SAV - AIR RETURN, AIRCRAFT EXPERIENCED A RIGHT A/C TEMP SUPPLY HIGH LIGHT ON. MAINTENANCE REPLACED T HE RIGHT A/C SUPPLY TEMP HIGH SENSOR. OPS CHECKS GOOD IAW 21-55. (M) 2 L 7 2 4F A6WE 1996032200585 19960322 00585 WP 1996 3 22 96ZZZM312 1 19960226 A 3260 GRD SENSE MECH DOUG DC9 DC932 3022066 WP NLG OUT OF ADJUST A VJ6A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 11 919VV 47260 ON FLT NR 550, ATL-ATL, AIR RETURN, AFTER TAKEOFF THE TAKEOFF WARNING HORN SOUNDED DURING FLAP RETRACTION. THE FLAP SLA T WERE RE-EXTENDED TO 5 DEGREES, DID NOT GET AIR MODE. AUTO SPOILER ' DO NOT USE' LIGHT WAS ON FOR LANDING. MAINTENANC E FOUND THE GROUND SHIFT MODE OUT OF RIG. RIGGED NOSE GEAR GROUND SENSE MECHANISM, OPS CHECK GOOD. SECURED TURNBARRELS MM 32-23-1. (M) 2 L 7 2 4F A6WE 1996032200586 19960322 00586 WP 1996 3 22 96ZZZM313 1 19960220 A 7931 41800044 CONNECTOR DOUG DC9 DC932 3022066 WP NR 2 ENG FAILED A VJ6A A UNSCHED LANDING O OTHER CL CLIMB 1 SO 11 931VV 47674 ON FLT NR 535, ATL-ATL, AIR RETURN, DURING THE CLIMB THE CAPTAIN NOTICED NR 2 ENGINE OIL PRESSURE AT 100 PSI. THE AIRCR AFT LANDED UNDER THE MAXIMUM LANDING WEIGHT. MAINTENANCE FOUND A BAD CANNON PLUG. REMOVED AND REPLACED THE CANNON PLUG , OPS CHECKED GOOD IAW MM 79-31. (M) 2 L 7 2 4F A6WE 1996032200587 19960322 00587 WP 1996 3 22 96ZZZM314 1 19960217 A 3260 92743643 RELAY DOUG DC9 DC932 3022066 WP LANDING GEAR FAILED A VJ6A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 11 931VV 47674 ON FLT NR 517 - ATL-ATL - AIR RETURN, ON GEAR RETRACTION ALL LIGHTS WENT OUT, ON UPLATCH CHECK GREEN LIGHT ON, DOOR LIGH TS CLOSED. GEAR CYCLED AND NOSE GEAR INDICATED UNSAFE. RECYCLED AND ALL LIGHTS GREEN. FOUND LEFT GEAR UPLOCK TARGET M ISALIGNED WITH RETENTION SPRING. REALIGNED RETENTION WITH TARGET AND ADJUSTED NOSE GEAR LOCK SENSOR TARGET. REPLACED P ROXIMITY BOX AND LANDING GEAR LEVER RELAYS AS PRECAUTIONARY. OPS CHECK NORMAL. (M) 2 L 7 2 4F A6WE 1996032200588 19960322 00588 NM 1996 3 22 96ZZZM315 1 19960209 A 5330 693535214 CLIP BOEING 737 7372A6 138448B NM STA 420 DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 145AW 20194 DURING SCHEDULED C-12 MAINTENANCE CHECK, FOUND STRINGER CLIP, AT STRINGER 22L BS 420, DAMAGED, FRAME ALSO DAMAGED IN SAM E AREA. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER. FITTED AND DRILLED IN PLACE, REMOVED, DEBURRED, ALODINED, PR IMED TWICE. INSTALLED REPAIR DOUBLER AND NEW STRINGER CLIP PER SRM 57-40-03, 51-10-02. REFERENCE AWXA960060. 2 L 7 2 4F A16WE 1996032200589 19960322 00589 SO 1996 3 22 96ZZZM316 1 19960213 A 5400 11592190119 ANGLE GULSTM G1159 G1159 3953505 SO LT PYLON CRACKED A KKYA K NONE O OTHER IN INSP/MAINT 1 NE 03 220FL 10966 50 DURING AN 18 MONTH INSPECTION OF THE LEFT PYLON, 1 INCH CRACKS WERE FOUND IN THE LEADING EDGE ATTACHMENT ANGLES, P/N 115 921901-19 AND -20. THE ANGLES WERE REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A12EA 1996032200590 19960322 00590 SO 1996 3 22 96ZZZM317 1 19960213 A 5400 11592190120 ANGLE GULSTM G1159 G1159 3953505 SO LT PYLON CRACKED A KKYA K NONE O OTHER IN INSP/MAINT 1 NE 03 220FL 10966 50 DURING AN 18 MONTH INSPECTION OF THE LEFT PYLON, 1 INCH CRACKS WERE FOUND IN THE LEADING EDGE ATTACHMENT ANGLES, P/N 115 921901-19 AND -20. THE ANGLES WERE REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A12EA 1996032200591 19960322 00591 EU 1996 3 22 96ZZZM318 1 19960221 A 2910 9302631001 LINE SAAB SF340 340B 7860101 EU HYDRAULIC SYSTEM FAILED A NVEA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 03 180AE 340B180 FLT NR 5798 - MIA - ON APPROACH, AIRCRAFT LOST HYD POWER WHEN LANDING GEAR WAS SELECTED DOWN. REPLACED RUPTURED HYD LIN E. 2 L 7 2 4T RT A52EU 1996032200593 19960322 00593 EU 1996 3 22 96ZZZM320 1 19960220 A 2910 FLUID BAG JETSTM JETSTM3201 1500217 EU HYD SYSTEM LOW A NVEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 03 927AE 927 FLT NR 4545 - BNA - PILOT REPORTED, AFTER TAKEOFF GEAR WAS SELECTED UP, INTRANSIT LIGHT STAYED ON AND HYD PUMPS CAVITATE D. GEAR WAS THEN SELECTED DOWN, THE NOSE GEAR WENT DOWN AND LOCKED, IT TOOK THE MAINS 3 MINUTES TO INDICATE DOWN AND LO CKED THEN LANDED WITHOUT INCIDENT. MAINTENANCE FOUND HYD QUANTITY VERY LOW. HYD SYSTEM RESERVICED AND OPS CHECKED ALL SYSTEMS GOOD. AIRCRAFT WAS ALSO TEST FLOWN AND IT OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A56EU 1996032200594 19960322 00594 WP 1996 3 22 96ZZZM321 1 19960225 A 2133 CONTROL WHEEL DOUG DC9 DC932 3022066 WP OUTFLOW VLV STUCK OPEN A VJ6A A UNSCHED LANDING O OTHER CL CLIMB 1 SO 11 917VV 47323 ON FLT NR 363 - BOS-RDU, CAPTAIN COULD NOT PRESSURIZE THE CABIN IN MANUAL OR AUTO. MAINTENANCE FOUND THE OUTFLOW VALVE CONTROL WHEEL STUCK IN FULL OPEN POSITION. MAINTENANCE FREED WHEEL AND OPS CHECKED OK. (M) 2 L 7 2 4F A6WE 1996032200595 19960322 00595 CE 1996 3 22 96ZZZM322 1 19960129 A 6120 BETA VALVE BEECH 1900 1900 1154160 CE LT ENGINE OUT OF ADJUST A GUUA E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 17ZR UB17 FLT NR 103 - MIA - ON CLIMB-OUT FROM TNT LEFT PROP SPEED INDICATOR STARTED DROPPING THEN SURGING. SHUT DOWN LEFT ENGINE AND DECLARED AN EMERGENCY INTO MIA. LANDED WITHOUT INCIDENT. ADJUSTED LEFT ENGINE BETA VALVE SETTING AND RERIGGED BOT H ENGINES FOR PROPER BETA VALVE SETTING. (M) 2 L 7 2 4T RT A24CE 1996032200596 19960322 00596 CE 1996 3 22 96ZZZM323 1 19960201 A 3230 RETRACT MECH BEECH 1900 1900C 1154161 CE LANDING GEAR REQ'D SERV A GUUA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 19 734GL UB34 FLT NR 923 - MIA - LANDING GEAR WOULD NOT CYCLE UP. SERVICED HYDRAULIC AND CYCLED 6 TIMES, OPS CHECK OK. (M) 2 L 7 2 4T RT A24CE 1996032200597 19960322 00597 CE 1996 3 22 96ZZZM324 1 19960201 A 3234 1013841375 GEAR HANDLE BEECH 1900 1900C 1154161 CE LANDING GEAR MALFUNCTIONED A GUUA O OTHER J WARNING INDICATION AP APPROACH 1 SO 19 259AF 36 UB55 FLT NR 107- TNT-MIA - LANDING GEAR FAILED TO EXTEND NORMALLY, PERFORMED MANUAL GEAR EXTENSION PER POH. DETERMINED IT TO BE LANDING GEAR HANDLE ASSEMBLY. REMOVED AND REPLACED GEAR HANDLE ASSEMBLY. GEAR SWINGS GOOD AIRCRAFT RELEASED. (M) 2 L 7 2 4T RT A24CE 1996032200598 19960322 00598 WP 1996 3 22 96ZZZM325 1 19960131 A 5730 SKIN DOUG DC8 DC861 3021952 WP WS 204 CRACKED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 30UA 45888 DUIRNG C-CHECK INSPECTION, FOUND LEFT WING LOWER SURFACE SKIN CRACK AT STATION XW204. REPAIRED LEFT WING LOWER SURFACE SKIN CRACK BY CUTTING OUT 2 INCH BY 5.4 INCH SKIN AND INSTALLED A 7075-T6 .188 2 INCH BY 5.4 INCH FILLER AND INSTALLED A 15 INCH BY 15 INCH 7075-T6 .100 REPAIR DOUBLER IAW EO 9601081. 8110-3 ISSUED BY DER SW-713. (M) 2 L 7 4 4F 4A25 1996032200599 19960322 00599 NM 1996 3 22 96ZZZM326 1 19960220 A 3260 H1410154 DNLOCK SENSOR BOEING 737 7372X6C 1384552 NM NLG INOPERATIVE A ASAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 01 746AS 23123 SMF - FLT 415 - AIR TURN BACK DUE TO NOSE LANDING GEAR UNSAFE LIGHT ILLUMINATED AFTER TAKEOFF. RECYCLED GEAR TWO TIMES AND LIGHT REMAINED ON. NOSE LANDING GEAR WOULD EXTEND IN THE OFF POSITION. LANDED WITHOUT INCIDENT. INSPECTED NOSE LA NDING GEAR AND RELEASED AIRCRAFT FOR MAINTENANCE FERRY FLIGHT TO OAK. OAK MAINTENANCE REPLACED THE NLG LOCK ACTUATOR AN D THE NLG DOWN LOCK SENSOR. GEAR OPERATED NORMALLY DURING ENTIRE GEAR CYCLE. REFERENCE ASAA9610021. 2 L 7 2 4F RT A16WE 1996032200634 19960322 00634 NM 1996 3 22 AALA960163 1 19960130 A 3230 RETRACT MECH BOEING 727 727227 1384078 NM LT MLG LACK OF LUBE A AALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SW 07 723AA 20731 ORD - FLT NR 517 - DURING APPROACH TO ORD WHEN LANDING GEAR EXTENDED, LEFT MAIN LANDING GEAR REQUIRED FOUR ATTEMPTS PLUS POSITIVE G-FORCE TO LOCK IN THE DOWN POSITION. AIRCRAFT LANDED ORD WITHOUT INCIDENT. CLEANED AND LUBRICATED LEFT MAIN LANDING GEAR DUE TO PIVOT POINTS FOUND DRY. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996032200635 19960322 00635 EU 1996 3 22 AALA960240 1 19960206 A 5210 A5217208900600 GEARBOX AIRBUS 300 A300B4605R 3930308 EU 1L DOOR DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 7055A 462 JFK - FLT NR 1445 - AFTER TAKEOFF JFK CLIMBING THROUGH FL 240, 1L DOOR RED SLIDE ARMING WARNING BEGAN TO FLASH. PUSHING ON DOOR HANDLE EXTINGUISHED THE WARNING LIGHT. DOOR LOCKED INDICATORS SHOWED MIDWAY BETWEEN LOCKED AND UNLOCKED. AIRC RAFT RETURNED TO JFK AND LANDED WITHOUT INCIDENT. LUBRICATED STUCK LATCH AT 1L DOOR (IPC 52-11-11-08, ITEM 240). SYSTE M GROUND CHECKED NORMAL OPERATION AND AIRCRAFT REDEPARTED. SUBSEQUENTLY, EN ROUTE JFK/SDQ, PROBLEM REPEATED WITH 1L DOO R LOCK INDICATOR SHOWING MIDWAY BETWEEN LOCKED AND UNLOCKED. AIRCRAFT DIVERTED TO MIA AND LANDED WITHOUT INCIDENT. REP AIRED 1L DOOR GEARBOX AND ADJUSTED DOOR LOCKING MECH RODS. SYSTEM GROUND CHECKED NORMAL OPERATIONS. (M) 2 L 7 2 4F RT A35EU 1996032200636 19960322 00636 NM 1996 3 22 AALA960241 1 19960207 A 3260 AAP2448A ACCESSORY UNIT BOEING 727 727227 1384078 NM LANDING GEAR DEFECTIVE A AALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SW 07 720AA 20613 DFW - FLT NR 1025 - DURING APPROACH TO DFW WHEN LANDING GEAR EXTENDED, ALL GREEN LANDING GEAR LIGHTS ILLUMINATED ALONG W ITH THE RIGHT GEAR RED LIGHT. RECYCLED LANDING GEAR WITH SAME RESULTS. VISUALLY CONFIRMED ALL LANDING GEAR DOWN AND LO CKED AND AIRCRAFT LANDED DFW WITHOUT INCIDENT. REPLACED LANDING GEAR ACCESSORY UNIT. ACCOMPLISHED LANDING GEAR RETRACT ION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996032200637 19960322 00637 NM 1996 3 22 AALA960243 1 19960207 A 3397 WIRE BOEING 767 767223 1385123 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 313AA 22316 SFO - DURING OVERNIGHT CHECK, MID-GALLEY EMERGENCY EXIT EGRESS LIGHTS INOPERATIVE. REPAIRED BROKEN WIRES AT MID-GALLEY FOR EMERGENCY EXIT EGRESS LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1996032200638 19960322 00638 WP 1996 3 22 AALA960257 1 19960211 A 3240 35950505 VALVE DOUG DC10 DC1010 3022110 WP MLG BRAKES DEFECTIVE A AALA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 129AA 46996 JFK - FLT NR 359 - AFTER LANDING ROLLOUT, MAIN WHEEL BRAKES APPEARED TO LOCK AFTER TURNING OFF RUNWAY. AIRCRAFT TOWED T O GATE. REPLACED DUAL BRAKE CONTROL VAVLE. ALSO, REPLACED LEFT LOWER ANTI-SKID MODULE. ACCOMPLISHED LEAK CHECK WITH N O DEFECTS FOUND. ACCOMPLISHED MULTIPLE TAXI CHECKS WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A22WE 1996032200639 19960322 00639 NM 1996 3 22 AALA960264 1 19960214 A 3350 PINS BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 373AA 25200 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS BETWEEN PAX SEAT ROWS 8B TO 23B AND 35H TO 41H INOPERATIVE. RESEATE D LOOSE EMERGENCY EXIT LIGHT PINS AT PAX SEAT ROWS 8B TO 23B AND 35H TO 41H. SYSTEM GROUND CHECKED NORMAL OPERATION. ( M) 2 L 7 2 4F RT A1NM 1996032200640 19960322 00640 NE 1996 3 22 AALA960266 2 19960214 A 7230 795073 RETAINING NUT BOEING 727 727223 1384074 NM PWA JT8 JT8D9 52048 NE NR 3 BEARING LOST TORQUE A A AALA E A ENGINE SHUTDOWN UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 SW 07 860AA 4757 21087 666112 AFTER TAKEOFF SLC CLIMBING THROUGH FL 323, NR 3 ENG FAILED WITH NO OIL PRESS OR N2 IND AFTER FAILURE. ACCOMP ENG FAILUR E AND PRECAUTIONARY SHUTDOWN CHECKLIST FOR NR 3 ENG AND A/C RETURNED W/O INCIDENT. REPLACED NR 3 ENG. ACCOMP LK CHKS A ND GROUND ENG RUN WITH NO DEFECTS FOUND. SYS GROUND CHECKED NORM OPS. ENG SHUTDOWN RESULTED FROM FAILURE OF THE NR 3 B EARING STACK. THE HARDWARE WAS ALLOWED TO ROTATE ON STUB SHAFT WHEN THE RETAINING NUT LOST ITS INSTALLATION TQ. EVENTU ALLY, RESULTANT WEAR CAUSED THE STUB SHAFT AND BEARING HARDWARE TO FAIL WHICH SEIZED THE N2 ROTOR. PWA S/B 5905, WHICH INCORP A PINNED NR 3 BEARING STACK ASSY, HAD NOT BEEN PERFORMED ON ENG. REPAIRED AND RETURNED TO SERV. (M) 2 L 7 3 4F 4 F A3WE E2EA 1996032200641 19960322 00641 WP 1996 3 22 AALA960276 1 19960219 A 3350 A3030398101 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 14551 53033 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS FROM PAX SEAT ROW 20 AND AFT INOPERATIVE. REPLACED BROKEN EMERGENC Y FLOOR LIGHT CONNECTOR AT AFT END OF MAIN CABIN SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996032200642 19960322 00642 NM 1996 3 22 AALA960277 1 19960220 A 3350 0201922001 HOUSING BOEING 767 767223 1385123 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 338AA 22335 ORD - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 33H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT HOUSING A T PAX SEAT 33H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1996032200643 19960322 00643 NM 1996 3 22 AALA960278 1 19960220 A 3350 A3030398101 CONNECTOR BOEING 727 727223 1384074 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 895AA 22011 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 16D AND 22D INOPERATIVE. RESECURED LOOSE EME RGENCY FLOOR LIGHT CONNECTOR BY PAX SEAT ROW 16D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996032200644 19960322 00644 NM 1996 3 22 AALA960280 1 19960221 A 3350 A3030398101 CONNECTOR BOEING 727 727223 1384074 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 878AA 21390 DFW - DURING OVERHEAT CHECK, EMERGENCY FLOOR LIGHTS IN FIRST CLASS CABIN INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR L IGHT CONNECTOR AT FORWARD PART OF FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996032200646 19960322 00646 NM 1996 3 22 AALA960301 1 19960222 A 3350 1722331 CONNECTOR BOEING 767 767223 1385123 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 321AA 22322 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT PAX SEATS 31B AND 37H INOPERATIVE. RESECURED LOOSE EMERGENCY EXI T LIGHT CONNECTORS AT PAX SEATS 31B AND 37H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1996032200647 19960322 00647 NM 1996 3 22 AALA960302 1 19960223 A 3350 1722331 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 371AA 25198 MIA - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT PAX SEAT 26H INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT C ONNECTOR AT PAX SEAT 26H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1996032200648 19960322 00648 NM 1996 3 22 AALA960303 1 19960223 A 3350 0201922001 LIGHT ASSY BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 355AA 24036 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT ROW 22A INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT HOUSING ASSEMBLY AT PASSENGER SEAT ROW 22A. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1996032200649 19960322 00649 NM 1996 3 22 AALA960304 1 19960224 A 3350 1721651 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 376AN 25445 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 28B INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LI GHT CONNECTOR AT PASSENGER SEAT 28B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1996032200650 19960322 00650 NM 1996 3 22 AALA960305 1 19960224 A 3350 8100022601 LIGHT BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 369AA 25196 SFO - DURING OVERNIGHT CHECK, FLOOR PROXIMITY AISLE LIGHTING SYSTEM BETWEEN PASSENGER SEATS 7H THROUGH 12H INOPERATIVE. REPLACED FLOOR PROXIMITY AISLE LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1996032200651 19960322 00651 EU 1996 3 22 AALA960306 1 19960224 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1400H 11340 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY INOPERATIVE. REPAIRED BROKEN EMERGENCY FLOOR LIG HT WIRING BY FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1996032200652 19960322 00652 NM 1996 3 22 ASAA9610018 1 19960214 A 3350 8821004 BATTERY PACK BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING MAINTENANCE CEHCK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE ROW 2 (PALLET 1-7). REPLAC ED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1996032200653 19960322 00653 NM 1996 3 22 ASAA9610020 1 19960219 A 3350 86210144 BATTERY PACK BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 ANC - DURING MAINTENANCE CHECK, THE SMOKE BARRIER EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1996032200654 19960322 00654 NM 1996 3 22 ASAA9610021 1 19960220 A 3230 651781914 LOCK ACTUATOR BOEING 737 7372X6C 1384552 NM NLG INOPERATIVE A ASAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 01 746AS 23123 SMF - FLT 415 - AIR TURN BACK DUE TO NOSE LANDING GEAR UNSAFE LIGHT ILLUMINATED AFTER TAKEOFF. RECYCLED GEAR TWO TIMES AND LIGHT REMAINED ON. NOSE LANDING GEAR WOULD EXTEND IN THE OFF POSITION. LANDED WITHOUT INCIDENT. INSPECTED NOSE LA NDING GEAR AND RELEASED AIRCRAFT FOR MAINTENANCE FERRY FLIGHT TO OAK. OAK MAINTENANCE REPLACED THE NLG LOCK ACTUATOR AN D THE NLG DOWN LOCK SENSOR. GEAR OPERATED NORMALLY DURING ENTIRE GEAR CYCLE. (M) 2 L 7 2 4F RT A16WE 1996032200655 19960322 00655 NM 1996 3 22 ASAA9610022 1 19960223 A 3350 1060091101 LIGHT BOEING 737 737210C 1384459 NM L-2 DOOR INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 744AS 21822 SEA - DURING MAINTENANCE CHECK, THE INTERIOR EMERGENCY EXIT LIGHT OVER THE L-2 DOOR WAS FOUND INOPERATIVE. REPLACED LIG HT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1996032200656 19960322 00656 NM 1996 3 22 ASAA9610023 1 19960228 A 5230 65549332 UPPER BEAM BOEING 737 737290C 138448V NM CARGO DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING D-CHECK, A 1 INCH CRACK WAS FOUND IN THE MAIN CARGO DOOR UPPER BEAM 1.3 INCHES FORWARD OF THE MAIN CARGO DO OR ACTUATOR ATTACHMENT FITTING, BS 465.5. REPAIRED PER EA 5230-01056 AND BOEING TELEX ASA-SEA-96-0069RR. (M) 2 L 7 2 4F A16WE 1996032200657 19960322 00657 NM 1996 3 22 ASAA9640009 1 19960216 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 763AS 25100 PVR - FLT NR 255 - CREW REPORTED, THAT THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE INOPERATIVE AT ROW 17. RESECURED AND RESPLICED WIRING AT ROW 17 AND THE LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996032200658 19960322 00658 NM 1996 3 22 ASAA964001 1 19960227 A 3230 6554791 SWITCH BOEING 737 7374Q8 NM LANDING GEAR DEFECTIVE A ASAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 01 765AS 25102 LAS - FLT NR 621 - DURING DEPARTURE THE GEAR HANDLE WOULD NOT MOVE UP. RAN 'GEAR WILL NOT GO UP' CHECKLIST AND THE TAKE OFF WARNING CONTINUED TO SOUND AFTER FLAPS WERE FULLY RETRACTED, RETURNED TO LAS. REPLACED LANDING GEAR SAFETY SWITCH. PERFORMED LANDING GEAR EXTENSION AND RETRACTION TEST AND GEAR OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996032200659 19960322 00659 NM 1996 3 22 ASAA9640010 1 19960216 A 5210 OPENING MECH BOEING 737 7374Q8 NM R-1 DOOR LACK OF LUBE A A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 773AS 25106 PDX - DURING MAINTENANCE CHECK, THE R-1 DOOR, P/N 65458491, WOULD NOT OPEN ALL THE WAY. INSPECTED DOOR, FOUND ROLLERS O N CAM DRY. LUBED ROLLERS AND RODENDS. (M) 2 L 7 2 4F RT A16WE 1996032200660 19960322 00660 NM 1996 3 22 ASAA9640012 1 19960227 A 5210 MS166241037 CLIP BOEING 737 7374Q8 NM L1 DOOR MISSING A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 762AS 25099 SEA - AFTER PASSENGERS HAD BOARDED, CREW TRIED TO CLOSE LEFT FORWARD ENTRY DOOR. DOOR WOULD NOT CLOSE. FOUND LEFT FWD DOOR HINGE LOCK PIN CLIP MISSING, CAUSING PIN TO SLIP. REPLACED CLIP ON UPPER HINGE LOCK PIN. DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996032200661 19960322 00661 NM 1996 3 22 ASAA9640013 1 19960229 A 5210 507945178 DOOR BOEING 737 7374Q8 NM L-1 LACK OF LUBE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 754AS 25095 LAX - FLT 538 - L-1 DOOR WAS DIFFICULT TO CLOSE. LUBED L-1 DOOR ROLLERS AND ACTUATOR, DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996032200662 19960322 00662 WP 1996 3 22 ASAA9680051 1 19960213 A 5210 5910081167 DOOR DOUG DC9 DC982 3022082 WP L1 DOOR OUT OF ADJUST A A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 931AS 49232 PDX - AFTER ARRIVAL OF FLIGHT 481, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN AND CLOSE. FOUND BOTTOM OF DOOR DRAG GING ON LOWER SILL. ADJUSTED DOOR PER MM AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996032200663 19960322 00663 WP 1996 3 22 ASAA9680052 1 19960214 A 3350 41B004AD07G3 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 951AS 49111 SEA - DURING MAINTENANCE CHECK, THE LEFT AND RIGHT AFT OVERWING EMERGENCY EXIT IDENTIFIER SIGNS WERE FOUND INOPERATIVE. (M) 2 L 7 2 4F A6WE 1996032200664 19960322 00664 WP 1996 3 22 ASAA9680053 1 19960214 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 951AS 49111 SEA - DURING MAINTENANCE CHECK, THE LEFT AND RIGHT AFT OVERWING EMERGENCY EXIT IDENTIFIER SIGNS WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996032200665 19960322 00665 WP 1996 3 22 ASAA9680054 1 19960217 A 3350 41B004AD07G3 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 943AS 53018 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY LIGHTS IN THE TAILCONE AREA WERE FOUND INOPERATIVE. REPLACED THE BATTERIE S AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996032200666 19960322 00666 WP 1996 3 22 ASAA9680055 1 19960217 A 3350 41B004AD07G3 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 944AS 53019 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE AFT CABIN AND THE EMERGENCY LIGHTS IN THE TAILCO NE AREA WERE FOUND DIM. REPLACED THE BATTERIES AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996032200667 19960322 00667 WP 1996 3 22 ASAA9680057 1 19960220 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 53016 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROW 32 AFT WERE FOUND INOPERATIVE. RECONNECTED WI RING AT ROW 32 AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996032200668 19960322 00668 WP 1996 3 22 ASAA9680058 1 19960220 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 943AS 53018 LAX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS AND THE OVERHEAD EMERGENCY LIGHTS ROWS 24-27 WERE FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996032200669 19960322 00669 WP 1996 3 22 ASAA9680059 1 19960222 A 3350 6011779 POWER SUPPLY DOUG DC9 DC982 3022082 WP OVERWING EXITS INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 967AS 49103 LAX - DURING MAINTENANCE CHECK, THE EXTERIOR OVERWING EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. REPLACED BATTERY PO WER SUPPLY AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996032200670 19960322 00670 WP 1996 3 22 ASAA9680061 1 19960225 A 5210 SEAL DOUG DC9 DC983 3022083 WP L1 DOOR EXCESS SEALANT A ASAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 01 945AS 49643 SEA - AFTER ARRIVAL OF FLT NR 367, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN. TRIMMED EXCESS SEALANT FROM UPPER D OOR SEAL AREA AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996032200671 19960322 00671 WP 1996 3 22 ASAA9680064 1 19960228 A 5210 MECHANISM DOUG DC9 DC982 3022082 WP R1 DOOR LACK OF LUBE A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 966AS 49104 LAX - ON ARRIVAL OF FLIGHT 594 - CREW REPORTED THE R1 DOOR WAS DIFFICULT TO CLOSE. LUBED THE DOOR ROLLER MECHANISM AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996032200672 19960322 00672 WP 1996 3 22 ASAA9680065 1 19960228 A 5311 9919605501 FRAME DOUG DC9 DC982 3022082 WP BS 1271 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 938AS 49365 OAK - DURING 30K CHECK, CORROSION WAS FOUND ON FRAME AT Y1271, X PLUS 20 TO X-15, Z-50. REMOVED DAMAGED AREA AND INSTAL LED NEW PIECES IAW DC-0 SRM 51-10-03, 51-30-02, 53-01 AND 53-03. (M) 2 L 7 2 4F A6WE 1996032200673 19960322 00673 SO 1996 3 22 ASOA96002 1 19960208 A 5330 12026335041 SKIN EMB 120 EMB120RT SO FWD FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 239AS 120057 DURING 4C INSPECTION, FOUND EXCESSIVE CORROSION ON SKIN DIRECTLY UNDER PILOTS YOKE AND STRINGER UNDER COCKPIT FLOOR BELO W PILOTS SEAT. REMOVED SKIN, TRIMMED AND FIT NEW SKIN AND INSTALLED. REMOVED AND REPLACED STRINGER ASSEMBLY UNDER COCK PIT ON LEFT SIDE ABOVE TIE STRAP FOR SKIN. REPLACED FITTING FORWARD OF SUBPANEL. ALL WORK PERFORMED IAW SRM 51-00-11. (M) 2 L 7 2 4T RT A31SO 1996032200674 19960322 00674 SO 1996 3 22 ASOA96005 1 19960306 A 2432 40769 MAIN BATTERY EMB 120 EMB120RT SO LT FWD BATT BAY DEFECTIVE A ASOA H DEACTIVATE SYST/CIRCUITS M J OVER TEMP WARNING INDICATION CR CRUISE 1 SO 11 241AS 120065 ABY/ATL - INBOUND DURING CRUISE FLIGHT, THE BATTERY OVERHEAT LIGHT ILLUMINATED. INITIALLY THE LIGHT WENT OUT AFTER APPR OX 1 SECOND, THEN ILLUMINATED AGAIN AND STAYED ON EACH TIME AN AURAL WARNING WAS ISSUED. CREW FOLLOWED EMERGENCY PROCED URES PER POH, AND LANDING WAS MADE SAFELY AND WITHOUT INCIDENT IN ATL. REMOVED AND REPLACED MAIN BATTERY. OEPRATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (X) 2 L 7 2 4T RT A31SO 1996032200675 19960322 00675 NM 1996 3 22 AWXA960046 1 19960206 A 5320 DOUBLER BOEING 737 7372A6 138448B NM BS 857 DISBOND A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 145AW 20194 PAE - FLT NR 3839 - DURING SCHEDULED C-12 MAINTENANCE CHECK, FOUND DISBOND OF SKIN BONDED DOUBLER AT STATION 857, BETWEE N STRINGER 24 AND 25 LEFT. REPAIRED DISBONDED DOUBLER AT STATION 857 BETWEEN STRINGER 24 AND 25 LEFT PER SRM 53-30-03, FIGURE 17, DETAIL II, III AND IV, SHEETS 1-7. (M) 2 L 7 2 4F A16WE 1996032200676 19960322 00676 NM 1996 3 22 AWXA960047 1 19960206 A 5320 DOUBLER BOEING 737 7372A6 138448B NM BS 877 DISBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 145AW 20194 PAE - FLT NR 3839 - DURING SCHEDULED C-12 MAINTENANCE CHECK, FOUND DISBOND OF SKIN BONDED DOUBLER AT STATION 877 BETWEEN STRINGER 21 AND 22 LEFT. REPAIRED DISBONDED DOUBLER AT STATION 877 BETWEEN STRINGER 21 AND 22 LEFT PER SRM 53-30-03, F IGURE 17, DETAIL 11, III AND IV, SHEETS 1-7. (M) 2 L 7 2 4F A16WE 1996032200677 19960322 00677 NM 1996 3 22 AWXA960048 1 19960206 A 5320 DOUBLER BOEING 737 7372A6 138448B NM BS 817 DISBOND A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 145AW 20194 PAE - FLT NR 3839 - DURING SCHEDULED C-12 MAINTENANCE CHECK, FOUND DISBOND OF SKIN BONDED DOUBLER AT STATION 817 BETWEEN STRINGERS 21 AND 23 LEFT. REPAIRED DISBONDED DOUBLER AT BS 817 BETWEEN STRINGER 21 AND 23 LEFT, PER SRM 53-30-03, FIGU RE 17, DETAILS II, III AND IV, SHEETS 1-7. (M) 2 L 7 2 4F A16WE 1996032200678 19960322 00678 NM 1996 3 22 AWXA960049 1 19960206 A 5320 DOUBLER BOEING 737 7372A6 138448B NM BS 917 DISBOND A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 145AW 20194 PAE - FLT NR 3839 - DURING SCHEDULED C-12 MAINTENANCE CHECK, FOUND DISBOND OF SKIN BONDED DOUBLER AT BS 917 BETWEEN STRI NGER 22 AND 23 RT. REPAIRED DISBONDED DOUBLER AT BS 917 BETWEEN STRINGER 22 AND 23 RIGHT PER SRM 53-30-03, FIGURE 17, D ETAILS II, II AND IV, SHEETS 1-7. (M) 2 L 7 2 4F A16WE 1996032200679 19960322 00679 NM 1996 3 22 AWXA960050 1 19960206 A 5313 STRINGER BOEING 737 7372A6 138448B NM BS 500 GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 145AW 20194 PAE - FLT NR 3839 - DURING SCHEDULED C-12 MAINTENANCE CHECK WHILE WORKING CARD NR 00294992, FOUND GOUGE IN STRINGER 22L AT BS 500A PLUS 4. REMOVED DAMAGE IN STRINGER 22L AT BS 500A PLUS 4. FABRICATED REPAIR PARTS PER SRM 53-10-03. APPLIE D ALODINE TO ALL BARE METAL AREAS PER MM 51-21-41. APPLIED 2 COATS OF PRIMER PER MM 51-21-171. INSTALLED REPAIR PARTS PER SRM 51-30-02 AND SRM 53-10-03. (M) 2 L 7 2 4F A16WE 1996032200680 19960322 00680 NM 1996 3 22 AWXA960056 1 19960208 A 5320 INTERCOSTAL BOEING 737 7372A6 138448B NM BS 332 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 145AW 20194 PAE - FLT NR 3839 - DURING SCHEDULED C-12 MAINTENANCE CHECK, FOUND S-8A INTERCOSTAL AT STATION 33 CRACKED JUST AFT OF FW D. GALLEY DOOR CUTOUT. REMOVED INTERCOSTAL, FABRICATED AND INSTALLED NEW INTERCOSTAL PER 737 SRM 51-40-02 AT BS 328 TO 344 RT. (M) 2 L 7 2 4F A16WE 1996032200681 19960322 00681 EU 1996 3 22 AWXA960057 1 19960208 A 3350 321454 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 622AW 633 054 LAS - FLT NR 85 - DURING ROUTINE MAINTENANCE CHECK, FOUND MISCELLANEOUS EMERGENCY LIGHTS IN AFT INOP. REMOVED AND REPLA CED EMERGENCY PACK, PACK CHECKS GOOD. REMOVED AND REPLACED BATTERY ON AFT POWER SUPPLY, CHECKS GOOD. (M) 2 L 7 2 4F RT A28NM 1996032200682 19960322 00682 EU 1996 3 22 AWXA960059 1 19960209 A 7710 CONNECTOR AIRBUS 320 A320231 3930325 EU NR 1 ENGINE LOOSE A AWXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 28 635AW 092 PAE-SEA - FLT NR 3851 - AIR TURN BACK, AFTER TAKEOFF, FMGC INDICATION ENGINE 1 EPR FAULT. AIRCRAFT RETURNED TO PAE LAND ING UNEVENTFUL. FOUND NR 1 ENGINE COWL CONNECTOR 8DOVC LOOSE, SEATED CONNECTOR FULLY. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4F RT A28NM 1996032200683 19960322 00683 NM 1996 3 22 AWXA960060 1 19960209 A 5311 FRAME BOEING 737 7372A6 138448B NM STA 420 DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 145AW 20194 DURING SCHEDULED C-12 MAINTENANCE CHECK, FOUND STRINGER CLIP AT STRINGER 22L, BS 420 DAMAGED, FRAME ALSO DAMAGED IN SAME AREA. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER. FITTED AND DRILLED IN PLACE, REMOVED, DEBURRED, ALODINED, PRI MED TWICE. INSTALLED REPAIR DOUBLER AND NEW STRINGER CLIP PER SRM 57-40-03, 51-10-02. (M) 2 L 7 2 4F A16WE 1996032200684 19960322 00684 NM 1996 3 22 AWXA960061 1 19960209 A 5311 FRAME BOEING 737 7372A6 138448B NM BS 277 DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 145AW 20194 PAE - FLT NR 3839 - DURING SCHEDULED C-12 MAINTENANCE CHECK, FOUND DRILL STARTS AND OPEN FASTENER HOLES IN FRAME AT STAT ION 277, STRINGER 4R. REMOVED DAMAGE FROM FRAME BS 270, STRINGER 4 RT AND THEN REMOVED FACTORY SPLICE AT BS 270 BETWEEN STRINGER 4 AND 5 RIGHT. DRILLED UP, ALODINED, PRIMED AND INSTALLED REPAIR PARTS AND FASTENERS. WET WITH SEALANT IAW S RM 51-40-02 AND 53-10-02 AND ER 020896JC. (M) 2 L 7 2 4F A16WE 1996032200685 19960322 00685 NM 1996 3 22 AWXA960062 1 19960210 A 5313 STRINGER BOEING 737 7372A6 138448B NM BS 1115 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 145AW 20194 PAE - FLT NR 3839 - DURING SCHEDULED C-12 MAINTENANCE CHECK, FOUND STRINGER CRACKED AT BS 1115, WL 244, STRINGER 13R. R EMOVED DAMAGED SECTION OF STRINGER 13R AND SECTION OF STIFFENER FOR ACCESS. FABRICATED REPAIR PARTS IAW SRM 53-10-03 AN D ER NR 020696JMI. INSTALLED REPAIR PARTS FOR STRINGER AND INSTALLED STIFFENER IAW SRM'S 53-10-03, 51-40-02 AND ER NR 0 20696JMI. (M) 2 L 7 2 4F A16WE 1996032200686 19960322 00686 NM 1996 3 22 AWXA960063 1 19960210 A 5330 SKIN BOEING 737 7372A6 138448B NM AFT FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 145AW 20194 PAE - FLT NR 3839 - DURING SCHEDULED C-12 MAINTENANCE CHECK, FOUND RT SIDE OF TAIL SECTION SKIN UNDER STAB, TAIL FIN CRA CKED, (VORTEX GEN). FUSELAGE SKIN CRACKED UNDER MIDDLE HORIZONTAL VORTEX GNERATOR SRM REPAIR INSTALLED WITH BLIND FASTE NERS. REMOVED DAMAGE AT RT SIDE OF TAIL SECTION SKIN UNDER VORTEX GENERATORS. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 53-30-03, FIGURE 6 AND ER 2-53-36-18. (M) 2 L 7 2 4F A16WE 1996032200687 19960322 00687 NM 1996 3 22 AWXA960064 1 19960210 A 5230 FRAME BOEING 737 7372A6 138448B NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 145AW 20194 PAE - FLT NR 3839 - DURING SCHEDULED C-12 MAINTENANCE CHECK, FOUND AFT CARGO DOOR, DOOR FRAME CRACKED IN LOWER RADIUS BY THE FWD NR 5 STOP PIN FITTING, BS 800. REPLACED FRAME WITH NEW IAW OHM 52-36-02. (M) 2 L 7 2 4F A16WE 1996032200688 19960322 00688 NM 1996 3 22 AWXA960065 1 19960210 A 5230 6547952524 SKIN BOEING 737 7372A6 138448B NM CARGO DOOR GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 145AW 20194 PAE - FLT NR 3839 - DURING SCHEDULED C-12 MAINTENANCE CHECK, FOUND AFT CARGO DOOR OUTER SKIN HAS GENERAL GOUGES OUT OF L IMITS. REMOVED AND REPLACED OUTER SKIN IAW OHM 52-36-02. (M) 2 L 7 2 4F A16WE 1996032200689 19960322 00689 NM 1996 3 22 AWXA960066 1 19960210 A 5230 DOOR FRAME BOEING 737 7372A6 138448B NM CARGO COMPT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 145AW 20194 PAE - FLT NR 3839 - DURING SCHEDULED C-12 MAINTENANCE CHECK, FOUND AFT CARGO DOOR, DOOR FRAME CRACKED IN LOWER RADIUS BY THE AFT NR 5 STOP PIN FITTING BS 877.09. REPLACED FRAME WITH NEW IAW OHM 52-36-02. (M) 2 L 7 2 4F A16WE 1996032200690 19960322 00690 NM 1996 3 22 AWXA960067 1 19960212 A 5320 65C352825 WINDOW POST BOEING 737 7372A6 138448B NM LT COCKPIT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 145AW 20194 DURING SCHEDULED C-12 MAINTENANCE CHECK, FOUND CRACK INDICATION NOTED BOTTOM LEFT E-F WINDOW POST. ACCESS REQUIRED TO D ETERMINE EXTENT OF CRACK. REPAIRED LEFT E-F WINDOW POST IAW EO 53-11-07. (M) 2 L 7 2 4F A16WE 1996032200691 19960322 00691 NM 1996 3 22 AWXA960068 1 19960211 A 5320 SILL BOEING 737 7372A6 138448B NM BS 314-344 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 145AW 20194 PAE - FLT NR 3839 - DURING SCHEDULED C-12 MAINTENANCE CHECK, FOUND CORROSION ON FWD ENTRY DOORWAY MOPSILL AT BS 312 TO 3 44, WL 208. REMOVED CORROSION AND TREATED. REMOVED DAMAGED AREA AT BS 333 AND INSTALLED REPAIR IAW SRM 51-10-06, 51-40 -03. (M) 2 L 7 2 4F A16WE 1996032200692 19960322 00692 NM 1996 3 22 AWXA960069 1 19960204 A 5330 SKIN BOEING 737 7372A6 138448B NM BS 350 DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 145AW 20194 PAE - FLT NR 3839 - DURING SCHEDULED C-12 MAINTENANCE CHECK, FOUND DENT IN SKIN STATION 350 RT BETWEEN STRINGER 17R AND 18R. REMOVED DAMAGED SKIN 1.25 DIAMETER. FABRICATED REPAIR PARTS AND INSTALLED ON AIRCRAFT. ALL WORK DONE IAW SRM 53- 30-03. (M) 2 L 7 2 4F A16WE 1996032200693 19960322 00693 NM 1996 3 22 AWXA960071 1 19960211 A 5311 FRAME BOEING 737 7372A6 138448B NM BS 420 DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 145AW 20194 PAE - FLT NR 3839 - DURING SCHEDULED C-12 MAINTENANCE CHECK, FOUND STRINGER CLIP AT STRINGER 22L, BS 420 DAMAGED. FRAME ALSO DAMAGED IN SAME AREA. REMOVED AND REPLACED DAMAGED STRINGER CLIP. REMOVED DAMAGED AREA OF FRAME AND INSTALLED RE PAIR IAW SRM 51-10-02, 51-40-03. (M) 2 L 7 2 4F A16WE 1996032200694 19960322 00694 NM 1996 3 22 AWXA960072 1 19960210 A 5511 BAC15141322 SPAR CHORD BOEING 737 7372A6 138448B NM RT HORIZ STAB CORROSION A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 145AW 20194 PAE - FLT NR 3839 - DURING SCHEDULED C-12 MAINTENANCE CHECK, FOUND THE RIGHT HORIZONTAL STABILIZER REAR SPAR LOWER CHORD CORRODED ON THE FORWARD SIDE FROM APPROXIMATELY STAB STA 244.5 TO 253.67. REPAIRED RIGHT HORIZONTAL STABILIZER REAR SP AR LOWER CHORD IAW SRM 55-10-01, 55-10-05, 55-10-04 AND 51-30-02. (M) 2 L 7 2 4F A16WE 1996032200695 19960322 00695 NM 1996 3 22 AWXA960073 1 19960212 A 5330 SKIN BOEING 737 7372A6 138448B NM FUSELAGE DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 145AW 20194 PAE - FLT NR 3839 - DURING SCHEDULED C-12 MAINTENANCE CHECK, FOUND FORWARD CARGO DOOR CUTOUT LOWER CORNER FUSELAGE SKIN DELAMINATED. REPAIRED IAW ER 2-53-33-13. (M) 2 L 7 2 4F A16WE 1996032200696 19960322 00696 NM 1996 3 22 AWXA960074 1 19960211 A 5330 SKIN BOEING 737 7372A6 138448B NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 145AW 20194 PAE - FLT NR 3839 - DURING SCHEDULED C-12 MAINTENANCE CHECK, FOUND FORWARD GALLEY DOOR WAY OUTER SKIN CRACKED THROUGH FA STENER HOLE AT FORWARD LOWER CORNER OF DOORWAY. REPAIRED IAW SB 737-53-1074 AND DRAWING 65C27287. (M) 2 L 7 2 4F A16WE 1996032200697 19960322 00697 NM 1996 3 22 AWXA960075 1 19960218 A 5755 SKIN BOEING 737 737277 1384570 NM NR 4 SPOILER DETERIORATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 PAE - FLT NR 3887 - DURING ROUTINE C-7 MAINTENANCE CHECK, FOUND NR 4 SPOILER HAS DETERIORATED PREVIOUS REPAIR ON UPPER S URFACE, CENTER OF PANEL. FILLED DENT IN UPPER SURFACE OF NR 4 SPOILER IAW SRM 51-40-06. (M) 2 L 7 2 4F RT A16WE 1996032200698 19960322 00698 NM 1996 3 22 AWXA960076 1 19960218 A 5753 SKIN BOEING 737 737277 1384570 NM LT TE FOREFLAP DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 PAE - FLT NR 3887 - DURING ROUTINE C-7 MAINTENANCE CHECK, FOUND LEFT WING OUTBOARD FOREFLAP HAS DELAMINATED SKIN ON LOWE R SURFACE 5 FEET FROM INBOARD END. REMOVED DELAMINATED SKIN SECTION AND REPAIRED IAW SRM 51-40-06. (M) 2 L 7 2 4F RT A16WE 1996032200699 19960322 00699 NM 1996 3 22 AWXA960077 1 19960216 A 5315 FLOOR BEAM BOEING 737 7373G7 1384595 NM BS 312 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 305AW 24012 PAE - FLT NR 3889 - DURING ROUTINE C-8 MAINTENANCE CHECK, FOUND FLOOR BEAM TOP FLANGE CORRODED AT FLOOR BOARD HOLES STAT ION 312. REMOVED DAMAGED AREA OF FLOOR BEAM UPPER CHORD FROM LBL 19 TO RBL 24. REPAIRED PER 737 SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1996032200700 19960322 00700 NM 1996 3 22 AWXA960078 1 19960216 A 5320 SUPPORT BOEING 737 737277 1384570 NM BS 727-747 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 PAE - FLT NR 3887 - DURING ROUTINE C-7 MAINTENANCE CHECK, FOUND CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS 727B-4 TO 747, RBL 22, WL 156. REMOVED AND REPLACED SUPPORT FROM BS 727 TO BS 767 IAW SRM 53-20-02, FIGURE 9, 51-10- 01, 51-30-02, 51-40-02. (M) 2 L 7 2 4F RT A16WE 1996032200701 19960322 00701 NM 1996 3 22 AWXA960079 1 19960218 A 5320 WEB BOEING 737 737277 1384570 NM BS 847 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 PAE - FLT NR 3887 - DURING ROUTINE C-7 MAINTENANCE CHECK, FOUND CRACKED WEB IN AFT CARGO BAY RIGHT SIDE AT BS 847, WL 15 6, RLB 19. REMOVED CRACKED WEB, FABRICATED NEW, AND INSTALLED IAW MM 51-21-41, 51-21-171, SRM 51-20-01, 51-30-05. (M) 2 L 7 2 4F RT A16WE 1996032200702 19960322 00702 NM 1996 3 22 AWXA960080 1 19960217 A 5512 SKIN BOEING 737 737277 1384570 NM LT HORIZ STAB DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 PAE - FLT NR 3887 - DURING ROUTINE C-7 MAINTENANCE CHECK, FOUND DENT ON LEFT HORIZONTAL STAB LEADING EDGE AT LEADING EDG E STATION 203, OUT OF LIMITS. RECONTOURED DENT IAW SRM 55-10-01. (M) 2 L 7 2 4F RT A16WE 1996032200703 19960322 00703 NM 1996 3 22 AWXA960081 1 19960218 A 5753 SKIN BOEING 737 737277 1384570 NM LT TE FORE FLAP DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 PAE - FLT NR 3887 - DURING ROUTINE C-7 MAINTENANCE CHECK, FOUND DELAMINATED SKIN ON LEFT WING OUTBOARD FOREFLAP LOWER SU RFACE 27 INCHES FROM INBOARD END. REMOVED DELAMINATED SKIN SECTION AND REPAIRED IAW SRM 51-40-06. (M) 2 L 7 2 4F RT A16WE 1996032200704 19960322 00704 NM 1996 3 22 AWXA960082 1 19960219 A 5330 SKIN BOEING 737 737277 1384570 NM BS 320 DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 PAE - FLT NR 3887 - DURING ROUTINE C-7 MAINTENANCE CHECK, FOUND DENT IN SEAM JUST BELOW THE FORWARD SERVICE DOOR BETWEEN STRINGER 18 AND 19 RT AT BS 320. FOUND DENT TO BE OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED REPAIR PART AND INS TALLED ON AIRCRAFT. ALL WORK DONE IAW SRM SRM 53-30-03. (M) 2 L 7 2 4F RT A16WE 1996032200705 19960322 00705 NM 1996 3 22 AWXA960083 1 19960220 A 5330 SKIN BOEING 737 737277 1384570 NM BS 807 DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 DURING ROUTINE C-7 MAINTNENANCE CHECK, FOUND FUSELAGE SKIN DENT AT STATION 807 STRINGER 28 REINSPECT FOR PULLING FASTENE RS, CORROSION AND DEVELOPMENT OF CRACKS. REMOVED RIVITS BETWEEN STRINGER 28R AND 28L AT BS 807, FOUND NO CRACK INDICATI ONS. REMOVED DAMAGE SHEAR TIE, FABRICATED, ALODINED, PRIMED REPAIR PARTS AND INSTALLED IAW SRM 53-10-04. (M) 2 L 7 2 4F RT A16WE 1996032200706 19960322 00706 NM 1996 3 22 AWXA960085 1 19960218 A 5320 STRAP BOEING 737 7373G7 1384595 NM BS 312 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 305AW 24012 PAE - FLT NR 3889 - DURING ROUTINE C-8 MAINTENANCE CHECK, FOUND CRACKS IN STABILIZER STRAP BS 312, WL 200, RBL 31. REPA IRED STABILIZER STRAP IAW SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1996032200707 19960322 00707 NM 1996 3 22 AWXA960086 1 19960220 A 5512 SKIN BOEING 737 7373G7 1384595 NM LT HORIZ STAB DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 305AW 24012 PAE - FLT NR 3889 - DURING ROUTINE C-8 MAINTENANCE CHECK, FOUND DENT ON LEFT HORIZONTAL STAB LEADING EDGE AT LEADING EDG E STATION 203. RECONTOURED DENT ON LEFT HORIZONTAL STABILIZER LEADING EDGE STATION 203 IAW SRM 55-10-01. (M) 2 L 7 2 4F RT A16WE 1996032200708 19960322 00708 NM 1996 3 22 AWXA960087 1 19960221 A 5347 SEAT TRACK BOEING 737 737277 1384570 NM BS 1016 CORROSION A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 PAE - FLT NR 3887 - DURING ROUTINE C-7 MAINTENANCE CHECK, FOUND CORROSION ON GALLEY SEAT TRACKS BS 987-1016, RBL 17, WL 208. REMOVED, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 51-30-8, 51-30-0 AND 51-30-2 AT BS 987-1016, RBL 17, WL 208 . (M) 2 L 7 2 4F RT A16WE 1996032200709 19960322 00709 NM 1996 3 22 AWXA960088 1 19960221 A 5347 SEAT TRACK BOEING 737 737277 1384570 NM BS 1016 CORROSION A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 PAE - FLT NR 3887 - DURING ROUTINE C-7 MAINTENANCE CHECK, FOUND CORROSION ON GALLEY SEAT TRACK BS 987-1016, RBL 37, WL 2 08. REMOVED, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-10-5, 51-30-8, 51-30-0 AND 51-30-2 AT BS 987-1016, RBL 37 , WL 208. (M) 2 L 7 2 4F RT A16WE 1996032200710 19960322 00710 NM 1996 3 22 AWXA960089 1 19960221 A 5320 MOPSILL BOEING 737 737277 1384570 NM BS 989-990 CORROSION A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 PAE - FLT NR 3887 - DURING ROUTINE C-7 MAINTENANCE CHECK, FOUND CORROSION ON AFT SERVICE DOOR MOPSILL BS 989-990, WL 208 . REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 51-10-02, 51-30-02 AND 51-10-06 AT BS 989-990, WL 208, RBL 58. (M) 2 L 7 2 4F RT A16WE 1996032200711 19960322 00711 NM 1996 3 22 AWXA960090 1 19960221 A 5315 BAC1505100617 FLOOR BEAM BOEING 737 737277 1384570 NM BS 987 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 PAE - FLT NR 3887 - DURING ROUTINE C-7 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM BS 987, LBL 5 - RBL 5, WL 208. F OUND CORROSION ON UPPER CHORD OF FLOOR BEAM BS 987 LBL-RBL 5 TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED CORRODED UP C HORD OF FLOOR BEAM FROM LBL 6 TO RBL 50, FABRICATED NEW UPPER CHORD REPAIR PARTS, APPLIED ALODINE AND PRIMER. INSTALLED WET WITH SEALANT AND INSTALLED FASTENERS PER SRM 53-10-9. (M) 2 L 7 2 4F RT A16WE 1996032200712 19960322 00712 NM 1996 3 22 AWXA960091 1 19960221 A 5330 SKIN BOEING 737 737277 1384570 NM BS 959 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 187AW 22654 PAE - FLT NR 3887 - DURING ROUTINE C-7 MAINTENANCE CHECK, FOUND SKIN CRACKED AT FWD LOWER CORNER OF AFT ENTRY DOOR AT BS 959, WL 211. ACCESSED AREA, CONTAINED CRACK. FABRICATED REPAIR PARTS. INSTALLED ON AIRCRAFT, REINSTALLED ITEMS ACCES SED. ALL WORK DONE IAW AWA EO 53-30-15. (M) 2 L 7 2 4F RT A16WE 1996032200713 19960322 00713 NM 1996 3 22 AWXA960092 1 19960220 A 3397 WIRE BOEING 737 7373B7 1384580 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 328AW 23377 PHX - FLT NR 1649 - PHX-SNA - CALL AT PUSH, FLOOR PROX EMERGENCY LIGHTS INOP. REPAIRED BROKEN WIRE, CHECKS GOOD. (M) 2 L 7 2 4F RT A16WE 1996032200714 19960322 00714 NM 1996 3 22 AWXA960093 1 19960224 A 3397 WIRE BOEING 757 7572S7 1384962 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 906AW 23568 PHX - FLT NR 20 - DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT INOP AT SEAT 20 A,B,C . REPAIRED WIRING. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 1996032200715 19960322 00715 NM 1996 3 22 AWXA960094 1 19960226 A 5330 SKIN BOEING 737 737277 1384570 NM BS 400 DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 PAE - FLT NR 3868 - DURING SCHEDULED C-14 MAINTENANCE CHECK, FOUND LARGE DENT IN SKIN AT BS 400, BETWEEN STRINGER 23 AND 24 RT. REMOVED DAMAGED SKIN AT BS 400, STRINGER 23 AND 24 RIGHT PER 53-30-3, FIGURE 1. FABRICATED REPAIR PARTS, INSTA LLED REPAIR PARTS, COUNTERSKIN FILLERS AND FASTENERS, WET THE SEAL. ALL WORK IAW SRM 53-30-3. (M) 2 L 7 2 4F RT A16WE 1996032200716 19960322 00716 NM 1996 3 22 AWXA960095 1 19960226 A 5512 SKIN BOEING 737 737277 1384570 NM RT HORIZ STAB DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 PAE - FLT NR 3868 - DURING SCHEDULED C-14 MAINTENANCE CHECK, FOUND 2 DENTS AT RIBS NR 12 AND NR 1 ON THE RIGHT HAND HORI ZONTAL STABILIZER. FOUND DENT AT RIB 12 OUT OF LIMITS. RECONTOURED DENT. SERVICEABLE PER SRM 55-10-1. (M) 2 L 7 2 4F RT A16WE 1996032200717 19960322 00717 NM 1996 3 22 AWXA960096 1 19960226 A 5320 654587545 SILL BOEING 737 7373G7 1384595 NM BS 292-340 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 PAE - FLT NR 3873 - DURING SCHEDULED C-8 MAINTENANCE CHECK, FOUND CORROSION ON MOP SILL BS 292-340, RBL 62, WL 208. BEA M CORROSION REMOVAL, DISCOVERED CRACK IN MOP SILL CREASE AT BS 294, RBL 62. REMOVED AND REPLACED MOP SILL IAW 737 SRM 5 3-10-15. (M) 2 L 7 2 4F RT A16WE 1996032200718 19960322 00718 NM 1996 3 22 AWXA960097 1 19960226 A 5320 SUPPORT BOEING 737 7373G7 1384595 NM BS 312-328 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 PAE - FLT NR 3873 - DURING SCHEDULED C-8 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR SUPPORT STATION 312-328, LBL 10, WL 208. REMOVED OLD, FABRICATED NEW FLOOR SUPPORT AND INSTALLED IAW SRM 51-10-1, 51-10-51, 53-10-13. (M) 2 L 7 2 4F RT A16WE 1996032200719 19960322 00719 NM 1996 3 22 AWXA960098 1 19960226 A 5320 SUPPORT BOEING 737 7373G7 1384595 NM BS 328-344 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 PAE - FLT NR 3873 - DURING SCHEDULED C-8 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR SUPPORT STATION 328-344, LBL 10, WL 208. REMOVED OLD SUPPORT, FABRICATED NEW FLOOR SUPPORT AND INSTALLED IAW SRM 51-10-1, 53-10-51, 53-10-13. (M) 2 L 7 2 4F RT A16WE 1996032200720 19960322 00720 NM 1996 3 22 AWXA960099 1 19960226 A 5315 BAC14902734 FLOOR BEAM BOEING 737 7373G7 1384595 NM BS 344 CORROSION A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 PAE - FLT NR 3873 - DURING SCHEDULED C-8 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM STATION 344 WL 208, LBL 3-50. REPAIRED FLOOR BEAM AT BS 344, WL 208, PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1996032200721 19960322 00721 NM 1996 3 22 AWXA960100 1 19960226 A 5512 SKIN BOEING 737 737277 1384570 NM LT HORIZ STAB DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 PAE - FLT NR 3868 - DURING SCHEDULED C-14 MAINTENANCE CHECK, FOUND THREE DENTS IN THE LEFT HORIZONTAL STABILIZER LEADING EDGE SKIN AT RIBS NR 16, NR 10 AND NR 6. REMOVED AND RECONTOURED LEFT HORIZONTAL STABILIZER LEADING EDGE AND REINSTALL ED PER SRM 55-10-01 AND MM 27-41-21. (M) 2 L 7 2 4F RT A16WE 1996032200722 19960322 00722 NM 1996 3 22 AWXA960101 1 19960226 A 5315 BAC14902734 FLOOR BEAM BOEING 737 7373G7 1384595 NM BS 344 CORROSION A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 PAE - FLT NR 3873 - DURING SCHEDULED C-8 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM STATION 344, WL 208, LBL 3-50. REPAIRED FLOOR BEAM AT BS 344, WL 208, PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1996032200723 19960322 00723 NM 1996 3 22 AWXA960102 1 19960227 A 5330 SKIN BOEING 737 737277 1384570 NM BS 929 DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 PAE - FLT NR 3868 - DURING SCHEDULED C-14 MAINTENANCE CHECK, FOUND 2 DENTS IN SKIN AT BS 929 BETWEEN STRINGER 17L AND 18 L. DENT IS .045 DEEP AND 1.3 INCHES ROUND. REMOVED DAMAGE. FABRICATED REPAIR PARTS AND INSTALLED REPAIR DOUBLER IAW S RM 53-30-3, FIGURE 1. (M) 2 L 7 2 4F RT A16WE 1996032200724 19960322 00724 NM 1996 3 22 AWXA960103 1 19960227 A 5315 BAC150529222 FLOOR BEAM BOEING 737 7373G7 1384595 NM BS 297 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 FLT NR 3873 - PAE - DURING SCHEDULED C-8 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM RBL 8-12 AND LBL 8, WL 208, BS 297. CORROSION OUT OF LIMITS. REMOVED AND REPLACED UPPER CHORD OF FLOOR BEAM AT BS 297, WL 208, LBL 24 TO RBL 29. (M ) 2 L 7 2 4F RT A16WE 1996032200725 19960322 00725 NM 1996 3 22 AWXA960104 1 19960227 A 5315 BAC1505100246 FLOOR BEAM BOEING 737 7373G7 1384595 NM BS 312 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303AW 24010 PAE - FLT NR 3873 - DURING SCHEDULED C-8 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM BS 312, RBL 8 TO LBL 25, WL 20 8. CORROSION OUT OF LIMITS. REMOVED AND REPLACED UPPER CHORD ON FLOOR BEAM BS 312, RBL 12 TO LBL 30, WL 208. (M) 2 L 7 2 4F RT A16WE 1996032200726 19960322 00726 NM 1996 3 22 AWXA960105 1 19960227 A 5330 SKIN BOEING 737 737277 1384570 NM BS 813 DENT A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 DURING SCHEDULED C-14 MAINTENANCE CHECK, FOUND DENT IN SKIN AT BS 813 BETWEEN STRINGER 18L AND 19L. DENT .037 INCH BY 1 INCH BY 1 INCH. DENT OUT OF LIMITS. CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND INSTALLED PER SRM 53-30-3. ( M) 2 L 7 2 4F RT A16WE 1996032200727 19960322 00727 NM 1996 3 22 CAL960153 1 19960129 A 3350 LIGHT BOEING 727 727224 1384076 NM GALLEY INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 79750 22452 STATION 31J - INSPECTION FOUND THE AFT GALLEY SERVICE DOOR AND FORWARD LIFE RAFT BIN EMERGENCY LIGHTS INOPERATIVE. THE EMERGENCY LIGHTS AT LIFE RAFT BIN WERE CHARGED. THE GALLEY PORTABLE LIGHT WAS REMOVED AND REPLACED. (M) 2 L 7 3 4F A3WE 1996032200728 19960322 00728 NM 1996 3 22 CAL960183 1 19960220 A 3260 LOGIC CARD BOEING 737 7373T0 1384582 NM NLG INOPERATIVE A CALA O OTHER N FALSE WARNING CR CRUISE 1 SW 09 69311 23362 FLT NR 1796 - PHL - THE NOSE GEAR RED LIGHT AND GREEN LIGHT ILLUMINATED WHILE IN FLIGHT FROM IAH TO PHL. PILOT TRIED GE AR HANDLE UP WITH NO CHANGE. WHEN GEAR WAS EXTENDED FOR LANDING AT PHL ALL THREE GREEN LIGHTS ILLUMINATED WITH NO RED. MAINTENANCE FOUND THE M983 LOGIC CARD AT FAULT. THE M983 LOGIC CARD WAS REMOVED AND REPLACED. THE SYSTEM WAS TESTED W ITH NO DEFECTS NOTED. THE NOSE GEAR WAS CYCLED IAW MM 32-09-20 WITH OPERATION AND INDICATIONS CHECKING GOOD. (M) 2 L 7 2 4F RT A16WE 1996032200729 19960322 00729 WP 1996 3 22 CAL960184 1 19960220 A 3260 DNLOCK SENSOR DOUG DC9 DC982 3022082 WP RT MLG INOPERATIVE A CALA O OTHER N FALSE WARNING CL CLIMB 1 SW 09 57837 49582 FLT NR 498 - BOS - THE A/C HAD A BRIEF HISTORY OF THE RIGHT MLG RED LIGHT REMAINING ILLUMINATED AFTER GEAR RETRACTION. W HEN GEAR WAS EXTENDED FOR LANDING THE GREEN LIGHT WOULD ILLUMINATE. MAINTENANCE FOUND THE RIGHT MLG DOWNLOCK SENSOR AT FAULT. THE RIGHT MLG DOWNLOCK SENSOR WAS REMOVED AND REPLACED IAW MM 32-60-05, PAGE 201. OPERATION AND INDICATIONS CHE CKED GOOD. THE AIRCRAFT HAS COMPLETED OVER 9 FLIGHTS WITHOUT A REPEAT OF THE PROBLEM SINCE THIS CORRECTIVE ACTION WAS I MPLEMENTED. (M) 2 L 7 2 4F A6WE 1996032200730 19960322 00730 NM 1996 3 22 CAL960185 1 19960222 A 2910 65445101218 HYD LINE BOEING 737 737130 1384435 NM A HYD SYSTEM CHAFED A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 44214 19031 FLT NR 1036 - GSO - THE 'A' HYDRAULIC SYSTEM FLUID QUANTITY DROPPED TO ZERO WHILE EN ROUTE FROM BNA TO EWR. A MANUAL GE AR EXTENSION WAS PERFORMED AND THE AIRCRAFT WAS DIVERTED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC LINE IN LEFT WING ROOT CHAFED. THE HYDRAULIC LINE WAS REMOVED AND REPLACED. THE HYDRAULIC SYSTEM WAS SERVIC ED TO FULL AND LEAK CHECK WAS GOOD. (M) 2 L 7 2 4F A16WE 1996032200731 19960322 00731 WP 1996 3 22 CAL960186 1 19960222 A 2420 947F9452 GEN CONTL PANEL DOUG DC9 DC982 3022082 WP OVERHEAD PANEL INOPERATIVE A CALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 09 33817 29888 49371 FLT NR 1994 - IAH - THE LEFT GENERATOR TRIPPED OFF FOLLOWED BY ILLUMINATION OF THE DC EMERGENCY BUS OFF LIGHT. THE GENE RATOR BUS OFF LIGHT PROCEDURES WERE FOLLOWED AND THE DC BUS CROSSTIE SWITCH WAS CLOSED. THE DC EMERGENCY BUS LIGHT CAME ON AND THE AIRCRAFT WAS RETURNED TO IAH. MAINTENANCE FOUND THE LEFT GCU AT FAULT. THE LEFT GCU WAS REMOVED AND REPLA CED. THE ENGINES WERE RUN AND THE SYSTEM CHECKED GOOD. (M) 2 L 7 2 4F A6WE 1996032200732 19960322 00732 NE 1996 3 22 CAL960187 2 19960222 A 7230 9128M36G06 AIR DUCT DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2B 30018 NE NR 3 ENGINE FAILED A CALA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SW 09 87070 66973 1388 48292 455431 IAH - FLT 0010 - TAKEOFF WAS REJECTED AT 100 KNOTS AFTER THE NR 3 ENGINE EXPERIENCED LOSS OF POWER. THE NR 3 ENGINE WAS REMOVED AND REPLACED. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION. SUPPLEMENT: PRELIMINARY I NVESTIGATION REVEALED UNCONTAINED FAILURE IN LPT ROTOR AREA. SHOP INSPECTION FOUND THE FAN MID-SHAFT SHEARED OFF. SUBM ITTER STATED THE SUSPECTED CAUSE OF FAILURE WAS THE HPC ROTOR AIR DUCT FAILED AND RUBBED ON FAN MID-SHAFT. (X) 2 L 7 3 4F 4 F A22WE E23EA 1996032200733 19960322 00733 NM 1996 3 22 CAL960188 1 19960223 A 3260 CIRCUIT BREAKER BOEING 737 7373T0 1384582 NM COCKPIT POPPED A CALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SW 09 17321 23372 FLT NR 1645 - EWR - WHEN GEAR WAS EXTENDED FOR LANDING AT PHX, THREE GREEN GEAR INDICATION LIGHTS WERE NOT RECEIVED. TH E NOSE GEAR AIR/GROUND CIRCUIT BREAKER WAS FOUND POPPED DURING A TOWER FLYBY. THE CIRCUIT BREAKER WAS RESET AND PANEL I NDICATED THREE GREEN. THE AIRCRAFT LANDED WITHOUT FURTHER PROBLEMS. (M) 2 L 7 2 4F RT A16WE 1996032200734 19960322 00734 WP 1996 3 22 CAL960189 1 19960224 A 3230 RETRACT MECH DOUG DC9 DC932 3022066 WP NLG MALFUNCTIONED A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 27522 47524 FLT NR 1047 - CLE - THE NOSE GEAR DID NOT RETRACT AFTER TAKEOFF FROM CLE. THE GEAR WAS CYCLED AND THE NOSE GEAR GREEN L IGHT ILLUMINATED IMMEDIATELY. THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. THE GEAR WAS SWUNG SE VERAL TIMES IAW MM 32-60-0 WITH ALL INDICATIONS AND OPERATION CHECKING GOOD. THE PROBLEM COULD NOT BE DUPLICATED. (M) 2 L 7 2 4F A6WE 1996032200735 19960322 00735 NM 1996 3 22 CAL960190 1 19960225 A 3260 LAMP BOEING 737 737130 1384435 NM RT MLG INOPERATIVE A CALA O OTHER N FALSE WARNING AP APPROACH 1 SW 09 33202 19019 FLT NR 591 - MSP - THE RIGHT MLG GREEN LIGHT DID NOT ILLUMINATED WHEN GEAR WAS EXTENDED FOR LANDING ON APPROACH TO MSP, AND IT WOULD NOT TEST. CHANGING BULBS DID NOT HELP. THE GEAR WAS VISUALLY INSPECTED AND CONFIRMED DOWN AND LOCKED. TH E AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RIGHT MLG DOWN INDICATION LIGHT BURNED OUT. THE INDICATOR LI GHT WAS RELAMPED AND OPERATION CHECKED NORMAL. (M) 2 L 7 2 4F A16WE 1996032200736 19960322 00736 NM 1996 3 22 CAL960191 1 19960225 A 5754 ROLLERS/TRACKS BOEING 737 7373T0 1384582 NM NR 5 LE SLAT LACK OF LUBE A CALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SW 09 69348 23586 FLT NR 1708 - EWR - WHEN FLAPS WERE SELECTED BEYOND 5 DEGREES CREW RECEIVED T/E FLAP ASYMMETRY. THE SAFETY WIRES WERE B ROKEN ON GPWS AND ALTERNATE FLAP MASTER SWITCH. THE LEFT INDICATOR WENT TO 10 DEGREES AND THE RIGHT STAYED AT 5 DEGREES . THE AIRCRAFT WAS DIVERTED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 5 SLAT ROLLERS AND TRACK S DRY. THE NR 5 SLAT ROLLERS AND TRACKS WERE LUBRICATED. AN ADJUSTMENT AND TEST OF THE SLAT LEADING EDGE SYSTEM WAS PE RFORMED IAW MM 27-81-00. THE FLAPS/SLATS WERE OPERATED SEVERAL TIMES WITH NO ASYMMETRY PROBLEMS NOTED. (M) 2 L 7 2 4F RT A16WE 1996032200737 19960322 00737 WP 1996 3 22 CAL960192 1 19960225 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP FORWARD ENTRY INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16804 49246 FLT NR 0697 - EWR - THE PORTABLE EMERGENCY LIGHT AT FORWARD ENTRY WOULD NOT ILLUMINATE. THE PORTABLE EMERGENCY LIGHT WA S REPLACED AND OPERATION CHECKED GOOD. (M) 2 L 7 2 4F A6WE 1996032200738 19960322 00738 NM 1996 3 22 CAL960193 1 19960219 A 5230 SKIN BOEING 737 7373T0 1384582 NM CARGO DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12313 33232 23364 GSO - INSPECTION FOUND THE C-1 DOOR SKIN DENTED AND CREASED IN SEVERAL PLACES ABOVE DOOR HANDLE LEVEL. THE DAMAGED AREA OF SKIN WAS CUT OUT. DOUBLER REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 52-00-01, 51-20-01, AND 51-40-00. (M) 2 L 7 2 4F RT A16WE 1996032200739 19960322 00739 NM 1996 3 22 CAL960194 1 19960219 A 5330 SKIN BOEING 737 7373T0 1384582 NM BS 847 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12313 33232 23364 GSO - INSPECTION FOUND THE FUSELAGE SKIN DENTED ON RIGHT SIDE AT STATION 847 ABOVE STRINGER 19R. THE DENTED AREA WAS CU T OUT. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-00-01, 51-20-01, AND 51-40-02. (M) 2 L 7 2 4F RT A16WE 1996032200740 19960322 00740 NM 1996 3 22 CAL960195 1 19960219 A 5321 FLOOR WEB BOEING 737 7373T0 1384582 NM RT AFT LAV CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12313 33232 23364 GSO - INSPECTION FOUND RIGHT AFT LAV FLOOR WEB CORRODED AT ATTACH AREAS, RBL 8 AND RBL 15. THE CORRODED AREAS WERE REMO VED. A REPLACEMENT WEB AND ATTACH ANGLE WERE FABRICATED AND INSTALLED IAW BAC DRAWING 65-52457 AND SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 1996032200741 19960322 00741 NM 1996 3 22 CAL960196 1 19960219 A 5315 FLOOR BEAM BOEING 737 7373T0 1384582 NM BS 312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12313 33232 23364 GSO - INSPECTION FOUND FLOOR BEAM CORRODED AT STATION 312 FROM RBL 30 TO LBL 11. THE UPPER T-CAP WAS REMOVED FROM LBL 1 1 TO RIGHT CUSP. A NEW T-CAP SEGMENT WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-70-12, 51-20-01, AND 51-40-00. ( M) 2 L 7 2 4F RT A16WE 1996032200742 19960322 00742 NM 1996 3 22 CAL960197 1 19960217 A 5230 SKIN BOEING 737 7373T0 1384582 NM CARGO DOR GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12313 33232 23364 GSO - INSPECTION FOUND TWO GOUGES IN C-2 DOOR EXTERNAL SKIN. THE GOUGED AREAS WERE CUT OUT. REPAIR FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 52-30-01. (M) 2 L 7 2 4F RT A16WE 1996032200743 19960322 00743 NM 1996 3 22 CAL960198 1 19960217 A 5330 SKIN BOEING 737 7373T0 1384582 NM BS 847 GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12313 33232 23364 GSO - INSPECTION FOUND THREE GOUGES IN RIGHT SIDE FUSELAGE SKIN AT STATION 847 BETWEEN STRINGER 20R AND STRINGER 21R. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-00-01, FIGURE 201, 51-20-01, AND 51-40-02. (M) 2 L 7 2 4F RT A16WE 1996032200744 19960322 00744 NM 1996 3 22 CAL960199 1 19960217 A 5315 FLOOR BEAM BOEING 737 7373T0 1384582 NM FS 986.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12313 33232 23364 GSO - INSPECTION FOUND FS 986.5 MAIN CABIN FLOOR BEAM UPPER CHORD CORRODED AT RBL 37, RBL 23, RBL 10, LBL 6.5, LBL 19.5 AND LBL 32. THE UPPER CHORD SECTION WAS CUT OFF FROM CUSP TO CUSP. A 'T' ANGLE WAS INSTALLED IAW SRM 53-00-51 AND A 'T ' CHORD UPPER SEGMENT WAS INSTALLED IN TWO SECTIONS IAW SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 1996032200745 19960322 00745 NM 1996 3 22 CAL960200 1 19960217 A 5315 FLOOR BEAM BOEING 737 7373T0 1384582 NM BS 940-986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12313 33232 23364 GSO - INSPECTION FOUND L-2 DOOR THRESHOLD FLOOR BEAM CHORD CORRODED FROM STATION 940 TO STATION 986. THE CHORD SEGMENT WAS REMOVED FROM STATION 910 TO 1006 AND A NEW CHORD WAS INSTALLED IAW SRM 51-40-02 AND BAC DRAWING 65C80735. (M) 2 L 7 2 4F RT A16WE 1996032200746 19960322 00746 WP 1996 3 22 CAL960201 1 19960226 A 3260 DNLOCK SWITCH DOUG DC9 DC931 3022065 WP NLG INOPERATIVE A CALA O OTHER N FALSE WARNING AP APPROACH 1 SW 09 14564 47490 FLT NR 1819 - IAH - THE AIRCRAFT HAD A BRIEF HISTORY OF THE NLG GREEN LIGHT NOT ILLUMINATING WHEN GEAR WAS EXTENDED FOR LANDING. CYCLING THE GEAR CAUSED THE LIGHT TO COME ON. THE NOSE GEAR DOWNLOCK SWITCH WAS REWIRED FROM S3-49 TO P1-133 PER WIRING DIAGRAM 32-61-00. IN ADDITION, THE P1-133 CANNON PLUG WAS REMOVED AND REPLACED. A GEAR SWING WAS PERFORMED WITH NOSE GEAR INDICATION AND OPERATION CHECKING GOOD. (M) 2 L 7 2 4F A6WE 1996032200747 19960322 00747 NM 1996 3 22 CAL960202 1 19960226 A 2450 T521 BUS PROTECT PNL BOEING 727 727227 1384078 NM AC PWR DISTR INOPERATIVE A CALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 09 73751 23047 21247 FLT NR 1957 - IAH - ALL THREE BUS TIE BREAKERS TRIPPED AND THE SECOND OFFICERS FAULT ANNUNCIATOR INDICATED A PHASE UNBAL ANCE WHILE EN ROUTE TO IAH. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE BUS PROTECTION PANEL AT FAULT. THE BUS PROTECTION PANEL WAS REMOVED AND REPLACED. THE ENGINES WERE RUN AND OPERATION CHECKED NORMAL. (M) 2 L 7 3 4F A3WE 1996032200748 19960322 00748 WP 1996 3 22 CAL960204 1 19960205 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 1463 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14839 26586 49635 HOU - INSPECTION FOUND TWO .375 INCH CRACKS IN LEFT FUSELAGE TO VERTICAL STABILIZER ATTACH ANGLE AT STATION 1463. THE C RACKED AREA WAS CUT OUT AND REPAIR DOUBLERS WERE INSTALLED IAW SRM 53-05, FIGURE 23. (M) 2 L 7 2 4F A6WE 1996032200749 19960322 00749 WP 1996 3 22 CAL960205 1 19960213 A 5210 591008111 ANGLE DOUG DC9 DC982 3022082 WP PAX DOOR BENT A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14839 26586 49635 HOU - INSPECTION FOUND THE FORWARD LOWER EDGE OF MAIN CABIN DOOR OUTER SKIN BENT AND THE LOWER SUPPORT ANGLE WAS ALSO BE NT. A NEW LOWER SUPPORT ANGLE WAS INSTALLED AND THE OUTER SKIN WAS STRAIGHTENED IAW SRM 52-01, FIGURE 1. (M) 2 L 7 2 4F A6WE 1996032200750 19960322 00750 WP 1996 3 22 CAL960207 1 19960227 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG LOW PRESSURE A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 16815 49113 FLT NR 455 - DEN - THE LANDING GEAR WOULD NOT RETRACT AND THE AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF FROM DEN. THE AIRCRAFT WAS RETURNED TO DEN WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE SERVICED THE NOSE GEAR STRUT IAW MM 32-21-0 2. THE GEAR WAS SWUNG SEVERAL TIMES WITH OPERATION CHECKING GOOD. (M) 2 L 7 2 4F A6WE 1996032200751 19960322 00751 WP 1996 3 22 CAL960209 1 19960215 A 5512 SKIN DOUG DC9 DC982 3022082 WP RT HORIZ STAB GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14839 26586 49635 HOU - INSPECTION FOUND MINOR GOUGES ON RIGHT HORIZONTAL STABILIZER SKIN AT STATION XS 142. THE GOUGES WERE REMOVED BY B URNISHING OUT IAW SRM 55-01, FIGURE 1, PAGE 3. (M) 2 L 7 2 4F A6WE 1996032200752 19960322 00752 WP 1996 3 22 CAL960210 1 19960206 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 237 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14839 26586 49635 HOU - INSPECTION FOUND A DENT IN SKIN WITH DAMAGE TO FORMER AT STATION 237 BETWEEN LONGERON 17L AND 16L. THE SKIN AND F ORMER WERE REPLACED IAW EC 5330-02163. (M) 2 L 7 2 4F A6WE 1996032200753 19960322 00753 WP 1996 3 22 CAL960211 1 19960216 A 5230 DOOR PAN DOUG DC9 DC982 3022082 WP AFT CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14839 26586 49635 HOU - INSPECTION FOUND A 2 INCH CRACK UNDER FORWARD LATCH MECHANISM OF AFT CARGO DOOR PAN. A DOUBLER WAS INSTALLED IAW SRM 52-05. (M) 2 L 7 2 4F A6WE 1996032200754 19960322 00754 WP 1996 3 22 CAL960212 1 19960227 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 1155-1211 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14839 26586 49635 HOU - INSPECTION FOUND CORROSION IN Z-ANGLE ACROSS BOTTOM OF AFT BAGGAGE BIN DOOR OPENING AT STATION 1155 TO 1211. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5. (M) 2 L 7 2 4F A6WE 1996032200755 19960322 00755 WP 1996 3 22 CAL960213 1 19960202 A 5320 3936409507 BRACKET DOUG DC9 DC982 3022082 WP BS 886 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14839 26586 49635 HOU - INSPECTION FOUND A 1.125 INCH CRACK IN FUSELAGE BELLY PANEL 'T' BRACKET AT STATION 886 AIRCRAFT CENTERLINE. A NEW 'T' BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-30-3. (M) 2 L 7 2 4F A6WE 1996032200756 19960322 00756 WP 1996 3 22 CAL960214 1 19960207 A 5753 TE SKIN DOUG DC9 DC982 3022082 WP RT TE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14839 26586 49635 HOU - INSPECTION FOUND A 7.5 INCH CRACK IN FIBERGLASS SECTION OF RIGHT WING INBOARD FLAP OUTBOARD TRAILING EDGE. A NEW SECTION OF TRAILING EDGE FLAP WAS INSTALLED IAW SRM 57-03, FIGURE 9. (M) 2 L 7 2 4F A6WE 1996032200758 19960322 00758 WP 1996 3 22 CAL960216 1 19960128 A 5313 AEA71321 LONGERON DOUG DC10 DC1030 3023501 WP BS 1436 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13067 77547 47866 KUL - INSPECTION FOUND LONGERON 30L CORRODED AT STATION 1436. THE LONGERON WAS REPAIRED IAW ECRA 5310-03218 AND SRM 53- 14-01. (M) 2 L 7 3 4F A22WE 1996032200759 19960322 00759 WP 1996 3 22 CAL960217 1 19960128 A 5313 LONGERON DOUG DC10 DC1030 3023501 WP BS 1405 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13067 77547 47866 KUL - INSPECTION FOUND CORROSION ON LONGERON 31L AT STATION 1405. THE CORROSION WAS REMOVED AND A DOUBLE ANGLE REPAIR W AS INSTALLED IAW ECRA 5310-03217 AND SRM 53-14-01. (M) 2 L 7 3 4F A22WE 1996032200760 19960322 00760 WP 1996 3 22 CAL960218 1 19960126 A 5230 DOOR FRAME DOUG DC10 DC1030 3023501 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13067 77547 47866 KUL - INSPECTION FOUND TWO EACH 4 INCH CRACKS ON CENTER CARGO DOOR OUTER FRAME BY FORWARD LOWER STRIKER PLATE. THE CRAC KS WERE REPAIRED IAW SRM 52-10-00, FIGURE 3. (M) 2 L 7 3 4F A22WE 1996032200761 19960322 00761 WP 1996 3 22 CAL960219 1 19960126 A 5320 STIFFENER DOUG DC10 DC1030 3023501 WP FS 1841 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13067 77547 47866 KUL - INSPECTION FOUND LATERAL STIFFENER CORRODED AT FS 1841 RBL 42 AND LBL 28. THE LATERAL STIFFENERS WERE REPLACED IA W SRM 53-16-01. (M) 2 L 7 3 4F A22WE 1996032200767 19960322 00767 WP 1996 3 22 CAL960225 1 19960131 A 5320 INTERCOSTAL DOUG DC10 DC1030 3023501 WP BS 464 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13066 75223 46591 KUL - INSPECTION FOUND INTERCOSTAL CORRODED AT LOWER FUSELAGE FORWARD SECTION STATION 464R. THE INTERCOSTAL WAS REPLACE D IAW SRM 53-11-01, FIGURE 5. (M) 2 L 7 3 4F A22WE 1996032200768 19960322 00768 WP 1996 3 22 CAL960226 1 19960131 A 5320 INTERCOSTAL DOUG DC10 DC1030 3023501 WP BS 470 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13066 75223 46591 KUL - INSPECTION FOUND INTERCOSTAL CORRODED ON LEFT SIDE OF AVIONICS COMPARTMENT AT STATION 470, STRINGER 48L. THE INTE RCOSTAL WAS REPLACED IAW SRM 53-11-01, FIGURE 5. (M) 2 L 7 3 4F A22WE 1996032200769 19960322 00769 WP 1996 3 22 CAL960227 1 19960117 A 5320 AGA70821 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1871 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13066 75223 46591 KUL - INSPECTION FOUND LAV 'E' OUTBOARD SUPPORT CORRODED AT STATION 1871. THE SUPPORT WAS REPAIRED IAW SRM 53-70-00, FI GURE 13. (M) 2 L 7 3 4F A22WE 1996032200770 19960322 00770 WP 1996 3 22 CAL960228 1 19960130 A 5320 AGA7086503 SUPPORT DOUG DC10 DC1030 3023501 WP GALLEY 'G' CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13066 75223 46591 KUL - INSPECTION FOUND A GALLEY 'G' SUPPORT CORRODED. THE SUPPORT WAS REPLACED IAW SRM 53-70-00, FIGURE 13. (M) 2 L 7 3 4F A22WE 1996032200771 19960322 00771 WP 1996 3 22 CAL960229 1 19960118 A 5320 AGA70821 SUPPORT DOUG DC10 DC1030 3023501 WP GALLEY 7 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13066 75223 46591 KUL - INSPECTION FOUND GALLEY 7 INBOARD SUPPORT CORRODED. THE SUPPORT WAS REPAIRED IAW SRM 53-70-00, FIGURE 13. (M) 2 L 7 3 4F A22WE 1996032200772 19960322 00772 CE 1996 3 22 GLBA96006 1 19960209 A 3233 11438004111 ACTUATOR BEECH 1900 1900D 1154162 CE LT MLG FAILED A GLBA O OTHER J WARNING INDICATION AP APPROACH 1 CE 01 118UX 3671 UE118 LEFT MAIN LANDING GEAR FAILED TO EXTEND AND CB POPPED. CIRCUIT BREAKER WAS RESET AND GEAR EXTENDED. AIRCRAFT WAS FERRI ED TO MX STATION. LEFT MLG ACTUATOR WAS CHANGED AND GEAR SWINGS COMPLETED. RII ITEM COMPLIED WITH. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1996032200773 19960322 00773 SO 1996 3 22 GLBA96011 1 19960220 A 2720 CONTROLS EMB 120 EMB120RT SO RUDDER MALFUNCTIONED A GLBA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CE 01 129AM 120119 RDU - SHORTLY FOLLOWING TAKEOFF, THE CREW REPORTED AN UNCOMMANDED FULL RIGHT RUDDER INPUT LASTING 2 TO 3 SECONDS. THIS INPUT COULD NOT BE OVERRIDDEN. THE CREW ELECTED AN AIR TURN BACK WHICH WAS FOLLOWED BY AN UNEVENTFUL LANDING. AIRCRAFT IS ON THE GROUND FOR REPAIRS. (M) 2 L 7 2 4T RT A31SO 1996032200774 19960322 00774 1996 3 22 GLBA96014 4 19960122 A 6122 3036817A PROP GOVERNOR BEECH 1900 1900C 1154161 CE RT ENGINE MALFUNCTIONED A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 01 84GL 9839 UC84 GRI - THE CREW REPORTED THAT THE RIGHT PROP RPM COMES BACK TO 1500 AFTER TAKEOFF. THEY ELECTED AN AIR TURN BACK AND MAD E AN UNEVENTRUL LANDING. MAINTENANCE REMOVED AND REPLACED THE RIGHT PRIMARY PROP GOVERNOR. OPS CHECK WAS GOOD. (M) 2 L 7 2 4T RT A24CE 1996032200775 19960322 00775 CE 1996 3 22 GLBA96016 1 19960123 A 3244 11480081 TIRE BEECH 1900 1900D 1154162 CE NR 3 FAILED A GLBA O OTHER O OTHER LD LANDING 1 CE 01 97UX 1780 UE97 FSD - CREW REPORTED NR 3 TIRE BLEW ON LANDING DUE TO FROZEN BRAKE. MAINTENANCE REMOVED AND REPLACED TIRE AND WHEEL ASSY AND THAWED BRAKE. (M) 2 L 7 2 4T RT A24CE 1996032200776 19960322 00776 CE 1996 3 22 GLBA96017 1 19960123 A 3260 UPLOCK SWITCH BEECH 1900 1900C 1154161 CE LANDING GEAR FROZEN A GLBA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 01 96UE UC96 ESC - CREW REPORTED, THE GEAR HANDLE LIGHT REMAINED ILLUMINATED AFTER GEAR WAS SELECTED UP. CREW ELECTED AN AIR TURN BA CK FOLLOWED BY AN UNEVENTFUL LANDING. MAINTENANCE THAWED ICE FROM GEAR UPLOCK SWITCHES. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4T RT A24CE 1996032200777 19960322 00777 EA 1996 3 22 GLBA96018 2 19960123 A 7314 1143890423 FUEL PUMP BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA RT ENGINE FAILED A GLBA O OTHER J WARNING INDICATION CR CRUISE 1 CE 01 126UE 11834 5498 UC126 32379 GFK - CREW REPORTED RIGHT FUEL PRESS ANNUN ILLUMINATED IN FLIGHT. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE DRIVEN LOW PRESS PUMP. SYSTEM CHECKS GOOD. (M) 2 L 7 2 4T 4 T RT A24CE E4EA 1996032200778 19960322 00778 CE 1996 3 22 GLBA96020 1 19960124 A 3260 327 BULB BEECH 1900 1900C 1154161 CE LT MLG FAILED A GLBA O OTHER P NO WARNING INDICATION TX TAXI/GRND HDL 1 CE 01 89UE UC89 CREW REPORTED LEFT GREEN LANDING GEAR DOWN AND LOCKED ANNUNCIATOR DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED BULB. SYSTEM CHECKS OK. (M) 2 L 7 2 4T RT A24CE 1996032200779 19960322 00779 CE 1996 3 22 GLBA96021 1 19960124 A 3240 MS28775112 O-RING SEAL BEECH 1900 1900C 1154161 CE LT BRAKES LEAKING A GLBA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 01 89UE UC89 MKE - CREW REPORTED BRAKES WERE INEFFECTIVE. MAINTENANCE REPLACED LEAKING O-RING SEALS ON LEFT BRAKES AND BLED SYSTEM. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A24CE 1996032200780 19960322 00780 CE 1996 3 22 GLBA96022 1 19960124 A 3260 DNLOCK SWITCH BEECH 1900 1900C 1154161 CE NLG OUT OF ADJUST A GLBA O OTHER N FALSE WARNING TO TAKEOFF 1 CE 01 123UE UC123 ORD - CREW REPORTED LDG GEAR ANNUNCIATES WITH GEAR DOWN AND LOCKED. MAINTENANCE ADJUSTED NLG DOWNLOCK SWITCH. OPS CHEC K GOOD. (M) 2 L 7 2 4T RT A24CE 1996032200781 19960322 00781 CE 1996 3 22 GLBA96023 1 19960124 A 3260 LIGHT SOCKET BEECH 1900 1900C 1154161 CE COCKPIT LOOSE A GLBA O OTHER P NO WARNING INDICATION LD LANDING 1 CE 01 41UE UC41 ABQ - CREW REPORTED THAT THE GREEN DOWN AND LOCKED LOG ANNUNCIATOR DID NOT ILLUMINATE WHEN GEAR WAS EXTENDED. FOLLOWING AN UNEVENTFUL LANDING. MAINTENANCE REPAIRED ANNUNCIATOR LIGHT SOCKET. SYSTEM CHECKS OK. (M) 2 L 7 2 4T RT A24CE 1996032200782 19960322 00782 NE 1996 3 22 GLBA96024 2 19960127 A 7324 3033960 FLOW DIVIDER EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE LEAKING A GLBA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 CE 01 267UE 243 120071 115377 ORD - CREW REPORTED AND EXCESSIVE FUEL FLOW INDICATION WITH LEFT ENGINE RUNNING AND FUEL LEAK AT LEFT ENGINE. MAINTENAN CE REPLACED LEFT FLOW DIVIDER. LEAK CHECK AND OPS CHECK GOOD. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1996032200783 19960322 00783 CE 1996 3 22 GLBA96025 1 19960127 A 3234 GEAR SELECTOR BEECH 1900 1900C 1154161 CE COCKPIT LOOSE WIRES A GLBA O OTHER N FALSE WARNING TO TAKEOFF 1 CE 01 105GL UC105 ORD - CREW REPORTED NLG DOWN ANNUNCIATOR ILLUMINATED WITH GEAR SELECTED UP AND POWER LEVERS PULLED BACK. MAINTENANCE RE PAIRED LOOSE WIRES AT GEAR HANDLE AND CHAFED WIRE AT TB150. OPS GOOD. (M) 2 L 7 2 4T RT A24CE 1996032200784 19960322 00784 CE 1996 3 22 GLBA96026 1 19960130 A 3230 1143640681 CIRCUIT BOARD BEECH 1900 1900C 1154161 CE LANDING GEAR FAILED A GLBA O OTHER J WARNING INDICATION LD LANDING 1 CE 01 123UE UC123 MSP - CREW REPORTED GEAR WOULD NOT EXTEND WHEN SELECTED DOWN. CREW EXTENDED GEAR MANUALLY AND MADE AN UNEVENTFUL LANDIN G. MAINTENANCE REMOVED AND REPLACED TIME DELAY PCB. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4T RT A24CE 1996032200785 19960322 00785 CE 1996 3 22 GLBA96027 1 19960131 A 3260 WARNING SYSTEM BEECH 1900 1900C 1154161 CE LANDING GEAR MALFUNCTIONED A GLBA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 CE 01 122GL UC122 OSH - CREW REPORTED THAT THE GEAR INTRANSIT LIGHT AND HORN WOULD NOT EXTINGUISH WHEN GEAR SELECTED UP. CREW ELECTED TO DO AN AIR TURN BACK AND MADE AN UNEVENTFUL LANDING. MAINTENANCE JACKED AIRCRAFT AND PEFORMED FOUR COMPLETE GEAR SWING C YCLES. SYSTEM OPS CHECKED GOOD. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A24CE 1996032200786 19960322 00786 CE 1996 3 22 GLBA96038 1 19960124 A 6120 PROP GOVERNOR BEECH 1900 1900C 1154161 CE LT PROP MALFUNCTIONED A GLBA O OTHER O OTHER CR CRUISE 1 CE 01 141UE UC141 MIE - CREW REPORTED, THE LEFT PROP WENT TO GROUND IDLE IN FLIGHT. MAINTENANCE PERFORMED GROUND RUN BUT COULD NOT DUPLIC ATE PROBLEM DURING OPS CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1996032200787 19960322 00787 WP 1996 3 22 GRAA9612 1 19960221 A 3350 079123 LENS DOUG DC9 DC987 3022087 WP CABIN MISSING A GRAA K NONE O OTHER IN INSP/MAINT 1 WP 11 1074T 49727 LINE MAINTENANCE AT RNO, DISCOVERED THAT THE EMERGENCY FLOOR LIGHTS WAS MISSING 1 EACH RED FLOOR TRACK LENS ASSEMBLY AT THE OVERWING EXITS. MAINTENANCE REPLACED THE MISSING RED LENS. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE EMERG ENCY LIGHT SYSTEM. OPERATIONALLY CHECKED NORMAL. AIRCRAFT CHECKED NORMAL. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SER VICE. (M) 2 L 7 2 4F RT A6WE 1996032200788 19960322 00788 WP 1996 3 22 GRAA9613 1 19960229 A 3350 079123 LENS DOUG DC9 DC987 3022087 WP CABIN MISSING A GRAA K NONE O OTHER IN INSP/MAINT 1 WP 11 1074T 49727 RNO - LINE MAINTENANCE DISCOVERED AT ROW 18, ONE EACH EMERGENCY FLOOR TRACK LIGHTING RED LENS WAS MISSING. MAINTENANCE REPLACED THE LENS. AN OPERATIONAL CHECK WAS PERFORMED ON THE EMERGENCY FLOOR TRACK LIGHTING SYSTEM. THE EMERGENCY FLOO R TRACK LIGHTING SYSTEM CHECKED NORMAL. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A6WE 1996032200789 19960322 00789 EA 1996 3 22 HNAA9690513 1 19960220 A 3233 154009 ACTUATOR DHAV DHC7 DHC7102 2802708 EA LT MLG FAILED A HNAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 07 905HA 32329 MC152 070 FLT NR 3186 - DCA-ORF - ON APPROACH INTO ORF, THE LEFT MAIN GEAR WOULD NOT EXTEND WHEN SELECTED DOWN. ONCE NOSE AND RIG HT MAIN LOCKED, LEFT MAIN STARTED DOWN AND LOCKED INTO PLACE. THE AIRCRAFT LANDED IN ORF WITHOUT INCIDENT. RETORQUED L OCK STRUT FITTING AND REMOVED AND REPLACED THE NR 1 MAIN LANDING GEAR RETRACTION ACTUATOR. (M) 2 H 7 4 4T A20EA 1996032200790 19960322 00790 NM 1996 3 22 IXKA960007 1 19960226 A 2612 1050800317510 FIRE SENSOR BOEING 727 727251 138408H NM NR 3 ENG SHORTED A IXKA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 25 258US 19977 DEPARTING PBI, FIRE WARNING INDICATION ON NR 3 ENGINE DURING CLIMB-OUT. FOLLOWED CHECK LIST AND DISCHARGED BOTH FIRE BO TTLES. DUMPED FUEL AND RETURNED TO PBI. REPLACED FIRE LOOP AND BOTTLES. NR 3 ENGINE FIRE WARNING LIGHT ON DURING CLIM B-OUT AGAIN. RETURNED TO PBI. REMOVED AND REPLACED BOTH FIRE BOTTLES LEFT AND RIGHT NR 3 ENGINE FIRE LOOP, PER MM 26-1 1-00, FIRST TIME. AFTER SECOND ATB, REPLACED 2 PINS ON C/P D1498. OPS CHECK OK PER MM 26-11-01. REPAIRED FIRE WALL DE TECTION HARNESS INSIDE NR 3 PYLON AND REPLACED FIRE WALL SENSOR AND OPS CHECK OK AS PER 26-11-01 AND MM 26-11-00. (M) 2 L 7 3 4F A3WE 1996032200791 19960322 00791 SW 1996 3 22 MALA964875 1 19960219 A 3230 1EN516 UPLIMIT SW SWRNGN SA227 SA227AC 8780603 SW NLG OUT OF ADJUST A MALA O OTHER J WARNING INDICATION CR CRUISE 1 GL 15 27465 AC755B DURING A MAINTENANCE TEST FLIGHT IN MSP, THE NOSE GEAR BEGAN TO CYCLE IN THE GEAR WELL AND THE RED INTRANSIT LIGHT ILLUM INATED. THE AIRCRAFT LANDED IN MSP WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED THE NOSE GEAR UPLIMIT POSITION SWITC HES. SYSTEM OPERATED SATISFACTORILY. (M) 1 L 7 2 4T A8SW 1996032200792 19960322 00792 SW 1996 3 22 MALA964876 1 19960218 A 5210 2724044012 FRAME CORNER SWRNGN SA227 SA227AC 8780603 SW PAX DOOR CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 27465 AC755B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE LOWER FORWARD PASSENGER DOOR FRAME CORN ER. THEY REPLACED THE CORNER IAW FAC SRM 51-40-01 AND 02. (M) 1 L 7 2 4T A8SW 1996032200793 19960322 00793 SW 1996 3 22 MALA964877 1 19960218 A 5311 FRAME SWRNGN SA227 SA227AC 8780603 SW FS 347.271 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 27465 AC755B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE LOWER RIGHT BELT FRAME AT FS 347.271. T HEY STOP DRILLED THE CRACK AND FABRICATED AND INSTALLED A DOUBLER IAW FAC SRM 53-90-20. (M) 1 L 7 2 4T A8SW 1996032200794 19960322 00794 SW 1996 3 22 MALA964878 1 19960218 A 5311 FRAME SWRNGN SA227 SA227AC 8780603 SW FS 227 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 27465 AC755B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE LOWER LEFT BELT FRAME AT FS 227. THEY STOP DRILLED THE CRACK AND FABRICATED AND INSTALLED A REPAIR DOUBLER IAW FAC SRM 53-90-20. (M) 1 L 7 2 4T A8SW 1996032200795 19960322 00795 SW 1996 3 22 MALA964879 1 19960218 A 5311 FRAME SWRNGN SA227 SA227AC 8780603 SW FS 212 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 27465 AC755B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE LOWER RIGHT BELT FRAME AT FS 212. THEY STOP DRILLED THE CRACK AND FABRICATED AND INSTALLED A REPAIR DOUBLER IAW FAC SRM 53-90-20. (M) 1 L 7 2 4T A8SW 1996032200796 19960322 00796 SW 1996 3 22 MALA964880 1 19960218 A 5311 FRAME SWRNGN SA227 SA227AC 8780603 SW FS 212 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 27465 AC755B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE LOWER LEFT BELT FRAME AT FS 212. THEY STOP DRILLED THE CRACK AND FABRICATED AND INSTALLED A REPAIR DOUBLER IAW FAC SRM 53-90-20. (M) 1 L 7 2 4T A8SW 1996032200797 19960322 00797 SW 1996 3 22 MALA964881 1 19960218 A 5311 FRAME SWRNGN SA227 SA227AC 8780603 SW FS 197.27 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 27465 AC755B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE LOWER LEFT BELT FRAME FLANGE AT FS 197. 27. THEY STOP DRILLED THE CRACK AND FABRICATED AND INSTALLED A REPAIR DOUBLER IAW FAC SRM 53-90-20. (M) 1 L 7 2 4T A8SW 1996032200798 19960322 00798 SW 1996 3 22 MALA964882 1 19960218 A 5311 FRAME SWRNGN SA227 SA227AC 8780603 SW FS 189 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 27465 AC755B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE LOWER LEFT BELT FRAME FLANGE AT FS 189. THEY STOP DRILLED THE CRACK AND FABRICATED AND INSTALLED A REPAIR DOUBLER IAW FAC SRM 53-90-20. (M) 1 L 7 2 4T A8SW 1996032200799 19960322 00799 SW 1996 3 22 MALA964883 1 19960218 A 5311 FRAME SWRNGN SA227 SA227AC 8780603 SW FS 174.06 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 27465 AC755B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE LOWER BELT FRAME AT FS 174.06. THEY ST OP DRILLED THE CRACK AND FABRICATED AND INSTALLED A REPAIR DOUBLER IAW FAC SRM 53-90-20. (M) 1 L 7 2 4T A8SW 1996032200800 19960322 00800 SW 1996 3 22 MALA964884 1 19960218 A 5330 SKIN SWRNGN SA227 SA227AC 8780603 SW FS 438.06 DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 27465 AC755B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A DENT IN THE FUSELAGE SKIN AT FS 438.06 AND WL 75.13. THEY FABRICATED AND INSTALLED AN EXTERNAL DOUBLER IAW 53-90-20. (M) 1 L 7 2 4T A8SW 1996032200801 19960322 00801 SW 1996 3 22 MALA964886 1 19960220 A 7712 310703411 TQ RING SWRNGN SA227 SA227AC 8780603 SW LT ENGINE FAILED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 445MA AC687 FLT NR 3334 - ON CLIMB-OUT FROM DTW, THE NR 1 TORQUE GAUGE BEGAN TO FLUCTUATE BETWEEN ZERO AND 120 PERCENT. ALL OTHER E NGINE INDICATORS WERE NORMAL. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE LEFT TORQUE RING. SYSTEM OPERATE D SATISFACTORILY. (M) 1 L 7 2 4T A8SW 1996032200802 19960322 00802 SW 1996 3 22 MALA964887 1 19960222 A 7712 31024766N TQ SIGNAL COND SWRNGN SA227 SA227AC 8780603 SW LT ENGINE FAILED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 445MA AC687 FLT NR 3416 - ON CLIMB-OUT FROM DTW, THE LEFT ENGINES TORQUE INDICATION BEGAN TO FLUCTUATE AND THEN FAILED. THE AIRCRAF T RETURNED TO DTW. MAINTENANCE REPLACED THE NR 1 TORQUE SIGNAL CONDITIONER. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2 L 7 2 4T RT A8SW 1996032200803 19960322 00803 SW 1996 3 22 MALA964888 1 19960223 A 3230 RETRACT MECH SWRNGN SA227 SA227AC 8780603 SW LANDING GEAR MALFUNCTIONED A MALA K NONE J WARNING INDICATION AP APPROACH 1 GL 15 60NE AC760B FLT NR 3370 - ON APPROACH TO DTW, THE NOSE GEAR INTRANSIT LIGHT WAS SLOW TO EXTINGUISH. THE PILOT ALSO REPORTED THAT, W HEN GEAR DID COME DOWN, IT CAME DOWN HARD. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. ALL CHECKS WERE SATISF ACTORY. (M) 1 L 7 2 4T A8SW 1996032200804 19960322 00804 SW 1996 3 22 MALA964889 1 19960223 A 3260 INTRANSIT LIGHT SWRNGN SA227 SA227AC 8780603 SW LANDING GEAR MALFUNCTIONED A MALA K NONE N FALSE WARNING CL CLIMB 1 GL 15 424MA AC639 FLT NR 3069 - ON CLIMB-OUT FROM CVG, THE GEAR INTRANSIT LIGHTS REMAINED ON AFTER GEAR RETRACTION. THE CREW CYCLED THE G EAR AND ALL INDICATIONS WERE NORMAL. THE AIRCRAFT CONTINUED TO DTW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE WA S UNABLE TO DUPLICATE THE DISCREPANCY. (M) 1 L 7 2 4T A8SW 1996032200805 19960322 00805 WP 1996 3 22 ORJA96005 1 19960214 A 3350 POWER SUPPLY 60030431 DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 840RA 2249 49424 AFT MOST EMERGENCY POWER SUPPLY RIGHT GALLEY HAS NO POWER OUTPUT PIN 5. INSTALLED NEW POWER SUPPLY, NEW OUTPUT 2.47 VOC . (M) 2 L 7 2 4F A6WE 1996032200806 19960322 00806 EU 1996 3 22 PLG21296J1 2 19960212 A 7250 BEARING SAAB SF340 340B 7860101 EU NR 2 ENGINE SPALLED A PLGA K NONE O OTHER AP APPROACH 1 NE 05 350BE 5963 1432 340B197 DURING LANDING APPROACH, CREW OBSERVED A NR 2 ENGINE CHIP LIGHT ILLUMINATION. FOLLOWING REPLACEMENT, THE POWERPLANT WAS DIRECTED TO A REPAIR FACILITY. UPON TEARDOWN THE SOURCE OF CHIPS WAS CONFIRMED TO BE SPALLED NR 4 AND AXIS B-B. (M) 2 L 7 2 4T RT A52EU 1996032200807 19960322 00807 EU 1996 3 22 RAIA960217 1 19960214 A 7722 31039201 THERMOCOUPLE BAG JETSTM JETSTM3201 1500217 EU RT ENG FAILED A RAIA O OTHER O OTHER CL CLIMB 1 CE 03 864AE 8048 864 FAT - FLT NR 4750 - RIGHT EGT FLUCTUATES. MAINTENANCE REPLACED RIGHT ENGINE THERMOCOUPLE RAKE, GROUND GOOD. (M) 2 L 7 2 4T RT A56EU 1996032200808 19960322 00808 EU 1996 3 22 RAIA960218 1 19960215 A 7722 EGT CONNECTOR BAG JETSTM JETSTM3201 1500217 EU RT ENG LOOSE A RAIA O OTHER O OTHER CL CLIMB 1 CE 03 864AE 864 FAT - FLT 4750 - RIGHT EGT FLUCUATES. MAINTENANCE SECURED LOOSE CONNECTION ON SHORT LEAD. GROUND RUNS GOOD. (M) 2 L 7 2 4T RT A56EU 1996032200809 19960322 00809 EU 1996 3 22 RAIA960219 1 19960216 A 7603 8691641 LEVER BAG JETSTM JETSTM3201 1500217 EU LT ENG LOOSE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 341TE 7606 950 STL - FLT NR 7332 - LEFT RPM STUCK AT 72 PERCENT REGARDLESS OF RPM OR POWER LEVER POSITION. MAINTENANCE SECURED LEFT EN GINE SPEED LEVER ARM TO USG SPLINE, GROUND RUNS GOOD. (M) 2 L 7 2 4T RT A56EU 1996032200810 19960322 00810 WP 1996 3 22 RAIA960220 2 19960215 A 7310 893083 MANUAL FUEL VLV BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT ENGINE LOOSE A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 426AM 9111 874 66176 STL - FLT NR 7034 - ON POWER UP FOR TAKEOFF, LEFT POWER LEVER FAILED TO GIVE ANY POWER INDICATION. MAINTENANCE SECURED MANUAL FUEL VALVE ARM TO MANUAL FUEL VALVE, GROUND RUNS GOOD. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996032200811 19960322 00811 EU 1996 3 22 RAIA960222 1 19960217 A 2932 NTA152504 GASKET AEROSP ATR42 ATR42300 8680920 EU GREEN HYD SYSTEM LEAKING A RAIA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CE 03 424TE 15949 124 STL - FLT NR 7524 - GREEN SYSTEM LOW LEVEL LIGHT CAME ON IN FLIGHT. MAINTENANCE REPLACED GREEN SYSTEM PRESSURE TRANSMIT TER GASKET. OPERATIONAL AND LEAK CHECKS GOOD. (M) 2 H 7 2 4T RT A53EU 1996032200812 19960322 00812 EU 1996 3 22 RAIA960223 1 19960217 A 7714 AG34 TACH GENERATOR BAG JETSTM JETSTM3201 1500217 EU RT ENG FAILED A RAIA O OTHER O OTHER CR CRUISE 1 CE 03 428AM 6065 4382 877 STL - FLT NR 7031 - RIGHT RPM INDICATOR FAILED IN FLIGHT. MAINTENANCE REPLACED RIGHT TACH GENERATOR PERFORMED GROUND RU NS OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A56EU 1996032200813 19960322 00813 EU 1996 3 22 RAIA960226 1 19960219 A 7722 8972052 EGT COMPENSATOR BAG JETSTM JETSTM3201 1500217 EU LT ENG OUT OF ADJUST A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 433AM 10270 885 STL - FLT NR 7456 - LEFT ENGINE TORQUE DROPPED TO 80 PERCENT ON TAKEOFF. MAINTENANCE DEFERRED SRL AND TTL SYSTEMS, DMI 76-1 AND 76-2. MAINTENANCE LATER CLEARED BOTH DMI'S BY CALIBRATING EGT COMPENSATOR. (M) 2 L 7 2 4T RT A56EU 1996032200814 19960322 00814 EU 1996 3 22 RAIA960227 1 19960219 A 2750 5148YMK83 FLAP HANDLE BAG JETSTM JETSTM3201 1500217 EU CENTER PEDESTAL FAILED A RAIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 CE 03 424AM 9164 865 STL - FLT NR 7334 - FLAPS STUCK AT 10 DEGREES WOULD NOT RETRACT AFTER TAKEOFF. MAINTENANCE REPLACED FLAP CONTROL HANDLE OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A56EU 1996032200815 19960322 00815 EU 1996 3 22 RAIA960228 1 19960219 A 3260 INDICATION BAG JETSTM JETSTM3201 1500217 EU LANDING GEAR MALFUNCTIONED A RAIA O OTHER N FALSE WARNING CL CLIMB 1 CE 03 866AE 866 SMF - FLT NR 4718 - LEFT GEAR DID NOT INDICATE UP AND LOCKED. MAINTENANCE INSPECTED SYSTEM AND PERFORMED GEAR SWING, NO DEFECTS NOTED. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A56EU 1996032200816 19960322 00816 1996 3 22 RAIA960229 4 19960219 A 3414 AIRSPEED IND BAG JETSTM JETSTM3201 1500217 EU LEFT MALFUNCTIONED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 343TE 955 BRL - FLT NR 7051 - CAPTAINS AIRSPEED INDICATOR STUCK AT 90 KNOTS ON TAKEOFF. AIRCRAFT RELEASED FOR FERRY FLIGHT TO STL . CREW REPORTED PROPER OPERATION OF SYSTEM DURING FERRY FLIGHT. MAINTENANCE PERFORMED OPERATION CHECK, NO DEFECTS NOTE D. (M) 2 L 7 2 4T RT A56EU 1996032200817 19960322 00817 WP 1996 3 22 RAIA960230 2 19960220 A 7320 89778025 FUEL CONTROL BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT ENG OUT OF ADJUST A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 432AM 11039 883 66322 STL - FLT NR 7410 - LEFT RPM DID NOT REACH 100 PERCENT RPM, ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE ADJUSTED RPM PERFORMED GROUND RUNS, OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996032200818 19960322 00818 EU 1996 3 22 RAIA960231 1 19960221 A 3010 32P15822 DE-ICE BOOT AEROSP ATR42 ATR42300 8680920 EU RT WING WORN A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 421TE 2884 102 STL - FLT NR 7176 - AIRFRAME DE-ICE FAULTED IN FLIGHT, RETURNED TO STL WITHOUT INCIDENT. MAINTENANCE PATCHED HOLES IN R IGHT WING DE-ICE BOOT, OPERATIONAL CHECK GOOD DURING GROUND RUNS. (M) 2 H 7 2 4T RT A53EU 1996032200819 19960322 00819 EU 1996 3 22 RAIA960232 1 19960221 A 2435 23095009 STARTER GEN BAG JETSTM JETSTM3201 1500217 EU NR 1 ENG FAILED A RAIA D RETURN TO BLOCK E H VIBRATION/BUFFET ELECT. POWER LOSS-50 PC CL CLIMB 1 CE 03 343TE 485 955 STL - FLT NR 7050 - HIGH FREQUENCY VIBRATION ON NR 1 ENGINE. MAINTENANCE REPLACED NR 1 STARTER GENERATOR AND SPLINE ADA PTER GROUND RUN GOOD. (M) 2 L 7 2 4T RT A56EU 1996032200820 19960322 00820 EU 1996 3 22 RAIA960233 1 19960222 A 3260 9005EN38 DNLOCK SWITCH BAG JETSTM JETSTM3201 1500217 EU NLG OUT OF ADJUST A RAIA O OTHER N FALSE WARNING LD LANDING 1 CE 03 342TE 7580 954 JLN - FLT NR 7072 - LANDING GEAR CIRCUIT BREAKER POPS AND NO DOWN AND LOCKED INDICATION. MAINTENANCE ADJUSTED DOWNLOCK SWITCH, GEAR SWING CHECKS GOOD. (M) 2 L 7 2 4T RT A56EU 1996032200822 19960322 00822 NM 1996 3 22 TAOA029617 1 19960224 A 3350 0L3071BPEGPL BULB BOEING 727 727225 1384077 NM CABIN MISSING A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 918TS 20445 'E' PATH LIGHTING ROW 22, BULB AND LENS MISSING. REPLACED BULB AND LENS. OPERATIONAL CHECK OK. (M) 2 L 7 3 4F A3WE 1996032200823 19960322 00823 NM 1996 3 22 TAOA039601 1 19960302 A 3350 0L3071BPEGPL BULB BRUCE BOEING 727 727254 138408L NM CABIN MISSING A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 914TS 20251 'E' PATH LIGHTS INOP AT ROWS 10 AND 23. INSTALLED MISSING BULBS AT ROWS 10 AND 23. OPERATIONAL CHECK OK. (M) 2 L 7 3 4F A3WE 1996032200845 19960322 00845 NM 1996 3 22 USAA960106 1 19960224 A 5311 FRAME BOEING 737 737201 1384454 NM BS 360 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 243US 36817 22445 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 4 INCH CRACK IN CIRCUMFERENTIAL FRAME STATION 360 4 INCHES BELOW STRINGE R 19 R. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-3. (M) 2 L 7 2 4F A16WE 1996032200846 19960322 00846 NM 1996 3 22 USAA960116 1 19960224 A 5311 FRAME BOEING 737 737201 1384454 NM BS 328 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 243US 36817 22445 INT - DURING Q-6 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND .75 INCH CRACK ON CIRCUMFERENTIAL FRAME WEB STATION 328 4 INCHES BELOW STRINGER 20R. INSTALLED REPAIR DOUBLER, REPAIRED PER SRM 51-40-3. (M) 2 L 7 2 4F A16WE 1996032200847 19960322 00847 NM 1996 3 22 USAA960134 1 19960224 A 5320 6325037 WEB BOEING 737 737201 1384454 NM BS 639 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 243US 36817 22445 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK STATION 639 STUB BEAM WEB LBL 48 WL 206.5. INSTALLED WEB, REPAIRED PER BOEING DRAWING 65C25211. (M) 2 L 7 2 4F A16WE 1996032200848 19960322 00848 NM 1996 3 22 USAA960273 1 19960224 A 5330 SKIN BOEING 737 737201 1384454 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 243US 36817 22445 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK ON SKIN BS 380 BETWEEN STRINGER 28 L AND BL 0. INSTALLED D OUBLER, REPAIRED PER TR 53-30-04 AND EA 25454. (M) 2 L 7 2 4F A16WE 1996032200849 19960322 00849 NM 1996 3 22 USAA960274 1 19960224 A 5330 SKIN BOEING 737 737201 1384454 NM BS 1156 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 243US 36817 22445 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK IN FUSELAGE SKIN 1156 BULKHEAD STRINGER 2 L AND STRINGER 3 L. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1996032200850 19960322 00850 NM 1996 3 22 USAA960275 1 19960224 A 5320 1121128 INTERCOSTAL BOEING 737 737201 1384454 NM BS 270-294 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 243US 36817 22445 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 6 INCH CORROSION INTERCOSTAL, STATION 270 TO STATION 294 LBL 1 0 INCHES. INSTALLED NEW PREFAB INTERCOSTAL, REPAIRED PER BOEING DRAWING 65-45634. (M) 2 L 7 2 4F A16WE 1996032200851 19960322 00851 NM 1996 3 22 USAA960276 1 19960224 A 5320 65495648 CLIP BOEING 737 737201 1384454 NM BS 540 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 243US 36817 22445 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH CORRODED AREA AT STRINGER TIE CLIP BS 540 STRINGER 26 L. REPLACE D STRINGER TIE CLIP, REPAIRED PER SRM 53-10-1. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996032200852 19960322 00852 NM 1996 3 22 USAA960277 1 19960224 A 5240 FRAME BOEING 737 737201 1384454 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 243US 36817 22445 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK NR 4 STOP CUTOUT (AFT FRAME) AT FORWARD CABIN SERVICE DOOR . STOP DRILLED CRACK, REPAIRED AND INSTALLED. REPAIRED PER SRM 52-00-2 PAGE 4 FIG 1 AND SRM 51-40-3 PAGE 1. (M) 2 L 7 2 4F A16WE 1996032200853 19960322 00853 NM 1996 3 22 USAA960278 1 19960224 A 5315 FLOOR BEAM BOEING 737 737201 1384454 NM BS 460-500 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 243US 36817 22445 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORRODED NUT PLATE HOLES AT FLOOR BEAM STATION 460-500 ABOVE STRINGER 27 R. REPLACED ANGLE, REPAIRED PER SRM 53-10-5 FIG 6. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996032200854 19960322 00854 NM 1996 3 22 USAA960279 1 19960224 A 5744 65634441 HINGE FITTING BOEING 737 737201 1384454 NM WS 537.8 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 243US 36817 22445 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK LEFT WING AT WS 537.8 LOWER FLANGE OF AILERON HINGE FITTI NG. FABRICATED AND INSTALLED FLANGE REPAIR PER EA 40893. (M) 2 L 7 2 4F A16WE 1996032200855 19960322 00855 NM 1996 3 22 USAA960280 1 19960224 A 5312 BULKHEAD BOEING 737 737201 1384454 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 243US 36817 22445 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH LONG CRACK FUSELAGE BULKHEAD STATION 178, WL 200, RBL 6 INCHES. I NSTALLED REPAIRED DOUBLER, REPAIRED PER TR 53-10-11. (M) 2 L 7 2 4F A16WE 1996032200856 19960322 00856 NM 1996 3 22 USAA960281 1 19960224 A 5320 ANGLE BOEING 737 737201 1384454 NM BS 940-1010 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 243US 36817 22445 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 4 INCH BY 20 INCH CORRODED AREA RIGHT Z-ANGLE AT AFT SERVICE DOOR STATIO N 940 TO STATION 1010. REMOVED CORROSION ON ALODINE AND PRIMED. COMPLETED REPAIR PER SRM 51-10-6. LEVEL 1 CORROSION. (M) 2 L 7 2 4F A16WE 1996032200857 19960322 00857 NM 1996 3 22 USAA960282 1 19960224 A 5240 FRAME BOEING 737 737201 1384454 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 243US 36817 22445 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK NR 3 STOP CUT OUT (AFT FRAME) AT FORWARD CABIN SERVICE DOO R. STOP DRILLED CRACK, REPAIRED PER SRM 52-00-2 PAGE 4, FIG 1 AND SRM 51-40-3 PAGE 1. (M) 2 L 7 2 4F A16WE 1996032200858 19960322 00858 NM 1996 3 22 USAA960283 1 19960224 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 243US 36817 22445 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK IN FUSELAGE SKIN AT STATION 727 B 2 INCH AND STRINGER 17. I NSTALLED REPAIR DOUBLER, REPAIRED PER SRM 53-30-3 FIG 6. (M) 2 L 7 2 4F A16WE 1996032200859 19960322 00859 EU 1996 3 22 USAA960284 1 19960226 A 5312 BLKHD FISHPLATE FOKKER F28 F28MK4000 4990810 EU FWD PRESS BLKHD CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 478US 21404 11227 PIT - DURING SIP VISIT INSPECTION, ACCOMPLISHED SIP 53-10-06 AND FOUND 4 INCH AND 3.5 INCH CRACK IN FRONT PRESSURE BULKH EAD FISHPLATE BETWEEN STRINGER 72 AND 73. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER SRM 53-02-18 PG 28. (M) 2 L 7 2 4F RT A20EU 1996032200860 19960322 00860 NM 1996 3 22 USAA960285 1 19960227 A 5311 FRAME BOEING 737 737301 1384611 NM BS 188 DAMAGE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 585US 26562 23930 CLT - INSPECTION VISUAL FOUND DAMAGED INNER, OUTER CHORD, WEGB AND FORMED ANGLES APPROX 8 INCHES BY 2 INCHES LOCATED AT THE FUSELAGE FRAME LOCATED AT BS 188 FROM 7 INCHES RIGHT OF BL 0 TO 23 INCHES RIGHT OF BL 0. INSTALLED REPAIR CHORD AND WEB AS PER BOEING SRM 51-70-11, 51-70-12 AND 51-70-13. (M) 2 L 7 2 4F RT A16WE 1996032200861 19960322 00861 NM 1996 3 22 USAA960287 1 19960224 A 5311 FRAME BOEING 737 737201 1384454 NM BS 328 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 243US 36817 22445 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK BS 328 AT NR 3 STOP FOR FORWARD CABIN SERVICE DOOR FRAME. STOP DRILLED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 51-40-3 PAGE 1. (M) 2 L 7 2 4F A16WE 1996032200862 19960322 00862 NM 1996 3 22 USAA960289 1 19960224 A 5320 CHORD BOEING 737 737201 1384454 NM BS 270 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 243US 36817 22445 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORROSION Z-ANGLE STATION 270 AT BL 0. REMOVED CORROSI ON AND INSTALLED DOUBLER, REPAIRED PER TR 53-20-04. (M) 2 L 7 2 4F A16WE 1996032200863 19960322 00863 NM 1996 3 22 USAA960290 1 19960223 A 5330 SKIN BOEING 737 737301 1384611 NM BS 400-420 DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 354US 25316 23557 INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND 2 INCH BY 4 INCH HOLE STATION 400-420 STRINGER 27 R SKIN AND STRINGE R. INSTALLED DOUBLER ON SKIN, SPLICED IN STRINGER SECTION, REPAIRED PER SRM 53-00-03 AND SRM 53-00-01. (M) 2 L 7 2 4F RT A16WE 1996032200864 19960322 00864 EU 1996 3 22 USAAF96021 1 19960211 A 3350 F0N96118DAL RELAY FOKKER F28 F28MK0100 4990807 EU CABIN FAILED A USAA K NONE O OTHER AP APPROACH 1 EA 19 854US 11282 LGA- FLT 301 - UPON GEAR EXTENSION, THE CABIN STANDBY LIGHTS AND EXIT IDENTIFIERS DID NOT ILLUMINATE. MAINTENANCE REPLA CED THE K2618A RELAY. (M) 2 L 7 2 4F RT 1996032200865 19960322 00865 1996 3 22 USAAF96024 4 19960223 A 2565 60049101 SLIDE FOKKER F28 F28MK0100 4990807 EU PAX DOOR SHIFTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 888AU 11357 FLT NR 1017 - PIT - EMERGENCY SLIDE AT MAIN ENTRY DOOR IS COMING OUT OF ITS PACK. REPLACED MED EMERGENCY SLIDE PER MM. OPS CHECK GOOD. (M) 2 L 7 2 4F RT 1996032200866 19960322 00866 EU 1996 3 22 USAAF96025 1 19960224 A 5610 D20543405 WINDSHIELD FOKKER F28 F28MK0100 4990807 EU LT FLIGHT DECK CRACKED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 882US 11334 FLT NR 275 - RDU - OUTER PANE OF CAPTIANS WINDSHIELD SHATTERED IN FLIGHT AT 29,000 FEET PRECAUTIONARY LANDING MADE AT RD U. REPLACED L1 WINDOW. (M) 2 L 7 2 4F RT 1996032200867 19960322 00867 EU 1996 3 22 USAAF96026 1 19960225 A 3260 BULB FOKKER F28 F28MK0100 4990807 EU LANDING GEAR FAILED A USAA O OTHER N FALSE WARNING AP APPROACH 1 EA 19 897US 11392 FLT 578 - CLT - RIGHT MAIN GEAR FAILED TO INDICATE DOWN AND GREEN. RECYCLED GEAR, CHANGED BULBS WITH NO CHANGE. LANDED NORMALLY, TAXIED WITH GEAR PINNED. PERFORMED BITE USING THE PSEU WITH NO DEFECTIVE SWITCHES OR TARGETS. INSPECTED IND ICATION PACK ON FORWARD PANEL AND FOUND ONE BROKEN BULB AND ONE BURNED OUT BULB. REMOVED AND REPLACED ALL BULBS AND GEA R WARNING SYSTEM OP'D NORMAL. AIRCRAFT OK FOR CONTINUED SERVICE. (M) 2 L 7 2 4F RT 1996032200868 19960322 00868 EU 1996 3 22 USAAF96027 1 19960304 A 2840 WARNING LIGHT FOKKER F28 F28MK0100 4990807 EU BOOST PUMP ILLUMINATED A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 885US 11345 PHL-MCI - FLT 439 - THE NR 1 BOOST PUMP WARNING LIGHT ILLUMINATED. SHORTLY THEREAFTER, THE NR 2 BOOST PUMP WARNING LIGH T ILLUMINATED. FLIGHT DIVERTED TO IND AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE OPERATED BOTH PUMPS ON THE GROU ND AND FOUND THEM BOTH WORKING PROPERLY. PERFORMED BITE AND COULD NOT DUPLICATE PROBLEM. AIRCRAFT RELEASED FOR SERVICE . (M) 2 L 7 2 4F RT 1996032200869 19960322 00869 NM 1996 3 22 USAASB96029 1 19960212 A 2131 7638102 CONTROLLER BOEING 737 7374B7 1384702 NM CABIN FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 780AU 24997 FLT NR 1201 - BWI - ON CLIMB-OUT FROM EWR AT 34.5 CABIN ALT. WARNING HORN CABIN AT 13,000 UNABLE TO CONTROL PRESSURE DE SCENT TO 10,000. MAINTENANCE REPLACED AUTO CONTROLLER, OPS CHECK NORMAL. PERFORMED OPERATIONAL TEST OF PRESS CONTROL S YSTEM IAW MM CH 21-31-00 PAGE 201. (M) 2 L 7 2 4F RT A16WE 1996032200870 19960322 00870 NE 1996 3 22 USAASB96031 2 19960213 A 7250 50033203022 T3 BLADE BOEING 737 7372B7 1384560 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE FAILED A A USAA C ABORTED TAKEOFF C A F.O.D. FLAME/FIRE TO TAKEOFF 1 EA 19 283AU 28277 23116 709147 FLT 1930 - PHL - NR 1 ENG COMPRESSOR STALLED, WOULD NOT SPOOL UP AFTER. DURING TAXI BACK IDLE EGT KEPT CREEPING UP, SHU T IT DOWN A T530. AT GATE GROUND PERSONNEL REPORTED TAIL PIPE FIRE. FIRED BOTH BOTTLES AND EVACUATED AIRCRAFT. NO FIR E WARNING, FIRE WARNING WAS CHECKED ON SHUTDOWN OK, TURBINE FAILURE CAUSED DAMAGE TO LEFT HORIZONTAL STABILIZER. MAINTE NANCE REPLACED NR 1 ENGINE AND LEFT LEADING EDGE OF HORIZONTAL STABILIZER. ENGINEERING ANALYSIS FOUND THAT A T3 BLADE F AILED POSSIBLY FROM EXCESSIVE SHROUD WEAR. (M) 2 L 7 2 4F 4 F A16WE E2EA 1996032200871 19960322 00871 NM 1996 3 22 USAASB96033 1 19960223 A 2613 OVERHEAT LIGHT BOEING 737 7372B7 1384560 NM NR 2 ENGINE ILLUMINATED A USAA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 EA 19 281AU 23114 FLT NR 800 - MCI - DURING CLIMB AT APPROXIMATELY 10,000 FEET, THE NR 2 ENGINE OVERHEAT LIGHT CAME ON. THE CAPTAIN REDUC ED POWER AND THE LIGHT WENT OUT. PULLED NR 2 ENGINE BACK TO IDLE AND RETURNED TO MCI. (M) 2 L 7 2 4F A16WE 1996032200872 19960322 00872 NM 1996 3 22 USAASB96034 1 19960224 A 5610 5893543110 WINDSHIELD BOEING 737 737201 1384454 NM RT FLT DECK DELAMINATED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 247US 22754 FLT NR 1129 - CRW - AFTER DEPARTING PIT AND CLIMBING TO FLT LEVEL 350, THE FIRST OFFICERS WINDSHIELD BEGAN TO BUBBLE/DEL AMINATE. CAPTAIN DECIDED TO DIVERT TO CRW BECAUSE HE COULD NOT TELL IF ONLY THE OUTER PANE WAS INVOLVED. MAINTENANCE R EPLACED FIRST OFFICERS WINDSHIELD PER MAINTENANCE MANUAL. OPS CHECKED GOOD. (M) 2 L 7 2 4F A16WE 1996032200873 19960322 00873 NM 1996 3 22 USAASB96035 1 19960225 A 3350 1012623 LIGHT BOEING 737 7374B7 1384702 NM CABIN BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 442US 24841 FLT NR 1759 - DCA - EMERGENCY EXIT LIGHT AT SEAT 12C IS BROKEN OFF. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY. OPS CHECKS SATISFACTORY. (M) 2 L 7 2 4F RT A16WE 1996032200874 19960322 00874 NE 1996 3 22 USAASB96036 2 19960229 A 7200 ENGINE BOEING 737 7372B7 1384560 NM PWA JT8 JT8D17A 52049 NE NR 1 VIBRATION A USAA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 EA 19 287AU 23134 FLT NR 885 - GSO - ON INITIAL CLB FLIGHT ATTENDANT NOTICED A VIBRATION THROUGH THE CABIN. AT CRUISE VIBRATION CONTINUES WIHT CAPTAIN ISOLATING PROBLEM TO NR 1 ENGINE. ALL ENGINE READINGS CONTINUED TO BE NORMAL. AIRCRAFT DIVERTED TO GSO. (M) 2 L 7 2 4F 4 F A16WE E2EA 1996032200875 19960322 00875 NM 1996 3 22 USAASB96037 1 19960301 A 2130 7207375 PRESS RELIEF VLV BOEING 737 7373B7 1384580 NM AFT CARGO COMPT FAILED A USAA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 384US 22957 FLT NR 2201 - CLT - AUTOPRESSURIZATION FAILED AT FL 370. EMERGENCY DESCENT MADE, WAS ABLE TO REGAIN CONTROL OF CABIN IN MANUAL. NEVER GOT THE 10,000 FEET ALT HORN AND FIRST INDICATION PAX OXYGEN LIGHT AND OVERHEAD ON RECALL. MAINTENANCE REMOVED AND REPLACED RIGHT PRESSURE RELIEF VALVE. CHECKS SATISFACTORY. REPLACED LEFT PRESSURE RELIEF VALVE PRECAUTIONA RY. CHECKS SATISFACTORY. (M) 2 L 7 2 4F RT A16WE 1996032200876 19960322 00876 NM 1996 3 22 USAASB96038 1 19960301 A 2150 1828202 HEAT EXCHANGER BOEING 737 7374B7 1384702 NM RT PACK FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 779AU 24996 SJU - FLT 1041 - RIGHT PACK TRIPPED, COULD NOT RESET. LEFT PACK RESET THEN TRIPPED AGAIN. LEFT PACK CONTINUALLY TRIPS. MAINTENANCE REPLACED RIGHT PRIMARY HEAT EXCHANGER. OPS CHECKS SATISFACTORY. (X) 2 L 7 2 4F RT A16WE 1996032200877 19960322 00877 NM 1996 3 22 USAASB96039 1 19960302 A 7930 1163P181 FILTER BYPASS SW BOEING 737 7372B7 1384560 NM NR 1 ENG INTERMITTENT A USAA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 274US 22886 FLT NR 797 - MCO - FIVE MINUTES AFTER TAKEOFF, 'OIL FILTER BYPASS' LIGHT FOR NR 1 ENGINE CAME ON. RETARDED THROTTLES, N O HELP. SHUT DOWN ENGINE AND RETURNED TO MCO. MAINTENANCE REPLACED THE FILTER BYPASS SWITCH. (M) 2 L 7 2 4F A16WE 1996032200878 19960322 00878 EU 1996 3 22 VTZA96067 1 19960211 A 2612 D2370240 FIRE DET LOOP JETAIR JETSTM JETSTM4101 1500501 EU RT ENG PINCHED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 311UE 1015 41029 FLT NR 6264 - BTV-IAD - DURING CLIMB-OUT, RETURNED TO BTV DUE TO THE RIGHT ENGINE FIRE DETECTION LIGHT ILLUMINATING. FL IGHT CREW FIRED THE ENGINE EXTINGUISHER AND SHUT ENGINE DOWN IN FLIGHT. AIRCRAFT LANDED AT BTV WITH NO FURTHER INCIDENT S AND ALL PASSENGERS SAFE. MAINTENANCE PERFORMED AN INSPECTION OF THE RIGHT ENGINE AND FOUND THAT THE FIRE DETECTION LO OP WAS PINCHED. REPLACED THE FIRE DETECTION LOOP. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996032200879 19960322 00879 EU 1996 3 22 VTZA96071 1 19960204 A 7712 TQ INDICATION BAG JETSTM JETSTM3201 1500217 EU LT/RT ENGINES MALFUNCTIONED A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 487UE 906 FLT NR 6387 - IAD-SYR - DURING CRUISE, RETURNED TO IAD DUE TO THE RIGHT TORQUE WAS AT 100 PERCENT AND THE LEFT TORQUE WA S AT 40 PERCENT. THE AIRCRAFT WAS STABLE WITH NO YAWING MOTION. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. M AINTENANCE PERFORMED INSPECTIONS BUT COULD NOT DUPLICATE PROBLEMS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SER VICE. (M) 2 L 7 2 4T RT A56EU 1996032200880 19960322 00880 EU 1996 3 22 VTZA96074 1 19960209 A 2611 S2902012 TEST SWITCH JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT FAILED A VTZA B EMER. DESCENT N FALSE WARNING AP APPROACH 1 EA 27 313UE 41026 FLT NR 6211 - IAD-PVD - DURING APPROACH, PERFORMED AN EMERGENCY DESCENT DUE TO THE MAIN BAGGAGE, POD BAGGAGE AND LAV SMO KE DETECTORS CAP LIGHTS ILLUMINATING. AIRCRAFT LANDED AT PVD WITH NO FURTHER INCIDENTS. MAINTENANCE COMPLIED WITH REST RICTIONS AND LIMITATIONS PER FERRY PERMIT. AIRCRAFT WAS THEN FERRIED TO IAD. AIRCRAFT LANDED AT IAD WITH NO INCIDENTS. MAINTENANCE REPLACED THE SMOKE DETECTOR TEST SWITCH. MAINTENANCE THEN TESTED SYSTEM IAW J41 MM CHAPTER 26. THIS CLEA RED ALL THREE DISCREPANCIES. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996032200881 19960322 00881 EU 1996 3 22 VTZA96093 1 19960228 A 2751 TY17604A POTENTIOMETER JETAIR JETSTM JETSTM4101 1500501 EU TE FLAPS OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 315UE 41033 FLT NR 6320 - IAD-RDU - ABORTED THE TAKEOFF DUE TO THE TAKEOFF CONFIGURATION SYSTEM ACTIVATING. AIRCRAFT RETURNED TO GA TE WITH NO FURTHER INCIDENTS. MAINTENANCE PERFORMED INSPECTIONS BUT COULD NOT DUPLICATE THE DISCREPANCIES. AIRCRAFT WA S RELEASED AND APPROVED FOR RETURN TO SERVICE. AIRCRAFT THEN ABORTED THE TAKEOFF AGAIN AT 1315 HRS DUE TO THE TAKEOFF C ONFIGURATION WARNING SYSTEM ACTIVATING. MAINTENANCE THEN ADJUSTED THE FLAP POSITION POTENTIOMETERS. A HIGH SPEED TAXI CHECK WAS PERFORMED. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996032200882 19960322 00882 EU 1996 3 22 VTZA96094 1 19960302 A 7603 14176007175 TENSION KNOB JETAIR JETSTM JETSTM4101 1500501 EU LT COND LEVER OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 27 311UE 41029 FLT NR 6578 - IAD-PWM - ABORTED TAKEOFF DUE TO THE LEFT CONDITION LEVER VIBRATED BACK. AIRCRAFT RETURNED TO GATE WITH N O FURTHER INCIDENT. MAINTENANCE TIGHTENED THE TENSION KNOB. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996032200883 19960322 00883 EU 1996 3 22 VTZA96095 1 19960303 A 5270 91SE16 SWITCH BAG JETSTM JETSTM3201 1500217 EU PAX DOOR BROKEN WIRE A VTZA O OTHER N FALSE WARNING LD LANDING 1 EA 27 488UE 907 FLT NR 6407 - IAD-LGA - DURING LANDING, THE PASSENGER DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT TAXIED TO GATE WITH NO F URTHER INCIDENTS. MAINTENANCE REPAIRED A CHAFED WIRE AT THE DOOR HANDLE MICROSWITCH. AIRCRAFT WAS RELEASED AND APPROVE D FOR RETURN TO SERVICE. (M0 2 L 7 2 4T RT A56EU 1996032200884 19960322 00884 NM 1996 3 22 W8PA960005 1 19960303 A 3350 362624 LIGHT BOEING 737 7373L9 1384470 NM CABIN INOPERATIVE A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 961WP 23332 AISLE PATH LIGHTING INOP AT ROWS 15 AND 17. PLACARDED PER MEL 33-19. (M) 2 L 7 2 4F RT A16WE 1996032200885 19960322 00885 NM 1996 3 22 W8PA960006 1 19960307 A 2913 6507506 HYD PUMP BOEING 737 7373B7 1384580 NM NR 1 ENG FROZEN A W8PA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 509AU 9925 23384 DURING FLIGHT, 'A' SYSTEM HYDRAULIC PUMP LIGHT CAME ON. LOSS OF 'A' SYSTEM HYDRAULICS. AIR RETURN. MAINTENANCE FOUND NR 1 ENGINE DRIVEN PUMP FROZEN. REMOVED AND REPLACED EDP. (M) 2 L 7 2 4F RT A16WE 1996032200886 19960322 00886 EU 1996 3 22 WTAA960037 1 19960218 A 3260 9005EN38 SWITCH BAG JETSTM JETSTM3101 1500215 EU NLG DAMAGED WIRE A WTAA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 17 401UE 729 SFO - NOSE LANDING GEAR INTRANSIT LIGHT INDICATION REPORTED INOPERATIVE. AIRCRAFT FERRIED TO FAT FOR REPAIRS. MAINTENA NCE REPAIRED WIRE AT NOSE LANDING GEAR UPLOCK MICROSWITCH. GEAR INDICATION OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996032200887 19960322 00887 EU 1996 3 22 WTAA960038 1 19960219 A 7712 1246433 TORQUE IND BAG JETSTM JETSTM3101 1500215 EU COCKPIT MALFUNCTIONED A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 WP 17 425UE 798 SFO - NR 2 ENGINE FAILED TO ACHIEVE REQUIRED TORQUE ON TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. RIGHT ENGINE AP PEARED TO BYPASS FUEL DURING TAKEOFF ROLL. MAINTENANCE DEFERRED TTL SYSTEM PER MEL 76-2. ENGINE OPERATIONS REPORTED NO RMAL DURING GROUND RUN WITH TTL OFF. AIRCRAFT RETURNED TO SERVICE. TTL SYSTEM DEFERRAL CLEARED AFTER THE REPLACEMENT O F THE RIGHT TORQUE INDICATOR. (M) 2 L 7 2 4T RT A21EU 1996032200888 19960322 00888 WP 1996 3 22 WTAA960040 2 19960223 A 7320 8974575 BYPASS VALVE BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110U 01514 WP RT ENG FUEL FAILED A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 17 431UE 813 SFO - RIGHT ENGINE FAILED TO OBTAIN REQUIRED TAKEOFF TORQUE. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE REPLACED RI GHT ENGINE FUEL BYPASS VALVE. ENGINE OPERATION NORMAL DURING GROUND CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A21EU E4WE 1996032200889 19960322 00889 EU 1996 3 22 WTAA960042 1 19960223 A 2730 13707F425 ELEVATOR ASSY BAG JETSTM JETSTM3101 1500215 EU TAIL SECTION LACK OF LUBE A WTAA O OTHER F FLT CONT AFFECTED CL CLIMB 1 WP 17 107XV 723 SEA - RESTRICTED MOVEMENT OF ELEVATOR CONTROLS REPORTED ON AIRCRFT CLIMB-OUT FROM PDX. CONTROLS RETURNED TO NORMAL OPER ATION FOLLOWING AIRCRAFT DESCENT TO LOWER ALTITUDE AND WARMER WEATHER CONDITIONS. MAINTENANCE INSPECTED ELEVATOR CONTRO L SYSTEM FOR DEFECTS OR SIGNS OF BINDING. NO DISCREPANCIES NOTED. APPLIED LUBRICATION TO ELEVATOR HINGES AND APPLIED ' ICEX' TO ELEVATOR BOOTS, HORN HEATERS AND HORN SURFACES. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996032200890 19960322 00890 EU 1996 3 22 WTAA960043A 1 19960226 A 3260 9005EN38 SWITCH BAG JETSTM JETSTM3101 1500215 EU NLG FAILED A WTAA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 WP 17 427UE 811 PSC - NOSE LANDING GEAR DOWN INDICATION LIGHT FAILED TO ILLUMINATE AND LEFT MAIN GEAR INTRANSIT LIGHT REPORTED INOPERATI VE. ON INITIAL GEAR EXTENSION, CREW CYCLED GEAR WITH NO CHANGE IN INDICATION. GEAR POSITION CONFIRMED WITH FLYBY PRIOR TO LANDING. NOSE GEAR DOWN INDICATION LIGHT ILLUMINATED PRIOR TO LANDING. AIRCRAFT FERRIED TO SEA FOR REPAIRS. MX RE PLACED NOSE LANDING GEAR DOWNLOCK MICROSWITCH AND REPAIRED WIRES AT LEFT MAIN LANDING GEAR UPLOCK MICROSWITCH. GEAR IND ICATION NORMAL DURING GROUND CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996032200891 19960322 00891 EU 1996 3 22 WTAA960044 1 19960226 A 3242 AC63742 MAXARET BAG JETSTM JETSTM3101 1500215 EU LT MLG FAILED A WTAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 17 421UE 804 PDX - LEFT BRAKE FAILED TO OPERATE ON TAXI OUT. MAINTENANCE REPLACED LEFT BRAKE MAXARET. LEFT BRAKE OPERATION NORMAL D URING TAXI CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996032200892 19960322 00892 NE 1996 3 22 YIEA96007 2 19960210 A 7310 52010481 LOW PRESS FILTER AMD FALC20 FALCON 2720302 EU GE CF700 CF7002D2 30010 NE LT ENG CRUSHED A YIEA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 GL 23 814AA 31 245U139 YIP - LEFT ENGINE FLAMED OUT DURING STEADY STATE CLIMB AT 36,000 FEET. AIRCRAFT DESCENDED AND THE ENGINE WAS AIRSTARTED PER THE CHECK LIST. AIRCRAFT RETURNED TO YIP AND MADE A NORMAL TWO ENGINE LANDING. LEFT ENGINE WAS INSPECTED FOR FOD IN THE INLET, EXHAUST AND BY BOROSCOPE METHODS WITH NO DEFECTS NOTED. LOW PRESSURE AND ENGINE FUEL FILTERS INSPECTED. F OUND LOW PRESSURE AND FUEL PUMP FILTERS CRUSHED UPON INSPECTION. REPLACED FILTERS WITH SERVICEABLE. AIRCRAFT RELEASED FOR TEST FLIGHT. (M) 2 L 7 2 4F 4 F A7EU E7EA 1996032200893 19960322 00893 NE 1996 3 22 YIEA96008 2 19960210 A 7200 ENGINE AMD FALC20 FALCON 2720302 EU GE CF700 CF7002D2 30010 NE RIGHT FLAMED OUT A YIEA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 GL 23 814AA 31 304207B YIP - RIGHT ENGINE FLAMED OUT DURING MAX ALTITUDE ACCELERATION TEST AT 35,000 FT. AIRCRAFT DESCENDED AND ENGINE RESTART WAS ATTEMPTED AT 24,000 FEET WITHOUT SUCCESS AND THEN AT 21,000 FEET WHERE ENGINE RELIT. AIRCRAFT RETURNED TO YIP AND MADE A NORMAL TWO ENGINE LANDING. RIGHT ENGINE WAS INSPECTED IAW GE SEI-187 TO DETERMINE CAUSE OF FLAMEOUT. NO DEFECTS NOTED. INSPECTED AIRCRAFT AND ENGINE FUEL FILTERS FOR DEFECTS AND CONTAMINATION. NO DEFECTS NOTED. ENGINE RELEASED F OR TEST FLIGHT AND MAX ALTITUDE ACCELERATION CHECK. NO CAUSE FOR FLAMEOUT FOUND. THIS ITEM REMAINS UNDER REVIEW FOR CA USE AND REPAIR OF PROBLEM. (M) 2 L 7 2 4F 4 F A7EU E7EA 1996032200894 19960322 00894 NE 1996 3 22 96ZZZX1291 2 19960112 A 7200 ENGINE BOEING 767 767205 1385121 NM PWA JT9 JT9D7R4D 52054 NE NR 1 MALFUNCTIONED A TWAA O OTHER O OTHER CL CLIMB 1 CE 05 650TW 23057 SEA - FLT 740 - DURING CLIMB, NR 1 ENGINE, SN 4609, SURGED. POWER WAS REDUCED TO IDLE. CHANGED NR 1 ENGINE. ENGINE TO TAL TIME: 29,752 HOURS; 8,040 CYCLES. CHECK C-4C - 10-25-95. LAX. 2 L 7 2 4F 4 F RT A1NM E3NE 1996032200921 19960322 00921 NM 1996 3 22 96ZZZX1318 1 19960210 A 5610 SPSD0328131 WINDSHIELD DORNER DO32 DO328100 2996000 NM RT COCKPIT SHATTERED A EQGA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 19 335LS 212 3035 DFW/ASE - WHILE EN ROUTE, THE FIRST OFFICER'S OUTSIDE WINDSHIELD SHATTERED. THE PILOT RETURNED TO DFW AND LANDED WITHOU T FURTHER INCIDENT. THIS IS THE THIRD WINDSHIELD FAILURE ON THIS ACFT IN THE PAST 6 MONTHS AND/OR 838.0 AIRCRAFT FLIGHT HOURS. THE AIRCRAFT WAS FERRIED TO HOT FOR REPLACEMENT OF THE WINDSHIELD. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A45NM 1996032200922 19960322 00922 NM 1996 3 22 96ZZZX1320 1 19960303 A 3230 2431600000 UPLOCK ROLLER ROTOL DORNER DO32 DO328100 2996000 NM MLG WW LACK OF LUBE A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 422JS 3018 FLT 4014 - AFTER TAKEOFF, LT MLG INTRANSIT LIGHT REMAINED ILLUMINATED AFTER THE GEAR WAS SELECTED 'UP'. AIRCRAFT RETURN ED TO FIELD, LANDED WITHOUT FURTHER INCIDENT. PIT MX CLEANED AND LUBRICATED THE MLG LOCK ROLLERS IAW MM 32-00-00 AND ST D MX PRACTICES. GROUND CHECKED 'GOOD'. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A45NM 1996032200923 19960322 00923 NM 1996 3 22 96ZZZX1321 1 19960222 A 3060 A56362 BRUSH BLOCK BFGOODRICH DORNER DO32 DO328100 2996000 NM LT/RT ENGINE DIRTY A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 424JS 3033 FLT 4028 - PROPELLER HEAT FAILED SHORTLY AFTER TAKEOFF. AIRCRAFT RETURNED TO FIELD, LANDED WITHOUT FURTHER INCIDENT. P IT MX CLEANED THE PROPELLER DEICE BRUSH BLOCK ASSEMBLIES (BOTH SIDES) IAW MM 61-00-01. GROUND CHECKED GOOD, AIRCRAFT RE TURNED TO SERVICE. (X) 2 H 7 2 4T RT A45NM 1996032200924 19960322 00924 NM 1996 3 22 96ZZZX1322 1 19960303 A 3230 2431600000 UPOCK ROLLERS ROTOL DORNER DO32 DO328100 2996000 NM LT MLG LACK OF LUBE A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 423JS 3032 FLT 4079 - AFTER TAKEOFF, CREW REPORTED A 'RED' INTRANSIT LIGHT LT MAIN GEAR, AFTER GEAR WAS SELECTED 'UP'. AIRCRAFT RE TURNED TO THE FIELD, LANDED WITHOUT FURTHER INCIDENT. PIT MX CLEANED AND LUBRICATED MLG 'UPLOCK' ROLLERS IAW MM 32-00-0 0 AND STD MX PRACTICES. GROUND CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A45NM 1996032200925 19960322 00925 NM 1996 3 22 96ZZZX1323 1 19960219 A 3150 701730014001 COMPUTER HONEYWELL PRIMUS20000 DORNER DO32 DO328100 2996000 NM RT AVIONICS RACK MALFUNCTIONED A VNAA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 GL 07 328JS 94100379 3030 PIT/LAN - FLT 4037 - EN ROUTE, BOTH OF THE FIRST OFFICER'S DISPLAY UNITS (PRIMARY AND MULTIFUNCTION FLIGHT DISPLAY UNITS ) FAILED. DURING THE COURSE OF ACCOMPLISHING THE ABNORMAL FLIGHT PROCEDURES CHECK LIST, THE CREW DISCOVERED THE NR 2 IN TEGRATED AVIONICS COMPUTER WAS INOPERATIVE. AIRCRAFT RETURNED TO PIT, LANDED WITHOUT FURTHER INCIDENT. PIT MX RERACKED THE NR 2 IAC COMPUTER IAW MM 31-41-00. GROUND CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A45NM 1996032200926 19960322 00926 NM 1996 3 22 96ZZZX1324 1 19960223 A 5610 D0328131 WINDSHIELD DORNER DO32 DO328100 2996000 NM RT COCKPIT DAMAGED A VNAA A B UNSCHED LANDING EMER. DESCENT O OTHER CR CRUISE 1 GL 07 426JS 166 3038 FLT 4153 - DURING CRUISE AT FL 190, CREW HEARD A LOUD NOISE FOLLOWED BY THE FRACTURING OF THE FIRST OFFICER'S WINDSHIELD . CREW DECREASED AIRSPEED, AND ALTITUDE. INCREASED THE CABIN PRESSURE. CREW DECLARED AN EMERGENCY AND DIVERTED TO SCE . AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. PIT MX TRAVELED TO SCE WHERE THEY REPLACED THE DAMAGED WINDSHIELD IAW MM 5 6-11-00. AIRCRAFT WAS THEN RETURNED TO SERVICE. 2 H 7 2 4T RT A45NM 1996032200927 19960322 00927 NM 1996 3 22 96ZZZX1325 1 19960225 A 5610 D0328131 WINDSHIELD DORNER DO32 DO328100 2996000 NM RT COCKPIT DAMAGED A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 07 429JS 328 3043 FLT 1001 - CREW REPORTED THE FIRST OFFICER'S WINDSHIELD CRACKED EN ROUTE BETWEEN PIT AND CVG. AIRCRAFT DIVERTED TO CAK, LANDED WITHOUT FURTHER INCIDENT. CAK MX REPLACED THE FIRST OFFICER'S WINDSHIELD IAW MM 56-11-00. GROUND CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A45NM 1996032200928 19960322 00928 NM 1996 3 22 96ZZZX1326 1 19960225 A 5610 D0328231 WINDSHIELD DORNER DO32 DO328100 2996000 NM LT COCKPIT DAMAGED A VNAA O OTHER O OTHER DE DESCENT 1 GL 07 433JS 161 3047 FLT 4045 - CAPTAIN'S WINDSHIELD (OUTER PANE) CRACKED DURING DESCENT INTO PIT. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. PIT MX REPLACED CAPTAIN'S WINDSHIELD IAW MM 56-11-00. GROUND CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A45NM 1996032200932 19960322 00932 WP 1996 3 22 CKSA6004 1 19960119 A 2612 D5020 FIRE LOOP DOUG DC8 DC863F 302198F WP NR 4 ENGINE BROKEN A CKSA F ACTIVATE FIRE EXT. N FALSE WARNING DE DESCENT 1 GL 23 867BX 75991 46049 KTOL - FLT 71266 - NR 4 ENGINE FIRE WARNING CAME ON IN-FLIGHT DURING DESCENT. PERFORMED IN-FLIGHT SHUT DOWN AND DISCHAR GED FIRE BOTTLE. LANDED WITHOUT INCIDENT. FOUND NR 4 ENGINE BOTTOM FIRE LOOP BROKEN. REPLACED LOWER FIRE LOOP. GROUN D OPS CHECK GOOD IAW MM CHAPTER 26. (X) 2 L 7 4 4F 4A25 1996032200933 19960322 00933 WP 1996 3 22 GRAA9611 1 19960218 A 3350 311 LAMP DOUG DC9 DC982 3022082 WP ACCESSORY COMPT INOPERATIVE A GRAA K NONE O OTHER IN INSP/MAINT 1 WP 11 500TR 49144 MYR - LINE MAINTENANCE DISCOVERED THE EMERGENCY LIGHTING IN THE AFT ACCESSORY COMPARTMENT, RT SIDE, INOPERATIVE. MAINTE NANCE REMOVED AND REPLACED THE LAMP. OPERATIONALLY, CHECKED NORMAL. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. ( X) 2 L 7 2 4F A6WE 1996032200934 19960322 00934 1996 3 22 MALA964891 4 19960228 A 2350 M1035CAABJLB2 AUDIO PANEL SWRNGN SA227 SA227AC 8780603 SW COCKPIT INTERNAL FAULT A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 15 436MA AC719B LAF - FLT 3426 - EN ROUTE, THE NR 1 AUDIO CIRCUIT BREAKER TRIPPED AND EMITTED SMOKE. THE CREW DID NOT ATTEMPT TO RESET THE CB AND CONTINUED TO LAF, WHERE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE NR 1 AUDIO PANE L. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 1 L 7 2 4T A8SW 1996032200935 19960322 00935 SW 1996 3 22 MALA964895 1 19960302 A 3260 1EN516 SWITCHES SWRNGN SA227 SA227AC 8780603 SW NLG FAILED A MALA A UNSCHED LANDING P NO WARNING INDICATION AP APPROACH 1 GL 15 428MA AC646 STC - FLT 3491 - DURING APPROACH, CREW NOTED NOSE GEAR GREEN DOWN AND LOCKED LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSI ON. THE CREW ELECTED TO RETURN TO MSP, AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE LT AND RT NOSE DOWN AND LOCKED SWITCHES. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 1 L 7 2 4T A8SW 1996032200936 19960322 00936 SW 1996 3 22 MALA964897 1 19960302 A 3230 1EN516 SWITCH SWRNGN SA227 SA227AC 8780603 SW NLG FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 439MA AC722 MSP - FLT 3402 - AFTER DEPARTURE, CREW NOTED NOSE GEAR WOULD NOT FULLY RETRACT. THE CREW ELECTED TO RETURN TO MSP, AND ACFT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED RT UPPER NLG LIMIT SWITCH. ALL SYSTEMS OPERATED SATISFACT ORILY. (X) 1 L 7 2 4T A8SW 1996032200937 19960322 00937 SW 1996 3 22 MALA964898 1 19960301 A 3397 WIRE SWRNGN SA227 SA227AC 8780603 SW ENTRANCE LIGHTS CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 CE 01 158MC AC726B MSP - DURING A MAINTENANCE GATE WALK-AROUND INSPECTION, MAINTENANCE PERSONNEL NOTED THE ENTRANCE LIGHTS WERE INOPERATIVE AND WOULD TRIP THE CIRCUIT BREAKER. MAINTENANCE FOUND AT TERMINAL END CONTACTING THE AIRCRAFT FRAME. THEY REPOSITIONE D THE WIRE AND ADDED ANTI-CHAFE MATERIAL. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 2 L 7 2 4T RT A8SW 1996032200938 19960322 00938 CE 1996 3 22 S2YA960001 1 19960221 A 2436 51538001A GCU BEECH 1900 1900D 1154162 CE LEFT FAILED A S2YA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 GL 13 145SK 263 UE145 MKE - FLT 1099 - THE LT DC GENERATOR WOULD NOT RESET AFTER TAKEOFF, RETURNED TO MKE. MAINTENANCE REPLACED THE LT DC GEN ERATOR CONTROL UNIT, PARALLELED THE CIRCUIT, CHECKED FOR PROPER OPERATION, AND RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1996032200939 19960322 00939 CE 1996 3 22 S2YA960002 1 19960118 A 5533 12944006156 VENTRAL FIN BEECH 1900 1900D 1154162 CE AFT FUSELAGE DAMAGED A S2YA K NONE O OTHER UK UNKNOWN 1 GL 13 901SK 4212 UE90 MAINTENANCE FOUND THE AFT BOTTOM SIDES OF BOTH VENTRAL FINS DAMAGED FROM OVERROTATION RUNWAY CONTACT DURING AN INSPECTIO N. DO NOT KNOW AT WHAT POINT THIS TOOK PLACE, TAKEOFF OR LANDING. RECEIVED BEECH ENGINEERING APPROVAL FOR THE REPAIR, COMPLETED IT, AND FILED A FAA FORM 337. (X) 2 L 7 2 4T RT A24CE 1996032200940 19960322 00940 CE 1996 3 22 S2YA960003 1 19960228 A 3260 6839 BULBS BEECH 1900 1900D 1154162 CE GEAR ANNUNCIATOR FAILED A S2YA O OTHER P NO WARNING INDICATION LD LANDING 1 GL 13 145SK 2020 UE145 CMH - FLT 1829 - THE FLIGHT CREW NOTICED THE LT MAIN GEAR ANNUNCIATOR FAILED TO ILLUMINATE WITH GEAR HANDLE IN THE DOWN POSITION. AN EMERGENCY WAS DECLARED AND FLIGHT LANDED UNEVENTFULLY. MAINTENANCE REPLACED BOTH LAMPS IN THAT POSITION A ND ONE MORE IN ANOTHER, OPERATIONALLY CHECKED OKAY. (X) 2 L 7 2 4T RT A24CE 1996032200941 19960322 00941 EU 1996 3 22 SABA960005 1 19960207 A 5270 DOOR WARNING BAG JETSTM JETSTM3101 1500215 EU COCKPIT ILLUMINATED A SABA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 33 190PC 750 CLT/OAJ - FLT 5002 - DURING TAKEOFF, DOOR WARNING CAPTION ILLUMINATED. TAKEOFF ABORTED AND ACFT RETURNED TO THE GATE. M AINTENANCE WAS DISPATCHED TO TROUBLESHOOT THE PROBLEM. IT WAS DETERMINED THAT IT WAS AN INDICATION PROBLEM AND THE DOOR WARNING INDICATION SYSTEM WAS DEFERRED TO THE MSL PER MEL 52-2 UNDER CONTROL NR 0207-04C. ACFT RETURNED TO SERVICE. ON 2-8-96, THE DEFERRAL WAS CLEARED. THE MICROSWITCHES FOR THE DOOR WARNING SYSTEM WERE CLEANED AND LUBRICATED AND THE SY STEM OPERATIONALLY TESTED GOOD. (X) 2 L 7 2 4T RT A21EU 1996032200942 19960322 00942 EU 1996 3 22 SIMA960631 1 19960303 A 3397 WIRE AEROSP ATR42 ATR42300 8680920 EU CABIN BROKEN A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 421MQ 014 ORD - FLT 4164 - WIRE FOR ENTRANCE EMERGENCY LIGHT BROKEN BY PASSENGER. MAINTENANCE REPAIRED BROKEN WIRE. AIRCRAFT RET URNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1996032200943 19960322 00943 EU 1996 3 22 SIMA960651 1 19960305 A 7931 81071100010 TRANSMITTER AEROSP ATR72 ATR72212 EU NR 2 ENGINE FAILED A SIMA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SW 21 369AT 781 369 CRP - FLT 3739 - NR 2 ENGINE OIL PRESSURE WENT TO ZERO, LOW OIL PRESSURE LIGHT ON, NO ASSOCIATED MASTER WARNING. SHUT D OWN NR 2 AND RESTARTED PER CREW EMERGENCY PROCEDURE. COULD NOT DUPLICATE REPLACED TRANSMITTER. OPS CHECKED GOOD, AIRCR AFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1996032200944 19960322 00944 EU 1996 3 22 SIMA960652 1 19960305 A 3350 7980132 FUSE AEROSP ATR72 ATR72202 8680940 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 252AM 253 DFW - WHILE PARKED AT THE GATE, SEVERAL FLOOR PROXIMITY LIGHTS WERE FOUND INOPERABLE. REPLACED BALLAST UNIT FUSE. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1996032200945 19960322 00945 EU 1996 3 22 SIMA960653 1 19960305 A 3350 7980132 FUSE AEROSP ATR72 ATR72212 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 248AT 248 DFW - WHILE PARKED AT THE GATE, THE DEPARTING CREW FOUND SEVERAL EMERGENCY LIGHTS INOPERABLE. MAINTENANCE REPLACED THE POWER SUPPLY FUSE. OPS CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1996032200946 19960322 00946 SO 1996 3 22 SRAA29603 1 19960204 A 2150 203430 COOLING TURBINE LKHEED 382 382B 5264104 SO COCKPIT SEIZED A SRAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 907SJ 4248 HOW/CHS - FLT AD004 - DURING FLIGHT, FLIGHT DECK COOLING TURBINE SMOKES AND RATTLES, SYSTEM DEACTIVATED. REPLACED FLIGH T DECK AIR CONTITIONING COOLING TURBINE AND OPS CHECKED GOOD PER MM, CHAPTER 21. (X) 2 H 7 4 4T A1SO 1996032200947 19960322 00947 EU 1996 3 22 WTAA960039 1 19960221 A 5270 MS161065 SWITCH BAG JETSTM JETSTM3101 1500215 EU BAGG DOOR OUT OF ADJUST A WTAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 17 422UE 782 CIC - POD DOOR WARNING INDICATION ACTIVATED ON ROTATION. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. DETERMINED POD DOOR WAS SECURED WITH FALSE INDICATIONS ONLY. DEFERRED POD DOOR CAPTION PER MEL 52-1. AIRCRAFT RETURNED TO SERVICE. M AINTENANCE SUBSEQUENTLY CLEARED DEFERRED ITEM WITH THE ADJUSTMENT OF THE POD DOOR HANDLE MICROSWITCH. (X) 2 L 7 2 4T RT A21EU 1996032200948 19960322 00948 SO 1996 3 22 WTAA960045 1 19960225 A 2731 6225734002 SERVO EMB 120 EMB120RT SO COCKPIT JAMMED A WTAA O OTHER F FLT CONT AFFECTED DE DESCENT 1 WP 17 216YV 120216 FAT - TRIM 'FAIL' WARNING ACTIVATED DURING AIRCRAFT DESCENT. CREW DISENGAGED AUTOPILOT SYSTEM AND ATTEMPTED TO MANUALLY TRIM AIRCRAFT. UNABLE TO MOVE ELEVATOR TRIM FORWARD OF (MINUS 1) INDEX. MAINTENANCE CLEANED DEBRIS FROM ELECTRIC TRIM SERVO GEAR. ITEM SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1996032200949 19960322 00949 EU 1996 3 22 WTAA960046 1 19960223 A 3240 AC66868 REDUCING VALVE BAG JETSTM JETSTM3101 1500215 EU LT/RT BRAKE SYS FAILED A WTAA O OTHER L NO TEST LD LANDING 1 WP 17 422UE 782 FAT - WHEN TOE BRAKES APPLIED, NO BRAKE PRESSURE INCREASE ON LT OR RT GAUGE NOTED DURING BRAKE TEST PRIOR TO LANDING. T HREE TO FIVE SECOND DELAY IN BRAKE ACTIVATION NOTED FOLLOWING BRAKE PEDAL APPLICATION. MAINTENANCE REPLACED BRAKE REDUC ING VALVE. BRAKE SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A21EU 1996032200950 19960322 00950 EU 1996 3 22 WTAA960047 1 19960229 A 3260 9005EN38 SWITCH BAG JETSTM JETSTM3101 1500215 EU LT MLG BROKEN WIRE A WTAA O OTHER P NO WARNING INDICATION AP APPROACH 1 WP 17 413UE 797 BFL - LT MLG INTRANSIT LIGHTS FAILED TO ILLUMINATE ON GEAR EXTENSION. MAINTENANCE REPAIRED BROKEN WIRE AT LT MLG UPLOCK MICROSWITCH. GEAR INDICATION OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A21EU 1996032200951 19960322 00951 EU 1996 3 22 WTAA960048 1 19960303 A 5330 SKIN BAG JETSTM JETSTM3101 1500215 EU FWD FUSELAGE BIRD STRIKE A WTAA K NONE C F.O.D. LD LANDING 1 WP 17 419UE 779 STS - BIRD STRIKE REPORTED AT NOSE AREA OF AIRCRAFT ABOVE WINDSCREEN. MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECTION O N AIRCRAFT. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A21EU 1996032200952 19960322 00952 EU 1996 3 22 WTAA960049 1 19960304 A 5270 MS16106 SWITCH BAG JETSTM JETSTM3101 1500215 EU BAGG DOOR LOOSE A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 17 103XV 747 PSC - TAKEOFF ABORTED WITHOUT INCIDENT. POD DOOR WARNING LIGHT ACTIVATED DURING TAKEOFF ROLL. VERIFIED POD DOOR WAS CL OSED AND LATCHED. DEFERRED POD DOOR CAPTION PER MEL 52-1. AIRCRAFT RETURNED TO SERVICE. DEFERRED POD DOOR CAPTION SUB SEQUENTLY CLEARED BY ADJUSTING AND RESECURING POD DOOR MICROSWITCH. (X) 2 L 7 2 4T RT A21EU 1996032200955 19960322 00955 NM 1996 3 22 96FDEA00453 1 19960307 A 5315 FLOOR BEAM BOEING 727 727233 138408A NM BS 277 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 FLOOR BEAM AT BS 277, LBL 15, WL 208, IS GOUGED. **** S/D **** REMOVED DAMAGE, FAB AND INSTALLED REPAIR PARTS PER FEDEX SRM 51-40-4, FIG 1. 2 L 7 3 4F RT A3WE 1996032200956 19960322 00956 WP 1996 3 22 96FDEA00638 1 19960320 A 3211 TRUNNION FITTING DOUG DC10 DC1010F 3022111 WP RT MLG CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 RIGHT MAIN GEAR TRUNNION SUPPORT FTG FWD ATTACH, AFT LUG, EXHIBITS HEAVY CORROSION WITH PITTING ON FWD FACE WITH CORROSI ON INSIDE INTERNAL BORE. REF NR7049. CORROSION REMOVED AND BUSHING REPLACED PER SRM 57-20-00, PAGE 71. 2 L 7 3 4F A22WE 1996032200957 19960322 00957 NM 1996 3 22 96FDEA00639 1 19960321 A 7120 ENGINE MOUNT BOEING 727 727227 1384078 NM BS 1183 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 AIRSTAIRS, FWD ENGINE MOUNT CASTING ON 1183 BULKHEAD LT SIDE HAS APPROX 10 INCH CRACK. REPLACED NR 1 ENGINE FWD MOUNT I AW EA 7-5410-28015 DATED 3-19-96. THIS WAS IN TUL ON PAE CLARIFICATION. 2 L 7 3 4F A3WE 1996032200958 19960322 00958 NM 1996 3 22 96FDEA00640 1 19960215 A 5315 FLOOR BEAM BOEING 727 727227 1384078 NM BS 344 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 FLOOR BEAM UPPER CHORD LOWER SURFACE CORRODED STA 344, LBL 50 - RBL 10, WL 200. INSTALLED FLOOR BEAM REPAIR PER STANDA RD REPAIR DRAWING MANUAL SR 27-53-007. 2 L 7 3 4F A3WE 1996032200959 19960322 00959 NM 1996 3 22 96FDEA00641 1 19960305 A 5712 RIB CHORD BOEING 727 727227 1384078 NM WS 760 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 LEFT 760 RIB CHORD AT BL 70.5, TOP FWD HOLE IND CRACK. ENLARGED TOP FWD HOLE. INSTALLED REPAIR PER DRAWING 65-68492-17, ESO 11782, DATED 2-24-96 AND EA. 2 L 7 3 4F A3WE 1996032200960 19960322 00960 NM 1996 3 22 96FDEA00642 1 19960308 A 5711 SPAR CHORD BOEING 727 727227 1384078 NM WS 304 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 WS 304 RT WING 3RD STRINGER AFT OF FWD UPPER STAR CHORD CRACKED. REPAIRED STRINGER AT WS 304, 3RD FROM TOP FRONT SPAR C HORD. REPAIRED PER SRM 57-10-4. 2 L 7 3 4F A3WE 1996032200961 19960322 00961 NM 1996 3 22 96FDEA00643 1 19960314 A 5311 FRAME BOEING 727 72725C 138400H NM BS 440 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 FRAME CRACKED AT STA 480, STR 9L. INSTALLED FUSELAGE CROWN FRAME REPAIR, STA 440, STR 9L, PER SRM 53-10-4, PG 18. 2 L 7 3 4F A3WE 1996032200962 19960322 00962 NM 1996 3 22 96FDEA00645 1 19960303 A 5313 STRINGER BOEING 727 72725C 138400H NM FS 1080 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 CABIN UPPER LOBE STRINGER NR 1 IS CRACKED HALF WAY THROUGH FS 1080. CUT OUT DAMAGE AND INSTALLED SPLICE PER SRM 51-10-3 . 2 L 7 3 4F A3WE 1996032200963 19960322 00963 NM 1996 3 22 96FDEA00646 1 19960308 A 5751 CASTING BOEING 727 72725C 138400H NM RT AILERON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 RIGHT WING PIVOT BOLT HOLE FOR OUTBOARD AILERON QUAD CORRODED AT BOTTOM. REPLACED OUTBOARD AILERON LOCK-OUT SUPPORT CAS TING PER 51-10-1. 2 L 7 3 4F A3WE 1996032200964 19960322 00964 NM 1996 3 22 96FDEA00647 1 19960303 A 5315 FLOOR BEAM BOEING 727 72725C 138400H NM BS 480 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 CABIN FLOOR BEAM CRACKED/CORRODED ON UPPER FLANGE, BS 480, LBL 28. REPAIRED CRACKED/CORRODED FLOOR BEAM, STA 480, LBL 2 8, PER SRM 53-10-8, FIG 5. 2 L 7 3 4F A3WE 1996032200965 19960322 00965 NM 1996 3 22 96FDEA00648 1 19960228 A 5320 SKATE ANGLE BOEING 727 72725C 138400H NM NOSE COMPT CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 RIGHT FWD SKATE ANGLE NOSE COMPARTMENT HAS CORROSION ON FWD END. REMOVED AND REPLACED RT FWD SKATE ANGLE PER SRM 51-10- 1. 2 L 7 3 4F A3WE 1996032200966 19960322 00966 NM 1996 3 22 96FDEA00649 1 19960311 A 5315 FLOOR BEAM BOEING 727 72725C 138400H NM BS 740 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 CABIN, FS 740, FLOOR BEAM HAS HEAVY INTERGRANULAR CORROSION AT SCREW HOLE AND NUTPLATE 3.50 INCHES TO THE RT OF BL ZERO FLOOR TRACK, BOTTOM SIDE FLANGE. INSTALLED FLOOR BEAM REPAIR PER ESO AND EA NR 7-5310-27774. 2 L 7 3 4F A3WE 1996032200967 19960322 00967 NM 1996 3 22 96FDEA00650 1 19960311 A 5315 FLOOR BEAM BOEING 727 72725C 138400H NM FS 740 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 CABIN, FS 740, FLOOR BEAM HAS CORROSION DEVELOPING IN SCREW HOLE AND NUTPLATES (BOTTOM SIDE) BETWEEN BL 8 RT TO BL 53 RT . INSTALLED FLOOR BEAM REPAIR PER ESO AND EA NR 7-5310-27774. 2 L 7 3 4F A3WE 1996032200968 19960322 00968 NM 1996 3 22 96FDEA00651 1 19960313 A 5315 FLOOR BEAM BOEING 727 72725C 138400H NM FS 480 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 CABIN, FS 480, FLOOR BEAM HAS CORROSION AROUND FASTENER NUTPLATES, BOTTOM FLANGE BL 45 - BL 60R. INSTALLED FLOOR BEAM R EPAIR PER SRM 53-10-8. 2 L 7 3 4F A3WE 1996032200969 19960322 00969 NM 1996 3 22 96FDEA00652 1 19960314 A 5315 FLOOR BEAM BOEING 727 72725C 138400H NM BS 640 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 UPPER LOBE CORROSION ON FLOOR BEAM STA 640, BL ZERO - RBL 65. REPAIRED IAW SRM 53-10-8. 2 L 7 3 4F A3WE 1996032200970 19960322 00970 NM 1996 3 22 96FDEA00653 1 19960315 A 5315 FLOOR BEAM BOEING 727 72725C 138400H NM BS 312-328 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 STA 312 - STA 328, BL ZERO, LBL 22, FLOOR BEAM CORRODED ON UPPER SURFACE. INSTALLED FLOOR BEAM REPAIR PER SRM 53-10-8. 2 L 7 3 4F A3WE 1996032200971 19960322 00971 NM 1996 3 22 96FDEA00654 1 19960318 A 5330 SKIN BOEING 727 72725C 138400H NM BS 1130-1183 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 FUSELAGE PLATES CORRODED. REPAIR TO LT SKIN ASSY STA 1130 - STA 1183, STR 14 - STR 20L. REPETITIVE ULTRASONIC INSPECTI ON. SKIN REMOVED AND REPLACED PER EA 7-5330-22692, DATE 11-16-94. 2 L 7 3 4F A3WE 1996032200973 19960322 00973 NM 1996 3 22 96FDEA00656 1 19960315 A 5315 FLOOR BEAM BOEING 727 72725C 138400H NM BS 268 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 FLIGHT DECK FLOOR BEAM, STA 268, UPPER CHORD CORRODED AND PREVIOUS REPAIR NOT PER SRM LBL 2. REMOVED AND REPLACED FITTI NG IAW SRM 51-10-1. 2 L 7 3 4F A3WE 1996032200974 19960322 00974 NM 1996 3 22 96FDEA00657 1 19960317 A 5315 FLOOR BEAM BOEING 727 72725C 138400H NM BS 312 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 CABIN FLOOR BEAM AT STA 312, BL ZERO WAS FOUND TO BE OUT OF LIMITS AFTER CORROSION REMOVAL, BUT NO REPAIR WAS INSTALLED. REMOVED CORRODED AREA, FABRICATED FILLER AND INSTALLED REPAIR PER SRM 53-10-8. 2 L 7 3 4F A3WE 1996032200975 19960322 00975 NM 1996 3 22 96FDEA00658 1 19960305 A 5320 651759318 INTERCOSTAL BOEING 727 727233 138408A NM BS 256-277 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 INTERCOSTAL, WL 208, BS 256 - BS 277, LBL 14, IS CORRODED BEYOND LIMITS. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAI R PARTS PER FEDEX SRM 51-40-4, FIG 1. 2 L 7 3 4F RT A3WE 1996032200976 19960322 00976 WP 1996 3 22 96UAL900193 1 19960315 A 4900 APU GARRET 3810262MOD DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE APU COMPT MALFUNCTIONED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 1858U 90496700 46987 PUNGENT ODOR OF SMOKE IN AIRCRAFT ON ENGINE PNEUMATICS AT HIGH ENGINE POWER. ODOR ISOLATED TO NR 2 PNEUMATICS WHEN USIN G APU BLEED. REPLACED APU. 2 L 7 3 4F 4 F A22WE E23EA 1996032200977 19960322 00977 NM 1996 3 22 96UAL900194 1 19960315 A 2621 FIRE BOTTLE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CARGO COMPT DISCHARGED A UALA K NONE N FALSE WARNING NR NOT REPORTED 1 WP 29 611UA 21872 CARGO FIRE BOTTLE SWITCH LIGHT ILLUMINATED INDICATING DISCHARGE. INSTALL A THERMOCOUPLE DURING FUTURE BOTTLE SHOP VISIT S TO MORE ACCURATELY MEASURE BOTTLE TEMPERATURE, WHICH AFFECTS PROPER FILL PRESSURE OF THE BOTTLE. 2 L 7 2 4F 4 F RT A1NM E3NE 1996032200978 19960322 00978 NM 1996 3 22 96UAL900195 1 19960315 A 7931 54T25001 OIL PRESS TUBE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE CRACKED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 644UA 6162 25094 717654 CREW REPORTS NR 1 ENGINE OIL QUANTITY WENT TO '0'. ENGINE SHUTDOWN AND WINDMILLED FOR APPROX 30 MINUTES. OIL PRESSURE DURING WINDMILL 4-6 PSI. SUPPLEMENTAL DATA UPDATE: ANGLE GEARBOX OIL PRESSURE LINE CRACKED CAUSING LOSS OF OIL QUANTIT Y. REPLACED OIL PRESSURE LINE. 2 L 7 2 4F 4 F RT A1NM E24NE 1996032200979 19960322 00979 NM 1996 3 22 96UAL900196 1 19960318 A 3350 LAMP BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 610UA 21871 EMERGENCY LIGHT AFT OF DOOR 1R IS INOPERABLE. REPLACED LAMP, OPERATION CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 1996032200980 19960322 00980 WP 1996 3 22 96UAL900197 1 19960319 A 3350 BATTERY PACK DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1856U 46975 EMERGENCY LIGHT BATTERY TEST FAILED. AFT POWER SUPPLY LIGHT ILLUMINATED BELOW SECOND OFFICER'S DESK. REPLACED BATTERY PACK AND POWER SUPPLY. 2 L 7 3 4F 4 F A22WE E23EA 1996032200981 19960322 00981 NM 1996 3 22 96UAL900198 1 19960319 A 3350 BATTERY PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7253U 21400 EMERGENCY LIGHTS INOPERATIVE AT LT FUSELAGE AFT FAIRING. REPLACED BATTERY PACK. 2 L 7 3 4F 4 F A3WE E2EA 1996032200982 19960322 00982 EU 1996 3 22 96UAL900199 1 19960319 A 5270 PROXIMITY SENSOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FWD CARGO DOOR OUT OF ADJUST A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 416UA 479 AT FL 310, RECEIVED ECAM MESSAGE THAT FORWARD CARGO DOOR OPEN. NO PRESSURIZATION PROBLEM. SUPPLEMENTAL DATA: UPDATE P ROXIMITY SENSORS WERE FOUND OUT OF ADJUSTMENT. ADJUSTED SENSORS AND OPERATIONALLY CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 1996032200983 19960322 00983 EU 1996 3 22 96UAL900200 1 19960320 A 3230 DOWNLOCK IND AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LANDING GEAR MALFUNCTIONED A UALA O OTHER N FALSE WARNING AP APPROACH 1 WP 29 403UA 442 ON SHORT FINAL, GEAR SELECTED DOWN, DID NOT RECEIVE GEAR LOCKED INDICATION LIGHT. RECYCLED GEAR LEVER AND GEAR LOCKED. HEARD GURGLING SOUND FROM CENTER CONSOLE. FIRST OFFICER'S PFD AND ND WENT BLANK AND THEN CAME BACK UP WITH NO PILOT AC TION. *S/D* COULD NOT DUPLICATE PROBLEM ON GROUND. REPLACED GEAR DOOR SENSOR 38GA AND LANDING GEAR SELECTOR VALVE PRE CAUTIONARY, SYSTEM CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 1996032200984 19960322 00984 1996 3 22 96UAL900201 4 19960320 A 2565 D40659126 UPPER TUBE AIRCRUISERS D30656126 BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SLIDE/RAFT WORN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 584UA 0595 26706 SLIDE/RAFT REMOVED FOR FIRST TIME OVERHAUL AND FAILED THE AIR RETENTION TEST. ONE SCREW HEAD SECURING THE PRESSURE RELI EF VALVE WORE A HOLE THROUGH THE RELIEF VALVE CHAFE COVER, TUBE SEAM TAPE, 2 LAYERS OF TUBE FABRIC, AND THE TUBE FABRIC OPPOSITE THE TUBE SEAM. THE DAMAGED SLIDE/RAFT RETURNED TO ORIGINAL EQUIPMENT MANUFACTURER FOR WARRANTY REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 1996032200985 19960322 00985 NM 1996 3 22 96UAL900202 1 19960320 A 2133 10607047 OUTFLOW VALVE BOEING 737 737322 1384676 NM FWD FUSELAGE LEAKING A UALA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 WP 29 360UA 24453 ON CLIMBOUT, HAD LOUD FLUTTERING TYPE NOISE IN FORWARD AREA OF FUSELAGE. *S/D* REPLACED FLOW CONTROL VALVE, CHECKS OK. 2 L 7 2 4F RT A16WE 1996032200986 19960322 00986 NM 1996 3 22 96UAL900203 1 19960320 A 3350 STRIP BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 919UA 25386 FORWARD GALLEY EMERGENCY ESCAPE PATH LIGHTING INOP. REPLACED LIGHT STRIP. CHECKS O.K. 2 L 7 2 4F 4 F RT A16WE E2GL 1996032200987 19960322 00987 NM 1996 3 22 96UAL900204 1 19960320 A 5610 5893543109 WINDSHIELD BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE COCKPIT FAILED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 9069U 19950 NR 1 LEFT WINDSHIELD OUTER PANE SHATTERED. WINDOW HEAT TURNED OFF AND OPERATED AT REDUCED PRESSURIZATION. SUPPLEMENTAL DATA UPDATE: MOISTURE AT THE POWER BUS CAUSED SHORT AND CRACKED THE OUTER PANE. REPLACED WINDSHIELD. CHECKS O.K. 2 L 7 2 4F 4 F A16WE E2EA 1996032200988 19960322 00988 NM 1996 3 22 96UAL900205 1 19960320 A 3350 LIGHT STRIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 334UA 24229 EMERGENCY ESCAPE PATH LIGHTING INOP FROM ROW 11 AFT. REPLACED AFT CHARGER AND LIGHT STRIP IN GALLEY. CHECKS O.K. 2 L 7 2 4F 4 F RT A16WE E2GL 1996032200989 19960322 00989 1996 3 22 96UAL900206 4 19960320 A 2565 D40657122 TOP TUBE AIRCRUISERS D30654122 BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SLIDE/RAFT LEAKING A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 576UA 0412 26690 SLIDE RAFT REMOVED FOR FIRST TIME. CONTROLLED OVERHAUL AND FAILED AIR RETENTION TEST. SLIDE RAFT HAD POROSITY AT ALL S EAMS AND A SEAM LEAK AT THE TOP TUBE. RETURNED FAULTY SLIDE RAFT TO ORGINAL EQUIPMENT MANUFACTURER FOR WARRANTY REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 1996032200990 19960322 00990 1996 3 22 ARWA9603008 4 19960320 A 3446 20671570153 RT UNIT DOUG DC8 DC863F 302198F WP RADAR INOPERATIVE A ARWA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 661AV 45969 ON CLIMB-OUT OF MIAMI, RADAR WENT BLANK. RETURNED TO MIAMI. REMOVED AND REPLACED RADAR RECEIVING TRANSMITTING UNIT. O PS NORMAL.  PER¡ MM 34-40-1. 2 L 7 4 4F 4A25 1996032200991 19960322 00991 SO 1996 3 22 COMA9610107 1 19960318 A 3620 M1160140242 LEAK SENSOR EMB 120 EMB120RT SO LT DUCT DEFECTIVE A COMA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 SO 01 244CA 120217 LEFT DUCT LEAK WARNING ACTIVATED DURING FLIGHT. REPLACED DUCT LEAK SENSOR IN LT WING ROOT. 2 L 7 2 4T RT A31SO 1996032200992 19960322 00992 EU 1996 3 22 COMA9630071 1 19960319 A 2750 8519M3 CONTROL BOX SAAB SF340 SF340A 7850100 EU TE FLAPS MALFUNCTION A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 342CA 15669 63 340A023 FLAP CAUTION ON CWP AND FLAP DISAGREEMENT INDICTOR ON. REPLACED THE FLAP CONTROL BOX. PART TOTAL CYCLES, 17,240. 2 L 7 2 4T RT A52EU 1996032200993 19960322 00993 EU 1996 3 22 COMA9630072 1 19960319 A 3020 SM15CXD1 RELAY SAAB SF340 SF340A 7850100 EU RT ENGINE FAILED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 140N 340A140 RIGHT ENGINE INTAKE HEAT FAILED. REPLACED THE AC CONTROL RELAY. 2 L 7 2 4T RT A52EU 1996032200994 19960322 00994 NE 1996 3 22 COMA9630073 2 19960319 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RIGHT MALFUNCTIONED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 SO 01 357CA 1627 340A044 367209 RIGHT ENGINE ITT REACHED 931 DEGREES DURING TAKEOFF. REPLACED THE RT ENGINE. 2 L 7 2 4T 4 T RT A52EU E8NE6 1996032200995 19960322 00995 EU 1996 3 22 COMA9630074 1 19960318 A 2751 WARNING LIGHT SAAB SF340 SF340A 7850100 EU TE FLAPS FLASHES A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 359CA 340A053 FLAP DISAGREEMENT LIGHT FLASHES BRIEFLY WHEN FLAP SELECTOR IS MOVED. INFORMATION FROM ACFT AND FLAP SYSTEM MANUFACTURER (DOC. NR72LAWF-0LW) INDICATED THIS TO BE AN ACCEPTABLE CONDITION. ACFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 1996032200996 19960322 00996 EU 1996 3 22 COMA9630075 1 19960319 A 7712 7239060502 CTOT SAAB SF340 SF340A 7850100 EU INST PANEL DEFECTIVE A COMA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 146CA 14566 2762 340A146 RIGHT ENGINE TAILPIPE HOT WARNING SHORTLY AFTER TAKEOFF. POWER WAS REDUCED AND WARNING CEASED. WHEN POWER WAS ADVANCED , THERE WERE WILD FLUCTUATIONS IN TORQUE AND ITT. THE ENGINE WAS SECURED AND ACFT RETURNED TO FIELD. THE TORQUE AND IT T FLUCTUATIONS WERE DETERMINED TO BE CAUSED BY A DEFECTIVE CONSTANT TORQUE ON TAKEOFF PANEL. THE TAILPIPE HOT WARNING W AS DUE TO RAIN AND MOISTURE CONDITIONS. PART TOTAL CYCLES, 16,171. 2 L 7 2 4T RT A52EU 1996032200997 19960322 00997 NE 1996 3 22 DL72E960583 2 19960314 A 7321 FUEL CONTL UNIT 37820113 BOEING 727 727247 138408F NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE FAILED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK X ENGINE FLAMEOUT TO TAKEOFF 1 SO 27 2829W 2403 21481 665478 NR 1 ENGINE FLAMED-OUT AS TAKEOFF POWER WAS BEING APPLIED. C/A: REPLACED FCU AND FUEL PUMP. LEAK CHECKED AND RIGGED P ER PFHB. OPS CKS OK. 2 L 7 3 4F 4 F A3WE E2EA 1996032200998 19960322 00998 NM 1996 3 22 DL72K960612 1 19960318 A 5754 ATTACH ANGLE BOEING 727 727232 1384082 NM NR 2 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 412DA 21232 FOUND ON MV-1 CHECK, .3750 INCH CRACK IN COVE SKIN ATTACH ANGLE BELOW TIA DUCT OF NR 2 L/E SLAT. REPAIR: REPAIRED PER M/M 57-54-0, PG 807A. 2 L 7 3 4F A3WE 1996032200999 19960322 00999 1996 3 22 VNAA9600002 4 19960317 A 3460 7510100811 COMPUTER DORNER DO32 DO328100 2996000 NM NR 1 DEFECTIVE A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 425JS 3037 PIT - FLT 4077 - FMS DEAD RECKONING MODE ILLUMINATED ON THE ANNUNICATION PANEL. CREW ELECTED TO RETURN TO PIT. PIT MX REPLACED THE NR 1 NAVIGATION COMPUTER IAW MM 34.41.00. GROUND CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A45NM 1996032600001 19960326 00001 NM 1996 3 26 AALA960190 1 19960124 A 5711 111T1000 REAR SPAR BOEING 767 767223 1385123 NM WING CTR SECTION CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 313AA 22316 AFW - FOUND AND REMOVED CORROSION ON WING BOX REAR SPAR ASSY UPPER CHORD. CORROSION ALSO REMOVED FROM UPPER SKIN AT SAM E LOCATION AND LOWER CHORD TO FLOOR BEAM (T-EXTRUSION) WAS CUT TO REMOVE CORROSION. APPROVED AND REPAIRED PER INSTRUCTI ONS OF MRB 767-1116. TST: 42,562.49 HRS. CYCLES, 10,821. (X) 2 L 7 2 4F RT A1NM 1996032600002 19960326 00002 WP 1996 3 26 GRAA9622 1 19960222 A 3350 0816901 SOCKET DOUG DC9 DC987 3022087 WP CABIN BROKEN WIRE A GRAA K NONE L NO TEST IN INSP/MAINT 1 WP 11 1074T 49727 LINE MAINTENANCE AT RNO, DISCOVERED THAT THE EMERGENCY FLOOR LIGHT TRACK HAS 1 EACH RED LIGHT INOPERATIVE AT THE AFT OVE RWING EXIT. MAINTENANCE FOUND THAT THE RED LIGHT HAD A BROKEN WIRE ON THE LAMP SOCKET. MAINTENANCE REMOVED AND REPLACE D THE SOCKET. MAINTENANCE PERFORMED AN OPERATIONAL CHECK ON THE EMERGENCY LIGHT SYSTEM. THE SYSTEM CHECKED NORMAL. NO DEFECT NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A6WE 1996032900003 19960329 00003 WP 1996 3 29 9606449605 1 19960118 A 5330 SKIN DOUG DC9 DC932 3022066 WP FS 996 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 605NW 47223 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND 3, .0625 INCH CRACKS IN THE FUSELAGE SKIN FORWARD OF THE APB SPLICE AT FS 996 BETWEEN LONGERONS 4L TO 5L. REPAIRED SKIN (P/N 5911422) PER EA 99-103149. 2 L 7 2 4F A6WE 1996032900004 19960329 00004 WP 1996 3 29 9606459605 1 19960123 A 5330 SKIN DOUG DC9 DC932 3022066 WP FS 389-406 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 605NW 47223 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FUSELAGE SKIN FS 389 TO 406, LONGERONS 27R TO 28R. REPAIRED PANEL ASSEMBLY (P/N 5911412) PER EA 99-108803. 2 L 7 2 4F A6WE 1996032900005 19960329 00005 WP 1996 3 29 9606469605 1 19960123 A 5311 FRAME DOUG DC9 DC932 3022066 WP FS 148 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 605NW 47223 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION AT THE FS 148 FRAME AT LONGERON 8R. REPAIRED FRAME (P/N 9 911514) PER EA 99-108799. 2 L 7 2 4F A6WE 1996032900006 19960329 00006 WP 1996 3 29 9606479605 1 19960204 A 5320 TRAPEZOIDAL PNL DOUG DC9 DC932 3022066 WP RIGHT CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 605NW 47223 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE RIGHT TRAPEZOIDAL PANEL AFT FLANGE AT LONGERON 20R. R EPAIRED PANEL (P/N 9919402-2) PER EA 99-103135. 2 L 7 2 4F A6WE 1996032900007 19960329 00007 WP 1996 3 29 9606489605 1 19960206 A 5330 SKIN DOUG DC9 DC932 3022066 WP FS 1095 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 605NW 47223 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FUSELAGE SKIN AT FS 1095, LONGERON 18R. REPAIRED S KIN PER EA 99-108841. 2 L 7 2 4F A6WE 1996032900008 19960329 00008 WP 1996 3 29 9606499605 1 19960206 A 5711 SPAR DOUG DC9 DC932 3022066 WP WS 470-531 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 605NW 47223 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE RIGHT WING REAR SPAR LOWER T-CAP BETWEEN XRS 470 TO 531. REPAIRED T-CAP (P/N 5911302-502) PER EA 99-108804. 2 L 7 2 4F A6WE 1996032900009 19960329 00009 WP 1996 3 29 9606509605 1 19960208 A 5713 LONGERON DOUG DC9 DC932 3022066 WP WS 58.5 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 605NW 47223 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION AND CRACKS IN THE CENTER WING TANK STR 19 AND 21 AT THE WS 58.5 BULKHEAD. REPAIRED STRINGERS PER EA 99-108792. 2 L 7 2 4F A6WE 1996032900010 19960329 00010 WP 1996 3 29 9606519605 1 19960212 A 5531 SPAR WEB DOUG DC9 DC932 3022066 WP VERT STAB CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 605NW 47223 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE VERTICAL STABILIZER AFT SPAR WEB AT ZRS 65 AND 75. REPAIRED WEB (P/N 9911834-175) PER EA 99-108802. 2 L 7 2 4F A6WE 1996032900011 19960329 00011 WP 1996 3 29 9606529605 1 19960220 A 5311 FRAME DOUG DC9 DC932 3022066 WP FS 1121 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 605NW 47223 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION AT THE FS 1121 WEB JUST OUTBOARD OF LONGERON 1 LOOKING AFT . REPAIRED THE WEB (P/N 9911839-117) PER EA 99-108851. 2 L 7 2 4F A6WE 1996032900012 19960329 00012 NM 1996 3 29 9606532297 1 19960221 A 5315 FLOOR BEAM BOEING 727 727251 138408H NM FS 1130 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 297US 21789 DURING H-CHECK, FOUND CORROSION ON THE BS 1130 FLOOR BEAM UPPER CHORD FROM LBL 18 TO 43. REPAIRED CHORD PER EA 22-10346 6. 2 L 7 3 4F A3WE 1996032900013 19960329 00013 WP 1996 3 29 9606549605 1 19960222 A 5312 BULKHEAD DOUG DC9 DC932 3022066 WP FS 1046 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 605NW 47223 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FS 1046 CANTED BULKHEAD UPPER CAP BETWEEN LONGERONS 3L TO 6L. REPAIRED CAP PER EA 99-108995. 2 L 7 2 4F A6WE 1996032900014 19960329 00014 NM 1996 3 29 9606555523 1 19960228 A 5315 FLOOR BEAM BOEING 757 757251 1384970 NM FS 345-365 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 523US 23617 DURING PERIODIC CHECK, FOUND CORROSION ON THE UPPER SURFACES OF THE BS 345 FLOOR BEAM AT RBL 8 AND THE BS 365 FLOOR BEAM FROM BL 0 TO RBL 18. REPAIRED BOTH BEAMS (P/N 141N5111, 141N5112 RESPECTIVELY) PER EA 55-99500 AND -82879 RESPECTIVELY . 2 L 7 2 4F RT A2NM 1996032900015 19960329 00015 WP 1996 3 29 9606569308 1 19960304 A 5320 WEB DOUG DC9 DC982 3022082 WP FS 1123-1164 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 311RC 48089 DURING H-CHECK, FOUND CORROSION ON THE AFT CARGO FLOOR CUSP MEMBRANE FS 1123 AND 1164 AT LBL 56 TO 57. REPAIRED CUSP (P /N 9930612-43) PER EA 93-099546, -099543. 2 L 7 2 4F A6WE 1996032900016 19960329 00016 WP 1996 3 29 9606579308 1 19960304 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP FS 417-437 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 311RC 48089 DURING H-CHECK, FOUND CORROSION ON THE LEFT CARGO TRACK SPLICE AT FS 417 TO 437. REPAIRED TRACK (P/N 5936594-501) PER E A 93-099537. 2 L 7 2 4F A6WE 1996032900017 19960329 00017 NM 1996 3 29 9606585523 1 19960305 A 5320 SILL BOEING 757 757251 1384970 NM FS 1380-1440 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 523US 23617 DURING PERIODIC CHECK, FOUND CORROSION ON THE AFT CARGO DOOR LOWER SILL, INNER CHORD, BS 1380 TO 1440, RBL 26. REPAIRED SILL CHORD (P/N 146N8522-52) PER EA 55-103937. 2 L 7 2 4F RT A2NM 1996032900018 19960329 00018 NM 1996 3 29 9606595523 1 19960306 A 5320 CREASE BEAM BOEING 757 757251 1384970 NM FS 1627 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 523US 23617 DURING PERIODIC CHECK, FOUND CORROSION ON THE CREASE BEAM INBOARD CHORD BS 1627 AT LBL 60. REPAIRED CHORD (P/N 146N5590 ) PER EA 55-103961. 2 L 7 2 4F RT A2NM 1996032900019 19960329 00019 WP 1996 3 29 9606609308 1 19960307 A 5241 PAN DOUG DC9 DC982 3022082 WP GALLEY DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 311RC 48089 DURING H-CHECK, FOUND A CRACK IN THE FORWARD GALLEY DOOR LOWER HINGE CUTOUT PAN. REPAIRED PAN (P/N 5910084-159) PER EA 93-099539. 2 L 7 2 4F A6WE 1996032900020 19960329 00020 WP 1996 3 29 9606619979 1 19960310 A 5330 SKIN DOUG DC9 DC931 3022065 WP FS 370 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9343 47439 DURING LINE CHECK, FOUND A CRACK IN THE FORWARD CARGO DOOR JAMB UPPER FORWARD SKIN AT FS 370. REPAIRED SKIN PER EA 99-9 9563. 2 L 7 2 4F A6WE 1996032900021 19960329 00021 NM 1996 3 29 9606626634 1 19960311 A 5753 FITTING BOEING 747 747227B 1384888 NM RT TE MIDFLAP BROKEN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 634US 22234 DURING LINE CHECK, FOUND THE RIGHT INBOARD MIDFLAP DEFLECTION CONTROL FITTING BROKEN AND THE ROLLER BEARING MISSING. RE PLACED THE FITTING (P/N 65B02048-2) AND BEARING (P/N 60B00178-616). 2 L 7 4 4F A20WE 1996032900022 19960329 00022 WP 1996 3 29 9606639611 1 19960316 A 7120 ENGINE MOUNT DOUG DC9 DC932 3022066 WP NR 1 ENGINE RUSTED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 611NA 47435 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND RUST ON THE NR 1 ENGINE AFT MOUNT CONE FITTING ASSEMBLY. REPLACED A FT MOUNT PER MM 71-20-2. 2 L 7 2 4F A6WE 1996032900023 19960329 00023 WP 1996 3 29 9606649950 1 19960318 A 5320 FITTING DOUG DC9 DC932 3022066 WP FS 752-775 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9346 47376 DURING H-CHECK, FOUND CORROSION ON THE LONGERON 30 END FITTING FROM FS 752 TO 775. REPLACED THE FITTING PER SRM 51-30-2 , 51-30-5. 2 L 7 2 4F A6WE 1996032900024 19960329 00024 WP 1996 3 29 9606659610 1 19960104 A 5713 LONGERON DOUG DC9 DC932 3022066 WP WS 58-69 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 610NW 47432 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LEFT WING STRINGERS 11, 16, 17 AND ON RIGHT WING ST RINGERS 11, 12, 17, 18 APPROXIMATELY WS 58 TO 69. REPAIRED STRINGER PER EA 12-5713-9-C0660. 2 L 7 2 4F A6WE 1996032900025 19960329 00025 WP 1996 3 29 9606669602 1 19960106 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP FS 598 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 602NW 47046 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LEFT KEEL BEAM CENTER TANK FINGER DOUBLER FS 598. R EPAIRED DOUBLER PER EA 12-5330-9-C0700. 2 L 7 2 4F A6WE 1996032900026 19960329 00026 WP 1996 3 29 9606679602 1 19960111 A 5330 SKIN DOUG DC9 DC932 3022066 WP FS 617-680 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 602NW 47046 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FUSELAGE INNER SKIN BELOW THE LEFT AFT OVERWING EXI T FS 658 TO 680, LONGERON 16L AND BELOW THE RIGHT FORWARD OVERWING EXIT FS 617 TO 639, LONGERON 16R TO 17R. REPAIRED SK IN (P/N 5911416) PER EA 12-5330-9-C0704. 2 L 7 2 4F A6WE 1996032900027 19960329 00027 WP 1996 3 29 9606689610 1 19960112 A 5720 DOUBLER DOUG DC9 DC932 3022066 WP FS 617 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 610NW 47432 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE WING CENTER SECTION LOWER DOUBLER AT STR 21, FS 617 AT LBL 10. REPAIRED DOUBLER PER EA 12-5730-9-C0732. 2 L 7 2 4F A6WE 1996032900028 19960329 00028 WP 1996 3 29 9606699602 1 19960115 A 5510 STRINGER DOUG DC9 DC932 3022066 WP RT HORIZ STAB CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 602NW 47046 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE RIGHT HORIZONTAL STABILIZER UPPER STRINGERS 1 TO 9 BETWEEN XFS 15 TO 60. REPAIRED STRINGERS (P/N 5922578-501, 5922577-501 AND 5922576-501) PER EA 12-5510-9-C0705. 2 L 7 2 4F A6WE 1996032900029 19960329 00029 WP 1996 3 29 9606709602 1 19960205 A 5411 RIB DOUG DC9 DC932 3022066 WP LT PYLON CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 602NW 47046 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND 2, 2 INCH CRACKS IN THE LEFT ENGINE PYLON CLOSING RIB WEB. REPAIRED WEB PER EA 12-5410-9-C0782. 2 L 7 2 4F A6WE 1996032900030 19960329 00030 WP 1996 3 29 9606711149 1 19960221 A 5313 LONGERON DOUG DC10 DC1040 3023508 WP FS 1501-1521 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 149US 46758 DURING T-CHECK, FOUND CORROSION ON EXTERNAL LONGERONS 29R TO 31R FROM FS 1501 TO 1521. REPAIRED LONGERONS (P/N AEA7133- 2, 7132-2, AND 7136-2, RESPECTIVELY) PER EA 11-103946. 2 L 7 3 4F A22WE 1996032900031 19960329 00031 WP 1996 3 29 9606729912 1 19960320 A 3260 DNLOCK SWITCH DOUG DC9 DC931 3022065 WP RT MLG CONTAMINATED A NWAA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 01 962N 47406 DURING APPROACH INTO PIT, THE RIGHT MAIN LANDING GEAR GREEN LIGHT FAILED TO ILLUMINATE AFTER GEAR WAS EXTENDED. RECYCLE D GEAR AND NORMAL INDICATIONS WERE ACHIEVED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RIGHT MAIN GEAR D OWNLOCK SWITCH RECEPTACLE CONTAMINATED WITH DIRT. REPLACED SWITCH, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996032900032 19960329 00032 NM 1996 3 29 9606732704 1 19960319 A 3230 RETRACT MECH BOEING 727 727225 1384077 NM LT MLG MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 801EA 22432 DURING GEAR RETRACTION ON TAKEOFF, THE LEFT MAIN GEAR DID NOT RETRACT. RECYCLED GEAR ONCE AND GEAR INDICATION ON LEFT G EAR WAS NORMAL WITH DOOR DISAGREE INDICATION. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. DTW MAINTENANCE PE RFORMED INSPECTION AND GEAR RETRACTION AND EXTENSION OF LANDING GEAR SYSTEM, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996032900033 19960329 00033 NM 1996 3 29 9606746601 1 19960320 A 7722 R41012 CONDITION MOTOR BOEING 747 747151 1384891 NM PWA JT9 JT9D7A 52054 NE NR 3 ENGINE MALFUNCTIONED A NWAA E D ENGINE SHUTDOWN RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 01 601US 24228 348 19778 62689 DURING TAXIING, THE NR 3 ENGINE EXPERIENCED HOT START AND EGT CLIMBED TO 900 DEGREES. THE ENGINE WAS SHUTDOWN AND THE A IRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 3 ENGINE CONDITION MOTOR AND PERFORM ED RUNUP CHECK. RUNUP WAS NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4 F A20WE E20EA 1996032900034 19960329 00034 WP 1996 3 29 9606759912 1 19960320 A 3260 BULB DOUG DC9 DC931 3022065 WP RT MLG FAILED A NWAA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 01 962N 47406 DURING APPROACH INTO MSP, THE RIGHT MAIN LANDING GEAR GREEN LIGHT FAILED TO ILLUMINATE AFTER GEAR EXTENSION. RECYCLED G EAR AND NORMAL INDICATIONS WERE ACHIEVED. AIRCRAFT LANDED WITHOUT INCIDENT. RELAMPED TOP RIGHT MAIN GEAR GREEN INDICAT OR AND RESEATED BOTTOM BULB INTO SOCKET. OPERATIONAL CHECK NORMAL, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996032900035 19960329 00035 1996 3 29 9606769979 4 19960321 A 3422 FLUX VALVE DOUG DC9 DC931 3022065 WP LT WING TIP MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 9343 47439 DURING CLIMBOUT, HEADING LIGHT ON INSTRUMENT WARNING COMPARATOR ILLUMINATED. RESLAVED RMI'S BUT UNABLE TO MAINTAIN HEAD ING WITHIN 22 TO 25 DEGREES OF MAGNETIC COMPASS. DIRECTIONAL GYRO AND RMI'S DRIFT 20 TO 25 DEGREES OFF MAGNETIC COMPASS WITHIN 120 SECONDS. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED FLUX VALVE IN LEFT WING TIP. ALSO, REPLACED NR 1 AND NR 2 DIRECTIONAL GYROS. OPERATIONAL CHECK NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996032900036 19960329 00036 NM 1996 3 29 96DHL7219A1 1 19960312 A 5342 FORGING BOEING 727 727228 NM FS 1195 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AFT AIRSTAIRS VERTICAL FIN FRONT SPAR FORGING APPROX FS 1195 HAS CRACK INDICATIONS IN RADIUS OF LOWER FLANGE EXTENDING A PPROX 3 INCHES TO THE RIGHT OF SPLICE PLATE AT 6 O'CLOCK. STOP DRILLED CRACK. HFEC INSPECTION CONFIRMED CRACK ENDS AT STOP HOLE. FABRICATED AND INSTALLED .125 INCH, 15 INCH BY 15 INCH REPAIR ANGLE, PER AVITAS ENGINEERING ORDER NR 96PMSI 114RO-1. 2 L 7 3 4F A3WE 1996032900037 19960329 00037 WP 1996 3 29 96FDEA00603 1 19960319 A 3211 ARG7557501 TRUNNION PIN DOUG DC10 DC1010 3022110 WP RT MLG CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 RT MAIN GEAR FWD TRUNNION PIN REMOVED, FOUND TO BE CORRODED WITH 4 CIRCUMFERENTIAL CORROSION GROOVES .040 TO .080 DEEP T HROUGH HARD CHROME PLATE, REF NR7040. INSTALLED NEW PIN ON WORK CARD 32T-1501, PAGE 12 STEP 1. NEW BUSHINGS WERE INSTA LLED IN BOTH POSITIONS OF THE FWD TRUNNIONS ON NR 6126, 6127, 6128, 6131, 6132. 2 L 7 3 4F A22WE 1996032900038 19960329 00038 EU 1996 3 29 96FDEA00605 1 19960319 A 3244 TIRE TREAD AIRBUS 310 A310222 3930315 EU NR 2 MLG FAILED A FDEA K NONE C F.O.D. UK UNKNOWN 1 SO 25 420FE 339 NR 2 MLG TIRE MISSING A LITTLE TREAD AND FLAT. RUBBER WENT INTO THE NR 1 ENG INLET. NR 1 ENG HAS 8 FAN BLADES BENT NEA R L/E TIRE AREA. NR 1 ENG INLET HAS HOLE IN SOUND ABSORBING MATERIAL APPROX 1.5 BY 1.5 BY 2.5 INCH DEEP AT 11:30 POS 3 INCHES FWD OF FAN. NR 1 ENG LINER SEG DAMAGED BET 11 AND 12 O'CLOCK POS BETWEEN FAN AND EXIT VANES. REMOVED AND REPLAC ED NR 1 AND NR 2 MAIN WHEEL ASSYS. C/W FOD BORESCOPE INSP OF NR 1 ENG HP COMP STAGES 4, 5, 14 AND 15, NO DISC. BLENDED FAN BLADES PER PRATT AND WHITNEY MM 72-21-02 PG 601 TO 617. REMOVED AND REPLACED NOSE COWL PER MM 71-11-00 AND ALL SOU ND ABSORBING LINERS PER MM 72-23-05. C/W INSP AFTER TIRE BURST PER MM 05-51-15. 2 L 7 2 4F RT A35EU 1996032900039 19960329 00039 NM 1996 3 29 96FDEA00644 1 19960303 A 5313 STRINGER BOEING 727 72725C 138400H NM FS 1045 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 CABIN UPPER LOBE STRINGER NR 1 CRACKED THROUGH AT FS 1045. CUT OUT DAMAGE AND INSTALLED SPLICE PER SRM 51-10-3. 2 L 7 3 4F A3WE 1996032900040 19960329 00040 WP 1996 3 29 96FDEA00659 1 19960319 A 5512 SKIN DOUG DC10 DC1010CF 3023502 WP RT HORIZ STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 RT HORIZ STAB FWD UPPER PANEL HAS CRACK IND AT 2 FASTENER HOLES, FWD UPPER SPAR CAP AFT TANG, I/B OF CLOSING RIB PLANE, BEING THE 2ND AND 3RD HOLES. CRACK LENGTHS ARE APPROX .0937 TO .1875 INCH LONG AT THE PERIPHERY. C/W HFEC ON FWD SPAR UPPER REAR TANG NO DEFECTS NOTED. REPAIRED PER EA 8-5510-27090. 2 L 7 3 4F RT A22WE 1996032900041 19960329 00041 WP 1996 3 29 96FDEA00660 1 19960320 A 3211 TRUNNION FITTING DOUG DC10 DC1010F 3022111 WP RT MLG CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68052 47806 RT MAIN GEAR TRUNNION SUPPORT FTG FWD ATTACH FWD LUG, EXHIBITS CORROSION INSIDE INTERNAL BORE REF NR7048. 2 L 7 3 4F A22WE 1996032900042 19960329 00042 NM 1996 3 29 96FDEA00661 1 19960320 A 5320 ANGLES BOEING 727 727233 138408A NM BS 1183 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CORROSION ON LOWER 1183 RBL 25 VERTICAL BEAM ATTACH ANGLES UNDER DITCHING PAN. REMOVED ANGLE ATTACHED TO VERTICAL BEAM UNDER DITCHING PAN AND REPLACED WITH NEW ANGLE. 2 L 7 3 4F RT A3WE 1996032900043 19960329 00043 NM 1996 3 29 96FDEA00662 1 19960320 A 5311 FRAME BOEING 727 727233 138408A NM BS 460 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CORROSION (C53-224-01) BS 460 BETWEEN STR 4 AND 5R FRAME HAS CORROSION. REMOVED CORROSION AND REPAIRED FRAME BS 460 BET WEEN STR 4 AND 5R PER FEDEX EA 7-5310-27747. 2 L 7 3 4F RT A3WE 1996032900044 19960329 00044 NM 1996 3 29 96FDEA00663 1 19960320 A 5347 652363735 SEAT TRACK BOEING 727 727233 138408A NM BS 480-680 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CORROSION ALONG SEAT TRACK FLANGE AND AROUND FASTENERS IS OUT OF LIMITS BS 480 TO 680 RBL 45 WL 208. REMOVED AND REPLAC ED SEAT TRACK REF SRM 51-30-2. 2 L 7 3 4F RT A3WE 1996032900045 19960329 00045 NM 1996 3 29 96UAL900207 1 19960321 A 3350 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 520UA 24890 EMERGENGY ESCAPE LIGHTING INOP ROWS 24 TO 32 ABC. SECURED LEAD IN CONNECTOR AND OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996032900046 19960329 00046 NM 1996 3 29 96UAL900208 1 19960321 A 5313 655848825 STRINGER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE BS 943 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7263U 21410 AT APPROXIMATELY BODY STATION 943, STRINGER 18AL A CRACK WAS FOUND IN THE VERTICAL FLANGE OF THE 65-58488-25 STRINGER. R EPAIRED STRINGER PER SPLICE REPAIR DRAWING. 2 L 7 3 4F 4 F A3WE E2EA 1996032900047 19960329 00047 1996 3 29 96UAL900209 4 19960321 A 2565 HINGE TAPE BFGOODRICH 7A14182 BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE LT OUTBD BLKHD TORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 4727U G016 19883 DURING ROUTINE OVERHAUL OF SLIDE, FOUND TORN HINGE TAPE AT LEFT HAND OUTBOARD INTERNAL BULKHEAD. ADDITIONALLY FOUND BUL KHEAD SEPARATION EXTENDING APPROXIMATELY 2.5 INCHES FROM TOP END. UNIT SENT TO OEM FOR REPAIR. 2 L 7 4 4F 4 F A20WE E20EA 1996032900048 19960329 00048 NM 1996 3 29 SWAA960152 1 19960318 A 5315 FLOOR BEAM BOEING 737 7372H4 138448C NM BS 294/238 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 83SW 22732 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 294, RBL 36 AND RBL 46, WL 208. ALSO, AT BS 328, RBL 15 AND 2 5, WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996032900049 19960329 00049 NM 1996 3 29 SWAA960153 1 19960318 A 5312 BLKHD WEB BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 83SW 22732 DURING SCHEDULED D-CHECK, FOUND BULKHEAD 178 PRESSURE WEB CRACKED AT RBL 9.7, WL 219. ALSO, AT LBL 11.3, WL 219. REPAI RED PER BOEING SRM. 2 L 7 2 4F A16WE 1996032900050 19960329 00050 NM 1996 3 29 SWAA960155 1 19960318 A 5320 WEB BOEING 737 7372H4 138448C NM BS 726 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 83SW 22732 DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AT BS 726, STRINGER 18A, RBL 61, WL 188.25. ALSO, AT BS 530, RBL 43, WL 161 . REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996032900051 19960329 00051 NM 1996 3 29 SWAA960156 1 19960318 A 5320 BEAM BOEING 737 7372H4 138448C NM BS 616 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 83SW 22732 DURING SCHEDULED D-CHECK, FOUND INBOARD CREASE BEAM CRACKED AT BS 616, RBL 65, WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996032900052 19960329 00052 NM 1996 3 29 SWAA960157 1 19960318 A 5320 SUPPORT BOEING 737 7372H4 138448C NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 83SW 22732 DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CRACKED AT BS 540, BL 0 TO LBL 25, WL 208. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996032900053 19960329 00053 NM 1996 3 29 SWAA960158 1 19960318 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 83SW 22732 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKS AT BS 663, RBL 24 AND LBL 24. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996032900054 19960329 00054 NM 1996 3 29 SWAA960159 1 19960318 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 328 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 83SW 22732 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 328, RBL 55, BETWEEN S20R AND 21R. REPAIRED PER BOEING SRM . 2 L 7 2 4F A16WE 1996032900055 19960329 00055 NM 1996 3 29 SWAA960160 1 19960318 A 5320 SPLICE BOEING 737 7372H4 138448C NM BS 907 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 83SW 22732 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CORRODED AT AFT BAY AT BS 907, S25L, LBL 21, WL 168. REPLACED SECTION P ER BOEING SRM. 2 L 7 2 4F A16WE 1996032900056 19960329 00056 NM 1996 3 29 SWAA960161 1 19960318 A 5240 DOOR SKIN BOEING 737 7372H4 138448C NM FWD SERV CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 81SW 22730 DURING SCHEDULED B2-CHECK, FOUND FWD SERVICE DOOR CRACKED AT LOWER HINGE UPPER RADIUS AT PREVIOUS REPAIR. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996032900057 19960329 00057 NM 1996 3 29 SWAA960162 1 19960318 A 5312 BULKHEAD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 67SW 22356 DURING SCHEDULED 1/4 D-CHECK, FOUND BS 178 PRESSURE BULKHEAD CRACKED SEVERAL PLACES, AT LBL 5.7, WL 192 TO 198.5. REPAI RED PER BOEING SRM. 2 L 7 2 4F A16WE 1996032900058 19960329 00058 NM 1996 3 29 SWAA960163 1 19960318 A 5312 BULKHEAD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 67SW 22356 DURING SCHEDULED 1/4 D-CHECK, FOUND BS 178 PRESSURE BULKHEAD CRACKED 6 INCHES TO 7 INCHES AT WL 219 AND BL 15.5, O/B RT OF RADAR UNIT. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996032900059 19960329 00059 NM 1996 3 29 SWAA960164 1 19960318 A 5320 CEILING BOEING 737 7372H4 138448C NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 23SW 21338 DURING SCHEDULED TERM CHECK, FOUND NOSE WHEEL WELL CEILING CRACKED NEAR ATTACH BRACKET FOR NLG MANUAL EXTENSION EXT SPRI NG. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996032900060 19960329 00060 NM 1996 3 29 SWAA960165 1 19960319 A 5713 STRINGER BOEING 737 7372H4 138448C NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 56SW 21721 DURING SCHEDULED D-CHECK, FOUND CRACK INDICATIONS AT RT WING STRINGER 13R, WRL 91 TO WBL 94 LOWER RADIUS. REPAIRED PER BOEING SRM AND DRAWING 65C34533. 2 L 7 2 4F A16WE 1996032900061 19960329 00061 NM 1996 3 29 SWAA960166 1 19960319 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 56SW 21721 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, WL 209, BL 64 LEFT. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996032900062 19960329 00062 NM 1996 3 29 SWAA960167 1 19960319 A 5330 SKIN BOEING 737 7373H4 1384600 NM FWD SERV DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 328SW 23692 DURING SCHEDULED B/C2 CHECK, FOUND FWD SERVICE DOOR LOWER HINGE CUTOUT CRACKED .25 INCHES AT UPPER CORNER. REPAIRED PER SWA RA 1-352-242. 2 L 7 2 4F RT A16WE 1996032900063 19960329 00063 NM 1996 3 29 SWAA960168 1 19960319 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 310 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED SERVICE CHECK, FOUND 3 INCHES FUSELAGE SKIN CRACK AT BS 310 AT S25L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996032900064 19960329 00064 NM 1996 3 29 SWAA960169 1 19960319 A 3350 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED A2 CHECK, FOUND EMERGENCY EXIT LIGHTS AT OVERWING EXIT INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F A16WE 1996032900065 19960329 00065 EU 1996 3 29 WWMA9600029 1 19960321 A 3260 184925 UPLOCK SPRING BAG JETSTM JETSTM3201 1500217 EU RT MLG BROKEN A WWMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 15 948AE 948 CREW REPORTED, THE RIGHT RED INTRANSIT LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE GEAR WAS CYCLED DOWN AND A LL THREE GREEN DOWN AND LOCKED LIGHTS ILLUMINATED. THE AIRCRAFT RETURNED TO SBP AND LANDED WITHOUT INCIDENT. MAINTENAN CE FOUND THE RIGHT UPLOCK SPRING BROKEN, THE SPRING WAS REPLACED AND GEAR SWINGS PERFORMED. 2 L 7 2 4T RT A56EU 1996032900066 19960329 00066 NM 1996 3 29 96FDEA00432 1 19960305 A 5330 SKIN BOEING 727 727233 138408A NM BS 720 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 SKIN IS CHAFED AT LAP BS 720D PLUS 12 STR 19R. REPAIRED CHAFED SKIN AT LAP BS 720D PLUS 12 STR 19R PER FEDEX SRM 53-30- 03 FIG 14. 2 L 7 3 4F RT A3WE 1996032900067 19960329 00067 NM 1996 3 29 96FDEA00433 1 19960305 A 5330 SKIN BOEING 727 727233 138408A NM BS 720 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 SKIN IS CHAFED AT LAP BS 720D PLUS 12 STR 19L. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER AS PER FEDEX SRM 53-30-3. 2 L 7 3 4F RT A3WE 1996032900068 19960329 00068 NM 1996 3 29 96FDEA00678 1 19960321 A 5315 FLOOR BEAM BOEING 727 727233 138408A NM BS 1130 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CORROSION ON BS 1130 FLOOR BEAM RBL 55 TO LBL 55 WL 200 AT NUTPLATE HOLES. REPAIRED DAMAGED AREA ON BS 1130 FLOOR BEAM RBL TO LBL 55 WL 200 AT NUTPLATE HOLES PER FEDEX EA NR 7-5310-28075. 2 L 7 3 4F RT A3WE 1996032900069 19960329 00069 1996 3 29 96FDEA00679 2 19960322 A 7532 BLEED VALVE AIRBUS 310 A310203 EU NR 1 ENGINE FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 414FE 400 NR 1 BLEED VALVE FAULT LIGHT ILLUMINATED DURING CLIMBOUT. COMPLIED WITH BLEED VALVE FAULT PROCEDURE, NR 2 BLEED VALVE F AULT LIGHT ILLUMINATED. UNABLE TO SHUTOFF BLEED AIR FROM NR 1 ENG BLEED TEMP 270 DEGREES CELSIUS, 42 PSI WITH BLEED VAL VE HP VALVE AND CROSSFEED CLOSED, LEFT PACK STILL OPERATED. DEFERRED PER MEL 36-6 MX PROCEDURE 36-6 CARRIED OUT, CTL NR 0322040 EXP 4-1-96. 2 L 7 2 4F RT A35EU 1996032900070 19960329 00070 NM 1996 3 29 96FDEA00680 1 19960325 A 5320 FAIRING FORMERS BOEING 727 727233 138408A NM BS 740-846 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CORROSION (C53-132-01) ON FAIRING FORMERS BS 740 TO 846 WL 138.5 LBL TO RBL 10. REMOVED DAMAGED SECTION AND REPLACED WI TH NEW PARTS USING OLD PARTS AS A TEMPLATE AT BS 740 TO 846 WL 138.5 LBL TO RBL 10 IAW PER FEDEX SRM 51-10-1. 2 L 7 3 4F RT A3WE 1996032900071 19960329 00071 NM 1996 3 29 96FDEA00681 1 19960325 A 5230 OUTER SKIN BOEING 727 727233 138408A NM CARGO DOOR DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 MCD HAS 2 BULGES IN THE OUTER SKIN AT FWD AND AFT LIFT ACTUATORS. REWORKED BULGES ON MCD OUTER SKIN AT FWD AND AFT LIFT ACT TO WITHIN LIMITS AS PER DRAWING 52FX1435. ADJUSTED CLEARANCES BETWEEN MCD OUTER SKIN AND FWD AND AFT LIFT ACT ROD ENDS IAW FEDEX MM 52-34-9. 2 L 7 3 4F RT A3WE 1996032900072 19960329 00072 WP 1996 3 29 96UAL900210 1 19960322 A 5400 AUB7031 SPAR WEB DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 3 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 1857U 46986 NR 3 PYLON UPPER SPAR WEB HAD A CRACK INDICATION IN A FASTENER HOLE COMMON TO THE SPAR CHORD. REPAIRED PER DC-10 SRM 54 -20-00 FIGURE 27. 2 L 7 3 4F 4 F A22WE E23EA 1996032900073 19960329 00073 NM 1996 3 29 96UAL900211 1 19960322 A 2550 CARGO NET BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CARGO DOOR OUT OF POSITION A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 7450U 21904 CABIN PRESSURE BEGAN TO CLIMB AFTER TAKEOFF. NORMAL BLEED CONFIGURATION, BOTH PACKS ON. AUTO, STANDBY OR MANUAL COULD NOT PRESSURE CABIN. FLIGHT RETURNED TO DEN. FOUND FORWARD CARGO DOOR SEAL AT LOWER END OBSTRUCTED BY THE CARGO NET AND FASTENER. SECURED NET AS REQUIRED AND PRESSURE CHECKED OKAY. 2 L 7 3 4F 4 F A3WE E2EA 1996032900074 19960329 00074 WP 1996 3 29 ABXA9600359 1 19960321 A 3230 RETRACT MECH DOUG DC9 DC941 302207N WP NLG MALFUNCTIONED A ABXA O OTHER J WARNING INDICATION DE DESCENT 1 GL 23 957AX 47759 NOSE GEAR DID NOT COME OUT OF WELL, RECYCLED GEAR AND NOSE GEAR CAME DOWN. CHECKED NOSE GEAR LINKS AND MECHANISM, FOUND OK. PERFORMED RETRACTION CYCLE, CHECKED UP/DOWN FOR THREE TIMES. RETRACT OK, EXTENSION ON NOSE GEAR OK. THIS OPERATI ON DONE I/A/W DC9 MM. 2 L 7 2 4F A6WE 1996032900081 19960329 00081 WP 1996 3 29 ABXA9600366 1 19960324 A 5610 SLIDING WINDOW DOUG DC8 DC861 3021952 WP RT COCKPIT LACK OF LUBE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 842AX 46015 FIRST OFFICER'S SLIDING WINDOW WILL NOT OPEN. ADJUSTED AND LUBED FIRST OFFICER'S SLIDING WINDOW MECHANISM. OPS CHECK G OOD IAW DC8 MM, CHAPTER 56-10-03. 2 L 7 4 4F 4A25 1996032900082 19960329 00082 WP 1996 3 29 ABXA9600367 1 19960315 A 5313 LONGERON DOUG DC8 DC863 302198A WP BS 1200 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 812AX 45954 DURING C-CHECK INSPECTION, DISCOVERED AFT CROSS-SLIDE DOOR AREA AT STATION 1200, LONGERON 31R WAS CORRODED. REPAIRED C- 3 DOOR TORQUE BOX WEB AT AFT CROSS-SLIDE DOOR THAT WAS CORRODED AT STATION 1200, LONGERON 31R. 2 L 7 4 4F 4A25 1996032900083 19960329 00083 WP 1996 3 29 ABXA9600368 1 19960315 A 5412 30112SS FIREWALL DOUG DC8 DC863 302198A WP NR 1 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 812AX 45954 DURING C-CHECK INSPECTION, DISCOVERED NR 1 PYLON LOWER FORWARD FIREWALL CRACKED. REPAIRED NR 1 PYLON LOWER SPAR WEB ON FORWARD FIREWALL THAT WAS CRACKED IAW ABX REA D854-13627MR. 2 L 7 4 4F 4A25 1996032900084 19960329 00084 WP 1996 3 29 ABXA9600369 1 19960321 A 5320 SILL DOUG DC8 DC862 3021970 WP PNEU ACCESS DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 808AX 45954 DURING C-CHECK INSPECTION, DISCOVERED THE GROUND PNEUMATIC AIR CONNECTOR DOOR SILL CRACKED. FABRICATED DOUBLER FOR THE GROUND PNEUMATIC ACCESS DOOR THAT WAS CRACKED IAW ABX REA D853-13606MR. 2 L 7 4 4F 4A25 1996032900085 19960329 00085 WP 1996 3 29 ABXA9600370 1 19960321 A 5320 97540193 JAMB DOUG DC8 DC862 3021970 WP C 2 DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 808AX 45954 DURING C-CHECK INSPECTION, DISCOVERED THE FUSELAGE SKIN CRACKED APPROXIMATELY 1.5 INCHES AT FUSELAGE STATION 560, LONGER ON 33R, C-2 DOOR JAMB. FABRICATED C-2 DOOR JAMB WEB AT FUSELAGE STATION 560 AND LONGERON 33R IAW ABX REA D853-13607MR. 2 L 7 4 4F 4A25 1996032900086 19960329 00086 WP 1996 3 29 ABXA9600371 1 19960321 A 5320 JAMB DOUG DC8 DC862 3021970 WP C 4 DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 808AX 45954 DURING C-CHECK INSPECTION, DISCOVERED AFT CARGO COMPARTMENT, AFT DOOR CUTOUT SKIN HAS A VISIBLE .25 INCH CRACK FROM EDGE TO FASTENER HOLE JUST ABOVE SKIN RADIUS AT LOWER FORWARD CORNER. FABRICATED C-4 DOOR JAMB PAN SPLICE AT AFT DOOR CUTOU T SKIN IAW ABX REA D853-13608MR. 2 L 7 4 4F 4A25 1996032900087 19960329 00087 WP 1996 3 29 ABXA9600372 1 19960321 A 5753 HINGE DOUG DC8 DC862 3021970 WP RT TE FLAP CHAFED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 808AX 45954 DURING C-CHECK INSPECTION, DISCOVERED RIGHT HAND INBOARD FLAP HINGE, INBOARD ARM CHAFED. REPAIRED RIGHT HAND INBOARD FL AP HINGE FITTING IAW ABX REA D857-13609MR. 2 L 7 4 4F 4A25 1996032900088 19960329 00088 WP 1996 3 29 ARWA9603009 1 19960323 A 7931 OIL PRESS LIGHT DOUG DC8 DC862 3021970 WP PWA JT3D JT3D7 52039 NE NR 4 ENGINE FLICKERED A ARWA E ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 SO 19 1803 45895 P678993 ON DESCENT, NR 4 ENGINE OIL PRESSURE LIGHT FLICKERED, OIL PRESSURE FLUCTUATED, OIL QUANTITY WENT DOWN TO ZERO. SHUTDOWN AND SECURED ENGINE. WINDMILLING PRESSURE 14 PSI FOR 17 MINUTES. UPON ARRIVAL CHECKED OIL QUANTITY, INDICATOR READS 5 GALLONS, CHECKED OIL TANK, FOUND FULL; CHECKED TAIL PIPE, NO OIL FOUND; CHECKED INLET, NO OIL FOUND. REMOVED AND REPLAC ED OIL SCREEN FOR PRECAUTION AS PER MM74-20-7. OPS AND LEAK CHECKED NORMAL ON ENGINE RUN AS PER ARROW J/C NR 6527. UNA BLE TO DUPLICATE, NO LEAKS NOTED, NO OIL ADDED. 2 L 7 4 4F 4 F 4A25 1E8 1996032900089 19960329 00089 SO 1996 3 29 COMA9610108 1 19960321 A 2731 ATG120TR PROX SENSOR EMB 120 EMB120RT SO ELEV TRIM TAB FAILED A COMA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 164D 120164 TAKEOFF TRIM AURAL WARNING SOUNDS WHEN TRIM IS CORRECTLY SET IN TAKEOFF RANGE. REPLACED THE ELEVATOR TRIM TAB PROXIMITY SENSOR. 2 L 7 2 4T RT A31SO 1996032900090 19960329 00090 SO 1996 3 29 COMA9610109 1 19960323 A 5753 KRP138112VT ROLLERS EMB 120 EMB120RT SO RT TE FLAP WORN A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 200CD 120200 FLAPS DISAGREEMENT WARNING AFTER TAKEOFF WHEN FLAPS SELECTED UP. REPLACED WORN ROLLERS AND TRACKS ON RT INBD FLAP. 2 L 7 2 4T RT A31SO 1996032900091 19960329 00091 SO 1996 3 29 COMA9610110 1 19960322 A 3260 UPLOCK SENSOR EMB 120 EMB120RT SO LT MLG OUT OF ADJUST A COMA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 256CA 120245 LT MLG INTRANSIT LIGHTS REMAINED ON AFTER GEAR RETRACTED. ADJUSTED THE UPLOCK PROXIMITY SENSOR TO M/M SPECIFICATIONS. 2 L 7 2 4T RT A31SO 1996032900092 19960329 00092 SO 1996 3 29 COMA9610111 1 19960322 A 3242 214791 BRAKE EMB 120 EMB120RT SO LT MLG WORN A COMA K NONE O OTHER LD LANDING 1 SO 01 159A 9698 1505 120159 LEFT ANTI-SKID INOP WARNING DURING LANDING. LT MLG OUTBD TIRE FOUND FLAT DURING POST FLIGHT. REPLACED THE LT MLG OUTBD BRAKE ASSY. 2 L 7 2 4T RT A31SO 1996032900093 19960329 00093 SO 1996 3 29 COMA9610112 1 19960320 A 3010 295705135 DE-ICE BOOTS EMB 120 EMB120RT SO EMPENNAGE LEAKING A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 249CA 120230 HORIZONTAL AND VERTICAL STABILIZER DE-ICE SYSTEM FAILED. REPLACED THE VERTICAL AND RT HORIZONTAL STABILIZER DE-ICE BOOT S. 2 L 7 2 4T RT A31SO 1996032900094 19960329 00094 EU 1996 3 29 COMA9630076 1 19960321 A 3260 AIR123273 WOW HARNESS SAAB SF340 SF340A 7850100 EU LT MLG FAILED A COMA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 380CA 340A012 LANDING GEAR SELECTOR COULD NOT BE SELECTED TO UP POSITION UNLESS OVER RIDE BUTTON ACTUATED. REPLACED DEFECTIVE WEIGHT ON WHEELS HARNESS SWITCH ASSY ON LT MLG. 2 L 7 2 4T RT A52EU 1996032900095 19960329 00095 EU 1996 3 29 COMA9630077 1 19960321 A 7603 POWER LEVERS SAAB SF340 SF340A 7850100 EU RT ENGINE OUT OF ADJUST A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 146CA 340A146 RT ENGINE POWER LAGGED BEHIND LEFT ENGINE DURING TAKEOFF. ADJUSTED THE LEFT ENGINE POWER AND CONDITION CONTROLS TO M/M SPECIFICATIONS. 2 L 7 2 4T RT A52EU 1996032900096 19960329 00096 EU 1996 3 29 COMA9630078 1 19960322 A 2742 DL3827M157 ACTUATOR SAAB SF340 SF340A 7850100 EU LT PITCH TRIM FAILED A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 158CA 13286 160 340A158 THE MAIN PITCH TRIM IS INOP. REPLACED THE PITCH TRIM ACTUATOR. 2 L 7 2 4T RT A52EU 1996032900097 19960329 00097 EU 1996 3 29 COMA9630079 1 19960321 A 2710 AIL CONTROLS SAAB SF340 SF340A 7850100 EU LT/RT WINGS LACK OF LUBE A COMA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 343CA 340A024 AILERON CONTROLS ARE BINDING. BINDING IS MORE PRONOUNCED IN RT TURNS. CLEANED AND LUBRICATED AILERON SYSTEM, NO DEFECT S FOUND. FIGHT CHECK SATISFACTORY. 2 L 7 2 4T RT A52EU 1996032900098 19960329 00098 EU 1996 3 29 COMA9630080 1 19960320 A 2420 WIRE SAAB SF340 SF340A 7850100 EU LT AC GENERATOR CHAFED A COMA O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION NR NOT REPORTED 1 SO 01 341CA 340A021 LEFT AC GENERATOR FAILED IN FLIGHT. REPAIRED WIRE NR XA510, XA509, XA508 AT WING FLAP INTERCONNECT AREA. WIRING WAS CH AFED AND BURNED. 2 L 7 2 4T RT A52EU 1996032900099 19960329 00099 EU 1996 3 29 COMA9630081 1 19960320 A 2750 8519M3 CONTROLLER SAAB SF340 SF340A 7850100 EU TE FLAPS DEFECTIVE A COMA K NONE J WARNING INDICATION UK UNKNOWN 1 SO 01 342CA 17447 340A023 FLAP DISAGREEMENT INDICATOR ON. REPLACED THE FLAP CONTROLLER. 2 L 7 2 4T RT A52EU 1996032900100 19960329 00100 EU 1996 3 29 COMA9630082 1 19960322 A 2750 HP14161005 CONTROL VALVE SAAB SF340 SF340A 7850100 EU TE FLAPS FAILED A COMA K NONE J WARNING INDICATION UK UNKNOWN 1 SO 01 347CA 7119 340A028 FLAP DISAGREEMENT WARNING INDICATOR ON, FLAPS STUCK IN DOWN POSITION. REPLACED THE FLAP CONTROL VALVE. 2 L 7 2 4T RT A52EU 1996032900101 19960329 00101 EU 1996 3 29 COMA9630083 1 19960325 A 3246 5009237 INNER RACE LORAL 5010488 SAAB SF340 SF340A 7850100 EU LT MLG SPUN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 357CA 4817 536 340A044 MECHANIC REMOVED WHEEL ASSY DUE TO TIRE WORN TO LIMITS. DURING VISUAL INSPECTION FOUND INNER RACE SPUN. SUBASSY HAS BE EN REMOVED FROM SERVICE AND SENT TO ABS FOR REPAIR. 2 L 7 2 4T RT A52EU 1996032900102 19960329 00102 EA 1996 3 29 COMA9660049 1 19960321 A 7400 IGNITION FERRULE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RT ENGINE MISSING A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 920CA 7022 807084 RT ENGINE COMBUSTION LINER, IGNITION FERRULE, FOUND MISSING DURING A CHECK INSP. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 1996032900103 19960329 00103 EA 1996 3 29 COMA9660050 1 19960320 A 2750 RETRACT SYSTEM CNDAIR CL600 CL6002B19 EA TE FLAPS FAILED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 915CA 7013 FLAPS FAIL MESSAGE ON EICAS. THIS DISCREPANCY WAS INTERMITTENT AND EXTENSIVE TROUBLESHOOTING AND COMPONENT REPLACEMENTS FAILED TO ELIMINATE PROBLEM. THE ENTIRE FLAPS SYSTEM WAS REPLACED WHICH INCLUDED ALL MECHANICAL, ELECTRICAL AND ELECTR ONIC COMPONENTS AND THEIR WIRING HARNESS. 2 L 7 2 4F RT A21EA 1996032900104 19960329 00104 NE 1996 3 29 COMA9660051 2 19960321 A 7230 6018T30P06 FAN BLADES CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LT ENGINE FOD DAMAGE A COMA K NONE C F.O.D. IN INSP/MAINT 1 SO 01 929CA 7035 807109 LEFT ENGINE FAN SECTION HAS FOD DAMAGE. REPLACED 5 SETS OF FAN BLADES. 2 L 7 2 4F 4 F RT A21EA E15NE 1996032900105 19960329 00105 EA 1996 3 29 COMA9660052 1 19960321 A 7332 FUEL PRESS LIGHT CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LEFT ILLUMINATED A COMA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 915CA 7013 LEFT LOW FUEL PRESSURE CAUTION MESSAGE ON EICAS. BLEED AIR FROM PRESSURE SWITCH LINES. 2 L 7 2 4F 4 F RT A21EA E15NE 1996032900106 19960329 00106 NM 1996 3 29 DL72K960621 1 19960320 A 3350 LIGHT BOEING 727 727232 1384082 NM AFT AIRSTAIRS INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 491DA 21060 EMERGENCY LIGHT INOP ABOVE AFT AIRSTAIR. REPLACED LIGHT ASSY PER MAINTENANCE MANUAL, OPS TESTS OK. 2 L 7 3 4F A3WE 1996032900107 19960329 00107 NM 1996 3 29 DL72K960623 1 19960318 A 5754 RIB BOEING 727 727232 1384082 NM NR 2 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 412DA 21232 FOUND ON MV1 CHECK, NR 2 SLAT (S/N BN1110) HAS .5 CRACKS IN INBD AND OUTBD NOSE RIBS ADJACENT TO ACTUATOR ROD END. REPA IRED PER M/M 57-54-0 PG 805. 2 L 7 3 4F A3WE 1996032900108 19960329 00108 NM 1996 3 29 DL72L960615 1 19960320 A 2761 659892423 ANGLE BOEING 727 727232 1384082 NM NR 4 SPOILER ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 514DA 21430 THE NR 4 SPOILER ACTUATOR ATTACH FITTING WAS REPLACED DUE TO A CRACK FOUND IN THE O/B FITTING. ALL WORK DONE PER SRM 5 7-50-6. 2 L 7 3 4F A3WE 1996032900109 19960329 00109 NE 1996 3 29 DL72L960622 2 19960320 A 7230 COMPRESSOR BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE STALLED A DALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 27 505DA 21307 687674 APPLYING TAKEOFF POWER HAD EXPERIENCED COMPRESSOR STALLS ON NR 2 ENG, WIND WAS APPROX 320 AT 17 TO 20 KTS, DEPARTED 35L DFW. AFTER TAKEOFF COMPRESSOR STALLS RETURNED ON CLIMBOUT AT 190 KTS. REPLACED PRBC AND P AND D VLV, NO HELP. ACTVAT ED 6TH STAGE BLEED PER M/M, RAN ENGINE AND OPN NORMAL. ALSO, BORESCOPED ENG 6, 7 AND 13TH STG HP COMPRESSOR AND NO TROU BLE FOUND. 2 L 7 3 4F 4 F A3WE E2EA 1996032900110 19960329 00110 NM 1996 3 29 DL72L960636 1 19960322 A 2782 1U109592 ACTUATOR BOEING 727 727232 1384082 NM NR 8 SLAT FAILED A DALA O OTHER J WARNING INDICATION CR CRUISE 1 SO 27 504DA 41297 21306 AFTER TAKEOFF, AMBER LE FLAP LIGHT REMAINED ON AND NR 8 SLAT AMBER LIGHT ON S/O PNL. ON RETURN TO LAX LE FLAPS LIGHT ST AYED ON, BUT ALL SLATS/FLAPS POS TEST SHOWS RETRACTED. RAN TEST USING TEST BOX 10M2425 PER M/M AND NR 8 SLAT ACTUATOR F AILED TEST. REPLACED NR 8 SLAT ACTUATOR AND OPS CK NORMAL PER M/M. 2 L 7 3 4F A3WE 1996032900111 19960329 00111 NM 1996 3 29 DL72L960639 1 19960322 A 2782 ATTACH FITTING BOEING 727 727232 1384082 NM NR 1 SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 506DA 21308 DURING D-1 LETTER CHECK, FOUND .5 INCH CRACK IN NR 1 SLAT ACTUATOR O/B ATTACH FITTING. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1996032900112 19960329 00112 NM 1996 3 29 DL72L960640 1 19960322 A 2782 ATTACH FITTING BOEING 727 727232 1384082 NM NR 1 SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 506DA 21308 A .5 INCH CRACK IN NR 1 SLAT ACTUATOR I/B ATTACH FITTING. FOUND DURING D-1 LETTER CHECK. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1996032900113 19960329 00113 NM 1996 3 29 DL72L960641 1 19960322 A 5754 RIB BOEING 727 727232 1384082 NM NR 3 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 506DA 21308 FOUND DURING D-1 LETTER CHECK, NR 3 L/E SLAT NOSE RIB CRACKED 1 INCH ON I/B AND O/B SIDES. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1996032900114 19960329 00114 NM 1996 3 29 DL72L960642 1 19960322 A 5754 SKIN BOEING 727 727232 1384082 NM NR 2 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 506DA 21308 A .25 INCH CRACK IN COVE SKIN LOWER ATTACH ANGLE BELOW NR 2 SLAT ACTUATOR ROD. FOUND DURING D-1 LETTER CHECK. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1996032900115 19960329 00115 NM 1996 3 29 DL72S960626 1 19960321 A 3350 BULB BOEING 727 727232 1384082 NM AFT GALLEY FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 544DA 22493 AFT GALLEY DOOR EXIT LIGHT INOP. RELAMPED, OPERATION NORMAL. 2 L 7 3 4F A3WE 1996032900116 19960329 00116 NM 1996 3 29 DL72S960629 1 19960321 A 2782 ANGLE BOEING 727 727232 1384082 NM NR 4 LE FLAP ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 499DA 21143 FOUND DURING A-1 LETTER CHECK, .75 INCH CRACK NR 4 KRUEGER FLAP ACTUATOR MOUNT BOX AT UPPER I/B FWD CORNER. REPA IRED PER M/M 57-20-21. 2 L 7 3 4F A3WE 1996032900117 19960329 00117 NM 1996 3 29 DL72S960630 1 19960321 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 5 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 499DA 21143 FOUND DURING A-1 LETTER CHECK, NR 5 L/E SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED AT I/B UPSTOP PAD. REPAIRED PER M/M 5 7-54-0 PAR 12. 2 L 7 3 4F A3WE 1996032900118 19960329 00118 NM 1996 3 29 DL72S960631 1 19960321 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 7 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 499DA 21143 FOUND DURING A-1 LETTER CHECK, NR 7 L/E SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED AT I/B UPSTOP PAD. REPAIRED PER M/M 5 7-54-0 PAR 12. 2 L 7 3 4F A3WE 1996032900119 19960329 00119 NM 1996 3 29 DL72S960634 1 19960321 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 5 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 499DA 21143 DURING LETTER CHECK, NR 5 L/E SLAT AFT ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER MM 57-54-0 PAR 12. 2 L 7 3 4F A3WE 1996032900120 19960329 00120 NM 1996 3 29 DL72S960637 1 19960319 A 5744 ACTUATOR BOLTS BOEING 727 727232 1384082 NM NR 13 SPOILER LOOSE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 520DA 21471 AT MV-2 VISIT, FOUND NR 13 SPOILER ACT LUGS LOOSE RT WING. REPAIRED MOUNT BOLTS WHERE THEY ATTACH TO VERTICAL ANGLES ON REAR SPAR PER MM 57-42-0. 2 L 7 3 4F A3WE 1996032900121 19960329 00121 NM 1996 3 29 DL72S960643 1 19960323 A 3350 BULB BOEING 727 727232 1384082 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 406DA 21150 EMERGENCY TRACK LIGHTING UNDER SEAT 31D IS OUT. RELAMPED BULB, CKS NORMAL. 2 L 7 3 4F A3WE 1996032900122 19960329 00122 NM 1996 3 29 DL72S960650 1 19960321 A 5754 WEB BOEING 727 727232 1384082 NM NR 8 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 520DA 21471 FROM MV-2 ATL, I/B WEB IS CRACKED ON NR 8 SLAT. FABRICATED AND INSTALLED DOUBLER PER M/M 57-54-0 FIG 814. 2 L 7 3 4F A3WE 1996032900123 19960329 00123 NM 1996 3 29 DL72W960592 1 19960316 A 3232 ATTACH FITTING BOEING 727 727247 138408F NM LT MLG DR ACT BROKEN A DALA O OTHER J WARNING INDICATION CR CRUISE 1 SO 27 2809W 20581 LT MAIN LANDING GEAR DOOR OPENED IN FLIGHT. FOUND LANDING GEAR DOOR ACTUATOR ATTACH FITTING BROKEN, IPC 32-10-4 FIG 2 I TEM 250. 2 L 7 3 4F A3WE 1996032900124 19960329 00124 NM 1996 3 29 DL733960632 1 19960321 A 3350 TRACK LIGHTS BOEING 737 737347 1384647 NM CABIN INOPERATIVE A DALA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 27 309WA 23442 ON AIRCRAFT ARRIVAL, EMERGENCY PATH TRACK LIGHTING INOP. CONTRACT MTC CALLED OUT, PARTS SENT BUT WERE UNABLE TO CORRECT PROBLEM. FLIGHT FERRIED TO DFW. REPLACED AFT CABIN FLOOR TRACK LIGHTING POWER SUPPLY AND BATTERIES, REPLACED BOTH AFT EMRGENCY LIGHTING POWER SUPPLY AND BATTERIES, OPERATION NORMAL. 2 L 7 2 4F RT A16WE 1996032900125 19960329 00125 NM 1996 3 29 DL73S960620 1 19960320 A 5210 DOOR BOEING 737 737232 1384475 NM L 1 JAMMED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 331DL 23103 DURING EVAC OF AIRCRAFT, THE LEFT NR 1 DOOR WOULD NOT OPEN ALL OF THE WAY. DOOR CHECKS GOOD PER MM 52-11-00, OPENED DO OR DEPLOYED AND INFLATED SLIDE OPS NORMAL. REPLACED SLIDE. 2 L 7 2 4F RT A16WE 1996032900126 19960329 00126 NM 1996 3 29 DL757960597 1 19960317 A 2120 AIR DISTR BOEING 757 757232 1384965 NM CABIN ODOR A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 613DL 22820 BURNING ELECT/RUBBER SMELL IN CABIN AREA, SUSPECT OVERHEAD READING PNL. REMOVED POWER FROM BOTH UTILITY BUSSES. SMELL WAS MOST PRONOUNCED ON THE LT OF THE CABIN AROUND SEAT ROW 35/36. CHECKED CABIN WITH ALL LEVELS OF LIGHT AND FAN OPERAT ION UNABLE TO DETECT ANY LOCALIZED HEAT AREAS OR SMELL ANYWHERE THROUGHT THE CABIN. 2 L 7 2 4F RT A2NM 1996032900127 19960329 00127 NM 1996 3 29 DL767960638 1 19960322 A 2530 COFFEE MAKER BOEING 767 767232 1385132 NM NR 3 FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 101DA 22213 SMOKE AND HOT SMELL IN AFT GALLEY. HOT WATER COMING OUT OF COLD WATER FAUCET UNDER LT SIDE COFFEE MAKERS. FOUND NR 3 C OFFEE MAKER OVERHEATING. PULLED AND COLLARED C/B. FWD TO MCO AND PLAC. REPLACED COFFEE MAKER, OPERATION NORMAL. 2 L 7 2 4F RT A1NM 1996032900128 19960329 00128 NM 1996 3 29 DL76S960644 1 19960323 A 3350 CONNECTOR BOEING 767 767332 1382001 NM R1 DOOR DIRTY A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 125DL 24075 EXTERIOR EMERGENCY LIGHT AFT OF R-1 DOOR INOP. RELAMPED. RIGHT OVERWING EXTERIOR EMERGENCY LIGHT INOP. CLEANED LIGHT CONTACT. 2 L 7 2 4F RT A1NM 1996032900129 19960329 00129 WP 1996 3 29 DLL10960624 1 19960321 A 3350 BATTERY PACK 5165741 LKHEED 1011 10113851 5265010 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 717DA 37146 193C1096 AFT RT EMERGENCY LIGHTS INOP. REPLACED CHARGER/BATTERY ASSEMBLY. 2 L 7 3 4F A23WE 1996032900130 19960329 00130 WP 1996 3 29 DLL10960625 1 19960321 A 3350 TRACK LIGHT LKHEED 1011 10113851 5265010 WP CABIN DAMAGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 717DA 193C1096 D-ZONE FWD RT SIDE EMERGENCY FLOOR TRACK IS DAMAGED. REPLACED TRACK ASSEMBLY. 2 L 7 3 4F A23WE 1996032900131 19960329 00131 WP 1996 3 29 DLL15960633 1 19960321 A 3350 337202180 LIGHT LKHEED 1011 10113853 5265020 WP CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 755DL 193Y1184 EMERGENCY LIGHT CAME APART L1 DOOR EXIT SIGN. REPLACED LIGHT ASSY. 2 L 7 3 4F A23WE 1996032900132 19960329 00132 NM 1996 3 29 DLM88960594 1 19960316 A 3320 03980 BALLAST DOUG MD88 MD88 3023688 NM CABIN OVERHEATED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 973DL 53241 DURING CRUISE HAD SMOKE IN THE MID CABIN CEILING. IT WAS AN ELECTRICAL SMELL THAT COULD HAVE BEEN FROM THE LT BALLASTS. MTC DEACTIVATED THE CABIN LTS AND FWD TO MCO. SEVERAL OF THE CEILING LTS WERE FOUND INOP. THE SMOKE HAD DISSIPATED W HEN THE A/C WAS IN DESCENT. BURNED OUT LIGHTS WERE REPLACED AND A INSPECTION OF THE LIGHTING SYSTEM WAS DONE, NO DISCRE PANCIES WERE FOUND. 2 L 7 2 4F RT A6WE 1996032900133 19960329 00133 NM 1996 3 29 DLM88960628 1 19960321 A 3350 LAMP DOUG MD88 MD88 3023688 NM CABIN LOOSE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 928DL 49715 EMERGENCY LIGHTING STRIP 3RD RED LIGHT FROM FWD GALLEY WILL NOT LIGHT. RESECURED LAMP, OPS NORMAL. 2 L 7 2 4F RT A6WE 1996032900134 19960329 00134 EU 1996 3 29 QXEA9600113 1 19960322 A 5312 BLKHD STIFFENER FOKKER F28 F28MK1000 4990808 EU FS 1385 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 457US 11036 A CRACK THROUGH RIVET ON VERTICAL STIFFENER BETWEEN NR 3 AND 4 HORIZONTAL BEAMS RT SIDE OF FRONT PRESSURE BULKHEAD FORWA RD SIDE. CRACK NOTED DURING C-CHECK. CRACK REPAIRED I/A/W SRM. 2 L 7 2 4F RT A20EU 1996032900135 19960329 00135 EU 1996 3 29 QXEA9600114 1 19960322 A 5312 BLKHD BEAM FOKKER F28 F28MK1000 4990808 EU FS 1385 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 457US 11036 AFT SURFACE OF FRONT PRESSURE BULKHEAD IS CRACKED AT RT HORIZONTAL BEAM NR 3, CRACK LENGTH IS APPROX 5 INCHES. CRACK NO TED DURING C-CHECK. CRACK REPAIRED I/A/W SRM. 2 L 7 2 4F RT A20EU 1996032900136 19960329 00136 EU 1996 3 29 QXEA9600115 1 19960322 A 5312 BLKHD FRAME FOKKER F28 F28MK1000 4990808 EU FWD PRESS BLKHD CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 457US 11036 CRACK NOTED ON FORWARD PRESSURE BULKHEAD FRAME 880/1550 LOWER CHORD LBL CRACK LENGH APPROX 2.5 INCH, LBL 3 TO 6. CRACK REPAIRED I/A/W EA 28-53-328. 2 L 7 2 4F RT A20EU 1996032900137 19960329 00137 EU 1996 3 29 QXEA9600116 1 19960322 A 5312 BLKHD BEAM FOKKER F28 F28MK1000 4990808 EU FWD PRESS BLKHD CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 457US 11036 A 4 TO 5 INCH CRACK ON FORWARD PRESSURE BULKHEAD AT BEAM NR 6 COPILOTS SIDE. CRACK NOTED DURING C-CHECK. CRACK REPAIRE D I/A/W SRM. 2 L 7 2 4F RT A20EU 1996032900138 19960329 00138 EU 1996 3 29 QXEA9600117 1 19960322 A 5312 BLKHD ANGLE FOKKER F28 F28MK1000 4990808 EU FWD PRESS BLKHD CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 457US 11036 FORWARD PRESSURE BULKHEAD CONNECTION ANGLE BETWEEN STRINGERS 2 AND 3 IS CRACKED 6 INCHES LEFT OF CENTER LINE BETWEEN 2ND AND 3RD HILOCK. CRACK LENGTH IS APPROX 1 INCH. CRACK NOTED DURING C-CHECK AND REPAIRED I/A/W SRM. 2 L 7 2 4F RT A20EU 1996032900139 19960329 00139 EU 1996 3 29 QXEA9600118 1 19960322 A 5330 SKIN FOKKER F28 F28MK1000 4990808 EU BS 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 457US 11036 FUSELAGE OUTER SKIN IS CRACKED AT BULKHEAD FRAME STA 15205 AND STRINGER LT 15. ALSO, STRINGER CROSSOVER CASTALLATION RE PAIR ON INTERIOR SIDE IS CRACKED. CRACK NOTED DURING C-CHECK AND REPAIRED I/A/W SRM. 2 L 7 2 4F RT A20EU 1996032900140 19960329 00140 EU 1996 3 29 QXEA9600119 1 19960322 A 5320 NLG BAY WEB FOKKER F28 F28MK1000 4990808 EU BS 2745 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 457US 11036 NOSE LANDING GEAR BAY TOP COVER IS CRACKED AT STA 2745, 4.5 TO 5 INCHES RIGHT ON CENTERLINE, CRACK LENGTH APPROX .5 INCH . SECOND CRACK NOTED AT RIVETS STA 2870, 3 RIVETS RIGHT OF CENTERLINE. CRACK NOTED DURING C-CHECK AND REPAIRED I/A/W S RM. 2 L 7 2 4F RT A20EU 1996032900141 19960329 00141 EU 1996 3 29 QXEA9600120 1 19960322 A 5320 BOX BEAM FOKKER F28 F28MK1000 4990808 EU BS 1890 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 457US 11036 LONGITUDINAL BOX BEAM LT SIDE OF PANEL 21A IS CRACKED AT FORWARD PRESS BULKHEAD. CRACK IS LOCATED ON TOP INBOARD CORNER . CRACK NOTED DURING C-CHECK AND REPAIRED I/A/W EA 28-53-327. 2 L 7 2 4F RT A20EU 1996032900142 19960329 00142 EU 1996 3 29 QXEA9600121 1 19960322 A 5320 BOX BEAM FOKKER F28 F28MK1000 4990808 EU BS 1890 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 457US 11036 LOGITUDINAL BOX BEAM AT RT SIDE OF PANEL 21A IS CRACKED AT FORWARD PRESS BULKHEAD. CRACK IS LOCATED ON TOP INBOARD CORN ER. CRACK NOTED DURING C-CHECK. CRACK REPAIRED I/A/W EA 28-53-327. 2 L 7 2 4F RT A20EU 1996032900143 19960329 00143 EU 1996 3 29 QXEA9600122 1 19960322 A 5210 A26076 FITTING FOKKER F28 F28MK1000 4990808 EU MAIN CABIN DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 457US 11036 AFT HOOK LATCH FITTING FOR MAIN CABIN DOOR IS CRACKED THROUGH THE FORWARD SUPPORT BRACKET IN THE DOOR STRUCTURE. CRACK NOTED DURING C-CHECK AND BRACKET REPLACED I/A/W SRM. 2 L 7 2 4F RT A20EU 1996032900144 19960329 00144 EU 1996 3 29 QXEA9600123 1 19960322 A 5210 A26076 BRACKET FOKKER F28 F28MK1000 4990808 EU MAIN CABIN DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 457US 11036 FORWARD HOOK LATCH BRACKET FOR MAIN CABIN DOOR IS CRACKED THROUGH AFT LOWER RADIUS. CRACK NOTED DURING C-CHECK AND BRAC KET REPLACED. 2 L 7 2 4F RT A20EU 1996032900146 19960329 00146 EU 1996 3 29 QXEA9600125 1 19960322 A 5312 BLKHD WEB FOKKER F28 F28MK1000 4990808 EU AFT PRESS BLKHD CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 457US 11036 REAR PRESSURE BULKHEAD 4 CRACKED BETWEEN BEAMS 425R AND 1050R AT HORIZONTIAL BEAM. CRACK RADIATES HORIZONTIALLY UNDER S UPPORT BRACKET BETWEEN HYDRAULIC LINES AND CANNON PLUGS. CRACK NOTED DURING C-CHECK AND REPAIRED I/A/W SRM. 2 L 7 2 4F RT A20EU 1996032900147 19960329 00147 EU 1996 3 29 QXEA9600126 1 19960322 A 5330 SKIN FOKKER F28 F28MK1000 4990808 EU BS 1890 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 457US 11036 THREE SMALL CRACKS NOTED IN FUSELAGE SKIN BELOW NUMBER TWO WINDOW POST ON LEFT SIDE OF FUSELAGE. CRACKS NOTED DURING C- CHECK AND REPAIRED I/A/W SRM. 2 L 7 2 4F RT A20EU 1996032900148 19960329 00148 EU 1996 3 29 QXEA9600127 1 19960322 A 5320 A24352003 WINDOW POST FOKKER F28 F28MK1000 4990808 EU NR 3 WINDOW CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 457US 11036 DURING HFEC INSPECTION OF LT NR 3 WINDOW POST REARWARD FLANGE TYPE-D, CRACK WAS NOTED AT BOLT HOLE NR 4 AND 6. CRACK LE NGTH AT BOLT HOLE NR 4 IS .625 INCH, CRACK LENGTH AT BOLT HOLE NR 6 IS .1563 INCH. NUMBER THREE WINDOW POST REPLACED I/ A/W EO 28-53-175. 2 L 7 2 4F RT A20EU 1996032900149 19960329 00149 EU 1996 3 29 QXEA9600128 1 19960321 A 3350 5515800104 CIRCUIT BOARD FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 466US 11075 CENTER OVERHEAD EXIT SIGN INOP. CIRCUIT BOARD REPLACED AND SIGN OPS CHECKED. 2 L 7 2 4F RT A20EU 1996032900150 19960329 00150 EU 1996 3 29 QXEA9600129 1 19960322 A 3350 5515800104 CIRCUIT BOARD FOKKER F28 F28MK1000 4990808 EU COCKPIT DOOR FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 457US 11036 EXIT LIGHT ABOVE COCKPIT DOOR IS INOP. LIGHT CIRCUIT BOARD REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996032900151 19960329 00151 EU 1996 3 29 QXEA9600130 1 19960323 A 3350 6008905 BATTERY PACK FOKKER F28 F28MK1000 4990808 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 801PH 11097 RIGHT OVERWING EXIT SIGN IS INOP. BATTERY PACK AT 10D REPLACED AND SIGN OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996032900152 19960329 00152 NM 1996 3 29 QXEA9600131 1 19960323 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 821PH 104 COCKPIT OVERHEAD EMERGENCY LIGHT IS INOP. LIGHT ASSY REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE . 2 H 7 2 4T RT A13NM 1996032900153 19960329 00153 NM 1996 3 29 UPS96205756 1 19960322 A 3350 S106 BATTERIES BOEING 727 72722C 138400F NM COCKPIT DOOR DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 942UP 19101 MAINTENANCE REPORTED, EMERGENCY EXIT LIGHT OVER COCKPIT DOOR DIM. REPLACED BOTH BATTERIES. RELAMPED, TEST NORMAL PER M M 33-50-101. 2 L 7 3 4F A3WE 1996032900154 19960329 00154 NM 1996 3 29 UPS96405748 1 19960321 A 5720 SUPPORT BOEING 747 747121 1384871 NM WS 1280 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED LT WING LOWER SURFACE FOUND CORROSION AT O/B SUPPORT JACK POINT WS 1280. REMOVED AND REPAIRED CORROSION DAMAGE IAW SRM 51-10-01, 57-30-01 AND UPS EFN 747-57-0322. 2 L 7 4 4F A20WE 1996032900155 19960329 00155 NM 1996 3 29 UPS96405749 1 19960306 A 5230 LATCH SUPPORT BOEING 747 747121 1384871 NM AFT DOOR SILL CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED FOUND CRACK IN AFT CARGO DOORWAY LOWER. SILL LATCH NR 10 INSPECTION PERF ORMED ACC NDT MANUAL D6-7170, PART 6 CHAPTER 51-00-00. REPLACED TRUSS AND LATCH SUPPORT FITTING AT POS NR 10 PER EO B74 7-5340-0191 APP D. ALSO, REPLACED SUPPORT BRACKET FOR GUIDE WHEEL ACC SRM 51-30-02. 2 L 7 4 4F A20WE 1996032900156 19960329 00156 WP 1996 3 29 UPS96805750 1 19960222 A 5320 4611067 FITTING DOUG DC8 DC873F 302199F WP FS 70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LONGERON END FITTING HEAVY CORROSION AT FS 70, LONGERON 30R. REPLACED FITTIN G PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996032900157 19960329 00157 WP 1996 3 29 UPS96805751 1 19960215 A 5320 5612298 DOUBLER DOUG DC8 DC873F 302199F WP FS 90 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED COCKPIT SUBFLOOR DOUBLER AT FS 90 HAS CORROSION DAMAGE RBL 35. REPAIRED PER UPS EO DC8-5310-8040-A. 2 L 7 4 4F RT 4A25 1996032900158 19960329 00158 WP 1996 3 29 UPS96805752 1 19960215 A 5320 561228 DOUBLER DOUG DC8 DC873F 302199F WP FS 25-90 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED COCKPIT SUBFLOOR DOUBLER AT FS 25 TO 90 HAS CORROSION DAMAGE LONGERON 22R. R EPAIRED PER UPS EO DC8-5310-8040-A. 2 L 7 4 4F RT 4A25 1996032900159 19960329 00159 WP 1996 3 29 UPS96805753 1 19960223 A 5315 5616795503 FLOOR BEAM DOUG DC8 DC873F 302199F WP FS 12 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON LOWER SURFACE OF FLOOR BEAM FS 12 RBL 50. REPAIRED PER UP S EO DC8-53-1582. 2 L 7 4 4F RT 4A25 1996032900160 19960329 00160 WP 1996 3 29 UPS96805754 1 19960224 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP FS 32-52 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FINGER DOUBLER AT FS 32 TO 52, RBL 15 HAS HEAVY CORROSION. REPLACED DOUBLER ON TASK CARD 424338. 2 L 7 4 4F RT 4A25 1996032900161 19960329 00161 WP 1996 3 29 UPS96805755 1 19960225 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP FS 8-80 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FINGER DOUBLER FROM FS 08 TO 80 HAS CORROSION OUT OF LIMITS, RBL 40. REPLACE D DOUBLER PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1996032900162 19960329 00162 WP 1996 3 29 UPS96805757 1 19960215 A 5320 3754930 FITTING DOUG DC8 DC873F 302199F WP FS 1200 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON B/T FITTING, FS 1200 LONGERON 23R. REPLACED FITTING PER S RM 53-2-0. 2 L 7 4 4F RT 4A25 1996032900163 19960329 00163 WP 1996 3 29 UPS96805758 1 19960215 A 5320 3755840 FITTING DOUG DC8 DC873F 302199F WP FS 1220 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON B/T FITTING, FS 1220 LONGERON 33R. REPLACED FITTING PER S RM 53-2-0. 2 L 7 4 4F RT 4A25 1996032900164 19960329 00164 WP 1996 3 29 UPS96805759 1 19960214 A 5320 4597643210 FITTING DOUG DC8 DC873F 302199F WP FS 360 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MODERATE CORROSION AT FRAME FITTING, LONGERON 21R FS 360. REPLACED FITTING P ER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996032900165 19960329 00165 WP 1996 3 29 UPS96805760 1 19960214 A 5330 561537271 SKIN DOUG DC8 DC873F 302199F WP FS 1395-1445 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED EXTERNAL SKIN FS 1395 TO 1445, LONGERON 33R TO 35L HAS MODERATE CORROSION UND ER SCUFF PLATE. REPLACED SKIN SECTON PER SRM 51-1-21, AND 51-1-20D. 2 L 7 4 4F RT 4A25 1996032900166 19960329 00166 WP 1996 3 29 UPS96805761 1 19960214 A 5313 9755802 LONGERON DOUG DC8 DC873F 302199F WP FS 445 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON LONGERON 21L, FS 445. REPAIRED PER UPS EO DC8-53-1574. 2 L 7 4 4F RT 4A25 1996032900167 19960329 00167 WP 1996 3 29 UPS96805762 1 19960215 A 5313 575032245 LONGERON DOUG DC8 DC873F 302199F WP FS 1270 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON LONGERON 31L, FS 1270. REPAIRED PER UPS EO DC8-53-1574. 2 L 7 4 4F RT 4A25 1996032900168 19960329 00168 WP 1996 3 29 UPS96805763 1 19960212 A 5320 4758514 FITTING DOUG DC8 DC873F 302199F WP FS 1260-1280 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MODERATE CORROSION AND CRACK AT FITTING, FS 1260 TO 1280, LONGERON 33R. REPL ACED FITTING PER SRM 51-1-8 AND 51-1-20D. 2 L 7 4 4F RT 4A25 1996032900169 19960329 00169 WP 1996 3 29 UPS96805764 1 19960218 A 5311 5154671502 FRAME DOUG DC8 DC873F 302199F WP FS 1140 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION AT FS 1140 BOLT FRAME FWD LOWER FLANGE, LONGERON 36 TO 35L. 2 L 7 4 4F RT 4A25 1996032900170 19960329 00170 WP 1996 3 29 UPS96805765 1 19960210 A 5311 56119433 FRAME DOUG DC8 DC873F 302199F WP FS 70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION AT FS 70 BOLT FRAME AFT SIDE ON LONGERON 29R TO 26R. REPAIRE D PER UPS EO DC8-53-1591. 2 L 7 4 4F RT 4A25 1996032900171 19960329 00171 WP 1996 3 29 UPS96805766 1 19960212 A 5311 3614944509 FRAME DOUG DC8 DC873F 302199F WP FS 180 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION AT FS 180, FWD SIDE OF BOLT FRAME, LONGERON 33R AND 33L. REP AIRED PER SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1996032900172 19960329 00172 WP 1996 3 29 UPS96805767 1 19960212 A 5320 4611667501 FITTING DOUG DC8 DC873F 302199F WP FS 70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON LONGERON 27R, END FITTING AFT SIDE OF FS 70. REPLACED FI TTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996032900173 19960329 00173 WP 1996 3 29 UPS96805768 1 19960210 A 5313 52645716 LONGERON DOUG DC8 DC873F 302199F WP FS 100-120 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LONGERON 30R, HEAVY CORROSION FS 100 TO 120. REPLACED LONGERON SECTION PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996032900174 19960329 00174 WP 1996 3 29 UPS96805769 1 19960210 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FS 120 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED BOLT FRAME ANGLE AT FS 120, LONG 27R, HEAVY CORROSION. REPLACED ANGLE PER SR M 51-1-20D. 2 L 7 4 4F RT 4A25 1996032900175 19960329 00175 WP 1996 3 29 UPS96805770 1 19960210 A 5311 5772958 FRAME DOUG DC8 DC873F 302199F WP FS 520 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON LONG 36, FS 520 BOLT FRAME. REPLACED FRAME PER SRM 53-2-0 . 2 L 7 4 4F RT 4A25 1996032900176 19960329 00176 WP 1996 3 29 UPS96805771 1 19960211 A 5311 5764347 FRAME DOUG DC8 DC873F 302199F WP FS 1060 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON BOLT FRAME FS 1060, LONG 36. REPLACED FRAME UPPER SECTION PER SRM 51-1-20D PER SRM 53-2-0. 2 L 7 4 4F RT 4A25 1996032900177 19960329 00177 WP 1996 3 29 UPS96805772 1 19960215 A 5311 5772958 FRAME DOUG DC8 DC873F 302199F WP FS 1060 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED BOLT FRAME UPPER FLANGE HEAVY CORROSION AT FS 1060 ABOVE LONG 36. REPAIRED F RAME PER SRM 53-4-1 AND 53-2-1. 2 L 7 4 4F RT 4A25 1996032900178 19960329 00178 WP 1996 3 29 UPS96805773 1 19960211 A 5320 SHEAR TIE DOUG DC8 DC873F 302199F WP FS 1080 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 1080 SHEAR TIE STRAP SHEARED ABOVE LONG 31L. REPLACED SHEAR TIE PER SRM 5 1-1-4 AND 51-1-8B. 2 L 7 4 4F RT 4A25 1996032900179 19960329 00179 WP 1996 3 29 UPS96805774 1 19960211 A 5320 51706317 SHEAR TIE DOUG DC8 DC873F 302199F WP FS 1140 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON BOLT FRAME SHEAR TIE, FS 1140 LONG 36. REPLACED SHEAR TIE PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996032900180 19960329 00180 WP 1996 3 29 UPS96805775 1 19960213 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP FS 1350 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON DOUBLER O/B OF LONG FS 1350. REPLACED DOUBLER SECTION PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1996032900181 19960329 00181 WP 1996 3 29 UPS96805776 1 19960213 A 5320 607756 ANGLE DOUG DC8 DC873F 302199F WP FS 1340 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON ANGLE AT LONGERON 31L, FS 1340. REPLACED ANGLE PER SRM 51 -1-20D. 2 L 7 4 4F RT 4A25 1996032900182 19960329 00182 WP 1996 3 29 UPS96805777 1 19960213 A 5311 FRAME DOUG DC8 DC873F 302199F WP FS 1400-1420 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON LONGERON 34R, FS 1400 TO 1420 AT FRAME. REPLACED FRAME SE CTION PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996032900183 19960329 00183 WP 1996 3 29 UPS96805778 1 19960214 A 5320 SHEAR TIE DOUG DC8 DC873F 302199F WP BS 100 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MODERATE CORROSION ON SHEAR TIE BOLT FRAME STA 100 LONGERON 21R. REPLACED SH EAR TIE PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996032900184 19960329 00184 WP 1996 3 29 UPS96805779 1 19960219 A 5320 WEB DOUG DC8 DC873F 302199F WP FS 1210 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON DOOR WEB FS 1210 I/B SIDE OF LONG 33R. REPLACED WEB PER S RM 53-2-0. 2 L 7 4 4F RT 4A25 1996032900185 19960329 00185 WP 1996 3 29 UPS96805780 1 19960221 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FS 1350 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LONGERON 31L CRACKED AT FS 1350. REPAIRED PER UPS EO DC8-53-1600. 2 L 7 4 4F RT 4A25 1996032900186 19960329 00186 WP 1996 3 29 UPS96805781 1 19960217 A 5315 FLOOR BEAM DOUG DC8 DC873F 302199F WP FS 55 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON LOWER SURFACE OF FLOOR BEAM FS 55 RBL 50. REPAIRED PER UP S EO DC8-53-1583. 2 L 7 4 4F RT 4A25 1996032900187 19960329 00187 WP 1996 3 29 UPS96805782 1 19960217 A 5315 FLOOR BEAM DOUG DC8 DC873F 302199F WP FS 35 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON LOWER SURFACE OF FLOOR BEAM FS 35 RBL 50. REPAIRED PER UP S EO DC8-53-1586. 2 L 7 4 4F RT 4A25 1996032900188 19960329 00188 WP 1996 3 29 UPS96805783 1 19960212 A 5330 SKIN DOUG DC8 DC873F 302199F WP FS 1766 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED EXTERIOR FUSELAGE SKIN HEAVY CORROSION AT FS 1766, LONG 28R. REPAIRED PER UP S EO DC8-53-1571. 2 L 7 4 4F RT 4A25 1996032900189 19960329 00189 EU 1996 3 29 WWMA9600030 1 19960322 A 2910 1379305A77 HOSE BAG JETSTM JETSTM3201 1500217 EU LT ENGINE RUPTURED A WWMA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 WP 15 949AE 949 LEFT MAIN HYDRAULIC PRESSURE WENT TO ZERO PSI ON DESCENT INTO SAN. THE LANDING GEAR WAS MANUALLY PUMPED DOWN AND THE AI RCRAFT LANDED WITHOUT INCIDENT. UPON INVESTIGATION MAINTENANCE FOUND A HOLE IN THE FLEXIBLE HOSE BETWEEN THE LEFT ENGIN E HYDRAULIC PUMP AND THE LEFT FIREWALL. THE HOSE WAS REPLACED, THE FILTERS WERE CHECKED, GEAR SWINGS AND LEAK CHECKS WE RE PERFORMED. THE AIRCRAFT WAS RELEASED TO SERVICE WITH NO FURTHER PROBLEMS. 2 L 7 2 4T RT A56EU 1996032900190 19960329 00190 GL 1996 3 29 HEEA966860 2 19960319 A 7250 6886407 WHEEL 6898735 AEROSP AS355 AS355F1 8680810 EU ALLSN 250C 250C20F 03013 GL 1ST STAGE BLADE ERODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5793Z 1067 CAT30033F 5142 CAE840382 ENGINE REMOVED DUE TO #1 AND #2 WHEEL CYCLE RETIREMENT. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: 1ST STAG E WHEEL BLADES MINOR SULFIDATION AND ERODED LEADING EDGE. SCRAPPED 1ST STAGE WHEEL. 1 G 7 2 3U 3 U H11EU E4CE 1996032900191 19960329 00191 GL 1996 3 29 HEEA966861 2 19960319 A 7230 23056634 GEARSHAFT 23051643 SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30 03013 GL SPUR ADAPTER STEPWEAR E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3122H 642 CAC90185 760233 CAE890181S ENGINE REMOVED DUE TO TURBINE WHEEL HIGH CYCLES. UPON INSPECTION OF COMPRESSOR PARTS NOTED THE FOLLOWING: STEP WEAR BE YOND LIMITS ON SPUR ADAPTER GEARSHAFT FWD AND AFT SPLINES. NEW PART INSTALLED. 1 G 7 2 3U 3 U H1NE E1GL 1996032900192 19960329 00192 GL 1996 3 29 HEEA966862 2 19960320 A 7230 23056634 GEARSHAFT 23033193 BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL SPUR ADAPTER STEPWEAR E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8589X 934 CAC90854 51487 CAE890024 ENGINE REMOVED DUE TO CRACKED COMPRESSOR SCROLL. UPON INSPECTION OF COMPRESSOR PARTS NOTED THE FOLLOWING: SPLINE STEP WEAR BEYOND OVERHAUL LIMITS ON SPUR ADAPTER GEARSHAFT AFT TURBINE SPLINES. NEW PART INSTALLED. 1 G 7 1 3U 3 U H2SW E1GL 1996032900193 19960329 00193 SW 1996 3 29 HEEA966863 1 19960320 A 6410 206310105101 BEARING 206016201127 BELL 206 206L1 1182107 SW T/R BLADE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2245Y 441 CS4665 45751 RETIRED BLADE. REMOVED BEARINGS TO CHECK FOR SERVICEABILITY. FOUND BEARING CRACKED. SCRAPPED LOCALLY. 1 G 7 1 3U H2SW 1996032900194 19960329 00194 SW 1996 3 29 HEEA966864 1 19960320 A 6220 206011132113A GRIP 206011100159 BELL 206 206L3 1182108 SW M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 206FS 1923 A2044 51506 ASSEMBLY LEAKING GREASE, DUE TO RETAINER SPINNING INSIDE OF GRIP. PRO SEAL UNBONDED. WORN AREA IN GRIP. MIN .007 MAX. .012 DEPTH. REPLACED WITH SERVICEABLE PARTS. 1 G 7 1 3U H2SW 1996032900195 19960329 00195 SW 1996 3 29 HEEA966865 1 19960320 A 6330 222331617101 ISOLATION MT BELL 230 230 1182149 SW M/R XMSN BEARING WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 1012 23009 LATERAL ISOLATION MOUNT HAS WORN BEARING BEYOND LIMITS. 1 G 7 2 3U NC H9SW 1996032900196 19960329 00196 EU 1996 3 29 HEEA966866 1 19960320 A 5610 1172416902 WINDOW BOLKMS 117 BK117B1 5626012 EU COCKPIT INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 117BK 7229 WINDOW INOPERATIVE. 1 G 7 2 3U H13EU 1996032900197 19960329 00197 EU 1996 3 29 HEEA966868 1 19960320 A 6730 SC50811 SERVO SNIAS 350 AS350B2 8680813 EU M/R LEAKS E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 6095S 1283 2777 RT AND LT SERVO LEAKS. 1 G 7 1 3U H9EU 1996032900198 19960329 00198 1996 3 29 HEEA966869 4 19960322 A 3452 6221270001 TRANSPONDER COLLINS TDR90 BEECH 200 200BEECH 1152920 CE COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 30PH BB635 WEAK RECEIVER AND NO POWER OUT. SENT TO COLLINS AVIONICS FOR INSPECTION AND REPAIR. 1 L 7 2 4T A24CE 1996032900199 19960329 00199 1996 3 29 HEEA966870 4 19960322 A 3451 066106602 TRANSCEIVER BELL 214 214ST 1182106 SW COCKPIT DME FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3897N 28106 DISPLAY STAYS BLANK AT ALL TIMES. SENT TO THE RADIO SHOP FOR INSPECTION AND REPAIR. 2 G 7 2 4U H10SW 1996032900200 19960329 00200 1996 3 29 HEEA966871 4 19960322 A 3444 066304401 INDICATOR BOLKMS 105 BO105S 5626006 EU COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 86CH S557 FLAG IS NOT GOING BEHIND MASK AFTER TESTING. SENT TO ALLIED SIGNAL AVIONICS FOR INSPECTION AND REPAIR. 1 G 7 2 3U H3EU 1996032900201 19960329 00201 SW 1996 3 29 HEEA966872 1 19960322 A 6210 412015300109 BLADE BELL 412 412 1182202 SW M/R DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 8081 33113 REMOVE EXCESS WEIGHT AND PAINT AND REFINISH BLADES AND SEAL THE EDGE OF THE INBOARD TRIM TAB ON BLADE S/N A94. 1 G 7 2 4U H4SW 1996032900202 19960329 00202 SW 1996 3 29 HEEA966873 1 19960322 A 6210 412015300109 BLADE BELL 412 412 1182202 SW M/R DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 8148 33113 REMOVE EXCESS WEIGHT AND PAINT AND REFINISH BLADES AND SEAL THE EDGE OF THE INBOARD TRIM TAB ON BLADE S/N A94. 1 G 7 2 4U H4SW 1996032900203 19960329 00203 1996 3 29 HEEA966874 4 19960322 A 3452 071119218 CONTROL DISPLAY BELL 214 214ST 1182106 SW COCKPIT XPONDR DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5748M 28102 TOO DIM. ADJUSTED INTENSITY BRIGHTER. REPAIRED. REPLACED MISSING RING RETAINER AT END OF SHAFT. REPLACED FADED LENS. BENCH CHECK GOOD. 2 G 7 2 4U H10SW 1996032900204 19960329 00204 1996 3 29 HEEA966875 4 19960322 A 2312 071121540 CONTROL BELL 412 412 1182202 SW COCKPIT COMM DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 108X 33115 VOLUME CONTROL IS NOT LINEAR AND DISPLAY FLASHES ON AND OFF. COULD NOT DUPLICATE PROBLEM. TESTED UNIT AND FOUND TRANSFE R SWITCH BAD. REPLACED SWITCH S102 P/N 031-0399-01. REPAIRED. ALSO PERFORMED HEADER MOD. REPLACED HEADER P201 P/N 03 0-2368-16. TOUCHED UP FACEPLATE AND CHECKED LIGHTING. BENCH CHECKGOOD. 1 G 7 2 4U H4SW 1996032900205 19960329 00205 1996 3 29 HEEA966876 4 19960322 A 3452 066106200 TRANSCEIVER KT76 BOLKMS 105 BO105S 5626006 EU COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 81982 S818 TOWER REPORTED UNABLE TO PICKUP TRANSPONDER SIGNAL. COULD NOT DUPLICATE PROBLEM. INSPECTED UNIT AND FOUND FACEPLATE CRA CKED AND PHOTOCELL NOT WORKING. REPLACED FACEPLATE P/N 200-02020-0001 AND PHOTOCELL V301 P/N 134-05005-0002. TESTED UN IT. ADJUSTED PULSE AND FREQUENCY TO SPECS. BENCH CHECK GOOD. 1 G 7 2 3U H3EU 1996032900206 19960329 00206 1996 3 29 HEEA966877 4 19960322 A 2312 071104302 CONTROL KFS570B SKRSKY S76 S76A 8143006 NE COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 31217 760229 LIGHT INOPERATIVE AND BROKEN COUNTER WHEELS. SENT TO ALLIED SIGNAL AVIONICS FOR INSPECTION AND REPAIR. 1 G 7 2 3U H1NE 1996032900207 19960329 00207 1996 3 29 HEEA966878 4 19960322 A 3451 066106901 INDICATOR BELL 412 412 1182202 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3893N 33010 INDICATOR UNREADABLE. 1 G 7 2 4U H4SW 1996032900208 19960329 00208 1996 3 29 HEEA966879 4 19960322 A 3454 066107800 RECEIVER BELL 412 412 1182202 SW COCKPIT NAV INTERMITTENT E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 107X 33113 INTERMITTENT OPERATION ON FLIGHT LINE. 1 G 7 2 4U H4SW 1996032900209 19960329 00209 SW 1996 3 29 HEEA966880 1 19960322 A 6710 206076062003 CYLINDER BELL 206 206L3 1182108 SW CYCLIC BINDING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3116L 14083 51529 CYCLIC HAS BINDING DURING LANDING. FOUND PILOT VALVE PIVOT BOLT TIGHT (TOP) 1 G 7 1 3U H2SW 1996032900210 19960329 00210 1996 3 29 HEEA966881 4 19960322 A 3416 5035P2P44 ALTIMETER SKRSKY S76 S76A 8143006 NE COCKPIT ENCODE ERRATIC E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5427S 760168 ENCODER HAS A ERRATIC OUTPUT. 1 G 7 2 3U H1NE 1996032900211 19960329 00211 1996 3 29 HEEA966882 4 19960322 A 2312 6221879001 TRANSCEIVER BEECH 200 200BEECH 1152920 CE COCKPIT VHF DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 30PH BB635 VOLUME CREEPS UP ON ITS OWN. UNABLE TO ADJUST TRANSMIT COMPRESSOR TO SPECS. 1 L 7 2 4T A24CE 1996032900212 19960329 00212 1996 3 29 HEEA966883 4 19960322 A 3442 MI585200 RADAR RT BELL 412 412 1182202 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3911L 33023 FOUND RT UNIT TO BE INTERMITTENT, UNIT CUTS OFF DURING OPERATION. FOUND BROKEN WIRE ON CONNECTOR J5001. RESOLDERED WIR E. DID NOT CURE PROBLEM, UNIT STILL INTERMITTENT. 1 G 7 2 4U H4SW 1996032900213 19960329 00213 EU 1996 3 29 HEEA966884 1 19960322 A 7714 65051008 INDICATOR BOLKMS 105 BO105S 5626006 EU TRIPLE TACH FLUCTUATES E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 7170D S840 AFTER ONE HOUR OF USE #2 NEEDLE STARTED TO FLUCTUATE. 1 G 7 2 3U H3EU 1996032900243 19960329 00243 CE 1996 3 29 96ZZZX1358 1 19960216 A 5512 SKIN MTSBSI MU2 MU2B40 CE HORIZ STAB CRACKED A S DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 16CG 1944 418SA FOUND UPPER SURFACE OF HORIZONTAL STABILIZER CRACKED DURING DEICE BOOT CHANGE. MITSUBISHI TECH SERVICE HAS BEEN NOTIFIE D. REPAIR WILL BE IAW SRM. 1 H 7 2 3T A10SW 1996032900247 19960329 00247 WP 1996 3 29 9606779180 1 19960323 A 5720 L/E FENCE DOUG DC9 DC914 3022034 WP RT WING SEPARATION A NWAA K NONE D INFLIGHT SEPARATION UK UNKNOWN 1 GL 01 3312L 45707 DURING LINE CHECK, FOUND THAT THE RIGHT WING LEADING EDGE FENCE WAS MISSING AFTER FLIGHT 0278, MEM-DTW. REPAIRED THE WI NG LEADING EDGE PER EA 91102665. 2 L 7 2 4F A6WE 1996032900248 19960329 00248 NM 1996 3 29 9606782204 1 19960323 A 2782 1U109592 ACTUATOR BOEING 727 727251 138408H NM NR 2 LE SLAT MALFUNCTIONED A NWAA A J UNSCHED LANDING DUMP FUEL F E FLT CONT AFFECTED VIBRATION/BUFFET CL CLIMB 1 GL 01 204US 24165 199 22544 DURING DEPARTURE CLIMB UPON FLAP RETRACTION, THE NR 2 LEADING EDGE SLAT REMAINED EXTENDED WITH FLAPS UP SELECTED. NOTAB LE VIBRATION WAS FELT. CREW JETTISONED 20,000 LBS OF FUEL AND RETURNED TO MSP WITHOUT FURTHER INCIDENT. MAINTENANCE RE PLACED THE NR 2 SLAT ACTUATOR AND SLAT ASSEMBLY. OPERATIONAL CHECKS WERE NORMAL. 2 L 7 3 4F A3WE 1996032900249 19960329 00249 NM 1996 3 29 9606792704 1 19960321 A 3231 SEQUENCE VALVE BOEING 727 727225 1384077 NM LT MLG DOOR MALFUNCTIONED A NWAA A UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS TO TAKEOFF 1 GL 01 801EA 22432 DURING TAKEOFF ON GEAR RETRACTION, THE LEFT MAIN LANDING GEAR WOULD NOT RETRACT, INDICATION LEFT MAIN GEAR DOWN AND LOCK ED WITH GEAR DOOR IN THE OPEN POSITION. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED THE LEFT DOOR S EQUENCE VALVE AND LEFT MAIN GEAR DOOR ACTUATOR. LUBRICATED THE LEFT LANDING GEAR AND PERFORMED EXTENSION AND RETRACTION TEST, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996032900250 19960329 00250 1996 3 29 9606809754 2 19960321 A 7320 PT2 TUBE DOUG DC9 DC941 302207N WP NR 1 ENGINE CRACKED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 754NW 47178 NR 1 ENGINE EPR INDICATION DID NOT REACH TARGET ON TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GA TE. MAINTENANCE FOUND THE PT2 TUBE CRACKED IN THE NOSE DOME. THE ENGINE NOSE DOME/PT2 PROBE ASSEMBLY WAS REPLACED WITH A SERVICEABLE UNIT. SUBSEQUENT RUNUP WAS SATISFACTORY. 2 L 7 2 4F A6WE 1996032900251 19960329 00251 NE 1996 3 29 9606812294 2 19960319 A 7260 GEAR BOX BOEING 727 727251 138408H NM PWA JT8 JT8D15A 52051 NE NR 3 ENGINE FAILED A NWAA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 294U 21505 700030 DURING CRUISE, THE NR 3 ENGINE LOST OIL PRESSURE AND QUANTITY. THE ENGINE WAS SHUTDOWN AND THE FLIGHT CONTINUED TO LGA AS SCHEDULED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LP6 FITTING LIBERATED FROM THE GEARBOX. THE GEARBOX WAS R EPLACED WITH A SERVICEABLE UNIT. 2 L 7 3 4F 4 F A3WE E2EA 1996032900252 19960329 00252 NE 1996 3 29 9606822296 2 19960319 A 7260 GEAR BOX BOEING 727 727251 138408H NM PWA JT8 JT8D15A 52051 NE NR 3 ENGINE FAILED A NWAA A E J UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 296U 21788 695274 ON CLIMBOUT, THE NR 3 ENGINE LOST OIL PRESSURE AND QUANTITY. THE ENGINE WAS SHUTDOWN AND 10,300 LBS OF FUEL WAS JETTISO NED. THE AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LP6 FITTING LIBERATED FRO M THE GEARBOX. THE ENGINE WAS REPLACED WITH A SERVICEABLE UNIT. 2 L 7 3 4F 4 F A3WE E2EA 1996032900253 19960329 00253 WP 1996 3 29 9606839311 1 19960323 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP TAIL COMPT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 314RC 49110 DURING LINE CHECK, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND OPERATIONAL CHECK GOO D. 2 L 7 2 4F A6WE 1996032900254 19960329 00254 WP 1996 3 29 9606849859 1 19960323 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 768NC 47729 DURING LINE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE AFT OVERHEAD. REPLACED THE POWER SUPPLY AND BATTERIES, OPERATIONA L CHECK GOOD. 2 L 7 2 4F A6WE 1996032900255 19960329 00255 WP 1996 3 29 9606859866 1 19960322 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP COCKPIT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 775NC 47785 DURING LINE CHECK, FOUND EMERGENCY LIGHTS IN COCKPIT AFT OVERHEAD SWITCH PANEL, FORWARD ENTRY LIGHT ASSEMBLY, GALLEY ARE A LIGHT ASSEMBLY AND FORWARD COMPANION WAY INOPERATIVE. REPLACED BATTERIES IN POWER SUPPLY AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996032900256 19960329 00256 WP 1996 3 29 9606869751 1 19960323 A 3397 WIRE DOUG DC9 DC941 302207N WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 751NW 47115 DURING LINE CHECK, FOUND EMERGENCY PATH LIGHTS INOPERATIVE FROM ROW 6 TO 13. REPAIRED BROKEN WIRE AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996032900257 19960329 00257 WP 1996 3 29 9606879604 1 19960323 A 2910 HYD LINE DOUG DC9 DC932 3022066 WP SPOILER ACT CHAFED A NWAA O OTHER K FLUID LOSS CR CRUISE 1 GL 01 604NW 47222 LOSS OF RIGHT HYDRAULIC SYSTEM QUANTITY OCCURRED ENROUTE RSW-DTW. FLIGHT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. CAPTAIN DID DECLARE A YELLOW EMERGENCY AND CPR EQUIPMENT WAS STANDING BY AS A PRECAUTION. MAINTENANCE FOUND RIGHT OUTB OARD SPOILER ACTUATOR HYDRAULIC LINE CHAFED BY AILERON CONTROL CABLE. REPLACED LINE, THE RIGHT ENGINE DRIVEN HYDRAULIC PUMP AND CASE DRAIN FILTER. LEAK AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996032900258 19960329 00258 1996 3 29 9606889911 4 19960323 A 3416 57023932951 ALTIMETER DOUG DC9 DC931 3022065 WP RT COCKPIT FAILED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 961N 28327 47405 FIRST OFFICER'S ALTIMETER FAILED DURING CLIMBOUT AT APPROXIMATELY 11,500 FEET. FLIGHT RETURNED TO MSP AND LANDED WITHOU T INCIDENT. MAINTENANCE REPLACED FIRST OFFICER'S ALTIMETER AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996032900259 19960329 00259 WP 1996 3 29 9606899930 1 19960322 A 2822 CIRCUIT BREAKERS DOUG DC9 DC931 3022065 WP FUEL BOOST PUMPS TRIPPED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 89S 47402 APPROXIMATELY THREE MINUTES AFTER TAKEOFF, NUMEROUS FUEL BOOST PUMP CIRCUIT BREAKERS POPPED. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED WIRING AT PUMP SWITCHES ON OVERHEAD PANEL, AT CIRCUIT BREAKER PANEL AND AT DISCONNECT AT FS 237, ALL CHECKED NORMAL. RAN PUMPS WITH ENGINE POWER, GROUND POWER AND APU POWER WITH NO PROBLEMS FOUND. DISCREPANCY COULD NOT BE DUPLICATED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996032900260 19960329 00260 WP 1996 3 29 9606909976 1 19960320 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9340 47389 DURING LINE MAINTENANCE INSPECTION, FOUND SEVERAL FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. REPAIRED BROKEN WIRE AN D OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996032900261 19960329 00261 WP 1996 3 29 9606919604 1 19960321 A 3350 CONNECTOR DOUG DC9 DC932 3022066 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 604NW 47222 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHT AT ROW 14C INOPERATIVE. REPAIRED BROKEN PLUG UNDER SEAT AND O PERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996032900262 19960329 00262 WP 1996 3 29 9606929954 1 19960321 A 2450 93468862 RELAY DOUG DC9 DC931 3022065 WP AC EMERG POWER FAILED A NWAA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 GL 01 921RW 47164 EMERGENCY BUS DROPPED OFF LINE AFTER TAKEOFF. FLIGHT RETURNED TO GSO AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED R2-47 EMERGENCY TRANSFER RELAY. OPERATIONAL CHECK NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996032900263 19960329 00263 NM 1996 3 29 9606936302 1 19960324 A 3350 CONNECTOR BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 662US 23720 DURING LINE CHECK, THE FLOOR MOUNTED EMERGENCY PATH LIGHTS AT SEAT ROWS 51L THROUGH 63L WERE FOUND INOPERATIVE. RECONNE CTED CONNECTOR PIN AT SEAT ROW 63L AND OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996032900264 19960329 00264 WP 1996 3 29 9606949606 1 19960322 A 7711 LG80A2 EPR TRANSMITTER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7 52053 NE NR 2 ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 606NW 47225 653943 NR 2 ENGINE EPR INDICATION TOO LOW ON TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENA NCE REPLACED THE EPR TRANSMITTER WITH A SERVICEABLE UNIT. 2 L 7 2 4F 4 F A6WE E2EA 1996032900265 19960329 00265 WP 1996 3 29 9606959606 1 19960322 A 7711 JF298H1 EPR INDICATOR DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7 52053 NE COCKPIT MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 606NW 47225 653943 NR 2 ENGINE EPR INDICATION TOO LOW ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAI NTENANCE REPLACED THE EPR INDICATOR WITH A SERVICEABLE UNIT. 2 L 7 2 4F 4 F A6WE E2EA 1996032900266 19960329 00266 NM 1996 3 29 9606962293 1 19960325 A 3260 DNLOCK SWITCH BOEING 727 727251 138408H NM NLG BUSHING MISSING A NWAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 01 293US 21504 DURING FINAL APPROACH, NOSE GEAR INDICATION DID NOT SHOW DOWN AND LOCKED, MADE MISSED APPROACH GO-AROUND. ON SECOND EXT ENSION OF LANDING GEAR INDICATIONS SHOW NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. BUSHING ON UPPER DOWN AND LOCK SWITC H WAS MISSING. REPLACED BUSHING AND BOTH UPPER AND LOWER GEAR DOWN AND LOCK SWITCHES AS A PRECAUTION. 2 L 7 3 4F A3WE 1996032900267 19960329 00267 1996 3 29 9606979604 4 19960326 A 3420 2587794 FLUX VALVE DOUG DC9 DC932 3022066 WP LT WING TIP MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 604NW 47222 CAPTAIN'S RMI WAS PRECESSING 5 DEGREES TO THE RIGHT DURING CLIMBOUT. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT . MAINTENANCE REPLACED LEFT FLUX VALVE AND DEGAUSED OUTER LEFT WING. OPERATIONAL CHECK NORMAL AND AIRCRAFT RETURNED TO NORMAL. 2 L 7 2 4F A6WE 1996032900268 19960329 00268 NM 1996 3 29 96FDEA00593 1 19960318 A 5320 ANGLE BOEING 727 72722 1384002 NM BS 740 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 NR0500 AND 042, CRACK FOUND IN BS 740 SILL REINFORCEMENT ANGLE FWD WL 170 LBL 38. REPAIRED 740 SILL ANGLE PER SRM 51-20 -1 AND 51-40-3. 2 L 7 3 4F A3WE 1996032900269 19960329 00269 NM 1996 3 29 96FDEA00664 1 19960320 A 5347 694121 SEAT TRACK BOEING 727 727233 138408A NM BS 850-870 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CORROSION (C53-224-01, 2) ON EXPANSION LINK SEAT TRACK IS OUT OF LIMITS AT BS 850 TO 870 RBL 25 WL 208.5. REMOVED CORRO DED EXPANSION LINK AND REPLACED REF SRM 51-10-1. 2 L 7 3 4F RT A3WE 1996032900270 19960329 00270 NM 1996 3 29 96FDEA00665 1 19960320 A 5230 SKIN BOEING 727 727233 138408A NM NR 1 CARGO DOOR GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 NR 1 CARGO DOOR OUTER SKIN IS GOUGED 20 INCHES FWD THE AFT EDGE, 2 INCHES UP FROM THE BOTTOM. REMOVED GOUGE WITH A .193 DRILL BIT AND INSTALLED RIVET WET WITH SEALANT. 2 L 7 3 4F RT A3WE 1996032900271 19960329 00271 WP 1996 3 29 96FDEA00682 1 19960326 A 3260 GEAR LIGHT DOUG DC10 DC1030 3023501 WP LT MLG MALFUNCTIONED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 319FE 47820 ON TAKEOFF, RAISED GEAR AND ALL LIGHTS OUT, BUT AFTER A FEW SECONDS THE LEFT MAIN LIGHT ON FWD PANEL CAME ON. NO LIGHTS ON S/O PANEL. CYCLED THE GEAR AND ALL LIGHTS WENT OUT AND REMAINED OUT. LIGHTS CAME BACK ON BRIEFLY DURING DESCENT AN D BACK OUT, SEVERAL TIMES. PERFORMED PROXIMITY BOX BITE CHECK AND ALL OK. CHECKED PROXIMITY SWITCH FOR SECURITY AND OP S WITH HAND HELD TARGET. CHECKED WIRING FOR SECURITY AND BREAKS, CHECKED PER TAFI 32-30-00 AND ALL CHECKS NORMAL. 2 L 7 3 4F A22WE 1996032900272 19960329 00272 WP 1996 3 29 96FDEA00683 1 19960326 A 3260 UPLOCK SENSOR DOUG DC10 DC1030 3023501 WP LT MLG MALFUNCTIONED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 319FE 47820 AFTER TAKEOFF, A FEW MINUTES AFTER GEAR WAS RAISED THE LEFT MAIN REG LIGHT ON THE FWD PANEL ILLUMINATED. NO LIGHTS ON S /O'S PANEL. CYCLED THE GEAR AND ALL LIGHTS EXTINGUISHED. LIGHTS ILLUMINATED AGAIN DURING APPROACH PHASE. REPEAT WRITE -UP. REPLACED D1-81 LT MAIN GEAR DOOR UP AND LATCHED SENSOR IAW MM 32-61-03, OPS CKS GOOD. 2 L 7 3 4F A22WE 1996032900273 19960329 00273 NM 1996 3 29 96FDEA00684 1 19960325 A 5320 WEB BOEING 727 72722 1384002 NM BS 294-351 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 WHILE WORKING NR0498, FOUND O/B RT DOGHOUSE WEB TO BE CRACKED BS 294 TO 351 RBL 25 AND 26 WL 169. REMOVED AND REPLACED O/B DOGHOUSE WEB ALL WORK IAW BAC DRW NR 65-18915 AT BS 294 TO 351 RBL 25 TO 36 WL 169. 2 L 7 3 4F A3WE 1996032900274 19960329 00274 NM 1996 3 29 96FDEA00685 1 19960325 A 5320 WEB BOEING 727 72722 1384002 NM BS 294-351 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 UPON REMOVAL OF I/B FLOOR WEB AT BS 294 TO 344 WL 169 RBL 15 TO 27 FOUND TO BE CRACKED. REMOVED AND REPLACED FLOOR WEB AND INSTALLED ALL BRACKETS AND ANGLES REMOVED FOR INSTALLATION AT BS 294 TO 351 WL 169 RBL 15 TO 27. ALL WORK IAW BAC D RW NR 65-18915. 2 L 7 3 4F A3WE 1996032900275 19960329 00275 NM 1996 3 29 96FDEA00686 1 19960325 A 5730 SKIN BOEING 727 72722 1384002 NM WING CTR SECT CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 CORROSION (C53-132-02, 1) ON INNER SURFACE OF WING CENTER SECTION UPPER SKIN BS 870 RBL TO LBL 70 PLUS ON RT SURFACE LBL 55 TO 70. REMOVED CORROSION AND BLENDED AREA, WITHIN LIMITS PER EA 7-5710-28042. 2 L 7 3 4F A3WE 1996032900276 19960329 00276 NM 1996 3 29 96FDEA00687 1 19960325 A 5313 STRINGER BOEING 727 72722 1384002 NM BS 522/517 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 UPON REMOVAL OF SPLICE AT BS 520, DISCOVERED CORROSION OF STR 27R BS 522 AND 517 TO BE OUT LIMITS. REMOVED AND REPLACED DAMAGED SECTION OF STR 27R. 2 L 7 3 4F A3WE 1996032900277 19960329 00277 NM 1996 3 29 96FDEA00688 1 19960325 A 5314 KEEL BEAM BOEING 727 72722 1384002 NM BS 979-1030 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 CORROSION (C53-113-01, 2) ON LT KEEL BEAM AT LBL 6 WL 190 BS 979, 1013 AND 1030. ALSO, MATERIAL CHIPPED AWAY FROM BEAM AT 1031. FABRICATED REPAIR PARTS AND INSTALLED PER EA 7-5310-28043. 2 L 7 3 4F A3WE 1996032900278 19960329 00278 NM 1996 3 29 96FDEA00689 1 19960325 A 5311 FRAME BOEING 727 72722 1384002 NM BS 1166 DOUBLE DRILLED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 DOUBLE DRILLED HOLES ON NESTLED FLANGE OF FRAME AT BS 1166 LBL 20 WL 159. TRIMMED DAMAGE AND INSTALLED DOUBLER PER FEDE X SRM 51-40-3. 2 L 7 3 4F A3WE 1996032900279 19960329 00279 NM 1996 3 29 96FDEA00690 1 19960322 A 5330 SKIN BOEING 727 72722 1384002 NM BS 660.3 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 BS 660.3 STR 20R WL 181, THERE IS A DEEP GOUGE IN SKIN. BLENDED GOUGE AT BS 660.3 STR 20R WL 181 WAS OUT OF LIMITS PER FEDEX SRM 53-30-1. REMOVED 2.75 INCH BY 1.8 INCH OF DAMAGED SKIN, FABRICATED DOUBLE AND INSTALLED IAW FEDEX SRM 53-30-3 . 2 L 7 3 4F A3WE 1996032900280 19960329 00280 NM 1996 3 29 96FDEA00691 1 19960323 A 5330 SKIN BOEING 727 72722 1384002 NM BS 277.2 GOUGE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 BS 277.2 STR 21R WL 180, THERE IS A DEEP GOUGE IN SKIN. BLENDED GOUGE IN SKIN AT BS 277.2 STR 21R WL 180 ORIGINAL SKIN THICKNESS WAS .040, AREA REMOVED WAS .030. A 1 INCH BY .5 INCH AREA AND WAS FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53- 30-1. DAMAGED AREA WAS REPAIRED PER FEDEX SRM 53-30-3. 2 L 7 3 4F A3WE 1996032900281 19960329 00281 NM 1996 3 29 96FDEA00692 1 19960322 A 5320 9086043 STRINGER CLIP BOEING 727 72725 1384006 NM BS 1148 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 MECH DAMAGE TO STR CLIP BS 1148 STR 16R. REMOVED DAMAGED STR CLIP AND INSTALL NEW STR CLIP AT BS 1148 STR 16R. 2 L 7 3 4F A3WE 1996032900282 19960329 00282 NM 1996 3 29 96FDEA00693 1 19960325 A 5315 FLOOR BEAM BOEING 727 72725 1384006 NM BS 360 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 CORROSION (C53-224-01) ON FLOOR BEAM BS 360 LBL 12 RBL 5 AND 48 WL 208. REPAIRED FLOOR BEAM BS 360 LBL 12 AND RBL 5 WL 208. FOUND FLOOR BEAM BS 360 RBL 48 TO BE WITHIN SERVICEABLE LIMITS. CLEANED AND TREATED BS 360 RBL 48 WL 208 PER FEDE X SRM 51-10-6. REPAIRED FLOOR BEAM BS 360 LBL 12 AND RBL 5 WL 208 PER FEDEX SRM 53-10-8. 2 L 7 3 4F A3WE 1996032900283 19960329 00283 NM 1996 3 29 96FDEA00694 1 19960325 A 5330 SKIN BOEING 727 72722 1384002 NM BS 1110-1128 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 WHILE WORKING NR0602, FOUND SKIN AND BONDED DOUBLER TO HAVE CORROSION ON MATING SURFACES AT BS 1110 TO 1128 FROM STR 25 TO 26R. REMOVED CORROSION FROM BLER AND TRIPLER. DAMAGE ON TRIPLER WAS OUT OF LIMITS. FABRICATED NEW TRIPLER, ALODINE D AND PRIMED TRIPLER AND THE BARE METAL ON THE SKIN AND DOUBLER IAW FEDEX SRM 53-30-2. 2 L 7 3 4F A3WE 1996032900284 19960329 00284 NM 1996 3 29 96FDEA00696 1 19960325 A 5330 SKIN BOEING 727 72725 1384006 NM BS 1107-1060 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 CORROSION C53-113-01(2). FOUND WHILE WORKING NR 0240 FWD AND AFT CORNERS OF DOOR THRESHOLD STA (1107) TO 1060, WL 160, RBL 37. *****S/D**** REPLACED BARE STRAP LOWER HALF IAW EA 7-5310-28087. 2 L 7 3 4F A3WE 1996032900285 19960329 00285 NM 1996 3 29 96FDEA00697 1 19960325 A 5313 STRINGER BOEING 727 72725 1384006 NM BS 482 DAMAGE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 NR0604 AND 036, WHILE WORKING NR0156, FOUND MECH DAMAGE ON STR 24 AT STA 482. 2 L 7 3 4F A3WE 1996032900286 19960329 00286 NM 1996 3 29 96FDEA00698 1 19960325 A 5320 BEAM BOEING 727 72725 1384006 NM BS 760-848 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 NR0486 AND 034, CORROSION (C53-224-01) ON LONGITUDINAL BEAM AND BARE METAL AROUND NUT CLIP HOLES LOWER SURFACE BS 780 TO 848 LBL 25. 2 L 7 3 4F A3WE 1996032900287 19960329 00287 NM 1996 3 29 96FDEA00699 1 19960325 A 5320 DOUBLER BOEING 727 72725 1384006 NM BS 1050-1125 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 NR0611 AND 033, WHILE WORKING NR0602, FOUND DOUBLER TO HAVE CORROSION FROM BS 1050 TO 1125 FRONT STRINGER 26 TO 27R. 2 L 7 3 4F A3WE 1996032900288 19960329 00288 NM 1996 3 29 96FDEA00700 1 19960325 A 5751 65192591 HINGE FITTING BOEING 727 72725 1384006 NM RT AILERON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 NR0348 AND 030, RT WING O/B AILERON NR 3 HINGE FITTING IS CRACKED. 2 L 7 3 4F A3WE 1996032900290 19960329 00290 NM 1996 3 29 96UAL900213 1 19960325 A 5522 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LT ELEVATOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7443U 21897 MULTIPLE SITE CRACKING WAS FOUND IN 2 LOWER SKIN PANELS OF LT ELEVATOR. TWO CRACKS TOTALING 9.5 INCHES IN LENGTH FOUND AT APPROX ES19, 9.0 INCH CRACK AT APPROX ES161 AND 7.0 INCH CRACK AT APPROX ES138. THE INBD LOCATION CRACK EXTENDED. 2 L 7 3 4F 4 F A3WE E2EA 1996032900291 19960329 00291 NM 1996 3 29 96UAL900214 1 19960325 A 3350 POWER SUPPLY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7441U 21895 LT OVERWING EMERGENCY LIGHTS FLASH WHEN ACTIVATED. REPLACED POWER SUPPLY MODULE. 2 L 7 3 4F 4 F A3WE E2EA 1996032900292 19960329 00292 NM 1996 3 29 96UAL900215 1 19960325 A 8011 STARTER AIRESEARCH 39268811MOD BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE FAILED A UALA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 WP 29 7257U P4336 21404 CLIMBING THROUGH 7,000 FEET, GOT NR 1 ENGINE FIRE WARNING FOR 3 SECONDS THEN WENT OUT. SHUT DOWN NR 1 ENGINE. FLIGHT A TTENDANT REPORTED STRANGE NOISE FROM ENGINES. MAINTENANCE FOUND A CONTAINED STARTER FAILURE. UNDER INVESTIGATION. SUP PLEMENTAL DATA UPDATE: REPLACED STARTER, STARTER SWITCH AND GUARD, STARTER SHUTOFF VALVE, STARTER DEFLECTOR, CSD HOSE, AND STARTER VALVE ARM SWITCH. 2 L 7 3 4F 4 F A3WE E2EA 1996032900293 19960329 00293 WP 1996 3 29 96UAL900216 1 19960325 A 5330 SKIN DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 1846U 48262 EXTENSIVE CORROSION AND SKIN CRACKING ON FUSELAGE SKIN ON CIRCUMFERENTIAL THAT RUNS DIRECTLY FORWARD OF CENTER EQUIPMENT DOOR ON RIGHT SIDE ABOVE SHEAR STRIP IN BLUE PAINTED AREA. INTERNAL STRUCTURE CORROSION WAS LIMITED TO LIGHT SURFACE C ORROSION WHICH WAS CLEANED AND PAINTED. PERFORMED CLASS 3 SKIN REPAIR TO AFFECTED AREA PER SRM 53-20-00. APPROXIMATE S IZE OF PATCH WAS 24 INCHES VERTICALLY BY 18 INCHES LONG. 2 L 7 3 4F 4 F A22WE E23EA 1996032900294 19960329 00294 NM 1996 3 29 96UAL900217 1 19960325 A 2934 EA1093A3679 QTY TRANSMITTER BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE A HYD SYST SHORTED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 9006U 19044 AFTER TAKEOFF ON GEAR RETRACTION, "A" SYSTEM HYDRAULIC QUANTITY DROPPED TO 1/2 GALLON. AFTER LOWERING GEAR, QUANTITY SH OWED FULL, THEN WENT BACK TO 1/2 GALLON. GAUGE JUMPED AROUND AFTER LANDING AND WENT TO FULL. SUPPLEMENTAL DATA UPDATE: REPLACED "A" SYSTEM HYDRAULIC RESERVOIR QUANTITY TRANSMITTER. SHOP VERIFIED 'DEAD SPOT' FOUND IN TRANSMITTER. 2 L 7 2 4F 4 F A16WE E2EA 1996032900295 19960329 00295 1996 3 29 ARWA9603010 4 19960327 A 3442 26071570157 RT UNIT DOUG DC8 DC863 302198A WP WEATHER RADAR FAILED A ARWA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 345JW 46042 AFTER DEPARTURE FROM MIAMI, 15 MINUTES OUT, WEATHER RADAR PAINTED AN UNDEFINABLE LINE AND BECAME UNRELIABLE FOR NAVIGATI ON PURPOSES. FLIGHT RETURNED TO MIA. REMOVED AND REPLACED NR 1 RADAR R T AND ANTENNA PER MM 34-41-00, OPS NORMAL. 2 L 7 4 4F 4A25 1996032900296 19960329 00296 SO 1996 3 29 COMA9610113 1 19960325 A 2434 30081001 GENERATOR EMB 120 EMB120RT SO RT ENGINE FAILED A COMA K NONE O OTHER CR CRUISE 1 SO 01 463CA 15325 1479 120267 RT ENGINE AUXILIARY GENERATOR FAILED. REPLACED THE AUXILIARY GENERATOR. 2 L 7 2 4T RT A31SO 1996032900297 19960329 00297 SO 1996 3 29 COMA9610114 1 19960325 A 3250 M10628023 RELAY EMB 120 EMB120RT SO NLG STEERING FAILED A COMA O OTHER O OTHER LD LANDING 1 SO 01 265CA 120257 NOSE WHEEL STEERING FAILED DURING LANDING. REPLACED RELAY KO 123. 2 L 7 2 4T RT A31SO 1996032900298 19960329 00298 1996 3 29 COMA9630084 2 19960325 A 7532 321935 BLEED AIR VALVE SAAB SF340 SF340A 7850100 EU LT ENGINE MALFUNCTION A COMA C D ABORTED TAKEOFF RETURN TO BLOCK M OVER TEMP TO TAKEOFF 1 SO 01 356CA 23945 340A034 LEFT ENGINE TEMP 952 DEGREES CELSIUS DURING TAKEOFF. REPLACED THE HIGH PRESSURE BLEED VALVE. 2 L 7 2 4T RT A52EU 1996032900299 19960329 00299 NE 1996 3 29 COMA9630085 2 19960326 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LEFT FAILED A COMA O OTHER O OTHER CR CRUISE 1 SO 01 344CA 340A025 367478 LEFT PROPELLER RPM FLUCTUATES WHEN ENGINE ANTI-ICE IS ON. EXTENSIVE TROUBLESHOOTING AND COMPONENT REPLACEMENT DID NOT F IX THIS PROBLEM. REPLACED THE LEFT ENGINE. 2 L 7 2 4T 4 T RT A52EU E8NE6 1996032900300 19960329 00300 EA 1996 3 29 COMA9660053 1 19960325 A 5610 NP1393211 WINDSHIELD CNDAIR CL600 CL6002B19 EA LT COCKPIT SHATTERED A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 947CA 7077 PILOTS FRONT WINDSHIELD SHATTERED. REPLACED WINDSHIELD. 2 L 7 2 4F RT A21EA 1996032900301 19960329 00301 WP 1996 3 29 DHL96801008 1 19960315 A 2910 000A5040534 HOSE DOUG DC8 DC873 302199C WP STBY PUMP RUPTURED A T DHLA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 801DH 46033 AFTER DEPARTURE, NOTICED HYD QTY AT THE N OF NORMAL. COMPLETED ABNORMAL PROCEDURE AND COULDN'T DETECT ANY FURTHER LOSS. AFTER MONITORING QTY FOR 1 HOUR, NOTICED CONTINUING QTY LOSS. DECIDED ON PRECAUTIONARY LANDING AT DEN. AFTER LANDING AND TAXIING OFF RUNWAY, HYD QTY DEPLETED TO AUX LEVEL AND LOST HYD PRESSURE, CALLED FOR TUG. FOUND LEAK IN RUDDER STAN DBY PUMP LINE TO ACCUMULATOR. REPLACED LINE IAW MM 29-11-71. NO LEAKS NOTED, SERVICED MAIN SYSTEM HYDRAULIC RESERVIOR. 2 L 7 4 4F RT 4A25 1996032900302 19960329 00302 WP 1996 3 29 MWEA96064 1 19960321 A 2560 5917689103 SLIDE COVER DOUG DC9 DC932 3022066 WP GALLEY SERV DOOR FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 302ME 47102 CREW REPORTS, GALLEY SERVICE DOOR EVACUATION SLIDE COVER FELL OFF. REINSTALLED SLIDE COVER. 2 L 7 2 4F A6WE 1996032900303 19960329 00303 WP 1996 3 29 MWEA96065 1 19960323 A 5751 5910045504 SKIN DOUG DC9 DC914 3022034 WP RT AILERON CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45728 DURING INSPECTION, FOUND RT AILERON SKIN CHAFED FROM FAIRING SKIN ON WING TRAILING EDGE. INSTALLED STAINLESS STEEL DOUB LER REPAIR IAW SRM 57-01 FIG 2 SHEET 2. REBALANCED. 2 L 7 2 4F A6WE 1996032900304 19960329 00304 WP 1996 3 29 MWEA96066 1 19960324 A 3260 SOCKET ASSY DOUG DC9 DC932 3022066 WP NLG INDICATOR FAILED A MWEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 401ME 47133 PILOT REPORTS, NOSE GEAR GREEN LIGHT WOULD NOT EXTINGUISH WITH GEAR HANDLE UP. FLIGHT RETURNED TO MKE. REPLACED NOSE G EAR INDICATION LIGHT SOCKET ASSY, OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996032900305 19960329 00305 NM 1996 3 29 P5CA9600165 1 19960326 A 5330 SKIN BOEING 747 747132 1384882 NM BS 1800-1810 DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 GROUND DAMAGE AFT FUSELAGE AT STA 1800 TO 1810 STR 34R TO 35R SHOWS DENT AND .75 INCH CRACK BETWEEN AFT CARGO DOOR AND D OOR CONTROL SWITCH. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-30-03. PRESSURIZED, LEAK CHECK OK. 2 L 7 4 4F A20WE 1996032900306 19960329 00306 NM 1996 3 29 P5CA9600166 1 19960326 A 2751 98010903 POSITION IND BOEING 747 747123 1384873 NM TE FLAP INOPERATIVE A P5CA O OTHER N FALSE WARNING DE DESCENT 1 WP 23 859FT 20326 TRAILING EDGE FLAPS SELECTED TO 30 DEGREES, THEY WOULD ONLY EXTEND TO 25 DEGREES. EXERCISED FLAP DOWN SWITCH FOR INBOAR D FLAPS. REPLACED INBOARD FLAP POSITION INDICATOR AND SWITCH S938 ON FLAP POSITION LEVER. OPS CHECKS NORMAL IAW MM 27- 51. 2 L 7 4 4F A20WE 1996032900307 19960329 00307 EU 1996 3 29 QXEA9600133 1 19960326 A 3350 1312 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 462AU 11054 LEFT OVERWING EXIT SIGN IS INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996032900308 19960329 00308 1996 3 29 RRXA9600011 4 19960321 A 3400 INSTR AMPLIFIER DOUG DC8 DC873F 302199F WP RT COCKPIT FAILED A RRXA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 WP 15 792FT 46046 KDAY - FLT 13 - SMOKE IN THE COCKPIT UPON LANDING. UNABLE TO IDENTIFY SOURCE. SMOKE CLEARED QUICKLY ON TAXI IN. MAINT ENANCE FOUND THE FIRST OFFICER'S HORIZON C/B OPEN AND THE FLIGHT DIRECTOR INOP. REMOVED AND REPLACED THE F/O'S INSTRUME NT AMPLIFIER AND HORIZON. NO DEFECTS NOTED ON GROUND CHECK. (M) 2 L 7 4 4F RT 4A25 1996032900309 19960329 00309 NE 1996 3 29 RRXA9600012 2 19960326 A 7530 CLAMP DOUG DC8 DC862F 3021972 WP PWA JT3D JT3D7 52039 NE NR 2 ENGINE MISSING A RRXA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 15 997CF 46154 669564 KAUS - FLT 107 - AFTER TAKEOFF FROM KAUS NR 2 ENGINE FIRE WARNING SOUNDED. THE FLIGHT CREW SHUTDOWN NR 2 ENGINE AND RET URNED TO KAUS. MAINTENANCE FOUND NO EVIDENCE OF FIRE. MAINTENANCE FOUND A CLAMP OFF AT THE HIGH STAGE BLEED VALVE ELBO W DUCT. MAINTENANCE RECLAMPED THE ELBOW DUCT AND REPAIRED DAMAGED WIRING TO THE PNEUMATIC PRESSURE REGULATOR. AN OPERA TIONAL CHECK OF THE NR 2 ENGINE PNEUMATIC REGULATOR, FIRE WARNING SYSTEM, AND THE ENGINE WAS GOOD. (M) 2 L 7 4 4F 4 F 4A25 1E8 1996032900310 19960329 00310 NM 1996 3 29 SCNA96035 1 19960320 A 2611 PC1604 SMOKE DET BATT BOEING 727 7272J4 1384006 NM LT AFT LAV DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 288SC 20765 LEFT AFT LAV SMOKE DETECTOR WOULD NOT TEST. REMOVED AND REPLACED BATTERY IN LEFT AFT LAV SMOKE DETECTOR. DETECTOR OPS CHECKED GOOD. 2 L 7 3 4F RT A3WE 1996032900311 19960329 00311 1996 3 29 SCNA96036 4 19960321 A 3418 9654020003 AOA DOUG DC10 DC1030F 3023504 WP FWD FUSELAGE FAILED A SCNA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 601GC 47921 STALL WARNING ACTIVATED AFTER TAKEOFF, AIRCRAFT RETURNED TO BLOCK. REMOVED AND REPLACED ANGLE OF ATTACK SENSOR. 2 L 7 3 4F RT A22WE 1996032900312 19960329 00312 WP 1996 3 29 SCNA96037 1 19960315 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 330 DAMAGED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 572SC 46977 THE FUSELAGE SKIN AND FRAME AT STATION 330 WERE DAMAGED DUE TO CONTACT WITH A GROUND VEHICLE. MAJOR REPAIR WAS ACCOMPLI SHED PER SUN COUNTRY ENGINEERING ORDER 53-5225-1. 2 L 7 3 4F A22WE 1996032900313 19960329 00313 NM 1996 3 29 SWAA960170 1 19960322 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 95SW 23054 DURING SCHEDULED SERVICE CHECK, FOUND 2 FUSELAGE SKIN CRACK 10 INCHES FWD OF WATER SERVICE DOOR. REPAIRED PER BOEING SR M. 2 L 7 2 4F A16WE 1996032900314 19960329 00314 NM 1996 3 29 SWAA960171 1 19960322 A 5315 FLOOR BEAM BOEING 737 7375H4 138449D NM BS 986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 511SW 24188 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM NUTPLATE HOLE CORRODED AT BS 986.5. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996032900315 19960329 00315 NM 1996 3 29 SWAA960172 1 19960322 A 5315 FLOOR BEAM BOEING 737 7375H4 138449D NM BS 986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 511SW 24188 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM NUTPLATE HOLE CORRODED AT BS 986.5 RBL 30. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996032900316 19960329 00316 NM 1996 3 29 SWAA960173 1 19960322 A 5320 ANGLE BOEING 737 7375H4 138449D NM BS 294 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 511SW 24188 DURING SCHEDULED 1/2 D-CHECK, FOUND 3.3 INCH CRACK IN RADIUS OF RT CREASE BEAM I/B CHORD ANGLE AT BS 294, RBL 54. REPAI RED PER BOEING SRM AND TYPICAL REPAIR T1-A53-023. 2 L 7 2 4F RT A16WE 1996032900317 19960329 00317 NM 1996 3 29 SWAA960174 1 19960322 A 5315 FLOOR BEAM BOEING 737 7375H4 138449D NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 511SW 24188 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM AFT FLANGE CORRODED AT BS 312 LBL 15. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996032900318 19960329 00318 NM 1996 3 29 SWAA960175 1 19960322 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 800 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 800 WL 205. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996032900319 19960329 00319 NM 1996 3 29 SWAA960176 1 19960322 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 972 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 62SW 22060 DURING SCHEDULED C-CHECK, FOUND FUSELAGE SKIN CRACK AT BS 972 AT S25L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996032900320 19960329 00320 NM 1996 3 29 SWAA960177 1 19960322 A 5240 SKIN BOEING 737 7372H4 138448C NM FWD SERV DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 81SW 22730 DURING SCHEDULED B2 CHECK, FOUND FWD SERVICE DOOR CRACKED AT LOWER HINGE UPPER RADIUS ON DOOR SKIN. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996032900321 19960329 00321 NM 1996 3 29 SWAA960178 1 19960322 A 5210 SKIN BOEING 737 7372H4 138448C NM AFT ENTRY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 81SW 22730 DURING SCHEDULED B2 CHECK, FOUND AFT ENTRY DOOR UPPER HINGE CUTOUT CRACKED ON DOOR AT RADIUS. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996032900322 19960329 00322 NM 1996 3 29 SWAA960179 1 19960322 A 5312 BULKHEAD WEB BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 83SW 22732 DURING SCHEDULED D-CHECK, FOUND 2 INCH CRACK AT BS 178 BULKHEAD PRESSURE WEB, RBL 9.7 WL 219. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996032900323 19960329 00323 NM 1996 3 29 SWAA960180 1 19960322 A 5312 BULKHEAD WEB BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 83SW 22732 DURING SCHEDULED D-CHECK, FOUND 1.8 INCH CRACK AT BS 178 BULKHEAD PRESSURE WEB, LBL 11.3 WL 219. REPAIRED PER BOEING S RM. 2 L 7 2 4F A16WE 1996032900324 19960329 00324 NM 1996 3 29 SWAA960181 1 19960322 A 5320 WEB BOEING 737 7372H4 138448C NM BS 530 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 83SW 22732 DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AT BS 530, RBL 43 WL 161. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996032900325 19960329 00325 NM 1996 3 29 SWAA960182 1 19960322 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 83SW 22732 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 663 RBL 24 AND LBL 24 WL 201. REPAIRED PER BOEING SRM AND B OEING DRAWING 691A0032. 2 L 7 2 4F A16WE 1996032900326 19960329 00326 NM 1996 3 29 SWAA960183 1 19960322 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 83SW 22732 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACK INDICATION AROUND FASTENER HEAD AT BS 178 WL 234 RBL 10. REPAIRED P ER BOEING SRM. 2 L 7 2 4F A16WE 1996032900327 19960329 00327 EA 1996 3 29 SWIA95723 1 19960210 A 5315 FLOOR BEAM CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE BS 295-349 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 408SW 7055 FLOOR BEAM RIGHT O/B RBL 27.00 WL 73.5 STA .295 TO 349, CORROSION FOUND ON TOP SURFACE. REMOVAL OF CORROSION IS BEYOND LIMITS OF REO 601R-53-00-005. FLOOR BEAM REPAIRED IAW 601R-53-21-058. 2 L 7 2 4F 4 F RT A21EA E15NE 1996032900328 19960329 00328 EA 1996 3 29 SWIA95724 1 19960210 A 5315 FLOOR BEAM CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE BS 310-349 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 408SW 7055 FLOOR BEAM RT RBL 9.0 WL 73.50 STA 310 TO 349, CORROSION FOUND ON UPPER SURFACE. CORROSION BEYOND LIMITS OF REO 601R-53 -00-00 SHT 3 FIG 1 .003 STN 319.0. FLOOR BEAM REPAIRED IAW REO 601R-53-21-058. 2 L 7 2 4F 4 F RT A21EA E15NE 1996032900329 19960329 00329 SO 1996 3 29 SWIA95725 1 19960305 A 2915 RELIEF VALVE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT HYD PACK FAILED A SWIA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 189SW 120048 LOSS OF HYDRAULIC FLUID ON LEFT SIDE. REPLACED MANUAL RELIEF VALUE ON LEFT HYDRAULIC PACK AND SERVICED FLUID TO PROPER LEVEL, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1996032900330 19960329 00330 SO 1996 3 29 SWIA95726 1 19960305 A 2910 HYD BLEED VALVE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE BLUE HYD SYST FAILED A SWIA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 07 189SW 120048 LOSS OF BLUE SYSTEM HYDRAULICS IN FLIGHT. CLEARED WATER FROM RIGHT HYDRAULIC RESERVIOR CHAMBER. INSTALLED NEW MANUAL B LEED VALUE. OPS CHECKED HYDRAULIC SYSTEM, OPS AND LEAK CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1996032900331 19960329 00331 NM 1996 3 29 VSTA9603002 1 19960111 A 2782 65507244 ACTUATOR FITTING BOEING 737 737204 1384458 NM NR 1 LE SLAT FAILED A VSTA K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 WP 07 312VA 20236 LOSS OF 'A' SYSTEM HYDRAULIC FLUID. NR 1 SLAT ACTUATOR ATTACH FITTING FAILED CAUSING HYDRAULIC LINE TO RUPTURE. REPLAC ED FITTING AND LINES. 2 L 7 2 4F A16WE 1996032900334 19960329 00334 CE 1996 3 29 96ZZZX1363 1 19960308 A 5751 9913000011 SKIN 991300003 BEECH 100 B100 1152919 CE RT AILERON CRACKED A A DSEA K NONE O OTHER IN INSP/MAINT 1 GL 25 771S 3742 LJ792 BE52 FOUND DURING INSPECTION. SKIN CRACKED APPROXIMATELY 12 INCHES FROM INBOARD END WHERE LEADING EDGE SKIN AND UPPER SKIN A RE ATTACHED TO SPAR. SUBMITTER STATED THIS IS THE THIRD AIRCRAFT WITH CRACKS IN THE SAME PLACE. 1 L 7 2 4T A14CE 1996032900343 19960329 00343 CE 1996 3 29 96ZZZX1372 1 19960308 A 5751 991300003 SKIN BEECH 100 B100 1152919 CE RT AILERON CRACKED A A DSEA K NONE O OTHER IN INSP/MAINT 1 GL 25 2025S 6074 LJ799 BE54 FOUND DURING INSPECTION. SKIN CRACKED APPROXIMATELY 6 INCHES FROM OUTBOARD END WHERE LEADING SKIN AND UPPER SKIN ARE AT TACHED TO SPAR. SUBMITTER STATES THIS IS FOURTH B100 AIRCRAFT WITH CRACKS ON UPPER SKIN. HAVE NOT HAD ANY PROBLEMS ON LT AILERONS. 1 L 7 2 4T A14CE 1996032900362 19960329 00362 WP 1996 3 29 9606989609 1 19960322 A 3350 6011779 BATTERY PACK DOUG DC9 DC932 3022066 WP LEFT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 609NW 47234 DURING LINE MAINTENANCE INSPECTION, FOUND THE LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AND OPERA TIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996032900363 19960329 00363 WP 1996 3 29 9606999612 1 19960320 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP TAILCONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 612NW 47436 DURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES AND OPERATIONAL CHE CK NORMAL. 2 L 7 2 4F A6WE 1996032900364 19960329 00364 WP 1996 3 29 9607009925 1 19960326 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 925US 47472 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE AND BATTERY PACK AN D OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996032900365 19960329 00365 1996 3 29 9607019960 4 19960326 A 2565 13621224 EVAC SLIDE DOUG DC9 DC931 3022065 WP TAILCONE LOW PRESSURE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 920RW 47163 DURING PERIODIC CHECK, FOUND TAILCONE EVACUATION SLIDE LOW ON PRESSURE. REPLACED SLIDE. 2 L 7 2 4F A6WE 1996032900366 19960329 00366 WP 1996 3 29 9607029996 1 19960327 A 2820 VENT VALVES DOUG DC9 DC931 3022065 WP WING FUEL TANKS OPEN A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 8932E 47141 FUEL BEGAN VENTING FROM THE RIGHT WING AFTER TAKEOFF. THE LEFT FUEL QUANTITY DROPPED 800 LBS BELOW RIGHT SIDE. BOTH FU EL QUANTITIES WERE BELOW 8,800 LBS. FLIGHT RETURNED TO YUL AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET CLIMB VENT V ALVES. 2 L 7 2 4F A6WE 1996032900367 19960329 00367 NM 1996 3 29 9607036614 1 19960327 A 2720 SERVO UNIT BOEING 747 747251B 1384892 NM RUDDER CONTROL MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 614US 20359 DURING TAKEOFF, THE RUDDER RATIO LIGHT ILLUMINATED. AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACED THE RU DDER AMPLIFIER AND SERVO UNIT AND OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996032900368 19960329 00368 NM 1996 3 29 9607046614 1 19960327 A 2720 RATIO COMPARATOR BOEING 747 747251B 1384892 NM RUDDER CONTROL MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 614US 20359 DURING TAKEOFF, THE RUDDER RATIO LIGHT ILLUMINATED. AIRCRAFT ABORTED TAKEOFF AT 20 KNOTS AND RETURNED TO THE GATE. REP LACED THE RUDDER RATIO COMPARATOR AND OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996032900369 19960329 00369 WP 1996 3 29 9607059759 1 19960326 A 3260 CONNECTOR DOUG DC9 DC941 302207N WP LT UPLIMIT SW DIRTY A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 759NW 47287 DURING TAKEOFF FROM MSP, THE LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON. RETURNED TO MSP AND LANDED WITHOUT INCIDE NT. FOUND DIRT ON THE UPLIMIT SWITCH CANNON PLUG. CLEANED CANNON PLUG. REPLACED UPLIMIT SWITCH AND DOWNLOCK SWITCH PRE CAUTIONARY. GEAR OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F A6WE 1996032900370 19960329 00370 NM 1996 3 29 96FDEA00384 1 19960304 A 5330 SKIN BOEING 727 727233 138408A NM BS 400 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 TWO DENTS IN FUSELAGE SKIN BS 400 STR 17L. REPAIRED TWO DENT IN FUSELAGE SKIN BS 400 STR 17L PER FEDEX SRM 53-30-03 FIG 1. 2 L 7 3 4F RT A3WE 1996032900371 19960329 00371 NM 1996 3 29 96FDEA00421 1 19960305 A 7110 65196854541 NOSE COWL BOEING 727 727233 138408A NM NR 1 ENGINE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 NR 1 ENG NOSE COWL LIP RING EXTERNAL SKIN HAS A DENT AT APPROX 9 O'CLOCK POSITION. REMOVED NR 1 ENG NOSE COWL AND SENT OUT FOR REPAIR. INSTALLED SERVICEABLE NR 1 ENG COWL IAW FEDEX MM 71-10-21. 2 L 7 3 4F RT A3WE 1996032900372 19960329 00372 NM 1996 3 29 96FDEA00425 1 19960305 A 5347 SEAT TRACK BOEING 727 727233 138408A NM BS 1045-1120 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CORROSION (C53-224-02, 3) (C53-224-04) ON SEAT TRACK FLANGES BS 1045 TO 1075 AND 1100 TO 1120 RBL 45 WL 208. REMOVED AN D REPLACED DAMAGED SECTION OF SEAT TRACK AT BS 1060 TO 1080 RBL 45 WL 208 IAW FEDEX SR 53-10-5. REMOVED CORROSION FROM SEAT TRACK FLANGES BS 1100 TO 1120 RBL 45 WL 208 FOUND TO BE WITHIN LIMITS PER FEDEX SRM 53-10-1. 2 L 7 3 4F RT A3WE 1996032900373 19960329 00373 NM 1996 3 29 96FDEA00427 1 19960305 A 5315 FLOOR BEAM BOEING 727 727233 138408A NM BS 1110 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CORROSION (C53-224-01, 3) (C53-22404) ON UPPER CHORD OF FLOOR BEAM BS 1110 RBL 35 AND 41 WL 208. REPAIRED UPPER CHORD O F FLOOR BEAM BS 1110 RBL 41 IAW FEDEX SRM 53-10-8. REMOVED CORROSION AT RBL 35 AND FOUND TO BE WITHIN LIMITS IAW FEDEX SRM 53-10-1. 2 L 7 3 4F RT A3WE 1996032900374 19960329 00374 NM 1996 3 29 96FDEA00428 1 19960305 A 5347 BAC1520793 SEAT TRACK BOEING 727 727233 138408A NM BS 720-740 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CORROSION (C53-224-01) ON BS 740 RBL 45 WL 208 SEAT TRACK I/B FLANGE. REMOVED AND REPLACED SEAT TRACK FROM BS 720E TO 7 40 RBL 45 WL 208 IAW FEDEX SRM 53-10-5. 2 L 7 3 4F RT A3WE 1996032900375 19960329 00375 NM 1996 3 29 96FDEA00431 1 19960305 A 5347 SEAT TRACK BOEING 727 727233 138408A NM BS 950 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CORROSION (C53-224-01-, 3) AND (C53-224-04) ON SEAT TRACK FLANGE AT BS 950E PLUS 5 RBL 25 WL 208. CANCELLED LLM 1677. 2 L 7 3 4F RT A3WE 1996032900376 19960329 00376 NM 1996 3 29 96FDEA00434 1 19960305 A 5320 FLOOR SUPPORT BOEING 727 727233 138408A NM BS 644 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CORROSION (C53-113-01,1) ON FLOOR SUPPORT AROUND NUTPLATE HOLES AT BS 644 RBL 8.5 WL 157.5. REMOVED DAMAGED PORTION OF FLOOR SUPT FABRICATED REPAIR PART AND INSTALLED PER FEDEX SRM 51-40-3. 2 L 7 3 4F RT A3WE 1996032900377 19960329 00377 NM 1996 3 29 96FDEA00438 1 19960305 A 5320 THRESHOLD BOEING 727 727233 138408A NM BS 601 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 FWD CARGO THRESHOLD HAS A ON O/B EDGE AT STA 601. CRACK ON FWD CARGO THRESHOLD AT STA 601 WAS TIG WELDED IAW BOEING DRW NR 65-56169SDR. 2 L 7 3 4F RT A3WE 1996032900378 19960329 00378 NM 1996 3 29 96FDEA00442 1 19960305 A 5320 FORMER BOEING 727 727233 138408A NM BS 720 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CRACKED FAIRING FORMER BS 720 WL 148 RIGHT. REMOVED AND REPLACED FAIRING FORMER AT BS 720 PLUS 8 WL 148 RT SIDE IAW FE DEX SRM 51-30-2. 2 L 7 3 4F RT A3WE 1996032900379 19960329 00379 NM 1996 3 29 96FDEA00706 1 19960327 A 5230 INNER SKIN BOEING 727 727233 138408A NM CARGO DOOR CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CORROSION (C53-111-02, 2) NR 3 CARGO DOOR INNER SKIN HAS CORROSION AROUND A RIVNUT 12 INCHES FROM THE AFT EDGE 10 INCHES FROM THE BOTTOM. REMOVED CORROSION FROM NR 3 CARGO DOOR INNER SKIN AROUND RIVNUT FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. REPAIRED DAMAGED AREA PER FEDEX SRM 51-40-2. 2 L 7 3 4F RT A3WE 1996032900380 19960329 00380 NM 1996 3 29 96FDEA00707 1 19960327 A 5311 FRAME BOEING 727 727233 138408A NM BS 720 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 DAMAGED FASTENER HOLE IN FRAME AT BS 20A LBL 10 STR 28L. REPAIRED PER FEDEX SRM 51-40-02. 2 L 7 3 4F RT A3WE 1996032900381 19960329 00381 NM 1996 3 29 96FDEA00709 1 19960319 A 5315 FLOOR BEAM BOEING 727 72722C 138400F NM BS 344 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 103FE 19199 UPPER LOBE SLAT BS 344 FLOOR BEAM HAS CORROSION FROM RBL 2 TO LBL 54. REMOVED CORRODED BEAM CAP OF FLOOR BEAM AND INSTA LLED NEW REPAIR PER SRM 53-10-8. 2 L 7 3 4F A3WE 1996032900382 19960329 00382 NM 1996 3 29 96FDEA00710 1 19960319 A 5330 SKIN LAP BOEING 727 72722C 138400F NM FS 420-440 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 130FE 19199 UPPER LOBE, CORROSION IN SKIN LAP FS 420 TO 440 BETWEEN STR 5 TO 6L. CORROSION REMOVED PER SRM 51-10-6, REPAIR INSTALLE D PER SRM 51-40-2 PAGES 1 TO 6. 2 L 7 3 4F A3WE 1996032900383 19960329 00383 NM 1996 3 29 96FDEA00711 1 19960320 A 5312 BULKHEAD BOEING 727 72722C 138400F NM FS 1183 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 103FE 19199 AFT CARGO COMPARTMENT FS 1183 BULKHEAD IS CRACKED BL 30 RT, 10 ABOVE STR 26L COMING OUT BEHIND HORIZ STIFFENER. CRACKED AREA OF BULKHEAD REMOVED AND FILLER AND DOUBLER INSTALLED PER BOEING SB 727-53-0215. 2 L 7 3 4F A3WE 1996032900384 19960329 00384 NM 1996 3 29 96FDEA00712 1 19960325 A 5311 BELLFRAME BOEING 727 72722C 138400F NM FS 1090 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 103FE 19199 AFT CARGO COMP FS 1090 BELLFRAME CRACKED IN FLANGE AND INTO WEB IN AREA BETWEEN STR 26 AND 27L. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 51-40-3. 2 L 7 3 4F A3WE 1996032900385 19960329 00385 NM 1996 3 29 96FDEA00713 1 19960326 A 5311 BELLFRAME BOEING 727 72722C 138400F NM BS 580 DENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 103FE 19199 UPPER LOBE BS 580 STR 6R DENT IN BELLFRAME. REMOVED DAMAGED SECTION OF BELLFRAME, FABRICATED SECTION OF BELLFRAME, INST ALLED BELLFRAME REPAIR PER SRM 53-10-4 FIG 1. 2 L 7 3 4F A3WE 1996032900386 19960329 00386 NM 1996 3 29 96UAL900218 1 19960326 A 3397 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 545UA 25323 AFT CABIN FLOOR EMERGENCY ESCAPE LIGHTING INOP AT LAVATORY. DISCOVERED FEEDER WIRE TO LIGHT STRIP BROKEN. REPLACED BRO KEN SECTION, LIGHT CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996032900387 19960329 00387 EU 1996 3 29 96UAL900219 1 19960326 A 3350 BATTERY PACK AIRBUS 320 A320232 3930326 EU IAE V2500 V2527A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 410UA 463 MID CABIN EMERGENCY ESCAPE PATH LIGHTING GOES OUT AFTER ONE MINUTE OF OPERATION. REPLACED MID CABIN EMERGENCY LIGHTING BATTERY PACKS AND OPERATED NORMAL. 2 L 7 2 4F RT A28NM E40NE 1996032900388 19960329 00388 NM 1996 3 29 96UAL900220 1 19960326 A 3350 LIGHT BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 163UA 21353 CEILING EMERGENCY LIGHT IS INOP. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F A20WE E20EA 1996032900390 19960329 00390 NM 1996 3 29 96UAL900222 1 19960327 A 5522 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LT ELEVATOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7443U 21897 MULTIPLE SITE CRACKING WAS FOUND IN 2 LOWER SKIN PANELS OF LT ELEVATOR. TWO CRACKS TOTALING 9.5 INCHES IN LENGTH FOUND AT APPROX ES19, 9.0 INCH CRACK AT APPROX ES161 AND 7.0 INCH CRACK AT APPROX ES138. THE INBD LOCATION CRACK EXTENDED. 2 L 7 3 4F 4 F A3WE E2EA 1996032900393 19960329 00393 WP 1996 3 29 ABXA9600356 1 19960309 A 5330 49157601 SKIN DOUG DC9 DC932 3022066 WP FWD FUSELAGE GOUGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 47364 DURING C-CHECK INSPECTION, FOUND THE FUSELAGE SKIN AND HOLD OPEN POCKET GOUGED AT THE SERVICE DOOR. REPAIRED SKIN IAW D C-9 SRM 53-04, REPLACED POCKET IAW DC-9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1996032900394 19960329 00394 WP 1996 3 29 ABXA9600357 1 19960306 A 5400 5913262 ANGLE DOUG DC9 DC932 3022066 WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 987AX 47364 DURING C-CHECK INSPECTION, FOUND A CRACK IN THE UPPER PYLON ATTACH ANGLE AT STA 980. REPAIRED IAW DC-9 SRM 54-04, FIGUR E 10. 2 L 7 2 4F A6WE 1996032900397 19960329 00397 WP 1996 3 29 ABXA9600374 1 19960125 A 5330 59114272 SKIN DOUG DC9 DC931 3022065 WP FS 966-987 DENTED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE RIGHT AFT FUSELAGE SKIN HAD TWO DENTS BETWEEN FS 966 AND 987, BET WEEN LONGERONS 16R AND 18R. REPAIRED AFT FUSELAGE SKIN IAW ABX REA D953-13715-MR. 2 L 7 2 4F A6WE 1996032900398 19960329 00398 WP 1996 3 29 ABXA9600375 1 19960108 A 5330 591142374 SKIN DOUG DC9 DC931 3022065 WP FS 980-1005 DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE RIGHT AFT FUSELAGE SKIN PANEL CREASED BETWEEN FS 980 AND FS 1005 AT LONGERON 21R. REPAIRED IAW ABX REA D953-13765-MR. 2 L 7 2 4F A6WE 1996032900403 19960329 00403 WP 1996 3 29 ABXA9600380 1 19960122 A 5315 99115451 FLOOR BEAM DOUG DC9 DC931 3022065 WP FS 389-408 CHAFED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE FLOOR BEAM AT FS 389 AND 408 GOUGED AND CHAFED. REPAIRED FLOOR B EAMS IAW ABX REA D953-13826-MR. 2 L 7 2 4F A6WE 1996032900404 19960329 00404 WP 1996 3 29 ABXA9600381 1 19960122 A 5315 9911544507 FLOOR BEAM DOUG DC9 DC931 3022065 WP FS 389-408 CHAFED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE FLOOR BEAMS AT FS 389 AND 408 GOUGED AND CHAFED. REPAIRED FLOOR BEAMS IAW ABX REA D953-13826-MR. 2 L 7 2 4F A6WE 1996032900407 19960329 00407 WP 1996 3 29 ABXA9600384 1 19960326 A 5730 99193723 SKIN DOUG DC9 DC932 3022066 WP WS 214 GOUGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 DURING C INSPECTION, FOUND A DEEP GOUGE IN NR 2 SLAT DRIVE TRACK CUTOUT IN LEADING EDGE SKIN. REPAIRED IAW ABX REA D957 -18788. 2 L 7 2 4F A6WE 1996032900409 19960329 00409 WP 1996 3 29 ABXA9600386 1 19960102 A 5512 5922577505 SKIN DOUG DC9 DC931 3022065 WP LT HORIZ STAB DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND AN EXISTING REPAIR ON THE LEFT HORIZONTAL STABILIZER LOWER CENTER SKI N PANEL THAT WAS NOT IAW THE DC-9 SRM. REPAIRED LEFT HORIZONTAL STABILIZER LOWER SKIN IAW ABX REA D955-13852-MR. 2 L 7 2 4F A6WE 1996032900410 19960329 00410 WP 1996 3 29 ABXA9600387 1 19960207 A 5330 5910142505 SKIN DOUG DC9 DC931 3022065 WP FS 370-427 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE FUSELAGE SKIN AT FORWARD EDGE OF THE FORWARD CARGO COMPARTMENT DO OR JAMB HAD TWO CRACKS AND EXCESSIVE CORROSION BLENDOUTS. REPAIRED IAW ABX REA D953-13853-MR. 2 L 7 2 4F A6WE 1996032900412 19960329 00412 WP 1996 3 29 ABXA9600389 1 19960111 A 5330 5911401147 SKIN DOUG DC9 DC931 3022065 WP FS 148 DENTED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE RIGHT FORWARD FUSELAGE SKIN AT FS 148 AND LONGERON 19R HAD A SHAR P DENT THAT EXCEEDED THE DC-9 SRM LIMITS. REPAIRED RIGHT FUSELAGE FORWARD SKIN IAW ABX REA D953-13887-MR. 2 L 7 2 4F A6WE 1996032900414 19960329 00414 WP 1996 3 29 ABXA9600391 1 19960118 A 5311 9919614501 FRAME DOUG DC9 DC931 3022065 WP FS 639 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE LEFT FUSELAGE FRAME AT FS 639 HAD A PREVIOUS REPAIR ON THE AFT SI DE AT LONGERON 18L THAT HAD CRACKED THROUGH THE PREVIOUS STOP DRILL. REPAIRED LEFT FUSELAGE FRAME AT FS 639 IAW ABX REA D953-13924-MR. 2 L 7 2 4F A6WE 1996032900415 19960329 00415 WP 1996 3 29 ABXA9600392 1 19960118 A 5311 9919615501 FRAME DOUG DC9 DC931 3022065 WP FS 658 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE LEFT FUSELAGE FRAME AT FS 658 HAD A PREVIOUS REPAIR THAT WAS CRAC KED THROUGH THE STOP DRILL. REPAIRED LEFT FUSELAGE FRAME FS 658 IAW ABX REA D953-13924-MR. 2 L 7 2 4F A6WE 1996032900416 19960329 00416 WP 1996 3 29 ABXA9600393 1 19960115 A 5512 5922576503 SKIN DOUG DC9 DC931 3022065 WP HORIZ STAB CHAFED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE HORIZONTAL STABILIZER RIGHT AND LEFT UPPER SKIN PANELS CHAFED AND BLENDED BEYOND THE DC-9 SRM LIMITS. REPAIRED HORIZONTAL STABILIZER LEFT AND RIGHT UPPER SKIN PANELS IAW ABX REA D955-1 4035-MR. 2 L 7 2 4F A6WE 1996032900417 19960329 00417 WP 1996 3 29 ABXA9600394 1 19960115 A 5512 5922576504 SKIN DOUG DC9 DC931 3022065 WP HORIZ STAB CHAFED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE HORIZONTAL STABILIZER RIGHT AND LEFT UPPER SKIN PANELS CHAFED AND BLENDED BEYOND THE DC-9 SRM LIMITS. REPAIRED HORIZONTAL STABILIZER LEFT AND RIGHT UPPER SKIN PANELS IAW ABX REA D955-1 4035-MR. 2 L 7 2 4F A6WE 1996032900418 19960329 00418 WP 1996 3 29 ABXA9600395 1 19960120 A 5315 99581883 FLOOR BEAM DOUG DC9 DC931 3022065 WP FS 980 CHAFED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE FLOOR BEAM AT FS 980 HAD UPPER FLANGE CHAFE DAMAGE AT BL 40.0 AND 50.0. REPAIRED FLOOR BEAM AT FS 980 IAW ABX REA D953-14061-MR. 2 L 7 2 4F A6WE 1996032900419 19960329 00419 WP 1996 3 29 ABXA9600396 1 19960112 A 5320 59147923 SERVICE PANEL DOUG DC9 DC931 3022065 WP FS 965-980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE AFT LAVATORY SERVICE PANEL DAMAGED BETWEEN FS 965 AND FS 980 AT L ONGERON 19L. REPAIRED LEFT AFT FUSELAGE SKIN PANEL IAW ABX REA D953-14063-MR. 2 L 7 2 4F A6WE 1996032900420 19960329 00420 WP 1996 3 29 ABXA9600397 1 19960126 A 5312 5910163185 WEB DOUG DC9 DC931 3022065 WP FS 996 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND A PREVIOUS REPAIR ON THE AFT PRESSURE BULKHEAD LOWER WEB THAT WAS COR RODED AND HAD DRILL STARTS. REPAIRED AFT PRESSURE BULKHEAD WEB IAW ABX REA D953-14176-MR. 2 L 7 2 4F A6WE 1996032900421 19960329 00421 WP 1996 3 29 ABXA9600398 1 19960124 A 5330 592032339 SKIN DOUG DC9 DC931 3022065 WP FS 351-364 DENTED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND TWO DENTS IN THE RIGHT FORWARD FUSELAGE SKIN BETWEEN FS 351 AND 364 A ND LONGERONS 24 AND 25R. REPAIRED FORWARD FUSELAGE SKIN IAW ABX REA D953-14200-MR. 2 L 7 2 4F A6WE 1996032900422 19960329 00422 WP 1996 3 29 ABXA9600399 1 19960125 A 5315 9911546137 FLOOR BEAM WEB DOUG DC9 DC931 3022065 WP FS 996 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND A FLOOR BEAM WEB CORRODED AT FS 996. REPAIRED FLOOR BEAM WEB AT FS 9 96 IAW ABX REA D953-14201-MR. 2 L 7 2 4F A6WE 1996032900423 19960329 00423 WP 1996 3 29 ABXA9600400 1 19960206 A 5210 591412155 DOOR PAN DOUG DC9 DC931 3022065 WP FS 160 BINDING A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND WHILE REPLACING THE LEFT FORWARD ENTRY DOOR, THE NEW DOOR REQUIRED EX CESSIVE TRIM OUT AROUND THE UPPER POCKET OF THE LOWER HINGE CAVITY. REPAIRED LEFT FORWARD ENTRY DOOR IAW REA D952-14205 -MR. 2 L 7 2 4F A6WE 1996032900424 19960329 00424 WP 1996 3 29 ABXA9600401 1 19960131 A 5330 59123751 SKIN DOUG DC9 DC931 3022065 WP FS 168 DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, AND EXISTING REPAIR ON THE SERVICE DOOR FORWARD JAMB UPPER CORNER INTERFERE D WITH THE ACCOMPLISHMENT OF SID INSPECTION PSE 53-09-033A, IAW AD 94-03-1. VERIFIED REPAIR AND PLACED ON CARRYOVER FOR DACO TO PERFORM DTA TO FULFILL SID REQUIREMENTS IAW ABX REA D953-14239-MR. 2 L 7 2 4F A6WE 1996032900425 19960329 00425 WP 1996 3 29 ABXA9600402 1 19960205 A 5315 9911546135 FLOOR BEAM DOUG DC9 DC931 3022065 WP FS 996 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE FLOOR BEAM WEB AT FS 996 AND BL 0 CRACKED AND CORRODED. REPAIRED FLOOR BEAM WEB AT FS 996 IAW ABX REA D953-14261-MR. 2 L 7 2 4F A6WE 1996032900426 19960329 00426 WP 1996 3 29 ABXA9600403 1 19960213 A 5321 995791917 FLOOR PANEL DOUG DC9 DC931 3022065 WP FS 237-313 DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND A FLOOR PANEL DAMAGED FROM FS 237 TO 313. REPAIRED FLOOR PANEL IAW A BX REA D953-14339-MR. 2 L 7 2 4F A6WE 1996032900427 19960329 00427 WP 1996 3 29 ABXA9600404 1 19960214 A 5320 991150073 PRESSURE PANEL DOUG DC9 DC931 3022065 WP FS 37 DEFECTIVE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE PRESSURE PANEL AT FS 37 HAD A ONE INCH DIAMETER HOLE ON THE RIGHT SIDE BELOW THE RADOME HINGE POINT. REPAIRED PRESSURE PANEL AT FS 37 IAW ABX REA D953-14357-MR. 2 L 7 2 4F A6WE 1996032900430 19960329 00430 WP 1996 3 29 ABXA9600407 1 19960116 A 5311 99196181 FRAME DOUG DC9 DC931 3022065 WP FS 718 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 78-07-05; SB 53-131, VISUAL INSPECTION OF LEFT AND R IGHT FUSELAGE FRAMES, FOUND THE LEFT FRAME CRACKED AT FS 718. REPLACED FRAME AT FS 718 IAW SB 53-131 AND DC-9 SRM CHAPT ERS 51-30-1, 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1996032900431 19960329 00431 WP 1996 3 29 ABXA9600408 1 19960116 A 5311 9919619503 FRAME DOUG DC9 DC931 3022065 WP FS 737 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 78-07-05; SB 53-131 VISUAL INSPECTION OF LEFT AND RI GHT FUSELAGE FRAMES, FOUND THE FRAME AT FS 737L CRACKED IN TWO PLACES. REPLACED FRAME AT FS 737 IAW SB 53-131 AND DC-9 SRM CHAPTERS 51-30-1, 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1996032900433 19960329 00433 WP 1996 3 29 ABXA9600410 1 19960110 A 5412 99122438 WEB DOUG DC9 DC931 3022065 WP FS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE PYLON BULKHEAD AT FS 965 CRACKED JUST ABOVE THE FLOOR LINE AT LBL 50. REPLACED PYLON BULKHEAD WEB IAW DC-9 SRM CHAPTERS 51-30-1, 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1996032900434 19960329 00434 WP 1996 3 29 ABXA9600411 1 19960110 A 5312 9912243107 WEB DOUG DC9 DC931 3022065 WP FS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE PYLON BULKHEAD AT FS 965 CRACKED JUST ABOVE THE FLOOR LINE AT RBL 50. REPLACED PYLON BULKHEAD WEB IAW DC-9 SRM CHAPTERS 51-30-1, 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1996032900442 19960329 00442 WP 1996 3 29 ABXA9600419 1 19960126 A 5730 591216137 TE PANEL DOUG DC9 DC931 3022065 WP WS 91 DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE LEFT WING TRAILING EDGE PANEL AT XRS 91.0 DELAMINATED AND RIVETS SHEARED. REPLACED LEFT WING TRAILING EDGE PANEL IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 1996032900443 19960329 00443 WP 1996 3 29 ABXA9600420 1 19960116 A 5730 59127371 TE PANEL DOUG DC9 DC931 3022065 WP WS 477-531 DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE LEFT WING TRAILING EDGE PANEL BETWEEN STATION XRS 445.0 AND XRS 5 09 CORRODED AND DELAMINATED. REPLACED TRAILING EDGE PANEL IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 1996032900444 19960329 00444 WP 1996 3 29 ABXA9600421 1 19960325 A 2510 CARPET NIHON YS11 YS11A500 6310416 WP LT SEAT TRACK OUT OF POSITION A ABXA K NONE O OTHER TO TAKEOFF 1 GL 23 910AX 2050 CAPTAINS SEAT WILL NOT STAY LOCKED IN RAIL, SEAT SLIDES BACK ON TAKEOFF. REMOVED CARPET FROM BETWEEN CAPTAINS RAILS. C ARPET WAS STUCK IN RIGHT SEAT RAIL. SEAT OPS CHECKED NORMAL. 2 L 7 2 4T A1PC 1996032900445 19960329 00445 WP 1996 3 29 ABXA9600422 1 19960221 A 5280 3923159505 LINK DOUG DC9 DC931 3022065 WP RT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND THE RIGHT MAIN LANDING GEAR OUTBOARD DOOR LINK HAD EXCESSIVE PLAY. R EPLACED LINK IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1996032900446 19960329 00446 SO 1996 3 29 COMA9610115 1 19960327 A 3260 922FS2A6N2735 PROX SENSOR EMB 120 EMB120RT SO RT MLG DEFECTIVE A COMA K NONE O OTHER LD LANDING 1 SO 01 265CA 120257 NOSE WHEEL STEERING FAILED DURING LANDING. REPLACED THE RT MLG WEIGHT ON WHEELS PROXIMITY SENSOR. 2 L 7 2 4T RT A31SO 1996032900447 19960329 00447 EA 1996 3 29 COMA9660054 1 19960327 A 5610 NP1393211 WINDSHIELD CNDAIR CL600 CL6002B19 EA LT COCKPIT DELAMINATION A COMA K NONE O OTHER CR CRUISE 1 SO 01 931CA 7037 PILOTS WINDSHIELD IS DELAMINATING. REPLACED WINDSHIELD. 2 L 7 2 4F RT A21EA 1996032900448 19960329 00448 EA 1996 3 29 COMA9660055 1 19960326 A 2750 860D10018 FECU CNDAIR CL600 CL6002B19 EA TE FLAPS FAILED A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 943CA 7062 FLAPS FAILED WHEN SELECTED TO TAKEOFF RANGE. REPLACED THE FLAP ELECTRONIC CONTROL UNIT. 2 L 7 2 4F RT A21EA 1996032900449 19960329 00449 NM 1996 3 29 DL72E960662 1 19960315 A 5754 651622374 RIB BOEING 727 727247 138408F NM NR 7 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 830WA 21482 DURING SHOP INSPECTION, THE SECOND AND SIXTH RIBS FROM THE OUTBOARD END OF NR 7 SLAT WERE FOUND TO BE CRACKED. THE DAMA GE WAS REPAIRED PER 727 M/M 57-54-0. 2 L 7 3 4F A3WE 1996032900450 19960329 00450 NM 1996 3 29 DL72E960677 1 19960315 A 5754 651622374 RIB BOEING 727 727247 138408F NM NR 7 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 830WA 21482 DURING SHOP INSPECTION, THE NINTH AND SIXTEENTH RIBS FROM THE OUTBOARD END OF NR 7 SLAT WERE FOUND TO BE CRACKED. THE D AMAGE WAS REPAIRED PER 727 M/M 57-54-0. 2 L 7 3 4F A3WE 1996032900451 19960329 00451 NM 1996 3 29 DL72L960653 1 19960318 A 5330 651842012 SKIN BOEING 727 727232 1384082 NM BS 340-400 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 503DA 21305 LAX REPORTED DAMAGE TO THE SKIN, STRINGERS AND FRAMES BETWEEN STA 340 TO STA 400 AND STR 22R TO S-24R. SEVERAL REPAIRS HAVE BEEN INSTALLED PER THE B727 SRM. DUE TO LIMITED ACCESS BLIND FASTENERS WILL BE INSTALLED IN SEVERAL LOCATIONS ON A TIME LIMITED BASIS, REPAIR APPROVAL PER DL ERA 303310-14. 2 L 7 3 4F A3WE 1996032900452 19960329 00452 NE 1996 3 29 DL72L960681 2 19960315 A 7314 37820113 PUMP BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE FAILED A DALA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SO 27 513DA 21315 NUMBER 2 ENGINE FLAMED OUT AT FL 310 NO INDICATIONS OF STALLS OR OTHER ENGINE DAMAGE. REPLACED FUEL PUMP AND FUEL CONTR OL, OPERATION NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1996032900453 19960329 00453 NM 1996 3 29 DL72S960655 1 19960325 A 5320 TORQUE BOX WEB BOEING 727 727232 1384082 NM BS 1223 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 534DA 22047 FOUND DURING B-2 LETTER CHECK, LWR LT TORQUE BOX CRACKED AT LIGHTNING HOLE AFT OF STA 1223 ADJACENT TO PREVIOUS REPAIR S. LOWER TORQUE BOX LIGHTNING HOLE ROUTED BEYOND LIP RT SIDE STA 1243 BOTH ITEMS REPAIRED PER M/M 53-11-0. 2 L 7 3 4F A3WE 1996032900454 19960329 00454 NM 1996 3 29 DL72S960656 1 19960325 A 5530 STRINGER BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 534DA 22047 FOUND DURING B-2 LETTER CHECK, STRINGER CRACKED IN TAIL CRAWLWAY BETWEEN 2ND AND 3RD BAY RT SIDE. REPAIRED PER M/M 5 5-30-0. 2 L 7 3 4F A3WE 1996032900455 19960329 00455 NM 1996 3 29 DL72S960657 1 19960325 A 5530 STRINGER BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 534DA 22047 FOUND DURING B-2 LETTER CHECK, STRINGER CRACKED RT SIDE TAIL CRAWLWAY ONE AND ONE HALF BAYS DOWN. REPAIRED PER M/M 5 5-30-0. 2 L 7 3 4F A3WE 1996032900456 19960329 00456 NM 1996 3 29 DL72S960659 1 19960326 A 2613 OVERHEAT SENSOR BOEING 727 727232 1384082 NM AFT FUSELAGE OUT OF POSITION A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 532DA 22045 LOWER AFT BODY OVERHEAT LIGHT ILLUM. C/W PROM LIGHT WENT OUT WHEN LT PACK AND BLEED TURNED OFF. REPOS OVERHEAT SENSOR IN 48 SECTION. RAN ENGINE WITH NO OVERHEAT IND. 2 L 7 3 4F A3WE 1996032900457 19960329 00457 NM 1996 3 29 DL72S960660 1 19960326 A 3350 17AT6 SWITCH BOEING 727 727232 1384082 NM COCKPIT FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 401DA 21145 ON INSPECTION, FOUND LT SIDE OF AIRCRAFT EMERGENCY EXIT SIGN ILLUMINATION LIGHTS INOP. REPLACED NO SMOKING SW ON PILOTS O/H PNL. 2 L 7 3 4F A3WE 1996032900458 19960329 00458 NM 1996 3 29 DL72S960665 1 19960326 A 5210 STOP LUGS BOEING 727 727225 1384077 NM FWD ENTRY DR BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 WHILE CHECKING FWD ENTRY DOOR SEAL DUE TO PRESS WRITEUP, FOUND STOP ROD ATTACH LUGS ON UPPER AND LOWER HINGED GATES BROK EN. REPAIRED PER M/M 52-11-01 PG 807. 2 L 7 3 4F A3WE 1996032900459 19960329 00459 NM 1996 3 29 DL72S960666 1 19960312 A 5712 RIB BOEING 727 727232 1384082 NM LT/RT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 546DA 22677 MTC DISCOVERED CRACKS IN THE LT AND RT WING RIB CHORD DURING MV-2 IN ATL. THE CRACK WAS REMOVED BY OVERSIZING THE HOLES TO .628 INCH IN THE LT RIB CHORD. IN THE RT RIB CHORD THE CRACK WAS REMOVED BY OVERSIZING THE UPPER HOLE TO .6435 INCH AND THE LOWER HOLE TO .629 INCH, .25 INCH MATERIAL REMAINS BETWEEN THE TWO HOLES. ACCOMPLISHED REPAIRS PER DL ERA 3032 99-14. 2 L 7 3 4F A3WE 1996032900460 19960329 00460 NM 1996 3 29 DL72S960668 1 19960313 A 5330 SKIN BOEING 727 727232 1384082 NM BS 480-500 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 546DA 22677 THE SKIN BETWEEN STA 480 TO 500 AND STR 27R TO 28R WAS FOUND CORRODED. THE DAMAGED SECTION WAS TRIMMED OUT LEAVING A C UTOUT DIMENSION OF 19.5 INCH BY 8.5 INCH. ER/A WILL INSTALL AN EXTERNAL DOUBLER AND TRIPLER FOR THE DAMAGE. REV A DETAI LS ADDITIONAL CORROSION FOUND. THE NEW DAMAGE IS LOCATED AT STA 500 AND 520. THE ER/A WILL INSTALL AN INTERNAL DOUBLER AT BOTH NEW DAMAGE LOCATIONS ON A TIME-LIMITED BASIS REF DL ERA 303302-14. 2 L 7 3 4F A3WE 1996032900461 19960329 00461 NM 1996 3 29 DL72W960647 1 19960324 A 3350 TRACK LIGHT BOEING 727 727247 138408F NM CABIN INOPERATIVE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 291WA 22109 THREE EMERGENCY EXIT TRACK LIGHTS INOP AT AFT GALLEY DOOR. REPAIRED TRACK LIGHTS, OPS NORMAL. 2 L 7 3 4F A3WE 1996032900462 19960329 00462 NM 1996 3 29 DL72W960654 1 19960104 A 5240 65569923 FRAME BOEING 727 727247 138408F NM L2 SERVICE DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 290WA 22108 DURING INSPECTION, FOUND L2 SERVICE DOOR WITH CRACKED FRAME AT UPPER FORWARD LATCH CUTOUT. ACCOMPLISHED REPAIRS PER SRM 52-40-02. 2 L 7 3 4F A3WE 1996032900463 19960329 00463 NM 1996 3 29 DL73S960651 1 19960314 A 5312 BLKHD WEB BOEING 737 737232 1384475 NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 330DL 23102 THE BS 178 BULKHEAD WEB WAS FOUND CRACKED BENEATH THE VERTICAL STIFFENERS AT LBL 5.7 AND RBL 5.7. DAMAGE REMOVAL RESULT ED IN A 1.45 INCH LEFT AND RIGHT BY 1.2 INCH UP AND DOWN CUTOUT ON THE LT SIDE AND A 1.5 INCH LEFT AND RIGHT BY 5.1 INCH UP AND DOWN CUTOUT ON THE RT SIDE. DAMAGE WAS FOUND ON LAYOVER IN ATL. ACCOMPLISHED REPAIRS PER SRM 53-10-11, REF DL ERA 303315-14. 2 L 7 2 4F RT A16WE 1996032900464 19960329 00464 NM 1996 3 29 DL73S960652 1 19960320 A 5330 6545769545 SKIN BOEING 737 737232 1384475 NM BS 379 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 301DL 23073 THE SKIN AT THE COOLING DUCT CUTOUT, BS 379 BL 0 WAS FOUND CRACKED AT THE AFT EDGE OF THE CUTOUT. THE CRACK IS APPROX 1 .5 INCH IN LENGTH AND IS TYPICAL OF CRACKS DESCRIBED IN BACO SB 737-53-1117 R1. CRACK FOUND AT MID VISIT IN ATL. THE C RACK WILL BE STOP DRILLED AND A PERMANENT REPAIR WILL BE INSTALLED PER THE BACO SERVICE BULLETIN REF DL ERA 303327-14. 2 L 7 2 4F RT A16WE 1996032900465 19960329 00465 NM 1996 3 29 DL73S960684 1 19960315 A 3350 BC50393105 LIGHT COVER BOEING 737 737232 1384475 NM CABIN MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 303DL 23075 ON INSPECTION, FOUND OVERWING EMERGENCY EXIT SIGN AT ROW 15A MISSING. REPLACED LENS AND REBULBED, OPERATION NORMAL. 2 L 7 2 4F RT A16WE 1996032900466 19960329 00466 NM 1996 3 29 DL757960663 1 19960326 A 2530 OVEN BOEING 757 757232 1384965 NM MID GALLEY FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 643DL 23997 HOT ELECTRICAL SMELL IN MID GALLEY, SEEMS TO BE COMING FROM AFT FACING OVENS. PULLED C/BS NO SUBSEQUENT PROBLEMS. REPL ACED MID GALLEY AFT FACING DOUBLE OVEN OPS OK. ALSO, INSPECTED ELECTRICAL CABLES TO OVEN, ALL OK. 2 L 7 2 4F RT A2NM 1996032900467 19960329 00467 NM 1996 3 29 DL757960670 1 19960326 A 3350 TRACK LIGHT BOEING 757 757232 1384965 NM CABIN MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 608DA 22815 DURING INSPECTION, CABIN EMERGENCY EXIT TRACK LIGHTS INOP AT ROW 6B. REPLACED MISSING TRACK LIGHT ASSEMBLY, OPERATION N ORMAL. 2 L 7 2 4F RT A2NM 1996032900468 19960329 00468 NM 1996 3 29 DL757960672 1 19960324 A 2560 SLIDE BOTTLE BOEING 757 757232 1384965 NM LT SIDE EMPTY A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 633DL 23614 DURING S/C FOUND LEFT OVERWING SLIDE WOULD NOT TEST. FOUND LEFT BOTTLE EMPTY. REPLACED SAME PER MM 25-65-02, SYS TEST OK. 2 L 7 2 4F RT A2NM 1996032900469 19960329 00469 WP 1996 3 29 DLL10960685 1 19960319 A 2720 CONTROL CABLE LKHEED 1011 10113851 5265010 WP LT RUDDER PEDAL MISROUTED A DALA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 27 714DA 193C1090 ON TAXIOUT, DURING FLT CONTROL CHECK, RUDDER JAMMED WOULD NOT CYCLE TO LEFT. FLIGHT RETURNED TO BLOCK. FOUND PEDAL ADJ USTMENT CONTROL CABLE HOOKED ON RIGHT PEDAL. REROUTED CABLE AND CLAMPED FOR SECURITY, OPERATION NORMAL. 2 L 7 3 4F A23WE 1996032900470 19960329 00470 WP 1996 3 29 MWEA96067 1 19960325 A 2150 PACK DOUG DC9 DC932 3022066 WP TAIL SECTION ICED UP A MWEA A G UNSCHED LANDING O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 GL 31 302ME 47102 PILOT REPORTS, THE CABIN ALTITUDE ROSE WHEN PACK SHUTDOWN. ALL O2 MASKS DEPLOYED, DIVERTED TO ATLANTA. MTC IN ATL STOW ED ALL MASKS. CHECKED FOR BLOWN DUCTS AND RAN PACKS, OPS CHECKED GOOD. SUSPECT ICING IN FLIGHT CAUSED PACK SHUTDOWN. 2 L 7 2 4F A6WE 1996032900471 19960329 00471 NM 1996 3 29 MWEA96068 1 19960328 A 3350 BATTERY DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 701ME 49760 DURING SERVICE CHECK FOUND EMERGENCY FLOOR TRACK LIGHTING IN AFT ACCESSORY COMPT DIM. REPLACED D-CELL NICAD BATTERIES I N AFT OVERHEAD BIN, OPS CHECK GOOD. 2 L 7 2 4F RT A6WE 1996032900472 19960329 00472 EU 1996 3 29 QXEA9600134 1 19960327 A 3350 1312 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 452US 11105 SERVICE/EMERGENCY DOOR EXIT LIGHT IS INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996032900473 19960329 00473 NM 1996 3 29 UPS96205784 1 19960319 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 277 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CRACKED SHEAR TIE AT STA 277 STR 16 RT. REPAIRED SHEAR TIE IAW SRM 51-30-00 , 51-40-2, 51-30-2 AND MM 51-20-151. 2 L 7 3 4F A3WE 1996032900474 19960329 00474 NM 1996 3 29 UPS96205785 1 19960320 A 5230 65186251 L ANGLE BOEING 727 72727C 138400J NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED AFT CARGO DOOR NR 3 O/B TRANSVERSE BEAM L-ANGLE CRACKED IN RADIUS AT NR 1 OU TER SKIN VERTICAL STIFFENER. REMOVED AND REPLACED DOOR L-ANGLE IAW SRM 51-10-1, 51-30-2, 51-40-2, 51-20-21, 51-30-1 AND MM 51-20-151 AND 51-20-21. 2 L 7 3 4F A3WE 1996032900475 19960329 00475 NM 1996 3 29 UPS96205786 1 19960321 A 5230 65186251 L-ANGLE BOEING 727 72727C 138400J NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED AFT CARGO DOOR NR 2 O/B TRANSVERSE BEAM L-ANGLE CRACKED IN RADIUS AT NR 2 OU TER SKIN VERTICAL STIFFENER. REMOVED AND REPLACED DOOR L-ANGLE IAW SRM 51-10-1, 51-30-2, 51-30-2, 51-30-5, 51-30-1 AND MM 51-20-151 AND 51-20-21. 2 L 7 3 4F A3WE 1996032900476 19960329 00476 NM 1996 3 29 UPS96205787 1 19960320 A 5320 ANGLE BOEING 727 72727C 138400J NM BS 305 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON SUPPORT ANGLE STA 305 RT STR 20. REMOVED AND REPLACED ANGLE IA W SRM 51-20-1, 51-30-2, 51-10-2, 51-20-4 AND MM 51-20-151. 2 L 7 3 4F A3WE 1996032900477 19960329 00477 NM 1996 3 29 UPS96205788 1 19960319 A 5320 ANGLE BOEING 727 72727C 138400J NM BS 304 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON L-ANGLE AT STA 304 RBL 33 TO 57 WL 208. REMOVED CORROSION REWO RK OUT OF LIMITS IAW SRM 53-10-1, REPAIRED ANGLE IAW SRM 51-20-1 AND 51-20-4. 2 L 7 3 4F A3WE 1996032900478 19960329 00478 NM 1996 3 29 UPS96205789 1 19960317 A 5315 BAC150529222 FLOOR BEAM BOEING 727 72727C 138400J NM STA 344 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON TOP OF FLOOR BEAM AT STA 344 WL 208 LBL 65 TO RBL 65. REMOVED CORROSION FROM FLOOR BEAM FOUND TO BE OUT OF LIMITS IAW 53-10-1, REPAIRED FLOOR BEAM IAW SRM 53-10-8, 51-30-2 AND MM 51- 30-00 AND 51-20-151. 2 L 7 3 4F A3WE 1996032900479 19960329 00479 NM 1996 3 29 UPS96205790 1 19960317 A 5320 69144723 STRINGER TIE BOEING 727 72727C 138400J NM BS 950 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED STR 7 LEFT TIE AT STA 950 CRACKED. REMOVED AND REPLACED STA IAW SRM 53-10-1 , 51-30-6, 51-30-5, AND 51-30-2. 2 L 7 3 4F A3WE 1996032900480 19960329 00480 NM 1996 3 29 UPS96205791 1 19960320 A 5313 BAC149895 STRINGER BOEING 727 72727C 138400J NM BS 356 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON STRINGERS 4 AND 5 RT AT BS 356. CORROSION REMOVAL ON STR 4R WI THIN LIMITS, CORROSION REMOVAL ON STR 5R OUT OF LIMITS. REMOVED DAMAGED SECTION OF STR BETWEEN BS 338 AND 356, FABRICAT ED REPAIR PARTS AND INSTALLED PER SRM 53-10-3. 2 L 7 3 4F A3WE 1996032900481 19960329 00481 NM 1996 3 29 UPS96205792 1 19960321 A 5754 65217492 BEARING BOEING 727 72727C 138400J NM NR 6 TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED NR 6 K-FLAP BULLNOSE I/B BEARING HAS CORROSION ON O/B SIDE. REPLACED K-FLAP NR 6 IAW MM 27-81-01. 2 L 7 3 4F A3WE 1996032900482 19960329 00482 EU 1996 3 29 WWMA9600031 1 19960315 A 3244 AHA1737 TIRE BAG JETSTM JETSTM3201 1500217 EU RT MLG DEFLATED A WWMA K NONE O OTHER LD LANDING 1 WP 15 957AE 957 RIGHT MAIN TIRE DEFLATED ON TOUCHDOWN ROLL. MAINTENANCE REPLACED THE RIGHT MAIN WHEEL ASSEMBLY AND PERFORMED A TIRE BUR ST/SHEDDING INSPECTION. NO DAMAGE WAS FOUND AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT A56EU 1996032900492 19960329 00492 WP 1996 3 29 96ZZZM370 1 19960213 A 5711 5911300502 SPAR CAP DOUG DC9 DC933F 302207A WP WS 137 CORROSION A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 944F 46705 47194 DURING C-CHECK INSPECTION DISCOVERED EXFOLIATION CORROSION IN THE REAR SPAR CAP UPPER AFT FLANGES, SLIGHTLY INBOARD OF T HE REAR STATION XRS 137 ON BOTH THE LEFT AND RIGHT WINGS. REPAIRED BY BLENDING OUT THE CORROSION, ALODNING, PRIMING AND FINISHED THE BLEND AREAS PER SRM CH 51 TO PROTECT AGAINST FURTHER CORROSION. INSTALLED FASTENERS USING TAPERED WASHERS AND SELF ALIGNING NUTS. ACCOMPLISHED IAW EVERGREENS ECRA NR 944-57-021-2 DATED 1-8-96. (M) 2 L 7 2 4F A6WE 1996032900493 19960329 00493 WP 1996 3 29 96ZZZM371 1 19960220 A 3260 70110047 PROX LOGIC BOX LKHEED 1011 10113851 5265010 WP NLG MALFUNCTIONED A WRNA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 05 311EA 9513 193A1012 NOSE GEAR OR DOOR LIGHT AND RED INTRANSIT LIGHT CAME ON DURING CLIMB, RETURNED TO AIRPORT. LANDING WAS NORMAL. ADJUSTE D NOSE GEAR UPLOCK SENSOR IAW 32-61-04. REMOVED AND REPLACED PROX LOGIC BOX IAW 31-22-01. INSTALLED PROX LOGIC CARD IA W 31-22-02, CARRIED OUT NOSE GEAR RETRACTION. SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A23WE 1996032900494 19960329 00494 NE 1996 3 29 96ZZZM372 2 19960201 A 7230 39216041 RELIEF VALVE DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3B 52039 NE NR 2 ENG MALFUNCTIONED A C1HA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 WP 23 802MG 46098 645997 AT 70 KNOTS NR 2 ENGINE COMPRESSOR STALLED. ABORTED TAKEOFF. REMOVED AND REPLACED NR 2 ENG REGULATOR AND RELIEF VALVE. OPS CHECK GOOD ON HIGH SPEED TAXI. (M) 2 L 7 4 4F 4 F 4A25 1E8 1996032900498 19960329 00498 NM 1996 3 29 96ZZZM376 1 19960107 A 3260 BULB BOEING 727 727227 1384078 NM LT MLG FAILED A AMTA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 GL 11 779AT 22091 ON GEAR RETRACTION RED UNSAFE LIGHT FOR LEFT MLG DID NOT ILLUMINATE. PUT GEAR HANDLE TO OFF RT MLG DOOR LIGHT ILLUMINAT ED. CYCLED GEAR TWICE WITH NO HELP. FOUND C/P LOOSE ON RT MLG DOOR POSITION SWITCH. FOUND BAD BULB LEFT MLG UNSAFE LI GHT INDICATION. TIGHTENED C/P AND RELAMPED. 2 L 7 3 4F A3WE 1996032900499 19960329 00499 NM 1996 3 29 96ZZZM377 1 19960128 A 3350 3315048 BATTERY BOEING 727 727264 138408M NM CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 763AT 014642 22983 RIGHT OVERWING HATCH EXIT SIGNS ARE INOP. REMOVED AND REPLACED BATTERY PACK, CHECKS OK. 2 L 7 3 4F A3WE 1996032900500 19960329 00500 WP 1996 3 29 96ZZZM378 1 19960204 A 5312 BLKHD STRINGERS LKHEED 1011 10113851 5265010 WP AFT PRESS BLKHD CRACKED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 191AT 193C1084 INSPECTED AFT PRESSURE BULKHEAD STRINGER ATTACH FITTINGS (VISUAL INSPECTION ONLY) PER EO L10-53AD-1573C. FOUND TWO STRI NGERS CRACKED A/C MAINTENANCE FERRIED TO KIND FOR REPAIRS. 2 L 7 3 4F A23WE 1996032900501 19960329 00501 WP 1996 3 29 96ZZZM379 1 19960131 A 2150 PACK LKHEED 1011 10113851 5265010 WP NR 2 PACK SMOKING A AMTA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 11 183AT 193A1153 DURING CLIMB HAD SMOKE IN CABIN AND COCKPIT, PERFORMED AIR CONDITION SMOKE EMERGENCY CHECK LIST. ISOLATED NR 2 PACK AND NO MORE EVIDENCE OF SMOKE. OPERATED NR 2 PACK OFF NR 2 ENGINE BLEED DURING MAINTENANCE GROUND RUN. NO ODOR, NO SMOKE, OK FOR SERVICE. 2 L 7 3 4F A23WE 1996032900502 19960329 00502 WP 1996 3 29 96ZZZM380 1 19960102 A 3260 3251022 CONTL MODULE LKHEED 1011 10113851 5265010 WP LANDING GEAR FAILED A AMTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 197AT 000332 193P1082 UPON GEAR RETRACTION WITH GEAR HANDLE UP, GEAR WOULD NOT RETRACT. SHOWED RED INTRANSIT LIGHT AND ALL THREE GREEN LIGHTS . REPLACED LANDING GEAR CONTROL MODULE. 2 L 7 3 4F A23WE 1996032900611 19960329 00611 NM 1996 3 29 96ZZZM489 1 19960203 A 5712 RIB BOEING 727 727228 NM WS 656 MIS REPAIRED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 724DH 46483 19862 DURING C-CHECK, FOUND WING RIB STATION 656 HAS PREVIOUS REPAIR WITH CUTOUT EXCEEDING 3 INCH LIMIT ON SRM 57-10-5 FIG 2. REMOVED AND REPLACED WING RIB AT STATION 656 PER SB 727-57-0127. 2 L 7 3 4F A3WE 1996032900612 19960329 00612 NM 1996 3 29 96ZZZM490 1 19960203 A 5712 RIB BOEING 727 727228 NM WS 686 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 DURING C-CHECK, FOUND LEFT WING, LOWER FLANGE OF WING RIB AT WS 686 CRACKED AT STRINGER 6 AND STRINGER 8. MARKED PENETR ANT INSPECTION PER OHM 20-20-2 PER SB 727-57-0127. STOP DRILLED EACH END OF CRACKS AS PER SRM 51-10-1. INSTALLED WING RIB REPAIR AS PER SRM 57-10-5 7075-T6 .090 LOT NR 93110848 10 INCH BY 4 INCH AT LW LOWER FLANGE WING BS AT WS 686 AT STR INGER 6. INSTALLED WING IN SPAR RIB REPAIR AS PER SRM 57-10-5 7075-T6 .090 LOT NR 93110848 10 INCH BY 4 INCH AT LW LOWE R FLANGE WING RIB AT WS 686 AT STRINGER 8. 2 L 7 3 4F A3WE 1996032900613 19960329 00613 NM 1996 3 29 96ZZZM491 1 19960203 A 5414 'S' DUCT SKIN BOEING 727 727228 NM NR 2 ENGINE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 46482 19862 DURING C-CHECK, FOUND NR 2 ENGINES 'S' DUCT INNER SKIN BULGED RIVET PULLED THROUGH 8 INCHES AFT OF SECOND ROW OF VORTEX GEN'S 6 O'CLOCK POSITION. CUT OUT DAMAGED AREA SKIN PER SRM 54-10-3 FIG 10. INSTALLED DOUBLER REPAIR PER SRM 54-10-3 F IG 10 IN NR 2 ENGINE. 'S' DUCT INNER SKIN LOT NR 472051, PO NR 93110300, SIZE 8 INCH BY 8 INCH. 2 L 7 3 4F A3WE 1996032900614 19960329 00614 NM 1996 3 29 96ZZZM492 1 19960203 A 5414 'S' DUCT SKIN BOEING 727 727228 NM NR 2 ENG CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 46482 19862 DURING C-CHECK, FOUND NR 2 ENGINE 'S' DUCT INNER SKIN BULGED RIVET PULLED THROUGH 50 INCHES AFT OF SECOND ROW OF VORTEX GEN'S 6 O'CLOCK POSITION. CUT DAMAGED AREA 2 INCH BY 2 INCH PER SRM 54-10-3. INSTALLED CENTER ENGINE INTAKE DUCT SKIN DOUBLE REPAIR PER SRM 54-10-3 FIG 10 SHEET 3 12 INCH BY 5 INCH .050 7075-T6 LOT NR 179521 PO NR 93110717. 2 L 7 3 4F A3WE 1996032900615 19960329 00615 NM 1996 3 29 96ZZZM493 1 19960203 A 5520 FITTINGS BOEING 727 727228 NM RT ELEV CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 DURING C-CHECK, FOUND RIGHT ELEVATOR HINGE SUPPORT FITTINGS ARE CRACKED AT STATION 50.5 AND 66.5 AS SEEN THROUGH ACCESS PANELS ON BOTTOM SIDE OF ELEVATOR AS PER MM CHAP 27-50-5. INSTALLED THE REPLACEMENT ELEVATOR AS PER MM CHAP 27-30-5. I NSTALLED ELEVATOR BALANCE PANEL AS PER 27-30-21. CLOSED RIGHT BALANCE PANELS. OPS CHECK RIGHT ELEVATOR PER MM 27-30-00 . 2 L 7 3 4F A3WE 1996032900616 19960329 00616 NM 1996 3 29 96ZZZM494 1 19960203 A 5311 FRAME BOEING 727 727228 NM BS 870 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 46482 19862 DURING C-CHECK, HFEC HAS INDICATED CRACKS ONE EACH STATION 870 JUST BELOW STRINGER 9R MAIN FRAME SPLICE OUTBOARD FLANGE, CRACKS LOCATED NEXT TO AFT ROW, ROW 3 NEXT TO BOTTOM HOLE (THIRD HOLE FROM TOP) AT ABOUT 11 O'CLOCK POSITION. REAMED H OLE TO NEXT SIZE .0156 AS PER SRM 51-30-2. PARTIAL REPLACEMENT OF TERMINAL FITTING STRINGER 9 TO STRINGER 12 RIGHT SIDE BS 870 AS PER SB 727-53-0194. COMPLIED WITH SB PER ECD 92-727-5311-006. 2 L 7 3 4F A3WE 1996032900617 19960329 00617 NM 1996 3 29 96ZZZM495 1 19960203 A 5311 FRAME BOEING 727 727228 NM BS 870 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 46482 19862 DURING C-CHECK, HFEC HAS INDICATED CRACKS TWO EACH STATION 870 JUST BELOW STRINGER 9 MAIN FRAME SPLICE OUTBOARD FLANGE, CRACKS LOCATED IN AFT ROW NR 4 BOTTOM HOLE IN MAIN FRAME AT 4 AND 5 O'CLOCK POSITION APPROX. REAMED HOLE TO NEXT SIZE . 0156 AS PER SRM 51-30-2. PARTIAL REPLACEMENT OF TERMINAL FITTING STRINGER 9 TO STRINGER 12 RT SIDE BS 870 AS PER SB 727 -53-0194. COMPLIED WITH SB PER FCD 92-727-5311-006. 2 L 7 3 4F A3WE 1996032900618 19960329 00618 NM 1996 3 29 96ZZZM496 1 19960203 A 5230 SKIN BOEING 727 727228 NM EXT CARGO DOOR GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 DURING C-CHECK, FOUND MAIN CARGO DOOR EXTERIOR SKIN GOUGED AND SEPARATING ALSO, SEAL RETAINER TORN AT LOWER FORWARD CORN ER OF MCD. REMOVED AND REPLACED AFT LOWER CORNER AT MAIN CARGO DOOR AS PER SRM 51-10-1 PAGE 4 2024-0 .025 12 INCH BY 3 INCH LOT NR 620352 PO NR 9319067. HEAT TREATING 2024-0 TO T3 PER BAC 5602. REPLACED FWD MCD LOWER CORNER PER SRM 51-10 -1 PAGE 4 12 INCH BY 1 INCH LOT NR 620352 PO NR 9319067 2024-0 .025. 2 L 7 3 4F A3WE 1996032900619 19960329 00619 NM 1996 3 29 96ZZZM497 1 19960203 A 5320 DOOR FRAME BOEING 727 727228 NM NR 2 CARGO DOOR CRACK A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 46482 19862 DURING C-CHECK, HFEC CRACK INDICATION AT NR 2 CARGO DOOR CUT OUT FWD FRAME WEB, JUST INBOARD OF LOWER FRAME DOOR STOP IN LINE WITH STRINGER 26R CRACK AND END OF CRACK. STOP DRILLED CRACK PER 51-10-1. INSTALLED WEB REPAIR PER SB 727-53-199 R1 P 93110229 .080 7075-T6 LOT 670971 12 INCH BY 3.5 INCH AT NR 2 CARGO DOOR CUT OUT FWD LWR CORNER. 2 L 7 3 4F A3WE 1996032900620 19960329 00620 NM 1996 3 29 96ZZZM498 1 19960203 A 5320 HAT CHANNEL BOEING 727 727228 NM LAV THRESHOLD CORROSION A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 DURING C-CHECK, FOUND FORWARD LAVATORY THRESHOLD HAD LIGHT CORROSION AROUND CLIP NUTS ON HAT CHANNEL. REMOVED AND REPLA CED HAT CHANNEL AS PER SRM 51-10-1 P4 AND SRM 51-30-2. P/N 60-357 7075-T6 PO NR 9600125 SIZE OF THE CHANNEL 40 INCH AT FWD LAVATORY AREA LOWER THRESHOLD AREA. 2 L 7 3 4F A3WE 1996032900621 19960329 00621 NM 1996 3 29 96ZZZM499 1 19960203 A 5712 RIB BOEING 727 727228 NM WS 601 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 46482 19862 DURING C-CHECK, FOUND STATION 601 WING RIB LOWER FLANGE HAS CRACKS AT NR 6 AND NR 8 STRINGER LOCATIONS. STOP DRILLED CR ACKS AT NR 6 AND NR 8 STRINGER TO RIB LOCATION, ON RIB LOWER FLANGE STATION 601.5 PER SB 727-57-0127 FIG 2. NO CRACKS P ROGRESSED AFTER STOP DRILLED. FABRICATED DOUBLER REPAIRS TWO EACH 10 INCH BY 4.5 INCH 7075-T6 .090 LOT NR 233-601 PO NR 93110848 AND 12 INCH BY 4.5 INCH 7075-T6 .090 LOT NR 1233-601 PO NR 93110848. INSTALLED DOUBLER REPAIRS AS PER SRM 57- 10-5 FIG 2. 2 L 7 3 4F A3WE 1996032900622 19960329 00622 NM 1996 3 29 96ZZZM500 1 19960203 A 5712 RIB BOEING 727 727228 NM WS 686 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 46482 19862 DURING C-CHECK, FOUND RIGHT WING LOWER FLANGE OF WING RIB CRACKED AT WS 686 AT STRINGER 8 TWO PARALLEL CRACKS AND AT STR INGER 6 AT PREVIOUS REPAIR. PENETRANT INSPECTION PER BOHM 20-20-2 PER SB 727-57-0127. ENDS OF CRACKS MARKED. REMOVED RT WING RIB AT WS 686 AS PER SB 727-57-0127. REPLACED RT WING RIB WS 686 AS PER SB 727-57-0127. 2 L 7 3 4F A3WE 1996032900623 19960329 00623 NM 1996 3 29 96ZZZM501 1 19960203 A 5712 RIB BOEING 727 727228 NM WS 629 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 46483 19862 DURING C-CHECK, FOUND RT WING LOWER FLANGE OF WING RIB CRACKED AT WS 629 AT LOWER STRINGER 8 PER PENETRANT INSPECTION PE R SB 727-57-0127 REV 3 ENDS OF CRACK MARKED. STOP DRILLED CRACK PER SRM 51-10-1 AT WS 629 LOWER STRINGER 8 OF WING RIB. INSTALLED WING INSPAR RIB REPAIR AS PER SRM 57-10-5 7075-T6 .090 LOT NR P13110848 9 INCH BY 3.5 INCH AT RT WING LOWER FLANGE WS 629 STRINGER. 2 L 7 3 4F A3WE 1996032900624 19960329 00624 NM 1996 3 29 96ZZZM502 1 19960203 A 5730 SKIN BOEING 727 727228 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 46482 19862 DURING C-CHECK, FOUND CRACK RIGHT WING UPPER SKIN PANEL JUST FWD OF NR 10 SPOILER. STOP DRILL AT CRACK RT UPPER SKIN PA NEL JUST FWD OF NR 10 SPOILER AS PER SRM 51-10-1. INSTALLED DOUBLER REPAIR AS PER SRM 51-40-2 7075-T6 .032 6 INCH BY 2. 5 INCH LOT 133261 PO 9318067 AT R/W UPPER SKIN PANEL FWD OF NR 10 SPOILER. 2 L 7 3 4F A3WE 1996032900625 19960329 00625 NM 1996 3 29 96ZZZM503 1 19960114 A 5522 SKIN BOEING 727 72723 1384004 NM LT ELEVATOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 19389 DURING C-CHECK, LEFT ELEVATOR LOWER SKIN CRACKED TWO PLACES APPROX STA ELEVATOR 130 JUST AFT OF ACCESS PNL 9312. STOP D RILLED CRACKS AS PER SRM 51-10-1 AT TWO PLACES. INSTALLED REPAIR 9 INCH BY 11.5 INCH 2024-T3 .032 PO NR 93110887 LOT NR 275-611 IAW SRM 55-20-3 AT LEFT ELEV LOWER SKIN STATION 130 JUST AFT OF ACCESS PANEL 9312. 2 L 7 3 4F A3WE 1996032900626 19960329 00626 NM 1996 3 29 96ZZZM504 1 19960114 A 5522 SKIN BOEING 727 72723 1384004 NM LT ELEVATOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 59690 19389 DURING C-CHECK, FOUND LEFT ELEVATOR LOWER SKIN CRACKED APPROX STA ELEV 100 2 INCH FROM TRAILING EDGE. ROUTED OUT CRACK AT LEFT ELEV LOWER SKIN APPROX STATION ELEV 100 2 INCH FROM T/E IAW SRM 55-20-3. INSTALLED REPAIR 3 INCH BY 7.75 INCH O F 2024-T3 .032 PO NR 9311087 LOT NR 275-611 IAW SRM 55-20-3 AT LEFT ELEV LOWER SKIN APPROX ELEV STATION 100 2 INCHES FRO M TRAILING EDGE. 2 L 7 3 4F A3WE 1996032900627 19960329 00627 NM 1996 3 29 96ZZZM505 1 19960114 A 5312 BLKHD BEAM BOEING 727 72723 1384004 NM BS 1183 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 59690 19389 DURING C-CHECK, FOUND AFT BULKHEAD STATION 1183 WL 283 LBL 26 VERTICAL BEAM CRACKED. REMOVED AND REPLACED VERTICAL BEAM PER BOEING SB 727-53-182 TYPE IV. 2 L 7 3 4F A3WE 1996032900628 19960329 00628 NM 1996 3 29 96ZZZM506 1 19960114 A 5230 DOOR FRAME BOEING 727 72723 1384004 NM BS 1050 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 59690 19389 DURING C-CHECK, FOUND AFT CARGO FRAME 1050 CRACKED, STRINGER 27L. REMOVED SEAT TRACK FOR ACCESS PER SRM 51-30-2. CRACK TERMINATES AT FAST, HOLE PER SRM 51-10-1. INSTALL FRAME REPAIR PER SRM 53-10-4 LOT NR 670917 PO NR 93110262 SIZE 7075- T6 .080. REINSTALL SEAT TRACK PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996032900629 19960329 00629 NM 1996 3 29 96ZZZM507 1 19960114 A 5312 BLKHD BEAM BOEING 727 72723 1384004 NM BS 1183 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 59690 19389 DURING C-CHECK, FOUND CABIN AFT BULKHEAD STATION 1183 WL 283 VERTICAL BEAM CRACKED RBL 3683. REMOVED FASTENERS, STOP DR ILLED CRACK AND ALODINED STOP DRILLED HOLES PER SRM 51-30-2, 51-10-1, AND 51-10-2. VERTICAL BEAM REPAIR INSTALLED AT RB L 3683 STATION 1183 AS PER DRW 65C34406 AND SB 727-53-0192. 2 L 7 3 4F A3WE 1996032900630 19960329 00630 NM 1996 3 29 96ZZZM508 1 19960114 A 5751 SKIN BOEING 727 72723 1384004 NM RT AILERON DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 59690 19389 DURING C-CHECK, FOUND MSI 727-0710-1001 RIGHT INBOARD AILERON HAS DENT BEYOND UNFILLED LIMITS AND SPEED TAPED PER BOEING 727 SRM 57-50-1 PAGE 13. CUT OUT DAMAGE AREA AT UPPER SKIN RIGHT OUTBOARD AILERON IAW SRM 57-50-5. FABRICATED AND INS TALLED DOUBLER AND FILLER 6 INCHES BY 5.5 INCHES AND FILLER 3 INCH BY 3 INCH MADE OF 2024-T3 .025 PO NR 9319061 AND IAW SRM 57-50-5. 2 L 7 3 4F A3WE 1996032900631 19960329 00631 NM 1996 3 29 96ZZZM509 1 19960114 A 5320 ANGLE BOEING 727 72723 1384004 NM BS 1176.5 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 59690 19389 DURING C-CHECK, FOUND REINFORCEMENT CHORD ANGLE AT BS 1176.5 CORROSION NOTED LBL 7 INCH BY RBL 7 INCH. REPLACED CHORD A T BS 1176.5 AS PER SRM 51-10-1 PAR 4 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996032900632 19960329 00632 NM 1996 3 29 96ZZZM510 1 19960114 A 5330 SKIN BOEING 727 72723 1384004 NM BS 203.8 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 59690 19389 DURING C-CHECK, FOUND EXTERIOR SKIN AROUND 2 FASTENERS CRACKED AT LEFT SIDE BS 203.8 WL 219.5. REMOVED PANELS IN THE CO CKPIT TO GET ACCESS TO THE AREA PER SRM 51-30-2. CUT OUT THE DAMAGE AREA PER SRM 53-30-3 FIG 3. FABRICATED EXTERNAL DO UBLER 2024-T3 .063 10 INCH BY 10.5 INCH LOT NR 938627 AND FILLER 2024-T3 .050 2 INCH BY 1 INCH LOT NR 253901. INSTALL D OUBLER AT LEFT SIDE BS 203.8 WL 219.5 AS PER SRM 53-30-3 FIG 3. INSTALL COCKPIT PANELS. 2 L 7 3 4F A3WE 1996032900633 19960329 00633 NM 1996 3 29 96ZZZM511 1 19960114 A 5320 FLOOR SUPPORT BOEING 727 72723 1384004 NM BS 764 CORROSION A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 59690 19389 DURING C-CHECK, FOUND WING SECTION HAS CORROSION ON FLOOR SUPPORT ANGLE BOTTOM SIDE AT STATION 764 RBL 65 INCHES. REMOV ED FASTENERS PER SRM 51-30-2. CUT OUT DAMAGED AREA IN LOWER WEB 1.5 INCH DIAMETER APPROX CLEANED AREA, ALODINED AND PRI MED PER SRM 51-10-2. INSTALLED DOUBLER 2024-T3 .040 7 INCH BY 3 INCH LOT NR 255933 AT STATION 764 RBL 65 INCHES AS PER SRM 51-40-2. 2 L 7 3 4F A3WE 1996032900634 19960329 00634 NM 1996 3 29 96ZZZM512 1 19960114 A 5320 WEB BOEING 727 72723 1384004 NM BS 247 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 59690 19389 DURING C-CHECK, FOUND NOSE W/W LEFT SIDE PRESSURE WEB CRACKED AT STATION 247 4 INCHES ABOVE GEAR DOOR. REMOVED FASTENER S PER SRM 51-30-2. CUT OUT DAMAGED AREA 2 INCH BY 1 INCH AT LEFT SIDE NOSE W/W STATION 247 PER SRM 51-10-1. FABRICATED EXTERNAL DOUBLER 2024-T3 .050 8 INCH BY 4 INCH PER SRM 53-10-9. INSTALLED DOUBLER PER SRM 53-10-9. 2 L 7 3 4F A3WE 1996032900635 19960329 00635 NM 1996 3 29 96ZZZM513 1 19960114 A 5210 SKIN BOEING 727 72723 1384004 NM ENTRY DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 59690 19389 DURING C-CHECK, FOUND FWD ENTRY DOOR EXTERIOR SKIN CRACKED AND BENT AT UPPER HINGE CUTOUT. REMOVED INNER SKIN PANEL AS PER SRM 52-40-2. ROUTED OUT CRACKS FWD ENTRY DOOR EXTERIOR SKIN UPPER HINGE AS PER SRM 51-10-1. FABRICATED DOUBLER .06 3 2024-T3 9 INCH BY 12 INCH PO NR 9317973 LOT NR 127-432 AS PER SRM 52-40-2. TREATED AND PRIMED REPAIR PARTS AS PER SRM 51-10-2. INSTALL REPAIR PARTS WITH FAYING SURFACE SEAL AND FILLET SEAL AS PER SRM 53-30-4 AND 52-40-2. INSTALL PANEL PLATE INNER SKIN, REMOVED ON NR 1 STEP PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996032900636 19960329 00636 NM 1996 3 29 96ZZZM514 1 19960114 A 5320 GUSSET BOEING 727 72723 1384004 NM BS 825.95 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 59690 19389 DURING C-CHECK, FOUND LEFT SIDE GUSSET CRACKED AT FWD SIDE OF FUSELAGE FRAME 825.95 SUB FLOOR. REMOVED CRACKED GUSSET A S REQUIRED PER SRM 51-10-1. FABRICATED NEW GUSSET 2024-T3 .090 5 INCH BY 4 INCH LOT NR 483-871 PO NR 93110393 AND SHIM 2024-T3 .125 2.5 INCH BY 2 INCH LOT NR 672-773 PO NR 9318078. ALODINED AND PRIMED GUSSET AND SHIM AS PER SRM 51-10-2. I NSTALLED NEW GUSSET AND SHIM AS PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996032900637 19960329 00637 NM 1996 3 29 96ZZZM515 1 19960114 A 5520 ELEV TIP BOEING 727 72723 1384004 NM RT ELEVATOR LOOSE RIVETS A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 59690 19389 DURING C-CHECK, RIGHT ELEVATOR OUTBOARD TE TIP REPAIR HAS LOOSE RIVETS UPPER AND LOWER SIDES. REMOVED FASTENERS PER SRM 51-30-2. CUT OUT 9 INCH BY 10 INCH AREA OUTBOARD TE TIP REPAIR, MADE TOP AND LOWER DOUBLER AND FILLER 2024-T3 .032 FIL LER .063 PER SRM 55-20-2. INSTALLED ELEVATOR T/E SKIN REPAIR PER SRM 55-20-3 11 INCH BY 12 INCH .032 AND FILLER .063 FI G 2 SHEET 2 PO (.3293110887) (.06393110848) LOT (.062 938627) (.032 275611). 2 L 7 3 4F A3WE 1996032900642 19960329 00642 NM 1996 3 29 96ZZZM520 1 19960114 A 5330 SKIN BOEING 727 72723 1384004 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 59690 19389 DURING C-CHECK, FOUND FUSELAGE SKIN ABOVE AFT LAV SERVICE DOOR BULGED. INSTALLED PLUB AND DOUBLER 22.25 INCH BY 22.25 I NCH PER AERONAUTICAL ENGINE DRAWING AE5093. 2 L 7 3 4F A3WE 1996032900684 19960329 00684 EU 1996 3 29 AALA960242 1 19960207 A 2422 1B8001G INVERTER FOKKER F28 F28MK0100 4990807 EU E/E COMPT DEFECTIVE A AALA K NONE H J ELECT. POWER LOSS-50 PC WARNING INDICATION AP APPROACH 1 SW 07 1471G 11507 BNA - FLT NR 580 - DURING APPROACH TO BNA, FWD BEGAN CHIMING NUMEROUS TRIPLE ALERTS, NR 1 FMC WENT OUT. NR 1 MFDU WENT OUT. ESSENTIAL AC BUS WARNING ANNUNCIATED ON RIGHT MFDU FOLLOWED BY FAULTS ON YAW DAMPER SYSTEM 1 AND 2 AND NR 1 AND 2 AUTOTHROTTLE SYSTEMS. LOST CAPTAINS RADION ALTIMETER AND GROUND PROX SYSTEM WARNING ALSO ANNUNCIATED. AIRCRAFT LANDED BNA WITHOUT INCIDENT. REPLACED EMERGENCY POWER INVERTER AND HEAT SINK GROUND HANDLING DIODE (CR3) ON BLOCK TB0609A. SY STEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1996032900685 19960329 00685 NM 1996 3 29 ASAA9610019 1 19960214 A 5314 KEEL BEAM BOEING 737 7372Q8C 138448S NM BS 500 CORRODED A ASAA O OTHER O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 SEA - DURING NON ROUTINE MAINTENANCE INSPECTION, CORROSION WAS FOUND ON THE KEEL BEAM LOWER CHORD AT THE FORWARD PRODUCT ION SPLICE WITH STRINGER 28R, BS 500. REPAIRED PER B737-200 SRM 53-10-3, ASA EA 5310-01404 AND BOEING TELEX ASA-SEA-96- 0078RR. (M) 2 L 7 2 4F A16WE 1996032900686 19960329 00686 WP 1996 3 29 ASAA9680045 1 19960207 A 5210 MECHANISM DOUG DC9 DC983 3022083 WP L1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 944AS 53019 SEA - PRIOR TO DEPARTURE OF FLT NR 524, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO CLOSE. ADJUSTED DOOR MECHANISM PER M M AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996032900687 19960329 00687 NE 1996 3 29 C1HA960008 2 19960201 A 7230 12254621 REG DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3B 52039 NE NR 2 ENG MALFUNCTIONED A C1HA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 WP 23 802MG 46098 645997 AT 70 KNOTS NR 2 ENGINE COMPRESSOR STALLED. ABORTED TAKEOFF. REMOVED AND REPLACED NR 2 ENG REGULATOR AND RELIEF VALVE. OPS CHECK GOOD ON HIGH SPEED TAXI. (M) 2 L 7 4 4F 4 F 4A25 1E8 1996032900688 19960329 00688 NE 1996 3 29 C1HA960009 2 19960131 A 7230 450041 PS4 LINE DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3B 52039 NE NR 2 ENG CLOGGED A C1HA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 WP 23 802MG 46098 645997 AT TAKEOFF ROTATION NR 2 ENGINE COMPRESSOR STALLED 4 OR 5 TIMES. REDUCED NR 2 THRUST LEVER TO CLEAR THE CONDITION. ADV ANCED THRUST LEVER BACK TO NORMAL MCT, ALL PARAMETERS NORMAL. NO FURTHER ABNORMALITY. CLEARED PS4 LINE AND RESECURED. ENGINE RUN PER MM 71-00 PAGE 501. (M) 2 L 7 4 4F 4 F 4A25 1E8 1996032900689 19960329 00689 NM 1996 3 29 CAL960107 1 19960127 A 2751 285N001140 ELECT UNIT BOEING 757 757224 1384958 NM E/E BAY INOPERATIVE A CALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 09 17104 27294 FLT NR 1106 - DEN - THE EICAS LE SLAT ASYMMETRY AND LEADING EDGE LIGHT ILLUMINATED IN FLIGHT. THE AIRCRAFT WAS DIVERTED TO DEN WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 FLAP AND SLAT ELECTRONIC UNIT AND THE S10340 SL AT LOSS SENSING SWITCH. GROUND TESTING WAS CONDUCTED IAW MM 27-81-41 AND SYSTEMS CHECKED GOOD. (M) 2 L 7 2 4F RT A2NM 1996032900690 19960329 00690 WP 1996 3 29 EIAA9604 1 19960213 A 5711 5911300501 SPAR CAP DOUG DC9 DC933F 302207A WP WS 137 CORROSION A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 944F 46705 47194 DURING C-CHECK INSPECTION DISCOVERED EXFOLIATION CORROSION IN THE REAR SPAR CAP UPPER AFT FLANGES, SLIGHTLY INBOARD OF T HE REAR STATION XRS 137 ON BOTH THE LEFT AND RIGHT WINGS. REPAIRED BY BLENDING OUT THE CORROSION, ALODNING, FR PRIMING AND FINISHED THE BLEND AREAS PER SRM CH 51 TO PROTECT AGAINST FURTHER CORROSION. INSTALLED FASTENERS USING TAPERED WASH ERS AND SELF ALIGNING NUTS. ACCOMPLISHED IAW EVERGREENS ECRA NR 944-57-021-2 DATED 1-8-96. (M) 2 L 7 2 4F A6WE 1996032900691 19960329 00691 NE 1996 3 29 EIAA9605 2 19960215 A 7200 ENGINE BOEING 747 747132 1384882 NM PWA JT9 JT9D7F 52054 NE NR 1 FLAMED OUT A EIAA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 NM 09 481EV 73019 8877 19896 662308 NR 1 ENGINE FLAMED OUT AT FL 370, NOTHING UNUSUAL NOTED, FUEL X-FEED AT TIME, NORMAL AIRSTART ACCOMPLISHED. ENGINE OPER ATED NORMAL FOR REST OF FLIGHT. INSPECTED COMPRESSOR INLET, TURBINE SECTION AND CHECKED FUEL SCREENS, FOUND NO DEFECTS IAW EIA MAINTENANCE PROCEDURES. WINDMILL INSPECTION ACCOMPLISHED IAW 71-00-00. MAINTAINED POSITIVE OIL PRESSURE AT ALL TIMES. (M) 2 L 7 4 4F 4 F A20WE E20EA 1996032900692 19960329 00692 NE 1996 3 29 EIAA9606 2 19960222 A 7230 COMPRESSOR BOEING 747 747212B 1384886 NM PWA JT9 JT9D7J 52054 NE NR 3 STALLED A EIAA O OTHER R PARTIAL RPM/PWR LOSS DE DESCENT 1 NM 09 485EV 69082 20712 662268 BRU - AT TOP OF DESCENT WHEN THROTTLES PULLED TO IDLE, NR 3 COMPRESSOR STALLED AND FLAMED OUT. RESTART OK. CHECKED OPE RATION OFF BLEED VALVES IAW FIM 71-01-20, NORMAL OPERATION, EVC FILTER NOT CONTAMINATED. AIRCRAFT RELEASED ACC FIM 71-0 1-00 PAGE 230. (M) 2 L 7 4 4F 4 F A20WE E20EA 1996032900716 19960329 00716 SW 1996 3 29 MALA964862 1 19960207 A 5320 2725008 CHANNEL SWRNGN SA227 SA227AC 8780603 SW LT COCKPIT CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 436MA AC719B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE CAPTAIN'S SEAT TRACK SUPPORT CHANNEL. T HEY INSTALLED A REPAIR DOUBLER IAW FAC ARP 53-10-9322. (M) 2 L 7 2 4T RT A8SW 1996032900717 19960329 00717 SW 1996 3 29 MALA964863 1 19960207 A 5210 2724044012 CORNER SWRNGN SA227 SA227AC 8780603 SW PAX DOOR CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 436MA AC719B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE UPPER FORWARD PASSENGER DOOR CORNER. T HEY REPLACED THE CORNER, P/N 27-24044-012, IAW FAC SRM 51-00-00 AND 51-40-01. (M) 2 L 7 2 4T RT A8SW 1996032900719 19960329 00719 SW 1996 3 29 MALA964865 1 19960206 A 2130 BLEED AIR SWRNGN SA227 SA227AC 8780603 SW RIGHT SMOKE A MALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 15 26863 AC650B FLT NR 3079 - EN ROUTE FROM FFM-RVF, THE CREW NOTED SMOKE COMING FROM THE BLEED AIR SYSTEM. THEY SHUT OFF THE RIGHT BLE ED AND THE SMOKE STOPPED. THE AIRCRAFT CONTINUED TO TVF AND LANDED WITHOUT INCIDENT. THE SYSTEM WAS DEFERRED UNDER MEL 21-9. 2 L 7 2 4T RT A8SW 1996032900720 19960329 00720 SW 1996 3 29 MALA964866 1 19960210 A 2170 8323715 COALESCER BAG SWRNGN SA227 SA227AC 8780603 SW CABIN DIRTY A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 15 422MA AC635 FLT NR 3011 - AFTER DEPARTURE FROM DTW, THE CABIN BEGAN TO FILL WITH SMOKE. THE CREW SHUT OFF THE BLEEDS AND RETURNED T O DTW WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE LEFT AND RIGHT WATER SEPARATOR SOCKS. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2 L 7 2 4T RT A8SW 1996032900721 19960329 00721 NM 1996 3 29 MALA964867 1 19960208 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A MALA O OTHER L NO TEST IN INSP/MAINT 1 GL 15 853MA 353 DURING A PREFLIGHT INSPECTION IN MSP, THE CREW NOTED THAT THE COCKPIT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAIN TENANCE REPLACED THE COCKPIT LIGHT ASSEMBLY, P/N 10-0055-11. SYSTEM OPERATED SATISFACTORILY. (M) 2 H 7 2 4T RT A13NM 1996032900722 19960329 00722 SW 1996 3 29 MALA964868 1 19960212 A 3260 WARNING HORN SWRNGN SA227 SA227AC 8780603 SW LANDING GEAR SOUNDED A MALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 15 425MA AC640 FLT NR 3460 - DURING APPROACH TO DTW, THE GEAR WARNING HORN SOUNDED WHEN FLAPS WERE SELECTED TO FULL. AFTER EXECUTING A GO-AROUND, THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL PERFORMED SEVERAL FUNCTIONAL TESTS OF THE GEAR WARNING HORN SYSTEM BUT WERE UNABLE TO DUPLICATE THIS DISCREPANCY. (M) 2 L 7 2 4T RT A8SW 1996032900723 19960329 00723 SW 1996 3 29 MALA964869 1 19960212 A 3610 2784086263 ORIFICE PLATE SWRNGN SA227 SA227AC 8780603 SW LT WING ROOT NOT INSTALLED A MALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 GL 15 2692P AC658B FLT NR 3081 - AFTER DEPARTURE FROM MSP, THE LEFT WING OVERHEAT LIGHT ILLUMINATED. THE CREW ELECTED TO RETURN TO MSP AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REINSTALLED THE BLEED AIR MIXING VALVE RESTRICTOR PLATE. A LL SYSTEMS OPERATED SATISFACTORILY. (M) 2 L 7 2 4T RT A8SW 1996032900724 19960329 00724 SW 1996 3 29 MALA964870 1 19960213 A 3260 1EN516 SWITCH SWRNGN SA227 SA227AC 8780603 SW RT MLG FAILED A MALA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 15 422MA AC635 FLT NR 3245 - DURING APPROACH TO MSP, THE RIGHT MAIN GEAR INTRANSIT LIGHT DID NOT ILLUMINATE WHEN THE LANDING GEAR WAS E XTENDED. THE AIRCRAFT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE RIGHT INBOARD M LG POSITION SWITCH. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2 L 7 2 4T RT A8SW 1996032900725 19960329 00725 SW 1996 3 29 MALA964871 1 19960216 A 3230 2791000291 UPLOCK HOOK SWRNGN SA227 SA227AC 8780603 SW NLG WORN A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 60NE AC760B FLT NR 3395 - EN ROUTE TO CRW, THE NOSE GEAR RED UNSAFE LIGHT ILLUMINATED AND THE NOSE GEAR BEGAN TO CYCLE. THE AIRCRAF T RETURNED TO DTW. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. UPON FURTHER INSPECTION, THE UPLOCK HOOK ROLLE R WAS FOUND TO BE WORN. THE UNIT WAS REPLACED. THE SYSTEM OPERATED SATISFACTORILY. (M) 2 L 7 2 4T RT A8SW 1996032900726 19960329 00726 SW 1996 3 29 MALA964872 1 19960219 A 5311 FRAME SWRNGN SA227 SA227AC 8780603 SW FS 159 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 26906 AC654B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE FUSELAGE FRAME AT FS 159. MAINTENANCE PERSONNEL REMOVED AND REPLACED A PREVIOUSLY INSTALLED REPAIR DOUBLER IAW FAC ARP 53-10-9114. (M) 2 L 7 2 4T RT A8SW 1996032900727 19960329 00727 NM 1996 3 29 MALA964873 1 19960217 A 3350 CONNECTORS DHAV DHC8 DHC8102 2809003 NM COCKPIT LOOSE A MALA K NONE L NO TEST CR CRUISE 1 GL 15 826MA 330 FLT NR 3166 - EN ROUTE FROM FNT TO DTW, THE COCKPIT OVERHEAD EMERGENCY LIGHT WAS FLICKERING ON AND OFF. THE AIRCRAFT CO NTINUED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL SECURED LOOSE CONNECTORS AT THE EMERGENCY LIGHT RECEP TACLE. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2 H 7 2 4T RT A13NM 1996032900728 19960329 00728 SW 1996 3 29 MALA964874 1 19960216 A 3230 RETRACT MECH SWRNGN SA227 SA227AC 8780603 SW NLG MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 60NE AC760B FLT NR 3345 - EN ROUTE FROM DTW TO CRW, THE NOSE GEAR INTRANSIT LIGHT ILLUMINATED AND THE NOSE GEAR BEGAN TO CYCLE IN TH E GEAR WELL. THE CREW ELECTED TO RETURN TO DTW AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL FUNCTIO NALLY TESTED THE SYSTEM BUT WERE UNABLE TO DUPLICATE THE DISCREPANCY. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2 L 7 2 4T RT A8SW 1996032900729 19960329 00729 NM 1996 3 29 TAOA029609 1 19960213 A 3350 ML3071BPE BULB BOEING 727 727225 1384077 NM CABIN FAILED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 918TS 20445 'E' PATH LIGHTS AT ROW 5 AND 25 INOP. REPLACED LIGHTS, OPERATIONAL CHECK OK. (M) 2 L 7 3 4F A3WE 1996032900730 19960329 00730 NM 1996 3 29 TAOA029610 1 19960213 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 918TS 20445 TWO EXTERIOR EMERGENCY LIGHTS ON LEFT SIDE INOP. REPLACED BATTERY PACKS. OPERATIONAL CHECK OK. (M) 2 L 7 3 4F A3WE 1996032900731 19960329 00731 NM 1996 3 29 TAOA029612 1 19960217 A 3397 WIRE BOEING 727 727254 138408L NM CABIN SEVERED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 913TS 20250 ESCAPE PATH LIGHTS AT ROW 24 INOP. REPAIRED BROKEN WIRES. OPERATIONAL CHECK OK. (M) 2 L 7 3 4F A3WE 1996032900732 19960329 00732 NM 1996 3 29 TAOA029613 1 19960218 A 3350 900835A BATTERY PACK BELL BOEING 727 727225 1384077 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 918TS 20445 FORWARD ENTRY EMERGENCY EXIT SIGN INOP. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. (M) 2 L 7 3 4F A3WE 1996032900733 19960329 00733 NM 1996 3 29 TAOA029614 1 19960218 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 918TS UA5014 20445 MID CABIN EMERGENCY EXIT SIGN INOP. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. (M) 2 L 7 3 4F A3WE 1996032900734 19960329 00734 NE 1996 3 29 TWRA9608 2 19960210 A 7530 LEVER BOEING 747 747212B 1384886 NM PWA JT9 JT9D7Q 52054 NE NR 3 ENGINE BROKEN A TWRA E ENGINE SHUTDOWN J WARNING INDICATION LD LANDING 1 EA 15 618FF 21937 702214 ON APPROACH TO BOMBAY, NR 3 ENGINE STALLED, EGT REACHED 735 DEGREES FOR 30 SECONDS. OIL PRESSURE 4 PSI WINDMILL HYDRAUL IC PRESSURE AVAILABLE WITHOUT ADP. ACCOMPLISHED ENGINE FAILURE PROCEDURES. FOUND EVBC ROD CONNECT LEVER BROKEN. REPLA CED LEVER, R/U OK. (M) 2 L 7 4 4F 4 F A20WE E3NE 1996032900735 19960329 00735 NM 1996 3 29 TWRA9609 1 19960210 A 2910 HYD LINE BOEING 747 747121 1384871 NM NR 4 ENGINE LEAKING A TWRA O OTHER J K WARNING INDICATION FLUID LOSS CL CLIMB 1 EA 15 613FF 19647 AFTER GEAR RETRACTION ON DURING CLIMB-OUT FROM MIA. NR 4 HYDRAULIC SYSTEM QUANTITY DECREASED TO 1 GALLON. SYSTEM DEPRE SSURIZED, QUANTITY INCREASED TO 2.5 GALLONS UPON GEAR EXTENSION. AIRCRAFT WAS BEING THREE ENGINE FERRIED TO JFK WITH NR 4 ENGINE INOP. OIL LOSS FROM ENGINE DISCONNECT. ENGINE REPLACED LINE TIGHTEN, NOW OK. (M) 2 L 7 4 4F A20WE 1996032900736 19960329 00736 1996 3 29 USAAF96020 4 19960212 A 3444 858202 PSEU COMPUTER FOKKER F28 F28MK1000 4990808 EU E/E COMPT FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 868US 8961 11313 PIT - FL 1193 - ON CLIMB-OUT FROM PHL, CREW RECEIVED TCAS FAULT AND GROUND/FLIGHT CONTROL FAULT. EN ROUTE TO MCI, CREW RECEIVED THE TAKEOFF CONFIGURATION STAB TRIM FAULT. FLIGHT DIVERTED TO PIT AND LANDED WITH NO FURTHER INCIDENT. MAINTE NANCE REPLACED THE PSEU COMPUTER. (M) 2 L 7 2 4F RT A20EU 1996032900737 19960329 00737 NM 1996 3 29 USAASB96024 1 19960202 A 5210 66109059 HINGE BOEING 737 737301 1384611 NM PAX DOOR BENT A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 300AU 23228 FLT NR 8945 - CLT - RETURNED TO FIELD, LOUD AIR DRAFT DOOR L-1, UNABLE TO MAINTAIN PRESSURIZATION. MAINTENANCE FOUND LO WER HINGE ARM FLAP BENT. REPOSITIONED FLAP. PRESSURIZED AIRCRAFT ON GROUND, NO LEAKS OR LOUD NOISE NOTED. OK FOR SERV ICE. (M) 2 L 7 2 4F RT A16WE 1996032900738 19960329 00738 NM 1996 3 29 USAASB96028 1 19960210 A 2150 1173T121 SWITCH BOEING 737 7373B7 1384580 NM RIGHT PACK FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 518AU 23704 FLT NR 1204 - PHL - AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. NO COCKPIT INDICATIONS. OUTFLOW VALVE WAS CLOSED. MA INTENANCE REPLACED RIGHT PACK TURBINE INLET SWITCH FOR PRECAUTIONARY MEASURES. (M) 2 L 7 2 4F RT A16WE 1996032900739 19960329 00739 EU 1996 3 29 WTAA960029 1 19960204 A 2611 72111211000 SMOKE DETECTOR BAG JETSTM JETSTM3101 1500215 EU BAGGAGE COMPT INTERMITTENT A WTAA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 WP 17 422UE 782 SFO - SMOKE DETECTION LIGHT ACTIVATED ON RAMP. NO SMOKE OR FIRE DETECTED. DETERMINED TO BE FALSE INDICATION. REPLACED SMOKE DETECTOR. SMOKE DETECTION SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A21EU 1996032900740 19960329 00740 SO 1996 3 29 WTAA960030 1 19960201 A 3260 922AA2YA6P PROX SENSOR EMB 120 EMB120RT SO LT MLG OUT OF ADJUST A WTAA O OTHER N FALSE WARNING CR CRUISE 1 WP 17 280UE 120090 MRY - LEFT MAIN LANDING GEAR 'A' SYSTEM RED INTRANSIT LIGHT ILLUMINATED IN FLIGHT. AIRCRAFT FERRIED TO FAT FOR REPAIRS. MAINTENANCE ADJUSTED LEFT MAIN GEAR 'A' SYSTEM UPLOCK PROXIMITY SENSOR. GEAR POSITION INDICATION SYSTEM OPERATIONAL C HECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 1996032900741 19960329 00741 NE 1996 3 29 WTAA960031 2 19960208 A 7320 7863904 HMU EMB 120 EMB120RT SO PWA 118 PW118A NE RT ENGINE FAILED A WTAA A UNSCHED LANDING J O WARNING INDICATION OTHER CL CLIMB 1 WP 17 122AM 120013 SFO - RIGHT ENGINE TORQUE DROPPED FROM 67 PERCENT TO 29 PERCENT WHILE CLIMBING THROUGH 14,000 FEET ITT AND FUEL FLOW RED UCTION NOTED WITH POWER LOSS. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT ENGINE HMU. R IGHT ENGINE OPERATIONAL CHECK NORMAL DURING GROUND RUN. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1996040500001 19960405 00001 CE 1996 4 5 131963CK 1 19960201 A 3260 1CH16 SWITCH LEAR 24 24A 5170304 CE RT MLG DNLOCK FAILED A KKFA O OTHER N FALSE WARNING AP APPROACH 1 GL 23 63CK 119 DURING GEAR EXTENSION, RT MAIN DOWN AND LOCK LIGHT FAILED TO ILLUMINATE IMMEDIATELY. AFTER SEVERAL ATTEMPTS, IT CAME ON , NORMAL LANDING MADE. LANDING GEAR INDICATING SYSTEM OPERATED NORMALLY ON JACKS. GEAR DOWN AND LOCK SWITCH REPLACED F OR POSSIBLE FREEZING. (X) 2 L 7 2 4J A10CE 1996040500009 19960405 00009 SO 1996 4 5 96ZZZX1398 1 19960112 A 5330 SKIN GULSTM G1159 G1159 3953505 SO FS 580-635 CORRODED A J7SA K NONE O OTHER IN INSP/MAINT 1 SW 21 17ND 10288 63 DURING ACCOMPLISHMENT OF CUSTOMER BULLETIN NR 411, CORROSION FOUND IN LOWER FUSELAGE BETWEEN FS 580 AND FS 635, REFERENC E K.C. AVIATION W/O 21945/6001. 2 L 7 2 4F RT A12EA 1996040500010 19960405 00010 NM 1996 4 5 96ZZZX1399 1 19960203 A 2910 171T1414CR019 HYD LINE BOEING 737 7372L9 1384497 NM NLG WW FAILED A ZZDA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SO 15 464AT 21278 AFTER TAKEOFF FROM BRADLEY, CONN, NLG WOULD NOT RETRACT RESULTING IN AN AIR TURNBACK. FOUND NLG LOCK ACTUATOR HYD FLEX LINE FAILED. REMOVED AND REPLACED FLEX LINE. LEAK CHECK GOOD PER MM 29-12-31. 2 L 7 2 4F RT A16WE 1996040500011 19960405 00011 SO 1996 4 5 96ZZZX1400 2 19960207 A 8520 CRANKCASE CESSNA 402 402B 207590P CE CONT O520 TSIO520E 17040 SO RT ENGINE CRACKED A AJZA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 19 13GM 402B0246 1821270E DURING TROUBLESHOOTING OIL LEAK ON RT ENGINE, MECHANIC FOUND CASE CRACKED. LT CASE HALF JUST FORWARD OF THE OIL COOLER. ENGINE REMOVED FOR REPAIR. 1 L 7 2 3O 3 O A7CE E8CE 1996040500012 19960405 00012 CE 1996 4 5 96ZZZX1401 1 19960227 A 2421 30B10719A GENERATOR LEAR 35 35A 5170602 CE RIGHT FAILED A AOQA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 EA 11 719JB 166 JFK/DTW, NITE IMC - ON 2-27-96 EN ROUTE, RT CURRENT LIMITER FAIL LIGHT ILLUMINATED FOLLOWED BY THE RT GEN FAIL LIGHT ILL UMINATED. AIRCRAFT DIVERTED TO BUF. AIRCRAFT LANDED WITHOUT INCIDENT. INSTALLED NEW CURRENT LIMITER, O/H GENERATOR, O /H VOLTAGE REGULATORS (VOLTAGE REGULATORS REPLACED FOR PRECAUTION). OPERATIONAL CHECKED DC ELECTRICAL SYSTEM GOOD. AIR CRAFT RETURNED TO SERVICE, 2-28-96. LANDINGS, 6,786. 2 L 7 2 4F A10CE 1996040500013 19960405 00013 SO 1996 4 5 96ZZZX1402 1 19960214 A 5280 47529032 HINGE PIPER PA31 PA31310 7103103 SO RT MLG DOOR CRACKED A A JIKA K NONE O OTHER IN INSP/MAINT 1 WP 01 199DS 317400980 DURING SCHEDULED ACFT INSPECTION, RT MAIN GEAR INBD DOOR'S FWD HINGE FORGING FND CRACKED IN INNER RADIUS. THE CRACK IS DETECTABLE VISUALLY EVEN THOUGH PART IS PAINTED; VISUAL PORTION OF CRACK IS THROUGH APPROX 25 PERCENT OF MATERIAL THICKN ESS. SUBMITTER STATES THIS IS THE HINGE INSTALLED IAW AD 80-26-05, & PIPER SB 682. THIS IS 7TH CRACKED OR FAILED HINGE FND SINCE BEGINNING OF 1995 BY THIS OPERATOR. WITH AD 80-26-05 UP FOR REVISION (DOCKET 90-CE-59-AD), FAA & PIPER MAY W ANT TO CONSIDER A FURTHER IMPROVED HINGE FORGING. WHILE CRACK RATE OF CURRENT P/N IS LESS THAN OLD PRE-AD STYLE, PROBLE M HAS NOT BEEN CORRECTED & BEARS FURTHER IMPROVEMENT. 1 L 7 1 3O RT A20SO 1996040500015 19960405 00015 WP 1996 4 5 96ZZZX1404 2 19960118 A 7261 8650914 GASKET 86504612 FRCHLD SA227 SA227DC 3377521 SW GARRTT TPE331 TPE33112UAR 01514 WP LT OIL SCAV PMP LEAKING A EQGA E ENGINE SHUTDOWN J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SW 19 853LS 36 DC853B P70219 DFW/WDG - FLT 1260 - WHILE EN ROUTE, LT ENGINE LOST ALL OIL PRESSURE. THE PILOT SHUT DOWN LT ENGINE AND PROCEEDED TO DF W WHERE HE LANDED WITHOUT FURTHER INCIDENT. UPON TROUBLESHOOTING, FOUND THE SCAVENGE OIL PUMP GASKET LEAKING AND THE MO UNT BOLTS LOOSE. MAINTENANCE REPLACED THE GASKET AND TORQUED TO MOUNT BOLTS. GROUND RUNS CHECKED NORMALLY AND AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 4T 4 T RT A18SW E4WE 1996040500016 19960405 00016 NM 1996 4 5 96ZZZX1405 1 19960124 A 5330 SKIN BOEING 737 7372H5 138448E NM BS 271 CRACKED A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 220US 20453 GSO - DURING SCHEDULED MAINTENANCE CHECK, VISUAL INSPECTION FOUND .625 INCH CRACK IN OUTER SKIN AT FS 271, STR 16L. INS TALLED EXTERNAL REPAIR PER SRM 53-30-3. (X) 2 L 7 2 4F A16WE 1996040500017 19960405 00017 NE 1996 4 5 96ZZZX1406 2 19960123 A 7310 3035681 FUEL FILTER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE RT ENGINE PUMP DIRTY A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 07 436JS 3052 FLT 4034 - CREW ABORTED TAKEOFF AFTER BEING ALERTED BY FUEL BYPASS CAS MESSAGE. AIRCRAFT RETURNED TO GATE WITHOUT FURTH ER INCIDENT. OUT STATION MAINTENANCE REMOVED, CLEANED, AND REINSTALLED THE H.P. FUEL FILTER IAW MM 71-00-00. GROUND RUN S CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 1996040500018 19960405 00018 NM 1996 4 5 96ZZZX1407 1 19960121 A 3260 0L3092 BULB DORNER DO32 DO328100 2996000 NM LT MLG DEFECTIVE A VNAA O OTHER N FALSE WARNING AP APPROACH 1 GL 07 436JS 3052 FLT 4134 - ON APPROACH WHILE EXTENDING THE LANDING GEAR IN PREPARATION FOR LANDING, THE LT MAIN GEAR DID NOT INDICATE DO WN AND LOCKED. THE CREW FOLLOWED PROCEDURES AS SPECIFIED IN THE QUICK REFERENCE HANDBOOK, AIRCRAFT LANDED WITHOUT FURTH ER INCIDENT. PIT MX REPLACED DEFECTIVE BULBS IN THE LANDING GEAR POSITION INDICATOR. GROUND CHECKED GOOD, AIRCRAFT RET URNED TO SERVICE. 2 H 7 2 4T RT A45NM 1996040500019 19960405 00019 WP 1996 4 5 96ZZZX1408 1 19960114 A 3350 58222 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 406EA 47686 STL - FIRST CLASS OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED TWO EACH BULBS, MFG PN 1315, AND ONE EACH BATTERY PACK, MFG PN 5822-2. OPERATIONAL CHECK NORMAL. CHECK C - 9-17-95 - STL. 2 L 7 2 4F A6WE 1996040500020 19960405 00020 SW 1996 4 5 96ZZZX1409 1 19960217 A 6410 222016001111 BLADE 222012701109 BELL 222 222U 1182140 SW T/R CRACKED A NXTA K NONE O OTHER IN INSP/MAINT 1 SW 19 141CF 2062 A00000005 47507 DURING C/W TAIL ROTOR BLADE VISUAL INSPECTION IN AD 96-01-08, A 5.3 INCH LONG CORD-WISE CRACK WAS DISCOVERED ON THE CONV EX SURFACE OF THE BLADE .25 INCH BELOW THE END OF THE DOUBLER. CRACK SIZE AND LOCATION IS THE SAME AS SHOWN IN THE ILLU STRATION CONTAINED IN THE AD. 1 G 7 2 3U H9SW 1996040500037 19960405 00037 NM 1996 4 5 96ZZZX1426 1 19960107 A 5320 SUPPORT BOEING 727 727259 138408J NM BS 1070-1090 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 203AV 22474 AFT CABIN AREA. FLOOR SUPPORT STRUCTURE AT STA 1070.0 - STA 1090.0, RBL-10, HAS LEVEL 2 CORROSION. REMOVED AND FABRICA TED FLOOR SUPPORT PER SRM 51-10-1, SRM 51-20-1, AND SRM 51-30-2. INSTALLED FLOOR SUPPORT AND FLOOR PANEL PER SRM 51-30- 2. 2 L 7 3 4F A3WE 1996040500039 19960405 00039 NM 1996 4 5 96ZZZX1428 1 19960102 A 5542 SKIN BOEING 727 727259 138408J NM RUDDER CRACKED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 203AV 22474 UPPER RUDDER T/E GOUGED AND CRACKED, LT SIDE. REPAIRED CRACK PER SRM 51-40-3, REPAIRED GOUGES ON AFT UPPER RUDDER L/M S IDE PER SRM 51-40-8. 2 L 7 3 4F A3WE 1996040500044 19960405 00044 NM 1996 4 5 96ZZZX1433 1 19960104 A 5315 FLOOR BEAM BOEING 727 727259 138408J NM BS 340 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 203AV 22474 STA 340, RBL 21 TO RBL 68 UPPER CHORD OF FLOOR BEAM HAS SEVERAL AREAS OF LEVEL 2 CORROSION. REMOVED AND REPLACED FLOOR BEAM (UPPER CHORD) STA 340, RBL 8 TO RBL 68 PER SRM 51-10-6, SRM 51-10-1, AND SRM 53-10-8. 2 L 7 3 4F A3WE 1996040500045 19960405 00045 NM 1996 4 5 96ZZZX1434 1 19960105 A 5320 SUPPORT BOEING 727 727259 138408J NM BS 312-354 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 203AV 22474 BS 312 - BS 354, RBL 55, FLOOR 2, SUPPORT AT DOOR SILL IS CORRODED LEVEL 2 AT DRAIN CHANNEL AND FITTINGS AND FLOOR BEAM ATTACHMENTS. REMOVED CORROSION PER SRM 51-10-6 FROM 2 CHANNELS AND DRAIN CHANNEL AND REINSTALLED PER SRM 51-10-2. 2 L 7 3 4F A3WE 1996040500046 19960405 00046 NM 1996 4 5 96ZZZX1435 1 19960107 A 2560 65659723 PLATES BOEING 727 727259 138408J NM L-2 DOOR CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 203AV 22474 LEVEL 2 CORROSION ON GIFT BAR BASE PLATES L-2 DOOR. REMOVED AND REPLACED PLATES PER SRM 51-10-02. 2 L 7 3 4F A3WE 1996040500047 19960405 00047 NM 1996 4 5 96ZZZX1436 1 19960105 A 5315 FLOOR BEAM BOEING 727 727259 138408J NM BS 1010-1130 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 203AV 22474 SEAT TRACK, STA 1010 - STA 1130, LBL 24 - LBL 25, HAS LEVEL 2 CORROSION. REMOVED CORRODED SECTION OF SEAT TRACK, FABRIC ATED AND INSTALLED NEW SECTION I SRM 53-10-5. REINSTALLED FLOOR BOARDS. 2 L 7 3 4F A3WE 1996040500048 19960405 00048 NM 1996 4 5 96ZZZX1437 1 19960105 A 5320 SUPPORT BOEING 727 727259 138408J NM BS 300 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 203AV 22474 RT FWD LAV AREA, STA 300, RBL 25, UPPER CHORD OF FLOOR SUPPORT STRUCTURE HAS LEVEL 2 CORROSION. REMOVED AND FABRICATED FLOOR SUPPORT UPPER CHORD MATERIAL 707517 LOCATED AND DRILLED, TREATED AND PRIMED, INSTALLED PER SRM 51-10-1 AND SRM 51- 30-2. 2 L 7 3 4F A3WE 1996040500049 19960405 00049 NM 1996 4 5 96ZZZX1438 1 19960215 A 3350 900835A BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SPAA K NONE L NO TEST IN INSP/MAINT 1 WP 07 703S 22529 DURING SCHEDULED CHECK, THE FORWARD AREA LIGHT/EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. THE ASSOCIATED BATTERY PACK WAS REMOVED, CHARGED, AND REINSTALLED. SUBSEQUENT OPS CHECK WAS SATISFACTORY PER B-737, MM 33-51-11. 2 L 7 2 4F A16WE 1996040500050 19960405 00050 NM 1996 4 5 96ZZZX1439 1 19960125 A 3350 900835A BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SPAA K NONE L NO TEST IN INSP/MAINT 1 WP 07 703S 22529 DURING SCHEDULED CHECK, THE FORWARD AREA LIGHT/EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. THE ASSOCIATED BATTERY PACK WAS REMOVED, CHARGED, AND REINSTALLED. SUBSEQUENT OPS CHECK WAS SATISFACTORY PER B-737, MM 33-51-11. 2 L 7 2 4F A16WE 1996040500051 19960405 00051 WP 1996 4 5 96ZZZX1440 1 19960126 A 3350 6404781 BATTERY PACK CVAC 440 440 2422902 WP CABIN DISCHARGED A SPAA K NONE L NO TEST IN INSP/MAINT 1 WP 07 73157 312 DURING SCHEDULED CHECK, NUMEROUS EXTERNAL EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. THE ASSOCIATED SYSTEM BATTERY P ACKS WERE REMOVED AND CHARGED, THEN REINSTALLED. SUBSEQUENT SYSTEM CHECKS WERE SATISFACTORY. 2 L 7 2 4R 6A6 1996040500052 19960405 00052 WP 1996 4 5 96ZZZX1441 1 19960206 A 3350 1102833 LIGHT CVAC 440 440 2422902 WP CABIN INOPERATIVE A SPAA K NONE L NO TEST IN INSP/MAINT 1 WP 07 73166 374 CREW REPORTED THE NR 2 CABIN INTERNAL EMERGENCY EXIT LIGHT CAME ON WHEN SYSTEM ARMING SWITCH PLACED IN THE 'OFF' POSITIO N. THE LIGHT ASSEMBLY WAS REPLACED, SUBSEQUENT SYSTEM CHECK WAS SATISFACTORY PER CV-580, MM 33-50-11. 2 L 7 2 4R 6A6 1996040500053 19960405 00053 EU 1996 4 5 96ZZZX1442 1 19960124 A 3097 WIRE AEROSP ATR42 ATR42300 8680920 EU RT ENGINE CHAFED A NVEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 03 142DD 17418 040 BWI - FLT 4941 - CREW REPORTS: SHORTLY AFTER TAKEOFF, FROM DCA TO JFK, THE FIRST OFFICER'S WINDSHIELD HEAT FAILED AND A N ELECTRICAL ODOR WAS SMELLED THROUGHOUT THE AIRCRAFT. ACFT DIVERTED TO BWI, DECLARED EMERGENCY, LANDED WITHOUT INCIDEN T. REPAIRED CHAFED WIRE IN BUNDLE ON RT ENGINE AND REPLACED RT AC GCU. 2 H 7 2 4T RT A53EU 1996040500056 19960405 00056 NE 1996 4 5 96ZZZX1445 2 19960219 A 7200 ENGINE EMB 120 EMB120RT SO PWA 118 PW118A NE LEFT FLAMED OUT A MASA A UNSCHED LANDING X ENGINE FLAMEOUT DE DESCENT 1 SW 01 453UE 120148 CEZ/DEN - AIRCRAFT WAS EN ROUTE WHEN LEFT ENGINE SUFFERED FROM APPARENT FLAME-OUT. AIRCRAFT WAS ON DESCENT AT APPROXIMA TELY 14,000 FEET. ENGINE SPOOLED DOWN, DROPPING EEC OFF-LINE AND CAUSING LOW OIL PRESSURE ANNUNCIATOR TO ILLUMINATE. P ILOT'S CONFIRMED LEFT ENGINE FAILED AND SECURED. AIRCRAFT LANDED IN CEZ WITHOUT FURTHER INCIDENT. AFTER MUCH INVESTIGA TION, NO APPARENT FAILURE FOUND, AND AIRCRAFT RETURNED TO SERVICE. CAUSE OF FLAME-OUT IS NOT DETERMINABLE AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 1996040500057 19960405 00057 NM 1996 4 5 AALA960044 1 19960111 A 3350 A3030398101 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 602AN 27053 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT MID-GALLEY FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR L IGHT CONNECTOR AT MID-GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1996040500058 19960405 00058 NM 1996 4 5 AALA960050 1 19960113 A 3350 STRIP BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 693AA 26973 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT BY PASSENGER SEAT 4E FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LI GHT STRIP BY PASSENGER SEAT 4E. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1996040500059 19960405 00059 NM 1996 4 5 AALA960056 1 19960115 A 3350 A3030398101 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 601AN 27052 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PASSENGER SEAT 9D INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR BY PASSENGER SEAT 9D. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1996040500060 19960405 00060 NM 1996 4 5 AALA960121 1 19960123 A 3350 STRIP BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 602AN 27053 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FIRST CLASS CABIN FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR L IGHT STRIP IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1996040500061 19960405 00061 NM 1996 4 5 AALA960175 1 19960204 A 3350 A3030398101 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 683A 25340 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 15 THROUGH 18 FOUND INOPERATIVE. RESEC URED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR BY PASSENGER SEAT ROW 15. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1996040500062 19960405 00062 WP 1996 4 5 AALA960177 1 19960204 A 3350 A3060720202 FLAT CONDUCTOR DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 245AA 49257 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT NEXT TO FIRST CLASS LAVATORY FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT FLAT CONDUCTOR BY FIRST CLASS LAVATORY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1996040500063 19960405 00063 NM 1996 4 5 AWXA96002 1 19960101 A 5210 STOP PAD BOEING 737 7373B7 1384580 NM R-1 DOOR JAMMED A AWXA K NONE O OTHER TX TAXI/GRND HDL 1 WP 28 328AW 23377 TPA\CMH - FLT 3105 - R-2 ENTRY DOOR JAMMED CLOSED. FOUND DOOR STOP JAMMED BETWEEN LOWER DOOR LEAF AND THRESHOLD PLATE. REMOVED STOP PAD, DOOR OPERATES NORMALLY. (X) 2 L 7 2 4F RT A16WE 1996040500064 19960405 00064 NM 1996 4 5 AWXA960032 1 19960124 A 3350 LIGHT BOEING 737 7373Q8 1384670 NM RT EMER EXIT INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 327AW 23507 PHX - FLT 0029 - DURING ROUTINE MAINTENANCE CHECK, FOUND RT OVERWING EXIT LOWER FORWARD EMERGENCY LIGHT INOPERATIVE. RE MOVED AND REPLACED RT HATCH DOOR IDENTIFIER. OPS CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1996040500065 19960405 00065 EU 1996 4 5 AWXA96006 2 19960106 A 7310 1090031 B-NUT BOEING 737 737301 1384611 NM CFMINT CFM56 CFM563B2 13802 EU NR 2 STRUT LOOSE A AWXA K NONE K FLUID LOSS TX TAXI/GRND HDL 1 WP 28 326AW 23258 SNA/PHX - FLT 0207 - FUEL LEAK SUSPECTED ON NR 2 ENGINE. OCCURRED DURING START AND APPEARS TO BE UNDER PRESSURE, NO SHA FT LEAK DETECTED. LOCATED AND RETORQUED LOOSE B-NUT TO M.E.C. FUEL INLET LINE AT FORWARD STRUT THROUGH-FITTING. RAN EN GINE. LEAK CHECK GOOD. (X) 2 L 7 2 4F 4 F RT A16WE E21EU 1996040500066 19960405 00066 1996 4 5 C2XA96CL016 4 19960206 A 3414 1303800057 AIRSPEED IND BEECH 1900 1900D 1154162 CE COCKPIT INOPERATIVE A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 09 16540 619 W21869 UE172 PIT - FLT 3333 - CREW REPORTED AFTER TAKEOFF, THE FIRST OFFICER'S AIRSPEED INDICATOR WAS INOPERATIVE. MAINTENANCE INSPE CTED AIRCRAFT AND REMOVED AND REPLACED THE FIRST OFFICER'S AIRSPEED INDICATOR. OPERATIONAL CHECKS WERE GOOD IAW B1900D MM 34-11-00. AIRCRAFT RELEASED FOR SERVICE. (X) 2 L 7 2 4T RT A24CE 1996040500067 19960405 00067 WP 1996 4 5 CAL960089 1 19960206 A 3230 RETRACT MECH DOUG DC9 DC982 3022082 WP LANDING GEAR MALFUNCTIONED A CALA O OTHER J WARNING INDICATION CL CLIMB 1 SW 09 14871 48022 IAH - FLT 1885 - THE LANDING GEAR WOULD NOT RETRACT INITIALLY AFTER TAKEOFF. THE GEAR HANDLE RELEASE BUTTON WAS USED TO RAISE THE GEAR. MAINTENANCE INSPECTED RIG OF ANTI-RETRACTION CABLE IAW MM 32-31-01, AND FOUND NO FAULTS. A GEAR RETRA CTION WAS PERFORMED WITH ALL OPERATION AND INDICATIONS CHECKING NORMAL. MAINTENANCE WAS UNABLE TO DUPLICATE THE PROBLEM . (X) 2 L 7 2 4F A6WE 1996040500068 19960405 00068 WP 1996 4 5 CAL960104 1 19960208 A 2520 INSULATION DOUG DC9 DC932 3022066 WP RT AIR COND PACK BURNED A CALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 12510 47799 CLE - FLT 1448 - THE PRESENCE OF FUMES WERE OBSERVED IN COCKPIT AND CABIN SHORTLY AFTER TAKEOFF FROM CLE. THE LEFT AND RIGHT PACKS WERE SEPARATELY ISOLATED, BUT THE FUMES CONTINUED. THE ACFT WAS RETURNED TO CLE. MAINTENANCE FOUND INSULAT ION ON RT PACK SYSTEM BURNED. THE INSULATION WAS REMOVED FROM DUCTS. A BURN-OUT OF HIGH PRESSURE PNEUMATIC DUCTING WAS PERFORMED IAW MM 21-20-02 AND THE PACKS OPERATED NORMALLY WITH NO FUMES NOTED. IN ADDITION, THE COALESCER BAGS WERE RE MOVED AND REPLACED. (X) 2 L 7 2 4F A6WE 1996040500069 19960405 00069 WP 1996 4 5 CAL960116 1 19960212 A 3230 GRD SENSE MECH DOUG DC9 DC982 3022082 WP NLG OUT OF RIG A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 14871 48022 CLE - FLT 0287 - THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM CLE. THE AIRCRAFT RETURNED TO CLE WHERE IT LANDE D WITHOUT INCIDENT. MAINTENANCE RE-RIGGED THE GROUND SENSING CONTROL MECHANISM AND ANTI-RETRACTION CABLE. THE GEAR WAS SWUNG AND OPERATION CHECKED NORMAL. IN ADDITION, THE NLG STRUT WAS SERVICED. A DIP WAS ISSUED TO CHECK THE NLG X-DIME NSION AFTER 4, BUT NO MORE THAN 20 LANDINGS. (X) 2 L 7 2 4F A6WE 1996040500074 19960405 00074 CE 1996 4 5 COEA9672801 1 19960206 A 2710 S20223L ROD END 26600029 CESSNA 208 208B 2073701 CE RT AILERON SEIZED A A COEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 13 728FX 152 208B0471 ON TAKEOFF OUT OF PHOENIX, PILOT REPORTED FLIGHT CONTROL SURFACES VERY HARD TO MOVE IN-FLIGHT. ACFT RETURNED WITHOUT IN CIDENT. INSPECTION REVEALED RT AILERON PUSH/PULL TUBE AFT ROD END SEIZED. MAINTENANCE REPLACED ROD END IAW CESSNA MM 2 7-10-01, RESET FUSELAGE LOOP AND HIGH TENSION LOOP CABLE TENSION PER CESSNA MM 27-10-01 AND MM 27-30-01. OPERATIONAL AN D FLIGHT CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 1 H 7 1 3T A37CE 1996040500075 19960405 00075 WP 1996 4 5 GAIA9523 1 19960131 A 3230 RETRACT MECH CVAC 240 600240D 2422660 WP LG MLG OUT OF ADJUST A GAIA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SW 07 94246 2900 102 DURING TRAINING FLIGHT, A SIMULATED LANDING APPROACH PROCEDURE WAS INITIATED. THE LT MLG DID NOT INDICATE DOWN AND LOCK ED CONDITION. THE FLIGHT CREW FOLLOWED EMERGENCY PROCEDURES, NOTIFIED ATC OF THE EMERGENCY, AND MADE AN UNEVENTFUL LAND ING. INSPECTION REVEALED LT MLG, PN BYC2758K, RETRACT MECHANISM WAS OUT OF RIG. LT MLG RIGGED IAW WITH KHAC CV 600 MAI NTENANCE PROCEDURES, CHAPTER 32, GEAR RETRACTION PERFORMED, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (X) 1 L 7 2 4T RT 2L72 1996040500077 19960405 00077 SW 1996 4 5 MALA964831 1 19960124 A 5330 SKIN SWRNGN SA227 SA227AC 8780603 SW FS 287 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 2692P AC658B DURING A SCHEDULED INSPECTION IN MSP, A CRACK WAS NOTED IN THE CONSTANT SECTION SKIN AT FS 287 AND WL 73.00. REPAIRS WE RE COMPLETED BY INSTALLING A STIFFENER AND DOUBLER IAW FAC SRM 53-90-20, REPAIR NR 20, PAGES 87-90. (X) 2 L 7 2 4T RT A8SW 1996040500078 19960405 00078 SW 1996 4 5 MALA964832 1 19960124 A 5520 CLIP SWRNGN SA227 SA227AC 8780603 SW LT ELEVATOR CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 2692P AC658B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND A CRACK IN A CLIP FOR THE LEFT ELEVATOR CLOSE-OUT FAIR ING END RIB. REPAIRS WERE COMPLETED BY REPLACING THE PART IAW FAC SRM 51-40-01 AND SRM 51-30-03. (X) 2 L 7 2 4T RT A8SW 1996040500079 19960405 00079 SW 1996 4 5 MALA964833 1 19960124 A 5230 STRUT ATTACH SWRNGN SA227 SA227AC 8780603 SW FS 438-491 WORN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 2692P AC658B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE CARGO DOOR FORWARD STRUT TO FUSELAGE ATTACH POINT AT FS 438.060, AND FS 491.060, TO NEED REPLACEMENT DUE TO CONDITION. REPAIRS WERE COMPLETED IAW FAC ARP 53-20-9503. (X ) 2 L 7 2 4T RT A8SW 1996040500080 19960405 00080 SW 1996 4 5 MALA964834 1 19960124 A 5210 DOOR CORNER SWRNGN SA227 SA227AC 8780603 SW PASSENGER DOOR CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 2692P AC658B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE LOWER PASSENGER DOOR CORNER CRACKED AT THE HANDRAI L SUPPORT NUTPLATE. REPAIRS COMPLETED BY REPLACING THE LOWER PASSENGER DOOR CORNER IAW FAC SRM 51-40-01. (X) 2 L 7 2 4T RT A8SW 1996040500081 19960405 00081 SW 1996 4 5 MALA964835 1 19960124 A 5311 FRAME SWRNGN SA227 SA227AC 8780603 SW FS 438 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 2692P AC658B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND A CUT-OUT IN THE FUSELAGE FRAME AT FS 438 TO BE CRACKE D. REPAIRS WERE COMPLETED BY INSTALLING A DOUBLER IAW FAIRCHILD LAR 96-MALA-001 AND SRM 51-40-00 AND SRM 51-30-04. (X) 2 L 7 2 4T RT A8SW 1996040500082 19960405 00082 SW 1996 4 5 MALA964836 1 19960123 A 6120 31057463 HTS SWITCH SWRNGN SA227 SA227AC 8780603 SW LT ENGINE FAILED A MALA E ENGINE SHUTDOWN K FLUID LOSS DE DESCENT 1 GL 15 445MA AC687 FLT 3269 - ON DESCENT TO MSP, THE LEFT OIL PRESSURE WARNING LIGHT ILLUMINATED AND THE LEFT OIL PRESSURE GAUGE INDICATED DECLINING PRESSURE. THE CREW SHUT THE ENGINE DOWN AND CONTINUED TO MSP. MAINTENANCE REPLACED THE NEGATIVE TORQUE SENSO R SWITCH. SYSTEM OPERATED SATISFACTORILY. (X) 2 L 7 2 4T RT A8SW 1996040500083 19960405 00083 SW 1996 4 5 MALA964846 1 19960128 A 3260 1EN516 SWITCH SWRNGN SA227 SA227AC 8780603 SW NLG FAILED A MALA O OTHER P NO WARNING INDICATION CL CLIMB 1 GL 15 2692P AC658B FLT 3462 - AFTER DEPARTURE FROM BRD, THE NOSE GEAR INTRANSIT LIGHT DID NOT ILLUMINATE WHEN THE GEAR WAS RETRACTED. THE AIRCRAFT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE RT INTRANSIT LIGHT SWITCH. A LL SYSTEMS OPERATED SATISFACTORILY. (X) 2 L 7 2 4T RT A8SW 1996040500084 19960405 00084 SW 1996 4 5 MALA964847 1 19960128 A 5270 8411K7 SWITCH SWRNGN SA227 SA227AC 8780603 SW PASSENGER DOOR FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 159MC AC728B FLT 3202 - ON CLIMB-OUT FROM MSP, THE CABIN DOOR ANNUNCIATOR LIGHT ILLUMINATED. AFTER THE CREW TURNED OFF THE BLEEDS AN D DEPRESSURIZED THE CABIN, THE LIGHT EXTINGUISHED. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE UPPER CENTER PASSENGER DOOR SWITCH. SYSTEM OPERATED SATISFACTORILY. (X) 2 L 7 2 4T RT A8SW 1996040500085 19960405 00085 SW 1996 4 5 MALA964848 1 19960130 A 3240 212033 BRAKEY SWRNGN SA227 SA227AC 8780603 SW LT/RT MLG WORN A MALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 15 425MA AC640 FLT 3045 - WHILE TAXIING IN DTW, CREW NOTED THE CAPTAIN'S BRAKES WERE SOFT AND NEEDED TO BE PUMPED IN ORDER TO OBTAIN BR AKE PRESSURE. MAINTENANCE REPLACED THE RT AND LT INBOARD AND OUTBOARD BRAKE ASSEMBLIES. AS A PRECAUTIONARY MEASURE, AL L FOUR BRAKES WERE ALSO BLED. SYSTEM OPERATED SATISFACTORILY. (X) 2 L 7 2 4T RT A8SW 1996040500086 19960405 00086 NM 1996 4 5 MALA964849 1 19960130 A 3230 10800113 UPLOCK ACTUATOR DHAV DHC8 DHC8102 2809003 NM RT MLG FAILED A MALA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 15 802MA 245 FLT 3421 - DURING APPROACH TO DTW, THE RT MAIN GEAR DOWN AND LOCKED GREEN LIGHT DID NOT ILLUMINATE WHEN GEAR SELECTED DO WN. THE CREW RECYCLED THE GEAR TWICE AND RECEIVED A GREEN LIGHT. THE AIRCRAFT CONTINUED TO DTW AND LANDED WITHOUT INCI DENT. MAINTENANCE PERSONNEL REPLACED THE RT MLG UPLOCK ACTUATOR. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 2 H 7 2 4T RT A13NM 1996040500087 19960405 00087 SW 1996 4 5 MALA964850 1 19960131 A 7712 TSC BRIDGE SWRNGN SA227 SA227AC 8780603 SW LT ENGINE MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 426MA AC645 FLT 3297 - AFTER DEPARTURE FROM MSP, CREW NOTED A FLUCTUATION IN THE LT ENGINE TORQUE INDICATION. THEY ELECTED TO RETU RN TO MSP AND THE ACFT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL CHANGED FROM NR 1 TO NR 2 TSC BRIDGE AND CLEANED THE LT TORQUE RING CANNON PLUG. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 2 L 7 2 4T RT A8SW 1996040500088 19960405 00088 NM 1996 4 5 MALA964851 1 19960129 A 3350 TRACK DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 831MA 339 DURING A PRE-FLIGHT INSPECTION IN DTW, THE CREW NOTED TWO FLOOR TRACK LIGHTS INOPERATIVE. MAINTENANCE PERSONNEL DEFERRE D THE SYSTEM UNDER MEL 33-13 (C). (X) 2 H 7 2 4T RT A13NM 1996040500089 19960405 00089 SW 1996 4 5 MALA964852 1 19960102 A 3260 1EN516 SWITCHES SWRNGN SA227 SA227AC 8780603 SW NLG FAILED A MALA O OTHER N FALSE WARNING CL CLIMB 1 GL 15 442MA AC725 FLT 3201 - ON CLIMB-OUT FROM YQT, THE NOSE GEAR CYCLED IN THE WHEELWELL AFTER GEAR RETRACTION. HOWEVER, THE GEAR INTRAN SIT LIGHT DID NOT ILLUMINATE WHILE THE GEAR WAS IN MOTION. THE CREW CYCLED THE GEAR AND THE PROBLEM CEASED. MAINTENANC E REPLACED THE NLG 'UP' POSITION AND LIMIT SWITCHES. SYSTEM OPERATED SATISFACTORILY. (X) 2 L 7 2 4T RT A8SW 1996040500090 19960405 00090 SW 1996 4 5 MALA964853 1 19960131 A 3230 2752000191192 TQ TUBE ARM SWRNGN SA227 SA227AC 8780603 SW NLG FAILED A MALA K NONE P NO WARNING INDICATION AP APPROACH 1 GL 15 428MA AC646 FLT 3017 - ON APPROACH TO DTW, THE NOSE GEAR DOWN AND LOCKED LIGHT FAILED TO ILLUMINATE. THE CREW CYCLED THE GEAR UNTIL A DOWN AND LOCKED INDICATION WAS RECEIVED. MAINTENANCE REPLACED THE NLG TORQUE TUBE ARM ASSY. SYSTEM OPERATED SATISFA CTORILY. (X) 2 L 7 2 4T RT A8SW 1996040500091 19960405 00091 SW 1996 4 5 MALA964854 1 19960202 A 3260 1EN516 SWITCH SWRNGN SA227 SA227AC 8780603 SW RT MLG FAILED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 26906 AC654B FLT 3342 - AFTER TAKEOFF FROM CWA, THE RT MAIN GEAR CONTINUED TO CYCLE IN THE GEAR WELL AFTER THE LANDING GEAR WAS RETRA CTED. THE CREW ELECTED TO RETURN TO CWA AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE R T MAIN GEAR UPLIMIT SWITCH. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 2 L 7 2 4T RT A8SW 1996040500092 19960405 00092 1996 4 5 MALA964855 4 19960202 A 3425 7003360941 AHRS COMPUTER DHAV DHC8 DHC8102 2809003 NM NR 2 FAILED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 819MA 251 FLT 3209 - AFTER DEPARTURE FROM MSP, THE NR 2 AHRS FAILED. THE CREW ELECTED TO RETURN TO MSP AND THE AIRCRAFT LANDED WI THOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE NR 2 AHRS COMPUTER AND REPAIRED A PIN IN THE AHRS COMPUTER CONNECTOR . ALL SYSTEMS OPERATED SATISFACTORILY. (X) 2 H 7 2 4T RT A13NM 1996040500093 19960405 00093 NM 1996 4 5 MALA964856 1 19960203 A 3350 6104781 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 826MA 330 FLT 3091 - DURING PRE-FLIGHT INSPECTION IN BMI, THE CREW NOTED THE EMERGENCY OVERHEAD LIGHTS WOULD NOT ILLUMINATE. MAIN TENANCE PERSONNEL REPLACED ALL SIX EMERGENCY LIGHT BATTERY PACKS. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 2 H 7 2 4T RT A13NM 1996040500094 19960405 00094 SW 1996 4 5 MALA964857 1 19960202 A 5270 DOOR WARNING SWRNGN SA227 SA227AC 8780603 SW CARGO COMPT ACTIVATED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 426MA AC645 FLT 3095 - AFTER DEPARTURE FROM DSM, THE CARGO DOOR WARNING LIGHT ILLUMINATED. THE CREW ELECTED TO RETURN TO DSM AND TH E AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL FUNCTIONALLY TESTED THE CARGO DOOR WARNING SYSTEM, BUT WERE U NABLE TO DUPLICATE THE DISCREPANCY. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 2 L 7 2 4T RT A8SW 1996040500095 19960405 00095 SW 1996 4 5 MALA964858 1 19960202 A 3260 1EN516 SWITCH SWRNGN SA227 SA227AC 8780603 SW LT MLG FAILED A MALA O OTHER N FALSE WARNING AP APPROACH 1 GL 15 446MA AC693 FLT 3214 - ON APPROACH TO MSP, THE LT GEAR INTRANSIT LIGHT FAILED TO ILLUMINATE DURING GEAR EXTENSION. ALL OTHER GEAR I NDICATIONS WERE NORMAL. MAINTENANCE REPLACED THE LT MLG UPLIMIT AND BOTH DOWNLOCK SWITCHES. SYSTEM OPERATED SATISFACTO RILY. (X) 2 L 7 2 4T RT A8SW 1996040500096 19960405 00096 SW 1996 4 5 MALA964859 1 19960204 A 2435 230790001 STARTER/GEN SWRNGN SA227 SA227AC 8780603 SW RT ENGINE FAILED A MALA O OTHER H B ELECT. POWER LOSS-50 PC SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 15 433MA AC714 FLT 3323 - DURING APPROACH TO MSP, THE LT AND RT BATTERY DISCONNECT, BATTERY FAULT, AND RT GENERATOR FAIL LIGHTS ILLUMIN ATED. THE CREW RESET ALL SWITCHES AND THE SYSTEM RETURNED TO NORMAL; HOWEVER, AT THAT TIME THEY NOTED AN ELECTRICAL SMO KE SMELL. THE ACFT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE RT STARTER/GENERAT OR AND SEVERAL CURRENT LIMITERS. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 2 L 7 2 4T RT A8SW 1996040500097 19960405 00097 SW 1996 4 5 MALA964860 1 19960203 A 3230 RETRACT MECH SWRNGN SA227 SA227AC 8780603 SW NLG LACK OF LUBE A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 439MA AC722 FLT 3242 - AFTER DEPARTURE FROM MSP, THE NOSE GEAR FAILED TO RETRACT WHEN THE GEAR WAS SELECTED UP. THE CREW EXTENDED T HE GEAR NORMALLY AND THE AIRCRAFT RETURNED TO MSP WITHOUT INCIDENT. MAINTENANCE PERSONNEL CLEANED AND LUBRICATED THE NL G ASSEMBLY. 2 L 7 2 4T RT A8SW 1996040500098 19960405 00098 WP 1996 4 5 ORJA96003 1 19960123 A 3350 41B004AD073 BATTERY EA1D13D3 DOUG DC9 DC987 3022087 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 EMERGENCY CEILING LIGHTING IN 1ST CLASS INOP. REPLACED BATTERY PACK AND OPS CHECKED GOOD. (X) 2 L 7 2 4F RT A6WE 1996040500099 19960405 00099 EU 1996 4 5 SIMA960331 1 19960202 A 3350 3011206 LIGHT AEROSP ATR42 ATR42300 8680920 EU EXTERIOR DEFECTIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 246AE 15887 269 243 RFD - DURING P5-2 CHECK, MAINTENANCE FOUND LT FORWARD EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REP LACED EMERGENCY LIGHT ASSY. EMERGENCY LIGHT SYSTEM OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1996040500100 19960405 00100 EU 1996 4 5 SIMA960401 1 19960209 A 5230 S5237663520400 LOCK PINS AEROSP ATR42 ATR42300 8680920 EU CARGO DOOR BROKEN A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 37AE 037 ORD - FLT 4067 - AFTER TAKEOFF, DOOR WARNING WENT OFF. RETURNED TO ORD FOUND PINS IN LEVER NR 1 BROKEN ON CARGO DOOR. R EPLACED LOCKING PINS. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1996040500101 19960405 00101 NE 1996 4 5 SIMA960521 2 19960221 A 7210 7758012 SHAFT 77590010 SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENG PGB DAMAGED A A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 314AE 12714 340B314 LAW - DURING INSPECTION OF RT ENGINE, POWER GEARBOX (PGB) PROPELLER SHAFT FOLLOWING PROPELLER REMOVAL, THE SHAFT FLANGE SHOWED EVIDENCE OF FRETTING IN AREA INBOARD OF MOUNTING BOLT HOLES. THIS DAMAGE TRAVELED 360 DEGREES AROUND FLANGE AREA AND APPEAR TO BE APPROX .035 INCH DEEP (MAX). THE PROPELLER HUB WAS INSPECTED, REVEALING EVIDENCE OF DAMAGE. THE PGB, PN 775900-10, SN UDAG071S, WAS REMOVED FROM SERVICE AND SENT TO VENDOR FOR TEAR DOWN AND REPAIRS. PART TOTAL CYCLES, 1 2,493. (X) 2 L 7 2 4T 4 T RT A52EU E8NE 1996040500102 19960405 00102 EU 1996 4 5 SIMA960542 1 19960223 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 414WF 234 414 DFW - FLT 3742 - EMERGENCY LIGHTS ON FLOOR LIGHTING STAYS ON CONTINUOUSLY. REPAIRED POWER SUPPLY AT 61WL. AIRCRAFT RET URNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1996040500103 19960405 00103 EU 1996 4 5 SIMA960551 1 19960224 A 7931 605T88601 OIL PRESS ALARM SAAB SF340 SF340A 7850100 EU NR 1 ENGINE ILLUMINATED A SIMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 21 114SB GEE367398 340A114 DFW - FLT 3573 - DURING TAKEOFF, NR 1 ENGINE OIL PRESSURE LOW LEVEL ALARM ILLUMINATED. TAKEOFF WAS ABORTED RESULTING IN NR 1 AND NR 2 TIRES DEFLATING DUE TO HIGH TEMPERATURE. REPAIRED ENGINE, CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. ( X) 2 L 7 2 4T RT A52EU 1996040500104 19960405 00104 EU 1996 4 5 SIMA960571 1 19960226 A 2720 7227200641 RUDDER CONSOLE SAAB SF340 340B 7860101 EU LT/RT CORROSION A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 587MA 14823 385 340B166 LAW - DURING THE EM-3 INSPECTION VISIT, BOTH THE LT AND RT RUDDER CONSOLE, PN 7227200-641, HAD EVIDENCE OF CORROSION ON 4 OF THE 6 ATTACH POINTS (BOLT HOLES) TO FLOOR STRUCTURE. BOTH CONSOLES REMOVED, FLOOR AREA INSPECTED, AND RUDDER CONSO LES REPLACED IAW AMM 27-21-05. PART TOTAL CYCLES, 14,159. (X) 2 L 7 2 4T RT A52EU 1996040500105 19960405 00105 WP 1996 4 5 SWIA96001 2 19960110 A 7250 31021069 TURBINE WHEEL SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP LT ENGINE DEFECTIVE A SWHA O OTHER O OTHER IN INSP/MAINT 1 SW 17 718C 465 AC572 P44202C FLT 432 - AT COMPLETION OF SCHEDULED FLIGHT, ON THE GROUND, PILOT SHUT DOWN LT ENGINE. THE FIRST OFFICER ATTEMPTED TO P ULL THE PROP BLADES THROUGH BY HAND TO FACILITATE COOLING OF THE ENGINE. THE PROP BLADES TURNED APPROXIMATELY 6 INCHES AND THE ENGINE SEIZED. THE PILOT REPORTED ALL ENGINE INDICATIONS TO BE NORMAL THROUGHOUT THE FLIGHT, LANDING, AND PRIOR TO SHUT DOWN. NORMAL COOL-DOWN PROCEDURES WERE FOLLOWED PRIOR TO SHUT DOWN. THE LT ENGINE WAS REMOVED AND REPLACED AN D THE AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T 4 T RT A8SW E4WE 1996040500106 19960405 00106 NE 1996 4 5 YIEA96001 2 19960118 A 7200 ENGINE AMD FALC20 FALCOND 2720304 EU GE CF700 CF7002D 30010 NE LEFT FLAME OUT A YIEA O OTHER X ENGINE FLAMEOUT CL CLIMB 1 GL 23 821AA 9597 5304 203 304016 PILOT REPORTED WHILE IN A STEADY STATE, CLIMB-OUT FOR FL 330 TO FL 370, LT ENGINE FLAMED OUT AT 34,300 FEET. ACFT FLYIN G AT .68 MACH. THERE WERE NO CLOUDS AND VERY LIGHT TURBULENCE. CREW DESCENDED AND RESTARTED ENGINE AT FL 290. ACFT CO NTINUED TO DESTINATION WITHOUT FURTHER INCIDENT. ENG GIVEN A THOROUGH INSPECTION OF INLET AND EXHAUST TO LOOK FOR EVIDE NCE OF FOD, BUT NONE WAS FOUND. ENG BORESCOPED WITH NO DISCREPANCIES NOTED. A FULL GROUND POWER RUN PERFORMED ON ENGIN E IAW WITH GE MM AND ALL PARAMETERS CHECKED WITHIN LIMITS. NO MECHANICAL CAUSE COULD BE FOUND FOR THE FLAME OUT. IT IS POSSIBLE LIGHT TURBULENCE OR CREW OPERATIONS MAY HAVE INDUCED FLAME OUT. ENG RETURNED TO SERVICE. (X) 2 L 7 2 4F 4 F A7EU E7EA 1996040500107 19960405 00107 WP 1996 4 5 9607069758 1 19960214 A 5720 CLIP DOUG DC9 DC941 302207N WP CENTER WING CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 758NW 47286 DURING SPECIAL MAINTENANCE VISIT, FOUND A CRACK IN THE CENTER WING STRINGER 11R CLIP AT RBL 42 AT THE REAR SPAR. REPLAC ED CLIP (P/N 4912014) PER EA 97-106790. 2 L 7 2 4F A6WE 1996040500108 19960405 00108 WP 1996 4 5 9607079875 1 19960315 A 5330 SKIN DOUG DC9 DC951 3022051 WP FS 1124 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 784NC 48109 DURING H-CHECK, FOUND TWO CRACKS, 1.25 INCH AND .25 INCH IN THE FUSELAGE SKIN AT FS 1124 BELOW LONGERON 14L. REPAIRED S KIN (P/N 5911427-3) PER EA 98-109449. 2 L 7 2 4F A6WE 1996040500109 19960405 00109 WP 1996 4 5 9607089930 1 19960318 A 5330 SKIN DOUG DC9 DC931 3022065 WP PAX DOOR JAMB CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 89S 47042 DURING LINE CHECK, FOUND A 2.25 INCH CRACK IN THE MAIN CABIN DOOR UPPER AFT DOOR JAMB CORNER SKIN AND DOUBLER. REPAIRED SKIN (P/N 591406-5) AND DOUBLER PER EA 99-99570. 2 L 7 2 4F A6WE 1996040500110 19960405 00110 WP 1996 4 5 9607099993 1 19960319 A 5330 SKIN DOUG DC9 DC931 3022065 WP PAX DOOR JAMB CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8986E 47402 DURING LINE CHECK, FOUND ONE CRACK EACH IN THE MAIN CABIN DOOR UPPER AFT DOOR JAMB CORNER SKIN .3 AND DOUBLER .25. REPA IRED SKIN (P/N 5911406-5) AND DOUBLER PER EA 99-104203. 2 L 7 2 4F A6WE 1996040500111 19960405 00111 WP 1996 4 5 9607109872 1 19960319 A 5330 SKIN DOUG DC9 DC951 3022051 WP PAX DOOR JAMB CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 781NC 48121 DURING LINE CHECK, FOUND A .3 INCH CRACK IN THE MAIN CABIN DOOR UPPER AFT DOOR JAMB CORNER SKIN AT THE DOOR STOP HOLE. R EPAIRED SKIN (P/N 5911406-5) PER EA 98-104202. 2 L 7 2 4F A6WE 1996040500112 19960405 00112 WP 1996 4 5 9607119950 1 19960320 A 5311 FRAME DOUG DC9 DC932 3022066 WP FS 917 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9346 47376 DURING H-CHECK, FOUND CORROSION ON THE FS 917 FRAME, UPPER FLANGE AT LONGERON 22L. REPAIRED FRAME (P/N 2777930-5) PER E A 99-109488. 2 L 7 2 4F A6WE 1996040500113 19960405 00113 NM 1996 4 5 9607125504 1 19960321 A 5320 FITTING BOEING 757 757251 1384970 NM BS 1383 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 504US 23193 DURING T-CHECK, FOUND CORROSION ON THE AFT CARGO THRESHOLD SUPPORT CASTING BS 1383. REPLACED FITTING. 2 L 7 2 4F RT A2NM 1996040500114 19960405 00114 WP 1996 4 5 9607139966 1 19960322 A 5320 FITTING DOUG DC9 DC931 3022065 WP FS 168 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9330 47138 DURING M-CHECK, FOUND CORROSION ON THE FS 168 FRAME TO LONGERON 18R ATTACH FITTING. REPLACED FITTING PER SRM 51-30. 2 L 7 2 4F A6WE 1996040500115 19960405 00115 WP 1996 4 5 9607149903 1 19960325 A 5320 FITTING DOUG DC9 DC931 3022065 WP FS 570 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 953N 47083 DURING H-CHECK, FOUND A CRACK IN THE LONGERON 30 SPLICE FITTING AT FS 570. REPLACED SPLICE PER SRM 51-30-2. 2 L 7 2 4F A6WE 1996040500116 19960405 00116 WP 1996 4 5 9607159106 1 19960223 A 7330 FUEL HEAT IND DOUG DC9 DC915 3022036 WP PWA JT8 JT8D7 52053 NE NR 2 ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 96S 47206 657348 NR 2 ENGINE FUEL HEAT INDICATOR ILLUMINATED MOMENTARILY ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETUR NED TO THE GATE. THE ENGINE WAS INSPECTED AND RUNUP. THE CONDITION COULD NOT BE DUPLICATED. 2 L 7 2 4F 4 F A6WE E2EA 1996040500117 19960405 00117 WP 1996 4 5 9607169956 1 19960328 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN CHAFED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 923RW 47183 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS BETWEEN ROWS 7 AND 12 INOPERATIVE. FOUND CHA FED WIRES INSIDE SIDEWALL AT ROW 12. REPAIRED WIRES AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996040500118 19960405 00118 NM 1996 4 5 DL72S960667 1 19960327 A 5754 65162249092 RIB BOEING 727 727232 1384082 NM NR 8 LE SLAT WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 469DA 20746 DURING INSPECTION, NR 8 L/E SLAT WAS FOUND WITH DAMAGED INTERNAL SUPPORT RIB. ACCOMPLISHED REPAIRS PER SRM 57-50-3. 2 L 7 3 4F A3WE 1996040500119 19960405 00119 NM 1996 4 5 DL72S960680 1 19960313 A 5754 65162249092 ANGLE BOEING 727 727232 1384082 NM NR 8 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 532DA 22045 A CRACK WAS FOUND 32.5 FROM I/B END ON LOWER AFT COVE SKIN ATTACH ANGLE BELOW ANTI-ICE DUCT. REPAIRED AS PER MM 57-54-0 FIG 805A, FOR NR 8 L/E SLAT. 2 L 7 3 4F A3WE 1996040500120 19960405 00120 NM 1996 4 5 DL72S960682 1 19960327 A 2761 FITTING BOEING 727 727225 1384077 NM NR 8 SPOILER ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 FOUND ON D-1 LETTER CHECK, .75 INCH CRACK IN RADIUS DOUBLER LOWER FWD SIDE OF NR 8 SPOILER ACTUATOR SUPPORT FITTING. FA STENERS LOOSE/MISSING AT LOWER FLANGE OF ITEM NR 1 DOUBLER. CRACK REPAIRED PER ERA 303369-14 M/M 57-20-22. REPLACED FA STENERS. 2 L 7 3 4F A3WE 1996040500121 19960405 00121 NM 1996 4 5 DL72S960683 1 19960327 A 5720 STIFFENER BOEING 727 727225 1384077 NM NR 3 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 FOUND ON D-1 LETTER CHECK, WING FRONT SPAR VERTICAL STIFFENER ANGLE CRACKED AT NR 3 SLAT O/B TRACK. REPAIRED PER M/M 57 -20-21 AND ERA NBR 303369-14. 2 L 7 3 4F A3WE 1996040500122 19960405 00122 NM 1996 4 5 DL72S960687 1 19960321 A 5754 651622296 SKIN BOEING 727 727232 1384082 NM NR 6 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 515DA 21431 INNER SKIN CRACKED BETWEEN RIB NR 9 AND NR 10. REPAIRED PER M/M 57-54-0, FOR NR 6 L/E SLAT. 2 L 7 3 4F A3WE 1996040500123 19960405 00123 NM 1996 4 5 DL72S960690 1 19960323 A 5312 BULKHEAD BOEING 727 727232 1384082 NM BS 870 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 470DA 20747 STA 870 BLKHD CRACKED AT RBL 10 JUST BELOW APU BLEED VALVE ON FWD SIDE APPROX 10. REPAIRED PER SRM 53-10-9 NR 09/010. 2 L 7 3 4F A3WE 1996040500124 19960405 00124 NM 1996 4 5 DL72W960698 1 19960227 A 7120 65187228 ENG MOUNT FTG BOEING 727 727247 138408F NM NR 3 ENGINE CRACKED A A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 290WA 22108 DURING ROUTING MAINTENANCE, NR 3 ENGINE WAS NOTICE TO BE LOOSE ON THE PYLON AND THE PYLON SEPARATED FROM THE FUSELAGE SK IN AT THE FORWARD ENGINE MOUNT AREA. THE ENGINE WAS REMOVED AND AREA INSPECTED. FOUND THE FORWARD ENGINE MOUNT FITTIN G AT FS 1183 COMPLETELY SEVERED. THE CRACK RAN VERTICALLY FROM THE TOP FLANGE TO THE BOTTOM FLANGE OF THE FITTING, APPR OXIMATELY 3 OUTBOARD OF THE FUSELAGE SKIN, INSIDE THE PYLON. THE AIRCRAFT WAS REMOVED FROM SERVICE FOR REPAIRS AND INVE STIGATION. A FLEET WIDE INSPECTION WAS IMMEDIATELY INITIATED TO VISUALLY INSPECT THE FORWARD ENGINE MOUNT FITTINGS. 2 L 7 3 4F A3WE 1996040500125 19960405 00125 NM 1996 4 5 DL73S960658 1 19960326 A 2560 WM15 BATTERY BOEING 737 737232 1384475 NM MEGAPHONE DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 305DL 23077 ON PREFLIGHT, FOUND AFT MEGAPHONE INOP. REPLACED BATTERIES, OPS CKS GOOD. 2 L 7 2 4F RT A16WE 1996040500126 19960405 00126 NE 1996 4 5 DL76L960679 2 19960327 A 7200 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 177DN 25122 724151 DUE TO HISTORY, NR 2 ENGINE WAS REMOVED FOR HIGH OIL CONSUMPTION AND ROUTED TO SHOP. 2 L 7 2 4F 4 F RT A1NM E24NE 1996040500127 19960405 00127 WP 1996 4 5 DLL14960676 1 19960327 A 3230 TRUCK POSITIONER LKHEED 1011 1011385115 5265015 WP LT GEAR FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 736DY 193C1227 AFTER TAKEOFF, GEAR HANDLE STUCK DOWN TRUCK LIGHT ON, OVERBD LIGHTS OUT. FLIGHT RETURNED ATL. REPLACED LT MLG TRUCK PO SITIONER AND SERVICED HYD FUSE, OPERATION NORMAL. 2 L 7 3 4F A23WE 1996040500128 19960405 00128 WP 1996 4 5 DLL17960674 1 19960327 A 3350 POWER SUPPLY LKHEED 1011 10113853 5265020 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 764DA 193H1202 D-ZONE RT EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY AND OPERATION NORMAL. 2 L 7 3 4F A23WE 1996040500129 19960405 00129 WP 1996 4 5 DLL17960675 1 19960327 A 3350 POWER SUPPLY LKHEED 1011 10113853 5265020 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 764DA 193H1202 EMERGENCY EXIT LIGHTS INOP FOR L-3 DOOR. REPLACED POWER SUPPLY. 2 L 7 3 4F A23WE 1996040500130 19960405 00130 NM 1996 4 5 P5CA9600168 1 19960120 A 3610 1896801 PRECOOLER MOUNT BOEING 747 747122 1384872 NM NR 3 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND NR 3 PRECOOLER LOWER AFT MOUNT CRACKED. REPAIRED AS PER MM 36-10-02. 2 L 7 4 4F A20WE 1996040500131 19960405 00131 NM 1996 4 5 P5CA9600169 1 19960120 A 7830 65B075511 CASCADE VANE BOEING 747 747122 1384872 NM NR 3 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND NR 3 ENGINE LEFT HAND UPPERMOST CASCADE VANE CRACKED. BLENDING CARRIED OUT AND VANE REINSTALLED AS PER MM 78-32-0 4. 2 L 7 4 4F A20WE 1996040500132 19960405 00132 NM 1996 4 5 P5CA9600170 1 19960118 A 7712 69B902623 MOUNT PLATE BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 4 TT2 SENSOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND NR 4 TT2 SENSOR MOUNT PLATES CRACKED. PLATES REPLACED ND SENSOR, REINSTALLED AS PER MM 73-21-04. LEAK CHECK SATI SFACTORY. 2 L 7 4 4F 4 F A20WE E20EA 1996040500133 19960405 00133 NM 1996 4 5 P5CA9600171 1 19960125 A 5411 WEB BOEING 747 747122 1384872 NM NR 4 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND NR 4 PYLON MIDSPAR WEB CRACKED AT APPROX NACELLE STA 205. WEB REPAIRED IAW SRM 54-10-03. 2 L 7 4 4F A20WE 1996040500134 19960405 00134 NM 1996 4 5 P5CA9600172 1 19960119 A 5520 WEIGHT BOEING 747 747122 1384872 NM RT ELEVATOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 BALANCE WEIGHT ON RT OUTBOARD ELEVATOR STA 306.8 HAD LEVEL 1 CORROSION. CORROSION REMOVED AND FOUND WITHIN LIMITS, REF SRM 51-20-03. 2 L 7 4 4F A20WE 1996040500135 19960405 00135 NM 1996 4 5 P5CA9600173 1 19960119 A 5520 WEIGHT BOEING 747 747122 1384872 NM LT ELEVATOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND LT OUTBOARD ELEVATOR WEIGHT AT STA 281.8 WITH LEVEL ONE CORROSION. REMOVED CORROSION, FOUND WITHIN LIMITS, REF SR M 51-20-03. 2 L 7 4 4F A20WE 1996040500136 19960405 00136 NM 1996 4 5 P5CA9600174 1 19960123 A 5730 PANEL BOEING 747 747122 1384872 NM LT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND OVERWING PANEL ABOVE REAR SPAR WBL 244.6 TO 277 FIXED T/E DELAMINATED. FIBERGLASS REPAIR CARRIED OUT IAW SRM 51-4 0-09. 2 L 7 4 4F A20WE 1996040500137 19960405 00137 NM 1996 4 5 P5CA9600175 1 19960120 A 5753 65B0207012 SKIN BOEING 747 747122 1384872 NM RT TE AFT FLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND RT INBOARD AFT FLAP DELAMINATED ON UPPER SKIN. REPAIRED IAW SRM 51-40-06. 2 L 7 4 4F A20WE 1996040500138 19960405 00138 NM 1996 4 5 P5CA9600176 1 19960118 A 5730 PANEL BOEING 747 747122 1384872 NM RT WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND FIBERGLASS PANEL FORWARD OF NR 8 SPOILER CRACKED AT WBL 353. REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996040500139 19960405 00139 NM 1996 4 5 P5CA9600177 1 19960118 A 5755 65B023001 SKIN BOEING 747 747122 1384872 NM NR 8 SPOILER DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND NR 8 SPOILER AFT EDGE DELAMINATED AT UPPER SKIN. REPAIRED IAW SRM 51-40-06. 2 L 7 4 4F A20WE 1996040500140 19960405 00140 NM 1996 4 5 P5CA9600178 1 19960119 A 5714 FRAME BOEING 747 747122 1384872 NM WS 570-590 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND CRACKED FRAME IN INBOARD LEADING EDGE BETWEEN STA 570 TO 590 AT LOWER CENTER POSITION. REPAIRED IAW SRM 51-40-03. 2 L 7 4 4F A20WE 1996040500141 19960405 00141 NM 1996 4 5 P5CA9600179 1 19960119 A 5730 65B116232 PANEL BOEING 747 747122 1384872 NM RT WING TE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND UPPER WING TRAILING EDGE PANEL CRACKED FORWARD OF NR 7 SPOILER. REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996040500142 19960405 00142 NM 1996 4 5 P5CA9600180 1 19960119 A 5730 65B116233 PANEL BOEING 747 747122 1384872 NM RT WING TE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND TRAILING EDGE FIXED PANEL CRACKED. REPAIRED AND REFITTED IAW SRM 57-30-O4. 2 L 7 4 4F A20WE 1996040500143 19960405 00143 NM 1996 4 5 P5CA9600181 1 19960118 A 5751 PANEL BOEING 747 747122 1384872 NM RT AILERON PUNCTURED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND OUTBOARD AILERON UPPER ACCESS PANEL PUNCTURED. REPAIRED AND REINSTALLED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996040500144 19960405 00144 NM 1996 4 5 P5CA9600182 1 19960122 A 5730 116353 PANEL BOEING 747 747122 1384872 NM LT WING BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND EDGE BROKEN ON UNDERWING REAR SPAR ACCESS PANEL. REPAIRED IAW SRM 51-40-09 AND REINSTALLED IAW MM 57-31-00. 2 L 7 4 4F A20WE 1996040500145 19960405 00145 NM 1996 4 5 P5CA9600184 1 19960122 A 5730 PANEL BOEING 747 747122 1384872 NM LT WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND UNDERWING PANEL FORWARD OF LANDING GEAR DELAMINATED AND CRACKED. REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996040500146 19960405 00146 NM 1996 4 5 P5CA9600185 1 19960121 A 5730 65B116199 PANEL BOEING 747 747122 1384872 NM LT WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND OVERWING PANEL LEFT WING CRACKED. PANEL REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996040500147 19960405 00147 NM 1996 4 5 P5CA9600186 1 19960118 A 5730 SKIN BOEING 747 747122 1384872 NM RT WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND UPPER WING SKIN WITH LEVEL ONE CORROSION AT WBL 520 CENTER SPAR AREA. CLEANED AND TREATED, FOUND WITHIN LIMITS OF 51-10-01. 2 L 7 4 4F A20WE 1996040500148 19960405 00148 NM 1996 4 5 P5CA9600187 1 19960119 A 5730 65B08170353 PANEL BOEING 747 747122 1384872 NM WS 1351 BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND UNDERWING PANEL AT STA 1351 BROKEN AT FORWARD EDGE. REPAIRED IAW SRM 51-40-09 AND REINSTALLED IAW MM 57-31-00. 2 L 7 4 4F A20WE 1996040500149 19960405 00149 NM 1996 4 5 P5CA9600188 1 19960119 A 5730 PANEL BOEING 747 747122 1384872 NM RT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND UPPER PANEL RIGHT WING DELAMINATED AFT OF NR 19 L/E FLAP. REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996040500150 19960405 00150 NM 1996 4 5 P5CA9600189 1 19960123 A 5230 DOOR BOEING 747 747122 1384872 NM AFT CARGO DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND CRACK ON AFT CARGO DOOR LEFT LOWER EDGE AT STA 1880. REPAIRED IAW SRM 52-00-03. 2 L 7 4 4F A20WE 1996040500151 19960405 00151 NM 1996 4 5 P5CA9600190 1 19960122 A 5280 STRUT DOOR BOEING 747 747122 1384872 NM LT WING GEAR DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND LEADING EDGE AREA OF LEFT WING GEAR UPPER STRUT DOOR DELAMINATED. REPAIRED IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1996040500152 19960405 00152 NM 1996 4 5 P5CA9600191 1 19960122 A 5280 DOOR BOEING 747 747122 1384872 NM LT WING GEAR DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND LEADING EDGE OF LEFT WING GEAR LOWER STRUT DOOR DELAMINATED. REPAIRED IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1996040500153 19960405 00153 NM 1996 4 5 P5CA9600192 1 19960122 A 5280 STRUT DOOR BOEING 747 747122 1384872 NM RT WING GEAR DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND RIGHT HAND WING GEAR LOWER STRUT DOOR LOWER EDGE DELAMINATED. REPAIRED IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1996040500154 19960405 00154 NM 1996 4 5 P5CA9600193 1 19960116 A 2612 65B9840613 BRACKET BOEING 747 747122 1384872 NM APU DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND LHS APU COWL DOOR FIRE DETECTOR BRACKET CRACKED. BRACKET REPLACED AND INSTALLED IAW MM 51-10-03. 2 L 7 4 4F A20WE 1996040500155 19960405 00155 NM 1996 4 5 P5CA9600194 1 19960119 A 4900 BRACKET BOEING 747 747122 1384872 NM APU COMPT CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND APU COMPARTMENT BRACKETS AT BS 2710 TO 2716 CRACKED. REPLACED BRACKET IAW MM 51-10-03. 2 L 7 4 4F A20WE 1996040500156 19960405 00156 NM 1996 4 5 P5CA9600195 1 19960119 A 3810 2XT0019 MOUNTING RING BOEING 747 747122 1384872 NM WATER TANK DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND MOUNTING RING FOR POTABLE WATER TANK DAMAGED. REPAIRED IAW SRM 38-10-01. 2 L 7 4 4F A20WE 1996040500157 19960405 00157 NM 1996 4 5 P5CA9600196 1 19960119 A 3810 65B547259 STRUT BOEING 747 747122 1384872 NM WATER TANK BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND LOWER HORIZONTAL STRUT FOR POTABLE WATER TANK BROKEN. NEW STRUT INSTALLED IAW IPC 38-11-02. 2 L 7 4 4F A20WE 1996040500158 19960405 00158 NM 1996 4 5 P5CA9600197 1 19960123 A 5532 321C LE SKIN BOEING 747 747122 1384872 NM VERTICAL FIN DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND LOWER VERTICAL FIN LEADING EDGE SKIN DENTED AT STA 124 AND STA 220. REPAIRED IAW SRM 51-40-06 AND REINSTALLED IAW MM 55-30-03. 2 L 7 4 4F A20WE 1996040500159 19960405 00159 NM 1996 4 5 P5CA9600198 1 19960120 A 5532 PANEL BOEING 747 747122 1384872 NM VERT FIN PUNCTURED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND VERTICAL FIN ACCESS PANEL PUNCTURED. REPAIRED IAW SRM 51-40-06 AND REINSTALLED IAW MM 53-30-10. 2 L 7 4 4F A20WE 1996040500160 19960405 00160 NM 1996 4 5 P5CA9600199 1 19960127 A 5753 FAIRING BOEING 747 747122 1384872 NM NR 4 TE FLAP PUNCTURED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND NR 4 CANOE FAIRING PUNCTURED. REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996040500161 19960405 00161 NM 1996 4 5 P5CA9600200 1 19960119 A 5753 FAIRING BOEING 747 747122 1384872 NM NR 1 TE FLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND NR 1 T/E FLAP TRACK MOVEABLE CANOE FAIRING CRACKED AT TWO LOCATIONS. REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996040500162 19960405 00162 NM 1996 4 5 P5CA9600201 1 19960119 A 5280 65B9082241 DOOR BOEING 747 747122 1384872 NM NR 2 AFT FAIRING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND NR 2 AFT FAIRING DOOR DELAMINATED. REPAIRED IAW SRM 51-40-06 AND REINSTALLED IAW MM 54-32-01. 2 L 7 4 4F A20WE 1996040500163 19960405 00163 NM 1996 4 5 P5CA9600202 1 19960319 A 3350 6016123 LIGHT BOEING 747 747122 1384872 NM CABIN INOPERATIVE A P5CA K NONE L NO TEST IN INSP/MAINT 1 WP 23 853FT 19753 FOUND CREW SERVICE DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED IAW MM 33-51-00. 2 L 7 4 4F A20WE 1996040500164 19960405 00164 EU 1996 4 5 QXEA9600135 1 19960328 A 3350 MGG1280 BULB FOKKER F28 F28MK1000 4990808 EU ROW 8 FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 468US 11095 EMERGENCY EXIT SIGN AT ROW 8 IS INOP ON AFT SIDE 28V. BULBS WERE REPLACED AND SIGN OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996040500165 19960405 00165 EU 1996 4 5 QXEA9600136 1 19960328 A 2560 D31697101 SLIDE FOKKER F28 F28MK1000 4990808 EU GALLEY DOOR DISCONNECTED A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 452US 11105 EMERGENCY EXIT SLIDE WILL NOT OPERATE CORRECTLY. SLIDE BECAME DISCONNECTED FROM DOOR. SLIDE REATTACHED I/A/W MAINT MAN UAL AND SLIDE INSTALLATION CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996040500166 19960405 00166 CE 1996 4 5 96ZZZX1446 1 19960216 A 2770 BOLT BEECH 1900 1900C 1154161 CE GUST LOCK JAMMED A A GUUA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 7243R UB24 MIA/NAS - FLT 429 - PILOT REPORT: SHORTLY AFTER TAKEOFF, EXPERIENCED EXTREME DIFFICULTY CONTROLLING THE ACFT PITCH ATTI TUDE. CREW DECLARED AN EMERGENCY, RETURNED TO MIA AND LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED CO NTROL COLUMN, DETERMINED A BOLT TO BE INSTALLED IN THE GUST LOCK. REMOVED BOLT, INSPECTED CONTROL COLUMN FOR DAMAGE AND FREEDOM OF MOVEMENT. NO DEFECTS NOTED. AIRCRAFT RELEASED. 2 L 7 2 4T RT A24CE 1996040500167 19960405 00167 SO 1996 4 5 96ZZZX1447 1 19960213 A 5330 1159B21311 SKIN GULSTM G1159 G1159 3953505 SO FS 598 CHAFED A KKYA K NONE O OTHER IN INSP/MAINT 1 NE 03 220FL 50 DURING AN 18-MONTH INSPECTION OF THE LEFT PYLON, THE FUSELAGE SKIN AT STA 598 WAS FOUND CHAFED BEYOND LIMITS. CHAFE WAS REPAIRED WITH GULFSTREAM DRAWINGS E35102164. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A12EA 1996040500168 19960405 00168 SW 1996 4 5 96ZZZX1448 1 19960207 A 2910 27810322682 HYD LINE FRCHLD SA227 SA227DC 3377521 SW LT ENGINE LEAKING A EQGA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SW 19 847LS DC847B JBR/ELD - WHILE EN ROUTE, AIRCRAFT LOST ALL HYDRAULIC PRESSURE. THE PILOT DIVERTED TO HOT AND LANDED WITHOUT FURTHER IN CIDENT. ON INSPECTION, MAINTENANCE FOUND THE LT MAIN PRESSURE LINE FROM THE HYDRAULIC PUMP TO THE FIREWALL HAD A HOLE I N IT AT A BEND. THE LINE WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1 L 7 2 4T RT A18SW 1996040500169 19960405 00169 SW 1996 4 5 96ZZZX1449 1 19960206 A 2910 27810322682 HYD LINE FRCHLD SA227 SA227DC 3377521 SW RT ENGINE LEAKING A EQGA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 19 847LS 5050 DC847B DURING PRE-FLIGHT, PILOT NOTICED A LARGE PUDDLE OF HYDRAULIC FLUID UNDER THE RT ENGINE AND VERY LITTLE FLUID IN THE SIGH T GLASS. THE PILOT WAS INSTRUCTED TO FERRY ACFT TO HOT FROM RUI WITH THE GEAR DOWN AND FLAPS UP. ON ARRIVAL AT HOT, MA IN PRESSURE LINE FROM THE HYDRAULIC PUMP TO THE ENGINE FIREWALL WAS FOUND LEAKING AT THE FLARE. THE LINE WAS CHANGED AN D THE AIRCRAFT WAS RETURNED TO SERVICE. 1 L 7 2 4T RT A18SW 1996040500170 19960405 00170 EU 1996 4 5 96ZZZX1450 1 19960116 A 3210 200633203 TORQUE LINK ROTOL 200739004 FOKKER F28 F28MK4000 4990810 EU RT MAIN GEAR FRACTURED A A21A K NONE O OTHER LD LANDING 1 WP 17 498US 2060 XC91551 11181 LAS - LOWER TORQUE LINK FAILED CAUSING INNER CYLINDER TO TURN 90 DEGREES AND SUBSEQUENT TIRE FAILURES. UPON LANDING AT LAS, RT LOWER MLG TORQUE LINK FAILED. REMOVED AND REPLACED RT MLG ASSY. 2 L 7 2 4F RT A20EU 1996040500171 19960405 00171 WP 1996 4 5 96ZZZX1451 1 19960223 A 3260 DNLOCK SW DOUG DC9 DC932 3022066 WP LT MLG MALFUNCTIONED A VJ6A K NONE P NO WARNING INDICATION LD LANDING 1 SO 11 902VV 47177 BOS/RDU - FLT 361 - NO GREEN LIGHT ON LEFT MAIN GEAR WHEN LOWERED IN RDU. APPROPRIATE PROCEDURES WERE FOLLOWED AND EVE NTUALLY LIGHT CAME ON STEADY. GEAR PINNED FOR TAXI. INSPECTED AND PINNED GEAR DOWN AND LOCKED FOR MAINTENANCE FERRY TO 31J. REPAIRED LEFT MLG DOWN AND LOCKED SWITCH AND CANNON PLUG, OPS CHECK GOOD IAW DC-9 MM 20-50-1 AND MM 32-30-1. 2 L 7 2 4F A6WE 1996040500172 19960405 00172 WP 1996 4 5 96ZZZX1452 1 19960216 A 3260 DS0775059 CONNECTOR DOUG DC9 DC932 3022066 WP NLG LOOSE A VJ6A O OTHER P NO WARNING INDICATION AP APPROACH 1 SO 11 906VJ 47379 BOS/PBI - FLT 395 - UPON GEAR EXTENSION, NEITHER RED UNSAFE NOR GREEN SAFE LIGHT ILLUMINATED FOR NOSE GEAR. FOUND A NOS E GEAR POSITION SWITCH CONNECTOR LOOSE. CANNON PLUG WOULD NOT LOCK. INSTALLED NEW PLUG PER MM 32-60-1, PAGES 20-23A. O PS CHECK GOOD. 2 L 7 2 4F A6WE 1996040500173 19960405 00173 1996 4 5 96ZZZX1453 4 19960217 A 3454 CONNECTOR DOUG DC9 DC932 3022066 WP VHF NAV ANTENNA LOOSE A VJ6A A UNSCHED LANDING O OTHER CL CLIMB 1 SO 11 966VV 47168 ATL/ATL - FLT 166 - AIR RETURN, BOTH VHF NAVS INOP ON ALL FREQUENCIES. FOUND BOTH ANTENNA CONNECTIONS LOOSE. RECONNECT ED, CHECKED BOTH NAV SYSTEMS WITH TIC 30, OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996040500174 19960405 00174 NM 1996 4 5 96ZZZX1454 1 19960301 A 3260 CM6829 BULB DORNER DO32 DO328100 2996000 NM LT MLG FAILED A VNAA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 07 440JS 3058 RIC - FLT 4177 - ON APPROACH AFTER SELECTING GEAR 'DOWN' CREW REPORTED NO GEAR DOWN AND LOCKED INDICATION FOR THE LEFT M LG. CREW CONDUCTED A TOWER FLY-BY TO CONFIRM GEAR DOWN. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. ONCE ON THE GROUND, OUT-STATION MAINTENANCE REPLACED BULBS IN THE LANDING GEAR POSITION INDICATOR IAW MM 32-00-00. GROUND CHECKED GOOD, AI RCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A45NM 1996040500175 19960405 00175 NM 1996 4 5 96ZZZX1455 1 19960227 A 5610 DO328131 WINDSHIELD DORNER DO32 DO328100 2996000 NM RT COCKPIT DAMAGED A A VNAA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 07 440JS 3058 PIT/EVV - FLT 4022 - AT CRUISE FL 220, CREW REPORTED HEARING A LOUD NOISE FOLLOWED BY THE FIRST OFFICER'S WINDSHIELD CRA CKING. AIRCRAFT DIVERTED TO DAY AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT WAS LATER FERRIED TO PIT WHERE MAIN TENANCE REPLACED THE FIRST OFFICER'S FRONT WINDSHIELD IAW MM 56-11-00. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A45NM 1996040500176 19960405 00176 1996 4 5 96ZZZX1456 4 19960226 A 3417 7014700011 AIR DATA COMP HONEYWELL DORNER DO32 DO328100 2996000 NM NR 1 DEFECTIVE A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 442JS 95040452 3060 PIT - FLT 4083 - ON CLIMB-OUT, CREW WAS ALERTED BY A CAS MESSAGE ADC 1 FAIL. CREW ELECTED TO RETURN TO FIELD, AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. PIT MAINTENANCE AIR DATA COMPUTER IAW MM 34-11-01. GROUND CHECKED GOOD, AIRCRAFT RETU RNED TO SERVICE. 2 H 7 2 4T RT A45NM 1996040500177 19960405 00177 CE 1996 4 5 96ZZZX1457 1 19960208 A 2450 ELB1728211PL CONNECTOR 60184075 LEAR 60 60LEAR 5170707 CE LT SIDE GCP INOPERATIVE A OICA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 09 799SC 35 067 STABILIZER HEAT LIGHT ON, STAB HEAT CONFIRMED INOPERATIVE. P745 ON GENERATOR CONTROL PANEL FOUND TO BE MAKING POOR CONT ACT. THE HEAVY (NR 10) WIRE ON THIS PLUG TENDS TO 'TIP' THE UPPER PORTION AFT CAUSING LOSS OF CONTACT ON THE SHORT PINS IN THIS PLUG. WHEN THIS PLUG WAS RECONNECTED, NR 2 RT BUS FEED WAS LOST. PROBLEM CORRECTED BY LEARJET, WICHITA CRS LJ 9R810J, BY REPLACING PN ELB-1728-211PL. SUBMITTER STATED THIS PLUG SHOULD BE RE-PINNED OR REPLACED USING LONGER PINS TO GIVE ADEQUATE PIN TO SOCKET CONTACT. 2 L 7 2 4F RT A10CE 1996040500178 19960405 00178 EA 1996 4 5 96ZZZX1458 2 19960208 A 7314 3033808A HP FUEL PUMP BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA RT ENGINE FAILED A GLBA C E A ABORTED TAKEOFF ENGINE SHUTDOWN UNSCHED LANDING Y ENGINE STOPPAGE TO TAKEOFF 1 CE 01 60UE 11722 UC60 PS32354 RIGHT ENGINE TORQUE FLUCTUATES ON TAKEOFF. PRECAUTIONARY SHUT DOWN OF RIGHT ENGINE WAS ACCOMPLISHED. MAINTENANCE REPLA CED THE PROPELLER GOVERNOR, FUEL CONTROL UNIT, AND HIGH PRESSURE PUMP (FUEL). PROPELLER GOVERNOR DID NOT FIX PROBLEM, B UT REMAINS INSTALLED ON AIRCRAFT. RII ITEMS C/W. AIRCRAFT RETURNED TO SERVICE. REFERENCE OPERATOR CONTROL NR GLBA9600 5. 2 L 7 2 4T 4 T RT A24CE E4EA 1996040500180 19960405 00180 NM 1996 4 5 AALA960265 1 19960214 A 3350 LIGHT STRIP BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 602AN 27053 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT MID-GALLEY AREA FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIG HT STRIP AT MID-GALLEY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1996040500181 19960405 00181 EU 1996 4 5 AALA960275 1 19960219 A 3231 715391 VALVE FOKKER F28 F28MK0100 4990807 EU NLG DOOR DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 1446A 714G 11449 DFW - FLT T1098 - AFTER TAKEOFF DFW WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR DID NOT RETRACT. AIRCRAFT RETURNED T O DFW AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR DOOR SELECTOR VALVE. ACCOMPLISHED NLG RETRACTION CHECK W ITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT 1996040500182 19960405 00182 SO 1996 4 5 ASOA96004 1 19960220 A 5230 12023348005 SEAL EMB 120 EMB120RT SO CARGO DOOR DEFECTIVE A ASOA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 11 274AS 120229 CRW/ATL - INBOUND, LOST CABIN PRESSURIZATION AT 20,000 FEET. CREW TRIED MANUAL PRESSURIZATION, IT DID NOT WORK. PERFOR MED AN EMERGENCY DESCENT. PASSENGER OXYGEN MASKS DID NOT DEPLOY, HOWEVER, GOT CABIN ALTITUDE LIGHT AND AURAL WARNING. L ANDED SAFELY AND WITHOUT INCIDENT IN ATL. REMOVED AND REPLACED CARGO DOOR SEAL. OPERATIONAL AND LEAK CHECKS WERE GOOD. INSPECTED PASSENGER OXYGEN MASKS, ALL MASKS DEPLOYED ON TEST. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1996040500183 19960405 00183 NE 1996 4 5 C1HA960011 2 19960309 A 7200 ENGINE DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3B 52039 NE NR 1 MALFUNCTIONED A C1HA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 23 802MG 46098 671331 DURING TAKEOFF ROLLOUT AT APPROX 70 KTS, NOTED EPR DROP ON NR 1 ENGINE, FELT A SLIGHT YAW AT THE SAME TIME. ELECTED TO REJECT TAKEOFF COMPLETED THE SAME WITHOUT INCIDENT. INSPECTED NR 1 EPR IND. FOUND NO DEFECTS PERFORMED 1.84 POWER SETT ING ON NR 1 AND NR 4 ENGINES, NO DEFECTS NOTED AT THIS TIME. RELEASED AIRCRAFT FOR FLIGHT. (M) 2 L 7 4 4F 4 F 4A25 1E8 1996040500184 19960405 00184 NM 1996 4 5 CAL960208 1 19960227 A 8011 35057165 STARTER BOEING 737 737524 1384721 NM NR 2 ENGINE FAILED A CALA K NONE O OTHER TX TAXI/GRND HDL 1 SW 09 59630 2358 27534 SNA - FLT 1516 - THE NR 2 ENGINE WOULD NOT ROTATE ON START AND THE CREW REPORTED A MINOR EXPLOSION. INSPECTION OF THE N R 2 ENGINE REVEALED AN UNCONTAINED STARTER FAILURE WITH RESULTANT DAMAGE TO THE LT FAN COWL, NOSE COWL, AND CSD. THE NR 2 ENGINE STARTER WAS REPLACED IAW MM 80-11-01. THE DAMAGED CSD, LT FAN COWL, AND NOSE COWL WERE REMOVED AND REPLACED. IN ADDITION, THE CSD OIL COOLER AND STARTER SHUT-OFF VALVE WERE REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. THE N R 2 ENGINE WAS RUN AND OPERATION CHECKED GOOD. (X) 2 L 7 2 4F RT A16WE 1996040500185 19960405 00185 WP 1996 4 5 DLSP96001 1 19960216 A 5330 SKIN LKHEED 1011 10113851 5265010 WP FS 1363 CRACKED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 311EA 193A1012 ATL - DURING CONTRACT MAINTENANCE AT DALA, THE FUSELAGE SKIN AT FS 1363 IS CRACKED IN THE TYPICAL MANNER DEPICTED IN SRM 53-11-00, FIGURE 826, REPAIR. THE CRACK IS APPROXIMATELY 2.25 INCHES LONG, LOCATED BETWEEN STR 21 AND STR 22. THE SUB JECT CRACK WAS PREVIOUSLY REPAIRED PER SRM 53-11-00, FIGURE 823. UPON REMOVAL OF THE EXISTING REPAIR FOR ACCOMPLISHMENT OF LAC SB 093-53-207, TWO ADDITIONAL CRACKS WERE FOUND IN THE SKIN UNDER THE STR 21 END FITTING. THE .75 INCH CRACKS R UN FROM THE FWD SKIN TO BULKHEAD CAP FASTENER HOLES TO THE FWD SKIN EDGE. ACCOMPLISHED REPAIRS PER DL ERA 273284-14AD. ACFT TT: 40,336 HRS. ACFT TOTAL CYCLES: 19,734. (X) 2 L 7 3 4F A23WE 1996040500186 19960405 00186 WP 1996 4 5 DLSP96002 1 19960216 A 5330 SKIN LKHEED 1011 10113851 5265010 WP FS 1363 CRACKED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 311EA 193A1012 ATL - DURING CONTRACT MAINTENANCE WITH DALA, FOUND FUSELAGE SKIN AT FS 1363 CRACKED IN THE TYPICAL MANNER DEPICTED IN TH E L1011 SRM 53-11-00, FIGURE 826, REPAIR. THE SUBJECT CRACK IS APPROXIMATELY 12 INCHES IN LENGTH AND HAD BEEN PREVIOUSL Y REPAIRED PER SRM 53-11-00, FIGURE 826. UPON REMOVAL OF THE EXISTING REPAIR FOR ACCOMPLISHMENT OF LAC SB 093-53-207, T HE CRACK WAS FOUND TO HAVE PROGRESSED FWD BEYOND THE ORIGINAL STOP-DRILL HOLE TO THE SKIN EDGE. ACCOMPLISHED REPAIRS PE R DL ERA 273285-14AD. ACFT TT: 40,336 HRS. ACFT TOTAL CYCLES: 19,734 (X) 2 L 7 3 4F A23WE 1996040500187 19960405 00187 WP 1996 4 5 DLSP96003 1 19960216 A 5320 1634985 ANGLE LKHEED 1011 10113851 5265010 WP WING/FUS ATTACH OVERSIZE HOLES A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 311EA 193A1012 ATL - DURING CONTRACT MAINTENANCE AT DALA, C/W AD 94-05-01, REPLACEMENT OF FUSELAGE LT AND RT WING TO FUSELAGE AT TACH U PPER ROOT JOINT FAIL-SAFE ANGLE, SEVERAL HOLES WERE FOUND OVERSIZED AND OUT-OF-ROUND. REAMED HOLES TO A ROUND CONDITION PER DL ERA 273277-14AD. ACFT 40,336 HRS. ACFT TOTAL CYCLES, 19,734. (X) 2 L 7 3 4F A23WE 1996040500188 19960405 00188 WP 1996 4 5 DLSP96004 1 19960216 A 5330 SKIN LKHEED 1011 10113851 5265010 WP FS 1363 CRACKED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 311EA 193A1012 ATL - DURING CONTRACT MAINTENANCE AT DALA, THE FUSELAGE SKIN WAS FOUND WITH AN APPROXIMATE 1 INCH LONG CRACK RUNNING HOR IZONTALLY FROM THE FORWARD EDGE OF THE SKIN AT FS 1363 LOCATED MIDWAY BETWEEN STR 18 AND STR 19. THE CRACK IS SIMILAR T O THOSE ADDRESSED IN THE SRM 53-11-00 REPAIRS, BUT AT DIFFERENT STRINGER LOCATIONS. THE STRUCTURAL MODIFICATION PER LAC SB 093-53-207 IS CURRENTLY BEING ACCOMPLISHED ON THE AIRCRAFT. ACCOMPLISHED REPAIRS PER DL ERA 273286-14AD. ACFT TT: 40,336 HRS. ACFT TOTAL CYCLES, 19,734. (X) 2 L 7 3 4F A23WE 1996040500189 19960405 00189 CE 1996 4 5 GLBA96004 1 19960205 A 3260 WARNING SYSTEM BEECH 1900 1900C 1154161 CE LANDING GEAR ACTIVATED A GLBA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 01 122GL UC122 UC-122 HAD FLAPS IN TAKEOFF POSITION, GEAR DOWN AND LOCKED WITH 3 GREEN INDICATED. THE RED LIGHTS ILLUMINATED IN THE GE AR HANDLE AND AURAL WARNING SOUNDED. THE AIRCRAFT WAS FERRIED TO SPI FROM ORD FOR REPAIRS. THE GEAR SWING COMPLETED IN SPI REVEALED NO DUPLICATE PROBLEMS. (X) 2 L 7 2 4T RT A24CE 1996040500190 19960405 00190 EA 1996 4 5 GLBA96005 2 19960208 A 7321 8061328 FCU BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA RT ENGINE FAILED A GLBA C E A ABORTED TAKEOFF ENGINE SHUTDOWN UNSCHED LANDING Y ENGINE STOPPAGE TO TAKEOFF 1 CE 01 60UE 10133 592 UC60 PS32354 RIGHT ENGINE TORQUE FLUCTUATES ON TAKEOFF. PRECAUTIONARY SHUT DOWN OF RIGHT ENGINE WAS ACCOMPLISHED. MAINTENANCE REPLA CED THE PROPELLER GOVERNOR, FUEL CONTROL UNIT, AND HIGH PRESSURE PUMP (FUEL). PROPELLER GOVERNOR DID NOT FIX PROBLEM, B UT REMAINS INSTALLED ON AIRCRAFT. RII ITEMS C/W. AIRCRAFT RETURNED TO SERVICE. REFERENCE OPERATOR CONTROL NR 96ZZZX14 58. (X) 2 L 7 2 4T 4 T RT A24CE E4EA 1996040500191 19960405 00191 NM 1996 4 5 P91A096004 1 19960215 A 2520 INSULATION BOEING 727 727231 1384079 NM RT OUTFLOW VALVE LOOSE A P9IA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 03 12305 63829 19562 REFERENCE LOG PAGE 0153 - AIRCRAFT WOULD NOT PRESSURIZE NORMALLY AFTER TAKEOFF IN NORMAL OR MANUAL. ALL PRESS AND TEMPS IN PACKS SHOWED OK. REMOVED INSULATION IN RT OUTFLOW VALVE POS. (X) 2 L 7 3 4F A3WE 1996040500192 19960405 00192 EU 1996 4 5 PLG11696E1 1 19960112 A 3020 INTAKE HEAT SAAB SF340 SF340A 7850100 EU LT ENGINE FAILED A PLGA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NE 05 749BA 340A152 BDL/YYZ - FLT 4833 - DURING FLIGHT, NOTED THE LEFT INTAKE HEAT FAILED. DUE TO EXISTING WEATHER CONDITIONS, THE AIRCRAFT DIVERTED INTO ALB. MAINTENANCE CLEANED MOISTURE FROM LOAD MONITOR CONNECTIONS AND RAN INTAKE HEAT SYSTEM. NO DEECTS N OTED. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1996040500193 19960405 00193 CE 1996 4 5 PLG11696E2 1 19960114 A 7120 12991003279 TRUSS BEECH 1900 1900C 1154161 CE RT ENGINE CRACKED A PLGA K NONE O OTHER IN INSP/MAINT 1 NE 05 823BE UB66 WHILE PERFORMING AD 95-02-18, AND 39-9136, BEECH SB 2255, REVISION 6, THE RT ENGINE TRUSS WAS FOUND CRACKED. THE CRACK WAS APPROXIMATELY .25 INCH IN LENGTH AT THE TRAILING EDGE OF THE UPPER INBOARD GUSSET. THE TRUSS WAS REPAIRED IAW BEECH SB 2255 AND BEECH KIT 114-9033-1S INSTRUCTIONS. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1996040500194 19960405 00194 CE 1996 4 5 PLG62996E1 1 19960209 A 5210 1144000301 SEAL BEECH 1900 1900C 1154161 CE PASSENGER DOOR DEFORMED A PLGA A UNSCHED LANDING O OTHER CR CRUISE 1 NE 05 15394 UC63 SDR CONTROL NR PLG62996E1 FOR FLT 4693 IS BEING CLOSED OUT WITH THE REMOVAL AND REPLACEMENT OF THE MAIN CABIN DOOR SEAL. THE OPERATIONAL CHECK OF THE PRESSURIZATION SYSTEM WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1996040500195 19960405 00195 EU 1996 4 5 RAIA960221 1 19960217 A 7603 91SE16 COND LEVER SW JETAIR JETSTM JETSTM4101 1500501 EU RIGHT OUT OF ADJUST A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 562HK 141 41078 JFK - FLT 7729 - TOCW WARNING ILLUMINATED DURING TAKEOFF. MAINTENANCE ADJUSTED RIGHT CONDITION LEVER MICROSWITCH, OPERA TION CHECK GOOD. (X) 2 L 7 2 4T RT A41NM 1996040500199 19960405 00199 EU 1996 4 5 REXA96001 1 19960116 A 3297 M2275916229 WIRE BAG JETSTM JETSTM3101 1500215 EU LANDING GEAR LOOSE A REXA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 302PX 661 MEM - FLT 5161 - GEAR DID NOT EXTEND WHEN SELECTED DOWN UPON APPROACH TO MEM. EMERGENCY EXTENSION PRODUCED 3 DOWN AND L OCKED. FOUND AND TIGHTENED LOOSE WIRE AT TERMINAL TIAC POSITION NR 6. GEAR SWUNG IAW AMM. ACFT RETURNED TO SERVICE. ( X) 2 L 7 2 4T RT A21EU 1996040500200 19960405 00200 GL 1996 4 5 REXA96002 3 19960126 A 6110 750350AF O-RING BAG JETSTM JETSTM3101 1500215 EU ROTOL R333 R333482F12 GL PROP PISTON FAILED A REXA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 25 318PX 18207 759 689 DRG401485 FLT 5827 - DIFFICULTY CLOSING FLOWS FOR LANDING CHECKLIST AND SMOKE FILLED CABIN. AFTER LANDING, PERFORMED EMERGENCY EV ACUATION. PROPELLER DOME O-RING HAD FAILED AND RESULTANT OIL LEAK ALLOWED OIL TO ENTER ENGINE INTAKE AND CONTAMINATE BL EED AIR TO CABIN. INSTALLED NEW O-RING AND RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A21EU 6 C P61GL 1996040500201 19960405 00201 EU 1996 4 5 REXA96005 1 19960211 A 2910 P240606040146R HYD LINE SAAB SF340 SF340A 7850100 EU LT MLG BROKEN A REXA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 324PX 340A048 HYDRAULIC LINE BROKEN ON LT MLG. REMOVED AND REPLACED LT MLG RETRACTION JACK LINE IAW SAAB AMM. SERVICED HYD QTY. OK FOR SERVICE. (X) 2 L 7 2 4T RT A52EU 1996040500202 19960405 00202 EU 1996 4 5 REXA96007 1 19960217 A 3240 189422 CLEVIS ASSEMBLY SAAB SF340 340B 7860101 EU LT BRAKE PEDAL BROKEN A REXA K NONE O OTHER TX TAXI/GRND HDL 1 SO 25 366PX 11214 340B267 CAPTAIN'S LEFT BRAKE RUDDER PEDAL BROKE. REMOVED AND REPLACED CAPTAIN'S LEFT FOOT PEDAL BRAKE CABLE ASSY IAW AMM CHAPTE R 32. (X) 2 L 7 2 4T RT A52EU 1996040500203 19960405 00203 EU 1996 4 5 REXA96008 1 19960218 A 2910 L387105A HYD SWIVEL 671102 SAAB SF340 SF340A 7850100 EU MLG BROKEN A REXA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 935MA 49 340A073 HYDRAULIC 'CAP' AFTER TAKEOFF. HYDRAULIC FLUID 'LOW PRESS' IN MAIN ACCUMULATOR DROPPED. REMOVED AND REPLACED UPLOCK HY DRAULIC SWIVEL, RT IAW AMM 32. NO LEAKS NOTED. (X) 2 L 7 2 4T RT A52EU 1996040500204 19960405 00204 EU 1996 4 5 REXA96009 1 19960221 A 2910 9302632001 HOSE SAAB SF340 340B 7860101 EU NLG WW BROKEN A REXA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 25 366PX 340B267 ON TAXIING, LOST HYDRAULIC QUANTITY 2 CWP, LEAK ON MAIN RESERVE IN NOSE WHEEL COMPARTMENT. REMOVED AND REPLACED UPPER H YDRAULIC PUMP RETURN LINE IAW AMM CHAPTER 29. NO LEAKS NOTED. ACFT OK FOR SERVICE. (X) 2 L 7 2 4T RT A52EU 1996040500205 19960405 00205 EU 1996 4 5 REXA9603 1 19960201 A 3320 BA08006281 BALLAST BRUCE SAAB SF340 SF340A 7850100 EU GALLEY SHORTED A REXA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 25 328PX 340A068 ELECTRIC ODOR COMING FROM GALLEY AREA. REPLACED BALLAST FOR WINDOW LIGHT. FUNCTIONAL TEST GOOD. (X) 2 L 7 2 4T RT A52EU 1996040500206 19960405 00206 EU 1996 4 5 REXA9604 1 19960209 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 SF340A 7850100 EU AVIONICS COMPT DIRTY A REXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 325PX 340A051 RETURNED TO RAMP WITH AVIONICS SMOKE CAPTION. FOUND NO SMOKE. REMOVED AND REPLACED SMOKE DETECTOR. OPS CHECK GOOD. ( X) 2 L 7 2 4T RT A52EU 1996040500209 19960405 00209 1996 4 5 VTZA96077 4 19960216 A 3420 7012100811 RMU JETAIR JETSTM JETSTM4101 1500501 EU AVIONIC BAY FAILED A VTZA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 27 320UE 41043 FLT NR 6384 - ROC-IAD - DURING CRUISE, THE FLIGHT CREW STATED THAT THEY DETECTED AND ELECTRICAL BURNING SMELL IN THE COC KPIT. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE NR 2 RMU. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996040500210 19960405 00210 WP 1996 4 5 VTZA96088 2 19960225 A 7320 89737527 FUEL CONTROL BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE331* 01514 WP RT ENGINE OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 484UE 2702 899 P66166 LYH/IAD - FLT 6189 - DURING TAKEOFF AT 1400 HRS ON 2-25-96, ABORTED THE TAKEOFF DUE TO RT ENGINE NOT MAKING TARGETED TAK EOFF TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED SCREW 'X' ON THE RT FUEL CONTRO L UNIT. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T 3 T RT A56EU E2WE 1996040500211 19960405 00211 EU 1996 4 5 VTZA96089 1 19960202 A 7797 WIRE BAG JETSTM JETSTM3201 1500217 EU EGT GAUGE FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 484UE 899 ABE/IAD - FLT 6153 - DURING CLIMB-OUT AT 1540 HRS ON 2-2-96, MADE AN UNSCHEDULED LANDING DUE TO RADICAL EGT FLUX. AIRCR AFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED EGT GAUGE, PN 6100144A, AND REPAIRED W IRE ON WIRE HARNESS. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR SERVICE. (X) 2 L 7 2 4T RT A56EU 1996040500212 19960405 00212 EU 1996 4 5 VTZA96090 1 19960221 A 2751 TY17604A POTENTIOMETER JETAIR JETSTM JETSTM4101 1500501 EU TE FLAPS FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 313UE 41026 IAD/BOS - DURING TAKEOFF AT 1430 HRS ON 2-21-96, ABORTED TAKEOFF DUE TO TAKEOFF CONFIGURATION SYSTEM ACTIVATING. AIRCRA FT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED FLAP POSITION TRANSDUCER. AIRCRAFT RELEASED AND AP PROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1996040500213 19960405 00213 EU 1996 4 5 VTZA96091 1 19960225 A 5270 91SE16 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU LT EMERG EXIT DIRTY A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 324UE 41017 IAD/PWM - FLT 6578 - DURING TAKEOFF AT 1622 HRS ON 2-25-96, ABORTED TAKEOFF DUE TO EMERGENCY DOOR WARNING LIGHT ILLUMINA TING ON THE TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE CLEANED THE EMERGENCY EXIT MICROSWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1996040500214 19960405 00214 EU 1996 4 5 YIEA96009 1 19960227 A 3230 A12380ML UPLOCK SWITCH MESSIER A237171 AMD FALC20 FALCOND 2720304 EU NLG DOOR ACT FAILED A YIEA O OTHER J WARNING INDICATION LD LANDING 1 GL 23 817AA 292 233 YIP - FLT 12323 - LANDING GEAR WOULD NOT EXTEND (INDICATION 3 RED LIGHTS AND NO GREEN LIGHTS). GEAR HANDLE CYCLED TWICE WITH NO RESULT. CREW EMPLOYED AFM "PROCEDURE A" TO EXTEND LANDING GEAR AND LANDED WITH 3 GREEN LIGHTS. NOTE: AIRCRAF T WAS ARRIVING AT YIP WHEN THIS DIFFICULTY WAS ENCOUNTERED. PROBLEM NOT DUPLICATED DURING GROUND RETRACTION TESTS. PER FORMED 'VOLTAGE DROP TEST' OF LANDING GEAR DOOR SWITCHES IAW MM PROCEDURES 32-60-10. NLG DOOR ACTUATOR SWITCH FOUND BAD . REPLACED WITH SERVICEABLE PART. LANDING GEAR CYCLED IAW MM 32-30-00 WITH NO DEFECTS NOTED. (X) 2 L 7 2 4F A7EU 1996040500215 19960405 00215 WP 1996 4 5 96ZZZW41 1 19960101 A 5730 SKIN DOUG DC8 DC863 302198A WP WS 0.00 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 4935C 45931 LEVEL 2 CORROSION, RIGHT WING UPPER SKIN AT XW 0.000 CENTER SPAR AREA SKIN HAS SURFACE CORROSION AT FUSELAGE STA 781.500 . REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER RICH DRAWING 95-10-06-OO1. 2 L 7 4 4F 4A25 1996040500216 19960405 00216 WP 1996 4 5 96ZZZW42 1 19960101 A 5320 SUPPORT DOUG DC8 DC863 302198A WP BS 1220 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 4935C 45931 LEVEL 2 CORROSION, HEAVY CORROSION ON CARGO TRACK SUPPORT FRAME AT STA 1220 BETWEEN STRINGERS 26L. REMOVED DAMAGED AREA , FABRICATED AND INSTALLED REPAIR PER SRM 51-2-0. 2 L 7 4 4F 4A25 1996040500217 19960405 00217 WP 1996 4 5 96ZZZW43 1 19960101 A 5542 SKIN DOUG DC8 DC863 302198A WP RUDDER CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 4935C 45931 LEVEL 2 CORROSION, RUDDER SURFACE IS CORRODED ON RIGHT SIDE ABOVE TAB CUTOUT. REMOVED DAMAGED AREA, FABRICATED AND INST ALLED REPAIR PER SRM 55-2-0. 2 L 7 4 4F 4A25 1996040500218 19960405 00218 WP 1996 4 5 96ZZZW44 1 19960101 A 5730 SKIN DOUG DC8 DC863 302198A WP WS 311 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 4935C 45931 LEVEL 2 CORROSION, RIGHT WING STA 311 STRINGER 8 UPPER SKIN HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED AND INSTALL ED REPAIR PER RICH DRAWING 459316. 2 L 7 4 4F 4A25 1996040500219 19960405 00219 WP 1996 4 5 96ZZZW45 1 19960205 A 5330 SKIN DOUG DC8 DC862 3021970 WP BS 1290 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 8974U 46110 LEVEL 2 CORROSION, TWO SMALL SKIN BULGES JUST AFT OF NR 4 PIT DOOR FS 1290 STRINGER 28R. REMOVED DAMAGED AREA, FABRICAT ED AND INSTALLED REPAIR PER SRM 53-2-1. 2 L 7 4 4F 4A25 1996040500220 19960405 00220 WP 1996 4 5 96ZZZW46 1 19960205 A 5330 SKIN DOUG DC8 DC862 3021970 WP BS 540 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 8974U 46110 LEVEL 2 CORROSION, LOWER FUSELAGE IS BULGED WITH CORROSION AT FS 540R BETWEEN LONGERONS 35R AND 34R BELOW FORWARD CARGO DOOR SILL PLATE. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR PER SRM 52-2-1. 2 L 7 4 4F 4A25 1996040500221 19960405 00221 WP 1996 4 5 96ZZZW47 1 19960205 A 5313 STRINGER DOUG DC8 DC862 3021970 WP BS 1240-1260 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 8974U 46110 LEVEL 2 CORROSION, AFT CARGO COMPARTMENT LEFT SIDE STRINGER 21L BETWEEN STA 1240 AND 1260 FUSELAGE SKIN HAS CORROSION. R EMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER RICH EO D85310-6124 REV 1. 2 L 7 4 4F 4A25 1996040500222 19960405 00222 WP 1996 4 5 96ZZZW48 1 19960205 A 5313 STRINGER DOUG DC8 DC862 3021970 WP BS 1160-1180 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 8974U 46110 LEVEL 2 CORROSION, AFT CARGO COMPARTMENT STRINGER 21R BETWEEN STA 1160 AND 1180 FLOOR SUPPORT HAS CORROSION. REMOVED DA MAGED AREA FABRICATED AND INSTALLED REPAIR PER SMR 53-2-5. 2 L 7 4 4F 4A25 1996040500223 19960405 00223 WP 1996 4 5 96ZZZW49 1 19960205 A 5330 SKIN DOUG DC8 DC862 3021970 WP BS 1220-1240 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 8974U 46110 LEVEL 2 CORROSION, AFT CARGO COMPARTMENT LOWER AREA STRINGER 34R BETWEEN STA 1220 AND 1240 FUSELAGE SKIN HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 51-1-0. 2 L 7 4 4F 4A25 1996040500224 19960405 00224 WP 1996 4 5 96ZZZW50 1 19960220 A 5320 TEAR STRAP LKHEED 1011 10113851 5265010 WP FS 1463 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 300AW 193P1134 LEVEL 2 CORROSION, C2 CARGO COMPARTMENT INTERIOR HAS CORROSION AT FS 1463 STRINGER 33 LEFT SIDE. REMOVED TEAR STRAP, RE MOVED DAMAGED AREA, FABRICATED, INSTALLED REPAIR AND REINSTALLED TEAR STRAP PER SRM 51-40-01. 2 L 7 3 4F A23WE 1996040500225 19960405 00225 WP 1996 4 5 96ZZZW51 1 19960220 A 5330 SKIN LKHEED 1011 10113851 5265010 WP BS 1735 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 300AW 193P1134 LEVEL 2 CORROSION, CORROSION CRACK AT STA 1735 STRINGER 34. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER PER SRM 53-31-00. 2 L 7 3 4F A23WE 1996040500226 19960405 00226 WP 1996 4 5 96ZZZW52 1 19960226 A 5320 ANGLE LKHEED 1011 10113851 5265010 WP BS 1373 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 300AW 193P1134 LEVEL 2 CORROSION, CENTER CARGO COMPARTMENT HAS CORROSION AROUND NUTPLATE INSIDE FLOOR SUPPORT CHANNEL AT STA 1373 RBL 6 . REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 51-40-04. 2 L 7 3 4F A23WE 1996040500227 19960405 00227 WP 1996 4 5 96ZZZW53 1 19960226 A 5330 SKIN LKHEED 1011 10113851 5265010 WP FS 1536 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 300AW 193P1134 LEVEL 2 CORROSION, LOWER AFT FUSELAGE HAS BULGING SKIN AND WITH MISSING AND CRACKED RIVET HEADS AT FS 1536 STRINGER 33 T O 35. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-31-00. 2 L 7 3 4F A23WE 1996040500228 19960405 00228 WP 1996 4 5 96ZZZW54 1 19960226 A 5320 FLOOR SUPPORT LKHEED 1011 10113851 5265010 WP BS 1525 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 300AW 193P1134 LEVEL 2 CORROSION, CENTER CARGO COMPARTMENT HAD CORROSION AROUND NUTPLATE AT LOGITUDINAL FLOOR SUPPORT AT RBL 36 FORWARD OF FLOOR SUPPORT BEAM AT STA 1525. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 51-50-02. 2 L 7 3 4F A23WE 1996040500229 19960405 00229 WP 1996 4 5 96ZZZW55 1 19960226 A 5320 STRAP LKHEED 1011 10113851 5265010 WP BS 1625 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 300AW 193P1134 LEVEL 2 CORROSION, C3 CARGO COMPARTMENT FORWARD BULKHEAD AT STA 1625 STRAP ALONG LOWER SIDE AT FLOOR LEVEL CORRODED. RE MOVED AND REPLACED LOWER STRAP PER SRM 51-50-00. 2 L 7 3 4F A23WE 1996040500230 19960405 00230 WP 1996 4 5 96ZZZW56 1 19960226 A 5320 SUPPORT LKHEED 1011 10113851 5265010 WP BS 1463-1480 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 300AW 193P1134 LEVEL 2 CORROSION, C2 CARGO FLOOR SUPPORT HAS CORROSION BETWEEN FS 1463 AND 1480 LEFT SIDE APPROX LBL 48. REMOVED DAMAG ED AREA AND FABRICATED AND INSTALLED REPAIR PER SRM 51-50-02. 2 L 7 3 4F A23WE 1996040500231 19960405 00231 WP 1996 4 5 96ZZZW57 1 19960226 A 5313 STRINGER LKHEED 1011 10113851 5265010 WP BS 629-649 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 300AW 193P1134 LEVEL 2 CORROSION, INSIDE C1 CARGO COMPARTMENT FS 629 TO 649 STRINGERS 31 AND 32. REMOVED DAMAGED AREAS AND INSTALLED N EW STRINGER SECTIONS PER SRM 51-13-00. 2 L 7 3 4F A23WE 1996040500232 19960405 00232 WP 1996 4 5 96ZZZW58 1 19960301 A 5270 DOOR LIGHT LKHEED 1011 10113851 5265010 WP CARGO COMPT ILLUMINATED A RIAA A J UNSCHED LANDING DUMP FUEL N FALSE WARNING CL CLIMB 1 SO 19 300AW 193P1134 MZH-MSP - FLT 814 - DURING CLIMB, C3 CARGO DOOR LIGHT CAME ON, A/C DUMPED FUEL AND RETURNED TO MZH. AFTER LANDING INSPE CTED C3 DOOR FRAME, DOOR STOPS, DOOR LINER, DOOR ACTUATOR AND LATCH MECHANISM PER 52-31-02. CYCLED C3 DOOR, OPS CHECKED PER 52-71-01. FOUND NO DISCREPANCIES AND NO FURTHER INCIDENTS. 2 L 7 3 4F A23WE 1996040500233 19960405 00233 NE 1996 4 5 DLM90960584 2 19960314 A 7321 EEC DOUG DC8 DC863 302198A WP IAE V2525 V2525D5 NE NR 1 ENGINE FAILED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 27 903DA 45931 ON TAKEOFF ROLL AFTER ADVANCING THROTTLES, THE LEFT ENGINE SURGE LIGHT CAME ON WITH THE LEFT ENGINE IGNITION LIGHT. BOT H LIGHTS CAME ON AND OFF, 3 TIMES TOTAL. REPLACED LEFT ENGINE EEC PER MM. PERFORMED ENGINE FAULT, DISPLAY SYSTEM CHECK AND OPERATIONAL/IDLE SYSTEM TEST NORMAL. 2 L 7 4 4F 4 F 4A25 A40NE 1996040500235 19960405 00235 NM 1996 4 5 9607272299 1 19960330 A 7711 LG14C14 EPR TRANSMITTER BOEING 727 727251 138408H NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 299U 40448 22153 696533 NR 2 ENGINE EPR INDICATION FROZE ON TAKEOFF ROLL. TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENAN CE REPLACED THE EPR TRANSMITTER WITH A SERVICEABLE UNIT. 2 L 7 3 4F 4 F A3WE E2EA 1996040500236 19960405 00236 NE 1996 4 5 9607286624 2 19960331 A 7261 OIL SYST BOEING 747 747251B 1384892 NM PWA JT9 JT9D7Q 52054 NE NR 1 ENGINE REQD SERVICE A NWAA E ENGINE SHUTDOWN J WARNING INDICATION TX TAXI/GRND HDL 1 GL 01 624US 71706 02171 AFTER LANDING IN NRT AND SUBSEQUENT TAXIING, THE NR 1 ENGINE OIL TEMPERATURE INCREASED INTO CAUTION RANGE, THE OIL PRESS URE DECREASED TO CAUTION AS WELL. CREW FOLLOWED COCKPIT OPERATING MANUAL, SHUTDOWN NR 1 ENIGNE AND FLIGHT CONTINUED TO GATE WITHOUT FURTHER INCIDENT. VISUAL CHECK WAS NORMAL. REPLACED ENGINE OIL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4 F A20WE E3NE 1996040500237 19960405 00237 NM 1996 4 5 9607292702 1 19960327 A 2421 700662 GENERATOR BOEING 727 727225 1384077 NM NR 3 ENGINE INOPERATIVE A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 GL 01 8877Z 39952 208 21450 AS THRUST LEVERS WERE ADVANCED FOR TAKEOFF, THE NR 3 GENERATOR DROPPED OFF LINE. ABORTED TAKEOFF AND RETURNED TO THE GA TE. MAINTENANCE SWAPPED NR 2 AND NR 3 LOAD CONTROLLERS AND DEFERRED NR 2 GENERATOR INOPERATIVE. AIRCRAFT RETURNED TO S ERVICE. 2 L 7 3 4F A3WE 1996040500238 19960405 00238 EU 1996 4 5 9607303249 1 19960331 A 3230 RETRACT MECH AIRBUS 320 A320211 3930320 EU NLG LACK OF LUBE A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 349NW 417 DURING CLIMBOUT UPON LANDING GEAR RETRACTION, LDG GEAR SHOCK ABSORBER FAULT ILLUMINATED AND GEAR WOULD NOT RETRACT. FAU LT CLEARED APPROXIMATELY 45 SECONDS LATER AND GEAR RETRACTED NORMALLY. FLIGHT CONTINUED TO MSP AND LANDED WITHOUT FURTH ER INCIDENT. MAINTENANCE LUBRICATED THE GEAR AND SERVICED THE NOSE LANDING GEAR. OPERATIONAL CHECK WAS NORMAL. 2 L 7 2 4F RT A28NM 1996040500239 19960405 00239 NM 1996 4 5 9607316301 1 19960329 A 3350 CONNECTOR BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 661US 23719 DURING LINE CHECK, THE FLOOR MOUNTED EMERGENCY PATH LIGHTS BETWEEN SEAT ROWS 35R TO 43R WERE FOUND INOPERATIVE. RECONNE CTED EMERGENCY LIGHT ASSEMBLY AT ROW 43 AND OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996040500240 19960405 00240 NM 1996 4 5 9607326301 1 19960329 A 3350 CONNECTOR BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 661US 23719 DURING LINE CHECK, THE FLOOR MOUNTED EMERGENCY PATH LIGHTS BETWEEN SEAT ROWS 77L TO 79L WERE FOUND INOPERATIVE. RECONNE CTED EMERGENCY LIGHT ASSEMBLY AT ROW 79L AND OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996040500241 19960405 00241 WP 1996 4 5 9607331225 1 19960331 A 3620 INDICATION SYST DOUG DC10 DC1030 3023501 WP PNEUMATIC SYST MALFUNCTIONED A NWAA A J UNSCHED LANDING DUMP FUEL N FALSE WARNING CR CRUISE 1 GL 01 225NW 46582 DURING CRUISE, THE NR 1 PNEUMATIC TEMPERATURE WAS 220 DEGREES AND THE NR 3 PNEUMATIC TEMPERATURE LIGHT ILLUMINATED WITH NR 3 TEMPERATURE INDICATING 150 DEGREES. DUMPED 70,000 LBS OF FUEL AND RETURNED TO HNL. MAINTENANCE SECURED THE PRESSU RE REGULATOR VALVE CLOSED AND DEFERRED PER MEL 36-4A AND MEL 36-15C. 2 L 7 3 4F A22WE 1996040500242 19960405 00242 WP 1996 4 5 9607349885 1 19960328 A 2120 DUCT DOUG DC9 DC951 3022051 WP RIGHT BLOWN A NWAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 01 401EA 47682 DURING CRUISE TO ATL, CABIN LOSE PRESSURE. AIRCRAFT DESCENDED TO 10,000 FEET AND CONTINUED TO ATL FOR NORMAL LANDING. F OUND BLOWN DUCT ON RIGHT TURBINE DISCHARGE. REPLACED DUCT AND PRESSURIZED CABIN AND OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996040500243 19960405 00243 WP 1996 4 5 ABXA9600423 1 19960330 A 3350 60030431 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 936AX 47269 EMERGENCY LIGHTS INTERMITTENTLY STAY ON WITH POWER OFF. REPLACED EMERGENCY LIGHT POWER SUPPLY. 2 L 7 2 4F A6WE 1996040500251 19960405 00251 SO 1996 4 5 COMA9610116 1 19960328 A 2997 WIRE EMB 120 EMB120RT SO RT NACELLE CHAFED A COMA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 205CA 120205 RT HYDRAULIC RESERVOIR LOW PRESSURE INDICATOR ILLUMINATED. REPAIRED CHAFED WIRE AT PRESSURE SWITCH. 2 L 7 2 4T RT A31SO 1996040500252 19960405 00252 SO 1996 4 5 COMA9610117 1 19960327 A 7921 1602824 OIL COOLER EMB 120 EMB120RT SO RT ENGINE LEAKING A COMA C D ABORTED TAKEOFF RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SO 01 168CA 120168 RT ENGINE LOST OIL PRESSURE DURING TAKEOFF. REPLACED THE ENGINE OIL COOLER. 2 L 7 2 4T RT A31SO 1996040500253 19960405 00253 EU 1996 4 5 COMA9630086 1 19960327 A 2720 MS3116F84S CONNECTOR SAAB SF340 SF340A 7850100 EU RUDDER LIMITER SHORTED A COMA K NONE F FLT CONT AFFECTED UK UNKNOWN 1 SO 01 347CA 340A028 RUDDER LIMITER OVERRIDE CIRCUIT BREAKER TRIPPED AND WILL NOT RESET. REPLACED WIRING CONNECTOR AT OVERRIDE ACTUATOR. 2 L 7 2 4T RT A52EU 1996040500254 19960405 00254 EU 1996 4 5 COMA9630087 1 19960327 A 6120 004WS00 WEU SAAB SF340 SF340A 7850100 EU AVIONICS MALFUNCTIONED A COMA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 356CA 16476 191 340A034 AUTO COURSEN FAULT LIGHT ILLUMINATED DURING GROUND OPS. REPLACED THE WARNING ELECTRONIC UNIT. 2 L 7 2 4T RT A52EU 1996040500255 19960405 00255 EA 1996 4 5 COMA9660056 1 19960327 A 2760 4916403 SECU CNDAIR CL600 CL6002B19 EA NR 2 SPOILER FAILED A COMA K NONE O OTHER LD LANDING 1 SO 01 933CA 2211 7040 GROUND SPOILERS DO NOT AUTO DEPLOY DURING LANDING. REPLACED THE NR 2 SPOILER ELECTRONIC CONTROL UNIT. 2 L 7 2 4F RT A21EA 1996040500256 19960405 00256 EA 1996 4 5 COMA9660057 1 19960327 A 3242 5010520 BRAKE ASSY CNDAIR CL600 CL6002B19 EA LT MLG GRABBING A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 947CA 1138 264 7077 BRAKES ARE GRABBING AND MAKE LOUD GRINDING NOISE. REPLACED THE LT MLG INBD BRAKE ASSY. 2 L 7 2 4F RT A21EA 1996040500257 19960405 00257 NM 1996 4 5 P5CA9600203 1 19960331 A 8011 7401793 STARTER BOEING 747 747122 1384872 NM NR 1 ENGINE INOPERATIVE A P5CA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 23 853FT 19753 RETURNED TO BLOCKS DUE TO UNABLE TO START NR 1 ENGINE. REPLACED STARTER, STARTER GEARBOX MOUNT ADAPTER AND MOUNT CLAMP IAW MM 80-11-01. 2 L 7 4 4F A20WE 1996040500258 19960405 00258 NM 1996 4 5 P5CA9600204 1 19960330 A 2450 WARNING LIGHT BOEING 747 747132 1384882 NM FE PANEL INOPERATIVE A P5CA D RETURN TO BLOCK P NO WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 857FT 20246 RETURNED TO BLOCKS DUE TO ADP AND EDP LOW PRESSURE WARNING LIGHTS AND ADP RUN LIGHTS INOP AT FEO PANEL AFTER ENGINE STA RT. CYCLED BETWEEN APU AND ENGINE GENERATORS AND LIGHTS OPERATED NORMALLY. 2 L 7 4 4F A20WE 1996040500259 19960405 00259 NM 1996 4 5 P5CA9600205 1 19960331 A 7830 12623643 TR DRIVE UNIT BOEING 747 747122 1384872 NM NR 2 ENGINE INOP A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NR 2 REVERSER DRIVE MOTOR FAILED AD 95-16-02 INSPECTION. PLACARDED AS INOP, REMOVED AND REPLACED NR 2 DRIVE UNIT AT LAX IAW MM 78-31-02. 2 L 7 4 4F A20WE 1996040500260 19960405 00260 WP 1996 4 5 RRXA96013 1 19960327 A 3231 RETRACT MECH DOUG DC8 DC863 302198A WP RT MLG DOOR LACK OF LUBE A RRXA K NONE J WARNING INDICATION CL CLIMB 1 WP 15 951R 46092 KDFW - FLT 22 - AFTER TAKEOFF AT KDAY DOORS NOT LATCH LIGHT CAME ON UPON GEAR RETRACTION WITH RIGHT ALT GEAR DOOR WARNIN G LIGHT ON. RECYCLED SEVERAL TIMES NO HELP. PROCEEDED TO DESTINATION. MAINTENANCE CLEANED AND LUBED GEAR DOOR UP LATC H AND INSPECTED GEAR DOOR UPLATCH MECHANISM AND RIGGING. NO DEFECT NOTED. JACKED AIRPLANE AND SWUNG GEAR 10 TIMES. OP S CHECKED GOOD NO DEFECT NOTED. (M) 2 L 7 4 4F 4A25 1996040500261 19960405 00261 NM 1996 4 5 SCNA96038 1 19960326 A 3350 1060091102 BATTERY PACK BOEING 727 7272J4 1384006 NM R 1 DOOR DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 284SC 21438 THE OVERHEAD R-1 DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AND POWER SUPPLY A ND LIGHT TESTED GOOD. 2 L 7 3 4F RT A3WE 1996040500262 19960405 00262 NM 1996 4 5 SWAA960184 1 19960325 A 3230 65446915 UPLOCK ACTUATOR BOEING 737 7372H4 138448C NM RT MLG FAILED A SWAA K NONE J WARNING INDICATION TO TAKEOFF 1 SW 07 95SW 23054 AFTER TAKEOFF WITH LANDING GEAR LEVER IN THE UP POSITION, RIGHT MAIN GEAR RED LIGHT ILLUMINATED. WHEN GEAR LEVER MOVED TO OFF, RIGHT MAIN GEAR EXTENDED AND WENT TO GREEN POSITION. GEAR LEVER WAS THEN POSITIONED TO UP AND GEAR RETRACTED. I NSPECTED AND REPLACED RIGHT MAIN GEAR UPLOCK ACTUATOR AND CYCLED GEAR SEVERAL TIMES PER BOEING M/M. 2 L 7 2 4F A16WE 1996040500263 19960405 00263 NM 1996 4 5 SWAA960185 1 19960327 A 2751 106079113 POS INDICATOR BOEING 737 7375H4 138449D NM CONTROL CABIN MALFUNCTIONED A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 526SW 26568 UNABLE TO LOWER OR RETRACT T/E FLAPS PAST 5 DEGREES USING HYDRAULICS. ALTERNATE/ELECTRICAL EXTENSION USED TO MOVE THEM TO 15 DEGREES. AIRCRAFT MADE AN UNEVENTFUL LANDING AT LAX. INSPECTED AND REPLACED FLAP POSITION INDICATOR PER BOEING M /M. 2 L 7 2 4F RT A16WE 1996040500264 19960405 00264 NM 1996 4 5 SWAA960186 1 19960328 A 5240 SKIN BOEING 737 7373H4 1384600 NM FWD SERV DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED C3 CHECK, FOUND FWD SERVICE DOOR SKIN CRACKED AT TOP AFT CORNER AT UPPER RIVET. REPAIRED PER BOEING SR M. 2 L 7 2 4F RT A16WE 1996040500265 19960405 00265 NM 1996 4 5 SWAA960187 1 19960328 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 380 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 51SW 21448 DURING SCHEDULED C2 CHECK, FOUND FWD LEFT FUSELAGE SKIN CRACKED 2 INCHES AT BS 380 S24L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996040500266 19960405 00266 NM 1996 4 5 SWAA960188 1 19960328 A 3240 BRAKE PEDAL BOEING 737 7372H4 138448C NM RT SYST FOULED A SWAA K NONE O OTHER TX TAXI/GRND HDL 1 SW 07 67SW 22356 AFTER LANDING, EXPERIENCED POOR BRAKING ACTION. ALSO, BRAKES WOULD NOT SET AT GATE. INSPECTED AND FOUND AN ADEL CLAMP UNDER F/O BRAKE PEDAL PANEL. REMOVED AND BRAKES OPERATED NORMALLY. 2 L 7 2 4F A16WE 1996040500267 19960405 00267 NM 1996 4 5 UPS9620 1 19960322 A 5347 SEAT TRACK BOEING 727 72727C 138400J NM BS 480-650 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED SEAT TRACK AT LBL 25 STA 480 TO 650 WL 208 HAS CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW SEAT TRACK. ALSO, FOUND INTERCOSTAL AND ANGLE DAMAGED, AL L WORK DONE IAW 51-10-2, 53-10-2, MM 51-20-151, SRM 51-30-5 AND 51-30-8. 2 L 7 3 4F A3WE 1996040500268 19960405 00268 NM 1996 4 5 UPS96205793 1 19960324 A 5313 STRINGER BOEING 727 72727C 138400J NM BS 480 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION STA 480 STR 21 RT LOWER FLANGE. REMOVED CORROSION, OUT OF LIMITS IAW SRM 53-10-1. REPAIRED STR 21R IAW SRM 53-10-3. 2 L 7 3 4F A3WE 1996040500269 19960405 00269 NM 1996 4 5 UPS96205794 1 19960324 A 5313 STRINGER BOEING 727 72727C 138400J NM BS 488 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION STA 488 STR 22 RT UPPER FLANGE WL 170 RBL 50. REMOVED CORROSION, OUT OF LIMITS IAW SRM 53-10-1. REPAIRED STR 22R FROM STA 470 TO 490 IAW SRM 53-10-3. 2 L 7 3 4F A3WE 1996040500270 19960405 00270 NM 1996 4 5 UPS96205795 1 19960223 A 5241 GATE BOEING 727 72727C 138400J NM GALLEY DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION AND CRACKING MID GALLEY DOOR LOWER GATE LOWER FWD CORNER. REMOVED AND REPLACED LOWER GATE IAW UPS OHM 52-46-01. 2 L 7 3 4F A3WE 1996040500271 19960405 00271 NM 1996 4 5 UPS96205796 1 19960223 A 5241 GATE BOEING 727 72727C 138400J NM GALLEY DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION AND CRACKING MID GALLEY DOOR UPPER GATE UPPER EDGE. REMOVED AND R EPLACED UPPER GATE IAW UPS OHM 52-46-01. 2 L 7 3 4F A3WE 1996040500272 19960405 00272 NM 1996 4 5 UPS96205797 1 19960223 A 5230 TRANSVERSE BEAM BOEING 727 72727C 138400J NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED FWD CARGO DOOR TRANSVERSE BEAM AND O/B L-ANGLE ARE CRACKED IN O/B RADIUS AT OUTER SKIN VERT STIFFENERS. REMOVED AND REPLACED TRANVERSE BEAM IAW SRM 51-10-1, 51-10-2, 51-30-5, 51-30-2, 51-20-4 AND MM 51-20-151. 2 L 7 3 4F A3WE 1996040500273 19960405 00273 NM 1996 4 5 UPS96205798 1 19960324 A 5313 STRINGER BOEING 727 72727C 138400J NM BS 360-410 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON STR 21R AT BS 400 WL 177. REMOVED CORROSION, OUT OF LIMITS IAW SRM 53-10-1. REMOVED SECTION OF STR FROM STA 360 TO 410 AND REPLACED SECTION IAW SRM 53-10-1 AND 51-40-3. 2 L 7 3 4F A3WE 1996040500274 19960405 00274 NM 1996 4 5 UPS96205799 1 19960324 A 5320 EXPANSION LINK BOEING 727 72727C 138400J NM BS 850-870 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON EXPANSION LINK STA 850 TO 870 LBL 45, WL 208. CORROSION REMOVA L WAS OUT OF LIMITS. FABRICATED NEW LINK AND INSTALLED IAW SRM 53-10-1, 51-10-2, OHM 20-50-3 AND MM 51-20-31. 2 L 7 3 4F A3WE 1996040500275 19960405 00275 NM 1996 4 5 UPS96205800 1 19960323 A 5752 TAB FITTING BOEING 727 72727C 138400J NM LT AILERON CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED LT WING I/B AILERON SIDE TAB HINGE FITTINGS ARE CORRODED. REMOVED AND REPLA CED TAB FITTINGS UPS SRM 51-30-2. 2 L 7 3 4F A3WE 1996040500276 19960405 00276 NM 1996 4 5 UPS96205801 1 19960321 A 5347 SEAT TRACK BOEING 727 72727C 138400J NM BS 1000-1050 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON SEAT TRACK STA 1000 TO 1050 RBL 45. REMOVED CORROSION AND FOUN D TO BE OUT OF LIMITS. CUT OUT AND REPLACED SEAT TRACK IAW SRM 53-10-1, 53-10-5, AND 51-20-4. 2 L 7 3 4F A3WE 1996040500277 19960405 00277 NM 1996 4 5 UPS96205802 1 19960323 A 5315 FLOOR BEAM BOEING 727 72727C 138400J NM BS 328 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON FLOOR BEAM STA 328 LBL 4, 19 AND 46, WL 208. REMOVED CORROSION , CUT FLOOR BEAM UPPER FLANGE AT RBL 18 TO LT END, FABRICATED NEW CHORD AND INSTALLED PER SRM 53-10-8. 2 L 7 3 4F A3WE 1996040500278 19960405 00278 NM 1996 4 5 UPS96205803 1 19960321 A 5320 THRESHOLD BOEING 727 72727C 138400J NM BS 304 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON COCKPIT THRESHOLD SUPPORT CHANNEL STA 304 WL 208 LBL 11 TO RBL1 1. REMOVED AND REPLACED C/P THRESHOLD CHANNEL IAW SRM 51-20-1, 51-20-31, 51-30-8, 53-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996040500279 19960405 00279 NM 1996 4 5 UPS96205804 1 19960323 A 5320 INTERCOSTAL BOEING 727 72727C 138400J NM BS 312-328 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON UPPER AND LOWER SURFACE OF INTERCOSTAL AROUND NUT CLIP HOLES ST A 312 TO 328 RBL 40 WL 208. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-30-2 AND 51-30-8. 2 L 7 3 4F A3WE 1996040500280 19960405 00280 NM 1996 4 5 UPS96205805 1 19960324 A 5320 INTERCOSTAL BOEING 727 72727C 138400J NM BS 316 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON UPPER AND LOWER SURFACE OF INTERCOSTAL AROUND NUT CLIP HOLES ST A 316 RBL 51 WL 208. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996040500281 19960405 00281 NM 1996 4 5 UPS96205806 1 19960323 A 5320 INTERCOSTAL BOEING 727 72727C 138400J NM BS 312-328 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON UPPER AND LOWER SURFACE OF INTERCOSTAL AROUND NUT CLIP HOLES ST A 312 TO 328, LBL 31 WL 208. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-30-2 AND 51-30-8. 2 L 7 3 4F A3WE 1996040500282 19960405 00282 NM 1996 4 5 UPS96205807 1 19960323 A 5347 SEAT TRACK BOEING 727 72727C 138400J NM BS 344-480 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED SEAT TRACK AT LBL 45 STA 344 TO 480 WL 208 HAS CORROSION. REMOVED CORROSION AND FOUND TO OUT OF LIMITS. FABRICATED NEW SEAT TRACK AND INSTALLED IAW SRM 53-10-3 AND 51-30-2. 2 L 7 3 4F A3WE 1996040500283 19960405 00283 NM 1996 4 5 UPS96205809 1 19960324 A 5320 HAT CHANNEL BOEING 727 72727C 138400J NM BS 1137 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON HAT CHANNEL BS 1137 RBL 62 WL 208. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED AND FABRICATED HAT CHANNEL AND INSTALLED PER SRM 51-30-2, 51-30-5 AND 51-30-8. 2 L 7 3 4F A3WE 1996040500284 19960405 00284 NM 1996 4 5 UPS96205810 1 19960324 A 5320 HAT CHANNEL BOEING 727 72727C 138400J NM BS 1130-1180 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED. CORROSION ON HAT CHANNEL BS 1130 TO 1180 RBL 25 WL 208. REMOVED CORROSION , FOUND TO BE OUT OF LIMITS. REMOVED AND FABRICATED HAT CHANNEL AND INSTALLED PER SRM 51-30-2, 51-30-5 AND 51-30-8. 2 L 7 3 4F A3WE 1996040500285 19960405 00285 NM 1996 4 5 UPS96205811 1 19960324 A 5320 HAT CHANNEL BOEING 727 72727C 138400J NM BS 1137 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON HAT CHANNEL BS 1137 LBL 25 TO 65 WL 208. REMOVED CORROSION, FO UND TO BE OUT OF LIMITS. REMOVED AND FABRICATED HAT CHANNEL AND INSTALLED PER SRM 51-30-2, 51-30-5 AND 51-30-8. 2 L 7 3 4F A3WE 1996040500286 19960405 00286 NM 1996 4 5 UPS96205812 1 19960324 A 5320 HAT CHANNEL BOEING 727 72727C 138400J NM BS 1130-1175 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON HAT CHANNEL BS 1130 TO 1175 LBL 25 TO 65 WL 208. REMOVED CORRO SION, FOUND TO BE OUT OF LIMITS. REMOVED, FABRICATED HAT CHANNEL AND INSTALLED PER SRM 51-30-2, 51-30-5, 51-30-8 AND 51 -20-1. 2 L 7 3 4F A3WE 1996040500287 19960405 00287 NM 1996 4 5 UPS96205813 1 19960328 A 5230 FITTING BOEING 727 72727C 138400J NM CARGO D00R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED TRANSFERRED FROM DMI LOG CONTROL NR M-106749 1 PRESSURE STOP FITTING CRACKED ON LOWER FWD CARGO DOOR. REMOVED AND REPLACED FITTING IAW EO B727-5230-0032 APP C. 2 L 7 3 4F A3WE 1996040500288 19960405 00288 NM 1996 4 5 UPS96205814 1 19960328 A 5320 SEAL RETAINER BOEING 727 72727C 138400J NM BS 870 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON STA 870 SEAL RETAINER LBL 60 RBL 60. REMOVED CORRODED SEAL RET AINER IAW 53-10-1, FABRICATED REPAIR PARTS AND INSTALLED EO 727-57-1690 AND SRM 51-30-2, 51-10-1. 2 L 7 3 4F A3WE 1996040500289 19960405 00289 NM 1996 4 5 UPS96205815 1 19960328 A 5330 SKIN BOEING 727 72727C 138400J NM BS 740-870 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON TOP OF FUEL CELL SKIN AT STA 740 TO 870 LBL 25 TO 45 WL 180 TO 202. REMOVED CORROSION, OUT OF LIMITS IAW SRM 57-30-1. REPAIRED SKIN IAW UPS EO 727-57-1689. 2 L 7 3 4F A3WE 1996040500290 19960405 00290 NM 1996 4 5 UPS96205816 1 19960328 A 5315 FLOOR BEAM BOEING 727 72727C 138400J NM BS 1130 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON FLOOR BEAM UPPER CHORD STA 1130 LBL 65 WL 207. REMOVED CORROSI ON PER SRM 53010-1 AND REPAIRED FLOOR BEAM IAW UPS EO 727-53-1744. 2 L 7 3 4F A3WE 1996040500291 19960405 00291 NM 1996 4 5 UPS96205817 1 19960328 A 5315 FLOOR BEAM BOEING 727 72727C 138400J NM BS 1130 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON FLOOR BEAM UPPER CHORD STA 1130 RBL 65 WL 207. REMOVED AND REP LACED CHORD PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996040500292 19960405 00292 NM 1996 4 5 UPS96205818 1 19960328 A 5711 SPAR BOEING 727 72727C 138400J NM PNL 7340 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON FRONT SPAR CUTOUT 7340 HAS CORROSION ON THE INSIDE. REPAIRED F RONT SPAR CUTOUT ON INSIDE OF TANK AT PNL 7340, IAW UPS EO 727-57-1687. 2 L 7 3 4F A3WE 1996040500293 19960405 00293 NM 1996 4 5 UPS96205819 1 19960328 A 5330 SKIN BOEING 727 72727C 138400J NM BS 856-864 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED WHILE WORKING NRC 437442 FOUND CORROSION ON FUSELAGE SKIN AT STA 856 TO 864 WL 191 LBL 70.5. REMOVED CORROSION PER UPS EO 96-2154. 2 L 7 3 4F A3WE 1996040500294 19960405 00294 NM 1996 4 5 UPS96505826 1 19960329 A 5320 ANGLE BOEING 757 75724APF 1384969 NM BS 845 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 442UP 27387 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FWD CARGO COMPARTMENT AFT BULKHEAD LOWER SUPPORT ANGLE STA 845 IS DENTED AND CRACKED. REMOVED AND FABRICATED NEW ANGLE AND INSTALLED PER SRM 51-40-2, 51-20-01, 51-30-01 AND MM 20-10-22. 2 L 7 2 4F RT A2NM 1996040500295 19960405 00295 NM 1996 4 5 UPS96505827 1 19960329 A 5753 SKIN BOEING 757 75724APF 1384969 NM RT TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 442UP 27387 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT FRONT WING O/B FLAP MOST O/B SKIN PNL TOP IS CRACKED. REMOVED AND FABRICA TED NEW SKIN PNL AND INSTALLED PER SRM 57-53-01, 51-40-02, 51-40-08, 51-40-05 AND MM 51-20-10. 2 L 7 2 4F RT A2NM 1996040500296 19960405 00296 WP 1996 4 5 UPS96805820 1 19960228 A 5230 FITTING DOUG DC8 DC873F 302199F WP FS 145 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MAIN CARGO DOOR JAMB HAS HEAVY CORROSION ON ATTACH ANGLE FITTING FWD OF NR 1 SPOOL FITTING. REPLACED ANGLE FITTING PER SRM 51-3-0. 2 L 7 4 4F RT 4A25 1996040500297 19960405 00297 WP 1996 4 5 UPS96805821 1 19960303 A 5230 BOLTS DOUG DC8 DC873F 302199F WP FS 145-255 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MAIN CARGO DOOR SPOOL BOLTS 1, 2, 4, 5, 6 AND 7 ARE CORRODED. REPLACED BOLTS PER MM 52-36-01. 2 L 7 4 4F RT 4A25 1996040500298 19960405 00298 WP 1996 4 5 UPS96805822 1 19960308 A 5512 SKIN DOUG DC8 DC873F 302199F WP LT HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT HORIZ STAB L/E SKIN AT ATTACHING SCREW HOLES HAS HEAVY CORROSION AT STA XF S 125 AND XFS 136 UPPER SIDE OF SKIN. REPAIRED SKIN PER SRM 55-2-1. 2 L 7 4 4F RT 4A25 1996040500299 19960405 00299 WP 1996 4 5 UPS96805823 1 19960308 A 5510 FITTING DOUG DC8 DC873F 302199F WP LT HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT HORIZ STAB FITTING HAS CORROSION DAMAGE AT NR 4 STR, STA XFS 135 BOTTOM IN SIDE SKIN. REPLACED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996040500300 19960405 00300 WP 1996 4 5 UPS96805824 1 19960229 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP FS 50-67 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON FINGER DOUBLER FS 50 TO 67 LONGERON 21L. REPLACED FINGER DOUBLER PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1996040500301 19960405 00301 WP 1996 4 5 UPS96805825 1 19960302 A 5312 BLKHD DOUBLER DOUG DC8 DC873F 302199F WP FS 980 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON FWD PRESS BULKHEAD. 2 L 7 4 4F RT 4A25 1996040500302 19960405 00302 NM 1996 4 5 VNAA9600009 1 19960327 A 5610 SPSDO328121 WINDSHIELD DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT COCKPIT DAMAGED A A VNAA K NONE O OTHER CR CRUISE 1 GL 07 426JS 3038 DURING CRUISE AT FL 220, CREW REPORTED HEARING A MODERATE BANG FOLLOWED IMMEDIATELY BY THE OUTER PANE OF CAPTAIN'S WINDS HIELD SHATTERING. CREW CONTINUED ON WITH THE FLIGHT, LANDED IN EVV WITHOUT FURTHER INCIDENT. MX PERSONNEL REPLACED LT WINDSHIELD IAW MM 56-11-00. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996040500303 19960405 00303 EU 1996 4 5 WWMA9600032 1 19960328 A 3320 F815 LAMP SAAB SF340 340B 7860101 EU CABIN FAILED A WWMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 15 245AE 340B245 THE CREW REPORTED A STRONG ELECTRICAL SMELL IN THE AFT CABIN. MAINTENANCE FOUND CABIN LIGHT AT SEAT 14A BURNED. THE LA MP WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE WITH NO FURTHER PROBLEMS. 2 L 7 2 4T RT A52EU 1996040500304 19960405 00304 WP 1996 4 5 96ZZZX1460 1 19960229 A 2697 3766696503 WIRE HARNESS DOUG DC8 DC851 3021920 WP NR 1 ENGINE SHORTED A FXLA O OTHER N FALSE WARNING DE DESCENT 1 SO 19 508DC 45935 ON DESCENT TO MIAMI, RECEIVED INTERMITTENT FIRE WARNING ON NR 1 ENGINE. LANDED MIAMI WITHOUT INCIDENT. INVESTIGATION R EVEALED A SHORTED WIRE IN THE HARNESS. REPAIRED HARNESS AND CHECKED OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4A25 1996040500305 19960405 00305 NM 1996 4 5 96ZZZX1461 1 19960306 A 5240 CORNER BOEING 737 737201 1384454 NM SERVICE DOOR CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 205AU 19421 DEN - DURING AN A-3 CHECK, MAINTENANCE REPORTED A CRACK IN THE FORWARD SERVICE DOOR (R-1). CRACK WAS APPROXIMATELY 1.25 INCHES IN LENGTH AND WAS LOCATED IN THE LOWER FORWARD CORNER. REPAIRED CRACK PER SB 737-52-1070. 2 L 7 2 4F A16WE 1996040500306 19960405 00306 NM 1996 4 5 96ZZZX1462 1 19960222 A 2915 1032261 HYD RELIEF VALVE BOEING 707 707323C 138367D NM LT MLG WW CRACKED A A MIRA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 19 751MA 19582 CCR402 - SBEG/KMIA - LOST UTILITY HYDRAULIC SYSTEM AT 16:52. UNABLE TO LOWER DOWN NOSE GEAR BY HAND CRANK AS WELL AS US E OF THE JOHNSON BAR. FOUND UTILITY SYSTEM RELIEF VALVE HOUSING CRACKED. REPLACED VALVE, SERVICED HYDRAULIC SYSTEM AND OPERATIONAL CHECKED SYSTEM. OK PER MM 29-00-00. AFTER AIRCRAFT WAS POSITIONED WITH A CRANE, PROCEEDED TO EXTEND NOSE GEAR PER THE EMERGENCY PROCEDURES, WHICH OPERATED NORMALLY. AFTER REPOSITIONING AIRCRAFT AT THE HANGAR, JACKED ACFT AND OPERATED NOSE GEAR BOTH HYDRAULICALLY AND MANUALLY THROUGH THE EMERGENCY PROCEDURES (WITH THE GUIDANCE OF NTSB) AND FOU ND ALL SYSTEMS TO OPERATE NORMALLY. 2 L 7 4 4F 4A26 1996040500307 19960405 00307 NM 1996 4 5 96ZZZX1463 1 19960221 A 2910 LINE BOEING 707 707323C 138367D NM HYD SYSTEM LOOSE A MIRA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 19 751MA 19582 OXO502 - SKBO/KMIA - LOST HYDRAULIC FLUID DURING APROACH, INSTALLED NOSE GEAR PIN ACCORDING TO PROCEDURE. QUANTITY INDI CATED LESS THAN 1 GALLON. ADJUSTED AND TIGHTENED HYDRAULIC PRESSURE LINE TO FILTER DUE TO VIBRATION. FILTER BRACKET FO UND BROKEN. REMOVED AND REPLACED BRACKET, CHECKED LINE FOR LEAK. OK PER BMM 29-00-00. RESET NLG PIN. HYDRAULIC FLUID ADDED, INDICATED FULL. 2 L 7 4 4F 4A26 1996040500308 19960405 00308 WP 1996 4 5 96ZZZX1464 1 19960223 A 2421 GENERATOR DOUG DC9 DC932 3022066 WP RIGHT FAILED A VJ6A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 902VV 47177 RDU/RDU - FLT 790 - AIR RETURN, AFTER TAKEOFF, RIGHT GENERATOR FAIL/CROSS TIE LOCK-OUT WARNING. C/W QRH PROCEDURES, DIS CONNECTED RIGHT GENERATOR/CSD. ASSIGNED MEL 24-01-01 CONTROL NR DM7319. 2 L 7 2 4F A6WE 1996040500309 19960405 00309 NM 1996 4 5 96ZZZX1465 1 19960110 A 5610 5893543095 WINDSHIELD BOEING 727 72723 1384004 NM LT COCKPIT CRACKED A NACA A UNSCHED LANDING O OTHER CR CRUISE 1 AL 03 930FT 19387 ANC - FLT 105 - RETURNED TO ANC DUE TO FAILURE OF CAPTAIN'S WINDSHIELD OUTER PANEL. MAINTENANCE REPLACED L1 WINDOW. RE PLACED WINDSHIELD HEAT CONTROLLER AS A PRECAUTIONARY MEASURE. ACFT RETURNED TO SERVICE. 2 L 7 3 4F A3WE 1996040500310 19960405 00310 NE 1996 4 5 96ZZZX1466 2 19960117 A 8530 327627 CYLINDER DOUG DC6 DC6A 3021706 WP PWA R2800 R2800* 52026 NE NR 1 ENGINE CRACKED A NACA E ENGINE SHUTDOWN E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 1377K 1375 44596 P36141 FLT 431 - SHUT DOWN NR 1 ENGINE AT 2245Z DUE TO RAPID BACKFIRING AND LOSS OF POWER. MAINTENANCE REPLACED NR 6 CYLINDER ASSY ON NR 1 ENGINE DUE TO CRACKED HEAD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4R 4 R 6A3 5E8 1996040500311 19960405 00311 1996 4 5 AALA960001 4 19960101 A 2320 4971262 PRINTER DOUG MD11 MD11 3023602 NM CTR PEDESTAL DEFECTIVE A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 1768D 48436 LHR - FLT T0142 - EN ROUTE JFK/LHR DURING CRUISE, SMOKE NOTED COMING FROM ACARS PRINTER FOLLOWED BY ACARS CIRCUIT BREAKE R TRIP. SMOKE DISSIPATED AFTER CIRCUIT BREAKER TRIP AND AIRCRAFT PROCEEDED TO LHR LANDING WITHOUT INCIDENT. PLACARDED ACARS PRINTER INOP AND AIRCRAFT RETURNED TO SERVICE. SUBSEQUENTLY REPLACED ACARS PRINTER. SYSTEM GROUND CHECKED NORMAL OPERATION AND PLACARD REMOVED. (X) 2 L 7 3 4F RT A22WE 1996040500312 19960405 00312 EU 1996 4 5 AALA960114 1 19960118 A 3350 CONDUCTOR AIRBUS 300 A300B4605R 3930308 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 34078 615 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT CROSS AISLE BETWEEN 2L AND 3R DOORS, FOUND INOPERATIVE. REPLACE D EMERGENCY FLOOR LIGHT FLAT CONDUCTOR AT CROSS AISLE BETWEEN 3L AND 3R DOOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A35EU 1996040500313 19960405 00313 EU 1996 4 5 AALA960133 1 19960125 A 3350 A3060720203 LIGHT STRIP AIRBUS 300 A300B4605R 3930308 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 11060 470 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT CROSS AISLE BETWEEN 3L AND 3R, FOUND DOORS INOPERATIVE. REPLACE D EMERGENCY FLOOR LIGHT STRIP AT CROSS AISLE BETWEEN 2L AND 3R DOORS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A35EU 1996040500314 19960405 00314 EU 1996 4 5 AALA960174 1 19960204 A 3350 A3030398101 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 41063 506 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 15B THROUGH 21B FOUND INOPERATIVE. RES ECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR BY PASSENGER SEAT ROW 15B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A35EU 1996040500315 19960405 00315 WP 1996 4 5 AALA960313 1 19960226 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1338 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 253AA 49286 TUL - CORROSION ON FWD SIDE OF FRAME 4 INCHES TO THE LEFT OF LONGERON 3 AND 2 INCHES ABOVE INTERIOR SKIN. SPLICED IN NE W SECTION OF FWD WEB LAYER. REF SRM 53-01, FIGURE 2. TST: 34,543.23 HRS. CYCLES, 19,744. (X) 2 L 7 2 4F A6WE 1996040500316 19960405 00316 WP 1996 4 5 AALA960314 1 19960226 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1338 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 253AA 49286 TUL - CORROSION ON FWD SIDE OF FRAME, 4 INCHES TO THE RIGHT OF LONGERON 30 AND 2 INCHES ABOVE INTERIOR SKIN. SPLICED IN NEW SECTION OF FWD WEB LAYER, REF SRM 53-01, FIGURE 2. TST: 34,543.23 HRS. CYCLES, 19,744. (X) 2 L 7 2 4F A6WE 1996040500317 19960405 00317 WP 1996 4 5 AALA960315 1 19960226 A 5320 CHANNEL DOUG DC9 DC982 3022082 WP BS 1315 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 253AA 49286 TUL - CORROSION AROUND FASTENER INSIDE CABIN FLOOR CHANNEL AT STA 1313, 18 INCHES RIGHT OF CENTER. APPLIED DOUBLER PER SRM 5301, FIGURE 2, SHEET 3. TST: 34,543, CYCLES, 19,744. (X) 2 L 7 2 4F A6WE 1996040500318 19960405 00318 WP 1996 4 5 AALA960323 1 19960228 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 1300 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 253AA 49286 TUL - CORROSION ON LONGERON 23R AT STA 1300. INSTALLED LONGERON REPAIR SPLICE PER SRM 53-02, FIGURE 5, PAGE 6. TST: 3 4,543.23. CYCLES, 19,744. (X) 2 L 7 2 4F A6WE 1996040500319 19960405 00319 NM 1996 4 5 AALA960324 1 19960227 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1148-1166 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - SKIN CORRODED AND BULGED OUT BOTTOM OF THE AFT LAV PANEL. INSTALLED DOUBLER PER ESO 11697, DATED 2-16-96. TST: 4 3,536. CYCLES, 21,736. (X) 2 L 7 3 4F A3WE 1996040500320 19960405 00320 NM 1996 4 5 AALA960325 1 19960227 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1096 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 701AA 22459 TUL - CROWN SKIN CRACKED IN 2 PLACES AT STA 1096 EACH SIDE STR 1 AT INLET DOGHOUSE ATTACH ANGLE. CUT OUT CRACKED AREAS AND INSTALLED DOUBLER PER SB 727-53A-204, REV 3, AND SRM 53-30-3, PAGES 12-14A. TST: 41,903 HRS. CYCLES, 22,088. (X) 2 L 7 3 4F A3WE 1996040500321 19960405 00321 NM 1996 4 5 AALA960326 1 19960227 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1011 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - STA 1011 - SKIN IS CORRODED BETWEEN STR 29L AND STR 30. REPAIRED WITH DOUBLER PER SRM 53-30-3. TST: 43,536. CY CLES 21,736. (X) 2 L 7 3 4F A3WE 1996040500322 19960405 00322 NM 1996 4 5 AALA960327 1 19960227 A 5320 WEB BOEING 727 727223 1384074 NM BS 950 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - CORROSION ON WEB AT FWD LWR CORNER OF NR 2 CARGO DOOR OPENING, CORRODED AFT OF FWD FITTING. REMOVED (CUT OUT) 6 I NCH SECTION OF CORRODED WEB AT BOTTOM FWD CARGO DOOR OPENING AND SPLICED IN NEW SECTION OF WEB PER SRM 51-40-2, PAGE 5 ( TYP WEB REPAIR). TST: 43,536 HRS. CYCLES, 21,736. (X) 2 L 7 3 4F A3WE 1996040500323 19960405 00323 NM 1996 4 5 AALA960328 1 19960227 A 5330 SKIN BOEING 727 727223 1384074 NM BS 680 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - CORROSION ON SKIN AND SKIN BUTT SPLICE DOUBLER. BLENDED OUT CORROSION PER SRM 51-10-6, AND INSTALLED DOUBLER OVER DAMAGED AREA PER ESO 11697 (AS REVISED 02-21-96) . TST: 43,536 HRS. CYCLES, 21,736. (X) 2 L 7 3 4F A3WE 1996040500324 19960405 00324 NM 1996 4 5 AALA960332 1 19960225 A 3350 1722331 CONNECTOR BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 355AA 24036 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 22AB FOUND INOPERATIVE. REPLACED BROKEN EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT 22AB. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1996040500325 19960405 00325 NM 1996 4 5 AALA960333 1 19960225 A 3350 1722331 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 353AA 24034 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT PASSENGER SEATS 21H AND 23H FOUND INOPERATIVE. SYSTEM GROUND CHE CKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1996040500326 19960405 00326 WP 1996 4 5 AALA960334 1 19960226 A 2170 21D101 COALESCER DOUG DC9 DC982 3022082 WP ACM BAY DIRTY A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 434AA 49452 DFW - FLT T0429 - EN ROUTE MEM/DFW, SLIGHT BURNING ODOR NOTED DURING ALL PHASES OF FLIGHT WITH NO OTHER ABNORMAL INDICAT IONS. AIRCRAFT LANDED DFW WITHOUT INCIDENT. REPLACED ALL COALESCER BAGS AND ACCOMPLISHED GROUND ENGINE RUN WITH NO DEF ECTS FOUND. ACCOMPLISHED FUNCTIONAL CHECK FLIGHT WITH NO ODOR OR OTHER DEFECTS FOUND. SYSTEM OPERATIONAL CHECKED NORMA L. (X) 2 L 7 2 4F A6WE 1996040500327 19960405 00327 NM 1996 4 5 AALA960335 1 19960227 A 3350 0201922001 HOUSING BOEING 767 767223 1385123 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 315AA 22317 SFO - DURING OVERNIGHT CHECK, EMERGENCY LIGHT AT PASSENGER SEAT 28B FOUND INOPERATIVE. REPLACED EMERGENCY LIGHT HOUSING AT PASSENGER SEAT 28B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1996040500328 19960405 00328 WP 1996 4 5 AALA960336 1 19960228 A 2170 21D101 COALESCER DOUG DC9 DC982 3022082 WP ACM BAY DIRTY A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 427AA 49339 DFW - FLT T2094 - AFTER TAKEOFF PSP DURING INITIAL CLIMB-OUT, SLIGHT BURNING ODOR NOTED IN COCKPIT AND CABIN. ODOR DISS IPATED AFTER CLIMB POWER SELECTED AND AIRCRAFT PROCEEDED TO DFW LANDING WITHOUT INCIDENT. REPLACED ALL COALESCER BAGS. ACCOMPLISHED GROUND ENGINE RUN WITH NO DEFECTS OR ODOR NOTED. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1996040500329 19960405 00329 WP 1996 4 5 AALA960337 1 19960228 A 2170 21D101 COALESCER DOUG DC9 DC982 3022082 WP ACM BAY DIRTY A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 468AA 49598 DFW - FLT T1341 - AFTER TAKEOFF MEM DURING INITIAL CLIMB-OUT, SLIGHT ODOR NOTED IN COCKPIT AND CABIN. ODOR DISSIPATED A FTER 10 MINUTES OF FLIGHT AND AIRCRAFT PROCEEDED TO DFW LANDING WITHOUT INCIDENT. REPLACED ALL COALESCER BAGS. ACCOMPL ISHED GROUND ENGINE RUN WITH NO DEFECTS OR ODOR NOTED. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1996040500330 19960405 00330 WP 1996 4 5 AALA960340 1 19960227 A 5320 JAMB DOUG DC9 DC982 3022082 WP BS 636-693 OUT OF ADJUST A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 253AA 49286 TUL - MID-CARGO DOOR BEAM (LOWER) FWD AND AFT STOP PAD AREA OUT OF LIMITS. INSTALLED DOUBLERS ON LOWER DOOR BEAM FWD OF AFT STOPS PER AARD 53-10-00-03 AND ESO 80559, DATED 2-26-96. TST: 34,543. CYCLES, 19,744. (X) 2 L 7 2 4F A6WE 1996040500331 19960405 00331 NM 1996 4 5 AALA960343 1 19960301 A 5753 SKIN DOUG MD11 MD11 3023602 NM TE FLAP DELAMINATED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1752K 48421 TUL - TRAILING EDGE OF OUTBOARD FLAP HAS SEVERAL AREAS OF DELAMINATION. REPAIRED PER ESO 41000 DATED 2-28-96. TST: 18 ,473 HRS. CYCLES, 3,001. (X) 2 L 7 3 4F RT A22WE 1996040500332 19960405 00332 WP 1996 4 5 AALA960344 1 19960228 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1309 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 269AA 49292 TUL - CORROSION ON BELL FRAME STA 1309, L30 TO 29 LEFT. INSTALLED DOUBLER, REF SRM 53-03, PAGE 4E. TST: 32,711 HRS. C YCLES, 18,961. (X) 2 L 7 2 4F A6WE 1996040500333 19960405 00333 WP 1996 4 5 AALA960354 1 19960304 A 3260 833703 SENSOR ELDEC DOUG DC9 DC982 3022082 WP RT MLG DEFECTIVE A AALA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 469AA 49599 ORD - FLT T1716 - DURING APPROACH TO ORD WHEN LANDING GEAR EXTENDED, RT MLG RED LIGHT REMAINED ILLUMINATED. RECYCLED LA NDING GEAR AND RED LIGHT EXTINGUISHED AFTER 2 MINUTES. AIRCRAFT LANDED ORD WITHOUT INCIDENT. REPLACED RT MLG DOWNLOCK SENSOR. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1996040500334 19960405 00334 WP 1996 4 5 AALA960358 1 19960305 A 5347 TIE DOWN TRACK DOUG DC9 DC982 3022082 WP BS 1003-1151 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 253AA 49286 TUL - FORWARD TIE-DOWN TRACK HAS CORROSION AFT END, LEFT. REMOVED AND REPLACED LEFT FWD TIE-DOWN TRACK. TST: 34,543.2 3 HRS. CYCLES, 19,744. (X) 2 L 7 2 4F A6WE 1996040500335 19960405 00335 NM 1996 4 5 BJNA96301 1 19960306 A 3350 P4010020 BATTERY PACK BOEING 737 737214 138446R NM CABIN DISCHARGED A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 457TM 20156 L2 DOOR EMERGENCY LIGHTS ARE DIM. REMOVED AND REPLACED L2 DOOR EMERGENCY LIGHTS BATTERY PACK. OPS CHECK GOOD. (X) 2 L 7 2 4F A16WE 1996040500336 19960405 00336 WP 1996 4 5 HAL96016 1 19960129 A 5310 STRUCTURE DOUG DC9 DC951 3022051 WP FUSELAGE CORROSION A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 673MC 42576 47726 HNL - SURFACE CORROSION RT SIDE FUSELAGE BELOW FWD OVERWING EXIT, LEVEL 1. SUBSEQUENTLY, UPGRADED TO MODERATE CORROSION , LEVEL 2. CLEANED AND TREATED PER SRM 51-10-3. INSTALLED INTERIM REPAIR PER HAL M105, FILE NR 64088. TRANSCRIBED TO FORM 46, NR 144223, PENDING PERMANENT REPAIR. AIRCRAFT TT: 42,576 HRS. AIRCRAFT TOTAL CYCLES, 56,230. (X) 2 L 7 2 4F A6WE 1996040500337 19960405 00337 WP 1996 4 5 HAL9620 1 19960308 A 2612 59585791 CONNECTOR DOUG DC9 DC951 3022051 WP NR 2 FIRE LOOP FAILED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 601AP 47658 HNL - FLT 202 - B-LOOP RIGHT ENGINE FIRE DETECTOR IS INOPERATIVE. RESPLICED NEW LOOP CONNECTOR. THE OPERATIONAL CHECK WAS OK. (X) 2 L 7 2 4F A6WE 1996040500338 19960405 00338 WP 1996 4 5 HAL9622 1 19960310 A 3350 60030431 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 669HA 2226 47654 HNL - MAINTENANCE - LT AFT EMERGENCY EXIT LIGHT WILL NOT TURN OFF. REPLACED BATTERY POWER PACK. OPERATONAL CHECK OK. ( X) 2 L 7 2 4F A6WE 1996040500339 19960405 00339 WP 1996 4 5 IXXA9610 1 19960207 A 5347 2772660 SEAT TRACK DOUG DC8 DC862F 3021972 WP FS 530 DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 46129 DURING THE C-CHECK INSPECTION, A SEAT TRACK AT FS 530 WAS FOUND DAMAGED. A REPAIR WAS PERFORMED TO THE TRACK BY THE INS TALLATION OF A PLUG PER ATI E.O. 53-DC8-219, AND DRAWING SKA95253-2, REV: IR, SHEETS 1 AND 2, DATED 1-4-96. THIS REPAIR WAS APPROVED BY FAA FORM 8110-3. (X) 2 L 7 4 4F 4A25 1996040500340 19960405 00340 WP 1996 4 5 IXXA9611 1 19960207 A 5347 2772660 SEAT TRACK DOUG DC8 DC862F 3021972 WP FS 440 DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 46129 DURING THE C-CHECK INPSECTION, A SEAT TRACK AT FS 440 WAS FOUND DAMAGED. A REPAIR WAS PERFORMED TO THE TRACK BY THE INS TALLATION OF A PLUG PER ATI E.O. 53-DC8-220, AND DRAWING SKA95253-1, REV: IR, SHEETS 1 AND 2, DATED 1-4-96. THIS REPAI R WAS APPROVED BY FAA FORM 8110-3. (X) 2 L 7 4 4F 4A25 1996040500341 19960405 00341 WP 1996 4 5 IXXA9612 1 19960207 A 5320 DOOR FRAME DOUG DC8 DC862F 3021972 WP FS 1190 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 61236 10413 46129 DURING THE C-CHECK INSPECTION, CORROSION WAS FOUND AT THE RT JET ESCAPE DOOR LOCATED ON THE FWD LOWER CORNER. A REPAIR WAS PERFORMED PER ATI E.O. 53-DC8-224, AND DRAWING SKA95253-6, REV: IR, DATED 1-6-96. (X) 2 L 7 4 4F 4A25 1996040500342 19960405 00342 WP 1996 4 5 IXXA9613 1 19960207 A 5553 ANGLE DOUG DC8 DC862F 3021972 WP LT VERT STAB CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 61236 10413 46129 DURING THE C-CHECK INSPECTION, THE VERTICAL STAB TO FUSELAGE ATTACH ANGLE WAS FOUND CORRODED AND CRACKED ON THE LT FROM FORWARD OF THE FRONT SPAR TO CENTER SPAR. A REPAIR WAS PERFORMED PER ATI E.O. 53-DC8-223, AND DRAWING SKA95253-5, REV: A, DATED 1-23-96. THIS REPAIR WAS APPROVED ON FAA FORM 8110-3. (X) 2 L 7 4 4F 4A25 1996040500343 19960405 00343 WP 1996 4 5 IXXA9614 1 19960207 A 5320 FITTING DOUG DC8 DC862F 3021972 WP FS 490-500 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 61236 10413 46129 DURING THE C-CHECK INSPECTION, EXFOLIATED CORROSION WAS FOUND AT FS 490 TO FS 500 LOCATED IN THE FWD LOWER CARGO BILGE, LONGERON 33L-34L INSIDE THE TORQUE BOX TO SKIN ATTACH ANGLES. INSTALLED NEW FITTING AT FS 492 AND LONGERONS 33L-34L IAW DACO SRM 51-1-8 AND SRM 53-2-0. A REPAIR WAS PERFORMED PER THE ATI DRAWING SKA95253-7 AND WAS APPROVED ON FAA FORM 811 0-3. (X) 2 L 7 4 4F 4A25 1996040500344 19960405 00344 WP 1996 4 5 IXXA9615 1 19960207 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FS 500 DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 61236 10413 46129 DURING THE C-CHECK INSPECTION, THE FRAME AT FS 500, LONGERON L35R WAS FOUND DAMAGED. A REPAIR WAS ACCOMPLISHED PER ATI DRAWING SKA95253-7, REV: IR, DATED 1-20-96 AND WAS APPROVED BY FAA FORM 8110-3. (X) 2 L 7 4 4F 4A25 1996040500345 19960405 00345 WP 1996 4 5 IXXA9616 1 19960207 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FS 740 DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 61236 10413 46129 DURING THE C-CHECK INSPECTION, FOUND A MISDRILLED HOLE IN FRAME AT FS 740R. THIS HOLE WAS REPAIRED PER ATI E.O. 53-DC8- 221 AND ATI DRAWING SKA95253-3, REV: IR, DATED 1-16-96 WHICH WAS APPROVED ON FAA FORM 8110-3. (X) 2 L 7 4 4F 4A25 1996040500346 19960405 00346 WP 1996 4 5 IXXA9617 1 19960207 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FS 460 DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 61236 10413 46129 DURING THE C-CHECK INSPECTION, FOUND A MISDRILLED HOLE IN FRAME AT FS 460R. THIS HOLE WAS REPAIRED PER ATI E.O. 53-DC8-2 22, AND ATI DRAWING SKA95253-4, REV: IR, DATED 1-6-96 AND IS APPROVED BY FAA FORM 8110-3. (X) 2 L 7 4 4F 4A25 1996040500347 19960405 00347 WP 1996 4 5 IXXA9626 1 19960226 A 5320 SUPPORT DOUG DC8 DC871 302199A WP FS 1460 CORROSION A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 71231 22629 46065 DURING THE D-CHECK INSPECTION, FOUND CORROSION ON STRUT SUPPORT LOWER LT SIDE AT FS 1460 IN THE AFT CARGO COMPARTMENT. A REPAIR WAS ACCOMPLISHED PER DACO SRM 51-1-21, 51-1-8, AND 51-00. (X) 2 L 7 4 4F 4A25 1996040500348 19960405 00348 WP 1996 4 5 IXXA9627 1 19960226 A 5320 ANGLE DOUG DC8 DC871 302199A WP FS 600 CORROSION A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 71231 22629 46065 DURING THE D-CHECK INSPECTION, FOUND CORROSION ON FLOOR SUPPORT ANGLE AT FS 600, L34R TO L34L, IN THE FWD CARGO COMPARTM ENT. A REPAIR WAS ACCOMPLISHED PER DACO SRM 51-1-21, 51-1-8, AND 51-00. (X) 2 L 7 4 4F 4A25 1996040500349 19960405 00349 WP 1996 4 5 IXXA9628 1 19960226 A 5320 ANGLE DOUG DC8 DC871 302199A WP FS 580 CORROSION A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 71231 22629 46065 DURING THE D-CHECK INSPECTION, FOUND CORROSION ON FLOOR SUPPORT ANGLE AT FS 580, L33R TO L33L, IN THE FWD CARGO COMPARTM ENT. A REPAIR WAS ACCOMPLISHED PER DACO SRM 51-1-21, 51-1-8, AND 51-00. (X) 2 L 7 4 4F 4A25 1996040500350 19960405 00350 WP 1996 4 5 IXXA9629 1 19960226 A 5210 SKIN DOUG DC8 DC871 302199A WP AFT PAX DOOR CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 71231 22629 46065 DURING THE D-CHECK INSPECTION, FOUND A CRACK ON THE AFT PASSENGER DOOR ON THE LOWER AFT CORNER. A REPAIR WAS PERFORMED PER DACO SRM 53-2-0, 51-1-20D, 51-1-21A, 51-1-8, 51-00, AND DRAWING CF-N820BX-13/96. (X) 2 L 7 4 4F 4A25 1996040500351 19960405 00351 WP 1996 4 5 IXXA9630 1 19960226 A 5400 FITTING DOUG DC8 DC871 302199A WP NR 1 PYLON CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 71231 22629 46065 DURING THE D-CHECK INSPECTION, FOUND A CRACK ON THE NR 1 PYLON SUPPORT FITTING AT FS YN 387 IN 2EA LOCATIONS. MANUFACTU RED FITTING PER DACO DRAWING 5756790 AND INSTALL FITTING PER DACO DRAWINGS 5756791, 5756801, AND DACO SRM 51-00, 51-1-20 , 51-3-0, AND 51-1-8. (X) 2 L 7 4 4F 4A25 1996040500352 19960405 00352 WP 1996 4 5 IXXA9631 1 19960226 A 5230 SKIN DOUG DC8 DC871 302199A WP FS 1420 DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 71231 22629 46065 DURING THE D-CHECK INSPECTION, FOUND DENTS IN THE OUTER SKIN OF THE AFT LOWER CARGO DOOR. REPAIR WAS PERFORMED PER DACO SRM 52-4-1,52-2-0, 51-1-4, 51-1-8, AND 51-1-21A. (X) 2 L 7 4 4F 4A25 1996040500353 19960405 00353 WP 1996 4 5 IXXA9632 1 19960226 A 5312 BLKHD COVER DOUG DC8 DC871 302199A WP FS 857.125 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 71231 22629 46065 DURING THE D-CHECK INSPECTION, FOUND CRACKS ON THE BULKHEAD COVER AT FS 857.125. REPAIR WAS PERFORMED PER DACO SRM 51- 1-4, 51-1-8, 51-1-21, AND 53-2-0. (X) 2 L 7 4 4F 4A25 1996040500354 19960405 00354 WP 1996 4 5 IXXA9633 1 19960226 A 5311 FRAME DOUG DC8 DC871 302199A WP FS 781.500 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 71231 22629 46065 DURING THE D-CHECK INSPECTION, FOUND CRACKS ON FRAME AT FS 781.500, L35R. REPAIR WAS PERFORMED PER DACO SRM 53-8-1,51-1 -4, 51-1-8, AND 51-1-21. (X) 2 L 7 4 4F 4A25 1996040500355 19960405 00355 WP 1996 4 5 IXXA9634 1 19960226 A 5320 WEB DOUG DC8 DC871 302199A WP FS 781.500 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 71231 22629 46065 DURING THE D-CHECK INSPECTION, FOUND CRACKS ON RT WEB AT FS 781.500. REPAIR WAS ACCOMPLISHED PER DACO SRM 53-8-1, 51-1- 4, 51-1-8, 53-2-0, AND 51-1-21. (X) 2 L 7 4 4F 4A25 1996040500356 19960405 00356 WP 1996 4 5 ORJA96006 1 19960217 A 3246 2601483 BOLT BENDIX 26088911 DOUG DC9 DC983 3022083 WP NR 4 MAIN WHEEL MISSING A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 871RA 5204 49788 THROUGH-BOLT MISSING, NR 4 TIRE. REMOVED AND REPLACED NR 4 MAIN WHEEL ASSY IAW 32-40-01. (X) 2 L 7 2 4F RT A6WE 1996040500357 19960405 00357 WP 1996 4 5 ORJA96007 1 19960219 A 3246 2601483 BOLT BENDIX 26088911 DOUG DC9 DC983 3022083 WP NR 4 MAIN WHEEL BROKEN A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 879RA 2537 53185 NR 4 MAIN TIRE HAS BROKEN THROUGH-BOLT. REMOVED AND REPLACED NR 4 MAIN TIRE FOR BROKEN THROUGH-BOLT PER MM 32. (X) 2 L 7 2 4F RT A6WE 1996040500358 19960405 00358 WP 1996 4 5 ORJA96008 1 19960220 A 3350 LENS DOUG DC9 DC987 3022087 WP CABIN MISSING A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 751RA 49779 'E' PATH LAMP AT ROW 26 MISSING A LENS. INSTALLED A NEW LENS FOR 'E' PATH LAMP AT ROW 26. (X) 2 L 7 2 4F RT A6WE 1996040500359 19960405 00359 WP 1996 4 5 ORJA96009 1 19960221 A 3350 RPS1 POWER SUPPLY DOUG DC9 DC987 3022087 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 752RA 7775 49780 ROW 23 TO EMP. FLOOR TRACK LIGHTING INOPERATIVE. INSTALLED NEW POWER SUPPLY. OPS CHECK NORMAL. (X) 2 L 7 2 4F RT A6WE 1996040500360 19960405 00360 WP 1996 4 5 ORJA96010 1 19960220 A 3350 LIGHT SOCKET DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 833RA 53045 AFT EMERGENCY LIGHT SOCKET BAD, AFT EMPENNAGE. REMOVED AND REPLACED ASSY, OPS NORMAL. (X) 2 L 7 2 4F RT A6WE 1996040500361 19960405 00361 WP 1996 4 5 ORJA96011 1 19960221 A 3246 26088911 TIE BOLT DOUG DC9 DC987 3022087 WP NR 4 MLG WHEEL BROKEN A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 754RA 2836 49641 REMOVED AND REPLACED NR 4 MAIN WHEEL ASSY (PN 26088911). REMOVED AND REPLACED NR 4 MAIN WHEEL ASSY DUE TO BROKEN TIE BO LT IAW MM 32. (X) 2 L 7 2 4F RT A6WE 1996040500362 19960405 00362 WP 1996 4 5 ORJA96012 1 19960223 A 3350 LENS DOUG DC9 DC987 3022087 WP CABIN MISSING A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 751RA 49779 THREE FLOOR EMERGENCY TRACK LIGHT LENSES MISSING. REPLACED MISSING LENSES IN FLOOR EMERGENCY LIGHTS. (X) 2 L 7 2 4F RT A6WE 1996040500363 19960405 00363 WP 1996 4 5 RAIA960224 2 19960217 A 7320 89778025 FUEL CONTROL BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT ENGINE OUT OF ADJUST A RAIA O OTHER O OTHER CL CLIMB 1 CE 03 432AM 11033 1495 883 66322 STL - FLT 7434 - LEFT ENGINE RPM 98.5 PERCENT IN CLIMB AFTER TAKEOFF. MAINTENANCE ADJUSTED LEFT ENGINE RPM, PERFORMED G ROUND RUNS. OPERATIONAL CHECK GOOD. ENGINE TT: 6,854.5 HRS. (X) 2 L 7 2 4T 4 T RT A56EU E4WE 1996040500364 19960405 00364 1996 4 5 RAIA960225 4 19960219 A 3442 MI5853505 RT UNIT AEROSP ATR72 ATR72202 8680940 EU RADAR SYSTEM FAILED A RAIA O OTHER O OTHER CR CRUISE 1 CE 03 723TE 16389 283 STL - FLT 7144 - RADAR PAINTS GROUND ONLY IN BANK. TI6TL INOP, DOES NOT PAINT WEATHER. MAINTENANCE REPLACED RADAR RT. PERFORMED OPERATIONAL TEST OF SYSTEM, TESTS GOOD. (X) 2 H 7 2 4T RT A53EU 1996040500365 19960405 00365 EU 1996 4 5 RAIA960306 1 19960305 A 2730 48635028010 INDICATOR AEROSP ATR42 ATR42300 8680920 EU PITCH TRIM FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 03 426TE 11490 228 STL - FLT 7408 - PITCH TRIM INDICATOR CIRCUIT BREAKER TRIPPED. REPLACED PITCH TRIM INDICATOR. (X) 2 H 7 2 4T RT A53EU 1996040500366 19960405 00366 EU 1996 4 5 RAIA960307 1 19960305 A 3350 7012210 LAMP AEROSP ATR72 ATR72202 8680940 EU CABIN INOPERATIVE A RAIA K NONE L NO TEST TX TAXI/GRND HDL 1 CE 03 721TE 217 STL - FLT 7003 - EMERGENCY ESCAPE PATH LIGHT INOPERATIVE AT ROW 6. REPLACED LAMPS. (X) 2 H 7 2 4T RT A53EU 1996040500367 19960405 00367 NE 1996 4 5 SRAA39602 2 19960307 A 7532 BLEED VALVE BOEING 747 747212B 1384886 NM PWA JT9 JT9D7J 52054 NE NR 3 ENGINE FAILED A SRAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 23 745SJ 20888 FLT 201 - AFTER TAKEOFF WHEN PACKS WERE TURNED ON, CREW NOTICED OILY FUMES IN COCKPIT, CLOSED NR 3 ENGINE BLEED VALVE AN D FUMES STOPPED. PERFORMED ENGINE RUN-UP, FOUND NR 3 ENGINE N2 SPEED NOT AT IDLE. UP-TRIMMED GROUND IDLE AND OPS CHECK ED GOOD ON GROUND, NO FUMES NOTED IN COCKPIT. (X) 2 L 7 4 4F 4 F A20WE E20EA 1996040500368 19960405 00368 WP 1996 4 5 TC8A96005 1 19960307 A 2910 HYDRAULIC LINE DOUG DC8 DC862 3021970 WP NR 3 ENGINE LEAKING A TC8A A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 23 803MG 45910 SCDA/KMIA - FLT 06603 - LOSS OF HYDRAULIC QUANTITY, PRESSURE NORMAL. FOUND NR 3 ENGINE HYDRAULIC PUMP CASE DRAIN LINE L EAKING. REPLACED LINE, RUN-UP CHECKS NORMAL. SERVICED HYDRAULICS. (X) 2 L 7 4 4F 4A25 1996040500378 19960405 00378 NM 1996 4 5 TSAA9653004 1 19960306 A 5330 SKIN BOEING 737 7372M6C 1384708 NM BS 747 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 21809 DURING OVERNIGHT CHECK, DISCOVERED FUSELAGE SKIN CRACK 1 INCH IN LENGTH AT BS 747 PLUS 3 AT STR 17L. REPAIRED END OF CR ACK WITH HFEC. REPAIRED PER SRM 53-30-3, FIGURE 25. AIRCRAFT RETURNED TO SERVICE. TAT: 35026.06 HRS. TAC: 39,796. (X) 2 L 7 2 4F RT A16WE 1996040500379 19960405 00379 1996 4 5 WRLA96013 4 19960306 A 3425 2594862908 ADI DOUG DC10 DC1030F 3023504 WP CAPTAIN FAILED A A WRLA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 EA 27 107WA 46836 IMMEDIATELY AFTER TAKEOFF DURING INITIAL CLIMB, FLIGHT CREW NOTED CAPTAIN ATTITUDE DIRECTIONAL INDICATOR (ADI) FAILED (A TTITUDE FLAG IN VIEW). FLIGHT CREW ELECTED TO RETURN TO THE POINT OF DEPARTURE. FUEL WAS DUMPED TO BRING ACFT BELOW MA XIMUM LANDING. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL CONFIRMED ADI FAILED. REPLACED ADI. G ROUND OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 3 4F RT A22WE 1996040500380 19960405 00380 NM 1996 4 5 ASAA9610025 1 19960307 A 3350 86210144 BATTERY PACK BOEING 737 737298C 1384490 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING MAINTENANCE CHECK, THE SMOKE BARRIER EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHT OPERATED NORMALLY. (W) 2 L 7 2 4F RT A16WE 1996040500381 19960405 00381 NM 1996 4 5 ASAA9610033 1 19960311 A 5315 65549141 FLOOR BEAM BOEING 737 737290C 138448V NM BS 500B CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING D-CHECK, CORROSION WAS FOUND ON THE FLOOR BEAM AT BS 500B LBL 8 TO 43 ON THE UPPER SURFACE OF THE LOWER FOR WARD FLANGE. CORROSION IS AROUND THE FASTENER HOLES USED TO SECURE THE CEILING PANELS FOR THE LOWER CARGO COMPARTMENT. REPAIRED PER EA 531001401 AND BOEING TELEX ASA-SEA 960076RR. (W) 2 L 7 2 4F A16WE 1996040500382 19960405 00382 NM 1996 4 5 ASAA9610034 1 19960311 A 5315 65549102 FLOOR BEAM BOEING 737 737290C 138448V NM BS 867 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING D-CHECK, CORROSION WAS FOUND ON THE FLOOR BEAM LOWER FLANGE BS 867 AT EACH FASTENER HOLE USED TO SECURE THE CEILING PANELS FOR THE AFT CARGO COMPARTMENT. REPAIRED PER EA 531001414 AND BOEING TELEX ASA-SEA 960108RR. (W) 2 L 7 2 4F A16WE 1996040500383 19960405 00383 NM 1996 4 5 ASAA9610036 1 19960313 A 3350 6013211 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING MAINTENANCE CHECK, THE AFT SERVICE DOOR AND AFT ENTRY DOOR EXTERIOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE . REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W) 2 L 7 2 4F RT A16WE 1996040500384 19960405 00384 NM 1996 4 5 ASAA9610037 1 19960313 A 5315 65549101 FLOOR BEAM BOEING 737 737290C 138448V NM BS 847 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING D-CHECK, CORROSION WAS FOUND ON THE FLOOR BEAM LOWER FLANGE, BS 847 AT EACH FASTENER HOLE USED TO SECURE TH E CEILING PANELS IN THE AFT CARGO COMPARTMENT. REPAIRED PER EA 531001416 AND BOEING TELEX ASA-SEA 960108RR. (W) 2 L 7 2 4F A16WE 1996040500385 19960405 00385 NM 1996 4 5 ASAA9610038 1 19960313 A 5315 56549081 FLOOR BEAM BOEING 737 737290C 138448V NM BS 787 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING D-CHECK, CORROSION WAS FOUND ON THE FLOOR BEAM LOWER FLANGE, BS 787 AT EACH FASTENER HOLE USED TO SECURE TH E CEILING PANELS IN THE AFT CARGO COMPARTMENT. REPAIRED PER EA 531001415 AND BOEING TELEX ASA-SEA 960108RR. (W) 2 L 7 2 4F A16WE 1996040500386 19960405 00386 NM 1996 4 5 ASAA9610039 1 19960314 A 3350 883200312 BATTERY BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING CREW PREFLIGHT, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHTS ILLUMINATED AT ROW 18. REMOVED AND REPLAC ED BATTERY AND LIGHTS OPERATED NORMALLY. (W) 2 L 7 2 4F A16WE 1996040500387 19960405 00387 NM 1996 4 5 ASAA9610040 1 19960315 A 3350 20131A BATTERY BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS FAILED AT ROWS 5, 14 AND 18. REPLACED RESPECTIVE BATTERIES AND LIGHTS OPERATED NORMALLY. (W) 2 L 7 2 4F A16WE 1996040500388 19960405 00388 NM 1996 4 5 ASAA9610041 1 19960318 A 5311 6545801512 FRAME BOEING 737 737290C 138448V NM BS 227 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING D-CHECK, CORROSION WAS FOUND ON THE BULKHEAD FRAME LOWER SECTION AT BS 227, BL 0. REPAIRED PER EA 53100142 1 AND BOEING TELEX ASA-SEA-960136RR. (W) 2 L 7 2 4F A16WE 1996040500389 19960405 00389 NM 1996 4 5 ASAA9610042 1 19960318 A 3350 8821004 BATTERY PACK BOEING 737 737210C 1384459 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 744AS 21822 SEA - DURING CREW PREFLIGHT, THE CREW REPORTED THAT THE AFT EMERGENCY FLOOR TRACK LIGHTS STAYED ON WITH THE SWITCH IN TH E OFF POSITION. REMOVED AND REPLACED BATTERY PACK. (W) 2 L 7 2 4F A16WE 1996040500390 19960405 00390 NM 1996 4 5 ASAA9640017 1 19960306 A 3350 MS250851 LIGHT SW BOEING 737 7374Q8 NM AFT F/A STA INOPERATIVE A ASAA K NONE L NO TEST UK UNKNOWN 1 NM 01 780AS 25112 SEA - FLT 103 - EMERGENCY EXIT LIGHTS WILL NOT TURN ON FROM AFT EMERGENCY LIGHT SWITCH. LIGHTS FAILED FROM AFT F/A STA WITH FLIGHT DECK SWITCH IN 'ARM' . CYCLED BOTH SWITCHES TO OFF AND BACK ON, EMERGENCY EXIT LIGHTS OPERATED NORMALLY IN ALL SWITCH POSITIONS. (W) 2 L 7 2 4F RT A16WE 1996040500391 19960405 00391 NM 1996 4 5 ASAA9640018 1 19960308 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 775AS 25108 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 14 TO 17 WERE FOUND INOPERATIVE. RECONNEC TED WIRING HARNESS AND LIGHTS OPERATED NORMALLY. (W) 2 L 7 2 4F RT A16WE 1996040500392 19960405 00392 NM 1996 4 5 ASAA9640019 1 19960311 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 774AS 25107 SEA - DURING MAINTENANCE CHECK, THE AFT FIVE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTE D LIGHTS/WIRING AND LIGHTS OPERATED NORMALLY. (W) 2 L 7 2 4F RT A16WE 1996040500393 19960405 00393 NM 1996 4 5 ASAA9640020 1 19960311 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 776AS 25109 SEA - FLT 230 - DURING CREW PREFLIGHT, THE CREW REPORTED THAT THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE INOPERATIVE ROW S 20 TO 26. REPAIRED WIRING AND LIGHTS OPERATED NORMALLY. (W) 2 L 7 2 4F RT A16WE 1996040500394 19960405 00394 WP 1996 4 5 ASAA9680067 1 19960305 A 3260 SR092700343 SWITCH ASSY DOUG DC9 DC983 3022083 WP LT THROTTLE DEFECTIVE A ASAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 01 973AS 53449 SEA - CREW REPORTED, THE LANDING GEAR AURAL WARNING SOUNDED AFTER GEAR HANDLE WAS RAISED AND ALL LANDING GEAR UNSAFE LIG HTS REMAINED ON AFTER LANDING GEAR RETRACTED AFTER TAKEOFF. LOWERED LANDING GEAR AND LANDED WITHOUT INCIDENT. REPLACED THE LEFT THROTTLE SWITCH ASSEMBLY AND ACCOMPLISHED LANDING GEAR RETRACTION/EXTENSION TEST AND OPERATED NORMALLY. (W) 2 L 7 2 4F RT A6WE 1996040500395 19960405 00395 WP 1996 4 5 ASAA9680068 1 19960306 A 3350 60030431 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 962AS 53076 PDX - DURING MAINTENANCE CHECK, THE EMERGENCY LIGHTS IN THE TAIL CONE AREA WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND OPERATED NORMALLY. (W) 2 L 7 2 4F RT A6WE 1996040500396 19960405 00396 WP 1996 4 5 ASAA9680069 1 19960307 A 3222 MS288892 SCHRADER VALVE DOUG DC9 DC982 3022082 WP NLG STRUT LEAKING A ASAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 01 954AS 49387 SEA - CREW REPORTED, THE NOSE LANDING GEAR DID NOT RETRACT ON FIRST ATTEMPT, CYCLED GEAR AND RETRACTED NORMALLY AND FLIG HT LANDED WITHOUT INCIDENT. FOUND NOSE LANDING GEAR STRUT LOW, REPLACED THE SCHRADER VALVE AND SERVICED STRUT. ACCOMPL ISHED NOSE LANDING GEAR RETRACTION/EXTENSION TEST AND OPERATED NORMALLY. (W) 2 L 7 2 4F A6WE 1996040500397 19960405 00397 WP 1996 4 5 ASAA9680070 1 19960308 A 3350 1001191 PORTABLE LIGHT DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 973AS 53449 SEA - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (W) 2 L 7 2 4F RT A6WE 1996040500398 19960405 00398 WP 1996 4 5 ASAA9680071 1 19960310 A 3350 0105610001 TRACK LIGHT DOUG DC9 DC983 3022083 WP FWD CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 969AS 53063 SEA - DURING MAINTENANCE CHECK, THE FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED LI GHT ASSEMBLY AT ROW 2 AND OPERATED NORMALLY. (W) 2 L 7 2 4F RT A6WE 1996040500399 19960405 00399 WP 1996 4 5 ASAA9680072 1 19960312 A 3350 41B004AD07G3 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 960AS 53074 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE BAT TERIES AND OPERATED NORMALLY. (W) 2 L 7 2 4F RT A6WE 1996040500400 19960405 00400 WP 1996 4 5 ASAA9680075 1 19960315 A 3350 D29984103 LIGHT DOUG DC9 DC983 3022083 WP TAIL CONE SLIDE INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 942AS 53052 OAK - DURING C-CHECK, THE TAIL CONE EMERGENCY EVACUATION SLIDE EMERGENCY LIGHTS FAILED TEST. REPLACED THE TAIL CONE EME RGENCY EVACUATION SLIDE. (W) 2 L 7 2 4F RT A6WE 1996040500401 19960405 00401 WP 1996 4 5 ASAA9680076 1 19960319 A 3350 41B004AD07G3 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 932AS 49233 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 9 TO 12 WERE FOUND INOPERATIVE. REPLACED THE BA TTERIES AND OPERATED NORMALLY. (W) 2 L 7 2 4F A6WE 1996040500417 19960405 00417 NM 1996 4 5 96ZZZX1482 1 19960301 A 5330 SKIN BOEING 737 7372H5 138448E NM BS 301 CRACKED A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 20454 GSO - 3 CRACKS FORWARD UPPER CORNER, FORWARD SERVICE DOORWAY. INSTALLED DOUBLER PER E.A. 40950. 2 L 7 2 4F A16WE 1996040500418 19960405 00418 NM 1996 4 5 96ZZZX1483 1 19960301 A 5330 SKIN BOEING 737 7372H5 138448E NM BS 375 CRACKED A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 20454 GSO - FIVE .25 INCH CRACKS AT RIVET HOLES FOUND. INSTALLED REPAIR PER E.A. 40951. 2 L 7 2 4F A16WE 1996040500419 19960405 00419 NM 1996 4 5 96ZZZX1484 1 19960301 A 5330 SKIN BOEING 737 7372H5 138448E NM BS 505 CRACKED A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 20454 GSO - .1250 INCH CRACK AT RIVET HOLE FOUND. INSTALLED DOUBLER SRM 53-30-3, FIGURE 6. 2 L 7 2 4F A16WE 1996040500420 19960405 00420 1996 4 5 96ZZZX1485 4 19960126 A 3444 GPWS WARNING FOKKER F28 F28MK0100 4990807 EU COCKPIT ACTIVATED A AALA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 1447L 11456 DFW/BHM - FLT 1412 - INBOUND TO BHM AT 10,000 FEET, PILOT RECEIVED A GPWS MODE 4 ALERT, 'TOO LOW TERRAIN'. PILOT IMMEDI ATELY MADE AN EVASIVE MANEUVER AND CLIMBED TO 12,000 FEET WHICH PUT THE AIRCRAFT INTO THE ATL TCA. AIRCRAFT WAS IN LIGH T RAIN AT THE TIME OF THE ALERT, AND THE PILOT HAD BEEEN MANEUVERING BECAUSE OF WEATHER PRIOR TO THE ALERT. PILOT THEN CONTINUED THE APPROACH AND LANDED AT BHM WITHOUT FURTHER INCIDENT. 2 L 7 2 4F RT 1996040500435 19960405 00435 NM 1996 4 5 AALA960270 1 19960216 A 5330 SKIN BOEING 727 727227 1384078 NM BS 684 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - SMALL HOLE IN BELLY SKIN BELOW FORWARD CARGO AREA CAUSED BY CORROSION. CUT OUT CORROSION, REPLACED CUT OUT PER SR M 53-30-3, PAGES 14B, 14C, AND 14D. INSTALLED 2024-T3 0.071 DOUBLER. TST: 62,772 HRS. CYCLES, 41,734. (X) 2 L 7 3 4F A3WE 1996040500436 19960405 00436 NM 1996 4 5 AALA960279 1 19960221 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 684 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 721AA 20729 TUL - LIGHT CORROSION ON STR 26L, STA 684. CUT OUT DAMAGED (CORRODED) SECTION OF STRINGER. INSTALLED NEW JOGGLED SECTI ON UNDER BELT FRAME AND INSTALLED SPLICES ON BOTH ENDS PER STRINGER SPLICE REPAIR SRM 53-10-3, PAGES 3-4B. TST: 62,86 2 HRS. CYCLES, 43,069. (X) 2 L 7 3 4F A3WE 1996040500437 19960405 00437 NM 1996 4 5 AALA960297 1 19960223 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1955 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1752K 48421 TUL - DURING C-CHECK, FOUND CORROSION ON NR 1 SEAT TRACK TOP SURFACE AT STA 1955 IN AFT CABIN BELOW LAV 'H'. INSTALLED SEAT TRACK REPAIR PER SRM VOL I, 53-70-00-0, PAGES 7, 8, 9. TST: 18,473.56 HRS. CYCLES, 3,801. (X) 2 L 7 3 4F RT A22WE 1996040500438 19960405 00438 NM 1996 4 5 AALA960298 1 19960225 A 5320 SUPPORT DOUG MD11 MD11 3023602 NM BS 439-457 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1752K 48421 TUL - CORROSION FLOOR BOARD SUPPORT AT L-1 DOORWAY. REMOVED AND REPLACED FLOOR BOARD SUPPORT PER SRM 53-70-00, PAGE 1. TST: 18,473.56 HRS. CYCLES, 3,001. (X) 2 L 7 3 4F RT A22WE 1996040500439 19960405 00439 NM 1996 4 5 AALA960299 1 19960225 A 5320 SUPPORT DOUG MD11 MD11 3023602 NM BS 439-457 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1752K 48421 TUL - CORROSION ON FLOOR BOARD SUPPORT AT R-1 DOORWAY. INSTALLED NEW TRACK FLOOR BOARD SUPPORT PER SRM 53-70-20. TST: 18,473.56 HRS. CYCLES, 3,001. (X) 2 L 7 3 4F RT A22WE 1996040500440 19960405 00440 NM 1996 4 5 AALA960307 1 19960222 A 5315 141T5114 FLOOR BEAM BOEING 767 767223 1385123 NM BS 347 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 328AA 22328 TUL - FLOOR BEAM CORRODED. AFTER BLENDING FOUND BEYOND SRM LIMITS. ALODINED AND FILLED BLENDED AREA. FABRICATED AND I NSTALLED REPAIR STRAP USING .063 INCH 7075-T6 ALUMINUM. PRIMED FLOOR BEAM AND STRAP. APPROVED BY ENGINEERING PER MRB 7 67-1155. TST: 38,277.19 HRS. CYCLES, 7,672. (X) 2 L 7 2 4F RT A1NM 1996040500441 19960405 00441 NM 1996 4 5 AALA960329 1 19960228 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1125-1126 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 6823 19701 TUL - BELLY SKIN AT STR 30, BS 1125-1126, IS CORRODED THROUGH SKIN. INSTALLED DOUBLER PER SRM 53-30-3, FIGURE 3. TST: 74,632 HRS. CYCLES, 51,110. (X) 2 L 7 3 4F A3WE 1996040500442 19960405 00442 NM 1996 4 5 AALA960330 1 19960228 A 5320 SIDE WALL BOEING 727 727223 1384074 NM BS 260-285 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 6823 19701 TUL - NOSE WHEELWELL, LEFT SIDE WALL, CRACKED IN 4 PLACES BELOW AND AFT OF THE AFT ACCESS PANEL. STOP DRILLED 2 CRACKS, CUT OUT 2 DAMAGED AREAS, INSTALLED FILLERS, DOUBLER, AND TRIPLER PER SRM 51-40-2, FIGURE 1, PAGE 1. TST: 74,632 HRS. CYCLES, 51,110. (X) 2 L 7 3 4F A3WE 1996040500443 19960405 00443 NM 1996 4 5 AALA960331 1 19960228 A 5712 RIB BOEING 727 727223 1384074 NM WS 656.5 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 6823 19701 TUL - LEFT 656.5 RIB CRACKED AT LOWER NR 8 STRINGER. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 57-10-5, PAGE 6. TST: 74,632 HRS. CYCLES, 51,110. (X) 2 L 7 3 4F A3WE 1996040500444 19960405 00444 WP 1996 4 5 AALA960341 1 19960227 A 5347 593056683 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1279 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 269AA 49292 TUL - DEEP CORROSION ON NR 1 SEAT TRACK AT STA 1279. REPLACED NR 2 SEAT TRACK FROM STA 1174 TO STA 1309, SRM 53-01. T ST: 32,717 HRS. CYCLES, 18,961. (X) 2 L 7 2 4F A6WE 1996040500445 19960405 00445 NM 1996 4 5 CAL960241 1 19960108 A 5320 SUPPORT BOEING 727 727227 1384078 NM BS 312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 49249 21247 INSPECTION FOUND A 1 INCH CRACK IN RT FORWARD LAV FLOOR SUPPORT AT BS 312, RBL 20. THE CORRODED SECTION OF FLOOR SUPPOR T WAS CUT OUT. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, SRM 51-40-3, AND MM 51-20-0. (X) 2 L 7 3 4F A3WE 1996040500446 19960405 00446 NM 1996 4 5 CAL960242 1 19960109 A 5315 FLOOR BEAM BOEING 727 727227 1384078 NM BS 344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 46249 21247 INSPECTION FOUND THE CABIN FLOOR BEAM CORRODED AT BS 344, RBL 20 TO LBL 60. THE CORROSION WAS REMOVED IAW SRM 51-10-6. A NEW T-CAP WAS DRILLED AND INSTALLED IAW SRM 51-10-1, 51-30-2, 51-10-1, 51-30-2. (X) 2 L 7 3 4F A3WE 1996040500447 19960405 00447 NM 1996 4 5 CAL960243 1 19960105 A 5320 DOOR FRAME BOEING 727 727227 1384078 NM BS 620 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 49249 21247 INSPECTION FOUND A 1.75 INCH CRACK AND DEEP GOUGE IN DOOR FRAME WEB AT BS 620, STR 26R. THE WEB WAS REMOVED AND A NEW W EB WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND SRM 51-30-2. (X) 2 L 7 3 4F A3WE 1996040500448 19960405 00448 NM 1996 4 5 CAL960244 1 19960118 A 2782 ACT BRACKET BOEING 727 727227 1384078 NM NR 6 LE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND A .75 INCH CRACK IN RADIUS OF NR 6 KRUGER FLAP ACTUATOR OUTBOARD MOUNTING BRACKET. A NEW BRACKET WAS F ABRICATED AND INSTALLED IAW SRM 51-40-3, 51-30-2, AND 57-20-2. (X) 2 L 7 3 4F A3WE 1996040500449 19960405 00449 NM 1996 4 5 CAL960245 1 19960104 A 5512 PANEL BOEING 727 727227 1384078 NM LT HORIZ STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 49249 21247 INSPECTION FOUND A .25 INCH CRACK AT MOUNT HOLE OF LT HORIZONTAL STABILIZER PANEL NR 9113. THE CRACKED SECTION OF PANEL WAS REMOVED. A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2, AND MM 51-20-1. (X) 2 L 7 3 4F A3WE 1996040500450 19960405 00450 NM 1996 4 5 CAL960246 1 19960107 A 5313 STRINGER BOEING 727 727227 1384078 NM STA 1010-1014 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 49249 21247 INSPECTION FOUND STRINGER AND FAIL-SAFE STRAP SKIN CORRODED AT STA 1010 - STA 1014, LBL 18. THE CORRODED AREAS WERE CUT OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-1 AND SRM 53-30-3. (X) 2 L 7 3 4F A3WE 1996040500451 19960405 00451 NM 1996 4 5 CAL960247 1 19960107 A 5320 DOOR FRAME BOEING 727 727227 1384078 NM BS 560 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 49249 21247 INSPECTION FOUND FORWARD CARGO DOOR FRAME AND NUTPLATE CORRODED AT BS 560, STR 24R AND STR 25R. THE CORROSION WAS REMOV ED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-2. (X) 2 L 7 3 4F A3WE 1996040500452 19960405 00452 NM 1996 4 5 CAL960249 1 19960229 A 5210 65B018398 DOOR FRAME BOEING 747 747230B 1384889 NM DOOR 2R CRACKED A A CALA K NONE O OTHER CR CRUISE 1 SW 09 78019 83031 20527 HNL - FLT 0908 - A LOUD HISSING NOISE WAS HEARD AT DOOR 2R DURING FLIGHT FROM NRT TO HNL. MAINTENANCE FOUND A 10 INCH L ONGITUDINAL CRACK IN THE DOOR FRAME RADIUS ABOVE THE LOWER GATE ON THE FORWARD SIDE OF THE 2R DOOR. THE DOOR WAS REMOVE D IAW MM 52-11-01, PAGES 401-407. THE DOOR WAS REPAIRED IAW SRM 52-10-02, FIGURE 10, PAGES 11-13 AND 17. THE DOOR WAS REINSTALLED IAW MM 52-11-01, PAGES 408-412. AN ADJUSTMENT/TEST WAS PERFORMED IAW MM 52-11-01, PAGES 501-521. PRESSURE CHECK WAS GOOD. (X) 2 L 7 4 4F A20WE 1996040500453 19960405 00453 NM 1996 4 5 CAL960250 1 19960113 A 5320 DOOR FRAME BOEING 727 727243 138408D NM BS 620 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 46469 21265 INSPECTION FOUND A 1.5 INCH CRACK IN INBOARD UPPER SURFACE OF BS 620 FORWARD CARGO COMPARTMENT DOOR CUT OUT AFT FRAME CO VER WEB. THE CRACKED AREA WAS REMOVED FROM THE WEB. A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 5 1-40-2, 51-30-2, AND 51-40-2, FIGURE 1. (X) 2 L 7 3 4F RT A3WE 1996040500454 19960405 00454 NM 1996 4 5 CAL960260 1 19960115 A 5320 THRESHOLD ANGLE BOEING 727 727243 138408D NM BS 344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 46469 21265 INSPECTION FOUND THRESHOLD ANGLE AT DRAIN PAN CORRODED AT BS 344. THE CORRODED AREA WAS CUT OUT. A THRESHOLD ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3. (X) 2 L 7 3 4F RT A3WE 1996040500455 19960405 00455 NM 1996 4 5 CAL960261 1 19960115 A 5315 FLOOR BEAM BOEING 727 727243 138408D NM BS 344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 46469 21265 INSPECTION FOUND FLOOR BEAM UPPER CHORD CORRODED AT BS 344, RBL 20 TO LBL 20. THE CORRODED UPPER CHORD WAS REMOVED. A NEW CHORD WAS FABRICATED AND INSTALLED IAW SRM 53-10-8. FIGURE 3. (X) 2 L 7 3 4F RT A3WE 1996040500456 19960405 00456 NM 1996 4 5 CAL960262 1 19960116 A 5320 DOOR FRAME BOEING 727 727243 138408D NM BS 380 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 46469 21265 INSPECTION FOUND R-1 DOOR INTERIOR LOWER FORWARD FRAME CORRODED AT BS 380, RBL 60. THE CORRODED AREA WAS CUT OUT. AN A NGLE AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND SRM 51-40-3, FIGURE 1. (X) 2 L 7 3 4F RT A3WE 1996040500457 19960405 00457 NM 1996 4 5 CAL960263 1 19960117 A 5320 FLOOR SUPPORT BOEING 727 727243 138408D NM BS 760 BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 46469 21265 INSPECTION FOUND FLOOR SUPPORT BROKEN AT BS 760, LBL 2. THE BROKEN SUPPORT WAS REMOVED AND A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-40-3. (X) 2 L 7 3 4F RT A3WE 1996040500458 19960405 00458 NM 1996 4 5 CAL960264 1 19960118 A 5754 RIB BOEING 727 727243 138408D NM NR 7 LE SLAT CHAFED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 46469 21265 INSPECTION FOUND A .3125 INCH CHAFED HOLE IN WEB AT INNER SKIN FLANGE OF RT WING L/E SLAT NR 7 OUTBOARD RIB. THE AREA W AS DRESSED OUT. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-50-3, FIGURE 9. (X) 2 L 7 3 4F RT A3WE 1996040500459 19960405 00459 NM 1996 4 5 CAL960265 1 19960121 A 5315 FLOOR BEAM BOEING 727 727243 138408D NM BS 1110 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 46469 21265 INSPECTION FOUND FLOOR BEAM UPPER CHORD CORRODED AT BS 1110, RBL 26 TO RBL 44. THE CORRODED SECTION OF FLOOR BEAM UPPER CHORD WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8, SRM 51-10-2, AND MM 51-20-151. (X) 2 L 7 3 4F RT A3WE 1996040500460 19960405 00460 NM 1996 4 5 CAL960266 1 19960127 A 5321 FLOOR PAN BOEING 727 727243 138408D NM BS 1140-1176 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 46469 21265 INSPECTION FOUND CENTER OF LT AFT LAV FLOOR PAN CORRODED AT BS 1140 TO BS 1176. THE CORROSION WAS REMOVED FROM THE FLOO R PAN. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND SRM 51-20-4. (X) 2 L 7 3 4F RT A3WE 1996040500461 19960405 00461 NM 1996 4 5 CAL960267 1 19960115 A 5320 BEAM BOEING 727 727243 138408D NM BS 803-812 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 46469 21265 INSPECTION FOUND CORROSION ON TOP SIDE OF DELTA BEAM AT BS 803, RBL 9 AND A 1.5 INCH CRACK AT BS 812. THE CORROSION WAS REMOVED IAW SRM 51-10-2. A TEE SECTION WAS FABRICATED AND INSTALLED IAW MM 51-20. (X) 2 L 7 3 4F RT A3WE 1996040500462 19960405 00462 NM 1996 4 5 CAL960273 1 19960124 A 5720 BEAM BOEING 727 727243 138408D NM LT MLG CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 46469 21265 INSPECTION FOUND CORROSION ON LT MLG BEAM LOWER FLANGE AT INBOARD FLAP INBOARD TRACK ATTACH POINT. A REPAIR WAS PERFORM ED IAW ECRA 5750-02437 AND SRM 51-10-6 AD SRM 51-10-2. (X) 2 L 7 3 4F RT A3WE 1996040500463 19960405 00463 NM 1996 4 5 CAL960284 1 19960307 A 3350 900835A BATTERY PACKS BOEING 747 747230B 1384889 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 78019 20527 LAX - INSPECTION FOUND OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE AT DOOR 1R, 4R, AND 5L. THE BATTERY PACKS AT EACH LOC ATION WERE REMOVED AND REPLACED. OPERATION OF THE OVERHEAD EMERGENCY LIGHTS WAS RESTORED. (X) 2 L 7 4 4F A20WE 1996040500464 19960405 00464 NM 1996 4 5 CAL960285 1 19960307 A 3242 26011826 BRAKE BOEING 727 727227 1384078 NM MLG NR 4 WHEEL INOPERATIVE A CALA K NONE O OTHER LD LANDING 1 SW 09 76752 15783 6968 B0590 21248 TPA - FLT 0437 - THE NR 4 MLG TIRE BLEW OUT ON LANDING AT TPA. THE LANDING WAS OTHERWISE ROUTINE WITH NO OTHER PROBLEMS . MAINTENANCE FOUND THE NR 4 BRAKE LOCKED. THE NR 4 BRAKE, TIRE AND WHEEL ASSMBLY WERE REMOVED AND REPLACED. IN ADDIT ION, THE NR 3 TIRE AND WHEEL ASSEMBLY WERE REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. THE SDR WILL REMAIN OPEN PE NDING BRAKE SHOP FINDINGS. (X) 2 L 7 3 4F A3WE 1996040500465 19960405 00465 NM 1996 4 5 CAL960288 1 19960309 A 3397 WIRE BOEING 727 727232 1384082 NM EMERGENCY EXIT BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 45793 20647 EWR - FLT 0242 - INSPECTION FOUND THE AFT EMERGENCY EXIT LIGHT BETWEEN SERVICE DOORS INOPERATIVE. MAINTENANCE FOUND A B ROKEN WIRE AT WIRE BUNDLE CONNECTION. THE WIRE WAS REPINNED AND OPERATION OF THE EXIT LIGHT WAS RESTORED. (X) 2 L 7 3 4F A3WE 1996040500466 19960405 00466 NM 1996 4 5 CAL960289 1 19960310 A 3350 CONNECTOR BOEING 747 747230B 1384889 NM R4 DOOR LOOSE WIRE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 78019 20527 LAX - FLT 0023 - INSPECTION FOUND EMERGENCY EXIT LIGHTS AT R-4 DOOR INOPERATIVE. REPLACING BATTERY PACK DID NOT HELP. M AINTENANCE FOUND LOOSE WIRING ON CANNON PLUG AT CHARGING UNIT. THE WIRING WAS REPAIRED AND OPERATION OF THE R-4 DOOR EX IT LIGHTS CHECKED GOOD. (X) 2 L 7 4 4F A20WE 1996040500467 19960405 00467 WP 1996 4 5 CAL960290 1 19960310 A 3232 ACTUATOR DOUG DC9 DC981 3022081 WP NLG DOOR ICED UP A A CALA A UNSCHED LANDING J E WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 SW 09 14880 48044 EWR - FLT 0491 - A SEVERE AIRFRAME VIBRATION WAS FELT IN THE VICINITY OF THE NOSE GEAR AREA AFTER GEAR WAS RAISED. THE NOSE GEAR UNSAFE LIGHT WAS ALSO ILLUMINATED. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTE NANCE FOUND THE RT NOSE GEAR DOOR OPEN. THE FORWARD DOOR ACTUATOR WAS FOUND CAKED WITH ICE AND ICE WAS FOUND ON THE GEA R AS WELL. THE ACTUATOR AND GEAR WERE HEATED TO MELT THE ICE. TH RT FORWARD DOOR ACTUATOR WAS LUBRICATED. THE GEAR WA S SWUNG AND OPERATION CHECKED GOOD. (X) 2 L 7 2 4F A6WE 1996040500468 19960405 00468 WP 1996 4 5 CAL960291 1 19960308 A 1420 SPLICE DOUG DC9 DC982 3022082 WP CABIN FAN FAILED A A CALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 09 14810 49264 IAH - FLT 1804 - WHEN EXTERNAL POWER WAS HOOKED UP AT GATE, SMOKE BEGAN COMING OUT OF OVERHEAD JUST AFT OF FORWARD ENTRY DOOR. THE POWER WAS SHUT OFF AND THE SMOKE CEASED. MAINTENANCE FOUND HEAT EXCHANGER COOLING FAN S9-7 SPLICES BURNED. THE SPLICES WERE REPLACED IN REFERENCE TO MM 20-51-01 AND EA 2450-01009. THE RT GROUND COOLING FAN REPLACED DUE TO BUR NED WIRING. SCORCHED AND TORN INSULATION (APPROX 1 FOOT IN AREA) OVER STA 218 OVERHEAD PANEL REPLACE AND AREA CLEANED. IT IS BELIEVED A SHORT STARTED AT SPLICE FOR FEEDER CABLE TO GROUND COOLING FAN, POSSIBLY CAUSED BY FAULTY CONNECTION. OPERATION OF COOLING FANS CHECKED GOOD. (X) 2 L 7 2 4F A6WE 1996040500469 19960405 00469 WP 1996 4 5 CAL960292 1 19960224 A 5312 BLKHD SKIN DOUG DC9 DC982 3022082 WP AFT PRESS BLKHD CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17812 36173 49250 HOU - INSPECTION FOUND CORROSION IN SKIN AT AFT PRESSURE BULKHEAD FORWARD FACE LOWER CENTER AREA. A DOUBLER WAS FABRICA TED AND INSTALLED IAW SRM 51-30-5. (X) 2 L 7 2 4F A6WE 1996040500470 19960405 00470 WP 1996 4 5 CAL960293 1 19960305 A 5230 9957644510 DOOR PAN DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17812 36173 49250 HOU - INSPECTION FOUND A 1.5 INCH CRACK UNDER FORWARD LOCK CAM OF AFT CARGO DOOR PAN SKIN. THE CRACK WAS TRIMMED OUT AN D A REPAIR ANGLE DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 26A. (X) 2 L 7 2 4F A6WE 1996040500471 19960405 00471 WP 1996 4 5 CAL960294 1 19960223 A 5720 3913503504 BRACKET DOUG DC9 DC982 3022082 WP RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17812 36173 49250 HOU - INSPECTION FOUND A .3750 INCH CRACK IN RT WING UPPER TRAILING EDGE BRACKET AT AILERON OUTBOARD HINGE. THE BRACKET WAS REPLACED IAW SRM 51-30-1. (X) 2 L 7 2 4F A6WE 1996040500472 19960405 00472 WP 1996 4 5 CAL960295 1 19960223 A 5730 9936280501 PANEL DOUG DC9 DC982 3022082 WP TE LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17812 36173 49250 HOU - INSPECTION FOUND A .6250 INCH CRACK IN LT WING UPPER TRAILING EDGE PANEL LOWER SURFACE. THE PANEL WAS REPAIRED IA W SRM 51-70-1. (X) 2 L 7 2 4F A6WE 1996040500473 19960405 00473 WP 1996 4 5 CAL960296 1 19960225 A 5315 9936534139 FLOOR BEAM DOUG DC9 DC982 3022082 WP BS 148-200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17812 36173 49250 HOU - INSPECTION FOUND CORROSION ON FLOOR BEAM AT STA 148 - STA 200, RIGHT OF CENTERLINE. THE FLOOR BEAM WAS REMOVED AN D REPLACED IAW SRM 51-10-1. (X) 2 L 7 2 4F A6WE 1996040500474 19960405 00474 WP 1996 4 5 CAL960300 1 19960225 A 5210 ANGLE DOUG DC9 DC982 3022082 WP PAX DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17812 36173 49250 HOU - INSPECTION FOUND FLOOR SUPPORT Z-ANGLE CORRODED JUST INBOARD OF MAIN CABIN DOOR. THE Z-ANGLE WAS REPLACED IAW SRM 51-30-2. (X). 2 L 7 2 4F A6WE 1996040500475 19960405 00475 WP 1996 4 5 CAL960301 1 19960225 A 5320 SUPPORT BEAM DOUG DC9 DC982 3022082 WP BS 200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17812 36173 49250 HOU - INSPECTION FOUND FORWARD ENTRY FLOOR SUPPORT BEAM CORRODED AT STA 200, CENTERLINE. THE FLOOR SUPPORT BEAM WAS REM OVED AND REPLACED IAW SRM 51-60-0. (X) 2 L 7 2 4F A6WE 1996040500476 19960405 00476 NM 1996 4 5 CAL960307 1 19960313 A 3242 26011826 BRAKE BOEING 727 727232 1384082 NM MLG WHEEL NR 3 BEARING DAMAGED A CALA K NONE O OTHER LD LANDING 1 SW 09 45793 12952 2360 20647 EWR - FLT 0700 - THE NR 3 MAIN WHEEL BRAKE CHATTERED ON LANDING ROLL-OUT WHILE TAXIING TO GATE IN EWR. MAINTENANCE REMO VED NR 3 TIRE AND FOUND INNER BEARING DAMAGED. THE NR 3 TIRE AND BRAKE WERE REMOVED AND REPLACED AND OPERATION CHECKED GOOD. (X) 2 L 7 3 4F A3WE 1996040500477 19960405 00477 NM 1996 4 5 USAABB96006 1 19960226 A 5270 WARNING LIGHT BOEING 757 757225 1384959 NM LT EMER EXIT ILLUMINATED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 604AU 22199 MIA - FLT 538 - LEFT EMERGENCY DOOR (L3) WARNING LIGHT CAME ON DURING CLIMB OUT FROM MIA. AIRCRAFT RETURNED TO FIELD. C ORRECTIVE ACTION: PENDING. (X) 2 L 7 2 4F RT A2NM 1996040500478 19960405 00478 EU 1996 4 5 USAAF96023 1 19960222 A 3246 WHEEL FOKKER F28 F28MK0100 4990807 EU NR 2 DEPARTED A USAA O OTHER D J INFLIGHT SEPARATION WARNING INDICATION CL CLIMB 1 EA 19 869US 11314 CLT - FLT 1543 - ON TAKEOFF FROM RDU RWY 23R, CAPT HAD GEAR FAULT MESSAGE, RDU TOWER TOLD HIM IT LOOKED LIKE SOMETHING F ELL OFF THE AIRCRAFT. WHILE THE FLT HELD IN THE AIR OVER RDU, THEY FOUND THE NR 2 MAIN WHEEL ASSY. FLT PROCEEDED TO CL T. CORRECTIVE ACTION: PENDING. (X) 2 L 7 2 4F RT 1996040500479 19960405 00479 EU 1996 4 5 USAAF96028 1 19960305 A 3010 12292611 ANTI ICE VALVE FOKKER F28 F28MK0100 4990807 EU EMPENNAGE FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 890US 9715 11365 PIT - FLT 946 - TAIL ANTI-ICE FAILED REPEATEDLY ON CLIMB-OUT. FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDEN T. MAINTENANCE REPLACED THE TAIL ANTI-ICE VALVE. (X) 2 L 7 2 4F RT 1996040500480 19960405 00480 NM 1996 4 5 USAASB96040 1 19960304 A 7110 COWL LATCH BOEING 737 7373B7 1384580 NM RT ENGINE NOT LATCHED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 517AU 23703 PIT - FLT 421 - RIGHT ENGINE COWLING LATCH CAME OPEN IN-FLIGHT, ACFT RETURNED. MAINTENANCE SECURED RIGHT ENGINE UPPER C OWLING LATCH, CHECKS NORMAL. CHECKED ALL OTHER COWLING LATCHES, CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1996040500481 19960405 00481 NM 1996 4 5 USAASB96041 1 19960304 A 3350 GROUND WIRE BOEING 737 7373B7 1384580 NM CABIN LOOSE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 530AU 24412 CLT - FLT 0035 - FORWARD SECTION OF FLOOR LEVEL EMERGENCY LIGHTING INOP. MAINTENANCE ADDED A GROUND WIRE TO TERMINAL BL OCK PIN 1 FOR SECTION 1 LIGHTS. WDM 33-51-41 SHEET 1 OF 2, PER EA 80599. EMERGENCY LIGHTS OPS CHECKS NORMAL. (X) 2 L 7 2 4F RT A16WE 1996040500482 19960405 00482 WP 1996 4 5 9607179606 1 19960212 A 5711 SPAR CAP DOUG DC9 DC932 3022066 WP WS 531 570 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 606NW 47225 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LEFT WING REAR SPAR UPPER CAP BETWEEN XRS 531-570. REPAIRED CAP (P/N 5911300-501) PER EA 99-108771. 2 L 7 2 4F A6WE 1996040500483 19960405 00483 WP 1996 4 5 9607189606 1 19960214 A 5311 FRAME DOUG DC9 DC932 3022066 WP FS 148 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 606NW 47225 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FS 148 FRAME BETWEEN LONGERONS 6R TO 7R. REPAIRED FRAME (P/N 9911514) PER EA 99-108988. 2 L 7 2 4F A6WE 1996040500484 19960405 00484 WP 1996 4 5 9607199606 1 19960219 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP DOOR CUTOUT CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 606NW 47225 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE AFT CARGO DOOR CUTOUT DOUBLER LOWER EDGE. REPAIRED DOUBLER (P/N 5910158-25) PER EA 99-108836. 2 L 7 2 4F A6WE 1996040500485 19960405 00485 WP 1996 4 5 9607209606 1 19960223 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP FS 389-408 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 606NW 47225 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE FORWARD CARGO DOOR JAMB DOUBLER BETWEEN FS 389 TO 4 08. REPAIRED DOUBLER (P/N 9912455) PER EA 99-108777. 2 L 7 2 4F A6WE 1996040500486 19960405 00486 WP 1996 4 5 9607219606 1 19960228 A 5330 SKIN DOUG DC9 DC932 3022066 WP FS 1038 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 606NW 47225 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE SKIN CUTOUT FOR THE LEFT PYLON AFT UPPER SPAR CAP STR AP FS 1038. REPAIRED SKIN (P/N 5952562-7) PER EA 99-109066. 2 L 7 2 4F A6WE 1996040500487 19960405 00487 WP 1996 4 5 9607229606 1 19960315 A 5713 STRINGER DOUG DC9 DC932 3022066 WP WS 58-91 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 606NW 47225 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LEFT AND RIGHT WING LOWER STRINGERS 17 TO 22 FROM X RS 58 TO 91. REPAIRED STRINGERS PER EA 99-108772. 2 L 7 2 4F A6WE 1996040500488 19960405 00488 WP 1996 4 5 9607239861 1 19960327 A 5320 FITTING DOUG DC9 DC951 3022051 WP FS 677 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 880NC 47758 DURING H-CHECK, FOUND A CRACK IN THE LONGERON 24L END FITTING AT FS 677. REPLACED FITTING PER SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1996040500489 19960405 00489 WP 1996 4 5 9607249861 1 19960328 A 5210 FITTING DOUG DC9 DC951 3022051 WP PAX DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 770NC 47758 DURING H-CHECK, FOUND A CRACK IN THE AFT ENTRY DOOR UPPER BEAM FITTING. REPLACED FITTING PER SRM 51-10-04. 2 L 7 2 4F A6WE 1996040500490 19960405 00490 WP 1996 4 5 9607259903 1 19960328 A 5230 FITTING DOUG DC9 DC931 3022065 WP CARGO DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 953N 47083 DURING H-CHECK, FOUND A CRACK IN THE AFT CARGO DOOR UPPER AFT BEAM END FITTING. REPLACED FITTING. 2 L 7 2 4F A6WE 1996040500491 19960405 00491 WP 1996 4 5 9607359163 1 19960331 A 3260 UPLIMIT SWITCH DOUG DC9 DC914 3022034 WP LT MLG MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 8906E 45747 DURING CLIMBOUT, THE GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. PERFORMED GEAR UPLATCH CHECK AND THE LIGHT EX TINGUISHED, RECYCLED GEAR AND THE LIGHT AGAIN REMAINED ON. RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE L EFT MAIN LANDING GEAR UPLIMIT SWITCH AND CANNON PLUG, GEAR OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996040500492 19960405 00492 WP 1996 4 5 9607369150 1 19960329 A 2841 QTY INDICATOR DOUG DC9 DC914 3022034 WP LT FUEL SYST MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 01 8908E 45749 DURING CRUISE, THE LEFT FUEL QUANTITY DECREASED AT A GREATER RATE THAN THE RIGHT. FUEL FLOW RATE WAS THE SAME FOR BOTH ENGINES. DIVERTED TO OMA AND LANDED WITHOUT INCIDENT. PERFORMED ALTERNATE FUELING PROCEDURE, INVESTIGATION CONTINUES. 2 L 7 2 4F A6WE 1996040500493 19960405 00493 WP 1996 4 5 9607379178 1 19960329 A 3397 WIRE DOUG DC9 DC914 3022034 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 3310L 45705 DURING LINE CHECK, FOUND THE FIRST TEN FLOOR PATH LIGHTS INOPERATIVE. REPLACED THE BATTERY PACK AND REPAIRED BROKEN WIR E AT ROW ONE RIGHT, OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996040500494 19960405 00494 WP 1996 4 5 9607389877 1 19960329 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 786NC 48148 DURING LINE CHECK, FOUND THE CABIN EMERGENCY LIGHTS FROM STA 750 TO 1020 INOPERATIVE. REPLACED THE POWER SUPPLY B5-26. REPLACED THE BATTERIES IN THE POWER SUPPLY B5-58, ALL LIGHTS OPERATIONALLY CHECKED GOOD. 2 L 7 2 4F A6WE 1996040500495 19960405 00495 WP 1996 4 5 9607399909 1 19960331 A 2120 DUCT CLAMP DOUG DC9 DC931 3022065 WP WATER SEPARATOR LOOSE A NWAA A B UNSCHED LANDING EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 01 959N 47255 LOSS OF CABIN PRESSURIZATION OCCURRED AT 35,000 FEET, AN EMERGENCY DESCENT WAS MADE TO 10,000 FEET AND FLIGHT DIVERTED T O MCO. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LOOSE DUCT CLAMP AND BOOT DISCONNECTED AT WATER SEPARAT OR. TIGHTENED CLAMP AND REPLACED THE BOOT, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996040500496 19960405 00496 1996 4 5 9607409943 4 19960401 A 2565 113317 EVAC SLIDE DOUG DC9 DC931 3022065 WP GALLEY DOOR LOW PRESSURE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 1308T 42862 3835 47315 DURING LINE MAINTENANCE INSPECTION, FOUND GALLEY DOOR EVACUATION SLIDE LOW ON PRESSURE. REPLACED SLIDE. 2 L 7 2 4F A6WE 1996040500497 19960405 00497 WP 1996 4 5 9607419940 1 19960330 A 3510 15830AB OXY REGULATOR DOUG DC9 DC932 3022066 WP LT COCKPIT MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 GL 01 3322L 47031 CREW OXYGEN DROPPED TO ZERO PRESSURE, FLIGHT DIVERTED TO ATL AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE CAPT AIN'S AND FIRST OFFICER'S OXYGEN REGULATORS, LEAK AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996040500498 19960405 00498 NM 1996 4 5 9607422289 1 19960329 A 3350 POWER PACK BOEING 727 727251 138408H NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 289US 21377 DURING PREFLIGHT, FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED THE POWER PACK, CHECKED OK. 2 L 7 3 4F A3WE 1996040500499 19960405 00499 NM 1996 4 5 96FDEA00418 1 19960307 A 5320 BEAR STRAP BOEING 727 72722 1384002 NM BS 1080 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 CORROSION (C53-113-01, 2) ON BEAR STRAP AT BS 1080 RBL 24 WL 145. REMOVED AND REPLACED LOWER PORTION OF BEAR STRAP PER EA 7-5310-28793. 2 L 7 3 4F A3WE 1996040500500 19960405 00500 NM 1996 4 5 96FDEA00507 1 19960311 A 5320 65242581 SILL STRAP BOEING 727 72722 1384002 NM BS 1057 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 NR 0217, CORROSION (C53-113-01, 2) ON SILL STRAP AT BS 1057 RBL 20 WL 149. REMOVED AND REPLACED SILL STRAP BS 1120 TO 1 030 RBL 20 WL 149. 2 L 7 3 4F A3WE 1996040500501 19960405 00501 NM 1996 4 5 96FDEA00511 1 19960308 A 5753 SKIN BOEING 727 72722 1384002 NM RT TE AFT FLAP DELAMINATION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 NR 407, RT WING O/B AFT FLAP HAS AN AREA OF DELAMINATION ON UPPER SURFACE 72 INCHES FROM O/B END. ACTUAL DAMAGE IS 38.2 5 BY 3.5 INCHES. REPAIRED DAMAGE ON UPPER SURFACE SRM 51-40-06. 2 L 7 3 4F A3WE 1996040500502 19960405 00502 NM 1996 4 5 96FDEA00512 1 19960308 A 5753 SKIN BOEING 727 72722 1384002 NM LT TE AFT FLAP DELAMINATION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 NR 412, LT WING I/B AFT FLAP HAS TWO AREAS OF DELAMINATION ON UPPER SURFACE T/E 36 INCHES FROM END. ACTUAL DAMAGE IS ON LOWER SURFACE APPROX 12.5 BY 5 INCHES. REPAIRED DELAMINATION ON UPPER SURFACE SRM 51-40-6. 2 L 7 3 4F A3WE 1996040500503 19960405 00503 NM 1996 4 5 96FDEA00592 1 19960318 A 5312 BLKHD WEB BOEING 727 72722 1384002 NM BS 870 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 NR 0518 AND 043, WHILE WORKING NR 0468 FOUND AFT BULKHEAD OF WING CENTER SECTION TO BE CORRODED BS 870 LBL TO RBL 65 WL 178. REMOVED DAMAGED WEB AND INSTALLED NEW WEB AT BS 870 WL 162 TO 188 RBL 65 TO LBL 65. 2 L 7 3 4F A3WE 1996040500504 19960405 00504 NM 1996 4 5 96FDEA00594 1 19960318 A 5311 FRAME BOEING 727 72722 1384002 NM BS 1148 DOUBLE DRILLED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 NR 0474 AND 038, DOUBLE DRILLED HOLES ON FRAME AT BS 1148 LBL 20 WL 156. REPAIRED DOUBLE DRILLED HOLES PER SRM 51-40-3. 2 L 7 3 4F A3WE 1996040500505 19960405 00505 NM 1996 4 5 96FDEA00597 1 19960318 A 5753 SKIN BOEING 727 72722 1384002 NM RT TE AFT FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 NR 0411 AND 035, RT WING O/B AFT FLAP HAS AN AREA OF DELAMINATION ON LOWER SKIN 60 INCHES FROM I/B END. REPAIRED DAMAGE D LOWER SURFACE SRM 51-40-6. 2 L 7 3 4F A3WE 1996040500506 19960405 00506 NM 1996 4 5 96FDEA00600 1 19960318 A 5230 65186256 WEB BOEING 727 72722 1384002 NM AFT CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 NR 0254 AND 029, AFT CARGO DOOR NR 4 FROM BOTTOM, TRANSVERSE BEAM IS CRACKED IN RADIUS 24 INCHES AFT OF FWD EDGE OF DOOR . REMOVED AND REPLACED NR 4 TRANSVERSE BEAM ON AFT CARGO DOOR. 2 L 7 3 4F A3WE 1996040500507 19960405 00507 NM 1996 4 5 96FDEA00601 1 19960318 A 5230 TRANSVERSE BEAM BOEING 727 72722 1384002 NM BS 532 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 NR 0248 AND 028, FWD CARGO DOOR NR 4 FROM BOTTOM, TRANSVERSE BEAM IS CRACKED IN O/B RADIUS 12 INCHES AND 24 INCHES OF F WD EDGE. REMOVED AND REPLACED NR 4 TRANSVERSE BEAM ON FWD CARGO DOOR MM 52-31-61. 2 L 7 3 4F A3WE 1996040500508 19960405 00508 NM 1996 4 5 96FDEA00602 1 19960318 A 5320 TRIPLER BOEING 727 72722 1384002 NM BS 1110-1130 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 NR 0074 AND 027, BS 1110 RBL 29 BETWEEN STR 25 TO 26R SKIN BULGE AROUND FASTENERS. REPAIRED DAMAGED SKIN IAW FEDEX EA 7 -5310-28049. 2 L 7 3 4F A3WE 1996040500509 19960405 00509 NM 1996 4 5 96FDEA00666 1 19960320 A 5320 THRESHOLD BOEING 727 72725 1384006 NM BS 1057.5-1110 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 CORROSION (C53-113-01, 2) ON DOOR THRESHOLD STIFFENER BS 1057.5 TO 1110 WL 164 RBL 35. INSTALLED NEW DOOR THRESHOLD STI FFENER. 2 L 7 3 4F A3WE 1996040500510 19960405 00510 EU 1996 4 5 96FDEA00717 1 19960329 A 5414 CPN5410424 PANEL AIRBUS 300 A300F4605R 3930327 EU NR 1 PYLON MISSING A FDEA O OTHER D INFLIGHT SEPARATION CR CRUISE 1 SO 25 653FE 736 LT WING I/B FLAP FAIRING I/B SIDE DAMAGED. PANEL 416AR TORN LOOSE FROM NR 1 ENG PYLON. PANEL EXITED A/C AND STRUCK TO LT WING I/B FLAP FAIRING. REPLACED MISSING PYLON PANEL, RELEASED FLAP FAIRING PER CDL 27-1. REMOVED MOVEABLE FLAP TRAC K FAIRINGS FROM LT NR 2 FLAP TRACK PER MM 27-50-21 AND 57-20-35. REMOVED FAIRING SIDE LOAD STAY PER 27-50-23. INSPECTE D ALL AREAS AFT, NO OTHER DAMAGE FOUND. 2 L 7 2 4F RT A35EU 1996040500511 19960405 00511 1996 4 5 96FDEA00718 2 19960329 A 7200 ENGINE AIRBUS 310 A310203 EU NR 1 VIBRATION A FDEA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 25 416FE 288 ON CLIMBOUT, THE A/C STARTED TO VIBRATE AND THE NR 1 ENG INSTRUMENTS, N1 WAS FLUCTUATING 4 TO 6 PERCENT AND THE VIBRATIO N ON ECAM SHOWED AN ENG PROBLEM. N1 WAS FLUCTUATING 4 TO 6 PERCENT AND THE VIB ON THE ECAM SHOWED 3.6 ON N1. WHEN POWE R WAS REDUCED TO IDLE VIB DECREASED, ADDING POWER VIB INCREASED. RETURNED TO IND WITH ENG IN REDUCED POWER. 2 L 7 2 4F RT A35EU 1996040500512 19960405 00512 NM 1996 4 5 96FDEA00719 1 19960330 A 3222 STRUT BOEING 727 72722 1384002 NM NLG REQD SERVICE A FDEA O OTHER J WARNING INDICATION TO TAKEOFF 1 SO 25 113FE 19894 NOSE GEAR DOORS WOULD NOT RETRACT ON TAKEOFF. RECYCLED THE GEAR AND TRIED AGAIN, STILL NO GEAR DOORS RETRACTED. WE OBS ERVED AIR SPEED LIMITS, LIGHT EXTINGUISHED EN ROUTE. FOUND NOSE STRUT DEFLATED. RESEALED UPPER GLAND NUT PER MM 32-21- 1 AND SERVICED SAME, NO LEAKS NOTED. COMPLIED WITH RII INSP PER MM 32-21-1. 2 L 7 3 4F A3WE 1996040500513 19960405 00513 NM 1996 4 5 96FDEA00720 1 19960330 A 2910 2900047 HYDRAULIC MODULE BOEING 727 72722 1384002 NM MAIN GEAR LEAKING A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 195FE 19144 MAIN GEAR AND USED ALT FLAP EXT IN FLT AND BOTH A-SYS LOW PRESS LIGHT CAME ON, FOLLOWED BY OVERHEAT TO SYS. OVERHEAT LI GHT WENT OUT, BUT HAD A-SYS PRESS WITH GOOD A-SYS QTY. RED TAB PROCEDURE AND EWR MX SUGGESTIONS, DID NOT REGAIN A-SYS P RESS. NOTE - IN RIC MX REQ FLAPS 5 DEG WITH GROUND INTER OPEN TO FUEL A/C BECAUSE NR 3 FUEL S/O VALVE WAS INOP. REMOVED AND REPLACED MANIFOLD AND PARTS. REMOVED AND REPLACED THE A-SYS MODULE IAW MM 29-41 HS 107008. A-SYS SERVICED, PRESS AND LEAK CHECK GOOD, ALL IND NORMAL. 2 L 7 3 4F A3WE 1996040500514 19960405 00514 NM 1996 4 5 96FDEA00721 1 19960328 A 5320 65684929 STRAP BOEING 727 72722 1384002 NM BS 760 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 WHILE WORKING EO 7-5310-7-3367B, FOUND REINFORCEMENT STRAP AND T-CLIP TO BE BADLY CORRODED AT BS 760 WL 206 LBL 70.5. R EMOVED AND REPLACED STRAP AND CLIP AT BS 760 WL 206 LBL 70.5. 2 L 7 3 4F A3WE 1996040500515 19960405 00515 NM 1996 4 5 96FDEA00722 1 19960328 A 5311 651985168 FRAME BOEING 727 72725 1384006 NM BS 970-990 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 WHILE WORKING ON NR 0412, FOUND CORROSION (7-5310-3364 PT 6) ON WINDOW FRAME AT BS 970 TO 990 ABOVE STR 11R. REMOVED CO RROSION, FOUND TO BE OUT OF LIMITS. REMOVED WINDOW FRAME AND INSTALLED NEW WINDOW FRAME AT BS 970 TO 990 STR 11R IAW S RM 53-10-1. 2 L 7 3 4F A3WE 1996040500516 19960405 00516 NM 1996 4 5 96FDEA00723 1 19960328 A 5720 65261187 BRACKET BOEING 727 72725 1384006 NM LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 LT WING I/B AILERON TRIM CABLE PULLEY TURNAROUND CASTING IS CORRODED AROUND MAIN PULLEY BOLT HOLE AND TWO OTHER AREAS ON CASTING WBL 410. REMOVED CORRODED LT WING I/B AILERON TRIM CABLE PULLEY TURNAROUND CASTING AND INSTALLED NEW CASTING I AW FEDEX MM 27-10-0, 27-61-0 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996040500517 19960405 00517 NM 1996 4 5 96FDEA00724 1 19960401 A 5313 STRINGER BOEING 727 72722 1384002 NM BS 990 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 CORROSION (C53-113-01, 2) ON STR 27R AT BS 990 RBL 22 WL 142. INSTALLED STR SPLICE REPAIR PER SRM 53-10-3. 2 L 7 3 4F A3WE 1996040500518 19960405 00518 NM 1996 4 5 96FDEA00725 1 19960329 A 5314 KEEL BEAM BOEING 727 72722 1384002 NM BS 1020-1085 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 CORROSION (C53-113-01, 2) ON RT KEEL BEAM RBL 6 WL 140 BS 1020, 1030, 1042, 1056 AND 1085. REPAIRED KEEL BEAM IAW FEDEX EA 7-5310-28083. 2 L 7 3 4F A3WE 1996040500519 19960405 00519 NM 1996 4 5 96FDEA00726 1 19960329 A 5320 DOOR FRAME BOEING 727 72722 1384002 NM BS 1057 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 CORROSION (C53-113-01, 2) ON DOOR FRAME AT BS 1057 RBL 30 WL 148 AT NUTPLATE HOLES. REPAIRED DAMAGE PER SRM 51-40-3. 2 L 7 3 4F A3WE 1996040500520 19960405 00520 NM 1996 4 5 96FDEA00727 1 19960329 A 5320 65207324 VERTICAL WEB BOEING 727 72722 1384002 NM BS 1057-1110 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 CORROSION (C53-113-01, 2) ON AFT BAY WEB SILL BS 1057 TO 1110 RBL 21 WL 148.5. FOUND UPON REMOVAL OF STRAP NR 0217. RE MOVED AND REPLACED AFT BAY WEB SILL FROM BS 1057 TO 1110 RBL 21 WL 148.5. 2 L 7 3 4F A3WE 1996040500521 19960405 00521 NM 1996 4 5 96FDEA00728 1 19960329 A 5313 BAC1498146 STRINGER BOEING 727 72725 1384006 NM BS 1059 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 NR 0624 AND 043, CORROSION FOUND ON END OF STR SECTION STR 28R BS 1059. 2 L 7 3 4F A3WE 1996040500522 19960405 00522 WP 1996 4 5 96FDEA00730 1 19960327 A 3252 ACG74405503 CYLINDER DOUG DC10 DC1030F 3023504 WP NLG STEERING FAILED A FDEA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 SO 25 302FE 46801 LOST SYS 3 HYD AFTER LANDING, MADE TURN ON TO TAXIWAY LOST ALL FLUID CONFIRMED EXTERNAL LEAK FROM A/C ON GROUND. REMOVE D AND REPLACED NOSEWHEEL STEERING CYLINDER PER MM 32-52-01. RESERVICED NR 3 HYDRO SYS TO FULL, ALL SYSTEMS CHECK GOOD. 2 L 7 3 4F RT A22WE 1996040500523 19960405 00523 NM 1996 4 5 96UAL900223 1 19960328 A 2133 7638101 CONTROLLER BOEING 737 737322 1384676 NM E/E COMPT INOPERATIVE A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 371UA 24540 AIRCRAFT DIVERTED TO LAX DUE TO LOSS OF CABIN PRESSURIZATION. *S/D* REPLACED CABIN PRESSURE CONTROLLER, CHECKS OK. 2 L 7 2 4F RT A16WE 1996040500524 19960405 00524 NM 1996 4 5 96UAL900224 1 19960328 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563B2 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 316UA 23948 ROW 3 EMERGENCY LIGHT INOP. RELAMPED, OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 1996040500525 19960405 00525 NM 1996 4 5 96UAL900225 1 19960328 A 3350 STRIP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 662UA 27159 MID CROSS AISLE EEL STRIP INOPERABLE. REPLACED EEL STRIP, OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 1996040500526 19960405 00526 EU 1996 4 5 96UAL900226 1 19960329 A 3260 PROXIMITY SENSOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RT MLG DOOR OUT OF ADJUST A UALA O OTHER N FALSE WARNING AP APPROACH 1 WP 29 403UA 442 DURING GEAR EXTENSION ON ARRIVAL AT SFO, LANDING GEAR UNLOCK LIGHTS ILLUMINATED WITH NO GREEN DOWN AND LOCKED INDICATION . RECYCLED GEAR HANDLE AND GEAR EXTENDED NORMALLY. SUPPLEMENTAL DATA: UPDATE FOUND RIGHT HAND LANDING GEAR DOOR PROXI MITY SENSOR OUT OF ADJUSTMENT. ADJUSTED SENSOR, SWUNG GEAR AND OPERATED NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 1996040500527 19960405 00527 NM 1996 4 5 96UAL900227 1 19960329 A 2121 GASPER FAN SUNDSTRAND 215201 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 7459U 1125 21913 CREW REPORTED, ELECTRICAL BURNING SMELL IN CABIN AND COCKPIT. REPLACED THE GASPER FAN WHICH HAD CAUSED THE PROBLEM. 2 L 7 3 4F 4 F A3WE E2EA 1996040500528 19960405 00528 NE 1996 4 5 96UAL900228 2 19960329 A 7200 ENGINE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 3 BIRDSTRIKE A UALA A UNSCHED LANDING C F.O.D. CR CRUISE 1 WP 29 181UA 25278 724676 SHORTLY AFTER TAKEOFF, INGESTED NUMEROUS BIRDS INTO NUMBER THREE ENGINE, ENGINE STALLED AND CREW WAS UNABLE TO RESTART. ACFT RETURNED TO SYD. *S/D* BIRD STRIKE IN NR 3 ENGINE. REPLACED ENGINE AND FAN BLADES. 2 L 7 4 4F 4 F RT A20WE E24NE 1996040500529 19960405 00529 NM 1996 4 5 96UAL900229 1 19960329 A 5522 65727841 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LT ELEVATOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7256U 21403 LEFT ELEVATOR HAS A 2.5 INCH CRACK 1 FOOT OUTBOARD OF TRIM TAB PANEL. ALSO, 1 RIVET MISSING AND 5 LOOSE RIVETS. FATIGU E CRACK IN LOWER SKIN OF LEFT ELEVATOR. ELEVATOR REPLACED WITH A SERVICEABLE UNIT. 2 L 7 3 4F 4 F A3WE E2EA 1996040500530 19960405 00530 NM 1996 4 5 96UAL900230 1 19960401 A 3230 PSEU BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE LANDING GEAR FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 185UA 25395 GEAR TILT AND GEAR DISAGREE MESSAGES DISPLAYED, UNABLE TO RETRACT GEAR. *S/D* PSEU SENT TO VENDOR FOR REPAIR. RESULTS INDICATE PSEU HAD FAILURE OF PRIMARY CARD FOR LBG DOOR AND UP SENSOR AND ALTERNATE CARD FOR LBG AND LWG TILT SENSOR. R EPLACED PSEU. 2 L 7 4 4F 4 F RT A20WE E24NE 1996040500531 19960405 00531 NM 1996 4 5 96UAL900231 1 19960401 A 2120 65544741 DUCT BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE RT PACK DAMAGED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 9067U 19948 HEARD LOUD NOISE AFTER TURNING ON RIGHT PACK AFTER TAKEOFF. *S/D* FOUND RIGHT AIR CONDITIONING DISTRIBUTION DUCT IN CE NTER BAY AFT OF FORWARD CARGO PIT DAMAGED. REPLACED DUCT, CHECKS OK. 2 L 7 2 4F 4 F A16WE E2EA 1996040500532 19960405 00532 NM 1996 4 5 96UAL900232 1 19960401 A 3350 BATTERY BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE CABIN DISCHARGED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 9066U 19947 RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES, CHECKS OK. 2 L 7 2 4F 4 F A16WE E2EA 1996040500533 19960405 00533 WP 1996 4 5 ABXA9600431 1 19960318 A 2110 5614845517 CTC DOUG DC8 DC861 3021952 WP NR 4 POSITION DEFECTIVE A ABXA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 23 844AX 1336 45848 NR 4 CTC MADE A LOUD HOWLING NOISE FOLLOWED BY THE SMELL OF SMOKE AND OIL IN THE COCKPIT. SHUTDOWN THE NR 4 CTC FOR THE REMAINDER OF THE FLIGHT. REPLACED THE NR 4 CTC IAW DC8 MM AND OPS CHECK GOOD. 2 L 7 4 4F 4A25 1996040500539 19960405 00539 SO 1996 4 5 COMA9610118 1 19960329 A 2910 LINE EMB 120 EMB120RT SO LT NACELLE CHAFED A COMA K NONE K J FLUID LOSS WARNING INDICATION UK UNKNOWN 1 SO 01 244CA 120217 HYDRAULIC FLUID DRIPPING FROM LEFT ENGINE NACELLE. REPAIRED CHAFED HYDRAULIC PRESSURE LINE UNDER ENGINE FIRE DECK. 2 L 7 2 4T RT A31SO 1996040500540 19960405 00540 NE 1996 4 5 COMA9630088 3 19960329 A 6111 EROSION GUARD SAAB SF340 SF340A 7850100 EU ROTOL R389 R3894123F25 NE RT PROP LOOSE A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 158CA 340A158 495883 EROSION GUARD ON ONE BLADE OF RT PROPELLER IS LOOSE AND PEELING. REBONDED EROSION GUARD. 2 L 7 2 4T RT A52EU 6 C P30NE 1996040500541 19960405 00541 EU 1996 4 5 COMA9630089 1 19960329 A 3230 4018501 HYD PUMP ASSY SAAB SF340 SF340A 7850100 EU LANDING GEAR FAILED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 158CA 16914 340A158 LT AND RT MLG DID NOT DOWN LOCK WHEN SELECTED DURING LANDING APPROACH. REPLACED THE HYDRAULIC PUMP ASSY. 2 L 7 2 4T RT A52EU 1996040500542 19960405 00542 EU 1996 4 5 COMA9630090 1 19960328 A 2750 5308211C FLAP SELECTOR SAAB SF340 SF340A 7850100 EU INSTR PANEL DEFECTIVE A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 342CA 17855 340A023 FLAPS ARE STUCK AT 7 DEGREES, THEY WILL NOT RETRACT OR EXTEND. REPLACED THE ENGINE CONTROL QUADRANT BECAUSE OF DEFECTIV E FLAP SELECTOR. 2 L 7 2 4T RT A52EU 1996040500543 19960405 00543 NE 1996 4 5 COMA9630091 3 19960329 A 6111 EROSION GUARD SAAB SF340 SF340A 7850100 EU ROTOL R389 R3894123F25 NE RT PROP SEPARATED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 341CA 340A021 109586 ONE BLADE ON RT PROPELLER, LEADING EDGE EROSION GUARD IS SEPARATING. REBONDED EROSION GUARD. 2 L 7 2 4T RT A52EU 6 C P30NE 1996040500544 19960405 00544 NE 1996 4 5 COMA9630092 3 19960330 A 6111 EROSION GUARD SAAB SF340 SF340A 7850100 EU ROTOL R389 R3894123F25 NE LT PROP DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 342CA 340A023 277284 LEFT PROPELLER HAS DAMAGE IN BLADE LEADING EDGE EROSION GUARD. REPLACED PROPELLER. 2 L 7 2 4T RT A52EU 6 C P30NE 1996040500545 19960405 00545 NM 1996 4 5 DL72E960694 1 19960328 A 5320 TQ BOX WEB BOEING 727 727247 138408F NM BS 1223 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 830WA 21482 FOUND ON D-2 LETTER CHECK, TORQUE BOX WEB LIGHTENING HOLE CRACKED .25 INCH, STA 1223 RT. REPAIRED PER M/M 53-11-0. 2 L 7 3 4F A3WE 1996040500546 19960405 00546 NM 1996 4 5 DL72E960699 1 19960328 A 5320 ANGLE BOEING 727 727247 138408F NM BS 133.8 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 830WA 21482 FOUND ON D-2 LETTER CHECK, WEB TO STRINGER ATTACH ANGLE CRACKED. VERTICAL CRAWL WAY 3RD BAY FROM TOP LT SIDE CRACK LOCA TED IN STA 133.8 AT STR 9. REPAIRED PER M/M 55-30-0. 2 L 7 3 4F A3WE 1996040500547 19960405 00547 NM 1996 4 5 DL72E960700 1 19960328 A 5240 DOOR PAN BOEING 727 727247 138408F NM FWD SERVICE DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 830WA 21482 FOUND ON D-2 LETTER CHECK, 3 INCH CRACK IN FWD SERVICE DOOR PAN EXTENDING FROM LOWER FWD STOP CASTING. REPAIRED PER ERA 303377-14 AND M/M 52-12-0. 2 L 7 3 4F A3WE 1996040500548 19960405 00548 NM 1996 4 5 DL72E960730 1 19960315 A 5754 651622374 RIB BOEING 727 727247 138408F NM NR 7 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 830WA 21482 DURING INITIAL INSPECTION OF THE NR 7 LEADING EDGE SLAT, THE NR 11 RIB WAS FOUND TO BE CRACKED. THE RIB WAS REPAIRED PE R M/M 57-54-0 FIG 804. 2 L 7 3 4F A3WE 1996040500549 19960405 00549 NM 1996 4 5 DL72K960706 1 19960329 A 5312 BLKHD CLIP BOEING 727 727232 1384082 NM BS 1342 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 481DA 20861 FOUND DURING A-2 LETTER CHECK, FS 1342 BULKHEAD AND UPPER ATTACH CLIP CRACKED 1.5 INCH AT RT SIDE AND CRACKED BEYOND STO P DRILL ON LT SIDE. REPAIRED PER MM 53-11-0. 2 L 7 3 4F A3WE 1996040500550 19960405 00550 NM 1996 4 5 DL72K960707 1 19960329 A 5330 SKIN BOEING 727 727232 1384082 NM L5 WINDOW CUTOUT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 481DA 20861 FOUND DURING A-2 LETTER CHECK, .3750 INCH VISIBLE CRACK IN SKIN AT L5 WINDOW CUTOUT UPPER AFT CORNER. REPAIRED PER SRM 53-30-3. 2 L 7 3 4F A3WE 1996040500551 19960405 00551 NM 1996 4 5 DL72K960708 1 19960329 A 5330 SKIN BOEING 727 727232 1384082 NM L2 DOOR CUTOUT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 481DA 20861 FOUND DURING A-2 LETTER CHECK, .5 INCH CRACK IN LT AFT SERVICE DOOR FWD FRAME AT LOWER I/B CORNER OF UPPER HINGE/GUIDE A RM CUTOUT. REPAIRED PER SRM 52-40-2. 2 L 7 3 4F A3WE 1996040500552 19960405 00552 NM 1996 4 5 DL72S960702 1 19960329 A 5754 6516221100 FENCE BOEING 727 727232 1384082 NM NR 5 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 527DA 21587 UPON ROUTINE INSPECTION, FOUND CRACKS IN MOUNTING HOLES OF FENCE. REPAIRED AS PER SRM 57-54-0 PG 817, FOR NR 5 L/E SLAT . 2 L 7 3 4F A3WE 1996040500553 19960405 00553 NM 1996 4 5 DL72S960727 1 19960327 A 5210 CLOSING MECH BOEING 727 727232 1384082 NM PAX DOOR BROKEN A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 524DA 21584 ON ARRIVAL AT GATE, THE FWD LT ENTRY DOOR WOULD NOT OPEN. FOUND SEVERAL BROKEN PARTS JAMMING UPPER HINGE AND LOWER CAM PLATE, UPPER HINGE WAS LOOSE IN AT FUSELAGE. REPLACED BROKEN SNAP RING AND TIGHTENED CAM PLATE, OPERATION NORMAL. 2 L 7 3 4F A3WE 1996040500554 19960405 00554 NM 1996 4 5 DL72W960695 1 19960329 A 5754 651622296 RIB BOEING 727 727247 138408F NM NR 6 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2809W 20581 DURING INSPECTION, NR 6 L/E SLAT WAS FOUND WITH INTERNAL SUPPORT RIB NR 11 CRACKED. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1996040500555 19960405 00555 NM 1996 4 5 DL72W960696 1 19960329 A 5754 651622296 RIB BOEING 727 727247 138408F NM NR 6 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2809W 20581 DURING INSPECTION, FOUND NR 6 L/E SLAT WITH INTERNAL SUPPORT RIB NR 10 CRACKED. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1996040500556 19960405 00556 NM 1996 4 5 DL72W960697 1 19960329 A 5754 651622296 SKIN BOEING 727 727247 138408F NM NR 6 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2809W 20581 INNER SKIN CRACKED AT NUTPLATES, RIBS 10, 11, 12 AND 13. REPAIRED PER M/M 57-54-0, FOR NR 6 L/E SLAT. 2 L 7 3 4F A3WE 1996040500558 19960405 00558 NM 1996 4 5 DL73E960715 1 19960330 A 3350 BATTERY PACK BOEING 737 7372J8 1384489 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 235WA 22859 EMERGENCY PATH LIGHTS BATTERY PACK INOP. REPLACED, CHECKS GOOD. 2 L 7 2 4F RT A16WE 1996040500559 19960405 00559 1996 4 5 DL757960709 4 19960329 A 2565 SLIDE BOEING 757 757232 1384965 NM R 1 DOOR DEPLOYED A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 684DA 27104 R-1 DOOR SLIDE WAS NOT DEACTIVATED BY CREW PRIOR TO ARRIVAL AT GATE. R-1 DOOR SLIDE DID NOT DEPLOY PROPERLY WHEN DOOR W AS OPENED BY CABIN SERVICE. DOOR SLIDE DID NOT CLEAR DOOR SLIDE COVER, UPON DOOR OPENING. DOOR WAS HUNG ON DOOR SLIDE IN PARTIALLY OPENED POSTION. SLIDE AND DOOR ASSIST BOTTLE WAS CHANGED. WHEN DOOR SLIDE WAS REMOVED AT FLOOR ATTACH POI NT THE DOOR OPENED FULLY. 2 L 7 2 4F RT A2NM 1996040500560 19960405 00560 NM 1996 4 5 DL757960711 1 19960330 A 2560 4566M37B PBE MASK BOEING 757 757232 1384965 NM F/C CLOSET RED IND POPPED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 673DL 25978 FRONT CLOSET PBE DISCOVERED BAD DURING PREFLIGHT. REPLACED, OK FOR SERVICE. 2 L 7 2 4F RT A2NM 1996040500561 19960405 00561 1996 4 5 DL757960713 4 19960330 A 2565 D30655123 SLIDE BOEING 757 757232 1384965 NM R2 DOOR LOW PRESS A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 629DL 22919 R2 DOOR SLIDE BOTTLE PRESSURE LOW. REPLACED SLIDE ASSY. 2 L 7 2 4F RT A2NM 1996040500562 19960405 00562 NM 1996 4 5 DL767960691 1 19960328 A 3350 LIGHT BOEING 767 767232 1385132 NM LT AFT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 102DA 22214 ON LAYOVER, FOUND LEFT AFT EMERGENCY LIGHT INOP. RELAMPED, CKS OK. 2 L 7 2 4F RT A1NM 1996040500563 19960405 00563 NM 1996 4 5 DL767960729 1 19960327 A 3260 SENSOR BOEING 767 767232 1385132 NM LANDING GEAR OUT OF ADJUST A DALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 27 102DA 22214 ON TAKEOFF, GEAR COULD NOT BE RAISED WITHOUT USING LOCK OVERRIDE. AIRCRAFT WAS FERRIED ATL FOR REPAIRS. PSEU SHOWS 246 RT GEAR TILT TARGET SHOWS FAR RESET. ADJUSTED SENSOR PER MM, OPERATION NORMAL. 2 L 7 2 4F RT A1NM 1996040500564 19960405 00564 1996 4 5 DL76E960678 4 19960328 A 2213 FLT CONTROLLER BOEING 767 767232 1385132 NM AUTO PILOT FAILED A DALA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 27 112DL 22224 ON APPROACH, FLT CREW REPORTED VERY STIFF AILERONS, ALMOST UNABLE TO TURN A/C. A/C WOULD NOT TURN ON A/P BOTH THE LEFT AND RIGHT A/P WOULD DISCONNECT IF ENGAGED AND A TURN INPUT MADE, CENTER A/P NOT USED. FLT CREW DECLARED AN EMERGENCY AND A/C LANDED WITHOUT INCIDENT IN VIE. FURTHER T/S REVEALED LEFT A/P FCC FAILED. CONFIRMED AILERONS OK AND NOT BINDI NG. REPLACED FCC. 2 L 7 2 4F RT A1NM 1996040500565 19960405 00565 WP 1996 4 5 DLL10960689 1 19960328 A 2150 COALESCER BAG LKHEED 1011 10113851 5265010 WP LT/RT DIRTY A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 728DA 193C1173 ON SHORT FINAL, AFT OF A/C FILLED WITH HAZY SMOKE AND ALL LAV SMOKE DETECTORS WENT OFF, PACK TEMPS NORMAL. RAN ENGS AND ALL THREE PACKS. FOUND NR 2 PACK RUNNING HOT AND GIVING OFF ODOR. LOCKED NR 2 PACK VALVE CLOSED AND FWD TO MCO AND PL AC PER 21-51-07A. REPLACED WATER SEPARATOR BAGS, RAN ALL PACKS AND NO ODOR NOTED, INSPECTED CROSSFEED VALVES FOR OIL CO NTAMINATION, NONE FOUND. 2 L 7 3 4F A23WE 1996040500566 19960405 00566 WP 1996 4 5 DLL10960712 1 19960330 A 2560 2377002242 MEGAPHONE LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1734D 193C1225 FWD MEGAPHONE INOP. REPLACED FWD MEGAPHONE, OPS CK NORMAL. 2 L 7 3 4F A23WE 1996040500567 19960405 00567 NM 1996 4 5 DLM88960714 1 19960330 A 2121 FAN DOUG MD88 MD88 3023688 NM RADIO RACK FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 902DE 53379 STRONG ELECT SMELL AND SMOKE AT PUSHBACK. FOUND RADIO RACK FAN FAILED. REPLACED FAN, OPS NORMAL. 2 L 7 2 4F RT A6WE 1996040500568 19960405 00568 NM 1996 4 5 MWEA96069 1 19960330 A 5280 GEAR DOOR DOUG MD88 MD88 3023688 NM LT MLG DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 DURING C-CHECK, FOUND LT MAIN GEAR DOOR HAS 5 INCH CRACK IN AFT OUTBD PAN. INSTALLED DOUBLER REPAIR IAW SRM 52-05, FIG 28. 2 L 7 2 4F RT A6WE 1996040500569 19960405 00569 WP 1996 4 5 MWEA96070 1 19960330 A 5320 ANTENNA MOUNT DOUG DC9 DC932 3022066 WP BS 470 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 TEMPORARY REPAIR INSTALLED AT FS 470 LONG 30, VHF ANTENNA MOUNT. REMOVED TEMP REPAIR AND INSPECTED SKIN, NO CRACKS. IN STALLED PERMANENT REPAIR MOD IAW SB 53-188 AND SRM 9530005. 2 L 7 2 4F A6WE 1996040500570 19960405 00570 WP 1996 4 5 MWEA96071 1 19960330 A 5230 ANGLE DOUG DC9 DC932 3022066 WP CARGO DOOR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FWD CARGO DOOR CORRODED AT LOWER ANGLE BOTTOM END OF DOOR. REPLACED CORRODED ANGLE IAW SRM 52-01 AND 51-10-3. 2 L 7 2 4F A6WE 1996040500571 19960405 00571 WP 1996 4 5 MWEA96073 1 19960330 A 5320 HANDLE MOUNT DOUG DC9 DC932 3022066 WP BS 1121 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND CRACK AT FS 1121 IN AFT ACCESSORY COMP WHERE THE VENTRAL STAIR OPEN/CLOSE HANDLE MOUNTS TO STAIR JAMB. INSTALLED REPAIR IAW SRM 53-03, FIG 34. 2 L 7 2 4F A6WE 1996040500572 19960405 00572 WP 1996 4 5 MWEA96074 1 19960330 A 5330 SKIN DOUG DC9 DC932 3022066 WP DOOR CUTOUT DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND DAMAGED SKIN AROUND FWD ENTRANCE DOOR HOLD OPEN HOOK RECEPTACLE. INSTALLED DOUBLER REPAIR IAW SRM 53-04, FIG 24. 2 L 7 2 4F A6WE 1996040500573 19960405 00573 WP 1996 4 5 MWEA96075 1 19960330 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP BS 917-996 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND CENTER FLOOR BEAM SUPPORT AT STA 917 TO 996 HAS MODERATE CORROSION AROUND SCREW HOLES. REPLACED FLOOR SUPPORT IAW SRM 53-11-3, FIG 11. 2 L 7 2 4F A6WE 1996040500574 19960405 00574 WP 1996 4 5 MWEA96076 1 19960330 A 5230 SKIN DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND FWD CARGO DOOR SKIN CRACKED AT LOWER FWD CORNER. INSTALLED DOUBLER REPAIR IAW SRM 52-01 FIG 2 SHEET 3. 2 L 7 2 4F A6WE 1996040500575 19960405 00575 WP 1996 4 5 MWEA96077 1 19960330 A 5713 STRINGER DOUG DC9 DC932 3022066 WP WS 77.5 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND CORROSION ON LT WING STA XRS 77.5 AT STRINGER 11 WHICH BLENDED OUT BEYOND LIMITS. INSTALLED STRAP REPAIR IAW DAC TELEX SVC-0RD-0034. 2 L 7 2 4F A6WE 1996040500576 19960405 00576 WP 1996 4 5 MWEA96078 1 19960330 A 5512 SKIN DOUG DC9 DC932 3022066 WP HORIZ STAB CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND RT HORIZONTAL UPPER SKIN AT STA XHS60 AND TRAILING EDGE HAS 2 SPOTS OF EXFOLIATION CORRSION. INSTALLED DOUBLER RE PAIR IAW DAC TELEX SVC-ORD-0043. 2 L 7 2 4F A6WE 1996040500577 19960405 00577 WP 1996 4 5 MWEA96079 1 19960330 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 1076 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND FRAME CRACKED 2 PLACES STA 1076 AT LONGERON 27L AND 27R. INSTALLED SPLICE REPAIR IAW SRM 53-03 FIG 32 SHT 4. 2 L 7 2 4F A6WE 1996040500578 19960405 00578 WP 1996 4 5 MWEA96080 1 19960330 A 5315 FLOOR BEAM DOUG DC9 DC932 3022066 WP BS 389 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND FLOOR BEAM AT STA 389 HAS DAMAGE ON LOWER FLANGE FROM CARGO DOOR CONTACT. INSTALLED DOUBLER REPAIR IAW SRM 53-05 FIG 86 AND DAC FAX 029183. 2 L 7 2 4F A6WE 1996040500579 19960405 00579 WP 1996 4 5 MWEA96081 1 19960330 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 389 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 INTERCOSTAL AT STA 389, 28L AND 28R CORRODED AROUND NUTPLATES. REPAIRED INTERCOSTAL IAW SRM 53-01 FIG 2. 2 L 7 2 4F A6WE 1996040500580 19960405 00580 WP 1996 4 5 MWEA96082 1 19960330 A 5311 FRAME DOUG DC9 DC932 3022066 WP AFT ACCESSORY CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND CRACK IN CANTED FRAME STA 1074 LONG 5L. REPLACED FRAME SECTION IAW SRM 53-01 PG 1. 2 L 7 2 4F A6WE 1996040500581 19960405 00581 WP 1996 4 5 MWEA96083 1 19960330 A 5510 STRINGER DOUG DC9 DC932 3022066 WP HORIZ STAB CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND LT HORIZ STAB NR 3 UPPER STRINGER CRACKED AT STA XHS32. INSTALLED REPAIR IAW SRM 55-03 FIG 16. 2 L 7 2 4F A6WE 1996040500582 19960405 00582 WP 1996 4 5 MWEA96084 1 19960330 A 5512 SKIN DOUG DC9 DC932 3022066 WP HORIZ STAB CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 RT HORIZONTAL STAB SKIN INNER SURFACE CORRODED AT STA XHS 132 FWD OF AFT SPAR. INSTALLED DOUBLER REPAIR IAW DAC TELEX S VC-0RD-0033DLP. 2 L 7 2 4F A6WE 1996040500583 19960405 00583 WP 1996 4 5 MWEA96085 1 19960330 A 5320 CHANNEL DOUG DC9 DC932 3022066 WP VENTRAL STAIR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FRAME AT VENTRAL STAIR OPENING J AND L CHANNELS HAVE CORROSION BOTH SIDES. INSTALLED REPAIR IAW SRM 53-11-4. 2 L 7 2 4F A6WE 1996040500584 19960405 00584 WP 1996 4 5 MWEA96086 1 19960330 A 5532 SKIN DOUG DC9 DC932 3022066 WP VERT STAB GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND VERTICAL STAB SKIN LT SIDE UPPER FWD SURFACE HAS SEVERAL DEEP GOUGES. INSTALLED REPAIR IAW SRM 55-01 PG 1. 2 L 7 2 4F A6WE 1996040500585 19960405 00585 WP 1996 4 5 MWEA96087 1 19960330 A 5522 SKIN DOUG DC9 DC932 3022066 WP RT ELEVATOR DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND RT ELEVATOR UPPER OUTBD SKIN HAS 2 CREASED DENTS RUNNING FORE AND AFT 22 INCHES INBD OF OUTBD END CAP. INSTALLED REPAIR DOUBLER IAW SRM 55-03 FIG 14. 2 L 7 2 4F A6WE 1996040500586 19960405 00586 WP 1996 4 5 MWEA96088 1 19960330 A 5320 JAMB DOUG DC9 DC932 3022066 WP AFT ACCESSORY CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND AFT ACCESSORY VENTRAL STAIRWAY JAMB ON LT SIDE STA 1121 SKIN AND STRUCTURE HAS MODERATE CORROSION. INSTALLED REPA IR IAW SRM 53-01 FIG 4 SHT 3. 2 L 7 2 4F A6WE 1996040500587 19960405 00587 WP 1996 4 5 MWEA96089 1 19960330 A 5320 JAMB DOUG DC9 DC932 3022066 WP AFT STAIRWAY CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND VENTRAL STAIR DOOR JAMB UPPER LT CORNER HAS A CRACK WITH ADJACENT RIVETS POPPED. INSTALLED DOUBLER REPAIR IAW SRM 53-05 FIG 29. 2 L 7 2 4F A6WE 1996040500588 19960405 00588 WP 1996 4 5 MWEA96090 1 19960330 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 351 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND MODERATE CORROSION IN FRAME STA 351 LONG 28L TO 28R IN FWD CARGO COMPT. BLENDED CORROSION, INSTALLED DOUBLER REPA IR IAW SRM 53-03 FIG 2A SHT 3. 2 L 7 2 4F A6WE 1996040500589 19960405 00589 WP 1996 4 5 MWEA96091 1 19960330 A 5312 BULKHEAD DOUG DC9 DC932 3022066 WP AFT PRESS BLKD GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND GOUGE MARKS ON AFT SIDE OF AFT PRESSURE BULKHEAD FWD OF RT APU DOOR HINGE. INSTALLED DOUBLER REPAIR IAW SRM 53-03 FIG 22. 2 L 7 2 4F A6WE 1996040500590 19960405 00590 WP 1996 4 5 MWEA96092 1 19960330 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 617 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND LONGERON 2L CRACKED AT STA 617. INSTALLED SPLICE REPAIR IAW SRM 53-03 FIG 2. 2 L 7 2 4F A6WE 1996040500591 19960405 00591 WP 1996 4 5 MWEA96093 1 19960330 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 908/963 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND SEAT TRACKS 1 AND 2 CORRODED AT STA 963 AND 908 RESPECTIVELY. INSTALLED PLUG REPAIR IAW SRM 53-05 FIG 86. 2 L 7 2 4F A6WE 1996040500592 19960405 00592 WP 1996 4 5 MWEA96094 1 19960330 A 5315 FLOOR BEAM DOUG DC9 DC932 3022066 WP BS 408 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND FLOOR BEAM AT STA 408 HAS DAMAGE ON LOWER FLANGE FROM FWD CARGO DOOR CONTACT. INSTALLED DOUBLER REPAIR IAW SRM 53 -05 FIG 86. 2 L 7 2 4F A6WE 1996040500594 19960405 00594 WP 1996 4 5 MWEA96096 1 19960330 A 5520 SKIN DOUG DC9 DC932 3022066 WP LT ELEVATOR LIGHTNING STRIKE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND LT ELEVATOR UPPER SKIN HAS LIGHTNING STRIKE DAMAGE ON FIBERGLASS TRAILING EDGE NEAR OUTBD END. INSTALLED REPAIR I AW SRM 55-03 FIG 15, WEIGHT AND BAL COMPLIED WITH. 2 L 7 2 4F A6WE 1996040500595 19960405 00595 WP 1996 4 5 MWEA96097 1 19960330 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 229 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND NR 4 SEAT TRACK CORRODED AT STA 229. INSTALLED REPAIR IAW SRM 53-05 FIG 4 SHT 1. 2 L 7 2 4F A6WE 1996040500596 19960405 00596 WP 1996 4 5 MWEA96098 1 19960330 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP CABIN CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND NR 3 SEAT TRACK CORRODED BEYOND LIMITS. INSTALLED REPAIR IAW SRM 53-05 FIG 4A SHT 1. 2 L 7 2 4F A6WE 1996040500597 19960405 00597 WP 1996 4 5 MWEA96099 1 19960330 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 503 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND NR 3 SEAT TRACK CORRODED BEYOND LIMITS AT STA 503. INSTALLED REPAIR IAW SRM 53-05 FIG 4A. 2 L 7 2 4F A6WE 1996040500598 19960405 00598 WP 1996 4 5 MWEA96100 1 19960330 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE LIGHTNING STRIKE A MWEA K NONE C F.O.D. IN INSP/MAINT 1 GL 31 207ME 47794 FOUND NUMEROUS LIGHTNING STRIKES ON UPPER FUS AT LONGERON 2R AND 3R. INSTALLED REPAIRS IAW SRM 53-04 FIG 38 VIEW H. 2 L 7 2 4F A6WE 1996040500599 19960405 00599 WP 1996 4 5 MWEA96101 1 19960330 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP CABIN CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND NR 3 SEAT TRACK CORRODED FROM STA 210 TO 229. SPLICED IN NEW SECTION OF SEAT TRACK IAW SRM 53-05 FIG 4A. 2 L 7 2 4F A6WE 1996040500600 19960405 00600 NE 1996 4 5 MWEA96102 2 19960322 A 7200 ENGINE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7B 52053 NE RIGHT FAILED A MWEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 31 302ME 47102 653655 AT CRUISE A LOUD NOISE CAME FROM RT ENGINE. EPR AND N1 DROPPED, ENG OIL STRAINER CLOGGING LIGHT ILLUMINATED AND OIL TEM P WENT TO 115. MADE UNSCHEDULED LANDING, FORT SMITH AR. FOUND BRASS LIKE METAL IN OIL FILTER AND REPLACED ENGINE. SUS PECT GEARBOX PROBLEM, WILL BE ANALYZED FURTHER. 2 L 7 2 4F 4 F A6WE E2EA 1996040500601 19960405 00601 WP 1996 4 5 MWEA9672 1 19960330 A 5230 DOOR DOUG DC9 DC932 3022066 WP CARGO COMPT GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FWD CARGO DOOR GOUGED BY FWD DOOR CAM. INSTALLED REPAIR IAW SRM 52-01 FIG 2 SHT 3. 2 L 7 2 4F A6WE 1996040500602 19960405 00602 WP 1996 4 5 RRXA96015 1 19960312 A 5730 5616122519 PANEL DOUG DC8 DC863 302198A WP RT WING DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 797AL 46163 KMCN - DURING C-CHECK, FOUND UPPER ACCESS PANEL 505C HAD ATTACH SCREW HOLE DAMAGE RIGHT WING. MAINTENANCE REMOVED THE D AMAGED AREA, FABRICATED BUSHING AND INSTALLED IAW DER APPROVED COTNEY ENGINEERING SKETCH A27-R01. (M) 2 L 7 4 4F 4A25 1996040500604 19960405 00604 WP 1996 4 5 9607529860 1 19960401 A 3241 ANTI-SKID COMP DOUG DC9 DC951 3022051 WP E/E COMPT FAILED A NWAA K NONE O OTHER LD LANDING 1 GL 01 769NC 47757 DURING LANDING WITH ANTI-SKID ON MEL, THE NR 2 AND NR 3 TIRES BLEW, NO DAMAGE TO AIRFRAME. CHANGED NR 2 AND NR 3 TIRES. REPLACED NR 1 ANTI-SKID VALVE AND ANTI-SKID COMPUTER. ANTI-SKID SYSTEM OPERATIONALLY CHECKED GOOD. 2 L 7 2 4F A6WE 1996040500605 19960405 00605 WP 1996 4 5 9607539942 1 19960401 A 7722 152BL705P EGT INDICATOR DOUG DC9 DC932 3022066 WP PWA JT8 JT8D15 52051 NE NR 1 ENGINE FAILED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 3991C 25396 2062 47175 674407 NR 1 ENGINE EGT INDICATION FAILED IN FLIGHT AND AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLA CED THE EGT INDICATOR WITH A SERVICEABLE UNIT. 2 L 7 2 4F 4 F A6WE E2EA 1996040500606 19960405 00606 EU 1996 4 5 9607543244 1 19960331 A 3350 321454 POWER SUPPLY AIRBUS 320 A320211 3930320 EU CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 344NW 15678 5018 388 DURING LINE MAINTENANCE, THE EMERGENCY LIGHTS TEST FAILED 'INT LOADS AFT LEFT'. REPLACED POWER SUPPLY AND OPERATIONAL C HECK OK. 2 L 7 2 4F RT A28NM 1996040500607 19960405 00607 EU 1996 4 5 9607553246 1 19960401 A 3350 321454 POWER SUPPLY AIRBUS 320 A320211 3930320 EU CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 346NW 10158 242 400 DURING LINE MAINTENANCE, THE EMERGENCY LIGHTS TEST FAILED EPSU 13WL. REPLACED EPSU AND OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996040500608 19960405 00608 NM 1996 4 5 96DHL70701D 1 19960209 A 5347 1520792 SEAT TRACK BOEING 727 72722 1384002 NM BS 600-740 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT D-CHECK, NUMBER 6 SEAT TRACK WAS CORRODED FROM BS 600 TO BS 740 RBL 44. INSTALLED NEW SEAT TRACK PER SRM 53-10-5 AN D 53-30-2. 2 L 7 3 4F A3WE 1996040500609 19960405 00609 NM 1996 4 5 96FDEA00731 1 19960402 A 3230 RETRACT MECH DOUG MD11 MD11F 3023600 NM LANDING GEAR MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 601FE 48401 AFTER TAKEOFF, THE LANDING GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. ACCOMPLISHED CHECKLIST AND LANDED. WE HAD NO SE WHEEL STEERING AVAILIABLE IN FLT AND THE AUTOPILOT AND THE FCP WORKED NORMALLY. RESET AND SAFTIED MLG TRIM CYLINDER INTERLOCK CYL FUSE PER MM 32-37-00. JACKED A/C AND PERFORMED 3 SUCCESSFUL GEAR SWINGS. 2 L 7 3 4F RT A22WE 1996040500610 19960405 00610 NM 1996 4 5 96FDEA00732 1 19960403 A 5320 WEB BOEING 727 72722 1384002 NM BS 760.95 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 UPON REMOVAL OF PRESSURE PAN, FOUND CORROSION ON WEB BS 760.95 WL 207 LBL 65 TO 68. REPAIRED BS 760.95 WEB WL 207 LBL 6 5-68 PER FEDEX EA 7-5310-28183. 2 L 7 3 4F A3WE 1996040500611 19960405 00611 NM 1996 4 5 96FDEA00733 1 19960403 A 5320 STRAP BOEING 727 72722 1384002 NM BS 825.95 MISDRILLED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 187FE 19079 WHILE WORKING 7-5310-7-3367B PT9, DISCOVERED FASTENER HOLES INTERFERED WITH RADIUS OF ANGLE AT BS 825.95 WL 207 TO 198 L BL 65, DUE TO INSTALLATION OF REPAIR STRAP. REPAIRED STRAP BS 825.95 WL 207 TO 198 LBL 65 PER FEDEX EA 7-5310-28184. 2 L 7 3 4F A3WE 1996040500612 19960405 00612 NM 1996 4 5 96UAL900233 1 19960402 A 3350 REFLECTOR BOEING 737 737322 1384676 NM GE CFM56 CFM563B1 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 385UA 24660 EMERGENCY EXIT LIGHT INOP AT DOOR TWO RIGHT HAND. REPLACED REFLECTOR ASSEMBLY, CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1996040500613 19960405 00613 NM 1996 4 5 DL72E960725 1 19960315 A 5754 651622374 HEAT SHIELD BOEING 727 727247 138408F NM NR 7 LE SLAT DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 830WA 21482 DURING INITIAL INSPECTION OF THE NR 7 LEADING EDGE SLAT, A DENT WAS FOUND IN THE HEAT SHIELD BETWEEN THE NR 11 AND NR 12 RIB. THE DENT WAS REPAIRED PER M/M 57-50-3 FIG 4. 2 L 7 3 4F A3WE 1996040500614 19960405 00614 NM 1996 4 5 DL72E960726 1 19960315 A 5754 651622374 RIB BOEING 727 727247 138408F NM NR 7 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 830WA 21482 DURING INITIAL INSPECTION OF THE NR 7 LEADING EDGE SLAT, THE NR 10 RIB WAS FOUND TO BE CRACKED. THE RIB WAS REPAIRED PE R M/M 57-54-0 FIG 814. 2 L 7 3 4F A3WE 1996040500615 19960405 00615 NM 1996 4 5 DL72E960728 1 19960315 A 5754 651622374 RIB BOEING 727 727247 138408F NM NR 7 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 830WA 21482 DURING INITIAL INSPECTION OF THE NR 7 LEADING EDGE SLAT, THE NR 8 RIB WAS FOUND TO BE CRACKED. THE RIB WAS REPAIRED PER M/M 57-54-0. 2 L 7 3 4F A3WE 1996040500616 19960405 00616 NM 1996 4 5 DL72S960721 1 19960331 A 2450 CIRCUIT BREAKER BOEING 727 727232 1384082 NM E/E COMPT CRACKED A DALA K NONE H ELECT. POWER LOSS-50 PC LD LANDING 1 SO 27 467DA 20744 ON FINAL, ALL 3 BUS TIE BREAKERS TRIPPED, PHASE UNBALANCE, OVER EXCITED NR 2 AND NR 3, NR 1 TR UNIT C/B POPPED. FOUND A PU GEN BREAKER CRACKED WITH LOOSE CONNECTIONS. REPLACED SAME. ALSO, REPLACED NR 1 ENG GEN BREAKER. RAN ENGS PARALLELE D, ALL CHECKS NORMAL. 2 L 7 3 4F A3WE 1996040500617 19960405 00617 NM 1996 4 5 DL72S960723 1 19960331 A 3350 TRACK LIGHTS BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST CR CRUISE 1 SO 27 470DA 20747 FIRST CLASS TRACK LIGHTS INOP. REPAIRED WIRING AT 3B AND REPLACED FUSE AT PWR SUPPLY, OPS OK. 2 L 7 3 4F A3WE 1996040500618 19960405 00618 NM 1996 4 5 DL733960710 1 19960330 A 3320 BALLAST BOEING 737 737347 1384647 NM CABIN SMOKING A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 302WA 23182 SIDEWALL LIGHTS ROW 23 TO 25 MOMENTARILY WENT OUT AND SMOKED. PULLED AND COLLARED C/B FOR RT SIDE, FWD TO MCO. REPLACE D BALLAST AND RELAMPED, OPERATION NORMAL. 2 L 7 2 4F RT A16WE 1996040500619 19960405 00619 1996 4 5 DL73E960686 4 19960328 A 3416 36023F2360140 ALTIMETER HOSE BOEING 737 737247 138448D NM LT COCKPIT LEAKING A DALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 27 244WA 23518 AT FL 240, CAPT AND F/O ALTIMETERS DIFFER BY 150 FT, PLACING CAPT ON ALT STATIC AND F/O NORMAL, F/O READ 150 FT HIGH AND CAPT READ CLOSE TO STANDBY. WITH F/O ON ALT AND CAPT NORMAL, F/O READS 100 FT LOW. FOUND HOSE TO STANDBY IND LEAKING AND REPLACED WITH APPROVED HOSE. LEAK CHECKS NORMAL PER M/M CHAPTER 34. 2 L 7 2 4F A16WE 1996040500620 19960405 00620 NM 1996 4 5 DL73E960716 1 19960327 A 3350 BATTERY PACK BOEING 737 7372J8 1384489 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 235WA 22859 DURING LAYOVER, EMERGENCY LIGHTS FOR OVERWING EMERGENCY EXITS FAILED TEST. REPLACED BATTERY PACK, OPERATION NORMAL. 2 L 7 2 4F RT A16WE 1996040500621 19960405 00621 NM 1996 4 5 DL76P960718 1 19960331 A 3350 BPS73 POWER SUPPLY BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 140LL 25988 ON PREFLIGHT, F0UND 2 EMERGENCY TRACK LIGHT STRIPS INOP. MTC FOUND L9028, L9021, L9007, L9010, L9008, L9011, L9022 AND L9030 ALL INOP. REPLACED BATTERY POWER SUPPLY M9008, OPERATION NOW NORMAL. 2 L 7 2 4F RT A1NM 1996040500622 19960405 00622 NM 1996 4 5 DLM88960724 1 19960331 A 3260 UPLOCK SENSOR DOUG MD88 MD88 3023688 NM NLG MALFUNCTIONED A DALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 27 931DL 49718 NOSE GEAR UNSAFE LIGHT ILLUMINATED AT CRUISE ALTITUDE AND REMAINED ILLUMINATED WHEN AUX AND TRANSFER PUMPS TURNED ON. R EPLACED NOSE GEAR UPLOCK SENSOR, SWUNG NOSE GEAR AND PERFORMED BITE ON PROX BOX, ALL INDICATIONS NORMAL. 2 L 7 2 4F RT A6WE 1996040500623 19960405 00623 1996 4 5 96ZZZX1500 4 19960314 A 2562 BP1025 BATTERY MERL CIR10 BEECH 200 200BEECH 1152920 CE ELT LEAKING A QLIA K NONE O OTHER IN INSP/MAINT 1 SW 15 18DN 22827 BB81 AT A YEARLY INSPECTION OF THE ELT, THE BATTERY WAS FOUND LEAKING AND CORROSION WAS STARTING IN ELT CASE. 1 L 7 2 4T A24CE 1996040500629 19960405 00629 CE 1996 4 5 96ZZZX1506 1 19960306 A 3230 MS250261 SWITCH BEECH 58 58 1152740 CE MLG UPLIMIT REQ LUBE A CUIA O OTHER J WARNING INDICATION AP APPROACH 1 WP 17 140S 4537 TH1155 WHEN LANDING GEAR SELECTED TO DOWN POSITION, MOTOR DID NOT RUN. PILOT MANUALLY EXTENDED GEAR. AIRCRAFT PLACED ON JACKS AND RETRACT TEST PERFORMED. FOUND SWITCH ACTUATING ARM STICKEY. CLEANED AND LUBED AS REQUIRED. SWITCH ACTUATED CORRE CTLY. TWELVE GEAR SWINGS PERFORMED, OK. TEST FLIGHT MADE, GEAR ACTUATED 6 TIMES, NO FAILURE TO RETRACT. 1 L 7 2 3O 3A16 1996040500636 19960405 00636 SO 1996 4 5 96ZZZX1513 1 19960227 A 3710 842CW PUMP AIRBORNE PIPER PA31 PA31P 7103120 SO VAC DRIVE SHAFT FAILED A EKIA K NONE O OTHER IN INSP/MAINT 1 WP 07 252MA 275 10AJ27 31P33 DRIVE COUPLING SHEARED FOLLOWING PUMP FAILURE. PUMPS SEEM TO ONLY RUN ABOUT 400 HOURS PRIOR TO FAILURE. SUBMITTER HAS 5 AIRCRAFT RUNNING 2 EACH PER AIRCRAFT. 1 L 7 2 3O A8EA 1996040500684 19960405 00684 1996 4 5 96ZZZX1561 4 19960305 A 6113 05502368 SPINNER CESSNA 172 172P 2072436 CE BLADE CUT OUT CRACKED A P GJAA K NONE O OTHER IN INSP/MAINT 1 NM 01 54983 449 170275098 INSPECTION FOUND CRACK ON LEADING EDGE OF BLADE CUT-OUT, HEADING TOWARDS NEAREST SCREW HOLE. ONE SIDE ONLY. SUBMITTER STATED HAVE HAD 5 CRACKED SPINNERS ON DIFFERENT ACFT IN THE LAST YEAR. 1 H 7 1 3O NT 3A12 1996040500728 19960405 00728 NM 1996 4 5 96ZZZM603 1 19960308 A 5313 6545768512 STRINGER BOEING 737 737290C 138448V NM BS 500B CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING D-CHECK A CRACK WAS FOUND AT THE ENDS OF STRINGER 16R, BS 500B WHICH TERMINATES AT THE OVERWING LIGHT. REP AIRED PER EA 5310-01400 AND BOEING SB 737-53-1145. REFERENCE ASAA9610031. 2 L 7 2 4F A16WE 1996040500729 19960405 00729 NM 1996 4 5 96ZZZM604 1 19960216 A 2730 BOB WEIGHT BOEING 727 727223 1384074 NM RT ELEV TAB CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20191 RIGHT ELEVATOR TAB, 3 EACH BOB WEIGHTS CRACKED. REPAIRED WEIGHTS PER MM 27-30-11 TAB BALANCE CHECKED PER SRM 51-80-9. ( M) 2 L 7 3 4F A3WE 1996040500730 19960405 00730 NM 1996 4 5 96ZZZM605 1 19960301 A 3230 DRUM BOEING 727 727223 1384074 NM LT MLG DIRTY A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20191 LEFT MAIN LANDING GEAR MANUAL EXTENSION DRUM WILL NOT ROTATE. LUBED MECHANISM, OPS CHECK GOOD PER MM 32-34-0. (M) 2 L 7 3 4F A3WE 1996040500736 19960405 00736 EU 1996 4 5 96ZZZM611 1 19960129 A 2810 SD3566001XA FUEL TANK STBROS SD3 SD360 8100606 EU LT UPPER DAMAGED A TRBA O OTHER K FLUID LOSS IN INSP/MAINT 1 SO 21 362MQ 23241 SH3612 AIRCRAFT ARRIVED WITH A HOLE IN THE FUSELAGE ON TOP OF FUEL TANK WITH LEAK COMING OUT OF LEFT UPPER FUSELAGE. PERFORMED REPAIR AND SEALED AREA PER STRUCTURAL REPAIR MANUAL 530000. 2 H 7 2 4T A41EU 1996040500738 19960405 00738 SO 1996 4 5 96ZZZM613 1 19960207 A 5270 SWITCH EMB 120 EMB120ER 3260203 SO AVIONICS DOOR OUT OF ADJUST A GLBA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 01 297UX 120297 SUX - CREW REPORTED SERVICE DOOR ANNUNCIATOR ILLUMINATED AFTER LIFTOFF. CREW ELECTED AN AIR TURN BACK AND MADE AN UNEVE NTFUL LANDING. MAINTENANCE ADJUSTED MICROSWITCH ON SERVICE DOOR. SYSTEM OPS CHECKED OK. (M) 2 L 7 2 4T RT A31SO 1996040500739 19960405 00739 1996 4 5 96ZZZM614 4 19960209 A 2210 7002260933 YAW DAMP SERVO BEECH 1900 1900C 1154161 CE AUTO PILOT FAILED A GLBA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CE 01 98GL 8198 UC98 CIU - CREW DETECTED SMELL OF ELECTRICAL SMOKE THEN YAW DAMP CB POPPED. MAINTENANCE REPLACED YAW DAMP SERVO, SYSTEM CHEC KED OK. (M) 2 L 7 2 4T RT A24CE 1996040500740 19960405 00740 SO 1996 4 5 96ZZZM615 1 19960305 A 6120 582855P4 VALVE HOUSING LKHEED 382 382E 526413U SO NR 2 PROP DEFECTIVE A SRAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 23 923SJ 4301 DURING FLIGHT AD08 NR 2 ENGINE RPM DECAYED TO 97 PERCENT, PRECAUTIONARY SHUTDOWN NR 2 ENGINE AND LANDED SAFELY AT AAB. F OUND NR 2 VALVE HOUSING MALFUNCTIONED, REPLACED VALVE HOUSING, PERFORMED ENGINE RUN, OPS CHECKED GOOD PER J/C 61013 AND 6103. 2 H 7 4 4T A1SO 1996040500741 19960405 00741 NM 1996 4 5 96ZZZM616 1 19960310 A 3350 90052 BATTERY CHARGER BOEING 727 727225 1384077 NM CABIN INOPERATIVE A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 918TS UA5019 20445 FORWARD ENTRY AISLE EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK AND BATTERY CHARGER OPERATIONAL CHECK OK. REFEREN CE TAOA039604. 2 L 7 3 4F A3WE 1996040500742 19960405 00742 NM 1996 4 5 96ZZZM617 1 19960310 A 3350 90052 BATTERY CHARGER BOEING 727 727225 1384077 NM CABIN INOPERATIVE A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 918TS 8203 20445 OVERWING EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK AND BATTERY CHARGER. OPERATIONAL CHECK OK. REFERENCE TAOA039605 . 2 L 7 3 4F A3WE 1996040500743 19960405 00743 NM 1996 4 5 96ZZZM618 1 19960306 A 8011 L925678 STARTER BOEING 757 7572S7 1384962 NM RROYCE RB211 RB211* 54555 NE NR 2 ENG FAILED A A AWXA A E UNSCHED LANDING ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 WP 28 906AW 27377 8761 94347 23568 JFK-PHX - ENGINE SHUTDOWN, AIRCRAFT DIVERTED TO CMH. NR 2 ENGINE SHUTDOWN IN FLIGHT DUE TO OIL QUANTITY DECREASING. RE MOVED THE COVER HOUSING OFF OF THE AIR/OIL SEPARATOR AND FOUND THE SEAL THAT GOES ON THE SEPARATOR SHAFT MISSING AND SHA FT GALLED, AS WELL AS THE BUSHING THAT GOES ON THE MATES TO THE COVER HOUSING AND SHAFT. REMOVED AND REPLACED 06 GEARBO X MODULE. STARTER FAILED DURING START. REMOVED AND REPLACED STARTER. REFERENCE AWXA960116. 2 L 7 2 4F 4 F RT A2NM A12EU 1996040500744 19960405 00744 WP 1996 4 5 96ZZZM619 1 19960301 A 7714 N2 INDICATOR LKHEED 1011 10113851 5265010 WP NR 1 ENG MALFUNCTIONED A RIAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 19 305GB 193P1127 FLT NR 7202 - KCLE/KMSP - AIRCRAFT ABORTED TAKEOFF AT 30 KNOTS DUE TO NR 1 ENGINE N2 OVERSPEED INDICATION. MAINTENANCE RESET N2 INDICATOR, INDICATOR PERFORMED NORMAL AT ALL ENGINE POWER SETTINGS. AIRCRAFT RELEASED FOR FLIGHT. 2 L 7 3 4F A23WE 1996040500745 19960405 00745 NE 1996 4 5 96ZZZM620 2 19960310 A 7532 563881 BLEED VLV BOEING 707 707330C 138367G NM PWA JT3D JT3D3B 52039 NE NR 3 ENG MALFUNCTIONED A CLCA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 19 707HE 20124 FLT NR 49 - MIA - TAKEOFF WAS ABORTED DUE TO NR 3 ENGINE COMPRESSOR STALL. VISUALLY INSPECTED ENGINE, FOUND NO DISCREPA NCIES. PERFORMED BORESCOPE, NO DISCREPANCIES. REMOVED AND REPLACED 12TH STAGE BLEED VALVE CONTROL. ENG RUN UP NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4 F 4A26 1E8 1996040500746 19960405 00746 NM 1996 4 5 96ZZZM621 1 19960229 A 3397 WIRE BOEING 737 7372T4 1384492 NM CABIN BROKEN A SPAA K NONE L NO TEST IN INSP/MAINT 1 WP 07 703S 22529 DURING SCHEDULED CHECK, THE FORWARD AREA LIGHT/EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. WIRING LEADING TO THE BATTER Y PACK POWER SUPPLY WAS FOUND TO BE BROKEN. THE WIRING WAS REPAIRED, SUBSEQUENT SYSTEM OPS CHECK WAS SATISFACTORY PER B -737 MM 33-51-11. (M) 2 L 7 2 4F A16WE 1996040500747 19960405 00747 NM 1996 4 5 96ZZZM622 1 19960308 A 2612 FIRE LOOP BOEING 737 7372T4 1384492 NM NR 1 ENG OUT OF POSITION A SPAA O OTHER N FALSE WARNING LD LANDING 1 WP 07 703S 22529 UPON LANDING AT TPA, THE NR 1 ENGINE OVERHEAT LIGHT CAME ON INTERMITTENTLY. THE NR 1 ENGINE OVERHEAT/FIRE DETECTION LOO PS WERE VISUALLY INSPECTED, SUSPECTED AREAS REPOSITIONED, CONNECTIONS CLEANED. SUBSEQUENT SYSTEM TESTS WERE SATISFACTOR Y PER BOEING MAINTENANCE MANUAL 26-11-0. 2 L 7 2 4F A16WE 1996040500748 19960405 00748 NM 1996 4 5 96ZZZM623 1 19960307 A 2612 655280915 FIRE DETECTOR BOEING 737 7372T4 1384492 NM NR 1 ENGINE INTERMITTENT A SPAA O OTHER N FALSE WARNING LD LANDING 1 WP 07 703S 22529 UPON LANDING AT TPA, THE NR 1 ENGINE OVERHEAT LIGHT CAME ON INTERMITTENTLY. THE FIRE DETECTION ACCESSORY UNIT WAS REPLA CED, SUBSEQUENT SYSTEM TEST WAS SATISFACTORY PER BOEING MM 26-11-0. 2 L 7 2 4F A16WE 1996040500754 19960405 00754 WP 1996 4 5 96ZZZM629 1 19960304 A 7930 FILTER CLOG IND DOUG DC9 DC951 3022051 WP NR 2 ENG MALFUNCTIONED A TWAA O OTHER N FALSE WARNING DE DESCENT 1 CE 05 418EA 47676 BNA - DURING DESCENT NR 2 ENGINE OIL FILTER CLOG LIGHT ILLUMINATED. REMOVED AND REPLACED OIL FILTER. PLACARDED FILTER CLOG INDICATOR LIGHT. (M) 2 L 7 2 4F RT A6WE 1996040500755 19960405 00755 NM 1996 4 5 96ZZZM630 1 19960308 A 3231 1U1084 SEQ VALVE BOEING 727 727231 1384079 NM LT MLG DOOR MALFUNCTIONED A TWAA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 54327 20234 MCI - AFTER TAKEOFF THE ELFT MAIN GEAR WOULD NOT RETRACT. REMOVED AND REPLACED LEFT MAIN GEAR DOOR SEQUENCE VALVE, MFG P/N 1U1084. ACCOMPLISHED GEAR SWING, OPERATIONAL CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1996040500756 19960405 00756 NM 1996 4 5 96ZZZM631 1 19960309 A 2781 1U11032 SWITCH BOEING 727 727231 1384079 NM NR 5 LE SLAT FAILED A TWAA O OTHER N FALSE WARNING CR CRUISE 1 CE 05 64346 21633 STL - DURING CRUISE LEADING EDGE AMBER LIGHTS ON FORWARD PANEL ILLUMINATED. REMOVED AND REPLACED NR 5 LEADING EDGE SLAT ACTUATOR SWITCH, MFG P/N 1U11032. OPERATIONAL CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1996040500757 19960405 00757 WP 1996 4 5 96ZZZM632 1 19960227 A 5312 BLKHD WEB LKHEED 1011 10113851 5265010 WP FS 1363 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 11003 193B1015 MCI - DURING SPECIAL CHECK, FOUND MULTIPLE CRACKS IN BULKHEAD AND STIFFENER WEBS, FS 1363, RBL 42.5, WL 102 TO WL 143. R EPAIRED PER SRM 51-10-02 AND 53-11-00. (M) 2 L 7 3 4F A23WE 1996040500758 19960405 00758 WP 1996 4 5 96ZZZM633 1 19960227 A 5312 BLKHD WEB LKHEED 1011 10113851 5265010 WP BS 1363 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 11003 193B1015 MCI - DURING SPECIAL CHECK, FOUND AFT BULKHEAD WEB CRACKED AT INBOARD SIDE OF WHEEL WELL STATION 1363, WL 102. REPAIRED PER SRM 53-11-00 AND 51-10-02. (M) 2 L 7 3 4F A23WE 1996040500759 19960405 00759 NM 1996 4 5 96ZZZM634 1 19960229 A 3350 58223 BATTERY PACK BOEING 747 747131 1384881 NM CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 93108 19674 STL - DURING ROUTINE MAINTENANCE, EMERGENCY EGRESS LIGHTS REMAINED ON. REMOVED AND REPLACED LOW BATTERY PACK, MFG P/N 5 822-3. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F A20WE 1996040500760 19960405 00760 WP 1996 4 5 96ZZZM635 1 19960302 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG REQ'D SERVICE A TWAA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 909TW 49170 LNK - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, NOSE LANDING GEAR DID NOT RETRACT. CYCLES LANDING GEAR. FOUND NOS E LANDING GEAR STRUT LOW. SERVICED NOSE LANDING GEAR STRUT WITH NITROGEN. NOSE LANDING GEAR OPERATION AND INDICATION C HECKED NORMAL. (M) 2 L 7 2 4F A6WE 1996040500761 19960405 00761 WP 1996 4 5 96ZZZM636 1 19960303 A 3260 PROX SENSOR LKHEED 1011 10113851 5265010 WP LT MLG DOOR OUT OF ADJUST A TWAA O OTHER N FALSE WARNING CL CLIMB 1 CE 05 31008 193B1028 MCO - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, LEFT MAIN LANDING GEAR DOOR LIGHT REMAINED ILLUMINATED. CYCLED LAN DING GEAR. FOUND LEFT MAIN LANDING GEAR DOOR PROXIMITY SENSOR OUT OF ADJUSTMENT. ADJUSTED PROXIMITY SENSOR TO MAINTENA NCE MANUAL LIMITS. LANDING GEAR DOOR OPERATION AND INDICATION CHECKED NORMAL. 2 L 7 3 4F A23WE 1996040500762 19960405 00762 NM 1996 4 5 ASAA9610024 1 19960306 A 7120 654954614 SUPPORT FITTING BOEING 737 737290C 138448V NM NR 2 ENGINE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING D-CHECK, THE NR 2 ENGINE OUTBOARD THRUST LINK AFT SUPPORT FITTING WAS FOUND TO HAVE A GOUGE ON THE LOWER SU RFACE. AFTER BLENDING OF THE GOUGED AREA, A CRACK WAS FOUND AT THE BOTTOM OF THE BLEND AREA. REPLACED SUPPORT FITTING. (M) 2 L 7 2 4F A16WE 1996040500763 19960405 00763 NM 1996 4 5 ASAA9610026 1 19960308 A 5314 6545866688 KEEL BEAM BOEING 737 737290C 138448V NM BS 716/720 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING D-CHECK, THE KEEL BEAM AT LBL 6.30 AND RBL 6.30, BL 716 AND 720 WAS FOUND TO BE CORRODED. REPAIRED PER EA 5310-01401 AND BOEING TELEX ASA-SEA-96-0055RR. (M) 2 L 7 2 4F A16WE 1996040500764 19960405 00764 NM 1996 4 5 ASAA9610027 1 19960308 A 5315 65671408 FLOOR BEAM BOEING 737 737290C 138448V NM BS 578 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING D-CHECK, THE LONGITUDINAL FLOOR BEAM INBOARD FLANGE AT RBL 45.5, BS 578 WAS FOUND CORRODED. REPAIRED PER E A 5310-01403 AND BOEING TELEX ASA-SEA-96-0061RR. (M) 2 L 7 2 4F A16WE 1996040500765 19960405 00765 NM 1996 4 5 ASAA9610028 1 19960308 A 5315 65549064 FLOOR BEAM BOEING 737 737290C 138448V NM BS 520 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING D-CHECK, A CRACK WAS FOUND IN THE RADIUS OF THE UPPER FLANGE TO WEB OF THE FLOOR BEAM AT BS 520, RBL 24.75. REPAIRED PER EA 5320-01260 AND BOEING SB 737-53-1120. (M) 2 L 7 2 4F A16WE 1996040500766 19960405 00766 NM 1996 4 5 ASAA9610029 1 19960308 A 5315 65549071 FLOOR BEAM BOEING 737 737290C 138448V NM BS 727B CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING D-CHECK, THE FLOOR BEAM AT BS 727B WAS FOUND TO HAVE CORROSIO ON THE UPPER CHORD FORWARD AND AFT FLANGE BET WEEN RBL 15 TO RBL 55, CONCENTRATED AT A FASTENER HOLE ON THE UPPER SURFACE OF THE FLANGE. REPAIRED PER EA 5310-01406 A ND BOEING TELEX ASA-SEA-96-0077RR. (M) 2 L 7 2 4F A16WE 1996040500767 19960405 00767 NM 1996 4 5 ASAA9610030 1 19960308 A 5315 65671406 FLOOR BEAM BOEING 737 737290C 138448V NM BS 600-727 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING D-CHECK CORROSION WAS FOUND ON THE LONGITUDINAL FLOOR BEAM INBOARD FLANGE AT BL 0, BS 600, BS 680, BS 687, AND AT RBL 25, BS 727. REPAIRED PER EA 5310-01412 AND BOEING TELEX ASA-SEA-96-0098. (M) 2 L 7 2 4F A16WE 1996040500768 19960405 00768 NM 1996 4 5 ASAA9610031 1 19960308 A 5313 6545768509 STRINGER BOEING 737 737290C 138448V NM BS 500B CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING D-CHECK A CRACK WAS FOUND AT THE ENDS OF STRINGER 16R, BS 500B WHICH TERMINATES AT THE OVERWING LIGHT. REP AIRED PER EA 5310-01400 AND BOEING SB 737-53-1145. (M) 2 L 7 2 4F A16WE 1996040500769 19960405 00769 NM 1996 4 5 ASAA9610032 1 19960309 A 5315 65549141 FLOOR BEAM BOEING 737 737290C 138448V NM BS 967 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING D-CHECK, CORROSION FOUND ON THE UPPER CHORD FLANGE OF THE FLOOR BEAM AT RBL 24.5 AND RBL 45, BS 967. DUE T O PREVIOUS REPAIRS THE FLANGE MUST BE RESTORED TO PROVIDE FUTURE ACCOMPLISHMENT OF SRM REPAIRS. REPAIRED PER EA 5310-01 407 AND BOEING TELEX ASA-SEA-96-0086RR. 2 L 7 2 4F A16WE 1996040500770 19960405 00770 NM 1996 4 5 ASAA9640014 1 19960229 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 776AS 25109 SMF - FLT NR 409 - DURING CREW PRE-FLIGHT THE CREW REPORTED THAT THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE INOPERATIVE ROWS 23-25. RECONNECTED WIRES IN SECTION OF INOPERATIVE TRACK LIGHTS AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996040500771 19960405 00771 NM 1996 4 5 ASAA9640015 1 19960302 A 3350 900835A BATTERY PACK BOEING 737 7374Q8 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 775AS 25108 SEA - DURING MAINTENANCE CHECK, THE AFT 6 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED LIGHTS AND REPLACED AFT BATTERY PACK. LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996040500772 19960405 00772 NM 1996 4 5 ASAA9640016 1 19960305 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 763AS 25100 JNU - DURING MAINTENANCE CHECK, FOUND TWO SECTIONS OF EMERGENCY EXIT TRACK LIGHTS INOPERATIVE FORWARD CABIN AREA. RECON NECTED LOOSE WIRES AT ROW 1C AND REPAIRED BROKEN WIRES AT FORWARD COAT CLOSET. EMERGNCY EXIT LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996040500773 19960405 00773 WP 1996 4 5 ASAA9680056 1 19960220 A 5210 HANDLE MECHANISM DOUG DC9 DC983 3022083 WP R1 DOOR LACK OF LUBE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 950AS 53023 SEA - DURING MAINTENANCE CHECK, THE R1 DOOR WAS FOUND DIFFICULT TO OPEN. LUBED THE DOOR HANDLE MECHANISM AND OPERATED N ORMALLY. (M) 2 L 7 2 4F RT A6WE 1996040500774 19960405 00774 WP 1996 4 5 ASAA9680060 1 19960224 A 3350 41B007AD07G3 BATTERIES DOUG DC9 DC982 3022082 WP AFT CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 956AS 48079 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE AFT GALLEY AREA WERE FOUND INOPERATIVE. REPLACED T HE BATTERIES AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996040500775 19960405 00775 WP 1996 4 5 ASAA9680062 1 19960226 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 969AS 53063 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 25 TO 28 WERE FOUND INOPERATIVE. RECONNECTED WIRING AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996040500776 19960405 00776 1996 4 5 ASAA9680063 4 19960228 A 2565 D29984103 SLIDE DOUG DC9 DC983 3022083 WP TAILCONE FAILED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 974AS 53450 OAK - DURING C-CHECK, THE TAILCONE EMERGENCY EVACUATION SLIDE EMERGENCY LIGHTS FAILED TEST. REPLACED THE TAILCONE EMERG ENCY EVACUATION SLIDE. (M) 2 L 7 2 4F RT A6WE 1996040500777 19960405 00777 WP 1996 4 5 ASAA9680066 1 19960302 A 5210 GUST LOCK MECH DOUG DC9 DC983 3022083 WP L1 DOOR MALFUNCTIONED A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 977AS 53453 SEA - AFTER ARRIVAL OF FLT NR 233 - CREW REPORTED THE L1 DOOR EXTERNAL LATCH WOULD NOT RELEASE. LUBRICATED GUS LOCK MEC HANISM AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996040500778 19960405 00778 SO 1996 4 5 ASOA96001 1 19960205 A 2612 6468 CONTROL MODULE EMB 120 EMB120RT SO APU DEFECTIVE A ASOA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 11 240AS 120060 EN ROUTE FROM BPT-DFW, THE APU FIRE LIGHT ILLUMINATED AND THE FIRE EXTINGUISHER DISCHARGED. FLIGHT RETURNED TO BPT, WHE RE AND FBO MECHANIC INSPECTED THE APU AND FOUND NO EVIDENCE TO INDICATE A FIRE. THE APU WAS DEFERRED AND THE FLIGHT CON TINUED ON TO DFW. REMOVED AND REPLACED APU FIRE CONTROL MODULE, LAMP TEST RELAY AND FIRE BOTTLE. OPS CHECK GOOD AND FI RE TEST NORMAL. AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M) 2 L 7 2 4T RT A31SO 1996040500779 19960405 00779 SO 1996 4 5 ASOA96003 1 19960213 A 3040 D0036 CURRENT SENSOR EMB 120 EMB120RT SO RT WINDSHIELD DEFECTIVE A ASOA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 11 266AS 120188 INBOUND LEI-ATL, 50 MILES IN RANGE OF ATL, ACRID SMOKE BEGAN FLOWING FROM THE RIGHT PANEL. DC BUSS 2 WAS DE-ENERGIZED A ND SMOKE STOPPED. EMERGENCY CREWS WERE CALLED OUT AS A PRECAUTION. LANDING WAS MADE SAFELY AND WITHOUT INCIDENT IN ATL . REMOVED AND REPLACED CURRENT SENSOR K0036 FOR THE RIGHT WINDSHIELD HEAT. CURRENT SENSOR WAS BURNED DUE TO A LOOSE WI RE (SOLDER JOINT WAS BROKEN). OPS CHECK WAS GOOD, AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1996040500780 19960405 00780 NM 1996 4 5 AWXA960107 1 19960227 A 3350 FUSE BOEING 737 73733A 1384673 NM CABIN BLOWN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 173AW 23632 PHX - FLT NR 480 - DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT MOUNTED EMERGENCY EXIT LIGHTS INOP ROW 1-6. REPLACED BL OWN FUSE IN BATTERY CHARGER ASSEMBLY. OPS GOOD. (M) 2 L 7 2 4F RT A16WE 1996040500781 19960405 00781 NE 1996 4 5 AWXA960116 2 19960306 A 7260 M06622AA GEARBOX BOEING 757 7572S7 1384962 NM RROYCE RB211 RB211* 54555 NE NR 2 ENG FAILED A A AWXA A E UNSCHED LANDING ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 WP 28 906AW 27377 8761 DM3676 23568 JFK-PHX - ENGINE SHUTDOWN, AIRCRAFT DIVERTED TO CMH. NR 2 ENGINE SHUTDOWN IN FLIGHT DUE TO OIL QUANTITY DECREASING. RE MOVED THE COVER HOUSING OFF OF THE AIR/OIL SEPARATOR AND FOUND THE SEAL THAT GOES ON THE SEPARATOR SHAFT MISSING AND SHA FT GALLED, AS WELL AS THE BUSHING THAT GOES ON THE MATES TO THE COVER HOUSING AND SHAFT. REMOVED AND REPLACED 06 GEARBO X MODULE. STARTER FAILED DURING START. REMOVED AND REPLACED STARTER. (M) 2 L 7 2 4F 4 F RT A2NM A12EU 1996040500782 19960405 00782 EU 1996 4 5 AWXA960117 1 19960307 A 2130 87292325V04 COMPUTER AIRBUS 320 A320231 3930325 EU E/E BAY FAILED A AWXA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 28 624AW 38 55 PHX/CMH - FLT NR 266 - ABORTED TAKEOFF, AVIONICS SKIN VALVE FAULT ON TAKEOFF ROLL. REMOVED AND REPLACED AVIONICS VENT C OMPUTER. (M) 2 L 7 2 4F RT A28NM 1996040500783 19960405 00783 EU 1996 4 5 AWXA960118 1 19960309 A 2160 341E010000 THERMO TEMP LMTR AIRBUS 320 A320231 3930325 EU NR 2 ENGINE FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 620AW 13623 00344 052 LAS/SEA - FLT 0843 - AIR TURN-BACK. CLASS 1 ECAM MESSAGE 'AIR ENGINE 2 BLEED ABNORMAL PRESSURE. CREW REPORTED THAT ON DESCENT BACK TO LAS, THE NR 2 ENGINE BLEED AIR WOULD RESET AND H.P. VALVE OPENED. PLACED ON MEL 36-11-1. MEL CLEARED 3 -10-96: REMOVED AND REPLACED THERMO TEMP LIMITER SOLENOID AND BLEED PRESSURE REGULATOR VALVE. REFERENCE OPERATOR CONTR OL NUMBER 96ZZZX2306. (X) 2 L 7 2 4F RT A28NM 1996040500784 19960405 00784 EU 1996 4 5 AWXA960125 1 19960313 A 5754 SKIN AIRBUS 320 A320231 3930325 EU NR 4 LE SLAT DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 637AW 099 PAE - FLT NR 3791 - DURING ROUTINE SCHEDULED C-4/S-1 MAINTENANCE CHECK, FOUND DENT ON RIGHT NR 4 SLAT ON L/E, 1540 MM C/ B FROM THE SLAT I/B END. REPAIRED DENT IAW ER 32-27-83-02C. (M) 2 L 7 2 4F RT A28NM 1996040500785 19960405 00785 EU 1996 4 5 AWXA960126 1 19960307 A 5320 ASNA2495 THRESHOLD AIRBUS 320 A320231 3930325 EU AFT SERVICE DOOR CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 637AW 099 PAE - FLT NR 3791 - DURING ROUTINE SCHEDULED C-4/S-1 MAINTENANCE CHECK, FOUND CORROSION AT AFT SERVICE DOOR THRESHOLD SU PPORT STRUCTURE X3254, 3CM FORWARD OF FR 68, Y-1250, Z-540. REMOVED CORRODED AREA AND FABRICATED REPAIR PART. ALODINED , PRIMED AND INSTALLED AT X3254, Y-1250, Z-540 PER SRM 53-00-14. (M) 2 L 7 2 4F RT A28NM 1996040500786 19960405 00786 EU 1996 4 5 AWXA960127 1 19960307 A 5320 ASNA2199 THRESHOLD EXT AIRBUS 320 A320231 3930325 EU AFT SERVICE DOOR CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 637AW 099 PAE - FLT NR 3791 - DURING ROUTINE SCHEDULED C-4/S-1 MAINTENANCE CHECK, FOUND CORROSION AT AFT SERVICE DOOR THRESHOLD SU PPORT STRUCTURE X3254, 3 CM FORWARD OF FR 68, Y-1250, Z-540. REMOVED CORROSION AND CUT OUT UPPER FLANGE. FABRICATED PA RT AND INSTALLED AT 3254, Y1250, Z-540 PER SRM 53-00-14. 2 L 7 2 4F RT A28NM 1996040500787 19960405 00787 EU 1996 4 5 AWXA960128 1 19960313 A 5320 SUPPORT RAIL AIRBUS 320 A320231 3930325 EU BS 440 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 637AW 099 PAE - FLT NR 3791 - DURING ROUTINE SCHEDULED C-4/S-1 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR SUPPORT RAIL AT AFT LEF T LAV HOLD DOWN SUPPORT X3155, 3 CM FORWARD OF FR 66, Y-440 - Z540. REPAIRED FLOOR SUPPORT RAIL PER AWA ER 32-53-15-04. (M) 2 L 7 2 4F RT A28NM 1996040500788 19960405 00788 EU 1996 4 5 AWXA960129 1 19960309 A 5320 D53472089000 SUPPORT RAIL AIRBUS 320 A320231 3930325 EU BS 1200 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 637AW 099 FLT NR 3791 - PAE - DURING ROUTINE SCHEDULED C-4/S-1 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR SUPPORT RAIL X3259, 2 C M AFT OF FR 68, Y-1200, Z-540. REMOVED CORROSION ON FLOOR SUPPORT RAIL AT X3259, Y-1200, Z-540. FABRICATED PARTS FILLE T RELIEF WASHERS, SPACERS ALODINED AND PRIMED, INSTALLED FASTENERS PER SRM 53-00-14. (M) 2 L 7 2 4F RT A28NM 1996040500789 19960405 00789 SO 1996 4 5 C2XA96IA059 1 19960224 A 3231 12032943001 SEQUENCE VLV EMB 120 EMB120RT SO RT MLG DOOR FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 16710 563 120106 IAH - FLT NR 2522 - AFTER TAKEOFF, UPON RETRACTION OF LANDING GEAR A LOUD RUMBLING NOISE WAS HEARD. FLIGHT CREW CYCLED LANDING GEAR, NOISE CONTINUED. AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED SEQUENCE VALVE FOR RT MLG INBOARD FORWARD DOOR. PERFORMED OPERATIONAL CHECK, NO DEFECTS NOTED. A/C RETURNED TO SERVICE . (M) 2 L 7 2 4T RT A31SO 1996040500790 19960405 00790 EU 1996 4 5 C2XA96IA060 1 19960304 A 3230 D22716000101 FREE FALL ASSIST AEROSP ATR42 ATR42320 8680930 EU RT MLG FAILED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 27806 12661 15504 MN251 075 IAH - DURING ACCOMPLISHMENT OF FREE FALL FUNCTIONAL TEST ATR 42 JIC 32-33-00 FUT 10000-002, THE RIGHT MAIN LANDING GEAR DOES NOT COME DOWN AND LOCK. MAINTENANCE REMOVED AND REPLACED THE FREE FALL ASSISTER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996040500791 19960405 00791 NE 1996 4 5 C2XA96IA061 2 19960303 A 7310 3035728 FUEL FILTER EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE CLOGGED A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 09 34712 120111 IAH - FLT 2581 - DURING CRUISE, THE NR 2 ENGINE FUEL FILTER CLOG LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LOWER PRESSURE FUEL FILTER, AND THE AIRCRAFT WAS APPROVED FOR RE TURN TO SERVICE. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1996040500792 19960405 00792 NE 1996 4 5 C2XA96IA062 2 19960303 A 7310 5905587 FUEL FILTER EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE CLOGGED A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 09 34712 120111 IAH - FLT NR 2581 - DURING CRUISE, THE NR 2 ENGINE FUEL FILTER CLOG LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO THE FIE LD WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE HIGH PRESSURE FUEL FILTER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1996040500793 19960405 00793 CE 1996 4 5 C2XA96IA063 1 19960302 A 2731 1295260331 ELEVATOR TRIM BEECH 1900 1900D 1154162 CE EMPENNAGE FROZE UP A A C2XA O OTHER O OTHER CR CRUISE 1 SW 09 38537 UE158 IAH - FLT NR 2805 - DURING CRUISE, THE ELEVATOR TRIM FROZE AT ALTITUDE. MAINTENACNE CLEANED AND LUBED TRIM TAB HINGES A ND LUBED BOTH ELEVATOR TRIM TAB ACTUATORS, AND THE AIRCRFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1996040500794 19960405 00794 NE 1996 4 5 C2XA96IA064 2 19960308 A 7260 TOWER SHAFT AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE NR 2 ENGINE FAILED A A C2XA E ENGINE SHUTDOWN J R WARNING INDICATION PARTIAL RPM/PWR LOSS CR CRUISE 1 SW 09 14813 10813 100 120956 BTR - FLT 2674 - PILOT REPORTED THAT THE NR 2 ENGINE EXPERIENCED PARTIAL POWER LOSS, AND THAT THE OIL DROPPED TO ZERO PS I. THE CREW SHUT THE ENGINE DOWN AND THE AIRCRAFT LANDED AT BTR WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE TOWER SHAFT ON THE TURBO MACHINE AGB TO HAVE FAILED. THE NR 2 ENGINE WAS REMOVED AND REPLACED AND THE AIRCRAFT WAS APPROVED F OR RETURN TO SERVICE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1996040500795 19960405 00795 NM 1996 4 5 EISA96002 1 19960222 A 5320 PLATE BOEING 727 727223 1384074 NM CABIN BROKEN A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20191 STRAP PLATE IS BROKEN 2ND FROM LEFT UNDER BEAM STATION 344 AND BEAM STATION 360. FORWARD CABIN UNDER FLOOR. FABRICATE NEW PLATE PER SRM 51-10-1. INSTALLED PLATE AND FASTENERS PER SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1996040500796 19960405 00796 NM 1996 4 5 EISA96003 1 19960216 A 5312 BULKHEAD BOEING 727 727223 1384074 NM BS 1183 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20191 FOUND 2.5 INCH VERTICAL CRACK IN FACE OF BS 1183 BULKHEAD LBL 36, WL 224. FABRICATED AND INSTALLED FILLER SHIM AND DOUB LER PER SRM 53-10-9. (M) 2 L 7 3 4F A3WE 1996040500797 19960405 00797 NM 1996 4 5 EISA96004 1 19960216 A 5755 SKIN BOEING 727 727223 1384074 NM NR 11 SPOILER CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20191 SKIN CRACKED AT CENTER OUTBOARD HINGE CUTOUT NR 11 SPOILER. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 57-30-04. ( M) 2 L 7 3 4F A3WE 1996040500798 19960405 00798 NM 1996 4 5 EISA96005 1 19960216 A 5755 SKIN BOEING 727 727223 1384074 NM NR 12 SPOILER CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20191 SKIN CRACKED AT TWO CENTER HINGE CUT OUTS AT NR 12 SPOILER. FABRICATED DOUBLERS PER SRM 57-30-4. INSTALLED DOUBLERS PE R SRM 57-30-02. (M) 2 L 7 3 4F A3WE 1996040500799 19960405 00799 NM 1996 4 5 EISA96006 1 19960216 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 610 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20191 FORWARD BAG BIN STATION 610, INSIDE OF STRINGER 27R IS CORRODED ALONG WITH SUPPORT CLIP. REMOVED CORROSION PER SRM 51-1 0-02. FABRICATED AND INSTALLED NEW SUPPORT CLIP PER SRM 51-10-01. (M) 2 L 7 3 4F A3WE 1996040500800 19960405 00800 NM 1996 4 5 EISA96007 1 19960216 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 620 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20191 FORWARD BAG BIN BS 620, ABOVE STRINGER 27R, FLOOR SUPPORT, 'Z' ANGLE IS CORRODED ON FORWARD SIDE. REMOVED 'Z' ANGLE, FA BRICATED NEW PER SRM 51-10-01. INSTALLED ANGLE PER SRM 51-13-01. (M) 2 L 7 3 4F A3WE 1996040500801 19960405 00801 NM 1996 4 5 EISA96008 1 19960225 A 5720 DOUBLER BOEING 727 727223 1384074 NM WS 686.5 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20191 NR 1 TANK AT WS 686.50 REPAIR DOUBLER CRACKED THROUGH AT LOWER CHORD. REMOVED DOUBLER, CRACK ON RIB, PREVIOUSLY STOP DR ILLED. HFEC CONFIRMS CRACK CONTAINED BY ORIGINAL STOP HOLES. FABRICATED NEW DOUBLER AND INSTALLED PER SRM 57-10-5. (M ) 2 L 7 3 4F A3WE 1996040500802 19960405 00802 NM 1996 4 5 EISA96009 1 19960225 A 5720 DOUBLER BOEING 727 727223 1384074 NM WS 656.5 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20191 NR 1 TANK INTERNAL RIB AT WS 656.50 REPAIR DOUBLER CRACKED THROUGH AT LOWER CHORD. REMOVED DOUBLER CRACK ON RIB PREVIOU SLY STOP DRILLED. HFEC CONFIRMS CRACK CRACK CONTAINED BY ORIGINAL STOP HOLE, FABRICATED NEW DOUBLER AND INSTALLED PER S RM 51-30-02. 2 L 7 3 4F A3WE 1996040500803 19960405 00803 NM 1996 4 5 EISA96010 1 19960225 A 5720 BRACE BOEING 727 727223 1384074 NM FRONT SPAR CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20191 CENTER TANK INTERIOR CRACK AT FRONT SPAR SUPPORT BRACE LEFT OF BL '0'. REMOVED SUPPORT BRACE, FABRICATED NEW BRACE PER SRM 51-40-3. INSTALLED NEW BRACE PER SRM 51-30-02. (M) 2 L 7 3 4F A3WE 1996040500804 19960405 00804 NM 1996 4 5 EISA96011 1 19960225 A 5230 CHANNEL BOEING 727 727223 1384074 NM CARGO DOOR CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20191 NR 3 AFT CARGO DOOR LOWER CENTER SECTION STIFFENER CHANNEL HAS CORROSION. FABRICATED NEW CHANNEL AND INSTALLED PER SRM 51-30-02. (M) 2 L 7 3 4F A3WE 1996040500805 19960405 00805 NM 1996 4 5 EISA96012 1 19960225 A 5530 PANEL BOEING 727 727223 1384074 NM VERT STAB DAMAGED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20191 VERTICAL STABILIZER INTERIOR STRUCTURE PANEL UNDER ELEVATOR CONTROL RODS AREA HAS A PROTRUDING HOLE ON PANEL. REMOVED P ROTRUSION FROM HOLE FABRICATED DOUBLER AND INSTALLED PER SRM 51-30-03. (M) 2 L 7 3 4F A3WE 1996040500806 19960405 00806 NM 1996 4 5 EISA96013 1 19960222 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 410 BROKEN A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20191 E/E COMPARTMENT FLOOR SUPPORT ANGLE, RT SIDE OF RADIO RACK, APPROX STATION 410, BROKEN AT OUTBOARD END. FABRICATED NEW ANGLE PER SRM 51-40-03 INSTALLED ANGLE PER SRM 51-40-03. (M) 2 L 7 3 4F A3WE 1996040500807 19960405 00807 NM 1996 4 5 EISA96014 1 19960225 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 360-380 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20191 STRINGER 26R BETWEEN STATION 360 AND 380 HAS HEAVY CORROSION. CUT OUT DAMAGED SECTION, FABRICATED A NEW SECTION PER SRM 51-30-03 AND INSTALLED PER SRM 51-10-3 AND 51-30. (M) 2 L 7 3 4F A3WE 1996040500808 19960405 00808 NM 1996 4 5 EISA96015 1 19960225 A 5230 DOUBLER BOEING 727 727223 1384074 NM CARGO DOOR DAMAGED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20191 TEMPORARY REPAIR AT FWD CARGO DOOR EXTERIOR. REMOVED TEMP REPAIR, FABRICATED AND INSTALLED NEW DOUBLER PER SRM 51-30-02 . (M) 2 L 7 3 4F A3WE 1996040500809 19960405 00809 NM 1996 4 5 EISA96016 1 19960226 A 5754 SKIN BOEING 727 727223 1384074 NM NR 6 SLAT CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20191 NR SLAT LOWER SKIN CRACKED OUTBOARD END. CUT OUT CRACKED AREA. FABRICATED FILLER AND DOUBLER PER SRM 51-50-03. INSTAL LED FILLER AND DOUBLER PER SRM 51-40-02. (M) 2 L 7 3 4F A3WE 1996040500810 19960405 00810 NM 1996 4 5 EISA96017 1 19960226 A 5311 FRAME BOEING 727 727223 1384074 NM BS 312 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20191 ONE-THIRD CRACK FROM RIVET IN FRAME STATION 312 STRINGER 16R, BEHIND LAVATORY AREA. FABRICATED DOUBLER PER SRM 53-10-4, INSTALLED PER SRM 53-10-04. (M) 2 L 7 3 4F A3WE 1996040500811 19960405 00811 NM 1996 4 5 EISA96018 1 19960301 A 5311 FRAME BOEING 727 727223 1384074 NM BS 930 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20191 CRACK FOUND IN TWO AREAS IN FRAME STATION 930 WITH STRINGER 14 RIGHT SIDE. REPAIRED PER SB 53-130 DRAWING 65C 10084. ( M) 2 L 7 3 4F A3WE 1996040500812 19960405 00812 NM 1996 4 5 EISA96019 1 19960301 A 5311 FRAME BOEING 727 727223 1384074 NM BS 930 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20191 CRACK FOUND IN FRAME STATION 930 WITH STRINGER 14 LEFT SIDE. INSTALLED REPAIR PER SB 53-130. (M) 2 L 7 3 4F A3WE 1996040500813 19960405 00813 NM 1996 4 5 EISA96020 1 19960228 A 5320 STIFFENER BOEING 727 727223 1384074 NM BS 1166-1183 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20191 AFT CARGO COMPARTMENT, STATION 1166-1183, FLOOR BOARD AND 17 INCH STIFFENER ATTACH POINT CORRODED. FABRICATED AND INSTA LLED NEW STIFFENER PER SRM 51-40-02. (M) 2 L 7 3 4F A3WE 1996040500814 19960405 00814 NM 1996 4 5 EISA96021 1 19960227 A 5712 RIB BOEING 727 727223 1384074 NM WS 656 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20191 RIGHT WING INTERNAL RIB CRACKED AT WS 656 SECOND LOWER STRINGER AFT OF FRONT SPAR. STOP DRILLED CRACK, FABRICATED REPAI R PER SB 727-57-0127 AND INSTALLED REPAIR PER SRM 57-10-05. (M) 2 L 7 3 4F A3WE 1996040500815 19960405 00815 NM 1996 4 5 EISA96022 1 19960227 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 295.5 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20191 ANGLE AT TOP RIGHT FORWARD CORNER STATION 295.5 ON BOXED AREA OF E/E COMPARTMENT CORRODED. REMOVED AND FABRICATED NEW A NGLE PER SRM 51-30-02, INSTALLED ANGLE PER SRM 51-30-02. (M) 2 L 7 3 4F A3WE 1996040500816 19960405 00816 NM 1996 4 5 EISA96023 1 19960220 A 5712 RIB BOEING 727 727223 1384074 NM WS 738 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20191 LEFT WING INTERNAL RIB CRACKED AT WS 738 FIRST LOWER STRINGER FORWARD OF REAR SPAR. FABRICATED AND INSTALLED DOUBLER PE R SRM 57-10-5. (M) 2 L 7 3 4F A3WE 1996040500817 19960405 00817 NM 1996 4 5 EISA96024 1 19960228 A 5712 RIB BOEING 727 727223 1384074 NM WS 601 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20191 LEFT WING INTERNAL RIB CRACKED AT WS 601 SECOND LOWER STRINGER FWD OF REAR SPAR. FABRICATED AND INSTALLED DOUBLER PER S RM 57-10-05. (M) 2 L 7 3 4F A3WE 1996040500818 19960405 00818 NM 1996 4 5 EISA96025 1 19960228 A 5712 RIB BOEING 727 727223 1384074 NM WS 629 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20191 LEFT WING INTERNAL RIB CRACKED AT WS 629 SECOND LOWER STRINGER FWD OF REAR SPAR. FABRICATED AND INSTALLED DOUBLER PER S RM 57-10-05. (M) 2 L 7 3 4F A3WE 1996040500819 19960405 00819 NM 1996 4 5 EISA96027 1 19960301 A 3230 JACKSCREW BOEING 727 727223 1384074 NM NOSE GEAR DIRTY A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20191 NOSE LANDING GEAR MANUAL EXTENSION DRUM WILL NOT TURN. CLEANED JACKSCREW AND LUBED, OPS CHECK GOOD PER MM 32-34-11. (M ) 2 L 7 3 4F A3WE 1996040500820 19960405 00820 NM 1996 4 5 EISA96029 1 19960301 A 3230 DRUM BOEING 727 727223 1384074 NM RT MLG DIRTY A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20191 RIGHT MAIN LANDING GEAR MANUAL EXTENSION DRUM DOES NOT ROTATE. LUBED MECHANISM, OPS CHECK GOOD PER MM 32-34-0. (M) 2 L 7 3 4F A3WE 1996040500821 19960405 00821 NM 1996 4 5 EISA96030 1 19960216 A 2730 BOB WEIGHTS BOEING 727 727223 1384074 NM LT ELEV TAB CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20191 LEFT ELEVATOR TAB, BOB WEIGHTS CRACKED. INSTALLED REPAIRED WEIGHTS PER 27-30-11, TAB CHECKED FOR BALANCE PER SRM 51-80- 9. (M) 2 L 7 3 4F A3WE 1996040500822 19960405 00822 NM 1996 4 5 EISA96031 1 19960306 A 5720 CHORD BOEING 727 727223 1384074 NM WS 760 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20191 CRACK FOUND AT STATION 760 LBL 70.5 WING UPPER CHORD. INSTALLED PREVENTATIVE MODIFICATION KIT PER SB 727-57-0112 AND DR AWING 65C 33202. (M) 2 L 7 3 4F A3WE 1996040500823 19960405 00823 NM 1996 4 5 EISA96032 1 19960308 A 5320 STIFFENER BOEING 727 727223 1384074 NM FS 294.5 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20191 SECOND STIFFENER AFT OF STATION 294.5 IN NOSE GEAR WELL CORRODED. FABRICATED NEW PART PER SRM 51-20-1, HEAT TREATED PER BAC 5602 AND INSTALLED PER SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1996040500824 19960405 00824 NM 1996 4 5 EISA96033 1 19960307 A 5311 FRAME BOEING 727 727223 1384074 NM FS 760.95 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20191 RIGHT FUSELAGE FRAME, INBOARD FLANGE FS 760.85 CRACKED AT SECOND FASTENER HOLE BELOW CABIN FLOOR. INSTALLED REPAIR PER BOEING DRAWING 65C36279. (M) 2 L 7 3 4F A3WE 1996040500825 19960405 00825 NM 1996 4 5 EISA96034 1 19960304 A 5712 RIB BOEING 727 727223 1384074 NM WS 738 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20191 RIGHT WING INTERNAL RIB CRACKED WS 738 FIRST LOWER STRINGER AFT OF REAR SPAR. INSTALLED RIB KIT PER SB 727-57-0127. (M ) 2 L 7 3 4F A3WE 1996040500826 19960405 00826 NM 1996 4 5 EISA96035 1 19960215 A 5753 SPAR BOEING 727 727223 1384074 NM LT TE MID FLAP CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20191 CRACK INBOARD AFT UPPER FLANGE ON LEFT INBOARD MID FLAP FRON SPAR. INSTALLED REPAIR PER SB 727-57-160. (M) 2 L 7 3 4F A3WE 1996040500827 19960405 00827 NM 1996 4 5 EISA96036 1 19960301 A 5311 FRAME BOEING 727 727223 1384074 NM BS 930 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20191 CRACK FOUND IN FRAME STATION 930 WITH STRINGER 14 LEFT SIDE. INSTALLED REPAIR PER SB 53-130 AND DRAWING 65C10084. (M) 2 L 7 3 4F A3WE 1996040500828 19960405 00828 1996 4 5 GLBA96008 4 19960210 A 3425 6226197001 EHSI BEECH 1900 1900C 1154161 CE INSTR PANEL FAILED A GLBA O OTHER O OTHER CR CRUISE 1 CE 01 98GL 12144 1871 UC98 CIU - CREW REPORT EHSI SCREEN WENT BLANK ON TWO OCCASSIONS. MAINTENANCE REMOVED AND REPLACED EHSI SCREEN WHICH CURED PR OBLEM. EHSI HAS BEEN RETURNED TO VENDER FOR REPAIR. (M) 2 L 7 2 4T RT A24CE 1996040500829 19960405 00829 NE 1996 4 5 GLBA96028 2 19960210 A 7200 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE LEFT FAILED A GLBA E A ENGINE SHUTDOWN UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 01 451UE 13692 120108 115440 ALO - CREW REPORTED THAT CABIN/COCKPIT FILLED WITH SMOKE FROM LEFT BLEED FOLLOWING TAKEOFF. THEY PERFORMED AND AIR TURN BACK AND UNEVENTFUL LANDING. FOLLOWING SHUTDOWN LEFT ENGINE WOULD NOT RESTART. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE. ALL SYSTEMS OPS CHECK GOOD. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1996040500830 19960405 00830 CE 1996 4 5 GLBA96030 1 19960212 A 2751 AN57861 FLAP POS TRANS BEECH 1900 1900D 1154162 CE RT TE FLAPS FAILED A GLBA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 CE 01 100UX 2200 4753A UE100 FSD - CREW REPORTED THE FLAPS WOULD NOT RETRACT FOLLOWING TAKEOFF. CREW MADE AN AIR TURN BACK FOLLOWED BY AN UNEVENTFUL LANDING. MAINTENANCE REMOVED AND REPLACED FLAP POSITION INDICATOR TRANSMITTER. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4T RT A24CE 1996040500831 19960405 00831 CE 1996 4 5 GLBA96031 1 19960213 A 3260 UPLOCK SWITCH BEECH 1900 1900D 1154162 CE RT MLG LACK OF LUBE A GLBA O OTHER N FALSE WARNING LD LANDING 1 CE 01 100UX UE100 FSD - CRWE REPORTED AUTOFEATHER CB POPPED ON FINAL WHEN GEAR WAS SELECTED DOWN. MAINTENANCE LUBRICATED RIGHT GEAR UPLOC K SWITCH. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4T RT A24CE 1996040500832 19960405 00832 CE 1996 4 5 GLBA96032 1 19960216 A 7331 1303800101 FUEL FLOW IND BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ENGINE FAILED A GLBA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 01 101UX 4874 301224 UE101 SPW - CREW REPORTED LEFT FUEL FLOW INDICATOR INOP AND RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED LEFT FUEL FLOW INDICATOR. OPS CHECK WAS GOOD. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 1996040500833 19960405 00833 CE 1996 4 5 GLBA96033 1 19960218 A 3230 1143880009 POWER PACK BEECH 1900 1900C 1154161 CE LANDING GEAR MALFUNCTIONED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 152GL 9737 4051 MX515528 UC152 DLH - CREW REPORTED, THE LANDING GEAR POWER PACK CYCLED APPROXIMATELY EVERY 45 SECONDS FOLLOWING TAKEOFF. CREW ELECTED AN AIR TURN BACK AND MADE AN UNEVENTFUL LANDING. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR POWER PACK. SYSTEM OPS CHECK GOOD. 2 L 7 2 4T RT A24CE 1996040500834 19960405 00834 SO 1996 4 5 GLBA96034 1 19960221 A 3230 922AA2YA6P2722A PROX SENSOR EMB 120 EMB120RT SO LT MLG FAILED A GLBA O OTHER J WARNING INDICATION AP APPROACH 1 CE 01 451UE 120108 ORD - CREW REPORTED THAT LANDING GEAR WOULD NOT EXTEND NORMALLY, USED ELECTRIC OVERRIDE T EXTEND GEAR AND MADE AND UNEVE NTFUL LANDING. MAINTENANCE REMOVED AND REPLACED 'A' SYSTEM DOWNLOCK PROX SENSOR. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4T RT A31SO 1996040500835 19960405 00835 SO 1996 4 5 GLBA96037 1 19960219 A 5246 12007993612 HYD SERV DOOR EMB 120 EMB120RT SO RIGHT MISSING A GLBA K NONE D INFLIGHT SEPARATION IN INSP/MAINT 1 CE 01 267UE 120071 ORD - CREW REPORTED ON POST FLIGHT INSPECTION, THAT THE RIGHT HYDRAULIC ACCESS PANEL SERVICE DOOR WAS MISSING. MAINTENA NCE REPLACED MISSING PANEL. (M) 2 L 7 2 4T RT A31SO 1996040500836 19960405 00836 CE 1996 4 5 GLBA96039 1 19960226 A 3230 MS2417101 MOTOR RELAY BEECH 1900 1900C 1154161 CE LANDING GEAR FAILED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 45GL UC45 ESC - THE CREW REPORTED LANDIGN GEAR WOULD NOT EXTEND AND HAD TO MANUALLY EXTEND GEAR. AIRCRAFT MADE AN UNEVENTFUL LAND ING. MAINTENANCE REMOVED AND REPLACED LANDING GEAR MOTOR RELAY. OPS CHECK WAS GOOD. (M) 2 L 7 2 4T RT A24CE 1996040500837 19960405 00837 CE 1996 4 5 GLBA96041 1 19960229 A 3260 INTRANSIT LIGHT BEECH 1900 1900C 1154161 CE LANDING GEAR MALFUNCTIONED A GLBA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 01 141UE UC141 SPW - CREW REPORTED, THE GEAR INTRANSIT LIGHT DID NOT EXTINGUISH FOLLOWING TAKEOFF. THEY MADE AN AIR TUN BACK AND AN UN EVENTFUL LANDING. MAINTENANCE CYCLED GEAR WITH A/C ON JACKS, BUT WAS UNABLE TO DUPLICATE DISCREPANCY. (M) 2 L 7 2 4T RT A24CE 1996040500838 19960405 00838 SO 1996 4 5 GLBA96042 1 19960226 A 2741 922AAZYA6P2722A PROX SENSOR EMB 120 EMB120RT SO LT STAB TRIM FAILED A GLBA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 CE 01 128AM 120109 MYR - CREW REPORTED AURAL WARNING INDICATING UNSAFE TRIM SETTING ON TAKEOFF. ELECTED AN AIR TURN BACK AND MADE AN UNEVE NTFUL LANDING. MX REMOVED AND REPLACED LEFT TRIM PROX SENSOR. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4T RT A31SO 1996040500839 19960405 00839 NM 1996 4 5 MALA964903 1 19960308 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 826MA 330 FLT NR 3106 - DURING PREFLIGHT IN DTW, THE CREW NOTED THE COCKPIT OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REPLACED THE LIGHT ASSEMBLY. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2 H 7 2 4T RT A13NM 1996040500840 19960405 00840 NM 1996 4 5 MALA964904 1 19960308 A 3350 BRACKET DHAV DHC8 DHC8102 2809003 NM COCKPIT OUT OF POSITION A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 826MA 330 FLT NR 3123 - DURING PREFLIGHT IN DTW, THE CREW NOTED THE COCKPIT OVERHEAD EMERGENCY LIGHT WAS FLICKERING ON AND OFF. M AINTENANCE PERSONNEL REALIGNED A HOLDING BRACKET FOR THE EMERGENCY LIGHT, SECURING IT IN ITS SOCKET. ALL SYSTEMS OPERAT ED SATISFACTORILY. (M) 2 H 7 2 4T RT A13NM 1996040500841 19960405 00841 SW 1996 4 5 MALA964905 1 19960308 A 3260 1EN516 SWITCH SWRNGN SA227 SA227AC 8780603 SW NLG DIRTY A MALA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 15 421MA AC634 FLT NR 3369 - DURING APPROACH TO DTW, THE NOSE GEAR DOWN AND LOCKED LIGHT DID NOT ILLUMINATE UPON GEAR EXTENSION. THE C REW RECYCLED THE GEAR TWICE AND THE LIGHT ILLUMINATED. THE AIRCRAFT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. MAIN TENANCE PERSONNEL CLEANED THE NOSE GEAR POSITION SWITCHES. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2 L 7 2 4T RT A8SW 1996040500842 19960405 00842 SW 1996 4 5 MALA964906 1 19960301 A 5311 FRAME SWRNGN SA227 SA227AC 8780603 SW BS 144 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 158MC AC762B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE RIGHT FUSELAGE LOWER BELT FRAME RELIEF RADIUS AT FS 144 AND BL 8. STOP DRILLED THE CRACK AND INSTALLED A DOUBLER AND STIFFENER IAW SRM 53-90-20. (M) 2 L 7 2 4T RT A8SW 1996040500843 19960405 00843 SW 1996 4 5 MALA964907 1 19960301 A 5730 SKIN SWRNGN SA227 SA227AC 8780603 SW WING CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 158MC AC762B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE RIGHT LOWER INBAORD WING SKIN TO NACELL E ATTACH ANGLE. THEY STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW FAC ARP 54-20-9101. (M) 2 L 7 2 4T RT A8SW 1996040500844 19960405 00844 SW 1996 4 5 MALA964913 1 19960301 A 5522 SKIN SWRNGN SA227 SA227AC 8780603 SW LT ELEVATOR DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 158MC AC762B DURNG A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED DAMAGE TO THE LEFT ELEVATOR LOWER SKIN. THEY REPAIRED THE DAMAGE IAW FAC SRM 51-90-04. (M) 2 L 7 2 4T RT A8SW 1996040500847 19960405 00847 NM 1996 4 5 PCAA9600268 1 19960225 A 2611 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM BAGG COMPT MALFUNCTIONED A PCAA O OTHER N FALSE WARNING AP APPROACH 1 EA 13 817EX 191 SMOKE WARNING IN AFT BAGGAGE COMPARTMENT AFTER SEVERE TURBULANCE ON SHORT FINAL. INSPECTED AFT BAGGAGE COMPARTMENT SMOK E DETECTORS. PERFORMED TEST IAW MM CHAPTER 26-12-00 PAGE 201. FOUND OK, INSPECTED AIRCRAFT IAW SEVERE TURBULANCE INSPE CTION OF DEHAVILLAND MM CHAPTER 05. NO DISCREPANCIES FOUND. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1996040500848 19960405 00848 NE 1996 4 5 PCAA9600269 2 19960222 A 7200 ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 FAILED A PCAA E ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 EA 13 416AW 282 121153 NR 1 ENGINE OIL PRESSURE WENT TO ZERO IN FLIGHT. SHUT DOWN NR 1 ENGINE IN FLIGHT. REMOVED AND REPLACED NR 1 ENGINE. O PERATIONAL CHECK NORMAL. INVESTIGATION CONTINUES. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T 4 T RT A13NM E20NE 1996040500849 19960405 00849 NM 1996 4 5 PCAA9600271 1 19960228 A 5541 85540026101 RIB DHAV DHC8 DHC8102 2809003 NM RUDDER CRACKED A A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 826EX 3508 3950 SA0050 389 LOWER CLOSING RIB ON FORE RUDDER IS CRACKED AND DOUBLER PLATE HALF MISSING. REMOVED RUDDER ASSEMBLY. REPLACED RIB PART NR 85540026-101. REINSTALLED RUDDER ASSEMBLY. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1996040500850 19960405 00850 CE 1996 4 5 PLG22796E1 1 19960227 A 5246 DOOR BEECH 1900 1900 1154160 CE LT ENGINE NOT LATCHED A PLGA A UNSCHED LANDING O OTHER CR CRUISE 1 NE 05 55280 UC116 DURNG FLIGHT NR 4693, FROM LGA TO ROC, CREW NOTICED LEFT ENGINE COWLING OIL SERVICE DOOR OPEN. AIRCRAFT DIVERTED TO ALB AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED AND INSPECTED DOOR AND LATCH MECHANISM. NO DEFECTS WERE NOTED . AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1996040500851 19960405 00851 NE 1996 4 5 PLG22996E2 3 19960229 A 6111 660732886 BLADE SAAB SF340 SF340A 7850100 EU ROTOL R389 R3894123F25 NE NR 1 DISBONDED A PLGA K NONE O OTHER IN INSP/MAINT 1 NE 05 744BA 14030 3228 340A105 DRG676287 PROPELLER WAS REMOVED FORM SERVICE DUE TO MOVEMENT OF THE NR 1 BLADE OUTBOARD OF THE OUTER SLEEVE. TEAR DOWN INSPECTION FOUND A DISBONDING BETWEEN THE COMPOSITE MATERIAL AND OUTER SLEEVE. ALL FOUR BLADES WERE REPLACED WITH OVERHAUL CONDIT IONED BLADES AND THE PROPELLER RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 6 C P30NE 1996040500852 19960405 00852 EU 1996 4 5 PLG22996E3 1 19960229 A 3260 WARN LIGHT SAAB SF340 SF340A 7850100 EU LANDNIG GEAR ILLUMINATED A PLGA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NE 05 747BA 340A148 FLT NR 4471 - PSM-PWM - UPON GEAR RETRACTION THE CREW NOTED AN OAT HEAT FAULT LIGHT AND A CONFIGURATION WARNING LIGHT. T HE AIRCRAFT RETURNED TO PSM AND LANDED WITHOUT INCIDENT. UPON GEAR EXTENSION, THE FAULT LIGHTS EXTINGUISHED. MAINTENAN CE RESERVICED THE MLG STRUTS AND CYCLED THE GEAR WITH NO FAULTS FOUND. THE AIRCRAFT WAS TEST FLOWN SUCCESSFULLY AND RET URNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1996040500853 19960405 00853 1996 4 5 PLG3196E1 4 19960301 A 2210 7003180901 COMPUTER BEECH 1900 1900C 1154161 CE YAW DAMP SYSTEM FAILED A PLGA G A O2 MASK DEPLOYED UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NE 05 7203C 6014 86040239 UB28 FLT NR 4356 - ALB-BOS - AFTER TAKEOFF, FUMES AND SMOKE APPEARED IN THE CABIN AND COCKPIT. CREW DECLEARED AN EMERGENCY, DEPLOYED THE OXYGEN MASKS AND RETUREND TO ALB LANDING WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND TH E YAW DAMP CIRCUIT BREAKERS HAD POPPED. INVESTIGATION FOUND THE YAW DAMP COMPUTER HAD SHORTED INTERNALLY. THE YAW DAMP SYSTEM WAS DEFERRED AND THE AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1996040500854 19960405 00854 CE 1996 4 5 PLGG22196E1 1 19960221 A 5730 11412002823 SKIN BEECH 1900 1900C 1154161 CE LT WING LE DEBONDED A PLGA K NONE O OTHER IN INSP/MAINT 1 NE 05 15503 UC72 WHEN THE LEFT INBOARD LEADING EDGE WAS REMOVED FOR MAINTENANCE, IT WAS NOTED THAT THE MOST FORWARD PORTION OF THE LEADIN G EDGE WAS DEBONDED THE FULL LENGTH OF THE LEADING EDGE. THE LEADING EDGE WAS REPLACED WITH A SERVICEABLE UNIT, AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1996040500855 19960405 00855 EU 1996 4 5 RAIA960236 1 19960223 A 7712 94959411 TTL CONTROLLER BAG JETSTM JETSTM3201 1500217 EU RT ENGINE OUT OF ADJUST A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 436AM 10351 891 STL - FLT NR 7424 - RIGHT ENGINE BYPASSED ON TAKEOFF ROLL. MAINTENANCE CALIBRATED TORQUE/TEMP LIMIT CONTROLLER. (M) 2 L 7 2 4T RT A56EU 1996040500856 19960405 00856 EU 1996 4 5 RAIA960238 1 19960225 A 7722 8974764 EGT COMPENSATOR BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 424AM 5403 865 STL - FLT NR 7054 - RIGHT ENGINE DOES NOT MAKE TARGET TORQUE FOR TAKEOFF. MAINTENANCE REPLACED EGT COMPENSATOR, GROUND RUN GOOD. (M) 2 L 7 2 4T RT A56EU 1996040500857 19960405 00857 EU 1996 4 5 RAIA960239 1 19960224 A 2730 137103F7 HINGE PIN BOLT BAG JETSTM JETSTM3201 1500217 EU RT ELEVATOR WORN A A RAIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 CE 03 972JX 5461 972 FAT - 800 - AIRCRAFT CONTROLS ARE STIFF AND DIFFICULT TO CONTROL IN FLIGHT. ALSO IT IS DIFFICULT TO TRIM THE AIRCRAFT. MAINTENANCE REPLACED RIGHT ELEVATOR HINGE PIN BOLT, OPERATION CHECK GOOD. (M) 2 L 7 2 4T RT A56EU 1996040500858 19960405 00858 EU 1996 4 5 RAIA960240 1 19960225 A 7712 31024766 TQ SIGNAL COND BAG JETSTM JETSTM3201 1500217 EU LT ENGINE OUT OF ADJUST A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 428AM 5561 5561 877 STL - FLT NR 7448 - LEFT ENGINE DID NOT ACHIEVE TARGET TORQUE, ABORTED TAKEOFF. MAINTENANCE ADJUSTED LEFT TORQUE SIGNAL CONDITIONER PERFORMED GROUNDS RUNS OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A56EU 1996040500859 19960405 00859 EU 1996 4 5 RAIA960241 1 19960226 A 7712 31024766 TQ SIGNAL COND BAG JETSTM JETSTM3201 1500217 EU LT ENGINE OUT OF ADJUST A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 433AM 10644 10644 885 STL - FLT NR 7416 - LEFT ENGINE DID NOT MAKE TARGET TORQUE. MAINTENANCE ADJUSTED LEFT TORQUE SIGNAL CONDITIONER PERFORM ED GROUND RUNS OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A56EU 1996040500860 19960405 00860 EU 1996 4 5 RAIA960242 1 19960226 A 7712 31024766 TQ SIGNAL COND BAG JETSTM JETSTM3201 1500217 EU LT ENG OUT OF ADJUST A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 433AM 10644 561 885 STL - FLT NR 7434 - ON TAKEOFF LEFT ENGINE ACHIEVED 89 PERCENT TORQUE. MAINTENANCE ADJUSTED LEFT TORQUE SIGNAL CONDITIO NER PERFORMED GROUND RUNS OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A56EU 1996040500861 19960405 00861 EU 1996 4 5 SABA960006 1 19960308 A 3234 SELECTOR STBROS SD3 SD360 8100606 EU LANDING GEAR MALFUNCTIONED A SABA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 SO 33 742CC SH3742 FLT NR 5058 - PGV-CLT - ON APPROACH TO CLT WHEN THE CREW SELECTED GEAR DOWN THE NOSE GEAR FAILED TO INDICATE DOWN AND LO CKED. THE CAPTAIN DECLARED AN EMERGENCY AND PERFORMED A FLYBY THE GEAR WAS IN THE DOWN POSITION. THE AIRCRAFT MADE A S AFE LANDING IN CLT. MX POSITIONED JACK UNDER THE THE NOSE GEAR WAS FOUND TO BE LOCKED. THE GEAR WAS PINNED AND THE RETR ACTION SYSTEM WAS DEFERRED TO THE MSL PER MEL 32-3 UNDER CONTROL NR 0308-07C. THE A/C WAS TAKEN TO THE HANGER TO HAVE T HE MSL CLEARED. THE AIRCRAFT WAS JACKED AND THE SELECTOR SWITCH WAS FOUND TO BE INOPERATIVE. THE SELECTOR WAS REPLACED AND THE SYSTEM TESTED. ALL INDICATIONS WERE NORMAL. THE MSL WAS THEN CLEARED AND THE A/C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T A41EU 1996040500862 19960405 00862 EU 1996 4 5 SABA960007 1 19960309 A 7714 AG34 TACH-GENERATOR BAG JETSTM JETSTM3101 1500215 EU LT ENGINE FAILED A SABA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 33 158PC 763 FLT NR 5204 - CLT-PGV - A/C WAS APPROXIMATELY 30 MINUTES OUTBOUND WHEN THE LEFT ENGINE RPM INDICATOR FELL TO ZERO. ALL OTHER ENGINE INDICATIONS WERE NORMAL. THE CAPTAIN DECIDED TO RETURN TO CLT FOR REPAIRS TO BE MADE. MAINTENANCE FOUND T HE LEFT ENGINE TACH-GENERATOR TO BE DEFECTIVE. THE TACH-GENERATOR WAS REPLACED AND TESTED, AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A21EU 1996040500863 19960405 00863 EU 1996 4 5 SIMA960632 1 19960303 A 7712 E0442SE1203SN CONNECTOR AEROSP ATR72 ATR72212 EU NR 1 ENG DIRTY A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 270AT 270 HOU - FLT NR 3618 - AFTER TAKEOFF LEFT ENGINE TORQUE INDICATIONS DROPPED TO 60 PERCENT CREW ELECTED TO RETURN TO HOU. C LEANED ELECTRICAL CONNECTOR ON LEFT ENGINE T 1.8 SENSOR. GROUND PERFORMANCE RUNS WERE SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996040500864 19960405 00864 NE 1996 4 5 SIMA960642 2 19960304 A 7261 3047500 CASE DRAIN AEROSP ATR72 ATR72212 EU PWA PW120 PW127 NE NR 1 ENG LEAKING A SIMA E ENGINE SHUTDOWN B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 SW 21 447AM 127144 447 127144 ORD - FLT NR 4031 - AFTER BOTH ENGINES WERE RUNNING THE ELECTRICAL SMOKE INDICATOR ILLUMINATED. THE CREW SHUT DOWN THE ENGINES AND PASSENGERS DEPLANED NORMALLY. MAINTENANCE FOUND A LEAK AT INNER COMPRESSOR CASE DRAIN. RAI'D NR 1 ENGINE D UE TO INTERNAL LEAK. PERFORMED GROUND PERFORMANCE RUN. OPS CHECKED GOOD AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1996040500865 19960405 00865 WP 1996 4 5 SRAA29604 1 19960227 A 3310 BAL70M0DB BALLAST DOUG DC8 DC873F 302199F WP COCKPIT FAILED A SRAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 23 873SJ 46091 DURING TAXI OUT FOR FLIGHT CWC 172 FROM MIA, FIRST OFFICERS OVERHEAD FLUORESCENT LAMP EMITS SMOKE, TAXIED AIRCRAFT BACK TO BLOCK. FOUND BALLAST DEFECTIVE, REMOVED BALLAST AND DEFERRED FLIGHT OFFICERS OVERHEAD FLUORESCENT LAMP. (M) 2 L 7 4 4F RT 4A25 1996040500866 19960405 00866 NM 1996 4 5 TAOA029601 1 19960206 A 3350 1000677 LIGHT GRIMES BOEING 727 727254 138408L NM CABIN INOPERABLE A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 914TS 1134 20251 FORWARD ENTRY EMERGENCY EXIT LIGHT INOP. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECK OK. (M) 2 L 7 3 4F A3WE 1996040500867 19960405 00867 NM 1996 4 5 TAOA029602 1 19960208 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 923TS 9228 20441 EMERGENCY EXIT SIGN AT ROW 16 INOP. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. (M) 2 L 7 3 4F A3WE 1996040500868 19960405 00868 NM 1996 4 5 TAOA029608 1 19960214 A 2751 1812993M POS IND BENDIX BOEING 727 727227 1384078 NM TE FLAPS MALFUNCTIONED A TAOA O OTHER N FALSE WARNING AP APPROACH 1 EA 15 925TS 1628ANV 21244 DURING APPROACH, OUTBOARD TRAILING EDGE FLAPS LOCKED AT 15 DEGREE PERFORMED ABNORMAL PROCEDURES AND LANDED. AT TOUCHDOW N OUTBOARD TRAILING EDGE FLAPS INDICATED 30 DEGREE. VISUALLY INSPECTED OUTBOARD AND INBOARD FLAPS, FOUND NORMAL. REPLA CED FLAP POSITION INDICATOR, SYSTEM OPS CHECKS OK IAW 27-21-0. (M) 2 L 7 3 4F A3WE 1996040500869 19960405 00869 NM 1996 4 5 TAOA029611 1 19960215 A 2750 BACP30F4 PULLEY BOEING 727 727227 1384078 NM RT TE FLAP FROZEN BRG A A TAOA L ABORTED APPROACH F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 EA 15 925TS 21244 ON APPROACH TO LANDING, OUTBOARD FLAPS STOPPED AT 15 DEGREES. COMPLIED WITH AOM ABONORMAL PROCEDURES, ON SECOND APPROAC H ALL FLAPS WENT TO 30 DEGREE. PROCEEDED TO MAKE NORMAL APPROACH AND LANDING. UNABLE TO DUPLICATE CONDITION. FOUND ON E RIGHT OUTBOARD FLAP POSITION CABLE PULLEY FROZEN AT BEARING. REPLACED PULLEY, OPERATED FLAPS NUMEROUS TIMES, FLAP POS ITION INDICATION AND OPERATION NORMAL. (M) 2 L 7 3 4F A3WE 1996040500870 19960405 00870 NM 1996 4 5 TAOA029615 1 19960223 A 2120 AIR DIST BOEING 727 727254 138408L NM CABIN SMOKE A TAOA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 15 913TS 20250 ON CLIMB-OUT A LOUD POP WAS HEARD FOLLOWED BY THE FLIGHT ATTENDANT REPORTING SMOKE IN THE AFT CABIN. THIS WAS IMMEDIATE LY FOLLOWED BY SMOKE IN THE COCKPIT. AN EMERGENCY DESCENT AND PRECAUTIONARY LANDING WERE MADE. TEH SMOKE DISSIPATED AF TER APPROXIMATELY 5 MINUTES. NO FIRE OR OVERHEATED CONDITION WAS OBSERVED ON ANY GAUGES. CHECKED ALL ENGINE INLETS AND EXHAUST, FOUND OK. OPENED ENGINE COWLS, ALL DUCTS FOUND OK. CHECKED ACM'S AND WATER SEPARATE BAGS, OK. CHECKED OPERA TION OF PACKS, OK. RAN ALL ENGINES, NO SMOKE NOTED AT ANYTIME. INSPECTED AFT AIRSTAIR AND A/C DISTRIBUTION BAY AREA, N O LEAKS NOTED. (M) 2 L 7 3 4F A3WE 1996040500871 19960405 00871 NM 1996 4 5 TAOA039602 1 19960305 A 5753 6521631274 FOREFLAP BOEING 727 727225 1384077 NM RT TE FLAP FAILED A TAOA O OTHER D INFLIGHT SEPARATION AP APPROACH 1 EA 15 918TS 2078 BN133 20445 SECTION OF RIGHT TRAILING EDGE FOREFLAP FOUND MISSING DURING POST FLIGHT. REPLACED RIGHT OUTBOARD FOREFLAP, OPS CHECKED OK PER MM 27-51-11. (M) 2 L 7 3 4F A3WE 1996040500872 19960405 00872 NM 1996 4 5 TAOA039603 1 19960308 A 3350 1000677 LIGHT BOEING 727 727254 138408L NM CABIN INOPERATIVE A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 913TS 20250 EMERGENCY EXIT LIGHT INOP AT FORWARD ENTRY DOOR AND RIGHT AFT SERVICE DOOR. REPLACED BOTH LIGHT ASSEMBLIES. OPERATIONA L CHECK OK. (M) 2 L 7 3 4F A3WE 1996040500873 19960405 00873 NM 1996 4 5 TAOA039604 1 19960310 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 918TS 20445 FORWARD ENTRY AISLE EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK AND BATTERY CHARGER OPERATIONAL CHECK OK. (M) 2 L 7 3 4F A3WE 1996040500874 19960405 00874 NM 1996 4 5 TAOA039605 1 19960310 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 918TS 20445 OVERWING EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK AND BATTERY CHARGER. OPERATIONAL CHECK OK. (M) 2 L 7 3 4F A3WE 1996040500875 19960405 00875 NM 1996 4 5 TAOA039606 1 19960310 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 918TS 9455 20445 RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. (M) 2 L 7 3 4F A3WE 1996040500876 19960405 00876 NM 1996 4 5 TAOA039609 1 19960310 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 918TS 10490 20445 LEFT OVERWING EMERGENCY EXIT SIGN INOP. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. (M) 2 L 7 3 4F A3WE 1996040500877 19960405 00877 NM 1996 4 5 USAA960212 1 19960207 A 5320 65C105922 ANGLE BOEING 737 7372B7 1384560 NM BS 967-947 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 35486 22886 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 20 INCH BY 1 INCH FLOOR SUPPORT ANGLE CORROSION STATION 967 TO 947 RBL 6 . REPAIRED PER SRM 51-10-1. REPLACED WITH IDENTICAL PART NR 65C10592-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996040500878 19960405 00878 NM 1996 4 5 USAA960267 1 19960220 A 5753 SKIN BOEING 767 767201 1385125 NM TE FLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647US 35510 23899 CLT - INSPECTION VISUALLY FOUND TWO DELAMINATION DENTS MEASURING 2 INCH BY 1 INCH BY .050 INCH AND 1 INCH BY .5 INCH .03 0 INCH LOCATED AT TRAILING EDGE WEDGE ASSEMBLY, OUTBOARD TRAILING EDGE FLAP STATION 260, 6 INCHES FORWARD OF TRAILING ED GE (LOWER SKIN). REMOVED DAMAGED SKIN AND INSTALLED COMPOSITE REPAIR PLIES AS PER SRM 51-70-17. (M) 2 L 7 2 4F RT A1NM 1996040500879 19960405 00879 NM 1996 4 5 USAA960268 1 19960216 A 5320 FITTINGS BOEING 737 737401 1384701 NM BS 521 GOUGE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 19822 23991 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND GOUGES, SEAT TRACK SUPPORT CHANNEL FITTING STATION 521, RBL 25, WL 207. REPAIRED PER EA 40888 STEP 3. (M) 2 L 7 2 4F RT A16WE 1996040500880 19960405 00880 NM 1996 4 5 USAA960269 1 19960216 A 5330 SKIN BOEING 737 737401 1384701 NM BS 800 GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 19822 23991 INT - DURNG Q-6 CHECK VISUAL INSPECTION, FOUND 4 INCH AND .75 INCH GOUGE IN SKIN AT BS 800 BETWEEN STRINGER 22R AND STRI NGER 24R. INSTALLED DOUBLER PER SRM 53-00-01. (M) 2 L 7 2 4F RT A16WE 1996040500881 19960405 00881 NM 1996 4 5 USAA960270 1 19960216 A 5315 FLOOR BEAM BOEING 737 737401 1384701 NM BS 328 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 19822 23991 INT - DURING Q-6 CHECK VISUAL INSPECTION, FUOND 1 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES TOP OF FLOOR BEAM BS 3 28 LBL 9 TO RBL 21. CUT OUT SECTION OF UPPER CHORD AND REPAIRED EPR SRM 53-10-51 FIG 205. CORROSION TASK NR C53-107-02 , CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996040500882 19960405 00882 NM 1996 4 5 USAA960271 1 19960216 A 5315 FLOOR BEAM BOEING 737 737401 1384701 NM BS 344 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 19822 23991 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES TOP OF FLOOR BEAM BS 3 44 LBL 50 TO RBL 8. CUT OUT SECTION OF UPPER CHORD AND SPLICED IN NEW SECTION OF T-CAP PER TR 53-10-03. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996040500883 19960405 00883 NM 1996 4 5 USAA960272 1 19960216 A 5315 FLOOR BEAM BOEING 737 737401 1384701 NM BS 986.5 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 19822 23991 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH OF CORROSION STATION 986.5 FLOOR BEAM UPPER FLANGE AT S CREW HOLES LBL 52 TO RBL 52. REMOVED UPPER CHORD AND SPLICED IN NEW CHORD PER EA 40883. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996040500884 19960405 00884 WP 1996 4 5 USAA960291 1 19960314 A 5320 MEMBRANE DOUG DC9 DC982 3022082 WP BS 1211 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 821US 36016 49138 PIT - DUIRNG Q6-C3 INSPECTION, FOUND LEVEL 1 CORROSION JUST AFT OF STATIN 1211 ABOVE LONGERON 26R IN WEB MEMBRANE. CORR OSION TASK NR C57-5330 PREVIOUSLY REWORKED. CUT OUT CORRODED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 3 AND SRM 53-14-3 FIG 3. (M) 2 L 7 2 4F A6WE 1996040500885 19960405 00885 NM 1996 4 5 USAA960295 1 19960306 A 5313 STRINGER BOEING 737 737296 1384486 NM BS 986-1006 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 238US 39902 22398 ROA - DURNG CX-4 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 10 INCH CORROSION, STRINGER 27 LEFT BETWEEN BS 986 TO 1006. IN STALLED STRINGER SPLICE, REPAIRED PER SRM 53-10-3. (M) 2 L 7 2 4F RT A16WE 1996040500886 19960405 00886 NM 1996 4 5 USAA960307 1 19960311 A 5330 SKIN BOEING 737 737201 1384454 NM BS 807 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 254AU 22796 ROA - DURING CX-6 CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK SKIN, STRINGER 19 LEFT BS 807. INSTALLED DOUBLER, REPAIRE D EPR SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1996040500887 19960405 00887 NM 1996 4 5 USAABB96004 1 19960214 A 3350 20131 BATTERY PACKS BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 609AU 22205 PIT - FL 1767 - PRIOR TO DEPARTURE, EMERGENCY EXIT LIGHTS AT ROWS 22, 23 AND 25 AND R-3 AND R-4 DOORS WERE INOPERATIVE. MAINTENANCE REPLACED THE APPROPRIATE BATTERY PACKS. (M) 2 L 7 2 4F RT A2NM 1996040500888 19960405 00888 NM 1996 4 5 USAABB96005 1 19960221 A 3350 873100151REV8 LIGHT BOEING 757 7572B7 1384964 NM CABIN FAILED A USAA K NONE L NO TEST NR NOT REPORTED 1 EA 19 632AU 27810 FLT NR 88 - PIT - EMERGENCY TRACK LIGHT AT SEAT 33D INO. ALL OTHER LIGHTS NORMAL. REPLACED EMERGENCY LGIHT AT 33D. OP ERATES NORMALLY. (M) 2 L 7 2 4F RT A2NM 1996040500889 19960405 00889 WP 1996 4 5 USAAD96029 1 19960305 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 928VJ 48131 CMH - FLOOR PATH EMERGENCY LIGHTING WAS INOPERATIVE. MAINTENANCE REPAIRED WIRING AT THE FORWARD POWER SUPPLY, SECTIONS 1 AND 2 OF THE FLOOR PATH LIGHTING AND THE FORWARD ENTRY DOOR. (M) 2 L 7 2 4F A6WE 1996040500890 19960405 00890 EU 1996 4 5 USAAF96023A 1 19960222 A 3240 5009638 HEAT SHIELD D07354415M FOKKER F28 F28MK0100 4990807 EU LT MLG BRAKE BENT A A USAA O OTHER D J INFLIGHT SEPARATION WARNING INDICATION TO TAKEOFF 1 EA 19 869US MAR890245 11314 FLT NR 1543 - CLT - ON TAKEOFF FROM RDU RWY 23R, CAPTAIN HAD GEAR FAULT MESSAGE, RDU TOWER TOLD HIM IT LOOKED LIKE SOMET HING FELL OFF THE AIRCRAFT. WHILE THE FLIGHT HELD IN THE AIR OVER RDU, THEY FOUND THE NR 2 MAIN WHEEL ASSEMBLY. FLIGHT PROCEEDED TO CLT. WHEEL DEPARTED AIRCRAFT DUE TO CIRCUMFERENTIAL WHEEL FAILURE DUE TO A BENT BRAKE HEAT SHIELD. MAINT ENANCE REPLACED THE LEFT MAIN LANDING GEAR. (M) 2 L 7 2 4F RT 1996040500891 19960405 00891 NM 1996 4 5 USAASB96044 1 19960308 A 2130 7110033 CONNECTORS BOEING 737 737201 1384454 NM OUTFLOW VLV DISCONNECTED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 254AU 22796 FLT NR 770 - ROA - AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. OUTFLOW VALVE INDICATED CLOSED IN AUTO, STANDBY, AND MA NUAL. RETURNED TO FIELD. MAINTENANCE FOUND AC AND DC CANNON PLUGS DISCONNECTED FROM THE OUTFLOW VALVE. SECURED PLUGS, OPS CHECK NORMAL. 2 L 7 2 4F A16WE 1996040500892 19960405 00892 EU 1996 4 5 VTZA96072 1 19960209 A 5270 91SE16 SWITCH BAG JETSTM JETSTM3201 1500217 EU BAGGAGE DOOR DIRTY A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 481UE 895 ISP-IAD - DURING CLIMB-OUT, RETURNED TO ISP DUE TO THE POD DOOR LIGHT COMING ON IN FLIGHT. AIRCRAFT LANDED AT ISP WITH NO FURTHER INCIDENTS. MAINTENANCE CLEANED POD DOOR WARNING MICROSWITCHES. AIRCRAFT WAS RELEASED AND APPROVED FOR RETUR N TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996040500893 19960405 00893 WP 1996 4 5 VTZA96097 2 19960227 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RIGHT BIRD STRIKE A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK C F.O.D. TO TAKEOFF 1 EA 27 471UE 821 P66020 FLT NR 6368 - CRW-IAD - ABORTED THE TAKEOFF DUE TO THE RIGHT ENGINE INGESTING A BIRD. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE PERFORMED A BIRD STRIKE INSPECTION AND DETERMINED THAT THE FIRST STAGE IMPELLER RECEIVE D TOO MUCH DAMAGE FOR THE AIRCRAFT TO BE FERRIED. AIRCRAFT REMAINS IN CRW FOR AN ENGINE CHANGE. MAINTENANCE CHANGED RI GHT ENGINE AT CRW, OPS CHECKS OK. AIRCRFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996040500895 19960405 00895 1996 4 5 VTZA96102 4 19960306 A 6122 PROP GOVERNOR JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE OUT OF ADJUST A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 302UE 41013 FLT NR 6578 - IAD-PWM - DURING CRUISE, MADE A UNSCHEDULED LANDING DUE TO RIGHT ENGINE RPM WOULD NOT GO DOWN BELOW 97 PER CENT IN CRUISE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED PROP GOVERNOR LOW RPM. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996040500896 19960405 00896 1996 4 5 VTZA96103 4 19960306 A 3417 7000700966 AIR DATA COMP JETAIR JETSTM JETSTM4101 1500501 EU LEFT FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 323UE 41059 FLT NR 6532 - IAD-ORF - DURING CLIMB, AIRCRAFT RETURNED TO IAD DUE TO LEFT AIR DATA COMPUTER FAILED ON ROTATION. AIRCRA FT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED AIR DATA COMPUTER, OPS CHECK OK. AIRCRAFT WAS RELE ASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996040500897 19960405 00897 EU 1996 4 5 VTZA96104 1 19960301 A 3350 14807020 CONNECTOR BAG JETSTM JETSTM3201 1500217 EU CABIN FAILED A VTZA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 EA 27 487UE 906 FLT NR 6456 - IAD-ABE - DURING PREFLIGHT INSPECTION, CREW DISCOVERED THAT RIGHT FORWARD CABIN LIGHT WAS EMITTING SMOKE. MAINTENANCE INSPECTED AND REPLACED THE CONNECTOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996040500898 19960405 00898 WP 1996 4 5 VTZA96105 2 19960308 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE3311 01514 WP LEFT OVERTORQUE A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 27 308UE 41023 FLT NR 6355 - IAD-TYS - DURING TAKEOFF, ABORTED THE TAKEOFF DUE TO THE LEFT ENGINE TORQUE WENT TO 109 PERCENT ON THE TAK EOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENT. MAINTENANCE PERFORMED INSPECTIONS AND ENGINE RUNS, BUT COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 3 T RT A41NM E3WE 1996040500899 19960405 00899 WP 1996 4 5 VTZA96108 2 19960309 A 7321 89737527 FUEL CONTL UNIT BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT ENGINE FAILED A A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 27 490UE 909 P66379 FLT NR 6281 - HPE-IAD - ABORTED TAKEOFF, DUE TO THE LEFT ENGINE NOT MAKING TAKEOFF TORQUE. AIRCRAFT RETURNED TO GATE WI TH NO FURTHER INCIDETNS. MAINTENANCE REPLACED THE LEFT ENGINE FUEL CONTROL UNIT. AIRCRAFT WAS RELEASED AND APPROVED FO R RETURN TO SERVICE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996040500900 19960405 00900 1996 4 5 VTZA96109 4 19960309 A 3414 39948B2236 AIRSPEED IND BAG JETSTM JETSTM3201 1500217 EU LT COCKPIT FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 27 477UE 890 FLT NR 6181 - IAD-BWI - ABORTED TAKEOFF, DUE TO THE CAPTAINS AIRSPEED INDICATOR FAILING ON THE TAKEOFF ROLL. AIRCRAFT R ETURNED TO GATE WITH NO FURTHR INCIDENTS. MAINTENANCE REPLACED THE LEFT AIRSPEED INDICATOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996040500901 19960405 00901 EU 1996 4 5 VTZA96110 1 19960308 A 5270 91SE16 SWITCH BAG JETSTM JETSTM3201 1500217 EU CABIN DOOR DIRTY A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 479UE 893 FLT NR 6565 - IAD-GSO - DURING CLIMB-OUT, RETURNED TO IAD DUE TO THE MAIN DOOR WARNING LIGHT ILLUMINATING IN FLIGHT. AI RCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTEANCE CLEANED THE DOOR WARNING MICROSWITCHES. AIRCRAFT WAS RELE ASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996040500902 19960405 00902 EU 1996 4 5 VTZA96111 1 19960307 A 2750 13730164K SWITCH BAG JETSTM JETSTM3201 1500217 EU FLAP SELECTOR LOOSE WIRE A VTZA O OTHER F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 EA 27 491UE 911 FLT NR 6379 - IAD-SYR - LANDED WITH ZERO FLAPS DUE TO FLAP FAILURE. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. M AINTENANCE RESECURED LOOSE WIRE AT FLAP SELECTOR, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVIC E. (M) 2 L 7 2 4T RT A56EU 1996040500903 19960405 00903 WP 1996 4 5 VTZA96112 2 19960307 A 7321 31059005 FUEL CONTL UNIT JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE3311 01514 WP LT ENG OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 319UE 41042 FLT NR 6416 - IAD-CHS - ABORTED TAKEOFF DUE TO LEFT ENGINE ONLY MADE 98 PERCENT TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED MAX FUEL FLOW. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 3 T RT A41NM E3WE 1996040500904 19960405 00904 1996 4 5 VTZA96113 4 19960307 A 3425 4020531574 ADI BAG JETSTM JETSTM3201 1500217 EU LEFT FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 495UE 818 FLT NR 6405 - IAD-HPE - DURING CLIMB-OUT RETURNED TO IAD DUE TO CAPTAINS ADI FLAGGED AND HORIZON TUMBLED IN FLIGHT. AIR CRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED NR ADI, OPS CHECK OK. AIRCRAFT WAS RELEASED AND AP PROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996040500905 19960405 00905 WP 1996 4 5 9607439606 1 19960218 A 5311 FRAME DOUG DC9 DC932 3022066 WP FS 718 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 606NW 47225 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A ONE INCH CRACK IN THE FS 718 RIB AT LONGERON 20R. REPAIRED RIB PE R EA 99-103161. 2 L 7 2 4F A6WE 1996040500906 19960405 00906 NM 1996 4 5 9607446601 1 19960229 A 5712 RIB BOEING 747 747151 1384891 NM WS 1453 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 601US 19778 DURING P-CHECK, FOUND A CRACK IN THE LEFT WING LEADING EDGE RIB AT FSSI 1453. REPAIRED RIB (P/N 65B07848-5) PER EA 66-9 9441. 2 L 7 4 4F A20WE 1996040500907 19960405 00907 WP 1996 4 5 9607459936 1 19960303 A 5713 LONGERON DOUG DC9 DC931 3022065 WP WS 58 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 1799U 47370 DURING SPECIAL MAINTENANCE VISIT, FOUND TWO CRACKS IN THE CENTER WING, STR 13, AT WS 58R. REPAIRED STRINGER PER EA 99-1 06792. 2 L 7 2 4F A6WE 1996040500908 19960405 00908 NM 1996 4 5 9607465504 1 19960321 A 5313 LONGERON BOEING 757 757251 1384970 NM FS 1520 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 504US 23193 DURING T-CHECK, FOUND CORROSION ON THE BS 1520 AFT CARGO FLOOR STRINGERS AT RBL 3 AND RBL 7. REPAIRED STRINGERS (P/N 14 6N5444) PER EA 55-102072. 2 L 7 2 4F RT A2NM 1996040500909 19960405 00909 WP 1996 4 5 9607479310 1 19960322 A 5220 DOOR PAN DOUG DC9 DC982 3022082 WP EMER EXIT CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 313RC 48091 DURING P-CHECK, FOUND A CRACK IN THE AFT LEFT EMERGENCY OVERWING EXIT DOOR PAN AT THE NR 6 STOP FITTING. REPAIRED PAN ( P/N 5910159-31) PER EA 93-104204. 2 L 7 2 4F A6WE 1996040500910 19960405 00910 WP 1996 4 5 9607489310 1 19960322 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FS 807 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 313RC 48091 DURING P-CHECK, FOUND CORROSION IN LONGERON 28L AT FS 807. REPAIRED LONGERON (P/N 5936051-501) PER EA 93-104205. 2 L 7 2 4F A6WE 1996040500911 19960405 00911 NM 1996 4 5 9607495504 1 19960325 A 5320 CHORD BOEING 757 757251 1384970 NM FS 1380-1440 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 504US 23193 DURING T-CHECK, FOUND CORROSION ON THE AFT CARGO DOOR LOWER SILL INNER CHORD; BS 1380 - 1440. REPAIRED CHORD (P/N 146N8 522-52) PER EA 55-99517. 2 L 7 2 4F RT A2NM 1996040500912 19960405 00912 NM 1996 4 5 9607506614 1 19960326 A 5754 SKIN BOEING 747 747251B 1384892 NM NR 11 LE FLAP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 614US 20359 DURING LINE CHECK (AMS), FOUND A CRACK IN THE NR 11 KRUEGER FLAP INNER SKIN. REPAIRED FLAP PER EA 66-99604. 2 L 7 4 4F A20WE 1996040500913 19960405 00913 WP 1996 4 5 9607519954 1 19960331 A 5313 LONGERON DOUG DC9 DC931 3022065 WP FS 585 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 921RW 47164 DURING H-CHECK, FOUND A CRACK IN THE LONGERON 25R END FITTING AT FS 585. REPLACED FITTING PER SRM 51-30-2. 2 L 7 2 4F A6WE 1996040500914 19960405 00914 NM 1996 4 5 9607566717 1 19960329 A 5320 INTERCOSTAL BOEING 747 747251F 1384898 NM FS 427 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 617US 21121 DURING P-CHECK, FOUND CORROSION ON THE INTERCOSTAL LOWER CHORD AT BS 427, STR 44L. REPAIRED CHORD (P/N 65B11046-14) PER EA 67-99608. 2 L 7 4 4F A20WE 1996040500915 19960405 00915 EU 1996 4 5 9607573226 1 19960403 A 3260 UPLOCK IND AIRBUS 320 A320211 3930320 EU LANDING GEAR MALFUNCTIONED A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 326US 282 DURING CLIMBOUT, RECEIVED LANDING GEAR NOT UPLOCKED MESSAGE. CYCLED LANDING GEAR HANDLE AND ALL INDICATIONS NORMAL. AI RCRAFT CONTINUED TO ORIGINAL DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTION REVEALED NO DISCREPANCY. 2 L 7 2 4F RT A28NM 1996040500916 19960405 00916 WP 1996 4 5 9607589994 1 19960403 A 3220 CABLE DOUG DC9 DC931 3022065 WP NLG DOOR STOP BROKEN A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 8979E 47328 AFTER TAKEOFF, A LOUD BANG WAS HEARD FROM NOSE LANDING GEAR WHEELWELL AREA. FLIGHT RETURNED TO EWR AND LANDED WITHOUT I NCIDENT. MAINTENANCE FOUND THE LEFT NOSE GEAR DOOR STOP CABLE BROKEN. DEFERRED CABLE PER MEL 32-7. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996040500917 19960405 00917 EU 1996 4 5 9607593249 1 19960401 A 3230 818101 PROX SENSOR AIRBUS 320 A320211 3930320 EU NLG MALFUNCTIONED A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 349NW 417 DURING CLIMB-OUT, THE LANDING GEAR DID NOT RETRACT. RECEIVED LANDING GEAR SHOCK ABSORBER FAULT. MESSAGE DISAPPEARED APP ROXIMATELY 30 SECONDS LATER AND THE LANDING GEAR OPERATED NORMALLY. AIRCRAFT CONTINUED TO ORIGINAL DESTINATION AND LAND ED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSE LANDING GEAR PROXIMITY SENSOR 24GA. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996040500918 19960405 00918 NM 1996 4 5 9607602286 1 19960403 A 2782 1U1110 ACTUATOR BOEING 727 727251 138408H NM NR 2 LE FLAP FAILED A A NWAA A J UNSCHED LANDING DUMP FUEL F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 01 286US 32946 5763 21325 DURING CLIMB, NR 2 LEADING EDGE FLAP INDICATED DOWN WITH FLAP HANDLE IN THE UP POSITION. AIRCRAFT HAD A 5 DEGREE ROLL A TTITUDE AT 2 DEGREES OF FLAPS. DUMPED FUEL, RETURNED TO MSP, AND LANDED WITHOUT INCIDENT. REPLACED THE NR 2 LEADING ED GE FLAP ACTUATOR. ACCOMPLISHED OPERATIONAL CHECK OF LEADING EDGE FLAPS AND SLAT SYSTEM. CHECKED OK. 2 L 7 3 4F A3WE 1996040500919 19960405 00919 NM 1996 4 5 96UAL900234 1 19960403 A 4940 38880585 EXCITER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU MALFUNCTIONED A UALA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 WP 29 516UA 24860 61493 LEFT IDG DISCONNECTED AND APU WOULD NOT START IN-FLIGHT AFTER 3 ATTEMPTS. FLIGHT DIVERTED TO SLC. SUPPLEMENTAL DATA UP DATE: REPLACED IGNITION EXCITER, IGNITION PLUG, AND LEAD. OPERATION CHECKS NORMAL. IGNITION EXCITERS ARE BEING UPGRAD ED PER OEM 49-41-09, TO IMPROVE HIGH ALTITUDE STARTS. 2 L 7 2 4F 4 F RT A2NM E17NE 1996040500920 19960405 00920 WP 1996 4 5 96UAL900235 1 19960403 A 2130 ABM7475501 CHECK VALVE DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 1 COND AIR FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 1838U 46632 RETURNED TO HNL BECAUSE THE AIRPLANE WOULD NOT PRESSURIZE. REPLACED BLOWN HOSE CONNECTOR AND REPAIRED DUCT DOWNSTREAM O F NR 1 PACK. AIRCRAFT RETURNED AGAIN DUE TO THE SAME HOSE FAILURE. A BEARING IN THE CONDITIONED AIR CHECK VALVE FAILED CAUSING THE CHECK VALVE TO NOT OPERATE PROPERLY. THEREFORE,THE CABIN DEPRESSURIZED. CHECK VALVE AND HOSE CONNECTOR RE PLACED, DUCT REPAIRED. 2 L 7 3 4F 4 F A22WE E23EA 1996040500921 19960405 00921 WP 1996 4 5 ABXA9600437 1 19960402 A 2931 HYD PRESS IND DOUG DC8 DC863 302198A WP HYD SYST MALFUNCTIONED A ABXA O OTHER N FALSE WARNING DE DESCENT 1 GL 23 816AX 46093 AIRCRAFT LOST HYDRAULIC PRESSURE AT TOP OF DESCENT. CHECKED AIRCRAFT FOR EVIDENCE OF HYDRAULIC LEAKAGE AND NO LEAKS WER E NOTED. HYDRAULIC FLUID QUANTITY WAS NORMAL. CHECKED HYDRAULIC PRESSURE AND POWER SYSTEM. INSPECTED BOTH ENGINE DRIV EN HYDRAULIC PUMP CASE DRAIN FILTERS FOR CONTAMINATION AND NONE WAS NOTED. REPLACED BOTH FILTERS FOR PRECAUTIONARY MAIN TENANCE. 2 L 7 4 4F 4A25 1996040500925 19960405 00925 SO 1996 4 5 COMA9610119 1 19960401 A 3250 STEERING EMB 120 EMB120RT SO NLG PULLED LEFT A COMA K NONE O OTHER LD LANDING 1 SO 01 256CA 120245 NOSE WHEEL STEERING PULLED TO LEFT TWICE DURING LANDING ROLL. COULD NOT DUPLICATE. INSPECTED N.W.S. SYSTEM AND TAXI CH ECK NORMAL. 2 L 7 2 4T RT A31SO 1996040500926 19960405 00926 SO 1996 4 5 COMA9610121 1 19960401 A 3040 2SC1175A SENSOR EMB 120 EMB120RT SO LT WINDSHIELD FAILED A COMA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 161CA 120143 BURNING ELECTRICAL SMELL NOTED IN COCKPIT WHEN WINDSHIELD HEAT SELECTED ON. REPLACED THE LT WINDSHIELD CURRENT SENSOR. 2 L 7 2 4T RT A31SO 1996040500927 19960405 00927 SO 1996 4 5 COMA9610122 1 19960331 A 2752 3203001005 ACTUATOR EMB 120 EMB120RT SO LT TE FLAP MALFUNCTION A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 159A 6698 2790 120159 FLAP DISAGREEMENT WARNING. INBD FLAPS INDICATE 5 DEGREES DOWN WHEN SELECTED UP. REPLACED THE LT INBD FLAP ACTUATOR. PA RT TOTAL CYCLES, 7,272. 2 L 7 2 4T RT A31SO 1996040500928 19960405 00928 EU 1996 4 5 COMA9630093 1 19960331 A 2613 1734362450 OVERHEAT DET SAAB SF340 SF340A 7850100 EU RT ENGINE DIRTY A COMA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 146CA 340A146 RIGHT ENGINE TAIL PIPE H0T WARNING CAME ON. WARNING REMAINED AT REDUCED POWER. CLEANED AND SEALED WIRING CONNECTIONS O N RT TAIL PIPE HEAT SENSORS. 2 L 7 2 4T RT A52EU 1996040500929 19960405 00929 NE 1996 4 5 COMA9630094 3 19960402 A 6111 EROSION GUARDS SAAB SF340 SF340A 7850100 EU ROTOL R389 R3894123F25 NE LT PROP CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 340SF 4564 340A014 876884 LEFT PROPELLER, BLADE EROSION GUARDS, ARE CRACKED AND DEBONDING. REPLACED PROPELLER. 2 L 7 2 4T RT A52EU 6 C P30NE 1996040500930 19960405 00930 EU 1996 4 5 COMA9630095 1 19960331 A 2530 6500192 WARMING POT SAAB SF340 SF340A 7850100 EU GALLEY DEFECTIVE A COMA K NONE O OTHER CR CRUISE 1 SO 01 320CA 340A064 BURNING ODOR NOTICED AT GALLEY AREA. REPLACED COFFEE WARMING POT. 2 L 7 2 4T RT A52EU 1996040500931 19960405 00931 EA 1996 4 5 COMA9660058 1 19960330 A 2751 CONNECTOR CNDAIR CL600 CL6002B19 EA TE FLAP IND SHORTED A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 943CA 7062 FLAP FAIL MESSAGE ON EICAS. WILL NOT RESET. REPAIRED SHOTED WIRING AT FLAP BRAKE AND POSITION SENSOR WIRING CONNECTOR. 2 L 7 2 4F RT A21EA 1996040500932 19960405 00932 EA 1996 4 5 COMA9660059 1 19960401 A 5610 NP1393221 SIDE WINDSHIELD CNDAIR CL600 CL6002B19 EA LT COCKPIT CRACKED A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 946CA 1901 7072 PILOT'S SIDE WINDSHIELD CRACKED. REPLACED WINDOW. PART TOTAL CYCLES, 1,663. 2 L 7 2 4F RT A21EA 1996040500933 19960405 00933 EA 1996 4 5 COMA9660060 1 19960403 A 2760 601R591473 SECU CNDAIR CL600 CL6002B19 EA NR 2 SPOILER MALFUNCTION A COMA K NONE J WARNING INDICATION LD LANDING 1 SO 01 926CA 395 7027 SPOILERS FAULT MESSAGE ON EICAS. REPLACED THE NR 2 SPOILER ELECTRONIC CONTROL UNIT. PART TOTAL CYCLES, 295. 2 L 7 2 4F RT A21EA 1996040500934 19960405 00934 EA 1996 4 5 COMA9660061 1 19960401 A 2750 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS DIRTY A COMA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 943CA 2597 7062 FLAPS FAIL MESSAGE ON EICAS. SYSTEM WOULD NOT RESET. DISASSEMBLED, CLEANED, AND REASSEMBLED FLAP WIRING HARNESS CONNEC TIONS IN MLG WHEELWELLS, ACFT RETURNED TO SERVICE. PART TOTAL CYCLES, 2,322. 2 L 7 2 4F RT A21EA 1996040500935 19960405 00935 EA 1996 4 5 COMA9660062 1 19960402 A 3040 NP1393221 WINDOW CNDAIR CL600 CL6002B19 EA LT COCKPIT BURNED A COMA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 912CA 7011 STRONG ELECTRICAL ODOR IN COCKPIT WHEN WINDSHIELD HEAT SELECTED ON. SMOKE DISSAPATED WHEN SYSTEM DE-ENERGIZED. 2 L 7 2 4F RT A21EA 1996040500936 19960405 00936 WP 1996 4 5 SCNA96039 1 19960330 A 2611 DAMA15SWS CONNECTOR DOUG DC10 DC1015 3022118 WP LAV SMOKE DET FAULTY A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 THE SMOKE DETECTOR IN LAVATORY 'A' WAS FOUND TO BE INOPERATIVE. REPLACED ELECTRICAL CONNECTOR AT SMOKE DETECTOR. DETEC TOR OPS CHECKED NORMAL. 2 L 7 3 4F A22WE 1996040500937 19960405 00937 NM 1996 4 5 UPS96205828 1 19960330 A 5315 6026998 FLOOR BEAM BOEING 727 72727C 138400J NM BS 1110 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON LOWER FLANGE OF FLOORBEAM STA 1110, WL 200, AND LBL 9-19. REMO VED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. CUT LOWER FLANGE AND REPAIRED PER E.O. 727-53-1745. 2 L 7 3 4F A3WE 1996040500938 19960405 00938 NM 1996 4 5 UPS96205829 1 19960331 A 5312 6026998 BLKHD SHEARTIE BOEING 727 72727C 138400J NM BS 351 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON UPPER END OF SHEARTIE AT BS 351, RBL 45, WL 168, FORWARD SIDE O F BS 351 BULKHEAD. CORROSION OUT OF LIMITS, REPAIRED WEB AND SHEARTIE IAW SRM 51-30-2, 53-10-3, 53-10-4, 51-10-2, 51-40 -2, AND 51-40-3. 2 L 7 3 4F A3WE 1996040500939 19960405 00939 NM 1996 4 5 UPS96205830 1 19960329 A 5320 CHORD BOEING 727 72727C 138400J NM BS 1152 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED WHILE WORKING NRC, FOUND BL ZERO CHORD, STA 1152, WL 200, TO BE CRACKED ON V ERTICAL LEG. REPAIRED BL ZERO CHORD AT STA 1152 IAW UPS E.O. 727-53-1748. 2 L 7 3 4F A3WE 1996040500940 19960405 00940 NM 1996 4 5 UPS96205831 1 19960331 A 5312 BLKHD ANGLE BOEING 727 72727C 138400J NM BS 480 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED WHILE WORKING AC/CG, DISCOVERED CORROSION AT BS 480 29 ON BULKHEAD Z-ANGLE. REMOVED CORROSION, REWORK OUT OF LIMITS IAW SRM 53-10-1, REMOVED AND REPLACED Z-ANGLE 51-20-1 AND IAW SRM 51-10-1 AND 5 1-30-2. 2 L 7 3 4F A3WE 1996040500941 19960405 00941 NM 1996 4 5 UPS96205832 1 19960401 A 5347 SEAT TRACK BOEING 727 72727C 138400J NM BS 960-1180 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED SEAT TRACK STA 960-1180, BL ZERO CORRODED. REPLACED IAW SRM EWO 96-2170 SRM 51-30-2. 2 L 7 3 4F A3WE 1996040500942 19960405 00942 NM 1996 4 5 UPS96205833 1 19960330 A 5230 FITTING BOEING 727 72727C 138400J NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED FORWARD CARGO DOORWAY UPPER FORWARD STOP PAD FITTING CRACKED. REMOVED OUTSI DE DIAMETER STOP PAD FITTING, RECEIVED AND INSTALLED ON AIRCRAFT, WORK DONE IAW SRM 51-30-2, AND 52-31-01. 2 L 7 3 4F A3WE 1996040500943 19960405 00943 NM 1996 4 5 UPS96205834 1 19960303 A 5230 BEAM BOEING 727 72727C 138400J NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED FORWARD CARGO DOOR NR 5 TRANSVERSE BEAM CRACKED IN OUTBOARD RADIUS AT NR 1 A ND NR 2 SKIN VERTICAL STIFFENERS. REMOVED INNER SKIN, REMOVED NR 5 TRANSVERSE BEAM, FABRICATED NEW TRANSVERSE BEAM, AND INSTALLED IN DOOR. ALSO, REPLACED INBOARD AND OUTBOARD L-ANGLES. INSTALLED INNER SKIN. ALL WORK DONE IAW SRM 51-30-2 . 2 L 7 3 4F A3WE 1996040500944 19960405 00944 NM 1996 4 5 UPS96205835 1 19960327 A 5230 651862586 DOOR FRAME BOEING 727 72727C 138400J NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED AFT CARGO DOOR FORWARD LOWER FRAME CRACKED AT FORWARD CENTERING GUIDE ROLLER FITTING. REMOVED AND REPLACED AFT CARGO DOOR FORWARD LOWER FRAME PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996040500945 19960405 00945 NM 1996 4 5 UPS96205836 1 19960327 A 5230 BEAM BOEING 727 72727C 138400J NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED AFT CARGO DOOR NR 5 TRAVERSE BEAM CRACKED IN OUTBOARD RADIUS AT NR 1, NR 2, AND NR 3 OUTER SKIN VERTICAL STIFFENERS. REMOVED AND REPLACED BEAM IAW SRM 51-30-2, 51-10-1, 51-20-21, 51-40-2. 2 L 7 3 4F A3WE 1996040500946 19960405 00946 NM 1996 4 5 UPS96205837 1 19960327 A 5230 651862011 BEAM BOEING 727 72727C 138400J NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CARGO DOOR NR 2 TRAVERSE BEAM CRACKED IN OUTBOARD RADIUS AT NR 1 OUTER SKIN VERTICAL STIFFENERS. REMOVED AND REPLACED NR 2 TRAVERSE BEAM IAW SRM 51-10-1, 51-10-2, 51-20-4, 51-30-2 AND M/M 51-20- 151. 2 L 7 3 4F A3WE 1996040500947 19960405 00947 NM 1996 4 5 UPS96205838 1 19960327 A 5230 651862016 ANGLE BOEING 727 72727C 138400J NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED FORWARD CARGO DOOR NR 2 OUTBOARD TRAVERSE BEAM L-ANGLE CRACKED IN RADIUS AT NR 2 OUTER SKIN VERTICAL STIFFENER. REMOVED AND REPLACED NR 2 OUTBOARD TRAVERSE BEAM L-ANGLE IAW SRM 51-10-1, 51-10-2, 51-20-4, 51-30-2 AND M/M 51-20-151. 2 L 7 3 4F A3WE 1996040500948 19960405 00948 NM 1996 4 5 UPS96205839 1 19960327 A 5230 651862013 ANGLE BOEING 727 72727C 138400J NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED FORWARD CARGO DOOR NR 4 TRAVERSE BEAM AND OUTBOARD L-ANGLE CRACKED IN RADIU S AT OUTER SKIN VERTICAL STIFFENER. REMOVED AND REPLACED NR 4 TRAVERSE BEAM AND OUTBOARD L-ANGLE IAW SRM 51-10-1, 51-30 -2, 51-30-5, 51-10-2 AND M/M 51-20-151. 2 L 7 3 4F A3WE 1996040500949 19960405 00949 NM 1996 4 5 UPS96205840 1 19960326 A 5311 FRAME BOEING 727 72727C 138400J NM BS 294.5 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON BS 294.5 FRAME WEB AT RBL 37, WL 168. REPAIRED FRAME WEB IAW S RM 51-20-1. UPPER WEB AT BS 290 WAS ALSO REPLACED IAW SRM 51-20-1, 51-30-2. 2 L 7 3 4F A3WE 1996040500950 19960405 00950 NM 1996 4 5 UPS96205841 1 19960326 A 5320 CHORD BOEING 727 72727C 138400J NM BS 294.5 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED WHILE WORKING ON CUSTOMER CARD NR 437378, FOUND HORIZONTAL CHORD AT STA 294. 5, WL 181, LBL 17, AND RBL 4-25, TO HAVE CORROSION. OUT OF LIMITS. REMOVED AND REPLACED FUSELAGE CHORD AND HORIZONTAL CHORD IAW SRM 51-30-2, 51-20-4, 51-30-5. 2 L 7 3 4F A3WE 1996040500951 19960405 00951 NM 1996 4 5 UPS96205842 1 19960326 A 5320 FLOOR SUPPORT BOEING 727 72727C 138400J NM BS 314 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED FINDING CORROSION ON FLOOR SUPPORT STA 314, RBL 15-40, WL 208 AROUND NUTPLAT E HOLES. OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-20-1, 51-30-2. 2 L 7 3 4F A3WE 1996040500952 19960405 00952 NM 1996 4 5 UPS96205843 1 19960305 A 5320 65261737 FLOOR SUPPORT BOEING 727 72727C 138400J NM BS 328-344 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED FINDING CORROSION ON FLOOR SUPPORT STA 328-344, RBL 41, WL 208 OUT OF LIMITS . REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-10-1, 51-30-2. 2 L 7 3 4F A3WE 1996040500953 19960405 00953 NM 1996 4 5 UPS96205844 1 19960326 A 5347 BAS15201430 SEAT TRACK BOEING 727 72727C 138400J NM BS 660-740 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED FINDING CORROSION ON SEAT TRACK LBL 62, STA 660-740, WL 208 OUT OF LIMITS. R EMOVED AND REPLACED SEAT TRACK IAW SRM 53-10-1, 51-30-2. 2 L 7 3 4F A3WE 1996040500954 19960405 00954 NM 1996 4 5 UPS96205845 1 19960326 A 5347 BAC15201432 SEAT TRACK BOEING 727 72727C 138400J NM BS 344 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED FINDING SEAT TRACK CRACKED ON FLANGE, STA 344, WL 208. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-20-151, 51-30-2. 2 L 7 3 4F A3WE 1996040500955 19960405 00955 NM 1996 4 5 UPS96205846 1 19960326 A 5350 SEAL BOEING 727 72727C 138400J NM BS 673-674 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED MOY SEAL HAS CRACKS AT BS 673-674.5 AND 135.702.5 - 704, WL 208, LBL 65 CONT AINED CRACKS AND FABRICATED REPAIR PARTS IAW SRM 51-40-3, AND INSTALLED PARTS IAW 51-30-2. 2 L 7 3 4F A3WE 1996040500956 19960405 00956 NM 1996 4 5 UPS96205847 1 19960327 A 5347 SEAT TRACK BOEING 727 72727C 138400J NM BS 1100-1300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED SEAT TRACK CORRODED OUT OF LIMITS AT STA 1100-1300, RBL 25, WL 208. REPLA CED IAW SRM 53-10-5, 51-10-6MM, 51-20-151, 51-30-2. 2 L 7 3 4F A3WE 1996040500957 19960405 00957 NM 1996 4 5 UPS96205848 1 19960327 A 5312 BULKHEAD BOEING 727 72727C 138400J NM BS 294.5 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED FINDING CORROSION ON AFT SIDE OF BS 294.5 BULKHEAD ALONG TOP OF HORIZONTAL C HORD BETWEEN RBL 4 + 25 WL 182. OUT OF LIMITS. REPAIRED 294.5 FROM LBL 26-RBL26 IAW SRM 51-10-1, 51-10-2, 51-20-4, 51- 30-2, 51-30-5, 51-40-2, AND M/M 51-20-151. 2 L 7 3 4F A3WE 1996040500958 19960405 00958 NM 1996 4 5 UPS96205849 1 19960326 A 5320 BAC1510335 HAT CHANNEL BOEING 727 72727C 138400J NM BS 304-344 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED FINDING CORROSION ON HAT CHANNEL STA 304 - 344, RBL 14, WL 208. OUT OF LIMI TS. REMOVED AND REPLACED HAT CHANNEL IAW SRM 51-10-2, 51-20-4, 51-30-2, 51-30-5, 51-30-8. 2 L 7 3 4F A3WE 1996040500959 19960405 00959 NM 1996 4 5 UPS96205850 1 19960327 A 5712 6597104123 WING RIB BOEING 727 72727C 138400J NM WS 601.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED FINDING WING RIB REPAIR AT WS 601.5 LT STR 7 LOWER HAS 1 INCH CRACK. REMOV ED CRACK IAW B727-5710-1325 APP A, REPLACED RIB, AND INSTALLED IAW B727-5710-1325 APP C. 2 L 7 3 4F A3WE 1996040500960 19960405 00960 NM 1996 4 5 UPS96205851 1 19960328 A 5720 WEB BOEING 727 72727C 138400J NM BS 1131 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED FINDING CORROSION ON SHEAR WEB BS 1131, RBL 62, WL 208. REMOVED AND REPLAC ED SHEAR WEB RT IAW SRM 51-30-2, 51-10-1, AND M/M 51-20-151. 2 L 7 3 4F A3WE 1996040500961 19960405 00961 NM 1996 4 5 UPS96205852 1 19960327 A 5320 65317731 CHORD BOEING 727 72727C 138400J NM BS 1176 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED FINDING THE 1176 CHORD CORRODED OUT OF LIMITS FROM RBL 65 TO LBL 65, WL 208, IAW SRM 53-10-1. REMOVED AND REPLACED CHORD IAW SRM 51-10-1, 51-10-2, 51-30-2, 51-30-5, 51-20-4, AND M/M 51-20-151. 2 L 7 3 4F A3WE 1996040500962 19960405 00962 NM 1996 4 5 UPS96205862 1 19960404 A 3350 1000679 LIGHT BOEING 727 727247 138408F NM COCKPIT DOOR INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 902UP 21698 MAINTENANCE REPORTED ON PRE-DEPARTURE CHECK, EXIT LIGHTS IN COCKPIT FOUND INOPERATIVE. LIGHT ABOVE DOOR. REMOVED AND R EPLACED LIGHT ASSY. OPS NORMAL. 2 L 7 3 4F A3WE 1996040500963 19960405 00963 NM 1996 4 5 UPS96405856 1 19960401 A 5320 ANGLE BOEING 747 747123 1384873 NM BS 2200-S-40RH CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 WHILE IN FOR C-CHECK AT AMS MAINTENANCE REPORTED - AREA AFT OF BULK CARGO COMP, FOUND CRACKED STIFFINER - ANGLE FROM INT ERCOSTAL ON FORWARD SIDE OF FRAME BS 2200, S40R. REPLACED STIFFENER-ANGLE IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996040500964 19960405 00964 WP 1996 4 5 UPS96805853 1 19960227 A 5532 SKIN DOUG DC8 DC871F 302199D WP VERT STAB CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED VERTICAL STABILIZER T/E, BOTH SIDES HAVE CORROSION BETWEEN NR 4 RUDDER SUPPOR T FITTING. REPLACED SKIN PANEL BY REBONDING NEW ONES IAW SRM 51-1-19. 2 L 7 4 4F RT 4A25 1996040500965 19960405 00965 WP 1996 4 5 UPS96805854 1 19960228 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 700 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT WING T/E, STA XW700 TO STA XW 710 HAS CORROSION BULGES ON SKIN. REPAIRED SKIN IAW DOUG DRAWING NR 5644654. 2 L 7 4 4F RT 4A25 1996040500966 19960405 00966 WP 1996 4 5 UPS96805855 1 19960402 A 2822 BOOST PUMP DOUG DC8 DC873F 302199F WP NR 1 ENGINE INOPERATIVE A IPXA E ENGINE SHUTDOWN X ENGINE FLAMEOUT CR CRUISE 1 SO 01 836UP 45936 CREW REPORTED NR 1 ENGINE FLAME-OUT AT FLT 370 (NO FUEL FLOW NOTED DURING RESTART ATTEMPT). INSPECTED INLET AND EXHAUST SECTIONS. ALSO, INSPECTED CHIP DETECTORS. RAN ENGINE AT IDLE AND 82 PERCENT N2. NO PROBLEMS DETECTED. ENGINE OK FOR CONTINUED SERVICE. NOTE: REMOVED AND REPLACED NR 1 ALT FUEL BOOST PUMP. 2 L 7 4 4F RT 4A25 1996040500967 19960405 00967 WP 1996 4 5 UPS96805857 1 19960313 A 5320 DOUBLER DOUG DC8 DC871F 302199D WP FS 1600-1650 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION DAMAGE ON FUSELAGE INNER DOUBLER, FS 1600-1650, LONGERONS 21R-31R. REPLACED DOUBLER SECTION PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1996040500968 19960405 00968 WP 1996 4 5 UPS96805858 1 19960302 A 5330 SKIN DOUG DC8 DC871F 302199D WP FS 1600-1650 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION DAMAGE ON FUSELAGE INNER SKIN, STA 1600-1680, LONGERONS 21R-31R. R EPLACED SECTION PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1996040500969 19960405 00969 WP 1996 4 5 UPS96805859 1 19960302 A 5320 ANGLE DOUG DC8 DC871F 302199D WP FS 702 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION DAMAGE ON LOWER ATTACH ANGLE UNDER MAIN CABIN SEAT TRACK NR 4, FS 7 02, BL ZERO. SPLICED ANGLE PER SRM 53-2-0. 2 L 7 4 4F RT 4A25 1996040500970 19960405 00970 WP 1996 4 5 UPS96805860 1 19960302 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP FS 759-781 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED SEAT TRACK NR 1 HAS CORROSION DAMAGE AND CRACKS AT FS 759-781, LBL 55. REPLA CED TRACK SECTION PER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1996040500971 19960405 00971 WP 1996 4 5 UPS96805861 1 19960302 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP FS 759-822 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON MAIN CABIN SEAT TRACK NR 5 AROUND FLOOR BEAM ATTACH HOLES FS 759-822, RBL 22. REPLACED TRACK SECTION PER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1996041200003 19960412 00003 1996 4 12 96ZZZX1565 4 19960128 A 3422 109290 GYRO BOLKMS 117 BK117A3 5626015 EU COCKPIT FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 528SF 109 0129 7104 GYRO UNABLE TO SPOOL UP. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996041200004 19960412 00004 EU 1996 4 12 96ZZZX1566 1 19960224 A 7712 105957411 INDICATOR BOLKMS 105 BO105LSA3 5626020 EU ENG TQ INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 202LF 107 2014 INDICATOR UNIT INOPERATIVE UPON INSTALL. GAUGE READS APPROXIMATELY 20 PERCENT TQ ON BOTH ENGINES WITH JUST ELECTRICAL P OWER APPLIED. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H3AU 1996041200005 19960412 00005 EU 1996 4 12 96ZZZX1567 1 19960223 A 6730 AC67246 SERVO DUNLOP SNIAS 350 AS350B2 8680813 EU M/R LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 07 96LG 437 244 QC038 2817 SERVO LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996041200006 19960412 00006 NE 1996 4 12 96ZZZX1568 2 19960208 A 7250 414129001 ROTOR ASSY BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE POWER TURBINE BLADE SHIFT A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 5188B 961 279 SC46938 7163 LE45757EF FAILED SB LT101-72-10-0153. EXCESSIVE IBPT BLADE SHIFT NR 1 PLUS 0.013 INCH, NR 12 PLUS 0.012 INCH, NR 14 PLUS 0.012 IN CH, NR 24 PLUS 0.010 INCH. REPLACED WITH USED UNIT, CORRECTED PROBLEM. PART TOTAL CYCLES, 3000.3. 1 G 7 2 3U 3 U H13EU E5NE10 1996041200007 19960412 00007 NE 1996 4 12 96ZZZX1569 2 19960123 A 7250 414129001 ROTOR ASSY BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE POWER TURBINE BLADE SHIFT A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 71703 1600 3452 7227 SC20489 FAILED SB LT101-72-10-0153. EXCESSIVE IBPT BLADE SHIFT NR 24 PLUS 0.015 INCH, NR 19 PLUS 0.020 INCH. REPLACED WITH USE D UNIT, CORRECTED PROBLEM. PART TOTAL CYCLES, 3452.2. 1 G 7 2 3U 3 U H13EU E5NE10 1996041200021 19960412 00021 NE 1996 4 12 96ZZZX1583 2 19960112 A 7313 3039260 NOZZLE SET DOUG MD900 MD900 3027375 NM PWA PW206 PW206A NE FN2 DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 901CF 10 1WK03276 90000012 PCE206080 TROUBLESHOOTING LT ENGINE FOR HUNG START AT 38 PERCENT NG AND ALSO FAILED TO REACH IDLE RPM. REPLACED WITH NEW NOZZLE S ET UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U NC H19NM E42NE 1996041200026 19960412 00026 CE 1996 4 12 96ZZZX1588 1 19960118 A 7712 99103313 TRANSDUCER CESSNA 441 441 2076020 CE ENG TORQUE DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 8970N 10 51705190 4410092 TRANSDUCER UNIT WILL NOT MAINTAIN ADJUSTMENT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 L 7 2 3T RT A28CE 1996041200027 19960412 00027 CE 1996 4 12 96ZZZX1589 1 19960109 A 7712 99103311 TRANSDUCER CESSNA 441 441 2076020 CE ENGINE TORQUE DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 8970N 365 1171A 4410092 TRANSDUCER CAUSES GAUGE TO DROP TO ZERO. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 L 7 2 3T RT A28CE 1996041200028 19960412 00028 SW 1996 4 12 96ZZZX1590 1 19960201 A 6730 222382001103 ACTUATOR BELL 222 222 1182122 SW M/R LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 07 30SV 0533A 47044 ACTUATOR LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H9SW 1996041200029 19960412 00029 NM 1996 4 12 96ZZZX1591 1 19960225 A 6230 900C2010183105 LINK ASSY DOUG MD900 MD900 3027375 NM M/R SCISSORS WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 901CF 199 90000012 EXCESSIVE PLAY IN LINK ASSY CAUSING MAIN ROTOR VIBRATION. INSTALLED NEW LINK ASSY PER INSTRUCTION FROM MIKE SUTT (MDHS FIELD SUPPORT). 1 G 7 2 3U NC H19NM 1996041200031 19960412 00031 SW 1996 4 12 96ZZZX1593 1 19960325 A 3213 412050010107 CROSS TUBE BELL 412 412 1182202 SW RT SIDE AFT FAILED A A HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3911L A0463 33023 AIRCRAFT PARKED ON RAMP WHEN AFT CROSS TUBE FAILED ON RT SIDE OF CENTER SUPPORT BEAM ASSEMBLY CLAMP. THE AIRCRAFT IMPAC TED THE GROUND RUPTURING RIGHT EXTERNAL STC FUEL CELL. 1 G 7 2 4U H4SW 1996041200060 19960412 00060 WP 1996 4 12 9607619163 1 19960403 A 3260 UPLOCK ROLLER DOUG DC9 DC914 3022034 WP LT MLG DOOR OUT OF ADJUST A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 8906E 45747 DURING CLIMBOUT, GEAR UNSAFE LIGHT REMAINED LIT AFTER GEAR WAS RETRACTED. PERFORMED COM PROCEDURES AND CONTINUED TO ATL AT A REDUCED AIRSPEED OF 250 KNOTS. FLIGHT LANDED NORMALLY AT ATL. FOUND LEFT GEAR DOOR UPLOCK ROLLER OUT OF TOLERANC E. ADJUSTED UPLOCK AND OPERATIONAL CHECK OF GEAR WAS GOOD. 2 L 7 2 4F A6WE 1996041200061 19960412 00061 EU 1996 4 12 9607623226 1 19960403 A 3230 848401 SENSOR AIRBUS 320 A320211 3930320 EU LT MLG MALFUNCTIONED A A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 326US 282 AFTER TAKEOFF THE LANDING GEAR DID NOT RETRACT, CYCLED LANDING GEAR HANDLE AND ALL INDICATIONS WERE NORMAL. AIRCRAFT CO NTINUED TO ORIGINAL DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR PROXIMITY SENSOR 20GA, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996041200062 19960412 00062 WP 1996 4 12 9607639153 1 19960405 A 3350 LIGHT DOUG DC9 DC914 3022034 WP CABIN SHORTED OUT A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8912E 45829 DURING LINE CHECK, FOUND LEFT OVERWING EMERGENCY EXIT EMERGENCY LIGHT INOPERATIVE. FOUND SHORT IN LIGHT ASSEMBLY. REPL ACED LIGHT ASSEMBLY AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996041200063 19960412 00063 WP 1996 4 12 9607649874 1 19960402 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 783NC 48108 DURING LINE CHECK, FOUND AFT WALKWAY EMERGENCY LIGHTS OUT. RESEATED BULBS AND REPLACED THE BATTERY PACK, OPERATIONAL CH ECK GOOD. 2 L 7 2 4F A6WE 1996041200064 19960412 00064 WP 1996 4 12 9607659991 1 19960403 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP TAIL COMPARTMENT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8957E 47215 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS IN TAIL COMPARTMENT AREA INOPERATIVE. REPLACED BATTERIES, OP ERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996041200065 19960412 00065 WP 1996 4 12 9607669610 1 19960306 A 2420 976J2544 CONTROL PANEL DOUG DC9 DC932 3022066 WP NR 2 GEN MALFUNCTION A NWAA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 GL 01 610NW 47432 LOSS OF B-PHASE ITEMS ON NR 2 GENERATOR OCCURRED EN ROUTE. FLIGHT DIVERTED TO DFW AND LANDED WITHOUT INCIDENT. MAINTEN ANCE REPLACED NR 2 GENERATOR CONTROL PANEL, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996041200066 19960412 00066 WP 1996 4 12 9607779979 1 19960403 A 3350 CONNECTORS DOUG DC9 DC931 3022065 WP CABIN CROSSED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9343 47439 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN AND ENTRY DOOR EMERGENCY LIGHTS INOPERATIVE. FOUND CONNECTORS C ROSSED IN GALLEY OVERHEAD PANEL. CORRECTED WIRING, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996041200067 19960412 00067 WP 1996 4 12 9607789937 1 19960401 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 908H 47517 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS BETWEEN ROWS 3 AND 5 INOPERATIVE. MAINTENANC E FOUND BROKEN WIRE AT ROW 3 AND LOOSE CONNECTOR AT ROW 5. REPAIRED WIRE AND RESECURED CONNECTOR, OPERATIONAL CHECK NO RMAL. 2 L 7 2 4F A6WE 1996041200068 19960412 00068 WP 1996 4 12 9607799952 1 19960402 A 3350 6011779 BATTERY PACK DOUG DC9 DC931 3022065 WP RT EXTERIOR DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 916RW 47144 DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATION AL CHECK NORMAL. 2 L 7 2 4F A6WE 1996041200069 19960412 00069 WP 1996 4 12 9607809933 1 19960404 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 1334U 47280 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. REPLACED BROKEN W IRING AT ROW 1, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996041200070 19960412 00070 WP 1996 4 12 9607819924 1 19960402 A 3350 60030451 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 926RC 47473 DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PA CK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996041200071 19960412 00071 1996 4 12 9607829612 4 19960403 A 2565 13621228 EVAC SLIDE DOUG DC9 DC932 3022066 WP TAIL CONE LOW PRESSURE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 610NW 1390 1376 47432 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL CONE EMERGENCY EVACUATION SLIDE LOW ON PRESSURE. REPLACED SLIDE. 2 L 7 2 4F A6WE 1996041200072 19960412 00072 NM 1996 4 12 96FDEA00734 1 19960115 A 5320 69B028034 SHEAR TIE BOEING 747 747245F 1384897 NM BS 1840 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 640FE 20826 NR 1233, MAIN DECK SHEAR TIE FOUND CRACKED AT BS 1840 BETWEEN STR 4 TO 55R AS MARKED. SHEAR TIE REPLACED AS PER DWG 65B 01786. 2 L 7 4 4F A20WE 1996041200073 19960412 00073 NM 1996 4 12 96FDEA00735 1 19960115 A 5320 69B028032 SHEAR TIE BOEING 747 747245F 1384897 NM BS 1840 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 640FE 20826 NR 1234, MAIN DECK SHEAR TIE FOUND CRACKED BS 1840 STR 11R AS MARKED. SHEAR TIE REPLACED AS PER DWG 65B01786. 2 L 7 4 4F A20WE 1996041200074 19960412 00074 NM 1996 4 12 96FDEA00736 1 19960115 A 5313 BAC1493412 STRINGER BOEING 747 747245F 1384897 NM BS 1980 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 640FE 20826 NR 1247, MAIN DECK STRINGER FOUND CRACKED AT BS 1980 AT STR 13L AS MARKED. STRINGER REPAIRED AS PER FEDEX 727 SRM REV 7 6 53-10-03 FIG 2. 2 L 7 4 4F A20WE 1996041200075 19960412 00075 WP 1996 4 12 ABXA9600441 1 19960404 A 2910 NAS161212 O-RING SEAL DOUG DC8 DC863 302198A WP NR 2 HYD PUMP DEFECTIVE A ABXA O OTHER K FLUID LOSS DE DESCENT 1 GL 23 811AX 46113 DURING DESCENT, HYDRAULIC FLUID QUANTITY DROPPED TO STANDPIPE LEVEL. REPLACED O-RING SEAL ON THE NR 2 HYDRAULIC PUMP PR ESSURE LINE FITTING, LEAK CHECK GOOD. 2 L 7 4 4F 4A25 1996041200081 19960412 00081 WP 1996 4 12 MWEA96103 1 19960403 A 2560 113313 EVAC SLIDE DOUG DC9 DC932 3022066 WP GALLEY DOOR FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 302ME 47102 CREW REPORTS EMERGENCY ESCAPE SLIDE FELL OFF GALLEY SERVICE DOOR. REINSTALLED EMERGENCY ESCAPE SLIDE ON GALLEY SERVICE DOOR. 2 L 7 2 4F A6WE 1996041200082 19960412 00082 EU 1996 4 12 QXEA9600140 1 19960404 A 3350 MGG1280 BULBS FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 450US 11101 FORWARD EXIT SIGN IS INOP. BULBS WERE REPLACED AND SIGN OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996041200087 19960412 00087 CE 1996 4 12 96ZZZX1626 1 19960202 A 3240 9980035 BRAKE ASSY BEECH 100 B100 1152919 CE LT MAIN GEAR FROZEN A A DSEA O OTHER O OTHER LD LANDING 1 GL 25 54CK 4663 BE73 CLE - ON TOUCH-DOWN, ACFT DECELLERATED ABRUPTLY AND YAWED TO THE LEFT. DIRECTIONAL CONTROL WAS MAINTAINED WITH OPPOSITE BRAKE AND RIGHT RUDDER. AFTER STOPPING ON THE RUNWAY, THE AIRCRAFT COULD NOT BE TAXIED. FOUND LT BRAKE ASSEMBLIES HAD FROZEN. AMBIENT TEMPS ON THIS DAY WERE ZERO DEGREES TO MINUS 5 DEGREES FAHRENHEIT. AIRCRAFT ON PREVIOUS DEPARTURE HAD TAXIED THROUGH SNOW AS DEEP AS 6 INCHES. BRAKES RELEASED AFTER THAWING. ALL BRAKE ASSEMBLIES WERE REPLACED. 1 L 7 2 4T A14CE 1996041200088 19960412 00088 EU 1996 4 12 96ZZZX1627 1 19960216 A 2910 NAS161204 O-RING ISRAEL 1124 1124 4500102 EU EQUIP BAY AFT FAILED A DSEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 25 331CW 5168 231 AT 1 PLUS 30 INTO A FLIGHT, ESTABLISHED IN CRUISE, THE LT HYD LOW PRESS ANNUNCIATOR ILLUMINATED. THIS WAS SUBSEQUENTLY FOLLOWED BY A RT HYD LOW PRESS ANNUNCIATOR LIGHT. THE MAIN SYS PRESS GAUGE INDICATED A 'ZERO'. A NORMAL LANDING WAS MA DE USING BACK-UP SYSTEMS FOR LANDING GEAR BRAKES, THRUST REVERSERS, AND FLAPS. LANDING WAS MADE AT JAX. AN O-RING SEAL , LOCATED ON A FITTING SITUATED BETWEEN THE MAIN SYS HYD SYS FILTER (AFT), AND A CHECK VALVE, FAILED. REASON FOR FAILUR E UNKNOWN. THIS ALLOWED ALL PRIMARY HYD SYS FLUID TO BLEED FROM SYS. THE O-RING WAS REPLACED, SYS SERVICED, AND ACFT R ETURNED TO SERVICE. 2 M 7 2 4F A2SW 1996041200089 19960412 00089 CE 1996 4 12 96ZZZX1628 1 19960212 A 7714 30738271 N1 MONOPOLE CESSNA 650 650 2076802 CE GARRTT TFE731 TFE7313B 01518 NE AFT ENG MODULE FAILED A A DSEA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 GL 25 41ST 5071 6500056 87255 APPROXIMATELY 45 MINUTES INTO THE FLIGHT, CLIMBING OUT OF FL 387, A SUDDEN YAW WAS FELT, THE RIGHT ENGINE POWER HAD DEC REASED, AND THE RT 'FUEL COMP MANUAL' LIGHT WAS ILLUMINATED. THE FUEL COMPUTER WAS CYCLED BACK PER CHECKLIST, BUT WOULD NOT REMAIN ON LINE ABOVE APPROX 94 PERCENT N1. THE ACFT DIVERTED TO WICHITA (CESSNA CITATION) FOR CORRECTIVE ACTION. T ROUBLESHOOTING DETERMINED THE N1 MONOPOLE TO HAVE FAILED CAUSING FUEL COMPUTER TO MALFUNCTION. THE PART WAS REPLACED. GROUND AND FLIGHT OPERATIONS SATISFACTORY. 2 L 7 2 4F 4 F A9NM E6WE 1996041200100 19960412 00100 NM 1996 4 12 96ZZZX1639 1 19960227 A 3230 RETRACT MECH BOEING 727 72722C 138400F NM RT MLG MALFUNCTIONED A RYNA O OTHER J WARNING INDICATION AP APPROACH 1 CE 07 421EX 19099 ON APPROACH INTO IND, LANDING GEAR HAD TO BE CYCLED THREE TIMES TO GET A DOWN AND LOCKED INDICATION ON THE RT MAIN GEAR. THE RED LIGHT REMAINED ON AND A GO-AROUND WAS INITIATED. AS THE AIRCRAFT PITCHED UP, THE LIGHT EXTINGUISHED AND THE G REEN LIGHT ILLUMINATED. THE GEAR WAS LEFT EXTENDED ON GO-AROUND, AND AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED LANDIN G GEAR ASSY PN 653756822 UNIT PER MM 32-9-211, GROUND CHECK NORMAL. ALSO, REPLACED RT MAIN GEAR SWITCH PER MM 32-32-0 A S PRECAUTION. OPS CHECK GOOD. 2 L 7 3 4F A3WE 1996041200101 19960412 00101 CE 1996 4 12 96ZZZX1640 1 19960316 A 3234 1013841371 GEAR HANDLE BEECH 1900 1900C 1154161 CE INSTRUMENT PANEL SHORTED A GUUA O OTHER J WARNING INDICATION CL CLIMB 1 SO 19 315BH UB25 FLT 158 - LPLL - 18874A, ALT - PILOT REPORT: GEAR STUCK IN DOWN POSITION. RESET CIRCUIT BREAKER AND GEAR RETRACTED. M AINTENANCE REPORT: FOUND INTERMITTENT SHORT IN GEAR HANDLE ASSY. REPLACED GEAR HANDLE ASSY. OPS CHECK GOOD. (X) 2 L 7 2 4T RT A24CE 1996041200102 19960412 00102 CE 1996 4 12 96ZZZX1641 1 19960316 A 3260 GEAR LIGHT BEECH 1900 1900C 1154161 CE LT MLG MALFUNCTIONED A GUUA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 SO 19 196GA UB31 FLT 434 - LPLL - 20711F, NAS, 03-16-96 - PILOT REPORT: LT MAIN GEAR LIGHT NOT ILLUMINATED ON FIRST CYCLE. CORRECTED WI TH SECOND GEAR CYCLE. MAINTENANCE: MULTIPLE GEAR SWINGS PERFORMED WITHOUT INCIDENT. AIRCRAFT RELEASED FOR SERVICE. ( X) 2 L 7 2 4T RT A24CE 1996041200103 19960412 00103 NE 1996 4 12 96ZZZX1642 3 19960302 A 6111 A10460E BLADE STBROS SD3 SD360 8100606 EU HARTZL HCA6A HCA6A3 NE RT PROPELLER SHEATH CRACKED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 831BE 8815 903 SH3757 GP82 AT SCHEDULED B-CHECK, INSPECTOR FOUND RIGHT PROPELLER PITTED. FURTHER INVESTIGATION REVEALED A CRACK IN THE FIBERGLASS SHEATH ON THE BACK FACE OF THE BLADE ROOT, APPROXIMATELY 3 INCHES FROM CUFF. REMOVED AND REPLACED RIGHT PROPELLER ASSY AND ROUTED TO HARTZELL, THE BLADE MANUFACTURER. 2 H 7 2 4T A41EU 6 C P14NE 1996041200104 19960412 00104 CE 1996 4 12 96ZZZX1643 1 19960319 A 2612 PHOTO CELL BEECH 99 C99 1154006 CE RT ENGINE DIRTY A GUUA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 SO 19 232BH U232 FPO/FPO - FLT 410 - PILOT REPORT: RIGHT FIRE PULL HANDLE ILLUMINATES IN-FLIGHT. PILOT DECLARED AN EMERGENCY AND RETURNE D TO FPO AND LANDED WITHOUT INCIDENT. MAINTENANCE REPORT: CLEANED AND DRIED PHOTO CELLS, OPERATIONAL CHECK NORMAL. SUS PECT MOISTURE FROM RAIN STORM MAY BE THE CAUSE. 1 L 7 2 3T A14CE 1996041200105 19960412 00105 CE 1996 4 12 96ZZZX1644 1 19960224 A 6120 CONTL LINKAGE BEECH 1900 1900 1154160 CE RT PROP GOV OUT OF ADJUST A GUUA E ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 SO 19 17ZR 4644 UB17 TLH/TLH - FLT 382 - PILOT REPORT: ON TEST FLIGHT, SHUT DOWN RIGHT ENGINE DUE TO LOW TORQUE. MAINTENANCE: ADJUSTED RIG HT PROPELLER RIGGING FOR CONTINUED SERVICE PRIMARY PROPELLER GOVERNOR, PN 8210212D, INSTALLED PRIOR TO TEST FLIGHT. 2 L 7 2 4T RT A24CE 1996041200106 19960412 00106 NM 1996 4 12 96ZZZX1645 1 19960316 A 3350 XB864041 LIGHT BOEING 737 737301 1384611 NM CABIN DAMAGED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 578US 23257 DEN - PRIOR TO DEPARTURE, FLIGHT CREW REPORTED THE EMERGENCY EXIT LIGHT ASSEMBLY ON AISLE ARM REST OF SEAT 11 DAMAGED. R EPLACED LIGHT ASSY AND SYSTEM CHECKED OKAY. AIRFRAME TT: 33,712.5 HRS. C-CHECK: 1,407.6 HRS. 2 L 7 2 4F RT A16WE 1996041200107 19960412 00107 EU 1996 4 12 96ZZZX1646 1 19960319 A 2170 18084932 COALESCENT SOCK FOKKER F28 F28MK4000 4990810 EU RIGHT DIRTY A A21A O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 17 498US 348 11181 FAT - ON CLIMB-OUT, NOTICED FUMES AND SMOKE IN COCKPIT AND CABIN. CHECKED COOLING TURBINE, FOUND OIL PRESENT. CHECKED COALESCENT SOCKS AND CLEANED BOTH. 2 L 7 2 4F RT A20EU 1996041200108 19960412 00108 NM 1996 4 12 AALA960351 1 19960302 A 3350 1722331 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 373AA 25200 SFO - DURING OVERNIGHT CHECK, EMERGENCY LIGHTS AT PASSENGER SEAT 24H FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT 24H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1996041200109 19960412 00109 NM 1996 4 12 AALA960352 1 19960301 A 3350 1722331 CONNECTOR BOEING 767 767223 1385123 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 338AA 22335 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 23H FOUND INOPERATIVE. REPLACED EMERGENCY EXIT LIG HT CONNECTOR AND TWO PINS AT PASSENGER SEAT 23H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1996041200110 19960412 00110 NM 1996 4 12 AALA960353 1 19960304 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7375A 25202 SFO - DURING OVERNIGHT CHECK, EMREGENCY EXIT LIGHTS AT PASSENGER SEAT 20B FOUND INOPERATIVE. REPAIRED BROKEN EMERGENCY EXIT LIGHT WIRE AT PASSENBER SEAT 20B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1996041200111 19960412 00111 WP 1996 4 12 AALA960372 1 19960306 A 3260 833703 UPLOCK SENSOR ELDEC DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA O OTHER N FALSE WARNING CL CLIMB 1 SW 07 426AA 49338 DFW - FLT 1351 - AFTER TAKEOFF IAD AND LANDING GEAR RETRACTED, RED NLG LIGHT ILLUMINATED FOR APPROXIMATELY 1 MINUTE AND THEN EXTINGUISHED WITH NO OTHER ABNORMAL INDICATIONS. AIRCRAFT PROCEEDED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED NLG UPLOCK SENSOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. 2 L 7 2 4F A6WE 1996041200112 19960412 00112 NM 1996 4 12 AALA960373 1 19960306 A 3320 OVERHEAD LIGHT BOEING 767 767323 1385205 NM MID LAVATORY DAMAGED A AALA K NONE A FLAME/FIRE IN INSP/MAINT 1 SW 07 359AA 24040 SFO - DURING OVERNIGHT CHECK, EVIDENCE OF PREVIOUS MINOR FIRE AT MID-RIGHT LAVATORY FROM PAPER TOWEL FOUND AROUND OVERHE AD LIGHT FIXTURE. REMOVED PAPER TOWEL AND CLEANED RESIDUE. NO ASSOCIATED DAMAGE FOUND AND SYSTEM GROUND CHECKED, NORMA L OPERATION. (X) 2 L 7 2 4F RT A1NM 1996041200113 19960412 00113 NM 1996 4 12 AALA960374 1 19960307 A 3350 1722331 CONNECTOR BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 388AA 27448 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 33B FOUND INOPERATIVE. REPLACED EMERGENCY EXIT LIG HT CONNECTOR AT PASSENGER SEAT 33B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1996041200114 19960412 00114 NE 1996 4 12 AALA960375 2 19960307 A 7250 798403 TURBINE BLADES DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE NR 2 ENG FAILED A AALA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 SW 07 73444 49470 718479 ORD - FLT 1853 - EN ROUTE ROC/ORD - DURING CRUISE, LOUD BANG FOLLOWED BY LOSS OF POWER FROM NR 2 ENGINE AND NO EPR OR N1 INDICATIONS. ACCOMPLISHED SHUTDOWN OF NR 2 ENGINE AND AIRCRAFT PROCEEDED SINGLE ENGINE TO ORD, LANDING WITHOUT INCIDEN T. REPLACED NR 2 ENGINE AND ACCOMPLISHED LEAK AND GROUND ENGINE RUN CHECKS WITH NO DEFECTS FOUND. ENGINE SHUTDOWN WAS THE RESULT OF 3RD AND 4TH STAGE TURBINE FAILURE. ALL 3RD AND 4TH STAGE TURBINE BLADES WERE BROKEN AT OR NEAR THE AIRFOI L ROOT. NO DEFINITIVE CAUSE OF FAILURE HAS BEEN DETERMINED. ENGINE ROUTED TO SHOP FOR REPAIR AND RETURN TO SERVICE. ( M) 2 L 7 2 4F 4 F A6WE E9NE 1996041200115 19960412 00115 EU 1996 4 12 AALA960383 1 19960306 A 3246 42687 BEARING FOKKER F28 F28MK0100 4990807 EU NR 2 WHEEL FAILED A A AALA O OTHER D INFLIGHT SEPARATION LD LANDING 1 SW 07 1455K 11467 DFW - FLT 0372 - DURING LANDING ROLL-OUT, NR 2 WHEEL ASSY DEPARTED AIRCRAFT. AIRCRAFT COMPLETED ROLL-OUT AND TAXI TO GA TE WITHOUT INCIDENT. REPLACED LT MLG STRUT INNER CYLINDER, NR 1 AND NR 2 BRAKE ASSYS AND NR 1 AND NR 2 WHEEL/TIRE ASSYS . SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT 1996041200116 19960412 00116 WP 1996 4 12 AALA960385 1 19960309 A 3350 LIGHT STRIP DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7544A 53026 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FIRST CLASS CABIN FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR L IGHT STRIP IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. 2 L 7 2 4F A6WE 1996041200117 19960412 00117 NM 1996 4 12 AALA960386 1 19960309 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7375A 25202 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT ON PASSENGER SEAT 23B FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY E XIT LIGHT CONNECTOR AT PASSENGER SEAT 23B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1996041200118 19960412 00118 WP 1996 4 12 CAL960287 1 19960308 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14810 49264 LAX - INSPECTION FOUND EMERGENCY TRACK LIGHTS IN AFT CABIN DIM. THE BATTERY PACK WAS REPLACED AND OPERATION OF THE EMER GENCY TRACK LIGHTING WAS RESTORED. (X) 2 L 7 2 4F A6WE 1996041200119 19960412 00119 WP 1996 4 12 CAL960305 1 19960312 A 2410 696233B CSD SPLINES DOUG DC9 DC982 3022082 WP NR 1 POSITION DAMAGED A CALA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 SW 09 76823 13004 12690 49483 MSY - FLT 1783 - THE LT GENERATOR TRIPPED OFF WHILE EN ROUTE FROM DCA TO IAH. ACFT DESCENDED TO FL 240 AND CREW MADE AN UNSUCCESSFUL ATTEMPT TO START APU. AT THAT TIME, DC EMERGENCY BUS C/B POPPED AND CAPT'S INSTRUMENTS WENT OFF. CIRCUIT BREAKER WAS NOT RESET. ACFT DIVERTED TO MSY WHERE IT LANDED WITHOUT INCIDENT. WHEN MAINTENANCE WAS REMOVING LT GENERA TOR, NR 1 CSD SHAFT SPLINES FOUND DAMAGED. THE NR 1 CSD, NR 1 GENERATOR, AND CSD OIL COOLER WERE REMOVED AND REPLACED. THE NR 1 GENERATING SYSTEM OPERATED NORMALLY. IN ADDITION, APU WAS STARTED AND CHECKED GOOD WITH NO TROUBLE FOUND. (X ) 2 L 7 2 4F A6WE 1996041200120 19960412 00120 1996 4 12 CAL960326 4 19960316 A 3460 4034241904 DFG COMPUTER DOUG DC9 DC981 3022081 WP EQUIP INSTAL INOPERATIVE A CALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SW 09 14880 11154 48044 EWR - FLT 0554 - THE LANDING GEAR AURAL WARNING SOUNDED ON FINAL APPROACH TO DWR WITH 3 GREEN LANDING GEAR LIGHTS INDICA TED. CHECK LIST PROCEDURES WERE C/W DURING A 'GO-AROUND' AND THE GEAR WAS VISUALLY CONFIRMED DOWN AND LOCKED. ACFT LAN DED WITHOUT INCIDENT. THE PROXIMITY UNIT, GEAR/FLAP SWITCHES, AND CAWS FUNCTION ALL TESTED GOOD. INSP OF CAWS/GPWS AT COCKPIT WAS GOOD. R2-295 LG LEVER RELAY FOUND BAD. RELAY REMOVED AND REPLACED. MAINTENANCE FOUND 'NO AUTOLAND' ON NR 2 DFGC DURING SENSORS/SWITCHES TROUBLESHOOTING. UNIT FAILED RETURN TO SERVICE TEST. NR 2 DFGC REMOVED AND REPLACED. U NIT PASSED RTS TEST PER MM 22-01-01. (X) 2 L 7 2 4F A6WE 1996041200121 19960412 00121 WP 1996 4 12 CAL960335 1 19960318 A 3020 ANTIICE DUCT DOUG DC9 DC982 3022082 WP RT ENGINE BLOWN A CALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 57837 49582 OCA - FLT 0611 - THE NR 2 ENGINE HAD A FIRE WARNING SHORTLY AFTER TAKEOFF FROM DCA. ACFT WAS RETURNED TO DCA WHERE IT L ANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE NOSE COWL ANTI-ICE DUCT BLOWN. THE ANTI-ICE DUCT WAS REPLACE D. LEAK AND OPERATIONAL CHECKS WERE GOOD. (X) 2 L 7 2 4F A6WE 1996041200122 19960412 00122 NM 1996 4 12 CAL960339 1 19960308 A 5230 SKIN BOEING 737 737130 1384435 NM CARGO DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14209 65656 19026 GSO - THE FORWARD LOWER CORNER OF FORWARD CARGO DOOR SKIN FOUND DENTED AND SCRATCHED. THE DAMAGED SKIN REMOVED OVER AN AREA OF APPROXIMATELY 6 INCHES IN DIAMETER IAW SRM 52-00-3, FIGURE 3. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SR M 52-00-3, FIGURE 3, SRM 51-10-2, AND SRM 51-30-2. (X) 2 L 7 2 4F A16WE 1996041200123 19960412 00123 NM 1996 4 12 CAL960340 1 19960305 A 5320 INTERCOSTAL BOEING 737 737130 1384435 NM FS 870-887 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14209 65656 19026 GSO - INSPECTION FOUND INTERCOSTAL CORRODED IN AFT CARGO COMPARTMENT AT FS 870 - FS 887, STR 20R TO STR 21R. THE INTERC OSTAL WAS REMOVED IAW SRM 51-30-2, A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 53-10-2. A DOUBLER WAS FABRIC ATED AND INSTALLED IAW SRM 51-40-2. (X) 2 L 7 2 4F A16WE 1996041200124 19960412 00124 NM 1996 4 12 CAL960341 1 19960301 A 5320 PANEL BOEING 737 737130 1384435 NM NLG WW CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14209 65656 19026 GSO - INSPECTION FOUND NOSE WHEELWELL UPPER FORWARD PANEL CORRODED. THE PANEL WAS REPAIRED IAW E.A. 5310-02452. (X) 2 L 7 2 4F A16WE 1996041200125 19960412 00125 NM 1996 4 12 CAL960342 1 19960308 A 5755 SPOILER BOEING 737 737130 1384435 NM NR 3 POSITION BULGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14209 65656 19026 GSO - INSPECTION FOUND THE NR 3 SPOILER UPPER SURFACE BULGED. THE SPOILER SKIN WAS RETURNED TO ORIGINAL CONTOUR BY FORM ING IAW SRM 51-40-1. (X) 2 L 7 2 4F A16WE 1996041200126 19960412 00126 NM 1996 4 12 CAL960343 1 19960221 A 5330 SKIN BOEING 737 737130 1384435 NM BS 188-251 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14209 65656 19026 GSO - INSPECTION FOUND CRACKS AROUND FASTENERS IN LT EXTERNAL SKIN AT BS 188 TO BS 251, WL 207 THROUGH WL 234. THE CRAC K LENGTHS WERE NOT IDENTIFIED, BUT THE REPAIRED AREAS WERE LESS THAN 6 INCHES IN DIAMETER. THE CRACKS WERE CUT OUT. RE PAIR DOUBLERS AND FILLERS WERE FABRICATED AND INSTALLED IAW E.A. 53-10-01188. (X) 2 L 7 2 4F A16WE 1996041200127 19960412 00127 NM 1996 4 12 CAL960344 1 19960218 A 5311 FRAME BOEING 737 737130 1384435 NM BS 400 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14209 65656 19026 GSO - INSPECTION FOUND A DENT AND .50 INCH CRACK IN FORWARD PIT BELT FRAME AT STA 400, STR 23L TO STR 25L. THE FRAME WA S REPAIRED BY FABRICATING AND INSTALLING ANGLE, DOUBLER, AND FILLER IAW SRM 51-40-3. (X) 2 L 7 2 4F A16WE 1996041200128 19960412 00128 NM 1996 4 12 CAL960345 1 19960305 A 5315 FLOOR BEAM BOEING 737 737130 1384435 NM BS 328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14209 65656 19026 GSO - INSPECTION FOUND FLOOR BEAM UPPER CAP CORRODED AT STA 328, RBL 45 TO RBL 65. THE FLOOR BEAM UPPER CAP WAS REMOVED IAW SRM 53-10-9. A NEW CAP AND SPLICE ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-10-9 AND SRM 51-30-0. (X) 2 L 7 2 4F A16WE 1996041200129 19960412 00129 NM 1996 4 12 CAL960347 1 19960305 A 5320 SHEAR TIE BOEING 737 737130 1384435 NM BS 440 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14209 65656 19026 GSO - INSPECTION FOUND A .50 INCH CRACK IN SHEAR TIE AT STA 440, BL ZERO. THE CRACKED SECTION SHEAR TIE WAS CUT OFF IAW SRM 53-10-4. AN ANGLE AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-4 AND SRM 51-30-2. (X) 2 L 7 2 4F A16WE 1996041200130 19960412 00130 NM 1996 4 12 CAL960348 1 19960305 A 5311 FRAME BOEING 737 737130 1384435 NM BS 440 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14209 65656 19026 GSO - INSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 440 ABOVE STR 21L. A NEW FRAME AND CLIP WERE FABRICATED AND INSTA LLED IAW BOEING DRAWING 65C25113 AND SRM 51-10-2. (X) 2 L 7 2 4F A16WE 1996041200131 19960412 00131 NM 1996 4 12 CAL960349 1 19960229 A 5311 FRAME BOEING 737 737130 1384435 NM BS 460 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14209 65656 19026 GSO - INSPECTION FOUND LEFT LOWER FRAME IN FORWARD PIT, STA 460, CRACKED AT NUTPLATES FOR CARGO LINER. THE CRACK LENGTH S WERE NOT IDENTIFIED. THE FRAME WAS REPAIRED IAW E.A. 5310-01211. (X) 2 L 7 2 4F A16WE 1996041200132 19960412 00132 NM 1996 4 12 CAL960350 1 19960312 A 5754 SLAT BOEING 737 737130 1384435 NM NR 5 POSITION DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14209 65656 19026 GSO - INSPECTION FOUND THE OUTBOARD END OF NR 5 SLAT TOP SURFACE DELAMINATED IN AN AREA APPROXIMATELY 10 INCHES SQUARE. THE DELAMINATED SKIN AND CORE WERE REMOVED. THE AREA WAS REPAIRED BY REPLACING CORE AND APPLYING WET FIBERGLASS OVERLA YS IAW SRM 51-40-6. (X) 2 L 7 2 4F A16WE 1996041200133 19960412 00133 NM 1996 4 12 CAL960351 1 19960312 A 5330 SKIN BOEING 737 737130 1384435 NM BS 767-804 BUCKLED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14209 65656 19026 GSO - INSPECTION FOUND FUSELAGE SKIN LAP BUCKLED AND A .25 INCH CRACK IN STR 20L, STA 767 TO STA 804. THE EFFECTED SECT ION OF SKIN AND STRINGER WERE REMOVED. A SKIN AND STRINGER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 13, SRM 53-10-3, FIGURE 1, AND SRM 51-30-2. (X) 2 L 7 2 4F A16WE 1996041200134 19960412 00134 NM 1996 4 12 CAL960352 1 19960226 A 2761 65671956 ACT FITTING BOEING 737 737130 1384435 NM NR 5 SPOILER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14209 65656 19026 GSO - INSPECTION FOUND A 1 INCH CRACK AT ROD ATTACH POINT OF NR 5 SPOILER INBOARD ACTUATOR FITTING. THE FITTING WAS REM OVED AND REPLACED IAW SRM 51-30-2. (X) 2 L 7 2 4F A16WE 1996041200135 19960412 00135 NM 1996 4 12 CAL960353 1 19960313 A 5752 TAB HINGE FTG BOEING 737 737130 1384435 NM NR 3 AILERON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14209 65656 19026 GSO - INSPECTION FOUND LT WING NR 3 AILERON HINGE FITTING CRACKED AT TAB ATTACH POINT. THE CRACK LENGTH WAS NOT IDENTIF IED. THE HINGE ASSY WAS REMOVED AND REPLACED IAW SRM 51-30-2. (X) 2 L 7 2 4F A16WE 1996041200136 19960412 00136 NM 1996 4 12 CAL960354 1 19960306 A 5753 6546430101 SKIN BOEING 737 737130 1384435 NM LT TE FOREFLAP GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14209 65656 19026 GSO - INSPECTION FOUND A GOUGE APPROXIMATELY 10 INCHES SQUARE IN TOP SURFACE OF LT WING INBOARD FOREFLAP. REMOVED GOUGE D AREA AND POTTED CORE. REPAIRED WITH FIBERGLASS OVERLAYS IAW SRM 51-40-9. (X) 2 L 7 2 4F A16WE 1996041200137 19960412 00137 NM 1996 4 12 CAL960355 1 19960306 A 5755 654645165SP SKIN BOEING 737 737130 1384435 NM NR 2 SPOILER DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14209 65656 19026 GSO - INSPECTION FOUND NR 2 SPOILER SKIN INBOARD LOWER SURFACE DELAMINATED OVER AN AREA OF APPROXIMATELY 10 INCHES BY 8 INCHES. THE DELAMINATED AREA WAS REMOVED AND FIBERGLASS OVERLAYS WERE APPLIED IAW SRM 57-50-5. (X) 2 L 7 2 4F A16WE 1996041200138 19960412 00138 NM 1996 4 12 CAL960356 1 19960308 A 5320 WEB BOEING 737 737130 1384435 NM FWD TORQUE BOX CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14209 65656 19026 GSO - INSPECTION FOUND A 1 INCH CRACK IN WEB SECTION AT FORWARD R-2 TORQUE BOX UPPER HINGE ARM. THE CRACK WAS CUT OUT I AW SRM 51-40-2. A NEW WEB WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND BOEING DRAWING 65-46561. (X) 2 L 7 2 4F A16WE 1996041200139 19960412 00139 NM 1996 4 12 CAL960357 1 19960229 A 5313 BAC1498139 STRINGER BOEING 737 737130 1384435 NM BS 360-440 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14209 65656 19026 GSO - INSPECTION FOUND TWO EACH .25 INCH CRACKS AT FASTENER HOLES OF STR 23R, STA 360 TO STA 440. THE STRINGER WAS REMO VED AND REPLACED IAW SRM 51-30-2. (X) 2 L 7 2 4F A16WE 1996041200140 19960412 00140 NM 1996 4 12 CAL960358 1 19960308 A 5330 SKIN BOEING 737 737130 1384435 NM R-2 DOORWAY CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14209 65656 19026 GSO - INSPECTION FOUND A 1 INCH CRACK IN SKIN AT FORWARD LOWER CORNER OF R-2 DOORWAY CUT-OUT. THE CRACK WAS CUT OUT. A DOUBLER, TRIPLER, AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. (X) 2 L 7 2 4F A16WE 1996041200141 19960412 00141 NM 1996 4 12 CAL960359 1 19960308 A 5320 DOOR FRAME BOEING 737 737130 1384435 NM R2 DOORWAY CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14209 65656 19026 GSO - INSPECTION FOUND A 1.25 INCH CRACK IN UPPER SECTION OF FORWARD R-2 DOORWAY FRAME AT STR 10R. THE FRAME SEGMENT WA S REMOVED AND REPLACED IAW SRM 51-30-2 AND BOEING DRAWING 65-46561. (X) 2 L 7 2 4F A16WE 1996041200142 19960412 00142 NM 1996 4 12 CAL960360 1 19960217 A 5713 STRINGER BOEING 737 737130 1384435 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14209 65656 19026 GSO - INSPECTION FOUND A .50 INCH CRACK IN RT WING STR 13 AT WBL 92.5. REPAIR ANGLES AND SPLICES WERE FABRICATED AND IN STALLED IAW BOEING DRAWING 65C34533 AFTER STOP DRILLING CRACK. (X) 2 L 7 2 4F A16WE 1996041200143 19960412 00143 NM 1996 4 12 CAL960361 1 19960226 A 5313 BAC1498139 STRINGER BOEING 737 737130 1384435 NM BS 478 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14209 65656 19026 GSO - INSPECTION FOUND STR 24R IN FORWARD PIT CORRODED AT STA 478. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 51-30- 2 AND BOEING DRAWING 65-45768. (X) 2 L 7 2 4F A16WE 1996041200144 19960412 00144 NM 1996 4 12 CAL960362 1 19960305 A 5320 WEB BOEING 737 737130 1384435 NM E/E COMPARTMENT GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14209 65656 19026 GSO - INSPECTION FOUND A 1 INCH LONG GOUGE IN WEB OF E AND E COMPARTMENT AT LT SIDE OF DOORWAY CUT-OUT. THE WEB WAS REM OVED. A NEW WEB WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND SRM 51-30-2. (X) 2 L 7 2 4F A16WE 1996041200145 19960412 00145 NM 1996 4 12 CAL960363 1 19960217 A 5330 SKIN BOEING 737 737130 1384435 NM BS 295-340 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14209 65656 19026 GSO - INSPECTION FOUND SKIN CORRODED AT STA 295 TO STA 340, STR 18R TO STR 19R. THE CORRODED SKIN WAS REMOVED. A DOUBL ER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. (X) 2 L 7 2 4F A16WE 1996041200146 19960412 00146 NM 1996 4 12 CAL960364 1 19960229 A 5315 FLOOR BEAM BOEING 737 737130 1384435 NM COCKPIT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14209 65656 19026 GSO - INSPECTION FOUND FLOOR BEAM AND WEB CORRODED IN COCKPIT UNDER CAPTAIN'S SEAT. THE AREA WAS REPAIRED IAW SRM 51-40 -2 AND ECRA 5310-03239. (X) 2 L 7 2 4F A16WE 1996041200147 19960412 00147 NM 1996 4 12 CAL960365 1 19960229 A 5311 FRAME BOEING 737 737130 1384435 NM BS 480 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14209 65656 19026 GSO - INSPECTION FOUND THE LT LOWER FRAME IN FORWARD PIT STA 480 CRACKED TWO PLACES AT NUTPLATE LOCATIONS FOR CARGO LINE R. THE CRACK LENGTHS WERE NOT IDENTIFIED. THE FRAME WAS REPAIRED IAW E.A. 5310-01211. (X) 2 L 7 2 4F A16WE 1996041200148 19960412 00148 NM 1996 4 12 CAL960366 1 19960308 A 5330 SKIN BOEING 737 737130 1384435 NM E/E DOOR CUTOUT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14209 65656 19026 GSO - INSPECTION FOUND SKIN AND CHORD CORROSION AT FORWARD RT CORNER OF E AND E BAY DOORWAY CUT-OUT. THE CORRODED SECTI ON OF SKIN AND CHORD WERE REMOVED IAW SRM 51-30-2 AND SRM 53-30-3. NEW SKIN AND TEE SECTIONS WERE FABRICATED AND INSTAL LED IAW SRM 53-30-3 AND ECRA 53-10-01233. (X) 2 L 7 2 4F A16WE 1996041200149 19960412 00149 NM 1996 4 12 CAL960367 1 19960305 A 5330 SKIN BOEING 737 737130 1384435 NM E/E DOOR CUTOUT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14209 65656 19026 GSO - INSPECTION FOUND SKIN CORROSION AT FORWARD LT CORNER OF E AND E BAY DOORWAY CUT-OUT. THE CORROSION WAS REMOVED AN D A T-CHORD SECTION WAS CUT OUT IAW SRM 51-10-6. A REPAIR STRAP AND NEW T-CHORD WERE FABRICATED AND INSTALLED IAW ECRA 5310-01233. (X) 2 L 7 2 4F A16WE 1996041200150 19960412 00150 NM 1996 4 12 CAL960368 1 19960313 A 5320 ANGLE BOEING 737 737130 1384435 NM LT SLIDING WNDW CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14209 65656 19026 GSO - INSPECTION FOUND SUPPORT ANGLE CORRODED AT LT SLIDING WINDOW, STA 248.7. THE CORRODED SECTION OF ANGLE WAS CUT OU T IAW SRM 51-40-4. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-40-4, AND SRM 51-30-2. (X) 2 L 7 2 4F A16WE 1996041200151 19960412 00151 NM 1996 4 12 CAL960369 1 19960216 A 5320 BEAR STRAP BOEING 737 737130 1384435 NM C1 DOOR CUTOUT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14209 65656 19026 GSO - INSPECTION FOUND A .3750 INCH CRACK IN BEAR STRAP AT C-1 DOOR CUT-OUT, LOWER AFT CORNER. THE SKIN WAS REPLACED AN D A DOUBLER INSTALLED IAW ECRA 5330-02366. (X) 2 L 7 2 4F A16WE 1996041200152 19960412 00152 NM 1996 4 12 CAL960370 1 19960315 A 3350 LIGHT BOEING 737 737130 1384435 NM LT OVERWING INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14209 19026 GSO - INSPECTION FOUND LT OVERWING EMERGENCY LIGHT INOPERATIVE. THE LT OVERWING EMERGENCY LIGHT ASSY REMOVED AND REPLAC ED. (X) 2 L 7 2 4F A16WE 1996041200153 19960412 00153 NM 1996 4 12 CAL960372 1 19960319 A 4990 38042814 APU BOEING 737 7373T0 1384582 NM A/C TAIL LOW ON OIL A CALA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SW 09 14320 25222 3676 23371 ATL - FLT 1424 - WHILE OPERATING THE APU WITH THE NR 1 GENERATOR PLACARDED INOPERATIVE, THE APU FAILED ON TAKEOFF AND CO ULD NOT BE RESET. THE ACFT WAS RETURNED TO ATL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE APU LOW ON OIL. THE APU OIL LEVEL WAS SERVICED TO FULL AND THE APU WAS RESET. OPERATIONAL CHECKS WERE GOOD. IN ADDITION, THE NR 1 CS D OIL LEVEL WAS CHECKED AND FOUND GOOD. THE CSD WAS RESET. THE ENGINE WAS RUN AND THE GENERATOR CAME ON-LINE. VOLTAGE AND FREQUENCIES CHECKED GOOD AND THE GENERATOR PLACARD WAS REMOVED. 2 L 7 2 4F RT A16WE 1996041200154 19960412 00154 NM 1996 4 12 CKSA96012 1 19960202 A 5320 65198613 ANGLE BOEING 727 727223 1384074 NM NLG WW CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6807 73431 19482 OSC - DURING 'C-4' CHECK INSPECTION FOUND CORRODED ANGLE LT SIDE LOWER INBOARD CORNER OF TUNNEL AREA BELOW NLG TRUNNION. REMOVED AND REPLACED T-C BOARD ANGLE IAW 51-10-1, 51-30-2, PN 65-19861-3. (X) 2 L 7 3 4F A3WE 1996041200155 19960412 00155 NM 1996 4 12 CKSA96013 1 19960202 A 5753 BMS65413015 FITTING BOEING 727 727223 1384074 NM RT NR 5 FLAP CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6807 73431 19482 OSC - DURING 'C-4' CHECK INSPECTION FOUND RT NR 5 FLAP TRACK INBOARD RETAINER BOLT BARREL NUT SUPPORT BRACKET CRACKED FO RWARD AUXILIARY SPAR. REMOVED AND REPLACED FITTING IAW 727 SRM 51-10-1 AND SRM 51-30-2. FABRICATED PER BOEING DRAWING 65-41301 AND 8110-3, SO-982. (X) 2 L 7 3 4F A3WE 1996041200156 19960412 00156 WP 1996 4 12 CKSA96014 1 19960206 A 3260 SWITCH DOUG DC8 DC851 3021920 WP RT MLG LOOSE WIRE A CKSA O OTHER P NO WARNING INDICATION DE DESCENT 1 GL 23 804CK 53152 45689 KDFW - FLT 71799 - NO GREEN LIGHT ON RT MAIN GEAR ON APPROACH (NO RED LIGHTS ALSO). CYCLED GEAR ONCE, 3 GREEN. FOUND L OOSE CONNECTION AT LANDING GEAR CONTROL LEVER LIMIT SWITCH. RESECURED WIRE AND CLEANED SWITCH, SWITCH OPS CHECKS NORMAL MM 32-7-6. (X) 2 L 7 4 4F 4A25 1996041200157 19960412 00157 WP 1996 4 12 CKSA96020 1 19960229 A 2612 WIRE DOUG DC8 DC8F55 3021928 WP NR 1 ENGINE BROKEN A CKSA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 GL 23 6161C 56838 45856 SBGR - FLT 9999 - ON CLIMB-OUT FROM SBGR, NR 1 ENGINE FIRE WARNING CAME ON, PERFORMED FIRE WARNING SHUT-DOWN. AT TIME O F FIRE WARNING, NR 1 ENGINE PARAMETERS WERE NORMAL. ENGINE WAS SHUT DOWN AT 1630Z, OIL PRESSURE WAS MAINTAINED AT 30 PS I, N1 26 PERCENT, N2 40 PERCENT. REPAIRED BROKEN WIRE AT FIRE LOOP CANNON PLUG. OPS CHECKED NORMAL ON RUN IAW 24-10. ( X) 2 L 7 4 4F 4A25 1996041200158 19960412 00158 NM 1996 4 12 DALR960001 1 19960201 A 5320 6518745223 WEB BOEING 727 727223 1384074 NM BS 870 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 710AA 22467 ATL - DURING HEAVY C-CHECK, THE LT MLG WHEELWELL PRESSURE DECK WAS FOUND WITH SEVERAL CRACKS AT THE FWD INBOARD CORNER O F THE WEB BEADS AT BS 870, LBL 4. ACCOMPLISHED REPAIRS PER DL ERA 303046-14, REV A. REF SB 727-53-0149. REFERENCE OPE RATOR CONTROL NR AALA960338. AIRCRAFT TT: 39,376 HRS. AIRCRAFT TC: 21,692. (X) 2 L 7 3 4F A3WE 1996041200159 19960412 00159 NM 1996 4 12 DALR960002 1 19960112 A 5314 6518363156 KEEL BEAM BOEING 727 727223 1384074 NM FS 873 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 710AA 22467 ATL - DURING CONTRACT MAINTENANCE AT DALA FOR HEAVY C-CHECK, THE RT AND LT SIDES OF THE KEEL BEAM JUST AFT OF STA 873 WE RE FOUND CRACKED. THE CRACK IN THE LT BEAM RESULTED IN THE REMOVAL OF A 0.750 INCH LONG BY 0.380 INCH WIDE BY 0.195 INC H DEEP SECTION OF THE CHORD BELOW THE CRACKED FLANGE. THE CRACKS WERE CONFINED TO THE UPPER FLANGE OF THE CHORD ONLY AN D WERE REPAIRED PER 727 SB 727-53-0208, REF DL ERA 303000-14. REFERENCE OPERATOR CONTROL NR AALA960339. AIRCRAFT TT: 3 9,376 HRS. AIRCRAFT TC: 21,692. (X) 2 L 7 3 4F A3WE 1996041200160 19960412 00160 NM 1996 4 12 96FDEA00738 1 19960405 A 5313 BAC1408146 STRINGER BOEING 727 72725 1384006 NM BS 1055 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 CORROSION (C53-113-01, 2) FOUND WHILE WORKING NR0602 STA 1055 STRINGER 28R IN STRINGER. FOUND CORROSION TO BE OUT OF LI MITS PER FEDEX SRM 53-10-1, REMOVED DAMAGED AREA, REPAIRED STR 28R IAW FEDEX SRM 53-10-3. 2 L 7 3 4F A3WE 1996041200161 19960412 00161 NM 1996 4 12 96FDEA00739 1 19960405 A 5315 BOC1505100617 FLOOR BEAM BOEING 727 72725 1384006 NM BS 380 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 CORROSION (C53-224-01) ON FLOOR BEAM BS 380, LBL 28 TO 34 AND LBL 55 WL 208. REMOVED CORROSION FROM FLOOR BEAM FOUND TO BE OUT OF LIMITS. ACCOMPLISHED FLOOR BEAM REPAIR PER FEDEX SRM 53-10-8. 2 L 7 3 4F A3WE 1996041200162 19960412 00162 NM 1996 4 12 96FDEA00740 1 19960405 A 5315 FLOOR BEAM BOEING 727 72725 1384006 NM BS 344 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 CORROSION (C53-224-01) ON FLOOR BEAM BS 344 LBL 45 AND RBL 37 WL 208. ACCOMPLISHED FLOOR BEAM REPAIR AT BS 344 LBL 45 A ND RBL 37 WL 208, PER FEDEX SRM 27-53-007. 2 L 7 3 4F A3WE 1996041200163 19960412 00163 NM 1996 4 12 96FDEA00741 1 19960405 A 5315 FLOOR BEAM BOEING 727 72725 1384006 NM BS 1110 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 CORROSION (C53-224-01) ON LOWER SURFACE OF UPPER FLANGE OF FLOOR BEAM AROUND FASTENER HOLES BS 1110, RBL 10 TO 60 WL 208 . REMOVED CORROSION FROM FLOOR BEAM, FOUND TO BE OUT OF LIMITS. ACCOMPLISHED FLOOR BEAM REPAIR BS 1110, RBL 10 TO 60 W L 208, IAW FEDEX SRM 53-10-1, 53-10-8. 2 L 7 3 4F A3WE 1996041200164 19960412 00164 NM 1996 4 12 96FDEA00742 1 19960405 A 5330 SKIN BOEING 727 72725 1384006 NM BS 307 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 WHILE WORKING NR0152, FOUND THE FUSELAGE SKIN TO BE GOUGED AT BS 307 RBL 63 WL 249, ADJACENT TO THE FORWARD ENTRY DOOR F USELAGE TORQUE TUBE. REMOVED DAMAGED AREA, REPAIRED SKIN IAW FEDEX SRM 53-30-3. 2 L 7 3 4F A3WE 1996041200165 19960412 00165 EU 1996 4 12 96UAL900237 1 19960404 A 3260 DOOR SENSOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LANDING GEAR MALFUNCTIONED A UALA O OTHER N FALSE WARNING DE DESCENT 1 WP 29 403UA 442 CREW REPORTED, AT THE OUTER MARKER THE GEAR WAS SELECTED DOWN AND THE INDICATIONS REMAINED RED. THE GEAR WAS RECYCLED A ND OPERATED NORMALLY. *S/D* ACCOMPLISHED CHECK OF DOOR SENSORS AND WIRING. SWUNG GEAR SEVERAL TIMES AND COULD NOT DUP LICATE PROBLEM. SYSTEM OPERATIONALLY CHECKED GOOD WITH NO FURTHER PROBLEMS. 2 L 7 2 4F 4 F RT A28NM E40NE 1996041200166 19960412 00166 WP 1996 4 12 ABXA9600447 1 19960405 A 3260 MS25231313 BULB DOUG DC8 DC863 302198A WP LT MLG FAILED A ABXA O OTHER N FALSE WARNING DE DESCENT 1 GL 23 817AX 45928 AFTER GEAR EXTENSION, LEFT MAIN LANDING GEAR DID NOT INDICATE DOWN AND LOCKED. RECYCLED LANDING GEAR AND LEFT MAIN LAND ING GEAR INDICATED DOWN AND LOCKED. REPLACED BULB IN LANDING GEAR INDICATOR FOR THE LEFT MAIN LANDING GEAR DOWN LOCK PO SITION AND OPS CHECK GOOD. 2 L 7 4 4F 4A25 1996041200167 19960412 00167 NM 1996 4 12 DL72K960743 1 19960309 A 5312 BULKHEAD BOEING 727 727232 1384082 NM BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 491DA 21060 A .5 INCH CRACK WAS FOUND IN THE 1183 BULKHEAD AT LBL 8 AND WL 168 AS A RESULT OF INSPECTIONS PER SI 4-59275-12. ACCOMP LISHED REPAIRS PER DL ERA 303278-14AD. 2 L 7 3 4F A3WE 1996041200168 19960412 00168 NM 1996 4 12 DL72L960768 1 19960404 A 5320 VERTICAL WEB BOEING 727 727232 1384082 NM BS 1214 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 502DA 21304 FOUND DURING D-2 LETTER CHECK, TWO .5 INCH CRACKS IN LT LOWER TORQUE BOX VERTICAL WEB UPPER END, APPROX STA 1214. REPAI RED PER SRM 53-11-0. 2 L 7 3 4F A3WE 1996041200169 19960412 00169 NM 1996 4 12 DL72P960745 1 19960322 A 5753 SHIM BOEING 727 727225 1384077 NM RT TE FLAP TRACK MISALIGNMENT A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8889Z 21858 THE LAMINATED SHIM INSTALLED ON THE RIGHT WING INBOARD TRAILING EDGE FLAP INBOARD TRACK WAS FOUND TO HAVE MIGRATED GREAT ER THAN THE .25 LIMIT SPECIFIED IN THE INSPECTION. IN COMPLIANCE WITH AD 90-07-05, THE MIGRATED SHIM WILL BE RELOCATED AND ATTACHMENTS RETORQUED. INSPECTIONS PER SI 4-58662-12AD WILL BE CONTINUED. ACCOMPLISHED REPAIRS PER DL ERA 303342-1 4AD. 2 L 7 3 4F A3WE 1996041200170 19960412 00170 NM 1996 4 12 DL72S960732 1 19960401 A 5230 SF15614541 SEAL BOEING 727 727232 1384082 NM CARGO DOOR TORN A DALA B EMER. DESCENT O OTHER CR CRUISE 1 SO 27 416DA 21258 AT FLIGHT LEVEL 290 LOUD RUMBLE FOLLOWED BY RAPID RISE IN CABIN ALT. BOTH OUTFLOW VALVES CLOSED AND FLT LEVEL 220, CABI N STILL CLIMBING SLOWLY. DESCENDED TO 10,000 FT TO MAINTAIN PRESS. FOUND FWD CARGO DOOR SEAL DAMAGE AND OUT OF RETAINE R. REPLACED DOOR SEAL AND CABIN PRESS NORMAL. 2 L 7 3 4F A3WE 1996041200171 19960412 00171 NM 1996 4 12 DL72S960733 1 19960310 A 5522 657278420 SKIN BOEING 727 727232 1384082 NM RT ELEVATOR DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 515DA 21431 DURING INSPECTION, RT ELEVATOR WAS FOUND WITH T/E DAMAGED AT 27 TO 63 INCHES FROM THE O/B END. REPAIRED DAMAGED UPPER S KIN PER SRM 55-20-3 FIG 2. 2 L 7 3 4F A3WE 1996041200172 19960412 00172 NM 1996 4 12 DL72S960746 1 19960325 A 5210 50079452 SKIN BOEING 727 727232 1384082 NM L1 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 520DA 21471 THE L-1 PASSENGER DOOR WAS FOUND WITH TWO CRACKS IN THE UPPER FWD CORNER. THESE CRACKS RESULTED IN TWO CUT OUTS, 2 INCH BY 1.25 INCH AND 2.5 INCH BY 1.5 INCH, EIGHT INCHES APART. ONE DOUBLER REPAIR WILL BE USED FOR BOTH CRACKS. THE DOOR SKIN IS MADE FROM 0.045 CLAD 2024-T42. ACCOMPLISHED REPAIRS PER DL ERA 303353-14. 2 L 7 3 4F A3WE 1996041200173 19960412 00173 NM 1996 4 12 DL72S960753 1 19960402 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 1 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 419DA 21272 FOUND ON C-2 LETTER CHECK, NR 1 SLAT COVE SKIN ATTACH ANGLE CRACKED BELOW THE ANTI-ICE DUCT. REPAIRED PER M/M 57-54-0. 2 L 7 3 4F A3WE 1996041200174 19960412 00174 NM 1996 4 12 DL72S960754 1 19960402 A 5530 STRINGER BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 419DA 21272 FOUND ON C-2 LETTER CHECK, VERT STAB STRINGER CRACKED RT SIDE TAIL CRAWLWAY, FOURTH BAY UP. REPAIRED PER M/M 53-30-0. 2 L 7 3 4F A3WE 1996041200175 19960412 00175 NM 1996 4 12 DL72S960760 1 19960403 A 5320 WEB BOEING 727 727232 1384082 NM BS 1263 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 492DA 21061 FOUND ON A2 LETTER CHECK, .375 INCH CRACK IN LT TORQUE BOX WEB STA 1263. REPAIRED PER MM 53-11-0. 2 L 7 3 4F A3WE 1996041200176 19960412 00176 NM 1996 4 12 DL72S960775 1 19960403 A 5330 6525607126 SKIN BOEING 727 727232 1384082 NM BS 1183 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 520DA 21471 DURING THE ACCOMPLISHMENT OF THE AFT LAV SERVICE PANEL REWORK PER EO 4-69078-3AD, THE INTERNAL BONDED DOUBLER WAS FOUND CORRODED. ALSO, THE LOWER CORNER OF THE OVERLAPPING SKIN AT APPROX STA 1183 STR 20L HAS TOOLING DAMAGE ON THE SKIN. AC COMPLISHED REPAIRS PER DL ERA 303349-14 REV, B. 2 L 7 3 4F A3WE 1996041200177 19960412 00177 NM 1996 4 12 DL72W960737 1 19960401 A 5330 SKIN BOEING 727 727247 138408F NM PNEU DOOR CUTOUT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 293WA 22111 FOUND ON A-2 LETTER CHECK, LOWER SKIN CRACKED .375 INCH AFT INBD CORNER OF PNEUMATIC GROUND AIR CONNECT DOOR CUTOUT. RE PAIRED PER MM 53-30-0. 2 L 7 3 4F A3WE 1996041200178 19960412 00178 NM 1996 4 12 DL72W960739 1 19960401 A 5210 SKIN BOEING 727 727247 138408F NM L 1 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 293WA 22111 FOUND ON A-2 LETTER CHECK, .25 INCH CRACK IN MAIN ENTRY DOOR OUTER DOOR SKIN AT UPPER HINGE CUTOUT LOWER AFT CORNER. RE PAIRED PER M/M 52-11-01. 2 L 7 3 4F A3WE 1996041200179 19960412 00179 NM 1996 4 12 DL72W960747 1 19960327 A 5330 65184203 SKIN BOEING 727 727247 138408F NM L 1 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2810W 20648 FUSELAGE SKIN AND UNDERLYING DOUBLER HAVE .25 INCH CRACK IN UPPER FWD CORNER OF L-1 DOOR CUTOUT. ACCOMPLISHED REPAIRS P ER DL ERS 303365-14AD. 2 L 7 3 4F A3WE 1996041200180 19960412 00180 NM 1996 4 12 DL72W960762 1 19960325 A 5400 S-DUCT BOEING 727 727247 138408F NM AFT FUS CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2810W 20648 FOUND ON MV1 CHECK, TIME LIMITED REPAIR INSTALLED, 1 INCH CRACK IN S-DUCT HOUSING LT SIDE JUST ABOVE AND AFT OF ACCESS P LATE 9523. REPAIRED PER M/M 54-30-0 PG 801 FIG 802, INSTALLED PERMANENT REPAIR. 2 L 7 3 4F A3WE 1996041200181 19960412 00181 NM 1996 4 12 DL72W960763 1 19960329 A 5210 FRAME BOEING 727 727247 138408F NM L 2 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2810W 20648 FOUND ON MV1 CHECK, L-2 DOOR FWD FRAME HAS .375 INCH CRACK AT UPPER HINGE CUTOUT. REPAIRED PER SRM 52-40-2 FIG 4. 2 L 7 3 4F A3WE 1996041200182 19960412 00182 NM 1996 4 12 DL72W960764 1 19960327 A 5240 SKIN BOEING 727 727247 138408F NM R2 SERVICE DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2810W 20648 FOUND ON MV1 CHECK, .375 INCH VISIBLE CRACK IN R-2 SERVICE DOOR AT UPPER FWD HINGE CUTOUT. REPAIRED PER SRM 52-40-2 FIG 4. 2 L 7 3 4F A3WE 1996041200183 19960412 00183 NM 1996 4 12 DL73E960741 1 19960329 A 5312 BULKHEAD WEB BOEING 737 7372J8 1384489 NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 235WA 22859 BULKHEAD 178 WAS FOUND CRACKED BENEATH THE VERTICAL STIFFENERS AT LBL 5.7 AND RBL 5.7. DAMAGE REMOVAL RESULTED IN CUT O UTS ON THE LT SIDE 3.5 AND 6 ABOVE WL 195, SAME FOR THE RT SIDE. THE WEB IS MANUFACTURED FROM 0.040 CLAD 2024-T3. ACCO MPLISHED REPAIRS PER DL ERA 303381-14. 2 L 7 2 4F RT A16WE 1996041200184 19960412 00184 NM 1996 4 12 DL73E960757 1 19960403 A 3244 MAIN TIRE B737400M BOEING 737 7372J8 1384489 NM NR 3 FAILED A DALA A UNSCHED LANDING K FLUID LOSS TO TAKEOFF 1 SO 27 235WA 4362 22859 SHORTLY AFTER TAKEOFF, A HYD SYS PRESS FAILED AND QTY WENT TO ZERO. ACCOMPLISHED CHECKLIST AND RETURNED FOR LANDING. A FTER LANDING FOUND NR 3 MAIN TIRE HAD COME APART AND DAMAGED 2 HYDRAULIC LINES. ALSO, TIRE DAMAGED RT WING AND I/B SPOI LER ABOVE RT MAIN GEAR. 2 L 7 2 4F RT A16WE 1996041200185 19960412 00185 NM 1996 4 12 DL73S960742 1 19960329 A 5330 SKIN BOEING 737 737232 1384475 NM R1 DOOR CUTOUT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 301DL 23073 A CRACK WAS FOUND IN THE LOWER AFT CORNER OF THE R-1 DOOR. THE SKIN PANEL AND THE BONDED DOUBLER AT THIS REGION WAS REP LACED. THERE WAS STILL A CRACK IN THE BEAR STRAP. THE CRACK IN THE BEAR STRAP WAS CUT OUT WHILE PERFORMING A REPAIR FO R THIS CORNER PER SRM 53-30-3, FIG 26. MTC SHORTENED THE NUMBER TWO PLATE, OMITTING 1 FASTENER LOCATION IN THE MIDDLE P LATE ONLY. THE OUTER PLATE IS 0.10 2024-T3 AND THE INNER PLATE IS 0.063 CLAD 2024-T3. ACCOMPLISHED REPAIRS PER DL ERA 303360-14. 2 L 7 2 4F RT A16WE 1996041200186 19960412 00186 NM 1996 4 12 DL73S960744 1 19960315 A 2761 65C2524216 ACTUATOR FITTING BOEING 737 737232 1384475 NM RT SPOILER FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 302DL 23047 ONE OF THE ACTUATOR FITTINGS HAS FAILED ON THE RT INBOARD GROUND SPOILER. THE FITTING IS THE SUBJECT OF S/B 737-57-1207 . ACCOMPLISHED REPAIRS PER DL ERA 357237-14. 2 L 7 2 4F RT A16WE 1996041200187 19960412 00187 NM 1996 4 12 DL757960735 1 19960401 A 3350 1317 BULB BOEING 757 757232 1384965 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 628DL 22918 EMERGENCY LIGHT ABOVE SEATS 34 D/E INOPERATIVE. RELAMPED, CHECKS NORMAL. 2 L 7 2 4F RT A2NM 1996041200188 19960412 00188 NM 1996 4 12 DL757960736 1 19960401 A 3350 BR9279108 SIGN BOEING 757 757232 1384965 NM L1/R1 DOOR DAMAGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 628DL 22918 L1 AND R1 EMERGENCY EXIT IDENTIFIER LAMP ASSEMBLIES DAMAGED. REPLACED SAME, CHECKS NORMAL. 2 L 7 2 4F RT A2NM 1996041200189 19960412 00189 NM 1996 4 12 DL757960761 1 19960213 A 5754 114N4004165A TE WEDGE BOEING 757 757232 1384965 NM NR 3 LE SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 642DL 23996 NR 3 SLAT T/E WEDGE DELAMINATED. REPLACED T/E WEDGE PER SRM 57-43-02. 2 L 7 2 4F RT A2NM 1996041200190 19960412 00190 NM 1996 4 12 DL757960769 1 19960403 A 5743 113N112811 BOLT BOEING 757 757232 1384965 NM LT MLG TRUNNION CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 606DL 22813 DURING LETTER CHECK INSPECTION, FOUND RUST AROUND NUTS FOR LT MAIN LANDING GEAR FORWARD TRUNNION BEARING SUPPORT LOWER B OLTS. REMOVED BOLTS AND FOUND RUSTY/PITTED. REPLACED BOLTS AND NUTS. 2 L 7 2 4F RT A2NM 1996041200191 19960412 00191 NM 1996 4 12 DL757960771 1 19960404 A 5743 113N11281 BOLT BOEING 757 757232 1384965 NM MLG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 611DL 22818 DURING LETTER CHECK INSPECTION, FOUND RUST AROUND NUTS FOR RT AND LT MLG FWD TRUNNION BEARING SUPPORT LOWER BOLTS. REMO VED BOLTS AND FOUND RUST AND PITTING. REPLACED BOLTS AND NUTS. 2 L 7 2 4F RT A2NM 1996041200192 19960412 00192 NM 1996 4 12 DL757960774 1 19960301 A 5330 SKIN BOEING 757 757232 1384965 NM FS 517 LIGHTNING STRIKE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 650DL 24390 A LIGHTNING STRIKE AT A FASTENER LOCATION DAMAGED THE UPPER SKIN AT THE STR 10R LAP JOINT. THE HOLE IS LOCATED AT STA 5 17 AND IS IN THE MIDDLE ROW OF FASTENERS IN THE LAP. THE DAMAGE HAS BEEN CUT OUT AND MEASURES .75 IN DIAMETER. ACCOMPL ISHED REPAIRS PER DL ERA 303248-14. 2 L 7 2 4F RT A2NM 1996041200193 19960412 00193 NM 1996 4 12 DL76L960749 1 19960320 A 5414 311T3450 SKIN BOEING 767 767332 1382001 NM NR 2 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 175DN 24803 TWO CRACK LOCATIONS HAVE BEEN REPORTED IN THE NR 2 ENGINE PYLON OUT'BD STRUT SKIN. THE CRACKS START FROM THE FWD TORQUE BOX ACCESS HOLE. A 1 INCH CRACK IS IN THE UPPER FWD CORNER AT NAC STA 158. SECOND CRACK IS IN THE UPPER AFT CORNER AT NAC STA 192 AND IS 2 INCHES LONG. BOTH CRACKS EXTEND THROUGH BOTH SHEETS OF 0.080 PLUS 0.080 2024-T3 BONDED SKIN ASSEM BLY. THE AFT CRACK TERMINATES IN AN EXISTING FASTENER HOLE. ACCOMPLISHED REPAIRS PER DL ERA 271951-14 REV, D. 2 L 7 2 4F RT A1NM 1996041200195 19960412 00195 WP 1996 4 12 DLL10960740 1 19960402 A 3350 5165741 BATTERY PACK LKHEED 1011 10113851 5265010 WP R 4 DOOR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 719DA 193C1135 EMERGENCY EXIT LIGHT AT R-4 DOOR IS INOP. REPLACED R4 DOOR BATTERY PACK, CHECK GOOD PER OPN. 2 L 7 3 4F A23WE 1996041200196 19960412 00196 WP 1996 4 12 DLL10960750 1 19960315 A 5330 1503140147 SKIN LKHEED 1011 10113851 5265010 WP BS 589 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 716DA 193C1095 THE FUESLAGE SKIN WAS FOUND BULGING ABOVE STRINGER 36 AT STA 589. A DYE-PENETRANT INSPECTION DETECTED A CRACK IN THE SK IN. FURTHER INVESTIGATION REVEALED THE PRESENCE OF CORROSION BETWEEN THE FUSELAGE OUTER SKIN AND THE FWD OUTFLOW VALVE CUTOUT, FINAL DIMENSION OF 6 FWD/AFT BY 5.5 CIRCUMFERENTIALLY. THE SKIN IS MADE FROM 0.068 THICK CLAD 2024-T3 SHEET AND THE INTERNAL DOUBLER IS MADE FROM 0.075 THICK CLAD 2024-T3 SHEET. ACCOMPLISHED REPAIRS PER DL ERA 273477-14 REV A. 2 L 7 3 4F A23WE 1996041200197 19960412 00197 WP 1996 4 12 DLL13960756 1 19960402 A 3230 IND LINE LKHEED 1011 10113851 5265010 WP HYD TEMP LINE LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 783DL 193A1009 AFTER TAKEOFF, SYSTEM C-HYD QTY INDICATOR DROPPED TO 1 QUARTER WITH QTY LIGHT AND HYD SYS ANNUNICATOR LIGHT. FOUND IND FITTING FOR TEMP LINE PULLED AWAY FROM HARD LINE. INSTALLED NEW FARREL AND SWEDGED. 2 L 7 3 4F A23WE 1996041200198 19960412 00198 WP 1996 4 12 DLL17960751 1 19960315 A 5711 1605415 REAR SPAR LKHEED 1011 10113853 5265020 WP WS 293-346 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 766DA 193H1207 CRACKS WERE FOUND EMANATING FROM EXISTING FASTENER HOLES BETWEEN IWS 293.58 AND IWS 346.109 ON THE LT AND RT WING. THE CRACKS WERE FOUND IN THE REAR SPAR UPPER CAP, WEB, UPPER WING SKIN. THE SUBJECT FASTENER HOLES WERE OVERSIZED TO REMOVE THE CRACKS IN THE DAMAGED MEMBERS ONLY WITH INSURANCE CUTS TAKEN. THE REAR SPAR UPPER CAP IS MADE FROM 7075-T76511 ALU MINUM EXTRUSION (LS12086). THE UPPER WING SKIN AT THE REAR SPAR LOCATION IS MANUFACTURED FROM 7075-T7651 PLATE. THE RE AR SPAR WEB IS MANUFACTURED FROM 7075-T651 BARE PLATE. ACCOMPLISHED REPAIRS PER DL ERA 27304-14 AD REV D. 2 L 7 3 4F A23WE 1996041200199 19960412 00199 NM 1996 4 12 DLM88960748 1 19960320 A 5330 5936021 SKIN DOUG MD88 MD88 3023688 NM BS 1271-1322 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DL 49537 FUSELAGE SKIN DAMAGED BETWEEN FS 1271 AND 1322 BETWEEN S24L AND 30L, DUE TO CONTACT WITH GROUND SUPPORT EQUIPMENT. STRI NGERS 25L, 26L AND 27L ARE DAMAGED AND NEW SECTIONS ARE SPLICED IN PER SRM REFERENCE DL ERA 273500-14 REV A. 2 L 7 2 4F RT A6WE 1996041200200 19960412 00200 NM 1996 4 12 DLM88960755 1 19960327 A 5321 SUB FLOOR DOUG MD88 MD88 3023688 NM BS 1300 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947DL 49878 LT SUBFLOOR IS CRACKED AT FS 1300. REMOVED OLD SUBFLOOR AT FS 1300, DRILLED UP NEW SUBFLOOR, INSTALLED SUBFLOOR PER SRM 53-05 PG 380. 2 L 7 2 4F RT A6WE 1996041200201 19960412 00201 1996 4 12 DLM88960770 4 19960405 A 2312 TR UNIT DOUG MD88 MD88 3023688 NM NR 2 VHF COMM MALFUNCTIONED A DALA O OTHER O OTHER CR CRUISE 1 SO 27 912DE 49997 LOST BOTH RADIOS INFLIGHT, ALL FREQUENCIES. JAMMED WHATEVER FREQ WAS SELECTED WITH CONSTANT TRANSMISSION. ATTEMPTED AL L COMBINATIONS OF AMPS, RADIOS AND MICS TO NO AVAIL. FINAILLY SOMETHING CHANGED AND WE WERE ABLE TO ISOLATE PROBLEM TO F/O'S SIDE. ANY RADIO COPILOT SELECTED WOULD WIPE OUT THE FREQUENCY. REPLACED F/O'S AUDIO SELECT PANEL AND NR 2 VHF CO MM TRANSCEIVER. CALLED DFW MTC FREQ 131.37 WITH BOTH RADIOS SELECTED TO SAME FREQ. BOTH RADIOS OP, NORMAL. 2 L 7 2 4F RT A6WE 1996041200202 19960412 00202 NM 1996 4 12 MWEA96105 1 19960406 A 3350 60030431 POWER SUPPLY DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 701ME 49760 DURING SERVICE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS FROM ROW 6 THROUGH 14 ILLUMINATE WHEN POWER IS TURNED OFF. REP LACED BATTERY POWER SUPPLY, OPS CHECK GOOD. 2 L 7 2 4F RT A6WE 1996041200203 19960412 00203 WP 1996 4 12 MWEA96106 1 19960407 A 2120 AIR DISTR DOUG DC9 DC932 3022066 WP CABIN ODOR A MWEA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 31 207ME 47794 PAX REPORTS, ELETRICAL SMELL AROUND ROW 19 DURING FINAL APPROACH, NO SMOKE OBSERVED. INSPECTED PSU PANEL WIRING IN AREA OF REPORT AND WAS UNABLE TO LOCATE SOURCE OF SMELL. UNABLE TO DUPLICATE. 2 L 7 2 4F A6WE 1996041200204 19960412 00204 WP 1996 4 12 MWEA96107 1 19960408 A 5210 SKIN DOUG DC9 DC932 3022066 WP FWD ENT DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 DURING C-CHECK, FOUND FWD ENTRANCE DOOR HAS CRACK .5 INCH ON EDGE OF DOOR SKIN, LOWER FWD CORNER. INSTALLED REPAIR IAW SRM 52-05, FIG 32. 2 L 7 2 4F A6WE 1996041200205 19960412 00205 WP 1996 4 12 UPS96805863 1 19960302 A 5315 FLOOR BEAM DOUG DC8 DC871F 302199D WP FS 920 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION AND CRACK AT FWD BEAM, FS 920 LBL 65 AFT SIDE. REPAIRED PER UPS EO . 2 L 7 4 4F RT 4A25 1996041200206 19960412 00206 WP 1996 4 12 UPS96805864 1 19960318 A 5320 5643131 DOUBLER DOUG DC8 DC871F 302199D WP FS 683-780 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON DOUBLER AROUND FASTENERS AT STA 683 TO 780 LBL 10 RBL 10. REPAI RED PER UPS EO. 2 L 7 4 4F RT 4A25 1996041200207 19960412 00207 WP 1996 4 12 UPS96805865 1 19960302 A 5320 5773275 ANGLE DOUG DC8 DC871F 302199D WP FS 781-759 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON LOWER SUPPORT ANGLE UNDER SEAT TRACK NR 7 FS 781 TO 759. REPAIR ED PER UPS EO. 2 L 7 4 4F RT 4A25 1996041200208 19960412 00208 WP 1996 4 12 UPS96805866 1 19960227 A 5320 47558118 INTERCOSTAL DOUG DC8 DC871F 302199D WP FS 1265 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON FS 1265 LONGERON 11R AT INTERCOSTAL. REPAIRED INTERCOSTAL PER S RM 51-1-20D, 53-2-0. 2 L 7 4 4F RT 4A25 1996041200209 19960412 00209 WP 1996 4 12 UPS96805867 1 19960228 A 5320 564695550B FITTING DOUG DC8 DC871F 302199D WP FS 980 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON FS 980 FWD OF FRAME FITTING LONGERON 20R. REPLACED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996041200210 19960412 00210 WP 1996 4 12 UPS96805868 1 19960227 A 5320 DOUBLER DOUG DC8 DC871F 302199D WP FS 857 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON BOLT FRAME DOUBLER FS 857 LONGERON 19R. REPLACED FRAME DOUBLER PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996041200211 19960412 00211 WP 1996 4 12 UPS96805869 1 19960225 A 5320 4613574 SPLICE DOUG DC8 DC871F 302199D WP FS 210 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON LONGERON 8R SPLICE FS 210. REPLACED SPLICE FITTING PER SRM 51-1 -20D. 2 L 7 4 4F RT 4A25 1996041200212 19960412 00212 WP 1996 4 12 UPS96805870 1 19960303 A 5320 DOUBLER DOUG DC8 DC871F 302199D WP FS 1227-1264 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON INNER DOUBLER BETWEEN LONG 31L TO 33R FS 1227 TO 1264. RE PLACED PER EO DC8-53-1599. 2 L 7 4 4F RT 4A25 1996041200213 19960412 00213 WP 1996 4 12 UPS96805871 1 19960228 A 5320 FITTING DOUG DC8 DC871F 302199D WP FS 920 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION AT FS 920 FITTING AFT OF LONG 24R. REPLACED FITTING PER SRM 53-2-0. 2 L 7 4 4F RT 4A25 1996041200214 19960412 00214 WP 1996 4 12 UPS96805872 1 19960301 A 5320 ANGLE DOUG DC8 DC871F 302199D WP FS 100 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON ATTACH ANGLE AT FS 100 LONG 31R. REPLACED ANGLE PER SRM 5 1-1-21. 2 L 7 4 4F RT 4A25 1996041200215 19960412 00215 WP 1996 4 12 UPS96805873 1 19960301 A 5311 FRAME DOUG DC8 DC871F 302199D WP FS 160 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON BOLT FRAME FS 160 LONG 36 TO 35R. REPAIRED PER SRM 53-2-0 FIG 2 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996041200216 19960412 00216 WP 1996 4 12 UPS96805874 1 19960301 A 5320 ATTACH ANGLE DOUG DC8 DC871F 302199D WP FS 360 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY INTERGRANULAR CORROSION ON FRAME ANGLE FS 360 LONG 27L. REPAIRED PER S RM SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996041200217 19960412 00217 WP 1996 4 12 UPS96805875 1 19960303 A 5320 SPLICE DOUG DC8 DC871F 302199D WP FS 1540-1520 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MODERATE CORROSION DAMAGE AT SPLICE LONG 31L BETWEEN FS 1520 TO 1540. REPLAC ED SPLICE PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996041200218 19960412 00218 WP 1996 4 12 UPS96805876 1 19960303 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FS 1380-1400 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON LONGERON 34L FS 1380 TO 1400 FS 1520 TO 540. REPLACED LON GERON SECTION PER SRM 51-2-2. 2 L 7 4 4F RT 4A25 1996041200219 19960412 00219 WP 1996 4 12 UPS96805877 1 19960303 A 5320 FITTING DOUG DC8 DC871F 302199D WP FS 1394 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON CORNER FITTING FS 1394 INSIDE LONG FWD TORQUE BOX HOLE. R EPLACED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996041200220 19960412 00220 WP 1996 4 12 UPS96805878 1 19960303 A 5311 FRAME DOUG DC8 DC871F 302199D WP FS 1360 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON FWD SIDE OF FRAME FS 1360 ABOVE LONG 36. REPAIRED FRAME P ER SRM 53-2-0, FIG 2. 2 L 7 4 4F RT 4A25 1996041200221 19960412 00221 WP 1996 4 12 UPS96805879 1 19960303 A 5320 FITTING DOUG DC8 DC871F 302199D WP FS 1160 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MODERATE CORROSION LONGERON FITTING. REPLACED FITTING PER SRM 53-2-0 AND 51- 1-20D. 2 L 7 4 4F RT 4A25 1996041200222 19960412 00222 WP 1996 4 12 UPS96805880 1 19960303 A 5320 FITTING DOUG DC8 DC871F 302199D WP FS 1228 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MODERATE CORROSION ON FITTING FS 1228 LONG 27 TO 28L. REPLACED FITTING PER S RM 51-1-20D. 2 L 7 4 4F RT 4A25 1996041200223 19960412 00223 WP 1996 4 12 UPS96805881 1 19960305 A 5320 FITTING DOUG DC8 DC871F 302199D WP FS 1680 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON FITTING, FWD SIDE OF FS 1680 LONG 31R. REPLACED FITTING P ER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996041200224 19960412 00224 WP 1996 4 12 UPS96805882 1 19960305 A 5320 FITTING DOUG DC8 DC871F 302199D WP FS 1680 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON FITTING, AFT SIDE OF FS 1680 LONG 21R. REPLACED FITTING P ER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996041200225 19960412 00225 WP 1996 4 12 UPS96805883 1 19960310 A 5320 FITTING DOUG DC8 DC871F 302199D WP FS 1190 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MODERATE CORROSION DAMAGE ON FITTING, FS 1190 LONGERONS 32 TO 33R. REPLACED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996041200226 19960412 00226 WP 1996 4 12 UPS96805884 1 19960310 A 5320 FITTING DOUG DC8 DC871F 302199D WP FS 1180 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED T-FITTING HEAVY CORROSION AT FS 1180 LONG 34R. REPLACED FITTING PER SRM 51- 1-20D. 2 L 7 4 4F RT 4A25 1996041200227 19960412 00227 WP 1996 4 12 UPS96805885 1 19960311 A 5320 SPLICE STRAP DOUG DC8 DC871F 302199D WP FS 1050 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 1050 SPLICE STRAP DOUBLER HAS HEAVY CORROSION ON LONGERONS 31R AND 31L. R EPLACED STRAP PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996041200228 19960412 00228 WP 1996 4 12 UPS96805886 1 19960311 A 5320 DOUBLER DOUG DC8 DC871F 302199D WP FS 1050 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 1050 SPLICE FINGER DOUBLER HAS HEAVY CORROSION AND CRACKS ON LONGERONS 31R AND 31L. REPLACED DOUBLER PER SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 1996041200229 19960412 00229 NM 1996 4 12 UPS96805887 1 19960405 A 2910 HYD LINE BOEING 747 747SR46 NM NR 3 ENGINE LEAKING A IPXA G O2 MASK DEPLOYED K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 01 688UP 20784 FLIGHT CREW REPORTED, ON FINAL APPROACH THE A/C FILLED WITH SMOKE. SKYDROL INDUCED INTO THE PNEUMATIC SYSTEM DUE TO CHA FED LINE AND DUCT. FOUND PNEUMATIC LINE CHAFING AGAINST EDP HYD LINE IN L/E ABOVE NR 3 ENGINE. REPAIRED PNEUMATIC DUCT IAW FAA FORM 8130-3. DUCT WAS REWELDED, INSTALLED INTERM REPAIR PER GMM 3-24-2. 2 L 7 4 4F A20WE 1996041200230 19960412 00230 WP 1996 4 12 9607839876 1 19960405 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 785NC 48110 DURING LINE CHECK, FOUND OVERHEAD AISLE EMERGENCY ESCAPE LIGHTS INOPERATIVE AT ROW 20 TO 24. REPLACED POWER SUPPLY, OPE RATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996041200231 19960412 00231 WP 1996 4 12 9607849152 1 19960405 A 3350 POWER SUPPLY DOUG DC9 DC914 3022034 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8911E 45825 DURING LINE CHECK, FOUND FORWARD EMERGENCY PATHWAY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996041200232 19960412 00232 WP 1996 4 12 9607859602 1 19960405 A 3260 UPLOCK ROLLER DOUG DC9 DC932 3022066 WP LT MLG OUT OF ADJUST A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 602NW 47046 LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INC IDENT. MAINTENANCE FOUND LEFT MAIN GEAR UPLOCK ROLLER TENSION WEAK. ADJUSTED TENSION, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996041200233 19960412 00233 EU 1996 4 12 9607863245 1 19960407 A 3230 RETRACT MECH AIRBUS 320 A320211 3930320 EU LANDING GEAR MALFUNCTIONED A A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 345NW 399 DURING APPROACH, THE LANDING GEAR DID NOT EXTEND. CYCLED THE LANDING GEAR HANDLE AND ALL INDICATIONS WERE NORMAL. AIRC RAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING REVEALED NO DISCREPANCIES. 2 L 7 2 4F RT A28NM 1996041200234 19960412 00234 1996 4 12 9607879917 4 19960408 A 3454 2587567901 RMI INDICATOR DOUG DC9 DC932 3022066 WP RIGHT MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 967N 36016 11484 47573 COMPASS FLAG APPEARED ON CAPTAIN'S HSI DURING CLIMBOUT. NEITHER CAPTAIN'S COMPASS CARD NOR FIRST OFFICER'S RMI WOULD FO LLOW HEADING CHANGES. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NR 2 DIRECTIONAL GYRO W ITH NO HELP. REPLACED FIRST OFFICER'S RMI, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996041200235 19960412 00235 1996 4 12 9607889602 4 19960408 A 3425 FLIGHT DIRECTOR DOUG DC9 DC932 3022066 WP LEFT MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 GL 01 602NW 47046 CAPTAIN'S GYRO FLAG APPEARED DURING TURNS AFTER TAKEOFF. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENAN CE REPLACED CAPTAIN'S FLIGHT DIRECTOR AND VERTICAL GYRO, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996041200236 19960412 00236 NE 1996 4 12 9607892293 2 19960406 A 7532 658385 PRBC VALVE BOEING 727 727251 138408H NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 293U 14582 153 21504 700540 NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL ON TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. M AINTENANCE REPLACED THE PRBC VALVE WITH A SERVICEABLE UNIT. 2 L 7 3 4F 4 F A3WE E2EA 1996041200237 19960412 00237 WP 1996 4 12 9607909305 1 19960403 A 5350 RELEASE MECH DOUG DC9 DC982 3022082 WP TAIL CONE OUT OF ADJUST A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 307RC 48086 DURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO ACTIVATE THE TAIL CONE RELEASE SYSTEM AND THAT THE TAIL CO NE FAILED TO DROP USING THE AFT EXIT DOOR HANDLE. FURTHER INVESTIGATION REVEALED THAT A PANEL WAS INTERFERRING WITH LAT CH FUNCTION. ALSO, THAT THE EXTERNAL RELEASE HANDLE WAS OBSTRUCTED BY THE HANDLE CUTOUT SKIN. CLEANED AND LUBED THE TA IL CONE LATCHES, TRIMMED THE PANEL AND TRIMMED THE HANDLE CUTOUT, CHECKED OK. 2 L 7 2 4F A6WE 1996041200238 19960412 00238 NM 1996 4 12 96FDEA00750 1 19960408 A 5312 BULKHEAD BOEING 727 72725 1384006 NM BS 178 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 CORROSION (C53-100-01, 4) ON FWD SIDE OF 178 BULKHEAD, RBL 21-26 WL 218. CORROSION WAS REMOVED WITHIN LIMITS ON BULKHEA D PER SRM 53-10-1, WEB WAS REPLACED. 2 L 7 3 4F A3WE 1996041200239 19960412 00239 NM 1996 4 12 96FDEA00751 1 19960406 A 5210 50794577 SIDE FRAME BOEING 727 72725 1384006 NM PAX DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 FWD ENTRY DOOR, FWD SIDE FRAME IS CRACKED IN RADIUS ON LOWER EDGE, ADJACENT TO THE LOWER FWD STOP PIN FITTING. REMOVED FWD ENTRY DOOR CRACKED FWD SIDE FRAME, INSTALLED ONE EACH FWD SIDE FRAME IAW FEDEX 727 SRM 51-30-2 MM 52-11-01. 2 L 7 3 4F A3WE 1996041200240 19960412 00240 NM 1996 4 12 96FDEA00752 1 19960408 A 5320 69463822 PRESSURE PAN BOEING 727 727233 138408A NM BS 757 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 269FE 21675 UPON REMOVAL OF PRESSURE PAN, FOUND TWO CRACKS AT BS 757 RBL 65 TO 68 WL 207. REMOVED DAMAGE ON PRESSURE PAN, FABRICATE D AND INSTALLED REPAIR PARTS AT BS 757 RBL 65 TO 68 WL 207 PER FEDEX SRM 51-40-2. 2 L 7 3 4F RT A3WE 1996041200241 19960412 00241 NM 1996 4 12 96FDEA00753 1 19960408 A 5330 SKIN BOEING 727 727233 138408A NM BS 650 LIGHTNING STRIKE A FDEA K NONE C F.O.D. IN INSP/MAINT 1 SO 25 269FE 21673 LIGHTNING STRIKE BS 650 STR 6R. CUT OUT DAMAGED AREA, FABRICATED FILLER AND DOUBLER PARTS AND INSTALLED. TREATED, PRIM ED AND PAINTED REPAIR PARTS AND AREA AT BS 650 STR 6R, ALL WORK DONE IAW FEDEX SRM 53-30-3. 2 L 7 3 4F RT A3WE 1996041200242 19960412 00242 NM 1996 4 12 96FDEA00754 1 19960408 A 5754 65162267A HINGE LUG BOEING 727 727233 138408A NM NR 2 LE FLAP CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 269FE 21675 NR 0381 AND 004, NR 2 K-FLAP O/B HINGE LUG O/B UPPER BOLT HAS CORROSION AROUND IT. REPLACED NR 2 K-FLAP PER FEDEX MM 27 -81-01, DUE TO CORROSION BEING EXCESSIVE. 2 L 7 3 4F RT A3WE 1996041200243 19960412 00243 NM 1996 4 12 96FDEA00755 1 19960408 A 5754 65162268A FLAP ASSY BOEING 727 727233 138408A NM NR 5 LE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 269FE 21675 NR 0130 AND 003, DUE TO NUMEROUS CORROSION DISCREPANCIES, NR 5 K-FLAP ASSY REQUIRES REPLACEMENT. 2 L 7 3 4F RT A3WE 1996041200244 19960412 00244 WP 1996 4 12 96UAL900238 1 19960408 A 3350 BATTERY DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1839U 46633 FORWARD EMERGENCY LIGHT FAILED BATTERY CHECK. REPLACED BATTERY, CHECKS NORMAL. 2 L 7 3 4F 4 F A22WE E23EA 1996041200245 19960412 00245 NM 1996 4 12 96UAL900239 1 19960408 A 3230 3232862 DNLOCK ACTUATOR BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE NLG FRACTURED A UALA O OTHER J WARNING INDICATION LD LANDING 1 WP 29 976UA 21598 NOSE GEAR WOULD NOT EXTEND NORMALLY. ATTEMPTED NORMAL EXTENSION TWICE, THEN EXTENDED MANUALLY. *S/D* THE NOSE GEAR DO WNLOCK ACTUATOR CYLINDER WAS FOUND FRACTURED AND A PUNCTURE IN THE BULKHEAD. REPLACED THE DOWNLOCK ACTUATOR AND REPAIRE D THE PUNCTURE IN THE BULKHEAD. 2 L 7 2 4F 4 F A16WE E2EA 1996041200246 19960412 00246 NM 1996 4 12 96UAL900240 1 19960408 A 4920 3820723 TURBINE WHEEL BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE APU FAILED A UALA O OTHER T ENGINE CASE PENETRATION IN INSP/MAINT 1 WP 29 9065U 6039 6039 19946 95115 APU DISCHARGED METAL FRAGMENTS ONTO RAMP. SUPPLEMENTAL DATA UPDATE: FOUND TURBINE WHEEL FAILED. CAUSE UNDER INVESTIGA TION. PART TOTAL CYCLES, 6,673. 2 L 7 2 4F 4 F A16WE E2EA 1996041200247 19960412 00247 1996 4 12 96UAL900241 4 19960408 A 3460 FMC BOEING 737 737322 1384676 NM E/E COMPT MALFUNCTIONED A UALA O OTHER J WARNING INDICATION TO TAKEOFF 1 WP 29 387UA 24662 FMC FAILS DURING TAKEOFF AT APPROXIMATELY 80 TO 100 KTS. FLAGS ARE DISPLAYED AND AUTO THROTTLES DISENGAGE. *S/D* NAVI GATION DATA BASE WAS RELOADED AND NO FURTHER PROBLEMS WERE FOUND. 2 L 7 2 4F RT A16WE 1996041200248 19960412 00248 NM 1996 4 12 96UAL900242 1 19960408 A 3350 STRIP LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM563B1 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 390UA 24665 AFT GALLEY EMERGENCY ESCAPE LIGHT STRIP INOP. REPLACED FAULTY LIGHT STRIP AND OPERATION NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 1996041200249 19960412 00249 NM 1996 4 12 96UAL900243 1 19960408 A 2913 HYD PUMP ABEX 6506606 BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 4 LEAKING A UALA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CL CLIMB 1 WP 29 4727U 19883 RIGHT BODY AND WING GEAR DOORS WOULD NOT CLOSE USING PRIMARY AND ALTERNATE SYSTEM. FAILED NR 4 HYDRAULIC PUMP. FOUND L EAKING PUMP SEAL SHAFT. REPLACED PUMP. 2 L 7 4 4F 4 F A20WE E20EA 1996041200250 19960412 00250 NM 1996 4 12 96UAL900244 1 19960408 A 3350 FEEDER WIRE BOEING 737 737322 1384676 NM GE CFM56 CFM563B1 13802 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 202UA 24717 EMERGENCY ESCAPE LIGHT STRIP BETWEEN ROWS 10 AND 16 INOP. REPLACED EMERGENCY ESCAPE LIGHT STRIP POWER FEEDER AND OPERAT ION NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 1996041200251 19960412 00251 1996 4 12 96UAL900245 4 19960408 A 3418 10620475 AOA SENSOR BOEING 737 737322 1384676 NM GE CFM56 CFM563B1 13802 NE FUSELAGE INOPERATIVE A UALA A UNSCHED LANDING J E WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 WP 29 385UA 24660 STICK SHAKER OCCURRED ON ROTATION, RETURNED TO LAX FOR NORMAL LANDING. *S/D* REPLACED ANGLE OF ATTACK SENSOR, SYSTEM C HECKS OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1996041200252 19960412 00252 EU 1996 4 12 COMA960097 1 19960404 A 3010 395OFS2 DE-ICE VALVE SAAB SF340 SF340A 7850100 EU LT NACELLE MALFUNCTION A COMA K NONE O OTHER CR CRUISE 1 SO 01 359CA 19507 2912 340A053 OUTBD WING DE-ICE SYSTEM IS INOPERATIVE. REPLACED THE LT DE-ICE DISTRIBUTOR VALVE. 2 L 7 2 4T RT A52EU 1996041200253 19960412 00253 SO 1996 4 12 COMA9610123 1 19960331 A 2750 3075001017 FCU EMB 120 EMB120RT SO TE FLAPS MALFUNCTIONED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 1110J 120110 FLAP CONTROL FAULT WARNING. REPLACED THE FLAP CONTROL UNIT. 2 L 7 2 4T RT A31SO 1996041200254 19960412 00254 EU 1996 4 12 COMA9630096 1 19960404 A 5610 7256100501 WINDSHIELD SAAB SF340 SF340A 7850100 EU LT COCKPIT LOOSE A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 140N 340A140 PILOTS WINDSHIELD MAKES A HORN LIKE NOISE ABOVE 3,000 FEET. REPAIRED EXTERNAL WEATHER SEAL ON WINDSHIELD. 2 L 7 2 4T RT A52EU 1996041200255 19960412 00255 NM 1996 4 12 DL72E960784 1 19960406 A 3350 1001141 LIGHT BOEING 727 727247 138408F NM AFT AIRSTAIR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 830WA 21482 ON LAYOVER, FOUND EMERGENCY LIGHT ABOVE AFT AIRSTAIR INOP. RESEATED BATTERY PACK, FOUND CONTACT BROKEN ON LIGHT ASSY. R EPLACED SAME. 2 L 7 3 4F A3WE 1996041200256 19960412 00256 NM 1996 4 12 DL72L960773 1 19960405 A 5312 651841615 PRESS BLKHD BOEING 727 727232 1384082 NM GE CF680 CF680A2 NE BS 289 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 502DA 21304 580346 ADDITIONAL CRACKING OF .75 WAS FOUND ON PRESSURED DECK AT FS 289 RBL4.5. REPAIRS ACCOMPLISHED PER DL ERA 258994-14 REV A. 2 L 7 3 4F 4 F A3WE E13NE 1996041200257 19960412 00257 NM 1996 4 12 DL72S960752 1 19960327 A 5330 65545906 SKIN BOEING 727 727232 1384082 NM BS 708-720 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 520DA 21471 THE FUSELAGE SKIN (2024-T3 CLAD) WAS FOUND TO HAVE CORRODED JUST O/B OF STR 28L, FROM STA 708 TO 720. THIS DAMAGE WILL REQUIRE A CUTOUT MEASURING 12 INCHES LONG BY 1.5 WIDE EXTENDING FROM STA 708 TO 720. THIS DAMAGE IS 9.5 TO THE LEFT OF AN EXISTING EXTERNAL SKIN REPAIR PER ER/A 221033-14AD. ALSO, THE SKIN CLIP WAS FOUND TO BE CORRODED BETWEEN STR 28L AND 27L AT STA 720 ON THE FWD SIDE OF THE FRAME. ACCOMPLISHED REPAIRS PER DL ERA 303354-14AD REV A. 2 L 7 3 4F A3WE 1996041200258 19960412 00258 NM 1996 4 12 DL72S960778 1 19960406 A 2782 ACTUATOR 269002914 BOEING 727 727232 1384082 NM NR 6 LE SLAT FAILED A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 421DA 21274 SLOW LEAK OF HYDRAULIC SYSTEM-A AT F310 AFTER 2 HRS AT CRUISE. POM PROCEDURES FOLLOWED FOR LOSS OF SYSTEM-A. RT SL AT NR 6 DID NOT EXTEND WITH ALTERNATE FLAPS EXTENSION SWITCH. FOUND NR 6 SLAT ACTUATOR LEAKING. REPLACED ACT SERVICED HYD SYSTEM, OPERATION NORMAL. 2 L 7 3 4F A3WE 1996041200259 19960412 00259 NM 1996 4 12 DL72S960791 1 19960407 A 3350 900835 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 420DA 21273 LEFT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK AND RACK OPN CHECKS NORMAL. 2 L 7 3 4F A3WE 1996041200260 19960412 00260 NM 1996 4 12 DL73E960780 1 19960406 A 5230 SEAL BOEING 737 737247 138448D NM CARGO DOOR BLOWN A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 381DL 23608 AFT CARGO LIGHT CAME ON IN FLT. COULD NOT MAINTAIN PRESSURATION. UPON LANDING FOUND AFT CARGO DOOR PARTIALLY OPEN AND SEAL BLOWN OUTS AT THE AFT LOWER CORNER. REINSTALLED SEAL, PRESSURISED TO 8 PSI DIFF SYS AND CHECKED NORMAL. 2 L 7 2 4F A16WE 1996041200261 19960412 00261 NM 1996 4 12 DL76E960790 1 19960407 A 2120 AIR DIST BOEING 767 767232 1385132 NM CABIN SMOKE A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 112DL 22224 LIGHT SMOKE COMING FROM AREA ABOVE CHILLER IN FRONT GALLEY. PULLED CHILLER CB'S SMOKE STOPPED. RESET C/B'S, OPERATED O VENS, BUNWARMER AND CHILLER AND ALL NORMAL. CHECKED WIRE BUNDLES FOR SIGN OF OVERHEAT, NO DISCREPANCIES FOUND. 2 L 7 2 4F RT A1NM 1996041200262 19960412 00262 NE 1996 4 12 DL76S960772 2 19960405 A 7321 1305M69P05 MEC 8062644 BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 2 ENGINE MALFUNCTIONED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 27 119DL WYG36237 23278 580346 TAKEOFF ABORTED AT 80 KTS, RT ENG ONLY 88 PERCENT, N1 ACC WAS ALSO SLOW. REPLACED RT ENG, MEC LEAK CHECKED PERFORMED, E NG RUN PER PFHB AND ALL IND NORMAL. 2 L 7 2 4F 4 F RT A1NM E13NE 1996041200263 19960412 00263 WP 1996 4 12 DLL10960786 1 19960407 A 2130 SEAL LKHEED 1011 10113851 5265010 WP C 1 DOOR TORN A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 718DA 193C1097 LOUD BEATING NOISE ABOVE FWD CARGO DOOR AND LOUD AIR NOISE IN LOWER GALLEY. FLIGHT RETURNED TO ATL. FOUND SECTION OF C -1 DOOR SEAL BLOWN. REPLACED SECTION OF SEAL, PRESS NORMAL. 2 L 7 3 4F A23WE 1996041200264 19960412 00264 NE 1996 4 12 DLM11960781 2 19960406 A 7200 ENGINE DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE NR 2 ENGINE FAILED A DALA E A ENGINE SHUTDOWN UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 SO 27 806DE 48477 733733 AFTER TAKEOFF AT 2,600 FT AND 270 KIAS, NR 2 ENGINE FAILED. A/C SHUDDERED, RPM ROLLED BACK AND TEMP WENT TO 754, FIRED EXT AGENT FOR NR 2 ENG. FLIGHT RETURNED TO LAX WHERE MAINTENANCE FOUND METAL IN TAIL PIPE. REPLACED ENGINE AND ROUTED TO SHOP. 2 L 7 3 4F 4 F RT A22WE E24NE 1996041200265 19960412 00265 NM 1996 4 12 DLM11960788 1 19960407 A 3350 6044113 BATTERY DOUG MD11 MD11 3023602 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 808DE 48479 BATTERY 3 LOW MSG ON TEST FOR EMERGENCY LIGHT SYSTEM. REPLACED BATTERY. 2 L 7 3 4F RT A22WE 1996041200266 19960412 00266 NE 1996 4 12 DLM88960785 2 19960406 A 7200 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 FAILED A DALA A F UNSCHED LANDING ACTIVATE FIRE EXT. J E A WARNING INDICATION VIBRATION/BUFFET FLAME/FIRE CL CLIMB 1 SO 27 934DL 49721 725507 NR 2 ENG HAD SEVERE VIBRATION IN CLIMB FROM FL31 TO 35. LOST OIL PRESS/RT HYD PRESS AND HAD FIRE WARNING. BOTH EXT BOT TLES USED AND ALT GEAR EXT MADE. ENG HAD DRAGGING FAN AND OIL IN TAIL PIPE. REPLACED ENGINE AND ROUTED TO SHOP. ****S /D**** ENGINE SHOP DISASSEMBLY FOUND N2 CENTER TUBE FRACTURED. ALSO FOUND T2 SHAFT TWISTED. OIL FIRE INDICATIONS FOUND IN ID OF N2 ROTOR. N2 REAR HUB PREVIOUSLY MODIFIED PER EO 49-63034-3. 2 L 7 2 4F 4 F RT A6WE E9NE 1996041200267 19960412 00267 NM 1996 4 12 DLM88960789 1 19960407 A 3350 PIGTAIL DOUG MD88 MD88 3023688 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 908DL 49539 EMERGENCY TRACK LIGHTS BROKEN AT ROWS 1 AND 2 C/D. REPLACED PIGTAILS AND LIGHT COVERS. 2 L 7 2 4F RT A6WE 1996041200268 19960412 00268 NM 1996 4 12 DLM88960792 1 19960405 A 3233 3937060501 ACTUATOR DOUG MD88 MD88 3023688 NM RT MLG FAILED A DALA O OTHER O OTHER TO TAKEOFF 1 SO 27 935DL 49722 TAKEOFF ROLL, BRAKE TEMP LIGHT AND GAUGE FLICKERED ON/OFF AND READ HIGH TEMP. RAISED GEAR AND GOT RT MAIN UNSAFE AND GE AR DOOR LIGHT. OTHER GEAR UP AND LOCKED. CYCLED GEAR AND GOT SAME INDICATION. CAN FEEL/HEAR GEAR DOOR RUMBLE AT CRUIS E. REPLACED RT MLG RETRACT ACTUATOR LOWER ATTACH FITTING AND LOWER PIN PER MM 32-32-02, OPERATION NORMAL. 2 L 7 2 4F RT A6WE 1996041200269 19960412 00269 NE 1996 4 12 DLM88960794 2 19960406 A 7200 ENGINE 8981501 DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 FAILED A DALA F ACTIVATE FIRE EXT. E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SO 27 934DL 81491EK 49721 725507 STRONG ENGINE NR 2 VIBRATION FOLLOWED BY LOW HYD-E PRESS, FOLLOWED BY ENGINE FIRE WARNING NR 2. EMERGENCY GEAR EXT USED, ZERO HYD FLUID ON LANDING. NR 2 ENG WAS SHUTDOWN, BOTH FIRE BOTTLES USED. NR 2 ENGINE WAS REPLACED AND ROUTED T O SHOP. 2 L 7 2 4F 4 F RT A6WE E9NE 1996041200270 19960412 00270 EU 1996 4 12 WWMA9600033 1 19960405 A 3260 D49412001 CONTROL UNIT SAAB SF340 340B 7860101 EU LANDING GEAR DEFECTIVE A WWMA O OTHER P NO WARNING INDICATION LD LANDING 1 WP 15 247AE 340B247 CREW REPORTED, THAT THEY WERE UNABLE TO GET A NOSE GEAR DOWN INDICATION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR CONTROL UNIT AND PERFORMED LANDING GEAR EXTENSION AND RETRACTION CHECKS. AIRCRAFT WAS RELEAS ED FOR SERVICE. 2 L 7 2 4T RT A52EU 1996041200271 19960412 00271 NE 1996 4 12 96ZZZX1647 2 19960307 A 7200 ENGINE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE LEFT FLAMED OUT A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK X ENGINE FLAMEOUT TO TAKEOFF 1 GL 07 434JS 3051 FLT 4148 - LEFT ENGINE FLAMED OUT ON TAKEOFF ROLL. PERFORMED A PRECAUTIONARY EVACUATION. AIRCRAFT WAS LATER RETURNED T O THE GATE WHERE PIT MAINTENANCE INSPECTED THE ENGINE, NO DISCREPANCIES NOTED. MAINTENANCE ALSO REMOVED, CLEANED, AND R EINSTALLED ALL ENGINE HARNESS-TO-SENSOR CANNON CONNECTORS. CONDUCTED ENGINE GROUND RUNS IAW MM 72-00-00. NO DISCREPANC IES NOTED DURING ANY OF THE SYSTEM GROUND CHECKS. CONDUCTED FLIGHT CHECK. ALL ENGINE SYSTEMS CHECKED GOOD. AIRCRAFT R ETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 1996041200272 19960412 00272 NM 1996 4 12 96ZZZX1648 1 19960306 A 3260 0I6839 BULB DORNER DO32 DO328100 2996000 NM GEAR HANDLE DEFECTIVE A VNAA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 GL 07 433JS 3047 FLT 4149 - ON APPROACH AFTER LANDING GEAR WAS SELECTED 'DOWN', CREW REPORTED 'NO' DOWN AND LOCKED INDICATION FOR THE LEF T MAIN GEAR. CREW CONDUCTED A TOWER FLY-BY TO CONFIRM A GEAR DOWN CONDITION. ATC DECLARED AN EMERGENCY, EQUIPMENT ROLL ED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. OUT STATION MAINTENANCE REPLACED BULBS IN THE LANDING GEAR POSITION INDI CATOR IAW MM 32-00-00. GROUND CHECK 'GOOD'. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A45NM 1996041200273 19960412 00273 NM 1996 4 12 96ZZZX1649 1 19960315 A 7603 MS202194 PULLEY BOEING 727 72751C 1384015 NM NR 1 THROTTLE BINDING A RYNA O OTHER O OTHER DE DESCENT 1 CE 07 416EX 19287 DURING DESCENT INTO INDY, THE NR 1 ENGINE THROTTLE HUNG AT APPROXIMATELY ONE-THIRD FORWARD TRAVEL AND WOULD NOT MOVE TO IDLE STOP. DURING APPROACH, THROTTLE CAME LOOSE AND WENT TO IDLE STOP. INSPECTED NR 1 ENGINE CONTROL RODS AT FUEL CONT ROL, NO DEFECTS. INSPECTED CABLE RUNS, PULLEYS, AND THROTTLE QUADRANT, FOUND PULLEY IN AFT AIRSTAIR AREA BINDING. CLEA NED AND LUBRICATED PULLEY. THROTTLE OPS CHECKS NORMAL PER MM 76-11-11. (X) 2 L 7 3 4F A3WE 1996041200274 19960412 00274 SO 1996 4 12 96ZZZX1650 1 19960313 A 3230 1159HM201201 TERMINAL ASSY 1159H202623B GULSTM G1159 G1159 3953505 SO NLG FAILED A KKYA O OTHER J WARNING INDICATION AP APPROACH 1 NE 03 220FL 10994 3263 50 LGA/BDL - AIRCRAFT DEPARTED LGA EN ROUTE TO BDL. ON APPROACH TO BDL, THE LANDING GEAR WAS EXTENDED AT 200 KNOTS, A LOUD BANG EMANATED FROM THE NOSE GEAR WELL. THE NOSE GEAR LIGHT WAS NOT ILLUMINATED AND THE RED LIGHT WAS STILL ON IN THE G EAR HANDLE. EMERGENCY SYSTEM WAS ACTIVATED, RESULTING IN NO CHANGE. AIRCRAFT LANDED AT BDL WITHOUT INCIDENT. UPON INV ESTIGATION, FOUND THE NOSE GEAR ACTUATOR ROD END HAD CRACKED AND OPENED. THIS ALLOWED THE LANDING GEAR TO FREE FALL CAU SING THE DOWN AND LOCK SWITCH MOUNTING BRACKET TO BEND. 2 L 7 2 4F RT A12EA 1996041200275 19960412 00275 CE 1996 4 12 96ZZZX1651 1 19960103 A 5530 CR3245 RIVETS BEECH 1900 1900D 1154162 CE VERT TAB LOOSE A A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 831CA 6730 UE20 DURING SCHEDULED INSPECTIONS, LOOSE FASTENERS ON BOTH SIDES OF VERTICAL STABILIZER FORWARD SPAR WERE NOTED. ALTHOUGH A SIMILAR PROBLEM WAS ADDRESSED IN SB 2044 ON EARLIER MODEL 1900S, ADDITIONAL EVALUATION AND STUDIES ARE RECOMMENDED AS OT HER PREVIOUS IDENTIFIED AREAS OF CONCERN IN THE EMPENNAGE SECTION MAY BE RELATED. REPAIR WAS ACCOMPLISHED PER BEECHCRAF T RECOMMENDED PROCEDURE. 2 L 7 2 4T RT A24CE 1996041200276 19960412 00276 CE 1996 4 12 96ZZZX1652 1 19960219 A 5530 CR3245 RIVETS BEECH 1900 1900D 1154162 CE VERT STAB LOOSE A A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 830CA 6776 UE19 DURING SCHEDULED INSPECTION, LOOSE FASTENERS ON BOTH SIDES OF VERTICAL STABILIZER FORWARD SPAR WERE NOTED. ALTHOUGH A S IMILAR PROBLEM WAS ADDRESSED IN SB 2004 ON EARLIER MODEL 1900S, ADDITIONAL EVALUATION AND STUDIES ARE RECOMMENDED AS OTH ER PREVIOUS IDENTIFIED AREAS OF CONCERN IN THE EMPENNAGE SECTION MAY BE RELATED. REPAIR WAS ACCOMPLISHED PER BEECHCRAFT RECOMMENDED PROCEDURE. 2 L 7 2 4T RT A24CE 1996041200277 19960412 00277 CE 1996 4 12 96ZZZX1653 1 19960205 A 5530 CR3245 RIVETS BEECH 1900 1900D 1154162 CE VERT STAB LOOSE A A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 840CA 5764 UE38 DURING SCHEDULED INSPECTIONS, LOOSE FASTENERS ON BOTH SIDES OF VERTICAL STABILIZER FORWARD SPAR WERE NOTED. ALTHOUGH A SIMILAR PROBLEM WAS ADDRESSED IN SB 2044 ON EARLIER MODEL 1900S, ADDITIONAL EVALUATION AND STUDIES ARE RECOMMENDED AS OT HER PREVIOUS IDENTIFIED AREAS OF CONCERN IN THE EMPENNAGE SECTION MAY BE RELATED. REPAIR WAS ACCOMPLISHED PER BEECHCRAF T RECOMMENDED PROCEDURE. 2 L 7 2 4T RT A24CE 1996041200278 19960412 00278 CE 1996 4 12 96ZZZX1654 1 19960112 A 5530 CR3245 RIVETS BEECH 1900 1900D 1154162 CE VERT STAB LOOSE A A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 842CA 5618 UE41 DURING SCHEDULED INSPECTIONS LOOSE FASTENERS ON BOTH SIDES OF VERTICAL STABILIZER FORWARD SPAR WERE NOTED. ALTHOUGH A S IMILAR PROBLEM WAS ADDRESSED IN SB 2044 ON EARLIER MODEL 1900S, ADDITIONAL EVALUATION AND STUDIES ARE RECOMMENDED AS OTH ER PREVIOUS IDENTIFIED AREAS OF CONCERN IN THE EMPENNAGE SECTION MAY BE RELATED. REPAIR WAS ACCOMPLISHED PER BEECHCRAFT RECOMMENDED PROCEDURE. 2 L 7 2 4T RT A24CE 1996041200279 19960412 00279 CE 1996 4 12 96ZZZX1655 1 19960314 A 5530 CR3245 RIVETS BEECH 1900 1900D 1154162 CE VERT STAB LOOSE A A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 844CA 5981 UE45 DURING SCHEDULED INSPECTIONS, LOOSE FASTENERS ON BOTH SIDES OF VERTICAL STABILIZER FORWARD SPAR WERE NOTED. ALTHOUGH A SIMILAR PROBLEM WAS ADDRESSED IN SB 2004 ON EARLIER MODEL 1900S, ADDITIONAL EVALUATION AND STUDIES ARE RECOMMENDED AS OT HER PREVIOUS IDENTIFIED AREAS OF CONCERN IN THE EMPENNAGE SECTION MAY BE RELATED. REPAIR WAS ACCOMPLISHED PER BEECHCRAF T RECOMMENDED PROCEDURE. 2 L 7 2 4T RT A24CE 1996041200280 19960412 00280 CE 1996 4 12 96ZZZX1656 1 19960126 A 5530 CR3245 RIVETS BEECH 1900 1900D 1154162 CE VERT STAB LOOSE A A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 855CA 4722 UE61 DURING SCHEDULED INSPECTIONS, LOOSE FASTENERS ON BOTH SIDES OF VERTICAL STABILIZER FORWARD SPAR WERE NOTED. ALTHOUGH A SIMILAR PROBLEM WAS ADDRESSED IN SB 2044 ON EARLIER MODEL 1900S, ADDITIONAL EVALUATION AND STUDIES ARE RECOMMENDED AS OT HER PREVIOUS IDENTIFIED AREAS OF CONCERN IN THE EMPENNAGE SECTION MAY BE RELATED. REPAIR WAS ACCOMPLISHED PER BEECHCRAF T RECOMMENDED PROCEDURE. 2 L 7 2 4T RT A24CE 1996041200281 19960412 00281 CE 1996 4 12 96ZZZX1657 1 19960126 A 5530 CR3245 RIVETS BEECH 1900 1900D 1154162 CE VERT STAB LOOSE A A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 855CA 4722 UE61 DURING SCHEDULED INSPECTIONS, LOOSE FASTENERS ON BOTH SIDES OF VERTICAL STABILIZER FORWARD SPAR WERE NOTED. ALTHOUGH A SIMILAR PROBLEM WAS ADDRESSED IN SB 2004 ON EARLIER MODEL 1900S, ADDITIONAL EVALUATION AND STUDIES ARE RECOMMENDED AT OT HER PREVIOUS IDENTIFIED AREAS OF CONCERN IN THE EMPENNAGE SECTION MAY BE RELATED. REPAIR WAS ACCOMPLISHED PER BEECHCRAF T RECOMMENDED PROCEDURE. 2 L 7 2 4T RT A24CE 1996041200282 19960412 00282 NM 1996 4 12 AALA960271 1 19960206 A 5315 146N5089 FLOOR BEAM BOEING 757 757223 1384957 NM BS 1640 SHORT ED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 649AA 24607 AFW - FLOOR BEAM AT STA 164 HAS SEVERAL FASTENER LOCATIONS THAT DO NOT MEET FASTENER SPACING REQUIREMENTS OF SRM 53-00-5 1, FIGURE 203. TST: 14,011.16 HRS. CYCLES: 5,028. (X) 2 L 7 2 4F RT A2NM 1996041200283 19960412 00283 NM 1996 4 12 AALA960272 1 19960213 A 5321 146N5300 DECK PLATE BOEING 757 757223 1384957 NM BS 1720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 641AA 24599 AFW - DECK PLATE HAS CORROSION REMOVED BEYOND SRM LIMITS ON UPPER SURFACE, PER MRB 757-721. TST: 15,773 HRS. CYCLES: 5,917. (X) 2 L 7 2 4F RT A2NM 1996041200284 19960412 00284 NM 1996 4 12 AALA960273 1 19960213 A 5751 113N1511 SUPPORT BOEING 757 757223 1384957 NM LT AILERON CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 641AA 24599 AFW - LEFT WING AILERON HINGE SUPPORT, RIB NR 1 AT STA 817.27, HAS CORROSION REMOVED AROUND NUTPLATE BEYOND SRM LIMITS, PER MRB 757-726. (X) 2 L 7 2 4F RT A2NM 1996041200285 19960412 00285 NM 1996 4 12 AALA960274 1 19960213 A 5315 141N2932 FLOOR BEAM BOEING 757 757223 1384957 NM BS 324 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 641AA 24599 AFW - CORROSION WAS BLENDED BEYOND SRM LIMITS ON FLOOR BEAM AT STA 324, RBL 58, PER MRB 757-723. TST: 15,773. CYCLES: 5,917. (X) 2 L 7 2 4F RT A2NM 1996041200286 19960412 00286 NM 1996 4 12 AALA960286 1 19960221 A 3213 160N02013 STRUT BUSHING BOEING 757 757223 1384957 NM RT MLG GEAR ROTATED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 655AA 24613 AFW - RIGHT MLG LOWER SIDE STRUT SWIVEL UPPER BUSHING HAS ROTATED SLIGHTLY. TST: 13,691. CYCLES: 4,900. (X) 2 L 7 2 4F RT A2NM 1996041200287 19960412 00287 NM 1996 4 12 AALA960316 1 19960226 A 5210 146N6201 HANDLE PAN BOEING 757 757223 1384957 NM R4 DOOR GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 642AA 24600 AFW - R4 DOOR HANDLE PAN HAS A SMALL GOUGE AFTER BLENDING IS BEYOND SRM LIMITS, PER MRB 757-740. TST: 15,758.46. CYCL ES: 5,958. (X) 2 L 7 2 4F RT A2NM 1996041200288 19960412 00288 NM 1996 4 12 AALA960317 1 19960226 A 5315 146N5089 FLOOR BEAM BOEING 757 757223 1384957 NM BS 1640 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 642AA 24600 AFW - FLOOR BEAM AT STA 1640 HAS CORROSION REMOVED ON UPPER SURFACE BEYOND SRM LIMITS, PER MRB 757-756. TST: 15,758.46 HRS. CYCLES: 5,958. (X) 2 L 7 2 4F RT A2NM 1996041200289 19960412 00289 NM 1996 4 12 AALA960318 1 19960226 A 5321 146N5300 DECK PLATE BOEING 757 757223 1384957 NM BS 1680 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 642AA 24600 AFW - DECK PLATE HAS CORROSION REMOVED IN VARIOUS LOCATIONS. MATERIAL REMOVED IS BEYOND SRM LIMITS, PER MRB 757-735. T ST: 15,758.46. CYCLES: 5,958. (X) 2 L 7 2 4F RT A2NM 1996041200290 19960412 00290 NM 1996 4 12 AALA960319 1 19960226 A 5320 146N8522 SILL BOEING 757 757223 1384957 NM BS 1398-1440 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 642AA 24600 AFW - T-CHORD (INNER) HAS CORROSION REMOVED BEYOND SRM LIMITS ON UPPER SURFACE. T-CHORD (OUTER) HAS CORROSION REMOVED B EYOND SRM LIMITS ON OUTER SURFACE OF VERTICAL LEG, PER MRB 757-743. TST: 15,758.46 HRS. CYCLES: 5,958. (X) 2 L 7 2 4F RT A2NM 1996041200291 19960412 00291 NM 1996 4 12 AALA960320 1 19960226 A 5315 141N5112 FLOOR BEAM BOEING 757 757223 1384957 NM BS 365 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 642AA 24600 AFW - FLOOR BEAM AT STA 365 HAS CORROSION REMOVED BEYOND SRM LIMITS, PER MRB 757-734. TST: 15,758.46 HRS. CYCLES: 5, 958. (X) 2 L 7 2 4F RT A2NM 1996041200292 19960412 00292 NM 1996 4 12 AALA960321 1 19960226 A 5315 141N5112 FLOOR BEAM BOEING 757 757223 1384957 NM FS 377.7 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 642AA 24600 AFW - FLOOR BEAM AT STA 377.7 HAS CORROSION REMOVED ON UPPER SURFACE BEYOND SRM LIMITS, PER MRB 757-737. TST: 15,758.4 6 HRS. CYCLES: 5,958. (X) 2 L 7 2 4F RT A2NM 1996041200293 19960412 00293 NM 1996 4 12 AALA960322 1 19960226 A 5315 141N5111 FLOOR BEAM BOEING 757 757223 1384957 NM BS 345 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 642AA 24600 AFW - FLOOR BEAM AT STA 345 HAS CORROSION REMOVED BEYOND SRM LIMITS, PER MRB 757-733. TST: 15,758.46 HRS. CYCLES: 5, 958. (X) 2 L 7 2 4F RT A2NM 1996041200294 19960412 00294 NM 1996 4 12 AALA960359 1 19960306 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 470 Y CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1757A 48505 TUL - NR 8 SEAT TRACK HAS CORROSION AT FURNISHING TIE-DOWN POINT AT STA 470. REMOVED CORRODED SECTION OF SEAT TRACK TIE -DOWN AND INSTALLED REPAIR PLUG PER SRM 53-70-00, VOLT I. TST: 16,835. CYCLES: 2,678. (X) 2 L 7 3 4F RT A22WE 1996041200295 19960412 00295 NM 1996 4 12 AALA960360 1 19960306 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1350-1353 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1757A 48505 TUL - CORROSION IN SEAT TRACK AT LEFT MID-LAV TIE DOWN POINT. REMOVED CORRODED AREA OF SEAT TRACK AND INSTALLED REPAIR PLUG PER SRM 53-70-00, VOL I. TST: 16,835. CYCLES: 2,678. (X) 2 L 7 3 4F RT A22WE 1996041200296 19960412 00296 WP 1996 4 12 AALA960361 1 19960305 A 5320 5936038501 JAMB BEAM DOUG DC9 DC982 3022082 WP CARGO DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 224AA 49174 CORROSION AROUND INBOARD DOOR STOP AND ALONG DOOR SILL BEAM. REMOVED CORROSION. TREATED AND PAINTED REWORK AREA PER ES O 80559, DATED 3-5-96. TST: 38,945:30 HRS. CYCLES: 22,142. (X) 2 L 7 2 4F A6WE 1996041200297 19960412 00297 WP 1996 4 12 AALA960362 1 19960305 A 7603 3957271507 BRACKET DOUG DC9 DC982 3022082 WP FS 1287 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 224AA 49174 TUL - PULLEY BRACKET ON RT AFT SIDE OF FS 1287 CEILING AREA (AFT ) CORRODED. REMOVED OLD CORRODED BRACKET, INSTALLED NE W PULLEY BRACKET. TST: 38,945.30 HRS. CYCLES: 22,142. (X) 2 L 7 2 4F A6WE 1996041200298 19960412 00298 NM 1996 4 12 AALA960363 1 19960307 A 5311 FRAME BOEING 727 727227 1384078 NM BS 825.95 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - CRACK IN FRAME WEB, STA 825.95, LT STR 16 CUT-OUT. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 51-40-2, PAGE S 1-8, AND SRM 51-40, PAGE 1. TST: 62,953 HRS. CYCLES: 41,811. (X) 2 L 7 3 4F A3WE 1996041200299 19960412 00299 NM 1996 4 12 AALA960364 1 19960307 A 5330 SKIN BOEING 727 727227 1384078 NM BS 248 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - CRACK IN FUSELAGE SKIN AT STA 243 AND STR 222. CUT OUT CRACKED AREA AND INSTALLED DOUBLER PER SRM 53-30-3, PAGES 5-8. TST: 62,953 HRS. CYCLES 41,211. (X) 2 L 7 3 4F A3WE 1996041200300 19960412 00300 NM 1996 4 12 AALA960365 1 19960307 A 5330 SKIN BOEING 727 727227 1384078 NM BS 680-700 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 729AA 20736 TUL - BULGE IN SKIN BETWEEN STA 680 TO STA 700 OR STR 27R. CORRODED PORTION OF SKIN REMOVED AND CORRODED PORTION. REPA IRED STRINGER PER SRM 53-10-3. REPAIRED FUSELAGE PER 53-30-3. TST: 63,275 HRS. CYCLES: 44,950. (X) 2 L 7 3 4F A3WE 1996041200301 19960412 00301 NM 1996 4 12 AALA960366 1 19960307 A 5330 SKIN BOEING 727 727227 1384078 NM BS 490 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 729AA 20736 TUL - CORROSION THROUGH SKIN AT STA 490 BETWEEN STR 27L - STR 28L. REPAIRED AREA PER SRM 53-30-3. TST: 63,275. CYCLE S: 44,950. (X) 2 L 7 3 4F A3WE 1996041200302 19960412 00302 NM 1996 4 12 AALA960367 1 19960307 A 5330 SKIN BOEING 727 727227 1384078 NM BS 660-680 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 729AA 20736 TUL - BULGES IN SKIN ALONG STR 27L, BETWEEN STA 660 - STA 680. REPAIRED CORRODED SKIN AND STRINGER PER SRM 53-10-3, FIG URE 1, AND SRM 53-30-3, FIGURE 3. TST: 63,275 HRS. CYCLES: 44,950. (X) 2 L 7 3 4F A3WE 1996041200303 19960412 00303 NM 1996 4 12 AALA960368 1 19960307 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - SKIN CORROSION ON BOTTOM OF STR 27R. COMPLETED REPAIR DOUBLER PER ESO 11697. TST: 44,049 HRS. CYCLES: 22,196. (X) 2 L 7 3 4F A3WE 1996041200304 19960412 00304 NM 1996 4 12 AALA960369 1 19960307 A 5330 SKIN BOEING 727 727223 1384074 NM BS 560 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - SKIN CORRODED BELOW STR 28R, STA 560 TO STA 565. INSTALLED FILLER AND DOUBLER PER SRM 53-30-3. TST: 44,049. CY CLES: 22,196. (X) 2 L 7 3 4F A3WE 1996041200305 19960412 00305 NM 1996 4 12 AALA960370 1 19960307 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 560 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 CORROSION ON DOUBLER AND STRINGER, STA 560, STR 28R. CUT OUT DAMAGED SECTION OF STR 28R, UNDER STA 560 FRAME. INSTALLE D STRINGER SPLICE REPAIR AT STA 550 AND STA 570 (SRM 53-10-3). TST: 44,049 HRS. CYCLES: 22,196. (X) 2 L 7 3 4F A3WE 1996041200306 19960412 00306 WP 1996 4 12 AALA960371 1 19960305 A 3350 A3060719101 LIGHT STRIP DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 597AA 53287 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY OVERWING EXITS FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIGH T STRIP BY OVERWING EXITS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A6WE 1996041200307 19960412 00307 WP 1996 4 12 AALA960376 1 19960308 A 3350 LIGHT STRIP DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7527A 49919 DFW - FLT 1373 - AT THE GATE AFTER ARRIVAL DFW, FOUND EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY INOPERATIVE. REPLACED EM ERGENCY FLOOR LIGHT STRIP BY FORWARD GALLEY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1996041200308 19960412 00308 NM 1996 4 12 CAL960346 1 19960305 A 5320 DOUBLER BOEING 737 737130 1384435 NM EXT PWR RECEPT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14209 65656 19026 GSO - INSPECTION FOUND .25 INCH CRACKS IN SEVERAL AREAS OF DOUBLER FOR EXTERNAL POWER RECEPTACLE. THE DOUBLER WAS REMOV ED IAW SRM 51-30-2. THE CORROSION WAS REMOVED IAW SRM 51-10-6. A NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-3 0-2 AND SRM 51-30-2. (X) 2 L 7 2 4F A16WE 1996041200309 19960412 00309 NM 1996 4 12 HNAA9692219 1 19960313 A 2910 HYD SYSTEM DHAV DHC8 DHC8102 2809003 NM NR 2 REQD SERVICE A HNAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 07 922HA 094 SBY/PHL - FLT 3184 - WHEN SELECTING LANDING GEAR DOWN ON APPROACH INTO PHL, THE DOORS DID NOT OPEN AND GEAR DID NOT COME DOWN. PERFORMED ALTERNATE GEAR EXTENSION AND LANDED IN PHL WITHOUT INCIDENT. BLED NR 2 HYDRAULIC SYSTEM, GEAR SWING C HECKED GOOD. (X) 2 H 7 2 4T RT A13NM 1996041200310 19960412 00310 WP 1996 4 12 IXXA9635 1 19960305 A 3231 4767621 TURNBUCKLE DOUG DC8 DC871F 302199D WP RT MLG DOOR SPLIT A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 828BX 45993 DFW - ON DEPARTURE, GEAR DOOR LIGHT WOULD NOT GO OUT WITH THE LANDING GEAR HANDLE IN THE 'UP' POSITION. CYCLING THE GEA R RESULTED IN NO CHANGE. THE AIRCRAFT RETURNED TO DFW FOR MAINTENANCE. MAINTENANCE FOUND THE RT MLG DOOR ACTUATOR FOLL OW-UP CABLE WAS OUT OF RIG DUE TO A TURNBUCKLE IN THAT CABLE RUN WHOSE BARREL HAD SPLIT LONGITUDINALLY. THE TURNBUCKLE BARREL WAS REPLACED, THE RT DOOR FOLLOW-UP SYSTEM RIGGED IAW THE DC-8 MM, THE LANDING GEAR OPERATIONALLY CHECKED IAW DC- 8 MM, AND THE AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 4 4F RT 4A25 1996041200311 19960412 00311 WP 1996 4 12 IXXA9639 1 19960322 A 5260 SWITCH DOUG DC8 DC871 302199A WP LT MLG DOOR DIRTY A IXXA O OTHER N FALSE WARNING CL CLIMB 1 SW 11 823BX 46064 MKE - WHEN LANDING GEAR WAS RETRACTED ON TAKEOFF, DOOR WARNING LIGHT REMAINED ILLUMINATED. THE GEAR WAS CYCLED, BUT THE INDICATION REMAINED THE SAME. UPON ARRIVAL AT TOL, MAINTENANCE INSPECTED THE MLG DOOR AND FOUND THE LANDING GEAR DOOR STRIKER AND SWITCH DIRTY. THE SWITCH AND STRIKER WERE CLEANED AND LUBRICATED, AND OPS CHECKED PER DC-8 MM 56-60-01. AL L WAS NORMAL, AND THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 4 4F 4A25 1996041200312 19960412 00312 SW 1996 4 12 MALA964914 1 19960312 A 3230 EMERGENCY PIN SWRNGN SA227 SA227AC 8780603 SW GEAR SELECTOR OUT OF POSITION A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 446MA AC693 MSP - FLT 3002 - ON CLIMB-OUT FROM MSP, LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE REPO SITIONED THE EMERGENCY PIN IN THE EMERGENCY GEAR SELECTOR TO THE NORMAL POSITION. SYSTEM OPERATED SATISFACTORILY. (X) 2 L 7 2 4T RT A8SW 1996041200313 19960412 00313 SW 1996 4 12 MALA964915 1 19960312 A 5230 2724051003 CORNER SWRNGN SA227 SA227AC 8780603 SW CARGO DOOR PUNCTURED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 26863 AC650B MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE CARGO DOOR AFT LOWER CORNER PUNCTURED. REPAIRS WERE COMPLETE D BY REPLACING THE LOWER AFT CORNER, PN 27-24051-003, IAW FAC SRM 51-00-00, SRM 51-30-03, AND SRM 51-40-01. (X) 2 L 7 2 4T RT A8SW 1996041200314 19960412 00314 NM 1996 4 12 MALA964916 1 19960312 A 3350 6104781 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 865MA 364 MSP - DURING A MAINTENANCE INSPECTION, CABIN EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPAIRS WERE COMPLETED BY REPLACI NG THE BATTERY PACKS. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 2 H 7 2 4T RT A13NM 1996041200315 19960412 00315 SW 1996 4 12 MALA964917 1 19960312 A 3234 7092011 SELECTOR SWRNGN SA227 SA227AC 8780603 SW LANDING GEAR FAILED A MALA O OTHER O OTHER CL CLIMB 1 GL 15 26863 AC650B ABR - FLT 3203 - ON CLIMB-OUT, LANDING GEAR LEVER LOCK OVERRIDE WAS REQUIRED TO RETRACT THE GEAR. THE AIRCRAFT CONTINUE D TO MSP. MAINTENANCE REPLACED THE LANDING GEAR SELECTOR. SYSTEM OPERATED SATISFACTORILY. (X) 2 L 7 2 4T RT A8SW 1996041200316 19960412 00316 NM 1996 4 12 MALA964918 1 19960314 A 3230 83221004005 LATCH ASSY DHAV DHC8 DHC8102 2809003 NM COCKPIT STICKING A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 817MA 249 DTW - FLT 3120 - DURING PRE-FLIGHT IN DTW, CREW WAS UNABLE TO OPEN THE LANDING GEAR ALTERNATE EXTENSION DOOR. MAINTENAN CE PERSONNEL REPLACED THE DOOR LATCH ASSEMBLY. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 2 H 7 2 4T RT A13NM 1996041200317 19960412 00317 NM 1996 4 12 P91A096007 1 19960329 A 2150 65239712 ACTUATOR BOEING 727 727231 1384079 NM RT PACK FAILED A P9IA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 03 12305 64005 19562 DEN - ON RAMP, RIGHT PACK COOLING DOOR CLOSED CAUSING LIGHT SMOKE IN CABIN. REPLACED RT COOLING FAN DOOR ACTUATOR PER M M 21-52-1. OPS CHECKS GOOD. (X) 2 L 7 3 4F A3WE 1996041200318 19960412 00318 EU 1996 4 12 SIMA960741 1 19960314 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 417AT 417 ORD - FLT 4275 - EMERGENCY LIGHT ROW 10 FOUND INOPERABLE. REPLACED EMERGENCY LIGHT POWER SUPPLY 61WL, OPS CHECKED GOOD AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1996041200319 19960412 00319 NM 1996 4 12 TAOA039611 1 19960313 A 3240 211473 BRAKE ASSY BFGOODRICH BOEING 727 727227 1384078 NM NR 4 BRAKE OUT OF ADJUST A TAOA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 EA 15 925TS 9195 21244 UPON LANDING, LGA TOWER REPORTED BRAKE SMOKING. FOUND NR 4 BRAKE HAD BEEN CHANGED ON THE OVERNIGHT SERVICE. CHECKED BR AKES PER MM 32-40 - CHECKED GOOD. (X) 2 L 7 3 4F A3WE 1996041200320 19960412 00320 NM 1996 4 12 TAOA039614 1 19960316 A 3350 S106 BATTERY MARATHON BOEING 727 727254 138408L NM AFT AIRSTAIRS DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 916TS 20437 EMERGENCY LIGHT AT AFT AIRSTAIRS INOPERABLE. REPLACED BATTERIES - EMERGENCY LIGHT AT AFT AIRSTAIRS - OPS CHECKED OK. ( X) 2 L 7 3 4F A3WE 1996041200321 19960412 00321 NM 1996 4 12 TAOA039615 1 19960315 A 3350 07912 EPL LENS BRUCE BOEING 727 727225 1384077 NM CABIN MISSING A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 919TS 20447 EPL LENS MISSING AT ROW 28. INSTALLED EPL LENS AT ROW 28 - CHECKED OK. (X) 2 L 7 3 4F A3WE 1996041200322 19960412 00322 NE 1996 4 12 TWRA9611 2 19960311 A 7310 22086 FUEL FILTER BOEING 747 747121 1384871 NM PWA JT9 JT9D7A 52054 NE NR 1 ENGINE CONTAMINATED A TWRA O OTHER X ENGINE FLAMEOUT DE DESCENT 1 EA 15 604FF 19659 662417 ON MARCH 11, 1996, AIRCRAFT, FLIGHT 42, ON DESCENT FROM FL 350 TO FL 330 EXPERIENCED A NR 1 ENGINE SHUT DOWN DUE TO NO T HROTTLE RESPONSE. ENGINE WAS RESTARTED AT FL 330, AIRCRAFT LANDED WITH NO FURTHER INCIDENTS. UPON LANDING, MAINTENANCE FOUND FUEL FILTER CONTAMINATED WITH DEBRIS AND WATER. THE FILTER WAS REPLACED. RUN-UP CHECK OK. AIRCRAFT WAS RETURNE D TO SERVICE. (X) 2 L 7 4 4F 4 F A20WE E20EA 1996041200323 19960412 00323 NM 1996 4 12 TWRA9612 1 19960318 A 2560 65B56492914 LOCK ASSY BOEING 747 747282B 1384860 NM L5 DOOR MISSING A A TWRA K NONE O OTHER IN INSP/MAINT 1 EA 15 610FF 20501 L-5 DOOR, PRIOR TO DEPARTURE MIA, FOUND GIRT BAR SLIDE BRACKET MISSING (LOCK ASSY). MAINTENANCE INSTALLED NEW SLIDE BRA CKET. (X) 2 L 7 4 4F A20WE 1996041200324 19960412 00324 EU 1996 4 12 WTAA960053 1 19960306 A 3260 9005EN38 DNLOCK SWITCH BAG JETSTM JETSTM3101 1500215 EU NLG MALFUNCTIONED A WTAA O OTHER N FALSE WARNING CL CLIMB 1 WP 17 402UE 734 SMF - ONE BULB OF NOSE GEAR DOWN/LOCKED INDICATOR REMAINS ILLUMINATED AFTER LANDING GEAR IS SELECTED UP. GEAR POSITION INDICATION NORMAL AFTER GEAR EXTENSION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED AND INSPECTED NOSE GEAR MICROSWITCHES. PROBLEM CONTINUED DURING NOSE GEAR RETRACTION CHECK ON GROUND. AIRCRAFT FERRIED TO FAT FOR REPAIRS. RE MOVED AND REPLACED NLG DOWNLOCK MICROSWITCH. GEAR POSITION INDICATION NORMAL DURING GEAR SWING. AIRCRAFT RETURNED TO S ERVICE. (X) 2 L 7 2 4T RT A21EU 1996041200325 19960412 00325 WP 1996 4 12 Y2PA960011 1 19960313 A 5320 991224644 SHEAR CLIP DOUG DC9 DC915F 3022037 WP FS 860 CORRODED A Y2PA K NONE O OTHER IN INSP/MAINT 1 GL 23 197US 40244 47154 YIP - FOUND CORRODED SHEAR CLIP DURING SCHEDULED MAINTENANCE. FABRICATED NEW SHEAR CLIP, HEAT TREATED TO T-6 CONDITION PER MIL-H-6088F AND INSTALLED NEW SHEAR CLIP. PART TC: 46,789. (X) 2 L 7 2 4F A6WE 1996041200326 19960412 00326 EU 1996 4 12 HEEA966885 1 19960327 A 6230 350A37112702 LINK SCISSORS SNIAS 350 AS350B2 8680813 EU M/R MAST GOUGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 350BZ 1577 2653 LINK SCISSORS GOUGED AT BEARING ARM. 1 G 7 1 3U H9EU 1996041200327 19960412 00327 SW 1996 4 12 HEEA966887 1 19960329 A 3213 412050010107 CROSSTUBE BELL 412 412 1182202 SW RT SIDE BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3911L 7359 33023 CROSSTUBE BROKEN AT R/H SIDE OF THE CENTER SUPPORT BEAM ASSEMBLY CLAMP. 1 G 7 2 4U H4SW 1996041200328 19960412 00328 SW 1996 4 12 HEEA966890 1 19960401 A 2730 214001970107 ACTUATOR ASSY BELL 214 214ST 1182106 SW ELEV INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 ACTUATOR INOPERATIVE. WON'T MOVE OR TEST. 2 G 7 2 4U H10SW 1996041200329 19960412 00329 1996 4 12 HEEA966891 4 19960402 A 3452 071119218 CONTROL DISPLAY BELL 412 412 1182202 SW COCKPIT XPONDER DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 22347 36005 LIGHTS TOO DIM. REPLACED PHOTOCELL V101 P/N 134-5005-02. REPAIRED. CLEANED AND TESTED UNIT. TOUCHED UP FACEPLATE. BEN CH CHECK GOOD. 1 G 7 2 4U H4SW 1996041200330 19960412 00330 1996 4 12 HEEA966892 4 19960402 A 3452 066106200 TRANSCEIVER KT76 BOLKMS 105 BO105S 5626006 EU COCKPIT ATC DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 624MB S751 TOWER REPORTS UNIT INTERMITTENT. REPLACED INOPERATIVE CR202 MIXER DIODE. ALSO REPLACED FACEPLATE ASSEMBLY DUE TO BROKEN KNOB. REPLACED DETERIORATED R477 RESISTOR. REPLACED WEAK V301 PHOTODETECTOR. ADJUSTED FREQUENCY AND PULSE AND ADJUST ED FOR BEST SLS LEVEL. UNIT BENCH CHECKGOOD. 1 G 7 2 3U H3EU 1996041200331 19960412 00331 SW 1996 4 12 HEEA966893 1 19960402 A 7714 412075010109 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 33008 36004 TRIPLE TACH NEEDLE SPLIT. TIME SINCE REPAIR 6:35. 1 G 7 2 4U H4SW 1996041200332 19960412 00332 1996 4 12 HEEA966894 4 19960402 A 3457 0845000000 SKYNAV 5000 SNIAS 350 AS350B2 8680813 EU COCKPIT GPS DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 350BZ 2653 DISPL AYS FOREIGN CHARACTERS AND DOUBLE IMAGERY. 1 G 7 1 3U H9EU 1996041200333 19960412 00333 1996 4 12 HEEA966895 4 19960402 A 3453 25410038 7000 CDU BELL 412 412 1182202 SW COCKPIT LORAN DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3893P 33012 LORAN LED INOPERATIVE. 1 G 7 2 4U H4SW 1996041200334 19960412 00334 SW 1996 4 12 HEEA966896 1 19960402 A 5320 206033110239 STIFFENER BELL 206 206L3 1182108 SW FUSELAGE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3116L 5822 51529 CRACKED ON STIFFENER AT BOTTOM 3/16 RIVET HOLE AT TOP OF ANGLE. INSTALLED SERVICEABLESTIFFENER. 1 G 7 1 3U H2SW 1996041200335 19960412 00335 SW 1996 4 12 HEEA966897 1 19960402 A 5320 206033110229 STIFFENER BELL 206 206L3 1182108 SW FUSELAGE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3116L 5822 51529 STIFFENER CRACKED FROM 2ND RIVET HOLE AT L/H LOWER SIDE. INSTALLED SERVICEABLESTIFFENER. 1 G 7 1 3U H2SW 1996041200336 19960412 00336 SW 1996 4 12 HEEA966898 1 19960402 A 3212 212050207009 FLOAT BAG BELL 212 212 1181420 SW TOP CENTER LEAKAGE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 WHILE PERFORMING ACCEPTANCE CHECK ON FLOAT BAG, LEAKAGE ON TOP CENTER OF FLOAT BAG WAS DETECTED AT SEAM. 1 G 7 1 4U H4SW 1996041200337 19960412 00337 NE 1996 4 12 HEEA966899 1 19960402 A 6310 7636109103104 SHAFT SKRSKY S76 S76 8143010 NE ENG OUTPUT BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5426U 760167 SHAFT BROKEN. BROKE BELOW SAFETY HOLE. REPLACED WITH SERVICEABLE UNIT. 1 G 7 2 3U H1NE 1996041200338 19960412 00338 1996 4 12 HEEA966900 4 19960402 A 3454 071121525 CONTROL UNIT BELL 412 412 1182202 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 108X 33115 TEST IS INTERMITTENT. REPLACED SWITCH S101 P/N 133-0135-00. REPAIRED. CLEANED UNIT AND TOUCHED UP FACEPLATE. BENCH CHE CK GOOD. 1 G 7 2 4U H4SW 1996041200339 19960412 00339 1996 4 12 HEEA966901 4 19960402 A 2312 4000106010 CONTROL UNIT C10 SKRSKY S76 S76A 8143006 NE COCKPIT VHF DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5427S 760158 2ND DIGIT FROM LEFT, #5 UNREADABLE ON FREQUENCY SELECTOR. REPLACED THUMBWHEEL ASSEMBLY. AFTER INSTALLATION OF THUMBWHEE L BY PREVIOUS TECHNICIAN, FOUND THUMBWHEEL TO BE INOPERATIVE. RESOLDERED SEVERAL COLD SOLDER JOINTS IN THUMBWHEEL ASSY. REPAIRED. BENCH CHECK GOOD. 1 G 7 2 3U H1NE 1996041200340 19960412 00340 1996 4 12 HEEA966902 4 19960402 A 3442 MI5852013 INDICATOR P4001 BELL 412 412 1182202 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3893P 33012 INDICATOR HAS HORIZONTAL LINES AND BLUE SCREEN, ALSO FOUND LOW VOLTAGE POWER SUPPLY BAD. REPLACED TRANSISTOR (Q4). REP AIRED POWER SUPPLY. UNIT STILL HAS BLUE SCREEN. 1 G 7 2 4U H4SW 1996041200341 19960412 00341 1996 4 12 HEEA966903 4 19960402 A 2312 4000103002 TRANSCEIVER RT450 BOLKMS 117 BK117A4 5626017 EU COCKPIT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 520WJ 7092 TRANSCEIVER WILL NOT TRANSMIT. 1 G 7 2 3U H13EU 1996041200342 19960412 00342 1996 4 12 HEEA966904 4 19960402 A 2312 40001278500 TRANSCEIVER RT406F BOLKMS 117 BK117A3 5626015 EU COCKPIT VHF FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 8765J 7054 TRANSCEIVER WILL NOT TRANSMIT OR RECEIVE. 1 G 7 2 3U H13EU 1996041200343 19960412 00343 1996 4 12 HEEA966905 4 19960402 A 3442 MI585200 RADAR RT BELL 212 212 1181420 SW FAN UNIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 27805 31106 UNIT POWERS UP, BUT FAN DOES NOT COME ON. ALSO FOUND (F202) FUSE MISSING. REPLACED FUSE (F202) WITH SPARE. DID NOT CU RE PROBLEM. ALSO UNIT TRANSMITS INTERMITTENTLY. 1 G 7 1 4U H4SW 1996041200344 19960412 00344 1996 4 12 HEEA966906 4 19960402 A 3442 MI585200 RADAR RT BRAERO DH125 HS125700A 4230170 EU COCKPIT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 125CS NA0212 RADAR INOPERATIVE. UNIT NOT POWERING UP. REPLACED FUSE (F202). REPAIRED. UNIT NOT TRANSMITTING. REPLACED MAGNETRON. 2 L 7 2 4F A3EU 1996041200346 19960412 00346 1996 4 12 HEEA966908 4 19960402 A 3450 071121004 CONTROL BOX BELL 412 412 1182202 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2148K 36001 CONTROL BOX SEGMENTS OUT ON DISPLAY. 1 G 7 2 4U H4SW 1996041200347 19960412 00347 1996 4 12 HEEA966909 4 19960402 A 3453 066402600 LORAN KLN88 BELL 206 206L3 1182108 SW COCKPIT FAULTY E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 6160Z 51610 LORAN INTERMITTENT. 1 G 7 1 3U H2SW 1996041200348 19960412 00348 1996 4 12 HEEA966910 4 19960402 A 3455 066107200 RECEIVER KR87 BOLKMS 117 BK117B1 5626012 EU COCKPIT ADF FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 217UC 7152 ADF DOES NOT RECEIVE. INSPECTED AND TESTED. FOUND POINTER ON INDICATOR TO GO OUT 10 DEGREES TO 15 DEGREES. REMOVED REC EIVER BOARD AND SWAPPED WITH ANOTHER RECEIVER BOARD TO GET ANOTHER UNIT OUT. PROBLEM IS ON MAIN BOARD. CURRENT RECEIVE R BOARD DOES NOT RECEIVE. 1 G 7 2 3U H13EU 1996041200349 19960412 00349 1996 4 12 HEEA966911 4 19960402 A 3416 8140BS20LW ALTIMETER SKRSKY S76 S76 8143010 NE COCKPIT ENCODER ERROR E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5427S 760168 CANNON PLUG WILL NOT LOCK ON ALTIMETER DUE TO PLUG ON ALT. BEING RECESSED TO FAR INSIDE. ALSO ENCODER IS OFF 100 FEET A T 10000 FEET. TIME SINCE REPAIR 0:00. 1 G 7 2 3U H1NE 1996041200350 19960412 00350 1996 4 12 HEEA966912 4 19960402 A 2370 9806019001 CVR BELL 412 412 1182202 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 21498 36003 CVR PINGER MOUNT NUT PLATES MISSING. 1 G 7 2 4U H4SW 1996041200351 19960412 00351 GL 1996 4 12 HEEA966913 2 19960402 A 7321 25249227R FUEL CONTROL BELL 230 230 1182149 SW ALLSN 250C 250C30G2 03013 GL ENGINE FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 230UN 1312 23009 FUEL CONTROL INVOLVED IN A HIGH SIDE GOVERNOR FAILURE AND ROTOR WENT TO 112%. 1 G 7 2 3U 3 U NC H9SW E1GL 1996041200352 19960412 00352 GL 1996 4 12 HEEA966914 2 19960402 A 7323 25490682 GOVERNOR BELL 230 230 1182149 SW ALLSN 250C 250C30G2 03013 GL ENGINE FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 230UN 23009 HIGH SIDE GOVERNOR FAILURE. 1 G 7 2 3U 3 U NC H9SW E1GL 1996041200353 19960412 00353 1996 4 12 HEEA966915 4 19960402 A 2312 064105430 TRANSCEIVER BOLKMS 105 BO105S 5626006 EU COCKPIT VHF DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 81832 S828 VOLUME WILL NOT CONTROL. COULD NOT VERIFY PROBLEM WITH VOLUME CONTROL BUT FOUND DISPLAY WOULD NOT DIM. REPLACED PHOTODE TECTOR V901. REPAIRED. ADJUSTED AND TESTED UNIT. BENCH CHECKGOOD. 1 G 7 2 3U H3EU 1996041200354 19960412 00354 1996 4 12 HEEA966916 4 19960402 A 2312 4000106010 CONTROL UNIT C10 BOLKMS 105 BO105S 5626006 EU COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 911EB S812 TRANSMITS BUT WILL NOT RECEIVE. VERIFIED UNIT DOES NOT RECEIVE. REPLACED ON/OFF SWITCH. REPAIRED. BENCH CHECK GOOD. 1 G 7 2 3U H3EU 1996041200355 19960412 00355 SW 1996 4 12 HEEA966918 1 19960404 A 2430 1820300150 SHUNT BELL 230 230 1182149 SW DC GEN SYS DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 230UN 2942 23009 #1 AND #2 GENERATOR NOT COMING ON LINE INTERMITTENTLY. 1 G 7 2 3U NC H9SW 1996041200356 19960412 00356 1996 4 12 HEEA966920 4 19960404 A 3442 MI5851345 INDICATOR P40 BELL 212 212 1181420 SW COCKPIT RADAR DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1079U 31122 UNIT HAD BROKEN "MAP" SWITCH, REPLACED SWITCH WITH SPARE. REPAIRED.TROUBLESHOT UNIT FURTHER AND FOUND VIDEO BOARD TO B E INTERMITTENT AND LOGIC #2BOARD BAD. CAUSES DISTORTED DISPLAY. 1 G 7 1 4U H4SW 1996041200357 19960412 00357 1996 4 12 HEEA966921 4 19960404 A 3452 066106200 TRANSCEIVER KT76 BELL 206 206L1 1182107 SW COCKPIT ATC FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2761X 45283 TRANSPONDER SYSTEM DOES NOT FUNCTION. ALSO TRANSPONDER WILL NOT TEST. FOUND UNIT TO HAVE LOW POWER OUT. ADJUSTED CAVIT Y TUBE. REPLACED CAVITY TUBE (V101) P/N C2080A. REPAIRED LOW POWER OUT. TESTED UNIT AND FOUND RECEIVER WEAK. ALIGNE D RECEIVER. REPLACED MIXER DIODE (CR202) P/N 007-06092-0000. REPAIRED.ADJUSTED FREQUENCY AND PULSE. BENCH CHECK GOOD. 1 G 7 1 3U H2SW 1996041200358 19960412 00358 1996 4 12 HEEA966922 4 19960404 A 3452 066106200 TRANSCEIVER KT76 BELL 206 206B 1181511 SW COCKPIT ATC DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2272V 3621 REPLY LIGHT DOES NOT COME ON AND TEST LIGHT WILL NOT ILLUMINATE. REPLACED SWITCH BOARD AND FUSE F401. REPAIRED. REPLACE D PHOTOCELL V301 DUE TO WEAK REPLY LIGHT. REPAIRED. REPLACED DETERIORATED RESISTOR R477. INSTALLED HEATSINK BEHIND TR ANSISTOR Q415. FOUND WEAK POWER OUT. REPLACED CAVITY TUBE V101.REPAIRED. ADJUSTED FREQUENCY AND ALIGNED RECEIVER. BEN CH CHECK GOOD. 1 G 7 1 3U H2SW 1996041200359 19960412 00359 1996 4 12 HEEA966923 4 19960404 A 3452 066106200 TRANSCEIVER KT76 BELL 206 206L1 1182107 SW COCKPIT ATC DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 50034 45169 CODE SET KNOB MISSING. REPLACED FACEPLATE ASSEMBLY. REPAIRED. REPLACED PHOTOCELL V301 DUE TO WEAK REPLY LIGHT. REPAIRE D. BENCH CHECK GOOD. 1 G 7 1 3U H2SW 1996041200360 19960412 00360 1996 4 12 HEEA966924 4 19960404 A 3455 071121009 CONTROL BELL 412 412 1182202 SW COCKPIT ADF DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2148K 36001 SELECTOR KNOB ROTATES 350 DEGREES. REPLACED SELECTOR KNOB P/N 073-0548-05. REPAIRED. TESTED UNIT AND CHECKED LIGHTING. BENCH CHECK GOOD. 1 G 7 2 4U H4SW 1996041200361 19960412 00361 SW 1996 4 12 HEEA966926 1 19960405 A 5320 206031302269S SUPPORT BELL 206 206B 1181511 SW FUSELAGE DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107PH 2789 SUPPORT IS CREASED AND RIPPLED ALONG EDGES OF CHEM-MILLED AREAS ALONG ENTIRE PART. 1 G 7 1 3U H2SW 1996041200362 19960412 00362 SW 1996 4 12 HEEA966928 1 19960405 A 7810 230063301102 EXHAUST STACK BELL 230 230 1182149 SW ENG CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 2798 23009 EXH STACK IS CRACKED. 1 G 7 2 3U NC H9SW 1996041200363 19960412 00363 SW 1996 4 12 HEEA966929 1 19960405 A 6730 222382001105 ACTUATOR ASSY BELL 230 230 1182149 SW FLIGHT CONT LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 230UN 2958 23009 ACTUATOR LEAKING FROM LOWER PISTON SEAL. 1 G 7 2 3U NC H9SW 1996041200364 19960412 00364 SW 1996 4 12 HEEA966932 1 19960405 A 6520 222042001007 GEARBOX BELL 230 230 1182149 SW T/R CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 2976 23009 300 HOUR INSPECTION DUE. NOTE: CORROSION FOUND BEYOND LIMITS) 1 G 7 2 3U NC H9SW 1996041200366 19960412 00366 WP 1996 4 12 9607679950 1 19960306 A 5330 SKIN DOUG DC9 DC932 3022066 WP PAX DOOR CUTOUT CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9346 47376 DURING M-CHECK, FOUND A CRACK IN THE MAIN CABIN DOOR CUTOUT SKIN, UPPER AFT CORNER. REPAIRED SKIN (P/N 5911406-5) PER E A 99-108518. 2 L 7 2 4F A6WE 1996041200367 19960412 00367 NM 1996 4 12 9607686634 1 19960320 A 5320 SUPPORT BOEING 747 747227B 1384888 NM FS 510 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 634US 22234 DURING P-CHECK, FOUND CORROSION IN THE UPPER DECK FLOOR PANEL SUPPORT FS 510 LBL 23. REPAIRED SUPPORT (P/N 65B21284-3) PER EA 66-99585. 2 L 7 4 4F A20WE 1996041200368 19960412 00368 NM 1996 4 12 9607696634 1 19960320 A 5347 SEAT TRACK BOEING 747 747227B 1384888 NM FS 608 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 634US 22234 DURING P-CHECK, FOUND CORROSION IN THE UPPER DECK SEAT TRACK AT FS 508 LBL 27. REPAIRED TRACK (P/N 65B14708-15) PER EA 66-99584. 2 L 7 4 4F A20WE 1996041200369 19960412 00369 NM 1996 4 12 9607706634 1 19960321 A 5400 WEB BOEING 747 747227B 1384888 NM NR 3 PYLON CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 634US 22234 DURING P-CHECK, FOUND A CRACK IN THE NR 3 PYLON MID SPAR WEB. REPAIRED WEB (P/N 65B90421-41) PER EA 66-99587. 2 L 7 4 4F A20WE 1996041200370 19960412 00370 NM 1996 4 12 9607716634 1 19960327 A 5414 SKIN BOEING 747 747227B 1384888 NM NR 3 PYLON CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 634US 22234 DURING P-CHECK, FOUND A .8 INCH CRACK IN THE NR 3 PYLON INBOARD SKIN NACELLE, STATION 175 WL 151. REPAIRED SKIN PER EA 66-99590. 2 L 7 4 4F A20WE 1996041200371 19960412 00371 NM 1996 4 12 9607725504 1 19960329 A 5313 LONGERON BOEING 757 757251 1384970 NM FS 1543 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 504US 23193 DURING T-CHECK, FOUND A CRACK IN THE FLOOR SUPPORT STRINGER AT FS 1543 AT RBL 3. REPAIRED STRINGER (P/N 146N5444) PER E A 55-102076. 2 L 7 2 4F RT A2NM 1996041200372 19960412 00372 NM 1996 4 12 9607736634 1 19960329 A 5414 SKIN BOEING 747 747227B 1384888 NM NR 1 PYLON CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 634US 22234 DURING P-CHECK, FOUND A CRACK IN THE NR 1 PYLON INBOARD SKIN NACELLE STATION 175 WL 151. REPAIRED SKIN PER EA 66-99591. 2 L 7 4 4F A20WE 1996041200373 19960412 00373 WP 1996 4 12 9607749954 1 19960401 A 5320 FITTING DOUG DC9 DC931 3022065 WP FS 586 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 921RW 47164 DURING H-CHECK, FOUND CRACKS ON THE LONGERON 26, 29R AND 30 END FITTINGS AT APPROXIMATELY FS 586. REPLACED ALL FITTINGS PER SRM 51-30-2. 2 L 7 2 4F A6WE 1996041200374 19960412 00374 WP 1996 4 12 9607759954 1 19960401 A 5320 FITTING DOUG DC9 DC931 3022065 WP FS 579-598 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 921RW 47164 DURING H-CHECK, FOUND CORROSION ON THE LONGERON 25R END FITTING AT FS 579 TO 598. REPLACED FITTING PER SRM 51-10-2. 2 L 7 2 4F A6WE 1996041200375 19960412 00375 WP 1996 4 12 9607769954 1 19960402 A 5230 FITTING DOUG DC9 DC931 3022065 WP CARGO DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 921RW 47164 DURING H-CHECK, FOUND CRACKS IN THE FORWARD CARGO DOOR UPPER AFT AND LOWER AFT DOOR STOP FITTINGS. REPLACED FITTINGS. 2 L 7 2 4F A6WE 1996041200376 19960412 00376 NE 1996 4 12 9607912708 2 19960406 A 7261 LP5 FITTING BOEING 727 727225 1384077 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE GB FAILED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN J K WARNING INDICATION FLUID LOSS CR CRUISE 1 GL 01 817E 22554 700029 NR 1 ENGINE LOST OIL PRESSURE AND QUANTITY EN ROUTE. A PRECAUTIONARY ENGINE SHUTDOWN WAS ACCOMPLISHED. THE FLIGHT DIVE RTED TO MCO AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LP5 FITTING LIBERATED FROM THE GEARBOX. THE GEARBOX THR EADS WERE REPAIRED AND THE LP5 FITTING WAS REPLACED. ENGINE RUNUP AND LEAK CHECK WERE SATISFACTORY. 2 L 7 3 4F 4 F A3WE E2EA 1996041200378 19960412 00378 NE 1996 4 12 9607933204 2 19960409 A 7530 VBV AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE NR 2 ENGINE FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 304US 40 731686 DURING TAKEOFF ROLL, ENG NR 2 COMPRESSOR VANE FAULT ANNUNCIATED. ABORTED TAKEOFF AT 80 KNOTS, AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE VBV POSITION SENSOR AND RIGGED FOLLOW-UP ROD. FADEC AND TAKEOFF POWER CHECKS WERE ACCOM PLISHED. 2 L 7 2 4F 4 F RT A28NM E29NE 1996041200379 19960412 00379 NM 1996 4 12 9607942714 1 19960409 A 3260 INDICATION BOEING 727 7272S7 138407Z NM GEAR DOORS MALFUNCTIONED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 718RC 22344 DURING APPROACH ON GEAR EXTENSION, INDICATION INDICATED GEAR DOORS AND TAIL SKID NOT IN LANDING CONFIGURATION, EXECUTED GO-AROUND. SECOND GEAR EXTENSION INDICATIONS WERE ALL NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MCO MAINTENANCE PERFO RMED GEAR OPERATIONAL AND INDICATION CHECK CHECKED OK. 2 L 7 3 4F A3WE 1996041200380 19960412 00380 WP 1996 4 12 9607959750 1 19960409 A 3397 WIRE DOUG DC9 DC941 302207N WP CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 750NW 47114 DURING LINE CHECK INSPECTION, EMERGENCY LIGHTS WOULD NOT EXTINGUISH WHEN SWITCH WAS PLACED IN THE 'OFF' POSITION. MAINT ENANCE REPLACED A BATTERY PACK (B5-901), WIRE (L853A20) AND CIRCUIT BREAKER (B1-387) AND OPERATIONAL CHECK WAS NORMAL. 2 L 7 2 4F A6WE 1996041200381 19960412 00381 1996 4 12 96FDEA00756 2 19960410 A 7230 786877 FAN CASE AIRBUS 310 A310222 3930315 EU NR 1 ENGINE WORN A A FDEA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 25 420FE 339 AFTER T/O, A/F VIB DEVELOPED AT 250 KTS/5000 FT STRAIGHT AND LEVEL. SLOWED TO 220 KTS VIB STOPPED, CLIMBED TO 23,000 FT A/S 250 VIB AGAIN AND SLOWING THROUGH 235 KTS VIB STOPPED. NO VIB BELOW 235 KTS, NO VIB THROUGH YOKE OR RUDDER PEDALS. ECAM STS NOT CAT 3/INCRS LDG DIST BY 1.1. FOUND FRONT NR 1 FAN CASE ASSY WORN, REMOVED AND REPLACED PER MM 72-23-01. RAN NR 1 ENG AND NO VIB, OK FOR SERVICE AND LEAK CHECK GOOD. REMOVED AND REPLACED FLEX LINE FOR HYD, PRESS CHECK GOOD. PERFORMED A/FLT SYS AND A/SELF TEST, NO FAULTS. 2 L 7 2 4F RT A35EU 1996041200383 19960412 00383 1996 4 12 96UAL900247 4 19960409 A 2565 D30664105 GIRT TUBE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE SLIDE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 410UA 463 SLIDE REMOVED FOR OVERHAUL. SLIDE HAD 3 HOLES ON THE LOWER SIDE OF THE GIRT INFLATION TUBE. REPAIRED SLIDE PER VENDORS MANUAL. 2 L 7 2 4F 4 F RT A28NM E40NE 1996041200385 19960412 00385 1996 4 12 DL72L960833 4 19960331 A 2565 146110016 SLIDE BOEING 727 727232 1384082 NM R 2 DOOR TORN WEBBING A DALA O OTHER O OTHER IN INSP/MAINT 1 SO 27 505DA 21307 ON PREFLIGHT, FOUND RT AFT SERVICE DOOR EMERGENCY SLIDE WEBBING AT GIRT BAR TORN. REPLACED SLIDE. 2 L 7 3 4F A3WE 1996041200386 19960412 00386 NM 1996 4 12 DL72S960805 1 19960408 A 5330 SKIN BOEING 727 727232 1384082 NM FWD OF L1 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 543DA 22392 FOUND ON A2 LETTER CHECK, L1 DOOR UPPER AND LOWER HINGE CUTOUTS CRACKED, UPPER .5 INCH LOWER .875 INCH. REPAIRED PER MM 53-30-0. 2 L 7 3 4F A3WE 1996041200387 19960412 00387 NM 1996 4 12 DL72S960806 1 19960408 A 5754 SKIN BOEING 727 727232 1384082 NM NR 7 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 543DA 22392 FOUND ON A2 LETTER CHECK, 1 INCH VISIBLE CRACK ON NR 7 SLAT COVE SKIN SUPPORT ANGLE. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1996041200388 19960412 00388 NM 1996 4 12 DL72S960807 1 19960408 A 2760 EE824184511 ROD END BOEING 727 727232 1384082 NM WS 950 BROKEN A A DALA O OTHER F FLT CONT AFFECTED LD LANDING 1 SO 27 520DA 21471 WHEN SPEEDBRAKES APPLIED ON LANDING, AIRCRAFT ROLLED TO RIGHT. FOUND NR 2 LEFT OUTBD SPOILER NOT DEPLOYING. FURTHER IN VESTIGATION FOUND ROD END BROKEN REF IPC 27-10-0- 22B ITEM 5. MAINT FROM ATL REPLACED ROD END AND OPS CHECK OK. 2 L 7 3 4F A3WE 1996041200389 19960412 00389 NM 1996 4 12 DL72S960815 1 19960331 A 5330 SKIN BOEING 727 727225 1384077 NM BS 900 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 LT FUSELAGE SKIN GOUGED JUST AFT OF STA 900 BETWEEN STR 21 AND 22. REPAIRED PER SRM 53-30-3. 2 L 7 3 4F A3WE 1996041200390 19960412 00390 NM 1996 4 12 DL72S960816 1 19960331 A 3211 TRUNNION BOEING 727 727225 1384077 NM LT MLG GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 LT MLG FWD TRUNNION I/B SUPPORT FITTING GOUGED LOWER SURFACE. REPAIRED PER BOEING DWG 65-19296-15. 2 L 7 3 4F A3WE 1996041200391 19960412 00391 NM 1996 4 12 DL72S960817 1 19960408 A 5730 PANEL BOEING 727 727225 1384077 NM NR 4 FLAP TRACK CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 NR 4 FLAP TRACK I/B CLOSE OUT FAIRING IS CRACKED OUT AT FASTENER HOLE. REPLACED PANEL. 2 L 7 3 4F A3WE 1996041200392 19960412 00392 NM 1996 4 12 DL72S960818 1 19960401 A 5311 TEE CLIP BOEING 727 727225 1384077 NM BS 1110 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 SKIN BULGED AT STA 1110 STR 27L. REPLACED FRAME TO SKIN ATTACH CLIP PER MM 53-11. 2 L 7 3 4F A3WE 1996041200393 19960412 00393 NM 1996 4 12 DL72S960819 1 19960405 A 3210 WALKING BEAM BOEING 727 727225 1384077 NM LT MLG CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 LT MLG WALKING BEAM HAD HEAVY CORROSION ON THE LOWER SURFACE. REPAIR PER ERA NR 303405-14. 2 L 7 3 4F A3WE 1996041200394 19960412 00394 NM 1996 4 12 DL72S960820 1 19960405 A 5313 STRINGER BOEING 727 727225 1384077 NM BS 1173 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 STR 27L HAS HEAVY CORROSION APPROX FS 1173. REPAIRED PER ERA 303400-14. 2 L 7 3 4F A3WE 1996041200395 19960412 00395 NM 1996 4 12 DL72S960821 1 19960404 A 5320 DOOR FRAME BOEING 727 727225 1384077 NM C 2 DOOR CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 C-2 FWD DOOR FRAME CORRODED AT LOWER STOP FITTING. REPAIRED PER ERA 303392-14. 2 L 7 3 4F A3WE 1996041200396 19960412 00396 NM 1996 4 12 DL72S960822 1 19960404 A 5311 FRAME BOEING 727 727225 1384077 NM RT FUSELAGE CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 CORROSION ON THE FRAME FWD OF PANEL 3355. REPAIR PER SRM 51-40-3. 2 L 7 3 4F A3WE 1996041200397 19960412 00397 NM 1996 4 12 DL72S960823 1 19960404 A 5311 FRAME BOEING 727 727225 1384077 NM FUSELAGE CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 CORROSION ON THE FRAME FWD OF PANEL 3455. REPAIRED PER SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 1996041200398 19960412 00398 NM 1996 4 12 DL72S960824 1 19960403 A 5320 WEB BOEING 727 727225 1384077 NM BS 270 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 A 4 INCH CRACK IN NOSE W/W PRESSURE DECK SKIN AT STA 270 AT APPROX RBL 14. REPAIRED PER SRM 53-10-9. 2 L 7 3 4F A3WE 1996041200399 19960412 00399 NM 1996 4 12 DL72W960808 1 19960408 A 5400 S-DUCT SKIN BOEING 727 727247 138408F NM NR 2 ENGINE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2810W 20648 FOUND ON MV1 CHECK, TIME LIMITED REPAIR INSTALLED, 1 INCH CRACK IN S-DUCT HOUSING RT SIDE JUST FWD OF SADDLE PANEL, VERT STAB FRONT SPAR. INSTALLED PERMANENT REPAIR PER M/M 54-30-0 PG 801 FIG 802. 2 L 7 3 4F A3WE 1996041200400 19960412 00400 NM 1996 4 12 DL73S960799 1 19960408 A 3230 MODULE BOEING 737 737232 1384475 NM LANDING GEAR NOT SEATED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 321DL 23093 AIRCRAFT RETURNED CVG AIR TURNBACK, LANDING GEAR WOULD NOT RETRACT. RESEATED LANDING GEAR MODULE AND SWUNG GEAR, ALL CH ECKS NORMAL. 2 L 7 2 4F RT A16WE 1996041200401 19960412 00401 1996 4 12 DL757960830 2 19960407 A 7261 5007436K OIL PUMP BOEING 757 757232 1384965 NM NR 1 ENGINE CRACKED A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 644DL 23998 LT ENG OIL QTY WENT FROM 21 TO 15, CVG LAS OIL POOLED AND DRIPPING FROM BOTTOM OF COWLING. FOUND NR 1 ENGINE OIL PUMP H OUSING CRACKED. REPLACED PUMP, OPERATION NORMAL. 2 L 7 2 4F RT A2NM 1996041200402 19960412 00402 NM 1996 4 12 DL767960829 1 19960407 A 2710 A2864010 ACTUATOR BOEING 767 767232 1385132 NM RT AILERON CONTL FAILED A DALA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 27 102DA 22214 DURING FLT CONTROL CHECK, AILERON AND ELEVATOR FELT VERY HEAVY. AIRCRAFT RETURNED TO BLOCK. REPLACED RT LCCA, RIGGED A ND LEAK CHECKED, OPERATION NORMAL. 2 L 7 2 4F RT A1NM 1996041200403 19960412 00403 WP 1996 4 12 DLL10960812 1 19960408 A 3350 5165741 POWER SUPPLY LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1732D 193C1213 D-ZONE EMERGENCY TRACK LIGHTING INOP. REPLACED BOTH RT SIDE POWER SUPPLYS, CHECKS OK. 2 L 7 3 4F A23WE 1996041200404 19960412 00404 WP 1996 4 12 DLL14960828 1 19960405 A 3260 450100109 CONTROL LKHEED 1011 1011385115 5265015 WP LANDING GEAR FAILED A DALA O OTHER N FALSE WARNING TO TAKEOFF 1 SO 27 1739D 193C1237 AFTER TAKEOFF, WHEN LANDING GEAR HANDLE PLACED IN NEUTRAL RECEIVED INTRANSIT LIGHT ON PILOT PANEL, LR, NOSE AND TAIL SKI D LIGHT. REPLACED GEAR HANDLE ASSEMBLY, OPERATION NORMAL. 2 L 7 3 4F A23WE 1996041200405 19960412 00405 WP 1996 4 12 DLL17960801 1 19960408 A 3350 5165741 P0WER SPPLY LKHEED 1011 10113853 5265020 WP CABIN INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 768DL 193H1216 EXTERIOR EVACUATION LIGHT AT 1L INOP WITH COCKPIT SWITCH ON. REPLACED BATTERY PACK AT 1L, LIGHTS CHECK GOOD. 2 L 7 3 4F A23WE 1996041200406 19960412 00406 NM 1996 4 12 DLM88960827 1 19960405 A 3350 LIGHT DOUG MD88 MD88 3023688 NM CABIN DAMAGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 930DL 49717 ON PREFLIGHT, EMERGENCY EXIT SIGN ON CEILING AT ROW 38 WILL NOT LIGHT AND DAMAGED ON BACK SIDE. REPLACED SIGN ASSEMBLY, OPERATION NORMAL. 2 L 7 2 4F RT A6WE 1996041200407 19960412 00407 NM 1996 4 12 DLM88960831 1 19960404 A 2740 SPRING DOUG MD88 MD88 3023688 NM STAB TRIM MISSING A DALA O OTHER F FLT CONT AFFECTED CL CLIMB 1 SO 27 904DL 49535 LEFT CAPTAINS AUTO PILOT COMMANDED AN UNCONTROLLED NOSE UP TRIM DURING CLIMB. ADDITIONALLY, IT COMMANDED A CLIMB WHEN L EVEL AT CRUISE. FOUND DETENT ROLLER SPRING MAIN HORIZONTAL STAB TRIM RELAY UPPER SPRING MISSING. REPLACED SPRING AND R AN STAB, OPERATION NORMAL. 2 L 7 2 4F RT A6WE 1996041200408 19960412 00408 NM 1996 4 12 DLM88960832 1 19960331 A 2560 LANYARD DOUG MD88 MD88 3023688 NM DOOR SLIDE BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 979DL 53266 ON PREFLIGHT, FWD GALLEY DOOR SLIDE LANYARD FOUND BROKEN. REPLACED LANYARD. 2 L 7 2 4F RT A6WE 1996041200409 19960412 00409 WP 1996 4 12 SCNA96040 1 19960406 A 2611 72130001010 DETECTOR DOUG DC10 DC1010 3022110 WP RT FWD LAV FAULTY A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 573SC 46905 THE RIGHT FORWARD LAVATORY CAUSED A CONTINUOUS AURAL WARNING IN THE GALLEY. REMOVED AND REPLACED SMOKE DETECTOR, OPS CH ECKED GOOD. 2 L 7 3 4F A22WE 1996041200428 19960412 00428 EU 1996 4 12 96ZZZX1676 1 19960116 A 6410 704A33633171 HINGE SNIAS 350 AS350B2 8680813 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 6099P 17 2818 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996041200431 19960412 00431 EU 1996 4 12 96ZZZX1679 1 19960118 A 6220 117775P BALL JOINT SNIAS 350 AS350B2 8680813 EU STARFLEX WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 94LG 642 2728 TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 3 EACH NEW UNTS, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996041200439 19960412 00439 WP 1996 4 12 96ZZZX1687 1 19960308 A 2612 FIRE WARNING DOUG DC8 DC851 3021920 WP NR 1 ENGINE MALFUNCTIONED A FXLA O OTHER N FALSE WARNING DE DESCENT 1 SO 19 507DC 45855 ON DESCENT INTO MIAMI, NR 1 ENGINE FIRE WARNING ILLUMINATED MOMENTARILY AND CEASED. LANDED MIAMI WITHOUT INCIDENT. INS PECTION REVEALED NO EVIDENCE OF FIRE OR OVERHEAT CONDITION. RAN ENGINE, CHECKED FIRE WARNING AND PNEUMATIC SYSTEM AND C OULD NOT DUPLICATE REPORTED CONDITION. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4A25 1996041200441 19960412 00441 NE 1996 4 12 96ZZZX1690 2 19960317 A 7261 214138022 OIL TUBE 200305004 CNDAIR CL600 CL6001A11 1900302 EA LYC ALF502 ALF502L2 41580 NE INBOARD CHAFED A A WH6A A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CR CRUISE 1 NE 03 601WW 1639 1639 1076 LF03146 FIRE WARNING INDICATION ON RT ENGINE AND REPORTED THROTTLE POWER LESSENED WHILE AT CRUISE. RESTARTED, THROTTLE WARNING WENT OUT. UNSCHEDULED LANDING AT ICT. ENGINE WAS NOT SHUT DOWN. FOUND FUEL DRAIN LINE FROM FUEL FLOW DIVIDER DISCONNE CTED AND NR 4 AND NR 5 BEARING PACKAGE OIL INLET TUBE CHAFED THROUGH DUE TO LOOSE BOLTS IN 4TH TURBINE NOZZLE VANE HITTI NG TUBE. RETORQUED AND RESAFTIED ALL RETENSION VANE BOLTS. REPLACED CHAFED OIL TUBE. C/W ALLIED SIGNAL SB ALF 502-72- 008, REV 8, AD 80-22-53, SB ALF 502-72-0221 WELDS RETENSION BOLT HEADS AS A SAFETY. 2 L 7 2 4F 4 F RT A21EA E6NE 1996041200442 19960412 00442 NM 1996 4 12 96ZZZX1691 1 19960329 A 3210 LANDING GEAR BOEING 737 737201 1384454 NM RT MLG DAMAGED A F3LA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 03 214AU 64078 20214 ABQ - BLOCK TURN-BACK. FLIGHT CREW REPORTED APPARENT RT MLG DAMAGE. MAINTENANCE FOUND NR 4 MAIN WHEEL, BRAKE, AND AXLE ASSYS DAMAGED. REPLACED THE LOWER STRUT ASSY, NR 4 BRAKE ASSY, NR 3 AND NR 4 TIRE ASSYS, WHEEL BEARING, WHEEL BEARING THRUST WASHER AND NUT, TRANSDUCER AND AXLE NUT, AND REPAIRED WIRING HARNESS AND CANNON PLUG. THE CAUSE OF DAMAGE IS UND ER INVESTIGATION. SUPPLEMENTAL INFORMATION WILL BE SUBMITTED AS ADDITIONAL INFORMATION IS OBTAINED. C-CHECK: 1242.5 H RS. (X) 2 L 7 2 4F A16WE 1996041200443 19960412 00443 NM 1996 4 12 96ZZZX1692 1 19960314 A 2822 2172005 BOOST PUMP BOEING 737 737222 1384473 NM RIGHT MALFUNCTIONED A ZZDA A UNSCHED LANDING P NO WARNING INDICATION CR CRUISE 1 SO 15 144AW 19074 MCO - FLT 570 - DEPARTED MCO TO ROCHESTER, NY. DURING FLIGHT, CREW REPORTED A FUEL IMBALANCE OCCURRED OUT OF RT MAIN TA NK. AIRCRAFT WAS DIVERTED TO GSP. MAINTENANCE AND FLT CREW WERE DISPATCHED TO GSP TO RECOVER A/C. SYSTEM WAS CHECKED BY MAINTENANCE. ALL SYSTEMS CHECKED NORMAL. A/C WAS FERRIED TO MCO. DURING FLT, CHIEF PILOT AND DIRECTOR OF OPERATION S AGAIN CHECKED SYSTEM. CHECK WAS NORMAL. FUEL BOOST PUMP AND CHECK VALVE REPLACED FOR PRECAUTIONARY REASON. NO FURTH ER INCIDENT OCCURRED. 2 L 7 2 4F A16WE 1996041200444 19960412 00444 NM 1996 4 12 96ZZZX1693 1 19960311 A 3020 693732053 CONTROL PANEL BOEING 737 7372L9 1384497 NM FLIGHT DECK SHORTED A ZZDA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 15 737Q M00567 21279 AFTER TAKEOFF, CREW TURNED ON THE ENGINE ANTI-ICE AND NOTICED ALL 3 BLUE ADVISORY LIGHTS FLICKERING ON THE NR 1 ENGINE S IDE. SMOKE STARTED APPEARING FROM THE PANEL. ANTI-ICE WAS SELECTED TO THE OFF POSITION AND THE CIRCUIT BREAKER WAS PUL LED. THE ACFT RETURNED TO BHM. NO EMERGENCY WAS DECLARED. CONTRACT MAINTENANCE (AMR COMBS) REMOVED PANEL AND VERIFIED THE DAMAGE WAS CONTAINED WITHIN THE PANEL (PN 69-37320-53). RECEIVED SERVICEABLE PANEL AND INSTALLED. AIRCRAFT DEPART ED BHM WITH NO FURTHER INCIDENTS. 2 L 7 2 4F RT A16WE 1996041200445 19960412 00445 NM 1996 4 12 96ZZZX1694 1 19960229 A 5270 WARNING LIGHT BOEING 757 757225 1384959 NM LT EMER EXIT ILLUMINATED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 604AU 22199 MIA - FLT 538 - LEFT EMERGENCY DOOR (L3) WARNING LIGHT CAME ON DURING CLIMB-OUT FROM MIA. AIRCRAFT RETURNED TO FIELD. M AINTENANCE PERFORMED DOOR FIM PROCEDURE. NO PROBLEMS WERE FOUND. DOOR WAS CHECKED OPERATIONALLY AND NO PROBLEMS WERE N OTED. AIRCRAFT WAS RELEASED FOR SERVICE. REFERENCE: OPERATOR CONTROL NR USAABB96006A. 2 L 7 2 4F RT A2NM 1996041200446 19960412 00446 WP 1996 4 12 ASAA9680073 1 19960311 A 2910 7936906518 HYD LINE DOUG DC9 DC982 3022082 WP LT MLG BROKEN A ASAA K NONE K FLUID LOSS CR CRUISE 1 NM 01 931AS 49232 PDX - FLT 427 - AFTER ARRIVAL, CREW REPORTED THAT 3 MINUTES AFTER REACHING CRUISE AT FL 350 DEPARTING OAK, LOST RIGHT HY DRAULIC SYSTEM QUANTITY AND PRESSURE. LANDED WITHOUT INCIDENT. FOUND GOOSE STUCK IN LT MLG STRUT ASSY AND BROKEN HYDRA ULIC LINE TO THE LT MLG DOWNLOCK CYLINDER. REPLACED LINE AND SERVICED HYDRAULIC RESERVOIR. (X) 2 L 7 2 4F A6WE 1996041200447 19960412 00447 WP 1996 4 12 ASAA9680074 1 19960312 A 2520 FLOOR COVERING DOUG DC9 DC982 3022082 WP FWD GALLEY EXCESS MATERIAL A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 936AS 49363 SEA - FLT 511 - AFTER ARRIVAL, CREW REPORTED R1 DOOR HANDLE WAS DIFFICULT TO MOVE. FOUND GIRT BAR FITTING CONTACTING BO TTOM OF DOOR. REMOVED PORTION OF FORWARD GALLEY FLOOR COVERING MATERIAL, REINSTALLED GIRT BAR, AND RESEALED FLOOR. DOO R AND GIRT BAR OPERATE NORMALLY. (X) 2 L 7 2 4F A6WE 1996041200448 19960412 00448 NM 1996 4 12 AWXA960109 1 19960228 A 5241 65C340681 HINGE ASSY BOEING 737 737277 1384570 NM FWD GALLEY DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 PAE - FLT 3868 - DURING ROUTINE C-14 MAINTENANCE CHECK, FOUND FORWARD GALLEY DOOR UPPER HINGE GATE CRACKED. REPLACED UP PER GALLEY HINGE GATE PER SRM 51-30-2. (X) 2 L 7 2 4F RT A16WE 1996041200449 19960412 00449 NM 1996 4 12 AWXA960110 1 19960229 A 5330 SKIN BOEING 737 737277 1384570 NM CARGO DOORWAY CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 PAE - FLT 3868 - DURING ROUTINE C-14 MAINTENANCE CHECK, FOUND POSSIBLE DELAMINATION ON FORWARD CARGO DOORWAY, FORWARD LO WER CORNER. PERFORMED ND1 TO MARK DISBOND. REMOVED DISBOND. FABRICATED AND INSTALLED REPAIR PER AWA ER NR 2-53-33-14, SRM 51-40-2. LOCATION: BS 450, RBL 36, WL 154. (X) 2 L 7 2 4F RT A16WE 1996041200450 19960412 00450 NM 1996 4 12 AWXA960111 1 19960229 A 5313 693535214 STRINGER BOEING 737 737277 1384570 NM BS 500 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 PAE - FLT 3868 - DURING ROUTINE C-14 MAINTENANCE CHECK, FOUND CORROSION ON INSIDE OF STR 27L, BS 500 TO BS 500B. REMOVE D STR 27L FROM BS 370 - BS 540. INSTALLED NEW STRINGER. CUT HOLE AT BS 445 - BS 465, STR 27L FOR ACCESS. FABRICATED A ND INSTALLED REPAIR DOUBLER PER SRM 53-10-3, ARM 53-30-3. (X) 2 L 7 2 4F RT A16WE 1996041200451 19960412 00451 NM 1996 4 12 AWXA960112 1 19960229 A 5330 SKIN BOEING 737 737277 1384570 NM BS 400 DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 182AW 22649 PAE - FLT 3868 - DURING ROUTINE C-14 MAINTENANCE CHECK, FOUND LARGE DENT IN SKIN AT BS 400, BETWEEN STR 23 AND STR 24 RT . REMOVED 1 INCH BY 7 INCH DAMAGED AREA. FABRICATED AND INSTALLED REPAIR. ALL PER SRM 53-30-3. (X) 2 L 7 2 4F RT A16WE 1996041200452 19960412 00452 NM 1996 4 12 AWXA960134 1 19960317 A 3350 FUSE BOEING 737 73733A 1384673 NM CABIN FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 173AW 23632 PHX - FLT 0480 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS AT ROW 3 AND ROW 4 INOPERATIVE. REPLACED FUSE ON BATTERY PACK. (X) 2 L 7 2 4F RT A16WE 1996041200453 19960412 00453 NM 1996 4 12 AWXA960135 1 19960315 A 3350 1000679 LIGHT BOEING 737 7373G7 1384595 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 151AW 23219 PHX - FLT 0480 - DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 10 EMERGENCY LIGHT BROKEN. REPLACED EMERGENCY LIGHT ASSEMB LY. (X) 2 L 7 2 4F RT A16WE 1996041200454 19960412 00454 EU 1996 4 12 AWXA960156 1 19960322 A 3350 321430 BATTERY PACK AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 28 622AW 3423 054 PHX\SNA - FLT 0657 - EMERGENCY LIGHTING ALL CAME ON IN CABIN DURING TAXI AND IN-FLIGHT. RESET WHEN EMERGENCY EXIT LIGHT SWITCH IS CYCLED ON AND OFF. REMOVED AND REPLACED LEFT AFT BATTERY PACK. OPERATIONS CHECK IS GOOD. (X) 2 L 7 2 4F RT A28NM 1996041200455 19960412 00455 NM 1996 4 12 BJNA96302 1 19960318 A 3350 6104781 BATTERY PACK BOEING 737 737214 138446R NM CABIN DISCHARGED A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 457TM 20156 LEFT EMERGENCY OVERWING EXIT LIGHT WILL NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACK IW MM 33-51-41. OPS CHECK GO OD. (X) 2 L 7 2 4F A16WE 1996041200456 19960412 00456 WP 1996 4 12 GRAA96 1 19960321 A 2131 21171802 PRESS CONTROLLER DOUG DC9 DC987 3022087 WP E/E COMPARTMENT FAILED A GRAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 11 1075T 49724 RNO - ON CLIMB-OUT, AIRCRAFT HAD THE AUTOPRESSURIZATION SYSTEM FAIL. AIRCRAFT RETURNED TO RNO WITHOUT FURTHER OCCURRENC E. MAINTENANCE DEFERRED THE AUTOPRESSURIZATION SYSTEM IAW MEL: 21-24. THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A6WE 1996041200457 19960412 00457 WP 1996 4 12 GRAA9621 1 19960323 A 3350 100865 POWER SUPPLY DOUG DC9 DC987 3022087 WP CABIN INOPERATIVE A GRAA K NONE L NO TEST IN INSP/MAINT 1 WP 11 1075T 49724 RNO - LINE MAINTENANCE DISCOVERED THE FLOOR PROXIMITY, EMERGENCY LIGHTS AT ROW 2 AND ROW 3 FAILED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM . SYSTEM OPERATIONALLY CHECKED NORMAL. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A6WE 1996041200458 19960412 00458 WP 1996 4 12 ORJA96017 1 19960318 A 3350 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 822RA 49932 AFT GALLEY OVERHEAD EMERGENCY LIGHTS INOPERATIVE. INSTALLED NEW BATTERIES IN CHARGER. OPS CHECK NORMAL. (X) 2 L 7 2 4F A6WE 1996041200459 19960412 00459 EU 1996 4 12 RAIA960308 1 19960308 A 3222 100A702957 O-RING BAG JETSTM JETSTM3201 1500217 EU NLG STRUT LEAKING A RAIA O OTHER J WARNING INDICATION CL CLIMB 1 CE 03 429AM 10581 10581 879 STL - FLT 7498 - NOSE GEAR WOULD NOT RETRACT UPON DEPARTURE. MAINTENANCE REPLACED NOSE GEAR TOP CAP O-RING, SERVICED GE AR, PERFORMED GEAR SWING, OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4T RT A56EU 1996041200460 19960412 00460 EU 1996 4 12 RAIA960309 1 19960307 A 7334 1103P0645 FUEL PRESS SW BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 871JX 5675 871 66125 FAT - FLT 4766 - LEFT FUEL PRESSURE CAPTION ILLUMINATED. MAINTENANCE REMOVED AND REPLACED LEFT FUEL PRESSURE SWITCH. P ERFORMED GROUND RUNS, OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4T 4 T RT A56EU E4WE 1996041200461 19960412 00461 EU 1996 4 12 RAIA960310 1 19960309 A 2422 PC125123B INVERTER JETAIR JETSTM JETSTM4101 1500501 EU RIGHT FAULTY A RAIA O OTHER J WARNING INDICATION CL CLIMB 1 CE 03 557HK 777 41074 JFK - FLT 7718 - RIGHT INVERTER FAILED. MAINTENANCE REPLACED RIGHT INVERTER, OPERATION CHECK GOOD. (X) 2 L 7 2 4T RT A41NM 1996041200462 19960412 00462 EU 1996 4 12 RAIA960311 1 19960312 A 5270 SP4594 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU AFT BAGGAGE OUT OF ADJUST A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 556HK 1096 41073 BOS - FLT 7705 - CARGO DOOR WARNING LIGHT ILLUMINATED ON TAKEOFF. MAINTENANCE ISSUED DMI 52-3, MAINTENANCE LATER CLEARE D DMI BY ADJUSTING DOOR MICROSWITCH, OPERATION CHECK GOOD. (X) 2 L 7 2 4T RT A41NM 1996041200463 19960412 00463 EU 1996 4 12 RAIA960312 1 19960310 A 7712 3036927 TQ SIGNAL COND AEROSP ATR42 ATR42300 8680920 EU LT ENGINE DIRTY A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O N OTHER FALSE WARNING TO TAKEOFF 1 CE 03 423TE 14741 11606 119 STL - FLT 7174 - ATPCS WILL NOT ARM. MAINTENANCE CLEANED LEFT ENGINE TORQUE SIGNAL CONDITIONER CONNECTIONS, OPERATIONAL CHECK GOOD. (X) 2 H 7 2 4T RT A53EU 1996041200464 19960412 00464 EU 1996 4 12 RAIA960313 1 19960310 A 7712 3036927 TQ SIGNAL COND AEROSP ATR42 ATR42300 8680920 EU RT ENGINE DIRTY A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 423TE 8561 119 STL - FLT 7174 - ATPCS WILL NOT ARM. MAINTENANCE CLEANED LEFT ENGINE TORQUE SIGNAL CONDITIONER CONNECTIONS, OPERATIONAL CHECK GOOD. (X) 2 H 7 2 4T RT A53EU 1996041200465 19960412 00465 EU 1996 4 12 RAIA960314 1 19960311 A 7797 WIRE BAG JETSTM JETSTM3201 1500217 EU LT ENGINE BROKEN A RAIA O OTHER N FALSE WARNING CL CLIMB 1 CE 03 862JX 9744 862 FAT - FLT 4710 - LEFT ENGINE EGT FLUCTUATION IN-FLIGHT. MAINTENANCE REPAIRED BROKEN WIRE NR KR40AL AT BULKHEAD CONNECTO R. OPERATIONAL CHECK GOOD DURING GROUND RUNS. (X) 2 L 7 2 4T RT A56EU 1996041200466 19960412 00466 WP 1996 4 12 RAIA960315 2 19960311 A 7530 8961153 GASKET BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 343TE 955 66161 STL - FLT 7031 - LEFT ENGINE TORQUE FLUCTUATES. MAINTENANCE REPLACED THE BLEED AIR GASKET, GROUND RUNS GOOD. (X) 2 L 7 2 4T 4 T RT A56EU E4WE 1996041200467 19960412 00467 EU 1996 4 12 RAIA960316 1 19960314 A 3230 185916 DNLK ACT BOLT BAG JETSTM JETSTM3201 1500217 EU NLG FAILED A RAIA A UNSCHED LANDING P NO WARNING INDICATION LD LANDING 1 CE 03 426AM 10876 874 STL - FLT 7544 - NOSE GEAR DID NOT INDICATE DOWN AND LOCKED. MAINTENANCE FOUND NOSE DOWNLOCK ACTUATOR HOOK BOLT HAD FAI LED. MAINTENANCE REPLACED NOSE DOWNLOCK ACTUATOR AND HOOK ASSY. PERFORMED GEAR SWINGS, OPERATIONAL CHECKS GOOD. (X) 2 L 7 2 4T RT A56EU 1996041200468 19960412 00468 NE 1996 4 12 RAIA960317 3 19960314 A 6111 SFA13M10A BLADE AEROSP ATR42 ATR42300 8680920 EU HAMSTD 14SF 14SF5 NE RT PROP NR 2 OUT OF BALANCE A RAIA A UNSCHED LANDING O E OTHER VIBRATION/BUFFET CR CRUISE 1 CE 03 421TE 10955 1971 102 890522 STL - FLT 7402 - RIGHT ENGINE IN-FLIGHT VIBRATION. MAINTENANCE REPLACED RIGHT PROPELLER NR 2 BLADE. PERFORMED PROPELLE R BALANCE AND GROUND RUNS, OPERATIONAL CHECK GOOD. (X) 2 H 7 2 4T RT A53EU 6 C P7NE 1996041200469 19960412 00469 EU 1996 4 12 RAIA960318 1 19960314 A 7722 8974694 SHORT LEAD BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 340TE 5460 939 STL - FLT 7025 - LEFT ENGINE EGT DROPPED TO ZERO ON TAKEOFF. MAINTENANCE REPAIRED SHORT LEAD, GROUND RUNS GOOD. (X) 2 L 7 2 4T RT A56EU 1996041200470 19960412 00470 EU 1996 4 12 RAIA960319 1 19960313 A 5270 SP4594 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU CARGO BAY OUT OF ADJUST A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 03 557HK 804 41074 BOS - FLT NR 7707 - CARGO DOOR WARNING ILLUMINATED DURING TAKEOFF ROLL. MAINTENACNE ISSUED DMI 52-3. MAINTENANCE LATER CLEARED BY ADJUSTING DOOR MICROSWITCH. (M) 2 L 7 2 4T RT A41NM 1996041200471 19960412 00471 EU 1996 4 12 RAIA960320 1 19960313 A 5270 SP4594 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGGAGE BAY OUT OF ADJUST A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 552HK 1988 41057 BHM - FLT NR 7461 - CARGO DOOR WARNING ILLUMINATED DURING TAXI OUT. MAINTENANCE ISSUED DMI 52-3. MAINTENANCE LATER CLE ARED DMI BY ADJUSTING DOOR MICROSWITCH, OPERATION CHECK GOOD. (M) 2 L 7 2 4T RT A41NM 1996041200472 19960412 00472 WP 1996 4 12 RAIA960321 2 19960313 A 7530 8961153 GASKET BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CE 03 340TE 5455 939 66224 STL - FLT 7496 - LEFT ENGINE LOST POWER ON TAKEOFF ROLL. MAINTENANCE REPLACED BLEED-AIR GASKET, GROUND RUNS GOOD. (X) 2 L 7 2 4T 4 T RT A56EU E4WE 1996041200473 19960412 00473 EU 1996 4 12 RAIA960323 1 19960320 A 7712 94959411 TTL CONNECTOR BAG JETSTM JETSTM3201 1500217 EU RT ENGINE DIRTY A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 972JX 5589 972 FAT - FLT 4750 - RIGHT ENGINE TORQUE FLUCTUATION IN FLIGHT. MAINTENANCE DEFERRED RIGHT ENGINE TTL PER MEL 76-2. MAINTE NANCE CLEARED DMI BY CLEANING TTL CONNECTOR, PERFORMED GROUND RUNS OPERATIONAL CHECKS GOOD. (M) 2 L 7 2 4T RT A56EU 1996041200474 19960412 00474 NM 1996 4 12 USAA960323 1 19960320 A 5315 FLOOR BEAM BOEING 737 737401 1384701 NM BS 947 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 19862 23992 INT - DURING 'Q-1' CHECK VISUAL INSPECTION, FOUND 4 AREAS 1 INCH BY 1 INCH CORRODED AREAS FLOOR BEAM BS 947, LBL 4 - RBL 11. INSTALLED T-CAP AND REPAIR ANGLES. REPAIRED PER SRM 53-00-051 AND EA 40947. (X) 2 L 7 2 4F RT A16WE 1996041200475 19960412 00475 NM 1996 4 12 USAA960324 1 19960320 A 5315 FLOOR BEAM BOEING 737 737401 1384701 NM BS 967 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 19862 23992 INT - DURING 'Q-1' CHECK VISUAL INSPECTION, FOUND .75 INCH CORROSION FLOOR BEAM BS 967, RBL 42. CUT OUT CORRODED AREA, FABRICATED AND INSTALLED REPAIR ANGLES AND FILLER. REPAIRED PER SRM 53-60-51, FIGURE 203. (X) 2 L 7 2 4F RT A16WE 1996041200476 19960412 00476 NM 1996 4 12 USAA960325 1 19960320 A 5315 FLOOR BEAM BOEING 737 737401 1384701 NM BS 986.5 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 INT - DURING 'Q-1' CHECK, VISUAL INSPECTION FOUND 10 AREAS 1 - 2 INCH SQUARES OF CORROSION FLOOR BEAM (FLOOR BOARD HOLES ) BS 986.5, RBL 46 - LBL 46. CUT OUT CORRODED UPPER T-CAP AND REPLACED T-CAP, PLACING A SPLICE AT LBL 7, REPAIRED PER E A 40946. (X) 2 L 7 2 4F RT A16WE 1996041200477 19960412 00477 NM 1996 4 12 USAA960326 1 19960320 A 5315 FLOOR BEAM BOEING 737 737401 1384701 NM BS 344 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 19862 23992 INT - DURING 'Q-1' CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA BS 344 FLOOR BEAM LBL 9 INCH AND LBL 21 INCH. INSTALLED T-CAP FROM RBL 17 TO LBL 36, REPAIRED PER T.R. 53-10-03. CORROSION LEVEL 2. CORROSION TASK NR C53-10 7-02. (X) 2 L 7 2 4F RT A16WE 1996041200478 19960412 00478 NM 1996 4 12 USAA960327 1 19960320 A 5315 FLOOR BEAM BOEING 737 737401 1384701 NM BS 328 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 23992 INT - DURING 'Q-1 CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY 2 INCH CORRODED AREAS BS 328 FLOOR BEAM, RBL 14 INCH TO RBL 56 INCH. SPLICED SECTION AND REPAIRED PER SRM 53-10-01. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2 L 7 2 4F RT A16WE 1996041200479 19960412 00479 NM 1996 4 12 USAA960328 1 19960320 A 5315 FLOOR BEAM BOEING 737 737401 1384701 NM BS 312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 425US 19862 23992 INT - DURING 'Q-1' CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA, BS 312, FLOOR BEAM BL ZERO. CUT OUT C ORRODED SECTION OF UPPER CHORD FROM LBL 38 TO RBL 25 AND SPLICED IN NEW CHORD SECTION. REPAIRED PER T.R. 53-10-03. COR ROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2 L 7 2 4F RT A16WE 1996041200480 19960412 00480 NM 1996 4 12 USAA960329 1 19960321 A 5320 FLOOR SUPPORT BOEING 737 7374B7 1384702 NM FS 328 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 19349 24548 CLT - INSPECTION VISUALLY FOUND SURFACE LEVEL 1 CORROSION .50 INCH IN DIAMETER AROUND NUT CLIP HOLES LOCATED AT FS 328 - RBL 12 TO RBL 56. CUT CORRODED T-CAP OFF AND REINSTALLED SAME PER BOEING SRM 53-10-03. (X) 2 L 7 2 4F RT A16WE 1996041200481 19960412 00481 NM 1996 4 12 USAA960330 1 19960321 A 5320 FLOOR SUPPORT BOEING 737 7374B7 1384702 NM FS 344 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 19349 24548 CLT - INSPECTION VISUALLY FOUND LEVEL 1 CORROSION AROUND SCREW HOLES 30 INCH LENGTH ON TOP OF BEAM LOCATED AT STA 344 - 181 BL TO 12 RBL. CUT CORRODED BEAM T-CAP OFF AND REPLACED PER BOEING SRM 53-10-51. (X) 2 L 7 2 4F RT A16WE 1996041200482 19960412 00482 NM 1996 4 12 USAA960331 1 19960321 A 5320 FLOOR SUPPORT BOEING 737 7374B7 1384702 NM FS 986.5 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 19349 24548 CLT - INSPECTION VISUALLY FOUND A LEVEL 1 SURFACE CORROSION MEASURING 3 INCH BY 85 INCH LOCATED AT BEAM STA 986.5 - LBL 29.0 TO RT AFT SERVICE DOOR. REPAIRED UPPER FLANGE (INSTALLED REPAIR FLANGE) PER USAIR TYPICAL REPAIR 53-10-05. (X) 2 L 7 2 4F RT A16WE 1996041200483 19960412 00483 NM 1996 4 12 USAA960332 1 19960321 A 5315 FLOOR BEAM BOEING 737 7374B7 1384702 NM BS 947-1008 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 19349 24548 CLT - INSPECTION VISUALLY FOUND LEVEL 2 CORROSION MEASURING 3 INCH BY 60 INCH LOCATED AT LT ENTRY AFT DOOR THRESHOLD LOC ATED AT STA 947 THROUGH STA 1006. INSTALLED REPLACEMENT ANGLE PER BOEING SRM 51-10-02. (X) 2 L 7 2 4F RT A16WE 1996041200484 19960412 00484 NM 1996 4 12 USAA960333 1 19960321 A 5330 65C2728713 SKIN BOEING 737 737201 1384454 NM BS 328 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AU 53066 22798 ROA - DURING 'CX-4' CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK IN SKIN AND BEAR STRAP FORWARD SERVICE DOOR CUT OUT (LOW ER AFT CORNER) STA 328. REPAIRED DOUBLER, PN 65C27287-13, REPAIR DOCUMENT T.R. 53-10-19, REV A. (X) 2 L 7 2 4F A16WE 1996041200485 19960412 00485 NE 1996 4 12 USAABB96008 2 19960309 A 7261 TOWER SHAFT SEAL BOEING 757 757225 1384959 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE FAILED A USAA A E UNSCHED LANDING ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 19 618AU 22210 30540 SMF - FLT 68 - AFTER TAKEOFF FROM SFO, CREW NOTED LOSS OF OIL FROM LT ENGINE. CREW SHUT DOWN ENGINE. FLIGHT DIVERTED T O SMF AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE TOWER SHAFT SEALS. (X) 2 L 7 2 4F 4 F RT A2NM E12EU 1996041200486 19960412 00486 NE 1996 4 12 USAABB96009 2 19960317 A 7230 COMPRESSOR BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE STALLED A A USAA A UNSCHED LANDING B R SMOKE/FUMES/ODORS/SPARKS PARTIAL RPM/PWR LOSS CR CRUISE 1 EA 19 620AU 27199 LAX - FLT 41 - AT FL 240, RT ENGINE EXPERIENCED COMPRESSOR STALL. PASSENGER REPORTED SMOKE AND FLAMES FROM RT ENGINE, A ND ACRID SMOKE FILLED THE CABIN. SMOKE DISSIPATED QUICKLY. CREW DECLARED AN EMERGENCY AND LANDED WITH NO FURTHER INCID ENT. MAINTENANCE PERFORMED A BORESCOPE OF THE COMPRESSOR, COMBUSTION CHAMBER, AND TURBINE NOZZLE SECTIONS OF THE RT ENG INE. FAN BLADE TAP TEST AND CHIP DETECTOR INSPECTION WERE COMPLETED. NO DISCREPANCIES WERE FOUND. AIRCRAFT WAS RETURN ED TO SERVICE. (X) 2 L 7 2 4F 4 F RT A2NM E12EU 1996041200487 19960412 00487 WP 1996 4 12 USAAD96027A 1 19960229 A 3230 RETRACT MECH DOUG DC9 DC931 3022065 WP NLG MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 980VJ 48156 BNA - FLT 1426 - UPON GEAR RETRACTION, CREW GOT TWO GREEN LIGHTS ON THE MAIN GEAR AND RED LIGHT ON THE NOSE GEAR. CREW ALSO HEARD A LOUD NOISE FROM THE NOSE GEAR AREA. RETURNED TO FIELD. (X) 2 L 7 2 4F A6WE 1996041200488 19960412 00488 1996 4 12 USAAD96031 4 19960319 A 3417 2587400437 ADC DOUG DC9 DC931 3022065 WP LEFT FAILED A USAA A UNSCHED LANDING O OTHER AP APPROACH 1 EA 19 939VJ 30211 48120 DAY - FLT 282 - ON DESCENT INTO IND, CAPTAIN'S ALTIMETER AND AIR DATA COMPUTER WERE ERRATIC. DUE TO WEATHER AT IND, FLI GHT DIVERTED TO DAY AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 AIR DATA COMPUTER. (X) 2 L 7 2 4F A6WE 1996041200489 19960412 00489 EU 1996 4 12 USAAF96029 1 19960318 A 4950 434897 MULTISPEED SW FOKKER F28 F28MK4000 4990810 EU APU COMPARTMENT FAILED A USAA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CL CLIMB 1 EA 19 494US 6277 11167 CLT - FLT 729 - DURING CLIMB-OUT WITH ONE CSD ON MEL AND THE APU RUNNING, APU EXPERIENCED AN OVERSPEED AND SHUTDOWN. FL IGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE MULTI-SPEED ELECTRONIC SWITCH. (X) 2 L 7 2 4F RT A20EU 1996041200490 19960412 00490 NM 1996 4 12 USAASB96049 1 19960320 A 2420 6130200003 AC GENERATOR BOEING 737 737201 1384454 NM RT ENGINE LOOSE WIRE A USAA A UNSCHED LANDING J N WARNING INDICATION FALSE WARNING CL CLIMB 1 EA 19 244US 22752 CMH - FL 868 - AFTER DEPARTURE FROM CMH, NR 2 AND NR 3 TRANSFORMER RECEIVER UNITS FAILED. FLIGHT RETURNED TO CMH AND LA NDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND A LOOSE ENGINE GENERATOR FEED HARNESS WIRE. WIRE 'S' WAS LOOSE AT THE NR 2 GENERATOR. SECURED WIRE IN TO TERMINAL. (M) 2 L 7 2 4F A16WE 1996041200491 19960412 00491 NM 1996 4 12 USAASB96050 1 19960320 A 7312 696R16S1S135 CONNECTOR BOEING 737 737201 1384454 NM PWA JT8 JT8D9A 52048 NE LT ENGINE DEFORMED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 229US 21818 CLT - FLT 1850 - AFTER TAKEOFF FROM CLT, CREW RECEIVED NR 1 FUEL HEAT LIGHT AND NR 1 OIL TEMPERATURE ROSE INTO THE YELLO W ARC. CREW REDUCED POWER TO ENGINE. FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND PI N IN FUEL HEAT VALVE CONNECTOR D1004 PUSHED BACK. CONNECTOR WAS REPAIRED. (X) 2 L 7 2 4F 4 F A16WE E2EA 1996041200492 19960412 00492 NM 1996 4 12 USAASB96051 1 19960331 A 3397 WIRE BOEING 737 7373B7 1384580 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 374US 22953 CLT - FLOOR TRACK LIGHTING SEGMENT FOUND INOPERATIVE. REPAIRED EXPOSED WIRING. (X) 2 L 7 2 4F RT A16WE 1996041200493 19960412 00493 NM 1996 4 12 WRLA96014 1 19960320 A 5248 AKC773110 SAFETY RAILING DOUG MD11 MD11 3023602 NM TAIL CONE BROKEN A WRLA O OTHER J WARNING INDICATION CL CLIMB 1 EA 27 273WA 48519 DURING INITIAL CLIMB-OUT FROM TAKEOFF, CREW RECEIVED 'TAIL CONE UNLOCK ALERT' ILLUMINATED ON EAD. MAINTENANCE REP ABOAR D ACFT WENT TO AFT OF CABIN TO INSPECT FOR ABNORMAL VIBRATION AND NOISE, NONE WERE NOTED. CREW ELECTED TO CONTINUE TO D ESTINATION IAW FLIGHT CREW OPERATION MANUAL, MISC ABNORMAL ALERT PROCEDURE. ACFT LANDED WITHOUT FURTHER INCIDENT. UPON ARRIVAL, MX NOTED NR 2 ENGINE FWD ACCESS DOORS WERE OPEN. DAMAGE SUSTAINED TO MAINTENANCE SAFETY RAILING AND OPEN/CLOS E MECHANISM. DOORS/LATCHES, LATCHING PINS WERE UNDAMAGED. DOOR MANUALLY CLOSED AND LATCHED SECURELY. DAMAGED PARTS WE RE ORDERED AND NOTED IN ACFT CARRY-OVER LOGS. ACFT RETURNED TO SERVICE. (X) 2 L 7 3 4F RT A22WE 1996041200494 19960412 00494 EU 1996 4 12 WTAA960056 1 19960312 A 5730 SKIN BAG JETSTM JETSTM3101 1500215 EU LT WING LE BIRD STRIKE A WTAA K NONE C F.O.D. NR NOT REPORTED 1 WP 17 424UE 796 ACV - BIRD STRIKE REPORTED LT WING OUTBOARD OF NACELLE. ACCOMPLISHED BIRD STRIKE INSPECTION ON AIRCRAFT. FOUND LEADING EDGE DENTED AT POINT OF IMPACT. REMOVED AND REPLACED LEADING EDGE. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A21EU 1996041200495 19960412 00495 WP 1996 4 12 96ZZZM637 1 19960304 A 3222 A03772REVH STRUT SEALS DOUG DC9 DC982 3022082 WP NLG FAILED A TWAA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 909TW 49170 JFK - AFTER TAKEOFF THE NOSE GEAR DID NOT FULLY RETRACT. REMOVED AND REPLACED NOSE GEAR STRUTS SEALS, MFG P/N A03772REV H. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F A6WE 1996041200497 19960412 00497 NM 1996 4 12 96ZZZM639 1 19960116 A 7110 001A711E1400006 DOOR DORNER DO32 DO328100 2996000 NM LT ENGINE DAMAGED A A VNAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 427JS 3039 FLT NR 4159 - SHORTLY AFTER TAKEOFF, WHILE CLIMBING THROUGH 6000 FEET, THE CREW REPORTED SEVERE CONTROL AND YAW PROBLEMS . CREW REPORTED SITUATION TO ATC, WERE ADVISED TO RETURN TO FIELD. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. ONCE ON THE GROUND, PIT MAINTENANCE DISCOVERED THE LEFT OUTBOARD COWLING DOOR HAD OPENED IN FLIGHT. DOOR WAS DAMAGED AT THE HIN GE POINTS, BUT DID NOT DEPART THE AIRCRAFT. PIT MAINTENANCE REPAIRED THE DAMAGED DOOR IAW MFG'S INSTRUCTIONS. AIRCRAFT WAS THEN RETURNED TO SERVICE. IT IS IMPORTANT TO NOTE THAT NO MAINTENANCE, IN THIS AREA OF THE AIRCRAFT, WAS PERFORMED PRIOR TO THE FLIGHT. SUBMITTER STATES, SUSPECT A LATCH PROBLEM IN FLT. 2 H 7 2 4T RT A45NM 1996041200498 19960412 00498 NM 1996 4 12 96ZZZM640 1 19960212 A 3230 2431600000 UPLOCK ROLLER DORNER DO32 DO328100 2996000 NM RT MLG DIRTY A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 434JS 3051 FLT NR 4166 - SHORTLY AFTER TAKEOFF, AFTER GEAR WAS SELECTED 'UP' THE RIGHT MAIN LANDING GEAR INTRASIT LIGHT REMAINED IL LUMINATED. CREW CYCLED THE GEAR SEVERAL TIMES, BUT THE INTRANSIT LIGHT REMAINED ILLUNMINATED. AIRCRAFT RETURNED TO THE FIELD, LANDED WITHOUT FURTHER INCIDENT. PIT MAINTENANCE CLEANED AND LUBRICATED THE UPLOCK ROLLERS IAW MM 32-00-00 AND STD MC PRACTICES. GROUND CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A45NM 1996041200499 19960412 00499 NM 1996 4 12 96ZZZM641 1 19960215 A 3230 2431600000 UPLOCK ROLLER DORNER DO32 DO328100 2996000 NM MLG DIRTY A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 429JS 3043 FLT NR 4023 - SHORTLY AFTER TAKEOFF WHEN THE LANDING WAS RETRACTED, BOTH THE LEFT AND RIGHT MAIN LANDING GEAR INTRANSIT LIGHTS REMAINED ILLUMINATED. AIRCRAFT RETURNED TO THE FIELD, LANDED WITHOUT FURTHER INCIDENT. PIT MX CLEANED AND LUBRI CATED THE MAIN LANDING GEAR UPLOCK ROLLER IAW MM 32-00-00 AND STD MX PRACTICES, CHECK FLIGHT WAS SATISFACTORY. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A45NM 1996041200500 19960412 00500 NM 1996 4 12 96ZZZM642 1 19960215 A 3230 2431600000 UPLOCK ROLLER DORNER DO32 DO328100 2996000 NM MLG DIRTY A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 328JS 3030 FLT NR 4160 - AFTER TAKEOFF, WHEN THE LANDING GEAR WAS RETRACTED, THE LEFT MAIN LANDING GEAR INTRANSIT LIGHT REMAINED IL LUMINATED. AIRCRAFT RETURNED TO THE FIELD, LANDED WITHOUT FURTHER INCIDENT. PIT MAINTENANCE CLEANED AND LUBRICATED THE MAIN LANDING GEAR UPLOCK ROLLERS IAW MM 32-00-00 AND STD MX PRACTICES. GEAR POSITION INDICATION SYSTEM OPERATED NORMAL LY DURING TEST FLIGHT. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A45NM 1996041200501 19960412 00501 NM 1996 4 12 96ZZZM643 1 19960212 A 3230 2431600000 UPLOCK ROLLER DORNER DO32 DO328100 2996000 NM LT MLG DIRTY A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 423JS 3032 FLT NR 4194 - LEFT MAIN LANDING GEAR WOULD NOT LOCK IN THE UP POSITION AFTER TAKEOFF, RED INTRANSIT LIGHT REMAINED ILLUM INATED. AIRCRAFT RETURNED TO THE FIELD, LANDED WITHOUT FURTHER INCIDENT. PIT MX CLEANED AND LUBRICATED THE UPLOCK ROLL ERS IAW MM 32-00-00 AND STD MX PRACTICES. GROUND CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A45NM 1996041200502 19960412 00502 NM 1996 4 12 96ZZZM644 1 19960206 A 5610 001A561A0000206 DV WINDOW DORNER DO32 DO328100 2996000 NM LT COCKPIT DEFECTIVE A VNAA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 GL 07 426JS 215 3038 FLT NR 4011 - EN ROUTE FROM PIT TO IAD THE CAPTAINS DV WINDOW BEGAN TO DELAMINATE. THE CREW ELECTED TO DIVERT TO CAK WH ERE MX COULD REPLACE THE WINDOW. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. CAK MAINTENANCE REPLACED THE CAPTAINS SIDE DV WINDOW IAW MM 56-10-00. GROUND CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A45NM 1996041200503 19960412 00503 NE 1996 4 12 96ZZZM645 2 19960224 A 7260 SEAL DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7B 52053 NE NR 2 GEARBOX FAILED A VJ6A A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 11 913VV 47318 ON FLT NR 183 - ATL-MSY - DIVERTED TO MGM, EN ROUTE TO MSY NR 2 ENGINE OIL QUANTITY WENT TO ZERO THEN OIL PRESSURE DROPP ED TO 35 PSI, SHUT DOWN NR 2 ENGINE AND LANDED IN MGM. MAINTENANCE FOUND OIL LEAKING FROM THE STARTER OIL SEAL ON GEAR BOX. REMOVED STARTER AND REPLACED STARTER SEAL AND REINSTALLED STARTER IAW MM 72-60. PERFORMED LEAK CHECK AND PART POW ER ENGINE RUN. NO DEFECTS NOTED. 2 L 7 2 4F 4 F A6WE E2EA 1996041200504 19960412 00504 NM 1996 4 12 96ZZZM646 1 19960209 A 3240 BRAKES DORNER DO32 DO328100 2996000 NM MLG HOT A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 07 423JS 3032 FLT NR 4028 - DURING THE TAKEOFF ROLL, THE FLIGHT CREW WAS ALERTED BY A RED TAKEOFF CONFIGURATION WARNING. TAKEOFF WAS ABORTED, AIRCRAFT WAS RETURNING TO THE GATE WHEN THE CREW WAS AGAIN ALERTED, THIS TIME BY AN 'AMBER' CAS MESSAGE BRAKE T EMP. AIRCRAFT CONTINUED TO THE GATE WITHOUT FURTHER INCIDENT. PIT MAINTENANCE ALLOWED THE BRAKES TO COOL, AMBER CAS ME SSAGE CANCELLED, AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A45NM 1996041200505 19960412 00505 WP 1996 4 12 96ZZZM647 2 19960206 A 7200 31033104 ENGINE BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110U 01514 WP RIGHT DEFECTIVE A A VNAA E C D ENGINE SHUTDOWN ABORTED TAKEOFF RETURN TO BLOCK X ENGINE FLAMEOUT TO TAKEOFF 1 GL 07 841JS 751 P63226 FLT NR 4066 - WHILE APPLYING TAKEOFF POWER, RIGHT ENGINE FLAMED OUT AT APPROXIMATELY 70 PERCENT TORQUE. AIRCRAFT RETURN ED TO THE GATE WITHOUT FURTHER INCIDENT. OUT STATION MAINTENANCE INSPECTED THE RIGHT ENGINE AND DISCOVERED THE PLENUM O N THE ENGINE WAS CRACKED. DAY MX LATER REMOVED AND REPLACED THE RIGHT ENGINE IAW MM 71-00-00. GROUND RUN CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A21EU E4WE 1996041200506 19960412 00506 NM 1996 4 12 96ZZZM648 1 19960207 A 2730 DOLN1081M4D4NC RELAY DORNER DO32 DO328100 2996000 NM TRIM CONTROL PNL DEFECTIVE A A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 430JS 3044 FLT NR 4134 - SHORTLY AFTER TAKEOFF, THE CREW REPORTED HAVING TO EXERT EXTREMELY HIGH FORWARD PRESSURE ON THE CONTROL YO KE TO KEEP THE NOSE OF THE AIRCRAFT DOWN. THIS WAS ACCOMPANIED WITH AN AMBER CAS 'ELEVATOR LOAD DISC HIGH' MESSAGE. TH E MANUAL TRIM SYSTEM DID NOT RESPOND, THE CREW THEN SWITCHED TO THE STANDBY SYSTEM. AIRCRAFT RETURNED TO THE FIELD, LAN DED WITHOUT FURTHER INCIDENT. PIT MX REPLACED ONE OF THE TRIM SYSTEM CONTROL RELAYS IAW MM 27-31-02. GROUND CHECKED GO OD, AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A45NM 1996041200507 19960412 00507 EU 1996 4 12 96ZZZM649 1 19960119 A 7931 8582 OIL PRESS SWITCH JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J K WARNING INDICATION FLUID LOSS TX TAXI/GRND HDL 1 EA 27 301UE 41012 FLT NR 6486 - JFK-IAD - DURING TAXI, ABORTED TAKEOFF DUE TO THE RIGHT ENGINE OIL LEAKING AND INDICATING LOW OIL PRESSURE . AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE RIGHT OIL PRESSURE SWITCH AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996041200508 19960412 00508 EU 1996 4 12 96ZZZM650 1 19960214 A 5210 DSC258103V BEARING BAG JETSTM JETSTM3201 1500217 EU MAIN PAX DOOR WORN A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 481UE 895 FLT NR 6521 - IAD-BDL - DURING CLIMB-OUT, RETURNED TO BDL DUE TO THE PAX DOOR WARNING LIGHT ILLUMINATING. AIRCRAFT RETU RNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE UPPER DRAWBOLT AND 4 BEARINGS. AIRCRAFT WAS RELEASED A ND APPROVED FOR RETURN TO SERVICE. REFERENCE VTZA96083. 2 L 7 2 4T RT A56EU 1996041200510 19960412 00510 NM 1996 4 12 96ZZZM652 1 19960313 A 3260 653756819 ACCESSORY UNIT BOEING 727 727231 1384079 NM RT MLG MALFUNCTIONED A TWAA O OTHER N FALSE WARNING CL CLIMB 1 CE 05 54336 20490 PBI - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, RIGHT MAIN GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED. CYCLED LAND ING GEAR. REPLACED LANDING GEAR ACCESSORY BOX, MFG P/N 65-37568-19, AND LANDING GEAR INDICATION CHECKED NORMAL. 2 L 7 3 4F A3WE 1996041200511 19960412 00511 WP 1996 4 12 96ZZZM653 1 19960314 A 3260 H146 UPLIMIT SW DOUG DC9 DC931 3022065 WP NLG BROKEN WIRE A TWAA O OTHER P NO WARNING INDICATION AP APPROACH 1 CE 05 978Z 47250 STL - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, NOSE LANDING GEAR DOWN AND LOCKED GREEN LIGHT DID NOT ILLUMINATE. CYCLED LANDING GEAR. FOUND BROKEN WIRE TO PIN 7 OF UPLIMIT SWITCH, MFG P/N H14-6. REPAIRED WIRE TO PIN 7 AND NOSE LAN DING GEAR INDICATION CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 1996041200512 19960412 00512 WP 1996 4 12 96ZZZM654 1 19960314 A 2710 DMD67E1501 BEARING DOUG DC9 DC982 3022082 WP LT AILERON WORN A TWAA O OTHER O OTHER AP APPROACH 1 CE 05 906TW 49160 STL - DURING APPROACH AIRCRAFT REQUIRED EXCESSIVE AILERON TRIM CHANGE WHEN POWER AND SPEED CHANGED, AND MORE POWER THAN NORMAL TO MAINTAIN PROPER SINK RATE. FOUND LEFT AILERON INBOARD HINGE EYEBOLT BEARING, MFG P/N DMD6-7E1-501, WORN. REP LACED HINGE EYEBOLT AND AILERON SYSTEM OPERATION CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 1996041200513 19960412 00513 WP 1996 4 12 96ZZZM655 1 19960311 A 3350 3350002621 BATTERY PACK DOUG DC9 DC941 302207N WP CABIN DISCHARGED A TWAA O OTHER O OTHER CR CRUISE 1 CE 05 935L 47603 STL - DURING CRUISE, EGRESS LIGHTS AT SEAT ROW 15 THROUGH 19 ILLUMINATED. FOUND LIGHTING SYSTEM BATTERIES, MFG P/N 3350 -0026-21, WEAK. REPLACED BATTERIES AND EGRESS LIGHT SYSTEM OPERATION CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 1996041200514 19960412 00514 WP 1996 4 12 96ZZZM656 1 19960312 A 7920 A029231 OIL LINE DOUG DC9 DC983 3022083 WP NR 1 ENG FRACTURED A TWAA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 05 9302B 49528 MCI - DURING CRUISE, SHUT DOWN NR 1 ENGINE DUE TO LOSS OF OIL QUANTITY. FOUND OIL LINE, MFG PN A02923-1, FROM SNUBBER ' T' TO OIL PRESSURE TRANSMITTER, FRACTURED. REPLACED OIL LINE AND SERVICED OIL. ENGINE OPERATION AND LEAK CHECKS NORMAL . (M) 2 L 7 2 4F RT A6WE 1996041200515 19960412 00515 WP 1996 4 12 96ZZZM657 1 19960309 A 2780 LOCKOUT LKHEED 1011 1011385115 5265015 WP RT LE SLATS TRIPPED A TWAA O OTHER J WARNING INDICATION AP APPROACH 1 CE 05 31031 193B1115 STL - DURING APPROACH, LEADING EDGE SLATS WOULD NOT EXTEND. RESET RIGHT SLAT ASYMMETRY LOCKOUT. OPERATIONAL CHECK NORM AL. (M) 2 L 7 3 4F A23WE 1996041200516 19960412 00516 WP 1996 4 12 96ZZZM658 1 19960311 A 3350 41B030CF00101 BATTERIES DOUG DC9 DC951 3022051 WP EXTERIOR DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 416EA 47751 STL - DURING ROUTINE MAINTENACNE CHECK, EXTERIOR EMERGENCY LIGHTS DID NOT ILLUMINATE. FOUND BATTERIES, MFG P/N 41B030CF 00101, WEAK. REPLACED BATTERIES AND EXTERIOR LIGHT OPERATION CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 1996041200517 19960412 00517 NM 1996 4 12 96ZZZM659 1 19960315 A 7930 A008032 FILTER BYPASS SW BOEING 727 727231 1384079 NM NR 3 ENG FAILED A TWAA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 CE 05 52313 19832 PHL - FLT NR 304 - DURING CRUISE SHUT DOWN NR 3 ENGINE, S/N 1539, DUE TO FILTER BYPASS LIGHT ILLUMINATING. FOUND OIL FI LTER BYPASS SWITCH AT FAULT. REPLACED OIL FILTER BYPASS SWITCH, MFG P/N A00803-2 AND ENGINE OPERATION AND INDICATION CH ECKED NORMAL. (M) 2 L 7 3 4F A3WE 1996041200518 19960412 00518 NM 1996 4 12 96ZZZM660 1 19960316 A 3350 582243 POWER SUPPLY BOEING 767 767205 1385121 NM CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 651TW 23058 LAX - FLT NR 15 - DURING CRUISE LEFT AISLE EGRESS LIGHT AT SEAT ROWS 30 TO 35 AND L3 DOOR, ILLUMINATED. CYCLED SWITCH A ND BACK TO ARMED. FOUND POWER SUPPLY, MFG P/N 5822-43, FAULTY. REPLACED POWER SUPPLY AND EGRESS LIGHT SYSTEM OPERATION CHECKED NORMAL. (M) 2 L 7 2 4F RT A1NM 1996041200519 19960412 00519 NM 1996 4 12 96ZZZM661 1 19960316 A 3260 652021159 ACCESSORY BOX BOEING 727 727231 1384079 NM NLG MALFUNCTIONED A TWAA O OTHER N FALSE WARNING AP APPROACH 1 CE 05 54327 20234 STL - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, NOSE LANDING GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED. CYCLED L ANDING GEAR. FOUND INTERNAL MALUNCTION IN LANDING GEAR ACCESSORY BOX AND NOSE LANDING GEAR INDICATION CHECKED NORMAL. ( M) 2 L 7 3 4F A3WE 1996041200520 19960412 00520 WP 1996 4 12 96ZZZM662 1 19960315 A 3020 5005253 ANTI-ICE DUCT DOUG DC9 DC931 3022065 WP NR 2 ENGINE COWL RUPTURED A TWAA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 CE 05 983Z 47411 STL - AFTER TAKEOFF SHUT DOWN NR 2 ENGINE, S/N 2153, DUE TO FIRE WARNING. FOUND 13TH STAGE ANTI-ICE DUCT TO NOSE COWL R UPTURED, MFG P/N 5005253. REPLACED ANTI-ICE DUCT. ENGINE OPERATION AND INDICATION SYSTEMS CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 1996041200521 19960412 00521 NM 1996 4 12 96ZZZM663 1 19960317 A 3231 69678897 MECH ROD BOEING 727 727231 1384079 NM NLG DOOR FRACTURED A TWAA O OTHER J WARNING INDICATION LD LANDING 1 CE 05 54342 21629 MSY - ON LANDING, NOSE LANDING GEAR DOOR LIGHT ILLUMINATED. FOUND NOSE GEAR DOOR MECHANISM 'A' ROD, MFG P/N 69-67889-7, FRACTURED. REPLACED NOSE GEAR DOOR MECHANISM 'A' ROD AND RIGGED NOSE GEAR DOOR SYSTEM. NOSE GEAR AND DOOR OPERATION C HECKED NORMAL. (M) 2 L 7 3 4F A3WE 1996041200522 19960412 00522 WP 1996 4 12 96ZZZM664 1 19960206 A 2530 3510005801 COFFEE MAKER DOUG DC9 DC932 3022066 WP GALLEY OVERHEATED A VJ6A A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 11 966VV 47168 ON FLT NR 444 - ATL-ATL - AIR RETURN, STRONG ACRID ODOR IN COCKPIT IN CLIMB-OUT SIMILAR TO ELECTRICAL SMOKE. INSPECTED ELECTRICAL SYSTEM IN AND AROUND FLIGHT DECK AREA AND GALLEY. RAN BOTH ENGINES, FOUND AN OVERHEATED COFFEE MAKER HOT PLA TE. REMOVED AND REPLACED COFFEE MAKER, OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996041200523 19960412 00523 WP 1996 4 12 96ZZZM665 1 19960204 A 2120 DUCT DOUG DC9 DC932 3022066 WP RIGHT LOOSE A VJ6A A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 11 905VJ 47378 FLT NR 283-2 - IAD-FLL - DIVERTED TO ATL, UNABLE TO CONROL CABIN PRESSURE AT FL 230, CABIN ALT WAS 9,000 AND CLIMBING AT 700 FPM WITH OUTFLOW VALVE FULLY CLOSED. RECONNECT DUCT FWD OF RIGHT WATER SEPARATOR HOUSING, PRESSURIZED A/C, OPS CHE CK GOOD. REF MM 36-10. 2 L 7 2 4F A6WE 1996041200524 19960412 00524 WP 1996 4 12 96ZZZM666 1 19960205 A 3222 STRUT DOUG DC9 DC932 3022066 WP NLG REQ'D SERVICE A VJ6A A UNSCHED LANDING O OTHER CL CLIMB 1 SO 11 901VJ 47275 FLT NR 381 - BOS-BOS - AIR RETURN, LANDING GEAR HANDLE WOULD NOT MOVE TO RETRACT POSITION FOLLOWING TAKEOFF. FOUND NOSE STRUT UNDER INFLATED, SERVICED NOSE STRUT FULLY. IN FLIGHT MODE WAS OBTAINED, LOWERED STRUT TO PROPER LEVEL, OPS CHECK GOOD. REF MM 32-30. 2 L 7 2 4F A6WE 1996041200525 19960412 00525 NE 1996 4 12 96ZZZM667 2 19960310 A 7200 ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 MALFUNCTIONED A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 07 979HA 5733 373 FLT NR 3340 - DCA-HPN - DURING DESCENT INTO HPN WITH LOW POWER SETTING, THE CABIN BEGAN TO FILL WITH SMOKE. CYCLED EACH BLEED OFF AND RAISED CABIN ALTITUDE TO REMOVE SMOKE. THE AIRCRAFT LANDED IN HPN WITHOUT INCIDENT. REMOVED AND REPLACED THE P2.5 AIR SWITCHING VALVE, NO FIX. REMOVED AND REPLACED THE NR 1 ENGINE. (M) 2 H 7 2 4T 4 T RT A13NM E20NE 1996041200526 19960412 00526 NM 1996 4 12 96ZZZM668 1 19960306 A 3350 6013211X BATTERY GRIMES DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 924HA 20714 13975 ORF34 105 FLT NR 3040 - FLL-TPA - DURING PREFLIGHT WALKAROUND, FOUND DS3 AND DS4 FLOOR PROX EMERGENCY LIGHTS INOP. REMOVED AND RE PLACED BASE AND BATTERY. REFERENCE HNAA9692417 2 H 7 2 4T RT A13NM 1996041200527 19960412 00527 EA 1996 4 12 96ZZZM669 1 19960301 A 2160 7506651 DUCT TEMP SWITCH HAMSTD DHAV DHC7 DHC7102 2802708 EA LEFT FAILED A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 EA 07 905HA 17723 15803 070 FLT NR 3055 - ORF-DCA - DURING PREFLIGHT CHECKS, THE CABIN FILLED WITH SMOKE. THE LEFT PACK WENT RED LINE AND AUTO SHUT OFF DID NOT WORK. FOUND AIR CYCLE MACHINE SEIZED. REMOVED AND REPLACED THE LEFT AIR CYCLE MACHINE AND THE LEFT DUCT TE MP SWITCH. REFERENCE HNAA9690514. 2 H 7 4 4T A20EA 1996041200528 19960412 00528 SO 1996 4 12 96ZZZM670 1 19960310 A 5414 1159P25046 SKIN GULSTM G1159 G1159B 3953535 SO RT PYLON DEBONDED A E9LA K NONE O OTHER IN INSP/MAINT 1 EA 05 928GF 8085 119 RIGHT LOWER AFT PYLON SKIN DELAMINATED BEYOND MANUFACTURE'S ACCEPTABLE LIMITS. 2 L 7 2 4F RT A12EA 1996041200529 19960412 00529 SO 1996 4 12 96ZZZM671 1 19960303 A 5320 1159B2132127 DOUBLER GULSTM G1159 G1159B 3953535 SO FS 580-635 CORRODED A E9LA K NONE O OTHER IN INSP/MAINT 1 EA 05 928GF 8085 119 ON FS 580 PRESSURE BULKHEAD COMM SCAN INSPECTION, CORROSION WAS DETECTED BETWEEN THE SKIN AND LONGERON NR 24 ON THE RIGH T SIDE OF AIRFRAME AT LOCATION NR 59 BETWEEN LAYERS NR 10 THROUGH 15. SKIN WAS REMOVED TO REPAIR PROBLEM AND A HOLE WAS DETECTED IN STRAP (P/N 1159B21321-27). CORROSION ALSO DETECTED ON LEFT AND RIGHT LONGERON NR 24 AT THE RADIUS. (M) 2 L 7 2 4F RT A12EA 1996041200530 19960412 00530 NM 1996 4 12 96ZZZM672 1 19960218 A 5610 001A561D006001 WINDSHIELD SIERRACIN DORNER DO32 DO328100 2996000 NM LT SIDE DELAMINATED A EQGA O OTHER O OTHER CR CRUISE 1 SW 19 340LS 774 3040 PILOTS LEFT SIDE WINDSHIELD DELAMINATED SEVERELY IN FLIGHT FROM ASE TO DFW. THE AIRCRAFT LANDED AT DFW WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS THEN FERRIED TO HOT WHERE THE WINDSHIELD WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVI CE. THIS IS AN ON GOING PROBLEM THAT THE MANUFACTURER IS AWARE OF. (M) 2 H 7 2 4T RT A45NM 1996041200531 19960412 00531 WP 1996 4 12 96ZZZM673 1 19960321 A 3260 DNLOCK SWITCH DOUG DC9 DC915F 3022037 WP NLG BROKEN WIRES A RYNA O OTHER P NO WARNING INDICATION LD LANDING 1 CE 07 567PC 47153 UPON GEAR EXTENSION THE NOSE GEAR RED AND GREEN POSITION INDICATION LIGHTS WERE INOP. CYCLED GEAR AND CHANGED BULBS, NO HELP. AIRCRAFT LANDED AT DAYTON WITHOUT INCIDENT. REPAIRED BROKEN WIRES AT NOSE GEAR LOCK SWITCH. OPS CHECK GOOD PER MM 32-61-00 AND 32-60-01. (M) 2 L 7 2 4F A6WE 1996041200532 19960412 00532 NM 1996 4 12 ASAA9610035 1 19960308 A 3260 6552811109 LG ACCY UNIT BOEING 737 7372X6C 1384552 NM E/E COMPT DEFECTIVE A A ASAA O OTHER N FALSE WARNING CL CLIMB 1 NM 01 746AS 33694 23123 SEA - AFTER DEPARTURE FROM KTN PASSING 256 KTS, GREEN NLG LIGHT CAME ON WITH GEAR UP. SLOWED AIRCRAFT AND CYCLED GEAR, LIGHT REMAINED ON. CYCLED LANDING GEAR C/B AND LIGHT WENT OUT. ACCELERATED THROUGH 270 KTS, LIGHT CAME ON AGAIN. AFTE R 1 MINUTE, LIGHT WENT OUT ON ITS OWN AND STAYED OUT FOR REMAINDER OF THE FLIGHT, UNTIL GEAR EXTENSION. MAINTENANCE VER IFIED THE INTEGRITY OF THE NLG UP AND DOWN LOCK SENSORS AND ASSOCIATED WIRING IN THE NOSE WHEEL WELL. COMPLIED WITH GEA R SWINGS, UNABLE TO DUPLICATE MALFUNCTION. REMOVED AND REPLACED LANDING GEAR ACCESSORY MODULE. FUNCTIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996041200533 19960412 00533 SO 1996 4 12 ASOA96007 1 19960317 A 5713 12016086001 STRINGER EMB 120 EMB120RT SO LT WING DEFECTIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 246AS 120100 DURING INSPECTION, FOUND THE LEFT WING NR 10 STRINGER INBOARD OF NACELLE CRACKED. DETERMINED TO BE A MAJOR REPAIR IAW S P663 AND FAR 43 APPENDIX A. REPAIRED STRINGER IAW SRM 57-20-03, FIGURE 201. AIRCRAFT LEAK CHECKED GOOD AND WAS RELEASE D FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1996041200534 19960412 00534 SO 1996 4 12 ASOA96008 1 19960325 A 7160 NH100533610 INLET CLAMP EMB 120 EMB120RT SO LT ENGINE DEFECTIVE A A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 501AS 120273 CLIMBING THROUGH 14,000 FEET ATL-FLO, AIRCRAFT EXPERIENCED A T6 SURGE AND THE TORQUE FELL APPROXIMATELY 10 PERCENT. CAP TAIN NOTICED THAT THE LEFT ENGINE INLET DUCT WAS SEPARATED FROM THE BOOT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RE TURNED TO ATL WHERE LANDING WAS MADE SAFELY AND WITHOUT INCIDENT. SECURED THROAT BOOT ASSEMBLY CLAMP AND REPLACED INLET DUCT CLAMP. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1996041200535 19960412 00535 SO 1996 4 12 ASOA96009 1 19960325 A 2450 3TC1435 CIRCUIT BREAKER EMB 120 EMB120RT SO LT ENGINE DEFECTIVE A ASOA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 SO 11 227AS 120023 IN CRUISE FLIGHT ATL-DHN AT 18,000 FEET, EMERGENCY BUS OFF LIGHT ILLUMINATED AND AIRCRAFT LOST ALL EMERGENCY DC BUS 1 PO WER. ALL AUXILLARY AND MAIN GENERATORS CONTINUED TO OPERATE NORMALLY. CREW DECLARED AN EMERGENCY, INITIATED A DESCENT TO GET OUT OF ICING, AND RETURNED TO ATL WHERE LANDING WAS MADE SAFELY AND WITHOUT INCIDENT. REMOVED AND REPLACED THE E MERGENCY DC BUS 1 CIRCUIT BREAKER. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1996041200536 19960412 00536 WP 1996 4 12 BDHA960004 2 19960122 A 7321 89356117 FUEL CONTROL SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP RT ENGINE OUT OF ADJUST A BDHA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 15 229AM 923493 TC305 MSP - FLT NR 475 - CREW REPORTED A POWER LEVER SPLIT ON TAKEOFF AND RETURNED. THE ENGINE RIGGING WAS INSPECTED AND MAX POWER WAS ADJUSTED. ENGINE POWER RUNS WERE PERFORMED AND ALL INDICATIONS WERE NORMAL. A TEST FLIGHT WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A8SW E4WE 1996041200537 19960412 00537 NM 1996 4 12 CAL960230 1 19960209 A 5320 STIFFENER BOEING 727 727227 1384078 NM BS 970-980 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79754 46935 21363 STATION 31J - INSPECTION FOUND A 1.5 INCH CRACK IN STRINGER STIFFENER AT BS 970 TO 980, RBL 2. THE CRACKED STIFFENER WA S REMOVED. A NEW STIFFENER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1996041200538 19960412 00538 NM 1996 4 12 CAL960231 1 19960209 A 5320 ANGLE BOEING 727 727227 1384078 NM BS 950 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79754 46935 21363 STATION 31J - INSPECTION FOUND A 1 INCH CRACK IN ANGLE AT BS 950C, LBL 18. AN L-ANGLE AND Z-ANGLE WERE FABRICATED AND I NSTALLED IAW SRM 51-10-2, 51-30-2, AND 51-40-4. (M) 2 L 7 3 4F A3WE 1996041200539 19960412 00539 NM 1996 4 12 CAL960232 1 19960207 A 5320 ANGLE BOEING 727 727227 1384078 NM BS 950B CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79754 46935 21363 STATION 31J - INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT ANGLE AT BS 950B, RBL 48. A NEW Z-ANGLE AND TWO PLATES W ERE FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-40-4, AND MM 51-20-15. (M) 2 L 7 3 4F A3WE 1996041200540 19960412 00540 NM 1996 4 12 CAL960233 1 19960201 A 5320 SUPPORT ANGLE BOEING 727 727227 1384078 NM BS 1010 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79754 46935 21363 STATION 31J - INSPECTION FOUND FLOOR STRINGER SUPPORT ANGLE CRUSHED IN AFT CARGO COMPARTMENT, BS 1010, BETWEEN STRINGER 29R AND 30R. A NEW SUPPORT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-4, 51-30-2, AND 51-10-2. (M) 2 L 7 3 4F A3WE 1996041200541 19960412 00541 NM 1996 4 12 CAL960234 1 19960211 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 950-970 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79754 46935 21363 STATION 31J - INSPECTION FOUND AFT CARGO FLOOR STRINGER WEB CORRODED AT BS 950F TO 970, STRINGER 28L. THE WEB WAS REMOV ED AND A NEW WEB WAS FABRICATED AND INSTALLED IAW SRM 51-20-1, 51-40-3, AND 51-30-2. (M) 2 L 7 3 4F A3WE 1996041200542 19960412 00542 NM 1996 4 12 CAL960235 1 19960211 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 950-970 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79754 46935 21363 STATION 31J - INSPECTION FOUND STRINGER 28L CORRODED IN AFT CARGO COMPARTMENT BETWEEN STATION 950F AND 970. THE CORRODE D SECTION OF STRINGER WAS REMOVED. A NEW SECTION OF STRINGER AND STRINGER SPLICES WERE FABRICATED AND INSTALLED IAW SRM 53-10-3, 51-20-4, AND 51-30-2. (M) 2 L 7 3 4F A3WE 1996041200543 19960412 00543 NM 1996 4 12 CAL960236 1 19960209 A 7110 NOSE COWL BOEING 727 727227 1384078 NM NR 3 ENGINE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79754 46935 21363 STATION 31J - INSPECTION FOUND A 1.75 INCH CRACK AT RIVET OF NR 3 ENGINE NOSE COWL SKIN. THE CRACKED AREA OF SKIN WAS C UT OUT. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 54-30-3, FIGURE 8 AND ECRA 5430-01377. (M) 2 L 7 3 4F A3WE 1996041200544 19960412 00544 NM 1996 4 12 CAL960237 1 19960214 A 5313 STRINGER BOEING 727 727227 1384078 NM AFT PIT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79754 46935 21363 STATION 31J - INSPECTION FOUND A .25 INCH CRACK IN FLANGE WHERE NUT PLATE MOUNTS, ON STRINGER 26L IN AFT PIT. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1, PAGE 6A. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-4 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1996041200545 19960412 00545 NM 1996 4 12 CAL960238 1 19960212 A 5330 SKIN BOEING 727 727227 1384078 NM BS 950-1010 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79754 46935 21363 STATION 31J - INSPECTION FOUND CORROSION IN SKIN UNDER STRINGER 28L AT STATION 950F TO 1010. THE CORRODED AREA OF SKIN WAS CUT OUT. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, 51-20-4, AND 51-30-2. (M) 2 L 7 3 4F A3WE 1996041200546 19960412 00546 NM 1996 4 12 CAL960239 1 19960209 A 5320 L-ANGLE BOEING 727 727227 1384078 NM BS 980 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79754 46935 21363 STATION 31J - INSPECTION FOUND L-ANGLE NEXT TO SKIN ON VERTICAL IN FT CARGO COMPARTMENT CORRODED AT BS 980, LBL 14. THE L-ANGLE WAS REMOVED AND A NEW L-ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-4, 51-10-2, 53-10-4, AND MM 51-20-15. (M) 2 L 7 3 4F A3WE 1996041200547 19960412 00547 NM 1996 4 12 CAL960240 1 19960228 A 2612 896768 FIRE DETECTOR GARRTT GTCP85129 BOEING 737 7373T0 1384582 NM APU TAILPIPE INOPERATIVE A CALA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 09 14334 P60415 23572 FLT NR 1603 - DCA - THE APU FIRE WARNING LIGHT AND BELL ACTIVATED IN FLIGHT. THE FIRE BOTTLE WAS DISCHARGED, BUT THE FI RE WARNING LIGHT REMAINED ILLUMINATED. THE AIRCRAFT WAS RETURNED TO DCA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. MAINTENANCE FOUND THE M717 APU TAILPIPE OVERHEAT DETECTION ELEMENT AT FAULT. THE FIRE BOTTL E WAS REMOVED AND REPLACED. THE APU FIRE DETECTION SYSTEM WAS TEMPORARILY PLACARDED INOPERATIVE, PENDING REPLACEMENT OF THE FAULTY OVERHEAT DETECTION ELEMENT. (M) 2 L 7 2 4F RT A16WE 1996041200548 19960412 00548 NM 1996 4 12 CAL960248 1 19960301 A 2910 HYD LINE BOEING 737 7373T0 1384582 NM B-HYD SYSTEM RUPTURED A CALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 14347 23585 FLT NR 778 - IAH - THE 'B' SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO WHILE IN CRUISE FLIGHT. ALTERNATE FLAPS WERE USED AND THE GROUND PROXIMITY FLAP INHIBIT SWITCH WAS ACTIVATED IAW THE AIRCRAFT FLIGHT MANUAL. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC FLEX LINE TO THE HYDRAULIC MODULE RUPTURED. THE HYDRAULIC FLEX LINE WAS REMO VED AND REPLACED. LEAK CHECK WAS GOOD. (M) 2 L 7 2 4F RT A16WE 1996041200549 19960412 00549 NM 1996 4 12 CAL960251 1 19960202 A 5320 ANGLE BOEING 727 727243 138408D NM BS 1168 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 46469 21265 STATION 31J - INSPECTION FOUND CORROSION AT BOTTOM OF FLOOR BEAM AT GILL SUPPORT FRAME ANGLE IN AFT CARGO PIT AT BS 1168 , RBL 55. THE CORRODED AREA OF ANGLE WAS CUT OUT. A NEW ANGLE AND DOUBLER ANGLE WERE FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-20-2, AND 51-40-3. (M) 2 L 7 3 4F RT A3WE 1996041200550 19960412 00550 NM 1996 4 12 CAL960252 1 19960112 A 5730 SKIN BOEING 727 727243 138408D NM WS 304 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 46469 21265 STATION 31J - INSPECTION FOUND A .5 INCH CRACK IN LOWER SKIN PANEL OUTBOARD OF PANEL 8505R AT RIGHT WING STATION 304. T HE CRACKED AREA WAS REMOVED. A NEW ATTACH ANGLE PLATE WAS FABRICATED AND INSTALLED IAW SRM 51-30-3, FIGURE 4. (M) 2 L 7 3 4F RT A3WE 1996041200551 19960412 00551 NM 1996 4 12 CAL960253 1 19960110 A 5320 BEAM BOEING 727 727243 138408D NM BS 870 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 46469 21265 STATION 31J - INSPECTION FOUND A .75 INCH CRACK AT TERMINAL FITTING ATTACH POINT OF BS 870 HORIZONTAL BEAM IN FORWARD UP PER OUTBOARD CORNER OF LEFT WHEEL AT STRINGER 18A. THE CRACKED SECTION OF BEAM WAS REMOVED. AN ANGLE AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, FIGURE 1. (M) 2 L 7 3 4F RT A3WE 1996041200552 19960412 00552 NM 1996 4 12 CAL960254 1 19960109 A 5521 65174393 FITTING RIB BOEING 727 727243 138408D NM LT ELEVATOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 46469 21265 STATION 31J - INSPECTION FOUND A 1.75 INCH CRACK IN LEFT ELEVATOR FITTING RIB BETWEEN BAYS 3 AND 4. THE LEFT ELEVATOR F ITTING RIB WAS REMOVED AND REPLACED IAW MM 55-20-0 AND SRM 51-30-2. (M) 2 L 7 3 4F RT A3WE 1996041200553 19960412 00553 NM 1996 4 12 CAL960255 1 19960110 A 5320 SUPPORT BOEING 727 727243 138408D NM BS 850 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 46469 21265 STATION 31J - INSPECTION FOUND KEEL BEAM PANEL SUPPORT AT BS 850 LBL 10 CORRODED THROUGH AND BOTTOM OF SUPPORT HAS SURFA CE CORROSION FROM RBL 10 TO LBL 10. A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-40-3. (M) 2 L 7 3 4F RT A3WE 1996041200554 19960412 00554 NM 1996 4 12 CAL960256 1 19960121 A 5320 SUPPORT BOEING 727 727243 138408D NM BS 780 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 46469 21265 STATION 31J - INSPECTION FOUND CORROSION ON INBOARD SIDE OF PANEL SUPPORT AT BS 780, LBL 9. THE CORROSION WAS MECHANICA LLY REMOVED. TWO BRACKETS WERE FABRICATED AND INSTALLED IAW SRM 51-40-4, FIGURE 2. (M) 2 L 7 3 4F RT A3WE 1996041200555 19960412 00555 NM 1996 4 12 CAL960257 1 19960121 A 5320 SUPPORT BOEING 727 727243 138408D NM BS 813 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 46469 21265 STATION 31J - INSPECTION FOUND FUSELAGE PANEL SUPPORT CORRODED BELOW ANCHOR NUT AT BS 813, LBL 9 BETWEEN LEFT AND RIGHT HEAT EXCHANGER. THE CORROSION WAS REMOVED IAW SRM 51-10-2, AN 'L' ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 5 1-30-2, AND MM 51-20. (M) 2 L 7 3 4F RT A3WE 1996041200556 19960412 00556 NM 1996 4 12 CAL960258 1 19960121 A 5320 SUPPORT BOEING 727 727243 138408D NM BS 813 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 46469 21265 STATION 31J - INSPECTION FOUND FUSELAGE PANEL SUPPORT CORRODED BELOW ANCHOR NUT AT BS 813, RBL 9 BETWEEN HEAT EXCHANGERS . THE CORRODED AREA WAS CUT OUT, TWO 'L' ANGLES AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, 51- 30-2, AND MM 51-20-0. (M) 2 L 7 3 4F RT A3WE 1996041200557 19960412 00557 NM 1996 4 12 CAL960259 1 19960114 A 5315 FLOOR BEAM BOEING 727 727243 138408D NM BS 380 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 46469 21265 STATION 31J - INSPECTION FOUND FLOOR BEAM CORRODED AT BS 380, RBL 40 TO RBL 60. A NEW FLOOR BEAM WAS FABRICATED AND INS TALLED IAW SRM 53-10-8, FIGURE 3, 51-10-2, AND 51-20-0. (M) 2 L 7 3 4F RT A3WE 1996041200558 19960412 00558 NM 1996 4 12 CAL960268 1 19960110 A 5712 RIB WEB BOEING 727 727243 138408D NM LT WING LE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 46469 21265 STATION 31J - INSPECTION FOUND A 1.5 INCH CRACK IN LEFT WING LEADING EDGE RIB WEB. THE CRACK WAS STOP DRILLED. A DOUBL ER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. (M) 2 L 7 3 4F RT A3WE 1996041200559 19960412 00559 NM 1996 4 12 CAL960269 1 19960124 A 5315 FLOOR BEAM BOEING 727 727243 138408D NM BS 1010 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 46469 21265 STATION 31J - INSPECTION FOUND ELONGATED HOLES AND PITTING CORROSION IN FLOOR BEAM AND SEAT TRACK AT BS 1010, RBL 55. T HE AREA OF ELONGATED HOLES WAS CUT OUT. REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, FIGURE 1. (M) 2 L 7 3 4F RT A3WE 1996041200560 19960412 00560 NM 1996 4 12 CAL960270 1 19960111 A 5320 FORMER BOEING 727 727243 138408D NM BS 774 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 46469 21265 STATION 31J - INSPECTION FOUND CORROSION ON HORIZONTAL FORMER AT BS 774, RBL 9-35. THE CORRODED AREA WAS CUT OUT. A RE PAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3. (M) 2 L 7 3 4F RT A3WE 1996041200561 19960412 00561 NM 1996 4 12 CAL960271 1 19960125 A 5320 PANEL SUPPORT BOEING 727 727243 138408D NM BS 880 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 46469 21265 STATION 31J - INSPECTION FOUND LOWER FUSELAGE PANEL SUPPORT CORRODED AT BS 880, LBL 9 AND RBL 9. THE CORRODED AREA WAS CUT OUT. REPAIR ANGLES AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 51-40-3. (M) 2 L 7 3 4F RT A3WE 1996041200562 19960412 00562 NM 1996 4 12 CAL960272 1 19960126 A 5320 CHANNEL SUPPORT BOEING 727 727243 138408D NM BS 803 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 46469 21265 STATION 31J - INSPECTION FOUND CORROSION ON CHANNEL SUPPORT AT BS 803, BL 0. THE CORROSION WAS REMOVED AND A 'T' ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-4. (M) 2 L 7 3 4F RT A3WE 1996041200563 19960412 00563 NM 1996 4 12 CAL960274 1 19960124 A 5753 FLAP TRACK BOEING 727 727243 138408D NM TE FLAPS CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 46469 21265 STATION 31J - INSPECTION FOUND CORROSION AT RIGHT MLG BEAM INBOARD FLAP INBOARD TRACK ATTACH POINT. THE AREA WAS REPAIR ED IAW ECRA 5750-02438. (M) 2 L 7 3 4F RT A3WE 1996041200564 19960412 00564 WP 1996 4 12 CAL960275 1 19960304 A 2915 AYG70155001 RELIEF VALVE DOUG DC10 DC1010 3022110 WP NR 3 HYD SYSTEM STICKING A A CALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 09 68042 23509 21132 46901 FLT NR 973 - NGO - THE A/C PITCHED DOWN SLIGHTLY DURING APPROACH TO NGO. THE OUT OF TRIM LIGHT FLASHED AND THEN THE HYD RAULIC SYSTEM 3 ELEVATOR OFF LIGHT ILLUMINATED. THE SYSTEM NR 3 HYDRAULIC QUANTITY GAUGE READ DOWN .5 GALLON. THE AIRC RAFT LANDED WITHOUT INCIDENT. THE NR 3 HYDRAULIC SYSTEM WAS SERVICED. THE SYSTEM WAS PRESSURIZED AND THE SLATS, FLAPS, STABILIZER, AND RUDDER WERE OPERATED WITH NO LEAKS FOUND. THE NR 3 ENGINE WAS MOTORED AND NO LEAKS WERE OBSERVED. MAI NTENANCE FOUND THE SYSTEM NR 3 RESERVOIR RELIEF VALVE STICKING AND THE OVERFLOW BOTTLE FULL. THE NR 3 SYSTEM RESERVOIR RELIEF VALVE WAS CLEANED AND OPERATION CHECKED GOOD. (M) 2 L 7 3 4F A22WE 1996041200565 19960412 00565 WP 1996 4 12 CAL960276 1 19960229 A 2913 6506606 HYD PUMP DOUG DC10 DC1030 3023501 WP NR 2 ENGINE LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 SW 09 19072 9560 5528 46576 FLT NR 6 - LAX - THE NR 2 ENG TEMP HIGH LIGHT ILLUMINATED AND WAS FOLLOWED SHORTLY AFTERWARDS BY THE LOSS OF NR 2 HYDRAU LIC QUANTITY. BOTH PUMPS WERE SHUTOFF AND TEMP WAS NORMAL. THE AIRCRAFT LANDED WITHOUT INCIDENT. BOTH NR 2 ENGINE HYD RAULIC PUMPS WERE REMOVED AND REPLACED DUE TO LEAKING AT CASE AND ONE HAD A SHEARED SHAFT. THE NR 2 ENGINE PRESSURE AND CASE DRAIN FILTERS WERE REMOVED AND REPLACED DUE TO CONTAMINATION. THE LINES BETWEEN PUMPS AND FILTERS WERE FLUSHED. L EAK AND OPERATIONAL CHECKS WERE GOOD. (M) 2 L 7 3 4F A22WE 1996041200566 19960412 00566 WP 1996 4 12 CAL960277 1 19960229 A 2913 6506606 HYD PUMP DOUG DC10 DC1030 3023501 WP NR 2 ENGINE LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 SW 09 19072 11843 60 46576 FLT NR 6 - LAX - THE NR 2 ENG TEMP HIGH LIGHT ILLUMINATED AND WAS FOLLOWED SHORTLY AFTERWARDS BY THE LOSS OF NR 2 HYDRAU LIC QUANTITY. BOTH PUMPS WERE SHUTOFF AND TEMP WAS NORMAL. THE AIRCRAFT LANDED WITHOUT INCIDENT. BOTH NR 2 ENGINE HYD RAULIC PUMPS WERE REMOVED AND REPLACED DUE TO LEAKING AT CASE AND ONE HAD A SHEARED SHAFT. THE NR 2 ENGINE PRESSURE AND CASE DRAIN FILTERS WERE REMOVED AND REPLACED DUE TO CONTAMINATION. THE LINES BETWEEN PUMPS AND FILTERS WERE FLUSHED. L EAK AND OPERATIONAL CHECKS WERE GOOD. (M) 2 L 7 3 4F A22WE 1996041200567 19960412 00567 WP 1996 4 12 CAL960278 1 19960227 A 5542 SKIN DOUG DC9 DC932 3022066 WP RUDDER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12532 67873 45791 HOU - INSPECTION FOUND A 2 INCH CRACK BETWEEN FOUR RIVETS AT RIVET LINE FOR UPPER CAP AND A .5 INCH CRACK BETWEEN TWO RI VETS AT RIVET LINE FOR UPPER CAP IN RIGHT UPPER RUDDER SKIN. THE CRACKS WERE REPAIRED BY FABRICATING AND INSTALLING A D OUBLER IAW SRM 55-01, FIGURE 2, SHEET 2. (M) 2 L 7 2 4F A6WE 1996041200568 19960412 00568 NM 1996 4 12 CAL960280 1 19960305 A 2910 HYD LINE BOEING 737 737217 1384464 NM B HYD SYSTEM LEAKING A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 09 12230 19884 FLT NR 512 - EWR - THE 'B' HYD SYSTEM WAS LOST AFTER TAKEOFF FROM EWR. THE LOSS WAS ACCOMPANIED BY ILLUMINATION OF SYST EM 'B' LOW PRESSURE LIGHTS. THE 'B' SYSTEM PUMPS WERE TURNED OFF AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED W ITHOUT INCIDENT. MAINTENANCE FOUND NR 1 'B' SYSTEM HYDRAULIC PRESSURE LINE TO NR 1 'B' PUMP LEAKING. THE LINE WAS REMO VED AND REPLACED. IN ADDITION, THE NR 1 'B' SYSTEM ELECTRIC DRIVEN HYDRAULIC PUMP WAS REPLACED AS A PRECAUTIONARY MEASU RE. THE HYDRAULIC SYSTEM WAS SERVICED TO FULL. BOTH THE NR 1 AND NR 2 'B' SYSTEM PUMPS WERE OPERATED AND NO LEAKS WERE NOTED. (M) 2 L 7 2 4F A16WE 1996041200569 19960412 00569 NM 1996 4 12 CAL960281 1 19960222 A 3350 LIGHT BOEING 737 7373T0 1384582 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14336 23574 HOU - THE OVERHEAD EMERGENCY LIGHT FORWARD OF AFT RIGHT GALLEY WAS FOUND INOPERATIVE. THE EMERGENCY LIGHT WAS REPLACED AND OPERATION CHECKED GOOD. (M) 2 L 7 2 4F RT A16WE 1996041200570 19960412 00570 NM 1996 4 12 CAL960282 1 19960306 A 2913 6507506 HYD PUMP BOEING 737 737217 1384464 NM NR 2 ENGINE LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 09 13234 8164 19888 FLT NR 1160 - EWR - THE AIRCRAFT LOST ALL PRESSURE AND FLUID FROM THE 'A' HYDRAULIC SYSTEM DURING FINAL APPROACH TO EWR. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE DRIVE HYDRAULIC PUMP AT FAULT. THE NR 2 HYDR AULIC PUMP WAS REMOVED AND REPLACED. HYDRAULIC PUMP OPERATION CHECKED GOOD. (M) 2 L 7 2 4F A16WE 1996041200571 19960412 00571 1996 4 12 CAL960283 4 19960213 A 2210 4030952906 YAW DAMPER BOEING 737 7373T0 1384582 NM E/E RACK FAILED A CALA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SW 09 59302 31133 23353 EWR - FLT 0485 - THE AIRCRAFT TAIL BEGAN TO KICK BACK AND FORTH IN-FLIGHT TO EWR. THERE WAS NO NOTICEABLE RUDDER PEDAL MOVEMENT. THE KICKING OCCURRED IN BOTH AUTOPILOT A AND B MODES. WHEN THE YAW DAMPER WAS TURNED OFF THE CONDITION WORSE NED. THE AUTOPILOT WAS RE-ENGAGED AND THEN TURNED OFF, BUT THE KICKING MOTION CONTINUED. THE AIRCRAFT LANDED WITHOUT I NCIDENT. YAW DAMPER COUPLER FAILED BITE TEST. YAW DAMPER COUPLER REMOVED AND REPLACED. AUTOPILOT ACCESSORY UNIT WAS A LSO REPLACED DUE TO BITE TEST FAILURE. SDR WILL REMAIN OPEN PENDING COMPONENT TEAR-DOWN FINDINGS. SUPPLEMENT: TEAR-DO WN FND YAW DAMPER COUPLER RATE GYRO AT FAULT. NO TROUBLE FND WITH A/P ACCY UNIT WHICH PASSED ALL BENCH TESTS. (X) 2 L 7 2 4F RT A16WE 1996041200572 19960412 00572 WP 1996 4 12 CAL960286 1 19960308 A 2910 ALK70151 HYD LINE DOUG DC10 DC1010 3022110 WP LT ELEVATOR LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 09 68044 46903 FLT NR 967 - NRT - THE SYSTEM NR 3 HYDRAULIC ELEVATOR OFF LIGHT ILLUMINATED AFTER GEAR WAS EXTENDED ON FINAL APPROACH TO NRT. THE HYDRAULIC QUANTITY INDICATED 5.2 GALLONS. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LEAK AT L EFT INBOARD ELEVATOR SUPPLY LINE. A NEW TUBE SECTION WAS MANUFACTURED AND A PERMASWAGE REPAIR WAS PERFORMED IAW GMM 10- 799-78. THE SYSTEM NR 3 HYDRAULIC RESERVOIR WAS SERVICED TO FULL AND LEAK CHECKS WERE GOOD. (M) 2 L 7 3 4F A22WE 1996041200573 19960412 00573 WP 1996 4 12 CAL960297 1 19960225 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP BS 175 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17812 36173 49250 HOU - INSPECTION FOUND FLOOR SUPPORT CORRODED AT STATION 175. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2. (M) 2 L 7 2 4F A6WE 1996041200574 19960412 00574 WP 1996 4 12 CAL960298 1 19960225 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP BS 160-200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17812 36173 49250 HOU - INSPECTION FOUND FLOOR SUPPORT CORRODED AT STATION 160-200, RIGHT OF CENTERLINE. A NEW FLOOR SUPPORT WAS INSTALLE D IAW SRM 51-30-2. (M) 2 L 7 2 4F A6WE 1996041200575 19960412 00575 WP 1996 4 12 CAL960299 1 19960226 A 5320 FLOOR DOUG DC9 DC982 3022082 WP BS 1174 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17812 36173 49250 HOU - INSPECTION FOUND CABIN SUB FLOOR CORRODED ON LEFT SIDE AT STATION 1174. THE CORRODED SECTION WAS REMOVED AND THE SURROUNDING AREA WAS CLEANED IAW SRM 51-10-3. A REPAIR SECTION OF SUB FLOOR WAS INSTALLED IAW SRM 53-01, FIGURE 2, SHE ET 3, SRM 51-30-2 AND 51-30-5. (M) 2 L 7 2 4F A6WE 1996041200576 19960412 00576 WP 1996 4 12 CAL960302 1 19960309 A 5400 AVB701610 GUSSET DOUG DC10 DC1010 3022110 WP NR 2 ENG PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68041 76758 46900 KUL - INSPECTION FOUND A 1.5 INCH CRACK IN NR 2 ENGINE PYLON RIGHT GUSSET. THE GUSSET WAS REPAIRED IAW ECRA 5410-01393. (M) 2 L 7 3 4F A22WE 1996041200577 19960412 00577 WP 1996 4 12 CAL960303 1 19960307 A 5210 INTERCOSTAL DOUG DC9 DC932 3022066 WP MAIN CABIN DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19504 55486 47638 HOU - INSPECTION FOUND A .5 INCH CRACK IN MAIN CABIN DOOR INTERCOSTAL. THE INTERCOSTAL WAS REPAIRED IAW SRM 52-05, FIGU RE 45. (M) 2 L 7 2 4F A6WE 1996041200578 19960412 00578 WP 1996 4 12 CAL960304 1 19960312 A 4990 3812761 APU DOUG DC9 DC983 3022083 WP ACFT TAIL LEAKING OIL A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 14879 21732 7149 49526 FLT NR 633 - IAH - THE AIRCRAFT HAD A BRIEF HISTORY OF SMOKE APPEARING BRIEFLY IN THE CABIN DURING CLIMB-OUT. MAINTENAN CE FOUND THE APU LEAKING OIL. THE OIL TANK LEVEL WAS FOUND LOW. THE OIL WAS PASSING BY COMPRESSOR CARBON SEAL AND THEN WAS BLOWN OUT OF LOAD CONTROL VALVE INTO THE BLEED SYSTEM CAUSING SMOKE IN CABIN. THE APU WAS REMOVED AND REPLACED. I N ADDITION, BOTH PACK COALESCER BAGS WERE REMOVED AND REPLACED. (M) 2 L 7 2 4F RT A6WE 1996041200579 19960412 00579 WP 1996 4 12 CKSA96010 1 19960201 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 420 CORROSION A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 39007 46147 KYIP - DURING B-CHECK INSPECTION, FOUND AT STATION 420 FUSELAGE SKIN RIGHT SIDE LEVEL 2 CORROSION BETWEEN LONGERON 35R A ND 34R. REMOVED CORROSION AND TREATED AREA IAW DC-8 SRM 51-1-8 PARA 1 THROUGH 3. INSTALLED DOUBLER REPAIR IAW DC-8 SRM 53-2-1 FUSELAGE SLATING REPAIR CLASS 1 REPAIR FIG 7. (M) 2 L 7 4 4F 4A25 1996041200580 19960412 00580 WP 1996 4 12 CKSA96011 1 19960201 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 600 CORROSION A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 39007 46147 KYIP - DURING B-CHECK INSPECTION, FOUND APPROXIMATELY STATION 600 FUSELAGE SKIN AT STRINGER 34R LEVEL 2 CORROSION AT LON GERON 34R. REMOVED CORROSION AND TREATED AREA IAW DC-8 SRM 51-1-8 PARA 1 THROUGH 3. INSTALLED DOUBLER REPAIR IAW SKETC H AIA/E/2351 DATED 1-26-96. COMPLIED WITH EA NR 96-027 DATED 1-27-96. (M) 2 L 7 4 4F 4A25 1996041200581 19960412 00581 WP 1996 4 12 CKSA96016 1 19960213 A 2612 24409921 FIRE LOOP DOUG DC8 DC8F55 3021928 WP NR 4 ENGINE FAILED A CKSA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 809CK 64536 45803 KMIA - NR 4 ENGINE FIRE WARNING LIGHT FLICKERED A FEW TIMES, WITH POWER PULLED BACK TO 1.50 EPR ALL PARAMETERS NORMAL AN D NO FLICKERING LIGHT. PERFORMED PRECAUTIONARY SHUT DOWN. REMOVED AND REPLACED LOWER FIRE WARNING LOOP ON NR 4 ENGINE. OPS CHECKS NORMAL IAW 26-2-0. (M) 2 L 7 4 4F 4A25 1996041200582 19960412 00582 NE 1996 4 12 GLBA96015 2 19960122 A 7310 FUEL LINE EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE LOOSE A GLBA C D ABORTED TAKEOFF RETURN TO BLOCK Y ENGINE STOPPAGE TO TAKEOFF 1 CE 01 129AM 120119 RDU - CREW ABORTED TAKEOFF WHEN RIGHT ENGINE FAILED ON TAKEOFF RUN. AIRCRAFT RETURNED TO GATE WHERE MAINTENANCE REPAIRE D LOOSE FUEL LINE ON RIGHT FLOW DIVIDER. OPS CHECK GOOD FOLLOWING REPAIR. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1996041200583 19960412 00583 NE 1996 4 12 GLBA96043 2 19960302 A 7261 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE LT/RT LOW OIL A GLBA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 01 281UE 120092 IMT - CREW REPORTED AURAL OIL PRESSURE WARNING SOUNDED WHILE TAXIING FOR TAKEOFF. CREW RETURNED TO GATE. MAINTENANCE S ERVICED ENGINE WITH OIL. OPS CHECK GOOD. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1996041200584 19960412 00584 CE 1996 4 12 GLBA96044 1 19960303 A 7603 MS250851 SWITCH BEECH 1900 1900C 1154161 CE POWER LEVER OUT OF ADJUST A GLBA O OTHER O OTHER AP APPROACH 1 CE 01 98GL UC98 CIU - CREW REPORTED PROPS GO TO LOW PITCH WHEN POWER IS PULLED TO IDLE IN FLAIR. MAINTENANCE ADJUSTED POWER LEVER MICRO SWITCH. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A24CE 1996041200585 19960412 00585 SO 1996 4 12 GLBA96045 1 19960303 A 3231 RETRACT MECH EMB 120 EMB120ER 3260203 SO NLG DOORS MALFUNCTIONED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 297UX 120297 BIS - CREW REPORTED NOSE GEAR DOORS DID NOT CLOSE AFTER TAKEOFF. CREW MADE AIR TURN BACK AND UNEVENTFUL LANDING. MAINT ENANCE CYCLED, MAINTENANCE SERVICED VALVE, BUT COULD NOT DUPLICATE DISCREPANCY. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A31SO 1996041200586 19960412 00586 EA 1996 4 12 GLBA96046 2 19960308 A 7261 ENGINE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA LEFT LOW OIL A GLBA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 01 67UE UC67 UIN - CREW REPORTED DROP IN LEFT OIL PRESSURE ON TAKEOFF ROLL. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE FOUND LEFT OIL LEVEL LOW AND SERVICED ENGINE WITH OIL. OPS CHECK GOOD. (M) 2 L 7 2 4T 4 T RT A24CE E4EA 1996041200587 19960412 00587 SO 1996 4 12 GLBA96047 1 19960307 A 2752 3203001007 ACTUATOR EMB 120 EMB120RT SO LT TE FLAP MALFUNCTIONED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 267UE 1154 120071 ORD - CREW REPORTED FLAP DISAGREEMENT FAULT ON TAKEOFF. THEY ELECTED AN AIR TURN BACK AND MADE AN UNEVENTFUL LANDING. M AINTENANCE COULD NOT FIND PROBLEM ON GROUND. LATER THE SAME DAY IN SUX THE PROBLEM REOCCURRED WITH AN AIR TURN BACK AND UNEVENTFUL LANDING. MAINTENANCE REMOVED AND REPLACED LEFT OUTBOARD FLAP ACTUATOR. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A31SO 1996041200588 19960412 00588 WP 1996 4 12 GRAA9614 1 19960210 A 3350 EA1D131DE BATTERIES DOUG DC9 DC982 3022082 WP COCKPIT DISCHARGED A GRAA K NONE L NO TEST IN INSP/MAINT 1 WP 11 500TR 49144 ON AIRCRAFT EMERGENCY LIGHTS IN THE COCKPIT WENT DIM. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERIES. M AINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM. NO DEFECTS NOTED. OPERATIONAL CHECKED NORMAL. 2 L 7 2 4F A6WE 1996041200589 19960412 00589 WP 1996 4 12 GRAA9615 1 19960222 A 3350 G011775 POWER SUPPLY DOUG DC9 DC915 3022036 WP CABIN FAILED A GRAA K NONE L NO TEST IN INSP/MAINT 1 WP 11 1070T 45784 LINE MAINTENANCE AT RNO DISCOVERED THE RIGHT EMERGENCY OVERWING EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACE D POWER SUPPLY. OPERATIONAL CHECKED NORMAL, NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1996041200590 19960412 00590 WP 1996 4 12 GRAA9616 1 19960313 A 3350 100865 BATTERY PACK DOUG DC9 DC987 3022087 WP CABIN DISCHARGED A GRAA K NONE L NO TEST IN INSP/MAINT 1 WP 11 1075T 49724 LINE MAINTENANCE AT RNO, DISCOVERED THAT THE LEFT ACCESSORY COMPARTMENT EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY POWER SUPPLY PACK. MAINTENANCE PERFORMED AND OPERATIONAL CHECK OF THE SYS TEM. THE EMERGENCY FLOOR TRACK SYSTEM CHECKED NORMAL, NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A6WE 1996041200591 19960412 00591 WP 1996 4 12 GRAA9617 1 19960314 A 3350 EA1D131DE BATTERY PACK DOUG DC9 DC915 3022036 WP CATWALK DISCHARGED A GRAA K NONE L NO TEST IN INSP/MAINT 1 WP 11 1068T 45782 LINE MAINTENANCE AT MYR, DISCOVERED THAT THE CATWALK EMERGENCY LIGHTING SYSTEM HAD FAILED. MAINTENANCE REMOVED AND REPL ACED THE BATTERIES. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM. THE EMERGENCY LIGHT SYST EM OPERATIONAL CHECKED NORMAL. NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1996041200592 19960412 00592 WP 1996 4 12 GRAA9618 1 19960314 A 3350 BRACKET DOUG DC9 DC915 3022036 WP CATWALK LOOSE A GRAA K NONE O OTHER IN INSP/MAINT 1 WP 11 1068T 45782 LINE MAINTENANCE AT MYR, DISCOVERED THE CATWALK EMERGENCY LIGHT BRACKET LOOSE. MAINTENANCE SECURED THE EMERGENCY LIGHT BRACKET TO THE CATWALK. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM. THE EMERGENCY LIGHT SYSTEM CHECKED NORMAL. NO DEFECTS NOTED. (M) 2 L 7 2 4F A6WE 1996041200593 19960412 00593 WP 1996 4 12 GRAA9619 1 19960311 A 3350 BC50444105 LENS DOUG DC9 DC915 3022036 WP CABIN CRACKED A GRAA K NONE O OTHER IN INSP/MAINT 1 WP 11 1068T 45782 LINE MAINTENANCE AT MYR, DISCOVERED THAT THE EMERGENCY EXIT SIGN LENS WERE CRACKED. MAINTENACNE REMOVED AND REPLACED TH E EMERGENCY EXIT SIGN LENS. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1996041200594 19960412 00594 EA 1996 4 12 HNAA9690514 1 19960301 A 2150 7506601 AIR CYCLE MACH HAMSTD DHAV DHC7 DHC7102 2802708 EA LEFT FAILED A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 EA 07 905HA 12200 1236 48907 070 FLT NR 3055 - ORF-DCA - DURING PREFLIGHT CHECKS, THE CABIN FILLED WITH SMOKE. THE LEFT PACK WENT RED LINE AND AUTO SHUT OFF DID NOT WORK. FOUND AIR CYCLE MACHINE SEIZED. REMOVED AND REPLACED THE LEFT AIR CYCLE MACHINE AND THE LEFT DUCT TE MP SWITCH. (M) 2 H 7 4 4T A20EA 1996041200595 19960412 00595 NM 1996 4 12 HNAA9692415 1 19960304 A 3232 82970018011 ACTUATOR DHAV DHC8 DHC8102 2809003 NM RT MLG DOOR FAILED A HNAA O OTHER N FALSE WARNING CL CLIMB 1 EA 07 924HA 1849 LI0430 105 FLT NR 3046 - FLL-TPA - AFTER TAKEOFF AND GEAR RETRACTION, THE RIGHT GEAR DOOR CAUTION LIGHT STAYED ILLUMINATED. THE DO OR CLOSED, BUT THE LIGHT REMAINED ON THE AIRCRAFT CONTINUED ON TO TPA AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE RIGHT FORWARD GEAR DOOR ACTUATOR. (M) 2 H 7 2 4T RT A13NM 1996041200596 19960412 00596 NM 1996 4 12 HNAA9692417 1 19960306 A 3350 6004791 BASE GRIMES DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 924HA 21071 105 FLT NR 3040 - FLL-TPA - DURING PREFLIGHT WALKAROUND, FOUND DS3 AND DS4 FLOOR PROX EMERGENCY LIGHTS INOP. REMOVED AND RE PLACED BASE AND BATTERY. (M) 2 H 7 2 4T RT A13NM 1996041200597 19960412 00597 SW 1996 4 12 MALA4896 1 19960303 A 2910 2781032265 HYD LINE SWRNGN SA227 SA227AC 8780603 SW RT NACELLE CHAFED A MALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 15 445MA AC687 FLT NR 3285 - AFTER DEPARTURE FROM MLI, BOTH HYDRAULIC PRESSURE CAUTION LIGHTS ILLUMINATED AND THE HYDRAULIC PRESSURE DR OPPED TO ZERO. THE CREW ELECTED TO RETURN TO MLI AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLA CED A HYDRAULIC PUMP PRESSURE LINE IN THE RIGHT NACELLE. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2 L 7 2 4T RT A8SW 1996041200598 19960412 00598 SW 1996 4 12 MALA964899 1 19960306 A 3230 RETRACT MECH SWRNGN SA227 SA227AC 8780603 SW NLG LACK OF LUBE A MALA O OTHER J WARNING INDICATION CL CLIMB 1 GL 15 60NE AC760B FLT NR 3271 - ON CLIMB-OUT FROM STC, THE NOSE GEAR BEGAN TO CYCLE AFTER THE GEAR WAS RETRACTED. THE CREW CYCLED THE GEA R UNTIL THE INTRANSIT LIGHT REMAINED EXTINGUISHED. THE AIRCRAFT CONTINUED TO MSP WITHOUT FURTHER INCIDENT. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. AS A PRECAUTION, THE GEAR WAS CLEANED AND LUBRICATED AND THE UPLOCK SWITCH WA S RERIGGED. (M) 2 L 7 2 4T RT A8SW 1996041200599 19960412 00599 SW 1996 4 12 MALA964900 1 19960307 A 3233 2751016003 ACTUATOR SWRNGN SA227 SA227AC 8780603 SW RT MLG DIRTY A MALA O OTHER J WARNING INDICATION AP APPROACH 1 GL 15 425MA AC640 FLT NR 3346 - ON APPROACH TO CWA, THE RIGHT GEAR INTRANSIT LIGHT REMAINED ILLUMINATED. THE CREW CYCLED THE GEAR AND THE PROBLEM PERSISTED. THE CREW PERFORMED AN EMERGENCY EXTENSION AND ALL INDICATIONS WERE NORMAL. MAINTENANCE NOTED THAT THE EMERGENCY EXTENSION ACTUATOR WOULD NOT FULLY EXTEND DURING GEAR SWINGS. MAINTENANCE CLEANED AND LUBED THE ACTUATOR AS WELL AS OTHER GEAR COMPONENTS. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2 L 7 2 4T RT A8SW 1996041200600 19960412 00600 SW 1996 4 12 MALA964901 1 19960306 A 5210 2724044010 CORNER SWRNGN SA227 SA227AC 8780603 SW PAX DOOR CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428MA AC646 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE LOWER FORWARD DOOR CORNER TO BE CRACKED. REPAIRS WERE COMPL ETED BY REPLACING THE CORNER IAW FAC SRM 51-00-00. (M) 2 L 7 2 4T RT A8SW 1996041200601 19960412 00601 SW 1996 4 12 MALA964902 1 19960307 A 5210 FRAME SWRNGN SA227 SA227AC 8780603 SW PAX DOOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428MA AC646 DURING A SCHEDULED INSPECTION IN MSP, THE PASSENGER DOOR FORWARD SIDE FRAME WAS CHAFED THROUGH AT THE CENTER BAYONET ARE A. REPAIRS WERE COMPLETED BY INSTALLING AN ELEVEN INCH DOUBLER IAW FAC SRM 52-90-10 PAGES 5-7 AS PER FAC LAR 96-MALA-04 3. (M) 2 L 7 2 4T RT A8SW 1996041200602 19960412 00602 WP 1996 4 12 RRXA9600010 1 19960306 A 3260 0080004002 PROX BOX DOUG DC8 DC863 302198A WP RT MLG DOOR MALFUNCTIONED A RRXA O OTHER N FALSE WARNING CL CLIMB 1 WP 15 951R 220 46092 KDAY - FLIGHT 212 - AFTER GEAR RETRACTION THE DOOR NOT LATCHED LIGHT AND THE RIGHT ALTERNATE GEAR DOOR LIGHT REMAINED IL LUMINATED. GEAR UPLATCH FAILURE PROCEDURE WAS ACCOMPLISHED. NO HELP WITH SEVERAL GEAR CYCLES. MAINTENANCE PERFORMED A N ALTERNATE GEAR DOOR CHECK AND GEAR SWING, NO DEFECTS NOTED. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND GEAR DOOR PROX SWITCH, PROXIMITY UNIT AND GREASED THE GEAR UPLATCH MECHANISM AS A PRECAUTION. (M) 2 L 7 4 4F 4A25 1996041200603 19960412 00603 EU 1996 4 12 SABA960008 1 19960308 A 3260 622800200 DOWNLOCK SWITCH BAG JETSTM JETSTM3101 1500215 EU NLG MALFUNCTIONED A SABA L A ABORTED APPROACH UNSCHED LANDING P NO WARNING INDICATION AP APPROACH 1 SO 33 170PC 717 ON APPROACH INTO ISO WHEN THE GEAR WAS SELECTED DOWN, THE N/G DOWN AND LOCKED LIGHT FAILED TO ILLUMINATE. ABORTED APPRO ACH RECYCLED THE GEAR AND STILL NO N/G IND. DECLARED EMERG AND DIVERTED TO RDU. CAPT DID A FLYBY AND THE TOWER VERIFIE D THE GEAR WAS IN THE DOWN POSITION. ON SHORT FINAL, THE N/G DOWN LIGHT ILLUMINATED. THE A/C LANDED W/O INCIDENT. SHU T THE A/C DOWN AND ATTEMPTED TO DEPLANE PAX, BUT THE MAIN CABIN DOOR COULD NOT BE OPENED. F/O DEPLANED PAX THRU EMERG E XIT. A/C WAS JACKED UP AND THE L/G IND SYS FUNCTION TESTED. ALL IND NORMAL. REPLACED N/G DN LOCK SW. THE SW WAS TESTE D. CABIN DOOR LINKAGED WAS CLEANED AND LUBED. DOOR CYCLED INSIDE AND OUTSIDE W/O PROBLEMS. A/C RETURNED TO SERV. (M) 2 L 7 2 4T RT A21EU 1996041200604 19960412 00604 WP 1996 4 12 SABA960009 2 19960315 A 7314 FULE PUMP BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110U 01514 WP LT ENGINE FAILED A A SABA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 SO 33 158PC 763 P63222 FLT NR 5017 - OAJ-CLT - ON FINAL APPROACH, LEFT ENGINE SHUT ITSELF DOWN. THE CAPTAIN DECLARED AND EMERGENCY, FOLLOWED C HECKLIST AND THEN LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL WAS DISPATCHED TO TROUBLESHOOT THE PROBLEM. THE CHIP DETECTOR WAS PULLED AND METAL GEAR TEETH WERE FOUND. FURTHER TROUBLESHOOTING FOUND THAT THESE WERE THE TEETH FOR THE FU EL PUMP DRIVE GEAR. THE AIRCRAFT IS CURRENTLY HAVING THE LEFT ENGINE REPLACED. (M) 2 L 7 2 4T 4 T RT A21EU E4WE 1996041200605 19960412 00605 EU 1996 4 12 SIMA0960491 1 19960218 A 3230 RETRACT MECH SAAB SF340 340B 7860101 EU LANDING GEAR MALFUNCTIONED A SIMA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 588MA 340B169 ON FINAL APPROACH, GOT A HYD CAP LIGHT. THE EMERG GEAR ACCUM WAS ZERO, THE MAIN WAS NORM. QTY WAS IN GREEN. SLOWED TO 200 KTS AND PUT THE GEAR HANDLE DOWN. THERE WAS NO MOVEMENT OF THE GEAR, NO INTRANSIT LIGHT IN GEAR HANDLE. NO GREEN GEAR IND LIGHTS, BY THIS TIME MAIN ACCUMULATOR PRESS WENT TO 0. INITIATED SUCCESSFUL EMERG GEAR EXTENSION. AFTER THE G EAR WAS DOWN AND LOCKED ALL HYD IND WERE NORM AFTER TOUCHDOWN. ALL BRAKING AND STEERING NORMAL, LANDED WITH FLAPS 20 DE GREES, THEY ALSO WORKED NORM. PERFORMED A COMPLETE HYD AND L/G CHECK. CHK'D PRESS SWITCH 9ML, C/B 1ML AND 5ML RELAG 7M L AND OPS CHK'D OF HYD PUMP AND PERFORMED GEAR SWING 25 TIMES, NO DISCREP IAW SAAB MM 29-10-00. A/C RETURNED TO SERV. M 2 L 7 2 4T RT A52EU 1996041200606 19960412 00606 EU 1996 4 12 SIMA960371 1 19960206 A 3350 330150 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 370AM 1109 340B370 DFW - WHILE PARKED AT THE GATE, MX FOUND ROW NINE FLOOR EMERGENCY LIGHTS INOPERABLE. MX REPLACED THE POWER SUPPLY. CHE CKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1996041200607 19960412 00607 NE 1996 4 12 SIMA960421 3 19960211 A 6114 660714258 HUB SAAB SF340 340B 7860101 EU ROTOL R375 R3754123F21 NE LT PROP CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 588MA 110890 340B169 DRG306387 LAW - SHOP DURING THE HUB P/N 660714258, S/N 110890 NDT, INSPECTION PER AD 93-19-01 A CRACK WAS FOUND BETWEEN MOUNTING B OLT HOLES NR 8 AND NR 9. THE HUB WAS REMOVED FROM SERVICE. (M) 2 L 7 2 4T RT A52EU 6 C P17NE 1996041200608 19960412 00608 1996 4 12 SIMA960461 4 19960215 A 3140 MULT FUNC COMP AEROSP ATR72 ATR72212 EU RIGHT MALFUNCTIONED A SIMA E ENGINE SHUTDOWN B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 SW 21 288AM 288 DFW - FLT NR 3596 - SMOKE IN COCKPIT AND CABIN, AIRCRAFT EMERGENCY EVACUATION. 1B MULTI FUNCTION COMPUTER FAULTED AND W OULD NOT RESET. GROUND RAN AIRCRAFT FOR 10 MINUTES, FOUND NO SMOKE IN COCKPIT OR CABIN, 1B MULTI FUNCTION COMPUTER DID NOT FAULT. AFTER RESET NO DEFECTS NOTED, AFTER FURTHER TROUBLESHOOTING RAI P2.5/P3 SWITCHING VALVE INNER HOUSING AND PI STON RING. GROUND RAN AIRCRAFT AND WITH NO DEFECTS NOTED AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996041200609 19960412 00609 EU 1996 4 12 SIMA960471 1 19960216 A 3350 14803180 CONNECTOR SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 592MA 340B199 DFW - FLT NR 3646 - EMERGENCY EXIT LIGHT INOP OVER EXIT ROW ON LEFT SIDE. FIXED PIN ON CANNON PLUG T LEFT EMERGENCY EXI T SIGN. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1996041200610 19960412 00610 EU 1996 4 12 SIMA960522 1 19960221 A 3260 15516 SWITCH AEROSP ATR72 ATR72212 EU NLG FAILED A SIMA O OTHER N FALSE WARNING CR CRUISE 1 SW 21 377AT 377 DFW - FLT NR 3651 - NOSE LANDING GEAR UPPER PANEL INDICATES UNLOCK INFLIGHT AND THE GEAR IS MAKING A CLICKING SOUND. MX REPLACED THE NOSE GEAR UPLOCK MICROSWITCH. CHECKED GOOD AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996041200611 19960412 00611 NE 1996 4 12 SIMA960641 2 19960304 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE NR 2 MALFUNCTIONED A SIMA O OTHER J R WARNING INDICATION PARTIAL RPM/PWR LOSS CR CRUISE 1 SW 21 591MA 340B192 GEE785538 FLT NR 3562 - DURING CRUISE FLIGHT THE NR 2 ENGINE EXPERIENCED A POWER INTERUPTION, ENGINE AUTO RELIGHTED, THERE WAS NO VISIBLE MOISTURE. INSPECTED NR 2 ENGINE COMPRESSOR AND VARIABLE GUIDE VANE ACTUATING SYSTEM. CHECKED GOOD, AIRCRAFT RE TURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 1996041200612 19960412 00612 EU 1996 4 12 SIMA960701 1 19960310 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 248AT 291 248 DFW - FLT NR 3851 - EMERGENCY FLOOR LIGHTS AT ROWS 1,3, 5 INOPERABLE ISSUED MEL. RAI'D FUSE AT 61WL AND RAI'D POWER SUP PLY AT 62WL NOTED BELOW. (M) 2 H 7 2 4T RT A53EU 1996041200613 19960412 00613 EU 1996 4 12 SIMA960711 1 19960311 A 3350 3011180 POWER SUPPLY AEROSP ATR42 ATR42300 8680920 EU CABIN DEFECTIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 422MQ 178 0028 RFD - DURING PS-2 CHECK MAINTENANCE DISCOVERED THE FORWARD CABIN INTERIOR EMERGENCY LIGHT REMAINED ILLUMINATED WHEN SELE CTED OFF. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT POWER SUPPLY IAW JIC 335121. SYSTEM OPERATIONAL LY CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996041200614 19960412 00614 EU 1996 4 12 SIMA960781 1 19960318 A 3040 NP1588121 WINDOW AEROSP ATR42 ATR42300 8680920 EU LT COCKPIT SHORTED A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 271AT 89312H1748 273 OFD - FLT NR 4074 - DISC-WIRE BURNING ODOR IN COCKPIT AFTER LEVEL TWO ANTI-ICE SELECTED. RAI'D CAPTAIN FORWARD SIDE WIN DSCREEN, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996041200618 19960412 00618 EU 1996 4 12 UF6A960205 1 19960216 A 3260 201139001 UPLOCK MECHANISM BAG ATP ATP EU LNG LACK OF LUBE A UF6A O OTHER N FALSE WARNING TO TAKEOFF 1 GL 31 856AW 8743 2032 SBN - UNSAFE GEAR INDICATION. MAINTENANCE LUBED NOSE GEAR UPLOCK MECHANISM. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4T RT A27NM 1996041200619 19960412 00619 WP 1996 4 12 USAA960214 1 19960228 A 5230 3912494501 PAN DOUG DC9 DC981 3022081 WP CARGO DOOR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 800US 37712 48034 PIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND SEVERAL AREAS OF LEVEL 1 CORROSION PREVIOUSLY REWORKED APPROXIMATELY 1 INCH BY 2 INCH SECTIONS FROM STATION 370 T0 427 CARGO DOOR PAN LOWER SECTION. SPLICED IN NEW LOWER PAN SECTION PER SRM 53-0 5 FIG 44. (M) 2 L 7 2 4F A6WE 1996041200620 19960412 00620 WP 1996 4 12 USAA960247 1 19960215 A 5330 SKIN DOUG DC9 DC981 3022081 WP BS 1437 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 809US 39406 48041 PIT - DURING C-1 CHECK INSPECTION, FOUND 1 INCH CRACK IN STATION 1437 LONGERON 4L FUSELAGE SKIN. INSTALLED DOUBLER REPA IR PER SRM 53-04 FIG 27. (M) 2 L 7 2 4F A6WE 1996041200621 19960412 00621 WP 1996 4 12 USAA960248 1 19960215 A 5330 SKIN DOUG DC9 DC981 3022081 WP BS 1437 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 809US 39406 48041 PIT - DURING C-1 CHECK INSPECTION, FOUND A 1 INCH CRACK IN STATION 1437 LONGERON 4R FUSELAGE SKIN. INSTALLED DOUBLER RE PAIR PER SRM 53-04 FIG 27. (M) 2 L 7 2 4F A6WE 1996041200622 19960412 00622 WP 1996 4 12 USAA960260 1 19960214 A 5530 ANGLE DOUG DC9 DC931 3022065 WP DORSAL FIN CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 912VJ 67588 47020 PIT - DURING C-3 CHECK INSPECTION, FOUND 1.5 INCH CRACK IN LEFT DORSAL FIN DRAG ANGLE AT STATION 1126. STOP DRILLED CRA CK AND INSTALLED DOUBLER REPAIR PER SRM 53-05 PG 506. (M) 2 L 7 2 4F A6WE 1996041200623 19960412 00623 WP 1996 4 12 USAA960261 1 19960218 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 930VJ 72891 45868 PIT - DURING C-4 CHECK INSPECTION, FOUND .125 INCH CRACK IN SKIN COMING FROM RIVET AT LOWER AFT CORNER OF MED STAIR DOOR OPENING STATION 200. INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 57A. (M) 2 L 7 2 4F A6WE 1996041200624 19960412 00624 WP 1996 4 12 USAA960262 1 19960218 A 5320 CLIP DOUG DC9 DC931 3022065 WP BS 775 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 930VJ 72891 45868 PIT - DURING C-4 CHECK INSPECTION, FOUND .125 INCH CRACK AT SKIN CLIP EMINATING FROM RIVET AT STATION 775 ON RIGHT SIDE LONGERON NR 1. INSTALLED CLASS 2 REPAIR DOUBLER PER SRM 53-04 FIG 12B. (M) 2 L 7 2 4F A6WE 1996041200625 19960412 00625 WP 1996 4 12 USAA960263 1 19960218 A 5320 CLIP DOUG DC9 DC931 3022065 WP BS 699 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 930VJ 72891 45868 PIT - DURING C-4 CHECK INSPECTION, FOUND .125 INCH CRACK AT SKIN CLIP EMINATING FROM A RIVET AT STATION 699 RIGHT LONGER ON NR 1. INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 12B CLASS 2. (M) 2 L 7 2 4F A6WE 1996041200626 19960412 00626 WP 1996 4 12 USAA960264 1 19960218 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 658 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 930VJ 72891 45868 PIT - DURING C-4 CHECK INSPECTION, FOUND .125 INCH CRACK IN SKIN CLIP EMINATING FROM RIVET AT STATION 658 RIGHT SIDE LON GERON NR 1. INSTALLED DOUBLER REPAIR CLASS 2 PER SRM 53-04 FIG 12B. (M) 2 L 7 2 4F A6WE 1996041200627 19960412 00627 WP 1996 4 12 USAA960265 1 19960219 A 5754 SKIN DOUG DC9 DC931 3022065 WP NR 1 LE SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 924VJ 35021 48144 PIT - PILOT REPORTED AFTER WALK AROUND THAT THERE WAS A 1 INCH CRACK IN THE LEFT WING LEADING EDGE NR 1 SLAT SKIN AT STA TION XF-126 ABOVE TELESCOPING ANTI-ICE DUCT. REMOVED CRACK AND INSTALLED FILLER AND DOUBLER REPAIR PER SRM 57-02 FIG 6. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1996041200628 19960412 00628 WP 1996 4 12 USAA960266 1 19960202 A 5532 59160886 SKIN DOUG DC9 DC981 3022081 WP VERT STAB CHAFFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 800US 37712 48034 PIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND .25 INCH BY 2 INCH CHAFFED .021 DEEP AT VERTICAL STABILIZER FORWARD LEFT SK IN. INSTALLED DOUBLER REPAIR PER SRM 55-01 FIG 2 SHEET 2. (M) 2 L 7 2 4F A6WE 1996041200629 19960412 00629 WP 1996 4 12 USAA960286 1 19960305 A 5320 991224355 ANGLE DOUG DC9 DC981 3022081 WP BS 1338 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 800US 37712 48034 PIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND SEVERAL 1 INCH BY 2 INCH AREAS OF LEVEL 1 CORROSION FLOOR BEAM RIGHT AFT LA V STATION 1338 IN UPPER CAP ANGLE '1'. CORROSION TASK NR C58-53300. SPLICED IN NEW SECTION OF UPPER CAP ANGLE PER USAI R TYPICAL REPAIR 53-10-14. (M) 2 L 7 2 4F A6WE 1996041200630 19960412 00630 WP 1996 4 12 USAA960288 1 19960305 A 5230 5912494501 PAN DOUG DC9 DC981 3022081 WP CARGO DOOR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 800US 37712 48034 PIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND LEVEL I CORROSION FORWARD CARGO LOWER DOOR PAN AT STATION 370 TO 427. CORR OSION TASK NR C51-53300. REMOVED AND REPLACED LOWER PAN WITH MODIFIED PAN P/N J060228-3 PER SRM 53-05 FIG 44. (M) 2 L 7 2 4F A6WE 1996041200631 19960412 00631 WP 1996 4 12 USAA960292 1 19960305 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 247-285 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 997VJ 69642 47336 PIT - DURING Q-4 INSPECTION DISCOVERED A CRACK 38.75 INCH LONG FORWARD FUSELAGE EXTERIOR SKIN FROM XPONDER ANT TO TCAS A NT STATION 247 TO 285 RUNNING ALONG LONGERON NR 1. AREA UNDER ADF CORRODED. (M) 2 L 7 2 4F A6WE 1996041200632 19960412 00632 WP 1996 4 12 USAA960293 1 19960305 A 5320 5930583183 JAMB CHANNEL DOUG DC9 DC981 3022081 WP RT MLG DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 800US 37712 48034 DURING Q-3/C-5 CHECK INSPECTION, FOUND 3.5 INCH CRACK IN FORWARD UPPER CORNER OF DOOR FRAME IN DOOR JAM 'Z' CHANNEL. RI GHT INBOARD GEAR DOOR. INSTALLED DOUBLERS J060200-52 AND -54 PER SRM 52-05 FIG 28. (M) 2 L 7 2 4F A6WE 1996041200633 19960412 00633 WP 1996 4 12 USAA960294 1 19960314 A 5320 9912243 CLIP DOUG DC9 DC982 3022082 WP BS 1307 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 821US 36106 49138 PIT - DURING Q6/C3 INSPECTION, FOUND LEVEL I CORROSION AT SKIN CLIP STATION 1307 FROM FLOOR LINE TO BULKHEAD SUPPORT. C ORROSION TASK NR C-58-53305 PREVIOUSLY REWORKED. MFG NEW SKIN CLIP P/N 9912043 PER DOUGLAS DRAWING 9912243. (M) 2 L 7 2 4F A6WE 1996041200634 19960412 00634 NM 1996 4 12 USAA960296 1 19960307 A 5240 65C340689 GATE HINGE BOEING 737 7372B7 1384560 NM RT SERV DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 275AU 35144 22887 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 13 INCH CRACK FORWARD RIGHT SERVICE DOOR, LOWER GATE HINGE. REPAIRED PE R EA 40887. (M) 2 L 7 2 4F A16WE 1996041200635 19960412 00635 NM 1996 4 12 USAA960297 1 19960307 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 1006 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 275AU 35144 22887 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 30 INCH BY 1 INCH FLOOR BEAM STATION 1006 BL '0' TO LBL 30. I NSTALLED FILLER AND STRAPS, REPAIRED PER TR 53-10-01A. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996041200636 19960412 00636 NM 1996 4 12 USAA960298 1 19960307 A 5313 STRINGER BOEING 737 7372B7 1384560 NM BS 767 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 275AU 35144 22887 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 3 INCH CORRODED AREA ON STRINGER 20L, BS 767 STRINGER. INSTAL LED STRINGER REPAIR, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-202-01, CORROSION LEVEL 1. (M) 2 L 7 2 4F A16WE 1996041200637 19960412 00637 NM 1996 4 12 USAA960299 1 19960307 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 967 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 275AU 35144 22887 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 5 INCH BY 2 INCH, 1 INCH BY 2 INCH AND 1 INCH BY 4 INCH FLOOR BEAM STATION 967 LBL 6, LBL 30, LBL 20 TO LBL 25. INSTALLED T-CAP, REPAIRED ANGLES AND STRAPS. REPAIRED PER TR 53-10-0 5C. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996041200638 19960412 00638 NM 1996 4 12 USAA960300 1 19960307 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 987 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 275AU 35144 22887 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 10 INCH BY 2 INCH, 2 INCH BY 33 INCH FLOOR BEAM STATION 987 RB L 12 TO RBL 45, LBL TO LBL 30. INSTALLED T-CAP REPAIR ENTIRE LENGTH, REPAIRED PER TR 53-10-05C. CORROSION TASK NR C53- 107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996041200639 19960412 00639 NM 1996 4 12 USAA960301 1 19960307 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 275AU 35144 22887 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND SIX 1 INCH BY 1 INCH CORRODED AREA AT FLOOR BEAM BS 344 LBL 50 INCH TO B L 'O'. SPLICED IN NEW SECTION OF T-ANGLE CAP. INSTALLED REPAIR ANGLES. REPAIRED PER TR 53-10-13. CORROSION TASK NR C 53-107-01, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996041200640 19960412 00640 NM 1996 4 12 USAA960302 1 19960307 A 5313 STRINGER BOEING 737 7372B7 1384560 NM BS 967-974 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 275AU 35144 22887 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND TWO CORRODED AREAS 7 INCH BY 1 INCH AT STRINGER BS 967 TO BS 974 AND BS 976 TO BS 982, S-25 L. REMOVED CORRODED STRINGER SECTION, FABRICATED AND INSTALLED NEW SECTION PER SRM 53-10-3. (M) 2 L 7 2 4F A16WE 1996041200641 19960412 00641 NM 1996 4 12 USAA960303 1 19960307 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 708-713 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 275AU 35144 22887 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 3 CRACKS .25 INCH AT WEB FOR FLOOR BEAM BL '0' BS 708 TO BS 713 WL 203. INSTALLED DOUBLERS, REPAIRED PER SRM 51-40-2. (M) 2 L 7 2 4F A16WE 1996041200642 19960412 00642 NM 1996 4 12 USAA960304 1 19960307 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 709-712 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 275AU 35144 22887 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND THREE .25 INCH CRACKED WEB, FLOOR BEAM BS 709 TO 712 BL 25 R WL 203. CU T OUT CRACKED SECTION OF WEB, FABRICATED AND INSTALLED DOUBLER PER SRM 51-40-2 FIG 1. (M) 2 L 7 2 4F A16WE 1996041200643 19960412 00643 NM 1996 4 12 USAA960305 1 19960307 A 5311 FRAME BOEING 737 7372B7 1384560 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 275AU 35144 22887 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK FRAME INNER CHORD, STATION 616 WL 203 LBL 60 LEFT SIDE. IN STALLED DOUBLER, PER EA 40894. (M) 2 L 7 2 4F A16WE 1996041200644 19960412 00644 NM 1996 4 12 USAA960306 1 19960307 A 5240 SKIN BOEING 737 7372B7 1384560 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 275AU 35144 22887 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND .375 INCH CRACK SKIN LOWER HINGE CUTOUT LOWER CORNER OF SERVICE DOOR. I NSTALLED DOUBLER, REPAIRED PER TR 52-10-05. (M) 2 L 7 2 4F A16WE 1996041200645 19960412 00645 WP 1996 4 12 USAA960308 1 19960314 A 5320 CUSP DOUG DC9 DC982 3022082 WP BS 1250 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 821US 36106 49138 PIT - DURING Q6/C3 INSPECTION, FOUND LEVEL 1 CORRSION PREVIOUSLY REWORKED AT STATION 1250 ON CUSP MEMBRANE. CORROSION T ASK NR C58-53301. FABRICATED NEW SECTION OF CUSP MEMBRANE OF 7075-T6 .040 INCH BY 10 INCHES WIDE FROM FUSELAGE TO SEAT TRACK PER SRM 53-05 FIG 97. (M) 2 L 7 2 4F A6WE 1996041200646 19960412 00646 WP 1996 4 12 USAA960309 1 19960314 A 5315 9958188 FLOOR BEAM DOUG DC9 DC982 3022082 WP BS 1322 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 821US 36106 49138 PIT - DURING Q6/C3 INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED ON FLOOR BEAM UNDER RIGHT LAV FLOOR PAN AT ST ATION 1322 UPPER FLANGE. CORROSION TASK NR C58-53300. CUT OUT DAMAGED AREA AND INSTALLED FABRICATED DOUBLERS PER SRM 5 3-05 FIG 73A AND USAIR EA 32198. (M) 2 L 7 2 4F A6WE 1996041200647 19960412 00647 NM 1996 4 12 USAA960310 1 19960314 A 5330 SKIN BOEING 737 737201 1384454 NM BS 767 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 248US 36852 22755 ROA - DURING CX-6 CHECK VISUAL INSPECTION, FOUND 2.5 INCH CRACK FUSELAGE SKIN STRINGER 18L BS 767. INSTALLED DOUBLER, R EPAIRED PER SRM 53-30-01. (M) 2 L 7 2 4F A16WE 1996041200648 19960412 00648 NM 1996 4 12 USAA960311 1 19960314 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 980-992 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 248US 36852 22755 ROA - DURING CX-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 12 INCH CORROSION S-27L BS 980 TO 992 STRINGER. REMOVED DAMA GED STRINGER, INSTALLED NEW STRINGER AND STRINGER SPLICE. REPAIRED PER SRM 53-10-3. (M) 2 L 7 2 4F A16WE 1996041200649 19960412 00649 EU 1996 4 12 USAA960312 1 19960313 A 5713 STRINGER FOKKER F28 F28MK4000 4990810 EU STA 4700 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 484US 20530 11234 PIT - DURING SIP VISIT INSPECTION, FOUND 2 INCH CRACK LEFT WING FUEL TANK 'Z' STRINGER NR 13 JUST OUTBOARD OF STATION 47 00, SIP REF 57-10-01. INSTALLED DOUBLER REPAIR PER USAIR EA NR 32309. (M) 2 L 7 2 4F RT A20EU 1996041200650 19960412 00650 EU 1996 4 12 USAA960313 1 19960313 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU NLG WW CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 484US 20530 11234 PIT - DURING SIP VISIT INSPECTION, FOUND .125 INCH CRACK IN FRAME STRIP AFT LEFT CORNER OF NOSE LANDING GEAR WHEEL WELL SIP REF 53-10-24. ROUTED OUT CRACKED AREA AND PRIMED AND PAINTED PER SRM 53-02-18 FIG 10 PARA 7. (M) 2 L 7 2 4F RT A20EU 1996041200651 19960412 00651 EU 1996 4 12 USAA960314 1 19960313 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU NR 2 WINDOW POST CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 484US 20530 11234 PIT -DURING SIP VISIT INSPECTION, FOUND .375 INCH CRACK IN FUSELAGE SKIN AT LEFT NR 2 WINDOW POST ATTACH FLANGE. EDDY C URRENT INSPECTION REF SIP 53-10-08, PG 2. STOP DRILLED CRACK AND INSTALLED DOUBLER PER USAIR EA NR 32299. (M) 2 L 7 2 4F RT A20EU 1996041200652 19960412 00652 NM 1996 4 12 USAABB96007 1 19960307 A 2150 PACK BOEING 767 7672B7 1385107 NM LT AIR COND FAILED A USAA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 EA 19 651US 24764 PIT - FLT 10 - DURING TAKEOFF FROM PIT, THE LEFT AIR CONDITIONING PACK KICKED OFF. FLIGHT RETURNED TO PIT AND LANDED WI TH NO FURTHER INCIDENT. MAINTENANCE PERFORMED BITE ON THE PACK CONTROLLERS. NO FAULT WAS FOUND. THE RIGHT PACK TEMPER ATURE CONTROL VALVE WAS REPLACED AS PRECAUTION. (M) 2 L 7 2 4F RT A1NM 1996041200653 19960412 00653 WP 1996 4 12 USAAD96019A 1 19960204 A 2130 94840213 PRESS AMPLIFIER DOUG DC9 DC931 3022065 WP COCKPIT FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 933VJ 31686 47216 LGA - FL 8002 - CREW REPORTED, THAT THE AIRCRAFT WOULD NOT PRESSURIZE ABOVE 10,000 FEET. FLIGHT DIVERTED TO LGA AND LAN DED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE CABIN PRESSURE AMPLIFIER. (M) 2 L 7 2 4F A6WE 1996041200654 19960412 00654 WP 1996 4 12 USAAD96020A 1 19960204 A 3230 RETRACT MECH DOUG DC9 DC981 3022081 WP NOSE GEAR MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 812US 48092 DCA - FLT NR 2287 - AFTER TAKEOFF AND ON GEAR RETRACTION, CREW COULD NOT RETRACT THE NOSE GEAR. CREW CYCLED THE GEAR TW ICE WITH THE SAME RESULT. FLIGHT RETURNED TO DCA AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE CHECKED THE RETRACTI ON OF THE NOSE GEAR, AND CYCLED IT SEVERAL TIMES. CHECKED GROUND SENSE CONTROL AND ANTI-RETRACTION CABLE RIG. NO PROBL EMS FOUND. SERVICED STRUT TO CORRECT PRESSURE. (M) 2 L 7 2 4F A6WE 1996041200655 19960412 00655 WP 1996 4 12 USAAD96023 1 19960214 A 4920 360452411 BURNER CAN DOUG DC9 DC931 3022065 WP APU CRACKED A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 EA 19 935VJ 48115 PIT - FLT 858 - FLT RETURNED TO FIELD WHEN APU SHUTDOWN. LEFT GENERATOR WAS ON MEL. MAINTENANCE REPLACED THE APU BURNE R CAN AND THE LEFT GENERATOR, CSD AND COOLER. (M) 2 L 7 2 4F A6WE 1996041200656 19960412 00656 WP 1996 4 12 USAAD96024 1 19960217 A 3231 RETRACT MECH DOUG DC9 DC931 3022065 WP RT MLG DOOR MALFUNCTIONED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 981VJ 48157 FLT NR 349 - BWI - DURING RETRACTION NOSE GEAR MADE LOUD NOISE, CYCLED NO HELP. MAINTENANCE FOUND RT DOOR OPEN, CLOSED DOOR, BOTH DOOR LATCHES CHECKED OK. (M) 2 L 7 2 4F A6WE 1996041200657 19960412 00657 1996 4 12 USAAD96025 4 19960225 A 2565 D29982121 SLIDE DOUG DC9 DC931 3022065 WP FWD GALLEY DR FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 927VJ 48154 FLT NR 517 - PHL - GALLEY EMERGENCY CHUTE PRESSURE IS 2500 PSI IN RED ZONE. REPLACED GALLEY EMERGENCY CHUTE. (M) 2 L 7 2 4F A6WE 1996041200658 19960412 00658 WP 1996 4 12 USAAD96026 1 19960229 A 2560 SLIDE DOUG DC9 DC982 3022082 WP CABIN DOOR FELL OUT A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 822US 49139 FLT NR 307 - LGA - LEFT AFT CABIN DOOR CHUTE DEPLOYED WHEN IT FELL FROM THE DOOR AFTER UTILITY ENTERED. GIRT BAR WAS ST OWED AND CAUGHT ON DOOR WHEN SLIDE PACK FELL. (M) 2 L 7 2 4F A6WE 1996041200659 19960412 00659 1996 4 12 USAAD96026A 4 19960229 A 2565 SLIDE DOUG DC9 DC982 3022082 WP CABIN DOOR MALFUNCTIONED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 822US 49139 FLT NR 307 - LGA - LEFT AFT CABIN DOOR CHUTE DEPLOYED WHEN IT FELL FROM THE DOOR AFTER UTILITY ENTERED. GIRT BAR WAS ST OWED AND CAUGHT ON DOOR WHEN SLIDE PACK FELL. MAINTENANCE REPLACED THE AFT DOOR EMERGENCY SLIDE. NO PROBLEM EXISTED WI TH THE SLIDES AS IT FUNCTIONED AS DESIGNED. (M) 2 L 7 2 4F A6WE 1996041200660 19960412 00660 WP 1996 4 12 USAAD96027 1 19960229 A 3230 RETRACT MECH DOUG DC9 DC931 3022065 WP NLG MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 980VJ 48156 FLT NR 1426 - BNA - UPON GEAR RETRACTION THE CREW GOT TWO GREEN LIGHTS ON THE MAIN GEAR AND RED LIGHT ON THE NOSE GEAR. CREW ALSO, HEARD A LOUD NOISE FROM THE NOSE GEAR AREA. RETURNED TO FIELD. (M) 2 L 7 2 4F A6WE 1996041200661 19960412 00661 WP 1996 4 12 USAAD96028 2 19960302 A 7510 577957 HEAT MANIFOLD DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7B 52053 NE RT ENGINE LEAKING A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 984VJ 47207 654808 CLT - FLT 1426 - IMMEDIATELY AFTER TAKEOFF FROM CLT, THE RIGHT ENGINE 'B' FIRE LOOP LIGHT ILLUMINATED. SHORTLY THEREAFT ER, THE RIGHT ENGINE FIRE WARNING LIGHTS ILLUMINATED. CREW REDUCED POWER ON THE ENGINE AND THE LIGHTS WENT OUT. FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT. ENGINE WAS NOT SHUT DOWN IN FLIGHT. MAINTENANCE FOUND THE THIRTE ENTH STAGE FUEL HEAT MANIFOLD LEAKING, REPLACED IT. (M) 2 L 7 2 4F 4 F A6WE E2EA 1996041200662 19960412 00662 WP 1996 4 12 USAAD96030 1 19960307 A 3260 801801 PROX SENSOR DOUG DC9 DC931 3022065 WP NLG MALFUNCTIONED A USAA O OTHER N FALSE WARNING AP APPROACH 1 EA 19 934VJ 48114 YUL - FLT 451 - ON APPROACH, WITH GEAR SELECTED DOWN, CREW RECEIVED NOSE GEAR UNSAFE LIGHT. CREW CYCLED THE GEAR, AND I NDICATIONS WERE NORMAL. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE NOSE LANDING GEAR PROXIMITY S ENSOR. (M) 2 L 7 2 4F A6WE 1996041200663 19960412 00663 NM 1996 4 12 USAASB96042 1 19960307 A 2410 731753 CSD BOEING 737 737201 1384454 NM NR 2 ENGINE OVERSERVICED A USAA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 EA 19 256AU 52704 16562 22798 FLT NR 2278 - LGA - AT FL 150 LOST RIGHT CSD. THE FLIGHT RETURNED TO FIELD AT LGA. THE APU WAS ON MEL. NR 2 CSD DISCO NNECTED FOR HIGH OIL PRESSURE. MAINTENANCE FOUND NR 2 CSD OVER SERVICED WITH OIL. DRAINED OIL LEVEL TO NORMAL. REMOVE D AND REPLACED CSD FILTER AS PRECAUTION. CHECKED IAW MM OPS CHECK OK. (M) 2 L 7 2 4F A16WE 1996041200664 19960412 00664 NM 1996 4 12 USAASB96043 1 19960307 A 2613 10604791 CONNECTOR BOEING 737 737201 1384454 NM LT WING FAILED A USAA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 EA 19 251AU 22757 FLT NR 311 - PHL - DURING TAKEOFF ROLL, LEFT WING BODY OVERHEAT LIGHT CAME ON. FLIGHT RETURNED TO FIELD. REPLACED CONN ECTOR D886. OPS CHECKS SATISFACTORY. (M) 2 L 7 2 4F A16WE 1996041200665 19960412 00665 WP 1996 4 12 UUSAA960215 1 19960228 A 5522 SKIN DOUG DC9 DC981 3022081 WP ELEVATOR HOLE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 800US 37712 48034 PIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND LIGHTING STRIKE HOLE APPROXIMATELY .250 INCH IN DIAMETER IN UPPER SKIN 30 I NCH FROM INBOARD END AND 18 INCH AFT OF LEADING EDGE. INSTALLED DOUBLER REPAIR PER SRM 55-03 FIG 15. (M) 2 L 7 2 4F A6WE 1996041200666 19960412 00666 EU 1996 4 12 VTZA96076 1 19960219 A 2120 AIR DIST JETAIR JETSTM JETSTM4101 1500501 EU CABIN ODOR A VTZA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 27 323UE 41059 FLT NR 6532 - LGA-IAD - DURING DESCENT, DECLARED A EMERGENCY DUE TO A SMOKE SMELL IN THE CABIN. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS AND ALL PASSENGERS SAFE. UPON FURTHER INVESTIGATIN, FLIGHT CREW TOLD MAINTENANCE THAT WHILE T HERE WAS NO VISIBLE SMOKE, THERE WAS A STRANGE SMELL. MAINTENACNE PEFORMED INSPECTION AND MAINTENANCE RUNS, BUT COULD F IND NO DEFECTS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996041200667 19960412 00667 1996 4 12 VTZA96078 4 19960214 A 3417 7000700953 DADC JETAIR JETSTM JETSTM4101 1500501 EU AVIONICS BAY FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 308UE 41023 FLT NR 6276 - IAD-EWR - DURING CRUISE, RETURNED TO IAD DUE TO THE LOSS OF RELIABLE AHRS INFORMATION ON BOTH SIDES. AIRC RAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE DIGITAL AIR DATA COMPUTER. AIRCRAFT WAS RELEA SED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996041200668 19960412 00668 EU 1996 4 12 VTZA96079 1 19960215 A 3240 91SE16 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU EMER BRAKE OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 305UE 41019 IAD-ORF - FLT NR 6432 - ABORTED THE TAKEOFF DUE TO THE TAKEOFF CONFIGURATION WARNING SYSTEM ACTIVATING. AIRCRAFT RETURN ED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED THE EMERGENCY BRAKE MICROSWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996041200669 19960412 00669 EU 1996 4 12 VTZA96080 1 19960215 A 5270 91SE16 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU EMER EXIT OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 325UE 41063 FLT NR 6205 - IAD-MHT - DURING TAKEOFF, ABORTED THE TAKEOFF DUE TO THE EMERGENCY DOOR WARNING LIGHT ILLUMINATING DURING THE TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED EMERGENCY DOOR MICROSWITCH ES. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996041200670 19960412 00670 EU 1996 4 12 VTZA96081 1 19960214 A 2611 72111211000 SMOKE DETECTORS JETAIR JETSTM JETSTM4101 1500501 EU BAGGAGE BAY FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 319UE 41042 FLT NR 6157 - IAD-RDU - TAKEOFF ABORTED DUE TO THE MAIN BAGGAGE BAY SMOKE LIGHT ILLUMINATING DURING THE TAKEOFF ROLL. A N EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS AND ALL PASSENGERS SAFE. MAINTENANCE R EPLACED THE AFT MAIN BAGGAGE BAY SMOKE DETECTOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996041200671 19960412 00671 EU 1996 4 12 VTZA96082 1 19960218 A 5270 31518217 SWITCH BAG JETSTM JETSTM3201 1500217 EU BAGGAGE DOOR FAILED A VTZA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 496UE 900 FLT NR 6236 - IAD-ELM - DURING TAXI FOR TAKEOFF, RETURNED TO GATE DUE TO THE POD DOOR WARNING LIGHT ILLUMINATING. AIRCR AFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE VERIFIED THAT THE DOOR WAS CLOSED AND OPENED DMI NR 04019 I AW MEL 52-1. MAINTENANCE LATER CLEARED DMI NR 04019 ON 02-19-96, BY REPLACING THE MICROSWITCH PLUNGER. AIRCRAFT WAS RE LEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996041200672 19960412 00672 EU 1996 4 12 VTZA96083 1 19960214 A 5210 1371383C402 DRAWBOLT BAG JETSTM JETSTM3201 1500217 EU MAIN PAX DOOR WORN A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 481UE 895 FLT NR 6521 - IAD-BDL - DURING CLIMB-OUT, RETURNED TO BDL DUE TO THE PAX DOOR WARNING LIGHT ILLUMINATING. AIRCRAFT RETU RNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE UPPER DRAWBOLT AND 4 BEARINGS. AIRCRAFT WAS RELEASED A ND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996041200673 19960412 00673 EU 1996 4 12 VTZA96084 1 19960213 A 3260 ATG1066 SWITCH BAG JETSTM JETSTM3201 1500217 EU LT MLG DIRTY A VTZA K NONE N FALSE WARNING AP APPROACH 1 EA 27 471UE 821 FLT NR 6198 - IAD-BDL - DURING APPROACH, DECLARED AN EMERGENCY DUE TO THE LEFT MAIN GEAR DID NOT INDICATE DOWN AND LOCKE D WHEN EXTENDED. AIRCRAFT LANDED WITH NO FURTHER INCIDENTS AND ALL PASSENGERS SAFE. MAINTENACNE CLEANED THE LEFT DOWNL OCK MICROSWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996041200674 19960412 00674 1996 4 12 VTZA96085 4 19960213 A 3418 13730612K STALL VANE BAG JETSTM JETSTM3201 1500217 EU LT/RT WING OUT OF ADJUST A VTZA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 27 481UE 895 FLT NR 6570 - IAD-MDT - ABORTED TAKEOFF DUE TO THE STALL WARNING AND STICK SHAKER SYSTEM ACTIVATING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED BOTH STALL VANES. AIRCRAFT WAS RELEASED AND APPROVED FOR RETUR N TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996041200675 19960412 00675 EU 1996 4 12 VTZA96086 1 19960220 A 3310 LT52A DIMMER SWITCH BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A VTZA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 27 470UE 814 FLT NR 6275 - ELM-IAD - DUIRNG CRUISE, NOTICED AN ELECTRICAL SMELL IN THE COCKPIT. AIRCRAFT LANDED AT IAD WITH NO FURTH ER INCIDENTS. MAINTENANCE REPLACED THE ROOF PANEL BACKLIGHTING DIMMER SWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR R ETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996041200676 19960412 00676 NM 1996 4 12 WRLA96001 1 19960106 A 2760 NAS6404U20 ACT ARM BOLT DOUG MD11 MD11F 3023600 NM SPOILER ACT MISSING A A WRLA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 EA 27 274WA 48633 WHILE TAXIING, FLIGHT CREW WAS PERFORMING FLIGHT CONTROL CHECK. LEFT INBOARD SPOILER WOULD NOT INDICATE 'FULL-UP' ON TE ST. FLIGHT CREW ELECTED TO RETURN TO GATE FOR CORRECTIVE ACTION. AIRCRAFT RETURN TO GATE WITHOUT FURTHER INCIDENT. MA INTENACNE TROUBLE SHOOTING NOTING SPOILER POSITION TRANSMITTER DISCONNECTED FROM ACTUATOR ARM (BOLT MISSING P/N NAS6404U 20). POSITION TRANSMITTER REINSTALLED. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. INSPECTED MD-11 FLEET, FOUND NO OTHER INCIDENT OF THIS TYPE. NO PREVIOUS HISTORY OF THIS TYPE. UNABLE TO DETERMINE IF FASTENER WAS IMPROPERLY INSTALL ED. NO FURTHER ACTION TAKEN. (M) 2 L 7 3 4F RT A22WE 1996041200677 19960412 00677 NM 1996 4 12 WRLA96008 1 19960206 A 2421 750875 IDG DOUG MD11 MD11 3023602 NM NR 2 ENG OVER SERVICED A WRLA E D ENGINE SHUTDOWN RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 273WA 48519 AFTER PUSHBACK FROM GATE, DURING ENG START, FLT CREW NOTED LOSS OF NR 2 ENG OIL PRESS IND ALONG WITH LOSS OF N1 AND OIL TEMPERATURE IND. FLT CREW SHUT DOWN NR 2 ENG AND TAXIED BACK TO GATE W/O FURTHER INCIDENT. MX TROUBLE SHOOTING LEAD MX PERSONNEL TO BELIEVE THAT NR 2 GENERATOR WAS DROPPING OFF LINE. MAINTENANCE PERSONNEL TROUBLE SHOT NR 2 INTEGRATED DRI VE GENERATOR (IDG), AND FOUND IT WAS OVER SERVICED WITH OIL. IDG WAS DRAINED OF ALL OIL. OIL FILTERS WERE REMOVED AND INSPECTED (NO CONTAMINATION FOUND), AND REINSTALLED. IDG WAS SERVICED TO THE CORRECT LEVEL. NR 2 ENGINE WAS GROUND RUN TO CHECK NR 2 IDG. NO FAULTS FOUND AND ALL ENGINE PARAMETERS WERE NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A22WE 1996041200678 19960412 00678 NE 1996 4 12 WRLA96010 2 19960210 A 7230 COMPRESSOR BLADE DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE NR 1 ENGINE FAILED A WRLA A E UNSCHED LANDING ENGINE SHUTDOWN E VIBRATION/BUFFET CR CRUISE 1 EA 27 271WA 48518 AT CRUISE/CLIMB TO 31,000 FEET, FLIGHT CREW EXPERIENCED WHAT THEY BELIEVE TO BE A COMPRESSOR STALL ON THE NR 1 ENGINE. E NGINE WAS RETARDED TO FLIGHT IDLE AND REACCELERATED TO CRUISE POWER. FLIGHT CREW AGAIN REPORTED POSSIBLE COMPRESSOR STA LL. FLT CREW ELECTED TO SHUT ENGINE DOWN AND DIVERT A/C TO RCTP. AIRCRAFT LANDED W/O FURTHER INCIDENT. MX PERSONNEL N OTICED METAL DEBRIS IN TAIL PIPE. ENG BORESCOPE IDENTIFIED ONE 5TH STAGE HIGH PRESSURE COMPRESSOR BLADE BROKEN AND MISS ING. SUBSTANTIAL DAMAGE NOTED IN ALL AREA OF HIGH PRESSURE COMPRESSOR AFT OF 5TH STAGE. ENG REPLACED, GROUND RUN OK. A/C RETURN TO SERVICE. WILL PROVIDE FOLLOW-UP DATA UPON COMPLETION OF INITIAL TEAR DOWN AT ENG REPAIR FACILILTY.(M) 2 L 7 3 4F 4 F RT A22WE E24NE 1996041200679 19960412 00679 WP 1996 4 12 WRLA96011 1 19960213 A 2611 30321R7 SMOKE DETECTOR DOUG DC10 DC1030F 3023504 WP CARGO COMPT DAMAGED A WRLA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 27 107WA 46836 DURING TAKEOFF, FLIGHT CREW HEARD A LOUD NOISE (BANG) COMING FROM UPPER DECK CARGO AREA. FLIGHT CREW ELECTED TO DISCONT INUE TAKEOFF (MAX SPEED ATTAINED 120 KNOTS). AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. UPON INSPECTION, MAIN TENANCE PERSONNEL FOUND NR 2 CENTER CEILING PANEL (WITH SMOKE DETECTOR) HAD FALLEN FROM CEILING TO CARGO FLOOR, DAMAGING SMOKE DETECTOR. SUSPECT CEILING PANEL WAS PARTIALLY DISLODGED DURING CARGO LOADING PROCESS AND FELL DOWN DUE TO VIBRAT ION OF TAKEOFF ROLL. DAMAGED SMOKE DETECTOR WAS REPLACED AND PANEL WAS REINSTALLED. SMOKE DETECTOR GROUND CHECKED GOOD . AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A22WE 1996041200680 19960412 00680 SO 1996 4 12 WTAA960032 1 19960213 A 5330 SKIN EMB 120 EMB120RT SO FWD FUSELAGE BIRD STIKE A WTAA K NONE C F.O.D. NR NOT REPORTED 1 WP 17 216YV 120216 ACV - BIRD STRIKE REPORTED AT UPPER LEFT FUSELAGE NOSE SECTION, AFT OF RADOME. MAINTENANCE ACCOMPLISHED BIRD STIKE INSP ECTION. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996041200681 19960412 00681 EU 1996 4 12 WTAA960033 1 19960212 A 7712 31024762 TQ SIGNAL COND BAG JETSTM JETSTM3101 1500215 EU NR 2 ENG OUT OF ADJUST A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 17 425UE 798 SFO - NR 2 ENGINE FAILED TO ACHIEVE REQUIRED TORQUE ON TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE REC ALIBRATED TORQUE INDICATION SYSTEM. ENGINE OPERATIONS NORMAL DURING GROUND RUN. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996041200682 19960412 00682 SO 1996 4 12 WTAA960035 1 19960216 A 3150 MS33202 CIRCUIT BREAKER EMB 120 EMB120RT SO COCKPIT TRIPPED A WTAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 17 201YW 120201 FAT - AURAL TRIM WARNING ACTIVATED DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. FOUND AURAL WARNING CIRCUIT BREAKER TRIPPED. RESET CIRCUIT BREAKER. WARNING SYSTEM OPERATIONAL CHECK NORMAL ON GROUND. UNABLE TO DUPLICATE REPORT ED DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996041200683 19960412 00683 EU 1996 4 12 WTAA960036 1 19960216 A 7712 31024766 TQ SIGNAL COND BAG JETSTM JETSTM3101 1500215 EU LT ENG FAILED A A WTAA A E UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 WP 17 420UE 788 LAX - LEFT ENGINE TORQUE INDICATION FLUCTUATION AND AIRCRAFT YAW TENDENCY REPORTED DURING CLIMB-OUT. CREW ACCOMPLISHED IN FLIGHT SHUTDOWN OF LEFT ENGINE AND RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE INSPECTED ENGINE AND INDICATING SYSTEM. DETERMINED PROBLEM TO BE CAUSED BY TORQUE INDICATION SYSTEM MALFUNCTION. REPLACED TORQUE SIGNAL CONDITIONER A ND CLEANED TORQUE RING CANNON PLUG. ENGINE OPERATION NORMAL DURING GROUND RUN. (M) 2 L 7 2 4T RT A21EU 1996041200684 19960412 00684 SO 1996 4 12 WTAA960052A 1 19960305 A 3010 38E966A PRESS REGULATOR EMB 120 EMB120RT SO LT WING FAILED A WTAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 17 276UE 120067 FAT - LEFT DUCT LEAK LIGHT ILLUMINATED AFTER DEPART. CREW DECLARED EMERG AND ACCOMP PRECAUTIONARY LT ENG SHUT DOWN PER 'QRH' PROCEDURES. LIGHT EXTINGUISHED AFTER INFLIGHT SHUTDOWN. A/C RETURNED TO STA WITHOUT INCIDENT. MX INSPECTED A/C AND FOUND THE LT WING DE-ICE SYSTEM PRESSURE REGULATOR TO HAVE ALLOWED AN OVER PRESSURE CONDITION, WHICH CAUSED THE WATE R SEPARATOR PRESSURE RELIEF VALVE TO OPEN. REPLACED PRESSURE REGULATOR AND WATER SEPARATOR. BLEED AIR SYSTEM OPERATION AL CHECK NORMAL DURING EXTENDED ENGINE GROUND RUN. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996041200685 19960412 00685 SO 1996 4 12 WTAA960052B 1 19960305 A 2170 44E202A WATER SEPARATOR EMB 120 EMB120RT SO LT WING LEAKING A WTAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 17 276UE 120067 FAT - LEFT DUCT LEAK LIGHT ILLUMINATED AFTER DEPART. CREW DECLARED EMERG AND ACCOMP PRECAUTIONARY LT ENG SHUT DOWN PER 'QRH' PROCEDURES. LIGHT EXTINGUISHED AFTER INFLIGHT SHUTDOWN. A/C RETURNED TO STA WITHOUT INCIDENT. MX INSPECTED A/C AND FOUND THE LT WING DE-ICE SYSTEM PRESSURE REGULATOR TO HAVE ALLOWED AN OVER PRESSURE CONDITION, WHICH CAUSED THE WATE R SEPARATOR PRESSURE RELIEF VALVE TO OPEN. REPLACED PRESSURE REGULATOR AND WATER SEPARATOR. BLEED AIR SYSTEM OPERATION AL CHECK NORMAL DURING EXTENDED ENGINE GROUND RUN. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996041200686 19960412 00686 SO 1996 4 12 WTAA960054 1 19960306 A 5270 JS5 ACTUATING ROLLER EMB 120 EMB120RT SO CARGO DOOR OUT OF ADJUST A WTAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 17 276UE 120067 SFO - CARGO DOOR WARNING LIGHT ILLUMINATED AFTER ROTATION. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE INSPECTED CARGO DOOR AND FOUND DOOR TO BE SECURE DETERMINED PROBLEM TO BE FLASE INDICATION. DEFERRED DOOR WARNING SYSTE M PER MRL 52-70-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED THE DEFERRED DOOR WARNING SYSTEM BY ADJUSTING THE CARGO DOOR ACTUATING ROLLER. (M) 2 L 7 2 4T RT A31SO 1996041200687 19960412 00687 WP 1996 4 12 WTAA960055 2 19960308 A 7200 ENGINE BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110U 01514 WP LEFT FAILED A A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 17 422UE 782 CIC - LEFT ENGINE TORQUE DROPPED TO 90 PERCENT TORQUE DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENAN CE REMOVED AND REPLACED LEFT ENGINE. OPERATIONAL CHECK OF LEFT ENGINE NORMAL DURING GROUND RUN. AIRCRAFT RETURNED TO S ERVICE. (M) 2 L 7 2 4T 4 T RT A21EU E4WE 1996041200701 19960412 00701 EA 1996 4 12 96ZZZX1708 2 19960322 A 7414 4371 MAGNETO SLICK PIPER PA28 PA28181 7102807 SO LYC O360 O360A4M 41514 EA IMPULSE COUPLING FAILED A CZPA K NONE O OTHER NR NOT REPORTED 1 EA 09 47431 1600 93060001 287690071 L2380436A IMPULSE COUPLING FAILED CAUSING SEIZURE OF MAGNETO, BREAKING MAGNETO CASE (SLICK). 1 L 7 1 3O 3 O 2A13 E286 1996041200709 19960412 00709 EU 1996 4 12 96ZZZX1716 1 19960125 A 6120 LEVER CAM HAMSTD AEROSP ATR72 ATR72212 EU PROP CONTL UNIT SHEARED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 PROPELLER CONTROL UNIT REMOVED PN 8088773 FROM SERVICE, HAD ITS CONDITION LEVER CAM SHEARED. PCU WAS AN EXCHANGE FROM S IMMONS WITH HAMILTON STANDARD ON AUGUST 14, 1994. 2 H 7 2 4T RT A53EU 1996041200724 19960412 00724 WP 1996 4 12 9607969102 1 19960209 A 5220 DOOR PAN DOUG DC9 DC915 3022036 WP LT EMER EXIT CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 92S 47064 DURING H-CHECK, FOUND A CRACK IN THE LEFT OVERWING EMERGENCY EXIT DOOR PAN AT THE NR 14 STOP. REPAIRED PAN (P/N 5913195 -1) PER EA 99-98739. 2 L 7 2 4F A6WE 1996041200725 19960412 00725 WP 1996 4 12 9607979611 1 19960227 A 5713 LONGERON DOUG DC9 DC932 3022066 WP WS 58-91 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 611NA 47435 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE CENTER WING STR 20 FROM WS 58R TO 91R. REPAIRED TH E STRINGER PER EA 12-5710-9-C0783. 2 L 7 2 4F A6WE 1996041200726 19960412 00726 WP 1996 4 12 9607989611 1 19960229 A 5320 ANGLE DOUG DC9 DC932 3022066 WP FS 200 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 611NA 47435 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE MAIN CABIN DOOR UPPER CUSP ANGLE FS 200 AT LONGERON 18L. REPAIRED ANGLE PER EA 12-5310-9-C0733. 2 L 7 2 4F A6WE 1996041200727 19960412 00727 WP 1996 4 12 9607999611 1 19960305 A 5511 CHORD DOUG DC9 DC932 3022066 WP LT HORIZ STAB CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 611NA 47435 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE LEFT HORIZONTAL STABILIZER REAR SPAR AT THE OUTBOAR D ELEVATOR HINGE BRACKET MOUNTING HOLES. REPAIRED THE UPPER AND LOWER SPAR CAPS PER EA 12-5510-9-C0794. 2 L 7 2 4F A6WE 1996041200728 19960412 00728 WP 1996 4 12 9608009861 1 19960327 A 5315 FLOOR BEAM DOUG DC9 DC951 3022051 WP FS 1151 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 770NC 47758 DURING H-CHECK, FOUND CORROSION ON THE FLOOR BEAM UPPER CAP AT FS 1151 LEFT SIDE. REPAIRED BEAM (P/N 9958188-1) PER EA 98-109489. 2 L 7 2 4F A6WE 1996041200729 19960412 00729 WP 1996 4 12 9608019611 1 19960327 A 5330 SKIN DOUG DC9 DC932 3022066 WP FS 370-427 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 611NA 47435 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE FUSELAGE SKIN AT LONGERON 27R FROM FS 370 TO 427. R EPAIRED SKIN PER EA 12-5330-9-C0829. 2 L 7 2 4F A6WE 1996041200730 19960412 00730 WP 1996 4 12 9608029750 1 19960403 A 5320 FITTING DOUG DC9 DC941 302207N WP FS 617 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 750NW 47114 DURING H-CHECK, FOUND A CRACK IN THE FS 617 FRAME FITTING AT THE RIGHT CUSP. REPLACED FITTING PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996041200731 19960412 00731 NM 1996 4 12 9608032296 1 19960404 A 5320 FITTING BOEING 727 727251 138408H NM TAIL SKID CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 296US 21788 DURING L-CHECK, FOUND CORROSION ON THE TAIL SKID HINGE FITTING RIGHT SIDE. REPLACED FITTING (P/N 65-25614-12) PER SRM 5 1-10-1 PG 4. 2 L 7 3 4F A3WE 1996041200732 19960412 00732 WP 1996 4 12 9608049751 1 19960404 A 5320 FITTING DOUG DC9 DC941 302207N WP FS 984 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 751NW 47115 DURING H-CHECK, FOUND CORROSION ON THE FS 984 FRAME FITTING AT THE RIGHT CUSP. REPLACED FITTING PER SRM 51-30-5 AND 51- 30-1. 2 L 7 2 4F A6WE 1996041200733 19960412 00733 WP 1996 4 12 9608059751 1 19960406 A 5320 FITTING DOUG DC9 DC941 302207N WP FS 1072 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 751NW 47115 DURING H-CHECK, FOUND CORROSION ON THE LONGERON 28L END FITTING AT FS 1072. REPLACED FITTING PER SRM 51-30-2 AND 51-30- 5. 2 L 7 2 4F A6WE 1996041200734 19960412 00734 WP 1996 4 12 9608069968 1 19960406 A 5320 FITTING DOUG DC9 DC931 3022065 WP FS 996 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9332 47264 DURING M-CHECK, FOUND CORROSION ON THE LONGERON 23L FITTING AT FS 996. REPLACED FITTING (P/N 3914654-1D). 2 L 7 2 4F A6WE 1996041200735 19960412 00735 WP 1996 4 12 9608079954 1 19960407 A 5320 FITTING DOUG DC9 DC931 3022065 WP RT MLG WW CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 921RW 47164 DURING H-CHECK, FOUND A CRACK AND CORROSION IN THE RIGHT MAIN LANDING GEAR WHEEL WELL KEEL, LONGERON 29R AFT END FITTING . REPLACED FITTING PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996041200736 19960412 00736 WP 1996 4 12 9608089609 1 19960410 A 5330 SKIN DOUG DC9 DC932 3022066 WP PAX DOOR CUTOUT CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 609NW 47234 DURING LINE CHECK, FOUND TWO CRACKS IN THE FUSELAGE SKIN AT THE MAIN CABIN DOOR CUTOUT UPPER AFT STOP FITTING. REPAIRED SKIN PER EA 96-104228. 2 L 7 2 4F A6WE 1996041200737 19960412 00737 WP 1996 4 12 9608099950 1 19960409 A 4900 38003621 APU DOUG DC9 DC932 3022066 WP WHEEL WELL MALFUNCTIONED A NWAA D RETURN TO BLOCK J O WARNING INDICATION OTHER TX TAXI/GRND HDL 1 GL 01 9346 54009 117 47376 BEFORE DEPARTURE, THE LEFT LAV FIRE DETECTOR WENT OFF, NO FIRE NOTED BUT FUMES WERE IN CABIN. AIRCRAFT RETURNED TO THE GATE. GROUND MAINTENANCE FOUND SOURCE OF FUMES CAME FROM THE APU. APU WAS PLACED ON MEL AND AIRCRAFT RETURNED TO SERVI CE. 2 L 7 2 4F A6WE 1996041200738 19960412 00738 NM 1996 4 12 9608102287 1 19960410 A 3350 LIGHT BOEING 727 727251 138408H NM AFT AIRSTAIR INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 287US 21375 DURING PREFLIGHT, FOUND AFT AIRSTAIR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERIES AND LAMPS, CHECKED OK. 2 L 7 3 4F A3WE 1996041200739 19960412 00739 NM 1996 4 12 9608112768 1 19960410 A 3350 BATTERIES BOEING 727 7272M7 138407S NM AFT AIRSTAIR DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 728RW 21741 DURING PREFLIGHT, FOUND AFT AIRSTAIR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERIES AND CHECKED OK. 2 L 7 3 4F A3WE 1996041200740 19960412 00740 NM 1996 4 12 9608122762 1 19960411 A 3350 POWER SUPPLY BOEING 727 7272M7 138407S NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 722RW 21201 DURING PREFLIGHT, FOUND AFT LEFT AND RIGHT EXTERIOR DOOR LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY PACK, CH ECKED OK. 2 L 7 3 4F A3WE 1996041200741 19960412 00741 NM 1996 4 12 9608136309 1 19960410 A 3350 POWER PACK FUSE BOEING 747 747451 1384940 NM CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 669US 24224 DURING LINE CHECK, TWO RIGHT AFT EXTERIOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED RESISTOR FUSE ON THE OVERWI NG EMERGENCY LIGHT POWER PACK, OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996041200742 19960412 00742 WP 1996 4 12 96FDEA00757 1 19960411 A 3234 SELECTOR DOUG DC10 DC1030F 3023504 WP LANDING GEAR MALFUNCTIONED A FDEA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 25 307FE 48291 LANDING GEAR WON'T COME DOWN, CYCLED GEAR AND STILL NO GEAR DOWN. USED ALTERNATE GEAR HANDLE AND GEAR CAME DOWN AND LOC KED. PRESS OK, QTY OK. REPLACED CENTER GEAR CONTROL VALVE AS PER MM 32-31-04. REPLACED L/GEAR SELECTOR VALVE AS PER M M 32-31-03. PERFORMED EXTENSION AND RETRACTION OF GEAR AS PER MM 32-30-00, CHECKS NORMAL. 2 L 7 3 4F RT A22WE 1996041200743 19960412 00743 WP 1996 4 12 96FDEA00758 1 19960410 A 2750 S4913802AS50408 CONTROL CABLE DOUG DC10 DC1010F 3022111 WP BS 1401 FRAYED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68055 47809 FLAP BODY CABLE FRAYED (NR 93C) IN LT WHEEL WELL, ABOVE FLAP MECHANICAL CONTROL VALVE AND .0625 FLAP CABLE (NR 93C) WITH 7 STRANDS HAS 6 BROKEN STRANDS, BS APPROX 1401. REPLACED WITH FABRICATED CABLE PER EA 8-2750-27938, INSTALLED AND RIGG ED CABLE PER MM 27-50-00 SNRM NR 7043. 2 L 7 3 4F A22WE 1996041200744 19960412 00744 NM 1996 4 12 96FDEA00759 1 19960411 A 5712 RIB BOEING 727 7272S2F 1384O81 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 217FE 22838 HFEC INSP EXHIBITS CRACKS EMANATING AT 12 AND 6 O'CLOCK FROM THE FWD MOST UPPER HOLE AT THE LT WING RIB CHORD BL 70.5 BS 760. REMOVED CRACK BY STOP DRILLING AND INSTALLED SMALL REPAIR AT STA 760 LBL 70.5 WL 209 TO 208 IAW FEDEX EA 7-5710-2 8232. 2 L 7 3 4F A3WE 1996041200745 19960412 00745 NM 1996 4 12 96UAL900248 1 19960410 A 3350 BATTERIES BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7255U 21402 LEFT WING EMERGENCY EXIT DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERIES AND CHECKS OKAY. 2 L 7 3 4F 4 F A3WE E2EA 1996041200746 19960412 00746 NM 1996 4 12 96UAL900249 1 19960410 A 2530 200212405 BUFFET MODULE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE AFT GALLEY INOPERATIVE A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 7276U 21423 ELECTRICAL ODOR THROUGHOUT AIRCRAFT. UPDATE AFT GALLEY BUFFET MODULE HAD AN ELECTRICAL FAULT. POWER REMOVED FROM MODUL E AND UNIT REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 1996041200747 19960412 00747 SO 1996 4 12 COMA9610124 1 19960405 A 5330 1202033049 SKIN EMB 120 EMB120RT SO AFT FUSELAGE DENTED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 162CA 120150 DURING ROUTINE MAINTENANCE, A LARGE DENT WAS FOUND ON THE FUSELAGE AFT RIGHT LOWER SKIN JUST FORWARD OF FRAME 45 BETWEEN STRINGERS 19R AND 20R. THE DAMGE WAS REPAIRED PER EMB120 SRM 53-00-01. 2 L 7 2 4T RT A31SO 1996041200748 19960412 00748 NE 1996 4 12 COMA9630098 2 19960408 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RIGHT FAILED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 140N 340A140 367197 RT ENGINE OIL CHIP DETECTOR WARNING CAME ON DURING TAXI. REPLACED THE RT ENGINE. 2 L 7 2 4T 4 T RT A52EU E8NE6 1996041200749 19960412 00749 EU 1996 4 12 COMA9630099 1 19960408 A 3246 5009237 INNER RACE LORAL 5010488 SAAB SF340 SF340A 7850100 EU MAIN WHEEL SPUN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 359CA 340A053 MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING VISUAL INSPECTION FOUND INNER RACE HAD SPUN INS IDE OF BUSHING. 2 L 7 2 4T RT A52EU 1996041200750 19960412 00750 EU 1996 4 12 COMA9630100 1 19960408 A 3246 5009237 BUSHING LORAL 5010488 SAAB SF340 SF340A 7850100 EU LT MLG WHEEL FAILED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 358CA JAN920177 340A047 MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING INSPECTION FOUND INNER RACE AND BUSHING HAD SPU N. 2 L 7 2 4T RT A52EU 1996041200751 19960412 00751 EU 1996 4 12 COMA9630101 1 19960410 A 3350 6104781 BATTERY SAAB SF340 SF340A 7850100 EU CABIN DISCHARGED A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 357CA 340A044 FORWARD SECTION CABIN EMERGENCY LIGHTS ARE INOP. REPLACED EMERGENCY LIGHTS BATTERY PACKS. 2 L 7 2 4T RT A52EU 1996041200752 19960412 00752 EA 1996 4 12 COMA9660063 1 19960409 A 2760 601R591473 SECU CNDAIR CL600 CL6002B19 EA SPOILERS MALFUNCTION A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 940CA 1171 7048 FLIGHT SPOILERS FAULT MESSAGE ON EICAS. REPLACED THE SPOILER ELECTRONIC CONTROL UNIT. 2 L 7 2 4F RT A21EA 1996041200753 19960412 00753 1996 4 12 MWEA96108 4 19960411 A 2565 13621225 EVAC SLIDE DOUG DC9 DC932 3022066 WP TAIL LOW PRESSURE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 DURING INSPECTION, FOUND TAIL SLIDE PRESSURE LOW AT 2,400 PSI. REPLACED TAIL SLIDE ASSY. 2 L 7 2 4F A6WE 1996041200754 19960412 00754 NM 1996 4 12 P5CA9600206 1 19960405 A 5320 SUPPORT BEAM BOEING 747 747122 1384872 NM PANEL 191M CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 FOUND FAIRING SUPPORT BEAM EXFOLIATED FWD END OF PANEL 191M. REMOVED DAMAGED AREA, FABRICATED REPAIR ANGLE AND INSTALLE D IAW SRM 51-40-03. 2 L 7 4 4F A20WE 1996041200755 19960412 00755 NM 1996 4 12 P5CA9600207 1 19960319 A 3350 SI356B37 LIGHT BOEING 747 747122 1384872 NM FLT COMPT INOPERATIVE A P5CA K NONE L NO TEST IN INSP/MAINT 1 WP 23 853FT 19753 FOUND FLIGHT COMPARTMENT EMERGENCY LIGHT INOP. REMOVED AND REPLACED SAME IAW MM 33-51-00. 2 L 7 4 4F A20WE 1996041200756 19960412 00756 NM 1996 4 12 SWAA960200 1 19960404 A 7830 315A1500535 TR SLEEVE BOEING 737 7373H4 1384600 NM NR 1 ENG CAME LOOSE A SWAA K NONE D INFLIGHT SEPARATION DE DESCENT 1 SW 07 323SW 23344 ON DESCENT AT 24,000 FL, NUMBER 1 ENGINE O/B THRUST REVERSER SLEEVE PARTIALLY SEPARATED FROM AIRCRAFT. AIRCRAFT MADE AN UNEVENTFUL LANDING AT AUS. REINSTALLED NEW SLEEVE PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996041200757 19960412 00757 NM 1996 4 12 SWAA960201 1 19960410 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 56SW 21721 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 7 FT AFT OF AFT CARGO DOOR. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996041200758 19960412 00758 NM 1996 4 12 SWAA960202 1 19960410 A 5512 SKIN BOEING 737 7373H4 1384600 NM RT HORZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 350SW 24409 DURING SCHEDULED BC3 CHECK, FOUND CRACK AT RT HORZ STAB AT RIB STA 120.3 AND 129.5 ON AFT SPAR ON RT LOWER IN SPAR. REP AIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996041200759 19960412 00759 NM 1996 4 12 SWAA960203 1 19960408 A 5414 PANEL BOEING 737 7373T5 NM RT PYLON CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 668SW 23060 DURING SCHEDULED C-CHECK, FOUND RT WING, AFT I/B PYLON PANEL CRACKED AT AFT BOTTOM PANEL(NR 5843R). REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996041200760 19960412 00760 NM 1996 4 12 SWAA960204 1 19960408 A 5312 BULKHEAD SKIN BOEING 737 7373T5 NM BS 1016 WRINKLED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 668SW 23060 DURING SCHEDULED C-CHECK, FOUND SKIN WRINKLED AT AFT PRESSURE BULKHEAD AT BS 1016, BETWEEN S9L TO S11L. REPAIRED PER BO EING SRM. 2 L 7 2 4F RT A16WE 1996041200761 19960412 00761 NM 1996 4 12 SWAA960205 1 19960408 A 5320 STRAP BOEING 737 7373Y0 1384671 NM BS 727D CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664WN 23495 DURING SCHEDULED 1/4 D-CHECK, FOUND FLOOR BEAM SUPPORT STRAP CORRODED AFT OF BS 727D, RBL 16. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996041200762 19960412 00762 NM 1996 4 12 SWAA960206 1 19960408 A 5330 SKIN BOEING 737 7373Y0 1384671 NM CARGO DR CUTOUT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664WN 23495 DURING SCHEDULED 1/4 D-CHECK, FOUND WEB AT LOWER AFT CORNER OF FWD CARGO DOOR CUTOUT DAMAGED. REPAIRED PER SWA RA 1-A53 -1285. 2 L 7 2 4F RT A16WE 1996041200763 19960412 00763 NM 1996 4 12 SWAA960207 1 19960408 A 5330 SKIN BOEING 737 7372H4 138448C NM AFT FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 DURING SCHEDULED TERMINAL CHECK, FOUND A 3 INCH CRACK, 41 INCHES FWD OF OUTFLOW VALVE AT RIGHT AFT FUSELAGE. REPAIRED P ER SWA RA 1-A53-1285. 2 L 7 2 4F A16WE 1996041200764 19960412 00764 NM 1996 4 12 SWAA960208 1 19960408 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 807 DAMAGE A SWAA K NONE C F.O.D. IN INSP/MAINT 1 SW 07 323SW 23344 BAGGAGE CART STRIKE TO LEFT SIDE FUSELAGE WHILE PARKED AT GATE, BETWEEN BS 807 AND 827, AT S24L. REPAIRED PER BOEING SR M. 2 L 7 2 4F RT A16WE 1996041200765 19960412 00765 NM 1996 4 12 SWAA960209 1 19960408 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 53SW 21534 DURING SCHEDULED C2 CHECK, FOUND LOWER FUSELAGE SKIN CRACKED 2 PLACES, FWD OF AIR CONDITIONING SERVICE PANEL, MEASURING .25 BY 1.5. REPAIRED BOTH PER BOEING SRM. 2 L 7 2 4F A16WE 1996041200766 19960412 00766 NM 1996 4 12 UPS96205907 1 19960305 A 5320 WEB BOEING 727 72725C 138400H NM BS 279 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED DOG HOUSE TUNNEL AREA RT SIDE APPROX STA 279, WALL OF NOSE W/W CUTOUT HAS 4 I NCH CRACK IN WEB. REMOVED DAMAGED SECTION PER SRM 51-40-2 AND FAB DOUBLER AND FILLER AND INSTALLLED PER SRM 51-40-2. 2 L 7 3 4F A3WE 1996041200767 19960412 00767 NM 1996 4 12 UPS96205908 1 19960316 A 5320 STIFFENER BOEING 727 72725C 138400H NM FS 351 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 351 STA 19L, FRAME TEE STIFFENER HAS HEAVY CORROSION. REMOVED AND FABRICA TED AND INSTALLED FRAME TEE STIFFENER AT FS 351, STR 19L PER SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996041200769 19960412 00769 NM 1996 4 12 UPS96205910 1 19960305 A 5311 FRAME BOEING 727 72725C 138400H NM BS 351 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 351 LT SIDE 2 INCHES AFT OF FWD AIR STAIR CUTOUT AT STR 18L, FRAME HAS LA RGE AREA OF CORROSION AND LARGE CRACK. REMOVED DAMAGED AREA PER SRM 51-40-2, FABRICATED PARTS AND INSTALLED PER SRM 51- 40-2. INSTALLED ATTACHING PARTS PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996041200770 19960412 00770 NM 1996 4 12 UPS96205911 1 19960305 A 5315 FLOOR BEAM BOEING 727 72725C 138400H NM FS 312 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 312, LBL 26 FLOOR BEAM UPPER FLANGE AFT BOTTOM SIDE FOUND TO BE OUT OF LIM ITS AFTER CORROSION REMOVAL. REPAIRED PER SRM 53-10-8, FIG 7. 2 L 7 3 4F A3WE 1996041200771 19960412 00771 NM 1996 4 12 UPS96205912 1 19960305 A 5755 FITTING BOEING 727 72725C 138400H NM NR 7 SPOILER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED NR 7 SPOILER I/B HINGE FITTING CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996041200772 19960412 00772 NM 1996 4 12 UPS96205913 1 19960316 A 5511 SPAR WEB BOEING 727 72725C 138400H NM FS 1342 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 1342 WL 260 VERT FIN SPAR WEB IS CRACKED. CUT OUT DAMAGED CENTER WEB, FAB RICATED REPLACEMENT SECTION AND REPAIRED PER SRM 55-30-6. 2 L 7 3 4F A3WE 1996041200773 19960412 00773 NM 1996 4 12 UPS96205914 1 19960325 A 5530 652566223 CHORD BOEING 727 72725C 138400H NM VERT FIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FIN STA 13.74 CHORD FOUND TO BE CRACKED. REMOVED, FABRICATED AND INSTALLED I AW SRM 51-30-2. 2 L 7 3 4F A3WE 1996041200774 19960412 00774 NM 1996 4 12 UPS96205915 1 19960325 A 5720 BOTTLE PIN BOEING 727 72727C 138400J NM LT WING SPAR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT WING FRONT SPAR WING BOTTLE PIN HAS CORROSION ON FLANGE. REMOVED BOTTLE P IN IAW MM 57-41-0. 2 L 7 3 4F A3WE 1996041200775 19960412 00775 NM 1996 4 12 UPS96205916 1 19960322 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1070 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 1070 STR 5R SHEAR TIE IS CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996041200776 19960412 00776 NM 1996 4 12 UPS96205917 1 19960322 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1070 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 1070 STR 6R SHEAR TIE IS CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996041200777 19960412 00777 NM 1996 4 12 UPS96205918 1 19960322 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1070 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 1070 STR 7R SHEAR TIE IS CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996041200778 19960412 00778 NM 1996 4 12 UPS96205919 1 19960322 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1070 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 1070 STR 8R SHEAR TIE IS CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996041200779 19960412 00779 NM 1996 4 12 UPS96205920 1 19960322 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1070 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 1070 STR 9R SHEAR TIE IS CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996041200780 19960412 00780 NM 1996 4 12 UPS96205921 1 19960322 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 970 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 970 STR 6R SHEAR TIE IS CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996041200781 19960412 00781 NM 1996 4 12 UPS96205922 1 19960322 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 990 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 990 STR 3R SHEAR TIE IS CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996041200782 19960412 00782 NM 1996 4 12 UPS96205923 1 19960322 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 970 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 970 STR 7L SHEAR TIE IS CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996041200783 19960412 00783 NM 1996 4 12 UPS96205924 1 19960322 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 970 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 970 STR 5L SHEAR TIE IS CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996041200784 19960412 00784 NM 1996 4 12 UPS96205925 1 19960322 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 970 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 970 STR 4R SHEAR TIE IS CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996041200785 19960412 00785 NM 1996 4 12 UPS96205926 1 19960322 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1050 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 1050 STR 8R SHEAR TIE IS CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996041200786 19960412 00786 NM 1996 4 12 UPS96205927 1 19960322 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1030 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 1030 STR 8R SHEAR TIE IS CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996041200787 19960412 00787 NM 1996 4 12 UPS96205928 1 19960322 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1030 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 1030 STR 7R SHEAR TIE IS CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996041200788 19960412 00788 NM 1996 4 12 UPS96205929 1 19960322 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1090 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 1090 STR 8R SHEAR TIE IS CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996041200789 19960412 00789 NM 1996 4 12 UPS96205930 1 19960322 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1030 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 1030 STR 8L SHEAR TIE IS CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996041200790 19960412 00790 NM 1996 4 12 UPS96205931 1 19960322 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1050 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 1050 STR 4R SHEAR TIE IS CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996041200791 19960412 00791 NM 1996 4 12 UPS96205932 1 19960322 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1050 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 1050 STR 6R SHEAR TIE IS CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996041200792 19960412 00792 NM 1996 4 12 UPS96205933 1 19960322 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1090 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 1090 STR 8L SHEAR TIE IS CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996041200793 19960412 00793 NM 1996 4 12 UPS96205934 1 19960322 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1070 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 1070 STR 4L SHEAR TIE IS CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996041200794 19960412 00794 NM 1996 4 12 UPS96205935 1 19960322 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1070 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 1070 STR 6L SHEAR TIE IS CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996041200795 19960412 00795 NM 1996 4 12 UPS96205936 1 19960322 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1050 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 1050 STR 7L SHEAR TIE IS CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996041200796 19960412 00796 NM 1996 4 12 UPS96205937 1 19960322 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1050 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 1050 STR 8L SHEAR TIE IS CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996041200797 19960412 00797 NM 1996 4 12 UPS96205938 1 19960322 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1070 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 1070 STR 7L SHEAR TIE IS CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996041200798 19960412 00798 NM 1996 4 12 UPS96205939 1 19960322 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1050 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 1050 STR 7R SHEAR TIE IS CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996041200799 19960412 00799 NM 1996 4 12 UPS96205940 1 19960322 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1010 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 1010 STR 7L SHEAR TIE IS CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996041200800 19960412 00800 NM 1996 4 12 UPS96205941 1 19960322 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 990 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 990 STR 4R SHEAR TIE IS CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996041200801 19960412 00801 NM 1996 4 12 UPS96205942 1 19960322 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1010 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 1010 STR 6L SHEAR TIE IS CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996041200802 19960412 00802 NM 1996 4 12 UPS96205943 1 19960322 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1010 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 1010 STR 5L SHEAR TIE IS CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996041200803 19960412 00803 NM 1996 4 12 UPS96205944 1 19960322 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1030 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 1030 STR 7L SHEAR TIE IS CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996041200804 19960412 00804 NM 1996 4 12 UPS96205945 1 19960322 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1030 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 1030 STR 9L SHEAR TIE IS CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996041200805 19960412 00805 NM 1996 4 12 UPS96205946 1 19960322 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1070 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 1070 STR 8L SHEAR TIE IS CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996041200806 19960412 00806 NM 1996 4 12 UPS96205947 1 19960322 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1090 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 1090 STR 1 SHEAR TIE IS CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996041200807 19960412 00807 NM 1996 4 12 UPS96205948 1 19960325 A 5720 BOTTLE PIN BOEING 727 72727C 138400J NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT FWD WING SPAR BOTTLE PIN IS CORRODED ON MATING FLANGE. REMOVED AND REPLAC ED RT FWD WING BOTTLE PIN PER MM 57-41-00. 2 L 7 3 4F A3WE 1996041200808 19960412 00808 NM 1996 4 12 UPS96205949 1 19960402 A 5350 ANGLE BOEING 727 72727C 138400J NM BS 560 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FAIRING SUPPORT ANGLE HAS CRACK AT GROUND. REMOVED FASTENER AND TERMINATED C RACK AT RIVET HOLE. INSTALLED DOUBLER PER SRM 53-50-1 AND 51-40-3. 2 L 7 3 4F A3WE 1996041200809 19960412 00809 NM 1996 4 12 UPS96205950 1 19960317 A 5320 FRAME TIE BOEING 727 72727C 138400J NM FS 344-360 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 344 TO 360 AT STR 21L, INTERCOSTAL FRAME TIE HAS HEAVY CORROSION. REMOVE D DEFECTIVE PARTS IAW 51-30-2, FABRICATED PARTS IAW SRM 53-10-2, INSTALLED PARTS IAW SRM 51-10-1 AND 53-30-2. 2 L 7 3 4F A3WE 1996041200810 19960412 00810 NM 1996 4 12 UPS96205951 1 19960403 A 5720 ANGLE BOEING 727 72727C 138400J NM RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT WING AT ACCESS PANEL JUST I/B OF NR 4 K-FLAP I/B END BULKHEAD ANGLE AT LOW ER END HAS NUMEROUS CRACKS AT FASTENERS. REMOVED CRACKED CHORD, FABRICATED CHORD PER SRM 57-20-2, ALODINED AND PRIMED P ER SRM 51-10-2 AND INSTALLED PART PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996041200811 19960412 00811 NM 1996 4 12 UPS96205954 1 19960410 A 3350 BATTERY BOEING 727 727247 138408F NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 209UP 21698 MAINTENANCE REPORTED, EMERGENCY EXIT LIGHT OVER FWD ENTRY DOOR DOES NOT ILLUMINATE. REPLACED BATTERY IN EMERGENCY LIGHT PANEL, OP CHECK GOOD. 2 L 7 3 4F A3WE 1996041200812 19960412 00812 NM 1996 4 12 UPS96505888 1 19960407 A 5311 FRAME BOEING 757 75724APF 1384969 NM BS 1320 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 445UP 27390 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED AFT CARGO BAY STA 1320 BETWEEN STR 25R AND 26R FRAME IS CRACKED. CUT OUT DAM AGE AND REPAIRED PER SRM 51-70-11. 2 L 7 2 4F RT A2NM 1996041200813 19960412 00813 NM 1996 4 12 UPS96505889 1 19960407 A 5753 BRACKET BOEING 757 75724APF 1384969 NM RT TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 445UP 27390 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RIGHT WING OUTBOARD FLAP OUTBOARD SKIN SUPPORT BRACKET IS CRACKED. REMOVED A ND REPLACED WITH FABRICATED BRACKET, INSTALLED PER SRM 51-30-01, 51-40-02, M/M 20-10-22. 2 L 7 2 4F RT A2NM 1996041200814 19960412 00814 NM 1996 4 12 UPS96505890 1 19960408 A 5753 SKIN BOEING 757 75724APF 1384969 NM LT TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 445UP 27390 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LEFT OUTBOARD FLAP, OUTBOARD LOWER AFT SKIN IS CRACKED. REMOVED AND REPLACE D CRACKED SKIN PANEL WITH FABRICATED PANEL, INSTALLED PER SRM 51-40-02, EO 757-57-0073. 2 L 7 2 4F RT A2NM 1996041200815 19960412 00815 WP 1996 4 12 UPS96805893 1 19960227 A 5711 SPAR DOUG DC8 DC871F 302199D WP WS 615-659 LT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED 6 CRACKS TOTALING 13 INCHES LONG AND HEAVY CORROSION AT LT WING REAR SPAR STA XRS615 TO STA XRS659. REPAIRED PER UPS EO DC8-57-0651. 2 L 7 4 4F RT 4A25 1996041200816 19960412 00816 WP 1996 4 12 UPS96805894 1 19960310 A 5320 FITTING DOUG DC8 DC871F 302199D WP FS 683 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON KEEL TEE FITTING FS 683 LONG 36. REPLACED PER UPS EO DC8- 53-1598. 2 L 7 4 4F RT 4A25 1996041200817 19960412 00817 WP 1996 4 12 UPS96805895 1 19960224 A 5330 SKIN DOUG DC8 DC871F 302199D WP FS 1612 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MODERATE CORROSION DAMAGE ON FUSELAGE SKIN AT THE CUTOUT FOR THE AFT ENTRY DO OR HOLD OPEN HOOK. REPAIRED PER UPS EO DC8-53-1608. 2 L 7 4 4F RT 4A25 1996041200818 19960412 00818 WP 1996 4 12 UPS96805896 1 19960301 A 5711 SPAR DOUG DC8 DC871F 302199D WP RT WING RT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT WING REAR SPAR AT WW IS CRACKED AT LOWER HORIZONTAL CAP RBL 30 FS 857. RE PAIRED PER UPS EO DC8-5710-8088A. 2 L 7 4 4F RT 4A25 1996041200819 19960412 00819 WP 1996 4 12 UPS96805897 1 19960318 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FS 683 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LONGERON 31R O/B SIDE HEAVY CORROSION AT FS 683. REPAIRED PER UPS EO DC8-53- 1602. 2 L 7 4 4F RT 4A25 1996041200820 19960412 00820 WP 1996 4 12 UPS96805898 1 19960305 A 5751 SKIN DOUG DC8 DC871F 302199D WP LT AILERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT O/B AILERON SKIN AND LOWER DOUBLER CRACKED AT THE I/B CLOSURE RIB. REPAIR ED PER UPS EO DC8-57-0652. 2 L 7 4 4F RT 4A25 1996041200821 19960412 00821 WP 1996 4 12 UPS96805900 1 19960223 A 5755 SKIN DOUG DC8 DC871F 302199D WP NR 1 SPOILER DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT WING NR 1 SPOILER DELAMINATION ON UPPER SURFACE. REPLACED SPOILER ASSY PE R MM 27-61-01. 2 L 7 4 4F RT 4A25 1996041200822 19960412 00822 WP 1996 4 12 UPS96805901 1 19960306 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FS 1260 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LONGERON 21L IS CRACKED FS 1260. REPAIRED LONGERON PER SRM 53-2-5. 2 L 7 4 4F RT 4A25 1996041200823 19960412 00823 WP 1996 4 12 UPS96805902 1 19960304 A 5320 FITTING DOUG DC8 DC871F 302199D WP FS 1290 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LONGERON 31L SPLICE FITTING CRACKS AT FS 1290. REPLACED FITTING PER SRM 51-1 -20D. 2 L 7 4 4F RT 4A25 1996041200824 19960412 00824 WP 1996 4 12 UPS96805903 1 19960226 A 5730 SKIN DOUG DC8 DC871F 302199D WP RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED 5 INCH LONG CRACK AT RT WING EXTERNAL LEADING EDGE ABOVE PYLON NR 4. REPAIRE D L/E SKIN PER SRM 57-2-1A. 2 L 7 4 4F RT 4A25 1996041200825 19960412 00825 WP 1996 4 12 UPS96805904 1 19960226 A 5711 SPAR DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CRACK IN TOP SIDE OF RT WING STA XRS 358 SPAR CAP. REPAIRED PER SRM 57-2-0 A ND UPS EO DC8-5720-487. 2 L 7 4 4F RT 4A25 1996041200826 19960412 00826 WP 1996 4 12 UPS96805905 1 19960304 A 5320 FITTING DOUG DC8 DC871F 302199D WP FS 1270 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LONGERON 34L SPLICE FITTING CRACKED AT FS 1270. REPLACED FITTING PER SRM 51- 1-20D. 2 L 7 4 4F RT 4A25 1996041200827 19960412 00827 WP 1996 4 12 UPS96805906 1 19960304 A 5320 FITTING DOUG DC8 DC871F 302199D WP FS 1270 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LONGERON 35L SPLICE FITTING CRACKED AT FS 1270. REPLACED FITTING PER SRM 51- 1-20D. 2 L 7 4 4F RT 4A25 1996041200828 19960412 00828 WP 1996 4 12 UPS96805952 1 19960409 A 8011 PLUG PACKING DOUG DC8 DC873F 302199F WP NR 2 ENG STARTER DETERIORATED A IPXA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 874UP 46074 CREW REPORTED, NR 2 ENGINE IN FLIGHT SHUTDOWN AND DECLARED EMERGENCY DUE TO LOSS OF OIL QUANTITY AND PRESSURE. REMOVED AND REPLACED STARTER SVC PLUG PACKING. 2 L 7 4 4F RT 4A25 1996041200829 19960412 00829 EU 1996 4 12 WWMA9600034 1 19960408 A 5280 7232110803 DOOR SAAB SF340 340B 7860101 EU LT MLG CRACKED A WWMA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 15 309AE 340B309 LEFT MAIN LANDING GEAR DOOR FOWARD INBOARD HINGE BROKE LOOSE RESULTING IN THE INBOARD GEAR DOOR CRACKING. AIRCRAFT RETU RNED TO FIELD WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR INBOARD GEAR DOOR. THE AIRCRAFT WAS FE RRIED TO ABI FOR GEAR SWINGS AND EXTENSION CHECKS. RETURNED TO SERVICE WITH NO FURTHER PROBLEMS. 2 L 7 2 4T RT A52EU 1996041200830 19960412 00830 EU 1996 4 12 WWMA9600035 1 19960409 A 3244 TIRES BAG JETSTM JETSTM3201 1500217 EU LT/RT MLG BLEW OUT A WWMA O OTHER O OTHER LD LANDING 1 WP 15 963AE 963 UPON LANDING BOTH LEFT AND RIGHT MAIN LANDING GEAR TIRES BLEW OUT. PILOT REPORTED LEAVING THE PARKING BRAKE OUT 1 INCH. MAINTENANCE REPLACED BOTH MAIN GEAR TIRES AND COMPLIED WITH A TIRE BURST INSPECTION. 2 L 7 2 4T RT A56EU 1996041800001 19960418 00001 NE 1996 4 18 9608146601 2 19960409 A 7532 BLEED CONTL VLV BOEING 747 747151 1384891 NM PWA JT9 JT9D7A 52054 NE NR 4 ENGINE MALFUNCTIONED A NWAA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 GL 01 601US 19778 62615 DURING APPROACH, THE NR 4 ENGINE STALLED. CREW SHUT DOWN THE ENGINE. WHEN ENGINE WAS RESTARTED, THE NR 4 EGT ROSE TO 7 60 DEGREES AND THE ENGINE WAS SHUT DOWN FOR THE REMAINDER OF THE FLIGHT. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. REP LACED THE PRESSURE RATIO BLEED CONTROL AND BLEED CONVERTER VALVE, BORESCOPED ENGINE, PERFORMED WINDMILL INSPECTION, AND TRIMMED THE ENGINE. OPERATIONAL CHECK GOOD. 2 L 7 4 4F 4 F A20WE E20EA 1996041800002 19960418 00002 NM 1996 4 18 9608155521 1 19960319 A 2410 IDG CONNECTOR BOEING 757 757251 1384970 NM RT ENGINE LOOSE A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 521US 23209 DURING APPLICATION OF TAKEOFF THRUST, THE RIGHT GENERATOR DRIVE EICAS MESSAGE ILLUMINATED. ABORTED TAKEOFF AT ZERO KNOT S. MAINTENANCE TIGHTENED THE ELECTRICAL CONNECTOR ON THE RIGHT IDG AND SERVICED OIL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 1996041800003 19960418 00003 WP 1996 4 18 9608161221 1 19960404 A 3350 BATTERY PACK DOUG DC10 DC1030 3023501 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 221NW 46579 DURING INSPECTION, FOUND THE CENTER ZONE EMERGENCY PROXIMITY FLOOR LIGHTS INOPERATIVE. REPAIRED EMERGENCY LIGHT AT SEAT 12AB AND REPLACED THE BATTERY PACK. 2 L 7 3 4F A22WE 1996041800004 19960418 00004 WP 1996 4 18 9608171152 1 19960322 A 3350 BATTERY PACK DOUG DC10 DC1040 3023508 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 152US 46761 DURING INSPECTION, FOUND THE EMERGENCY LIGHTS IN THE FORWARD CABIN FAILED THE SELF-TEST. REPLACED THE BATTERY PACK. 2 L 7 3 4F A22WE 1996041800005 19960418 00005 WP 1996 4 18 9608189913 1 19960409 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 963N 47415 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS AT ROWS 5 THROUGH 10 INOPERATIVE. REPLACED BATTERIE S. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996041800006 19960418 00006 WP 1996 4 18 9608199979 1 19960409 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9343 47439 DURING LINE MAINTENANCE INSPECTION, FOUND OVERWING EMERGENCY EXIT SIGN LIGHTS AT ROW 1 AND FLOOR PROXIMITY EMERGENCY LIG HTS AT ROWS 1 THROUGH 4 INOPERATIVE. REPAIRED WIRING AT SEATS 3C AND 3D. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996041800007 19960418 00007 WP 1996 4 18 9608209996 1 19960408 A 3350 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8932E 47141 DURING LINE MAINTENANCE INSPECTION, FOUND AFT OVERWING EMERGENCY EXIT SIGN LIGHTS INOPERATIVE. REPLACED BATTERY IN BATT ERY PACK. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996041800008 19960418 00008 WP 1996 4 18 9608219903 1 19960411 A 3260 DOOR SWITCH DOUG DC9 DC931 3022065 WP LT MLG MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 01 953N 47083 DURING CRUISE FLIGHT, LANDING GEAR DOOR OPEN LIGHT ILLUMINATED. LIGHT COULD NOT BE EXTINGUISHED USING COCKPIT OPERATING PROCEDURES. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT MAIN GEAR DOOR POSITION SW ITCH BAD. REPLACED SWITCH. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996041800009 19960418 00009 EU 1996 4 18 9608223245 1 19960410 A 3260 PROX SENSORS AIRBUS 320 A320211 3930320 EU LANDING GEAR DIRTY A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 345NW 399 DURING APPROACH AFTER LANDING GEAR EXTENSION, RECEIVED L/G GEAR NOT DOWNLOCKED MESSAGE. ALL THREE LANDING GEAR INDICATI ON TRIANGLES WERE ILLUMINATED RED. CYCLED LANDING GEAR HANDLE AND ALL INDICATIONS WERE NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED ALL DOWNLOCK PROXIMITY SENSORS. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996041800010 19960418 00010 NM 1996 4 18 96FDEA00760 1 19960404 A 5330 SKIN BOEING 727 72725 1384006 NM BS 870 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 CORROSION (C53-132-02(1)). ON UPPER FUEL CELL AT BS 870, WL 190, RBL 44, RUNNING ORDER CAP. REMOVED CORROSION ON UPPER FUEL CELL SKIN AT BS 870, WL 190, RBL 44, AND REPAIRED DAMAGED SKIN PER FEDEX EA 7-5710-28189. 2 L 7 3 4F A3WE 1996041800011 19960418 00011 NM 1996 4 18 96FDEA00762 1 19960412 A 5330 SKIN BOEING 727 72725 1384006 NM BS 330 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 EXTERIOR SKIN SURFACE IS BULGING AND HAS TWO SKIN PLUGS MISDRILLED AT BS 330 - 334 AT LOWER LT NOSE CHORD STR 27L. REMO VED SKIN IN AREA OF REPAIR PLUGGED HOLES AND FABRICATED REPAIR FILLER AND DOUBLER. INSTALLED REPAIR PARTS PER FEDEX EA 7-5330-28230. 2 L 7 3 4F A3WE 1996041800012 19960418 00012 WP 1996 4 18 ABXA9600449 1 19960409 A 5610 TRIM DOUG DC9 DC932 3022066 WP RT CV WINDOW LOOSE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 939AX 47201 FIRST OFFICER'S CLEARVIEW WINDOW WILL NOT OPEN. REGLUED INTERIOR TRIM IN PLACE. 2 L 7 2 4F A6WE 1996041800018 19960418 00018 NM 1996 4 18 MWEA960109 1 19960412 A 3350 5103 BATTERY DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 601ME 49762 EMERGENCY LIGHTING ON CABIN AISLE AT SEAT 27, 29, AND OVER AFT LEFT EMERGENCY EXIT INOPERATIVE. -- REPLACED BATTERY PA CK NICAD BATTERIES. 2 L 7 2 4F RT A6WE 1996041800019 19960418 00019 NM 1996 4 18 QXEA9600146 1 19960409 A 7712 311694201 TQ PROBE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE NR 2 ENGINE CORRODED A QXEA E A ENGINE SHUTDOWN UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 NM 09 339PH 2271 2271 3015 116030 NR 2 ENGINE TORQUE FLUX AT ROTATION, INCREASED DURING CLIMB AT 500 FT AGL THE ENGINE FEATHERED AND ALL OTHER INDICATIONS WERE NORMAL. AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT FURTHER PROBLEMS. NR 2 TORQUE PROBE PINS FOUND CORRODE D. PROBE REPLACED AND ENGINE INDICATIONS CHECKED GOOD ON GROUND RUN. 2 H 7 2 4T 4 T RT A45NM E20NE 1996041800020 19960418 00020 NM 1996 4 18 SCNA96041 1 19960409 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 282SC 22558 THE R-2 DOOR EMERGENCY EXIT LIGHTING WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AND POWER SUPPLY PE R MM 33-50-01. EMERGENCY LIGHTING OPS CHECKED GOOD. 2 L 7 3 4F A3WE 1996041800021 19960418 00021 NM 1996 4 18 UPS96405955 1 19960410 A 3350 900835 BATTERY PACK BOEING 747 747SR46 NM UPPER DECK DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 688UP 20784 WHILE ON GROUND AT NRT, MAINTENANCE REPORTED UPPER DECK EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED UPPER DEC K BATTERY PACK. OK FOR SERVICE. 2 L 7 4 4F A20WE 1996041800022 19960418 00022 NM 1996 4 18 UPS96405958 1 19960403 A 5313 STRINGER BOEING 747 747123 1384873 NM BS 2200-2220 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED AREA AFT OF BULK CARGO COMP. FOUND CORROSION ON STR FLANGE S-36 RT BETWEE N BS 2200-2220. REMOVED CORRODED SECTION OF STRINGER AND REPAIRED STRINGER IAW SRM 53-10-3. 2 L 7 4 4F A20WE 1996041800023 19960418 00023 NM 1996 4 18 UPS96405959 1 19960328 A 5312 BULKHEAD WEB BOEING 747 747123 1384873 NM BS 2160 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED BULK CARGO COMP. FOUND SEVERAL HOLE DAMAGES ON BULKHEAD WEB AT BS 2160, L T OF ACCESS DR. REMOVED DAMAGED SECTION OF BULKHEAD WEB AND REPAIRED WEB ACCORDING TO SRM 51-40-02. 2 L 7 4 4F A20WE 1996041800024 19960418 00024 WP 1996 4 18 UPS96805956 1 19960411 A 2910 000AE506D0301 BOGIE TRIM LINE DOUG DC8 DC871F 302199D WP LT MLG RUPTURED A IPXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SO 01 713UP 46014 AIR TURN BACK DUE TO LOSS OF HYD FLUID. FOUND BOGIE TRIM CYLINDER LINE RUPTURED, REPLACED LINE HYD SYS FILTERS, ALL BR AKES AND TIRES DUE TO HIGH ENERGY STOP AND SUBSEQUENT SOAKING WITH WATER BY C.F.R. DUE TO HEAVY SMOKE FROM LT GEAR. 2 L 7 4 4F RT 4A25 1996041800025 19960418 00025 WP 1996 4 18 UPS96805957 1 19960411 A 3250 CONTROL VALVE DOUG DC8 DC871F 302199D WP NLG STEERING OUT OF ADJUST A IPXA O OTHER O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED BLOCK TURN BACK RUDDER PEDAL STEERING STIFF TO THE RIGHT. ADJUSTED NOSE WHE EL STEERING CNTRL VALVE. OPS CHECKED GOOD PER MM 32-51-01. 2 L 7 4 4F RT 4A25 1996041800026 19960418 00026 1996 4 18 UPS96805960 4 19960411 A 2565 515610040GACR ESCAPE SLIDE DOUG DC8 DC871F 302199D WP CREW ENTRY FAILED TO DEPLOY A IPXA K NONE O OTHER UK UNKNOWN 1 SO 01 713UP 46014 CREW REPORTED ESCAPE SLIDE FAILED TO DEPLOY. REPLACED SLIDE ASSY, DAMAGED LANYARD. 2 L 7 4 4F RT 4A25 1996041800027 19960418 00027 NM 1996 4 18 VNAA9600013 1 19960406 A 3241 AE20768 CONTROL UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ANTI SKID MALFUNCTIONED A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 07 441JS 65611 3059 PIT - FLT 4169 - DURING TAKEOFF ROLL, THE CREW WAS ALERTED BY A C.A.S. MESSAGE THAT BRAKES WERE HOT. CREW ABORTED TAKE OFF AND RETURNED TO THE GATE. PIT MX RE-RACKED THE ANTI-SKID CONTROL UNIT IAW MM 32-43-10. ALSO, ALLOWED SEVERAL MINUT ES FOR THE BRAKES TO COOL. AIRCRAFT RETURNED TO SERVICE. AIRCRAFT TOTAL CYCLES, 649. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996041800028 19960418 00028 NM 1996 4 18 AALA960377 1 19960308 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 420-467 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1757A 48505 TUL - FLANGE ON NR 8 SEAT TRACK CORRODED IN R-1 DOORWAY. REPAIRED SEAT TRACK PER SRM 53-70-00 BY INSTALLING STRAP AND F ILLER. TREATED, SEALED, AND PRIMED PER SRM 51-21-01, VOL 2. TST: 16,835. CYCLES: 2,678. (X) 2 L 7 3 4F RT A22WE 1996041800029 19960418 00029 NM 1996 4 18 AALA960378 1 19960308 A 5320 MOUNT DOUG MD11 MD11 3023602 NM GALLEY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1757A 48505 TUL - NR 3 GALLEY RT FWD MOUNT HAS CORROSION. REMOVED GALLEY TIE-DOWN AND INSTALLED NEW ONE PER SRM 53-00-01. TST: 16 ,835. CYCLES, 2,678. (X) 2 L 7 3 4F RT A22WE 1996041800030 19960418 00030 NM 1996 4 18 AALA960379 1 19960308 A 5320 MOUNT DOUG MD11 MD11 3023602 NM GALLEY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1757A 48505 TUL - INBOARD GALLEY TIE-DOWN POINTS FOR LT FWD GALLEY ARE CORRODED. REMOVED GALLEY TIE-DOWN AND INSTALLED NEW ONE PER SRM 53-00-01. TST: 16,835. CYCLES: 2,678. (X) 2 L 7 3 4F RT A22WE 1996041800031 19960418 00031 NM 1996 4 18 AALA960380 1 19960308 A 5320 SUPPORT DOUG MD11 MD11 3023602 NM BS 395-467 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1757A 48505 TUL - DIAGONAL FLOOR SUPPORT FOR RT FWD GALLEY HAS HEAVY CORROSION. REMOVED OLD GALLEY FLOOR SUPPORT AND INSTALLED NEW PART PER SRM 53-00-01. TST: 16,835. CYCLES: 2,678. (X) 2 L 7 3 4F RT A22WE 1996041800032 19960418 00032 NM 1996 4 18 AALA960381 1 19960308 A 5347 TIE DOWN TRACK DOUG MD11 MD11 3023602 NM FWD GALLEY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1757A 48505 TUL - RT FWD GALLEY INBOARD SUPPORT RACK HAS CORROSION AT TIE-DOWN POINTS. REMOVED OLD TIE-DOWN SUPPORT TRACK AND INSTA LLED A NEW PART PER SRM 53-00-01. TST: 16,835. CYCLES: 2,678. (X) 2 L 7 3 4F RT A22WE 1996041800033 19960418 00033 NM 1996 4 18 AALA960382 1 19960311 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 467-515 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1757A 48505 TUL - NR 2 SEAT TRACK CORRODED AT TIE-DOWN POINTS FOR LT FWD LAVATORY - BEYOND ALLOWABLE LIMITS. REMOVED AND REPLACED T RACK SECTION PER SRM 53-70-00 AND ESO 41,000, DATED 3-8-96. (X) 2 L 7 3 4F RT A22WE 1996041800034 19960418 00034 WP 1996 4 18 AALA960393 1 19960313 A 5320 CUSP DOUG DC9 DC982 3022082 WP BS 1136-1155 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 218AA 49168 TUL - CUSP CORRODED LT SIDE, STA 1136 TO STA 1155. INSTALLED DOUBLER REPAIR PER CHAPTER 53 AND ESO 80559. TST: 39,429 .01. CYCLES: 22,544. (X) 2 L 7 2 4F A6WE 1996041800035 19960418 00035 WP 1996 4 18 AALA960394 1 19960312 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 1155 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 218AA 49168 TUL - FORWARD LOWER CORNER DOOR CUT-OUT, LOWER ANGLE FITTING CORRODED. REMOVED DAMAGED ANGLE FITTING. REPLACED WITH NE W ANGLE FITTING. TST: 39,421. CYCLES: 22,544. (X) 2 L 7 2 4F A6WE 1996041800036 19960418 00036 WP 1996 4 18 AALA960397 1 19960313 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 1322 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 218AA 49168 TUL - LOWER J-ANGLE CORRODED. REMOVED AFFECTED AREA OF J-ANGLE. INSTALLED NEW SECTION OF FRAME AND DOUBLERS PER SRM 53 -03, FIGURE 2A, SHEET 1, PAGE 4A AND ESO 80559, DATED 3-13-96. TST: 39,427. CYCLES: 22,544. (X) 2 L 7 2 4F A6WE 1996041800037 19960418 00037 NM 1996 4 18 AALA960398 1 19960314 A 5330 SKIN BOEING 727 727227 1384078 NM BS 483 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 719AA 20612 TUL - CORROSION OUT OF LIMITS ON FUSELAGE SKIN. REPLACED PER SRM 53-30-3, FIGURE 3A (SHEET 3). TST: 64,356. CYCLES: 46,864. (X) 2 L 7 3 4F A3WE 1996041800038 19960418 00038 NM 1996 4 18 AALA960399 1 19960314 A 5312 BLKHD SKIN BOEING 727 727227 1384078 NM BS 1183 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 719AA 20612 TUL - CRACK IN FORWARD SKIN OF TAIL SKID, LT SIDE, AT ANGLE BRACKET, STA 1183. INSTALLED DOUBLER PER SRM 53-10-2, PAGE 28. TST: 64,360. CYCLES: 46,865. (X) 2 L 7 3 4F A3WE 1996041800039 19960418 00039 WP 1996 4 18 AALA960413 1 19960318 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1183-1309 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 262AA 49290 TUL - CORROSION ON NR 3 SEAT TRACK, STA 1183, 1271, AND 1309. REMOVED AND REPLACED SEAT TRACK SECTION FROM STA 1145 TO STA 1309. TST: 33,315.25. CYCLES: 19,198. (X) 2 L 7 2 4F A6WE 1996041800040 19960418 00040 NM 1996 4 18 AALA960444 1 19960322 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1351 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1768D 48436 TUL - SEAT TRACK NR 2 HAS AREA OF CORROSION IN CHANNEL. INSTALLED REPAIR PER SRM 53-70-00. TST: 15,125.39. CYCLES: 2 ,471. (X) 2 L 7 3 4F RT A22WE 1996041800041 19960418 00041 NM 1996 4 18 AALA960445 1 19960322 A 5320 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1351 CORRODED A A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1768D 48436 TUL - SEAT TRACK NR 7 HAS CORROSION IN CHANNEL. INSTALLED REPAIR PER SRM 53-70-00. TST: 15,125.39 HRS. CYCLES: 2,47 1. (X) 2 L 7 3 4F RT A22WE 1996041800042 19960418 00042 WP 1996 4 18 AALA960456 1 19960324 A 5347 TIE DOWN TRACK DOUG DC9 DC982 3022082 WP BS 1212-1290 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 407AA 49318 TUL - RT AFT CARGO TIE-DOWN TRACK CORRODED FROM AFT END OF DOOR TO STA 1290. REMOVED AND REPLACED TIE-DOWN TRACK FROM S TA 1212, TO STA 1320. TST: 30,420.55 HRS. CYCLES: 17,612. (X) 2 L 7 2 4F A6WE 1996041800043 19960418 00043 WP 1996 4 18 AALA960457 1 19960322 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 160-200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 262AA 49290 TUL - CORROSION ON FLOORBOARD SUPPORT ANGLE AT FASTENER HOLES. REPLACED SUPPORT ANGLE WITH NEW SECTION. TST: 33,315 H RS. CYCLES: 19,198. (X) 2 L 7 2 4F A6WE 1996041800044 19960418 00044 NM 1996 4 18 AALA960486 1 19960326 A 5330 SKIN DOUG MD11 MD11 3023602 NM BS 1815 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1768D 48436 TUL - DENT IN FUSELAGE SKIN 34 INCHES AFT OF CENTER CARGO DOOR THAT CRACKED INTERNAL FINGER DOUBLER ABOVE LONGERON 40R. TRIMMED OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLERS PER MD-11 SRM 53-50-00, VOL 1, FIGURE 6, AND ENG. ESO 41000, DAT ED 3-21-96. TST: 15,125.39 HRS. CYCLES: 2,471. (X) 2 L 7 3 4F RT A22WE 1996041800045 19960418 00045 NM 1996 4 18 AWXA960106 1 19960225 A 3350 276005 FUSE BOEING 737 73733A 1384673 NM CABIN FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 167AW 23628 PHX - FLT 0029 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE ON SEATS IN THE FORWARD MID-S ECTION. FOUND WIRE TOUCHING GROUND AT ROW 5 SEAT TRACK, REPAIRED, INSTALLED NEW FUSE. OPS GOOD. (X) 2 L 7 2 4F RT A16WE 1996041800046 19960418 00046 NM 1996 4 18 CAL960327 1 19960317 A 3260 UPLOCK SENSOR BOEING 737 7373T0 1384582 NM LT MLG OUT OF ADJUST A CALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 14346 23584 IAH - FLT 8954 - THE LT MLG RED LIGHT CAME BACK ON AFTER GEAR RETRACTION. CYCLING THE GEAR WAS NO HELP. THE AIRCRAFT W AS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT MLG UPLOCK SENSOR TARGET OUT OF RIG. THE SENSOR/TARGET WAS SHIMMED IAW MM 32-61-21. THE GEAR WAS SWUNG AND ALL INDICATIONS CHECKED GOOD. (X) 2 L 7 2 4F RT A16WE 1996041800047 19960418 00047 NM 1996 4 18 CAL960334 1 19960318 A 3230 65448105 UPLOCK ACT BOEING 737 7373T0 1384582 NM RT MLG INOPERATIVE A CALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SW 09 71314 33494 23365 IAH - FLT 1703 - THE RT MLG GREEN LIGHT WOULD NOT ILLUMINATE WHEN GEAR WAS EXTENDED ON APPROACH TO IAH. A TOWER FLYBY V ERIFIED THE RT GEAR WAS NOT EXTENDED. A MANUAL GEAR EXTENSION WAS PERFORMED WITH 3 GREEN LIGHTS INDICATED AND A SECOND TOWER FLYBY CONFIRMED GEAR WAS DOWN AND LOCKED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT MLG UPL OCK ACTUATOR AT FAULT. THE ACTUATOR WAS REMOVED AND REPLACED IAW MM 32-32-41. THE GEAR WAS SWUNG WITH OPERATION AND IN DICATIONS CHECKING GOOD. (X) 2 L 7 2 4F RT A16WE 1996041800048 19960418 00048 WP 1996 4 18 CAL960376 1 19960213 A 5720 SUPPORT BRACKETS DOUG DC9 DC982 3022082 WP RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14890 38914 49114 MIA - INSPECTION FOUND 3 SUPPORT BRACKETS CRACKED AT RT WING FIXED LEADING EDGE INNER RIB. TWENTY INCHES OUTBOARD OF SL AT TRACK NR 2. THE CRACKS WERE 2 INCHES, .50 INCH, AND .50 INCH LONG. THE BRACKETS WERE REMOVED. NEW BRACKETS WERE FA BRICATED AND INSTALLED IAW SRM 51-10-2, AND SRM 57-02, FIGURE 6. (X) 2 L 7 2 4F A6WE 1996041800049 19960418 00049 NM 1996 4 18 CAL960384 1 19960322 A 3233 65446104 ACTUATOR BOEING 737 7373T0 1384582 NM NLG INOPERATIVE A CALA O OTHER P NO WARNING INDICATION AP APPROACH 1 SW 09 12322 21698 23373 EWR - FLT 0744 - THE LANDING GEAR WOULD NOT EXTEND INITIALLY ON APPROACH TO EWR. THE GEAR DID NOT MOVE AND THERE WERE N O WARNING LIGHTS. THE GEAR HANDLE WAS CYCLED, AND THE GEAR EXTENDED WITH A LOUD BANG AFTER FIVE SECONDS. MAINTENANCE F OUND THE NLG RETRACT ACTUATOR AT FAULT. THE NLG RETRACT ACTUATOR WAS REMOVED AND REPLACED. THE NOSE GEAR HYDRAULIC MOD ULE, NLG HYDRAULIC TRANSFER CYLINDER, AND NLG LOCK ACTUATOR WERE REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. LEAK AND OPERATIONAL CHECKS WERE GOOD. (X) 2 L 7 2 4F RT A16WE 1996041800050 19960418 00050 NM 1996 4 18 CAL960385 1 19960323 A 2780 NOSE LINK BOEING 737 7373T0 1384582 NM NR 2 LE FLAP BROKEN A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 12349 23587 EWR - FLT 0725 - THE NR 2 LEADING EDGE FLAP TRANSIT LIGHT ON OVERHEAD PANEL AND FORWARD PANEL LEADING EDGE FLAP TRANSIT LIGHT ILLUMINATED WITH THE FLAPS RETRACTED WHILE IN CLIMB. THE AIRCRAFT WAS RETURNED TO EWR. MAINTENANCE FOUND THE NR 2 KRUGER FLAP NOSE LINK AT INBOARD END BROKEN. THE NOSE LINK WAS REPLACED. THE FLAP WAS RIGGED IAW MM 27-81-11. (X) 2 L 7 2 4F RT A16WE 1996041800051 19960418 00051 NM 1996 4 18 CAL960386 1 19960324 A 5210 65445101472 HYD LINE BOEING 737 737130 1384435 NM A-HYD SYSTEM LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 44214 19031 BUF - FLT 1420 - AIRCRAFT LOST A-SYSTEM HYDRAULIC QUANTITY WHILE EN ROUTE FROM EWR TO BUF. THE AIRCRAFT LANDED IN BUF W ITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC PRESSURE LINE AT SYSTEM 'A' MODULAR UNIT LEAKING. THE PRESSURE LINE W AS REMOVED AND REPLACED. IN ADDITION, BOTH ENGINE DRIVE HYDRAULIC PUMPS WERE REMOVED AND REPLACED AS A PRECAUTIONARY ME ASURE. AN ENGINE RUN WAS PERFORMED WITH ALL FLIGHT CONTROLS OPERATED AND THE GEAR HANDLE CYCLED. LEAK AND OPERATIONAL CHECKS WERE GOOD. (X) 2 L 7 2 4F A16WE 1996041800052 19960418 00052 WP 1996 4 18 CAL960387 1 19960324 A 3397 WIRE DOUG DC9 DC981 3022081 WP CABIN SHORTED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16883 48073 EWR - FLT 0621 - INSPECTION FOUND THE EMERGENCY AISLE PATH LIGHTING BEYOND ROW 25, INOPERATIVE. MAINTENANCE FOUND A SHO RT IN WIRING AND A BLOWN FUSE AT ROW 30 DEF. THE FUSE WAS REPLACED AND THE SECTION AT ROW 30 DEF WAS REWIRED. (X) 2 L 7 2 4F A6WE 1996041800053 19960418 00053 WP 1996 4 18 CAL960388 1 19960209 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP FS 807 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14890 38914 49114 MIA - INSPECTION FOUND A .6250 INCH CRACK IN FUSELAGE FAIRING SUPPORT ANGLE AT FS 807 BETWEEN LONGERON 25L AND LONGERON 26L. (X) 2 L 7 2 4F A6WE 1996041800054 19960418 00054 WP 1996 4 18 CAL960389 1 19960211 A 5720 5936838503 SUPPORT DOUG DC9 DC982 3022082 WP LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14890 38914 49114 MIA - INSPECTION FOUND A 1 INCH CRACK IN LT WING TRAILING EDGE X-SUPPORT MEMBER AT UPPER AFT LEG FORWARD OF ATTACH POINT , JUST OUTBOARD OF NR 1 SPOILER ACTUATOR. THE SUPPORT MEMBER WAS REMOVED AND REPLACED IAW SRM 51-30-2. (X) 2 L 7 2 4F A6WE 1996041800055 19960418 00055 WP 1996 4 18 CAL960390 1 19960211 A 5720 5936838505 SUPPORT DOUG DC9 DC982 3022082 WP LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14890 38914 49114 MIA - INSPECTION FOUND A .75 INCH CRACK IN LT WING TRAILING EDGE X-SUPPORT MEMBER AT UPPER AFT LEG FORWARD OF ATTACH POI NT, JUST INBOARD OF NR 1 SPOILER ACTUATOR. THE SUPPORT MEMBER WAS REMOVED AND REPLACED IAW SRM 51-30-2. (X) 2 L 7 2 4F A6WE 1996041800056 19960418 00056 WP 1996 4 18 CAL960391 1 19960226 A 5330 SKIN DOUG DC9 DC983 3022083 WP BS 120 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 938MC 27165 49525 MIA - INSPECTION FOUND 2 DENTS IN EXTERNAL LT FUSELAGE SKIN AT STA 120. THE DENTED AREA WAS REMOVED. REPAIR DOUBLERS W ERE FABRICATED AND INSTALLED IAW ECRA 5330-02363. (X) 2 L 7 2 4F RT A6WE 1996041800057 19960418 00057 WP 1996 4 18 CAL960392 1 19960210 A 5330 SKIN DOUG DC9 DC983 3022083 WP BS 237 NICKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 938MC 27165 49525 MIA - INSPECTION FOUND A .50 INCH LONG NICK IN RT FUSELAGE SKIN AT STA 237. THE AREA WAS REPAIRED IAW SRM 53-04, FIGURE 38, SHEET 21. (X) 2 L 7 2 4F RT A6WE 1996041800058 19960418 00058 WP 1996 4 18 CAL960393 1 19960202 A 5210 SKIN DOUG DC9 DC983 3022083 WP PASSENGER DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 938MC 27165 49525 MIA - INSPECTION FOUND A 1 INCH CRACK IN OUTER SKIN AT LOWER AFT CORNER OF LT FORWARD ENTRY DOOR. A REPAIR WAS FABRICAT ED AND INSTALLED IAW SRM 52-05 AND SRM 51-30-2. (X) 2 L 7 2 4F RT A6WE 1996041800059 19960418 00059 WP 1996 4 18 CAL960394 1 19960206 A 5320 WEB DOUG DC9 DC983 3022083 WP FS 256 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 938MC 27165 49525 MIA - INSPECTION FOUND CORROSION ON CABIN FLOOR HORIZONTAL WEB OUTBOARD OF RT OUBOARD FLOOR TRACK, FS 256. A DOUBLER AN D FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-08-00, PAGE 8. (X) 2 L 7 2 4F RT A6WE 1996041800060 19960418 00060 WP 1996 4 18 CAL960395 1 19960206 A 5320 ANGLE DOUG DC9 DC983 3022083 WP FS 200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 938MC 27165 49525 MIA - INSPECTION FOUND CORROSION IN FLOOR ATTACH ANGLE FROM RT INBOARD FLOOR TRACK TO RT CABIN SIDEWALL AT FS 200. A NE W FLOOR SUPPORT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-00. (X) 2 L 7 2 4F RT A6WE 1996041800061 19960418 00061 WP 1996 4 18 CAL960396 1 19960206 A 5320 GUSSET DOUG DC9 DC983 3022083 WP BS 946 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 938MC 27165 49525 MIA - INSPECTION FOUND 1.5 INCH CRACKS IN GUSSET PLATES AT LEFT AND RIGHT SIDES OF KEEL BEAM RIB AT STA 946. THE GUSSET PLATES WERE REMOVED. NEW GUSSET PLATES WERE FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2, 51-10-4B, AND 51-30-5. (X) 2 L 7 2 4F RT A6WE 1996041800062 19960418 00062 WP 1996 4 18 CAL960397 1 19960207 A 5320 FLOOR WEB DOUG DC9 DC983 3022083 WP BS 550-560 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 938MC 27165 49525 MIA - INSPECTION FOUND CABIN FLOOR WEB CORRODED AT CUSP LINE BETWEEN STA 550 TO STA 560 RIGHT. A FILLER AND DOUBLER REP AIR WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 4. (X) 2 L 7 2 4F RT A6WE 1996041800063 19960418 00063 WP 1996 4 18 CAL960398 1 19960325 A 2910 HYD LINE DOUG DC9 DC982 3022082 WP LT TR CONTL VLV LOOSE A CALA O OTHER B K SMOKE/FUMES/ODORS/SPARKS FLUID LOSS AP APPROACH 1 SW 09 92874 49122 EWR - FLT 0362 - THE LT HYDRAULIC QUANTITY DROPPED TO 3 QUARTS ON APPROACH TO EWR. THE CABIN BEGAN TO FILL WITH SMOKE W HILE TAXIING IN AFTER LANDING. THE COCKPIT WINDOWS WERE OPENED AND CABIN WAS PRESSURIZED TO CLEAR THE AIR. MAINTENANCE FOUND THE LT THRUST REVERSER CONTROL VALVE SYSTEM PRESSURE SUPPLY LINE LEAKING AT B-NUT WHICH HAD BACKED OFF. THE B-NU T WAS RESECURED. THE HYDRAULIC SYSTEM WAS SERVICED TO FULL. LEAK AND OPERATIONAL CHECKS WERE GOOD. THE CABIN SMOKE WA S A RESULT OF THE LEAKING HYDRAULIC LINE. BOTH PACK WATER SEPARATOR BAGS WERE REMOVED AND REPLACED. THE SYSTEM WAS BUR NED OUT AND NO SMOKE OR SMELL WAS REMAINING. (X) 2 L 7 2 4F A6WE 1996041800064 19960418 00064 NM 1996 4 18 CAL960399 1 19960312 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM BS 380-400 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16339 29593 23577 HOU - INSPECTION FOUND TWO 1 INCH CRACKS IN FLOOR SUPPORT AT STA 380 - STA 400. A NEW FLOOR SUPPORT WAS INSTALLED IAW S RM 53-30-51. (X) 2 L 7 2 4F RT A16WE 1996041800065 19960418 00065 NM 1996 4 18 CAL960400 1 19960312 A 5280 GEAR DOOR BOEING 737 7373T0 1384582 NM LT MLG CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16339 29593 23577 HOU - INSPECTION FOUND A CRACK IN RADIUS TOP/AFT END FLANGE OF LT MLG CENTER DOOR. THE CRACK LENGTH WAS NOT IDENTIFIED. THE DOOR WAS REPAIRED IAW ECRA 5280-01076. THE DOOR WAS INSTALLED AND RIGGED PER MM 32-13-11. (X) 2 L 7 2 4F RT A16WE 1996041800066 19960418 00066 NM 1996 4 18 CAL960401 1 19960312 A 5280 GEAR DOOR BOEING 737 7373T0 1384582 NM LT MLG CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16339 29593 23577 HOU - INSPECTION FOUND A CRACK IN RADIUS INBOARD/AFT FLANGE OF LT MLG INNER DOOR. THE CRACK LENGTH WAS NOT IDENTIFIED. THE DOOR WAS REPAIRED IAW ECRA 5280-01076. THE DOOR WAS INSTALLED AND RIGGED PER MM 32-13-11. (X) 2 L 7 2 4F RT A16WE 1996041800067 19960418 00067 WP 1996 4 18 CAL960404 1 19960304 A 5512 SKIN DOUG DC10 DC1030 3023501 WP LT HORIZ STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14062 86736 47863 KUL - INSPECTION FOUND A DENT AND 1.25 INCH CRACK IN THE TOP SKIN OF THE LT HORIZONTAL STABILIZER INBOARD PANEL. A FILL ER AND DOUBLER REPAIR WAS INSTALLED IAW SRM 51-71-00 AND A FIBERGLASS REPAIR WAS INSTALLED IAW SRM 57-71-00, PAGE 65. ( X) 2 L 7 3 4F A22WE 1996041800068 19960418 00068 WP 1996 4 18 CAL960405 1 19960304 A 5320 ANGLE DOUG DC10 DC1030 3023501 WP BS 2123 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14062 86736 47863 KUL - INSPECTION FOUND TWO 1 INCH CRACKS IN ANGLE AT STA XCW 14 LT AND XCW 14 RT, BS 2123. A REPAIR WAS CARRIED OUT PER SRM 53-00-01, PAGE 7. (X) 2 L 7 3 4F A22WE 1996041800069 19960418 00069 WP 1996 4 18 CAL960406 1 19960229 A 5311 FRAME DOUG DC10 DC1030 3023501 WP BS 1841 DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14062 86736 47863 KUL - INSPECTION FOUND A .50 INCH DIAMETER HOLE IN FRAME, STA 1841, ABOVE CENTER CARGO FLOOR AREA ON LT SIDE. THE FRAME WAS REPAIRED IAW ECRA 5310-03243. (X) 2 L 7 3 4F A22WE 1996041800070 19960418 00070 WP 1996 4 18 CAL960407 1 19960308 A 5330 SKIN DOUG DC10 DC1030 3023501 WP CARGO DR CUTOUT DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14062 86736 47863 KUL - INSPECTION FOUND IMPACT DAMAGE AT LOWER AFT SECTION OF FORWARD CARGO DOOR CUT-OUT. THE AREA WAS REPAIRED IAW ECRA 5330-02370. (X) 2 L 7 3 4F A22WE 1996041800071 19960418 00071 WP 1996 4 18 CAL960408 1 19960225 A 5711 SPAR CAP DOUG DC10 DC1030 3023501 WP WS 1043 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14062 86736 47863 KUL - INSPECTION FOUND A 6 INCH CRACK JUST ABOVE RADIUS ON FORWARD SIDE OF RT WING AFT LOWER SPAR CAP AT STA 1043. THE SPAR CAP WAS REPAIRED IAW ECRA 5710-01720. (X) 2 L 7 3 4F A22WE 1996041800072 19960418 00072 WP 1996 4 18 CAL960409 1 19960321 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 229-303 PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 477AC 41441 48062 LGA - FLT 1807 - TUG PUNCTURED LT SIDE OF FUSELAGE DURING PUSHBACK AT LGA WITH RESULTANT DAMAGE TO LONGERONS 23L TO 26L, FRAME, AND SKIN AT STA 229 TO STA 303. THE LT FLYING GEAR DOOR WAS ALSO DAMAGED AT LOWER TRAILING EDGE. THE LONGERONS AND SKIN WERE REPAIRED IAW ECRA 5330-02377. THE FRAME WAS REPAIRED IAW SRM 53-03, FIGURE 2A. THE FLYING GEAR DOOR WAS REPAIRED BY INSTALLING A SKIN AND DOUBLER REPAIR IAW SRM 51-30-0 AND ECRA 520C01082. (X) 2 L 7 2 4F A6WE 1996041800073 19960418 00073 WP 1996 4 18 CAL960411 1 19960313 A 5350 CABLES DOUG DC9 DC932 3022066 WP TAILCONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69523 47520 HOU - THE PULL FROM BOTH THE INTERIOR AND EXTERIOR EMERGENCY TAILCONE RELEASE HANDLES WAS LOW. THE TAILCONE CABLE SYSTE M WAS ADJUSTED IAW MM 53-50-3. (X) 2 L 7 2 4F A6WE 1996041800074 19960418 00074 WP 1996 4 18 CAL960412 1 19960313 A 5512 SKIN DOUG DC9 DC932 3022066 WP RUDDER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69523 64836 47520 HOU - INSPECTION FOUND TWO 1.25 INCH CRACKS IN TOP RT SIDE OF RUDDER SKIN. A REPAIR DOUBLER WAS INSTALLED IAW SRM 55-01 , FIGURE 2. (X) 2 L 7 2 4F A6WE 1996041800075 19960418 00075 WP 1996 4 18 CAL960413 1 19960313 A 5512 SKIN DOUG DC9 DC932 3022066 WP RUDDER LOOSE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69523 64836 47520 HOU - INSPECTION FOUND SEVERAL LOOSE RIVETS ON LEFT AND RIGHT SIDES OF RUDDER SKIN. THE RIVETS WERE REMOVED AND NEW FAS TENERS WERE INSTALLED IAW SRM 51-30-2. (X) 2 L 7 2 4F A6WE 1996041800076 19960418 00076 WP 1996 4 18 CAL960414 1 19960319 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 658 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69523 64836 47520 HOU - INSPECTION FOUND CORROSION AND .50 INCH CRACKS IN SKIN AT LONGERON 30, STA 658. A REPAIR DOUBLER WAS INSTALLED IA W SRM 53-01, FIGURE 4, SHEET 3. (X) 2 L 7 2 4F A6WE 1996041800077 19960418 00077 CE 1996 4 18 GLBA96007 1 19960209 A 7331 1143890301 FUEL FLOW TRANS BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA LEFT INOPERATIVE A GLBA O OTHER O OTHER CR CRUISE 1 CE 01 55522 10402 2659 UC171 32561 DEN - CREW OBSERVED FLUCTUATION OF LT FUEL FLOW INDICATOR. MAINTENANCE REPLACED FUEL FLOW TRANSMITTER. SYSTEM OPS CHEC K GOOD. (X) 2 L 7 2 4T 4 T RT A24CE E4EA 1996041800078 19960418 00078 CE 1996 4 18 GLBA96035 1 19960219 A 2120 AIR DISTR BEECH 1900 1900C 1154161 CE CABIN ODOR A GLBA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 01 55594 UC145 GFK - CREW REPORTED SMELL LIKE JET FUEL IN CABIN DURING FLIGHT. MAINTENANCE INSPECTED AIRCRAFT, COULD NOT DUPLICATE DIS CREPANCY. (X) 2 L 7 2 4T RT A24CE 1996041800079 19960418 00079 EU 1996 4 18 SIMA960581 1 19960227 A 2910 NAS1601112 O-RING AEROSP ATR72 ATR72212 EU GREEN HYD SYSTEM FAILED A SIMA D RETURN TO BLOCK J K WARNING INDICATION FLUID LOSS TX TAXI/GRND HDL 1 SW 21 407AT 407 DFW - FLT 3811 - DURING TAXI OUT, GREEN SYSTEM HYD LOW LEVEL ALARM ILLUMINATED. NORMAL BRAKING CONTROL WAS LOST. AIRCR AFT RETURNED TO THE GATE. MAINTENANCE FOUND HYDRAULIC LEAK AT THE GREEN SYSTEM LOW PRESSURE WARNING SWITCH IN THE HYD B AY CAUSED BY FAILED O-RING. REPLACED O-RING AND SERVICED HYD SYSTEM. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1996041800080 19960418 00080 EU 1996 4 18 SIMA960782 1 19960318 A 7120 54112010XXXX MOUNT AEROSP ATR72 ATR72212 EU NR 2 ENGINE CRACKED A SIMA K NONE O OTHER DE DESCENT 1 SW 21 349AT ER2263 349 HOU - FLT 3623 - INSPECTED AND FOUND FORWARD OUTBOARD ENGINE MOUNT CRACKED AND BENT. REPLACED FORWARD ENGINE MOUNT AND REPAIRED COWLING. AIRCRAFT RETURNED TO SERVICE. ENGINE MOUNT TO BE SENT FOR FURTHER ANALYSIS. (X) 2 H 7 2 4T RT A53EU 1996041800081 19960418 00081 WP 1996 4 18 9608239105 1 19960411 A 3350 BATTERY PACK DOUG DC9 DC915 3022036 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 95S 47205 DURING LINE CHECK, FOUND EMERGENCY FLOOR LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER, OPERATIO NAL CHECK GOOD. 2 L 7 2 4F A6WE 1996041800082 19960418 00082 EU 1996 4 18 9608243230 1 19960412 A 3350 321430 BATTERY PACK AIRBUS 320 A320211 3930320 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 330NW 307 DURING LINE MAINTENANCE, THE EMERGENCY LIGHTS TEST FAILED. REPLACED BATTERY PACK, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996041800083 19960418 00083 WP 1996 4 18 9608259924 1 19960414 A 3397 WIRE DOUG DC9 DC932 3022066 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 926RC 47473 DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPAIRED BROKEN GROUND WIRE AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996041800084 19960418 00084 WP 1996 4 18 9608269917 1 19960414 A 3397 WIRE HARNESS DOUG DC9 DC932 3022066 WP CABIN WORN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 967N 47573 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS AT SEAT 3C INOPERATIVE. MAINTENANCE FOUND WI RE HARNESS BAD FROM LEFT CAPSULE TO SEAT FRAME CONNECTION. DEFERRED PER MEL 33-24B, AWAITING NEW WIRE HARNESS. 2 L 7 2 4F A6WE 1996041800085 19960418 00085 NM 1996 4 18 9608272296 1 19960414 A 3350 BATTERY PACK BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 296US 21788 DURING PREFLIGHT, FOUND AFT EMERGENCY EXIT SIGN INOPERATIVE. REPLACED BATTERY CARTRIDGE, CHECKED OK. 2 L 7 3 4F A3WE 1996041800086 19960418 00086 NM 1996 4 18 9608282771 1 19960414 A 3350 POWER SUPPLY BOEING 727 7272M7 138407S NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 742RW 21952 DURING PREFLIGHT, FOUND EXTERIOR EMERGENCY LIGHT AT DOOR 2L AND 2R INOPERATIVE. REPLACED POWER SUPPLIES AND BATTERIES, CHECKED. 2 L 7 3 4F A3WE 1996041800087 19960418 00087 NM 1996 4 18 96FDEA00768 1 19960325 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 1155 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 493FE 21531 AFT CARGO STA 1155 STR 30 HEAVY CORROSION ON STRINGER. CUT OUT CORRODED AREA, INSTALLED STRINGER REPAIR PER 53-10-3. 2 L 7 3 4F A3WE 1996041800088 19960418 00088 NM 1996 4 18 96FDEA00769 1 19960328 A 5312 BULKHEAD BOEING 727 72722C 138400F NM BS 1183 RIPPLES A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 103FE 19199 FUSE RIPPLES IN 1183 BULKHEAD AT BOTTOM INSIDE TAIL SKID COMP. REPAIRED RT 1183 BULKHEAD AT TAIL SKID AREA PER ESO 1178 2 DATED 03-18-96 AND EA NR 7-5310-28179 DATED 3-26-96. 2 L 7 3 4F A3WE 1996041800089 19960418 00089 NM 1996 4 18 96FDEA00770 1 19960402 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 365 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 103FE 19199 FUSE STR 25R CRACKED AROUND FASTENER STA 365. FABRICATED AND INSTALLED REPAIR SECTION OF STR 25R, STR 365 PER SRM 53-1 0-3 PAGE 4C AND E. 2 L 7 3 4F A3WE 1996041800090 19960418 00090 NM 1996 4 18 96FDEA00771 1 19960404 A 5315 FLOOR BEAM BOEING 727 72722C 138400F NM BS 480 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 103FE 19199 UPPER LOBE, CORROSION BEYOND LIMITS IN DEPTH ON TOP SURFACE OF FLOOR BEAM BS 480, RBL 26 TO 35. CUT OUT AREA OF CORROSI ON AND INSTALLED FLOOR BEAM REPAIR PER SRM 51-10-6, 51-10-8 FIG 6 AND 8, ESO 11782 DATE 3-20-96 AA AND EA 7-5310-28846 D ATED 3-20-96 FEDEX. 2 L 7 3 4F A3WE 1996041800091 19960418 00091 NM 1996 4 18 96FDEA00772 1 19960405 A 5315 FLOOR BEAM BOEING 727 727227 1384078 NM BS 360 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 493FE 21531 CORROSION REMOVED AT FLOOR BEAM STA 360 LBL 3, AREA NOW BELOW SRM LIMITS FOR THICKNESS. TRANSFERRED FROM NR 0958. CORR ODED AREA REMOVED AND FLOOR BEAM REPAIRED PER SRM 53-10-8 FIG 8. 2 L 7 3 4F A3WE 1996041800092 19960418 00092 NM 1996 4 18 96FDEA00773 1 19960408 A 5315 FLOOR BEAM BOEING 727 727227 1384078 NM BS 380 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 493FE 21531 CABIN FLOOR BEAM CORRODED ON BOTTOM SIDE STA 380 RBL 23 TO 42. REMOVED CORROSION, INSTALLED REPAIR PER SRM 53-10-8 FIG 3. 2 L 7 3 4F A3WE 1996041800093 19960418 00093 WP 1996 4 18 ABXA9600456 1 19960411 A 2910 436392218 O-RING DOUG DC8 DC863 302198A WP HYD SLOT VALVE DEFECTIVE A ABXA L ABORTED APPROACH K J FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 23 816AX 46093 HYDRAULIC QUANTITY DROPPED TO MID SCALE AND HYDRAULIC PRESSURE INDICATOR FLUCTUATED FULL SCALE DURING LANDING GEAR EXTEN SION. RAISED LANDING GEAR DURING MISSED APPROACH AND HYDRAULIC PRESSURE INDICATION STABILIZED. FOUND LARGE HYDRAULIC L EAK IN LEFT WHEEL WELL AREA AFTER LANDING. REPLACED O-RING BETWEEN SLOT CONTROL VALVE AND RIGHT MANIFOLD PRESSURE ASSEM BLY IAW DC8 MM. LEAK CHECK WAS GOOD. 2 L 7 4 4F 4A25 1996041800094 19960418 00094 NE 1996 4 18 ABXA9600457 2 19960412 A 7261 OIL FILTER DOUG DC8 DC863 302198A WP PWA JT3D JT3D7 52039 NE NR 4 ENGINE DIRTY A ABXA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 GL 23 824AX 46141 669445 NR 4 ENGINE HAD A LOW OIL PRESSURE INDICATION. SHUTDOWN THE NR 4 ENGINE AND ENGINE MAINTAINED 6 PSI OIL PRESSURE WHILE WINDMILLING. REPLACED NR 4 OIL FILTER FOR PRECAUTIONARY PROCEDURE IAW PWA MM, CHAPTER 72-00. GROUND RAN ENGINE AND OIL PRESSURE INDICATION WAS WITHIN LIMITS, NO DEFECTS NOTED. 2 L 7 4 4F 4 F 4A25 1E8 1996041800098 19960418 00098 NM 1996 4 18 DHL96708002 1 19960411 A 2710 69301082 AILERON SPRING BOEING 727 72725 1384006 NM LT CONTROL YOKE WORN A T DHLA A UNSCHED LANDING O OTHER DE DESCENT 1 SO 01 708DH 18275 LEFT CONTROL YOKE INPUTS BEYOND 30O YOKE BECOMES STIFF AND IF RELEASED AT MORE THAN 30O, LEFT YOKE WILL STAY AT THAT POS ITION UNTIL MANUALLY RETURNED TO ZERO. PROBLEM DID NOT OCCUR BELOW 10,000 FT ON CLIMB OR DECENT. REPLACED AILERON QUAD RANT CENTERING SPRINGS. REPLACED CAPTAINS CONTROL YOKE GEAR ASSY, OPERATIONAL CHECK PER MM 27-00-11, OK. 2 L 7 3 4F A3WE 1996041800099 19960418 00099 CE 1996 4 18 96ZZZX1731 1 19960301 A 5530 CR3245 RIVETS BEECH 1900 1900D 1154162 CE VERT STAB LOOSE A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 835CA 6463 UE30 DURING SCHEDULED INSPECTIONS, LOOSE FASTENERS ON BOTH SIDES OF VERTICAL STABLILIZER FORWARD SPAR WERE NOTED. ALTHOUGH A SIMILAR PROBLEM WAS ADDRESSED IN SB 2044 ON EARLIER MODEL 1900S, ADDITIONAL EVALUATION AND STUDIES ARE RECOMMENDED AS O THER PREVIOUS IDENTIFIED AREAS OF CONCERN IN THE EMPENNAGE SECTION MAY BE RELATED. REPAIR WAS ACCOMPLISHED PER BEECHCRA FT RECOMMENDED PROCEDURE. 2 L 7 2 4T RT A24CE 1996041800100 19960418 00100 CE 1996 4 18 96ZZZX1732 1 19960130 A 5530 CR3245 RIVETS BEECH 1900 1900D 1154162 CE VERT STAB LOOSE A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 856CA 4785 UE66 DURING SCHEDULED INSPECTIONS, LOOSE FASTENERS ON BOTH SIDES OF VERTICAL STABILIZER FORWARD SPAR WERE NOTED. ALTHOUGH A SIMILAR PROBLEM WAS ADDRESSED IN SB 2044 ON EARLIER MODEL 1900S, ADDITIONAL EVALUATION AND STUDIES ARE RECOMMENDED AS OT HER PREVIOUS IDENTIFIED AREAS OF CONCERN IN THE EMPENNAGE SECTION MAY BE RELATED. REPAIR WAS ACCOMPLISHED PER BEECHCRAF T RECOMMENDED PROCEDURE. 2 L 7 2 4T RT A24CE 1996041800101 19960418 00101 CE 1996 4 18 96ZZZX1733 1 19960228 A 5530 CR3245 RIVETS BEECH 1900 1900D 1154162 CE VERT STAB LOOSE A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 858CA 4876 UE72 DURING SCHEDULED INSPECTIONS, LOOSE FASTENERS ON BOTH SIDES OF VERTICAL STABILIZER FORWARD SPAR WERE NOTED. ALTHOUGH A SIMILAR PROBLEM WAS ADDRESSED IN SB 2044 ON EARLIER MODEL 1900S, ADDITIONAL EVALUATION AND STUDIES ARE RECOMMENDED AS OT HER PREVIOUS IDENTIFIED AREAS OF CONCERN IN THE EMPENNAGE SECTION MAY BE RELATED. REPAIR WAS ACCOMPLISHED PER BEECHCRAF T RECOMMENDED PROCEDURE. 2 L 7 2 4T RT A24CE 1996041800120 19960418 00120 NE 1996 4 18 96ZZZX1752 2 19960216 A 7200 ENGINE LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B02 54555 NE NR 2 VIBRATION A RIAA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 19 302MB 193A1129 10218 ON RIA FERRY FLT 7104 - KMKE/DTW - A/C RETURNED TO KMKE AFTER EXPERIENCING VIBRATION (4.0 A AND B) ON NR 2 ENGINE AT ABO UT 4,000 FEET. REDUCING POWER REDUCED VIBRATION TO 1.0. UPON LANDING, INSPECTED CHIP DETECTORS AND OIL FILTERS, FAN BL ADES, NO DAMAGE FOUND. LUBED MID-SPAN BLADES PER MM 72-31-05. ENGINE RUN-UP ACCOMPLISHED WITH ALL INDICATIONS NORMAL. 2 L 7 3 4F 4 F A23WE E12EU 1996041800123 19960418 00123 WP 1996 4 18 96ZZZX1755 1 19960203 A 3230 RETRACT MECH LKHEED 1011 1011385115 5265015 WP NLG MALFUNCTIONED A RIAA O OTHER J WARNING INDICATION LD LANDING 1 SO 19 306GB 193U1138 RIA - FLT APW243 FROM MIA/KBO - NOSE GEAR FAILED TO EXTEND INTO KBO. GEAR EXTENDED USING ALTERNATE EXTENSION. GEAR IN SPECTION AT KBO, NO VISUAL PROBLEMS NOTED. A/C FERRIED WITH NOSE GEAR EXTENDED TO MIA FOR MAINTENANCE. MAINTENANCE JAC KED NOSE OF A/C AND PERFORMED NORMAL RATE RETREAT AND EXTENSION CHECK PER MM 32-30-00 AND ALT. EXTENSION CHECK PER MM 32 -36-01 AND MECHANICAL EXTENSION CHECK PER MM 32-37-00. NLG OPS CHECKED NORMALLY, A/C RELEASED FOR SERVICE. (X) 2 L 7 3 4F A23WE 1996041800124 19960418 00124 WP 1996 4 18 96ZZZX1756 1 19960205 A 3230 1506376101 UPLOCK ACT 1516855203 LKHEED 1011 1011385115 5265015 WP NLG FAILED A RIAA O OTHER J WARNING INDICATION AP APPROACH 1 SO 19 306GB M0262 193U1138 RIA - FLT APW240 - KBO TO MIA - NOSE GEAR FAILED TO EXTEND INTO MIA. NOSE GEAR EXTENDED USING ALTERNATE EXT. ON GROUND , NLG UPLOCK ACTUATOR REPLACED. A/C RELEASED INTO SERVICE, NO FURTHER INCIDENTS. 2 L 7 3 4F A23WE 1996041800126 19960418 00126 EU 1996 4 18 96ZZZX1758 1 19960123 A 3231 S5287900100064 DOOR LINK AEROSP ATR72 ATR72211 EU RT MLG CRACKED A TRBA K NONE O OTHER TX TAXI/GRND HDL 1 SO 21 EICBC 12934 12147 147 AFTER LANDING AND TAXI, FOUND RIGHT MAIN GEAR DOOR LINK CRACKED AND SPLIT IN TWO PIECES. RIGHT MLG DOOR WAS REMOVED ALO NG WITH BOTH CONCERTINA FOLDABLE DOORS AND VISUAL INSPECTION OF GEAR AREA PERFORMED WITH NO OTHER DEFECTS NOTED. (IRELA ND) 2 H 7 2 4T RT A53EU 1996041800127 19960418 00127 SO 1996 4 18 96ZZZX1759 1 19960212 A 7712 CONNECTOR EMB 120 EMB120ER 3260203 SO RT SIG COND UNIT LOOSE A GLBA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CE 01 299UX 120299 BIS - CREW REPORTED RIGHT ENGINE LOST POWER AND TORQUE FELL TO ZERO ON TAKEOFF ROLL. MAINTENANCE CLEANED AND RESECURED CANNON PLUG ON RIGHT SIGNAL CONDITION UNIT. SYSTEM OPS CHECK GOOD. (X) 2 L 7 2 4T RT A31SO 1996041800128 19960418 00128 CE 1996 4 18 96ZZZX1760 1 19960216 A 2612 24412886 FIRE LOOP BEECH 1900 1900D 1154162 CE RT ENGINE FAILED A GLBA O OTHER N FALSE WARNING CR CRUISE 1 CE 01 169GL UE169 RDU - CREWS MADE SEVERAL REPORTS OF RIGHT FIRE T-HANDLE ILLUMINATING IN-FLIGHT. MAINTENANCE CURED PROBLEM BY REPLACING BOTH RIGHT FIRE LOOPS. REFERENCE: OPERATOR CONTROL GLBA96012. 2 L 7 2 4T RT A24CE 1996041800138 19960418 00138 CE 1996 4 18 GLBA96012 1 19960216 A 2612 244091018 FIRE LOOP BEECH 1900 1900D 1154162 CE RT ENGINE FAILED A GLBA O OTHER N FALSE WARNING CR CRUISE 1 CE 01 169GL UE169 RDU - CREWS MADE SEVERAL REPORTS OF RIGHT FIRE T-HANDLE ILLUMINATING IN-FLIGHT. MAINTENANCE CURED PROBLEM BY REPLACING BOTH RIGHT FIRE LOOPS. REFERENCE: OPERATOR CONTROL NR 96ZZZX1760. (X) 2 L 7 2 4T RT A24CE 1996041800139 19960418 00139 NE 1996 4 18 GLBA96036 2 19960223 A 7320 7863904 HMU EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE RT ENGINE MALFUNCTIONED A GLBA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 01 299UX 965 120299 115680 CIU - CREW REPORTED RT TORQUE FLUCTUATION OF 30 PERCENT AFTER TAKEOFF. CREW ELECTED AN AIR TURN BACK AND MADE AN UNEVEN TFUL LANDING. MAINTENANCE REMOVED AND REPLACED RT HMU. OPS CHECK WAS GOOD. (X) 2 L 7 2 4T 4 T RT A31SO E20NE 1996041800140 19960418 00140 SO 1996 4 18 GLBA96040 1 19960228 A 2510 13910016 LATCH PIN EMB 120 EMB120ER 3260203 SO COPILOT SEAT WORN A GLBA O OTHER O OTHER TO TAKEOFF 1 CE 01 292UX 120292 ORD - CREW REPORTED CO-PILOT'S SEAT SLID AFT ON TAKEOFF ROLL. MAINTENANCE REMOVED AND REPLACED SEAT LATCH PINS. OPS CH ECK WAS GOOD. (X) 2 L 7 2 4T RT A31SO 1996041800143 19960418 00143 EU 1996 4 18 RAIA960234 1 19960223 A 2910 MS21912D6 FITTING AEROSP ATR42 ATR42300 8680920 EU HYD BAY CRACKED A RAIA O OTHER K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 CE 03 EICBF 13875 176 STL - FLT 7211 - GREEN SYSTEM LOW LEVEL LIGHT ILLUMINATED ON CCAS AFTER TAKEOFF. MAINTENANCE REPLACED TEE FITTING ON GR EEN SYSTEM HYDRAULIC ACCUMULATOR, LEAK AND OPERATIONAL CHECKS GOOD. (IRELAND) (X) 2 H 7 2 4T RT A53EU 1996041800144 19960418 00144 NE 1996 4 18 RAIA960235 3 19960223 A 6111 SFA13M10A BLADE AEROSP ATR42 ATR42300 8680920 EU HAMSTD 14SF 14SF5 NE NR 1 PROPELLER SEAL DAMAGE A RAIA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 CE 03 EICBF 13534 698 176 STL - FLT 7174 - OIL LEAK NR 1 PROPELLER. MAINTENANCE REPLACED PROPELLER BLADE. (IRELAND) (X) 2 H 7 2 4T RT A53EU 6 C P7NE 1996041800145 19960418 00145 NE 1996 4 18 RAIA960301 2 19960304 A 7320 7863927 HMU AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE NR 2 ENGINE FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 EICBK 6841 5885 199 120561 BHM - FLT 7459 - NR 2 ENGINE TORQUE DROPPED DURING CLIMB. REPLACED HYDRO-MECHANICAL UNIT. (IRELAND). (X) 2 H 7 2 4T 4 T RT A53EU E20NE 1996041800146 19960418 00146 EU 1996 4 18 RAIA960304 1 19960304 A 5270 SP4594 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU CARGO DOOR OUT OF ADJUST A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 436JX 2575 41036 STL - FLT 7452 - SUPPLEMENT: AFT CARGO DOOR WARNING ILLUMINATED DURING TAKEOFF. MAINTENANCE ISSUED DMI 52-3, MAINTENAN CE LATER CLEARED DMI BY ADJUSTING DOOR WARNING MICROSWITCH, OPERATION CHECK GOOD. (X) 2 L 7 2 4T RT A41NM 1996041800147 19960418 00147 EU 1996 4 18 SIMA960811 1 19960321 A 2612 6500006 BULB SAAB SF340 340B 7860101 EU LAVATORY MALFUNCTIONED A SIMA K NONE N FALSE WARNING CR CRUISE 1 SW 21 359SB 340B359 DFW - FLT 3722 - LAVATORY FIRE WARNING ILLUMINATED DURING FLIGHT. INVESTIGATION SHOWED THE FLUORESCENT LIGHT AND THE SM OKE DETECTOR SHARE A COMMON GROUND. WHEN THE LIGHT GOES OUT, IT ACTIVATES THE SMOKE WARNING. BULB WAS REMOVED AND INSP ECTED AND SYSTEM OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINEERING DEPARTMENT HAS BEEN NOTIFIED OF THIS SITUAT ION AND EXPECT FOLLOW-UP ACTION TO RESOLVE THIS CONDITION. (X) 2 L 7 2 4T RT A52EU 1996041800148 19960418 00148 EU 1996 4 18 SIMA9960541 1 19960223 A 3397 WIRE AEROSP ATR42 ATR42300 8680920 EU PX DOOR STEP BROKEN A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 213AT 211 ORD - FLT 4385 - PASSENGER DOOR STEP LIGHT INOPERABLE. REPAIRED BROKEN WIRE UNDER TOP STEP. OPS CHECKED GOOD. AIRCRAF T RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1996041800149 19960418 00149 NE 1996 4 18 VTZA96100 2 19960305 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE LEFT FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 327UE 41080 P75095 IAD/MHT - FLT 6207 - DURING CRUISE AT 2230 HRS ON 3-5-96, MADE AN UNSCHEDULED LANDING BACK AT IAD DUE TO LT ENGINE CHIP LIGHT. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. AIRCRAFT AUTHORIZED FERRY FLIGHT TO LYH FOR ENGINE CHRONIC CHIP DETECTOR LIGHT. MAINTENANCE REMOVED AND REPLACED ENGINE, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RET URN TO SERVICE. (X) 2 L 7 2 4T 4 T RT A41NM E18NE 1996041800150 19960418 00150 NE 1996 4 18 VTZA96107 2 19960310 A 7260 5725109162 CHIP DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE RT ENGINE DIRTY A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 327UE 86 41080 P76096 IAD/EWR - FLT 6369 - DURING CLIMB-OUT AT 2215 HRS ON 3-10-96, RETURNED TO IAD DUE TO THE RT ENGINE OIL CONTAMINATION LIG HT ILLUMINATING. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE CLEANED CHIP DETECTOR. AIRCRAFT RELEAS ED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T 4 T RT A41NM E18NE 1996041800184 19960418 00184 EU 1996 4 18 96ZZZX1803 1 19960311 A 6420 35033215300 LAMINATED HINGE AEROSP AS355 AS355F1 8680810 EU T/R YOKE EXCESS WEAR A M3XA K NONE O OTHER IN INSP/MAINT 1 WP 07 911TM 60 5059 INSTALLED TEETERING BEARINGS (LAMINATED HINGE) AT ONE-HUNDRED HOUR INSPECTION, 60 HOURS AGO, THEN AT PRE-FLIGHT, NOTICED SEVERE WEAR. REMOVED FROM SERVICE. SUBMITTED TO MANUFACTURE FOR WARRANTY. 1 G 7 2 3U H11EU 1996041800187 19960418 00187 NM 1996 4 18 96FDEA00781 1 19960411 A 5313 STRINGER BOEING 727 727233 138408A NM BS 540 DOUBLE DRILLED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 269FE 21675 FOUND DOUBLE DRILLED HOLE IN STRINGER AT BS 540 STR 15R. REMOVED DAMAGE PER FEDEX SRM 53-10-03 FIG 1, DETAIL 1. FABRIC ATED AND REPAIRED SPLICES AND FILLER PER FEDEX SRM 53-10-03, FIG 1 DETAIL 1. ALODINE AND PRIMERED PER FEDEX SRM 51-10-2 AND INSTALLED FASTENERS PER FEDEX SRM 53-10-3, FIG 1 SHEET 3. 2 L 7 3 4F RT A3WE 1996041800188 19960418 00188 NM 1996 4 18 96FDEA00782 1 19960415 A 5314 65C330232 KEEL BEAM BOEING 727 727233 138408A NM BS 950-1010 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 269FE 21675 RT KEEL BEAM CRACKED AT BS 990 PLUS 1 TO PLUS 4 W/L. REPAIRED RT KEEL BEAM AT BS 990 PLUS 1 TO PLUS 4, PER FEDEX EO 7-5 310-7-2356C PT 5 AND EA 7-53-10-27778. 2 L 7 3 4F RT A3WE 1996041800189 19960418 00189 NM 1996 4 18 96FDEA00783 1 19960415 A 5320 BAC1505100257 CHORD BOEING 727 72725 1384006 NM BS 745 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 CRACK IN REINFORCEMENT CHORD ON UPPER FUEL CELL SKIN BS 745 WL 204.5 RBL 45.5. REMOVED DAMAGED CHORD BS 745 TO 783 RBL 45 WL 204. FABRICATED NEW CHORD AND INSTALLED IAW FEDEX EA 7-5710-28237. 2 L 7 3 4F A3WE 1996041800190 19960418 00190 NM 1996 4 18 96FDEA00784 1 19960415 A 5330 6519850194 SKIN BOEING 727 72725 1384006 NM BS 1083 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 CORROSION BETWEEN SKIN AND WINDOW CUTOUT DOUBLER BETWEEN STR 10 TO 11R STA 1083. REMOVED WINDOW FRAME, FOUND CORROSION TO BE OUT OF LIMITS ON FRAME AT 2 AREAS OF OUTER SKIN. FABRICATED AND INSTALLED REPAIR DOUBLES ON OUTER SKIN AND REPLAC ED FRAME IAW FEDEX EA 7-5310-28236 AND EA 7-5330-28226. 2 L 7 3 4F A3WE 1996041800191 19960418 00191 NM 1996 4 18 96FDEA00785 1 19960415 A 5320 BEAM BOEING 727 72725 1384006 NM BS 740 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 WHILE WORKING NR0470, FOUND CORROSION ON 740 BEAM UPPER SEAT AT LBL 25. 2 L 7 3 4F A3WE 1996041800192 19960418 00192 NM 1996 4 18 96FDEA00788 1 19960416 A 5240 SKIN BOEING 727 727233 138408A NM AFT SRV DOOR DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 269FE 21675 WHILE REMOVING SCUFF PLATES FROM LT AFT SERVICE DOOR ON CARD NR 72C200-01, FOUND DAMAGED HOLE ON OUTER SKIN AFT UPPER CO RNER WHERE SCUFF PLATE FASTENER ATTACH POINT. REPAIRED DAMAGED HOLE ON OUTER SKIN AFT UPPER CORNER WHERE SCUFF PLATE FA STENER ATTACH POINT PER FEDEX EA 7-5310-28242. WHILE WORKING REPAIR FOUND DRILL START ON STR 17L, REPAIRED PER FEDEX SR M 51-40-4. 2 L 7 3 4F RT A3WE 1996041800194 19960418 00194 WP 1996 4 18 ABXA9600462 1 19960408 A 5330 5911408219 SKIN DOUG DC9 DC931 3022065 WP BS 265-303 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 948AX 47065 DURING C-CHECK INSPECTION, CORROSION WAS FOUND UNDER THE FORWARD ADF ANTENNA FROM STA 265 TO 303. FUSELAGE SKIN WAS REP AIRED IAW ABX REA D953-14979-MR. 2 L 7 2 4F A6WE 1996041800195 19960418 00195 WP 1996 4 18 ABXA9600463 1 19960405 A 5210 5910081131 SKIN DOUG DC9 DC931 3022065 WP ENTRY DOOR DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 948AX 52890 DURING C-CHECK INSPECTION, A TEMPORARY REPAIR WAS REMOVED FROM THE MAIN ENTRY DOOR OUTER SKIN FOR INSTALLATION OF A PERM ANENT REPAIR. FUSELAGE SKIN WAS REPAIRED IAW ABX REA D952-14946-MR. 2 L 7 2 4F A6WE 1996041800196 19960418 00196 WP 1996 4 18 ABXA9600464 1 19960320 A 5330 59114013 SKIN DOUG DC9 DC941 302207N WP BS 138 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 47511 DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN CRACKED AT LEFT FORWARD CORNER OF THE E AND E DOOR. REPAIRED IAW ABX REA D953-14813-MR. 2 L 7 2 4F A6WE 1996041800197 19960418 00197 WP 1996 4 18 ABXA9600465 1 19960319 A 5240 39536851 FITTING DOUG DC9 DC941 302207N WP FWD SERVICE DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 47511 DURING C-CHECK INSPECTION, FOUND THE SERVICE DOOR INTERNAL STRUCTURE ABOVE THE HINGE CRACKED. REPLACED FITTING IAW DC-9 SRM 1-30-1, 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1996041800198 19960418 00198 WP 1996 4 18 ABXA9600466 1 19960321 A 5315 99234849 FLOOR BEAM WEB DOUG DC9 DC941 302207N WP BS 180 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 47511 DURING C-CHECK INSPECTION, FOUND CRACKS IN THE FLOOR BEAM WEBS AT STA 180 LBL 19 AND LBL 22. REPAIRED IAW DC-9 SRM 53-0 5, FIGURE 75. 2 L 7 2 4F A6WE 1996041800199 19960418 00199 WP 1996 4 18 ABXA9600467 1 19960321 A 5512 5912175502K1 PANEL DOUG DC9 DC941 302207N WP HORZ STAB DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 47511 DURING C-CHECK INSPECTION, FOUND PANEL 3806A DELAMINATED. REPLACED PANEL IAW DC-9 SERVICE BULLETIN DC-9-55-1. 2 L 7 2 4F A6WE 1996041800200 19960418 00200 WP 1996 4 18 ABXA9600468 1 19960317 A 5753 5910042503 VANE DOUG DC9 DC941 302207N WP LT TE FLAP DENTED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 47511 DURING C-CHECK INSPECTION, FOUND THE LEFT WING INBOARD FIXED VANE CHAFED AND DENTED. REPLACED VANE IAW DC-9 MM 27-51-3. 2 L 7 2 4F A6WE 1996041800201 19960418 00201 WP 1996 4 18 ABXA9600469 1 19960322 A 5512 59121761 PANEL DOUG DC9 DC941 302207N WP HORZ STAB DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 47511 DURING C-CHECK INSPECTION, FOUND PANEL 3703A DELAMINATED. REPLACED PANEL IAW DC-9 SRM 51-10-4. 2 L 7 2 4F A6WE 1996041800202 19960418 00202 WP 1996 4 18 ABXA9600470 1 19960321 A 5320 99234551 FITTING DOUG DC9 DC941 302207N WP FS 718 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 973AX 47511 DURING C-CHECK INSPECTION, FOUND FORWARD KEEL WEB ATTACH FITTING CRACKED AT FS 718 IN THE LEFT WHEEL WELL. REPLACED FIT TING IAW DC-9 SRM 51-30-5 AND 51-30-2. 2 L 7 2 4F A6WE 1996041800203 19960418 00203 WP 1996 4 18 ABXA9600471 1 19960402 A 5755 3923251501 FITTING DOUG DC9 DC941 302207N WP RT SPOILER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 DURING COMPLIANCE OF AD 90-18-03; SB'S 27-228, REV 4, 27-229, REV 3 AND 27-240, REV 5, FOUND INBOARD SPOILER AFT ATTACH FITTING HAD A CRACK INDICATION. REPLACED INBOARD SPOILER ATTACH FITTING IAW DC-9 SUPP MM 27-61-1. 2 L 7 2 4F A6WE 1996041800204 19960418 00204 WP 1996 4 18 ABXA9600472 1 19960316 A 3231 NAS110520 LINK DOUG DC9 DC931 3022065 WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, INSPECTION OF THE LEFT MAIN LANDING GEAR DOOR AND ATTACHMENTS, FOUND THE A RTICULATING DOOR LINK HAD EXCESSIVE PLAY. REPLACED THE LEFT ARTICULATING DOOR LINK ATTACH BOLT. 2 L 7 2 4F A6WE 1996041800205 19960418 00205 WP 1996 4 18 ABXA9600473 1 19960316 A 5280 5910557102 SKIN DOUG DC9 DC931 3022065 WP RT MLG DOOR CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244 INSPECTION OF THE RIGHT MAIN LANDING GEAR DOOR AND ATTACHMENTS, FOUND A SKI N BULGE ON THE ARTICULATING DOOR. REPLACED THE RIGHT MAIN LANDING GEAR ARTICULATING DOOR IAW DC-9 MM 32-12-1. 2 L 7 2 4F A6WE 1996041800206 19960418 00206 WP 1996 4 18 ABXA9600474 1 19960414 A 5347 SEAT TRACK DOUG DC8 DC863 302198A WP RT COCKPIT LACK OF LUBE A ABXA K NONE O OTHER TO TAKEOFF 1 GL 23 819AX 45927 FIRST OFFICER'S SEAT SLID BACK OUT OF LOCKED POSITION DURING TAKEOFF AND AGAIN DURING CRUISE. CLEANED AND LUBED FIRST O FFICER'S SEAT TRACKS AND OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1996041800207 19960418 00207 WP 1996 4 18 ABXA9600475 1 19960405 A 5753 5910041504 VANE DOUG DC9 DC932 3022066 WP RT TE FLAP DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 981AX 47273 DURING C-CHECK INSPECTION, FOUND THE RIGHT FLAP INBOARD FIXED VANE DELAMINATED. REPLACED THE VANE IAW DC-9 MM 27-51-3. 2 L 7 2 4F A6WE 1996041800208 19960418 00208 WP 1996 4 18 ABXA9600476 1 19960331 A 5280 5910557138 SEAL DOUG DC9 DC932 3022066 WP RT MLG DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND THE RIGHT MAIN LANDING GEAR OUTBOARD DOOR SEAL CRACKED. REPLACED SE AL IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 1996041800209 19960418 00209 WP 1996 4 18 ABXA9600477 1 19960331 A 5280 5933787501 HINGE DOUG DC9 DC932 3022066 WP RT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND THE RIGHT MAIN LANDING GEAR OUTBOARD DOOR, ARTICULATING DOOR HINGE H AD EXCESSIVE PLAY. REPLACED HINGE IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 1996041800210 19960418 00210 WP 1996 4 18 ABXA9600478 1 19960331 A 3231 77330 ROD END BRG DOUG DC9 DC932 3022066 WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND THE LEFT MAIN LANDING GEAR DOOR LINK ROD END BEARING HAD EXCESSIVE P LAY. REPLACED ROD END IAW DC-9 MM 32-10-6. 2 L 7 2 4F A6WE 1996041800211 19960418 00211 WP 1996 4 18 ABXA9600479 1 19960408 A 5320 2777976 SKIN SPLICE DOUG DC9 DC932 3022066 WP BS 967 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 981AX 47273 DURING C-CHECK INSPECTION, FOUND THE T-CAP FOR WATER LINE SKIN SPLICE CORRODED AT STA 967, LONGERON 18L. REPAIRED IAW A BX REA D953-14995-MR. 2 L 7 2 4F A6WE 1996041800212 19960418 00212 WP 1996 4 18 ABXA9600480 1 19960406 A 5320 991224357 ANGLE DOUG DC9 DC932 3022066 WP BS 965 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 981AX 47273 DURING C-CHECK INSPECTION, FOUND THE FLOOR BEAM ANGLE AT STA 965 CORRODED AT LBL 45. REPAIRED IAW ABX REA D953-14971-MR . 2 L 7 2 4F A6WE 1996041800213 19960418 00213 WP 1996 4 18 ABXA9600481 1 19960407 A 5330 59114273 SKIN DOUG DC9 DC932 3022066 WP BS 950 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 981AX 47273 DURING C-CHECK INSPECTION, FOUND THE FUSELAGE SKIN CRACKED AT STA 950, BETWEEN L14L AND L15L. REPAIRED IAW ABX REA D953 -14980-MR. 2 L 7 2 4F A6WE 1996041800214 19960418 00214 WP 1996 4 18 ABXA9600482 1 19960405 A 5330 59114273 SKIN DOUG DC9 DC932 3022066 WP BS 990 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 981AX 47273 DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN CRACKED AT STA 990, BETWEEN L16L AND L15L. REPAIRED IAW ABX REA D953-149 86-MR. 2 L 7 2 4F A6WE 1996041800215 19960418 00215 SO 1996 4 18 COMA9610125 1 19960413 A 2752 3203001007 ACTUATOR EMB 120 EMB120RT SO RT TE FLAP MALFUNCTION A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 1110J 7414 539 120110 FLAP DISAGREEMENT AND CONTROL FAULT WARNINGS. REPLACED THE RT OUTBD FLAP ACTUATOR. 2 L 7 2 4T RT A31SO 1996041800216 19960418 00216 NE 1996 4 18 COMA9610126 3 19960411 A 6114 7822911 RELIEF VALVE EMB 120 EMB120RT SO HAMSTD 14RF 14RF9 NE LT PROP MALFUNCTIONED A COMA O OTHER E VIBRATION/BUFFET TX TAXI/GRND HDL 1 SO 01 265CA 120257 LEFT PROPELLER HAS UNUSUAL VIBRATION AND IS SLOW TO ACCELERATE WHEN COMING OUT OF FEATHER. REPLACED THE PROPELLER HUB R ELIEF VALVE. 2 L 7 2 4T RT A31SO 6 C P11NE 1996041800217 19960418 00217 SO 1996 4 18 COMA9610127 1 19960412 A 2120 AIR DISTR EMB 120 EMB120RT SO COCKPIT ODOR A COMA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SO 01 267CA 120259 BURNING ELECTRICAL SMELL IN COCKPIT. COULD NOT DUPLICATE DISCREPANCY, INSPECTED WIRING, PANELS AND OPERATED ALL SYSTEMS . 2 L 7 2 4T RT A31SO 1996041800218 19960418 00218 SO 1996 4 18 COMA9610128 1 19960412 A 5753 KRP138112VT ROLLERS EMB 120 EMB120RT SO LT TE FLAP WORN A COMA K NONE O OTHER LD LANDING 1 SO 01 161CA 120143 AFTER LANDING, OUTBD FLAPS WOULD NOT RETRACT FULLY. REPLACED THE LT OUTBD FLAP ROLLERS. 2 L 7 2 4T RT A31SO 1996041800219 19960418 00219 SO 1996 4 18 COMA9610129 1 19960412 A 3250 3085501003 STEERING ASSY EMB 120 EMB120RT SO NLG FAILED A COMA O OTHER O OTHER LD LANDING 1 SO 01 266CA 120258 NOSE WHEEL STEERING FAILED AFTER LANDING. REPLACED THE NOSE WHELL STEERING ASSY. 2 L 7 2 4T RT A31SO 1996041800220 19960418 00220 SO 1996 4 18 COMA9610130 1 19960414 A 3010 PE200732 HOSE EMB 120 EMB120RT SO CENTER WING LOOSE A COMA E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 01 168CA 120168 LEFT BLEED AIR DUCT LEAK WARNING CAME ON SHORTLY AFTER TAKEOFF. ENGINE WAS SECURED AND ACFT DIVERTED BACK TO FIELD. TI GHTENED LOOSE VENT LINE ON DE-ICE SYSTEM PRESSURE REGULATOR. 2 L 7 2 4T RT A31SO 1996041800221 19960418 00221 1996 4 18 COMA9610131 4 19960415 A 3425 6226342022 EFD-86 EMB 120 EMB120RT SO E/E COMPT FAILED A COMA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 01 257CA 11055 10283 120248 CREW SMELLED SMOKE AND COPILOT'S EADI WENT BLANK AND CIRCUIT BREAKER TRIPPED. REPLACED THE EFD-86. 2 L 7 2 4T RT A31SO 1996041800222 19960418 00222 NE 1996 4 18 COMA9610132 2 19960415 A 7260 3022375 OIL SEAL EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENG GB LEAKING A COMA A E UNSCHED LANDING ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 189CA 120189 LEFT ENGINE OIL PRESSURE DECREASING DURING FLIGHT. ENGINE WAS SECURED AND FLIGHT DIVERTED. REPLACED THE STARTER/GENERA TOR DRIVE OIL SEAL. 2 L 7 2 4T 4 T RT A31SO E20NE 1996041800223 19960418 00223 EU 1996 4 18 COMA9630102 1 19960413 A 7722 523347 ITT INDICATOR SAAB SF340 SF340A 7850100 EU RT ENGINE DEFECTIVE A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 358CA 21271 3656 340A047 RT ENGINE ITT INDICATED 947 DEGREE DURING TAKEOFF. REPLACED THE RT ITT INDICATOR. 2 L 7 2 4T RT A52EU 1996041800224 19960418 00224 EA 1996 4 18 COMA9660064 1 19960415 A 2910 AE2460210G0184 HYD LINE CNDAIR CL600 CL6002B19 EA 3B HYD SYST LEAKING A COMA K NONE K J FLUID LOSS WARNING INDICATION UK UNKNOWN 1 SO 01 915CA 7013 HYDRAULIC FLUID LEVEL IN SYSTEM NR 3 FELL TO ZERO QUANTITY. REPLACED LEAKING LINE ASSY AT THE 3B HYDRUALIC SYSTEM. 2 L 7 2 4F RT A21EA 1996041800225 19960418 00225 EA 1996 4 18 COMA9660065 1 19960413 A 7830 TR UNIT CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RT ENGINE MALFUNCTIONED A COMA O OTHER J WARNING INDICATION LD LANDING 1 SO 01 954CA 7100 807354 THE RT ENGINE THRUST REVERSER WILL NOT STOW. THE NOSE COWL ASSY (P/N 22850020-113), THE TORQUE BOX ASSY (P/N 22850200-1 40) AND THE SLIDER BLOCK ASSY (P/N 22850281-113) HAD EXTENSIVE DAMAGE. THE 10 O'CLOCK POSITION DRIVE ACTUATOR ASSY (P/N 3272570-6) FAILED AT THE CLEVIS ATTACH PIN. ALL COMPONENTS HAVE 561 HOURS TOTAL TIME SINCE NEW. PROBABLE CAUSE OF FAI LURE IS TRACK BINDING AS ADDRESSED IN SERVICE BULLETIN A 601R-78-012. ALL DAMAGED COMPONENTS REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 1996041800226 19960418 00226 NM 1996 4 18 P5CA9600208 1 19960414 A 2613 9750304001 OVERHEAT SW BOEING 747 747122 1384872 NM LT WING MALFUNCTIONED A P5CA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 WP 23 851FT 19756 LEFT WING LEADING EDGE OVERHEAT LIGHT CAME ON AFTER ENGINE START. REPLACED OVERHEAT SWITCH INBOARD OF NR 2 ENGINE STA 3 88 IAW MM 26-18-02. 2 L 7 4 4F A20WE 1996041800227 19960418 00227 NM 1996 4 18 UPS96205967 1 19960412 A 3350 1000677 BATTERY PACK BOEING 727 727172C 1384058 NM COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 916UP 19808 MAINTENANCE REPORTED, EMERGENCY EXIT LIGHT OVER CREW ENTRY AND COCKPIT DOOR BATTERIES DEAD. REPLACED BATTERY PACKS. 2 L 7 3 4F A3WE 1996041800228 19960418 00228 NM 1996 4 18 UPS96205970 1 19960404 A 5311 FRAME BOEING 727 72725C 138400H NM BS 720 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 933UP 19857 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION AFT SIDE OF FRAME WEB BS 720 BL 0 WL 159. REPAIRED IAW SRM 53-10-1 , 51-40-2, 51-10-2, 51-30-2. 2 L 7 3 4F A3WE 1996041800229 19960418 00229 NM 1996 4 18 UPS96205971 1 19960408 A 5753 SKIN BOEING 727 72725C 138400H NM RT TE FLAP DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 933UP 19857 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT AFT O/B FLAP 3 FEET I/B, 1 INCH LONG BY .125 INCH WIDE DELAMINATION MPIP-6 098. REPAIRED PER SRM 51-40-06. 2 L 7 3 4F A3WE 1996041800230 19960418 00230 NM 1996 4 18 UPS96205972 1 19960406 A 5713 BAC15104427178 STRINGER BOEING 727 72725C 138400H NM WS 629 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 933UP 19857 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RWS 629.0 STR 12 HAS A CRACKED VENT STR TAB. REPAIRED STR 12 RWS 629.0 IAW U PS EO B727-5710-0314 APP 8.3. 2 L 7 3 4F A3WE 1996041800231 19960418 00231 NM 1996 4 18 UPS96205973 1 19960411 A 5754 BULLNOSE BOEING 727 72725C 138400H NM NR 1 LE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 933UP 19857 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED NR 1 BULLNOSE I/B LUG CORRODED. REMOVED AND REPLACED NR 1 K-FLAP BULLNOSE IA W MM 27-81-0 AND OHM 57-51-01. 2 L 7 3 4F A3WE 1996041800232 19960418 00232 NM 1996 4 18 UPS96405968 1 19960410 A 3350 900835A BATTERY PACK BOEING 747 747SR46 NM UPPER DECK DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 688UP 20784 MAINTENANCE REPORTED, EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED UPPER DECK EMERGENCY EXIT SIGN BATTERY PACK, OK FO R SERVICE. 2 L 7 4 4F A20WE 1996041800233 19960418 00233 WP 1996 4 18 UPS96805961 1 19960228 A 5230 47732851 FITTING DOUG DC8 DC871F 302199D WP FS 145 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MCD JAMB HEAVY CORROSION ON ATTACH ANGLE FITTING FWD OF NR 1 SPOOL FITTING. R EPLACED ANGLE FITTING PER SRM 51-3-0. 2 L 7 4 4F RT 4A25 1996041800234 19960418 00234 WP 1996 4 18 UPS96805962 1 19960303 A 5230 4801056 BOLTS DOUG DC8 DC871F 302199D WP FS 145-255 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MCD SPOOL BOLTS 1, 2, 4, 5, 6 AND 7 ARE CORRODED. REPLACED BOLTS PER MM 52-3 6-01 (T/C 420269). 2 L 7 4 4F RT 4A25 1996041800235 19960418 00235 WP 1996 4 18 UPS96805963 1 19960308 A 5512 SKIN DOUG DC8 DC871F 302199D WP LT HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT HORIZONTAL STAB L/E SKIN AT ATTACHING SCREW HOLES HAD HEAVY CORROSION AT S TA XFS 125 AND 136 UPPER SIDE OF SKIN. REPAIRED SKIN PER SRM 55-2-1. 2 L 7 4 4F RT 4A25 1996041800236 19960418 00236 WP 1996 4 18 UPS96805964 1 19960228 A 5510 35537301 FITTING DOUG DC8 DC871F 302199D WP LT HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT HORIZONTAL STAB FITTING HAD CORROSION DAMAGE AT NR 4 STR STA XFS 135 BOTTO M INSIDE SKIN. REPLACED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996041800237 19960418 00237 WP 1996 4 18 UPS96805965 1 19960229 A 5320 DOUBLER DOUG DC8 DC871F 302199D WP FS 50-67 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION DAMAGE ON FINGER STR DOUBLER FS 50 TO 67 LONG 21L. REPLACED FINGER DOUBLER PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1996041800238 19960418 00238 WP 1996 4 18 UPS96805966 1 19960302 A 5320 DOUBLER DOUG DC8 DC871F 302199D WP FS 980 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON FWD PRESS BULKHEAD RADIUS DOUBLER, FS 980 LONG 36. REPLAC ED RADIUS DOUBLER PER SRM 51-3-0. 2 L 7 4 4F RT 4A25 1996041800239 19960418 00239 EU 1996 4 18 WWMA9600036 1 19960413 A 3320 BAO8006281 BALLAST SAAB SF340 340B 7860101 EU CABIN DEFECTIVE A WWMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 15 349SB 340B349 CREW REPORTED, SMELL OF SMOKE FROM THE RIGHT SIDE CABIN OVERHEAD CABIN VENTS WHEN THE RECIRCULATION FAN IS ON. UPON INV ESTIGATION, MAINTENANCE FOUND THE OVERHEAD LIGHT BALLAST AT SEAT 7B/8B AND P2 CONNECTOR PLUG BAD. THE BALLAST WAS REPLA CED AND THE CONNECTOR WAS REMOVED AND SECURED FOR SAFETY. THE LIGHT WAS DEFERRED PER THE MEL 33-7. 2 L 7 2 4T RT A52EU 1996041800245 19960418 00245 SW 1996 4 18 96ZZZX1810 1 19960214 A 7910 206061505109 TANK ASSY BELL 206 206L4 1182110 SW ENG OIL WORN A NYBA K NONE O OTHER IN INSP/MAINT 1 EA 11 123NH 52076 WHILE PERFORMING A 100-HOUR INSPECTION, THE MECHANIC NOTED THE BOLTS SECURING THE ENGINE OIL TANK TO THE SUPPORT WERE FO UND WEARING INTO THE TANK FLANGE, ON THE FORWARD END OF TANK. SUBMITTER BELIEVES BOLTS SECURING THE TANK TO SUPPORT HAD WORN INTO THE FLANGE DUE TO IMPROPER SHIMMING. REPLACED ENGINE OIL TANK, PN 206-061-505-109, IAW BELL 206L-4 MM. 1 G 7 1 3U NC H2SW 1996041800246 19960418 00246 SW 1996 4 18 96ZZZX1811 1 19960216 A 5510 206020121009 FITTING 206020123007 BELL 206 206B 1181511 SW STAB LT INBD CRACKED A S A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 152AL 1703 INSPECTION FOUND FITTING CRACKED THROUGH UPPER RIVET HOLES. 1 G 7 1 3U H2SW 1996041800249 19960418 00249 GL 1996 4 18 96ZZZX1814 2 19960216 A 7323 23006260 GOVERNOR BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20 03013 GL NR 1 ENGINE ERRATIC A ALGA O OTHER O OTHER CR CRUISE 1 SW 03 2906T 7275 3275 1AAD471 S573 DURING LEVEL FLIGHT, NOTED THE TORQUE NEEDLES WERE ERRATIC. NR 1 GOVERNOR SHAFT WAS FOUND BINDING. REPLACED GOVERNOR, OPS CHECKED GOOD. 1 G 7 2 3U 3 U H3EU E4CE 1996041800250 19960418 00250 SW 1996 4 18 96ZZZX1815 1 19960223 A 7810 4606AC CLAMP BELL 206 206B 1181511 SW ENGINE EXHAUST BROKEN A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 42AL 33 918 DURING POST-FLIGHT WALKAROUND, DISCOVERED THE LT EXHAUST HAD BECOME DISLODGED AND DIRECTING EXHAUST ONTO THE ENGINE COVE R. FOUND THE EXHAUST CLAMP BROKEN. THE CLAMP WAS REPLACED WITH A SERVICEABLE ONE. 1 G 7 1 3U H2SW 1996041800258 19960418 00258 1996 4 18 96ZZZX1823 4 19960308 A 3416 A30 ENCODER BOLKMS 105 BO105CBS 5626008 EU NOSE COMPARTMENT OVERHEAT A ALGA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 03 5412J 52 48725 S784 IN CRUISE FLIGHT, AN ODOR OF BURNING WIRE WAS NOTED. AFTER INSPECTING AIRCRAFT, FOUND A-30 ENCODER HAD A BURNED SMELL. REMOVED A-30 ENCODER AND INSTALLED SERVICEABLE ENCODER. PERFORMED INTEGRATED SYSTEM TEST. TESTED OK. SUSPECT CAUSE W AS MOISTURE INFILTRATION INTO UNIT. 1 G 7 2 3U NC H3EU 1996041800262 19960418 00262 EU 1996 4 18 96ZZZX1827 1 19960220 A 2841 7165861 GAUGE AEROSP SA365 AS365N2 8680815 EU FUEL QTY STICKS A ZYWA K NONE O OTHER IN INSP/MAINT 1 GL 09 365WM 1001 130 6429 FUEL GAUGE STICKS ON HIGH SIDE INTERMITTENTLY. REMOVED AND REPLACED FUEL GAUGE. 1 G 7 2 3U RT H10EU 1996041800263 19960418 00263 EU 1996 4 18 96ZZZX1828 1 19960319 A 2435 524031 STARTER AEROSP SA365 SA365N 8680669 EU NR 2 ENGINE FAILED A ZYWA K NONE O OTHER IN INSP/MAINT 1 GL 09 365SJ 139 2299 6018 NR 2 ENGINE WILL NOT START. STARTER NOT TURNING. REMOVED AND REPLACED NR 2 ENGINE STARTER GENERATOR. 1 G 7 2 3U H10EU 1996041800264 19960418 00264 EU 1996 4 18 96ZZZX1829 1 19960320 A 2436 D19035 REGULATOR AEROSP SA365 SA365N 8680669 EU DC SYSTEM DEFECTIVE A ZYWA K NONE O OTHER IN INSP/MAINT 1 GL 09 365SJ 4518078 6018 NR 2 VOLTS LOW. VOLTAGE REGULATOR ALLOWS OUTPUT OF 26.9 VOLTS. REMOVED AND REPLACED VOLTAGE REGULATOR. 1 G 7 2 3U H10EU 1996041800265 19960418 00265 EU 1996 4 18 96ZZZX1830 1 19960325 A 3220 18547 ROD END AEROSP SA365 SA365N 8680669 EU NLG WRONG PART A ZYWA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 09 365SJ 6018 PART ORDERED PER IPC, HOWEVER, BARREL ON A/C REVERSED OR OPPOSITE OF IPC. WRONG PART ORDERED. RETURNED WRONG PART. 1 G 7 2 3U H10EU 1996041800266 19960418 00266 EU 1996 4 18 96ZZZX1831 1 19960325 A 3220 18547 ROD END AEROSP SA365 SA365N 8680669 EU NLG BROKEN A ZYWA K NONE O OTHER IN INSP/MAINT 1 GL 09 365SJ 2996 6018 ROD END BROKEN. REMOVED AND REPLACED ROD END. 1 G 7 2 3U H10EU 1996041800268 19960418 00268 SW 1996 4 18 96ZZZX1833 1 19960315 A 5302 214031431105 LONGERON BELL 214 214ST 1182106 SW UPPER TAILBOOM CRACKED A S A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 390AL 3611 HN2307 28198 UPPER TAILBOOM ATTACHMENT LONGERON CRACKED THROUGH ATTACHMENT FITTING. CRACK WAS DISCOVERED DURING THE DAILY VISUAL INS PECTION. PART WAS TAGGED AND SHIPPED TO BELL HELICOPTER IN FORT WORTH, TEXAS. 2 G 7 2 4U H10SW 1996041800269 19960418 00269 EU 1996 4 18 96ZZZX1834 1 19960312 A 2841 7165861 GAUGE AEROSP SA365 AS365N2 8680815 EU FUEL QTY STICKS A ZYWA K NONE O OTHER IN INSP/MAINT 1 GL 09 365WM 14 113 6429 NR 2 NEEDLE STICKS ON FILL. TAPPING GAUGE WILL RELEASE. REMOVED AND REPLACED FUEL GAUGE. 1 G 7 2 3U RT H10EU 1996041800270 19960418 00270 WP 1996 4 18 96ZZZX1835 1 19960125 A 5400 SKIN DOUG DC9 DC981 3022081 WP LT PYLON DELAMINATED A A4JA K NONE O OTHER IN INSP/MAINT 1 SO 15 818SJ 48058 DURING C-CHECK, LT PYLON ABOVE AFT HINGE POINT FOUND DELAMINATED. REPAIRED IAW DC9 SRM CH 54. AIRCRAFT TT: 22,205 HRS . AIRCRAFT TC: 42,206. 2 L 7 2 4F A6WE 1996041800271 19960418 00271 WP 1996 4 18 96ZZZX1836 1 19960125 A 5320 SPLICE DOUG DC9 DC981 3022081 WP BS 229 CORRODED A A4JA K NONE O OTHER IN INSP/MAINT 1 SO 15 818SJ 48058 DURING C-CHECK, FORWARD CARGO COMPARTMENT, LONGERON SPLICE CORRODED, LONGERON 28L AT STA 229. REPAIRED IAW DC9 SRM CH 5 3. AIRCRAFT TT: 22,205 HRS. AIRCRAFT TC: 42,206. 2 L 7 2 4F A6WE 1996041800272 19960418 00272 WP 1996 4 18 96ZZZX1837 1 19960125 A 5312 BLKHD FRAME DOUG DC9 DC981 3022081 WP CARGO COMPT CRACKED A A4JA K NONE O OTHER IN INSP/MAINT 1 SO 15 818SJ 48058 DURING C-CHECK, FORWARD CARGO COMPARTMENT, CRACK IN FRAME ON AFT BULKHEAD AT FLOOR LEVEL. REPAIRED IAW DC9 SRM CH 53. A IRCRAFT TT: 22,205 HRS. AIRCRAFT TC: 42,206. 2 L 7 2 4F A6WE 1996041800273 19960418 00273 WP 1996 4 18 96ZZZX1838 1 19960125 A 5753 VANE DOUG DC9 DC981 3022081 WP LT TE FLAP DELAMINATED A A4JA K NONE O OTHER IN INSP/MAINT 1 SO 15 818SJ 48058 DURING C-CHECK, LEFT WING, NR 2 FLAP VANE DELAMINATED. REPAIRED IAW DC9 SRM CH 57. AIRCRAFT TT: 22,205 HRS. AIRCRAF T TC: 42,206. 2 L 7 2 4F A6WE 1996041800274 19960418 00274 WP 1996 4 18 96ZZZX1839 1 19960125 A 5330 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE CRACKED A A4JA K NONE O OTHER IN INSP/MAINT 1 SO 15 818SJ 48058 DURING C-CHECK, FOUND FUSELAGE SKIN CRACKED, AFT OF NOSE GEAR DOOR CUTOUT. REPAIRED IAW DC9 SRM CH 53. AIRCRAFT TT: 2 2,205. AIRCRAFT TC: 42,206. 2 L 7 2 4F A6WE 1996041800275 19960418 00275 WP 1996 4 18 96ZZZX1840 1 19960125 A 5730 SKIN DOUG DC9 DC981 3022081 WP LT WING TE DELAMINATED A A4JA K NONE O OTHER IN INSP/MAINT 1 SO 15 818SJ 48058 DURING C-CHECK, FOUND LT WING TRAILING EDGE, JUST OUTBOARD OF AILERON, DELAMINATED. REPAIRED IAW DC9 SRM CH 57. AIRCR AFT TT: 22,205. AIRCRAFT TC: 42,206. 2 L 7 2 4F A6WE 1996041800302 19960418 00302 1996 4 18 P9IA096006 4 19960226 A 2565 D31073101 EVAC SLIDE AIRCRUISERS BOEING 727 727231 1384079 NM L2 DOOR LOW PRESSURE A P9IA K NONE O OTHER IN INSP/MAINT 1 SO 03 12305 63843 20510 19562 L2 EVACUATION SLIDE BOTTLE PRESSURE BELOW LIMITS. REPLACED L2 EVACUATION SLIDE PRESSURE BOTTLE IAW MM 25-0-15. (X) 2 L 7 3 4F A3WE 1996041800303 19960418 00303 WP 1996 4 18 9608299979 1 19960310 A 5330 SKIN DOUG DC9 DC931 3022065 WP FS 370 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9343 47439 DURING LINE CHECK, FOUND A CRACK IN THE FORWARD CARGO DOOR CUTOUT SKIN AT THE UPPER FORWARD CORNER FS 370. REPAIRED SKI N PER EA 99-99563. 2 L 7 2 4F A6WE 1996041800304 19960418 00304 WP 1996 4 18 9608301226 1 19960326 A 5730 SKIN DOUG DC10 DC1030 3023501 WP WS 610 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 226NW 46583 DURING M-CHECK, FOUND TWO CRACKS IN THE LEFT WING FIXED LEADING EDGE SKIN AND T-ANGLE AT THE PANEL 519CB CUTOUT, XOS 610 . REPAIRED SKIN (P/N ARB2887-501) AND ANGLE (P/N ARB1137-9) PER EA 12-103936. 2 L 7 3 4F A22WE 1996041800305 19960418 00305 WP 1996 4 18 9608319861 1 19960327 A 5315 FLOOR BEAM DOUG DC9 DC951 3022051 WP FS 1167 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 770NC 47758 DURING H-CHECK, FOUND CORROSION ON THE FS 1167 FLOOR BEAM UPPER CAP FROM THE RIGHT CUSP TO THE RIGHT INBOARD LAV WALL. R EPAIRED BEAM (P/N 9915561-1) PER EA 98-109486. 2 L 7 2 4F A6WE 1996041800306 19960418 00306 WP 1996 4 18 9608329861 1 19960328 A 5315 FLOOR BEAM DOUG DC9 DC951 3022051 WP FS 1136 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 770NC 47758 DURING H-CHECK, FOUND CORROSION ON THE FS 1136 FLOOR BEAM UPPER CAP UNDER THE RIGHT LAV INBOARD FLOOR SUPPORT. REPAIRED BEAM (P/N 9912243-55) PER EA 98-109466. 2 L 7 2 4F A6WE 1996041800307 19960418 00307 WP 1996 4 18 9608331226 1 19960329 A 5712 RIB DOUG DC10 DC1030 3023501 WP WS 644 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 226NW 46583 DURING M-CHECK, FOUND A CRACK IN THE LEFT WING LEADING EDGE FORMER AT XORS 644. REPAIRED FORMER (P/N ARB2917-11) PER EA 12-103929. 2 L 7 3 4F A22WE 1996041800308 19960418 00308 WP 1996 4 18 9608349954 1 19960401 A 5311 FRAME DOUG DC9 DC931 3022065 WP FS 484-522 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 921RW 47164 DURING H-CHECK, FOUND CORROSION ON THE FUSELAGE FRAME STRAPS AT FS 484 AND 522 BETWEEN LONGERONS 29L AND 29R. REPAIRED STRAPS (P/N RW2800206-8) PER EA 99-109471 AND 99-109475. 2 L 7 2 4F A6WE 1996041800309 19960418 00309 NM 1996 4 18 9608352712 1 19960401 A 5315 FLOOR BEAM BOEING 727 7272S7 138407Z NM FS 312 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 712RC 22020 DURING H-CHECK, FOUND CORROSION ON THE BS 312 FLOOR BEAM UPPER CHORD AT THE A/C CENTER LINE. REPAIRED CHORD (P/N 65-163 14) PER EA 27-104215. 2 L 7 3 4F A3WE 1996041800310 19960418 00310 NM 1996 4 18 9608362712 1 19960402 A 5315 FLOOR BEAM BOEING 727 7272S7 138407Z NM FS 1130 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 712RC 22020 DURING H-CHECK, FOUND CORROSION ON THE BS 1130 FLOOR BEAM UPPER CHORD AT LBL 16, 42 AND 48. REPAIRED CHORD (P/N 65-2082 2-3) PER EA 27-79525. 2 L 7 3 4F A3WE 1996041800311 19960418 00311 NM 1996 4 18 9608372712 1 19960402 A 5320 INTERCOSTAL BOEING 727 7272S7 138407Z NM FS 740 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 712RC 22020 DURING H-CHECK, FOUND CORROSION ON THE FS 740 KEEL BEAM INTERCOSTAL FROM LBL 6 TO RBL 6. REPAIRED INTERCOSTAL (P/N 69-4 7111-2) PER EA 27-104209. 2 L 7 3 4F A3WE 1996041800312 19960418 00312 WP 1996 4 18 9608389954 1 19960405 A 5320 SPLICE DOUG DC9 DC931 3022065 WP FS 560 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 921RW 47164 DURING H-CHECK, FOUND CORROSION ON THE LONGERON 30 SPLICE AT FS 560. REPLACED SPLICE (P/N 5920319-504) PER EA 99-109493 . 2 L 7 2 4F A6WE 1996041800313 19960418 00313 NM 1996 4 18 9608392712 1 19960406 A 5313 LONGERON BOEING 727 7272S7 138407Z NM FS 690 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 712RC 22020 DURING H-CHECK, FOUND CORROSION ON STR 28R AT BS 690. REPAIRED STRINGER (P/N 65-56236-22) PER EA 27-104217. 2 L 7 3 4F A3WE 1996041800314 19960418 00314 WP 1996 4 18 9608409968 1 19960409 A 5210 FITTING DOUG DC9 DC931 3022065 WP PAX DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9332 47264 DURING M-CHECK, FOUND CRACKS ON THE AFT CABIN DOOR RIGHT SIDE BEAM FITTINGS; NR 3 AND NR 4 UPPER AND LOWER. REPLACED FI TTINGS (P/N 9915565-161, 99-15563-157 AND 99-15565-155) PER SRM 51-30-2, -3. 2 L 7 2 4F A6WE 1996041800315 19960418 00315 WP 1996 4 18 9608419968 1 19960409 A 5720 FITTING DOUG DC9 DC931 3022065 WP FS 598-617 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9332 47264 DURING M-CHECK, FOUND CORROSION ON THE WING BOX FITTING AT FS 598 TO 617, LBL 50. REPLACED FITTING PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996041800316 19960418 00316 WP 1996 4 18 9608421160 1 19960409 A 5330 SKIN DOUG DC10 DC1040 3023508 WP FS 869 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 160US 46769 DURING C-CHECK, FOUND CORROSION ON THE FUSELAGE SKIN AT FS 869, LONGERON 39R, UNDER THE PRIMARY STATIC PORT. REPAIRED S KIN (P/N ADA7030-1) PER EA 11-103927. 2 L 7 3 4F A22WE 1996041800317 19960418 00317 NM 1996 4 18 9608436718 1 19960409 A 5313 FITTING BOEING 747 747251F 1384898 NM FS 2360 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 618US 21122 DURING P-CHECK, FOUND A CRACK AND CORROSION IN THE STR 36L END FITTING AT BS 2360. REPLACED FITTING PER SRM 51-10-01, P AR 10, PG 18. 2 L 7 4 4F A20WE 1996041800318 19960418 00318 NM 1996 4 18 9608442712 1 19960409 A 5313 LONGERON BOEING 727 7272S7 138407Z NM FS 950 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 712RC 22020 DURING H-CHECK, FOUND CORROSION ON STR 29R AT BS 950B PLUS 7 TO 12 AND AT BS 950E. REPAIRED STRINGER (P/N 65-56441-4) P ER EA 27-104219. 2 L 7 3 4F A3WE 1996041800319 19960418 00319 NM 1996 4 18 9608452712 1 19960409 A 5320 CHORD BOEING 727 7272S7 138407Z NM FS 335 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 712RC 22020 DURING H-CHECK, FOUND A CRACK IN THE NOSE LANDING GEAR WHEEL WELL RIGHT SIDE PANEL CHORD AT BS 335, RBL 17. REPAIRED CH ORD (P/N 65-19861-6) PER EA 27-104221. 2 L 7 3 4F A3WE 1996041800320 19960418 00320 WP 1996 4 18 9608469751 1 19960410 A 5210 LATCH FITTING DOUG DC9 DC941 302207N WP PAX DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 751NW 47115 DURING H-CHECK, FOUND A CRACK IN THE AFT ENTRY DOOR UPPER LATCH FITTING. REPLACED FITTING PER SRM 51-30-2. 2 L 7 2 4F A6WE 1996041800321 19960418 00321 WP 1996 4 18 9608479968 1 19960410 A 5320 SILL DOUG DC9 DC931 3022065 WP FS 340 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9332 47264 DURING M-CHECK, FOUND CORROSION ON THE FORWARD CARGO DOOR JAMB LOWER SILL AT FS 340. REPAIRED SILL (P/N 5912494) PER EA 99-109426. 2 L 7 2 4F A6WE 1996041800322 19960418 00322 WP 1996 4 18 9608489609 1 19960410 A 5330 SKIN DOUG DC9 DC932 3022066 WP FS 200 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 609NW 47234 DURING LINE CHECK, FOUND TWO CRACKS .25 INCH AND .19 INCH IN THE FORWARD ENTRY DOOR JAMB CUTOUT SKIN, UPPER AFT CORNER, FS 200 AT LONGERON 9L. REPAIRED SKIN (P/N 5911406-5) PER EA 96-104228. 2 L 7 2 4F A6WE 1996041800323 19960418 00323 WP 1996 4 18 9608499751 1 19960410 A 5210 FITTING DOUG DC9 DC941 302207N WP PAX DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 751NW 47115 DURING H-CHECK, FOUND CRACKS IN THE AFT ENTRY DOOR BEAM RIGHT SIDE END FITITNGS; NR 1 UPPER, NR 3 UPPER AND LOWER AND NR 4 UPPER. REPLACED ALL FITTINGS PER SRM 51-00. 2 L 7 2 4F A6WE 1996041800324 19960418 00324 WP 1996 4 18 9608509751 1 19960411 A 3232 ACT FITTING DOUG DC9 DC941 302207N WP RT MLG DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 751NW 47115 DURING H-CHECK, FOUND A TWO INCH CRACK IN THE RIGHT MAIN LANDING GEAR INBOARD DOOR RETURN CYLINDER SUPPORT FITTING AT TH E KEEL. REPLACED FITTING PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996041800325 19960418 00325 NM 1996 4 18 9608512297 1 19960411 A 7711 EPR TRANS BOEING 727 727251 138408H NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 297U 21789 695245 NR 2 ENGINE EPR INDICATION FAILED TO RESPOND TO THROTTLE MOVEMENT ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRC RAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE EPR TRANSMITTER AND INDICATOR WITH A SERVICEABLE UNIT. 2 L 7 3 4F 4 F A3WE E2EA 1996041800326 19960418 00326 NE 1996 4 18 9608522291 2 19960411 A 7230 COMPRESSOR BOEING 727 727251 138408H NM PWA JT8 JT8D15A 52051 NE ENGINE STALLED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 01 291U 21379 UNIDENTIFIED ENGINE COMPRESSOR STALLED ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED ALL THREE ENGINES AND NO DISCREPANCIES NOTED. 2 L 7 3 4F 4 F A3WE E2EA 1996041800327 19960418 00327 NE 1996 4 18 9608535514 2 19960414 A 7230 COMPRESSOR BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE NR 2 ENGINE STALLED A NWAA E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 GL 01 514US 23202 716364 DURING CLIMB, THE NR 2 ENGINE EXPERIENCED A VIBRATION AND A COMPRESSOR STALL, THE ENGINE WAS SHUTDOWN. THE AIRCRAFT RET URNED TO LAS AND LANDED WITHOUT FURTHER INCIDENT. THE NR 2 ENGINE WAS BORESCOPE INSPECTED AND FOUND TO HAVE DAMAGE TO T HE 6TH THROUGH 10TH STAGES OF THE HPC AND FOD DAMAGE TO THE HPT AND LPT. NR 2 ENGINE CHANGE TO BE ACCOMPLISHED. 2 L 7 2 4F 4 F RT A2NM E17NE 1996041800328 19960418 00328 WP 1996 4 18 9608541161 1 19960413 A 7714 7424372 TACH GENERATOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 3 ENGINE MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 161US 46770 86138 DURING CLIMBOUT, THE NR 3 ENGINE N1, N2 AND NR 3 EPR BECAME ERRATIC, ALL OTHER INDICATIONS NORMAL. CREW FOLLOWED COCKPI T OPERATING PROCEDURES AND RETURNED TO DTW WITHOUT FURTHER INCIDENT. REPLACED THE N1 AND N2 INDICATORS. ALSO, REPLACED THE NR 3 N2 TACH GENERATOR, PERFORMED NR 3 ENGINE RUNUP AT FULL POWER AND NOTED N2 STILL FLUCTUATING. N2 WAS MEL'D AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A22WE E20EA 1996041800329 19960418 00329 WP 1996 4 18 9608559104 1 19960410 A 5350 CLIPS DOUG DC9 DC915 3022036 WP TAIL CONE OUT OF ADJUST A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 94S 47204 DURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR TAIL CONE HANDLE FROM THE CLIPS. ADJUST ED THE CLIPS, CHECKED OK. 2 L 7 2 4F A6WE 1996041800330 19960418 00330 NM 1996 4 18 9608562289 1 19960415 A 3297 WIRE BOEING 727 727251 138408H NM NLG FAILED A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 289US 21377 DURING APPROACH ON GEAR EXTENSION, NOSE GEAR FAILED TO INDICATE DOWN AND LOCKED. RECYCLED GEAR, ALL INDICATIONS WERE NO RMAL AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPAIRED WIRE IN NOSE WHEEL WELL, PERFORMED GEAR SWING AND OPERA TIONAL CHECK OK. 2 L 7 3 4F A3WE 1996041800331 19960418 00331 WP 1996 4 18 9608579759 1 19960412 A 2810 7912854537 ELBOW DOUG DC9 DC941 302207N WP LT FUEL TANK CRACKED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK K FLUID LOSS TO TAKEOFF 1 GL 01 759NW 47287 DURING TAKEOFF, NOTICED FUEL VENTING FROM THE RIGHT WING. ABORTED TAKEOFF AND RETURNED TO THE GATE. FOUND CRACKED ELBO W ON INBOARD PUMP VOLUTE IN THE LEFT TANK. REPLACED ELBOW AND CHECKED VENT POPPETS, LEAK AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996041800332 19960418 00332 1996 4 18 9608589106 4 19960413 A 3425 ADI DOUG DC9 DC915 3022036 WP RT COCKPIT MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 96S 47206 DURING CLIMB, THE FIRST OFFICER'S ATTITUDE INDICATOR FAILED. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REP LACED THE NR 2 VERTICAL GYRO, NR 2 AMPLIFIER AND ADI. TESTED SYSTEM AND ALL CHECKED GOOD. 2 L 7 2 4F A6WE 1996041800333 19960418 00333 EU 1996 4 18 9608593245 1 19960413 A 3260 PROX SENSOR AIRBUS 320 A320211 3930320 EU LT MLG DOOR FAILED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 345NW 399 DURING APPROACH AFTER LANDING GEAR EXTENSION, THREE RED LANDING GEAR INDICATION LIGHTS ILLUMINATED. CYCLED LANDING GEAR HANDLE AND ALL INDICATIONS NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR DOOR PROXIMITY SENSOR (33GA) AND OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996041800334 19960418 00334 NM 1996 4 18 9608606612 1 19960417 A 3350 BATTERY PACK BOEING 747 747251B 1384892 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 612US 20357 DURING LINE CHECK, FOUND EMERGENCY DOOR EXIT SIGNS AT DOOR 3L AND 3R INOPERATIVE. REPLACED BATTERY PACKS AND OPERATIONA L CHECK GOOD. 2 L 7 4 4F A20WE 1996041800335 19960418 00335 NM 1996 4 18 9608616305 1 19960416 A 3350 WIRE BOEING 747 747451 1384940 NM CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 665US 23820 DURING LINE CHECK, FOUND EMERGENCY LIGHTS FROM ROWS 35ABC TO 42ABC INOPERATIVE. REPAIRED BROKEN WIRE AND OPERATIONAL CH ECK GOOD. 2 L 7 4 4F RT A20WE 1996041800336 19960418 00336 NE 1996 4 18 9608636739 2 19960416 A 7200 ENGINE BOEING 747 747251F 1384898 NM PWA JT9 JT9D7Q 52054 NE NR 2 FAILED A NWAA A E J UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 GL 01 639US 23887 02241 DURING CLIMBOUT, THE NR 2 ENGINE EXPERIENCED TWO COMPRESSOR STALLS AT FL 200, FOLLOWED BY LOSS OF OIL PRESSURE AND QUANT ITY. THE FIRE WARNING BELL THEN SOUNDED AND ILLUMINATED. CREW SHUTDOWN THE ENGINE PER COM PROCEDURES, DUMPED 140,000 L BS OF FUEL AND RETURNED TO ANC WITHOUT FURTHER INCIDENT. FOUND HOLE IN NR 3 BEARING BREATHER TUBE, METAL AND OIL IN TAI LPIPE AND SEVERAL WIRES WERE FOUND WITH HEAT DISTRESS. THE AIRCRAFT WILL BE FERRIED TO MSP FOR FURTHER ANALYSIS OF NR 2 ENGINE. 2 L 7 4 4F 4 F A20WE E3NE 1996041800337 19960418 00337 1996 4 18 9608649913 4 19960415 A 2565 113319 SLIDE DOUG DC9 DC931 3022065 WP MAIN CABIN DOOR LOW PRESSURE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 963N 34167 47415 DURING PERIODIC CHECK, FOUND MAIN CABIN DOOR EVACUATION SLIDE LOW ON PRESSURE. REPLACED SLIDE. 2 L 7 2 4F A6WE 1996041800338 19960418 00338 WP 1996 4 18 9608659946 1 19960415 A 3350 60030451 POWER SUPPLY DOUG DC9 DC931 3022065 WP TAIL COMPT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8926E 45863 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY LIGHT POWER SUPPLY BROKEN. REPLACED POWER SUPPLY A ND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996041800339 19960418 00339 WP 1996 4 18 9608669949 1 19960415 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP TAIL COMPT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8928E 45865 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES AND OPERATI ONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996041800340 19960418 00340 NM 1996 4 18 96UAL900251 1 19960412 A 2611 03061122 SMOKE DET WIRES BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE AFT LT LAV BROKEN A UALA O OTHER L NO TEST IN INSP/MAINT 1 WP 29 7452U 21906 AFT LEFT LAVATORY SMOKE DETECTOR INOPERATIVE DUE TO WIRES TO DETECTOR FOUND BROKEN. SUPPLEMENTAL DATA UPDATE: SUBMITTE R SUGGESTS CAUSE AS PASSENGER ACTION TO DISABLE THE SMOKE DETECTOR. INSTALLED NEW WIRING ASSEMBLY AND CONNECTOR REPAIR. SMOKE DETECTOR OPERATION NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1996041800341 19960418 00341 NM 1996 4 18 96UAL900252 1 19960412 A 5754 65162212 SLAT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 5 LE SLAT CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7293U 21571 NR 5 SLAT HAS A 2.5 INCH CRACK. SUPPLEMENTAL DATA UPDATE: SLAT REPAIRED PER SRM 57-50-03, REPAIR NR 1. 2 L 7 3 4F 4 F A3WE E2EA 1996041800342 19960418 00342 NM 1996 4 18 96UAL900253 1 19960412 A 3350 BATTERY PACK BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE CABIN DISCHARGED A UALA K NONE L NO TEST CR CRUISE 1 WP 29 165UA 21658 EMERGENCY FLUORSCENT STRAP LIGHT AND EMERGENCY DOOR LIGHT AT DOOR 2R STAYED ON DURING FLIGHT. EMERGENCY BATTERY INOP. R EPLACED BATTERY PACK. 2 L 7 4 4F 4 F A20WE E20EA 1996041800343 19960418 00343 NM 1996 4 18 96UAL900254 1 19960412 A 5523 657379946 TAB BOEING 737 737291 138448W NM PWA JT8 JT8D9A 52048 NE RT ELEVATOR FRACTURED A UALA O OTHER E VIBRATION/BUFFET DE DESCENT 1 WP 29 981UA 21546 CREW ADVISED OF SEVERE AIRFRAME VIBRATION AT 350 KNOTS. IT CONTINUED DOWN THROUGH 250 KNOTS AND THEN STOPPED. UPON ARR IVAL, FOUND RIGHT ELEVATOR TRIM TAB TORN OFF AND STICKING UP. SUPPLEMENTAL DATA UPDATE: THE RIGHT ELEVATOR CONTROL TAB FRACTURED INTO TWO PIECES AT THE NR ONE TAB HINGE POSITION. THE TAB WAS REPLACED AND MINOR DAMAGE TO THE ELEVATOR ASSE MBLY WAS REPAIRED. 2 L 7 2 4F 4 F A16WE E2EA 1996041800344 19960418 00344 NM 1996 4 18 96UAL900255 1 19960412 A 2750 RETRACT MECH BOEING 737 737322 1384676 NM TE FLAPS MALFUNCTIONED A A UALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 29 303UA 23644 DURING FLAP EXTENSION FELT SLIGHT ROLL, THERE WAS NO INDICATION OF FLAP EXTENSION EITHER VISUALLY OR INDICATION. SEVERA L SECONDS LATER THE FLAPS STARTED DOWN AND AN ASYMMETRY CONDITION DEVELOPED AT 15 DEGREES. 2 L 7 2 4F RT A16WE 1996041800345 19960418 00345 NM 1996 4 18 96UAL900256 1 19960412 A 3260 DT2RA7 SWITCH BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE NLG INOPERATIVE A UALA O OTHER N FALSE WARNING AP APPROACH 1 WP 29 9009U 19047 WHEN GEAR EXTENDED FOR LANDING GOT A RED UNSAFE LIGHT FOR NOSE LANDING GEAR. RECYCLED GEAR AND SECOND EXTENSION GOT NO LIGHTS AT ALL. VISUALLY CONFIRMED NOSE GEAR WAS DOWN. MAIN GEAR INDICATIONS WERE NORMAL. *S/D* REPLACED NOSE LANDING GEAR INDICATION SWITCH, CHECKS OK. 2 L 7 2 4F 4 F A16WE E2EA 1996041800347 19960418 00347 WP 1996 4 18 96UAL900258 1 19960415 A 3350 POWER SUPPLY DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1811U 46610 EEL FLOOR LIGHTING ROWS 9 TO 17AB ARE INTERMITTENT. REPLACED EEL BATTERY POWER SUPPLY, CHECKS OKAY. 2 L 7 3 4F 4 F A22WE E23EA 1996041800348 19960418 00348 WP 1996 4 18 96UAL900259 1 19960415 A 2740 AJG704119 TRIM CONTL VLV AJG70415535 DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 1 STAB CRACKED A UALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 1810U 14500 467 46609 NR 3 HYDRAULIC SYSTEM LOSS. RETURNED TO DTW. SUPPLEMENTAL DATA UPDATE: NR 1 (UPPER) STABILIZER TRIM CONTROL VALVE HOU SING CRACKED. REPLACED CONTROL VALVE AND BOTH NR 3 ENGINE HYDRAULIC PUMPS. PART TOTAL CYCLES, 3,800. 2 L 7 3 4F 4 F A22WE E23EA 1996041800349 19960418 00349 EU 1996 4 18 96UAL900260 2 19960415 A 7320 THROTTLE CONTROL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563B2 13802 EU NR 1 ENGINE MALFUNCTIONED A UALA A E UNSCHED LANDING ENGINE SHUTDOWN O OTHER CR CRUISE 1 WP 29 316UA 23948 724478C56 AFTER LEVEL OFF AT CRUISE ALTITUDE, NR 1 THROTTLE WOULD NOT RETARD BELOW 93 PERCENT N1 WITH AUTOTHROTTLES ON OR OFF. RE TURNED TO DEN AND SHUTDOWN NR 1 ENGINE PRIOR TO LANDING IN DEN. 2 L 7 2 4F 4 F RT A16WE E21EU 1996041800350 19960418 00350 NM 1996 4 18 96UAL900261 1 19960415 A 3234 HANDLE BOEING 737 737522 138449F NM COCKPIT OUT OF RIG A UALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 WP 29 915UA 25382 ON FINAL APPROACH, LANDING GEAR RED WARNING LIGHTS CAME ON AND SOUNDED ALARM. DURING GO-AROUND, MANUAL ADJUSTMENT OF GE AR HANDLE ELIMINATED RED WARNING LIGHTS. *S/D* MANUALLY ADJUSTED GEAR HANDLE. MAINTENANCE CHECKED POSITION SWITCH AND MOUNTS, OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A16WE 1996041800351 19960418 00351 NM 1996 4 18 96UAL900262 1 19960415 A 3150 T/O WARNING BOEING 737 737322 1384676 NM COCKPIT SOUNDED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 29 373UA 24638 DURING TAKEOFF WARNING HORN SOUNDED, RETURNED TO BLOCKS. *S/D* MAINTENANCE PERFORMED OPERATIONAL CHECK OF TAKEOFF WARN ING SYSTEM WITH NO FAULTS FOUND. 2 L 7 2 4F RT A16WE 1996041800352 19960418 00352 NM 1996 4 18 96UAL900263 1 19960416 A 3350 CONNECTORS BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 644UA 25094 FORWARD CROSS AISLE EEL STRIP INOPERABLE. REPLACED CONNECTORS ON EEL STRIPS, OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 1996041800353 19960418 00353 NM 1996 4 18 96UAL900264 1 19960416 A 3350 LIGHTS BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7259U 21406 EMERGENCY LIGHTS COME ON WHEN SWITCHED TO ARMED POSITION. REPLACED R-70 AND SYSTEM CHECKS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1996041800354 19960418 00354 EU 1996 4 18 96UAL900265 1 19960416 A 3350 CIRCUIT BREAKER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN TRIPPED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 409UA 462 EMERGENCY LIGHTS FAILED SYSTEM TEST. RESET CIRCUIT BREAKERS AND SYSTEM OPERATED NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 1996041800355 19960418 00355 EU 1996 4 18 96UAL900266 1 19960416 A 3350 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 420UA 489 EMERGENCY LIGHTS FAILED TEST. REPLACED POWER SUPPLY AND SYSTEM OPERATED NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 1996041800356 19960418 00356 WP 1996 4 18 DHL96802002 1 19960413 A 3610 12J82400 SHUTOFF VLV DOUG DC8 DC873F 302199F WP NR 2 ENG LEAKING A T DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 802DH 46076 MANIFOLD NR 2 OVER TEMP ILLUMINATED IN FLIGHT, TEMP WAS 215 DEGREES CELSIUS, PERFORMED CHECK LIST AND LIGHT WENT OUT. E NGINE DE-ICE WAS ON AT THE TIME. OPENED PYLON, CHECKED DUCTING FOR SECURITY, FOUND OKAY. PRE-COOLER VALVE FOR OPERATIO N WAS OKAY, REGULATING VALVE AND MUSCLE LINE OKAY, TEMP SENSOR MANIFOLD FOUND OKAY AND SECURED. FOUND AIR LEAKAGE ON NR 2 ENGINE FIREWALL SHUT OFF VALVE, SECURED CLAMPS AND OPERATES OKAY. 2 L 7 4 4F RT 4A25 1996041800357 19960418 00357 NM 1996 4 18 SCNA96042 1 19960413 A 5315 FLOOR BEAM BOEING 727 727227 1384078 NM BS 344 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 275AF 22092 DURING HEAVY MAINTENANCE VISIT, THE FLOOR BEAM UPPER CHORD AT STATION 344 WAS FOUND CORRODED FROM LBL 47 TO RBL 44. REP AIRED CORRODED FLOOR BEAM IAW BOEING SRM 53-10-08 FIGURE 8 AND REPLACED UPPER CHORD FROM RBL 434 TO BULKHEAD. 2 L 7 3 4F A3WE 1996041800358 19960418 00358 NM 1996 4 18 SCNA96043 1 19960413 A 5315 FLOOR BEAM BOEING 727 727227 1384078 NM BS 360 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 275AF 22092 DURING HEAVY MAINTENANCE VISIT, THE FLOOR BEAM UPPER CHORD AT STATION 360 WAS FOUND CORRODED BETWEEN RBL 12 TO LBL 19. R EPAIRED CORRODED FLOOR BEAM IAW BOEING SRM 53-10-08 FIGURE 8. 2 L 7 3 4F A3WE 1996041800359 19960418 00359 NM 1996 4 18 SCNA96044 1 19960413 A 5315 652082616 FLOOR BEAM BOEING 727 727227 1384078 NM BS 380 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 275AF 22092 DURING HEAVY MAINTENANCE VISIT, THE FLOOR BEAM UPPER CHORD AT STATION 380 WAS FOUND CORRODED UNDERNEATH THE CENTER AISLE . REPAIRED CORRODED FLOOR BEAM IAW BOEING SRM 53-10-08 FIGURE 8. 2 L 7 3 4F A3WE 1996041800360 19960418 00360 NM 1996 4 18 SCNA96045 1 19960413 A 5315 652082753 FLOOR BEAM BOEING 727 727227 1384078 NM BS 400 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 275AF 22092 DURING HEAVY MAINTENANCE VISIT, THE FLOOR BEAM UPPER CHORD AT STATION 400 WAS FOUND CORRODED UNDERNEATH THE CENTER AISLE . REPAIRED CORRODED FLOOR BEAM IAW BOEING SRM 53-10-08 FIGURE 8. 2 L 7 3 4F A3WE 1996041800361 19960418 00361 WP 1996 4 18 SCNA96046 1 19960413 A 2560 541589001 INDICATOR BULB DOUG DC10 DC1015 3022118 WP R 4 DOOR FAILED A SCNA K NONE N FALSE WARNING NR NOT REPORTED 1 GL 15 152SY 48289 THE R4 DOOR SLIDE INDICATOR WOULD NOT ILLUMINATE WHEN PRESSED. RELAMPED SLIDE INDICATOR LIGHT, SLIDE TESTED GOOD. 2 L 7 3 4F A22WE 1996041800363 19960418 00363 WP 1996 4 18 96ZZZM675 2 19960313 A 7320 CA3108R12S3SF80 CONNECTOR BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LEFT FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 27 488UE 907 P66150 FLT NR 6175 - ELM-IAD - ABORTED THE TAKEOFF DUE TO THE LEFT ENGINE EGT FLUCTUATING ON THE TAKEOFF ROLL. AIRCRAFT RETURN ED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 06498 IAW MEL 76-1 ON THE SRL SYSTEM. MAINTENANCE LATE R CLEARED DMI NR 06498 ON 3-14-96 BY REPLACING THE LEFT EGT GAUGE AND THE T2 SENSOR CANNON PLUG. PERFORMED OPERATIONAL CHECKS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. REFERENCE VTZA96119. 2 L 7 2 4T 4 T RT A56EU E4WE 1996041800364 19960418 00364 EU 1996 4 18 96ZZZM676 1 19960321 A 2150 1379254L402 ACM DUCT BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP RT WING DISCONNECTED A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 475UE 850 FTL NR 6586 - IAD-ISP - DURING CLIMB-OUT, RETURNED TO IAD DUE TO THE AIRCRAFT NOT PRESSURIZING. AIRCRAFT LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED LEFT P3 LINE AND RECONNECTED RIGHT ACM DUCT. AIRCRAFT WAS RELEASED AND APPROV ED FOR RETURN TO SERVICE. REFERENCE VTZA96129. 2 L 7 2 4T 3 T RT A56EU E3WE 1996041800366 19960418 00366 NM 1996 4 18 96ZZZM678 1 19960304 A 3040 65528038 CONTROLLER BOEING 737 7373S3 1384711 NM LT COCKPIT MALFUNCTIONED A AWXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 28 313AW 2691 23712 LAS - FLT 192 - AIR TURN BACK, CLIMBING THROUGH 18000 MSL, CAPTAINS WINDSHIELD BEGAN ARCING BADLY. THEN HEARD A DISTINC T POP AND IMMEDIATELY NOTICED A LARGE CRACK. REMOVED AND REPLACED LEFT WINDOW PER T/C R1B56001. REPLACED LEFT WINDOW C ONTROLLER PER GPP. REFERENCE AWXA960113. 2 L 7 2 4F RT A16WE 1996041800367 19960418 00367 NE 1996 4 18 96ZZZM679 2 19960311 A 7510 320115 FUEL HEAT VALVE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7B 52053 NE RT ENGINE STUCK OPEN A VJ6A A UNSCHED LANDING M OVER TEMP CR CRUISE 1 SO 11 917VV 47323 ON FLT NR 525 - ATL-DFW - RIGHT ENGINE FUEL HEAT VALVE STUCK IN THE OPEN POSITION. AIRCRAFT RETURNED TO ATL. REMOVED A ND REPLACED ENGINE FUEL HEAT VALVE PER MM 73-10. LEAK CHECK GOOD. (M) 2 L 7 2 4F 4 F A6WE E2EA 1996041800368 19960418 00368 WP 1996 4 18 96ZZZM680 1 19960228 A 3230 39140165503 BUNGEE CYLINDER DOUG DC9 DC932 3022066 WP LT MLG BROKEN A VJ6A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 901VJ 47275 ON FLT 101 - ATL - AIR RETURN, AFTER GEAR RETRACTION THE LEFT GEAR UNSAFE LIGHT STAYED ON AND GEAR DOOR OPEN LIGHT STAYE D ON, CYCLED ONCE, NO CHANGE. FOUND BUNGEE CYCLE PISTON ROD BROKEN. REPLACED PER MM 32-10. ACCOMPLISHED GEAR SWING. ( M) 2 L 7 2 4F A6WE 1996041800369 19960418 00369 WP 1996 4 18 96ZZZM681 1 19960219 A 3520 OXY MASKS DOUG DC9 DC932 3022066 WP CABIN DROPPED A VJ6A A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 SO 11 921VV 47284 ON FLT NR 248 - AIR RETURN, DURING CLIMB-OUT OF ATL IN MANUAL PRESSURE AND CABIN AT 5000 FEET. CLIMBING AT 500 FPM NR 1 FLIGHT ATTENDANT ADVISED THE CREW THAT ALL OXYGEN MASKS HAD DROPPED. NO WARNING FROM THE COCKPIT AND NO CABIN PRESSURE LIGHT. PERFORMED OPERATIONAL CHECK OF MASKS, CLEANED AND RESTOWED MASKS, OPS CHECK GOOD PER MM 35-20-00. (M) 2 L 7 2 4F A6WE 1996041800370 19960418 00370 NE 1996 4 18 96ZZZM682 2 19960306 A 7200 ENGINE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7B 52053 NE NR 1 FAILED A VJ6A E A ENGINE SHUTDOWN UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 SO 11 907VJ 47444 654810 ON FLT NR 236 - DFW - THE LEFT ENGINE FAILED AFTER TAKEOFF. REMOVED AND REPLACED FUEL PUMP AND FUEL CONTROL PER MM 73-0 0, NO HELP. REMOVED AND REPLACED ENGINE PER MM 71-00, OPS CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F 4 F A6WE E2EA 1996041800371 19960418 00371 NE 1996 4 18 96ZZZM683 2 19960306 A 7200 ENGINE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7B 52053 NE LEFT FAILED A VJ6A E A ENGINE SHUTDOWN UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 SO 11 907VJ 47444 654810 ON FLT NR 236 - DFW-DFW - AIR RETURN AFTER TAKEOFF, LEFT ENGINE FAILED. 2 L 7 2 4F 4 F A6WE E2EA 1996041800372 19960418 00372 1996 4 18 96ZZZM684 4 19960315 A 3442 61519 RADAR CONTL PNL DOUG DC9 DC932 3022066 WP CABIN MALFUNCTIONED A VJ6A A UNSCHED LANDING O OTHER CL CLIMB 1 SO 11 918VV 47320 ON FLT NR 270 - ATL - AIR RETURN, WEATHER RADAR INOP. REMOVED AND REPLACED CONTROL PANEL. OPS CHECK NORMAL PER MM 34-4 0. (M) 2 L 7 2 4F A6WE 1996041800373 19960418 00373 SO 1996 4 18 96ZZZM685 1 19960313 A 3230 1159HM201201 ROD END 1159H202623B GULSTM G1159 G1159 3953505 SO NLG FAILED A KKYA O OTHER J WARNING INDICATION AP APPROACH 1 NE 03 220FL 10994 3263 50 AIRCRAFT DEPARTED LGA EN ROUTE TO BDL, ON APPROACH TO BDL THE LANDING GEAR WAS EXTENDED AT 200 KTS, A LOUD BANG EMINATED FROM THE NOSE GEAR WELL. THE NOSE GEAR LIGHT WAS NOT ILLUMINATED AND THE RED LIGHT WAS STILL ON IN THE GEAR HANDLE. E MERGENCY SYSTEM WAS ACTIVATED, RESULTING IN NO CHANGE. AIRCRAFT LANDED AT BDL WITHOUT INCIDENT. UPON INVESTIGATION, IT WAS FOUND THAT THE NOSE GEAR ACTUATOR ROD END HAD CRACKED AND OPENED. THIS ALLOWED THE LANDING GEAR TO FREE FALL, CAUS ING THE DOWN AND LOCK SWITCH MOUNTING BRACKET TO BEND. (M) 2 L 7 2 4F RT A12EA 1996041800374 19960418 00374 NM 1996 4 18 96ZZZM686 1 19960317 A 2910 NAS161216 O-RING BOEING 727 727151C 138404V NM 'A' HYD SYSTEM LEAKING A RYNA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 07 432EX 19867 IN FLIGHT THR NR 1 'A' SYSTEM HYDRAULIC PRESSURE FLUCTUATED AND THE LOW PRESSURE LIGHT ILLUMINATED INTERMITTENTLY. 'A' SYSTEM HYDRAULIC QUANTITY AND PRESSURE WENT TO ZERO. COMPLETED LOSS OF HYDRAULIC CHECK LIST NORMAL LANDING COMPLETED AT IND. FOUND O-RING LEAKING AT ELEVATOR FEEL COMPUTER FILTER ASSY. REMOVED AND REPLACED O-RING. LEAK AND ELEVATOR OPS CHECKS NORMAL PER MM 27-30-91. (M) 2 L 7 3 4F A3WE 1996041800375 19960418 00375 EU 1996 4 18 96ZZZM687 1 19960224 A 7920 AE3663161M0167 FLEX HOSE SAAB SF340 SF340A 7850100 EU LT ENGINE LEAKING A REXA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 25 326PX 340A054 ON TAXI OUT, FLIGHT ATTENDANT REPORTED SMOKE IN CABIN. SHUT DOWN LEFT ENGINE AND DEPLANED PAX. SMOKE CEASED. INSPECTE D LEFT ENGINE, FOUND OIL LEAKING FROM 2 TRANSFER LINES, ON OUTBOARD SIDE OF MIDFRAME CASING UNIONS, TO BOTTOM OF ENGINE BAY. INSTALLED CONICAL SEALS ON BOTH LINES. ALSO, BAGGED DRAIN LINES AND PERFORMED RUN WITH BLEEDS ON, NO SMOKE VISIBL E AND LEAK CHECK GOOD. SUBMITTER STATES, SUSPECT THE LINES LEAKING WERE ACTUALLY THE PGB OIL COOLER HOSES. REFERENCE RE XA96010. 2 L 7 2 4T RT A52EU 1996041800376 19960418 00376 NM 1996 4 18 96ZZZM688 1 19960301 A 2782 1U109592 SLAT ACTUATOR RONSON 10605597 BOEING 727 727231 1384079 NM NR 1 LE SLAT FAILED A MYWA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 808MA 556 4627ABCDEFGH 21988 RETURN FROM FLIGHT, AFTER TAKEOFF AT FLL, NR 1 LE SLAT WOULD NOT RETRACT. CYCLED FLAPS, NO HELP. RETURNED TO FLL. REP LACED THE NR 1 SLAT ACTUATOR IAW MM 27-81-32. OPERATIONAL CHECK GOOD. 2 L 7 3 4F A3WE 1996041800377 19960418 00377 WP 1996 4 18 96ZZZM689 2 19960323 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UAR 01514 WP RIGHT FAILED A NVEA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 03 944AE 944 P66234 FLT NR 4567 - BNA - DURING CRUISE FLIGHT, THE RIGHT ENGINE TORQUE DROPPED TO 20 PERCENT AND THE RPM ROSE TO 120 PERCENT. THE CREW SHUT DOWN THE RIGHT ENGINE, DECLARED AN EMERGENCY AND RETURNED TO BNA WITHOUT INCIDENT. REPLACED ENGINE. (M ) 2 L 7 2 4T 4 T RT A56EU E4WE 1996041800378 19960418 00378 EU 1996 4 18 96ZZZM690 1 19960309 A 3260 SWITCHES SAAB SF340 340B 7860101 EU LANDING GEAR ICED UP A NVEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 03 273AE 340B273 FLT NR 4879 - JFK - CREW REPORTS UNSAFE GEAR LIGHT WHEN GEAR RETRACTED. SAFELY RETURNED TO JFK. REMOVED LARGE AMOUNTS OF ICE FROM LANDING GEAR SWITCHES. (M) 2 L 7 2 4T RT A52EU 1996041800379 19960418 00379 NM 1996 4 18 AALA960388 1 19960310 A 3260 189915 SENSOR ELDEC BOEING 727 727223 1384074 NM RT MLG DEFECTIVE A AALA K NONE N FALSE WARNING CR CRUISE 1 SW 07 896AA 22012 DFW - FLT NR 1089 - EN ROUTE PHL/DFW DURING CRUISE AT FL 310, RIGHT MAIN LANDING GEAR RED WARNING LIGHT ILLUMINATED WITH GEAR HANDLE IN OFF POSITION. CYCLED LANDING GEAR HANDLE TO UP HAD NO EFFECT. AFTER APPROXIMATELY 10 MINUTES, LIGHT EX TINGUISHED AND REMAINED OUT FOR REMAINDER OF FLIGHT. AIRCRAFT PROCEEDED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED R IGHT MAIN LANDING GEAR UPLOCK SENSOR. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996041800380 19960418 00380 WP 1996 4 18 AALA960389 1 19960311 A 3350 LIGHT STRIP DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 480AA 49655 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT STRIP FOUND DISCONNECTED BETWEEN PAX SEAT ROWS 20 AND 21. RESECURED EMERGENCY FLOOR LIGHT STRIP BETWEEN PAX SEAT ROWS 20 AND 21. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996041800381 19960418 00381 1996 4 18 AALA960391 4 19960309 A 2565 29984109 SLIDE AIRCRUISERS DOUG DC9 DC982 3022082 WP AFT FUSELAGE LOW PRESSURE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 466AA A5223 49596 ATL - DURING OVERNIGHT CHECK, TAIL CONE EMERGENCY EVACUATION SLIDE PRESSURE GAUGE INDICATED IN RED (LOW) ZONE. REPLACED TAIL CONE EMERGENCY EVACUATION SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996041800382 19960418 00382 NM 1996 4 18 AALA960392 1 19960321 A 3350 0201820001 LIGHT BOEING 767 767223 1385123 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 329AA 22329 SFO - DURING OVERNIGHT CHECK, EMERGENCY LIGHT ON RIGHT SIDE OF G4 GALLEY BROKEN. REPLACED EMERGENCY LIGHT ON RIGHT SIDE OF G4 GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1996041800383 19960418 00383 NM 1996 4 18 AALA960395 1 19960312 A 3246 WHEEL BEARING BFGOODRICH BOEING 757 757223 1384957 NM NLG FAILED A AALA K NONE D INFLIGHT SEPARATION AP APPROACH 1 SW 07 640A 24598 SNA - FLT NR 1689 - AFTER GATE ARRIVAL, LEFT NOSE WHEEL/TIRE FOUND TO BE MISSING WITH NO ABNORMAL INDICATIONS DURING LAN DING, ROLLOUT OR TAXI. REPLACED LEFT NOSE WHEEL/TIRE ASSEMBLY. ALSO, REPLACED RIGHT NOSE WHEEL/TIRE ASSEMBLY. AIRCRAF T MAINTENANCE FERRY SNA/AFW. REPLACED NOSE LANDING GEAR STRUT INNER CYLINDER ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OP ERATION. (M) 2 L 7 2 4F RT A2NM 1996041800384 19960418 00384 WP 1996 4 18 AALA960396 1 19960313 A 3260 SS092900097003 SWITCH DOUG DC9 DC982 3022082 WP LANDING GEAR DEFECTIVE A AALA K NONE N FALSE WARNING CR CRUISE 1 SW 07 226AA 49176 DFW - FLT NR 1732 - EN ROUTE YYC/DFW DURIGN CRUISE, RED GEAR UNSAFE LIGHT ILLUMINATED WITH NO OTHER ABNORMAL INDICATIONS . AIRCRAFT PROCEEDED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR LEVER SWITCH. ACCOMPLISHED LANDING GEA R RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996041800385 19960418 00385 WP 1996 4 18 AALA960400 1 19960314 A 3222 MS28775015 O-RING DOUG DC9 DC982 3022082 WP NLG STRUT LEAKING A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 271AA 49293 ORD - FLT NR 750 - AFTER TAKEOFF ORD WHEN LANDING GEAR RETRACTED. RED NOSE LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINAT ED. EXTENDED LANDING GEAR AND AIRCRAFT RETURNED TO ORD, LANDING WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR STRUT SCH RADER VALVE O-RING. SERVICED NOSE LANDING GEAR STRUT WITH OIL AND NITROGEN. SYSTEM GROUND CHECKED NORMAL OPERATION. ( M) 2 L 7 2 4F A6WE 1996041800386 19960418 00386 WP 1996 4 18 AALA960402 1 19960315 A 3222 GA70363 SCHRADER VLV DOUG DC9 DC982 3022082 WP NLG STRUT DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 16545 53027 ORD - FLT 1185 - AFTER TAKEOFF ORD WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR DID NOT RETRACT. RECYCLED LANDING GEA R WITH SAME RESULT. EXTENDED LANDING GEAR AND AIRCRAFT RETURNED TO ORD, LANDING WITHOUT INCIDENT. REPLACED NOSE LANDIN G GEAR STRUT SCHRADER VALVE. SERVICED NOSE GEAR STRUT WITH OIL AND NITROGEN. ACCOMPLISHED NOSE LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FUOND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996041800387 19960418 00387 WP 1996 4 18 AALA960404 1 19960315 A 3350 A3060698101 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 286AA 49298 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 17 AND 31 INOPERATIVE. REPLACED BROKEN EMERG ENCY FLOOR LIGHT STRIP CONNECTOR BY PAX SEAT ROW 31. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996041800388 19960418 00388 WP 1996 4 18 AALA960409 1 19960318 A 3230 UPLOCK HOOK DOUG DC9 DC982 3022082 WP LT MLG OUT OF ADJUST A AALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 450AA 49476 FDW - FLT NR 1279 - EN ROUTE MEX/DFW DURIGN CRUISE, LEFT MAIN LANDING GEAR RED LIGHT AND DOOR OPEN LIGHT ILLUMINATED WIT H GEAR HANDLE IN UP POSITION. GEAR DOOR OPEN LIGHT EXTINGUISHED WITH HYDRAULIC PUMPS ON. NO OTHER ABNORMAL INDICATIONS . AIRCRAFT PROCEEDED DFW, LANDING WITHOUT INCIDENT. RIGGED LEFT MAIN LANDING GEAR UPLOCK HOOK. ACCOMPLISHED LANDING G EAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996041800389 19960418 00389 NM 1996 4 18 AALA960410 1 19960318 A 3350 1721651 CONNECTOR BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 355AA 24036 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 21B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 21B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1996041800390 19960418 00390 WP 1996 4 18 AALA960430 1 19960322 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 474 49649 MIA - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS SECTION INOPERATIVE. REPAIRED S PLICE IN EMERGENCY EXIT FLOOR PATH LIGHTING WIRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996041800391 19960418 00391 WP 1996 4 18 AALA960432 1 19960321 A 4930 38303952 FUEL MANIFOLD DOUG DC9 DC982 3022082 WP APU DEFECTIVE A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 271AA 49293 ORD - FLT NR 402 - DURING CRUISE, WITH PACKS ON THERE WAS A STRONG FUEL SMELL IN CABIN. FUEL LEAK AT APU. LANDED ORD W ITHOUT INCIDENT. REPLACED APU MANIFOLD AND PRECAUTIONARY REPLACED BOTH PACK WATER SEPARATOR BAGS. ACCOMPLISHED BURNOUT CHECK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996041800392 19960418 00392 WP 1996 4 18 AALA960448 1 19960322 A 3260 801801 SENSOR ELDEC DOUG DC10 DC1030 3023501 WP NLG DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 137AA 47847 HNL - FLT NR 0005 - AFTER TAKEOFF HNL WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR RED LIGHT REMAINED ILLUMINATED WITH SLIGHT VIBRATION NOTED. RECYCLED LANDING GEAR AND RED LIGHT AGAIN ILLUMINATED WITH NO VIBRATION. EXTENDED LANDING GEA R AND AIRCRAFT RETURNED TO HNL, LANDING WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR DOWNLOCK SENSORS. ACCOMPLISHED BI TE CHECK OF LANDING GEAR PROXIMITY SWITCH CONTROL UNIT AND ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FO UND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A22WE 1996041800393 19960418 00393 WP 1996 4 18 AALA960449 1 19960323 A 3222 STRUT DOUG DC10 DC1030 3023501 WP NLG REQ'D SERV A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 07 137AA 47847 DFW - FLT NR 102 - DURING APPROACH TO DFW, WHEN LANDING GEAR EXTENDED, NOSE LANDING GEAR EXPERIENCED LOUD CLUNK AND RED LIGHT REMAINED ILLUMINATED. RECYCLED LANDING GEAR WITH SAME RESULTS. CONFIRMED NOSE LANDING GEAR DOWN AND LOCKED AND A IRCRAFT LANDED DFW WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR STRUT SEALS AND SERVICED NOSE STRUT WITH OIL AND NITROG EN. ALSO, REPLACED LANDING GEAR PROXIMITY SWITCH CONTROL UNIT. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFE CTS FOUND. SYSTEM CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A22WE 1996041800394 19960418 00394 WP 1996 4 18 AALA960450 1 19960324 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 236AA 49251 ORD - DURING OVERNIGHT CHECK, EMERGENCY EXIT SIGN AT AFT SIGN AT AFT GALLEY DOOR INOPERATIVE. CLEANED AND RESEATED EMER GENCY EXIT SIGN CONNECTOR API-4 AT AFT GALLEY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996041800395 19960418 00395 WP 1996 4 18 AALA960455 1 19960324 A 3350 CONDUCTOR DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 466AA 49596 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT FORWARD PART OF FIRST CLASS CABIN INOPERATIVE. REPLACED EMERGEN CY FLOOR LIGHT FLAT CONDUCTOR WIRE AT FORWARD PART OF FIRST CLASS CABIN. SYSTEM GRUOND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996041800396 19960418 00396 NM 1996 4 18 AWXA960113 1 19960304 A 5610 5893543109 WINDOW BOEING 737 7373S3 1384711 NM LT COCKPIT CRACKED A AWXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 28 313AW 88H0822655 23712 LAS - FLT 192 - AIR TURN BACK, CLIMBING THROUGH 18000 MSL, CAPTAINS WINDSHIELD BEGAN ARCING BADLY. THEN HEARD A DISTINC T POP AND IMMEDIATELY NOTICED A LARGE CRACK. REMOVED AND REPLACED LEFT WINDOW PER T/C R1B56001. REPLACED LEFT WINDOW C ONTROLLER PER GPP. (M) 2 L 7 2 4F RT A16WE 1996041800397 19960418 00397 NM 1996 4 18 AWXA960114 1 19960307 A 2612 894481 FIRE LOOP BOEING 737 7373G7 1384595 NM APU FAILED A AWXA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 28 307AW 20201B1 24634 AUS - FLT 889 - AIR TURN BACK, AFTER TAKEOFF WITH APU RUNNING, APU FIRE WARNING LIGHT ILLUMINATED WITH BELL WARNING. AC COMPLISHED EMERGENCY PROCEDURES, PULLED FIRE HANDLE, DISCHARGED BOTTLE. SWITCH OFF LIGHT STAYED ON. REMOVED AND REPLAC ED MAIN APU FIRE DETECTOR LOOP. REMOVED AND REPLACED FIRE BOTTLE. (M) 2 L 7 2 4F RT A16WE 1996041800398 19960418 00398 NM 1996 4 18 AWXA960119 1 19960309 A 2910 271N63111099 HYD LINE BOEING 757 7572S7 1384962 NM LT PYLON BROKEN A AWXA H DEACTIVATE SYST/CIRCUITS J K WARNING INDICATION FLUID LOSS CR CRUISE 1 WP 28 903AW 23323 LAS - FLT 739 - PILOT REPORTED, THAT EN ROUTE TO LAS THE LEFT HYDRAULIC SYSTEM LOST ALL FLUID AND THE LOW PRESSURE LIGHT ILLUMINATED. LEFT HAND PRESSURE LIGHT ILLUMINATED. LEFT HAND PRESSURE SWITCH IN LEFT HAND PYLON HAS BROKEN LINE. REP LACED WITH NEW LINE. LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 1996041800399 19960418 00399 NM 1996 4 18 AWXA960121 1 19960308 A 5320 SHEAR WEB BOEING 737 7373G7 1384595 NM BS 1006 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 PAE - FLT NR 3861 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CORROSION ON SHEAR WEB STATION 1006, LBL 40, W L 208. REMOVED CORRODED SHEAR WEB, FABRICATED AND INSTALLED NEW SHEAR WEB IAW SRM 51-20-01, 31-10-02, 51-40-02. (M) 2 L 7 2 4F RT A16WE 1996041800400 19960418 00400 NM 1996 4 18 AWXA960123 1 19960308 A 5315 BAC1505100617 FLOOR BEAM BOEING 737 7373G7 1384595 NM BS 967 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 PAE - FLT 3861 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CORROSION ON STATION 967 FLOOR BEAM, LBL 43 TO 49 , WL 208. REMOVED CORROSION AREA FROM STATION 967, LBL 43 TO 49, WL 208 FLOOR BEAM, FABRICATED PART AND INSTALLED. ALO DINED PER SRM 53-00-51, PAGE 207. (M) 2 L 7 2 4F RT A16WE 1996041800401 19960418 00401 NM 1996 4 18 AWXA960124 1 19960308 A 5315 BAC1506100617 FLOOR BEAM BOEING 737 7373G7 1384595 NM BS 9475 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 309AW 24711 PAE - FLT NR 3861 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CORROSION ON STATION 9475 FLOOR BEAM UPPER SUR FACE LBL 21 TO RBL 36, WL 208. REMOVED CORRODED UPPER CHORD, FABRICATED AND INSTALLED REPAIR PIECES IAW SRM 53-00-51, P AGE 202. (M) 2 L 7 2 4F RT A16WE 1996041800402 19960418 00402 NM 1996 4 18 AWXA960130 1 19960313 A 2121 731376 COOLING FAN BOEING 757 7572S7 1384962 NM E/E BAY FAILED A AWXA K NONE J WARNING INDICATION CR CRUISE 1 WP 28 905AW 40130 284 23567 CMH - FLT 820 - SMELLED ELECTRICAL BURNING ODOR AT CRUISE. FIFTEEN MINUTES LATER, EICAS MESSAGE EQUIPMENT COOLING FAN D ISPLAYED. REMOVED AND REPLACED ALTERNATE EQUIPMENT COOLING FAN. (M) 2 L 7 2 4F RT A2NM 1996041800403 19960418 00403 NM 1996 4 18 AWXA960132 1 19960312 A 5610 SEALANT BOEING 737 7372M8 1384483 NM NR 1 WINDOW FAILED A AWXA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 28 141AW 21955 FLT NR 510 - PHX-OMA - AIR TURN BACK, WINDOW NR 1 REPAIR TAPE AND SEALANT BLEW OUT PASSING THROUGH 230K. PRESSURIZATION OK, BUT WINDOW SCREEN WIND NOISE OUITE BAD. RETORQUED AND RESEALED PER 56-11-11, CLEARED DMI 56956, MAINTENANCE CONTRO L NOTIFIED. (M) 2 L 7 2 4F A16WE 1996041800404 19960418 00404 NM 1996 4 18 AWXA960136 1 19960316 A 5610 5893543030 WINDSHIELD BOEING 737 737301 1384611 NM RT COCKPIT LEAKING A AWXA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 28 325AW 33824 91228H6383 23260 LAS-SNA - AIR TURN BACK, EXTREMELY LOUD WING NOISE NEAR FIRST OFFICERS WINDOWN. REMOVED AND REPLACED FIRST OFFICERS NR 1 WINDOW IAW CARD R1BS6001. LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996041800405 19960418 00405 1996 4 18 AWXA960137 4 19960318 A 2565 D31039202 DOOR SLIDE BOEING 757 7572S7 1384962 NM L-2 DOOR FELL OFF A AWXA K NONE O OTHER CR CRUISE 1 WP 28 902AW 14665 370 23322 LAS - FLT 292 - L-2 SLIDE FELL OFF DURING FLIGHT. REHUNG L-2 DOOR SLIDE. (M) 2 L 7 2 4F RT A2NM 1996041800406 19960418 00406 NM 1996 4 18 AWXA960155 1 19960321 A 2433 60B400232 STATIC INVERTER BOEING 737 7372M8 1384483 NM NR 1 FAILED A AWXA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 28 141AW 1776 21955 LAS - FLT NR 1931 - AIR TURN BACK, AFTER TAKEOFF LOST NAVIGATION AND COMMUNICATION ON CAPTAINS SIDE. REMOVED AND REPLAC ED STATIC INVERTER AND R-36 RELAY IN P-6. CHANGED R-37 AS A PRECAUTION. (M) 2 L 7 2 4F A16WE 1996041800407 19960418 00407 NM 1996 4 18 AWXA960158 1 19960325 A 2761 65449616 ACTUATOR BOEING 737 7372M8 1384483 NM NR 8 SPOILER BROKEN A AWXA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 WP 28 141AW 1481 21955 TUS-PHX - FLT NR 604 - GATE RETURN, A SYSTEM HYDRAULIC FAILURE DURING TAXI. NR 8 SPOILER ACTUATOR BROKEN AT CASTING. R EPLACED NR 8 SPOILER ACTUATOR PER CARD R3M27016. LEAK AND OPERATION CHECK GOOD. (M) 2 L 7 2 4F A16WE 1996041800408 19960418 00408 NM 1996 4 18 AWXA960160 1 19960329 A 2910 O-RING BOEING 737 737277 1384570 NM NR 4 SPOILER BLOWN A AWXA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CL CLIMB 1 WP 28 186AW 22653 PHX-TUS - FLT 606 - AIR TURN BACK, SHORTLY AFTER GEAR RETRACTION, 'B' SYSTEM HYDRAULIC QUANTITY DROPPED TO 1 GALLON AND HELD. SHUT OFF 'B' SYSTEM. FOUND NR 1 SPOILER PRESSURE RELIEF CAP O-RING BLOWN OUT. REPLACED O-RING, SERVICED HYDRAUL ICS. FUNCTION CHECKED GOOD, OPERATES NORMAL. (M) 2 L 7 2 4F RT A16WE 1996041800409 19960418 00409 SO 1996 4 18 C2XA96IA065 1 19960315 A 3231 MS203921C55 PIN EMB 120 EMB120RT SO LT MLG BENT A C2XA K NONE O OTHER AP APPROACH 1 SW 09 57734 120199 IAH - FLT NR 2582 - DURING APPROACH TO IAH, WHEN LANDING GEAR WAS SELECTED DOWN, LEFT MLG FORWARD DOOR REMAINED OPEN. A IRCRAFT LANDED WITHOUT INCIDENT. INSPECTED AND FOUND GEAR DOOR MAINTENANCE SAFETY LATCH NOT SECURED. PROBLEM WAS CAUSE D BY A BENT CATCH PIN FOR SAFETY LATCH. MAINTENANCE REPLACED CATCH PIN AND PERFORMED OPERATIONAL CHECK. AIRCRAFT WAS A PPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996041800410 19960418 00410 EU 1996 4 18 C2XA96IA066 1 19960315 A 3297 WIRE AEROSP ATR42 ATR42320 8680930 EU LANDING GEAR CHAFED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 17831 185 IAH - FLT NR 2797 - AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT, FOUND CONTROL CIRCUIT BREAKER OUT. CREW COULD NOT RE SET CIRCUIT BREAKER, A/C RETURNED TO IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL LEVER, PROBLEM WAS NOT FIXED, DESCREPANCY WAS DEFFERED PER COEX MEL MANUAL. ON 3-17-96 MAINTENANCE TROUBLE SHOT LANDING GEAR CONTROL SYSTEM AND FOUND A WIRE TO BE CHAFED ADJACENT TO LANDING GEAR CONTROL VALVE. WIRE HARNESS WAS REPAIRED AND OPER ATIONAL TESTS WERE PERFORMED, AIRCRAFT WAS RELEASED FOR A TEST FLIGHT AS A PRECAUTIONARY MEASURE, ALL CHECKS WERE SATISF ACTORY. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996041800411 19960418 00411 EU 1996 4 18 C2XA96IA067 1 19960319 A 5753 S5751065000200 FITTING AEROSP ATR42 ATR42320 8680930 EU LT TE FLAP WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14830 184 IAH - DURING INSPECTION CHECK 6C, LEFT INBOARD FLAP WAS FOUND TO HAVE PLAY AT CENTER ATTACHMENT BRACKET LOWER ATTACH BOL T. MAINTENANCE REMOVED FITTING, CLEANED HOLE AND REAMED TO OVERSIZE .590 INCH. A BUSHING WAS INSTALLED, AFFECTED AREA WAS ALODINED, PRIMED AND PAINTED, AND ATTACHMENT FITTING WAS REINSTALLED. ALL WORK WAS PERFORMED IAW COEX EC 5750-01083 . (M) 2 H 7 2 4T RT A53EU 1996041800412 19960418 00412 EU 1996 4 18 C2XA96IA068 1 19960319 A 5320 S53371226220 THRESHOLD AEROSP ATR42 ATR42320 8680930 EU CARGO COMPT CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14830 184 IAH - DURING INSPECTION CHECK 6C, FORWARD CARGO COMPARTMENT DOORWAY THRESHOLD WEB WAS FOUND TO BE CORRODED BEYOND MANUFA CTURERS LIMITS. MAINTENANCE REMOVED AND REPLACED THRESHOLD SUPPORT PLATE, DRAIN CHANNEL AND THRESHOLD WEB. (M) 2 H 7 2 4T RT A53EU 1996041800413 19960418 00413 EU 1996 4 18 C2XA96IA069 1 19960319 A 3350 3011206 LIGHT AEROSP ATR42 ATR42320 8680930 EU RT FUSELAGE INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14830 296 184 IAH - DURING INSPECTION CHECK 6C, EXTERIOR EMERGENCY GROUND ILLUMINATION LIGHT FAILED TO OPERATE. MAINTENANCE REMOVED A ND REPLACED RIGHT AFT GROUND ILLUMINATION LIGHT ASSEMBLY, OPERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1996041800414 19960418 00414 EU 1996 4 18 C2XA96IA070 1 19960319 A 2761 S2711010900101 ACTUATOR SUPPORT AEROSP ATR42 ATR42320 8680930 EU LT SPOILER WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14830 184 IAH - DURING INSPECTION CHECK 6C, LEFT AILERON TRIM TAB ACTUATOR WAS FOUND TO HAVE EXCESSIVE PLAY. INSPECTED AND FOUND ACTUATOR SUPPORT BRACKET WORN AT ATTACHMENT POINTS. MAINTENANCE REMOVED AND REPLACED SUPPORT BRACKET, PERFORMED DEFLECT ION AND OPERATIONAL CHECKS, ALL CHECKS GOOD. (M) 2 H 7 2 4T RT A53EU 1996041800415 19960418 00415 EU 1996 4 18 C2XA96IA071 1 19960318 A 2910 HYD SYSTEM AEROSP ATR42 ATR42320 8680930 EU GREEN HYD SYS REQ'D SERVICE A C2XA O OTHER J WARNING INDICATION DE DESCENT 1 SW 09 27806 075 IAH - FLT NR 2594 - DURING DESCENT, PILOT REPORTED THAT THE GREEN HDYRAULIC SYSTEM LOW PRESSURE LIGHT ILLUMINATED IN FLI GHT. PRESSURE DROPPED TO ZERO, ATTEMPTED ONE RESET UNSUCCESSFULLY, PERFORMED MANUAL GEAR EXTENSION AND THE AIRCRAFT LAN DED WITHOUT INCIDENT. MAINTENANCE SERVICED THE HYDRAULIC SYSTEM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ( M) 2 H 7 2 4T RT A53EU 1996041800416 19960418 00416 EU 1996 4 18 C2XA96IA072 1 19960319 A 3350 202 CONNECTOR 1011309111 AEROSP ATR42 ATR42320 8680930 EU CABIN FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14830 184 IAH - INSPECTION CHECK 6C, UPON REMOVAL OF AISLE PATH FLOOR EMERGENCY LIGHTING AFT SECTION, A BROKEN WIRE WAS DETECTED A T LIGHTING STRIP ELECTRICAL CONNECTOR. MAINTENANCE REPLACED CONNECTOR PIN AND REINSTALLED IN CONNECTOR ASSY. PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED. (M) 2 H 7 2 4T RT A53EU 1996041800417 19960418 00417 EU 1996 4 18 C2XA96IA074 1 19960320 A 2711 48635028010 TRIM INDICATOR AEROSP ATR42 ATR42320 8680930 EU COCKPIT MALFUNCTIONED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 18814 264 103 IAH - INSPECTION CHECK 6C, WITH AILERON TRIM ACTUATOR AT ITS ELECTRICAL ZERO POSITION, COCKPIT TRIM POSITION INDICATOR S HOWED LEFT WING UP CONDITION. MAINTENANCE REMOVED AND REPLACED TRIM POSITION INDICATOR, OPERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1996041800418 19960418 00418 EU 1996 4 18 C2XA96IA075 1 19960320 A 2730 E0242A28A0 RELAY AEROSP ATR42 ATR42320 8680930 EU PITCH/TRIM FAILED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 18814 103 IAH - INSPECTION CHECK 6C, DURING ROUTINE CHECK OF PITCH TRIM SYSTEM, TRIM ACTUATORS COULD BE OPERATED USING LEFT HALF O F TRIM SWITCH AT CAPTAIN AND F/O'S CONTROL COLUMNS. INSPECTED AND FOUND RELAY NR 23CG FAULTING. REMOVED AND REPLACED R ELAY, OPERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1996041800419 19960418 00419 EU 1996 4 18 C2XA96IA076 1 19960320 A 2730 E0237E9S02B CONNECTOR AEROSP ATR42 ATR42320 8680930 EU F/O CONTL COL DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 18814 103 IAH - INSPECTION CHECK 6C - DURING ROUTINE CHECK OF PITCH TRIM SYSTEM, TRIM ACTUATORS COULD BE OPERATED USING LEFT HALF OF TRIM SWITCH AT CAPTAIN AND FLIGHT OFFICERS CONTROL COLUMNS. INSPECTED AND FOUND A BROKEN WIRE AT PIN NR 5 OF CONNECT OR LOCATED INSIDE FLIGHT OFFICER'S CONTROL YOKE. REPAIRED WIRE AT CONTROL YOKE CONNECTOR, OPERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1996041800420 19960418 00420 EU 1996 4 18 C2XA96IA078 1 19960322 A 5720 MS2125005016 BOLT AEROSP ATR42 ATR42300 8680920 EU LT WING NOT SEALED A C2XA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 09 16824 166 IAH - DURING C-CHECK INSPECTION, THE LEFT ENGINE, INBOARD LOWER MOUNT BOLTS WERE FOUND TO BE LEAKING FUEL. MAINTENANCE REMOVED THE CENTER WING PLANK, REF ATR MM JIC 57-14-12, INSPECTED THE BOLT HOLES, REPLACED THE LOWER TWO BOLTS, AND RESE ALED THE BOLTS ON INSTALLATION. THE AIRCRAFT LEAK CHECKED GOOD AND WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996041800421 19960418 00421 WP 1996 4 18 CAL960279 1 19960227 A 5542 SKIN DOUG DC9 DC932 3022066 WP RUDDER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12532 67873 45791 HOU - INSPECTION FOUND A 4.5 INCH CRACK IN LEFT UPPER RUDDER SKIN. THE CRACKED AREA WAS ROUTED OUT. A FILLER AND DOUBL ER REPAIR WERE FABRICATED AND INSTALLED IAW SRM 55-03. (M) 2 L 7 2 4F A6WE 1996041800422 19960418 00422 NM 1996 4 18 CAL960308 1 19960313 A 2913 6507506 HYD PUMP BOEING 737 7373T0 1384582 NM NR 1 ENG LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 14347 6058 23585 FLT NR 784 - IAH - THE 'A HYDRAULIC SYSTEM QUANTITY DROPPED TO ONE FOURTH AFTER DEPARTING ATL. THE NR 1 ENGINE LOW PRES SURE LIGHT FLICKERED ON AND OFF WHILE AT CRUISE. CHECKLIST PROCEDURES WERE COMPLIED WITH AND THE 'A' SYSTEM ENGINE PUMP WAS TURNED OFF. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP LEAKING. THE PUMP WAS REMOVED AND REPLACED. THE HYDRAULIC SYSTEM WAS SERVICED AND NO LEAKS WERE NOTED DURING ENGINE RUN. (M) 2 L 7 2 4F RT A16WE 1996041800423 19960418 00423 NM 1996 4 18 CAL960309 1 19960313 A 3397 WIRE BOEING 737 737217 1384464 NM CABIN SHORTED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 12230 19884 FLT NR 1087 - EWR - THE CREW NOTICED APPROXIMATELY ONE THIRD OF THE EMERGENCY PATH LIGHTING SYSTEM WAS INOPERATIVE AFTER LOSING GROUND POWER. MAINTENANCE FOUND SHORTED WIRING BY ROW 4 WITH ASSOCIATED FUSES BLOWN. THE WIRING WAS REPAIRED A ND THE FUSES WERE REPLACED. (M) 2 L 7 2 4F A16WE 1996041800424 19960418 00424 WP 1996 4 18 CAL960310 1 19960314 A 3260 7000010101 UPLOCK SWITCH DOUG DC9 DC932 3022066 WP NLG INOPERATIVE A CALA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 SW 09 12507 47788 FLT NR 1147 - CLE - THE NLG WARNING LIGHTS DID NOT INDICATE GREEN OR RED WHEN GEAR WAS EXTENDED ON APPROACH TO CLE. THE GEAR WAS RECYCLED DURING A GO-AROUND AND THE NOSE GEAR INDICATIONS WERE NORMAL. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR UPLOCK SWITCH AT FAULT. THE SWITCH WAS REMOVED AND REPLACED. GEAR OPERATION AND INDIC ATIONS CHECKED GOOD. (M) 2 L 7 2 4F A6WE 1996041800425 19960418 00425 WP 1996 4 18 CAL960311 1 19960227 A 5320 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP STATION 1811 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68041 76758 46900 KUL - INSPECTION FOUND FLOOR SUPPORT BEAM CORRODED ON RIGHT SIDE NEAR DOOR R-4, STATION 1811. THE BEAM WAS REPLACED IAW SRM 51-31-01 AND 53-24-15, FIGURE 4, ITEM 85. (M) 2 L 7 3 4F A22WE 1996041800426 19960418 00426 WP 1996 4 18 CAL960312 1 19960229 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 1786 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68041 76758 46900 KUL - INSPECTION FOUND LONGERON 38R AND 39R CORRODED AT STATION 1786. THE AREA WAS REPAIRED IAW SRM 53-20-00. (M) 2 L 7 3 4F A22WE 1996041800427 19960418 00427 WP 1996 4 18 CAL960313 1 19960221 A 5320 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP REAR GALLEY 2B CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68041 76758 46900 KUL - INSPECTION FUOND THE REAR GALLEY 2B INBOARD FLOOR SUPPORT BEAM CORRODED. THE BEAM WAS REPLACED IAW SRM 53-60-07, FIGURE 1. (M) 2 L 7 3 4F A22WE 1996041800428 19960418 00428 WP 1996 4 18 CAL960314 1 19960221 A 5320 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP REAR GALLEY 2A CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68041 76758 46900 KUL - INSPECTION FOUND REAR GALLEY 2A OUTBOARD FLOOR SUPPORT BEAM CORRODED. THE BEAM WAS REPLACED IAW SRM 53-60-07, FIG URE 1. (M) 2 L 7 3 4F A22WE 1996041800429 19960418 00429 WP 1996 4 18 CAL960315 1 19960219 A 5754 SKIN DOUG DC10 DC1010 3022110 WP NR 1 SLAT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68041 76758 46900 KUL - INSPECTION FOUND INNER SKIN OF NR 1 SLAT CORRODED AROUND TRACK FITTING NR 1 AND NR 2. THE SLAT SKIN WAS REPAIRED IAW SRM 57-10-00, FIGURE 31. (M) 2 L 7 3 4F A22WE 1996041800430 19960418 00430 WP 1996 4 18 CAL960316 1 19960218 A 5720 FORMER DOUG DC10 DC1010 3022110 WP WS 709 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68041 76758 46900 KUL - INSPECTION FOUND A 1 INCH CRACK IN WING LEADING EDGE FORMER AT STATION XOS 709. THE FORMER WAS REPAIRED IAW SRM 5 7-20-00, FIGURE 1. (M) 2 L 7 3 4F A22WE 1996041800431 19960418 00431 WP 1996 4 18 CAL960317 1 19960218 A 5720 FORMER DOUG DC10 DC1010 3022110 WP WS 873 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68041 76758 46900 KUL - INSPECTION FOUND A .75 INCH CRACK IN WING LEADING EDGE FORMER AT STATION XOS 873. THE FORMER WAS REPAIRED IAW SRM 57-20-00, FIGURE 1. (M) 2 L 7 3 4F A22WE 1996041800432 19960418 00432 WP 1996 4 18 CAL960318 1 19960218 A 5720 FORMER DOUG DC10 DC1010 3022110 WP WS 879 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68041 76758 46900 KUL - INSPECTION FOUND A 1 INCH CRACK IN WING LEADING EDGE FORMER AT STATION XOS 879. THE FORMER WAS REPAIRED IAW SRM 5 7-20-00, FIGURE 1. (M) 2 L 7 3 4F A22WE 1996041800433 19960418 00433 WP 1996 4 18 CAL960319 1 19960218 A 5720 FORMER DOUG DC10 DC1010 3022110 WP WS 862 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68041 76758 46900 KUL - INSPECTION FOUND A .5 INCH CRACK IN WING LEADING EDGE FORMER AT STATION XOS 862. THE FORMER WAS REPAIRED IAW SRM 57-20-00, FIGURE 1. (M) 2 L 7 3 4F A22WE 1996041800434 19960418 00434 WP 1996 4 18 CAL960320 1 19960218 A 5720 FORMER DOUG DC10 DC1010 3022110 WP WS 928 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68041 76758 46900 KUL - INSPECTION FUND A 1 INCH CRACK IN WING LEADING EDGE FORMER AT STATION XOS 928. THE FORMER WAS REPAIRED IAW SRM 57 -20-00, FIGURE 1. (M) 2 L 7 3 4F A22WE 1996041800435 19960418 00435 WP 1996 4 18 CAL960321 1 19960218 A 5720 FORMER DOUG DC10 DC1010 3022110 WP WS 987 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68041 76758 46900 KUL - INSPECTION FOUND A 1 INCH CRACK IN WING LEADING EDGE FORMER AT STATION XOS 987. THE FORMER WAS REPAIRED IAW SRM 5 7-20-00, FIGURE 1. (M) 2 L 7 3 4F A22WE 1996041800436 19960418 00436 WP 1996 4 18 CAL960322 1 19960218 A 5720 FORMER DOUG DC10 DC1010 3022110 WP WS 981 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68041 76758 46900 KUL - INSPECTION FUOND A .75 INCH CRACK IN WING LEADING EDGE FORMER AT STATION XOS 981. THE FORMER WAS REPAIRED IAW SRM 57-20-00, FIGURE 1. (M) 2 L 7 3 4F A22WE 1996041800437 19960418 00437 WP 1996 4 18 CAL960323 1 19960218 A 5720 FORMER DOUG DC10 DC1010 3022110 WP WS 867 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68041 76758 46900 KUL - INSPECTION FOUND A .5 INCH CRACK IN WING LEADING EDGE FORMER AT STATION XOS 867. THE FORMER WAS REPAIRED IAW SRM 57-20-00, FIGURE 1. (M) 2 L 7 3 4F A22WE 1996041800438 19960418 00438 WP 1996 4 18 CAL960324 1 19960223 A 5320 BRACKET DOUG DC10 DC1010 3022110 WP BS 999 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68041 76758 46900 KUL - INSPECTION FOUND THE FLOOR SUPPORT BRACKET CORRODED AT DOOR SILL, STATION 999. THE FLOOR SUPPORT BRACKET WAS REPL ACED IAW SRM 51-13-01. (M) 2 L 7 3 4F A22WE 1996041800439 19960418 00439 WP 1996 4 18 CAL960325 1 19960315 A 2120 AIR DISTR DOUG DC9 DC982 3022082 WP CABIN SMOKE A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 09 819NY 49479 FLT NR 1623 - CLE - SMOKE APPEARED IN THE CABIN AND COCKPIT ON FINAL APPROACH TO CLE. MAINTENANCE REPLACED BOTH WATER S EPARATOR BAGS AND NOTED PACK DUCTING WAS DRY OF FLUID. THE ENGINE SADDLE DUCTS WERE INSPECTED FOR OIL AND NONE WAS FOUN D. THE GEAR WAS PINNED AND THE GEAR HANDLE, FLAPS, AND THRUST REVERSER WWERE CYCLED SEVERAL TIMES WITH NO LEAKS NOTED. A HIGH POWER RUN WAS CONDUCTED WHILE THE AIR CONDITIONING SYSTEM WAS CYCLED HOT AND COLD SEVERAL TIMES OVER A PERIOD OF ABOUT ONE HOUR. NO INDICATIONS OF SMOKE OR SMELL WERE FOUND. THE ANOMALY COULD NOT BE DUPLICATED. (M) 2 L 7 2 4F A6WE 1996041800440 19960418 00440 WP 1996 4 18 CAL960328 1 19960312 A 2560 3753213143 LANYARD DOUG DC9 DC932 3022066 WP SERVICE DOOR FRAYED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19504 47638 HOU - INSPECTION FOUND THE FORWARD SERVICE DOOR SLIDE LANYARD CABLE FRAYED. THE LANYARD WAS REMOVED AND REPLACED. (M) 2 L 7 2 4F A6WE 1996041800441 19960418 00441 WP 1996 4 18 CAL960329 1 19960307 A 5210 BEAM DOUG DC9 DC932 3022066 WP MAIN CABIN DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19504 55486 47638 HOU - INSPECTION FOUND A .5 INCH CRACK NR 5 BEAM OF MAIN CABIN DOOR. THE CRACK WAS STOP DRILLED. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 31, SHEET 6. (M) 2 L 7 2 4F A6WE 1996041800442 19960418 00442 WP 1996 4 18 CAL960330 1 19960307 A 5210 BEAM DOUG DC9 DC932 3022066 WP MAIN CABIN DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19504 55486 47638 INSPECTION FOUND A .5 INCH CRACK IN NR 8 BEAM OF MAIN CABIN DOOR. A REPAIR WAS INSTALLED IAW SRM 52-05, FIGURE 31, SHEE T 9. (M) 2 L 7 2 4F A6WE 1996041800443 19960418 00443 WP 1996 4 18 CAL960331 1 19960308 A 5753 SPAR CAP DOUG DC9 DC932 3022066 WP RT TE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19504 55486 47638 HOU - INSPECTION FUOND A 1.5 INCH CRACK IN RIGHT FLAP SPAR CAP AT INBOARD ATTACH FITTING, OUTBOARD FIXED VANE. THE CRAC KED AREA WAS CUT OUT. REPAIR DOUBLERS WERE INSTALLED IAW ECRA 5710-01719 AND SRM 57-01. (M) 2 L 7 2 4F A6WE 1996041800444 19960418 00444 WP 1996 4 18 CAL960332 1 19960303 A 5312 991150985 BLKHD T-CAP DOUG DC9 DC932 3022066 WP BS 110 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19504 55486 47638 HOU - INSPECTION FOUND T-CAP CORRODED AT AFT BULKHEAD STATION 110 IN NLG WHEEL WELL RIGHT TUNNEL. THE CORROSION WAS REM OVED AND THE AREA WAS TREATED IAW SRM 51-10-3. (M) 2 L 7 2 4F A6WE 1996041800445 19960418 00445 WP 1996 4 18 HALA9628 1 19960321 A 2780 S4913801GF06614 CONTROL CABLE DOUG DC9 DC951 3022051 WP NR 1 LE SLAT BROKEN A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 709HA 47764 HNL - OVERNIGHT CHECK, FOUND NR 1 RIGHT SLAT NOT FULLY EXTENDED, FOUND DEFECTIVE CABLE, NR 2 RIGHT SLAT DAMAGED INBOARD END AND RIGHT WING L/E CAP DAMAGED OUTBOARD OF NR 3 SLAT TRACK. REPAIRED WING L/E CAP AND NR 2 SLAT, REPLACED SLAT CARR IAGE ASSY AND NR 1 SLAT CABLES PER MM 27-80-02. OPERATIONAL CHECK OK. (M) 2 L 7 2 4F RT A6WE 1996041800446 19960418 00446 WP 1996 4 18 IXXA9619 1 19960226 A 5330 SKIN DOUG DC8 DC871 302199A WP FS 505 GOUGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 71231 22629 46065 DURING D-CHECK INSPECTION, GOUGED AREA WAS FOUND AT 'B' PIT DOOR JAMB AT FS NR 505, L31 RT. REPAIR WAS ACCOMPLISHED BY INSTALLING FILLER AND DOUBLER PER DRAWING NR CF-N820BX, 11/96, DATED 1/27/96. THIS DRAWING IS APPROVED UNDER DACO SRM A ND MAINTENANCE MANUAL AND GRANTED APPROVAL BY FAA FORM 8110-3. (M) 2 L 7 4 4F 4A25 1996041800447 19960418 00447 WP 1996 4 18 IXXA9620 1 19960226 A 5330 SKIN DOUG DC8 DC871 302199A WP FS 360-380 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 22629 46065 DURING THE D-CHECK INSPECTION, FOUND CRACK AT FS NR 360 TO 380, L30 RT. REPAIR WAS ACCOMPLISHED PER DRAWING CF-N820BX-3 /96, DATED 1/9/96. THIS REPAIR WAS PERFORMED IAW DACO SRM AND MAINTENANCE MANUALS AND APPROVED ON FAA FORM 8110-3 DATED 1/31/96. (M) 2 L 7 4 4F 4A25 1996041800448 19960418 00448 WP 1996 4 18 IXXA9621 1 19960226 A 5510 37014272 FITTING DOUG DC8 DC871 302199A WP HORIZ STAB CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 71231 46065 DURING THE D-CHECK INSPECTION, FOUND CRACKED FITTING ON THE RIGHT HORIZONTAL STABILIZER L/E AT FS XFS 47. FITTING WAS M ANUFACTURED PER DRAWING CF-N820BX-15/96, DATED 2/9/96 AND WAS APPROVED BY FAA FORM 8110-3 DATED 2/20/96. (M) 2 L 7 4 4F 4A25 1996041800449 19960418 00449 WP 1996 4 18 IXXA9622 1 19960226 A 7110 COWLING DOUG DC8 DC871 302199A WP ENGINE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 71231 46065 DURING THE D-CHECK INSPECTION, FOUND CRACK ON THE INBOARD COWL ON ENGINE. REPAIR WAS ACCOMPLISHED PER DRAWING CF-N820BX , 10/96 DATED 1/18/96. REPAIR WAS APPROVED ON FAA FORM 8110-3 DATED 1/25/96. (M) 2 L 7 4 4F 4A25 1996041800450 19960418 00450 WP 1996 4 18 IXXA9623 1 19960226 A 5320 JAMB DOUG DC8 DC871 302199A WP FS 250 DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 71231 46065 DURING THE D-CHECK INSPECTION, FOUND DENTS AND SCRATCHES AT FWD CARGO DOOR UPPER DOOR JAMB OF 'A' PIT AT FS NR 250. REP AIR WAS ACCOMPLISHED PER DRAWING CF-N820BX-11/96 DATED 1/27/96 AND APPROVED ON FAA FORM 8110-3 DATED 2/2/96. (M) 2 L 7 4 4F 4A25 1996041800451 19960418 00451 WP 1996 4 18 IXXA9624 1 19960226 A 5753 SKIN DOUG DC8 DC871 302199A WP RT TE FLAP CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 71231 22629 46065 DURING THE D-CHECK INSPECTION, FOUND DAMAGE ON RIGHT LOWER FLAP AT FS NR 215. REPAIR WAS ACCOMPLISHED BY INSTALLING NEW SKIN PANEL PER DRAWING CF-N820BX, 2/96 DATED 1/6/96 AND WAS APPROVED BY FAA FORM 8110-3 DATED. (M) 2 L 7 4 4F 4A25 1996041800452 19960418 00452 WP 1996 4 18 IXXA9625 1 19960226 A 5720 LE FORMERS DOUG DC8 DC871 302199A WP LT WING CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 820BX 71231 22629 46065 DURING THE D-CHECK INSPECTION, FOUND TWO CRACKED FORMERS AT FS NR 422. REPAIR WAS ACCOMPLISHED PER DACO SRM 57-3-1 AND 57-0 CODE 5 AND DRAWING CF-N820, 7/96 DATED 1/18/96 WHICH HAS APPROVAL ON FAA FORM 8110-3 DATED 1/22/96. (M) 2 L 7 4 4F 4A25 1996041800453 19960418 00453 WP 1996 4 18 IXXA9636 1 19960312 A 5260 PROX SWITCH DOUG DC8 DC862 3021970 WP MLG DOORS DIRTY A IXXA O OTHER N FALSE WARNING CL CLIMB 1 SW 11 21CX 45955 ON TAKEOFF OUT OF BGTL, THE MLG 'NOT LATCHED' LIGHT CAME ON AFTER GEAR RETRACTION. THE GEAR WAS CYCLED, WITH NO CHANGE IN THE INDICATION. THE UPLATCH CHECK WAS NORMAL. AT KWRI, MAINTENANCE INSPECTED THE AIRCRAFT AND DETERMINED THE PROBLE M TO BE CAUSED BY DIRTY GEAR DOOR PROXIMITY SWITCHES. THE SWITCHES WERE CLEANED, THE DOOR UPLATCH ASSEMBLY PRECAUTIONAR ILY LUBRICATED, AND OPS CHECKS ACCOMPLISHED IAW THE DC-8 MM. DOOR INDICATION RETURNED TO NORMAL OPERATION, AND THE AIRC RAFT WAS RETURNED TO SERVICE. (M) 2 L 7 4 4F 4A25 1996041800454 19960418 00454 WP 1996 4 18 IXXA9637 1 19960318 A 3231 UPLATCH DOUG DC8 DC862F 3021972 WP LT/RT MLG DOOR LACK OF LUBE A IXXA O OTHER N FALSE WARNING CL CLIMB 1 SW 11 41CX 46129 ON DEPARTURE OUT OF RODN, THE GEAR DOOR 'NOT LATCHED' LIGHT ILLUMINATED. THE LANDING GEAR WAS CYCLED, AND THE WARNING L IGHT EXTINGUISHED. IN RJTY, MAINTENANCE CLEANED THE MLG DOOR UPLATCH SWITCHES, CLEANED AND LUBRICATED THE MLG DOOR UPLA TCH ROLLERS IAW THE DC-8 MM. THE INDICATION AND DOOR UPLOCK OPERATION WERE NORMAL, AND THE AIRCRAFT WAS RETURNED TO SER VICE. (M) 2 L 7 4 4F 4A25 1996041800456 19960418 00456 WP 1996 4 18 IXXA9640 1 19960326 A 3230 27735101 BOLT DOUG DC8 DC862 3021970 WP RT MLG BROKEN A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 728PL 45918 ON TAKEOFF OUT OF PHIK, AFTER LANDING GEAR RETRACTION, BOTH THE MLG DOOR NOT LATCHED LIGHT AND THE GEAR NOT LATCHED LIGH T STAYED ON. AFTER SEVERAL GEAR CYCLES, THE GEAR UPLATCHED. THE AIRCRAFT RETURNED TO PHIK, WHERE MAINTENANCE INSPECTED THE LANDING GEAR AND FOUND THAT THE FORWARD BOLT ON THE RIGHT BOGIE TRIM CYLINDER HAD BROKEN. THE BOLT WAS REPLACED IA W THE DC-8 MM, AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 4 4F 4A25 1996041800457 19960418 00457 WP 1996 4 18 IXXA9646 1 19960328 A 3240 BRAKES DOUG DC8 DC871 302199A WP NR 5 LOOKED UP A IXXA O OTHER O OTHER LD LANDING 1 SW 11 823BX 46064 DURING LANDING AT BOS, THE NR 5 BRAKE EXPERIENCED SHINGLED LININGS, CAUSING THE BRAKE TO LOCK UP AND BLOW THE NR 5 MAIN TIRE. THE NR 5 BRAKE AND MAIN TIRE WERE REPLACED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. THE NR 6 MAIN TIRE CHANGE WAS CARRIED OVER TO THE NEXT STATION IAW THE ATI DC-8 MM PAGE 15-10. THE CAUSE OF THE LINING FAILURE TO BE DETERMINED I N THE SHOP. (M) 2 L 7 4 4F 4A25 1996041800458 19960418 00458 SW 1996 4 18 MALA964908 1 19960301 A 5400 ANGLE SWRNGN SA227 SA227AC 8780603 SW WING/NACELLE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 158MC AC726B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE LEFT LOWER INBOARD WING SKIN TO NACELLE ATTACH ANGLE. THEY STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW FAC ARP 54-20-9101. (M) 2 L 7 2 4T RT A8SW 1996041800459 19960418 00459 SW 1996 4 18 MALA964909 1 19960301 A 5400 ANGLE SWRNGN SA227 SA227AC 8780603 SW WING/NACELLE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 158MC AC726B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE RIGHT UPPER INBOARD WING SKIN TO NACELL E ATTACH ANGLE. THEY STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW FAC ARP 54-20-9101. (M) 2 L 7 2 4T RT A8SW 1996041800460 19960418 00460 SW 1996 4 18 MALA964910 1 19960301 A 5210 DOOR FRAME SWRNGN SA227 SA227AC 8780603 SW BS 159 DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 158MC AC726B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED CHAFFED DAMAGE ON THE FS 159 BELT FRAME WEB ABOVE THE PASSENGER DOOR CLOSER BELL CRANK. THEY INSTALLED A DOUBLER ON THE BACK SIDE OF FILLED THE CHAFE DAMAGE IAW FAC LAR 96-M ALA-033. (M) 2 L 7 2 4T RT A8SW 1996041800461 19960418 00461 SW 1996 4 18 MALA964911 1 19960301 A 5311 FRAME SWRNGN SA227 SA227AC 8780603 SW BS 212 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 158MC AC726B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE LOWER BELT FRAME FLANGE RELIEF RADIUS A T FS 212. THEY STOP DRILLED THE CRACK AND INSTALLED A DOUBLER AND STIFFENER IAW FAC SRM 53-90-20. (M) 2 L 7 2 4T RT A8SW 1996041800462 19960418 00462 SW 1996 4 18 MALA964912 1 19960301 A 5347 SEAT TRACK SWRNGN SA227 SA227AC 8780603 SW RT COCKPIT CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 158MC AC726B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE FIRST OFFICERS OUTBOARD SEAT TRACK CHAN NEL. THEY INSTALLED A REPAIR DOUBLER IAW FAC ARP 53-10-9322. (M) 2 L 7 2 4T RT A8SW 1996041800463 19960418 00463 SW 1996 4 18 MALA964919 1 19960314 A 2720 2744026007 TORQUE TUBE SWRNGN SA227 SA227AC 8780603 SW RT ELEVATOR WORN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 438MA AC721B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED WEAR ON THE RIGHT ELEVATOR TORQUE TUBE. THEY REPLACED THE TORQUE TUBE IAW FAC MM 27-30-00. (M) 2 L 7 2 4T RT A8SW 1996041800464 19960418 00464 SW 1996 4 18 MALA964920 1 19960314 A 5330 SKIN SWRNGN SA227 SA227AC 8780603 SW FUSELAGE DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 438MA AC721B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED DAMAGE TO THE OUTER FUSELAGE SKIN AT THE PASSENGER DOO R FORWARD CORNER. THEY REPAIRED THE DAMAGE BY INSTALLING A DOUBLER IAW FAC LAR 96-MALA-042. (M) 2 L 7 2 4T RT A8SW 1996041800465 19960418 00465 SW 1996 4 18 MALA964921 1 19960314 A 5320 2722085 CARGO DOOR FRAME SWRNGN SA227 SA227AC 8780603 SW CARGO DOOR CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 438MA AC721B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED CRACKS IN THE FORWARD CARGO DOOR FRAME GAS STRUT MOUNT HOLE. THEY REMOVED THE CRACKED PORTION AND FABRICATED AND INSTALLED A REPAIR ANGLE, PLATE AND FILLER IAW FAC ARP 53-20 -9503. (M) 2 L 7 2 4T RT A8SW 1996041800466 19960418 00466 SW 1996 4 18 MALA964923 1 19960314 A 5330 SKIN SWRNGN SA227 SA227AC 8780603 SW FS 512 DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 438MA AC721B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A DENT IN THE FUSELAGE SKIN AFT OF FS 512. THEY REPAI RED THE DENT BY FABRICATING AND INSTALLING A REPAIR DOUBLER IAW FAC SRM 53-90-20. (M) 2 L 7 2 4T RT A8SW 1996041800467 19960418 00467 SW 1996 4 18 MALA964924 1 19960314 A 5330 SKIN SWRNGN SA227 SA227AC 8780603 SW FS 493 DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 438MA AC721B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A DENT IN THE FUSELAGE SKIN AFT OF FS 493. THEY REPAI RED THE DENT BY FABRICATING AND INSTALLING A REPAIR DOUBLER IAW FAC SRM 53-90-20. (M) 2 L 7 2 4T RT A8SW 1996041800468 19960418 00468 SW 1996 4 18 MALA964925 1 19960314 A 5753 2736015 RIB SWRNGN SA227 SA227AC 8780603 SW RT TE FLAP CRACK A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 438MA AC721B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE RIGHT FLAP OUTBOARD END NOSE RIB. THEY REPLACED THE OUTBOARD END NOSE RIB IAW FAC SRM 57-90-60. (M) 2 L 7 2 4T RT A8SW 1996041800469 19960418 00469 SW 1996 4 18 MALA964926 1 19960321 A 3260 1EN516 SWITCH SWRNGN SA227 SA227AC 8780603 SW RT MLG FAILED A MALA O OTHER N FALSE WARNING AP APPROACH 1 GL 15 446MA AC693 FLIGHT NR 3078 - INBOUND TO MSP, THE CREW NOTED THE LEFT MAIN GEAR INTRANSIT LIGHT WAS INTERMITTENT. THE AIRCRAFT CONTI NUED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE LEFT MAIN GEAR UP POSITION SWITCH. ALL SYS TEMS OPERATED SATISFACTORILY. (M) 2 L 7 2 4T RT A8SW 1996041800470 19960418 00470 SW 1996 4 18 MALA964927 1 19960323 A 5210 DOOR SEAL SWRNGN SA227 SA227AC 8780603 SW PAX DOOR LOOSE A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 26863 AC650B FLT NR 3487 - AFTER DEPARTURE FROM YQT, THE CREW NOTED A FLAPPING NOISE FROM THE PASSENGER DOOR AREA. THE AIRCRAFT RETU RNED TO YQT AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL SECURED A SHIM FOR THE PASSENGER DOOR SEAL. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2 L 7 2 4T RT A8SW 1996041800471 19960418 00471 SW 1996 4 18 MALA964928 1 19960322 A 3230 1EN516 UPLOCK SWITCH SWRNGN SA227 SA227AC 8780603 SW NLG FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 60NE AC760B FLT NR 3353 - AFTER DEPARTURE FROM DTW, THE CREW NOTED THE NOSE GEAR WOULD NOT REMAIN UP AND LOCKED WHEN THE GEAR WAS RE TRACTED. THE AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE NOSE GEAR UPLIMI T SWITCH. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2 L 7 2 4T RT A8SW 1996041800472 19960418 00472 WP 1996 4 18 ORJA96013 1 19960305 A 3350 RPSIB POWER SUPPLY DOUG DC9 DC987 3022087 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 752RA 7776 49780 INTERMITTENT OPERATION OF FORWARD CABIN FLOOR TRACK POWER SUPPLY. REMOVED AND REPLACED FORWARD CABIN FLOOR TRACK POWER SUPPLY DUE TO SUSPECTED INTERMITTENT OPERATION. OPS CHECKS OK. (M) 2 L 7 2 4F RT A6WE 1996041800473 19960418 00473 WP 1996 4 18 ORJA96014 1 19960311 A 2560 LANYARD DOUG DC9 DC982 3022082 WP ENTRY SLIDE BROKEN A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 842RA 49604 ENTRY SLIDE LANYARD BROKEN. INSTALLED NEW LANYARD. (M) 2 L 7 2 4F A6WE 1996041800474 19960418 00474 WP 1996 4 18 ORJA96016 1 19960317 A 3350 41B004AD073 BATTERY BRUCE EA1D13D3 DOUG DC9 DC987 3022087 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 REMOVED LEFT FORWARD EMERGENCY EXIT LIGHT BATTERY PACK. INSTALLED LEFT FORWARD EMERGENCY EXIT LIGHT BATTERY PACK. (M) 2 L 7 2 4F RT A6WE 1996041800475 19960418 00475 WP 1996 4 18 ORJA96018 1 19960325 A 3350 41B994AD073 BATTERIES DOUG DC9 DC987 3022087 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 751RA 49779 AFT OVERHEAD EMERGENCY LIGHT IN EMPANNAGE INOP. INSTALLED NEW BATTERIES. OPS CHECKS NORMAL. (M) 2 L 7 2 4F RT A6WE 1996041800476 19960418 00476 EU 1996 4 18 RAIA960237 1 19960223 A 7797 8974694 WIRE HARNESS BAG JETSTM JETSTM3201 1500217 EU LT ENGINE SHORTED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 427AM 9696 876 CMI - FLT NR 7437 - LEFT ENGINE BEGAN SURGING DURING TAKEOFF ROLL. MAINTENANCE REPAIRED WIRE ON SHORT LEAD, GROUND RUNS GOOD. (M) 2 L 7 2 4T RT A56EU 1996041800477 19960418 00477 WP 1996 4 18 RAIA960302 2 19960303 A 7310 137905A73 FUEL LINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP NR 1 ENGINE OUT OF POSITION A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 03 339TE 8075 935 STL - FLT 7466 - LOW FUEL PRESSURE WARNING ON TAKEOFF. REPOSITIONED FUEL LINE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996041800478 19960418 00478 EU 1996 4 18 RAIA960303 1 19960301 A 5270 SP4594 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGG DOOR OUT OF ADJUST A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 556HK 1035 41073 DCA - FLT NR 7744 - BAGGAGE DOOR LIGHT ILLUMINATED DURING TAKEOFF. MAINTENANCE ISSUED DMI 52-3. MAINTENANCE LATER CLEA RED DMI BY ADJUSTING BAGGAGE DOOR SWITCH. (M) 2 L 7 2 4T RT A41NM 1996041800479 19960418 00479 WP 1996 4 18 RAIA960305 2 19960304 A 7530 1379293L407 BLEED LINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT ENGINE LOOSE A RAIA O OTHER O OTHER CL CLIMB 1 CE 03 429AM 10556 879 66321 STL - FLT 7466 - WHEN TURNING LEFT BLEED ON, TORQUE DROPPED FROM 100 PERCENT TO 80 PERCENT. MAINTENANCE SECURED BLEED L INE BEHIND ASPIRATOR, GROUND RUNS GOOD. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996041800480 19960418 00480 NE 1996 4 18 RAIA960324 2 19960318 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE LEFT FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 03 550HK 1945 41039 75075 DCA - FLT NR 7750 - LEFT ENGINE LOST TORQUE DURING TAKEOFF ROLL. MAINTENANCE REPLACED LEFT ENGINE, GROUND RUNS GOOD. ( M) 2 L 7 2 4T 4 T RT A41NM E18NE 1996041800481 19960418 00481 EU 1996 4 18 RAIA960330 1 19960325 A 5270 91SE13 SWITCH BAG JETSTM JETSTM3201 1500217 EU PAX DOOR DIRTY A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 340TE 8537 939 STL - FLT NR 7051 - PAX DOOR CAP ILLUMINATED. MAINTENANCE CLEANED PAX DOOR MICROSWITCHES PERFORMED OPERATIONAL CHECK OF PAX DOOR SYSTEM, OPS CHECK GOOD. (M) 2 L 7 2 4T RT A56EU 1996041800482 19960418 00482 EU 1996 4 18 REXA96010 1 19960224 A 7920 AE3663161M0385 FLEX HOSE SAAB SF340 SF340A 7850100 EU LT ENGINE LEAKING A REXA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 25 326PX 340A054 ON TAXI OUT, FLIGHT ATTENDANT REPORTED SMOKE IN CABIN. SHUT DOWN LEFT ENGINE AND DEPLANED PAX. SMOKE CEASED. INSPECTE D LEFT ENGINE, FOUND OIL LEAKING FROM 2 TRANSFER LINES, ON OUTBOARD SIDE OF MIDFRAME CASING UNIONS, TO BOTTOM OF ENGINE BAY. INSTALLED CONICAL SEALS ON BOTH LINES. ALSO, BAGGED DRAIN LINES AND PERFORMED RUN WITH BLEEDS ON, NO SMOKE VISIBL E AND LEAK CHECK GOOD. SUBMITTER STATES, SUSPECT THE LINES LEAKING WERE ACTUALLY THE PGB OIL COOLER HOSES. (M) 2 L 7 2 4T RT A52EU 1996041800483 19960418 00483 EU 1996 4 18 REXA96011 1 19960312 A 7110 7271110806 COWLING SAAB SF340 SF340A 7850100 EU RT NACELLE BENT A REXA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 407BH 340A078 AFTER TAKEOFF RIGHT COWLING DOOR CAME OPEN IN FLIGHT, AIR RETURN. REMOVED AND REPLACED FORWARD AND AFT COWLINGS. (M) 2 L 7 2 4T RT A52EU 1996041800484 19960418 00484 EU 1996 4 18 REXA96012 1 19960317 A 2910 L38710SA SWIVEL AIR843104 SAAB SF340 SF340A 7850100 EU LT MLG BROKEN A REXA D RETURN TO BLOCK K FLUID LOSS CL CLIMB 1 SO 25 321PX 25330 LK8503397 340A031 RUPTURED HYDRAULIC LINE IN LEFT WHEEL WELL. REMOVED AND REPLACED LEFT LANDING GEAR DOWNLOCK ACTUATOR HYDRAULIC LINE SWI VEL. LEAK CHECK GOOD. SERVICED HYDRAULIC SYSTEM IAW AMM. (M) 2 L 7 2 4T RT A52EU 1996041800485 19960418 00485 EU 1996 4 18 SIMA960942 1 19960403 A 3210 D602592 LANDING GEAR MESSIER D22685040113 AEROSP ATR42 ATR42300 8680920 EU LT MLG FAILED A A SIMA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 21 421MQ 14136 155B4 014 TVC - FLT 4245 - AFTER LANDING AT TVC, DURING ROLL OUT TO TAXI WAY, AIRCRAFT LT MLG FAILED. CREW COMPLIED WITH ENGINE S HUTDOWN AND EMERGENCY EVACUATION OF PASSENGERS. INVESTIGATION SHOWED THAT THE MLG LANDING GEAR SEPARATED AT THE SWIVEL POINT BETWEEN LEG ASSY AND TRAILING ARM ASSY. SUBMITTER STATES, THIS IS STRUCTURAL FAILURE OF THE LEG ASSY. AN INDEPTH VISUAL INSPECTION WAS COMPLIED WITH AND ANOTHER GEAR WAS INSTALLED. AIRCRAFT IS BEING FERRIED TO MQT. FOR FURTHER INV ESTIGATION AND INSPECTION. DAMAGED GEAR COMPONENTS ARE BEING SENT TO THE NTSB. (M) 2 H 7 2 4T RT A53EU 1996041800486 19960418 00486 NM 1996 4 18 TAOA039612 1 19960313 A 3350 900835A BATTERY PACK GRIMES BOEING 727 727294 1384088 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 921TS 11299 22043 LEFT FORWARD EXTERIOR EMERGENCY LIGHT INOP. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. (M) 0 4 A3WE 1996041800487 19960418 00487 NM 1996 4 18 TAOA039613 1 19960313 A 3350 5106 BATTERY PACK BOEING 727 727294 1384088 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 921TS 22043 EMERGENCY EXIT LIGHT AT AFT STAIRWAY INOP. REPLACED BATTERY PACK OPERATIONAL CHECK OK. (M) 0 4 A3WE 1996041800488 19960418 00488 NM 1996 4 18 TAOA039618 1 19960326 A 3242 Z11423 BRAKE ASSY GOODYEAR BOEING 727 727227 1384078 NM NR 3 SMOKING A TAOA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 EA 15 924TS 2482 21041 NR 3 BRAKE REPORTED SMOKING AFTER LANDING. REPORTED BY LGA ALT TOWER. REPLACED ON OVERNIGHT DCA. LEAK CHECKED THE BRA KE, NO LEAKS FOUND. SUBMITTER STATES, SUSPECT RESIDUE ON BRAKE THAT WAS CHANGED LAST NIGHT. OK FOR SERVICE. (M) 2 L 7 3 4F A3WE 1996041800489 19960418 00489 NM 1996 4 18 TWRA9613 1 19960323 A 3350 S1356B37 BATTERY PACK BOEING 747 747282B 1384860 NM CABIN DISCHARGED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 610FF 20501 DURING GROUND CHECKS, FOUND SEVERAL EMERGENCY LIGHTS INOP. FOUND WATER UNDER GALLEY MAT, TROUBLESHOT AND CORRECTED INOP EMERGENCY LIGHTS. REPLACED BATTERY PACK, EMERGENCY CEILING LIGHT ABOVE ROW 59HJK. (M) 2 L 7 4 4F A20WE 1996041800490 19960418 00490 NM 1996 4 18 TWRA9614 1 19960323 A 3350 363781 STRIP LIGHT BOEING 747 747282B 1384860 NM CABIN BROKEN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 610FF 20501 DURING GROUND CHECKS, FOUND SEVERAL EMERGENCY LIGHTS INOP. FOUND STRIP LIGHT WIRE BROKEN. TROUBLESHOT AND CORRECTED IN OP EMERGENCY LIGHTS. 1 REPLACED 2 SECTIONS OF STRIP LIGHT. (M) 2 L 7 4 4F A20WE 1996041800491 19960418 00491 NM 1996 4 18 USAA960315 1 19960316 A 5312 BULKHEAD WEB BOEING 737 737201 1384454 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 263AU 33548 22869 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK, 2 INCH CRACK, 1 INCH CRACK AND .5 INCH CRACK AT 178 BULKH EAD WEB AT LOWER LEFT RADAR DISH MOUNT. INSTALLED DOUBLER REPAIR, REPAIRED PER TR 53-10-11. (M) 2 L 7 2 4F A16WE 1996041800492 19960418 00492 NM 1996 4 18 USAA960316 1 19960316 A 5312 BULKHEAD SKIN BOEING 737 737201 1384454 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 263AU 33548 22869 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 178 BULKHEAD SKIN. INSTALLED DOUBLER, REPAIRED PER TR 5 3-10-11. (M) 2 L 7 2 4F A16WE 1996041800493 19960418 00493 NM 1996 4 18 USAA960317 1 19960316 A 5320 ANGLE BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 263AU 33548 22869 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH LONG CRACK STATION 727 UPPER COMPRESSION CHORD ANGLE. INSTALLED REPAIR ANGLE, REPAIRED PER TR 53-10-03. (M) 2 L 7 2 4F A16WE 1996041800494 19960418 00494 NM 1996 4 18 USAA960318 1 19960316 A 5330 SKIN BOEING 737 737201 1384454 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 263AU 33548 22869 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK BS 178 WL 210 AT SKIN. INSTALLED DOUBLER, REPAIRED PER TR 53-10-11. (M) 2 L 7 2 4F A16WE 1996041800495 19960418 00495 NM 1996 4 18 USAA960319 1 19960316 A 5330 SKIN BOEING 737 737201 1384454 NM BS 767 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 263AU 33548 22869 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK BS 767 STRINGER 19 R FUSELAGE SKIN. INSTALLED REPAIR, REP AIRED PER SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1996041800496 19960418 00496 NM 1996 4 18 USAA960320 1 19960316 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 767 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 263AU 33548 22869 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK BS 767 STRINGER 19 RT. INSTALLED REPAIR, REPAIRED PER SRM 53-10-3. (M) 2 L 7 2 4F A16WE 1996041800497 19960418 00497 NM 1996 4 18 USAA960321 1 19960316 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 947-957 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 263AU 33548 22869 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION ON STRINGER APPROXIMATELY 10 INCHES BY .5 INCH STRINGER 29L ST ATION 947 TO 957. REPLACED APPROXIMATELY 22.5 INCHES OF STRINGER. REPAIRED PER SRM 53-10-3. (M) 2 L 7 2 4F A16WE 1996041800498 19960418 00498 NM 1996 4 18 USAA960322 1 19960318 A 5330 SKIN BOEING 737 737201 1384454 NM BS 970 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 245US 36367 22751 INT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND 4 INCH CRACK SKIN BS 970 STRINGER 21L. DOUBLER INSTALLED PER SRM 53 -30-3, REPAIRED PER SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1996041800499 19960418 00499 NM 1996 4 18 USAA960334 1 19960324 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 947-967 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 233US 41690 22273 ROA - DURING CX-4 CHECK VISUAL INSPECTION FOUND 2 INCH BY 20 INCH CORROSION STRINGER 27 LEFT FROM BS 947 TO BS 967 DUE T O LAV SPILLS. REMOVED DAMAGED SECTION OF STRINGER. FABRICATED NEW STRINGER, DOUBLERS, SPLICES AND SHIMMS, INSTALLED SA ME. REPAIRED PER SRM 53-10-3 FIG 1. (M) 2 L 7 2 4F A16WE 1996041800500 19960418 00500 NM 1996 4 18 USAABB96010 1 19960322 A 2820 7G1103 PRESS SWITCH BOEING 767 7672B7 1385107 NM LEFT FUEL SYSTEM FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 652US 24765 BOS - FLT NR 16 - EN ROUTE PHL-CDG, CREW NOTED THE LEFT FUEL BOOST PUMP LIGHT ILLUMINATED. CREW ELECTED TO DIVERT TO BO S. MAINTENANCE REPLACED THE LEFT FORWARD FUEL BOOST PUMP OUTPUT PRESSURE SWITCH. (M) 2 L 7 2 4F RT A1NM 1996041800501 19960418 00501 EU 1996 4 18 USAAF960303 1 19960324 A 3230 RETRACT MECH FOKKER F28 F28MK4000 4990810 EU LANDING GEAR MALFUNCTIONED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 494US 11167 CLT - FLT 2052 - CREW COULD NOT RETRACT GEAR AFTER TAKEOFF. FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT. (M) 2 L 7 2 4F RT A20EU 1996041800502 19960418 00502 EU 1996 4 18 USAAF96030A 1 19960324 A 3230 8SD8181 SOLENOID FOKKER F28 F28MK4000 4990810 EU COCKPIT FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 494US 11167 CLT - FLT 2052 - CREW COULD NOT RETRACT GEAR AFTER TAKEOFF. FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR LEVER LATCH SOLENOID. (M) 2 L 7 2 4F RT A20EU 1996041800503 19960418 00503 EU 1996 4 18 USAAF96031 2 19960325 A 7530 D74075445 TUBE FOKKER F28 F28MK0100 4990807 EU RROYCE SPEY SPEY55515 54521 EU RT ENGINE CRACKED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 881US 11333 CLT - FLT 242 - AFTER TAKEOFF, CREW RECEIVED A NR 2 BLEED FAULT MESSAGE AND THEN A NR 2 DUCT LEAK MESSAGE. FLIGHT RETUR NED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND A CRACKED LINE IN THE NR 2 ENGINE SUB WING TEST BLOCK AREA. A TEMPORARY LINE WAS INSTALLED AND A PERMANENT LINE PROGRAMMED. (M) 2 L 7 2 4F 4 F RT E2EU 1996041800504 19960418 00504 1996 4 18 USAASB96047 4 19960314 A 3441 HG1050AD05 IRU BOEING 737 7373B7 1384580 NM NR 1 FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 526AU 23861 FLT NR 2195 - DCA - ON CLIMB-OUT, NR 1 ATTITUDE FLAG CAME IN VIEW. HEADING FLAG ON HSI IN VIEW. MAINTENANCE REPLACED N R 1 IRU AND PERFORMED OPS CHECK. SYSTEM CHECKS NORMAL. (M) 2 L 7 2 4F RT A16WE 1996041800505 19960418 00505 NE 1996 4 18 USAASB96048 2 19960319 A 7200 ENGINE BOEING 737 737201 1384454 NM PWA JT8 JT8D9A 52048 NE LEFT WING FAILED A A USAA A UNSCHED LANDING A P Y FLAME/FIRE NO WARNING INDICATION ENGINE STOPPAGE CL CLIMB 1 EA 19 224US 52021 21666 674229 GSO - FL 8028 - AT APPROXIMATELY 600 FEET AGL AFTER TAKEOFF FROM GSO, THE LEFT ENGINE EXPLODED. TOWER ADVISED CREW THAT ENGINE WAS TRAILING SMOKE AND FIRE. FLIGHT RETURNED TO GSO AND GROUND EMERGENCY CREWS EXTINGUISHED THE ENGINE FIRE. N O FIRE WARNINGS RECEIVED IN COCKPIT. SINGLE ENGINE TIME 4 MINUTES. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE AN D TRIM RAN PER JOB CARD. (M) 2 L 7 2 4F 4 F A16WE E2EA 1996041800506 19960418 00506 NE 1996 4 18 USAASB96053 2 19960325 A 7320 8063207 FUEL CONTROL BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE NR 1 ENG OUT OF ADJUST A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 524AU 23859 FLT NR 627 - PIT - TEN MINUTES AFTER LEVEL OFF (31,000) IN CRUISE THERE WAS A (4) KNOB THROTTLE SPLIT. ENGINE 1 WAS BEH IND ENGINE 2. PMCS WERE TURNED OFF. THE SPLIT REMAINED. ALL OTHER INDICATIONS WERE NORMAL. MAINTENANCE ACCOMPLISHED MEC ADJUSTMENT OF NR 1 ENGINE IAW MM 71-00-00 TEST 6. ACCOMPLISHED PART POWER TRIM RUN AND TAKEOFF RUN. NO THROTTLE SP LIT NOTED. RIG CHECK NORMAL. (M) 2 L 7 2 4F 4 F RT A16WE E2GL 1996041800507 19960418 00507 NM 1996 4 18 USAASB96061 1 19960402 A 2761 65449617 SPOILER ACTUATOR BOEING 737 7372B7 1384560 NM LT WING CRACKED A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION DE DESCENT 1 EA 19 277AU 22889 FLT NR 1126 - DCA - AIRCRAFT DIVERTED FROM BWO TO DCA DUE TO LOSS OF 'A' SYSTEM HYDRAULIC SYSTEM. MAINTENANCE FOUND NR 1 SPOILER ACTUATOR CRACKED. REMOVED AND REPLACED NR 1 SPOILER ACTUATOR. AS A PRECAUTIONARY MEASURE BOTH 'A' SYSTEM HYD RAULIC PUMP WERE CHANGED. OPS CHECK AND LEAK CHECKS WERE SATISFACTORY. (M) 2 L 7 2 4F A16WE 1996041800508 19960418 00508 EU 1996 4 18 VTZA96114 1 19960319 A 5270 91SE16 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU EMERG EXITS OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 325UE 41063 FLT NR 6444 - BOS-IAD - ABORTED TAKEOFF DUE TO THE EMERGENCY EXIT DOOR WARNING ILLUMINATING DURING THE TAKEOFF ROLL. AI RCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE CLEANED AND INSPECTED THE EMERGENCY EXIT MICROSWITCHES. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996041800509 19960418 00509 EU 1996 4 18 VTZA96115 1 19960319 A 7714 AG34 TACH GENERATOR BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A VTZA A UNSCHED LANDING O OTHER TO TAKEOFF 1 EA 27 487UE 906 FLT NR 6320 - IAD-ISP - AFTER TAKEOFF, RETURNED TO IAD DUE TO THE LEFT RPM INDICATION FAILED. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE LEFT TACH GENERATOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996041800510 19960418 00510 WP 1996 4 18 VTZA96116 2 19960317 A 7320 89778025 FUEL CONTL UNIT BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RT ENGINE OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 27 481UE 895 P66009 FLT NR 6286 - IAD- CMH - ABORTED TAKEOFF, DUE TO THE RIGHT ENGINE NOT MAKING TAKEOFF TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED THE MAX FUEL FLOW. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SE RVICE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996041800511 19960418 00511 EU 1996 4 18 VTZA96118 1 19960315 A 2437 DVM41B AMMETER JETAIR JETSTM JETSTM4101 1500501 EU RIGHT FAILED A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 302UE 41013 FLT NR 6444 - BOS-IAD - DURING CLIMB-OUT, RETURNED TO BOS DUE TO THE RIGHT AMMETER INDICATING 700 AMPS. AIRCRAFT LANDED AT BOS WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE RIGHT AMMETER. AIRCRAFT WAS RELEASED AND APPROVED FOR RETU RN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996041800512 19960418 00512 EU 1996 4 18 VTZA96119 1 19960313 A 7722 6100116 EGT GAUGE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LEFT FAILURE A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 27 488UE 907 P66150 FLT NR 6175 - ELM-IAD - ABORTED THE TAKEOFF DUE TO THE LEFT ENGINE EGT FLUCTUATING ON THE TAKEOFF ROLL. AIRCRAFT RETURN ED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 06498 IAW MEL 76-1 ON THE SRL SYSTEM. MAINTENANCE LATE R CLEARED DMI NR 06498 ON 3-14-96 BY REPLACING THE LEFT EGT GAUGE AND THE T2 SENSOR CANNON PLUG. PERFORMED OPERATIONAL CHECKS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996041800513 19960418 00513 EU 1996 4 18 VTZA96120 1 19960314 A 3240 91SE16 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU PARKING BRAKE DIRTY A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 325UE 41063 FLT NR 6485 - IAD-JFK - ABORTED THE TAKEOFF DUE TO THE TAKEOFF CONFIGURATION WARNING SYSTEM ACTIVATING. AIRCRAFT RETURN ED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE CLEANED THE PARKING BRAKE MICROSWITCH. AIRCRAFT WAS RELEASED AND APP ROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996041800514 19960418 00514 EU 1996 4 18 VTZA96121 1 19960314 A 2751 TY1760A4 FLAP POS TRANSD JETAIR JETSTM JETSTM4101 1500501 EU TE FLAPS WATER CONTAM A VTZA O OTHER F FLT CONT AFFECTED LD LANDING 1 EA 27 321UE 41045 FLT NR 6204 - MHT-IAD - DURING LANDING, FLAP FAULT OCCURRED AND WOULD NOT RESET. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WITH ZERO FLAPS. AIRCRAFT LANDED WITH NO FURTHER INCIDENTS AND ALL PASSENGERS SAFE. MAINTENANCE INSPECTED FLAP SYSTEM AND CLEANED MOISTURE FROM THE FLAP POSITION TRANSDUCERS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVI CE. (M) 2 L 7 2 4T RT A41NM 1996041800515 19960418 00515 WP 1996 4 18 VTZA96122 2 19960317 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RIGHT BIRD INGESTION A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK C F.O.D. TO TAKEOFF 1 EA 27 477UE 12520 890 P66088 FLT 6240 - PHF-IAD - ABORTED TAKEOFF DUE TO THE RIGHT ENGINE INGESTING A BIRD ON THE TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE INSPECTED ENGINE AND FOUND TWO BENT IMPELLER BLADES. AIRCRAFT WAS FERRIED TO LYH WHERE IT IS UNDER GOING AN ENGINE CHANGE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996041800516 19960418 00516 1996 4 18 VTZA96123 4 19960317 A 3417 7700966 ADC JETAIR JETSTM JETSTM4101 1500501 EU AVIONICS BAY FAILED A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 308UE 41023 FLT NR 6595 - IAD-LGA - DURING CLIMB-OUT, RETURNED IAD, AIR DATA COMPUTER INDICATIONS BEING INTERMITTENT. AIRCRAFT LAND ED AT IAD WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED BOTH AIR DATA COMPUTERS. AIRCRAFT RELEASED AND APPROVED FOR R ETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996041800517 19960418 00517 1996 4 18 VTZA96124 3 19960317 A 6140 310389813 BETA PRESS SW JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 27 320UE 41043 FLT NR 6225 - IAD-RIC - ABORTED TAKEOFF, DUE TO THE LEFT RED BETA LIGHT ILLUMINATING DURING THE TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE LEFT BETA PRESSURE SWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996041800518 19960418 00518 EU 1996 4 18 VTZA96125 1 19960314 A 5270 91SE16 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGGAGE BAY OUT OF ADJUST A VTZA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 27 322UE 41058 FLT NR 6515 - JFK-ROC - ABORTED TAKEOFF, DUE TO THE BAGGAGE DOOR WARNING LIGHT ILLUMINATING ON THE TAKEOFF ROLL. AIRCRA FT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 17599 IAW MEL 52-3. MAINTENANCE LATER CLEARED DMI NR 17599 ON 3-16-96 BY RERIGGING THE FORWARD BAGGAGE DOOR MICROSWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETU RN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996041800519 19960418 00519 EU 1996 4 18 VTZA96126 1 19960319 A 2611 SMOKE DET JETAIR JETSTM JETSTM4101 1500501 EU BAGG COMPT MALFUNCTIONED A VTZA K NONE N FALSE WARNING AP APPROACH 1 EA 27 321UE 41045 FLT NR 6529 - IAD-JFK - DURING APPROACH, THE VENTRAL BAGGAGE BAY SMOKE DETECTOR LIGHT ILLUMINATED. AN EMERGENCY WAS DEC LARED AND AIRCRAFT LANDED AT JFK WITH NO FURTHER INCIDENTS. MAINTENANCE INSPECTED, BUT FOUND NO FIRE OR SMOKE EVIDENCE. MAINTENANCE OPENED DMI NR 21970 IAW MEL 26-3 ON THE VENTRAL BAGGAGE SMOKE DETECTION SYSTEM. (M) 2 L 7 2 4T RT A41NM 1996041800520 19960418 00520 EU 1996 4 18 VTZA96127 1 19960319 A 2611 72111211000 SMOKE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU BAGGAGE BAY FAILED A VTZA O OTHER N FALSE WARNING AP APPROACH 1 EA 27 321UE 41045 FLT NR 6529 - IAD-JFK - DURING APPROACH, THE VENTRAL BAGGAGE BAY SMOKE DETECTOR LIGHT ILLUMINATED. AN EMERGENCY WAS DEC LARED AND AIRCRAFT LANDED AT JFK WITH NO FURTHER INCIDENTS. MAINTENANCE INSPECTED BUT FOUND NO FIRE OR SMOKE EVIDENCE. MAINTENANCE OPENED DMI NR 21970 IAW MEL 26-3 ON THE VENTRAL BAGGAGE SMOKE DETECTION SYSTEM. MAINTENANCE LATER CLEARED DMI NR 21970 ON 3-19-96, BY REPLACING THE BAGGAGE BAY SMOKE DETECTOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996041800521 19960418 00521 EU 1996 4 18 VTZA96128 1 19960321 A 5270 91SE16 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU MAIN BAG DOOR OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 322UE 41058 FLT NR 6353 - IAD-TYS - ABORTED THE TAKEOFF DUE TO THE MAIN BAGGAGE DOOR WARNING LIGHT ILLUMINATING DURING THE TAKEOFF R OLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED THE FORWARD MICROSWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996041800522 19960418 00522 WP 1996 4 18 VTZA96129 2 19960321 A 7320 137223L401 P3 LINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP LT WHEEL WELL FAILED A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 475UE 850 FTL NR 6586 - IAD-ISP - DURING CLIMB-OUT, RETURNED TO IAD DUE TO THE AIRCRAFT NOT PRESSURIZING. AIRCRAFT LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED LEFT P3 LINE AND RECONNECTED RIGHT ACM DUCT. AIRCRAFT WAS RELEASED AND APPROV ED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 3 T RT A56EU E3WE 1996041800523 19960418 00523 WP 1996 4 18 VTZA99117 2 19960317 A 7321 89778025 FUEL CONTL UNIT BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RT ENG FAILED A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 481UE 895 P66009 FLT NR 6326 - IAD-ROC - DURING CLIMB-OUT, RETURNED TO IAD, DUE TO THE RIGHT ENGINE WOULD NOT MAKE TORQUE ON CLIMB-OUT. A IRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE RIGHT FUEL CONTROL UNIT. AIRCRAFT WAS RELEAS ED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996042200001 19960422 00001 NM 1996 4 22 P5CA9600183 1 19960122 A 5414 ACCESS PANEL BOEING 747 747122 1384872 NM LT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND 5TH POD ACCESS PANEL AT UNDERWING ROOT DELAMINATED. REPAIRED IAW SRM 51-40-09 AND REINSTALLED IAW MM 57-44-02. 2 L 7 4 4F A20WE 1996042200002 19960422 00002 GL 1996 4 22 HEEA966917 2 19960404 A 7210 6876925 TUBE ASSY. 23001938 AEROSP AS355 AS355F1 8680810 EU ALLSN 250C 250C20F 03013 GL ENG GR BOX DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5774M 11526 CAG34189 5009 CAE840464 ENGINE REMOVED DUE TO METAL IN OIL. UPON INSPECTION OF GEARBOX PARTS NOTED THE FOLLOWING: OIL TRANSFER TUBE FAILED DIM ENSIONAL CHECK IN ACCORDANCE WITH CEB1307. INSTALLED A NEW OIL TUBE ASSEMBLY. 1 G 7 2 3U 3 U H11EU E4CE 1996042200003 19960422 00003 WP 1996 4 22 UPS96805899 1 19960223 A 5753 VANE DOUG DC8 DC871F 302199D WP LT WING TE FLAP DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT WING NR 5 FLAP VANE DELAMINATED. REPLACED VANE ASSY PER MM 27-51-14. 2 L 7 4 4F RT 4A25 1996042500045 19960425 00045 EU 1996 4 25 96ZZZX1911 1 19960301 A 6410 704A33633171 HINGE SNIAS 350 AS350B 8680801 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 152AC 157 1101 TAIL ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECT ED PROBLEM. 1 G 7 1 3U H9EU 1996042500046 19960425 00046 EU 1996 4 25 96ZZZX1912 1 19960301 A 6410 704A33633171 HINGE SNIAS 350 AS350B 8680801 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 58045 587 1602 TAIL ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECT ED PROBLEM. 1 G 7 1 3U H9EU 1996042500047 19960425 00047 EU 1996 4 25 96ZZZX1913 1 19960301 A 6410 704A33633116 BEARING SNIAS 350 AS350B 8680801 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 58045 360 1602 TAIL ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 4 EACH NEW UNITS FROM KIT 355A09-1036-01, CORRECT ED PROBLEM. 1 G 7 1 3U H9EU 1996042500048 19960425 00048 EU 1996 4 25 96ZZZX1914 1 19960301 A 6220 704A33633156 SPHERICAL STOP SNIAS 350 AS350B 8680801 EU M/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 3593X 343 4242 1081 MAIN ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996042500049 19960425 00049 EU 1996 4 25 96ZZZX1915 1 19960301 A 6220 704A33633156 SPHERICAL STOP SNIAS 350 AS350B 8680801 EU M/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 3593X 343 4257 1081 MAIN ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996042500050 19960425 00050 EU 1996 4 25 96ZZZX1916 1 19960301 A 6220 704A33633156 SPHERICAL STOP SNIAS 350 AS350B 8680801 EU M/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 3593X 343 4244 1081 MAIN ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996042500051 19960425 00051 EU 1996 4 25 96ZZZX1917 1 19960301 A 6220 704A33633109 SPHERICAL STOP SNIAS 350 AS350B2 8680813 EU M/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 6099P 416 7615 2818 MAIN ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996042500052 19960425 00052 EU 1996 4 25 96ZZZX1918 1 19960301 A 6220 704A33633109 SPHERICAL STOP SNIAS 350 AS350B2 8680813 EU M/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 6099P 416 7617 2818 MAIN ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996042500053 19960425 00053 EU 1996 4 25 96ZZZX1919 1 19960301 A 6220 704A33633109 SPHERICAL STOP SNIAS 350 AS350B2 8680813 EU M/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 6099P 416 7634 2818 MAIN ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996042500054 19960425 00054 EU 1996 4 25 96ZZZX1920 1 19960301 A 6410 704A33633171 HINGE SNIAS 350 AS350B 8680801 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 779LF 422 1621 TAIL ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECT ED PROBLEM. 1 G 7 1 3U H9EU 1996042500055 19960425 00055 EU 1996 4 25 96ZZZX1921 1 19960301 A 6410 704A33633171 HINGE SNIAS 350 AS350B2 8680813 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 96LG 106 2817 TAIL ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECT ED PROBLEM. 1 G 7 1 3U H9EU 1996042500056 19960425 00056 EU 1996 4 25 96ZZZX1922 1 19960301 A 6410 704A33633171 HINGE SNIAS 350 AS350B2 8680813 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 96LG 374 2817 TAIL ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECT ED PROBLEM. 1 G 7 1 3U H9EU 1996042500057 19960425 00057 EU 1996 4 25 96ZZZX1923 1 19960301 A 6410 704A33633116 BEARING SNIAS 350 AS350B2 8680813 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 96LG 374 2817 TAIL ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 4 EACH NEW UNITS FROM KIT 355A09-1036-01, CORRECT ED PROBLEM. 1 G 7 1 3U H9EU 1996042500058 19960425 00058 EU 1996 4 25 96ZZZX1924 1 19960301 A 6410 704A33633171 HINGE SNIAS 350 AS350B2 8680813 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 911LR 237 2404 TAIL ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECT ED PROBLEM. 1 G 7 1 3U H9EU 1996042500059 19960425 00059 EU 1996 4 25 96ZZZX1925 1 19960301 A 6410 704A33633116 BEARING SNIAS 350 AS350B2 8680813 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 911LR 550 2404 TAIL ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 4 EACH NEW UNITS FROM KIT 355A09-1036-01, CORRECT ED PROBLEM. 1 G 7 1 3U H9EU 1996042500060 19960425 00060 EU 1996 4 25 96ZZZX1926 1 19960301 A 6410 704A33633171 HINGE SNIAS 350 AS350B2 8680813 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 93LG 172 2654 TAIL ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECT ED PROBLEM. 1 G 7 1 3U H9EU 1996042500061 19960425 00061 EU 1996 4 25 96ZZZX1927 1 19960301 A 6410 704A33633116 BEARING SNIAS 350 AS350B2 8680813 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 93LG 238 2654 TAIL ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 4 EACH NEW UNITS FROM KIT 355A09-1036-01, CORRECT ED PROBLEM. 1 G 7 1 3U H9EU 1996042500062 19960425 00062 EU 1996 4 25 96ZZZX1928 1 19960301 A 6410 704A33633171 HINGE SNIAS 350 AS350B2 8680813 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 94LG 33 2728 TAIL ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECT ED PROBLEM. 1 G 7 1 3U H9EU 1996042500063 19960425 00063 EU 1996 4 25 96ZZZX1929 1 19960301 A 6410 704A33633171 HINGE SNIAS 350 AS350B2 8680813 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 94LG 139 2728 TAIL ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECT ED PROBLEM. 1 G 7 1 3U H9EU 1996042500064 19960425 00064 EU 1996 4 25 96ZZZX1930 1 19960301 A 6410 704A33633171 HINGE SNIAS 350 AS350B2 8680813 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 94LG 137 2728 TAIL ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECT ED PROBLEM. 1 G 7 1 3U H9EU 1996042500065 19960425 00065 EU 1996 4 25 96ZZZX1931 1 19960301 A 6410 704A33633171 HINGE SNIAS 350 AS350B2 8680813 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 94LG 371 2728 TAIL ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECT ED PROBLEM. 1 G 7 1 3U H9EU 1996042500066 19960425 00066 EU 1996 4 25 96ZZZX1932 1 19960301 A 6410 704A33633116 BEARING SNIAS 350 AS350B2 8680813 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 94LG 630 2728 TAIL ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 4 EACH NEW UNITS FROM KIT 355A09-1036-01, CORRECT ED PROBLEM. 1 G 7 1 3U H9EU 1996042500067 19960425 00067 WP 1996 4 25 9608629949 1 19960417 A 5610 5912290505 WINDSHIELD DOUG DC9 DC931 3022065 WP LT COCKPIT CRACKED A NWAA A UNSCHED LANDING O OTHER UK UNKNOWN 1 GL 01 8928E 45865 DURING FLIGHT, THE LEFT WINDSHIELD OUTER PANE CRACKED. RETURNED TO DTW WITHOUT FURTHER INCIDENT. REPLACED THE LEFT WIN DSHIELD AND LEFT HEAT CONTROL PER MM 56-10-2, WINDSHIELD HEAT CHECKED OK. 2 L 7 2 4F A6WE 1996042500068 19960425 00068 NM 1996 4 25 9608676308 1 19960417 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 668US 24223 DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING BETWEEN DOOR 2R AND 3R INOPERATIVE. RECONNECTED WIRE, OPERATION AL CHECK GOOD. 2 L 7 4 4F RT A20WE 1996042500069 19960425 00069 NM 1996 4 25 9608686310 1 19960418 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 670US 24225 DURING LINE CHECK, FOUND TWO RIGHT AFT OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND POWER SUPPLY, O PERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1996042500070 19960425 00070 EU 1996 4 25 9608693215 1 19960417 A 3350 321454 POWER SUPPLY AIRBUS 320 A320211 3930320 EU CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 315US 19819 6338 171 DURING MAINTENANCE, THE EMERGENCY LIGHTS TEST FAILED INT LOADS AFT L AND COMM AFT L. REPLACED POWER SUPPLY, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996042500071 19960425 00071 WP 1996 4 25 9608709758 1 19960418 A 2913 AS66411LS666 HYD PUMP DOUG DC9 DC941 302207N WP LT ENIGNE FAIL A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 758NW 34551 8864 47286 DURING CLIMB, THE LEFT HYDRAULIC SYSTEM LOST HYDRAULIC PRESSURE. LEFT HYDRAULIC SYSTEM PRESSURE WAS RESTORED WITH ALTER NATE HYDRAULIC PUMP AND RIGHT HYDRAULIC SYSTEM ON HIGH. AIRCRAFT RETUREND TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE LEFT ENGINE HYDRAULIC PUMP, OPERATIONAL TEST GOOD. 2 L 7 2 4F A6WE 1996042500072 19960425 00072 NE 1996 4 25 9608715517 2 19960417 A 7200 ENGINE BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE NR 2 FAILED A NWAA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CR CRUISE 1 GL 01 517US 23205 716473 DURING CRUISE, NR 2 ENGINE OIL QUANTITY AND PRESSURE INDICATIONS DROPPED. ENGINE POWER WAS REDUCED TO IDLE FOR REMAINDE R OF THE FLIGHT. AIRCRAFT DIVERTED TO ATL AND LANDED WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED NR 2 ENGINE WITH A SERVICEABLE ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 1996042500073 19960425 00073 WP 1996 4 25 9608729971 1 19960417 A 2410 696233B CSD DOUG DC9 DC931 3022065 WP RT ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 9335 47337 RIGHT CSD OIL PRESSURE LOW LIGHT FLICKERED DURING TAKEOFF ROLL. ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACED CSD AND OIL COOLER, LEAK AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996042500074 19960425 00074 WP 1996 4 25 9608739958 1 19960417 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 917RW 47145 DURING PREFLIGHT CHECK, FOUND CABIN FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS AND CONTROL AT ROW 12, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996042500075 19960425 00075 WP 1996 4 25 96FDEA00779 1 19960414 A 5510 ANGLE DOUG DC10 DC1010CF 3023502 WP RT HORIZ STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68054 47808 THE RT HORIZ STAB CENTER L/E SECTION O/B RIB UPPER CHORD ANGLE IS CRACKED IN 3 PLACES ON IN FLANGE BETWEEN RADIUS AND FA STENERS HOLES. REMOVED AND REPLACED UPPER CHORD ANGLE PER SRM 55-00-01. 2 L 7 3 4F RT A22WE 1996042500076 19960425 00076 NM 1996 4 25 96FDEA00786 1 19960415 A 5313 BAC1498145 STRINGER BOEING 727 727277 138408S NM BS 1052 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 242FE 21178 NR0338 AND 004 STR 28L AT BS 1052 IS CORRODED. REPAIRED STR AT 28L BS 1052 REMAINING FASTENERS TO BE INSTALLED ON NR011 9. ALL WORK DONE IAW FEDEX SRM 53-10-3. 2 L 7 3 4F RT A3WE 1996042500077 19960425 00077 NM 1996 4 25 96FDEA00789 1 19960417 A 5330 SKIN BOEING 727 727277 138408S NM BS 1052 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 242FE 21178 CORROSION (C53-100-01, -4) ON EXTERNAL SKIN AT BS 1052 STR 28L. FOUND CORROSION OUT OF LIMITS, CUT OUT DAMAGE AND REPAI RED SKIN PER FEDEX SRM 53-30-3 FIG 3. 2 L 7 3 4F RT A3WE 1996042500078 19960425 00078 NM 1996 4 25 96FDEA00790 1 19960417 A 5330 SKIN BOEING 727 727277 138408S NM BS 344 DENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 242FE 21178 TWO DENTS ON SKIN BS 344 STR 19 RT, .5 BY .065 DEPTH OUT OF LIMITS. CUT OUT DAMAGED AREA ON SKIN BS 344 STR 19 RT, FABR ICATED REPAIR PARTS, INSTALLED COUNTER SINK FILLERS AND FASTENED INTO PLACE WET WITH SEALENT. ALL WORK ACCOMPLISHED PER FEDEX SRM 53-30-3. 2 L 7 3 4F RT A3WE 1996042500079 19960425 00079 NM 1996 4 25 96FDEA00791 1 19960418 A 7830 B277806401 TR SWITCH BOEING 727 727233 138408A NM NR 1 ENGINE FAILED A FDEA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 25 257FE 20939 AFTER T/O, ENG NR 1 REVERSER OPERATING LIGHT CAME ON NR 1 ENGINE, SHUTDOWN AS PER PROCEDURE. A/C RELEASED FOR SERV PER MEL 78-2A. CHECKED WIRING HARNESS AT SWITCH FOR CONDITION, FOUND GOOD. CHECKED SW ADJ, WITHIN LIMITS. DURING T/S HAD NR 1 T/R OPS LIGHT GLOW DIM FOR SEVERAL SECONDS AND EXTINGUISH, WHILE NOTHING AROUND SW WAS TOUCHED. SUSPECT EITHER INT ERNAL FAILURE OF SW (P/N B27-78-064-01) OR LIGHT SOCKET (10-61803-78). REPLACED NR 1 T/R SW, OPS CHECK GOOD. 2 L 7 3 4F RT A3WE 1996042500080 19960425 00080 NM 1996 4 25 96FDEA00793 1 19960417 A 5320 WEB BOEING 727 727233 138408A NM BS 1230 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 269FE 21675 LIGHTENING HOLE ON TORQUE BOX VERTICAL WEB IS CRACKED .5 INCH LONG BS 1230 LBL 20 WL 185. STOP DRILLED CRACK IN TORQUE BOX WEB AT BS 1230 LBL 20 WL 185. FABRICATED REPAIR DOUBLER AND INSTALLED IAW FEDEX 51-40-2 AND 51-10-1. 2 L 7 3 4F RT A3WE 1996042500081 19960425 00081 NM 1996 4 25 96FDEA00794 1 19960417 A 5320 WEB BOEING 727 727233 138408A NM BS 1330 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 269FE 21675 LIGHTENING HOLE ON TORQUE BOX VERTICAL WEB IS CRACKED .5 INCH LONG BS 1330 RBL 20 WL 185. STOP DRILLED CRACK ON TORQUE BOX WEB AT BS 1330 RBL 20 WL 185. FABRICATED REPAIR AND INSTALLED REPAIR WORK IAW FEDEX SRM 51-10-1 AND 51-40-2. 2 L 7 3 4F RT A3WE 1996042500082 19960425 00082 NM 1996 4 25 96FDEA00795 1 19960418 A 5311 FRAME DOUG MD11 MD11F 3023600 NM LT MLG WW CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 605FE 48514 LT MLG GEAR WELL DOOR UPPER FRAME CRACKED. LOCATED 16 AFT OF GEAR WELL DOOR ACTUATOR I/B STRUT FAIRING. CRACK GOES TO EXISTING HOLE AS PER SRM 52-10-11 FIG 13 SHEET 2. FABRICATED DOUBLERS REF SRM 52-10-00 FIG 13 SHEET 2 AND INSTALLED DOU BLERS REF SRM 52-10-00 FIG 13 SHEET 2. 2 L 7 3 4F RT A22WE 1996042500083 19960425 00083 NM 1996 4 25 96FDEA00796 1 19960418 A 5311 FRAME DOUG MD11 MD11F 3023600 NM LT MLG WW CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 605FE 48514 LT MLG GEAR WELL DOOR UPPER FRAME CRACKED. LOCATED 12 INCHES FWD OF GEAR WELL DOOR ACTUATOR I/B STRUT FAIRING. STOP DR ILLED CRACK PER SRM 52-10-00, FABRICATED REPAIR DOUBLER PARTS REF SRM 52-10-00 AND INSTALLED REPAIR DOUBLERS REF SRM 52- 10-00 PAGE 46. 2 L 7 3 4F RT A22WE 1996042500084 19960425 00084 NM 1996 4 25 96FDEA00797 1 19960418 A 5280 SKIN DOUG MD11 MD11F 3023600 NM LT MLG DOOR BULGE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 605FE 48514 LT MLG GEAR WELL DOOR EXTERNAL SKIN BULGED ADJACENT TO CENTER HINGE SEGMENT, 52 INCHES FROM L/E OF DOOR. 2 L 7 3 4F RT A22WE 1996042500085 19960425 00085 NM 1996 4 25 96FDEA00798 1 19960418 A 5712 RIB DOUG MD11 MD11F 3023600 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 605FE 48514 RT WING L/E RIB HAS A VISUAL CRACK INDICATION AT THE LOWER RADIUS APPROX 1.5 INCH LONG ON XORSS562. 2 L 7 3 4F RT A22WE 1996042500086 19960425 00086 WP 1996 4 25 ARWA9604002 1 19960418 A 3211 5893930508N TRUNNION DOUG DC8 DC862 3021970 WP RT MLG CRACKED A ARWA K NONE O OTHER UK UNKNOWN 1 SO 19 802BN 45909 DURING RIGHT MLG REMOVAL, FOUND CRACKS IN TRUNNION FITTING LUGS. REPLACED TRUNNION (P/N 5893930-508N) PER DC-8 S/B 57-9 4. 2 L 7 4 4F 4A25 1996042500087 19960425 00087 EU 1996 4 25 COMA9630103 1 19960416 A 2436 51539007A GCU SAAB SF340 SF340A 7850100 EU LT DC GEN OUT OF ADJUST A COMA K NONE H ELECT. POWER LOSS-50 PC CR CRUISE 1 SO 01 341CA 13522 176 340A021 LEFT DC GENERATOR FAILED AND WOULD NOT RESET. ADJUSTED THE LT GENERATOR CONTROL UNIT. 2 L 7 2 4T RT A52EU 1996042500088 19960425 00088 EA 1996 4 25 COMA9660066 1 19960416 A 3242 5010520 BRAKE ASSY CNDAIR CL600 CL6002B19 EA RT MLG SMOKING A COMA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 957CA 7109 LARGE AMOUNT OF SMOKE COMING FROM RT MLG AFTER LANDING. REPLACED THE RT MLG OUTBD BRAKE ASSY. 2 L 7 2 4F RT A21EA 1996042500089 19960425 00089 EA 1996 4 25 COMA9660067 1 19960416 A 3411 PITOT CNDAIR CL600 CL6002B19 EA LEFT WATER CONTAM A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 949CA 7080 PILOTS AIRSPEED IS FLUCTUATING 20 KNOTS. DRAINED WATER FROM NR 1 PITOT SYSTEM. 2 L 7 2 4F RT A21EA 1996042500090 19960425 00090 NM 1996 4 25 DL72E960868 1 19960415 A 3397 WIRE BOEING 727 727247 138408F NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 831WA 21483 EMERGENCY TRACK LIGHTS INOP FROM 20ABC TO 27ABC. FOUND WIRES BROKEN AT 20ABC AND 27ABC. REPAIRED SAME, EMERGENCY TRACK LIGHTING SYSTEM OPS CHECKS GOOD. 2 L 7 3 4F A3WE 1996042500091 19960425 00091 NM 1996 4 25 DL72L960878 1 19960416 A 3350 1000679 LIGHT BOEING 727 727232 1384082 NM FWD ENTRY DOOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 505DA 21307 FWD ENTRY OVERHEAD EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY, CKS GOOD. 2 L 7 3 4F A3WE 1996042500092 19960425 00092 NM 1996 4 25 DL72L960905 1 19960417 A 2752 ACTUATOR BRACKET BOEING 727 727232 1384082 NM NR 5 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 509DA 21311 FOUND ON D-1 LETTER CK, .5 INCH CRACK IN NR 5 L/E FLAP ACTUATOR I/B SUPPORT BRACKET. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1996042500093 19960425 00093 NM 1996 4 25 DL72P960825 1 19960401 A 5720 BEAM BOEING 727 727225 1384077 NM LT WING CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 NR 4 FLAP TRACK TO SPOILER BEAM HAS CORROSION EMANATING FROM MATING SURFACE. REMOVED CORROSION. 2 L 7 3 4F A3WE 1996042500094 19960425 00094 NM 1996 4 25 DL72P960865 1 19960415 A 5754 COVE SKIN BOEING 727 727225 1384077 NM NR 3 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8891Z 21860 FOUND ON C-CHECK, NR 3 SLAT LWR COVE SKIN ATTACH ANGLE IS CRACKED AT I/B STOP PAD. REPAIRED PER M/M 57-54-0. 2 L 7 3 4F A3WE 1996042500095 19960425 00095 NM 1996 4 25 DL72P960866 1 19960415 A 5754 ANGLE BOEING 727 727225 1384077 NM NR 2 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8891Z 21860 FOUND ON C-CHECK, NR 2 SLAT COVE SKIN LWR ATTACH ANGLE IS CRACKED AT TIA DUCT. REPAIRED PER M/M 57-54-0. 2 L 7 3 4F A3WE 1996042500096 19960425 00096 NM 1996 4 25 DL72P960867 1 19960415 A 5754 ANGLE BOEING 727 727225 1384077 NM NR 7 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8891Z 21860 FOUND ON C-CHECK, NR 7 SLAT COVE SKIN LWR ATTACH ANGLE IS CRACKED. REPAIRED PER M/M 57-54-0. 2 L 7 3 4F A3WE 1996042500097 19960425 00097 NM 1996 4 25 DL72P960877 1 19960402 A 5320 FRAME BOEING 727 727225 1384077 NM CARGO DR OPENING CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 DURING THE MODIFICATION OF THE NR 2 CARGO DOOR OPENING FWD FRAME PER EO 4-61247-3AD, CORROSION WAS FOUND NEAR THE LWR ST OP FITTING. DAMAGE CUT OUT IS WITHIN REPAIRABLE AREA PER SB 727-53A0199. ACCOMPLISHED REPAIRS PER DL ERA 303392-14AD. 2 L 7 3 4F A3WE 1996042500098 19960425 00098 NM 1996 4 25 DL72S960814 1 19960409 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 3 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 544DA 22493 FOUND ON A-1 LETTER CHECK, 1.5 INCH CRACK IN NR 3 L/E SLAT LWR COVE SKIN ANGLE. REPAIRED PER M/M 57-54-0. 2 L 7 3 4F A3WE 1996042500099 19960425 00099 NM 1996 4 25 DL72S960838 1 19960411 A 3350 BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 538DA 22076 EMERGENCY LIGHT OVER L1 DOOR INOP. REPLACED BATTERY PACK MFR NR 3106 DAL 334101877, BATTERY WEAK. 2 L 7 3 4F A3WE 1996042500100 19960425 00100 NM 1996 4 25 DL72S960841 1 19960405 A 5240 SKIN BOEING 727 727232 1384082 NM R2 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 498DA 21142 AT MID-VISIT, THE R2 DOOR UPPER HINGE ARM CUTOUT WAS FOUND TO BE CRACKED. THE DAMAGE WAS ROUTED OUT AND A DOUBLER PREPA RED AND INSTALLED PER SRM 52-40-2. 2 L 7 3 4F A3WE 1996042500101 19960425 00101 NM 1996 4 25 DL72S960842 1 19960405 A 5240 FRAME BOEING 727 727232 1384082 NM R2 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 498DA 21142 AT MID-VISIT, THE R2 DOOR FRAME WAS FOUND CRACKED JUST BELOW UPPER HINGE CUTOUT. THE DAMAGE WAS ROUTED OUT AND DOUBLER PREPARED AND INSTALLED PER SRM 52-40-2. 2 L 7 3 4F A3WE 1996042500102 19960425 00102 NM 1996 4 25 DL72S960843 1 19960411 A 5320 ANGLE BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 407DA 21151 FOUND ON E-2 LETTER CHECK, LWR T-ANGLE CRACKED AT AFT HINGE FOR LWR FUS PANEL 3448R. REPAIRED PER M/M 53-30-1 PG 807. 2 L 7 3 4F A3WE 1996042500103 19960425 00103 NM 1996 4 25 DL72S960848 1 19960412 A 5400 SKIN BOEING 727 727232 1384082 NM NR 2 ENG CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 533DA 22046 A 1 INCH CRACK IN NR 2 ENG INLET OUTER SKIN LT SIDE 8 O'CLOCK POSITION APPROX 36 INCHES AFT OF L/E. INSTALLED DOUBLER P ER SRM 55-30-0. 2 L 7 3 4F A3WE 1996042500104 19960425 00104 NM 1996 4 25 DL72S960849 1 19960412 A 5530 STRINGER BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 533DA 22046 A .75 INCH CRACK IN VERT STAB STR 7 AT 3RD BULKHEAD ABOVE OPENING TO CRAWLWAY. REPAIRED PER M/M 55-30-0. 2 L 7 3 4F A3WE 1996042500105 19960425 00105 NM 1996 4 25 DL72S960850 1 19960412 A 5320 WEB BOEING 727 727232 1384082 NM BS 1213 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 533DA 22046 A .375 INCH CRACK IN LT LOWER TORQUE BOX VERTICAL WEB UPPER FWD END STA 1213. REPAIRED PER M/M 53-11-0. 2 L 7 3 4F A3WE 1996042500106 19960425 00106 NM 1996 4 25 DL72S960851 1 19960412 A 5320 WEB BOEING 727 727232 1384082 NM BS 1228 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 533DA 22046 LOWER LT TORQUE BOX VERTICAL WEB CRACKED BEYOND ROUTED OUT REPAIR, UPPER LIGHTENING HOLE STA 1228. REPAIRED PER M/M 53- 11-0 PG 828. 2 L 7 3 4F A3WE 1996042500107 19960425 00107 NM 1996 4 25 DL72S960863 1 19960415 A 3310 69162688 LIGHT PANEL BOEING 727 727232 1384082 NM FE PANEL SMOKING A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 532DA 22045 PRIOR TO DEPARTURE WITH PSGRS ON BOARD, B-SYS STBY HYD PANEL WAS SMOKING. PSGRS WERE DEPLANED IN A NORMAL MANNER. FOUN D BACKGROUND LIGHTING PANEL DAMAGED. REPLACED PANEL ASSEMBLY. 2 L 7 3 4F A3WE 1996042500108 19960425 00108 NM 1996 4 25 DL72S960872 1 19960416 A 5754 65162231 RIB BOEING 727 727232 1384082 NM NR 2 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 402DA 21146 THE 3RD RIB WAS FOUND CRACKED. REPAIRED RIB PER MM 57-54-0, FOR NR 2 L/E SLAT. 2 L 7 3 4F A3WE 1996042500109 19960425 00109 NM 1996 4 25 DL72S960873 1 19960416 A 5754 65162231 SLAT BOEING 727 727232 1384082 NM NR 2 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 402DA 21146 THE INNR SKIN WAS FOUND CRACKED BY THE TELESCOPING ANTI-ICE DUCT. REPAIRED INNR SKIN PER SRM 57-50-3, FOR NR 2 L/E SLAT . 2 L 7 3 4F A3WE 1996042500110 19960425 00110 NM 1996 4 25 DL72S960874 1 19960416 A 5754 65162231 RIB BOEING 727 727232 1384082 NM NR 2 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 402DA 21146 RIB MARKED NR 14 WAS FOUND CRACKED IN THE LOWER RADIUS NEAR ATTACH ANGLE. THE NOTED RIB WAS REPAIRED IN COMPLIANCE WITH MM 57-54-0 FIGURE 805, FOR NR 2 L/E SLAT. 2 L 7 3 4F A3WE 1996042500111 19960425 00111 NM 1996 4 25 DL72S960875 1 19960412 A 5330 6554566 SKIN BOEING 727 727232 1384082 NM BS 500-520 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 407DA 21151 CORROSION WAS REMOVED AT STR 28R BETWEEN BS 500 AND BS 520, RESULTING IN A 5.5 BY 2.25 CUT OUT. THERE IS AN EXISTING ST RINGER SPLICE AT BS 490 AND A NEW SPLICE BEING INSTALLED AT BS 510 PER B727 SRM. THE SKIN IS MANUFACTURED FROM MACHINED CLAD 2024-T3 WITH A LOCAL THICKNESS OF .090. AN EXTERNAL REPAIR DOUBLER WAS INSTALLED PER DL ERA 303440-14. 2 L 7 3 4F A3WE 1996042500112 19960425 00112 NM 1996 4 25 DL72S960876 1 19960412 A 5330 65545662 SKIN BOEING 727 727232 1384082 NM BS 520-540 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 407DA 21151 CORROSION DAMAGE WAS REMOVED FROM AROUND THE HOLE CUTOUT FOR THE RADIO ALTIMETER ANTENNA BETWEEN STATION 520 AND STATION 540, BETWEEN STRINGER 28 LEFT AND STRINGER 29 RIGHT. THE SKIN IS MACHINED CLAD 2024-T3 SHEET WITH A LOCAL THICKNESS OF 0.090 THICK. AN INTERNAL REPAIR DOUBLER WILL BE INSTALLED. DURING THE LETTER CHECK ON 4/12/96, ADDITIONAL CORROSION W AS FOUND IN THE FUSELAGE SKIN AT STA 540 AND STR 28L. DAMAGE REMOVAL RESULTED IN A CUT OUT MEASURING 2 BY 2.625. DUE T O TIME CONSTRAINTS ON THE LETTER CHECK VISIT, A TIME LIMITED REPAIR WAS INSTALLED PER DL ERA 259289-14. 2 L 7 3 4F A3WE 1996042500113 19960425 00113 NM 1996 4 25 DL72S960879 1 19960405 A 5210 DOUBLER BOEING 727 727232 1384082 NM L1 DOOR DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 498DA 21142 AT MID-VISIT, A TEMP REPAIR WAS FOUND TO BE INSTALLED ON THE TOP AFT CORNER OF THE L1 DOOR OUTER SKIN. THE DOUBLER WAS REMOVED AND REPAIR INSTALLED PER MM 52-11-01 FIG 804. 2 L 7 3 4F A3WE 1996042500114 19960425 00114 NM 1996 4 25 DL72S960880 1 19960416 A 5330 SKIN BOEING 727 727232 1384082 NM BS 1233 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 485DA 20865 FOUND ON B-1 LETTER CHECK, 1 INCH CRACK VERT WEB OF TORQUE BOX TOP ROW OF RIVETS LT SIDE AT STA 1233. REPAIRED PER M/M 53-11-0 PG 832. 2 L 7 3 4F A3WE 1996042500115 19960425 00115 NM 1996 4 25 DL72S960881 1 19960412 A 5512 SKIN BOEING 727 727232 1384082 NM HORIZ STAB DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 498DA 21142 AT MID-VISIT, THE HORIZ STAB PANEL NR 9215 WAS FOUND TO HAVE A HOLE IN THE TOP SURFACE. THE HOLE WAS REPAIRED PER SRM 5 5-10-2. 2 L 7 3 4F A3WE 1996042500116 19960425 00116 NM 1996 4 25 DL72S960882 1 19960416 A 5400 SKIN BOEING 727 727232 1384082 NM CTR ENGINE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 485DA 20865 FOUND ON B-1 LETTER CHECK, THREE .5 INCH CRACKS EXTENDING FROM FASTENERS FWD OF PANEL 9501 RT SIDE AND TWO .5 INCH CRACK S EXTENDING FROM FASTENERS BELOW PANEL 9501 RT SIDE. REPAIRED PER M/M 54-30-0 PG 801 AND 802. 2 L 7 3 4F A3WE 1996042500117 19960425 00117 NM 1996 4 25 DL72S960883 1 19960416 A 2782 ACT ATTACH BOX BOEING 727 727232 1384082 NM NR 2 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 485DA 20865 FOUND ON B-1 LETTER CHECK, 1 INCH CRACK NR 2 L/E FLAP ACT ATTACH BOX O/B SIDE. REPAIRED PER M/M 57-20-21. 2 L 7 3 4F A3WE 1996042500118 19960425 00118 NM 1996 4 25 DL72S960884 1 19960416 A 5720 STIFFENER BOEING 727 727232 1384082 NM RT WING LE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 485DA 20865 FOUND ON B-1 LETTER CHECK, 1 INCH CRACK VERT SPAR STIFFENER AT NR 7 O/B SLAT TRACK O/B ANGLE. REPLACED STIFFENER PER M/ M 57-20-21 PG 813. 2 L 7 3 4F A3WE 1996042500119 19960425 00119 NM 1996 4 25 DL72S960885 1 19960416 A 2782 ACT MOUNT BOX BOEING 727 727232 1384082 NM NR 5 LE FLAP CRACKED ANGLE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 485DA 20865 FOUND ON B-1 LETTER CHECK, NR 5 L/E FLAP ACT MOUNT BOX I/B LWR ANGLE CRACKED. REPAIRED PER M/M 57-20-21 PG 811. 2 L 7 3 4F A3WE 1996042500120 19960425 00120 NM 1996 4 25 DL72S960886 1 19960416 A 5720 STIFFENER BOEING 727 727232 1384082 NM LT WING LE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 485DA 20865 FOUND ON B-1 LETTER CHECK, VERT SPAR STIFFENER CRACKED AT NR 3 SLAT INBD TRACK O/B SIDE. REPLACED PER M/M 57-20-21. 2 L 7 3 4F A3WE 1996042500121 19960425 00121 NM 1996 4 25 DL72S960890 1 19960416 A 3350 BATTERIES BOEING 727 727232 1384082 NM L1 DOOR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 497DA 21077 EMERGENCY EXIT LIGHT AT L1 DOOR INOP. REPLACED BATTERIES, CKS GOOD. 2 L 7 3 4F A3WE 1996042500122 19960425 00122 NM 1996 4 25 DL72S960899 1 19960416 A 5542 SKIN BOEING 727 727232 1384082 NM RUDDER CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 485DA 20865 FOUND ON B1 LETTER CHECK, UPPER RUDDER OUTER SKIN CRACKED 3 INCH RT SIDE, 1 FT FROM TOP CENTER. INSTALLED DOUBLER PER S RM 55-40-2 FIG 1. 2 L 7 3 4F A3WE 1996042500123 19960425 00123 NM 1996 4 25 DL72W960809 1 19960409 A 2612 FIRE DETECTOR BOEING 727 7272Q8 138407W NM AFT LAV FAILED A DALA K NONE N FALSE WARNING CR CRUISE 1 SO 27 831L 21826 PILOT REPORT, AFT LAV FIRE DETECTOR GIVES FIRE INDICATION WITH NO EVIDENCE OF FIRE OR SMOKE. REPLACED DETECTOR AFT LAV , TEST NORMAL. 2 L 7 3 4F A3WE 1996042500124 19960425 00124 NM 1996 4 25 DL72W960835 1 19960410 A 5522 SKIN BOEING 727 727247 138408F NM LT ELEVATOR PUNCTURE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 295WA 22532 A .25 INCH LONG PUNCTURE HOLE IN LOWER SKIN OF LT ELEVATOR, 14 INCHES AFT OF NR 2 BALANCE BOARD. INSTALLED DOUBLER PER SRM 55-20-3 FIG 4, RECALCULATE BALANCE PER SRM 51-80-7. 2 L 7 3 4F A3WE 1996042500125 19960425 00125 NM 1996 4 25 DL72W960869 1 19960327 A 3350 900835A BATTERY PACK BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 290WA 22108 ON SERVICE CHECK, FOUND OVERWING EXIT SIGNS RIGHT SIDE INOP. REPLACED BATTERY PACK M1086, CHECKS OK. 2 L 7 3 4F A3WE 1996042500126 19960425 00126 NM 1996 4 25 DL73E960846 1 19960411 A 3350 POWER SUPPLY BOEING 737 737247 138448D NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 376DL 23603 RIGHT AFT EXIT DOOR SLIDE LIGHT FOUND INOP ON SERVICE CHECK. ALSO, LEFT FWD SLIDE LIGHT INOP. RELAMPED LEFT FWD SLIDE LIGHT WITH BULB 1519. REPLACED FAULTY POWER SUPPLY FOR AFT RIGHT SLIDE LIGHT. 2 L 7 2 4F A16WE 1996042500127 19960425 00127 NM 1996 4 25 DL73E960901 1 19960417 A 3350 LIGHT BOEING 737 7372S3 NM CABIN MALFUNCTIONED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 369DL 21776 FORWARD ENTRY DOOR EMERGENCY LIGHT COMES ON WHEN SWITCH NOT ARMED AND AIRCRAFT POWER OFF. REPLACED LIGHT ASSEMBLY (P/N 10-0067-7). 2 L 7 2 4F RT A16WE 1996042500128 19960425 00128 NM 1996 4 25 DL73S960811 1 19960409 A 3230 GEAR MODULE BOEING 737 737232 1384475 NM LANDING GEAR MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 27 321DL 23093 UNABLE TO RETRACT LANDING GEAR AFTER TAKEOFF FROM CVG. ALSO, T/R REV ILLUM MSG ON IN FLT. REPLACED LANDING GEAR MODULE AND CKD PER M/M CHAP 32 AND RESERVICED RT MAIN STRUT, JACKED A/C AND CKS OK. 2 L 7 2 4F RT A16WE 1996042500129 19960425 00129 NM 1996 4 25 DL73S960840 1 19960411 A 3350 TRACK LIGHT BOEING 737 737232 1384475 NM CABIN CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 302DL 23047 ON LAYOVER, FOUND FLOOR TRACK TOP COVER CRACKED BETWEEN ROWS 15 AND 18. REPLACED TOP TRACK BETWEEN ROWS 15 AND 18. 2 L 7 2 4F RT A16WE 1996042500130 19960425 00130 NM 1996 4 25 DL73S960904 1 19960416 A 3230 NAS41046 BOLT BOEING 737 737232 1384475 NM NOSE GEAR LOOSE A DALA L ABORTED APPROACH J WARNING INDICATION LD LANDING 1 SO 27 308DL 23080 ON ARRIVAL, A/C HAD NOSE GEAR UNSAFE LIGHT. CYCLED GEAR SEVERAL TIMES, NO HELP. A/C MADE UNEVENTFUL LANDING. FOUND OVER CENTER MECH STOP BLOCK ATTACH BOLT BACKED OUT, PREVENTING OVER CENTER LINKS FROM FULLY LOCKING. RESECURED STOP BLO CK BOLT, MADE SEVERAL NOSE GEAR RETRACTIONS AND ALL IND NOW NORMAL. 2 L 7 2 4F RT A16WE 1996042500131 19960425 00131 NM 1996 4 25 DL757960836 1 19960410 A 3350 LIGHT BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 632DL 23613 FWD RIGHT OVERWING EMERGENCY EXIT TRACK LIGHT SIGN INOP. REPLACED LIGHT ASSY, OPN OK. 2 L 7 2 4F RT A2NM 1996042500132 19960425 00132 NM 1996 4 25 DL757960858 1 19960413 A 2120 AIR DIST BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE CABIN ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 650DL 24390 716408 SMOKE DET IN AFT CABIN WENT OFF WITH PUNGENT ODOR THROUGHOUT ACFT. ODOR SUBSIDED AND DETECTORS CEASED ALARM. F/A SEARC H FOUND NO SOURCE OR CAUSE. FLT CONTINUED MTC. CHECKED CABIN AT TIME OF ARRIVAL, NO SMOKE NOTED ANYWHERE. NR 1 ENG WA SH PERFORMED THE NIGHT PRIOR. 2 L 7 2 4F 4 F RT A2NM E17NE 1996042500133 19960425 00133 NM 1996 4 25 DL757960860 1 19960414 A 3350 LIGHT BOEING 757 757232 1384965 NM 2R DOOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 640DL 23994 DOOR 2R SLIDE LIGHT INOP. REPLACED S10220 AND S10221 DOOR 2R SLIDE LIGHT, CHECKS NORMAL. 2 L 7 2 4F RT A2NM 1996042500134 19960425 00134 NM 1996 4 25 DL757960861 1 19960414 A 2910 HYD LINE BOEING 757 757232 1384965 NM MLG LOCK ACT LEAKING A DALA K NONE J K WARNING INDICATION FLUID LOSS LD LANDING 1 SO 27 667DN 25035 ON SHORT FINAL, LOST A-SYSTEM QUANTITY, DECREASED NWY TO .13 WITH ALL RESULTING INDICATIONS. REPLACED LEFT MLG OVER CEN TER ACTUATOR RETURN LINE WITH AN INTERIM FLEXIBLE LINE, SERVICED. 2 L 7 2 4F RT A2NM 1996042500135 19960425 00135 NM 1996 4 25 DL76S960802 1 19960408 A 3350 TRACK LIGHT BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 127DL 24077 EMERGENCY TRACK LIGHT AT 32AB AND 41AB OUT. RELAMPED, OPERATION NORMAL. 2 L 7 2 4F RT A1NM 1996042500136 19960425 00136 NM 1996 4 25 DL76S960803 1 19960408 A 3350 POWER SUPPLY BOEING 767 767332 1382001 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 127DL 24077 OVERHEAD EMERGENCY LIGHTS FROM 17AB TO 36AB OUT AND TWO OVERHEAD EXIT SIGNS OUT. REPLACED POWER SUPPLY, OPERATION NORMA L. 2 L 7 2 4F RT A1NM 1996042500137 19960425 00137 NM 1996 4 25 DL76S960908 1 19960402 A 5754 114T4105 TE WEDGE BOEING 767 767332 1382001 NM NR 5 LE FLAP DELAMINATION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 120DL 23279 THE NR 5 LEADING EDGE SLAT TRAILING EDGE WEDGE WAS FOUND TO HAVE UPPER SKIN DELAMINATED. THE DELAMINATED AREA IS APPROX 3 INCH BY 3 INCH AND IS LOCATED AT THE INBOARD AFT END OF THE TRAILING EDGE. ACCOMPLISHED REPAIRS PER DL ERA 273577-14 AD. 2 L 7 2 4F RT A1NM 1996042500138 19960425 00138 NM 1996 4 25 DL76S960917 1 19960409 A 5754 114T410529A TE WEDGE BOEING 767 767332 1382001 NM NR 5 LE SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 127DL 24077 THE NR 5 SLAT T/E WEDGE WAS FOUND DELAMINATED. THE DAMAGE WAS TRIMMED OUT AND REPAIRED PER THE B-767-300 SRM 51-70-10 F IG 9 PARAGRAPH 2K. 2 L 7 2 4F RT A1NM 1996042500139 19960425 00139 WP 1996 4 25 DLL10960847 1 19960412 A 3350 POWER SUPPLY LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1732D 193C1213 AISLE EMERGENCY LIGHT OUT ABOVE 6B. REPLACED POWER SUPPLY, OPERATION NORMAL. 2 L 7 3 4F A23WE 1996042500140 19960425 00140 WP 1996 4 25 DLL10960887 1 19960417 A 3350 5165741 PWR SUPPLY LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 728DA 193C1173 NR 1 RT DOOR EMERGENCY SLIDE LIGHT INOP. REPLACED POWER SUPPLY, OPERATION NORMAL. 2 L 7 3 4F A23WE 1996042500141 19960425 00141 WP 1996 4 25 DLL10960888 1 19960417 A 3350 5165741 BATTERY PACK LKHEED 1011 10113851 5265010 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 735D 193C1226 CABIN EMERGENCY LIGHTS WOULDN'T STAY ON REQUIRED TIME. REPLACED BATT PACK, OPN CKS NORMAL. 2 L 7 3 4F A23WE 1996042500142 19960425 00142 WP 1996 4 25 DLL10960889 1 19960417 A 3350 5165741 POWER SUPPLY LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 735D 193C1226 WHILE WORKING OPN NR 78100 ITEM 2 STEP 9, PACKS FAIL TO ILLUMINATE EMERGENCY LIGHTS FOR TEN MINUTES. REPLACED POWER SUP PLY, OPERATION NORMAL. 2 L 7 3 4F A23WE 1996042500143 19960425 00143 WP 1996 4 25 DLL10960910 1 19960330 A 5312 1504400 BULKHEAD LKHEED 1011 10113851 5265010 WP FS 1212 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 728DA 193C1173 WHILE PERFORMING THE FS 1212 CANTED BULKHEAD INSPECTION PER SI 7-70645-12, A CRACK WAS FOUND AT LBL 10.0. THE CRACK WAS TRIMMED OUT AND REPAIRED PER DL ERA 273562-14. 2 L 7 3 4F A23WE 1996042500144 19960425 00144 WP 1996 4 25 DLL13960845 1 19960412 A 2622 HALON FIRE BOTT LKHEED 1011 10113851 5265010 WP LOWER GALLEY DISCHARGED A DALA F ACTIVATE FIRE EXT. A FLAME/FIRE CR CRUISE 1 SO 27 786DL 193A1123 HALON FIRE BOTTLE ON CAPTS SIDE, USED IN LOWER GALLEY, SMALL FOOD TRAY FIRE. REPLACED HALON BOTTLE, INSPECTED OVENS AND ALL CHECK NORMAL. SUSPECT PART OF FOOD WRAPPER INADVERTENLY LEFT ON TRAY. 2 L 7 3 4F A23WE 1996042500145 19960425 00145 WP 1996 4 25 DLL13960859 1 19960414 A 3350 TRACK COVERS LKHEED 1011 10113851 5265010 WP CABIN CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 786DL 193A1123 FWD LT AND RT EMERGENCY TRACK LIGHT COVERS CRACKED IN FIRST CLASS. REPLACED BAD TRACK, CHECKED GOOD. 2 L 7 3 4F A23WE 1996042500146 19960425 00146 WP 1996 4 25 DLL14960902 1 19960417 A 5753 1529517113 SKIN LKHEED 1011 1011385115 5265015 WP NR 3 TE VANE WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1739D 193C1237 NR 3 FLAP VANE UPPER SKIN WAS FOUND WITH EXCESSIVE WEAR ON THE ENTIRE LENGTH. THE NOTED SKIN WAS REPAIRED PER SRM 57-53 -00 PG 831. 2 L 7 3 4F A23WE 1996042500147 19960425 00147 WP 1996 4 25 DLL15960916 1 19960315 A 5753 1529518110 FITTING LUG LKHEED 1011 10113853 5265020 WP NR 4 FLAP VANE OVERSIZED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 751DA 193W1166 DURING SI REWORK, THE NR 4 FLAB VANE I/B FITTING LUG WAS OVERSIZED. A BUSHING WAS INSTALLED PER DL ERA 357239-14AD. 2 L 7 3 4F A23WE 1996042500148 19960425 00148 WP 1996 4 25 DLL17960907 1 19960304 A 5711 1605415 REAR SPAR LKHEED 1011 10113853 5265020 WP LT/RT WING FATIGUE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 766DA 193H1207 DURING THE ACCOMPLISHMENT OF EO 7-59089-3AD, CRACKS WERE FOUND EMANATING FROM EXISTING FASTENER HOLES BETWEEN IWS 293.58 -346 ON THE LT AND RT WING. THE CRACKS WERE FOUND IN THE REAR SPAR UPPER CAP, WEB, UPPER WING SKIN. THE SUBJECT FASTEN ER HOLES WERE OVERSIZED TO REMOVE CRACKS IN THE DAMAGED MEMBERS PER DL ERA 273404-14AD. 2 L 7 3 4F A23WE 1996042500149 19960425 00149 WP 1996 4 25 DLL17960933 1 19960322 A 5320 1512169101 FITTING LKHEED 1011 10113853 5265020 WP FS 901 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 767DA 193H1209 THE LOWER DOOR SILL INBOARD CAP FITTING AT FS 901, LEFT AND RIGHT HAND SIDES, WERE FOUND CORRODED AND REQUIRED REPL ACEMENT. THE NEW FITTINGS WILL BE M/F FROM 17-4 PH ANNEALED STAINLESS HEAT TREATED TO 160-180 KSI. REPLACEMENT APPROVA L PER DL ERA 273519-14/ 2 L 7 3 4F A23WE 1996042500150 19960425 00150 1996 4 25 DLM11960834 4 19960410 A 2210 AUTOPILOT DOUG MD11 MD11 3023602 NM NR 1/2 INOPERATIVE A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 806DE 48477 BOTH A/P INOP, NO CURRENT FAULTS. ACFT RETURNED ATL. PERFORMED RTS ON BOTH FCC, ALL NORMAL. 2 L 7 3 4F RT A22WE 1996042500151 19960425 00151 NM 1996 4 25 DLM88960844 1 19960412 A 3300 20131A BATTERY PACK DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 970DL 43173 ON LAYOVER, FOUND ALL EMERGENCY LIGHTS INOP IN AFT CABIN. REPLACED BATTERY PACK, ALL LIGHTS OP NORMAL. 2 L 7 2 4F RT A6WE 1996042500152 19960425 00152 NM 1996 4 25 DLM88960852 1 19960409 A 3350 BATTERY PACK DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 999DN 53371 EMERGENCY LIGHTS IN AFT CABIN INOP. REPLACED BATTERY PACK. 2 L 7 2 4F RT A6WE 1996042500153 19960425 00153 NM 1996 4 25 DLM88960853 1 19960412 A 3350 BATTERY PACK DOUG MD88 MD88 3023688 NM CABIN LOOSE IN RACK A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 915DL 49546 EMERGENCY PATH LIGHTS IN FIRST CLASS INOP. RESEATED BATTERY PACK. 2 L 7 2 4F RT A6WE 1996042500154 19960425 00154 NM 1996 4 25 DLM88960854 1 19960412 A 3350 CONNECTOR DOUG MD88 MD88 3023688 NM AFT AIRSTAIR LOOSE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 915DL 49546 EMERGENCY LIGHT SIGN IN AFT AIRSTAIR INOP. RESEATED PUSHED PINS IN QUICK DISCONNECT IN AFT COMPARTMENT. 2 L 7 2 4F RT A6WE 1996042500155 19960425 00155 NM 1996 4 25 DLM88960862 1 19960414 A 2170 SEPARATOR BAG DOUG MD88 MD88 3023688 NM CABIN DIRTY A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 959DL 49978 DURING CLIMB SEVERAL MINUTES AFTER TURNING ON ENG ANTI-ICE, BURNING ODOR WAS DETECTED AND FLT ATT AND PAX REPORTED FAINT SMOKE IN CABIN. CHECKED APU LT AND RT HYD SYS AND LT AND RT PACKS FOR LEAKS, NONE FOUND. ACMS BOTH FULL OF OIL PREFOR MED DUCT BURN OUT PER M/M 36-10-00 AND REPLACED BOTH WATER SEPARATOR BAGS, NO FUMES FROM LT OR RT PACKS WITH APU OR ENG ANTI-ICE ON OR OFF. 2 L 7 2 4F RT A6WE 1996042500156 19960425 00156 NM 1996 4 25 DLM88960891 1 19960416 A 3350 OL3071BEGPL BULB DOUG MD88 MD88 3023688 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 917DL 49573 ONE RED LIGHT OUT ON EMERGENCY TRACK LIGHTING F/O SIDE, ACROSS FROM AFT GALLEY. REPLACED ONE LIGHT BULB AND REPAIRED DA MAGED WIRING. 2 L 7 2 4F RT A6WE 1996042500157 19960425 00157 NM 1996 4 25 DLM88960892 1 19960416 A 2450 947F9463 BUSS PROTECT PNL DOUG MD88 MD88 3023688 NM E/E COMPT MALFUNCTIONED A DALA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 SO 27 966DL 53115 AFTER TAKEOFF, CROSS TIE LOCKOUT, GEN AND OR CROSSTIE RELAY CHATTER. TURNED OFF LEFT GEN, RETURNED DFW. REPLACED BUS P ROTECTION PANEL, OPERATION NORMAL. 2 L 7 2 4F RT A6WE 1996042500158 19960425 00158 NM 1996 4 25 DLM88960893 1 19960410 A 5311 59135953 FRAME DOUG MD88 MD88 3023688 NM BS 1418 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947DL 49878 THE UPPER FLANGE OF THE FUSELAGE FRAME AT FS 1418 AND LONGERON 2L WAS FOUND WITH TWO CRACKS. THE FIRST CRACK IS LOCATED IN THE FRAME RADIUS AND THE SECOND ON THE HORIZONTAL FLANGE PARALLEL TO THE FIRST CRACK. THE DAMAGE WAS TRIMMED OUT AN D FILLED PER DAL EO 9-63538-3. 2 L 7 2 4F RT A6WE 1996042500159 19960425 00159 NM 1996 4 25 DLM88960894 1 19960323 A 5311 9912246 FRAME DOUG MD88 MD88 3023688 NM BS 1382 DAMAGED A DALA K NONE O OTHER LD LANDING 1 SO 27 957DL 49976 THE LOWER LOBE OF THE FS 1382 FRAME WAS DAMAGED FROM A TAIL STRIKE BETWEEN L-21L AND L-24L. ALSO, BETWEEN L-18R AND L-2 1R. THE DAMAGE WAS REPLACED WITH FABRICATED PARTS PER DL ERA 273498-14. 2 L 7 2 4F RT A6WE 1996042500160 19960425 00160 NM 1996 4 25 DLM88960895 1 19960404 A 5330 59114123 SKIN DOUG MD88 MD88 3023688 NM BS 365-371 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947DL 49878 THE FUSELAGE SKIN AT FS 365 TO 371 AND BETWEEN L-19R AND 21R WAS PREVIOUSLY DENTED AND TIME-LIMITED REPAIRED. THE REPAI R WAS REMOVED AND A PERMANENT REPAIR WAS INSTALLED PER DL ERA 273591-14. 2 L 7 2 4F RT A6WE 1996042500161 19960425 00161 NM 1996 4 25 DLM88960896 1 19960401 A 5330 5924802133 SKIN DOUG MD88 MD88 3023688 NM BS 237 DENT A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947DL 49878 THE FUSELAGE SKIN IS DENTED AFT OF FS 237, 5 INCHES ABOVE THE L-18L CUSP. THE DENT IS APPROX .125 INCH DEEP, 4 INCHES L ONG, 2.5 INCHES WIDE. THE DAMAGE WAS CUT OUT AND A FILLER AND DOUBLER WAS INSTALLED PER DL ERA 273568-14. 2 L 7 2 4F RT A6WE 1996042500162 19960425 00162 NM 1996 4 25 DLM88960897 1 19960407 A 5312 5910130387 BLKHD TEE CAP DOUG MD88 MD88 3023688 NM BS 1338 DAMAGED A DALA K NONE O OTHER LD LANDING 1 SO 27 957DL 49976 THE LOWER TEE CAP SECTION OF THE AFT PRESSURE BULKHEAD AT FS 1338 WAS FOUND DAMAGED AND REQUIRED REPLACEMENT. THE DAMA GED TEE CAP WAS REMOVED AND REPLACED PER DL ERA 273379-14. 2 L 7 2 4F RT A6WE 1996042500163 19960425 00163 NM 1996 4 25 DLM88960900 1 19960417 A 3260 SWITCH DOUG MD88 MD88 3023688 NM FLT DECK FAILED A DALA O OTHER N FALSE WARNING TO TAKEOFF 1 SO 27 908DL 49539 RETRACTED THE LANDING GEAR AFTER TAKEOFF, RECEIVED LANDING GEAR WARNING AND ALL 3 RED UNSAFE LIGHTS WITH GEAR HANDLE UP. POM PROCEDURES CYCLED GEAR, NO HELP. GEAR HANDLE UP, 3 RED WARNING LIGHTS, GEAR DETERMINED TO BE UP. INSPECTED GEAR SYSTEMS, NO TROUBLE FOUND. ON SUBSEQUENT OCCURENCE INSPECTION, FOUND S1-320 SWITCH BAD IN RT THROTTLE SWITCH PACK R AND R RT SWITCH PACK AND ADJ PER MM, GEAR SWING NORMAL. 2 L 7 2 4F RT A6WE 1996042500164 19960425 00164 NM 1996 4 25 DLM88960909 1 19960331 A 5330 5953050 SKIN DOUG MD88 MD88 3023688 NM BS 313-332 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 941DL 49814 GROUND DAMAGE HAS BEEN TRIMMED OUT FROM JUST FORWARD OF FS 313 TO JUST AFT OF FS 332 AND FROM JUST ABOVE S-23 TO JUST BE LOW S-25. CUT OUT SIZE IS APPROX 15.5 INCHES HIGH AND 20 INCHES LONG. ACCOMPLISHED REPAIRS PER DL ERA 273564-14. 2 L 7 2 4F RT A6WE 1996042500165 19960425 00165 NM 1996 4 25 DLM88960912 1 19960325 A 5330 5930483 SKIN DOUG MD88 MD88 3023688 NM C3 DOOR CUTOUT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 973DL 53241 THE FUSELAGE SKIN AND UNDERLYING DOUBLER HAVE BEEN TORN/CRACKED AT THE AFT EDGE OF THE C-3 DOOR CUTOUT, AT THE NR 3 DOOR STOP. FURTHER DAMAGE WAS FOUND TO THE AFT EDGE OF THE C-3 DOOR CUTOUT BELOW THE NR 3 DOOR STOP. THE TOTAL SIZE OF THE DAMAGE IS APPROX 6 INCHES BY .625 INCH. ACCOMPLISHED REPAIRS PER DL ERA 268651-14 REV D. 2 L 7 2 4F RT A6WE 1996042500166 19960425 00166 NM 1996 4 25 DLM88960913 1 19960323 A 5330 5911406 SKIN DOUG MD88 MD88 3023688 NM FS 237 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 950DL 49881 THE FUSELAGE SKIN WAS FOUND TO BE BADLY DENTED AROUND FS 237 BETWEEN 18L AND 20L. THE DENT WAS CUT OUT AND A FILLER AND DOUBLER WAS INSTALLED PER DL ERA 273527. 2 L 7 2 4F RT A6WE 1996042500167 19960425 00167 NM 1996 4 25 DLM88960914 1 19960331 A 5330 5911406 SKIN DOUG MD88 MD88 3023688 NM FS 237 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947DL 49878 THE FUSELAGE SKIN WAS FOUND TO BE BADLY DENTED AROUND FS 237 AND BETWEEN 18L AND 20L. THE DENT WAS CUT OUT AND A FILLER AND DOUBLER WAS INSTALLED PER DL ERA 273565. 2 L 7 2 4F RT A6WE 1996042500168 19960425 00168 NM 1996 4 25 DLM88960915 1 19960303 A 5312 5910130285 BLKHD WEB DOUG MD88 MD88 3023688 NM BS 1338 DAMAGED A DALA K NONE O OTHER LD LANDING 1 SO 27 957DL 49976 THE P-DOME LOWER WEB AT STA 1338 WAS DAMAGED DURING A TAIL STRIKE INCIDENT. THE DAMAGE IN THE LOWER WEB WAS SPLICED PER DL ERA 273378-14. 2 L 7 2 4F RT A6WE 1996042500169 19960425 00169 NM 1996 4 25 DLM90960911 1 19960326 A 5330 5920323 SKIN DOUG MD90 MD9030 3023690 NM FS 261-286 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DA 53389 THE FUSELAGE SKIN WAS SEVERELY DENTED BETWEEN FS 261 AND FS 286 AND BETWEEN LONGERONS 25R AND 27R. THE FRAME FORMER SKI N ATTACH ANGLES AT FS 275. ALSO, ABOVE AND BELOW LONGERON 26R ARE BROKEN. REPAIRED GROUND DAMGE PER DL ERA 273532-14. 2 L 7 2 4F RT A6WE 1996042500170 19960425 00170 SW 1996 4 25 QXEA9600141 1 19960405 A 2120 AIR DISTR SWRNGN SA227 SA227AC 8780603 SW CABIN ODOR A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 09 385PH AC595 NUMBER TWO BLEED AIR HAS NOXIOUS ODOR. INSPECTED AND PLACED ON MEL 21-4. 2 L 7 2 4T RT A8SW 1996042500171 19960425 00171 NM 1996 4 25 QXEA9600142 1 19960406 A 2497 311627005 WIRE HARNESS DORNER DO32 DO328100 2996000 NM NR 2 ENGINE DEFECTIVE A QXEA O OTHER B H J SMOKE/FUMES/ODORS/SPARKS ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 NM 09 336PH 3014 THE RIGHT ENGINE SURGES FOLLOWED BY NR 2 AC GENERATOR FAILURE, FLASHING CAS MESSAGES AND SMOKE IN THE COCKPIT. GROUND R UN SHOWED SURGES ARE CAUSED BY ECU WIRING HARNESS AND SMOKE TO BE COMING FROM LABRINTH SEAL DRAINS. ENGINE SURGES CAUSE D AC GENERATOR TO DROP OFF LINE. REPLACED WIRING HARNESS IAW MAINT MANUAL. COMPLIED WITH RUNS IAW MAINT MANUAL AND ENG INE OPS CHECKED GOOD. BLEED AIR CHECKED GOOD. 2 H 7 2 4T RT A45NM 1996042500172 19960425 00172 EU 1996 4 25 QXEA9600143 1 19960408 A 3260 ROLLER FOKKER F28 F28MK1000 4990808 EU RT MLG OUT OF ADJUST A QXEA K NONE N FALSE WARNING CL CLIMB 1 NM 09 452US 11105 AFTER GEAR UP SELECTION, RT MAIN GEAR RED LIGHT REMAINED ON. COMPLIED WITH EMERGENCY CHECKLIST, CYCLED GEAR AND GEAR RE TRACTED NORMALLY, NO ABNORMAL INDICATIONS. AIRCRAFT FERRIED TO PDX. UPLOCK ROLLER ADJUSTED IAW MAINT MANUAL, GEAR SWIN G ACCOMPLISHED AND LIGHT CHECKED NORMAL WITH AND WITHOUT PRESSURE. 2 L 7 2 4F RT A20EU 1996042500173 19960425 00173 EU 1996 4 25 QXEA9600144 1 19960408 A 3260 BRACKET FOKKER F28 F28MK1000 4990808 EU RT MLG DOOR OUT OF ADJUST A QXEA K NONE J WARNING INDICATION CL CLIMB 1 NM 09 452US 11105 AFTER GEAR RETRACTION RIGHT MLG RED LIGHT REMAINED ON. GEAR WAS RECYCLED, LIGHT REMAINED ON. UTILITY SYSTEM HYDRAULIC PUMPS WERE TURNED TO OFFLOAD, NO GREEN LIGHT WITHIN 1 MINUTE. RIGHT MAIN GEAR DOOR UPLOCK BRACKET ADJUSTED IAW MAINT MA NUAL. RETRACTION AND EXTENSION CHECKED NORMAL PER MAINT TASK CARD. AIRCRAFT RELEASED FOR TEST FLIGHT. TEST FLIGHT WAS SATISFACTORY. 2 L 7 2 4F RT A20EU 1996042500174 19960425 00174 NM 1996 4 25 QXEA9600145 1 19960408 A 3350 OL3071BPEGPL LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 817PH 56 RIGHT HAND FORWARD EMERGENCY EXIT LIGHT IS INOP. SOCKET AND LAMP WERE REPLACED AND LIGHT OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 1996042500175 19960425 00175 NM 1996 4 25 QXEA9600147 1 19960413 A 3350 6038441 POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM COAT CLOSET SHORTED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 09 811PH 23 BURNT ELECTRICAL SMELL COMING FROM COCKPIT AND COAT CLOSET AREA. LOWER EMERGENCY LIGHT POWER SUPPLY IN THE COAT CLOSET REPLACED. POWER SUPPLY OPS, CHECKED GOOD. 2 H 7 2 4T RT A13NM 1996042500176 19960425 00176 NM 1996 4 25 QXEA9600148 1 19960413 A 3350 6038441 POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM COAT CLOSET FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 811PH 23 EMERGENCY LIGHT POWER SUPPLY IN COAT CLOSET THE LOWER PACK FAILED SHORTLY AFTER INSTALLATION. POWER SUPPLY AND BATTERY REPLACED AND POWER SUPPLY, OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 1996042500177 19960425 00177 1996 4 25 QXEA9600149 4 19960414 A 2565 S130508 SLIDE FOKKER F28 F28MK1000 4990808 EU GALLEY LOW PRESS A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 450US 11101 EVACUATION SLIDE BOTTLE PRESSURE IS OUT OF THE GREEN ARC .SLIDE WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996042500178 19960425 00178 NM 1996 4 25 QXEA9600150 1 19960416 A 3350 6038441 POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM COAT CLOSET INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 811PH 23 SEVERAL EMERGENCY LIGHTS FAILED TO ILLUMINATE. UPPER POWER SUPPLY IN COAT CLOSET REPLACED, LIGHT OPS CHECKED GOOD. AIR CRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1996042500179 19960425 00179 EU 1996 4 25 QXEA9600151 1 19960418 A 3350 312003 FUSE GRIMES 6008905 FOKKER F28 F28MK1000 4990808 EU BATTERY PACK FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 457US 11036 ENTRANCE WAY EXIT SIGN EVAC LIGHT BULBS ARE INOP. FUSE WAS REPLACED IN BATTERY PACK, LIGHTS OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996042500180 19960425 00180 EU 1996 4 25 QXEA9600152 1 19960418 A 3350 1315 BULB FOKKER F28 F28MK1000 4990808 EU GALLEY FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 802PH 11017 LOWER EVAC LIGHT BY SERVICE/EMERGENCY DOOR IS OUT. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996042500181 19960425 00181 EU 1996 4 25 QXEA9600153 1 19960418 A 3350 1315 BULB FOKKER F28 F28MK1000 4990808 EU GALLEY FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 452US 11105 BOTTOM EMERGENCY LIGHT AT SERVICE/EMERGENCY DOOR DOESN'T ILLUMINATE. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996042500182 19960425 00182 NM 1996 4 25 SCNA96047 1 19960410 A 5347 BAC15205841 SEAT TRACK BOEING 727 7272J4 1384006 NM BS 1050-1090 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 THE AFT CARGO COMPARTMENT SEAT TRACK UPPER SIDE EDGES AND AROUND SCREW HOLES HAVE CORROSION. MECHANICALLY REMOVED CORRO SION FROM STATIONS 1030 TO 1050 AND STATIONS 1090 TO 1130, MATERIAL LOSS LESS THAN .002. FABRICATED AND INSTALLED A NEW SECTION FROM STATION 1050 TO 1090 IAW B727, SRM 53-10-05 FIGURE 1. 2 L 7 3 4F RT A3WE 1996042500183 19960425 00183 NM 1996 4 25 SCNA96048 1 19960410 A 5320 INTERCOSTAL BOEING 727 7272J4 1384006 NM BS 1030-1110 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 INTERCOSTAL FLOOR SUPPORT WAS FOUND CORRODED. MECHANICALLY REMOVED CORROSION, TREATED AND PRIMED AREA. FABRICATED AND INSTALLED REPAIR STRAPS IAW B727 SRM 51-40-04. 2 L 7 3 4F RT A3WE 1996042500184 19960425 00184 NM 1996 4 25 SWAA960210 1 19960413 A 8012 979102 START VALVE BOEING 737 7372H4 138448C NM NR 1 FAILED A SWAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 90SW 22905 ON CLIMBOUT, NUMBER 1 ENGINE START VALVE LIGHT ILLUMINATED, UNABLE TO RESET. PERFORMED ENGINE SHUTDOWN CHECKLIST AND AI RCRAFT RETURNED AND MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED START VALVE PER BOEING M/M. 2 L 7 2 4F A16WE 1996042500185 19960425 00185 NM 1996 4 25 SWAA960211 1 19960411 A 3260 SENSOR BOEING 737 7373H4 1384600 NM LANDING GEAR OUT OF ADJUST A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 351SW 24572 ON CLIMBOUT, CREW HAD TO USE OVERRIDE TRIGGER TO RAISE GEAR HANDLE, GEAR EXTENDED NORMALLY. AIRCRAFT RETURNED TO SLC AN D MADE AN UNEVENTFUL LANDING. AIRCRAFT MX FERRIED TO PHX, ADJUSTED GROUND SHIFT SENSOR PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996042500186 19960425 00186 NM 1996 4 25 SWAA960212 1 19960413 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED 1/4 D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E S15R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996042500187 19960425 00187 NM 1996 4 25 SWAA960213 1 19960414 A 5312 BULKHEAD BOEING 737 7372H4 138448C NM CONTROL CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED C3 CHECK, FOUND BULKHEAD SKIN CRACKED AT CONTROL CABIN LEFT SIDE, 6 INCHES UP FROM FLOOR AND 6 INCHES F ROM O/B EDGE. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996042500188 19960425 00188 NM 1996 4 25 SWAA960214 1 19960414 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 349 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 83SW 22732 DURING SCHEDULED D-CHECK, FOUND LEFT FRAME CRACKED AT BS 349 WL 225. REPLACED FRAME CHORD PER BOEING SRM. 2 L 7 2 4F A16WE 1996042500189 19960425 00189 NM 1996 4 25 SWAA960215 1 19960414 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 294 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 83SW 22732 DURING SCHEDULED D-CHECK, FOUND L-ANGLE CRACKED AT BS 294 RBL 55 WL 208. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996042500190 19960425 00190 NM 1996 4 25 SWAA960216 1 19960414 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 289 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 83SW 22732 DURING SCHEDULED D-CHECK, FOUND L-ANGLE CRACKED FWD OF SERVICE DOOR AT BS 289 WL 248. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996042500191 19960425 00191 NM 1996 4 25 SWAA960217 1 19960414 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 302 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 83SW 22732 DURING SCHEDULED D-CHECK, FOUND L-ANGLE CRACKED AT BS 302 AT S10L. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996042500192 19960425 00192 NM 1996 4 25 SWAA960218 1 19960414 A 3350 6104781 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED TERMINAL CHECK, FOUND AFT SECTION OF CABIN FLOOR TRACK LIGHTING INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F A16WE 1996042500193 19960425 00193 NM 1996 4 25 SWAA960219 1 19960411 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 750 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED 1/4 D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, 1.5 INCH LENGTH. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996042500194 19960425 00194 NM 1996 4 25 SWAA960220 1 19960411 A 5320 JAMB BOEING 737 7373H4 1384600 NM EXT POWER DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 391SW 27378 DURING SCHEDULED C-CHECK, FOUND EXTERNAL POWER DOOR JAMB CRACKED, 1.5 INCH LENGTH. REPAIRED PER SWA RA 1-353-1447. 2 L 7 2 4F RT A16WE 1996042500195 19960425 00195 WP 1996 4 25 UPS96205987 1 19960412 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT REARSPAR LEAKING A IPXA K NONE O OTHER CR CRUISE 1 SO 01 803UP 46073 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED REAR SPAR LEAKING ALONG LT SIDE 57 TO 88, BETWEEN REAR SPAR CAP AND WING SKIN . REPAIRED BUSHINGS, LT WING SKI FITTING. 2 L 7 4 4F RT 4A25 1996042500196 19960425 00196 WP 1996 4 25 UPS96205988 1 19960412 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER CR CRUISE 1 SO 01 803UP 46073 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT WING T/E PNL CRACKED AND LIFTING FWD OF NR 1 SPOILER I/B HINGE. REPAIRED T/E PNL AT HINGE FITTING CUTOUT IAW UPS EO DC8-57-0654. 2 L 7 4 4F RT 4A25 1996042500197 19960425 00197 WP 1996 4 25 UPS96205989 1 19960412 A 5315 FLOOR BEAM DOUG DC8 DC873F 302199F WP BS 1540 CORRODED A IPXA K NONE O OTHER CR CRUISE 1 SO 01 803UP 46073 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED AFT ACCESSORY COMP FLOOR BEAM STA 1540 LT SIDE CORRODED AT TOP. REPAIRED FUS ELAGE STA 1540 FLOOR BEAM THAT WAS CORRODED BEYOND 50 PERCENT IAW UPS EO DC8-53-1605. 2 L 7 4 4F RT 4A25 1996042500198 19960425 00198 NM 1996 4 25 UPS96205991 1 19960416 A 5220 ESCAPE ROPE DOOR BOEING 727 72725C 138400H NM COCKPIT OUT OF ADJUST A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 MAINTENANCE REPORTED, ESCAPE ROPE DOOR ON CAPT'S SIDE WILL NOT STAY CLOSED. TRIMMED DOOR SO AS TO NOT INTERFERE WITH LA TCHING MECHANISM. CYCLED DOOR SEVERAL TIMES, DOOR OPENS, CLOSES AND LOCKS GOOD. 2 L 7 3 4F A3WE 1996042500199 19960425 00199 NM 1996 4 25 UPS96205992 1 19960416 A 3350 BATTERIES BOEING 727 72727C 138400J NM COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 910UP 19117 MAINTENANCE REPORTED, EMERGENCY EXIT LIGHT INOP IN COCKPIT. REMOVED AND REPLACED EXIT LIGHT BATTERIES. 2 L 7 3 4F A3WE 1996042500200 19960425 00200 NM 1996 4 25 UPS96205993 1 19960408 A 5315 FLOOR BEAM BOEING 727 72727C 138400J NM BS 560 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FLOOR BEAM UPPER FLANGE CORROSION WAS FOUND TO BE BEYOND LIMITS PER SRM 53-10 -1, AT STA 560 WL 208 FROM LBL 50 TO LBL 60. REMOVED AND REPLACED FLOOR BEAM UPPER FLANGE PER SRM 53-10-8 FIG 5. 2 L 7 3 4F A3WE 1996042500201 19960425 00201 NM 1996 4 25 UPS96205994 1 19960328 A 5320 FITTING BOEING 727 72727C 138400J NM RT TERM FITTING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HFEC ON RT UPPER TERMINAL FITTING RECEIVED A CRACK IN THE CORNER FITTING. RE MOVED AND REPLACED CORNER FITTING PER SRM 57-12-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996042500202 19960425 00202 NM 1996 4 25 UPS96205995 1 19960404 A 5320 BRACKET BOEING 727 72727C 138400J NM BS 1130 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MAIN CABIN FLOOR BEAM SUPPORT BRACKET IS CRACKED AT THE UPPER EDGE TWO PLACES , BS 1130 AND RBL 44. REMOVED AND FABRICATED PART PER DRW 65-45373, ALODINED AND PRIMED PER SRM 51-10-2, AND INSTALLED PER SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996042500203 19960425 00203 NM 1996 4 25 UPS96205996 1 19960410 A 5315 FLOOR BEAM BOEING 727 72727C 138400J NM FS 360 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 360 WL 208, FLOOR BEAM UPPER FLANGE AFTER NUTPLATE AND CORROSION REMOVAL, FLOOR BEAM WAS FOUND TO BE BEYOND LIMITS FROM RBL 4.45 TO RBL 10.45 AT THE AREAS TO BE WITHIN LIMITS PER SRM 53-10-1. R EPAIRED AREA. 2 L 7 3 4F A3WE 1996042500204 19960425 00204 NM 1996 4 25 UPS96205998 1 19960410 A 5315 FLOOR BEAM BOEING 727 72727C 138400J NM FS 1166 UNPLUGGED HOLE A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FASTENER HOLE UNPLUGGED FS 1166 RBL 45 FLOOR BEAM SUPPORT CHANNEL. INSTALLED FREEZE PLUG, FAB AND INSTALLED REPAIR PARTS PER SRM 51-10-6 AND 51-30-2. 2 L 7 3 4F A3WE 1996042500205 19960425 00205 NM 1996 4 25 UPS96205999 1 19960411 A 5347 SEAT TRACK BOEING 727 72727C 138400J NM FS 360-550 WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 500 BL 0 SEAT TRACK IS WORN BEYOND LIMITS. FAB AND INSTALLED SEAT TRACK P ER SRM 51-10-2. 2 L 7 3 4F A3WE 1996042500206 19960425 00206 NM 1996 4 25 UPS96206000 1 19960330 A 5315 FLOOR BEAM BOEING 727 72727C 138400J NM BS 680 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FLOOR BEAM UPPER FLANGE AFTER CORROSION REMOVAL, FLOOR BEAM WAS FOUND TO BE B EYOND LIMITS. REMOVED DAMAGED SECTION OF FLOOR BEAM FAB AND INSTALLED PER SRM 53-10-8 FIG F, STA 680 RBL 26 TO 44 RBL 6 0 WL 208. 2 L 7 3 4F A3WE 1996042500207 19960425 00207 NM 1996 4 25 UPS96206001 1 19960403 A 5313 STRINGER BOEING 727 72727C 138400J NM WS 224-230 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT EXTERNAL FUEL TANK AT WS 224 TO 230 STR 1 REQUIRES REPAIR DUE TO CORROSION BEYOND LIMITS. SPLICED STR 1 AT STA 209 TO TERMINATING END, FUEL LEAK CHECK GOOD IAW MM 28-00-00. 2 L 7 3 4F A3WE 1996042500208 19960425 00208 NM 1996 4 25 UPS96206002 1 19960416 A 5311 FRAME BOEING 727 72727C 138400J NM FS 825.95 MISDRILLED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FRAME 825.95 HAS HOLE DRILLED IN FASTENER STR 16L. FAB AND INSTALLED DOUBLER REPAIR IAW BAC DRWG 65C36281 SHT 1. 2 L 7 3 4F A3WE 1996042500209 19960425 00209 NM 1996 4 25 UPS96206003 1 19960416 A 5311 FRAME BOEING 727 72727C 138400J NM FS 760 MISDRILLED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FRAME FS 760 HAS HOLE DRILLED STR 16L. FAB AND INSTALLED DOUBLER REPAIR IAW BAC DRWG 65C36279 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996042500210 19960425 00210 NM 1996 4 25 UPS96206004 1 19960416 A 5311 FRAME BOEING 727 72727C 138400J NM FS 783 MISDRILLED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FRAME FS 783 HAS HOLE DRILLED STR 16L. FAB AND INSTALLED DOUBLER REPAIR IAW BAC DRWG 65C36281 SHEET 1. 2 L 7 3 4F A3WE 1996042500211 19960425 00211 NM 1996 4 25 UPS96206005 1 19960416 A 5311 FRAME BOEING 727 72727C 138400J NM FS 783 MISDRILLED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FRAME FS 783 HAS HOLE DRILLED STR 16R. FAB AND INSTALLED DOUBLER REPAIR IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996042500212 19960425 00212 NM 1996 4 25 UPS96206006 1 19960416 A 5311 FRAME BOEING 727 72727C 138400J NM FS 760 MISDRILLED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FRAME FS 760 HAS HOLE DRILLED STR 16R. FAB AND INSTALLED DOUBLER REPAIR IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996042500213 19960425 00213 NM 1996 4 25 UPS96206007 1 19960412 A 5320 6515974 FITTING BOEING 727 72727C 138400J NM FS 870 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 915UP 19533 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED BS 870 RT TERMINAL SEVERLY CORRODED ON VAPOR SEAL ATTACH FLANGE WL 190 RBL 65 TO 71. CUT OUT AND BLENDED CORROSION PER SRM 51-10-6, PERFORMED HFEC INSPECTION FOR CRACKS AND CORROSION PER NDT MANUA L A, 6 51-00-00 FIG 23. REPAIRED AREA PER UPS EO B727-5310-8126A. 2 L 7 3 4F A3WE 1996042500214 19960425 00214 NM 1996 4 25 UPS96206008 1 19960322 A 5531 SPAR SKIN BOEING 727 72727C 138400J NM FS 1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED BS 1342 LT INTERSPAR SKIN IS CORRODED BEYOND LIMITS. CUTOUT DAMAGED AREA, FA B AND INSTALLED REPAIR PARTS IAW BAC DRWG 65C29055. 2 L 7 3 4F A3WE 1996042500215 19960425 00215 NM 1996 4 25 UPS96206009 1 19960322 A 5531 SPAR SKIN BOEING 727 72727C 138400J NM FS 1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED BS 1342 RT INTERSPAR SKIN IS CORRODED BEYOND LIMITS AT TERMINAL FITTING. CUT OUT DAMAGED AREA, FAB AND INSTALLED REPAIR PARTS IAW BAC DRWG 65C29055 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996042500216 19960425 00216 NM 1996 4 25 UPS96206010 1 19960403 A 5320 TEE CHORD BOEING 727 72727C 138400J NM BS 1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED BS 1342 WL 270 UPPER T-CHORD IS CORRODED. REMOVED AND REPLACED T-CHORD 65-17 508-2 IAW 51-30-2, 51-10-1 AND BAC DWG 65-17508. 2 L 7 3 4F A3WE 1996042500217 19960425 00217 NM 1996 4 25 UPS96206011 1 19960404 A 5320 TEE CHORD BOEING 727 72727C 138400J NM BS 1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT O/B CHORD AT FS 1342 RBL 30 WL 250 IAW BAC 65-19532 DWG AND UPS EO B727-55 30-4601 B. 2 L 7 3 4F A3WE 1996042500218 19960425 00218 NM 1996 4 25 UPS96206012 1 19960404 A 5320 TEE CHORD BOEING 727 72727C 138400J NM BS 1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT O/B CHORD FS 1342 LBL 30 WL 250 IS CORRODED. REMOVED AND REPLACED O/B CHO RD IAW BAC 65-19532 AND UPS EO B727-5530-4601 B. 2 L 7 3 4F A3WE 1996042500219 19960425 00219 NM 1996 4 25 UPS96206013 1 19960414 A 5320 CHANNEL BOEING 727 72727C 138400J NM BS 1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED BS 1342 CENTER CHANNEL IS CORRODED. REMOVED AND REPLACED CHANNEL NR 65-22551 -7 IAW BAC DWG 65-22551 AND UPS EO B727-5530-4601-B. 2 L 7 3 4F A3WE 1996042500220 19960425 00220 NM 1996 4 25 UPS96206014 1 19960414 A 5311 FRAME BOEING 727 72727C 138400J NM BS 1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT LWR FRAME CHORD RBL 24 WL 220 STA 1342 IS CORRODED. REMOVED AND REPLACED LWR FRAME CHORD NR 65-17508-224 IAW UPS EO 727-5530-4601-B AND BAC DWG 65-17508. 2 L 7 3 4F A3WE 1996042500221 19960425 00221 NM 1996 4 25 UPS96206015 1 19960404 A 5311 FRAME BOEING 727 72727C 138400J NM BS 1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT LWR FRAME CHORD LBL 24 WL 220 STA 1342 IS CORRODED. REMOVED AND REPLACED FRAME CHORD IAW SRM 51-17508 SRM 51-30-2. 2 L 7 3 4F A3WE 1996042500222 19960425 00222 NM 1996 4 25 UPS96206016 1 19960405 A 5320 FITTING BOEING 727 72727C 138400J NM BS 870 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FITTING AT RT WHEEL WELL STA 870 HAS HEAVY CORROSION ON LWR END. REMOVED COR ROSION IAW SRM 53-10-9 FIG NR 6 HFEC INSP PER B727NTM PT 6 51-00-00 FIG 23, DETECTED NO CRACKS AND REPAIRED IAW SRM 53-1 0-9. 2 L 7 3 4F A3WE 1996042500223 19960425 00223 NM 1996 4 25 UPS96206017 1 19960407 A 5730 SKIN BOEING 727 72727C 138400J NM WS 870 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT WING NR 5 SLAT CRACK GOING PAST DRILL HOLE AT BOTTOM OF SLAT. REMOVED DAM AGED SECTION SKIN PER SRM 57-30-3. FAB AND INSTALLED REPAIR PARTS PER SRM 57-50-3 FIG 1. 2 L 7 3 4F A3WE 1996042500224 19960425 00224 NM 1996 4 25 UPS96206018 1 19960407 A 5320 RIB BOEING 727 72727C 138400J NM FS 1367 RT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT RIB CRACKED AT FS 1367 BL 22.5. REMOVED DAMAGED AREA PER SRM 51-40-3, FAB AND INSTALLED REPAIR ANGLE PER SRM 51-40-3. 2 L 7 3 4F A3WE 1996042500225 19960425 00225 NM 1996 4 25 UPS96206019 1 19960407 A 5320 RIB BOEING 727 72727C 138400J NM FS 1367 LT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT RIB CRACKD AT FS 1367 BL 22.5. REMOVED DAMAGED AREA PER SRM 51-40-3, FAB AND INSTALLED REPAIR ANGLE PER SRM 51-40-3. 2 L 7 3 4F A3WE 1996042500226 19960425 00226 NM 1996 4 25 UPS96206020 1 19960308 A 5311 FRAME BOEING 727 72727C 138400J NM BS 1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT FRAME CHORD AT STA 1342 RBL 20 WL 238 IS CORRODED. REPLACED RT I/B CHORD PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996042500227 19960425 00227 NM 1996 4 25 UPS96206021 1 19960308 A 5311 FRAME BOEING 727 72727C 138400J NM BS 1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT FRAME CHORD AT STA 1342 RBL 20 WL 238 IS CORRODED. REPLACED LT I/B CHORD PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996042500228 19960425 00228 NM 1996 4 25 UPS96206022 1 19960308 A 5320 65225511 CHANNEL BOEING 727 72727C 138400J NM FS 1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 1342 LT CHANNEL WL 247 LBL 18 IS CORRODED AFT SIDE OF 1342 FRAME. REMOVED AND REPLACED CHANNEL IAW BAC DWG 65-93155 B727-5530-4601 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996042500229 19960425 00229 NM 1996 4 25 UPS96206023 1 19960308 A 5320 65225512 CHANNEL BOEING 727 72727C 138400J NM FS 1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 1342 RT CHANNEL WL 247 RBL 18 IS CORRODED AFT SIDE OF 1342 FRAME. REMOVED AND REPLACED CHANNEL IAW BAC DWG 65-93155 B727-5530-4601 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996042500230 19960425 00230 NM 1996 4 25 UPS96206024 1 19960314 A 5320 ANGLE BOEING 727 72727C 138400J NM FS 1345 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT SKIN SUPPORT ANGLE IS CRACKED AT FS 1345 AND FIN STA 22.5. REMOVED DAMAGE D SECTION IAW SRM 51-40-3, FAB AND INSTALLED REPAIR IAW SRM 51-40-3. 2 L 7 3 4F A3WE 1996042500231 19960425 00231 WP 1996 4 25 UPS96805975 1 19960415 A 3350 6012255 LIGHT DOUG DC8 DC871F 302199D WP COCKPIT INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 748UP 45948 MAINTENANCE PRE-DEPARTURE CHECK, EMERGENCY EXIT LIGHT INOP. EMERGENCY LIGHT BATTERY PACK REPLACED. 2 L 7 4 4F RT 4A25 1996042500232 19960425 00232 WP 1996 4 25 UPS96805977 1 19960412 A 5320 SUPPORT DOUG DC8 DC873F 302199F WP BS 1900 CRACKED A IPXA K NONE O OTHER CR CRUISE 1 SO 01 803UP 46073 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 1900 NR 4 HORIZONTAL SUPPORT RT AND LT SIDE ATTACH CRACKED, SEEN FROM AFT SIDE. FAB REPAIR DOUBLERS AND INSTALLED IA W DC-8 SRM 51-9-0 AND 53-2-0. 2 L 7 4 4F RT 4A25 1996042500233 19960425 00233 WP 1996 4 25 UPS96805978 1 19960412 A 5711 SPAR DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER CR CRUISE 1 SO 01 803UP 46073 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT WING LWR SPAR HOLE NR 6 FOUND CRACKED WHILE PERFORMING EO DC8-5710-7761-A. FAB REPAIR DOUBLER, FILLER AND BUSHINGS AND INSTALLED IAW DAC DWG J060232 AND EO DC8-5710-7761A. 2 L 7 4 4F RT 4A25 1996042500234 19960425 00234 WP 1996 4 25 UPS96805979 1 19960412 A 5751 SKIN DOUG DC8 DC873F 302199F WP LT AILERON CRACKED A IPXA K NONE O OTHER CR CRUISE 1 SO 01 803UP 46073 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT WING BOTTOM I/B AILERON, SKIN AT MIDDLE FWD GOUGED CRACKED AND DENTED. ST OP DRILLED CRACKS, FAB REPAIR DOUBLERS AND INSTALLED IAW DC8-SRM 57-2-1 AND 57-8-0. 2 L 7 4 4F RT 4A25 1996042500235 19960425 00235 WP 1996 4 25 UPS96805980 1 19960412 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING LE CRACKED A IPXA K NONE O OTHER CR CRUISE 1 SO 01 803UP 46073 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT CENTER L/E RIB CRACKED AT APPROX STA XFS 353 UPPER SIDE. STOP DRILLED CRA CKS, FAB REPAIR ANGLES AND INSTALLED IAW DC8-SRM 57-3-0 AND 57-2-0. 2 L 7 4 4F RT 4A25 1996042500236 19960425 00236 WP 1996 4 25 UPS96805981 1 19960412 A 5400 RIB DOUG DC8 DC873F 302199F WP NR 2 PYLON CRACKED A IPXA K NONE O OTHER CR CRUISE 1 SO 01 803UP 46073 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT STUB WING AT NR 2 PYLON RIB CRACKED ON UPPER SIDE APPROX AT STA XRS 440. S TOP DRILLED CRACK, FAB REPAIR DOUBLERS AND INSTALLED IAW DC8-SRM 57-2-0 AND 57-3-0. 2 L 7 4 4F RT 4A25 1996042500237 19960425 00237 WP 1996 4 25 UPS96805982 1 19960412 A 7170 DRAIN LINE DOUG DC8 DC873F 302199F WP NR 1 ENGINE DENTED A IPXA K NONE O OTHER CR CRUISE 1 SO 01 803UP 46073 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED DRAIN LINE FOR NR 1 ENGINE OIL FUEL HEAT EXCHANGER DENTED. REMOVED LINE, FAB AND PRESSURE TESTED LINE IAW DPS 3.805, FOUND NO LEAKAGE. INSTALLED SERVICEABLE LINE IAW DC8-MM 75-20-02. 2 L 7 4 4F RT 4A25 1996042500238 19960425 00238 WP 1996 4 25 UPS96805984 1 19960412 A 5720 SPLICE CAP DOUG DC8 DC873F 302199F WP WS 408.343 CRACKED A IPXA K NONE O OTHER CR CRUISE 1 SO 01 803UP 46073 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT WING STA 408.343 HAS 4.5 INCH CRACK JUST ABOVE RADIUS BETWEEN STR 51 AND 5 2. REPAIRED XW 408.343 LWR SPLICE CAP ON RT WING THAT HAD 2 CRACKS IN VERT LEG BETWEEN STR 51 AND 52 IAW UPS EO DC8-571 0-8090A. 2 L 7 4 4F RT 4A25 1996042500239 19960425 00239 WP 1996 4 25 UPS96805985 1 19960412 A 1420 GROMMET DOUG DC8 DC873F 302199F WP NR 2 PYLON BROKEN A IPXA O OTHER O OTHER CR CRUISE 1 SO 01 803UP 46073 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED NR 2 PYLON WIRING SUPPORT GROMMETS ARE BROKEN, 2 EACH. REMOVED AND REPLACED IAW DC8 MM 20-11-0 AND UPS EO DC8- 71-0036. 2 L 7 4 4F RT 4A25 1996042500240 19960425 00240 WP 1996 4 25 UPS96805986 1 19960412 A 5415 FITTING DOUG DC8 DC873F 302199F WP NR 2 PYLON BROKEN A IPXA K NONE O OTHER CR CRUISE 1 SO 01 803UP 46073 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED EO DC8-5710-40-80-E, WING FRONT SPAR PYLON SUPPORT FITTING REPLACEMENT OF NR 2 PYLON. REPAIRED NR 2 PYLON FOOTSTOOL, T-DOUBLER, SKATE ANGLE IAW UPS EO DC8-57-0660. 2 L 7 4 4F RT 4A25 1996042500241 19960425 00241 WP 1996 4 25 UPS96805990 1 19960409 A 3350 LIGHT DOUG DC8 DC873F 302199F WP DOOR MAIN ENT BROKEN A IPXA K NONE L NO TEST CR CRUISE 1 SO 01 809UP 46109 MAINTENANCE REPORTED, RADIO ACTIVE EXIT SIGN ON FWD ENTRANCE DOOR IS BROKEN. 2 L 7 4 4F RT 4A25 1996042500242 19960425 00242 WP 1996 4 25 9608889949 1 19960419 A 2751 H61004 POSITION SWITCH DOUG DC9 DC931 3022065 WP TE FLAPS STUCK A NWAA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS N FALSE WARNING CL CLIMB 1 GL 01 8928E 45865 LANDING GEAR WARNING HORN SOUNDED AFTER GEAR HANDLE WAS RAISED, CIRCUIT BREAKER WAS PULLED AND HORN CEASED. FLIGHT RETU RNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND FLAP SWITCH S1-85 STUCK CLOSED. REPLACED SWITCH, OPERATIONA L CHECK NORMAL ON GEAR SWING. 2 L 7 2 4F A6WE 1996042500243 19960425 00243 NM 1996 4 25 9608896634 1 19960421 A 2613 OVERHEAT SENSOR BOEING 747 747227B 1384888 NM LT WING FAILED A NWAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 01 634US 22234 DURING CRUISE, THE LEFT WING OVERHEAT LIGHT ILLUMINATED. AIRCRAFT DIVERTED TO SEA AND LANDED WITHOUT INCIDENT. REPLACE D THE LEFT WING OVERHEAT SENSOR, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996042500244 19960425 00244 NE 1996 4 25 9608903244 2 19960418 A 7320 HMU AIRBUS 320 A320211 3930320 EU GE CFM56 CFM565A 13802 NE NR 2 ENGINE MALFUNCTIONED A NWAA A E F UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. X ENGINE FLAMEOUT CR CRUISE 1 GL 01 344NW 388 731741 DURING CRUISE FLIGHT NR 2 ENGINE FLAME-OUT OCCURRED, ONE UNSUCCESSFUL RELIGHT WAS ATTEMPTED. THE NR 2 ENGINE FIRE BOTTL E DISCHARGED AND NO ABNORMAL ENGINE OPERATING PARAMETERS WERE NOTICED PRIOR TO FLAME-OUT. AIRCRAFT DIVERTED TO SLC AND LANDED WITHOUT FURTHER INCIDENT. GROUND INSPECTION PERSONNEL BORESCOPED ENGINE AND FOUND NO OUT OF LIMIT CONDITIONS. M AINTENANCE REPLACED THE HYDRO MECHANICAL UNIT, FUEL PUMP, AND THE LP VALVE ACTUATOR. THE NR 2 ENGINE FIRE BOTTLE WAS RE PLACED AND THE NR 2 ENGINE LEAK AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A28NM E29NE 1996042500245 19960425 00245 WP 1996 4 25 9608911151 1 19960418 A 3350 6013217 POWER PACK DOUG DC10 DC1040 3023508 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 151US 46760 DURING LINE INSPECTION, THE EMERGENCY FLOOR PATH LIGHTS OVER THE AFT WING AREA WERE INOPERATIVE. REPLACED THE POWER SUP PLY AND BATTERIES. 2 L 7 3 4F A22WE 1996042500246 19960425 00246 NM 1996 4 25 96089256309 1 19960421 A 3350 CONNECTOR BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 669US 24224 DURING LINE CHECK, FOUND THE RIGHT EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE FROM ROWS 35 TO 42. RECONNECTED CONNECTOR P IN AND OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1996042500247 19960425 00247 NM 1996 4 25 9608936305 1 19960421 A 3350 CONNECTOR BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 665US 23820 DURING LINE CHECK, FOUND THE RIGHT EMERGENCY FLOOR TRACK LIGHTING FROM ROWS 51 TO 55 INOPERATIVE. RECONNECTED TERMINALS AND OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1996042500248 19960425 00248 NM 1996 4 25 9608946303 1 19960420 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 663US 23818 DURING LINE CHECK, FOUND UPPER DECK EMERGENCY DOOR HANDLE LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND POWER SUPPLY, O PERATIONAL CHECK GODD. 2 L 7 4 4F RT A20WE 1996042500249 19960425 00249 WP 1996 4 25 9608959979 1 19960421 A 2420 GENERATING SYST DOUG DC9 DC931 3022065 WP LT ENGINE MALFUNCTIONED A NWAA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 GL 01 9343 47439 LEFT GENERATOR VOLTS AND FREQUENCY WENT TO ZERO DURING CLIMB. THIS WAS ACCOMPANIED BY AC CROSSTIE LOCKOUT. FLIGHT DIVE RTED TO DSM AND LANDED WITHOUT INCIDENT. MAINTENANCE DEFERRED LEFT AC GENERATOR SYSTEM PER MEL 24-1A. 2 L 7 2 4F A6WE 1996042500250 19960425 00250 WP 1996 4 25 9608969971 1 19960421 A 3412 RAT PROBE DOUG DC9 DC931 3022065 WP COCKPIT MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 9335 47337 RAM AIR TEMPERATURE INDICATOR PEGGED OUT AT TOP OF SCALE AFTER TAKEOFF. CIRCUIT BREAKER WAS PULLED AND RESET WITH NO HE LP. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RAT PROBE, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996042500251 19960425 00251 WP 1996 4 25 9608979949 1 19960419 A 2751 H209B SWITCH DOUG DC9 DC931 3022065 WP FLAP POSITION FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 8928E 45865 FLAP/RUDDER STOP INOPERATIVE LIGHT ILLUMINATED DURING TAKEOFF ROLL. ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE REPLACED FLAP SWITCH S1-351 AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996042500252 19960425 00252 WP 1996 4 25 9608989911 1 19960420 A 3230 59151695506 UPLOCK ASSY DOUG DC9 DC931 3022065 WP RT MLG FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 961N 40390 34365 47405 RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. FLIGHT RETURNED TO MSP AND LANDED WITHOUT IN CIDENT. MAINTENANCE FOUND FAULT IN RIGHT MAIN GEAR UPLOCK ASSEMBLY. REPLACED UPLOCK ASSEMBLY AND OPERATIONAL CHECK NOR MAL. 2 L 7 2 4F A6WE 1996042500253 19960425 00253 WP 1996 4 25 9608999964 1 19960421 A 2133 OUTFLOW VALVE DOUG DC9 DC931 3022065 WP CABIN MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 912RW 47150 AIRCRAFT WOULD NOT PRESSURIZE IN AUTO MODE AFTER TAKEOFF. OUTFLOW VALVE WORKED NORMALLY IN MANUAL POSITION. FLIGHT RET URNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED CABIN PRESSURE AMPLIFIER AND OUTFLOW VALVE ACTUATOR, OPE RATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996042500254 19960425 00254 WP 1996 4 25 9609009965 1 19960420 A 2150 SEALS DOUG DC9 DC931 3022065 WP HEAT EXCHANGER WORN A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 911RW 47149 TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND WORN SEALS AT LEFT SUPPLY DUCT TO HEAT EXCHANGER. REPLACED SEALS, LEFT AND RIGHT TAIL COMPARTMENT TE MPERATURE SENSORS AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996042500255 19960425 00255 WP 1996 4 25 9609019908 1 19960420 A 3231 39567851 RELEASE LINK DOUG DC9 DC931 3022065 WP RT NLG DOOR MALFUNCTIONED A NWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 01 958N 47254 EXCESSIVE VIBRATION IN NOSE GEAR AREA OCCURRED AFTER TAKEOFF. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAIN TENANCE FOUND THE RIGHT NOSE GEAR DOOR OPEN AND MANUAL RELEASE INTERMITTENT. REPLACED MANUAL RELEASE LINK AND OPERATION AL CHECK NORMAL. 2 L 7 2 4F A6WE 1996042500256 19960425 00256 NM 1996 4 25 96UAL900270 1 19960418 A 3320 BALLAST BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN FAILED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 7464U 21918 RETURNED TO COS WITH SMOKE IN AFT CABIN. PACK OPERATION CHECKS NORMAL. NOTED THAT LIGHTS IN SIDE PANEL AT 19 AND 20 WE RE INOPERATIVE AND OVERHEAD LIGHTS AT 15, 16, 17 ABC, 3 AND 4 AB WERE INOPERATIVE. SUPPLEMENTAL DATA UPDATE: POSSIBLY OVERHEATED BALLAST. REPLACED BALLAST AND REPAIRED LIGHTS AT SEATS 15, 16, 17 ABC AND 3 AND 4 AB. 2 L 7 3 4F 4 F A3WE E2EA 1996042500257 19960425 00257 1996 4 25 COMA9610133 4 19960419 A 3425 6226190204 AHRS COMPUTER EMB 120 EMB120RT SO NR 1 FAILED A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 168CA 10444 30 120168 NR 1 AHRS FAILED. REPLACED THE NR 1 AHRS COMPUTER. 2 L 7 2 4T RT A31SO 1996042500258 19960425 00258 1996 4 25 COMA9610134 4 19960419 A 6122 3034719 GOVERNOR EMB 120 EMB120RT SO LT PROPELLER DEFECTIVE A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 247CA 14272 3172 120225 LT PROPELLER IS SLOW COMING OUT OF FEATHER. REPLACED THE LEFT OVER SPEED GOVERNOR. 2 L 7 2 4T RT A31SO 1996042500259 19960425 00259 EA 1996 4 25 COMA9660068 1 19960420 A 3230 RETRACT MECH CNDAIR CL600 CL6002B19 EA NLG MALFUNCTIONED A COMA K NONE O OTHER AP APPROACH 1 SO 01 916CA 7014 WHEN LANDING GEAR SELECTED DOWN THE NOSE LANDING GEAR REMAINED UP AND LOCKED. THEN 15 SECONDS LATER NLG CAME DOWN AND A LL GEAR INDICATED DOWN AND LOCKED. COULD NOT DUPLICATE, RETRACTION CHECKS WERE NORMAL. 2 L 7 2 4F RT A21EA 1996042500260 19960425 00260 EA 1996 4 25 COMA9660069 1 19960418 A 3010 124112450 TEMP SWITCH CNDAIR CL600 CL6002B19 EA LT WING DEFECTIVE A COMA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 SO 01 931CA 7037 LEFT WING ANTI-ICE DUCT WARNING CAME ON DURING FLIGHT. REPLACED DEFECTIVE WING TEMP SENSOR. 2 L 7 2 4F RT A21EA 1996042500261 19960425 00261 EA 1996 4 25 COMA9660070 1 19960420 A 3350 363782 CONNECTOR CNDAIR CL600 CL6002B19 EA CABIN DIRTY A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 915CA 7013 FORWARD SECTION OF EMERGENCY FLOOR PATH LIGHTING IS INOP. CLEANED CONNECTION AT FLOOR PATH LIGHTING SYSTEM, TEST NORMAL . 2 L 7 2 4F RT A21EA 1996042500262 19960425 00262 NM 1996 4 25 DHL96740001 1 19960419 A 3232 AN31671 ACTUATOR BOEING 727 7272Q9 138448M NM NLG DOOR WORN A DHLA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 740DH 21930 ON DESCENT, NOSE GEAR DOOR LIGHT ILLUMINATED. PLACED LEVER UP AND DOWN, LIGHT EXTINGUISHED. REMOVED AND REPLACED NOSE GEAR DOOR ACTUATOR MM 32-60. 2 L 7 3 4F RT A3WE 1996042500263 19960425 00263 NE 1996 4 25 P5CA9600209 2 19960422 A 7532 7344441 FLOW DIVIDER BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE NR 2 ENGINE MALFUNCTIONED A P5CA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 23 859FT 20326 685982 NUMBER 2 ENGINE SURGE BLEED VALVE STUCK OPEN AT FLIGHT LEVEL 39, EGT 100 DEGREES CELSIUS HOTTER THAN OTHER ENGINES AND F UEL FLOW 500 LBS HIGHER. REMOVED AND REPLACED ENGINE FLOW DIVIDER IAW MM 75-32-05. REMOVED AND REPLACED TT2 SENSOR IAW MM 73-21-04 AS PRECAUTIONARY. ENGINE RUNUP NORMAL IAW MM 71-00-00. 2 L 7 4 4F 4 F A20WE E20EA 1996042500264 19960425 00264 NM 1996 4 25 P5CA9600210 1 19960226 A 5512 PANEL BOEING 747 747122 1384872 NM HORIZ STAB CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 FOUND LEVEL ONE CORROSION AT RT HORIZONTAL STABILIZER TIP, AROUND STATIC DISCHARGE BASE SECOND FROM THE FRONT SIDE. CO RROSION REMOVED AND AREA REPROTECTED IAW SRM 51-10-01. 2 L 7 4 4F A20WE 1996042500265 19960425 00265 NM 1996 4 25 P5CA9600211 1 19960301 A 5512 PANEL BOEING 747 747122 1384872 NM HORIZ STAB CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 FOUND SMALL CRACKS ON THE HORIZONTAL STABILIZER, RT T/E UNDER STATIC DISCHARGE BASE THIRD FROM OUTSIDE. REPAIRED IAW SR M 51-40-15. 2 L 7 4 4F A20WE 1996042500266 19960425 00266 NM 1996 4 25 P5CA9600212 1 19960227 A 5330 SKIN BOEING 747 747122 1384872 NM BS 2484-2658 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 FOUND LEVEL ONE CORROSION ON FUSELAGE SKIN BETWEEN STA 2484 TO 2658 WL 366.50 RT SIDE. REMOVED CORROSION AND TREATED IA W SRM 51-10-01. 2 L 7 4 4F A20WE 1996042500267 19960425 00267 NM 1996 4 25 P5CA9600213 1 19960304 A 2120 HEAT DUCT BOEING 747 747122 1384872 NM BS 1480 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 FOUND CRACKED WELD AT AFT CARGO STATION 1480 HEAT DUCT. REPAIRED IAW OHM 36-10-04. 2 L 7 4 4F A20WE 1996042500268 19960425 00268 NM 1996 4 25 UPS96206025 1 19960419 A 3350 S106 LIGHT BOEING 727 7271A7C 13840X2 NM MAIN ENTRY DR INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 935UP 20143 MAINTENANCE REPORTED, EMERGENCY EXIT LIGHT INOP ABOVE ENTRY DOOR. ALL BATTERIES IN STOCK FAILED TO WORK. ROBBED PART O FF A/C 926 AND INSTALLED ON A/C 935. OPS CHECK GOOD. 2 L 7 3 4F A3WE 1996042500269 19960425 00269 WP 1996 4 25 UPS96806026 1 19960407 A 5320 SHEAR TIE DOUG DC8 DC873F 302199F WP FS 1580 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 1580 SHEAR TIE CRACKED AT LONGERON 31, 32 AND 34R. REPAIRED SHEAR TIE PER SRM 53-3-0 AND 51-1-20D. 2 L 7 4 4F RT 4A25 1996042500270 19960425 00270 WP 1996 4 25 UPS96806027 1 19960405 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FS 242 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 20143 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LONGERON 34R I/B SECTION CRACKED AT FS 242. REPLACED LONGERON SECTION PER SR M 51-1-20D. 2 L 7 4 4F RT 4A25 1996042500271 19960425 00271 WP 1996 4 25 UPS96806028 1 19960405 A 5320 FITTING DOUG DC8 DC873F 302199F WP FS 280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 20143 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED BANANA FITTING CRACKED AT FS 280 LONG 32R. REPLACED FITTING PER SRM 51-1-20D . 2 L 7 4 4F RT 4A25 1996042500272 19960425 00272 WP 1996 4 25 UPS96806029 1 19960401 A 5751 AILERON DOUG DC8 DC873F 302199F WP RT INBD WING CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 20143 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT I/B AILERON HAS INTERNAL CORROSION. REPLACED AILERON ASSY PER MM 27-11-01 . 2 L 7 4 4F RT 4A25 1996042500273 19960425 00273 WP 1996 4 25 UPS96806030 1 19960330 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FS 881 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 20143 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED ATTACH ANGLE ON BOTTOM SIDE OF FITTING HAS .75 INCH CRACK AT STA 881. REPLAC ED ANGLE PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996042500274 19960425 00274 WP 1996 4 25 UPS96806031 1 19960330 A 5330 SKIN DOUG DC8 DC873F 302199F WP FS 1660 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 20143 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CRACK ON SKIN AND LONGERON UPPER AFT CORNER OF RT SERVICE DOOR CUTOUT. REPAI RED PER UPS EO DC8-53-1612. 2 L 7 4 4F RT 4A25 1996042500275 19960425 00275 WP 1996 4 25 UPS96806032 1 19960330 A 5400 ANGLE DOUG DC8 DC873F 302199F WP NR 1 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 20143 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED NR 1 PYLON I/B DRAG ANGLE CRACKED BEYOND STOP DRILL. REPAIRED ANGLE PER SRM ADDENDUM DC8-5740-0716. 2 L 7 4 4F RT 4A25 1996042500276 19960425 00276 WP 1996 4 25 UPS96806033 1 19960420 A 2560 GIRT BAR DOUG DC8 DC873F 302199F WP ESCAPE SLIDE NOT CONNECTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 MAINTENANCE REPORTED, ESCAPE SLIDE BAR COULD NOT BE ENGAGED. THERE IS ABOUT A 3 INCH SPACE BETWEEN BAR AND CONNECTOR. R EMOVED SLIDE AND PLACED IN PFM PER UPS EO DC8-2566-7565A, DEFFERED AS PER MMOC D108876. 2 L 7 4 4F RT 4A25 1996042500277 19960425 00277 WP 1996 4 25 UPS96806034 1 19960419 A 2560 GIRT BAR DOUG DC8 DC873F 302199F WP ESCAPE SLIDE NOT CONNECTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 MAINTENANCE REPORTED, UNABLE TO ENGAGE METAL BAR OF ESCAPE SLIDE IN ITS ARMED POSITION. REPACKED BOTTOM OF SLIDE DOOR S ETS PROPERLY. 2 L 7 4 4F RT 4A25 1996042500278 19960425 00278 WP 1996 4 25 UPS96806035 1 19960328 A 5755 56551672 SKIN DOUG DC8 DC873F 302199F WP NR 3 SPOILER DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT NR 3 SPOILER PNL DELAMINATED AT LWR SIDE. REPLACED SPOILER PNL PER MM 27- 61-01. 2 L 7 4 4F RT 4A25 1996042500279 19960425 00279 WP 1996 4 25 UPS96806036 1 19960330 A 5753 5701152502 VANE ASSY DOUG DC8 DC873F 302199F WP NR 3 TE FLAP DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT NR 3 WING FLAP VANE DELAMINATED. REPLACED FLAP VANE ASSY PER MM 27-50-00. 2 L 7 4 4F RT 4A25 1996042500280 19960425 00280 WP 1996 4 25 UPS96806037 1 19960331 A 5320 37730732N FITTING DOUG DC8 DC873F 302199F WP FS 280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 280 LONGERON 21L FITTING CRACKED. REPLACED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996042500281 19960425 00281 WP 1996 4 25 UPS96806038 1 19960404 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP FS 70-80 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 70 TO 80, LONGERON 31L FINGER DOUBLER CRACKED. REPLACED DOUBLER PER SRM 5 1-1-20D AND 53-2-0. 2 L 7 4 4F RT 4A25 1996042500282 19960425 00282 WP 1996 4 25 UPS96806039 1 19960403 A 5400 STRAP DOUG DC8 DC873F 302199F WP NR 2 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STRAP CRACKED AT NR 3 PYLON INSIDE FWD TANK AT NR 2 STR. REPLACED STRAP PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996042500283 19960425 00283 WP 1996 4 25 UPS96806040 1 19960407 A 5313 5615374 LONGERON DOUG DC8 DC873F 302199F WP FS 1600 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 1600 LONGERON 31R CRACKED. REPLACED PER UPS EO DC8-53-1613. 2 L 7 4 4F RT 4A25 1996042500284 19960425 00284 WP 1996 4 25 UPS96806041 1 19960404 A 5320 SHEAR TIE DOUG DC8 DC873F 302199F WP FS 80 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED SHEAR TIE CRACKED AT FS 80, LONGERON 34R AND 35R. REPLACED SHEAR TIE PER SRM 53-2-0. 2 L 7 4 4F RT 4A25 1996042500285 19960425 00285 WP 1996 4 25 UPS96806043 1 19960331 A 5311 561237617 FRAME DOUG DC8 DC873F 302199F WP FS 52 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION AT FRAME BELOW LONGERON 21L, FS 52. 2 L 7 4 4F RT 4A25 1996042500290 19960425 00290 CE 1996 4 25 96ZZZX1937 1 19960311 A 2434 AT9422 ALTERNATOR PRESTOLITE BEECH 58 58 1152740 CE RT ENGINE INOPERATIVE A BAKA O OTHER H ELECT. POWER LOSS-50 PC NR NOT REPORTED 1 GL 13 9446Q 1013 922000029 TH236 DURING FLIGHT, RT ALTERNATOR QUIT. INSTALLED OVERHAULED UNIT, ELECTRICAL SYSTEM OPERATED NORMALLY. SENT ALTERNATOR TO OVERHAUL SHOP AND HAD THEM RUN IT FIRST. THEY SAID UNIT WORKED OK. TOLD THEM TO OVERHAUL IT. HAVE NOT HAD ALTERNATOR PROBLEM SINCE. SUBMITTER STATED, NORMALLY, THIS MODEL ALTERNATOR WILL NOT GO 1,000 HOURS. 1 L 7 2 3O 3A16 1996042500294 19960425 00294 CE 1996 4 25 96ZZZX1941 1 19960321 A 3260 57412025 SWITCH CESSNA 402 402C 207590R CE RT MLG UPLOCK OUT OF RIG A SQFA K NONE O OTHER IN INSP/MAINT 1 SO 17 2651Y 402C0343 PILOT REPORTS 'ONE OF THE GEAR WILL NOT LOCK IN THE 'UP' POSITION'. OPERATED GEAR MANY TIMES, COULD NOT DUPLICATE PROBL EM. FOUND UPLOCK SWITCH ON RIGHT SIDE A LITTLE OUT OF ADJUSTMENT; REF: CHAPTER 32 OF THE SM. ADJUSTED SWITCH PER MANU AL. OPERATED GEAR 8 MORE TIMES, OPERATION NORMAL. 1 L 7 2 3O A7CE 1996042500295 19960425 00295 SO 1996 4 25 96ZZZX1942 1 19960301 A 3260 31285000 BRACKET PIPER PA23 PA23250 7102308 SO NLG DOWNLOCK SW WORN A CFCA K NONE O OTHER IN INSP/MAINT 1 GL 03 54757 277554068 THE SUPPORT BRACKET FOR THE NOSE GEAR DOWNLOCK SWITCH WAS WORN ALLOWING POOR CONTACT OF SWITCH. SUBMITTER RECOMMENDS 5, 000-HOUR INSPECTION OR REPLACEMENT. 1 L 7 2 3O 1A10 1996042500338 19960425 00338 WP 1996 4 25 CAL90456 1 19960327 A 5720 DOUBLER DOUG DC9 DC932 3022066 WP LT WING LE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16521 72275 47521 HOU - INSPECTION FOUND A 2 INCH CRACK IN L/E SKIN SPLICE DOUBLER AND ANGLE CLIP JUST OUTBOARD OF LEFT WING VORTILON. A DOUBLER AND CLIP WERE INSTALLED IAW ECRA 5710-01697. (X) 2 L 7 2 4F A6WE 1996042500339 19960425 00339 NM 1996 4 25 CAL960402 1 19960326 A 4990 38042814 APU BOEING 737 7373T0 1384582 NM AFT FUSELAGE LEAKING OIL A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 14320 25290 3943 23371 CLE - FLT 0258 - THE APU AUTOMATICALLY SHUT DOWN AFTER TAKEOFF FROM LAX. THERE WERE NO ABNORMAL INDICATIONS OR LIGHTS. THE AIRCRAFT CONTINUED FLIGHT TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE RESET THE CIRCUIT BREAKER ON ACCESS ORY UNIT. THE APU WAS STARTED AND FULLY LOADED WITH NORMAL EGT, VOLTS, AND FREQUENCIES EXHIBITED. PRIOR TO BOARDING FOR NEXT FLIGHT, THE APU AUTOMATICALLY SHUT DOWN AGAIN, AND EMITTED SMOKE INTO THE CABIN. MAINTENANCE FOUND EVIDENCE OF AN INTERNAL APU OIL LEAK. THE APU OIL LEVEL WAS FOUR QUARTS LOW. THE APU WAS PLACARDED INOPERATIVE, PENDING REMOVAL AND R EPLACEMENT. (X) 2 L 7 2 4F RT A16WE 1996042500340 19960425 00340 NM 1996 4 25 CAL960410 1 19960321 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM BS 520 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 39340 29031 23578 HOU - INSPECTION FOUND A 1 INCH CRACK ON RT SUPPORT AND A 1 INCH CRACK ON LT SUPPORT IN FORWARD BAGGAGE BIN AT BS 520. T HE CRACKS WERE STOP DRILLED AND REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 51-70-11. (X) 2 L 7 2 4F RT A16WE 1996042500341 19960425 00341 NM 1996 4 25 CAL960437 1 19960322 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM BS 847-867 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 39340 29031 23578 HOU - INSPECTION FOUND CORROSION ON FLOOR SUPPORT BETWEEN BS 847 AND BS 867, RT SIDE. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-2. (X) 2 L 7 2 4F RT A16WE 1996042500342 19960425 00342 NM 1996 4 25 CAL960438 1 19960325 A 5320 SUPPORT ANGLE BOEING 737 7373T0 1384582 NM BS 380-400 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 39340 29031 23578 HOU - INSPECTION FOUND A 1 INCH CRACK IN CENTER CABIN FLOOR SUPPORT ANGLE BETWEEN BS 380 AND BS 400. A NEW ANGLE WAS FA BRICATED AND INSTALLED IAW SRM 51-10-2. (X) 2 L 7 2 4F RT A16WE 1996042500343 19960425 00343 WP 1996 4 25 CAL960439 1 19960330 A 2530 WK623C58 CONNECTOR DOUG DC9 DC932 3022066 WP RT COFFEE MAKER FAILED A CALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 09 19504 47638 IAH - FLT 1809 - WHITE SMOKE WITH BURNING ELECTRICAL SMELL ENTERED THE COCKPIT ON APPROACH TO IAH. THE SMOKE AND SMELL DISSIPATED AFTER TURNING OFF THE GALLEY POWER AND PULLING ALL CIRCUIT BREAKERS IN GALLEY. THE AIRCRAFT LANDED WITHOUT I NCIDENT. MAINTENANCE FOUND CANNON PLUG ON RT COFFEEMAKER BURNED. THE CONNECTOR PLUG WAS REPLACED. OPERATION OF BOTH T HE RT AND LT COFFEEMAKERS CHECKED GOOD. (X) 2 L 7 2 4F A6WE 1996042500344 19960425 00344 NM 1996 4 25 CAL960441 1 19960405 A 2750 CONTROL CABLE BOEING 737 737219 1384469 NM LT TE FLAP BROKEN A CALA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SW 09 10248 20344 EWR - FLT 1160 - THE AIRCRAFT ROLLED LEFT ON FLAP EXTENSION FOR LANDING ON APPROACH TO EWR. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT INBOARD TRAILING EDGE FLAP JAMMED DUE TO A BROKEN FOLLOW-UP CABLE ON INBOARD JACKSC REW. CABLES BC-3 AND BC-4 AND THE FLAP DRIVE MECHANISM WERE REMOVED AND REPLACED IAW MM 27-51-35 AND OHM 57-53-22. AN ADJUSTMENT AND TEST OF THE FLAP WERE PERFORMED IAW MM 27-51-12. OPERATIONAL CHECKS WERE GOOD. (X) 2 L 7 2 4F A16WE 1996042500345 19960425 00345 WP 1996 4 25 CAL960442 1 19960406 A 5330 SKIN DOUG DC9 DC981 3022081 WP BS 427 DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14880 35072 48044 EWR - FLT 0611 - THE FUSELAGE SKIN WAS DAMAGED BY A BELT LOADER AT STA 427, FORWARD CARGO DOOR JAMB. THE AREA WAS REPAI RED BY INSTALLING AN EXTERNAL DOUBLER IAW ECRA 5330-02381. (X) 2 L 7 2 4F A6WE 1996042500346 19960425 00346 WP 1996 4 25 CAL960443 1 19960313 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 332 CREASED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16804 38567 49246 MIA - INSPECTION FOUND A 3.5 INCH LONG CREASE IN RT FUSELAGE SKIN AT STA 332. THE DAMAGED SECTION WAS CUT OUT. A REPAI R DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-04, FIGURE 12B. (X) 2 L 7 2 4F A6WE 1996042500347 19960425 00347 WP 1996 4 25 CAL960444 1 19960306 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1155 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16804 38567 49246 MIA - INSPECTION FOUND FLOOR FRAME CORRODED AROUND NUTPLATES AT STA 1155. A NEW FLOOR FRAME WAS FABRICATED AND INSTALLE D IAW SRM 51-00 AND SRM 51-30-2. (X) 2 L 7 2 4F A6WE 1996042500348 19960425 00348 WP 1996 4 25 CAL960445 1 19960304 A 5320 FLOOR WEB DOUG DC9 DC982 3022082 WP BS 180-218 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16804 38567 49246 MIA - INSPECTION FOUND FLOOR WEB CORRODED BELOW FORWARD ENTRY FLOOR SUPPORT AT STA 180-STA 218. THE CORRODED AREA WAS C UT OUT AND REPAIRED IAW SRM 53-01. (X) 2 L 7 2 4F A6WE 1996042500349 19960425 00349 WP 1996 4 25 CAL960446 1 19960303 A 5320 SUPPORT ANGLE DOUG DC9 DC982 3022082 WP BS 180-218 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16804 38567 49246 MIA - INSPECTION FOUND FORWARD ENTRY FLOOR SUPPORT ANGLE CORRODED AFT OF DOOR CUTOUT, STA 180-STA 218. A NEW FLOOR SUPP ORT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND SRM 51-30-2. (X) 2 L 7 2 4F A6WE 1996042500350 19960425 00350 NM 1996 4 25 CAL960447 1 19960405 A 5315 FLOORBEAM BOEING 737 737217 1384464 NM BS 459 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14233 74695 19887 GSO - INSPECTION FOUND A .50 INCH CRACK AND CORROSION ON COCKPIT AFT FLOORBEAM AT STA 459. THE CORRODED AREAS WERE REMO VED. NEW ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-40-3. (X) 2 L 7 2 4F A16WE 1996042500351 19960425 00351 NM 1996 4 25 CAL960448 1 19960328 A 5414 SKIN BOEING 737 737217 1384464 NM NR 2 ENGINE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14233 19887 GSO - INSPECTION FOUND THE NR 2 ENGINE FORWARD OUTBOARD COWL OUTER SKIN CORRODED AROUND ENGINE RADIUS WARNING PLACARD. T HE CORRODED SECTION OF SKIN WAS CUT OUT. A DOUBLER AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 54-30-2. (X) 2 L 7 2 4F A16WE 1996042500352 19960425 00352 NM 1996 4 25 CAL960449 1 19960330 A 5230 654692118 FRAME BOEING 737 737217 1384464 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14233 74695 19887 GSO - INSPECTION FOUND A 3 INCH CRACK IN LOWER FORWARD FRAME OF C-1 DOOR. THE FRAME SECTION WAS REMOVED AND REPLACED IA W SRM 51-30-2. (X) 2 L 7 2 4F A16WE 1996042500353 19960425 00353 WP 1996 4 25 CAL960451 1 19960328 A 5210 591412157 DOOR PAN DOUG DC9 DC932 3022066 WP PASSENGER DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16521 72275 47521 HOU - INSPECTION FOUND A 5 INCH AND 3 INCH CRACK ON UPPER FORWARD CORNER FORWARD PASSENGER DOOR PAN. REMOVED AND REPLAC ED CORNER PAN PER SRM 52-05. (X) 2 L 7 2 4F A6WE 1996042500354 19960425 00354 WP 1996 4 25 CAL960452 1 19960330 A 3350 41B004AD07G3 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 27509 47798 IAH - INSPECTION FOUND THE CENTER AISLE OVERHEAD EMERGENCY LIGHTS INOPERATIVE FROM ROW 7 TO ROW 17. THE BATTERIES IN BA TTERY PACK AT ROW 8 LEFT WERE REPLACED AND OPERATION OF THE LIGHTS WAS RESTORED. (X) 2 L 7 2 4F A6WE 1996042500355 19960425 00355 WP 1996 4 25 CAL960454 1 19960403 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 1087 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16521 72275 47521 HOU - INSPECTION FOUND A .50 INCH CRACK IN SKIN AT LONGERON 16L AND A 1 INCH CRACK IN SKIN AT LONGERON 15L, STA 1087. T HE SKIN WAS REPAIRED IAW SRM 53-01, FIGURE 2 AND SRM 53-04, FIGURE 18. 2 L 7 2 4F A6WE 1996042500356 19960425 00356 WP 1996 4 25 CAL960455 1 19960328 A 5712 NOSE RIB DOUG DC9 DC932 3022066 WP WING LE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16521 72275 47521 HOU - INSPECTION FOUND A .75 INCH CRACK IN BEND RADIUS AT UPPER AFT END OF NOSE RIB AND A .75 INCH CRACK IN NOSE RIB ANG LE CLIP OUTBOARD OF NR 10 SLAT TRACK. THE CLIP WAS REPLACED AND THE RIB WAS REPAIRED PER ECRA 5720-01260. (X) 2 L 7 2 4F A6WE 1996042500357 19960425 00357 WP 1996 4 25 CAL960457 1 19960402 A 5312 BLKHD BRACKET DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16521 72275 47521 HOU - INSPECTION FOUND A 1 INCH CRACK IN BRACKET AT AFT PRESSURE BULKHEAD, LONGERON 24R. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-60-0 AND SRM 51-30-25. (X) 2 L 7 2 4F A6WE 1996042500358 19960425 00358 WP 1996 4 25 CAL960458 1 19960328 A 5210 ANGLE DOUBLER DOUG DC9 DC932 3022066 WP PASSENGER DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16521 72275 47521 HOU - INSPECTION FOUND A 1.5 INCH CRACK ON L-ANGLE DOUBLER OF FORWARD PASSENGER DOOR. A REPAIR WAS INSTALLED IAW SRM 52 -05, PAGE 179. (X) 2 L 7 2 4F A6WE 1996042500359 19960425 00359 WP 1996 4 25 CAL960459 1 19960328 A 5311 BELTFRAME DOUG DC9 DC932 3022066 WP BS 794 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16521 72275 47521 HOU - INSPECTION FOUND FORWARD AND BOTTOM SIDE OF BELTFRAME CORRODED IN AFT BAGGAGE BIN AT STA 794, LONGERON 28L TO LONG ERON 28R. THE CORROSION WAS REMOVED IAW SRM 53-01. (X) 2 L 7 2 4F A6WE 1996042500360 19960425 00360 WP 1996 4 25 CAL960460 1 19960327 A 5313 27779223 LONGERON DOUG DC9 DC932 3022066 WP BS 215 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16521 72275 47521 HOU - INSPECTION FOUND CORROSION ON LONGERON 30L AT E AND E COMPARTMENT, STA 215. THE LONGERON WAS REPLACED IAW SRM 53- 11-1. (X) 2 L 7 2 4F A6WE 1996042500361 19960425 00361 WP 1996 4 25 CAL960461 1 19960327 A 5320 SPLICE DOUG DC9 DC932 3022066 WP BS 378-389 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16521 72275 47521 HOU - INSPECTION FOUND A 2 INCH CRACK IN LONGERON 30 SPLICE AT STA 378 - STA 389. THE SPLICE WAS REMOVED AND REPLACED I AW SRM 51-30-0. (X) 2 L 7 2 4F A6WE 1996042500362 19960425 00362 WP 1996 4 25 CAL960462 1 19960329 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 218 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16521 72275 47521 HOU - INSPECTION FOUND LONGERON 27 CORRODED AT STA 218. THE CORRODED SECTION OF LONGERON WAS REMOVED AND A NEW SECTION WAS SPLICED IAW SRM 53-02, FIGURE 4. (X) 2 L 7 2 4F A6WE 1996042500404 19960425 00404 SO 1996 4 25 96ZZZX2026 2 19960405 A 7414 103493504 MAGNETO BENDIX BEECH 58 58 1152740 CE CONT O520 IO520C 17032 SO ROTOR FAILED A YQSA K NONE R PARTIAL RPM/PWR LOSS IN INSP/MAINT 1 CE 09 738T 1369 D218916FR TH706 244419R ROUGH MAGNETO ENCOUNTERED ON RUN-UP MAGNETO CHECK. INSPECTION FOUND FAILED ROTOR AT TRAILING FINGER TOWER WHICH CAUSED ROTOR TO LOCK UP IN TOWER, SHEARING DRIVE GEARS ON PLASTIC GEAR BENDING DRIVE COUPLING TIN, AND DESTROYING DRIVE CUSHION S AND DEFORMING END OF GEAR DRIVE SHAFT. SUSPECT CAUSE IS AGE OF PLASTIC GEAR. 1 L 7 2 3O 3 O 3A16 E5CE 1996042500407 19960425 00407 WP 1996 4 25 9608749751 1 19960410 A 5315 FLOOR BEAM DOUG DC9 DC941 302207N WP FS 1056 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 751NW 47115 DURING H-CHECK, FOUND CORROSION ON THE FS 1056 FLOOR BEAM AT APPROXIMATELY LBL 26 AND RBL 34. REPAIRED BEAM (P/N 995818 7-1) PER EA 97-109476. 2 L 7 2 4F A6WE 1996042500408 19960425 00408 WP 1996 4 25 9608759751 1 19960410 A 5315 FLOOR BEAM DOUG DC9 DC941 302207N WP FS 1041 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 751NW 47115 DURING H-CHECK, FOUND CORROSION ON THE FS 1041 FLOOR BEAM AT APPROXIMATELY LBL 18. REPAIRED BEAM (P/N 9958212-3) PER EA 97-109477. 2 L 7 2 4F A6WE 1996042500409 19960425 00409 EU 1996 4 25 9608763215 1 19960412 A 5313 STRINGER AIRBUS 320 A320211 3930320 EU FS 14300-14834 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 315US 171 DURING IL CHECK, FOUND CORROSION ON STR 43L BETWEEN FRAMES 33 AND 34. REPAIRED STRINGER PER EA 32-104252. 2 L 7 2 4F RT A28NM 1996042500410 19960425 00410 WP 1996 4 25 9608779959 1 19960413 A 5330 SKIN DOUG DC9 DC931 3022065 WP PAX DOOR CUTOUT CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 919RW 47162 DURING LINE CHECK, FOUND A CRACK IN THE MAIN CABIN DOOR CUTOUT SKIN AT THE UPPER AFT STOP. REPAIRED SKIN (P/N 5911406-5 ) PER EA 99-104250. 2 L 7 2 4F A6WE 1996042500411 19960425 00411 NM 1996 4 25 9608785530 1 19960415 A 5320 FITTING BOEING 757 757251 1384970 NM FS 1380 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 530US 23845 DURING PERIODIC CHECK, FOUND CORROSION ON THE AFT CARGO DOOR FORWARD THRESHOLD FITTING FS 1380. REPLACED FITTING. 2 L 7 2 4F RT A2NM 1996042500412 19960425 00412 WP 1996 4 25 9608791146 1 19960416 A 5320 WEB DOUG DC10 DC1040 3023508 WP FS 495 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 146US 46755 DURING L-CHECK, FOUND CRACKS IN THE NOSE LANDING GEAR WHEEL WELL LEFT AND RIGHT SIDE WEBS AT FS 495, Z= -64. REPAIRED W EBS (P/N NCA6246-25, -27) PER EA 11-102158. 2 L 7 3 4F A22WE 1996042500413 19960425 00413 WP 1996 4 25 9608809763 1 19960417 A 5240 FITTING DOUG DC9 DC941 302207N WP SERVICE DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 763NW 47396 DURING H-CHECK, FOUND A CRACK IN THE FORWARD SERVICE DOOR END FITTING AT THE LOWER FORWARD HINGE. REPLACED FITTING PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996042500414 19960425 00414 WP 1996 4 25 9608811146 1 19960417 A 5522 SKIN DOUG DC10 DC1040 3023508 WP RT ELEVATOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 146US 46755 DURING L-CHECK, FOUND A .5 INCH CRACK IN THE UPPER SKIN OF THE RIGHT INBOARD ELEVATOR. REPAIRED SKIN PER EA 11-104237. 2 L 7 3 4F A22WE 1996042500415 19960425 00415 WP 1996 4 25 9608821146 1 19960417 A 5320 HEADER DOUG DC10 DC1040 3023508 WP FS 938 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 146US 46755 DURING L-CHECK, FOUND A .75 INCH CRACK IN THE FORWARD CARGO DOOR CUTOUT UPPER HEADER FS 938. REPAIRED HEADER (P/N ADA02 17) PER EA 11-103925. 2 L 7 3 4F A22WE 1996042500416 19960425 00416 WP 1996 4 25 9608839751 1 19960417 A 5342 ANGLE DOUG DC9 DC941 302207N WP FS 1171 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 751NW 47115 DURING H-CHECK, FOUND A TWO INCH CRACK IN THE RIGHT SIDE DORSAL FIN ATTACH ANGLE FS 1171. REPAIRED ANGLE (P/N 5912141-6 0) PER EA 97-109496. 2 L 7 2 4F A6WE 1996042500417 19960425 00417 WP 1996 4 25 9608849862 1 19960418 A 5320 FITTING DOUG DC9 DC951 3022051 WP FS 674 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 771NC 47769 DURING H-CHECK, FOUND A CRACK IN THE LONGERON 25R END FITTING AT FS 674. REPLACED FITTING PER SRM 51-30. 2 L 7 2 4F A6WE 1996042500418 19960425 00418 WP 1996 4 25 9608859862 1 19960418 A 5744 FITTING DOUG DC9 DC951 3022051 WP NR 3 TE FLAP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 771NC 47769 DURING H-CHECK, FOUND CORROSION IN THE NR 3 FORWARD FLAP HINGE FITTING BOLT HOLE. REPLACED FITTING (P/N 5919217-502) PE R CITEXT 90-2750-1-9806. 2 L 7 2 4F A6WE 1996042500419 19960425 00419 WP 1996 4 25 9608869763 1 19960418 A 5230 FITTING DOUG DC9 DC941 302207N WP CARGO DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 763NW 47396 DURING H-CHECK, FOUND A CRACK IN THE AFT CARGO DOOR NR 4 BEAM AFT END FITTING. REPLACED FITTING. 2 L 7 2 4F A6WE 1996042500420 19960425 00420 WP 1996 4 25 9608879763 1 19960418 A 5320 FITTING DOUG DC9 DC941 302207N WP FS 1056 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 763NW 47396 DURING H-CHECK, FOUND CORROSION ON THE FS 1056 FLOOR BEAM END FITTING AT THE LEFT CUSP. REPLACED FITTING PER SRM 51-30- 5. 2 L 7 2 4F A6WE 1996042500421 19960425 00421 EU 1996 4 25 9609023245 1 19960416 A 3230 RETRACT MECH AIRBUS 320 A320211 3930320 EU LANDING GEAR MALFUNCTIONED A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 345NW 399 DURING CLIMBOUT, THE LANDING GEAR DID NOT RETRACT ACCOMPANIED BY LANDNG GEAR NOT UPLOCKED MESSAGE. CYCLED THE LANDING G EAR HANDLE AND ALL INDICATIONS WERE NORMAL. AIRCRAFT CONTINUED TO ORIGINAL DESTINATION AND LANDED WITHOUT INCIDENT. 2 L 7 2 4F RT A28NM 1996042500422 19960425 00422 NM 1996 4 25 9609032289 1 19960419 A 3231 RETRACT MECH BOEING 727 727251 138408H NM NLG DOOR LACK OF LUBE A NWAA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 01 289US 21377 DURING APPROACH ON LANDING GEAR EXTENSION, THE NOSE GEAR DOOR LIGHT DID NOT ILLUMINATE AND NO AURAL INDICATION. RECYCLE D GEAR AND ALL INDICATIONS WERE NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. TPA MAINTENANCE LUBRICATED NOSE GEAR AND PER FORMED MAINTENANCE CHECK, CHECKED OK. 2 L 7 3 4F A3WE 1996042500423 19960425 00423 NM 1996 4 25 9609045503 1 19960423 A 3350 BATTERY PACK BOEING 757 757251 1384970 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 503US 23192 DURING PREFLIGHT, FOUND EMERGENCY LIGHTS AT DOOR 3R AND OVERHEAD LIGHTS AFT RIGHT SIDE OF AIRCRAFT INOPERATIVE. REPLACE D BATTERY PACK AT DOOR 3R, SYSTEM CHECKED OK. 2 L 7 2 4F RT A2NM 1996042500424 19960425 00424 WP 1996 4 25 9609059949 1 19960420 A 7931 61701441 OIL PRESS IND DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7B 52053 NE COCKPIT MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 8928E 45865 653447 THE NR 1 ENGINE OIL PRESSURE INDICATION WAS ABOVE THE RECOMMENDED MAXIMUM AND FLUCTUATING ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE OIL PRESSURE INDICATOR WITH A SERVICEABLE U NIT. 2 L 7 2 4F 4 F A6WE E2EA 1996042500425 19960425 00425 WP 1996 4 25 9609069917 1 19960421 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP TAIL CONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 967N 47573 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTING ALONG CATWALK IN TAIL CONE INOPERATIVE. REPLACED BATTERY P ACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996042500426 19960425 00426 WP 1996 4 25 9609079949 1 19960420 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP TAIL CONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8928E 45865 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL CONE HANDLE AND CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY P ACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996042500427 19960425 00427 WP 1996 4 25 9609089950 1 19960421 A 3350 FUSE DOUG DC9 DC932 3022066 WP BATTERY PACK FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9346 47376 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL CONE EMERGENCY PATH AND HANDLE LIGHTS INOPERATIVE. REPLACED BATTERIES AN D FUSE, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996042500428 19960425 00428 WP 1996 4 25 9609099957 1 19960421 A 3350 6104789 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 915RW 47139 DURING LINE MAINTENANCE INSPECTION, FOUND MID CABIN FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK , OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996042500429 19960425 00429 NE 1996 4 25 9609101229 2 19960417 A 7200 ENGINE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 3 FAILED A NWAA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 GL 01 229NW 46551 17441 DURING TAXI TO RAMP, THE NR 3 ENGINE WAS SHUTDOWN DUE TO FUEL LEAKING OUT OF FRONT OF COMPRESSOR. REPLACED NR 3 ENGINE AFTER REPLACING THE FUEL/OIL EXCHANGER AND INDUCTOR VALVE. CHECK WAS NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A22WE E23EA 1996042500430 19960425 00430 NE 1996 4 25 9609111155 2 19960421 A 7532 8DJ185LWC1 BLEED VALVE DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 2 ENGINE MALFUNCTIONED A NWAA O OTHER R PARTIAL RPM/PWR LOSS DE DESCENT 1 GL 01 155US 46764 86152 AT TOP OF DESCENT, THE NR 2 ENGINE EXPERIENCED COMPRESSOR STALL. THE EGT ROSE TO 800 DEGREES AND BACK TO NORMAL WITHIN A MINUTE. ALSO, WITH LOW FUEL FLOW N1 AND N2 WOULD NOT RESPOND TO THROTTLE MOVEMENTS. CREW FOLLOWED COCKPIT OPERATING MANUAL AND CONTINUED FLIGHT TO MSP. VISUAL AND BORESCOPE INSPECTION OF NR 2 ENGINE 6, 7 AND 15TH HPC, 13TH STAGE STATOR WERE NORMAL. REPLACED BLEED VALVE, PRESSURE CONTROL AND EGT INDICATOR. 2 L 7 3 4F 4 F A22WE E20EA 1996042500431 19960425 00431 NM 1996 4 25 96DHL708004 1 19960420 A 3310 671213 BALLAST BOEING 727 72725 1384006 NM COCKPIT FAILED A T DHLA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 708DH 18275 SMOKE IN COCKPIT, ISOLATED TO GLARE SHEILD FLOOD LIGHT BALLAST M356 AND M357. PULLED AND COLLARD C/B. 2 L 7 3 4F A3WE 1996042500432 19960425 00432 NM 1996 4 25 96FDEA00746 1 19960405 A 5712 RIB BOEING 727 7272S2F 1384O81 NM BS 760 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 217FE 22938 NR 0137, -001, HFEC INSP EXHIBITS A CRACK IN THE FWD MOST UPPER HOLE AT APPROX 12 O'CLOCK AT RT WING RIB CHORD BL 70.5 B S 760. CUT OUT DAMAGE AT 630 JUST BELOW STR 22R AND REPAIRED PER FEDEX SRM 53-30-3 AND EA 7-5710-28223. 2 L 7 3 4F A3WE 1996042500433 19960425 00433 EU 1996 4 25 96FDEA00799 1 19960420 A 5270 DOOR WARNING AIRBUS 300 A300F4605R 3930327 EU AVIONICS COMPT ACTIVATED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 656FE 745 AVIONICS DOOR UNSAFE AT 12,000 FT. AVIONICS DOOR FOUND CLOSED. DOOR CYCLED OPEN AND CLOSED, COCKPIT INDICATION SHOWS L OCKED AND GREEN ON ECAM. 2 L 7 2 4F RT A35EU 1996042500434 19960425 00434 EU 1996 4 25 96FDEA00800 1 19960420 A 2820 REFUELING PANEL AIRBUS 310 A310203 EU FUEL SYST POWERED UP A FDEA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 407FE 254 LARGE FUEL INBALANCE, APPROX 7,000 LBS LT WING HEAVY. DIVERTED TO SLC. FOUND REFUELING PANEL POWERED UP AND TRANSFER V ALVE OPEN. REFUELED A/C AND SECURED FUELING PANEL. 2 L 7 2 4F RT A35EU 1996042500435 19960425 00435 WP 1996 4 25 96FDEA00802 1 19960422 A 3260 806125 GROUND PROX BOX DOUG DC10 DC1030F 3023504 WP E/E COMPT DEFECTIVE A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 303FE 46802 ALL FOUR GEAR LIGHTS ILLUM WITH HANDLE UP, NO OTHER WARNINGS. RECYCLED GEAR IAW RED TAB PROCEDURES, GOT 4 GREEN ON BOTH PANELS WITH GEAR EXTENDED. AFTER THE GEAR WAS RETRACTED, THE FOUR RED LIGHTS REILLUMINATED, NO HORN. REMOVED AND REPL ACED GROUND PROX BOX AS PER MM 32-61-01, OPS CHECK OK. 2 L 7 3 4F RT A22WE 1996042500436 19960425 00436 NM 1996 4 25 96FDEA00803 1 19960422 A 5313 STRINGER BOEING 727 727277 138408S NM BS 1070-1098 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 242FE 21178 CORROSION (C53-113-01) BS 1098 TO 1070 STR 29R. REMOVED AND REPLACED CHANNEL AT BS 1070 TO 1098 AT STR 29R, ALL WORK DO NE IAW FEDEX SRM 51-30-2. 2 L 7 3 4F RT A3WE 1996042500437 19960425 00437 NM 1996 4 25 96FDEA00805 1 19960422 A 5330 SKIN BOEING 727 727277 138408S NM BS 295 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 242FE 21178 DAMAGED EXTERIOR SKIN AT BS 295 STR 11 RT. CUT OUT DAMAGED SKIN AND REPAIRED IAW SRM 53-30-3 AND ER NR 041986JDW. 2 L 7 3 4F RT A3WE 1996042500438 19960425 00438 NM 1996 4 25 96FDEA00806 1 19960422 A 5320 DOUBLER BOEING 727 727233 138408A NM BS 720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 270FE 22035 CORROSION (C53-113-01, -1) ON DOUBLER AT BS 720 PLUS 6 WL 149 RBL 23. MECHANICALLY REMOVED CORROSION ON DOUBLER AT BS 7 20A PLUS 6 WL 149 RBL 23 IN AN AREA OF .7 INCH BY 1.3 INCH BY .021 INCH OF ORIGINAL THICKNESS OF .050, AREA WAS FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-30-1. FABRICATED NEW DOUBLER USING ORIGINAL AS TEMPLATE AND INSTALLED NEW DOUBLER. 2 L 7 3 4F RT A3WE 1996042500440 19960425 00440 NM 1996 4 25 96FDEA00808 1 19960422 A 5330 SKIN BOEING 727 727233 138408A NM BS 680-685 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 CORROSION BETWEEN SKIN LAP FROM STA 680 TO 685 AT STR 14R. CUT OUT CORRODED SKIN BEHIND LAPPED SKIN AND INSTALLED REPAI R PER SRM 53-30-03. 2 L 7 3 4F RT A3WE 1996042500441 19960425 00441 NM 1996 4 25 96FDEA00809 1 19960419 A 5315 BAC150529222 FLOOR BEAM BOEING 727 727223 1384074 NM BS 344 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 MAIN CARGO STA 344 FLOOR BEAM UPPER CHORD CORRODED WL 208 FROM RBL 23 TO LBL 65. REMOVED DAMAGED SECTION OF UPPER CHOR D. INSTALLED NEW UPPER CHORD SECTION, RBL 23 TO LBL 65, PER STANDARD REPAIR DRAWING NR SR 27-53-007, DATED 03-15-94. 2 L 7 3 4F A3WE 1996042500442 19960425 00442 NM 1996 4 25 96FDEA00810 1 19960416 A 5311 FRAME BOEING 727 72725C 138400H NM BS 804 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 124FE 19360 NRO232, STA 804 ABOVE CUSP, FRAME CRACKED FROM I/B LIP TO FASTENER HOLE IN CENTER OF FRAME. *S/D* FABRICATED REPAIR PAR TS IAW SRM 51-40-3 AND INSTALLED DOUBLER IAW SRM 51-40-3. 2 L 7 3 4F A3WE 1996042500443 19960425 00443 NM 1996 4 25 96FDEA00811 1 19960412 A 5320 CHANNEL BOEING 727 727233 138408A NM BS 640 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 NR0168, UPPER LOBE STA 640 STR 3R, 2 DEEP GOUGES IN CHANNEL AND FLANGE CUT. *S/D* INSTALLED STR REPAIR PER SRM 53-10-3. 2 L 7 3 4F RT A3WE 1996042500444 19960425 00444 NM 1996 4 25 96FDEA00812 1 19960412 A 5330 SKIN BOEING 727 727233 138408A NM BS 1160 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 NR0198, SKIN BULGED FWD LWR CORNER OF AFT LAV SERVICE PANEL STA 1160 STR 22L. *S/D* REMOVED RIVETS AS MARKED PER SRM 51 -30-2, NO EVIDENCE OF CORROSION. INSTALLED FASTENERS PER SRM 51-30-2. 2 L 7 3 4F RT A3WE 1996042500445 19960425 00445 NM 1996 4 25 96FDEA00813 1 19960413 A 5311 FRAME BOEING 727 727233 138408A NM BS 227.8 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 NR0704, FRAME CORRODED AT STA 227.8 BELOW F/O'S SLIDING WINDOW NEAR FLOOR. *S/D* REMOVED AND REPLACED STA 227.8 RT FRAM E WEB SRM 51-10-1. 2 L 7 3 4F RT A3WE 1996042500446 19960425 00446 NM 1996 4 25 96FDEA00814 1 19960413 A 5315 FLOOR BEAM BOEING 727 727233 138408A NM BS 268 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 NR0708, FLOOR BEAM BELOW F/E'S SEAT AFT TRACK CORRODED ON TOP SURFACE STA 268 LBL 5. *S/D* REMOVED CORROSION PER SRM 51 -10-06, INSTALLED DOUBLER PER ESO 11782 AND EA 7-5300-28617. 2 L 7 3 4F RT A3WE 1996042500447 19960425 00447 NM 1996 4 25 96FDEA00815 1 19960413 A 5320 INTERCOSTAL BOEING 727 727233 138408A NM BS 259.5-277 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 NR0710, FLT DECK FLOOR SUPPORT INTERCOSTAL CORRODED ON TOP SURFACE FROM STA 259.5 TO 277 LBL 18. 2 L 7 3 4F RT A3WE 1996042500448 19960425 00448 NM 1996 4 25 96FDEA00816 1 19960422 A 5210 GATE BEAM BOEING 727 727233 138408A NM BS 314 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 270FE 22035 NR0150, 002 FWD ENTRY DOOR LWR GATE BEAM IS CORRODED FWD SIDE BS 314 WL 214 LBL 60. 2 L 7 3 4F RT A3WE 1996042500449 19960425 00449 NM 1996 4 25 96FDEA00817 1 19960422 A 5320 STRINGER SPLICE BOEING 727 727233 138408A NM BS 683 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 270FE 22035 NRO238 001, CORROSION (C53-113-01, -1) AND MISSING LEVELING COMPOUND ON STR SPLICE BS 683 LB 15 WL 149. *S/D* REMOVED AND REPLACED STRINGER SPLICE BS 683, LBL 15, WL 149. 2 L 7 3 4F RT A3WE 1996042500450 19960425 00450 WP 1996 4 25 ABXA9600483 1 19960420 A 3230 S491474012024 PIN DOUG DC9 DC932 3022066 WP LDG CONTL VLV MISSING A ABXA K NONE O OTHER TO TAKEOFF 1 GL 23 989AX 47314 DURING DEPARTURE, SOME LOOSENESS AND BINDING NOTED WHEN RAISING THE GEAR HANDLE AS IT APPROACHED THE UP POSITION. RECYC LED THE GEAR, THE UPLATCH CHECK WAS UNSATISFACTORY, LEFT THE RIGHT HYDRAULIC PUMP ON HIGH. INSTALLED MISSING PIN TO THE LANDING GEAR CONTROL VALVE SECTOR WHICH HAD ALLOWED THE CABLE TO FALL PARTIALLY OFF OF THE SECTOR. THE LANDING GEAR CO NTROL LEVER OPS CHECKED GOOD IAW ABX DC9 SUPP MM. 2 L 7 2 4F A6WE 1996042500451 19960425 00451 SO 1996 4 25 COMA9610135 1 19960422 A 2150 COOLING FAN EMB 120 EMB120RT SO ACM FAILED A COMA C H ABORTED TAKEOFF DEACTIVATE SYST/CIRCUITS M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 SO 01 261CA 120254 RT DUCT LEAK WARNING DURING TAKEOFF. DUCT LEAK WARNING CAUSED BY A FAILED ACM COOLING FAN. SYSTEM PLACED ON DEFERRED M AINTENANCE LIST AND ACFT CONTINUED SERVICE. 2 L 7 2 4T RT A31SO 1996042500452 19960425 00452 1996 4 25 COMA9660071 4 19960422 A 3418 3995100207A COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING FAILED A COMA O OTHER N FALSE WARNING UK UNKNOWN 1 SO 01 945CA 5596 1796 7069 STALL FAIL MESSAGE ON EICAS. REPLACED THE STALL PROTECTION COMPUTER. 2 L 7 2 4F RT A21EA 1996042500453 19960425 00453 EA 1996 4 25 COMA9660072 1 19960421 A 3260 864806 PSEU CNDAIR CL600 CL6002B19 EA E/E COMPT DEFECTIVE A COMA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 954CA 611 7100 PROXIMITY SYSTEM FAULT STATUS MESSAGE ON EICAS. REPLACED THE PROXIMITY SYSTEM ELECTRONIC UNIT. 2 L 7 2 4F RT A21EA 1996042500454 19960425 00454 1996 4 25 COMA9660073 4 19960420 A 2210 6229968001 YAW DAMPER CNDAIR CL600 CL6002B19 EA AUTO PILOT INTERMITTENT A COMA K NONE F FLT CONT AFFECTED TO TAKEOFF 1 SO 01 951CA 963 7091 YAW DAMPER 2 WILL INTERMITTENTLY ENGAGE AND DISENGAGE. REPLACED NR 2 YAW DAMPER ACTUATOR. 2 L 7 2 4F RT A21EA 1996042500455 19960425 00455 WP 1996 4 25 MWEA96114 1 19960419 A 2560 591769037 COVER DOUG DC9 DC932 3022066 WP GALLEY DOOR FELL OFF A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 203ME 47673 UPON ARRIVAL, GALLEY DOOR EVACUTAION SLIDE COVER FELL OFF DOOR. REINSTALLED GALLEY SERVICE DOOR EMERGENCY EVAC SLIDE CO VER. 2 L 7 2 4F A6WE 1996042500456 19960425 00456 WP 1996 4 25 MWEA96115 1 19960419 A 3350 07912 BULB DOUG DC9 DC914 3022034 WP CABIN LOOSE A MWEA K NONE L NO TEST UK UNKNOWN 1 GL 31 80ME 45795 ONE FLOOR EMERGENCY TRACK LIGHT BULB IS LOOSE. INSTALLED NEW LENS ASSEMBLY. 2 L 7 2 4F A6WE 1996042500457 19960425 00457 1996 4 25 MWEA96116 4 19960420 A 2565 SR09250059 CABLE DOUG MD88 MD88 3023688 NM ESCAPE SLIDE BROKEN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 AFT GALLEY EVACUTAION SLIDE LATCH CABLE IS BROKEN. FABRICATED CABLE IAW SB A25-316, REINSTALLED CABLE. 2 L 7 2 4F RT A6WE 1996042500458 19960425 00458 WP 1996 4 25 MWEA96117 1 19960421 A 3350 08199 LIGHT TRACK DOUG DC9 DC914 3022034 WP CABIN LENS MISSING A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 80ME 45795 EMERGENCY FLOOR TRACK LIGHT AND LENS MISSING AT 14C LOCATION. REPLACED LAST SECTION OF LIGHT TRACK AND INSTALLED NEW B ULB AND LENS. 2 L 7 2 4F A6WE 1996042500459 19960425 00459 WP 1996 4 25 MWEA96118 1 19960422 A 2560 591769037 COVER DOUG DC9 DC932 3022066 WP FWD ENT DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 502ME 48132 ESCAPE SLIDE AND COVER BECAME DETACHED FROM FORWARD ENTRANCE DOOR AT GATE ARRIVAL IN GRR. RESTOWED SLIDE AND COVER IN M AIN CABIN DOOR. 2 L 7 2 4F A6WE 1996042500460 19960425 00460 NM 1996 4 25 QXEA9600154 1 19960422 A 3350 6104781 BATTERY PACKS DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 831PH 328 NR 2 AND NR 6 EMERGENCY LIGHT BATTERY PACKS ARE WEAK. NR 2 AND NR 6 BATTERY PACKS REPLACED, PACKS OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 1996042500461 19960425 00461 NM 1996 4 25 QXEA9600155 1 19960422 A 3350 PIN GRIMES 6104781 DHAV DHC8 DHC8102 2809003 NM NR3 BATTERY PACK LOOSE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 831PH 328 AFT CENTER AISLE EMERGENCY LIGHT INOP. LOOSE PIN IN CANNON FOR NR 3 EMERGENCY LIGHT BATTERY PACK RESECURED, LIGHT OPS C HECKED GOOD. 2 H 7 2 4T RT A13NM 1996042500462 19960425 00462 SW 1996 4 25 HEEA966933 1 19960408 A 6410 206310105101 BEARING 206016201127 BELL 206 206L3 1182108 SW T/R DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8589X 702 CS7224 51487 TEFLON RACE LOOSE IN BEARING. ALSO REPLACED 2 EACH NEW SLEEVES P/N 206-010-733-003. 1 G 7 1 3U H2SW 1996042500464 19960425 00464 EU 1996 4 25 HEEA966936 1 19960408 A 6510 1053180301 SHAFT BOLKMS 105 BO105S 5626006 EU T/R SCORED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911FL S717 T/R SHAFT IS SCORED. (SCORING AT ZONE F AND PITTING AT ZONE D) 1 G 7 2 3U H3EU 1996042500465 19960425 00465 1996 4 25 HEEA966937 4 19960408 A 3421 222375033103 INDICATOR BELL 412 412 1182202 SW COCKPIT ATTITUDE PRECESSING E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 107X 33113 PRECESSING IN PITCH AND ROLL. SENT TO TIME SINCE REPAIR 58:30. 1 G 7 2 4U H4SW 1996042500466 19960425 00466 EU 1996 4 25 HEEA966938 1 19960408 A 6320 4638201004 LOWER HOUSING BOLKMS 105 BO105S 5626006 EU M/R GR BOX LINER LOOSE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 721MB S752 STEEL LINER ON RIGHT INPUT BORE LOOSE. 1 G 7 2 3U H3EU 1996042500467 19960425 00467 EU 1996 4 25 HEEA966939 1 19960408 A 6320 4638201005 UPPER HOUSING BOLKMS 105 BO105S 5626006 EU M/R GR BOX WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 721MB S752 BUSHING BORE WORN BEYOND 151.04 MIN. 1 G 7 2 3U H3EU 1996042500468 19960425 00468 EU 1996 4 25 HEEA966940 1 19960408 A 6520 4619311022 OUTPUT SHAFT BOLKMS 105 BO105S 5626006 EU T/R GR BOX PAINT PEEL E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 131AE S787 OUTPUT SHAFT PAINT IS PEELING. 1 G 7 2 3U H3EU 1996042500470 19960425 00470 SW 1996 4 25 HEEA966942 1 19960408 A 7714 412075010109 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 33008 36004 #2 ENG. N2 NEEDLE STAYS BELOW #1 ENG AND ROTOR NEEDLES. SENT TO B.F. GOODRICH AEROSPACE FOR INSPECTION AND REPAIR. 1 G 7 2 4U H4SW 1996042500471 19960425 00471 SW 1996 4 25 HEEA966943 1 19960408 A 2844 BSE20630G TRANSDUCER BELL 206 206L1 1182107 SW FUEL PRESS DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 14 TRANSDUCER WILL CAUSE FUEL PRESSURE NEEDLE TO JUMP WHEN FM RADIO IS KEYED. 1 G 7 1 3U H2SW 1996042500472 19960425 00472 SW 1996 4 25 HEEA966944 1 19960408 A 2436 104217A REGULATOR BELL 206 206B3 1181506 SW DC SYS DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 REGULATOR UNSTABLE, WILL NOT HOLD SET VALUES. KNOCKS GENERATOR OFF LINE. 1 G 7 1 3U H2SW 1996042500474 19960425 00474 1996 4 25 HEEA966946 4 19960408 A 3416 D120P2T ALTIMETER BELL 206 206L3 1182108 SW COCKPIT ERRORS E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 41128 51134 ALTITUDE INDICATES 1300 FEET AT GROUND LEVEL. 1 G 7 1 3U H2SW 1996042500475 19960425 00475 1996 4 25 HEEA966947 4 19960408 A 3416 01200102 ALTIMETER BELL 206 206L3 1182108 SW COCKPIT ENCODER ERROR E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 80C 51092 ENCODER EXCEEDS TRANSITION POINTS BY UP TO 25 FEET. THIS IS THE THIRDTIME THIS UNIT IS SENT TO VENDOR FOR SAME PROBLEM. 1 G 7 1 3U H2SW 1996042500476 19960425 00476 1996 4 25 HEEA966948 4 19960408 A 3416 5035P2P44 ALTIMETER BELL 412 412 1182202 SW COCKPIT ENCODER ERRATIC E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 108X 33115 ALTIMETER ERRATIC IN FLIGHT. 1 G 7 2 4U H4SW 1996042500477 19960425 00477 SW 1996 4 25 HEEA966949 1 19960408 A 5260 FYLM735023 MOTOR ASSY BELL 412 412 1182202 SW STEP WEAK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 ACTUATOR IS VERY SLOW. INSPECTED BY ACCESSORY SHOP AND FOUND MOTOR IS WEAK, SLOW AND NOISY. 1 G 7 2 4U H4SW 1996042500478 19960425 00478 NE 1996 4 25 HEEA966950 1 19960408 A 7810 7630507003044 EJECTOR SKRSKY S76 S76A 8143006 NE EXH CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3122H 760233 EJECTOR IS CRACKED 1 G 7 2 3U H1NE 1996042500479 19960425 00479 1996 4 25 HEEA966951 4 19960408 A 3416 214175278101 ALTIMETER BELL 412 412 1182202 SW COCKPIT ENCODER ERRATIC E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 21498 36003 ENCODER HAS ERRATIC OUTPUT. SENT TO B.F. GOODRICH AEROSPACE FOR WARRANTY REPAIR. TIME SINCE REPAIR0:00. 1 G 7 2 4U H4SW 1996042500480 19960425 00480 NE 1996 4 25 HEEA966952 1 19960408 A 7810 7630507003044 EJECTOR SKRSKY S76 S76A 8143006 NE EXH CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 EJECTOR IS CRACKED. 1 G 7 2 3U H1NE 1996042500481 19960425 00481 SW 1996 4 25 HEEA966953 1 19960408 A 6730 206076031023 SERVO BELL 206 206B 1181511 SW FLT CONTROL LEAKING E HEEA K NONE K FLUID LOSS NR NOT REPORTED 1 SW 03 2269A 13626 3608 SERVO LEAKING AT PISTON SHAFT. 1 G 7 1 3U H2SW 1996042500482 19960425 00482 SW 1996 4 25 HEEA966954 1 19960408 A 6730 206076031023 SERVO BELL 206 206B 1181511 SW FLT CONTROL LEAKING E HEEA K NONE K FLUID LOSS NR NOT REPORTED 1 SW 03 2269A 10520 3608 SERVO LEAKING AT PISTON SHAFT. 1 G 7 1 3U H2SW 1996042500483 19960425 00483 SW 1996 4 25 HEEA966955 1 19960408 A 2824 L88010501 VALVE BELL 412 412 1182202 SW FUEL XFER LEAKING E HEEA K NONE K FLUID LOSS NR NOT REPORTED 1 SW 03 2149S 36002 VALVE LEAKING FUEL AFTER SHUTDOWN. 1 G 7 2 4U H4SW 1996042500484 19960425 00484 EU 1996 4 25 HEEA966956 1 19960408 A 2435 150SG122Q GENERATOR SNIAS 350 AS350B2 8680813 EU START/GEN NOISE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6095S 961 2777 STARTER GENERATOR HAS BAD SPOT ON COMMUTATOR AND MAKING NOISE. 1 G 7 1 3U H9EU 1996042500485 19960425 00485 1996 4 25 HEEA966957 4 19960408 A 3421 258719343 GYRO BEECH 200 200CBEECH 1152926 CE COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 500PH BL29 GYRO INTERMITTENT SIGNAL. 1 L 7 2 4T A24CE 1996042500486 19960425 00486 1996 4 25 HEEA966958 4 19960408 A 3413 7130 INDICATOR BEECH 200 200BEECH 1152920 CE COCKPIT VSI FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 30PH BB635 INDICATOR WOULD NOT RETURN TO ZERO. 1 L 7 2 4T A24CE 1996042500487 19960425 00487 SW 1996 4 25 HEEA966959 1 19960408 A 7933 209070262009 INDICATOR BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2298Z 33077 OIL TEMP WOULD NOT INDICATE. 1 G 7 2 4U H4SW 1996042500489 19960425 00489 EU 1996 4 25 HEEA966961 1 19960408 A 7712 10594575 TRANSMITTER BOLKMS 105 BO105S 5626006 EU ENG TORQUE WONT TEST E HEEA K NONE L NO TEST NR NOT REPORTED 1 SW 03 5368F S718 TORQUE TRANSMITTER WON'TTEST CORRECTLY. CAUSES INDICATOR TO READ LOW. 1 G 7 2 3U H3EU 1996042500490 19960425 00490 EU 1996 4 25 HEEA966962 1 19960408 A 6240 10594565 INDICATOR BOLKMS 105 BO105S 5626006 EU MAST MOMENT WONT TEST E HEEA K NONE L NO TEST NR NOT REPORTED 1 SW 03 5368F S718 INDICATOR WON'TTEST CORRECTLY. CAUSES INDICATOR TO READ LOW. 1 G 7 2 3U H3EU 1996042500491 19960425 00491 1996 4 25 HEEA966963 4 19960408 A 3416 13012001 ALTIMETER SKRSKY S76 S76A 8143006 NE COCKPIT ERROR E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1545X 760050 ALTIMETER NEEDLE INDICATES 120 FEET OFF AT ZERO. 1 G 7 2 3U H1NE 1996042500492 19960425 00492 SW 1996 4 25 HEEA966964 1 19960408 A 2432 39563001 BATTERY PACK BELL 412 412 1182202 SW DC SYS FAIL TEST E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 21498 1520 36003 BATTERY UNIT WILL NOT PASS CAPACITY TEST. 1 G 7 2 4U H4SW 1996042500494 19960425 00494 SW 1996 4 25 HEEA966966 1 19960408 A 6730 206076062003 CYLINDER BELL 206 206L3 1182108 SW M/R LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 8587X 19176 51464 CYLINDER STATIC LEAK. 1 G 7 1 3U H2SW 1996042500495 19960425 00495 EA 1996 4 25 HEEA966968 2 19960408 A 7250 VANE RING BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA TURB 2ND STAGE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 39PH 9512 BL3 PCE81468 CRACKED POWER TURBINE 2ND STAGE VANE RING. 1 L 7 2 4T 4 T A24CE E4EA 1996042500496 19960425 00496 EU 1996 4 25 HEEA966969 1 19960408 A 7722 9560167090 COMPENSATOR SNIAS 350 AS350B2 8680813 EU ENG TEMP DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 6097Z 1537 2820 FLUCTUATING POWER CHECKS. SENT TO TURBOMECA...THEIR PROPERTY BEING RETURNED. 1 G 7 1 3U H9EU 1996042500497 19960425 00497 SW 1996 4 25 HEEA966970 1 19960408 A 7712 206075739103 TORQUEMETER BELL 206 206L1 1182107 SW ENG TORQUE READS HIGH E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2761N 45277 TORQUEMETER INDICATES HIGH OUT OF TOLERANCE AT 60%. 1 G 7 1 3U H2SW 1996042500498 19960425 00498 1996 4 25 HEEA966972 4 19960408 A 3421 7660002113103 GYRO SKRSKY S76 S76A 8143006 NE COCKPIT VG DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 GYRO WILL NOT AUTOMATICALLY ERECT AFTER IT TURNS IN FLIGHT 1 G 7 2 3U H1NE 1996042500499 19960425 00499 1996 4 25 HEEA966973 4 19960408 A 3421 7660002113103 GYRO SKRSKY S76 S76A 8143006 NE COCKPIT VG DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 GYRO INTERMITTENTLY CAUSES ADI TO ROLL 90 DEGREES. KICKS OFF AFCS. 1 G 7 2 3U H1NE 1996042500500 19960425 00500 SW 1996 4 25 HEEA966974 1 19960408 A 6320 212075036101 INDICATOR BELL 412 412 1182202 SW GB OIL INOP E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7128R 36007 GR BOX INDICATOR NEEDLES INOPERATIVE. 1 G 7 2 4U H4SW 1996042500501 19960425 00501 EU 1996 4 25 HEEA966975 1 19960408 A 2841 1179405401 INDICATOR BOLKMS 117 BK117B1 5626012 EU FUEL QTY DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 191BK 7146 #2 SUPPLY TANK FUEL ADJUSTMENT SCREW COULD NOT ADJUST FUEL INDICATION PAST 25 KG. 1 G 7 2 3U H13EU 1996042500502 19960425 00502 SW 1996 4 25 HEEA966978 1 19960410 A 6220 206011149105 YOKE 206011100159 BELL 206 206L1 1182107 SW M/R BEARING FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1076Y 1203 A2388 45380 DISASSEMBLED TO COMPLY WITH 1200 HOUR INSPECTION. FOUND YOKE BEARING JOURNAL AND TRUNNION RACES BREAKING DOWN. SCRAPPED PARTS LOCALLY. ALSO SCRAPPED BEARINGS (4 EACH) P/N 206-011-113-001 AND (2 EACH) P/N 206-011-111-001. 1 G 7 1 3U H2SW 1996042500503 19960425 00503 1996 4 25 9609159608 4 19960422 A 3442 G1519 CONTROL PANEL DOUG DC9 DC932 3022066 WP FWD PEDESTAL MALFUNCTIONED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 608NW 47233 WEATHER RADAR SYSTEM WOULD NOT PAINT KNOWN WEATHER AFTER TAKEOFF. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. M AINTENANCE REPLACED RADAR CONTROL PANEL, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996042500504 19960425 00504 1996 4 25 9609169928 4 19960422 A 3442 RADAR DOUG DC9 DC931 3022065 WP FWD FUSELAGE MALFUNCTIONED A NWAA A UNSCHED LANDING O OTHER UK UNKNOWN 1 GL 01 8921E 45836 WEATHER RADAR SYSTEM FAILED EN ROUTE. RADAR WOULD NOT PAINT GROUND AND WAS SPOKING DOWN MIDDLE OF SCREEN. FLIGHT DIVER TED TO DTW DUE TO KNOWN THUNDERSTORMS AHEAD. MAINTENANCE REPLACED WAVE GUIDE ASSEMBLY AND MISSING SPRING AND POST. ALS O, REPLACED RADAR TRANSCEIVER AND ANTENNA, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996042500505 19960425 00505 WP 1996 4 25 96DHL804009 1 19960418 A 3260 CONNECTOR DOUG DC8 DC873F 302199F WP RT MLG DOOR SW DIRTY A T DHLA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 804DH 46124 ON CLIMB, RIGHT HAND GEAR DOOR UNSAFE LIGHT ON AFTER GEAR RETRACTION. CYCLED GEAR TWO TIMES LIGHT WENT OUT. CLEANED CA NNON PLUG AT SWITCH AND OPS CHECK NORMAL IAW MM 32-10-0. 2 L 7 4 4F RT 4A25 1996042500506 19960425 00506 SO 1996 4 25 SWIA95728 1 19960415 A 3260 LATCH MECH EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE NLG MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 212SW 120276 NOSE LANDING GEAR WOULD NOT CYCLE UP AND RED TRANSIENT 'A' AND 'B' LIGHTS STAYED ON. JACKED AIRCRAFT AND INSPECTED GEAR DOORS AND LATCHING MECHANISMS, FOUND NO DEFECTS. CYCLED GEAR NUMEROUS TIMES IN HANGER, ALL CHECKS NORMAL. DID FIND LA NDING GEAR LT HAND DOOR LATCH DISCONNECTED AFTER GOING BACK TO GATE AND INSPECTING. DOOR WAS HANGING DOWN. RELATCHED D OOR. 2 L 7 2 4T 4 T RT A31SO E20NE 1996042500507 19960425 00507 EA 1996 4 25 SWIA95730 1 19960418 A 3230 RETRACT MECH CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE NLG MALFUNCTIONED A SWIA O OTHER N FALSE WARNING CL CLIMB 1 NM 07 410SW 7066 NOSE GEAR DID NOT RETRACT AFTER TAKEOFF. ATTEMPTED QRH PROCEDURES WITH NO CHANGE. RECEIVED GEAR DISAGREE AND NOSE DOOR OPEN MESSAGE A FEW SECONDS LATER. INSPECTED NOSE GEAR AND COMPONENT, ADJUSTED DOOR PROX SENSOR, SWUNG GEAR PER RJ MM. PERFORMED FUNCTIONAL CHECK OF LANDING GEAR EXTENSION AND RETRACTION, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 1996042500508 19960425 00508 SO 1996 4 25 SWIA95731 1 19960420 A 5610 WINDSHIELD EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT COCKPIT FAILED A SWIA O OTHER O OTHER CL CLIMB 1 NM 07 195SW 120127 AT 15,000 FEET, HEARD LOUD THUMP AND LEFT WINDSHIELD CRAZED. NO EVIDENCE OF BIRD STRIKE. SLOWED DOWN AND STARTED DESCE ND. NO FURTHER PROBLEMS. REPLACED RIGHT WINDSHIELD PER MM 56-10-01. 2 L 7 2 4T 4 T RT A31SO E20NE 1996042500510 19960425 00510 NM 1996 4 25 96ZZZM691 1 19960218 A 5610 001A561D006001 WINDSHIELD DORNER DO32 DO328100 2996000 NM LT COCKPIT DELAMINATED A EQGA O OTHER O OTHER CR CRUISE 1 SW 19 340LS 774 191 3040 PILOTS LEFT SIDE WINDSHIELD DELAMINATED SEVERELY IN FLIGHT FROM ASE TO DFW. THE AIRCRAFT LANDED AT DFW WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS THEN FERRIED TO HOT WHERE THE WINDSHIELD WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVI CE. THIS IS AN ON GOING PROBLEM THAT THE MANUFACTURER IS AWARE OF. (M) 2 H 7 2 4T RT A45NM 1996042500511 19960425 00511 EU 1996 4 25 96ZZZM692 1 19960325 A 3260 MY2071839810 BRACKET AMD FALC20 FALCOND 2720304 EU LANDING GEAR FAILED A YIEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 815AA 205 YIP - AFTER TAKEOFF IN RETRACTING, LANDING GEAR WARNING HORN WOULD NOT SILENCE AND THE 3 RED GEAR LIGHTS REMAINED ON. L ANDING GEAR WAS EXTENDED NORMALLY AND AIRCRAFT RETURNED TO YIP WITHOUT INCIDENT. FOUND BROKEN 24G SWITCH LEVER ARM WHIC H WAS CAUSED BY A BROKEN LEVER ARM SUPPORT BRACKET. REPLACED BROKEN LEVER ARM AND LEVER ARM SUPPORT BRACKET. OPERATION ALLY CHECKED LANDING GEAR SYSTEM IAW FALCON MM 32-60-4. NO DEFECTS WERE NOTED. REFERENCE YIEA96012. 2 L 7 2 4F A7EU 1996042500512 19960425 00512 NM 1996 4 25 96ZZZM693 1 19960314 A 2910 6517840 HYD LINE BOEING 727 72722C 138400F NM NR 2 SPOILER CRACKED A CKSA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 23 727CK 19195 TOTAL LOSS OF 'A' HYDRAULIC SYSTEM IN FLIGHT. REMOVED AND REPLACED LINE, TRANSFERRED TO CARRYOVER NR 032 IAW EA 94-192. SERVICED HYD SYSTEM IAW MM 29-00-06. OPS CHECK GOOD ON GROUND HARD LINE. REPLACED WITH FLEX LINE WHICH IS REASON FOR C/O 4032. 2 L 7 3 4F A3WE 1996042500513 19960425 00513 WP 1996 4 25 96ZZZM694 1 19960309 A 3260 7000010101 SWITCH DOUG DC9 DC932 3022066 WP LT MLG FAILED A VJ6A E ENGINE SHUTDOWN N FALSE WARNING TO TAKEOFF 1 SO 11 902VJ 47177 FLT NR 360, RDU-BOS, LEFT MAIN GEAR UNSAFE INDICATION ON GEAR DOWN. REPLACED NR 1 MLG DOWN LOCK SWITCH, OPS CHECK NORMA L, REF 32-50-1. GEAR SWING ACCOMPLISHED. (M) 2 L 7 2 4F A6WE 1996042500514 19960425 00514 WP 1996 4 25 96ZZZM695 1 19960310 A 5711 SPAR CAP DOUG DC8 DC8F55 3021928 WP LT WING CRACKED A TC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 808CK 45817 RIGHT WING REAR SPAR CAP AT XW 69.50 HAS 2 CRACKS BETWEEN STIFFENERS, 2.5 THROUGH 7 INCHES. REPAIRED AFFECTED AREA AS P ER SRM 57-5-0. REFERENCE TC8A96024. 2 L 7 4 4F 4A25 1996042500515 19960425 00515 EU 1996 4 25 96ZZZM696 1 19960326 A 5270 91SE13 SWITCH BAG JETSTM JETSTM3201 1500217 EU PAX DOOR OUT OF ADJUST A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 436AM 10518 891 STL - FLT RN 7470 - PAX DOOR WARNING ILLUMINATED DURING FLIGHT. MAINTENANCE ISSUED DMI 52-2. MAINTENANCE LATER CLEARED DMI BY ADJUSTING DOOR MICROSWITCH, OPERATION CHECK GOOD. (M) 2 L 7 2 4T RT A56EU 1996042500516 19960425 00516 WP 1996 4 25 96ZZZM697 1 19960404 A 2161 60714621 TEMP CONTROLLER DOUG DC9 DC951 3022051 WP COCKPIT MALFUNCTIONED A A4JA A UNSCHED LANDING B M SMOKE/FUMES/ODORS/SPARKS OVER TEMP CL CLIMB 1 SO 15 919PJ 47663 AUTO TEMP CONTROLLER HAD FAILED (AUTO MODE) CAUSING THE SMELL OF HOT AIR AND SLIGHT SMOKE IN THE CABIN. AN ENGINE RUN W AS PERFORMED, CONTROLLING TEMP IN MANUAL MODE, CHECKED OK WITH NO OTHER DISCREPANCIES NOTED. AIR CONDITIONING SYSTEM AN D COMPONENTS CHECKED SATISFACTORY. AUTO TEMP CONTROL SYSTEM MEL PROCEDURES ACCOMPLISHED AND AIRCRAFT DEPARTED WITH NO F URTHER PROBLEMS NOTED. 2 L 7 2 4F A6WE 1996042500517 19960425 00517 EU 1996 4 25 96ZZZM698 1 19960205 A 3210 20098002 DRAG BRACE STBROS SD3 SD360 8100606 EU LT MLG MALFUNCTIONED A TRBA O OTHER J WARNING INDICATION AP APPROACH 1 SO 21 360MQ 28473 13587 DRG182984 SH3602 LEFT MAIN GEAR INDICATES UPLOCK, EMERGENCY LANDING ACCOMPLISHED. REMOVED AND REPLACED DRAG BRACE. 2 H 7 2 4T A41EU 1996042500518 19960425 00518 NE 1996 4 25 96ZZZM699 2 19960330 A 7200 ENGINE STBROS SD3 SD360 8100606 EU PWA PT6 PT6A65AR 52043 NE RIGHT MALFUNCTIONED A A GUUA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 828BE SH3749 FLT NR 396 - MCO/MIA - AFTER TAKEOFF, APPROXIMATELY 4000 FEET RIGHT ENGINE PRODUCED BANGING NOISE AND TORQUE FLUCTUATION S. PERFORMED PRECAUTIONARY SHUT DOWN OF RIGHT ENGINE AND RETURNED TO MCO. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED THE RIGHT ENGINE INLET, EXHAUST, CONTROLS AND BLEED VALVE WITH NO DEFECTS NOTED. PERFORMED POWER ASSURANCE AND STALL C HECK RUNS WITH NO DEFECTS NOTED. SERVICED ENGINE OIL. THE AIRCRAFT WAS SATISFACTORY TEST FLOWN FOR 1.5 HOURS. AIRCRAF T THEN RELEASED TO SERVICE. (M) 2 H 7 2 4T 4 T A41EU E4EA 1996042500519 19960425 00519 NE 1996 4 25 CAL960371 2 19960319 A 7250 772203 T3 BLADE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 2 ENGINE BROKEN A CALA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SW 09 76823 49483 717418 THE AIRCRAFT REJECTED TAKEOFF AT HIGH SPEED AFTER THE NR 2 ENGINE FAILED. THE ENGINE FAILURE WAS ACCOMPANIED BY A LOUD POP AND LOW N1. MAINTENANCE FOUND BLADES MISSING FROM COMPRESSOR WITH HEAVY DAMAGE TO TURBINE. THE NR 2 ENGINE WILL BE REMOVED AND REPLACED. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION. SHOP TEARDOWN FINDINGS REV EALED FAILURE OF A T3 BLADE. 2 L 7 2 4F 4 F A6WE E9NE 1996042500520 19960425 00520 NM 1996 4 25 CAL960373 1 19960320 A 2910 BACH80C08NN0290 FLEX HOSE BOEING 727 727243 138408D NM 'B' HYD SYS LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 17402 21265 FLT NR 477 - TPA - A/C LOST THE 'B' SYS HYD FLUID IN FLT. THE LOSS WAS ACCOMPANIED BY FLICKERING 'B' SYS HYD LOW PRESS LIGHTS. CHECKLIST PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MX FOUND THE HYD PRESS FLEX HOSE FROM THE NR 2 ELECTRIC 'B' PUMP LEAKING. THE HOSE WAS REPLACED USING 3000 PSI FLEX HOSE PER GMM 10-799-78, PAGE 14 . A DIP WAS ISSUED TO REPLACED THE INTERIM FLEX HOSE WITHIN 500 FLIGHTS OR 1200 FLIGHT HOURS. THE HYD SYSTEM WAS SERVI CED TO FULL. ALL CONTROL SURFACES WERE EXERCISED AND OPERATION WAS NORMAL WITH NO LEAKS NOTED. (M) 2 L 7 3 4F RT A3WE 1996042500521 19960425 00521 NM 1996 4 25 CAL960374 1 19960320 A 2913 6500103 HYD PUMP BOEING 727 727243 138408D NM NR 1 ENGINE FAILED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 12437 21270 FLT NR 1929 - IAH - THE NR 1 ENGINE 'A' SYSTEM HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATED IN FLIGHT. THE HYDRAULIC P RESSURE ON BOTH PUMPS APPEARED NORMAL. 'ABNORMAL' CHECKLIST PROCEDURES WERE FOLLOWED AND THE AIRCRAFT LANDED WITHOUT IN CIDENT. MAINTENANCE FOUND THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP SHAFT SHEARED. THE PUMP WAS REMOVED AND REPLACED. (M) 2 L 7 3 4F RT A3WE 1996042500522 19960425 00522 WP 1996 4 25 CAL960377 1 19960214 A 5320 BRACKET DOUG DC9 DC982 3022082 WP BS 1338 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14890 38914 49114 MIA - INSPECTION FOUND BRACKET PLATE CORRODED AT INTERSECTION OF FUSELAGE RIGHT CUSP FITTING AND FLOORBEAM, STATION 1338 . THE CORRODED PLATE WAS REMOVED AND A NEW PLATE WAS FABRICATED AND INSTALLED IAW SRM 51-01. (M) 2 L 7 2 4F A6WE 1996042500523 19960425 00523 WP 1996 4 25 CAL960378 1 19960212 A 5320 FASTENERS DOUG DC9 DC982 3022082 WP BS 1000/1005 BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14890 38914 49114 MIA - INSPECTION FOUND TWO FASTENER HEADS POPPED ON RIGHT SIDE OF FUSELAGE AT FS 1000 AND 1005 BETWEEN L18R AND L19R, BE LOW CUSP LINE. THE FASTENERS WERE REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5. (M) 2 L 7 2 4F A6WE 1996042500524 19960425 00524 WP 1996 4 25 CAL960379 1 19960211 A 5320 WEB DOUG DC9 DC982 3022082 WP PAX DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14890 38914 49114 MIA - INSPECTION FOUND HORIZONTAL WEB CORRODED AT THRESHOLD OF FORWARD ENTRY DOOR, 4 INCHES INBOARD OF AFT CORNER OF CUT OUT. THE CORROSION WAS REMOVED IAW SRM 53-01. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-01. (M) 2 L 7 2 4F A6WE 1996042500525 19960425 00525 WP 1996 4 25 CAL960380 1 19960211 A 5320 99365347C ANGLE DOUG DC9 DC982 3022082 WP DOOR SILL CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14890 38914 49114 MIA - INSPECTION FOUND THREE FLOOR SUPPORT 'Z' ANGLES CORRODED UNDER FLOORBOARD AT FORWARD ENTRY DOOR SILL AREA. THE FL OOR SUPPORT ANGLES WERE REMOVED AND REPLACED IAW SRM 51-10-4. (M) 2 L 7 2 4F A6WE 1996042500526 19960425 00526 WP 1996 4 25 CAL960381 1 19960209 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FS 807 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14890 38914 49114 MIA - INSPECTION FOUND A .5625 INCH CRACK IN FUSELAGE FAIRING SUPPORT ANGLE AT FS 807, BETWEEN L26R AND L27R. THE CRACK WAS STOP DRILLED. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-01. (M) 2 L 7 2 4F A6WE 1996042500527 19960425 00527 NM 1996 4 25 CAL960382 1 19960321 A 2910 HYD LINE BOEING 737 7372C0 1384488 NM PYLON CHAFED A CALA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS TO TAKEOFF 1 SW 09 14241 20070 FLT NR 1598 - GSO - THE AIRCRAFT LOST 'A' SYSTEM HYDRAULIC QUANTITY AFTER TAKEOFF FROM GSO. THE AIRCRAFT WAS RETURNED T O GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND HYDRAULIC SUPPLY LINE IN PYLON CHAFED THROUGH. THE LINE WAS REPLACED AND LEAK CHECK WAS GOOD. (M) 2 L 7 2 4F A16WE 1996042500528 19960425 00528 NM 1996 4 25 CAL960383 1 19960321 A 3350 BATTERY PACK BOEING 737 7372C0 1384488 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 73243 20072 FLT NR 1626 - CLE - INSPECTION FOUND BOTH THE INTERIOR AND EXTERIOR EMERGENCY LIGHTS AT RIGHT WING EMERGENCY EXIT INOPER ATIVE. THE CHARGER AND BATTERY PACK WERE REMOVED AND THE CONNECTIONS TO BOTH WERE CLEANED. EXTERIOR SOCKET WAS RELAMPE D AND OPERATION OF THE LIGHTS WAS GOOD. (M) 2 L 7 2 4F A16WE 1996042500529 19960425 00529 WP 1996 4 25 CAL960403 1 19960326 A 3260 PROX SWITCH DOUG DC9 DC982 3022082 WP LT MLG INOPERATIVE A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 819NY 49479 FLT NR 1823 - IAH - THE LT GEAR UNSAFE LIGHT AND GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION DEPARTI NG IAH. THE AUTO SPOILER 'DO NOT USE' LIGHT WAS ALSO ON. CYCLING THE GEAR DID NOT HELP. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT MLG AND DOOR LATCH PROXIMITY SWITCH INOPERATIVE. THE PROXIMITY SWITCH WAS REMOVED AND REPLACED. AN OPERATIONAL CHECK WAS PERFORMED AND SWITCH FUNCTION WAS GOOD. THE AUTO SPOILER SYSTEM WAS RESET AND THE LIGHT EXTINGUISHED. (M) 2 L 7 2 4F A6WE 1996042500530 19960425 00530 WP 1996 4 25 CAL960417 1 19960311 A 5320 3952158501 MOUNT SUPPORT DOUG DC9 DC982 3022082 WP C-2 GALLEY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14831 28910 49491 HOU - INSPECTION FOUND THE C-2 GALLEY AFT MOUNT SUPPORT CORRODED. THE MOUNT SUPPORT WAS REMOVED AND REPLACED IAW SRM 51 -30-5. (M) 2 L 7 2 4F A6WE 1996042500531 19960425 00531 WP 1996 4 25 CAL960418 1 19960314 A 5330 5911401 SKIN DOUG DC9 DC982 3022082 WP BS 120 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14831 28910 49491 HOOU - INSPECTION FOUND A SMALL DENT IN LEFT FUSELAGE SKIN AT STATION 120 ABOVE LONGERON 19. A REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 38. (M) 2 L 7 2 4F A6WE 1996042500532 19960425 00532 WP 1996 4 25 CAL960419 1 19960308 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 154 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14831 28910 49491 HOU - INSPECTION FOUND A SMALL DENT IN FORWARD LOWER FUSELAGE SKIN AT STATION 154, LONGERON 26L. A DOUBLER WAS INSTALLE D IAW SRM 53-04, FIGURE 38, SHEET 21. (M) 2 L 7 2 4F A6WE 1996042500533 19960425 00533 WP 1996 4 25 CAL960420 1 19960312 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP BS 1155 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14831 28910 49491 HOU - INSPECTION FOUND FLOOR SUPPORT CORRODED AT STATION 1155. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-30-5. (M) 2 L 7 2 4F A6WE 1996042500534 19960425 00534 WP 1996 4 25 CAL960421 1 19960318 A 5230 59101417 DOOR PAN DOUG DC9 DC982 3022082 WP CARGO DOOR GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14831 28910 49491 HOU - INSPECTION FOUND A GOUGE INBOARD OF HOLD OPEN ON AFT CARGO DOOR PAN. A DOUBLER WAS FABRICATED AND INSTALLED IAW E CRA 5230C01117. (M) 2 L 7 2 4F A6WE 1996042500535 19960425 00535 WP 1996 4 25 CAL960422 1 19960311 A 5320 993653557 SUPPORT DOUG DC9 DC982 3022082 WP G-2 GALLEY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14831 28910 49491 HOU - INSPECTION FOUND CORROSION ON G-2 GALLEY FORWARD ATTACH POINT SUPPORT. A SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-30-2. (M) 2 L 7 2 4F A6WE 1996042500536 19960425 00536 WP 1996 4 25 CAL960423 1 19960311 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP BS 788 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14831 28910 49491 HOU - INSPECTION FOUND A .875 INCH CRACK IN CABIN FLOOR SUPPORT AT STATION 788, AIRCRAFT CENTERLINE. A NEW DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2. (M) 2 L 7 2 4F A6WE 1996042500537 19960425 00537 WP 1996 4 25 CAL960424 1 19960329 A 3222 STRUT DOUG DC9 DC981 3022081 WP NLG FLAT A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 37882 48027 FLT NR 303 - EWR - THE N/G WOULD NOT RETRACT AFTER T/O FROM EWR. THE GEAR HANDLE WAS CYCLED SEVERAL TIMES, BUT WOULD NO T RAISE BEYOND HALFWAY POINT. THE AUTO SPOILER 'DO NOT' USE LIGHT WAS ON AND THE A/C WOULD NOT PRESSURIZE. THE A/C WAS RETURNED TO EWR WHERE IT LANDED W/O INCIDENT. MX SERVICED THE NLG STRUT TO PROPER X-DIMENSION. THE N/G WAS JACKED AND ALL FUNCTIONS CHECKED GOOD DURING N/G RETRACTION TEST. THE N/G FAILED TO RETRACT ON A SUBSEQUENT FLT, BUT CYCLING THE GEAR REMEDIED THE PROBLEM. THE N/G STRUT WAS SERVICED WITH NITROGEN AGAIN AND THE GEAR WAS LUBRICATED. A DIP WAS ISSUE D FOR FULL SERVICE OF THE NOSE STRUT. FULL SERVICE OF THE NOSE STRUT ACCOMP PER GMM 09-31-01 AND DIP WAS CLOSED. (M) 2 L 7 2 4F A6WE 1996042500538 19960425 00538 WP 1996 4 25 CAL960426 1 19960330 A 2150 A/C PACK DOUG DC9 DC982 3022082 WP RT A/C PACK INOPERATIVE A CALA A B G UNSCHED LANDING EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 SW 09 83870 48056 FLT NR 1620 - DEN - THE A/C CABIN BEGAN TO CLIMB AT 5000 FPM WHILE AT FL 330 EN ROUTE FROM LAS TO CLE. AN EMERGENCY DES CENT WAS INITIATED, THE OXYGEN MASKS WERE DEPLOYED, AND THE AIRCRAFT WAS DIVERTED TO DEN WHERE IT LANDED WITHOUT FURTHER INCIDENT. THE RT PACK AUTO TEMP CONTROL SYS HAD BEEN PREVIOUSLY PLACARDED INOPERATIVE. MAINTENANCE REPLACED THE RIGHT PACK ANTICIPATOR AND THE PLACARD WAS REMOVED. OPERATION OF BOTH PACKS WAS NORMAL. ALL OXYGEN MASKS HAD OPERATED PROPE RLY. ALL OXYGEN GENERATORS WERE REMOVED AND REPLACED IAW MM 35-22-01 AND ALL OXYGEN MASKS WERE RESTOWED IAW MM 35-22-02 . (M) 2 L 7 2 4F A6WE 1996042500539 19960425 00539 NM 1996 4 25 CAL960427 1 19960227 A 5311 FRAME BOEING 727 727243 138408D NM BS 1166 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17410 42993 21663 INSPECTION FOUND A 1.5 INCH CRACK IN AFT BAG PIT FLOOR LEVEL FRAME AT BS 1166, RBL 24. THE CRACKED AREA WAS CUT OUT. R EPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-40-4, 51-10-2, AND 51-30-2. (M) 2 L 7 3 4F RT A3WE 1996042500540 19960425 00540 NM 1996 4 25 CAL960428 1 19960221 A 5320 FLOOR SUPPORT BOEING 727 727243 138408D NM BS 643 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17410 42993 21663 INSPECTION FOUND THE FORWARD FUSELAGE CARGO FLOOR SUPPORT CORRODED AND A CRACK ON UPPER FLANGE AT BS 643, RBL 20.5. THE CRACKED AREA OF FLOOR SUPPORT WAS CUT OUT. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, AND MM 51-40-5. (M) 2 L 7 3 4F RT A3WE 1996042500541 19960425 00541 NM 1996 4 25 CAL960431 1 19960225 A 5315 FLOORBEAM BOEING 727 727243 138408D NM BS 350 OVERSIZED HOLE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17410 42993 21663 INSPECTION FOUND OVERSIZED HOLE ON MAIN CABIN INTERIOR FLOORBEAM AT BS 350, RBL 40. THE EFFECTED SECTION WAS REMOVED. A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-1, 51-10-2, 51-30-8 AND MM 51-20-2. (M) 2 L 7 3 4F RT A3WE 1996042500542 19960425 00542 NM 1996 4 25 CAL960432 1 19960222 A 5315 FLOORBEAM WEB BOEING 727 727243 138408D NM BS 312 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17410 42993 21663 INSPECTION FOUND A .375 INCH CRACK IN LEFT FRAME OF FLOOR BEAM WEB OF RIGHT FORWARD LAV, BS 312, RBL 29. THE CRACKED AR EA WAS REMOVED. A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-30-2. (M) 2 L 7 3 4F RT A3WE 1996042500543 19960425 00543 NM 1996 4 25 CAL960433 1 19960222 A 5313 STRINGER BOEING 727 727243 138408D NM BS 620 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17410 42993 21663 INSPECTION FOUND STRINGER 28R CORRODED AT FORWARD CARGO COMPARTMENT BS 620. THE CORRODED SECTION OF STRINGER WAS CUT OU T. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-3, 51-10-2, AND 51-30-2. (M) 2 L 7 3 4F RT A3WE 1996042500544 19960425 00544 NM 1996 4 25 CAL960434 1 19960219 A 5753 SKIN BOEING 727 727243 138408D NM LT TE MID FLAP SEPARATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17410 42993 21663 INSPECTION FOUND A 9 INCH SECTION OF SEPARATION ON AFT EDGE OF LEFT INBOARD MID FLAP TRAILING EDGE. THE INNER AND OUTER SKIN AND HONEYCOMB WERE REMOVED. INNER AND OUTER SKIN AND HONEYCOMB WERE FABRICATED AND COLD BONDED IAW SRM 51-40-6, 5 1-10-3, AND 57-50-2. (M) 2 L 7 3 4F RT A3WE 1996042500545 19960425 00545 NM 1996 4 25 CAL960435 1 19960219 A 5720 652165835 CHANNEL BOEING 727 727243 138408D NM WS 447.9 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17410 42993 21663 INSPECTION FOUND A .5 INCH CRACK AT INBOARD SIDE OF OUTBOARD TRAILING EDGE LOWER SUPPORT CHANNEL, RIGHT WING STATION 447 .9. THE CRACKED CHANNEL WAS REMOVED. A NEW CHANNEL WAS DRILLED AND INSTALLED IAW SRM 51-10-1, 51-10-2, AND 51-30-2. ( M) 2 L 7 3 4F RT A3WE 1996042500546 19960425 00546 NE 1996 4 25 CAL960436 2 19960401 A 7250 TURBINE BLADES DOUG DC9 DC932 3022066 WP PWA JT8 JT8D15 52051 NE NR 2 ENGINE BROKEN A CALA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SW 09 33506 47765 701018 THE NR 2 ENGINE BEGAN TO VIBRATE WITH N1 DROPPING OFF TO 40 PERCENT DURING CLIMB-OUT OF CLE. THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND METAL IN THE NR 2 ENGINE TAILPIPE. THE NR 2 ENGINE WAS REMO VED AND REPLACED. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION. SHOP FINDINGS REVEALED TWO BROK EN FIRST STAGE TURBINE BLADES DUE TO IMPACT. 2 L 7 2 4F 4 F A6WE E2EA 1996042500547 19960425 00547 NM 1996 4 25 CAL960440 1 19960403 A 2120 AIR DISTR BOEING 757 757224 1384958 NM CABIN SMOKE A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 17104 27294 FLT NR 234 - EWR - SMOKE APPEARED IN THE CABIN WHILE IN CRUISE FLT AT FL 330. THE A/C SMOKE CHECKLIST WAS COMPLETED. T HE RECIRCULATION FANS, RIGHT ENGINE BLEED, AND RIGHT PACK WERE TURNED OFF. THE SMOKE CEASED AND THE A/C LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE INSPECTED BOTH ENGINE SUPPLY DUCTS, THE APU BLEED DUCTS, AND THE PACK DUCTING FOR OIL CONT AMINATION. NO CONTAMINATION WAS FOUND. THE RIGHT RECIRCULATION FILTERS WERE REPLACED DUE TO CONTAMINATION. THE LEFT R ECIRCULATION FILTERS WERE REPLACED AS A PRECAUTION. AIR CONDITIONING OIL CONTAMINATION REMOVAL PROCEDURES WERE PERFORME D IAW MM 21-00-01 AND NO SMOKE WAS NOTED. THE SMOKE COULD NOT BE DUPLICATED. (M) 2 L 7 2 4F RT A2NM 1996042500548 19960425 00548 NM 1996 4 25 EISA96037 1 19960321 A 5320 WEB BOEING 727 727223 1384074 NM FS 328 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20191 LEFT SIDE DOG HOUSE, STATION 328 WEB BULGED. REMOVED CORROSION IAW SRM 51-10-3, FABRICATED DOUBLER REPAIR AND INSTALLED REPAIR WET IAW DWG 25363-5320. (M) 2 L 7 3 4F A3WE 1996042500549 19960425 00549 NM 1996 4 25 EISA96038 1 19960325 A 5400 SKIN BOEING 727 727223 1384074 NM S-DUCT CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20191 SEVERAL CRACKS ON RIGHT SIDE, UPPER S-DUCT. CUT OUT CRACKED SECTION OF S-DUCT. FABRICATED AND INSTALLED DOUBLER WET PE R SRM 54-10-3. (M) 2 L 7 3 4F A3WE 1996042500550 19960425 00550 NM 1996 4 25 EISA96039 1 19960319 A 3610 DUCT BOEING 727 727223 1384074 NM 13TH STAGE SEPARATION A EISA K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 07 315NE 20191 NR 1 ENGINE FIRE WARNING AT POWER. REPAIRED DAMAGED WIRING AND REPLACED FIRE WALL SENSOR PERFORMED HARDNESS TEST ON ENG INE MOUNTS, REPLACED ALL ENGINE MOUNT VIBRATION ISOLATIONS. REPLACED BURNED NYLON SEALS AND REPLACED ENG COWL DUE TO HE AT DAMAGE. (M) 2 L 7 3 4F A3WE 1996042500551 19960425 00551 NM 1996 4 25 F3LA96011 1 19960410 A 3530 4566M37B042NM PBE BOEING 737 737301 1384611 NM CABIN MALFUNCTIONED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 DEN - FLT 401 - PRIOR TO DEAPRTURE, FLIGHT CREW REPORTED, CREW PBE UNSERVICEABLE. REPLACED PBE AND CHECKED OK. (M) 2 L 7 2 4F RT A16WE 1996042500552 19960425 00552 WP 1996 4 25 HALA9626 1 19960323 A 3350 P4010049 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 709HA 4975 47764 HNL - FIRST HALF OF FLOOR EMERGENCY LIGHTS INOP. FLOOR STRIP, STOMPING ON FLOOR CAN MAKE THEM COME ON. REPLACED EMERGE NCY LIGHT BATTERY. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1996042500553 19960425 00553 WP 1996 4 25 HALA9629 1 19960327 A 3230 39147385001 BUNGEE CYL DOUG DC9 DC951 3022051 WP NLG FAILED A HALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 13 699HA DVA0633 47763 HNL - FLT NR 535 - NOSE GEAR WOULD NOT EXTEND, (RED LIGHT) DOORS DID NOT OPEN, ALTERNATE GEAR EXTENSION PROCEDURES WAS P ERFORMED, SUCCESSFULLY. REPLACED NOSE GEAR BUNGEE CYLINDER. LEAK AND OPERATIONAL CHECK OK PER MM 32-30-00. (M) 2 L 7 2 4F A6WE 1996042500554 19960425 00554 WP 1996 4 25 HALA9630 1 19960402 A 3233 39281375001 ACTUATOR DOUG DC9 DC951 3022051 WP NLG MALFUNCTIONED A CALA K NONE J WARNING INDICATION DE DESCENT 1 SW 09 699HA FAS166 47763 NLG - FLT NR 319 - ON ARRIVAL IN HNL, FIRST SELECTION OF 'GEAR DOWN' SYSTEM DID NOT RESPOND. RE-SELECTED 'GEAR DOWN' AN D GEAR EXTENDED NORMALLY. REPLACED NOSE GEAR ACTUATOR CYLINDER PER MM 32-32-6. RE-RIGGED NOSE GEAR DOORS PER MM 32-22- 1. GEAR SWING CHECKS OK. (M) 2 L 7 2 4F A6WE 1996042500555 19960425 00555 NM 1996 4 25 N3VR96001 1 19960227 A 5313 STRINGER BOEING 727 727231 1384079 NM BS 1050 CORROSION B N3VR K NONE O OTHER IN INSP/MAINT 1 SO 03 590CA 57434 20098 REF N/R 3498, STRINGER 21LT AT BS 1050 HAS CORROSION BLOWOUT. CORRODED STRINGER REMOVED FABRICATED REPAIR PARTS FROM 12 FEET BAC-1498-132, .063 EXTRUSION AND 12 FEET BAC 1498-143, .050 EXTRUSION IAW SRM 53-10-3. INSTALLED REPAIR PARTS IAW SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1996042500556 19960425 00556 NM 1996 4 25 N3VR96002 1 19960226 A 5320 INTERCOSTAL BOEING 727 727231 1384079 NM BS 1020 CORROSION B N3VR K NONE O OTHER IN INSP/MAINT 1 SO 03 590CA 57434 20098 REF N/R 3465, FLOOR INTERCOSTAL BLOWN OUT CORROSION AT BS 1020 APPROXIMATELY 30 INCHES LEFT OF CENTER LINE. FABRICATED NEW PART, 21 INCHES PIECE OF 130188-1-1 7075-T6511 T-EXTRUSION AND 12 INCH BY 21 INCH 7075-T6 .125 IAW SRM 51-10-1, ALOD INE AND PRIMED AND PAINTED IAW SRM 51-10-2, INSTALLED IAW SRM 51-20-2. (M) 2 L 7 3 4F A3WE 1996042500557 19960425 00557 NM 1996 4 25 N3VR96003 1 19960217 A 5320 69550012 FITTING BOEING 727 727231 1384079 NM BS 760 CRACKED B N3VR K NONE O OTHER IN INSP/MAINT 1 SO 03 590CA 57434 20098 REF N/R 3269, FITTING CRACKED UNDER RIGHT FORWARD EMERGENCY EXIT DOOR FRAME AFT OF B/S 760, FRAME. FABRICATED FITTING F ROM 7078-T6 LOCATED AND DRILLED TO AIRCRAFT, TREATED AND PRIMED IAW SRM 51-10-2, INSTALLED IAW SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1996042500558 19960425 00558 NM 1996 4 25 N3VR96004 1 19960217 A 5313 STRINGER BOEING 727 727231 1384079 NM BS 720 CRACKED B N3VR K NONE O OTHER IN INSP/MAINT 1 SO 03 590CA 57434 20098 REF N/R 3268, STRINGER CRACKED AFT OF B/S 720B, RT STRINGER 15 RT AT WING FLOOD LIGHT HOUSING. STOP DRILLED CRACK AND F ABRICATED REPAIR PARTS FROM 7075-T6 IAW SRM 53-10-3. INSTALLED PARTS IAW SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1996042500559 19960425 00559 NM 1996 4 25 N3VR96005 1 19960228 A 5347 BAC1520792 SEAT TRACK BOEING 727 727231 1384079 NM BS 990 CORROSION B N3VR K NONE O OTHER IN INSP/MAINT 1 SO 03 590CA 57434 20098 REF N/R 3589 - SEAT TRACK CORROSION LEFT OUTBOARD TRACK F/S 990. TRANSFERRED FASTENER HOLES TO NEW SEAT TRACK SECTION P /N BAC 1520-792, TREATED AND PRIMED, INSTALLED NEW SEAT TRACK IAW SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1996042500560 19960425 00560 NM 1996 4 25 N3VR96006 1 19960227 A 5315 FLOOR BEAM BOEING 727 727231 1384079 NM BS 380 CORROSION B N3VR K NONE O OTHER IN INSP/MAINT 1 SO 03 590CA 57434 20098 REF N/R 3560, FLOOR BEAM CORROSION STATION 380 LEFT OF SEAT TRACK NR 4 APPROXIMATELY 12 INCHES AREA. REMOVED CORROSION IAW SRM 51-10-6 NEG MATERIAL REMOVED, TREATED AND PRIMED IAW SRM 51-10-2. (M) 2 L 7 3 4F A3WE 1996042500561 19960425 00561 NM 1996 4 25 N3VR96007 1 19960227 A 5330 SKIN BOEING 727 727231 1384079 NM BS 430 CRACK B N3VR K NONE O OTHER IN INSP/MAINT 1 SO 03 590CA 57434 20098 REF N/R 3563, FUSELAGE SKIN CRACK STATION 430 RIGHT BETWEEN STRINGER 16 AND 17 RT. REMOVED DAMAGED SKIN IAW SRM 53-30-3 , FABRICATED INTERNAL DOUBLER FROM 7575-T6 .090 8 INCHES BY 12 INCHES IAW SRM 53-30-3, TREATED AND PRIMED IAW SRM 51-10- 2. INSTALLED REPAIR DOUBLER IAW SRM 53-30-3. (M) 2 L 7 3 4F A3WE 1996042500562 19960425 00562 NM 1996 4 25 N3VR96008 1 19960227 A 5347 BAC1520792 SEAT TRACK BOEING 727 727231 1384079 NM BS 420-46 CORROSION B N3VR K NONE O OTHER IN INSP/MAINT 1 SO 03 590CA 57434 20098 REF N/R 3562, SEAT TRACK NR 5 HAS CORROSION STATION 420 TO 460. FABRICATED NEW SEAT TRACK FROM BAC 1520-792 TREATED AND PRIMED, INSTALLED IAW SRM 51-30-2, 51-10-1 AND 51-10-2. (M) 2 L 7 3 4F A3WE 1996042500563 19960425 00563 NM 1996 4 25 N3VR96009 1 19960227 A 5347 BAC1520792 SEAT TRACK BOEING 727 727231 1384079 NM BS 344.440 CORROSION B N3VR K NONE O OTHER IN INSP/MAINT 1 SO 03 590CA 57434 20098 REF N/R 3561, SEAT TRACK HAS CORROSION STATION 344 TO 440 TRACK NR 4. REMOVED SEAT TRACK, DRILLED OUT NEW SEAT TRACK SE CTION P/N BAC 1520-792, TREATED AND PRIMED IAW 51-10-2, INSTALLED IAW SRM 51-30-2 AND 51-10-1. (M) 2 L 7 3 4F A3WE 1996042500564 19960425 00564 NM 1996 4 25 N3VR96010 1 19960228 A 5312 652427649 BLKHD FITTING BOEING 727 727231 1384079 NM BS 1183 CORROSION B N3VR K NONE O OTHER IN INSP/MAINT 1 SO 03 590CA 57434 20098 REF N/R 3592, FS 1183 BULKHEAD TO FLOOR ATTACH FITTING IS BLOWN IN CORNER LEFT SIDE STRINGER 17 LEFT. REMOVED AND REPLA CED FITTING IAW SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1996042500565 19960425 00565 NM 1996 4 25 N3VR96011 1 19960228 A 5347 BAC1520792 SEAT TRACK BOEING 727 727231 1384079 NM BS 344-400 CORROSION B N3VR K NONE O OTHER IN INSP/MAINT 1 SO 03 590CA 57434 20098 REF N/R 3591, SEAT TRACK NR 3 FS 344 TO 400 CORRODED. REMOVED NR 3 SEAT TRACK PICKED UP HOLES IN NEW SEAT TRACK P/N BAC 1520-792, TREATED AND PRIMED IAW 51-10-2. INSTALLED IAW SRM 51-30-2 AND 51-10-1. (M) 2 L 7 3 4F A3WE 1996042500566 19960425 00566 NM 1996 4 25 N3VR96012 1 19960228 A 5510 CHORD BOEING 727 727231 1384079 NM RT HORIZ STAB CORROSION B N3VR K NONE O OTHER IN INSP/MAINT 1 SO 03 590CA 57434 20098 REF N/R 3642, RIGHT HORIZONTAL STABILIZER FRONT UPPER CHORD CORRODED STATION 170, 188, 195, 205 (INTERNAL). REMOVED COR ROSION IAW SRM 51-10-6, FORWARD INFORMATION TO ENGINEERING MATERIAL. REMOVED DETERMINED TO BE ACCEPTABLE PER ENGINEERIN G, PREPARED AREA PER ENGINEERING REPORT 96-027 TREATED, PRIMED AND RETURNED AREA BACK TO NORMAL. (M) 2 L 7 3 4F A3WE 1996042500567 19960425 00567 NM 1996 4 25 N3VR96013 1 19960228 A 5320 ANGLE BOEING 727 727231 1384079 NM FWD LAVATORY CORROSION B N3VR K NONE O OTHER IN INSP/MAINT 1 SO 03 590CA 57434 20098 REF N/R 3629, FORWARD LAV AISLE SIDE WALL SUPPORT ANGLE CORRODED FORWARD SECTION. FABRICATED FLOOR SUPPORT FROM EXTRUSI ON 60-357 7075-T6 PRIMED IAW 51-10-2. INSTALLED IAW SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1996042500568 19960425 00568 NM 1996 4 25 N3VR96014 1 19960228 A 5315 BEAM BOEING 727 727231 1384079 NM BS 312 CORROSION B N3VR K NONE O OTHER IN INSP/MAINT 1 SO 03 590CA 57434 20098 REF N/R 3658, SURFACE CORROSION ON FLOOR BEAM STATION 312 AT CLIP NUT HOLES FT OF COCKPIT DOOR (BOTH SURFACES). REMOVED CORROSION IAW SRM 51-10-6 AT 3 INCHES LT OF C/L AND AT 19 INCHES OF C/L MAX MATERIAL REMOVED .050, TREATED AND PRIMED I AW SRM 51-10-2. FABRICATED REPAIR IAW ENGINEERING REPORT NR 96-027. INSTALLED REPAIR IAW ENGINEERING REPORT 96-027. (M ) 2 L 7 3 4F A3WE 1996042500569 19960425 00569 NM 1996 4 25 N3VR96015 1 19960229 A 5315 CHORD BOEING 727 727231 1384079 NM BS 1030 CORROSION B N3VR K NONE O OTHER IN INSP/MAINT 1 SO 03 590CA 20098 REF N/R 3699, FS 1030, 20 INCHES LT OF C/L FLOOR BEAM CORROSION BEYOND BLEND OUT LIMITS UPPER CHORD. REMOVED CORRODED S ECTION OF FLOOR BEAM, FABRICTED REPAIR PARTS IAW SRM 53-10-8 USING MATERIAL BAC 1505-100617, 7075-T73 TREATED AND PRIMED BEAM AND REPAIRED PARTS IAW SRM 51-10-2. INSTALLED REPAIR PART IAW SRM 53-10-8. (M) 2 L 7 3 4F A3WE 1996042500570 19960425 00570 NM 1996 4 25 N3VR96016 1 19960229 A 5315 FLOOR BEAM BOEING 727 727231 1384079 NM BS 312 CORROSION B N3VR K NONE O OTHER IN INSP/MAINT 1 SO 03 590CA 57434 20098 REF N/R 3691, FS 312, 37 INCHES RIGHT OF C/L FLOOR BEAM HAS CORROSION BEYOND BLEND LIMITS. REMOVED DAMAGED SECTION OF F LOOR BEAM IAW SRM 51-30-2. FABRICATED MATERIAL FROM TM 560-23934 PICKED UP HOLES IAW SRM 51-10-1, TREATED AND PRIMED IA W SRM 51-10-2, INSTALLED IAW SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1996042500571 19960425 00571 NM 1996 4 25 N3VR96017 1 19960228 A 5313 STRINGER BOEING 727 727231 1384079 NM BS 1166 CORROSION B N3VR K NONE O OTHER IN INSP/MAINT 1 SO 03 590CA 57434 20098 REF N/R 3600, STRINGER 22 LT AT FS 1166 HAS CORROSION. CUT OUT DAMAGED SECTION OF STRINGER IAW SRM 53-10-3, FABRICATED REPAIR PART USING STRINGER MATERIAL BAC 1498-142 AND BAC 1498-132 IAW SRM 53-10-3, TREATED ADN PRIMED IAW SRM 51-10-2 IN STALLED PARTS IAW SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1996042500572 19960425 00572 NM 1996 4 25 N3VR96018 1 19960227 A 5315 6023934 FLOOR BEAM BOEING 727 727231 1384079 NM BS 344 CORROSION B N3VR K NONE O OTHER IN INSP/MAINT 1 SO 03 590CA 57434 20098 REF N/R 3559, FLOOR BEAM HAS CORROSION STATION 344 C/L LT AND RT 10 INCHES. FABRICATED T-CAP IAW SRM 51-40-4 USING T-EX TRUSION 60-23934 TREATED AND PRIMED, INSTALLED IAW SRM 51-40-4. (M) 2 L 7 3 4F A3WE 1996042500573 19960425 00573 NM 1996 4 25 N3VR96019 1 19960227 A 5320 INTERCOSTAL BOEING 727 727231 1384079 NM BS 420 CORROSION B N3VR K NONE O OTHER IN INSP/MAINT 1 SO 03 590CA 57434 20098 REF N/R 3572, INTERCOSTAL FORWARD OF STATION 420 CORROSION BETWEEN SEAT TRACK NR 3 AND NR 4. REMOVED DAMAGED AREA, FABR ICATED AND INSTALLED DOUBLER IAW SRM 53-10-4 AND 51-30-2 USING EXTRUSION 1506-3418, 7075-T6. INSTALLED INTERCOSTAL IAW SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1996042500574 19960425 00574 NM 1996 4 25 N3VR96020 1 19960228 A 5315 FLOOR BEAM BOEING 727 727231 1384079 NM BS 344 CORROSION B N3VR K NONE O OTHER IN INSP/MAINT 1 SO 03 590CA 57434 20098 REF N/R 3626, CORROSION STATION 344 AT CLIP NUT HOLE FLOOR BEAM PANEL NR 2 FORWARD EDGE BOTH SURFACES. REMOVED CORROSIO N IAW SRM 51-10-6. INSPECTION FOUND OUT OF LIMITS, CUT OUT DAMAGED SECTION. FABRICATED REPAIR PARTS IAW SRM 53-10-8-8- 2A USING BAC 1505-100617 EXT, 7075-T73 EXT .050 ANGLE, 7075-T73 EXT .090 ANGLE, 7075-T6, .090 FILLER, 7075-T6 .080 STRAP , 7075-T6 .050 STRAP IAW SRM 51-10-2. INSTALLED REPAIR ITEMS IAW SRM 53-10-2 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1996042500575 19960425 00575 EU 1996 4 25 RAIA960322 1 19960316 A 5270 SP4594 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGGAGE BAY OUT OF ADJUST A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 556HK 1113 41073 DCA - FLT NR 7742 - CARGO DOOR WARNING LIGHT ILLUMINATED ON TAKEOFF. MAINTENANCE ISSUED DMI 52-3, MAINTENANCE LATER CLE ARED DMI BY ADJUSTING BAGGAGE DOOR MICROSWITCH. (M) 2 L 7 2 4T RT A41NM 1996042500576 19960425 00576 EU 1996 4 25 RAIA960325 1 19960324 A 7712 31024766 TQ SIGNAL COND BAG JETSTM JETSTM3201 1500217 EU RT ENG OUT OF ADJUST A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 337TE 8533 8533 929 STL - FLT NR 7034 - RIGHT ENGINE WOULD NOT MAKE TARGET TORQUE. MAINTENANCE ADJUSTED TORQUE SIGNAL CONDITIONER, PERFORME D GROUND RUNS, OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A56EU 1996042500577 19960425 00577 1996 4 25 RAIA960327 4 19960323 A 3442 6227337001 RADAR R/T UNIT BAG JETSTM JETSTM3201 1500217 EU FWD AVIONICS FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 425AM 8690 870 STL - FLT NR 7029 - RADAR QUIT WORKING DURING FLIGHT. MAINTENANCE REPLACED RADAR R/T, OPERATION CHECK GOOD. (M) 2 L 7 2 4T RT A56EU 1996042500578 19960425 00578 EU 1996 4 25 RAIA960328 1 19960324 A 5270 SP4594 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU CARGO BAY OUT OF ADJUST A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 550HK 2949 41039 CARGO DOOR WARNING ILLUMINATED DURING TAKEOFF ROLL. MAINTENANCE ISSUED DMI 52-3. MAINTENANCE LATER CLEARED DMI BY ADJU STING DOOR MICROSWITCH. (M) 2 L 7 2 4T RT A41NM 1996042500579 19960425 00579 EU 1996 4 25 RAIA960331 1 19960326 A 2711 82363 ACTUATOR AEROSP ATR42 ATR42300 8680920 EU LT AILERON DIRTY A RAIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CE 03 425TE 13147 125 STL - FLT NR 7398 - IN FLIGHT ROLL TRIM INOP. MAINTENANCE CLEANED CONNECTOR ON AILERON TRIM ACTUATOR, SYSTEM CHECKS GOO D. (M) 2 H 7 2 4T RT A53EU 1996042500580 19960425 00580 EU 1996 4 25 RAIA960332 1 19960327 A 3230 5EN16N95 WOW SWITCH BAG JETSTM JETSTM3201 1500217 EU NOSE GEAR OUT OF ADJUST A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 436AM 10521 891 STL - FLT NR 7420 - GEAR WOULD NOT RETRACT. MAINTENANCE ADJUSTED WOW SWITCH, GEAR SWING GOOD. (M) 2 L 7 2 4T RT A56EU 1996042500581 19960425 00581 EU 1996 4 25 RAIA960333 1 19960328 A 3060 B40610 DE-ICE LEAD JETAIR JETSTM JETSTM4101 1500501 EU LT PROP FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 03 551HK 3118 41040 STL - FLT NR 7023 - PROP DE-ICE WARNING ILLUMINATED. MAINTENANCE REPLACED THE PROP DE-ICE LEAD ON NR 3 BLADE OF LEFT PR OP, OPERATION CHECK GOOD. (M) 2 L 7 2 4T RT A41NM 1996042500582 19960425 00582 EU 1996 4 25 RAIA960334 1 19960329 A 2133 2099K021000 OUTFLOW VLV JETAIR JETSTM JETSTM4101 1500501 EU FWD BULKHEAD CONTAMINATED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 558HK 730 41071 STL - FLT NR 7326 - PRESSURIZATION SQUEAL FROM FORWARD PRESSURE BULKHEAD DURING CLIMB. MAINTENANCE CLEANED AND LUBRICAT ED FORWARD OUTFLOW VALVE, OPERATION CEHCK GOOD. (M) 2 L 7 2 4T RT A41NM 1996042500583 19960425 00583 1996 4 25 RAIA960401 4 19960401 A 3425 7001676903 FLIGHT DIR PANEL BAG JETSTM JETSTM3201 1500217 EU INST PANEL FAILED A RAIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 864AE 6084 864 SAN - FLT NR 4777 - ON START FLIGHT DIRECTOR PANEL FILLED COCKPIT WITH SMOKE. MAINTENANCE REMOVED AND REPLACED FLIGHT D IRECTOR PANEL. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A56EU 1996042500584 19960425 00584 CE 1996 4 25 S2YA960004 1 19960329 A 2120 1295500511 DUCT BEECH 1900 1900D 1154162 CE LT ACM CRACKED A S2YA K NONE O OTHER IN INSP/MAINT 1 GL 13 891SK 4818 UE89 DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND BLEED AIR DUCT, P/N 129-550051-1, CRACKED ALL AROUND THE BASE OF THE AC M OVERTEMPERATURE SENSOR WELD FITTING. THE PART WAS REPLACED. SUBMITTER STATES,WE HAVE NOW HAD THREE OCCURENCES ON DIF FERENT AIRCRAFT, SAME MODEL. (M) 2 L 7 2 4T RT A24CE 1996042500585 19960425 00585 NM 1996 4 25 TAOA049602 1 19960401 A 2612 1061096125 FIRE ELEMENT BOEING 727 727254 138408L NM NR 1 ENGINE FAILED A TAOA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 15 916TS 3916 20437 ON TAKEOFF ROLL, NR 1 ENGINE FIRE WARNING LIGHT AND BELL WENT ON, ABORTED TAKEOFF, FLIGHT NR 6421. REMOVED AND REPLACED NR 1 ENGINE LOWER FIRE WARNING SYSTEM ELEMENT. (M) 2 L 7 3 4F A3WE 1996042500586 19960425 00586 WP 1996 4 25 TC8A96006 1 19960308 A 2910 HYD SYSTEM DOUG DC8 DC862 3021970 WP HYD RESERVOIR REQ'D SERV A TC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 803MG 45910 ON TAXI, FOUND HYDRAULIC QUANTITY INDICATOR TO STANDPIPE LEVEL. SERVICED HYDRAULIC RESERVOIR, CHECKED ALL SYSTEMS FOR L EAKAGE, NO LEAKS FOUND. (M) 2 L 7 4 4F 4A25 1996042500587 19960425 00587 WP 1996 4 25 TC8A96007 1 19960319 A 2612 CLAMP DOUG DC8 DC8F54 3021926 WP NR 3 ENG LOOSE A TC8A O OTHER N FALSE WARNING CR CRUISE 1 GL 23 802CK 45679 NR 3 ENGINE FIRE WARNING LIGHT AND BELL COMES ON, PROCEED AS FOM. FOUND CLAMP LOOSE ON PNEUMATIC MANIFOLD TO PYLON. RE POSITIONED AND TIGHTENED CLAMP, OPS CHECK GOOD IAW DC-8 MM 36-0. (M) 2 L 7 4 4F 4A25 1996042500588 19960425 00588 WP 1996 4 25 TC8A96008 1 19960320 A 2730 4710542 ARM ASSEMBLY DOUG DC8 DC851 3021920 WP RT ELEVATOR BROKEN A TC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 805CK 45649 STAB TRIM, OR PROBLEM WITH LOAD CAUSING FULL DOWN ELEVATOR. ON POST FLIGHT INSPECTION FOUND RIGHT ELEVATOR GEAR TAB CRA NK ARMS BROKEN. REPLACED INBOARD AND OUTBOARD CRANK ARMS AND INBOARD LINK. CHECKED ELEVATOR RIGGING, FOUND GOOD PER RE F 27-15-0. (M) 2 L 7 4 4F 4A25 1996042500589 19960425 00589 NE 1996 4 25 TC8A96009 2 19960320 A 7320 PS4 LINE DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3B 52039 NE NR 2 ENGINE LOOSE A TC8A O OTHER O OTHER TO TAKEOFF 1 GL 23 803MG 45910 669173 NR 2 ENGINE WILL NOT ACCELERATE PAST IDLE POWER WHEN THROTTLE IS ADVANCED. FOUND PS4 LINE LOOSE, TIGHTENED. ALSO, CLEA NED PS4 FILTER, OPS CHECKED ON RUN UP AS PER MM 71-00 NORMAL. (M) 2 L 7 4 4F 4 F 4A25 1E8 1996042500590 19960425 00590 WP 1996 4 25 TC8A96010 1 19960322 A 2697 WIRE DOUG DC8 DC8F54 3021926 WP NR 3 ENGINE FAILED A TC8A O OTHER N FALSE WARNING CR CRUISE 1 GL 23 802CK 45679 NR 3 ENGINE FIRE WARNING, NO FIRE. ISOLATED FIRE SENSOR ELEMENT ON AFT DOOR AND REPAIRED WIRES AT CANNON PLUG. CHECKED AS PER MM 26-0-3, OPS NORMAL. (M) 2 L 7 4 4F 4A25 1996042500591 19960425 00591 WP 1996 4 25 TC8A96011 1 19960323 A 2612 CLAMP DOUG DC8 DC8F54 3021926 WP NR 3 ENG LOOSE A TC8A O OTHER N FALSE WARNING CR CRUISE 1 GL 23 802CK 45679 ENGINE FIRE NR 3 AT FL 280, FIRE EXTINGUISHED. POST FLIGHT NR 3 ENGINE, NO FIRE DAMAGE DETECTED CONTRARY TO COCKPIT WAR NING PROCEDURES. DETERMINED FIRE WARNING CAUSED BY LEAK AT PNEUMATIC DUCT ATTACHING CLAMP. REMOVED AND REPLACED CLAMP AND DID ENGINE RUN AT POWER. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 4 4F 4A25 1996042500592 19960425 00592 1996 4 25 TC8A96012 4 19960328 A 3421 WIRE DOUG DC8 DC8F55 3021928 WP LT ATTITUDE IND BROKEN A TC8A C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 23 808CK 45817 CAPTAINS ATTITUDE INDICATOR TUMBLED ON TAKEOFF ROLL. TAKEOFF ABORTED AT 90 KNOTS. REPAIRED BROKEN WIRE AT CAPTAINS ATT ITUDE INDICATOR. PERFORMED HIGH SPEED TAXI, SYSTEM OPS CHECKS GOOD. (M) 2 L 7 4 4F 4A25 1996042500593 19960425 00593 WP 1996 4 25 TC8A96013 1 19960311 A 5511 RIBS DOUG DC8 DC8F55 3021928 WP LT HORIZ STAB CRACKED A TC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 808CK 45817 LEFT HORIZONTAL STAB L/E HAS 3 RIBS CORRODED, LEVEL 2. REPAIRED AFFECTED AREA PROPERLY AS PER SRM 55-3-0. (M) 2 L 7 4 4F 4A25 1996042500594 19960425 00594 WP 1996 4 25 TC8A96014 1 19960311 A 5511 RIB DOUG DC8 DC8F55 3021928 WP RT HORIZ STAB CORRODED A TC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 808CK 45817 RIGHT HORIZONTAL STABILIZER L/E INTERNAL PART RIB HAS CORROSION, LEVEL 2. REMOVED CORROSION, TREATED AREA, AND REPAIRED INTERNAL PART RIB AS NECESSARY PER SRM 55-2-3, 55-3-0. (M) 2 L 7 4 4F 4A25 1996042500595 19960425 00595 WP 1996 4 25 TC8A96015 1 19960311 A 5320 DOUBLER DOUG DC8 DC8F55 3021928 WP BS 265-275 CORRODED A TC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 808CK 45817 MAIN CARGO COMPARTMENT AROUND FORWARD LAVATORY FLOOR TRACK DOUBLER HAS CORROSION, LEVEL 2, BETWEEN STATION 265 AND 275 ( RT SIDE). (M) 2 L 7 4 4F 4A25 1996042500596 19960425 00596 WP 1996 4 25 TC8A96016 1 19960312 A 5321 FLOOR DOUG DC8 DC8F55 3021928 WP BS 141-245 CORRODED A TC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 808CK 45817 COCKPIT FLOOR FROM FS 141 THROUGH FS 245 LEFT SIDE (AROUND NR 91 ACCESS PANEL), HAS CORROSION, LEVEL 2. REMOVED CORROSI ON AND REPAIRED AFFECTED AREA PROPERLY AS PER SRM 52-4-0. (M) 2 L 7 4 4F 4A25 1996042500597 19960425 00597 WP 1996 4 25 TC8A96017 1 19960307 A 5720 DOUBLER DOUG DC8 DC8F55 3021928 WP WS 408.343 BROKEN A TC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 808CK 45817 LW T/E LOWER SURFACE XW 408.343 HAS DOUBLER BROKEN AND CRACKED (5 INCHES). MADE AND INSTALLED NEW DOUBLER AS PER SRM 57 -2-3. (M) 2 L 7 4 4F 4A25 1996042500598 19960425 00598 WP 1996 4 25 TC8A96018 1 19960307 A 5720 RIVETS DOUG DC8 DC8F55 3021928 WP WS 230.5 LOOSE A TC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 808CK 45817 LEFT WING, STATION XRS 230.500 T/E LOWER PART SHOWS STRUCTURAL REPAIR WITH 4 LOOSE RIVETS AND BUCKED HEAD OVERSIZED. RE PAIRED AFFECTED AREA AS REQUIRED PER SRM 57-2-1. (M) 2 L 7 4 4F 4A25 1996042500599 19960425 00599 WP 1996 4 25 TC8A96019 1 19960307 A 5720 DOUBLER DOUG DC8 DC8F55 3021928 WP WS 60.250 CRACKED A TC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 808CK 45817 LW T/E LOWER SURFACE XW 60.250, DOUBLER HAS A CRACK 4.5 INCH. REPLACED DOUBLER AS PER SRM 57-2-1. (M) 2 L 7 4 4F 4A25 1996042500600 19960425 00600 WP 1996 4 25 TC8A96020 1 19960307 A 5753 DOUBLER DOUG DC8 DC8F55 3021928 WP RT TE FLAP BROKEN A TC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 808CK 45817 RW T/E FLAP LOWER SURFACE ACTUATOR ROD DOUBLER BROKEN, 1 INCH. MADE AND INSTALLED DOUBLER AT AFFECTED AREA AS EPR SRM 5 7-2-1. (M) 2 L 7 4 4F 4A25 1996042500601 19960425 00601 WP 1996 4 25 TC8A96021 1 19960307 A 5720 DOUBLER DOUG DC8 DC8F55 3021928 WP WS 300.344 BROKEN A TC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 808CK 45817 RIGHT WING ERS 300.344, TE STEEL DOUBLER LOWER SURFACE IS BROKEN. MADE AND INSTALLED DOUBLER AT AFFECTED AREA AS REQUIR ED PER SRM 57-2-3. (M) 2 L 7 4 4F 4A25 1996042500602 19960425 00602 WP 1996 4 25 TC8A96022 1 19960311 A 5350 BRACKET DOUG DC8 DC8F55 3021928 WP TAIL CONE CORRODED A TC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 808CK 45817 TAIL CONE, HORIZONTAL SUPPORT AND BRACKET BASE RIGHT SIDE HAS LEVEL 2 CORROSION. MADE AND INSTALLED DOUBLER AS REQUIRED PER SRM 53-2-5. (M) 2 L 7 4 4F 4A25 1996042500603 19960425 00603 WP 1996 4 25 TC8A96023 1 19960308 A 5280 DOOR SKIN DOUG DC8 DC8F55 3021928 WP RT MLG CRACKED A TC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 808CK 45817 RIGHT MAIN LANDING GEAR DOOR UPPER SURFACE SKIN CRACKED, 1 INCH. REPAIRED AFFECTED AREA AS PER SRM 57-2-1. (M) 2 L 7 4 4F 4A25 1996042500604 19960425 00604 WP 1996 4 25 TC8A96024 1 19960310 A 5711 SPAR CAP DOUG DC8 DC8F55 3021928 WP RT WING CRACKED A TC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 808CK 45817 RIGHT WING REAR SPAR CAP AT XW 69.50 HAS 2 CRACKS BETWEEN STIFFENERS, 2.5-7 INCHES. REPAIRED AFFECTED AREA AS PER SRM 5 7-5-0. (M) 2 L 7 4 4F 4A25 1996042500605 19960425 00605 WP 1996 4 25 TC8A96025 1 19960307 A 5320 DOUBLER DOUG DC8 DC8F55 3021928 WP BS 1080-1040 CORRODED A TC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 808CK 45817 AFT FUSELAGE STATION 1080 AND STATION 1040, RIGHT STRINGER NR 34 DOUBLER HAS LEVEL 2 CORROSION. REPAIRED DOUBLER AS PER SRM 53-4-0. (M) 2 L 7 4 4F 4A25 1996042500606 19960425 00606 WP 1996 4 25 TC8A96026 1 19960307 A 5313 STRINGER DOUG DC8 DC8F55 3021928 WP BS 1080-1040 CORRODED A TC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 808CK 45817 AFT FUSELAGE STATION 1080 AND STATION 1040, RIGHT STRINGER NR 32 HAS CORROSION LEVEL 2. TREATED AND REPAIRED STRINGER 3 2 RT, MADE AND INSTALLED UPPER PLATE AS PER SRM 52-4-0. (M) 2 L 7 4 4F 4A25 1996042500607 19960425 00607 WP 1996 4 25 TC8A96027 1 19960307 A 5313 STRINGER DOUG DC8 DC8F55 3021928 WP BS 1220-1240 CORRODED A TC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 808CK 45817 AFT FUSELAGE FS 1220 AND 1240, RIGHT STRINGER NR 34 HAS CORROSION, LEVEL 2. NR 34 STRINGER REPAIRED AS PER SRM 53-4-0. (M) 2 L 7 4 4F 4A25 1996042500608 19960425 00608 WP 1996 4 25 TC8A96028 1 19960307 A 5320 DOUBLER DOUG DC8 DC8F55 3021928 WP FS 1080 CORRODED A TC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 808CK 45817 AFT FUSELAGE FS 1080, RIGHT STRINGER NR 34 DOUBLER HAS CORROSION, LEVEL 2. MADE AND INSTALLED NEW DOUBLER AS PER SRM 51 -10-O. (M) 2 L 7 4 4F 4A25 1996042500609 19960425 00609 WP 1996 4 25 TC8A96029 1 19960308 A 5320 WALL DOUG DC8 DC8F55 3021928 WP BS 560 CRACKED A TC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 808CK 45817 LOWER FORWARD CARGO COMPARTMENT WALL, STATION 560, BOTTOM AREA RIGHT SIDE EDGE CRACKED, 2 INCHES. AFFECTED AREA REPAIRE D AS REQUIRED PER SRM 51-1-19, 52-4-0. (M) 2 L 7 4 4F 4A25 1996042500610 19960425 00610 WP 1996 4 25 TC8A96030 1 19960308 A 5320 DOUBLER DOUG DC8 DC8F55 3021928 WP BS 560 BROKEN A TC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 808CK 45817 LOWER FORWARD CARGO COMPARTMENT LINING STATION 560 TOP SURFACE RIGHT SIDE AFT DOOR HOUSING HAS DOUBLER BROKEN. MADE AND INSTALLED DOUBLER AT AFFECTED AREA AS REQUIRED PER SRM 52-4-0. (M) 2 L 7 4 4F 4A25 1996042500611 19960425 00611 WP 1996 4 25 TC8A96031 1 19960308 A 5320 DOUBLER DOUG DC8 DC8F55 3021928 WP BS 520 CRACKED A TC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 808CK 45817 LOWER FORWARD CARGO COMPARTMENT STATION 520 TOP SURFACE RIGHT SIDE LINING SPLICE DOUBLER CRACKED, 2 INCHES. REPAIRED DO UBLER AT AFFECTED AREA AS REQUIRED PER SRM 52-4-0. (M) 2 L 7 4 4F 4A25 1996042500612 19960425 00612 WP 1996 4 25 TC8A96032 1 19960308 A 5320 DOUBLER DOUG DC8 DC8F55 3021928 WP BS 1120 CORRODED A TC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 808CK 45817 LOWER AFT CARGO COMPARTMENT STATION 1120 RIGHT SIDE 532R, CARGO DOOR DOUBLER IS BROKEN, ALSO CORRODED, LEVEL 2. REPAIRE D AFFECTED AREA AND CCONTROLLED CORROSION AS PER SRM 52-4-0. (M) 2 L 7 4 4F 4A25 1996042500613 19960425 00613 WP 1996 4 25 TC8A96034 1 19960309 A 5320 DOUBLER DOUG DC8 DC8F55 3021928 WP BS 880 BROKEN A TC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 808CK 45817 CARGO COMPARTMENT FLOOR STATION 880 MLG UPPER SKIN DOUBLER BETWEEN STACK AND WEB IS BROKEN. REPAIRED AFFECTED AREA AS PER SRM 52-1-0. (M) 2 L 7 4 4F 4A25 1996042500614 19960425 00614 WP 1996 4 25 TC8A96035 1 19960311 A 5321 FLOOR DOUG DC8 DC8F55 3021928 WP BS 265-295 CORRODED A TC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 808CK 45817 MAIN CARGO COMPARTMENT, GALLEY AND FWD LAV AREA FLOOR HAS LEVEL 2 CORROSION, STATION 265 TO 295. MADE AND INSTALLED GAL LEY AND FWD LAV AREA FLOOR AS PER SRM 52-4-0. (M) 2 L 7 4 4F 4A25 1996042500615 19960425 00615 WP 1996 4 25 TC8A96036 1 19960311 A 5315 FLOOR BEAM DOUG DC8 DC8F55 3021928 WP FS 1504 CORRODED A TC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 808CK 45817 AFT MAIN CARGO COMPARTMENT FS 1504 BEAM UPPER SIDE HAS CORROSION, LEVEL 2. REPAIRED AFFECTED AREA AS REQUIRED PER SRM 5 2-2-0. (M) 2 L 7 4 4F 4A25 1996042500616 19960425 00616 WP 1996 4 25 TC8A96037 1 19960312 A 5347 FLOOR TRACKS DOUG DC8 DC8F55 3021928 WP CARGO COMPT BROKEN A TC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 808CK 45817 MAIN CARGO COMPARTMENT FLOOR 5 TRACKS ARE BROKEN. REPAIRED TRACKS AS PER 52-1-0. (M) 2 L 7 4 4F 4A25 1996042500617 19960425 00617 WP 1996 4 25 TC8A96038 1 19960312 A 5321 FLOOR DOUG DC8 DC8F55 3021928 WP BS 460/480/500 CORRODED A TC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 808CK 45817 MAIN CARGO COMPARTMENT FLOOR RT SIDE STATION 460, STATION 480 AND STATION 500, TRACK AND WEB AREA HAS CORROSION, LEVEL 2 , 5 AREAS. REMOVED AND REPAIRED TRACK AS PER SRM 52-4-0. (M) 2 L 7 4 4F 4A25 1996042500618 19960425 00618 WP 1996 4 25 TC8A96039 1 19960315 A 5315 FLOOR BEAM DOUG DC8 DC8F55 3021928 WP FS 1530 CORRODED A TC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 808CK 45817 FUSELAGE AFT SECTION FS 1530, FLOOR BEAM HAS CORROSION AT 2 PLACES LEVEL 2, REQUIRES REPAIRING, 2 INCH BY 3 INCH AND 2 I NCH BY 4 INCH. REPAIRED AFFECTED AREA AS REQUIRED PER SRM 53-4-0. (M) 2 L 7 4 4F 4A25 1996042500619 19960425 00619 WP 1996 4 25 TC8A96040 1 19960316 A 5320 SUPPORT DOUG DC8 DC8F55 3021928 WP CARGO COMPT CORRODED A TC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 808CK 45817 LOWER AFT CARGO COMPARTMENT, 'D' ENTRANCE DOOR CENTER METAL PANEL SUPPORT HAS LEVEL 2 CORROSION AND SHEARED NUTS. MADE AND INSTALLED DOOR CENTER METAL PANEL SUPPORT. REMOVED AND REPLACED ANCHOR NUTS AS PER SRM 52-4-0. (M) 2 L 7 4 4F 4A25 1996042500620 19960425 00620 NE 1996 4 25 TSAA9679007 2 19960328 A 7260 71700 GEARBOX BOEING 737 737297 1384480 NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE STRIPPED STUDS A TSAA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 13 726AL 22426 FLT NR 291 - HNL-LIH - NR 2 ENGINE LOST OIL PRESSURE AND OIL QUANTITY. SHUTDOWN ENGINE AND FOLLOWED QRH. PERFORMED JT8 D ENGINE OIL FILTER HOUSING ASSY. FLY HOME REPAIR IAW STANDARD PRACTICE MANUAL 8-06, PAGE 1 AND 2. SERVICED OIL TO FUL L. FERRY A/C TO HNL. REPLACED NR 2 ENGINE GEARBOX. FOUND OIL FILTER HOUSING MOUNT STUDS ON GEARBOX STRIPPED. OPS CHE CK AND LEAK CHECK WITH HIGH POWER RUN OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F 4 F A16WE E2EA 1996042500621 19960425 00621 NE 1996 4 25 TSAA9679008 2 19960328 A 7261 O-RING BOEING 737 737297 1384480 NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE FAILED A TSAA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 13 726AL 22426 FLT NR 88, - LIH-HNL - NR 2 ENGINE LOST ALL OIL. FOLLOWED QRH. SHUTDOWN ENGINE. REPLACED OIL FILTER O-RING. SERVICED OIL. GROUND OPS CHECK AND LEAK CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F 4 F A16WE E2EA 1996042500622 19960425 00622 NE 1996 4 25 TWRA9619 2 19960406 A 7200 ENGINE BOEING 747 747121 1384871 NM PWA JT9 JT9D7A 52054 NE NR 1 DAMAGED A TWRA E A ENGINE SHUTDOWN UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 EA 15 617FF 71681 1630 19650 662270 NR 1 ENGINE SHUTDOWN IN FLIGHT DUE TO LOUD BANG. RETURNED TO LIMA, PERU. NR 1 ENGINE EXPERIENCED TURBINE FAILURE. ENG INE REPLACED. (M) 2 L 7 4 4F 4 F A20WE E20EA 1996042500623 19960425 00623 NM 1996 4 25 USAA360355 1 19960403 A 5320 693535214 TIE CLIP BOEING 737 7372B7 1384560 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 280AU 34606 22892 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK BS 747 AT STRINGER 5R TIE CLIP. MODIFIED PART NR 69-3535 2-14, REPAIRED PER EO 5393G227. (M) 2 L 7 2 4F A16WE 1996042500624 19960425 00624 WP 1996 4 25 USAA960337 1 19960328 A 5512 SKIN DOUG DC9 DC931 3022065 WP HORIZ STAB LE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 997VJ 69642 69642 47336 PIT - DURING Q-4/C-6 INSPECTION, FOUND 1.5 INCH CRACK UPPER LEADING EDGE SURFACE HORIZONTAL STABILIZER LEFT SIDE APPROXI MATELY 6 FEET OUTBOARD OF VERT STAB. INSTALLED DOUBLER REPAIR .071 2024TS ALU PER SRM 55-03 FIG 3 AND SRM 55-01 FIG 2. (M) 2 L 7 2 4F A6WE 1996042500625 19960425 00625 WP 1996 4 25 USAA960338 1 19960328 A 5320 99101513 CUSP MEMBRANE DOUG DC9 DC931 3022065 WP BS 617 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 997VJ 69642 47336 PIT - DURING Q-4/C-6 INSPECTION, FOUND TWO 2 INCH CRACKS IN CUSP MEMBRANE STATION 617 RIGHT SIDE. REPLACED SECTION OF C USP MEMBRANE FROM STATION 598 TO 637 PER SRM 53-05 FIG 97. (M) 2 L 7 2 4F A6WE 1996042500626 19960425 00626 WP 1996 4 25 USAA960339 1 19960328 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 945 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 997VJ 69642 47336 PIT - DURING Q-4/C-6 INSPECTION, FOUND 1 INCH CRACK IN LONGERON 17L, AT STATION 945. SPLICED IN LONGERON SECTION PER US AIR TYPICAL REPAIR 53-10-17. (M) 2 L 7 2 4F A6WE 1996042500627 19960425 00627 WP 1996 4 25 USAA960340 1 19960328 A 5311 BELT FRAME DOUG DC9 DC931 3022065 WP BS 180 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 997VJ 69642 47336 PIT - DURING Q-4/C-6 INSPECTION, FOUND A .25 INCH CRACK AT FASTENER STA 180, BELT FRAME LONGERON 23L. INSTALLED FILLER AND DOUBLER REPAIR PER SRM 53-03, FIGURE 4. (X) 2 L 7 2 4F A6WE 1996042500628 19960425 00628 WP 1996 4 25 USAA960341 1 19960328 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 180/200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 997VJ 69642 47336 PIT - DURING Q-4/C-6 INSPECTION, FOUND .25 INCH CRACKS AT FASTENER HOLES LONGERON 23L STATION 180 AND STATION 200. SPLI CED IN SECTION OF LONGERON FROM STATION 160 TO STATION 230 PER SRM 53-02 FIG 2. (M) 2 L 7 2 4F A6WE 1996042500629 19960425 00629 WP 1996 4 25 USAA960342 1 19960328 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 180 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 997VJ 69642 47336 PIT - DURING Q-4/C-6 INSPECTION, FOUND .25 INCH CRACK IN LONGERON 4L AT STATION 180. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 2. (M) 2 L 7 2 4F A6WE 1996042500630 19960425 00630 WP 1996 4 25 USAA960343 1 19960328 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 965 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 997VJ 69642 47336 PIT - DURING Q-4/C-6 INSPECTION, FOUND .25 INCH CRACK IN LONGERON 12R AT ATTACH FASTENERS STATION 965. REPLACED SECTION OF LONGERON BY SPLICING PER USAIR TYPICAL REPAIR 53-10-17. (M) 2 L 7 2 4F A6WE 1996042500631 19960425 00631 WP 1996 4 25 USAA960344 1 19960328 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 160 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 997VJ 69642 47336 PIT - DURING Q-4/C-6 INSPECTION, FOUND .25 INCH CRACK AT FASTENER HOLES STATION 160 LONGERON 25L. SPLICED IN NEW SECTIO N OF LONGERON STATION 150 TO 190 PER SRM 53-02 FIG 2. (M) 2 L 7 2 4F A6WE 1996042500632 19960425 00632 WP 1996 4 25 USAA960345 1 19960328 A 5220 5913195 PAN DOUG DC9 DC931 3022065 WP EMER EXIT DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 997VJ 69642 47336 PIT - DURING Q-4/C-6 INSPECTION, FOUND .5 INCH CRACK IN FORWARD LEFT OVERWING EMERGENCY EXIT IN DOOR PAN BOTTOM FORWARD NR 5 STOP. INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 52-20-03 AND SRM 52-05 FIG 51. (M) 2 L 7 2 4F A6WE 1996042500633 19960425 00633 WP 1996 4 25 USAA960346 1 19960328 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 160/200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 997VJ 69642 47336 PIT - DURING Q-4/C-6 INSPECTION, FOUND .25 INCH CRACK IN FASTENER HOLES LONGERON 24L STATION 160 AND 200. REPLACED SECT ION OF LONGERON BY SPLICING PER SRM 53-02 FIG 2. (M) 2 L 7 2 4F A6WE 1996042500634 19960425 00634 EU 1996 4 25 USAA960347 1 19960331 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU RT AC BAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 483US 20716 11233 PIT - DURING SIP VISIT INSPECTION, FOUND .375 INCH CRACK RIGHT AIRCONDITION BAY SKIN REF SIP 53-10-19. INSTALLED DOUBLE R REPAIR PER SRM 53-02-18 FIG 12. (M) 2 L 7 2 4F RT A20EU 1996042500635 19960425 00635 EU 1996 4 25 USAA960348 1 19960322 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU BS 2620/2200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 480AU 21430 11229 PIT - DURING SIP VISIT INSPECTION, FOUND 1.5 INCH CRACK RIGHT NOSE LANDING GEAR BAY SKIN STATION 2620 AND 2200, SIP REF 53-10-19. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER SRM 53-02-07. (M) 2 L 7 2 4F RT A20EU 1996042500636 19960425 00636 EU 1996 4 25 USAA960349 1 19960322 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU BS 4850 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 480AU 21430 11229 PIT - DURING SIP VISIT INSPECTION, FOUND .375 INCH CRACK UPPER AFT CORNER SKIN OF SERVICE DOOR FRAME AT STATION 4850, RE F SIP 53-10-20. INSTALLED DOUBLER REPAIR PER SRM 53-02-16. (M) 2 L 7 2 4F RT A20EU 1996042500637 19960425 00637 WP 1996 4 25 USAA960350 1 19960323 A 5313 LONGERON DOUG DC9 DC931 3022065 WP FS 427-408 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 970VJ 74491 47050 PIT - DURING C-6 CHECK INSPECTION, FOUND TWO .25 INCH CRACKS IN LONGERON 16R FRAME 427 AND LONGERON 17R FRAME 408, 427 E DDY CURRENT INSPECTION. INSTALLED NEW SECTIONS OF LONGERON 16R AND 17R PER SRM 53-02 FIG 2 AND USAIR EA NR 32408. (M) 2 L 7 2 4F A6WE 1996042500638 19960425 00638 WP 1996 4 25 USAA960351 1 19960323 A 5320 DOOR FRAME DOUG DC9 DC931 3022065 WP CARGO COMPT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 970VJ 74491 47050 PIT - DURING C-6 CHECK INSPECTION, FOUND THREE .5 INCH CRACKS IN SKIN 7TH, 8TH AND 13TH RIVITS ABOVE STOP TOP FORWARD CO RNER FORWARD CARGO DOR FRAME EDDY CURRENT INSPECTION. INSTALLED DOUBLER REPAIR PER USAIR EA NR 32409 AND SRO 09530117. (M) 2 L 7 2 4F A6WE 1996042500639 19960425 00639 NM 1996 4 25 USAA960352 1 19960403 A 5313 STRINGER BOEING 737 7372B7 1384560 NM BS 950-990 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 280AU 34606 22892 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION IN STRINGER CHANNEL ,APPROX 10 INCHES IN LENGTH AND THREE 4 IN CHES IN LENGTH, STATION 950-990 STRINGER 27L. REPLACED STRINGER FROM BS 950-990, REPAIRED PER SRM 53-10-3. CORROSION T ASK NR C53-208-01, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996042500640 19960425 00640 NM 1996 4 25 USAA960353 1 19960403 A 5320 693535214 TIE CLIP BOEING 737 7372B7 1384560 NM BS 706 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 280AU 34606 22892 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK BS 706 AT STRINGER 4L TIE CLIP. MODIFIED PART NR INSTALL ED 69-35352-14, REPAIRED PER EO 5393G227. (M) 2 L 7 2 4F A16WE 1996042500641 19960425 00641 NM 1996 4 25 USAA960354 1 19960403 A 5320 693535214 TIE CLIP BOEING 737 7372B7 1384560 NM BS 706 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 280AU 34606 22892 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK BS 706 AT STRINGER 6L TIE CLIP. MODIFIED PART NR INSTALL ED, 69-35352-14, REPAIRED PER EO 5393G227. (M) 2 L 7 2 4F A16WE 1996042500642 19960425 00642 NM 1996 4 25 USAA960356 1 19960403 A 3233 BRACKET BOEING 737 7372B7 1384560 NM BS 233 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 280AU 34606 22892 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CRACK APPROXIMATELY 1 INCH AT WEB NOSE GEAR ACTUATOR SUPPORT BRACKET STA TION 233. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2. (M) 2 L 7 2 4F A16WE 1996042500643 19960425 00643 NM 1996 4 25 USAA960357 1 19960403 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 986.5 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 280AU 34606 22892 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 71 INCHES BY 3 INCHES CORROSION FLOOR BEAM BS 986.5 LBL 25 TO RBL 46. F ILLER T-CAP AND SPLICES, REPAIRED PER SRM 53-10-9 TR 53-10-05C. CORROSION TASK NR C53-107-02. (M) 2 L 7 2 4F A16WE 1996042500644 19960425 00644 NM 1996 4 25 USAA960358 1 19960403 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 947.5 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 280AU 34606 22892 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 71 INCHES BY 30 INCHES CORROSION FLOOR BEAM BS 947.5 LBL 51 TO RBL 20. R EPAIRED FLOOR BEAM, REPAIRED PER TR 53-10-05C, EA 41019. (M) 2 L 7 2 4F A16WE 1996042500645 19960425 00645 NM 1996 4 25 USAA960359 1 19960403 A 5320 FLOOR SUPPORT BOEING 737 7372B7 1384560 NM BS 270 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 280AU 34606 22892 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 14 INCH CORRODED AREA COCKPIT ENTRANCE BS 270.0 4 INCHES LBL - 10 INCHES RBL FLOOR SUPPORT. INSTALLED Z-ANGLE REPAIR, REPAIRED PER TR 53-20-04. CORROSION TASK NR C53-107-01. CORRO SION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996042500646 19960425 00646 NM 1996 4 25 USAA960360 1 19960403 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 360 GOUGES A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 280AU 34606 22892 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND TWO .5 INCH GOUGES AT BS 360 BL ZERO LBL 12 FLOOR BEAM. INSTALLED REPAI R STRAPS, REPAIRED PER TR53-10-01A. (M) 2 L 7 2 4F A16WE 1996042500647 19960425 00647 NM 1996 4 25 USAA960361 1 19960403 A 5320 CHORD BOEING 737 7372B7 1384560 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 280AU 34606 22892 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK AT LOWER FAST HOLE OF INNER CHORD ANGLE BS 616 RIGHT FRAME WL 203. INSTALLED REPAIR ANGLE AND FILLER, REPAIRED PER EA 40996. (M) 2 L 7 2 4F A16WE 1996042500648 19960425 00648 NM 1996 4 25 USAA960362 1 19960403 A 5313 STRINGER BOEING 737 7372B7 1384560 NM BS 520-540 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 280AU 34606 22892 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH CORRODED AREA STRINGER 26R BS 520-540. INSTALLED STRINGER REPAIR , REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996042500649 19960425 00649 NM 1996 4 25 USAA960363 1 19960403 A 5313 STRINGER BOEING 737 7372B7 1384560 NM BS 966 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 280AU 34606 22892 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION IN STRINGER (APPROX 3 INCHES LONG) STRINGER 26L AT STATION 966 . INSTALLED STRINGER REPAIR, REPAIRED PER SRM 53-10-3 FIG 1. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996042500650 19960425 00650 NM 1996 4 25 USAA960364 1 19960403 A 5320 T-CAP BOEING 737 7372B7 1384560 NM BS 344 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 280AU 34606 22892 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION AT 2 NUT PLATE HOLES T-CAP, STATION 344 LBL 12 TO RBL 12. REP LACED T-CAPS, REPAIRED PER TR 53-10-13. CORROSION TASK NR C53-107-01, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996042500651 19960425 00651 NM 1996 4 25 USAA960365 1 19960403 A 5311 FRAME BOEING 737 7372B7 1384560 NM BS 500 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 280AU 34606 22892 DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA ON FRAME AT BS 500 STRINGER 26R. INSTALLED DOU BLER, REPAIRED PER SRM 51-40-3. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996042500652 19960425 00652 WP 1996 4 25 USAAD96032 1 19960325 A 2130 45501635 LINE DOUG DC9 DC931 3022065 WP COCKPIT OVERHEAD CRIMPED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 970VJ 47050 PIT - FL 441 - AFTER TAKEOFF FROM PIT AND REACHING 6000 FEET, CREW COULD NOT PRESSURIZE THE AIRCRAFT. FLIGHT RETURNED T O PIT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND A CRIMPED SENSE LINE TO THE PRESSURE CONTROLLER. LINE WAS REPLACED AND REPOSITIONED SO AS NOT TO CAUSE A CRIMPING CONDITION. (M) 2 L 7 2 4F A6WE 1996042500653 19960425 00653 WP 1996 4 25 USAAD96033A 1 19960326 A 3220 AN815A BOLTS DOUG DC9 DC931 3022065 WP NOSE GEAR MISSING A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 921VJ 48141 YOW - FL 1171 - UPON GEAR RETRACTION, THE NOSE GEAR UNSAFE LIGHT FAILED TO EXTINGUISH. NOISE FROM THAT AREA INDICATED T HAT THE DOORS WERE NOT CLOSED. FLIGHT RETURNED TO YOW AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND TWO BOLTS MISSING FROM THE NOSE GEAR SPRAY DEFLECTOR AND INSTALLED REPLACEMENTS. (M) 2 L 7 2 4F A6WE 1996042500654 19960425 00654 NE 1996 4 25 USAAD96034 2 19960331 A 7200 ENGINE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9A 52048 NE LEFT FAILED A USAA A E UNSCHED LANDING ENGINE SHUTDOWN Y ENGINE STOPPAGE CL CLIMB 1 EA 19 936VJ 48116 667182 BWI FL 349 - CLIMBING THROUGH 9000 FEET OUT OF BWI, LEFT ENGINE FAILED. CREW HEARD LOUD BANG (SIMILAR TO A COMPRESSOR) STALL AND ENGINE RPM BEGAN TO DECREASE. CREW SHUT DOWN ENGINE. FLIGHT RETURNED TO BWI AND LANDED WITH NO FURTHER INCID ENT. SET 8 MINUTES. MAINTENANCE REPLACED THE ENGINE. (M) 2 L 7 2 4F 4 F A6WE E2EA 1996042500655 19960425 00655 WP 1996 4 25 USAAD96035 1 19960331 A 2120 DUCT DOUG DC9 DC981 3022081 WP LEFT A/C PACK SEPARATED A USAA B G EMER. DESCENT O2 MASK DEPLOYED O OTHER CR CRUISE 1 EA 19 806US 48038 CAE - FL 256 - EN ROUTE SRQ-CLT, IN THE VICINITY OF CAE, CREW NOTED LOSS OF CABIN PRESSURIZATION. CREW PERFORMED AN EME RGENCY DESCENT TO 10,000 FEET. FLIGHT CONTINUED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND AND REPA IRED A SEPARATED DUCT ON THE FORWARD OUTLET ON THE LEFT AIR CONDITIONING PACK. (M) 2 L 7 2 4F A6WE 1996042500656 19960425 00656 NE 1996 4 25 USAAD96036 2 19960316 A 7200 ENGINE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9A 52048 NE LEFT BIRD STRIKE A USAA A UNSCHED LANDING C R F.O.D. PARTIAL RPM/PWR LOSS CL CLIMB 1 EA 19 976VJ 48147 667214 BIRD STRIKE ON TAKEOFF ROLL. DROP IN LEFT ENGINE EPR. PERFORMED ENGINE INSPECTION FOR BIRD STRIKE PER MM 72-00, PAGE 6 12. FOUND DAMAGE TO C1 BLADE. REMOVED AND REPLACED LEFT ENGINE IAW MM AND JOB CARD J971-00-01. (M) 2 L 7 2 4F 4 F A6WE E2EA 1996042500657 19960425 00657 NM 1996 4 25 USAASB96046 1 19960311 A 3350 XB864041 LIGHT BOEING 737 737201 1384454 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 233US 22273 FLT NR 492 - PHL - FOUND OVERWING EXIT LIGHT INOP AT LEFT AISLE SEAT EXIT. MAINTENANCE REPLACED LIGHT ASSEMBLY. (M) 2 L 7 2 4F A16WE 1996042500658 19960425 00658 NE 1996 4 25 USAASB96055 2 19960324 A 7200 ENGINE BOEING 737 7372B7 1384560 NM PWA JT8 JT8D15 52051 NE LEFT FAILED A USAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 EA 19 276AU 35915 22888 700178 FLT NR 571 - CLT - NR 1 ENGINE WAS SHUT DOWN IN FLIGHT. LOUD BANG WAS HEARD AND SHORTLY THERE AFTER THE ENGINE FAILED. NO FIRE WARNING OR OTHER INDICATIONS WERE NOTED. TOTAL SINGLE ENGINE TIME WAS APPROXIMATELY 30 MINUTES. MAINTENANCE R EPLACED NR 1 ENGINE ASSEMBLY PER JOB CARD. OPERATIONAL CHECK AND LEAK CHECK NORMAL. (M) 2 L 7 2 4F 4 F A16WE E2EA 1996042500659 19960425 00659 NE 1996 4 25 USAASB96056 2 19960327 A 7261 OIL SYSTEM BOEING 737 7372B7 1384560 NM PWA JT8 JT8D15A 52051 NE LT ENGINE OVER SERVICED A USAA A E UNSCHED LANDING ENGINE SHUTDOWN M W OVER TEMP INADEQUATE Q C CL CLIMB 1 EA 19 276AU 22888 709101 MIA FL - 652 - AFTER TAKEOFF, CREW NOTED OIL PRESSURE RISE ON LEFT ENGINE. CREW REDUCED POWER ON ENGINE AND NOTED OIL T EMPERATURE RISE. CREW SECURED THE LEFT ENGINE. FLIGHT RETURNED TO MIA AND LANDED WITH NO FURTHER INCIDENT. SET - 12 M INUTES. MAINTENANCE CLEANED AND SECURED THE CANNON PLUG ON THE NR 1 ENGINE OIL PRESSURE TRANSMITTER AND REPLACED THE OI L TEMPERATURE BULB. THE NEXT FLIGHT EXPERIENCED SIMILAR READINGS. MAINTENANCE FOUND THE OIL OVERSERVICED AND DRAINED T O THE PROPER LEVEL. (M) 2 L 7 2 4F 4 F A16WE E2EA 1996042500660 19960425 00660 NM 1996 4 25 USAASB96057 1 19960328 A 2751 2061141 FLAP INDICATOR BOEING 737 737201 1384454 NM COCKPIT FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 265AU 15911 22962 CLT - FLT 1632 - AFTER TAKEOFF, CREW RECEIVED FLAP ASYMMETRY LIGHT UPON RETRACTION OF FLAPS. NO UNCOMMANDED ROLL WAS EX PERIENCED. FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE FLAP INDICATOR. (M) 2 L 7 2 4F A16WE 1996042500661 19960425 00661 NM 1996 4 25 USAASB96058 1 19960328 A 2750 ATTACH PIN BOEING 737 7374B7 1384702 NM NR 7 TE FLAP DISENGAGED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 442US 24841 PIT - FL 975 - AFTER TAKEOFF, CREW COULD NOT GET THE FLAPS TO RETRACT. FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHE R INCIDENT. MAINTENANCE FOUND THE ATTACH PIN FOR THE NR 7 FLAP JACKSCREW BACKED OUT, JAMMING THE FLAP TRANSMISSION. TH E PIN WAS REINSTALLED AND SECURED. (M) 2 L 7 2 4F RT A16WE 1996042500662 19960425 00662 NM 1996 4 25 USAASB96059 1 19960330 A 5210 PAX DOOR BOEING 737 7374B7 1384702 NM CABIN LEAKING A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 433US 24555 FLT NR 830 - PHL - AIRCRAFT WOULD NOT PRESSURIZE DUE TO LARGE LEAK ON LEFT SIDE FORWARD ENTRY DOOR. MAINTENANCE COULD N OT DUPLICATE THE PROBLEM. FOUND THAT THE FORWARD ENTRY DOOR WARNING LIGHT AND DOOR OPERATED NORMAL. PRESSURE CHECK WAS GOOD. (M) 2 L 7 2 4F RT A16WE 1996042500663 19960425 00663 NM 1996 4 25 USAASB96060 1 19960401 A 5610 5893543109 WINDSHIELD BOEING 737 737301 1384611 NM LT COCKPIT CRACKED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 574US 16554 23739 FLT NR 0731 - PIT - WINDSHIELD CRACKED WHILE CLIMBING THROUGH FL 205. AIRCRAFT DIVERETED TO PIT. MAINTENANCE REPLACED CAPTAINS WINDSHIELD. (M) 2 L 7 2 4F RT A16WE 1996042500664 19960425 00664 1996 4 25 VTZA96138 4 19960329 A 3425 402053157 ADI BAG JETSTM JETSTM3201 1500217 EU LEFT FAILED A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 476UE 884 FLT NR 6281 - IAD-HPN - DURING CLIMB-OUT, RETURNED TO IAD DUE TO LEFT ADI IN LEVEL FLIGHT SHOWS 18 DEGREE PITCH UP AND 2 0 DEGREE LEFT TURN. AIRCRAFT LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED LEFT ADI. AIRCRAFT WAS RELEASED A ND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996042500665 19960425 00665 EU 1996 4 25 VTZA96139 1 19960329 A 2761 TY176301C SPOILER ACTUATOR JETAIR JETSTM JETSTM4101 1500501 EU RT FLAP FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 309UE 41022 FLT NR 6182 - TYS-IAD - ABORTED TAKEOFF AND LANDED AT TYS DUE TO CONFIGURATION WARNING AND SPOILER NO LOCKED LIGHT. AIR CRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI (52679) MEL 27-30 AT TYS. MAINTENANCE REMOVED AND REPLACED SPOILER ACTUATOR AT IAD CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996042500666 19960425 00666 EU 1996 4 25 VTZA96140 1 19960330 A 2435 23095002D STARTER GEN JETAIR JETSTM JETSTM4101 1500501 EU RT ENG FAILED A VTZA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 EA 27 313UE 41026 FLT NR 6191 - BOS-IAD - DURING CLIMB-OUT, RETURNED TO BOS, DUE TO RIGHT GENERATOR FAILURE. AIRCRAFT LANDED AT BOS WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED STARTER/GENERATOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE . (M) 2 L 7 2 4T RT A41NM 1996042500667 19960425 00667 1996 4 25 VTZA96141 4 19960330 A 3417 7000700966 AIR DATA COM JETAIR JETSTM JETSTM4101 1500501 EU NR 2 FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 312UE 41025 FLT NR 6150 - IAD-EWR - DURING TAKEOFF, BOTH TIMES RETURNED TO IAD DUE TO NR 2 ALTIMETER FLAGGED AND NR 2 EADI SHOWED FL AG. AIRCRAFT RETURNED TO GATE AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE RERACKED BOTH AHARS COMPUTERS AND REPLACED ADC. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996042500668 19960425 00668 EU 1996 4 25 VTZA96142 1 19960330 A 5270 SP4594 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGGAGE DOOR OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 303UE 41015 FLT NR 6356 - BOS-IAD - DURING TAXI, RETURNED TO GATE DUE TO MAIN BAGGAGE DOOR LIGHT CAME ON. MAINTENANCE DEFERRED PER MEL 52-30 (DMI 18523). AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. ON 3-30-96 MX CLOSED DMI 18523 BY ADJ USTING MAIN BAGGAGE DOOR MICROSWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996042500669 19960425 00669 EU 1996 4 25 WTAA960057 1 19960308 A 3260 9005EN38 SWITCH BAG JETSTM JETSTM3101 1500215 EU LT MLG BROKEN WIRE A WTAA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 17 402UE 734 FAT - LEFT MAIN LANDING GEAR INTRANSIT LIGHT REPORTED INOPERATIVE. MAINTENANCE REPAIRED DAMAGED WIRE AT LEFT MAIN LANDI NG GEAR UPLOCK MICROSWITCH. GEAR INDICATION NORMAL DURING GROUND CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996042500670 19960425 00670 EU 1996 4 25 WTAA960058 1 19960311 A 3230 AIR873601 GEAR SELECTOR BAG JETSTM JETSTM3101 1500215 EU LANDING GEAR MALFUNCTIONED A WTAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 17 403UE 743 MOD - LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. AIRCRAFT FERRIED TO FAT FOR REPAIRS. MAINTENANCE RESET EMERGENCY GEAR SELECTOR POP OUT PIN. GEAR RETRACTION NORMAL DURING GROUND CHECK. A IRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996042500671 19960425 00671 SO 1996 4 25 WTAA960059 1 19960312 A 3020 3D237606 EJECTOR VALVE EMB 120 EMB120RT SO LT ENGINE DIRTY A WTAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 17 122AM 120013 SFO - LEFT ENGINE INLET DE-ICE BOOTS FAILED TO OPERATE AFTER 5 SECONDS OF OPERATION. AIRCRAFT RETURNED TO STATION DUE T O EXISTING EN ROUTE WEATHER CONDITIONS. MAINTENANCE CLEANED AND LUBED EJECTOR VALVE. INLET BOOT OPERATIONAL CHECK NORM AL ON GROUND. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996042500672 19960425 00672 SO 1996 4 25 WTAA960060 1 19960315 A 5246 12016900010 FUEL DOOR EMB 120 EMB120RT SO RT WING LOOSE A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 17 285UE 120153 LAX - SERVICE DOOR WARNING LIGHT ILLUMINATED DURING TAKEOFF ROLL. MAINTENANCE INSPECTED SERVICE DOOR, FOUND FUEL SINGLE POINT REFUELING DOOR TO HAVE UNSECURED FASTENERS. SECURED FASTENERS AND CAPTION EXTINGUISHED. AIRCRAFT RETURNED TO SE RVICE. (M) 2 L 7 2 4T RT A31SO 1996042500673 19960425 00673 SO 1996 4 25 WTAA960061 1 19960317 A 5246 12016900010 FUEL DOOR EMB 120 EMB120RT SO RT WING LOOSE A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 17 285UE 120153 LAX - SERVICE DOOR WARNING LIGHT ILLUMINATED DURING TAKEOFF ROLL. MAINTENANCE INSPECTED SERVICE DOORS, FOUND FUEL SINGL E POINT REFUELING DOOR TO HAVE ONE UNSECURED FASTENER. RESECURED DOOR. DOOR WARNING SYSTEM OPERATIONAL CHECK NORMAL. A IRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996042500674 19960425 00674 SO 1996 4 25 WTAA960062 1 19960318 A 5246 12016900010 FUEL DOOR EMB 120 EMB120RT SO RT WING LOOSE A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 17 284UE 120145 SBP - SERVICE DOOR WARNING ILLUMINATED DURING TAKEOFF ROLL. FOUND FORWARD FASTENER OF INBOARD FUELING DOOR UNLATCHED. R ESECURED DOOR. SUBSEQUENT TAKEOFF NORMAL. (M) 2 L 7 2 4T RT A31SO 1996042500675 19960425 00675 SO 1996 4 25 WTAA960063 1 19960318 A 3234 12025226501 SELECTOR EMB 120 EMB120RT SO COCKPIT MALFUNCTIONED A WTAA O OTHER N FALSE WARNING CL CLIMB 1 WP 17 251YV 120251 SFO - RED 'B' SYSTEM INTRANSIT LIGHT REMAINS ILLUMINATED AFTER GEAR RETRACTION. MAINTENANCE DEFERRED SYSTEM 'B' GEAR PO SITION INDICATIONS PER MEL 32-60-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFFERAL WITH THE R EPLACEMENT OF THE LANDING GEAR SELECTOR. LANDING GEAR 'B' SYSTEM POSITION INDICATION OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4T RT A31SO 1996042500676 19960425 00676 EU 1996 4 25 WTAA960064 1 19960322 A 7712 310703411 TORQUE RING BAG JETSTM JETSTM3101 1500215 EU LT ENGINE MALFUNCTIONED A WTAA C E D ABORTED TAKEOFF ENGINE SHUTDOWN RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 17 431UE 813 FAT - LEFT ENGINE TORQUE FLUCTUATION BETWEEN 100 PERCENT AND 80 PERCENT DURING TAKEOFF ROLL REPORTED. TAKEOFF ABORTED W ITHOUT INCIDENT. CREW ACCOMPLISHED ENGINE GROUND RUN CHECK AT 104.5 PERCENT WITH NO DISCREPANCIES NOTED. PROBLEM REOCC URED ON SECOND ABORTED TAKEOFF ATTEMPT. MAINTENANCE DEFERRED LEFT ENGINE ON SECOND ABORTED TAKEOFF ATTEMPT. MAINTENANC E DEFERRED LEFT ENGINE SRL AND TTL SYSTEM PER MEL'S 76-1 AND 76-2. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUEN TLY CLEARED DEFERRED SRL AND TTL SYSTEM BY SWAPPING FROM BRIDGE ONE TO BRIDGE TWO OF THE LEFT ENGINE TORQUE RING. NO TO RQUE FLUCTATION REPORTED DURING ENGINE GROUND RUN. (M) 2 L 7 2 4T RT A21EU 1996042500677 19960425 00677 EU 1996 4 25 WTAA960065 1 19960324 A 3260 9005EN38 SWITCH BAG JETSTM JETSTM3101 1500215 EU LT MLG BROKEN WIRE A WTAA O OTHER N FALSE WARNING TO TAKEOFF 1 WP 17 420UE 788 FAT - LEFT MAIN LANDING GEAR INTRASIT LIGHT REPORTED INOPERATIVE. MAINTENANCE REPAIRED DAMAGED WIRE AT LEFT MAIN LANDIN G GEAR UPLOCK MICROSWITCH. GEAR INDICATIONS NORMAL DURING GROUND CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996042500678 19960425 00678 EU 1996 4 25 WTAA960066 1 19960329 A 3260 9005EN38 SWITCH BAG JETSTM JETSTM3101 1500215 EU RT MLG DIRTY A WTAA O OTHER N FALSE WARNING AP APPROACH 1 WP 17 431UE 813 SMF - RT MAIN LANDING GEAR INTRANSIT LIGHT AND GEAR WARNING HORN ACTIVATION REPORTED WITH GEAR EXTENDED AND FLAPS SET TO 20 PERCENT. MAINTENANCE INSPECTED WIRING AT RIGHT MAIN LANDING GEAR UPLOCK MICROSWITCH. DISCOVERED LOOSE AND DIRTY TE RMINAL CAUSING FAULT. CLEANED TERMINAL AND RESECURED CONNECTION. GEAR INDICATIONS NORMAL DURING GROUND CHECK. AIRCRAF T RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996042500679 19960425 00679 1996 4 25 Y2PA96013 4 19960327 A 3414 B020081104 AIRSPEED IND DOUG DC9 DC915F 3022037 WP RT COCKPIT INOPERATIVE A Y2PA K NONE O OTHER IN INSP/MAINT 1 GL 23 194US 930 47016 YIP - NR 1 FIRST OFFICERS AIRSPEED INDICATOR INOP. DUPLICATED MALFUNCTION, REMOVED AND REPLACED FIRST OFFICERS AIRSPEED INDICATOR. SYSTEM OPERATIONAL CHECKS GOOD IAW DC9 MM CHAPTER 34-10-01. (M) 2 L 7 2 4F A6WE 1996042500680 19960425 00680 EU 1996 4 25 YIEA96012 1 19960325 A 3260 MY20718378202 LEVER ARM AMD FALC20 FALCOND 2720304 EU LANDING GEAR FAILED A YIEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 815AA 205 YIP - AFTER TAKEOFF, IN RETRACTING LANDING GEAR WARNING HORN WOULD NOT SILENCE AND THE 3 RED GEAR LIGHTS REMAINED ON. L ANDING GEAR WAS EXTENDED NORMALLY AND AIRCRAFT RETURNED TO YIP WITHOUT INCIDENT. FOUND BROKEN 24G SWITCH LEVER ARM WHIC H WAS CAUSED BY A BROKEN LEVER ARM SUPPORT BRACKET. REPLACED BROKEN LEVER ARM AND LEVER ARM SUPPORT BRACKET. OPERATION ALLY CHECKED LANDING GEAR SYSTEM IAW FALCON MM 32-60-4. NO DEFECTS WERE NOTED. (M) 2 L 7 2 4F A7EU 1996042500686 19960425 00686 CE 1996 4 25 96ZZZX2034 1 19960401 A 3240 30100 BRAKE VALVE PARKERHANFIN CESSNA 402 402C 207590R CE LT MLG LOOSE A OEZA O OTHER K FLUID LOSS NR NOT REPORTED 1 WP 19 3283M 402C0303 LEFT BRAKE LOST FLUID WHEN BRAKE APPLIED. FOUND BLEEDER VALVE HAD COME LOOSE AND WAS CAUSING THE LEAK. TIGHTENED BLEED ER AND SERVICED BRAKE. 1 L 7 2 3O A7CE 1996050200002 19960502 00002 WP 1996 5 2 9609129150 1 19960328 A 5713 LONGERON DOUG DC9 DC914 3022034 WP WS 65-109 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8908E 45749 DURING SPECIAL MTC VISIT, FOUND CORROSION ON SEVERAL LOWER WING STRINGERS; 11L FROM XRS 78 - 88 AND ON 14R, 15R, 17R AND 18R FROM APPROXIMATELY XRS 65 - 109. REPAIRED PER EA 91-100821. 2 L 7 2 4F A6WE 1996050200003 19960502 00003 WP 1996 5 2 9609139763 1 19960416 A 5230 FITTING DOUG DC9 DC941 302207N WP CARGO DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 763NW 47396 DURING "H" CHECK, FOUND A CRACK IN THE AFT CARGO DOOR NR 1 BEAM FORWARD END FITTING. REPLACED FITTING PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996050200004 19960502 00004 WP 1996 5 2 9609149906 1 19960420 A 5311 FRAME DOUG DC9 DC931 3022065 WP FS 169 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 956N 47252 DURING "M" CHECK, FOUND CORROSION ON THE FS 169 FRAME AT THE RIGHT CUSP. REPLACED FITTING PER SRM 51-30-5 AND 51-30-1. 2 L 7 2 4F A6WE 1996050200005 19960502 00005 WP 1996 5 2 9609179956 1 19960424 A 3231 LATCH MECH DOUG DC9 DC931 3022065 WP LT NLG DOOR MALFUNCTIONED A NWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 01 923RW 47183 A LOUD VIBRATION WAS COMING FROM NOSE GEAR AREA AFTER TAKEOFF. FLIGHT RETURNED TO DAY AND LANDED WITHOUT INCIDENT. MAI NTENANCE FOUND THE LEFT NOSE GEAR DOOR OPEN. LATCHED NOSE GEAR DOOR TO SECURED POSITION. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996050200006 19960502 00006 WP 1996 5 2 9609189947 1 19960424 A 3260 UNSAFE LIGHT DOUG DC9 DC931 3022065 WP RT MLG ILLUMINATED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 8938E 47161 RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. RECYCLED GEAR WITH SAME RESULTS. FLIGHT RET URNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE CHECKED CONTINUITY OF UPLOCK AND DOWNLOCK SWITCHES. SWITCHES WER E REINSTALLED AND GEAR SWING WAS PERFORMED. OPERATIONAL CHECK WAS NORMAL. DISCREPANCY COULD NOT BE DUPLICATED. REPLAC ED UPLOCK AND DOWNLOCK SWITCHES AS A PRECAUTION. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996050200007 19960502 00007 NM 1996 5 2 9609192203 1 19960424 A 2130 39854021 SHUTOFF VALVE BOEING 727 727251 138408H NM RT PACK MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 203US 8939 4139 22543 DURING CLIMB, UNABLE TO CONTROL CABIN PRESSURIZATION IN AUTO OR MANUAL MODE. AIRCRAFT RETURNED TO TPA AND LANDED WITHOU T INCIDENT. REPLACED RIGHT PACK AIR SHUTOFF VALVE. PERFORMED PRESSURIZATION CHECK. CHECKED OK. 2 L 7 3 4F A3WE 1996050200008 19960502 00008 NM 1996 5 2 9609206632 1 19960424 A 7711 CONNECTOR BOEING 747 747251B 1384892 NM PWA JT9 JT9D7R4G2 52054 NE NR 1 EPR DIRTY A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 632US 23112 25320 DURING TAKEOFF ROLLOUT, THE NR 1 EPR AND N1 FAILED TO INCREASE. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO GATE. MAI NTENANCE CLEANED CANNON PLUG D15J AND PERFORMED RUN-UP CHECK. CHECK WAS NORMAL AND AIRCRAFT WAS APPROVED FOR SERVICE. 2 L 7 4 4F 4 F A20WE E3NE 1996050200009 19960502 00009 NM 1996 5 2 96UAL900150 1 19960227 A 2120 AIR DISTR BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE COCKPIT ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 9030U 19068 ELECTRIC SMOKE SMELL IN COCKPIT AND CABIN SWITCHING BLEEDS. CEILING IN FORWARD GALLEY HOT TO TOUCH. EMERGENCY EQUIPMEN T REQUESTED. SUPPLEMENTAL DATA UPDATE: ACCOMPLISHED POWER RUN, CHECKED ALL SYSTEMS, COULD NOT DUPLICATE. REMOVED CEIL ING PANELS AND CHECKED FOR CHAFED WIRES AND BURNED OR DAMAGED COMPONENTS. SYSTEMS ALL CHECKED NORMAL. 2 L 7 2 4F 4 F A16WE E2EA 1996050200010 19960502 00010 NM 1996 5 2 96UAL900271 1 19960422 A 5522 65727841 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LT ELEVATOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7464U 21918 LEFT ELEVATOR HAS PREVIOUS REPAIR DOUBLER THAT HAS LOOSENED AND SEVERAL CRACKS IN LOWER SKIN AFT OF DOUBLER. SUPPLEMENTA L DATA UPDATE: REPLACED THE LEFT ELEVATOR WITH A SERVICEABLE UNIT AND SENT THE REMOVED UNIT TO THE SHOP FOR REPAIR. 2 L 7 3 4F 4 F A3WE E2EA 1996050200011 19960502 00011 NM 1996 5 2 96UAL900272 1 19960422 A 5330 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE BS 1020 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7297U 21892 A 4 INCH CRACK IN LOWER BELLY, ONE FOOT OUTBOARD LEFT OF LOWER AFT VHF ANTENNA. EVIDENCE OF CORROSION. *S/D* ACTUALLY THE CRACK WAS 2.5 INCHES. REPAIRED PER SRM 53-30-3. 2 L 7 3 4F 4 F A3WE E2EA 1996050200012 19960502 00012 NM 1996 5 2 96UAL900273 1 19960422 A 2810 FUEL STORAGE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT AFT SPAR LEAKING A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 560UA 26660 EVIDENCE OF FUEL LEAKING FROM REAR SPAR INBOARD OF NR 2 ENGINE PYLON. AIRCRAFT INSPECTED AND DETERMINED SAFE TO FERRY T O SFO FOR REPAIR. *S/D* SEALED LEAK AT WB 16 RIGHT AFT SPAR, OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996050200013 19960502 00013 NE 1996 5 2 96UAL900274 2 19960422 A 7230 COMPRESSOR BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LT ENGINE WORN A UALA E ENGINE SHUTDOWN M OVER TEMP CR CRUISE 1 WP 29 611UA 21872 709608 AT FLIGHT LEVEL 390, THE LEFT ENGINE INDICATED 742 DEGREES AND A PILOT-ELECTED IN FLIGHT SHUTDOWN OCCURRED. THE ENGINE EXPERIENCED SEVERAL COMPRESSOR STALLS WHILE FLYING THROUGH TURBULENCE CAUSED BY THUNDERSTORMS. *S/D* A BORESCOPE INSPE CTION RESULTED IN NO FINDINGS. THE ENGINE WAS REMOVED, IT WAS THEN RUN IN THE ENGINE TEST CELL AND NOTHING WAS FOUND DU RING THE PERFORMANCE RUN. THE ENGINE'S COMPRESSOR WAS DETERIORATED BEYOND THE ANTICIPATED LEVEL, BUT NOT BEYOND ACCEPTA BLE LIMITS. THE ENGINE WILL BE REFURBISHED DUE TO THE INABILITY TO ISOLATE A SPECIFIC MALFUNCTION. 2 L 7 2 4F 4 F RT A1NM E3NE 1996050200014 19960502 00014 NM 1996 5 2 96UAL900275 1 19960422 A 3350 BATTERY PACK BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 617UA 21877 MID-RIGHT AISLE OVERHEAD EMERGENCY LIGHT INOPERABLE. REPLACED BATTERY PACK, OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 1996050200015 19960502 00015 EU 1996 5 2 96UAL900276 1 19960423 A 2133 OUTFLOW VALVE NORD MICRO 6331166394 AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN MALFUNCTIONED A UALA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 WP 29 422UA 503 LOST CABIN PRESSURE AT FL350. EXECUTED EMERGENCY DESCENT AND REGAINED CONTROL OF CABIN IN MANUAL MODE. *S/D* ELECTRON IC BOX NR 1 FAILED ON OUTFLOW VALVE DRIVING THE VALVE OPEN. REPLACED OUTFLOW VALVE AND OPERATIONALLY CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 1996050200016 19960502 00016 1996 5 2 96UAL900277 4 19960424 A 2565 7A1338104 SLIDE PACKBOARD BF GOODRICH 7A1323107 BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE UPPER DDECK DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 173UA GS945 24380 STRETCHED UPPER DECK EVACUATION SLIDE INADVERTANTLY DEPLOYED. DURING DEPLOYMENT, SLIDE PACKBOARD WAS DAMAGED. PACKBOAR D DAMAGE. SLIDE REPLACED, AND REMOVED SLIDE WAS REPAIRED AND MODIFIED PER BFG S/B 25-266. 2 L 7 4 4F 4 F RT A20WE E24NE 1996050200017 19960502 00017 1996 5 2 96UAL900278 4 19960424 A 2565 7A1338104 SLIDE PACKBOARD BF GOODRICH 7A1323107 BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE UPPER DECK DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 187UA G683 26876 STRECTHED UPPER DECK EVACUATION SLIDE INADVERTANTLY DEPLOYED. DURING DEPLOYMENT, SLIDE PACKBOARD WAS DAMAGED. PACKBOA RD DAMAGE. SLIDE REPLACED, AND REMOVED SLIDE WAS REPAIRED AND MODIFIED PER BFG S/B 25-266. 2 L 7 4 4F 4 F RT A20WE E24NE 1996050200019 19960502 00019 NM 1996 5 2 96UAL900280 1 19960424 A 5610 WINDOW SEAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT LOOSE A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 574UA 26686 VERY LOUD SQUEAL FROM FLIGHT OFFICER'S WINDOW. FLIGHT DIVERTED TO ORD. SECURED FLIGHT OFFICER'S WINDOW SEAL IN THE FRA ME. PRESSURE CHECKS OK. FLIGHT CONTINUED TO SEA, OPERATION NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996050200020 19960502 00020 NM 1996 5 2 96UAL900281 1 19960424 A 3350 LIGHT SOCKET BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE L2 DOOR INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 378UA 24653 EMERGENCY LIGHT ON THE OUTSIDE OF DOOR TWO LEFT INOPERABLE. REPLACED SOCKET ASSEMBLY. CHECKS O.K. 2 L 7 2 4F 4 F RT A16WE E2GL 1996050200021 19960502 00021 NM 1996 5 2 96UAL900282 1 19960424 A 3350 BULB BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE COCKPIT FAILED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 956UA 26704 COCKPIT EMERGENCY LIGHT INOPERABLE. RELAMPED. CHECKS O.K. 2 L 7 2 4F 4 F RT A16WE E2GL 1996050200022 19960502 00022 EU 1996 5 2 COMA9630104 1 19960423 A 2613 HOT WARNING SAAB SF340 SF340A 7850100 EU RT TAIL PIPE ACTIVATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 146CA 340A146 RIGHT TAILPIPE HOT WARNING CAME ON DURING CLIMB. RETURNED POWER LEVER AND WARNING EXTINGUISHED. AIRCRAFT RETURNED TO C VG. COULD NOT DUPLICATE DISCREPANCY. FALSE WARNING CAUSED BY RAIN. 2 L 7 2 4T RT A52EU 1996050200023 19960502 00023 EA 1996 5 2 COMA9660074 1 19960423 A 2760 FE210302 CAM SWITCH CNDAIR CL600 CL6002B19 EA THROTTLE QUAD DEFECTIVE A COMA K NONE O OTHER LD LANDING 1 SO 01 936CA 4582 7043 AFTER LANDING, GROUND SPOILERS RETRACTED AND THEN REDEPLOYED UNCOMMANDED. REPLACED THE THROTTLE ADJUSTABLE CAM SWITCH U NIT. PART TOTAL CYCLES, 2 L 7 2 4F RT A21EA 1996050200024 19960502 00024 EA 1996 5 2 COMA9660075 1 19960423 A 3010 14463102 ANTI ICE DUCT CNDAIR CL600 CL6002B19 EA RT WING CRACKED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 932CA 7038 RIGHT WING ANTI-ICE DUCT WARNING CAME ON AFTER TAKEOFF. AIRCRAFT RETURNED TO CVG. REPLACED CRACKED DUCT ASSY, RIGHT WI NG. 2 L 7 2 4F RT A21EA 1996050200025 19960502 00025 NM 1996 5 2 DL72K960942 1 19960419 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 1 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 479DA 20756 FOUND ON A2 LTR CK - COVE SKIN ATTACH ANGLE CRACKED NR 1 SLAT AT INBOARD UPSTOP PAD. REPAIR - REPAIRED PER M/M 57-54-0. 2 L 7 3 4F A3WE 1996050200026 19960502 00026 NM 1996 5 2 DL72K960943 1 19960419 A 5320 WEB BOEING 727 727232 1384082 NM BS 1270/1280 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 479DA 20756 FOUND ON A2 LTR CK - RT VERTICAL TORQUE BOX WEB CRACKED AT UPPER LIGHTNING HOLE STA 1270. RT VERTICAL TORQUE BOX WEB CR ACKED AT LOWER LIGHTNING HOLE, STA 1280. REPAIRED PER M/M 53-11-0 PG 828. 2 L 7 3 4F A3WE 1996050200027 19960502 00027 NM 1996 5 2 DL72K960944 1 19960419 A 5320 WEB BOEING 727 727232 1384082 NM BS 1240/1248 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 479DA 20756 FOUND ON A2 LTR CK - RT VERTICAL TORQUE BOX WEB CRACKED AT UPPER LIGHTNING HOLE, STA 1240. RT TORQUE BOX WEB CRACKED AT LOWER LIGHTNING HOLE STA 1248. REPAIRED PER M/M 53-11-0. 2 L 7 3 4F A3WE 1996050200028 19960502 00028 NM 1996 5 2 DL72K960945 1 19960419 A 5320 WEB BOEING 727 727232 1384082 NM LT TQ BOX CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 479DA 20756 FOUND ON A2 LTR CK. LT TORQUE BOX VERTICAL WEB 2 EACH CRACKS AT FORWARD UPPER LIGHTNING HOLE. LT TORQUE BOX VERTICAL W EB CRACKED AT 2ND FROM FORWARD UPPER LIGHTNING HOLE. REPAIRED PER M/M 53-11-0 PG 828. 2 L 7 3 4F A3WE 1996050200029 19960502 00029 NM 1996 5 2 DL72K960946 1 19960419 A 5320 WEB BOEING 727 727232 1384082 NM BS 1235 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 479DA 20756 FOUND ON A2 LTR CK. RT VERTICAL TORQUE BOX WEB CRACKED AT UPPER END STA 1235. REPAIRED PER M/M 53-11-0 NR 19. 2 L 7 3 4F A3WE 1996050200030 19960502 00030 NM 1996 5 2 DL72K960948 1 19960419 A 5414 PANEL BOEING 727 727232 1384082 NM NR 9524 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 479DA 20756 FOUND ON A2 LTR CK. ONE INCH CRACK AT PANEL 9524. REPAIRED PER M/M 54-30-0 PG 803/804. 2 L 7 3 4F A3WE 1996050200031 19960502 00031 NM 1996 5 2 DL72K960949 1 19960419 A 5320 WEB BOEING 727 727232 1384082 NM BS 1263/1310 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 479DA 20756 FOUND ON A2 LTR CK. LT VERTICAL TORQUE BOX WEB CRACKED AT LOWER LIGHTNING HOLE STA 1263. LT VERTICAL TORQUE BOX WEB C RACKED AT UPPER LIGHTNING HOLE STA 1310. REPAIRED PER M/M 53-11-0, PG 828. 2 L 7 3 4F A3WE 1996050200032 19960502 00032 NM 1996 5 2 DL72K960962 1 19960422 A 3350 1102833 LIGHT BOEING 727 727232 1384082 NM AFT AIRSTAIRS DEFECTIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 474DA 11988 20751 AFT 3 SECTIONS OF EMERGENCY PATH LIGHTS REMAIN ON WITH SWITCH IN OFF POSITION. FOUND EMERGENCY LIGHT ASSY L622 OVER AFT STAIRS DEFECTIVE. REPLACED-OPS NML. 2 L 7 3 4F A3WE 1996050200033 19960502 00033 NM 1996 5 2 DL72P960963 1 19960422 A 5320 WEB BOEING 727 727225 1384077 NM BS 1243 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8890Z 21859 FOUND DURING C-CHECK, .6250 INCH CRACK AT TORQUE BOX WEB LIGHTNING HOLE STA 1243R. REPAIRED PER M/M 53-11-0. 2 L 7 3 4F A3WE 1996050200034 19960502 00034 NM 1996 5 2 DL72P960964 1 19960422 A 5320 WEB BOEING 727 727225 1384077 NM BS 1213 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8890Z 21859 FOUND DURING C CHECK - .1250 INCH CRACK TORQUE BOX WEB ABOVE STAIRWAY CLOSEOUT PANEL, STA 1213. REPAIRED PER M/M 53-11- 0. 2 L 7 3 4F A3WE 1996050200035 19960502 00035 NM 1996 5 2 DL72P960965 1 19960422 A 2782 ACT MOUNT BRKT BOEING 727 727225 1384077 NM RT LE FLAPS CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8890Z 21859 FOUND DURING C-CHECK - CRACK NR 8 SLAT ACTUATOR MOUNT BRACKETS, INBOARD AND OUTBOARD SIDES. REPAIRED PER M/M 57-20-21. 2 L 7 3 4F A3WE 1996050200036 19960502 00036 NM 1996 5 2 DL72P960966 1 19960422 A 5754 ANGLE BOEING 727 727225 1384077 NM NR 6 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8890Z 21859 FOUND DURING C-CHECK - FOUND NR 7 SLAT ANGLE CRACKED AT ANTI-ICE DUCT CUTOUT. REPAIRED PER M/M 57-54-0. NR 6 SLAT OUTB OARD TRACK WING CUTOUT CRACKED .25 INCH. REPAIRED PER M/M 57-20-21. 2 L 7 3 4F A3WE 1996050200037 19960502 00037 NM 1996 5 2 DL72P960967 1 19960422 A 5754 RIB BOEING 727 727225 1384077 NM NR 6 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8890Z 21859 FOUND DURING C-CHECK - NR 6 SLAT ACTUATOR ROD END ATTACH RIB CRACKED PAST PREVIOUS STOP DRILL INBOARD SIDE AND CRACKED . 3750 INCH ON OUTBOARD SIDE. REPAIRED INBOARD RIB PER M/M 57-54-0, FIG 804 AND REPAIRED OUTBOARD RIB PER M/M 57-54-0, PG 803. 2 L 7 3 4F A3WE 1996050200038 19960502 00038 NM 1996 5 2 DL72S960925 1 19960418 A 5330 SKIN BOEING 727 727232 1384082 NM BS 380-400 PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 542DA 22391 PUNCTURE IN FUSELAGE - STA 380-400 BETWEEN S-19L AND 20L, 2 INCH TEAR IN FUSE (GROUND DAMAGE). CUT OUT DAMAGE AREA AND INSTALL DOUBLER PER SRM 53-30-3, PAGES 5 THRU 8. 2 L 7 3 4F A3WE 1996050200039 19960502 00039 NM 1996 5 2 DL72S960952 1 19960421 A 3231 ROD ASSY 652676134 BOEING 727 727232 1384082 NM RT MLG DOOR BROKEN A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 542DA 22391 RT MLG FLYING GEAR DOOR ROD ASSY DMN NR 65-26761-34 BROKEN CAUSING DOOR INDICATION PROBLEM AND AIRCRAFT VIBRATION. RETU RNED TO ATL. REPLACED GEAR DOOR. 2 L 7 3 4F A3WE 1996050200040 19960502 00040 NM 1996 5 2 DL72S960960 1 19960421 A 5320 651751736 BEAM ANGLE BOEING 727 727232 1384082 NM AFT STAIR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 497DA 21077 TORQUE BOX BEAM ANGLE CRACKED BELOW FORWARD ACTUATOR ATTACH FITTING. REPLACE CRACKED ANGLE. REF: E.O. 4-061071-12. 2 L 7 3 4F A3WE 1996050200041 19960502 00041 NM 1996 5 2 DL72W960926 1 19960418 A 5320 WEB BOEING 727 727247 138408F NM BS 1263 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2819W 21057 .3750 INCH CRACK IN LIGHTNING HOLE OF LT LOWER TORQUE BOX WEB, STA 1263, TOP HOLE. REPAIR PER M/M 53-11-0. 2 L 7 3 4F A3WE 1996050200042 19960502 00042 NM 1996 5 2 DL72W960927 1 19960418 A 5743 SWIVEL FITTING BOEING 727 727247 138408F NM MLG DOOR OUT OF ADJUST A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2819W 21057 MLG SPAR BEING CHAFED BY STRUT DOOR SIDE BRACE SWIVEL FITTING. REWORK PER M/M 57-43-0. 2 L 7 3 4F A3WE 1996050200043 19960502 00043 NM 1996 5 2 DL72W960929 1 19960418 A 2782 ACT SUPPORT BOEING 727 727247 138408F NM NR 8 SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2819W 21057 FOUND TWO-INCH CRACK IN NR 8 SLAT OUTBOARD ACTUATOR SUPPORT WHILE SHOWING MAINTENANCE LOCATION OF CRACK AT INBOARD SUPPO RT. REPAIR PER M/M 57-20-21. 2 L 7 3 4F A3WE 1996050200044 19960502 00044 NM 1996 5 2 DL72W960930 1 19960418 A 2782 ACT ANGLE BOEING 727 727247 138408F NM NR 8 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2819W 21057 NR 8 SLAT ACTUATOR INBOARD ATTACH ANGLE CRACKED. REPAIR PER M/M 57-20-21. 2 L 7 3 4F A3WE 1996050200045 19960502 00045 NM 1996 5 2 DL72W960938 1 19960412 A 5315 FLOOR BEAM BOEING 727 727247 138408F NM BS 1050 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2811W 20649 FOUND ON MV1 CHECK - CORROSION ON FLOOR BEAM TOP SURFACE STA 1050 FROM RBL 10 TO 14. REPAIR - REPAIRED PER M/M 53-20-11 . 2 L 7 3 4F A3WE 1996050200046 19960502 00046 NM 1996 5 2 DL72W960978 1 19960405 A 5330 65545661 SKIN BOEING 727 727247 138408F NM BS 480 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2810W 20648 FUSELAGE SKIN WAS FOUND CORRODED JUST AFT OF THE BUTT SPLICE AT STA 480 FROM STRINGER 28R-28L. CORROSION WAS ALSO FOUND ON THE SPLICE STRAP AT ONE FASTENER LOCATION BETWEEN BL ZERO AND 28L. THE SKIN DAMAGE RESULTED IN CUTOUT THAT EXTENDS AFT APPROX. 1.75 INCHES AND ACROSS THE BUTT SPLICE FROM OUTBD STR 28L TO OUTBD OF STR 28R. ADDITIONAL CORROSION WAS DIS COVERED, RESULTING IN CUTOUT OF 1 INCH BY 2 INCHES. ACCOMPLISHED REPAIR IAW DL ER/A 3033801-14 REV B. 2 L 7 3 4F A3WE 1996050200047 19960502 00047 NM 1996 5 2 DL73S960928 1 19960418 A 3350 20131A BATTERY PACK BOEING 737 737232 1384475 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 315DL 23087 R1 OVRHD AND L1 SLIDE EMERGENGY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. CKS GOOD. 2 L 7 2 4F RT A16WE 1996050200048 19960502 00048 NM 1996 5 2 DL73S960959 1 19960422 A 3350 LIGHTS 20131A BOEING 737 737232 1384475 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 334DL 23105 LAST 5 EMERGENCY ESCAPE PATH LIGHTS ARE INOPERATIVE. C.A. DOWN-POWERED POWER SUPPLY AND RECONNECTED POWER AND LIGHTS CK GOOD. AS PRECAUTION, REPLACED BATTERY PACK M1197. 2 L 7 2 4F RT A16WE 1996050200049 19960502 00049 NM 1996 5 2 DL757960931 1 19960418 A 3350 LIGHTS 767 BOEING 757 757232 1384965 NM EXTERIOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 670DN 25331 FOUND THREE EMERGENCY EXITS LIGHTS OUT DURING S/C--NR'S L560, L561, AND L569. RELAMPED LIGHTS, CKS GOOD. 2 L 7 2 4F RT A2NM 1996050200050 19960502 00050 NM 1996 5 2 DL757960958 1 19960422 A 3320 S283N7021 BALLAST BOEING 757 757232 1384965 NM CABIN FAILED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 629DL 22919 PASSENGER REPORTED SMOKE AND FUMES AT SEAT 21F ON PUSHBACK FROM SLC. REPLACED BALLAST FOR SIDE WALL LIGHTS AT 21F. 2 L 7 2 4F RT A2NM 1996050200051 19960502 00051 NM 1996 5 2 DL76L960956 1 19960321 A 5400 311T311024 UPPER SPAR BOEING 767 767332 1382001 NM NR 1 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 175DN 24803 TWO CRACKS WERE FOUND IN THE NR 1 ENGINE PYLON UPPER SPAR WEB AT THE OUTBOARD DRAIN HOLE AT NAC STA 156 AND WL 149.21. T HE CRACKS WERE STOP DRILLED AND REINFORCED WITH A FILLER AND DOUBLER PER DL ERA 273499-14, REV A. 2 L 7 2 4F RT A1NM 1996050200052 19960502 00052 NM 1996 5 2 DL76L960990 1 19960423 A 2560 SLIDE SENSOR BOEING 767 767332 1382001 NM LEFT WING OUT OF ADJUST A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 184DN 27111 AT 270 KNOTS, LEFT WING SLIDE EICAS MESSAGE ILLUMINATED. FOUND PROXIMITY SENSOR 218 OUT OF ADJUSTMENT. ADJUSTED SAME. OPS CHECK NORMAL. 2 L 7 2 4F RT A1NM 1996050200053 19960502 00053 WP 1996 5 2 DLL10960969 1 19960415 A 3233 1523554 ACT ATTACH FTG LKHEED 1011 10113851 5265010 WP LT MLG CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 720DA 193C1136 THE LEFT MLG ATTACH RIB FITTING WAS CORRODED AT THE MLG RETRACT ACTUATOR ATTACH FITTING LOCATION. THE DAMAGE WAS CLEANE D UP AND INSPECTED PER DL ERA 273650-14. 2 L 7 3 4F A23WE 1996050200054 19960502 00054 WP 1996 5 2 DLL14960924 1 19960418 A 3350 BATTERY PACK 5165741 LKHEED 1011 1011385115 5265015 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 737D 65610 193C1228 EMERGENCY LIGHTS BATTERY PACK FOUND INOPERABLE ON L/O. REPLACED SAME, CKS OK. 2 L 7 3 4F A23WE 1996050200055 19960502 00055 WP 1996 5 2 DLL16960968 1 19960422 A 5551 1515255 FITTING LKHEED 1011 10113853 5265020 WP HORIZ STAB OUT OF POSITION A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 763DL 193Y1197 THE UPPER STABILIZER POWER SERVO FITTINGS ATTACHED TO THE 1860 BULKHEAD WERE ORIGINALLY MISPLACED. AFTER REALIGNMENT, T HE FITTINGS' INBOARD ATTACH FASTENERS DID NOT HAVE E.D. THIS ER/A AUTHORIZES PLUGGING THE DISCREPANT HOLES AND RELOCATI NG THEM PER DL ERA 273641-14. 2 L 7 3 4F A23WE 1996050200056 19960502 00056 WP 1996 5 2 DLL17960935 1 19960408 A 5711 1617204103 REAR SPAR LKHEED 1011 10113853 5265020 WP WS 320 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 767DA 193H1209 ON THE LT WING, CRACKS WERE FOUND EMANATING FROM FASTENER HOLES BETWEEN IWS 293.58 AND IWS 346.109. CRACKS WERE FOUND IN THE UPPER CAP, WEB AND UPPER WING SKIN. ACCOMPLISHED REPAIRS PER DL ERA 273597-14AD. 2 L 7 3 4F A23WE 1996050200057 19960502 00057 WP 1996 5 2 DLL17960936 1 19960408 A 5711 1605415102 REAR SPAR LKHEED 1011 10113853 5265020 WP WS 320 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 767DA 193H1209 ON THE RT WING, REAR SPAR, CRACKS WERE FOUND EMANATING FROM FASTENER HOLES BETWEEN IWS 293.58 AND IWS 346.109. CRACKS W ERE FOUND IN THE UPPER CAP, WEB, AND UPPER WING SKIN. ACCOMPLISHED REPAIRS PER DL ERA 273600-14AD. 2 L 7 3 4F A23WE 1996050200058 19960502 00058 WP 1996 5 2 DLL17960954 1 19960419 A 5320 1552177129 LOWER SILL LKHEED 1011 10113853 5265020 WP L2 PAX DOOR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 767DA 193H1209 THE L2 PASSENGER DOOR SURROUND LOWER SILL WAS CORRODED ON ITS INNER AND OUTER CAPS. ACCOMPLISHED REPAIRS PER DL ERA 273 538-14. 2 L 7 3 4F A23WE 1996050200059 19960502 00059 NM 1996 5 2 DLM11960937 1 19960419 A 3260 POSITION SENSOR 863701 DOUG MD11 MD11 3023602 NM LT MLG MALFUNCTIONED A DALA L ABORTED APPROACH N FALSE WARNING LD LANDING 1 SO 27 811DE 985 48566 ON APPROACH, LEFT GEAR POSITION INDICATOR RED ON SYNOPTIC PAGE, POSITION SHOWED GREEN ON MAIN PILOT PANEL. MANUAL POSIT ION INDICATOR SHOWED DOWN AND LOCKED. CREW WENT THROUGH ALTERNATE EXTENSION PROCEDURE. DECLARED EMERGENCY AND LANDING WAS NORMAL. GEAR WAS PINNED ON RUNWAY AND AIRCRAFT TOWED TO GATE. REPLACED SECONDARY SENSOR D1-82 ON LEFT MAIN GEAR. P ERFORMED NORMAL CHECK-OUT OF POSITION SYSTEM. ALL GEAR POSITION LIGHTS NOW NORMAL. RESET ALTERNATE GEAR EXTENSION SYST EM. 2 L 7 3 4F RT A22WE 1996050200060 19960502 00060 NM 1996 5 2 DLM88960919 1 19960418 A 3260 THROTTLE SWITCH SS092200010 DOUG MD88 MD88 3023688 NM CENTER PEDESTAL FAILED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 908DL 43539DL 49539 ON TAKEOFF, HAD LANDING GEAR WARNING WITH GEAR RAISED. REPLACED RIGHT THROTTLE SWITCH PACK DUE TO SWITCH 320 FAILED. S YSTEM CHECKS GOOD PER M/M. 2 L 7 2 4F RT A6WE 1996050200061 19960502 00061 NM 1996 5 2 DLM88960923 1 19960418 A 3320 D77311001 BALLAST DOUG MD88 MD88 3023688 NM CABIN OVERHEATING A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 996DL 53363 ELECTRICAL SMELL ABOVE ROW 17, FOUND BALLAST OVERHEATING AT 16 DEF. REPLACED BALLAST. 2 L 7 2 4F RT A6WE 1996050200062 19960502 00062 NM 1996 5 2 DLM88960932 1 19960418 A 7931 42D1091A OIL PRESS SW DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE STICKING A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 947DL 49878 718178 AT FL 180, THE LEFT OIL STRAINER CLOGGING MSG. ON THE O.A.P. ILLUMINATED THEN WENT OFF. THEN, 10 SECONDS LATER, THE LIG HT REILLUMINATED. PER P.O.M., ENGINE STRUT DOWN AND RETURNED TO ATL. CORRECTIVE: CHECKED CHIP DETECTOR. CHECKS GOOD. CHECKED MAIN OIL FILTER, CHECKS GOOD. REPLACED OIL FILTER, LEAK CHECKS GOOD. REPLACED OIL DIFFERENTAL PRESSURE SWIT CH PER M/M, CHECKS GOOD. RAN ENG PER P.F.H.B. CHECKS OKAY. NO MRR. REJECTED GT 595. 2 L 7 2 4F 4 F RT A6WE E9NE 1996050200063 19960502 00063 NM 1996 5 2 P5CA9600214 1 19960421 A 3010 5201200 SEAL BOEING 747 747122 1384872 NM LT WING LEAKING A P5CA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 851FT 19756 ****CORRECTION****RETURNED TO GATE DUE TO LEFT WING L/E OVERHEAT LIGHT CAME ON DURING PUSHBACK. REPLACED LEFT WING ANTI -ICE VALVE IAW MM 30-11-03. REPLACED D-D SEALS AT NR 4 LED UNIT AT 2 INCH DUCT ASSY AND TWO NEW CLAMPS INSTALLED AT THE MANIFOLD ELBOW AND LED UNIT IAW MM 27-81-03. PRESSURE CHECK NORMAL, NO OVERHEAT LIGHTS NOTED. 2 L 7 4 4F A20WE 1996050200064 19960502 00064 NM 1996 5 2 P5CA9600215 1 19960424 A 2720 6905F CONTROL UNIT BOEING 747 747122 1384872 NM RUDDER FAILED A P5CA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 853FT 19753 AIRCRAFT RETURNED TO BLOCKS DUE TO RUDDER RATIO LIGHT ILLUMINATED. LOWER RUDDER STAYED IN HIGH-SPEED MODE. REMOVED AND REPLACED LOWER RUDDER RATIO CONTROL UNIT IAW MM 27-21-13. 2 L 7 4 4F A20WE 1996050200065 19960502 00065 WP 1996 5 2 RRXA96016 1 19960316 A 5730 5769600501 SKIN DOUG DC8 DC873F 302199F WP WS 507.5 CRACKED A RRXA K NONE D INFLIGHT SEPARATION IN INSP/MAINT 1 WP 15 2674U 46062 KMCN - DURING C-CHECK, FOUND 2 FASTENERS CORRODED AND SURROUNDING SKIN CRACKED JUST FORWARD OF THE FRONT SPAR ON UPPER L EADING EDGE LT WS XRS 507.5 TO 509.5. REMOVED CORROSION AND CRACKS. FABRICATED AND INSTALLED REPAIR IAW DC8 SRM 51-1-2 0A, SRM 51-1-21, AND DER APPROVED ENGINEERING SKETCH NR A37-R01. (X) 2 L 7 4 4F RT 4A25 1996050200066 19960502 00066 WP 1996 5 2 RRXA96017 1 19960316 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 216/233 TORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 2674U 46062 KMCN - DURING C-CHECK, FOUND FUSELAGE SKIN DOUBLER TORN BENEATH MAIN CARGO DOOR Y=216 TO Y=233 AND WORN AT Y=237 AT LONG ERON 22 LEFT. REMOVED DAMAGE AREAS, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DER APPROVED ENGINEERING SKETCH NR A37- R04. (X) 2 L 7 4 4F RT 4A25 1996050200067 19960502 00067 WP 1996 5 2 RRXA96018 1 19960316 A 5311 2537716 FRAME DOUG DC8 DC873F 302199F WP BS 1100 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 2674U 46062 KMCN - DURING C-CHECK, FOUND FRAME CORRODED WHERE NUTPLATES WERE MISSING F/S 1100 ABOVE LONGERON 33 LEFT LOWER SIDE OF U PPER FLANGE. REMOVED DAMAGED PORTION OF FLANGE, FABRICATED REPAIR DOUBLER AND FILLERS AND INSTALLED IAW DER APPROVED EN GINEERING SKETCH A37-R03 AND DC8 SRM 51-1-20. (X) 2 L 7 4 4F RT 4A25 1996050200068 19960502 00068 NM 1996 5 2 UPS96206052 1 19960424 A 3350 BATTERIES BOEING 727 72751C 1384015 NM ENTRY DOOR DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 903UP 18945 MAINTENANCE REPORTED EMERGENCY EXIT LIGHTS FAIL TO ILLUMINATE. CHANGED BATTERIES IN BOTH UNITS, CHECK SATISFACTORY WITH REF TO MM 33-50-01. 2 L 7 3 4F A3WE 1996050200069 19960502 00069 NM 1996 5 2 UPS96406051 1 19960319 A 5712 RIB BOEING 747 747123 1384873 NM WS 1094.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 WHILE IN FOR "C" CHECK AT AMS, MAINTENANCE REPORTED LT L/E INTERIOR INBOARD OF PYLON NR 1 RIB CRACKED UPPER CHORD AT ILE S 1094.25. REPLACED RIB IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996050200070 19960502 00070 NM 1996 5 2 UPS96406053 1 19960319 A 5311 FRAME BOEING 747 747123 1384873 NM BS 1760 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 WHILE IN FOR "C" CHECK AT AMS, MAINTENANCE REPORTED FRAME AT BS 1760, STR 10 - 15, DEFORMED AND CRACKED. REPAIRED FRAME IAW SRM 51-40-03. 2 L 7 4 4F A20WE 1996050200071 19960502 00071 NM 1996 5 2 UPS96406054 1 19960319 A 5311 FRAME BOEING 747 747123 1384873 NM BS 1880 DEFORMED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 WHILE IN FOR "C" CHECK AT AMS, MAINTENANCE REPORTED FRAME AT BS 1880, STR 10 - 15, DEFORMED. REPAIRED FRAME IAW SRM 51- 40-03, FIG. 2. 2 L 7 4 4F A20WE 1996050200072 19960502 00072 NM 1996 5 2 UPS96406055 1 19960319 A 5311 FRAME BOEING 747 747123 1384873 NM BS 1820 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 WHILE IN FOR "C" CHECK AT AMS, MAINTENANCE REPORTED FRAME AT BS 1820, STR 10 - 16, DEFORMED AND CRACKED. REPAIRED FRAME IAW SRM 51-40-03, FIG. 2. 2 L 7 4 4F A20WE 1996050200073 19960502 00073 NM 1996 5 2 UPS96406056 1 19960319 A 5311 FRAME BOEING 747 747123 1384873 NM BS 1780 R/H CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 WHILE IN FOR "C" CHECK AT AMS, MAINTENANCE REPORTED FRAME AT BS 1780, STR 10 - 15, DEFORMED AND CRACKED. REPAIRED FRAME IAW SRM 51-40-03, FIG. 2. 2 L 7 4 4F A20WE 1996050200074 19960502 00074 NM 1996 5 2 UPS96406057 1 19960319 A 5311 FRAME BOEING 747 747123 1384873 NM BS 1800 DEFORMED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 WHILE IN FOR "C" CHECK AT AMS, MAINTENANCE REPORTED FRAME AT BS 1800 STR 10 - 15, DEFORMED. REPAIRED FRAME IAW SRM 51-4 0-03, FIG. 2. 2 L 7 4 4F A20WE 1996050200075 19960502 00075 NM 1996 5 2 UPS96406058 1 19960319 A 5311 FRAME BOEING 747 747123 1384873 NM BS 1900 DEFORMED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 WHILE IN FOR "C" CHECK AT AMS, MAINTENANCE REPORTED FRAME AT BS 1900, STR 10 - 14, DEFORMED. REPAIRED FRAME IAW SRM 51- 40-03, FIG. 2.4. 2 L 7 4 4F A20WE 1996050200076 19960502 00076 NM 1996 5 2 UPS96406059 1 19960319 A 5311 FRAME BOEING 747 747123 1384873 NM BS 1740 DEFORMED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 WHILE IN FOR "C" CHECK AT AMS, MAINTENANCE REPORTED FRAME AT BS 1740, STR 10 - 15, DEFORMED. REPAIRED FRAME IAW SRM 51- 40-03, FIG. 2.4. 2 L 7 4 4F A20WE 1996050200077 19960502 00077 WP 1996 5 2 UPS96806046 1 19960403 A 5315 561387523 FLOOR BEAM DOUG DC8 DC873F 302199F WP FS 80 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 WHILE IN FOR "C" CHECK, MAINTENANCE REPORTED WEB JUST ABOVE OUTBOARD END OF FS 80, FLOOR BEAM HAS HEAVY CORROSION. REPL ACED WEB SECTION PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996050200078 19960502 00078 WP 1996 5 2 UPS96806047 1 19960329 A 2560 3753213141 LATCH CABLE DOUG DC8 DC873F 302199F WP PAX DOOR SLIDE FRAYED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 WHILE IN FOR "C" CHECK, MAINTENANCE REPORTED FORWARD ENTRAHCE DOOR, EVACUATION SLIDE GIRT BAR LATCH ASSY, CABLE FRAYED. REPLACED ASSY. REP MM 25-61-01. 2 L 7 4 4F RT 4A25 1996050200079 19960502 00079 WP 1996 5 2 UPS96806048 1 19960410 A 5320 DOOR JAMB DOUG DC8 DC873F 302199F WP FS 1350 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 WHILE IN FOR "C" CHECK, MAINTENANCE REPORTED AFT BAG BIN DOOR JAM CRACKED .50 INCH LONG AT FS 1350, LONGERONS 32R-33R. R EPAIRED PER UPS EO DC853-1615. 2 L 7 4 4F RT 4A25 1996050200080 19960502 00080 WP 1996 5 2 UPS96806049 1 19960407 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP FS 1595-1600 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 WHILE IN FOR "C" CHECK, MAINTENANCE REPORTED FS 1595-1600, FINGER DOUBLER CRACKED AT LONGERON 31R. REPLACED FINGER DOUB LER PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996050200081 19960502 00081 WP 1996 5 2 UPS96806050 1 19960401 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP FS 1540-1655 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 WHILE IN FOR "C" CHECK MAINTENANCE REPORTED HEAVY CORROSION ON INNER DOUBLER, FS 1540-1655, LONGERONS 29R-31R. REPLACED INNER DOUBLER PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1996050200082 19960502 00082 WP 1996 5 2 9609219856 1 19960423 A 2131 10256861 CONTROLLER DOUG DC9 DC951 3022051 WP AVIONICS COMPT MALFUNCTIONED A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 765NC 47718 DURING CLIMBOUT, CABIN CLIMBED ABOVE 10,000 FEET, RED CABIN PRESSURE LIGHT ILLUMINATED. DESCENDED AND OPERATED SYSTEM O N MANUAL. FLIGHT CONTINUED TO DTW AND LANDED WITHOUT FURTHER INCIDENT. REPLACED CABIN PRESSURE CONTROLLER AND PRESSURE AMPLIFIER, OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996050200083 19960502 00083 WP 1996 5 2 9609229993 1 19960421 A 2163 12911211 ANTICIPATOR DOUG DC9 DC931 3022065 WP CABIN MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 8986E 2289 2284 47402 RIGHT AIR CONDITIONING SUPPLY TEMPERATURE HIGH LIGHT ILLUMINATED WHEN THROTTLES WERE ADVANCED FOR TAKEOFF. ABORTED TAKE OFF AND RETURNED TO GATE. DEFERRED THE RIGHT AIR CONDITIONING SYSTEM PER MEL 21-1A. RIGHT ANTICIPATOR WAS SUBSEQUENTLY REPLACED IN MSP. 2 L 7 2 4F A6WE 1996050200084 19960502 00084 1996 5 2 9609239977 4 19960425 A 3414 AIR SPEED IND DOUG DC9 DC931 3022065 WP COCKPIT MALFUNCTIONED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 9341 47390 CAPTAIN'S AND FIRST OFFICER'S AIRSPEED INDICATED A DIFFERENCE OF APPROXIMATELY 40 KNOTS DURING CLIMBOUT. FLIGHT RETURNE D TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED CAPTAIN'S AND FIRST OFFICER'S AIRSPEED INDICATORS. ALSO, RE PLACED FIRST OFFICER'S ALTIMETER, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996050200085 19960502 00085 WP 1996 5 2 9609249998 1 19960425 A 3230 59516395001 BUNGEE CYLINDER DOUG DC9 DC931 3022065 WP NLG MALFUNCTIONED A NWAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 01 8934E 47143 ON APPROACH, NOSE LANDING GEAR GREEN DOWNLOCK LIGHT DID NOT ILLUMINATE AFTER GEAR WAS EXTENDED. CREW EXECUTED A GO-AROU ND AND EMERGENCY GEAR EXTENSION PROCEDURES WERE UTILIZED TO LOWER GEAR. NORMAL INDICATIONS WERE ACHIEVED AND AIRCRAFT L ANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NOSE LANDING GEAR BUNGEE CYLINDER AND OPERATIONAL CHECK NORMAL ON GEAR SWI NG. 2 L 7 2 4F A6WE 1996050200086 19960502 00086 WP 1996 5 2 9609259611 1 19960423 A 3350 6011779 BATTERY PACK DOUG DC9 DC931 3022065 WP LT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 611NA 47435 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996050200087 19960502 00087 WP 1996 5 2 9609269991 1 19960422 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8957E 47215 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD OVERWING EMERGENCY EXIT SIGN DIM. REPLACED BATTERIES, OPERATIONAL CHE CK NORMAL. 2 L 7 2 4F A6WE 1996050200088 19960502 00088 WP 1996 5 2 9609279913 1 19960423 A 3350 60030451 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 963N 47415 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AN D OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996050200089 19960502 00089 WP 1996 5 2 9609281153 1 19960425 A 3397 WIRE DOUG DC10 DC1040 3023508 WP CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 153US 46762 DURING LINE INSPECTION, FOUND THE FLOOR TRACK LIGHT INOPERATIVE ON THE RIGHT SIDE OF THE FIRST CLASS CABIN. REPAIRED TR ACK WIRING AT DOOR 2R. 2 L 7 3 4F A22WE 1996050200090 19960502 00090 NM 1996 5 2 96UAL900283 1 19960425 A 3350 LIGHTS BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 574UA 26686 EMERGENCY ESCAPE LIGHTING INOP AT AFT LAVATORY. REPLACED EMERGENCY ESCAPE LIGHT ASSEMBLY AT AFT LAVATORY, OP CHECKS NOR MAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996050200091 19960502 00091 NM 1996 5 2 96UAL900284 1 19960425 A 5210 CONTROL ROD BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FWD ENTRY DOOR OUT OF ADJUST A UALA K NONE O OTHER LD LANDING 1 WP 29 7293U 21571 FORWARD ENTRY DOOR 1L CAME UNLOCKED ON LANDING. *S/D* ACTUALLY, THE DOOR HANDLE MOVED TOWARD OPEN AFTER THE AIRPLANE LANDED. MAINTENANCE ADJUSTED THE UPPER LATCH TORQUE TUBE CONTROL ROD PER MM 52-10-04. SUBSEQUENT DOOR PERFORMANCE NORM AL. 2 L 7 3 4F 4 F A3WE E2EA 1996050200092 19960502 00092 NM 1996 5 2 96UAL900285 1 19960425 A 3350 BATTERIES BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7276U 21423 EMERGENCY LIGHT ON FWD FACE OF DROP CEILING AT AFT AIRSTAIR ENTRY INOPERATIVE. REPLACED BATTERIES, CHECKS OKAY. 2 L 7 3 4F 4 F A3WE E2EA 1996050200093 19960502 00093 WP 1996 5 2 96UAL900286 1 19960425 A 3350 BATTERY DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1817U 46616 EMERGENCY LIGHTS BATTERY CHECK FAILED MID AFT BATTERY POSITION. REPLACED BATTERY, CHECKS OKAY. 2 L 7 3 4F 4 F A22WE E23EA 1996050200094 19960502 00094 WP 1996 5 2 96UAL900287 1 19960425 A 7830 REVERSER COWL DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 2 ENGINE DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 1855U 47837 LARGE AREA OF HEAT AND DELAMINATION DAMAGE ON THE NR 2 ENGINE RIGHT REVERSER COWL. THERE IS ALSO INSULATION DAMAGE. TH ERE WAS NO FIRE WARNING INDICATION ON THE FLIGHT DECK. UNDER INVESTIGATION. SUPPLEMENTAL DATA UPDATE: DAMAGE CAUSED B Y NR 2 PNEUMATIC DUCT CLAMP FAILURE. DAMAGE REPAIRED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A22WE E23EA 1996050200095 19960502 00095 WP 1996 5 2 ARWA9604003 1 19960426 A 7931 161741A OIL PRESS SWITCH DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3B 52039 NE NR 2 ENGINE INOPERATIVE A ARWA E ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 SO 19 1803 45895 645988 DURING DESCENT, NR 2 ENGINE OIL PRESSURE LIGHT CAME ON. RETARDED THROTTLE, LIGHT STAYED ON AS PER ABNORMAL CHECK LIST. SHUTDOWN NR 2 ENGINE AT 10.52Z FL 350 OIL PRESS 15 PSI WINDMILLING. TROUBLESHOT FOUND OIL PRESSURE SWITCH BAD. REMOVE D AND REPLACED SWITCH, OPS AND LEAK CHECKED NORMAL IAW 79-30-00. 2 L 7 4 4F 4 F 4A25 1E8 1996050200096 19960502 00096 WP 1996 5 2 MWEA96121 1 19960421 A 3350 087691 LAMP HOLDER DOUG DC9 DC932 3022066 WP CABIN LOOSE A MWEA K NONE L NO TEST UK UNKNOWN 1 GL 31 502ME 48132 CABIN EMERGENCY LIGHT FLOOR PATH LIGHT AT SEAT 8C HAS BECOME DISLODGED FROM ITS SOCKET. REPLACED FLOOR TRACK LIGHT SOCK ET, OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996050200097 19960502 00097 NM 1996 5 2 P5CA9600216 1 19960424 A 3244 2605509A TIRE BOEING 747 747122 1384872 NM NR 9 MAIN BLOWN A P5CA K NONE O OTHER TO TAKEOFF 1 WP 23 852FT 19757 ON TAKEOFF, TOWER ADVISED AIRCRAFT OF RUBBER FOUND ON RUNWAY, NO COCKPIT INDICATIONS. WHEN GEAR EXENDED ON LANDING ANC BOTH PRIM AND ALT GEAR TILT LIGHTS OF RIGHT BODY GEAR CAME ON. FOUND NR 9 MAIN TIRE BLOWN. REMOVED AND REPLACED SAME I AW MM 32-45-01, COMPLIED WITH BLOWN TIRE INSPECTION IAW MM 5-51-25, C/W ANTI-SKID BITE CHECK IAW 32-42-00. REMOVED TIRE DEBRIS FROM TRUCK POSITION SWITCH AREA, PERFORMED FUNCTIONAL TEST OF BOTH PRI AND ALT TILT SWITCH SYSTEM IAW 32-13-00, NO DEFECTS NOTED. 2 L 7 4 4F A20WE 1996050200098 19960502 00098 NM 1996 5 2 P5CA9600217 1 19960423 A 5753 FOREFLAP BOEING 747 747122 1384872 NM LT/RT TE FLAP DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 FOUND DAMAGE TO LT O/B FOREFLAP AND RT I/B FOREFLAP DUE TO LOOSE BOLT IN MIDFLAP. INTERIM AIRWORTHY REPAIR PERFORMED IA W MA 5750-04-01, PERMANENT REPAIR PERFORMED JFK IAW SRM 51-00-04. 2 L 7 4 4F A20WE 1996050200099 19960502 00099 NM 1996 5 2 SCNA96049 1 19960419 A 3350 S106 BATTERIES BOEING 727 727227 1384078 NM AFT AIRSTAIR DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 275AF 22092 OVERHEAD AIRSTAIR EMERGENCY LIGHT DIM. REPLACED BATTERIES IN EMERGENCY LIGHT AND LIGHT OPS CHECKED GOOD. 2 L 7 3 4F A3WE 1996050200100 19960502 00100 NM 1996 5 2 SCNA96050 1 19960420 A 3350 582214 BATTERY PACK BOEING 727 727282 138408T NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 281SC 21949 AFT FLOOR TRACK EMERGENCY LIGHTS ARE VERY DIM. REMOVED AND REPLACED BATTERY PACK. SYSTEM OPS CHECKED NORMAL IAW 33-50- 01. 2 L 7 3 4F RT A3WE 1996050200101 19960502 00101 WP 1996 5 2 SCNA96051 1 19960420 A 2560 199821001 INDICATOR DOUG DC10 DC1010 3022110 WP L 1 DOOR SLIDE FAILED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 907WA 46946 L-1 DOOR SLIDE WOULD NOT TEST. REMOVED AND REPLACED INDICATOR ASSEMBLY, SLIDE TESTED GOOD. 2 L 7 3 4F A22WE 1996050200112 19960502 00112 CE 1996 5 2 96ZZZX2079 1 19960308 A 3230 GEAR BEECH 58 58 1152740 CE NLG ICE FROZEN A BSYA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 9069Q TH96 LANDING GEAR WOULD NOT EXTEND EITHER ELECTRICALLY OR MANUALLY. DETERMINED NOSE WHEEL ASSY WAS FROZEN IN WHEELWELL NOT L ETTING GEAR COME DOWN DUE TO FROZEN ICE SLUSH. 1 L 7 2 3O 3A16 1996050200136 19960502 00136 CE 1996 5 2 96ZZZX2103 1 19960307 A 2612 P820 CONNECTOR LEAR 35 35A 5170602 CE RT FIRE WARNING SHORT A DJFA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 EA 23 425AS 281 DURING LAST 5 MINUTES OF FLIGHT THE AIRCRAFT WAS ON APPROACH, THE RIGHT ENGINE FIRE WARNING LIGHT CAME ON. THE RIGHT EN GINE WAS SHUT DOWN AND THE FIRE BOTTLE WAS DISCHARGED. AFTER LANDING, THE FIRE WARNING LIGHT WENT OUT. NO FIRE WAS PRE SENT ON THE ENGINE. THE RIGHT FIRE WARNING CONTROL UNIT CONNECTOR P820 WAS FOUND TO HAVE AN INTERMITTENT SHORT CAUSING A FALSE FIRE INDICATION. CONNECTOR P820 WAS REPLACED AND WIRES REROUTED TO PROVIDE BETTER STRAIN RELIEF ON THE BACK OF P820. 2 L 7 2 4F A10CE 1996050200139 19960502 00139 WP 1996 5 2 96ZZZX2106 2 19960312 A 7200 ENGINE LEAR 35 35LEAR 5170600 CE GARRTT TFE731 TFE73122B 01518 WP RT ENGINE FAILED A BSYA K NONE O OTHER NR NOT REPORTED 1 GL 07 130F 044 P74216 RIGHT ENGINE HAD INTERNAL FAILURE. SUBMITTER STATED CAUSE UNKNOWN AT THIS TIME. 2 L 7 2 4F 4 F A10CE E6WE 1996050200149 19960502 00149 NM 1996 5 2 9609295521 1 19960425 A 7720 TT2 SENSOR BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE NR 2 ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J M WARNING INDICATION OVER TEMP TO TAKEOFF 1 GL 01 521US 23209 716500 DURING FULL THRUST TAKEOFF, NR 2 ENGINE EGT REACHED 630 DEGREES AND WAS CLIMBING. TAKEOFF WAS ABORTED AT 110 KNOTS AND AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED PT2/TT2 SENSOR AND REPLACED THE ENGINE OIL SCREEN, NO OIL CONTAMINA TION WAS FOUND. PERFORMED ENGINE RUNUP AND ALL OPERATING PARAMETERS WERE FOUND TO BE WITHIN LIMITS. 2 L 7 2 4F 4 F RT A2NM E17NE 1996050200150 19960502 00150 1996 5 2 9609301143 4 19960428 A 3417 HG280D5 AIR DATA COMP DOUG DC10 DC1040 3023508 WP E/E COMPT FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 133JC 14175 6354 46752 DURING TAKEOFF ROLL, THE CAPTAIN'S AIRSPEED READ 20 KNOTS HIGHER THAN THE FIRST OFFICER'S AIRSPEED INDICATOR. ABORTED T AKEOFF AND RETURED TO THE GATE. DURING TAXI THE CAPTAIN'S ALTIMETER READ 120 FEET HIGHER THAN THE FIRST OFFICER'S ALTIM ETER. REPLACED THE NR 1 AIR DATA COMPUTER. 2 L 7 3 4F A22WE 1996050200151 19960502 00151 NM 1996 5 2 9609316613 1 19960424 A 2710 ACTUATOR BOEING 747 747251B 1384892 NM AILERON CONTROL ICED UP A NWAA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 01 613US 20358 DURING CRUISE, THE AIRCRAFT WOULD NOT TURN, APPLIED A MODERATE AMOUNT OF PRESSURE TO FREE AILERONS. AIRCRAFT CONTINUED TO NRT AND LANDED WITHOUT INCIDENT. REMOVED ICE FROM THE CENTRAL CONTROL ACTUATOR LOAD LIMITER. REPLACED THE NR 2 PACK WATER SEPARATOR COALESCER AND PLENUM CHAMBER, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996050200152 19960502 00152 WP 1996 5 2 96FDEA00848 1 19960425 A 7830 9105M20G09 REVERSER HALF DOUG DC10 DC1030F 3023504 WP NR 2 ENGINE MISSING A FDEA O OTHER D J INFLIGHT SEPARATION WARNING INDICATION LD LANDING 1 SO 25 305FE 47870 NR 2 THRUST REVERSER UNLOCK LIGHT ILLUMINATED AFTER LANDING AT ISD. FOUND NR 2 LT TRANSLATING SLEEVE MISSING FROM A/C. TRANSLATING SLEEVE WAS FOUND ON RUNWAY AFTER A/C LANDED. REPLACED NR 2 LT ENGINE THRUST REVERSER ASSY, AS PER WORK CAR D NR 78T3101 AND 78T3101. NR 2 THRUST REVERSER OPS CHECK GOOD. 2 L 7 3 4F RT A22WE 1996050200153 19960502 00153 NM 1996 5 2 96FDEA00849 1 19960425 A 7603 BOLT BOEING 727 72725 1384006 NM NR 3 ENGINE MISSING A FDEA E ENGINE SHUTDOWN W INADEQUATE Q C CL CLIMB 1 SO 25 154FE 18286 AFTER T/O, NR 3 ENG THROTTLE DID NOT AFFECT ENGINE PRODUCTION, APPEARS AS IF THROTTLE LINKAGE DISCONNECTED. SHUT ENGINE DOWN USING NORMAL PROCEDURES. FOUND A BOLT HAD FALLEN OUT OF LINKAGE ON NR 3 ENGINE. REINSTALLED COTTER PIN AND CHECK ED RIG WHICH WAS GOOD. 2 L 7 3 4F A3WE 1996050200154 19960502 00154 NM 1996 5 2 96FDEA00850 1 19960425 A 2780 H1010171 EXTEND SWITCH BOEING 727 72725 1384006 NM NR 7 SLAT MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 510FE 18282 DURING FLAP RETRACTION THE NR 7 SLAT FAILED TO RETRACT. AMBER LIGHT REMAINED ON AT PILOT'S PANEL AND GREEN LIGHT REMAIN ED ON AT THE SLAT/FLAP INDICATOR PANEL. REPLACED NR 7 SLAT ACTUATOR, DID NOT CURE PROBLEM IAW 727-100 MM PAGE 401 TO 40 9 CHAP 27-81-32. REPLACED NR 7 SLAT EXTENDED SWITCH IAW 727-100 MM CHAP 27-81-11 PGS 401 TO 405, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1996050200155 19960502 00155 NM 1996 5 2 96FDEA00851 1 19960426 A 2931 ST7RM1 TRANSMITTER BOEING 727 7272S2F 1384O81 NM A-HYD SYST LEAKING A FDEA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 203FE 22925 DURING CRUISE, A-SYS HYD QTY NOTED LOW, READING LESS THAN HALF GALLON. FOLLOWED EMERGENCY PROCEDURES AND FOLLOWED LOSS OF A-SYSTEM MANUAL GEAR EXTENSION AT IAD. GEAR PINS INSTALLED AND TOWED TO GATE. FOUND SYS-A HYD TRANSMITTER LEAKING I NTERNALLY. REPLACED SAME IAW MM 29-31-00, LEAK AND OPS CHECKS GOOD. SERVICED HYD A-SYS TO FULL AND REMOVED GEAR PINS. 2 L 7 3 4F A3WE 1996050200156 19960502 00156 NM 1996 5 2 96FDEA00854 1 19960426 A 5320 STRINGER SPLICE BOEING 727 727233 138408A NM BS 680 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 270FE 22035 NR0246 AND 019 CORROSION (C53-113-01, -1) ON O/B FLANGE OF STR 27R BS 680 RBL 16. 2 L 7 3 4F RT A3WE 1996050200157 19960502 00157 NM 1996 5 2 96FDEA00855 1 19960426 A 5330 SKIN BOEING 727 727233 138408A NM BS 450 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 270FE 22035 DENT IN EXTERIOR SKIN BS 450 BETWEEN STR 15 AND 16R. REPAIRED DENT AT BS 450 BETWEEN STR 15 AND 16R PER FEDEX SRM 53-30 -03. 2 L 7 3 4F RT A3WE 1996050200158 19960502 00158 NM 1996 5 2 96FDEA00856 1 19960425 A 5311 FRAME BOEING 727 72725 1384006 NM BS 990 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 FRAME CRACKED AROUND FASTENER HOLE BS 990 I/B OF STR 4R. REPAIRED CRACK AT BS 990 I/B OF STR 4R AT FASTENER HOLE. ALOD INED AND PRIMED, DONE IAW FEDEX SRM 53-10-4. 2 L 7 3 4F A3WE 1996050200159 19960502 00159 NM 1996 5 2 96FDEA00857 1 19960426 A 5320 SHEAR TIE BOEING 727 72725 1384006 NM BS 1030 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 NR0521 AND 010 CORROSION ON FRAME SHEAR TIE AT BS 1030 RBL 10 WL 141. 2 L 7 3 4F A3WE 1996050200160 19960502 00160 NM 1996 5 2 96FDEA00858 1 19960425 A 5330 SKIN BOEING 727 72725 1384006 NM BS 1229 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 NR0583 AND 011, 3 GOUGES IN SKIN AT BS 1229 RBL 41 WL 180. 2 L 7 3 4F A3WE 1996050200161 19960502 00161 NM 1996 5 2 96FDEA00859 1 19960426 A 5330 6523688 SKIN BOEING 727 72725 1384006 NM BS 1352 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 NR0590 AND 012, CRACK SKIN AT BS 1352 RBL 23 WL 192. *S/D* REMOVED DAMAGE AREAS AT BS 1352 RBL 23 WL 192.195, FOUND TO BE IN LIMITS PER FEDEX EA 7-5330-28356. 2 L 7 3 4F A3WE 1996050200162 19960502 00162 NM 1996 5 2 96FDEA00860 1 19960426 A 5330 SKIN BOEING 727 72725 1384006 NM BS 1344 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 NR0591 AND 013, GOUGE IN SKIN AT BS 1344 LBL 29 WL 155. *S/D* CUT OUT DAMAGED AREA, FABRICATED FILLER AND DOUBLER, INST ALLED AT BS 1344 LBL 29 WL 185 AS PER SRM 54-30-3. 2 L 7 3 4F A3WE 1996050200163 19960502 00163 NM 1996 5 2 96FDEA00863 1 19960411 A 5320 PRESS DECK BOEING 747 7472R7F NM LT MLG WW CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 639FE 21650 AFTER REMOVAL OF Z-ANGLE BECAUSE OF EXTENSIVE EXFOLIATION CORROSION, ADDITIONAL CORROSION WAS NOTED UNDER Z-ANGLE ON PRE SSURE DECK WEB BS 1289 LT WW WITH SEVERAL AREAS. CORROSION WAS BEYOND ALLOWABLE LIMITS. FABRICATED DOUBLERS AS PER TRA VELER NR 51627, INSTALLED DOUBLERS IAW EA B53-10-328 AND INSTALLED NEW Z-ANGLE IAW SRM 55-10-01. 2 L 7 4 4F RT A20WE 1996050200164 19960502 00164 EU 1996 5 2 96FDEA00864 1 19960427 A 2750 RETRACT MECH AIRBUS 310 A310203 EU TE FLAPS MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 423FE 281 DEPARTING DFW, FLAPS WOULD NOT RETRACT PART APPROX 2 TO 3 DEGREES. BOTH SYSTEM 1 AND 2 FAULT LIGHTS ILLUMINATED. RETUR NED TO DFW AND FLAPS EXTENDED NORMALLY, SYS 1 AND 2 FAULT LIGHTS EXTINGUISHED AS SOON AS FLAPS EXTENED. REMOVED AND REP LACED FLAP VANE JAME BUFFER AND VERIFIED ADJ ON VETECTOR IAW MM 27-56-15. OPS FLAPS DOWN AND UP/STOWED POSITIONS SEVERA L TIMES ALL CHECKED GOOD. 2 L 7 2 4F RT A35EU 1996050200165 19960502 00165 SO 1996 5 2 COMA9610136 1 19960425 A 3260 INDICATION EMB 120 EMB120RT SO RT MLG MALFUNCTIONED A COMA O OTHER N FALSE WARNING UK UNKNOWN 1 SO 01 266CA 120258 RT MLG A-SYSTEM INDICATOR WAS GREEN WHILE LANDING GEAR WAS RETRACTED. PLACED THE 'A' INDICATION SYSTEM ON DEFERRED MAIN TENANCE LIST AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 1996050200166 19960502 00166 NE 1996 5 2 COMA9630105 2 19960425 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LEFT MALFUNCTIONED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 358CA 340A047 367171 LEFT ENGINE OVER TEMP WARNING DURING TAKEOFF ROLL. REPLACED THE LEFT ENGINE. 2 L 7 2 4T 4 T RT A52EU E8NE6 1996050200167 19960502 00167 SW 1996 5 2 MEJA960202 1 19960222 A 2710 2734042069 BELLCRANK SWRNGN SA227 SA227AT 8780610 SW LT AILERON CRACKED E MEJA K NONE O OTHER IN INSP/MAINT 1 SW 17 544UP AT544 DURING A ROUTINE INSPECTION, MAINTENANCE FOUND THE LT AILERON BELLCRANK CENTER HINGE HAD A SLIGHT CRACK. THE AIRCRAFT W AS REMOVED FROM SERVICE, INSPECTED AND FOUND SAFE FOR A ONE TIME FERRY FLIGHT FROM RAP TO SAT. UPON ARRIVAL AT SAT THE DEFECTIVE BELLCRANK WAS REMOVED AND REPLACED IN ACCORDANCE WITH FAC SRM 51-40-01. 2 L 7 2 4T RT A5SW 1996050200168 19960502 00168 WP 1996 5 2 MEJA960302 2 19960325 A 7321 89737515 FUEL CONTROL SWRNGN SA227 SA227AT 8780610 SW GARRTT TPE331 TPE33111U 01514 WP RT ENGINE DEFECTIVE E MEJA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SW 17 573G AT446B 44063C ABORTED TAKEOFF DUE TO LOSS OF POWER TO THE RIGHT ENGINE. REMOVED AND REPLACED THE RIGHT ENGINE FUEL CONTROL. GROUND R UNUP CHECK SHOWED ALL ENGINE PARAMETERS NORMAL, NO DISCREPANCIES. AIRCRAFT WAS RELEASED FOR A FUNCTIONAL CHECK FLIGHT, ALL PARAMETERS NORMAL. 2 L 7 2 4T 4 T RT A5SW E4WE 1996050200169 19960502 00169 WP 1996 5 2 MEJA960303 2 19960329 A 7200 ENGINE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE3311U 01514 WP RIGHT FAILED E MEJA E ENGINE SHUTDOWN E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SW 17 340AE AC510 44149 DURING LEVEL FLIGHT, THE RT ENGINE BEGAIN TO VIBRATE, THE ONLY ENGINE INDICATION WAS A 20 PERCENT LOSS OF TORQUE AND ALL OTHER INDICATIONS WERE NORMAL. AFTER ABOUT 15 SECONDS THE OIL PRESSURE GAUGE FLICKERED ONCE AND THE PILOTS SECURED THE ENGINE. THERE WAS NO RISE IN THE OIL TEMP INDICATION AND THE OIL PRESSURE LIGHT REMAINED EXTINGUISHED PRIOR TO SECURIN G THE ENGINE. MAINTENANCE REMOVED AND REPLACED THE ENGINE, PERFORMED ALL THE NECESSARY GROUND RUNUP CHECKS, PERFORMED A SATISFACTORY FLIGHT TEST AND RELEASED THE AIRCRAFT FOR SERVICE. 2 L 7 2 4T 3 T RT A8SW E3WE 1996050200170 19960502 00170 WP 1996 5 2 MWEA96122 1 19960426 A 7711 PT 7 LINE DOUG DC9 DC932 3022066 WP RT ENGINE LEAKING A MWEA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 31 401ME 47133 PILOT REPORTS, RT ENGINE DID NOT DEVELOPE TAKEOFF EPR ON TAKEOFF ROLL AND ABORTED TAKEOFF. SPEED WAS UNDER 90 KIAS. RE PLACED PT-7 LINE AT 12 O'CLOCK POSITION, PERFORMED LEAK CHECK AND OPS CHECK. 2 L 7 2 4F A6WE 1996050200171 19960502 00171 WP 1996 5 2 MWEA96123 1 19960426 A 2612 892809040001 FIRE LOOP DOUG DC9 DC914 3022034 WP LT ENGINE INTERMITTENT A MWEA O OTHER N FALSE WARNING CL CLIMB 1 GL 31 400ME 45727 ON CLIMB, THE LT ENGINE LOOP-B LIGHT FLICKERED, NO BELL. USED QRH, LOOP-B WAS UNRELIABLE. TESTED LOOP A AND B AGAIN. L OOP-A FLICKERED, LOOP-B TESTED GOOD. REPLACED LOOP A AND B LIGHT BULBS AND FIRE DETECTION UNIT. 2 L 7 2 4F A6WE 1996050200172 19960502 00172 EU 1996 5 2 QXEA9600160 1 19960425 A 3350 MGG12801055 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 454US 11107 EXIT SIGN ABOVE COCKPIT DOOR AND CABIN ENTRANCE ARE INOP. REPLACED BULBS, BOTH SIGNS OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996050200173 19960502 00173 EU 1996 5 2 QXEA9600161 1 19960427 A 3350 5515800106 LIGHT FOKKER F28 F28MK1000 4990808 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 802PH 11017 BOI- EMERGENCY EXIT LIGHT ABOVE COCKPIT ENTRANCE INOP. LIGHT ASSY REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996050200174 19960502 00174 NM 1996 5 2 UPS96220001 1 19960426 A 5347 BAC1521434 SEAT TRACK BOEING 727 727173C 1384059 NM BS 870 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 938UP 19506 SEAT TRACK AT BS 870 LBL 1 WL 208 HAS CORNER CRACKED OFF. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-10-5. 2 L 7 3 4F A3WE 1996050200175 19960502 00175 NM 1996 5 2 UPS96406061 1 19960402 A 5720 65B1013517 TUBE BOEING 747 747123 1384873 NM WS 1071 WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED LT L/E INTERIOR I/B OF PYLON NR 1 FOUND WEAR HOLE IN SUPPORT TUBE ON AISL ES 1071.25. REMOVED TUBE IAW MM 20-50-03, INSTALLED BUSHINGS IAW OHM 20-50-03 AND INSTALLED NEW TUBE IAW MM 20-50-03. 2 L 7 4 4F A20WE 1996050200176 19960502 00176 WP 1996 5 2 UPS96806060 1 19960425 A 3350 5708458503 BATTERY PACK DOUG DC8 DC871F 302199D WP CREW ENTRY DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 705UP 45949 MAINTENANCE REPORTED, EMERGENCY EXIT LIGHTS DO NOT TEST PROPERLY DURING PRE/FLT. REPLACED BATTERY AND RELAY UNIT WITH R EF TO MM 33-50-01, GROUND CKS GOOD. 2 L 7 4 4F RT 4A25 1996050200177 19960502 00177 WP 1996 5 2 UPS96806062 1 19960405 A 5320 FITTING DOUG DC8 DC873F 302199F WP FS 280 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED B/T FITTING HAS HEAVY CORROSION AT FS 280 BETWEEN LONGERONS 32R AND 33R. REP LACED FITTINGS PER SRM 51-1-21D. 2 L 7 4 4F RT 4A25 1996050200178 19960502 00178 WP 1996 5 2 UPS96806063 1 19960405 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP FS 155 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED AFT ADF ANTENNA INNER AND OUTER DOUBLERS HAVE HEAVY CORROSION AT FS 155 LONGE RONS 35L AND 36L. REPLACED BOTH DOUBLERS PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1996050200179 19960502 00179 WP 1996 5 2 UPS96806064 1 19960402 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP FS 220 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED 'A' CSD FWD DOUBLER HAS CORROSION AT FS 220 TO 260 LONGERONS 30R TO 35L. REP LACED DOUBLER PER SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 1996050200180 19960502 00180 WP 1996 5 2 UPS96806065 1 19960402 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP FS 260-360 CORROSION A IPXA O OTHER O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, 'A' CSD INNER DOUBLER HAS CORROSION REPAIRS ON FS 260 TO 360 LONGERONS 27R T O 35L. REPLACED DOUBLER PER SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 1996050200181 19960502 00181 WP 1996 5 2 UPS96806066 1 19960329 A 5330 SKIN DOUG DC8 DC873F 302199F WP FS 70-190 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION DAMAGE ON FUSELAGE BELLY SKIN FS 70 TO 190. REPLACED BELLY SKIN SE CTION PER DAC DRAWING NR 5779925. 2 L 7 4 4F RT 4A25 1996050200182 19960502 00182 WP 1996 5 2 UPS96806067 1 19960404 A 5313 9754913 LONGERON DOUG DC8 DC873F 302199F WP FS 280-300 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON I/B SIDE OF LONGERON 34R BETWEEN FS 280 TO 300. REPLACED LONGERON ON T/C 43627 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996050200183 19960502 00183 WP 1996 5 2 UPS96806068 1 19960329 A 5330 57552713N1 SKIN DOUG DC8 DC873F 302199F WP FS 190-450 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION BULGES ON FUSELAGE BELLY SKIN FS 190 TO 450. REPLACED BELLY SKIN P ANEL PER DRAWING NR 5755271. 2 L 7 4 4F RT 4A25 1996050200184 19960502 00184 WP 1996 5 2 UPS96806069 1 19960402 A 5311 FRAME DOUG DC8 DC873F 302199F WP FS 1680 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 1680 BELTFRAME HAS HEAVY CORROSION AND CRACKED AT LONGERON 21L. REPAIRED FRAME PER SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1996050200185 19960502 00185 WP 1996 5 2 UPS96806070 1 19960331 A 5320 FITTING DOUG DC8 DC873F 302199F WP FS 1580 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 1580 LONGERON 21L HAS HEAVY CORROSION AFT SIDE. REPAIRED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996050200186 19960502 00186 WP 1996 5 2 UPS96806071 1 19960401 A 5320 FITTING DOUG DC8 DC873F 302199F WP FS 140 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FWD AND AFT SIDES OF FITTING TOP SIDE HAS HEAVY CORROSION ON LONGERON 21R FS 140. REPLACED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996050200187 19960502 00187 WP 1996 5 2 UPS96806072 1 19960403 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FS 70-190 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 80 HEAVY CORROSION ON LONGERONS 35R. REPLACED LONGERONS FS 70 TO 190 PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996050200188 19960502 00188 WP 1996 5 2 UPS96806073 1 19960402 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FS 215-260 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LONGERON 36L HAS MODERATE CORROSION AT FS 215 TO 260. REPLACED LONGERON SECT ION PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1996050200189 19960502 00189 WP 1996 5 2 UPS96806074 1 19960331 A 5320 FITTING DOUG DC8 DC873F 302199F WP FS 1440 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED MODERATE CORROSION ON LONGERONS 21L FITTING FS 1440. REPLACED FITTING PER SR M 51-1-20D. 2 L 7 4 4F RT 4A25 1996050200190 19960502 00190 WP 1996 5 2 UPS96806075 1 19960403 A 5320 FITTING DOUG DC8 DC873F 302199F WP FS 1230 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON B/T FITTING FS 1230 LONG 35R TO 36. REPLACED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996050200191 19960502 00191 WP 1996 5 2 UPS96806076 1 19960403 A 5320 SHEAR TIE DOUG DC8 DC873F 302199F WP FS 1080 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED SHEAR TIE HAS CORROSION DAMAGE AND BROKEN AT FS 1080 O/B OF LONG 35R. REPLAC ED SHEAR TIE PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996050200192 19960502 00192 WP 1996 5 2 UPS96806077 1 19960402 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FS 194-246 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION DAMAGE ON LONG 35L I/B FS 194 TO 246. REPLACED LONG SECTION PER SR M 51-1-20D. 2 L 7 4 4F RT 4A25 1996050200193 19960502 00193 WP 1996 5 2 UPS96806078 1 19960402 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FS 216-246 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LONGERON 35L O/B HAS CORROSION DAMAGE AT FS 216 TO 246. REPLACED LONGERON SE CTION PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996050200194 19960502 00194 WP 1996 5 2 UPS96806079 1 19960401 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP FS 160-170 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 160 TO 170, LONGERON 31R HAD HEAVY CORROSION ON FINGER DOUBLER. REPLACED PER SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 1996050200195 19960502 00195 WP 1996 5 2 UPS96806080 1 19960402 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FS 215-260 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION AND CRACK AT LONGERON 36 RT SIDE AT FS 215 AND FS 260. REPLA CED LONGERON SECTION PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1996050200196 19960502 00196 WP 1996 5 2 UPS96806081 1 19960401 A 5311 FRAME DOUG DC8 DC873F 302199F WP FS 140 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 140 LONGERON 36 HAD HEAVY CORROSION ON BELTFRAME. REPLACED FRAME PER SRM 53-2-0. 2 L 7 4 4F RT 4A25 1996050200197 19960502 00197 WP 1996 5 2 UPS96806082 1 19960402 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP FS 180-335 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FINGER DOUBLER HAD HEAVY CORROSION AT LONGERON 31L FS 180 TO 335. REPLACED D OUBLER SECTION PER SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 1996050200198 19960502 00198 WP 1996 5 2 UPS96806083 1 19960401 A 5311 FRAME DOUG DC8 DC873F 302199F WP FS 180 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION DAMAGE BEYOND LIMITS AT BELTFRAME FS 180 BETWEEN LONGERONS 35R AND 36. REPAIRED FRAME PER SRM 53-2-0, FIG 2. 2 L 7 4 4F RT 4A25 1996050200199 19960502 00199 NM 1996 5 2 96ZZZX2116 1 19960203 A 3020 DEICE BOOT DORNER DO32 DO328100 2996000 NM LT ENGINE INLET DEFECTIVE A VNAA O A OTHER UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 07 441JS 0770 3059 BLD/IAD - FLT 4126 - EN ROUTE, CREW REPORTED A PROBLEM WITH THE LEFT ENGINE INLET DEICE BOOT. THEY WERE ALERTED BY AN A MBER CAS MESSAGE DEICE BOOT FAIL. AIRCRAFT DIVERTED TO PIT. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. PIT MAINTENANCE REPLACED THE LEFT ENGINE INLET DEICE BOOT E.F.C.V. IAW MM 30-22-03, GROUND RUN CHECKED GOOD. 2 H 7 2 4T RT A45NM 1996050200200 19960502 00200 NM 1996 5 2 96ZZZX2117 1 19960307 A 5270 WARNING LIGHT DORNER DO32 DO328100 2996000 NM CARGO DOOR ILLUMINATED A VNAA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 GL 07 441JS 3059 FLT 4165 - CREW REPORTED THE CARGO DOOR WARNING LIGHT ILLUMINATED DURING FLIGHT. AIRCRAFT RETURNED TO AZO, LANDED 400 P OUNDS OVERWEIGHT. AIRCRAFT WAS FERRIED WHERE CAK MAINTENANCE CONDUCTED AN OVERWEIGHT LANDING INSPECTION IAW MM 05-00-00 . NO DEFECTS NOTED. MAINTENANCE ALSO INSPECTED THE CARGO DOOR WARNING SYSTEM, NO DEFECTS NOTED. SUSPECT CARGO DOOR MI CROSWITCHES MAY HAVE FROZEN DURING THE NIGHT. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A45NM 1996050200201 19960502 00201 WP 1996 5 2 96ZZZX2118 1 19960310 A 3150 102ADP12 ANNUNCIATOR PNL DOUG DC9 DC983 3022083 WP NR 1 ENGINE MALFUNCTIONED A TWAA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 CE 05 110HM 49787 PHL - FLT 343 - DURING CRUISE, NR 1 ENGINE OIL STRAINER CLOG LIGHT ILLUMINATED. SHUT DOWN NR 1 ENGINE. REMOVED AND REP LACED ELECTRONIC OVERHEAD ANNUNCIATOR PANEL, MFG P/N 102ADP1-2. OPERATIONAL CHECK NORMAL. CHECK C-1D - 6-25-95 - MCI. 2 L 7 2 4F RT A6WE 1996050200207 19960502 00207 NE 1996 5 2 96ZZZX2124 2 19960210 A 7321 CONNECTORS 81118103003 DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE LT ECU DIRTY A VNAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 07 439JS 3057 FLT 4168 - LEFT ENGINE ECU (ELECTRONIC CONTROL UNIT) FAILED IN-FLIGHT. AIRCRAFT RETURNED TO FIELD, AIRCRAFT LANDED WITH OUT INCIDENT. PIT MAINTENANCE REMOVED, CLEANED, AND REINSTALLED THE CANNON CONNECTORS FOR THE NP AND P1.8 SENSORS. ALS O, THE CONNECTORS ON THE ECU. WORK ACCOMPLISHED IAW MM 71-00-00 AND STD MAINTENANCE PRACTICES. GROUND RUN CHECKED GOO D. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T 4 T RT A45NM E20NE 1996050200208 19960502 00208 NE 1996 5 2 96ZZZX2125 2 19960302 A 7200 ENGINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE NR 2 OIL LEAK A TWAA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 05 9401W 53137 LNK - FLT 235 - DURING CRUISE, SHUT DOWN NR 2 ENGINE, SN 1402, DUE TO OIL LOSS. FOUND OIL LEAK IN TURBINE AREA. REPLAC ED NR 2 ENGINE AND ENGINE OPERATION CHECKED NORMAL. ENGINE TOTAL TIME: 9,465 HOURS; 4,437 CYCLES. CHECK C-1D - 12-23- 95 - JFK. 2 L 7 2 4F 4 F RT A6WE E9NE 1996050200209 19960502 00209 WP 1996 5 2 96ZZZX2126 1 19960308 A 7920 7938314 OIL LINE DOUG DC9 DC982 3022082 WP NR 1 ENGINE RUPTURED A TWAA E ENGINE SHUTDOWN J K WARNING INDICATION FLUID LOSS CR CRUISE 1 CE 05 951U 49245 STL - FLT 712 - DURING CRUISE, SHUT DOWN NR 1 ENGINE, SN 3215, DUE TO OIL FILTER DIFFERENTIAL PRESSURE LIGHT ILLUMINATIO N. FOUND OIL LINE, MFG PN 7938314, TO DIFFERENTIAL PRESSURE SWITCH RUPTURED. REPLACED OIL LINE. ENGINE OPERATION, LEA K CHECK AND INDICATION WAS NORMAL. ENGINE TOTAL TIME: 33,308 HOURS; 17,329 CYCLES, CHECK C-1D - 4-1-95 - MCI. 2 L 7 2 4F A6WE 1996050200212 19960502 00212 NM 1996 5 2 96ZZZX2129 1 19960411 A 3260 656021132 ACCESSORY UNIT BOEING 727 727225 1384077 NM LANDING GEAR FAILED A UHVA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 11 355PA 20625 FLL/IND - FLT FKYC9355, 4/11/96 - AFTER TAKEOFF FLL WHEN GEAR RETRACTED, ALL 3 RED GEAR LIGHTS ILLUMINATED AS WELL AS F/ O TAIL SKID LIGHT. AIRCRAFT RETURNED TO FLL. REPLACED LANDING GEAR ACCESSORY UNIT. JACKED AIRCRAFT, SWUNG GEAR NUMERO US TIMES. LANDING GEAR POSTION INDICATING SYSTEM OPERATIONALLY CHECKS OKAY PER MM 32. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A3WE 1996050200213 19960502 00213 WP 1996 5 2 96ZZZX2130 1 19960408 A 3231 LATCH ASSY DOUG DC9 DC915 3022036 WP RT MLG DOOR OUT OF ADJUST A TWAA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 490SA 45798 STL - FLT 692 - AFTER TAKEOFF FOLLOWING GEAR RETRACTION, THE RT MAIN GEAR UNSAFE LIGHT REMAINED ON. ADJUSTED RT MAIN GE AR DOOR LATCH ASSY. PERFORMED GEAR SWING, OPERATION NORMAL. CHECK C - 2-17-95 - MCI. (X) 2 L 7 2 4F A6WE 1996050200214 19960502 00214 NE 1996 5 2 96ZZZX2131 2 19960409 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 2 FAILED A TWAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 CE 05 918TW 49367 STL - FLT 85 - DURING CRUISE, NR 2 ENGINE, SN 3240, OIL FILTER CLOG LIGHT ILLUMINATED. ENGINE WAS SHUT-DOWN AND SUBSEQU ENTLY CHANGED. ENGINE TOTAL TIME 28,723 HOURS; 14,781 TOTAL CYCLES. CHECK C-2D - 6/5/95 - MCI. 2 L 7 2 4F 4 F A6WE E9NE 1996050200215 19960502 00215 NM 1996 5 2 96ZZZX2132 1 19960409 A 7820 HUSH KIT BOEING 707 707330C 138367G NM NR 2 ENGINE DAMAGED A CLCA E ENGINE SHUTDOWN D INFLIGHT SEPARATION CR CRUISE 1 SO 19 707HE 20124 MNMG/MSLP - FLT 049 - DURING CRUISE, NR 2 FIRE WARNING CAME ON, WHEN THROTTLE RETARDED, WARNING WENT OUT. PROCEEDED WIT H PRECAUTIONARY SHUT-DOWN OF ENGINE. ON VISUAL INSPECTION OF ENGINE, FOUND LOWER SECTION OF HUSH KIT DAMAGED. CONTINUE D TO INSPECT FIRE WARNING SYSTEM, FOUND NORMAL. BORESCOPED ENGINE, NO DAMAGE NOTED. REPLACED ENGINE HUSH KIT ASSEMBLY. PERFORMED RUN-UP PER MM 71-00-00, ENGINE OPERATION NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4A26 1996050200216 19960502 00216 EA 1996 5 2 96ZZZX2133 2 19960402 A 7321 32447731 FUEL CONTROL STBROS SD3 SD330 8100602 EU PWA PT6 PT6A45R 52043 EA LT ENGINE OUT OF ADJUST A DATA O OTHER O OTHER LD LANDING 1 GL 13 335MV SH3017 PCE84125 FLT 1256 - UPON LANDING IN BKW, PILOT SELECTED BETA ON BOTH ENGINES, THE LEFT ENGINE WENT INTO REVERSE CAUSING THE AIRCR AFT TO VIOLENTLY PULL TO THE LEFT GOING OFF RUNWAY STRIKING RUNWAY LIGHTS AND CAUSING MINOR DAMAGE TO AIRCRAFT STUBWING. MAINTENANCE FOUND INSUFFICIENT DEAD BAND IN ENGINE CONTROL SYSTEM, RE-RIGGED ENGINE CONTROL SYSTEM AND MADE REPAIR TO AIRCRAFT STUBWING SKIN. 2 H 7 2 4T 4 T A41EU E4EA 1996050200217 19960502 00217 NE 1996 5 2 96ZZZX2134 2 19960302 A 7250 LPT 3 SEAL DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE NR 2 ENGINE FAILED A TWAA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 05 9401W 53137 LNK - FLT 235 - DURING CRUISE SHUT DOWN NR 2 ENGINE, SN 1402, DUE TO OIL LOSS. FOUND OIL LEAK IN TURBINE AREA. REPLACE D NR 2 ENGINE AND ENGINE OPERATION CHECKED NORMAL. ENGINE TOTAL TIME: 9,465 HOURS; 4,437 CYCLES. CHECK C-1D - 12-23-9 5 - JFK. FURTHER INVESTIGATION INTO NR 2 ENGINE SHUT-DOWN REVEALED A FAILED LPT 3 SEAL RESULTING IN THE OIL LOSS. THE SEAL HAS BEEN REPLACED AND ENGINE, SN 1402, HAS BEEN RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A6WE E9NE 1996050200218 19960502 00218 NE 1996 5 2 96ZZZX2135 2 19960112 A 7200 ENGINE BOEING 767 767205 1385121 NM PWA JT9 JT9D7R4D 52054 NE NR 1 MALFUNCTIONED A TWAA O OTHER O OTHER CL CLIMB 1 CE 05 650TW 23057 SEA - FLT 740 - DURING CLIMB, NR 1 ENGINE, SN 4609, SURGED. POWER WAS REDUCED TO IDLE. CHANGED NR 1 ENGINE. ENGINE TO TAL TIME: 29,752 HOURS; 8,040 CYCLES. CHECK C-4C - 10-25-95 - LAX. 2 L 7 2 4F 4 F RT A1NM E3NE 1996050200220 19960502 00220 WP 1996 5 2 AALA960401 1 19960314 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1307 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 255AA 49287 TUL - CORROSION ON NR 3 SEAT TRACK AT STA 1307. INSTALLED SEAT TRACK PLUG PER AARD 53-20-00. TST: 34,667.47 HRS. CY CLES: 19,822. (X) 2 L 7 2 4F A6WE 1996050200221 19960502 00221 WP 1996 5 2 AALA960411 1 19960318 A 5320 FITTING DOUG DC9 DC982 3022082 WP BS 693 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 255AA 49287 TUL - MID-CARGO LOWER DOOR BEAM AFT ANGLE FITTING CORRODED. INSTALLED NEW ANGLE AFT END OF CARGO DOOR BEAM. TST: 34, 667.47 HRS. CYCLES: 19,822. (X) 2 L 7 2 4F A6WE 1996050200222 19960502 00222 WP 1996 5 2 AALA960412 1 19960318 A 5320 FITTING DOUG DC9 DC982 3022082 WP BS 636 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 255AA 49287 TUL - MID-CARGO LOWER DOOR BEAM FORWARD ANGLE FITTING CORRODED. INSTALLED NEW FORWARD ANGLE FITTING IN MID-CARGO DOORWA Y. TST: 34,667.47 HRS. CYCLES: 19,822. (X) 2 L 7 2 4F A6WE 1996050200223 19960502 00223 WP 1996 5 2 AALA960418 1 19960319 A 5315 FLOOR BEAM DOUG DC9 DC982 3022082 WP BS 1338 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 255AA 49287 TUL - CORROSION AROUND NUT CLIP HOLE IN FLOORBEAM. CUT OUT CORRODED AREA, INSTALLED FILLER AND DOUBLER PER SRM 53-05, F IGURE 20A. TST: 34,667.47 HRS. CYCLES: 19,822. (X) 2 L 7 2 4F A6WE 1996050200224 19960502 00224 WP 1996 5 2 AALA960419 1 19960319 A 5311 BELL FRAME DOUG DC9 DC982 3022082 WP BS 1323 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 255AA 49287 TUL - CORROSION ON BELL FRAME FORWARD SIDE LOWER LIP AT LONGERON 30. CUT OUT DAMAGE (CORRODED AREA) ON LOWER J-ANGLE (F RAME) INSTALLED REPAIR SPLICE AND DOUBLER PER SRM 53-03, FIGURE 2A, SHEETS 3-5, PAGES 4E-4J. TST: 34,667.47 HRS. CYC LES: 19,822. (X) 2 L 7 2 4F A6WE 1996050200225 19960502 00225 WP 1996 5 2 AALA960420 1 19960319 A 5347 TIE DN TRACK DOUG DC9 DC982 3022082 WP CARGO COMPT CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 255AA 49287 TUL - CORROSION ON TIE-DOWN TRACK, STA 1060 TO STA 1174. INSTALLED NEW TRACK FORWARD LEFT SECTION, STA 1003 - STA 1222. TST: 34,667.47 HRS. CYCLES: 19,822. (X) 2 L 7 2 4F A6WE 1996050200226 19960502 00226 WP 1996 5 2 AALA960421 1 19960319 A 5347 TIE DN TRACK DOUG DC9 DC982 3022082 WP CARGO COMPT CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 255AA 49287 TUL - CORROSION AT EACH FRAME ATTACH FASTENER THE FULL LENGTH OF TRACK, RIGHT SIDE. INSTALLED NEW TRACK, FORWARD RIGHT SECTION, STA 1003 - STA 1155. TST: 34,667.47 HRS. CYCLES: 19,822. (X) 2 L 7 2 4F A6WE 1996050200227 19960502 00227 WP 1996 5 2 AALA960427 1 19960320 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 1336 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 255AA 49287 TUL - CORROSION AROUND NUT CLIP HOLE AT LONGERON 18L T-ANGLE AT STA 1336. REMOVED CORROSION, MADE DOUBLER AND INSTALLED PER SRM 53-01, PAGE 8, WHICH ALSO REPLACED ATTACH CLIP TO FLOORBEAM AT STA 1338. TST: 34,667.47 HRS. CYCLES: 19,82 2. (X) 2 L 7 2 4F A6WE 1996050200228 19960502 00228 WP 1996 5 2 AALA960428 1 19960319 A 5320 SHEAR TIE DOUG DC9 DC982 3022082 WP BS 1322 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 255AA 49287 TUL - INBOARD END OF SHEAR TIE CORRODED BETWEEN 29L AND 30L AT FS 1322. TRIM SHEAR TIE PER ESO 80559, TREATED AND PRIME D AREA ESO DATED 3-19-96. TST: 34,667.47 HRS. CYCLES: 19,822. (X) 2 L 7 2 4F A6WE 1996050200229 19960502 00229 WP 1996 5 2 AALA960442 1 19960321 A 5320 593666065L ANGLE DOUG DC9 DC982 3022082 WP BS 1211 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 255AA 49287 TUL - CORROSION ON ANGLE. REPLACED ANGLE. TST: 34,667.47 HRS. CYCLES: 19,822. (X) 2 L 7 2 4F A6WE 1996050200230 19960502 00230 WP 1996 5 2 AALA960446 1 19960318 A 5315 FLOOR BEAM DOUG DC9 DC982 3022082 WP BS 1322 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 255AA 49287 TUL - CORROSION AROUND NUT CLIP HOLE 2.50 FEET OUTBOARD OF INBOARD WALL, STA 1322, FLOOR BEAM RIGHT. REMOVED CORROSION AND INSTALLED STAINLESS STRAP ON FLOOR BEAM, STA 1322 PER SRM 53-05, FIGURE 20. TST: 34,667.47 HRS. CYCLES: 19,822. (X) 2 L 7 2 4F A6WE 1996050200231 19960502 00231 WP 1996 5 2 AALA960487 1 19960320 A 5320 SHEAR TIE DOUG DC9 DC982 3022082 WP BS 1309 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 255AA 49287 TUL - SHEAR TIE CRACKED AT STA 1309 BETWEEN LONGERON 14L AND LONGERON 15L. STOP DRILLED CRACK AND BLENDED FRAME BEHIND SHEAR-TIE, TREATED AND PRIMED PER ESO 80559, 3-20-96. TST: 34,667.47 HRS. CYCLES: 19,822. (X) 2 L 7 2 4F A6WE 1996050200232 19960502 00232 CE 1996 5 2 BUHA96003 1 19960219 A 2730 AN416 PIVOT BOLT 081400010 CESSNA 310 310R 2074245 CE ELEVATOR WORN A BUHA K NONE O OTHER IN INSP/MAINT 1 GL 23 22DM 8987 310R0069 DURING A 100-HOUR INSPECTION, THE ELEVATOR BELLCRANK PIVOT BOLT WAS FOUND LOOSE, WHICH CAUSED WEAR ON THE BELLCRANK SUPP ORT BRACKET. THIS WAS CAUSED BY THE PIVOT COMING LOOSE AND ALLOWING THE BOLT TO WORK IN THE SUPPORT BRACKETS. (X) 1 L 7 2 3O 3A10 1996050200233 19960502 00233 NE 1996 5 2 CAL960108 2 19960208 A 7230 ANNULUS SEAL BOEING 757 757224 1384958 NM RROYCE RB211 RB211535E4 54555 NE NR 1 ENGINE DISRUPTING SEAL A CALA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SW 09 14106 5735 25296 31213 IAH - FLT 0711 - NR 1 ENGINE N1 VIBRATION MONITOR CAME UP ON SCREEN AT 37,000 FEET. YELLOW (AMBER) APPROX 2.7. QRH PRO CEDURES FOLLOWED TO REDUCE VIBRATION AND NO VIBRATION FELT IN ACFT OR LEFT THROTTLE. WHEN NR 1 ENG REDUCED TO 83.5 N1, VID READ 2.5, NORMAL COLOR. ACFT DIVERTED TO DEN WHERE IT LANDED WITHOUT INCIDENT. EICAS CHECKED AND SHOWED HIGH VIB ASSOCIATED WITH N1 FAN. FAN BLADES AND SPINNER INSPECTED. FAN BLADE ANNULUS FILLER SEALS WERE DISRUPTING AIRSEAL. AN ANNULUS SEAL REALIGNMENT PERFORMED IAW MM 72-31-13. AN ANNULUS FILLER SEAL REPAIR PERFORMED ON ALL ANNULUS FILLERS NR 1 ENG IAW ECRA 7231-01064, MOD 72-B106. T/O POWER CHK PERFORMED PER MM 71-00-00 AND MAX VIB WAS AT 1.6 UNITS.(X) 2 L 7 2 4F 4 F RT A2NM E12EU 1996050200234 19960502 00234 NE 1996 5 2 CAL960206 2 19960226 A 7200 ENGINE BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 3 FAILED A A CALA A UNSCHED LANDING J E WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 SW 09 511PE 37948 1973 20634 700708 IAH - FLT 1926 - THE NR 3 ENGINE THROTTLE BEGAN TO VIBRATE AT 1,200 FEET DURING CLIMB-OUT OF IAH. A STRONG VIBRATION WA S REPORTED IN REAR CABIN. THE NR 3 ENGINE POWER WAS REDUCED, BUT THE VIBRATION CONTINUED. A LOUD BANG ACCOMPANIED BY N R 3 ENGINE SHUTDOWN OCCURRED AS ENGINE POWER WAS ADDED TO RESUME CLIMB. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDE D WITHOUT INCIDENT. THE NR 3 ENGINE WAS REMOVED AND REPLACED. THE SDR WILL REMAIN OPEN FOR PART INFORMATION EPNDING IN VESTIGATION. (X) 2 L 7 3 4F 4 F A3WE E2EA 1996050200236 19960502 00236 WP 1996 5 2 HAL96018 1 19960227 A 2782 VTA03440 EYEBOLT DOUG DC9 DC951 3022051 WP LT LE SLAT ACT FAILED A HALA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 WP 13 EICBG 47742 HNL - FLT 564 - WHEN SELECTING SLATS AND FLAPS 50-250 KIAS, AIRPLANE ROLLS ABRUPTLY TO THE RIGHT AND THEN LEFT. MUST BE THEN FLOWN TO STRAIGHT AND LEVEL. AIRCRAFT REACTS NORMALLY TO ALL ADDITIONAL FLAP SETTINGS. FOUND LEFT BOTTOM SLAT LO WER ACTUATOR EYEBOLT FAILED. REPLACED LOWER ACTUATOR EYEBOLT. ADJUSTED AND OPERATIONAL CHECK OK IAW MM CHAPTER 27-80-5 . (X) 2 L 7 2 4F A6WE 1996050200237 19960502 00237 WP 1996 5 2 HAL9639 1 19960411 A 3350 BATTERY PACK DOUG DC10 DC1010 3022110 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 119AA 46519 HNL - FLT 10 - ON PRE-FLIGHT IN HNL, FOUND AFT POWER PACK OF EMERGENCY LIGHTING SYSTEM INOPERATIVE. REPLACED POWER PACK . OPS CHECK OK. (X) 2 L 7 3 4F A22WE 1996050200238 19960502 00238 WP 1996 5 2 IXXA9648 1 19960414 A 2110 5614845517 TURBOCOMPRESSOR DOUG DC8 DC862 3021970 WP NR 1 MALFUNCTIONED A IXXA O H OTHER DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 11 61CX 2662 46142 RJTY/RJOI - EN ROUTE BETWEEN RJTY AND RJOI, NR 1 CABIN TURBOCOMPRESSOR BECAME NOISY AND PRODUCED AN OILY SMELL. THE NR 12 TC WAS SHUT OFF, AND WAS DEFERRED AT RJOI. THE NR 12 TC WAS SCHEDULED FOR REPLACEMENT DUE TO POSSIBLE BEARING/OIL SE AL FAILURE. (X) 2 L 7 4 4F 4A25 1996050200239 19960502 00239 WP 1996 5 2 IXXA9649 1 19960416 A 2910 436392218 O-RING DOUG DC8 DC862 3021970 WP SLOT CNTRL VALVE FAILED A IXXA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SW 11 735PL 46153 KLCK/TJSJ - EN ROUTE, ALL MAIN HYDRAULIC SYSTEM QUANTITIES DROPPED TO THE STANDPIPE LEVEL. AN UNEVENTFUL LANDING WAS AC COMPLISHED AT TJSJ, AND THE AIRCRAFT WAS TOWED BACK TO THE RAMP. INSPECTION OF THE AIRCRAFT REVEALED AN O-RING HAD BLOW N ON THE SLOT CONTROL VALVE. THE O-RING WAS REPLACED AND LEAK-CHECKED IAW THE DC-8 MM, AND THE AIRCRAFT RETURNED TO SER VICE. (X) 2 L 7 4 4F 4A25 1996050200240 19960502 00240 NM 1996 5 2 PCAA9600276 1 19960308 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM FUSELAGE DAMAGED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 827EX 390 DURING ENGINE START ON GROUND, THE DC GROUND POWER CART CABLE SHORTED AGAINST AIRCRAFT SKIN AND CAUSED FIRE DAMAGE TO AR EA AFT OF GPU CONNECTION. AIRCRAFT WAS FERRIED TO MDT FOR REPAIR. DAMAGED AREA WAS REPAIRED IAW DHC REPAIR DRAWING 8-5 3-1939, ISSUE 2. AIRCRAFT RETURNED TO SERVICE. ACTT: 3,453:36 HRS. ACTC: 3,975. (X) 2 H 7 2 4T RT A13NM 1996050200241 19960502 00241 EU 1996 5 2 REXA96006 1 19960216 A 2150 147D000 COOLING TURBINE BAG JETSTM JETSTM3101 1500215 EU CENTER BAY SEIZED A REXA D RETURN TO BLOCK B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 SO 25 308P 1234 674 PIB - FLT 5519 - ON TAXI OUT, PILOT HAD RIGHT DUCT OVERTEMP LIGHT AND ACRID SMELL/SMOKE IN CABIN. RETURNED TO RAMP. CO OLING SYSTEM INSPECTED AND RENDERED INOPERATIVE PER MEL 21-01. (X) 2 L 7 2 4T RT A21EU 1996050200242 19960502 00242 WP 1996 5 2 RRXA96019 1 19960317 A 5347 FLOOR TRACK DOUG DC8 DC873F 302199F WP BS 500-510 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 2674U 46062 KMCN - DURING C-CHECK, FOUND CARGO COMPARTMENT FLOOR TRACK CORRODED AT Y=500 TO Y=510 X = .59. ROUTED OUT DAMAGE AREA. FABRICATED AND INSTALLED REPAIR IAW DER APPROVED ENGINEERING SKETCH A37-R02. (X) 2 L 7 4 4F RT 4A25 1996050200243 19960502 00243 EU 1996 5 2 SIMA960791 1 19960319 A 2911 291F00200000 ACCUMULATOR AEROSP ATR42 ATR42300 8680920 EU GREEN LEAKS A SIMA O OTHER J K WARNING INDICATION FLUID LOSS CL CLIMB 1 SW 21 135MQ 0343 135 ORD - FLT 4218 - SHORTLY AFTER TAKEOFF DURING CLIMB-OUT WITH GEAR AND FLAPS UP, THE GREEN SIDE HYDRAULIC LOW LEVEL INDIC ATION ILLUMINATED, AND REMAINED ON FOR THE ENTIRE FLIGHT. THE LANDING GEAR GRAVITY EXTENSION PROCEDURE WAS APPLIED DURI NG THE APPROACH AT THAT TIME. THE LOW LEVEL INDICATION EXTINGUISHED FOLLOWED BY SINGLE CHIME WARNING AND HYDRAULIC INDI CATION ON CWP. C/A - REPAIRED THE GREEN SYSTEM ACCUMULATOR, NO OTHER LEAKS NOTED. OPERATIONAL CHECK OF GEAR OPS CHECKE D GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1996050200244 19960502 00244 EU 1996 5 2 SIMA961012 1 19960410 A 3350 0341519 FUSE AEROSP ATR72 ATR72212 EU CABIN BLOWN A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 426AT 426 DFW - FLT 3741 - PASSENGER COMPARTMENT EMERGENCY LIGHTS FOUND TO BE INOPERATIVE. REPLACED POWER SUPPLY FUSE. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1996050200245 19960502 00245 EU 1996 5 2 SIMA961022 1 19960411 A 2910 4019501 PUMP AEROSP ATR72 ATR72212 EU BLUE HYD SYST FAILED A SIMA O OTHER J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SW 21 348AE FB68 349 DFW - FLT 3750 - EN ROUTE TO DFW, PILOT REPORTED THE BLUE SYSTEM HYDRAULIC LOW LEVEL INDICATOR ILLUMINATED. AIRCRAFT LA NDED WITHOUT INCIDENT AFTER DECLARING EMERGENCY. MAINTENANCE INSPECTED SYSTEM AND FOUND PUMP TO HAVE INTERNAL DAMAGE AN D WAS LEAKING OVERBOARD. PUMP REPLACED IAW THE J.I.C. AND OPS CHECK AND LEAK CHECK WAS SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1996050200246 19960502 00246 EU 1996 5 2 SIMA961061 1 19960415 A 3350 3011210 LIGHT AEROSP ATR42 ATR42300 8680920 EU PASSENGER DOOR FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 223AT 625 223 ORD - FLT 4015 - PASSENGER DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY. AIRCRAFT RETURNED TO SE RVICE. (X) 2 H 7 2 4T RT A53EU 1996050200247 19960502 00247 EU 1996 5 2 SIMA961062 1 19960415 A 3350 301151 POWER SUPPLY AEROSP ATR42 ATR42300 8680920 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 223AT 223 ORD - FLT 4015 - FORWARD CABIN INTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1996050200248 19960502 00248 NE 1996 5 2 SRAA49602 2 19960413 A 7200 ENGINE BOEING 747 747246F NM PWA JT9 JT9D7J 52054 NE NR 3 FAILED A A SRAA E A ENGINE SHUTDOWN UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 GL 23 741SJ 32190 22063 702288 JFK/JAL - FLT 037 - ON TAKEOFF FOR FLIGHT JAL 037 OUT OF JFK, NR 3 ENGINE LOST N1 FOLLOWED BY TOTAL POWER FAILURE AND A LOUD BANG AT THE SAME TIME. ACCOMPLISHED EMERGENCY PROCEDURES AND AIR TURN-BACK TO JFK. PERFORMED BORESCOPE INSPECTION , FOUND NO DEFECTS. ATTEMPTED TO PERFORM ENGINE RUN, BUT N1 WOULD NOT ROTATE. REPLACED NR 3 ENGINE AND PERFORMED ENGIN E RUN, OPS CHECK PER MM CHAPTER 71-00-00. (X) 2 L 7 4 4F 4 F A20WE E20EA 1996050200249 19960502 00249 WP 1996 5 2 TC8A96042 1 19960414 A 2910 AA960230 FLEX LINE DOUG DC8 DC8F55 3021928 WP SPOILER FAILED A TC8A D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 808CK 45817 SBSV-SBSV - FLT NR 10501 - TAXIING OUT FROM SBSV, NO SPOILER PRESSURE. REMOVED AND REPLACED HYDRAULIC PRESSURE LINE. C HECK GROUND OPS OK IAW MM 27-33-1. (X) 2 L 7 4 4F 4A25 1996050200250 19960502 00250 NM 1996 5 2 TSAA9653006 1 19960318 A 5320 SILL BOEING 737 737297 1384480 NM BS 360 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 723AL 21739 DURING SCHEDULED INSPECTION OF FORWARD AIRSTAIR DOORWAY SILL BS 351.2 AND BS 360 BODY FRAME INSPECTION (ECO 1391 R2), A CRACK WAS FOUND AT BS 360 BETWEEN STR 20L AND STR 21L. VERIFIED CRACK WITH HFEC AND DYE PENETRANT. STOP DRILLED CRACK A T BS 360. REPAIRED PER ECO 1380 R1 AND DRAWING 65C23267. AIRCRAFT RETURNED TO SERVICE. TAC: 63,805. TAT: 32,329.57 HRS. (X) 2 L 7 2 4F A16WE 1996050200251 19960502 00251 NM 1996 5 2 TSAA9653019 1 19960407 A 5330 SKIN BOEING 737 7372Q9 138448M NM BS 727 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 804AL 21719 DURING OVERNIGHT INSPECTIONS, DISCOVERED FUSELAGE SKIN CRACK 1 INCH IN LENGTH, 2 INCHES FORWARD OF BS 727A AND ABOVE S17 R. VERIFIED BY HFEC. CARRIED OUT REPAIR WORK WITH REFERENCE PER SRM 53-30-5. AIRCRAFT RETURNED TO SERVICE. TAT: 38, 401:42 HRS. TAC: 49,191. (X) 2 L 7 2 4F A16WE 1996050200252 19960502 00252 NM 1996 5 2 USAASB96064 1 19960410 A 3397 WIRE BOEING 737 7372B7 1384560 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 287AU 23134 DCA - FLT 1126 - EMERGENCY FLOOR LIGHTING BROKEN RIGHT SIDE, ROW 9. MAINTENANCE FOUND BROKEN WIRE AT RIGHT SIDE, ROW 9. SPLICED BROKEN WIRE AND RESECURED LIGHT STRIP. (X) 2 L 7 2 4F A16WE 1996050200253 19960502 00253 EU 1996 5 2 VTZA96150 1 19960411 A 2150 DUCT JETAIR JETSTM JETSTM4101 1500501 EU LT ACM LOOSE A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 302UE 41013 ROC/JFK - FLT 6518 - AT 1045 HRS ON 4-11-96, ABORTED TAKEOFF DUE TO LT PACK DUCT FAIL CAPTION ILLUMINATED DURING THE TAK EOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE RESECURED ACM DUCT TO THE ACM. AIRCRAFT W AS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1996050200254 19960502 00254 EU 1996 5 2 VTZA96151 1 19960414 A 5270 91SE16 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU MAIN BAGG DOOR OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 325UE 41063 IAD/LYH - FLT 6310 - DURING TAKEOFF TO LYH AT 1938 HRS ON 4-14-96, ABORTED TAKEOFF DUE TO MAIN BAGGAGE DOOR LIGHT ILLUMI NATING DURING THE TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED THE BAGGAGE DOOR WARNING MICROSWITCHES. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1996050200255 19960502 00255 EU 1996 5 2 VTZA96152 1 19960413 A 3150 T/O WARNING JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT ACTIVATED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 310UE 41028 BOS/IAD - FLT 6157 - DURING TAKEOFF AT 1125 HRS ON 4-13-96, ABORTED TAKEOFF DUE TO THE TAKEOFF CONFIGURATION WARNING SYS TEM ACTIVATING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE PERFORMED OPS CHECKS BUT COULD NOT FI ND ANY DEFECTS. AIRCRAFT WAS RELEASED AND APPROVED FOR SERVICE. (X) 2 L 7 2 4T RT A41NM 1996050200256 19960502 00256 SO 1996 5 2 WTAA960070 1 19960401 A 2750 3075001017 FLAP CONTL UNIT EMB 120 EMB120RT SO LT TE FLAPS INTERMITTENT A WTAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 17 454UE 120155 SFO - FLAP ASYMMETRY REPORTED WITH LEFT NACELLE FLAP INDICATING '2 BARS' IN CRUISE FLIGHT. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE REPLACED FLAP CONTROL UNIT. FLAP SYSTEM OPERATIONAL CHECK NORMAL. (X) 2 L 7 2 4T RT A31SO 1996050200257 19960502 00257 WP 1996 5 2 Y2PA96017 1 19960408 A 5330 5911401 SKIN DOUG DC9 DC915F 3022037 WP BS 108 CRACKED A Y2PA K NONE O OTHER IN INSP/MAINT 1 GL 23 198US 65107 47045 YIP - ONE .25 INCH CRACK IN THE RIGHT SIDE OF THE NLG WHEELWELL SKIN AT STA 108. REMOVED DAMAGED SKIN AREA. FABRICATED AND INSTALLED REPAIR FILLER AND REPAIR DOUBLER PER USA JET AIRLINES ENGINEERING AUTHORIZATION NR 96-53-02R1. THESE DAT A WERE DER APPROVED BY R. MNASHI, DER NR SW-810 ON FAA FORM 8110-3 DATED 4-7-96. PART TC: 78,559. (X) 2 L 7 2 4F A6WE 1996050200258 19960502 00258 NE 1996 5 2 Y2PA96021 2 19960422 A 7230 589470 FAN GUIDE VANE DOUG DC9 DC915F 3022037 WP PWA JT8 JT8D7B 52053 NE NR 1 ENGINE CRACKED A A Y2PA O OTHER J E WARNING INDICATION VIBRATION/BUFFET NR NOT REPORTED 1 GL 23 197US JX6364 47154 P657238 YIP - FLIGHT CREW REPORTED LIGHT ENGINE VIBRATION EN ROUTE TO YIP. UPON LANDING, ENGINE WAS INSPECTED AND A 30-INCH CRA CK WAS DETECTED IN THE LEFT ENGINE LOWER FAN EXIT GUIDE VANE CASE. CRACK WAS IN THE FORWARD RADIUS OF THE CASE AND RAN DOWN FROM THE TOP OF THE LOWER CASE SECTION IN A VERTICAL DIRECTION ALONG THE RADIUS. REMOVED AND REPLACED FAN EXIT GUI DE VANE. PERFORMED ENGINE VIBRATION MONITORING PERFORMANCE ENGINE RUN AND CONDUCTED A TEST FLIGHT OF THE AIRCRAFT. (X) 2 L 7 2 4F 4 F A6WE E2EA 1996050200259 19960502 00259 SO 1996 5 2 96ZZZX2137 2 19960403 A 7414 101630601 MAGNETO CESSNA 402 402B 207590P CE CONT O520 TSIO520EB 17040 SO LEFT DEFECTIVE A OEZA K NONE O OTHER IN INSP/MAINT 1 WP 19 765EA 370 K109412ER 402B0401 271333R PILOT COMPLAINED OF MISFIRING ENGINE. FOUND BOTH MAGNETOS WOULD CAUSE MISFIRING. REPLACED BOTH MAGS AND PROBLEM WENT A WAY. TCM REBUILT ENGINE WAS INSTALLED ON 10-95 WHICH INCLUDED THE MAGS. 1 L 7 2 3O 3 O A7CE E8CE 1996050200260 19960502 00260 SO 1996 5 2 96ZZZX2138 2 19960403 A 7414 101630203 MAGNETO CESSNA 402 402B 207590P CE CONT O520 TSIO520EB 17040 SO RIGHT DEFECTIVE A OEZA K NONE O OTHER IN INSP/MAINT 1 WP 19 765EA 370 K159411ER 402B0401 271333R PILOT COMPLAINED OF MISFIRING ENGINE. FOUND BOTH MAGNETOS WOULD CAUSE MISFIRING. REPLACED BOTH MAGS AND PROBLEM WENT A WAY. TCM REBUILT ENGINE WAS INSTALLED ON 10-95 WHICH INCLUDED THE MAGS. 1 L 7 2 3O 3 O A7CE E8CE 1996050200261 19960502 00261 CE 1996 5 2 96ZZZX2139 1 19960315 A 3230 GEAR BEECH 58 58 1152740 CE RT MLG COLLAPSED A BSYA K NONE O OTHER LD LANDING 1 GL 07 1814W TH287 RIGHT GEAR COLLAPSED ON LANDING. SUBMITTER STATED CAUSE UNKNOWN AT THIS TIME. 1 L 7 2 3O 3A16 1996050200262 19960502 00262 CE 1996 5 2 96ZZZX2140 1 19960308 A 3260 SAB2R31 SWITCH BEECH 58 58 1152740 CE MLG DOWNLOCK FAULTY A BSYA O OTHER O OTHER AP APPROACH 1 GL 07 696BD TH352 GEAR WOULD NOT EXTEND, HAND CRANKED GEAR DOWN, LANDED OK. CHANGED BOTH DOWN AND LOCK SWITCHES ON GEARBOX. OPS CHECKED OK. 1 L 7 2 3O 3A16 1996050200280 19960502 00280 CE 1996 5 2 96ZZZX2158 1 19960409 A 7931 INDICATION CESSNA 421 421C 2076016 CE OIL PRESSURE MALFUNCTION A BXSA E ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 EA 09 60RR 61 421C0885 PILOT MADE A PRECAUTIONARY ENGINE SHUT-DOWN AND PROPELLER FEATHER DUE TO A PERCEIVED LOSS OF ENGINE OIL PRESSURE. THE F OLLOWING MAINTENANCE INSPECTION COULD NOT FIND ANY DEFECTS IN THE ENGINE OR OIL PRESSURE INDICATING SYSTESM. TWO GROUND RUNS AND A TEST FLIGHT WERE PERFORMED WITH NO DEFECTS NOTED. 1 L 7 2 3O A7CE 1996050200313 19960502 00313 NE 1996 5 2 9609321143 2 19960428 A 7230 COMPRESSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 2 ENGINE STALLED A NWAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DE DESCENT 1 GL 01 133JC 46752 86117 AT TOP OF DESCENT, THE NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL. THE ENGINE WAS SHUTDOWN AND A HIGH ALTITUDE RAPID RE START WAS ATTEMPTED BUT DID NOT START. A SECOND RESTART WAS SUCCESSFUL AND FLIGHT CONTINUED TO MCO WITHOUT FURTHER INCI DENT. MAINTENANCE PERFORMED VISUAL INSPECTIONS. ENGINE WAS REPLACED DUE TO FAILED BORESCOPE INSPECTION. 2 L 7 3 4F 4 F A22WE E20EA 1996050200314 19960502 00314 WP 1996 5 2 9609339872 1 19960426 A 7931 42D110 OIL PRESS SW DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE LT ENGINE MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 781NC 35823 23442 48121 696727 NR 1 ENGINE LOW OIL PRESSURE WARNING LIGHT ILLUMINATED IN FLIGHT. THE FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDEN T. MAINTENANCE REPLACED THE LOW OIL PRESSURE SWITCH WITH A SERVICEABLE UNIT. 2 L 7 2 4F 4 F A6WE E2EA 1996050200315 19960502 00315 NM 1996 5 2 9609342705 1 19960428 A 3150 T/O WARNING BOEING 727 727225 1384077 NM COCKPIT ACTIVATED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 802EA 22433 DURING TAKEOFF ROLL, THE AIRCRAFT EXPERIENCED TAKEOFF WARNING INDICATION. TAKEOFF WAS ABORTED WITHOUT INCIDENT AND RETU RNED TO THE GATE. SRQ MAINTENANCE PERFORMED FLIGHT CONTROL AND TAKEOFF WARNING CHECK, SYSTEM CHECKED OK. 2 L 7 3 4F A3WE 1996050200316 19960502 00316 WP 1996 5 2 9609359862 1 19960427 A 2130 PRESS AMPLIFIER DOUG DC9 DC951 3022051 WP CABIN BROKEN WIRES A A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 771NC 47769 AFTER TAKEOFF, CABIN PRESSURIZATION STARTED CLIMBING AND DESCENDING ABOUT 800 FEET IN EACH DIRECTION. THE LEFT MAIN LAN DING GEAR UNSAFE LIGHT REMAINED ILLUMINATED. ACFT RETURNED TO ATL AND LANDED WITHOUT INCIDENT. FOUND WIRES H538A24-RD AND H539A24-BL BROKEN AT P1-230 CABIN PRESSURE AMPLIFIER. RECRIMPED WIRES AND AUTO PRESSURE SYSTEM TESTED GOOD. FOUND LEFT INBOARD DOOR PROXIMITY SENSOR TARGET CONTACTING DOOR JAMB STRUCTURE THUS NOT LETTING DOOR FULLY CLOSE. ADJUSTED DO OR SENSOR TARGET AND SWUNG GEAR, OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996050200317 19960502 00317 WP 1996 5 2 9609369750 1 19960428 A 3150 SPOILER HANDLE DOUG DC9 DC941 302207N WP COCKPIT OUT OF ADJUST A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 750NW 47114 TAKEOFF DISCONTINUED AT APPROXIMATELY 20 KNOTS DUE TO TAKEOFF WARNING. TAXIED CLEAR AND ADJUSTED SPEEDBRAKE HANDLE, AFT ER WHICH TAKEOFF WARNING DISCONTINUED. MAINTENANCE ADJUSTED SPOILER/SPEEDBRAKE SWITCH S1-143 AND TAKEOFF WARNING SYSTEM CHECKED GOOD PER MM 27-00. 2 L 7 2 4F A6WE 1996050200318 19960502 00318 WP 1996 5 2 9609379307 1 19960428 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 309RC 48088 DURING LINE CHECK, FOUND CENTER AISLE EMERGENCY LIGHTS INOPERATIVE AT ROW 14 TO 19. REPLACED BATTERY AND PACK, OPERATIO NAL CHECK GOOD. 2 L 7 2 4F A6WE 1996050200319 19960502 00319 WP 1996 5 2 9609389180 1 19960429 A 3350 BATTERY PACK DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 3312L 45707 DURING LINE CHECK, FOUND BOTH LEFT AND RIGHT EMERGENCY ESCAPE LIGHTS FOR NACELLES INOPERATIVE. REPLACED LEFT AND RIGHT EMERGENCY LIGHT BATTERY PACKS, OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996050200320 19960502 00320 WP 1996 5 2 9609399752 1 19960426 A 3350 POWER SUPPLY DOUG DC9 DC941 302207N WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 752NW 47116 DURING LINE CHECK, FOUND COCKPIT FORWARD ENTRY AND GALLEY OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED P OWER SUPPLY, OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996050200321 19960502 00321 WP 1996 5 2 9609409103 1 19960425 A 3350 LIGHT DOUG DC9 DC915 3022036 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 93S 47078 DURING LINE CHECK, FOUND FIRST CLASS DIVIDER OVERHEAD EMERGENCY LIGHT INOPERATIVE. REWIRED EMERGENCY AND STANDBY POWER LIGHTS, OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996050200322 19960502 00322 EU 1996 5 2 9609413202 1 19960428 A 2780 831A000005 BRAKE ACTUATOR AIRBUS 320 A320211 3930320 EU LT LE SLAT MALFUNCTIONED A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 302US 32 DURING APPROACH AFTER SELECTING FLAPS ONE POSITION, RECEIVED F/CTL SLATS LOCKED MESSAGE. THE WING TIP BRAKE ENGAGED. C REW FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES, DECLARED AN EMERGENCY, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLA CED THE LEFT WING SLAT WING TIP BRAKE ACTUATOR AND OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996050200323 19960502 00323 WP 1996 5 2 9609429608 1 19960426 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 608NW 47233 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS AT ROWS 11, 12, 13 AND LEFT OVERWING EMERGENCY EXIT LIGHT INO PERATIVE. REPLACED BATTERY PACK AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996050200324 19960502 00324 WP 1996 5 2 9609439602 1 19960427 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 602NW 47046 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. REPLACED THREE SETS OF BATTERY PACKS AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996050200325 19960502 00325 WP 1996 5 2 9609449950 1 19960429 A 3260 DNLOCK SWITCH DOUG DC9 DC932 3022066 WP NLG MALFUNCTIONED A NWAA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 01 9346 47376 ON APPROACH, NOSE LANDING GEAR RED UNSAFE LIGHT DID NOT ILLUMINATE WITH POWER LEVERS AT FLIGHT IDLE AND GREEN DOWNLOCK L IGHT DID NOT ILLUMINATE AFTER GEAR WAS EXTENDED. EMERGENCY GEAR EXTENSION PROCEDURES WERE UTILIZED AND THE AIRCRAFT LAN DED WITHOUT INCIDENT. MAINTENANCE FOUND FAULT IN THE NOSE GEAR DOWNLOCK SWITCH. REPLACED SWITCH, RIGHT AND LEFT MAIN G EAR DOORS DUE TO DAMAGE INCURRED ON LANDING, OPERATIONAL CHECK NORMAL ON GEAR SWING. 2 L 7 2 4F A6WE 1996050200326 19960502 00326 NM 1996 5 2 SCNA96052 1 19960423 A 3350 1000677 LIGHT BOEING 727 727225 1384077 NM CABIN FAILED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 282SC 22558 THE AFT ENTRY OVERHEAD EMERGENCY EXIT LIGHT IN OVERHEAD LIGHT PANEL IS INOP WITH EMERGENCY LIGHTS TURNED ON. REMOVED AN D REPLACED AFT ENTRY OVERHEAD EMERGENCY EXIT LIGHT IAW MM 33-50-101, LIGHT OPS CHECKED GOOD. 2 L 7 3 4F A3WE 1996050200327 19960502 00327 WP 1996 5 2 SCNA96053 1 19960420 A 5311 FRAME DOUG DC10 DC1015 3022118 WP BS 1841 PUNCTURED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 THE FRAME WEB AT STATION 1841 WAS FOUND PUNCTURED AT APPROXIMATELY LONGERON 39L. REPAIRED FRAME IAW DC10 SRM 53-30-00, VOLUME I. 2 L 7 3 4F A22WE 1996050200328 19960502 00328 NM 1996 5 2 SCNA96054 1 19960416 A 2761 ACTUATOR BRACKET BOEING 727 7272J4 1384006 NM NR 8 SPOILER CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 285SC 21676 DURING HEAVY MAINTENANCE VISIT, THE NUMBER 8 SPOILER ACTUATOR SUPPORT FITTING WAS FOUND CRACKED ON THE VERTICAL FLANGE O F THE RIGHT TRAILING EDGE BEAM. INSTALLED REPAIR IAW LOCKHEED ENGINEERING ORDER NUMBER 3753. 2 L 7 3 4F RT A3WE 1996050200329 19960502 00329 NM 1996 5 2 SCNA96055 1 19960416 A 5743 FITTING BOEING 727 7272J4 1384006 NM RT MLG BEAM ELONGATED HOLE A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 285SC 21676 DURING HEAVY MAINTENANCE VISIT, THE RIGHT HAND MAIN LANDING GEAR BEAM OUTBOARD SUPPORT FITTING RETAINER BOLT HOLE WAS FO UND ELONGATED. REPAIRED SUPPORT FITTING PER SUN COUNTRY ENGINEERING ORDER 57-5242-1. 2 L 7 3 4F RT A3WE 1996050200330 19960502 00330 NM 1996 5 2 SWAA960232 1 19960425 A 5320 SPLICE BOEING 737 7372H4 138448C NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED D-CHECK, FOUND KEEL BEAM I/B SPLICE-T CRACKED AT BS 727 LBL 6, WL 154. REMOVED AND REPLACED WITH NEW P ART PER BOEING SRM. 2 L 7 2 4F A16WE 1996050200331 19960502 00331 NM 1996 5 2 SWAA960233 1 19960424 A 5315 FLOOR BEAM BOEING 737 7373H4 1384600 NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 312SW 23334 DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORROSION AT BS 344 LBL 35 LBL 7.5 BL 0 AND RBL 1.5. REPAIRED PER BOEING SRM . 2 L 7 2 4F RT A16WE 1996050200332 19960502 00332 NM 1996 5 2 SWAA960234 1 19960424 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 827 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 312SW 23334 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827 S9L AT FASTENER HOLE. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996050200333 19960502 00333 NM 1996 5 2 SWAA960235 1 19960424 A 5260 DOOR STOP BOEING 737 7372H4 138448C NM AIRSTAIR DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED B/C CHECK, FOUND FWD UPPER AIRSTAIR DOOR STOP AFT T-CAP SECTION CRACKED 1.5 LONG. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996050200334 19960502 00334 NM 1996 5 2 SWAA960236 1 19960424 A 3350 FLASHLIGHT BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 20SW 21337 AT GATE, FOUND AFT O/B EMERGENCY FLASHLIGHT TEST LIGHT INDICATOR INOP. REPLACED FLASHLIGHT PER BOEING M/M. 2 L 7 2 4F A16WE 1996050200335 19960502 00335 NM 1996 5 2 SWAA960237 1 19960425 A 5315 FLOOR BEAM BOEING 737 7373G7 1384595 NM BS 315 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED 1/4 D-CHECK, FOUND FLOOR BEAM STRAP CRACKED AT BS 315 LBL 12. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996050200336 19960502 00336 NM 1996 5 2 SWAA960238 1 19960425 A 5320 ANGLE SUPPORT BOEING 737 7375H4 138449D NM BS 303.9 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 512SW 24189 DURING SCHEDULED 1/2 D-CHECK, FOUND Z-ANGLE SUPPORT STRIP AT BS 303.9 CORRODED. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996050200337 19960502 00337 NM 1996 5 2 SWAA960239 1 19960425 A 5312 BULKHEAD BOEING 737 7375H4 138449D NM BS 948 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 512SW 24189 DURING SCHEDULED 1/2 D-CHECK, FOUND SEVERAL CRACKS AT BLOW OUT PANEL CUTOUT IN CENTER OF BULKHEAD AT BS 948. REPAIRED P ER BOEING SRM. 2 L 7 2 4F RT A16WE 1996050200338 19960502 00338 NM 1996 5 2 SWAA960240 1 19960425 A 5320 ANGLE BOEING 737 7375H4 138449D NM BS 947/986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 512SW 24189 DURING SCHEDULED 1/2 D-CHECK, FOUND AFT SERVICE DOOR THRESHOLD Z-ANGLE CORRODED AT BS 947 AND 986.5. REPLACED PER BOEIN G SRM. 2 L 7 2 4F RT A16WE 1996050200339 19960502 00339 NM 1996 5 2 SWAA960241 1 19960425 A 5312 BLKHD STRAP BOEING 737 7375H4 138449D NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 512SW 24189 DURING SCHEDULED 1/2 D-CHECK, FOUND RT HORIZ STRAP CRACKED AT FWD END AT BS 727 BULKHEAD, AT S22R. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996050200340 19960502 00340 NM 1996 5 2 SWAA960242 1 19960425 A 5320 CLIP BOEING 737 7375H4 138449D NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 512SW 24189 DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER TO LT FRAME TIE CLIP CRACKED AT I/B END, BS 663. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996050200341 19960502 00341 NM 1996 5 2 SWAA960243 1 19960425 A 5320 ANGLE BOEING 737 7375H4 138449D NM BS 380-400 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 512SW 24189 DURING SCHEDULED 1/2 D-CHECK, FOUND UPPER ANGLE WEBS CRACKED EXTENDING FROM CLIP NUT, BS 380 TO 400, BL 0 AND AT BS 482 TO 520. REPLACED ANGLES PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996050200342 19960502 00342 NM 1996 5 2 SWAA960244 1 19960425 A 5320 ANGLE BOEING 737 7375H4 138449D NM BS 291.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 512SW 24189 DURING SCHEDULED 1/2 D-CHECK, FOUND ANGLE CRACKED BETWEEN S10 AND 9R AT BS 291.5. REPLACED ANGLE PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996050200343 19960502 00343 NM 1996 5 2 SWAA960245 1 19960425 A 5312 BLKHD CHANNEL BOEING 737 7375H4 138449D NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 512SW 24189 DURING SCHEDULED 1/2 D-CHECK, FOUND U-CHANNEL CRACKED AT BS 727 BULKHEAD AT RBL 3. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996050200344 19960502 00344 NM 1996 5 2 SWAA960246 1 19960425 A 5320 BEAM BOEING 737 7375H4 138449D NM RT WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 512SW 24189 DURING SCHEDULED 1/2 D-CHECK, FOUND CRACK IN AFT EDGE OF RT W/W STRINGER 18A SHEAR BEAM O/B HOLE. REPAIRED PER SWA ACO 6580-53. 2 L 7 2 4F RT A16WE 1996050200345 19960502 00345 NM 1996 5 2 SWAA960247 1 19960425 A 5320 ANGLE BOEING 737 7375H4 138449D NM BS 294.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 512SW 24189 DURING SCHEDULED 1/2 D-CHECK, FOUND RT SKATE ANGLE CRACKED AT BS 294.5 RBL 55. REPAIRED PER TI-A53-0233. 2 L 7 2 4F RT A16WE 1996050200346 19960502 00346 NM 1996 5 2 SWAA960248 1 19960425 A 5313 STRINGER BOEING 737 7375H4 138449D NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 512SW 24189 DURING SCHEDULED 1/2 D-CHECK, FOUND LT AFT STRINGER 18A CRACKED TO 1ST FASTENER AT BS 727. REPAIRED PER ACO 6580-53. 2 L 7 2 4F RT A16WE 1996050200347 19960502 00347 NM 1996 5 2 SWAA960249 1 19960425 A 5320 ANGLE BOEING 737 7375H4 138449D NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 512SW 24189 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM SUPPORT ANGLE CRACKED AT BS 540, O/B OF SWING LINK AT BL 0 LEFT SIDE. RE PLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996050200348 19960502 00348 NM 1996 5 2 SWAA960250 1 19960425 A 5315 SUPPORT BOEING 737 7372H4 138448C NM BS 284-286 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 85SW 22826 DURING SCHEDULED HD CHECK, FOUND FLOOR BEAM SUPPORT CORRODED AT BS 284 TO 286 LBL 11 WL 208. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996050200349 19960502 00349 NM 1996 5 2 SWAA960251 1 19960425 A 5320 SILL BOEING 737 7372H4 138448C NM BS 316-344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 85SW 22826 DURING SCHEDULED HD CHECK, FOUND FWD ENTRY DOORWAY MOPSILL CORRODED AT BS 316 TO 344 LBL 57 TO 59 WL 208. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996050200350 19960502 00350 NM 1996 5 2 SWAA960252 1 19960425 A 5320 SILL BOEING 737 7372H4 138448C NM BS 955-996 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 85SW 22826 DURING SCHEDULED HD CHECK, FOUND AFT SERVICE DOORWAY MOPSILL CORRODED AT BS 955 TO 996 RBL 47TO 52 WL 208 TO 209. REPLA CED PER BOEING SRM. 2 L 7 2 4F A16WE 1996050200351 19960502 00351 NM 1996 5 2 SWAA960253 1 19960425 A 5320 CHORD BOEING 737 7372H4 138448C NM BS 1156 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 85SW 22826 DURING SCHEDULED HD CHECK, FOUND O/B CHORD CRACKED AT BS 1156 WL 240 RBL 18. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996050200352 19960502 00352 NM 1996 5 2 SWAA960254 1 19960425 A 5315 FLOOR BEAM BOEING 737 7372H4 138448C NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 85SW 22826 DURING SCHEDULED HD CHECK, FOUND UPPER FLOOR BEAM CORRODED AT BS 1016 RBL 10, 20 TO 34, WL 208. REPLACED PER BOEING SRM . 2 L 7 2 4F A16WE 1996050200353 19960502 00353 NM 1996 5 2 SWAA960255 1 19960425 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 291 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 85SW 22826 DURING SCHEDULED HD CHECK, FOUND ANGLE CRACK AT BS 291 RBL 60 WL 248 208. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996050200354 19960502 00354 NM 1996 5 2 SWAA960256 1 19960425 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 296 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 85SW 22826 DURING SCHEDULED HD CHECK, FOUND CRACKED DOOR FRAME AT BS 296 RBL 57 WL 216. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996050200355 19960502 00355 NM 1996 5 2 SWAA960257 1 19960425 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 291 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 85SW 22826 DURING SCHEDULED HD CHECK, FOUND ANGLE CRACKED AT BS 291 RBL 60 WL 248. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996050200356 19960502 00356 NM 1996 5 2 SWAA960258 1 19960425 A 5320 FRAME BOEING 737 7372H4 138448C NM BS 296 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 85SW 22826 DURING SCHEDULED HD CHECK, FOUND CRACK LOWER FWD DOOR FRAME AT BS 296 RBL 57, WL 216. REPLACED FRAME PER BOEING SRM. 2 L 7 2 4F A16WE 1996050200357 19960502 00357 NM 1996 5 2 SWAA960259 1 19960425 A 5315 FLOOR BEAM BOEING 737 7372H4 138448C NM BS 294 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 85SW 22826 DURING SCHEDULED HD CHECK, FOUND FLOOR BEAM CRACKED AT BS 294 RBL 55 WL 208. REPLACED BEAM PER BOEING SRM. 2 L 7 2 4F A16WE 1996050200358 19960502 00358 NM 1996 5 2 SWAA960260 1 19960425 A 5320 STRAP BOEING 737 7372H4 138448C NM BS 326 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 85SW 22826 DURING SCHEDULED HD CHECK, FOUND TENSION STRAP CRACKED AT BS 326 RBL 31 WL 200. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996050200359 19960502 00359 NM 1996 5 2 SWAA960261 1 19960425 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 348 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 85SW 22826 DURING SCHEDULED HD CHECK, FOUND CRACKED ANGLE AND STRAP AT FWD ENTRY DOOR STOP FITTINGS NR 9 AND 10 BS 348. REPAIRED P ER BOEING SRM. 2 L 7 2 4F A16WE 1996050200360 19960502 00360 NM 1996 5 2 SWAA960262 1 19960425 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 302 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 85SW 22826 DURING SCHEDULED HD CHECK, FOUND CRACKED ANGLE ABOVE STRINGER 10L AT BS 302. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996050200361 19960502 00361 NM 1996 5 2 SWAA960263 1 19960425 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 85SW 22826 DURING SCHEDULED HD CHECK, FOUND Z-ANGLE CRACKED BS 663, AFT SIDE LBL 6 WL 170 LEFT WHEEL WELL. REPAIRED PER BOEING SRM . 2 L 7 2 4F A16WE 1996050200362 19960502 00362 NM 1996 5 2 SWAA960264 1 19960425 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 500 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 85SW 22826 DURING SCHEDULED HD CHECK, FOUND FUSELAGE FRAME DENTED AT BS 500A S24L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996050200363 19960502 00363 NM 1996 5 2 SWAA960265 1 19960425 A 5320 CLIP BOEING 737 7372H4 138448C NM BS 520/400 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 85SW 22826 DURING SCHEDULED HD CHECK, FOUND STRINGER CLIPS CRACKED AT BS 520 S19L AND AT BS 400 S27L. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996050200364 19960502 00364 NM 1996 5 2 SWAA960266 1 19960425 A 5320 WEB BOEING 737 7373G7 1384595 NM BS 787-794 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED 1/4 D-CHECK, FOUND WEB CRACKED AT AFT CARGO DOOR BS 787 TO 794, S 24 TO 25. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996050200365 19960502 00365 NM 1996 5 2 SWAA960267 1 19960429 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 675AA 23253 DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT RBL 6.7, WL 197.5-198.6, AT LBL 4.7, WL 197-198.6, AT LBL 4.7 , WL 202.5-203.5, AND RBL 4.7, WL 197.5 -198.5. REPAIRED PER SWA EWO 97-0189. 2 L 7 2 4F RT A16WE 1996050200366 19960502 00366 NM 1996 5 2 SWAA960268 1 19960429 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 675AA 23253 DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AROUND 3 FASTENERS, AT WL 234, RBL 7-10. REPAIRED PER TI T1-A53 -015. 2 L 7 2 4F RT A16WE 1996050200367 19960502 00367 NM 1996 5 2 SWAA960269 1 19960429 A 3350 20131 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 330SW 23694 DURING SCHEDULED TERMINAL CHECK, FOUND MIS CABIN EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996050200368 19960502 00368 NM 1996 5 2 SWAA960270 1 19960429 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 380-410 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 327SW 23691 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 380-410, BETWEEN S22 AND 23R, AND AT BS 862-886, FROM LBL 5 T O RBL 5. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996050200369 19960502 00369 NM 1996 5 2 SWAA960271 1 19960429 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 328 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 327SW 23691 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED FWD SERVICE DOOR CUTOUT AT LWR AFT CORNER, BS 328, RBL 66, WL 211. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996050200370 19960502 00370 NM 1996 5 2 SWAA960272 1 19960429 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 947.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 327SW 23691 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 947.5 PLUS 14 AND 18, BELOW S19L, WL 189, AND AT BS 1006, BET WEEN S21 AND 22L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996050200371 19960502 00371 NM 1996 5 2 SWAA960273 1 19960429 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 747 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED TERMINAL CHECK, FOUND FUSELAGE SKIN LAP CRACKED AT BS 747, AT S10R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996050200372 19960502 00372 NM 1996 5 2 SWAA960274 1 19960429 A 3350 1000679 LIGHT BOEING 737 7372H4 138448C NM AFT GALLEY INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 57SW 21722 DURING SCHEDULED C1 CHECK, FOUND AFT GALLEY EMERGENCY EXIT LIGHT ABOVE SERVICE DOOR INOP. REPLACED LIGHT ASSEMBLY PER B OEING M/M. 2 L 7 2 4F A16WE 1996050200373 19960502 00373 NM 1996 5 2 SWAA960275 1 19960429 A 3350 20131 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 330SW 23694 DURING SCHEDULED TERMINAL CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK AND CHARGER PER BOEIN G M/M. 2 L 7 2 4F RT A16WE 1996050200374 19960502 00374 NM 1996 5 2 9609456608 1 19960429 A 2752 ACTUATOR BOEING 747 747151 1384891 NM TE FLAPS FAILED A NWAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 01 608US 19785 DURING CLIMB, THE OUTBOARD FLAPS STOPPED AT TWO DEGREES ON RETRACTION. AIRCRAFT RETURNED TO NRT AND LANDED WITHOUT INCI DENT. REPLACED THE RIGHT OUTBOARD TRAILING EDGE FLAP ACTUATOR, NR 7 FLAP TRANSMISSION AND THE OUTBOARD FLAP TRACK FAIRI NG HINGE FITTING LINK. 2 L 7 4 4F A20WE 1996050200375 19960502 00375 WP 1996 5 2 9609469919 1 19960429 A 7711 PT7 LINE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D15 52051 NE NR 1 ENGINE BROKEN A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 941N 47450 657207 ON POWER REDUCTION AFTER TAKEOFF, THE NR 1 EPR INDICATION BECAME ERRATIC. THE AIRCRAFT RETURNED TO MSP AND LANDED WITHO UT INCIDENT. MAINTENANCE REPLACED A BROKEN PT7 LINE WITH A SERVICEABLE PART AND SYSTEM OPERATION RETURNED TO NORMAL. 2 L 7 2 4F 4 F A6WE E2EA 1996050200377 19960502 00377 WP 1996 5 2 9609489753 1 19960430 A 3260 BRACKET DOUG DC9 DC941 302207N WP RT MLG DOOR BENT A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 753NW 47117 DURING CLIMBOUT OF MSP, GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR RETRACTION. RETURNED TO MSP AND LANDED WITHOUT INCI DENT. AT RIGHT GEAR DOOR, FOUND BRACKET THAT STRIKER BOLT MOUNTS ON BENT, CAUSING THE SWITCH LEVER TO MISS THE STRIKER. REPLACED AND ADJUSTED THE BRACKET AND DOOR LIGHT OPERATIONAL CHECKED GOOD. 2 L 7 2 4F A6WE 1996050200378 19960502 00378 NM 1996 5 2 96UAL900267 1 19960417 A 2910 H61CO551 CHECK VALVE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE A-HYD SYST RUPTURED A UALA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 7272U 21419 HYDRAULIC 'A' SYSTEM PRESSURE AND QUANTITY LOSS JUST AFTER PUSH BACK FROM GATE AND SELECTING 'A' PUMPS ON. FOUND 'A' SY SYEM INBOARD CHECK VALVE LEAKING. REPLACED CHECK VALVE, SERVICED HYDRAULIC SYSTEM AND ACCOMPLISHED A LEAK CHECK. 2 L 7 3 4F 4 F A3WE E2EA 1996050200379 19960502 00379 NM 1996 5 2 96UAL900288 1 19960426 A 3350 BULB BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 605UA 21866 EMERGENCY LIGHT BEHIND LEFT WING IS INOPERABLE. REPLACED LAMP, OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 1996050200380 19960502 00380 WP 1996 5 2 96UAL900289 1 19960426 A 2170 COALESCER BAGS DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN DIRTY A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 1830U 46629 EARLY IN FLIGHT, LEFT SIDE OF AIRPLANE HAD LIGHT SMELL OF HOT INSULATION BY ROWS 14 TO 18. *S/D* MAINTENANCE SET CABIN LIGHTS TO FULL BRIGHT WITH NO SMELL NOTED. PACKS RAN, SMELL COULD NOT BE DUPLICATED. REPLACED COALESCER BAGS, NO REOC CURANCE. 2 L 7 3 4F 4 F A22WE E23EA 1996050200381 19960502 00381 NM 1996 5 2 96UAL900290 1 19960426 A 2421 B4301 IDG BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT ENGINE FAILED A UALA O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION NR NOT REPORTED 1 WP 29 643UA 25093 LOST RIGHT INTEGRATED DRIVE GENERATOR AND RECEIVED RIGHT EEC MESSAGE. RESET RIGHT EEC, BUT IT REMAINED IN ALTERNATE MOD E. *S/D* REPLACED RIGHT INTEGRATED DRIVE GENERATOR, GENERATOR CONTROL UNIT AND GENERATOR CONTROL BREAKER. IDG AND GC U WERE SHOP TESTED AND IN GOOD WORKING CONDITION. THE FAILURE MOST LIKELY RESULTED IN A GCB MALFUNCTION. 2 L 7 2 4F 4 F RT A1NM E24NE 1996050200382 19960502 00382 NM 1996 5 2 96UAL900291 1 19960426 A 5540 173N20011 HINGE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RUDDER DAMAGED A UALA K NONE O OTHER AP APPROACH 1 WP 29 516UA 24860 AIRCRAFT EXPERIENCED A SEVERE LIGHTNING STRIKE ON APPROACH TO EWR. *S/D* DUE TO LIGHTNING STRIKE, RUDDER AND IT' SUPPE R HINGE WAS DAMAGED. REMOVED AND REPLACED DAMAGED RUDDER, UPPER HINGE, UPPER FITTING AND ASSOCIATED HARDWARE. RIGGED R UDDER PER MAINTENANCE MANUAL, OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996050200383 19960502 00383 NM 1996 5 2 96UAL900292 1 19960426 A 2421 GENERATOR SUNSTRAND 757066D BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE BACKUP SYST FAILED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 773UA 169 26929 STATUS MESSAGE FLIGHT CONTROL SYS DISPLAYED, MAINTENANCE MESSAGE DISPLAYED WAS 24 502 01. REPLACED LEFT BACKUP GENERATO R. *S/D* BACKUP GENERATOR WAS DEFECTIVE AND BACKUP GENERATOR WAS REPLACED. 2 L 7 2 4F 4 F RT T0001SE E46NE 1996050200384 19960502 00384 NM 1996 5 2 96UAL900293 1 19960426 A 3240 BRAKE LINE BOEING 737 737522 138449F NM LT MLG FAILED A UALA K NONE K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 918UA 25385 HYDRAULIC BRAKE LINE TO LEFT HAND OUTBOARD BRAKE FAILED JUST UPSTREAM OF QUICK DISCONNECT. *S/D* REPLACED LEFT HAND OU TBOARD BRAKE LINE AND BLED SYSTEM, CHECKS OK. 2 L 7 2 4F RT A16WE 1996050200385 19960502 00385 NM 1996 5 2 96UAL900294 1 19960426 A 2782 DRIVE UNIT ALLIED SIGNA 12624841 BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE NR 1 LE FLAP FAILED A UALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 WP 29 159UA 30P1080 21140 NR 1 LEADING EDGE FLAP FAILED TO RETRACT. *S/D* DRIVE UNIT FAILED TO RETRACT PNEUMATICALLY OR ALTERNATELY AFTER TAKEOF F. DISASSEMBLY OF THE FAILED UNIT REVEALED A FAILED AIR ROTOR BEARING. ADDITIONALLY THE ALTERNATE DRIVE MOTOR FAILED, PROBABLY DUE TO EXTENDED OPERATION OF THE DRIVE UNIT AFTER THE PNEUMATIC MODE FAILURE. 2 L 7 4 4F 4 F A20WE E20EA 1996050200386 19960502 00386 NM 1996 5 2 96UAL900295 1 19960426 A 3350 POWER SUPPLY BOEING 737 737322 1384676 NM CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 379UA 24654 BULLNOSE EMERGENCY LIGHTS INOP ROWS 7DEF AND 9ABC. FOUND BATTERY CHARGER AND BATTERY POWER SUPPLY DEFECTIVE. REPLACED BATTERY CHARGER M1135 AND BATTERY POWER SUPPLY. 2 L 7 2 4F RT A16WE 1996050200387 19960502 00387 NM 1996 5 2 96UAL900296 1 19960429 A 2780 114W210011 RETRACT MECH BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 7 LE FLAP OUT OF ADJUST A UALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 29 769UA 26921 AFTER TAKEOFF, NOTICED LOUD SUSTAINED VIBRATION IN CABIN FROM LEADING EDGE OF WING AFT INTO MID CABIN AREA. ALSO, FELT IN FLOOR OF COCKPIT. VIBRATION REMAINS AT ALL POWER SETTINGS. AIRCRAFT RETURNED TO FIELD. *S/D* ADJUSTED NR 7 SLAT P ER AMM 27-81-00. 2 L 7 2 4F 4 F RT T0001SE E46NE 1996050200388 19960502 00388 1996 5 2 96UAL900297 4 19960429 A 2565 SLIDE BF GOODRICH 7A13492 BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE CREW COMPT LEAKING A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 4735U G005 19928 DURING ROUTINE OVERHAUL OF CREW SLIDE, UNIT FAILED AIR RETENTION TEST DUE TO SEAM LEAKS, POROSITY AND MINOR PUNCTURES. S CRAPPED UNIT. 2 L 7 4 4F 4 F A20WE E20EA 1996050200389 19960502 00389 NE 1996 5 2 96UAL900298 2 19960429 A 7530 AIR21596 BUSHING HAMILTON STA 802170 BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE SHAFT HOUSING FAILED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 659UA 920260 27114 ABORTED TAKEOFF AT 70 KNOTS DUE TO BLEED VALVE EICAS MESSAGE. *S/D* A FAILED NITRONIC BUSHING CAUSED THE BLEED VALVE E ICAS MESSAGE. THE LEFT HIGH PRESSURE SHUTOFF VALVE WAS REPLACED, OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 1996050200390 19960502 00390 NM 1996 5 2 96UAL900300 1 19960429 A 3610 802152 HPSOV BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT ENGINE FAILED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 29 650UA 25287 ABORTED TAKEOFF DUE TO RIGHT ENGINE HIGH STAGE BLEED LIGHT. *S/D* A FAILED NITRONIC BUSHING CAUSED THIS DISCREPANCY. T HE RIGHT HPSOV WAS DEACTIVATED IN THE CLOSED POSITION PER MEL 36-11. DURING THE NEXT FLIGHT THE RIGHT HPSOV WAS REPLACE D. OPERATIONS CHECK NORMAL AFTER ENGINE RUN. 2 L 7 2 4F 4 F RT A1NM E24NE 1996050200391 19960502 00391 NM 1996 5 2 96UAL900301 1 19960429 A 3230 65B8324843 HOSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE RT MLG CHAFED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 189UA 26878 UNABLE TO RETRACT GEAR. *S/D* UNABLE TO RETRACT GEAR DUE TO TILT INDICATION ON FLIGHT DECK. RIGHT BODY LANDING GEAR T RUCK NOT TILTED DUE TO LEAKING TRUCK TILT POSITIONER HOSE. HYDRAULIC FUSE SHUT OFF DUE TO LEAK. REPLACED HOSE. 2 L 7 4 4F 4 F RT A20WE E24NE 1996050200392 19960502 00392 NM 1996 5 2 96UAL900302 1 19960430 A 3350 LIGHT STRIP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 578UA 26694 EMERGENCY ESCAPE LIGHTING STRIP IN FRONT OF LAVATORY 108 INOP. REPLACED EMERGENCY ESCAPE LIGHTING STRIP AT LAVATORY 108 , OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996050200393 19960502 00393 WP 1996 5 2 ABXA9600486 1 19960429 A 7931 318100 TRANSMITTER DOUG DC8 DC861 3021952 WP PWA JT3D JT3D3B 52039 NE NR 4 ENGINE DEFECTIVE A ABXA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 GL 23 848AX 46032 669702 DURING CLIMB, NR 4 ENGINE OIL PRESSURE INCREASED TO 61 PSI MOMENTARILY AND THEN DROPPED TO 59 PSI WITH MAXIMUM POWER SET FOR TAKEOFF. REDUCED POWER TO MCT AND OIL PRESSURE DROPPED TO 53 PSI AND THEN BEGAN TO INCREASE. ENGINE WAS SHUTDOWN WHEN THE OIL PRESSURE INDICATED 64 PSI. ENGINE MAINTAINED POSITIVE OIL PRESSURE FOR REMAINDER OF FLIGHT. REPLACED THE NR 4 ENGINE OIL PRESSURE TRANSMITTER. GROUND RAN ENGINE AND ADJUSTED THE OIL PRESSURE. OIL PRESSURE INDICATION CHECKED GOOD AT TAKEOFF AND IDLE POWER SETTINGS IAW DC8 MM. 2 L 7 4 4F 4 F 4A25 1E8 1996050200394 19960502 00394 NM 1996 5 2 DHL96720001 1 19960427 A 3040 2312 CONTROLLER BOEING 727 727228 NM L1 WINDOW MALFUNCTIONED A T DHLA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 720DH 19544 L1 WINDOW HEAT AMBER OVERHEAT LIGHT ON ZERO DEGREES, RESET 14 MINUTES TO OVERHEAT AGAIN. FOUND A LOOSE SPARE SENSOR TER MINAL END. REPLACED SAME, CHECKED L1 WINDOW RESISTANCE AND TAP SETTING. VOLTAGE WAS WITHIN LIMITS. REPLACED HEAT CONT ROLLER FOR PRECAUTION. 2 L 7 3 4F A3WE 1996050200395 19960502 00395 WP 1996 5 2 MWEA96124 1 19960428 A 5330 SKIN DOUG DC9 DC914 3022034 WP BS 859 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 DURING C-CHECK, FOUND CRACK IN FUSELAGE SKIN, .50 INCH AT STA 859 ABOVE LT PYLON. INSTALLED DOUBLER REPAIR IAW SRM 53-0 1, FIG. 2. 2 L 7 2 4F A6WE 1996050200397 19960502 00397 WP 1996 5 2 96ZZZM700 1 19960326 A 2170 1808492 COALESCERS DOUG DC9 DC982 3022082 WP CABIN DIRTY A ASAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 01 938AS 49365 LAS - FLT NR 624 - CREW REPORTED AN ELECTRICAL OR HOT PLASTIC ODOR IN THE CABIN DURING DESCENT AND LANDING. INSPECTION OF ALL LAVATORY WASTE CONTAINERS, OVENS, BUN WARMERS AND COFFEE MAKERS REVEALED NO PLASTIC RESIDUE OR OVERHEAT CONDITION , ODOR HAS DISSIPATED. HOWEVER, DURING BOARDING OF OUTBOUND FLIGHT 651, THE ODOR RETURNED WITH THE AIR CONDITIONING PAC KS OPERATING. FOUND THE LEFT THRUST REVERSER RETURN LINE LEAKING SKYDROL. TIGHTENED THE 'B' NUT AND SYSTEM LEAK CHECKE D GOOD. CLEANED TAIL COMPARTMENT AREA, PERFORMED HIGH PRESSURE BURNOUT OF HIGH PRESSURE DUCTING AND REPLACED BOTH COALE SCERS. SYSTEM OPERATED NORMALLY WITH NO ODORS DETECTED. REFERENCE ASAA9680080. 2 L 7 2 4F A6WE 1996050200398 19960502 00398 NM 1996 5 2 96ZZZM701 1 19960216 A 5330 SKIN BOEING 737 7372H5 138448E NM BS 986.5-1016 DISBOND A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION BY ULTRASONIC, FOUND FUSELAGE SKIN AND DOUBLER DISBOND, 13 INCH BY 13 INCH LOCATED AT STATION 986.5 TO STATION 1016 AND STRINGER 12R TO STRINGER 13R. INSTALLED FIELD RIVETS AS PER BOEING SRM 53-30-3 FIG 17 DETAIL I. (M) 2 L 7 2 4F A16WE 1996050200399 19960502 00399 NM 1996 5 2 96ZZZM702 1 19960216 A 5330 SKIN BOEING 737 7372H5 138448E NM BS 954 DISBOND A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION VISUALLY FOUND 6 INCH DISBONDED FUSELAGE SKIN LOCATED AT STATION 954 BETWEEN STRINGER 24 AND STRINGER 2 3 RT. REPLACED SKIN AS PER USAIR EA NR 58009 AND JOB CARD JZ-57-53500 C-1. (M) 2 L 7 2 4F A16WE 1996050200400 19960502 00400 NM 1996 5 2 96ZZZM703 1 19960216 A 5320 STR SPLICE BOEING 737 7372H5 138448E NM BS 908 CORROSION A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION VISUALLY FOUND A LEVEL I CORRODED PRODUCTION STRINGER SPLICE 6 INCHES AT THE FUSELAGE SKIN LOCATED AT S TATION 908 AND STRINGER 20R. REPLACED AND REPAIR STRINGER PRODUCTION SPLICE AS PER BOEING SRM 51-00-00. (M) 2 L 7 2 4F A16WE 1996050200401 19960502 00401 NM 1996 5 2 96ZZZM704 1 19960216 A 5532 SKIN BOEING 737 7372H5 138448E NM VERT STAB DAMAGED A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION VISUALLY FOUND MISSING TRAILING EDGE HONEYCOMB CORE MATERIAL LOCATED AT THE VERTICAL STAB AT RUDDER STA TION 218 RIGHT TRAILING EDGE PANEL. COMPOSITE REPAIRED AS PER BOEING SRM 51-40-13. (M) 2 L 7 2 4F A16WE 1996050200402 19960502 00402 NM 1996 5 2 96ZZZM705 1 19960216 A 5330 SKIN BOEING 737 7372H5 138448E NM BS 927-947 DISBOND A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION BY ULTRASONIC FOUND DISBONDED SKIN AND DOUBLER AT THE FUSELAGE SKIN LOCATED AT STATION 927 TO 947 AND S TRINGER 21R TO STRINGER 20R. REMOVED AND REPLACED SKIN DOUBLER AS PER BOEING SRM 53-30-3 FIG 17. (M) 2 L 7 2 4F A16WE 1996050200403 19960502 00403 NM 1996 5 2 96ZZZM706 1 19960216 A 5330 SKIN BOEING 737 7372H5 138448E NM FS 360 GOUGED A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION VISUALLY FOUND A 1.5 INCH GOUGE .019 DEEP AT FUSELAGE SKIN LOCATED AT FS 360 1 INCH ABOVE STRINGER 18L. INSTALLED DOUBLER AS PER BOEING SRM 53-30-3 FIG 28. (M) 2 L 7 2 4F A16WE 1996050200404 19960502 00404 NM 1996 5 2 96ZZZM707 1 19960216 A 5320 SUPPORT BEAM BOEING 737 7372H5 138448E NM BS 1014 CORROSION A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION VISUALLY FOUND LEVEL I CORROSION AT THE FUSELAGE FLOOR SUPPORT BEAM LOCATED AT LBL 2 TO LBL 6 AND STATI ON 1014. FABRICATED REPLACEMENT H-CHANNEL AND ATTACH ANGLE AS PER BOEING SRM 51-00-02. (M) 2 L 7 2 4F A16WE 1996050200405 19960502 00405 NM 1996 5 2 96ZZZM708 1 19960216 A 5330 SKIN BOEING 737 7372H5 138448E NM FS 1137 CRACKED A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION VISUALLY FOUND AND VERIFIED WITH HFEC A 1.25 INCH CRACK LOCATED AT FUSELAGE SKIN, FS 1137 AND STRINGER 12L. INSTALLED DOUBLER AS PER BOEING SRM 53-30-3 FIG 30. (M) 2 L 7 2 4F A16WE 1996050200406 19960502 00406 NM 1996 5 2 96ZZZM709 1 19960216 A 5330 SKIN BOEING 737 7372H5 138448E NM BS 902-915 DISBONDED A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION BY ULTRASONIC FOUND SKIN AND DOUBLER DISBOND LOCATED AT FUSELAGE SKIN MEASURING 14 INCHES BY 2.5 INCHES AT STATION 902 TO 914 AND STRINGER 13R TO STRINGER 14R. INSTALLED FIELD RIVETS AS PER BOEING SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1996050200407 19960502 00407 NM 1996 5 2 96ZZZM710 1 19960216 A 5330 SKIN BOEING 737 7372H5 138448E NM BS 356 DISBOND A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION BY ULTRASONIC, FOUND SKIN AND DOUBLER DISBOND LOCATED AT FUSELAGE SKIN MEASURING 5 INCHES BY 4 INCHES A T STATION 356, S15L AND 16L. INSTALLED FIELD FASTENERS AS PER BOEING SRM 53-30-3 DETAIL I AND TABLE III FIG 17. (M) 2 L 7 2 4F A16WE 1996050200408 19960502 00408 NM 1996 5 2 96ZZZM711 1 19960216 A 5330 SKIN BOEING 737 7372H5 138448E NM BS 967 DISBOND A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION BY ULTRASONIC FOUND SKIN AND DOUBLER DISBOND LOCATED AT FUSELAGE SKIN MEASURING 3 INCHES BY 4 INCHES AT STATION 967 ABOVE STRINGER 5L. INSTALLED FIELD RIVETS AS PER SRM 53-30-3 FIG 17. (M) 2 L 7 2 4F A16WE 1996050200409 19960502 00409 NM 1996 5 2 96ZZZM712 1 19960216 A 5330 SKIN BOEING 737 7372H5 138448E NM BS 920-927 DISBOND A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION BY ULTRASONIC FOUND DISBONDED SKIN AND DOUBLER AT THE FUSELAGE SKIN MEASURING 5 INCHES BY 18 INCHES LOC ATED AT STATION 920 TO 927 AND STRINGER 9R TO STRINGER 10R. INSTALLED FIELD RIVETS AS PER BOEING SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1996050200410 19960502 00410 NM 1996 5 2 96ZZZM713 1 19960216 A 5330 SKIN BOEING 737 7372H5 138448E NM BS 288 DISBONDED A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION BY ULTRASONIC FOUND DISBONDED SKIN AND DOUBLER MEASURING 9 INCHES BY 5 INCHES LOCATED AT THE FUSELAGE S KIN AT STATION 288, STRINGER 14L AND STRINGER 15L. INSTALLED FIELD DOUBLERS AS PER BOEING SRM 53-30-3 DETAIL 1 FIG 17. (M) 2 L 7 2 4F A16WE 1996050200411 19960502 00411 NM 1996 5 2 96ZZZM714 1 19960216 A 5330 SKIN BOEING 737 7372H5 138448E NM BS 251 CRACKED A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION VISUALLY FOUND A CRACK THROUGH RIVET .1875 INCH UP AND .125 INCH DOWN LOCATED AT FUSELAGE SKIN AT STATI ON 251 AND STRINGER 11L. INSTALLED DOUBLER AS PER BOEING SRM 53-30-03 AND USAIR EO NR 22870. (M) 2 L 7 2 4F A16WE 1996050200412 19960502 00412 NM 1996 5 2 96ZZZM715 1 19960216 A 5330 SKIN BOEING 737 7372H5 138448E NM BS 927-947 DISBONDED A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION BY ULTRASONIC, FOUND SKIN AND DOUBLER DISBOND MEASURING 12 INCHES BY 2.5 INCHES LOCATED FUSELAGE SKIN A T STATION 927-947 AND STRINGER 14L. INSTALLED FIELD FASTENERS AS EPR SRM 53-30-3 FIG 17, DETAIL 1. (M) 2 L 7 2 4F A16WE 1996050200413 19960502 00413 NM 1996 5 2 96ZZZM716 1 19960216 A 5330 SKIN BOEING 737 7372H5 138448E NM BS 986.5-1016 DISBOND A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION BY ULTRASONIC, FOUND FUSELAGE SKIN AND DOUBLER DISBOND, 13 INCHES BY 13 INCHES LOCATED AT STATION 986.5 TO 1016 AND STRINGER 12R TO STRINGER 13R. INSTALLED FIELD RIVETS AS PER BOEING SRM 53-30-3 FIG 17 DETAIL I. (M) 2 L 7 2 4F A16WE 1996050200414 19960502 00414 NM 1996 5 2 96ZZZM717 1 19960216 A 5330 SKIN BOEING 737 7372H5 138448E NM BS 986.5-1016 DISBOND A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION BY ULTRASONIC, FOUND FUSELAGE SKIN AND DOUBLER DISBOND 7 INCHES BY 2 INCHES LOCATED AT STATION 986.5 TO 1016, STRINGER 9R TO STRINGER 10R. INSTALLED FIELD FASTENERS AS PER BOEING SRM 53-30-3, DETAIL I, FIG 17. (M) 2 L 7 2 4F A16WE 1996050200415 19960502 00415 NM 1996 5 2 96ZZZM718 1 19960216 A 5330 SKIN BOEING 737 7372H5 138448E NM BS 635 DISBOND A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION BY ULTRASONIC FOUND FUSELAGE SKIN AND DOUBLER DISBOND LOCATED AT STATION 635, STRINGER 8R AND STRINGER 9R. INSTALLED FIELD RIVETS AS PER BOEING SRM 53-30-3, FIG 17. (M) 2 L 7 2 4F A16WE 1996050200416 19960502 00416 NM 1996 5 2 96ZZZM719 1 19960216 A 5330 SKIN BOEING 737 7372H5 138448E NM BS 312-344 DISBOND A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION BY ULTRASONIC, FOUND TWO AREAS OF DISBOND, 14 INCHES BY 8 INCHES AND 4 INCHES BY 8 INCHES LOCATED AT TH E FUSELAGE SKIN AT STATION 312-344 AND STRINGER 5R AND STRINGER 6R. INSTALLED FIELD FASTENERS AS PER BOEING SRM 53-30-3 FIG 17, DETAILS I AND II. (M) 2 L 7 2 4F A16WE 1996050200417 19960502 00417 NM 1996 5 2 96ZZZM720 1 19960216 A 5330 SKIN BOEING 737 7372H5 138448E NM BS 9270947 DISBOND A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION BY ULTRASONIC, FOUND FUSELAGE SKIN AND DOUBLER DISBOND LOCATED AT STATION 927 TO 947, STRINGER 9L AND S TRINGER 10L. INSTALLED FIELD DOUBLERS AS PER BOEING SRM 53-30-3 FIG 17. (M) 2 L 7 2 4F A16WE 1996050200418 19960502 00418 NM 1996 5 2 96ZZZM721 1 19960216 A 5330 SKIN BOEING 737 7372H5 138448E NM BS 277/294.5 DISBOND A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION BY ULTRASONIC, FOUND TWO 6 INCH BY 6 INCH AND 8 INCH BY 2 INCH AREAS OF SKIN AND DOUBLER DISBOND LOCATE D AT THE FUSELAGE SKIN BETWEEN STATION 277 AND 294.5, STRINGER 5R AND STRINGER 8R. INSTALLED FIELD FASTENERS AS PER BOE ING SRM 53-30-3 FIG 17. (M) 2 L 7 2 4F A16WE 1996050200419 19960502 00419 NM 1996 5 2 96ZZZM722 1 19960216 A 5320 ANGLE BOEING 737 7372H5 138448E NM FS 1085 CRACKED A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION VISUALLY FOUND A 1.5 INCH CRACK LOCATED AT THE FUSELAGE RADIUS OF ANGLE AT FS 1085 AND STRINGER 2L. IN STALLED AND MANUFACTURED ANGLE AS PER BOEING SRM 20-30-06. (M) 2 L 7 2 4F A16WE 1996050200420 19960502 00420 NM 1996 5 2 96ZZZM723 1 19960216 A 5320 CHORD BOEING 737 7372H5 138448E NM BS 727 CRACKED A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58129 20454 CLT - INSPECTION FOUND BY ULTRASONIC AND EDDY CURRENT, A CRACK APPROXIMATELY 1 INCH, LOCATED AT THE FUSELAGE CHORD, RHS BS 727, OUTBOARD AT STRINGER 18A. CHORD SECTION REPLACED AS PER EO 5394G068, EO 5394G6075 AND SB 737-53-1088. (M) 2 L 7 2 4F A16WE 1996050200421 19960502 00421 NM 1996 5 2 96ZZZM724 1 19960216 A 5532 VERTICAL FIN BOEING 737 7372H5 138448E NM FIN STA 209.90 DENTED A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 20454 CLT - INSPECTION VISUALLY FOUND A DENT LOCATED AT VERTICAL STABILIZER MEASURING 1 INCH BY 2.5 INCH AT FIN STATION 209.90 , RIGHT INSPAR. CUT OUT DAMAGE, INSTALLED DOUBLER AS PER USAIR EA NR 40708. (M) 2 L 7 2 4F A16WE 1996050200422 19960502 00422 NM 1996 5 2 96ZZZM725 1 19960216 A 5320 CHORD BOEING 737 7372H5 138448E NM BS 727 CRACKED A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58129 20454 CLT - INSPECTION FOUND BY ULTRASONIC AND EDDY CURRENT A CRACK APPROXIMATELY 1 INCH LOCATED AT THE FUSELAGE CHORD, RHS BS 727, OUTBOARD CHORD AT STRINGER 18A. CHORD SECTION REPLACED AS PER EO 5394G068, EO 5394G6075 AND SB 737-53-1088. (M) 2 L 7 2 4F A16WE 1996050200423 19960502 00423 NM 1996 5 2 96ZZZM726 1 19960216 A 5330 SKIN BOEING 737 7372H5 138448E NM BS 986.5-1016 DISBONDED A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION BY ULTRASONIC FOUND FUSELAGE SKIN AND DOUBLER DISBOND 7 INCH BY 2 INCH LOCATED AT STATION 986.5 TO 1016 , STRINGER 9R TO STRINGER 10R. INSTALLED FIELD FASTENERS AS PER BOEING SRM 53-30-3, DETAIL I, FIG 17. (M) 2 L 7 2 4F A16WE 1996050200424 19960502 00424 NM 1996 5 2 96ZZZM727 1 19960216 A 5330 SKIN BOEING 737 7372H5 138448E NM BS 635 DISBONDED A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION BY ULTRASONIC FOUND FUSELAGE SKIN AND DOUBLER DISBOND LOCATED AT STATION 635, STRINGER 8R AND STRINGER 9R. INSTALLED FIELD RIVETS AS PER BOEING SRM 53-30-3, FIG 17. (M) 2 L 7 2 4F A16WE 1996050200425 19960502 00425 NM 1996 5 2 96ZZZM728 1 19960216 A 5330 SKIN BOEING 737 7372H5 138448E NM BS 312-344 DISBOND A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION BY ULTRASONIC, FOUND TWO AREAS OF DISBOND, 14 INCHES BY 8 INCHES AND 4 INCHES BY 8 INCHES LOCATED AT TH E FUSELAGE SKIN AT STATION 312-344 AND STRINGER 5R AND STRINGER 6R. INSTALLED FIELD FASTENERS AS PER BOEING SRM 53-30-3 FIG 17 DETAILES I AND II. (M) 2 L 7 2 4F A16WE 1996050200426 19960502 00426 NM 1996 5 2 96ZZZM729 1 19960216 A 5330 SKIN BOEING 737 7372H5 138448E NM BS 927-947 DISBONDED A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION BY ULTRASONIC, FOUND FUSELAGE SKIN AND DOUBLER DISBOND LOCATED AT STATION 927 TO 947, STRINGER 9L AND S TRINGER 10L. INSTALLED FIELD DOUBLERS AS PER BOEING SRM 53-30-3 FIG 17. (M) 2 L 7 2 4F A16WE 1996050200427 19960502 00427 NM 1996 5 2 96ZZZM730 1 19960216 A 5330 SKIN BOEING 737 7372H5 138448E NM BS 277/294.5 DISBOND A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION BY ULTRASONIC, FOUND TWO 6 INCHES BY 6 INCHES AND 8 INCHES BY 2 INCHES AREAS OF SKIN AND DOUBLER DISBON D LOCATED AT THE FUSELAGE SKIN BETWEEN STATION 277 AND 294.5, STRINGER 5R AND STRINGER 8R. INSTALLED FIELD FASTENERS AS PER BOEING SRM 53-30-3 FIG 17. (M) 2 L 7 2 4F A16WE 1996050200428 19960502 00428 NM 1996 5 2 96ZZZM731 1 19960216 A 5320 ANGLE BOEING 737 7372H5 138448E NM FS 1085 CRACKED A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION VISUALLY FOUND A 1.5 INCH CRACK LOCATED AT THE FUSELAGE RADIUS OF ANGLE AT FS 1085 AND STRINGER 2L. IN STALLED AND MANUFACTURED ANGLE AS PER BOEING SRM 20-30-06. (M) 2 L 7 2 4F A16WE 1996050200429 19960502 00429 NM 1996 5 2 96ZZZM732 1 19960216 A 5330 SKIN BOEING 737 7372H5 138448E NM BS 954 DISBONDED A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION VISUALLY FOUND 6 INCH DISBONDED FUSELAGE SKIN LOCATED AT STATION 954 BETWEEN STRINGER 24 AND STRINGER 2 3R. REPLACED SKIN AS PER USAIR EA NR 58009 AND JOB CARD JZ-57-53500 C-1. (M) 2 L 7 2 4F A16WE 1996050200430 19960502 00430 NM 1996 5 2 96ZZZM733 1 19960216 A 5330 SKIN BOEING 737 7372H5 138448E NM BS 908 CORROSION A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION VISUALLY FOUND A LEVEL I CORRODED PRODUCTION STRINGER SPLICE 6 INCHES AT THE FUSELAGE SKIN LOCATED AT S TATION 908 AND STRINGER 20R. REPLACED AND REPAIR STRINGER PRODUCTION SPLICE AS PER BOEING SRM 51-00-00. (M) 2 L 7 2 4F A16WE 1996050200431 19960502 00431 NM 1996 5 2 96ZZZM734 1 19960216 A 5330 SKIN BOEING 737 7372H5 138448E NM BS 927-947 DISBOND A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION BY ULTRASONIC FOUND DISBONDED SKIN AND DOUBLER AT THE FUSELAGE SKIN LOCATED AT STATION 927 TO 947 AND S TRINGER 21R TO STRINGER 20R. REMOVED AND REPLACED SKIN DOUBLER AS PER BOEING SRM 53-30-3 FIG 17. (M) 2 L 7 2 4F A16WE 1996050200432 19960502 00432 NM 1996 5 2 96ZZZM735 1 19960216 A 5330 SKIN BOEING 737 7372H5 138448E NM FS 360 GOUGED A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION VISUALLY FOUND A 1.5 INCH GOUGE .019 DEEP AT FUSELAGE SKIN LOCATED AT FS 360 1 INCH ABOVE STRINGER 18L. INSTALLED DOUBLER AS PER BOEING SRM 53-30-3, FIG 28. (M) 2 L 7 2 4F A16WE 1996050200433 19960502 00433 NM 1996 5 2 96ZZZM736 1 19960216 A 5320 SUPPORT BEAM BOEING 737 7372H5 138448E NM BS 1014 CORROSION A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION VISUALLY FOUND LEVEL I CORROSION AT THE FUSELAGE FLOOR SUPPORT BEAM LOCATED AT LBL 2 TO LBL 6 AND STATI ON 1014. FABRICATED REPLACEMENT H-CHANNEL AND ATTACH ANGLE AS PER BOEING SRM 51-00-02. (M) 2 L 7 2 4F A16WE 1996050200434 19960502 00434 NM 1996 5 2 96ZZZM737 1 19960216 A 5330 SKIN BOEING 737 7372H5 138448E NM FS 1137 CRACKED A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION VISUALLY FOUND AND VERIFIED WITH HFEC A 1.25 INCH CRACK LOCATED AT FUSELAGE SKIN FS 1137 AND STRINGER 1 2L. INSTALLED DOUBLER AS PER BOEING SRM 53-30-3 FIG 30. (M) 2 L 7 2 4F A16WE 1996050200435 19960502 00435 NM 1996 5 2 96ZZZM738 1 19960216 A 5330 SKIN BOEING 737 7372H5 138448E NM BS 902-915 DISBOND A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION BY ULTRASONIC, FOUND SKIN AND DOUBLER DISBOND LOCATED AT FUSELAGE SKIN MEASURING 14 INCHES BY 2.5 INCHE S AT STATION 902 TO 914 AND STRINGER 13R TO STRINGER 14R. INSTALLED FIELD RIVETS AS PER BOEING SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1996050200436 19960502 00436 NM 1996 5 2 96ZZZM739 1 19960216 A 5330 SKIN BOEING 737 7372H5 138448E NM BS 356 DISBOND A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 221US 58141 20454 CLT - INSPECTION BY ULTRASONIC, FOUND SKIN AND DOUBLER DISBOND LOCATED AT FUSELAGE SKIN MEASURING 5 INCHES BY 4 INCHES A T STATION 356, STRINGER 15L AND 16L. INSTALLED FIELD FASTENERS AS PER BOEING SRM 53-30-3 DETAIL I AND TABLE III FIG 17. (M) 2 L 7 2 4F A16WE 1996050200437 19960502 00437 NM 1996 5 2 96ZZZM740 1 19960216 A 5330 SKIN BOEING 737 7372H5 138448E NM BS 967 DISBOND A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION BY ULTRASONIC, FOUND SKIN AND DOUBLER DISBOND LOCATED AT FUSELAGE SKIN MEASURING 3 INCHES BY 4 INCHES A T STATION 967 ABOVE STRINGER 5L. INSTALLED FIELD RIVETS AS PER SRM 53-30-3 FIG 17. (M) 2 L 7 2 4F A16WE 1996050200438 19960502 00438 NM 1996 5 2 96ZZZM741 1 19960216 A 5330 SKIN BOEING 737 7372H5 138448E NM BS 920-927 DISBOND A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION BY ULTRASONIC, FOUND DISBONDED SKIN AND DOUBLER AT THE FUSELAGE SKIN MEASURING 5 INCHES BY 18 INCHES LO CATED AT STATION 920 TO 927 AND STRINGER 9R TO STRINGER 10R. INSTALLED FIELD RIVETS AS PER BOEING SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1996050200439 19960502 00439 NM 1996 5 2 96ZZZM742 1 19960216 A 5330 SKIN BOEING 737 7372H5 138448E NM BS 288 DISBOND A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION BY ULTRASONIC, FOUND DISBONDED SKIN AND DOUBLER MEASURING 9 INCHES BY 5 INCHES LOCATED AT THE FUSELAGE SKIN AT STATION 288, STRINGER 14L AND STRINGER 15L. INSTALLED FIELD DOUBLERS AS PER BOEING SRM 53-30-3 DETAIL 1 FIG 17. (M) 2 L 7 2 4F A16WE 1996050200440 19960502 00440 NM 1996 5 2 96ZZZM743 1 19960216 A 5330 SKIN BOEING 737 7372H5 138448E NM BS 251 CRACKED A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION VISUALLY FOUND A CRACK THROUGH RIVET .1875 INCH UP AND .125 INCH DOWN LOCATED AT FUSELAGE SKIN AT STATI ON 251 AND STRINGER 11L. INSTALLED DOUBLER AS PER BOEING SRM 53-30-03 AND USAIR EO NR 22870. (M) 2 L 7 2 4F A16WE 1996050200441 19960502 00441 NM 1996 5 2 96ZZZM744 1 19960216 A 5330 SKIN BOEING 737 7372H5 138448E NM BS 927-947 DISBOND A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION BY ULTRASONIC, FOUND SKIN AND DOUBLER DISBOND MEASURING 12 INCHES BY 2.5 INCHES LOCATED FUSELAGE SKIN A T STATION 927-947 AND STRINGER 14L. INSTALLED FIELD FASTENERS AS PER SRM 53-30-3 FIG 17 DETAIL 1. (M) 2 L 7 2 4F A16WE 1996050200442 19960502 00442 NE 1996 5 2 96ZZZM745 2 19960314 A 7250 TURBINE BLADES BOEING 707 707330C 138367G NM PWA JT3D JT3D3B 52039 NE NR 1 ENG DAMAGED A CLCA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 SO 19 707HE 20124 FLT 047 - KMIA-KMIA - DURING FLIGHT, NR 1 ENGINE ENCOUNTERED A SERIES OF MILD COMPRESSOR STALLS. EPR DROPPED TO '0', N1 WAS SET AT 106.0. VISUAL INSPECTION REVEALED TURBINE BLADE DAMAGE. REMOVED ENGINE ASSEMBLY AND INSTALLED SERVICEABLE ENGINE ASSEMBLY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 4 4F 4 F 4A26 1E8 1996050200446 19960502 00446 NE 1996 5 2 96ZZZM749 2 19960316 A 7321 77390010 FUEL CONTROL BAG BAE146 BAE146300A 1500267 EU LYC ALF502 ALF502R5 41580 NE NR 4 ENGINE FAILED A A6WA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 GL 31 616AW E3145 EN ROUTE TO ORD ON FLT 572 AT CRUISE POWER, NR 4 ENGINE DECELERATED BY ITSELF AND FLAMED OUT. ORD MAINTENANCE FOUND FCU SHAFT SHEARED. REPLACED FCU. (M) 2 H 7 4 4F 4 F RT A49EU E6NE 1996050200449 19960502 00449 EU 1996 5 2 96ZZZM752 1 19960103 A 5753 SEAL RETAINER BAG BAE146 BAE146100A 1500260 EU RT TE FLAPS BROKEN A A6WA O OTHER E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 GL 31 463AP E1063 AT 295 KTS, THERE IS A NOTICEABLE AIRFRAME VIBRATION FROM LEFT SIDE OF AIRCRAFT AT ROW 10. VIBRATION REDUCES AS SPEED D ECREASES AND GOES AWAY BELOW 265 KTS. FOUND RT FLAP SEAL RETAINER BROKEN, REPLACED. FOUND SEAL LOOSE ON PANELS 281CT A ND 282CT. SECURED SEALS. 2 H 7 4 4F RT A49EU 1996050200450 19960502 00450 EU 1996 5 2 96ZZZM753 1 19960102 A 3230 RETRACT MECH BAG BAE146 BAE146100A 1500260 EU LT MLG ICED UP A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 246SS E1003 AFTER TAKEOFF LEFT MLG INTRANSIT LIGHT REMAINED ON, RESELECTED TO DOWN, GREEN LIGHT CAME ON IMMEDIATELY. WE TAXIED IN S LUSH. SUBMITTER STATES, SUSPECT ICE ON GEAR. INSPECTED LEFT MLG AND BAY FOR DEFECTS, NONE NOTED. WIRE BUNDLES AND UPL OCKS OK. FOUND ICE AND SLUSH ON LOCK LINK AND OLEO LOCK JACK ASSY. DE-ICED GEAR OK FOR SERVICE. (M) 2 H 7 4 4F RT A49EU 1996050200452 19960502 00452 EU 1996 5 2 96ZZZM755 1 19960331 A 2750 RETRACT MECH BAG BAE146 BAE146300A 1500267 EU TE FLAPS MALFUNCTIONED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 615AW E3141 ON CLIMB-OUT FROM DEN WHEN FLAPS SELECTED FROM 18-0, FLAP FAULT AND INOP LIGHTS ILLUMINATED, FLAPS STUCK AT 18 DEGREES, AIR RETURN. CLEARED FLAP FAULT, RAN FLAPS NORMALLY. (M) 2 H 7 4 4F RT A49EU 1996050200453 19960502 00453 NE 1996 5 2 96ZZZM756 2 19960311 A 7200 ENGINE BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE NR 1 FAILED A A6WA E ENGINE SHUTDOWN J E WARNING INDICATION VIBRATION/BUFFET CR CRUISE 1 GL 31 607AW E2052 NR 1 ENGINE VIB INDICATION WENT TO 2.4 FOLLOW BY ERRATIC TGT READING, SHUTDOWN PER ABNORMAL CHECKLIST. REMOVED AND REPL ACED NR 1 ENGINE IAW MM. GROUND RAN AND LEAK CHECK OK. (M) 2 H 7 4 4F 4 F RT A49EU E6NE 1996050200454 19960502 00454 EU 1996 5 2 96ZZZM757 1 19960203 A 3297 WIRE HARNESS BAG BAE146 BAE146300A 1500267 EU LT MLG DOOR FAILED A A6WA O OTHER N FALSE WARNING CL CLIMB 1 GL 31 611AW E3120 UPON GEAR RETRACTION LEFT MAIN GEAR SHOWS RED UNSAFE WITH GEAR HANDLE LT ON. REMOVED AND REPLACED LEFT MLG DOOR UPLOCK SENSOR HARNESS. 2 H 7 4 4F RT A49EU 1996050200455 19960502 00455 EU 1996 5 2 96ZZZM758 1 19960203 A 3260 HARNESS BAG BAE146 BAE146300A 1500267 EU RT MLG FAILED A A6WA O OTHER O OTHER CL CLIMB 1 GL 31 614AW E3132 LANDING GEAR HANDLE REQ OVERRIDE ON GEAR RETRACTION AFTER TAKEOFF FROM ORD. REMOVED AND REPLACED RIGHT MLG WEIGHT OFF H ARNESS ASSY. 2 H 7 4 4F RT A49EU 1996050200456 19960502 00456 EU 1996 5 2 96ZZZM759 1 19960404 A 3350 CONTACTS BAG BAE146 BAE146200A 1500266 EU CABIN DIRTY A A6WA K NONE L NO TEST IN INSP/MAINT 1 GL 31 606AW E2033 EMERGENCY LIGHT ABOVE FWD PAX DOOR INOP, ON TEST. CLEANED CONTACTS ON LIGHT ASSY. 2 H 7 4 4F RT A49EU 1996050200457 19960502 00457 WP 1996 5 2 96ZZZM760 1 19960405 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 964AS 53078 SEA - DURING MAINTENANCE CHECK, AFT SECTION OF EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPAIRED SECTI ON OF WIRING AND REPLACED BATTERIES IN POWER PACK. LIGHTS OPERATED NORMALLY. REFERENCE ASAA9680090. 2 L 7 2 4F RT A6WE 1996050200458 19960502 00458 NM 1996 5 2 96ZZZM761 1 19960305 A 7120 8DK1763001 STRUT DHAV DHC8 DHC8102 2809003 NM RIGHT BROKEN A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 808EX A43174 299 PROPELLER VIBRATION FELT IN BETA, 950, AND 1050 RPM. INSPECTED AND FOUND LEFT AND RIGHT REAR ENGINE MOUNTS STRUTS BROKE N. REMOVED AND REPLACED ALL ENGINE MOUNTS AND PERFORMED PROPELLER BALANCE. AIRCRAFT RETURNED TO SERVICE. REFERENCE PC AA9600275. 2 H 7 2 4T RT A13NM 1996050200459 19960502 00459 EU 1996 5 2 96ZZZM762 1 19960325 A 2730 7227705643 CABLES SAAB SF340 340B 7860101 EU ELEVATOR CHAFED A PLGA K NONE O OTHER IN INSP/MAINT 1 NE 05 347BE 340B187 PSM - DURING ROUTINE C-CHECK INSPECTION, RIGHT INBOARD AND OUTBOARD ELEVATOR CONTROL CABLES WERE FOUND CHAFED AT SEVERAL GUIDES. BOTH CONTROL CABLES WERE REPLACED AND RIGGED IAW SAAB AMM CHAP 27. REFERENCE PLG32596DG1. 2 L 7 2 4T RT A52EU 1996050200460 19960502 00460 EU 1996 5 2 96ZZZM763 1 19960325 A 2730 7227105643 CONTROL CABLE SAAB SF340 340B 7860101 EU ELEVATOR CHAFED A PLGA K NONE O OTHER IN INSP/MAINT 1 NE 05 347BE 340B187 DURING ROUTINE C-CHECK INSPECTION, LEFT INBOARD AND OUTBOARD ELEVATOR CONTROL CABLES WERE FOUND CHAFED AT SEVERAL GUIDES . BOTH CONTROL CABLES WERE REPLACED AND RIGGED IAW SAAB AMM CHAPTER 27. REFERENCE PLG32596DG8. 2 L 7 2 4T RT A52EU 1996050200461 19960502 00461 NM 1996 5 2 ASAA9610043 1 19960319 A 3230 6554791 SAFETY SENSOR BOEING 737 737290C 138448V NM LANDING GEAR OUT OF ADJUST A ASAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 01 742AS 23136 SEA - ATB OF FLT 9301 - ALL THREE LANDING GEARS FAILED TO RETRACT AFTER TAKEOFF, GEAR HANDLE ONLY WENT TO 'OFF' POSITION . LANDED WITHOUT INCIDENT. ADJUSTED AIR SAFETY SENSOR GAP, COMPLETED GEAR SWING AND GEAR OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1996050200462 19960502 00462 NM 1996 5 2 ASAA9610044 1 19960328 A 3350 8821004 BATTERY PACK BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROW 18. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1996050200463 19960502 00463 NM 1996 5 2 ASAA9610045 1 19960328 A 3350 8821004 BATTERY PACK BOEING 737 737210C 1384459 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 744AS 21822 SEA - DURING RECON, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT PALLET 1-5. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1996050200464 19960502 00464 NM 1996 5 2 ASAA9610046 1 19960407 A 3350 8821004 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROW 8. REPLACED B ATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996050200465 19960502 00465 NM 1996 5 2 ASAA9640021 1 19960319 A 3350 0816901 SOCKET BOEING 737 7374Q8 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 771AS 25104 SEA - DURING MAINTENANCE CHECK, THE AFT EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED LIG HT SOCKET/WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996050200466 19960502 00466 NM 1996 5 2 ASAA9640022 1 19960323 A 3397 WIRE BOEING 737 737490 1384715 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 767AS 27081 SEA - FLT NR 98 - CREW REPORTED THAT THE FORWARD 4 EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTE D WIRING THAT HAD BECOME DISCONNECTED AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996050200467 19960502 00467 NM 1996 5 2 ASAA9640023 1 19960327 A 3350 CONNECTOR BOEING 737 7374Q8 NM CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 755AS 25096 ANC - MAINTENANCE CHECK, FOUND EMERGENCY EXIT FLOOR TRACK LIGHTS INOPERATIVE FROM ROW 27 AFT. RESEATED CONNECTOR/WIRING AT ROW 27 AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996050200468 19960502 00468 NM 1996 5 2 ASAA9640024 1 19960403 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 776AS 25109 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 22 THROUGH 25 AND ROWS 26 AFT WERE FOUND I NOPERATIVE. RECONNECTED LOOSE WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996050200469 19960502 00469 WP 1996 5 2 ASAA9680077 1 19960321 A 3350 1001191 LIGHT ASSY DOUG DC9 DC983 3022083 WP L-1 DOOR INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 976AS 53452 SEA - DURING MAINTENANCE CHECK, THE PORTABLE EMERGENCY EXIT LIGHT AT THE L-1 DOOR WAS FOUND INOPERATIVE. REPLACED LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996050200470 19960502 00470 WP 1996 5 2 ASAA9680078 1 19960324 A 3260 833703 DOWNLOCK SENSOR DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A ASAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 01 936AS 49363 SEA - FLT 467 - CREW REPORTED THE NOSE LANDING GEAR LIGHT REMAINED ILLUMINATED AFTER TAKEOFF OAK. FOLLOWED ABNORMAL GEA R INDICATION CHECKLIST, RECYCLED LANDING GEAR AND INDICATION SYSTEM OPERATED NORMALLY. LANDED IN SEA WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR UP/DOWNLOCK SENSOR AND CONNECTOR, ADJUSTED UPLOCK SENSOR AND THE NOSE LANDING GEAR INDICATIO N SYSTEM OPERATED NORMALLY DURING GEAR RETRACTION. (M) 2 L 7 2 4F A6WE 1996050200471 19960502 00471 WP 1996 5 2 ASAA9680079 1 19960324 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 965AS 53079 SEA - DURING MAINTENANCE CHECK, FORWARD 4 EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED LIGHTS/ WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996050200472 19960502 00472 WP 1996 5 2 ASAA9680080 1 19960326 A 7830 TR RETURN LINE DOUG DC9 DC982 3022082 WP LT ENGINE LEAKING A ASAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 01 938AS 49365 LAS - FLT NR 624 - CREW REPORTED AN ELECTRICAL OR HOT PLASTIC ODOR IN THE CABIN DURING DESCENT AND LANDING. INSPECTION OF ALL LAVATORY WASTE CONTAINERS, OVENS, BUN WARMERS AND COFFEE MAKERS REVEALED NO PLASTIC RESIDUE OR OVERHEAT CONDITION , ODOR HAS DISSIPATED. HOWEVER, DURING BOARDING OF OUTBOUND FLIGHT 651, THE ODOR RETURNED WITH THE AIR CONDITIONING PAC KS OPERATING. FOUND THE LEFT THRUST REVERSER RETURN LINE LEAKING SKYDROL. TIGHTENED THE 'B' NUT AND SYSTEM LEAK CHECKE D GOOD. CLEANED TAIL COMPARTMENT AREA, PERFORMED HIGH PRESSURE BURNOUT OF HIGH PRESSURE DUCTING AND REPLACED BOTH COALE SCERS. SYSTEM OPERATED NORMALLY WITH NO ODORS DETECTED. (M) 2 L 7 2 4F A6WE 1996050200473 19960502 00473 WP 1996 5 2 ASAA9680081 1 19960327 A 2170 1808492 COALESCERS DOUG DC9 DC982 3022082 WP CABIN CONTAM CHECK A ASAA K NONE A FLAME/FIRE CL CLIMB 1 NM 01 938AS 49365 LAS - FLT NR 9000, AIRCRAFT WAS RELEASED FOR MAINTENANCE FERRY FLIGHT TO SEA (REF MRR ASAA9680080). AFTER TAKEOFF, BOTH PILOTS DETECTED AND ODOR IN THE COCKPIT WHICH MAINTENANCE TECH FOREMAN OCCUPYING THE OBSERVERS SEAT ATTRIBUTED TO A HOT DUCT ODOR. AIRCRAFT RETURNED TO LAS AND THE AIR CONDITIONING PACKS WERE INSPECTED FOR HYDRAULIC AND PNEUMATIC LEAKS, N O LEAKS WERE FOUND. ODOR DIMINISHED AFTER EXTENDED PACK OPERATIONS. REPLACED BOTH COALESCERS AND RELEASED AIRCRAFT. N O ODORS WERE DETECTED DURING FERRY FLIGHT TO SEA. (M) 2 L 7 2 4F A6WE 1996050200474 19960502 00474 WP 1996 5 2 ASAA9680082 1 19960328 A 3350 41B004AD07G3 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 938AS 49365 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 13 THROUGH 18 WERE FOUND INOPERATIVE. REP LACED BATTERIES IN POWER SUPPLY AND LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996050200475 19960502 00475 WP 1996 5 2 ASAA9680083 1 19960329 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 200-255 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 967AS 49103 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON THE DOOR FRAME AND WEB FED Y200 PLUS 2 X PLUS 55. REPAIRED PER EA 5310-0 1426 AND EA 5310-01424. (M) 2 L 7 2 4F A6WE 1996050200476 19960502 00476 WP 1996 5 2 ASAA9680084 1 19960329 A 3350 D29982107 SLIDE LIGHT DOUG DC9 DC982 3022082 WP L-1 DOOR INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 930AS 49231 OAK - DURING C-CHECK, THE L-1 DOOR EMERGENCY EXIT EVACUATION SLIDE FAILED THE EMERGENCY LIGHT TEST. REPLACED L-1 SLIDE DUE TO DEFECTIVE EMERGENCY LIGHT BATTERY PACK. (M) 2 L 7 2 4F A6WE 1996050200477 19960502 00477 1996 5 2 ASAA9680085 4 19960329 A 2565 1321225L14A00 SLIDE BOTTLE DOUG DC9 DC982 3022082 WP TAILCONE EXIT LOW PRESS A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 932AS 49233 SEA - FLT NR 242 - CREW REPORTED TAILCONE EMERGENCY EVACUATION SLIDE PRESSURE LOW. REPLACED TAILCONE SLIDE ASSEMBLY. ( M) 2 L 7 2 4F A6WE 1996050200478 19960502 00478 WP 1996 5 2 ASAA9680086 1 19960329 A 5313 27779223 LONGERON DOUG DC9 DC982 3022082 WP BS 214 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 967AS 49103 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON LONGERON 30 AT Y214, X0, -50. REPLACED LONGERON PER EWO 96-8049. (M) 2 L 7 2 4F A6WE 1996050200479 19960502 00479 WP 1996 5 2 ASAA9680087 1 19960329 A 5730 SKIN DOUG DC9 DC982 3022082 WP WING CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 967AS 49103 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON THE WING LOWER SKIN T/E AT L/W, INBOARD FLAP, OUTBOARD HINGE SUPPORT FITT ING. REPAIRED PER EWO 96-8052. (M) 2 L 7 2 4F A6WE 1996050200480 19960502 00480 WP 1996 5 2 ASAA9680088 1 19960329 A 5720 DOUBLER DOUG DC9 DC982 3022082 WP BS 231-237 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 967AS 49103 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON THE INNER SKIN AT Y231 TO Y237, X PLUS 1 TO X-1, Z-50. REPAIRED PER EO 0 322966M2, SRM 51-10-3 AND 53-01. (M) 2 L 7 2 4F A6WE 1996050200481 19960502 00481 WP 1996 5 2 ASAA9680089 1 19960403 A 3350 S103 BATTERIES DOUG DC9 DC982 3022082 WP AFT O'WING EXIT DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 966AS 49104 SEA - DURING MAINTENANCE CHECK, THE AFT OVEWING EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. REPLACED BATTERIES AND LI GHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996050200482 19960502 00482 WP 1996 5 2 ASAA9680090 1 19960405 A 3350 41B004AD07G3 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 964AS 53078 SEA - DURING MAINTENANCE CHECK, AFT SECTION OF EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPAIRED SECTI ON OF WIRING AND REPLACED BATTERIES IN POWER PACK. LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996050200483 19960502 00483 WP 1996 5 2 ASAA9680091 1 19960406 A 3350 41B004AD07G3 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 954AS 49387 SEA - DURING MAINTENANCE CHECK, THE AFT SECTION OF EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. ALLOWED BATTERI ES TO CHARGE AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996050200484 19960502 00484 WP 1996 5 2 ASAA9680092 1 19960408 A 3230 GRD SENSE CABLE DOUG DC9 DC982 3022082 WP NLG OUT OF ADJUST A ASAA K NONE O OTHER CL CLIMB 1 NM 01 956AS 48079 SFO - UPON ARRIVAL OF FLT 430 - CREW REPORTED THE LANDING GEAR HANDLE WOULD NOT MOVE TO UP POSITION, USED GEAR HANDLE RE LEASE BUTTON TO MOVE GEAR HANDLE TO UP POSITION AFTER TAKEOFF FROM PDX. ADJUSTED GROUND SENSE CONTROL CABLES AND ANTI-R ETRACTION CABLE PER MM, ACCOMPLISHED RETRACTION/EXTENSION TEST AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996050200485 19960502 00485 WP 1996 5 2 ASAA9680093 1 19960409 A 3350 1001191 PORTABLE LIGHT DOUG DC9 DC983 3022083 WP CABIN DIM A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 976AS 4098 53452 PDX- DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND DIM. REPLACED THE LIGHT ASSEMBLY AND OPER ATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996050200486 19960502 00486 EU 1996 5 2 ASOA96012 1 19960403 A 7170 S0003001500000 DRAIN HOSE AEROSP ATR72 ATR72212 EU LT ENG CLOGGED A ASOA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. A J FLAME/FIRE WARNING INDICATION AP APPROACH 1 SO 11 641AS 387 FLT NR 8641 - ON APPROACH MCN-ATL, THE LEFT ENGINE FIRE WARNING ILLUMINATED AND THE LEFT ENGINE WAS IMMEDIATELY SHUT DOW N, FIRE HANDLE PULLED, AND AGENT 1 WAS DISCHARGED. THE FIRE WAS EXTINGUISHED AFTER APPROX 25 SECONDS. AN EMERGENCY WAS DECLARED AND FIRE EQUIPMENT REQUESTED. LANDING WAS MADE SAFELY AND WITHOUT INCIDENT, EMERGENCY PERSONNEL CONFIRMED THA T THE FIRE WAS EXTINGUISHED. FOUND LEFT ENGINE FUEL DRAIN HOSE CLOGGED. REMOVED LINE, CLEANED AND REPLACED. AS AN ADD ITIONAL PREVENTIVE MEASURE, CLEANED ALL DRAINS LINES ON BOTH ENGINES. REPLACED DAMGED COWLING. (M) 2 H 7 2 4T RT A53EU 1996050200487 19960502 00487 SW 1996 5 2 BDHA960007 1 19960319 A 7400 CONNECTOR SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP ENG WIRE HARNESS BROKEN WIRE A BDHA O OTHER O OTHER NR NOT REPORTED 1 GL 15 229AM TC305 P54119 PIR - FLT NR 421 - ON FIRST START ATTEMPT, ENGINE WOULD NOT LIGHT OFF. AFTER A LONG PREHEAT, THE ENGINE STARTED. MAINT ENANCE INVESTIGATED AND FOUND THE WIRE TO THE PRIMARIES ONLY SOLENOID CANNON PLUG BROKEN. AFTER REPLACING THE CANNON PL UG, THE ENGINE START CYCLE WAS SATISFACTORY. (M) 2 L 7 2 4T 4 T RT A8SW E4WE 1996050200488 19960502 00488 EU 1996 5 2 C2XA96IA080 1 19960328 A 2710 MS276434 BEARING AEROSP ATR42 ATR42320 8680930 EU LT AILERON WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15818 153 IAH - DURING C-CHECK INSPECTION, THE LEFT AILERON CONTROL SYSTEM BELLCRANK AT THE CENTER WING WAS FOUND TO HAVE A WORN A ND RUSTED BEARING. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEARING, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO S ERVICE. (M) 2 H 7 2 4T RT A53EU 1996050200489 19960502 00489 EU 1996 5 2 C2XA96IA081 1 19960328 A 5347 S53678001210 FLOOR TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15818 153 IAH - DURING C-CHECK INSPECTION, THE GALLEY FLOOR TRACK WAS FOUND TO CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFF ECTED PORTION OF TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996050200490 19960502 00490 EU 1996 5 2 C2XA96IA082 1 19960322 A 5315 S53672407202 FLOOR BEAM AEROSP ATR42 ATR42320 8680930 EU FS 38 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15818 153 IAH - DURING C-CHECK INSPECTION, FOUND CORROSION ON FS 38 FLOOR SUPPORT BEAM. REMOVED FS 38 FLOOR SUPPORT BEAM, FABRICA TED AND INSTALLED NEW SUPPORT BEAM, AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996050200491 19960502 00491 EU 1996 5 2 C2XA96IA083 1 19960322 A 5315 S53672406208 FLOOR BEAM AEROSP ATR42 ATR42320 8680930 EU FS 36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15818 153 IAH - DURING C-CHECK INSPECTION, FOUND CORROSION ON FRAME 36 FLOOR SUPPORT BEAM. REMOVED FRAME 36 FLOOR SUPPORT BEAM, F ABRICATED, AND INSTALLED NEW SUPPORT BEAM, AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996050200492 19960502 00492 EU 1996 5 2 C2XA96IA084 1 19960328 A 5320 S53671217294 THRESHOLD AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15818 153 IAH - DURING C-CHECK INSPECTION, THE PASSENGER DOOR THRESHOLD PLATE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND R EPLACED THE AFFECTED PLATE AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996050200493 19960502 00493 EU 1996 5 2 C2XA96IA085 1 19960328 A 5320 S53671318280 THRESHOLD AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15818 153 IAH - DURING C-CHECK INSPECTION, THE SERVICE DOOR THRESHOLD PLATE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REP LACED THE AFFECTED THRESHOLD PLATE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996050200494 19960502 00494 NM 1996 5 2 CKSA96022 1 19960329 A 2612 60B0002388 A12 CARD BOEING 747 747132 1384882 NM APU FAILED A CKSA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 GL 23 625PL 76066 20247 KSUU - APU FIRE WARNING AND MASTER LIGHT WITH BELL WENT OFF, PULLED HANDLE AND DISCHARGED BOTTLE. TROUBLESHOT SYSTEM FO UND A12 AND APU 'LOOP B FIRE' BAD FIRE WARNING NO LONGER USEABLE. TRANSFERRED TO DMI 342 FOR FURTHER TROUBLESHOOTING, P ULLED AND COLLARD APU CIRCUIT BREAKERS IAW MEL 49-1 PLACARDS INSTALLED. (M) 2 L 7 4 4F A20WE 1996050200495 19960502 00495 NM 1996 5 2 CKSA96023 1 19960314 A 2910 6517840 HYDRAULIC LINE BOEING 727 72722C 138400F NM NR 2 SPOILER CRACKED A CKSA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 23 727CK 54903 19195 ONT - TOTAL LOSS OF 'A' HYDRAULIC SYSTEM IN FLIGHT. REMOVED AND REPLACED LINE. OPS CHECK GOOD ON GROUND. BLED SYSTEM, LEAK CHECKED, OPS CHECKED GOOD. (M) 2 L 7 3 4F A3WE 1996050200496 19960502 00496 NM 1996 5 2 CKSA96025 1 19960308 A 3260 656021132 ACCESSORY UNIT BOEING 727 727223 1384074 NM RT MLG/NLG FAILED A CKSA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 856AA 52832 20997 KHUF - RIGHT MAIN GEAR UNSAFE LIGHT ILLUMINATED INTERMITTENTLY IN FLIGHT AND ON GROUND. NOSE GEAR UNSAFE LIGHT DOES NOT ILLUMINATE DURING RETRACTION. MASTER DIM AND MASTER TEST SECTION NR 3 LIGHTS INOP. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT, SYSTEM OPS CHECK GOOD IAW MM CHAPTER 32-09-121. REMOVED AND REPLACED MASTER DIM AND TEST MODULE LOGIC C ARD IAW B727 MM CHAPTER 33-15-11 SYSTEM OPS CHECKED GOOD. (M) 2 L 7 3 4F A3WE 1996050200497 19960502 00497 WP 1996 5 2 CKSA96026 1 19960310 A 3260 0080004005 PROX SWITCH DOUG DC8 DC863F 302198F WP LANDING GEAR FAILED A CKSA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 815CK 34296 46151 AFTER TAKEOFF, DOORS NOT LATCHED LIGHT AND GEAR NOT LATCHED LIGHT REMAINED ON BRIGHT. ON LANDING BOTH RED LIGHTS WERE O N AND RIGHT MAIN GEAR LIGHT WAS OUT. REMOVED AND REPLACED LANDING GEAR PROXIMITY SWITCH CONTROL BOX. SYSTEM OPS CHECK GOOD IAW DC-8 MM 32-60-0. (M) 2 L 7 4 4F 4A25 1996050200498 19960502 00498 NE 1996 5 2 CKSA96027 2 19960316 A 7200 ENGINE DOUG DC8 DC8F55 3021928 WP PWA JT3D JT3D3B 52039 NE NR 2 FAILED A CKSA O OTHER E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 GL 23 6161M 71393 45762 645142 NR 2 ENGINE FAILED IN FLIGHT, ENGINE VIBRATED STRONGLY AND EPR DECREASED IMMEDIATELY, EGT WENT TO APPROX 650C. REMOVED AND REPLACED NR 2 ENGINE IAW DC8 MIP-1 SECTION 9. OPS AND LEAK CHECK GOOD IAW DC8 MIP-1 SECTION 10. (M) 2 L 7 4 4F 4 F 4A25 1E8 1996050200499 19960502 00499 NM 1996 5 2 E9WA 1 19960216 A 5532 SKIN BOEING 737 7372H5 138448E NM VERT STAB DAMAGED A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION VISUALLY FOUND MISSING TRAILING EDGE HONEYCOMB CORE MATERIAL LOCATED AT THE VERTICAL STAB AT RUDDER STA TION 218 RIGHT TRAILING EDGE PANEL. COMPOSITE REPAIRED AS PER BOEING SRM 51-40-13. (M) 2 L 7 2 4F A16WE 1996050200500 19960502 00500 WP 1996 5 2 GAIA9602 1 19960209 A 3297 WIRE DOUG DC9 DC915F 3022037 WP LT MLG BROKEN A GAIA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 562PC 45123 47012 KHA FERRY FLT NR 562 - LRD-DFW - ON APPROACH TO DFW, AFTER EXTENDING THE LANDING GEAR THE LEFT MAIN GEAR DOWN AND LOCKED GREEN LIGHT WOULD NOT COME ON. ABNORMAL PROCEDURES WERE FOLLOWED TO EXTEND THE LANDING GEAR AND AN EMERGENCY WAS DECLA RED. AN UNEVENTFUL LANDING WAS MADE. INSPECTION REVEALED A BROKEN WIRE ON THE LEFT MLG DOWN LOCK SWITCH CONNECTOR. RE PAIRED WIRE AND OPS CHECKED SYSTEM PER DC9 MM. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1996050200501 19960502 00501 WP 1996 5 2 GAIA9603 1 19960222 A 3230 24051501052 UPLOCK SPRING CVAC 240 240D 2422660 WP LANDING GEAR HEAT DAMAGED A GAIA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 94279 65914 101 FLT 163 - MMMY-LRD - AFTER TAKEOFF, THE LANDING GEAR UNSAFE WARNING LIGHT ILLUMINATED WHEN THE HYDRAULIC SELECTOR WAS PU T IN BYPASS. REPRESSURIZED HYDRAULIC SYSTEM, LIGHT EXTINGUISHED. PROCEEDED TO LRD MADE NORMAL UNEVENTFUL LANDING AT LR D. THE AIRCRAFT WAS FERRIED FROM LRD TO DFW WITH THE LANDING GEAR EXTENDED. INVESTIGATION REVEALED THAT THE UPLOCK SPR INGS WERE HEAT DAMAGED. THE UPLOCK SPRINGS WERE REPLACED AND THE LANDING GEAR WAS OPERATIONALLY CHECKED IAW THE CONVAIR MM. (M) 2 L 7 2 4R RT A793 1996050200502 19960502 00502 NM 1996 5 2 GAIA9604 1 19960304 A 2780 651725613 RIB BOEING 727 727223 1384074 NM RT WING L/E CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6833 71048 20186 DURING NR 7 SLAT ACTUATOR REPLACEMENT AT MSP, MECHANIC FOUND OUTBOARD SLAT ACTUATOR TRUNNION SUPPORT RIB CRACKED THROUGH LOWER BOLT HOLE. SUPPORT RIB REPLACED PER SB 727-57-130R2, ACTUATOR INSTALLED, RIG AND LEAK CHECKED SATISFACTORY. AGI NG AIRCRAFT MOD PER SB 57-130R2 HAS NOT BEEN PREVIOUSLY ACCOMPLISHED ON THIS AIRCRAFT. (M) 2 L 7 3 4F A3WE 1996050200503 19960502 00503 NM 1996 5 2 GAIA9605 1 19960319 A 2611 SMOKE LIGHT BOEING 727 727251 138408H NM CARGO COMPT ILLUMINATED A GAIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 279US 21158 FLT NR 711 - SJC-TOL - WHILE IN CRUISE TO TOL, THE FLIGHT CREW NOTICED THE CARGO COMPARTMENT SMOKE DETECTION LIGHT ILLUM INATED, NO EVIDENCE OF SMOKE WAS PRESENT. THE FLIGHT CREW MADE A PRECAUTIONARY LANDING AT SLC. INSPECTION DID NOT FIND ANY DEFECT AND COULD NOT DUPLICATE THE PROBLEM. AIRCRAFT RELEASED FOR FLIGHT. SUSPECT MOISTURE CONDENSATION ON THE SM OKE DETECTOR LENS. (M) 2 L 7 3 4F A3WE 1996050200504 19960502 00504 SO 1996 5 2 GLBA96050 1 19960311 A 3230 12032943001 SEQUENCE VLV EMB 120 EMB120RT SO RT MLG OUT OF ADJUST A GLBA O OTHER J WARNING INDICATION CL CLIMB 1 CE 01 281UE 120092 ORD - CREW REPORTED THE RIGHT MAIN GEAR DID NOT RETRACT WHEN SELECTED UP. UPON RECYCLING GEAR, RIGHT GEAR OPERATED NORM ALLY. MAINTENANCE ADJUSTED RIGHT SEQUENCE VALVES. SYSTEM OPS CHECK WAS GOOD. (M) 2 L 7 2 4T RT A31SO 1996050200505 19960502 00505 SO 1996 5 2 GLBA96051 1 19960314 A 2910 MS28775013 PCU O-RING EMB 120 EMB120RT SO RUDDER LEAKING A GLBA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 CE 01 452UE 120096 BRL - CREW REPORTED HYDRAULIC LOW LEVEL AND LOW PRESSURE ANNUNCIATORS ILLUMINATED. CREW PERFORMED A MANUAL GEAR EXTENSI ON AND LANDED UNEVENTUALLY. MX REMOVED AND REPLACED A LEAKING O-RING ON THE RUDDER PCU. LEAK CHECK AND OPS CHECK WERE GOOD. (M) 2 L 7 2 4T RT A31SO 1996050200506 19960502 00506 SO 1996 5 2 GLBA96052 1 19960315 A 3230 12032943001 SEQUENCE VALVE EMB 120 EMB120RT SO LT MLG OUT OF ADJUST A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 129AM 14406 120119 MYR - CREW REPORTED LEFT MAIN LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. CREW ELECTED AN AIR TURN BACK AND MADE AN U NEVENTFUL LANDING. MAINTENANCE ADJUSTED LEFT MAIN LANDING GEAR SEQUENCE VALVE. GEAR SWING WAS PERFORMED, OPS CHECK GOO D. (M) 2 L 7 2 4T RT A31SO 1996050200507 19960502 00507 SO 1996 5 2 GLBA96053 1 19960317 A 3260 922AAZYA6P2722A PROXIMITY SENSOR EMB 120 EMB120RT SO RT MLG DIRTY A GLBA O OTHER N FALSE WARNING LD LANDING 1 CE 01 451UE 120108 DLH - CREW REPORTED THAT THEY HAD NO RIGHT 'DOWN AND LOCKED' INDICATION AFTER GEAR EXTENSION. CREW MADE AN UNEVENTFUL L ANDING. MAINTENANCE CLEANED RIGHT DOWNLOCK PROXIMITY SENSORS. GEAR SWING OPS CHECK GOOD. (M) 2 L 7 2 4T RT A31SO 1996050200508 19960502 00508 EA 1996 5 2 GLBA96054 2 19960319 A 7532 311271401 BLEED VALVE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA RT ENGINE MALFUNCTIONED A GLBA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 01 126UE 498 3N786 UC126 32379 GRI - CREW REPORTED RIGHT TORQUE SURGED ON TAKEOFF ROLL AND ELECTED TO RETURN TO GATE. MAINTENANCE REPLACED RIGHT BLEED VALVE. OPS CHECK WAS GOOD. (M) 2 L 7 2 4T 4 T RT A24CE E4EA 1996050200509 19960502 00509 SO 1996 5 2 GLBA96055 1 19960319 A 3230 RETRACT MECH EMB 120 EMB120RT SO RT MLG MALFUNCTIONED A GLBA O OTHER J WARNING INDICATION LD LANDING 1 CE 01 451UE 120108 DLH - CREW REPORTED RIGHT GEAR WOULD NOT EXTEND IN PRIMARY MODE. A BACKUP ELECTRICAL EXTENSION WAS MADE. MAINTENANCE C OULD NOT DUPLICATE DISCREPANCY DURING OPERATIONAL CHECK. (M) 2 L 7 2 4T RT A31SO 1996050200510 19960502 00510 CE 1996 5 2 GLBA96056 1 19960319 A 7110 B140048 COWL LATCH BEECH 1900 1900C 1154161 CE LT ENG WORN A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 01 101UE UC101 LAN - DURING CLIMB-OUT, CREW OBSERVED LEFT TOP COWL WAS DETACHED FROM INBOARD LATCHES (OUTBOARD LATCHES REMAINED LATCHED ). CREW ELECTED AN AIR TURN BACK AND MADE AN UNEVENTFUL LANDING. MAINTENANCE REPLACED INBOARD, AFT COWL LATCH AND RESE CURED COWL. (M) 2 L 7 2 4T RT A24CE 1996050200511 19960502 00511 CE 1996 5 2 GLBA96057 1 19960321 A 5297 WIRE BEECH 1900 1900C 1154161 CE FWD CABIN DOOR BROKEN A GLBA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 01 104GL UC104 DEN - FORWARD CABIN DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT. CREW ELECTED AN AIR TURN BACK AND MADE AN UNEVENTFUL LANDIN G. MAINTENANCE REPAIRED BROKEN WIRE AT UPPER AIRSTAIR DOOR MICROSWITCH. OPS CHECK WAS GOOD. (M) 2 L 7 2 4T RT A24CE 1996050200512 19960502 00512 CE 1996 5 2 GLBA96058 1 19960322 A 5210 11440321 BRACKET BEECH 1900 1900C 1154161 CE AIRSTAIR DOOR FAILED A GLBA K NONE O OTHER IN INSP/MAINT 1 CE 01 104GL UC104 SPW - DURING VISUAL INSPECTION, AIRSTAIR DOOR DAMPNER LOWER ATTACH BRACKET WAS FOUND TO HAVE PULLED AWAY FROM DOOR. MAI NTENANCE REPLACED BRACKET IAW BEECHCRAFT BRACKET KIT NR 114-4032-1. (M) 2 L 7 2 4T RT A24CE 1996050200515 19960502 00515 NM 1996 5 2 PCAA9600272 1 19960305 A 6120 82455011S011 CABLE ASSY DHAV DHC8 DHC8102 2809003 NM NR 2 PROP SHORTED A PCAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 13 820EX 019 AUTO FEATHER ARMED ADVISORY LIGHT FLICKERED ON AND OFF DURING CLIMB-OUT. FURTHER TESTING ON GROUND REVEALED NR 2 PROP W OULD NOT FEATHER. TROUBLESHOT AND FOUND RIGHT ENGINE TSCU INTERFACE HARNESS AT FAULT. REMOVED AND REPLACED HARNESS. O PERATIONAL CHECKED GOOD. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1996050200516 19960502 00516 NM 1996 5 2 PCAA9600275 1 19960305 A 7120 8DK1763001 STRUT DHAV DHC8 DHC8102 2809003 NM LEFT BROKEN A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 808EX A43176 299 PROPELLER VIBRATION FELT IN BETA, 950, AND 1050 RPM. INSPECTED AND FOUND LEFT AND RIGHT REAR ENGINE MOUNTS STRUTS BROKE N. REMOVED AND REPLACED ALL ENGINE MOUNTS AND PERFORMED PROPELLER BALANCE. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1996050200517 19960502 00517 NM 1996 5 2 PCAA9600277 1 19960308 A 2910 82950010271 HYD LINE DHAV DHC8 DHC8102 2809003 NM RT SPOILER FAILED A PCAA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 13 811AW 201 WHILE IN CRUISE FLIGHT, CREW NOTICED THE NR 1 HYDRAULIC QUANTITY READ ZERO. PRESSURE REMAINED NORMAL. WHEN FLAPS WERE SELECTED UP, THE SPOILER CAUTION LIGHT ILLUMINATED. INSPECTED AND FOUND HYDRAULIC LINE AT THE RIGHT INBOARD ROLL SPOILE R FAILED. INSTALLED FLEXIBLE LINE PER DHC STANDARD PRACTICES. SYSTEM SERVICED AND BLED LEAK AND OPERATIONAL CHECK GOOD . AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1996050200518 19960502 00518 NM 1996 5 2 PCAA9600278 1 19960314 A 3350 LIGHTS DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 820EX 019 RIGHT SIDE CABIN FLOOR EMERGENCY LIGHTS ARE INOP. REPLACED BATTERY PACK FUSES. LIGHTS OP CHECK NORMALLY. AIRCRAFT RET URNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1996050200519 19960502 00519 NM 1996 5 2 PCAA9600279 1 19960323 A 5610 17180003 WINDOW DHAV DHC8 DHC8102 2809003 NM LT COCKPIT CRACKED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 804EX 7624 225 227 LEFT SIDE WINDOW HAS CRACKED OUTER PANE FROM BOTTOM TO TOP. REMOVED AND REPLACED LEFT SIDE WINDOW, OPS CHECK OK. AIRCR AFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1996050200520 19960502 00520 EU 1996 5 2 PLG32596DG1 1 19960325 A 2730 7227105711 CABLES SAAB SF340 340B 7860101 EU ELEVATOR CHAFED A PLGA K NONE O OTHER IN INSP/MAINT 1 NE 05 347BE 340B187 PSM - DURING ROUTINE C-CHECK INSPECTION, RIGHT INBOARD AND OUTBOARD ELEVATOR CONTROL CABLES WERE FOUND CHAFED AT SEVERAL GUIDES. BOTH CONTROL CABLES WERE REPLACED AND RIGGED IAW SAAB AMM CHAP 27. (M) 2 L 7 2 4T RT A52EU 1996050200521 19960502 00521 EU 1996 5 2 PLG32596DG2 1 19960325 A 5712 RIB SAAB SF340 340B 7860101 EU LT/RT WING CRACKED A PLGA K NONE O OTHER IN INSP/MAINT 1 NE 05 347BE 340B187 PSM - DURING ROUTINE C-CHECK INSPECTION, CRACKS WERE FOUND ON RIBS ON LEFT AND RIGHT INBOARD MOST WING LEADING EDGES AND RIGHT WING LEADING EDGE JUST OUTBOARD NACELLE. ALL CRACKS WERE REPAIRED IAW SAAB SRM CHAPTERS 51-57. (M) 2 L 7 2 4T RT A52EU 1996050200522 19960502 00522 EU 1996 5 2 PLG32596DG3 1 19960325 A 5321 FLOOR SAAB SF340 340B 7860101 EU COCKPIT CORRODED A PLGA K NONE O OTHER IN INSP/MAINT 1 NE 05 347BE 340B187 PSM - DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS FOUND PILOTS AND CO-PILOTS FLOOR AREA IN COCKPIT. REMOVED CORROS ION AND REPAIRED IAW SAAB SRM CHAPTERS 51-53. (M) 2 L 7 2 4T RT A52EU 1996050200523 19960502 00523 EU 1996 5 2 PLG32596DG4 1 19960325 A 5210 DOOR FRAME SAAB SF340 340B 7860101 EU COCKPIT DOOR CORROSION A PLGA K NONE O OTHER IN INSP/MAINT 1 NE 05 347BE 340B187 PSM - DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS FOUND ON COCKPIT DOOR FRAME. REMOVED CORROSION AND REPAIRED IAW SAAB SRM CHAPTERS 51, 51 AND SAAB DOC NR 72LAWD960315A. (M) 2 L 7 2 4T RT A52EU 1996050200524 19960502 00524 EU 1996 5 2 PLG32596DG8 1 19960325 A 2730 7227105711 CONTROL CABLE SAAB SF340 340B 7860101 EU ELEVATOR CHAFED A PLGA K NONE O OTHER IN INSP/MAINT 1 NE 05 347BE 340B187 DURING ROUTINE C-CHECK INSPECTION, LEFT INBOARD AND OUTBOARD ELEVATOR CONTROL CABLES WERE FOUND CHAFED AT SEVERAL GUIDES . BOTH CONTROL CABLES WERE REPLACED AND RIGGED IAW SAAB AMM CHAPTER 27. (M) 2 L 7 2 4T RT A52EU 1996050200525 19960502 00525 WP 1996 5 2 RRXA96014 1 19960312 A 5320 37549462 FITTING DOUG DC8 DC863 302198A WP FS 1220 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 797AL 46163 KMCN - DURING C-CHECK, FOUND FLOOR BEAM TO CUSP ATTACH BRACKET CRACKED AT FS 1220, RIGHT SIDE. MAINTENANCE REMOVED AND FABRICATED NEW FITTING IAW DER APPROVED COTNEY ENGINEERING SKETCH A27-D01. INSTALLED IAW DC8-SRM 53-1-0. (M) 2 L 7 4 4F 4A25 1996050200526 19960502 00526 EU 1996 5 2 SABA9600010 1 19960324 A 7603 A552326 FLEX CABLE STBROS SD3 SD360 8100606 EU RT PWR CONTROL SEIZED A SABA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 33 748CC SH3748 FLT NR 5153 -THE FLIGHT WAS CLEARED FOR TAKEOFF AND HAD JUST TAKEN THE RUNWAY WHEN THE POWER LEVERS WERE ADVANCED AND TH E RIGHT POWER LEVER COULD NOT BE ADVANCED PAST ONE-THIRD OF THE WAY. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MX PERSONNEL WAS DISPATCHED TO HKY TO CORRECT THE PROBLEM. THE POWER LEVER CONTROL SYSTEM WAS TROUBLESHOT AND THE RIGHT 'BODEN FLEX' CABLE WAS FOUND TO BE BINDING INTERNALLY. THE 'BODEN FLEX' CABLE WAS REPLACED. THE AIRCRAF T WAS GROUND RUN AND CHECKED FOR PROPER ENGINE OPERATION, AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T A41EU 1996050200527 19960502 00527 NM 1996 5 2 SABA9600011 1 19960321 A 2930 HYD WARN LIGHT DHAV DHC8 DHC8102 2809003 NM NR 2 ENGINE ILLUMINATED A SABA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 33 881CC 294 FLT NR 5033 - CLT-MGM - FLIGHT JUST DEPARTED WHEN THE GEAR WAS SELECTED UP AND THE NR 2 ENGINE HYD CAPTION LIGHT ILLUMIN ATED. AS THE GEAR CYCLE COMPLETED THE CAPTION EXTINGUISHED, THE CAPTAIN THEN SELECTED THE GEAR DOWN. RECEIVED THREE GR EEN DOWN AND LOCKED LIGHTS AND RETURNED TO THE FIELD FOR AN UNEVENTFUL LANDING. MAINTENANCE PERSONNEL INSPECTED THE NR 2 HYDRAULIC SYSTEM. NO DISCREPANCIES WERE FOUND. THE AIRCRAFT WAS THEN GROUND RAN WITH THE NR 2 HYD POWERED ALL INDICA TIONS WERE NORMAL. THE DECISION WAS THEN MADE TO PERFORM A TEST FLIGHT. A/C WAS THEN TEST FLOWN UNDER FLT NR 9103 AND ALL HYDRAULIC INDICATIONS WERE NORMAL. THE A/C WAS THEN RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1996050200528 19960502 00528 EU 1996 5 2 SABA9600013 1 19960326 A 5620 1379595C3 WINDOW BAG JETSTM JETSTM3101 1500215 EU RT CABIN CRACKED A SABA O OTHER O OTHER DE DESCENT 1 SO 33 693JX 693 FLT NR 5217 - DURING DESCENT INTO RDU, THE RIGHT NR 1 CABIN WINDOW OUTER PANE CRACKED. THE CAPTAIN DID NOT DECLARE AND EMERGENCY BUT BEGAN HIS DESCENT INTO RDU AS NORMAL. THE INNER PANE FOR THE NR 1 CABIN WINDOW STAYED INTACT AND PRESSURI ZATION OF THE AIRCRAFT WAS NOT EFFECTED. MAINTENANCE PERSONNEL WAS DISPATCHED TO RDU TO CORRECT THE PROBLEM. THE RIGHT NR 1 CABIN WINDOW OUTER PANE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996050200529 19960502 00529 EU 1996 5 2 SIMA960921 1 19960401 A 3350 3011004 POWER SUPPLY AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 12MQ 104 012 GRR - EMERGENCY LIGHT ABOVE FRONT RIGHT EXIT WINDOW FOUND TO BE INOPERATIVE ON MAINTENANCE CHECK. REPLACED POWER SUPPLY 10 WL. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996050200530 19960502 00530 EU 1996 5 2 SIMA960941 1 19960403 A 3397 WIRE AEROSP ATR42 ATR42300 8680920 EU PAX DOOR BROKEN A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 427MQ 091 ORD - REPAIRED WIRING TO AIRSTAIR EMERGENCY LIGHT. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996050200531 19960502 00531 WP 1996 5 2 TC8A96041 1 19960404 A 3230 3709309502 CABLE DOUG DC8 DC851 3021920 WP RT MLG BROKEN A TC8A O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 805CK 45649 MCO-DAY - RIGHT GEAR DOOR UNSAFE LIGHT ON IN FLIGHT. CONTINUED TO DESTINATION AT 230 KIAS PER FOM. SUBMITTER STATES, S USPECT GEAR DOOR NOT UP. FOUND CABLE FOR RIGHT BOGIE UNLOCK VALVE BROKEN, (40B/111B). VALVE WAS FOUND IN FULL RIGHT PO SITION. REMOVED AND REPLACED CABLE RUN (40B/111B) AND ADJUSTED STEERING. OPS CHECK GOOD IAW DC-8 M/M 32-12-0. AIRCRAF T RELEASED PER GMM CHAP II, PAGE 3. (M) 2 L 7 4 4F 4A25 1996050200532 19960502 00532 NM 1996 5 2 TWRA9615 1 19960330 A 2140 HEATER BOEING 747 747131 1384881 NM CABIN DIRTY A TWRA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 608FF 19672 IN CRUISE, UPPER DECK HEATER HAS A STRONG SMELL OF BURNING RUBBER. FOUND INSULATION IN HEATER ELEMENT, REMOVED INSULATI ON IAW MM 21-44-00. (M) 2 L 7 4 4F A20WE 1996050200533 19960502 00533 NM 1996 5 2 TWRA9616 1 19960403 A 3350 363781 LIGHT STRIPS BOEING 747 747282B 1384860 NM CABIN SHORTED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 611FF 20502 EMERGENCY EXIT LIGHTS WILL NOT EXTINGUISH WITH OVERHEAD CONTROL SWITCH IN 'ARM' POSITION. REPLACED SHORTED LIGHT STRIPS ON FLOOR. (M) 2 L 7 4 4F A20WE 1996050200534 19960502 00534 NM 1996 5 2 TWRA9617 1 19960403 A 3350 900835A BATTERY PACK BOEING 747 747282B 1384860 NM CABIN DISCHARGED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 611FF 20502 EGRESS LIGHTS INTERMITTENTLY COMING ON AT TIMES (BUSTLE LT AT R-1 DOOR AND EXIT LT AT R-1 DOOR). REPLACED BATTERY PACK AT BUSTLE LT, R-1 DOOR AND AT EXIT LT, R-1 DOOR. (M) 2 L 7 4 4F A20WE 1996050200535 19960502 00535 NM 1996 5 2 TWRA9618 1 19960406 A 3350 900835A BATTERY PACK BOEING 747 747130 1384880 NM CABIN LOOSE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 603FF 19746 DURING PREFLIGHT, FEO FOUND EMERGENCY LIGHTS 'E' PATH INOP. TROUBLESHOT TO UPPER DECK LEFT CEILING BATTERY PACK. RESEA TED BATTERY PACK. LIGHTS OK. (M) 2 L 7 4 4F A20WE 1996050200536 19960502 00536 1996 5 2 UF6A960304 4 19960314 A 3444 9650576020 GPWS COMPUTER BAG ATP ATP EU E/E COMPT FAILED A UF6A C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 31 857AW 7307 2034 ORD - MX 5725 - GPWS ACTIVATED ON TAKEOFF ROLL. MAINTENANCE REMOVED AND REPLACED GPWS COMPUTER. (M) 2 L 7 2 4T RT A27NM 1996050200537 19960502 00537 EU 1996 5 2 UF6A960305 1 19960315 A 2611 CG7PT2 SMOKE DETECTOR BAG ATP ATP EU LAVATORY FAILED A UF6A K NONE N FALSE WARNING TX TAXI/GRND HDL 1 GL 31 859AW 7554 1225 2036 ORD - FLT 5733 - SMOKE CWP ILLUMINATED FOR LAVATORY. MAINTENANCE REMOVED AND REPLACED THE LAVATORY SMOKE DETECTOR. SYS TEM OPS CHECK GOOD. (M) 2 L 7 2 4T RT A27NM 1996050200538 19960502 00538 EU 1996 5 2 UF6A960306 1 19960316 A 3320 F5113WW LAMP BAG ATP ATP EU CABIN FAILED A UF6A K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 31 858AW 8027 2035 ORD - FLT NR 5709 - FLIGHT ATTENDANT REPORTED ELECTRICAL ODOR COMING FROM THE NR 2 OVERHEAD BIN ON LEFT SIDE. MAINTENAN CE REMOVED AND REPLACED LIGHT BULB. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4T RT A27NM 1996050200539 19960502 00539 EU 1996 5 2 UF6A960307 1 19960317 A 3240 AIR44900 PRESS RELIEF VLV BAG ATP ATP EU LT BRAKE SYSTEM FAILED A UF6A O OTHER J WARNING INDICATION CR CRUISE 1 GL 31 856AW 8890 2032 ORD - FLT NR 5703 - BRAKE LOW PRESSURE CWP ILLUMINATED. INNER BRAKE PRESSURE READS ZERO PSI. MAINTENANCE REMOVED AND R EPLACED PRESSURE RELIEF VALVE. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4T RT A27NM 1996050200540 19960502 00540 WP 1996 5 2 USAA960246 1 19960214 A 5330 SKIN DOUG DC9 DC981 3022081 WP BS 1437 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 809US 39383 48041 PIT - DURING THE C-1 INSPECTION, FOUND TWO CRACKS, 1 INCH AND 2 INCHES AT STATION 1437 LONGERON 4L IN FUSELAGE SKIN. RE MOVED CRACK AND INSTALLED FILLER AND DOUBLER SRM 53-04 FIG NR 27. (M) 2 L 7 2 4F A6WE 1996050200541 19960502 00541 NM 1996 5 2 USAA960366 1 19960403 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 312 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 280AU 34606 22892 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH AREA OF CORROSION ON FLOOR BEAM BS 312 8 INCH RBL. REP LACED T-CAP AND INSTALLED SPLICE ANGLES, REPAIRED PER TR NR 53-10-13. CORROSION TASK NR C53-107-01, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996050200542 19960502 00542 NM 1996 5 2 USAABB96011 1 19960402 A 2931 TC125UK00ZY1 DIFF PRESS IND BOEING 767 767201 1385125 NM LT HYD SYSTEM LEAKING A USAA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CL CLIMB 1 EA 19 649US 23901 BOS - FL 816, CREW RECEIVED EICAS MESSAGE 'L HYD QTY', QUANTITY READ .45. FLIGHT RETURNED TO BOS AND LANDED WITH NO FUR THER INCIDENT. MAINTENANCE FOUND THE DIFFERENTIAL PRESSURE INDICATOR LEAKING AT THE PRESSURE MODULE AND REPLACED IT. ( M) 2 L 7 2 4F RT A1NM 1996050200543 19960502 00543 WP 1996 5 2 USAAD96021 1 19960209 A 5242 DOOR DOUG DC9 DC931 3022065 WP E/E COMPT NOT LATCHED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 980VJ 48156 CLT - FLT 1851 - AFTER TAKEOFF FROM CLT, CREW COULD NOT PRESSURIZE AIRCRAFT AND ALSO RECEIVED THE E/E DOOR LIGHT. FLIGH T RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE E/E DOOR NOT LATCHED PROPERLY. THE MECHAN ISM WAS CHECKED AND FOUND TO BE IN PROPER WORKING ORDER. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F A6WE 1996050200544 19960502 00544 WP 1996 5 2 USAAD96022 1 19960211 A 5610 9615059002 WINDSHIELD DOUG DC9 DC931 3022065 WP LT COCKPIT FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 976VJ 36226 48147 PIT - FL 209 - ON CLIMB-OUT, CAPTAINS WINDSHIELD BEGAN TO ARC AND THEN CRACKED. FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE TEMPERATURE CONTROL (P/N 9615059002) UNIT AND THE WINDSHIELD. (M) 2 L 7 2 4F A6WE 1996050200545 19960502 00545 WP 1996 5 2 USAAD96037 1 19960331 A 3244 3292D TIRE DOUG DC9 DC931 3022065 WP NOSE GEAR WORN A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 980VJ 48156 STRONG BURNING RUBBER SMELL AFTER TAKEOFF (OUT OF ATL). DECLARED EMERGENCY INBOUND TO CLT. LANDED UNEVENTFULLY. INSPE CTED BOTH ENGINE INTAKES, GROUND RAN PACKS. NO SMELLS PRESENT. FOUND BOTH NOSE TIRES WORN. REMOVED AND REPLACED BOTH NOSE TIRES. (M) 2 L 7 2 4F A6WE 1996050200546 19960502 00546 NM 1996 5 2 USAASB96045 1 19960312 A 5210 507945178 DOOR ASSY BOEING 737 7374B7 1384702 NM CABIN FALSE LOCK A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 433US 24555 FLT 904 - PIT - AFTER TAKEOFF UNABLE TO CONTROL CABIN ALTITUDE. WENT TO STANDBY MODE ON CONTROLLER, STILL UNABLE TO CON TROL CABIN. USING MANUAL AC MODE, REGAINED CABIN CONTROL. MAINTENANCE VISUALLY INSPECTED EXTERIOR DOORS. FOUND THE MA IN ENTRANCE DOOR 'FALSE LOCKED'. CYCLED THE MAIN ENTRANCE DOOR SEVERAL TIMES. DOOR OPENS AND CLOSED NORMALLY. AIRCRAF T OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 1996050200547 19960502 00547 NM 1996 5 2 USAASB96062 1 19960402 A 3297 WIRE BOEING 737 7373B7 1384580 NM NLG LOOSE A USAA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 EA 19 393US 23315 FLT NR 15 - IAD - NOSE GEAR RED UNSAFE LIGHT ON. NO GREEN LIGHT, FOLLOWED ALL USAIR PILOT HANDBOOK PROCEDURES. PERFORM ED TOWER FLYBY. DECLARED AN EMERGENCY. LANDED SAFELY IN IAD. MAINTENANCE FOUND THE GROUND WIRE FROM SWITCH S845 DOWN LOCK SWITCH PULLED FROM A SPLICE. REPAIRED SAME. (M) 2 L 7 2 4F RT A16WE 1996050200548 19960502 00548 NM 1996 5 2 USAASB96063 1 19960327 A 5270 694280980 SENSOR BOEING 737 7374B7 1384702 NM AFT CARGO DOOR FAILED A USAA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 EA 19 780AU 24997 FLT NR 380 - MKE - 1500 FEET AFTER TAKEOFF FROM MKE, LOST CABIN PRESSURE. NO INDICATION IN COCKPIT, RETURNED TO MKE. M AINTENANCE FOUND AFT CARGO DOOR OPEN. REPLACED AFT CARGO DOOR WARNING SENSOR. OPS CHECKS GOOD. (M) 2 L 7 2 4F RT A16WE 1996050200550 19960502 00550 EU 1996 5 2 VTZA96131 1 19960326 A 5270 SP4594 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGG DOOR FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 322UE 41058 FLT NR 6167 - IAD-LGA - ABORTED THE TAKEOFF DUE TO THE MAIN BAGGAGE DOOR WARNING LIGHT ILLUMINATING DURING THE TAKEOFF R OLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 17607 IAW MEL 52-3 ON THE DOOR WAR NING SYSTEM. MX LATER CLEARED DMI NR 17607 ON 3-27-96 BY REPLACING THE BAGGAGE DOOR WARNING MICROSWITCHES. AIRCRAFT WA S RELEASED AND APPROVED FOR RETURN TO SERVICE. MANUFACTURER IS CURRENTLY INVESTIGATING TO DETERMINE IF THE SWITCH DESIG N OR THEIR PLACEMENT IS AT FAULT FOR THE HIGH INCIDENCE OF FALSE BAGG DOOR WARNINGS. (M) 2 L 7 2 4T RT A41NM 1996050200551 19960502 00551 EU 1996 5 2 VTZA96132 1 19960323 A 5270 91SE16 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGGAGE DOOR OUT OF RIG A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 27 322UE 41058 FLT NR 6215 - CHS-IAD - ABORTED THE TAKEOFF DUE TO THE MAIN BAGGAGE DOOR WARNING LIGHT ILLUMINATING DURING THE TAKEOFF R OLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 17606 IAW MEL 52-3 ON THE DOOR WAR NING SYSTEM. MAINTENANCE LATER CLEARED DMI NR 17606 ON 3-26-96, BY RERIGGING THE BAGGAGE DOOR WARNING MICROSWITCHES. A IRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996050200552 19960502 00552 EU 1996 5 2 VTZA96133 1 19960327 A 5270 91SE16 SWITCH BAG JETSTM JETSTM3201 1500217 EU PAX DOOR DIRTY A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 488UE 907 FLT NR 6424 - IAD-BUF - DURING CLIMB-OUT, RETURNED TO IAD DUE TO THE PASSENGER DOOR WARNING LIGHT ILLUMINATING. AIRCRAF T LANDED AT IAD WITH NO FURTHER INCIDENTS. MX CLEANED AND LUBED THE DOOR MICROSWITCHES. AIRCRAFT WAS RELEASED AND APPR OVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996050200553 19960502 00553 EU 1996 5 2 VTZA96134 1 19960322 A 5610 14156002406 WINDSHIELD JETAIR JETSTM JETSTM4101 1500501 EU RT COCKPIT CRACKED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 306UE 41020 FLT NR 6276 - IAD-EWR - DURING CRUISE, RETURNED TO IAD DUE TO THE RIGHT WINDSHIELD OUTER PANE CRACKING. AN EMERGENCY WA S DECLARED AND AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS AND ALL PASSENGERS AND CREW SAFE. MAINTENANCE REPLACED THE RIGHT WINDSHIELD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996050200554 19960502 00554 EU 1996 5 2 VTZA96135 1 19960321 A 5270 91SE16 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGG DOOR OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 322UE 41058 FLT NR 6225 - IAD-BOS - ABORTED TAKEOFF DUE TO THE MAIN BAGGAGE DOOR WARNING LIGHT ILLUMINATING DURING THE TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 17604 IAW MEL 52-3 ON THE DOOR WARNING SYSTEM. MAINTENANCE LATER CLEARED DMI 17604 ON 3-23-96 BY INSPECTING AND RERIGGING THE BAG DOOR MICROSWITCHES. AIRCRA FT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996050200555 19960502 00555 EU 1996 5 2 VTZA96136 1 19960323 A 5270 WARNING LIGHT JETAIR JETSTM JETSTM4101 1500501 EU BAGG DOOR ILLUMINATING A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 322UE 41058 FLT NR 6215 - CHS-IAD - ABORTED TAKEOFF DUE TO THE MAIN BAGGAGE DOOR WARNING LIGHT ILLUMINATING DURING THE TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 17606 IAW MEL 52-3 ON THE DOOR WARNING SYSTEM. (M) 2 L 7 2 4T RT A41NM 1996050200556 19960502 00556 EU 1996 5 2 VTZA96137 1 19960312 A 5270 WARNING LIGHT JETAIR JETSTM JETSTM4101 1500501 EU BAGG DOOR ILLUMINATED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 322UE 41058 FLT NR 6330 - IAD - PIT - ABORTED THE TAKEOFF, DUE TO THE BAGGAGE DOOR WARNING LIGHT ILLUMINATING ON THE TAKEOFF ROLL. A IRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 17598 IAW MEL 52-3. MAINTENANCE LATER CL EARED DMI 17598 BY PERFORMING AN INSPECTION IAW J41 MM CHAPTER 52-70, BUT NOTED NO DEFECTS. AIRCRAFT WAS RELEASED AND A PPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996050200557 19960502 00557 EU 1996 5 2 VTZA96143 1 19960403 A 3411 PITOT BAG JETSTM JETSTM3201 1500217 EU LT SYSTEM WATER CONTAM A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 480UE 894 FLT NR 6372 - IAD-ALB - ABORTED TAKEFOFF DUE TO 30 KT AIRSPEED SPLIT BETWEEN INDICATOR. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE DRAINED EXCESSIVE WATER FROM PILOTS PITOT SYSTEM, INSPECTION AND OPS CHECK OK. AIRC RAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M0 2 L 7 2 4T RT A56EU 1996050200558 19960502 00558 EU 1996 5 2 VTZA96144 1 19960403 A 7600 21188408 IEC JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 315UE 41033 FLT NR 6167 - IAD-LGA - DURING CRUISE, RETURNED TO IAD DUE TO RIGHT ENGINE TORQUE INDICATION FLUCTUATION 20 PERCENT, ENG INE PARAMETERS NORMAL. MX REMOVED AND REPLACED IEC. OPS CHECK OK. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. ( M) 2 L 7 2 4T RT A41NM 1996050200559 19960502 00559 EU 1996 5 2 VTZA96145 1 19960407 A 3260 ATG135026 UPLOCK SWITCH JETAIR JETSTM JETSTM4101 1500501 EU MLG FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 317UE 41031 FLT 6485 - IAD-JFK - DURING CLIMB, AN UNSCHEDULED LANDING AT IAD DUE TO GEAR HANDLE RED LIGHT WOULD NOT EXTINGUISH. MAI NTENANCE REMOVED AND REPLACED MAIN GEAR UPLOCK SWITCH. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996050200560 19960502 00560 EU 1996 5 2 VTZA96146 1 19960407 A 3233 6158D ACTUATOR BAG JETSTM JETSTM3201 1500217 EU LT/RT MLG REQ'D SERV A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 479UE 893 FLT 6248 - IAD-BGM - DURING CLIMB, MADE A UNSCHEDULED LANDING AT IAD DUE TO UNSAFE GEAR INDICATION. AIRCRAFT RETURNED T O GATE WITH NO FURTHER INCIDENTS. MAINTENANCE BLED MAIN GEAR ACTUATORS. OPS CHECKS OK. AIRCRAFT WAS RELEASED AND APPR OVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996050200561 19960502 00561 EU 1996 5 2 VTZA96147 1 19960404 A 5320 3151791 BAGGAGE POD BAG JETSTM JETSTM3201 1500217 EU FUSELAGE BIRD STRIKE A VTZA K NONE C F.O.D. AP APPROACH 1 EA 27 480UE 894 FLT NR 6274 - BUF-IAD - DURING APPROACH, LANDED AT IAD DUE TO BIRD STRIKE TO BAGGAGE POD. AIRCRAFT WENT TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED BAGGAGE POD, OPS CHECK OK. AIRCRAFT RELEASED AND APPROVED FOR RET URN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996050200562 19960502 00562 EU 1996 5 2 VTZA96148 1 19960408 A 5210 91SE16 SWITCH BAG JETSTM JETSTM3201 1500217 EU PAX DOOR DIRTY A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 488UE 907 FLT NR 6387 - IAD-SYR - DURING CRUISE, RETURNED TO IAD DUE TO THE MAIN PASSENGER DOOR WARNING LIGHT ILLUMINATED IN FLIGH T. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE CLEANED AND LUBED MICROSWITCH. AIRCRAFT WAS RELEAS ED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996050200563 19960502 00563 EU 1996 5 2 VTZA96149 1 19960402 A 5230 91SE16 SWITCH BAG JETSTM JETSTM3201 1500217 EU BAGGAGE POD BROKEN WIRE A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 487UE 906 FLT NR 6151 - IAD-PHF - DURING TAKEOFF, RETURNED TO IAD DUE TO POD DOOR WARNING CAPTION ILLUMINATED ON TAKEOFF ROLL. AI RCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI 03741 IAW MEL 52-1. MX LATER CLEARED DMI 037 41 ON 4-4-96 BY REPAIRING THE WIRE TO THE AFT MICROSWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. ( M) 2 L 7 2 4T RT A56EU 1996050200564 19960502 00564 WP 1996 5 2 Y2PA96015 1 19960402 A 5313 LONGERON DOUG DC9 DC915F 3022037 WP BS 332 CRACKED A Y2PA K NONE O OTHER IN INSP/MAINT 1 GL 23 194US 63928 47016 YIP - CRACKS IN NR 1 (.375 INCH) AND NR 2 (.5 INCH) LONGERONS, AT FUSELAGE STATION NR 332. FABRICATED AND INSTALLED REP AIR DOUBLERS IAW FLIGHT VEHICLES, INC DRAWING 'FUS-LONGERON 1 AND 2 R AT STATION 332 REPAIR'. THESE DATA DER, ON FAA FO RM 8110-3, DATED 3/31/96. INSTALLATION APPROVED BY REPAIR STATION ZIAR650A, ON FAA FORM 337, DATED 4/2/96. (M) 2 L 7 2 4F A6WE 1996050200565 19960502 00565 GL 1996 5 2 96ZZZX2191 2 19960101 A 7240 6870892 COMBUSTION CASE BELL 206 206L 1181522 SW ALLSN 250C 250C20B 03013 GL ARMPIT CRACKED A NYBA O OTHER J WARNING INDICATION CR CRUISE 1 EA 11 121NH 22324 961 27892 46610 CAE830074 WHILE IN CRUISE, PILOT NOTED ENGINE TOT WAS AT 800 DEGREES CELSIUS. MECHANIC INSPECTED ENGINE ASSY FOR EXTERNAL DAMAGE NOTING THE COMBUSTION CASE, PN 6870892-J, SN 27892, WAS CRACKED AT ARMPIT REINFORCEMENT. DURING TEAR-DOWN INSPECTION, T HE FOLLOWING ITEMS WERE FOUND DAMAGED: 1ST STAGE FUEL NOZZLE, PN 6878496, SN C-89720 (804.0 TSO), AND LINER, PN 2305613 0, SN 10-82-401 (804.0 TSO). WHEN THE COMBUSTION CASE SEAM RUPTURED, THE AIR FLOW WAS REDUCED TO THE FUEL NOZZLE CAUSIN G DAMAGE TO THE NOZZLE AND LINER. REPLACED COMBUSTION CASE, 1ST FUEL NOZZLE AND COMBUSTION LINER, PN 23056130, IAW ALLI SON 250-C20 MM. 1 G 7 1 3U 3 U H2SW E4CE 1996050200566 19960502 00566 SW 1996 5 2 96ZZZX2192 1 19960411 A 7810 206064600005 EXHAUST STACK BELL 206 206L4 1182110 SW ENGINE CRACKED A A NYBA K NONE O OTHER IN INSP/MAINT 1 EA 11 123NH 3886 52076 DURING A DAILY INSPECTION AT THE LAST FLIGHT OF THE DAY, THE MECHANIC NOTED THE ENGINE EXHAUST STACK WAS CRACKED. THE C RACK ORIGINATED AT THE CENTER WELDED SEAM APPROXIMATELY 2 INCHES FROM THE FLANGE ON THE FORWARD SIDE OF THE STACK. THE CRACK CONTINUED DOWNWARD AND CONTINUED APPROXIMATELY 4 INCHES ALONG THE WELDED SEAM OF THE FLANGE. REPLACED THE EXHAUST STACK, PN 206-064-300-005, IAW BELL 206L-4 MM. 1 G 7 1 3U NC H2SW 1996050200567 19960502 00567 SW 1996 5 2 96ZZZX2193 1 19960411 A 7810 206064300005 EXHAUST STACK BELL 206 206B 1181511 SW ENGINE CRACKED A NYBA K NONE O OTHER IN INSP/MAINT 1 EA 11 125NH 3144 52099 DURING A DAILY INSPECTION AT THE LAST FLIGHT OF THE DAY, THE MECHANIC NOTED THE ENGINE EXHAUST STACK WAS CRACKED. THE C RACK ORIGINATED AT THE CENTER WELDED SEAM APPROXIMATELY 2 INCHES FROM THE FLANGE ON THE FORWARD SIDE OF THE STACK. THE CRACK CONTINUED DOWNWARD AND CONTINUED APPROXIMATELY 4 INCHES ALONG THE WELDED SEAM OF THE FLANGE. REPLACED THE EXHAUST STACK, PN 206-064-300-005, IAW BELL 206L-4 MM. 1 G 7 1 3U H2SW 1996050200568 19960502 00568 SW 1996 5 2 96ZZZX2194 1 19960402 A 6220 206310005101 BOLT 206011100159 BELL 206 206B 1181511 SW M/R HUB LOOSE A NYBA K NONE O OTHER IN INSP/MAINT 1 EA 11 125NH 847 HB560 52099 DURING DAILY INSPECTION, MECHANIC NOTED 2 EACH PILLOW BLOCK BOLTS, PN 206-310-005-101, LOOSE (TORQUE AT 55 INCHES/POUNDS ), DIAGONALLY OPPOSED. DURING LAST 100-HOUR INSPECTION (89.0 TSI) BOLTS WERE FOUND PROPERLY TORQUED. RETORQUED PILLOW BLOCK BOLTS IAW BELL ASB206L-92-79. 1 G 7 1 3U H2SW 1996050200569 19960502 00569 NE 1996 5 2 96ZZZX2195 1 19960402 A 6210 S161520201041 BLADE SKRSKY S58T S58ET 8141803 NE M/R LEAKAGE A NYBA K NONE O OTHER IN INSP/MAINT 1 EA 11 26567 2640 581514 DURING A 3-HOUR BIM CHECK, PILOT NOTED A RED BIM INDICATION. DURING A PRELIMINARY INSPECTION, LEAKAGE HAS BEEN NOTED TO BE EMANATING FROM THE SEAM BETWEEN POCKETS 19 AND 18. REPLACED BLADE IAW SIKORSKY S-58T MM. 2 G 7 2 4U 1H11 1996050200572 19960502 00572 SW 1996 5 2 96ZZZX2198 1 19960312 A 6230 206010335001 LEVER ASSY 206010350021 BELL 206 206B3 1181506 SW PYLON WORN B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 116AL 509 2389 DAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH PN 206-010-338-00 1 SPACERS, 4 EACH PN 206-010-337-001 BEARINGS, 2 EACH PN 206-010-338-003 BUSHINGS, 2 EACH PN NAS6605D64 BOLTS, AND 1 EAC H PN 206-010-470-101 BEARING. SUBMITTER STATED NORMAL USE CAUSES PARTS TO WEAR OUT TOO SOON. WORN PARTS TT 508.5 HOURS . 1 G 7 1 3U H2SW 1996050200573 19960502 00573 SW 1996 5 2 96ZZZX2199 1 19960312 A 6230 206010336005 LINK IDLER 206010350021 BELL 206 206B3 1181506 SW PYLON WORN B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 116AL 509 2389 DAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH PN 206-010-338-00 1 SPACERS, 4 EACH PN 206-010-337-001 BEARINGS, 2 EACH PN 206-010-338-003 BUSHINGS, 2 EACH PN NAS6605D64 BOLTS, AND 1 EAC H PN 206-010-470-101 BEARING. SUBMITTER STATED NORMAL USE CAUSES PARTS TO WEAR OUT TOO SOON. WORN PARTS TT 508.5 HOURS . 1 G 7 1 3U H2SW 1996050200580 19960502 00580 SW 1996 5 2 96ZZZX2206 1 19960312 A 6230 206010335001 LEVER ASSY 206010350021 BELL 206 206L1 1182107 SW PYLON WORN B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 2758L 461 45266 DAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH PN 206-010-338-00 1 SPACERS, 4 EACH PN 206-010-337-001 BEARINGS, 2 EACH PN 206-010-338-003 BUSHINGS, 2 EACH PN NAS6605D64 BOLTS, AND 1 EAC H PN 206-010-470-101 BEARING. SUBMITTER STATED NORMAL USE CAUSES PARTS TO WEAR OUT TOO SOON. WORN PARTS TT 461.1 HOURS . 1 G 7 1 3U H2SW 1996050200581 19960502 00581 SW 1996 5 2 96ZZZX2207 1 19960321 A 6230 206010336005 LINK IDLER 206010350021 BELL 206 206L1 1182107 SW PYLON WORN B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 2758L 461 45266 DAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH PN 206-010-338-00 1 SPACERS, 4 EACH PN 206-010-337-001 BEARINGS, 2 EACH PN 206-010-338-003 BUSHINGS, 2 EACH PN NAS6605D64 BOLTS, AND 1 EAC H PN 206-010-470-101 BEARING. SUBMITTER STATED NORMAL USE CAUSES PARTS TO WEAR OUT TOO SOON. WORN PARTS TT 461.1 HOURS . 1 G 7 1 3U H2SW 1996050200589 19960502 00589 SW 1996 5 2 96ZZZX2215 1 19960315 A 5313 214031431105 LONGERON BELL 214 214ST 1182106 SW LT T/B ATTACH CRACKED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 390AL 3612 28198 DAILY INSPECTION FOUND CRACK AT UPPER LEFT TAIL BOOM ATTACH POINT, AIRFRAME SIDE. THIS LONGERON BASE IS ONE OF ONLY FOU R ATTACH POINTS. THE UPPER LEFT CARRIES HIGHEST LOADS. 2 G 7 2 4U H10SW 1996050200590 19960502 00590 1996 5 2 96ZZZX2216 4 19960308 A 3416 A30 ENCODER BOLKMS 105 BO105CBS 5626008 EU NOSE COMPARTMENT BURNED A ALGA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 03 5412J 52 48725 S784 IN CRUISE FLIGHT, AN ODOR OF BURNING WIRE WAS NOTED. AFTER INSPECTING AIRCRAFT, FOUND A-30 ENCODER HAD A BURNED SMELL. REMOVED A-30 ENCODER AND INSTALLED SERVICEABLE ENCODER. PERFORMED INTEGRATED SYSTEM TEST. TESTED OK. SUSPECT CAUSE W AS MOISTURE INFILTRATION INTO UNIT. 1 G 7 2 3U NC H3EU 1996050200593 19960502 00593 WP 1996 5 2 AALA960480 1 19960326 A 3350 P401005111 MODULE DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 287AA 0049 49299 ORD - DURING OVERNIGHT CHECK, FOUND FORWARD SERVICE EXIT SIGN INOPERATIVE. REPLACED NR 1 EMERGENCY LIGHT CONTROL AND BA TTERY PACK. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1996050200594 19960502 00594 WP 1996 5 2 AALA960491 1 19960328 A 3350 L201011 SPOTLIGHT DOUG DC9 DC982 3022082 WP FWD ENTRY DOOR DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 479AA 49654 DFW - DURING OVERNIGHT CHECK, FORWARD EMERGENCY LIGHT SPOTLIGHT FOUND INOPERATIVE. REPLACED EMERGENCY SPOTLIGHT. SYSTE M GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1996050200595 19960502 00595 WP 1996 5 2 AALA960493 1 19960329 A 3260 SS092200017021 SWITCH DOUG DC9 DC982 3022082 WP LT POWER LEVER DEFECTIVE A AALA O OTHER N FALSE WARNING CL CLIMB 1 SW 07 7539A 49993 DFW - FLT 2093 - AFTER TAKEOFF PBI DURING CLIMB, RED GEAR LIGHT ILLUMINATED WITH GEAR HANDLE UP AND POWER LEVERS AT CLIM B POWER. ACCOMPLISHED QRH PROCEDURE AND AIRCRAFT PROCEEDED TO DFW, LANDING WITHOUT INCIDENT. REPLACED LEFT POWER LEVER SWITCH UNIT. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION . (X) 2 L 7 2 4F A6WE 1996050200596 19960502 00596 WP 1996 5 2 AALA960496 1 19960401 A 3350 LIGHT STRIP DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 488AA 49681 RDU - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FIRST CLASS CABIN FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR L IGHT STRIP IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1996050200597 19960502 00597 WP 1996 5 2 AALA960534 1 19960408 A 3350 CONDUCTOR DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 587AA 53250 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN AREA OF MID-CABIN FOUND INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT FLAT CONDUCTOR WIRE AT MID-CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1996050200598 19960502 00598 WP 1996 5 2 AALA960564 1 19960406 A 3350 A3060698101 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 219AA 49171 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY FLO OR LIGHT STRIP CONNECTOR BY FORWARD GALLEY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1996050200599 19960502 00599 WP 1996 5 2 AALA960578 1 19960411 A 3350 LIGHT STRIP DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 446AA 49472 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FORWARD PART OF MAIN CABIN FOUND INOPERATIVE. REPLACED EMERGENC Y FLOOR LIGHT STRIP IN FORWARD PART OF MAIN CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1996050200600 19960502 00600 NM 1996 5 2 CAL960425 1 19960329 A 3260 H10101531HA11 DNLOCK SWITCHES BOEING 727 727243 138408D NM NLG INOPERATIVE A CALA O OTHER N FALSE WARNING CL CLIMB 1 SW 09 571PE 21264 IAH - FLT 1902 - THE AIRCRAFT HAD A BRIEF HISTORY OF THE NLG RED UNSAFE LIGHT REMAINING ILLUMINATED AFTER GEAR RETRACTIO N. THE LIGHT EXTINGUISHED WHEN GEAR WAS CYCLED. MAINTENANCE REMOVED AND REPLACED THE NLG LOCK AND POSITION SWITCHES PE R MM 32-61-71, PAGE 401. A NOSE GEAR SWING WAS PERFORMED AND OPERATION CHECKED GOOD. (X) 2 L 7 3 4F RT A3WE 1996050200601 19960502 00601 NM 1996 5 2 CAL960430 1 19960331 A 2450 CIRCUIT BREAKER BOEING 737 7373T0 1384582 NM NR 1 XSFER BUS INOPERATIVE A A CALA O OTHER H ELECT. POWER LOSS-50 PC CR CRUISE 1 SW 09 70353 23591 PHL - FLT 1798 - ALL NORMAL POWER FAILED WHILE EN ROUTE FROM IAH TO PHL, WHEN THE NR 1 NORMAL TRANSFER BUS CIRCUIT BREAK ER TRIPPED APPROXIMATELY 300 MILES FROM PHL. THE AIRCRAFT WAS ON BATTERY POWER ONLY. THE AIRCRAFT LANDED AT PHL WITHOU T INCIDENT. MAINTENANCE OPERATED THE BUS TRANSFER SYSTEM OFF APU AND NR 1 ENGINE GENERATOR POWER. THE FAILURE COULD NO T BE DUPLICATED. THE NR 1 NORMAL TRANSFER BUS CIRCUIT BREAKER WAS REPLACED AS A PRECAUTIONARY MEASURE. OPERATION CHECK ED GOOD ON THE GROUND. (X) 2 L 7 2 4F RT A16WE 1996050200602 19960502 00602 NM 1996 5 2 CAL960453 1 19960410 A 2612 CONNECTOR BOEING 737 737217 1384464 NM NR 1 ENGINE SHORTED A CALA A E F UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 09 12230 19884 CAE - FLT 1598 - THE NR 1 ENGINE FIRE LIGHT FLICKERED OFF AND ON AND THEN THE FIRE LIGHT AND BELL CAME ON STEADY WHILE E N ROUTE FROM TPA TO GSO. THE NR 1 ENGINE WAS SHUT DOWN. ONE FIRE BOTTLE WAS DISCHARGED, BUT THE LIGHT REMAINED ON. TH E SECOND FIRE BOTTLE WAS DISCHARGED AND THE AIRCRAFT WAS DIVERTED TO CAE WHERE IT LANDED WTIHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE D1096 FIRE DETECT CONNECTOR PLUG WAS FOUND SHORTED. THE CONNECTOR WAS REPAIRED. IN ADD ITION, A REPAIR WAS MADE TO A CONNECTOR ON THE PYLON LOOP. NO OTHER FAULTS WERE NOTED. OPERATION OF THE FIRE DETECTION SYSTEM CHECKED GOOD DURING AN ENGINE RUN. BOTH ENGINE FIRE BOTTLES WERE REMOVED AND REPLACED. (X) 2 L 7 2 4F A16WE 1996050200603 19960502 00603 NM 1996 5 2 CAL960463 1 19960410 A 4990 380029815 APU GARRTT GTCP331200ER BOEING 757 757224 1384958 NM ACFT TAIL LEAKING OIL A CALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 17104 3075 P2162 27294 PHX - FLT 0134 - SMOKE WITH AN OILY ODOR APPEARED IN THE CABIN AT ABOUT LEVEL OFF WHILE EN ROUTE FROM LAX TO IAH. A DIV ERSION TO PHX WAS INITIATED. SMOKE CLEARED AT APPROX 10,000 FEET AND ACFT LANDED AT PHX WITHOUT INCIDENT. T/S BY MX FO UND EVIDENCE OF OIL STREAKING IN DUCT DOWNSTREAM OF APU BLEED SHUTOFF VALVE. APU PLACARDED INOPERATIVE. BURN-OUT PROCE DURES C/W PER MM 20-00-01, AND NO SMOKE PRODUCED. EVIDENCE OF OIL FROM COMPRESSOR SEAL OBSERVED AFTER REMOVING APU BLEE D AIR DUCT. REMOVAL OF APU IS PLANNED. SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING CORRECTIVE ACTION. SUPPLEMEN T: APU REMOVED AND REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD. PLACARD REMOVED. (X) 2 L 7 2 4F RT A2NM 1996050200604 19960502 00604 WP 1996 5 2 CAL960464 1 19960412 A 3231 UPLOCK SPRING DOUG DC9 DC932 3022066 WP RT MLG DOOR BROKEN A CALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 09 58545 47094 IAH - FLT 1453 - THE GEAR DOOR OPEN LIGHT ILLUMINATED IN-FLIGHT WITH HYDRAULIC SYSTEM ON LOW. A GEAR UPLATCH CHECK WAS PERFORMED AND THE LIGHT EXTINGUISHED AND REMAINED OUT. MAINTENANCE FOUND RT MLG DOOR UPLATCH MECHANISM SPRING BROKEN. T HE MECHANISM WAS REMOVED AND THE SPRING WAS REPLACED. THE MECHANISM WAS REINSTALLED IAW MM 32-31-4. AN EXTENSION AND R ETRACTION FOR THE LANDING GEAR WAS PERFORMED IAW MM 32-30-0, CODE 1 AND OPERATION CHECKED GOOD. (X) 2 L 7 2 4F A6WE 1996050200605 19960502 00605 WP 1996 5 2 CAL960465 1 19960413 A 3222 STRUT DOUG DC9 DC932 3022066 WP NLG FLAT A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 17543 45789 GSO - FLT 1147 - THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM GSO. 'ABNORMAL' PROCEDURES WERE C/W, BUT, THE GE AR HANDLE WOULD ONLY GO TO THE UPLATCH POSITION AND THE AIRCRAFT WOULD NOT PRESSURIZE. THE AIRCRAFT WAS RETURNED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NLG STRUT ALMOST FLAT. THE NOSE STRUT WAS FULLY SERVICED PER MM 32-21-2 AND THE SCHRADER VALVE WAS REPLACED. A NOSE GEAR RETRACTION WAS PERFORMED AND OPERATION CHECKED GOOD. (X) 2 L 7 2 4F A6WE 1996050200606 19960502 00606 WP 1996 5 2 CAL960466 1 19960327 A 5350 RETAINING CLIPS DOUG DC9 DC982 3022082 WP TAILCONE HANDLE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 71828 49488 HOU - THE FORCE REQUIRED TO PULL TAILCONE INTERIOR RELEASE HANDLE FROM RETAINING CLIPS WAS EXCESSIVE. THE RETAINING CLI PS WERE ADJUSTED PER MM 53-33-00. (X) 2 L 7 2 4F A6WE 1996050200607 19960502 00607 WP 1996 5 2 CAL960467 1 19960327 A 5350 LATCHES DOUG DC9 DC982 3022082 WP TAILCONE OUT OF RIG A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 71828 49488 HOU - THE FORCE REQUIRED TO RELEASE TAILCONE USING THE INTERIOR HANDLE EXCEEDED THE MAXIMUM LIMIT OF 35 POUNDS. THE TAI LCONE LATCHES WERE ADJUSTED PER MM 53-33-00. (X) 2 L 7 2 4F A6WE 1996050200608 19960502 00608 WP 1996 5 2 CAL960468 1 19960327 A 5350 RETAINING CLIPS DOUG DC9 DC982 3022082 WP TAILCONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 71828 49488 HOU - THE FORCE REQUIRED TO PULL EXTERIOR TAILCONE RELEASE HANDLE FROM RETAINING CLIPS WAS LOW. THE RETAINING CLIPS WER E ADJUSTED PER MM 53-53-00. (X) 2 L 7 2 4F A6WE 1996050200609 19960502 00609 NM 1996 5 2 CAL960469 1 19960411 A 5330 SKIN BOEING 737 7373T0 1384582 NM BS 480 PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14341 29445 23579 EWR - INSPECTION FOUND A 2 INCH BY 2 INCH PUNCTURE IN RT FUELAGE SKIN ABOVE WINDOW NR 8 AT STA 480. THE AREA WAS REPAIR ED IAW SRM 53-00-01, FIGURE 202. (X) 2 L 7 2 4F RT A16WE 1996050200610 19960502 00610 WP 1996 5 2 CAL960470 1 19960402 A 5320 SUBFLOOR WEB DOUG DC9 DC982 3022082 WP BS 160 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 71828 29029 49488 HOU - INSPECTION FOUND CORROSION ON SUBFLOOR WEB BELOW GALLEY NR 1 DRAIN PAN AT STA 160 (RT OTBD FLOOR, 4 INCH BY 5 INCH AREA, COMPLETELY THROUGH SKIN). THE CORROSION WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 53-01. (X) 2 L 7 2 4F A6WE 1996050200611 19960502 00611 WP 1996 5 2 CAL960471 1 19960329 A 5230 59101419 DOOR PAN DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 71828 29029 49488 HOU - INSPECTION FOUND A .50 INCH CRACK IN FORWARD CARGO DOOR INNER PAN. THE DOOR PAN WAS REPAIRED IAW SRM 52-05. (X) 2 L 7 2 4F A6WE 1996050200612 19960502 00612 WP 1996 5 2 CAL960472 1 19960403 A 5230 DOOR PAN DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 71828 29029 49488 HOU - INSPECTION FOUND A .50 INCH CRACK IN FORWARD CARGO DOOR OUTER PAN. THE DOOR PAN WAS REPAIRED IAW SRM 52-03. (X) 2 L 7 2 4F A6WE 1996050200613 19960502 00613 WP 1996 5 2 CAL960473 1 19960331 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP BS 1155 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 71828 29029 49488 HOU - INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1155. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51- 30-3. (X) 2 L 7 2 4F A6WE 1996050200614 19960502 00614 WP 1996 5 2 CAL960474 1 19960329 A 5320 BRACKET DOUG DC9 DC982 3022082 WP RT MLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 71828 29029 49488 HOU - INSPECTION FOUND A 1 INCH CRACK IN RIGHT WHEELWELL AFT INBOARD CORNER BRACKET. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-01. (X) 2 L 7 2 4F A6WE 1996050200615 19960502 00615 NM 1996 5 2 USAA960403 1 19960423 A 5330 SKIN BOEING 737 737201 1384454 NM BS 757 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 36906 22754 GSO - DURING 'WALK-AROUND', VISUAL INSPECTION FOUND 1.2 INCH CRACK IN FUSELAGE SKIN BS 767 AT STR 18 RIGHT. INSTALLED D OUBLER, REPAIRED SRM 53-30-3, FIGURE 6. (X) 2 L 7 2 4F A16WE 1996050200616 19960502 00616 WP 1996 5 2 USAAD96042 1 19960424 A 3260 PROX SENSOR DOUG DC9 DC981 3022081 WP LT MLG DOOR LOOSE A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 800US 48034 PIT - FL 1137 - CLIMBING OUT OF PHL EN ROUTE DTW, CREW RECEIVED A GEAR DOOR WARNING LIGHT. FLIGHT DIVERTED TO PIT AND L ANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE PROXIMITY SENSOR ON THE LEFT GEAR DOOR LOOSE. SENSOR WAS ADJUSTE D AND TIGHTENED. (M) 2 L 7 2 4F A6WE 1996050200617 19960502 00617 1996 5 2 USAASB96072 4 19960423 A 3442 6225135201 RADAR ANTENNA BOEING 737 7373B7 1384580 NM RADOME FAILED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 524AU 23859 IND - FLT 102 - ATTEMPTED TO USE WEATHER RADAR EN ROUTE. RADAR INOPERATIVE SHOWING 'NO WXR'. TEST SHOWED ANTENNA FAULT . MAINTENANCE FOUND WEATHER RADAR ANTENNA AT FAULT. REPLACED RADAR ANTENNA. TEST MADE. OKAY FOR SERVICE. (X) 2 L 7 2 4F RT A16WE 1996050200618 19960502 00618 NE 1996 5 2 USAASB96073 2 19960425 A 7200 ENGINE BOEING 737 737201 1384454 NM PWA JT8 JT8D15 52051 NE NR 1 BIRD STRIKE A USAA A UNSCHED LANDING C F.O.D. CL CLIMB 1 EA 19 249US 22756 PHL - FLT 819 - AIRCRAFT RETURNED TO FIELD DUE TO INGESTION OF BIRD IN NR 1 ENGINE. MAINTENANCE FOUND DAMAGE FROM BIRD INGESTION THAT WAS CAUSE FOR NR 1 ENGINE REPLACEMENT. (X) 2 L 7 2 4F 4 F A16WE E2EA 1996050800001 19960508 00001 WP 1996 5 8 MWEA96128 1 19960428 A 2560 5917689103 SLIDE COVER DOUG DC9 DC932 3022066 WP GALLEY SVC DOOR FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 203ME 47673 CREW REPORTS, GALLEY SERVICE DOOR EVACUATION SLIDE COVER FELL OFF. REINSTALLED EVACUATION SLIDE COVER. 2 L 7 2 4F A6WE 1996050900001 19960509 00001 NM 1996 5 9 9609492709 1 19960430 A 2751 1812993 FLAP INDICATOR BOEING 727 727225 1384077 NM TE FLAPS MALFUNCTIONED A NWAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 01 818EA 7863 469 22555 DURING CLIMB ON RETRACTION, OUTBOARD FLAPS STAYED AT 5 DEGREES WITH THE INBOARD FLAPS WENT TO 2 DEGREES AND STOPPED. AI RCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED BOTH INBOARD AND OUTBOARD FLAP INDICATORS. PERFORMED FLAP SYSTEM RIG CHECK. SYSTEM CHECKED OK. 2 L 7 3 4F A3WE 1996050900002 19960509 00002 NE 1996 5 9 9609502283 2 19960501 A 7230 COMPRESSOR BOEING 727 727251 138408H NM PWA JT8 JT8D7B 52053 NE NR 2 ENGINE STALLED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 01 283U 21322 653658 NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE FLIGHT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE ENGINE. NO DISCREPANCIES WERE NOTED. THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 1996050900003 19960509 00003 NM 1996 5 9 9609516308 1 19960501 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 668US 24223 DURING LINE CHECK, FOUND THE NR 3 RIGHT DOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED THE BATTERY CHARGER AND BATTERY. O PERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1996050900004 19960509 00004 WP 1996 5 9 9609529855 1 19960428 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP TAILCONE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 764NC 47717 DURING LINE CHECK, FOUND EMERGENCY LIGHTS IN TAILCONE WOULD NOT ARM OR TEST. REPLACED THE POWER SUPPLY B5-28 AND OPERA TIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996050900005 19960509 00005 NM 1996 5 9 9609726719 1 19960502 A 2720 CONNECTOR BOEING 747 747251F 1384898 NM RUDDER CONTROL DIRTY A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 619US 21321 DURING TAKEOFF, THE RUDDER RATIO LIGHT ILLUMINATED. ABORTED TAKEOFF AND RETURNED TO THE GATE. CLEANED LOWER AND UPPER RUDDER RATIO AMPLIFIER CANNON PLUGS. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996050900006 19960509 00006 EU 1996 5 9 9609733221 1 19960501 A 3260 848401 SENSOR AIRBUS 320 A320211 3930320 EU NLG DOOR MALFUNCTIONED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 321US 262 DURING APPROACH AFTER LANDING GEAR EXTENSION, RECEIVED 'L/G GEAR NOT DOWNLOCKED' AND 'L/G DOORS NOT CLOSED' MESSAGES. CY CLED THE LANDING GEAR HANDLE AND ALL INDICATIONS NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIG HT AFT NOSE LANDING GEAR DOOR OPEN PROXIMITY SENSOR (38GA). OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996050900007 19960509 00007 NM 1996 5 9 96UAL900303 1 19960501 A 3350 LIGHT STRIP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 562UA 26664 EMERGENCY ESCAPE LIGHT STRIP INOPERATIVE AT ROW 13 ABC. RESECURED EMERGENCY LIGHT STRIP AT ROW 13 ABC. OP CHECKS NORMA L. 2 L 7 2 4F 4 F RT A2NM E17NE 1996050900008 19960509 00008 1996 5 9 96UAL900304 4 19960501 A 2210 2588880901 YAW COUPLER BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE E/E COMPT MALFUNCTION A UALA K NONE F FLT CONT AFFECTED CR CRUISE 1 WP 29 995UA 22399 DURING TEN DEGREE RIGHT TURN EXPERIENCED FULL YAW DAMPER DEFLECTION TO THE LEFT. AUTOPILOT WAS ON, RUDDER AND AILERON T RIM WERE SET AT ZERO. SIGNIFICANT AILERON REQUIRED TO KEEP AIRPLANE LEVEL UNTIL YAW DAMPER WAS TURNED OFF. *S/D* REPL ACED YAW COUPLER. YAW COUPLER HAD RATE GYRO MALFUNCTION, SYSTEM CHECKS OK. 2 L 7 2 4F 4 F A16WE E2EA 1996050900009 19960509 00009 NM 1996 5 9 96UAL900305 1 19960501 A 3350 LIGHT STRIP BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 9008U 19046 EMERGENCY ESCAPE PATH LIGHTING AT ROW 12 INOPERABLE. REPLACED EMERGENCY ESCAPE PATH LIGHT STRIP. CHECKS O.K. 2 L 7 2 4F 4 F A16WE E2EA 1996050900010 19960509 00010 WP 1996 5 9 ABXA9600485 1 19960429 A 6120 LINKAGE NIHON YS11 YS11A500 6310416 WP RROYCE DART DART54210K 54522 EU ROTOL R2094 R209440 EU RT ENGINE NOT CONNECTED A ABXA O OTHER J WARNING INDICATION CR CRUISE 1 GL 23 911AX 2051 21310 DRG4667 RIGHT ENGINE HIGH STOP LIGHT ILLUMINATED IN FLIGHT AT APPROXIMATELY 5,000 FEET, 230 KNOTS AND 20 DEGREES CELSIUS. FOUND HIGH STOP LINKAGE UNDONE. RE-CONNECTED LINKAGE. GROUND OPS CHECKED GOOD. 2 L 7 2 4T 4 T A1PC E5EU 6 C P2EU 1996050900011 19960509 00011 WP 1996 5 9 ABXA9600487 1 19960430 A 3260 1EN16 DOWNLOCK SWITCH NIHON YS11 YS11A500 6310416 WP RT MLG DEFECTIVE A ABXA O OTHER J WARNING INDICATION TO TAKEOFF 1 GL 23 912AX 2052 AFTER DEPARTURE FROM RDU, RIGHT MAIN LANDING GEAR GREEN DOWN LIGHT REMAINED ON. RE-CYCLED LANDING GEAR AND THE LIGHT RE MAINED ILLUMINATED WITH GEAR UP. VISUALLY CONFIRMED RIGHT GEAR WAS UP AND CONTINUED TO ILN. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR DOWNLOCK SWITCH SI-905 I/A/W YS-11 M.M. 32-61-0. SWITCH RIGGED I/A/W YS-11 M.M. 32-61-1. GEAR SWING ACCOMPLISHED, CHECKED GOOD I/A/W YS-11 M.M. 32-30-0. 2 L 7 2 4T A1PC 1996050900012 19960509 00012 SO 1996 5 9 COMA9610137 1 19960426 A 3020 3D237606 CONTROL VALVE EMB 120 EMB120RT SO LT ENGINE INLET FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 205CA 11880 120205 LEFT INLET BOOT FAILED IN-FLIGHT. REPLACED LEFT INLET DEICE EJECTOR VALVE. 2 L 7 2 4T RT A31SO 1996050900013 19960509 00013 SO 1996 5 9 COMA9610138 1 19960429 A 5246 12048166003 FUEL DOOR EMB 120 EMB120RT SO RT WING UNLATCHED A COMA D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 247CA 120225 DOOR LIGHT ON M.A.P. ILLUMINATED ON TAKEOFF ROLL. SECURED FORWARD FASTENER ON INBOARD FUEL DOOR. 2 L 7 2 4T RT A31SO 1996050900014 19960509 00014 EA 1996 5 9 COMA9660076 1 19960430 A 2910 NAC16124 O-RING CNDAIR CL600 CL6002B19 EA NR 3 HYD SYST CUT A COMA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 946CA 7072 NR 3 HYDRAULIC SYSTEM LOST ALL FLUID IN CRUISE FLIGHT. REPLACED O-RING. 2 L 7 2 4F RT A21EA 1996050900015 19960509 00015 1996 5 9 DHL96702002 4 19960430 A 3422 25883024 DIRECTIONAL GYRO BOEING 727 72730C 1384009 NM NR 1 MALFUNCTIONED A T DHLA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 702DH 19793 ON CRUISE, COMPASS CARD IN HSI PRECESSES. REMOVED AND REPLACED DIRECTIONAL GYRO AND REMOVED WATER FROM E AND E BAY, MM 34-20. 2 L 7 3 4F A3WE 1996050900016 19960509 00016 NM 1996 5 9 DL72K960975 1 19960420 A 5330 65184203119 SKIN BOEING 727 727232 1384082 NM L1 DOOR CUTOUT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 479DA 20756 THE FUSELAGE SKIN AND UNDERLYING DOUBLER WAS FOUND TO HAVE A 0.6 INCH CRACK IN THE UPPER FORWARD CORNER OF THE L-1 DOOR CUT-OUT. A TIME LIMITED REPAIR WAS INSTALLED WITH THE PERMANENT TO BE INSTALLED AT HMV PER DL ERA 303491-14. 2 L 7 3 4F A3WE 1996050900017 19960509 00017 NM 1996 5 9 DL72L960971 1 19960423 A 3350 LIGHT BOEING 727 727232 1384082 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 514DA 21430 IRREGULAR EMERGENCY EXIT LIGHT ON LOWER SIDEWALL AT ROW 20A IS MISSING. INSTALLED LIGHT ASSY. CKS NORMAL. 2 L 7 3 4F A3WE 1996050900018 19960509 00018 NM 1996 5 9 DL72P961026 1 19960429 A 5522 SKIN BOEING 727 727225 1384077 NM RT ELEVATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8873Z 21291 1.25 INCH CRACK IN ELEVATOR LOWER SKIN AFT OF NR 2 RT BALANCE BOARD ACCESS PANEL. FOUND DURING C-LETTER CHECK. REPAIRE D PER SRM 55-20-3, FIG 4. 2 L 7 3 4F A3WE 1996050900019 19960509 00019 NM 1996 5 9 DL72S960586 1 19960314 A 5522 657278412 SKIN BOEING 727 727232 1384082 NM RT ELEVATOR DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 540DA 22386 DURING SHOP INSPECTION, RIGHT ELEVATOR WAS REPAIRED FOR SKIN DAMAGE PER SRM 55-20-3, REF DL ERA 303316-14. 2 L 7 3 4F A3WE 1996050900020 19960509 00020 NM 1996 5 9 DL72S960972 1 19960423 A 5754 SKIN BOEING 727 727232 1384082 NM NR 7 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 516DA 21432 FOUND ON A-1 LETTER CHECK, NR 7 SLAT COVE SKIN ATTACH ANGLE CRACKED .25 INCH AT TIA DUCT. REPAIRED PER M/M 57-54-0. 2 L 7 3 4F A3WE 1996050900021 19960509 00021 NM 1996 5 9 DL72S960973 1 19960423 A 5210 SKIN BOEING 727 727232 1384082 NM L1 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 516DA 21432 FOUND ON A-1 LETTER CHECK, FORWARD SERVICE DOOR SKIN CRACKED AT UPPER FORWARD CORNER .50 INCH AT 2 RIVETS. REPAIRED PER M/M 52-12-0. 2 L 7 3 4F A3WE 1996050900022 19960509 00022 NM 1996 5 9 DL72S960974 1 19960423 A 5754 RIB BOEING 727 727232 1384082 NM NR 4 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 516DA 21432 FOUND ON A-1 LETTER CHECK, CRACK IN NR 4 L/E SLAT NOSE RIB RADIUS OUTBOARD SIDE OF OUTBOARD TRACK. REPAIRED PER M/M 57 -54-0. 2 L 7 3 4F A3WE 1996050900023 19960509 00023 NM 1996 5 9 DL72S960976 1 19960408 A 5312 BLKHD STIFFENER BOEING 727 727232 1384082 NM BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 498DA 21142 A CRACK WAS FOUND EMANATING FROM THE BOTTOM OF THE LT FLANGE ON THE VERTICAL STIFFENER FS 1183 AT RBL 8. THE CRACK WAS APPROXIMATELY 0.25 INCH IN LENGTH. S/B 727-53-0175, REV 2, WHICH IS REQUIRED BY A.D. 90-06-09, CONTAINS INSPECTION, MOD IFICATION, AND REPAIR INSTRUCTIONS FOR THIS AREA. THE REMAINDER OF THE MOD WILL BE ACCOMPLISHED PER E.O. 4-59275-3AD AT THE NEXT OVERHAUL. 2 L 7 3 4F A3WE 1996050900024 19960509 00024 NM 1996 5 9 DL72S960977 1 19960419 A 5521 REAR SPAR BOEING 727 727232 1384082 NM LT ELEV CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 538DA HL24009LC 22076 THE REAR SPAR OF THE LT ELEVATOR IS CRACKED ON THE INBOARD SIDE OF THE THIRD FROM OUTBOARD HINGE FITTING. THE CRACK IS APPROXIMATELY .1250 INCH LONG. THE CRACK LENGTH IS WITHIN THE .250 INCH STOP DRILL LIMITS OF THE BAC S/B 727-55-0087. T HE CRACK WILL BE STOP-DRILLED UNTIL REPAIR/MODIFICATION PER DAL E.O. 4-57713-3AD. 2 L 7 3 4F A3WE 1996050900025 19960509 00025 NM 1996 5 9 DL72S960981 1 19960425 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 404DA 21148 AFT EXIT DOOR EMERGENCY LIGHT INOP. REPLACED M1089 EMERENCY BATTERY PACK. 2 L 7 3 4F A3WE 1996050900026 19960509 00026 NM 1996 5 9 DL72S960982 1 19960425 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 404DA 21148 ON LAYOVER, FOUND LT FORWARD OVERWING EMERGENCY LICHTS INOPERATIVE. REPLACED M654 EMERGENCY LIGHT BATTERY PACK. 2 L 7 3 4F A3WE 1996050900027 19960509 00027 NM 1996 5 9 DL72S960983 1 19960424 A 2782 ACTUATOR BRACKET BOEING 727 727232 1384082 NM NR 1 SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 402DA 21146 FOUND ON F1 LETTER CHECK, NR 1 SLAT ACTUATOR INBOARD MOUNT BRACKET CRACKED AT UPPER MOUNT BOLT. REPAIRED PER MM57-20-21 . 2 L 7 3 4F A3WE 1996050900028 19960509 00028 NM 1996 5 9 DL72S960984 1 19960424 A 5720 STIFFENER BOEING 727 727232 1384082 NM WING LE SPAR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 402DA 21146 FOUND ON F1 LETTER CHECK, 1.25 INCH CRACK AT L/E EDGE SPAR VERTICAL STIFFENER AFT OF NR 6 SLAT OUTBOARD TRACK OUTBOARD S IDE. REPLACED STIFFENER PER MM 57-20-21. 2 L 7 3 4F A3WE 1996050900029 19960509 00029 NM 1996 5 9 DL72S960985 1 19960424 A 2782 ACTUATOR BRACKET BOEING 727 727232 1384082 NM NR 5 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 402DA 21146 FOUND ON F1 LETTER CHECK, NR 5 LE FLAP ACTUATOR ATTACH ANGLE CRACKED. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1996050900030 19960509 00030 NM 1996 5 9 DL72S960986 1 19960424 A 5210 SKIN BOEING 727 727232 1384082 NM MAIN ENTRY DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 402DA 21146 FOUND ON LETTER CHECK, MAIN ENTRY DOOR UPPER AFT SKIN HAS A CRACK EXTENDING FROM FASTENER. REPAIR: REPAIRED PER M/M 52 -12-0, NR 10, FIG 806 10P PER PS 900-5-1, NR 04. 2 L 7 3 4F A3WE 1996050900031 19960509 00031 NM 1996 5 9 DL72S960987 1 19960424 A 3350 900835D BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 411DA 21223 ON LAYOVER, FOUND RT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1996050900032 19960509 00032 NM 1996 5 9 DL72S960994 1 19960425 A 3260 SWITCH BOEING 727 727232 1384082 NM RT MLG DOOR FAILED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 520DA 21471 RT GEAR DOOR LIGHT STAYED ON AFTER TAKEOFF AND RED DOORS LIGHT AT GEAR HANDLE. CYCLED GEAR DOOR. OPENED NORMALLY. FOR WARD RT GEAR DOOR INDICATION TO MCO AND PACKARD PER MEL 32-00-01. REPLACED SWITCH ON GEAR DOOR. OPS TEST OK. REMOVED MCO/PLAC. 2 L 7 3 4F A3WE 1996050900033 19960509 00033 NM 1996 5 9 DL72S960995 1 19960425 A 2782 ACTUATOR BRACKET BOEING 727 727232 1384082 NM NR 8 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 538DA 22076 NR 8 SLAT ACTUATOR MOUNT BRACKETS CRACKED OUTBOARD AND INBOARD SIDES. REPAIRED PER M/M 57-20-21. 2 L 7 3 4F A3WE 1996050900034 19960509 00034 NM 1996 5 9 DL72S960998 1 19960425 A 3246 WHEEL BEARING BOEING 727 727232 1384082 NM LT MAIN GEAR FAILED A A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 476DA 20753 ON TAXI IN TO GATE, NR 1 MAIN WHEEL ASSY LOCKED UP. FOUND NR 1 WHEEL ASSY DAMAGED. INBOARD WHEEL BEARING DESTROYED, AX LE CRACKED AND BROKEN AT INBOARD BEARING RACE. FOUND BRAKE ATTACH BOLT FROM ELEVEN O`CLOCK POSTION LAYING BETWEEN AXLE AND WHEEL ASSY. REPAIR WILL REQUIRE THE REPLACEMENT OF LT MAIN GEAR STRUT INTER-CYLINDER ASSY. 2 L 7 3 4F A3WE 1996050900035 19960509 00035 NM 1996 5 9 DL72S961003 1 19960426 A 5320 TORQUE BOX WEB BOEING 727 727232 1384082 NM BS 1213 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 535DA 22048 10635 FOUND ON B2 LETTER CHECK, .1875 INCH CRACK UPPER END OF TORQUE BOX WEB STA 1213 ABOVE STAIRWAY CLOSEOUT PANEL. REPAIRED PER MM 53-11-0. 2 L 7 3 4F A3WE 1996050900036 19960509 00036 NM 1996 5 9 DL72S961004 1 19960426 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 6 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 535DA 22048 10635 FOUND ON B2 LETTER CHECK, NR 6 SLAT COVE SKIN SUPPORT ANGLE CRACKED INBOARD END. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1996050900037 19960509 00037 NM 1996 5 9 DL72S961018 1 19960429 A 2810 TANK PLATE BOEING 727 727232 1384082 NM LT WING LEAKING A DALA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SO 27 499DA 21143 FUEL LEAK LEFT WING, IN-FLIGHT. REPORTED BY PASSENGER. DIVERTED ATL. FOUND FIFTH TANK PLATE FROM LT WING TIP LEAKING FUEL. SECURED TANK PLATE. NO LEAKS NOTED. 2 L 7 3 4F A3WE 1996050900038 19960509 00038 NM 1996 5 9 DL72S961027 1 19960430 A 3350 900542 BATTERY PACK BOEING 727 727232 1384082 NM CARGO DOOR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 409DA 21153 EMERGENCY ESCAPE FLOOD LIGHT ON CENTER CARGO DOOR IS ON ALL THE TIME. REPLACED RT OVERWING BATTERY PACK RACK. OPS CHEC KS GOOD. 2 L 7 3 4F A3WE 1996050900039 19960509 00039 NM 1996 5 9 DL72S961031 1 19960430 A 5320 TORQUE BOX WEB BOEING 727 727232 1384082 NM BS 1263 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 469DA 20746 FOUND ON C-2 LETTER CHECK, .50 INCH CRACK AT LOWER EDGE OF TORQUE BOX LIGHTING HOLE, STA 1263 RT SIDE. REPAIRED PER M/M 53-11-0. 2 L 7 3 4F A3WE 1996050900040 19960509 00040 NM 1996 5 9 DL72S961032 1 19960430 A 5530 STRINGER BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 469DA 20746 FOUND ON C-2 LETTER CHECK, STRINGER CRACKED TOP BAY RT SIDE AT ATTACH BOLT, INSIDE VERTICAL FIN. REPAIRED PER M/M 55-30 -0, FIGURE 803. 2 L 7 3 4F A3WE 1996050900042 19960509 00042 NM 1996 5 9 DL72S961034 1 19960430 A 5400 SEAL STRIKER BOEING 727 727232 1384082 NM NR 2 ENG CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 469DA 20746 FOUND ON C-2 LETTER CHECK, SEAL STRIKER FOR L/E OF RT FORWARD COWLS DAMAGED AT 3.00 AND 9.00 POSITIONS. REPAIRED PER M/ M 53-11-0, PAGE 801. 2 L 7 3 4F A3WE 1996050900043 19960509 00043 NM 1996 5 9 DL72W961019 1 19960422 A 5312 6516350 BULKHEAD FITTING BOEING 727 727247 138408F NM NR3 ENGINE MISDRILLED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 290WA 22108 WHILE ACCOMPLISHING A PRELIMINARY ATTEMPT TO FIT THE 65-18722-8 FORWARD MOUNT FITTING INTO POSITION, NOTED THAT SEVEN OF THE HOLES COMMON TO THE B.S. 1183 FRAME DO NOT LINE UP. THESE HOLES AND THE AMOUNT OF OFFSET ARE INDICATED ON FIGURE 1 . DL ERA 3033483-14 AUTHORIZES REWORK OF FS 1183 BULHEAD RING AND WEB. 2 L 7 3 4F A3WE 1996050900044 19960509 00044 NM 1996 5 9 DL72W961020 1 19960415 A 5312 6516350344 BLKHD WEB BOEING 727 727247 138408F NM BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2811W 20649 THE STA 1183 BULKHEAD WEB WAS FOUND CRACKED IN TWO LOCATIONS. THE DAMAGE WAS TRIMMED OUT WITH DIMENSIONS OF 2.6250 INCH AT LBL 8, WL 190 AND 8 INCH BY 3.1250 INCH AT LBL 14, WL 173. THE BULKHEAD WEB IS MANUFACTURED FROM 0.050 INCH CLAD 20 24-T3. THIS ER/A AUTHORIZES INSTALLATION OF A REPAIR DOUBLER. TPA MTC DISCOVERED AN ADDITIONAL CRACK JUST OUTBOARD OF THE BL ZERO STIFFENER AT APPROXIMATELY WL 170. AS A RESULT, A SINGLE TRIANGULAR CUT-OUT WAS MADE TO INCORPORATE THE ORI GINAL CRACK AT LBL 14 AND THE NEW CRACK DISCOVERED OUTBOARD OF BL ZERO. THE NEW CUT-OUT RUNS FROM APPROXIMATELY LBL 15 TO LBL 4. REPAIRS ERA 303452-14. 2 L 7 3 4F A3WE 1996050900045 19960509 00045 NM 1996 5 9 DL757960997 1 19960425 A 3350 LIGHT 767 BOEING 757 757232 1384965 NM OVERWING EXIT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 685DA 27588 LT FORWARD OVERWING EMERGENCY LIGHT INOPERATIVE. RELAMPED LT FORWARD OVERWING EMERGENCY LIGHT, CHECKS NORMAL. 2 L 7 2 4F RT A2NM 1996050900046 19960509 00046 NE 1996 5 9 DL757961007 2 19960427 A 7230 COMPRESSOR BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 ENGINE STALLED A DALA K NONE R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 27 675DL 29072 25980 716359 AFTER TAKEOFF AT 500 FEET, HAD 3 COMPRESSOR STALLS ON RT ENGINE, THROTTLE RETURNED TO IDLE. EMERGENCY DECLARED AND RETU RNED TO SFO WITH ENGINE AT IDLE. VISUALLY INSPECTED ENGINE AND CHECKED ALL CHIP DETECTORS AND MAIN OIL FILTER, ALL OK. BORESCOPE INSPECTION FOUND DAMAGE BEYOND LIMITS TO HPC STAGE 16. REPLACED RT ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 1996050900047 19960509 00047 NM 1996 5 9 DL757961008 1 19960426 A 3610 DUCT 114N150914 BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE RT WING LE FAILED A DALA K NONE D INFLIGHT SEPARATION TO TAKEOFF 1 SO 27 613DL 22820 716359 RIGHT BLOWOUT DOOR ASSY FORWARD OF RT WING LEADING EDGE PANEL. 611EB MISSING, REF. 57-2551-25 ITEM 75, CAUSED BY A BLOW N DUCT IN THE RT WING LEADING IPC REF 36-11-01-03, ITEM 145. 2 L 7 2 4F 4 F RT A2NM E17NE 1996050900048 19960509 00048 WP 1996 5 9 DLL10961000 1 19960425 A 2530 OVEN LKHEED 1011 10113851 5265010 WP LOWER GALLEY SMOKING A DALA F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 716DA 193C1095 SMOKE COMING FROM NR 6 OVEN. F/A USED FIRE EXTINGUISHER TO CONTROL SMOKE COMING FROM SMOLDERING FOOD IN OVEN. 2 L 7 3 4F A23WE 1996050900049 19960509 00049 WP 1996 5 9 DLL10961025 1 19960426 A 5330 1503141147 SKIN LKHEED 1011 10113851 5265010 WP FS 605 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 723DA 193C1150 THE FUSELAGE SKIN AT F.S. 605 AND STR 27 HAS BEEN CUT OUT DUE TO GROUND DAMAGE. ACCOMPLISHED REPAIRS PER DL ERA 273710- 14. 2 L 7 3 4F A23WE 1996050900050 19960509 00050 WP 1996 5 9 DLL13960979 1 19960423 A 3350 5165141 POWER SUPPLY LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 790DL 193A1143 EMERGENCY FLOOR TRACK LIGHTS IN D-ZONE INOPERABLE. ALSO, EXIT IDENTIFIERS INOPERATIVE AT LEFT AND RIGHT DOORS IN D-ZONE . C/A REPLACED BATTERY PACK AND POWER SUPPLY IN D-ZONE. CHECKS OK. 2 L 7 3 4F A23WE 1996050900051 19960509 00051 WP 1996 5 9 DLL13961001 1 19960426 A 2612 CONNECTORS 267201245 LKHEED 1011 10113851 5265010 WP NR 1 ENGINE DIRTY A DALA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 SO 27 787DL 193A1126 10635 NR 1 ENGINE FIRE INDICATION ON CLIMB-OUT ON A-LOOP (B-LOOP ON MCO). C/A REMOVED ALL CONNECTORS AND CLEANED 7 SECTORS. R EPLACED B-CONNECTORS, UPPER GAS FAIRING LOOP. BOTH SYSTEMS TEST OK. 2 L 7 3 4F A23WE 1996050900052 19960509 00052 WP 1996 5 9 DLL13961002 1 19960426 A 5210 MECHANISM LKHEED 1011 10113851 5265010 WP L1 DOOR JAMMED A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 786DL 193A1123 10635 ON ARRIVAL, L1 DOOR WOULD NOT OPEN. FOUND SHEET METAL INSULATION SHIELD OVER DOOR RIPPED LOOSE AND JAMMING DOOR. REMOV ED METAL DOOR. OPERATED NORMALLY. 2 L 7 3 4F A23WE 1996050900053 19960509 00053 WP 1996 5 9 DLL13961005 1 19960423 A 3350 TRACK LIGHT 0816322591 LKHEED 1011 10113851 5265010 WP CABIN MISSING A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 790DL 193A1143 10635 EMERGENCY FLOOR TRACK IS MISSING AT CROSS-AISLE BETWEEN 'C' AND 'D' ZONES. INSTALLED MISSING FLOOR TRACK. CHECKS NORMA L. 2 L 7 3 4F A23WE 1996050900054 19960509 00054 WP 1996 5 9 DLL13961006 1 19960423 A 3350 BATTERY PACK RPS1516574 LKHEED 1011 10113851 5265010 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 790DL 193A1143 10635 EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN 'D' ZONE. ALSO, LEFT AND RIGHT IDENTIFIER IN 'D' ZONE INOPERATIVE. REPLACE D 'D' ZONE EMERGENCY LIGHTS POWER SUPPLY AND BATTERY PACK. OPS CHECKS NORMAL. 2 L 7 3 4F A23WE 1996050900055 19960509 00055 WP 1996 5 9 DLL13961024 1 19960426 A 5312 1504400113 BULKHEAD WEB LKHEED 1011 10113851 5265010 WP BS 1212 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 790DL 193A1143 CRACKS WERE FOUND IN THE F.S. 1212 CANTED BULKHEAD WEB. THE DAMAGE WAS TRIMMED OUT, FILLED AND REINFORCED. ACCOMPLISHED REPAIRS PER DL ERS 273699-14. 2 L 7 3 4F A23WE 1996050900056 19960509 00056 WP 1996 5 9 DLL14960980 1 19960424 A 3350 POWER SUPPLY 5165741 LKHEED 1011 1011385115 5265015 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 737D 37712 193C1228 FOUND ON LAYOVER CHECK. R2 EMERGENCY EXIT SIGN AND F2 EMERGENCY EXTERIOR ILLUMINATION LIGHT INOPERATIVE. REPLACED POWE R SUPPLY. SYSTEM CHECKS NORMAL. 2 L 7 3 4F A23WE 1996050900057 19960509 00057 WP 1996 5 9 DLL16961040 1 19960430 A 2820 CHECK VALVE 112803 LKHEED 1011 10113853 5265020 WP 2L FUEL TANK FAILED A DALA K NONE K FLUID LOSS TO TAKEOFF 1 SO 27 759DA 193Y1176 AFTER TAKEOFF, TOWER INFORMED FUEL WAS VENTING FROM LEFT WING. PASSENGER INFORMED OF FUEL VENTING FROM LEFT WING TIP. CONFIRMED THIS. 2L TANK NOT FEEDING. TURNED OFF 2R PUMP AND 2L STARTED TO FEED. TRIED TO FEED OUT OF TANKS 1 AND 3 AND QUANTITY IN 2L STARTED TO INCREASE. FIRM CODE 28-24-43-14. REPLACED BYPASS CHECK VALVE MANIFOLD TO 2L BOOST PUMP BOX. OPERATION CHECKS OK. 2 L 7 3 4F A23WE 1996050900058 19960509 00058 NM 1996 5 9 DLM11960996 1 19960425 A 3350 0105606203 LIGHT DOUG MD11 MD11 3023602 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 809DE 48480 BATTERY 5 LOW MESSAGE AND EMERGENCY LIGHTS OUT AFT CABIN. REPLACED LIGHT ASSY. 2 L 7 3 4F RT A22WE 1996050900059 19960509 00059 NM 1996 5 9 DLM88961017 1 19960429 A 3230 59516395001 BUNGEE CYLINDER DOUG MD88 MD88 3023688 NM NOSE GEAR FAILED A DALA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 912DL 49543 LANDING GEAR WOULD NOT EXTEND, (NOSE GEAR) RECYCLED, NO NOSE GEAR. USED EMERGENCY EXTENSION, NOSE GEAR EXTENDED. REPLA CED NLG BUNGEE CYLINDER AND LUBED NLG. CYCLED NLG SEVERAL TIMES. OPS CKS NORMAL. 2 L 7 2 4F RT A6WE 1996050900060 19960509 00060 NM 1996 5 9 DLM88961021 1 19960429 A 3350 41B004AD073 BATTERY DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 902DE 53379 REPORTS OF LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS INTERMITTENT OR INOPERATIVE. REPLACED BATTERY PACKS FOR OVERWI NG EMERGENCY EXIT SIGNS. OPERATION CHECKS GOOD. 2 L 7 2 4F RT A6WE 1996050900061 19960509 00061 WP 1996 5 9 MWEA96126 1 19960502 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 240 PUNCTURED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 AIRCRAFT RECEIVED PUNCTURE IN SKIN WHILE PARKED IN MSN. APPROX .3750 INCH TEAR IN FUSELAGE AT STA 240 BETWEEN LONGERON 1 9 AND LONGERON 20R. FERRIED AIRCRAFT TO MKE FOR REPAIR. INSTALLED REPAIR IAW SRM 53-04, FIG. 38. 2 L 7 2 4F A6WE 1996050900062 19960509 00062 WP 1996 5 9 MWEA96127 1 19960501 A 5311 FRAME DOUG DC9 DC914 3022034 WP BS 525 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 DURING C-CHECK, FOUND FRAME CRACKED AT STA 525 BELOW FLOOR LEVEL. SPLICED IN NEW FRAME SECTION IAW SB 53-117 AND DRAWIN G NR 5932658. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F A6WE 1996050900063 19960509 00063 NM 1996 5 9 P5CA9600219 1 19960502 A 2710 DL1326M1192 ACTUATOR BOEING 747 747123 1384873 NM RT AILERON INOPERATIVE A P5CA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 859FT 20326 ON TAXI OUT DURING CONTROL CHECK, RIGHT OUTBOARD AILERON WOULD NOT UNLOCK WITH FLAPS IN TAKEOFF RANGE. REMOVED AND REPL ACED LOCK-OUT ACTUATOR IAW MM 27-11-16. OPS CHECK NORMAL. 2 L 7 4 4F A20WE 1996050900064 19960509 00064 NM 1996 5 9 SCNA96056 1 19960501 A 3350 900835A BATTERY PACK BOEING 727 7272J4 1384006 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 285SC 21676 FOUND LEFT FORWARD OVERWING EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK, OPS CHECK GOOD . 2 L 7 3 4F RT A3WE 1996050900065 19960509 00065 NM 1996 5 9 SCNA96057 1 19960411 A 5752 6521740501 TRIM TAB FITTING BOEING 727 7272J4 1384006 NM INBD AILERON CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 LEFT WING INBOARD AILERON TRIM TAB CONTROL FITTING WAS FOUND CORRODED. REMOVED AND REPLACED WITH NEW FITTINGS IN ACCORD ANCE WITH B727 MM, 27-10-11. 2 L 7 3 4F RT A3WE 1996050900066 19960509 00066 NE 1996 5 9 96ZZZX2219 2 19960415 A 7260 803605 ACCESSORY PAD DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 1 ENGINE CRACKED A CALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 83872 34850 6353 49120 708465 EWR - FLT 0480 - SMOKE ENTERED THE CABIN IMMEDIATELY AFTER TAKEOFF FROM BWI. THE AIRCRAFT WAS RETURNED TO BWI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND OIL LEAKING FROM THE NR 1 ENGINE FRONT ACCESSORY PAD WHICH WAS CRACKED IN SE VERAL PLACES. THE FRONT ACCESSORY PAD WAS REPLACED. A BURN-OUT OF HIGH PRESSURE PNEUMATIC DUCTING WAS PERFORMED IAW MM 21-20-02 BOTH COALESCER BAGS WERE REPLACED. THE NR 1 ENGINE WAS RUN AND OPERATION CHECKED GOOD WITH NO FURTHER SMOKE OBSERVED. (X) 2 L 7 2 4F 4 F A6WE E9NE 1996050900067 19960509 00067 WP 1996 5 9 CAL960475 1 19960327 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 240 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 71828 29029 49488 HOU - INSPECTION FOUND A 1 INCH WIDE BY .25 INCH DEEP DENT IN LEFT FUSELAGE SKIN ABOVE CUSP LINE AT STA 240. A REPAIR W AS INSTALLED IAW SRM 53-04, FIGURE 38. (X) 2 L 7 2 4F A6WE 1996050900068 19960509 00068 WP 1996 5 9 CAL960476 1 19960327 A 5320 DOUBLER DOUG DC9 DC982 3022082 WP AFT BAGGAGE BIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 71828 29029 49488 HOU - INSPECTION FOUND LOWER DOOR JAMB Z-ANGLE DOUBLER CORRODED IN AFT BAGGAGE BIN. A DOUBLER WAS FABRICATED AND INSTAL LED IAW SRM 51-30-4 AND SRM 51-30-5. (X) 2 L 7 2 4F A6WE 1996050900069 19960509 00069 WP 1996 5 9 CAL960477 1 19960329 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP BS 200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 71828 29029 49488 HOU - INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 200. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-30-2. (X) 2 L 7 2 4F A6WE 1996050900070 19960509 00070 WP 1996 5 9 CAL960478 1 19960327 A 5320 CUSP MEMBRANE DOUG DC9 DC982 3022082 WP BS 1300 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 71828 29029 49488 HOU - INSPECTION FOUND LT CUSP MEMBRANE CRACKED AT STA 1300. THE CRACK LENGTH WAS NOT IDENTIFIED. A DOUBLER WAS FABRIC ATED AND INSTALLED IAW SRM 53-05, FIGURE 96. (X) 2 L 7 2 4F A6WE 1996050900071 19960509 00071 WP 1996 5 9 CAL960479 1 19960327 A 5320 CUSP MEMBRANE DOUG DC9 DC982 3022082 WP BS 1300 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 71828 29029 49488 HOU - INSPECTION FOUND RT CUSP MEMBRANE CRACKED AT STA 1300. THE CRACK LENGTH WAS NOT IDENTIFIED. A DOUBLER WAS FABRIC ATED AND INSTALLED IAW SRM 53-05, FIGURE 96, SHEET 4. (X) 2 L 7 2 4F A6WE 1996050900072 19960509 00072 NM 1996 5 9 CAL960480 1 19960304 A 5730 SKIN BOEING 737 737130 1384435 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77215 66681 19032 GSO - INSPECTION FOUND A 1 INCH CRACK IN LEFT WING LEADING EDGE SKIN AT NR 2 SLAT AUXILIARY TRACK CUT-OUT. THE CRACKED AREA WAS CUT OUT. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-30-4, SR 51-10-2, AND SRM 51-30-2 . (X) 2 L 7 2 4F A16WE 1996050900073 19960509 00073 NM 1996 5 9 CAL960481 1 19960321 A 5320 ANGLE BOEING 737 737130 1384435 NM BS 663.75 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77215 66681 19032 GSO - INSPECTION FOUND A .75 INCH CRACK IN AFT UPPER ATTACH ANGLE AND A 1 INCH CRACK IN FORWARD ATTACH ANGLE OF RT PRESS URE PANEL AT BS 663.75. BOTH ANGLES WERE REMOVED. NEW ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND SRM 51- 10-2. (X) 2 L 7 2 4F A16WE 1996050900074 19960509 00074 NM 1996 5 9 CAL960482 1 19960321 A 5730 SKIN BOEING 737 737130 1384435 NM RT WING LE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77215 66681 19032 GSO - INSPECTION FOUND A 0.3 INCH CRACK IN RT WING LEADING EDGE SKIN ON OUTBOARD EDGE OF OUTBOARD SLAT TRACK CUT-OUT, WB L 304. THE CRACK WAS ROUTED OUT IAW ECRA 5720-01512. (X) 2 L 7 2 4F A16WE 1996050900075 19960509 00075 NM 1996 5 9 CAL960483 1 19960325 A 5751 SKIN BOEING 737 737130 1384435 NM RT AILERON DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77215 66681 19032 GSO - INSPECTION FOUND RT AILERON UPPER SURFACE DELAMINATED AT OUTBOARD END OF TRIM TAB CUT-OUT. THE DELAMINATED AREA W AS REMOVED. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-6, SRM 51-10-2, AND SRM 51-20-21. ( X) 2 L 7 2 4F A16WE 1996050900076 19960509 00076 NM 1996 5 9 CAL960484 1 19960325 A 5315 FLOOR BEAM BOEING 737 737130 1384435 NM BS 675 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77215 66681 19032 GSO - INSPECTION FOUND A 2 INCH CRACK IN RADIUS OF FLOOR BEAM LOWER T-CHORD AT BBL ZERO, STA 675. THE FLOOR BEAM CHORD WAS REPAIRED IAW ECRA 5710-01462 AND BOEING DRAWINGS 65C19643, 65C17173, ND 65C17103. (X) 2 L 7 2 4F A16WE 1996050900077 19960509 00077 NM 1996 5 9 CAL960485 1 19960327 A 5330 CHORD BOEING 737 737130 1384435 NM BS 727 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77215 66681 19032 GSO - INSPECTION FOUND LT OUTBOARD CHORD CRACKED PAST SECOND FASTENER HOLE AT STA 727. THE CHORD SEGMENT WAS REMOVED AN D RPELACED IAW BOEING DRAWING 65C33722. (X) 2 L 7 2 4F A16WE 1996050900078 19960509 00078 NM 1996 5 9 CAL960486 1 19960323 A 5313 STRINGER BOEING 737 737130 1384435 NM BS 294.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77215 66681 19032 GSO - INSPECTION FOUND STR 21R AND SKIN PANEL CORRODED AT STA 294.5. THE STRINGER AND SKIN PANEL WERE REMOVED. A NEW S TRINGER, SKIN SECTION, AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-30-3 AND SRM 53-10-4. (X) 2 L 7 2 4F A16WE 1996050900079 19960509 00079 NM 1996 5 9 CAL960487 1 19960323 A 5330 SKIN BOEING 737 737130 1384435 NM BS 259-306 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77215 66681 19032 GSO - INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 259 TO STA 306, STR 24L TO STR 27L. THE CORRODED SECTION OF SKIN W AS CUT OUT. A NEW SECTION OF SKIN AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-30-2. (X) 2 L 7 2 4F A16WE 1996050900080 19960509 00080 NM 1996 5 9 CAL960488 1 19960321 A 5320 CHORD BOEING 737 737130 1384435 NM BS 294.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77215 66681 19032 GSO - INSPECTION FOUND LOWER CHORD CORRODED AT LEFT AND RIGHT ENDS ON UPPER AND LOWER SURFACES OF HORIZONTAL FLANGE, STA 294.5. THE CORRODED CHORD SEGMENT WAS REMOVED AND A REPLACEMENT WAS INSTALLED IAW SRM 51-30-2, SRM 51-30-5, AND SRM 51 -10-2. (X) 2 L 7 2 4F A16WE 1996050900081 19960509 00081 NM 1996 5 9 CAL960489 1 19960321 A 5542 SKIN BOEING 737 737130 1384435 NM RUDDER DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77215 66681 19032 GSO - INSPECTION FOUND UPPER AFT TRAILING EDGE SECTION OF RUDDER DELAMINATING. THE LENGTH OF DELAMINATION WAS APPROXIMA TELY 12 INCHES. THE DELAMINATED SECTION OF RUDDER WAS REMOVED. A NEW CORE SECTION AND SKIN PLIES WERE FABRICATED AND B ONDED IAW SRM 51-40-9. (X) 2 L 7 2 4F A16WE 1996050900082 19960509 00082 NM 1996 5 9 CAL960490 1 19960303 A 5230 FRAME BOEING 737 737130 1384435 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77215 66681 19032 GSO - INSPECTION FOUND FORWARD CARGO DOOR INTERNAL FRAME WEB CRACKED. LOCATED AT BOTTOM AFT CORNER OF FIRST LOWER FRAME . THE CRACK LENGTH WAS NOT IDENTIFIED. THE CRACKED WEB WAS CUT OUT. REPAIRS WERE INSTALLED IAW SRM 51-40-2 AND SRM 51- 30-2. (X) 2 L 7 2 4F A16WE 1996050900083 19960509 00083 NM 1996 5 9 CAL960492 1 19960415 A 3350 BATTERY BOEING 737 737130 1384435 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 77215 19032 GSO - THE LEFT OVERWING EXTERIOR EMERGENCY LIGHTS FAILED CAPACITY CHECK. THE LEFT POWER SUPPLY BATTERY WAS REPLACED IAW MM 33-51-31 AND OPERATION OF THE LIGHTS WAS RESTORED. (X) 2 L 7 2 4F A16WE 1996050900084 19960509 00084 NM 1996 5 9 CAL960494 1 19960416 A 3610 PNEUMATIC DUCT BOEING 727 727224 1384076 NM NR 1 ENGINE RUPTURED A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 66734 69148 10420 20663 IAH - FLT 1876 - THE NR 1 ENGINE FIRE BELL AND LIGHT ACTIVATED AFTER TAKEOFF FROM IAH. THE ENGINE WAS RUN IN IDLE AND T HE NR 1 BLEED WAS TURNED OFF. THE FIRE WARNING CEASED. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDE NT. MAINTENANCE FOUND THE NR 1 ENGINE 8TH STAGE PNEUMATIC DUCT RUPTURED BETWEEN CHECK VALVE AND FIREWALL. THE DUCT WAS REPLACED. THE FIREWALL FIRE LOOP WAS REPLACED DUE TO HEAT DAMAGE. THE NR 1 ENGINE WAS RUN AND OPEATION CHECKED GOOD W ITH NO LEAKS FOUND. (X) 2 L 7 3 4F A3WE 1996050900085 19960509 00085 WP 1996 5 9 CAL960496 1 19960410 A 5532 SKIN DOUG DC9 DC932 3022066 WP VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17543 66930 45789 GSO - INSPECTION FOUND A 4 INCH BY 2 INCH HOLE AND SEVERAL CRACKS TOTALING 12 INCHES IN LENGTH IN SKIN PANEL ABOVE RUDDE R ON RIGHT SIDE OF VERTICAL STABILIZER. THE DAMAGED SKIN WAS CUT OUT. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND I NSTALLED IAW SRM 55-01 AND SRM 51-30-8. (X) 2 L 7 2 4F A6WE 1996050900086 19960509 00086 WP 1996 5 9 CAL960497 1 19960412 A 5543 TAB DOUG DC9 DC932 3022066 WP RUDDER DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17543 66930 45789 GSO - INSPECTION FOUND A 2 SQUARE INCH AREA OF RUDDER TAB LEADING EDGE DELAMINATED. THE AREA WAS REPAIRED USING BONDED DOUBLER AND FILLER. A WEIGHT AND BALANCE CHECK OF TAB WAS PERFORMED AFTER REPAIR. (X) 2 L 7 2 4F A6WE 1996050900087 19960509 00087 WP 1996 5 9 CAL960501 1 19960416 A 5350 2274640 RETAINING CLIP DOUG DC9 DC932 3022066 WP TAIL CONE MALFUNCTIONED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 27509 46350 47798 HOU - TAIL CONE EXTERIOR RELEASE HANDLE PULLS FROM CLIPS LESS THAN MINIMUM REQUIRED. INSTALLED NEW CLIPS AND ADJUSTED G AP PER MM 53-50-3. C/W PULL TEST PER MM 53-50-3, PULLED AT 29 INCHES/POUNDS. (X) 2 L 7 2 4F A6WE 1996050900088 19960509 00088 NM 1996 5 9 CAL960505 1 19960403 A 5312 BULKHEAD SKIN BOEING 737 7372C0 1384488 NM BS 540 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10242 70390 20071 GSO - CORROSION FOUND AT BS 540 BETWEEN 27L AND 26L. REMOVED DAMAGE FROM WEB. FABRICATED FILLER, DOUBLER AND SHIMS. A LODINED AND PRIMED FILLER DOUBLER AND SHIMS. INSTALLED FILLER, DOUBLER AND SHIMS IAW SRM 51-10-02 AND EC/RA 5710-01723. (X) 2 L 7 2 4F A16WE 1996050900089 19960509 00089 NM 1996 5 9 CAL960506 1 19960402 A 5312 BULKHEAD SKIN BOEING 737 7372C0 1384488 NM BS 540 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10242 70390 20071 GSO - CORROSION FOUND AT BS 540 BETWEEN 27R AND 26R. REMOVED CORRODED AREA AROUND PNEUMATIC DUCT. FABRICATED FILLER AN D DOUBLER. ALODINED AND PRIMED AS REQUIRED. INSTALLED FILLER AND DOUBLER IAW B737 SRM 51-10-2, SRM 51-30-2, AND EC/RA 5 710-01723. (X) 2 L 7 2 4F A16WE 1996050900090 19960509 00090 NM 1996 5 9 CAL960507 1 19960410 A 5315 FLOOR BEAM BOEING 737 7372C0 1384488 NM BS 986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10242 70390 20071 GSO - FLOOR BEAM AT STA 986 AT RBL 65 AND LAV SUPPORT CHANNEL CORRODED. REMOVED FLOOR BEAM CAP. FABRICATED NEW CAP AND INSTALLED PER B737 SRM 51-10-2, SRM 51-30-2, AND BOEING DWG 65-61381. REMOVED PARTITION SUPPORT AND REPLACED WITH NEW PART PER B737 SRM 51-10-2 AND SRM 51-30-2. (X) 2 L 7 2 4F A16WE 1996050900091 19960509 00091 NM 1996 5 9 CAL960508 1 19960401 A 5315 BAC1505100257 FLOOR BEAM BOEING 737 7372C0 1384488 NM BS 727 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10242 70390 20071 GSO - AFT PIT FLOOR BEAM CRACKED, STA 727B, STR 27R AND STR 27L. CRACK APPROXIMATELY .5 INCH IN EXTRUSION. FABRICATED REPAIR PARTS IAW B737 SRM 53-10-5. TREATED AND PRIMED IAW B737 SRM 51-10-2. INSTALLED PARTS. (X) 2 L 7 2 4F A16WE 1996050900092 19960509 00092 NM 1996 5 9 CAL960509 1 19960406 A 5321 FLOOR WEB BOEING 737 7372C0 1384488 NM BS 259.5 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10242 70390 20071 GSO - COCKPIT FLOOR HAS BULGING IN 2 PLACES AND CRACKED FLOOR WEB AT STA 259.5. CRACK LENGTH = .1250 INCH. CUT OUT AND REPLACED FLOOR SECTION AT BS 259.5. CORD SECTION CUT AND SPLICED, FLOOR SUPPORT REPAIRED, FLOOR BEAM WEB CUT AND SPLIC ED IAW B737, SRM 53-10-9, 51-40-2, 51-40-4, 51-10-2, AND 51-10-6. (X) 2 L 7 2 4F A16WE 1996050900093 19960509 00093 NM 1996 5 9 CAL960510 1 19960402 A 5311 FRAME BOEING 737 7372C0 1384488 NM BS 520 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10242 70390 20071 GSO - FRAME STA 520 CORRODED BETWEEN STR 28L AND STR 28R ON UPPER LEG. CUT OUT DAMAGED AREA 12 INCHES LONG BY 3 INCHES DEEP. FABRICATED L-ANGLE REPAIR AND FILLER PER B737, SRM 51-40-3 AND SRM 51-40-4. INSTALLED REPAIR IAW B737, SRM 51-40 -3 AND SRM 51-40-4. (X) 2 L 7 2 4F A16WE 1996050900094 19960509 00094 NM 1996 5 9 CALA960491 1 19960415 A 3350 BATTERY BOEING 737 737130 1384435 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 77215 19032 GSO - THE RIGHT OVERWING EXTERIOR EMERGENCY LIGHTS FAILED CAPACITY CHECK. THE RIGHT POWER SUPPLY BATTERY WAS REPLACED I AW MM 33-51-31 AND OPERATION OF THE LIGHTS WAS RESTORED. (X 2 L 7 2 4F A16WE 1996050900105 19960509 00105 NE 1996 5 9 96ZZZX2230 2 19960104 A 7230 BLADE BOEING 767 767259 1385136 NM PWA 4056 PW4056 NE NR 2 LPC FAILED W ANCF O OTHER X ENGINE FLAMEOUT DE DESCENT 1 SO 23 985AN 15475 15475 24618 717627 ON TOP OF DESCENT FINISHING FLIGHT 019 FROM FRA TO BOG, ENGINE NR 2 (RIGHT) FLAMED OUT. RESTART WAS NOT SUCCESSFUL. PR ELIMINARY INSPECTION SHOWED SOME ROTOR BLADES OF LOW PRESSURE COMPRESSION WERE DESTROYED. 2 L 7 2 4F 4 F RT A1NM E24NE 1996050900112 19960509 00112 NE 1996 5 9 96ZZZX2237 2 19960330 A 7321 5002T94G42 FUEL CONTROL LEAR 25 25D 5170514 CE GE CJ610 CJ6106 30006 NE LT ENGINE FAULTY A APMA E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CR CRUISE 1 EA 11 522GS 348 LEFT ENGINE WOULD NOT RESPOND TO POWER LEVER INPUT. ENGINE RPM INCREASED TO 100 PERCENT WITH POWER LEVER AT IDLE. ENGI NE SHUT DOWN (PRECAUTIONARY) VIA NORMAL PROCEDURE. LANDING MADE. T/S, REPLACED DEFECTIVE FUEL CONTROL AND PUMP ASSY. R EMOVED P/N 5002T94G42, S/N GAT 60192 AND PUMP ASSY, P/N 37E501242P107, S/N CGW 312740, AND INSTALLED FUEL CONTROL, P/N 5 002T94G42, S/N GAT 60015 FUEL PUMP, P/N 9234-AB, S/N CGW 312618. AIRCRAFT WAS GROUND RUN, LEAK CHECKED. OPS CHECKED, N O DEFECTS NOTED. 2 L 7 2 4J 4 J A10CE 1E16 1996050900113 19960509 00113 EA 1996 5 9 96ZZZX2238 1 19960309 A 5610 WINDSHIELD CNDAIR CL600 CL6002B16 1900305 EA COPILOT CRACKED A APMA B A EMER. DESCENT UNSCHED LANDING D INFLIGHT SEPARATION CR CRUISE 1 EA 11 48FU 5021 DURING A PART 91 REPOSITION FLIGHT AT FLIGHT LEVEL 350 FEET, CREW HEARD LOUD BANG AGAINST COPILOT'S WINDSHIELD. CLOSE E XAMINATION REVEALED A CRACK RUNNING DOWN CENTER OF COPILOT'S WINDSHIELD TOP-TO-BOTTOM OF NR 1 MAIN PLY. WHILE DESCENDIN G TO A LOWER ALTITUDE, A 6 INCH PIECE OF THE OUTER PLY SEPARATED AND DEPARTED AIRCRAFT. CREW DIVERTED TO LAX. WINDSHIE LD REPLACED BY GARRETT. 2 L 7 2 4F RT A21EA 1996050900121 19960509 00121 EA 1996 5 9 96ZZZX2246 2 19960301 A 8540 76327 GEAR BELL 47 47G5A 1181034 SW LYC O435 VO435B1A 41516 EA ASSORY DRV FAILED A P A HZXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 17 10231 582 ENGINE ABRUPTLY QUIT RUNNING WHILE ON GROUND. INVESTIGATION REVEALED ASSESSORY DRIVE GEAR, WHICH IS A TWO-PIECE GEAR AS SEMBLED AT THE FACTORY, HAD FAILED. THE 6 BOLTS THAT ATTACH THE 2 PIECES HAD SHEARED & THE 3 DOWELS THAT SHOULD BE A PR ESS FIT IN BOTH PIECES HAD FALLEN OUT. ACCORDING TO LYC, LOCKING TABS WHICH SAFETY THE BOLTS SHD BE INSTALLED SO THEY C OVER DOWELS, PREVENTING THEM FROM FALLING DOWN. TABS WERE INSTALLED IN A WAY THAT DID NOT COVER DOWEL PINS. IT APPEARE D THEY HAD BEEN LIKE THAT SINCE NEW. REPLACEMENT GEAR INSTALLED WHICH WAS A USED SERVICEABLE GEAR, ALSO HAD TABS INSTAL LED WRONG. SUBMITTER RECOMMENDS INSPECTION TO VERIFY INTEGRITY OF BOLTS & PROPER INSTALL OF DOWEL PINS & LOCKING TABS. 1 G 7 1 3O 3 O 2H3 E279 1996050900122 19960509 00122 EU 1996 5 9 96ZZZX2247 1 19960413 A 7931 81071010012 SWITCH AEROSP AS355 AS355F1 8680810 EU ENG OIL PRESS FAILED A EJYA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 07 911BB 70 5099 ON 4-13-96 SEVERAL MINUTES AFTER TAKEOFF, NR 1 ENGINE OIL PRESSURE DROPPED ALMOST TO ZERO. REPLACED NR 1 ENGINE OIL PRE SSURE SWITCH. SYSTEM OPERATIONAL CHECK GOOD. AIRCRAFT HOBBS TIME 141.5. 1 G 7 2 3U H11EU 1996050900123 19960509 00123 EU 1996 5 9 96ZZZX2248 1 19960414 A 7931 81071010012 SWITCH AEROSP AS355 AS355F1 8680810 EU ENG OIL PRESS FAILED A EJYA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 07 911BB 1 5099 ON 4-14-96 SHORTLY AFTER TAKEOFF, THE OIL PRESSURE DROPPED FROM 7 BARS TO 2.8 BARS. REPLACED NR 1 ENGINE OIL PRESSURE S WITCH. SYSTEM OPERATIONAL CHECK GOOD. AIRCRAFT HOBBS TIME 142.2. SECOND SWITCH FAILURE IN .7 HRS. 1 G 7 2 3U H11EU 1996050900124 19960509 00124 NE 1996 5 9 96ZZZX2249 2 19960328 A 7261 9752008044 SEAL SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE OIL FILTER FAILED A EJYA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 07 911MV 2926 2262 4225 DURING FLIGHT, ENGINE OIL FILTER SEAL FAILED CAUSING A LOSS OF ENGINE OIL. WARNING SYSTEM FUNCTIONED PROPERLY ALLOWING PILOT TIME TO LAND AIRCRAFT WITH NO DAMAGE. AIRCRAFT GROUND RUN 30 MINUTES AND MAGNETO PLUGS CHECKED, NO DEFECTS FOUND. AIRCRAFT WILL HAVE MAGNETO PLUGS CHECKED AFTER EACH FLIGHT FOR NEXT 25 HOURS OF FLIGHT. 1 G 7 1 3U 3 U NC H9EU E19EU 1996050900125 19960509 00125 WP 1996 5 9 9609539968 1 19960406 A 5320 DOOR JAMB DOUG DC9 DC931 3022065 WP CARGO DOOR CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9332 47264 DURING H-CHECK, FOUND CORROSION IN THE FORWARD CARGO DOOR LOWER JAMB PAN. REPAIRED PAN (P/N 5912494) PER EA 99-109426. 2 L 7 2 4F A6WE 1996050900126 19960509 00126 NM 1996 5 9 9609546718 1 19960412 A 5315 FLOOR BEAM BOEING 747 747251F 1384898 NM FS 620 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 618US 21122 DURING P-CHECK, FOUND CORROSION ON THE BS 620 FLOOR BEAM LOWER CHORD AT LBL 11. REPAIRED BEAM (P/N 65B38031-1) PER EA 6 7-99621. 2 L 7 4 4F A20WE 1996050900127 19960509 00127 NM 1996 5 9 9609556718 1 19960415 A 5315 FLOOR BEAM BOEING 747 747251F 1384898 NM FS 1300 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 618US 21122 DURING P-CHECK, FOUND A CRACK IN THE LBL 34 LONGITUDINAL FLOOR BEAM LOWER CHORD AT BS 1300. REPAIRED CHORD (P/N 65B1548 5-1) PER EA 67-99624. 2 L 7 4 4F A20WE 1996050900128 19960509 00128 NM 1996 5 9 9609562768 1 19960418 A 5320 FITTING BOEING 727 7272M7 138407S NM FS 1342 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 728RW 21741 DURING H-CHECK, FOUND A 1.50 INCH CRACK INSIDE THE UPPER LEFT TORQUE BOX AFT LOWER OUTBOARD CORNER END FITTING FS 1342. REPLACED FITTING PER SRM 51-10-1, PG. 4. 2 L 7 3 4F A3WE 1996050900129 19960509 00129 NM 1996 5 9 9609576623 1 19960418 A 5414 SKIN BOEING 747 747251B 1384892 NM NR 3 PYLON CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 623US 21705 DURING P-CHECK, FOUND A 2 INCH CRACK IN THE NR 3 PYLON INBOARD SKIN, NACELLE STA 180. REPAIRED SKIN PER EA 66-99629. 2 L 7 4 4F A20WE 1996050900130 19960509 00130 NM 1996 5 9 9609586623 1 19960419 A 5347 SEAT TRACK BOEING 747 747251B 1384892 NM FS 667 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 623US 21705 DURING P-CHECK, FOUND CORROSION ON THE RBL 33 SEAT TRACK AT BS 667. REPAIRED TRACK (P/N 65B23461-3) PER EA 66-99632. 2 L 7 4 4F A20WE 1996050900131 19960509 00131 NM 1996 5 9 9609596623 1 19960419 A 5315 FLOOR BEAM BOEING 747 747251B 1384892 NM FS 660 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 623US 21705 DURING P-CHECK, FOUND CORROSION ON THE BS 660 FLOOR BEAM, LBL 2 - RBL 34 UPPER CHORD UPPER SURFACE. REPAIRED BEAM (P/N 65B22606-4) PER EA 66-99634 AND 66-99633. 2 L 7 4 4F A20WE 1996050900132 19960509 00132 NM 1996 5 9 9609602768 1 19960422 A 5744 CASTING BOEING 727 7272M7 138407S NM AILERON CONTROL CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 728RW 21741 DURING H-CHECK, FOUND CORROSION ON THE MAGNESIUM SUPPORT CASTING FOR THE INBOARD AILERON CONTROL SECTOR. REPLACED CASTI NG PER SRM 51-10-1, PG. 4. 2 L 7 3 4F A3WE 1996050900133 19960509 00133 NM 1996 5 9 9609616718 1 19960423 A 5320 DOUBLER BOEING 747 747251F 1384898 NM FS 1339-1346 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 618US 21122 DURING P-CHECK, FOUND CORROSION ON THE UPPER SURFACE OF THE BONDED DOUBLER LOCATED OVER THE KEEL BEAM BOX UPPER WEB; BS 1339 - 1346, LBL 2 - 7, WL 116. REPAIRED DOUBLER (P/N 65B15069-288) PER EA 67-99636. 2 L 7 4 4F A20WE 1996050900134 19960509 00134 WP 1996 5 9 9609629859 1 19960424 A 5753 FLAP HINGE DOUG DC9 DC951 3022051 WP WS 164 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 768NC 48211 47729 DURING H-CHECK, FOUND CORROSION IN THE NR 2 FLAP FORWARD HINGE BOLT HOLES WS 164. REPLACED HINGE (P/N 5919218-506) PER CITEXT 90-5740-1-9800. 2 L 7 2 4F A6WE 1996050900135 19960509 00135 WP 1996 5 9 9609639859 1 19960425 A 5320 FITTING DOUG DC9 DC951 3022051 WP FS 701 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 768NC 47729 DURING H-CHECK, FOUND CORROSION ON THE LONGERON 28R END FITTING AT FS 701. REPLACED FITTING PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996050900136 19960509 00136 NM 1996 5 9 9609646623 1 19960425 A 5415 FITTING BOEING 747 747251B 1384892 NM NR 3 PYLON CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 623US 21705 DURING P-CHECK, FOUND A .3750 INCH CRACK IN THE NR 3 PYLON STRUT TO DIAGONAL BRACE ATTACH FITTING. REPLACED FITTING. 2 L 7 4 4F A20WE 1996050900138 19960509 00138 EU 1996 5 9 9609663216 1 19960426 A 5313 LONGERON AIRBUS 320 A320211 3930320 EU FS 13767-14300 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 316US 192 DURING IL CHECK, FOUND CORROSION ON STR 42R BETWEEN FRAMES 32 - 33. REPAIRED STRINGER PER EA 32-106870. 2 L 7 2 4F RT A28NM 1996050900139 19960509 00139 EU 1996 5 9 9609673216 1 19960426 A 5313 LONGERON AIRBUS 320 A320211 3930320 EU FS 14300-14834 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 316US 192 DURING IL CHECK, FOUND CORROSION ON STR 41R BETWEEN FRAMES 33 - 34. REPAIRED STRINGER PER EA 32-106869. 2 L 7 2 4F RT A28NM 1996050900140 19960509 00140 WP 1996 5 9 9609689941 1 19960427 A 5320 FITTING DOUG DC9 DC932 3022066 WP FS 996 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3324L 47103 DURING M-CHECK, FOUND A CRACK IN THE FS 996 FLOOR BEAM TO LONGERON 18L ATTACH FITTING. REPLACED FITTING (P/N 5913700-1) PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996050900141 19960509 00141 WP 1996 5 9 9609699859 1 19960427 A 5320 FITTING DOUG DC9 DC951 3022051 WP FS 693 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 768NC 47729 DURING H-CHECK, FOUND CORROSION ON THE LONGERON 29L END FITTING AT FS 693. REPLACED FITTING PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996050900142 19960509 00142 WP 1996 5 9 9609709973 1 19960429 A 5320 FITTING DOUG DC9 DC931 3022065 WP DOOR STOP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9337 47346 DURING M-CHECK, FOUND TWO CRACKED AFT CABIN DOOR STOP FITTINGS, RIGHT SIDE LOWER AND CENTER FITTINGS. REPLACED FITTINGS PER SRM 51-30-2. 2 L 7 2 4F A6WE 1996050900143 19960509 00143 WP 1996 5 9 9609719973 1 19960430 A 5320 FITTING DOUG DC9 DC931 3022065 WP FS 237 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9337 47346 DURING M-CHECK, FOUND CORROSION ON THE FS 237 FRAME TO LONGERON 18R FLOOR BEAM ATTACH FITTING. REPLACED FITTING PER SRM 51-30-1. 2 L 7 2 4F A6WE 1996050900144 19960509 00144 WP 1996 5 9 9609749866 1 19960501 A 3231 DOOR LINK DOUG DC9 DC951 3022051 WP NLG DOOR FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 775NC 47785 AFTER TAKEOFF DURING GEAR RETRACTION, A LOUD NOISE CAME FROM THE NOSE WHEEL AREA. UPLATCH CHECK WAS NORMAL, HOWEVER, AF TER 5 MINUTES, NOSE GEAR UNSAFE LIGHT ILLUMINATED. FOLLOWED COM PROCEDURE AND RETURNED TO MSP. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND THE RIGHT NOSE GEAR DOOR OPEN AND RIGHT GEAR DOOR LINK INOPERATIVE. REPLACED THE RIGHT GEAR DOOR LI NK AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996050900145 19960509 00145 NE 1996 5 9 9609756632 2 19960430 A 7530 7765555 EVBC BOEING 747 747251B 1384892 NM PWA JT9 JT9D7R4G2 52054 NE NR 1 ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 01 632US 17240 7331 23112 725320 DURING TAKEOFF, THE NR 1 ENGINE DID NOT ACCELERATE. ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACED THE ENGINE VANE BLEED CONTROL AND TRIMMED ENGINE. OPERATIONAL CHECK GOOD. PART TOTAL CYCLES, 2,343. 2 L 7 4 4F 4 F A20WE E3NE 1996050900146 19960509 00146 NE 1996 5 9 9609765635 2 19960430 A 7230 BEARINGS BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE NR 1 ENGINE FAILED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN J E WARNING INDICATION VIBRATION/BUFFET CR CRUISE 1 GL 01 536US 26482 727158 DURING CRUISE FLIGHT, THE NR 1 ENGINE OIL FILTER EICAS MESSAGE ENUNCIATED AND N2 VIBRATION LEVEL WAS 4.0 MAX. THE NR 1 ENGINE WAS SHUT DOWN AND THE AIRCRAFT DIVERTED TO CVG AND LANDED WITHOUT FURTHER INCIDENT. GROUND MAINTENANCE FOUND MET AL ON CHIP DETECTOR FOR THE NR 1, NR 2, AND NR 3 MAIN SHAFT BEARING COMPARTMENT. THE NR 1 ENGINE WAS REMOVED AND REPLAC ED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A2NM E17NE 1996050900147 19960509 00147 WP 1996 5 9 9609779925 1 19960430 A 3350 FUSE DOUG DC9 DC932 3022066 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 925US 47472 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD GALLEY SERVICE DOOR EMERGENCY EXIT SIGN AND FORWARD CABIN FLOOR PROXIM ITY EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996050900148 19960509 00148 WP 1996 5 9 9609789955 1 19960501 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 922RW 47182 DURING PERIODIC CHECK, FOUND FLOOR PROXIMITY LIGHTS AT AFT RIGHT EMERGENCY EXIT AND ROWS 14 THRU 17 INOPERATIVE. REPLAC ED BATTERIES. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996050900149 19960509 00149 WP 1996 5 9 9609799958 1 19960430 A 3350 CONNECTOR DOUG DC9 DC931 3022065 WP CABIN SHORTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 917RW 47145 DURING PREFLIGHT CHECK, FOUND AFT FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND POWER SUPPLY WITH NO HELP. FOUND PIN 10 ON CANNON PLUG TO POWER SUPPLY SHORTED OUT. SHOOK WIRING IN CATWALK AND AFT TAILCONE SLIDE AREA. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996050900150 19960509 00150 1996 5 9 9609809968 4 19960501 A 2565 113317 EVAC SLIDE DOUG DC9 DC931 3022065 WP FWD SERVICE DR FAILED BATT CHK A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9332 7790 1421 47264 DURING PERIODIC CHECK, FORWARD SERVICE DOOR EVACUATION SLIDE FAILED BATTERY TEST. REPLACED SLIDE. 2 L 7 2 4F A6WE 1996050900151 19960509 00151 WP 1996 5 9 9609819979 1 19960501 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9343 47439 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS AT ROWS 1 THRU 4 INOPERATIVE. REPAIRED BROKEN WIRE ABOVE GAL LEY COMPARTMENT. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996050900152 19960509 00152 WP 1996 5 9 9609829992 1 19960501 A 3260 SWITCH DOUG DC9 DC932 3022066 WP RT MLG DOOR MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 8960E 45869 LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. FLIGHT RETURNED TO PHX AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT MAIN GEAR DOOR LIGHT SWITCH. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996050900153 19960509 00153 WP 1996 5 9 9609839992 1 19960501 A 3260 STRIKER DOUG DC9 DC931 3022065 WP RT MLG DOOR OUT OF POSITION A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 8960E 45869 LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. FLIGHT RETURNED TO PHX AND LANDED WITHOUT INCIDENT. MAINTENANCE REPOSITIONED RIGHT MAIN GEAR DOOR LIGHT SWITCH STRIKER. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996050900154 19960509 00154 WP 1996 5 9 9609849992 1 19960501 A 3260 STRIKER DOUG DC9 DC931 3022065 WP RT MLG DOOR OUT OF POSITION A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 8960E 45869 LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. FLIGHT RETURNED TO PHX AND LANDED WITHOUT INCIDENT. MAINTENANCE REPOSITIONED RIGHT MAIN GEAR DOOR LIGHT SWITCH STRIKER. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996050900155 19960509 00155 NM 1996 5 9 96DHL72601C 1 19960410 A 5315 FLOOR BEAM BOEING 727 727228 NM BS 480 CORROSION A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT C-CHECK, FOUND CABIN FLOOR BEAM AT STA 480 SURFACE HAS MORE THAN 20 PERCENT OF MATERIAL REMOVED DUE TO CORROSION. CU T OUT SECTION OF FLOOR BEAM, INSTALLED REPAIR RBL ZERO TO RBL 32 PER SRM 53-10-8. 2 L 7 3 4F A3WE 1996050900156 19960509 00156 NM 1996 5 9 96FDEA00881 1 19960502 A 5753 6521630174 SKIN BOEING 727 72725 1384006 NM RT TE FOREFLAP DISBONDED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 RIGHT WING INBOARD FOREFLAP INBOARD RUB STRIP MISSING. UPON FURTHER INVESTIGATION, FOUND A 7.50 INCH BY 3.25 INCH PRE VIOUS REPAIR IN RUB STRIP AREA TO BE DISBONDED. ******S/D****** REPAIRED DAMAGED SKIN TO RIGHT WING INBOARD FOREFLAP RU B STRIP AREA IAW FEDEX SRM 51-40-6. 2 L 7 3 4F A3WE 1996050900157 19960509 00157 NM 1996 5 9 96FDEA00887 1 19960502 A 3610 CLAMP BOEING 727 727233 138408A NM NR 3 ENGINE LOOSE A FDEA H DEACTIVATE SYST/CIRCUITS J M WARNING INDICATION OVER TEMP CL CLIMB 1 SO 25 282FE 22349 AT 3,000 FEET ON DEPARTURE, NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. RIGHT DUCT PRESSURE ROSE STEADILY AND NR 3 EN GINE BLEED TRIPPED. WING ANTI-ICE WAS CLOSED. FOLLOWED RED TABS AND WENT TO 1 PACK OPS (NR 2 PACK AND NR 2 AND NR 3 BL EED OFF). STRUT LOWER AFT BODY HEAT TEST WAS PERFORMED AND TESTED GOOD. PRESSURE REMAINED GOOD. INSPECTED ENGINE AN D STRUT FOR AIR LEAKS AND DAMAGED DUCTS. FOUND LARGE AIR LEAK AT CLAMP ON BLEED VALVE AND PRECOOLER. REPAIRED LEAK AND REPLACED BLEED AIR PRESSURE REGULATOR. SYS OPS CK'D GOOD PER JET RUN HANDBOOK. 2 L 7 3 4F RT A3WE 1996050900158 19960509 00158 NM 1996 5 9 96FDEA00888 1 19960502 A 5315 FLOOR BEAM BOEING 727 72725 1384006 NM BS 680 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 DAMAGED FLOOR BEAM (LOWER) DUE TO SCREW PROTRUSION CHAFING AT BS 680, LBL-RBL 18 (11 PLACES) WL 200. REMOVED DAMAGED A REA. FABRICATED REPAIR PARTS, DRILLED, AND INSTALLED. WORKED IAW FEDEX SRM 53-10-8, FIG 2. 2 L 7 3 4F A3WE 1996050900159 19960509 00159 NM 1996 5 9 96FDEA00889 1 19960502 A 5313 BAC1498138 STRINGER BOEING 727 72725 1384006 NM BS 408 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 NR 0547 AND NR 029, CORROSION UNDER STANDOFF ON STR 28L AT BS 408. ******S/D****** COMING. 2 L 7 3 4F A3WE 1996050900160 19960509 00160 NM 1996 5 9 96UAL900307 1 19960502 A 3350 LIGHT STRIP BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 614UA 21875 EEL STRIP AT ROWS 10-12 RIGHT SIDE IS INOPERABLE. REPAIRED EEL STRIP, OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 1996050900161 19960509 00161 NM 1996 5 9 96UAL900308 1 19960502 A 5522 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE RT ELEVATOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7259U 21406 POSSIBLE CRACK IN LOWER SKIN SURFACE OF RIGHT ELEVATOR. *S/D* A 1.5 INCH CRACK CONFIRMED. REPAIRS ACCOMPLISHED IN AC CORDANCE WITH UA 727 MM 55-24-01. 2 L 7 3 4F 4 F A3WE E2EA 1996050900162 19960509 00162 NM 1996 5 9 96UAL900310 1 19960502 A 2820 INLET BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT FUEL PUMP BLOCKED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 550UA 25398 DURING CLIMBOUT, RIGHT FUEL PUMP ALTERNATED ON AND OFF. *S/D* INTERMITTENT PUMP OPERATION DUE TO PARTIAL BLOCKAGE OF P UMP INLET. BLOCKAGE CAUSED BY IN TANK DEBRIS. 2 L 7 2 4F 4 F RT A2NM E17NE 1996050900163 19960509 00163 NE 1996 5 9 96UAL900311 2 19960502 A 7260 769767 IMPELLER BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE NR 4 ENG GEARBOX FAILED A UALA A E UNSCHED LANDING ENGINE SHUTDOWN J R WARNING INDICATION PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 155UA 20104 AFTER TAKEOFF, DETECTED LOW OIL PRESSURE NR 4 ENGINE. ENGINE SHUTDOWN, FLIGHT RETURNED TO HNL. *S/D* MAIN GEARBOX DE- AERATOR IMPELLER DRIVE FAILED. REPLACED MAIN GEARBOX ASSY. 2 L 7 4 4F 4 F A20WE E20EA 1996050900164 19960509 00164 NM 1996 5 9 DL72S961037 1 19960501 A 5754 WEB 651622194 BOEING 727 727232 1384082 NM NR 5 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 527DA BN222 21587 WEB CRACKED BETWEEN RIBS NR 6 AND NR 7. REPAIRED PER SRM 57-54-00 DURING SHOP INSPECTION OF NR 5 LE SLAT. 2 L 7 3 4F A3WE 1996050900165 19960509 00165 NM 1996 5 9 DL72S961038 1 19960501 A 5754 RIB 651622194 BOEING 727 727232 1384082 NM NR 5 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 527DA BN222 21587 TWO CRACKS IN RIB NR 11. REPAIRED PER MM 57-54-00, FIG. 804 DURING SHOP INSPECTION OF NR 5 LE SLAT. 2 L 7 3 4F A3WE 1996050900166 19960509 00166 NM 1996 5 9 DL72S961039 1 19960501 A 5754 SKIN 651622194 BOEING 727 727232 1384082 NM NR 5 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 527DA BN222 21587 SKIN CRACKED AT OUTBOARD HOOK. REPAIRED PER SRM 57-50-3 FIG. 10 DURING SHOP INSPECTION OF NR 5 LE SLAT. 2 L 7 3 4F A3WE 1996050900167 19960509 00167 NM 1996 5 9 DL72S961048 1 19960423 A 5210 FRAME BOEING 727 727232 1384082 NM R2 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 401DA 21145 AT MID-VISIT, THE R2 DOOR FORWARD SIDE FRAME WAS FOUND CRACKED OUT OF UPPER HINGE CUTOUT LOWER RADIUS; ALSO, CORROSION F OUND AROUND AREA. AREA WAS REPAIRED PER SRM 52-40-2, FIG 4. 2 L 7 3 4F A3WE 1996050900168 19960509 00168 NM 1996 5 9 DL72S961050 1 19960501 A 3350 BATTERY PACK 6013211 BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 546DA 22677 LOWER LEFT SLIDE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, CHECKS NORMAL. 2 L 7 3 4F A3WE 1996050900169 19960509 00169 NM 1996 5 9 DL72S961051 1 19960501 A 3350 BATTERY PACK 900835A BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 403DA 12918 21147 LEFT OVERWING ESCAPE PATH AFT EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK IN POWER SUPPLY M654. 2 L 7 3 4F A3WE 1996050900170 19960509 00170 NM 1996 5 9 DL72S961052 1 19960501 A 3350 BATTERY PACK 900835A BOEING 727 727232 1384082 NM CABIN LOOSE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 403DA 21147 RIGHT OVERWING ESCAPE PATH AFT EMERGENCY LIGHT INOPERATIVE. RESEATED BATTERY PACK IN POWER SUPPLY M956. 2 L 7 3 4F A3WE 1996050900171 19960509 00171 NM 1996 5 9 DL72S961053 1 19960501 A 3350 6104789 BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 546DA 22677 AFT SERVICE DOOR LOWER LEFT SLIDE EMERGENCY LIGHT INOPERATIVE. FOUND ON LAYOVER. REPLACED BATTERY PACK FOR AFT LOWER L EFT AND RIGHT EMERGENCY LIGHT. CHECKS OK. 2 L 7 3 4F A3WE 1996050900172 19960509 00172 NM 1996 5 9 DL72S961057 1 19960501 A 5315 FLOOR BEAM BOEING 727 727232 1384082 NM BS 1110 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 418DA 21271 FOUND ON MV-1 CHECK CORROSION AT STA 1110, FLOOR BEAM LBL 12, REF N/R 123. REPAIR: REPAIRED PER M/M 53-20-11. 2 L 7 3 4F A3WE 1996050900173 19960509 00173 NM 1996 5 9 DL72W961035 1 19960430 A 3350 LIGHT 1001141 BOEING 727 727247 138408F NM AFT AIRSTAIRS INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 295WA 22532 AFT AIRSTAIRS EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSY AND BATTERIES. CHECKS NORMAL. 2 L 7 3 4F A3WE 1996050900174 19960509 00174 NM 1996 5 9 DL72W961044 1 19960501 A 2913 051791813 HYD PUMP 651791813 BOEING 727 727247 138408F NM B HYD SYST INOPERATIVE A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 292WA 162434 22110 FLT 893 - AIR TURN BACK DUE TO B-SYSTEM HYDRAULIC WENT TO ZERO WITH LOW PRESSURE LIGHT ON. A-SYSTEM AT 2.5 GALLONS. RE PLACED INBOARD B-SYSTEM HYDRAULIC PUMP AND FILTERS. REPLACED NR 5 SPOILER FILTER HOUSING PACKING. RESERVICED HYDRAULIC SYSTEM. OPS AND LEAK CHECK OK. 2 L 7 3 4F A3WE 1996050900175 19960509 00175 NM 1996 5 9 DL72W961047 1 19960428 A 3350 1060091102 LIGHT BOEING 727 727247 138408F NM L1 DOOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2809W 20581 EMERGENCY EXIT LIGHT AT L1 DOOR INOPERATIVE. REPLACED LIGHT ASSY AND BATTERIES. 2 L 7 3 4F A3WE 1996050900176 19960509 00176 NM 1996 5 9 DL767961046 1 19960501 A 3230 RETRACT MECH BOEING 767 767232 1385132 NM RT MLG MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 103DA 22215 AIRCRAFT'S ATB RIGHT MLG WOULD NOT RETRACT. PRESSURE GOOD. JACKED AIRCRAFT, CYCLED GEAR SERVERAL TIMES PER MM. CHECKS NORMAL. TILTED TRUCK, TURNED ON HYDRAULIC, TRUCK TILTED NORMAL. RETURNED TO SERVICE. 2 L 7 2 4F RT A1NM 1996050900177 19960509 00177 WP 1996 5 9 DLL13961036 1 19960430 A 3397 WIRE LKHEED 1011 10113851 5265010 WP CABIN DAMAGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 782DL 193A1006 EMERGENCY PATH LIGHTING IN FIRST CLASS SECTION INOPERATIVE. 2 L 7 3 4F A23WE 1996050900178 19960509 00178 NM 1996 5 9 QXEA9600163 1 19960430 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 817PH 056 PDX - COCKPIT EMERGENCY LIGHT IS INOPERATIVE. COCKPIT EMERGENCY LIGHT REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RE TURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1996050900179 19960509 00179 NM 1996 5 9 QXEA9600164 1 19960430 A 3350 82410162007 CONTROLLER DHAV DHC8 DHC8102 2809003 NM COAT CLOSET MALFUNCTIONING A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 817PH 056 BOI - EMERGENCY LIGHTS REMAIN ON WITH SWITCH IN THE OFF POSITION AND AIRCRAFT POWER ON. AIRCRAFT INSPECTED AND FERRIED TO PDX FOR REPAIR. EMERGENCY LIGHT CONTROLLER REPLACED AND LIGHTS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1996050900180 19960509 00180 NM 1996 5 9 SCNA96058 1 19960413 A 5320 BRACE BOEING 727 7272J4 1384006 NM BS 720 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT A FORWARD BRACE AT BS 720 IN THE FORWARD CARGO BAY WAS FOUND TO BE CORRODED AT THE NR 3 M OUNTING HOLE. CORROSION WAS MECHANICALLY REMOVED, THE AREA WAS TREATED, PRIMED, AND A REPAIR WAS FABRICATED AND INSTALL ED IN ACCORDANCE WITH B727 SRM 51-40-03 FIGURE 1, B727 SRM 51-10-02, AND MAINTENANCE MANUAL 51-20-11. 2 L 7 3 4F RT A3WE 1996050900181 19960509 00181 NM 1996 5 9 SCNA96059 1 19960410 A 5315 BAC15123353 FLOOR BEAM BOEING 727 7272J4 1384006 NM BS 1110 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT AN AFT CARGO FLOOR BEAM AND REPAIR WERE FOUND TO BE CORRODED AT APPROXIMATELY BS 1110, RB L 12 TO LBL 12. CORRODED SECTION WAS REMOVED, A NEW MEMBER WAS FABRICATED AND SPLICED IN ACCORDANCE WITH B727 SRM 53-10 -08. 2 L 7 3 4F RT A3WE 1996050900182 19960509 00182 NM 1996 5 9 SCNA96060 1 19960415 A 5311 FRAME BOEING 727 7272J4 1384006 NM BS 950 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT CORROSION WAS FOUND ON A CIRCUMFERENTIAL FRAME, FORWARD WEB, AND THE OUTBOARD SIDE OF THE LOWER CHORD AT APPROXIMATELY BS 950. THE CORROSION WAS MECHANICALLY REMOVED, THE AREA WAS TREATED, PRIMED, AND A DOUBL ER WAS FABRICATED AND INSTALLED IN ACCORDANCE WITH B727 SRM 51-40-02, FIGURE 1. 2 L 7 3 4F RT A3WE 1996050900183 19960509 00183 NM 1996 5 9 SCNA96061 1 19960418 A 5320 INTERCOSTAL BOEING 727 7272J4 1384006 NM BS 1050 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT CORROSION WAS FOUND ON AN INTERCOSTAL AT BS 1050. REMOVED CORRODED INTERCOSTAL, FABRICAT ED AND INSTALLED A NEW INTERCOSTAL IN ACCORDANCE WITH B727 SRM 51-40-04. 2 L 7 3 4F RT A3WE 1996050900184 19960509 00184 NM 1996 5 9 SCNA96062 1 19960414 A 5530 66133532 BOLT BOEING 727 7272J4 1384006 NM VERT STAB CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT CORROSION WAS FOUND AT THE VERTICAL STABILIZER TRAILING EDGE SPLICE BOLTS NR 3 AND NR 4 O F RS 124. REMOVED BOLTS, CLEANED CORROSION FROM THE HOLES, TREATED WITH LP5.3 AND INSTALLED NEW BOLTS IN ACCORDANCE WIT H B727 MM 51-20-11 AND MM 20-80-01. 2 L 7 3 4F RT A3WE 1996050900185 19960509 00185 NM 1996 5 9 SCNA96063 1 19960418 A 5320 WEB BOEING 727 7272J4 1384006 NM BS 1140-1148 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT, NUMEROUS AREAS OF CORROSION WERE FOUND ON A WEB ENCLOSURE IN THE AFT CARGO COMPARTMENT, APPROXIMATE BS 1140-BS 1148. MECHANICALLY REMOVED THE CORROSION, FABRICATED AND INSTALLED A NEW WEB IN ACCORDANCE WITH B727 SRM 51-40-02, FIGURE 1. 2 L 7 3 4F RT A3WE 1996050900186 19960509 00186 NM 1996 5 9 SCNA96064 1 19960412 A 5315 BAC14902831 FLOOR BEAM BOEING 727 7272J4 1384006 NM BS 1110 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT CORROSION WAS FOUND AROUND NUTPLATES ON A FLOOR BEAM AT APPROXIMATELY BS 1110 IN THE AFT GALLEY. MECHANICALLY REMOVED THE CORROSION, FABRICATED AND INSTALLED A NEW SECTION IN ACCORDANCE WITH B727 SRM 53-10-08 , FIGURE 3. 2 L 7 3 4F RT A3WE 1996050900187 19960509 00187 NM 1996 5 9 SCNA96065 1 19960413 A 5320 INTERCOSTAL BOEING 727 7272J4 1384006 NM BS 1035 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT CORROSION WAS FOUND ON AN INTERCOSTAL AT BS 1035. REMOVED INTERCOSTAL, FABRICATED AND IN STALLED A NEW INTERCOSTAL IN ACCORDANCE WITH B727 SRM 53-10-03. 2 L 7 3 4F RT A3WE 1996050900188 19960509 00188 NM 1996 5 9 SCNA96066 1 19960412 A 5347 BAC1520721 SEAT TRACK BOEING 727 7272J4 1384006 NM BS 1050-1130 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT CORROSION WAS FOUND ON A SEAT TRACK FLANGE BETWEEN BS 1050 AND BS 1130. REMOVED SEAT TRA CK, FABRICATED AND INSTALLED A NEW SEAT TRACK IN ACCORDANCE WITH B727 SRM 53-10-05. 2 L 7 3 4F RT A3WE 1996050900189 19960509 00189 NM 1996 5 9 SCNA96067 1 19960410 A 5347 BAC1520721 SEAT TRACK BOEING 727 7272J4 1384006 NM BS 1110-1130 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT CORROSION WAS FOUND ON A SEAT TRACK FLANGE AROUND CLIP NUT LOCATIONS BETWEEN BS 1110 AND BS 1130. REMOVED CORRODED SECTION OF SEAT TRACK, FABRICATED AND INSTALLED A NEW SEAT TRACK SECTION IN ACCORDANCE WITH B 727 SRM 53-10-05. 2 L 7 3 4F RT A3WE 1996050900190 19960509 00190 NM 1996 5 9 SCNA96068 1 19960417 A 5347 BAC1520792 SEAT TRACK BOEING 727 7272J4 1384006 NM BS 1110-1137 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT CORROSION WAS FOUND ON A SEAT TRACK BETWEEN BS 1110 AND BS 1137. REMOVED CORRODED SECTIO N OF SEAT TRACK, FABRICATED AND INSTALLED A NEW SEAT TRACK SECTION IN ACCORDANCE WITH B727 SRM 53-10-05. 2 L 7 3 4F RT A3WE 1996050900191 19960509 00191 NM 1996 5 9 SCNA96069 1 19960412 A 2810 10600313002 ACCESS PANEL BOEING 727 7272J4 1384006 NM FUEL TANK CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT CORROSION WAS FOUND ON THE RETAINING RING FOR THE FUEL TANK ACCESS PLATE AT 7340L. REMOV ED AND REPLACED WITH A NEW PANEL. 2 L 7 3 4F RT A3WE 1996050900192 19960509 00192 NM 1996 5 9 SCNA96070 1 19960415 A 5315 FLOOR BEAM BOEING 727 7272J4 1384006 NM BS 400 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT CORROSION WAS FOUND AROUND FASTENER HOLES ON THE TOP CAP OF A FLOOR BEAM AT BS 400, RBL 8 -28. REMOVED CORRODED SECTION, FABRICATED AND INSTALLED A REPAIR IN ACCORDANCE WITH B727 SRM 53-10-08. 2 L 7 3 4F RT A3WE 1996050900193 19960509 00193 NM 1996 5 9 SCNA96071 1 19960415 A 5347 BAC1520792 SEAT TRACK BOEING 727 7272J4 1384006 NM BS 610 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT CORROSION WAS FOUND ON SEAT TRACK SCALLOP CUT-OUTS AT APPROXIMATELY BS 610, RBL 24. REMO VED CORRODED SECTION, FABRICATED AND INSTALLED A REPAIR IN ACCORDANCE WITH B727 SRM 53-10-05, PAGE 18. 2 L 7 3 4F RT A3WE 1996050900194 19960509 00194 NM 1996 5 9 SCNA96072 1 19960415 A 5315 BAC1505100612 FLOOR BEAM BOEING 727 7272J4 1384006 NM BS 360 DAMAGED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT, FOUR HOLES WERE PARTLY DRILLED INTO THE UPPER SURFACE OF A FLOOR BEAM AT BS 360, LBL 6. REMOVED THE DRILL MARKED AREA, FABRICATED AND INSTALLED A REPAIR IN ACCORDANCE WITH B727 SRM 53-10-08. 2 L 7 3 4F RT A3WE 1996050900195 19960509 00195 NM 1996 5 9 SCNA96073 1 19960415 A 5315 BAC15061534 FLOOR BEAM BOEING 727 7272J4 1384006 NM BS 328-344 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT CORROSION WAS FOUND AROUND FASTENER HOLES ON THE TOP FLANGE OF A FLOOR BEAM AT BS 328-BS 344, LBL 30. REMOVED EFFECTED AREA, FABRICATED AND INSTALLED A REPAIR IN ACCORDANCE WITH B727 SRM 51-20-2. 2 L 7 3 4F RT A3WE 1996050900196 19960509 00196 NM 1996 5 9 SCNA96074 1 19960415 A 5347 BAC1520721T6511 SEAT TRACK BOEING 727 7272J4 1384006 NM BS 970-1010 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT THE LEFT HAND OUTBOARD SEAT TRACK WAS FOUND GOUGED AND CORRODED AT THE SCALLOP CUTOUT, AP PROXIMATELY BS 970-BS 1010. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED A REPAIR IN ACCORDANCE WITH B727 SRM 53-1 0-1. 2 L 7 3 4F RT A3WE 1996050900197 19960509 00197 NM 1996 5 9 SCNA96075 1 19960413 A 5311 65163279 FRAME BOEING 727 7272J4 1384006 NM BS 804 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT FOUND A FUSELAGE FRAME CRACKED AT BS 804, ABOVE STRINGER 13L, AND ATTACH CLIP HAS A SHEAR ED RIVET. REMOVED CRACKED SECTION, FABRICATED AND INSTALLED A REPAIR IN ACCORDANCE WITH B727 SRM 51-10-1 AND SRM 51-30- 2. REPLACED SHEARED RIVET IN ACCORDANCE WITH B727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 1996050900198 19960509 00198 NM 1996 5 9 SCNA96076 1 19960415 A 5347 BAC1520721T6511 SEAT TRACK BOEING 727 7272J4 1384006 NM BS 950 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT CORROSION WAS FOUND IN THE SCALLOPS OF A SEAT TRACK AT BS 950A-BS 950C, RBL 25. REMOVED CORRODED SECTION, FABRICATED AND INSTALLED A NEW SECTION IN ACCORDANCE WITH B727 SRM 53-10-5 2 L 7 3 4F RT A3WE 1996050900199 19960509 00199 NM 1996 5 9 SCNA96077 1 19960415 A 5347 BAC1520721T6511 SEAT TRACK BOEING 727 7272J4 1384006 NM BS 380-440 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT CORROSION WAS FOUND ON SEAT TRACK UPPER AND LOWER SURFACES AROUND FASTENER HOLES AT BS 38 0-BS 440, RBL 20. REMOVED CORRODED SECTION, FABRICATED AND INSTALLED A NEW SECTION IN ACCORDANCE WITH B727 SRM 53-10-2, FIGURE 7. 2 L 7 3 4F RT A3WE 1996050900200 19960509 00200 NM 1996 5 9 SCNA96078 1 19960415 A 5347 BAC1520721165V SEAT TRACK BOEING 727 7272J4 1384006 NM BS 400-440 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT CORROSION WAS FOUND ON SEAT TRACK UPPER AND LOWER SURFACES AROUND FASTENER HOLES AND SCAL LOP CUT-OUTS AT BS 400-BS 440, BL 45. REMOVED CORRODED SECTION, FABRICATED AND INSTALLED A NEW SECTION IN ACCORDANCE WI TH B727 SRM 53-10-5. 2 L 7 3 4F RT A3WE 1996050900201 19960509 00201 NM 1996 5 9 SCNA96079 1 19960411 A 5313 BAC1495146 STRINGER BOEING 727 7272J4 1384006 NM BS 1166-1183 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT CORROSION WAS FOUND ON STRINGER 25L, BS 1166-BS 1183. REMOVED CORRODED SECTION, FABRICAT ED AND INSTALLED A NEW SECTION IN ACCORDANCE WITH B727 SRM 53-10-3, FIGURE 2. 2 L 7 3 4F RT A3WE 1996050900202 19960509 00202 NM 1996 5 9 SCNA96080 1 19960412 A 5320 ANGLE BOEING 727 7272J4 1384006 NM R 1 DOOR SILL CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT CORROSION WAS FOUND ON R-1 DOOR SCUFF PLATE SUPPORT BRACKETS AND MOUNTING SURFACE. REMOV ED CORROSION, FABRICATED AND INSTALLED A NEW Z-ANGLE IN ACCORDANCE WITH B727 SRM 51-40-3. 2 L 7 3 4F RT A3WE 1996050900203 19960509 00203 NM 1996 5 9 SCNA96081 1 19960415 A 5320 FLOOR SUPPORT BOEING 727 7272J4 1384006 NM BS 385-420 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT CORROSION WAS FOUND ON FLOOR SUPPORT AROUND FASTENER HOLES AT BS 385-BS 420, RBL 14. REM OVED CORROSION, FABRICATED AND INSTALLED FLOOR BEAM REPAIRS IN ACCORDANCE WITH B727 SRM 51-40-4. 2 L 7 3 4F RT A3WE 1996050900204 19960509 00204 NM 1996 5 9 SCNA96082 1 19960422 A 5330 SKIN BOEING 727 727225 1384077 NM BS 268 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING HEAVY MAINTENANCE VISIT A CRACK WAS DISCOVERED IN THE SKIN AT THE BOTTOM FASTENER IN THE NOSE LANDING GEAR WHEELW ELL, RIGHT SIDE, APPROXIMATE BS 268.25, WL 148. STOP DRILLED CRACK, FABRICATED AND INSTALLED A DOUBLER AND STRAP REPAIR IN ACCORDANCE WITH B727 SB 727-53-0065 AND SRM 51-40-2. 2 L 7 3 4F A3WE 1996050900205 19960509 00205 NM 1996 5 9 SCNA96083 1 19960422 A 5330 SKIN BOEING 727 727225 1384077 NM BS 268 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING HEAVY MAINTENANCE VISIT A CRACK WAS DISCOVERED IN THE SKIN AT THE BOTTOM FASTENER IN THE NOSE LANDING GEAR WHEELW ELL, LEFT SIDE, APPROXIMATE BS 268.25, WL 148. STOP DRILLED CRACK, FABRICATED AND INSTALLED A DOUBLER AND STRAP REPAIR IN ACCORDANCE WITH B727 SB 727-53-0065 AND SRM 51-40-2. 2 L 7 3 4F A3WE 1996050900206 19960509 00206 NM 1996 5 9 9609846719 1 19960504 A 2720 RATIO CHANGER BOEING 747 747251F 1384898 NM RUDDER CONTROL FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 619US 21321 DURING CLIMB, THE RUDDER RATIO LIGHT ILLUMINATED AFTER RETRACTING THE FLAPS. RESET CIRCUIT BREAKER AND LIGHT REMAINED I LLUMINATED. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE UPPER RUDDER RATIO CHANGER. FLAP OPERA TIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996050900207 19960509 00207 NM 1996 5 9 9609852716 1 19960503 A 3350 BATTERY PACK BOEING 727 7272S7 138407Z NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 720RC 22491 DURING PREFLIGHT, FOUND AISLE EMERGENCY EXIT LIGHTS ADJACENT NR 1 GALLEY INOPERATIVE. REPLACED THE BATTERY PACK. CHECK ED OK. 2 L 7 3 4F A3WE 1996050900208 19960509 00208 NM 1996 5 9 9609862716 1 19960503 A 3350 POWER SUPPLY BOEING 727 7272S7 138407Z NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 720RC 22491 DURING PREFLIGHT, FOUND DOOR 2L AND 2R SLIDE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND POWER SUPPLY. LIG HTS CHECKED OK. 2 L 7 3 4F A3WE 1996050900209 19960509 00209 WP 1996 5 9 9609879994 1 19960502 A 2410 CSD DOUG DC9 DC931 3022065 WP RT ENGINE FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 8979E 47328 RIGHT CSD OIL PRESSURE LOW LIGHT ILLUMINATED DURING TAKEOFF ROLL AT 80 KNOTS. ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE DEFERRED THE RIGHT GENERATOR AND DISCONNECTED CSD PER MEL 21-1A. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996050900210 19960509 00210 NM 1996 5 9 9609882769 1 19960506 A 3350 BATTERY PACK BOEING 727 7272M7 138407S NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 729RW 21742 DURING PREFLIGHT, FOUND SLIDE LIGHTS AT DOOR 2R AND 2L INOPERATIVE. REPLACED AFT SLIDE LIGHT BATTERY PACKS. CHECKED OK . 2 L 7 3 4F A3WE 1996050900211 19960509 00211 NM 1996 5 9 9609892713 1 19960506 A 3350 BATTERY PACK BOEING 727 7272S7 138407Z NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 716RC 22021 DURING PREFLIGHT, FOUND AFT RIGHT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK. CHECKED OK. 2 L 7 3 4F A3WE 1996050900212 19960509 00212 NM 1996 5 9 9609902202 1 19960503 A 3350 BATTERY PACK BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 202US 22155 DURING PREFLIGHT, FOUND LEFT EMERGENCY GALLEY LIGHT INOPERATIVE. REPLACED BATTERY PACK. CHECKED OK. 2 L 7 3 4F A3WE 1996050900213 19960509 00213 NM 1996 5 9 9609915506 1 19960504 A 3350 POWER SUPPLY BOEING 727 727251 138408H NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 506US 23195 DURING PREFLIGHT, FOUND EMERGENCY LIGHTS LEFT SIDE AISLE OVERHEAD IN AFT GALLEY AND OVER DOOR 4L INOPERATIVE. REPLACED POWER SUPPLY M737. CHECKED OK. 2 L 7 3 4F A3WE 1996050900214 19960509 00214 NM 1996 5 9 9609922768 1 19960504 A 3350 LIGHT BOEING 727 7272M7 138407S NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 728RW 21741 DURING PREFLIGHT, FOUND EMERGENCY AREA LIGHT ABOVE ROW 38 INOPERATIVE. REPLACED BATTERY PACK AND LIGHT ASSEMBLY. CHECK ED OK. 2 L 7 3 4F A3WE 1996050900215 19960509 00215 NM 1996 5 9 9609932768 1 19960504 A 3350 LIGHT BOEING 727 7272M7 138407S NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 728RW 21741 DURING PREFLIGHT, FOUND EMERGENCY LIGHT ABOVE FOOT OF AIRSTAIRS INOPERATIVE. REPLACED BATTERIES AND LIGHT ASSEMBLY. CH ECKED OK. 2 L 7 3 4F A3WE 1996050900216 19960509 00216 WP 1996 5 9 9609949178 1 19960504 A 3350 BATTERY PACK DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 3310L 45705 DURING LINE CHECK, FOUND TAILCONE AREA CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED B5-28 POWER SUPPLY BATTERIES. OPE RATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996050900217 19960509 00217 WP 1996 5 9 9609959162 1 19960403 A 3350 BATTERIES DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8907E 45748 DURING LINE CHECK, FOUND LEFT OVERWING EMERGENCY LIGHTS DIM. REPLACED BATTERIES AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996050900218 19960509 00218 WP 1996 5 9 9609969150 1 19960503 A 3350 BATTERY PACK DOUG DC9 DC914 3022034 WP LT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8908E 45749 DURING LINE CHECK, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996050900219 19960509 00219 NM 1996 5 9 96FDEA00890 1 19960502 A 3260 UPLOCK SWITCH BOEING 727 72725 1384006 NM RT MLG MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 152FE 18285 RT MAIN GEAR DOOR LIGHT WOULD NOT GO OUT AFTER RAISING GEAR, LIGHT STAYED ON AFTER LANDING GEAR RECYCLED FOR LANDING. * S/D* REPLACED RT MLG DOOR UPLOCK SWITCH PER MM 32-62-11, OPS CKS NORMAL. 2 L 7 3 4F A3WE 1996050900220 19960509 00220 NM 1996 5 9 96FDEA00891 1 19960503 A 5754 65162262 BULLNOSE BOEING 727 72725 1384006 NM NR 5 LE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 CORROSION ON NR 5 K-FLAP AT 1/B BULLNOSE BONDING JUMPER UPPER ATTACH POINT. REPAIRED AREA PER FEDEX SRM 57-50-3. 2 L 7 3 4F A3WE 1996050900221 19960509 00221 NM 1996 5 9 96FDEA00893 1 19960503 A 5315 BAC1518391 FLOOR BEAM BOEING 727 72725 1384006 NM BS 560 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 505FE 18276 NR0481 AND 006, CORROSION (C53-224-01) ON BS 560 FLOOR BEAM AT LBL 36 TO 7, RBL 8 WL 208. *S/D* REMOVED CORRODED FLOOR BEAM UPPER FLANGE AT LBL 43.5, RBL 13.5 WL 208. FABRICATED REPAIR PARTS, CLEANED AND TREATED, FASTENED INTO PLACE IAW FEDEX SRM 53-10-8. 2 L 7 3 4F A3WE 1996050900222 19960509 00222 NM 1996 5 9 96FDEA00894 1 19960503 A 5330 6554583 SKIN BOEING 727 72725 1384006 NM BS 1178 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 505FE 18276 NR0438 AND 005, EXTERNAL SKIN HOLE IN SKIN BS 1178 AT STR 22L. *S/D* REMOVED DAMAGED SKIN AT BS 1178 STR 22L AND INS TALLED REPAIR DOUBLER AND FILLER. ALL WORK DONE PER FEDEX SRM 53-30-3. 2 L 7 3 4F A3WE 1996050900223 19960509 00223 NM 1996 5 9 96FDEA00895 1 19960506 A 5313 BAC1498138 STRINGER BOEING 727 72725 1384006 NM BS 414-420 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 505FE 18276 CORROSION ON STR 1 BS 414 TO 420. *S/D* COMPLETED REPAIR ON STR 1 BS 414 TO 420 PER FED EX SRM 53-10-3. 2 L 7 3 4F A3WE 1996050900224 19960509 00224 NM 1996 5 9 96FDEA00896 1 19960503 A 5315 FLOOR BEAM BOEING 727 72725 1384006 NM BS 640 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 505FE 18276 NR 0514 AND 003, CORROSION C53-224-01(1) ON UPPER FLANGE OF FLOOR BEAM BS 640 BETWEEN RBL 14 - 43, WL 208. *****S/D**** * COMING. 2 L 7 3 4F A3WE 1996050900225 19960509 00225 1996 5 9 96UAL900313 4 19960503 A 2564 SLIDE RAFT AIRCRUISERS 16D1719416 DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE CABIN DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 1854U 1476 47813 DOOR 3 LEFT OFFWING SLIDE/RAFT REMOVED FOR TIME LIMIT. SHOP FOUND RAMP PORTION OF SLIDE DAMAGED DUE TO SEPARATION OF TH E INTERNAL BULKHEADS. SCRAPPED RAMP PORTION OF SLIDE/RAFT. 2 L 7 3 4F 4 F A22WE E23EA 1996050900226 19960509 00226 NM 1996 5 9 P5CA9600220 1 19960505 A 5414 SKIN BOEING 747 747132 1384882 NM NR 2 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 DURING SCHEDULED ENGINE CHANGE, FOUND NUMEROUS CRACKS IN NR 2 PYLON BOTTOM PLATE. REPAIRED PER SRM 54-10-03, FIG. 3. 2 L 7 4 4F A20WE 1996050900227 19960509 00227 NM 1996 5 9 SCNA96084 1 19960430 A 3350 1012611 EXIT SIGN BOEING 727 727227 1384078 NM CABIN DAMAGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 275AF 22092 LEFT FORWARD LOWER EMERGENCY EXIT SIGN WAS FOUND BROKEN. REMOVED AND REPLACED EXIT SIGN ASSEMBLY. CHECKS OK. 2 L 7 3 4F A3WE 1996050900228 19960509 00228 NM 1996 5 9 SCNA96085 1 19960430 A 3350 900835A POWER SUPPLY BOEING 727 7272J4 1384006 NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 285SC 21676 LEFT FORWARD OVERWING EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED THE BATTERY POWER SUPPLY. O PS CHECKS OK. 2 L 7 3 4F RT A3WE 1996050900229 19960509 00229 NM 1996 5 9 UPS96220028 1 19960422 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1050 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE: D. SHEAR TIE IS CRACKED AT STA 1050 AND STR 4L. REMOVED SHEAR TIE AND FABRICATED REPLACEMENT PART IA W SRM 51-10-1 AND SRM 51-30-2. INSTALLED SHEAR TIE IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996050900230 19960509 00230 NM 1996 5 9 UPS96220029 1 19960422 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1050 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE: D. SHEAR TIE IS CRACKED AT STA 1050 AND STR 5L. REMOVED AND REPLACED SHEAR TIE AND FABRICATED REPLAC EMENT PART IAW SRM 51-10-1 AND SRM 51-30-2. INSTALLED SHEAR TIE IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996050900231 19960509 00231 NM 1996 5 9 UPS96220030 1 19960422 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1050 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE: D. SHEAR TIE IS CRACKED AT STA 1010 AND STR 5L. REMOVED AND REPLACED SHEAR TIE AND FABRICATED REPLAC EMENT PART IAW SRM 51-10-1 AND SRM 51-30-2, INSTALLED SHEAR TIE IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996050900232 19960509 00232 NM 1996 5 9 UPS96220031 1 19960422 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1050 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE: D. SHEAR TIE CRACKED AT STA 1050 AND STR 6L. REMOVED AND REPLACED PART IAW SRM 51-10-1 AND SRM 51-30 -2. INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996050900233 19960509 00233 NM 1996 5 9 UPS96220032 1 19960422 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1090 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE: D. SHEAR TIE CRACKED AT STA 1090 AND STR 7L. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996050900234 19960509 00234 NM 1996 5 9 UPS96220033 1 19960422 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1090 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE: D. SHEAR TIE IS CRACKED AT STA 1090, STR 6R. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996050900235 19960509 00235 NM 1996 5 9 UPS96220034 1 19960422 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1090 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE: D. SHEAR TIE IS CRACKED AT STA 1090, STR 5R. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996050900236 19960509 00236 NM 1996 5 9 UPS96220035 1 19960422 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1070 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE: D. SHEAR TIE IS CRACKED AT STA 1070, STR 6R. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996050900237 19960509 00237 NM 1996 5 9 UPS96220036 1 19960422 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1050 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE: D. SHEAR TIE IS CRACKED AT STA 1050, STR 6R. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996050900238 19960509 00238 NM 1996 5 9 UPS96220037 1 19960422 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1070 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE: D. SHEAR TIE IS CRACKED AT STA 1070, STR 6L. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996050900239 19960509 00239 NM 1996 5 9 UPS96220038 1 19960422 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1010 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE: D. SHEAR TIE IS CRACKED AT STA 1010, STR 4L. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996050900240 19960509 00240 NM 1996 5 9 UPS96220039 1 19960422 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 990 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE: D. SHEAR TIE IS CRACKED AT STA 990, STR 5L. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 SRM AND 5 1-30-2. 2 L 7 3 4F A3WE 1996050900241 19960509 00241 NM 1996 5 9 UPS96220040 1 19960422 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1010 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE: D. SHEAR TIE IS CRACKED AT STA 1010, STR 7L. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996050900242 19960509 00242 NM 1996 5 9 UPS96220041 1 19960422 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1010 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE: D. SHEAR TIE IS CRACKED AT STA 1010, STR 6L. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996050900243 19960509 00243 NM 1996 5 9 UPS96220042 1 19960422 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1030 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE: D. SHEAR TIE IS CRACKED AT STA 1030, STR 5L. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996050900244 19960509 00244 NM 1996 5 9 UPS96220043 1 19960422 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 990 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE: D. SHEAR TIE IS CRACKED AT STA 990, STR 9R. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-10-1 AND SRM 5 1-30-2. 2 L 7 3 4F A3WE 1996050900245 19960509 00245 NM 1996 5 9 UPS96220044 1 19960314 A 5320 ANGLE BOEING 727 72725C 138400H NM FS 1345 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE: C. LEFT SKIN SUPPORT ANGLE IS CRACKED AT FS 1345 AND FIN STA 22.5. REMOVED DAMAGED AREA IAW SRM 51-4 0-3 AND FABRICATED AND INSTALLED REPAIR IAW SRM 51-40-3. 2 L 7 3 4F A3WE 1996050900246 19960509 00246 NM 1996 5 9 UPS96220045 1 19960314 A 5330 SKIN BOEING 727 72725C 138400H NM BS 360 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE: C. LFEC INSPECTION REVEALED MATERIAL LOSS OF GREATER THAN 10 PERCENT, BUT LESS THAN 20 PERCENT ON AFT SIDE BS 360, BETWEEN STR 25L AND STR 26L. CUT OUT DAMAGED AREA AT AFT STA 360 BETWEEN STR 25L AND STR 26L. REPAIRED S KIN PER DRAWING NR 69-62161 AND SRM 51-30-2 AND EO B727-5310-1371. 2 L 7 3 4F A3WE 1996050900247 19960509 00247 NM 1996 5 9 UPS96220046 1 19960314 A 5320 SHEAR WEB BOEING 727 72725C 138400H NM FS 1185 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE: C. STA 1185, LBL 65 SHEAR WEB CORRODED BEYOND LIMITS. REMOVED DAMAGED AREA IAW SRM 51-40-2 AND FABRI CATED AND INSTALLED REPAIR DOUBLER IAW 51-40-2 AND 51-30-2. 2 L 7 3 4F A3WE 1996050900248 19960509 00248 NM 1996 5 9 UPS96420023 1 19960326 A 5311 FRAME BOEING 747 747123 1384873 NM BS 2220 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE: C. AREA AFT OF BULK CARGO COMPARTMENT, FOUND CRACKS IN FRAME SHEAR TIE DUE TO CORROSION AT BS 2220 NE AR RIGHT OUTFLOW VALVE BETWEEN STR 40 AND STR 44R. REPLACED FRAME AT BS 2220 RIGHT BETWEEN STR 44 AND STR 36R IAW SRM 5 1-30-02. 2 L 7 4 4F A20WE 1996050900249 19960509 00249 NM 1996 5 9 UPS96420024 1 19960326 A 5311 FRAME BOEING 747 747123 1384873 NM BS 2220 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE: C. AREA AFT OF BULK CARGO COMPARTMENT, FOUND CORROSION ON INNER FLANGE OF FRAME AT BS 2220 NEAR RIGHT OUTFLOW VALVE. CORROSION DAMAGES OUT OF LIMITS IAW SRM 51-10-01. REPLACED FRAME AT BS 2220 IAW SRM 53-10-01. 2 L 7 4 4F A20WE 1996050900250 19960509 00250 NM 1996 5 9 UPS96520019 1 19960501 A 5220 EMER EXIT WINDOW BOEING 757 75724APF 1384969 NM RT COCKPIT POPPED OUT A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 443UP 27388 INSPECTION TYPE: FIRST OFFICER'S EMERGENCY EXIT WINDOW HANDLE POPPED PUT APPROXIMATELY 3 FEET AFTER ENGINE SHUTDOWN. R EQUIRES EXCESSIVE FORCE TO PULL HANDLE OUT ON GROUND. SUPPLEMENTAL MRR: INSTALLED NEW WINDOW LATCH STILL STIFF. RFD M X TO REMOVE WINDOW AND CHECK THE RIGGING PER CMM 56-11-51. 2 L 7 2 4F RT A2NM 1996050900251 19960509 00251 NM 1996 5 9 VNAA9600029 1 19960505 A 2422 PC2512A INVERTER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NR 1 DEFECTIVE A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 434JS 17432 3051 ON THE TAKEOFF ROLL, CREW WAS ALERTED BY AN AMBER CAS MESSAGE NR 1 INVERTER FAIL. CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. PIT MX INSPECTED THE AIRCRAFT AND DETERMINED THAT THE NR 1 INVERTER WAS FAULTY. REPLACED THE NR 1 INVERT ER IAW MM 24-20-00, GROUND CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. PART TOTAL CYCLES, 1,758. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996050900255 19960509 00255 WP 1996 5 9 96ZZZX2265 1 19960422 A 5320 INTERCOSTAL LKHEED 1011 10113851 5265010 WP BS 1565/1585 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 302MB 193P1129 LEVEL 2 CORROSION, CENTER CARGO COMPARTMENT, STA 1565 AND STA 1585, LBL 35 INTERCOSTAL BELOW FLOOR CORRODED. REMOVED AN D REPLACED DAMAGED AREA PER SRM 51-40-04. 2 L 7 3 4F A23WE 1996050900256 19960509 00256 WP 1996 5 9 96ZZZX2266 1 19960422 A 5315 FLOOR BEAM LKHEED 1011 10113851 5265010 WP BS 1463 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 302MB 193P1129 LEVEL 2 CORROSION, CENTER CARGO COMPARTMENT, LT AND RT SIDES OF FLOOR SUPPORT BEAM UPPER CAP AT STA 1463, HAS CORROSION. REMOVED AND REPLACED DAMAGED AREA PER SRM 51-50-04. 2 L 7 3 4F A23WE 1996050900257 19960509 00257 WP 1996 5 9 96ZZZX2267 1 19960101 A 5347 SEAT TRACK DOUG DC8 DC863 302198A WP BS 1520-1620 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 4935C 45931 LEVEL 2 CORROSION, CABIN FLOOR STA 1520 - STA 1620, LT SIDE OUTBOARD SEAT TRACK HAS CORROSION. REMOVED DAMAGED AREA AND SPLICED IN NEW SEAT TRACK PER SRM 51-2-3. 2 L 7 4 4F 4A25 1996050900258 19960509 00258 WP 1996 5 9 96ZZZX2268 1 19960422 A 5347 FLOOR TRACK LKHEED 1011 10113851 5265010 WP AFT CARGO CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 302MB 193P1129 LEVEL 2 CORROSION, AFT CARGO COMPARTMENT, LT FLOOR TRACK AT STA 1665 - STA 1685, AND STA 1705. REMOVED AND REPLACED FLO OR TRACK SECTION PER SRM 53-24-00. 2 L 7 3 4F A23WE 1996050900259 19960509 00259 WP 1996 5 9 96ZZZX2269 1 19960422 A 5312 BLKHD BRACKET LKHEED 1011 10113851 5265010 WP BS 1363 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 302MB 193P1129 LEVEL 2 CORROSION, CENTER CARGO COMPARTMENT BELOW FLOOR PANEL AT FORWARD BULKHEAD, STA 1363, BL 6 ON LT SIDE SUPPORT BRA CKET, HAS CORROSION. REMOVED AND REPLACED DAMAGED BRACKET PER SRM 51-10-5. 2 L 7 3 4F A23WE 1996050900260 19960509 00260 EU 1996 5 9 96ZZZX2270 1 19960403 A 2730 7227715841 CABLES SAAB SF340 340B 7860101 EU LT ELEVATOR CHAFED A PLGA K NONE O OTHER IN INSP/MAINT 1 NE 05 359BE 340B285 DURING C-CHECK INSPECTION, LEFT ELEVATOR CABLES IN REAR FUSELAGE FOUND CHAFING. REPLACED AND RIGGED CABLES IAW SAAB MM, CHAPTER 27. REFERENCE OPERATOR CONTROL NR PLG4396DG3. (X) 2 L 7 2 4T RT A52EU 1996050900261 19960509 00261 EU 1996 5 9 96ZZZX2271 1 19960403 A 2700 7227705643 CABLES SAAB SF340 340B 7860101 EU COCKPIT CHAFED A PLGA K NONE O OTHER IN INSP/MAINT 1 NE 05 359BE 340B285 DURING ROUTINE C-CHECK INSPECTION, CHAFING FOUND IN LEFT INBOARD AND OUTBOARD CONTROL CABLES AT SEVERAL FRAMES. BOTH CA BLES WERE REPLACED IN FORWARD AREA OF CABIN IAW SAAB AMM CHAPTER 27. ALL RIGGING AND REQUIRED CHECKS WERE PERFORMED PER AMM CHAPTER 27. REFERENCE OPERATOR CONTROL NR PLG4396DG4. (X) 2 L 7 2 4T RT A52EU 1996050900262 19960509 00262 EA 1996 5 9 96ZZZX2272 2 19960415 A 7320 3032125 PY LINE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA LT ENGINE CRACKED A AMWA A E UNSCHED LANDING ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 CE 07 143AM 11195 3020 UC143 32591 MCI - FLT 5727 - DURING CLIMB-OUT, THE LEFT ENGINE LOST POWER. THE CREW SHUT THE ENGINE DOWN AND RETURNED TO FIELD. MA INTENANCE REPLACED PY-LINE AND RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T 4 T RT A24CE E4EA 1996050900263 19960509 00263 EA 1996 5 9 96ZZZX2273 2 19960415 A 7320 3031829 P3 LINE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA RT ENGINE CRACKED A AMWA A E UNSCHED LANDING ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 CE 07 134YV 32422 UC134 32422 OMA - FLT 5737 - DURING CLIMB, THE RIGHT ENGINE LOST POWER. CREW LANDED IN OMA WITHOUT INCIDENT. MAINTENANCE REMOVED A ND REPLACED THE CRACKED P-3 LINE. OPS CHECKED NORMAL, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A24CE E4EA 1996050900264 19960509 00264 EU 1996 5 9 C2XA96BT001 1 19960416 A 3234 1005383Y00 CONTROL VALVE AEROSP ATR42 ATR42320 8680930 EU LANDING GEAR FAILED A C2XA O A OTHER UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 26826 172 PIT - FLT 3448 - AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. RETURNED TO PIT. FOUND LANDING GEAR CONTROL VALVE UP S OLENOID MALFUNCTION. LANDING GEAR CONTROL VALVE REMOVED AND REPLACED WITH SERVICEABLE UNIT. TEST FLIGHT SATISFACTORY. AIRCRAFT TOTAL TIME, 12,929.1 HOURS. CYCLES, 15,683. (X) 2 H 7 2 4T RT A53EU 1996050900265 19960509 00265 SO 1996 5 9 C2XA96CI018 1 19960416 A 7712 30005000052 TQ SIGNAL UNIT EMB 120 EMB120RT SO RT ENGINE FAILED A C2XA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 09 27707 5401 1323 120095 CLE - FLT 3096 - CREW REPORTED THAT ON TAKEOFF, THE RIGHT ENGINE SURGED ABOUT 100 PERCENT AND THEN AUTOFEATHEREDTO 40 PE RCENT. THE CREW PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED THE RIGHT ENGINE TORQUE SIGNAL CONDITIONING UNIT, MAINTENANCE ALSO REMOVED AND REPLACED THE LEFT ENGINE TORQUE SIGNAL CONDI TIONING UNIT AS A PRECAUTION. ALL WORK WAS PERFORMED IAW EMB-120 MM 77-11-01. OPERATIONAL CHECKS WERE GOOD, AIRCRAFT R ETURNED TO SERVICE. LEFT ENGINE, T.S.C.U. P/N 30005-0000-52, S/N 1732. (X) 2 L 7 2 4T RT A31SO 1996050900266 19960509 00266 SO 1996 5 9 C2XA96IA090 1 19960411 A 5730 12033270001 SKIN EMB 120 EMB120RT SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 31711 120107 IAH - DURING A 20,000 CYCLE INSPECTION, THE LEFT WING LOWER SKIN WAS FOUND CRACKED AT THE OUTBOARD NACELLE CHORDWISE ATT ACHMENT FLANGE FASTENER HOLE. MAINTENANCE OVERSIZED THE FASTENER HOLE, INSERTED A NEW FASTENER, AND THE AIRCRAFT WAS AP PROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1996050900267 19960509 00267 SO 1996 5 9 C2XA96IA091 1 19960410 A 3246 31446 WHEEL EMB 120 EMB120RT SO RT MLG FAILED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16729 120185 IAH - FLT 3950 - DURING POST-FLIGHT INSPECTION, PILOT REPORTED THE NR 4 MAIN TIRE WAS BLOWN. MAINTENANCE FOUND THE WHEE L RIM HAD FAILED, REMOVED AND REPLACED THE WHEEL ASSEMBLY, AND APPROVED THE AIRCRAFT FOR RETURN TO SERVICE. AIRCRAFT T OTAL TIME, 13,896.1 HOURS. TOTAL CYCLES, 17,612. (X) 2 L 7 2 4T RT A31SO 1996050900268 19960509 00268 SO 1996 5 9 C2XA96IA095 1 19960414 A 2121 EVAC2322C2 FAN EMB 120 EMB120RT SO COCKPIT FAILED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 09 26714 120118 IAH - FLT 3994 - PILOT REPORTED THAT WHILE ON THE GROUND, THERE WAS SMOKE IN THE COCKPIT. MAINTENANCE INSPECTED THE AIR CRAFT AND FOUND THE LEFT GROUND COOLING FAN TO BE FAULTING. MAINTENANCE DISPATCHED THE AIRCRAFT BACK TO SERVICE UNDER M EL 21-51-2, OF THE CONTINENTAL EXPRESS MEL/CDL MANUAL. (X) 2 L 7 2 4T RT A31SO 1996050900269 19960509 00269 EU 1996 5 9 C2XA96IA096 1 19960423 A 5320 S5367800121000 THRESHOLD AEROSP ATR42 ATR42320 8680930 EU SERVICE DOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14821 160 DURING C-CHECK INSPECTION, THE SERVICE DOOR THRESHOLD WEB WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE THRE SHOLD WEB AND THE AIRCRAFT WAS RETURNED TO SERVICE. AIRCRAFT TOTAL TIME, 13,896.1 HOURS. TOTAL CYCLES, 17,612. (X) 2 H 7 2 4T RT A53EU 1996050900270 19960509 00270 EU 1996 5 9 C2XA96IA097 1 19960423 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14821 160 DURING C-CHECK INSPECTION, FLIGHT ATTENDANT'S SEAT, RT SEAT TRACK, WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK AND THE AIRCRAFT WAS RETURNED TO SERVICE. AIRCRAFT TOTAL TIME, 13,896.1 HOURS. TOTAL CYCLES, 17,612. ( X) 2 H 7 2 4T RT A53EU 1996050900271 19960509 00271 EU 1996 5 9 C2XA96IA098 1 19960423 A 5320 S5367240720202 FLOOR SUPPORT AEROSP ATR42 ATR42320 8680930 EU FRAME 38 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14821 160 DURING C-CHECK INSPECTION, THE FLOOR SUPPORT BEAM AT FRAME 38 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SUPPORT BEAM AND THE AIRCRAFT WAS RETURNED TO SERVICE. AIRCRAFT TOTAL TIME, 13,896.1 HOURS. TOTAL CYCLES, 17,612. (X) 2 H 7 2 4T RT A53EU 1996050900272 19960509 00272 EU 1996 5 9 C2XA96IA099 1 19960423 A 5320 S5367240620801 FLOOR SUPPORT AEROSP ATR42 ATR42320 8680930 EU FRAME 36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14821 160 DURING C-CHECK INSPECTION, THE FLOOR SUPPORT BEAM AT FRAME NR 36 WAS FOUND CORRODED. MAINTENANCE REMOVED AND RPELACED T HES UPPORT BEAM AND AIRCRAFT WAS RETURNED TO SERVICE. AIRCRAFT TOTAL TIME, 13,896.1 HOURS. TOTAL CYCLES, 17,612. (X) 2 H 7 2 4T RT A53EU 1996050900273 19960509 00273 EU 1996 5 9 C2XA96IA100 1 19960423 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14821 160 DURING C-CHECK INSPECTION, FLIGHT ATTENDANT'S SEAT, LEFT SEAT TRACK, FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED T HE SEAT TRACK AND THE AIRCRAFT WAS RETURNED TO SERVICE. AIRCRAFT TOTAL TIME, 13,896.1 HOURS. TOTAL CYCLES, 17,612. (X ) 2 H 7 2 4T RT A53EU 1996050900274 19960509 00274 EU 1996 5 9 C2XA96IA101 1 19960423 A 5720 S57510052800304 SUPPORT ROD AEROSP ATR42 ATR42320 8680930 EU RT WING WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14821 160 DURING C-CHECK INSPECTION, THE INBOARD SUPPORT ROD FOR THE UPPER FLAP WELL PANEL UNDER 632BB WAS FOUND WORN. MAINTENANC E REMOVED AND REPLACED THE SUPPORT ROD AND THE AIRCRAFT WAS RETURNED TO SERVICE. AIRCRAFT TOTAL TIME, 13,896.1 HOURS. T OTAL CYCLES, 17,612. (X) 2 H 7 2 4T RT A53EU 1996050900275 19960509 00275 EU 1996 5 9 C2XA96IA102 1 19960423 A 5347 S53678001201 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FR NR 36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14821 160 DURING C-CHECK INSPECTION, THE RIGHT OUTBOARD SEAT TRACK AT FRAME 36 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLAC ED THE SEAT TRACK AND THE AIRCRAFT WAS RETURNED TO SERVICE. AIRCRAFT TOTAL TIME, 13,896.1 HOURS. TOTAL CYCLES, 17,612. (X) 2 H 7 2 4T RT A53EU 1996050900276 19960509 00276 EU 1996 5 9 C2XA96IA103 1 19960423 A 5313 S53671000203 STRINGER AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14821 160 DURING C-CHECK INSPECTION, STR 17RT BETWEEN FRAMES NR 33 AND NR 35 WAS FOUND CORRODED. MAINTENANCE REMOVED THE CORROSIO N AND PERFORMED A STRINGER REPAIR PER ATR-42 SRM 51-21-42 AND SRM 53-00-00. AIRCRAFT TOTAL TIME, 13,896.1 HOURS. TOTAL CYCLES, 17,612. (X) 2 H 7 2 4T RT A53EU 1996050900277 19960509 00277 NM 1996 5 9 CKSA96017 1 19960223 A 3260 INDICATION LIGHT BOEING 727 727223 1384074 NM 52801 MALFUNCTIONED A CKSA O OTHER P NO WARNING INDICATION CL CLIMB 1 GL 23 856AA 53801 20997 DURING GEAR RETRACTION, NOSE GEAR RED LIGHT DOES NOT COME ON, BUT DURING EXTENSION, NOSE GEAR RED LIGHT WORKS FINE. (X) 2 L 7 3 4F A3WE 1996050900278 19960509 00278 NM 1996 5 9 CKSA96018 1 19960223 A 3260 INDICATION LIGHT BOEING 727 727223 1384074 NM LT MLG MALFUNCTIONED A CKSA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 856AA 52801 20997 DURING GEAR EXTENSION, LEFT MAIN GEAR RED LIGHT DOES NOT COME ON, BUT DURING RETRACTION, LEFT GEAR RED LIGHT WORKS FINE. (X) 2 L 7 3 4F A3WE 1996050900279 19960509 00279 WP 1996 5 9 EIAA9607 1 19960420 A 3246 95502673 TIRE 59104475029 DOUG DC9 DC933F 302207A WP NLG SEPARATION A EIAA O OTHER E VIBRATION/BUFFET TO TAKEOFF 1 NM 09 945F 147 KLM0020 47279 SEA - NOSE WHEEL VIBRATION NOTED PRIOR TO LIFT-OFF AT PDX. RETURNED FOR FULL STOP LANDING AT SEA. REPLACED BOTH NOSE T IRES PER 32-40-2, DUE TO LT NOSE TIRE CAP SEPARATION. INSPECTED AIRPLANE FOR FOD - NONE FOUND. (X) 2 L 7 2 4F A6WE 1996050900280 19960509 00280 WP 1996 5 9 HAL9640 1 19960413 A 3350 601177 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 709HA 296 47764 HNL - LEFT OVERWING EMERGENCY LAMP INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. OPS CHECK OK. (X) 2 L 7 2 4F A6WE 1996050900281 19960509 00281 WP 1996 5 9 HAL9641 1 19960413 A 3350 6011777 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 709HA 1249 47764 HNL - RIGHT OVERWING EMERGENCY LAMP INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. OPS CHECK OK. (X) 2 L 7 2 4F A6WE 1996050900282 19960509 00282 EU 1996 5 9 PLG31696G1 1 19960316 A 3020 NH24668081 INTAKE DUCT SAAB SF340 SF340A 7850100 EU RT ENGINE BURNED A PLGA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NE 05 343BE 498082 340A101 BGR/BOS - FLT 4589 - A STRONG BURNING ODOR WAS NOTED BY THE FLIGHT CREW WHICH SUBSIDED WHEN THE RIGHT BLEED WAS CLOSED. NO OTHER WARNINGS WERE RECEIVED, AND THE AIRCRAFT LANDED WITHOUT INCIDENT IN BOS. MAINTENANCE WAS DISPATCHED TO THE AI RCRAFT AND FOUND THE RIGHT INTAKE DUCT WITH A LARGE BURN AREA. MAINTENANCE REMOVED AND REPLACED THE LOWER DUCT AND RETU RNED THE AIRCRAFT TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1996050900283 19960509 00283 CE 1996 5 9 PLG31996G1 1 19960319 A 7120 118910025121 TRUSS ASSY BEECH 1900 1900C 1154161 CE LT ENGINE CRACKED A PLGA K NONE O OTHER IN INSP/MAINT 1 NE 05 3068M UB69 WHILE C/W AD 95-02-18 IAW BEECH SB 255 PART A, THE LEFT ENGINE TRUSS ASSEMBLY WAS FOUND TO HAVE A 1 INCH CRACK AT THE UP PER INBOARD CLUSTER. TRUSS WAS REPLACED WITH A SERVICEABLE UNIT. (X) 2 L 7 2 4T RT A24CE 1996050900284 19960509 00284 EU 1996 5 9 PLG33096DG1 1 19960330 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 SF340A 7850100 EU CARGO COMPT MALFUNCTIONED A PLGA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NE 05 341BE 340A063 BTV/BOS - FLT 4329 - DURING FLIGHT, PILOT HAD A CARGO SMOKE WARNING LIGHT ILLUMINATE. CARGO FIRE BOTTLE WAS DISCHARGED. AIRCRAFT DIVERTED TO MHT. MAINTENANCE WAS DISPATCHED TO AIRCRAFT AND FOUND NO EVIDENCE OF FIRE IN CARGO COMPARTMENT. AIRCRAFT WAS FLOWN TO PSM WITH CARGO FIRE SYSTEM MEL'D. CARGO SMOKE DETECTOR WAS REPLACED AND CARGO FIRE BOTTLE WAS RE PLACED IAW SAAB AMM CHAPTER 26. S/N FWD - A3744. S/N AFT - A2555. (X) 2 L 7 2 4T RT A52EU 1996050900285 19960509 00285 CE 1996 5 9 PLG33196DG1 1 19960331 A 7931 1241011 OIL PRESS TRANS BEECH 1900 1900C 1154161 CE LT ENGINE FLUCTUATING A PLGA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NE 05 15486 14529 UC131 BOS - AFTER DEPARTING, PILOT EXPERIENCED OIL PRESSURE FLUCTUATIONS ON LEFT ENGINE. AIRCRAFT RETURNED TO BOS WIHOUT INCI DENT. MAINTENANCE REPLACED LEFT ENGINE OIL PRESSURE TRANSMITTER AND CANNON PLUG. ALL CHECKS WERE GOOD PER BEECH MM, CH APTER 79. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1996050900286 19960509 00286 EU 1996 5 9 PLG4396DG1 1 19960403 A 5310 STRUCTURE SAAB SF340 340B 7860101 EU UNDER GALLEY CORROSION A PLGA K NONE O OTHER IN INSP/MAINT 1 NE 05 359BE 340B285 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS FOUND ON STRUCTURE UNDER GALLEY FLOOR. CORROSION WAS REMOVED AND TREAT ED IAW SAAB SRM, CHAPTER 51. (X) 2 L 7 2 4T RT A52EU 1996050900287 19960509 00287 EU 1996 5 9 PLG4396DG2 1 19960403 A 2720 7227105561 CONTROL CABLE SAAB SF340 340B 7860101 EU FUSELAGE CHAFED A PLGA K NONE O OTHER IN INSP/MAINT 1 NE 05 359BE 340B285 DURING ROUTINE C-CHECK INSPECTION, CHAFING WAS FOUND ON LEFT OUTBOARD CABLE IN OVAL CIRCUIT OF RUDDER CIRCUIT 1. REPLAC ED CABLE AND RIGGED IAW SAAB AMM CHAPTER 27. (X) 2 L 7 2 4T RT A52EU 1996050900288 19960509 00288 EU 1996 5 9 PLG4396DG3 1 19960403 A 2730 7227215746 CABLES SAAB SF340 340B 7860101 EU LT ELEVATOR CHAFED A PLGA K NONE O OTHER IN INSP/MAINT 1 NE 05 359BE 340B285 DURING C-CHECK INSPECTION, LEFT ELEVATOR CABLES IN REAR FUSELAGE FOUND CHAFING. REPLACED AND RIGGED CABLES IAW SAAB MM, CHAPTER 27. REFERENCE OPERATOR CONTROL NR 96ZZZX2270. (X) 2 L 7 2 4T RT A52EU 1996050900289 19960509 00289 EU 1996 5 9 PLG4396DG4 1 19960403 A 2700 7227105711 CABLES SAAB SF340 340B 7860101 EU COCKPIT CHAFED A PLGA K NONE O OTHER IN INSP/MAINT 1 NE 05 359BE 340B285 DURING ROUTINE C-CHECK INSPECTION, CHAFING FOUND IN LEFT INBOARD AND OUTBOARD CONTROL CABLES AT SEVERAL FRAMES. BOTH CA BLES WERE REPLACED IN FORWARD AREA OF CABIN IAW SAAB AMM CHAPTER 27. ALL RIGGING AND REQUIRED CHECKS WERE PERFORMED PER AMM CHAPTER 27. REFERENCE OPERATOR CONTROL NR 96ZZZX2271. (X) 2 L 7 2 4T RT A52EU 1996050900290 19960509 00290 EU 1996 5 9 PLG4896EB1 1 19960408 A 2910 72MEF20151 HYD SWIVEL SAAB SF340 SF340A 7850100 EU RT MLG BROKEN A PLGA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NE 05 741BA 340A090 PWM/BOS - FLT 4605 - DURING CLIMB-OUT, CREW NOTED THE HYDRAULIC PRESSURE DROPPING DURING GEAR RETRACTION. THE AIRCRAFT RETURNED TO PWM AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT GEAR DOWNLOCK HYDRAULIC SWIVEL. GEAR SWINGS AND OPS CHECKS WERE PERFORMED, AND AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1996050900292 19960509 00292 WP 1996 5 9 RRXA96020 1 19960424 A 2910 CONTROL VALVE DOUG DC8 DC863 302198A WP RT MLG WW LEAKING A RRXA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 15 964R 46000 KONT-KDAY - FLT 023 - LOSS OF HYDRAULIC FLUID DURING CRUISE. MAINTENANCE FOUND FLUID LEAKING FROM THE SLOT CONTROL VALV E IN THE RT WHEELWELL. MAINTENANCE REMOVED AND REPLACED THE SLOT CONTROL VALVE. A LEAK CHECK OF THE HYDRAULIC SYSTEM R EVEALED NO LEAKS. (X) 2 L 7 4 4F 4A25 1996050900293 19960509 00293 EU 1996 5 9 SIMA961091 1 19960418 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 591MA 17643 340B192 DFW - FLT 3754 - EMERGENCY LIGHTS SECOND AND THIRD FLOOR LIGHT, FORWARD EMERGENCY EXIT SIGN, FIRST COVE AND FIRST AND SE COND RT COVE EMERGENCY LIGHT INOPERATIVE. C/A - REPLACED EMERGENCY POWER SUPPPLY 20LN. AIRCRAFT WAS RETURNED TO SERVIC E. (X) 2 L 7 2 4T RT A52EU 1996050900294 19960509 00294 EU 1996 5 9 SIMA961141 1 19960423 A 3350 3011140 BATTERY AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 422MQ 1333 0028 ORD - FLT 4245 - FORWARD EMERGENCY LIGHTS INOPERABLE. C/A - REPLACED POWER PACK AND BATTERY 3WL CHECK GOOD. AIRCRAFT W AS RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1996050900295 19960509 00295 NM 1996 5 9 TAOA049607 1 19960415 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 918TS P2841 20445 RIGHT INTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERABLE. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. (X) 2 L 7 3 4F A3WE 1996050900296 19960509 00296 NM 1996 5 9 TAOA049608 1 19960413 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 918TS 3899 20445 LEFT INTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERABLE. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. (X) 2 L 7 3 4F A3WE 1996050900297 19960509 00297 WP 1996 5 9 USAAD96040 1 19960421 A 2150 DUCT DOUG DC9 DC981 3022081 WP RT PACK LOOSE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 806US 48038 RSW - FL 1028 - AFTER TAKEOFF, CREW RECEIVED MASTER WARNING LIGHT DUE TO THE TAIL HIGH TEMPERATURE SIGNAL. FLIGHT RETUR NED TO RSW AND LANDED WITH NO FURTHER INCIDENT. MX FOUND THE DUCTING AT THE WATER SEPARATOR ON THE RIGHT PACK LEAKING. DUCTING WAS SECURED AND THE AIRCRAFT RELEASED FOR FLIGHT. (M) 2 L 7 2 4F A6WE 1996050900298 19960509 00298 1996 5 9 VTZA96156 4 19960421 A 3425 7003380948 AHRS JETAIR JETSTM JETSTM4101 1500501 EU AVIONICS BAY OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 323UE 41059 IAD/ORF - FLT 6489 - DURING TAKEOFF AT 1630 HRS ON 4-21-96, ABORTED TAKEOFF DUE TO THE HEADING COMPUTER SHOWING ERRORS. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE RERACKED THE NR 1 AND NR 2 AHRS. AIRCRAFT WAS RELEAS ED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1996050900299 19960509 00299 EU 1996 5 9 VTZA96157 1 19960420 A 5270 1XE201 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU AFT EMERG EXIT OUT OF ADJUST A VTZA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 EA 27 306UE 41020 IAD/EWR - FLT 6261 - AFTER TAKEOFF AT 0815 HRS ON 4-20-96, RETURNED TO IAD DUE TO THE EMERGENCY DOOR WARNING LIGHT ILLUM INATED. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED THE AFT EMERGENCY EXIT DOOR WARNING MIC ROSWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1996050900300 19960509 00300 EU 1996 5 9 VTZA96159 1 19960419 A 3260 ATG135022 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU LT MLG FAILED A VTZA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 EA 27 319UE 41042 PVD/IAD - FLT 36416 - DURING CLIMB-OUT AT 0930 HRS ON 4-19-96, RETURNED TO PVD DUE THE LEFT MAIN GEAR INTRANSIT LIGHT RE MAINED ILLUMINATED. THERE WAS NO RED GEAR HANDLE LIGHT ILLUMINATED AND THE GREEN DOWNLOCK LIGHTS ILLUMINATED NORMALLY. AIRCRAFT LANDED AT PVD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE LEFT UPLOCK MICROSWITCH. AIRCRAFT WAS RELE ASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1996050900301 19960509 00301 1996 5 9 VTZA96160 3 19960421 A 6140 8659566 BETA PRESS SW BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 489UE 908 IAD/CLE - FLT 6552 - DURING TAKEOFF AT 2200 HRS ON 4-21-96, ABORTED THE TAKEOFF DUE TO THE LEFT BETA LIGHT ILLUMINATING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE BETA PRESSURE SWITCH. AIRCRAFT WAS REL EASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1996050900302 19960509 00302 EU 1996 5 9 VTZA96161 1 19960421 A 2435 23095002 STARTER/GEN BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A VTZA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 27 493UE 805 IAD/CMG - FLT 6381 - DURING CRUISE AT 1225 HRS ON 4-21-96, RETURNED TO IAD DUE TO THE RT STARTER/GENERATOR FAILING IN-FL IGHT. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE RT STARTER/GENERATOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1996050900303 19960509 00303 1996 5 9 VTZA96162 4 19960421 A 3418 C771065 SIG SUMMING UNIT BAG JETSTM JETSTM3201 1500217 EU STALL WARNING OUT OF ADJUST A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 475UE 850 IAD/ALB - FLT 6556 - DURING CLIMB-OUT AT 1255 HRS ON 4-21-96, RETURNED TO IAD DUE TO THE STALL WARNING AND STICK SHAKER ACTIVATING DURING THE CLIMB-OUT. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED THE LT AND R T STALL WARNING SIGNAL SUMMING UNITS. (X) 2 L 7 2 4T RT A56EU 1996050900304 19960509 00304 EU 1996 5 9 VTZA96163 1 19960420 A 3260 91SE16 SWITCH BAG JETSTM JETSTM3201 1500217 EU CENTER CONSOLE DIRTY A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 471UE 821 IAD/EWR - FLT 6295 - DURING CLIMB-OUT AT 1330 HRS ON 4-20-96, RETURNED TO IAD DUE TO THE GEAR WARNING HORN SOUNDING. AI RCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE CLEANED MICROSWITCH AT POWER LEVER. AIRCRAFT WAS RELEASE D AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1996050900305 19960509 00305 EU 1996 5 9 VTZA96164 1 19960421 A 5270 727422 CIRCUIT BREAKER BAG JETSTM JETSTM3201 1500217 EU DOOR WARNING TRIPPED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 488UE 907 IAD/SYR - FLT 6343 - AFTER TAKEOFF AT 1312 HRS ON 4-21-96, RETURNED TO IAD WITH NO FURTHER INCIDENTS DUE TO THE PASSENGE R DOOR WARNING ILLUMINATING. MAINTENANCE RESET THE DOOR WARNING CIRCUIT BREAKER. AIRCRAFT WAS RELEASED AND APPROVED FO R RETURN TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1996050900336 19960509 00336 1996 5 9 96ZZZX2304 4 19960410 A 2215 SERVO BENDIX MTSBSI MU2 MU2B60 5780460 CE AUTOPILOT YAW BURNED A F5MA O OTHER F FLT CONT AFFECTED DE DESCENT 1 SO 05 196MA 2700 8244 764SA AFTER SWITCHING OFF AUTOPILOT FOR DESCENT TO LAND, RUDDER BECAME STIFF. AFTER LANDING, IT BECAME NORMAL AGAIN. PILOT S USPECTED ICE. INVESTIGATION TO THIS FOUND YAW SERVO MOTOR BURNED UP TO THE POINT THAT PAINT WAS COMING OFF CASE. 1 H 7 2 3T RT A10SW 1996050900337 19960509 00337 NM 1996 5 9 9610062713 1 19960504 A 2120 AIR DISTR BOEING 727 7272S7 138407Z NM CABIN SMOKE A NWAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 01 716RC 22021 DURING TAXI OUT AND MOMENTS AFTER THE APU WAS SHUT DOWN, THE CABIN BEGAN TO FILL WITH SMOKE. AIRCRAFT RETURNED TO GATE AND PASSENGERS WERE DEPLANNED THROUGH THE FORWARD CABIN DOOR WITHOUT FURTHER INCIDENT. GROUND MAINTENANCE INSPECTED AND RAN THE PACKS USING BOTH ENGINES AND THE APU. NO SMOKE OR SMELL WAS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A3WE 1996050900338 19960509 00338 NE 1996 5 9 9610073204 2 19960504 A 7200 ENGINE AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE NR 1 VIBRATION A NWAA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 GL 01 304US 40 731304 DURING CLIMB AFTER FLAP RETRACTION, AN AIRCRAFT VIBRATION WHICH SEEMED TO FOLLOW NR 1 ENGINE RPM WAS FELT. AIRCRAFT RET URNED TO MSP. GROUND MAINTENANCE INSPECTION OF AIRFRAME REVEALED NO DISCREPANCIES. NR 1 ENGINE WAS GROUND RUN AND FAN TRIM BALANCE WAS PERFORMED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A28NM E29NE 1996050900339 19960509 00339 WP 1996 5 9 9610089979 1 19960505 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9343 47439 DURING LINE MAINTENANCE INSPECTION, FOUND THAT THE EMERGENCY LIGHTS WOULD NOT EXTINGUISH WITH EXTERNAL POWER APPLIED. R EPLACED THE POWER SUPPLY, BATTERIES, AND BROKEN WIRE AT TERMINAL 7 AT B5-23 BATTERY PACK. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996050900340 19960509 00340 1996 5 9 9610099968 4 19960504 A 2565 13621224 EVAC SLIDE DOUG DC9 DC931 3022065 WP TAILCONE LOW PRESSURE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9332 48466 455 47264 DURING LINE MAINTENANCE INSPECTION, FOUND THE TAILCONE EVACUATION SLIDE BOTTLE PRESSURE LOW. REPLACED SLIDE. 2 L 7 2 4F A6WE 1996050900341 19960509 00341 WP 1996 5 9 9610109925 1 19960503 A 3350 229015 FUSE DOUG DC9 DC932 3022066 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 925US 47472 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS AT GALLEY DOOR AND FORWARD CABIN INOPERATIVE. REPLACED FUSE. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996050900342 19960509 00342 WP 1996 5 9 9610119979 1 19960503 A 2820 3912791501 VENT FLOAT VALVE DOUG DC9 DC931 3022065 WP LT WING STUCK OPEN A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION UK UNKNOWN 1 GL 01 9343 47439 FUEL BEGAN VENTING FROM RIGHT WING FUEL TANK EN ROUTE YHZ-DTW. FLIGHT DIVERTED TO BOS AND LANDED WITHOUT INCIDENT. MAI NTENANCE REPLACED UPPER VENT DRAIN VALVE WITH NO HELP. REPLACED THE LEFT TANK CLIMB VENT FLOAT VALVE. LEAK AND TRANSFE R CHECK WERE NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996050900343 19960509 00343 EU 1996 5 9 9610123240 1 19960503 A 3260 INDICATION AIRBUS 320 A320211 3930320 EU LANDING GEAR MALFUNCTIONED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 340NW 372 DURING CLIMB-OUT AFTER LANDING GEAR RETRACTION, RECEIVED L/G DOOR NOT CLOSED MESSAGE AND NOSE GEAR NOT LOCKED INDICATION . CYCLED THE LANDING GEAR HANDLE AND ALL INDICATIONS WERE NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUB LESHOOTING REVEALED NO DISCREPANCIES. 2 L 7 2 4F RT A28NM 1996050900344 19960509 00344 EU 1996 5 9 9610133231 1 19960430 A 3350 321430 BATTERY PACK AIRBUS 320 A320211 3930320 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 331NW 318 DURING LINE MAINTENANCE, ROWS 13, 14, 15, 19, 20, 21, 25, 26, AND 27 ESCAPE PATH LIGHTS WERE FOUND INOPERATIVE. REPLACE D BATTERY PACK. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996050900345 19960509 00345 WP 1996 5 9 9610149304 1 19960503 A 3350 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 931MC 48057 DURING LINE CHECK, FOUND EMERGENCY LIGHTS IN CABIN CEILING INOPERATIVE FROM ROWS 20 - 25. REPLACED BATTERIES AND OPERAT IONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996050900346 19960509 00346 WP 1996 5 9 9610159877 1 19960504 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 786NC 48148 DURING LINE CHECK, FOUND FORWARD CABIN EMERGENCY CEILING LIGHTS INOPERATIVE. REPLACED BATTERIES. OPERATIONAL CHECK GOO D. 2 L 7 2 4F A6WE 1996050900347 19960509 00347 WP 1996 5 9 9610169913 1 19960506 A 3260 DOOR SWITCH DOUG DC9 DC931 3022065 WP MAIN GEAR MALFUNCTIONED A NWAA O OTHER N FALSE WARNING DE DESCENT 1 GL 01 963N 47415 LANDING GEAR DOOR OPEN LIGHT ILLUMINATED DURING DESCENT INTO DTW. COCKPIT OPERATING MANUAL PROCEDURES WERE ACCOMPLISHED WITH NO SUCCESS IN EXTINGUISHING LIGHT. CREW REQUESTED EMERGENCY EQUIPMENT ON STANDBY DURING LANDING AS A PRECAUTION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED BOTH MAIN GEAR DOOR SWITCHES. OPERATIONAL CHECK NORMAL. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996050900348 19960509 00348 WP 1996 5 9 9610179977 1 19960506 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9341 47390 DURING LINE MAINTENANCE INSPECTION, FOUND NUMEROUS OVERHEAD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN P ACKS. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996050900349 19960509 00349 NM 1996 5 9 96FDEA00897 1 19960503 A 2782 651626942 ACT BRACKET BOEING 727 72725 1384006 NM NR 2 LE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 505FE 18276 NR 0089 AND NR 002, NR 2 K-FLAP ACTUATOR AFT I/B MOUNT IS CRACKED AT UPPER FWD CORNER. ****S/D ****** COMING. REMOVED AND REPLACED NR 2 K-FLAP ACTUATOR APT I/B MOUNT IAW FEDEX SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996050900350 19960509 00350 NM 1996 5 9 96FDEA00904 1 19960507 A 3230 RETRACT MECH BOEING 727 72725C 138400H NM RT MLG MALFUNCTIONED A FDEA O OTHER E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 25 127FE 19719 AFTER LANDING RETRACTION, LANDING HANDLE PLACED TO OFF, RED DOORS LIGHT ILLUMINATED ALONG WITH RT MAIN GEAR DOOR LT ON S/O PANEL. VIBRATION WAS FELT. PERFORMED ABNORMAL LIST AND PROCEEDED WITH LEVER IN UP POSITION. INSTALLED GEAR PINS - INSP RT GEAR DOOR - NO DEFECTS NOTED. DEPRESSURIZED HYD SYSTEM, PLACED GEAR HANDLE IN OFF POSITION, AND PULLED ON DOOR . DOOR REMAINED UP AND LOCKED. UNABLE TO DUPLICATE AT THIS TIME, OK FOR SERVICE. REMOVED GEAR PINS. 2 L 7 3 4F A3WE 1996050900351 19960509 00351 EU 1996 5 9 96FDEA00905 1 19960503 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU CARGO COMPT DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 650FE 726 SEAT TRACK NR 1 LT SIDE OF MAIN CARGO DECK AT FRAME 19 IS DAMAGED AT LUG SUPPORTS. ACCOMPLISHED SEAT TRACK REPAIR PER S RM 53-10-16 FROM FRAMES 18-22. SECTION REPLACED AND SPLICED IN. 2 L 7 2 4F RT A35EU 1996050900352 19960509 00352 NM 1996 5 9 96FDEA00906 1 19960506 A 5330 SKIN BOEING 727 72725 1384006 NM BS 1178 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 505FE 18276 EXTERNAL SKIN HOLE IN SKIN BS 1178 AT STR 22L. REMOVED DAMAGED SKIN AT BS 1178, STR 22L AND INSTALLED REPAIR DOUBLER AN D FILLER. ALL WORK DONE PER FEDEX SRM 53-30-3. 2 L 7 3 4F A3WE 1996050900353 19960509 00353 NM 1996 5 9 96FDEA00907 1 19960506 A 5210 BEAM BOEING 727 72725 1384006 NM FWD ENTRY DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 505FE 18276 FORWARD ENTRY DOOR LOWER GATE BEAM IS CRACKED IN LOWER FORWARD STOP PIN FITTING. REPAIRED FORWARD ENTRY DOOR LOWER GATE BEAM IAW FEDEX EA 7-5210-28328. 2 L 7 3 4F A3WE 1996050900354 19960509 00354 NM 1996 5 9 96FDEA00908 1 19960506 A 5315 6516348 FLOOR BEAM BOEING 727 72725 1384006 NM BS 1148 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 NR 0439 AND NR 033. CORROSION ON LOWER FLOOR BEAM FLANGE AT BS 1148, RBL 14, 27, 36 AND LBL 8 AND 21, WL 200. *****S/D ***** REMOVED CORROSION FROM FLOOR BEAM FOUND TO BE OUT OF LIMITS. REPAIRED FLOOR BEAM PER FEDEX SRM 53-10-8. 2 L 7 3 4F A3WE 1996050900355 19960509 00355 NM 1996 5 9 96FDEA00909 1 19960506 A 5320 DOOR FRAME BOEING 727 72725 1384006 NM BS 592 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 NR 0057 AND 034. CORROSION UNDER LATCH SERRATED PLATE OF FORWARD CARGO DOORWAY AFT FRAME. **********S/D ********** CO MING. 2 L 7 3 4F A3WE 1996050900356 19960509 00356 NM 1996 5 9 96FDEA00910 1 19960506 A 5330 6518420 SKIN BOEING 727 72725 1384006 NM BS 308 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 NR0659 AND 035, CORROSION ON INNER SKIN STA 308 LBL 49 WL 180. *S/D* REPAIRED CORROSION ON INNER SKIN STA 308 LBL 49 W L 180 PER FEDEX SRM 53-30-03. 2 L 7 3 4F A3WE 1996050900357 19960509 00357 WP 1996 5 9 ABXA9600488 1 19960503 A 2170 39706211 DRAIN LINE DOUG DC9 DC932 3022066 WP LEFT PLUGGED A ABXA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 23 981AX 47273 CABIN PRESSURE ANNUNCIATOR LIGHT AND MASTER WARNING LIGHT ON AT FL 310, OUTFLOW VALVE FULLY CLOSED, BOTH AIR CONDITIONIN G PACKS NORMAL PRESSURE, CABIN CONTINUED TO CLIMB DURING DESCENT TO 12,000 FEET. REPLACED LEFT AND RIGHT COALESCER BAGS , REPLACED LEFT WATER SEPARATOR TEMPATURE CONTROL VALVE. FOUND THE LEFT WATER SEPARATOR DRAIN LINE NOT DRAWING PROPERLY , ADJUSTED DRAIN LINE. RAN LEFT AND RIGHT PACKS, PRESSURIZED AIRCRAFT TO 4 PSID, OPS CK GOOD. 2 L 7 2 4F A6WE 1996050900358 19960509 00358 SO 1996 5 9 COMA9610140 1 19960506 A 3231 12012347001 DOOR LATCH EMB 120 EMB120RT SO RT MLG BROKEN A COMA K NONE O OTHER AP APPROACH 1 SO 01 244CA 120217 RIGHT MLG OUTBOARD DOOR HANGING OPEN AND WILL NOT CLOSE. REPLACED BROKEN LATCH ASSY. 2 L 7 2 4T RT A31SO 1996050900359 19960509 00359 EA 1996 5 9 COMA9660079 1 19960504 A 2750 7804011 FLAP SELECTOR CNDAIR CL600 CL6002B19 EA TE FLAPS DEFECTIVE A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 918CA 7001 7018 FLAPS FAILED WHEN SELECTED TO 20 DEGREES FOR APPROACH. REPLACED THE FLAP SELECTOR CONTROL. PART TOTAL CYCLES, 6,234. 2 L 7 2 4F RT A21EA 1996050900360 19960509 00360 EA 1996 5 9 COMA9660080 1 19960506 A 3230 7179015 RETRACT MECH CNDAIR CL600 CL6002B19 EA LANDING GEAR MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 916CA 3290 7014 LANDING GEAR DISAGREE MESSAGE ON EICAS. WHEN GEAR SELECTED DOWN, THE NLG REMAINED UP. NLG DOWNLOCKED AFTER 2 MINUTES. COULD NOT DUPLICATE DISCREPANCY. REPLACED THE LANDING GEAR SELECTOR FOR TROUBLESHOOTING. PART TOTAL CYCLES, 2,838. 2 L 7 2 4F RT A21EA 1996050900361 19960509 00361 EA 1996 5 9 COMA9660081 1 19960506 A 5330 SKIN CNDAIR CL600 CL6002B19 EA BS 409 DAMAGED A COMA K NONE C F.O.D. IN INSP/MAINT 1 SO 01 937CA 7044 V-SHAPED TEAR FOUND IN RT FUSELAGE AT STATION 409 +12. TEAR WAS APROXIMATELY 1 INCH ON EACH SIDE AND PENETRATED THE SKI N. THIS TEAR IS PRESUMED TO BE CAUSED BY GROUND SERVICING EQUIPMENT. TEAR WAS REPAIRED IAW SRM. 2 L 7 2 4F RT A21EA 1996050900362 19960509 00362 WP 1996 5 9 DHL9680501C 1 19960410 A 5330 SKIN DOUG DC8 DC873F 302199F WP PAX DOOR AREA DENTED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, FOUND LARGE DENT ABOVE FORWARD ENTRANCE DOOR. REPAIRED DENT PER DACO SRM 53-2-1, 14 INCH BY 18 INCH. 2 L 7 4 4F RT 4A25 1996050900363 19960509 00363 NM 1996 5 9 DL72L961069 1 19960503 A 5532 SKIN BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 .75 INCH CRACK EXTENDING FROM RIVET HOLE AT LT VERTICAL STABILIZER SKIN 6 INCHES FORWARD OF FRONT SPAR BASE. REPAIRED P ER M/M 54-30-0, PG 801. 2 L 7 3 4F A3WE 1996050900364 19960509 00364 NM 1996 5 9 DL72L961070 1 19960503 A 5320 WEB BOEING 727 727232 1384082 NM FUS TORQUE BOX CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 .4375 INCH CRACK EXTENDING FROM LIGHTNING HOLE 48 SEC. RT TORQUE BOX AFT END. REPAIRED PER M/M 53-11-0. 2 L 7 3 4F A3WE 1996050900365 19960509 00365 NM 1996 5 9 DL72L961071 1 19960503 A 5530 STRINGER BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 TWO VERTICAL STABILIZER STRINGERS CRACKED RT SIDE FOURTH BAY FROM TOP, STR 8 AND STR 10. REPAIRED PER M/M 55-30-0, FIG 803. 2 L 7 3 4F A3WE 1996050900366 19960509 00366 NM 1996 5 9 DL72P961059 1 19960503 A 3350 BULB 1000677 BOEING 727 727225 1384077 NM AFT SVC DOOR FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8875Z 1630 21293 AFT LT SERVICE DOOR EMERGENCY LIGHT, ONE BULB OUT (LT UPPER). REPLACED EMERGENCY LIGHT ASSY. OPS CHECK GOOD. 2 L 7 3 4F A3WE 1996050900367 19960509 00367 NM 1996 5 9 DL72S961056 1 19960502 A 5530 STRINGER BOEING 727 727232 1384082 NM VERT STAB CRACKED A A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 527DA 21587 FOUND ON LETTER CHECK, RT STRINGER 10 CRACKED AT FIN STA 133 INSIDE VERTICLE STABILIZER CRAWL WAY. REPAIRED PER M/M 55- 30-0, FIG 803 - ID PER PS900-5-1 NR 04. 2 L 7 3 4F A3WE 1996050900368 19960509 00368 NM 1996 5 9 DL72S961058 1 19960502 A 3350 BATTERY PACK 900542 BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 520DA 5139 21471 EXTERIOR EMERGENCY LIGHT ON C2 DOOR FAIRING INOPERATIVE. REPLACED BATTERY PACK RACK M957. 2 L 7 3 4F A3WE 1996050900369 19960509 00369 NM 1996 5 9 DL72S961061 1 19960430 A 5754 6565162256A BULLNOSE BOEING 727 727232 1384082 NM NR 4 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 418DA 21271 INBOARD ATTACH POINT FOR BULLNOSE CRACKED. REPAIRED PER SRM 57-50-3. 2 L 7 3 4F A3WE 1996050900370 19960509 00370 NM 1996 5 9 DL72S961066 1 19960503 A 3350 BATTERY PACK 900835A BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 527DA A9205 21587 LEFT SIDE SLIDE LIGHT OUT BETWEEN ESCAPE DOORS. REPLACED LEFT SIDE SLIDE LIGHT BATTERY PACK, CHECKS NORMAL. 2 L 7 3 4F A3WE 1996050900371 19960509 00371 NM 1996 5 9 DL73E961068 1 19960502 A 5312 BLKHD STIFFENER BOEING 737 737247 138448D NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 DURING ACCOMPLISHMENT OF S.I. 3-69482-12, CRACKS WERE DISCOVERED IN THE BS 178 BULKHEAD WEB AND THE RBL 5.7 VERTICAL STI FFENER. THE VERTICAL STIFFENER AT RBL 5.7 ADJACENT TO WL 15 HAS A 1 INCH CRACK ALONG THE RADIUS. THE CHORD IS MANUFACT URED FROM BAC1505-100361 7075-T6 ALTERED EXTRUSION. THE WEB WAS FOUND CRACKED AT SEVERAL LOCATIONS BETWEEN WL 184.5 AND WL 207 AND LBL 5.7 TO RBL 5.7. THE WEB IS MANUFACTURED FROM 0.040 INCH 2024-T3 CLAD. 2 L 7 2 4F A16WE 1996050900372 19960509 00372 NM 1996 5 9 DL73E961081 1 19960505 A 3350 LIGHT 72914 BOEING 737 737247 138448D NM R1 DOOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 377DL 23604 FORWARD RIGHT EXTERIOR EMERGENCY EXIT LIGHT IS INOPERATIVE. REPLACED LIGHT ASSY AND RELAMPED. CKS GOOD. 2 L 7 2 4F A16WE 1996050900373 19960509 00373 NM 1996 5 9 DL73S961054 1 19960502 A 2170 WATER SEPARATOR BOEING 737 737232 1384475 NM CABIN CONTAMINATED A DALA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 316DL 21350 23088 AFTER TAKEOFF, CVG UNABLE TO PRESSURIZE. OUTFLOW VALVE WAS FULL, CLOSED BOTH BLEEDS, AND LT PACK WERE ON AS WAS ISOLATI ON VALVE. OPEN CBS WERE ALL IN CABIN CLIMBED AND DESCENTED WITH THE A/C. REPLACED RT PACK WATER SEPARATOR BAG. 2 L 7 2 4F RT A16WE 1996050900374 19960509 00374 NE 1996 5 9 DL73S961060 2 19960309 A 7261 701577 SCAVENGE PUMP BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE FAILED A DALA E ENGINE SHUTDOWN Y J ENGINE STOPPAGE WARNING INDICATION TO TAKEOFF 1 SO 27 318DL 23367 23090 717150 THE FOLLOWING IS A SUPPLEMENT TO MRR NR 960534. SUBEQUENT FINDINGS AFTER ENGINE TEAR DOWN REVEALED THAT THE NR 4 AND NR 5 SCAVENGE PUMP FAILED RESULTING IN THE OIL STARVATION AND FAILURE OF THE NR 4 BEARING AND SUBSEQUENT DAMAGE TO THE 12 AND 13 STAGE BLADES AND 12 STAGE DISK. 2 L 7 2 4F 4 F RT A16WE E2EA 1996050900375 19960509 00375 NM 1996 5 9 DL73S961067 1 19960501 A 3350 FUSE 20131A BOEING 737 737232 1384475 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 311DL 23083 EMERGENCY TRACK LIGHTS OUT AT ROWS 1 AND 16. AISLE LIGHTS AT ROWS 11, 15, 21, 24 INOPERATIVE. RELAMPED TRACK LIGHTS, A ISLE LIGHTS AT ROWS 11 AND 15. REPLACED BATTERY PACK FUSE. FOUND BATTERY PACK LOOSE FOR ROWS 21 AND 24. 2 L 7 2 4F RT A16WE 1996050900376 19960509 00376 NM 1996 5 9 DL73S961074 1 19960504 A 2530 OVEN 5334E BOEING 737 737232 1384475 NM GALLEY FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 326DL 044 23098 AIRCRAFT RETURNED WITH LOG BOOK IRREG STRONG ODOR BEHIND PILOT SEATS BETWEEN C/B PANEL. THEN SMOKE FROM FORWARD GALLE Y VENT AND OVENS. CORRECTIVE ACTION: FOUND FIRST CLASS OVEN FAN MOTOR BAD. REPLACED OVEN. 2 L 7 2 4F RT A16WE 1996050900377 19960509 00377 NM 1996 5 9 DL76L961083 1 19960504 A 3350 BATTERY PACK 337101963 BOEING 767 767332 1382001 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 178DN 44888 25143 LEFT EMERGENCY ESCAPE SLIDE NO TEST SYSTEM ONE. REPLACED LEFT ESCAPE SLIDE BATTERY PACK AND CHARGER. OPERATION CHECK S GOOD. NO HISTORY. REPLACED BATTERY PACK, CHARGER, AND K838. OPS CHECK OK. 2 L 7 2 4F RT A1NM 1996050900378 19960509 00378 NM 1996 5 9 DLM88961029 1 19960430 A 3222 STRUT 39132445501 DOUG MD88 MD88 3023688 NM NLG FAILED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 955DL 49886 AFTER TAKEOFF, NOSE GEAR UNSAFE LIGHT AND DOORS OPEN. CYCLED GEAR NO HELP. PUT GEAR BACK DOWN WITH THREE GREEN LIGHTS. CORRECTIVE ACTION: REPLACED NLG PISTON ASSY. 2 L 7 2 4F RT A6WE 1996050900379 19960509 00379 NM 1996 5 9 DLM88961041 1 19960501 A 3260 PROX BOX 833605MODA DOUG MD88 MD88 3023688 NM NLG MALFUNCTIONED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 985DL 243 53312 ON GEAR RETRACTION, NOSE UNSAFE LIGHT REMAINS ILLUMINATED. RAN POM, LIGHT EXTINGUISHED ON APPROACH. TROUBLESHOT SYSTEM , REPLACED PROXIMITY BOX, ALL CHECKS NORMAL. NOSE GEAR SWING CHECKS OK. 2 L 7 2 4F RT A6WE 1996050900380 19960509 00380 NM 1996 5 9 DLM88961042 1 19960501 A 5610 5613217520 WINDOW DOUG MD88 MD88 3023688 NM COCKPIT CRACKED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 926DL 49713 FIRST OFFICER'S WINDSHIELD CRACKED AND SHATTERED AT FL 350. ACCOMPLISHED ABNORMAL PROCEDURES. DIVERTED TO CVG. C/A RE MOVED AND REPLACED F/O'S WINDSHIELD AND CONTROLLER PER M/M CHAPTER 56 (CONTROLLER P/N 617-2). 2 L 7 2 4F RT A6WE 1996050900381 19960509 00381 NM 1996 5 9 DLM88961043 1 19960501 A 4990 OIL SEAL DOUG MD88 MD88 3023688 NM APU LEAKING A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 908DL 3000 49539 ON CLIMB-OUT ABOUT 4,000 FEET, BOTH SMOKE ALARMS IN REAR OF A/C SOUNDED AND THERE WAS A LIGHT MIST/SMOKE VISIBLE IN THE A/C. THE SMOKE ALARMS COULD NOT BE SILENCED BY FANNING TO VENTILATE BOTH HPS BLEEDS ON A/C. PACKS TURNED OFF. NO HELP . CORRECTIVE ACTION FOUND APU LEAKING OIL IN EXHAUST AND BACK INTO A/C SYSTEM. REPLACED OIL SEAL AND BURNED OUT DUCT. OPS CHECK OK. 2 L 7 2 4F RT A6WE 1996050900382 19960509 00382 NM 1996 5 9 DLM88961072 1 19960503 A 3350 D43637 SPLICE DOUG MD88 MD88 3023688 NM CABIN MISSING A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 911DE 49967 ONE EACH EMERGENCY ESCAPE PATH LIGHT INOPERATIVE AFT OF GALLEY. ITEM WAS ON MCO 807665001. SPLICED IN BROKEN WIRE AT M ODULE. 2 L 7 2 4F RT A6WE 1996050900383 19960509 00383 NM 1996 5 9 DLM90961023 1 19960429 A 3240 BRAKE 5012193 DOUG MD90 MD9030 3023690 NM NR 2 FAILED A DALA K NONE O OTHER LD LANDING 1 SO 27 907DA 3032 53387 B20023 NR 1 ENGINE FOD DAMAGE TO 1ST STAGE BLADES DUE TO NR 2 BRAKE FAILURE. 2 L 7 2 4F RT A6WE 1996050900384 19960509 00384 NM 1996 5 9 DLM90961030 1 19960430 A 2910 LINES DOUG MD90 MD9030 3023690 NM RT HYD SYST CHAFED A DALA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 906DA 53386 RT HYD QTY DECREASED TO 6 QTS IN-FLIGHT. TURNED OFF RT HYD PUMP IAW CHECK LIST. QTY/PRESSURE HELD THROUGH CONFIGURATIO N THEN WENT TO QTY 2 PRESSURE 5. FOUND PRESSURE AND RETURN LINES CHAFED ON AUXILIARY HYDRAULIC PUMP. REPLACED SAME. 2 L 7 2 4F RT A6WE 1996050900385 19960509 00385 NM 1996 5 9 DLM90961080 1 19960505 A 2612 FIRE LOOP MOUNT DOUG MD90 MD9030 3023690 NM NR 1 ENGINE LOOSE A DALA K NONE N FALSE WARNING DE DESCENT 1 SO 27 907DA 1877 53387 V20023 A-LOOP FIRE DETECTOR LT ENG ILLUMINATED IN-FLIGHT DURING DESCENT TO DFW. B-LOOP ALREADY ON MCO. CORRECTIVE ACTION: FO UND MOUNT PLATE FOR A/B LOOPS LOOSE. SECURED SAME. A-LOOP TEST GOOD. ALSO, REPAIRED BAD WIRE AT LOOP CANNON PLUG. A/ B LOOPS NOW TEST NORMAL. 2 L 7 2 4F RT A6WE 1996050900386 19960509 00386 NE 1996 5 9 P5CA9600221 2 19960507 A 7261 350887 O-RING BOEING 747 747132 1384882 NM PWA JT9 JT9D7A 52054 NE NR 3 ENGINE DAMAGED A P5CA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 WP 23 857FT 20246 662376 ON DEPARTURE CLIMB-OUT PASSING 15,000 FEET, NR 3 ENGINE OIL PRESSURE LIGHT BEGAN FLICKERING. OIL PRESS WAS AT 50 PSI PL US OR MINUS 10 PSI AND DECREASING. OIL QUANTITY INDICATED 1.2 GALLONS. WHEN OIL PRESSURE DECREASED TO 35 PSI, ENGINE W AS SHUT DOWN. ACCOMPLISHED ONE ENGINE INOP DESCENT, APPROACH AND LANDING. APPROACH AND LANDING WERE NORMAL. NO DAMAGE NOTED TO AIRCRAFT ON INSPECTION AFTER LANDING. FOUND EDP SHAFT O-RING SEAL DAMAGED. REMOVED AND REPLACED SAME IAW MM 29-11-05. WINDMILL INSPECTION COMPLETED PER 72-00-00, IDLE POWER LEAK CHECK GOOD. ENGINE RUNUP PER 71-00-00. 2 L 7 4 4F 4 F A20WE E20EA 1996050900387 19960509 00387 WP 1996 5 9 RRXA96024 1 19960503 A 3260 WARNING LIGHT DOUG DC8 DC863 302198A WP GEAR DOORS ILLUMINATED A RRXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 15 951R 46092 KDAY-KEWR - FLT 118 - AFTER GEAR RETRACTION, DOORS NOT LATCHED LIGHT AND RIGHT ALT GEAR DOOR WARNING LIGHT ON. LIGHTS D ID NOT GO OUT AFTER UPLATCH CHECK. CYCLED GEAR AND EXTENDED FLAPS NO HELP. LIGHTS WENT OUT ON FINAL WITH FLAP EXTENSIO N. MAINTENANCE STILL WORKING DISCREPANCY. (M) 2 L 7 4 4F 4A25 1996050900388 19960509 00388 WP 1996 5 9 RRXA96025 1 19960504 A 2612 FIRE WARNING DOUG DC8 DC863 302198A WP NR 4 ENGINE MALFUNCTIONED A RRXA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 WP 15 964R 46000 KDAY- ENGINE FIRE ON TAKEOFF, BOTH BOTTLES DISCHARGED, LIGHT WENT OUT 5 MINUTES AFTER 2ND DISCHARGED. MX INSPECTED NR 4 ENGINE FOUND NO EVIDENCE OF FIRE, NO PNEUMATIC LEAKS DETECTED ON GROUND POWER RUN. COULD NOT DUPLICATE. FOR PRECAUTIO NARY REMOVED AND REPLACED ALL THREE FIRE LOOPS ON NR 4 ENGINE, LOWER AND BOTH UPPER. ALL CHECK GOOD, ENGINE CHECK GOOD. (M) 2 L 7 4 4F 4A25 1996050900389 19960509 00389 NM 1996 5 9 VNAA9600019 1 19960419 A 3040 328510 HEAT CONTROLLER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT WINDSHIELD FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 437JS 9503 3055 CMH - FLT 4103 - EN ROUTE FROM CMH TO IAD CREW REPORTED THAT THE FIRST OFFICER'S WINDSHIELD HEAT FAILED. AIRCRAFT DIV ERTED TO PIT, WHERE MAINTENANCE REPLACED THE NR 2 WINDSHIELD HEAT CONTROLLER IAW MM 30-42-00. GROUND CHECKED 'GOOD'. A IRCRAFT RETURNED TO SERVICE. PART TOTAL CYCLES, 88. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996050900390 19960509 00390 NM 1996 5 9 VNAA9600020 1 19960420 A 5610 SPSDO328231 WINDSHIELD DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT COCKPIT FAILED A VNAA O OTHER O OTHER CR CRUISE 1 GL 07 423JS 25591 3032 CLT - FLT 4081 - EN ROUTE FROM CLT TO CAK, CREW REPORTED THAT OUTER PANE OF CAPTAIN'S WINDSHIELD FAILED. CREW THEN F OLLOWED ESTABLISHED ABNORMAL PROCEDURES BY DESCENDING FL 100 REDUCING CABIN PRESSURE DIFFERENTAL. FLIGHT CONTINUED TO ITS ORIGINAL DESTINATION, AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. CAK MX REPLACED LT WINDSHIELD IAW MM 56-10-00. AI RCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996050900391 19960509 00391 NM 1996 5 9 VNAA9600021 1 19960423 A 2824 2193552 JET PUMP DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE RT WING DEFECTIVE A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 07 432JS 19195 3045 PIT - FLT 4072 - DURING THE TAKEOFF ROLL, CREW WAS ALERTED BY RT LOW FUEL PRESSURE WARNING. CREW THEN ABORTED THE TAKEO FF AND RETURNED TO THE GATE. PIT MX REPLACED THE RT FUEL JET PUMP IAW MM 28-21-04. GROUND CHECKED GOOD, AIRCRAFT RETUR NED TO SERVICE. PART TOTAL CYCLES, 1,976. 2 H 7 2 4T 4 T RT A45NM E20NE 1996050900392 19960509 00392 NM 1996 5 9 VNAA9600022 1 19960423 A 3150 TO WARNING DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE COCKPIT FALSE WARN A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 07 434JS 3051 TOL - FLT 4029 - DURING THE TAKEOFF ROLL, CREW WAS ALERTED BY A TAKEOFF CONFIGURATION WARNING. CREW ABORTED THE TAKEOF F AND RETURNED TO THE GATE. OUT STATION MX INSPECTED THE AIRCRAFT FOUND NOTHING IRREGULAR. COULD NOT DUPLICATE THE PRO BLEM. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 1996050900393 19960509 00393 NM 1996 5 9 VNAA9600023 1 19960423 A 5610 SPSDO328231 WINDSHIELD DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT COCKPIT BROKEN A VNAA O OTHER O OTHER CR CRUISE 1 GL 07 439JS 7633 3057 PIT - FLT 4059 - EN ROUTE FROM CAE TO PIT, THE OUTER PANE OF LT WINDSHIELD FAILED. CREW FOLLOWED ESTABLISHED ABNORMAL P ROCEDURES BY DESCENDING TO FL 100 (OR LOWER) AND REDUCING THE CABIN PRESSURE DIFFERENTIAL. CREW CONTINUED ON WITH THE FLIGHT AND LANDED AT THE ORIGINAL DESTINATION WITHOUT FURTHER INCIDENT. PIT MX REPLACED THE LT WINDSHIELD IAW MM 56-10- 00. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996050900394 19960509 00394 NM 1996 5 9 VNAA9600024 1 19960425 A 5610 SPSDO328232 WINDSHIELD DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT COCKPIT CRACKED A VNAA O OTHER O OTHER CR CRUISE 1 GL 07 434JS 6485 3051 CVG - FLT 4010 - EN ROUTE FROM PHL INBOUND TO CVG, CREW REPORTED THAT THE FIRST OFFICER'S WINDSHIELD CRACKED. CREW PRO CEEDED ON WITH THE FLIGHT AND LANDED WITHOUT FURTHER INCIDENT AT CVG. MX REPLACED THE F/O'S WINDSHIELD IAW MM 56-11-00 . AIRCRAFT WAS THEN RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996050900395 19960509 00395 NM 1996 5 9 VNAA9600025 1 19960425 A 3150 TO WARNING DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT ACTIVATED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 442JS 3060 AZO - FLT 4165 - RIGHT ALT. TRIPPED OFF LINE DURING TAKEOFF. CREW WAS THEN ALERTED BY SEVERAL AMBER CAS MESSAGES. CR EW THEN ABORTED TAKEOFF AND RETURNED TO THE TAXI WAY. CREW CLEARED ALL CAS MESSAGES IAW QUICK REFERENCE HANDBOOK. C REW THEN CONTINUED ON WITH THE FLIGHT. SUSPECT A TAKEOFF CONFIGURATION PROBLEM WAS THE CAUSE OF THE CAS MESSAGES. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996050900396 19960509 00396 NM 1996 5 9 VNAA9600026 1 19960502 A 3150 TO WARNING DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT SOUNDED A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 07 436JS 3052 PIT - FLT 4014 - DURING THE TAKEOFF ROLL THE CREW WAS ALERTED BY TAKEOFF CONFIGURATION WARNING, CREW THEN ABORTED THE TA KEOFF AND RETURNED TO THE TAXI-WAY. CANCELED THE CAS MESSAGES AND CONTINUED ON WITH THE FLIGHT WITHOUT FURTHER INCIDENT . SUSPECT TRIM MAY HAVE BEEN OUT OF POSITION FOR TAKEOFF. CREW THEN RESET TRIM TO PROPER POSITION FOR TAKEOFF. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996050900397 19960509 00397 NM 1996 5 9 VNAA9600028 1 19960505 A 7332 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE LOOSE A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 07 426JS 3038 PIT - FLT 4046 - DURING THE TAKEOFF ROLL, THE CREW WAS ALERTED BY A LEFT FUEL PRESSURE LOW WARNING. CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. PIT MX INSPECTED THE AIRCRAFT AND DISCOVERED THAT THE CANNON PLUG ON THE LEFT ENGINE FUEL PRESSURE PROBE WAS LOOSE AND DIRTY. PIT MX CLEANED AND SECURED THE CANNON PLUG CONNECTOR IAW MM 3-10-00 AND STD M X PRACTICES, GROUND CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996050900398 19960509 00398 EU 1996 5 9 AALA960498 1 19960401 A 3350 A3060698101 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 3075A 606 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT IN FIRST CLASS CABIN INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR L IGHT STRIP CONNECTORS IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996050900399 19960509 00399 NM 1996 5 9 AALA960508 1 19960312 A 5321 146N5300 DECK PLATE BOEING 757 757223 1384957 NM BS 1681 COORODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 644AA 24602 DECK PLATE HAD CORROSION REMOVED AND AREA LEFT IS BEYOND SRM ALLOWABLE LIMITS. REPAIR PER MRB 757-754. (M) 2 L 7 2 4F RT A2NM 1996050900400 19960509 00400 NM 1996 5 9 AALA960509 1 19960312 A 5320 146N6201 DOOR PAN BOEING 757 757223 1384957 NM R4 DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 644AA 24602 DOOR PAN AFTER BLENDING GOUGE IS BEYOND SRM. REPAIR PER MRB 757-748. (M) 2 L 7 2 4F RT A2NM 1996050900401 19960509 00401 NM 1996 5 9 AALA960510 1 19960312 A 5210 141N63023 DOOR PAN BOEING 757 757223 1384957 NM L1 DOOR GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 644AA 24602 L1 DOOR PAN AFTER BLENDING GOUGE IS BEYOND SRM LIMITS. REPAIR PER MRB 757-751. (M) 2 L 7 2 4F RT A2NM 1996050900402 19960509 00402 NM 1996 5 9 AALA960511 1 19960312 A 5210 DOOR PAN BOEING 757 757223 1384957 NM L4 DOOR GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 644AA 24602 L4 DOOR PAN AFTER BLENDING GOUGE IS BEYOND SRM LIMITS. REPAIR PER MRB 757-752. (M) 2 L 7 2 4F RT A2NM 1996050900403 19960509 00403 NM 1996 5 9 AALA960522 1 19960402 A 5321 146N5300 DECK PLATE BOEING 757 757223 1384957 NM BS 1720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 650AA 24608 DECK PLATE HAS CORROSION REMOVAL ON UPPER SURFACE AT VARIOUS LOCATIONS. MATERIAL REMAINING IS BEYOND SRM LIMITS. PER M RB 757-767. (M) 2 L 7 2 4F RT A2NM 1996050900404 19960509 00404 NM 1996 5 9 AALA960523 1 19960402 A 5315 141N5112 FLOORBEAM BOEING 757 757223 1384957 NM BS 365 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 650AA 24608 FLOORBEAM AT STATION 365, RBL 10 AND RBL 58 HAD CORROSION REMOVED BEYOND SRM LIMITS. PER MRB 757-765. (M) 2 L 7 2 4F RT A2NM 1996050900405 19960509 00405 NM 1996 5 9 AALA960524 1 19960402 A 5315 141N2932 FLOORBEAM BOEING 757 757223 1384957 NM BS 324 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 650AA 24608 FLOORBEAM AT STATION 324 RBL 58 AND RBL 59 HAD CORROSION BLENDED BEYOND SRM LIMITS. PER MRB 75-763. (M) 2 L 7 2 4F RT A2NM 1996050900406 19960509 00406 NM 1996 5 9 AALA960525 1 19960402 A 5210 146N6201 DOOR PAN BOEING 757 757223 1384957 NM R4 DOOR GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 650AA 24608 R-4 DOOR HANDLE PAN HAS A SMALL GOUGE. AFTER BLENDING IS BEYOND SRM LIMITS. PER MRB 757-762. (M) 2 L 7 2 4F RT A2NM 1996050900407 19960509 00407 NM 1996 5 9 AALA960526 1 19960402 A 5320 141N51618 FLOOR STRUCTURE BOEING 757 757223 1384957 NM BS 300 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 650AA 24608 FLOOR STRUCTURE AT STATION 300 RBL 40 HAD CORROSION BLENDED BEYOND SRM LIMITS. PER MRB 757-769. (M) 2 L 7 2 4F RT A2NM 1996050900408 19960509 00408 NM 1996 5 9 AALA960527 1 19960402 A 5210 146N6201 DOOR PANEL BOEING 757 757223 1384957 NM L4 DOOR GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 650AA 24608 L-4 EXTERNAL HANDLE PAN HAS A GOUGE BEYOND SRM LIMITS, AREA WAS BLENDED OUT. PER MRB 757-771. (M) 2 L 7 2 4F RT A2NM 1996050900409 19960509 00409 NM 1996 5 9 AALA960528 1 19960402 A 5310 146N8522 STRUCTURE BOEING 757 757223 1384957 NM BS 1384 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 650AA 24608 AFT CARGO DOOR SURROUND STRUCTURE LOWER STILL CHORD AT STATION 1384, UPPER SURFACE, HAD CORROSION BLENDED BEYOND SRM LIM ITS. PER MRB 757-772. (M) 2 L 7 2 4F RT A2NM 1996050900410 19960509 00410 NM 1996 5 9 AALA960529 1 19960402 A 5330 146N3300 SKIN BOEING 757 757223 1384957 NM BS 36 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 650AA 24608 FUSELAGE SKIN HAS GOUGES BLEND OUT BEYOND SRM LIMITS. PER MRB 757-774. (M) 2 L 7 2 4F RT A2NM 1996050900411 19960509 00411 WP 1996 5 9 AALA960530 1 19960404 A 5312 5910136 BLKHD PLATE DOUG DC9 DC982 3022082 WP BS 1338 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 259AA 49289 AFT SIDE OF STATION 1338 AFT PRESSURE BULKHEAD LOWER SIDE IN AFT CARGO COMPARTMENT HEAVY CORROSION ON PLATE. INSTALLED NEW DOUBLER PLATE SRM 53-14-3. (M) 2 L 7 2 4F A6WE 1996050900412 19960509 00412 WP 1996 5 9 AALA960531 1 19960404 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 259AA 49289 NR 2 SEAT TRACK CORRODED. REPAIRED BY PLUG INSTALLATION PER SRM 5305 FIG 4A. (M) 2 L 7 2 4F A6WE 1996050900413 19960509 00413 NM 1996 5 9 AALA960538 1 19960408 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 781-783 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1758B 48527 FROM STATION 781-783 SEAT TRACK NR 7 BELOW LAV DD ANCHOR HAS CORROSION. REPAIRED PER SRM 53-70-00-0 VOL 1 FIG NR 4. (M ) 2 L 7 3 4F RT A22WE 1996050900414 19960509 00414 NM 1996 5 9 AALA960539 1 19960405 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 810-820 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1758B 48527 DURING C-CHECK, FOUND CORROSION ON NR 5 SEAT TRACK INBOARD FLANGE FROM STATION 810 TO 820 IN MID CABIN. CUT OUT CORROSI ON AND INSTALLED TRACK REPAIR PER SRM 53-70-00-0 VOL 1, FIG 5, SH 1-3. (M) 2 L 7 3 4F RT A22WE 1996050900415 19960509 00415 NM 1996 5 9 AALA960540 1 19960405 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 810-820 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1758B 48527 DURING C-CHECK, FOUND CORROSION ON NR 6 SEAT TRACK INBOARD FLANGE FROM STATION 810 TO 820 IN MID CABIN. CUT OUT CORROSI ON AND INSTALLED TRACK REPAIR PER SRM 53-70-00-0 VOL 1, SH 1-3. (M) 2 L 7 3 4F RT A22WE 1996050900416 19960509 00416 NM 1996 5 9 AALA960541 1 19960408 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1321 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1758B 48527 DURING C-CHECK, FOUND CORROSION ON NR 7 SEAT TRACK IN CABIN AT 'M' LAVATORY STATION 1321. CUT OUT CORRODED TRACK AND IN STALLED PLUG REPAIR PER SRM 53-70-00-0 VOL 1. (M) 2 L 7 3 4F RT A22WE 1996050900417 19960509 00417 NM 1996 5 9 AALA960542 1 19960408 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1321 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1758B 48527 DURING C-CHECK, FOUND CORROSION ON NR 2 SEAT TRACK IN CABIN AT 'L LAVATORY STATION 1321. CUT OUT CORRODED TRACK AND INS TALLED PLUG REPAIR PER SRM 53-70-00-0 VOL I. (M) 2 L 7 3 4F RT A22WE 1996050900418 19960509 00418 NM 1996 5 9 AALA960543 1 19960408 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1321 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1758B 48527 DURING C-CHECK, FOUND CORROSION ON NR 1 SEAT TRACK IN CABIN AT 'L' LAVATORY, STATION 1321. CUT OUT CORRODED TRACK SECTI ON AND INSTALLED PLUG REPAIR PER SRM 53-70-00-00-0 VOK 1. (M) 2 L 7 3 4F RT A22WE 1996050900419 19960509 00419 WP 1996 5 9 AALA960552 1 19960409 A 5321 995782821 PLATE DOUG DC9 DC982 3022082 WP AFT GIRT BAR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 259AA 49289 PLATE IS CORRODED AT AFT GIRT BAR FLOOR FITTING AT FWD SERVICE. REMOVED AND REPLACED WITH NEW PLATE. (M) 2 L 7 2 4F A6WE 1996050900420 19960509 00420 WP 1996 5 9 AALA960553 1 19960409 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 205 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 259AA 49289 CORROSION ON SEAT TRACK AT STATION 205 AND 237. REMOVED AND REPLACED SEAT TRACK. (M) 2 L 7 2 4F A6WE 1996050900421 19960509 00421 EU 1996 5 9 AALA960563 1 19960405 A 3350 A3060698101 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN FLOOR LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 3075A 606 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT RIGHT AISLE AFT CABIN INOPERATIVE. RESECURED LOOSE EMERGENCY FL OR LIGHT STRIP CONNECTOR BY RIGHT AFT ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996050900422 19960509 00422 NM 1996 5 9 AALA960565 1 19960406 A 3397 WIRE BOEING 727 727227 1384078 NM L1 DOOR BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 719AA 20612 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT SYSTEM SIDEWALL LIGHT AT L1 DOOR INOPERATIVE. REPAIRED BROKEN EMERG ENCY FLOOR LIGHT SYSTEM SIDEWALL LIGHT WIRE AT L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996050900423 19960509 00423 EU 1996 5 9 AALA960566 1 19960407 A 3350 A3060698101 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 14053 420 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT LEFT AISLE IN AFT SECTION OF MAIN CABIN INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT STRIP CONNECTOR AT LEFT AISLE IN AFT SECTION OF MAIN CABIN. SYSTEM GROUND CHECKED NORMAL OP ERATION. (M) 2 L 7 2 4F RT A35EU 1996050900424 19960509 00424 EU 1996 5 9 AALA960567 1 19960407 A 3350 LIGHT STRIP AIRBUS 300 A300B4605R 3930308 EU CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 33069 512 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY L3 DOOR FOUND DAMAGED CAUSING SECTION OF LIGHTS AFT OF L3 DOOR T O BE INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BY L3 DOOR. SYSTEM GROUND CHECKED NORMAL OPEATION. (M) 2 L 7 2 4F RT A35EU 1996050900425 19960509 00425 NM 1996 5 9 AALA960570 1 19960410 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 361AA 24042 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 41H INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CO NNECTOR AT PAX SEAT 41H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1996050900426 19960509 00426 NM 1996 5 9 AALA960575 1 19960411 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1964-1966 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1758B 48527 DURING C-CHECK, FOUND CORROSION ON OUTBOARD FLANGE OF NR 1 SEAT TRACK UNDER 'H' LAV, STATION 1964 TO 1966 IN AFT CABIN. BLENDED OUT CORROSION AND INSTALLED STRAP DOUBLER PER ESO 41000, DATED 4-10-96. (M) 2 L 7 3 4F RT A22WE 1996050900427 19960509 00427 NM 1996 5 9 AALA960580 1 19960411 A 3350 02019220011 LAMP ASSY BOEING 767 767323 1385205 NM CABIN SHORTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 381AN 25450 EZE - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEATS 22H, 23H AND 24H INOPERATIVE. PROBLEM DETERMINED TO BE SHORTED LIGHT SOCKET AT SEAT 23H. ISOLATED LIGHT AT SEAT 23H AND REINSTATED SYSTEM WITH SEAT LIGHT 22H AND 24H FUNCTION ING NORMALLY. PLACARDED EMERGENCY EXIT LIGHT AT PAX SEAT 23H. SUBSEQUENTLY REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT P AX SEAT 23H AND REMOVED PLACARD AT MIA/12. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1996050900428 19960509 00428 NM 1996 5 9 AALA960587 1 19960413 A 2913 PV32402F PUMP DOUG MD11 MD11 3023602 NM NR 3 DEFECTIVE A AALA K NONE K FLUID LOSS AP APPROACH 1 SW 07 1759 48481 MIA - FLT 908 - DURING APPROACH TO MIA, NR 3 HYDRAULIC SYSTEM QUANTITY DROPPED TO ZERO. ACCOMPLISHED ALTERNATE LANDING GEAR EXTENSION AND AIRCRAFT LANDED MIA WITHOUT INCIDENT. REPLACED NR 3 ENGINE LOWER HYDRAULIC PUMP. PRECAUTIONARY REPL ACED NR 3 ENGINE UPPER HYDRAULIC PUMP. REPLACED ALL NR 3 SYSTEM HYDRAULIC FILTERS. SYSTEM LEAK AND GROUND CHECKED NORM AL OPERATION. (M) 2 L 7 3 4F RT A22WE 1996050900429 19960509 00429 NM 1996 5 9 AALA960593 1 19960412 A 5330 SKIN DOUG MD11 MD11 3023602 NM DR 1R OPENING DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1758B 48527 DURING C-CHECK, FOUND DAMAGE ON THE LOWER FORWARD CORNER OF R1 DOOR OPENING SURROUND INNER SKIN AT STATIN 420. TRIMMED OUT DAMAGED AREA OF INNER SKIN AND INSTALLED DOUBLER PER EWO 41000, DATED 4-11-96 AND DOUGLAS ROD SKETCH 94-08-24-001. ( M) 2 L 7 3 4F RT A22WE 1996050900430 19960509 00430 NM 1996 5 9 AALA960599 1 19960416 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN INOP A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 710AA 22467 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN MAIN CABIN INOPERATIVE. CORRECTED REVERSE POLARITY CONDITION AT EMERGENCY FLOOR LIGHT STRIP BY PAX SEAT ROW 29. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996050900431 19960509 00431 EU 1996 5 9 RAIA960402 1 19960402 A 7933 MS280343 OIL TEMP BULB BAG JETSTM JETSTM3201 1500217 EU LT ENG FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 337TE 9310 929 STL - FLT 7034 - LEFT OIL TEMPERATURE FLUCTUATES OFF THE TOP END OF THE SCALE ON TAKEOFF, ABORTED TAKEOFF. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE OIL TEMP BULB, PERFORMED GROUND RUNS, OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A56EU 1996050900432 19960509 00432 EU 1996 5 9 RAIA960403 1 19960403 A 7712 31024766 TQ SIGNAL COND BAG JETSTM JETSTM3201 1500217 EU LT ENG FAILED A RAIA A UNSCHED LANDING O OTHER TO TAKEOFF 1 CE 03 429AM 10484 394 879 STL - FLT NR 7424 - LEFT ENGINE ONLY PRODUCED 85 PERCENT TORQUE. MAINTENANCE REPLACED LEFT TORQUE SIGNAL CONDITIONER, G ROUND RUNS GOOD. (M) 2 L 7 2 4T RT A56EU 1996050900433 19960509 00433 NE 1996 5 9 UF6A960206 2 19960226 A 7530 1071590200 LP BLD TAP CLAMP BAG ATP ATP EU PWA PW120 PW126A NE LT ENGINE DISLODGED A UF6A A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 31 854AW 8625 2028 124223 SBN - FLT NR 5756 - LEFT ENGINE WILL NOT MAKE SCHEDULED TORQUE/EXCEEDS ITT LIMITS FOR TAKEOFF POWER AND ENGINE NH EXCEED S LIMITS. MAINTENANCE FOUND NR 1 LP BLEED TAP CLAMP DISLODGED. REPLACED GASKET, INSULATION MUFF AND RESECURED CLAMP ON NR 1 BLEED TAP. ALL ENGINE RUNS CHECK GOOD. (M) 2 L 7 2 4T 4 T RT A27NM E2ONE 1996050900434 19960509 00434 EU 1996 5 9 UF6A960303 1 19960312 A 2430 1PF3 RCCB BAG ATP ATP EU DC ELECT SYS FAILED A UF6A O OTHER N FALSE WARNING CR CRUISE 1 GL 31 855AW 9079 2029 SBN - FLT NR 5721 - NR 1 TRU FELL OFF LINE IN FLIGHT. MAINTENANCE REMOVED AND REPLACED RCCB 1PF3. (M) 2 L 7 2 4T RT A27NM 1996050900435 19960509 00435 EU 1996 5 9 UF6A960308 1 19960318 A 3260 1ENN14 SWITCH BAG ATP ATP EU RT MLG DIRTY A UF6A O OTHER N FALSE WARNING LD LANDING 1 GL 31 853AW 10106 2022 FWA - FLT NR 5727 - RIGHT MAIN LANDING GEAR WOULD NOT INDICATE GREEN. RECYCLED LANDING GEAR AND GOT 3 GREEN LIGHTS. MA INTENANCE FOUND DOWNLOCK SWITCH TO HAVE EXCESSIVE DEBRIS. CLEANED SWITCH AND PERFORMED EXTENSION AND RETRACTION TEST. S YSTEM OPS CHECK GOOD. (M) 2 L 7 2 4T RT A27NM 1996050900436 19960509 00436 EU 1996 5 9 UF6A960402 1 19960403 A 6123 30048000014 AUTOFEATHER BAG ATP ATP EU NR 2 ENGINE FAILED A UF6A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 31 860AW 6913 2037 YNG - FLT 5709 - RIGHT ENGINE AUTOFEATHER UNIT WILL NOT ARM, NO UPTRIM OR FEATHER. MAINTENANCE REMOVED AND REPLACED THE NR 2 AUTOFEATHER UNIT. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4T RT A27NM 1996050900437 19960509 00437 EU 1996 5 9 UF6A96309 1 19960319 A 2611 CG7PT2 SMOKE DETECTOR BAG ATP ATP EU LAVATORY FAILED A UF6A O OTHER N FALSE WARNING CL CLIMB 1 GL 31 852AW 5852 2021 SBN - 5751 - AFTER TAKEOFF SMOKE CWP ILLUMINATED IN LAVATORY. MAINTENANCE REMOVED AND REPLACED THE LAVATORY SMOKE DETEC TOR. (M) 2 L 7 2 4T RT A27NM 1996050900438 19960509 00438 NM 1996 5 9 9609972768 1 19960419 A 5315 FLOOR BEAM BOEING 727 7272M7 138407S NM FS 1166 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 728RW 21741 DURING H-CHECK, FOUND CORROSION ON THE BS 1166 FLOOR BEAM BETWEEN RBL 43 TO 46. REPAIRED BEAM (P/N 65-20824-2) PER EA 2 7-102155. 2 L 7 3 4F A3WE 1996050900439 19960509 00439 NM 1996 5 9 9609982768 1 19960424 A 5313 LONGERON BOEING 727 7272M7 138407S NM FS 992-1000 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 728RW 21741 DURING H-CHECK, FOUND CORROSION ON STR 29L BETWEEN BS 992 TO 1000. REPAIRED STRINGER (P/N 65-56441-3) PER EA 27-102156. 2 L 7 3 4F A3WE 1996050900440 19960509 00440 WP 1996 5 9 9609999859 1 19960425 A 5311 FRAME DOUG DC9 DC951 3022051 WP FS 1292 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 768NC 47729 DURING H-CHECK, FOUND A .375 INCH CRACK IN THE FS 1292 CANTED BULKHEAD AFT OF LONGERON 17R. REPAIRED BULKHEAD (P/N 9911 839-521) PER EA 98-109500. 2 L 7 2 4F A6WE 1996050900441 19960509 00441 NM 1996 5 9 9610005522 1 19960426 A 5315 FLOOR BEAM BOEING 757 757251 1384970 NM FS 1681 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 522US 23616 DURING P-CHECK, FOUND CORROSION ON THE BS 1681 FLOOR BEAM UPPER CHORD AT LBL 32. REPAIRED CHORD (P/N 146N5091) PER EA 5 5-102159. 2 L 7 2 4F RT A2NM 1996050900442 19960509 00442 WP 1996 5 9 9610019163 1 19960426 A 5330 SKIN DOUG DC9 DC914 3022034 WP FS 817 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8906E 45747 DURING LINE CHECK, FOUND TWO CRACKS IN THE FUSELAGE SKIN AT FS 817, LONGERON 16L, BENEATH THE PYLON ATTACH ANGLE. REPAI RED SKIN PER EA 91-105275. 2 L 7 2 4F A6WE 1996050900443 19960509 00443 WP 1996 5 9 9610029859 1 19960426 A 5330 SKIN DOUG DC9 DC951 3022051 WP FS 974-1167 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 768NC 47729 DURING H-CHECK, FOUND CORROSION ON THE FUSELAGE SKIN FROM FS 974 TO 1167 BELOW THE LOWER CARGO DOOR OPENING. REPAIRED S KIN (P/N 59197071-501) PER EA 98-108989. 2 L 7 2 4F A6WE 1996050900444 19960509 00444 WP 1996 5 9 9610039859 1 19960426 A 5315 FLOOR BEAM DOUG DC9 DC951 3022051 WP FS 1167 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 768NC 47729 DURING H-CHECK, FOUND CORROSION ON THE FS 1167 FLOOR BEAM CAP, RIGHT SIDE. REPAIRED BEAM (P/N 9915561-71) PER EA 98-109 432 PER EA 98-109432. 2 L 7 2 4F A6WE 1996050900445 19960509 00445 WP 1996 5 9 9610049941 1 19960501 A 5320 FITTING DOUG DC9 DC932 3022066 WP FS 218-237 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3324L 47103 DURING M-CHECK, FOUND A CRACK IN THE LONGERON 18L CUSP FITTING BETWEEN FS 218 TO 237. REPLACED FITTING PER SRM 51-30-5 AND 51-30-3. 2 L 7 2 4F A6WE 1996050900446 19960509 00446 WP 1996 5 9 9610059973 1 19960501 A 5320 STOP FITTING DOUG DC9 DC931 3022065 WP AFT CABIN DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9337 47346 DURING M-CHECK, FOUND A CRACK IN THE AFT CABIN DOOR LEFT CENTER DOOR STOP FITTING. REPLACED FITTING PER SRM 57-30-2. 2 L 7 2 4F A6WE 1996050900447 19960509 00447 NM 1996 5 9 96FDEA00819 1 19960412 A 5313 STRINGER BOEING 727 727233 138408A NM BS 430-450 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 STR 3R CRACKED AND GOUGED BETWEEN STA 420 TO 440. *S/D* REPLACED STR FROM STA 430 TO 450 PER SRM 53-10-3. 2 L 7 3 4F RT A3WE 1996050900448 19960509 00448 NM 1996 5 9 96FDEA00880 1 19960501 A 5315 BAC1518338 FLOOR BEAM BOEING 727 72725 1384006 NM BS 620 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 NR0555 AND 024, CORROSION AT BS 620 FLOOR BEAM WL 208 LBL 17 TO 51. *S/D* REPAIRED FLOOR BEAM BS 620 WL 208 RBL 15 TO L BL 51 PER FEDEX SRM 53-10-8. 2 L 7 3 4F A3WE 1996050900449 19960509 00449 NM 1996 5 9 96FDEA00912 1 19960502 A 5320 WEB BOEING 727 72725C 138400H NM BS 870 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 124FE 19360 LT STA 870 LOWER INTEGRAL WEB IS CRACKED. FABRICATED A MACHINED BATHTUB FITTING. MATERIAL TO BE 4130 TREATED TO SPECIF ICATION 180 TO 200 KSI CAD PLATE, PRIME AS REQUIRED. INSTALLED BATHTUB FITTING PER ESO 11782 DATED 04-22-96 AND EA 7-53 10-28607. REF SHOP W/O NR L6RU, M09H. 2 L 7 3 4F A3WE 1996050900450 19960509 00450 NM 1996 5 9 96FDEA00913 1 19960504 A 5313 STRINGER BOEING 727 727233 138408A NM BS 480-720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 CORROSION INSIDE UPPER LOBE AT STR 14R FROM STA 480 TO 720E AT SKIN LAP. REMOVED CORROSION OUT OF LIMITS, INSTALLED DOU BLER PER SRM 53-30-3 FIG 5. 2 L 7 3 4F RT A3WE 1996050900451 19960509 00451 NM 1996 5 9 96FDEA00915 1 19960506 A 5320 GUSSET BOEING 727 72725C 138400H NM BS 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 124FE 19360 CABIN INTERIOR STA FS 600 RIB GUSSET IS CRACKED IN TWO AT STR 2L AREA. REPLACED GUSSET WITH 7075-T6 X.063 DOUBLER AS SH OWN IN FIG NR 1 AS PER EA 7-5330-28637 DATED APRIL 30 1996. 2 L 7 3 4F A3WE 1996050900452 19960509 00452 NM 1996 5 9 96FDEA00916 1 19960507 A 5315 FLOOR BEAM BOEING 727 72725 1384006 NM BS 540 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 CORROSION (C53-111-01) ON LOWER FLANGE OF FLOOR BEAM BS 540 LBL 12 WL 200. REMOVED DAMAGED AREA OF BEAM AT BS 540 WL 20 0 RBL 28 TO LBL 20 AND INSTALLED REPAIR PART PER FEDEX SRM 53-10-5 FIG 2. 2 L 7 3 4F A3WE 1996050900453 19960509 00453 NM 1996 5 9 96FDEA00917 1 19960507 A 5320 SUPPORT BOEING 727 72725 1384006 NM BS 540 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 NR0415 AND 036, CORROSION UNDER NUTPLATES ON FRAME UNDER FLOOR SUPPORT. 2 L 7 3 4F A3WE 1996050900454 19960509 00454 NM 1996 5 9 96FDEA00919 1 19960507 A 5330 SKIN BOEING 727 72725 1384006 NM BS 441 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 505FE 18276 NR0498 AND 014, BOND DEGREGATION IN THE FORM OF CORROSION AT BS 441 BETWEEN STR 14 TO 15R, 3.5 BY .3 AREA MARKED. FOUN D CORROSION TO BE OUT OF LIMITS. CUT OUT DAMAGE SECTION AT BS 441 RT, FABRICATED REPAIR PARTS AND INSTALLED AND SEALED PER FEDEX EO 753330-7-23196. 2 L 7 3 4F A3WE 1996050900455 19960509 00455 NM 1996 5 9 96FDEA00920 1 19960507 A 5330 SKIN BOEING 727 72725 1384006 NM BS 360 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 505FE 18276 NR0496 AND 013, CORROSION BETWEEN SKIN AND BONDED DOUBLER AT BS 360 STR 5 TO 6R. 2 L 7 3 4F A3WE 1996050900456 19960509 00456 NM 1996 5 9 96FDEA00921 1 19960507 A 5313 STRINGER BOEING 727 72725 1384006 NM BS 359 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 505FE 18276 NR0099 AND 011, STR 20R CRACKED AT EQUIPMENT COOLING DUCT CLAMP AREA AT STA 359. 2 L 7 3 4F A3WE 1996050900457 19960509 00457 NM 1996 5 9 96FDEA00925 1 19960508 A 5321 FLOOR PANEL BOEING 727 72725 1384006 NM BS 200-288 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 505FE 18276 NR0420 AND 016, CORROSION (C53-221-01) ON FLOOR PANEL UNDER WIRE BUNDLE ON RT SIDE OF CENTER CONSOLE BS 200 TO 288 WL 20 8 RBL 4 TO 12. 2 L 7 3 4F A3WE 1996050900458 19960509 00458 NM 1996 5 9 96FDEA00926 1 19960508 A 5320 69144723 STRINGER TIE BOEING 727 72725 1384006 NM BS 950 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 505FE 18276 MECHANICAL DAMAGE ON STR EXTENSION ON BOTH SIDES OF THE BS 950 FORGING AT STR 8L. REMOVED AND REPLACED STR EXTENSION ON BOTH SIDES OF THE BS 950 FORGING AT STR 8L. 2 L 7 3 4F A3WE 1996050900459 19960509 00459 NM 1996 5 9 96FDEA00927 1 19960424 A 5315 FLOOR BEAM BOEING 727 72725 1384006 NM BS 1030 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 CORROSION (C53-111-01) ON LOWER FLOOR BEAM FLANGE BS 1030 RBL 47 WL 200. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53 -10-1 FIG 4. REPAIRED LOWER FLOOR BEAM FLANGE AT BS 1030 RBL 47 WL 200 IAW SRM 53-10-8 FIG 8. 2 L 7 3 4F A3WE 1996050900460 19960509 00460 NM 1996 5 9 96FEDA00914 1 19960504 A 5313 STRINGER BOEING 727 727233 138408A NM BS 640 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 STA 640 STR 3R CRACKED IN RADIUS. REPAIRED STR PER SRM 53-10-3 FIG 3. 2 L 7 3 4F RT A3WE 1996050900461 19960509 00461 WP 1996 5 9 ABXA9600489 1 19960504 A 2910 7912641924 HYD LINE DOUG DC9 DC931 3022065 WP RT WING LEAKING A ABXA K NONE K J FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 23 924AX 47403 ON FINAL APPROACH, RIGHT HYDRAULIC SYSTEM FAILED WITH LOSS OF ALL HYDRAULIC FLUID WHEN FLAPS WERE SELECTED TO 5 DEGREES. FOUND A HYDRAULIC LINE IN THE RIGHT WING ROOT AREA LEAKING. INSTALLED A TEMPORARY FLEX LINE IAW SPM 29.01. 2 L 7 2 4F A6WE 1996050900462 19960509 00462 SO 1996 5 9 COMA9610139 1 19960502 A 3230 RETRACT MECH EMB 120 EMB120RT SO LANDING GEAR MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 244CA 120217 LANDING GEAR WILL NOT RETRACT. ALL GREEN DOWN INDICATORS AND ALL RED INTRANSIT INDICATORS ARE ILLUMINATED. REVERSED TH E NLG UPLOCK PROXIMITY SENSORS AND DEFERRED SYSTEM PER EMB SNL 032-0015. 2 L 7 2 4T RT A31SO 1996050900463 19960509 00463 EA 1996 5 9 COMA9660077 1 19960501 A 3412 102AH2AG TAT PROB CNDAIR CL600 CL6002B19 EA FUSELAGE FAILED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 924CA 4373 7026 TAT HEAT PROBE CAUTION MESSAGE ILLUMINATED. REPLACED TAT HEAT PROBE. 2 L 7 2 4F RT A21EA 1996050900464 19960509 00464 EA 1996 5 9 COMA9660078 1 19960503 A 3220 16400105 DRAG BRACE CNDAIR CL600 CL6002B19 EA NLG FAILED A COMA K NONE O OTHER AP APPROACH 1 SO 01 916CA 5092 210 7014 LANDING GEAR DISAGREE MESSAGE ON EICAS WHEN L/G SELECTED DOWN. REPLACED THE NLG DRAG BRACE ASSY. 2 L 7 2 4F RT A21EA 1996050900465 19960509 00465 1996 5 9 MWEA96131 4 19960507 A 3460 92743654 THROTTLE SWITCH DOUG DC9 DC932 3022066 WP COCKPIT FAILED A MWEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 502ME 48132 AFTER DEPARTURE AND RAISING GEAR, ALL THREE GEAR UNSAFE LIGHTS REMAINED ON, RETURNED TO MKE. PERFORMED SEVERAL GEAR SWI NGS, COULD NOT DUPLICATE. CHANGED THROTTLE TRANSFER RELAY AND BOTH INDICATOR LIGHT THROTTLE SWITCHES. ALL SYSTEMS CHEC K GOOD IAW MM 32-60-0 AND 76-10-3. 2 L 7 2 4F A6WE 1996050900466 19960509 00466 NM 1996 5 9 SCNA96086 1 19960410 A 5320 INTERCOSTAL BOEING 727 7272J4 1384006 NM BS 1030-1110 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT, AN INTERCOSTAL FLOOR SUPPORT WAS FOUND CORRODED AT BS 1030 TO 1110. CORROSION WAS REMOV ED, INTERCOSTAL WAS TREATED AND PRIMED. FABRICATED AND INSTALLED REPAIR STRAPS IN ACCORDANCE WITH B727 SRM 51-40-4. 2 L 7 3 4F RT A3WE 1996050900467 19960509 00467 NM 1996 5 9 SCNA96087 1 19960410 A 5347 BAC1520841 SEAT TRACK BOEING 727 7272J4 1384006 NM BS 1030-1130 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT, A SEAT TRACK WAS FOUND CORRODED IN THE AFT CARGO COMPARTMENT AT VARIOUS LOCATIONS BETWEE N BS 1030 AND 1130. CLEANED CORROSION, TREATED AND PRIMED SEAT TRACK. FABRICATED AND INSTALLED A NEW SECTION FROM BS 1 050 TO BS 1090 IN ACCORDANCE WITH SRM 53-10-5, FIGURE 1. 2 L 7 3 4F RT A3WE 1996050900468 19960509 00468 NM 1996 5 9 SCNA96088 1 19960412 A 5321 FLOOR WEB BOEING 727 7272J4 1384006 NM BS 1175 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON A FLOOR WEB SECTION AT BS 1175, RT SIDE. REMOVED CORROSION, FABR ICATED REPAIR WEB AND INSTALLED IN ACCORDANCE WITH B727 SRM 51-10-2, 51-30-2 AND MM 51-20-11. 2 L 7 3 4F RT A3WE 1996050900469 19960509 00469 NM 1996 5 9 SCNA96089 1 19960415 A 5311 FRAME BOEING 727 7272J4 1384006 NM BS 274 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT, A STUB FRAME WAS FOUND CRACKED AT TWO PLACES NEAR STRINGER 22R, BS 274. REMOVED DAMAGED MATERIAL, FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH B727 SRM 51-10-2, 51-40-2 AND MM 51-20-11. 2 L 7 3 4F RT A3WE 1996050900470 19960509 00470 NM 1996 5 9 SCNA96090 1 19960415 A 5313 BAC1498131 STRINGER BOEING 727 7272J4 1384006 NM CARGO DOOR AREA CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON THE STRINGER AT THE FRAME CUTOUT ON THE AFT SIDE OF THE AFT CARGO DOOR. REMOVED CORROSION, FABRICATED AND INSTALLED STRINGER REPAIR IN ACCORDANCE WITH B727 SRM 53-10-3. 2 L 7 3 4F RT A3WE 1996050900471 19960509 00471 NM 1996 5 9 SCNA96091 1 19960410 A 5315 BAC1505100997 FLOOR BEAM BOEING 727 7272J4 1384006 NM BS 1070 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON A FLOOR BEAM LOCATED IN THE AFT CARGO AT BS 1070, LBL 70 TO RBL 6 5. CLEANED CORROSION, FABRICATED AND INSTALLED A REPAIR IN ACCORDANCE WITH B727 SRM 53-10-8. 2 L 7 3 4F RT A3WE 1996050900472 19960509 00472 NM 1996 5 9 SCNA96092 1 19960414 A 5400 COWL RIVETS BOEING 727 7272J4 1384006 NM BS 1333-1383 LOOSE A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT, LOOSE AND WORKING RIVETS WERE FOUND AT SEVERAL LOCATIONS NEAR THE NR 2 RIGHT FORWARD COW L, LATCH POSITIONS ABOVE THE CUTOUT, BS 1333 TO 1343 AND BS 1363 TO 1383. FABRICATED FILLER DOUBLER AND SPLICE, INSTALL ED IN ACCORDANCE WITH B727 SRM 51-10-2, 51-30-2 AND 54-30-3. 2 L 7 3 4F RT A3WE 1996050900473 19960509 00473 NM 1996 5 9 SCNA96093 1 19960430 A 3350 BULB BOEING 727 727282 138408T NM CABIN FAILED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 281SC 21949 CENTER AISLE EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED BULBS, OPS CHECK OK. 2 L 7 3 4F RT A3WE 1996050900474 19960509 00474 NM 1996 5 9 SWAA960276 1 19960506 A 5330 SKIN BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED 1 INCH FROM FWD RT CORNER OF AC EXTERNAL RECEPTACLE. REPAIRED PE R BOEING SRM. 2 L 7 2 4F A16WE 1996050900475 19960509 00475 NM 1996 5 9 SWAA960277 1 19960506 A 3350 6104781 BATTERY BOEING 737 7373T5 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 667SW 23063 DURING SCHEDULED RON CHECK, FOUND MID CABIN FLOOR TRACK LIGHTING INOP FROM ROW 19 TO 23. REPLACED BATTERY PACK PER BOEI NG M/M. 2 L 7 2 4F RT A16WE 1996050900476 19960509 00476 NM 1996 5 9 SWAA960278 1 19960506 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 986.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 986.5. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996050900477 19960509 00477 NM 1996 5 9 SWAA960279 1 19960506 A 5210 HINGE SEAL BOEING 737 7373H4 1384600 NM FWD ENTRY DOOR LEAKING A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 309SW 22948 DURING CLIMBOUT, NOTED LOUD AIR SQUEAL FROM FWD ENTRY DOOR, LEVELED OFF AIRCRAFT AT 10,000 WITH CABIN PRESSURE CONTINUOU SLY CLIMBING. AIRCRAFT RETURNED TO RNO AND MADE AN UNEVETFUL LANDING. INSPECTED DOOR, RE-ADJUSTED UPPER HINGE SEAL PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996050900478 19960509 00478 NM 1996 5 9 SWAA960280 1 19960506 A 2410 735511A CSD BOEING 737 7373H4 1384600 NM NR 1 FAILED A SWAA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CR CRUISE 1 SW 07 398SW 27692 EN ROUTE, CREW REPORTED LOSS OF NR 1 AND STANDBY GENERATOR BUSS, AND APU WOULD NOT POWER NR 1. AIRCRAFT RETURNED TO OAK AND MADE AN UNEVETFUL LANDING. REMOVED AND REPLACED NUMBER 1 CSD AND LEAKED CHECKED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996050900479 19960509 00479 NM 1996 5 9 SWAA960281 1 19960506 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 277 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SPECIAL VISIT CHECK, FOUND FUSELAGE SKIN CRACK AT BS 277, AT S16L, APPROX 4 INCHES LONG. REPAIRED PER BOEING SRM . 2 L 7 2 4F RT A16WE 1996050900480 19960509 00480 NM 1996 5 9 SWAA960282 1 19960506 A 5320 FRAME BOEING 737 7372H4 138448C NM EMERGENCY EXIT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 96SW 23055 DURING SCHEDULED C3 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT AFT FRAME CRACKED APPROX .75 INCH LONG THROUGH RIVET AT FL OOR LINE. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996050900481 19960509 00481 NM 1996 5 9 SWAA960283 1 19960506 A 5330 SKIN BOEING 737 7372H4 138448C NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 62SW 22060 DURING SCHEDULED B-CHECK, FOUND FUSELAGE SKIN CRACKED APPROX .1875 INCH AT UPPER HINGE CUTOUT AT AFT SERVICE DOOR. REPA IRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996050900482 19960509 00482 NM 1996 5 9 SWAA960284 1 19960505 A 3230 UPLOCK ACTUATOR BOEING 737 7375H4 138449D NM LT GEAR FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 512SW 24189 AFTER TAKEOFF, LEFT MAIN GEAR UPLOCK FAILURE, RED UNSAFE LIGHT REMAINS ILLUMINATED AND GEAR FREE FALLS TO DOWN AND LOCKE D POSITION WITH GEAR HANDLE IN OFF. AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING. REPLACED LEFT GEAR UPLOCK ACTUATOR, MODULE CHECK VALVE AND PERFORMED GEAR RETRACTION TEST PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996050900483 19960509 00483 NM 1996 5 9 SWAA960285 1 19960225 A 3350 1000679 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 28SW 21339 AT GATE, FOUND AFT SERVICE DOOR OVERHEAD EMERGENCY LIGHT BLINKING. REPLACED LIGHT PACK ASSEMBLY PER BOEING M/M. 2 L 7 2 4F A16WE 1996050900484 19960509 00484 NM 1996 5 9 SWAA960286 1 19960113 A 3350 61046791 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 50SW 21447 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY ESCAPE SLIDE LIGHTING INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F A16WE 1996050900485 19960509 00485 NM 1996 5 9 SWAA960287 1 19960403 A 3350 900835A BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED SERVICE CHECK, FOUND CABIN OVERWING EMERGENCY EXIT SIGN INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F A16WE 1996050900486 19960509 00486 NM 1996 5 9 SWAA960288 1 19960121 A 3350 900835A BATTERY PACK BOEING 737 7372H4 138448C NM FWD ENTRY DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 64SW 22062 DURING SCHEDULED TERMINAL CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F A16WE 1996050900487 19960509 00487 NM 1996 5 9 SWAA960289 1 19960128 A 3350 900835A BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 68SW 22357 DURING SCHEDULED SERVICE CHECK, FOUND LT AND RT CENTER CABIN EMERGENCY EXIT WALL LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F A16WE 1996050900488 19960509 00488 NM 1996 5 9 SWAA960290 1 19960406 A 3350 900835A BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 73SW 22673 DURING SCHEDULED SERVICE CHECK, FOUND FWD AND MID CABIN EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACKS PER BOEING M /M. 2 L 7 2 4F A16WE 1996050900489 19960509 00489 NM 1996 5 9 SWAA960291 1 19960405 A 3350 1060031101 SIGN BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 82SW 22731 DURING SCHEDULED TERMINAL CHECK, FOUND AFT RIGHT OVERHEAD EMERGENCY EXIT SIGN INOP. REPLACED SIGN PER BOEING M/M. 2 L 7 2 4F A16WE 1996050900490 19960509 00490 NM 1996 5 9 SWAA960292 1 19960316 A 3350 900835A BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 87SW 22903 DURING SCHEDULED TERMINAL CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F A16WE 1996050900491 19960509 00491 NM 1996 5 9 SWAA960293 1 19960212 A 3350 1000679 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 90SW 22905 DURING SCHEDULED A2 CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK AND LIGHT ASSEMBLY PER BOEING M/M. 2 L 7 2 4F A16WE 1996050900492 19960509 00492 NM 1996 5 9 SWAA960294 1 19960225 A 3350 900835A BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 94SW 23053 DURING SCHEDULED SERVICE CHECK, FOUND OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F A16WE 1996050900493 19960509 00493 NM 1996 5 9 SWAA960295 1 19960426 A 3350 6104781 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 102SW 23108 DURING SCHEDULED A1 CHECK, FOUND FWD LT AND RT EMERGENCY ESCAPE SLIDE LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M . 2 L 7 2 4F A16WE 1996050900494 19960509 00494 NM 1996 5 9 SWAA960296 1 19960429 A 3350 900835A BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED A1 CHECK, FOUND AFT CABIN FLOOR LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F A16WE 1996050900495 19960509 00495 NM 1996 5 9 SWAA960297 1 19960413 A 3350 6104781 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED A1 CHECK, FOUND AFT CABIN FLOOR LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F A16WE 1996050900496 19960509 00496 NM 1996 5 9 SWAA960298 1 19960108 A 3350 6104781 BATTERY PACK BOEING 737 7372K6 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED A1 CHECK, FOUND CABIN FLOOR LIGHTS INOP AT OVERWING EXIT. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996050900497 19960509 00497 NM 1996 5 9 SWAA960299 1 19960310 A 3350 900835A BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED A1 CHECK, FOUND MID CABIN CEILING LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F A16WE 1996050900498 19960509 00498 NM 1996 5 9 SWAA960300 1 19960305 A 3350 20131 BATTERY PACK BOEING 737 7373H4 1384600 NM COCKPIT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED SERVICE CHECK, FOUND COCKPIT EMERGENCY LIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996050900499 19960509 00499 NM 1996 5 9 SWAA960301 1 19960122 A 3350 20121 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK AND CHARGER HOU SING PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996050900500 19960509 00500 NM 1996 5 9 SWAA960302 1 19960130 A 3350 20121 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 330SW 23694 DURING SCHEDULED TERMINAL CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK AND HOUSING PER BOEIN G M/M. 2 L 7 2 4F RT A16WE 1996050900501 19960509 00501 NM 1996 5 9 SWAA960303 1 19960420 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY OVERHEAD EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M /M. 2 L 7 2 4F RT A16WE 1996050900502 19960509 00502 NM 1996 5 9 SWAA960304 1 19960129 A 3350 20121 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 378SW 26585 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOP AT MID CABIN. REPAIRED BROKEN WIRES AND REPLA CED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996050900503 19960509 00503 NM 1996 5 9 SWAA960305 1 19960205 A 3350 BATT PACK BASE BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 604SW 27955 DURING SCHEDULED C3 CHECK, FOUND LEFT AFT EMERGENCY EXIT LIGHTING INOP. REPLACED BATTERY PACK BASE PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996050900504 19960509 00504 NM 1996 5 9 SWAA960306 1 19960323 A 3350 20131 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 604SW 27955 DURING SCHEDULED A1 CHECK, FOUND OVERHEAD EXIT SIGNS INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996050900505 19960509 00505 NM 1996 5 9 SWAA960307 1 19960127 A 3350 20121 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 607SW 27927 DURING SCHEDULED A1 CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996050900506 19960509 00506 NM 1996 5 9 SWAA960308 1 19960310 A 3350 20121 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 607SW 27927 DURING SCHEDULED SERVICE CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996050900507 19960509 00507 NM 1996 5 9 SWAA960309 1 19960404 A 3350 20131 BATTERY PACK BOEING 737 7373G7 1384595 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR AND GALLEY EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996050900508 19960509 00508 NM 1996 5 9 SWAA960310 1 19960315 A 3350 20131 BATTERY PACK BOEING 737 7373G7 1384595 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996050900509 19960509 00509 NM 1996 5 9 SWAA960311 1 19960307 A 3350 20131 BATTERY PACK BOEING 737 7373G7 1384595 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED SERVICE CHECK, FOUND RIGHT AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK PER BOEIN G M/M. 2 L 7 2 4F RT A16WE 1996050900510 19960509 00510 NM 1996 5 9 SWAA960312 1 19960424 A 3350 20131 BATTERY PACK BOEING 737 7373G7 1384595 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996050900511 19960509 00511 NM 1996 5 9 SWAA960313 1 19960426 A 3350 20121 BATTERY PACK BOEING 737 7373G7 1384595 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED RON CHECK, FOUND LEFT AFT DOOR EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996050900512 19960509 00512 NM 1996 5 9 SWAA960314 1 19960303 A 3350 20131 BATTERY PACK BOEING 737 7373Q8 1384670 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 689SW 23387 DURING SCHEDULED A2 CHECK, FOUND OVERWING EXIT LIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996050900513 19960509 00513 NM 1996 5 9 SWAA960315 1 19960203 A 3350 20131 BATTERY PACK BOEING 737 7373G7 1384595 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 690SW 23783 DURING SCHEDULED SERVICE CHECK, FOUND AFT GALLEY AND CENTER OVERHEAD EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996050900514 19960509 00514 NM 1996 5 9 SWAA960316 1 19960221 A 3350 20131 BATTERY PACK BOEING 737 737317 138447P NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 693SW 23174 DURING SCHEDULED C4 CHECK, FOUND CENTER AISLE AND LT EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK AND CONNECTOR PI NS PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996050900515 19960509 00515 NM 1996 5 9 UPS96220047 1 19960410 A 5530 FORGING BOEING 727 72725C 138400H NM VERT STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE C-HFEC INSP, DET CRACK ON RT SIDE OF VERT STAB FRONT SPAR FORGING AT FIRST HOLE AFT OF STA 1233 TOP ROW OF FASTENERS. CRACK IS .5 INCH LONG RUNS AFT OF HOLE. STOP DRILLED CRACK, REPAIRED VERT STAB CRACK PER DRAWING 65-6234 6 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996050900516 19960509 00516 NM 1996 5 9 UPS96220048 1 19960410 A 5531 FORGING BOEING 727 72725C 138400H NM VERT STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 INSPECTION TYPE C-NFEC, DET A CRACK ON RT SIDE OF VERT STAB FRONT SPAR FORGING AT 1ST HOLE OF STA 1233 BOTTOM ROW OF FAS TENERS. CRACK IS 1 INCH LONG AND RUNS A FT OF HOLE. STOP DRILLED CRACK, REPAIRED PER DRAWING 65-62346 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996050900517 19960509 00517 NM 1996 5 9 UPS96220049 1 19960422 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 970 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE 'C', SHEAR TIE IS CRACKED AT STA 970 AND STR 9L. REMOVED AND FAB REPLACEMENT PART IAW SRM 51-10-1 AND 5 1-30-2, INSTALLED LED SHEAR TIE IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996050900518 19960509 00518 NM 1996 5 9 UPS96220050 1 19960422 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 970 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE 'C', SHEAR TIE CRACKED AT STA 970 AND STR 5R. REMOVED AND FAB REPLACEMENT PART IAW SRM 51-10-1 AND 51-3 0-2, INSTALLED SHEAR TIE IAW 51-30-2. 2 L 7 3 4F A3WE 1996050900519 19960509 00519 NM 1996 5 9 UPS96220051 1 19960503 A 5741 BOTTLE PIN BOEING 727 72727C 138400J NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE 'C', RT WING FWD BOTTLE PIN HAS CORROSION ON MATING FLANGE. REMOVED AND REPLACED RT TERMINAL PIN IAW MM 57-41-1. 2 L 7 3 4F A3WE 1996050900520 19960509 00520 NM 1996 5 9 UPS96220052 1 19960503 A 5741 106051615 BUSHING BOEING 727 72727C 138400J NM RT FWD WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE 'C', RT WING FWD BOTTLE PIN HOLE HAS CORROSION. REMOVED AND REPLACED BOTTLE PIN BUSHING FWD IAW MM 57-4 1-11. 2 L 7 3 4F A3WE 1996050900521 19960509 00521 NM 1996 5 9 UPS96220053 1 19960504 A 5720 WEB BOEING 727 72727C 138400J NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE 'C', RT WING WEB CRACKED AT FS 106.8 APPROX 6 INCHES FROM LWR END. FAB AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 57-20-2, 51-40-2 AND 51-30-2. 2 L 7 3 4F A3WE 1996050900522 19960509 00522 NM 1996 5 9 UPS96220054 1 19960504 A 5320 ANGLE BOEING 727 72727C 138400J NM BS 485 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE 'C', FRAME 485 ANGLE CRACKED AT STR 19L. FAB AND INSTALLED FRAME REPAIR AND DOUBLER IAW SRM 53-10-2, BA C DRAWING 65-40509 SRM 51-32. 2 L 7 3 4F A3WE 1996050900523 19960509 00523 NM 1996 5 9 UPS96420026 1 19960505 A 5730 SKIN BOEING 747 747121 1384871 NM LT WING TE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION, I/B TRAILING EDGE WING PANEL HAS A TWO FT CRACK ON BOTTOM OF PANEL, CAUSED BY DAMAGED O/B MLG FOLLOW UP DOOR . L/E WRITTEN UP ON ITEM 1 LOG PAGE 751782. INSTALLED SPEED TAPE, AWAITING EO FOR SAID INTRIM REPAIR. DEF PER NR 747- 5700-8279A D109480 ASSIGNED. 2 L 7 4 4F A20WE 1996050900524 19960509 00524 NM 1996 5 9 UPS96420027 1 19960505 A 5753 SKIN BOEING 747 747121 1384871 NM LT TE FLAP DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION, FWD SIDE OF LT WING I/B TRAILING EDGE FLAP HAS TWO, .375 INCH DIA HOLES, 5 INCHES APART, CORE NOT DAMAGED. P ER SRM 51-40-06 PG 30A APPLIED SPEED TAPE AND DEF UNDER D-NOTE: THIS DEF GOOD FOR 20 FLT HOURS PER SRM 51-40-06 D109465 ASSIGNED. 2 L 7 4 4F A20WE 1996050900525 19960509 00525 NM 1996 5 9 UPS96520025 1 19960505 A 5350 141N782012 RADOME BOEING 757 75724APF 1384969 NM FWD FUSELAGE FAILED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 419UP 23906 INSPECTION, A/C NOSE RADOME BUCKLED/CAVED IN AT UPPER MIDDLE PORTION. APPEARS TO HAVE BEEN RADOME STRUCTURAL FAILURE. N O EVIDENCE OF BIRD OR LIGHTNING STRIKE. *S/D* REPLACED RADOME IAW MM 53-12-01. 2 L 7 2 4F RT A2NM 1996050900526 19960509 00526 WP 1996 5 9 UPS96820055 1 19960423 A 5711 3646971 SPAR DOUG DC8 DC873F 302199F WP WS 60 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE 'C', REAR SPAR UPPER CHORD ANGLE 9 CRACK APPROX XCW60 FS 850 LT W/W. REPAIRED SPAR CHORD PER SRM 53-2-5 FIG 2 AND DOUBLER DRAWING 3646971. 2 L 7 4 4F RT 4A25 1996050900527 19960509 00527 WP 1996 5 9 UPS96820056 1 19960415 A 5755 56552652 PANEL DOUG DC8 DC873F 302199F WP NR 1 SPOILER DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE 'C', RT WING NR 1 SPOILER PANEL DELAMINATION ON BOTTOM SIDE. REPLACED SPOILER PANEL PER MM 27-01-00. 2 L 7 4 4F RT 4A25 1996050900528 19960509 00528 WP 1996 5 9 UPS96820057 1 19960429 A 5320 BAC14902685 ANGLE DOUG DC8 DC873F 302199F WP BS 781 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE 'C', T-ANGLE CRACKED AT FS 781 XLW LONGERON 23R. REPAIRED ANGLE PER SRM 53-2-0. 2 L 7 4 4F RT 4A25 1996050900529 19960509 00529 WP 1996 5 9 UPS96820058 1 19960424 A 5320 WEB DOUG DC8 DC873F 302199F WP BS 781 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE 'C', WEB CRACKED AT STA 781 LONGERON 23R. REPAIRED WEB PER DC8-5350-7876. 2 L 7 4 4F RT 4A25 1996050900530 19960509 00530 WP 1996 5 9 UPS96820059 1 19960419 A 5712 5710123 RIB DOUG DC8 DC873F 302199F WP LT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE 'C', 4 RIBS CRACKED LT WING L/E ABOVE I/B FUELING PORT. REPAIRED RIBS PER SRM 57-2-0. 2 L 7 4 4F RT 4A25 1996050900531 19960509 00531 WP 1996 5 9 UPS96820060 1 19960419 A 5320 36410041N FITTING DOUG DC8 DC873F 302199F WP FS 878 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE 'C', HEAVY CORROSION ON VERTICAL FITTING ABOVE LONGERON 24L FS 878. REPLACED ANGLE PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996050900532 19960509 00532 WP 1996 5 9 UPS96820061 1 19960429 A 5313 97585083 LONGERON DOUG DC8 DC873F 302199F WP FS 1163 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE 'C', LONGERON 36 LT FS 1163 CRACKED. REPLACED LONGERON SECTION PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996050900533 19960509 00533 NE 1996 5 9 WWMA9600038 2 19960421 A 7261 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LEFT FAILED A WWMA A E UNSCHED LANDING ENGINE SHUTDOWN J K WARNING INDICATION FLUID LOSS CR CRUISE 1 WP 15 283AE 340B283 THE LEFT ENGINE OIL PRESSURE WARNING ILLUMINATED IN FLIGHT WITH FLUCTUATING OIL PRESSURE, THE ENGINE WAS SHUT DOWN IN FL IGHT. MAINTENANCE FOUND THE ENGINE TO HAVE LOST OIL BEYOND SERVICABLE LIMITS. REPLACED THE LEFT ENGINE AND RETURNED TH E AIRCRAFT TO SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE 1996050900534 19960509 00534 WP 1996 5 9 WWMA9600039 2 19960422 A 7530 8961153 BLEED AIR GASKET BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UAR 01514 WP RT ENGINE DEFECTIVE A WWMA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 15 958AE 958 THE RIGHT ENGINE HAD FLUCTUATING AND LOW TORQUE ON CLIMBOUT. AIRCRAFT RETURNED TO FIELD WITHOUT INCIDENT. MAINTENANCE FOUND A DAMAGED BLEED AIR GASKET ON THE RIGHT ENGINE. THE GASKET WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A56EU E4WE 1996050900535 19960509 00535 EU 1996 5 9 WWMA9600040 1 19960422 A 2910 1379305A155 FLEX LINE BAG JETSTM JETSTM3201 1500217 EU RT MLG RUPTURED A WWMA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 15 961AE 961 THE CREW REPORTED THEY LOST ALL HYDRAULIC PRESSURE. THE AIRCRAFT LANDED IN LAX WITHOUT INCIDENT. MAINTENANCE FOUND RIG HT LANDING GEAR UP FLEX LINE RUPTURED. THE LINE WAS REPLACED, GEAR SWINGS AND FLUID LOSS CHECKS WERE PERFORMED. 2 L 7 2 4T RT A56EU 1996050900536 19960509 00536 EU 1996 5 9 WWMA9600041 1 19960425 A 2611 72111211002 SMOKE DETECTOR BAG JETSTM JETSTM3201 1500217 EU CARGO COMPT DIRTY A WWMA O OTHER N FALSE WARNING CR CRUISE 1 WP 15 941AE 941 THE CARGO SMOKE LIGHT ILLUMINATED TWICE INTERMITTENTLY THEN EXTINGUISHED. MAINTENANCE CLEANED THE CARGO SMOKE DETECTOR SENSOR AND VACUUMED THE CARGO COMPARTMENT. 2 L 7 2 4T RT A56EU 1996050900537 19960509 00537 EU 1996 5 9 WWMA9600042 1 19960425 A 2611 721112110 SMOKE DETECTOR SAAB SF340 340B 7860101 EU LAVATORY DIRTY A WWMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 15 307AE 340B307 THE LAVATORY SMOKE LIGHT ILLUMINATED AT 100 KNOTS DURING TAKEOFF ROLL, THE CREW ABORTED THE TAKEOFF. MAINTENANCE CLEANE D THE LAVATORY SMOKE DETECTOR AND RETURNED THE AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 1996050900538 19960509 00538 EU 1996 5 9 WWMA9600043 1 19960426 A 3230 TOWBAR PIN BAG JETSTM JETSTM3201 1500217 EU NOSE GEAR NOT REMOVED A WWMA O OTHER J WARNING INDICATION TO TAKEOFF 1 WP 15 953LM 953 ON TAKEOFF AFTER RAISING THE LANDING GEAR THE RED NOSE GEAR INTRANSIT LIGHT STAYED ON, THE GEAR WAS CYCLED AND THE LIGHT WENT OUT. ALL OTHER INDICATIONS WERE NORMAL. UPON INVESTIGATION MAINTENANCE FOUND THE TOW BAR PIN INSTALLED ON THE NO SE GEAR TORQUE LINKS. THE PIN WAS REMOVED AND GEAR SWINGS WERE PERFORMED. 2 L 7 2 4T RT A56EU 1996050900539 19960509 00539 EU 1996 5 9 WWMA9600044 1 19960505 A 2710 AILERON CONTROLS SAAB SF340 340B 7860101 EU LEFT/RIGHT LACK OF LUBE A WWMA O OTHER O OTHER CR CRUISE 1 WP 15 247AE 340B247 CREW REPORTED, THAT THE ROLL CONTROL WAS ABNORMAL, AT LOWER AIRSPEEDS. ROLL TRIM CORRECTIONS VARYING LEFT TO RIGHT, BUT GENERAL TENDENCY IS A LEFT ROLL AS INDICATED AIRSPEED INCREASES. AILERONS FELL HEAVIER THAN NORMAL. QUICK SNAP INPUTS OF AILERON REQUIRED TO MAINTAIN WINGS LEVEL AT LANDING AIRSPEEDS AND CONFIGURATION. PILOT SUSPECTS CONTROL BALANCE OR R IGGING PROBLEMS. MAINTENANCE PERFORMED CHECK OF AILERON CONTROL AND INSPECTION OF AILERON CONTROL IAW SAAB 340B AMM 27- 10-00, AILERON SYSTEM FELT GOOD ON THE GROUND. GREASED LEFT AND RIGHT AILERON HINGE POINTS AND FOUND NO EVIDENCE OF BIN DING. ROLL PITCH SYSTEM CHECKED GOOD IAW SAAB AMM. 2 L 7 2 4T RT A52EU 1996050900540 19960509 00540 EU 1996 5 9 WWMA9600045 1 19960506 A 3520 OXY MASKS BAG JETSTM JETSTM3201 1500217 EU CABIN DEPLOYED A WWMA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 15 966AE 966 ON AIRCRAFT PREFLIGHT CREW REPORTED, THAT THE OXYGEN MASKS DEPLOYED. MAINTENANCE PERFORMED A FUNCTIONAL CHECK OF THE PA SSENGER OXYGEN SYSTEM AND REPACKED THE MASKS. 2 L 7 2 4T RT A56EU 1996050900541 19960509 00541 EU 1996 5 9 96ZZZX2305 1 19960416 A 2913 PV304426 PUMP BAG JETSTM JETSTM3201 1500217 EU HYD SYSTEM FAILED A VTZA O OTHER J WARNING INDICATION AP APPROACH 1 EA 27 480UE 894 CRW/IAD - FLT 6397 - DURING APPROACH TO LANDING AT 1615 HRS ON 4-16-96, DECLARED AN EMERGENCY DUE TO THE NOSE GEAR NOT I NDICATING DOWN AND LOCKED WHEN GEAR WAS EXTENDED. FLIGHT CREW PERFORMED AN EMERGENCY EXTENSION AND GEAR INDICATED SAFE. AIRCRAFT LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE PERFORMED AN INSPECTION AND REPLACED BOTH MAIN HYDRAULIC FILTE R CARTRIDGES AND MAIN HYDRAULIC PUMPS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. REFERENCE OPERATOR CO NTROL NR VTZA96153. 2 L 7 2 4T RT A56EU 1996050900542 19960509 00542 EU 1996 5 9 96ZZZX2306 1 19960309 A 3610 6714D050000 BLEED REG AIRBUS 320 A320231 3930325 EU NR 2 ENGINE FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 620AW 11869 00294 052 LAS/SEA - FLT 0843 - AIR TURN-BACK. CLASS 1 ECAM MESSAGE 'AIR ENGINE 2 BLEED ABNORMAL PRESSURE. CREW REPORTED THAT ON DESCENT BACK TO LAS, THE NR 2 ENGINE BLEED AIR WOULD RESET AND H.P. VALVE OPENED. PLACED ON MEL 36-11-1. MEL CLEARED 3 -20-96: REMOVED AND REPLACED THERMO TEMP LIMITER SOLENOID AND BLEED PRESSURE REGULATOR VALVE. REFERENCE OPERATOR CONTR OL NR AWXA960118. 2 L 7 2 4F RT A28NM 1996050900543 19960509 00543 NM 1996 5 9 ASAA9610052 1 19960412 A 5320 65621241 DOOR SILL BOEING 737 737298C 1384490 NM BS 380-480 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING C-CHECK, CORROSION WAS FOUND ON THE MAIN CARGO DOOR LOWER SILL CHORD, STA 380 - STA 480, LBL 65. REPAIRED PER EA 5330-01247 AND BOEING TELEX ASA-SEA-96-017RR AND ASA-SEA-96-167RR. (X) 2 L 7 2 4F RT A16WE 1996050900544 19960509 00544 NM 1996 5 9 ASAA9610053 1 19960416 A 3350 6013211 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING CREW PRE-FLIGHT, CREW REPORTED THE RT WING EMERGENCY EXIT LIGHT WAS INOPERATIVE. REPLACED EXIT LIGHT BATTE RY PACK AND LIGHT OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1996050900545 19960509 00545 NM 1996 5 9 ASAA9610054 1 19960417 A 5210 DOOR MECHANISM BOEING 737 7372X6C 1384552 NM L2 DOOR OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING MAINTENANCE CHECK, THE L-1 ENTRY DOOR WAS DIFFECULT TO CLOSE. ADJUSTED L1 DOOR MECHANISM PER MM AND DOOR O PERATED NORMALLY. 2 L 7 2 4F RT A16WE 1996050900546 19960509 00546 NM 1996 5 9 ASAA9610055 1 19960419 A 5540 6550866501 FITTING BOEING 737 737298C 1384490 NM RUDDER STA 86.59 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING C-CHECK, THE RUDDER HINGE TO VERTICAL STABILIZER ATTACH BRACKET AT RUDDER STA 86.59 WAS FOUND CRACKED IN TH REE PLACES. REPLACED ATTACH BRACKET. FOUND HINGE FAIRING CHAFING BRACKET. REPAIRED NR 4 HINGE FAIRING IAW EA 5540-010 14 AND BOEING 737-200, SB 737-55-1107. (X) 2 L 7 2 4F RT A16WE 1996050900547 19960509 00547 NM 1996 5 9 ASAA9610056 1 19960420 A 2432 CA72720 BATTERY BOEING 737 737298C 1384490 NM MAIN BATT COMPT DISCHARGED A ASAA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 NM 01 745AS 8975 4 20794 KTN - FLT 65 - DURING TAXI IN, CREW REPORTED THE EMERGENCY EXIT LIGHTS ILLUMINATED, AND WOULD NOT EXTINGUISH. MAINTENAN CE REMOVED AND REPLACED MAIN BATTERIES AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1996050900548 19960509 00548 NM 1996 5 9 ASAA9640029 1 19960416 A 3350 654681530 TRACK LIGHT BOEING 737 7374Q8 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 773AS 25106 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 15-18. RECON NECTED TRACK AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1996050900549 19960509 00549 NM 1996 5 9 ASAA9640030 1 19960418 A 3397 WIRE BOEING 737 7372X6C 1384552 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 JNU - DURING MAINTENANCE CHECK, THE TWO AFT MOST RED EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNEC TED WIRES AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1996050900550 19960509 00550 NM 1996 5 9 ASAA9640031 1 19960418 A 3397 WIRE BOEING 737 7374Q8 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 772AS 25105 JNU - DURING MAINTENANCE CHECK, SEVERAL EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE FROM ROW 22 TO THE AFT CABIN. RECONNECTED WIRES AT FOUR SOCKETS FROM ROW 22 TO THE AFT CABIN AND ALL EMERGENCY EXIT FLOOR TRACK LIGHTS OPERATE D NORMALLY. 2 L 7 2 4F RT A16WE 1996050900551 19960509 00551 NM 1996 5 9 ASAA9640032 1 19960419 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 763AS 25100 SEA - DURING MAINTENANCE CHECK, THE FORWARD AND AFT RED EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECON NECTED WIRE HARNESSES AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1996050900552 19960509 00552 WP 1996 5 9 ASAA9680100 1 19960416 A 5210 DOOR MECHANISM DOUG DC9 DC982 3022082 WP L1 DOOR OUT OF ADJUST A ASAA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 NM 01 936AS 49363 SEA - FLT 191 - PRIOR TO DEPARTURE, CREW REPORTED THE L1 DOOR HANDLE WOULD NOT REMAIN IN THE LOCKED POSITION AND THE DOO R WARNING LIGHT WOULD NOT EXTINGUISH. RERIGGED THE L1 DOOR MECHANISM PER MM AND OPERATED NORMALLY. (X) 2 L 7 2 4F A6WE 1996050900553 19960509 00553 WP 1996 5 9 ASAA9680101 1 19960416 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1061 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 953AS 49386 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FRAME AT Y1061, X+1, Z-49. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM. TAT: 28,268. TAC: 18,804. (X) 2 L 7 2 4F A6WE 1996050900554 19960509 00554 WP 1996 5 9 ASAA9680102 1 19960416 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1322 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 953AS 49386 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FRAME AT Y1322, X+15 TO X-15, Z-43. REMOVED DAMAGED AREA AND INSTALLED N EW PIECES IAW DC-9 SRM. TAT: 28,268 HOURS. TAC: 18,804. (X) 2 L 7 2 4F A6WE 1996050900555 19960509 00555 WP 1996 5 9 ASAA9680103 1 19960416 A 5320 SHEAR TIE DOUG DC9 DC982 3022082 WP BS 1322 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 953AS 49386 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON SHEAR TIE AT Y1322, X-5, Z-43. REMOVED DAMAGED AREA AND INSTALLED NEW PI ECES IAW DC-9 SRM. TAT: 28,268. TAC: 18,804. (X) 2 L 7 2 4F A6WE 1996050900556 19960509 00556 WP 1996 5 9 ASAA9680104 1 19960423 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 936AS 16166 49363 PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND DIM. REPLACED THE LIGHT ASSEMBLY AND OPE RATED NORMALLY. (X) 2 L 7 2 4F A6WE 1996050900557 19960509 00557 NM 1996 5 9 AWXA960165 1 19960328 A 5315 FLOOR BEAM BOEING 757 757225 1384959 NM BS 350 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 915AW 22209 PAE - FLT 3838 - DURING ROUTINE SCHEDULED C-3 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM AT BS 350, RBL 2 - LBL 20 , WL 208. PER ERR, BLENDED CORROSION ON BEAM. FABRICATED REPAIR ANGLE, ALODINED, PRIMED, AND INSTALLED PART WITH SEALA NT PER ER 5-53-12-05, AND BOEING TELEX TCO-PAN-96-0413RR. (X) 2 L 7 2 4F RT A2NM 1996050900558 19960509 00558 EU 1996 5 9 AWXA960175 1 19960406 A 3350 321430 BATTERY PACK AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 636AW 098 PXH - FLT 0031 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE. FOUND BAD BATTERY PACK. REMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD. (X) 2 L 7 2 4F RT A28NM 1996050900559 19960509 00559 NM 1996 5 9 IXKA960009 1 19960402 A 3244 313061M TIRE BOEING 727 727225 1384077 NM NR 3 FLAT A IXKA K NONE O OTHER LD LANDING 1 EA 25 8882Z A2481517 21579 NEWARK TO TAMPA - FLT 25 - NR 3 TIRE FLAT AFTER LANDING. ALSO, APPARENT DAMAGE TO WHEEL AND BRAKE. REMOVED AND REPLACE D TIRE, BRAKE, AND AXLE SLEEVE. (X) 2 L 7 3 4F A3WE 1996050900560 19960509 00560 NM 1996 5 9 IXKA960011 1 19960413 A 3350 S106 BATTERY PACK BOEING 727 727251 138408H NM CABIN DISCHARGED A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 259US 19978 EWR - POST-FLIGHT - OVERHEAD EMERGENCY EXIT LIGHT ROW 11, INOPERATIVE. REMOVED AND REPLACED BATTERIES. 2 L 7 3 4F A3WE 1996050900561 19960509 00561 NM 1996 5 9 IXKA960012 1 19960413 A 3350 SIGN BOEING 727 727225 1384077 NM CABIN FELL OFF A IXKA K NONE O OTHER IN INSP/MAINT 1 EA 25 361KP 20627 EWR - FLT 58 - EMERGENCY EXIT SIGN MISSING AT ROW 7. FOUND EXIT SIGN ON FLOOR. REINSTALLED AND SECURED SAME. (X) 2 L 7 3 4F A3WE 1996050900562 19960509 00562 NM 1996 5 9 IXKA960013 1 19960414 A 3350 07912 LENSE BOEING 727 727224 1384076 NM CABIN MISSING A IXKA K NONE O OTHER IN INSP/MAINT 1 EA 25 32719 20388 EWR - POST-FLIGHT - EMERGENCY LIGHT AT ROW 2 NEEDS LENSE AND TO BE SECURED. REPLACED LENSE AND SECURED EMERGENCY LIGHT. (X) 2 L 7 3 4F A3WE 1996050900563 19960509 00563 NM 1996 5 9 IXKA960014 1 19960415 A 3350 307BP8L LAMP BOEING 727 727225 1384077 NM CABIN FAILED A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8880Z 21453 EWR - POST-FLIGHT CHECK - 'E' PATH LIGHT, ROW 17 INOPERATIVE. RELAMPED SAME. (X) 2 L 7 3 4F A3WE 1996050900564 19960509 00564 NM 1996 5 9 IXKA960015 1 19960417 A 2611 8240PY SMOKE DETECTOR BOEING 727 727225 1384077 NM FWD LAVATORY INOPERATIVE A IXKA K NONE O OTHER IN INSP/MAINT 1 EA 25 8883Z 21580 ATL - FLT 22 - POST-FLIGHT CHECK, FORWARD LAVATORY SMOKE DETECTOR INOPERATIVE. REMOVED AND REPLACED SMOKE DETECTOR. (X ) 2 L 7 3 4F A3WE 1996050900565 19960509 00565 NM 1996 5 9 IXKA960016 1 19960417 A 3350 1102837 POWER PACK GRIMES BOEING 727 727251 138408H NM CABIN INOPERATIVE A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 259US 19978 EWR - FLT 81 - POST-FLIGHT, AFT OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED AND RPELACED POWER PACK. (X) 2 L 7 3 4F A3WE 1996050900566 19960509 00566 NM 1996 5 9 IXKA960017 1 19960421 A 3350 90052 POWER PACK BOEING 727 727225 1384077 NM CABIN INOPERATIVE A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8882Z UA5176 21579 EWR - POST-FLIGHT INSPECTION - EMERGENCY EXIT SIGN AT ROW 17 CEILING INOPERATIVE. REMOVED AND REPLACED POWER PACK. (X) 2 L 7 3 4F A3WE 1996050900567 19960509 00567 NM 1996 5 9 IXKA960018 1 19960418 A 3350 LIGHT CAPSULE BOEING 727 727225 1384077 NM CABIN MISSING A IXKA K NONE O OTHER IN INSP/MAINT 1 EA 25 352PA 20616 EWR - POST-FLIGHT - FORWARD EMERGENCY 'E' PATH LIGHT ASSEMBLY NR 3 LIGHT CAPSULE MISSING. CAPSULE FOUND AND REINSTALLED . (X) 2 L 7 3 4F A3WE 1996050900568 19960509 00568 NM 1996 5 9 IXKA960019 1 19960423 A 3350 LENSE BOEING 727 727225 1384077 NM CABIN BROKEN A IXKA K NONE O OTHER IN INSP/MAINT 1 EA 25 354PA 20624 ATL - LOG ITEM - 6TH EMERGENCY RED LENSE WOULD NOT STAY DOWN. REPLACED MODULE. (X) 2 L 7 3 4F A3WE 1996050900569 19960509 00569 NM 1996 5 9 USAA360399 1 19960419 A 5315 6545808 FLOOR BEAM BOEING 737 7374B7 1384702 NM BS 312 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 19391 24549 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .25 INCH BY .25 INCH CORROSION AROUND FASTENER HOLES, FLOOR BEAM STA 3 12, RBL 21 TO LBL 48. INSTALLED SPLICE ANGLES AND NEW T-CAP SECTION, REPAIRED PER SRM 53-10-51. CORROSION TASK NR: C5 3-107-02. CORROSION LEVEL: 2. (X) 2 L 7 2 4F RT A16WE 1996050900570 19960509 00570 NM 1996 5 9 USAA360400 1 19960419 A 5315 FLOOR BEAM BOEING 737 7374B7 1384702 NM BS 294.5 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 19391 24549 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .50 INCH BY 1 INCH CORRODED AREA AROUND CLIP NUT HOLES BL ZERO - RBL 4 5, BS 294.5 FLOOR BEAM UPPER T-CAP, BL ZERO TO RBL 45. REMOVED CORRODED SECTION FROM LBL 21 TO RT END. FABRICATED AND INSTALLED NEW T-CAP SECTION AND SPLICE ANGLES. REPAIRED PER SRM 53-10-51, FIGURE 205. CORROSION TASK NR: C53-107-02. CORROSION LEVEL: 2. (X) 2 L 7 2 4F RT A16WE 1996050900571 19960509 00571 NM 1996 5 9 USAA360401 1 19960419 A 5315 FLOOR BEAM BOEING 737 7374B7 1384702 NM BS 328 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 19391 19391 24549 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .50 INCH BY 1 INCH CORRODED AREAS AROUND CLIP NUT HOLES RBL 14 TO RBL 55, BS 328, FLOOR BEAM UPPER T-CAP. REMOVED CORRODED SECTION FROM LBL 36 TO RT END. FABRICATED AND INSTALLED NEW T-CAP SECTION AND SPLICE ANGLES, REPAIRED PER SRM 53-10-51, FIGURE 205. CORROSION LEVEL: 2. CORROSION TASK NR: C53-107-02 . (X) 2 L 7 2 4F RT A16WE 1996050900572 19960509 00572 NM 1996 5 9 USAA360402 1 19960419 A 5330 SKIN BOEING 737 7374B7 1384702 NM BS 887 WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 19391 24549 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .50 INCH BY 4 INCH BY 0.016 INCH MAXIMUM WORN AREAS, 2 EACH, BS 887; T OP OF FUSELAGE SKIN UNDER DORSAL FIN. BLENDED WORN AREAS, CHECKED FOR CRACKS AND SKIN THICKNESS, FABRICATED AND INSTALL ED REPAIR DOUBLER PER T/R 53-30-03 AND SRM 53-00-01, FIGURE 202. (X) 2 L 7 2 4F RT A16WE 1996050900573 19960509 00573 NM 1996 5 9 USAA960394 1 19960412 A 5312 BULKHEAD BOEING 737 737201 1384454 NM BS 1156 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 260AU 34273 22866 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK 1156 BULKHEAD. STOP DRILLED BOTH ENDS OF CRACK, MANUFA CTURED, HEAT TREATED, AND INSTALLED REPAIR. REPAIRED PER EO 5391G3569. (X) 2 L 7 2 4F A16WE 1996050900574 19960509 00574 NM 1996 5 9 USAA960395 1 19960419 A 5754 SKIN BOEING 737 7374B7 1384702 NM NR 1 SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 19391 24549 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .1250 INCH CRACK NR 1 SLAT LOWER SKIN AFT FASTENER ROW ABOVE INBOARD A UXILIARY TRACK. CUT OUT CRACKED SKIN SECTION AND INSTALLED DOUBLER PER EA 41028. (X) 2 L 7 2 4F RT A16WE 1996050900575 19960509 00575 NM 1996 5 9 USAA960396 1 19960419 A 5754 SKIN BOEING 737 7374B7 1384702 NM NR 1 SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 19391 24549 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .1250 INCH CRACK NR 1 SLAT LOWER SKIN AFT FASTENER ROW, 3 INCHES FROM INBOARD END. CUT OUT DAMAGED SKIN AND INSTALLED DOUBLER PER DRAWING 65C30133. (X) 2 L 7 2 4F RT A16WE 1996050900576 19960509 00576 NM 1996 5 9 USAA960397 1 19960419 A 5315 FLOOR BEAM BOEING 737 7374B7 1384702 NM BS 986.5 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 9391 24549 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 3 INCH BY 60 INCH COMBINED AREA OF SURFACE CORROSION UPP ER T-CAP OF FLOOR BEAM AT STA 986.5 (CABIN). INSTALLED T-CAP AND REPAIRED ANGLE, REPAIRED PER EA 986.5, SRM 53-00-51. C ORROSION TASK NR: C53-107-02. CORROSION LEVEL 2. (X) 2 L 7 2 4F RT A16WE 1996050900577 19960509 00577 NM 1996 5 9 USAA960398 1 19960419 A 5315 FLOOR BEAM BOEING 737 7374B7 1384702 NM BS 344 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 19391 24549 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER AREA OF CORROSION, STA 344 FLOOR BEAM UPPER T-CHORD, R BL 9 TO LBL 18, WL 208, AT CLIP NUT HOLES. REPAIRED BEAM CHORD CUT OUT FROM LBL 33 TO RBL 19 AND SPLICED IN NEW CHORD S ECTION PER SRM 53-10-51. CORROSION TASK NR: C53-107-02. CORROSION LEVEL 2. (X) 2 L 7 2 4F RT A16WE 1996050900578 19960509 00578 NM 1996 5 9 USAABB96013 1 19960416 A 2120 2022433 ACTUATOR BOEING 757 757225 1384959 NM RT RAM AIR DOOR FAILED A USAA A B UNSCHED LANDING EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 19 609AU 35946 22205 CLT - FLT 1104 - EN ROUTE PIT/MIA, CREW RECEIVED EICAS MESSAGE: LT BLD DUCT LEAK. CREW ISOLATED THE LEAK. CREW THEN E XPERIENCED A RIGHT PACK OVERHEAT AND RECEIVED THE EICAS MESSAGE: RT PACK OFF. CREW PERFORMED AN EMERGENCY DESCENT AND DIVERTED THE FLIGHT TO CLT. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE COULD NOT DUPLICATE THE LT DUCT LEAK P ROBLEM. HOWEVER, THE RAM AIR DOOR INLET ACTUATOR WAS FOUND STUCK IN THE CLOSED POSITION. THE ACTUATOR WAS REPLACED. ( X) 2 L 7 2 4F RT A2NM 1996050900579 19960509 00579 WP 1996 5 9 USAAD96038 1 19960414 A 2424 976J2544 GEN CONTROL UNIT DOUG DC9 DC931 3022065 WP LEFT FAILED A USAA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 EA 19 935VJ 22085 48115 ON CLIMB-OUT LEFT GENERATOR FAILED WITH A GOOD CROSSTIE. RESET THE LT GENERATOR. GOOD VOLTS AND FREQUENCY. LT GENERAT OR FAILED AGAIN WITH A CROSSTIE LOCKOUT. APU STARTED TO BACKUP LT SIDE. APU FAILED. RT GENERATOR ONLY OPERATION. DIV ERTED TO PHL. REPLACED LT GENERATOR GCU. RAN ENGINE AND APPLIED LOAD TO LT GENERATOR. STARTED APU, OPS CHECKS GOOD. ( X) 2 L 7 2 4F A6WE 1996050900580 19960509 00580 WP 1996 5 9 USAAD96039 1 19960413 A 3350 6011777LB POWER SUPPLY DOUG DC9 DC931 3022065 WP RT NACELLE INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 977VJ 48155 RIGHT NACELLE LIGHT INOPERATIVE IN EMERGENCY LIGHTING MODE ONLY. REPLACED EMERGENCY LIGHT POWER PACK. (X) 2 L 7 2 4F A6WE 1996050900581 19960509 00581 WP 1996 5 9 USAAD96041 1 19960424 A 5610 WINDSHIELD DOUG DC9 DC931 3022065 WP COCKPIT CRACKED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 921VJ 31928 48141 BOS-YYZ - FL 930 - EN ROUTE THE CENTER WINDSHIELD CRACKED. FLIGHT RETURNED TO BOS AND LANDED WITHOUT NO FURTHER INCIDEN T. MAINTENANCE REPLACED THE WINDSHIELD AND THE WINDSHIELD HEAT CONTROLLER, (P/N 9615059002. (M) 2 L 7 2 4F A6WE 1996050900582 19960509 00582 EU 1996 5 9 USAAF96032 1 19960412 A 2750 A83235409 SYNCHRONIZER FOKKER F28 F28MK0100 4990807 EU NR 4 TE FLAP FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 855US 11283 CLT - FLT 1138 - AFTER TAKEOFF FROM CLT, CREW NOTED A FLAP DISAGREEMENT. FLIGHT RETURNED TO CLT AND LANDED WITH NO FURT HER INCIDENT. MAINTENANCE REPLACED THE NR 4 FLAP SYNCHRONIZER. (X) 2 L 7 2 4F RT 1996050900583 19960509 00583 EU 1996 5 9 USAAF96033 1 19960415 A 5245 ACCESS DOOR FOKKER F28 F28MK4000 4990810 EU LT AIR COND SYST NOT SECURED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 480AU 11229 PIT - FLT 682 - AFTER TAKEOFF AND REACHING 8,000 FEET, CREW WAS UNABLE TO PRESSURIZE AIRCRAFT. FLIGHT RETURNED TO PIT A ND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPOSITIONED/SECURED LEFT AIR CONDITIONING ACCESS DOOR. 2 L 7 2 4F RT A20EU 1996050900584 19960509 00584 EU 1996 5 9 USAAF96034 1 19960417 A 3230 10SD8001 SOLENOID FOKKER F28 F28MK0100 4990807 EU LANDING GEAR FAULTY A USAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 19 893US 11373 RIC - FLT 1294 - AFTER TAKEOFF FROM PHL, NOSE LANDING GEAR WOULD NOT RETRACT. CREW RECYCLED GEAR USING MANUAL OVERRIDE TO RETRACT GEAR. FLIGHT LANDED IN RIC WITHOUT FURTHER INCIDENT. AIRCRAFT FERRIED TO PIT FOR REPAIR. MAINTENANCE REPLA CED THE LANDING GEAR ANTI-RETRACTION SOLENOID AND ADJUSTED THE LANDING GEAR SELECTOR VALVE. OPS CHECK GOOD. (X) 2 L 7 2 4F RT 1996050900585 19960509 00585 NM 1996 5 9 USAASB96066 1 19960413 A 2910 MS21916D108 REDUCER FITTING VICKERS 696601 BOEING 737 737301 1384611 NM A HYD SYSTEM LEAKING A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 573US 398 23560 DEN - FLT 8641 - EN ROUTE SYR TO LAS, CREW NOTED LOSS IN SYSTEM 'A' HYDRAULIC QUANTITY. CAPTAIN ELECTED TO DIVERT TO DE N. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE REDUCER FITTING ON THE HYDRAULIC TRANSFER VALVE LEAKI NG AND REPLACED IT. (X) 2 L 7 2 4F RT A16WE 1996050900586 19960509 00586 NM 1996 5 9 USAASB96067 1 19960414 A 3230 RETRACT MECH BOEING 737 7374B7 1384702 NM RT MLG MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 783AU 25022 SJU - FLT 1041 - AFTER TAKEOFF FROM STT, CREW RECEIVED RIGHT MLG UNSAFE LIGHT. TOWER CONFIRMED RIGHT GEAR STLL IN DOWN POSTION. FLIGHT DIVERTED TO SJU AND LANDED WITH NO FURTHER INCIDENT. AIRCRAFT FERRIED TO TPA. MAINTENANCE CYCLED THE GEAR TWICE AND COULD NOT FIND A DEFECT. THE 'A' SYSTEM HYDRAULIC FILTERS WERE CHANGED, AND THE RIGHT MLG HYDRAULIC VALV E AND THE RIGHT DOWNLOCK ACTUATOR WERE REPLACED AS A PRECAUTION. (X) 2 L 7 2 4F RT A16WE 1996050900587 19960509 00587 NM 1996 5 9 USAASB96068 1 19960417 A 2133 7110033 OUTFLOW VALVE BOEING 737 737301 1384611 NM AFT CABIN FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 585US 6548 23930 CLT - FLT 1139 - RIGHT A/C PACK WAS ON MEL. AFTER TAKEOFF, AIRCRAFT WOULD NOT PRESSURIZE. FLIGHT RETURNED TO CLT AND L ANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE AFT OUTFLOW VALVE. (X) 2 L 7 2 4F RT A16WE 1996050900588 19960509 00588 NM 1996 5 9 USAASB96069 1 19960418 A 2410 731753 CSD BOEING 737 7372B7 1384560 NM RT ENGINE FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 279AU 66450 14917 22891 CLT - FLT 1527 - AFTER TAKEOFF, CREW RECEIVED RIGHT GENERATOR HIGH OIL TEMPERATURE LIGHT. APU GENERATOR WAS ON MEL. FL IGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT CSD. (X) 2 L 7 2 4F A16WE 1996050900589 19960509 00589 EU 1996 5 9 VTZA96153 1 19960416 A 2910 QA03044 FILTER CARTRIDGE BAG JETSTM JETSTM3201 1500217 EU LT/RT FAILED A VTZA O OTHER J WARNING INDICATION AP APPROACH 1 EA 27 480UE 894 CRW/IAD - FLT 6397 - DURING APPROACH TO LANDING AT 1615 HRS ON 4-16-96, DECLARED AN EMERGENCY DUE TO THE NOSE GEAR NOT I NDICATING DOWN AND LOCKED WHEN GEAR WAS EXTENDED. FLIGHT CREW PERFORMED AN EMERGENCY EXTENSION AND GEAR INDICATED SAFE. AIRCRAFT LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE PERFORMED AN INSPECTION AND REPLACED BOTH MAIN HYDRAULIC FILTE R CARTRIDGES AND MAIN HYDRAULIC PUMPS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. REFERENCE OPERATOR CO NTROL NR 96ZZZX2305. (X) 2 L 7 2 4T RT A56EU 1996050900590 19960509 00590 EU 1996 5 9 VTZA96154 1 19960409 A 3320 31851A CONNECTOR BAG JETSTM JETSTM3201 1500217 EU CABIN FAILED A VTZA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 27 481UE 895 BGM/IAD - FLT 6152 - DURING CRUISE AT 1,415 HRS ON 4-9-96, RETURNED TO IAD DUE TO THE OVERHEAD CABIN LIGHT AT SEAT 2BC S TARTED SMOKING. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 09070 IAW MEL 33-2. MAINT ENANCE LATER CLEARED DMI NR 09070 ON 4-9-96, BY REPLACING THE OVERHEAD LAMP CONNECTOR. AIRCRAFT WAS RELEASED AND APPROV ED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1996050900591 19960509 00591 1996 5 9 VTZA96155 4 19960418 A 3418 C771076 LIFT TRANSDUCER BAG JETSTM JETSTM3201 1500217 EU LT WING LE FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 497UE 904 CMH/IAD - FLT 36286 - DURING CLIMB-OUT AT 0845 HRS ON 4-18-96, RETURNED TO CMH DUE TO THE LEFT STALL WARNING SYSTEM IDEN T, STICK SHAKER, AND HORN SOUNDED IN-FLIGHT ON CLIMB-OUT. AIRCRAFT WAS THEN FERRIED TO IAD AND LANDED AT IAD WITH NO FU RTHER INCIDENTS. MAINTENANCE REPLACED THE LEFT STALL VANE. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. ( X) 2 L 7 2 4T RT A56EU 1996051000001 19960510 00001 NM 1996 5 10 MWEA96129 1 19960429 A 2150 20495054 ACM DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A MWEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 31 601ME 49762 PILOT REPORTS, SMOKE IN CABIN WHEN RT PACK IS TURNED ON WITH APU RUNNING. REPLACED RT AIR CYCLE MACHINE, OPS CHECK GOOD . 2 L 7 2 4F RT A6WE 1996051000002 19960510 00002 WP 1996 5 10 MWEA96130 1 19960501 A 2840 1TL118 TEST SWITCH DOUG DC9 DC932 3022066 WP COCKPIT MALFUNCTIONED A MWEA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 31 207ME 47794 PILOT REPORTS RT, LT, AND CENTER FUEL QUANTITY INDICATORS STOPPED FUNCTIONING AND WOULD NOT TEST. AIRCRAFT DIVERTED TO MCI. FOUND DEFECTIVE TEST SWITCH. REPLACED SWITCH. OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996051500001 19960515 00001 NE 1996 5 15 DL733961075 2 19960504 A 7261 O-RING BOEING 737 737347 1384647 NM GE CFM56 CFM563B1 13802 NE NR 2 ENGINE LEAKING A DALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 312WA 23651 23651 23598 721286 NR 2 ENGINE SHUT-DOWN IN CRUISE AFTER OIL PRESSURE DROP AND OIL QUANTITY LOSS. FOUND OIL LEAKING FROM N2 GEAR BOX MANUA L CRANK PAD. REPLACED O-RING AND INSTALLED CRANK PAD COVER. 2 L 7 2 4F 4 F RT A16WE E2GL 1996051600001 19960516 00001 WP 1996 5 16 9609729927 1 19960507 A 2130 PRESSURIZATION DOUG DC9 DC931 3022065 WP CABIN MALFUNCTIONED A NWAA B G EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 GL 01 8920E 45835 LOSS OF CABIN PRESSURIZATION OCCURRED AT 35,000 FEET, CABIN PRESSURE WARNING LIGHT ILLUMINATED AND OXYGEN MASKS WERE DEP LOYED THROUGHOUT THE CABIN. EMERGENCY DESCENT WAS MADE TO 24,000 FEET AND PRESSURE WAS REGAINED, DESCENDED TO 18,000 FE ET AND CONTINUED TO DESTINATION WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED ALL PNEUMATIC DUCTING, PACK PRESSURE RE GULATOR VALVES, AUGMENTATION VALVES AND FLOW CONTROL VALVES, ALL CHECKED NORMAL. PRESSURIZED AIRCRAFT TO 4 PSI AND NO V ESSEL LEAKS WERE FOUND. REPLACED THE WATER SEPARATOR BAGS. 2 L 7 2 4F A6WE 1996051600002 19960516 00002 WP 1996 5 16 9610189968 1 19960504 A 5350 CLIPS DOUG DC9 DC931 3022065 WP TAIL CONE OUT OF ADJUST A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9332 47264 DURING H-CHECK, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO PULL THE INTERIOR TAIL CONE HANDLE FROM THE CLIPS AND EXCESS IVE FORCE WAS REQUIRED TO DROP THE TAIL CONE, SAME HANDLE. ADJUSTED THE CLIPS AND THE RELEASE SYSTEM PER MM 53-50-3, CH ECKED OK. 2 L 7 2 4F A6WE 1996051600003 19960516 00003 WP 1996 5 16 9610199937 1 19960507 A 2424 93902171 REGULATOR DOUG DC9 DC931 3022065 WP LEFT MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 908H 47517 LEFT GENERATOR DROPPED OFF LINE DURING TAKEOFF ROLL AT APPROXIMATELY 30 KNOTS. ABORTED TAKEOFF AND RETURNED TO THE GATE . MAINTENANCE FOUND REGULATOR FAULT AT GENERATOR CONTROL UNIT. REPLACED THE LEFT VOLTAGE REGULATOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996051600004 19960516 00004 WP 1996 5 16 9610209311 1 19960509 A 3350 LIGHTS DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 314RC 49110 DURING LINE CHECK, FOUND EMERGENCY CEILING LIGHTS FROM ROW 1 TO ROW 15 INOPERATIVE. REPLACED BATTERIES AT CHARGER B5-32 , OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996051600005 19960516 00005 WP 1996 5 16 9610219140 1 19960506 A 3350 BATTERY PACK DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 930RC 45729 DURING LINE CHECK, FOUND LEFT AND RIGHT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS, OPERATIONAL CHEC K GOOD. 2 L 7 2 4F A6WE 1996051600006 19960516 00006 WP 1996 5 16 9610229180 1 19960509 A 3350 BATTERY PACK DOUG DC9 DC914 3022034 WP RT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 3312L 45707 DURING LINE CHECK, FOUND RIGHT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERAITONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996051600007 19960516 00007 WP 1996 5 16 9610319604 1 19960507 A 3350 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 604NW 47222 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERI ES. 2 L 7 2 4F A6WE 1996051600008 19960516 00008 WP 1996 5 16 9610329978 1 19960508 A 3350 60030451 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9342 47391 DURING LINE MAINTENANCE INSPECTION, FOUND COCKPIT AND FORWARD CABIN EMERGENCY LIGHTS DIM. REPLACED FORWARD BATTERY PACK IN CEILING. 2 L 7 2 4F A6WE 1996051600009 19960516 00009 NM 1996 5 16 9610335514 1 19960508 A 2930 HYD BYPASS IND BOEING 727 727251 138408H NM LT HYD SYST MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 01 514US 23202 DURING CRUISE FLIGHT, AIRCRAFT INDICATED LOSS OF LEFT SYSTEM HYDRAULICS. AIRCRAFT DIVERTED TO DTW AND LANDED WITHOUT IN CIDENT. REPLACED THE LEFT HYDRAULIC FILTER BYPASS INDICATOR. PERFORMED PRESSURE AND LEAK CHECK, CHECKS WERE OK. 2 L 7 3 4F A3WE 1996051600010 19960516 00010 1996 5 16 96UAL900314 4 19960506 A 2565 MAIN TUBE AIR CRUISERS D31038201 BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SLIDE SEPARATION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 0391 24763 SLIDE REMOVED FOR SECOND TIME CONTROLLED OVERHAUL. A 3 INCH SEAM SEPARATION LOCATED ON THE RIGHT HAND MAIN TUBE APPROXI MATELY 1 FOOT FROM CROSS OVER TUBE. RETURNED UNIT TO ORIGINAL EQUIPMENT MANUFACTURER FOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 1996051600011 19960516 00011 NM 1996 5 16 96UAL900315 1 19960506 A 2421 GENERATOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LT ENGINE MALFUNCTIONED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 777UA 26916 LEFT ENGINE DRIVEN GENERATOR WILL NOT COME ON LINE. 2 L 7 2 4F 4 F RT T0001SE E46NE 1996051600012 19960516 00012 NM 1996 5 16 96UAL900316 1 19960506 A 2761 S251W150 PWR CONT UNIT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 4 SPOILER FAILED A UALA O OTHER J WARNING INDICATION LD LANDING 1 WP 29 767UA 26918 SPOILERS EICAS MESSAGE DURING LANDING ROLL. *S/D* REPLACED NUMBER FOUR SPOILER POWER CONTROL UNIT. 2 L 7 2 4F 4 F RT T0001SE E46NE 1996051600013 19960516 00013 NM 1996 5 16 96UAL900317 1 19960506 A 3350 SOCKET BOEING 737 737322 1384676 NM GE CFM56 CFM563B1 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 304UA 23665 EMERGENCY SLIDE LIGHT AT DOOR ONE LEFT INOP. REPLACED LIGHT SOCKET, CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1996051600014 19960516 00014 NM 1996 5 16 96UAL900318 1 19960506 A 5320 HI-LOK COLLARS BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE WHEEL WELL AREA CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 NUMEROUS UNIVERSAL .25 ORANGE COLORED HI-LOK COLLARS WERE FOUND CRACKED FROM THE BASE TO THE TOP, IN THE WHEEL WELL AREA . COLLARS ARE COMMON TO FRAME SPLICES AND VERTICAL STIFFENERS ALONG THE KEEL BEAM. *S/D* CRACKED COLLARS DUE TO IMPRO PER HEAT TREATMENT, -T6 INSTEAD OF -T73. REFERENCED BOEING MESSAGE M-7272-94-4800 AND REPLACED CRACKED HI-LOK COLLARS. 2 L 7 2 4F 4 F RT A2NM E17NE 1996051600015 19960516 00015 NM 1996 5 16 96UAL900319 1 19960506 A 3350 STRIP BOEING 737 737322 1384676 NM GE CFM56 CFM563B1 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 304UA 23665 EMERGENCY ESCAPE PATH LIGHTING INOP ROWS 4 AND 5. REPLACED LIGHT STRIP, CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1996051600016 19960516 00016 NM 1996 5 16 96UAL900320 1 19960506 A 3350 LAMP BOEING 737 737322 1384676 NM GE CFM56 CFM563B1 13802 NE COCKPIT INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 304UA 23665 COCKPIT EMERGENCY LIGHT INOP. REPLACED LAMP, CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1996051600017 19960516 00017 NM 1996 5 16 96UAL900321 1 19960506 A 3350 LAMP BOEING 737 737322 1384676 NM GE CFM56 CFM563B1 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 359UA 24452 EMERGENCY LIGHT INOP AT SEAT 3D. REPLACED LAMP, CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1996051600018 19960516 00018 NM 1996 5 16 96UAL900322 1 19960506 A 3350 BATTERY PACK BOEING 737 737322 1384676 NM GE CFM56 CFM563B1 13802 NE CABIN DISCHARGED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 392UA 24667 EMERGENCY ESCAPE PATH LIGHTING INOP BETWEEN THE OVERWING EXIT AND ROW 24. REPLACED BATTERY PACK, CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1996051600020 19960516 00020 1996 5 16 96UAL900324 4 19960507 A 2565 D31865101 SLIDE AIR CRUISERS AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LT OFF WING LEAKING A A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 416UA A5823 479 LEFT HAND OFF WING ESCAPE SLIDE REMOVED FOR FIRST OVERHAUL WAS FOUND TO HAVE NUMEROUS AREAS OF POROSITY AND A SEAM LEAK ON THE CROSS TUBE WHICH CAUSED THE UNIT TO FAIL AN AIR RETENTION TEST. PATCHED AND REPAIRED DAMAGED AREAS PER VENDORS M ANUAL. 2 L 7 2 4F 4 F RT A28NM E40NE 1996051600021 19960516 00021 NM 1996 5 16 96UAL900325 1 19960507 A 2740 INPUT ROD BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE STAB TRIM OUT OF ADJUST A UALA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 WP 29 7455U 21909 EN ROUTE, STABILIZER STUCK IN NOSEDOWN POSITION. LANDED DEN UNDER AMBER ALERT. *S/D* STABILIZER BRAKE UNDER COCKPIT F LOOR WAS NOT COMPLETELY DISENGAGING. ADJUSTED STABILIZER TRIM INPUT ROD PER THE MAINTENANCE MANUAL. 2 L 7 3 4F 4 F A3WE E2EA 1996051600022 19960516 00022 NM 1996 5 16 96UAL900326 1 19960507 A 5330 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE BS 1040 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7447U 21901 AFT LOWER FUSELAGE LT OB OF VHF ANTENNA SKIN IS CRACKED AND EXFOLIATED. CRACK APPEARS TO BE ABOUT ONE AND ONE HALF INCH ES LONG WITH EVIDENCE OF CORROSION. *S/D* CORROSION CONFIRMED, AFFECTED FUSELAGE SKIN REPAIRED PER SRM 53-30-3. 2 L 7 3 4F 4 F A3WE E2EA 1996051600023 19960516 00023 NM 1996 5 16 96UAL900327 1 19960508 A 3610 MVT69331681 CLAMP BOEING 747 747222B 1384904 NM PWA JT9 JT9D7R4G2 52054 NE NR 3 ENGINE FAILED A UALA F ACTIVATE FIRE EXT. J WARNING INDICATION CL CLIMB 1 WP 29 152UA 23737 715251 DURING INITIAL CLIMBOUT, RECEIVED A FIRE WARNING FOR NR 3 ENGINE. EXECUTED EMERGENCY PROCEDURES, DISCHARGED FIRE BOTTLE AND RETURNED TO SFO. *S/D* FIRE WARNING PROBABLE CAUSE WAS DUE TO FAILURE OF MANIFOLD CLAMP BETWEEN THE PNEUMATIC MAN IFOLD AND HIGH STAGE VALVE. CLOSE VISUAL INSPECTION INITIATED FOR I800 HOUR INTERVALS. 2 L 7 4 4F 4 F RT A20WE E3NE 1996051600024 19960516 00024 NE 1996 5 16 96UAL900328 2 19960508 A 7230 BLADES BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT ENGINE FAILED A UALA A UNSCHED LANDING E M R VIBRATION/BUFFET OVER TEMP PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 524UA 24977 726610 DURING GEAR RETRACTION DETECTED A LOUD REPORT ACCOMPANIED BY AIRCRAFT SHAKING. SHORTLY AFTER, HEARD TWO ADDITIONAL BAN GS ALONG WITH JERKING. EGT BEGAN TO RISE, RETURNED RIGHT ENGINE TO IDLE. RE-APPLICATION OF POWER TO RIGHT ENGINE RESUL TED IN CONTINUED COMPRESSOR STALL. ENGINE RETURNED TO IDLE, AIRCRAFT RETURNED TO FIELD. 9TH STAGE BLADE FAILURE. REPL ACED ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 1996051600025 19960516 00025 NM 1996 5 16 96UAL900329 1 19960508 A 3350 BATTERY PACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 551UA 25399 EMERGENCY EXIT LIGHTS AT DOOR 3L AND FLOOR LIGHTS AT ROWS 16 THROUGH 23, 32 THROUGH 38, CYCLE ON AND OFF INTERMITTENTLY. REPLACED M10818 BATTERY CHARGER AND BATTERY PACK, OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996051600026 19960516 00026 NM 1996 5 16 96UAL900330 1 19960508 A 5330 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE BS 1060 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7446U 21900 AFT LOWER FUSELAGE OB RT 6 INCHES AFT OF VHF ANTENNA HAS THREE CRACKS IN AN AREA 4 INCHES LONG. *S/D* CRACKS CONFIRMED TO BE BETWEEN .25 TO .38 INCHES LONG EACH. CAUSE CONFIRMED AS CORROSION INTERNALLY IN FUSELAGE SKIN AT FAYING SURFACE OF S-28R AND AT ADJACENT INTERCOSTAL. PORTIONS OF S-28R BETWEEN BS 1050 AND 1070 ALSO CORRODED. STRINGER REPAIRED PER SRM 53-10-3, SKIN REPAIRED PER SRM 53-30-3. 2 L 7 3 4F 4 F A3WE E2EA 1996051600027 19960516 00027 NM 1996 5 16 96UAL900332 1 19960508 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 576UA 26690 LEFTSIDE, FORWARD OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED INOP OVERWING EMERGENCY EXIT LIGHT, OPERATION CHECKS NOR MAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996051600028 19960516 00028 NM 1996 5 16 96UAL900333 1 19960508 A 3350 LIGHT BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 934UA 26662 EMERGENCY LIGHT FOR SLIDE AT DOOR ONE LEFT INOP. REPLACED LAMP, CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E21EU 1996051600029 19960516 00029 NM 1996 5 16 96UAL900334 1 19960508 A 3350 LIGHT STRIP BOEING 737 737322 1384676 NM GE CFM56 CFM563B1 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 391UA 24666 EMERGENCY ESCAPE PATH LIGHTING INOP BY AFT GALLEY. REPLACED EMERGENCY ESCAPE PATH LIGHT STRIP, CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1996051600030 19960516 00030 SO 1996 5 16 COMA9610141 1 19960505 A 3230 18190003 SOLENOID VALVE EMB 120 EMB120RT SO LT MLG DEFECTIVE A COMA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 246CA 120223 WHEN LANDING GEAR SELECTED UP, THE LT MLG REMAINED DOWN. REPLACED THE LANDING GEAR SOLENOID VALVE. 2 L 7 2 4T RT A31SO 1996051600031 19960516 00031 EU 1996 5 16 COMA9630106 1 19960507 A 3020 NH2466881 INLET SAAB SF340 SF340A 7850100 EU LT ENGINE BURNED A COMA A UNSCHED LANDING A FLAME/FIRE CR CRUISE 1 SO 01 342CA 4226 432 340A023 FLAMES OBSERVED COMING FROM LEFT ENGINE INLET. REPLACED THE LEFT ENGINE FWD LOWER INLET ASSY. 2 L 7 2 4T RT A52EU 1996051600032 19960516 00032 EA 1996 5 16 COMA9660082 1 19960508 A 3230 555405 SELECTOR VALVE CNDAIR CL600 CL6002B19 EA NLG MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 916CA 6981 6155 7014 WHEN LANDING GEAR SELECTED DOWN THE NLG REMAINED UP AND GEAR DISAGREE MESSAGE ON EICAS. COULD NOT DUPLICATE DISCREPANCY . REPLACED THE NLG SELECTOR VALVE FOR TROUBLESHOOTING. 2 L 7 2 4F RT A21EA 1996051600033 19960516 00033 EA 1996 5 16 COMA9660083 1 19960508 A 3260 PROX SWITCH CNDAIR CL600 CL6002B19 EA LT MLG OUT OF ADJUST A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 951CA 7091 LT MLG INDICATED INTRANSIT AFTER COMPLETION OF LANDING GEAR RETRACTION. ADJUSTED THE RT MLG UPLOCK PROXIMITY SWITCH. 2 L 7 2 4F RT A21EA 1996051600034 19960516 00034 NM 1996 5 16 P5CA9600222 1 19960502 A 5230 65B381742 ACTUATOR FITTING BOEING 747 747122 1384872 NM AFT CARGO DOOR SHEARED BOLTS A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 LOWER AFT CARGO DOOR AFT LIFT ACTUATOR MOUNTING BOLTS SHEARED. REMOVED AND REPLACED AFT ROTARY ACTUATOR IAW MM 52-34-03 . FOUND AFT ROTARY ACTUATOR CASTING CRACKED AFT SIDE, 5.5 INCH LONG BY .5 INCH WIDE. REMOVED AND REPLACED CRACKED CAST ING IAW SRM 51-10-01. REMOVED AND REPLACED CRACKED WIRING HARNESS SUPPORT BRACKET, AFT CARGO DOOR, STA 1800 RIGHT SIDE IAW SRM 51-10-01. REMOVED AND REPLACED DAMAGED FRAME AT BS 1900 IAW SRM 51-10-01. REPAIRED AFT ROTARY ACTUATOR SUPPORT FITTING IAW SRM 51-10-01. REMOVED AND REPLACED FWD ROTARY ACTUATOR AS PRECAUTIONARY IAW MM 52-34-03. 2 L 7 4 4F A20WE 1996051600035 19960516 00035 CE 1996 5 16 96ZZZX2334 1 19960306 A 2520 DRAIN TUBE LEAR 60 60LEAR 5170707 CE VANITY SINK LOOSE A OICA K NONE O OTHER IN INSP/MAINT 1 SW 09 799SC 71 067 BEACON/STROBE - CIRCUIT BREAKER TRIPPED. LOWER BEACON FOUND WATER CONTAMINATED. REMOVED CENTER AISLE FLOOR BOARDS FROM COCKPIT TO LAVATORY, DRIED OUT INSULATION AND UNDER FLOOR AREA. FOUND ICE BUCKET DRAIN TUBE LOOSE AT DRAIN MAST FITTIN G. INSTALLED A FLARED .3750 INCH STUB TUBE AND CLAMPED TYGON DRAIN TUBE TO IT WITH EXISITNG CLAMP. FOUND VANITY SINK D RAIN B-NUT LEAKING AT MAST. TIGHTENED B-NUT, ALL LEAK CHECKS OK. REINSTALLED INTERIOR AS NECESSARY. INSTALLED NEW LOW ER BEACON. 2 L 7 2 4F RT A10CE 1996051600036 19960516 00036 SO 1996 5 16 96ZZZX2335 1 19960308 A 5730 8343761 SKIN LKHEED 188 188C 5262604 SO WS 83 CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 285F 62485 188A1107 YIP - DURING SCHEDULED CHECK, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION IAW AD 66-04-02 AND LOCKHEED SB 62 0 REVEALED THE FOLLOWING WING PANEL CRACKS. REFERENCE OPERATOR CONTROL NR ZIAA96009, 96ZZZX2336, NR 96ZZZX2337, AND NR 96ZZZX2338. 2 L 7 4 4T 4A22 1996051600038 19960516 00038 SO 1996 5 16 96ZZZX2337 1 19960308 A 5730 8005481 SKIN LKHEED 188 188C 5262604 SO WS 54 CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 285F 62485 188A1107 YIP - DURING SCHEDULED CHECK, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION IAW AD 66-04-02 AND LOCKHEED SB 62 0 REVEALED THE FOLLOWING WING PANEL CRACKS. REFERENCE OPERATOR CONTROL NR ZIAA96009, 96ZZZX2335, NR 96ZZZX2336, AND NR 96ZZZX2338. 2 L 7 4 4T 4A22 1996051600039 19960516 00039 SO 1996 5 16 96ZZZX2338 1 19960308 A 5730 8398012 SKIN LKHEED 188 188C 5262604 SO WS 151 CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 285F 62485 188A1107 YIP - DURING SCHEDULED CHECK, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION IAW AD 66-04-02 AND LOCKHEED SB 62 0 REVEALED THE FOLLOWING WING PANEL CRACKS. REFERENCE OPERATOR CONTROL NR ZIAA96009, 96ZZZX2335, NR 96ZZZX2336, AND NR 96ZZZX2337. 2 L 7 4 4T 4A22 1996051600040 19960516 00040 NE 1996 5 16 96ZZZX2339 2 19960222 A 7200 ENGINE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9A 52048 NE RIGHT MALFUNCTIONED A VJ6A A UNSCHED LANDING O OTHER CL CLIMB 1 SO 11 946ML 47170 666186 DFW/DFW - FLT 234 - AIR RETURN, THE RIGHT ENGINE WAS SLOW TO SPOOL UP ON TAKEOFF, DID NOT PRODUCE FULL POWER. INSPECTED INTAKE, EXHAUST, AND AIR RETURN FOR DAMAGE. FOUND NORMAL. RAN ENGINE AND TRIMMED WITHIN PARAMETERS OF TRIM CHART MM 7 1-00. (X) 2 L 7 2 4F 4 F A6WE E2EA 1996051600062 19960516 00062 NE 1996 5 16 96ZZZX2361 1 19960208 A 2612 30326E7 AMPLIFIER SKRSKY S76 S76A 8143006 NE BAGG MALFUNCTION A ALGA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 03 741SW 19159 760070 AFTER TAKEOFF, THE NR 1 ENGINE FIRE LIGHT ILLUMINATED. ALL OTHER INDICATIONS WERE NORMAL. RETURNED TO BASE. REPLACED FIRE DETECTOR CONTROL AMP. OPS CHECK OK. (X) 1 G 7 2 3U H1NE 1996051600065 19960516 00065 GL 1996 5 16 AALA960453 2 19960324 A 7200 ENGINE DOUG MD11 MD11 3023602 NM GE CF6 CF680C GL NR 3 MALFUNCTIONED A AALA O OTHER J WARNING INDICATION DE DESCENT 1 SW 07 1761R 48551 LHR - FLT 0046 - DURING DESCENT INTO LHR WITH ALL POWER LEVERS AT IDLE, NR 3 ENGINE LOW RPM ALERT. N1 AND N2 DID NOT R ESPOND TO POWER LEVER MOVEMENT. SELECTED ENGINE IGNITION OVERRIDE AND ALL ENGINE INDICATIONS INCREASED IMMEDIATELY. NR 3 ENGINE CONTINUED TO OPERATE NORMALLY AND AIRCRAFT LANDED LHR WITHOUT INCIDENT. CHECKED NR 3 ENGINE INLET AND EXHAUST WITH NO DEFECTS FOUND. CHECKED ECU 3A AND 3B FOR FAULT REVIEW WITH NO DEFECTS FOUND. CHECKED ECU 3A AND 3B FOR CURREN T FAULTS WITH NO DEFECTS FOUND. CHECKED MAIN FUEL FILTER ELEMENT WITH NO DEFECTS FOUND. ACCOMPLISHED RTS ON ECU 3A AND 3B WITH ALL TESTS PASSED. NR 3 ENGINE RETURNED TO SERVICE. (X) 2 L 7 3 4F 4 F RT A22WE E23EA 1996051600066 19960516 00066 NM 1996 5 16 AWXA960131 1 19960312 A 3230 6552811109 ACCESSORY UNIT BOEING 737 737277 1384570 NM LANDING GEAR FAILED A AWXA A UNSCHED LANDING O OTHER TO TAKEOFF 1 WP 28 187AW 22654 PHX/ICT - FLT 0897 - AIR TURN-BACK. LANDING GEAR LEVER WOULD NOT RETRACT PAST OFF ON TAKEOFF. USED OVERRIDE TO RETRACT LOWERED GEAR NORMALLY AND RETURNED TO PHX. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT. (X) 2 L 7 2 4F RT A16WE 1996051600067 19960516 00067 EU 1996 5 16 RAIA960326 1 19960319 A 5270 SP4594 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGGAGE BAY OUT OF ADJUST A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 03 561HK 396 41077 MAIN BAGGAGE LIGHT ILLUMINATED DURING TAKEOFF. MAINTENANCE ISSUED DMI 52-3, MAINTENANCE LATER CLEARED DMI BY ADJUSTING DOOR MICROSWITCH. (X) 2 L 7 2 4T RT A41NM 1996051600068 19960516 00068 SO 1996 5 16 SRAA39603 1 19960328 A 3610 15015071 DUCT LKHEED 382 382E 526413U SO NR 2 ENGINE BLOWN A SRAA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 GL 23 910SJ 4383 DURING DESCENT FOR FLT ADH3 INTO EZE, NR 2 ENGINE NACELLE OVERHEAT LIGHT ILLUMINATED AT 6,000 FEET ALTITUDE, FEATHERED N R 2 PROPELLER AND SHUT DOWN NR 2 ENGINE, 'T' HANDLE WAS ALSO PULLED. AIRCRAFT LANDED SAFELY. FOUND 'F' STACK BLEED AIR DUCT BLOWN, REPLACED DUCT AND OPS CHECKED FOR LEAK PER MM CHAPTERS 72, 75. (X) 2 H 7 4 4T A1SO 1996051600069 19960516 00069 NM 1996 5 16 TAOA039610 1 19960312 A 3350 1102833 LIGHT GRIMES BOEING 727 727254 138408L NM CABIN SHORTED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 916TS 11990 20437 RIGHT CABIN CONTROL LIGHTING CIRCUIT BREAKER TRIPPED. RESET, BUT TRIPPED AGAIN. REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK OK. (X) 2 L 7 3 4F A3WE 1996051600070 19960516 00070 WP 1996 5 16 ZIAA96008 1 19960318 A 5730 8398012 SKIN LKHEED 188 188A 5262602 WP WS 275 CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 344HA 188A1038 YIP - DURING INSPECTION, FOUND RIGHT WING NR 1 PLANK CRACKED AT WS 275 ON LOWER SURFACE AT THE LEADING EDGE. FABRICATED , INSTALLED AND SEALED A REPAIR PER L-188 SRM 57-2-1, FIGURE 3, SHEET 37. (X) 2 L 7 4 4T RT 4A22 1996051600071 19960516 00071 SO 1996 5 16 ZIAA96009 1 19960308 A 5730 8233361 SKIN LKHEED 188 188C 5262604 SO WS 72 CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 285F 62485 188A1107 YIP - DURING SCHEDULED CHECK, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION IAW AD 66-04-02 AND LOCKHEED SB 62 0 REVEALED THE FOLLOWING WING PANEL CRACKS. REFERENCE OPERATOR CONTROL NR 96ZZZX2335, NR 96ZZZX2336, NR 96ZZZX2337, AND NR 96ZZZX2338. (X) 2 L 7 4 4T 4A22 1996051600072 19960516 00072 WP 1996 5 16 9610239998 1 19960414 A 5330 SKIN DOUG DC9 DC931 3022065 WP PAX DOOR CUTOUT CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8934E 47143 DURING M-CHECK, FOUND A CRACK IN THE FUSELAGE SKIN AT THE MAIN CABIN DOOR CUTOUT, AFT SIDE 3RD STOP FROM THE BOTTOM. RE PAIRED SKIN PER EA 99-108538. 2 L 7 2 4F A6WE 1996051600073 19960516 00073 WP 1996 5 16 9610249905 1 19960430 A 5330 SKIN DOUG DC9 DC931 3022065 WP SERV DOOR CUTOUT CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 955N 47160 DURING M-CHECK, FOUND A .75 INCH CRACK IN THE FUSELAGE SKIN AT THE FORWARD SERVICE DOOR CUTOUT LOWER AFT CORNER. REPAIR ED SKIN PER EA 99-108544. 2 L 7 2 4F A6WE 1996051600074 19960516 00074 WP 1996 5 16 9610259935 1 19960503 A 5230 FITTING DOUG DC9 DC931 3022065 WP CARGO DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 1332U 47404 DURING H-CHECK, FOUND A CRACK IN THE FORWARD CARGO DOOR NR 4 BEAM AFT END FITTING. REPLACED FITTING PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996051600075 19960516 00075 WP 1996 5 16 9610269906 1 19960507 A 5320 FITTINGS DOUG DC9 DC931 3022065 WP STRINGER 30 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 956N 47252 DURING M-CHECK, FOUND CRACKS IN THE LONGERON 30 RIGHT AND LEFT END FITTINGS AT THE FORWARD CANTED KEEL. REPLACED FITTIN GS PER SRM 51-30-1, 51-30-2. 2 L 7 2 4F A6WE 1996051600076 19960516 00076 WP 1996 5 16 9610279906 1 19960507 A 5320 FITTING DOUG DC9 DC931 3022065 WP FS 760 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 956N 47252 DURING M-CHECK, FOUND A CRACK IN THE LONGERON 29L END FITTING AT FS 760. REPLACED FITTING PER SRM 51-30-2, 51-30-5. 2 L 7 2 4F A6WE 1996051600077 19960516 00077 WP 1996 5 16 9610289906 1 19960507 A 5320 FITTING DOUG DC9 DC931 3022065 WP FUS 691 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 956N 47252 DURING M-CHECK, FOUND A CRACK IN THE FS 691 FITTING IN THE LEFT MAIN LANDING GEAR WHEEL WELL AT THE ANTI-ICE DUCT. REPA IRED FITTING PER SRM 51-30-2. 2 L 7 2 4F A6WE 1996051600078 19960516 00078 WP 1996 5 16 9610299906 1 19960507 A 5320 FITTING DOUG DC9 DC931 3022065 WP FS 690 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 956N 47252 DURING M-CHECK, FOUND CORROSION IN THE FS 690 LEFT SUPPORT FITTING AT THE INBOARD ATTACH CLIP. REPLACED FITTING PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996051600079 19960516 00079 WP 1996 5 16 9610309906 1 19960507 A 5320 FITTING DOUG DC9 DC931 3022065 WP FS 690 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 956N 47252 DURING M-CHECK, FOUND A .75 INCH CRACK IN THE FORWARD LOWER INBOARD LIGHTENING HOLE FITTING, RIGHT MAIN LANDING GEAR WHE EL WELL FS 690. REPLACED FITTING PER SRM 51-30-1. 2 L 7 2 4F A6WE 1996051600080 19960516 00080 NM 1996 5 16 9610342299 1 19960508 A 3210 65178102 LOCK ACTUATOR BOEING 727 727251 138408H NM NLG FAILED A NWAA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 01 299US 22153 ON APPROACH WITH GEAR SELECTED DOWN, SYSTEM A-HYDRAULIC QUANTITY DEPLETED TO ZERO. NOSE GEAR WOULD NOT EXTEND, NOSE GEA R WAS MANUALLY EXTENDED. AIRCRAFT LANDED WITHOUT INCIDENT. PHX MAINTENANCE REPLACED NOSE GEAR LOCK ACTUATOR. PERFORME D SYSTEM LEAK CHECK AND OPERATIONAL CHECK OF NOSE GEAR SYSTEM, CHECKED OK. 2 L 7 3 4F A3WE 1996051600081 19960516 00081 WP 1996 5 16 9610359908 1 19960508 A 3350 BATTERY DOUG DC9 DC931 3022065 WP LT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 958N 47254 DURING PERIODIC CHECK, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996051600082 19960516 00082 WP 1996 5 16 9610369903 1 19960507 A 3350 6011779 POWER SUPPLY DOUG DC9 DC931 3022065 WP LT NACELLE MALFUNCTIONED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 953N 47083 DURING PERIODIC CHECK, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996051600083 19960516 00083 NM 1996 5 16 9610386623 1 19960510 A 3350 BATTERY PACK BOEING 747 747251B 1384892 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 623US 21705 DURING LINE CHECK, FOUND CEILING EMERGENCY LIGHTS INOPERATIVE AT DOOR 3L, 2R AND 2L. FOUND BOTH EXIT SIGNS AT NR 3 GALL EY INOPERATIVE AND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE ON BOTH SIDES OF ZONE-D. REPLACED BATTERY PACKS, OPERATIO NAL CHECK GOOD. 2 L 7 4 4F A20WE 1996051600084 19960516 00084 NM 1996 5 16 9610392705 1 19960506 A 3350 BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 802EA 22433 DURING PREFLIGHT, FOUND AFT FLASHLIGHT WOULD NOT TEST. REPLACED BATTERY PACK, CHECKED OK. 2 L 7 3 4F A3WE 1996051600085 19960516 00085 WP 1996 5 16 9610409993 1 19960509 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8986E 47402 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 6 THROUGH 10 INOPERATIVE. REPLACED BAT TERIES IN PACKS, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996051600086 19960516 00086 NM 1996 5 16 96FDEA00928 1 19960509 A 5330 SKIN BOEING 727 727227 1384078 NM BS 286 DENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 DENT AT BS 286 STR 23R SKIN. FOUND DENT ON SKIN TO BE OUT OF LIMITS PER FEDEX SRM 53-30-3 AT BS 286 STR 23R. REPAIRED SKIN PER FEDEX SRM 53-30-3. 2 L 7 3 4F A3WE 1996051600087 19960516 00087 NM 1996 5 16 96FDEA00929 1 19960509 A 5311 FRAME BOEING 727 72725 1384006 NM BS 680 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 505FE 18276 CORROSION (C53-111-01, -2) IN FWD CARGO BAY ON FRAME AT BS 680 RBL 62 WL 196. REMOVED CORRODED AREA OF FRAME AT BS 680 RBL 62 WL 196 AND REPAIRED IAW FEDEX SRM 51-40-3. 2 L 7 3 4F A3WE 1996051600088 19960516 00088 NM 1996 5 16 96FDEA00930 1 19960509 A 5315 BAC1518391 FLOOR BEAM BOEING 727 72725 1384006 NM BS 680 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 505FE 18276 CORROSION (C53-224-01, -1) ON UPPER FLANGE OF FLOOR BEAM BS 680 BETWEEN LBL 9 TO 13 LBL 19 TO 2 RBL 10 WL 208. REMOVED CORRODED UPPER FLANGE OF FLOOR BEAM BS 680 LBL 31.5 TO RBL 12 WL 208. FABRICATED, CLEANED, TREATED AND INSTALLED REPAIR PARTS IAW FEDEX SRM 53-10-8. 2 L 7 3 4F A3WE 1996051600089 19960516 00089 NM 1996 5 16 96FDEA00931 1 19960509 A 5754 65162251 BONDING JUMPER BOEING 727 727173C 1384059 NM NR 4 LE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 199FE 19509 NR0264 AND 001, NR 4 K-FLAP I/B BONDING JUMPER BETWEEN K-FLAP AND BULLNOSE HAS CORROSION ON UPPER MOUNT BRACKET. *S/D* REPAIRED NR 4 K-FLAP I/B BONDING JUMPER UPPER ATTACH POINT IAW FEDEX SRM 57-50-3. 2 L 7 3 4F A3WE 1996051600090 19960516 00090 NM 1996 5 16 96FDEA00932 1 19960509 A 5754 65162276 BONDING JUMPER BOEING 727 727173C 1384059 NM NR 6 LE FLAP CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 199FE 19509 NR0265 AND 002, NR 6 K-FLAP I/B BONDING JUMPER BETWEEN BULLNOSE AND K-FLAP HAS CORROSION AT BOTH MOUNT POINTS. *S/D* R EMOVED AND REPLACED NR 6 K-FLAP ON FEDEX NR0477. 2 L 7 3 4F A3WE 1996051600091 19960516 00091 WP 1996 5 16 96FDEA00933 1 19960509 A 5400 1239855 BOLT DOUG DC10 DC1030F 3023504 WP NR 1 PYLON SHEARED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 304FE 46992 SNRM 4126. NR 1 PYLON FORWARD ENGINE MOUNT TRUSS FITTINGS HAVE NUMEROUS LOOSE BOLTS AT BOTTOM, TOP, AND SIDES. APPROXI MATELY 50 PERCENT OF THE FASTENERS ARE LOOSE. ONE BOLT IN THE BOTTOM RIGHT IS SHEARED. YN222 STA. S/D: TORQUED BOLTS PER E.O. 8-5410-7-4319. REPLACED AND TORQUED ONE SHEARED BOLT AS MENTIONED ABOVE. 2 L 7 3 4F RT A22WE 1996051600092 19960516 00092 WP 1996 5 16 96FDEA00934 1 19960509 A 5400 SCREWS DOUG DC10 DC1030F 3023504 WP NR 3 PYLON LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 304FE 46922 SNRM 4343, NR 3 PYLON HAD 5 TRI-WING SCREWS LOOSE ON LT SIDE OF PYLON AT AFT MOUNT BULKHEAD, STA YN 420. 2 L 7 3 4F RT A22WE 1996051600093 19960516 00093 WP 1996 5 16 96FDEA00935 1 19960509 A 5400 SCREWS DOUG DC10 DC1030F 3023504 WP NR 3 PYLON LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 304FE 46992 SNRM 4342, NR 3 PYLON HAD 8 TRI-WING SCREWS LOOSE ON PYLON AFT MOUNT BULKHEAD, STA YN420 RT SIDE OF PYLON. 2 L 7 3 4F RT A22WE 1996051600095 19960516 00095 NM 1996 5 16 96FDEA00937 1 19960509 A 2781 POS IND SWITCH BOEING 727 727233 138408A NM NR 4 FLAP MALFUNCTION A FDEA A J UNSCHED LANDING DUMP FUEL N FALSE WARNING CL CLIMB 1 SO 25 218FE 21101 L/E DEVICE MALFUNCTION ON FLAP RETRACTION. WHEN FLAPS MOVED TO 2 DEGREE YELLOW L/E FLAP LIGHT IS ON AND 2, 3, 6, 7 AND 4 POSITION TEST LIGHTS ARE GREEN. REPLACED NR 4 FLAP POSITION INDICATING SWITCH IAW MM 27-82-11, OPS CK GOOD. 2 L 7 3 4F RT A3WE 1996051600096 19960516 00096 WP 1996 5 16 96FDEA00938 1 19960509 A 5400 FASTENERS DOUG DC10 DC1030 3023501 WP NR 3 PYLON LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 304FE 46922 SNRM 4353, NR 3 PYLON INSIDE ACCESS PANEL 488 BL PYLON FWD BULKHEAD AT STA YN 342, BOTTOM ROW OF FASTENERS ARE ALL LOOSE . 2 L 7 3 4F A22WE 1996051600097 19960516 00097 WP 1996 5 16 96FDEA00939 1 19960509 A 5400 THRUST LINKS DOUG DC10 DC1030F 3023504 WP NR 3 PYLON LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 304FE 46992 SNRM 4359, NR 3 PYLON FWD ENG MOUNT LOWER THRUST LINKS, 7 MOUNTING BOLTS ARE LOOSE ON PYLON BOTTOM LT AND RT SIDES APPRO XIMATE PYLON STA YN 222. *S/D* RT SIDE TORQUED PER MM 20-50-02, REMOVED AND REPLACED NUTS ON BOTTOM OF FWD THRUST LINK LT AND RT AND RETORQUED PER EO 8-5410-7-4319. 2 L 7 3 4F RT A22WE 1996051600098 19960516 00098 WP 1996 5 16 96FDEA00940 1 19960509 A 5400 THRUST LINK DOUG DC10 DC1030F 3023504 WP NR 3 PYLON LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 304FE 46992 SNRM 4360, NR 3 PYLON FWD ENG MOUNT, LWR THRUST LINK RT SIDE OF PYLON HAS VERTICAL ROW OF .25 BOLTS AND HORIZONTAL ROW O F .3125 IN BOLTS LOOSE, TOTAL OF 18 BOLTS LOOSE AT APPROX PYLON STA YN 222 TO 226. *S/D* REPLACED NUTS WITH NEW AND RE TORQUED PER EO 8-5410-7-4319. 2 L 7 3 4F RT A22WE 1996051600099 19960516 00099 WP 1996 5 16 96FDEA00941 1 19960509 A 5400 THRUST LINK DOUG DC10 DC1030F 3023504 WP NR 3 PYLON LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 304FE 46992 SNRM 4361, NR 3 PYLON FWD ENG MOUNT AREA LOWER THRUST LINK LT SIDE OF PYLON HORIZONTAL ROW OF .3125 BOLTS ARE LOOSE, AS VIEWED FWD LOWER LT SIDE OF PYLON AT APPROX YN222 TO 226, 3 BOLTS LOOSE. *S/D* REPLACED NUTS WITH NEW AND RETORQUED PE R EO 8-5410-7-4319. 2 L 7 3 4F RT A22WE 1996051600100 19960516 00100 WP 1996 5 16 96FDEA00942 1 19960509 A 5753 ARC2499506 FLAP TRACK DOUG DC10 DC1030F 3023504 WP RT TE FLAP GROOVE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 304FE 46992 SNRM 6030, RT I/B FLAP I/B TRACK VERTICAL FACE UPPER AND LWR BEARING SURFACES DAMAGED WITH GROOVES AND GOUGED METAL APP ROX .020 INCHES DEEP DUE TO I/B FLAP CARRIAGE SIDE LOAD BEARING FAILURE. *S/D REMOVED AND REPLACED RT I/B FLAP TRACK PER GMM 57-52-01, INSTALLED TRACK TO FLAP ASD PER GMM 57-52-01. 2 L 7 3 4F RT A22WE 1996051600101 19960516 00101 NM 1996 5 16 96FDEA00943 1 19960510 A 5330 SKIN BOEING 727 727227 1384078 NM BS 1120-1130 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 NR0253 AND 002, CORROSION (C53-100-01) UNDER SKIN BS 1120 TO 1130 STR 30. 2 L 7 3 4F A3WE 1996051600102 19960516 00102 NM 1996 5 16 96FDEA00944 1 19960510 A 5315 FLOOR BEAM BOEING 727 727227 1384078 NM BS 400 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 NR 0342 AND NR 003. CORROSION C53-224-01 ON BS 400 FLOOR BEAM FROM RBL 3-12, WL 208. S/D: REPAIRED TOP CHORD OF FLOOR BEAM AT BS 400, RBL 9-12, WL 208.1 PER FEDEX SRM 53-10-8. 2 L 7 3 4F A3WE 1996051600103 19960516 00103 NM 1996 5 16 96FDEA00945 1 19960510 A 5320 65209102 DOUBLER BOEING 727 727227 1384078 NM BS 731 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 NR 0354 AND NR 004, CORROSION C53-132-01-2 UNDER MOUNTING FLANGE OF DISTRIBUTION DUCT STA 740 - 9, RBL 18 UNDER FAIRING ACCESS OF LOWER DUCT REQUIRED. ****S/D***** COMING. CORRECTIVE ACTION: REMOVED CORROSION FROM DOUBLER IN A 3 INCH X 1 4 INCH AREA. MAXIMUM MATERIAL LOSS IS .010 INCH. ORIGINAL DOUBLER THICKNESS WAS .125 INCH FOUND TO BE WITHIN LIMITS PE R FED EX SRM 53-30-01. TREATED AND RE-FINISHED DOUBLER IAW SRM 53-10-03. 2 L 7 3 4F A3WE 1996051600104 19960516 00104 NM 1996 5 16 96FDEA00946 1 19960510 A 5753 65162276 BONDING JUMPER BOEING 727 727173C 1384059 NM NR 6 K-FLAP CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 199FE 19509 NR0477 AND 003, NR 6 K-FLAP O/B BONDING JUMPER BETWEEN K-FLAP AND L/E STRUCTURE HAS CORROSION AROUND LOWER MOUNT POINT. 2 L 7 3 4F A3WE 1996051600105 19960516 00105 NM 1996 5 16 96FDEA00947 1 19960510 A 5315 FLOOR BEAM BOEING 727 72725 1384006 NM BS 360 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 505FE 18276 CORROSION BS 360 FLOOR BEAM WL 208 RBL 5. CUT OUT DAMAGED PORTION OF FLOOR BEAM AT BS 360 WL 208 RBL 6 TO LBL 10 AND RE PAIRED PER FEDEX SRM 53-10-8. 2 L 7 3 4F A3WE 1996051600106 19960516 00106 WP 1996 5 16 DHL9680304 1 19960507 A 2910 10534040534 HOSE DOUG DC8 DC873F 302199F WP STBY RUDDER PUM RUPTURED A T DHLA A J UNSCHED LANDING DUMP FUEL K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 803DH 46123 HYDRAULIC QUANTITY LEVEL DROPPED TO AUX LEVEL, REQUESTED RETURN CLEARANCE FOR FUEL DUMPING. DUMPED 40,000 LBS, PUMPS PL ACED INTO BYPASS AS SOON AS PREVIOUS DROP WAS NOTED. FOUND THE STANDBY RUDDER PUMP PRESSURE HOSE HAD DEVELOPED PIN HOLE LEAK. REMOVED AND REPLACED HYD FLEX LINE HOSE ASSY, SERVICED HYD RESERVOIR AND LEAK CHECKED AS PER M/M 29-07-00 AND 12 -31-01. 2 L 7 4 4F RT 4A25 1996051600107 19960516 00107 WP 1996 5 16 DHL96804007 1 19960507 A 3260 3280183 STRIKER DOUG DC8 DC873F 302199F WP RT MLG DOOR OUT OF ADJUST A T DHLA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 804DH 46124 ON CLIMB, RIGHT HAND GEAR DOOR UNSAFE LIGHT AND DOORS NOT LATCHED LIGHT ON AFTER GEAR RETRACTION. ADJUSTED STRIKER PER M/M 32-12-1. 2 L 7 4 4F RT 4A25 1996051600108 19960516 00108 NM 1996 5 16 DL72L961079 1 19960505 A 3350 BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 504DA 21306 AFT RT CABIN EMERGENCY LIGHT WILL NOT ILLUMINATE. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1996051600109 19960516 00109 NM 1996 5 16 DL72L961087 1 19960110 A 5754 651622199 RIB BOEING 727 727232 1384082 NM LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 504DA 21306 REPAIRED CRACKED RIB AS PER SRM 57-54-0 FIG 814. 2 L 7 3 4F A3WE 1996051600110 19960516 00110 NM 1996 5 16 DL72L961099 1 19960506 A 3350 POWER PACK BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 506DA 21308 FOUND TRACK LIGHTING INOP FROM ROW 27 TO AFT. REPLACED POWER PACK, LIGHTS OPERATED NORMAL. 2 L 7 3 4F A3WE 1996051600111 19960516 00111 NM 1996 5 16 DL72P961089 1 19960506 A 5240 FRAME BOEING 727 727225 1384077 NM RT SVC DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8889Z 21858 FOUND DURING C-CHECK, AFT RT SVC DOOR FWD FRAME CRACKED AT LWR I/B END OF UPPER HINGE CUTOUT. REPAIRED PER SRM 52-40-2. 2 L 7 3 4F A3WE 1996051600112 19960516 00112 NM 1996 5 16 DL72P961090 1 19960506 A 5711 AUX SPAR BOEING 727 727225 1384077 NM LT WING CHAFED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8889Z 21858 FOUND DURING C-CHECK, LT MLG STRUT DOOR CHAFING AUX SPAR I/B END MARKED, FWD OF NR 4 SCREWJACK. REPAIRED PER M/M 57-4 3-0 PG 802. 2 L 7 3 4F A3WE 1996051600113 19960516 00113 NM 1996 5 16 DL72P961091 1 19960506 A 5754 ANGLE BOEING 727 727225 1384077 NM NR 1 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8889Z 21858 FOUND DURING C-CHECK, .5 INCH CRACK IN NR 1 SLAT SKIN ATTACH ANGLE BELOW TAI DUCT. REPAIRED PER M/M 51-54-0 AND ERA DUE TO EFFECTIVITY. 2 L 7 3 4F A3WE 1996051600114 19960516 00114 NM 1996 5 16 DL72P961093 1 19960506 A 2782 BRACKET BOEING 727 727225 1384077 NM LE FLAP ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8889Z 21858 NR 1 L/E FLAP ACTUATOR MOUNT BRACKET CRACKED AT LOWER I/B CORNER. REPAIRED PER M/M 57-20-21 AND ERA DUE TO A/C EFFECTIV ITY. 2 L 7 3 4F A3WE 1996051600115 19960516 00115 NM 1996 5 16 DL72P961094 1 19960506 A 2782 BRACKET BOEING 727 727225 1384077 NM NR 1 SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8889Z 21858 APPROX 2 INCH CRACK IN NR 1 SLAT I/B AND O/B ACTUATOR MOUNT BRACKET'S. REPAIRED PER M/M 57-20-21 AND ERA DUE TO A/C EFF ECTIVITY. 2 L 7 3 4F A3WE 1996051600116 19960516 00116 NM 1996 5 16 DL72P961095 1 19960506 A 5320 WEB BOEING 727 727225 1384077 NM BS 1237 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8889Z 21858 A .625 INCH CRACK IN LT LOWER TORQUE BOX VERTICAL WEB AT LOWER LIGHTENING HOLE STA 1237. REPAIRED PER M/M 53-11-0 AND E RA DUE TO EFFECTIVITY. 2 L 7 3 4F A3WE 1996051600117 19960516 00117 NM 1996 5 16 DL72P961105 1 19960506 A 5313 STRINGER BOEING 727 727225 1384077 NM BS 940 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8889Z 21858 STRINGER 18A RT CRACKED AT STA 940 SUPPORT FITTING AFT BOLT. REPAIRED PER MM 53-12-0. 2 L 7 3 4F A3WE 1996051600118 19960516 00118 NM 1996 5 16 DL72S961085 1 19960506 A 5320 INTERCOSTAL BOEING 727 727232 1384082 NM BS 985 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 527DA 21587 SKIN CLIP IN AFT B/B HAS CORROSION ON LWR I/B CORNER AT STA 985 O/B OF STR 29R. REF NR 12, TASK C53-100-01. 2 L 7 3 4F A3WE 1996051600119 19960516 00119 NM 1996 5 16 DL72S961086 1 19960506 A 5330 SKIN BOEING 727 727232 1384082 NM BS 992 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 527DA 21587 TRANSFERRED FROM A/C LOG BOOK ITEM 013269001: RIVET SHEARED AND BULGE IN FUSELAGE SKIN AT FS 992 AT STR 28R CORROSION I TEM MARKED NR 41, TRANSFERRED FROM NR 19 TPA D-2 LTR CHK 5-2-96. 2 L 7 3 4F A3WE 1996051600120 19960516 00120 NM 1996 5 16 DL72S961097 1 19960423 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 942 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 401DA 21145 THE RT STRINGER 18A CRACKED AT STA 942. REPAIRED PER MM 53-12-0, PAGE 819. 2 L 7 3 4F A3WE 1996051600121 19960516 00121 NM 1996 5 16 DL72S961104 1 19960103 A 5753 652163262 CHORD BOEING 727 727232 1384082 NM RT TE MID FLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 525DA 21585 AFT LOWER CHORD CRACKED AT 22, 33, 37 AND 55 INCHES FROM I/B END. REPLACED SECTION OF CHORD AND REPAIR DOUBLER PER MM 5 7520. 2 L 7 3 4F A3WE 1996051600122 19960516 00122 NM 1996 5 16 DL72W961106 1 19960507 A 3350 BATTERY PACK BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 293WA 22111 RIGHT AFT OVERWING SLIDE LIGHT INOP. REPLACED BATTERY PACK AND RACK, LIGHT CHECKS NORMAL. 2 L 7 3 4F A3WE 1996051600123 19960516 00123 NM 1996 5 16 DL73S961082 1 19960506 A 7931 OIL PRESS IND BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE INOP A DALA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SO 27 307DL 23079 709124 ON T/O, NR 2 ENGINE OIL PRESSURE WENT TO 58 PSI INITIALLY ENG RETARDED TO IDLE AND OIL PRESS REMAINED OUT OF LIMITS. AL L OTHER INDICATIONS NORMAL EVENTUALLY NR 2 OIL PRESS RETURNED TO NORMAL WITH ENGINE AT REDUCED THRUST OIL TEMP SLIGHTLY LOWER THAN NR 1. REPLACED OIL PRESSURE REGULATOR (P/N 811131) OIL PRESSURE TRANSMITTER (P/N ST104Z) AND PRESSURE GUAGE (P/N SRL04L). 2 L 7 2 4F 4 F RT A16WE E2EA 1996051600124 19960516 00124 WP 1996 5 16 DLL10961100 1 19960506 A 5330 1542224 SKIN LKHEED 1011 10113851 5265010 WP FS 718 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 720DA 193C1136 AT FS 717 AND 719 BETWEEN STRINGERS 23 AND 24, TWO DENTS WERE FOUND JUST AFT OF THE LOWER AFT CORNER OF THE C-1 CARGO DO OR. THE DENTS WERE CUT OUT, FILLED AND REINFORCED. 2 L 7 3 4F A23WE 1996051600125 19960516 00125 WP 1996 5 16 DLL10961101 1 19960506 A 5330 1505393109 SKIN LKHEED 1011 10113851 5265010 WP FS 189 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 720DA 193C1136 A DENT WAS DISCOVERED AT FS 189 LBL 30.6. THE DENT WAS CUT OUT, FILLED AND REINFORCED. 2 L 7 3 4F A23WE 1996051600126 19960516 00126 WP 1996 5 16 DLL14961102 1 19960506 A 5330 1503141 SKIN LKHEED 1011 1011385115 5265015 WP C1 DOOR CUTOUT DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 737D 193C1228 DENT IN THE FUSELAGE SKIN WAS FOUND APPROX 15 AFT OF THE AFT EDGE OF THE C-1 DOOR OPENING BETWEEN STR 24, 25. THE DAMA GE WAS CUT OUT, FILLED AND REINFORCED. 2 L 7 3 4F A23WE 1996051600127 19960516 00127 WP 1996 5 16 DLL15961092 1 19960506 A 3350 POWER PACK LKHEED 1011 10113853 5265020 WP L2 DOOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 752DA 193W1172 EMERGENCY EXIT SIGNS AND EXTERIOR LIGHT NEAR L2 DOOR INOP. REMOVED AND REPLACED EMERGENCY POWER PACK PER MM, OPS CHECKS GOOD PER MM. 2 L 7 3 4F A23WE 1996051600128 19960516 00128 WP 1996 5 16 DLL17961055 1 19960503 A 3350 LIGHT LKHEED 1011 10113853 5265020 WP EXTERIOR R1 DOOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 767DA 193H1209 FOUND EXTERIOR EMERGENCY LIGHT INOP AT R1 DOOR. REPLACED LIGHT ASSEMBLY. 2 L 7 3 4F A23WE 1996051600129 19960516 00129 NM 1996 5 16 DLM88961096 1 19960506 A 2910 HYD LINE DOUG MD88 MD88 3023688 NM NR 2 PRESS MOD CHAFED A DALA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 27 952DL 49883 DURING DESCENT, HYD PRESS LOW LIGHT ON FLAT PLATE DISPLAY ILLUMINATED. IMMEDIATELY LOST ALL HYDRAULIC QTY, ACCOMPLISHED PROCEDURE FOR LOSS OF RIGHT HYD SYSTEM. MANUALLY LOWERED GEAR AND LANDING WAS UNEVENTFUL. 2 L 7 2 4F RT A6WE 1996051600130 19960516 00130 NM 1996 5 16 DLM88961098 1 19960507 A 3350 LIGHT TRACK DOUG MD88 MD88 3023688 NM CABIN CRACKED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 936DL 49723 EMERGENCY LIGHT TRACK CRACKED. 2 L 7 2 4F RT A6WE 1996051600131 19960516 00131 WP 1996 5 16 MWEA96132 1 19960508 A 2612 W283A16N GROUND WIRE DOUG DC9 DC914 3022034 WP LT ENGINE NOT ATTACHED A MWEA A UNSCHED LANDING L NO TEST CR CRUISE 1 GL 31 400ME 45727 WITH B-LOOP DEFERRED FROM PREVIOUS WRITEUP AND AT CRUISE ALTITUDE, A-LOOP WOULD NOT TEST ON LT ENGINE. FOUND GROUND WIR E ON FIRE LOOP NOT GROUNDED. FIXED WIRE AND REATTACHED GROUND. 2 L 7 2 4F A6WE 1996051600132 19960516 00132 WP 1996 5 16 MWEA96133 1 19960509 A 2612 1W256A24 CONNECTOR DOUG DC9 DC914 3022034 WP LT ENGINE CORRODED A MWEA A UNSCHED LANDING L NO TEST CR CRUISE 1 GL 31 400ME 45727 A/C DIVERTED TO MKE, LT ENG FIRE LOOP-B FLICKERING AMBER LIGHT AND ANNUNCIATOR LIGHT, SELECTED A-LOOP LT ENG, IT WOULD N OT TEST. REPAIRED CHAFING WIRE NEAR FWD PYLON CONNECTOR FOR LOOP-B. SLIGHT CORROSION IN CANNON PLUG IN PYLON FOR LOOP- A. CLEANED CANNON PLUG, OPS CHECK GOOD ON BOTH A/B FIRE LOOPS LT ENGINE. 2 L 7 2 4F A6WE 1996051600133 19960516 00133 EU 1996 5 16 QXEA9600165 1 19960506 A 3350 6008905 BATTERY PACK FOKKER F28 F28MK1000 4990808 EU CABIN DISCHARGED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 450US 11101 CABIN EVACUATION LIGHT ON ROW 4, 5, 6, 7 AND 8 ARE INOP. BATTERY PACKS REPLACED AT BINS 7 RT, 8 LT IAW MAINT MANUAL AND LIGHTS OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996051600134 19960516 00134 EU 1996 5 16 QXEA9600166 1 19960506 A 3397 WIRE FOKKER F28 F28MK1000 4990808 EU CABIN BROKEN A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 450US 11101 EMERGENCY EXIT SIGN ABOVE ROW 8 INOP. BROKEN WIRE REPAIRED AT SIGN AND SIGN OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996051600135 19960516 00135 NM 1996 5 16 QXEA9600167 1 19960509 A 3350 82410162007 CONTROL BOX DHAV DHC8 DHC8102 2809003 NM CABIN MALFUNCTIONED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 822PH 106 EMERGENCY LIGHTS WOULD NOT TURN OFF. EMERGENCY LIGHT CONTROL BOX REPLACED AND EMERGENCY LIGHTS OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 1996051600136 19960516 00136 NM 1996 5 16 SCNA96094 1 19960410 A 5320 651960623324 TIE FITTING BOEING 727 7272J4 1384006 NM BS 1183 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON FLOOR SUPPORT TIE FITTINGS AND BOLTS IN THE AFT CARGO COMPARTMENT , BODY STATION 1183, RBL 38. REMOVED AND REPLACED FITTINGS IN ACCORDANCE WITH B727 SRM 51-10-1, 51-30-3 AND 51-10-2. 2 L 7 3 4F RT A3WE 1996051600137 19960516 00137 NM 1996 5 16 SCNA96095 1 19960410 A 5320 TIE FITTING BOEING 727 7272J4 1384006 NM BS 1180 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON STRINGER 17R TIE FITTING AND BETWEEN STRINGER 18R TIE FITTING AND FUSELAGE SKIN. FABRICATED AND INSTALLED REPAIRS FOR STRINGER 17R TIE FITTING AND STRINGER 18R TIE FITTING IN ACCORDANC E WITH B727 SRM 53-10-3. 2 L 7 3 4F RT A3WE 1996051600138 19960516 00138 NM 1996 5 16 SCNA96096 1 19960410 A 5315 FLOOR BEAM BOEING 727 7272J4 1384006 NM BS 1130 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON FLOOR BEAM CHORDS AT BS 1130, RBL 70 AND LBL 70. TRIMMED OUT DAM AGED AREA, FABRICATED AND INSTALLED FILLERS, ANGLES, AND STRAPS IN ACCORDANCE WITH B727 SRM 53-10-8. 2 L 7 3 4F RT A3WE 1996051600139 19960516 00139 NM 1996 5 16 SCNA96097 1 19960411 A 5313 STRINGER BOEING 727 7272J4 1384006 NM BS 1180 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON STRINGER 26R, BS 1180 TO 1183. REMOVED CORRODED MATERIAL, FABRIC ATED AND INSTALLED REPAIR IN ACCORDANCE WITH B727 SRM 51-10-6, 51-30-2 AND 51-10-2. 2 L 7 3 4F RT A3WE 1996051600140 19960516 00140 NM 1996 5 16 SCNA96098 1 19960413 A 5320 ANGLE BOEING 727 7272J4 1384006 NM BS 1263 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT, A CRACK WAS FOUND ON THE RT TORQUE BOX ATTACH ANGLE AT APPROXIMATELY BS 1263. ADDITIONA LLY, THE ACTUATOR FITTING HAD MISSING COLLARS AND LOOSE FASTENERS. REMOVED ALL EFFECTED PARTS. MAGNETIC PARTICLE INSPE CTION OF ACTUATOR REVEALED NO DEFECTS. FABRICATED AND INSTALLED REPAIRS IN ACCORDANCE WITH SRM 51-40-2. REINSTALLED IT EMS IN ACCORDANCE WITH SB B727-53-129 AND 130. 2 L 7 3 4F RT A3WE 1996051600141 19960516 00141 NM 1996 5 16 SCNA96099 1 19960413 A 5347 806019401 SEAT TRACK BOEING 727 7272J4 1384006 NM COCKPIT WORN A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT, HOLES WERE FOUND WORN INTO THE FLIGHT ENGINEER SEAT TRACK. FABRICATED A NEW SHIM AND IN STALLED NEW SEAT TRACK IN ACCORDANCE WITH B727 SRM 53-10-1. 2 L 7 3 4F RT A3WE 1996051600142 19960516 00142 NM 1996 5 16 SCNA96100 1 19960415 A 5315 FLOOR BEAM BOEING 727 7272J4 1384006 NM BS 1170 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT, A FLOOR BEAM UPPER CHORD WAS FOUND CORRODED AT BS 1170, LBL 12 AND LBL 25. REMOVED CORR OSION, FABRICATED AND INSTALLED AN ANGLE REPAIR IN ACCORDANCE WITH B727 SRM 53-10-8. 2 L 7 3 4F RT A3WE 1996051600143 19960516 00143 NM 1996 5 16 SCNA96101 1 19960415 A 5315 FLOOR BEAM BOEING 727 7272J4 1384006 NM BS 1070 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT, A FLOOR BEAM UPPER CHORD WAS FOUND CORRODED AT BS 1070, RBL 50 TO 60. REMOVED CORROSION , FABRICATED AND INSTALLED A REPAIR IN ACCORDANCE WITH B727 SRM 53-10-8, FIGURE 8. 2 L 7 3 4F RT A3WE 1996051600144 19960516 00144 NM 1996 5 16 SCNA96102 1 19960415 A 5320 BAC1493577 BRACE BOEING 727 7272J4 1384006 NM BS 1125 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT, A CABIN FLOOR SUPPORT BRACE WAS FOUND CORRODED AT MOUNT HOLES AT BS 1125, LBL 12. FABRI CATED AND INSTALLED NEW FLOOR SUPPORT BRACE IN ACCORDANCE WITH B727 SRM 51-40-3, FIGURE 1. 2 L 7 3 4F RT A3WE 1996051600145 19960516 00145 NM 1996 5 16 SCNA96103 1 19960415 A 5320 THRESHOLD BOEING 727 7272J4 1384006 NM L 1 DOOR CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON FLOOR ANGLES AT THE L-1 DOOR THRESHOLD. REMOVED FLOOR ANGLE, THR ESHOLD AND Z-ANGLE. FABRICATED AND INSTALLED NEW PARTS IN ACCORDANCE WITH B727 SRM 51-40-2 AND FIGURE 1, 51-40-3, FIGUR E 1. 2 L 7 3 4F RT A3WE 1996051600146 19960516 00146 NM 1996 5 16 SCNA96104 1 19960416 A 5320 65185112 TIE FITTING BOEING 727 7272J4 1384006 NM BS 1140 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON STRINGER TIE FITTINGS AT THE AFT SIDE OF THE NR 3 CARGO DOOR FRAM E CUTOUT, UNDER THE WEB. FABRICATED AND INSTALLED WEB AND TIE FITTINGS IN ACCORDANCE WITH B727 SRM 51-30-2. FABRICATED AND INSTALLED T-ANGLES IN ACCORDANCE WITH B727 SRM 51-40-2 AND 51-40-3. 2 L 7 3 4F RT A3WE 1996051600147 19960516 00147 NM 1996 5 16 SCNA96105 1 19960420 A 5315 FLOOR BEAM BOEING 727 7272J4 1384006 NM BS 1110 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON THE LOWER CHORD OF A FLOOR BEAM AT BS 1110, BL 0. REMOVED CORROD ED SECTION, FABRICATED REPAIR PARTS AND INSTALLED IN ACCORDANCE WITH B727 SRM 53-10-8, FIGURE 8 AND 51-30-2. 2 L 7 3 4F RT A3WE 1996051600148 19960516 00148 NM 1996 5 16 SCNA96106 1 19960429 A 5241 DOORSTOP BOEING 727 7272J4 1384006 NM GALLEY CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 284SC 21438 DURING HEAVY MAINTENANCE VISIT, A CRACK WAS FOUND ON THE FORWARD GALLEY LOWER DOORSTOP. STOP DRILLED CRACK, FABRICATED AND INSTALLED A REPAIR DOUBLER IN ACCORDANCE WITH B727 SRM 51-30-2 AND AERO CORP E0 96-296 DATED 4/25/96. 2 L 7 3 4F RT A3WE 1996051600149 19960516 00149 NM 1996 5 16 SCNA96107 1 19960427 A 5347 BAC1520792 SEAT TRACK BOEING 727 727225 1384077 NM BS 1030-1130 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON THE LEFT SIDE CABIN SEAT TRACK, BS 1030 TO 1130. CORROSION WAS W ITHIN LIMITS BETWEEN BS 1070 TO 1130. REMOVED, FABRICATED AND INSTALLED A NEW SECTION FROM BS 1010 TO 1070 IN ACCORDANC E WITH B727 SRM 53-10-5. 2 L 7 3 4F A3WE 1996051600150 19960516 00150 NM 1996 5 16 SCNA96108 1 19960427 A 5320 BAC1518344 FLOOR SUPPORT BOEING 727 727225 1384077 NM BS 1030 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON FLOOR SUPPORT NEXT TO L2 DOOR, BS 1030. REMOVED CORRODED FLOOR S UPPORT, FABRICATED AND INSTALLED A NEW SUPPORT IN ACCORDANCE WITH B727 SRM 51-40-4. 2 L 7 3 4F A3WE 1996051600151 19960516 00151 NM 1996 5 16 SCNA96109 1 19960424 A 5312 BLKHD STIFFENER BOEING 727 727225 1384077 NM BS 1183 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON AFT PRESSURE BULKHEAD STIFFENER, BS 1183 RBL 61, WL 220. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR IN ACCORDANCE WITH B727 SRM 51-40-4. 2 L 7 3 4F A3WE 1996051600152 19960516 00152 NM 1996 5 16 SCNA96110 1 19960424 A 5312 BLKHD STIFFENER BOEING 727 727225 1384077 NM BS 1183 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON AFT PRESSURE BULKHEAD STIFFENER, BS 1183 LBL 59 WL 220. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR IN ACCORDANCE WITH B727 SRM 51-40-4. 2 L 7 3 4F A3WE 1996051600153 19960516 00153 NM 1996 5 16 UPS96220064 1 19960503 A 5241 65167209 DOOR GATE BOEING 727 72725C 138400H NM GALLEY DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 937UP 19302 INSPECTION TYPE 'C', MID GALLEY DOOR UPPER GATE BEAM CRACKED ON I/B RADIUS ALL AFT SIDE. REMOVED AND REPLACED BEAM IAW SRM 51-30-2, 51-20-4 AND MM 52-12-11. 2 L 7 3 4F A3WE 1996051600154 19960516 00154 NM 1996 5 16 UPS96220065 1 19960501 A 5320 INTERCOSTAL BOEING 727 72725C 138400H NM BS 1045 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 937UP 19302 INSPECTION TYPE 'C', CORROSION ON THE INTERCOSTAL AT BS 1045, RBL 6 WL 146. REMOVED CORROSION AND REPAIRED INTERCOSTAL IAW SRM 51-30-2, 51-10-2 AND MM 51-20-15. 2 L 7 3 4F A3WE 1996051600155 19960516 00155 NM 1996 5 16 UPS96220066 1 19960506 A 5752 6521773501 FITTING BOEING 727 72725C 138400H NM RT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 937UP 19302 INSPECTION TYPE 'C', CENTER HINGE 0N RT WING AILERON TAB AILERON SIDE IS CORRODED. REMOVED CORRODED HINGE FITTING AND I NSTALLED NEW HINGE FITTING PER SRM 51-30-2 AND MM 27-10-11. 2 L 7 3 4F A3WE 1996051600156 19960516 00156 NM 1996 5 16 UPS96220067 1 19960506 A 5751 65247811 NOSE BOEING 727 72725C 138400H NM AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 937UP 19302 INSPECTION TYPE 'C' AILERON SERVO HOUSING IN FWD NOSE COMP IS CORRODED. REMOVED CORRODED HOUSING, INSTALLED NEW HOUSING PER MM 22-11-11. 2 L 7 3 4F A3WE 1996051600157 19960516 00157 NM 1996 5 16 UPS96220068 1 19960507 A 5720 6516200361 STIFFENER BOEING 727 72725C 138400H NM LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 937UP 19302 INSPECTION TYPE 'C', CORROSION ON LT WING FRONT SPAR VERT STIFFENER 5TH STIFFENER O/B FROM ACCESS CUTOUT 7340. REMOVED CORRODED STIFFENER, INSTALLED NEW SIFFENER PER SRM 51-3-2, 57-10-4 AND MM 28-11-0. 2 L 7 3 4F A3WE 1996051600158 19960516 00158 NM 1996 5 16 UPS96220082 1 19960428 A 5320 CLIP BOEING 727 72727C 138400J NM BS 400 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE 'D', E AND E COMP STR CLIP CORRODED STA 400 STR 24R. REMOVED FAB AND INSTALLED CLIP IAW SRM 53-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 1996051600159 19960516 00159 NM 1996 5 16 UPS96220083 1 19960428 A 5320 CLIP BOEING 727 72727C 138400J NM BS 400 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE 'D', E AND E COMP STR CLIP CORRODED STA 400 STR 22R. REMOVED FAB AND INSTALLED CLIP IAW SRM 53-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 1996051600160 19960516 00160 NM 1996 5 16 UPS96220084 1 19960504 A 5311 FRAME BOEING 727 72727C 138400J NM FS 615 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE 'D', FRAME 615 ANGLE CRACKED AT STR 19L. REMOVED, FAB AND INSTALLED FRAME REPAIR DOUBLER IAW SRM 53-10- 2, BAC DRAWING 65-40509 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996051600161 19960516 00161 NM 1996 5 16 UPS96220085 1 19960505 A 5712 RIB BOEING 727 72727C 138400J NM WS 519 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE 'D', RIGHT WING INTERNAL RIB STA 519 AT STR 6 IS CRACKED IN RADIUS ON LWR SIDE. STOP DRILLED CRACK, FAB AND INSTALLED REPAIR IAW SRM 57-10-5, 51-10-1 AND 57-10-5. 2 L 7 3 4F A3WE 1996051600162 19960516 00162 NM 1996 5 16 UPS96220086 1 19960503 A 5320 INTERCOSTAL BOEING 727 72727C 138400J NM BS 219.8-211.8 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE 'D', LWR NOSE COMP SURFACE CORROSION ON ALL SIDES OF INTERCOSTAL STA 211.8 TO 219.8 STR 26R. REMOVED IN TERCOSTAL AND CORROSION FOUND TO BE BEYOND LIMITS 51-10-65, 3-10-1, FAB AND INSTALLED INTERCOSTAL. 2 L 7 3 4F A3WE 1996051600163 19960516 00163 NM 1996 5 16 UPS96220087 1 19960430 A 5320 U69144925 SPLICE BOEING 727 72727C 138400J NM FS 440 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE 'D', STR 21L SPLICE AT BS 440 HAS MODERATE CORROSION. REMOVED AND REPLACED SPLICE SECTON IAW SRM 51-30- 2. 2 L 7 3 4F A3WE 1996051600164 19960516 00164 NM 1996 5 16 UPS96220088 1 19960430 A 5320 SPLICE BOEING 727 72727C 138400J NM BS 440 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE 'D', STR 20L SPLICE AT BS 440 HAS MODERATE CORROSION. REMOVED AND REPLACED SPLICE SECTON IAW SRM 51-30- 2. 2 L 7 3 4F A3WE 1996051600165 19960516 00165 NM 1996 5 16 UPS96220089 1 19960507 A 5313 STRINGER BOEING 727 72727C 138400J NM BS 458 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE 'D', E AND E COMP EXFOLIATED CORROSION ON STR 26L STA 458. REMOVED DAMAGED AREA FAB REPAIR PART AND INS TALLED REPAIR PART FROM STA 430 TO 480 IAW SRM 53-10-3, AND 51-30-2. 2 L 7 3 4F A3WE 1996051600166 19960516 00166 NM 1996 5 16 UPS96420063 1 19960419 A 5711 SPAR WEB BOEING 747 747123 1384873 NM WS 550 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE 'C', LT WING REAR SPAR WEB OF LT WING REAR SPAR HAS CORROSION AT WS 550. REPAIRED CORROSION IAW UPS EFN 747-57-0323. 2 L 7 4 4F A20WE 1996051600167 19960516 00167 GL 1996 5 16 UPS96820062 2 19960508 A 7200 ENGINE DOUG DC8 DC871F 302199D WP GE CFM CFM562 GL NR 1 FLAME-OUT A IPXA E ENGINE SHUTDOWN X ENGINE FLAMEOUT CR CRUISE 1 SO 01 730UP 46030 INSPECTION, NR 1 ENGINE FLAMED OUT IN FLIGHT. NR 1 ENGINE OVER PRESSURE LIGHT REMAIN'S ILLUMINATED. PERFORMED TROUBLES HOOTING PROCEDURES PER MM 71-00-00 PAGE 153-169, NO ABNORMALITIES NOTED. 2 L 7 4 4F 4 F RT 4A25 E2GL 1996051600168 19960516 00168 WP 1996 5 16 UPS96820069 1 19960509 A 2560 EXIT SLIDE DOUG DC8 DC873F 302199F WP MAIN ENTRY DOOR LOOSE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION, MAIN ENTRY DOOR EMERGENCY EXIT SLIDE UNFASTENED. RESTOWED ENTRANCE SLIDE. 2 L 7 4 4F RT 4A25 1996051600169 19960516 00169 WP 1996 5 16 UPS96820070 1 19960504 A 5400 SLOT SECTION DOUG DC8 DC873F 302199F WP NR 3 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE 'C', NR 3 PYLON STUB WING SLOT SECTION OUTER I/B END HAS CRACKS. FAB REPAIR FILLER AND DOUBLERS, ALODIN ED, PRIMED AND INSTALLED IAW TIMCO REO 01915 AND UPS EO DC8-57-0668. 2 L 7 4 4F RT 4A25 1996051600170 19960516 00170 WP 1996 5 16 UPS96820071 1 19960504 A 5720 ATTACH POINTS DOUG DC8 DC873F 302199F WP RT WING LE CHAF A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE 'C', RT WING LEADING EDGE O/B EDGE ATTACH POINTS HEAVY CHAFED. FAB DOUBLER, ALODINED AND INSTALLED IAW UPS EO DC8-57-0665. 2 L 7 4 4F RT 4A25 1996051600171 19960516 00171 WP 1996 5 16 UPS96820072 1 19960504 A 5400 WING SLOT DOUG DC8 DC873F 302199F WP NR 2 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE 'C', 32 PYLON STUB WING SLOT SECTION O/B END HAS SEVERAL CRACKS INSIDE OF AREA. STOP DRILLED CRACKS AND INSTALLED FILLER AND DOUBLER IAW UPS EO DC8-57 -0667. 2 L 7 4 4F RT 4A25 1996051600172 19960516 00172 WP 1996 5 16 UPS96820073 1 19960504 A 5720 CAP DOUG DC8 DC873F 302199F WP AUX SPAR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE 'C', LWR AUX SPAR CAP HAS A CRACK IN THE BOLT HOLE. DRILLED NEW FITTING AND INSTALLED FITTING IAW SRM 5 1-1-20D, 51-3-2, 5 1-1-24 AND UPS EO DC8-5720-0956F. 2 L 7 4 4F RT 4A25 1996051600173 19960516 00173 WP 1996 5 16 UPS96820074 1 19960504 A 5320 SUPPORT DOUG DC8 DC873F 302199F WP BS 240 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE 'C', STATION 240 RT FLOOR BEAM SUPPORT LWR END IS CORRODED AT FUSELAGE FRAME. REMOVED GUSSET AND ATTACH ANGLE, FAB REPAIR DOUBLERS, REINSTALLED GUSSET AND INSTALLED REPAIR DOUBLERS IAW SRM 51-1-20D, 51-1-21 AND 53-2-0. 2 L 7 4 4F RT 4A25 1996051600174 19960516 00174 WP 1996 5 16 UPS96820075 1 19960504 A 5720 CAP DOUG DC8 DC873F 302199F WP AUX SPAR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE 'C', UPPER AUX SPAR CAP HAS CRACK IN ATTACHMENT HOLE WHICH EXTENDS TO EDGE. DRILLED FITTING AND INSTALL ED IAW 51-3-2, 51-1-20D AND 51-1-24 TO BE INSTALLED ON UPS TASK CARD NR 1056. 2 L 7 4 4F RT 4A25 1996051600175 19960516 00175 WP 1996 5 16 UPS96820076 1 19960418 A 5320 3641004501 FITTING DOUG DC8 DC873F 302199F WP FS 878 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE 'C', HEAVY CORROSION ON VERTICAL FITTING ABOVE LONG 24L FS 878. REPLACED FITTING PER SRM 53-2-0 FIG 8. 2 L 7 4 4F RT 4A25 1996051600176 19960516 00176 WP 1996 5 16 UPS96820077 1 19960423 A 5320 SHEAR TIE DOUG DC8 DC873F 302199F WP BS 700 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE 'C', SHEAR TIE CRACKED AT STA 700XLW LONGERON 10R. REPAIRED SHEAR TIE PER SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1996051600177 19960516 00177 WP 1996 5 16 UPS96820078 1 19960424 A 5320 WEB DOUG DC8 DC873F 302199F WP BS 800 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE 'C', WEB CRACKED AT STA 800 XCW LONG 5L. REPAIRED WEB PER DC8-5350-7876. 2 L 7 4 4F RT 4A25 1996051600178 19960516 00178 WP 1996 5 16 UPS96820079 1 19960418 A 5240 4655987 HINGE DOUG DC8 DC873F 302199F WP NR 4 BELLY DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE 'C', BELLY DOOR SKIN HINGE CRACKED AND BROKEN LUGS. REPLACED HINGE PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1996051600179 19960516 00179 WP 1996 5 16 UPS96820080 1 19960418 A 5240 SKIN DOUG DC8 DC873F 302199F WP NR 4 BELLY DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE 'C', 34 BELLY SKIN DOOR HAS A CRACK BEYOND SCOPE OR EO REPAIR. REPAIRED SKIN PER SRM 52-2-0 AND EO NR D C8-5530-6643D. 2 L 7 4 4F RT 4A25 1996051600180 19960516 00180 WP 1996 5 16 UPS96820081 1 19960421 A 5540 BRACKET DOUG DC8 DC873F 302199F WP RUDDER LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE 'C', 2ND RUDDER HINGE POINT 2, 2 INCH LONG CRACK ON BRACKETS ALONG TOP AND BOTTOM ENDS. REPLACED BRACKE TS PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996051600181 19960516 00181 NE 1996 5 16 9610379874 2 19960506 A 7532 PRBC DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7B 52053 NE NR 1 ENGINE FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 9338 47347 657371 NR 1 ENGINE EPR INDICATION FLUCTUATED ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. M AINTENANCE REPLACED THE PRBC WITH A SERVICEABLE UNIT. 2 L 7 2 4F 4 F A6WE E2EA 1996051600182 19960516 00182 NE 1996 5 16 9610411155 2 19960509 A 7200 ENGINE DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 3 MALFUNCTIONED A NWAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS LD LANDING 1 GL 01 155US 46764 86186 DURING LANDING ROLLOUT, THE NR 3 ENGINE EXPERIENCED REVERSE STALL WITH A SUBSEQUENT TAILPIPE FLAME WHICH WAS REPORTED BY THE CONTROL TOWER. THE NR 3 ENGINE WAS SHUTDOWN AND FIRE BOTTLE DISCHARGED AS EGT CLIMBED TO 915 DEGREES CELSIUS. HOW EVER, THERE WAS NO FIRE WARNING INDICATION EXPERIENCED. BORESCOPE INSPECTION BY BOS MAINTENANCE REVEALED NO DISCREPANCI ES. AIRCRAFT RETURNED TO SERVICE WITH NR 3 ENGINE PUT ON 75 HOUR MONITOR. 2 L 7 3 4F 4 F A22WE E20EA 1996051600183 19960516 00183 EU 1996 5 16 9610423214 1 19960510 A 3260 848401 PROX SENSOR AIRBUS 320 A320211 3930320 EU RT MLG DOOR MALFUNCTIONED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 314US 160 DURING CLIMBOUT AFTER LANDING RETRACTION, RECEIVED L/G GEAR NOT UPLOCKED AND L/G DOORS NOT CLOSED MESSAGES. ALL DOORS I NDICATIONS WERE ILLUMINATED AMBER INTRANSIT AND ALL GEAR INDICATION TRIANGLES WERE ILLUMINATED RED. CYCLED LANDING GEAR HANDLE AND ALL INDICATIONS WERE NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED ALL GEAR DOOR OPEN PROX IMITY SENSORS AND REPLACED THE RIGHT MAIN LANDING GEAR DOOR PROXIMITY SENSOR, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996051600184 19960516 00184 WP 1996 5 16 96104311596 1 19960513 A 3350 EMSE299 BATTERY PACK DOUG DC10 DC1040 3023508 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 159US 46768 DURING LINE INSPECTION, FOUND THE EMERGENCY ESCAPE PATH LIGHT FROM DOOR 3L TO ROW 28 DIM. REPLACED EMERGENCY LIGHT BATT ERY PACK. 2 L 7 3 4F A22WE 1996051600185 19960516 00185 EU 1996 5 16 96FDEA00948 1 19960511 A 2750 CONNECTOR AIRBUS 310 A310203 EU LT TE FLAP VANE WATER CONTAM A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 423FE 281 DURING FLAP RETRACTION ECAM WARNING FLAPS VANE JAM, FLAP RETRACTION LIMITED. RESET BOTH SFCC'S HAD FAULTS ON LEFT O/B V ANE INSPECTED ALL VANES FOR SECURITY, NO DEFECTS. FOUND H20 IN CANNON PLUG OF LT O/B VANE, CLEANED. CYCLED FLAPS USING GREEN PUMPS AND NR 1 ENG, CKD GOOD BOTH TIMES. 2 L 7 2 4F RT A35EU 1996051600186 19960516 00186 NM 1996 5 16 96FDEA00949 1 19960511 A 2780 RETRACT MECH BOEING 727 727233 138408A NM NR 4 LE FLAP MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 218FE 21101 AFTER T/O, NR 4 L/E FLAP WOULD SHOW INTRANSIT, AMBER LIGHT ON SECOND OFFICER'S PANEL. COMPLIED WITH L/E DEVICE MALFUNCT ION DURING FLAP RETRACTION A. NR 4 L/E FLAP W/N RETRACT, RETURNED TO MIA. REMOVED JUMPER FROM NR 4 L/E FLAP SWITCH AND RECONNECTED SWITCH. FUNCTION CHECKED TEST LEADING FLAPS PER MM 27-81-0 PAGE 512. BOTH FWD AND SECOND OFFICER'S PANEL AND L/E FLAPS NORMAL. WORK RELEASE ITEM NR 27-80/1079, CLEARED MOCC NOTIFIED. 2 L 7 3 4F RT A3WE 1996051600187 19960516 00187 WP 1996 5 16 96FDEA00950 1 19960510 A 5412 BULKHEAD DOUG DC10 DC1010CF 3023502 WP NR 1 ENG PYLON LOOSE SCREWS A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68049 47803 NR 1 ENG PYLON I/B SIDE AFT BULKHEAD AREA, THERE ARE 8 LOOSE TRI-WING SCREWS ON STA YN 417.212. REMOVED BOLTS FOR INSPE CTION AND CLEARED BOLT HOLES. COMPLIED WITH HFEC INSPECTION ON 8 BOLTS HOLES, NO DEFECT NOTED. INSTALLED BOLTS AND TOR QUED PER MM 20-50-02. 2 L 7 3 4F RT A22WE 1996051600188 19960516 00188 WP 1996 5 16 96FDEA00951 1 19960510 A 5412 BULKHEAD DOUG DC10 DC1010CF 3023502 WP NR 1 ENG PYLON LOOSE BOLTS A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68049 47803 NR 1 ENG PYLON AFT BULKHEAD AFT FACE TWO ATTACH BOLTS ARE LOOSE AT UPPER AREA. REMOVED BOLTS FOR INSPECTION AND CLEANED BOLT HOLES. COMPLIED WITH HFEC INSPECTION ON 2 BOLT HOLES, NO DEFECTS NOTED. INSTALLED AND TORQUED BOLTS PER MM 20-50 -02. 2 L 7 3 4F RT A22WE 1996051600189 19960516 00189 SO 1996 5 16 COMA9610142 1 19960509 A 2913 63163 HYD PUMP EMB 120 EMB120RT SO LT ENGINE FAILED A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 249CA 1658 343 120230 LEFT ENGINE DRIVEN HYDRAULIC PUMP FAILED. REPLACED HYDRAULIC PUMP. 2 L 7 2 4T RT A31SO 1996051600190 19960516 00190 SW 1996 5 16 COMA9620006 1 19960511 A 7712 31024766 TQ SIGNAL COND SWRNGN SA227 SA227AC 8780603 SW RT ENGINE OUT OF ADJUST A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 704C 12670 12670 AC704 RT ENGINE DID NOT ACHIEVE REQUIRED TORQUE, TAKEOFF ABORTED. ADJUSTED THE TORQUE SIGNAL CONDITIONER AND ACFT RETURNED TO SERVICE. 2 L 7 2 4T RT A8SW 1996051600191 19960516 00191 EA 1996 5 16 COMA9660084 1 19960509 A 3230 16600101 UPLOCK CNDAIR CL600 CL6002B19 EA NLG MALFUNCTIONED A COMA K NONE O OTHER AP APPROACH 1 SO 01 916CA 7014 WHEN LANDING GEAR SELECTED DOWN, GEAR DISAGREE AND NOSE DOORS MESSAGE ON EICAS, NLG REMAINED UP. COULD NOT DUPLICATE DI SCREPANCY. REPLACED THE NLG UPLOCK FOR TROUBLESHOOTING. 2 L 7 2 4F RT A21EA 1996051600192 19960516 00192 EA 1996 5 16 COMA9660085 1 19960512 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 EA RT COCKPIT BIRD STRIKE A COMA A UNSCHED LANDING C F.O.D. TO TAKEOFF 1 SO 01 956CA 7105 BIRD STRIKE ON COPILOTS WINDSHIELD, DURING TAKEOFF. BIRD STRIKE INSPECTION AND NO DAMAGE FOUND. 2 L 7 2 4F RT A21EA 1996051600193 19960516 00193 EA 1996 5 16 COMA9660086 1 19960511 A 5240 SERVICE DOOR CNDAIR CL600 CL6002B19 EA OXY COMPT OPENED IN FLIGHT A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 949CA 7080 OXYGEN SERVICE DOOR OPENED IN FLIGHT. INSPECTED AND FOUND NO DAMAGE OR DEFECTS WITH SERVICE DOOR. SECURED DOOR AND ACF T RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1996051600194 19960516 00194 EA 1996 5 16 COMA9660087 1 19960510 A 2910 AE2460010H0264 HYD HOSE CNDAIR CL600 CL6002B19 EA NR 1 HYD SYST LEAKING A COMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 929CA 7035 NR 1 HYDRAULIC SYSTEM CAUTION MESSAGE RECEIVED AFTER TAKEOFF. NR 1 HYDRAULIC SUPPLY LINE CHAFED AND LEAKING AT SUPPORT CLAMP. REPLACED LEAKING LINE. 2 L 7 2 4F RT A21EA 1996051600195 19960516 00195 WP 1996 5 16 MWEA96134 1 19960510 A 3350 60030431 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 302ME 47102 DURING SERVICE CHECK, FOUND EMERGENCY OVERHEAD LIGHTS IN TAIL COMPT INOP. REPLACED BATTERY POWER SUPPLY, OPS CHECK GOOD . 2 L 7 2 4F A6WE 1996051600196 19960516 00196 NM 1996 5 16 P5CA9600223 1 19960513 A 5610 60B100286 WINDSHIELD BOEING 747 747122 1384872 NM RT COCKPIT CRACKED A P5CA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 23 850FT 19755 FIRST OFFICER'S WINDSHIELD CRACKED ON TAXI OUT. REMOVED AND REPLACED WINDSHIELD IAW MM 56-11-01. 2 L 7 4 4F A20WE 1996051600197 19960516 00197 NE 1996 5 16 P5CA9600224 2 19960509 A 7321 7479944 FUEL CONTROL BOEING 747 747132 1384882 NM PWA JT9 JT9D7A 52054 NE NR 4 ENGINE INOPERATIVE A P5CA D E RETURN TO BLOCK ENGINE SHUTDOWN X J ENGINE FLAMEOUT WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 857FT 20246 662566 ON TAXI FOR DEPARTURE, NR 4 ENGINE FLAMED OUT. ACFT RETURNED TO GATE. REMOVED AND REPLACED FUEL CONTROL IAW MM 73-21-0 1. REMOVED AND REPLACED FUEL PUMP IAW MM 73-11-01. FUEL PUMP PART NR 705300, SERIAL NR 2027, TSI 2541. 2 L 7 4 4F 4 F A20WE E20EA 1996051600198 19960516 00198 NM 1996 5 16 SWAA960317 1 19960505 A 2130 CIRCUIT BREAKER BOEING 737 7375H4 138449D NM PRESS CONTL SYST TRIPPED A SWAA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 503SW 24180 AT 35,000 FT CABIN ALTITUDE BEGAN TO CLIMB AT 500 FPM TO 1800 FPM. AIRCRAFT INITIATED DESCENT AND CABIN PRESSURE STABIL IZED AT 12.000. AIRCRAFT CONTINUED AND LANDED AT STL WITHOUT INCIDENT. RESET PRESSURE CONTROL SYSTEM CIRCUIT BREAKER A ND OPERATION CHECKED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996051600199 19960516 00199 NM 1996 5 16 SWAA960318 1 19960502 A 2782 654465115 ACTUATOR BOEING 737 7372H4 138448C NM NR 6 LE FLAP FAILED A SWAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 07 20SW 21337 DURING CLIMBOUT, NUMBER 6 L/E SLAT WOULD NOT RETRACT. RECYCLED FLAPS, NO HELP. AIRCRAFT RETURNED TO ONT AND MADE AN UN EVENTFUL LANDING. REPLACED NR 6 SLAT ACTUATOR AND OPERATION CHECKED PER BOEING M/M. 2 L 7 2 4F A16WE 1996051600200 19960516 00200 NM 1996 5 16 SWAA960319 1 19960502 A 5320 CLIP BOEING 737 7372H4 138448C NM BS 908 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT THE FOLLOWING LOCATION: BS 908 S8L, AT BS 867 S20R, AT BS 663 .5 S20L AND S10R, AT BS 500A S1, AT BS 500B AND 520 S1, AND AT BS 727A S19R. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996051600201 19960516 00201 NM 1996 5 16 SWAA960320 1 19960502 A 5320 SPLICE BOEING 737 7372H4 138448C NM BS 908 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, S4L. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996051600202 19960516 00202 NM 1996 5 16 SWAA960321 1 19960502 A 5312 BLKHD WEB BOEING 737 7372H4 138448C NM BS 1016 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED D-CHECK, FOUND PRESSURE BULKHEAD WEB AND BULKHEAD STIFFENER DAMAGED AT BS 1016 TO 1020. REPAIRED PER B OEING SRM. 2 L 7 2 4F A16WE 1996051600203 19960516 00203 NM 1996 5 16 SWAA960322 1 19960502 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 957 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED D-CHECK, FOUND STRINGER CORRODED AT BS 957 RBL 5 WL 177.5. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996051600204 19960516 00204 NM 1996 5 16 SWAA960323 1 19960502 A 5315 FLOOR BEAM BOEING 737 7372H4 138448C NM BS 294/344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORROSION AT BS 294 LBL 12 LBL 7 BL 0 WL 208 AND AT BS 344 LBL 7 BL 0 RBL 1, 9 WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996051600205 19960516 00205 NM 1996 5 16 SWAA960324 1 19960502 A 5230 DOOR FRAME BOEING 737 7372H4 138448C NM FWD CARGO COMPT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT NR 5 STOP FITTING. INSTALLED REPAIR DOUBLER PER TRAMCO EWO 96-0105. 2 L 7 2 4F A16WE 1996051600206 19960516 00206 NM 1996 5 16 SWAA960325 1 19960502 A 5312 BLKHD WEB BOEING 737 7372H4 138448C NM BS 727 CHAFING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED D-CHECK, FOUND PRESSURE BULKHEAD WEB CHAFING DAMAGE AT BS 727 RBL 6 WL 164 UNDER FLAP DRIVE GEARBOX. I NSTALLED REPAIR PER TRAMCO EWO 96-0115. 2 L 7 2 4F A16WE 1996051600207 19960516 00207 NM 1996 5 16 SWAA960326 1 19960502 A 5320 STRAP BOEING 737 7372H4 138448C NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED D-CHECK, FOUND FLOOR TIE STRAP CORRODED AT BS 500 PLUS 4, LBL 24 WL 157. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996051600208 19960516 00208 NM 1996 5 16 SWAA960327 1 19960502 A 5320 CREASE BEAM BOEING 737 7372H4 138448C NM BS 637/639 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM INBOARD CHORD CRACKED AT BS 639 RBL 64 WL 208. ALSO, AT BS 637 RBL 70 WL 20 8. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996051600209 19960516 00209 NM 1996 5 16 SWAA960328 1 19960502 A 5320 WEB BOEING 737 7372H4 138448C NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AT BS 540 BL 0 TO LBL 25 WL 208. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996051600210 19960516 00210 NM 1996 5 16 SWAA960329 1 19960502 A 5320 SUPPORT BOEING 737 7372H4 138448C NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CRACKED AT BS 540 BL 0 TO LBL 25. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996051600211 19960516 00211 NM 1996 5 16 SWAA960330 1 19960502 A 5320 FLOOR SUPPORT BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CORROSION AT BS 280 TO 282, RBL 11 WL 208, AT BS 286 AND 291, LBL 11 WL 20 8, AT BS 314 LBL 11 WL 208, AT BS 276 RBL 11 WL 208 AND AT BS 296 LBL 11. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996051600212 19960516 00212 NM 1996 5 16 SWAA960331 1 19960502 A 5320 SHEAR TIE BOEING 737 7372H4 138448C NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN S13 AND 14L AND AT BS 1104, 1 INCH ABOVE S17R. REP AIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996051600213 19960516 00213 NM 1996 5 16 SWAA960332 1 19960502 A 5320 MOPSILL BOEING 737 7372H4 138448C NM BS 316/346 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED D-CHECK, FOUND MOPSILL CORRODED FROM BS 316 TO 346 LBL 55 WL 208. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996051600214 19960516 00214 NM 1996 5 16 SWAA960333 1 19960502 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 294 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 294 S4L. REPLACED FRAME SECTION PER BOEING SRM. 2 L 7 2 4F A16WE 1996051600215 19960516 00215 NM 1996 5 16 SWAA960334 1 19960502 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 301 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED D-CHECK, FOUND L-ANGLE CRACKED AT BS 301 S13L. REPLACED FRAME SECTION PER BOEING SRM. 2 L 7 2 4F A16WE 1996051600216 19960516 00216 NM 1996 5 16 SWAA960335 1 19960502 A 5320 FLOOR SUPPORT BOEING 737 7372H4 138448C NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CRACKED AT BS 540 BL 0 TO RBL 25 WL 208. REPLACED SUPPORT PER BOEING SRM. 2 L 7 2 4F A16WE 1996051600217 19960516 00217 NM 1996 5 16 SWAA960336 1 19960502 A 5320 STRAPS BOEING 737 7372H4 138448C NM BS 1138 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED D-CHECK, FOUND FUSELAGE VERTICAL AND HORZ STRAPS CRACKED AT BS 1138 ABOVE S12L. REPAIRED PER BOEING SR M. 2 L 7 2 4F A16WE 1996051600218 19960516 00218 NM 1996 5 16 SWAA960337 1 19960502 A 5320 CHORD BOEING 737 7372H4 138448C NM BS 1154-1156 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED D-CHECK, FOUND FUSELAGE LOWER CHORD CRACKED FROM BS 1154 TO 1156 S5L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996051600219 19960516 00219 NM 1996 5 16 SWAA960338 1 19960502 A 5320 ANGLES BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED D-CHECK, FOUND ANGLES CRACKED AT BS 294.5, RBL 55 WL 208 AND AT BS 328 RBL 33 WL 201, AT BS 290 RBL 59 WL 240 AND 248 AND AT BS 328 RBL 33 WL 201. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996051600220 19960516 00220 NM 1996 5 16 SWAA960339 1 19960502 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 523/967 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED D-CHECK, FOUND STRINGER CRACKED AT BS 523 S15R AND AT BS 967 S27L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996051600221 19960516 00221 NM 1996 5 16 SWAA960340 1 19960502 A 5320 WEB BOEING 737 7372H4 138448C NM BS 280 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AND A CHAFED SUPPORT AT BS 280, S5R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996051600222 19960516 00222 NM 1996 5 16 SWAA960341 1 19960502 A 5312 BLKHD WEB BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED D-CHECK, FOUND PRESSURE BULKHEAD WEB CRACKED AT BS 178 WL 277 AND AT RBL 11.7 WL 219. REPAIRED PER BOE ING SRM. 2 L 7 2 4F A16WE 1996051600223 19960516 00223 NM 1996 5 16 SWAA960342 1 19960502 A 5210 SKIN BOEING 737 7372H4 138448C NM AFT ENTRY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED D-CHECK, FOUND AFT ENTRY DOOR UPPER HINGE CUTOUT CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996051600224 19960516 00224 NM 1996 5 16 SWAA960343 1 19960502 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 328 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 328 WL 173. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996051600225 19960516 00225 NM 1996 5 16 SWAA960344 1 19960502 A 5320 CHORD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED D-CHECK, FOUND LT SIDE FUSELAGE CHORD CRACKED AT BS 178 WL 193.5 TO 196.5. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996051600226 19960516 00226 NM 1996 5 16 SWAA960345 1 19960502 A 3350 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED D-CHECK, FOUND FWD EMERGENCY LIGHT INOP. REPLACED LIGHT PER BOEING M/M. 2 L 7 2 4F A16WE 1996051600227 19960516 00227 NM 1996 5 16 SWAA960346 1 19960502 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CORRODED AT PRODUCTION SPLICE AT BS 1016 S27R WL 187. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996051600228 19960516 00228 NM 1996 5 16 SWAA960347 1 19960502 A 5320 CHANNEL BOEING 737 7372H4 138448C NM BS 1150 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED D-CHECK, FOUND V-CHANNEL CRACKED AT HORZ WEB LOWER SURFACE AT BS 1150 RBL 24 IN RT LOWER TORQUE BOX. R EPAIRED PER BOEING DRAWING 65-46585 AND SRM. 2 L 7 2 4F A16WE 1996051600229 19960516 00229 NM 1996 5 16 SWAA960348 1 19960502 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 977 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED D-CHECK, FOUND STRINGER 26R CORRODED AT BS 977. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996051600230 19960516 00230 NM 1996 5 16 SWAA960349 1 19960502 A 5320 CHORD BOEING 737 7372H4 138448C NM BS 927 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED D-CHECK, FOUND FAIL-SAFE CHORD CRACKED AT BS 927 S27R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996051600231 19960516 00231 NM 1996 5 16 SWAA960350 1 19960502 A 5240 SKIN BOEING 737 7372H4 138448C NM AFT GALLEY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 50SW 21447 DURING SCHEDULED B2 CHECK, FOUND AFT GALLEY DOOR UPPER HINGE CUTOUT CRACKED .125. REPAIRED PER BOEING TYPICAL REPAIR T1 -A52-005. 2 L 7 2 4F A16WE 1996051600232 19960516 00232 NM 1996 5 16 SWAA960351 1 19960507 A 5330 SKIN BOEING 737 7373A4 1384585 NM BS 298/315 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 298 BETWEEN S28R AND L AND AT BS 315 BETWEEN S28L AND R. REP AIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996051600233 19960516 00233 NM 1996 5 16 SWAA960352 1 19960507 A 5320 ANGLE BOEING 737 7373A4 1384585 NM BS 570 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED D-CHECK, FOUND SKATE ANGLE CRACKED AT BS 570 LBL 45 TO 48 WL 170. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996051600234 19960516 00234 NM 1996 5 16 SWAA960353 1 19960507 A 5330 SKIN BOEING 737 7373A4 1384585 NM BS 1075-1080 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED 3 PLACES AND GOUGED AT BS 1075 TO 1080, BETWEEN S18L AND 16L. REPA IRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996051600235 19960516 00235 NM 1996 5 16 SWAA960354 1 19960507 A 5330 SKIN BOEING 737 7373A4 1384585 NM BS 996 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED 3 PLACES AFT OF AFT ENTRY DOOR JUST BELOW LIGHT AT BS 996 LEFT SIDE S12. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996051600236 19960516 00236 NM 1996 5 16 SWAA960355 1 19960506 A 3350 FLASHLIGHT BOEING 737 7372H4 138448C NM FWD GALLEY INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 52SW 21533 AT GATE, FOUND EMERGENCY FLASHLIGHT IN FWD GALLEY INOP. REPLACED PER BOEING M/M. 2 L 7 2 4F A16WE 1996051600237 19960516 00237 NM 1996 5 16 SWAA960356 1 19960507 A 3350 P4010021 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 55SW 21593 AT GATE, FOUND ONE FWD EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY PER BOEING M/M. 2 L 7 2 4F A16WE 1996051600238 19960516 00238 NM 1996 5 16 SWAA960357 1 19960507 A 5320 CAP BOEING 737 7372H4 138448C NM AIRSTAIR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 27SW 21262 DURING SCHEDULED B-CHECK, FOUND AIRSTAIR DOORWAY FWD UPPER STOP ATTACH AFT T-CAP CRACKED. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996051600239 19960516 00239 NM 1996 5 16 SWAA960358 1 19960507 A 5230 DOOR FRAME BOEING 737 7373Y0 1384671 NM FWD CARGO COMPT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 682SW 23496 DURING SCHEDULED B/C1 CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT UPLOCK HOOK. REPAIRED PER TI NR T1-A52-003. 2 L 7 2 4F RT A16WE 1996051600240 19960516 00240 NM 1996 5 16 SWAA960359 1 19960507 A 5330 SKIN BOEING 737 7372K6 NM BS 727/800 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKS AT BS 800 S15R, AT BS 727B S17R AND AT BS 727B S16L. REPAIRE D PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996051600241 19960516 00241 NM 1996 5 16 SWAA960360 1 19960502 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 400, BELOW SKIN PATCH AND ABOVE S18L. ALSO, AT BS 1002 S22R, AT BS 250 BETWEEN S21 AND 22R, AT BS 1001 S15 TO 16R, AT BS 1056, 13 INCHES BELOW APU INLET CUTOUT AND AT BS 926, 2 INC HES ABOVE S23R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996051600242 19960516 00242 NM 1996 5 16 SWAA960361 1 19960503 A 3350 20131A BATTERY PACK BOEING 737 7375H4 138449D NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 510SW 24187 DURING SCHEDULED A1 CHECK, FOUND AFT DOOR SLIDE LIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996051600243 19960516 00243 NM 1996 5 16 UPS96420100 1 19960402 A 5330 SKIN BOEING 747 747123 1384873 NM BS 2360 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE 'C', FOUND CORROSION AT BS 2360 AFT PRESSURE SKIN PLATES AND Y-CHORD BETWEEN STR 46R AND STR 46L. REPLA CED AFT PRESSURE WEB SEGMENT, PARTLY REPLACED Y-CHORD BETWEEN LBL 44 TO RBL 55. INSTALLED FASTENERS IAW SRM 51-30-02, A PPR EFN 747-53-0760. 2 L 7 4 4F A20WE 1996051600244 19960516 00244 NM 1996 5 16 UPS96420101 1 19960501 A 5312 BLKHD WEB BOEING 747 747123 1384873 NM BS 2360 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE 'C', FOUND ON WEB EDGE FASTENER SEM AT LT AT STR 38L WL 225 AT BS 2360 REAR PRESS BULK. REPAIRED DAMAGE IAW SRM 51-10-04 FIG 86 BOEING TELEX UPS-AMS-96-012 3RE APP DOC DFX 96-104, EFN 747-0761. 2 L 7 4 4F A20WE 1996051600245 19960516 00245 NM 1996 5 16 UPS96520102 1 19960511 A 7930 215N04404 PRESSURE SWITCH BOEING 757 75724APF 1384969 NM LT ENGINE INTERMITTENT A IPXA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 409UP 23731 INSPECTION, INFLIGHT SHUTDOWN OF LT ENGINE DUE TO EICAS MESSAGE LT ENG OIL FILTER, ALL OTHER ENG INDICATION NORMAL. C/W F/M 79-21-00 FIG 104 REMOVED MAIN ENG OIL FILTER AND CHECKED ALL MAGNETIC CHIP DET, NO CONTAMINATION FOUND ON DETECTORS . INSTALLED NEW FILTER PER MM 79-21-05. REMOVED AND REPLACED LT ENG DIFF PRESSURE SWITCH PER MM 79-35-01. RAN ENG, NO LEAKS OR MESSAGES. 2 L 7 2 4F RT A2NM 1996051600246 19960516 00246 WP 1996 5 16 UPS96820090 1 19960510 A 5730 SKIN DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE 'B', CRACK PROTRUDING FROM RIVET HEAD OUTBOARD AND FWD PANEL 523, FIRE BOTTLE ACCESS MARKED. REMOVED CR ACKED AREA OF THE SKIN. INSTALLED FILLER AND DOUBLER PER SRM 57-2-1. 2 L 7 4 4F RT 4A25 1996051600247 19960516 00247 WP 1996 5 16 UPS96820091 1 19960510 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE BELLY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE 'B', 3 CRACKS IN SKIN PROTRUDING FROM RIVETS IN BELLY SKIN 3 INCHES AFT OF LT AFT NOSE WHEEL WELL DOOR. INSTALLED DOUBLER PER SRM 53-2-1. 2 L 7 4 4F RT 4A25 1996051600248 19960516 00248 WP 1996 5 16 UPS96820092 1 19960501 A 5313 5750198 LONGERON DOUG DC8 DC871F 302199D WP FS 882 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE 'B', CRACK BEYOND STOP DRILL .5 INCH LONG AT LONGERON 24R FS 882. REPAIRED PER SRM 53-2-2. 2 L 7 4 4F RT 4A25 1996051600249 19960516 00249 WP 1996 5 16 UPS96820093 1 19960430 A 5320 37558272N FITTING DOUG DC8 DC871F 302199D WP FS 1200 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE 'B', B/T FITTING CRACKED AT FS 1200 LONGERON 33R TO 34R FWD SIDE. REPLACED FITTING PER SRM 53-2-0. 2 L 7 4 4F RT 4A25 1996051600250 19960516 00250 WP 1996 5 16 UPS96820094 1 19960430 A 5320 37558541 FITTING DOUG DC8 DC871F 302199D WP FS 1200 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE 'B', B/T FITTING CRACKED AT FS 1200 LONGERON 28L AFT SIDE. REPLACED FITTING PER SRM 53-2-0. 2 L 7 4 4F RT 4A25 1996051600251 19960516 00251 WP 1996 5 16 UPS96820095 1 19960419 A 5320 36410042N FITTING DOUG DC8 DC873F 302199F WP FS 878 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE 'B', VERTICAL FITTING ABOVE LONGERON 24R CRACKED FS 878. REPLACED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996051600252 19960516 00252 WP 1996 5 16 UPS96820096 1 19960423 A 5320 WEB DOUG DC8 DC873F 302199F WP FS 790 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE 'B', WEB CRACKED AT FS 790 XLW LONGERON 23R. REPLACED WEB PER SRM 53-2-0. 2 L 7 4 4F RT 4A25 1996051600253 19960516 00253 WP 1996 5 16 UPS96820097 1 19960422 A 5320 46198102 FITTING DOUG DC8 DC873F 302199F WP FS 940 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE 'B', T-ANGLE SUPPORT FITTING CRACKED AT FS 940 LONGERON 24R. REPLACED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996051600254 19960516 00254 WP 1996 5 16 UPS96820098 1 19960419 A 5320 37797021 FITTING DOUG DC8 DC873F 302199F WP FS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE 'B', FITTING CRACKED AT LONGERON 21R AFT SIDE OF FS 680. REPLACED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996051600255 19960516 00255 WP 1996 5 16 UPS96820099 1 19960420 A 5755 56551671 SKIN DOUG DC8 DC873F 302199F WP NR 3 SPOILER DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE 'B', NR 3 SPOILER LT WING DELAMINATION ON BOTTOM SIDE. REPLACED SPOILER PNL PER MM 27-61-01. 2 L 7 4 4F RT 4A25 1996051600261 19960516 00261 CE 1996 5 16 96ZZZX2393 1 19960221 A 2720 0411307 ARM CESSNA 206 U206G 2073356 CE LT RUDDER CORRODED A ERHA K NONE O OTHER IN INSP/MAINT 1 AL 03 4891Z 4700 20606044 WHEN REMOVING LT RUDDER PEDAL AND ARM ASSYS TO ACCESS FIREWALL INSIDE OF RUDDER ARM, TUBE WAS FOUND BADLY CORRODED. THE RE WAS NO EVIDENCE OF CORROSION ON OUTSIDE OF TUBE. THE TUBE IS MOUNTED VERTICALLY AND IS OPEN ON TOP AND SEALED ON BOT TOM. ANY WATER THAT ENTERS TUBE IS TRAPPED. WATER PROBABLY CAME FROM PILOT'S BOOTS DURING SEAPLANE OPERATIONS AND MAY HAVE BEEN SALTWATER. SUBMITTER RECOMMENDS SEALING UPPER END OF TUBE TO PREVENT WATER ENTRY. 1 H 7 1 3O A4CE 1996051600266 19960516 00266 SO 1996 5 16 96ZZZX2398 1 19960318 A 3260 31285000 BRACKET PIPER PA23 PA23250 7102308 SO NLG SWITCH WORN A CFCA K NONE O OTHER IN INSP/MAINT 1 GL 03 54757 277554068 THE SUPPORT BRACKET FOR THE NOSE GEAR DOWNLOCK SWITCH WAS WORN ALLOWING POOR CONTACT OF SWITCH. SUBMITTER RECOMMENDS A 5,000-HOUR INSPECTION OR REPLACEMENT. 1 L 7 2 3O 1A10 1996051600271 19960516 00271 SO 1996 5 16 96ZZZX2403 1 19960229 A 3260 487862 SWITCH PIPER PA31 PA31350 7103110 SO RT MLG REQUIRED ADJ A BIAA O OTHER P NO WARNING INDICATION AP APPROACH 1 WP 13 683ML 317552124 KOA - ON APPROACH, RIGHT MAIN LANDING GEAR WOULD NOT ILLUMINATE 'SAFE'. CREW PERFORMED EMERGENCY GEAR PROCEDURES AND AI RCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL ADJUSTED DOWNLOCK MICROSWITCH, AND PERFORMED OPERATIONAL CHECK WITH NO FURTHER DEFECTS. DATE 2-29-96, STA KOA. SUBMITTER STATED TO ENSURE DETAILED INSPECTION PERFORMED DURING SCHEDULED MAINTENANCE. 1 L 7 2 3O A20SO 1996051600285 19960516 00285 CE 1996 5 16 96ZZZX2417 1 19960330 A 5312 12121315 BULKHEAD CESSNA 210 T210N 2073456 CE STAB ATTACH CRACKED A GONA K NONE O OTHER IN INSP/MAINT 1 SW 01 6185N 2292 21062956 ON INSTALLATION OF HORIZONTAL STABILIZER ATTACH BULKHEAD MOD PER SB SEB 88-3, DYE PENETRANT INSPECTION OF BULKHEAD REVEA LED SEVERAL CRACKS AROUND THE TOP RIVET HOLE UNDER THE LT DOUBLER, .3125 INCH LONG, AND VISIBLE BEYOND DOUBLER ON RT FOR E AND AFT DOUBLERS. TOP RIVET HAD SHEARED AND DOUBLERS WERE PULLING AWAY FROM BULKHEAD. 1 H 7 1 3O 3A21 1996051600286 19960516 00286 CE 1996 5 16 96ZZZX2418 1 19960330 A 5511 12326212 SPAR CESSNA 210 T210N 2073456 CE LT ATTACH BRKT CRACKED A GONA K NONE O OTHER IN INSP/MAINT 1 SW 01 6185N 2292 21062956 DURING REPLACEMENT OF HORIZONTAL STABILIZER REAR ATTACH BRACKET WITH NEW IMPROVED BRACKET PN 1232624-1 IAW SE84-17, DYE PENETRANT INSPECTION REVEALED A .75 INCH CRACK UNDER LEFT REAR ATTACH BRACKET AT OUTBOARD BOLT HOLE, IN RADIUS OF SPAR F LANGE. REPAIRED SPAR WITH DOUBLER. THIS SUBMITTER HAS REPAIRED 8 AIRCRAFT WITH CRACKED BRACKETS. IF THE BRACKETS ARE REPLACED AT THE FIRST SIGN OF CRACKING, THE SPAR WILL PROBABLY BE OK. IF BRACKETS ARE KEPT IN SERVICE UNTIL CRACKING IS SEVERE, THEN SPARS WILL LIKELY BE CRACKED ALSO. 1 H 7 1 3O 3A21 1996051600306 19960516 00306 WP 1996 5 16 9610449929 1 19960512 A 3150 T/O WARNING DOUG DC9 DC931 3022065 WP COCKPIT SOUNDED A NWAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 01 8923E 45838 TAKEOFF WARNING HORN SOUNDED DURING TAKEOFF ROLL AT 30 KNOTS. ABORTED TAKEOFF AND RETURNED TO GATE. HORN WAS SILENCED AFTER SPOILERS WERE CYCLED. MAINTENANCE PERFORMED TAKEOFF WARNING SYSTEM TEST PER MAINTENANCE MANUAL 27-00, CODE 4, PG 215, SYSTEM CHECKED NORMAL. DISCREPANCY COULD NOT BE DUPLICATED. 2 L 7 2 4F A6WE 1996051600307 19960516 00307 1996 5 16 9610459989 4 19960510 A 2565 113317 EVAC SLIDE DOUG DC9 DC931 3022065 WP FWD SERVICE DOOR FAILED TEST A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8945E 43992 1724 47181 DURING PERIODIC CHECK, FORWARD SERVICE DOOR EVACUATION SLIDE FAILED BATTERY TEST. REPLACED SLIDE. 2 L 7 2 4F A6WE 1996051600308 19960516 00308 NM 1996 5 16 9610466608 1 19960514 A 2610 FIRE LOOP-B BOEING 747 747151 1384891 NM APU MALFUNCTIONED A NWAA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 01 608US 19785 WHILE TAXIING, THE APU FIRE WARNING ACTIVATED AND THE APU FIRE BOTTLE WAS DISCHARGED. AIRCRAFT RETURNED TO THE GATE. F OUND B-LOOP FIRE WARNING SYSTEM INOPERATIVE, SYSTEM ON DEFERRAL. 2 L 7 4 4F A20WE 1996051600309 19960516 00309 WP 1996 5 16 9610479885 1 19960510 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 401EA 47682 DURING LINE CHECK, FOUND ONE SECTION OF FLOOR PATH ESCAPE LIGHTING INOPERATIVE. REPLACED BATTERY PACK AND POWER SUPPLY, OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996051600310 19960516 00310 WP 1996 5 16 9610489884 1 19960510 A 3350 SOCKET DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 677MC 47756 DURING LINE CHECK, FOUND FLOOR PROXIMITY LIGHTS INOPERATIVE. REPLACED LIGHT SOCKET, OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996051600311 19960516 00311 WP 1996 5 16 9610499863 1 19960510 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 772NC 47774 DURING LINE CHECK, FOUND FORWARD OVERWING EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED BATTERY PACK AND ONE POWER SUPPLY, OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996051600312 19960516 00312 WP 1996 5 16 9610509863 1 19960510 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP TAIL CONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 772NC 47774 DURING LINE CHECK, FOUND ALL EMERGENCY LIGHTS IN TAIL CONE AREA EXCEPT DISCO LIGHTS INOPERATIVE. REPLACED BOTH BATTERY PACK AND POWER SUPPLIES, OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996051600313 19960516 00313 WP 1996 5 16 9610519140 1 19960513 A 3350 BATTERY PACK DOUG DC9 DC914 3022034 WP TAIL CONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 930RC 45729 DURING LINE CHECK, FOUND INTERIOR TAIL CONE EMERGENCY SLIDE LIGHTS AND NACELLE LIGHTS INOPERATIVE. REPLACED BATTERY PAC KS IN POWER SUPPLIES B5-49 AND B5-50, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996051600314 19960516 00314 WP 1996 5 16 9610529140 1 19960510 A 3350 BATTERY PACK DOUG DC9 DC914 3022034 WP LT/RT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 930RC 45729 DURING LINE CHECK, FOUND LEFT AND RIGHT NACELLE EMERGENCY LIGHTS OUT. REPLACED BATTERY PACK, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996051600315 19960516 00315 WP 1996 5 16 9610539921 1 19960513 A 3350 60030451 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 943N 47647 DURING LINE MAINTENANCE INSPECTION, FOUND AFT TAIL COMPARTMENT AND VENTRAL STAIR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996051600316 19960516 00316 WP 1996 5 16 9610549933 1 19960513 A 7603 LINKAGE DOUG DC9 DC931 3022065 WP LEFT ENGINE LACK OF LUBE A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 1334U 47280 LEFT THROTTLE WAS STICKING WHEN POWER WAS PULLED BACK AT TOP OF CLIMB. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDE NT. MAINTENANCE CLEANED AND LUBED PUSH/PULL LINKAGE ON LEFT ENGINE, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996051600317 19960516 00317 WP 1996 5 16 9610559610 1 19960513 A 3260 DOOR SWITCH DOUG DC9 DC932 3022066 WP LT/RT MLG MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 610NW 47432 DURING CLIMBOUT, LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. FLIGHT DIVERTED TO LGA AND LANDED W ITHOUT INCIDENT. LIGHT REMAINED ON AFTER GEAR EXTENSION, GEAR WAS VISUALLY CONFIRMED THROUGH PERISCOPE TO BE DOWN AND L OCKED. MAINTENANCE REPLACED RIGHT AND LEFT MAIN GEAR DOOR SWITCHES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996051600318 19960516 00318 EU 1996 5 16 9610563239 1 19960511 A 3610 COMPUTER AIRBUS 320 A320211 3930320 EU NR 1 ENGINE FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 339NW 367 DURING CLIMBOUT AT 25,000 FEET, RECEIVED ENG 1 BLEED FAULT FOLLOWED BY ENG 2 BLEED FAULT. THE AIRCRAFT BEGAN TO DEPRESS URIZE, FOLLOWED ECAM PROCEDURES AND NR 1 ENGINE BLEED RESET SUCCESSFUL AND AIRCRAFT PRESSURIZED. DECISION WAS MADE TO D IVERT TO MSP WHERE AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE REPLACED THE NR 1 BLEED MONITOR COMPUTER, NR 2 E NGINE OVERPRESSURE PNEUMATIC VALVE AND TRANSDUCERS 7HA2 AND 8HA2, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996051600319 19960516 00319 EU 1996 5 16 9610573214 1 19960513 A 3230 INTERFACE UNIT AIRBUS 320 A320211 3930320 EU LANDING GEAR MALFUNCTIONED A NWAA O OTHER O OTHER CL CLIMB 1 GL 01 314US 160 DURING CLIMBOUT AFTER PLACING THE LANDING GEAR HANDLE IN THE UP POSITION, ALL GEAR REMAINED EXTENDED. CYCLED LANDING GE AR HANDLE AND ALL INDICATIONS WERE NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 LANDING GEA R CONTROL INTERFACE UNIT, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996051600320 19960516 00320 EU 1996 5 16 9610583214 1 19960513 A 3230 114079015 SELECTOR VALVE AIRBUS 320 A320211 3930320 EU MLG WW MALFUNCTIONED A NWAA O OTHER O OTHER CL CLIMB 1 GL 01 314US 160 DURING CLIMBOUT AFTER PLACING THE LANDING GEAR HANDLE IN THE UP POSITION, THE LANDING GEAR DID NOT RETRACT WHILE THE GEA R DOORS INDICATED OPEN. CYCLED LANDING GEAR HANDLE AND ALL INDICATIONS WERE NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 LANDING GEAR CONTROL INTERFACE UNIT AND THE LANDING GEAR SELECTOR VALVE, OPERATIONAL CHEC K OK. 2 L 7 2 4F RT A28NM 1996051600321 19960516 00321 WP 1996 5 16 96DHL802003 1 19960510 A 8011 8901180 STARTER SHAFT FB65310A DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C1 13802 NE NR 4 ENGINE SHEARED A T DHLA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 SO 01 802DH FB66125 46076 693490 NR 4 ENGINE FLAMED OUT AT FL 350, ENGINE WOULD NOT RESTART. TROUBLESHOT ENGINE PER M/M FOUND STARTER SHAFT SHEARED. RE MOVED AND REPLACED STARTER PER M/M 80-10-00, AS PRECAUTION. REMOVED AND REPLACED CIT SENSOR AND NASH PUMP PER THE M/M. RAN ENGINE, ALL PARAMETERS CHECK OK. 2 L 7 4 4F 4 F RT 4A25 E2GL 1996051600322 19960516 00322 NM 1996 5 16 96FDEA00955 1 19960513 A 5311 FRAME BOEING 727 727227 1384078 NM BS 520 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 DENTS IN FRAME AT BS 520 LBL 32 WL 160. CUT OUT DAMAGE AND REPAIRED FRAME AT BS 520 LBL 32 WL 160 PER FEDEX SRM 51-40-3 . 2 L 7 3 4F A3WE 1996051600323 19960516 00323 NM 1996 5 16 96FDEA00956 1 19960511 A 5754 65162268A FLAP BOEING 727 727225 1384077 NM NR 5 LE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 468FE 21452 CORROSION UNDER NR 5 K-FLAP O/B LOWER BONDING JUMPER UPPER ATTACH POINT WENT BEYOND LIMITS. REMOVED DAMAGED SECTION, FA BRICATED AND INSTALLED REPAIR PER FEDEX SRM 57-50-3. 2 L 7 3 4F A3WE 1996051600324 19960516 00324 NM 1996 5 16 96FDEA00957 1 19960513 A 5320 CLIP BOEING 727 727225 1384077 NM BS 580 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 468FE 21452 CRACKED STRINGER CLIP BS 580 STR 27L. REMOVED CLIP, FABRICATED NEW CLIP AND INSTALLED. 2 L 7 3 4F A3WE 1996051600325 19960516 00325 NM 1996 5 16 96FDEA00958 1 19960513 A 5330 SKIN BOEING 727 727225 1384077 NM BS 490 CANNED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 468FE 21452 SKIN IS OIL CANNED AT BS 490 BETWEEN STR 20 TO 21R RBL 65. DAMAGED AREA CUT OUT, FABRICATED DOUBLER FROM 2024 T-3.063, INSTALLED REPAIR PARTS PER FEDEX SRM 53-30-3 FIG 1. 2 L 7 3 4F A3WE 1996051600326 19960516 00326 NM 1996 5 16 96FDEA00959 1 19960513 A 5320 CLIP BOEING 727 727225 1384077 NM BS 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 468FE 21452 CRACKED STRINGER CLIP AT BS 600 STR 27L. REMOVED CLIP, FABRICATED NEW CLIP AND INSTALLED. 2 L 7 3 4F A3WE 1996051600327 19960516 00327 NM 1996 5 16 96FDEA00960 1 19960513 A 5320 WEB BOEING 727 727225 1384077 NM BS 1120-1125 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 468FE 21452 WEB IS DAMAGED FROM BS 1120 TO 1125 BL 0 WL 201. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS ON WEB AT BS 112 0 TO 1125 BL 0 WL 201 PER FEDEX SRM 51-40-2. 2 L 7 3 4F A3WE 1996051600328 19960516 00328 NM 1996 5 16 96FDEA00961 1 19960512 A 5320 WEB BOEING 727 727225 1384077 NM BS 1241 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 468FE 21452 PUNCTURE/CRACK IN TORQUE BOX WEB BS 1241 RBL 20 WL 178. REPAIRED DAMAGE IN TORQUE BOX WEB AT BS 1241 RBL 208 PER FEDEX SRM 51-40-2. 2 L 7 3 4F A3WE 1996051600329 19960516 00329 NM 1996 5 16 96FDEA00962 1 19960513 A 5311 FRAME BOEING 727 727227 1384078 NM BS 660 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 FOUND DENT IN FRAME BS 660 BETWEEN STR 22 TO 23R. CUT OUT DAMAGE AND REPAIRED FRAME AT BS 660 BETWEEN STR 22 TO 23R PE R FEDEX SRM 51-40-3. 2 L 7 3 4F A3WE 1996051600330 19960516 00330 NM 1996 5 16 96FDEA00963 1 19960513 A 5330 SKIN BOEING 727 727227 1384078 NM BS 1120 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 DENT IN SKIN BS 1120 BETWEEN STR 28 TO 29L. REPAIRED SKIN PER FEDEX SRM 53-30-3. 2 L 7 3 4F A3WE 1996051600331 19960516 00331 NM 1996 5 16 96FDEA00964 1 19960513 A 5311 FRAME BOEING 727 727227 1384078 NM BS 660 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 FOUND DENT IN FRAME STA 660 LT BETWEEN STR 22 TO 23L, FWD BAY. CUT OUT DAMAGE AND REPAIRED FRAME AT BS 660 BETWEEN STR 22 TO 23L PER FEDEX SRM 51-40-3. 2 L 7 3 4F A3WE 1996051600332 19960516 00332 NM 1996 5 16 96FDEA00965 1 19960513 A 5311 FRAME BOEING 727 727227 1384078 NM BS 680 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 FOUND DENT IN FRAME STA 680 LT BETWEEN STR 23 TO 4L, FWD BAY. CUT OUT DAMAGE AND REPAIRED FRAME AT BS 680 BETWEEN STR 2 3 TO 24L PER FEDEX SRM 51-40-3. 2 L 7 3 4F A3WE 1996051600333 19960516 00333 NM 1996 5 16 96FDEA00966 1 19960513 A 5313 BAC15061133 STRINGER BOEING 727 72725 1384006 NM BS 849 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 505FE 18276 CRACK IN THE HORIZONTAL FLANGE OF STR 17R AND BS 849. CUT OUT DAMAGED AREA, FABRICATED FILLER, DOUBLER ANGLES, RADIUS F ILLERS, DRILLED UP REPAIR PARTS, ALODINED AND PRIMED AND INSTALLED WET WITH SEAL PER FEDEX SRM 51-40-4. 2 L 7 3 4F A3WE 1996051600334 19960516 00334 NM 1996 5 16 96FDEA00967 1 19960513 A 5320 BAC1505199360 SUPPORT BOEING 727 72725 1384006 NM BS 351 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 505FE 18276 CORROSION (C53-100-01) ON TOP AND BOTTOM FLANGES OF FAIRING SUPPORT CHORD BS 351 LBL TO RBL 17 WL 145 AT VARIOUS LOCATIO NS. REMOVED FAIRING SUPPORT CHORD BS 351 LBL TO RBL 17 WL 145 AND REPLACED WITH NEW CHORD PER FEDEX SRM 51-30-2. 2 L 7 3 4F A3WE 1996051600335 19960516 00335 WP 1996 5 16 96FDEA00968 1 19960507 A 5400 BOLT DOUG DC10 DC1030 3023501 WP NR 1 PYLON SHEAR OFF A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 304FE 46992 DURING ACCOMPLISHMENT OF EO 8-5410-7-3321 PART 1, FOUND FLATHEAD BOLT SHEAR OFF ON NR 1 PYLON AFT SUPPORT BULKHEAD. 2 L 7 3 4F A22WE 1996051600336 19960516 00336 NM 1996 5 16 96FDEA00969 1 19960513 A 5320 651864002 CHORD BOEING 727 72725 1384006 NM BS 740 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 505FE 18276 NR0316 AND 024, CORROSION (C53-224-05) ON THE BS 740 LWR CHORD RBL 15 TO 20 ON VERTICAL FLANGE. *S/D* REMOVED LOWER CH ORD, CORROSION WAS OUT OF LIMITS, LOCATED NEW LOWER CHORD, DRILLED, FABRICATED SPLICES, TREATED AND INSTALLED ALL PARTS IAW FEDEX EA 7-5710-28401. 2 L 7 3 4F A3WE 1996051600337 19960516 00337 NM 1996 5 16 96FDEA00970 1 19960513 A 5513 77TA176XEAL70 SKIN BOEING 727 72725 1384006 NM RT ELEV TAB DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 505FE 18276 NR0402 AND 022, RT ELEVATOR TAB T/E O/B CORNER IS DELAMINATED. *S/D* REPAIRED RT ELEVATOR TAB IAW FEDEX SRM 51-40-06 A ND 51-80-09. 2 L 7 3 4F A3WE 1996051600338 19960516 00338 NM 1996 5 16 96UAL900335 1 19960510 A 2540 TRASH BIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LAVATORY FIRE A UALA F ACTIVATE FIRE EXT. A P FLAME/FIRE NO WARNING INDICATION CR CRUISE 1 WP 29 774UA 26936 REPORT OF SMOKE IN LAVATORY AT DOOR 4 RIGHT SIDE. ADDITIONAL, REPORT OF FIRE IN LAVATORY TRASH BIN. ALARM DID NOT SOUN D. WASTE COMPARTMENT EXTINGUISHER DID NOT DISCHARGE. 2 L 7 2 4F 4 F RT T0001SE E46NE 1996051600339 19960516 00339 WP 1996 5 16 96UAL900336 1 19960510 A 3350 LIGHT STRIP DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1838U 46632 LEFT SIDE FIRST CLASS EEL LIGHTS INOPERATIVE. REPAIRED LIGHT STRIP, LIGHTING CHECKS OK. 2 L 7 3 4F 4 F A22WE E23EA 1996051600340 19960516 00340 NM 1996 5 16 96UAL900337 1 19960513 A 3350 LIGHT STRIP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 520UA 24890 EMERGENCY ESCAPE LIGHTING INOP ROWS 24A THROUGH 31A. REPLACED DEFECTIVE LIGHT STRIP, OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996051600341 19960516 00341 NM 1996 5 16 96UAL900339 1 19960513 A 3230 DOWNLOCK PIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NLG NOT REMOVED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 775UA 26947 NOSE GEAR DOOR WOULD NOT CLOSE WITH GEAR UP, AN EICAS MESSAGE INDICATED NOSE GEAR DISAGREEMENT. *S/D* DISCREPANCY WAS CAUSED BY THE NOSE GEAR DOWNLOCK PIN BEING LEFT IN PLACE. THE PROBLEM WAS CORRECTED BY REMOVING THE DOWNLOCK PIN. 2 L 7 2 4F 4 F RT T0001SE E46NE 1996051600342 19960516 00342 NM 1996 5 16 96UAL900340 1 19960513 A 2910 LINE BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE A-HYD SYST LEAKING A UALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 WP 29 9003U 19041 CREW REPORTS LOSS OF A-SYSTEM HYDRAULIC FLUID WHEN GEAR LOWERED ON APPROACH. DECLARED AN AMBER ALERT. *S/D* FOUND HYD RAULIC LINE TO A-SYSTEM LEAKING. INSTALLED NEW LINE, CHECKS OK. 2 L 7 2 4F 4 F A16WE E2EA 1996051600344 19960516 00344 WP 1996 5 16 96UAL900342 1 19960513 A 3350 BATTERY PACK DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1810U 46609 FLOOR EMERGENCY EXIT LIGHTS DAMAGED. REPLACED BATTERY PACK, U17100. 2 L 7 3 4F 4 F A22WE E23EA 1996051600345 19960516 00345 NM 1996 5 16 96UAL900343 1 19960513 A 3233 69191222 CHANNEL BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NLG ACTUATOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7466U 21920 NOSE LANDING GEAR LOCK ACTUATOR SUPPORT CHANNEL HAS A CRACK IN SIDE PLATE AT UPPER RIGHT BOLT HOLE. *S/D* CRACKED CHAN NEL REPLACED PER UA 727 MM53-40-01. 2 L 7 3 4F 4 F A3WE E2EA 1996051600346 19960516 00346 WP 1996 5 16 ABXA9600491 1 19960509 A 3231 59151695514 UPLATCH DOUG DC9 DC933F 302207A WP MLG DOORS LACK OF LUBE A ABXA O OTHER J WARNING INDICATION AP APPROACH 1 GL 23 933AX 47291 GEAR DOOR OPEN LIGHT STAYED ON AFTER LOWERING GEAR. WE RECYCLED GEAR AND LIGHT WENT OUT AFTER THE GEAR HAD BEEN DOWN FO R APPROXIMATELY 30 SECONDS. CLEANED AND LUBED MAIN LANDING GEAR DOOR UPLATCH HOOKS AND ROLLERS. OPERATIONAL CHECKED TH E GEAR DOOR UNSAFE SWITCHES AND GEAR DOORS IAW DC-9 MM. 2 L 7 2 4F A6WE 1996051600347 19960516 00347 WP 1996 5 16 ABXA9600492 1 19960510 A 3260 DS07S059 CONNECTOR DOUG DC9 DC932 3022066 WP NLG CONTAMINATED A ABXA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 23 986AX 47543 ON GEAR EXTENSION NOSE GREEN LIGHT DID NOT ILLUMINATE, ALL OTHER RED AND MAIN GREENS NORMAL. RECYCLED AND LIGHTS NORMAL . CLEANED WATER FROM NOSE GEAR DOWNLOCK SWITCH CANNON PLUG. NOSE DOWNLOCK GREEN LIGHT INDICATION NORMAL IAW DC-9 SUPP MM. 2 L 7 2 4F A6WE 1996051600348 19960516 00348 SO 1996 5 16 COMA9610143 1 19960511 A 3030 GEB240175 CURRENT SENSOR EMB 120 EMB120RT SO NR 2 PITOT HEAT FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 246CA 120223 NR 2 PITOT STATIC HEAT INOP WARNING ON. REPLACED THE NR 2 PITOT STATIC HEAT CURRENT SENSOR. 2 L 7 2 4T RT A31SO 1996051600349 19960516 00349 EA 1996 5 16 COMA9660088 1 19960509 A 2750 RETRACT MECH CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 914CA 7012 FLAPS FAILED WHEN SELECTED FOR LANDING. COULD NOT DUPLICATE DISCREPANCY. FLAP SYSTEM OPERATIONAL CHECK SATISFACTORY. 2 L 7 2 4F RT A21EA 1996051600350 19960516 00350 EA 1996 5 16 COMA9660089 1 19960512 A 3040 WINDSHIELD HEAT CNDAIR CL600 CL6002B19 EA LT COCKPIT MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 924CA 7026 LEFT WINDSHIELD HEAT CAUTION MESSAGE ON EICAS. SWITCHED WINDOW WIRING TO THE SPARE THERMISTOR. SYSTEM CHECK SATISFACTO RY AND ACFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1996051600351 19960516 00351 WP 1996 5 16 MWEA96135 1 19960511 A 5230 BEAM DOUG DC9 DC932 3022066 WP AFT CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 DURING CARGO DOOR INSPECTION, FOUND AFT CARGO DOOR NR 5 HORIZONTAL BEAM CRACKED NEAR AFT END AT PAN CUTOUT, RADIUS 1 .06 25 INCH IN LENGTH. INSTALLED DOUBLER REPAIR IAW DAC TELEX SVC-ORD-0048/JMP. 2 L 7 2 4F A6WE 1996051600352 19960516 00352 WP 1996 5 16 MWEA96136 1 19960511 A 5230 FORMER DOUG DC9 DC932 3022066 WP FWD CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 DURING CARGO DOOR INSPECTION, FOUND FWD CARGO DOOR FORMER CRACKED IN RADIUS BELOW NR 1 BEAM ABOVE AFT LOWER DOOR STOP. I NSTALLED REPAIR IAW SRM 52-01 FIG 2 SHT 4. 2 L 7 2 4F A6WE 1996051600353 19960516 00353 WP 1996 5 16 MWEA96137 1 19960511 A 5230 ANGLE DOUG DC9 DC932 3022066 WP FWD CARGO DOOR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 DURING CARGO DOOR INSPECTION, FOUND FWD CARGO DOOR LOWER AFT INTERNAL ANGLE HAS 1 INCH AREA OF HEAVY CORROSION. SPLICED IN SECTION OF ANGLE IAW SRM 52-01 FIG 2 SHT 4. 2 L 7 2 4F A6WE 1996051600354 19960516 00354 NM 1996 5 16 SCNA96111 1 19960510 A 5320 ANGLE BOEING 727 7272J4 1384006 NM BS 351 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 288SC 20765 DURING HEAVY MAINTENANCE VISIT, LEVEL 2 CORROSION WAS FOUND ON AFT UPPER ATTACH ANGLE AT BS 351.2 RBL 24. REMOVED CORRO DED ANGLE, FABRICATED AND INSTALLED NEW ANGLE, SPLICE, AND SHIMS IN ACCORDANCE WITH B727 SRM 51-40-4 FIGURE 2. 2 L 7 3 4F RT A3WE 1996051600355 19960516 00355 NM 1996 5 16 SCNA96112 1 19960426 A 5315 FLOOR BEAM BOEING 727 727225 1384077 NM BS 740 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING HEAVY MAINTENANCE VISIT, A CRACK WAS FOUND IN THE FLOOR BEAM WEB AT BS 740 BL 0. FABRICATED AND INSTALLED A WEB REPAIR IAW B727 SRM 51-40-2. 2 L 7 3 4F A3WE 1996051600356 19960516 00356 EU 1996 5 16 WWMA9600046 1 19960513 A 2150 5419C000 COOLING TURBINE BAG JETSTM JETSTM3201 1500217 EU LEFT OVERSERVICED A WWMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 15 969AE 969 CREW REPORTED AN OILY SOUR SMELL COMING FROM THE LEFT FLOW DURING FLIGHT. MAINTENANCE INSPECTED THE LEFT COOLING TURBIN E AND FOUND RESIDUAL OIL IN THE HOUSING. DRAINED RESIDUAL OIL AND PERFORMED GROUND RUNS. 2 L 7 2 4T RT A56EU 1996051600357 19960516 00357 SO 1996 5 16 96ZZZX2439 1 19960325 A 3233 758440 ROD END WIEBEL WTC21151 PIPER PA31T PA31T3 7103128 SO RT MLG WELL BROKEN A SOCA O OTHER J WARNING INDICATION CL CLIMB 1 AL 03 311SC 9495 31T8275006 AFTER TAKEOFF, PILOT DETERMINED RT MLG WOULD NOT LOCK UP (GEAR IN-TRANSIENT LIGHT). PILOT CONTINUED FLIGHT TO KENAI. P ILOT OVERFLEW HANGAR, AND TOWER WAS ADVISED THE GEAR WAS DOWN. PILOT ACTIVATED EMERGENCY GEAR BLOW-DOWN SYSTEM WITHOUT INCIDENT. UPON INSPECTION OF RT LANDING GEAR, MECHANIC FOUND THE ROD END BROKEN AT THE THREADS WHICH IS ATTACHED TO THE ACTUATOR. 1 L 7 2 3T A8EA 1996051600358 19960516 00358 WP 1996 5 16 96ZZZX2440 1 19960311 A 5220 DOOR DOUG DC9 DC932 3022066 WP RT AFT OVERWING NOT SEATED A VJ6A A UNSCHED LANDING O OTHER CL CLIMB 1 SO 11 921VV 47284 TPA/TPA - FLT 462 - AIR RETURN, THE RIGHT AFT OVERWING EXIT DOOR WAS NOT SEATED PROPERLY. RESEATED DOOR AND PRESSURIZED AIRCRAFT. NO LEAKS NOTED. AIRCRAFT OK TO CONTINUE SERVICE. 2 L 7 2 4F A6WE 1996051600359 19960516 00359 SO 1996 5 16 96ZZZX2441 1 19960216 A 5523 1159CSH205001 SKIN GULSTM G1159 G1159 3953505 SO ELEV TRIM TAB CRACKED A KKYA K NONE O OTHER IN INSP/MAINT 1 NE 03 510US 7184 223 DURING AN INSPECTION OF THE TAIL SECTION, 4 CRACKS WERE FOUND IN THE LEFT ELEVATOR TRIM TAB. THE CRACKS WERE LOCATED IN THE FIRST .50 INCH OF SKIN FORWARD OF THE SPAR. THE TAB WAS REPAIRED WITH GULFSTREAM DRAWINGS. (X) 2 L 7 2 4F RT A12EA 1996051600360 19960516 00360 SO 1996 5 16 96ZZZX2442 1 19960305 A 5720 1159W307101 PANEL GULSTM G1159 G1159A 3970109 SO LEFT WINGLET DELAMINATED A KKYA K NONE O OTHER IN INSP/MAINT 1 NE 03 165G 4427 414 DURING AN INSPECTION, A SMALL AREA OF DISBOND WAS NOTICED ON THE TRAILING EDGE PANEL OF THE LT WINGLET. WHEN A HOLE WAS CUT IN THE SKIN TO INITIATE A REPAIR, WATER SPILLED OUT. A SUBSEQUENT X-RAY SHOWED SEVERAL AREAS OF CORROSION ABOVE TH E DELAMINATION. IT IS NOT READILY APPARENT WHERE OR HOW THE WATER WAS ABLE TO ENTER. THE PANEL WAS REPLACED AND THE AI RCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F A12EA 1996051600361 19960516 00361 CE 1996 5 16 96ZZZX2443 1 19960229 A 2910 2407003300 HYD LINE LEAR 35 35A 5170602 CE FS 346.63 CHAFED A KKYA K NONE O OTHER IN INSP/MAINT 1 NE 03 404KA 3734 404 IN THE COURSE OF CHANGING THE EXTEND HYDRAULIC LINE FOR THE RIGHT LANDING GEAR FOR A SMALL DENT, NOTICED THE LINE WAS BA DLY CHAFED 31 INCHES FORWARD OF THE BULKHEAD FITTING LOCATED AT FS 346.63. THE LINE WAS CHANGED AND THE AIRCRAFT RETURN ED TO SERVICE. 2 L 7 2 4F A10CE 1996051600362 19960516 00362 SO 1996 5 16 96ZZZX2444 1 19960413 A 2710 12027655029 CABLE ASSY EMB 120 EMB120RT SO RT WS X2902 BROKEN STRANDS A MASA K NONE O OTHER IN INSP/MAINT 1 SW 01 193YV 120193 WHILE PERFORMING A 1,600 FLIGHT HOUR CABLE INSPECTION, FOUND RT WING AILERON LOWER WING CABLE WITH BROKEN STRANDS AT WS Y2902 WHERE THE CABLE PASSES THROUGH THE NACELLE. 2 L 7 2 4T RT A31SO 1996051600363 19960516 00363 SO 1996 5 16 96ZZZX2445 1 19960413 A 2710 12027655005 CABLE ASSY EMB 120 EMB120RT SO LT WS Y3678 BROKEN STRANDS A MASA K NONE O OTHER IN INSP/MAINT 1 SW 01 193YV 120193 WHIEL PERFORMING A 1,600 FLIGHT HOUR CABLE INSPECTION, FOUND LT WING AILERON LOWER WING CABLE HAD BROKEN STRANDS AT WS Y 3678 WHERE CABLE PASSES THROUGH THE NACELLE. 2 L 7 2 4T RT A31SO 1996051600364 19960516 00364 EA 1996 5 16 96ZZZX2446 2 19960401 A 7250 3018834 COUPLING DHAV DHC6 DHC6300 EA PWA PT6 PT6A27 52043 EA RT ENGINE BROKEN A A ASWA K NONE O OTHER IN INSP/MAINT 1 WP 07 142SA 23828 15877 41936P 241 PCE40263 DURING PHASE INSPECTION, MAINTENANCE PERSONNEL FOUND ABNORMAL AMOUNT OF METAL IN RIGHT ENGINE MAIN OIL FILTER. UPON FUR THER INVESTIGATION FOUND LARGE STEEL FRAGMENT ON REDUCTION GEARBOX MAGNETIC PLUG. AFTER REMOVAL OF GEARBOX FROM ENGINE, FOUND POWER TURBINE NOT COUPLED TO PROPELLER SHAFT. UPON DISASSEMBLY OF REDUCTION GEARBOX, FOUND POWER TURBINE SHAFT C OUPLING BROKEN AT FORWARD RETAINING RING GROOVE AROUND APPROXMATELY 320 DEGREES OF CIRCUMFERENCE. 1 H 7 2 3T 4 T A9EA E4EA 1996051600372 19960516 00372 WP 1996 5 16 AALA960387 1 19960310 A 4990 OIL LINE GARRTT DOUG DC9 DC982 3022082 WP APU LOOSE A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 462AA 49592 DFW - FLT 2386 - AFTER TAKEOFF SAT DURING INITIAL CLIMB, OIL SMOKE, AND FUMES NOTED IN AFT PORTION OF MAIN CABIN. SMOKE AND FUMES DISSIPATED AFTER APPROXIMATELY 2 MINUTES AND AIRCRAFT PROCEEDED TO DFW, LANDING WITHOUT INCIDENT. TIGHTENED EXTERNAL OIL LINE ON APU. ACCOMPLISHED PACK BURN-OUT PROCEDURE AND REPLACED ALL COALESCER BAGS. ACCOMPLISHED GROUND EN GINE AND APU RUN AND OPERATED PACKS WITH NO SMOKE OR FUMES NOTED. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1996051600373 19960516 00373 NM 1996 5 16 AALA960407 1 19960317 A 2910 2249409501 TUBE ROHR DOUG MD11 MD11 3023602 NM NR 1 HYD SYS LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 1762B 48552 JFK - FLT 0086 - EN ROUTE ORD/LHR DURING CRUISE, HYDRAULIC SYSTEM NR 1 QUANTITY WENT TO ZERO AND SYSTEM NR 1 FAILED. AI RCRAFT DIVERTED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED NR 1 ENGINE, NR 1 HYDRAULIC SYSTEM UPPER ENGINE PUMP CASE DRAIN TUBE. ALSO, REPLACED BOTH SYSTEM 1 ENGINE DRIVEN HYDRAULIC PUMP, CASE DRAIN PRESSURE AND SYSTEM FILTERS. SERVICE D SYSTEM AND ACCOMPLISHED LEAK AND GROUND CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2 L 7 3 4F RT A22WE 1996051600374 19960516 00374 WP 1996 5 16 AALA960479 1 19960326 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 228AA 49178 DFW - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTING IN THE FORWARD CABIN DIM. REPLACED CONNECTOR WIR E. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1996051600375 19960516 00375 WP 1996 5 16 AALA960481 1 19960326 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 228AA 49178 DFW - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTING IN THE FORWARD CABIN AND MAIN CABIN DIM. REPAIRE D EMERGENCY EXIT FLOOR PATH LIGHTING WIRE BETWEEN FIRST CLASS AND MAIN CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1996051600376 19960516 00376 EU 1996 5 16 ASOA96011 1 19960327 A 7931 81071100010 OIL PRESS TRANSM AEROSP ATR72 ATR72212 EU LT ENGINE INOPERATIVE A ASOA O OTHER N FALSE WARNING AP APPROACH 1 SO 11 633AS 344 OKC/DFW - ON APPROACH, THE LEFT ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED BRIEFLY AND CREW DECLARED AN EMERGENCY. THE C APTAIN REDUCED POWER DUE TO TURBULENCE AND THE OIL PRESSURE STABILIZED FOR THE REST OF THE FLIGHT. CREW NOTIFIED THE TO WER THE ENGINE WAS NOT SHUT DOWN AND THAT EVERYTHING WAS NORMAL. LANDING WAS MADE SAFELY AND WITHOUT INCIDENT AT DFW. R EMOVED AND REPLACED THE LEFT ENGINE OIL PRESSURE TRANSMITTER. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RELEASED FOR SERVICE. (X) 2 H 7 2 4T RT A53EU 1996051600377 19960516 00377 NM 1996 5 16 AWXA90139 1 19960318 A 5311 FRAME BOEING 737 737275 1384485 NM BS 500 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 CGCPW 20959 PAE - FLT 3812 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND CRACK IN RADIUS OF INBOARD CHORD OF STA 500H, RT STR 24. CUT OUT DAMAGE, FABRICATED REPAIR PART AND INSTALLED PER SRM 51-40-3. (X) 2 L 7 2 4F A16WE 1996051600378 19960516 00378 NM 1996 5 16 AWXA960120 1 19960306 A 5320 CHORD BOEING 737 737275 1384485 NM BS 727 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 CGAPW 20922 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND CRACKS ON INSPECTION PER 14M53005, STA 727, CHORD AT STR 18A, LT SIDE, FOR WARD, 2 HOLES .1250 INCH AND 1.50 INCH LONG. REPAIRED PER EO 53-11-03. (X) 2 L 7 2 4F A16WE 1996051600379 19960516 00379 NM 1996 5 16 AWXA960138 1 19960318 A 5311 FRAME BOEING 737 737275 1384485 NM BS 500 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 CGCPW 20959 PAE - FLT 3812 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND CRACK IN RADIUS OF INBOARD CHORD OF STA 500A FRAM E AT STR Z/L. REMOVED CRACKED PORTION OF CHORD. FABRICATED AND INSTALLED REPAIR PIECES IAW SRM 51-40-03. (X) 2 L 7 2 4F A16WE 1996051600380 19960516 00380 NM 1996 5 16 AWXA960140 1 19960318 A 5315 FLOOR BEAM BOEING 737 737275 1384485 NM BS 1016 CORROSION A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 CGCPW 20959 PAE - FLT 3812 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM AT BS 1016, RBL 5, WL 208 . FABRICATED AND INSTALLED REPAIR PARTS AT STA 1016, WL 208, RBL 5, IAW SRM 53-10-9. (X) 2 L 7 2 4F A16WE 1996051600381 19960516 00381 NM 1996 5 16 AWXA960141 1 19960318 A 5315 FLOOR BEAM BOEING 737 737275 1384485 NM BS 947 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 CGCPW 20959 PAE - FLT 3812 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND CORROSION AT BS 947, WL 208, BL ZERO, RBL 25, RBL 45, AND LBL 25 FLOOR BEAM. REPAIRED FLOOR BEAM PER ER 2-53-15-31. (X) 2 L 7 2 4F A16WE 1996051600382 19960516 00382 NM 1996 5 16 AWXA960142 1 19960318 A 5315 FLOOR BEAM BOEING 737 737275 1384485 NM BS 987 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 CGCPW 20959 PAE - FLT 3812 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND CORROSION AT STA 987, WL 208, BL ZERO TO RBL 7 FL OOR BEAM. REPLACED FLOOR BEAM PER ER 2-53-15-32. (X) 2 L 7 2 4F A16WE 1996051600383 19960516 00383 NM 1996 5 16 AWXA960143 1 19960318 A 5347 BAC1520792 SEAT TRACK BOEING 737 737275 1384485 NM BS 987-1016 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 CGCPW 20959 PAE - FLT 3812 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND CORROSION ON SEAT TRACK AT BS 987 TO BS 1016, RBL 45, WL 208. REMOVED AND REPLACED SEAT TRACK FROM BS 987 - BS 1016, RBL 45, WL 208, IAW SRM 51-10-1 AND SRM 51-30-20. ( X) 2 L 7 2 4F A16WE 1996051600384 19960516 00384 NM 1996 5 16 AWXA960144 1 19960318 A 5320 66221871 SUPPORT BOEING 737 737275 1384485 NM BS 520 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 CGCPW 20959 PAE - FLT 3812 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND SUPPORT CHANNEL CRACKED ON AFT SIDE OF FLOOR BEAM BS 520, RBL 25, WL 207. REMOVED EXPANSION LINK AND FLOOR SUPPORT TO GAIN ACCESS TO U-CHANNEL. REMOVED AND REPLACED U- CHANEL, BS 520, RBL 25, IAW SRM 51-10-1. (X) 2 L 7 2 4F A16WE 1996051600385 19960516 00385 NM 1996 5 16 AWXA960145 1 19960318 A 5320 WEB BOEING 737 737275 1384485 NM BS 706-716 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 CGCPW 20959 PAE - FLT 3812 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND LONGITUDINAL FLOOR WEB CRACKED AT BL ZERO, BS 706 - BS 716, SL 203. REMOVED DAMAGED AREA OF LONGITUDINAL WEB AND REPAIRED PER SRM 31-40-2, SRM 53-10-2, SRM 51-30-2, AND MM 52-21-131. (X) 2 L 7 2 4F A16WE 1996051600386 19960516 00386 NM 1996 5 16 AWXA960146 1 19960314 A 5311 FRAME BOEING 737 737275 1384485 NM BS 420 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 CGCPW 20959 PAE - FLT 3812 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND CRACK IN RADIUS OF INBOARD CHORD OF STA 420 FRAME AT STR 22L. REPAIRED PER AWA, SRM 51-40-3, FIGURE 1. (X) 2 L 7 2 4F A16WE 1996051600387 19960516 00387 NM 1996 5 16 AWXA960147 1 19960315 A 5320 STIFFENER BOEING 737 737275 1384485 NM BS 727 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 CGCPW 20959 PAE - FLT 3812 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND CRACK AT BS 727, STR 18A, LT OUTBOARD CHORD. TRI MMED SHEAR BEAM WEB HORIZONTAL STIFFENER ON BS 727, WL 189, STR 18A PER SB 737-53A116, FIGURE 3. NDT VERIFIED CRACK CON TAINMENT, FABRICATED AND INSTALLED PER SRM 51-10-2, SRM 51-30-2, SRM 51-20-4. (X) 2 L 7 2 4F A16WE 1996051600388 19960516 00388 NM 1996 5 16 AWXA960148 1 19960318 A 5260 STRAP BOEING 737 737275 1384485 NM AIRSTAIR DOOR CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 CGCPW 20959 PAE - FLT 3812 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND CORROSION IN AIRSTAIR DOOR, FORWARD LOWER CORNER ON STRAP. REMOVED CORROSION AT FORWARD LOWER CORNER STRAP OF AIRSTAIR DOOR 1 INCH BY 2 INCH BY .019 INCH. FABRICATED N EW STRAP PER SRM 52-60-1, ALODINED, PRIMED, SEALED AND INSTALLED PER SRM 51-10-1. (X) 2 L 7 2 4F A16WE 1996051600389 19960516 00389 NM 1996 5 16 AWXA960149 1 19960318 A 5330 SKIN BOEING 737 737275 1384485 NM BS 443.5 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 CGCPW 20959 PAE - FLT 3812 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND CRACK IN FUSELAGE SKIN AT STA 443.5, STR 817R, LO WER ROW OF FASTENERS. REMOVED DAMAGED AREA OF SKIN, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-30-3. (X) 2 L 7 2 4F A16WE 1996051600390 19960516 00390 NM 1996 5 16 AWXA960150 1 19960318 A 5754 SKIN BOEING 737 737275 1384485 NM NR 6 LE SLAT CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 CGCPW 20959 PAE - FLT 3812 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND NR 6 SLAT CENTER AUXILIARY TRACK CUT OUT ON FIXED LEADING EDGE HAS CRACK CONTINUING PAST PREVIOUS BLEND OUT. CUT OUT DAMAGED SKIN SECTION. FABRICATED NEW SKIN AND REPA IR DOUBLER AND INSTALLED REPAIR PARTS PER ER NR 2-57-31-16. (X) 2 L 7 2 4F A16WE 1996051600391 19960516 00391 NM 1996 5 16 AWXA960151 1 19960318 A 5512 SKIN BOEING 737 737275 1384485 NM LT HORIZ STAB DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 CGCPW 20959 PAE - FLT 3812 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND LT HORIZONTAL STABILIZER FIXED L/E DENTED 1.5 INC HES BY .040 INCH DEEP AT STA 65.73, APPROXIMATELY 8 INCHES OUTBOARD FROM FUSELAGE. REWORKED DENT TO WITHIN LIMITS PER S RM 51-40-1 AND SRM 55-10-1. (X) 2 L 7 2 4F A16WE 1996051600392 19960516 00392 NM 1996 5 16 AWXA960152 1 19960318 A 5311 FRAME BOEING 737 737275 1384485 NM BS 947.75 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 CGCPW 20959 PAE - FLT 3812 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND CRACK IN CIRCUMFERENTIAL FRAME BS 947.75, RBL 17, STR 26R, RADIUS CUT OUT UNDER FAIL SAFE CHORD ANGLE. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS PER S RM 53-10-4. (X) 2 L 7 2 4F A16WE 1996051600393 19960516 00393 NM 1996 5 16 AWXA960153 1 19960319 A 5311 FRAME BOEING 737 737275 1384485 NM BS 500 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 CGCPW 20959 PAE - FLT 3812 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND CRACK IN STA 500B FRAME AT STR 24L. REMOVED DAMA GE AND REPAIRED PER SRM 51-40-3, SRM 51-10-1, SRM 51-10-2, MM 51-21-17. (X) 2 L 7 2 4F A16WE 1996051600394 19960516 00394 NM 1996 5 16 AWXA960154 1 19960319 A 5311 FRAME BOEING 737 737275 1384485 NM BS 460 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 CGCPW 20959 PAE - FLT 3810 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND CRACK IN RADIUS OF INBOARD CHORD OF STA 460 FRAME AT STR 21L. REMOVED DAMAGE AND REPAIRED PER SRM 51-40-3, SRM 51-10-2. (X) 2 L 7 2 4F A16WE 1996051600395 19960516 00395 NM 1996 5 16 CAL960429 1 19960331 A 3244 TIRE BOEING 727 727232 1384082 NM LT MLG RUPTURED A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 09 59792 20646 GYE - FLT 0777 - THE NR 2 TIRE RUPTURED ON TAKEOFF FROM UIO RESULTING IN DAMAGE TO HYDRAULIC LINES WITH FLUID LOSS FROM 'A' AND 'B' HYDRAULIC SYSTEM. THE AIRCRAFT WAS DIVERTED TO GYE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND DAM AGE TO THE LT INBD T/E FLAP, NR 1 ENGINE FAN BLADES, AND APU GROUND CONTROL PANEL IN LT WHEELWELL. THE AIRCRAFT WAS TAK EN OUT OF SERVICE FOR REPAIR. THE SDR WILL REMAIN OPEN FOR PART INFO PENDING CORRECTIVE ACTION. SUPPLEMENT - THE NR 1 AND NR 2 TIRES WERE REPLACED. THE DAMAGED HYD LINES IN LT MLG WHEELWELL WERE REPLACED. DAMAGE TO ACFT FROM IMPACT BY T IRE DEBRIS REPAIRED. THE NR 1 ENGINE FIRST STAGE FAN WAS REPLACED. (X) 2 L 7 3 4F A3WE 1996051600396 19960516 00396 WP 1996 5 16 CAL960498 1 19960416 A 5753 5912168504 VANE DOUG DC9 DC932 3022066 WP RT TE FLAP DAMAGED A A CALA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SW 09 12538 16865 47218 IAH - FLT 1905 - WHEN FLAPS SELECTED PAST 25 DEGREES, AIRCRAFT WANTS TO ROLL TO RIGHT. WHEN FLAPS PASS ABOUT 30 DEGREES , CLUNK SOUND HEARD. REQUIRED 40 DEGREES WHEEL DEFLECTION TO MAINTAIN LEVEL FLIGHT AT 40 DEGREES FLAP. REMOVED DAMAGED FORWARD AND AFT RT FLAP MOVEABLE VANES AND REPLACED WITH SERVICEABLE VANES. INSTALLED NEW CABLES AND ADJUSTED PER MM 2 7-51-1. (X) 2 L 7 2 4F A6WE 1996051600397 19960516 00397 EU 1996 5 16 PLG3196E4 1 19960301 A 2730 WARNING LIGHT SAAB SF340 SF340A 7850100 EU PITCH TRIM ILLUMINATED A PLGA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 NE 05 749BA 340A152 BOS/MHT - FLT 4745 - DURING TAKEOFF, TAKEOFF WAS ABORTED DUE TO A CONFIGURATION WARNING LIGHT FROM A PITCH TRIM. MAINTE NANCE INSPECTED THE TRIM SYSTEM AND COULD NOT FIND ANY DEFECTS. SUSPECT TRIM WAS JUST TOO FAR DOWN. AIRCRAFT WAS RETUR NED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1996051600398 19960516 00398 EU 1996 5 16 SIMA960771 1 19960317 A 7712 3037603 SENSOR AEROSP ATR72 ATR72212 EU NR 2 ENGINE FAILED A SIMA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SW 21 348AE 00610 349 TUL - FLT 3734 - RIGHT ENGINE TORQUE FLUCTUATION OF 23 PERCENT IN CRUISE, IN-FLIGHT SHUT DOWN BY CREW. REPLACED 1.8 SEN SOR, GROUND RUN GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1996051600399 19960516 00399 EU 1996 5 16 SIMA960943 1 19960403 A 3240 BRAKES AEROSP ATR42 ATR42300 8680920 EU LANDING GEAR MALFUNCTIONED A SIMA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 21 265AE 266 DFW - FLT 3665 - DURING TAXI, NORMAL BRAKE FAILED TO STOP AIRCRAFT TWICE. EMERGENCY BRAKES STOPPED AIRCRAFT. THERE WER E NO FAULTS ON ANY SYSTEM. ACCUMULATORS WERE UP AND ANTI-SKID CHECKED OK. BLED ALL FOUR BRAKES. GROUND OPERATIONAL CH ECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1996051600400 19960516 00400 1996 5 16 USAAF96036 4 19960424 A 3442 20412222451 INDICATOR FOKKER F28 F28MK4000 4990810 EU RADAR FAULTY A A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 477AU 8556 11226 RDU - FLT 994 - AT FL 270, SMOKE STARTED TO APPEAR IN COCKPIT CAUSING THE CREW TO DON THE MASKS AND DIVERT TO RDU. NO E MERGENCY WAS DECLARED AND THE FLIGHT LANDED WITH NO FURTHER COMPLICATIONS. MAINTENANCE REPLACED THE RADAR INDICATOR AND TRANSCEIVER. (X) 2 L 7 2 4F RT A20EU 1996051600401 19960516 00401 NE 1996 5 16 VTZA96158 2 19960416 A 7261 31050131 OIL TUBE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE RT ENGINE FAILED A VTZA E ENGINE SHUTDOWN K FLUID LOSS AP APPROACH 1 EA 27 325UE 4978 2060 41063 IAD/EWR - FLT 6270 - DURING APPROACH AT 1315 HRS ON 4-16-96, SHUT DOWN RT ENGINE DUE TO OIL PRESSURE INDICATION LOST ON APPROACH. AN EMERGENCY DECLARED AND AIRCRAFT LANDED WITH NO FURTHER INCIDENTS AND ALL PASSENGERS AND CREW SAFE. MAINTE NANCE REPLACED THE REAR BEARING OIL SUPPLY LINE. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T 4 T RT A41NM E18NE 1996051600402 19960516 00402 NM 1996 5 16 W8PA960007 1 19960328 A 2612 659401 FIRE WARN MODULE BOEING 737 7373B7 1384580 NM APU FAILED A W8PA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 NM 03 952WP 1019 23378 SAN - AT 23,000 FEET DURING CLIMB-OUT, APU FIRE WARNING ILLUMINATED. FIRED EXTINGUISHER BOTTLE. LIGHT REMAINED ON. DE CLARED IN-FLIGHT EMERGENCY. FLIGHT DIVERTED TO LAX. FOUND FIRE WARNING MODULE HAD FAILED. REMOVED AND REPLACED FIRE W ARNING MODULE. (X) 2 L 7 2 4F RT A16WE 1996051600403 19960516 00403 NM 1996 5 16 W8PA960009 1 19960412 A 5610 57176145 WINDSHIELD BOEING 737 7373B7 1384580 NM LT COCKPIT SHATTERED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 951WP 22951 OUT PANEL L-1 (CAPTAIN'S) WINDSHIELD SHATTERED. REMOVED AND REPLACED L-1 WINDSHIELD. (X) 2 L 7 2 4F RT A16WE 1996051600404 19960516 00404 WP 1996 5 16 Y2PA96014 1 19960327 A 5330 5911401 SKIN DOUG DC9 DC915F 3022037 WP BS 108 CRACKED A Y2PA K NONE O OTHER IN INSP/MAINT 1 GL 23 195US 65107 47017 TWO 1 INCH CRACKS IN THE RIGHT SIDE OF THE NLG WHEELWELL SKIN AT STA 108. REMOVED DAMAGED SKIN AREA. FABRICATED AND IN STALLED REPAIR FILLER AND REPAIR DOUBLER PER USA JET AIRLINES ENGINEERING AUTHORIZATION NR 96-53-02. THESE DATA WERE DE R APPROVED BY R. MNASHI, DER NR SW-810 ON FAA FORM 8110-3, DATED 3-26-96. PAR TOTAL CYCLES, 78,559. (X) 2 L 7 2 4F A6WE 1996051600405 19960516 00405 WP 1996 5 16 Y2PA96016 1 19960402 A 3260 7000010101 DOOR SWITCH DOUG DC9 DC915F 3022037 WP LT/RT MLG MALFUNCTIONED A Y2PA O OTHER N FALSE WARNING DE DESCENT 1 GL 23 195US 65137 47017 YIP - FLT 13336 - ON DESCENT INTO YIP WITH GEAR UP, THE DOOR LIGHT CAME ON AND REMAINED ON. REPLACED LEFT AND RIGHT GEA R DOOR SWITCHES AND REPAIRED WIRING ON LEFT AND RIGHT DOOR SWITCH CANNON PLUGS. PART TOTAL CYCLES, 78,574. S/N OFF LT, 9471. S/N NR OFF RT, 9325. (X) 2 L 7 2 4F A6WE 1996051600406 19960516 00406 EU 1996 5 16 Y2PA96018 1 19960412 A 2133 142212B VALVE AMD FALC20 FALCON 2720302 EU CABIN LOCATION CONTAMINATED A Y2PA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 827AA 298 ELP - FLT 13608 - CABIN WOULD NOT PRESSURIZE PAST 2.5 PSI DURING CLIMB OUT. THE CABIN CONTINUED TO CLIMB DURING ASCENT PHASE OF FLIGHT AND CREW ELECTED TO RETURN TO POINT OF DEPARTURE AT EL PASO, TEXAS. NO EMERGENCY PROCEDURES WERE REQUIR ED AND AIRCRAFT LANDED WITHOUT EVENT. DURING TROUBLESHOOTING AND INSPECTION OF THE SYSTEM, DISCOVERED THE OUTFLOW VALVE CONTAINED SOME DEBRIS PREVENTING IT FROM CLOSING. THE DEBRIS WAS REMOVED AND FROM THE OUTFLOW VALVE, THE AIRCRAFT WAS GROUND RUN AND THE PRESSURIZATION SYSTEM CHECKED NORMAL PER MM, CHAPTER 21-30-5. (X) 2 L 7 2 4F A7EU 1996051600407 19960516 00407 WP 1996 5 16 Y2PA96022 1 19960408 A 5330 5911401 SKIN PANEL DOUG DC9 DC915F 3022037 WP NLG WELL FS 108 CRACKED A Y2PA K NONE O OTHER IN INSP/MAINT 1 GL 23 195US 65216 47017 YIP - FOUND ONE .25 INCH CRACK IN THE LT SIDE OF NLG WHEELWELL SKIN AT STA 108. NOTE: THIS SAME AREA WAS DISCOVERED CR ACKED ON RT SIDE OF 195US (SN 47017) ON 3-27-96 - MRR NR 96014, AND ON THE RT SIDE OF 198US (SN 47045) ON 4-8-96 - MRR N R 96017. ALL CRACKS WERE DETECTABLE DURING A 'VISUAL INSPECTION'. REMOVED DAMAGED SKIN AREA. FABRICATED AND INSTALLED REPAIR FILLER AND REPAIR DOUBLER PER USA JET AIRLINES ENGINEERING AUTORIZATION NR 96-53-02R1. THESE DATA WERE DER APPR OVED BY R. MINASHI, DER NR SW-810 ON FAA FORM 8110-3, DATED 4-7-96. PART TOTAL CYCLES, 78,626. (X) 2 L 7 2 4F A6WE 1996051600408 19960516 00408 SW 1996 5 16 HEEA966979 1 19960410 A 6300 222044685101 SHAFT ASSY 222044006109 BELL 230 230 1182149 SW M/R DRIVE CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 2976 A217 23009 CORROSION PITS ON I/D OF SHAFT. 1 G 7 2 3U NC H9SW 1996051600409 19960516 00409 SW 1996 5 16 HEEA966980 1 19960410 A 6300 222044685101 SHAFT ASSY 222044006109 BELL 230 230 1182149 SW M/R DRIVE CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 2976 A216 23009 CORROSION PITS ON I/D OF SHAFT. 1 G 7 2 3U NC H9SW 1996051600410 19960516 00410 1996 5 16 HEEA966983 4 19960410 A 2210 214074305105 AMPLR ASSY BELL 214 214ST 1182106 SW AUTO FLIGHT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 8045T 28101 WILL NOT MONITOR TEST. WILL NOT MOVE ACTUATOR. 2 G 7 2 4U H10SW 1996051600412 19960516 00412 SW 1996 5 16 HEEA966985 1 19960410 A 2840 222366685101 CONTROL UNIT BELL 230 230 1182149 SW FUEL QTY DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 230UN 2937 23009 R/H FUEL QUANTITY INTERMITTENTLY READS ZERO. 1 G 7 2 3U NC H9SW 1996051600413 19960516 00413 EU 1996 5 16 HEEA966988 1 19960410 A 6520 350A33200403 SPIDER SNIAS 350 AS350B2 8680813 EU T/R BEARING WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6095S 1285 2777 T/R SPIDER SPHERICAL BEARING WORN. 1 G 7 1 3U H9EU 1996051600414 19960516 00414 EU 1996 5 16 HEEA966989 1 19960410 A 3340 356H2801 LIGHT SNIAS 350 AS350B2 8680813 EU ANTI COLL INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100R 483 2862 LIGHT INOPERATIVE. 1 G 7 1 3U H9EU 1996051600415 19960516 00415 EU 1996 5 16 HEEA966990 1 19960410 A 6730 350A27191004 ACTUATING ROD SNIAS 350 AS350B2 8680813 EU SERVO BEARING FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 350BZ 1560 2653 ACTUATING ROD AFT BEARING BAD. 1 G 7 1 3U H9EU 1996051600416 19960516 00416 EU 1996 5 16 HEEA966991 1 19960410 A 6520 350A33200403 SPIDER SNIAS 350 AS350B2 8680813 EU T/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100R 922 2862 SPIDER BUSHINGS AND SPHERICAL BEARING ARE WORN. 1 G 7 1 3U H9EU 1996051600417 19960516 00417 EU 1996 5 16 HEEA966992 1 19960410 A 7722 SELOC19EH INDICATOR SNIAS 350 AS350B2 8680813 EU COCKPIT T4 STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 350BZ 1580 2653 T4 INDICATOR UNIT STICKING. 1 G 7 1 3U H9EU 1996051600418 19960516 00418 SW 1996 5 16 HEEA966993 1 19960412 A 5320 206031301025S SUPPORT BELL 206 206B 1181511 SW FUSELAGE LT MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 FGHRU 2789 SUPPORT IS MANUFACTURED TOO WIDE. THE ORIGINAL SUPPORT BRACKET FITS INSIDE THE NEW BRACKET. 1 G 7 1 3U H2SW 1996051600419 19960516 00419 SW 1996 5 16 HEEA966994 1 19960412 A 5320 20603130126S SUPPORT BELL 206 206B 1181511 SW FUSELAGE RT MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 FGHRU 2789 SUPPORT IS MANUFACTURED TOO WIDE. THE ORIGINAL SUPPORT BRACKET FITS INSIDE THE NEW BRACKET. 1 G 7 1 3U H2SW 1996051600420 19960516 00420 SW 1996 5 16 HEEA966997 1 19960415 A 6220 204010937009 DAMPER ASSY BELL 212 212 1181420 SW M/R DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1079U 31122 FLUID CONTAMINATION AND GLASS IS UNREADABLE. 1 G 7 1 4U H4SW 1996051600421 19960516 00421 SW 1996 5 16 HEEA966998 1 19960415 A 6220 204010937009 DAMPER ASSY BELL 212 212 1181420 SW M/R DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1079U 31122 FLUID CONTAMINATION AND GLASS IS UNREADABLE. 1 G 7 1 4U H4SW 1996051600422 19960516 00422 EU 1996 5 16 HEEA966999 1 19960415 A 7722 50061036 INDICATOR BOLKMS 105 BO105S 5626006 EU EXH TEMP ERROR E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5368F S718 EXCESSIVE FRICTION ERROR 20 DEGREES TO 30 DEGREES. S/N 690 & 775 1 G 7 2 3U H3EU 1996051600423 19960516 00423 SW 1996 5 16 HEEA967002 1 19960415 A 3340 214175127103 POWER SUPPLY BELL 214 214ST 1182106 SW ANTI COLL LIGHT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 POWER SUPPLY WOULD NOT POWER UP ANTI-COLLISION SYSTEM. TIME SINCE REPAIR 0:00. 2 G 7 2 4U H10SW 1996051600424 19960516 00424 EU 1996 5 16 HEEA967003 1 19960416 A 6320 SL100153B PIN SPACER SNIAS 350 AS350B2 8680813 EU M/R GR BOX BROKE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6095S 1319 2777 M/R GR BOX EXPANSION PIN SPACER BROKE. 1 G 7 1 3U H9EU 1996051600425 19960516 00425 1996 5 16 HEEA967005 4 19960417 A 2200 2593996333 TARSYN 333 BELL 412 412 1182202 SW AUTO FLIGHT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 107X 33113 PILOT COMPASS NEEDLE STAYS CENTERED AT ALL TIMES. 1 G 7 2 4U H4SW 1996051600426 19960516 00426 1996 5 16 HEEA967006 4 19960417 A 2210 11788904 TRANSDUCER BOLKMS 117 BK117B2 5626013 EU YAW SYS DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 132AE 7238 CAUSED REPEATED YAW KICKING. 1 G 7 2 3U NC H13EU 1996051600427 19960516 00427 1996 5 16 HEEA967007 4 19960417 A 2210 7611123 AMPLIFIER SKRSKY S76 S76A 8143006 NE PITCH SLICE DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 22342 760096 #1 PITCH KICKING IN FLIGHT. 1 G 7 2 3U H1NE 1996051600428 19960516 00428 NE 1996 5 16 HEEA967008 1 19960417 A 5610 7620710002144 WINDOW SKRSKY S76 S76A 8143006 NE PILOT DOOR MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 13911 WINDOW IS NOT PRE-DRILLED AND IT DOES NOT HAVE THE SMALL OPENABLE WINDOW. 1 G 7 2 3U H1NE 1996051600430 19960516 00430 1996 5 16 HEEA967010 4 19960417 A 3421 4020936903 INDICATOR BELL 412 412 1182202 SW 3 AXIS GYRO DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 6559Z 36019 CO-PILOT'S INDICATOR (HEADING) PRECESSES EXCESSIVELY AND AT TIMES WILL NOT SLAVE PILOT'S INDICATOR WILL STICK AND CANNOT BE ADJUSTED. 1 G 7 2 4U H4SW 1996051600432 19960516 00432 EU 1996 5 16 HEEA967012 1 19960417 A 7722 10590947 INDICATOR BOLKMS 105 BO105S 5626006 EU COCKPIT TOT ERROR E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 54191 S804 NEEDLE HAS EXCESSIVE FRICTION ERROR AND INDICATES 45 DEGREES AT ZERO. 1 G 7 2 3U H3EU 1996051600433 19960516 00433 NE 1996 5 16 HEEA967014 1 19960417 A 6410 7610105101041 BLADE SKRSKY S76 S76A 8143006 NE T/R ERODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2743E 3111 760155 PART IS ERODED. (LEADING EDGE ABRASION STRIP HAS EROSION HOLE THROUGH THE STRIP. 1 G 7 2 3U H1NE 1996051600434 19960516 00434 NE 1996 5 16 HEEA967015 1 19960417 A 6410 7610105001045 BLADE SKRSKY S76 S76A 8143006 NE T/R ERODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2743E 8316 760155 PART IS ERODED. (EROSION THROUGH THE LEADING EDGE ABRASION STRIP ON PADDLE "B") 1 G 7 2 3U H1NE 1996051600435 19960516 00435 NE 1996 5 16 HEEA967016 1 19960417 A 6210 7615009043050 TIP CAP SKRSKY S76 S76A 8143006 NE M/R BLADE SEPARATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546G 760076 LOWER INTERNAL DOUBLER SEPARATED BEYOND THE MAX LIMITS. 1 G 7 2 3U H1NE 1996051600436 19960516 00436 NE 1996 5 16 HEEA967017 1 19960417 A 6210 7615009100052A BLADE SKRSKY S76 S76A 8143006 NE BLADE STA 168 SEPARATION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5426U 4016 760167 SPLICE ON THE LEADING EDGE AT STATION 168 WITH SEPARATION BEYOND LIMITS. 1 G 7 2 3U H1NE 1996051600437 19960516 00437 EU 1996 5 16 HEEA967018 1 19960417 A 6210 10515150 BLADE BOLKMS 105 BO105S 5626006 EU M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4294R 2760 S860 BLADE NOSE AND NECK SHELL CRACKED AND DISCOLORED BELOW ROOT/WRAP AND PENDULUM WRAP. 1 G 7 2 3U H3EU 1996051600438 19960516 00438 1996 5 16 HEEA967019 4 19960417 A 3452 066106200 TRANSCEIVER KT76 BELL 206 206L3 1182108 SW XPONDER DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 32041 51539 TOWER REPORTED TRANSPONDER INOPERATIVE. REPLACED CAVITY OSCILLATOR V101 AND FUSE F401. UNIT QUIT BLOWING FUSES; BUT DOE S NOT RECEIVE. 1 G 7 1 3U H2SW 1996051600440 19960516 00440 1996 5 16 HEEA967021 4 19960417 A 3442 MI5851345 INDICATOR P40 BELL 412 412 1182202 SW RADAR DEFECTIVE E HEEA K NONE L NO TEST NR NOT REPORTED 1 SW 03 2149S 36002 NO RF BAND IN TEST AND VERY INTERMITTENT TEST PATTERN. 1 G 7 2 4U H4SW 1996051600441 19960516 00441 1996 5 16 HEEA967022 4 19960417 A 3442 MI5851345 INDICATOR P40 BELL 412 412 1182202 SW RADAR FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2149S 36002 STANDBY FUNCTION INOPERATIVE; DISPLAY SHRINKS AND SPOKES. 1 G 7 2 4U H4SW 1996051600442 19960516 00442 SW 1996 5 16 HEEA967023 1 19960417 A 3340 214175127103 POWER SUPPLY BELL 214 214ST 1182106 SW STROBE DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 8045T 28101 STROBE HAS SLOW FLASH RATE (4 PER MINUTE) 2 G 7 2 4U H10SW 1996051600443 19960516 00443 1996 5 16 HEEA967024 4 19960417 A 3457 0845000000 SKYNAV 5000 BELL 206 206L1 1182107 SW COCKPIT GPS FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2777D 45299 GPS UNIT NOT LOCKING ON THE SATELLITES AND NOT UPDATING PRESENT POSITION. 1 G 7 1 3U H2SW 1996051600444 19960516 00444 1996 5 16 HEEA967025 4 19960417 A 3444 066304400 ALTIMETER BELL 412 412 1182202 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2149S 36002 NEEDLE ERRATIC ABOVE 2000 FEET. REPLACED PHOTOCELL V101 DUE TO WEAK DH LIGHT. PERFORMED COMPLETE CALIBRATION AND ALIGNM ENT. FOUND WHEN NEEDLE IS REVOLVING, NEEDLE GETS STUCK BEHIND MASK. 1 G 7 2 4U H4SW 1996051600446 19960516 00446 1996 5 16 HEEA967027 4 19960417 A 2312 071121540 CONTROL BELL 412 412 1182202 SW COCKPIT COMM FAULTY E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 22347 36005 LED DISPLAY DIM AND DIFFICULT TO READ IN SUNLIGHT. REPLACED PHOTOCELL V101 P/N 134-05005-0002. ALSO REPLACED PHOTOCELL LENS P/N 088-0548-00. REPAIRED. CHECKED LIGHTING AND TOUCHED UP FACEPLATE. BENCH CHECK GOOD. 1 G 7 2 4U H4SW 1996051600447 19960516 00447 1996 5 16 HEEA967028 4 19960417 A 2312 064105430 TRANSCEIVER BELL 206 206B 1181511 SW COCKPIT VHF DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2269A 3608 READOUT STAYS DIM IN BRIGHT LIGHT. FOUND THAT DISPLAY LENS HAD LOST IT'S TINT. REPLACED DISPLAY LENS - REPAIRED PROBLEM . ADJUSTED SIDETONE. BENCH CHECK GOOD. 1 G 7 1 3U H2SW 1996051600448 19960516 00448 1996 5 16 HEEA967029 4 19960417 A 3444 066104802 ALTIMETER BELL 412 412 1182202 SW COCKPIT ERRATIC E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2149S 36002 SUSPECT CAUSING THE NEEDLE TO SWING FROM TOP TO BOTTOM, ERRATIC ABOVE 1700 FEET. FOUND NEEDLE TO BE ERRATIC AND PRECISIO N EQUIPMENT OUTPUT VOLTAGE TO BE BAD. 1 G 7 2 4U H4SW 1996051600449 19960516 00449 1996 5 16 HEEA967030 4 19960417 A 2312 064105430 TRANSCEIVER AEROSP AS355 AS355F1 8680810 EU COCKPIT INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5796S 5164 TRANSCEIVER INOPERATIVE DISPLAY. DOESN'T TRANSMIT OR RECEIVE. SMELLS BURNT. 1 G 7 2 3U H11EU 1996051600450 19960516 00450 1996 5 16 HEEA967031 4 19960417 A 3444 066104802 ALTIMETER SKRSKY S76 S76A 8143006 NE COCKPIT INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 706AE 760275 INOPERATIVE. NEEDLE SPINS CONTINOUSLY. FOUND OPEN RUNS ON MOTHER BOARD. REPLACED MOTHER BOARD AND INTEGRATED CIRCUIT I 206 AND CAPACITOR C224. FOUND NEEDLE ON INDICATOR TO SPIN CONTINOUSLY. 1 G 7 2 3U H1NE 1996051600451 19960516 00451 1996 5 16 HEEA967032 4 19960417 A 2312 064101902 TRANSCEIVER KY196 BELL 206 206L3 1182108 SW COCKPIT VHF DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 206LS 51070 FLICKERING DISPLAY AND GARBLED RECEPTION. 1 G 7 1 3U H2SW 1996051600452 19960516 00452 1996 5 16 HEEA967033 4 19960417 A 3442 MI5852013 INDICATOR P4001 SKRSKY S76 S76A 8143006 NE COCKPIT RADAR FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5435V 760158 INDICATOR UNIT HAS NO PICTURE. 1 G 7 2 3U H1NE 1996051600453 19960516 00453 1996 5 16 HEEA967034 4 19960417 A 3442 MI585136 PEDESTAL P40 SKRSKY S76 S76A 8143006 NE COCKPIT RADAR DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 31217 760229 P40 PEDESTAL CAUSES RADAR SYSTEM TO SHUTDOWN AFTER 10-15 SECONDS OF OPERATION. 1 G 7 2 3U H1NE 1996051600454 19960516 00454 1996 5 16 HEEA967035 4 19960417 A 3442 MI585202 PEDESTAL BELL 214 214ST 1182106 SW RADAR ANTENNA DEFECTIVE E HEEA K NONE J WARNING INDICATION NR NOT REPORTED 1 SW 03 3897N 28106 DISPLAY FLASHES "ANTENNA" INTERMITTENTLY. ALSO, PITCH AND ROLL NOT ADJUSTING. 2 G 7 2 4U H10SW 1996051600455 19960516 00455 1996 5 16 HEEA967036 4 19960417 A 3442 MI585202 PEDESTAL SKRSKY S76 S76A 8143006 NE RADAR ANTENNA FAULTY E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 31217 760229 UNIT HAS A JERKING MOTION WHEN SCANNING FROM LEFT TO RIGHT IN DOWN POSITION. 1 G 7 2 3U H1NE 1996051600456 19960516 00456 1996 5 16 HEEA967037 4 19960417 A 2370 9806019001 CVR BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE L NO TEST NR NOT REPORTED 1 SW 03 108X 2562 33115 CVR DOES NOT COMPLETE TEST. NO LIGHT-NO AUDIO. 1 G 7 2 4U H4SW 1996051600457 19960516 00457 SW 1996 5 16 HEEA967038 1 19960417 A 6330 206033554101 LINK ASSY BELL 206 206L1 1182107 SW XMSN MOUNT BEARING FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1078D 45397 LINK ASSY LOWER BEARING SEPARATED. 1 G 7 1 3U H2SW 1996051600458 19960516 00458 SW 1996 5 16 HEEA967039 1 19960417 A 7714 206075681117 INDICATOR BELL 206 206L3 1182108 SW DUAL TACH INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3207Q 50540 TURBINE NEEDLE INOPERATIVE AND PLUGS REVERSED. 1 G 7 1 3U H2SW 1996051600459 19960516 00459 1996 5 16 HEEA967040 4 19960417 A 3457 0110010600 GPS165 BELL 212 212 1181420 SW COCKPIT GPS INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5736J 31140 UNIT DOES NOT PICK UP SATELLITE SIGNAL AT ALL. 1 G 7 1 4U H4SW 1996051600461 19960516 00461 GL 1996 5 16 HEEA967042 2 19960418 A 7250 23037413 SHAFT 6898735 AEROSP AS355 AS355F1 8680810 EU ALLSN 250C 250C20B 03013 GL ENG PT OUTER DEFECTIVE E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 5793Z CAT37538 5142 UPON INSPECTION OF NEW OUTER PT SHAFT NOTED THE FOLLOWING: ALSEAL COATING FLAKING ON SHAFT O.D. NEW PART INSTALLED. 1 G 7 2 3U 3 U H11EU E4CE 1996051600462 19960516 00462 1996 5 16 HEEA967043 4 19960418 A 3455 066104701 RECEIVER SKRSKY S76 S76A 8143006 NE COCKPIT ADF FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1546G 760076 ADF DOES NOT RECEIVE. 1 G 7 2 3U H1NE 1996051600463 19960516 00463 1996 5 16 HEEA967044 4 19960418 A 2312 064100900 TRANSCEIVR KTR905 BELL 212 212 1181420 SW COCKPIT VHF DISTORTED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 27805 31106 DISTORTED TRANSMISSION. 1 G 7 1 4U H4SW 1996051600464 19960516 00464 1996 5 16 HEEA967045 4 19960418 A 2312 064100900 TRANSCEIVR KTR905 BELL 412 412 1182202 SW COCKPIT VHF FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2258F 33073 TRANSCEIVER WON'T RECEIVE. 1 G 7 2 4U H4SW 1996051600465 19960516 00465 1996 5 16 HEEA967046 4 19960418 A 3455 066107200 RECEIVER KR87 BELL 206 206L1 1182107 SW COCKPIT ADF FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5014V 45217 ADF DOESN'T WORK. 1 G 7 1 3U H2SW 1996051600466 19960516 00466 1996 5 16 HEEA967047 4 19960418 A 2312 064100900 TRANSCEIVR KTR905 BELL 412 412 1182202 SW COCKPIT COMM DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2014K 33020 TRANSMITS AND RECEIVES WEAK. 1 G 7 2 4U H4SW 1996051600467 19960516 00467 1996 5 16 HEEA967049 4 19960418 A 3453 25410038 7000 CDU BELL 412 412 1182202 SW COCKPIT LORAN DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2261D 33076 TOP LEFT NUMBER BURNED OUT. 1 G 7 2 4U H4SW 1996051600468 19960516 00468 SW 1996 5 16 HEEA967050 1 19960418 A 5520 205030856111 ELEVATOR ASSY BELL 412 412 1182202 SW SPAR FLANGE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2014K 33020 MOUNTING FLANGE THATS BONDED TO SPAR IS CRACKED FROM SPAR TOWARDS OUTER FLANGE. SCRAPPED ELEVATOR ASSEMBLY. 1 G 7 2 4U H4SW 1996051600469 19960516 00469 EU 1996 5 16 HEEA967051 1 19960418 A 7720 10594383 WIRING HARNESS BOLKMS 105 BO105S 5626006 EU ENG TEMP CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5368F S718 PART IS CORRODED. (ENG HARNESS CORRODED) REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1996051600470 19960516 00470 EU 1996 5 16 HEEA967052 1 19960418 A 5320 LONGERON BOLKMS 105 BO105S 5626006 EU ENG PAN CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5368F S718 R/H UPPER AFT ENGINE PAN OUTBOARD LONGERON IS CORRODED THROUGH AND CRACKED OUT AT SEVERAL RIVET HOLES IN THE AREA WHERE THE ECU LINE GOES THROUGH THE ENGINE DECK. THE INNER ALUM. DOUBLERS ARE ALSO CORRODED THROUGH IN THIS AREA. REMOVED TRA NS DECK AFT A-FRAME SUPPORT. REMOVED ENGINE DECK. REMOVED INNER DOUBLERS. REMOVED UPPER OUTBOARD LONGERON. CUT OUT DAMA GED AREA OF LONGERON AND SPLICED. MFG NEW INNER DOUBLERS. MFG NEW ENGINE DECK. REASSEMBLED AREA AS NEEDED. 1 G 7 2 3U H3EU 1996051600471 19960516 00471 1996 5 16 HEEA967053 4 19960418 A 2564 214070943107 LIFE RAFT BELL 214 214ST 1182106 SW EMERG EQUIP WONT INSTALL E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 8045T 28101 COULD NOT INSTALL RAFT. MEASURED OLD RAFT AT APPROX. 9 1/2" AND NEW RAFT MEASURED APPROX. 10 1/2". 2 G 7 2 4U H10SW 1996051600472 19960516 00472 CE 1996 5 16 HEEA967054 1 19960418 A 6121 5485020 ACTUATOR BEECH 200 200BEECH 1152920 CE PROP SYNC FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 30PH BB635 PROP SYNC INOPERATIVE. 1 L 7 2 4T A24CE 1996051600473 19960516 00473 EU 1996 5 16 HEEA967056 1 19960418 A 2150 20475591 TURBINE BOLKMS 105 BO105S 5626006 EU ECU EQUIP SEIZED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 54191 S804 TURBINE WILL NOT ROTATE AND TO COMPLY WITH SB.2200850-21-92019 AND SB.204755-21-92046. 1 G 7 2 3U H3EU 1996051600474 19960516 00474 SW 1996 5 16 HEEA967057 1 19960418 A 3212 206377010 FLOAT BOTTLE BELL 206 206L3 1182108 SW EMERG FLOAT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3116L 51529 SUSPECTED WRAPPING FAILURE. NOTE: WHEN THE FLOAT BOTTLE ASSEMBLY IS DEPRESSURIZED HEAR A LOUD CRACKING NOISE. FURTHE R MORE UPON INSPECTION OF THE CYLINDER; NOTICED BULGES AND DEFORMATION OF THE LINER. ON THIS CYLINDER . ALSO NOTICED C RACKSIN THE PAINT AS INDICATED BY THE RED MARKS. 1 G 7 1 3U H2SW 1996051600475 19960516 00475 SW 1996 5 16 HEEA967058 1 19960418 A 3212 206377010 FLOAT BOTTLE ASS BELL 206 206L1 1182107 SW EMERG FLOAT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5000K 45167 SUSPECT WRAPPING FAILURE. WHEN THE FLOAT BOTTLE ASSEMBLY IS DEPRESSURIZED, HEAR A LOUD CRACKING NOISE. FURTHER MORE UP ON INSPECTION OF THE CYLINDER NOTICED BULGES AND DEFORMATION OF THE LINER. 1 G 7 1 3U H2SW 1996051600476 19960516 00476 SW 1996 5 16 HEEA967059 1 19960418 A 2422 412075101101 INVERTER BELL 412 412 1182202 SW AC SYS INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 22347 36005 INVERTER IS INOPERATIVE. 1 G 7 2 4U H4SW 1996051600477 19960516 00477 SW 1996 5 16 HEEA967060 1 19960418 A 2422 412075101101 INVERTER BELL 412 412 1182202 SW AC SYS FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 22347 36005 INVERTER DOES NOT COME ON LINE. 1 G 7 2 4U H4SW 1996051600478 19960516 00478 1996 5 16 HEEA967061 4 19960418 A 2312 4000106010 CONTROL UNIT C10 BOLKMS 105 BO105S 5626006 EU COCKPIT COMM FUSE BLOWN E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5368F S718 DOES NOT COME ON. REPLACED FUSE F1. REPAIRED. BENCH CHECK GOOD. 1 G 7 2 3U H3EU 1996051600479 19960516 00479 SW 1996 5 16 HEEA967062 1 19960419 A 6320 222040003119 TRANSMISSION BELL 230 230 1182149 SW M/R DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 2561 23009 REPLACEMENT PART INFORMATION LISTED BELOW: 1 EACH, P/N 222-340-044-001, BEARING,S/N J0154, T.T. 2560:55, SPALLED 1 EAC H, P/N 222-040-112-103, SUN GEAR, S/N A187, T.T. 2560:55, GEARTEETH BROKEN 1 EACH, P/N 222-040-079-002, CASE, S/NA268, T .T. 2560:55, CHIPPED AROUND INSERT 2 EACH, P/N 222-340-049-001, RETAINER ASSY, S/N FD582 & FD693, FLAKING 1 EACH, P/N 22 2-040-117-107, GEAR, S/N A267, SEATING SURFACE NOT FULL CONTACT 1 EACH, P/N 222-040-123-001, SHAFT, S/N A188, SEATING SURFACE NOT FULL CONTACT 1 EACH , P/N 222-040-115-101, GEAR, S/N A104, TOOTH CHIPPED 1 EACH, P/N 222-040-131-101, GEAR , S/N A168,SCARRED FROM MATING GEAR 1 EACH, P/N 222-040-062-101, CASE, S/N A190, WORN LINER 1 G 7 2 3U NC H9SW 1996051600480 19960516 00480 EU 1996 5 16 HEEA967064 1 19960419 A 2435 150SG122Q STARTER SNIAS 350 AS350B2 8680813 EU START/GEN DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 6097Z 1446 2820 INTERMITTENT CRANKING. 1 G 7 1 3U H9EU 1996051600481 19960516 00481 GL 1996 5 16 HEEA967065 2 19960422 A 7230 23056634 GEARSHAFT 23051643 SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL SPUR ADAPTER STEPWEAR E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 706AE 675 CAC90094 760275 CAE890071S ENGINE REMOVED DUE TO TURBINE WHEELS CYCLED OUT. UPON INSPECTION OF COMPRESSOR PARTS NOTED THE FOLLOWING: STEP WEAR BE YOND OVERHAUL LIMITS ON SPUR ADAPTER GEARSHAFT FWD AND AFT SPLINES. NEW PART INSTALLED. 1 G 7 2 3U 3 U H1NE E1GL 1996051600482 19960516 00482 SW 1996 5 16 HEEA967066 1 19960423 A 7722 206375007103 INDICATOR BELL 206 206L3 1182108 SW COCKPIT TOT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 32041 51539 NO INDICATION ON TOT INDICATOR WITH EITHER SHIPS POWER OR BARFIELD T-1000. 1 G 7 1 3U H2SW 1996051600483 19960516 00483 GL 1996 5 16 HEEA967067 2 19960423 A 7532 23005366 BLEED VALVE BELL 230 230 1182149 SW ALLSN 250C 250C30G2 03013 GL ENGINE DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 230UN 1382 23009 BLEED VALVE CAUSING ENGINE SURGE DURING POWER CHECK AT 70% TORQUE SINGLE ENGINE. 1 G 7 2 3U 3 U NC H9SW E1GL 1996051600484 19960516 00484 SW 1996 5 16 HEEA967068 1 19960423 A 7714 412075010109 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH STICKS E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 33008 36004 #1 NEEDLE INTERMITTENTLY STICKS THROUGHOUT SCALE; #2 NEEDLE INOPERATIVE. 1 G 7 2 4U H4SW 1996051600485 19960516 00485 SW 1996 5 16 HEEA967069 1 19960423 A 5610 D204513101 BUBBLE WINDOW BELL 212 212 1181420 SW DOOR MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 5736J 31140 DOOR MODIFIED UNDER LIMITED SUPPLEMENTAL TYPE APPROVAL # P-LSH-91-219/D. WILL NOT FIT AIRFRAME. WITH BUBBLE WINDOW INS TALLED PULLS UPPER SECTION OF DOOR AWAY FROM AIRFRAME APPROX. 1 1/2 INCHES. 1 G 7 1 4U H4SW 1996051600486 19960516 00486 1996 5 16 HEEA967070 4 19960423 A 2312 4000106010 CONTROL UNIT C10 BOLKMS 105 BO105S 5626006 EU COCKPIT COMM FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5368F S718 CONTROL UNIT DOES NOT WORK. REPLACED FUSE F1. REPAIRED. FOUND VOLUME TO HAVE DEAD SPOTS WHEN TURNING VOLUME KNOB. REP LACED ON/OFF PONTENTIOMETER R1/S5. REPAIRED. BENCH CHECK GOOD. 1 G 7 2 3U H3EU 1996051600487 19960516 00487 1996 5 16 HEEA967071 4 19960423 A 2312 064105430 TRANSCEIVER BELL 206 206L3 1182108 SW COCKPIT COMM FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 6748D 51106 TRANSMITS BUT DOESN'T RECEIVE. FOUND UNIT WOULD RECEIVE BUT NOT TRANSMIT. REPLACED MODULATORS Q124. REPAIRED. BENCH C HECK GOOD. 1 G 7 1 3U H2SW 1996051600488 19960516 00488 1996 5 16 HEEA967072 4 19960423 A 2312 069102525 TRANSCEIVER KX165 BELL 206 206L1 1182107 SW COCKPIT VHF DISPLAY INOP E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 21240 45647 DISPLAY DOES NOT FUNCTION WHEN IT IS DARK. REPLACED DS101 DISPLAY, REPAIRED. ADJUSTED FREQUENCY, C/W SQUELCH AND SIDETO NE. BENCH CHECK GOOD. 1 G 7 1 3U H2SW 1996051600489 19960516 00489 1996 5 16 HEEA967073 4 19960423 A 3453 066402600 LORAN KLN88 BELL 206 206L1 1182107 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2759U 45267 KNOB AND SHAFT CAME OUT. FOUND SWITCH S202 BROKEN. REPLACED SWITCH SW202 - REPAIRED. UNIT BENCH CHECKS GOOD. 1 G 7 1 3U H2SW 1996051600490 19960516 00490 1996 5 16 HEEA967074 4 19960423 A 3444 066305401 ALTIMETER KI250 BELL 206 206L3 1182108 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 206LS 51070 CRACKED GLASS. REPLACED GASKET AND LENS, REPAIRED. PHOTOCELL IS BAD, REPLACED PHOTOCELL V101. REPAIRED. ANALOG ALTITU DE VOLTAGES OUT OF TOLERANCE, PERFORMED CALIBRATION AND ALIGNMENT, REPAIRED. UNIT BENCH CHECK GOOD. 1 G 7 1 3U H2SW 1996051600492 19960516 00492 1996 5 16 HEEA967077 4 19960423 A 2312 064101902 TRANSCEIVER KY196 BELL 206 206L1 1182107 SW COCKPIT VHF FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5006F 45181 RADIO DOES NOT TRANSMIT OR RECEIVE. TRANSCEIVER DOESN'T TRANSMIT OR RECEIVE. 1 G 7 1 3U H2SW 1996051600494 19960516 00494 1996 5 16 HEEA967079 4 19960425 A 3442 MI5852013 INDICATOR P4001 SKRSKY S76 S76A 8143006 NE RADAR FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5426U 760167 DISPLAY SHRINKS IN SIZE INTERMITTENTLY. VERIFIED UNIT HAS BAD VIDEO BOARD. 1 G 7 2 3U H1NE 1996051600495 19960516 00495 GL 1996 5 16 HEEA967080 2 19960429 A 7230 23056634 GEARSHAFT 23051643 SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL SPUR ADAPTER STEPWEAR E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31219 673 CAC90549 760230 CAE890388S ENGINE REMOVED DUE TO TURBINE CYCLES. UPON INSPECTION OF COMPRESSOR PARTS NOTED THE FOLLOWING: STEP WEAR BEYOND OVERHA UL LIMITS ON AFT SPLINES. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U 3 U H1NE E1GL 1996051600496 19960516 00496 GL 1996 5 16 HEEA967081 2 19960429 A 7250 23032345 N1 COUPLING 23035128 SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL FWD SPLINES STEP WEAR E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31219 673 CAT90576 760230 CAE890388S ENGINE REMOVED DUE TO TURBINE CYCLES. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: STEP WEAR BEYOND OVERHAUL LIMITS IN N1 COUPLING FWD SPLINES. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U 3 U H1NE E1GL 1996051600497 19960516 00497 SW 1996 5 16 HEEA967082 1 19960429 A 6320 204040386001 CASE ASSY 212040001191 BELL 212 212 1181420 SW NR 7 OIL JET DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 ABW45068 #7 OIL JET BORE IMPROPERLY MACHINED, OIL JET WILL NOT FIT. REMOVED FROM CUSTOMER AIRCRAFT N703H. 1 G 7 1 4U H4SW 1996051600498 19960516 00498 1996 5 16 HEEA967083 4 19960429 A 3423 KCA0113W COMPASS SNIAS 350 AS350B2 8680813 EU COCKPIT STDBY ERROR E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 6097Z 1667 2820 COMPASS READS 20 DEGREES OFF AND UNABLE TO ADJUST OUT. 1 G 7 1 3U H9EU 1996051600499 19960516 00499 EU 1996 5 16 HEEA967089 1 19960429 A 6420 350A33211905 BODY SNIAS 350 AS350B2 8680813 EU T/R BEARING WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4000L 116 2873 LAMINATE BEARING FAILED (FORK BEARINGS WORN) 1 G 7 1 3U H9EU 1996051600500 19960516 00500 1996 5 16 HEEA967090 4 19960502 A 2210 214074303115 AMPLIFIER ASSY BELL 214 214ST 1182106 SW AUTO FLIGHT FAULTY E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 8045T 173 28101 ROLL CHANNEL WILLNOT ENGAGE WHEN AMP IS COLD OR HIGH HUMIDITY. 2 G 7 2 4U H10SW 1996051600502 19960516 00502 SW 1996 5 16 HEEA967092 1 19960502 A 6220 206011132113A GRIP 206011100159 BELL 206 206L1 1182107 SW M/R GREASE LEAK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5742N 464 A2467 45477 GREASE LEAKING FROM BOTH GRIPS. S/N A6065&A6067 1 G 7 1 3U H2SW 1996051600503 19960516 00503 SW 1996 5 16 HEEA967093 1 19960502 A 6220 206011132113A GRIP 206011100159 BELL 206 206L1 1182107 SW M/R GREASE LEAK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2764F 1964 A2200 45279 GREASE LEAKING. AT DISASSEMBLY FOUND RETAINERS UNBONDED. REBONDED WITH NEW EXCLUDERS AND ORINGS. S/N A5317 & A5310 1 G 7 1 3U H2SW 1996051600504 19960516 00504 SW 1996 5 16 HEEA967095 1 19960502 A 7722 206375007103 INDICATOR BELL 206 206L3 1182108 SW COCKPIT TOT STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6160Y 3846 51609 NEEDLE STICKS DURING INITIAL ENGINE START. WHEN NEEDLE BREAKS LOOSE MOVEMENT IS ERRATIC. 1 G 7 1 3U H2SW 1996051600505 19960516 00505 GL 1996 5 16 HEEA967096 2 19960502 A 7250 23008064 NOZZLE 23035128 SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL 1ST STAGE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31219 673 CAT90576 760230 CAE890388S ENGINE REMOVED DUE TO CYCLED OUT 1ST AND 2ND STAGE WHEELS. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: CRACK S BEYOND OVERHAUL LIMITS ON OUTER BAND (2 EA) AND 50% OF VANES AT TRAILING EDGE. REPLACED PART. NOTE: FUEL NOZZLE SPRA Y PATTERN CHECKED GOOD. SUBMITTAL FOR CREDIT ACCOMPLISHED ON AFA# 24473A. 1 G 7 2 3U 3 U H1NE E1GL 1996051600515 19960516 00515 CE 1996 5 16 96ZZZX2463 1 19960421 A 3230 57271162 PISTON ASSY CESSNA 402 402C 207590R CE RT MLG UPLOCK WORN A OEZA K NONE O OTHER IN INSP/MAINT 1 WP 19 3283M 12770 S111088 402C0303 INSPECTION FOUND THE HARDENED SURFACE OF PISTON AND ROD WAS WORN OUT BY CHECK BALL S272-5 CAUSING A MALFUNCTION OF THE U PLOCK. IT APPEARS THIS PISTON AND ROD WERE MALFUNCTIONING PREVIOUSLY BECAUSE, AT ONE TIME, IT WAS TURNED 180 DEGREES AN D RE-ASSEMBLED. ALSO, DURING THE INSPECTION, THE LARGER BALL SEAT IN THE 5727110-5 HOUSING WAS NOTICED TO BE DAMAGED AND SOME FLAKES OF HARDENED MATERIAL WERE NOTICED INSIDE THE ACTUATOR. 1 L 7 2 3O A7CE 1996051600571 19960516 00571 SO 1996 5 16 96ZZZX2520 1 19960422 A 3213 8360503 TRUNNION PIPER PA46 PA46310P 7104605 SO RT MLG STRUT SCORED A AMYA K NONE O OTHER IN INSP/MAINT 1 CE 05 355DC 2609 468408079 AFTER LANDING, STRUT WAS FOUND WITH SNAP-RING, WASHER AND BEARING ASSY HAVING FALLEN FROM WITHIN TRUNNION HOUSING. STRU T WAS COCKED TO THE OUTSIDE. NO FLUID OR AIR PRESSURE PRESENT. REMOVED STRUT ASSY AND FOUND SCORE MARK INSIDE TRUNNION . RESEARCHED LOG BOOKS AND FOUND NO ENTRIES OF MAIN LANDING GEAR STRUT WORK. 1 L 7 1 3O A25SO 1996051600576 19960516 00576 WP 1996 5 16 96FDEA00974 1 19960515 A 5400 SPAR CHORD DOUG DC10 DC1030F 3023504 WP NR 1 PYLON SHEARED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 304FE 46992 SNRM 4145, NR 1 PYLON UPPER SPAR WEB STA 363, 1 FASTENER HEAD HAS SHEARED OFF. 2 L 7 3 4F RT A22WE 1996051600577 19960516 00577 WP 1996 5 16 96FDEA00975 1 19960515 A 5400 SPAR CHORD DOUG DC10 DC1030F 3023504 WP NR 3 PYLON SHEARED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 304FE 46992 SNRM 4358, NR 3 PYLON UPPER LT SPAR CHORD AFT AREA EXHIBITS TWO SHEARED HOCK BOLTS HEADS INSIDE PYLON. 2 L 7 3 4F RT A22WE 1996051600578 19960516 00578 WP 1996 5 16 96FDEA00976 1 19960515 A 5311 BELLFRAME DOUG DC10 DC1010CF 3023502 WP BS 919 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68049 47803 SURFACE CORROSION ON BELLFRAME AT STA 919 STR 48L TO 48R. CLEANED OUT CORROSION, FOUND TO BE OUT OF LIMITS. FABRICATED DOUBLER PER SRM 53-30-00 FIG 8L, INSTALLED DOUBLER REPAIR PER SRM 53-30-00 FIG 8. 2 L 7 3 4F RT A22WE 1996051600579 19960516 00579 NM 1996 5 16 96UAL900344 1 19960514 A 3350 LIGHT STRIP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 565UA 26669 EMERGENCY ESCAPE LIGHT FORWARD OF MID LAVATORY INOP. REPLACED EMERGENCY ESCAPE LIGHT STRIP, OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996051600580 19960516 00580 NM 1996 5 16 96UAL900345 1 19960514 A 2421 736664D IDG BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE RIGHT FAILED A UALA O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION NR NOT REPORTED 1 WP 29 617UA 21877 CREW REPORTED RIGHT INTEGRATED DRIVE GENERATOR LIGHT FOLLOWED BY A GENERATOR OFF LIGHT. THE IDG WAS DISCONNECTED. *S/D * OIL LOSS FROM A LEAKING OIL LINE IN THE INTEGRATED DRIVE GENERATOR EXTERNAL COOLING SYSTEM CAUSED THE IDG TO BE DISCO NNECTED. REPLACED INTEGRATED DRIVE GENERATOR AND CARBON SEAL AND RIGHT GENERATOR CONTROL UNIT. 2 L 7 2 4F 4 F RT A1NM E3NE 1996051600581 19960516 00581 NM 1996 5 16 96UAL900346 1 19960514 A 2497 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE MISWIRED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 546UA 25367 DURING A SCHEDULED 4C MAINTENANCE VISIT, A WIRING ANOMALY WAS DISCOVERED. THE IRREGULARITY PREVENTED THE HYDRAULIC MOTO R GENERATOR OUTPUT FROM BEING SUPPLIED IN PARALLEL WITH THE SHIPS BATTERY DURING GENERATOR USAGE. SIMILAR CONDITIONS WE RE FOUND ON AIRCRAFT 5143 AND 5147. IT APPEARS THAT ALL THE AIRCRAFT WERE DELIVERED IN THIS CONDITION. *S/D* CORRECT ED WIRING, CHECKS OK. ISSUED EG ITEM TO CHECK ALL ETOPS AIRCRAFT, CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 1996051600582 19960516 00582 NM 1996 5 16 96UAL900347 1 19960514 A 2782 65445516 ACTUATOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 2 LE FLAP INOPERATIVE A UALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 WP 29 384UA 24659 FLIGHT CREW VISUAL VERIFICATION THAT THE NUMBER TWO LEADING EDGE FLAP WAS HANGING UP IN THE EXTENDED POSITION. *S/D* N UMBER TWO LEADING EDGE FLAP ACTUATOR MALFUNCTIONED. REPLACED ACTUATOR AND SYSTEM CHECKED OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1996051600583 19960516 00583 NM 1996 5 16 96UAL900348 1 19960514 A 3260 835107 DRIVER CARD BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LT MLG FAILED A UALA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 WP 29 606UA 21867 LANDED UNDER AMBER ALERT DUE TO A LEFT MAIN GEAR INDICATION. AN UNEVENTFUL LANDING OCCURRED. SUPPLEMENTAL DATA UPDATE: A FAULTY KORRY SWITCH AND A5 DRIVER CARD FAILURE IN PSEU CAUSED THE WARNING INDICATION. THE KORRY SWITCH AND A5 DRIVE R CARD AT 010 LOCATION SLOT IN PSEU WAS REPLACED. PSEU BITE AND GROUND SYSTEM OPERATIONAL CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 1996051600584 19960516 00584 NM 1996 5 16 DL72E961141 1 19960513 A 5240 FRAME BOEING 727 727247 138408F NM RT AFT SERV DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 283WA 21485 A .375 INCH VISUAL CRACK R-2 DOOR UPPER HINGE CUTOUT AT FWD FRAME. REPAIRED PER SRM 52-40-2. 2 L 7 3 4F A3WE 1996051600585 19960516 00585 NM 1996 5 16 DL72E961142 1 19960513 A 5530 STRINGER BOEING 727 727247 138408F NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 283WA 21485 STRINGER CRACKED INSIDE TAIL CRAWLWAY 3RD BAY FROM TOP LT SIDE. REPAIRED PER MM 55-30-0 FIG 803. 2 L 7 3 4F A3WE 1996051600586 19960516 00586 NM 1996 5 16 DL72E961143 1 19960513 A 5313 65C139133 STRINGER BOEING 727 727247 138408F NM FS 1050-1070 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2829W 21481 UPON REMOVAL OF TIME-LIMITED REPAIR AT HMV, ADDITIONAL DAMAGE HAS BEEN DICOVERED. STRINGER 28R AT STATION 1050 HAS EXTE NSIVE CORROSION AND WILL REQUIRE INSTALLATION OF A SPLICE SECTION. ADDITIONAL CORROSION DAMAGE IS LOCATED APPROXIMATELY 2 INCHES INBOARD AND 2 INCHES FORWARD OF THE EXIST, IN CUTOUT. THE RESULTING CUTOUT IS 4 INCHES BY 5 INCHES BY 0.050 A ND LOCATED APPROXIMATELY 15 INCHES AFT OF THE ORIGINAL DAMAGE LOCATION. 2 L 7 3 4F A3WE 1996051600587 19960516 00587 NM 1996 5 16 DL72K961121 1 19960510 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 7 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 413DA 21233 SKIN ANGLE CRACKED PAST PREVIOUS ROUT OUT BELOW NR 7 SLAT TAI DUCT. REPAIRED PER M/M 57-54-0 PG 807A. 2 L 7 3 4F A3WE 1996051600588 19960516 00588 NM 1996 5 16 DL72K961123 1 19960510 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 3 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 413DA 21233 NR 3 SLAT INBD STOP PAD ANGLE CRACKED. REPAIRED PER M/M 57-54-0 FIG 812. 2 L 7 3 4F A3WE 1996051600589 19960516 00589 NM 1996 5 16 DL72L961133 1 19960512 A 3350 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 512DA 21314 AFT AIRSTAIRS EMERGENCY LIGHT INOP. REMOVED AND REPLACED AFT AIRSTAIRS EMERGENCY LIGHT ASSEMBLY, OPS CHECK NORMAL. 2 L 7 3 4F A3WE 1996051600590 19960516 00590 NM 1996 5 16 DL72L961134 1 19960512 A 3350 BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 512DA 21314 RT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED RT OVERWING EMERGENCY EXIT LIGHT BATTERY PACK, OPS CHECK NORMAL. 2 L 7 3 4F A3WE 1996051600591 19960516 00591 NM 1996 5 16 DL72L961135 1 19960512 A 3350 081691 LIGHT BOEING 727 727232 1384082 NM CABIN FRAYED WIRES A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 505DA 21307 EMERGENCY LIGHTS OUT FROM ROWS 12 TO 19. FOUND FRAYED WIRES RUBBING AT ROW 17. REPLACED BULB SOCKET, FUSES IN M9026 AN D M9027 POWER SUPPLIES, OP CKS NORMAL. 2 L 7 3 4F A3WE 1996051600592 19960516 00592 NM 1996 5 16 DL72L961140 1 19960513 A 3350 1001141 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 502DA 21304 AFT AIRSTAIR EMERGENCY EXIT LIGHT INOP. FWD TO MCO AND PLAC PER MEL 33-00-16, AFTER CHANGING BATTERY AND LIGHT BULBS. 2 L 7 3 4F A3WE 1996051600593 19960516 00593 NM 1996 5 16 DL72P961144 1 19960416 A 5312 6516350344 BULKHEAD WEB BOEING 727 727225 1384077 NM BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8891Z 21860 THE BS 1183 BULKHEAD WEB WAS FOUND CRACKED AT RBL 26. THERE IS A .25 INCH CRACK AT WL 170. THE WEB IS A BONDED ASSEMBL Y OF 2024-T3 CLAD WITH A LOCAL THICKNESS OF .050 INCH. THE CRACK LOCATION IS OUTSIDE OF THE INSPECTION AREA SPECIFIED B Y BOEING SERVICE BULLETIN 727-53-171. THE VERTICAL STIFFENER AT RBL 26, THE TOPIC OF BOEING SERVICE BULLETIN 727-53-018 2, IS NOT DAMAGED. 2 L 7 3 4F A3WE 1996051600594 19960516 00594 NM 1996 5 16 DL72S961109 1 19960508 A 5542 SKIN BOEING 727 727232 1384082 NM RUDDER CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 520DA 21471 A .375 INCH CRACK IN LOWER RUDDER SKIN LT SIDE BELOW 'A' IN DELTA. REPAIRED PER SRM 55-20-3. 2 L 7 3 4F A3WE 1996051600595 19960516 00595 NM 1996 5 16 DL72S961116 1 19960509 A 5330 SKIN BOEING 727 727232 1384082 NM R2 DOOR CUTOUT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 528DA 21702 FOUND ON D-1 LETTER CHECK, R-2 DOOR UPPER FWD HINGE CUTOUT CRACKED ON FUSELAGE SKIN. REPAIRED PER SRM 52-40-2. 2 L 7 3 4F A3WE 1996051600596 19960516 00596 NM 1996 5 16 DL72S961145 1 19960412 A 5312 6516350344 BULKHEAD WEB BOEING 727 727232 1384082 NM BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 407DA 21151 THE BS 1183 BULKHEAD WEB WAS FOUND CRACKED AT RBL 26. THERE IS A 1 INCH CRACK AT WL 170. THE WEB IS A BONDED ASSEMBLY OF 2024-T3 CLAD WITH A LOCAL THICKNESS OF 0.050 INCH. THE CRACK LOCATION IS OUTSIDE OF THE INSPECITON AREA SPECIFIED BY BOEING SERVICE BULLETIN 727-53-171. THE VERTICAL STIFFENER AT RBL 26, THE TOPIC OF BOEING SERVICE BULLETIN 727-53-0182 , IS NOT DAMAGED. THE CRACK WILL BE STOP DRILLED AND A REPAIR DOUBLER INSTALLED. 2 L 7 3 4F A3WE 1996051600597 19960516 00597 NM 1996 5 16 DL72S961146 1 19960505 A 5330 65C139131 SKIN BOEING 727 727232 1384082 NM BS 990 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 527DA 21587 THE FUSELAGE SKIN WAS FOUND CORRODED AT STATION 990 ALONG STRINGER 28R. MAXIMUM LENGTH OF THE CUTOUT IS 7.5 WHILE MAXIM UM WIDTH IS 4.5. THE SKIN IS FABRICATED FROM CLAD 2024-T3 WITH A THICKNESS OF 0.145. 2 L 7 3 4F A3WE 1996051600598 19960516 00598 NM 1996 5 16 DL73S961110 1 19960508 A 3350 20131A BATTERY PACK BOEING 737 737232 1384475 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 334DL 23105 AFT TRACK OF FLOOR EMERENGY EXIT LIGHTS VERY DIM. REPLACED BATT PACK AT M9222 AFT TRACK LIGHTS, NOW OPS TEST OK. 2 L 7 2 4F RT A16WE 1996051600599 19960516 00599 NM 1996 5 16 DL73S961111 1 19960508 A 3350 FUSE BOEING 737 737232 1384475 NM CABIN BLOWN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 322DL 23094 R1 AND L1 DOORS LWR EMERGENCY LIGHTS EXIT IDENT LIGHTS INOP. REPLACED FUSE ON RACK M9221, OPS CHECKS GOOD. 2 L 7 2 4F RT A16WE 1996051600600 19960516 00600 NM 1996 5 16 DL767961119 1 19960510 A 3350 TRACK LIGHTS BOEING 767 767232 1385132 NM CABIN DAMAGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 105DA 22217 EMERGENGY FLOOR TRACK DAMAGED IN SEVERAL AREAS OF CABIN, AT SEATS 28FG, 30FG AND 13FG. REPLACED FLOOR TRACK AT SEATS 28 FG, 30FG AND 13FG, TESTS GOOD. 2 L 7 2 4F RT A1NM 1996051600601 19960516 00601 NM 1996 5 16 DLM88961107 1 19960508 A 3240 BRAKE DOUG MD88 MD88 3023688 NM NR 2 LOCKED UP A DALA A UNSCHED LANDING M OVER TEMP TO TAKEOFF 1 SO 27 955DL 49886 LEFT INBOARD BRAKE OVERHEATED ON TAKEOFF, RETURNED TO ATL. REPLACED NR 2 BRAKE DUE TO BEING LOCKED UP. ALSO, REPLACED BOTH LT MLG WHEEL ASSYS. 2 L 7 2 4F RT A6WE 1996051600602 19960516 00602 NM 1996 5 16 P5CA9600225 1 19960509 A 3350 SI356B37 LIGHT BOEING 747 747123 1384873 NM CABIN MALFUNCTIONED A P5CA K NONE L NO TEST IN INSP/MAINT 1 WP 23 858FT 20109 EMERGENCY LIGHT ABOVE CREW SERVICE DOOR ILLUMINATES WITH EMERGENCY LIGHT SWITCH IN OFF POSITION. REMOVED AND REPLACED E MERGENCY LIGHT ASSEMBLY IAW MM 33-51-00, OPS CHECK NORMAL. 2 L 7 4 4F A20WE 1996051600603 19960516 00603 NM 1996 5 16 P5CA9600226 1 19960509 A 3350 SI356B37 LIGHT ASSY BOEING 747 747123 1384873 NM CABIN INOPERATIVE A P5CA K NONE L NO TEST IN INSP/MAINT 1 WP 23 858FT 20109 FOUND EMERGENCY LIGHT ABOVE CREDENZA LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT ASSY IAW MM 33-51-00, OPS CHECKS NORMAL. 2 L 7 4 4F A20WE 1996051600604 19960516 00604 NM 1996 5 16 P5CA9600227 1 19960508 A 3350 60B400535 POWER SUPPLY BOEING 747 747124 1384874 NM CABIN INOPERATIVE A P5CA K NONE L NO TEST IN INSP/MAINT 1 WP 23 855FT 19733 FOUND CREW SLIDE DOOR EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY ASSY AND RELAMPED IAW MM 33-51-00, OPS CHECK NORMAL. 2 L 7 4 4F A20WE 1996051600605 19960516 00605 NM 1996 5 16 P5CA9600228 1 19960515 A 3230 A42006289400 SOLENOID BOEING 747 747122 1384872 NM COCKPIT FAILED A P5CA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 23 852FT 19757 DURING CRUISE, EXPERIENCED SMOKE IN COCKPIT FOR 4 TO 5 MINUTES. SMOKE DISPERSED ON ITS OWN. UPON LANDING FOUND LANDING GEAR LEVER LOCK CIRCUIT BREAKER POPPED, SOLENOID FAILED. DEFERRED PER MEL 32-16 CATEGORY A, TO BE REPAIRED WITHIN 7 FL IGHT DAYS. 2 L 7 4 4F A20WE 1996051600606 19960516 00606 NM 1996 5 16 SCNA96113 1 19960510 A 3350 EXIT SIGN BOEING 727 7272J4 1384006 NM LOWER AFT ENTRY BROKEN WIRE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 284SC 21438 FOUND LOWER AFT ENTRY EMERGENCY EXIT SIGN NOT FUNCTIONING. REPAIRED A BROKEN WIRE AND OPS CHECKED OK. 2 L 7 3 4F RT A3WE 1996051600607 19960516 00607 NM 1996 5 16 SCNA96114 1 19960513 A 3350 1000677 EXIT LIGHT BOEING 727 7272J4 1384006 NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 284SC 21438 FOUND EMERGENCY OVERHEAD LIGHT AT AFT AIRSTAIR EXIT DOOR INOPERATIVE. REMOVED AND INSTALLED A LIGHT ASSEMBLY IN ACCORDA NCE WITH MM 33-50-01. OPS CHECKED GOOD. 2 L 7 3 4F RT A3WE 1996051600608 19960516 00608 SW 1996 5 16 SWIA95733 1 19960510 A 3310 LIGHTING PANEL SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP GEAR HANDLE OUT OF POSITION A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 2685L AC648 LANDING GEAR WOULD NOT RETRACT. CHECKED CIRCUIT BREAKERS, TRIED OVER RIDE, STILL WOULD NOT RETRACT. EMERGENCY VALVE WA S PINNED AFT. FOUND OVER RIDE BUTTON FOR GEAR HANDLE BINDING ON FROM LIGHTING PANEL CAUSING HANDLE NOT TO MOVE. REPOSI TIONED FRONT PANEL, SWUNG GEAR TEN TIMES AND OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A8SW E4WE 1996051600609 19960516 00609 SO 1996 5 16 SWIA95734 1 19960506 A 3231 LATCH EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT MLG DOOR FAILED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 223SW 120291 AFTER DEPARTURE WITH GEAR UP AND LOCKED, NOTICED LEFT MAIN OUTBOARD GEAR DOOR WAS STILL DOWN. RETURNED AND LANDED AT EK O. REPLACED LEFT OUTBOARD GEAR DOOR LATCH AS REQUIRED, OPS CKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1996051600610 19960516 00610 SO 1996 5 16 SWIA95735 1 19960506 A 2750 3075001007 CONTROL UNIT EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE TE FLAPS MALFUNCTIONED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 07 195SW 120127 AFTER TAKEOFF, FLAPS WOULD NOT RETRACT TO THE FULL UP POSITION, TWO SEGMENTS OUTBOARD, ONE SEGMENT NACELLE, ONE SEGMENT INBOARD, FOUR FLAP DISAGREEMENT INDICATION. CLEANED FLAP TRACK AND ROLLERS. REMOVED AND REPLACED FLAP CONTROL UNIT WIT H SERVICEABLE UNIT. OPERATED FLAPS NUMEROUS TIMES AND OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1996051600611 19960516 00611 SO 1996 5 16 SWIA95736 1 19960504 A 3231 LATCH EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT MLG BROKEN A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 196SW 120151 LEFT INBOARD FORWARD DOOR GEAR LATCH BROKE OFF. ACFT RETURNED TO THE GATE. REMOVED AND REPLACED LEFT INBOARD GEAR DOOR LATCH IAW MM 32-12-01, OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1996051600612 19960516 00612 SO 1996 5 16 SWIA95737 1 19960504 A 3233 1959500007 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT MLG FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 212SW 120276 AFTER DEPARTURE, LEFT MAIN LANDING GEAR WOULD NOT RETRACT. GEAR DOORS SEEMED TO BE OPEN, BUT NOT CLOSING. LANDING GEAR CAME DOWN WITHOUT ANY PROBLEM. REPLACED LEFT GEAR ACTUATOR AND LEFT GEAR SHUTOFF VALUE IAW MM 32-32-11, OPS CHECK AND LEAK CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1996051600613 19960516 00613 EA 1996 5 16 SWIA95738 1 19960502 A 3230 PROX SENSOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE NLG OUT OF ADJUST A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 413SW 7102 AFTER DEPARTURE, NOSE GEAR WOULD NOT RETRACT AND FOLLOWING MESSAGES OBSERVED; RED GEAR DISAGREE AND NOSE DOOR OPEN. NOS E GEAR WAS DOWN AND LOCKED AND NEVER INDICATED AN INTRANSIT LIGHT. ADJUSTED THE NOSE GEAR EXTENDED PROXIMITY SENSOR IAW CRJ MM 32-61-05. PERFORMED GEAR SWINGS AND OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 1996051600614 19960516 00614 SO 1996 5 16 96ZZZM764 1 19960331 A 2710 12027655005 CABLE EMB 120 EMB120RT SO LT AILERON FRAYED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 01 284YV 5578 120284 DURING A 1600 HOUR CONTROL CABLE INSPECTION, FOUND LEFT WING LOWER AILERON CABLE, P/N 12027655-005, WORN WITH BROKEN STR ANDS AT WING STATION Y2902 WHERE CABLE PASSES THROUGH NYLON GROMMET, P/N PE49068-505, AT OUTBOARD NACELLE STRUCTURE. IT APPEARS THAT THE CABLE ROUTING THROUGH THE NACELLE ALLOWS FOR THE CABLE TO RUB CONTINUOUSLY ON THE BULKHEAD GROMMET CAU SING PREMATURE WEAR OF THE CABLE ASSEMBLY. 2 L 7 2 4T RT A31SO 1996051600615 19960516 00615 NE 1996 5 16 96ZZZM765 2 19960320 A 7321 7425111 MOISTURE TRAP DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3B 52039 NE NR 2 ENG FCU FULL A C1HA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 23 802MG 46098 669726 ON TAKEOFF ROLL AT 95 KNOTS NR 2 ENGINE COMPRESSOR STALLED THREE. ABORTED TAKEOFF WITHOUT INCIDENT. INSPECTED NR 2 ENG INE BLEED SYSTEM OK, PBRC OK. OK ENG EXHAUST AND INLET CHECK OK. FOUND MOISTURE TRAP FULL ON FCU. CLEANED AS REQUIRED , PERFORMED ENGINE GROUND RUN IAW CHAP 71MM. GROUND OPS CHECK GOOD. (M) 2 L 7 4 4F 4 F 4A25 1E8 1996051600616 19960516 00616 NE 1996 5 16 96ZZZM766 2 19960331 A 7250 TURBINE BOEING 727 727231 1384079 NM PWA JT8 JT8D9 52048 NE NR 2 ENGINE FAILED A A TWAA O OTHER Y ENGINE STOPPAGE TO TAKEOFF 1 CE 05 84355 21987 SLC - DURING TAKEOFF NR 2 ENGINE, S/N 1548, SUFFERED A TURBINE FAILURE. ENGINE TOTAL TIME 33,348. TOTAL CYCLES 21,618. 2 L 7 3 4F 4 F A3WE E2EA 1996051600617 19960516 00617 NM 1996 5 16 96ZZZM767 1 19960329 A 2530 OVEN BOEING 727 727231 1384079 NM GALLEY SMOKING A TWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 54354 21986 ONT - DURING CRUISE SMOKE WAS OBSERVED INSIDE REAR GALLEY OVEN. OVEN WAS OPENED AND A SMOKING PIECE OF PAPER/NAPKIN WAS REMOVED FROM THE OVEN. MAINTENANCE CLEANED AND CHECKED OVEN FOR PROPER OPERATION. (M) 2 L 7 3 4F A3WE 1996051600618 19960516 00618 NM 1996 5 16 96ZZZM768 1 19960329 A 2781 10608198 FLAP SWITCH BOEING 727 727231 1384079 NM NR 6 LE FLAP FAILED A TWAA K NONE N FALSE WARNING CL CLIMB 1 CE 05 54344 21631 ATL - DURING CLIMB NR 6 LEADING EDGE FLAP INTRANSIT LIGHT ILLUMINATED. REMOVED AND REPLACED NR 6 LEADING EDGE FLAP SWIT CH, MFG P/N 10-60819-8. OPERATIONAL CHECK NORMAL. 2 L 7 3 4F A3WE 1996051600619 19960516 00619 NM 1996 5 16 96ZZZM769 1 19960325 A 5510 STRINGER BOEING 767 767231 1385131 NM HORIZ STAB DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 601TW 22564 DURING SPECIAL CHECK, FOUND LOWER HORIZONTAL STABILIZER STRINGER 5L DAMAGED AT STATION 300. REPAIRED PER SRM 55-10-03, FIGURE 101, DETAIL NR 1 AND TWA STANDARD PRACTICES. 2 L 7 2 4F RT A1NM 1996051600620 19960516 00620 WP 1996 5 16 96ZZZM770 1 19960325 A 7930 OIL CLOG LIGHT DOUG DC9 DC915 3022036 WP NR 1 ENGINE ILLUMINATED A TWAA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 CE 05 971Z 45773 DURING CLIMB NR 1 ENGINE, S/N 3810, WAS SHUT DOWN DUE TO OIL STRAINER CLOG LIGHT ILLUMINATION. ENGINE TOTAL TIME 39,869 , TOTAL CYCLES 46,939. 2 L 7 2 4F A6WE 1996051600621 19960516 00621 NM 1996 5 16 96ZZZM771 1 19960313 A 5753 RIB BOEING 747 747257B 1384853 NM RT TE FORE FLAP CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 303TW 20116 DURING OP-16, FOUND A 6 INCH CRACK IN RIGHT INBOARD FOREFLAP INBOARD RIB, AND FOUND CRACK IN ANGLE. REPAIRED BY REPLACI NG RIB AND ANGLE PER SRM 50-10-01 AND TWA STANDARD PRACTICES. 2 L 7 4 4F A20WE 1996051600622 19960516 00622 NM 1996 5 16 96ZZZM772 1 19960325 A 5720 HAT SECTION BOEING 727 727231 1384079 NM WS 601.5 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 52311 19830 DURING C-CHECK, FOUND CRACK ON FORWARD TANG OF HAT SECTION, RIGHT WING WS 601.5. REPAIRED PER SSRM 57-20-201 AND TWA ST ANDARD PRACTICES. (M) 2 L 7 3 4F A3WE 1996051600623 19960516 00623 NM 1996 5 16 96ZZZM773 1 19960325 A 5320 HAT SECTION BOEING 727 727231 1384079 NM WS 656.5 BROKEN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 52311 19830 DURING C-CHECK, FOUND TANG BROKEN OFF, AFT SIDE OF HAT SECTION, WING STATION 656.5. REPAIRED PER SRM 57-20-201, FIGURE 214. (M) 2 L 7 3 4F A3WE 1996051600624 19960516 00624 NM 1996 5 16 96ZZZM774 1 19960325 A 5720 DOUBLER BOEING 727 727231 1384079 NM WS 686.5 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 52311 19830 DURING C-CHECK, FOUND DOUBLER CRACKED ON WING RIB AT STATION 686.5 AND STRINGER 1. REPAIRED BY REPLACING DOUBLER PER SR M 57-10-5. 2 L 7 3 4F A3WE 1996051600625 19960516 00625 NM 1996 5 16 96ZZZM775 1 19960322 A 5200 SKIN BOEING 747 747257B 1384853 NM NR 32 DOOR CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 303TW 20116 DURING OP-16, FOUND THREE CRACKS OVER ONE INCH LONG ON LOWER FORWARD CORNER OF NR 32 DOOR OUTER SKIN AND TWO CRACKS ON I NNER SKIN. INSTALLED DOUBLER REPAIR PER SSRM 53-30-303 AND TWA STANDARD PRACTICES. (M) 2 L 7 4 4F A20WE 1996051600626 19960516 00626 NM 1996 5 16 96ZZZM776 1 19960325 A 5510 STRINGER BOEING 767 767231 1385131 NM HORIZ STAB CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 601TW 22564 DURING SPECIAL CHECK, FOUND CRACK IN LOWER HORIZONTAL STABILIZER STRINGER 6L, STATION 290. REPAIRED PER SRM 55-10-03, F IGURE 101, DETAIL NR 1 AND TWA STANDARD PRACTICES. 2 L 7 2 4F RT A1NM 1996051600627 19960516 00627 NM 1996 5 16 96ZZZM777 1 19960325 A 5313 STRINGER BOEING 767 767231 1385131 NM BS 1582-1660 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 601TW 22564 DURING SPECIAL CHECK, FOUND FUSELAGE STRINGERS 16, 17L, 18L AND 19L, DENTED AND CRACKED, FS 1582 TO FS 1660. REPAIRED P ER ARA 9958 AND SRM 53-00-03, PAGE 201, FIGURE 201. (M) 2 L 7 2 4F RT A1NM 1996051600628 19960516 00628 NM 1996 5 16 96ZZZM778 1 19960325 A 5510 STRINGER BOEING 767 767231 1385131 NM HORIZ STAB DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 601TW 22564 DURING SPECIAL CHECK, FOUND LOWER HORIZONTAL STABILIZER DAMAGE AT STATION 304, STRINGER 7L. REPAIRED PER SRM 55-10-03, PAGE 101, DETAIL NR 1 AND TWA STANDARD PRACTICES. 2 L 7 2 4F RT A1NM 1996051600629 19960516 00629 WP 1996 5 16 96ZZZM779 1 19960325 A 3260 WARNING LIGHTS LKHEED 1011 10113851 5265010 WP GEAR DOORS ILLUMINATED A TWAA O OTHER N FALSE WARNING CR CRUISE 1 CE 05 11004 193B1016 DURING CRUISE GEAR DOOR LIGHTS ILLUMINATED. CHECKED GEAR DOOR SENSOR GAPS, FOUND WITHIN LIMITS AND RESEATED PROXIMITY C ARDS. GROUND CHECKS NORMAL. 2 L 7 3 4F A23WE 1996051600630 19960516 00630 WP 1996 5 16 96ZZZM780 1 19960323 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 699 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 978Z 47250 DURING C-CHECK, FOUND .5 INCH CRACKS AT UPPER AND LOWER LEGS OF LONGERON 5L, STATION 699. REPAIRED PER SRM 53-02, FIGUR E 2. 2 L 7 2 4F A6WE 1996051600631 19960516 00631 WP 1996 5 16 96ZZZM781 1 19960323 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 688 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 978Z 47250 DURING C-CHECK, FOUND .5 INCH CRACKS IN UPPER AND LOWER LEGS OF LONGERON 6L, STATION 688. REPAIRED PER SRM 53-02, FIGUR E 2. (M) 2 L 7 2 4F A6WE 1996051600632 19960516 00632 WP 1996 5 16 96ZZZM782 1 19960308 A 5315 FLOORBEAM DOUG DC9 DC931 3022065 WP BS 980 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 981Z 47345 DURING OP-15, FOUND CORROSION AROUND TWO ADJACENT NUT PLATES UPPER CAP, FLOORBEAM STATION 980, INBOARD OF CUSP ANGLE. R EMOVED CORRODED AREAS AND INSTALLED REPAIR PER SRM 53-05, FIGURE 20A. 2 L 7 2 4F A6WE 1996051600633 19960516 00633 WP 1996 5 16 96ZZZM783 1 19960307 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 400 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 981Z 47345 DURING OP-15, FOUND CORROSION AT LONGERON SPLICE OF LONGERON 30, STATION 400. REPAIRED BY INSTALLING NEW SECTION OF LON GERON PER ARA 10074 AND SRM 53-07, FIGURE 14. (M) 2 L 7 2 4F A6WE 1996051600634 19960516 00634 WP 1996 5 16 96ZZZM784 1 19960305 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 160 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 981Z 47345 DURING OP-15, FOUND A ONE INCH CRACK IN E/E COMPARTMENT, STATION 160, LONGERON 25L, AT ATTACH POINT. REPAIRED PER SRM 5 3-02, PAGE 2A, FIGURE 2. 2 L 7 2 4F A6WE 1996051600635 19960516 00635 WP 1996 5 16 96ZZZM785 1 19960302 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 617 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 981Z 47345 DURING OP-15, FOUND A .75 INCH CRACK IN LONGERON 4R, STATION 617. REPAIRED BY INSTALLING NEW SECTION OF LONGERON PER SR M 53-04. 2 L 7 2 4F A6WE 1996051600636 19960516 00636 WP 1996 5 16 96ZZZM786 1 19960302 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 699/737 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 981Z 47345 DURING OP-15, FOUND TWO CRACKS IN LONGERON 5R, .5 INCH AT STATION 699, AND .25 INCH AT STATION 737. REPAIRED BOTH PER S RM 53-02, FIGURE 2. 2 L 7 2 4F A6WE 1996051600637 19960516 00637 WP 1996 5 16 96ZZZM787 1 19960324 A 3260 833605 PROX COMPUTER DOUG DC9 DC982 3022082 WP LT MLG FAILED A TWAA O OTHER N FALSE WARNING CL CLIMB 1 CE 05 912TW 49183 AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, THE LEFT MAIN LANDING GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED. RECYCL E LANDING GEAR, FOUND INTERNAL MALFUNCTION IN LANDING GEAR WARNING PROXIMITY COMPUTER, MFG P/N 8-336-05. REPLACED PROXI MITY COMPUTER AND LANDING GEAR WARNING SYSTEM CHECKED NORMAL. 2 L 7 2 4F A6WE 1996051600638 19960516 00638 WP 1996 5 16 96ZZZM788 1 19960320 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 200 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 981Z 47345 DURING OP-15, FOUND A .75 INCH CRACK AT BELT RING ATTACH POINT OF LONGERON 23L, STATION 200. REPAIRED BY INSTALLING NEW LONGERON PER SRM 53-02, FIGURE 2. 2 L 7 2 4F A6WE 1996051600639 19960516 00639 WP 1996 5 16 96ZZZM789 1 19960320 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 190 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 981Z 47345 DURING OP-15, FOUND .75 INCH CRACK IN LONGERON 22L AND CORROSION AT STATION 190. REPAIRED BY INSTALLING NEW LONGERON AN D HI-LOKS IN LONGERON 22L PER SRM 53-02, FIGURE 2. 2 L 7 2 4F A6WE 1996051600641 19960516 00641 WP 1996 5 16 96ZZZM791 1 19960313 A 5412 BLKHD WEB DOUG DC9 DC931 3022065 WP BS 965 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 981Z 47345 DURING OP-15, FOUND A SIX INCH CRACK AT LOWER OUTBOARD CORNER OF RIGHT FORWARD ENGINE MOUNT BULKHEAD WEB, STATION 965. R EPAIRED PER SRM 53-03, FIGURE 21. 2 L 7 2 4F A6WE 1996051600642 19960516 00642 WP 1996 5 16 96ZZZM792 1 19960312 A 5400 ANGLE DOUG DC9 DC931 3022065 WP BS 980 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 981Z 47345 DURING OP-15, FOUND .75 INCH CRACK IN LEFT PYLON ATTACHED ANGLE VERTICAL LEG TOP SIDE, STATION 980. STOP DRILLED CRACK AND REPAIRED PER SRM 54-04. 2 L 7 2 4F A6WE 1996051600643 19960516 00643 WP 1996 5 16 96ZZZM793 1 19960321 A 3350 CONNECTOR DOUG DC9 DC932 3022066 WP CABIN LOOSE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 995Z 47027 DURING CRUISE EGRESS LIGHTING IN AFT CABIN WOULD ILLUMINATE. CYCLED SWITCH OFF AND BACK TO ARMED. FOUND CONNECTOR AT P OWER SUPPLY, NOT FIRMLY CONNECTED. RESEATED CONNECTOR AT POWER SUPPLY AND EGRESS LIGHTING SYSTEM OPERATION CHECK NORMAL . 2 L 7 2 4F A6WE 1996051600644 19960516 00644 WP 1996 5 16 96ZZZM794 1 19960322 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 995Z 47027 DURING CRUISE, EGRESS LIGHT AT SEAT ROW 15 THROUGH 19 ILLUMINATED. FOUND BATTERY PACK WEAK. REPLACED BATTERY PACK AND EGRESS LIGHTS OPERATION CHECKED NORMAL. 2 L 7 2 4F A6WE 1996051600645 19960516 00645 NM 1996 5 16 96ZZZM795 1 19960321 A 3230 RETRACT MECH BOEING 727 727231 1384079 NM NLG LACK OF LUBE A TWAA O OTHER J WARNING INDICATION AP APPROACH 1 CE 05 54337 20491 DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, NOSE LANDING GEAR DID NOT EXTEND. CYCLED LANDING GEAR. LUBRICATED NOSE LANDING GEAR TRUNNIONS AND DRAG BRACE. NOSE LANDING GEAR CHECKED NORMAL. 2 L 7 3 4F A3WE 1996051600646 19960516 00646 WP 1996 5 16 96ZZZM796 1 19960401 A 3350 58222 POWER SUPPLY DOUG DC9 DC941 302207N WP CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 934L 47618 DURING CRUISE THE EMERGENCY EGRESS LIGHTS ILLUMINATED. REMOVED AND REPLACED THE POWER SUPPLY, MFG P/N 5822-2. OPERATIO NAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996051600647 19960516 00647 WP 1996 5 16 96ZZZM797 1 19960401 A 2120 AIR DISTRIBUTION DOUG DC9 DC982 3022082 WP COCKPIT SMOKE A TWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 CE 05 950U 49230 DURNG DESCENT, SMOKE FROM AN UNDETERMINED SOURCE APPEARED IN THE COCKPIT AND CABIN. PERFORMED MD9-21-02 AIR CONDITIONIN G DUCT OIL CONTAMINATION CHECK, AND MD9-49-04 APU AND ECS PERFORMANCE CHECK, ALL CHECKS NORMAL. 2 L 7 2 4F A6WE 1996051600648 19960516 00648 NM 1996 5 16 96ZZZM798 1 19960216 A 5330 SKIN BOEING 737 7372H5 138448E NM FS 727 DAMAGED A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 221US 58141 20454 CLT - INSPECTION FOUND 2 PREVIOUSLY INSTALLED DOUBLERS WITH BLIND FASTENERS LOCATED AT FUSELGE SKIN, FS 727A AT STRINGER 15R AND 16R. INSTALLED EXTERNAL DOUBLER AS PER BOEING SRM 53-30-3 FIG 6 AND USAIR EA NR 24906. (M) 2 L 7 2 4F A16WE 1996051600649 19960516 00649 WP 1996 5 16 96ZZZM799 1 19960401 A 3350 58222 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 981Z 47345 DURING A PREFLIGHT CHECK OF THE EMERGENCY EGRESS LIGHTS, THEY REMAINED ILLUMINATE. REMOVED AND REPLACED EGRESS POWER SU PPLY, MFG P/N 5322-2. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996051600650 19960516 00650 NM 1996 5 16 96ZZZM800 1 19960330 A 2910 AE100880912030 HYD LINE BOEING 727 727231 1384079 NM LT MLG FAILED A TWAA O OTHER K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 CE 05 54350 21969 DURING TAKEOFF LEFT MAIN LANDING GEAR ACTUATOR TOP SIDE HYDRAULIC LINE FAILED. REMOVED AND REPLACED HYDRAULIC LINE, MFG P/N AE100880912030. PRESSURIZED SYSTEM, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996051600651 19960516 00651 WP 1996 5 16 96ZZZM801 1 19960331 A 7930 42D1091A BYPASS SW DOUG DC9 DC983 3022083 WP NR 1 ENG FAILED A TWAA O OTHER N FALSE WARNING DE DESCENT 1 CE 05 110HM 49787 DURING DESCENT NR 1 ENGINE OIL SCREEN CLOG LIGHT ILLUMINATED. REMOVED AND REPLACE ENGINE OIL FILTER GYPASS SWITCH, MFG P/N 42D109-1A. ALL FILTERS CHECKED OK. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1996051600652 19960516 00652 NM 1996 5 16 96ZZZM802 1 19960313 A 5730 PANEL BOEING 747 747257B 1384853 NM RT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 303TW 20116 DURING OP-16, FOUND A 23 INCH CRACK AT RIGHT WING TOP, IN LEADING EDGE PANEL, AFT OF CENTER OF NR 18 LEADING EDGE FLAP. REPAIRED PER SRM 51-40-12 AND TWA STANDARD PRACTICES. 2 L 7 4 4F A20WE 1996051600653 19960516 00653 1996 5 16 96ZZZM803 4 19960131 A 3197 1KU26 WIRE BAG ATP ATP EU LT MLG WW CHAFED A UF6A C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 31 853AW 9870 2022 ORD - FLT 5020 - TAKEOFF CONFIGURATION WARNING ON TAKEOFF. MAINTENANCE REPAIRED CHAFED WIRE IN LEFT GEAR BAY. SYSTEM O PS CHECK GOOD. (M) 2 L 7 2 4T RT A27NM 1996051600654 19960516 00654 NM 1996 5 16 ASAA9610047 1 19960408 A 3230 65446916 NLG MODULE BOEING 737 737290C 138448V NM NLG DEFECTIVE A ASAA O OTHER J WARNING INDICATION CL CLIMB 1 NM 01 730AS 22577 OTZ - FLT NR 52 - ON DEPARTURE FROM OTZ, NOSE LANDING GEAR WOULD NOT RETRACT. SLOWED TO 140 KNOTS, CYCLED GEAR AND NOSE GEAR CAME UP. NORMAL INDICATION FOR REMAINDER OF FLIGHT AND AIRCRAFT LANDED IN ANC WITHOUT INCIDENT. REPLACED NOSE LA NDING GEAR MODULE, COMPLETED GEAR SWING AND GEAR OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1996051600655 19960516 00655 NM 1996 5 16 ASAA9610051 1 19960413 A 3350 883200312 RECEIVER BOEING 737 737210C 1384459 NM CABIN INOP A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROW 16. REMOVED A ND REPLACED THE EMERGENCY TRACK LIGHT RECEIVER AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1996051600656 19960516 00656 NM 1996 5 16 ASAA9640025 1 19960411 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN SEPARATED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 771AS 25104 JNU - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 15 THROUGH 18 . RECONNECTED SEPARATED WIRES AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996051600657 19960516 00657 NM 1996 5 16 ASAA9640026 1 19960412 A 3397 WIRE BOEING 737 7374Q8 138447Q NM FWD CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 763AS 25100 JNU - DURING MAINTENANCE CHECK, THE FORWARD TWO RED EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNEC TED WIRES AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996051600658 19960516 00658 NM 1996 5 16 ASAA9640027 1 19960413 A 3230 BACC18Z3R CIRCUIT BREAKER BOEING 737 7374Q8 NM COCKPIT POPPED A ASAA O OTHER J WARNING INDICATION CL CLIMB 1 NM 01 756AS 25097 SEA - FLT 491 - AFTER TAKEOFF FROM SJC, THE GEAR HANDLE WOULD NOT MOVE UP PAST OFF. CREW COMPLETED CHECKLIST AND GEAR W AS RAISED. CREW NOTICED THAT THE LANDING GEAR LATCH AND PRESS WARNING CIRCUIT BREAKER WAS POPPED AND RESET SAME. AIRCR AFT LANDED IN SEA WITHOUT INCIDENT. MAINTENANCE COULD NOT DUPLICATE PROBLEM ON GROUND, SUSPECT CIRCUIT BREAKER CAUSED T HE ORIGINAL DISCREPANCY. CIRCUIT BREAKER REPLACED AS PRECAUTIONARY. AIRCRAFT RELEASED. (M) 2 L 7 2 4F RT A16WE 1996051600659 19960516 00659 NM 1996 5 16 ASAA9640028 1 19960413 A 3397 WIRE BOEING 737 7374Q8 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 756AS 25097 SEA - DURING MAINTENANCE CHECK, THE AFT 2 RED EMERGENCY TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRES AN D THE LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996051600660 19960516 00660 WP 1996 5 16 ASAA9680094 1 19960409 A 3260 833703 PROX SENSOR DOUG DC9 DC983 3022083 WP NLG OUT OF ADJUST A ASAA O OTHER N FALSE WARNING AP APPROACH 1 NM 01 973AS 53449 ANC - FLIGHT 113, CREW REPORTED THE NOSE LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR EXTENDED FOR LANDING. ACCOMPLISHED GEAR UNSAFE LIGHT CHECK LIST AND LANDED WITHOUT INCIDENT. UNSAFE LIGHT EXTINGUISHED ON TOUCHDOWN. ADJUS TED NOSE LANDING GEAR PROXIMITY SENSOR AND ACCOMPLISHED RETRACTION/EXTENSION TEST AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996051600661 19960516 00661 WP 1996 5 16 ASAA9680096 1 19960414 A 3350 41B004AD07G3 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 963AS 53077 SEA - DURING MAINTENANCE CHECK, ALL CABIN OVERHEAD EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996051600662 19960516 00662 WP 1996 5 16 ASAA9680097 1 19960414 A 3350 6011779 POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 963AS 28108 53077 SEA - DURING MAINTENANCE CHECK, THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPL Y AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996051600663 19960516 00663 WP 1996 5 16 ASAA9680098 1 19960414 A 3350 1001191 PORTABLE LIGHT DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 974AS 25924 53450 SEA - DURING MAINTENACNE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996051600664 19960516 00664 WP 1996 5 16 ASAA9680099 1 19960415 A 3350 D29982107 EMERG EVAC SLIDE DOUG DC9 DC983 3022083 WP L1 DOOR FAILED LIGHT TES A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 972AS 53448 OAK - DURING C-CHECK, THE L1 DOOR EMERGENCY EVACUATION SLIDE EMERGENCY LIGHTS FAILED TEST. REPLACED THE L1 DOOR EMERGEN CY EVACUATION SLIDE. (M) 2 L 7 2 4F RT A6WE 1996051600665 19960516 00665 NM 1996 5 16 AWXA960161 1 19960331 A 5630 140N20351 PRISM WINDOW BOEING 757 7572S7 1384962 NM L-4 DOOR CRAZED A AWXA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 28 903AW 23323 PHX-JFK - AIR TURNBACK, IN FLIGHT CREW REPORTS, THE L-4 DOOR WINDOW APPEARS CRACKED. CAPTAIN AGREED AND ELECTED TO RETU RN TO PHOENIX. VIEWER WINDOW IN EXIT L-4 CRAZED DURING CLIMB. REMOVED AND REPLACED L-4 DOOR PRISM WINDOW. (M) 2 L 7 2 4F RT A2NM 1996051600666 19960516 00666 NM 1996 5 16 AWXA960162 1 19960328 A 5330 SKIN BOEING 757 757225 1384959 NM BS 620 DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 915AW 22209 PAE - FLIGHT 3838 - DURING ROUTINE SCHEDULED C-3 MAINTENANCE CHECK, FOUND A TEMPORARY REPAIR INSTALLED AT BS 620, .5 INC H BELOW STRINGER 16L. REMOVED TEMPORARY REPAIR, FABRICATED EXTERNAL DOUBLER AND REPAIR PARTS PER ENGINEERING REPAIR NR 5-53-33-01 AND INSTALLED. (M) 2 L 7 2 4F RT A2NM 1996051600667 19960516 00667 NM 1996 5 16 AWXA960164 1 19960328 A 5347 SEAT TRACK BOEING 757 757225 1384959 NM BS 373 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 915AW 22209 PAE - FLT 3838 - DURING ROUTINE SCHEDULED C-3 MAINTENANCE CHECK, FOUND CORROSION ON SEAT TRACK BS 373, RBL 25, WL 208. R EMOVED CORRODED SEAT TRACK. FABRICATED AND INSTALLED SEAT TRACK IAW SRM 51-40-02. (M) 2 L 7 2 4F RT A2NM 1996051600668 19960516 00668 NM 1996 5 16 AWXA960166 1 19960328 A 5320 INTERCOSTAL BOEING 757 757225 1384959 NM BS 350-365 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 915AW 22209 PAE - FLT NR 3838 - DURING ROUTINE SCHEDULED C-3 MAINTENANCE CHECK, FOUND CORROSION ON INTERCOSTAL STATION 350 - STATION 365, LBL 60 WL 208. REMOVED CORRODED INTERCOSTAL STATION 350-365, LBL 60, WL 208. (M) 2 L 7 2 4F RT A2NM 1996051600669 19960516 00669 NM 1996 5 16 AWXA960167 1 19960328 A 5347 SEAT TRACK BOEING 757 757225 1384959 NM BS 377 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 915AW 22209 PAE - FLT NR 3838 - DURING ROUTINE SCHEDULED C-3 MAINTENANCE CHECK, FOUND CORROSION ON SEAT TRACK STATION 377, LBL 45, W L 208. REMOVED SEAT TRACK STATION 377 - STATION 428, LBL 45, WL 208 AND INSTALLED NEW PART PER SRM 53-00-52, SRM 51-20- 01, SRM 51-40-08 AND SRM 51-40-02. (M) 2 L 7 2 4F RT A2NM 1996051600670 19960516 00670 NM 1996 5 16 AWXA960168 1 19960328 A 5347 SEAT TRACK BOEING 757 757225 1384959 NM BS 377 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 915AW 22209 PAE - DLT NR 3838 - DURING ROUTINE SCHEDULED C-3 MAINTENANCE CHECK, FOUND CORROSION ON SEAT TRACK STATION 377, LBL 25, W L 208. REMOVED CORRODED SEAT TRACK STATION 377-428, LBL 25, WL 208 AND INSTALLED NEW PART PER SRM 53-00-52, SRM 51-20-0 1, SRM 51-40-08 AND SRM 51-40-02. (M) 2 L 7 2 4F RT A2NM 1996051600671 19960516 00671 NM 1996 5 16 AWXA960169 1 19960328 A 5315 FLOORBEAM BOEING 757 757225 1384959 NM BS 350 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 915AW 22209 DURING ROUTINE SCHEDULED C-3 MX CHECK, FOUND CORROSION ON FLOORBEAM AT STATION 350, RBL 2-LBL 20, WL 208. REPAIR AREAS OF FLOORBEAM THAT ARE OUT OF LIMITS WITH REPAIR ANGLE AND FILLERS PER SRM 53-00-51. ALODINE, PRIME AND INSTALL WET WITH SEALANT. (M) 2 L 7 2 4F RT A2NM 1996051600672 19960516 00672 NM 1996 5 16 AWXA960170 1 19960328 A 5315 FLOORBEAM BOEING 757 757225 1384959 NM BS 365 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 915AW 22209 FLT NR 3838 - PAE - DURING ROUTINE SCHEDULED C-3 MAINTENANCE CHECK, FOUND CORROSION ON FLOORBEAM UPPER CHORD STATION 365 , BL 0 TO RBL 60, WL 208. BLENDED CORROSION, FOUND OUT OF LIMITS. FABRICATED REPAIR CHORD AND ANGLES. ALODINED AND PR IMED PER SRM 53-00-51. INSTALLED WET WITH SEALANT. (M) 2 L 7 2 4F RT A2NM 1996051600673 19960516 00673 NM 1996 5 16 AWXA960171 1 19960328 A 5320 SUPPORT BOEING 757 757225 1384959 NM BS 960 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 915AW 22209 PAE - FLT NR 3838 - DURING ROUTINE SCHEDULED C-3 MAINTENANCE CHECK, FOUND SUPPORT STRUCTURE T-FRAME HAS CORROSION, STATI ON 960, BL 0, WL 133. FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 53-40-12. (M) 2 L 7 2 4F RT A2NM 1996051600674 19960516 00674 NM 1996 5 16 AWXA960172 1 19960328 A 5230 CLIP BOEING 757 757225 1384959 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 915AW 22209 FLT NR 3838 - PAE - DURING ROUTINE SCHEDULED C-3 MAINTENANCE CHECK, FOUND FORWARD CARGO DOOR FORWARD END OF DOOR FRAME N R 3, FRAME CLIP FROM BOTTOM OF DOOR IS CRACKED IN RADIUS. REMOVED CRACKED FRAME CLIP AND FABRICATED PER SRM 51-30-01, A LODINED, PRIMED AND APPLIED SEALANT AND INSTALLED FASTENERS PER SRM 51-40-02, SRM 51-31-01. (M) 2 L 7 2 4F RT A2NM 1996051600675 19960516 00675 NM 1996 5 16 AWXA960173 1 19960404 A 7312 B10010 P1 PROBE BOEING 757 757225 1384959 NM LT ENGINE FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 915AW 22209 PHX-JFK - LEFT ENGINE PROBE HEAT STATUS MESSAGE. FOUND BURNT PINS ON CONNECTOR D1498. REMOVED AND REPLACED P1 PROBE PE R MM 73-21-04. RETERMINATED D1498. REMOVED AND REPLACED RELAYS K10478 AND K10308. PROBE LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 1996051600676 19960516 00676 NM 1996 5 16 AWXA960179 1 19960408 A 7933 162GL802 OIL TEMP IND BOEING 737 7372U9 1384498 NM NR 2 ENGINE FAILED A AWXA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 WP 28 149AW 162GL802 22575 FLT 445 - PHX - GATE RETURN FOR NR 2 ENGINE OIL TEMPERATURE INDICATOR PEGGING OUT. TEMPERATURE INDICATOR INSTALLED AT E NGINE CHANGE WAS BAD FROM STOCK. REMOVED AND REPLACED TEMPERATURE INDICATOR AND RAN ENGINE. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996051600677 19960516 00677 EU 1996 5 16 AWXA960193 1 19960413 A 2700 3945122502 ELAC AIRBUS 320 A320231 3930325 EU NR 1 FAILED A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 624AW 5136 55 PHX - FLT 845 - ABORTED TAKEOFF, ELAC PITCH TRIM FAULT. REMOVED AND REPLACED ELEVATOR AILERON COMPUTER. (M) 2 L 7 2 4F RT A28NM 1996051600678 19960516 00678 WP 1996 5 16 GRAA9623 1 19960405 A 3350 20131A POWER SUPPLY DOUG DC9 DC987 3022087 WP CABIN INOPERATIVE A GRAA K NONE L NO TEST IN INSP/MAINT 1 WP 11 1075T 49724 LINE MAINTENANCE AT RNO, DISCOVERED THE FORWARD EMERGENCY FLOOR LIGHT LIGHT STRIP INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT POWER SUPPLY. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE SYSTEM. THE EMERGEN CY FLOOR LIGHT SYSTEM OPERATED NORMALLY. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A6WE 1996051600679 19960516 00679 WP 1996 5 16 GRAA9624 1 19960406 A 3350 BC50444105 LENS DOUG DC9 DC987 3022087 WP CABIN MISSING A GRAA K NONE O OTHER IN INSP/MAINT 1 WP 11 1075T 49724 LINE MAINTENANCE AT ENV, DISCOVERED THAT THE EMERGENCY FLOOR TRACK LENS WAS MISSING AT ROW 18. MX REPLACED THE LENS ON THE EMERGENCY FLOOR TRACK AT ROW 18. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY FLOOR LIGHT SYSTEM. T HE SYSTEM OPERATIONALLY CHECKED NORMAL. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A6WE 1996051600680 19960516 00680 NE 1996 5 16 GRAA9625 2 19960407 A 7261 7578678 OIL FILTER DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE NR 2 ENGINE DIRTY A GRAA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 11 1075T 49724 718220 AT RNO, ON ENGINE START HAD THE RIGHT 'ENGINE OIL CLOGGING' LIGHT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE MAIN ENGINE OIL FILTER. MAINTENANCE PERFORMED AN OPERATIONAL AND LEAK CHECK OF NR 2 ENGINE. NR 2 ENGINE OPERAT IONALLY CHECKED NORMAL. NO LEAKS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 1996051600681 19960516 00681 WP 1996 5 16 GRAA9626 1 19960408 A 3350 FASTENERS DOUG DC9 DC982 3022082 WP CABIN MISSING A GRAA K NONE O OTHER IN INSP/MAINT 1 WP 11 500TR 49144 LINE MAINTENANCE AT MYR, DISCOVERED THE CABIN EMERGENCY LIGHTING HANGING FROM THE CEILING. MAINTENANCE REPLACED THE MIS SING FASTENERS. MAINTENANCE PEFORMED AND OPERATIONAL CHECK OF THE CABIN EMERGENCY LIGHT SYSTEM. THE SYSTEM OPERATIONAL LY CHECKED NORMAL. NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1996051600682 19960516 00682 WP 1996 5 16 HALA9634 1 19960401 A 3244 TIRE DOUG DC10 DC1010 3022110 WP NR 8 RT MLG BLOWN A HALA K NONE O OTHER TO TAKEOFF 1 WP 13 148AA 46703 HNL - FLT NR 921 - RIGHT SIDE MAIN GEAR TIRE BLOWN ON TAKEOFF AS REPORTED BY ANOTHER AIRCRAFT. FOUND NR 8 TIRE BLOWN, R IGHT FLAP L/E DENTED AND SPOILER CONTROL ACCESS PANEL DAMAGED. REPLACED NR 7 AND NR 8 TIRES. INSTALLED TEMPORARY REPAI R ON SPOILER ACCESS PANEL. AIRCRAFT FERRIED TO TUL FOR FURTHER REPAIRS. (M) 2 L 7 3 4F A22WE 1996051600683 19960516 00683 WP 1996 5 16 HALA9635 1 19960404 A 3260 0080004003 PROX CONTL BOX DOUG DC9 DC951 3022051 WP LANDING GEAR INOP A HALA O OTHER N FALSE WARNING IN INSP/MAINT 1 WP 13 673MC 293 47726 HNL - FLT NR 504 - ON 'UPLATCH CHECK' LT MLG INDICATED 'UNSAFE'. LIGHT REMAINED ILLUMINATED WHEN 'UP' SELECTED. CYCLED GEAR IAW PROCEDURES. ALL DOWN SAFE. CYCLED 'UP' LT MLG STILL UNSAFE IN UP POSITION. REPLACED LANDING GEAR PROXIMITY BOX CONTROL, CLEANED LT LANDING GEAR UPLOCK SENSOR. OPERATED GEAR SEVERAL TIMES. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1996051600684 19960516 00684 WP 1996 5 16 HALA9636 1 19960404 A 2760 420913 CONTROL BOX DOUG DC9 DC951 3022051 WP SPOILER SYSTEM INOP A HALA O OTHER J WARNING INDICATION LD LANDING 1 WP 13 672MC 1851 47661 HNL - FLT 509 - SPOILERS WOULD NOT ARM FOR LANDING. WORKED OK MANUAL. REPLACED SPOILER ACTUATOR CONTROL BOX. OPS CHEC KED OK. (M) 2 L 7 2 4F A6WE 1996051600685 19960516 00685 WP 1996 5 16 HALA9637 1 19960404 A 3260 LOCK SENSOR DOUG DC9 DC951 3022051 WP NLG WW FAILED A HALA O OTHER N FALSE WARNING DE DESCENT 1 WP 13 679HA 47662 HNL - FLT 534 - NOSE GEAR UNSAFE LIGHT ON AFTER GEAR EXTENSION. CYCLED GEAR SEVERAL TIMES. UNSAFE LIGHT OUT AND 3 GREE N. LANDED OGG. REPLACED NLG LOCK SENSOR, CANNON PLUG AND CONDUIT. GEAR SWING CHECK OK. (M) 2 L 7 2 4F A6WE 1996051600686 19960516 00686 SW 1996 5 16 MALA964929 1 19960326 A 3260 1EN516 SWITCH SWRNGN SA227 SA227AC 8780603 SW NLG DOWNLOCK FAILED A MALA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 15 158MC AC726B MSP - FLT 3082 - ON APPROACH, THE NOSE GEAR RED INTRANSIT LIGHT DID NOT ILLUMINATE DURING GEAR EXTENSION. ALL OTHER GEA R INDICATIONS WERE NORMAL. MAINTENANCE REPLACED BOTH NOSE LANDING GEAR DOWN POSITION SWITCHES. SYSTEM OPERATED SATISFA CTORILY. (X) 2 L 7 2 4T RT A8SW 1996051600687 19960516 00687 SW 1996 5 16 MALA964930 1 19960328 A 3260 ML345 SWITCH SWRNGN SA227 SA227AC 8780603 SW LT MLG DOWNLOCK FAILED A MALA O OTHER J WARNING INDICATION CL CLIMB 1 GL 15 439MA AC722 STC - FLT 3494 - ON CLIMB-OUT, THE LEFT GEAR INTRANSIT LIGHT FAILED TO ILLUMINATE UPON GEAR RETRACTION. THE LIGHT ALSO FAILED TO ILLUMINATE WHEN THE GEAR WAS SELECTED DOWN ON APPROACH TO MSP. ALL OTHER INDICATIONS WERE NORMAL. MAINTENANC E REPLACED THE LEFT MLG INDICATION DOWN POSITION SWITCH. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 2 L 7 2 4T RT A8SW 1996051600688 19960516 00688 NM 1996 5 16 MALA964931 1 19960328 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 854MA 357 DTW - FLT 3407 - DURING PRE-FLIGHT, CREW NOTED THE COCKPIT OVERHEAD EMERGENCY LAMP ASSEMBLY WAS INOPERATIVE. MAINTENANC E REPLACED THE LIGHT ASSEMBLY. SYSTEM OPERATED SATISFACTORILY. (X) 2 H 7 2 4T RT A13NM 1996051600689 19960516 00689 NM 1996 5 16 MALA964932 1 19960331 A 2422 DH103024600S INVERTER DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A MALA O OTHER O OTHER CR CRUISE 1 GL 15 832MA 341 AZO - FLT 3003 - IN CRUISE FLIGHT, THE SEC INV CAUTION LIGHT ILLUMINATED, AND A LOUD POPPING SOUND WAS HEARD BY THE CREW . THE CREW ALSO NOTED AN AMMONIA TYPE SMELL. THE INVERTER SWITCH WAS SELECTED OFF AND THE AIRCRAFT CONTINUED TO AZO WI THOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE SECONDARY INVERTER. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 2 H 7 2 4T RT A13NM 1996051600690 19960516 00690 SW 1996 5 16 MALA964933 1 19960328 A 5311 FRAME SWRNGN SA227 SA227AC 8780603 SW BS 51.31 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 426MA AC645 MSP - DURING SCHEDULED MAINTENANCE, MAINTENANCE FOUND THE FUSELAGE FRAME AT FS 51.31 CRACKED AT THE RIGHT BAGGAGE DOOR L OWER LATCH RECEPTACLE CUT OUT. REPAIRS WERE COMPLETED BY STOP DRILLING THE CRACK AND INSTALLING AN INTERNAL DOUBLER IAW FAC LAR 96-MALA-057. (X) 2 L 7 2 4T RT A8SW 1996051600691 19960516 00691 SW 1996 5 16 MALA964934 1 19960401 A 5320 SILL FRAME SWRNGN SA227 SA227AC 8780603 SW BS 438 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 159MC AC728B MSP - DURING A SCHEDULED INSPECTION, THE CARGO DOOR SILL FRAME AT FS 438 WAS FOUND TO HAVE A .25 INCH CRACK. REPAIRS WE RE COMPLETED BY STOP DRILLING THE CRACK, ENLARGING THE CUT OUT IN THE SILL, AND WET INSTALLING TWO DOUBLERS IAW FAC ARP 53-30-5507. (X) 2 L 7 2 4T RT A8SW 1996051600692 19960516 00692 SW 1996 5 16 MALA964935 1 19960401 A 5720 ANGLE SWRNGN SA227 SA227AC 8780603 SW WING/NACELLE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 159MC AC728B MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE RIGHT INBOARD LOWER WING TO NACELLE TRANSIT/ATTACH ANGLE CRAC KED APPROXIMATELY .750 INCHES AT THE FORWARD END. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR DOUBLER IAW FAC SRM 51- 00-00 AND ARP 54-20-9101. (X) 2 L 7 2 4T RT A8SW 1996051600693 19960516 00693 SW 1996 5 16 MALA964936 1 19960401 A 5210 SKIN SWRNGN SA227 SA227AC 8780603 SW PASSENGER DOOR CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 159MC AC728B MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE PASSENGER DOOR LOWER SKIN EDGE CRACKED OFF AT THE AFT HINGE R ECESS. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR DOUBLER IAW ARP 52-10-8701, SRM 51-30-04, AND SRM 51-40-01. (X) 2 L 7 2 4T RT A8SW 1996051600694 19960516 00694 SW 1996 5 16 MALA964937 1 19960401 A 5210 SKIN SWRNGN SA227 SA227AC 8780603 SW PASSENGER DOOR CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 159MC AC728B MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE PASSENGER DOOR LOWER SKIN EDGE CRACKED OFF AT THE FORWARD HIN GE RECESS. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR DOUBLER IAW ARP 52-10-8701, SRM 51-30-04 AND SRM 51-40-01. (X ) 2 L 7 2 4T RT A8SW 1996051600695 19960516 00695 SW 1996 5 16 MALA964938 1 19960401 A 5210 2724044 CORNER SWRNGN SA227 SA227AC 8780603 SW PASSENGER DOOR CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 159MC AC728B MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE LOWER AFT PASSENGER DOOR CORNER, PN 27-24044, CRACKED AT SNUB BER ATTACH NUTPLATE. REPAIRS WERE COMPLETED BY REPLACING THE CORNER IAW FAC SRM'S 51-00-00, 51-30-02, 51-30-04, AND 51- 40-00. (X) 2 L 7 2 4T RT A8SW 1996051600696 19960516 00696 SW 1996 5 16 MALA964939 1 19960401 A 5320 2722104 INTERCOSTAL SWRNGN SA227 SA227AC 8780603 SW BS 212.37 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 159MC AC728B MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE LEFT LOWER FUSELAGE INTERCOSTAL, AT FS 212.37 (PN 27-22104), CRACKED IN THE FLANGE RELIEF RADIUS. REPAIRS WERE COMPLETED BY STOP DRILLING THE CRACK AND INSTALLING A REPAIR DOUBLER AND STIFFENER IAW FAC SRM 53-90-20, PAGES 87-89. (X) 2 L 7 2 4T RT A8SW 1996051600697 19960516 00697 SW 1996 5 16 MALA964940 1 19960401 A 5320 2722085 DOOR FRAME SWRNGN SA227 SA227AC 8780603 SW BS 438 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 159MC AC728B MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND A CRACK IN THE FUSELAGE FORWARD CARGO DOOR FRAME (PN 27-22085) AT FS 438. REPAIRS WERE COMPLETED BY REMOVING THE CRACKED AREA AND INSTALLING REPAIR DOUBLERS IAW FAC ARP 53-20-5503. (X ) 2 L 7 2 4T RT A8SW 1996051600698 19960516 00698 NM 1996 5 16 MZZA96025 1 19960317 A 5711 SPAR BOEING 727 727232 1384082 NM RT WING CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON RIGHT WING FRONT SPAR LOWER CH ORD PLATE BELOW NR 5 SLAT ACTUATOR. THE CORRODED CHORD PLATE WAS CLEAN UP AND REPAIRED PER B727 51-10-6 AND 51-40-4. H ANGAR NON ROUTINE REPAIR ITEM CARD NR 819631 (SEQ NR 06031). (M) 2 L 7 3 4F A3WE 1996051600699 19960516 00699 NM 1996 5 16 MZZA96026 1 19960325 A 5241 SUPPORT PLATE BOEING 727 727232 1384082 NM R1 GALLEY DOOR CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, 6 INCH LONG CRACK WAS FOUND ON R1 GALLEY DOOR LOWER FORWARD DOOR STOP BOLT FITTING SUPPORT PLATE. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM 51-40-2. HANGAR NON ROUTINE REPAIR ITEM CARD NR 807054 (SEQ NR 02260). (M) 2 L 7 3 4F A3WE 1996051600700 19960516 00700 NM 1996 5 16 MZZA96027 1 19960322 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 720 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, 1 INCH LONG CRACK WAS FOUND ON PASSENGER CABIN SEAT TRACK LO W PORTION AT BS 720D, RBL 45.5. THE DAMAGED SEAT TRACK FROM BS 720C TO BS 720D WAS TRIMMED OUT AND REPAIRED PER B727 SR M 53-10-5. HANGAR NON ROUTINE REPAIR ITEM CARD NR 818897. (M) 2 L 7 3 4F A3WE 1996051600701 19960516 00701 NM 1996 5 16 MZZA96028 1 19960321 A 5320 CHANNEL BOEING 727 727232 1384082 NM BS 380-400 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON PASSENGER CABIN FLOOR PANEL SU PPORT 'J' CHANNEL AT BS 395, RBL 15. THE CORRODED 'J' CHANNEL FROM BS 380 TO 400 WAS REMOVED AND REPLACED WITH NEW 'J' CHANNEL. HANGAR NON ROUTINE REPAIR ITEM CARD NR 818889. (M) 2 L 7 3 4F A3WE 1996051600702 19960516 00702 NM 1996 5 16 MZZA96029 1 19960321 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 344-380 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON PASSENGER CABIN SEAT TRACK UPP ER FLANGE AT BS 350, RBL 45.5. THE DAMAGED SEAT TRACK FROM BS 344 TO BS 380 WAS TRIMMED OUT AND REPAIRED PER B727 SRM 5 3-10-5. HANGAR NON ROUTINE REPAIR ITEM CARD NR 818882. (M) 2 L 7 3 4F A3WE 1996051600703 19960516 00703 NM 1996 5 16 MZZA96030 1 19960320 A 5320 INTERCOSTAL BOEING 727 727232 1384082 NM BS 950 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, 1 INCH LONG CRACK WAS FOUND ON PASSENGER CABIN FLOORBEAM INT ERCOSTAL BETWEEN BS 950A AND 950B, BL 0. THE DAMAGED INTERCOSTAL FROM BS 950A AND 950B WAS REMOVED AND REPLACED WITH NE W CHANNEL. HANGAR NON ROUTINE REPAIR ITEM CARD NR 818860. (M) 2 L 7 3 4F A3WE 1996051600704 19960516 00704 NM 1996 5 16 MZZA96031 1 19960321 A 5320 SUPPORT BOEING 727 727232 1384082 NM CABIN CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, 2 INCH LONG CRACK WAS FOUND ON PASSENGER CABIN FLOOR PANEL S UPPORT 'L' ANGLE BETWEEN BS 720A AND 720B, BL 0. THE DAMAGED FLOOR PANEL SUPPORT 'L' ANGLE FROM BS 720A TO 720B WAS REM OVED AND REPLACED WITH NEW 'L' ANGLE. HANGAR NON ROUTINE REPAIR ITEM CARD NR 818863. (M) 2 L 7 3 4F A3WE 1996051600705 19960516 00705 NM 1996 5 16 MZZA96032 1 19960318 A 5320 GUSSET BOEING 727 727232 1384082 NM BS 823 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, 1.5 INCH LONG CRACK WAS FOUND ON BS 823 FRAME FORWARD GUSSET AT RBL 62.5. THE CRACK WAS STOP DRILLED AND REPAIRED PER SRM 51-40-3. HANGAR NON ROUTINE REPAIR ITEM CARD NR 818598. (M) 2 L 7 3 4F A3WE 1996051600706 19960516 00706 NM 1996 5 16 MZZA96033 1 19960315 A 5320 INBOARD WEB BOEING 727 727232 1384082 NM AFT AIRSTAIR CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CRACKS WERE FOUND ON AFT AIRSTAIR TORQUE BOX INBOARD WEB LIG HTENING HOLE CUTOUT, AT THE FOLLOWING AREA; 1 INCH LONG CRACK AT BS 1238 LEFT SIDE, 2 INCHES LONG CRACK AT BS 1218 RIGHT SIDE, 4 INCHES LONG CRACK AT BS 1238 RIGHT SIDE. THE CRACKS WERE STOP DRILLED AND REPAIRED PER B727 SRM 51-40-2. HANG AR NON ROUTINE REPAIR ITEM CARD NR 819400, 819401 AND 819431. (M) 2 L 7 3 4F A3WE 1996051600707 19960516 00707 NM 1996 5 16 MZZA96034 1 19960315 A 5320 INBOARD WEB BOEING 727 727232 1384082 NM AFT AIRSTAIR OIL CANNING A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING WAS FOUND ON AFT AIRSTAIR RT/LT TORQUE BOX INBOA RD WEB AT THE FOLLOWING AREAS; RT SIDE BETWEEN BS 1213 AND 1223. RT SIDE BETWEEN BS 1243 AND 1253. RT SIDE BETWEEN BS 1263 AND 1273. RT SIDE BETWEEN BS 1283 AND 1293. RT SIDE BETWEEN BS 1303 AND 1313. RT SIDE BETWEEN BS 1313 AND 1323. LT SIDE BETWEEN BS 1213 AND 1223. LT SIDE BETWEEN BS 1233 AND 1243. LT SIDE BETWEEN BS 1253 AND 1263. LT SIDE BETWEE N BS 1313 AND 1323. THE AFT AIRSTAIR RT/LT TORQUE BOX INBOARD WEB OIL CANNING AREAS WERE INSTALLED REINFORCEMENT STIFFE NER ANGLES PER B727 SRM 53-30-1. HANGAR NON ROUTINE REPAIR ITEM CARD NR 819390 THROUGH 819399. (M) 2 L 7 3 4F A3WE 1996051600708 19960516 00708 EU 1996 5 16 PLG32596DG5 1 19960325 A 5310 STRUCTURE SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A PLGA K NONE O OTHER IN INSP/MAINT 1 NE 05 347BE 340B187 PSM - DURING ROUTINE C-CHECK INSPECTION, FOUND CORROSION ON STRUCTURE UNDER GALLEY AND ENTRY FLOOR AREA. REMOVED CORROS ION AND REPAIRED IAW SAAB SRM CHAPTERS 51-53. (M) 2 L 7 2 4T RT A52EU 1996051600709 19960516 00709 EU 1996 5 16 PLG32596DG6 1 19960325 A 2720 7227105571 CONTROL CABLE SAAB SF340 340B 7860101 EU RUDDER CHAFED A PLGA K NONE O OTHER IN INSP/MAINT 1 NE 05 347BE 340B187 PSM - DURING ROUTINE C-CHECK INSPECTION, CHAFING WAS FOUND ON LEFT INBOARD RUDDER CABLE OF DUAL CABLE RUN IN CIRCUIT 1. CABLE ASSEMBLY WAS REPLACED AND RIGGED IAW SAAB AMM CH 27. (M) 2 L 7 2 4T RT A52EU 1996051600710 19960516 00710 EU 1996 5 16 PLG32596DG7 1 19960325 A 2720 7227105581 CONTROL CABLE SAAB SF340 340B 7860101 EU RUDDER CHAFED A PLGA K NONE O OTHER IN INSP/MAINT 1 NE 05 347BE 340B187 PSM - DURING ROUTINE C-CHECK INSPECTION, BOTH CABLES AT AFT END OF RUDDER CIRCUIT 1 WERE FOUND TO BE CHAFED. REPLACED C ONTROL CABLES AND RIGGED IAW SAAB AMM CHAPTER 27. (M) 2 L 7 2 4T RT A52EU 1996051600711 19960516 00711 EU 1996 5 16 UD5960204 1 19960209 A 3330 30180B230 FLOOD LIGHT BAG ATP ATP EU FWD BAGGAGE BAY FAILED A UF6A K NONE N FALSE WARNING IN INSP/MAINT 1 GL 31 857AW 2034 SBN - SMOKE CWP ILLUMINATED WITH SMOKE LIGHT IN FORWARD BAGGAGE COMPARTMENT. MAINTENANCE RECRIMPED AND SECURED WIRES ON AFT BAGGAGE LIGHT IN FORWARD BAGGAGE BAY. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4T RT A27NM 1996051600715 19960516 00715 EU 1996 5 16 UF6A960101 1 19960116 A 3350 58786 POWER CABLE BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 854AW 921 2028 ORD - AFT 2 EMERGENCY FLOOR LIGHTING STRIPS INOP. REMOVED AND REPLACED AFT POWER CABLE, OPS CHECK GOOD. (M) 2 L 7 2 4T RT A27NM 1996051600716 19960516 00716 EU 1996 5 16 UF6A960105 1 19960126 A 2422 ASH6641PB INVERTER BAG ATP ATP EU NR 1 FAILED A UF6A K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 31 859AW 7966 2036 SBN - NR 1 INVERTER TRIPPED OFF AND EMITTED SMOKE AND ODOR. MAINTENANCE REMOVED AND REPLACED THE NR 1 INVERTER. SYTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1996051600717 19960516 00717 EU 1996 5 16 UF6A960106 1 19960128 A 3350 6013211 POWER SUPPLY BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 852AW 5106 421 2021 SBN - NR 2 EMERGENCY LIGHT POWER SUPPLY INOP. MAINTENANCE REMOVED AND REPLACED NR 2 EMERGENCY LIGHT POWER SUPPLY. (M) 2 L 7 2 4T RT A27NM 1996051600718 19960516 00718 EU 1996 5 16 UF6A960107 1 19960130 A 7603 7451832 SWITCH BAG ATP ATP EU LT COND LEVER OUT OF ADJUST A UF6A C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 31 852AW 10006 2021 ORD - FLT 5043 - EEC AND AFU RIGHT SIDE DID NOT ARM ON TAKEOFF. MAINTENANCE ADJUSTED LEFT CONDITION LEVER MICROSWITCH, AUTOFEATHER SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4T RT A27NM 1996051600719 19960516 00719 1996 5 16 UF6A960202 4 19960204 A 2350 899926930 CCS BOX BAG ATP ATP EU COCKPIT FAILED A UF6A O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 31 856AW 7380 2032 ORD - FLT 5065 - JUMPSEAT STATION BOX HAS SMOKE RISING FROM THE TOP OF IT. MAINTENANCE REMOVED ADN REPLACED THE ACM CCS BOX. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4T RT A27NM 1996051600720 19960516 00720 EU 1996 5 16 UF6A960203 1 19960208 A 3320 65R290424B BALLAST BAG ATP ATP EU CABIN FAILED A UF6A K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 31 858AW 2035 SBN - STRONG ODOR OF SMOKE IN BETWEEN FLIGHT DECK AND CABIN. MAINTENANCE REMOVED AND REPLACED BALLAST UNIT IN ROOF PANE L BALLAST L1. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4T RT A27NM 1996051600721 19960516 00721 EU 1996 5 16 UF6A960207 1 19960226 A 6123 30048000013 AUTOFEATHER UNIT BAG ATP ATP EU LT ENG FAULTY A UF6A K NONE L NO TEST TX TAXI/GRND HDL 1 GL 31 854AW 8629 4683 2028 FWA - FLT 5754 - LEFT AUTOFEATHER TEST FAILED. MAINTENANCE STRAIGHTENED BENT PIN ON AFU CANNON PLUG. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4T RT A27NM 1996051600722 19960516 00722 EU 1996 5 16 UF6A960208 1 19960226 A 3240 ACA2100 BRAKE CONTL VLV BAG ATP ATP EU LANDING GEAR FAILED A UF6A K NONE O OTHER CR CRUISE 1 GL 31 860AW 7196 2057 2037 ORD - FLT NR 5729 - OUTER BRAKE PRESSURE DROPS IN FLIGHT. MAINTENANCE REMOVED AND REPLACED BRAKE CONTROL VALVE. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4T RT A27NM 1996051600723 19960516 00723 NE 1996 5 16 UF6A960313 2 19960328 A 7321 7919002002 EEC BAG ATP ATP EU PWA PW120 PW126A NE NR 2 ENG FAILED A UF6A C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 31 860AW 6190 2037 FWA - FLT 5726 - RIGHT AUTOFEATHER WOULD NOT ARM DURING TAKEOFF. MAINTENACNE REMOVED AND REPLACED NR 2 EEC. (M) 2 L 7 2 4T 4 T RT A27NM E2ONE 1996051600724 19960516 00724 EU 1996 5 16 UF6A96311 1 19960322 A 3350 10620BAC6 SWITCH BAG ATP ATP EU COCKPIT FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 852AW 10126 2021 ORD - FLT 5705 - COCKPIT EMERGENCY LIGHT SWITCH, UNABLE TO TURN ON. MAINTENANCE CLEANED CONTACT 3 ON LIGHT SWITCH. SYS TEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1996051600725 19960516 00725 NM 1996 5 16 USAA960368 1 19960410 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM FUSELAGE CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 28202 23595 CLT - INSPECTION VISUALLY, FOUND A LEVEL 2 CORROSION LOCATED ENTIRE LENGTH, TOP AND BOTTOM AT S46L TO S46R FLOORBEAM ARE A. REPLACED UPPER FLOORBEAM T-CAP CAP AS PER TYPICAL REPAIR 53-10-05. (M) 2 L 7 2 4F RT A16WE 1996051600726 19960516 00726 NM 1996 5 16 USAA960369 1 19960322 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 706 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 234US 41702 22274 INT - DURING 'DROP-IN' CHECK VISUAL PCI INSPECTION, FOUND 2.2 INCH CRACK, STATION 706 STRINGER 18A RIGHT. INSTALLED REP AIR, REPAIRED PER EA 41018. (M) 2 L 7 2 4F A16WE 1996051600727 19960516 00727 WP 1996 5 16 USAA960370 1 19960409 A 5312 BULKHEAD DOUG DC9 DC931 3022065 WP BS 996 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 946VJ 73099 47026 PIT - DURING C-4 CHECK INSPECTION, FOUND A 1.25 INCH AND 3 INCH CRACK IN REAR PRESSURE BULKHEAD Z-63 LEFT SIDE OF DOOR F RAME AT STATION 996. CUT OUT CRACKED AREAS AND INSTALLED FILLER AND DOUBLER PER USAIR EA NR 32410A. (M) 2 L 7 2 4F A6WE 1996051600728 19960516 00728 NM 1996 5 16 USAA960371 1 19960412 A 5320 ANGLE BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 260AU 34273 22866 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH LONG CRACK FRAME CHORD ANGLE STATION FRAME 727, BETWEEN STRINGER 16R AND STRINGER 17R. REMOVED DAMAGED AREA MANUFACTURED HEAT TREATED AND INSTALLED REPAIR. REPAIRED PER SRM 51-40-4 FI G 1 SRM 20-30-06. (M) 2 L 7 2 4F A16WE 1996051600729 19960516 00729 NM 1996 5 16 USAA960372 1 19960412 A 5320 ANGLE BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 260AU 34273 22866 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK AT TWO FASTENERS AT BS 727, STRINGER 18 IN FRAME CHORD ANG LE. REPLACED SECTION OF CHORD ANGLE, REPAIRED PER EO 5394G068. (M) 2 L 7 2 4F A16WE 1996051600730 19960516 00730 NM 1996 5 16 USAA960373 1 19960412 A 5330 SKIN BOEING 737 737201 1384454 NM BS 349 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 260AU 34273 22866 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK DOOR FRAME SKIN BS 349, STRINGER 15L. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2, FIG 1. (M) 2 L 7 2 4F A16WE 1996051600731 19960516 00731 NM 1996 5 16 USAA960374 1 19960412 A 5320 STAB STRAP BOEING 737 737201 1384454 NM BS 344 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 260AU 22866 22866 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK STABILIZER STRAP (FLOOR BEAM BOTTOM) BS 344, RBL 32. INSTA LLED DOUBLER, REPAIRED PER SRM 53-10-9. (M) 2 L 7 2 4F A16WE 1996051600732 19960516 00732 NM 1996 5 16 USAA960375 1 19960412 A 5320 STAB STRAP BOEING 737 737201 1384454 NM BS 312 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 260AU 34273 22866 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK STABILIZER STRAP (BOTTOM OF FLOOR BEAM) BS 312, RBL 45. IN STALLED DOUBLER, REPAIRED PER SRM 53-10-9. (M) 2 L 7 2 4F A16WE 1996051600733 19960516 00733 NM 1996 5 16 USAA960376 1 19960412 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 360` CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 260AU 34273 22866 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 CRACK STRINGER TIE CLIP STATION 360, STRINGER 4L. FABRICATED AND IN STALLED NEW TIE CLIP, REPAIRED PER SRM 57-10-1. (M) 2 L 7 2 4F A16WE 1996051600734 19960516 00734 NM 1996 5 16 USAA960377 1 19960412 A 5313 STRIGNER BOEING 737 737201 1384454 NM BS 294 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 260AU 34273 22866 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK WEB OF BUILD UP STRINGER BS 294, STRINGER 7L. FABRICATED AND INSTALLED WEB PER BAC PRINT NR 65-27684 SRM 51-30-2, PAGE 5 AND SRM 53-10-1 NOTED. (M) 2 L 7 2 4F A16WE 1996051600735 19960516 00735 NM 1996 5 16 USAA960378 1 19960412 A 5330 SKIN BOEING 737 737201 1384454 NM BS 328 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 260AU 34273 22866 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK EXTERIOR SKIN AND BEAR STRAP BS 328 WL 210 RIGHT SIDE LOWER AFT CORNER OF DOOR CUTOUT. INSTALLED REPAIR DOUBLER PER SRM 53-30-3 FIG 26. (M) 2 L 7 2 4F A16WE 1996051600736 19960516 00736 NM 1996 5 16 USAA960379 1 19960412 A 5311 FRAME BOEING 737 737201 1384454 NM BS 350 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 260AU 34273 22866 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CRACK 1 INCH LONG STATION 350 AT STRINGER 17L FRAME. REMOVED DAMAGED AR EA FABRICATED REPAIR AND REPAIRED PER SRM 20-30-06 SRM 51-40-4. (M) 2 L 7 2 4F A16WE 1996051600737 19960516 00737 NM 1996 5 16 USAA960380 1 19960412 A 5313 6517684642 STRINGER BOEING 737 737201 1384454 NM BS 294 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 260AU 34273 22866 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK BS 294 AND STRINGER 7 LEFT. REMOVED CRACK SECTION OF STR INGER WEB, FABRICATED NEW SECTION AND INSTALLED PER SRM. REPAIRED PER BOEING DRAWING 65-17684 AND SRM 53-10-1 AND 51-30 -2 PAGE 5. (M) 2 L 7 2 4F A16WE 1996051600738 19960516 00738 NM 1996 5 16 USAA960381 1 19960412 A 5320 WEB BOEING 737 737201 1384454 NM BS 350 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 260AU 34273 22866 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK AT WEB, BS 350 STRINGER 16L. FABRICATED AND INSTALLED REPL ACEMENT WEB. REPAIRED PER BOEING DRAWING 65-17685. (M) 2 L 7 2 4F A16WE 1996051600739 19960516 00739 NM 1996 5 16 USAA960382 1 19960413 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 947-1016 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 36599 22757 ROA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 69 INCH CORROSION STRINGER 27L, BS 947 TO 1016. INSTALLED ST RINGER/DOUBLERS. REPAIRED PER SRM 53-10-3, DETAIL VI. (M) 2 L 7 2 4F A16WE 1996051600740 19960516 00740 WP 1996 5 16 USAA960383 1 19960413 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1380 CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 822US 36027 49139 PIT - DURING A SCHEDULED Q-1/C-1 CHECK INSPECTION, FOUND STATION 1380 FORWARD SIDE FRAME CHAFED BETWEEN LONGERON 4L AND 5L. ROUTED OUT CHAFED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 2 SHEET 3 AND SRM 53-14-1. (M) 2 L 7 2 4F A6WE 1996051600741 19960516 00741 WP 1996 5 16 USAA960384 1 19960413 A 5530 ANGLE DOUG DC9 DC982 3022082 WP LT VERT STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 822US 36027 49139 PIT - DURING A SCHEDULED Q-1/C-1 CHECK INSPECTION, FOUND 3.5 INCH CRACK RIGHT SIDE DRAG ANGLE LOWER VERT STABILIZER. IN STALLED DOUBLER REPAIR PER USAIR EA 32426. (M) 2 L 7 2 4F A6WE 1996051600742 19960516 00742 WP 1996 5 16 USAA960385 1 19960413 A 5530 ANGLE DOUG DC9 DC982 3022082 WP LT VERT STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 822US 36027 49139 PIT - DURING A SCHEDULED Q-1/C-1 CHECK INSPECTION, FOUND 3.5 INCH CRACK LEFT SIDE AFT DRAG ANGLE AT LOWER VERT STAB. IN STALLED DOUBLER REPAIR PER USAIR EA 32425. (M) 2 L 7 2 4F A6WE 1996051600743 19960516 00743 WP 1996 5 16 USAA960386 1 19960413 A 5320 593659215 SUPPORT DOUG DC9 DC982 3022082 WP BS 541 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 822US 36027 49139 PIT - DURING A SCHEDULED Q-1/C-1 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED IN CARGO FLOOR SUPPORT ST ATION 541, BETWEEN LONGERON 28L AND 28R. MANU SUPPORT USING 7075-T6 PER DACO DRAWING NR 5936592. (M) 2 L 7 2 4F A6WE 1996051600744 19960516 00744 WP 1996 5 16 USAA960387 1 19960413 A 5512 5922578 PANEL DOUG DC9 DC982 3022082 WP HORIZ STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 822US 36027 49139 PIT - DURING A SCHEDULED Q-1/C-1 CHECK INSPECTION, FOUND A 1.75 INCH CRACK IN SKIN PANEL JUST OUTBOARD OF REAR SPAR STAT ION XH=7.234 RIGHT SIDE HORIZONTAL STAB. REMOVED DAMAGE AND INSTALLED FILLER REPAIR PER SR09550010-3 AND USAIR EO NR 55 92X156. (M) 2 L 7 2 4F A6WE 1996051600745 19960516 00745 WP 1996 5 16 USAA960388 1 19960413 A 5313 59366717 LONGERON DOUG DC9 DC982 3022082 WP BS 1211-1250 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 822US 36027 49139 PIT - DURING A SCHEDULED Q-1/C-1 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED ON LONGERON 29R STATION 1 211-1250. CORROSION TASK NR C57-53300. INSTALLED NEW SECTION OF LONGERON PER USAIR EA 32559. (M) 2 L 7 2 4F A6WE 1996051600746 19960516 00746 WP 1996 5 16 USAA960389 1 19960413 A 5313 59366717 LONGERON DOUG DC9 DC982 3022082 WP BS 1211-1250 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 822US 36027 49139 PIT - DURING A SCHEDULED Q-1/C-1 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED SECTION OF LONGERON 28L S TATION 1211-1250. CORROSION TASK NR C57-53300. SPLICED IN NEW SECTION OF LONGERON PER USAIR EA 32559. (M) 2 L 7 2 4F A6WE 1996051600747 19960516 00747 WP 1996 5 16 USAA960390 1 19960413 A 5320 PL591014249 DOOR PAN DOUG DC9 DC982 3022082 WP CARGO COMPT CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 822US 36027 49139 PIT - DURING A SCHEDULED Q-1/C-1 CHECK INSPECTION, FOUND APPROXIMATELY 38 INCHES OF CORROSION IN FWD CARGO DOOR STATION 389 THROUGH STATION 427 DOOR PAN. INSTALLED NEW SECTION OF PAN PER SRM 53-05 FIG 44. (M) 2 L 7 2 4F A6WE 1996051600748 19960516 00748 NM 1996 5 16 USAABB96012 1 19960408 A 3610 16J081 DUCT ASSEMBLY BOEING 757 757225 1384959 NM LT ENG CRACKED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 602AU 22196 SJU - FL 1970 - AFTER TAKEOFF, CREW REPORTED A PNEUMATIC LEAK ON THE LEFT ENGINE (EICAS MESSAGE - 'L ENG OVHT'). FLIGHT RETURNED TO SJU. MAINTENANCE CONFIRMED A BLEED PROBLEM AND TIGHTENED A CLAMP ON THE LEFT ENGINE DUCTING. FLIGHT TOOK OFF AND RETURNED A SECOND TIME FOR THE SAME PROBLEM. MAINTENANCE FOUND THE LEFT ENGINE EXPANSION JOINT CRACKED AND REPL ACED IT. (M) 2 L 7 2 4F RT A2NM 1996051600749 19960516 00749 EU 1996 5 16 96ZZZM804 1 19960407 A 7722 8974696 EGT PIG TAIL BAG JETSTM JETSTM3201 1500217 EU RT ENG SHORTED A NVEA E ENGINE SHUTDOWN N FALSE WARNING IN INSP/MAINT 1 SO 03 928AE 928 FLT NR 4762 - BNA - ON DESCENT RIGHT ENGINE EGT WENT TO 750 DEG PILOT SHUT DOWN ENGINE WF AND TQ STAYED THE SAME. MAINT ENANCE INSPECTED AND FOUND RIGHT ENGINE EGT HARNESS PIG TAIL SHORTED. MAINTENANCE REPLACED HARNESS, ENG TEST RUNS CHECK ED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996051600750 19960516 00750 EU 1996 5 16 96ZZZM805 1 19960403 A 7800 1379049H401 EXHAUST PIPE BAG JETSTM JETSTM3201 1500217 EU RT ENGINE CRACKED A NVEA K NONE O OTHER IN INSP/MAINT 1 SO 03 938AE 938 FLT NR 4675 - CHA - ON POST FLT INSPECTION, THE CAPTAIN NOTICED THE RIGHT ENG COWL HAD THE PAINT DISCOLORED DUE TO HEAT ON BOTH SIDES. THE RIGHT ENG EXHAUST STUB PIPE WAS FOUND TO BE CRACKED AT THE FLANGE. REPLACED THE RIGHT ENGINE EXHAUS T STUB PIPE. (M) 2 L 7 2 4T RT A56EU 1996051600751 19960516 00751 NM 1996 5 16 96ZZZM806 1 19960419 A 2611 SMOKE LIGHT BOEING 727 727222 1384073 NM CARGO COMPT ILLUMINATED A RYNA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 07 7639U 19912 IN CRUISE FROM DAY TO MCI, THE MAIN CARGO SMOKE DETECTOR LIGHT ILLUMINATED. AIRCRAFT MADE UNSCHEDULED LANDING STL. DUR ING DESCENT THE WARNING LIGHT EXTINGUISHED. NO EVIDENCE OF FIRE NOTED. TESTED CARGO SMOKE DETECTION SYSTEM PER MM 26, SYSTEM CHECKS NORMAL. COULD NOT DUPLICEATE DISCREPANCY. SUSPECT CONDENSATION IN CARGO HOLD GAVE FALSE WARNING. NO PAR TS CHANGED. 2 L 7 3 4F A3WE 1996051600752 19960516 00752 NM 1996 5 16 96ZZZM807 1 19960403 A 3260 69157472 DNLOCK PUSHROD BOEING 727 727231 1384079 NM RT MLG BROKEN A TWAA O OTHER N FALSE WARNING CL CLIMB 1 CE 05 54336 20490 ORD - DURING GEAR RETRACTION, RIGHT GEAR LIGHT STAYED ON. VISUAL CHECK OF ALIGNMENT STRIPES INDICATED GEAR WAS NOT DOWN AND LOCKED. NEITHER GEAR RECYCLE NOR MANUAL EXTENSION ALIGNED STRIPES. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED BROKEN DOWNLOCK PUSHROD, MFG P/N 69-15747-2. PERFORMED BOTH NORMAL AND MANUAL GEAR SWINGS, BOTH CHECKED NORMA L. (M) 2 L 7 3 4F A3WE 1996051600753 19960516 00753 1996 5 16 96ZZZM808 4 19960404 A 3417 HG280D80 AIR DATA COMP DOUG DC9 DC982 3022082 WP E/E COMPT FAILED A TWAA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 CE 05 905TW 49157 JFK - DURING TAKEOFF THE CENTRAL AIR DATA COMPUTER FAILED. AIRCRAFT RETURNED TO JFK. REMOVED AND REPLACED THE CADC, MF G P/N HG280D80. SELF TEST AND LEAK CHECK NORMAL. (M) 2 L 7 2 4F A6WE 1996051600754 19960516 00754 WP 1996 5 16 96ZZZM809 1 19960404 A 2410 CSD DOUG DC9 DC982 3022082 WP NR 2 FAILED A TWAA O OTHER J WARNING INDICATION CR CRUISE 1 CE 05 905TW 49157 JFK - DURING CRUISE, THE NR 2 CONSTANT SPEED DRIVE FAILED. REMOVED AND REPLACED NR 2 CSD. OPERATIONAL CHECK NORMAL. ( M) 2 L 7 2 4F A6WE 1996051600755 19960516 00755 1996 5 16 96ZZZM810 4 19960402 A 2210 7015327901 CONTROL PANEL HONEYWELL GP300 DORNER DO32 DO328100 2996000 NM COCKPIT DAMAGED A EQGA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 19 335LS 2047 94050150 3035 WHILE EN ROUTE TO CUU FROM DFW, THE PILOT NOTICED A BURNING SMELL AND SAW SMOKE COMING FROM THE FLIGHT GUIDANCE CONTROL PANEL. HE TRIED TO DISCONNECT THE AUTOPILOT, HOWEVER, IT WOULD NOT DISENGAGE. WHILE THEY WERE LOOKING FOR THE CIRCUIT BREAKER IT POPPED BY ITSELF AND THE AUTO PILOT THEN DISENGAGED. THE CREW THEN TURNED BACK TO DFW AND LANDED WITHOUT FUR THER INCIDENT. THE PANEL WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A45NM 1996051600756 19960516 00756 NM 1996 5 16 96ZZZM811 1 19960411 A 2131 7102985 CONTROLLER BOEING 747 747212B 1384886 NM CABIN FAILED A TWRA A G UNSCHED LANDING O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 EA 15 616FF 21939 DURING CRUISE AT FL 350, AIRCRAFT EXPERIENCED AN UNCONTROLLABLE CABIN CLIMB. RAPID DECOMPRESSION AND EMERGENCY DESCENT CHECKLIST WAS ACCOMPLISHED. INITIATED DESCENT TO 10,000 FEET RIGHT OUTFLOW VALVE CIRCUIT BREAKER POPPED, RESCENT AND PO PPED AGAIN. AIRCRAFT DIVERTED TO MUSCAT (MCT) UPON LANDING AT MCT, THE ITEM WAS DEFERRED TO THE ODI 04593 AND THE RIGHT OUTFLOW VALVE LOCKED IN THE CLOSE POSITION. OXYGEN MASK STOWED AND ITEM DEFERRED. DURING TROUBLESHOOTING, MAINTENANCE FOUND BURNT PIN ON RELAY R352 AND BURNT CONNECTOR AT CONTROLLER. ALL ITEMS WERE REPLACED AS REQUIRED. PRESSURIZATION CHECK COMPLETED. AIRCRAFT RETURNED TO SERVICE. REFERENCE TWRA9620. 2 L 7 4 4F A20WE 1996051600757 19960516 00757 CE 1996 5 16 96ZZZM812 1 19960423 A 5730 SKIN BEECH 1900 1900C 1154161 CE LT WING CRACKED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 198GA UB5 AT SCHEDULED INSPECTION, THE LEFT UPPER WING SKIN CRACKED, ZONE 532. REMOVED DAMAGED AREA, INSTALLED FILLER AND DOUBLER IAW BEECH SRM 51-70-00, FIGURE 15. (M) 2 L 7 2 4T RT A24CE 1996051600758 19960516 00758 CE 1996 5 16 96ZZZM813 1 19960423 A 5730 SKIN BEECH 1900 1900C 1154161 CE RT WING CRACKED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 198GA UB5 AT SCHEDULED INSPECTION, THE RIGHT UPPER WING SKIN WAS DETERMINED TO BE CRACKED, ZONE 632. REMOVED DAMAGED AREA, INSTAL LED FILLER DOUBLER IAW BEECH SRM CHAPTER 51-70-00, FIGURE 15. (M) 2 L 7 2 4T RT A24CE 1996051600759 19960516 00759 EU 1996 5 16 96ZZZM814 1 19960424 A 3260 M22885790 RECEPTACLE STBROS SD3 SD360 8100606 EU MLG FAILED A GUUA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 19 831BE SH3757 FLT NR 173 - EYW-MIA - MAIN GEAR INDICATOR LIGHT INOP. AIRCRAFT LANDING GEAR SYSTEM WAS DEFERRED WITH GEAR PINS INSTALL ED. REMOVED AND REPLACED INDICATOR RECEPTACLE. OPERATIONAL CHECK GOOD. 2 H 7 2 4T A41EU 1996051600760 19960516 00760 CE 1996 5 16 96ZZZM815 1 19960424 A 3260 1013641791 SENSOR BEECH 1900 1900C 1154161 CE LANDING GEAR FAILED A GUUA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 19 11ZR UB11 FLT 488 - MIA-FLL - LANDING GEAR POSITION INDICATION LIGHTS INOP. AIRCRAFT WAS FERRIED TO MIA. REMOVED AND REPLACED L OW LEVEL SENSOR. SWUNG GEAR. OPS CHECK GOOD. 2 L 7 2 4T RT A24CE 1996051600761 19960516 00761 CE 1996 5 16 96ZZZM816 1 19960424 A 3260 404EN16 DNLOCK SWITCH BEECH 1900 1900C 1154161 CE RT MLG FAILED A GUUA O OTHER N FALSE WARNING AP APPROACH 1 SO 19 11ZR UB11 FLT 480 - NAS-MAI - LANDING GEAR POSITION, RIGHT MAIN, LIGHT EXTINGUISHED ON SHORT FINAL. REMOVED AND REPLACED RIGHT DO WN LOCK SWITCH, OPS CHECK GOOD ON GEAR SWINGS. (M) 2 L 7 2 4T RT A24CE 1996051600762 19960516 00762 WP 1996 5 16 96ZZZM817 1 19960401 A 5270 SWITCH DOUG DC9 DC932 3022066 WP CARGO DOOR OUT OF ADJUST A VJ6A C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 11 904VJ 47377 ON FLT 235, ATL-ATL, GATE RETURN, THE AFT CARGO DOOR LIGHT CAME ON TAKEOFF ROLL. ADJUSTED SWITCH PER 52-30, OPS CHECK N ORMAL. (M) 2 L 7 2 4F A6WE 1996051600763 19960516 00763 WP 1996 5 16 96ZZZM818 1 19960315 A 2420 GEN CONTL PANEL DOUG DC9 DC932 3022066 WP LEFT LOOSE A VJ6A A UNSCHED LANDING O OTHER CR CRUISE 1 SO 11 904VJ 47377 ON FLT 236, DFW-ATL, DIVERTED TO MSY WITH THE LEFT AC BUS INOP. FOUND THE LEFT GENERATOR CONTROL PANEL LOOSE IN THE RAC K, SECURED PANEL, RAN ENGINES WITH AC LOAD, OPS CHECKED NORMAL. 2 L 7 2 4F A6WE 1996051600764 19960516 00764 NM 1996 5 16 AALA960390 1 19960312 A 3350 A3030398101 CONNECTOR BOEING 727 727227 1384078 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 729AA 20736 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN AFT CABIN BETWEEN AFT GALLEY AND AFT ENTRY DOOR INOPERATIVE. RE PLACED BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTOR AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996051600765 19960516 00765 NM 1996 5 16 AALA960403 1 19960315 A 3350 A3030398101 CONNECTOR BOEING 727 727223 1384074 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 868AA 21373 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FIRST CLASS CABIN INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996051600766 19960516 00766 NM 1996 5 16 AALA960422 1 19960319 A 3350 A3030398101 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 681AA 25338 DFW - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS FOR SEATS 1 THROUGH 6 INOPERATIVE. REPOSITIONE D LOOSE CONNECTOR AT FORWARD END OF EMERGENCY EXIT FLOOR PATH LIGHT TRACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1996051600767 19960516 00767 NM 1996 5 16 AALA960423 1 19960320 A 3350 A3030398101 CONNECTOR BOEING 727 727223 1384074 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 6819 19494 DFW - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS AT ROWS 26 AND 27 INOPERATIVE. RECONNECTED LOO SE CONNECTOR AT EMERGENCY EXIT FLOOR PATH LIGHT TRACK STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996051600768 19960516 00768 NM 1996 5 16 AALA960429 1 19960321 A 3397 WIRE BOEING 727 727223 1384074 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 873AA 21385 DFW - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS IN THE ENTIRE CABIN INOPERATIVE. REPAIRED EMER GENCY EXIT FLOOR PATH LIGHTING WIRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996051600769 19960516 00769 NM 1996 5 16 AALA9604331 1 19960322 A 3397 WIRE BOEING 727 727223 1384074 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 898AA 22014 MIA - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS SECTION INOPERATIVE. REPAIRED S PLICE IN EMERGENCY EXIT FLOOR PATH LIGHTING WIRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996051600770 19960516 00770 EU 1996 5 16 AALA960447 1 19960322 A 3350 A3060398101 CONNECTOR FOKKER F28 F28MK0100 4990807 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1416A 11395 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN AFT CABIN INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT ST RIP CONNECTOR AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1996051600771 19960516 00771 NM 1996 5 16 AALA960451 1 19960323 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 363AA 24044 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 36H INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LI GHT CONNECTOR AT PASSENGER SEAT 36H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1996051600772 19960516 00772 NM 1996 5 16 AALA960452 1 19960323 A 3350 A3060698101 CONNECTOR BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 629AA 24587 ORD - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PASSENGER SEAT ROWS 6E AND 28D INOPERATIVE. REPLACED BROKEN EME RGENCY FLOOR LIGHT STRIP CONNECTORS BY PASSENGER SEAT ROWS 6E AND 28D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1996051600773 19960516 00773 NM 1996 5 16 AALA960460 1 19960325 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1148 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 701AA 22459 FOUND CORROSION ON 1148 FRAME IN AFT CARGO BILGE. REPAIRED PER SRM 53-10-4 FIG 12. (M) 2 L 7 3 4F A3WE 1996051600774 19960516 00774 NM 1996 5 16 AALA960461 1 19960325 A 5330 SKIN BOEING 727 727223 1384074 NM BS 580-585 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 FOUND SKIN CORROSION BEYOND LIMITS ON FUSELAGE. CUT OUT CORRODED AREA AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 1, PG 1 -4. (M) 2 L 7 3 4F A3WE 1996051600775 19960516 00775 NM 1996 5 16 AALA960462 1 19960325 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 690 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 701AA 22459 FOUND CORROSION ON STRINGER 27L, FS 690. CUT OUT DAMAGED AREA INSTALLED DOUBLER REF 53-10-3. (M) 2 L 7 3 4F A3WE 1996051600776 19960516 00776 NM 1996 5 16 AALA960463 1 19960325 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 680 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 701AA 22459 FOUND CORROSION IN STRINGER SPLICE 28R, STATION 680. REPAIRED STRINGER 28R AT STATION 680, IAW SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1996051600777 19960516 00777 NM 1996 5 16 AALA960464 1 19960325 A 5330 SKIN BOEING 727 727223 1384074 NM BS 680-685 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 FOUND CORROSION ON STRINGER 27R AND FUSELAGE SKIN AT STATION 680-685. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER AND STRINGER PER SRM 53-30-3 PG 3C. (M) 2 L 7 3 4F A3WE 1996051600778 19960516 00778 NM 1996 5 16 AALA960465 1 19960325 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 950-970 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 862AA 21089 FOUND STATION 950F TO 970 STRINGER 28R IS CORRODED. REPLACED CORRODED SECTION OF STRINGER REF ESO 11697, DTD 3-15-96. ( M) 2 L 7 3 4F A3WE 1996051600779 19960516 00779 NM 1996 5 16 AALA960466 1 19960325 A 5330 SKIN BOEING 727 727223 1384074 NM BS 950-970 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 862AA 21089 TUL - FOUND STATION 950F TO 970 SKIN IS CORRODED ON OUTBOARD SIDE OF STRINGER 28R. REMOVED (BLENDED) CORROSION FROM SKI N 950F-970. INSTALLED DOUBLER AND TRIPLER IN AREA OF CORROSION AND SPLICED IN 2 SECTIONS OF STRINGER REPAIRS IAW ES1169 7, DTD 3-15-96. (M) 2 L 7 3 4F A3WE 1996051600780 19960516 00780 NM 1996 5 16 AALA960467 1 19960325 A 5320 INTERCOSTAL BOEING 727 727223 1384074 NM BS 950-970 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 862AA 21089 FOUND CORROSION ON INBOARD SIDE OF INTERCOSTAL STRINGER 28R, STATION 950F AND 970. REMOVED AND REPLACED INTERCOSTAL STR INGER 28R, STATION 950F-970. (M) 2 L 7 3 4F A3WE 1996051600781 19960516 00781 NM 1996 5 16 AALA960468 1 19960325 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 992-1002 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 701AA 22459 FOUND CORROSION ON STRINGER 29RT, STATION 992 TO 102. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER PER SRM 53-10-3 PG S 11A THROUGH 11E. (M) 2 L 7 3 4F A3WE 1996051600782 19960516 00782 NM 1996 5 16 AALA960469 1 19960325 A 5330 SKIN BOEING 727 727223 1384074 NM BS 695 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 701AA 22459 FOUND SKIN HAS CRACK AND CORROSION AT STRINGER 27R, STATION 695. CUT OUT CORROSION ON SKIN FROM STATION 695-680 ALONG S TRINGER 27R. INSTALLED DOUBLER ON SKIN FROM STATION 680-710 PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 1996051600783 19960516 00783 NM 1996 5 16 AALA960470 1 19960325 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 680-706 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 701AA 22459 FOUND CORROSION ON STRINGER 27R STATION 680-706. CUT OUT CORRODED AREA OF STRINGER, FABRICATED AND INSTALLED SPLICE PLA CE PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1996051600784 19960516 00784 NM 1996 5 16 AALA960471 1 19960325 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 680 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 701AA 22459 TUL - FOUND CORROSION IN STRINGER SPLICE STRINGER 28L, STATION 680. INSTALLED STRINGER REPAIR STATION 680, STRINGER 28L IAW SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1996051600785 19960516 00785 NM 1996 5 16 AALA960472 1 19960325 A 5230 WEB BOEING 727 727223 1384074 NM CARGO DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 701AA 22459 FOUND CORROSION FORWARD CARGO DOOR WEB LANDING AT FWD AND AFT ENDS. REMOVED CORRODED WEB BOTH ENDS AT FWD CARGO DOOR MA NUFACTURED NEW WEBS 7075-T6 .071 AND CHORD ANGLES TREATED AND PRIMED AND INSTALLED PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1996051600786 19960516 00786 NM 1996 5 16 AALA960473 1 19960325 A 5330 SKIN BOEING 727 727223 1384074 NM BS 690 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 701AA 22459 TUL - FOUND CORROSION INSIDE FUSELAGE SKIN FWD CARGO BILGE. REMOVED CORROSION INSIDE SKIN AND BLENDED OUT SRM 51-10-6 D AMAGED AREA NOT CUT OUT PER ESO 11697 DATED 1/24/96 2024-T3 .063 DOUBLER INSTALLED OUTSIDE SKIN SRM 53-30-3. (M) 2 L 7 3 4F A3WE 1996051600787 19960516 00787 NM 1996 5 16 AALA960474 1 19960325 A 5312 BLKHD BEAM BOEING 727 727223 1384074 NM BS 1183 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 701AA 22459 FOUND VERTICAL BEAM CRACKED AT STATION 1183 RBL 36, BOTH SIDES APPROX 30 INCHES ABOVE FLOOR LINE. REPAIRED IAW BOEING 7 27 SB NR 727-53-0192. (M) 2 L 7 3 4F A3WE 1996051600788 19960516 00788 NM 1996 5 16 AALA960475 1 19960325 A 5730 SKIN BOEING 727 727223 1384074 NM WS 423-425 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 701AA 22459 TUL - CORROSION LOWER WING SKIN EXTENSION OUTBOARD OF NR 4 SLAT TRACK. REPAIRED PER B727 AARD 57-30-00-2 PG 1-3. (M) 2 L 7 3 4F A3WE 1996051600789 19960516 00789 NM 1996 5 16 AALA960476 1 19960325 A 5330 SKIN BOEING 727 727223 1384074 NM BS 950 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 701AA 22459 FOUND CORROSION ON STRINGER 29L AND SKIN FWD OF 950E AFT CARGO FROM 950D-950E. REMOVED CORROSION FROM SKIN AND STRINGER 29L AT 950D-950E NDT DETERMINED THICKNESS OF SKIN TO BE BELOW SRM LIMITS, TREATED PRIMED AREA DOUBLER TRIPLER INSTALLED PER ECO11697. (M) 2 L 7 3 4F A3WE 1996051600790 19960516 00790 NM 1996 5 16 AALA960477 1 19960325 A 5330 SKIN BOEING 727 727223 1384074 NM BS 950 WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 701AA 22459 TUL - UPPER FWD CORNER OF CARGO DOOR OPENING WORN. REPORTED PER ESO 11697, DATED 2-28-96. (M) 2 L 7 3 4F A3WE 1996051600791 19960516 00791 NM 1996 5 16 AALA960478 1 19960325 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 615-620 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 701AA 22459 FOUND CORROSION IN STRINGER 27 RT FROM STATION 615 TO STATION 620. REPAIRED STRINGER 27 RT STATION 615 TO STATION 620 P ER SRM 53-10-3, FIG 1. (M) 2 L 7 3 4F A3WE 1996051600792 19960516 00792 NM 1996 5 16 AALA960484 1 19960325 A 5753 SKIN BOEING 727 727227 1384078 NM LT TE MID FLAP CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 719AA 20612 TUL - OUTBOARD LEFT MID FLAP TOP SKIN IS CRACKED APPROXIMATELY ON TOP OF TRAILING EDGE FLAP OUTBOARD SPRING ROD END (MAR KED ON FLAP) STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 57-50-4. EDGE SEALED, TREATED, PRIMED AND PAINTED. (M) 2 L 7 3 4F A3WE 1996051600793 19960516 00793 NM 1996 5 16 AALA960488 1 19960327 A 3350 P40110051112 MODULE BOEING 767 767223 1385123 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 322AA 22323 SFO - DURING OVERNIGHT CHECK, FOUND THAT THE EMERGENCY LIGHTS AT SEATS 10H AND 11J STAY ON WHEN SWITCH IS IN OFF POSITIO N. REPLACED EMERGENCY LIGHTS MODULE AND BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1996051600794 19960516 00794 NM 1996 5 16 AALA960490 1 19960328 A 3350 CONNECTOR BOEING 767 767223 1385123 NM LT EXTERIOR LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 306AA 22312 SFO - DURING OVERNIGHT CHECK, COULD NOT TEST LEFT EXTERIOR EMERGENCY LIGHTS FROM THE NOSE GEAR TEST SWITCH. TIGHTENED C ONNECTOR ON REMOTE SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1996051600795 19960516 00795 WP 1996 5 16 AALA960492 1 19960328 A 2751 ST12BH TRANSMITTER DOUG DC9 DC982 3022082 WP RT TE FLAPS DEFECTIVE A AALA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 573AA 53092 DFW - FLT 1789 - DURING APPROACH DFW FLAPS SPLIT RIGHT FLAP HUNG AT 11 DEGREES AND LEFT FLAP WENT TO 15 DEGREES. NO NOT ICEABLE ROLL WAS NOTED. DECLARED EMERGENCY AND LANDED DFW WITHOUT INCIDENT. REPLACED RIGHT FLAP POSITION TRANSMITTER A ND ACCOMPLISHED REQUIRED CHECKS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996051600796 19960516 00796 NM 1996 5 16 AALA960494 1 19960326 A 5753 113N300319 SKIN BOEING 757 757223 1384957 NM LT TE FLAP GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 602AN 27053 AFW - FOUND LEFT WING OUTBOARD MAIN FLAP UPPER SKIN PANEL HAS GOUGES BLENDED AS SHOWN ON SKETCH. GOUGES ARE FROM CONTAC T WITH FASTENERS ON NR 3 SPOILER. PER MRB 757-768. (M) 2 L 7 2 4F RT A2NM 1996051600797 19960516 00797 NM 1996 5 16 AALA960504 1 19960401 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 458-460 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 702AA 22460 TUL - STATION 458 TO 460, RIGHT INBOARD SEAT TRACK HAS CRACK AND CORRSION INSIDE CHANNEL FOR FEET LOCK DOWNS. INSTALLED NEW SEAT TRACK FROM STAITON 440 TO 480 AS PER SRM 53-10-5. (M) 2 L 7 3 4F A3WE 1996051600798 19960516 00798 NM 1996 5 16 AALA960505 1 19960401 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 804.5 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 702AA 22460 TUL - FOUND CRACK IN CHORD ANGLE AT FASTENER HOLE BS 804.5, STRINGER 14L. STOP DRILLED CRACK PER SRM 51-10-1, INSTALLED DOUBLER PER SRM 51-40-3. (M) 2 L 7 3 4F A3WE 1996051600799 19960516 00799 NM 1996 5 16 AALA960506 1 19960401 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 804.5 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 702AA 22460 TUL - CRACK IN CHORD ANGLE AT FASTENER HOLE BS 804.5, STRINGER 14R. STOP DRILLED CRACKS PER SRM 51-10-1, INSTALLED DOUB LER PER SRM 51-40-3. (M) 2 L 7 3 4F A3WE 1996051600800 19960516 00800 NM 1996 5 16 AALA960507 1 19960402 A 5311 FRAME BOEING 727 727223 1384074 NM BS 420 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 878AA 21390 TUL - FOUND CRACK ON FRAME AT STATION 420 IN E/E COMPT. INSTALLED DOUBLER PER SRM 51-40-3. (M) 2 L 7 3 4F A3WE 1996051600801 19960516 00801 NM 1996 5 16 AALA960513 1 19960403 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1183 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 892AA 22008 TUL - FOUND .3125 INCH CRACK IN SUPPORT STRINGER BETWEEN VERTICAL BEAMS, STATION 1183 RBL 36 WL 270. INSTALLED NEW STRI NGER AT RBL 36 WL 270 STATION 1183. (M) 2 L 7 3 4F A3WE 1996051600802 19960516 00802 WP 1996 5 16 AALA960514 1 19960403 A 5347 TIE DOWN TRACK DOUG DC9 DC982 3022082 WP BS 1212-1320 CORRODED A AALA O OTHER O OTHER IN INSP/MAINT 1 SW 07 225AA 49175 TUL - CORROSION AT STATION 1212 TO 1320 RIGHT TRACK. REMOVED AND REPLACED TIE DOWN TRACK STATION 1212 TO 1320. (M) 2 L 7 2 4F A6WE 1996051600803 19960516 00803 WP 1996 5 16 AALA960515 1 19960329 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1320 CORRODED A AALA O OTHER O OTHER IN INSP/MAINT 1 SW 07 225AA 49175 TUL - FRAME CORROSION STATION 1320 L27B BOTTOM OF J ANGLE MATERIAL WAS REMOVED AND REPAIRED PER ESO. REPAIRED PER ESO 8 0559 DATED 4/3/96. (M) 2 L 7 2 4F A6WE 1996051600804 19960516 00804 SO 1996 5 16 ASOA96014 1 19960422 A 2730 3094301 ELEV TRIM SWITCH EMB 120 EMB120RT SO COCKPIT INOPERATIVE A ASOA H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED AP APPROACH 1 SO 11 240AS 120060 DURING APPROACH ATL-MYR, AIRCRAFT AUTOPILOT TRIM RAN AWAY FULL PITCH UP AND WOULD NOT DISENGAGE. CAPTAIN PULLED CIRCUIT BREAKER, REGAINED CONTROL AND DECLARED AN EMERGENCY. AIRCRAFT LANDED SAFELY IN MYR WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED CAPTAINS ELEVATOR TRIM SWITCH. OPERATIONAL CHECKS WERE GOOD IN ALL MODES, AIRCRAFT WAS RELEASED FOR FURTHE R SERVICE. (M) 2 L 7 2 4T RT A31SO 1996051600805 19960516 00805 WP 1996 5 16 CAL960495 1 19960416 A 2510 3A0710005163 SEAT DOUG DC9 DC982 3022082 WP LT COCKPIT INOP A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 17812 21263 376 49250 FLT NR 1832 - IAH - THE NR 2 GENERATOR FAILED IN FLIGHT. A SLIGHT ELECTRICAL BURNING ODOR WAS ALSO OBSERVED MOMENTARILY IN THE COCKPIT. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE NR 2 GENERATOR GCU WAS RERACKED. AN AC CROSSTIE CHECK WAS PERFORMED WITH THE NR 2 GENERATOR ON LINE AND AT FULL ELECTRICAL LOAD. OPERATION CHECKED GOOD WITH NO FAULTS NOTED. MA INTENANCE FOUND THE CAPTAIN'S SEAT AS THE SOURCE OF THE ELECTRICAL ODOR. THE CAPTAINS SEAT WAS REMOVED AND REPLACED. ( M) 2 L 7 2 4F A6WE 1996051600806 19960516 00806 NM 1996 5 16 CAL960499 1 19960416 A 5753 654643090 FLAP BOEING 737 737130 1384435 NM RT TE FORE FLAP DAMAGED A CALA O OTHER F FLT CONT AFFECTED LD LANDING 1 SW 09 14212 19029 FLT NR 439 - ORD - WHILE FLAPS WERE BEING MOVED AFTER TAKEOFF, THE AIRCRAFT ROLLED RIGHT. ABNORMAL AMOUNT OF LEFT RUDDE R WAS REQUIRED TO MAINTAIN DIRECTIONAL CONTROL OF AIRCRAFT. MAINTENANCE FOUND THE RIGHT INBOARD TRAILING EDGE FOREFLAP DAMAGED AND THE INBOARD FITTING WAS BROKEN. THE FOREFLAP AND FITTING WERE REMOVED AND REPLACED. THE FLAP WAS RIGGED IA W MM 27-51-41. OPERATIONAL CHECKS WERE GOOD. (M) 2 L 7 2 4F A16WE 1996051600807 19960516 00807 WP 1996 5 16 GRAA9627 1 19960412 A 3350 EA1D131DE BATTERIES DOUG DC9 DC987 3022087 WP CABIN DISCHARGED A GRAA K NONE L NO TEST IN INSP/MAINT 1 WP 11 1075T 49724 LINE MAINTENANCE AT RNO, DISCOVERED THAT BOTH OVERWING EXITS OVERHEAD EMERGENCY LIGHTS FAILED. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES. MAINTENANCE PERFORMED AN OPEATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM. THE EMERG ENCY LIGHT SYSTEM OPERATIONALLY CHECKED NORMAL. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A6WE 1996051600808 19960516 00808 NE 1996 5 16 HNAA9697918 2 19960319 A 7250 O-RING DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 ENGINE CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 979HA 373 FLT 3340 - DCA-HPN - DURING DESCENT INTO HPN WITH LOW POWER SETTING, THE CABIN BEGAN TO FILL WITH SMOKE. CYCLED EACH BL EED OFF AND RAISED CABIN ALTITUDE TO REMOVE SMOKE. THE AIRCRAFT LANDED IN HPN WITHOUT INCIDENT. REMOVED AND REPLACED T HE P2.5 AIR SWITCHING VALVE, NO FIX. REMOVED AND REPLACED THE NR 1 ENGINE. S/D - AFTER TEARDOWN WAS COMPLETE ON ENGINE S/N 121315, IT WAS FOUND THAT THE O-RING BETWEEN THE NR 6 AND NR 7 BEARING HOUSING WAS CRACKED AND DETERIORATED. (M) 2 H 7 2 4T 4 T RT A13NM E20NE 1996051600809 19960516 00809 NM 1996 5 16 IXKA960010 1 19960411 A 2133 10328051 OUTFLOW VALVE BOEING 727 727251 138408H NM LEFT STICKING A IXKA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 25 267US 2783 1232178 20289 FLT 11 - EWR-MCO - AFTER TAKEOFF, UNABLE TO MAINTAIN PRESSURIZATION, MANUAL CONTROLLER NO HELP. FOUND LEFT OUTFLOW VALV E STICKING AND DUMPING CABIN AIR. REPLACED SAME. (M) 2 L 7 3 4F A3WE 1996051600810 19960516 00810 WP 1996 5 16 IXXA9650 1 19960417 A 5270 SWITCH DOUG DC8 DC861 3021952 WP CARGO DOOR OUT OF ADJUST A IXXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 11 861PL 45964 ON CLIMB-OUT OF DAY, THE CARGO DOOR WARNING LIGHT CAME ON. THE AIRCRAFT RETURNED TO DAY FOR MAINTENANCE. MAINTENANCE I NSPECTED THE AIRCRAFT AND FOUND THE GANGBAR MICROSWITCH OUT OF ADJUSTMENT. THE SWITCH WAS ADJUSTED IAW THE ATI DC-8 MM AND OPS CHECKED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 4 4F 4A25 1996051600811 19960516 00811 NE 1996 5 16 M3HA96009 2 19960409 A 7313 SEALS AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE NR 2 ENG CRACKED A M3HA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 13 4209G 129 KOA - FLT 703 - ENGINE NR 2 ROLL BACK TO ABOUT 50 PERCENT TQ ALL OTHER IND GOOD, NO RESPONSE WITH THROTTLE. FOUND FUEL LEAK ON NR 2 ENGINE REPLACED SEALS ON FUEL NOZZLE 2, 3, 4, 5 LEAK CK GOOD ENG RUN CK GOOD IAW JIC 73-13-61 RAI 10000-001 . (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1996051600812 19960516 00812 1996 5 16 MZZA96019 4 19960409 A 3442 20704090101 RADAR ANTENNA BOEING 727 727224 1384076 NM FWD FUSELAGE FAILED A MZZA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 13 69741 10738 22250 GUM - FLT NR 868 - AFTER DEPARTURE FROM GUAM, WEATHER RADAR WILL NOT PAINT ON GROUND CLUTTER. SCREEN BLANKS OUT BETWEEN 30 DEGREES AND 60 DEGREES. AIRCRAFT DIVERTED BACK TO GUAM. MAINTENANCE FOUND WEATHER RADAR ANTENNA NO GOOD, REMOVED A ND REPLACED WEATHER RADAR ANTENNA, AS PRECAUTIONARY, ALSO REMOVED AND REPLACED WEATHER RADAR TRANSCEIVER UNIT. WEATHER RADAR SYSTEM TEST GOOD AND AIRCRAFT DISPATCHED. (M) 2 L 7 3 4F A3WE 1996051600813 19960516 00813 WP 1996 5 16 ORJA96019 1 19960327 A 3241 4062582 TRANSDUCER PINS DOUG DC9 DC982 3022082 WP NR 2 WHEEL AXLE FAILED A ORJA O OTHER N FALSE WARNING TO TAKEOFF 1 WP 11 824RA 53017 AT 50 KTS ON TAKEOFF ROLL, WHEEL NOT TURNING LIGHT ILLUMINATED. REPLACED ANTI-SKID TRANDUCER PINS IN NR 2 WHEEL AXLE. O PS CHECKED GOOD. (M) 2 L 7 2 4F A6WE 1996051600814 19960516 00814 WP 1996 5 16 ORJA96020 1 19960330 A 3350 41B994AD073 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 873RA 53093 AFT OVERWING EXIT EMERGENCY LIGHTS INOP. REPLACED BATTERIES IN BATTERY PACKS. OPS NORMAL. (M) 2 L 7 2 4F RT A6WE 1996051600815 19960516 00815 NE 1996 5 16 PLG22796E2 2 19960227 A 7250 6064T1 COOLING PLATE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE STG 2 ROTOR FAILED A PLGA E A ENGINE SHUTDOWN UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CR CRUISE 1 NE 05 363BE 340B293 785425 EN ROUTE FROM BOS-PHL - WHILE TRANSITIONING OUT OF A SLOWDOWN FROM ATC, PILOT ADVANCED POWER LEVERS AND HEARD A LOUD BAN G EMINATE FROM THE RIGHT ENGINE. CREW OBSERVED ENGINE INSTRUMENTS INDICATING LOSS OF POWER AND A CLIMBING ITT THAT REAC HED 1130 CELSIUS PRIOR TO SHUTDOWN. AN UNEVENTFUL SINGLE ENGINE LANDING WAS MADE IN ISLIP, NY. MAINTENANCE PERSONNEL O BSERVED EXTREME OIL LOSS FROM NACELLE DRAINS, STG 4 PT BLADES MISSING AND UPPER STRUTS IN PT MODULE FRACTURED. ENGINE R EMOVED AND DIRECTED TO O/H SHOP FOR INVESTIGATION. S/D TEAR DOWN INSPECTION REVEALED FAILURE OF THE STG 2 FWD COOLING P LATE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 1996051600816 19960516 00816 EU 1996 5 16 RAIA960404 1 19960404 A 5270 SP4594 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU CARGO BAY OUT OF ADJUST A RAIA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 CE 03 557HK 939 41074 BOS - FLT 7707 - CARGO DOOR WARNING ILLUMINATED DURING TAKEOFF ROLL. MAINTENANCE ISSUED DMI 52-3. MAINTENANCE LATER CL EARED DMI BY ADJUSTING CARGO DOOR MICROSWITCH, OPERATION CHECK GOOD. (M) 2 L 7 2 4T RT A41NM 1996051600817 19960516 00817 EU 1996 5 16 RAIA960405 1 19960407 A 3060 7826894 BRUSH BLOCK AEROSP ATR42 ATR42300 8680920 EU LT PROP WORN A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 422TE 1730 106 STL - FLT NR 7270 - LEFT PROP DE-ICE FAILED IN FLIGHT. MAINTENANCE REPLACED LEFT PROP DE-ICE BRUSH BLOCK, PERFORMED GRO UND RUNS, OPERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1996051600818 19960516 00818 EU 1996 5 16 RAIA960406 1 19960409 A 5311 S53672406200 FRAME AEROSP ATR42 ATR42300 8680920 EU AFT FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 421TE 17312 102 STL - DURING MAINTENANCE CHECK, FRAME 36 WAS FOUND TO HAVE CORROSION. MAINTENANCE REPAIRED FRAME 36 PER ATR SRM. (M) 2 H 7 2 4T RT A53EU 1996051600819 19960516 00819 EU 1996 5 16 RAIA960407 1 19960409 A 5313 S53671400203 STRINGER AEROSP ATR42 ATR42300 8680920 EU RT FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 421TE 17312 102 STL - DURING MAINTENANCE CHECK, CORROSION FOUND ON STRINGER 18 RIGHT SIDE, BETWEEN FRAMES 36 AND 37. MAINTENANCE REPAIR ED STRINGER PER ATR SRM. (M) 2 H 7 2 4T RT A53EU 1996051600820 19960516 00820 WP 1996 5 16 RAIA960408 2 19960409 A 7320 13711543C401 P3 LINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RT ENG FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 338TE 7701 932 66169 STL - NR 7280 - RIGHT BETA LIGHT ILLUMINATED ON TAKEOFF ROLL. MAINTENANCE REPLACED P3 LINE, GROUND RUNS GOOD. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996051600821 19960516 00821 EU 1996 5 16 RAIA960409 1 19960409 A 5315 S53672400000 FLOOR BEAM AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 421TE 17312 102 STL - DURING MAINTENANCE CHECK, SURFACE CORROSION WAS FOUND ON FLOOR BEAMS 36, 37, 38, 39. MAINTENANCE TREATED CORROSIO N PER ATR STRUCTURAL REPAIR MANUAL. (M) 2 H 7 2 4T RT A53EU 1996051600822 19960516 00822 EU 1996 5 16 RAIA960410 1 19960409 A 5347 S536780001000 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 421TE 17312 102 STL - DURING MAINTENANCE CHECK, FOUND SEAT TRACKS BETWEEN FRAMES 36 AND 39 HAD SURFACE CORROSION. MAINTENANCE TREATED C ORROSION PER ATR STRUCTURAL REPAIR MANUAL. (M) 2 H 7 2 4T RT A53EU 1996051600823 19960516 00823 EU 1996 5 16 RAIA960411 1 19960409 A 5347 S53678001200 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 421TE 17312 102 STL - DURING MAINTENANCE CHECK, CORROSION WAS FOUND ON RIGHT INBOARD SEAT TRACK BETWEEN FRAMES 36 AND 37. MAINTENANCE R EPLACED SEAT TRACK PER ATR STRUCTURAL REPAIR MANUAL. (M) 2 H 7 2 4T RT A53EU 1996051600824 19960516 00824 EU 1996 5 16 RAIA960412 1 19960409 A 2430 10200311 CONTROL UNIT AEROSP ATR72 ATR72202 8680940 EU NR 2 ENGINE FAILED A RAIA O OTHER H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 CE 03 722TE 10197 220 MLI - FLT NR 7165 - NR 2 DC GENERATOR FAULTED UNABLE TO RESET, DC BUS 2 INOP, GREEN HYD SYSTEM INOP. MAINTENANCE REPLAC ED NR 2 GEN LINE CONTACTOR AND GCU. OPERATIONAL CHECKS GOOD. (M) 2 H 7 2 4T RT A53EU 1996051600825 19960516 00825 EU 1996 5 16 RAIA960413 1 19960410 A 7332 41SG107100G14 PRESS TRANS BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT ENGINE FLUCTUATES A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 871JX 9662 871 66324 LAX - FLT NR 4735 - LEFT FUEL PRESSURE FLUCTUATIONS IN FLIGHT. MAINTENANCE REPLACED LEFT FUEL PRESSURE TRANSMITTER, PER FORMED GROUND RUNS OPERATIONAL CHECKS GOOD. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996051600826 19960516 00826 EU 1996 5 16 RAIA960414 1 19960411 A 2810 14128007404 NEGATIVE 'G' TAN JETAIR JETSTM JETSTM4101 1500501 EU RIGHT LOOSE LINE A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 552HK 2213 41057 STL - FLT NR 7215 - RIGHT FUEL PRESSURE LIGHT ILLUMINATED DURING FLIGHT MAINTENANCE TIGHTENED B-NUT ON NEGATIVE 'G' TANK , GROUND RUN GOOD. (M) 2 L 7 2 4T RT A41NM 1996051600827 19960516 00827 EU 1996 5 16 RAIA960415 1 19960411 A 2435 23079009 STARTER/GEN BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAULTY A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 426AM 874 CMI - FLT 7542 - BOTH GENERATOR LIGHTS ILLUMINATED AND ENGINES WERE SURGING. MAINTENANCE REPLACED LEFT STARTER GENERATO R AND PARALLELED GENERATORS, GROUND RUNS GOOD. (M) 2 L 7 2 4T RT A56EU 1996051600828 19960516 00828 EU 1996 5 16 RAIA960416 1 19960411 A 7712 31024766 TQ SIGNAL COND BAG JETSTM JETSTM3201 1500217 EU LT ENG OUT OF ADJUST A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 342TE 7848 7848 954 STL - FLT NR 7364 - LEFT ENGINE WILL NOT MAKE TARGET TORQUE. MAINTENANCE ADJUSTED TORQUE SIGNAL CONDITIONER, PERFORMED GROUND RUNS OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A56EU 1996051600829 19960516 00829 EU 1996 5 16 RAIA960417 1 19960412 A 7797 3035967 WIRE AEROSP ATR42 ATR42300 8680920 EU LT ENG EGT IND FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 421TE 14062 102 STL - FLT RN 7136 - LOST LEFT ENGINE ITT IN FLIGHT. MAINTENANCE REPLACED LEFT ENGINE ITT CABLE, PERFORMED GROUND RUNS O PERATIONAL CHECKS GOOD. (M) 2 H 7 2 4T RT A53EU 1996051600830 19960516 00830 EU 1996 5 16 RAIA960418 1 19960415 A 7714 AG34 TACH GENERATOR BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 429AM 7548 879 STL - FLT NR 7280 - LEFT RPM WENT TO ZERO. MAINTENANCE REPLACED LEFT ENGINE TACH GENERATOR, PERFORMED GROUND RUNS OPERA TIONAL CHECKS GOOD. (M) 2 L 7 2 4T RT A56EU 1996051600831 19960516 00831 EU 1996 5 16 RAIA960419 1 19960415 A 2150 2942A000 PRESSURE SWITCH JETAIR JETSTM JETSTM4101 1500501 EU LEFT AIR FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 554HK 1899 41067 JFK - FLT 7706 - AIR OFF CAPTION ILLUMINATED DURING CLIMB. MAINTENACNE REPLACED LEFT PRESSURE SWITCH, GROUND RUNS GOOD. (M) 2 L 7 2 4T RT A41NM 1996051600832 19960516 00832 EU 1996 5 16 RAIA960420 1 19960415 A 3260 9005EN38 UPLOCK SWITCH BAG JETSTM JETSTM3201 1500217 EU LT MLG FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 429AM 10777 879 STL - FLT NR 7508 - LEFT MAIN GEAR INTRANSIT LIGHT REMAINED ON AFTER GEAR RETRACTION. MAINTENANCE REPLACED LEFT GEAR UP LOCK SWITCH, PERFORMED GEAR SWING OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A56EU 1996051600833 19960516 00833 WP 1996 5 16 RAIA960421 2 19960416 A 7320 89778025 FUEL CONTROL BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT ENGINE OUT OF ADJUST A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 427AM 8067 876 66152 STL - FLT 7456 - LEFT ENGINE RPM WAS 103 DEGREES IN PROP GOV RANGE. MAINTENANCE ADJUSTED LEFT ENGINE RPM, GROUND RUNS G OOD. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996051600834 19960516 00834 WP 1996 5 16 RRXA96023 1 19960424 A 3231 CONTL VLV DOUG DC8 DC873F 302199F WP MLG DOOR OUT OF ADJUST A RRXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 15 791FT 46045 KDAY - FLT 8 - AFTER TAKEOFF DOOR NOT LATCHED LIGHT AND ALTERNATE MAIN DOOR LIGHT REMAINED ILLUMINATED. THE FLIGHT CREW RECYCLED THE LANDING GEAR, RETURNED TO KDAY. MAINTENANCE RIGGED THE MLG DOOR CONTROL VALVE. MAINTENANCE REMOVED AND R EPLACED THE MLG DOOR ACTUATOR AND CONTROL VALVE AS A PRECAUTION. OPERATIONAL CHECK OF THE MLG DOOR INDICATION SYSTEM WA S NORMAL ON GROUND CHECK. (M) 2 L 7 4 4F RT 4A25 1996051600835 19960516 00835 EU 1996 5 16 SIMA961201 1 19960429 A 5753 7257800504 SKIN SAAB SF340 340B 7860101 EU TE FLAP DELAMINATION A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 590MA 1069 340B181 LAW - DURING EM-1 CHECK, FOUND THE RIGHT FLAP LEADING EDGE HAD A VOID/DELAMINATION APPROXIMATELY 4 INCHES BY 30 INCHES L ONG. THE DAMAGE STARTED 39 INCHES FROM INBOARD END OF FLAP AND RUNNING OUTBOARD ALONG THE LEADING EDGE. FLAP WAS REMOV ED FROM SERVICE FOR REPAIRS AND ANOTHER SERVICEABLE FLAP ASSEMBLY WAS INSTALLED IAW SAAB AMM. (M) 2 L 7 2 4T RT A52EU 1996051600836 19960516 00836 EU 1996 5 16 SIMA961221 1 19960501 A 3320 3717 BALLAST AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 427MQ 4258 091 MSN - FLT 4046 - AFTER DEPARTURE FROM MSN THE PASSENGERS AND CREW DETECTED AN ELECTRICAL SMOKE SMELL IN THE CABIN, AIRCR AFT RETURNED TO MSN AND CFR RESPONED. INSPECTED AND FOUND THE LIGHT BALLAST FOR THE FORWARD LATERAL LIGHTS WAS THE SOUR CE OF THE ODOR. RAI'D BALLAST AND AIRED OUT THE CABIN, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996051600837 19960516 00837 NM 1996 5 16 TAOA049606 1 19960410 A 3260 69482726 CIRCUIT CARD BOEING 727 727225 1384077 NM E/E COMPT DEFECTIVE A TAOA O OTHER N FALSE WARNING AP APPROACH 1 EA 15 919TS 20447 RIGHT MAIN GEAR GREEN LIGHT DID NOT ILLUMINATE WHEN LANDING GEAR WAS POSITIONED DOWN. GEAR VERIFIED DOWN AND LOCKED FRO M VIEWING PORT. REPLACED MASTER WARNING DIMMER CARD, SYSTEM OPS CHECKED NORMAL IAW MM 33-10. (M) 2 L 7 3 4F A3WE 1996051600838 19960516 00838 NM 1996 5 16 TWRA9620 1 19960411 A 2130 BACR13CF2A RELAY R352 BOEING 747 747212B 1384886 NM CABIN FAILED A TWRA A G UNSCHED LANDING O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 EA 15 616FF 21939 DURING CRUISE AT FL 350, AIRCRAFT EXPERIENCED AN UNCONTROLLABLE CABIN CLIMB. RAPID DECOMPRESSION AND EMERGENCY DESCENT CHECKLIST WAS ACCOMPLISHED. INITIATED DESCENT TO 10,000 FEET RIGHT OUTFLOW VALVE CIRCUIT BREAKER POPPED, RESCENT AND PO PPED AGAIN. AIRCRAFT DIVERTED TO MUSCAT (MCT) UPON LANDING AT MCT. THE ITEM WAS DEFERRED TO THE ODI 04593 AND THE RIGHT OUTFLOW VALVE LOCKED IN THE CLOSE POSITION. OXYGEN MASK STOWED AND ITEM DEFERRED. DURING TROUBLESHOOTING, MAINTENANCE FOUND BURNT PIN ON RELAY R352 AND BURNT CONNECTOR AT CONTROLLER. ALL ITEMS WERE REPLACED AS REQUIRED. PRESSURIZATION CHECK COMPLETED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 4 4F A20WE 1996051600839 19960516 00839 NM 1996 5 16 TWRA9621 1 19960412 A 2560 GIRT BAR BOEING 747 747282B 1384860 NM L3 DOOR STUCK A TWRA K NONE O OTHER IN INSP/MAINT 1 EA 15 610FF 20501 AT DEPARTURE L-3 DOOR WOULD NOT GO INTO AUTOMATIC POSITION. INVESTIGATION FOUND GIRT BAR HANGING UP. GIRT BAR WAS FREE D. OPS CHECK, IAW MM 52-10-00. (M) 2 L 7 4 4F A20WE 1996051600840 19960516 00840 1996 5 16 UF6A96310 4 19960319 A 3420 2589419901 FLUX VALVE BAG ATP ATP EU NR 1 POSITION FAILED A UF6A A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 31 860AW 8030 2037 ORD - FLT 5708 - 'CHECK HEADING' ILLUMINATED IN FLIGHT BOTH NAV DISPLAY UNITS REMAINED ILLUMINATED WITH HEADING DIFFEREN CE EXCEEDING 65 DEGREES. MAINTENANCE REMOVED AND REPLACED NR 1 MAGNETIC SENSOR UNIT AND PERFORMED COMPASS SWING. SYSTE M CHECKED SATISFACTORY. (M) 2 L 7 2 4T RT A27NM 1996051600841 19960516 00841 EU 1996 5 16 USAAF96035 1 19960418 A 5270 DOOR WARNING FOKKER F28 F28MK4000 4990810 EU CARGO COMPT DR ACTIVATED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 475AU 11222 LEX - FLT 1147 - AT FL 260, CREW NOTICED AFT CARGO DOOR WARNING LIGHT ILLUMINATED. THE CREW DESCENDED TO 10,000 FEET, D EPRESSURIZED THE AIRCRAFT AND DIVERTED TO LEX. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT INCIDENT. MAINT ENANCE ACCOMPLISHED FUNCTIONAL TEST OF ALL THREE CARGO DOORS PER MAINTENANCE MANUAL 52-70-2. (M) 2 L 7 2 4F RT A20EU 1996051600842 19960516 00842 NM 1996 5 16 USAASB96052 1 19960320 A 3350 20131A BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 442US 24841 PIT - EMERGENCY LIGHTS NOT WORKING PROPERLY. MAINTENANCE REPLACED THE NR 1 EMERGENCY LIGHT BATTERY PACK. (M) 2 L 7 2 4F RT A16WE 1996051600843 19960516 00843 NM 1996 5 16 W8PA960010 1 19960417 A 3260 655825029 LOGIC CARD BOEING 737 737301 1384611 NM E/E COMPT FAILED A W8PA O OTHER N FALSE WARNING AP APPROACH 1 NM 03 949WP 23230 WITH GEAR UP, 3 RED LIGHTS ARE ON. REPLACED LANDING GEAR LOGIC CARD. (M) 2 L 7 2 4F RT A16WE 1996051600844 19960516 00844 NM 1996 5 16 WRLA96017 1 19960413 A 3246 43059940 TIRE PRESS SEN DOUG MD11 MD11 3023602 NM LT MLG MALFUNCTIONED A WRLA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 272WA 48437 ON TAKEOFF ROLL, FLIGHT CREW NTOED NR 4 MAIN WHEEL ASSY 'TIRE FAILURE ALERT' WAS DISPLAYED. FLIGHT CREW ELECTED TO RETU RN TO GATE FOR MAINTENANCE. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL NOTED NR 4 MAIN WHEEL TIRE PRESSURE INDICATION INOPERATIVE. ASSIGNED DMI M32AP13-43. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. M ANUFACTURER OF SUSPECTED PART IS 'LABINAL'. (M) 2 L 7 3 4F RT A22WE 1996051600845 19960516 00845 SO 1996 5 16 WTAA960067 1 19960331 A 5246 12016900010 FUEL SERVICE DR EMB 120 EMB120RT SO RT WING UNSECURED A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 17 454UE 120155 LAX - SERVICE DOOR WARNING LIGHT ILLUMINATED DURING TAKEOFF ROLL. MAINTENANCE INSPECTED SERVICE DOORS, FUOND FUEL SINGL E POINT REFUELING DOOR TO HAVE UNSECURED FASTENER. RESECURED DOOR. DOOR WARNING SYSTEM OPERATIONAL CHECK NORMAL. AIRC RAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996051600846 19960516 00846 SO 1996 5 16 WTAA960068B 1 19960401 A 7330 FUEL FILTER IND EMB 120 EMB120RT SO LT ENGINE ILLUMINATED A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 17 122AM 120013 SMF - LEFT ENGINE FUEL FILTER LIGHT ILLUMINATED ON TAKEOFF ROLL ABOVE 50 PERCENT TORQUE. TAKEOFF ABORTED WITHOUT INCIDE NT. MAINTENANCE DETERMINED TO BE INDICATION PROBLEM. DEFERRED FUEL FILTER LIGHT PER MEL 73-33-1. MAINTENANCE PROCEDUR ES COMPLIED WITH NO CONTAMINATION OF FILTERS NOTED DURING INSPECTION. AIRCRAFT RETURNED TO SERVICE. DEFERRAL SUBSEQUEN TLY CORRECTED BY THE INSPECTION OF THE INDICATION SYSTEM AND THE REPLACEMENT OF THE HIGH AND LOW PRESSURE FUEL FITLERS. (M) 2 L 7 2 4T RT A31SO 1996051600847 19960516 00847 SO 1996 5 16 WTAA960069 1 19960403 A 3230 1959500007 UPLOCK ACTUATOR EMB 120 EMB120RT SO LT MLG OUT OF ADJUST A WTAA O OTHER J WARNING INDICATION TO TAKEOFF 1 WP 17 455UE 120163 FAT - LEFT MAIN LANDING GEAR INTRANSIT LIGHT REMAINS ILLUMINATED MOMENTARILY AFTER GEAR RETRACTION. GEAR DOOR REPORTED SLOW TO CLOSE. MAINTENANCE ADJUSTED UPLOCK ACTUATOR ON LEFT MAIN LANDING GEAR. GEAR RETRACTION AND EXTENSION NORMAL DU RING GROUND CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996051600848 19960516 00848 SO 1996 5 16 WTAA960071 1 19960403 A 3230 20960 HOOK ASSY EMB 120 EMB120RT SO LT MLG OUT OF ADJUST A WTAA O OTHER J WARNING INDICATION TO TAKEOFF 1 WP 17 455UE 120163 SFO - LEFT MAIN LANDING GEAR INTRANSIT LIGHT REMAINS ILLUMINATED FOR 30 SECONDS AFTER GEAR RETRACTION. MAINTENANCE ADJU STED UPLOCK HOOK ROD ON LEFT MAIN LANDING GEAR. GEAR RETRACTION AND EXTENSION NORMAL DURING GROUND CHECK. AIRCRAFT RET URNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996051600849 19960516 00849 EU 1996 5 16 Y2PA96019 1 19960415 A 2932 11021SB PRESS SWITCH AMD FALC20 FALCOND 2720304 EU NR 2 HYD SYSTEM FAILED A Y2PA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 815AA 205 ELP - HYDRAULIC JEWEL LIGHT INTERMITTENT AFTER TAKEOFF, WAS THEN ON CONTINOUSLY ABOVE 10,000 FEET. CREW RETURNED TO POI NT OF DEPARTURE FOR MAINTENANCE. NO EMERGENCY PROCEDURES WERE REQUIRED. THE PROBLEM WAS DETERMINED TO BE A FAULTY PRES SURE SWITCH IN THE NR 2 HYDRAULIC SYSTEM. THE PRESSURE SWITCH WAS REPLACED, AN ENGINE WAS RUN, AND THE SYSTEM WAS GROUN D CHECKED GOOD. (M) 2 L 7 2 4F A7EU 1996051600850 19960516 00850 NE 1996 5 16 Y2PA96024 2 19960426 A 7260 544B38 GEAR BOX DOUG DC9 DC915F 3022037 WP PWA JT8 JT8D7B 52053 NE NR 2 ENG OIL LEAK A Y2PA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 23 197US 47154 P655239 DFW - SHUT DOWN RIGHT ENGINE DUE TO LOW OIL PRESSURE AND QUANTITY. INSPECTED AND FOUND ENGINE GEARBOX LEAKING AT SCAVEN GE PORT. REMOVED AND REPLACED GEARBOX. (M) 2 L 7 2 4F 4 F A6WE E2EA 1996052000001 19960520 00001 GL 1996 5 20 DHL9680303 2 19960323 A 7260 GARLOC SEAL DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C5 GL NR 1 ENGINE FAILED A T DHLA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 803DH 46123 NR 1 ENGINE OIL QUANTITY INDICATION WENT DOWN TO TWO QUARTS PERFORMED ENGINE SHUTDOWN. ALL OTHER PARAMETERS NORMAL. RE MOVED AND REPLACED GARLOC SEAL. 2 L 7 4 4F 4 F RT 4A25 E2GL 1996052000002 19960520 00002 NE 1996 5 20 96ZZZW59 2 19960106 A 7200 ENGINE LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B NE NR 1 FAILED A RIAA E A ENGINE SHUTDOWN UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SO 19 319EA 193A1040 DURING CRUISE, LOSS OF OIL PRESSURE ON NR 1 ENGINE, ENGINE SHUTDOWN. AIRCRAFT DIVERTED TO SAN JUAN PR. METAL FOUND ON CHIP DETECTORS. AIRCRAFT FERRIED ON 1-7-96 TO MIA FOR NR 1 ENGINE CHANGE. 2 L 7 3 4F 4 F A23WE E12EU 1996052000003 19960520 00003 EU 1996 5 20 SIMA960831 1 19960323 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 351AT 2170 354 DFW - FLT 3818 - FLIGHT ATTENDANT REPORTS EMERGENCY LIGHTS OVER WINDOW EXITS DO NOT TEST, BOTH LEFT AND RIGHT SIDES. RE PLACED FORWARD EMERGENCY BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1996052000004 19960520 00004 EU 1996 5 20 SIMA960501 1 19960219 A 3350 3101210 LIGHT AEROSP ATR42 ATR42300 8680920 EU AIRSTAIR INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 351AT 447 354 ORD - FLT NR 4006 - AIRSTAIR EMERGENCY EXIT LIGHT INOPERABLE. REPLACED LIGHT ASSY. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996052000005 19960520 00005 GL 1996 5 20 WTAA960051A 3 19960301 A 6114 7503503AF SEAL BAG JETSTM JETSTM3101 1500215 EU ROTOL R333 R333482F12 GL LT PROPELLER WORN A WTAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 17 413UE 797 CIC - SMOKE REPORTED IN CABIN DURING TAXI. AIRCRAFT RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE DETERMINED SOURCE O F SMOKE ODOR TO BE OIL LEAK AT LEFT PROPELLER. REPLACED LEFT PROPELLER DOME SEALS. SYSTEM OPERATIONALLY AND LEAK CHECK ED NORMAL DURING ENGINE GROUND RUN. NO EVIDENCE OF SMOKE ODOR IN CABIN AFTER REPLACEMENT OF DOME SEALS. AIRCRAFT RETUR NED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 6 C P61GL 1996052000006 19960520 00006 GL 1996 5 20 WTAA960051B 3 19960301 A 6114 750350333 SEAL BAG JETSTM JETSTM3101 1500215 EU ROTOL R333 R333482F12 GL LT PROPELLER WORN A WTAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 17 413UE 797 CIC - SMOKE REPORTED IN CABIN DURING TAXI. AIRCRAFT RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE DETERMINED SOURCE O F SMOKE ODOR TO BE OIL LEAK AT LEFT PROPELLER. REPLACED LEFT PROPELLER DOME SEALS. SYSTEM OPERATIONALLY AND LEAK CHECK ED NORMAL DURING ENGINE GROUND RUN. NO EVIDENCE OF SMOKE ODOR IN CABIN AFTER REPLACEMENT OF DOME SEALS. AIRCRAFT RETUR NED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 6 C P61GL 1996052000007 19960520 00007 NM 1996 5 20 UPS96405892 1 19960327 A 5311 FRAME BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE BS 1580 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED AFT CARGO COMP FOUND CRACKED IN FRAME UPPER FLANGE AT BS 1580 RT NEAR RT SIDE GUIDE. STOP DRILLED CRACK AND REPAIRED FRAME UPPER FLANGE ACC SRM 53-10-04, FIG 66. 2 L 7 4 4F 4 F A20WE E20EA 1996052000008 19960520 00008 GL 1996 5 20 UPS96805953 2 19960408 A 7200 ENGINE DOUG DC8 DC873F 302199F WP GE CFM CFM562 GL NR 3 FAILED A IPXA E A ENGINE SHUTDOWN UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 SO 01 812UP 46112 CREW REPORTED ON CLIMBOUT THROUGH 12,500 FT, NR 3 ENGINE SHUTDOWN WITH LOUD BANG AND RAPID SPOOL DOWN. ADVISED TO RETUR N TO SDF. IN PROCESS OF REMOVING AND REPLACING NR 3 ENGINE. 2 L 7 4 4F 4 F RT 4A25 E2GL 1996052000009 19960520 00009 NM 1996 5 20 UPS96405969 1 19960302 A 5313 STRINGER BOEING 747 747123 1384873 NM BS 920-940 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 MAINTENANCE REPORTED, BETWEEN STA 920 TO 940 STR 35 RT STRINGER IS CORRODED. CORROSION OUT OF LIMITS PER SRM 53-10-01. REPAIRED STR PER SRM 53-1003. 2 L 7 4 4F A20WE 1996052000010 19960520 00010 NM 1996 5 20 DLM88960939 1 19960419 A 4990 36280 APU DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE AFT FUSELAGE OIL LEAK A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 926DL 2840 P80509 49713 AFTER TAKEOFF, 3 LAV SMOKE DETECTORS WENT OFF. FLIGHT ATTENDANT REPORTED FUMES IN CABIN. FOUND APU LEAKING OIL AT GEAR BOX, BEING INGESTED, FWD TO MCO. PLACARD PER MEL 49-00-01A. RAN PACKS OFF ENG AIR. NO SMOKE NOTED. 2 L 7 2 4F 4 F RT A6WE E9NE 1996052100001 19960521 00001 NM 1996 5 21 C1HA960099 1 19960222 A 2760 414001410 ROD END BOEING 727 727223 1384074 NM RT SPOILER BROKEN A C1HA O OTHER F FLT CONT AFFECTED CR CRUISE 1 WP 23 706CA 19496 RIGHT OUTBOARD SPOILERS FLOATING, REQUIRES 10 UNITS OF LEFT RUDDER TRIM. FOLLOWED ABNORMAL SPOILER FLOAT PROCEDURE. FO UND ROD END FOR SPOILER CABLE TO NR 14 SPOILER BROKEN AT MIX BOX RIG BAR. REPLACED ROD END, RIGGED SPOILER CABLES AND S POILERS PER MM 2761-31, PAGE 502, ITEM 3. (X) 2 L 7 3 4F A3WE 1996052100005 19960521 00005 CE 1996 5 21 96ZZZX2368 1 19960325 A 3241 NAS16126 O-RING CESSNA 501 501 2076603 CE ANTI-SKID PUMP LEAKING A FZRA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 22TP 1964 5010014 O-RING AT T-FITTING AN917-6D WHERE ANTI-SKID PUMP PRESSURE SWITCH IS LOCATED WAS LEAKING. THE ACCUMULATOR PRESSURE WOUL D DROP AND COULD CAUSE BRAKING PROBLEMS. TIGHTENED B-NUT AT FITTING AND PRESSURE CHECKED. MARKED WITH TORQUE SEAL. SU BMITTER STATED ALL TYPE FITTINGS SHOULD BE MARKED WITH TORQUE SEAL FOR INSPECTION. 1 L 7 2 4F A27CE 1996052100009 19960521 00009 CE 1996 5 21 96ZZZX2372 1 19960214 A 3230 404188696 TUBE ASSY BEECH 18 E18S 1151006 CE TAIL GEAR SEIZED A VPDA O OTHER O OTHER AP APPROACH 1 SO 33 32M BA150 DURING APPROACH TO ROC, THE PILOT EXTENDED THE LANDING GEAR. THE TAIL GEAR DID NOT EXTEND TO THE FULL DOWN POSITION CAU SING THE SHEAR PIN TO FAIL AND GEAR TO RETRACT ON LANDING. AT FIRST, IT WAS SUSPECTED THE CAUSE WAS LACK OF LUBRICATION . AFTER REMOVING THE SLIDE TUBE ASSY, P/N 404-188696, DISCOVERED SOMETHING STRUCK THE SLIDE TUBE CAUSING IT TO SEIZE. A LL PARTS REPLACED AND GEAR RETRACTION PERFORMED. 1 L 7 2 3R A765 1996052300001 19960523 00001 WP 1996 5 23 9610599754 1 19960513 A 3350 BATTERY PACK DOUG DC9 DC941 302207N WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 754NW 47178 DURING LINE CHECK, FOUND CEILING EMERGENCY LIGHTS INOPERATIVE AT ROWS 6 AND 7. INSTALLED NEW BATTERIES. OPERATIONAL CH ECK OK. 2 L 7 2 4F A6WE 1996052300002 19960523 00002 WP 1996 5 23 9610609305 1 19960514 A 3233 59370365001 CYLINDER DOUG DC9 DC982 3022082 WP RT MLG DOOR MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 307RC 38738 2323 48086 DURING CLIMB-OUT OF GEG, GEAR DOOR OPEN AND RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED UPON GEAR RETRACTI ON. RECYCLED GEAR. DOWN AND LOCKED INDICATION GOOD. ON RETRACTION, GEAR DOOR OPEN AND GEAR UNSAFE LIGHT AGAIN REMAINE D ILLUMINATED. DIVERTED TO GTF AND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT MAIN LANDING GEAR RETRACT CYLINDER. LE AK AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996052300003 19960523 00003 WP 1996 5 23 9610619987 1 19960513 A 2613 OVERHEAT SENSOR DOUG DC9 DC932 3022066 WP TAIL COMPT FAILED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 987US 47458 TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED DURING CLIMBOUT. FLIGHT RETURNED TO SLC AND LANDED WITHOUT INCIDENT . MAINTENANCE REPLACED BOTH THE LEFT AND RIGHT TAIL COMPARTMENT OVERHEAT SENSORS AND RIGHT CHECK VALVE. OPERATIONAL CH ECK NORMAL. 2 L 7 2 4F A6WE 1996052300004 19960523 00004 NM 1996 5 23 9610622703 1 19960510 A 5350 655518668 RADOME BOEING 727 727225 1384077 NM FWD FUSELAGE WATER CONTAM A NWAA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 01 8878Z 21478 741 21451 DURING CRUISE FLIGHT, WEATHER RADAR BECAME UNRELIABLE. AIRCRAFT DIVERTED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED RADOME AND SEAL DUE RADOME FULL OF WATER ON LEFT SIDE. RADAR OPERATIONALLY CHECKED OK. 2 L 7 3 4F A3WE 1996052300005 19960523 00005 NM 1996 5 23 9610635501 1 19960413 A 3411 PITOT TUBE BOEING 757 757251 1384970 NM RIGHT FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 01 501US 23190 DURING FLIGHT, THE RIGHT AUXILIARY PITOT CAUTION MESSAGE APPEARED. AIRCRAFT DIVERTED TO DEN AND LANDED WITHOUT INCIDENT . MAINTENANCE REPLACED THE RIGHT AUXILIARY PITOT TUBE. SYSTEM OPERATIONAL CHECK OK. 2 L 7 2 4F RT A2NM 1996052300006 19960523 00006 NE 1996 5 23 9610642762 2 19960514 A 7321 FUEL CONTROL BOEING 727 7272M7 138407S NM PWA JT8 JT8D17 52049 NE NR 2 ENGINE MALFUNCTIONED A NWAA O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 GL 01 722RW 14411 14411 21201 DURING LEVEL OFF AND RETARDING OF THE THROTTLES, NR 2 ENGINE HAD A COMPRESSOR STALL. AIRCRAFT CONTINUED ON TO DESTINATI ON AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED CHECK OF INLET AND EXHAUST PS3 AND 13TH STAGE DUCT END CAPS. REP LACED FUEL CONTROL AND PUMP. PERFORMED FULL RUN AND TRIM. OPERATIONAL CHECK OK. 2 L 7 3 4F 4 F A3WE E2EA 1996052300007 19960523 00007 1996 5 23 9610651159 4 19960515 A 2330 1033452S WIRE DOUG DC10 DC1040 3023508 WP FUSELAGE FAILED A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 159US 46768 DURING CRUISE, MULTIPLEX SYSTEM POWER CABLE SHORTED AND SPARKED BETWEEN SEATS 33DE. MECHANIC ON BOARD DISCONNECTED THE POWER SOURCE FROM THE MUX BOX. FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. REPLACED SEATS, CABLES, AND SEAT BOXES. 2 L 7 3 4F A22WE 1996052300008 19960523 00008 EU 1996 5 23 9610663231 1 19960514 A 3250 C24736001 STEERING UNIT AIRBUS 320 A320211 3930320 EU RT COCKPIT CORRODED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 331NW 13280 318 WHILE ADDING POWER FOR TAKEOFF ROLL, LOST NOSE WHEEL STEERING. TAKEOFF WAS ABORTED AT APPROXIMATELY 10 KNOTS. AFTER COM ING TO A STOP, CREW RESET THE ANTI-SKID NOSE WHEEL STEERING SWITCH, CLEARED THE RUNWAY, AND RETURNED TO THE GATE. MAINT ENANCE REPLACED THE FIRST OFFICER'S STEERING CONTROL UNIT WITH NO HELP. AFTER CONFERRING WITH THE SHOP, REMOVED COVER F ROM THE NEW STEERING UNIT AND FOUND CORROSION BUILD-UP INSIDE ON CONNECTOR. CLEANED CORROSION FROM THE UNIT. OPERATION AL CHECK OK. 2 L 7 2 4F RT A28NM 1996052300009 19960523 00009 NE 1996 5 23 9610679304 2 19960513 A 7250 TURBINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE NR 2 ENGINE FAILED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 01 931MC 27567 3632 48057 709845 NR 2 ENGINE EXPERIENCED A CONTAINED TURBINE FAILURE DURING CLIMB-OUT. FLIGHT RETURNED TO ATL AND LANDED WITHOUT INCIDEN T. MAINTENANCE REPLACED NR 2 ENGINE ASSEMBLY. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F A6WE E9NE 1996052300010 19960523 00010 WP 1996 5 23 9610689943 1 19960515 A 2150 DUCT DOUG DC9 DC931 3022065 WP HEAT EXCHANGER LEAKING A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 1308T 47315 TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT RETURNED TO MSY AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND RIGHT HEAT EXCHANGER DUCT LEAKING. REPOSITIONED CLAMP. ALSO, CLEANED SENSOR CANNON PLUGS AND VENTS. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996052300011 19960523 00011 WP 1996 5 23 9610699926 1 19960514 A 3260 POSITION SWITCH DOUG DC9 DC932 3022066 WP NLG FAILED A NWAA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 01 926NW 47425 DURING APPROACH INTO HOU, NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR WAS EXTENDED. RECYCLED GEAR AND N ORMAL INDICATIONS WERE ACHIEVED. MAINTENANCE REPLACED NOSE LANDING GEAR LOCK SWITCH, OPERATIONAL CHECK NORMAL. AIRCRAF T RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996052300012 19960523 00012 NM 1996 5 23 96FDEA00977 1 19960515 A 5320 6556128 DOOR FRAME BOEING 727 727225 1384077 NM BS 950 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 468FE 21452 NR0408 AND 008, FOUND CORROSION UNDER LOWER DOOR STOP ON THE AFT CARGO DOOR FWD FRAME, BS 950E WL 155. *S/D* REPAIRED CORRODED FRAME AT BS 950E, WL 155 PER EA 7-5310-28290. 2 L 7 3 4F A3WE 1996052300013 19960523 00013 NM 1996 5 23 96FDEA00979 1 19960515 A 5741 TERMINAL PIN BOEING 727 727227 1384078 NM WING/FUS ATTACH CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 CORROSION C53-100-05-2/4 RIGHT WING REAR SPAR TO BODY FITTING TERMINAL PIN FOUND TO BE CORRODED. REMOVED AND REPLACED RIGHT WING REAR SPAR TO BODY FITTING TERMINAL PIN PER FEDEX MM 57-41-1. 2 L 7 3 4F A3WE 1996052300014 19960523 00014 NM 1996 5 23 96FDEA00980 1 19960515 A 5741 TERMINAL PIN BOEING 727 727227 1384078 NM WING/FUS ATTACH CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 CORROSION C53-100-05-1/3 LEFT AFT WING TO BODY FITTING TERMINAL PIN. REMOVED AND REPLACED LEFT WING REAR SPAR TO BODY F ITTING TERMINAL PIN PER FEDEX MM 57-41-1. 2 L 7 3 4F A3WE 1996052300015 19960523 00015 NM 1996 5 23 96UAL900349 1 19960515 A 3350 BULB BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 4719U 19880 LEFT SIDE AFT EXTERNAL OVERWING EMERGENCY LIGHT INOPERATIVE. BULB ELEMENT BURNED OUT. REPLACED BULB. 2 L 7 4 4F 4 F A20WE E20EA 1996052300016 19960523 00016 WP 1996 5 23 ABXA9600493 1 19960514 A 3260 7000010101ABX1 SWITCH DOUG DC9 DC932 3022066 WP NLG DEFECTIVE A ABXA K NONE N FALSE WARNING AP APPROACH 1 GL 23 986AX 47543 GREEN NOSE LANDING GEAR INDICATOR INTERMITTENTLY INOPERATIVE. BOTH BULBS. RECYCLED GEAR ON FINAL APPROACH, LIGHT CAME ON, BUT LATER WENT OUT. REPLACED NOSE GEAR DOWNLOCK SWITCH PER DC-9 M.M. 2 L 7 2 4F A6WE 1996052300017 19960523 00017 WP 1996 5 23 ABXA9600494 1 19960514 A 3260 7000010101ABX1 DNLOCK SWITCH DOUG DC9 DC933F 302207A WP NLG DEFECTIVE A ABXA O OTHER N FALSE WARNING AP APPROACH 1 GL 23 934AX 47462 DURING APPROACH WHEN LANDING GEAR HANDLE WAS PLACED DOWN, NO GREEN NOSE GEAR DOWN LIGHT ILLUMINATED. RECYCLED GEAR HAND LE AND ALL INDICATIONS WERE NORMAL. REPLACED NOSE GEAR DOWNLOCK AND UPLIMIT SWITCHES PER DC-9 M.M. 2 L 7 2 4F A6WE 1996052300018 19960523 00018 SO 1996 5 23 COMA9610144 1 19960515 A 6120 3036928 SIG COND UNIT EMB 120 EMB120RT SO RT ENGINE MALFUNCTION A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 255CA 15335 3420 120238 AUTO FEATHER SYSTEM WILL NOT TEST OR ARM. REPLACED THE RT ENGINE SIGNAL CONDITIONER UNIT. 2 L 7 2 4T RT A31SO 1996052300019 19960523 00019 SO 1996 5 23 COMA9610145 1 19960514 A 6120 78249024 PROP CONTL UNIT EMB 120 EMB120RT SO LT PROP MALFUNCTION A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 247CA 12695 704 120225 LEFT PROPELLER TAKES 30 SECONDS TO TRANSITION FROM FEATHER TO BETA RANGE. REPLACED THE PROPELLER CONTROL UNIT. 2 L 7 2 4T RT A31SO 1996052300020 19960523 00020 SO 1996 5 23 COMA9610146 1 19960514 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 161CA 12224 120143 EMERGENCY LIGHTING SYSTEM IS INOP. REPLACED THE EMERGENCY LIGHTS BATTERIES. 2 L 7 2 4T RT A31SO 1996052300021 19960523 00021 EU 1996 5 23 COMA9630107 1 19960515 A 2710 7227151692 CAM LEVER ASSY SAAB SF340 SF340A 7850100 EU RT AILERON BEARING FROZE A COMA O OTHER F FLT CONT AFFECTED UK UNKNOWN 1 SO 01 343CA 340A024 AILERON CONTROLS ARE BINDING DURING FLIGHT. REPLACED THE RT AILERON CENTERING CAM LEVER ASSY. ACFT RETURNED TO SERVICE . 2 L 7 2 4T RT A52EU 1996052300022 19960523 00022 EU 1996 5 23 COMA9630108 1 19960515 A 3411 PITOT SYST SAAB SF340 SF340A 7850100 EU FWD FUSELAGE WATER CONTAM A COMA K NONE O OTHER AP APPROACH 1 SO 01 146CA 340A146 ON APPROACH, ALL 3 AIR SPEED INDICATORS WERE DIFFERENT. DRAINED WATER FROM PITOT SYSTEM, AIR SPEED SYSTEM TEST NORMAL. 2 L 7 2 4T RT A52EU 1996052300023 19960523 00023 EA 1996 5 23 COMA9660090 1 19960515 A 3230 16215103 SWITCH BRACKET CNDAIR CL600 CL6002B19 EA NLG BENT A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 932CA 7038 NOSE LANDING GEAR WOULD NOT RETRACT. REPLACED BENT NLG PROXIMITY SWITCH BRACKET ASSY. ACFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1996052300024 19960523 00024 NM 1996 5 23 P5CA9600229 1 19960515 A 2710 AB10 CONTROL CABLE BOEING 747 747123 1384873 NM RT AILERON WORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 DURING PRE-DEPARTURE CHECK, FOUND RIGHT WING GEAR SHELF AREA AILERON CONTROL CABLE FORWARD OF HYDRAULIC RETURN FILTER WO RN BEYOND LIMITS. REMOVED AND REPLACED AB-10 CABLE PER MM 20-11-03. SWAGED NEW TERMINALS, INSTALLED, SAFETIED AND TENS IONED IAW MM 27-11-00. 2 L 7 4 4F A20WE 1996052300025 19960523 00025 WP 1996 5 23 SCNA96115 1 19960513 A 3350 EMBS1392 BATTERY PACK DOUG DC10 DC1030F 3023504 WP CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 602GC 47923 EMERGENCY LIGHT FAILED TO TEST. REPLACED EMERGENCY BATTERY PACK, OPS TEST NORMAL. 2 L 7 3 4F RT A22WE 1996052300026 19960523 00026 NM 1996 5 23 SCNA96116 1 19960423 A 5320 ANGLE BOEING 727 727225 1384077 NM BS 870 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING HEAVY MAINTENANCE VISIT, A CRACK WAS FOUND EXTENDING FROM A FASTENER LOCATION IN THE LEFT MLG WW LOWER CHORD AT B S 870 LBL 50. REMOVED TWO CRACKED ANGLES, FABRICATED AND INSTALLED NEW ANGLES IN ACCORDANCE WITH B727 SRM 51-30-2 AND 5 1-40-3 FIGURE 1. 2 L 7 3 4F A3WE 1996052300027 19960523 00027 NM 1996 5 23 SCNA96117 1 19960423 A 5311 FRAME BOEING 727 727225 1384077 NM BS 1090-1110 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON A FRAME IN THE AFT PIT BETWEEN BS 1090 AND BS 1110, AT LBL 12, WL 208.1. REMOVED CORROSION, FABRICATED AND INSTALLED A NEW SUPPORT AND STRAP IN ACCORDANCE WITH B727 SRM 53-10-2 AND MM 51-20-11. 2 L 7 3 4F A3WE 1996052300028 19960523 00028 NM 1996 5 23 SCNA96118 1 19960427 A 5315 BAC14902785 FLOOR BEAM BOEING 727 727225 1384077 NM BS 1110 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON A FLOOR BEAM ON THE LEFT SIDE OF THE CABIN AT BS 1110. REMOVED C ORROSION, FABRICATED AND INSTALLED A REPAIR IN ACCORDANCE WITH B727 SRM 53-10-8, FIGURE 3, AND MM 51-20-11. 2 L 7 3 4F A3WE 1996052300029 19960523 00029 NM 1996 5 23 SCNA96119 1 19960423 A 5311 FRAME BOEING 727 727225 1384077 NM BS 1110-1130 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON A FRAME IN THE AFT PIT AT BS 1110 TO 1130, BL 0, WL 208.1. REMOV ED CORROSION, FABRICATED AND INSTALLED AN ANGLE IN ACCORDANCE WITH B727 SRM 51-30-2, 51-20-1 AND MM 51-20-11. 2 L 7 3 4F A3WE 1996052300030 19960523 00030 NM 1996 5 23 SCNA96120 1 19960425 A 5315 BAC150643 FLOOR BEAM BOEING 727 727225 1384077 NM BS 344 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON THE UPPER SURFACE OF A FLOOR BEAM AT BS 344, LBL 30 TO RBL 16. R EMOVED CORRODED SECTION, FABRICATED AND INSTALLED A REPAIR SECTION IN ACCORDANCE WITH B727 SRM 53-10-8 AND MM 51-20-11. 2 L 7 3 4F A3WE 1996052300031 19960523 00031 NM 1996 5 23 SCNA96121 1 19960425 A 5315 BAC1505100617 FLOOR BEAM BOEING 727 727225 1384077 NM BS 1030 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON A FLOOR BEAM IN THE AFT CARGO PIT, BS 1030, BL ZERO, WL 208. REM OVED CORROSION, FABRICATED AND INSTALLED A REPAIR IN ACCORDANCE WITH B727 SRM 53-10-8, FIGURE 3. 2 L 7 3 4F A3WE 1996052300032 19960523 00032 NM 1996 5 23 SCNA96122 1 19960427 A 5315 BAC150643 FLOOR BEAM BOEING 727 727225 1384077 NM BS 1030 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON A FLOOR BEAM SUPPORT AT BS 1130. FABRICATED AND INSTALLED A NEW FLOOR BEAM SUPPORT IN ACCORDANCE WITH B727 SRM 53-10-4. 2 L 7 3 4F A3WE 1996052300033 19960523 00033 NM 1996 5 23 SCNA96124 1 19960422 A 5312 BULKHEAD STRAP BOEING 727 727225 1384077 NM BS 178 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING HEAVY MAINTENANCE VISIT, CRACKS WERE FOUND IN THE FORWARD BULKHEAD STRAP/SKIN BETWEEN THE 2ND, 3RD, 4TH, AND 5TH FASTENERS AT BS 178, BL ZERO, WL 183. FABRICATED A REPAIR DOUBLER AND STRAP IN ACCORDANCE WITH B727 SRM 51-30-2, AND SB 727-23-0065. 2 L 7 3 4F A3WE 1996052300034 19960523 00034 NM 1996 5 23 SCNA96125 1 19960422 A 5754 321ALSI ANGLE BOEING 727 727225 1384077 NM NR 4 SLAT CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING HEAVY MAINTENANCE VISIT, CRACKS WERE FOUND IN TWO SUPPORT ANGLE BRACKETS LOCATED AT THE NR 4 SLAT IN THE LEFT WIN G. FABRICATED AND INSTALLED TWO REPAIR DOUBLERS IN ACCORDANCE WITH B727 SRM 27-81-11, OPS CHECKED OK. 2 L 7 3 4F A3WE 1996052300035 19960523 00035 NM 1996 5 23 SCNA96126 1 19960429 A 5315 BAC14902785 FLOOR BEAM BOEING 727 727225 1384077 NM BS 1110 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON A FLOOR BEAM IN THE AFT PIT AT BS 1110, LBL 12 TO RBL 17, WL 208. REMOVED T-FLANGE, FABRICATED AND INSTALLED NEW T-FLANGE IN ACCORDANCE WITH B727 SRM 53-10-8, FIGURE 3. 2 L 7 3 4F A3WE 1996052300036 19960523 00036 NM 1996 5 23 SCNA96127 1 19960426 A 5711 SPAR BOEING 727 727225 1384077 NM LT WING CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING HEAVY MAINTENANCE VISIT, CRACKS WERE FOUND IN SKIN AROUND RIVETS JUST BELOW THE LOWER CHORD OF THE REAR SPAR UNDE R NR 2 AND NR 3 SPOILERS. FABRICATED AND INSTALLED A WAFFLE DOUBLER IN ACCORDANCE WIITH B727 SRM 51-40-3, FIGURE 1. 2 L 7 3 4F A3WE 1996052300037 19960523 00037 NM 1996 5 23 SCNA96128 1 19960426 A 5320 652427635 END CAP BOEING 727 727225 1384077 NM BS 1177 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON AN END CAP IN THE AFT PIT, BS 1177, STRINGER 25R. REMOVED CORROD ED END CAP FITTING AND INSTALLED A NEW FITTING IN ACCORDANCE WITH B727 SRM 51-30-2 AND MM 53-11-0. 2 L 7 3 4F A3WE 1996052300038 19960523 00038 NM 1996 5 23 SCNA96129 1 19960428 A 5347 BAC1520792 SEAT TRACK BOEING 727 727225 1384077 NM BS 340-480 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON SEVERAL SEAT TRACKS IN THE G-1 GALLEY AT BS 360 TO 380, RBL 24.5, RBL 45 AND RBL 56.5. REMOVED SEAT TRACK FROM BS 340 TO 480, RBL 24.5; BS 340 TO 420, RBL 45 AND BS 340 TO 380, RBL 56. 5. FABRICATED AND INSTALLED NEW SEAT TRACK SECTIONS IN ACCORDANCE WITH B727 SRM 53-10-5 FIGURE 7, 51-30-2 AND 51-10-2. 2 L 7 3 4F A3WE 1996052300039 19960523 00039 NM 1996 5 23 SCNA96130 1 19960513 A 3350 1102833 LIGHT BOEING 727 7272J4 1384006 NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 284SC 21438 AFT CENTER AISLE SELF-CONTAINED EMERGENCY LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED CENTER AISLE LIGHT ASSEMBLY AT ROW 25. 2 L 7 3 4F RT A3WE 1996052300040 19960523 00040 NM 1996 5 23 SWAA960362 1 19960509 A 5320 SPLICE BOEING 737 7373A4 1384585 NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICES CRACKED AT BS 907, S4R AND S4L. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996052300041 19960523 00041 NM 1996 5 23 SWAA960363 1 19960509 A 5320 WEB BOEING 737 7373A4 1384585 NM BS 639 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED D-CHECK, FOUND WEB CRACKS AT BS 639, RBL 65, WL 221 AND AT BS 616, RBL 65, WL 221. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996052300042 19960523 00042 NM 1996 5 23 SWAA960364 1 19960509 A 5320 STRAP BOEING 737 7373A4 1384585 NM BS 315 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM TENSION STRAP CRACKED AT BS 315, WL 200, RBL 30. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996052300043 19960523 00043 NM 1996 5 23 SWAA960365 1 19960509 A 5320 6545834261 SUPPORT BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORTS CORRODED AT BETWEEN BS 277 AND BS 294. ALSO, BETWEEN BS 294 AND BS 312, LBL 12. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996052300044 19960523 00044 NM 1996 5 23 SWAA960366 1 19960509 A 5320 MOP SILL BOEING 737 7373A4 1384585 NM BS 312/322 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED D-CHECK, FOUND MOP SILL CORRODED BETWEEN BS 312 AND BS 322, WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996052300045 19960523 00045 NM 1996 5 23 SWAA960367 1 19960509 A 5330 SKIN BOEING 737 7373A4 1384585 NM GALLEY DR CUTOUT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT LOWER AFT CORNER OF FORWARD GALLEY DOOR CUTOUT. REPAIRED PER B OEING SRM. 2 L 7 2 4F RT A16WE 1996052300046 19960523 00046 NM 1996 5 23 SWAA960368 1 19960508 A 3350 20121 BATTERY PACK BOEING 737 7373A4 1384585 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED SERVICE CHECK, FOUND RT AFT SERVICE DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK HOUS ING PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996052300047 19960523 00047 NM 1996 5 23 SWAA960369 1 19960508 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED B-CHECK, FOUND FUSELAGE SKIN DENTED 15 INCHES AFT OF AFT ENTRY DOOR, 26 INCHES BELOW EMERGENCY EXIT LIG HT. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996052300048 19960523 00048 NM 1996 5 23 SWAA960370 1 19960510 A 3230 651781914 UPLOCK ACTUATOR BOEING 737 7373H4 1384600 NM NLG FAILED A SWAA K NONE O OTHER AP APPROACH 1 SW 07 304SW 22944 ON APPROACH, NOSE GEAR DID NOT EXTEND, SLOWED AND RETRIED. NOSE GEAR EXTENDED. AIRCRAFT LANDED NORMALLY IN PHX. REPLA CED UPLOCK ACTUATOR, NOSE GEAR SEQUENCING VALVE AND OPS CHECKED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996052300049 19960523 00049 NM 1996 5 23 SWAA960371 1 19960510 A 3397 20121 WIRE BOEING 737 7373H4 1384600 NM CABIN SHORTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 361SW 26572 DURING SCHEDULED RON, FOUND EMERGENCY LIGHTS INOPERATIVE FROM BS 500 TO BS 616. REPAIRED SHORTED WIRE OVER LEFT EMERGEN CY EXIT AND REPLACED M1134 DUE TO BLOWN FUSE. OPS CHECKED NORMAL PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996052300050 19960523 00050 NM 1996 5 23 SWAA960372 1 19960510 A 3350 BATTERY BOEING 737 7375H4 138449D NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 519SW 25318 FOUND AFT LOWER EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT BATTERY PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996052300051 19960523 00051 NM 1996 5 23 SWAA960373 1 19960510 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 481 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED D-CHECK, FOUND MULTIPLE DENTS AND CRACKS IN FUSELAGE FRAME AT BS 481, LBL 35, LBL 59, WL 162-182. REPA IRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996052300052 19960523 00052 NM 1996 5 23 SWAA960374 1 19960510 A 5730 SKIN BOEING 737 7373A4 1384585 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/4 D-CHECK, FOUND RT WING SKIN CRACKED AT NR 5 L/E SLAT ACTUATOR CUT-OUT. REPAIRED PER BOEING DRAWING 65C30133. 2 L 7 2 4F RT A16WE 1996052300053 19960523 00053 NM 1996 5 23 SWAA960375 1 19960513 A 5350 RADOME BOEING 737 7372H4 138448C NM NOSE DAMAGED A SWAA A UNSCHED LANDING C F.O.D. TO TAKEOFF 1 SW 07 91SW 22963 ON TAKEOFF, AIRCRAFT HAD LIGHTNING STRIKE TO RADOME AREA. ALL SYSTEMS FUNCTIONING NORMALLY. AIRCRAFT RETURNED TO MDW A ND MADE AN UNEVENTFUL LANDING. PERFORMED LIGHTNING STRIKE INSPECTION AND REPLACED RADOME PER BOEING M/M. 2 L 7 2 4F A16WE 1996052300054 19960523 00054 NE 1996 5 23 SWAA960376 2 19960512 A 7200 332A1000 ENGINE BOEING 737 7373H4 1384600 NM GE CFM56 CFM563B1 13802 NE NR 2 DAMAGED A SWAA K NONE O OTHER TX TAXI/GRND HDL 1 SW 07 315SW 23337 720293 ON LANDING ROLL, AIRCRAFT LEFT GEAR LEFT RUNWAY. AIRCRAFT RETURNED TO RUNWAY AND CONTINUED TO GATE. PERFORMED GEAR SID ELOAD INSPECTION, REPLACED NR 2 ENGINE DUE TO FOD DAMAGE, REPAIRED 3 SKIN AREAS FOR GOUGES, AND RT I/B AFT FLAP. REPLAC ED ONE AND REPAIRED ANOTHER NR 2 ENGINE REVERSER CASCADES. TEST HOPPED AIRCRAFT. REPLACED ALL GEAR WHEEL/TIRE ASSEMBLI ES. ALL WORK PER BOEING M/M AND SRM. 2 L 7 2 4F 4 F RT A16WE E2GL 1996052300055 19960523 00055 NM 1996 5 23 SWAA960377 1 19960513 A 2782 65446519 ACTUATOR BOEING 737 7372T4 1384492 NM NR 5 LE FLAP FAILED A SWAA D RETURN TO BLOCK F FLT CONT AFFECTED CL CLIMB 1 SW 07 130SW 22699 AFTER TAKEOFF, NR 5 L/E SLAT WOULD NOT RETRACT. AIRCRAFT RETURNED TO HOU AND MADE AN UNEVENTFUL LANDING. REPLACED SLAT ACTUATOR PER BOEING M/M. 2 L 7 2 4F A16WE 1996052300056 19960523 00056 NM 1996 5 23 SWAA960378 1 19960513 A 3397 WIRE BOEING 737 7373H4 1384600 NM CABIN DAMAGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 387SW 26602 FOUND EXIT FLOOR LIGHTING INOPERATIVE IN ONE AREA. REPAIRED TRACK WIRING PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996052300057 19960523 00057 NM 1996 5 23 SWAA960379 1 19960510 A 3397 WIRE BOEING 737 7375H4 138449D NM CABIN DAMAGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 506SW 24183 FOUND CABIN EMERGENCY FLOOR LIGHTING INOPERATIVE AT MID-CABIN AREA. REPAIRED TRACK WIRING PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996052300058 19960523 00058 NM 1996 5 23 SWAA960380 1 19960511 A 5312 BULKHEAD WEB BOEING 737 7373Q8 1384670 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED SV CHECK, FOUND BULKHEAD AT BS 178 PRESSURE WEB CRACKED AT WL 213, RBL 6.7. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996052300059 19960523 00059 NM 1996 5 23 SWAA960381 1 19960511 A 5312 BULKHEAD WEB BOEING 737 7373Q8 1384670 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED SV CHECK, FOUND BULKHEAD AT BS 178 PRESSURE WEB CRACKED 3 PLACES AT WL 201, WL 199 AND WL 198, RBL 4.7. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996052300060 19960523 00060 NM 1996 5 23 SWAA960382 1 19960511 A 5312 BULKHEAD WEB BOEING 737 7373Q8 1384670 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED SV CHECK, FOUND BULKHEAD AT BS 178 PRESSURE WEB CRACKED 3 PLACES AT WL 213, LBL 4.7 AND LBL 6.7, WL 209 .5. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996052300061 19960523 00061 NM 1996 5 23 SWAA960383 1 19960511 A 5320 ANGLE BOEING 737 7373Q8 1384670 NM BS 380 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED SV CHECK, FOUND INTERCOSTAL TO FRAME ANGLE CRACKED AT BS 380, LBL 24, WL 155. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996052300062 19960523 00062 NM 1996 5 23 SWAA960384 1 19960511 A 5320 CLIP BOEING 737 7373Q8 1384670 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED SV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, S19L, WL 192. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996052300063 19960523 00063 NM 1996 5 23 SWAA960385 1 19960511 A 5330 SKIN BOEING 737 7373Q8 1384670 NM BS 294.5-312 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED SV CHECK, FOUND FUSELAGE SKIN DENTED AT BS 294.5 TO BS 312, BETWEEN S20 AMD 21R. REPAIRED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1996052300064 19960523 00064 NM 1996 5 23 SWAA960386 1 19960511 A 5330 SKIN BOEING 737 7373Q8 1384670 NM BS 328 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED SV CHECK, FOUND FUSELAGE OUTER SKIN CRACKED AT BS 328, WL 211, RBL 65. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996052300065 19960523 00065 NM 1996 5 23 SWAA960387 1 19960511 A 5320 WEB BOEING 737 7373Q8 1384670 NM BS 639 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED SV CHECK, FOUND WEB CRACKED AT BS 639, RBL 66, WL 221. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996052300066 19960523 00066 NM 1996 5 23 SWAA960388 1 19960511 A 5330 SKIN BOEING 737 7373Q8 1384670 NM BS 460-480 CREASED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED SV CHECK, FOUND FUSELAGE SKIN CREASED AT BS 460 TO BS 480, RBL 1 TO RBL 4, WL 149. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996052300067 19960523 00067 NM 1996 5 23 UPS96220118 1 19960515 A 3350 LIGHT BOEING 727 72725C 138400H NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE: EMERGENCY EXIT LIGHT FAILED TO TEST. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY. 2 L 7 3 4F A3WE 1996052300068 19960523 00068 NM 1996 5 23 UPS96420104 1 19960515 A 5270 SWITCH BOEING 747 747121 1384871 NM CARGO DOOR DIRTY A IPXA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 SO 01 681UP 19661 INSPECTION TYPE: C. AFT CARGO DOOR LIGHT ILLUMINATED WHEN REACHING 2.4 PSI DIFF. REQUIRED AIR TURN BACK. CLEANED AFT CARGO DOOR LIGHT SWITCHES, CYCLED DOOR OPEN AND CLOSED, PRESSURIZED AIRCRAFT TO 7.0 PSID. OPS CHECKED NORMAL. 2 L 7 4 4F A20WE 1996052300069 19960523 00069 WP 1996 5 23 UPS96820103 1 19960514 A 3350 5708458503 BATTERY PACK DOUG DC8 DC871F 302199D WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE: C. COCKPIT EMERGENCY EXIT LIGHTS FAIL TO ILLUMINATE WHEN TESTED. REMOVED AND REPLACED COCKPIT EMERGE NCY LIGHT BATTERY PACK. 2 L 7 4 4F RT 4A25 1996052300070 19960523 00070 WP 1996 5 23 UPS96820105 1 19960425 A 5320 57500922 FITTING DOUG DC8 DC873F 302199F WP FS 902 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE: C. RIGHT TRAP FITTING AFT OUTBOARD VERTICAL FLANGE HAS .75 INCH CRACK, FS 902, LONGERON 24R. REPLACED FITTING PER DRAWING NR 5750092. 2 L 7 4 4F RT 4A25 1996052300071 19960523 00071 WP 1996 5 23 UPS96820106 1 19960418 A 5313 5750198502 LONGERON DOUG DC8 DC873F 302199F WP FS 857 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE: C. HIGH FREQUENCY EDDY CURRENT INSPECTION INDICATES CRACK AT LONGERON 24R, FS 857 AT BOLT ATTACH HOLE . REPLACED LONGERON SECTION PER DRAWING NR 575198 AND NR 5750127. 2 L 7 4 4F RT 4A25 1996052300072 19960523 00072 WP 1996 5 23 UPS96820107 1 19960418 A 5711 5597841502 SPAR DOUG DC8 DC873F 302199F WP WS 624 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE: C. RIGHT WING REAR SPAR UPPER CHORD ANGLE CRACKS AT STA XRS624. REPAIRED PER UPS EO DC8-57-0671. 2 L 7 4 4F RT 4A25 1996052300073 19960523 00073 WP 1996 5 23 UPS96820108 1 19960426 A 5541 5656223 RIB DOUG DC8 DC873F 302199F WP RUDDER STA XR120 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE: C. RUDDER NOSE RIB, STA XR120, LT CRACKED. REPAIRED RIB PER UPS EO DC8-55-0083. 2 L 7 4 4F RT 4A25 1996052300074 19960523 00074 WP 1996 5 23 UPS96820109 1 19960426 A 5512 565174758 SKIN DOUG DC8 DC873F 302199F WP LT HORIZ STAB CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE: C. LEFT HORIZONTAL STABILILZER, LOWER SURFACE INBOARD T/E SKIN PANEL HAS CORROSION BULGES. REPLACED SKIN PANEL PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1996052300075 19960523 00075 WP 1996 5 23 UPS96820110 1 19960422 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP FS 15 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE: C. COCKPIT SUBFLOOR FINGER DOUBLER HAS CORROSION DAMAGE AT FS 15, LONGERON 22L. REPLACED FINGER DOUB LER SECTION PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996052300076 19960523 00076 WP 1996 5 23 UPS96820111 1 19960419 A 5753 37754062 FLAP TRACK DOUG DC8 DC873F 302199F WP RT TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE: C. RIGHT WING FLAP TRACK HAS CORROSION AT STA XW340. REPLACED TRACK PER MM 27-51-03. 2 L 7 4 4F RT 4A25 1996052300077 19960523 00077 WP 1996 5 23 UPS96820112 1 19960418 A 5753 37759051 FLAP TRACK DOUG DC8 DC873F 302199F WP RT TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE: C. RIGHT WING FLAP TRACK HAS CORROSION AT STA XW219. REPLACED TRACK PER MM 27-51-03. 2 L 7 4 4F RT 4A25 1996052300078 19960523 00078 WP 1996 5 23 UPS96820113 1 19960419 A 5753 37758041 FLAP TRACK DOUG DC8 DC873F 302199F WP RT TE FLAP CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE: C. RIGHT WING FLAP TRACK HAS CORROSION AT STA STA 98. REPLACED TRACK PER MM 27-51-03. 2 L 7 4 4F RT 4A25 1996052300079 19960523 00079 WP 1996 5 23 UPS96820114 1 19960419 A 5753 WING TRACK DOUG DC8 DC873F 302199F WP RT TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE: C. RIGHT WING FLAP HAS CORROSION AT STA XW3. REPLACED TRACK PER MM 27-51-03. 2 L 7 4 4F RT 4A25 1996052300080 19960523 00080 WP 1996 5 23 UPS96820115 1 19960419 A 5753 3775990702 FLAP TRACK DOUG DC8 DC873F 302199F WP RT TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE: C. RIGHT WING FLAP HAS CORROSION AT STA XW 428. REPLACED TRACK PER MM 27-51-03. 2 L 7 4 4F RT 4A25 1996052300081 19960523 00081 WP 1996 5 23 UPS96820116 1 19960418 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FS 300-320 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE: C. MODERATE CORROSION DAMAGE ON BOTTOM SIDE OF THE SEAT TRACK. SPLICE BETWEEN STA 300-320. REPLACED SPLICES PER SRM 51-3-0. 2 L 7 4 4F RT 4A25 1996052300082 19960523 00082 WP 1996 5 23 UPS96820117 1 19960419 A 5320 WEB DOUG DC8 DC873F 302199F WP FS 240-260 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE: C. FS 240 - FS 260, TUNNEL WEB CRACKED AND CORRODED. REPLACED DOUBLER WEB SECTION PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996052300083 19960523 00083 NM 1996 5 23 VNAA9600031 1 19960510 A 3234 7178011 GEAR SELECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT INSTR PANEL DEFECTIVE A VNAA K NONE J WARNING INDICATION AP APPROACH 1 GL 07 436JS 1891 3052 ON APPROACH TO TYS, CREW SELECTED GEAR DOWN. NO RESPONSE. THE F/O THEN CYCLED THE LANDING GEAR SELECTOR HANDLE SEVERAL TIMES, STILL NO RESPONSE. CREW THEN ELECTED TO MANUALLY EXTEND THE LANDING GEAR. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT WAS LATER FERRIED TO P.I.T. WHERE MX REPLACED THE LANDING GEAR SELECTOR I.A.W. M.M. 32-31-01, JACKE D THE AIRCRAFT AND SWUNG THE GEAR, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. PART TOTAL CYCLES, 185. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996052300084 19960523 00084 NM 1996 5 23 VNAA9600032 1 19960513 A 7712 311197801 TORQUE SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE DEFECTIVE A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 07 457PS 1144 3048 ON THE TAKEOFF ROLL, LT ENGINE TORQUE INDICATION WAS NOT AT THE MINIMUM LEVEL FOR TAKEOFF. CREW ABORTED THE TAKEOFF AND RETURNED TO THE TAXIWAY. CONDUCTED A POWER ASSURANCE RUN TO CHECK ENGINE PARAMETERS. ALL CHECKED NORMAL, CREW CONTINU ED WITH TAKEOFF. PROBLEM OCCURRED IN-FLIGHT, CREW CONTINUED WITH THE FLIGHT AND LANDED AT THE ORIGINAL DESTINATION WITH OUT FURTHER INCIDENT. CAK MX REPLACED LT ENGINE TORQUE SENSOR I.A.W. M.M. 77-11-00. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996052300086 19960523 00086 EU 1996 5 23 96ZZZX2526 1 19960215 A 6410 704A33633171 HINGE SNIAS 350 AS350B 8680801 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 22UM 78 1065 TAIL ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00. CORREC TED PROBLEM. 1 G 7 1 3U H9EU 1996052300096 19960523 00096 GL 1996 5 23 96ZZZX2537 2 19960313 A 7250 6898735 TURBINE BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL NR 8 BEARING MAKING METAL A NYBA O OTHER J WARNING INDICATION AP APPROACH 1 EA 11 83086 10432 1785 914 ENGINE CHIP LIGHT ILLUM ON FINAL APPROACH. MECHANIC INSPECTED ENG CHIP PLUGS & FND FUZZ & LIGHT METAL ON UPPER CHIP PLU G. PENALTY RUN ACCOMPLISHED & WHILE ON SHUT DOWN AT APPROX 35-40 PERCENT N1, MECHANIC HEARD NOISE (HVY GRINDING) FROM E NG AREA. MECHANIC MOTORED ENG & ON SPOOL DOWN, HEARD A GRINDING NOISE COMING FROM TURB ASSY. MECH PULLED ENG CHIP PLUG S & FND A MASSIVE AMT OF METAL ON UPPER CHIP PLUG. UPON TEAR DOWN OF ENG ASSY, INSP REVEALED N1 TURB HARD TO TURN, & A LARGE AMT OF METAL NOTED IN ENG GEARBOX. FURTHER INSP REVEALED FUEL NOZZLE CRACKED APPROX 6-8 INCHES IN LENGTH. NOTED NR 8 BEARING DESTROYED. BOTH GRBX ASSYS SN CAG-35884 & MINI SN KEY-1028 IST (780.5) WERE SENT FOR REPAIR & EVALUATION. 1 G 7 1 3U 3 U H2SW E4CE 1996052300097 19960523 00097 GL 1996 5 23 96ZZZX2538 2 19960319 A 7250 6887190 ENGINE ASSY BELL 206 206L 1181522 SW ALLSN 250C 250C20B 03013 GL NR 8 BEARING MAKING METAL A A NYBA O OTHER J WARNING INDICATION AP APPROACH 1 EA 11 122NH 10432 45101 CAE821672F PILOT NOTED A HIGH PITCH WHINE EMANATING FROM THE ENGINE AREA. A VISUAL INSPECTION WAS PERFORMED OF THE ENGINE AND DRIV E TRAIN AREAS. NO DEFECTS NOTED. THE ENGINE CHIP PLUGS WERE INSPECTED. NO METAL NOTED. APPROX 1.50 HRS AFTER INSPECT ION, ENGINE CHIP LIGHT ILLUMINATED WHILE PILOT WAS ON FINAL APPROACH. UPON SHUT DOWN, MECHANIC INSPECTED ENGINE CHIP PL UGS AND FOUND MODERATE AMOUNTS OF METAL ON UPPER PLUG. ENGINE ASSY REMOVED FOR REPAIR. UPON TEAR DOWN INSPECTION, NO B INDING NOTED IN THE TURBINE ASSY. NR 8 BEARING COVER REMOVED AND SHEAR PIN WHICH RETAINS THE RETAINER PLATE WAS FOUND L YING IN THE PLATE. NOTED THE NUT RETAINING THE TIE-BOLT HAD LOST TORQUE. 1 G 7 1 3U 3 U H2SW E4CE 1996052300098 19960523 00098 WP 1996 5 23 96ZZZX2539 1 19960204 A 2120 DUCT DOUG DC9 DC932 3022066 WP LEFT LOOSE A VJ6A G O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 SO 11 916VV 47445 CABIN PRESSURIZATION FAILED AT FL 350 (1,000-1,500 FEET FPM CABIN CLIMB), CABIN PRESSURE MASTER WARNING ILLUMINATED AND ALL MASKS DROPPED. RESECURED DUCT AFT SIDE OF LEFT WATER SEPARATOR. PRESSURIZATION CHECK OK PER MM 21-30 SYSTEM. OPS CHECK GOOD, SECURED MASKS. 2 L 7 2 4F A6WE 1996052300099 19960523 00099 NE 1996 5 23 96ZZZX2540 2 19960312 A 7320 ENGINE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7B 52053 NE NR 1 OUT OF ADJUST A VJ6A C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 11 916VV 47445 ABORTED TAKEOFF, NR 1 ENGINE WOULD NOT MAKE TARGET EPR (1.95) N1 INDICATED 847 DEGREES WITH LEFT THROTTLE ALL THE WAY TO STOP (N2, FUEL FLOW, EGT APPEARED NORMAL ON NR 1 ENGINE). EPR WOULD ONLY MAKE 1.84 THROTTLE FULL FORWARD. TRIMMED NR 1 ENGINE TO MM REF 71-00, PAGE 549, FIGURE 508, SHEET 11. 2 L 7 2 4F 4 F A6WE E2EA 1996052300100 19960523 00100 WP 1996 5 23 96ZZZX2541 1 19960225 A 3320 PAX WARN SIGN DOUG DC9 DC932 3022066 WP CABIN SMOKING A VJ6A K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 11 939VV 47089 WHILE SITTING AT GATE IN MCO MAKING PA ANNOUNCEMENTS, THE CIRCUIT BREAKER'S FOR PA INTERPHONE, 'NO SMOKING' AND 'FASTEN SEAT BELT' LIGHTED SIGNS TRIPPED. SMOKE SMELL IN THE CABIN. ACCOMPLISHED VALUJET AIRLINES EO DC-9-3396005, SEAT BELT, NO SMOKING SIGN, PASSENGER WARNING SYSTEM WIRING. 2 L 7 2 4F A6WE 1996052300101 19960523 00101 EU 1996 5 23 96ZZZX2542 1 19960308 A 3230 C24589000 UPLOCK BOX AEROSP ATR42 ATR42300 8680920 EU LANDING GEAR CLOSED A NVEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 03 144DD 074 LANDING GEAR WOULD NOT FULLY RETRACT AFTER TAKEOFF. SAFELY RETURNED TO MIA. RESET UPLOCK BOXES VIA AUXILIARY EXTENSION HANDLE. GEAR RETRACTION TESTS SATISFACTORY. 2 H 7 2 4T RT A53EU 1996052300102 19960523 00102 NM 1996 5 23 96ZZZX2543 1 19960303 A 3320 61362 BALLAST DAYRAY BOEING 737 7372T4 1384492 NM AFT GALLEY OVERHEATED A ZZDA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 15 467AT 9216 22055 ORLANDO - FLT 900 - DEPARTED AT APPROX 14:20, 3-3-96. AT 14:25, FLIGHT WAS RETURNING TO ORLANDO. IT WAS REPORTED AN EL ECTRICAL BURNING SMELL WAS COMING FROM THE AFT LAVATORY AND GALLEY AREA. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURT HER INCIDENT. MAINTENANCE INVESTIGATION REVEALED A SHORTED WIRE TO GROUND BETWEEN RELAY M303 AND THE WORK LIGHT FIXURE CAUSING THE BALLAST TO BURN OUT. THIS CAUSED THE BURNING SMELL IN THE AFT GALLEY AND LAVATORY AREA. REPLACED BALLAST A ND BURNED WIRE. FUNCTIONALLY CHECKED GOOD IAW B737-33-26-21. FLEET CAMPAIGN ACCOMPLISHED ON ALL THE AIRCRAFT OPERATED AND MAINTAINED BY AIR TRAN. NO FURTHER POSSIBLE PROBLEMS FOUND. 2 L 7 2 4F A16WE 1996052300103 19960523 00103 NM 1996 5 23 96ZZZX2544 1 19960328 A 2520 INSULATION BOEING 737 7372P6 NM CABIN OUT OF POSITION A ZZDA A G UNSCHED LANDING O2 MASK DEPLOYED J WARNING INDICATION CL CLIMB 1 SO 15 EICJW 21355 MCO - FLT 560 - DURING CLIMB-OUT THROUGH 13,000 FEET, PRESSURIZATION CONTROL BECAME ERRATIC. THE FLIGHT CREW RETURNED T HE AIRCRAFT TO MCO. AFTER INSPECTION, A PIECE OF INSULATION WAS FOUND STUCK IN THE OUTFLOW VALVE. INSULATION WAS REMOV ED AND ALL RELATED SYSTEMS OPERATIONALLY CHECKED OK. OXYGEN MASKS WERE DEPLOYED AND WERE REPLACED, OXYGEN BOTTLES WERE SERVICED. AIRCRAFT WAS RETURNED TO SERVICE. FLEET CAMPAIGN ACCOMPLISHED ON ALL THE AIRCRAFT OPERATED AND MAINTAINED BY AIR TRAN. POSSIBLE PROBLEM AREAS WILL BE INSPECTED ON A RECURRENT BASIS. 2 L 7 2 4F RT A16WE 1996052300104 19960523 00104 WP 1996 5 23 96ZZZX2545 1 19960409 A 3241 TRANSDUCER PINS DOUG DC9 DC983 3022083 WP BRAKE SYSTEM LOOSE A TWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 05 9403W 53139 SEA - FLT 350 - DURING THE TAKEOFF ROLL AT APPROXIMATELY 40 KNOTS, THE 'WHEEL NOT TURNING' LIGHT ILLUMINATED. THE TAKEO FF WAS ABORTED. REINSTALLED TRANSDUCER PINS. OPERATIONAL CHECK AND BITE CHECK NORMAL. CHECK C-1D - 11/3/95 - JFK. 2 L 7 2 4F RT A6WE 1996052300105 19960523 00105 CE 1996 5 23 96ZZZX2546 1 19960326 A 6120 BETA CABLE BEECH 1900 1900C 1154161 CE RT ENGINE OUT OF ADJUST A GUUA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 187GA UC31 EYW/TPA - FLT 435A - PILOT REPORT: AFTER TAKEOFF (APPROXIMATELY 200 FEET), RIGHT PROPELLER RPM BEGAN DECREASING, RIGHT TORQUE INCREASED, RIGHT ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNED TO EYW AND LANDED WITHOUT INCIDENT. MAINTENANCE: TR OUBLESHOT SYSTEM, RIGGED RIGHT ENGINE BETA CABLE. 2 L 7 2 4T RT A24CE 1996052300106 19960523 00106 NM 1996 5 23 96ZZZX2547 1 19960320 A 2720 591005017 PWR CONTROL UNIT BOEING 727 727222 1384073 NM RUDDER LEAKING A RYNA O OTHER K FLUID LOSS DE DESCENT 1 CE 07 7642U 19915 THE A-SYSTEM HYDRAULICS FAILED ON DESCENT INTO DAYTON. USED ALTERNATE LANDING GEAR AND FLAP EXTENSION PROCEDURES. AIRC RAFT LANDED WITHOUT INCIDENT. FOUND LOWER RUDDER POWER CONTROL UNIT LEAKING. REPLACED LOWER RUDDER POWER CONTROL UNIT PER MM 27-20-00. LEAK CHECK GOOD. RESET MANUAL GEAR EXTENSION SYSTEM PER MM 32-30-00. (X) 2 L 7 3 4F A3WE 1996052300107 19960523 00107 NM 1996 5 23 96ZZZX2548 1 19960303 A 3150 106180387 LIGHT ASSY BOEING 727 727225 1384077 NM F/O PANEL SHORTED A MYWA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 19 886MA 21855 MIA - REETURN FROM FLIGHT. PASSING THROUGH 17,000 FEET, THE FOLLOWING MASTER CAUTION WARNING LIGHTS AND AURAL WARNING C AME ON. ALSO, ENGINE FILTER BYPASS LIGHTS, AUTOPILOT DISENGAGED LIGHTS, BOTH COMPASS LIGHTS, STAB OUT-OF-TRIM LIGHT, EL EVATOR LOW PRESSURE AND FLIGHT CONTROL (A AND B) LOW PRESSURE LIGHTS. 2 L 7 3 4F A3WE 1996052300108 19960523 00108 EU 1996 5 23 ASOA96010 1 19960326 A 5330 HC537L0160008 SKIN BAG BAE146 BAE146200A 1500266 EU FUSELAGE DENTED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 815AS E2084 DURING INSPECTION, FOUND THE AERODYNAMIC PUTTY IN A DENT ON THE RIGHT FORWARD SIDE OF THE FUSELAGE LOCATED BETWEEN FRAME S 14 AND 15 IS CRACKING OUT. REPAIRED BY INSTALLING 'METAL TO METAL' TO THE DENT PER EO 146-53-0003 AND 8110 OF DER REP ORT 95-109, DATED SEPTEMBER 6, 1995. 2 H 7 4 4F RT A49EU 1996052300109 19960523 00109 CE 1996 5 23 C2XA96IA073 1 19960320 A 3233 11438004111 ACTUATOR BEECH 1900 1900D 1154162 CE LT MLG FAILED A C2XA O OTHER J WARNING INDICATION AP APPROACH 1 SW 09 81546 416 0398A UE187 TLH - FLT 2801 - DURING APPROACH TO TLH, LT MLG DOWNLOCK LIGHT DID NOT ILLUMINATE UNTIL APPROXIMATELY 1 MINUTE AFTER NOS E AND RT MLG LIGHTS ILLUMINATED. AIRCRAFT LANDED AT TLH WITHOUT INCIDENT. INSPECTED AND APPROVED FOR FERRY FLIGHT FROM TLH TO IAH IN A GEAR DOWN CONDITION. IAH MAINTENANCE REMOVED AND REPLACED LT MLG ACTUATOR. PERFORMED OPERATION CHECK OF LANDING GEAR SYSTEM, NO DEFECTS NOTED, AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1996052300110 19960523 00110 NM 1996 5 23 CKSA96021 1 19960305 A 3260 BACC45FT18A31P6 CONNECTOR BOEING 727 727223 1384074 NM NLG DIRTY A CKSA K NONE N FALSE WARNING AP APPROACH 1 GL 23 729CK 73509 19482 HUF/IAH - FLT 72669 - ON EXTENSION, NOSE GEAR DID NOT GO GREEN UNTIL THIRD ATTEMPT. INSPECTED NOSE GEAR, FOUND NO DEFEC TS. LUBED ALL GREASE FITTINGS IN NOSE. CLEANED AND RE-SECURED CANNON PLUGS ON BOTH SWITCHES. JACKED NOSE GEAR IAW 727 MM 7-11-0. PERFORMED NOSE GEAR RETRACTION TEST IAW 32-33-0. CYCLED 15 TIMES. POSITON AND WARNING SYSTEMS. OPS CHECK GOOD IAW 32-61-0. (X) 2 L 7 3 4F A3WE 1996052300111 19960523 00111 NE 1996 5 23 DJSA2396001 2 19960326 A 8530 84088 CYLINDER DOUG DC3 DC3C 3021457 WP PWA R1830 R183094 52020 NE NR 1 ENGINE CRACKED A DJSA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 GL 23 9382 74513 12331 P139763 NR 3 CYLINDER CRACKED ON NR 1 ENGINE, CAUSE UNKNOWN, CHANGED CYLINDER. (X) 2 L 7 2 4R 4 R A669 5E4 1996052300112 19960523 00112 CE 1996 5 23 GLBA96049 1 19960309 A 7714 TACHOMETER BEECH 1900 1900C 1154161 CE RT ENGINE MALFUNCTIONED A GLBA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 01 170GL UE170 HHH - CREW ABORTED TAKEOFF BECAUSE RIGHT RPM INDICATOR DROPPED TO ZERO. MAINTENANCE COULD NOT DUPLICATE. OPS CHECK WAS GOOD. (X) 2 L 7 2 4T RT A24CE 1996052300113 19960523 00113 NM 1996 5 23 SABA960004 1 19960218 A 3150 WARNING SWITCH DHAV DHC8 DHC8102 2809003 NM RT COND LEVER OUT OF ADJUST A SABA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 33 882CC 168 CVB/CLT - FLT 5157 - FLIGHT HAD STARTED TAKEOFF ROLL. WHEN POWER LEVERS WERE ADVANCED PAST 62 PERCENT TORQUE, THE WARNI NG HORN SOUNDED. TAKEOFF ABORTED AND AIRCRAFT RETURNED TO GATE. PASSENGERS WERE DEPLANED AND CAPTAIN WENT TO CONTACT M AINTENANCE. AFTER MAINTENANCE WAS BRIEFED BY THE CAPTAIN ON THE PROBLEM, A DECISION WAS MADE TO FERRY ACFT BACK TO CLT SO REPAIRS COULD BE MADE. ACFT FERRIED BACK TO CLT UNDER FERRY PERMIT NR 021896-02. UPON N882CC'S ARRIVAL IN CLT, AVIO NICS PERSONNEL DISPATCHED TO TROUBLESHOOT PROBLEM. PROBLEM FOUND TO BE THE MICROSWITCH FOR RT CONDITION LEVER. MICROSW ITCH ADJUSTED IAW DHC-8 MM ATA 3151 AND SYSTEM FUNCTION TESTED GOOD. DISCREPANCY WAS THEN 'SIGNED-OFF".(X) 2 H 7 2 4T RT A13NM 1996052300114 19960523 00114 EU 1996 5 23 SIMA961001 1 19960409 A 3350 330151 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 371AE 1080 340B371 DFW - FLT 3811 - INTERIOR EMERGENCY LIGHTS INOPERATIVE. ITEM WAS DEFERRED UNTIL 4-12-96. REPLACED THE EMERGENCY EXIT P OWER SUPPLY AT SEAT ROW 8. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1996052300115 19960523 00115 EU 1996 5 23 SIMA961011 1 19960410 A 2750 RETRACT MECH AEROSP ATR72 ATR72212 EU TE FLAPS MALFUNCTIONED A SIMA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 260AE 263 SBN - FLT 4127 - FLAP EXTENSION FLAG STUCK WHEN FLAPS WERE SELECTED TO 30 DEGREES WITH A FLAP UNSTUCK WARNING. FLAPS WO RKED OK AT 15 DEGREE SETTING. RESET NR 1 AND NR 2 MFC'S AND PERFORMED OPERATIONAL CHECK OF THE FLAP SYSTEM. UNABLE TO DUPLICATE DISCREPANCY. AIRCRAFT COMPLETED SATISFACTORY TEST FLIGHT. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1996052300116 19960523 00116 EU 1996 5 23 SIMA961021 1 19960411 A 3350 330150 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 376AE 755 340B376 DFW - SEVERAL EMERGENCY LIGHTS FOUND INOPERATIVE DURING ROUTINE MAINTENANCE. REPLACED EMERGENCY POWER SUPPLY AT 23LN LO CATION IAW SAAB MM 33-50-10 WITH OPERATIONAL CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. PART TOTAL CYCLES, 793. (X ) 2 L 7 2 4T RT A52EU 1996052300117 19960523 00117 EU 1996 5 23 SIMA961051 1 19960414 A 3350 330150 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 374AE 1086 340B374 DFW - FLT 3906 - EMERGENCY FLOOR LIGHTING SYSTEM WILL NOT OPERATE. REPLACED POWER SUPPLY. AIRCRAFT RETURNED TO SERVICE . (X) 2 L 7 2 4T RT A52EU 1996052300118 19960523 00118 WP 1996 5 23 SRAA49603 1 19960422 A 3260 SWITCH WIRE DOUG DC8 DC871F 302199D WP LT MLG DOOR DEFECTIVE A SRAA J A DUMP FUEL UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 872SJ 46040 DOV - FLT AD01 - ON TAKEOFF AFTER GEAR RETRACTED, GEAR DOORS AND GEAR UNSAFE WARNING LIGHTS REMAINED ON, CYCLED GEAR THR EE TIMES, PROBLEM REMAINS. DUMPED FUEL AND DIVERTED TO JFK. AIRCRAFT LANDED SAFELY. AIRCRAFT IS CURRENTLY ON JACKS, F OUND WIRING TO LT MAIN GEAR DOOR SWITCH DEFECTIVE. REPAIRED WIRING PER WDM 32-1-0, GEAR SWING PERFORMED PER CHAPTER 32- 60-00. OPS CHECKED GOOD. (X) 2 L 7 4 4F RT 4A25 1996052300119 19960523 00119 SO 1996 5 23 SRAA49604 1 19960419 A 6120 582855 VALVE HOUSING HAMSTD 54H60117 LKHEED 382 382G 526414U SO NR 4 ENGINE DEFECTIVE A SRAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 23 905SJ 235797 4472 FLT 1201 - DURING CRUISE, NR 4 PROPELLER RPM DECREASING BELOW 98 PERCENT, PRECAUTIONARY SHUT DOWN NR 4 ENGINE AND ACCOMP LISHED AIR TURN-BACK TO LIM. LANDED SAFELY. FOUND NR 4 PROPELLER VALVE HOUSING DEFECTIVE. REPLACED VALVE HOUSING PER MM, CHAPTER 61. OPS CHECKED GOOD MER MM, CHAPTER 71. (X) 2 H 7 4 4T A1SO 1996052300120 19960523 00120 NM 1996 5 23 TSAA9653012 1 19960401 A 5320 TRANSVERSE BEAM BOEING 737 73725A 1384481 NM BS 677 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 819AL 23791 DURING HEAVY MAINTENANCE VISIT, BS 677 TRANSVERSE BEAM CRACKED, 2ND SEAT TRACK FROM LEFT. REPAIRED PER ECO 1933R3. AIR CRAFT RETURNED TO SERVICE. NRTC: 11,579. (X) 2 L 7 2 4F RT A16WE 1996052300121 19960523 00121 NM 1996 5 23 TSAA9653013 1 19960401 A 5320 TRANSVERSE BEAM BOEING 737 73725A 1384481 NM BS 674 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 819AL 23791 DURING HEAVY MAINTENANCE VISIT, BS 674 TRANSVERSE BEAM CRACKED, THIRD SEAT TRACK FROM LEFT. REPAIRED PER ECO 1933R3. A IRCRAFT RETURNED TO SERVICE. NRTC: 11,582. (X) 2 L 7 2 4F RT A16WE 1996052300122 19960523 00122 NM 1996 5 23 TSAA9653014 1 19960401 A 5320 DOORWAY FRAME BOEING 737 73725A 1384481 NM BS 787 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 819AL 23791 DURING HEAVY MAINTENANCE VISIT, FUSELAGE AFT LOWER CARGO DOORWAY FRAME CRACKED AT BS 787 PLUS 6 INCHES BETWEEN S24R - S2 6R. REPAIRED PER ECO 2679. AIRCRAFT RETURNED TO SERVICE. NRTC: 11,369. (X) 2 L 7 2 4F RT A16WE 1996052300123 19960523 00123 NM 1996 5 23 TSAA9653015 1 19960401 A 5330 SKIN BOEING 737 73725A 1384481 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 819AL 23791 DURING HEAVY MAINTENANCE VISIT, SEVERAL CRACKS NOTED AT FORWARD AND AFT SIDES OF THE LT WING ILLUMINATION LIGHT ASSY. R EPAIRED PER ECO 2429. AIRCRAFT RETURNED TO SERVICE. NRTC: 11,646. (X) 2 L 7 2 4F RT A16WE 1996052300124 19960523 00124 NM 1996 5 23 TSAA9653018 1 19960401 A 5315 FLOOR BEAM BOEING 737 73725A 1384481 NM BS 312 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 819AL 23791 DURING HEAVY MAINTENANCE VISIT, FLOOR BEAM AT BS 312, FILIFORM CORROSION NOTED AROUND SEVERAL NUTPLATE HOLES. REPLACED FLOOR BEAM FROM LBL 62 TO RBL 20 PER SRM 53-10-9. AIRCRAFT RETURNED TO SERVICE. NRTC: 11,911. (X) 2 L 7 2 4F RT A16WE 1996052300125 19960523 00125 NM 1996 5 23 TSAA9655009 1 19960401 A 5510 ATTACH LUGS BOEING 737 73725A 1384481 NM HORIZ STABILIZER CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 819AL 23791 DURING HEAVY MAINTENANCE VISIT, FOUND CORROSION ON LEFT AND RIGHT HORIZONTAL STABILIZER ATTACH LUGS, FACE AND BORES. RE PAIRED PER ECO 2689, PARTS I AND II. AIRCRAFT RETURNED TO SERVICE. TAT: 24,124.20 HOURS. TAC: 14,610. 2 L 7 2 4F RT A16WE 1996052300126 19960523 00126 NM 1996 5 23 USAASB96071 1 19960422 A 3350 110049 BATTERY CHARGER BOEING 737 7373B7 1384580 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 387US 22959 MCO - FLT 2208 - AISLE EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE FOUND FUSE BLOWN IN POWER SUPPLY. REPLACED FUSE, LIGH T OPS CHECK SATISFACTORY. (X) 2 L 7 2 4F RT A16WE 1996052300127 19960523 00127 WP 1996 5 23 WRLA96015 1 19960328 A 2781 806125 PROX ELECT UNIT DOUG DC10 DC1030 3023501 WP LE FLAPS FAILED A WRLA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 9MMAZ 46933 DURING TAXI, FLIGHT CREW NOTED 'SLAT DISAGREE' LIGHT ILLUMINATED WITH FLAPS EXTENDED. FLIGHT CREW ELECTED TO RETURN TO GATE FOR MAINTENANCE. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL TROUBLESHOT SYSTEM AND IDENTIFIED 'PROXIMITY ELECTRONIC UNIT' FAULTY. UNIT WAS REPLACED. GROUND CHECKS WERE PERFORMED WITH NO FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 3 4F A22WE 1996052300128 19960523 00128 WP 1996 5 23 WRLA96016 1 19960401 A 7714 9053M20P02 N1 SPEED SENSOR DOUG DC10 DC1030 3023501 WP NR 3 ENGINE INTERMITTENT A WRLA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 9MMAS 46955 DURING INITIAL TAKEOFF ROLL, FLIGHT CREW NOTED NR 3 ENGINE WOULD NOT ACCELERATE TO 100 PERCENT N1 SPEED. FLIGHT CREW EL ECTED TO DISCONTINUE TAKEOFF ROLL, AND RETURN TO GATE FOR MAINTENANCE. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDE NT. MAINTENANCE PERSONNEL INSPECTED ENGINE, AND FOUND NO APPARENT REASON FOR MALFUNCTION. SWAPPED N1 SENSOR FROM NR 1 TO NR 3 ENGINES. CLEANED CANNON PLUG TO NR 3 N1 SENSOR. GROUND RUN OF BOTH NRS 1 AND 3 ENGINES PERFORMED PER MM 71-00- 00, NO MALFUNCTIONS NOTED. AS A PRECAUTION, REPLACED NR 1 N1 SENSOR (ORIGINALLY INSTALLED IN NR 3 ENGINE). OPS CHECK NR 1 ENGINE. NO FAULT FOUND. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 3 4F A22WE 1996052300129 19960523 00129 NE 1996 5 23 9610379974 2 19960506 A 7532 PRBC DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7B 52053 NE NR 1 ENGINE FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 9338 47347 657371 NR 1 ENGINE EPR INDICATION FLUCTUATED ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. M AINTENANCE REPLACED THE PRBC WITH A SERVICEABLE UNIT. 2 L 7 2 4F 4 F A6WE E2EA 1996052300130 19960523 00130 NM 1996 5 23 9610702291 1 19960511 A 3350 CONTROL SWITCH BOEING 727 727251 138408H NM CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 291US 21379 DURING PREFLIGHT, FOUND ALL EMERGENCY LIGHTS ON RIGHT SIDE OF AIRCRAFT INOPERATIVE. REPLACED MAIN EMERGENCY LIGHT CONTR OL SWITCH S-264 IN COCKPIT, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996052300131 19960523 00131 NM 1996 5 23 9610712768 1 19960511 A 3350 BATTERIES BOEING 727 7272M7 138407S NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 728RW 21741 DURING PREFLIGHT, FOUND EMERGENCY EXIT LIGHT ABOVE BOTTOM OF AFT AIRSTAIR STEP INOPERATIVE. REPLACED BATTERIES, CHECKED OK. 2 L 7 3 4F A3WE 1996052300132 19960523 00132 NM 1996 5 23 9610722704 1 19960511 A 3350 BATTERY BOEING 727 727225 1384077 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 801EA 22432 DURING PREFLIGHT, FOUND ONE SECTION OF FLOOR PROXIMITY LIGHTS INOPERATIVE. REPLACED BATTERY, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996052300133 19960523 00133 NM 1996 5 23 9610732291 1 19960513 A 3350 BATTERY PACK BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 291US 21379 DURING PREFLIGHT, FOUND EMERGENCY EXIT SIGNS ON RIGHT SIDE OF AIRCRAFT INOPERATIVE. REPLACED SHORTED BATTERY PACK, LIGH TS CHECKED OK. 2 L 7 3 4F A3WE 1996052300134 19960523 00134 NM 1996 5 23 9610742704 1 19960515 A 3350 POWER SUPPLY BOEING 727 727225 1384077 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 801EA 22432 DURING PREFLIGHT, FOUND LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996052300135 19960523 00135 NM 1996 5 23 9610752276 1 19960514 A 2782 1U109592 ACTUATOR BOEING 727 727251 138408H NM NR 2 LE FLAP FAILED A NWAA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 GL 01 276US 21155 DURING CLIMB, NR 2 SLAT FAILED TO RETRACT. AIRCRAFT RETURNED TO ABQ AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NR 2 SLAT ACTUATOR, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996052300136 19960523 00136 1996 5 23 9610762286 4 19960511 A 3442 20704100101 RADAR T/R UNIT BOEING 727 727251 138408H NM E/E COMPARTMENT MALFUNCTIONED A NWAA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 01 286US 21325 DURING CRUISE, FLIGHT WEATHER RADAR BECAME UNRELIABLE. AIRCRAFT RETURNED TO DCA AND LANDED WITHOUT INCIDENT. REPLACED RADAR TRANSCEIVER, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996052300137 19960523 00137 NE 1996 5 23 9610776302 2 19960516 A 7261 OIL LINE BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE NR 2 ENGINE FAILED A NWAA E ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 GL 01 662US 23720 717661 DURING CRUISE, THE NR 2 ENGINE WAS SHUT DOWN DUE TO LOW OIL QUANTITY. ENGINE WAS RESTARTED DURING APPROACH AND THE AIRC RAFT LANDED WITHOUT INCIDENT. REPLACED THE ANGLE GEARBOX PRESSURE LINE. 2 L 7 4 4F 4 F RT A20WE E24NE 1996052300138 19960523 00138 NM 1996 5 23 9610782713 1 19960517 A 3350 BATTERIES BOEING 727 7272S7 138407Z NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 716RC 22021 DURING PREFLIGHT, FOUND EMERGENCY LIGHTS AT BOTTOM OF AIRSTAIRS INOPERATIVE. REPLACED BATTERIES, CHECKED OK. 2 L 7 3 4F A3WE 1996052300139 19960523 00139 WP 1996 5 23 96FDEA00981 1 19960516 A 5311 BELLFRAME DOUG DC10 DC1010CF 3023502 WP BS 1942 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 049FE 46992 SNRM 1144, SURFACE CORROSION ON BELLFRAME AT STA 1942 STR 51L AND 51 R. BURNISHED SURFACE CORROSION AND REMOVED DAMAGED AREA PER SRM 51-21-01, FABRICATED NEW SPLICES AND SECTION OF FRAME PER SRM 53-30-00, INSTALLED REPAIR SRM 53-30-00 FIG 5. 2 L 7 3 4F RT A22WE 1996052300140 19960523 00140 WP 1996 5 23 96FDEA00982 1 19960520 A 5311 ASA37897 BELL FRAME DOUG DC10 DC1010CF 3023502 WP BS 1841 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68049 47803 SNRM 1137, SURFACE CORROSION ON BELL FRAME AT STA 1841 STR 49L AND 49R. REMOVED CORROSION BEYOND SRM 51-21-01 REMOVED F ASTENERS, FACTORY SPLICE AND TWO VERTICAL STIFFENERS, FABRICATED NEW SPLICES AND NEW SECTION OF BELL FRAME PER SRM 51-30 -00 VOL 1 FIG 5 AND SRM 53-30-00. 2 L 7 3 4F RT A22WE 1996052300141 19960523 00141 NM 1996 5 23 96FDEA00983 1 19960515 A 5347 SEAT TRACK BOEING 727 72725 1384006 NM BS 950 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 505FE 18276 SEAT TRACK RBL 45 CORROSION ON SPLICE AT BS 950 PLUS 10 WL 208. REMOVED CORRODED SEAT TRACK AND REPLACED WITH NEW SEAT TRACK BS 950 PLUS 10 TO 870 RBL 45 PER FEDEX SRM 53-10-5. 2 L 7 3 4F A3WE 1996052300142 19960523 00142 NM 1996 5 23 96FDEA00984 1 19960516 A 5315 BAC1505100246 FLOOR BEAM BOEING 727 72725 1384006 NM BS 312 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 505FE 18276 CORROSION BS 312 FLOOR BEAM WL 208 LBL 4 TO 19 AND 30. CORROSION ON FLOOR BEAM FOUND TO BE OUT OF LIMITS. REMOVED DAMA GED AREA, FABRICATED NEW BEAM AND REPAIR PARTS AND INSTALLED BS 312 LBL 65 TO RBL 8 WL 208 IAW FEDEX SRM 53-10-8. 2 L 7 3 4F A3WE 1996052300143 19960523 00143 NM 1996 5 23 96FDEA00985 1 19960516 A 5313 STRINGER BOEING 727 72725 1384006 NM BS 950-985 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 505FE 18276 CORROSION (C53-224-04) ON STR 3L AT BS 950 TO 985. REMOVED CORRODED SECTION OF STR, FABRICATED AND INSTALLED REPAIR AT BS 950 TO 985 STR 3L IAW SRM 53-10-3. 2 L 7 3 4F A3WE 1996052300144 19960523 00144 NM 1996 5 23 96UAL900350 1 19960516 A 3350 LIGHT STRIP BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 933UA 26659 FORWARD GALLEY EMERGENCY ESCAPE LIGHT STRIP INOP. REPLACED FORWARD GALLEY EMERGENCY ESCAPE LIGHT STRIP, OP CHECKS NORMA L. 2 L 7 2 4F 4 F RT A16WE E21EU 1996052300145 19960523 00145 WP 1996 5 23 ABXA9600495 1 19960514 A 5610 4616968 SLIDE WINDOW DOUG DC8 DC861 3021952 WP LT COCKPIT OUT OF ADJUST A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 842AX 46015 DURING SERVICE CHECK, FOUND THE CAPTAIN'S SLIDING WINDOW WOULD NOT OPEN. FOUND UPPER LINKAGE ROD END LOOSE AND OUT OF A DJUSTMENT. ADJUSTED CLEARVIEW WINDOW PER DC-8 MM 56-10-3. CLEANED AND LUBRICATED MECHANISM, WINDOW OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1996052300146 19960523 00146 SW 1996 5 23 QXEA9600171 1 19960516 A 2120 AIR DIST SWRNGN SA227 SA227AC 8780603 SW CABIN ODOR A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 09 2727B AC730 COCKPIT AND CABIN HAVE STRONG ODOR OF ENGING OIL. NUMBER TWO BLEED AIR PLACED ON MEL 21-4. 2 L 7 2 4T RT A8SW 1996052300147 19960523 00147 NM 1996 5 23 QXEA9600172 1 19960516 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT MALFUNCTIONED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 814PH 43 COCKPIT EMERGENCY LIGHT REMAINS ON WITH EMERGENCY LIGHTS ARMED. OVERHEAD EMERGENCY LIGHT REPLACED AND LIGHT OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 1996052300148 19960523 00148 NM 1996 5 23 QXEA9600173 1 19960516 A 3350 MS25237327 BULB GRIMES 10005511 DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 817PH 60152 56 EMERGENCY LIGHT IN COCKPIT IS INOP. LAMP WAS REPLACED AND BROKEN WIRE TO TEST SWITCH ON LANTERN REPAIRED, LIGHT OPS CHE CKED GOOD. 2 H 7 2 4T RT A13NM 1996052300149 19960523 00149 NM 1996 5 23 QXEA9600174 1 19960516 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT INOPERATIVE A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 829PH 304 COCKPIT EMERGENCY LIGHT IS INOP. COCKPIT EMERGENCY LIGHT REPLACED AND LIGHT OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 1996052300150 19960523 00150 EU 1996 5 23 QXEA9600175 1 19960516 A 3350 362624 STRIP LIGHT FOKKER F28 F28MK1000 4990808 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 802PH 11017 FLOOR PROXIMITY LIGHTS FROM SEATS 3 TO 6 ARE INOP. SHORTED SECTION OF STRIP LIGHTING WAS REPLACED AND STRIP LIGHT OPS C HECKED GOOD. 2 L 7 2 4F RT A20EU 1996052300151 19960523 00151 NM 1996 5 23 SCNA96123 1 19960427 A 5347 BAC1520792 SEAT TRACK BOEING 727 727225 1384077 NM BS 1110-1130 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON A SEAT TRACK AT BS 1110 TO 1130, RBL 45. REMOVED SEAT TRACK SECT ION, FABRICATED AND INSTALLED A NEW SECTION IN ACCORDANCE WITH B727 SRM 53-10-5. 2 L 7 3 4F A3WE 1996052300152 19960523 00152 NM 1996 5 23 SCNA96131 1 19960514 A 3350 S106 BATTERY BOEING 727 7272A1 138407F NM AFT AIRSTAIR DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 287SC 21345 THE AFT AIRSTAIRS OVERHEAD EMERGENCY LIGHT WAS FOUND INOP. REPLACED BATTERIES, OPS CHECKED OK. 2 L 7 3 4F A3WE 1996052300153 19960523 00153 NM 1996 5 23 SCNA96132 1 19960428 A 5320 WEB BOEING 727 727225 1384077 NM BS 420-428 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON A CABIN WEB LOCATED AT BS 420 TO 428, RBL 65 WL 208. REMOVED COR RODED SECTION OF WEB, FABRICATED AND INSTALLED A NEW WEB IN ACCORDANCE WITH B727 SRM 51-20-2. 2 L 7 3 4F A3WE 1996052300154 19960523 00154 NM 1996 5 23 SCNA96133 1 19960424 A 5311 FRAME BOEING 727 727225 1384077 NM BS 1166 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON A FRAME IN THE AFT PIT AT BS 1166, BL 0, WL 200. FABRICATED AND INSTALLED A NEW FRAME IN ACCORDANCE WITH B727 SRM 51-30-2 AND 51-40-4 FIGURE 1. 2 L 7 3 4F A3WE 1996052300155 19960523 00155 NM 1996 5 23 SCNA96134 1 19960510 A 5347 BAC1520792 SEAT TRACK BOEING 727 727225 1384077 NM BS 344 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON A SEAT TRACK AT BS 344, LBL 24. REMOVED CORRODED SECTION, FABRIC ATED AND INSTALLED A NEW SECTION IN ACCORDANCE WITH B727 SRM 53-10-5. 2 L 7 3 4F A3WE 1996052300156 19960523 00156 NM 1996 5 23 SCNA96135 1 19960427 A 5347 BAC1520792 SEAT TRACK BOEING 727 727225 1384077 NM BS 1050-1183 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON A LT SEAT TRACK AT BS 1050 TO 1183. REMOVED CORRODED SECTION OF SEAT TRACK, FABRICATED AND INSTALLED A NEW SECTION IN ACCORDANCE WITH B727 SRM 53-10-5 FIGURE 7 AND 51-30-2. 2 L 7 3 4F A3WE 1996052300157 19960523 00157 NM 1996 5 23 SCNA96136 1 19960428 A 5347 BAC152029222 SEAT TRACK BOEING 727 727225 1384077 NM BS 400 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON A SEAT TRACK AT BS 400, RBL 24.5. REMOVED SEAT TRACK, FABRICATED AND INSTALLED A NEW SEAT TRACK IN ACCORDANCE WITH B727 SRM 53-10-2, 51-30-2 AND MM 51-20-11. 2 L 7 3 4F A3WE 1996052300158 19960523 00158 NM 1996 5 23 SCNA96137 1 19960428 A 5347 BAC1520792 SEAT TRACK BOEING 727 727225 1384077 NM BS 480 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON A SEAT TRACK IN THE GALLEY AREA AT BS 480 RBL 45 WL 208. REMOVED SEAT TRACK, FABRICATED AND INSTALLED A NEW SECTION OF SEAT TRACK IN ACCORDANCE WITH B727 SRM 53-10-5. 2 L 7 3 4F A3WE 1996052300159 19960523 00159 NM 1996 5 23 SCNA96138 1 19960428 A 5320 FORMED SECTION BOEING 727 727225 1384077 NM BS 360-380 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON FORMED SECTIONS IN THE GALLEY AREA AT BS 360 TO 380 RBL 65, WL 20 8. REMOVED FORMED SECTIONS, FABRICATED AND INSTALLED NEW FORMED SECTIONS IN ACCORDANCE WITH B727 SRM 51-30-2 AND 51-20- 2. 2 L 7 3 4F A3WE 1996052300160 19960523 00160 NM 1996 5 23 SCNA96139 1 19960424 A 5320 FITTING BOEING 727 727225 1384077 NM BS 870 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING HEAVY MAINTENANCE VISIT, A CRACK WAS FOUND EXTENDING FROM A FLANGE RADIUS AT THE BOTTOM OUTBD CORNER OF THE REAR SPAR WING TO BODY FITTING. FABRICATED AND INSTALLED REPAIRS IN ACCORDANCE WITH B727 SRM 51-20-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996052300161 19960523 00161 NM 1996 5 23 SCNA96140 1 19960425 A 5320 ANGLE BOEING 727 727225 1384077 NM BS 312-344 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON MAIN CABIN FLOOR STRUCTURE AT BS 312 AND BS 344 LBL 30. REMOVED CORRODED FLOOR ANGLES, FABRICATED AND INSTALLED NEW ANGLES IN ACCORDANCE WITH B727 SRM 51-40-4. 2 L 7 3 4F A3WE 1996052300162 19960523 00162 WP 1996 5 23 96ZZZX2549 1 19960428 A 2150 39613011 CONTROL VALVE DOUG DC9 DC983 3022083 WP NR 2 PACK FAILED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9409F 53121 STL - FLT 463 - DURING CRUISE, AIRCRAFT CABIN PRESSURIZATION BLED OFF. REMOVED AND REPLACED NR 2 PACK FLOW CONTROL VALV E, MFG PN 396130-1-1. OPERATIONAL CHECK AND LEAK CHECK NORMAL. CHECK C-1D - 5-18-95 - MCI. 2 L 7 2 4F RT A6WE 1996052300163 19960523 00163 WP 1996 5 23 96ZZZX2550 1 19960425 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 639 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 990Z 47136 DURING SPECIAL CHECK, FOUND A 1.50 INCH CRACK IN LONGERON 6L, STA 639. REPAIRED PER SRM 53-02, PAGE 2A, FIGURE 2. AIRC RAFT TOTAL TIME: 68,821 HOURS. CYCLES, 8,390. 2 L 7 2 4F A6WE 1996052300164 19960523 00164 EU 1996 5 23 C2XA96BT002 1 19960428 A 7931 S7931000600000 OIL PRESS LINE AEROSP ATR42 ATR42320 8680930 EU RT ENGINE CRACKED A C2XA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 09 14825 170 BTV - FLT 3682 - ON APPROACH INTO BTV, RIGHT LOW OIL PRESSURE LIGHT ILLUMINATED. CAPTAIN PERFORMED PRECAUTIONARY ENGINE SHUT DOWN. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND RIGHT OIL PRESSURE TRANSDUCER LINE HAD A CRACKED FLARE CAUSING OIL LEAK AND PRESSURE LOSS. REMOVED AND REPLACED LINE WITH SERVICEABLE UNIT, RESERVICED OIL, AND OPERATIONALLY CHECKED AND LEAK CHECKED GOOD. ACFT TT, 13,233.8 HRS. CYCLES, 16,277. (X) 2 H 7 2 4T RT A53EU 1996052300165 19960523 00165 SO 1996 5 23 C2XA96IA104 1 19960430 A 5400 12030995001 ANGLE EMB 120 EMB120RT SO RT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 27716 120128 IAH - DURING C-CHECK INSPECTION, THE RIGHT NACELLE FRAME 2 ANGLE WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED TH E ANGLE AND THE AIRCRAFT WAS RETURNED TO SERVICE. AIRCRAFT TT: 14,059.3 HRS. CYCLES, 18,999. (X) 2 L 7 2 4T RT A31SO 1996052300166 19960523 00166 EU 1996 5 23 C2XA96IA105 1 19960430 A 2730 S5517310920400 BUSHING AEROSP ATR42 ATR42320 8680930 EU RT ELEV HINGE WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 47801 60 IAH - DURING C-CHECK INSPECTION, THE RIGHT ELEVATOR INBOARD ATTACH POINT WAS FOUND TO HAVE PLAY. MAINTENANCE REMOVED AN D REPLACED THE FORWARD BUSHINGS ON THE INBOARD AND OUTBOARD HINGES FOR THE RIGHT ELEVATOR AND THE AIRCRAFT WAS RETURNED TO SERVICE. ACFT TT: 18,278.2 HRS. CYCLES, 21,241. (X) 2 H 7 2 4T RT A53EU 1996052300167 19960523 00167 SO 1996 5 23 C2XA96IA106 1 19960430 A 5730 12033270001 SKIN EMB 120 EMB120RT SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 27716 120128 IAH - DURING C-CHECK INSPECTION, THE WING SKIN ADJACENT TO ACCESS PANEL 522EB WAS FOUND CRACKED. MAINTENANCE FABRICATED AND INSTALLED A DOUBLER PER EMB-120, SRM 5720-01 AND SRM 51-40-02, AND THE AIRCRAFT WAS RETURNED TO SERVICE. ACFT TT: 14,059.3 HRS. CYCLES, 18,999. (X) 2 L 7 2 4T RT A31SO 1996052300168 19960523 00168 SO 1996 5 23 C2XA96IA107 1 19960430 A 5530 12015374002 ANGLE EMB 120 EMB120RT SO RT VERT STAB CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 27716 120128 IAH - DURING C-CHECK INSPECTION, THE VERTICAL STABILIZER RIGHT DRAG ANGLE WAS FOUND CRACKED. MAINTENANCE REMOVED AND RE PLACED THE DRAG ANGLE AND THE AIRCRAFT WAS RETURNED TO SERVICE. ACFT TT: 14,059.3 HRS. CYCLES, 18,999. (X) 2 L 7 2 4T RT A31SO 1996052300169 19960523 00169 EU 1996 5 23 C2XA96IA108 1 19960430 A 2721 NTA14452S06A019 BUSHING AEROSP ATR42 ATR42320 8680930 EU RUDDER TAB WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 47801 60 IAH - DURING C-CHECK INSPECTION, THE RUDDER TAB UPPER BEARING WAS FOUND TO HAVE PLAY. MAINTENANCE REMOVED AND REPLACED THE UPPER AND LOWER BUSHINGS OF THE RUDDER TAB UPPER BEARING AND THE AIRCRAFT WAS RETURNED TO SERVICE. ACFT TT: 18,278 .1 HRS. CYCLES, 21,241. (X) 2 H 7 2 4T RT A53EU 1996052300170 19960523 00170 EU 1996 5 23 C2XA96IA109 1 19960430 A 5520 S2738196320400 FITTINGS AEROSP ATR42 ATR42320 8680930 EU ELEVATOR WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 47801 60 IAH - DURING C-CHECK INSPECTION, THE ELEVATOR PITCH COUPLE FITTINGS WERE FOUND TO HAVE PLAY. MAINTENANCE REMOVED AND RE PLACED THE BELLCRANK COUPLING AND SHEAR PIN, AND THE AIRCRAFT WAS RETURNED TO SERVICE. AIRCRAFT TT: 18,278.2 HRS. CYC LES, 21,241. (X) 2 H 7 2 4T RT A53EU 1996052300171 19960523 00171 SO 1996 5 23 C2XA96IA110 1 19960430 A 5347 12026864007 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 27716 120128 IAH - DURING C-CHECK INSPECTION, THE LEFT AFT SEAT TRACK WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK AND THE AIRCRAFT WAS RETURNED TO SERVICE. ACFT TT: 14,059.3 HRS. CYCLES, 18,999. (X) 2 L 7 2 4T RT A31SO 1996052300172 19960523 00172 SO 1996 5 23 C2XA96IA111 1 19960424 A 7603 2008655001 PIN EMB 120 EMB120RT SO RT POWER LEVER WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 27716 120128 IAH - DURING C-CHECK INSPECTION, THE RIGHT POWER LEVER DID NOT DETENT AT THE FLIGHT IDLE POSITION. MAINTENANCE REMOVED AND REPLACED THE POWER LEVER PIN AND ROLLER AND THE AIRCRAFT WAS RETURNED TO SERVICE. ACFT TT: 14,059.3 HRS. CYCLES , 18,999. (X) 2 L 7 2 4T RT A31SO 1996052300173 19960523 00173 SO 1996 5 23 C2XA96IA112 1 19960430 A 5400 12030995001 ANGLE EMB 120 EMB120RT SO LT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 27716 120128 IAH - DURING C-CHECK INSPECTION, THE LEFT ENGINE NACELLE FRAME 2 TO NACELLE PAN ANGLE WAS FOUND CRACKED. MAINTENANCE RE MOVED AND REPLACED THE ANGLE AND THE AIRCRAFT WAS RETURNED TO SERVICE. ACFT TT: 14,059.3 HRS. CYCLES, 18,999. (X) 2 L 7 2 4T RT A31SO 1996052300174 19960523 00174 EU 1996 5 23 C2XA96IA113 1 19960430 A 5230 S52376114204 FITTING AEROSP ATR42 ATR42320 8680930 EU CARGO DOOR CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 47801 60 IAH - DURING C-CHECK INSPECTION, FOUND CARGO DOOR ACTUATOR ATTACH BRACKET INSIDE THE CARGO DOOR CRACKED. MAINTENANCE RE MOVED AND REPLACED THE BRACKET AND THE AIRCRAFT WAS RETURNED TO SERVICE. ACFT TT: 18,278.2 HRS. CYCLES, 21,241. (X) 2 H 7 2 4T RT A53EU 1996052300175 19960523 00175 SO 1996 5 23 C2XA96IA114 1 19960430 A 5530 12015374001 ANGLE EMB 120 EMB120RT SO LT VERT STAB CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 27716 120128 IAH - DURING C-CHECK INSPECTION, THE LEFT VERTICAL STABILIZER DRAG ANGLE WAS FOUND CRACKED. MAINTENANCE REMOVED AND REP LACED THE DRAG ANGLE AND THE AIRCRAFT WAS RETURNED TO SERVICE. ACFT TT: 14,059.3 HRS. CYCLES, 18,999. (X) 2 L 7 2 4T RT A31SO 1996052300176 19960523 00176 NE 1996 5 23 C2XA96IA115 2 19960502 A 7321 7863904 FUEL CONTROL EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE FAILED A C2XA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 SW 09 27716 7772 1185 120128 115388 IAH - FLT 3797 - PILOT REPORTED THAT DURING CRUISE, RIGHT ENGINE BEGAN TO DROP TORQUE. THE CREW SHUT DOWN THE ENGINE AN D RETURNED TO IAH WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 HMU, PERFORMED ENGINE CHECK RUNS AND APPROVED THE AIRCRAFT FOR RETURN TO SERVICE. (X) 2 L 7 2 4T 4 T RT A31SO E20NE 1996052300177 19960523 00177 NM 1996 5 23 EIAA9608 1 19960429 A 2612 89494301 CARD CONNECTOR BOEING 747 747121 1384871 NM APU LOOSE A EIAA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING DE DESCENT 1 NM 09 480EV 20348 DOV - ON DESCENT INTO DOV, GOT APU FIRE INDICATION (APU NOT RUNNING). COMPLETED EMERGENCY ITEMS AFTER APU FIRE TEST WOU LD NOT TEST. PULLED B-LOOP CIRCUIT BREAKER. LIGHT WENT OUT. A-LOOP FIRE TEST OK (SUSPECT FALSE FIRE INDICATION). CHE CKED BOTH APU, 'A' AND 'B' LOOP RESISTANCE. FOUND NORMAL. FOUND A-12 CARD CONNECTOR LOOSE. CLEANED AND RESECURED CONN ECTOR. APU FIRE DETECTOR SYSTEM CHECKED NORMAL IAW MM. (X) 2 L 7 4 4F A20WE 1996052300178 19960523 00178 WP 1996 5 23 GAIA9606 1 19960305 A 5311 9922042 FRAME DOUG DC9 DC915F 3022037 WP CARGO COMPT CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 563PC 47765 47055 DURING C-CHECK INSPECTION REVEALED 6 CRACKED STRUT FRAME ATTACH FITTINGS IN THE LOWER FUSELAGE CARGO COMPARTMENTS. CLOS ER INSPECTION REVEALED THE CRACKS TO BE CORROSION CRACKS ALONG GRAIN LINES. FOUR FRAMES WERE REPLACED IAW THE DOUGLAS S RM AND TWO OF THE FRAMES WERE REPAIRED IAW KITTY HAWK E.A. D9-53-011. REF: STA 427, 680 BETWEEN L22L AND L25L. STA 38 7, 661, 680, 699 BETWEEN L22R AND L25R. (X) 2 L 7 2 4F A6WE 1996052300179 19960523 00179 WP 1996 5 23 GAIA9607 1 19960412 A 5311 9922D42 FRAME DOUG DC9 DC915F 3022037 WP CARGO COMPT CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 562PC 45207 47012 DURING C-CHECK INSPECTION REVEALED 6 CRACKED STRUT FRAME ATTACH FTTINGS IN THE LOWER FUSELAGE CARGO COMPARTMENTS ON THE LEFT SIDE. CLOSER INSPECTION REVEALED THE CRACKS TO BE CORROSION CRACKS ALONG GRAIN LINES. THREE FRAMES WERE REPLACED IAW THE DOUGLAS SRM AND 3 OF THE FRAMES WERE REPAIRED IAW KITTY HAWK E.A. D9-53-018. THE AIRCRAFT WAS RETURNED TO SERVI CE. REF: STA 294, 313, 332, 408, 699, 766 BETWEEN L22L AND L25L. (X) 2 L 7 2 4F A6WE 1996052300180 19960523 00180 NE 1996 5 23 GAIA9608 2 19960305 A 7230 BEARING BOEING 727 727223 1384074 NM PWA JT8 JT8D9A 52048 NE NR 4 FAILED A GAIA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SW 07 6809 19484 666256 DURING CRUISE FLIGHT, ENGINE DEVELOPED HIGH OIL TEMPERATURE AND ENGINE ROUGHNESS, AND WAS SHUT DOWN. THE AIRCRAFT LANDE D WITHOUT INCIDENT. SUBSEQUENT TEAR DOWN REVEALED TOTAL FAILURE OF THE NR 4 DUPLEX BEARINGS WITH SECONDARY DAMAGE TO OT HER INTERNAL COMPONENTS. (X) 2 L 7 3 4F 4 F A3WE E2EA 1996052300181 19960523 00181 NM 1996 5 23 GAIA9609 1 19960506 A 3350 1000679 LIGHT BOEING 727 727223 1384074 NM L-1 DOOR INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 854AA 20995 L-1 BATTERY PACK FOR EMERGENCY LIGHTS WAS FOUND INOPERATIVE DURING GROUND TEST. PACK WAS REPLACED WITHOUT FURTHER INCID ENCE. (X) 2 L 7 3 4F A3WE 1996052300182 19960523 00182 WP 1996 5 23 HAL9649 1 19960422 A 3222 STRUT DOUG DC9 DC951 3022051 WP NOSE WW NLG OVERSERVICED A HALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 709HA 47764 HNL - FLT 537 - NOSE GEAR UNSAFE LIGHT AFTER GEAR RETRACTION. RECYCLED - NO JOY. GROUND SHIFT REMAINED ON GROUND. RES ERVICED NOSE GEAR STRUT. FOUND EXCESSIVE FLUID. GEAR SWING CHECK OK. (X) 2 L 7 2 4F A6WE 1996052300183 19960523 00183 WP 1996 5 23 HAL9651 1 19960423 A 3350 P4010049 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 679HA 4947 47662 HNL - FLT 503 - FORWARD CABIN EMERGENCY FLOOR LIGHTS DIM WHEN SELECTED. REPLACED BATTERY PACK FORWARD AND AFT. OPS OK. (X) 2 L 7 2 4F A6WE 1996052300184 19960523 00184 WP 1996 5 23 HAL9653 1 19960425 A 5320 SPLICE DOUG DC9 DC951 3022051 WP BS 389 CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 679HA 47662 HNL - LEFT WINDOW BELT UPPER SPLICE CRACK INDICATION AT STA 389 IS PAST AFT STOP DRILL HOLE. REMOVED DOUBLER, STOP DRIL LED PER REPAIR SCHEME J060131. REINSTALLED DOUBLER PER HAL M133. LEAK CHECKED OK PER MM 56-20-2. (X) 2 L 7 2 4F A6WE 1996052300185 19960523 00185 WP 1996 5 23 HAL9655 1 19960505 A 3260 PROX BOX DOUG DC10 DC1010 3022110 WP E/E COMPT MALFUNCTIONED A HALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 WP 13 148AA 46703 HNL - FLT 921 - LANDING GEAR INDICATED THREE RED ON FINAL. CYCLED GEAR TWICE AND GOT THREE GREEN AFTER GO-AROUND. REPL ACED PROXIMITY SWITCH CONTROL BOX. BITE CHECK GOOD. (X) 2 L 7 3 4F A22WE 1996052300186 19960523 00186 WP 1996 5 23 IXAA9666 1 19960414 A 5313 4751770 LONGERON DOUG DC8 DC862 3021970 WP FS 535 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 728PL 70866 20327 45918 DURING ROUTINE C-CHECK, LONGERON 35 RIGHT WAS FOUND WITH CORROSION, CORROSION REMOVAL WAS BEYOND SRM LIMITS. THE AFFECT ED SECTION OF LONGERON WAS REMOVED, FABRICATED, AND INSTALLED IAW AIRCRAFT SRM 51-1-8 AND SRM 53-2-3. (X) 2 L 7 4 4F 4A25 1996052300187 19960523 00187 WP 1996 5 23 IXXA9652 1 19960419 A 5415 57530111 PLANK DOUG DC8 DC862 3021970 WP NR 1 PYLON CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 728PL 70866 20327 45918 DURING ROUTINE C-CHECK INSPECTION, THE NR 1 OUTBOARD PYLON REMOVABLE PLANK WAS FOUND CRACKED. THE PLANK WAS REMOVED, RE PAIRED, AND REINSTALLED IAW AIRCRAFT SRM 54-2-2 AND SRM 5-1-21. (X) 2 L 7 4 4F 4A25 1996052300188 19960523 00188 WP 1996 5 23 IXXA9653 1 19960419 A 5320 T-FITTING DOUG DC8 DC862 3021970 WP FS 950 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 728PL 70866 20327 45918 DURING ROUTINE C-CHECK INSPECTION, THE KEEL BEAM SUPPORT FITTING AT FS 950 WAS FOUND CRACKED. THE FITTING WAS REMOVED, FABRICATED AND INSTALLED IAW AIRCRAFT SRM 53-1-0. (X) 2 L 7 4 4F 4A25 1996052300189 19960523 00189 WP 1996 5 23 IXXA9654 1 19960419 A 5320 FITTING DOUG DC8 DC862 3021970 WP FS 895 AND 902 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 728PL 70866 20327 45918 DURING ROUTINE C-CHECK INSPECTION, KEEL BEAM SUPPORT FITTINGS AT FS 895 AND FS 902 WERE FOUND CRACKED. THE FITTINGS WER E REMOVED, FABRICATED, AND INSTALLED IAW AIRCRAFT SRM 53-1-0. (X) 2 L 7 4 4F 4A25 1996052300190 19960523 00190 WP 1996 5 23 IXXA9655 1 19960416 A 5720 AUX SPAR WEB DOUG DC8 DC862 3021970 WP XW 97 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 728PL 70866 20327 45918 DURING ROUTINE C-CHECK INSPECTION, THE RIGHT AUXILIARY SPAR WEB AT APPROXIMATE WS XW 97 WAS FOUND WITH LOCAL CORROSION. THE CORROSION WAS REMOVED, TREATED, AND PROTECTED IAW AIRCRAFT SRM 51-1-8. (X) 2 L 7 4 4F 4A25 1996052300191 19960523 00191 WP 1996 5 23 IXXA9656 1 19960416 A 5313 57501981 LONGERON DOUG DC8 DC862 3021970 WP FS 920 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 728PL 70866 20327 45918 DURING ROUTINE C-CHECK INSPECTION, LONGERON 24 LEFT WAS FOUND CRACKED BETWEEN FASTENER HOLES AT FS 920. THE CRACK WAS S TOP DRILLED. REPAIR WAS ACCOMPLISHED BY FABRICATING AND INSTALLING REPAIR DOUBLER IAW THE AIRCRAFT SRM 53-2-2 AND SRM 5 1-1-21. (X) 2 L 7 4 4F 4A25 1996052300192 19960523 00192 WP 1996 5 23 IXXA9657 1 19960416 A 5400 RIB DOUG DC8 DC862 3021970 WP NR 2 PYLON CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 728PL 45918 DURING ROUTINE C-CHECK INSPECTION, THE NR 2 PYLON STUB WING, INBOARD RIB, FORWARD SECTION, WAS FOUND WITH 2 CRACKS. THE RIB ASSEMBLY WAS REMOVED AND REPLACED IAW THE AIRCRAFT SRM 51-2-0. (X) 2 L 7 4 4F 4A25 1996052300193 19960523 00193 WP 1996 5 23 IXXA9658 1 19960416 A 5400 RIB DOUG DC8 DC862 3021970 WP NR 2 PYLON CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 728PL 70866 20327 45918 DURING ROUTINE C-CHECK INSPECTION, THE NR 2 PYLON STUB WING UPPER CENTER RIB WAS FOUND CRACKED. REPAIR TO THE RIB WAS A CCOMPLISHED BY FABRICATING AND INSTALLING REPAIR DOUBLER AND ANGLE IAW THE AIRCRAFT SRM 57-2-0 AND SRM 51-1-20D. (X) 2 L 7 4 4F 4A25 1996052300194 19960523 00194 WP 1996 5 23 IXXA9659 1 19960405 A 5330 PLATING DOUG DC8 DC862 3021970 WP BS 1500-1530 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 728PL 70866 20327 45918 DURING ROUTINE C-CHECK INSPECTION, EXTERNAL CORROSION OF THE FUSEAGE SKIN WAS FOUND. DAMAGE LOCATED BETWEEN FS 1500 AND FS 1530 AT LONGERON 1. REPAIR WAS ACCOMPLISHED BY CORROSION REMOVAL, FABRICATION AND INSTALLATION OF REPAIR DOUBLER. R EPAIR WAS ACCOMPLISHED IAW FAA DER APPROVED SKETCH A40-R02. (X) 2 L 7 4 4F 4A25 1996052300195 19960523 00195 WP 1996 5 23 IXXA9660 1 19960416 A 5313 57501982 LONGERON DOUG DC8 DC862 3021970 WP FS 920 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 728PL 70866 20327 45918 DURING ROUTINE C-CHECK INSPECTION, THE RIGHT LONGERON 24 WAS FOUND CRACKED BETWEEN FASTENER HOLES AT FS 920. REPAIR OF THE LONGERON WAS ACCOMPLISHED BY STOP DRILLING THE CRACK, FABRICATING AND INSTALLING REPAIR DOUBLER IAW AIRCRAFT SRM 53- 2-2 AND SRM 51-1-21. (X) 2 L 7 4 4F 4A25 1996052300196 19960523 00196 WP 1996 5 23 IXXA9661 1 19960423 A 5720 AUX SPAR WEB DOUG DC8 DC862 3021970 WP RT WING CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 728PL 70866 20327 45918 DURING ROUTINE C-CHECK AND MLG ATTACH FITTING REPLACEMENT, THE LEFT AUXILIARY SPAR WEB WAS FOUND WITH LOCAL CORROSION AN D CRACKS. THE WEB WAS REPLACED WITH A NEW WEB IAW DOUGLAS DRAWING 3641823-1. (X) 2 L 7 4 4F 4A25 1996052300197 19960523 00197 WP 1996 5 23 IXXA9662 1 19960424 A 5720 COVER PLATE SIMMONDS B277XXX DOUG DC8 DC862 3021970 WP LEFT WING CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 728PL 70866 20327 45918 DURING ROUTINE C-CHECK INSPECTION, FUEL PROBE ATTACH PLATES 9, 15, AND 17, OF THE LEFT WING WERE FOUND CRACKED. REPAIR OF THE ATTACH PLATES WAS ACCOMPLISHED IAW FAA DER APPROVED SKETCHES 96108-1, 96108-2, AND 96108-3. 2 L 7 4 4F 4A25 1996052300198 19960523 00198 WP 1996 5 23 IXXA9663 1 19960424 A 5230 DOOR TRACK DOUG DC8 DC862 3021970 WP CARGO COMPT WORN A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 728PL 70866 20327 45918 DURING ROUTINE C-CHECK INSPECTION, THE AFT LOWER FORWARD CARGO DOOR FORWARD GUIDE TRACK WAS FOUND WORN BEYOND LIMITS. R EPAIR OF THE DOOR TRACK WAS ACCOMPLISHED IAW REPAIR SKETCH A40-R05 WHICH IS FAA DER APPROVED. (X) 2 L 7 4 4F 4A25 1996052300199 19960523 00199 WP 1996 5 23 IXXA9664 1 19960424 A 5730 SKIN DOUG DC8 DC862 3021970 WP WS 195 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 728PL 70866 20327 45918 DURING ROUTINE C-CHECK INSPECTION, LOCALIZED CORROSION WAS FOUND TO THE LEFT LEADING EDGE, STA XFS 195, UPPER ATTACH BOL T HOLES. REPAIR TO THE LEADING EDGE WAS ACCOMPLISHED IAW FAA DER APPROVED SKETCH A40-R04. (X) 2 L 7 4 4F 4A25 1996052300200 19960523 00200 WP 1996 5 23 IXXA9665 1 19960424 A 5530 2649896 ANGLE DOUG DC8 DC862 3021970 WP VERTICAL CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 728PL 70866 20327 45918 DURING ROUTINE C-CHECK INSPECTION, THE VERTICAL STABILIZER FUSELAGE ATTACH ANGLE AT STATIONS 1626, 1640, AND 1667, WAS F OUND CRACKED. REPAIR OF THE CRACKED ANGLE WAS ACCOMPLISHED IAW DOUGLAS ROD SKETCH 96-04-02-005, WHICH IS FAA DER APPROV ED. (X) 2 L 7 4 4F 4A25 1996052300201 19960523 00201 WP 1996 5 23 IXXA9667 1 19960414 A 5520 HINGE FLANGE DOUG DC8 DC862 3021970 WP LT ELEVATOR BENT A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 728PL 70866 20327 45918 DURING ROUTINE C-CHECK INSPECTION, THE LEFT ELEVATOR, NR 4 HINGE FLANGE WAS FOUND BENT. THE DAMAGED AREA WAS REMOVED IA W THE AIRCRAFT SERVICE REPAIR MANUAL. (X) 2 L 7 4 4F 4A25 1996052300202 19960523 00202 WP 1996 5 23 IXXA9668 1 19960412 A 5532 LE SKIN DOUG DC8 DC862 3021970 WP VERTICAL STAB CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 728PL 70866 20327 45918 DURING ROUTINE C-CHECK INSPECTION, LOCALIZED CORROSION WAS FOUND ON THE VERTICAL STABILIZER LEADING EDGE. DAMAGE WAS AT STA ZFS 173, RIGHT, ATTACHMENT SCREW HOLE. THE CORROSION WAS REMOVED, REPAIR DOUBLERS FABRICATED AND INSTALLED IAW WIT H THE AIRCRAFT SRM 55-2-1. (X) 2 L 7 4 4F 4A25 1996052300203 19960523 00203 WP 1996 5 23 IXXA9669 1 19960412 A 5330 PLATING DOUG DC8 DC862 3021970 WP FS 1620 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 728PL 70866 20327 45918 DURING ROUTINE C-CHECK INSPECTION, LOCALIZED CORROSION OF THE FUSELAGE PLATING, AT FS 1620, LONGERON 5 LEFT, WAS FOUND. THE CORROSION WAS REMOVED, REPAIR DOUBLERS FABRICATED AND INSTALLED IAW THE AIRCRAFT SRM 51-1-8 AND SRM 53-2-1. (X) 2 L 7 4 4F 4A25 1996052300204 19960523 00204 WP 1996 5 23 IXXA9670 1 19960411 A 5320 5757781 SPLICE FITTING DOUG DC8 DC871 302199A WP FS 1620 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 829BX 75885 7751 45994 DURING ROUTINE C-CHECK INSPECTION, LONGERON 33 LEFT, SPLICE FITTING, AT STA 1694, WAS FOUND CRACKED. THE CRACK WAS .375 INCH IN LENGTH AT THE FORWARD END OF THE FITTING. THE CRACK WAS REMOVED FROM THE SPLICE FITTING AND REINSTALLED IAW DR AWING COO-SJO-96-0139DAC AND COO-SJO-96-014DAC, WHICH IS FAA DER APPROVED. (X) 2 L 7 4 4F 4A25 1996052300205 19960523 00205 WP 1996 5 23 IXXA9671 1 19960411 A 5330 SKIN DOUG DC8 DC871 302199A WP FS -50 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 829BX 75885 7751 45994 DURING ROUTINE C-CHECK INSPECTION, THE FUSELAGE PLATING AT THE EXTERNAL POWER RECEPTACLE WAS FOUND CRACKED. THE CRACK W AS LOCATED BETWEEN LONGERONS 31 AND 32 RT, AT FS -50. THE CRACK WAS REMOVED, REPAIR FILLERS, DOUBLERS WERE FABRICATED A ND INSTALLED IAW DRAWING 853-28-96 WHICH IS FAA DER APPROVED. (X) 2 L 7 4 4F 4A25 1996052300206 19960523 00206 WP 1996 5 23 IXXA9672 1 19960409 A 5330 SKIN DOUG DC8 DC871 302199A WP FS 336 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 829BX 75885 7751 45994 DURING ROUTINE C-CHECK INSPECTION, AN EXTERNAL FUSELAGE SKIN CRACK, LOCATED AT FS 336.5 AND LONGERON 36, WAS FOUND. THE DAMAGED SKIN WAS REMOVED, FILLERS AND DOUBLERS FABRICATED AND INSTALLED. THE REPAIR WAS IAW WITH DRAWING 8-53-29-96, W HICH IS FAA DER APPROVED. (X) 2 L 7 4 4F 4A25 1996052300207 19960523 00207 WP 1996 5 23 IXXA9673 1 19960412 A 5730 PANEL DOUG DC8 DC871 302199A WP LEFT WING DELAMINATED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 829BX 75885 7751 45994 DURING ROUTINE C-CHECK INSPECTION, A LEFT WING TRAILING EDGE HONEYCOMB PANEL WAS FOUND DELAMINATED ON THE LEFT WING UPPE R SURFACE BETWEEN STATIONS XRS 436. AND XA 588.5. THE PANEL WAS REPAIRED IAW DRAWING 8-57-066-96, WHICH IS FAA DER APPR OVED. (X) 2 L 7 4 4F 4A25 1996052300208 19960523 00208 WP 1996 5 23 IXXA9674 1 19960409 A 5730 PANEL DOUG DC8 DC871 302199A WP RT WING DELAMINATED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 829BX 75885 7751 45994 DURING ROUTINE C-CHECK INSPECTION, A RIGHT WING TRAILING EDGE FIXED PANEL WAS FOUND DELAMINATED. THE PANEL WAS DELAMINA TED BETWEEN WING STATIONS XA 589.0 AND XA 624.0. REPAIR OF THE PANEL WAS ACCOMPLISHED INSTALLING AN EXTERNAL DOUBLER IA W DRAWING 8-57-064-96, WHICH IS FAA DER APPROVED. (X) 2 L 7 4 4F 4A25 1996052300209 19960523 00209 WP 1996 5 23 IXXA9675 1 19960409 A 5330 SKIN DOUG DC8 DC871 302199A WP DOOR CUT OUT DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 829BX 75885 7751 45994 DURING ROUTINE C-CHECK INSPECTION, DAMAGED WAS NOTED TO THE LOWER FORWARD CARGO COMPARTMENT DOOR CUT-OUT AT THE FORWARD EDGE. THE DAMAGE WAS REMOVED, REPAIR FILLER AND DOUBLERS WERE FABRICATED AND INSTALLED IAW DRAWING 8-53-27-96, WHICH IS FAA DER APPROVED. (C) 2 L 7 4 4F 4A25 1996052300210 19960523 00210 WP 1996 5 23 IXXA9676 1 19960409 A 5330 SKIN DOUG DC8 DC871 302199A WP FS 340 DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 829BX 75885 7751 45994 DURING ROUTINE C-CHECK INSPECTION, THE FUSELAGE EXTERIOR PLATING WAS FOUND DAMAGED. DAMAGE WAS LOCATED AT THE FORWARD L OWER, RIGHT AFT CORNER OF THE NR 1 BASKET DOOR CUT-OUT, AT FS 340. THE DAMAGED AREA WAS REMOVED. THE REPAIR WAS ACCOMP LISHED BY FABRICATING AND INSTALLING A FILLER AND EXTERNAL DOUBLERS BETWEEN FS 328-FS 340 AND LONGERONS 29-31 RIGHT. RE PAIR WAS ACCOMPLISHED IAW DRAWING 8-53-24-96 WHICH IS FAA DER APPROVED. (X) 2 L 7 4 4F 4A25 1996052300211 19960523 00211 WP 1996 5 23 IXXA9677 1 19960413 A 5753 1656396 CHANNEL DOUG DC8 DC871 302199A WP LT TE FLAP CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 829BX 75885 7751 45994 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND IN THE INBOARD FLAP, OUTBOARD END, UPPER CENTER CHANNEL SECTION. T HE CRACKED PART WAS REMOVED, FABRICATED AND INSTALLED IAW EO 8-57-067-96, AND THE AIRCRAFT SRM 51-2-0. (X) 2 L 7 4 4F 4A25 1996052300212 19960523 00212 NM 1996 5 23 MZZA96005 1 19960206 A 2782 141110 ACTUATOR 651781820 BOEING 727 727227 1384078 NM NR 3 LE FLAP FAILED A MZZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 89427 5473 21365 TPE - FLT CS921 - DURING CLIMB-OUT, NR 3 KRUEGER FLAP FAILED TO RETRACT. FLIGHT CREW RAN CHECK LIST AND AIR RETURNED TO TPE. MAINTENANCE REMOVED AND REPLACED NR 3 LEADING EDGE FLAP ACTUATOR PER MM 27-87-22 AND SYSTEM OPERATION CHECK GOOD. AIRCRAFT RELEASED FOR FLIGHT. (X) 2 L 7 3 4F A3WE 1996052300213 19960523 00213 1996 5 23 MZZA96012 4 19960306 A 3418 2566A21 AOA SENSOR BOEING 727 727232 1384082 NM E/E COMPT FAILED A MZZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 13 15790 1602 20644 GUM - FLT 873 - STICK SHAKER CAME ON RIGHT AFTER TAKEOFF, FLAPS 15 FEET, 5 FEET, 2 FEET, STAYED ON CONSTANTLY. IT CAME ON AFTER 2 FOOT FLAPS FOR EXTENSION ON LANDING. MAINTENANCE FOUND WIRE LOSE ON NLG GROUND/AIR SENSE SWITCH. MECHANIC S ECURED WIRE AND REPLACED ANGLE OF ATTACK SENSOR AS PRECAUTIONARY IAW 727-200 MM 34-18-51. (X) 2 L 7 3 4F A3WE 1996052300214 19960523 00214 NM 1996 5 23 MZZA96015 1 19960402 A 3230 65258519 UPLOCK SHAFT BOEING 727 727224 1384076 NM LT MLG BROKEN A MZZA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 WP 13 79743 22252 GUM - FLT 992 - DURING APPROACH TO GUM, LEFT MLG WOULD NOT EXTEND. MANUALLY HAD TO EXTEND GEAR. GEAR DOWN AND LOCKED N ORMALLY. MAINTENANCE FOUND THE UPLOCK SHAFT ASSY BROKEN. THE GEAR UPLOCK SHAFT ASSY WAS REMOVED AND REPLACED PER MM 32 -30-51 AND GEAR SWING CHECK NORMAL PER MM 32-32-0, PAGE 501. (X) 2 L 7 3 4F A3WE 1996052300215 19960523 00215 NM 1996 5 23 MZZA96016 1 19960403 A 2782 1U11032 SLAT ACTUATOR BOEING 727 727224 1384076 NM NR 6 LE SLAT CRACKED A MZZA A J UNSCHED LANDING DUMP FUEL K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 13 79744 8709 22253 GUM - FLT 0956 - ON TAKEOFF CLIMB OUT OF TKK, NR 6 LEADING EDGE SLAT DID NOT RETRACT AND A HYDRAULIC SYSTEM HAD FLUID LO SS. ALL REQUIRED CHECK LISTS WERE COMPLETED AND AIRCRAFT DIVERTED TO GUM. MAINTENANCE FOUND THE NR 6 LEADING EDGE SLAT ACTUATOR FORWARD END CAP HAD CRACKED OFF. THE NR 6 SLAT ACTUATOR WAS REPLACED PER MM 27-81-32/22. ALSO, THE A-SYSTEM HYDRAULIC MODULE FILTERS AND THE NR 1 AND NR 2 ENGINE HYDRAULIC PUMPS WERE REPLACED DUE TO HYDRAULIC FLUID LOSS. (X) 2 L 7 3 4F A3WE 1996052300216 19960523 00216 NM 1996 5 23 MZZA96017 1 19960405 A 2612 18252 FIRE DETECTOR BOEING 727 727224 1384076 NM NR 1 ENGINE FAILED A MZZA A J UNSCHED LANDING DUMP FUEL N FALSE WARNING CR CRUISE 1 WP 13 79743 22252 GUM - FLT 0956 - DURING FLIGHT EN ROUTE TO TKK, THE NR 1 ENGINE GROUND FAULT DETECTION LIGHT ILLUMINATED. FLIGHT CREW D ECIDED TO RETURN TO GUM. FUEL DUMP WAS ACCOMPLISHED TO LANDING WEIGHT OF 154.5 POUNDS. MAINTENANCE INSPECTED FIRE LOOP FOR POSSIBLE GROUNDING TO STRUCTURE AND NONE FOUND. MAINTENANCE PRECAUTIONARY REPLACED THE NR 1 ENGINE FIRE LOOP PER M M 26-11-22. ALSO, DURING INSPECTION, MAINTENANCE NOTICED THE N2 TACHOMETER GENERATOR WITH ENGINE OIL LEAKING AT THE BAS E AND THE GASKET WAS REPLACED. GROUND RUN-UP CHECKED GOOD. NO GROUND FAULT AND FIRE WARNING TEST CHECKED GOOD. COWLIN G SECURED. (X) 2 L 7 3 4F A3WE 1996052300217 19960523 00217 NM 1996 5 23 MZZA96020 1 19960410 A 3350 110049 CHARGER BOEING 727 727212 138407G NM CABIN FAILED A MZZA K NONE L NO TEST IN INSP/MAINT 1 WP 13 296AS 1795 21459 GUM - DURING SERVICE CHECK, EMERGENCY LIGHT CHECK, EXIT PATH LIGHTING FROM ROW 23 TO AFT BULKHEAD FADED AFTER 10-15 SECO NDS, REMAINDER OF LIGHTING TESTED GOOD. MAINTENANCE REMOVED AND REPLACED AFT EMERGENCY PACK CHARGER PER MM 33-50-01 AND SYSTEM CHECKED GOOD. (X) 2 L 7 3 4F A3WE 1996052300245 19960523 00245 WP 1996 5 23 96DHL802004 1 19960516 A 2530 03910808P4 LIGHT SOCKET DOUG DC8 DC873F 302199F WP GALLEY FAILED A T DHLA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 802DH 46076 ELECTRICAL SMOKE IN GALLEY FROM HOT CUP LIGHT. REMOVED AND REPLACED HOT CUP LIGHT SOCKET, CHECK OK PER M/M 25-20. 2 L 7 4 4F RT 4A25 1996052300246 19960523 00246 NM 1996 5 23 DL72S961149 1 19960509 A 5330 6554583164 SKIN BOEING 727 727232 1384082 NM BS 1010 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 418DA 21271 CORROSION REMOVAL RESULTED IN TWO NEW CUTOUTS JUST AFT OF FS 1010, BETWEEN S-29L AND S-28R. THE FIRST, JUST OUTBOARD OF S-28R AND EXTENDS FURTHER OUTBOARD, MEASURES 6.5 FWD TO AFT BY 3.125 INBOARD AFT. EXT DOUBLER REMOVED REVEALING CUTOUT , EXISTING INTERNAL DOUBLER WAS REMOVED REVEALING A CUTOUT. THE LOCAL SKIN AT ALL DAMAGE LOCATIONS IS 0.070 THICK 2024- T3 CLAD ALUMINUM. 2 L 7 3 4F A3WE 1996052300247 19960523 00247 NM 1996 5 23 DL72S961150 1 19960510 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM R-1 DOOR CUTOUT FATIGUE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 528DA 21702 THE FUSELAGE SKIN, DOUBLER, ANT TRIPLER ARE CRACKED IN THE UPPER FORWARD CORNER OF THE R-1 DOOR CUTOUT. THE CRACK IS 0. 5 LONG AND RAN FROM THE EDGE OF THE CUTOUT TO A LOCAL RIVET HOLE. THE SKIN IN THE AREA IS 0.040 THICK, THE DOUBLER IS 0 .025 THICK AND THE TRIPLER IS 0.020 THICK ALL THREE LAYERS ARE MANUFACTURED FROM CLAD 2024-T3 SHEET. 2 L 7 3 4F A3WE 1996052300248 19960523 00248 NM 1996 5 23 DL72S961154 1 19960514 A 5414 SKIN BOEING 727 727232 1384082 NM NR 2 INLET CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 498DA 21142 A 2 INCH CRACK IN NR 2 ENG INLET OUTER SKIN 3 FT FROM INLET LIP, 2 FT UP FROM FUSELAGE SKIN LT SIDE. REPAIRED PER M/M 5 4-30-0 FIG 801. 2 L 7 3 4F A3WE 1996052300249 19960523 00249 NM 1996 5 23 DL72S961160 1 19960513 A 5753 651927011 SHIM BOEING 727 727232 1384082 NM TE FLAP OUT OF POSITION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 468DA 20745 DURING INSPECTIONS PER SI 4-58663-12AD, THE LAMINATED SHIMS INSTALLED ON THE RIGHT AND LEFT WING INBOARD TRAILING EDGE F LAP INBOARD TRACKS WERE FOUND TO HAVE MIGRATED GREATER THAN THE 0.25 LIMIT SPECIFIED IN THE INSPECTION. IN COMPLIANCE W ITH AD 90-07-05, THE MIGRATED RIGHT HAND SHIM WILL BE RELOCATED, THE LEFT HAND SHIM WILL BE REPLACED AND ATTACHMENTS RET ORQUED. 2 L 7 3 4F A3WE 1996052300250 19960523 00250 NM 1996 5 23 DL72S961163 1 19960515 A 5320 651751731 WEB BOEING 727 727232 1384082 NM BS 1263 FATIGUE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 498DA 21142 THE AFT VENTRAL STAIRWAY TORQUE BOX RT VERTICAL WEB AT STA 1263 HAD A .75 INCH CRACK AT THE NR 2 ENGINE FUEL LINE CUTOUT . MADE SPLICE REPAIR PER ER/A 303593-14. 2 L 7 3 4F A3WE 1996052300251 19960523 00251 NM 1996 5 23 DL72S961164 1 19960515 A 5240 DOOR BOEING 727 727232 1384082 NM R-2 SERVICE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 482DA 20862 A .25 INCH VISIBLE CRACK UPPER FWD END OF RT AFT SERVICE DOOR. REPAIRED PER SRM 52-40-2 FIG 4, INSTALLED DOOR ON AIRCRA FT AND LEAK OPS CHECK OK. 2 L 7 3 4F A3WE 1996052300252 19960523 00252 NM 1996 5 23 DL72S961172 1 19960515 A 3350 900835A BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 469DA 20746 OVERWING EMERGENCY LIGHT INOP. REPLACED RACK AND BATTERY. 2 L 7 3 4F A3WE 1996052300254 19960523 00254 NM 1996 5 23 DL73E961151 1 19960509 A 5320 INTERCOSTAL BOEING 737 737247 138448D NM BS 332 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 245WA 23519 THE R1 DOOR FRAME INTERCOSTAL AT STR 8A WAS FOUND CRACKED IN THE TYPICAL MANNER SHOWN IN S/B 737-53A1108, REV 5. THIS E R/A ACCOMPLISHES A REPAIR AT THIS LOCATIONS IN ACCORDANCE WITH BACO S/B 737-53A1108 AND AIRWORTHINESS DIRECTIVE 88-03-03 . 2 L 7 2 4F A16WE 1996052300255 19960523 00255 NM 1996 5 23 DL73S961159 1 19960514 A 3350 20131A BATTERY BOEING 737 737232 1384475 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 305DL 23077 RIGHT LOWER WING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK, ALL OPS NORMAL. 2 L 7 2 4F RT A16WE 1996052300256 19960523 00256 NM 1996 5 23 DL757961118 1 19960509 A 3350 BULB BOEING 757 757232 1384965 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 602DL 22809 LEFT AFT EXTERIOR EMERGENCY LIGHT FAILS TO LIGHT. RELAMPED LIGHT, CKS GOOD. 2 L 7 2 4F RT A2NM 1996052300257 19960523 00257 NM 1996 5 23 DL757961129 1 19960511 A 3350 BULB BOEING 757 757232 1384965 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 649DL 24389 LEFT AFT OVERWING SLIDE LIGHT INOP. RELAMPED, OPS CK NORMAL. 2 L 7 2 4F RT A2NM 1996052300258 19960523 00258 NM 1996 5 23 DL757961152 1 19960514 A 5210 SAFETY BUTTON BOEING 757 757232 1384965 NM R2 DOOR DAMAGED A DALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 27 677DL 25982 R2 DOOR HANDLE POPPED UP ON TAKEOFF ROLL. RETURNED TO MEX, FOUND DOOR SAFETY STRAP BUTTON JAMMED IN DOOR SILL. REMOVED DOOR, OPERATION NORMAL. 2 L 7 2 4F RT A2NM 1996052300259 19960523 00259 WP 1996 5 23 DLL10961122 1 19960511 A 3350 081691 HOLDER LKHEED 1011 10113851 5265010 WP CABIN MISSING A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 715DA 193C1092 ON LAYOVER, FOUND EMERGENCY FLOOR TRACK LIGHT MISSING AT 28AB. REPLACED EMERGENCY FLOOR TRACK LIGHT HOLDER AT 28AB, CHE CKS NORMAL. 2 L 7 3 4F A23WE 1996052300260 19960523 00260 WP 1996 5 23 DLL10961137 1 19960422 A 5330 1503492 SKIN LKHEED 1011 10113851 5265010 WP FS 200 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 720DA 193C1136 THE SKIN SECTION BETWEEN FS 158 AND 267 AT WL 198 WAS FOUND TO HAVE FURTHER DAMAGE THAN THAT WHICH WAS REPAIRED BY E R/A 266918-14. THE NEW DAMAGE CONSISTED OF SEVERAL GOUGES. THE GOUGES WERE REMOVED AND REINFORCED, REV A TO ER/A 27365 3-14 PROVIDES FAA APPROVAL. 2 L 7 3 4F A23WE 1996052300261 19960523 00261 WP 1996 5 23 DLL10961138 1 19960418 A 5330 1503140103 SKIN LKHEED 1011 10113851 5265010 WP FS 915 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 720DA 193C1136 THE FUSELAGE SKIN BETWEEN FS 887, 940 AND STR 42 AND 2 BELOW STR 40 REQUIRES REPLACEMENT, REV B TO ER/A PROVIDES FAA APP ROVAL. 2 L 7 3 4F A23WE 1996052300262 19960523 00262 WP 1996 5 23 DLL10961139 1 19960422 A 5712 1527031504 RIB CAPS LKHEED 1011 10113851 5265010 WP WS 503 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 720DA 193C1136 THE RT WING IWS 503 RIB UPPER AND LOWER CAPS HAVE CRACKS IN THE TYPICAL LOCATION AT THE ATTACH TABS. THE CAPS ARE TO BE REPLACED PER EO 7-59208-3AD, BUT THE COMPLETE REMOVAL OF THE UPPER CAP PROVIDES SUFFICIENT ACCESS TO ALLOW ONE SPLICE L OCATION IN EACH CAP TO BE ELIMINATED. THIS WILL SAVE MTC TIME AND EFFORT AS WELL AS PRODUCE A STRUCTURALLY SUPERIOR INS TALLATION, REV A TO ER/A PROVIDES FAA APPROVAL. 2 L 7 3 4F A23WE 1996052300263 19960523 00263 WP 1996 5 23 DLL14961157 1 19960508 A 5320 1518590175 FAIRING SUPT LKHEED 1011 1011385115 5265015 WP BS 1363-1443 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 736DY 193C1227 P/N 1518590-175 T, FOR FUSELAGE FAIRING SUPPORT STRUCTURE CRACKED AFT OF STA 1363. REPLACED. 2 L 7 3 4F A23WE 1996052300264 19960523 00264 NE 1996 5 23 DLM11961115 2 19960509 A 7230 COMPRESSOR DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE NR 1 ENGINE FAILED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 27 806DE 48477 733731 ON TAKEOFF LOUD BANG LEFT SIDE, VIBRATION, ABORTED T/O. A/C REPORTED SMOKE AND FIRE, FIRED NR 1 AGENT BOTTLE. SHUTDOWN PER CHECKLIST. FOUND COMPRESSOR HAD FAILED, METAL IN TAILPIPE AND BELOW 2.5 BLEED OPENING. MTC IN PROGRESS. 2 L 7 3 4F 4 F RT A22WE E24NE 1996052300265 19960523 00265 NE 1996 5 23 DLM11961124 2 19960509 A 7200 ENGINE DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE NR 1 FAILED A DALA E F C D ENGINE SHUTDOWN ACTIVATE FIRE EXT. ABORTED TAKEOFF RETURN TO BLOCK N Y FALSE WARNING ENGINE STOPPAGE TO TAKEOFF 1 SO 27 806DE 48477 733731 NR 1 ENGINE FAILED DURING T/O RUN. LOUD BANG FROM LEFT SIDE OF A/C HEARD, T/O ABORTED AT 50 KNOTS. A/C REPORTED SMOKE AND FIRE. BLEW NR 1 FIRE BOTTLE AND SHUT DOWN ENGINE. NO EVIDENCE OF FIRE FOUND DURING INSPECTION. CHANGED ENGINE, ME TAL FOUND IN BLEED VALVE. 2 L 7 3 4F 4 F RT A22WE E24NE 1996052300266 19960523 00266 NM 1996 5 23 DLM90961131 1 19960512 A 2421 GENERATOR DOUG MD90 MD9030 3023690 NM RT ENGINE FAILED A DALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 SO 27 901DA 53381 ON DEPARTURE OUT OF DFW LOST RT GENERATOR. NO OTHER ELECTRICAL MALFUNCTIONS NOTED. 2 L 7 2 4F RT A6WE 1996052300267 19960523 00267 WP 1996 5 23 MWEA96139 1 19960516 A 2560 113313 SLIDE COVER DOUG DC9 DC932 3022066 WP GALLEY SERV DOOR FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 301ME 47190 CREW REPORTS, GALLEY SERVICE DOOR EVAC SLIDE AND COVER NOT ATTACHED. 2 L 7 2 4F A6WE 1996052300268 19960523 00268 WP 1996 5 23 MWEA96140 1 19960518 A 5330 SKIN DOUG DC9 DC915 3022036 WP BS 40/55 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 DURING TOWING, THE A/C RECEIVED SKIN DAMAGE WHEN COMING IN CONTACT WITH TOWING UNIT. TWO DENTS AT STA 40 AND 55 ABOVE L T NOSE GEAR DOOR. INSTALLED REPAIRS IAW SRM 53-01 FIG 4, SHT 3. 2 L 7 2 4F A6WE 1996052300269 19960523 00269 1996 5 23 MWEA96141 4 19960519 A 3418 9640041027 STALL WARN COMP DOUG DC9 DC932 3022066 WP E/E COMPT INOP A MWEA C D ABORTED TAKEOFF RETURN TO BLOCK R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 31 207ME 47794 PILOT REPORTS, ON TAKEOFF ROLL RH ENGINE WOULD NOT DEVELOP FULL TAKEOFF EPR. ABORTED TAKEOFF AT APPROX 80 KTS. N1 AND N2 SLIGHTLY LESS THAN LT ENGINE. WHILE TAXIING BACK TO GATE STALL IND FAILURE LIGHT CAME ON AS FLAPS/SLATS RETRACTED. R EPLACED NR 2 STALL WARNING COMP, PERFORMED FULL TAKEOFF POWER RUN AND ALL PARAMETERS WITHIN LIMITS. 2 L 7 2 4F A6WE 1996052300270 19960523 00270 NM 1996 5 23 SCNA96141 1 19960507 A 5315 FLOOR BEAM BOEING 727 7272J4 1384006 NM FS 1065 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 288SC 20765 DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON A FLOOR BOARD SUPPORT BEAM AT FS 1065, RBL 28. REMOVED CORROSION , FABRICATED AND INSTALLED A REPAIR IN ACCORDANCE WITH B727 SRM 51-40-4. 2 L 7 3 4F RT A3WE 1996052300271 19960523 00271 NM 1996 5 23 SWAA960389 1 19960516 A 5730 SKIN BOEING 737 7373G7 1384595 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691WN 23781 DURING SCHEDULED 1/4 D-CHECK, FOUND RT WING LOWER SKIN CRACKED JUST I/B OF NUMBER 6 AUX TRACK. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996052300273 19960523 00273 NM 1996 5 23 SWAA960391 1 19960516 A 5320 ANGLE BOEING 737 7373G7 1384595 NM BS 787 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691WN 23781 DURING SCHEDULED 1/4 D-CHECK, FOUND RIGHT TRANSITION ANGLE CRACKED AT BS 787. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996052300274 19960523 00274 NM 1996 5 23 SWAA960392 1 19960515 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 727/747/500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED SV CHECK, FOUND FUSELAGE SKIN CRACKS AT BS 747 LEFT SIDE, AT 727B, 747 AND 500 RIGHT SIDE. REPAIRED PE R BOEING SRM. 2 L 7 2 4F RT A16WE 1996052300275 19960523 00275 NM 1996 5 23 SWAA960393 1 19960514 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 90SW 22905 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT A/C GROUND SERVICING CUTOUT, FWD LT CORNER. REPAIRED PER BOEI NG SRM. 2 L 7 2 4F A16WE 1996052300276 19960523 00276 NM 1996 5 23 SWAA960394 1 19960514 A 3350 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED SC CHECK, FOUND RT FWD SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F A16WE 1996052300277 19960523 00277 NM 1996 5 23 SWAA960395 1 19960516 A 5330 SKIN BOEING 737 7373A4 1384585 NM BS 474 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 474, S22 TO 23L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996052300278 19960523 00278 NM 1996 5 23 SWAA960396 1 19960516 A 5330 SKIN BOEING 737 7373A4 1384585 NM BS 455/500 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 455, S17 TO 18L AND AT BS 500A PLUS 15 BETWEEN S14 AND 15L. R EPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996052300279 19960523 00279 NM 1996 5 23 SWAA960397 1 19960516 A 5320 SHEAR TIE BOEING 737 7373A4 1384585 NM BS 277 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE DAMAGED AT BS 277, BETWEEN S23 AND 24R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996052300280 19960523 00280 NM 1996 5 23 SWAA960398 1 19960516 A 5312 BULKHEAD BOEING 737 7373A4 1384585 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED D-CHECK, FOUND BULKHEAD AT BS 178 CRACKED AT RBL 5.7, WL 193 TO 202, AT LBL 5.7, WL 195 TO 202, AT RBL 10 TO 5.7 AND LBL 5.5, WL 207 TO 214. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996052300281 19960523 00281 NM 1996 5 23 SWAA960399 1 19960516 A 5311 FRAME BOEING 737 7373A4 1384585 NM BS 294 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AROUND GROUNDING WIRES AT BS 294, LBL 56, WL 219. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996052300282 19960523 00282 NM 1996 5 23 SWAA960400 1 19960516 A 5312 BULKHEAD BOEING 737 7373A4 1384585 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AFT SIDE AT RBL 1, WL 189. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996052300283 19960523 00283 NM 1996 5 23 SWAA960401 1 19960516 A 5311 FRAME BOEING 737 7373A4 1384585 NM BS 219 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED D-CHECK, FOUND UPPER SIDE OF FRAME CORRODED AT AFT SIDE OF LOWER NOSE COMPARTMENT, BS 219 WL 165 LBL 7. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996052300284 19960523 00284 NM 1996 5 23 SWAA960402 1 19960516 A 5312 BULKHEAD ANGLE BOEING 737 7373A4 1384585 NM BS 729 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED D-CHECK, FOUND BULKHEAD SUPPORT ANGLE CRACKED AT BS 729, BL 0, WL 164. REPLACED CRACKED SECTION PER BO EING SRM. 2 L 7 2 4F RT A16WE 1996052300285 19960523 00285 NM 1996 5 23 SWAA960403 1 19960516 A 5311 FRAME BOEING 737 7373A4 1384585 NM BS 827 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME DENTED AT BS 827, LBL 32, WL 163. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996052300286 19960523 00286 NM 1996 5 23 SWAA960404 1 19960516 A 5320 SUPPORT BOEING 737 7373A4 1384585 NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CRACKED AT FASTENER HOLE BS 540, LBL 1, WL 208. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996052300287 19960523 00287 NM 1996 5 23 SWAA960405 1 19960516 A 5313 CLIPS BOEING 737 7373A4 1384585 NM BS 663/867 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 663 S10L ,S10R AND AT BS 867 S9L. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996052300288 19960523 00288 NM 1996 5 23 SWAA960406 1 19960511 A 3397 WIRE BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 506SW 24183 FOUND EMERGENCY TRACK LIGHTING AT MID CABIN INOP. REPAIRED WIRING PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996052300289 19960523 00289 NM 1996 5 23 SWAA960407 1 19960511 A 5320 ANGLE BOEING 737 7373A4 1384585 NM BS 767-793 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677SW 23289 DURING 1/4 D-CHECK, FOUND RT TRANSITION ANGLE CORRODED AT BS 767 TO 793. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996052300290 19960523 00290 NM 1996 5 23 SWAA960408 1 19960513 A 5330 SKIN BOEING 737 7372K6 NM BS 727/800 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED SC CHECK, FOUND FUSELAGE SKIN CRACKS AT BS 800, S15R AND AT BS 727B, S17R AND S16L. REPAIRED PER BOEIN G SRM. 2 L 7 2 4F RT A16WE 1996052300291 19960523 00291 NM 1996 5 23 SWAA960409 1 19960513 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE SCRAPED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING WALKAROUND CHECK, FOUND SCRAPED AREA ON LOWER FUSELAGE SKIN NEAR MAIN OUTFLOW VALVE. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996052300292 19960523 00292 NM 1996 5 23 SWAA960410 1 19960516 A 5320 ANGLE BOEING 737 7373Q8 1384670 NM BS 570 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED SV CHECK, FOUND CRACKED SKATE ANGLE AT BS 570, WL 171, LBL 43 TO 60. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996052300293 19960523 00293 NM 1996 5 23 SWAA960411 1 19960516 A 5241 SKIN BOEING 737 7373Q8 1384670 NM GALLEY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED SV CHECK, FOUND FWD GALLEY DOOR UPPER HINGE CUTOUT OUTER SKIN CRACKED AT UPPER OUTER EDGE. REPAIRED PE R SWA ACO 3189-52. 2 L 7 2 4F RT A16WE 1996052300294 19960523 00294 NM 1996 5 23 SWAA960412 1 19960516 A 5311 FRAME BOEING 737 7373Q8 1384670 NM BS 727 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED SV CHECK, FOUND FUSELAGE FRAME DENTED AT BS 727E, S25R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996052300295 19960523 00295 NM 1996 5 23 SWAA960413 1 19960516 A 5320 WEB BOEING 737 7373Q8 1384670 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED SV CHECK, FOUND WEB CRACKED AT BS 178, BL 0, WL 188.1. REPAIRED PER TRAMCO EWO 96-0228. 2 L 7 2 4F RT A16WE 1996052300296 19960523 00296 NM 1996 5 23 SWAA960414 1 19960516 A 5320 STIFFENER BOEING 737 7373Q8 1384670 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED SV CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 178, LBL 5.5, WL 184. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996052300297 19960523 00297 NM 1996 5 23 SWAA960415 1 19960516 A 5311 FRAME BOEING 737 7373Q8 1384670 NM BS 492 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED SV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 492, RBL 36, WL 162. REPAIRED PER TRAMCO EWO 96-0229. 2 L 7 2 4F RT A16WE 1996052300298 19960523 00298 NM 1996 5 23 SWAA960416 1 19960516 A 5330 SKIN BOEING 737 7373Q8 1384670 NM BS 807 CREASE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED SV CHECK, FOUND FUSELAGE SKIN CREASE AT BS 807, BL 0, WL 148. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996052300299 19960523 00299 NM 1996 5 23 SWAA960417 1 19960516 A 5240 DOOR FRAME BOEING 737 7373Q8 1384670 NM FWD SERV CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED SV CHECK, FOUND FWD SERV DOOR, LWR FWD FRAME CRACKED AT BS 295, RBL 56, WL 209. REPLACED FRAME PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1996052300300 19960523 00300 NM 1996 5 23 SWAA960418 1 19960516 A 5312 BULKHEAD BRACKET BOEING 737 7373Q8 1384670 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED SV CHECK, FOUND AFT CARGO BULKHEAD SUPPORT BRACKET CRACKED AT BS 727 PLUS 4, BL 0, WL 160. REPAIRED PE R BOEING SRM. 2 L 7 2 4F RT A16WE 1996052300301 19960523 00301 NM 1996 5 23 SWAA960419 1 19960516 A 5330 SKIN BOEING 737 7373Q8 1384670 NM BS 947-957 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED SV CHECK, FOUND FUSELAGE SKIN DENTED FROM BS 947 TO 957, BETWEEN S18 AND 19L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996052300302 19960523 00302 NM 1996 5 23 UPS96220129 1 19960516 A 2750 BEARING BOEING 727 727185C 138406N NM PWA JT8 JT8D7B 52053 NE TE FLAPS FAILED A IPXA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 01 954UP 19827 INSPECTION TYPE: DURING FLAP EXT FROM 5 DEG TO 15 DEG, ONLY O/B T/E FLAPS INDICATED 15 DEG, I/B FLAPS SHOWED 5 DEG. ATT EMPTED AGAIN WITH NO CHANGE. DECLARED AN EMERGENCY AND LANDED UNEVENTFUL AT SDF. FOUND RT ELEPHANT EAR LOCKED UP, PART IALLY REMOVED SAME. REPLACED ELEPHANT EAR FWD BEARING. 2 L 7 3 4F 4 F A3WE E2EA 1996052300303 19960523 00303 NM 1996 5 23 UPS96220132 1 19960516 A 3350 1000679 LIGHT BOEING 727 72725C 138400H NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 947UP 19722 COCKPIT EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY, OP CHECKS GOOD (P/N 10-0067-9), OFF (S/N 19703), ON (S/N 26798) . 2 L 7 3 4F A3WE 1996052300305 19960523 00305 NM 1996 5 23 UPS96420133 1 19960518 A 3350 60B5003737 LIGHT BOEING 747 747SR46 NM L1 DOOR INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 689UP 21033 FWD EMERGENCY EXIT LIGHT INOP L1 DOOR FRAME L1853. REPLACED MODULE 415. 2 L 7 4 4F A20WE 1996052300306 19960523 00306 1996 5 23 UPS96820120 4 19960418 A 2565 51561004 SLIDE DOUG DC8 DC871F 302199D WP MAIN ENTRY LOW PRESSURE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 702UP 45902 FWD ENTRY DOOR SLIDE HAS LOW PRESSURE. REPLACED ESCAPE SLIDE ASSY PER MM 25-62-00. 2 L 7 4 4F RT 4A25 1996052300307 19960523 00307 WP 1996 5 23 UPS96820121 1 19960418 A 5720 DOUBLER DOUG DC8 DC873F 302199F WP RT WING TE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 RT WING O/B WEDGE CORROSION DAMAGE ON LWR INNER SKIN DOUBLER. REPLACED DOUBLER PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1996052300308 19960523 00308 WP 1996 5 23 UPS96820122 1 19960420 A 5313 577981211 LONGERON DOUG DC8 DC873F 302199F WP FS 460 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 MODERATE TO HEAVY CORROSION IN LONGERON 31L FWD SIDE AT FS 460. REPAIRED PER EO DC8-53-1622. 2 L 7 4 4F RT 4A25 1996052300309 19960523 00309 WP 1996 5 23 UPS96820123 1 19960422 A 5320 5979914 DOUBLER DOUG DC8 DC873F 302199F WP FS 1340-1360 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 MODERATE CORROSION ON LONGERON 31L FS 1340 TO 1360 AT DOUBLER. FABRICATED AND REPLACED DOUBLER PER SRM 51-1-21D. 2 L 7 4 4F RT 4A25 1996052300310 19960523 00310 WP 1996 5 23 UPS96820124 1 19960422 A 5311 3614944 BELT FRAME DOUG DC8 DC873F 302199F WP FS 1460 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 FS 1460 LONGERON 31L TTO 34R BELT FRAME HAS HEAVY CORROSION. REPAIRED FRAME PER SRM 53-2-0. 2 L 7 4 4F RT 4A25 1996052300311 19960523 00311 WP 1996 5 23 UPS96820125 1 19960422 A 5311 FRAME DOUG DC8 DC873F 302199F WP FS 1340 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 UPPER SURFACE OF LOWER FLANGE OF BELT FRAME HAS CORROSION OUT OF LIMITS AT STA 1340 LONGERON 36. REPAIRED FRAME PER SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1996052300312 19960523 00312 WP 1996 5 23 UPS96820126 1 19960422 A 5320 9754924IN DOUBLER DOUG DC8 DC873F 302199F WP FS 1120-1100 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 HEAVY CORROSION ON DOUBLER FS 1120 TO 1100 LONGERON 35L TO 34L. REPLACED DOUBLER PER SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 1996052300313 19960523 00313 WP 1996 5 23 UPS96820127 1 19960428 A 5320 3755845IN FITTING DOUG DC8 DC873F 302199F WP FS 1200 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 HEAVY CORROSION ON B/T FITTING FS 1200 LONGERON 34L AND 33L. REPLACED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996052300314 19960523 00314 WP 1996 5 23 UPS96820128 1 19960428 A 5320 37558452N FITTING DOUG DC8 DC873F 302199F WP FS 1180 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 HEAVY CORROSION ON B/T FITTING 1180 LONGERON 33L AND 34L. REPLACED FITTING PER SRM 53-2-0. 2 L 7 4 4F RT 4A25 1996052300315 19960523 00315 WP 1996 5 23 UPS96820130 1 19960425 A 5230 57542604 DOOR DOUG DC8 DC873F 302199F WP CARGO BAG BIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 CARGO BAG BIN DOOR HAS CRACK ABOUT 3 INCHES AT LWR FWD AREA OF FRAME BETWEEN FITTING AND END BUMPER. REPAIRED PER UPS E O DC8-52-0124. 2 L 7 4 4F RT 4A25 1996052300316 19960523 00316 WP 1996 5 23 UPS96820131 1 19960427 A 5320 4779907 SPLICE DOUG DC8 DC873F 302199F WP FS 1350 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 LONGERON 31L SPLICE CRACK AT FS 1350. REPLACED SPLICE PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996052300317 19960523 00317 WP 1996 5 23 UPS96820134 1 19960517 A 3350 6012235 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 874UP 46074 EMERGENCY LIGHTS FAILED, BATTERY PACK LOW. REMOVED AND REPLACED EMERGENCY LIGHTS BATERY PACK PER M/M 33-50. 2 L 7 4 4F RT 4A25 1996052300318 19960523 00318 NM 1996 5 23 96ZZZX2562 1 19960320 A 3340 TAXI LIGHT BOEING 737 7372P6 NM NLG FOD TO ENGINE A A6XA A UNSCHED LANDING C F.O.D. CL CLIMB 1 SO 13 EICLK JAX - FLT 904 - APPROXIMATE V1 SPEED HEARD LOUD POP, THOUGHT IT MIGHT BE A TIRE. LEFT GEAR DOWN AND MADE A GO-AROUND. A FTER LANDING AND BACK AT THE GATE AFTER SHUTTING ENGINES DOWN, DISCOVERED DAMAGE TO NR 1 ENGINE 1ST AND 2ND STAGE FAN. UPON INVESTIGATION, FOUND NR 1 AND NR 2 ENGINES WITH FOD. FOUND TAXI LIGHT HOUSING AND BRACKET HAD SEPARATED FROM NOSE GEAR AND WAS INJECTED BY NR 1 AND NR 2 ENGINES. REPLACED BOTH NR 1 AND NR 2 ENGINES, TAXI LIGHT AND BRACKET ASSY, AND T AXI LIGHT HARNESS. INSPECTED NOSE GEAR AND AIRCRAFT FOR ANY FURTHER DAMAGE. NONE FOUND. AIRCRAFT TT, 35,682.89 HRS. 2 L 7 2 4F RT A16WE 1996052300322 19960523 00322 NM 1996 5 23 96ZZZX2566 1 19960410 A 7160 AIR FILTER PIPER PA60 PA60600 7106001 NM LT ENG INDUC AIR ICED UP A BSYA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 GL 07 222KD 600557181 LEFT ENGINE SURGING F/FLOW AND MANIFOLD PRESSURE ERRATIC. FOUND INDUCTION AIR FILTER COVERED WITH ICE. 1 M 7 2 3O RT A17WE 1996052300323 19960523 00323 NM 1996 5 23 96ZZZX2567 1 19960410 A 7160 AIR FILTER PIPER PA60 PA60600 7106001 NM LT ENG INDUC AIR ICED UP A BSYA O OTHER Y ENGINE STOPPAGE CR CRUISE 1 GL 07 3643D 600835816123 LEFT ENGINE QUIT IN-FLIGHT. FOUND INDUCTION AIR FILTER COVERED WITH ICE. 1 M 7 2 3O RT A17WE 1996052300324 19960523 00324 NM 1996 5 23 96ZZZX2568 1 19960410 A 7160 AIR FILTER PIPER PA60 PA60600 7106001 NM LT ENG INDUC AIR ICED UP A BSYA O OTHER Y ENGINE STOPPAGE CR CRUISE 1 GL 07 6076L 600713796122 LEFT ENGINE QUIT IN-FLIGHT. FOUND INDUCTION AIR FILTER COVERED WITH ICE. 1 M 7 2 3O RT A17WE 1996052300335 19960523 00335 WP 1996 5 23 9610799751 1 19960515 A 3350 BATTERIES DOUG DC9 DC941 302207N WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 751NW 47115 DURING LINE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE ON FIRST CLASS FLOOR TRACK. REPLACED BATTERIES IN BATTERY PACKS. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996052300336 19960523 00336 WP 1996 5 23 9610809865 1 19960517 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 765NC 47718 DURING LINE CHECK, FOUND EMERGENCY EXIT SIGN AT MAIN CABIN DOOR INOPERATIVE. REPLACED BATTERY PACK, POWER SUPPLY, AND L IGHT ASSEMBLY. REPLACED BAD SPLICE TO LIGHT ASSEMBLY. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996052300337 19960523 00337 WP 1996 5 23 9610819308 1 19960516 A 3350 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 311RC 48089 DURING LINE CHECK, FOUND EMERGENCY CEILING LIGHTS IN FIRST CLASS SECTION INOPERATIVE. REPLACED BATTERIES IN PACK B5-24. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996052300338 19960523 00338 WP 1996 5 23 9610829162 1 19960516 A 3350 POWER SUPPLY DOUG DC9 DC914 3022034 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8907E 45748 DURING LINE CHECK, FOUND AFT SECTION OF DISCO LIGHTS INOPERATIVE. REPLACED POWER SUPPLIES AND BATTERIES. OPERATIONAL C HECK OK. 2 L 7 2 4F A6WE 1996052300339 19960523 00339 1996 5 23 9610839106 4 19960516 A 3442 RADAR TR UNIT DOUG DC9 DC915 3022036 WP FWD FUSELAGE MALFUNCTIONED A NWAA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 01 96S 47206 WEATHER RADAR WORKED OK ON GROUND, BUT WOULD NOT PAINT ANYTHING IN FLIGHT. DUE TO WEATHER EN ROUTE, FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED RADAR TRANSCEIVER, ANTENNA, AND NR 1 VERTICAL GYRO. SYSTEMS TESTED OK. 2 L 7 2 4F A6WE 1996052300340 19960523 00340 NE 1996 5 23 9610843204 2 19960516 A 7532 FLEX SHAFT AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE NR 2 ENGINE WORN A NWAA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 GL 01 304US 040 731304 DURING CLIMB, THE NR 1 ENGINE EGT REACHED 892 DEGREES CELSIUS. RETARDED THRUST, EGT DECREASED, BUT WAS STILL 50 DEGREES CELSIUS GREATER THAN NR 2 ENGINE. RETURNED TO MSP AND LANDED WITHOUT FURTHER EVENT. GROUND MAINTENANCE INSPECTED ENGI NE AND FOUND LOWER VARIABLE BLEED VALVE FLEX DRIVE SHAFT END WORN. REPLACED FLEX SHAFT, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A28NM E29NE 1996052300341 19960523 00341 WP 1996 5 23 9610859941 1 19960518 A 2820 FUEL SYST DOUG DC9 DC932 3022066 WP LT WING LEAKING A NWAA A UNSCHED LANDING K FLUID LOSS UK UNKNOWN 1 GL 01 3324L 47103 FUEL BEGAN LEAKING FROM THE LEFT WING AFTER TAKEOFF. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE FO UND 92,000 POUNDS OF FUEL IN LEFT WING TANK (WHICH WAS VERY CLOSE TO CAPACITY). IT IS SUSPECTED THAT THE FUEL EXPANDED WITH HEAT AND DRIPPED OUT OF THE VENT BOX. NO LEAKS WERE NOTED ON GROUND. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996052300342 19960523 00342 WP 1996 5 23 9610869998 1 19960518 A 3230 RETRACT MECH DOUG DC9 DC931 3022065 WP NLG MALFUNCTIONED A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 8934E 47143 NOSE LANDING GEAR FAILED TO EXTEND DURING APPROACH INTO MSP. EMERGENCY GEAR EXTENSION PROCEDURES WERE UTILIZED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR RETRACT AND EXTEND IN-LINE RESTRICTORS. ADJUSTM ENT WAS ALSO MADE TO NOSE GEAR DOOR. CYCLED GEAR SEVERAL TIMES. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVIC E. 2 L 7 2 4F A6WE 1996052300343 19960523 00343 1996 5 23 9610871220 4 19960518 A 3442 20704090101 ANTENNA DOUG DC10 DC1030 3023501 WP FWD FUSELAGE FAILED A NWAA A J UNSCHED LANDING DUMP FUEL O OTHER CR CRUISE 1 GL 01 220NW 36141 11768 46577 DURING CRUISE, BOTH WEATHER RADARS BECAME INOPERATIVE DUE THE WEATHER EN ROUTE. FLIGHT DIVERTED TO NRT AND DUMPED 22,00 0 POUNDS OF FUEL. MAINTENANCE REPLACED THE WEATHER RADAR ANTENNA. 2 L 7 3 4F A22WE 1996052300344 19960523 00344 WP 1996 5 23 9610889993 1 19960519 A 3260 SWITCH DOUG DC9 DC931 3022065 WP NLG DOWNLOCK MALFUNCTIONED A NWAA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 01 8986E 47402 NOSE LANGING GEAR GREEN DOWNLOCK LIGHT DID NOT ILLUMINATE ON GEAR EXTENSION. RED UNSAFE LIGHT WAS ALSO EXTINGUISHED. C REW VISUALLY CONFIRMED THROUGH PERISCOPE THAT GEAR WAS DOWN AND LOCKED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSE GEAR DOWNLOCK SWITCH. OPERATIONAL CHECK NORMAL ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996052300345 19960523 00345 WP 1996 5 23 9610899943 1 19960519 A 2613 TEMP SENSORS DOUG DC9 DC931 3022065 WP TAIL COMPT MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 1308T 47315 TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED DURING CLIMB-OUT. FLIGHT RETURNED TO IND AND LANDED WITHOUT INCIDEN T. MAINTENANCE REPLACED BOTH TEMPERATURE SENSORS. LEAK AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996052300346 19960523 00346 WP 1996 5 23 9610909943 1 19960517 A 2613 TEMP SENSOR DOUG DC9 DC931 3022065 WP TAIL COMPT MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 1308T 47315 TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED DURING CLIMB-OUT. FLIGHT RETURNED TO DFW AND LANDED WITHOUT INCIDEN T. MAINTENANCE REPLACED THE RIGHT TEMPERATURE SENSOR. LEAK CHECK WAS PERFORMED ON ALL PNEUMATIC DUCTING IN THE TAIL CO MPARTMENT. NO LEAKS WERE FOUND. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996052300347 19960523 00347 WP 1996 5 23 9610919862 1 19960418 A 5312 BULKHEAD FORMER DOUG DC9 DC951 3022051 WP AFT PRESS BLKHD CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 771NC 47769 DURING H-CHECK, FOUND A .50 INCH CRACK IN THE AFT PRESSURE BULKHEAD HORIZONTAL FORMER AT Z=14. REPAIRED FORMER (P/N 991 5558-27) PER EA 98-108866. 2 L 7 2 4F A6WE 1996052300348 19960523 00348 WP 1996 5 23 9610929763 1 19960419 A 5311 FRAME DOUG DC9 DC941 302207N WP FS 1072 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 763NW 47396 DURING H-CHECK, FOUND CORROSION ON THE FS 1072 FRAME AT THE LEFT CUSP ANGLE. REPAIRED FRAME (P/N 5910163-73) PER EA 97- 108880. 2 L 7 2 4F A6WE 1996052300349 19960523 00349 WP 1996 5 23 9610939968 1 19960430 A 5312 PRESS DOME T CAP DOUG DC9 DC931 3022065 WP FS 604 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9332 47264 DURING H-CHECK, FOUND CORROSION ON THE PRESSURE DOME T-CAP AT FS 604, LONGERON 30. REPAIRED T-CAP (P/N 5914865-29) PER EA 99-109435. 2 L 7 2 4F A6WE 1996052300350 19960523 00350 WP 1996 5 23 9610949968 1 19960430 A 5330 SKIN DOUG DC9 DC931 3022065 WP FS 676 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9332 47264 DURING H-CHECK, FOUND CORROSION ON THE UNDER WING KEEL SKIN FS 676. REPAIRED SKIN (P/N 5911418-9) PER EA 99-109434. 2 L 7 2 4F A6WE 1996052300351 19960523 00351 WP 1996 5 23 9610959968 1 19960430 A 5313 LONGERON DOUG DC9 DC931 3022065 WP FS 606 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9332 47264 DURING H-CHECK, FOUND A CRACK IN THE LONGERON 30 KEEL CAP AT FS 606. REPAIRED CAP (P/N 9915525-509) PER EA 99-108990. 2 L 7 2 4F A6WE 1996052300352 19960523 00352 NM 1996 5 23 9610962295 1 19960430 A 2782 ACTUATOR FITTING BOEING 727 727251 138408H NM NR 4 LE FLAP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 295US 21506 DURING H-CHECK, FOUND A CRACK AND CORROSION IN THE RIGHT WING NR 4 LEADING EDGE FLAP ACTUATOR FITTING. REPLACED FLAP (P /N 65-16225-6A) PER MM 27-81-01. 2 L 7 3 4F A3WE 1996052300353 19960523 00353 WP 1996 5 23 9610979968 1 19960501 A 5713 LONGERON DOUG DC9 DC931 3022065 WP WS 164 BROKEN TAB A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9332 47264 DURING H-CHECK, FOUND A 1.25 INCH BY .75 INCH TAB BROKEN OFF THE LEFT WING TRAILING EDGE STR 28L AT WS 164. REPAIRED ST RINGER (P/N 5912156-39) PER EA 99-109002. 2 L 7 2 4F A6WE 1996052300354 19960523 00354 WP 1996 5 23 9610989906 1 19960508 A 5343 FITTING DOUG DC9 DC931 3022065 WP FS 756 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 956N 47252 DURING H-CHECK, FOUND CORROSION IN THE RIGHT MAIN LANDING GEAR WHEELWELL INBOARD AND OUTBOARD KEEL FITTINGS FS 756. REP LACED FITTINGS PER SRM 51-30-2, SRM 51-30-5. 2 L 7 2 4F A6WE 1996052300355 19960523 00355 NM 1996 5 23 9610996627 1 19960509 A 5320 SILL BOEING 747 747251B 1384892 NM FS 2280 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 627US 21709 DURING P-CHECK, FOUND CORROSION ON THE 5L DOOR LOWER SILL BS 2280. REPAIRED SILL (P/N 65B04423-1) PER EA 66-101923. 2 L 7 4 4F A20WE 1996052300356 19960523 00356 WP 1996 5 23 9611001145 1 19960511 A 5313 LONGERON DOUG DC10 DC1040 3023508 WP FS 1652 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 145US 46754 DURING T-CHECK, FOUND CORROSION ON LONGERON 52 AT FS 1652. REPAIRED LONGERON (P/N AFA 7078-1) PER EA 11-104261. 2 L 7 3 4F A22WE 1996052300357 19960523 00357 WP 1996 5 23 9611019876 1 19960512 A 5320 FITTINGS DOUG DC9 DC951 3022051 WP FS 1167 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 785NC 48110 DURING H-CHECK, FOUND CRACKS IN THREE AFT ENTRY DOOR STOP FITTINGS FS 1167, LOWER RIGHT, LOWER LEFT, AND CENTER LEFT. R EPLACED FITTINGS PER SRM 51-30-2 AND SRM 51-30-5. 2 L 7 2 4F A6WE 1996052300358 19960523 00358 WP 1996 5 23 9611029876 1 19960513 A 5230 FITTING DOUG DC9 DC951 3022051 WP CARGO DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 785NC 48110 DURING H-CHECK, FOUND CRACKS IN THREE AFT CARGO DOOR INTERNAL STOP FITTINGS AT THE FORWARD SIDE. REPLACED FITTINGS. 2 L 7 2 4F A6WE 1996052300359 19960523 00359 WP 1996 5 23 9611031145 1 19960513 A 5313 LONGERON DOUG DC10 DC1040 3023508 WP FS 1690 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 145US 46754 DURING T-CHECK, FOUND CORROSION ON LONGERON 45R AT FS 1690. REPAIRED LONGERON (P/N AFA 7097-1) PER EA 11-104262. 2 L 7 3 4F A22WE 1996052300360 19960523 00360 WP 1996 5 23 9611049973 1 19960514 A 5744 HINGE FITTING DOUG DC9 DC931 3022065 WP NR 2 TE FLAP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9337 47346 DURING M-CHECK, FOUND CORROSION ON THE LEFT WING UPPER OUTBOARD NR 2 FLAP FORWARD HINGE FITTING. REPLACED FITTING (P/N 5919218-505) PER CITEXT 09-5740-1-9800. 2 L 7 2 4F A6WE 1996052300361 19960523 00361 WP 1996 5 23 9611059940 1 19960514 A 5311 FRAME DOUG DC9 DC932 3022066 WP FS 612 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3322L 47031 DURING M-CHECK, FOUND A CRACK IN THE FS 612 FRAME ATTACH FITTING AT LONGERON 17L. REPLACED FITTING PER SRM 51-10-2. 2 L 7 2 4F A6WE 1996052300362 19960523 00362 WP 1996 5 23 9611061145 1 19960514 A 5320 WEB DOUG DC10 DC1040 3023508 WP FS 481-496 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 145US 46754 DURING T-CHECK, FOUND A CRACK IN THE RIGHT NOSE LANDING GEAR WHEELWELL WEB FS 481 - FS 496, WATER LINE -60 TO -70. REPA IRED WEB (P/N NCA 6246-28) PER EA 11-104263. 2 L 7 3 4F A22WE 1996052300363 19960523 00363 WP 1996 5 23 9611079918 1 19960515 A 5320 FITTING DOUG DC9 DC932 3022066 WP FS 996 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 940N 47572 DURING M-CHECK, FOUND CORROSION ON THE FS 996 FRAME TO FLOOR SUPPORT FITTING BETWEEN LONGERONS 17R - 19R. REPLACED FITT ING (P/N 5931700-2) PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996052300364 19960523 00364 WP 1996 5 23 9611089973 1 19960516 A 5230 FITTING DOUG DC9 DC931 3022065 WP CARGO DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9337 47346 DURING M-CHECK, FOUND A CRACK IN THE AFT CARGO DOOR FORWARD UPPER END FITTING. REPLACED FITTING PER SRM 51-30. 2 L 7 2 4F A6WE 1996052300365 19960523 00365 WP 1996 5 23 9611099973 1 19960516 A 5320 FITTING DOUG DC9 DC931 3022065 WP FS 585 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9337 47346 DURING M-CHECK, FOUND A CRACK IN THE LONGERON 24L FITTING AT FS 585. REPLACED FITTING PER SRM 51-30-5, SRM 51-30-2. 2 L 7 2 4F A6WE 1996052300366 19960523 00366 WP 1996 5 23 9611109876 1 19960516 A 5320 FITTING DOUG DC9 DC951 3022051 WP FS 664-693 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 785NC 48110 DURING H-CHECK, FOUND CORROSION IN THE LONGERON 30 END FITTING AT FS 664 - FS 693. REPLACED FITTING PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996052300367 19960523 00367 WP 1996 5 23 9611119938 1 19960519 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN MALFUNCTIONED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 1798U 47369 DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. OPERATIONAL CHE CK NORMAL. 2 L 7 2 4F A6WE 1996052300368 19960523 00368 WP 1996 5 23 9611129938 1 19960517 A 3350 60030451 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 1798U 47369 DURING LINE MAINTENANCE INSPECTION, FOUND TWO OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONA L CHECK NORMAL. 2 L 7 2 4F A6WE 1996052300369 19960523 00369 WP 1996 5 23 9611139955 1 19960518 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 922RW 47182 DURING LINE MAINTENANCE INSPECTION, FOUND PROXIMITY EMERGENCY LIGHTS AT AFT RIGHT EMERGENCY EXIT AND ROWS 12 THROUGH 15 INOPERATIVE. REPLACED BATTERIES. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996052300370 19960523 00370 WP 1996 5 23 9611149969 1 19960519 A 3350 FUSE DOUG DC9 DC931 3022065 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9333 47246 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE. O PERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996052300371 19960523 00371 WP 1996 5 23 9611159960 1 19960516 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 920RW 47163 DURING LINE MAINTENANCE INSPECTION, FOUND AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERIES. OPERATION AL CHECK NORMAL. 2 L 7 2 4F A6WE 1996052300372 19960523 00372 WP 1996 5 23 9611169979 1 19960516 A 3350 FUSE DOUG DC9 DC931 3022065 WP CABIN BLOWN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9343 47439 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996052300373 19960523 00373 NM 1996 5 23 9611176628 1 19960517 A 5744 FITTING BOEING 747 747251B 1384892 NM RT WING CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 628US 22389 DURING P-CHECK, FOUND CORROSION IN THE RIGHT WING INBOARD FLAP, NR 6 FORWARD FITTING BORE. REPLACED THE FITTING ASSEMBL Y PER EO 5753-01098. 2 L 7 4 4F A20WE 1996052300374 19960523 00374 WP 1996 5 23 9611189983 1 19960517 A 5320 FITTING DOUG DC9 DC932 3022066 WP FS 996 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 983US 47282 DURING M-CHECK, FOUND CORROSION ON THE FS 996 FLOOR SUPPORT, WEB, UPPER ANGLE, AND CORNER FITTING AT LBL 48. REPLACED T HE SAME PER SRM 51-30-2 AND SRM 51-30-5. 2 L 7 2 4F A6WE 1996052300375 19960523 00375 NM 1996 5 23 9611192201 1 19960518 A 5320 FITTING BOEING 727 727251 138408H NM FS 1183 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 201US 22154 DURING H-CHECK, FOUND CORROSION ON THE STR 29L TENSION TIE FITTING BS 1183. REPLACED FITTING (P/N 22-5300-3-0246) PER S RM 51-10-01. 2 L 7 3 4F A3WE 1996052300376 19960523 00376 WP 1996 5 23 9611209876 1 19960519 A 5210 FITTING DOUG DC9 DC951 3022051 WP PAX DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 785NC 48110 DURING H-CHECK, FOUND A .50 INCH CRACK IN THE AFT ENTRY DOOR UPPER BEAM END FITTING, LEFT SIDE. REPLACED FITTING PER DW G 9929480. 2 L 7 2 4F A6WE 1996052300377 19960523 00377 NM 1996 5 23 96FDEA00986 1 19960517 A 5330 SKIN BOEING 727 727225 1384077 NM BS 378 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 468FE 21452 GOUGE IN SKIN AT BS 378 BETWEEN STRS 17-18L, LBL 70. CUT OUT DAMAGED SKIN AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 1. 2 L 7 3 4F A3WE 1996052300378 19960523 00378 NM 1996 5 23 96FDEA00987 1 19960517 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 540 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 GOUGES IN STRINGER AT BS 540, STR 7R. REPAIRED, OUT OF LIMITS, STR 7R, BS 540 IAW FEDEX SRM 53-10-3. 2 L 7 3 4F A3WE 1996052300379 19960523 00379 NM 1996 5 23 96FDEA00988 1 19960517 A 5330 SKIN BOEING 727 727227 1384078 NM BS 400-510 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 GOUGES AND PITS ON EXTERIOR OF SKIN BS 400-BS 510, STR 26R - BL ZERO. REPAIRED DAMAGED SKIN THAT WAS OUT OF LIMITS IAW FEDEX SRM 53-30-3. 2 L 7 3 4F A3WE 1996052300380 19960523 00380 NM 1996 5 23 96FDEA00989 1 19960517 A 5330 SKIN BOEING 727 72725 1384006 NM BS 334-352 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 505FE 18276 CORROSION C53-100-01 SKIN AND DOUBLER BULGING BS 334 - BS 352, LBL 21 - LBL 26, WL 145. REMOVED FASTENERS FROM SKIN, FO UND NO CORROSION UNDER SKIN OR DOUBLER. FABRICATED DOUBLER AND INSTALLED, AND INSTALLED ALL FASTENERS IAW SRM 53-30-03. 2 L 7 3 4F A3WE 1996052300381 19960523 00381 NM 1996 5 23 96FDEA00990 1 19960517 A 5320 65C8067862 BRACKET BOEING 727 72725 1384006 NM BS 228 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 CORROSION C53-10-01(1) AROUND UPPER FASTENERS ON FORGING BS 228, LBL 6 - LBL 13, WL 184. REMOVED AND REPLACED FORGING B RACKET AT BS 228, LBL 6 - LBL 13, WL 184. 2 L 7 3 4F A3WE 1996052300382 19960523 00382 NM 1996 5 23 96FDEA00991 1 19960517 A 5312 6517508224 BLKHD STIFFENER BOEING 727 72725 1384006 NM BS 1342 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 S-DUCT OPENING CIRCUMFERENTIAL STRAP AND STIFFENER ON 1342 BULKHEAD RT SIDE, WL 180 - WL 270, RBL 15.5 IS CORRODED. REM OVED AND REPLACED CIRCUMFERENTIAL STRAP AND STIFFENER ON BS 1342, RBL 15.5, WL 180 - WL 270. (STIFFENER P/N 69154056) . 2 L 7 3 4F A3WE 1996052300383 19960523 00383 NM 1996 5 23 96FDEA00993 1 19960517 A 5311 FRAME BOEING 727 727227 1384078 NM BS 720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 CORROSION C53-224-01(1) ON FRAME AT BS 720C, STR 17R - STR 10R. REPAIRED FRAME STA 720C, STR 17R - STR 10R OUT OF LIMIT AREA IAW FEDEX SRM 53-10-4. 2 L 7 3 4F A3WE 1996052300384 19960523 00384 NM 1996 5 23 96FDEA00994 1 19960517 A 5313 BAC1498145 STRINGER BOEING 727 727227 1384078 NM BS 1060 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 NR0925 AND 028, CORROSION (C53-111-01, -3) ON STR 28L BETWEEN SKIN AND STRINGER BS 1060. *S/D* BS 1060 STR 28 LEFT REP AIRED CORRODED STRINGER PER FEDEX SRM 53-10-3. 2 L 7 3 4F A3WE 1996052300385 19960523 00385 NM 1996 5 23 96FDEA00995 1 19960517 A 5311 FRAME BOEING 727 727227 1384078 NM BS 950 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 NR0373 AND 026, DENTS IN FRAME BS 950F LBL 29 TO 36 WL 148 TO 152. REPAIRED FRAM AT BS 950, LBL 29 TO 36, WL 148 TO 152 , IAW FED EX SRM 51-40-3. 2 L 7 3 4F A3WE 1996052300386 19960523 00386 NM 1996 5 23 96FDEA00996 1 19960517 A 5312 BULKHEAD WEB BOEING 727 727227 1384078 NM BS 1183 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 NR0064 AND 024, MECH DAMAGE TO THE FWD SIDE OF THE 1183 BULKHEAD AT LBL 56 WL 226. REPAIRED BULKHEAD WEB PER SRM 53-10- 9. 2 L 7 3 4F A3WE 1996052300387 19960523 00387 WP 1996 5 23 96FDEA00997 1 19960516 A 5280 HINGE FITTING DOUG DC10 DC1010CF 3023502 WP LT MLG DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68049 47803 SNRM 7009, LT MAIN GEAR DOOR CENTER HINGE ATTACH FITTING, CRACKED, APPROX BELOW DOOR ACT. FABRICATED REPAIR PER SRM 52- 00-00 AND INSTALLED. 2 L 7 3 4F RT A22WE 1996052300388 19960523 00388 WP 1996 5 23 96FDEA00998 1 19960517 A 5713 ARB2541 STRINGER DOUG DC10 DC1030F 3023504 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 304FE 46992 RIGHT WING STR 41 OUTBOARD HOLE HAS VERTICAL CRACK AT 2 O/C POSITION INTO UPPER STR RADIUS APPROX .3125 INCH LONG. REF: EO 8-5710-7-4310. 2 L 7 3 4F RT A22WE 1996052300389 19960523 00389 NM 1996 5 23 96FDEA00999 1 19960517 A 5310 STRUCTURE DOUG MD11 MD11F 3023600 NM AFT FUSELAGE DAMAGED A FDEA K NONE O OTHER LD LANDING 1 SO 25 614FE 48528 HARD LANDING WITH TAIL STRIKE. STRUCTURAL DAMAGE BEING EVALUATED IN ANC BY ENGINEERING AND DAC RAMS TEAM. *S/D* DURIN G MAINTENANCE C-CHECK, A HARD LANDING INSPECTION WAS ACCOMPLISHED. ALSO, DURING THE C-CHECK THE STRUCTURAL DAMAGE CAUSE D AS A RESULT OF HARD LANDING WAS REPAIRED IAW EA 15310-28929. 2 L 7 3 4F RT A22WE 1996052300390 19960523 00390 WP 1996 5 23 96FDEA01000 1 19960520 A 5412 AJC729012 BLKHD STIFFENER DOUG DC10 DC1010CF 3023502 WP NOSE COWL CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68049 47803 SNRM 4259. BULKHEAD STIFFENER CRACKED AT THE NR 2 ENGINE NOSE COWL L/E AS SEEN THROUGH ACCESS PANEL NR 361FL. S/D COMI NG. 2 L 7 3 4F RT A22WE 1996052300391 19960523 00391 WP 1996 5 23 96FDEA01001 1 19960520 A 5400 AJC71735 STIFFENER RING DOUG DC10 DC1010CF 3023502 WP NOSE COWL CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68049 47803 SNRM 4260, CIRCUMFERENTIAL STIFFENER RING CRACKED AT THE NR 2 ENG NOSE COWL L/E AS SEEN THROUGH ACCESS PANEL 361 FL. RE PLACED NOSE COWL LEADING EDGE ASSY IAW MM 54-22-01 WITH LEASED UNIT. DAMAGED NOSE COWL L/E ROUTED TO VENDOR OR SHOP FOR REPAIR (S/N 572826). 2 L 7 3 4F RT A22WE 1996052300392 19960523 00392 NM 1996 5 23 96FDEA01002 1 19960521 A 2933 QTY XMITTER BOEING 727 727233 138408A NM A HYD SYST BROKEN WIRE A FDEA K NONE N FALSE WARNING TO TAKEOFF 1 SO 25 267FE 21673 LOSS OF 'A' QTY DECREASED FROM 5 GAL TO 1.2 GAL, LEAK STOPPED. PRESSURE NORMAL ENTIRE FLIGHT. REPAIRED WIRE AT A-SYSTE M QTY XMTR, VERIFIED QTY AT SYSTEM 'A' TO PROPER LEVEL. NO LEAKS FOUND OR NOTED. 2 L 7 3 4F RT A3WE 1996052300393 19960523 00393 NM 1996 5 23 96FDEA01003 1 19960520 A 3260 ELECT TEST BOX BOEING 747 747245F 1384897 NM LANDING GEAR FAILED A FDEA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 SO 25 638FE 21841 UAM - IND LIGHTS PILOT AND FLIGHT ENGINEER C/B POPPED DURING FLT. INITIAL UNSAFE GEAR IND NO LIGHTS FOR GEAR DOWN, DOOR OPEN, OR GEAR. RESET C/B AND REPLACED 15 LIGHT BULBS. C/B POPPED AND RESET AGAIN AND AGAIN. REPLACED 4 BULBS, GEAR D OWN IND 9 GREEN LIGHTS, GEAR RECYCLED 3 TIMES WITH 2 TOWER FLY-BYS TO CONFIRM POS GEAR DOWN IND. ENTER UAM, DURING T/S FOUND MASTER DIM TEST ELECTRONIC BOX WITH 5 DAMAGED CIRCUIT CARDS, REPLACED MASTER DIM TEST ELECTRONIC BOX AND IND LIGHT S, PILOT AND FE C/B, GROUND TEST GOOD PER MM 33-11-01, ALSO SIMULATED LANDING MODE, EXT FLAPS/SLATS ALL SYS NORMAL, C/N DUP REQUIRES FURTHER EVALUATION BY FLT CREW. 2 L 7 4 4F A20WE 1996052300394 19960523 00394 NM 1996 5 23 96FDEA01004 1 19960520 A 5210 507945216 EDGE BEAM BOEING 727 727227 1384078 NM ENTRY DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 FORWARD ENTRY DOOR AFT SIDE FRAME IS CRACKED AND GOUGED AT UPPER END. REMOVED AND REPLACED FORWARD ENTRY DOOR, AFT SIDE FRAME. 2 L 7 3 4F A3WE 1996052300395 19960523 00395 NM 1996 5 23 96FDEA01005 1 19960520 A 5330 SKIN BOEING 727 727227 1384078 NM BS 1055 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 CORROSION C53-100-01 ON SKIN BS 1055, STR 28L. AT BS 1055 STR 28L, REPAIRED CORRODED SKIN PER FEDEX SRM 53-30-3. 2 L 7 3 4F A3WE 1996052300396 19960523 00396 NM 1996 5 23 96FDEA01006 1 19960520 A 5315 BAC150529222 FLOOR BEAM BOEING 727 727227 1384078 NM BS 344 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 CORROSION C53-224-01 ON 344 BEAM FROM LBL 59 - RBL 37, WL 208.1. REPAIRED BS 344 FLOOR BEAM UPPER CHORD PER FEDEX DRAWI NG SR 27-53-007. 2 L 7 3 4F A3WE 1996052300397 19960523 00397 NM 1996 5 23 96FDEA01007 1 19960520 A 5315 BAC1505100617 FLOOR BEAM BOEING 727 727227 1384078 NM BS 480 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 CORROSION C53-224-01 AND BARE METAL AT BS 480 BEAM FROM LBL 44 - RBL 23, WL 208.1. REPAIRED BS 480 FLOOR BEAM FROM RBL 16 - LBL 17, WL 208 PER FEDEX SRM 53-10-8 AND ALODINED AND PRIMED BARE METAL AREAS. 2 L 7 3 4F A3WE 1996052300398 19960523 00398 NM 1996 5 23 96FDEA01008 1 19960520 A 5313 BAC1498138 STRINGER BOEING 727 72725 1384006 NM BS 414-420 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 505FE 18276 CORROSION ON STR 1, BS 414 - BS 420. COMPLETED REPAIR ON STR 1, BS 414 - BS 420, PER FEDEX SRM 53-10-3. 2 L 7 3 4F A3WE 1996052300399 19960523 00399 NM 1996 5 23 96FDEA01009 1 19960520 A 5330 SKIN BOEING 727 72725 1384006 NM BS 1080-1110 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 505FE 18276 WHILE WORKING NR 0351, FOUND CORROSION IN SKIN LAP BETWEEN BONDED DOUBLER AND LOWER SKIN AT BS 1080 - BS 1110, STR 14L. CUT OUT TO REMOVE CORROSION AND REPAIRED SKIN LAP AT BS 1080 - BS 1110, STR 14L PER FEDEX SRM 53-30-3. 2 L 7 3 4F A3WE 1996052300400 19960523 00400 NM 1996 5 23 96FDEA01010 1 19960520 A 5313 BAC1498145 STRINGER BOEING 727 727227 1384078 NM BS 1060 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 CORROSION C53-111-01(3) ON STR 28L BETWEEN SKIN AND STR, BS AT BS 1060, STR 28L. REPAIRED CORRODED STRINGER PER FEDEX S RM 53-10-3. 2 L 7 3 4F A3WE 1996052300401 19960523 00401 NM 1996 5 23 96UAL900312 1 19960503 A 2782 ACTUATOR 10617927 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 LE FLAP FAILED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 WP 29 7285U DA4413 21563 ABORTED TAKEOFF SJC AT 115 KNOTS DUE TO THE LOSS OF 'A' HYDRAULIC SYSTEM. TOWED TO GATE. SUPPLEMENTAL DATA UPDATE: NR 1 LEADING EDGE SLAT ACTUATOR CRACKED AT HOUSING AFT END. REPLACED NR 1 LEADING EDGE SLAT ACTUATOR. SERVICED 'A' HYDRA ULIC SYSTEM. 2 L 7 3 4F 4 F A3WE E2EA 1996052300402 19960523 00402 NM 1996 5 23 96UAL900352 1 19960517 A 7930 21SN04389A PRESSURE SWITCH BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 1 ENGINE FAILED A UALA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 WP 29 173UA 24380 724628 NR 1 ENGINE OIL FILTER EICAS MESSAGE, ENGINE SHUT DOWN. *S/D* TE OIL FILTER DELTA PRESSURE SWITCH FAILED. REPLACED SW ITCH AND OIL FILTER. 2 L 7 4 4F 4 F RT A20WE E24NE 1996052300403 19960523 00403 NM 1996 5 23 96UAL900353 1 19960517 A 3350 BATTERY PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7451U 21905 EMERGENCY LIGHT AT ROW 21 FAILED TO TEST PER CREW. REPLACED BATTERY PACK AND LIGHT ASSEMBLY. CHECKS OKAY. 2 L 7 3 4F 4 F A3WE E2EA 1996052300404 19960523 00404 NM 1996 5 23 96UAL900354 1 19960517 A 3350 BATTERY PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7279U 21557 EMERGENCY EXIT LIGHT AT FORWARD DROP CEILING ROW 8 INOPERATIVE. REPLACED BATTERY PACK. 2 L 7 3 4F 4 F A3WE E2EA 1996052300405 19960523 00405 NM 1996 5 23 96UAL900355 1 19960517 A 2910 HYD LINE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE VERT STAB CHAFED A UALA O OTHER K FLUID LOSS IN INSP/MAINT 1 WP 29 7265U 21412 LOWER RUDDER HYD ACTUATOR LEAKING. *S/D* BROKEN HYDRAULIC LINE STANDOFF AND HYDRAULIC LINE CHAFED THROUGH AT VERTICAL STABILIZER RIGHT SIDE ABOVE RUDDER ACTUATOR. INSTALLED SERVICEABLE HYDRAULIC LINE AND STANDOFF. 2 L 7 3 4F 4 F A3WE E2EA 1996052300406 19960523 00406 NE 1996 5 23 96UAL900356 2 19960517 A 7230 739483 BEARING BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 7253U 23521 9038 21400 700268 NR 3 ENGINE OIL FILTER BYPASS LIGHT CAME ON IN CLIMB. REDUCED POWER AND LIGHT STAYED ON. OIL PRESSURE AND TEMPERATURE NORMAL. RETURNED TO SFO. *S/D* THE NR 3 BEARING CAGE FAILURE WAS DUE TO A FRACTURE AT THE CAGE RIVET HOLE CAUSED BY E XCESSIVE BALL SOCKET WEAR AND RESULTANT ABNORMAL BALL MOVEMENT. A NEW REQUIREMENT TO ROUTE THE NR 3 BEARING FOR OVERHAU L WHENEVER THE HOT SECTION IS REMOVED HAS SIGNIFICANTLY REDUCED NR 3 BEARING FAILURES. 2 L 7 3 4F 4 F A3WE E2EA 1996052300407 19960523 00407 NM 1996 5 23 96UAL900357 1 19960517 A 2781 834403 SENSOR BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LE FLAP DAMAGED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 605UA 21866 LEADING EDGE FLAP ASYMMETRY DISPLAYED UPON SLAT RETRACTION, SLATS LOCKED OUT. AIRCRAFT RETURNED TO FIELD. *S/D* A FAU LTY SLAT PROXIMITY SENSOR CAUSED THIS DISCREPANCY. REPLACED PROXIMITY SENSOR, OPERATIONS CHECK NORMAL. PERFORMED PSEU BITE CHECK, FOUND NO FAULTS. 2 L 7 2 4F 4 F RT A1NM E3NE 1996052300408 19960523 00408 NM 1996 5 23 96UAL900358 1 19960517 A 2781 INDICATION BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LE FLAPS MALFUNCTIONED A UALA O OTHER N FALSE WARNING CL CLIMB 1 WP 29 606UA 21867 LEADING EDGE SLAT INDICATION MESSAGE OCCURRED DURING FLAP RETRACTION. SUPPLEMENTAL DATA UPDATE: PERFORMED PSEU BITE TE ST AND OPERATED FLAPS. FOUND NO FAULTS PERTAINING TO LEADING EDGE SLATS. SYSTEM GROUND CHECKS NORMAL. NO PARTS WERE R EMOVED FROM AIRCRAFT. THE DISCREPANCY WAS MOST LIKELY THE RESULT OF A FAULTY INDICATION MESSAGE. 2 L 7 2 4F 4 F RT A1NM E3NE 1996052300409 19960523 00409 NM 1996 5 23 96UAL900359 1 19960517 A 2780 CIRCUIT BREAKER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LE FLAPS TRIPPED A UALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 771UA 26932 RETURNED TO BLOCKS, DUE TO A FLAP DISAGREEMENT PROBLEM. *S/D* RESET 'FLAPS ELEC MOT PWR' CIRCUIT BREAKER (C27301) AND 'SLATS ELEC MOT PWR' CIRCUIT BREAKER (C27300). 2 L 7 2 4F 4 F RT T0001SE E46NE 1996052300410 19960523 00410 NM 1996 5 23 96UAL900360 1 19960520 A 2781 834403 SENSOR BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LE FLAP DIRTY A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 608UA 21869 AIRCRAFT RETURNED TO FIELD DUE TO SLAT INDICATION PROBLEM. *S/D* GREASE AND GRIME ON SLAT NR 5 PROXIMITY SENSOR, S280 C AUSED THE FALSE INDICATION. THE SENSOR WAS CLEANED AND ADJUSTED, ACCOMPLISHED TARGET AND SENSOR BITE TEST AND FOUND NO DISCREPANCIES. OPERATED FLAPS SEVERAL TIMES AND PERFORMED BITE TEST OF FSEU, FOUND NO FAULTS. GROUND CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 1996052300411 19960523 00411 SO 1996 5 23 COMA9610149 1 19960518 A 5610 12041591001 WINDOW EMB 120 EMB120RT SO LT COCKPIT AIR LEAK A COMA K NONE O OTHER AP APPROACH 1 SO 01 1110J 18697 120110 CABIN WILL NOT HOLD PRESSURIZATION. ADJUSTED AND RESEALED PILOT'S DIRECT VISION WINDOW. 2 L 7 2 4T RT A31SO 1996052300412 19960523 00412 1996 5 23 COMA9610150 4 19960520 A 3442 RADAR EMB 120 EMB120RT SO COCKPIT MALFUNCTIONED A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 244CA 120217 RADAR DISPLAY IS ERRATIC AND ERRONEOUS. PLACED WEATHER RADAR SYSTEM ON DEFERRED MAINTENANCE LIST. ACFT RETURNED TO SER VICE. 2 L 7 2 4T RT A31SO 1996052300413 19960523 00413 NE 1996 5 23 COMA9630110 2 19960519 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RIGHT FAILED A COMA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 158CA 340A158 367262 RIGHT ENGINE FAILED DURING TAKEOFF. REPLACED RIGHT ENGINE. 2 L 7 2 4T 4 T RT A52EU E8NE6 1996052300414 19960523 00414 GL 1996 5 23 SWIA95739 3 19960519 A 6110 P65253220307 PROPELLER SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP HARTZL HCB3T HCB3TN5 GL RT ENGINE MALFUNCTIONED A SWIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 2698C AC665 HAD SMOKE IN CABIN AND COCKPIT SHORTLY AFTER TAKEOFF. COULD NOT ISOLATE. RETURNED TO SAN. REPLACED RIGHT ENGINE PROPE LLER ASSEMBLY. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C P15EA 1996052300415 19960523 00415 SO 1996 5 23 SWIA95740 1 19960518 A 3230 RETRACT MECH EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LANDING GEAR MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 204SW 120243 LANDING GEAR WILL NOT COME UP. JACKED AIRCRAFT. GEAR CAME UP ON FIRST ATTEMPT. SWUNG GEAR SEVERAL TIMES, COULD NOT DU PLICATE PROBLEM. INSPECTED ALL 'A' AND 'B' SYSTEMS UP CANNON PLUGS FOR CLEANLINESS. FOUND GOOD. SWUNG GEAR SEVERAL MO RE TIMES. ALL CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1996052300416 19960523 00416 SO 1996 5 23 SWIA95741 1 19960515 A 3150 7002743 ALARM CONTL EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT ENGINE MALFUNCTIONED A SWIA E ENGINE SHUTDOWN O OTHER AP APPROACH 1 NM 07 186SW 120034 LT ENGINE DUCT LEAK LIGHT REMAINS ON. SHUT DOWN AND CALLED SGU MX CONTROL. REMOVED AND REPLACED ALARM LIGHT CONTROLLER WITH SERVICEABLE UNIT. RAN LT ENGINE EXTENSIVELY FOR 15 MINUTES. OPS CHECK GOOD ON GROUND AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 1996052300417 19960523 00417 EA 1996 5 23 SWIA95742 1 19960512 A 3260 864806 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LANDING GEAR MALFUNCTIONED A SWIA A L UNSCHED LANDING ABORTED APPROACH N FALSE WARNING CL CLIMB 1 NM 07 407SW 7034 STANDBY PITOT HEAT PRESS CAME ON DURING INITIAL CLIMB FOLLOWED BY A PROX SYSTEM FAULT ABOUT FIVE MINUTES LATER AND CHIME S SOUNDING (CABIN/COCKPIT) AT RANDOM. RETURNED TO SLC, HAD TO DO A MANUAL GEAR EXTENSION BECAUSE OF THREE RED INDICATIO NS ON GEAR AND NORMAL EXTENSION WOULD NOT WORK. THREE GREEN AFTER MANUAL EMERGENCY EXTENSION PLUS ANTI-SKID MESSAGE AND STEERING INOPERATIVE. FLY-BY, TOWER TO VERIFY THREE DOWN AND LOCKED. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED P SEU IAW CRJ M/M 52-61-00. PERFORMED GEAR SWING AND CHECKS OF OTHER EFFECTED SYSTEMS. ALL CHECKED GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 1996052300418 19960523 00418 NM 1996 5 23 UPS96220138 1 19960507 A 5315 FLOORBEAM BOEING 727 72727C 138400J NM BS 340 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE: D. MAIN CABIN AT STA 340, LBL 20 TO RBL 25, FLOOR BEAM UPPER FLANGE ANGLE AND SPLICE ANGLE HAVE HEAVY CORROSION THROUGHOUT. CUT OUT DAMAGE AREA PER SPM 53-10-8 AND REPLACED FLOOR BEAM UPPER ANGLE AND SPLICE ANGLE IAW 53- 10-8. 2 L 7 3 4F A3WE 1996052300419 19960523 00419 NM 1996 5 23 UPS96220139 1 19960422 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 1030 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE: D. STA 1030 AT STA 6R - SHEAR TIE IS CRACKED. REMOVED FABRICATED AND INSTALLED SHEAR TIE I.A.W SRM 5 1-10-1 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996052300420 19960523 00420 NM 1996 5 23 UPS96220140 1 19960430 A 5320 65429492 SPLICE BOEING 727 72727C 138400J NM BS 440 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE: D. STRINGER SPLICE AT 18L AND BS 440 HAS MODERATE CORROSION. REMOVED AND REPLACED STRINGER SPLICE, P /N 65-42949-2 IAW 727 SRM 51-1 0-1 AND SRM 51-20-2. 2 L 7 3 4F A3WE 1996052300421 19960523 00421 NM 1996 5 23 UPS96220141 1 19960505 A 5313 STRINGER BOEING 727 72727C 138400J NM BS 440 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE: D. STRINGER 4R HAS A CRACK AND A DOUBLE-DRILLED HOLE AT BS 440. CUT OUT DAMAGED SECTION OF STRINGER IAW 53-10-3, FIGURE 3. FABRICATED AND INSTALLED REPAIR PARTS IAW 727, SRM 53-10-3 AND SRM 51-10-6. 2 L 7 3 4F A3WE 1996052300422 19960523 00422 NM 1996 5 23 UPS96220142 1 19960428 A 5311 FRAME BOEING 727 72727C 138400J NM BS 380 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE: D. FRAME 580 HAS EXFOLIATED CORROSION ON BASE OF FRAME AT STRINGER 26L. REMOVED CORROSION AND FOUND TO BE BEYOND LIMITS PER SRM 53-10-1. FABRICATED REPAIR ANGLE AND DOUBLER AND INSTALLED SAME IAW 727 SRM 53-10-3 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996052300423 19960523 00423 NM 1996 5 23 UPS96220143 1 19960506 A 5315 FLOOR BEAM BOEING 727 72727C 138400J NM BS 312 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE: D. FLOOR BEAM CORRODED AT NUTPLATE IN UPPER FLANGE, BS 312 AT BL ZERO TO LBL 24. REMOVED DAMAGED SEC TION OF UPPER FLOOR BEAM CHORD AT BS 312 IAW SRM 53-10-8. FABRICATED REPAIR ANGLES AND INSTALLED SAME IAW SRM 53-10-8, FIGURE 7 AND SRM 53-10-2, FIGURE 7. 2 L 7 3 4F A3WE 1996052300424 19960523 00424 NM 1996 5 23 UPS96220144 1 19960503 A 5313 STRINGER BOEING 727 72727C 138400J NM BS 425 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE: D. STRINGER 25L, CORROSION REMOVAL BEYOND LIMITS AT BS 425.00. CUT OUT DAMAGED PORTION OF STRINGER. FABRICATED AND INSTALLED TYPICAL REPAIR IAW SRM 53-10-3, FIGURE 1. REPAIR EXTENDS FROM BS 410 - BS 440. 2 L 7 3 4F A3WE 1996052300425 19960523 00425 NM 1996 5 23 UPS96220145 1 19960430 A 5313 STRINGER BOEING 727 72727C 138400J NM BS 450 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE: D. STR 24L, BS 450, HAS EXFOLIATION CORROSION AT THE STAND-OFF AND THE GROUND STUD. CUT OUT DAMAGED AREA IAW SRM 53-10-3. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-10-2, SRM 53-10-3, AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996052300426 19960523 00426 NM 1996 5 23 UPS96220146 1 19960430 A 5313 STRINGER BOEING 727 72727C 138400J NM BS 440 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE: D. STR SPLICE, STR 24L AT BS 440 HAS HEAVY CORROSION. REMOVED AND REPLACED SPLICE SECTION IAW SRM 57 -30-2. 2 L 7 3 4F A3WE 1996052300427 19960523 00427 NM 1996 5 23 UPS96220147 1 19960508 A 5320 672492 CLIP BOEING 727 72727C 138400J NM BS 360 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE: D. NR 1 STRINGER ATTACH FITTING CRACKED, FRAME 360C FORWARD ATTACH FITTING. REMOVED AND REPLACED STR INGER ATTACH CLIP NR 6-72492 IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996052300428 19960523 00428 NM 1996 5 23 UPS96220148 1 19960503 A 5320 INTERCOSTAL BOEING 727 72727C 138400J NM BS 227 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE: D. FS 227.8, STR 19L, 2ND FASTENER LOCATION, AFT OF FRAME, WAS FOUND TO HAVE 4 INCH CRACKS IN FRAME A TTACH ANGLE (INTERCOSTAL ZERO AFTER EXISTING DOUBLER REMOVAL. REMOVED EXISTING DOUBLER AND INTERCOSTAL, FABRICATED REPL ACEMENT INTERCOSTAL, INSTALLED INTERCOSTAL, AND EXISTING DOUBLER IAW SRM 51-30-2 AND 51-30-1. 2 L 7 3 4F A3WE 1996052300429 19960523 00429 NM 1996 5 23 UPS96220149 1 19960426 A 5320 INTERCOSTAL BOEING 727 72727C 138400J NM BS 1110 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE: D. AFT LOWER PIT - CORROSION ON INTERCOSTAL, STA 1110, STR 24R. REMOVED INTERCOSTAL, FABRICATED AND INSTALLED NEW INTERCOSTAL IAW SR M 51-30-2 AND SRM 51-10-2. 2 L 7 3 4F A3WE 1996052300430 19960523 00430 NM 1996 5 23 UPS96220150 1 19960426 A 5315 FLOORBEAM BOEING 727 72727C 138400J NM BS 480 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE: D. STA 480 AT LBL 8, FLOORBEAM UPPER FORWARD. FLANGE UNDERSIDE HAS INTERGRANULAR CORROSION. REMOVED DAMAGED SECTION OF FLOOR BEAM AND NEW SECTION AT STA 480, LBL 12 TO RBL 68 IAW SRM 53-10-8, FIGURE 5. 2 L 7 3 4F A3WE 1996052300431 19960523 00431 NM 1996 5 23 UPS96220151 1 19960429 A 5315 FLOORBEAM BOEING 727 72727C 138400J NM BS 560 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE: D. FLOORBEAM 560, BACKSIDE OF CAP, HAS CORROSION REMOVAL OUT OF LIMITS. REMOVED DAMAGED SECTION PER SRM 53-10-8, FABRICATED REPAIR PARTS PER SRM 53-10-8, REPAIRED FLOORBEAM 560 LT IAW 53-10-8 AND 51-30-2. REPAIR IS FRO M RBL 12 TO LBL 65.5. 2 L 7 3 4F A3WE 1996052300432 19960523 00432 NM 1996 5 23 UPS96220152 1 19960508 A 5320 STRINGER TIE BOEING 727 72725C 138400H NM BS 1010 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE: C. STA 1010 AT STR 9R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AN D INSTALLED PER SRM 51-10-1, SRM 51-30-1, AND SRM 53-10-2. 2 L 7 3 4F A3WE 1996052300433 19960523 00433 NM 1996 5 23 UPS96220153 1 19960508 A 5320 STRINGER TIE BOEING 727 72725C 138400H NM FS 1010 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE: C. STA 1010 AT STR 6R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AN D INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2. 2 L 7 3 4F A3WE 1996052300434 19960523 00434 NM 1996 5 23 UPS96220154 1 19960508 A 5320 STRINGER TIE BOEING 727 72725C 138400H NM BS 970 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE: C. STA 970 AT STR 6R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2. 2 L 7 3 4F A3WE 1996052300435 19960523 00435 NM 1996 5 23 UPS96220155 1 19960508 A 5320 STRINGER TIE BOEING 727 72725C 138400H NM BS 990 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE: C. STA 990 AT STR 4R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2. 2 L 7 3 4F A3WE 1996052300436 19960523 00436 NM 1996 5 23 UPS96220156 1 19960508 A 5320 654531314 STRINGER TIE BOEING 727 72725C 138400H NM BS 990 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE: C. STA 990 AT STR 9R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2. 2 L 7 3 4F A3WE 1996052300437 19960523 00437 NM 1996 5 23 UPS96220157 1 19960508 A 5320 654531314 STRINGER TIE BOEING 727 72725C 138400H NM BS 1010 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE: C. STA 1010 AT STR 4R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AN D INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2. 2 L 7 3 4F A3WE 1996052300438 19960523 00438 NM 1996 5 23 UPS96220158 1 19960508 A 5320 654531314 STRINGER TIE BOEING 727 72725C 138400H NM BS 1010 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE: C. STA 1010 AT STR 7R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AN D INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2. 2 L 7 3 4F A3WE 1996052300439 19960523 00439 NM 1996 5 23 UPS96220159 1 19960508 A 5320 654531314 STRINGER TIE BOEING 727 72725C 138400H NM BS 1030 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE: C. STA 1030 AT STR 9R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AN D INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2. 2 L 7 3 4F A3WE 1996052300440 19960523 00440 NM 1996 5 23 UPS96220160 1 19960508 A 5320 654531314 STRINGER TIE BOEING 727 72725C 138400H NM BS 1050 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE: C. STA 1050 AT STR 6R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AN D INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2. 2 L 7 3 4F A3WE 1996052300441 19960523 00441 NM 1996 5 23 UPS96220161 1 19960508 A 5320 654531314 STRINGER TIE BOEING 727 72725C 138400H NM BS 1090 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE: C. STA 1090 AT STR 5R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AN D INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2. 2 L 7 3 4F A3WE 1996052300442 19960523 00442 NM 1996 5 23 UPS96220162 1 19960508 A 5320 654531314 STRINGER TIE BOEING 727 72725C 138400H NM BS 1010 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE: C. STA 1010 AT STR 8L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE. FABRICATED REPLACEMENT PART A ND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2. 2 L 7 3 4F A3WE 1996052300443 19960523 00443 NM 1996 5 23 UPS96220163 1 19960508 A 5320 654531314 STRINGER TIE BOEING 727 72725C 138400H NM BS 1010 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE: C. STA 1010 AT STR 7L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AN D INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2. 2 L 7 3 4F A3WE 1996052300444 19960523 00444 NM 1996 5 23 UPS96220164 1 19960508 A 5320 654531314 STRINGER TIE BOEING 727 72725C 138400H NM BS 1030 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE: C. STA 1030 AT STR 3R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AN D INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2. 2 L 7 3 4F A3WE 1996052300445 19960523 00445 NM 1996 5 23 UPS96220165 1 19960508 A 5320 654531314 STRINGER TIE BOEING 727 72725C 138400H NM BS 1090 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE: C. STA 1090 AT STR 7L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AN D INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2. 2 L 7 3 4F A3WE 1996052300446 19960523 00446 NM 1996 5 23 UPS96220166 1 19960508 A 5320 654531314 STRINGER TIE BOEING 727 72725C 138400H NM BS 1070 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE: C. STA 1070 AT STR 9L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AN D INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2. 2 L 7 3 4F A3WE 1996052300447 19960523 00447 NM 1996 5 23 UPS96220167 1 19960508 A 5320 654531314 STRINGER TIE BOEING 727 72725C 138400H NM BS 1070 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE: C. STA 1070 AT STR 6L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AN D INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2. 2 L 7 3 4F A3WE 1996052300448 19960523 00448 NM 1996 5 23 UPS96220168 1 19960508 A 5320 654531314 STRINGER TIE BOEING 727 72725C 138400H NM BS 1050 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE: C. STA 1050 AT STR 9L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AN D INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2. 2 L 7 3 4F A3WE 1996052300449 19960523 00449 NM 1996 5 23 UPS96220169 1 19960508 A 5320 654531314 STRINGER TIE BOEING 727 72725C 138400H NM BS 1030 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE: C. STA 1030 AT STR 8L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AN D INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2. 2 L 7 3 4F A3WE 1996052300450 19960523 00450 NM 1996 5 23 UPS96220170 1 19960508 A 5320 654531314 STRINGER TIE BOEING 727 72725C 138400H NM BS 1070 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE: C. STA 1070 AT STR 7L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AN D INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2. 2 L 7 3 4F A3WE 1996052300451 19960523 00451 NM 1996 5 23 UPS96220171 1 19960508 A 5320 654531314 STRINGER TIE BOEING 727 72725C 138400H NM BS 1050 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE: C. STA 1050 AT STR 6L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AN D INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2. 2 L 7 3 4F A3WE 1996052300452 19960523 00452 NM 1996 5 23 UPS96220172 1 19960508 A 5320 654531314 STRINGER TIE BOEING 727 72725C 138400H NM BS 1050 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE: C. STA 1050 AT STR 4L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AN D INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2. 2 L 7 3 4F A3WE 1996052300453 19960523 00453 NM 1996 5 23 UPS96220173 1 19960508 A 5320 654531314 STRINGER TIE BOEING 727 72725C 138400H NM BS 1030 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE: C. STA 1030 AT STR 9L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AN D INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2. 2 L 7 3 4F A3WE 1996052300454 19960523 00454 NM 1996 5 23 UPS96220174 1 19960508 A 5320 654531314 STRINGER TIE BOEING 727 72725C 138400H NM BS 1030 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE: C. STA 1030 AT STR 7L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AN D INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2. 2 L 7 3 4F A3WE 1996052300455 19960523 00455 NM 1996 5 23 UPS96220175 1 19960508 A 5320 654531314 STRINGER TIE BOEING 727 72725C 138400H NM BS 1030 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE: C. STA 1030 AT STR 6L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AN D INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2. 2 L 7 3 4F A3WE 1996052300456 19960523 00456 NM 1996 5 23 UPS96220176 1 19960508 A 5320 654531314 STRINGER TIE BOEING 727 72725C 138400H NM BS 1010 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE: C. STA 1010 AT STR 6L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AN D INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2. 2 L 7 3 4F A3WE 1996052300457 19960523 00457 NM 1996 5 23 UPS96220177 1 19960508 A 5320 654531314 STRINGER TIE BOEING 727 72725C 138400H NM BS 990 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE: C. STA 990 AT STR 8L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2. 2 L 7 3 4F A3WE 1996052300458 19960523 00458 NM 1996 5 23 UPS96220178 1 19960508 A 5320 654531314 STRINGER TIE BOEING 727 72725C 138400H NM BS 990 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE: C. STA 990 AT STR 6L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2. 2 L 7 3 4F A3WE 1996052300459 19960523 00459 NM 1996 5 23 UPS96220179 1 19960508 A 5320 654531314 STRINGER TIE BOEING 727 72725C 138400H NM BS 970 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE: C. STA 970 AT STR 8L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2. 2 L 7 3 4F A3WE 1996052300460 19960523 00460 NM 1996 5 23 UPS96220180 1 19960508 A 5320 654531314 STRINGER TIE BOEING 727 72725C 138400H NM BS 1010 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE: C. STA 1010 AT STR 5L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AN D INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2. 2 L 7 3 4F A3WE 1996052300461 19960523 00461 NM 1996 5 23 UPS96220181 1 19960508 A 5320 654531314 STRINGER TIE BOEING 727 72725C 138400H NM BS 970 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE: C. STA 9700 AT STR 4L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AN D INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2. 2 L 7 3 4F A3WE 1996052300462 19960523 00462 NM 1996 5 23 UPS96220182 1 19960508 A 5320 654531314 STRINGER TIE BOEING 727 72725C 138400H NM BS 970 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE: C. STA 970 AT STR 6L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2. 2 L 7 3 4F A3WE 1996052300463 19960523 00463 NM 1996 5 23 UPS96220183 1 19960508 A 5320 654531314 STRINGER TIE BOEING 727 72725C 138400H NM BS 970 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE: C. STA 970 AT STR 7L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2. 2 L 7 3 4F A3WE 1996052300464 19960523 00464 NM 1996 5 23 UPS96220184 1 19960508 A 5320 654531314 STRINGER TIE BOEING 727 72725C 138400H NM BS 970 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE: C. STA 970 AT STR 2R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2. 2 L 7 3 4F A3WE 1996052300465 19960523 00465 NM 1996 5 23 UPS96220185 1 19960508 A 5320 654531314 STRINGER TIE BOEING 727 72725C 138400H NM BS 970 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE: C. STA 970 AT STR 7R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2. 2 L 7 3 4F A3WE 1996052300466 19960523 00466 NM 1996 5 23 UPS96220186 1 19960508 A 5320 654531314 STRINGER TIE BOEING 727 72725C 138400H NM BS 990 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE: C. STA 990 AT STR 7L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2. 2 L 7 3 4F A3WE 1996052300467 19960523 00467 NM 1996 5 23 UPS96420136 1 19960508 A 5511 RIB BOEING 747 747121 1384871 NM LT HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 INSPECTION TYPE: MODERATE CORROSION ON LOWER ANGLE ON RIB AT STABILIZER, BL 372 LEFT. CORRODED ANGLE REMOVED. REPAIR CARRIED OUT PER QUERY NOTE 3/3/96 AND SRM 51-40-04, FIGURE 2. 2 L 7 4 4F A20WE 1996052300468 19960523 00468 NM 1996 5 23 UPS96520187 1 19960504 A 3350 LIGHT BOEING 757 75724APF 1384969 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 411UP 23851 INSPECTION TYPE: CABIN EMERGENCY EXIT LIGHTS BURNED OUT. RELAMPED ASSEMBLY - TEST NORMAL. 2 L 7 2 4F RT A2NM 1996052300469 19960523 00469 WP 1996 5 23 9611219875 1 19960519 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 784NC 48109 DURING LINE CHECK, FOUND FLOOR ESCAPEMENT LIGHTS INOPERATIVE AT ROW 16 TO 22. REPLACED BATTERY PACK AND POWER SUPPLY, O PERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996052300470 19960523 00470 NE 1996 5 23 9611221155 2 19960520 A 7230 COMPRESSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 1/3 ENGINE STALLED A NWAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS LD LANDING 1 GL 01 155US 46764 86176 DURING LANDING ROLLOUT, THE NR 1 AND NR 3 ENGINES EXPERIENCED COMPRESSOR STALLS IN REVERSE. MAXIMUM TEMPERATURE WAS AT 700 DEGRESS CELSIUS FOR BOTH ENGINES. BOTH ENGINES WERE SHUT DOWN AND RESTARTED. CREW FOLLOWED COCKPIT PROCEDURE AND T AXIED TO THE GATE WITHOUT FURTHER INCIDENT. PERFORMED RABS OPERATIONAL CHECK. CHECK WAS NORMAL AND AIRCRAFT RETURNED T O SERVICE. 2 L 7 3 4F 4 F A22WE E20EA 1996052300471 19960523 00471 EU 1996 5 23 9611233227 1 19960521 A 3350 321430 BATTERY PACK AIRBUS 320 A320211 3930320 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 327NW 297 DURING LINE MAINTENANCE, CABIN EMERGENCY LIGHTS TEST FAULTS BATT 12WL. REPLACED BATTERY PACK, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996052300472 19960523 00472 WP 1996 5 23 9611249920 1 19960521 A 3350 60030451 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 942N 47459 DURING LINE MAINTENANCE INSPECTION, FOUND TWO OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996052300473 19960523 00473 WP 1996 5 23 9611259604 1 19960520 A 2560 113317 GIRT BAR DOUG DC9 DC932 3022066 WP MAIN CABIN DOOR BENT A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 604NW 47222 DURING LINE MAINTENANCE INSPECTION, FOUND MAIN CABIN DOOR EVACUATION SLIDE GIRT BAR BENT AND DIFFICULT TO ENGAGE. REPLA CED SLIDE. 2 L 7 2 4F A6WE 1996052300474 19960523 00474 NM 1996 5 23 96FDEA00992 1 19960517 A 5320 65196914 BEAM BOEING 727 72725 1384006 NM BS 1344-1379 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 CORROSION ON BEAM AT RBL 18 TO 75 WL 205 BS 1344 TO 1379. REMOVED AND REPLACED BEAM AT BS 1344 TO 1379 WL 255 RBL 255. 2 L 7 3 4F A3WE 1996052300475 19960523 00475 NM 1996 5 23 96FDEA01012 1 19960521 A 7500 BLEED SYST BOEING 727 727233 138408A NM NR 1 ENGINE ODOR A FDEA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 25 221FE 20932 ON DESCENT WHEN NR 1 BLEED SELECTED STRONG BURNING ODOR UNTIL BLEED TURNED OFF. RAN ENGINE AND CHECKED OUT NR 1 BLEED S YS, NO STRONG BURNING ODORS WERE DETECTED. A/C OK FOR SERVICE. 2 L 7 3 4F RT A3WE 1996052300476 19960523 00476 NM 1996 5 23 96FDEA01013 1 19960521 A 3310 MAP LIGHT CONN BOEING 727 727233 138408A NM COCKPIT BURNED A FDEA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 25 221FE 20932 IMMEDIATELY AFTER TURNING THE NR 1 ON, DURING THE START OF DESCENT A BURNING SMELL WAS NOTICEABLE IN THE COCKPIT. REPEA T WRITE UP, REF 522004. RAN NR 1 PACK, FOUND NO TRACE OF BURNING ODOR. OPENED NR 1 ENG, CHECKED DUCTING, FOUND OK. RA N ENGINE, STILL NO BURNING ODOR, INSPECTED DUCTING AT NR 1 PACK CHECKED OK. FOUND SECOND OFFICER'S LEFT MAP LIGHT TERMI NAL BURNED. REPLACED TERMINAL, LIGHT CHECKED OK. C/N DUP ODOR PROBLEM. 2 L 7 3 4F RT A3WE 1996052300477 19960523 00477 NM 1996 5 23 96FDEA01014 1 19960521 A 7931 TRANSMITTER LINE BOEING 727 7272D4 138407U NM NR 2 ENGINE LEAKING A FDEA E ENGINE SHUTDOWN N K FALSE WARNING FLUID LOSS UK UNKNOWN 1 SO 25 287FE 21849 SHUTDOWN NR 2 ENGINE DUE TO LOW OIL PRESSURE IN FLT. OIL PRESS DECREASED TO 20 PSI JUST PRIOR TO SHUTDOWN. FOUND LINE LEAKING OIL AT OIL PRESS TRANSMITTER. TIGHTENED LINE LEAK, CHECKS GOOD. PERFORMED INSPECTION IAW JET RUN HANDBOOK 6-59 . NO DEFECTS, SERVICED OIL TO FULL PRESS NOW NORMAL. 2 L 7 3 4F A3WE 1996052300478 19960523 00478 NM 1996 5 23 96UAL900351 1 19960517 A 2421 IDG BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE RT ENGINE FAILED A UALA O OTHER J H WARNING INDICATION ELECT. POWER LOSS-50 PC CL CLIMB 1 WP 29 617UA 21877 SHORTLY AFTER TAKEOFF, RIGHT INTEGRATED DRIVE GENERATOR FAILED. THE IDG WAS DISCONNECTED. 2 L 7 2 4F 4 F RT A1NM E3NE 1996052300479 19960523 00479 NM 1996 5 23 96UAL900361 1 19960521 A 3397 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 EMERGENCY EXIT LIGHT AT CROSS AISLE IN FORWARD GALLEY INOP. BROKEN EMERGENCY EXIT LIGHT CABLE, REPAIRED CABLE. 2 L 7 4 4F 4 F RT A20WE E24NE 1996052300480 19960523 00480 NM 1996 5 23 96UAL900362 1 19960521 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 FLOOR EMERGENCY EXIT LIGHTS INOP IN RIGHT HAND FORWARD E-ZONE IN ADDITION TO CEILING LIGHT AND FLOOR LIGHTS IN D-ZONE. B ATTERY PACKS LOW, REPLACED BATTERY PACKS. 2 L 7 4 4F 4 F RT A20WE E24NE 1996052300481 19960523 00481 NM 1996 5 23 96UAL900363 1 19960521 A 2612 WIRE BOEING 737 737322 1384676 NM APU SHORTED A UALA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 WP 29 321UA 23953 APU FIRE WARNING DETECTOR INOP LIGHT ILLUMINATED IN CRUISE. FIRE LIGHT ILLUMINATED AND BELL SOUNDED. BLEW BOTTLE, LIGH T REMAINED ON. *S/D* FOUND WIRE IN APU FIRE WARNING HARNESS WITH TWO CUTS THAT WERE SHORTING. REPLACED WIRE CHECKS OK . 2 L 7 2 4F RT A16WE 1996052300483 19960523 00483 NM 1996 5 23 96UAL900365 1 19960521 A 7933 162BL804A OIL TEMP IND BOEING 737 737322 1384676 NM COCKPIT MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 335UA 24230 FLIGHT CREW ADVISED THAT AFTER TAKEOFF NUMBER TWO ENGINE OIL TEMPERATURE STARTED TO RISE AND PEGGED. REDUCED THROTTLE, NO HELP. TEMPERATURE REMAINED PEGGED. *S/D* REPLACED THE OIL TEMPERATURE INDICATOR. THE INDICATOR WAS FOUND TO BE SL UGGISH AND STUCK AT 100 DEGREE AND 150 DEGREE READINGS. 2 L 7 2 4F RT A16WE 1996052300484 19960523 00484 NM 1996 5 23 96UAL900366 1 19960521 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 571UA 26681 EMERGENCY EXIT LIGHT INOP AT RIGHT HAND FORWARD OVERWING DOOR. REPLACED DEFECTIVE LIGHT ASSEMBLY, OPERATION CHECKS NORM AL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996052300485 19960523 00485 NM 1996 5 23 96UAL900367 1 19960521 A 3350 BATTERY PACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 551UA 25399 EMERGENCY EXIT AND AISLE EMERGENCY ESCAPE LIGHTS OPERATION INTERMITTENT. REPLACED BATTERY PACKS M10817 AND M10818, OPER ATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996052300486 19960523 00486 NM 1996 5 23 DL72E961226 1 19960513 A 5330 65C139133 SKIN BOEING 727 727247 138408F NM FS 1065 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2829W 21481 THE FUSELAGE SKIN HAS A 2 BY 2 CUTOUT AT FS 1050, NEAR S-28R. THE SKIN IS 2024-T3 CLAD CHEM-MILLED SKIN WITH A LOCAL TH ICKNESS OF 0.050 AND 0.070. UPON REMOVAL OF TIME-LIMITED REPAIR AT HMV, ADDITIONAL DAMAGE HAS BEEN DICOVERED. S-28R AT STATION 1050 HAS EXTENSIVE CORROSION AND WILL REQUIRE INSTALLATION OF A SPLICE SECTION. ADDITIONAL CORROSION DAMAGE IS LOCATED APPROXIMATELY 2.0 I/B AND 2.0 FWD OF THE EXISTING CUTOUT. THE RESULTING CUTOUT IS 4.0 BY 5.0 IN 0.050 AND 0.00 2024-T3 CLAD SKIN. IN ADDITION, AN EXISTING REPAIR, INSTALLED PER ER/A 259545, ADD DAMAGE AFT OF FWD CUTOUT. 2 L 7 3 4F A3WE 1996052300487 19960523 00487 NM 1996 5 23 DL72K961227 1 19960311 A 5330 65545905 SKIN BOEING 727 727232 1384082 NM BS 700 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 412DA 21232 CORROSION WAS REMOVED FROM THE FUSELAGE SKIN AT STATION 700 AND STRINGER 28L RESULTING IN A 3 INCH FWD, AFT BY 1.25 INCH I/B, O/B CUTOUT. THE SKIN IS MADE FROM .160 2024-T3 MILLED TO 0.050 LOCALLY. 2 L 7 3 4F A3WE 1996052300488 19960523 00488 NM 1996 5 23 DL72P961225 1 19960507 A 5312 6516350344 BULKHEAD WEB BOEING 727 727225 1384077 NM BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8889Z 21858 THE BS 1183 BULKHEAD WEB WAS FOUND CRACKED AT RBL 27. THERE IS A .125 VERTICAL CRACK AND A .5 HORIZONTAL CRACK AT WL 17 0. THE WEB IS A BONDED ASSEMBLY OF 2024-T3 CLAD WITH A LOCAL THICKNESS OF 0.050. THE CRACK LOCATION IS OUTSIDE OF THE INSPECTION AREA SPECIFIED BY BOEING SERVICE BULLETIN 727-53-171. THE CRACKS WILL BE CUT OUT AND A REPAIR DOUBLER INSTAL LED. 2 L 7 3 4F A3WE 1996052300489 19960523 00489 NM 1996 5 23 DL72S961165 1 19960516 A 5230 65569271 ANGLE BOEING 727 727232 1384082 NM AFT CARGO DOOR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 495DA 21075 LOWER AFT T-ANGLE CORRODED BEYOND NEGLIGABLE DAMAGE LIMITS. REPLACED ANGLE PER CMM 65-56927-1. 2 L 7 3 4F A3WE 1996052300490 19960523 00490 NM 1996 5 23 DL72S961166 1 19960516 A 5230 65569271 FRAME BOEING 727 727232 1384082 NM AFT CARGO DOOR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 495DA 21075 LOWER FWD FRAME SECTION CORRODED BEYOND ALLOWABLE LIMITS. REPLACED FRAME SECTION PER CMM 65-56927-1. 2 L 7 3 4F A3WE 1996052300491 19960523 00491 NM 1996 5 23 DL72S961174 1 19960516 A 3350 7335 BULB BOEING 727 727232 1384082 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 411DA 21223 EXIT SIGN AT L1 DOOR DIM. RELAMPED. 2 L 7 3 4F A3WE 1996052300492 19960523 00492 NM 1996 5 23 DL72S961175 1 19960516 A 3350 7335 BULB BOEING 727 727232 1384082 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 411DA 21223 EXIT LIGHT AT R1 DOOR DIM. RELAMPED. 2 L 7 3 4F A3WE 1996052300493 19960523 00493 NM 1996 5 23 DL72S961176 1 19960516 A 3350 328 BULB BOEING 727 727232 1384082 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 411DA 21223 EXIT SIGN AT OVERHEAD 1ST CLASS DIM. RELAMPED. 2 L 7 3 4F A3WE 1996052300494 19960523 00494 NM 1996 5 23 DL72S961177 1 19960516 A 3350 900542 BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 411DA 21223 OVERHEAD EXIT SIGN AT SEAT ROW 21 INOP. REPLACED BATT PACK M1086. 2 L 7 3 4F A3WE 1996052300495 19960523 00495 NM 1996 5 23 DL72S961178 1 19960516 A 3350 900542 BULB BOEING 727 727232 1384082 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 411DA 21223 OVERWING EMERGENCY DOOR EXIT SIGNS DIM. REPLACED BULB. 2 L 7 3 4F A3WE 1996052300496 19960523 00496 NM 1996 5 23 DL72S961179 1 19960516 A 3350 328 BULB BOEING 727 727232 1384082 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 411DA 21223 OVERHEAD EXIT SIGN AT SEAT ROW 32 DIM. RELAMPED. 2 L 7 3 4F A3WE 1996052300497 19960523 00497 NM 1996 5 23 DL72S961180 1 19960516 A 3350 7335 BULB BOEING 727 727232 1384082 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 411DA 21223 AFT RT SERVICE DOOR EXIT SIGN DIM. RELAMPED. 2 L 7 3 4F A3WE 1996052300498 19960523 00498 NM 1996 5 23 DL72S961182 1 19960516 A 3350 7335 BULB BOEING 727 727232 1384082 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 411DA 21223 AFT AIRSTAIR EXIT SIGN DIM. RELAMPED. 2 L 7 3 4F A3WE 1996052300499 19960523 00499 NM 1996 5 23 DL72S961184 1 19960516 A 3350 LIGHT BOEING 727 727232 1384082 NM L2 DOOR INOPERATIVE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 533DA 22046 L2 DOOR EXTERIOR EMERGENCY SLIDE ILLUMINATION LIGHT INOP. CLEANED LIGHT SOCKET CENTER CONTACT, REBULBED AND OPN NOW NOR MAL. 2 L 7 3 4F A3WE 1996052300500 19960523 00500 NM 1996 5 23 DL72S961195 1 19960517 A 3350 BULB BOEING 727 727232 1384082 NM BS 840/926 FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 489DA 21019 RT SIDE EXT O/W EMER LTS AT STA 926 AND 840 INOP. RELAMPED LTS, OPS CK NORMAL. 2 L 7 3 4F A3WE 1996052300501 19960523 00501 NM 1996 5 23 DL72S961197 1 19960517 A 3350 SWITCH BOEING 727 727232 1384082 NM AFT STEW PANEL DIRTY A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 489DA 21019 EMERGENCY EXIT LIGHTS DO NOT OPERATE FROM AFT STEW PANEL ON/OFF SWITCH. CLEANED TERMINALS ON SWITCH, OPS CK NORMAL. 2 L 7 3 4F A3WE 1996052300502 19960523 00502 NM 1996 5 23 DL72S961202 1 19960516 A 3350 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 545DA 22494 FLASHLIGHT INOP. BASE CRACKED AND BATTERY DEAD, REPLACED FLASHLIGHT ASSY WITH FRESH BATTERY. 2 L 7 3 4F A3WE 1996052300503 19960523 00503 NM 1996 5 23 DL72S961212 1 19960518 A 3350 LIGHT BOEING 727 727232 1384082 NM FLOOR TRACK MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 516DA 21432 EMERGENCY TRACK LIGHT FIXTURE MISSING. REPLACED SAME, NOW OK. 2 L 7 3 4F A3WE 1996052300504 19960523 00504 NM 1996 5 23 DL72S961214 1 19960519 A 3350 1001441 LIGHT BOEING 727 727232 1384082 NM AFT AIR STAIR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 409DA 21153 FLIGHT ENGINEER TESTED EMER EXIT SYS AFT AIRSTAIR UPPER LT DID NOT TEST. FWD TO MCO AND PLAC PER M3L 33-00-16. 2 L 7 3 4F A3WE 1996052300505 19960523 00505 NM 1996 5 23 DL72W961199 1 19960517 A 5540 DOUBLER BOEING 727 727247 138408F NM VERT STAB DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2814W 20870 DOUBLER DAMAGED LOWER RUDDER LOWER RT HINGE AREA. REPLACED RUDDER PER SRM 55-2-3. 2 L 7 3 4F A3WE 1996052300506 19960523 00506 NM 1996 5 23 DL72W961200 1 19960517 A 5754 STIFFENER BOEING 727 727247 138408F NM NR 3 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2814W 20870 FOUND ON A-1 LETTER CHECK, FWD SPAR STIFFENER CRACKED I/B SIDE NR 3 SLAT I/B TRACK. REPLACED STIFFENER PER MM 57-20-21. 2 L 7 3 4F A3WE 1996052300507 19960523 00507 NM 1996 5 23 DL733961198 1 19960517 A 2612 FIRE DETECTOR BOEING 737 737347 1384647 NM NR 1 ENGINE SHORTED A DALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 27 307WA 23440 AT FL 330 NR 1 ENG OVHT LT CAME ON, REDUCED PWR SLIGHTLY LT WENT OUT. LT CAME ON SEVERAL MINS LATER THEN FAULT LT CAME ON, OVHT LT STAYED ON, SO SHUT DWN ENG FIRE LT AND BELL CAME ON, FIRED EXT LT STAYED ON FIRED 2ND BOTTLE. LANDED LAS, F IRE TRKS SAW NO IND OF SMOKE OR FIRE. REPLACED BOTH FIRE BOTTLES, INSPECTED ENG FOR CRACKED OR BLOWN DUCTS, NONE FOUND. PRESS PNEU SYS CHECKED FOR LKS, NONE FOUND. FOUND CORE COWL FIRE LP BAD AND REPLACED CORE COWL FIRE WARN LP, TEST OK. 2 L 7 2 4F RT A16WE 1996052300508 19960523 00508 NM 1996 5 23 DL733961208 1 19960518 A 3350 LIGHT BOEING 737 737347 1384647 NM L2 DOOR INOPERATIVE A DALA K NONE L NO TEST CR CRUISE 1 SO 27 305WA 23346 CREW REPORTS, AFT L-2 DOOR EXIT IDENTIFIER LENS BROKEN. REPLACED ASSY AND FOUND AFT .25 INCH OF TRACK LIGHTING AND BOTH EXITS IDENTIFIERS DOOR LIGHT INOP. 2 L 7 2 4F RT A16WE 1996052300509 19960523 00509 NM 1996 5 23 DL733961209 1 19960518 A 3350 LIGHT BOEING 737 737347 1384647 NM CABIN INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 305WA 23346 FOUND TRACK LIGHT AT AFT TWO DOOR INDENTIFIERS INOP. REPLACED RACK AND REPAIRED WIRING. 2 L 7 2 4F RT A16WE 1996052300510 19960523 00510 NM 1996 5 23 DL73E961207 1 19960518 A 2420 TEST MODULE BOEING 737 7372J8 1384489 NM NR 2 ENGINE INOPERATIVE A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 235WA 22859 NR 2 GENERATOR WOULD NOT HOOK UP TO BUS DUE TO NO VOLTAGE. FREQUENCY WAS NORMAL. REPLACED POWER TEST MODULE, OPS CK OK FOR SERVICE. 2 L 7 2 4F RT A16WE 1996052300511 19960523 00511 NM 1996 5 23 DL73S961162 1 19960514 A 5315 6545410224 FLOOR BEAM BOEING 737 737232 1384475 NM BS 695 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 315DL 23087 UPPER T-CAP CRACKED AT APPROX STA 695 BL 0 CENTER FLOOR BEAM. REPAIRED PER ERA 303591-14. 2 L 7 2 4F RT A16WE 1996052300512 19960523 00512 NM 1996 5 23 DL757961194 1 19960517 A 2910 HOSE BOEING 757 757232 1384965 NM CTR HYD BAY LEAKING A DALA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 656DL 24396 AFTER T/O, C-HYD SYS PRESS AND QTY LIGHT CAME ON, CENTER SYS WENT TO .37. FOUND FLEX LINES FROM HYD PUMP LEAKING. REPL ACED FLEX LINES, LEAK CKS GOOD. 2 L 7 2 4F RT A2NM 1996052300513 19960523 00513 NM 1996 5 23 DL767961161 1 19960515 A 2530 811150417 COFFEEMAKER BOEING 767 767232 1385132 NM AFT GALLEY FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 103DA 22215 SMOKE IN REAR GALLEY REPORTED COMING FROM AIR VENT. INSPECTED AFT GALLEY AREA AND ABOVE CEILING AREA FOR EVIDENCE OF BU RNING OR SMELL, NONE FOUND AND ALL WIRING OK. REMOVED NR 3 AND NR 4 COFFEEMAKERS AND INSPECTED WIRING HARNESS FOR CONDI TION, ALL OK, SLIGHT ACRID ODOR FROM COFFEEMAKERS. REPLACED NR 3 AND NR 4, ALL OK FOR SERVICE. 2 L 7 2 4F RT A1NM 1996052300514 19960523 00514 NM 1996 5 23 DL767961183 1 19960516 A 3397 WIRE BOEING 767 767232 1385132 NM CABIN CUT A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 104DA 22216 SECTION OF FLOOR TRACK LIGHTS INOP IN MID GALLEY. REPAIRED WIRING. 2 L 7 2 4F RT A1NM 1996052300515 19960523 00515 NM 1996 5 23 DL767961188 1 19960510 A 5754 SKIN BOEING 767 767232 1385132 NM NR 1 SLAT DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 110DL 22222 THE NR 1 SLAT, TRAILING EDGE WEDGE WAS FOUND DENTED IN THE UPPER SKIN. THE DAMAGE WAS REPAIRED PER B767-200 SRM 51-70-1 0 FIG 9. 2 L 7 2 4F RT A1NM 1996052300516 19960523 00516 WP 1996 5 23 DLL10961169 1 19960507 A 5320 1520384 LOWER SILL LKHEED 1011 10113851 5265010 WP C2 CARGO DOOR CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 720DA 193C1136 CORROSION WAS FOUND ON THE C2 DOOR SURROUND LOWER SILL OUTER CAP STA 1625. THE CORROSION WAS CUT OUT, FILLED AND REINFO RCED, REV A ADDS FAA APPROVAL. 2 L 7 3 4F A23WE 1996052300517 19960523 00517 WP 1996 5 23 DLL10961189 1 19960514 A 5712 RIB CAP LKHEED 1011 10113851 5265010 WP WS 555 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 722DA 193C1147 THE LEFT HAND WING WAS FOUND WITH A 1 INCH CRACK IN THE IWS 555 UPPER RIB CAP. THE DAMAGED AREA WAS CUT OUT AND A NEW R IB WAS SPLICED IN, REV A ADDS FAA APROVAL. REV B CHANGES THE FWD CUT LOCATION TO PREVENT INTERFERENCE. 2 L 7 3 4F A23WE 1996052300518 19960523 00518 WP 1996 5 23 DLL10961201 1 19960517 A 2560 GIRT BAR LKHEED 1011 10113851 5265010 WP R1 DOOR OUT OF ADJUST A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 735D 193C1226 R-1 DOOR GIRT BAR WOULD NOT ENGAGE. ADJUSTED SLIDE IN DOOR MOUNTS AND GIRT BAR ENGAGES NORMALLY NOW. 2 L 7 3 4F A23WE 1996052300519 19960523 00519 WP 1996 5 23 DLL10961213 1 19960519 A 3230 RETRACT MECH LKHEED 1011 10113851 5265010 WP RT MLG MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 716DA 193C1095 AFTER TAKEOFF, RT MAIN LANDING GEAR WOULD NOT RETRACT. JACKED AIRCRAFT AND PERFORMED TEST PER M/M, NO TROUBLE FOUND. 2 L 7 3 4F A23WE 1996052300520 19960523 00520 WP 1996 5 23 DLL12961205 1 19960518 A 2710 671670 ACTUATOR LKHEED 1011 1011385115 5265015 WP LT AILERON FAILED A DALA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 724DA 193C1151 ON TAXI OUT, AFTER STARTING ENGINES THE A-SYSTEM HYD QUANTITY WENT TO .125 WITH LOW QTY LIGHT ON. SYSTEM PRESSURE WAS O K. DEPRESSURIZED SYSTEM AND RETURNED TO GATE. FOUND THE LEFT INBOARD AILERON THE OUTBOARD ACTUATOR HAD FAILED ALSO BRE AKING ONE OF THE 3 HYD LINES CONNECTED TO ACTUATOR. 2 L 7 3 4F A23WE 1996052300521 19960523 00521 WP 1996 5 23 DLL12961219 1 19960519 A 2560 VIEWING WINDOW LKHEED 1011 1011385115 5265015 WP 3L DOOR SLIDE MISSING A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 724DA 193C1151 3L DOOR ESCAPE SLIDE CASE MISSING 2.5 INCH WINDOW FOR VIEWING SLIDE BOTTLE PRESSURE. FWD TO MCO AND PLCD. 2 L 7 3 4F A23WE 1996052300522 19960523 00522 WP 1996 5 23 DLL13961167 1 19960516 A 3350 BULB LKHEED 1011 10113851 5265010 WP L 1 EXT SLIDE FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 789DL 193A1142 L-1 EXTERIOR SLIDE LIGHT HAS ONE BULB IS INOP. RELAMPED, OP CKS GOOD. 2 L 7 3 4F A23WE 1996052300523 19960523 00523 WP 1996 5 23 DLL14961190 1 19960514 A 5330 SKIN LKHEED 1011 1011385115 5265015 WP FS 1363-1453 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 736DY 193C1227 THE BELLY SKIN FOR STA 1363 TO 1453 BETWEEN 31, 32, 34 AND 35 HAD CORROSION. THE REPAIR WAS ACCOMPLISHED PER SRM 53-31- 00 FIG 827. REV A CHANGES INSTRUCTIONS AND ADDS DRAWING TO ALLOW DEVIATION FROM REFERENCE SRM. 2 L 7 3 4F A23WE 1996052300524 19960523 00524 NM 1996 5 23 DLM11961206 1 19960518 A 3610 DUCT CLAMP DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE NR 3 ENGINE LOOSE A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 804DE 48475 733745 NR 3 ENG FIRE WARNING AT 13,500 FT ON CLIMBOUT, APPROX 1.36 EPR. FIRE WARNING EXT WHEN THROTTLE PLACED AT IDLE. REPAIR ED PNEU LEAK AT PRSOV AND REPLACED BOTH LOWER LOOPS. RAN ENG, NO HELP. FOUND BLEED AIR DUCT LEAKING AT CLAMP AT 12 O'C LOCK POSITION. REPLACED CLAMP, CKS GOOD. 2 L 7 3 4F 4 F RT A22WE E24NE 1996052300525 19960523 00525 NM 1996 5 23 DLM11961210 1 19960518 A 2530 831610405 OVEN DOUG MD11 MD11 3023602 NM AFT GALLEY MALFUNCTIONED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 812DE 48601 OVEN NR 307 IN AFT GALLEY WOULD NOT TURNED OFF WITH SWITCH. PULLED C/B'S TO ALL TO STOP OVERHEATING. IT WAS GIVING OFF A BURNING ODOR AND VERY HOT. ATL MTC NOTIFIED. 2 L 7 3 4F RT A22WE 1996052300526 19960523 00526 NM 1996 5 23 DLM88961173 1 19960516 A 3350 BR9279109 LIGHT DOUG MD88 MD88 3023688 NM OVERWING INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 907DL 49538 OVERWING EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY. 2 L 7 2 4F RT A6WE 1996052300527 19960523 00527 NM 1996 5 23 DLM88961196 1 19960517 A 3040 ANTI-ICE SENSOR DOUG MD88 MD88 3023688 NM LT WINDSHIELD FAILED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 992DL 53344 PILOTS W/S A/I SNSR BEGAN SMOKING. TURNED OFF W/S A/I AND SMOKE ABATED. T/S IN PROGRESS, REPOSITIONED WIRE BUNDLE, CKD ALL LUGS, WIRES, TERMINALS. PHENOLIC ON WINDOW SMELLS OF SMOKE. NO APPARENT BLUEING, SCORCH, CHAR OR BURN MARKS. REP LACED WINDOW AS PRECAUTION. 2 L 7 2 4F RT A6WE 1996052300528 19960523 00528 NM 1996 5 23 DLM88961217 1 19960519 A 3350 BATTERIES DOUG MD88 MD88 3023688 NM OVERHEAD CEILING DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 909DL 49540 OVERWING EMERGENCY EXIT SIGNS INOP ON EMERGENCY LIGHT TEST. REPLACED BATTERIES DPN 339101293, LIGHTS TEST OK. 2 L 7 2 4F RT A6WE 1996052300529 19960523 00529 NM 1996 5 23 DLM88961229 1 19960422 A 5280 5930583 Z-CHANNEL DOUG MD88 MD88 3023688 NM LT MLG DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 948DL 49879 LT MAIN LANDING GEAR DOOR INNER PAN Z-CHANNEL HAS CRACK APPROX 3.25 INCH LONG RUNNING IN THE AFT RADIUS ALONG THE AFT ED GE OF SUBJECT CHANNEL, 19.5 INCHES FROM THE AFT I/B CORNER STRAP. A REPAIR ANGLE WAS USED TO REPAIR THIS CRACK. REV A AND B REVISED THE PERMANENT REPAIR INSTRUCTIONS, PERMANENT REPAIR PER SRM 52-05 FIG 28. 2 L 7 2 4F RT A6WE 1996052300530 19960523 00530 NE 1996 5 23 P5CA9600230 2 19960519 A 7320 PS4 LINE BOEING 747 747132 1384882 NM PWA JT9 JT9D7A 52054 NE NR 1 ENGINE LOOSE A P5CA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 23 857FT 20246 662581 AFTER AIRCRAFT WAS PUSHED OFF BLOCKS, UNABLE TO START NR 1 ENGINE, HANGING WITH NO ACCELERATION. INSPECTED AND FOUND BU RNER PRESSURE SENSE PS4 LINE LOOSE AT FCU. TIGHTENED SAME, ENGINE START AND OPERATION NORMAL IAW MM 71-00-00. 2 L 7 4 4F 4 F A20WE E20EA 1996052300531 19960523 00531 NE 1996 5 23 P5CA9600231 2 19960521 A 7510 ANTI-ICE VLV LT BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 4 ENGINE MALFUNCTIONED A P5CA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 WP 23 853FT 19753 AIRCRAFT HAD GATE TURNBACK DUE TO NR 4 ENGINE ANTI-ICE LIGHT ON. VALVE OPS CHECKS NORMAL IAW MM 75-11-00. DEFERRED NR 4 ENGINE ANTI-ICE VALVE LIGHT PER MEL 30-04-1, DUE 31 MAY 96. 2 L 7 4 4F 4 F A20WE E20EA 1996052300532 19960523 00532 NE 1996 5 23 P5CA9600232 2 19960520 A 7230 COMP BLADES BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE NR 1 ENGINE BIRD STRIKE A P5CA K NONE C F.O.D. IN INSP/MAINT 1 WP 23 858FT 20109 662383 UPON INSPECTION OF NR 1 ENGINE DURING MAINTENANCE, FOUND EVIDENCE OF BIRD STRIKE ON FAN BLADES AND FAN EXIT DIAPHRAGM. C OMPLIED WITH CONDITIONAL INSPECTION PER 5-51-14 AND BORESCOPE INSPECTION PER MM 72-00-00. FOUND 6 EACH 5TH STAGE COMPRE SSOR BLADES BENT BEYOND LIMITS. REMOVED AND REPLACED ENGINE, RUNUP CHECK NORMAL PER MM 71-00-0. 2 L 7 4 4F 4 F A20WE E20EA 1996052300533 19960523 00533 NE 1996 5 23 P5CA9600233 2 19960520 A 7200 ENGINE BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 3 ENGINE BIRD STRIKE A P5CA K NONE C F.O.D. IN INSP/MAINT 1 WP 23 852FT 19757 662628 UPON INSPECTION OF NR 3 ENGINE FOUND EVIDENCE OF BIRD STRIKE. COMPLIED WITH CONDITIONAL INSPECTION PER 5-51-14 AND BORE SCOPE INSPECTION PER MM 72-00-00, NO DAMAGE FOUND. 2 L 7 4 4F 4 F A20WE E20EA 1996052300534 19960523 00534 NM 1996 5 23 SCNA96142 1 19960520 A 5311 FRAME BOEING 727 7272J4 1384006 NM BS 760/783 DAMAGED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 288SC 20765 WHILE ACCOMPLISHING AD 94-02-04, ELONGATED HOLES WERE FOUND IN THE BS 760 AND 783 FRAMES. REPAIRED HOLES IN ACCORDANCE WITH B727 SB53-197 AND BOEING TELEX 32-9430. 2 L 7 3 4F RT A3WE 1996052300535 19960523 00535 NM 1996 5 23 VNAA9600034 1 19960518 A 3610 DON545T3FEL002C RELAY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT AVIONIC RACK DEFECTIVE A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 433JS 3047 SHORTLY AFTER CLIMBOUT, RECEIVED AN AMBER CAS MESSAGE PAK OVERHEAT ASSOCIATED WITH A SWEET SMELL IN THE CABIN. AIRCRAFT DIVERTED TO PIT WHERE MX REPLACED THE LEFT BLEED SHUT OFF VALVE TIME DELAY RELAY IAW MM 31-14-00. GROUND CHECKED GOOD. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996052300536 19960523 00536 NM 1996 5 23 VNAA9600035 1 19960520 A 7712 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT ENGINE DIRTY A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 07 436JS 3052 CREW ABORTED THE TAKEOFF AT APPROXIMATELY V1 BECAUSE RIGHT ENGINE TORQUE INDICATION WAS FLUCTUATING BETWEEN 0 AND 100 PERCENT. AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. REMOVED, CLEANED AND REINSTALLED THE CANNON PLUG CONN ECTOR FOR THE TORQUE SIGNAL PICK-UP IAW MM 77-00-00. GROUND CHECKED GOOD. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996052300537 19960523 00537 NM 1996 5 23 VNAA9600036 1 19960520 A 2133 2097H020900 OUTFLOW VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DEFECTIVE A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 439JS 3057 DURING CLIMBOUT, THE CREW WAS ALERTED BY A CAS MESSAGE CABIN OVER PRESSURE. CREW ATTEMPTED TO CONTROL CABIN PRESSURE IN MANUAL MODE, WITHOUT SUCCESS. AIRCRAFT RETURNED TO THE FIELD, LANDED WITHOUT FURTHER INCIDENT. REPLACED THE OUTFLOW V ALVE IAW MM 21-31-00. GROUND CHECKED GOOD. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996052300538 19960523 00538 NE 1996 5 23 96ZZZM819 2 19960420 A 7270 652244117 SADDLE DUCT BOEING 727 72751C 1384015 NM PWA JT8 JT8D7B 52053 NE NR 1 ENGINE RUPTURED A RYNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 07 413EX 19206 FIRE WARNING SOUNDED ON NR 1 ENGINE AFTER TAKEOFF. DISCHARGED LEFT FIRE BOTTLE. AIRCRAFT LANDED WITHOUT FURTHER INCIDE NT. REPLACED 13TH STAGE SADDLE DUCT ON NR 1 ENGINE. REPLACED LEFT FIRE BOTTLE. 2 L 7 3 4F 4 F A3WE E2EA 1996052300539 19960523 00539 1996 5 23 96ZZZM820 4 19960402 A 3454 G4816 VHF CONTL PANEL DOUG DC9 DC932 3022066 WP NR 1 INOPERATIVE A VJ6A A UNSCHED LANDING O OTHER CR CRUISE 1 SO 11 914VV 47486 ON FLT NR 270, ATL-ATL, AIR RETURN FOR MTC CONVENIENCE, THE NR 1 VHF RADIO WOULD NOT TRANSMIT OR RECEIVE ON MOST FREQUEN CIES. THE NR 2 AZIMUTH AND RMI NEEDLE INOP. REMOVED AND REPLACED NR 1 VHF CONTROL PANEL PER 23-10, OPS CHECK GOOD, AND REMOVED AND REPLACED NR 2 NAV/COMM PANEL PER 34-51, OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996052300540 19960523 00540 1996 5 23 96ZZZM821 4 19960402 A 3454 G4816 NAV/COM PANEL DOUG DC9 DC932 3022066 WP NR 2 INOPERATIVE A VJ6A A UNSCHED LANDING O OTHER CR CRUISE 1 SO 11 914VV 47486 ON FLT NR 270, ATL-ATL, AIR RETURN FOR MTC CONVENIENCE, THE NR 1 VHF RADIO WOULD NOT TRANSMIT OR RECEIVE ON MOST FREQUEN CIES. THE NR 2 AZIMUTH AND RMI NEEDLE INOP. REMOVED AND REPLACED NR 1 VHF CONTROL PANEL PER 23-10, OPS CHECK GOOD, AND REMOVED AND REPLACED NR 2 NAV/COMM PANEL PER 34-51, OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996052300541 19960523 00541 WP 1996 5 23 96ZZZM822 1 19960402 A 2410 CSD DOUG DC9 DC932 3022066 WP RIGHT MALFUNCTIONED A VJ6A A UNSCHED LANDING O OTHER CL CLIMB 1 SO 11 911VV 47285 FLT 520 - ATL-ATL, AIR RETURN FOR MTC CONVENIENCE, THE RIGHT CSD ROSE INTO THE CAUTION RANGE, APPROACHING THE RED LINE. LEFT GENERATOR PREVIOUSLY ON MEL. CLEARED MEL ON LEFT GENERATOR BY ADJUSTING CSD FREQUENCY PER 24-10 AND ASSIGNED MEL TO RIGHT CSD. (M) 2 L 7 2 4F A6WE 1996052300542 19960523 00542 WP 1996 5 23 96ZZZM823 1 19960413 A 3260 PROX SWITCH DOUG DC9 DC932 3022066 WP RT MLG BROKEN WIRE A VJ6A O OTHER N FALSE WARNING AP APPROACH 1 SO 11 931VV 47674 DURING TEST FLIGHT FOR NOSE GEAR INDICATION PROBLEMS, RIGHT MAIN GEAR UNSAFE LIGHT REMAINED ON. GEAR POSITION VISUALLY VERIFIED. MAINTENANCE FOUND BROKEN WIRE ON RIGHT GEAR PROXIMITY SWITCH. MAINTENANCE REPAIRED WIRING SYSTEM GROUND CHEC K GOOD. (M) 2 L 7 2 4F A6WE 1996052300543 19960523 00543 WP 1996 5 23 96ZZZM824 1 19960411 A 2410 696233B CSD DOUG DC9 DC932 3022066 WP RIGHT INOP A VJ6A A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CL CLIMB 1 SO 11 938VV 47442 FLT NR 383 - BOS-BOS, AIR RETURN DUE TO RIGHT GEN FLUCTUATES ON AND OFF AFTER TAKEOFF. APU PREVIOUSLY ON MEL. ASSIGNED MEL TO RIGHT GEN AND CLEARED MEL ON APU. REMOVED AND REPLACED NR 2 CSD PER VJ MM 24-10-1. (M) 2 L 7 2 4F A6WE 1996052300544 19960523 00544 WP 1996 5 23 96ZZZM825 1 19960422 A 3150 TQ WARNING DOUG DC9 DC932 3022066 WP COCKPIT SOUNDED A VJ6A C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 11 940VV 47523 ON FLT 555 - MDW-MDW- ABORTED TAKEOFF DUE TO TAKEOFF WARNING HORN ON TAKEOFF ROLL. ADJUSTED FLAP POSITION SWITCH AND TA KEOFF WARNING SYSTEM. OPS CHECK NORMAL, IAW MM 27-55. (M) 2 L 7 2 4F A6WE 1996052300545 19960523 00545 WP 1996 5 23 96ZZZM826 1 19960421 A 7722 EGT INDICATOR DOUG DC9 DC932 3022066 WP NR 2 ENGINE INOPERATIVE A VJ6A A UNSCHED LANDING O OTHER CL CLIMB 1 SO 11 938VV 47442 ON FLT 498 - ATL-ATL, AIR RETURN, THE NR 2 EGT WENT INOP. REMOVED AND REPLACED NR 2 EGT INDICATOR PER VJ MM 77-20-00, O PS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1996052300546 19960523 00546 WP 1996 5 23 96ZZZM827 1 19960425 A 3260 SWITCH DOUG DC9 DC932 3022066 WP NLG MALFUNCTIONED A VJ6A L ABORTED APPROACH O OTHER AP APPROACH 1 SO 11 930VV 47723 FLT NR 396 - PBI-BOS, THE NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE ON GEAR EXTENSION. EXECUTED MISSED APPROACH, NOSE LIGHT ILLUMINATED DURING CLIMB AND LANDED NORMALLY. CHECKED NOSE GEAR ASSEMBLY SWITCH, NO DEFECTS FOUND. 2 L 7 2 4F A6WE 1996052300547 19960523 00547 1996 5 23 96ZZZM828 4 19960322 A 3452 ATC TRANSPONDER DOUG DC9 DC932 3022066 WP LT/RT INOPERATIVE A VJ6A A UNSCHED LANDING O OTHER CR CRUISE 1 SO 11 905VJ 47378 FLT 471 - IAD-MSY - DIVERTED TO ATL, BOTH ATC TRANSPONDERS BECAME INOP. REMOVED AND REPLACED NR 1 ALTIMETER AND REPAIRE D BROKEN WIRE ON NR 2 TRANSPONDER. ASSIGNED MEL TO NR 1 TRANSPONDER READING LOW. 2 L 7 2 4F A6WE 1996052300548 19960523 00548 WP 1996 5 23 96ZZZM829 1 19960223 A 5610 5912290501 WINDSHIELD DOUG DC9 DC932 3022066 WP LT COCKPIT FAILED A VJ6A A UNSCHED LANDING O OTHER CR CRUISE 1 SO 11 914VV 47486 ON FLT 229 - ATL-ATL, AIR RETURN, CAPTAINS WINDSHIELD SHATTERED (OUTER PANE) NO IMPACT. REMOVED AND REPLACED CAPTAINS S IDE WINDSHIELD IAW 56-10-2. NO DEFECTS NOTED. 2 L 7 2 4F A6WE 1996052300549 19960523 00549 WP 1996 5 23 96ZZZM830 1 19960219 A 2133 54447211 OUTFLOW ACTUATOR DOUG DC9 DC932 3022066 WP CABIN MALFUNCTIONED A VJ6A A G UNSCHED LANDING O2 MASK DEPLOYED P NO WARNING INDICATION CL CLIMB 1 SO 11 921VV 47284 FLT 248 - ATL-ATL, AIR RETURN, DURING CLIMB-OUT OF ATL IN MANUAL PRESSURE AND CABIN AT 5000 FEET CLIMBING AT 500 FPM NR 1 FLIGHT ATTENDANT ADVISED THE CREW THAT ALL OXYGEN MASKS HAD DROPPED. NO WARNING FROM THE COCKPIT AND NO CABIN PRESSUR E LIGHT. FOUND OUTFLOW VALVE ACTUATOR INTERMITTENT. REMOVED AND REPLACED OUTFLOW VALVE ACTUATOR. PERFORMED OPERATIONA L CHECK OF MASKS, CLEANED AND RESTOWED MASKS, OPS CHECK GOOD PER MM 35-20-00. 2 L 7 2 4F A6WE 1996052300550 19960523 00550 WP 1996 5 23 96ZZZM831 1 19960404 A 3260 DNLOCK SENSOR DOUG DC9 DC932 3022066 WP NLG DIRTY A VJ6A L ABORTED APPROACH P NO WARNING INDICATION LD LANDING 1 SO 11 930VV 47723 FLT NR 470, IAD-MCO, UPON GEAR EXTENSION NO GREEN LIGHT ON, NOSE GEAR CYCLED FOUR TIMES, CHECKED VISUALLY. CLEANED DOWN LOCK SENSOR OF RUST AND ELECT COMM. PERFORMED NOSE GEAR SWING, CHECK PER MM 32-30 7-11-0 PAGE 201-211. OPS CHECK NORMA L. 2 L 7 2 4F A6WE 1996052300551 19960523 00551 WP 1996 5 23 96ZZZM832 1 19960404 A 3260 PROX SWITCH DOUG DC9 DC932 3022066 WP LT MLG OUT OF ADJUST A VJ6A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 11 931VV 47674 FLT 206 - MCO-MCO, AIR RETURN, AFTER TAKEOFF THE RED LEFT GEAR UNSAFE LIGHT REMAINED ON. RECYCLED GEAR, NO HELP, LIGHT REMAINED ON. GEAR DOOR OPEN LIGHT WAS OUT. REPAIRED AND ADJUSTED LEFT MLG UPLOCK PROXIMITY SWITCH SYSTEM. OPS CHECKED OK IAW 32-10-0. 2 L 7 2 4F A6WE 1996052300552 19960523 00552 WP 1996 5 23 96ZZZM833 1 19960402 A 3260 0080004003 PROX CONTROL BOX DOUG DC9 DC932 3022066 WP LT MLG FAILED A VJ6A A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 11 931VV 47674 FLT N 360 - RDU-IAD, THE LEFT GEAR UNSAFE LIGHT INDICATION CAME ON DURING GEAR RETRACTION. CYCLED GEAR AND THE LIGHT ST AYED ON, SAFE INDICATION ON APPROACH AND LANDING. TROUBLESHOT SYSTEM AND PERFORMED OPS CHECK. REMOVED AND REPLACED PRO XIMITY SWITCH CONTROL BOX. SYSTEM OPS CHECKS GOOD IAW DC-9 MM 32-30-0. 2 L 7 2 4F A6WE 1996052300553 19960523 00553 WP 1996 5 23 96ZZZM834 1 19960309 A 3260 SWITCH DOUG DC9 DC932 3022066 WP LT MLG DOWNLOCK FAILED A VJ6A O OTHER N FALSE WARNING AP APPROACH 1 SO 11 902VJ 47177 LEFT GEAR UNSAFE LIGHT REMAINS ILLUMINATED FOLLOWING GEAR EXTENSION. GEAR VISUALLY VERIFIED DOWN. REMOVED AND REPLACED MAIN LANDING GEAR DOWNYOCK SWITCH, OPS CHECK NORMAL, REF 32-50-1 MM GEAR SWING. 2 L 7 2 4F A6WE 1996052300554 19960523 00554 WP 1996 5 23 96ZZZM835 1 19960409 A 5270 SWITCH DOUG DC9 DC932 3022066 WP CARGO DOOR OUT OF ADJUST A VJ6A C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 11 917VV 47323 FLT 402 - ATL-ATL, TAKEOFF WAS ABORTED DUE TO FORWARD CARGO DOOR WARNING LIGHT ON. ASSIGNED MEL TO FORWARD CARGO DOOR W ARNING LIGHT ON PREVIOUS MRR ON 4/9/96. ADJUSTED FORWARD CARGO DOOR LIGHT SWITCH, OPS CHECKED NORMAL. 2 L 7 2 4F A6WE 1996052300555 19960523 00555 1996 5 23 96ZZZM836 4 19960330 A 3421 285733513 VERTICAL GYRO DOUG DC9 DC932 3022066 WP RIGHT MALFUNCTIONED A VJ6A K NONE O OTHER CL CLIMB 1 SO 11 931VV 47674 FLT 412 - ATL-ATL - AIR RETURN, FIRST OFFICERS ADI QUIT WORKING. REMOVED AND REPLACED FIRST OFFICERS VERTICAL GYRO. OP S IAW 34-20 GOOD. NO DEFECTS NOTED. 2 L 7 2 4F A6WE 1996052300556 19960523 00556 1996 5 23 96ZZZM837 4 19960307 A 3442 RADAR DOUG DC9 DC932 3022066 WP FWD FUSELAGE MALFUNCTIONED A VJ6A A UNSCHED LANDING O OTHER CL CLIMB 1 SO 11 905VJ 47378 FLT 509 - ATL-ATL, AIR RETURN, THE RADAR WAS MALFUNCTIONING AND THE WEATHER PRESENTATION WAS UNUSABLE. REMOVED AND REPL ACED RADAR INDICATOR AND RADAR R/T. OPS CHECK NORMAL. 2 L 7 2 4F A6WE 1996052300557 19960523 00557 WP 1996 5 23 96ZZZM838 1 19960311 A 5220 EMER EXIT DOOR DOUG DC9 DC932 3022066 WP RT OVERWING NOT LATCHED A VJ6A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 921VV 47284 FLT 462 - TPA-TPA, AIR RETURN, THE RIGHT AFT OVERWING EXIT DOOR WAS NOT SEATED PROPERLY. RESEATED THE DOOR AND PRESSURI ZED THE A/C. NO LEAKS NOTED. A/C OK TO CONTINUE SERVICE. 2 L 7 2 4F A6WE 1996052300558 19960523 00558 EA 1996 5 23 96ZZZM839 2 19960425 A 7320 FUEL TUBE BEECH 1900 1900 1154160 CE PWA PT6 PT6A65B 52043 EA RT ENGINE OUT OF POSITION A GUUA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 SO 19 194GA UB8 FLT 442 - MHH/MIA - RIGHT ENGINE LOST POWER IN FLIGHT, UNABLE TO INCREASE OR DECREASE POWER. PRECAUTIONARY ENGINE SHUT DOWN. TROUBLE SHOT SYSTEM, REPOSITIONED FUEL TRANSFER TUBE. LEAK CHECK AND OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A24CE E4EA 1996052300559 19960523 00559 EA 1996 5 23 96ZZZM840 2 19960424 A 7200 ENGINE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA NR 2 FAILED A GUUA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 19 734GL UB34 FLT 442 - MHN/MIA - NR 2 ENGINE OIL PRESSURE DROPPED TO ZERO ITT 900, RPM ZERO, TORQUE ZERO. ENGINE SHUT DOWN. REMOVED AND REPLACED POWER PLANT. 2 L 7 2 4T 4 T RT A24CE E4EA 1996052300560 19960523 00560 SO 1996 5 23 96ZZZM841 1 19960402 A 3230 4204202 ARM 4027917 PIPER PA31T PA31T3 7103128 SO RT MLG BROKEN A S A SOCA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 314SC 6135 851643 31T8275007 ON DEPART, WHILE RETRACTING THE L/G THE CREW NOTED THAT THE GEAR UNSAFE LIGHT REMAINED ILLUMINATED AND THE GEAR SELECTOR HANDLE DID NOT RETURN TO NEUTRAL. SELECTED GEAR DOWN AND NOTED THAT THE GEAR UNSAFE LIGHT REMAINED ON AND THE RT MAIN DOWN LIGHT DID NOT ILLUMINATE. MX AND OPERATIONS WERE NOTIFIED BY RADIO AND A FLYBY WAS REQUESTED AND EXECUTED. DURING THE FLYBY IT WAS DETERMINED BY GRD OBSERVERS THAT THE GEAR WAS DOWN AND APPEARED LOCKED. THE CREW WAS ADVISED TO UTILI ZE THE EMERG AIR BLOWDOWN SYSTEM TO PROVIDE POSITIVE PRESS TO THE DOWN SYS IN CASE THE MECH LOCK WAS NOT ENGAGED, AND AD VISED TO CALL FOR THE EQUIP AND LAND AND STOP ON RUNWAY TO ALLOW MX TO ENSURE GEAR WAS MECH LOCKED DOWN. 1 L 7 2 3T A8EA 1996052300561 19960523 00561 SW 1996 5 23 96ZZZM842 1 19960305 A 3040 140132100 MOTOR SWRNGN SA226 SA226TC 8780404 SW WINDSHIELD WIPER FAILED A BSAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 05 139PA TC296 GGW - STRONG BURNT ELECTRICAL SMELL IN COCKPIT. CO-PILOTS WINDSHIELD WIPER MOTOR OVERHEATED. PULLED WINDSHIELD WIPER C IRCUIT BREAKER AND CONTINUED FLIGHT PER MEL. REPLACED WINDSHIELD WIPER MOTOR AND WIPER TENSION SPRING. OPS CHECKED NOR MAL. (M) 2 L 7 2 4T RT A8SW 1996052300562 19960523 00562 SW 1996 5 23 96ZZZM843 1 19960313 A 3260 UPLOCK SWITCH SWRNGN SA226 SA226TC 8780404 SW NLG OUT OF ADJUST A BSAA O OTHER N FALSE WARNING CL CLIMB 1 NM 05 115BS TC324 BIL - NOSE GEAR INTRANSIT RED LIGHT WOULD NOT EXTINGUISH UPON GEAR RETRACTION DURING CLIMB-OUT. SELECTED GEAR DOWN, SHO WED THREE GREEN, RETURNED AND LANDED UNEVENTFULLY. UPLOCK SWITCH OUT OF ADJUSTMENT. ADJUSTED UPLOCK SWITCH PER MM. GE AR RETRACT FUNCTION CHECK PERFORMED NORMALLY SEVERAL TIMES. 2 L 7 2 4T RT A8SW 1996052300563 19960523 00563 SW 1996 5 23 96ZZZM844 1 19960207 A 7722 6110002344 EGT INDICATOR SWRNGN SA226 SA226TC 8780404 SW LT ENGINE MALFUNCTIONED A BSAA O OTHER M OVER TEMP IN INSP/MAINT 1 NM 05 116BS TC311 GTF - GTF - LEFT ENGINE OVERTEMPED ON START IN GTF. EGT GAUGE STUCK AT 230 DEGREES CELSIUS WHEN STOP BUTTON RELEASED, T EMP CLIMBED TO 900 DEGREES CELSIUS, ABORTED START. STICKING EGT GAUGE. REMOVED ENGINE, COMPLIED WITH OVERTEMP INSPECTI ON PER GARRETT MM AND REINSTALLED ENGINE. GROUND RUN AND TEST FLIGHT PERFORMED NORMAL. REMOVED AND REPLACED EGT INDICA TOR. 2 L 7 2 4T RT A8SW 1996052300564 19960523 00564 SW 1996 5 23 96ZZZM845 1 19960129 A 3251 2719875 ACTUATOR SWRNGN SA226 SA226TC 8780404 SW NLG STEERING FAILED A BSAA O OTHER O OTHER LD LANDING 1 NM 05 115BS TC324 GDV - NO NOSEWHEEL STEERING, POSSIBLE UNCOMMANDED HYDRAULIC PRESSURE TO THE RIGHT. TEMP IN GDV WAS -23 DEGREES FAHRENHE IT. SUSPECT INTERNAL FAILURE OF NOSEWHEEL STEERING ACTUATOR. DEACTIVATED NWS PER MEL AND FERRIED A/C TO BIL. REMOVED AND REPLACED NWS ACTUATOR. REPLACED WIRE BUNDLE, SPECIFICALLY WIRE 713B-22 WHICH WAS BROKEN IN NOSE WHEELWELL. NWS OPS CHECKED OK AND GEAR RETRACT FUNCTION CHECKED NORMAL. 2 L 7 2 4T RT A8SW 1996052300565 19960523 00565 WP 1996 5 23 96ZZZM846 1 19960422 A 2911 AS14308 HYD ACCUMULATOR DOUG DC6 DC6B 3021712 WP HYD COMP FAILED A TALA C D ABORTED TAKEOFF RETURN TO BLOCK K FLUID LOSS TO TAKEOFF 1 SO 19 841TA 44891 MSDS - ON TAKEOFF ROLL, MAIN HYDRAULIC ACC EXPLODED CAUSING EXTENSIVE DAMAGE TO AIRCRAFT STRUCTURE AND SYSTEMS. TAKEOFF ABORTED. SUBMITTER STATES, PROBABLE CAUSE, MAIN HYDRAULIC ACCUMULATOR FAILURE. 2 L 7 4 4R 6A4 1996052300566 19960523 00566 EU 1996 5 23 96ZZZM847 1 19960412 A 3260 200918001 SWITCH STBROS SD3 SD360 8100606 EU RT MLG OUT OF ADJUST A GUUA O OTHER P NO WARNING INDICATION AP APPROACH 1 SO 19 826BE SH3745 FLT 406 - MCO-MIA - RIGHT MAIN WOULD NOT INDICATE GREEN, DOWN AND LOCKED GEAR EMERGENCY EXTENDED. AIRCRAFT LANDED WITHO UT INCIDENT. THE LANDING GEAR EXTERNAL RETRACTION SYSTEM WAS DEFERRED WITH GEAR PINS LOCK WIRED IN PLACE. SYSTEM TROUB LE SHOT, RIGHT DOWN LOCK ADJUSTED. RETRACTION TEST COMPLIED WITH SATISFACTORILY. 2 H 7 2 4T A41EU 1996052300567 19960523 00567 NM 1996 5 23 96ZZZM848 1 19960412 A 5510 65241892 LOWER TE BEAM BOEING 727 727227 1384078 NM HORIZ STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 723AA 20731 TUL - FOUND CORROSION ON UPPER AND LOWER TRAILING EDGE BEAMS, HORIZ STAB UPPER FROM 196 TO 201 ELEVATOR STATION LOWER FR OM ELEVATOR STATION 21 TO 29, RIGHT SIDE. REPAIRED PER ESO 11697, DATED 4/9/96. REFERENCE AALA960598. 2 L 7 3 4F A3WE 1996052300568 19960523 00568 NM 1996 5 23 96ZZZM849 1 19960329 A 2410 735511A CSD BOEING 737 7373Q8 1384670 NM GEAR BOX CONTAMINATED B RJEY O OTHER J H WARNING INDICATION ELECT. POWER LOSS-50 PC DE DESCENT 1 SO 23 373TA 6822 26283 FLT 690 - SAL/MST/SFO - DESCENDING AT MAZATLAN, NR 1 GEN OFF BUS, BUSS OFF, AND HIGH OIL TEMP LIGHTS CAME ON. AT THIS T IME, THE APU WAS DEFERRED AS PER MEL 49-1. DURING GROUND INSPECTION, CHIP DETECTOR METAL IN THE CSD AND THE CSD OIL COO LER WERE FOUND CONTAMINATED. AS CORRECTIVE ACTION, CSD NR 1 WAS REPLACED AS PER MM 24-21-11. AFTER THIS, THE AIRPLANE WAS RETURNED TO OPERATION. 2 L 7 2 4F RT A16WE 1996052300569 19960523 00569 WP 1996 5 23 96ZZZM850 1 19960411 A 2410 696233B CSD DOUG DC9 DC932 3022066 WP RT ENGINE MALFUNCTIONED A VJ6A A UNSCHED LANDING O OTHER CL CLIMB 1 SO 11 938VV 47442 FLT 383 - BOS-B0S - AIR RETURN, DUE TO RIGHT GEN FLUCTUATES ON AND OFF AFTER TAKEOFF. APU PREVIOUSLY ON MEL. ASSIGNED MEL TO RIGHT GEN AND CLEARED MEL ON APU. REMOVED ADN REPLACED NR 2 CSD PER VJ MM 24-10-1. 2 L 7 2 4F A6WE 1996052300570 19960523 00570 WP 1996 5 23 96ZZZM851 1 19960411 A 2421 GENERATOR DOUG DC9 DC932 3022066 WP RT ENG MALFUNCTIONS A VJ6A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 938VV 47442 FLT NR 383 - BOS-BOS - AIR RETURN, DUE TO RIGHT GEN FLUCTUATES ON AND OFF AFTER TAKEOFF. APU PREVIOUSLY ON MEL. ASSIGN ED MEL TO RIGHT GEN AND CLEARED MEL ON APU. 2 L 7 2 4F A6WE 1996052300571 19960523 00571 WP 1996 5 23 96ZZZM852 1 19960421 A 7722 EGT INDICATOR DOUG DC9 DC932 3022066 WP NR 2 ENG FAILED A VJ6A A UNSCHED LANDING O OTHER CL CLIMB 1 SO 11 938VV 47442 FLT 498 - ATL-ATL - AIR RETURN, THE NR 2 EGT WENT INOP. REMOVED AND REPLACED NR 2 EGT INDICATOR PER VJ MM 77-20-00, OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996052300572 19960523 00572 1996 5 23 96ZZZM853 4 19960330 A 3421 285733513 VERTICAL GYRO DOUG DC9 DC932 3022066 WP RT COCKPIT FAILED A VJ6A K NONE O OTHER CL CLIMB 1 SO 11 931VV 47674 FLT NR 412 - ATL-ATL - AIR RETURN, FIRST OFFICERS ADI QUIT WORKING. REMOVED AND REPLACED FIRST OFFICERS VERTICAL GYRO. OPS IAW 34-20 GOOD. NO DEFECTS NOTED. 2 L 7 2 4F A6WE 1996052300573 19960523 00573 WP 1996 5 23 96ZZZM854 1 19960402 A 3260 0080004003 CONTROL BOX DOUG DC9 DC932 3022066 WP LT MLG FAILED A VJ6A A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 11 931VV 47674 FLT NR 360 - RDU-IAD - THE LEFT GEAR UNSAFE LIGHT INDICATION CAME ON DURING GEAR RETRACTION. CYCLED GEAR AND THE LIGHT STAYED ON, SAFE INDICATION ON APPROACH AND LANDING. TROUBLESHOT SYSTEM AND PERFORMED OPS CHECK. REMOVED AND REPLACED P ROXIMITY SWITCH CONTROL BOX. SYSTEM OPS CHECKS GOOD IAW DC-9 MM 32-30-0. 2 L 7 2 4F A6WE 1996052300574 19960523 00574 WP 1996 5 23 96ZZZM855 1 19960404 A 3260 UPLOCK SWITCH DOUG DC9 DC932 3022066 WP LT MLG OUT OF ADJUST A VJ6A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 11 931VV 47674 FLT NR 206 - MCO-MCO - AIR RETURN, AFTER TAKEOFF THE RED LEFT GEAR UNSAFE LIGHT REMAINED ON. RECYCLED GEAR, NO HELP, LI GHT REMAINED ON. GEAR DOOR OPEN LIGHT WAS OUT. REPAIRED AND ADJUSTED LEFT MLG UPLOCK PROXIMITY SWITCH SYSTEM. OPS CHE CKED OK IAW 32-10-0. 2 L 7 2 4F A6WE 1996052300575 19960523 00575 WP 1996 5 23 96ZZZM856 1 19960413 A 3260 PROX SWITCH DOUG DC9 DC932 3022066 WP NLG BROKEN WIRE A VJ6A O OTHER N FALSE WARNING AP APPROACH 1 SO 11 931VV 47674 DURING TEST FLIGHT FOR NOSE GEAR INDICATION PROBLEMS, RIGHT MAIN GEAR UNSAFE LIGHT REMAINED ON. GEAR POSITION VISUALLY VERIFIED. MAINTENANCE FOUND BROKEN WIRE ON RIGHT GEAR PROX SWITCH. MAINTENANCE REPAIRED WIRING SYSTEM GROUND CHECK GOO D. (M) 2 L 7 2 4F A6WE 1996052300576 19960523 00576 WP 1996 5 23 96ZZZM857 1 19960425 A 3260 GREEN LIGHT DOUG DC9 DC932 3022066 WP NLG MALFUNCTIONED A VJ6A L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 SO 11 930VV 47723 FLT NR 396 - PBI-BOS - THE NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE ON GEAR EXTENSION. EXECUTED MISSED APPROACH , NOSE LIGHT ILLUMINATED DURING CLIMB AND LANDED NORMALLY. CHECKED NOSE GEAR ASSEMBLY SWITCH, NO DEFECTS FOUND. 2 L 7 2 4F A6WE 1996052300580 19960523 00580 NM 1996 5 23 96ZZZM861 1 19960304 A 5320 69455963 GUSSETT BOEING 727 727290 138408W NM BS 825.95 CRACKED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 294AS 22146 DURING AD 94-02-04 REPETITIVE INSPECTION FOUND GUSSETT AT STATION 825.95 LEFT SIDE CRACKED. REPLACEMENT PART FABRICATED AND INSTALLED PER BOEING SB 727-53-0197, FIG 11 ON SBN NR B014219N00054. 2 L 7 3 4F A3WE 1996052300582 19960523 00582 NM 1996 5 23 96ZZZM863 1 19960229 A 5320 DOUBLER BOEING 727 727191 1384063 NM BS 1070 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 503MG 19392 FUSELAGE EXTERIOR HAS LEVEL 1 CORROSION AROUND FASTENER AT STATION 1070 STRINGER 10R AT DOUBLE REPAIR. CORROSION REMOVE D AROUND FASTENER, TREATED AREA PER SRM 51-10-6 AND 51-10-2 MATERIAL LOSS WITHIN LIMITS PER SRM 53-10-1. 2 L 7 3 4F A3WE 1996052300583 19960523 00583 NM 1996 5 23 96ZZZM864 1 19960311 A 5330 SKIN BOEING 727 727191 1384063 NM BS 481 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 503MG 19392 FOUND BS 481 SKIN THICKNESS LOSS 10 PERCENT AT MANY STRINGER STATIONS IN BETWEEN STRINGER 10L AND STRINGER 10R, CROWN AR EA INSPECTED PER AD 90-26-09. REMOVED AND REPLACED FASTENERS WITH OVERSIZE FASTENERS FROM STRINGER 2L TO 10L AND FROM S TRINGER 7R TO 10R PER SB 727-53-0084. SKIN REPAIRED FROM STRINGER 2L TO 4R ON NR 19N00043 AND FROM STRINGER 4R TO 7R ON NR 19N00039. 2 L 7 3 4F A3WE 1996052300584 19960523 00584 NM 1996 5 23 96ZZZM865 1 19960311 A 5330 SKIN BOEING 727 727191 1384063 NM BS 360 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 503MG 19392 FOUND BS 360 SKIN THICKNESS LOSS 10 PERCENT AT DIFFERENT STRINGER STATIONS IN BETWEEN STRINGER 10L AND STRINGER 10R, CRO WN AREA INSPECTED PER AD 90-26-09. REMOVED AND REPLACED FASTENERS WITH OVERSIZE FASTENERS FROM STRINGER 5R TO 10R AND F ROM STRINGER 5L TO 10L PER SB 727-53-0084. SKIN REPAIRED FROM STRINGER 5L TO 5R ON NR 19N00041. 2 L 7 3 4F A3WE 1996052300585 19960523 00585 NM 1996 5 23 96ZZZM866 1 19960311 A 5330 SKIN BOEING 727 727191 1384063 NM BS 481 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 503MG 19392 FOUND BS 481 AFT OF SPLIT SKIN. THICKNESS LOSS STRINGER R-4 TO R4 PLUS 8 INCHES PLUS 20 PERCENT, R4 PLUS 8 INCH TO R-5 20 PERCENT, STRINGER R-5 TO R5 PLUS 6 INCHES PLUS 10 PERCENT, R6 PLUS 6 INCH TO R6 PLUS 8 INCHES 10 PERCENT, STRINGER 6 PLUS 8 INCHES TO R7 PLUS 10 PERCENT STRINGER R7 TO R8 10 PERCENT, STRINGER R9 TO R-10 10 PERCENT. FABRICATED AND INSTAL LED DOUBLER, FILLER, AND FILLET SEALED PER SB 727-53-0084 AND DRAWING 69-62161 SHEET 1, 2, AND 5 FROM STRINGER 4R TO 7R STATION 481. 2 L 7 3 4F A3WE 1996052300586 19960523 00586 NM 1996 5 23 96ZZZM867 1 19960311 A 5313 SKIN BOEING 727 727191 1384063 NM BS 481 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 503MG 19392 FOUND BS 481 AFT OF SPLIT SKIN, THICKNESS LOSS STRINGER 1 PLUS 2 INCHES L TO 1 PLUS 3 INCHES R PLUS 10 PERCENT, STRINGER 1 PLUS 3L TO R2 PLUS 10 PERCENT, STRINGER R-2 TO R-2 PLUS 3 INCHES 10 PERCENT, R2 PLUS 3 INCHES TO R3 PLUS 8 INCHES PLU S 10 PERCENT, R3 PLUS 8 INCHES TO R4 20 PERCENT AS MARKED. FABRICATED AND INSTALLED REPAIR DOUBLER, FILLER, AND FILLET SEALED PER SB 727-53-0084 AND DRAWING 69-62161 SHEET 1, 2, AND 5 FROM STRINGER 2L TO 4R STATION 481. 2 L 7 3 4F A3WE 1996052300587 19960523 00587 NM 1996 5 23 96ZZZM868 1 19960311 A 5330 SKIN BOEING 727 727191 1384063 NM BS 360 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 503MG 19392 FOUND BS 360 AFT OF SPLIT SKIN THICKNESS LOSS STRINGER R3 TO R3 PLUS 8 INCHES 10 PERCENT, R3 PLUS 8 INCHES TO R4 20 PERC ENT, STRINGER R2 TO L2 PLUS 10 PERCENT, L2 TO L3 10 PERCENT, L3 PLUS 10 INCHES TO L4 20 PERCENT AS MARKED AND STRINGER R 2 TO R3 10 PERCENT. FABRICATED AND INSTALLED REPAIR DOUBLERS, FILLER, AND FILLET SEALED PER SB 727-53-0084 AND DWG 69-6 2161 SHEET 1, 3, AND 10 FROM STRINGER 5L TO 2L AND 2L TO 2R AND 2R TO 5R. 2 L 7 3 4F A3WE 1996052300588 19960523 00588 NM 1996 5 23 96ZZZM869 1 19960428 A 3350 90052 BATTERY CHARGER BOEING 727 727225 1384077 NM CABIN INOPERATIVE A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 361KP P2852 20627 FOUND LEFT OVERWING EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED POWER PACK AND BATTERY CHARGER ASSY. OPS CH ECKS GOOD. REFERENCE IXKA960024. 2 L 7 3 4F A3WE 1996052300589 19960523 00589 NM 1996 5 23 96ZZZM870 1 19960511 A 2611 302842 SMOKE DETECTOR BOEING 727 727222 1384073 NM CARGO COMPT FAILED A RYNA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 7639U 19912 DURING CRUISE FROM STL-DAY - THE MAIN CARGO SMOKE DETECTOR LIGHT ILLUMINATED. COMPLIED WITH EMERGENCY CHECKLISTS. AIRC RAFT LANDED IN DAY WITHOUT INCIDENT. NO EVIDENCE FO FIRE NOTED. REPLACED NR 2, NR 4, AND NR 6 SMOKE DETECTORS PER MM 2 6-10-0. OPS CHECKS NORMAL. (M) 2 L 7 3 4F A3WE 1996052300590 19960523 00590 NE 1996 5 23 96ZZZM871 2 19960421 A 7200 ENGINE BOEING 727 727225 1384077 NM PWA JT8 JT8D15A 52051 NE NR 1 FAILED A UHVA E ENGINE SHUTDOWN J WARNING INDICATION TO TAKEOFF 1 SO 11 805EA 35426 22436 7005910 ON TAKEOFF NR 1 ENGINE OIL BYPASS LIGHT CAME ON. BROUGHT THROTTLE BACK TO IDLE, ALL INDICATIONS NORMAL. AFTER CRUISE T HROTTLE WAS MOVED FROM IDLE AND OIL TEMP CLIMBED WITH THROTTLE MOVEMENT. THROTTLE RETARDED AND SHUT ENGINE DOWN FOR PRE CAUTION. WHEN AIRCRAFT ARRIVED, PULLED ENGINE OIL FILTERS. FOUND EXCESSIVE METAL IN SCREEN, SENT OIL OUT FOR ANALYSIS. RESULTS INDICATE BEARING FAILURE. REMOVED AND REPLACED NR 1 ENGINE. 2 L 7 3 4F 4 F A3WE E2EA 1996052300591 19960523 00591 NM 1996 5 23 96ZZZM872 1 19960426 A 5610 001A561A0000207 SIDE WINDOW SIERRACIN DORNER DO32 DO328100 2996000 NM RT CRACKED A EQGA I CABIN DEPRESSURIZATION O OTHER CR CRUISE 1 SW 19 335LS 2195 236 3035 WHILE EN ROUTE TO DFW FROM CUU, THE FIRST OFFICERS SIDE WINDOW CRACKED FROM BOTTOM TO TOP. THE AIRCRAFT LANDED AT DFW W ITHOUT FURTHER INCIDENT. IT WAS THEN FERRIED TO HOT UNPRESSURIZED WHERE THE WINDOW WAS REPLACED. NORMALLY, THESE WINDO WS HAVE BEEN DELAMINATING. THIS IS THE FIRST ONE THAT CRACKED. 2 H 7 2 4T RT A45NM 1996052300592 19960523 00592 1996 5 23 96ZZZM873 4 19960419 A 2210 177600151 CONTROLLER SP1510 DOUG DC8 DC8F54 3021926 WP AUTOPILOT OVERHEATED A FXLA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 19 426FB P305 45667 IN CRUISE EXPERIENCED O-ZONE ODOR AND INTERMITTENT SMOKE FROM BEHIND INSTRUMENT PANEL WHEN AUTO-PILOT WAS ENGAGED. GROU ND INSPECTION REVEALED AUTOPILOT CONTROLLER WAS SHORTED/OVERHEATED. REPLACED CONTROLLER AND AIRCRAFT RETURNED TO SERVIC E. 2 L 7 4 4F 4A25 1996052300593 19960523 00593 1996 5 23 AALA960425 4 19960320 A 2565 29984109 SLIDE DOUG DC9 DC982 3022082 WP PAX DOOR SCRAPPED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 LAX - DURING A SHOP OVER PRESSURE CHECK, FOUND THE EMERGENCY EVACUATION SLIDE TUBE TORN OPEN. SCRAPPED EMERGENCY EVACUA TION SLIDE. (M) 2 L 7 2 4F A6WE 1996052300594 19960523 00594 WP 1996 5 23 AALA960546 1 19960409 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 200-230 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 294AA 49306 TUL - FOUND NR 2 SEAT TRACK CORRODED, BLENDED BEYOND LIMITS. REMOVED BAD SECTION OF TRACK TO PRODUCTION SPLICE, INSTALL ED NEW TRACK SRM 53-05. (M) 2 L 7 2 4F A6WE 1996052300595 19960523 00595 WP 1996 5 23 AALA960562 1 19960410 A 5320 CUSP DOUG DC9 DC982 3022082 WP BS 1240-1243 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 409AA 49320 TUL - FOUND CORROSION ON BOTTOM SIDE OF CUSP, LEFT SIDE OF AIRCRAFT OVER BUTTERFLY OUTFLOW VALVE. INSTALLED CUSP DOUBLE R PER SRM 53-01, FIG 2 SHEET 2 AND 3. (M) 2 L 7 2 4F A6WE 1996052300596 19960523 00596 WP 1996 5 23 AALA960569 1 19960410 A 3260 833708 SENSOR ELDEC DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 415AA 49326 DFW - FLT 2233 - EN ROUTE ORD/DFW - DURING CRUISE, NOSE LANDING GEAR UNSAFE LIGHT ILLUMINATED EACH TIME AIRCRAFT MADE A TURN. NO OTHER ABNORMAL INDICATIONS AND AIRCRAFT PROCEEDED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING G EAR UPLOCK SENSOR. ACCOMPLISHED NOSE LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996052300597 19960523 00597 WP 1996 5 23 AALA960571 1 19960410 A 5320 99365347 ANGLE DOUG DC9 DC982 3022082 WP BS 160-200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 259AA 49289 TUL - FOUND CORROSION ON FLOOR BOARD SUPPORT ANGLE FORWARD OF NR 1 SEAT TRACK, STATION 160 TO 200. REMOVED AND REPLACED FLOOR SUPPORT ANGLE, REF NR 658 0073684. (M) 2 L 7 2 4F A6WE 1996052300598 19960523 00598 WP 1996 5 23 AALA960573 1 19960411 A 5320 99365347 ANGLE DOUG DC9 DC982 3022082 WP BS 200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 294AA 49306 TUL - ANGLE HAS CORROSION STATION 200 INBOARD OF BELL FRAME SAME STATION. REPLACED WITH NEW ANGLE PER SRM. (M) 2 L 7 2 4F A6WE 1996052300599 19960523 00599 WP 1996 5 23 AALA960581 1 19960411 A 5320 CUSP DOUG DC9 DC982 3022082 WP BS 1174 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 409AA 49320 TUL - FOUND STATION 1174 LEFT BOTTOM OF CUSP MEMBRANE HAS CORROSION. REMOVED CORROSION AND DAMAGED AREA. INSTALLED DOU BLER REPAIR PER SRM 53-01, FIG 2. (M) 2 L 7 2 4F A6WE 1996052300600 19960523 00600 NM 1996 5 23 AALA960582 1 19960412 A 5512 SKIN BOEING 727 727227 1384078 NM HORIZ STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 723AA 20731 TUL - FOUND LOWER TRAILING EDGE HORIZ STABILIZER SKIN CORRODED. CUT OUT CORROSION AND REPAIRED PER ESO 11677 DATED 4/9/ 96. (M) 2 L 7 3 4F A3WE 1996052300601 19960523 00601 NM 1996 5 23 AALA960583 1 19960412 A 5510 BEAM BOEING 727 727227 1384078 NM HORIZ STAB TE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 723AA 20731 TUL - FOUND CORROSION ON HORIZ STAB TRAILING EDGE BEAM, 8 INCHES INBOARD OF END OF TOP BEAM. REMOVED CORRODED AREA AND INSTALLED DOUBLER PER ESO 11697 DATED 4-9-96. (M) 2 L 7 3 4F A3WE 1996052300602 19960523 00602 NM 1996 5 23 AALA960584 1 19960412 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 480-520 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 879AA 21391 TUL - REMOVED CORRODED STRINGER AND INSTALLED NEW STRINGER AND DOUBLERS PER 53-10-3. (M) 2 L 7 3 4F A3WE 1996052300603 19960523 00603 NM 1996 5 23 AALA960585 1 19960412 A 5330 SKIN BOEING 727 727223 1384074 NM BS 680 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 879AA 21391 TUL - FOUND CORROSION ON SKIN BUTT JOINT AFT SIDE FRAME 680, STRINGER 28L TO 28R. REMOVED CORROSION PER SRM CHAP 51-10- 6. INSTALLED DOUBLER IAW SRM 53-30-3 P14D. DOUBLER MANUFACTURED FROM .07 INCH 2024-T3. (M) 2 L 7 3 4F A3WE 1996052300604 19960523 00604 WP 1996 5 23 AALA960586 1 19960412 A 5531 SPAR DOUG DC9 DC982 3022082 WP VERT STAB CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 294AA 49306 TUL - FOUND CRACK IN FWD VERT STAB LEFT SPAR LEG ON AFT SIDE OF STATION 1388 CANT FRAME IN AFT ACCY. STOP DRILLED CRACK MANUFACTURED DOUBLER AND INSTALLED PER ESO 80559, DATED 4-12-96. (M) 2 L 7 2 4F A6WE 1996052300605 19960523 00605 NM 1996 5 23 AALA960597 1 19960512 A 5720 ANGLE BOEING 727 727227 1384078 NM WS 750 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 723AA 20731 TUL - FOUND CORROSION ON FRONT SPAR LOWER CHORD ANGLE UNDER LEADING EDGE PANEL. REMOVED CORROSION AND INSTALLED CHORD A NGLE REPAIR PER SRM 57-30-2 PAGES 1-3 FIG 1. (M) 2 L 7 3 4F A3WE 1996052300606 19960523 00606 NM 1996 5 23 AALA960598 1 19960412 A 5510 65245712 UPPER TE BEAM BOEING 727 727227 1384078 NM HORIZ STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 723AA 20731 TUL - FOUND CORROSION ON UPPER AND LOWER TRAILING EDGE BEAMS, HORIZ STAB UPPER FROM 196 TO 201 ELEVATOR STATION LOWER FR OM ELEVATOR STATION 21 TO 29, RIGHT SIDE. REPAIRED PER ESO 11697, DATED 4/9/96. (M) 2 L 7 3 4F A3WE 1996052300607 19960523 00607 WP 1996 5 23 AALA960602 1 19960416 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 435 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 406A 49317 TUL - FOUND CORROSION ON FRAME BETWEEN L-26R AND 27R, STATION 435. REPAIRED PER ESO 80559, DATED 4-17-96. (M) 2 L 7 2 4F A6WE 1996052300608 19960523 00608 NM 1996 5 23 AALA960604 1 19960418 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 366AA 25193 MIA - DURING OVERNIGHT CHECK, EMERGENCY LIGHT INOPERATIVE IN BUSINESS CLASS CABIN LEFT SIDE ROWS 7 THROUGH 12 AND IN MAI N CABIN LEFT SIDE ROWS 37 THROUGH 42. RESECURED LOOSE EMERGENCY LIGHT WIRES AT ROW 12 AND ROW 42. SYSTEM GROUND CHECKE D NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1996052300609 19960523 00609 WP 1996 5 23 AALA960605 1 19960417 A 3350 A3060698101 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 493AA 49731 ORD - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 3 AND 6 INOPERATIVE. RESECURED LOOSE EMERGEN CY FLOOR LIGHT CONNECTOR BY PAX SEAT ROW 3. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996052300610 19960523 00610 NE 1996 5 23 AALA960606 2 19960417 A 7314 384300 FUEL PUMP DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE RT ENGINE DEFECTIVE A AALA A E UNSCHED LANDING ENGINE SHUTDOWN X ENGINE FLAMEOUT CL CLIMB 1 SW 07 14551 53033 ORD - FLT 1236 - AFTER TAKEOFF ORD DURING INITIAL CLIMB, RIGHT ENGINE EXPERIENCED FLAME OUT. ACCOMPLISHED ENGINE SHUTDO WN PROCEDURE AND AIRCRAFT RETURNED TO ORD, LANDING WITHOUT INCIDENT. REPLACED RIGHT ENGINE FUEL PUMP AND FUEL CONTROL. ACCOMPLISHED LEAK CHECK AND GROUND ENGINE RUN WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F 4 F A6WE E9NE 1996052300611 19960523 00611 WP 1996 5 23 AALA960609 1 19960418 A 3350 LIGHT STRIP DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 510AM 49804 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT STRIP AT AFT CABIN HAD LIGHTS UNDER EXIT PLACARD INOPERATIVE. REPLA CED EMERGENCY FLOOR LIGHT STRIP AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996052300612 19960523 00612 NM 1996 5 23 AALA960610 1 19960418 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 359AA 24040 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEATS 17H AND 17J INOPERATIVE. REPAIRED BROKEN EMERGENCY EXIT LIGHT WIRING AT SEAT 17H AND J LOWER SEAT CONNECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1996052300613 19960523 00613 NM 1996 5 23 AALA960611 1 19960418 A 3260 AAP2448A ACCESSORY UNIT BOEING 727 727223 1384074 NM LANDING GEAR DEFECTIVE A AALA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 878AA 21390 DFW - FLT 1176 - EN ROUTE CUN/DFW - DURING CRUISE, LEFT MAIN LANDING GEAR WARNING LIGHT ILLUMINATED. ALL GEAR DOOR WARN ING LIGHTS REMAINED OUT. NO OTHER ABNORMAL INDICATIONS AND AIRCRAFT PROCEEDED TO DFW AND LANDED WITHOUT INCIDENT. REPL ACED LANDING GEAR ACCESSORY UNIT. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHEC KED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996052300614 19960523 00614 WP 1996 5 23 AALA960614 1 19960419 A 3260 S189 SWITCH DOUG DC9 DC982 3022082 WP LDG GEAR LEVER DEFECTIVE A AALA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 7542A 49996 DFW - FLT 2034 - DURING APPROACH TO DFW WHEN LANDING GEAR EXTENDED, GEAR UNSAFE LIGHT ILLUMINATED WITH NO ABNORMAL HYDRA ULIC QUANTITY OR PRESSURE INDICATIONS. RECYCLED LANDING GEAR AND LANDING GEAR EXTENDED AND LOCKED NORMALLY. AIRCRAFT L ANDED DFW WITHOUT INCIDENT. REPLACED LANDING GEAR LEVER SWITCH S1-89. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996052300615 19960523 00615 NM 1996 5 23 AALA960615 1 19960420 A 3350 STB1304 LIGHT BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 712AA 22468 DFW - DURING OVERNIGHT CHECK, EMERGENCY LIGHT AT FORWARD GALLEY DOOR INOPERATIVE. REPLACED EMERGENCY LIGHT AT FORWARD G ALLEY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996052300616 19960523 00616 WP 1996 5 23 AALA960619 1 19960422 A 3350 A3060733101 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7539A 49993 ORD - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AFT OF PAX SEAT ROW 21F INOPERATIVE. REPLACED BROKEN EMERGENCY FLO OR LIGHT CONNECTOR BY PAX SEAT ROW 21F. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996052300617 19960523 00617 NM 1996 5 23 ASAA9610048 1 19960411 A 5315 65549102 FLOOR BEAM BOEING 737 737298C 1384490 NM BS 867 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING C-CHECK, CORROSION WAS FOUND ON THE FLOOR BEAM BS 867, LBL 10 ON THE LOWER SURFACE OF THE LOWER FORWARD FLA NGE. THE CORROSION IS CONCENTRATED AROUND THE FASTENER HOLES. REPAIRED PER EA 5310-01432 AND BOEING TELEX ASA-SEA-96-0 170RR. (M) 2 L 7 2 4F RT A16WE 1996052300618 19960523 00618 NM 1996 5 23 ASAA9610049 1 19960411 A 5315 65549051 FLOOR BEAM BOEING 737 737298C 1384490 NM BS 400 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING C-CHECK, CORROSION WAS FOUND ON THE FLOOR BEAM BS 400, LBL 51 ON THE LOWER SURFACE OF THE LOWER AFT FLANGE. THE CORROSION IS CONCENTRATED AROUND THE FASTENER HOLES USED TO SECURE THE CEILING PANEL. REPAIRED PER EA 5310-10433 AND BOEING TELEX ASA-SEA-96-0176RR. (M) 2 L 7 2 4F RT A16WE 1996052300619 19960523 00619 NM 1996 5 23 ASAA9610057 1 19960428 A 3230 65446916 MODULE BOEING 737 737290C 138448V NM NLG MALFUNCTIONED A ASAA O OTHER J WARNING INDICATION AP APPROACH 1 NM 01 742AS 23136 SEA - FLT 896 - DURING APPROACH CREW REPORTED THAT THE NOSE LANDING GEAR FAILED TO EXTEND ON FIRST ATTEMPT. RECYCLED AN D GEAR EXTENDED NORMALLY. LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR MODULE, PERFORMED GEAR RETRACTION AND GE AR OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1996052300620 19960523 00620 NM 1996 5 23 ASAA9610058 1 19960429 A 3350 6013211 BATTERY PACK BOEING 737 737290C 138448V NM CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING MAINTENANCE CHECK, THE RIGHT EXTERIOR OVERWING AND AFT WING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1996052300621 19960523 00621 NM 1996 5 23 ASAA9610059 1 19960429 A 5210 507945178 DOOR BOEING 737 737290C 138448V NM L1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 730AS 22577 SEA - FLT NR 64 - L1 DOOR DIFFICULT TO OPEN AND CLOSE. ADJUSTED UPPER HINGE GUIDE ARM, LUBRICATED UPPER AND LOWER HINGE FITTINGS AND ALL LATCH CAM ROLLERS. DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1996052300622 19960523 00622 NM 1996 5 23 ASAA9610060 1 19960428 A 3350 RPS1B BATTERY PACK BOEING 737 737298C 1384490 NM NR 6 PALLET DISCHARGED A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 745AS 20794 ANC - FLT 20 - DURING RECON, SEVERAL FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK IN NR 6 PAL LET RECEIVER AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996052300623 19960523 00623 NM 1996 5 23 ASAA9610061 1 19960505 A 5210 507945178 DOOR BOEING 737 737210C 1384459 NM L1 DOOR LACK OF LUBE A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 743AS 21821 SEA - FLT 64 - CREW REPORTED, THAT THE L-1 DOOR WAS HARD TO CLOSE. INSPECTED, CLEANED, AND LUBED DOOR. DOOR OPERATED N ORMALLY. (M) 2 L 7 2 4F A16WE 1996052300624 19960523 00624 NM 1996 5 23 ASAA9640033 1 19960424 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 772AS 25105 SEA - DURING MAINTENANCE CHECK, THE AFT 3 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED W IRES/LIGHTS AND THE LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996052300625 19960523 00625 NM 1996 5 23 ASAA9640034 1 19960425 A 3350 S417N50914 LAMP BOEING 737 7374Q8 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 763AS 25100 SEA - DURING MAINTENANCE CHECK, THE FIRST TWO RED EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPIN NED LAMP ASSY AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996052300626 19960523 00626 EU 1996 5 23 ASAA9640036 2 19960503 A 7321 8063210 MEC BOEING 737 7374Q8 NM CFMINT CFM56 CFM563C1 13802 EU NR 1 ENGINE MALFUNCTIONED A ASAA H DEACTIVATE SYST/CIRCUITS X ENGINE FLAMEOUT AP APPROACH 1 NM 01 763AS 25100 6256 PVR - FLT 110 - ON ARRIVAL, CREW REPORTED THE NR 1 ENGINE FLAMED OUT DURING DESCENT AT 15,000 FEET. ACCOMPLISHED ENGINE FAILURE/SHUTDOWN AND INFLIGHT START CHECK LIST. ENGINE RESTARTED NORMALLY AND LANDED WITHOUT INCIDENT. AT THE TIME OF FLAME OUT, THE AIRCRAFT HAD BEEN AT IDLE THRUST FOR 10 MINUTES DURING THE DESCENT. ACCOMPLISHED EXTENSIVE TROUBLE SHOO TING PER TSR 0900041, PERFORMED GROUND RUN UP AND NO TROUBLE WAS FOUND. FERRIED AIRCRAFT TO SEA AND REPLACED NR 1 ENGIN E MAIN ENGINE CONTROL AS PRECAUTIONARY, ENGINE OPERATED NORMALLY. (M) 2 L 7 2 4F 4 F RT A16WE E21EU 1996052300627 19960523 00627 NM 1996 5 23 ASAA9640037 1 19960506 A 3397 WIRE BOEING 737 7374Q8 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 772AS 25105 SEA - DURING MAINTENANCE CHECK, SEVERAL EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE FROM ROW 22 TO TH E AFT CABIN. RECONNECTED WIRES AT FEED THROUGH FROM BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996052300628 19960523 00628 WP 1996 5 23 ASAA9680095 1 19960411 A 3260 H141009 DOWNLOCK SWITCH DOUG DC9 DC983 3022083 WP NLG DEFECTIVE A ASAA O OTHER N FALSE WARNING AP APPROACH 1 NM 01 973AS 53449 PDX - FLT 433 - CREW REPORTED, THE NOSE LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GER EXTENDED FOR LANDING. A CCOMPLISHED GEAR UNSAFE LIGHT CHECK LIST AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR DOWNLOCK SWITCH S1-412 AND ACCOMPLISHED RETRACTION/EXTENSION TEST AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996052300629 19960523 00629 WP 1996 5 23 ASAA9680105 1 19960423 A 5240 4954341501 SPRING DOUG DC9 DC983 3022083 WP L2 DOOR BROKEN A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 962AS 53076 LAX - PRIOR TO DEPARTURE OF FLT 256, CREW REPORTED THE L2 DOOR WOULD NOT CLOSE. REPLACED BROKEN DOOR BAYONET SPRING AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996052300630 19960523 00630 WP 1996 5 23 ASAA9680106 1 19960425 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 935AS 49236 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 6 TO 9 WERE FOUND INOPERATIVE. REPAIRED BROK EN WIRE AT ROW 6 AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996052300631 19960523 00631 1996 5 23 ASAA9680107 4 19960425 A 2565 D29984103 SLIDE ASSY DOUG DC9 DC983 3022083 WP TAILCONE FAILED TEST A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 976AS 53452 OAK - DURING C-CHECK, THE TAILCONE EMERGENCY EVACUATION SLIDE FAILED LIGHT TEST. REMOVED AND REPLACED THE TAILCONE EMER GENCY EVACUATION SLIDE. (M) 2 L 7 2 4F RT A6WE 1996052300632 19960523 00632 WP 1996 5 23 ASAA9680108 1 19960426 A 3350 20131A BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 942AS 53052 SFO - DURING SERVICE CHECK, THE AISLE EMERGENCY EXIT LIGHTS AT THE FORWARD AND AFT OVERHEAD PANELS WOULD GO DIM AFTER TW O MINUTES. REPLACED TWO BATTERY PACKS AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996052300633 19960523 00633 WP 1996 5 23 ASAA9680109 1 19960426 A 3222 5958412511 STRUT DOUG DC9 DC983 3022083 WP NLG REQ'D SERVICE A ASAA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 NM 01 973AS 53449 LAX - FLT NR 524 - THE NOSE LANDING GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR HANDLE WAS RAISED DURING TAKEO FF AT SAN. THE NOSE GEAR INDICATOR PIN IN THE COCKPIT RETRACTED, BUT CONSIDERABLE AIRSTREAM NOISE WAS EVIDENT IN NOSE A REA. RECYCLED LANDING GEAR AND LIGHT REMAINED ILLUMINATED. DIVERTED TO LAX AND LANDED WITHOUT INCIDENT. FOUND NOSE STR UT LOW. INSPECTED NOSE GEAR UP POSITION SENSOR AND FOUND TO BE WITHIN TOLERANCES. SERVICED NOSE GEAR STRUT, PERFORMED GEAR RETRACTION AND SYSTEM OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996052300634 19960523 00634 WP 1996 5 23 ASAA9680110 1 19960427 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP L1 DOOR INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 947AS 53020 SEA - DURING MAINTENANCE CHECK, THE L1 DOOR PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996052300635 19960523 00635 WP 1996 5 23 ASAA9680111 1 19960428 A 3397 WIRE DOUG DC9 DC982 3022082 WP AFT BATTERY PACK DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 967AS 49103 SEA -DURING MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHTS IN THE TAILCONE ALONG THE SIDE OF THE CATWALK AND AT THE RELEAS E HANDLE WERE FOUND INOPERATIVE. REPAIRED DAMAGED WIRE AT AFT BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996052300636 19960523 00636 WP 1996 5 23 ASAA9680112 1 19960429 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP L1 DOOR INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 934AS 49235 PDX - DURING MAINTENANCE CHECK, THE L-1 DOOR PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED LIGHT ASSEMBLY AN D OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996052300637 19960523 00637 SO 1996 5 23 ASOA96013 1 19960415 A 2910 12035015009 HYDRAULIC LINE EMB 120 EMB120RT SO RT ENGINE CHAFFED A ASOA H DEACTIVATE SYST/CIRCUITS J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SO 11 215AS 120010 DURING CRUISE FLIGHT ROA-ATL, AIRCRAFT LOST BLUE HYDRAULIC SYSTEM PRESSURE. THE CREW SHUT OFF THE ELECTRIC DRIVEN PUMP AND ADVISED ATC, WHO DECLARED AN EMERGENCY. THE AIRCRAFT LANDED ZERO FLAPS IN ATL SAFELY AND WITHOUT INCIDENT. REMOVED AND REPLACED THE RIGHT MAIN PUMP PRESSURE LINE AND SERVICED THE RIGHT RESEVOIR. OPERATIONAL CHECKS WERE GOOD AND THE A IRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1996052300638 19960523 00638 NM 1996 5 23 AWXA960194 1 19960417 A 5240 SERVICE DOOR BOEING 737 737275 1384485 NM RIGHT OUT OF ADJUST A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 CGAPW 20922 PAE - FLT 3710 - AIR TURNBACK. R-2 AFT SERVICE DOOR LIGHT CAME ON CLIMBING OUT OF 29,500 FEET. REMOVED LINER, ADJUSTED UPPER AND LOWER GATES, ADJUSTED TIMING PER MM 52-41-0. REINSTALLED LINER, PRESSURIZED AIRCRAFT. OPS CHECK GOOD. ACFT TT: 60,705 HRS. ACFT TC: 66,781. (X) 2 L 7 2 4F A16WE 1996052300639 19960523 00639 NE 1996 5 23 AWXA960195 2 19960418 A 7320 714810 PRESS/DUMP VLV BOEING 737 737277 1384570 NM PWA JT8 JT8D15 52051 NE NR 1 ENG FAILED A AWXA A UNSCHED LANDING J R WARNING INDICATION PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 28 187AW 24399 7521 6153280 22654 PHX - FLT 630 - COULD NOT MAKE FULL TAKEOFF POWER, NR 2 =2.14, NR 1=2.08. REMOVED AND REPLACED PRESSURIZING AND DUMP VA LVE PER IAW R5M73008. LEAK CHECK GOOD. (M) 2 L 7 2 4F 4 F RT A16WE E2EA 1996052300640 19960523 00640 NM 1996 5 23 AWXA960196 1 19960416 A 5315 65C3453721 FLOOR BEAM BOEING 737 737275 1384485 NM BS 669 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 CGAPW 20922 PAE - FLT 3802 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CRACK ON FLOOR BEAM BS 669, LBL 25, WL 205. REPL ACED CHANNEL PER SB 727-57-1139. (M) 2 L 7 2 4F A16WE 1996052300641 19960523 00641 NM 1996 5 23 AWXA960197 1 19960410 A 5320 693535214 CLIP BOEING 737 737275 1384485 NM BS 440 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 CGAPW 20922 PAE - FLT 3802 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CRACKED STRINGER CLIP AT BS 440, STRINGER 27L. R EPLACED CRACKED STRINGER CLIP, SRM REF 51-10-01, 51-10-02. (M) 2 L 7 2 4F A16WE 1996052300642 19960523 00642 NM 1996 5 23 AWXA960198 1 19960411 A 5315 FLOOR BEAM BOEING 737 737275 1384485 NM BS 678 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 CGAPW 20922 PAE - FLT 3802 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CRACK ON FLOOR BEAM BS 678, RBL 25, WL 205. REMO VED CRACKED DOUBLER BS 678, RBL 25, WL 205. FABRICATED NEW DOUBLER, ALODINED AND PRIMED. INSTALLED NEW DOUBLE ONTO AIR CRAFT. ALL WORK DONE IAW SERVICE BULLETIN 737-57-1139. (M) 2 L 7 2 4F A16WE 1996052300643 19960523 00643 NM 1996 5 23 AWXA960199 1 19960411 A 5711 SPAR CHORD BOEING 737 737275 1384485 NM BS 663 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 CGAPW 20922 PAE - FLT 3802 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CRACK ON FORWARD UPPER SPAR CHORD AT BS 663, LBL 24, WL 201. REMOVED DAMAGED SECTION AND REPAIRED IAW, AWA ER 2-53-13-34. (M) 2 L 7 2 4F A16WE 1996052300644 19960523 00644 NM 1996 5 23 AWXA960202 1 19960414 A 5753 891361 RIB BOEING 737 737275 1384485 NM TE FLAP CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 CGAPW 20922 PAE - FLT 3802 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CRACK ON THE LEFT INBOARD FLAP FORWARD RIB AT WIN G BL 82.58 ON THE LOWER FLANGE. REMOVED CRACKED RIB AND REPLACED WITH SERVICEABLE RIB IAW SRM 51-30-02. (M) 2 L 7 2 4F A16WE 1996052300645 19960523 00645 NM 1996 5 23 AWXA960203 1 19960414 A 5311 FRAME BOEING 737 737275 1384485 NM BS 500 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 CGAPW 20922 PAE - FLT NR 3802 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CRACK IN FRAME BS 500, RBL 25, WL 154. REMOVE D DAMAGED AREA. FABRICATED AND INSTALLED REPAIR PARTS, IAW SRM 51-40-03. (M) 2 L 7 2 4F A16WE 1996052300646 19960523 00646 NM 1996 5 23 AWXA960204 1 19960416 A 5315 FLOOR BEAM BOEING 737 737275 1384485 NM BS 708 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 CGAPW 20922 PAE - FLT 3802 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CRACK ON LONGITUDINAL FLOOR BEAM BS 708, BL 07, W L 202. REMOVED FASTENERS AND CUT DAMAGED SEALANT FROM LONGITUDINAL BEAM. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-40-02. (M) 2 L 7 2 4F A16WE 1996052300647 19960523 00647 NM 1996 5 23 AWXA960205 1 19960417 A 5320 65C352421 DOOR FRAME BOEING 737 737275 1384485 NM BS 440 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 CGAPW 20922 PAE - FLT 3802 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND FORWARD CARGO DOOR, FORWARD FRAME CRACKED AT STRI NGER 21R AND 23R. REMOVED AND REPLACED FORWARD DOOR FRAME BS 440, STRINGER 18R TO 26R, IAW SRM 51-20-04. (M) 2 L 7 2 4F A16WE 1996052300648 19960523 00648 NM 1996 5 23 AWXA960206 1 19960417 A 5320 65C352427 DOOR FRAME BOEING 737 737275 1384485 NM BS 492 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 CGAPW 20922 PAE - FLT 3802 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND FORWARD CARGO DOOR, AFT FRAME CRACKED AT STRINGER 14. REMOVED AND REPLACED AFT DOOR FRAME BS 492, STRINGER R18R TO 26R, IAW SRM 51-20-04. (M) 2 L 7 2 4F A16WE 1996052300649 19960523 00649 NM 1996 5 23 AWXA960207 1 19960417 A 5315 FLOOR BEAM BOEING 737 737275 1384485 NM BS 669 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 CGAPW 20922 PAE - FLT 3802 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CRACK ON FLOOR BEAM BS 669, LBL 28, WL 208, (LBL 25 LONGITUDINAL BEAM CRACKS EMANATING FROM OVER CUTOUTS BS 665 TO BS 678). STOP DRILLED CRACK TIPS AND REPAIRED IAW, AW A ER NR 2-57-12-10, BOEING TELEX TCO-PAN-96-0493RR. (M) 2 L 7 2 4F A16WE 1996052300650 19960523 00650 NM 1996 5 23 CAL960337 1 19960314 A 3350 10617844 POWER SUPPLY BOEING 727 727227 1384078 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 76752 21248 FLT NR 1852 - LAX - INSPECTION FOUND THE LEFT CENTER OVERWING EXTERIOR EMERGENCY LIGHT INOPERATIVE. THE BATTERY POWER S UPPLY WAS REMOVED AND REPLACED. (M) 2 L 7 3 4F A3WE 1996052300651 19960523 00651 NM 1996 5 23 CAL960511 1 19960421 A 3260 SWITCH BOEING 737 737130 1384435 NM RT MLG DOWNLOCK INOPERATIVE A CALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SW 09 16201 65836 19018 FLT NR 234 - EWR - RIGHT MAIN LANDING GEAR RED UNSAFE LIGHT ILLUMINATED, AFTER GEAR LOWERED DURING APPROACH FOR LANDING. CYCLED GEAR, RED AND GREEN LIGHT FLICKERED ALTERNATELY DURING SECOND APPROACH. FOUND RIGHT DOWNLOCK SENSOR AT FAULT, REPLACED SAME PER MX MAN 32-61-31. (M) 2 L 7 2 4F A16WE 1996052300652 19960523 00652 NM 1996 5 23 CAL960512 1 19960420 A 3350 110049 POWER SUPPLY BOEING 727 727224 1384076 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 93738 60249 20666 DEN - EMERGENCY AISLE LIGHT ROW 23 AND AFT INOPERATIVE. REPLACED AFT BATTERY CHARGER AND REPAIRED SPLICE AT SERVICE DOO R, CHECKS GOOD. (M) 2 L 7 3 4F A3WE 1996052300653 19960523 00653 NM 1996 5 23 CAL960513 1 19960420 A 5753 FLAP FAIRING BOEING 727 727224 1384076 NM RT TE FLAP DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 66734 62796 20663 FLT NR 663 - EWR - RIGHT OUTBOARD FLAP TRACK FAIRING (AFT SECTION) HAS DENT. REMOVED AND REINSTALLED FAIRING. OPS CHEC K GOOD. (M) 2 L 7 3 4F A3WE 1996052300654 19960523 00654 NM 1996 5 23 CAL960514 1 19960422 A 3232 DOOR ACTUATOR BOEING 727 727227 1384078 NM RT MLG CRACKED A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 09 15774 53920 21242 FLT 281 - EWR - ON TAKEOFF AFTER RAISING GEAR HANDLE, SYSTEM 'A' HYDRAULIC QUANTITY DROPPED TO ZERO AND PRESSURE FLUCTUA TED BETWEEN 0/3000 PSI RAN APPROPRIATE CHECK LISTS AND RETURNED TO EWR. OPERATED HYDRAULIC SYSTEM AND FOUND RIGHT GEAR DOOR ACTUATOR HOUSING CRACKED, REPLACED PER MM 32-32-81 AND CHECKED GOOD. CYCLED ALL SYSTEMS AND FILLED RESERVOIR TO FU LL. (M) 2 L 7 3 4F A3WE 1996052300655 19960523 00655 NE 1996 5 23 CAL960515 2 19960421 A 7250 T1 BLADE BOEING 737 737130 1384435 NM PWA JT8 JT8D7B 52053 NE NR 1 ENGINE BROKEN A CALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 09 14206 19023 655871 THE NR 1 ENGINE OIL PRESSURE READ 60 PSI, BUT FLUCTUATED PLUS OR MINUS 5 PSI AND WITHIN 30 SECONDS THE OIL TEMPERATURE B EGAN RISING RAPIDLY. THE ENGINE WAS SHUT DOWN AND RETURNED TO GSO. THE NR 1 ENGINE WAS REMOVED AND REPLACED. SHOP TEA R-DOWN FINDINGS REVEALED A BROKEN T1 BLADE CAUSED BY FOD. 2 L 7 2 4F 4 F A16WE E2EA 1996052300656 19960523 00656 WP 1996 5 23 CAL960516 1 19960417 A 3350 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 13512 45328 48111 GSO - THE FORWARD DROP CEILING EMERGENCY POWER SUPPLY SELF TEST ILLUMINATES ALL FLOOR TRACK LIGHTING INSTEAD OF 75 PERCE NT OF TRACK LIGHTING. FOUND DEFECTIVE DIODE AT OVERWING EXIT ROW. REPLACED DIODE IAW WDM 33-15-03. CHECKED SYSTEM OPE RATION PER DC-9 MM 33-53-0. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1996052300657 19960523 00657 WP 1996 5 23 CAL960517 1 19960418 A 5523 SKIN DOUG DC9 DC932 3022066 WP LT ELEV TAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13512 45328 48111 GSO - LEFT INBOARD ELEVATOR TAB T/E SKIN CRACKED AND DENTED. CRACK APPROXIMATELY .75 INCH. DENTED APPROXIMATELY 1.5 IN CH DIAMETER. PREPARED DAMAGED AREA FOR BONDING. BONDED DOUBLER TO REPAIR AREA. ALODINED, PRIMED, SEALED AND PAINTED R EPAIR AREA. WORK COMPLETED IAW DC9 SRM 51-70-2, 51-10-3, 51-20-0, AND 51-10-30. (M) 2 L 7 2 4F A6WE 1996052300658 19960523 00658 WP 1996 5 23 CAL960519 1 19960416 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 27509 46350 47798 HOU, -11 INTERCOSTAL FOUND WITH 1 INCH CRACK. REPAIRED PER SRM 52-05, FIG 45. (M) 2 L 7 2 4F A6WE 1996052300659 19960523 00659 WP 1996 5 23 CAL960520 1 19960418 A 5210 DOOR PAN DOUG DC9 DC932 3022066 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 27509 46350 47798 HOU - FOUND 1.5 INCH CRACK IN PAX DOOR PAN, FORWARD INBOARD CORNER. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER SRM 52-05, FIG 11. (M) 2 L 7 2 4F A6WE 1996052300660 19960523 00660 NM 1996 5 23 CAL960521 1 19960402 A 5330 SKIN BOEING 737 7372C0 1384488 NM BS 980 DISBONDED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10242 70340 20071 GSO - DISBOND FOUND AT 6TH WINDOW FORWARD OF STATION 980 LEFT 8 INCH AREA. ADDED FIELD FASTENERS AT DISBOND AND OVERSIZ E EXISTING FASTENERS AND INSTALLED PER SA004-5310-01827, SA007-5310-01827 AND JA5310-0182702001. (M) 2 L 7 2 4F A16WE 1996052300661 19960523 00661 NM 1996 5 23 CAL960523 1 19960406 A 5330 SKIN BOEING 737 7372C0 1384488 NM NLG WW CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10242 70390 20071 GSO - RIGHT OUTBOARD AFT CORNER OF NOSE WHEEL WELL UPPER PRESS. PANEL HAS SEVERE BULGING AROUND FASTENERS. REMOVED COR ROSION, INSTALLED DOUBLER PER CAL EA 5310-02452 OP 1. ALODINED AND PRIMED BARE METAL. (M) 2 L 7 2 4F A16WE 1996052300662 19960523 00662 NM 1996 5 23 CAL960524 1 19960402 A 5330 SKIN BOEING 737 7372C0 1384488 NM BS 727 DISBONDED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10242 70390 20071 GSO - DISBOND FOUND BETWEEN WINDOWS AT STATION 727 LEFT, 6 INCHES DISBOND AREA. DRILLED LOCATION FOR FIELD RIVETS AND O VERSIZED FASTENERS AND INSTALLED PER SA 004-5310-01827, SA 007-5310-01827, AND CAL CARD JA5310-0182702001. (M) 2 L 7 2 4F A16WE 1996052300663 19960523 00663 NM 1996 5 23 CAL960525 1 19960322 A 5330 SKIN BOEING 737 7372C0 1384488 NM BS 253.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10242 70390 20071 GSO - RIGHT FORWARD FUSELAGE OUTER SKIN BULGED AND RIVETS PULLING THROUGH JUST FORWARD OF BS 253.5 AT STRINGER 526R. RE MOVED DAMAGED SECTION OF SKIN, REMOVED RIGHT CHORD ANGLE. FABRICATED REPAIR DOUBLERS AND FILLERS. INSTALLED NEW RIGHT C HORD ANGLE AND SKIN FILLER AND DOUBLER PER B737 SRM 53-20-2 AND 52-30-2. (M) 2 L 7 2 4F A16WE 1996052300664 19960523 00664 NM 1996 5 23 CAL960526 1 19960409 A 5330 SKIN BOEING 737 7372C0 1384488 NM R1 DOOR CUTOUT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10242 20071 GSO - R1 DOOR CUTOUT, LOWER AFT CORNER CRACKED. CRACK APPROXIMATELY 1.5 INCH LONG. CUT OUT 1.5 INCH CRACK, FABRICATED REPAIR PARTS IAW B737 SRM 53-30-3 FIG 26. ALODINED AND PRIMED PER SRM 51-10-2. SEALED AND INSTALLED REPAIR IAW SRM 53- 30-3 FIG 26. SCUFF PLATE MODIFIED IAW B737 SRM 53-30-3 FIG 26. (M) 2 L 7 2 4F A16WE 1996052300665 19960523 00665 NM 1996 5 23 CAL960527 1 19960402 A 5320 BAC1517 STIFFENER BOEING 737 7372C0 1384488 NM BS 540 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10242 70390 20071 GSO - FOUND BS 540 STIFFENER RBL 26 CRACKED. APPROXIMATELY 1 INCH IN LENGTH. REMOVED CRACKED SUPPORT BEAM. FABRICATED NEW SUPPORT BEAM AND TAPERED SHIMS. INSTALLED SUPPORT BEAM AND SHIMS IAW B737 SRM 51-30-2. ALODINED AND PRIMED SUPPOR T AND SHIMS IAW SRM 51-10-2. (M) 2 L 7 2 4F A16WE 1996052300666 19960523 00666 WP 1996 5 23 GRAA9628 1 19960501 A 3350 079123 LENS DOUG DC9 DC987 3022087 WP CABIN MISSING A GRAA K NONE O OTHER IN INSP/MAINT 1 WP 11 1074T 49727 LINE MAINTENANCE AT ENV, DISCOVERED THE EMERGENCY FLOOR TRACK LIGHT AT ROW 18 WS MISSING LENS. MAINTENANCE REPLACED THE MISSING LENS. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM. NO DEFECTS NOTED. AIRCRAFT W AS RETURNED TO SERVICE. (M0 2 L 7 2 4F RT A6WE 1996052300667 19960523 00667 GL 1996 5 23 HALA9648 2 19960420 A 7200 ENGINE DOUG DC10 DC1010 3022110 WP GE CF6 CF6* 30020 GL LEFT FAILED A A HALA A J UNSCHED LANDING DUMP FUEL A N FLAME/FIRE FALSE WARNING TO TAKEOFF 1 WP 13 161AA 46942 LAX - FLT 3 - NR 1 ENGINE FAILED ON TAKEOFF AT GEAR RETRACTION, FIRE REPORTED BY ANOTHER AIRCRAFT. NO FIRE WARNING, FIR E WARNING TESTED NORMALLY ACCOMPLISHED ENGINE FAILURE CHECK LIST. RETURNED AFTER DUMPING FUEL. REMOVED AND REPLACED NR 1 ENGINE PER DK 719401. PERFORMED POWER ASSURANCE CHECK PER DK719518. OPS CHECK AND LEAK CHECK OK. (M) 2 L 7 3 4F 4 F A22WE E23EA 1996052300668 19960523 00668 NM 1996 5 23 IXKA960021 1 19960426 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8883Z 13251 21580 ON POST FLIGHT INSPECTION FOUND RIGHT AFT OVERWING HATCH LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BATTERY PACK. OP ERATIONALLY CHECKS GOOD. (M) 2 L 7 3 4F A3WE 1996052300669 19960523 00669 NM 1996 5 23 IXKA960022 1 19960426 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8883Z 18937 21580 ON POST FLIGHT INSPECTION FOUND RIGHT FORWARD OVERWING HATCH EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BAT TERY PACK. OPERATIONALLY CHECKS GOOD. (M) 2 L 7 3 4F A3WE 1996052300670 19960523 00670 NM 1996 5 23 IXKA960023 1 19960427 A 3350 08199000111 TRACK LIGHT BOEING 727 727224 1384076 NM CABIN INOPERATIVE A IXKA K NONE L NO TEST CR CRUISE 1 EA 25 32719 20388 INBOUND ITEM ON FLIGHT 46 TRACK LIGHTING COMING OUT OF FLOOR (NEAR ROW2). MAINTENANCE INSTALLED NEW 'E' PATH TRACK AND SECURED LENS. PERFORMED OPS CHECK, NO DEFECTS NOTED. (M) 2 L 7 3 4F A3WE 1996052300671 19960523 00671 NM 1996 5 23 IXKA960024 1 19960428 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 361KP 3595 20627 FOUND LEFT OVERWING EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED POWER PACK AND BATTERY CHARGER ASSY. OPS CH ECKS GOOD. (M) 2 L 7 3 4F A3WE 1996052300672 19960523 00672 NM 1996 5 23 IXKA960025 1 19960430 A 3350 P4010021 BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A IXKA K NONE L NO TEST CR CRUISE 1 EA 25 356PA 20626 FLT 44 - ATL - AFT FLASH LIGHT NO BLINKING. REMOVED AND REPLACED AFT FLASH LIGHT BATTERY PACK. (M) 2 L 7 3 4F A3WE 1996052300673 19960523 00673 NM 1996 5 23 IXKA960026 1 19960503 A 3397 WIRE BOEING 727 727225 1384077 NM CABIN DAMAGED A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 353PA 20622 MEL CI NR 050001-C FORWARD RED EMERGENCY PATH LIGHT OUT. MX TROUBLESHOT EMERGENCY TRACK LIGHT INOP, DUE TO BAD SPLICE A T PIGTAIL. REPAIRED SPLICE AND EMERGENCY PATH LIGHTS CHECK GOOD. (M) 2 L 7 3 4F A3WE 1996052300674 19960523 00674 EU 1996 5 23 M3HA96006 1 19960315 A 3350 TRACK LIGHT AEROSP ATR42 ATR42300 8680920 EU CABIN OUT OF ADJUST A M3HA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 13 4210G 149 HNL - FLT 445 - CHECK OPERATION OF EMERGENCY FLOOR TRACK LIGHTING. ADJUSTED TRACK LENS AS REQUIRED OPS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1996052300675 19960523 00675 EU 1996 5 23 M3HA96007 1 19960322 A 3350 CONNECTOR AEROSP ATR42 ATR42300 8680920 EU CABIN LOOSE A M3HA K NONE L NO TEST IN INSP/MAINT 1 WP 13 4209G 129 HNL - FLT 404 - ROW 5 FLOOR EMERGENCY LIGHT BULB OUT. RESEATED PIN 'A' ON CANNON PLUG. (M) 2 H 7 2 4T RT A53EU 1996052300676 19960523 00676 EU 1996 5 23 M3HA96008 1 19960330 A 3240 BRAKE 50068571 AEROSP ATR42 ATR42320 8680930 EU NR 1 BROKEN A M3HA K NONE O OTHER TX TAXI/GRND HDL 1 WP 13 988MA 380 HNL - FLT 423 - NR 1 MAIN TIRE FLAT. FOUND NR 1 BRAKE ASSY BROKEN STUCK IN NR 1 WHEEL ASSY. REMOVED AND INSTALLED SERV ICEABLE BRAKE AND MAIN WHEEL ASSY NR 1 POSITION. (M) 2 H 7 2 4T RT A53EU 1996052300677 19960523 00677 EU 1996 5 23 M3HA96010 1 19960411 A 7712 NP SENSOR AEROSP ATR42 ATR42300 8680920 EU NR 2 ENG DIRTY A M3HA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 13 4206G 081 HNL - FLT 231 - SHORTLY AFTER DEPARTURE FROM HNL, THE PILOT NOTICED A PLUS OR +/-3 PERCENT TORQUE FLUCTUATION ON NR 2 EN GINE. AIRCRAFT WAS RETURNED BACK TO HNL, AN UNEVENTFUL LANDING WAS MADE. REMOVED, CLEANED AND REINSTALLED CANNON PLUGS ON THE SYNCROPHASER, NP SENSOR AND SYNCHROPHASER PICKUP ON THE ENGINE. PERFORMED HIGH POWER ENGINE RUN UP, NO FLUCTUAT ION NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996052300678 19960523 00678 SW 1996 5 23 MALA964947 1 19960410 A 3240 212033 BRAKE SWRNGN SA227 SA227AC 8780603 SW RT MLG WORN A MALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 15 446MA AC693 FLT 3089 - WHILE TAXIING IN DTW, THE CREW NOTED THAT THE RIGHT BRAKE WOULDN'T HOLD PRESSURE. MX REPLACED THE RIGHT INBO ARD AND OUTBOARD BRAKE ASSEMBLIES. ALL CHECKS GOOD. (M) 2 L 7 2 4T RT A8SW 1996052300679 19960523 00679 SW 1996 5 23 MALA964950 1 19960414 A 3097 WIRE SWRNGN SA227 SA227AC 8780603 SW RT INTAKE HEAT BROKEN A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 26906 AC654B FLT 3004 - ON CLIMB-OUT FROM MSP, THE RIGHT ENGINE INTAKE HEAT BECAME INOPERATIVE. THE AIRCRAFT RETURNED TO MSP. MAINT ENANCE REPAIRED A WIRE AT THE INTAKE HEAT VALVE. (M) 2 L 7 2 4T RT A8SW 1996052300680 19960523 00680 SW 1996 5 23 MALA964962 1 19960413 A 5753 2731141 DOUBLER SWRNGN SA227 SA227AC 8780603 SW RT TE FLAP WORN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 60NE AC760B DURING AN INSPECTION IN MSP, MAINTENANCE PERSONNEL REPAIRED WEAR TO RIGHT FLAP WALKING BEAM ROLLER DOUBLER BY REPLACING WITH A NEW DOUBLER P/N 27-31141 AND INSTALLING A SECOND ROLLER PLATE P/N 27-31141-003. ALL WORK PERFORMED IAW FAIRCHILD ARP 57-10-9513 AND ARP 57-20-9424 FOR FORWARD MOST FASTENER OMISSION. (M) 2 L 7 2 4T RT A8SW 1996052300681 19960523 00681 SW 1996 5 23 MALA964963 1 19960413 A 5210 SKIN SWRNGN SA227 SA227AC 8780603 SW PAX SKIN DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 60NE AC760B DURING AN INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE PASSENGER DOOR SKIN AT FORWARD AND AFT HINGE CUT OUT CHAFFE D AND DAMAGED. COMPLETED REPAIR BY REMOVING DAMAGED AREAS AND WET INSTALLING REPAIR DOUBLERS IAW ARP 52-10-8701 DATED 2 /13/87. (M) 2 L 7 2 4T RT A8SW 1996052300682 19960523 00682 SW 1996 5 23 MALA964964 1 19960411 A 5230 SKIN SWRNGN SA227 SA227AC 8780603 SW CARGO DOOR DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 60NE AC760B DURING AN INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED AFT CARGO DOOR SKIN AT FORWARD AND AFT HINGE CUT OUTS, SKIN CHA FED ADN DAMAGED. COMPLETED REPAIRS BY REMOVING CHAFED AREAS AND INSTALLING REPAIR PATCHES IAW FAC ARP 52-30-9130 DATED 20 JUNE 1991. (M) 2 L 7 2 4T RT A8SW 1996052300683 19960523 00683 SW 1996 5 23 MALA964965 1 19960411 A 5330 SKIN SWRNGN SA227 SA227AC 8780603 SW BS 493.247 DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 60NE AC760B DURING AN INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND DENT DAMAGE TO LOWER FUSELAGE SKIN JUST AFT OF FS 493.247 AND O N BOTH LEFT AND RIGHT SIDE OF BL 0. COMBINED AREA OF DENT DAMAGE IS APPROX 14 INCHES BY 9 INCHES. DETEMINED THAT A SUR FACE REPAIR DOUBLER OF 15 INCHES BY 7.5 INCHES WOULD SUFFICIENTLY COVER AND REINFORCE AFFECTED AREA. FABRICATED A 15 IN CH BY 7.5 INCH REPAIR SURFACE DOUBLER, PREPPED, PRIMED AND INSTALLED IAW FAIRCHILD SRM 53-90-20, PGS 61-62, REV JAN 18/9 3. (M) 2 L 7 2 4T RT A8SW 1996052300684 19960523 00684 NE 1996 5 23 ORJA9621 2 19960408 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE RIGHT MALFUNCTIONED A ORJA O OTHER R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 11 841RA 725441 49421 ON TAKEOFF, NO TAKEOFF POWER, V1 PLUS 5 KNOTS FT EGT WENT TO 620 DEGREES FOR 2 MINUTES THEN POWER WAS REDUCED TO MCT 580 DEGREES. ENTERED DMI 5990. REPLACED NR 2 ENGINE ASSY. LEAK AND OPS CHECKED GOOD. (M) 2 L 7 2 4F 4 F A6WE E9NE 1996052300685 19960523 00685 WP 1996 5 23 ORJA9622 1 19960419 A 3350 60030431 POWER PACK DOUG DC9 DC983 3022083 WP VENTRAL INOP A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 832RA 15831 53044 EMERGENCY EXIT LIGHTS IN AIRCRAFT VENTRAL AREA OUT (4 EACH). REMOVED AND REPLACED EMERGENCY EXIT LIGHT POWER PACK, IAW MM CHAPTER 33. OPS GOOD. (M) 2 L 7 2 4F RT A6WE 1996052300686 19960523 00686 WP 1996 5 23 ORJA9624 1 19960505 A 3350 LIGHTS DOUG DC9 DC982 3022082 WP CABIN INOP A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 823RA 49889 EMERGENCY EXIT LIGHTS, FIRST TWO ROWS AND FORWARD LIGHTS COME ON IN 'ARMED' POSITION, GO OFF IN 'ON' POSITION, GOES OFF IN 'OFF' POSITION. REPOSITIONED WIRING AT F/C FORWARD BULKHEAD. OPERATION CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 1996052300687 19960523 00687 NM 1996 5 23 TAOA049610 1 19960423 A 3350 1000677 LIGHT GRIMES BOEING 727 727254 138408L NM CABIN INOPERATIVE A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 915TS 1185 20252 RIGHT AFT EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSEMBLY, OPS CHECK OK, PER MM 33-51-00. (M) 2 L 7 3 4F A3WE 1996052300688 19960523 00688 NM 1996 5 23 TAOA049611 1 19960424 A 3350 0L3071BPGPL LAMP BOEING 727 727254 138408L NM CABIN MISSING A TAOA K NONE O OTHER IN INSP/MAINT 1 EA 15 915TS 20252 E-PATH LAMP AND LENS MISSING, ROW 29. REPLACED LAMP AND LENS AT ROW 29, OPS CHECK OK PER MM 33-50. (M) 2 L 7 3 4F A3WE 1996052300689 19960523 00689 NM 1996 5 23 TAOA049613 1 19960425 A 2612 394120 FIRE LOOP BOEING 727 727254 138408L NM NR 1 ENGINE MALFUNCTIONED A TAOA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 EA 15 916TS 3916 20437 NR 1 ENGINE FIRE WARNING BELL SOUNDED AND SWITCH ILLUMINATED IN CRUISE. ENGINE SHUTDOWN, FIRE WARNING WENT OUT FOR REMA INDER OF THE FLIGHT. ENGINE INSPECTED FOR FIRE DAMAGE NONE FOUND. FIRE WARNING SELF TEST CHECKED OK. REPLACED ENGINE WIRING HARNESS AND FIRE LOOP PRECAUTIONARY. RAN ENGINE AT TAKEOFF POWER FOR 5 MINUTES, SYSTEM CHECKED OK. INSPECTED AN D REPLACED ENGINE MAIN OIL SCREEN. (M) 2 L 7 3 4F A3WE 1996052300690 19960523 00690 NM 1996 5 23 TSAA9621021 1 19960422 A 2150 CLAMP BOEING 737 7372S2C 138448G NM CABIN LOOSE A TSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 806AL 21927 FLT NR 286 - HNL-OGG - LEFT WING/BODY OVERHEAT LIGHT ILLUMINATED IN FLIGHT. LIGHT WENT OUT WHEN AIR SOURCE WAS REMOVED. RETURNED AIRCRAFT TO HNL. REPLACED CLAMP ON HEAT EXCHANGER DUCT DUE TO BLOW BY AS EVIDENT ON FLANGE MATING SURFACES. LEAK CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1996052300691 19960523 00691 EU 1996 5 23 VTZA96175 1 19960501 A 7722 SRL LIGHT BAG JETSTM JETSTM3201 1500217 EU LEFT ILLUMINATED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 481UE 895 FLT NR 6359 - IAD-SWF - ABORTED THE TAKEOFF DUE TO THE LEFT SRL CAP LIGHT ILLUMINATING DURING THE TAKEOFF ROLL. AIRCRAF T RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 09074 IAW MEL 76-1. MAINTENANCE LATER CLEARED DMI NR 09074 ON 5-5-96 BY PERFORMING AN OPERATIONAL CHECK OF THE LT SRL SYSTEM, OPS CHECKED GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996052300692 19960523 00692 EU 1996 5 23 VTZA96178 1 19960503 A 2770 91SE16 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU GUST LOCK OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 306UE 41020 FLT NR 6420 - PWM-IAD - ABORTED TAKEOFF DUE TO THE TAKEOFF CONFIGURATION WARNING SYSTEM ACTIVATING. AIRCRAFT RETURNED T O PWM WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED THE GUST LOCK HANDLE MICROSWITCH. AIRCRAFT WAS RELEASED AND APPR OVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996052300693 19960523 00693 EU 1996 5 23 VTZA96179 1 19960503 A 2611 S5202007SN CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU BAY BAGGAGE WATER CONTAM A VTZA K NONE N FALSE WARNING LD LANDING 1 EA 27 324UE 41017 FLT NR 6217 - IAD-PVD - DURING LANDING, AN EMERGENCY WAS DECLARED DUE TO THE BAGGAGE POD SMOKE WARNING LIGHT ILLUMINATIN G. AIRCRAFT COMPLETED LANDING WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED MOISTURE FROM THE SMOKE DETECTOR CANNON P LUG. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996052300694 19960523 00694 1996 5 23 VTZA96180 4 19960503 A 3417 7000700953 ADC JETAIR JETSTM JETSTM4101 1500501 EU NR 1 FAILED A VTZA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 307UE 41021 FLT NR 6563 - JFK-IAD - ABORTED THE TAKEOFF DUE TO THE NR 1 AIR DATA COMPUTER FAILING ON THE TAKEOFF ROLL. AIRCRAFT RET URNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE AIR DATA COMPUTER. AIRCRAFT WAS RELEASED AND APPROVE D FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996052300695 19960523 00695 EU 1996 5 23 VTZA96181 1 19960503 A 5270 WARNING LIGHT JETAIR JETSTM JETSTM4101 1500501 EU BAGG DOOR ILLUMINATED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 307UE 41021 FLT NR 6563 - JFK-IAD - ABORTED THE TAKEOFF DUE TO THE MAIN BAGAGE DOOR WARNING LIGHT ILLUMINATING ON THE TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE CYCLED BAGGAGE DOOR AND RESET DOOR WARNING SYSTEM. A IRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996052300696 19960523 00696 NM 1996 5 23 WRLA96018 1 19960423 A 2913 6506606 HYD PUMP DOUG MD11 MD11F 3023600 NM NR 3 ENG FAILED A WRLA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 27 274WA 48633 DURING CLIMB-OUT, FLT CREW NOTED NR 2 L HYD PUMP OFF' ALERT. HYD SYS CONTROLLER SHUTDOWN NR 3 LT TO ACTIVATED NR 3 RT H YD PUMP. CREW NOTED SLOW LOSS OF NR 3 HYD SYS FLUID QTY. WHEN SYS REACHED 5.5 GAL, FLT CREW UTILIZED ABNORMAL PROCEDUR ES AND SHUTDOWN NR 3 HYD SYSTEM. FLT CONTINUED TO DESTINATION AND LANDED WITHOUT FURTHER INCIDENT. MX PERSONNEL FOUND HYD FLUID LEAKING OUT OF NR 3 ENG COWLING. IT WAS NOTED THAT NR 3 LT PUMP WAS LEAKING FLUID THROUGH A CRACK IN PUMP CAS E. PUMP WAS REPLACED, ENG COWLINGS WERE CLEANED. ENG WAS GROUND RUN WITH NO DEFECTS NOTED. A/C RETURNED TO SERV. (M) 2 L 7 3 4F RT A22WE 1996052300697 19960523 00697 SO 1996 5 23 WTAA960072 1 19960408 A 7714 SEL0C29DH INDICATOR EMB 120 EMB120RT SO RT ENGINE ERRATIC A WTAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 17 454UE 120155 SMF - RIGHT ENGINE PROPELLER 'NP' INDICATION REPORTED ERRATIC DURING CLIMB-OUT. ALL OTHER ENGINE INDICATIONS NORMAL. A IRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE CLEANED AND INSPECTED RIGHT PROPELLER 'NP' INDICATOR CANNON A ND SWAPPED GAUGES FROM RIGHT TO LEFT POSITION. PROPELLER INDICATIONS REPORTED NORMAL DURING ENGINE GROUND RUN. AIRCRAF T RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 1996052300698 19960523 00698 SO 1996 5 23 WTAA960073 1 19960404 A 2150 PACK EMB 120 EMB120RT SO CABIN SMOKING A WTAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 17 251YV 120251 ACV - RIGHT AIR CONDITIONING PACK REPORTED TO CAUSE SMOKE ODOR IN CABIN. MANTENANCE DEFERRED RIGHT PACK PER MEL 21-50-2 . AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL BY INSPECTING THE RIGHT PACK SYSTEM WITH NO DEFECTS NOTED. SYSTEM OPERATIONAL CHECK NORMAL WITH APU AND BLEED AIR SYSTEMS ON. NO SMOKE ODOR REPORTED IN CABIN DURI NG GROUND CHECK. (M) 2 L 7 2 4T RT A31SO 1996052300699 19960523 00699 SO 1996 5 23 WTAA960074 1 19960413 A 3233 1959500007 ACTUATOR EMB 120 EMB120RT SO LT MLG SLOW TO RETRACT A WTAA O OTHER J WARNING INDICATION TO TAKEOFF 1 WP 17 455UE 120163 SFO - LEFT MAIN LANDING GEAR INTRANSIT LIGHT REMAINS ILLUMINATED AFTER GEAR RETRACTION. MX REPLACED LEFT MAIN LANDING G AER RETRACTION ACTUATOR. GEAR RETRACTION AND EXTENSION NORMAL DURING GROUND CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996052300700 19960523 00700 EU 1996 5 23 WTAA960075 1 19960412 A 2912 QA03043 FILTER BAG JETSTM JETSTM3101 1500215 EU HYDRAULIC SYSTEM BLOCKED A WTAA K NONE J WARNING INDICATION LD LANDING 1 WP 17 423UE 799 IPL - NOSE GEAR RED INTRANSIT LIGHT ILLUMINATED WITH ASSOCIATED GEAR WARNING HORN ACTIVATION DURING LANDING ROLLOUT. MA INTENANCE FOUND RESTRICTION IN HYDRAULIC FILTERS. REPLACED HYDRAULIC FILTERS. NOSE GEAR POSITION INDICATION SYSTEM OPE RATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996052300701 19960523 00701 WP 1996 5 23 WTAA960076 2 19960415 A 7320 89737526 FUEL CONTROL BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110U 01514 WP LT/RT ENG OUT OF ADJUST A WTAA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 17 428UE 806 SMF - BOTH ENGINE REPORTED TO NOT DEVELOP RATED POWER AT 14,000 FEET DURING CLIMB. ENGINES REPORTED POWER LEVER LIMITED . AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE ACCOMPLISHED ENGINE GROUND RUN AND FOUND BOTH ENGINES TO OBTAIN REQUIRED POWER. ACCOMPLISHED PRECAUTIONARY ADJUSTMENT TO MAX FUEL FLOW OF BOTH ENGINES. AIRCRAFT RETURNED TO SE RVICE. (M) 2 L 7 2 4T 4 T RT A21EU E4WE 1996052300702 19960523 00702 SO 1996 5 23 WTAA960079 1 19960416 A 3620 M1160140242 SENSOR EMB 120 EMB120RT SO LT ENGINE BROKEN WIRE A WTAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 17 276UE 120067 FAT - LEFT DUCT LEAK LIGHT ILLUMINATED AFTER TAKEOFF WITH BLEED SYSTEM PREVIOUSLY DEFERRED. AIRCRAFT RETURNED TO STATIO N WITHOUT INCIDENT. MX FOUND DAMAGED WIRES AT DUCT LEAK SENSOR S0367 AT FRAME 29 LT. REPAIRED WIRES. BLEED AIR DUCT L EAK INDICATION SYSTEM CHECKS NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996052300703 19960523 00703 SO 1996 5 23 WTAA960080 1 19960419 A 2751 M817142BC1 CONNECTOR EMB 120 EMB120RT SO TE FLAPS LOOSE WIRE A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 17 275UE 120058 LAX - 'TAKEOFF FLAPS' AURAL WARNING ACTIVATED DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. AIRCRAFT FERRIED TO FAT FOR REPAIRS. MX UNABLE TO DUPLICATE DISCREPANCY. PRECAUTIONARY REPLACEMENT OF FLAP ANNUNCIATOR AURAL WARNING CO MPUTER ACCOMPLISHED. AURAL WARNING SYSTEM OPERATIONAL CHECK NORMAL ON GROUND AND DURING SUBSEQUENT TEST FLIGHT. AIRCRA FT RETURNED TO SERVICE. PROBLEM REOCCURRED ON 4/20/96. FOUND INTERMITTENT ELECTRICAL CONNECTION AT TERMINAL JUNCTION 2 204. REPAIRED AS REQUIRED. (M) 2 L 7 2 4T RT A31SO 1996052300704 19960523 00704 SO 1996 5 23 WTAA960081 1 19960424 A 5101 STRUCTURE EMB 120 EMB120RT SO AIRFRAME BIRD STRIKE A WTAA K NONE C F.O.D. NR NOT REPORTED 1 WP 17 275UE 120058 SMF - BIRD STRIKE REPORTED ON AIRCRAFT. MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECTION. NO DAMAGE NOTED. AIRCRAFT RE TURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996052300705 19960523 00705 EU 1996 5 23 WTAA960082 1 19960423 A 5610 WINDSHIELD BAG JETSTM JETSTM3101 1500215 EU RT COCKPIT BIRD STRIKE A WTAA K NONE C F.O.D. NR NOT REPORTED 1 WP 17 331CA 793 LAX - BIRD STRIKE REPORTED ON AIRCRAFT AT FLIGHT OFFICERS WINDSHIELD WIPER AREA. MAINTENANCE ACCOMPLISHED BIRD STRIKE I NSPECTION. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996052300706 19960523 00706 EU 1996 5 23 WTAA960083 1 19960424 A 5270 MS161065 SWITCH BAG JETSTM JETSTM3101 1500215 EU POD DOOR OUT OF ADJUST A WTAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 17 403UE 743 SEA - POD DOOR LIGHT ILLUMINATED AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION. MAINTENANCE ADJUSTED POD DOOR MICROSWITC H. DOOR WARNING SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996052300707 19960523 00707 1996 5 23 WTAA960084 3 19960422 A 6112 R333482F12 PROP DE-ICE BOOT BAG JETSTM JETSTM3101 1500215 EU LT ENGINE SEPARATED A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK D INFLIGHT SEPARATION TO TAKEOFF 1 WP 17 402UE 17858 282 DRG44288 734 STS - LEFT PROPELLER DE-ICE BOOT SEPARATED FROM PROPELLER ASSEMBLY DURING INITIAL STAGE OF TAKEOFF ROLL. TAKEOFF ABORTE D WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED LEFT PROPELLER ASSEMBLY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996052300708 19960523 00708 SO 1996 5 23 WTAA960085 1 19960428 A 5330 SKIN EMB 120 EMB120RT SO FUSELAGE BIRDSTRIKE A WTAA K NONE C F.O.D. NR NOT REPORTED 1 WP 17 275UE 120058 FAT - BIRD STRIKE REPORTED ON AIRCRAFT FUSELAGE AT FLIGHT OFFICERS ANGLE OF ATTACK VANE. MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECTINO. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (M0 2 L 7 2 4T RT A31SO 1996052300740 19960523 00740 GL 1996 5 23 96ZZZX2612 3 19960213 A 6111 PROPELLER BLADE BEECH 1900 1900D 1154162 CE HARTZL HCB3T HCB3TN3 GL LEFT ENGINE SPLIT A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 176YV UE176 HJ459 DURING ROUTINE MAINTENANCE, THE LEFT PROPELLER WAS FOUND DELAMINATED ON ONE BLADE. MAINTENANCE REMOVED AND REPLACED PRO PELLER. 2 L 7 2 4T RT A24CE 6 C P15EA 1996052900001 19960529 00001 NM 1996 5 29 UPS96205974 1 19960412 A 5343 SUPPORT FITTING BOEING 727 72725C 138400H NM BS 940 MISDRILLED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 933UP 19857 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED DOUBLE HOLE IN HOR FLANGE OF RT MLG SUPPORT FITTING BS 940 RBL 66 WL 208. RE MOVED DAMAGED AREA AND REPAIRED PER EO 727-53-1754. 2 L 7 3 4F A3WE 1996052900002 19960529 00002 EU 1996 5 29 HEEA967063 1 19960419 A 6320 704A34130004 CABLE SNIAS 350 AS350B2 8680813 EU XMSN BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100U 659 2863 CABLE BROKEN AT TRANSMISSION END. 1 G 7 1 3U H9EU 1996053000060 19960530 00060 WP 1996 5 30 9611269867 1 19960520 A 2131 CONTROLLER DOUG DC9 DC951 3022051 WP CABIN MALFUNCTIONED A NWAA B EMER. DESCENT J WARNING INDICATION DE DESCENT 1 GL 01 776NC 47786 DURING DESCENT, CABIN BEGAN TO CLIMB AT 1,500 FPM. BEGAN A RAPID DESCENT TO 10M AND WORKED CONTROLLER MANUALLY. CABIN PRESSURE LIGHT CAME ON AND CABIN GOT TO APPROXIMATELY 10,500 FEET, NO MASKS DROPPED. REPLACED CABIN PRESSURE AMPLIFIER AND CABIN PRESSURE CONTROLLER. PRESSURIZED CABIN AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996053000061 19960530 00061 NM 1996 5 30 9611276310 1 19960522 A 2910 S271U1211 HYDRAULIC SYS BOEING 747 747451 1384940 NM NR 4 HYD SYS REQD SERVICE A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 670US 24225 DURING CRUISE, THE NR 4 HYDRAULIC SYSTEM LOST HYDRAULIC FLUID. FLUID LOSS STOPPED WHEN HYDRAULIC SYSTEM PRESSURE WAS RE MOVED. AIRCRAFT DIVERTED TO ANC AND LANDED WITHOUT INCIDENT. VISUALLY INSPECTED HYDRAULIC SYSTEM, NO LEAKS FOUND. SER VICED HYDRAULIC SYSTEM, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1996053000062 19960530 00062 NM 1996 5 30 9611285504 1 19960522 A 7931 OIL PRESS IND BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE NR 2 ENGINE MALFUNCTIONED A NWAA D E RETURN TO BLOCK ENGINE SHUTDOWN J WARNING INDICATION TX TAXI/GRND HDL 1 GL 01 504US 23193 716473 DURING TAXI OUT, NR 2 ENGINE OIL PRESSURE DROPPED TO 14 PSI. NR 2 ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNED TO GATE. M AINTENANCE PERSONNEL INSPECTED NR 2 ENGINE, NO SIGNS OF OIL LEAKAGE NOTED. BOTH ENGINES STARTED AND OPERATING PARAMETER S CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 1996053000063 19960530 00063 WP 1996 5 30 9611291155 1 19960520 A 7830 TR UNIT DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 3 ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 155US 46764 86155 DURING TAKEOFF ROLLOUT, THE NR 3 ENGINE REVERSER UNLOCK LIGHT ILLUMINATED. TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNE D TO THE GATE. MAINTENANCE INSPECTED THE NR 3 REVERSER AND FOUND IT TO BE NORMAL. DURING REVERSER OPERATION WITH GROUN D AIR, REVERSER DEPLOYED NORMALLY BUT WOULD NOT GO BEYOND REVERSE IDLE. THE AIRCRAFT WAS RETURNED TO SERVICE WITH REVER SER ON MEL 78-1A. 2 L 7 3 4F 4 F A22WE E20EA 1996053000064 19960530 00064 WP 1996 5 30 9611309903 1 19960522 A 3350 LIGHT DOUG DC9 DC931 3022065 WP LT NACELLE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 953N 47083 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. PROBLEM COULD NOT BE DUPLICATED ON SECOND ATTEMPT. 2 L 7 2 4F A6WE 1996053000065 19960530 00065 WP 1996 5 30 9611319925 1 19960522 A 3350 FUSE DOUG DC9 DC932 3022066 WP CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 925US 47472 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY PROXIMITY LIGHTS AT GALLEY DOOR AND FIRST CLASS CABIN INOPERATIVE. R EPLACED FUSE, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996053000066 19960530 00066 NM 1996 5 30 9611322702 1 19960519 A 2130 PACK BOEING 727 727225 1384077 NM RIGHT MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 8877Z 21450 DURING CLIMB, LOST RIGHT PACK, COULD NOT CONTROL CABIN PRESSURIZATION ON SINGLE PACK OPERATION. AIRCRAFT DIVERTED TO TP A AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED LEAK CHECK AND OPERATIONAL CHECK ON SINGLE PACK, SYSTEM CHECKED OK . 2 L 7 3 4F A3WE 1996053000067 19960530 00067 NM 1996 5 30 9611332296 1 19960521 A 2751 181229932 INDICATOR BOEING 727 727251 138408H NM COCKPIT IND MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 296US 12036 3225 21788 DURING CLIMB ON FLAP RETRACION, OUTBOARD FLAPS WOULD NOT RETRACT BEYOND 5 DEGREES. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED OUTBOARD INDICATOR AND PERFORMED FLAP OPERATIONAL CHECK, CHECKED OK. 2 L 7 3 4F A3WE 1996053000068 19960530 00068 NE 1996 5 30 9611345529 2 19960522 A 7230 COMPRESSOR BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE NR 2 ENGINE STALLED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 01 529US 23844 716427 DURING CLIMB, THE NR 2 ENGINE EXPERIENCED TWO COMPRESSOR STALLS AND THEN SHUT DOWN, NO RESTART WAS ATTEMPTED. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT FURTHER INCIDENT. THE ENGINE WAS BORESCOPE INSPECTED, NO DAMAGE FOUND. ENGINE MAG P LUGS WERE INSPECTED AND FOUND CLEAN. THE ENGINE ELECTRONIC CONTROL WAS REPLACED. THE BLEED SYSTEM, STATOR VANE ACTUATO R AND FUEL CONTROL WERE INSPECTED AND FOUND SERVICEABLE. ENGINE GROUND RUN AND ALL OPERATING PARAMETERS FOUND WITHIN LI MITS. 2 L 7 2 4F 4 F RT A2NM E17NE 1996053000069 19960530 00069 NM 1996 5 30 9611352294 1 19960517 A 2782 1U1110 ACTUATOR BOEING 727 727251 138408H NM NR 3 LE FLAP MALFUNCTIONED A A NWAA J A DUMP FUEL UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 01 294US 52646 34713 21505 DURING TAKEOFF CLIMB, THE NR 3 LEADING EDGE KRUEGER FLAP WOULD NOT RETRACT AND FUEL WAS DUMPED TO LANDING WEIGHT. AIRC RAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE NR 3 KRUEGER FLAP ACTUATOR, FUNCTIONAL CHECK OK. 2 L 7 3 4F A3WE 1996053000070 19960530 00070 NM 1996 5 30 9611362296 1 19960519 A 3260 DOOR SWITCH BOEING 727 727251 138408H NM NLG LACK OF LUBE A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 296US 21788 DURING APPROACH ON GEAR DOWN, NOSE GEAR DOOR LIGHT DID NOT ILLUMINATE AND NOSE GEAR INDICATION WAS NOT DOWN AND LOCKED. RECYCLED GEAR AND ALL INDICATIONS WERE NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED AND LUBRICATED L ANDING GEAR DOOR SWITCH AND PERFORMED GEAR CHECK, CHECKED OK. 2 L 7 3 4F A3WE 1996053000071 19960530 00071 WP 1996 5 30 9611379753 1 19960523 A 3350 BATTERY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 753NW 47117 DURING LINE CHECK, FOUND OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY AND CHARGER, OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996053000072 19960530 00072 NM 1996 5 30 96FDEA00902 1 19960504 A 5315 FLOOR BEAM BOEING 727 72725 1384006 NM BS 344 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 505FE 18276 NR0469 AND 008, CORROSION AT BS 344 FLOOR BEAM LBL 40 TO RBL 15 WL 208. ACCOMPLISHED FLOOR BEAM REPAIR AT BS 344 LBL 40 TO RBL 15 WL 208 PER FED EX DRW SR 27-53-007. 2 L 7 3 4F A3WE 1996053000073 19960530 00073 NM 1996 5 30 96FDEA01016 1 19960507 A 5320 TEAR STRAP BOEING 727 72725 1384006 NM BS 418-464 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 505FE 187276 NR0564 -032C, WHILE WORKING NRO498 DISCOVERED CORROSION IN BETWEEN BONDED DOUBLER AND OVERLAPPED SKIN BS 418 TO 464 STR 4R. ACCESSED REPAIR AREA, FOUND BONBED TEAR STRAP CORRODED BEYOND LIMITS. REMOVED FABRICATED AND INSTALLED BONDED TEAR STRAP, REINSTALLED ITEMS REMOVED FOR ACCESS IAW SRM 53-30-4, 51-40-4. 2 L 7 3 4F A3WE 1996053000074 19960530 00074 NM 1996 5 30 96FDEA1015 1 19960522 A 2120 AIR DISTR BOEING 727 72725 1384006 NM COCKPIT ODOR A FDEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 25 154FE 18287 STRONG ACRID ODOR IN COCKPIT AT FLIGHT LEVEL 330. PACK TEMPERATURES NORMAL, NOTHING ABNORMAL INDICATED AND DETECTION SY STEM TESTED NORMAL. SUSPECT EITHER ELECTRICAL MALFUNCTION OR TOILET CHEMICAL MIXING CAUSED TOXIC FUMES. NO VISIBLE SMO KE. AIRCRAFT RELEASED FOR SERVICE PER MINIMUM EQUIPMENT LIST 21:24 CATEGORY D EXPIRATION 19 SEPT 96. REMOVED A REPLACE D GASPER FAN PER M/M, OPERATIONAL CHECK GOOD. 2 L 7 3 4F A3WE 1996053000075 19960530 00075 NM 1996 5 30 96FDEA1017 1 19960522 A 5230 65571463 SEAL DEPRESSOR BOEING 727 727225 1384077 NM NR 1 CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 468FE 21452 0370 -010C, NR 1 CARGO DOOR LWR AFT CORNER SEAL DEPRESSOR IS CRACKED AND DENTED. REMOVED AND REPLACED AFT SEAL DEPRESSO R ON NR 1 CARGO DOOR. 2 L 7 3 4F A3WE 1996053000076 19960530 00076 NM 1996 5 30 96FDEA1018 1 19960522 A 5230 65571464 SEAL DEPRESSOR BOEING 727 727225 1384077 NM NR 1 CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 468FE 21452 0378 -011C, NR 1 CARGO DOOR LWR FWD CORNER SEAL DEPRESSOR IS CRACKED AND DENTED. REMOVED AND REPLACED LWR SEAL DEPRESSO R ON NR 1 CARGO DOOR. 2 L 7 3 4F A3WE 1996053000077 19960530 00077 NM 1996 5 30 96FDEA1019 1 19960522 A 5230 655714052 SEAL DEPRESSOR BOEING 727 727225 1384077 NM NR 1 CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 468FE 21452 0379 -012C, NR 1 CARGO DOOR LWR CENTER SEAL DEPRESSOR IS CRACKED AND DENTED. REMOVED AND REPLACED LWR CENTER SEAL DEPRE SSOR ON NR 1 CARGO DOOR. 2 L 7 3 4F A3WE 1996053000078 19960530 00078 WP 1996 5 30 96FDEA1020 1 19960522 A 2913 HYD PUMP DOUG DC10 DC1030F 3023504 WP NR 3 ENG LEAKING A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 319FE 47820 TOTAL LOSS OF HYDRO SYSTEM NR 3 ON CLIMBOUT, PERFORMED RED TAB PROCEDURE AND LANDED 35/EXT 16L SEA WITHOUT INCIDENT. MA INTENANCE FOUND 2/3 REVIISABLE MOTOR PUMP LEAKING. REMOVED AND REPLACED 2/3 REVIISABLE MOTOR PUMP PER M/M 29-22-01, LEA K AND OPS CHECK GOOD. REMOVED AND REPLACED NR 3 ENG PRESSURE AND CASE DRAIN FILTERS, NO CONTAMINATION NOTED. 2 L 7 3 4F RT A22WE 1996053000079 19960530 00079 NM 1996 5 30 96FDEA1021 1 19960522 A 5311 FRAME BOEING 727 727227 1384078 NM BS 1110 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 NR 0317 (018C), CORROSION (C53-224-01) ON FWD SIDE OF BS 1110 FRAME AT STR 4 LT. REPAIRED FRAME FWD SIDE OF BS 1110 FRA ME AT STR 4 LT IAW FEDEX SRM 51-40-3. 2 L 7 3 4F A3WE 1996053000080 19960530 00080 NM 1996 5 30 96FDEA1022 1 19960522 A 5313 STRINGER BOEING 727 727225 1384077 NM BS 960.5 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 468FE 21669 CORROSION (C53-224-01, -3) AND TOOL MARKS BS 970. REMOVED DAMAGED STR BS 960.5, FABRICATED REPAIR PARTS AND INSTALLED P ER FEDEX SRM 727 53-10-3 FIG 3. 2 L 7 3 4F A3WE 1996053000081 19960530 00081 NM 1996 5 30 96FDEA1023 1 19960522 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 950 CORRISION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 NR 0314 (032), CORROSION (C53-224-01, -3) AND TOOLING MARKS BS 950A, STR 7 RT AFT SIDE OF FRAME MARKED IN RED. 2 L 7 3 4F A3WE 1996053000082 19960530 00082 NM 1996 5 30 96FDEA1024 1 19960522 A 5315 FLOOR BEAM BOEING 727 727227 1384078 NM BS 1130 CORRISION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 NR 0391 (034), CORROSION (C53-111-01(3) ON LOWER CHORD OF FLOOR BEAM AT NUTPLATE HOLES BS 1130 LBL 54 TO RT 54 LT 200. 2 L 7 3 4F A3WE 1996053000084 19960530 00084 SO 1996 5 30 COMA9610151 1 19960519 A 5320 12025211002 SKIN SUPPORT EMB 120 EMB120RT SO FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 200CD 120200 DURING 400FC INSPECTION, FOUND ONE RIVET AT FRAME 9 JUST BELOW RIGHT DIRECT WINDOW TO BE DEFORMED. FURTHER INSPECTION R EVEALED SKIN SUPPORT TO BE CRACKED. REPLACED CRACKED SUPPORT. 2 L 7 2 4T RT A31SO 1996053000085 19960530 00085 EU 1996 5 30 COMA9630111 1 19960520 A 2721 7255433007 FAIRING SAAB SF340 SF340A 7850100 EU RUDDER LOOSE A COMA A UNSCHED LANDING E F VIBRATION/BUFFET FLT CONT AFFECTED CL CLIMB 1 SO 01 359CA 340A053 RUDDER VIBRATION DURING FLIGHT ABOVE 180 KTS. REPAIRED LOOSE FASTENERS SECURING THE RUDDER TRIM TAB CONTROL ROD FAIRING . 2 L 7 2 4T RT A52EU 1996053000087 19960530 00087 EU 1996 5 30 COMA9630113 1 19960521 A 2460 A2042C PWR DISTR UNIT SCBFLG SF34 SF34A 3801351 EU LEFT FAILED A COMA K NONE H ELECT. POWER LOSS-50 PC UK UNKNOWN 1 SO 01 358CA 23405 694 340A047 RT MAIN ELECTRIC BUS OFF LINE, GENERATOR WOULD NOT RESET. REPLACED THE LT POWER DISTRIBUTION UNIT. 1 K 0 0 G48EU 1996053000088 19960530 00088 EU 1996 5 30 COMA9630114 1 19960521 A 2520 6510376 PSU SAAB SF340 SF340A 7850100 EU CABIN OVERHEATED A COMA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SO 01 643CA 340A024 FAINT ELECTRICAL ODOR NOTICED IN CABIN AREA AT ROW 2. REPLACED OVERHEATED PASSENGER SERVICE UNIT AT ROW 2BC. 2 L 7 2 4T RT A52EU 1996053000089 19960530 00089 EA 1996 5 30 COMA9660993 1 19960522 A 2742 83963 TRIM ACTUATOR CNDAIR CL600 CL6002B19 EA HORIZ STAB MALFUNCTION A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 924CA 2341 7026 HORIZONTAL STABILIZER CHANNEL 1 WILL NOT ENGAGE. REPLACED THE HORIZONTAL STABILIZER TRIM ACTUATOR. 2 L 7 2 4F RT A21EA 1996053000090 19960530 00090 EA 1996 5 30 COMA9660994 1 19960522 A 2742 83963 TRIM ACTUATOR CNDAIR CL600 CL6002B19 EA HORIZ STAB MALFUNCTION A COMA K NONE J WARNING INDICATION CR CRUISE 1 SO 01 952CA 4096 973 7092 STABILIZER TRIM CHANNEL 1 INOPERATIVE MESSAGE ON EICAS. REPLACED THE HORIZONTAL STABILIZER TRIM ACTUATOR. 2 L 7 2 4F RT A21EA 1996053000091 19960530 00091 WP 1996 5 30 DHL96804008 1 19960522 A 3231 37749361 HOOK ASSY DOUG DC8 DC873F 302199F WP RT MLG DOOR MALFUNCTIONED A T DHLA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 SO 01 804DH 46124 RIGHT HAND GEAR DOOR UNSAFE LIGHT AND DOOR UNLATCH LIGHT ON. AFTER GEAR RETRACTION, CYCLED GEAR NUMEROUS TIMES AND LIGH T STAYED ON. FOUND UPPER DOOR TO DOOR LATCH WITH FROZEN BEARING ON PIVOT. REPLACED UPPER DOOR LATCH LINK ASSY AND DOOR HOOK ASSY, OPS CHECK GOOD PER MM 32-31-4. 2 L 7 4 4F RT 4A25 1996053000092 19960530 00092 1996 5 30 DL72K961228 4 19960520 A 2565 146110015 PAX SLIDE BOEING 727 727232 1384082 NM R1 DOOR ZERO PRESS A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 414DA 21256 ON LAYOVER CK, MECH FOUND BOTTLE PRESS ON R-1 SLIDE DAL PART NR 254001002, S/N 43-11 ZERO PRESS REF LOG NR Z713181-002. REMOVED AND REPLACED SLIDE ASSY, NO OTHER PROBLEMS. 2 L 7 3 4F A3WE 1996053000093 19960530 00093 NM 1996 5 30 DL72S961221 1 19960520 A 5320 DOOR FRAME BOEING 727 727232 1384082 NM SERVICE DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 406DA 21150 1 INCH CRACK AT RT AFT SERVICE DOOR FWD FRAME ON FUSE, EXTENDING FROM UPPER STOP PAD CASTING. REPAIRED PER MM 53-13-0. 2 L 7 3 4F A3WE 1996053000094 19960530 00094 NM 1996 5 30 DL72S961222 1 19960520 A 5320 TQ BOX WEB BOEING 727 727232 1384082 NM BS 1233 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 406DA 21150 TORQUE BOX VERTICAL WEB CRACKED 1 INCH AT FASTENER, UPPER ROW OF RIVETS STA 1233 LT LOWER TORQUE BOX. REPAIRED PER M/M 53-11-0 FIG 819. 2 L 7 3 4F A3WE 1996053000095 19960530 00095 NM 1996 5 30 DL72S961223 1 19960520 A 5330 SKIN BOEING 727 727232 1384082 NM R4 WINDOW CUTOUT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 406DA 21150 A .5 INCH CRACK IN FUSELAGE SKIN AT LWR INBD CORNER OF R-4 WINDOW CUTOUT. REPAIRED PER SRM 53-30-3. 2 L 7 3 4F A3WE 1996053000096 19960530 00096 NM 1996 5 30 DL72S961224 1 19960520 A 5522 SKIN BOEING 727 727232 1384082 NM RT ELEV CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 406DA 21150 A .5 INCH CRACK FROM FASTENER RT ELEVATOR LOWER SKIN JUST INBD OF 3RD FROM OUTBD HINGE. REPAIRED PER SRM 55-20-3. 2 L 7 3 4F A3WE 1996053000097 19960530 00097 NM 1996 5 30 DL72W961234 1 19960515 A 5315 FLOOR BEAM BOEING 727 727247 138408F NM BS 1070 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2809W 20581 FOUND ON MV1 CK, CORROSION/RIVETS SHEARD AT CABIN FLOOR BEAM STA 1070 AT RT O/B GALLEY FLOOR TRACK. REPAIRED PER M/M 53 -20-11 FIG 804. 2 L 7 3 4F A3WE 1996053000098 19960530 00098 1996 5 30 DL76L961236 4 19960521 A 2211 FCC COMPUTER BOEING 767 767332 1382001 NM LEFT FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 174DN 24802 EN ROUTE, A/C DIV KEF DUE LT FCC COMPUTER FAILED. ELECTRICAL SMELL IN COCKPIT REPORTED BY FLT CREW. MTC REPLACED THE L T FCC COMPUTER. 2 L 7 2 4F RT A1NM 1996053000099 19960530 00099 NE 1996 5 30 DL76S961254 2 19960522 A 7200 ENGINE BOEING 767 767332 1382001 NM GE CF6 CF680A 30025 NE NR 2 MALFUNCTIONED A DALA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION TO TAKEOFF 1 SO 27 120DL 23279 580372 RT ENG FLAME-OUT JUST AFTER ROTATION. ALL INDICATIONS NORMAL AT LIFTOFF, THEN FLAME-OUT OCCURRED. REPLACED LEAKING FUE L MANIFOLD LINE AND LEAKING FUEL NOZZLE, LEAK CHECK AND ENGINE RUN OK. 2 L 7 2 4F 4 F RT A1NM E13NE 1996053000100 19960530 00100 WP 1996 5 30 MWEA96142 1 19960522 A 3350 1001191 LIGHT ASSY DOUG DC9 DC932 3022066 WP FWD ENTRY INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 502ME 48132 DURING SERVICE CHECK, FOUND FWD ENTRANCE EMERGENCY LIGHT WOULD NOT ILLUMINATE DURING TEST. MAINTENANCE REMOVED AND REPL ACED FWD ENTRANCE EMERGENCY LIGHT ASSEMBLY, OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996053000101 19960530 00101 EU 1996 5 30 QXEA9600176 1 19960517 A 3350 MGG1280 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 457US 11036 OVERHEAD EVACUATION LIGHT ROW 7 WON'T ILLUMINATE. BULBS WERE REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996053000102 19960530 00102 EU 1996 5 30 QXEA9600177 1 19960521 A 3397 WIRE FOKKER F28 F28MK1000 4990808 EU CABIN BROKEN A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 802PH 11017 A PORTION OF THE FLOOR PROXIMITY LIGHTS DID NOT ILLUMINATE WHEN SELECTED ON. BROKEN WIRE REPAIRED AND SEVERAL INOP BULB S WERE REPLACED, LIGHTS OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996053000103 19960530 00103 EU 1996 5 30 QXEA9600178 1 19960523 A 3350 1820 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 452US 11105 CABIN OVERHEAD EMERGENCY LIGHTS SYSTEM HAS SEVERAL BULBS INOP. BULBS WERE REPLACED AND LIGHTS OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996053000104 19960530 00104 NM 1996 5 30 QXEA9600179 1 19960523 A 3350 MS25237327 BULB GRIMES 10005511 DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 815PH 49432 50 COCKPIT EMERGENCY LIGHT WILL NOT TEST. BULB WAS REPLACED AND LANTERN SELF TEST WAS GOOD. 2 H 7 2 4T RT A13NM 1996053000105 19960530 00105 NM 1996 5 30 SCNA96143 1 19960521 A 2910 B-NUT BOEING 727 7272J4 1384006 NM AFT OF PIT WALL DAMAGED A SCNA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 15 284SC 21438 ON ENGINE START, SKYDROL FUMES FILLED THE AFT THIRD OF THE CABIN. INSPECTED A/C AND FOUND A B-NUT LEAKING HYDRAULIC FLU ID BEHIND AFT PIT WALL. REMOVED AND REPLACED LINE WITH A FLEX LINE IN ACCORDANCE WITH MM 20-10-10. SECURED LINE AND LE AK CHECKED WITH ENGINE RUNNING. REMOVED FLEX LINE AND INSTALLED A RIGID LINE ON 5/23/96. 2 L 7 3 4F RT A3WE 1996053000106 19960530 00106 NM 1996 5 30 SCNA96144 1 19960520 A 2612 894120 FIRE LOOP BOEING 727 727259 138408J NM MR 3 FIRE LOOP MALFUNCTIONED A SCNA E ENGINE SHUTDOWN N FALSE WARNING IN INSP/MAINT 1 GL 15 289SC 22475 THE NUMBER 3 ENGINE FIRE WARNING LIGHT ILLUMINATED AND HORN SOUNDED. SHUT DOWN NUMBER 3 ENGINE. REMOVED AND REPLACED N UMBER 3 ENGINE FIRE LOOP, OPS CHECKED OK. 2 L 7 3 4F A3WE 1996053000107 19960530 00107 WP 1996 5 30 SCNA96145 1 19960518 A 3350 BULB DOUG DC10 DC1010 3022110 WP CABIN FAILED A SCNA K NONE L NO TEST UK UNKNOWN 1 GL 15 573SC 46905 ONE EMERGENCY LIGHT BY THE FORWARD LEFT HAND LAV WAS FOUND INOP. PLACED ON MEL. REMOVED AND REPLACED LIGHT BULB IN FLO OR TRACK LIGHT. 2 L 7 3 4F A22WE 1996053000108 19960530 00108 NM 1996 5 30 SCNA96146 1 19960521 A 3350 TRACK LIGHT BOEING 727 7272J4 1384006 NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 288SC 20765 FLOOR EMERGENCY TRACK LIGHTING WAS FOUND INOP AT SEATS 21 DEF. REPAIRED WIRES IN TRACK, OPS CHECK OK. 2 L 7 3 4F RT A3WE 1996053000109 19960530 00109 NM 1996 5 30 UPS96220189 1 19960516 A 5320 STIFFENER BOEING 727 72731C 1384011 NM BS 336 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE-C, CORROSION ON TOP DOGHOUSE BEAM AT BS 336 LBL 15. REMOVED CORROSION, REWORKED OUT OF LIMITS IAW SRM 5 3-10-1, REMOVED AND REPLACED STIFFENER, BEAM IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996053000110 19960530 00110 NM 1996 5 30 UPS96220190 1 19960516 A 5330 SKIN BOEING 727 72731C 1384011 NM BS 1180 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE-C, CORROSION ON SKIN AT STA 1180 STR 7 LT WL 260. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-30-1. REPAIRED SKIN AT STA 1180 STR 7 LT WL 260 IAW SRM 53-30-1. 2 L 7 3 4F A3WE 1996053000111 19960530 00111 NM 1996 5 30 UPS96220191 1 19960516 A 5751 HINGE BOEING 727 72731C 1384011 NM RT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE-C, R/W I/B AILERON CENTER AND O/B TAB HINGE FITTINGS ARE CORRODED AILERON SIDE. REMOVED AND REPLACED CE NTER AND O/B TAB FITTINGS ON R/W, I/B AILERON IAW SRM 51-30-02. 2 L 7 3 4F A3WE 1996053000112 19960530 00112 NM 1996 5 30 UPS96220192 1 19960516 A 5751 AILERON HINGE BOEING 727 72731C 1384011 NM RT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE-C, R/W, O/B AILERON O/B CENTER HINGE FITTING IS CORRODED AILERON SIDE. REMOVED AND REPLACED R/W, O/B AI LERON O/B CENTER HINGE FITTING ON AILERON SIDE IAW SRM 51-30-05, 51-30-02 OHM 20-50-03 AND M/M 57-50-11. 2 L 7 3 4F A3WE 1996053000113 19960530 00113 NM 1996 5 30 UPS96220193 1 19960517 A 5720 HAT CHANNEL BOEING 727 72731C 1384011 NM BS 304-344 CORRDED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE-C, CHANNEL AT BS 304 TO 344 RBL 17, WL 708 WAS FOUND TO BE CORRODED BEYOND LIMITS. REMOVED CORRODED HAT CHANNEL, FABRICATED NEW CHANNEL, REINSTALLED IAW SRM 53-10-01, 51-30-2. 2 L 7 3 4F A3WE 1996053000114 19960530 00114 NM 1996 5 30 UPS96220194 1 19960517 A 5320 HAT CHANNEL BOEING 727 72731C 1384011 NM BS 344 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE-C, CORROSION ON HAT CHANNEL AT STA 344, RBL 25 TO 35 WL 208. CORROSION REMOVAL OUT OF LIMITS, REMOVED C HANNEL, FABRICATED NEW PART, INSTALLED IAW SRM 53-10-1, 51-30-2. 2 L 7 3 4F A3WE 1996053000115 19960530 00115 NM 1996 5 30 UPS96220195 1 19960517 A 5530 FITTING BOEING 727 72731C 1384011 NM RT VERT STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE-C, CRACKED L-EXTRUSION AT RT FIN REAR SPAN CLOSURE RIB FITTING, ACCESS UNDER PANEL 9780. REMOVED AND RE PLACED FITTING IAW SRM 51-30-2, 51-30-5. 2 L 7 3 4F A3WE 1996053000116 19960530 00116 NM 1996 5 30 UPS96420188 1 19960515 A 5320 SHEAR TIE BOEING 747 747123 1384873 NM BS 1560 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE-C, AFT CARGO COMPARTMENT FRAME SHEAR TIE CRACKED AT BS 1560, BETWEEN S-35/36 LT. REMOVED DAMAGED SHEAR TIE AND REPAIRED SHEAR TIE IAW SRM 53-10-04, FIG 4. 2 L 7 4 4F A20WE 1996053000117 19960530 00117 NM 1996 5 30 UPS96420196 1 19960514 A 5311 FRAME BOEING 747 747123 1384873 NM BS 1500 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE-C, AFT CARGO COMP HAD CRACK IN FRAME INNER CHORD AT BS 1500 RT NEAR FLOOR. REMOVED DAMAGED SECTION OF F RAME INNER CHORD AND REPAIRED FRAME IAW SRM 51-40-03. 2 L 7 4 4F A20WE 1996053000118 19960530 00118 NM 1996 5 30 UPS96420197 1 19960517 A 5320 SPLICE BOEING 747 747123 1384873 NM BS 2350 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE-C, CORROSION ON STRINGER SPLICE END STRAP AT BS 2350 S-48R. STRINGER SPLICE END STRAP REPLACED IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996053000119 19960530 00119 NM 1996 5 30 UPS96420198 1 19960517 A 5320 SPLICE BOEING 747 747123 1384873 NM BS 2350 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE-C, CORROSION ON STRINGER SPLICE END STRAP AT STA 2350, S-50 LT. REPLACED STRINGER SPLICE END STRAP IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996053000120 19960530 00120 NE 1996 5 30 9611389926 2 19960522 A 7321 FUEL CONTROL DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9A 52048 NE NR 2 ENGINE LACK OF LUBE A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 926NW 47425 667105 ON CLIMBOUT, THE NR 2 ENGINE EPR INDICATION SPIKED .4 WITH A CORRESPONDING RISE IN N1. THE FLIGHT RETURNED TO MEM AND L ANDED WITHOUT INCIDENT. MAINTENANCE DRAINED THE MOISTURE TRAP AND LUBED THE FUEL CONTROL BELLOWS. ENGINE RUNUP WAS SAT ISFACTORY. 2 L 7 2 4F 4 F A6WE E2EA 1996053000121 19960530 00121 WP 1996 5 30 9611391154 1 19960526 A 2913 887673 HYD PUMP DOUG DC10 DC1040 3023508 WP NR 1 ENGINE BROKEN PLUG A A NWAA A J UNSCHED LANDING DUMP FUEL K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 154US 6188 46763 DURING CLIMBOUT, LOST THE NR 1 HYDRAULIC SYSTEM FLUID. FLIGHT DUMPED 40,000 LBS OF FUEL AND RETURNED TO HNL. MAINTENAN CE REPLACED THE RIGHT HYDRAULIC PUMP AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A22WE 1996053000122 19960530 00122 WP 1996 5 30 9611401149 1 19960523 A 3150 FAIL LIGHT DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20J 52054 NE NR 2 ENGINE ILLUMINATED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 149US 46758 86183 AFTER TAKEOFF POWER WAS APPLIED, THE NR 2 ENGINE FAIL LIGHT ILLUMINATED AT 48 PERCENT N1. CREW ABORTED TAKEOFF AND RETU RNED TO THE GATE. INSPECTED THE NR 2 ENGINE FOR DISCREPANCIES AND NON WERE FOUND. AIRCRAFT RETURNED TO SERVICE, THE NR 2 ENGINE FAIL LIGHT DETECTOR PLACED ON MEL 77-7A. 2 L 7 3 4F 4 F A22WE E20EA 1996053000123 19960530 00123 WP 1996 5 30 9611419974 1 19960523 A 7931 OIL PRESS REG DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7B 52053 NE LT ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 9338 47347 657371 ON TAKEOFF ROLL, NR 1 ENGINE OIL PRESSURE EXCEEDED NORMAL LIMITS. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE OIL FILTER AND OIL PRESSURE REGULATOR VALVE WITH SERVICEABLE UNITS. 2 L 7 2 4F 4 F A6WE E2EA 1996053000124 19960530 00124 WP 1996 5 30 9611429990 1 19960523 A 2910 37723745503 SHUTOFF VALVE DOUG DC9 DC931 3022065 WP RT HYD SYST LEAKING A NWAA D RETURN TO BLOCK B K SMOKE/FUMES/ODORS/SPARKS FLUID LOSS TX TAXI/GRND HDL 1 GL 01 8950E 47186 LOSS OF NOSE WHEEL STEERING ACCOMPANIED BY SMOKE IN CABIN OCCURRED DURING TAXI OUT. RIGHT HYDRAULIC SYSTEM QUANTITY WEN T TO ZERO. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE FOUND RUDDER POWER SHUTOFF VALVE LEAKING. REPLACED VALVE, OPERA TIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996053000125 19960530 00125 WP 1996 5 30 9611439973 1 19960523 A 3230 GEAR HANDLE DOUG DC9 DC931 3022065 WP COCKPIT JAMMED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 9337 47346 LANDING GEAR HANDLE WAS JAMMED IN THE UP POSITION AFTER TAKEOFF. FLIGHT RETURNED TO ATL AND LANDED WITHOUT INCIDENT. E MERGENCY GEAR EXTENSION PROCEDURES WERE UTILIZED FOR LANDING. MAINTENANCE INSPECTED COMPLETE GEAR SYSTEM AND PERFORMED GEAR SWING UP TO TEN TIMES. PROBLEM COULD NOT BE DUPLICATED. 2 L 7 2 4F A6WE 1996053000126 19960530 00126 EU 1996 5 30 COMA9630115 1 19960525 A 3350 6104781 BATTERY PACK SAAB SF340 SF340A 7850100 EU CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 158CA 340A158 FOUR EMERGENCY LIGHTS WERE INOP. REPLACED EMERGENCY LIGHT BATTERY PACK. 2 L 7 2 4T RT A52EU 1996053000127 19960530 00127 EA 1996 5 30 COMA9660093 1 19960524 A 2130 PRESSURE MODULE CNDAIR CL600 CL6002B19 EA CABIN MALFUNCTIONED A COMA G O2 MASK DEPLOYED J WARNING INDICATION DE DESCENT 1 SO 01 914CA 7012 PASSENGER OXYGEN CAUTION MESSAGE ON EICAS, ALL MASK DEPLOYED AUTOMATICALLY. PROBLEM OCCURRED ON TWO SUCCESSIVE FLIGHTS. PLACED THE CABIN PRESSURE ACQUISITION MODULE ON THE DEFERRED MAINTENANCE LIST. ACFT CONTINUED SERVICE. 2 L 7 2 4F RT A21EA 1996053000128 19960530 00128 EA 1996 5 30 COMA9660094 1 19960524 A 2740 13740002 TRIM SWITCH CNDAIR CL600 CL6002B19 EA COCKPIT FAILED A COMA K NONE F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 01 924CA 7026 STABILIZER TRIM CHANNEL 1 INOP MESSAGE ON EICAS. REPLACED FAULTY TRIM SELECT BUTTON. 2 L 7 2 4F RT A21EA 1996053000129 19960530 00129 EA 1996 5 30 COMA9660095 1 19960526 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA RT TE FLAPS MALFUNCTION A COMA O OTHER O OTHER AP APPROACH 1 SO 01 952CA 956 906 7092 FLAPS FAILED AT 18 DEGREES WHEN SELECTED FOR APPROACH. REPLACED THE RT FLAP BRAKE AND POSITION SENSOR UNIT. 2 L 7 2 4F RT A21EA 1996053000130 19960530 00130 NM 1996 5 30 DL72E961269 1 19960513 A 5320 ANGLE BOEING 727 727247 138408F NM BS 400 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2829W 21481 AT MID VISIT FASTENER HOLES WERE FOUND CORRODDED AT STA 400 RBL 33. CAP AND ANGLES REPLACED PER SRM 53-10-8. 2 L 7 3 4F A3WE 1996053000131 19960530 00131 NM 1996 5 30 DL72L961266 1 19960523 A 5743 BEAM BOEING 727 727232 1384082 NM RT MLG CHAFED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 513DA 21315 AFT SIDE OF MLG LOWER SIDE STRUT CHAFING INTO FWD SIDE OF WALKING BEAM RT WING. REPAIRED PER M/M 57-43-0. 2 L 7 3 4F A3WE 1996053000132 19960530 00132 NM 1996 5 30 DL72L961267 1 19960523 A 5754 FITTING BOEING 727 727232 1384082 NM NR 5 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 513DA 21315 A .6875 INCH CRACK IN NR 5 SLAT AT ACTUATOR ATTACH FITTING. REPAIRED PER M/M 57-54-0. 2 L 7 3 4F A3WE 1996053000133 19960530 00133 NM 1996 5 30 DL72L961281 1 19960524 A 5240 6556992553 DOOR FRAME BOEING 727 727232 1384082 NM L2 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 513DA 21315 THE L-2 DOOR FORWARD FRAME HAS A .5 CRACK EMANATING FROM THE LOWER INBOARD CORNER OF THE UPPER HINGE CUTOUT. THIS DAMAG E IS ADDRESSED BY B727 SRM 52-40-2, FIGURE 4. THERE IS AN EXISTING REPAIR LOCATED APPROXIMATELY 2 INCHES ABOVE THE UPPE R HINGE CUTOUT. THE EXISTING REPAIR EXTENDS TO THE UPPER FORWARD CORNER OF THE DOOR FRAME. 2 L 7 3 4F A3WE 1996053000134 19960530 00134 NM 1996 5 30 DL72S961240 1 19960521 A 5530 STRINGER BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 537DA 22073 FOUND DURING B-2 LETTER CHECK, STRINGER CRACKED RT SIDE 2ND BAY UP FROM ACCESS PNL 9504. REPAIRED PER M/M 55-30-0 FI G 803. 2 L 7 3 4F A3WE 1996053000135 19960530 00135 NM 1996 5 30 DL72S961241 1 19960521 A 5530 STRINGER BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 537DA 22073 FOUND DURING B-2 LETTER CHECK, TWO STRINGERS CRACKED 3RD BAY FROM TOP RT SIDE VERT STAB. REPAIRED PER M/M 55-30-0 PG 80 3. 2 L 7 3 4F A3WE 1996053000136 19960530 00136 NM 1996 5 30 DL72S961242 1 19960521 A 5530 WEB BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 537DA 22073 FOUND DURING B-2 LETTER CHECK, WEB ANGLE CRACKED LT SIDE 2ND BAY UP FROM ACCESS PANEL 9504. REPAIRED PER M/M 55-30-0 FI G 802. 2 L 7 3 4F A3WE 1996053000137 19960530 00137 NM 1996 5 30 DL72S961244 1 19960521 A 5530 STRINGER BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 537DA 22073 FOUND DURING B-2 LETTER CHECK, STRINGER CRACKED 2ND BAY FROM TOP LT SIDE. REPAIRED PER M/M 55-30-0 FIG 803. 2 L 7 3 4F A3WE 1996053000138 19960530 00138 NM 1996 5 30 DL72S961245 1 19960521 A 5530 STRINGER BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 537DA 22073 FOUND DURING B-2 LETTER CHECK, STRINGER CRACKED 1ST BAY FROM TOP OF VERT STAB LT SIDE. REPAIRED PER M/M 55-30-0 FIG 803 . 2 L 7 3 4F A3WE 1996053000139 19960530 00139 NM 1996 5 30 DL72S961246 1 19960521 A 5330 SKIN BOEING 727 727232 1384082 NM BS 1243 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 537DA 22073 FOUND DURING B-2 LETTER CHECK, LIGHTENING HOLE CRACKED RT LOWER TORQUE BOX STA 1243. REPAIRED PER M/M 53-11-0 PG 828. 2 L 7 3 4F A3WE 1996053000140 19960530 00140 NM 1996 5 30 DL72S961247 1 19960521 A 5542 SKIN BOEING 727 727232 1384082 NM LWR RUDDER CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 537DA 22073 FOUND DURING B-2 LETTER CHECK, 1 INCH CRACK LWR RUDDER SKIN LT SIDE. REPAIRED PER SRM 55-20-3 FIG 1. 2 L 7 3 4F A3WE 1996053000141 19960530 00141 NM 1996 5 30 DL72S961248 1 19960521 A 5210 DOOR FRAME BOEING 727 727232 1384082 NM L 2 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 537DA 22073 FOUND DURING B-2 LETTER CHECK, L-2 DOOR FRAME CRACKED AT UPPER HINGE CUTOUT. REPAIRED PER SRM 52-40-4. 2 L 7 3 4F A3WE 1996053000142 19960530 00142 NM 1996 5 30 DL72S961249 1 19960521 A 5330 SKIN BOEING 727 727232 1384082 NM BS 1080-1100 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 490DA 21020 FROM AC LOG 759101001, FUSELAGE SKIN DENTED FS 1080 THROUGH 1100 STR 23L. STR 23L AND SKIN REPAIRED PER ERA 303624-14. 2 L 7 3 4F A3WE 1996053000143 19960530 00143 NM 1996 5 30 DL72S961251 1 19960521 A 3350 LIGHT BOEING 727 727232 1384082 NM AIRSTAIRS INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 475DA 20752 EMERGENCY EXIT LIGHT OVER BOTTOM STEP OF AIRSTAIRS INOP. REPLACED BATTERIES AND BULB, NO HELP. REPLACED LIGHT ASSY, OP N NORMAL. 2 L 7 3 4F A3WE 1996053000144 19960530 00144 NM 1996 5 30 DL72S961268 1 19960523 A 3350 1000677 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 405DA 21149 L-1 DOOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY, OP CKS GOOD. 2 L 7 3 4F A3WE 1996053000145 19960530 00145 NM 1996 5 30 DL72S961273 1 19960524 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 2 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 490DA 21020 COVE SKIN ATTACH ANGLE CRACKED 1 INCH AT ANTI-ICE TUBE CUTOUT, NR 2 SLAT. REPAIRED PER M/M 57-54-0. 2 L 7 3 4F A3WE 1996053000146 19960530 00146 NM 1996 5 30 DL72S961279 1 19960526 A 3350 90085A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 537DA 22073 ON L/O, FOUND RT AFT EMERGENCY SLIDE LIGHT FLASHING. REPLACED BATTERY PACK, CK'S GOOD. 2 L 7 3 4F A3WE 1996053000147 19960530 00147 NM 1996 5 30 DL72S961284 1 19960526 A 5312 BULKHEAD BOEING 727 727232 1384082 NM BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 522DA 21582 CRACKS EMANATING FROM VERTICAL STIFFENERS AT LBL AND RBL 8 ON STA 1183 BULKHEAD. REPAIRED PER EO 4-59275-3AD. 2 L 7 3 4F A3WE 1996053000148 19960530 00148 NM 1996 5 30 DL72S961286 1 19960522 A 5330 65C139132 SKIN BOEING 727 727232 1384082 NM BS 1044 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 537DA 22073 SKIN CORROSION AT STRINGER 28L, STA 1044 TO 1047, CUTOUT IS 3 BY 1.75 INCH. REPAIRED PER DAL ER/A 303626-14. 2 L 7 3 4F A3WE 1996053000149 19960530 00149 NM 1996 5 30 DL72S961287 1 19960522 A 5330 SKIN BOEING 727 727232 1384082 NM BS 1080 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 490DA 21020 AIRCRAFT STRUCK BY A GROUND SERVICE TRUCK, DAMAGE CONSISTED OF A DENTED SKIN, A BROKEN STRINGER AND A CRACKED SHEAR CLIP . THE DENT WAS REMOVED WITH A CUTOUT AT STA 1080, THE STRINGER HAS BEEN CUT AND WILL BE SPLICED IN THE BAYS FWD AND AFT OF THE DAMAGE. ALSO, THE CLIP ABOVE STR-22L HAS BEEN TRIMMED OFF. ALL DAMAGE WILL BE REPAIRED PER THE SRM. 2 L 7 3 4F A3WE 1996053000150 19960530 00150 NM 1996 5 30 DL72S961291 1 19960522 A 5320 651751737 TRANSVERSE BEAM BOEING 727 727232 1384082 NM FS 1263 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 537DA 22073 CRACK IN ANGLE OF THE FWD TRANSVERSE BEAM AND AFT CHANNEL OF THE RT TORQUE BOX AT FS 1263. THIS AREA IS SUBJECT OF AD 9 4-07-08 WHICH REQUIRES INSPECTION PER S/B 53-0129. THIS ERA WILL REPLACE THE DAMAGED PART IN ACCORDACE WITH THE S/B. 2 L 7 3 4F A3WE 1996053000151 19960530 00151 NM 1996 5 30 DL72S961293 1 19960521 A 5320 651751737 TRANSVERSE BEAM BOEING 727 727232 1384082 NM FS 1263 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 406DA 21150 CRACK IN ANGLE OF THE FWD TRANSVERSE BEAM AND AFT CHANNEL OF THE RT TORQUE BOX AT FS 1263. THIS AREA IS SUBJECT OF AD 9 4-07-08 WHICH REQUIRES INSPECTION PER S/B 53-0129. THIS ERA WILL REPLACE THE DAMAGED PART IN ACCORDANCE WITH THE S/B. 2 L 7 3 4F A3WE 1996053000152 19960530 00152 NM 1996 5 30 DL72S961295 1 19960517 A 5330 65545661 SKIN BOEING 727 727232 1384082 NM FS 480-496 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 477DA 20754 CORROSION WAS FOUND IN THE SKIN AT FS 496 AND S-27R. THE CUTOUT FOR THE CORROSION MEASURED 1.25 IB/OB AND 2.75 FORE/AFT . IN ADDITION, AN INTERNAL REPAIR DOUBLER PREVIOUSLY INSTALLED PER 207602-14 WAS REMOVED JUST FWD OF THE NEW CUTOUT. T HE PREVIOUS CUTOUT RUNS FROM S-28R TO THE S-26R LAP AND FROM FS 480 SPLICE AFT TO APPROX FS 490. REPAIRED PER DAL ER/A 303236-14, REV A. 2 L 7 3 4F A3WE 1996053000153 19960530 00153 NM 1996 5 30 DL72S961299 1 19960523 A 5343 TRUNNION FTG BOEING 727 727232 1384082 NM NLG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 522DA 21582 AT MID VISIT, BORE OF NLG FITTING WAS FOUND TO BE PITTED. AREA SPOTFACED, BORED DYE CHECKED, ROTOPEENED AND BUSHING INS TALLED PER M/M 53-40-0. 2 L 7 3 4F A3WE 1996053000154 19960530 00154 NM 1996 5 30 DL72S961300 1 19960523 A 3221 TRUNNION FTG BOEING 727 727232 1384082 NM NLG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 522DA 21582 AT MID VISIT, THE NLG TRUNNION FITTING WAS FOUND TO BE CORRODED. REPAIRED PER MM 53-40-0. 2 L 7 3 4F A3WE 1996053000155 19960530 00155 NE 1996 5 30 DL72W961250 2 19960521 A 7314 734001139 FUEL PUMP BOEING 727 727247 138408F NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE FAILED A DALA E ENGINE SHUTDOWN X ENGINE FLAMEOUT TO TAKEOFF 1 SO 27 2817W 20873 687605 NUMBER 1 ENGINE SHUTDOWN 30 SECONDS AFTER LIFT OFF. FOUND SHAFT SHEARED ON FUEL PUMP. REPLACED PUMP AND CONTROL. 2 L 7 3 4F 4 F A3WE E2EA 1996053000156 19960530 00156 NM 1996 5 30 DL72W961256 1 19960522 A 5530 STRINGER BOEING 727 727247 138408F NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2813W 20869 FOUND DURING A-2 LETTER CHECK, 1 INCH CRACK AT STRINGER TO BULKHEAD ATTACH BOLT AT FIN STA 180.6 STR 8 LT SIDE. REPAIRE D PER M/M 55-30-0 FIG 803. 2 L 7 3 4F A3WE 1996053000157 19960530 00157 NM 1996 5 30 DL72W961257 1 19960522 A 5532 SKIN BOEING 727 727247 138408F NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2813W 20869 FOUND DURING A-2 LETTER CHECK, TWO .25 INCH CRACKS AT CONSECUTIVE RIVET HOLES LT SIDE OF VERT STAB 10 FT AFT OF NR 2 ENG INLET. REPAIRED PER M/M 54-30-0 FIG 801. 2 L 7 3 4F A3WE 1996053000158 19960530 00158 NM 1996 5 30 DL72W961258 1 19960522 A 5240 HINGE CUTOUT BOEING 727 727247 138408F NM L2 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2813W 20869 FOUND DURING A-2 LETTER CHECK, L-2 DOOR UPPER HINGE CUTOUT CRACKED. REPAIRED PER SRM 52-40-2. 2 L 7 3 4F A3WE 1996053000159 19960530 00159 NM 1996 5 30 DL72W961270 1 19960523 A 3350 LIGHT BOEING 727 727247 138408F NM COCKPIT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2815W 20871 ON T/S INSP, FOUND COCKPIT OVER DOOR EMERGENCY EXIT/FLASHLIGHT DID NOT OPERATE IN THE ON POSITION DURING TEST. REPLACED ASSEMBLY 334701743. 2 L 7 3 4F A3WE 1996053000160 19960530 00160 NM 1996 5 30 DL72W961282 1 19960518 A 5330 6554590 SKIN BOEING 727 727247 138408F NM BS 720 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2809W 20581 SKIN CORROSION AT STA 720F AT STRINGER 27R. DAMAGE REMOVAL RESULTED IN A 1.75 BY 5 INCH CUTOUT JUST FWD OF AN EXISTING REPAIR AT STA 730, ERA 213172. EXISTING REPAIR REQUIRED THE REMOVAL OF THE CORNER OF THE LWR SKIN AT STA 740 AND STRING ER 26R. REPAIRED PER DAL ER/A 303611-14, REV A. 2 L 7 3 4F A3WE 1996053000161 19960530 00161 NM 1996 5 30 DL72W961283 1 19960524 A 5330 6554590 SKIN BOEING 727 727247 138408F NM BS 700 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2809W 20581 SKIN CORROSION AND CRACK JUST FWD OF STA 700 BETWEEN STRINGERS 28L AND 28R NEAR BL 0. CUTOUT MEASURED 7.5 BY 3.75 INCH. REPAIRED PER DAL ER/A 303637-14, REV A. 2 L 7 3 4F A3WE 1996053000162 19960530 00162 NM 1996 5 30 DL72W961289 1 19960523 A 5312 BULKHEAD BOEING 727 727247 138408F NM STA 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2813W 20869 A .5 CRACK FOUND IN 1183 BULKHEAD AT RBL 8 AND WL 172. THIS ERA WILL GIVE INSTRUCTIONS TO ACCOMPLISH A REPAIR UNTIL THE FULL MODIFICATION REQUIRED BY AD 90-06-09 IS ACCOMPLISHED. THE REPAIR WILL BE INSTALLED ON THE FORWARD SIDE OF THE 118 3 BULKHEAD. 2 L 7 3 4F A3WE 1996053000163 19960530 00163 NM 1996 5 30 DL72W961290 1 19960519 A 5330 6518420482 SKIN BOEING 727 727247 138408F NM L1 DOOR CUTOUT FATIGUE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2807W 20579 THE FUSELAGE SKIN AND UNDERLYING DOUBLER WAS FOUND TO HAVE A ONE INCH CRACK IN THE UPPER FWD CORNER OF THE L-1 DOOR CUTO UT. REPAIRED PER DAL ER/A 303614-14AD. 2 L 7 3 4F A3WE 1996053000164 19960530 00164 NM 1996 5 30 DL72W961294 1 19960522 A 5320 651751737 TRAVERSE BEAM BOEING 727 727247 138408F NM FS 1263 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2813W 20869 CRACK IN ANGLE OF THE FWD TRANSVERSE BEAM AND AFT CHANNEL OF THE RT TORQUE BOX AT FS 1263. THIS AREA OF THE TORQUE BOX IS THE SUBJECT OF AD 94-07-08 WHICH REQUIRES INSPECTION PER S/B 53-0129. THIS ER/A WILL REPLACE THE DAMAGED PART IN ACC ORDANCE WITH THE S/B. 2 L 7 3 4F A3WE 1996053000165 19960530 00165 NE 1996 5 30 P5CA9600234 2 19960527 A 7320 63030006 CONDITION MOTOR BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 2 ENGINE INOPERATIVE A P5CA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 23 851FT 19756 663048 NR 2 ENGINE WOULD NOT START AFTER PUSH BACK, RETURNED TO BLOCKS. REMOVED AND REPLACED NR 2 FUEL CONDITION MOTOR PER MM 76-11-04. 2 L 7 4 4F 4 F A20WE E20EA 1996053000166 19960530 00166 EU 1996 5 30 QXEA9600181 1 19960526 A 3350 1315 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 462AU 11054 ONE 28V AISLE EMERGENCY LIGHT IS INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996053000167 19960530 00167 EU 1996 5 30 QZEA9600180 1 19960525 A 3350 1820 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 802PH 11017 EVAC LIGHT AT GALLEY IS OUT. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996053000168 19960530 00168 NM 1996 5 30 SCNA96147 1 19960523 A 5313 BAC1498132 STRINGER BOEING 727 727225 1384077 NM BS 950-970 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 282SC 22558 DURING HEAVY MAINTENANCE VISIT, CORROSION AND A CRACK WERE FOUND AT BS 970, STRINGER 28L. CUT OUT CORRODED SKIN AND STR INGER AT BS 960 TO 980, FABRICATED AND INSTALLED REPAIRS IN ACCORDANCE WITH B727 SRM 51-30-2. 2 L 7 3 4F A3WE 1996053000169 19960530 00169 NM 1996 5 30 SCNA96148 1 19960523 A 5313 BAC1498132 STRINGER BOEING 727 727225 1384077 NM BS 993 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 282SC 22558 DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON STRINGER 29R AT BS 993. FABRICATED AND INSTALLED REPAIR IN ACCOR DANCE WITH SB 727-53-0179, LMAC EO 3775, B727 SRM 53-10-2 FIGURE 5, SHEET 22, ITEM 42, AND SRM 53-30-10. 2 L 7 3 4F A3WE 1996053000170 19960530 00170 NM 1996 5 30 SCNA96149 1 19960521 A 5320 ATTACH ANGLES BOEING 727 727225 1384077 NM BS 1263 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 282SC 22558 DURING HEAVY MAINTENANCE VISIT, CRACKS WERE FOUND IN THE AFT VENTRAL STAIRWAY RT TORQUE BOX ATTACH ANGLES. REMOVED AND REPLACED ANGLES IN ACCORDANCE WITH SRM 51-30 AND SB 727-53-0129 REVISION 4, PART 3. 2 L 7 3 4F A3WE 1996053000171 19960530 00171 NM 1996 5 30 SWAA960420 1 19960517 A 3320 BALLAST BOEING 737 7373H4 1384600 NM AFT LAV OVERHEAT A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 310SW 22949 IN FLIGHT, AIRCRAFT DIVERTED TO PHX DUE TO CHEMICAL SMELL IN AFT CABIN AREA. AIRCRAFT LANDED AT PHX WITHOUT INCIDENT. I NSPECTED AND FOUND MIRROR LIGHT C/B TRIPPED. AFT LAVATORY BALLAST HAD OVERHEATED AND WAS CAUSING SMELL. REPLACED BALLA ST AND SOCKET PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996053000172 19960530 00172 NM 1996 5 30 SWAA960421 1 19960522 A 3350 P4010021 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 325SW 23689 DURING SCHEDULED A1 CHECK, FOUND FWD I/B EMERGENCY FLASHLIGHT LOW BATTERY. REPLACED BATTERY PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996053000173 19960530 00173 NM 1996 5 30 SWAA960422 1 19960522 A 3350 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 355SW 25250 DURING SCHEDULED B/C CHECK, FOUND EMERGENCY TRACK LIGHTING INOP AT ROWS 12 DEF AND 14ABC. REPLACED BATTERY PACK AND HOU SING PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996053000174 19960530 00174 NM 1996 5 30 SWAA960423 1 19960521 A 5330 SKIN BOEING 737 7372H4 138448C NM SERV DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 95SW 23054 DURING SCHEDULED B-CHECK, FOUND AFT SERV DOOR UPPER HINGE CUTOUT CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996053000175 19960530 00175 NM 1996 5 30 SWAA960424 1 19960521 A 5330 SKIN BOEING 737 7372H4 138448C NM FWD PAX DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 95SW 23054 DURING SCHEDULED B-CHECK, FOUND FWD ENTRY DOORWAY CRACKED AT LOWER HINGE CUTOUT AND AT FWD UPPER CORNER. REPAIRED PER B OEING SRM. 2 L 7 2 4F A16WE 1996053000176 19960530 00176 NM 1996 5 30 SWAA960425 1 19960409 A 3350 20121 BATTERY PACK BOEING 737 7375H4 138449D NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 506SW 24183 FOUND ESCAPE PATH LIGHTING INOP AT ROW 10. RECONNECTED NUMEROUS WIRES AND REPLACED BATTERY PACK AT MID CABIN AREA PER B OEING M/M. 2 L 7 2 4F RT A16WE 1996053000177 19960530 00177 NM 1996 5 30 SWAA960426 1 19960521 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 312 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 95SW 23054 DURING SCHEDULED B-CHECK, FOUND UPPER LOBE FUSELAGE SKIN GOUGED AT BS 312, BETWEEN S4 AND 5L, ABOVE FWD ENTRY DOOR. REP AIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996053000178 19960530 00178 NM 1996 5 30 SWAA960427 1 19960520 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727B AT S18R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996053000179 19960530 00179 NM 1996 5 30 SWAA960428 1 19960520 A 3260 GEAR LIGHT BOEING 737 7373G7 1384595 NM RT MLG ILLUMINATED A SWAA O OTHER N FALSE WARNING IN INSP/MAINT 1 SW 07 691WN 23781 INBOARD INTO DAL, RIGHT MAIN GEAR UNSAFE LIGHT ILLUMINATED. GEAR WAS RECYCLED AND RECEIVED NORMAL INDICATION. AIRCRAFT LANDED AT DAL WITHOUT INCIDENT. GEAR RETRACTION TESTED SEVERAL TIMES AND CHECKED SENSORS PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996053000180 19960530 00180 NM 1996 5 30 SWAA960429 1 19960522 A 3350 6128251 CHARGER BOEING 737 7373Y0 1384671 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 682SW 23496 DURING SCHEDULED A1 CHECK, FOUND FWD TRACK LIGHTING INOP. REPLACED BATTERY CHARGER PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996053000181 19960530 00181 NM 1996 5 30 SWAA960430 1 19960521 A 3350 BATTERY PACK BOEING 737 7373G7 1384595 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 690SW 23783 FOUND AFT UPPER EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996053000182 19960530 00182 NM 1996 5 30 SWAA960431 1 19960519 A 3350 BATTERY PACK BOEING 737 7373T0 1384582 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 697SW 23838 FOUND AFT CABIN UPPER EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996053000183 19960530 00183 NM 1996 5 30 SWAA960432 1 19960519 A 3350 P42010021 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 374SW 26582 FOUND AFT CABIN LOWER EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996053000184 19960530 00184 NM 1996 5 30 SWAA960433 1 19960519 A 2612 FIRE WARNING BOEING 737 7372H4 138448C NM APU SOUNDED A SWAA F ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 SW 07 27SW 21262 ON TAXI OUT, APU FIRE WARNING SOUNDED. CREW PERFORMED APU SHUTDOWN PROCEDURES AND FIRE BOTTLE DISCHARGED. AIRCRAFT RET URNED TO GATE. INSPECTED WITH NO EVIDENCE OF FIRE OR OVERHEAT CONDITION. REPLACED FIRE BOTTLE PER BOEING M/M, CONTINUE D PER MEL 26-6. 2 L 7 2 4F A16WE 1996053000185 19960530 00185 NM 1996 5 30 SWAA960434 1 19960520 A 3260 SPLICE BOEING 737 7373H4 1384600 NM NLG LOOSE A SWAA O OTHER N FALSE WARNING DE DESCENT 1 SW 07 307SW 22947 IN FLIGHT, RED NOSE GEAR LIGHT ILLUMINATED, NO AIR NOISE NOTED. CYCLED GEAR HANDLE, NO HELP. ON GEAR EXTENSION HAD ALL GREEN INDICATION. INSPECTED AND FOUND A WIRE PULLED FROM SPLICE IN NOSE W/W. REPAIRED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996053000186 19960530 00186 NM 1996 5 30 SWAA960435 1 19960520 A 5330 SKIN BOEING 737 7373A4 1384585 NM BS 956 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 956, 1 BELOW S19R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996053000187 19960530 00187 NM 1996 5 30 SWAA960436 1 19960520 A 5330 SKIN BOEING 737 7372T4 1384492 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED TERMINAL CHECK, FOUND LEFT FUSELAGE SKIN CRACKED AT BS 727 BELOW WINDOW 7TH FROM EMERGENCY EXIT S15. R EPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996053000188 19960530 00188 NM 1996 5 30 SWAA960437 1 19960520 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 90SW 22905 DURING SCHEDULED TERMINAL CHECK, FOUND RIGHT FUSELAGE SKIN CRACKED AT GROUND SERVICE DOOR CUTOUT LT CORNER. REPAIRED PE R BOEING SRM. 2 L 7 2 4F A16WE 1996053000189 19960530 00189 NM 1996 5 30 SWAA960438 1 19960520 A 5320 STR CLIP BOEING 737 7372H4 138448C NM BS 747 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21722 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP DAMAGED AT BS 747, S20L. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996053000190 19960530 00190 NM 1996 5 30 SWAA960439 1 19960520 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21722 DURING SCHEDULED D-CHECK, FOUND L-ANGLE CRACKED AT BS 540, LBL 41, WL 156. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996053000191 19960530 00191 NM 1996 5 30 SWAA960440 1 19960520 A 5320 WEB BOEING 737 7372H4 138448C NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 85SW 22826 DURING SCHEDULED D-CHECK, FOUND WEB CRACK AT BS 727, LBL 15, WL 176. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996053000192 19960530 00192 NM 1996 5 30 SWAA960441 1 19960520 A 5320 SHEAR TIE BOEING 737 7372H4 138448C NM BS 947.5 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 85SW 22826 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE GOUGED AT BS 947.5 BETWEEN STRINGER 22 AND 23R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996053000193 19960530 00193 NM 1996 5 30 SWAA960442 1 19960520 A 5320 STR CLIP BOEING 737 7372H4 138448C NM BS 867 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 85SW 22826 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 867 AT S20R. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996053000194 19960530 00194 NM 1996 5 30 SWAA960443 1 19960520 A 5320 SPLICE BOEING 737 7372H4 138448C NM BS 907 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 85SW 22826 DURING SCHEDULED D-CHECK, FOUND CORROSION ON O/B SIDE OF STRINGER PRODUCTION SPLICE AT BS 907, S25L. REPAIRED PER BOEIN G SRM. 2 L 7 2 4F A16WE 1996053000195 19960530 00195 NM 1996 5 30 SWAA960444 1 19960520 A 5230 DOOR FRAME BOEING 737 7372H4 138448C NM BS 847 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 85SW 22826 DURING SCHEDULED D-CHECK, FOUND AFT CARGO DOOR FRAME WEB CRACKED AT BS 847, RBL 26, WL 166. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996053000196 19960530 00196 NM 1996 5 30 SWAA960445 1 19960520 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 400 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 85SW 22826 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME AT BS 400 DENTED AT LBL 28, WL 157, LBL 36, LBL 161, LBL 53, WL 173. REP AIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996053000197 19960530 00197 NM 1996 5 30 SWAA960446 1 19960520 A 5241 FRAME BOEING 737 7372H4 138448C NM FWD GALLEY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 85SW 22826 DURING SCHEDULED D-CHECK, FOUND FWD GALLEY DOOR FRAME CRACKED AT NR 3 STOP FITTING CUTOUT. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996053000198 19960530 00198 NM 1996 5 30 SWAA960447 1 19960520 A 5210 GATE BEAM BOEING 737 7372H4 138448C NM FWD ENTRY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 85SW 22826 DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR LOWER GATE BEAM CRACKED AT LOWER FORWARD CORNER. REPAIRED PER BOEING SRM . 2 L 7 2 4F A16WE 1996053000199 19960530 00199 NM 1996 5 30 SWAA960448 1 19960520 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 308 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 85SW 22826 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED JUST FWD OF FWD ENTRY, BS 308 BETWEEN S10 AND 13L. REPAIRED PER BO EING SRM AND EWO 96-0187. 2 L 7 2 4F A16WE 1996053000200 19960530 00200 NM 1996 5 30 SWAA960449 1 19960520 A 5320 SPLICE CAP BOEING 737 7372H4 138448C NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 85SW 22826 DURING SCHEDULED D-CHECK, FOUND CHORD SPLICE CAP CORRODED AT BS 1016, LBL 4, WL 188. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996053000201 19960530 00201 NM 1996 5 30 SWAA960450 1 19960520 A 3350 LIGHT BOEING 737 7372H4 138448C NM PAX DOOR DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 85SW 22826 DURING SCHEDULED D-CHECK, AFT LEFT ENTRY DOOR EXTERNAL EMERGENCY EXIT LIGHT ASSEMBLY DAMAGED. REPLACED AND PERFORMED EM ERGENCY LIGHT TEST PER BOEING M/M. 2 L 7 2 4F A16WE 1996053000202 19960530 00202 NM 1996 5 30 SWAA960451 1 19960520 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 997 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 85SW 22826 DURING SCHEDULED D-CHECK, FOUND STRINGER 27L DAMAGED AT BS 997. REPLACED DAMAGED SECTION PER BOEING SRM. 2 L 7 2 4F A16WE 1996053000203 19960530 00203 NM 1996 5 30 SWAA960452 1 19960520 A 5320 CHORD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 85SW 22826 DURING SCHEDULED D-CHECK, FOUND VERTICAL CHORD CRACKED AT BS 178, WL 184, LBL 4.7. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996053000204 19960530 00204 NM 1996 5 30 UPS96220199 1 19960519 A 5241 GATE BEAM BOEING 727 72731C 1384011 NM MID GALLEY DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE-C, CORROSION ON MID GALLEY LOWER GATE BEAM FORWARD SIDE INSIDE ON DOOR UNDER LEVELING COMPOUND STA 642, WL 217, RBL 69. CORROSION REMOVAL ON BEAM WAS OUT OF LIMITS, RELOCATED MID GALLEY LOWER GATE BEAM PER SRM 51-30-02. 2 L 7 3 4F A3WE 1996053000205 19960530 00205 NM 1996 5 30 UPS96220200 1 19960518 A 5330 SKIN BOEING 727 72731C 1384011 NM BS 705-713 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE-C, CORROSION ON INNER SKIN AT BS 705 TO 713, RBL 27 WL 153 UNDER RIGHT HAND WATER SEPARATOR. MECHANICAL LY REMOVED CORROSION, REWORK OUT OF LIMITS IAW SRM 53-10-01 AND 53-30-01. REPAIRED SKIN STA 705 TO 713 RBL 27, WL 153, IAW SRM 53-30-03. 2 L 7 3 4F A3WE 1996053000206 19960530 00206 NM 1996 5 30 UPS96220201 1 19960517 A 5320 SHEAR TIE BOEING 727 72731C 1384011 NM BS 660 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE-C, CORROSION ON SHEAR TIE AT BS 660 LBL 11 WL 150. REMOVED CORROSION, REWORK OUT OF LIMITS IAW SRM 53-1 0-01. REPAIRED FRAME SHEAR TIE STA 660 IAW SRM 51-40-03. 2 L 7 3 4F A3WE 1996053000207 19960530 00207 NM 1996 5 30 UPS96220202 1 19960517 A 5320 BEAM BOEING 727 72731C 1384011 NM BS 344 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE-C, CORROSION ON TOP DOGHOUSE BEAM AT BS 344, LBL 15. REMOVED AND REPLACED STIFFENER IAW SRM 51-30-02. 2 L 7 3 4F A3WE 1996053000208 19960530 00208 NM 1996 5 30 UPS96220203 1 19960422 A 5320 SHEAR TIE BOEING 727 72727C 138400J NM BS 990 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE-D, STA 990 AT STR 3R SHEAR TIE IS CRACKED. REMOVED, FABRICATED AND INSTALLED CLIP IAW SRM 51-10-01, 51- 30-02. 2 L 7 3 4F A3WE 1996053000209 19960530 00209 NM 1996 5 30 UPS96220209 1 19960521 A 5312 BULKHEAD FITTING BOEING 727 72731C 1384011 NM BS 1183 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE-C, FOUND BULKHEAD FITTINGS TO BE CORRODED AND CRACKED STR 20R BS 1183 WL 190. REMOVED AND REPLACED CRAC KED AND CORRODED FITTINGS STA 1183 STR 20R IAW 51-10-1, 51-10-2, 51-30-5. 2 L 7 3 4F A3WE 1996053000210 19960530 00210 NM 1996 5 30 UPS96220210 1 19960521 A 5754 BULLNOSE LUGS BOEING 727 72731C 1384011 NM NR 2 LE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE-C, NR 2 K-FLAP BULLNOSE LUGS CORRODED. REMOVED AND REPLACED NR 2 K-FLAP BULLNOSE IAW OHM 57-51-21 AND M /M 27-81-01. 2 L 7 3 4F A3WE 1996053000211 19960530 00211 NM 1996 5 30 UPS96220211 1 19960521 A 5754 BULLNOSE LUGS BOEING 727 72731C 1384011 NM NR 1 LE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE-C, NR 1 K-FLAP BULLNOSE LUGS CORRODED. REMOVED AND REPLACED BULLNOSE LUGS IAW M/M 27-81-01 AND OHM 57-5 1-01. 2 L 7 3 4F A3WE 1996053000212 19960530 00212 NM 1996 5 30 UPS96220212 1 19960521 A 5754 HINGE FITTING BOEING 727 72731C 1384011 NM NR 4 LE FLAP PITTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE-C, R/W NR 4 K-FLAP FIXED L/E CTR HINGE FITTING IS PITTIED. REMOVED AND REPLACED NR 4 K-FLAP CENTER HING E FITTING IAW OHM 57-51-21. 2 L 7 3 4F A3WE 1996053000213 19960530 00213 NM 1996 5 30 UPS96220213 1 19960521 A 5754 BULLNOSE LUGS BOEING 727 72731C 1384011 NM NR 3 LE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE-C, NR 3 K-FLAP BULLNOSE LUGS CORRODED. REMOVED AND REPLACED NR 3 BULLNOSE IAW 57-51-21. 2 L 7 3 4F A3WE 1996053000214 19960530 00214 NM 1996 5 30 UPS96220214 1 19960520 A 5753 SKIN BOEING 727 72731C 1384011 NM RT TE FLAP DISBONDED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE-C, RIGHT WING I/B AFT FLAP UPPER SIDE 17 O/B FROM I/B END AND 13 FWD FROM T/E IS DISBONDED. REMOVED DAM AGE AND REPAIRED DISBONDED IAW SRM 51-40-06. 2 L 7 3 4F A3WE 1996053000215 19960530 00215 NM 1996 5 30 UPS96220215 1 19960520 A 5313 STRINGER BOEING 727 72731C 1384011 NM BS 1125-1180 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE-C, FOUND STRINGER 15R CRACKED AT SEVERAL LOCATIONS FROM STA 1125 TO 1180. REMOVED AND REPLACED STRINGER SECTION NR 15R STATION 1125 TO 1180 IAW 53-10-03. 2 L 7 3 4F A3WE 1996053000216 19960530 00216 NM 1996 5 30 UPS96220216 1 19960526 A 5330 SKIN BOEING 727 72731C 1384011 NM BS 1108 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE: C. CORROSION ON EXTERIOR FUSELAGE SKIN ABOVE AFT CARGO DOOR. REMOVED CORROSION AND FOUND TO BE OUT O F LIMITS IAW 53-10-1. REMOVED DAMAGED SKIN AND FABRICATED REPAIR PARTS IAW TRANCO EWO - 96-2307, SRM'S 53-30-0, 51-10-2 , 51-20-1. 2 L 7 3 4F A3WE 1996053000217 19960530 00217 NM 1996 5 30 UPS96520205 1 19960504 A 3350 BULBS BOEING 757 75724APF 1384969 NM CABIN FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 411UP 23851 CABIN EMERGENCY EXIT LIGHT ASSEMBLY HAS SEVERAL BURNED OUT BULBS. RELAMPED ASSEMBLY, TEST NORMALLY. 2 L 7 2 4F RT A2NM 1996053000218 19960530 00218 NM 1996 5 30 UPS96520206 1 19960525 A 3260 43467410332205 GEAR IND LGHT BOEING 757 75724APF 1384969 NM INSTR PANEL DEFECTIVE A IPXA O OTHER P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 454UP 25475 CREW HAD ON GEAR DOWN AND LOCKED INDICATION. FOUND THE CAP ASSEMBLY OF THE INDICATOR LIGHT WOULD NOT LOCK INTO THE BASE , THIS CAUSED THE BULB TO NOT WORK. REPLACED NOSE GEAR INDICATION LIGHT ASSEMBLY NR 434-674-1033-2205, CHECKED OP AND O PS OK. 2 L 7 2 4F RT A2NM 1996053000219 19960530 00219 NM 1996 5 30 UPS96620207 1 19960525 A 2560 DOOR ROPE BOEING 767 76734AF 1385212 NM L1 DOOR FRAYED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 301UP 27239 L1 DOOR ROPE HAS FRAYED ENDS. REPLACED L1 DOOR ROPE. 2 L 7 2 4F RT A1NM 1996053000220 19960530 00220 WP 1996 5 30 UPS96820208 1 19960524 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 660 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE-C, MID ACCESSORY COMPARTMENT FUSELAGE FRAME AT STATION 660 CORRODED BETWEEN L35L TO L35R ESPECIALLY INSI DE FRAME. REMOVED FRAME CLIP AT STA 660 BETWEEN L35L TO L35R LOWER SECTION, FAB'D NEW CLIP, ALODINED AND PRIMED IAW SRM 53-4-0 AND 51-1-8. INSTALLED NEW FRAME IAW SRM 51-1-21, 51-1-20 AND 51-3-0. 2 L 7 4 4F RT 4A25 1996053000221 19960530 00221 WP 1996 5 30 UPS96820217 1 19960508 A 5711 SUPPORT FTG DOUG DC8 DC873F 302199F WP NR 2/3 PYLON DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE-C, WING FRONT SPAR AT PYLON SUPPORT FITTING NR 2 AND NR 3 REQUIRES REPLACEMENT. MODIFIED NR 2 AND NR 3 FOOT STOOL SKATE ANGLE IAW EO DC-8-5710-4080E AND TIMCO REO-01940. 2 L 7 4 4F RT 4A25 1996053000222 19960530 00222 WP 1996 5 30 UPS96820218 1 19960507 A 5320 HOOK FRAME DOUG DC8 DC873F 302199F WP AFT CROSS DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE-C, AFT CROSS SLIDE DOOR LEFT HAND ACCESS NR 2 HOOK FRAME CORRODED AND CRACKED. FABRICATED REPAIR ANGLE AND SHIM IAW REO-01947, INSTALLED REPAIR AND SHIM IAW REO-01947 AND DC8 SRM 51-1-11, 51-1-20A, 51-1-21 AND INSTALLED CRO SS SLIDE IAW DC8 MM 52-31-01. 2 L 7 4 4F RT 4A25 1996053000223 19960530 00223 WP 1996 5 30 UPS96820219 1 19960506 A 5320 ANGLES DOUG DC8 DC873F 302199F WP NR 4 ALT TANK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE-C, NR 4 ALT TANK BOOST PUMP SUPPORT ATTACH ANGLES CRACKED. REMOVED AND REPLACED STRONGER END FITTING AN D FORWARD AND AFT BOOST PUMP BRACKETS IAW DC8 SRM 51-1-8, 51-3-2, 51-1-20D AND 51-1-23. 2 L 7 4 4F RT 4A25 1996053000224 19960530 00224 WP 1996 5 30 UPS96820220 1 19960504 A 5330 SKIN DOUG DC8 DC873F 302199F WP SERV DOOR AREA CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE-C, EXT FUSELAGE SKIN CRACKED AT RADIUS OF PREVIOUS REPAIR JUST AFT OF RT FWD SERVICE DOOR. INSTALLED RE PAIR PER DC8 SRM 53-2-1 AND REO-01941, INSTALLED FASTENER PER DC8 SRM 51-1-20D, SEALED PER SRM 51-1-15 AND 51-1-17, TREA TED AND PRIMED PER SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996053000225 19960530 00225 WP 1996 5 30 UPS96820221 1 19960511 A 5711 SPAR CAP DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE-C, CRACKS IN NR 5, NR 10 AND NR 11 HOLES IN SPAR CAP ON LEFT WING. REPAIRED CRACKS NR 5, NR 10, NR 11 H OLES IN SPAR CAP BY FABRICATING REPAIR DOUBLERS IAW SRM 51-3-2 AND EO DC8-5710-7761A. 2 L 7 4 4F RT 4A25 1996053000226 19960530 00226 WP 1996 5 30 UPS96820222 1 19960507 A 5230 DOOR LATCH DOUG DC8 DC873F 302199F WP CARGO DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE-C, AFT CROSS DOOR NR 6 T-LATCH BACK UP CORRODED. REMOVED FITTINGS IAW SRM 51-1-20D AND 51-1-21, DRILLED UP REPAIR FITTING IAW SRM 53-2-0 AND 51-1-20D, INSTALLED REPAIRED FITTING IAW SRM 51-1-20DD AND 53-2-0 PGS 15/16. 2 L 7 4 4F RT 4A25 1996053000227 19960530 00227 WP 1996 5 30 UPS96820223 1 19960508 A 5720 FITTING DOUG DC8 DC873F 302199F WP WS 435 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE-C, STR NR 58 FITTING CRACKED AT O/B END APPROX XRS 435, ACCESS PANEL 505B, RT WING NR 4 ALT TANK. REMOV ED AND REPLACED STRINGER END FITTING IAW SRM 51-1-8, 51-3-2 AND 51-1-23. 2 L 7 4 4F RT 4A25 1996053000228 19960530 00228 NM 1996 5 30 VNAA9600038 1 19960528 A 5610 001A5610000207 DV WINDOW DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT COCKPIT DELAMINATED A A VNAA K NONE O OTHER IN INSP/MAINT 1 GL 07 429JS 972 3043 DURING PREFLIGHT PRIOR TO BOARDING PASSENGERS, FLIGHT CREW NOTICED THE F/O'S DIRECT VISION WINDOW WAS DELAMINATED. INSP ECTED THE WINDOW AND FOUND THAT THE WINDOW DELAMINATION WAS BEYOND SERVICABLE LIMITS. REPLACED THE F/O'S DIRECT VISION WINDOW IAW MM 56-12-00. AIRCRAFT WAS THEN RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996053000229 19960530 00229 NE 1996 5 30 VNAA9600039 2 19960528 A 7320 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENG EEC LOOSE A A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 07 328JS 3030 LEFT ENGINE TORQUE INDICATOR SURGED AND PROPELLER RPM INDICATOR FLUCUATED DURING TAKEOFF. CREW CONTINUED ON WITH THE TA KEOFF. THE FLUCUATION AND SURGE PROBLEMS CONTINUED AFTER T/O. THE CREW ELECTED TO RETURN TO THE FIELD. AIRCRAFT LANDE D WITHOUT FURTHER INCIDENT. INSPECTED THE LT ENGINE AND NOTICED THAT THE MAIN CANNON CONNECTOR TO THE ELECTRONIC ENGINE CONTROL WAS LOOSE, TIGHTENED THE CONNECTOR AND GROUND CHECKED GOOD. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996053000230 19960530 00230 NM 1996 5 30 VNAA9600040 1 19960528 A 3150 T/O WARNING DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT ACTIVATED A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 07 422JS 3018 CREW RECEIVED A TAKEOFF, CONFIGURATION WARNING ASSOCIATED WITH AN AMBER CAS MESSAGE DURING THE TAKEOFF ROLL. CREW ABORT ED THE TAKEOFF AND RETURNED TO THE TAXIWAY. CREW THEN CLEARED ALL CAS MESSAGES, CONDUCTED A POWER ASSURANCE RUN, EVERYT HING CHECKED GOOD. AIRCRAFT CONTINUED ON WITH THE FLIGHT. SUSPECT ELEVATOR TRIM MAY HAVE BEEN OUT OF CONFIGURATION FO R TAKEOFF, THIS CAUSING THE WARNING. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996053000281 19960530 00281 NE 1996 5 30 96ZZZX2748 2 19960403 A 7261 SWITCH BOEING 767 767383 1385214 NM PWA 4060 PW4060 52119 NE NR 1 ENG FILTER MALFUNCTION A ANCF E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 23 984AN 24357 724505 AFTER 7:15 HOURS FLY-TIME FROM GOB TO CDG, EICAS MESSAGE FOR LEFT ENGINE OIL FILTER CAME ON. MESSAGE REMAINED WHEN THRU ST REDUCED. ENGINE SHUT DOWN. UNSCHEDULED LANDING MADE. INSPECTED LT ENGINE OIL CHIP DETECTOR AND OIL TANK AND GEARBO X FOUND NORMAL. REMOVED OIL FILTER AND CLEANED. PERFORMED ENGINE RUN-UP. CHECKED FOR OIL LEAKS, NO LEAKS FOUND. CHAN GED DIFFERENTIAL PRESSURE SWITCH. SUSPECT CAUSE WAS FAULTY DIFFERENTIAL PRESSURE SWITCH. 2 L 7 2 4F 4 F RT A1NM E24NE 1996053000302 19960530 00302 EA 1996 5 30 96ZZZX2768 2 19960501 A 7414 10682016 GEAR ASSY BENDIX D6LN3000 PIPER PA32 PA32R300 7103213 SO LYC O540 IO540K1G5 41532 EA LT MAG TEETH FAILED G A A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 CE 05 38945 4020154 32R7780490 LT MAG FAILED DURING CLIMB-OUT. RETURNED TO AIRPORT. DURING ROLL-OUT, RT MAG FAILED. INVESTIGATION REVEALED BOTH DIST RIBUTOR GEARS HAD BROKEN TEETH. MAG HAD BEEN OVERHAULED APPROXIMATELY 400 HOURS PRIOR, BUT GEARS DID NOT APPEAR TO BE N EW DUE TO DISCOLORATION OF PLASTIC. TOTAL TIME ON GEARS UNKNOWN. OUTSIDE AIR TEMP WAS MINUS 9 DEGREES BELOW ZERO. ENG INE HAD BEEN PREHEATED AND GROUND RUN PRIOR TO FLIGHT. 1 L 7 1 3O 3 O A3SO 1E4 1996053000308 19960530 00308 WP 1996 5 30 9611449152 1 19960527 A 2130 94840213 AMPLIFIER DOUG DC9 DC914 3022034 WP E/E COMPARTMENT MALFUNCTIONED A NWAA A B G UNSCHED LANDING EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CL CLIMB 1 GL 01 8911E 38118 34770 45825 DURING CLIMBOUT, CABIN PRESSURE WARNING LIGHT ILLUMINATED WITH CABIN DECOMPRESSION. MASKS DEPLOYED, CABIN CONTROLLED MA NUALLY AND ACFT RETURNED TO DSM AND LANDED WITHOUT INCIDENT. FOUND CIRCUIT BREAKER Z-31 POPPED. REPLACED THE PRESSURE AMPLIFIER AND RESET THE CIRCUIT BREAKER. CLEANED AND STOWED ALL MASKS, SYSTEM OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996053000309 19960530 00309 WP 1996 5 30 9611459302 1 19960527 A 3150 NOT TURNING WARN DOUG DC9 DC982 3022082 WP LANDING GEAR ILLUMINATED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 302RC 48055 WHEEL NOT TURNING, LIGHT ILLUMINATED AT 80 KNOTS. ABORTED TAKEOFF AND AIRCRAFT WAS TOWED TO THE GATE. ALL WHEELS TURNE D NORMALLY, INSPECTED TIRES, ALL WERE NORMAL. PLACED ON MEL 32-12. 2 L 7 2 4F A6WE 1996053000310 19960530 00310 1996 5 30 9611469941 4 19960525 A 3442 20671570153 RADAR TR UNIT DOUG DC9 DC932 3022066 WP FWD FUSELAGE FAILED A A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 3324L 12707 294 47103 WEATHER RADAR SYSTEM FAILED AFTER TAKEOFF. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RA DAR TRANSCEIVER, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996053000311 19960530 00311 WP 1996 5 30 9611479903 1 19960524 A 2820 VENT VALVE DOUG DC9 DC931 3022065 WP LEFT FUEL TANK STUCK OPEN A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 953N 47083 FUEL BEGAN VENTING FROM RIGHT WING AFTER TAKEOFF. FLIGHT DIVERTED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE TRAN SFERRED FUEL INTO CENTER TANK AND RAN ALL SIX PUMPS WITH CROSSFEED VALVE OPEN. NO TRANSFERRING OF FUEL WAS NOTED. FOUN D DEBRIS IN LEFT TANK FLOAT VENT VALVE. REPLACED VALVE, LEAK AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996053000312 19960530 00312 NE 1996 5 30 9611489876 2 19960526 A 7220 NOSE DOME DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE NR 2 ENGINE MISSING A A NWAA A UNSCHED LANDING D INFLIGHT SEPARATION CR CRUISE 1 GL 01 785NC 48110 688796 DURING CRUISE FLIGHT, NR 2 ENGINE BEGAN TO EXPERIENCED COMPRESSOR STALLS. THRUST REDUCED AND STALL CEASED. OPERATED NR 2 ENGINE AT IDLE THE REMAINDER OF THE FLIGHT. AIRCRAFT DIVERTED TO DSM AND LANDED WITHOUT FURTHER INCIDENT. GROUND MA INTENANCE INSPECTED THE ENGINE AND FOUND NR 2 ENGINE INTAKE NOSE DOME MISSING. NEW NOSE DOME WAS INSTALLED. BORESCOPE INSPECTED ENGINE, NO DAMAGE FOUND. AIRCRAFT WAS GROUND RUN AND RETURNED TO SERVICE. 2 L 7 2 4F 4 F A6WE E2EA 1996053000313 19960530 00313 WP 1996 5 30 9611499958 1 19960526 A 5250 SEAL DOUG DC9 DC931 3022065 WP TAIL CONE CONTAMINATED A NWAA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 01 917RW 47145 DURING FLIGHT, A LOUD AIR LEAK FROM THE AFT CABIN PLUG DOOR, AIRCRAFT PRESSURIZATION WAS NORMAL. RETURNED TO DTW WITHOU T FURTHER INCIDENT. REMOVED INSULATION FROM THE PLUG HATCH SEAL. 2 L 7 2 4F A6WE 1996053000314 19960530 00314 EU 1996 5 30 9611503247 1 19960527 A 3350 BATTERY PACK AIRBUS 320 A320211 3930320 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 347NW 408 DURING LINE MAINTENANCE WHILE PERFORMING THE EMERGENCY LIGHTS SYSTEM TEST, THE FORWARD LEFT BATTERY FAULTED. REPLACED B ATTERY PACK, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996053000315 19960530 00315 WP 1996 5 30 9611519862 1 19960524 A 5330 SKIN DOUG DC9 DC951 3022051 WP FS 965 DISBONDED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 771NC 47769 DURING FLIGHT, AN AIR LEAK WAS HEARD IN THE AFT CABIN. LANDED IN DTW WITHOUT FURTHER INCIDENT. FOUND APPROXIMATELY 18 TO 20 FASTENERS LOOSE ALONG THE FS 965 SKIN LAP SEAM FROM LONGERON 10L TO 10R. REPLACED LOOSE FASTENERS. PRESSURE CHEC K REVEALED AN ADDITIONAL AIR LEAK FOUND FROM THE MAIN LANDING GEAR DOWNLOCK INSPECTION COVER. CLEANED AND LUBRICATED CO VER SEAL, PRESSURIZATION CHECK OK. 2 L 7 2 4F A6WE 1996053000316 19960530 00316 NM 1996 5 30 96FDEA00973 1 19960513 A 5230 WEB BOEING 727 727225 1384077 NM NR 2 CARGO DOOR CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 468FE 21452 NR0335 AND 006, ON NR 2 CARGO DOOR AFT SUPPORT WEB FRAME, CORROSION EXITS I/B OF FRAME WEB C17 LOWER L-BRACKET, C/T LOWE R DOOR GUIDE ROLLER. CORROSION ON NR 2 CARGO DOOR I/B OF FRAME WEB FOUND TO BE OUT OF LIMITS. REPAIRED PER SRM 51-40-3 FIG 1 ON AFT SUPPORT WEB FRAME. 2 L 7 3 4F A3WE 1996053000317 19960530 00317 NM 1996 5 30 96FDEA01021 1 19960522 A 5311 FRAME BOEING 727 727227 1384078 NM BS 1110 CORRISION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 NR 0317 (018C), CORROSION (C53-224-01) ON FWD SIDE OF BS 1110 FRAME AT STR 4 LT. REPAIRED FRAME FWD SIDE OF BS 1110 FRA ME AT STR 4 LT IAW FEDEX SRM 51-40-3. 2 L 7 3 4F A3WE 1996053000318 19960530 00318 NM 1996 5 30 96FDEA01023 1 19960522 A 5313 6556119 STRINGER BOEING 727 727227 1384078 NM BS 950 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 NR 0314, 032 CORROSION (C53-224-01, -3) AND TOOLING MARKS BS 950A, STR 7 RT AFT SIDE OF FRAME. *S/D* REMOVED AND REPLA CED STRINGER 7 RT FROM BS 950 TO 950B PLUS 10 IAW SRM 53-10-1 SRM 53-10-3 FIG 3. 2 L 7 3 4F A3WE 1996053000319 19960530 00319 NM 1996 5 30 96FDEA01024 1 19960522 A 5315 FLOOR BEAM BOEING 727 727227 1384078 NM BS 1130 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 NR 0391 (034), CORROSION (C53-111-01, -3) ON LOWER CHORD OF FLOOR BEAM AT NUTPLATE HOLES BS 1130 LBL 54 TO RT 54 LT 200. 2 L 7 3 4F A3WE 1996053000320 19960530 00320 NM 1996 5 30 96FDEA01025 1 19960524 A 2612 FIRE CONNECTOR BOEING 727 7272S2F 1384O81 NM NR 1 ENGINE LOOSE A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 212FE 22934 NR 1 ENG FIRE LIGHT INTERMITTENT IND DURING CLIMBOUT. FIRE TEST CHECKED GOOD, NO SECONDARY INDICATIONS. INSPECTED FIRE LOOP AND FOUND LOOSE CONNECTOR, RESEATED SAME AND CHECKED AS PER MM 26-11-01, NO FAULTS NOTED. RAN NR 1 ENG PER JET HA NDBOOK, NO FAULTS NOTED OK FOR SERVICE. 2 L 7 3 4F A3WE 1996053000321 19960530 00321 NM 1996 5 30 96FDEA01026 1 19960524 A 2120 AIR DISTR BOEING 727 727227 1384078 NM CABIN ODOR A FDEA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 25 487FE 21490 AFTER LEVEL OFF AT FLT LEVEL 310, SMELLED A FAINT SCENT OF HOT ELECTRICAL INSULATION. TURNED OFF THE GASPER FAN AND THE SMELL WENT AWAY, THOUGHT WE HAD ANOTHER WHIFF ABOUT 30 MINUTES LATER. SMELL WAS VERY FAINT AND MOMENTARY SLIGHTLY STRO NGER BEHIND S/O PANEL, 30 MINUTES LATER WE SMELLED IT AGAIN, NO HAZARDOUS MATERIAL ON A/C. INSPECTED GASPER FAN MOTOR, E/E COMPT, BEHIND SECOND OFFICER'S PANEL. RAN GASPER FAN AND PACKS 2 HOURS, NO SMELL NOTES. REMOVED AND REPLACED LEFT AND RIGHT WATER SEPARATOR FILTERS, OPERATIONAL CHECKS GOOD. 2 L 7 3 4F A3WE 1996053000322 19960530 00322 NM 1996 5 30 96FDEA01028 1 19960524 A 5312 BULKHEAD WEB BOEING 727 727227 1384078 NM BS 1183 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 MECHANICAL DAMAGE TO THE AFT SIDE OF THE 1183 BULKHEAD WEB AT LBL 36 WL 261. REPAIRED AFT SIDE OF THE 118.3 BULKHEAD WE B AT LBL 36 WL 261 IAW FEDEX SRM 53-10-09 FIG 4. 2 L 7 3 4F A3WE 1996053000323 19960530 00323 NM 1996 5 30 96FDEA01029 1 19960524 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 720 GOUGES A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 GOUGES IN STR 7L BS 720B PLUS 15. GOUGES IN STR 7L OUT OF LIMITS, FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 5 3-10-3. 2 L 7 3 4F A3WE 1996053000324 19960530 00324 NM 1996 5 30 96FDEA01030 1 19960524 A 5320 65453132 STRINGER CLIP BOEING 727 727227 1384078 NM BS 680 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 CRACKED STR CLIP AT BS 680 STR 3L. REMOVED STR CLIP AT BS 680 STR 3L AND INSTALLED NEW STR CLIP PER FEDEX SRM 51-10-1. 2 L 7 3 4F A3WE 1996053000325 19960530 00325 NM 1996 5 30 96FDEA01031 1 19960524 A 5320 65453132 STRINGER CLIP BOEING 727 727227 1384078 NM BS 660 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 CRACKED STR CLIPS AT BS 660 STR 3 AND 4L. REMOVED STR CLIPS AT BS 660 STR 3 AND 4L AND INSTALLED NEW STR CLIPS PER FEDE X SRM 51-10-1. 2 L 7 3 4F A3WE 1996053000326 19960530 00326 NM 1996 5 30 96FDEA01032 1 19960525 A 2612 FIRE WARNING BOEING 727 7272S2F 1384O81 NM NR 1 ENGINE ACTIVATED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 212FE 22934 NR 1 ENG FIRE IND INTERMITTENT BELL AND LIGHT ON CLIMBOUT. RETARDING THROTTLE HAD NO EFFECT ON THE INDICATIONS. 2 L 7 3 4F A3WE 1996053000327 19960530 00327 NM 1996 5 30 96FDEA01033 1 19960528 A 5320 65579969 SHEAR WEB BOEING 727 727227 1384078 NM BS 720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 WHILE WORKING NR0475 FOUND CORROSION ON WEB BS 720D TO 720E WL 20 RBL 68 TO 75. REMOVED CORRODED WEB FROM BS 720D TO 72 0E WL 208 RBL 68 TO 75. FABRICATED NEW WEB AND INSTALLED. FABRICATED IAW FEDEX SRM 53-10-2. 2 L 7 3 4F A3WE 1996053000328 19960530 00328 NM 1996 5 30 96FDEA01034 1 19960528 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 700-720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 CORROSION (C53-224-01, -1) ON STR NR 4R BS 720 A TO 700. MECHANICALLY REMOVED CORROSION ON STR NR 4R BS 720 A TO 700 FO UND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. REPLACED STR 720 PLUS 10 TO BS 720 A PLUS 10 PER FEDEX SRM 53-10-3. 2 L 7 3 4F A3WE 1996053000329 19960530 00329 WP 1996 5 30 ABXA9600497 1 19960524 A 2913 NAS161210 O-RING SEAL DOUG DC8 DC861 3021952 WP NR 3 HYD PUMP DEFECTIVE A ABXA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 23 845AX 46157 DURING APPROACH, HYDRAULIC FLUID QUANTITY DROPPED TO THE STANDPIPE LEVEL AND THE HYDRAULIC PRESSURE DECREASED AFTER THE LANDING GEAR WAS EXTENDED. REPLACED DEFECTIVE O-RING SEAL ON THE NR 3 ENGINE DRIVEN HYDRAULIC PUMP PRESSURE FITTING. O PERATED HYDRAULIC SYSTEM AND NO LEAKS WERE NOTED. 2 L 7 4 4F 4A25 1996053000330 19960530 00330 NM 1996 5 30 CALA9600644 1 19960524 A 3260 CARD BOEING 737 7373T0 1384582 NM LG LOGIC SHELF INOPERATIVE A CALA O OTHER J WARNING INDICATION TO TAKEOFF 1 SW 09 17316 23367 THE LT MLG RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION DEPARTING SLC. THE GEAR WAS RECYCLED, BUT THE LI GHT DID NOT EXTINGUISH UNTIL SEVERAL MINUTES LATER. THE FLIGHT WAS CONTINUED WITHOUT FURTHER PROBLEM. MAINTENANCE COUL D NOT DUPLICATE THE PROBLEM. THE M986 LOGIC CARD WAS REPLACED AS A PRECAUTIONARY MEASURE. A-SYSTEM CHECK WAS PERFORMED PER MM 32-09-20, PAGE 411 AND 412 AND OPERATION CHECKED GOOD. 2 L 7 2 4F RT A16WE 1996053000331 19960530 00331 NM 1996 5 30 CALA9600645 1 19960524 A 2530 416100129 COFFEEMAKER BOEING 737 737524 1384721 NM FWD GALLEY FAILED A CALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 09 17620 27333 THE NR 2 COFFEEMAKER IN FORWARD GALLEY BEGAN TO SMOKE DURING PUSHBACK FROM GATE. THE AIRCRAFT WAS RETURNED TO THE GATE. MAINTENANCE FOUND THE NR 2 COFFEEMAKER PRINTED CIRCUIT CARD BURNED. THE COFFEEMAKER WAS REMOVED AND REPLACED, OPERATI ON CHECKED GOOD. 2 L 7 2 4F RT A16WE 1996053000332 19960530 00332 WP 1996 5 30 CALA9600646 1 19960524 A 3610 9194M14G02 Y-DUCT DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 3 ENGINE RUPTURED A CALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 09 68065 46590 THE NR 3 ENGINE FIRE WARNING ACTIVATED MOMENTARILY WHILE EN ROUTE. THE FIRE WARNING SYSTEM OF ALL ENGINES WAS TESTED AN D ALL SYSTEMS CHECKED GOOD. THE FLIGHT WAS CONTINUED TO LGW WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 3 ENGINE 8TH STAGE BLEED Y-DUCT FAILED WITH RESULTANT DAMAGE TO THE 10TH STAGE BLEED AND B-A VENT COOLING DUCTS. THE D UCTS WERE REPLACED AND LEAK CHECKS DURING ENGINE RUN WERE GOOD. 2 L 7 3 4F 4 F A22WE E23EA 1996053000333 19960530 00333 WP 1996 5 30 CALA9600647 1 19960525 A 3233 ACTUATOR DOUG DC9 DC982 3022082 WP NLG INOPERATIVE A CALA K NONE J WARNING INDICATION TO TAKEOFF 1 SW 09 33805 49249 THE NOSE GEAR WAS SLOW TO RETRACT AFTER TAKEOFF. THE RED LIGHT EXTINGUISHED AND DOORS CLOSED AFTER APPROXIMATELY 20 TO 25 SECONDS. THE FLIGHT WAS CONTINUED AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR RETRACT CYLINDER AT FAULT. THE NOSE GEAR RETRACT CYLINDER WAS REMOVED AND REPLACED IAW MM 32-32-06. OPERATIONAL AND LE AK CHECKS WERE GOOD, THE NOSE GEAR RETRACTED IN FOUR SECONDS. 2 L 7 2 4F A6WE 1996053000334 19960530 00334 WP 1996 5 30 CALA9600648 1 19960527 A 2750 S4913809CW11202 CONTROL CABLE DOUG DC10 DC1030 3023501 WP RT TE FLAP BROKEN A A CALA O OTHER J F WARNING INDICATION FLT CONT AFFECTED TO TAKEOFF 1 SW 09 68065 46590 CREW HAD A FLAP ASYMMETRY FLAG AFTER TAKEOFF. TAPES SHOWED FLAP TRAVELING SYMMETRICALLY, RIGHT FLAP WAS LEADING LEFT AP PROXIMATELY 5 DEGREES. THE FLIGHT CONTINUED TO EWR WHERE IT LANDED WITH FLAPS OPERATING NORMALLY. MAINTENANCE CYCLED F LAPS SEVERAL TIMES AND VERIFIED RT INBOARD FLAP LOCKED IN UP POSITION. THE FLAP FOLLOW-UP CABLE ON RT INBOARD FLAP WAS FOUND BROKEN. THE CABLE WAS REPLACED AND ADJUSTED IAW MM 27-50-00, PAGE 503, ITEM 3, OPERATION CHECKED GOOD. IN ADDITI ON, THE RT I/B FLAP INBOARD ACTUATOR WAS REPLACED DUE TO BINDING. 2 L 7 3 4F A22WE 1996053000335 19960530 00335 NM 1996 5 30 CALA9600649 1 19960528 A 3260 SENSOR BOEING 737 737291 138448W NM LEVER LK SYS OUT OF ADJUST A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 10251 20361 THE LANDING GEAR HANDLE WOULD NOT MOVE PAST THE OFF POSITION AFTER TAKEOFF. THE LANDING GEAR REMAINED DOWN WITH THREE G REEN LIGHTS AT ALL TIMES. THE AIRCRAFT WAS RETURNED TO DFW WHERE IT LANDED WITHOUT INCIDENT. TROUBLESHOOTING THE LEVER LOCK SYSTEM IAW MM 32-31-21 FOUND THE AIR SAFETY SENSOR OUT OF ADJUSTMENT. THE AIR SAFETY SENSOR WAS ADJUSTED AND TEST ED IAW MM 32-09-200, PAGE 501 AND OPERATION CHECKED GOOD. 2 L 7 2 4F A16WE 1996053000336 19960530 00336 NE 1996 5 30 96ZZZM874 2 19960320 A 7260 6004T40G12 GEARBOX AMD FALC20 FALCON 2720302 EU GE CF700 CF7002D2 30010 NE LT ENGINE STRIPPED FITTING A FUBA K NONE K FLUID LOSS IN INSP/MAINT 1 NE 03 20AE 13376 258 299G003 WHILE PERFORMING A PREFLIGHT INSPECTION, OIL WAS NOTICED TO BE EXCESSIVELY LEAKING AT OIL SCAVENGE LINE FITTING ATTACHIN G SCAVENGER LINE TO ACCESSORY GEARBOX. FITTING WAS FOUND TO BE LOOSE. UPON FURTHER INVESTIGATION FITTING WAS FOUND TO BE STRIPPED. ACCESSORY GEARBOX WAS REMOVED FROM ENGINE FOR REPAIR. 2 L 7 2 4F 4 F A7EU E7EA 1996053000337 19960530 00337 SW 1996 5 30 96ZZZM875 1 19960413 A 5753 2736003001 RIB SWRNGN SA227 SA227AC 8780603 SW LT TE FLAP CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 60NE AC760B DURING AN INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE LEFT FLAP INBOARD AFT END RIB CHAFED APPROXIMATELY .200 INC H BY .500 INCH, OUTBOARD NOSE END RIB CRACKED IN RELIEF RADIUS AND OUTBOARD HINGE ARM BENT. COMPLETED REPAIR 'PART FOR PART' REPLACEMENT WITH A NEW LEFT INBOARD AFT END RIB P/N 27-36003-001, NEW OUTBOARD NOSE END RIB P/N 27-36015-009 AND N EW OUTBOARD HINGE ARM P/N 27-36044-005. ALL WORK DONE IAW FAIRCHILD SRM 51-00-00, PG 4, REV JUNE 1/93, AND 57-90-60 PGS 43-46. FAIRCHILD SRM CHANGERS REF 51-30-04, REV JUNE 1/93 AND 51-40-00 REV JUNE 1/93. REFERENCE MALA964961. 2 L 7 2 4T RT A8SW 1996053000338 19960530 00338 SW 1996 5 30 96ZZZM876 1 19960413 A 5753 2736044005 HINGE ARM SWRNGN SA227 SA227AC 8780603 SW LT TE FLAP BENT A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 60NE AC760B DURING AN INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE LEFT FLAP INBOARD AFT END RIB CHAFED APPROXIMATELY .200 INC H BY .500 INCH, OUTBOARD NOSE END RIB CRACKED IN RELIEF RADIUS AND OUTBOARD HINGE ARM BENT. COMPLETED REPAIR 'PART FOR PART' REPLACEMENT WITH A NEW LEFT INBOARD AFT END RIB P/N 27-36003-001, NEW OUTBOARD NOSE END RIB P/N 27-36015-009 AND N EW OUTBOARD HINGE ARM P/N 27-36044-005. ALL WORK DONE IAW FAIRCHILD SRM 51-00-00, PG 4, REV JUNE 1/93, AND 57-90-60 PGS 43-46. FAIRCHILD SRM CHANGERS REF 51-30-04, REV JUNE 1/93 AND 51-40-00 REV JUNE 1/93. REFERENCE MALA964961. 2 L 7 2 4T RT A8SW 1996053000339 19960530 00339 NM 1996 5 30 96ZZZM877 1 19960314 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 560 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 17789 20643 FORWARD CARGO STATION 560 LEFT STRINGER 18 LEVEL 2 CORROSION ON STRINGER. REMOVED CORROSION PER SRM 51-10-6 MATERIAL LO SS OUT OF LIMITS PER SRM 53-10-1. REMOVED DAMAGED STRINGER SECTION, FABRICATED 1 REPAIR STATION AND 4 FILLERS PER SRM 5 3-10-3, FIGURE 1, INSTALLED PER SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1996053000341 19960530 00341 EU 1996 5 30 96ZZZM879 1 19960501 A 7712 COMP RESISTOR BAG JETSTM JETSTM3201 1500217 EU LT/RT ENG OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 485UE 901 FLT 6546 - IAD-ROA - ABORTED THE TAKEOFF DUE TO BOTH ENGINES BEING TEMPERATURE LIMITED DURING THE TAKEOFF ROLL. AIRCRAF T RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE COMPLETED THE FOLLOWING ADJUSTMENTS/REPLACEMENTS, LEFT ADJUST ED THE COMPENSATING RESISTOR, REPLACED THE TORQUE SIGNAL CONDITIONER AND REPLACED THE FLOW CONTROL VALVE. RIGHT ADJUSTE D THE COMPENSATING RESISTOR. PERFORMED ENGINE RUNS, ALL CHECKS GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. REFERENCE VTZA96176. 2 L 7 2 4T RT A56EU 1996053000342 19960530 00342 WP 1996 5 30 96ZZZM880 2 19960501 A 7320 FLOW CONTL VLV BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT/RT ENG FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 485UE 901 FLT 6546 - IAD-ROA - ABORTED THE TAKEOFF DUE TO BOTH ENGINES BEING TEMPERATURE LIMITED DURING THE TAKEOFF ROLL. AIRCRAF T RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE COMPLETED THE FOLLOWING ADJUSTMENTS/REPLACEMENTS, LEFT ADJUST ED THE COMPENSATING RESISTOR, REPLACED THE TORQUE SIGNAL CONDITIONER AND REPLACED THE FLOW CONTROL VALVE. RIGHT ADJUSTE D THE COMPENSATING RESISTOR. PERFORMED ENGINE RUNS, ALL CHECKS GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. REFERENCE VTZA96176. 2 L 7 2 4T 4 T RT A56EU E4WE 1996053000343 19960530 00343 NM 1996 5 30 96ZZZM881 1 19960407 A 5540 85530025003 LOWER ARM ASSY DHAV DHC8 DHC8102 2809003 NM RUDDER WORN A A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 801MX 20383 008 DURING A SCHEDULED RUDDER CHANGE, THE VERTICAL STABILIZER UPPER AND LOWER CENTER HINGE FITTING RUDDER ATTACH POINTS WERE FOUND WORN. THE BUSHINGS WOULD NOT INSTALL CORRECTLY DUE TO THE HOLES BEING OVERSIZED. REMOVED AND REPLACED UPPER AND LOWER CENTER HINGE FITTINGS IAW DEHAVILLAND DRAWINGS. INSTALLED RUDDER ASSEMBLY IAW DEHAVILLAND MM. AIRCRAFT RETURNED TO SERVICE. REFERENCE PCAA9600280. 2 H 7 2 4T RT A13NM 1996053000344 19960530 00344 NM 1996 5 30 96ZZZM882 1 19960506 A 5610 001A561A0000204 WINDSHIELD DORNER DO32 DO328100 2996000 NM LT COCKPIT SHATTERED A A EQGA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 19 340LS 1328 167 3040 WHILE EN ROUTE AT CRUISE ALTITUDE, THE FLIGHT CREW HEARD A POPPING SOUND AND THE LEFT WINDSHIELD OUTER PANE SHATTERED. T HE AIRCRAFT CONTINUED INTO DFW WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS FERRIED TO HOT WHERE THE WINDSHIELD WAS REPLA CED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A45NM 1996053000345 19960530 00345 NM 1996 5 30 96ZZZM883 1 19960506 A 3610 16J081 HP6 DUCT BOEING 757 757225 1384959 NM LT ENGINE LEAKING A USAA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 EA 19 606AU 22202 SFO - FLT 56 - AFTER TAKEOFF FROM SFO, CREW RECEIVED OVETEMP LIGHT ON LEFT ENGINE. LIGHT EXTINGUISHED WHEN THROTTLE RET ARDED. FLIGHT RETURNED TO SFO AND LANDED WITH NO FURTHER INCIDENTS. MX REPLACED THE HP2 AND P6 DUCTS DUE TO LEAKAGE. R EFERENCE USAABB96015. 2 L 7 2 4F RT A2NM 1996053000346 19960530 00346 NM 1996 5 30 AALA960384 1 19960308 A 3350 A3030398101 CONNECTOR DOUG MD11 MD11 3023602 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1761R 48551 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT BETWEEN PAX SEAT ROWS 2D THROUGH 13D INOPERATIVE. REPLACED BROKEN E MERGENCY FLOOR LIGHT CONNECTORS BY PAX SEAT ROWS 2D AND 13D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1996053000347 19960530 00347 NM 1996 5 30 AALA960405 1 19960315 A 3350 CONDUCTOR DOUG MD11 MD11 3023602 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1764B 48554 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY SEAT ROW 6H INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT FLAT CO NDUCTOR BY R2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1996053000348 19960530 00348 NM 1996 5 30 AALA960406 1 19960316 A 3350 LIGHT STRIP DOUG MD11 MD11 3023602 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1755 48490 JFK - DURING OVERNIHT CHECK, EMERGENCY FLOOR LIGHTS AFT OF L2 DOOR INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP AF T OF L2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1996053000349 19960530 00349 EU 1996 5 30 AALA960495 1 19960330 A 3350 A3060698101 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 14077 612 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 20HJ AND 23HJ INOPERATIVE. REPLACED BROKEN E MERGENCY FLOOR LIGHT STRIP CONNECTOR BY PAX SEAT ROW 20HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996053000350 19960530 00350 EU 1996 5 30 AALA960603 1 19960417 A 3397 WIRE AIRBUS 300 A300B4605R 3930308 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7082A 643 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 21B THROUGH 24B INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT WIRE STRIP FROM SIDEWALL CONNECTOR TO LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996053000351 19960530 00351 EU 1996 5 30 AALA960607 1 19960418 A 3350 LIGHT STRIP AIRBUS 300 A300B4605R 3930308 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 90070 513 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT STRIP BY 4L DOOR INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BY 4L DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996053000352 19960530 00352 EU 1996 5 30 AALA960616 1 19960421 A 3350 LIGHT STRIP AIRBUS 300 A300B4605R 3930308 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 19059 469 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PAX SEAT ROW 1H INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STR IP BY PAX SEAT ROW 1H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996053000353 19960530 00353 NM 1996 5 30 AALA960617 1 19960418 A 5210 146N6201 DOOR PAN BOEING 757 757223 1384957 NM L-4 DOOR GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 660AM 25294 AFW - FOUND L-4 DOOR HANDLE PAN HAD GOUGE BLENDED BEYOND SRM LIMITS. PER MRB 757-818. (M) 2 L 7 2 4F RT A2NM 1996053000354 19960530 00354 NM 1996 5 30 AALA960621 1 19960415 A 3213 160N02019 BUSHING BOEING 757 757223 1384957 NM NLG ROTATED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 615AM 24491 AFW - NOSE GEAR SHOCK STRUT BUSHINGS AT DRAG STRUT ATTACH POINT HAS CRACKED SEALANT, POSSIBLE BUSHING ROTATION, REQUEST TO CLEAN SEALANT CHECK FOR CORROSION, RESEAL AND APPLY TORQUE STRIPE FOR FURTHER INSPECTION. PER MRB 757-790. (M) 2 L 7 2 4F RT A2NM 1996053000355 19960530 00355 NM 1996 5 30 AALA960622 1 19960415 A 3213 161N18171 BUSHINGS BOEING 757 757223 1384957 NM LT/RT MLG ROTATED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 615AM 24491 AFW - FOUND LEFT AND RIGHT MAIN GEAR INNER SHOCK STRUT BUSHINGS AT TRACK ATTACH POINT HAS CRACKED SEALANT, POSSIBLE BUSH ING ROTATION. REQUEST TO CLEAN SEALANT CHECK FOR CORROSION, RESEAL AND APPLY TORQUE STRIPE FOR FURTHER INSPECTION. PER MRB 757-789. (M) 2 L 7 2 4F RT A2NM 1996053000356 19960530 00356 NM 1996 5 30 AALA960634 1 19960422 A 5280 149N60011 SKIN BOEING 757 757223 1384957 NM LT MLG DOOR PUNCTURED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 617AM 24525 AFW - FOUND LEFT MAIN LANDING GEAR DOOR OUTER SURFACE HAS PUNCTURE IN CRITICAL AREA. PER MRB 757-828. (M) 2 L 7 2 4F RT A2NM 1996053000357 19960530 00357 NM 1996 5 30 AALA960635 1 19960416 A 5315 141N2932 FLOOR BEAM BOEING 757 757223 1384957 NM BS 324 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 648AA 24606 AFW - FLOOR BEAM AT STATION 324 RBL 42 AND RBL 62 HAS CORROSION REMOVED BEYOND SRM LIMITS. PER MRB 757-777. (M) 2 L 7 2 4F RT A2NM 1996053000358 19960530 00358 NM 1996 5 30 AALA960636 1 19960416 A 5315 146N5089 FLOOR BEAM BOEING 757 757223 1384957 NM BS 1640 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 648AA 24606 AFW - FOUND FLOOR BEAM AT STATION 1640 HAS CORROSION REMOVED AT VARIOUS LOCATIONS MATERIAL REMOVED IS BEYOND SRM LIMITS. MRB 757-778. (M) 2 L 7 2 4F RT A2NM 1996053000359 19960530 00359 NM 1996 5 30 AALA960637 1 19960416 A 5321 146NS300 DECK PLATE BOEING 757 757223 1384957 NM BS 1680 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 648AA 24606 AFW - DECK PLATE HAS CORROSION REMOVAL ON UPPER SURFACE MATERIAL REMAINING AT VARIOUS LOCATIONS ARE BEYOND SRM LIMITS. P ER MRB 757-779. (M) 2 L 7 2 4F RT A2NM 1996053000360 19960530 00360 NM 1996 5 30 AALA960638 1 19960416 A 5315 141N5111 FLOOR BEAM BOEING 757 757223 1384957 NM BS 345 MISDRILLED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 648AA 24606 AFW - FLOOR BEAM AT STATION 345 LBL HAS A MISDRILLED HOLE. PER MRB 757-788. (M) 2 L 7 2 4F RT A2NM 1996053000361 19960530 00361 NM 1996 5 30 AALA960639 1 19960416 A 5210 146N6201 PAN BOEING 757 757223 1384957 NM L-4 DOOR GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 648AA 24606 AFW - FOUND L-4 DOOR HANDLE PAN HAS A GOUGE BLENDED BEYOND SRM LIMITS. PER MRB 757-781. (M) 2 L 7 2 4F RT A2NM 1996053000362 19960530 00362 NM 1996 5 30 AALA960640 1 19960416 A 5210 146N6201 PAN BOEING 757 757223 1384957 NM R-4 DOOR GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 648AA 24606 AFW - FOUND R-4 DOOR HAS A SMALL GOUGE AFTER BLENDING. BLENDED AREA IS BEYOND SRM LIMITS. PER MRB 757-775. (M) 2 L 7 2 4F RT A2NM 1996053000363 19960530 00363 NM 1996 5 30 AALA960641 1 19960416 A 5310 146N8522 SURROUND STRUCT BOEING 757 757223 1384957 NM BS 1440 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 648AA 24606 AFW - FOUND AFT CARGO DOOR SURROUND STRUCTURE UPPER CHORD HAS CORROSION BLENDED OFF BEYOND SRM LIMITS. PER MRB 757-783. (M) 2 L 7 2 4F RT A2NM 1996053000364 19960530 00364 EU 1996 5 30 AALA960668 1 19960427 A 3350 LIGHT STRIP AIRBUS 300 A300B4605R 3930308 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 14056 463 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 21AB AND 23AB INOPERATIVE. REPLACED BROKEN E MERGENCY FLOOR LIGHT STRIP BETWEEN PAX SEAT ROWS 21AB AND 23AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996053000365 19960530 00365 EU 1996 5 30 AALA960674 1 19960429 A 3350 LIGHT STRIP AIRBUS 300 A300B4605R 3930308 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 33069 512 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY 4R DOOR INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BY 4R DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996053000366 19960530 00366 NM 1996 5 30 AALA960712 1 19960223 A 5314 144N8070 KEEL BEAM BOEING 757 757223 1384957 NM BS 1170 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 656AA 24614 AFW - FOUND KEEL BEAM HORIZONTAL WEB HAS CORROSION. PER MRB 757-747. (M) 2 L 7 2 4F RT A2NM 1996053000367 19960530 00367 NM 1996 5 30 AALA960713 1 19960502 A 3350 A3060698101 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 620AA 24578 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 6 THROUGH 17 INOPERATIVE. REINSTALLED LOOSE EMERGENCY FLOOR LIGHT STRIP CONNECTOR BY PAX SEAT ROW 6. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1996053000368 19960530 00368 WP 1996 5 30 AALA960720 1 19960504 A 3350 LIGHT STRIP DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 479AA 49654 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRI P BY FORWARD GALLEY. SYSTEM GROUND CEHCKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996053000369 19960530 00369 NM 1996 5 30 AALA960725 1 19960505 A 3350 FCC4007 RELAY BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST CR CRUISE 1 SW 07 6822 19700 FLT 1920 - ORD-BDL - DURING CRUISE, EMERGENCY FLOOR LIGHT SYSTEM UNCOMMANDED ILLUMINATION. AIRCRAFT PROCEEDED BDL AND L ANDED WITHOUT INCIDENT. REPLACED EMERGENCY FLOOR LIGHT SYSTEM R70 RELAY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996053000370 19960530 00370 WP 1996 5 30 AALA960727 1 19960502 A 2121 6054578 FAN DOUG DC9 DC982 3022082 WP ACM BAY DEFECTIVE A AALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 246AA 49238 DFW-DEN - FLT 1295 - DURING CRUISE, ELECTRICAL BURNING ODOR NOTED IN AFT CABIN AREA WITH NO OTHER ABNORMAL INDICATIONS. PRECAUTIONARY TURNED POWER OFF TO REAR GALLEY AND AIRCRAFT PROCEEDED TO DEN, LANDING WITHOUT INCIDENT. PLACARDED AIR C ONDITIONING SYSTEM RECIRC FAN AND AIRCRAFT RETURNED TO SERVICE. SUBSEQUENTLY REPLACED AIR CONDITIONING SYSTEM RECIRC FA N AT DFW/04. SYSTEM GROUND CHECKED NORMAL OPERATION WITH NO ODOR NOTED. PLACARD REMOVED. (M) 2 L 7 2 4F A6WE 1996053000371 19960530 00371 WP 1996 5 30 AALA960728 1 19960504 A 3260 833708 SENSOR DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA K NONE N FALSE WARNING CL CLIMB 1 SW 07 246AA 49238 DFW - FLT 296 - AFTER TAKEOFF TUS, WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR RED LIGHT STAYED ILLUMINATED INITIALLY AND THEN FLICKERED AND FINALLY EXTINGUISHED DURING CLIMB-OUT. AIRCRAFT PROCEEDED TO DFW AND LANDED WITHOUT INCIDENT. R EPLACED NOSE LANDING GEAR UPLOCK SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996053000372 19960530 00372 NM 1996 5 30 ASAA9640035 1 19960430 A 5240 69584321 ROLLER BOEING 737 7374Q8 NM R1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 780AS 25112 PDX - FLT NR 437 - CREW REPORTS, THAT THE R-1 DOOR HANDLE POPS UP FROM THE CLOSE POSITION. FOUND FORWARD LOWER ROLLER O UT OF RIG TOLERANCE. RE-RIGGED PER MM AND HANDLE OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996053000373 19960530 00373 WP 1996 5 30 ASAA9680113 1 19960428 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 943AS 53018 SFO - DURING MAINTENANCE CHECK, THE AFT TWO OVERHEAD EMERGENCY LIGHTS AND THE OVERHEAD EMERGENCY LIGHT ABOVE THE TAILCON E EMERG EVAC SLIDE WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996053000374 19960530 00374 EU 1996 5 30 AWXA960222 1 19960427 A 3350 321430 BATTERY AIRBUS 320 A320232 3930326 EU CABIN FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 639AW 11096 471 PHX - FLT NR 583 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT AT FWD DOORS INOP. REMOVED AND REPLACED FWD EMERGENCY LIGHT BATTERY. LIGHTS OPERATE NORMALLY AT THIS TIME. (M) 2 L 7 2 4F RT A28NM 1996053000375 19960530 00375 NM 1996 5 30 AWXA960223 1 19960429 A 3350 LIGHT BOEING 737 7373G7 1384595 NM CABIN LOOSE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 306AW 24633 PHX - FLT 544 - DURING ROUTINE MX CHECK, FOUND 2 OVERHEAD BIN MOUNTED EMERGENCY EXIT LIGHTS BROKEN LOOSE ON THE LEFT SID E. RESECURED 2 OVERHEAD BIN MOUNTED EMERGENCY EXIT LIGHTS. (M) 2 L 7 2 4F RT A16WE 1996053000376 19960530 00376 SW 1996 5 30 BDHA960008 1 19960411 A 6120 8702A22 NTS WIRE SWRNGN SA226 SA226TC 8780404 SW RT ENGINE FAILED A BDHA O OTHER O OTHER NR NOT REPORTED 1 GL 15 329BA TC238 MSP - FLT 434 - THE CREW REPORTED THE RIGHT ENGINE NTS TEST WAS INOP. MX PERSONNEL REPAIRED WIRE AT LARGE FIREWALL PLUG . TEST WAS PERFORMED AND THE AIRCRAFT WAS RELEASED. (M) 2 L 7 2 4T RT A8SW 1996053000377 19960530 00377 SW 1996 5 30 BDHA960009 1 19960407 A 2612 FIRE DETECTOR SWRNGN SA226 SA226TC 8780404 SW RT ENGINE OPEN WIRE A BDHA K NONE P NO WARNING INDICATION NR NOT REPORTED 1 GL 15 329BA TC238 RAP - FLT 475 - CREW REPORTED THE RIGHT ENGINE FIRE WARNING LIGHT WOULD NOT TEST. MX PERSONNEL REPAIRED WIRE P/N 5710A2 2, AT THE TOP INBOARD FIRE DETECTOR. SYSTEM TEST SHOWED NORMAL. THE AIRCRAFT WAS RELEASED. (M) 2 L 7 2 4T RT A8SW 1996053000378 19960530 00378 SW 1996 5 30 BDHA960010 1 19960411 A 3040 140132100 WIPER MOTOR SWRNGN SA226 SA226TC 8780404 SW LT WINDSHIELD INOPERATIVE A BDHA O OTHER O OTHER NR NOT REPORTED 1 GL 15 329BA TC238 RAP - FLT 434 - LEFT WINDSHIELD WIPER INOP. REPLACED MOTOR AND PERFORMED OPERATIONAL CHECK. THE AIRCRAFT WAS RELEASED. (M) 2 L 7 2 4T RT A8SW 1996053000379 19960530 00379 NM 1996 5 30 CKSA96030 1 19960327 A 2530 244E10001 OVEN BOEING 747 747146 NM AFT GALLEY SMOKING A CKSA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 704CK 69430 20528 VIDP - LEFT NR 2 OVEN (FACING FORWARD) AND LEFT NR 2 OVEN FACING AFT IN AFT GALLEY, BOTH EMITTED A LOUD RATTLING NOISE, GOT EXTREMELY HOT AND EMITTED SMOKE WITH NOTHING HAVING BEEN PUT IN OVEN. LUBED NR 2 OVEN FACING FORWARD AND LUBED NR 2 OVEN FACING AFT IN AFT GALLEY. OPS CHECKED GOOD. (M) 2 L 7 4 4F A20WE 1996053000380 19960530 00380 WP 1996 5 30 EIAA9609 1 19960503 A 3230 NAS3544281 ROD DOUG DC9 DC933F 302207A WP NLG BROKEN A A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 945F 39410 10519 47279 BIL - ON DEPARTURE LEVER LATCH (ANTI-RETRACTION PIN) WOULD NOT ALLOW RETRACTION OF LANDING GEAR. NOSE WHEEL STEERING WH EEL TURNED FREELY SO DID OVERRIDE AS PER ABNORMAL PROCEDURE. RETURNED FOR NORMAL LANDING AFTER ACCOMPLISHMENT OF ABNORM AL PROCEDURE. REPLACED BROKEN CONNECTOR LINK AT NOSE GEAR GROUND SHIFT SENSE FITTING ANTI-RETRACT. 'LEVER LATCH' OPS C HECK GOOD PER DC-9 MM 32-31-1. (M) 2 L 7 2 4F A6WE 1996053000381 19960530 00381 NM 1996 5 30 EIAA9610 1 19960504 A 3230 366103 SELECTOR VLV BOEING 747 747273C 1384896 NM LT MLG FAILED A A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 MEL - DURING TAXI NR 1 HYDRAULIC SYSTEM DROPPED SUDDENLY. NO STEERING CONTROL. PUMPS SHUT DOWN WITHIN 10 SECONDS. LEF T BODY GEAR SELECTOR VALVE BODY FOUND SPLIT. SAME REPLACED PER MM 32-31-03. CHECKED NR 1 EDP AND ADP CASE DRAIN FILTER S, FOUND CLEAN. SERVICED NR 1 HYD SYSTEM. OPERATED NR 1 EDP AND ADP FOR 2 MINUTES AND CYCLED FLIGHT CONTROLS. RE-CHEC KED CASE DRAIN FILTERS, FOUND CLEAN. BLED BODY GEAR NOSE SLECTOR VALVE AND CHECKED VALVE OPERATION PER MM 32-31-03. (M ) 2 L 7 4 4F A20WE 1996053000382 19960530 00382 NM 1996 5 30 MALA964941 1 19960324 A 3350 6104781 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 831MA 339 DURING A MAINTENANCE INSPECTION IN DTW, THE AFT TWO EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENA NCE REPLACED THE LEFT AFT BATTERY PACK. SYSTEM OPERATED SATISFACTORILY. (M) 2 H 7 2 4T RT A13NM 1996053000383 19960530 00383 NM 1996 5 30 MALA964942 1 19960408 A 2611 3023143 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM CARGO BAY FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 861MA 362 FLT 3005 - ON CLIMB-OUT FROM DTW, THE SMOKE WARNING LIGHT INTERMITTENTLY ILLUMINATED. THE AIRCRAFT RETURNED TO DTW. MA INTENANCE REPLACED THE FORWARD AND AFT SMOKE DETECTORS. ALL CHECKS SATISFACTORY. (M) 2 H 7 2 4T RT A13NM 1996053000384 19960530 00384 SW 1996 5 30 MALA964943 1 19960409 A 3260 1EN516 SWITCH SWRNGN SA227 SA227AC 8780603 SW RT MLG LACK OF LUBE A MALA K NONE P NO WARNING INDICATION CL CLIMB 1 GL 15 2692P AC658B YXU - FLT 3345 - ON CLIMB-OUT, THE RIGHT MAIN GEAR INTRANSIT LIGHT FAILED TO ILLUMINATE UPON GEAR RETRACTION. ALL OTHER GEAR INDICATIONS NORMAL. THE AIRCRAFT CONTINUE TO DTW. MAINTENANCE CLEARED AND LUBED THE RIGHT LANDING GEAR SWITCHES. ALL CHECKS SATISFACTORY. (X) 2 L 7 2 4T RT A8SW 1996053000385 19960530 00385 SW 1996 5 30 MALA964944 1 19960406 A 5330 SKIN SWRNGN SA227 SA227AC 8780603 SW FS 493 DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 426MA AC645 MSP - DURING AN INSPECTION, FOUND FUSELAGE SKIN DENTED AFT OF CARGO DOOR AT FS 493.00 AND WL 75.00. REMOVED DAMAGED ARE A (8.00 INCHES BY 9.75 INCHES), FABRICATED REPAIR DOUBLER, REPAIR FILLER, AND INSTALLED IAW FAIRCHILD SRM 53-90-20, PAGE S 64-65. (X) 2 L 7 2 4T RT A8SW 1996053000386 19960530 00386 SW 1996 5 30 MALA964945 1 19960412 A 5320 2722085 DOOR FRAME SWRNGN SA227 SA227AC 8780603 SW BS 438.06 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 421MA AC634 MSP - DURING AN INSPECTION, FOUND AN APPROXIMATE .575 INCH CRACK IN THE CARGO DOOR FRAME PN 27-22085 AT FS 438.060. REP AIRED DAMAGE BY REMOVING DAMAGED GAS STRUT MOUNT HOLE (1.625 INCH BY 1.825 INCH), FABRICATING, TREATING, AND INSTALLING A REPAIR ANGLE, REPAIR PLATE, AND FILLER IAW FAIRCHILD ARP 53-20-9503. (X) 2 L 7 2 4T RT A8SW 1996053000387 19960530 00387 SW 1996 5 30 MALA964946 1 19960412 A 5330 SKIN SWRNGN SA227 SA227AC 8780603 SW FS 512-530.8 DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 421MA AC634 DURING AN INSPECTION IN MSP, FOUND FUSELAGE SKIN DENTED AFT OF CARGO DOOR BETWEEN FS 512 AND FS 530.810, JUST BELOW WL 7 5. DENTED AREA DIMENSIONS 8 INCHES BY .375 INCHES. FABRICATED A REPAIR DOUBLER (13 INCHES BY 5.25 INCHES ) AND INSTALL ED IAW FAIRCHILD SRM 53-90-20 REPAIR NR 14, PGS 61-64. WEIGHT AND BALANCE CHANGE IS NEGLIGIBLE. (M) 2 L 7 2 4T RT A8SW 1996053000388 19960530 00388 SW 1996 5 30 MALA964948 1 19960411 A 2437 BUS LIGHT SWRNGN SA227 SA227AC 8780603 SW COCKPIT FLICKERS A MALA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 15 428MA AC646 YNG - FLT 3367 - ON APPROACH THE RIGHT NON-ESSENTIAL BUS LIGHTS BEGAN TO FLICKER AND THE CREW NOTED AN ELECTRICAL SMELL. MAINTENANCE DEFERRED THE SYSTEM PER MEL 33-1C. (X) 2 L 7 2 4T RT A8SW 1996053000389 19960530 00389 SW 1996 5 30 MALA964949 1 19960412 A 2612 FIRE DETECTOR SWRNGN SA227 SA227AC 8780603 SW LT ENGINE MALFUNCTIONED A MALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 15 425MA AC640 FLT NR 3302 - DURING THE TAKEOFF ROLL IN MSP, THE LEFT ENGINE FIRE LIGHT ILLUMINATED. THE TAKEOFF ATTEMPT WAS ABORTED A ND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. MX TESTED THE ENGINE WIRING . ALL CHECKS GOOD. AS A PRECAUTION, THE FIRE DETECTORS WERE REPLACED. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2 L 7 2 4T RT A8SW 1996053000390 19960530 00390 NM 1996 5 30 MALA964951 1 19960415 A 3230 MS2452333 INHIBIT SWITCH DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A MALA O OTHER O OTHER AP APPROACH 1 GL 15 827MA 331 FLT 3099 - ON APPROACH TO MSP, THE LANDING GEAR DIDN'T EXTEND WHEN SELECTED DOWN. THE CREW NOTED THAT THE INHIBIT SWITC H WAS LOOSE. THE CREW ACTUATED THE SWITCH SEVERAL TIMES. THE GEAR THEN EXTENDED NORMALLY. MAINTENANCE REPLACED THE IN HIBIT SWITCH. ALL SYSTEMS OPERATED SATISFACTORILY DURING GEAR SWINGS. (M) 2 H 7 2 4T RT A13NM 1996053000391 19960530 00391 NM 1996 5 30 MALA964952 1 19960415 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT INOPERATIVE A MALA O OTHER O OTHER CR CRUISE 1 GL 15 829MA 335 FLT 3450 - DURING THE PREFLIGHT IN DTW, THE CREW NOTED THAT THE COCKPIT EMERGENCY EXIT LIGHT ASSEMBLY WAS INOPERATIVE. M AINTENANCE REPLACED THE LIGHT ASSEMBLY. ALL CHECKS SATISFACTORY. (M) 2 H 7 2 4T RT A13NM 1996053000392 19960530 00392 NM 1996 5 30 MALA964953 1 19960410 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 831MA 339 DTW - FLT 3152 - DURING POST-FLIGHT INSPECTION, THE OVERHEAD EMERGENCY LIGHT WOULD INTERMITTENTLY ILLUMINATE. MAINTENAN CE REPLACED THE LIGHT ASSEMBLY. SYSTEM OPERATED SATISFACTORILY. (X) 2 H 7 2 4T RT A13NM 1996053000393 19960530 00393 SW 1996 5 30 MALA964954 1 19960415 A 2612 CONNECTORS SWRNGN SA227 SA227AC 8780603 SW FIRE PANELS FAILED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 425MA AC640 MSP - FLT 3495 - ON CLIMB-OUT, LEFT ENGINE FIRE INDICATORS ILLUMINATED. ALL OTHER ENGINE INDICATIONS WERE NORMAL. THE AIRCRAFT RETURNED TO MSP WITHOUT INCIDENT. MAINTENANCE REPLACED CONNECTOR PLUGS FOR THE ANNUNCIATOR AND FIRE PANELS. ( X) 2 L 7 2 4T RT A8SW 1996053000394 19960530 00394 SW 1996 5 30 MALA964955 1 19960417 A 5400 ANGLE SWRNGN SA227 SA227AC 8780603 SW RT WING/NACELLE BROKEN RIVET A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 60NE AC760B DURING AN INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED LOWER RIGHT OUTBOARD WING TO NACELLE TRANSIT ANGLE HAS A RIVET HEAD BROKEN HALF OFF AND A .125 INCH CRACK EMANATING FROM RIVET. LOCATION IS 9 RIVETS AFT OF DE-ICE BOOT EDGE. COMPLET ED REPAIR BY REMOVING RIVETS IN DAMAGED AREA, STOP DRILLING CRACK AND WET INSTALLING REPAIR DOUBLER IAW ARP 54-20-9101. REV B DATED MAY 12, 1993. (M) 2 L 7 2 4T RT A8SW 1996053000395 19960530 00395 SW 1996 5 30 MALA964956 1 19960417 A 5311 FRAME SWRNGN SA227 SA227AC 8780603 SW BS 493.347 DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 60NE AC760B DURING AND INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND LOWER BELT FRAME AT FS 493.247 SLIGHTLY OIL CANNED HORIZONTALL Y JUST ABOVE STRINGER PASS THROUGH AT FUSELAGE CENTERLINE. OIL CANNING EXTENDED FROM WL 67.88 LEFT THROUGH BL 0.90 TO W L 67.88 RIGHT. COMPLETED REPAIR TO LOWER BELT FRAME AT FS 493.247 BY REINFORCING FRAME WITH THE INSTALLATION OF TWO .08 BY .75 BY 5 INCH REPAIR ANGLES. FABRICATED, PREPPED, AND INSTALLED REPAIR ANGLES AND FILLER STRAPS IAW AERO TECH DESIG NS EAN NR01-96026. (M) 2 L 7 2 4T RT A8SW 1996053000396 19960530 00396 SW 1996 5 30 MALA964957 1 19960417 A 5310 STRUCTURE SWRNGN SA227 SA227AC 8780603 SW BS 491 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 60NE AC760B DURING AN INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND .300 CRACK IN CENTER SUB FLOOR STRUCTURE LIGHTING HOLE FLANGE J UST FORWARD OF FS 491.00. STOP DRILLED CRACK AND DRESSED OUT AREA. FABRICATED, PREPPED AND INSTALLED A 8.5 INCH BY 5 I NCH ELLIPITCAL REPAIR DOUBLER TO FLANGE AREA. ALL WORK IAW AERO TECH DESIGNS EA 01-96025. (M) 2 L 7 2 4T RT A8SW 1996053000397 19960530 00397 SW 1996 5 30 MALA964958 1 19960417 A 5730 COVER PANEL SWRNGN SA227 SA227AC 8780603 SW WS 266 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 60NE AC760B DURING AN INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE RIGHT WING EXTENSION AT TOP SKIN COVER PANEL, ONE SCREW HOL E CRACKED AND OTHERS WORN ELONGATED. LOCATION IS AT WS 266.00. FABRICATED, TREATED AND INSTALLED REPAIR DOUBLER IAW FA IRCHILD SRM 57-90-20 PGS 19-21, REV NOV 1/94. (M) 2 L 7 2 4T RT A8SW 1996053000398 19960530 00398 SW 1996 5 30 MALA964959 1 19960417 A 5522 2744001161 SKIN SWRNGN SA227 SA227AC 8780603 SW ELEVATOR CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 60NE AC760B DURING AN INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND ELEVATOR P/N 27-44001-161 TO HAVE INBOARD MOST LEADING EDGE SKI N PANEL CRACKED FROM SKIN EDGE TO RIVET HOLE APPROX .300 INCH (AREA PREVIOUSLY REPAIRED). REMOVED PREVIOUS REPAIR AND R EPLACED WITH NEW REPAIR DOUBLER IAW FAIRCHILD SRM 51-90-04, RPAIR NR 6 PGS 11-12 (REPAIR DOUBLER 6 INCH BY 2.5). (M) 2 L 7 2 4T RT A8SW 1996053000399 19960530 00399 SW 1996 5 30 MALA964960 1 19960417 A 5320 2725008005 ANGLE SWRNGN SA227 SA227AC 8780603 SW BS 107 WORN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 60NE AC760B DURING AN INSPECTION INS MSP, MAINTENANCE PERSONNEL AT FS 107 CAPTAINS SIDE INBOARD SEAT TRACK, BOX BEAM INBOARD SUPPORT ANGLE P/N 27-25008-005 WORN. REMOVED AND REPLACED SUPPORT ANGLE WITH SERVICEABLE BY FABRICATION. FABRICATED NEW ANGLE FROM 2024-T4 STOCK, PREPPED, PRIMED AND INSTALLED. ALL WORK IAW FAIRCHILD SRM 51-30-00, 51-40-00, AND 51-50-00 REV JUN 01/93. (M) 2 L 7 2 4T RT A8SW 1996053000400 19960530 00400 SW 1996 5 30 MALA964961 1 19960413 A 5753 2736003001 RIB SWRNGN SA227 SA227AC 8780603 SW LT TE FLAP CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 60NE AC760B DURING AN INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE LEFT FLAP INBOARD AFT END RIB CHAFFED APPROXIMATELY .200 IN CH BY .500 INCH, OUTBOARD NOSE END RIB CRACKED IN RELIEF RADIUS AND OUTBOARD HINGE ARM BENT. COMPLETED REPAIR 'PART FOR PART' REPLACEMENT WITH A NEW LEFT INBOARD AFT ENG RIB P/N 27-36003-001, NEW OUTBOARD NOSE END RIB P/N 27-26015-009 AND NEW OUTBOARD HINGE ARM P/N 27-36044-005. ALL WORK DONE IAW FAIRCHILD SRM 51-00-00, PG 4 REV JUNE 1/93, AND 57-90-60 PGS 43-46. FAIRCHILD SRM CHANGERS REFERENCED 51-30-04, REV JUNE 1/93 AND 51-40-00 REV JUNE 1/93. (M) 2 L 7 2 4T RT A8SW 1996053000401 19960530 00401 SW 1996 5 30 MALA964966 1 19960414 A 5730 SKIN SWRNGN SA227 SA227AC 8780603 SW LT WING DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 60NE AC760B DURING AN INSPECTION IN MSP, MAINTENANCE PERSONNEL COMPLETED REPAIR TO THE LEFT LOWER WING SKIN JUST FORWARD OF WING PAN EL NR 663 DUE TO THREE SMALL DENTS BELOW REFUELING PORT BY INSTALLING A .040 2024 T-3 EXTERNAL DOUBLER MEASURING 7.5 INC HES LONG BY 3.6 INCHES WIDE. ALL WORK DONE IAW FAC SRM 57-90-20 PGS 41-42 (ARP 57-90-9118 REV A). (M) 2 L 7 2 4T RT A8SW 1996053000402 19960530 00402 NM 1996 5 30 MALA964968 1 19960418 A 3150 WARNING LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT FLASHED A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 827MA 331 MLI - FLT 3312 - EN ROUTE, MASTER CAUTION LIGHT BEGAN TO FLASH WITH NO ASSOCIATED ANNUNCIATOR LIGHT. THE AIRCRAFT RETUR NED TO MSP. MAINTENANCE CYCLED THE POWER AND ALL CHECKS WERE GOOD. MAINTENANCE CHECKED SYSTEM CONNECTIONS AND COMPONEN TS. ALL CHECKS SATISFACTORY. (X) 2 H 7 2 4T RT A13NM 1996053000403 19960530 00403 SW 1996 5 30 MALA964969 1 19960418 A 3260 8496 LOGIC BOX SWRNGN SA227 SA227AC 8780603 SW COCKPIT MALFUNCTIONED A MALA O OTHER P NO WARNING INDICATION CR CRUISE 1 GL 15 442MA AC725 MSP - FLT 3074 - IN CRUISE FLIGHT, THE CREW NOTED THAT, WITH THE FLAPS AND GEAR UP, THE GEAR WARNING HORN WOULD NOT SOUN D. MAINTENANCE REPLACED THE MONITOR AMP LOGIC BOX PN 8496, AND ADJUSTED IAW FAC 27-50-10, PAGE 206. ALL CHECKS SATISFA CTORY. (X) 2 L 7 2 4T RT A8SW 1996053000404 19960530 00404 SW 1996 5 30 MALA964970 1 19960419 A 3230 1EN516 SWITCH SWRNGN SA227 SA227AC 8780603 SW NLG OUT OF ADJUST A MALA K NONE J WARNING INDICATION CL CLIMB 1 GL 15 430MA AC710 FLIGHT 3234 - ON CLIMB-OUT FROM BJI, THE NOSE GEAR CONTINUED TO CYCLE IN THE WHEEL WELL AFTER THE GEAR WAS RETRACTED. M AINTENANCE ADJUSTED THE UPLIMIT SWITCH. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2 L 7 2 4T RT A8SW 1996053000405 19960530 00405 NM 1996 5 30 PCAA9600280 1 19960407 A 5540 85530024003 UPPER ARM ASSY DHAV DHC8 DHC8102 2809003 NM RUDDER WORN A A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 801MX 20383 008 DURING A SCHEDULED RUDDER CHANGE, THE VERTICAL STABILIZER UPPER AND LOWER CENTER HINGE FITTING RUDDER ATTACH POINTS WERE FOUND WORN. THE BUSHINGS WOULD NOT INSTALL CORRECTLY DUE TO THE HOLES BEING OVERSIZED. REMOVED AND REPLACED UPPER AND LOWER CENTER HINGE FITTINGS IAW DEHAVILLAND DRAWINGS. INSTALLED RUDDER ASSEMBLY IAW DEHAVILLAND MM. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1996053000406 19960530 00406 NM 1996 5 30 PCAA9600281 1 19960417 A 6120 78249028 PROP CONTL UNIT DHAV DHC8 DHC8102 2809003 NM RT ENGINE MALFUNCTIONED A PCAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 13 810EX 880530 308 DURING TAKEOFF, CREW NOTICED RIGHT PROPELLER RPM WAS 1236. CREW ABORTED TAKEOFF WITHOUT INCIDENT. REMOVED AND REPLACED RIGHT PROPELLER CONTROL UNIT IAW DHC 8 MM. LEAK CHECK AND OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M ) 2 H 7 2 4T RT A13NM 1996053000407 19960530 00407 NM 1996 5 30 PCAA9600284 1 19960422 A 3350 LIGHTS DHAV DHC8 DHC8102 2809003 NM CABIN MALFUNCTIONED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 810EX 10952 308 EMERGENCY LIGHTS ACTIVATED DURING TAXI. POWERED AIRCRAFT DOWN, CYCLED FLIGHT ATTENDANTS EMERGENCY LIGHT SWITCH, OPERATI ONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1996053000408 19960530 00408 NM 1996 5 30 PCAA9600286 1 19960426 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 831EX 6092 010342 160 EMERGENCY LIGHTS CIRCUIT BREAKER POPPED IN FLIGHT. TROUBLESHOT, FOUND FAULTY COCKPIT OVERHEAD EMERGENCY LIGHT ASSY. RE PLACED EMERGENCY LIGHT ASSEMBLY, OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1996053000409 19960530 00409 NM 1996 5 30 PCAA9600287 1 19960426 A 5320 MS21250H06022 BOLT DHAV DHC8 DHC8102 2809003 NM BATH TUB FTG CRACKED A A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 800MX 20370 007 DEHAVILLAND TASK 5310/08F DUE FOR TIME COMPLETED TASK 531008F, INSPECTION OF FORWARD BATH TUB FITTINGS AND BOLTS. FOUND CRACK LIKE INDICATION OF LEFT FORWARD BOLT AND RIGHT FORWARD BOLT DOES NOT GIVE FULL BACK REFLECTION. REMOVED AND REPL ACED LEFT AND RIGHT BOLTS IAW DHC S/B 8-57-22. BATHTUB FITTING CHECK REVEALED NO DEFECTS. AIRCRAFT RETURNED TO SERVICE . (M) 2 H 7 2 4T RT A13NM 1996053000410 19960530 00410 WP 1996 5 30 RAIA960423 2 19960417 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RIGHT LOW POWER A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CE 03 436AM 9328 3324 891 66184 COU - FLT 7026 - RIGHT ENGINE WOULD NOT MAKE TARGET TORQUE. MX REPLACED RIGHT ENGINE, PERFORMED GROUND RUNS OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996053000411 19960530 00411 1996 5 30 RAIA960424 4 19960421 A 3442 7008470822 TR UNIT JETAIR JETSTM JETSTM4101 1500501 EU NOSE FAULTY A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 558HK 900 41071 STL - FLT 7460 - WEATHER RADAR BECAME INOP DURING FLIGHT. MAINTENANCE REPLACED RADAR TRANSMITTER, OPERATION CHECK GOOD. (M) 2 L 7 2 4T RT A41NM 1996053000412 19960530 00412 EU 1996 5 30 RAIA960427 1 19960418 A 5610 NP1588622 WINDSHIELD AEROSP ATR42 ATR42300 8680920 EU RT COCKPIT CRACKED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 424TE 6498 124 STL - FLT 7180 - COCKPIT RIGHT SIDE WINDOW CRACKED. MX INSPECTED WINDSHIELD FOUND CRACK IN LIMITS PER ATR SRM, AS A PRE CAUTION MX REPLACED CRACKED WINDSHIELD, OPERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1996053000413 19960530 00413 EU 1996 5 30 REXA96013 1 19960331 A 2613 CONNECTOR SAAB SF340 SF340A 7850100 EU LT ENGINE BROKEN WIRE A REXA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 SO 25 327PX 24362 340A059 LEFT TAIL PIPE 'HOT' LIGHT (CAPTION) ON DURING CLIMB-OUT. SHUT ENGINE DOWN AND RETURNED RAMP. LIGHT WAS ON WHOLE WAY B ACK. REPLACED BROKEN WIRE ON LEFT ENGINE TAIL PIPE SPOT DETECTOR CANNON PLUG. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1996053000414 19960530 00414 EU 1996 5 30 REXA96014 1 19960503 A 2612 51653151 CONTROL UNIT FENWAL BAG JETSTM JETSTM3101 1500215 EU LT ENGINE FAILED A A REXA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 SO 25 311PX 104 679 DURING START OF LEFT ENGINE, LEFT FIRE WARNING LIGHT ILLUMINATED. AS PER CHECKLIST, CREW SECURED ENGINE AND INITIATED S HOT ONE OF FIRE EXT SYSTEM. SHOT ONE POPPED CIRCUIT BREAKER. SHOT TWO SELECTED AND FIRED. REPLACED LEFT FIREWIRE CONT ROL UNIT WHICH ACCOUNTED FOR THE FALSE INDICATION. UPON REPLACEMENT OF THE EXPENDED FIRE BOTTLE, CORRECTED MISWIRED FIR ING CIRCUIT CONNECTIONS FOR BOTH LEFT FIRE PROTECTION CIRCUITS. (M) 2 L 7 2 4T RT A21EU 1996053000415 19960530 00415 NM 1996 5 30 TAOA059601 1 19960507 A 3350 079123 LAMP HOLDER BRUCE BOEING 727 727225 1384077 NM CABIN MISSING A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 918TS 20445 FLT NR 6141 - BOS-LGA - FOUND ON L/S CHECK, ESCAPE PATH LIGHTING CAPSULE AND LAMP MISSING AT ROW 17. REPLACED MISSING C APSULE AND LAMP. (M) 2 L 7 3 4F A3WE 1996053000416 19960530 00416 NM 1996 5 30 TSAA9625020 1 19960422 A 2120 AIR DISTRIBUTION BOEING 737 7372M6C 1384708 NM COCKPIT ODOR A TSAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 13 805AL 21809 FLT NR 950 - BURNING SMELL IN COCKPIT. DIVERTED AIRCRAFT TO OGG. VISUALLY INSPECTED AIRCRAFT SYSTEM, ELECTRICAL SYSTEM , AND ENGINE AND FOUND NO DEFECTS. OPERATED ENGINES AND AIRCRAFT SYSTEMS AND FOUND NO DEFECTS. AIRCRAFT RETURNED TO SE RVICE. (M) 2 L 7 2 4F RT A16WE 1996053000417 19960530 00417 NM 1996 5 30 TSAA9653022 1 19960505 A 5330 SKIN BOEING 737 737297 1384480 NM BS 727 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 725AL 22051 DURING DAILY CHECK, DISCOVERED FUSELAGE SKIN CRACK 2.75 INCH IN LENGTH AT BS 727A PLUS 15 INCHES AND STRINGER 16L. CONF IRMED WITH HFEC. REPAIRED PER SRM 53-30-3 FIG 6. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1996053000418 19960530 00418 NM 1996 5 30 TSAA9653023 1 19960505 A 5330 SKIN BOEING 737 737297 1384480 NM BS 727 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 725AL 22051 DURING DAILY CHECK, DISCOVERED FUSELAGE SKIN CRACK 2.25 INCH IN LENGTH AT BS 727 B PLUS 15 INCHES AND STRINGER 17L. CON FIRMED WITH HFEC. REPAIRED PER SRM 53-30-3 FIG 25. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1996053000419 19960530 00419 NM 1996 5 30 TSAA9653024 1 19960507 A 5330 SKIN BOEING 737 7372Q9 138448M NM BS 328 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 804AL 21719 DURING DAILY CHECK, DISCOVERED FUSELAGE SKIN CRACK 4 INCHES IN LENGTH AT BS 328 PLUS 6 INCHES AND 2 INCHES BELOW STRINGE R 22R. HFEC CONFIRMED. REPAIRED PER SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1996053000420 19960530 00420 NM 1996 5 30 TSAA9653025 1 19960507 A 5330 SKIN BOEING 737 7372Q9 138448M NM BS 727 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 804AL 21719 DISCOVERED FUSELAGE SKIN CRACKS, 1.25 INCH AT BS 727A PLUS 15, 1 INCH ABOVE STRINGER 16L, AND 4.5 INCHES AT BS 727A PLUS 15, 1 INCH ABOVE STRINGER 17L. HFEC VERIFIED. REPAIRED PER SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1996053000421 19960530 00421 NM 1996 5 30 TSAA9653026 1 19960507 A 5330 SKIN BOEING 737 7372Q9 138448M NM BS 727 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 804AL 21719 DISCOVERED FUSELAGE SKIN CRACK 2.25 INCH AT BS 727A, 1 INCH BETWEEN STRINGER 17L AND STRINGER 18L. HFEC CONFIRMED. REP AIRED PER SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1996053000422 19960530 00422 WP 1996 5 30 USAA960367 1 19960404 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 965 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 925VJ 35350 48145 PIT - DURING SCHEDULED PRODUCTION CONTROL ITEM, FOUND A 2 INCH CRACK RIGHT SIDE SKIN LONGERON 14R-15R AT STATION 965. I NSTALLED TITANIUM DOUBLER PER USAIR EA NR 32460. (M) 2 L 7 2 4F A6WE 1996053000423 19960530 00423 NM 1996 5 30 USAA960404 1 19960425 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 1016 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 242US 38249 22444 ROA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND 6 INCH CORROSION ON STRINGER, FORWARD OF AFT PRESSURE BULKHEAD STRINGER 26R BS 1016. INSTALLED NEW STRINGER, REPAIRED PER SRM 53-10-3. (M) 2 L 7 2 4F A16WE 1996053000424 19960530 00424 WP 1996 5 30 USAA960405 1 19960430 A 5320 59132624 ANGLE DOUG DC9 DC931 3022065 WP BS 1019 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 978VJ 70202 47371 PIT - DURING A Q-1C-1 CHECK INSPECTION, FOUND .75 INCH CRACK RIGHT PYLON TOP DRAG ANGLE AT STATION 1019. INSTALLED DOUB LER REPAIR PER SRM 54-04 FIG 10. (M) 2 L 7 2 4F A6WE 1996053000425 19960530 00425 WP 1996 5 30 USAA960406 1 19960430 A 5320 991224355 ANGLE DOUG DC9 DC931 3022065 WP BS 996 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 978VJ 70202 47371 PIT - DURING A Q-1/C-1 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED APPROXIMATELY 3 FEET LONG FLOOR BEA M STATION 996 LEFT SIDE ON CAP ANGLE. CPCP TASK NR C58-53300. REPLACED CORRODED SECTION OF CAP ANGLE PER USAIR TYPICA L REPAIR NR 53-10-14. (M) 2 L 7 2 4F A6WE 1996053000426 19960530 00426 WP 1996 5 30 USAA960407 1 19960430 A 5311 991224671A BELTFRAME DOUG DC9 DC931 3022065 WP BS 1038 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 978VJ 70202 47371 PIT - DURING A Q-1/C-1 CHECK INSPECTION, FOUND 2 CRACKS, ONE CRACK IS 1 INCH LONG AND THE OTHER CRACK IS 2.25 INCHES LON G IN BELTFRAME SKIN STATION 1038 LEFT SIDE BETWEEN LONGERON 12L AND 13L. INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 3. (M) 2 L 7 2 4F A6WE 1996053000427 19960530 00427 WP 1996 5 30 USAA960408 1 19960430 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 1095 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 978VJ 70202 47371 PIT - DURING A Q-1/C-1 CHECK INSPECTION, FOUND .5 INCH CRACK IN LEFT FUSELAGE SKIN BETWEEN LONGERON 3L AND 4L STATION 10 95. INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 27. (M) 2 L 7 2 4F A6WE 1996053000428 19960530 00428 WP 1996 5 30 USAA960409 1 19960430 A 5320 5913262538 ANGLE DOUG DC9 DC931 3022065 WP BS 945 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 978VJ 70202 47371 PIT - DURING A Q-1/C-1 CHECK INSPECTION, FOUND A 1 INCH CRACK RIGHT PYLON LOWER ATTACH ANGLE STATION 945 BETWEEN LONGERO N 15R AND 16R. INSTALLED DOUBLER REPAIR PER SRM 54-04 FIG 10. (M) 2 L 7 2 4F A6WE 1996053000429 19960530 00429 WP 1996 5 30 USAA960410 1 19960430 A 5320 PRESS PANEL DOUG DC9 DC931 3022065 WP BS 105 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 978VJ 70202 47371 PIT - DURING A Q-1/C-1 CHECK INSPECTION, FOUND TWO 3 INCH CRACKS IN THE FORWARD HORIZONTAL PRESSURE PANEL AT FS 105 UNDE R COCKPIT FLOOR NOSE WHEEL WELL. REMOVED CRACKED SECTION AND INSTALLED REPAIR DOUBLER PER USAIR EA 32641. (M) 2 L 7 2 4F A6WE 1996053000430 19960530 00430 NM 1996 5 30 USAA960411 1 19960430 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 328 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 277AU 35249 22889 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORRODED FLOOR BEAM T-CAP STATION 328 RBL 12 TO RBL 48. REMOVED OUT OF LIMITS FLOOR BEAM, FABRICATED T-CAP AND SPLICED NEW SECTION IN, REPAIRED PER 737 TR 53-10-13 PART 2. (M) 2 L 7 2 4F A16WE 1996053000431 19960530 00431 NM 1996 5 30 USAA960412 1 19960430 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 397 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 277AU 35249 22889 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND DENT 6 INCHES BY 1 INCHES AREA FUSELAGE SKIN BS 397 BETWEEN STRINGER 22L AND STRINGER 23L. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 1. (M) 2 L 7 2 4F A16WE 1996053000432 19960530 00432 NM 1996 5 30 USAA960413 1 19960430 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 324 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 277AU 35249 22889 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK LOWER AFT CORNER FORWARD SERVICE DOOR CUTOUT OUTER SKIN AND BEAR STRAP, BS 324 WL 210 RBL 68. INSTALLED DOUBLERS, REPAIRED PER SRM 53-30-3 FIG 26. (M) 2 L 7 2 4F A16WE 1996053000433 19960530 00433 NM 1996 5 30 USAA960414 1 19960430 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 891 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 277AU 35249 22889 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH BY .50 INCH DEEP DENT IN SKIN AT BS 891 BETWEEN STRINGE R 22R AND STRINGER 23R. CUT OUT DAMAGE AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 1. (M) 2 L 7 2 4F A16WE 1996053000434 19960530 00434 NM 1996 5 30 USAA960415 1 19960430 A 5315 FLOOR BEAAM BOEING 737 7372B7 1384560 NM BS 986.5 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 277AU 35249 22889 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 2 INCH BY 40 INCH AREA OF SURFACE CORROSION, FLOOR BEAM UP PER T-CAP AT STATION 986.5 LBL 45 TO RBL 45. INSTALLED T-CAP SPLICE, REPAIRED PER SRM 53-10-05C. (M) 2 L 7 2 4F A16WE 1996053000435 19960530 00435 NM 1996 5 30 USAA960416 1 19960430 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 967 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 277AU 35249 22889 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 3 INCH BY 40 INCH AREA OF SURFACE CORROSION, FLOOR BEAM T- CAP STATION 967, LBL 22 TO RBL 32. REPLACED T-CAP, REPAIRED PER TR 53-10-05C. (M) 2 L 7 2 4F A16WE 1996053000436 19960530 00436 NM 1996 5 30 USAA960417 1 19960430 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 1016 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 277AU 35249 22889 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROX 2 INCH BY 5 INCH AREA OF SURFACE CORROSION, FLOOR BEAM UPPER T-CA P, STATION 1016, RBL 1 TO RBL 6. CUT OFF ENTIRE T-CAP, FABRICATED NEW PART AND INSTALLED PER EA 41077. (M) 2 L 7 2 4F A16WE 1996053000437 19960530 00437 NM 1996 5 30 USAA960418 1 19960504 A 5330 SKIN BOEING 737 737201 1384454 NM BS 390 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 229US 44252 21818 ROA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND 12/32 INCH BY .065 DENT RIGHT FUSELAGE SKIN AT STRINGER 20 BS 390. REM OVED DAMAGED SKIN AND INSTALLED DOUBLER. REPAIRED PER EA 58327. (M) 2 L 7 2 4F A16WE 1996053000438 19960530 00438 NM 1996 5 30 USAABB96014 1 19960427 A 3230 DNLOCK ACTUATOR BOEING 757 7572B7 1384964 NM NLG FAILED A USAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 19 633AU 27811 LAX - FLT 0017 - ON APPROACH TO LAX, CREW RECEIVED NOSE GEAR NOT DOWN INDICATION. CREW CYCLED THE GEAR TWICE AND DID A TOWER FLYBY. TOWER CONFIRMED THAT THE NOSE GEAR WAS STILL RETRACTED. ON THIRD RECYCLE, THE NOSE GEAR EXTENDED. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE NOSE GEAR LOCK ACTUATOR, NOSE GEAR OPERATED SEQUENCE VALVE A ND THE NOSE GEAR DOOR SEQUENCE VALVE. (M) 2 L 7 2 4F RT A2NM 1996053000439 19960530 00439 NM 1996 5 30 USAABB96015 1 19960506 A 3610 312N53061 HP2 DUCT BOEING 757 757225 1384959 NM LT ENGINE LEAKING A USAA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 EA 19 606AU 22202 SFO - FLT 56 - AFTER TAKEOFF FROM SFO, CREW RECEIVED OVETEMP LIGHT ON LEFT ENGINE. LIGHT EXTINGUISHED WHEN THROTTLE RET ARDED. FLIGHT RETURNED TO SFO AND LANDED WITH NO FURTHER INCIDENTS. MX REPLACED THE HP2 AND P6 DUCTS DUE TO LEAKAGE. ( M) 2 L 7 2 4F RT A2NM 1996053000440 19960530 00440 NE 1996 5 30 USAAD96043 2 19960428 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE RIGHT BIRD STRIKE A USAA A UNSCHED LANDING B C SMOKE/FUMES/ODORS/SPARKS F.O.D. CL CLIMB 1 EA 19 824US 49143 708117 FLT 730 - MSY-PHL - CLIMBING THROUGH APPROXIMATELY 12,000 FEET, CABIN AND COCKPIT STARTED TO FILL WITH NOXIOUS FUMES. P ACKS WERE TURNED OFF, AND FUMES BEGAN TO CLEAR. RETURNED TO MSY. FOUND BIRD STRIKE AT INTAKE RIGHT ENGINE. INSPECTED INTAKE AND EXHAUST AND FOUND NO DAMAGE. PERFORMED INSPECTION PER MD-80 MM 05-31-08, PG 601 AND 602. (M) 2 L 7 2 4F 4 F A6WE E9NE 1996053000441 19960530 00441 WP 1996 5 30 USAAD96044 1 19960428 A 2130 54447222 ACTUATOR DOUG DC9 DC931 3022065 WP OUTFLOW VLV INOPERATIVE A USAA B EMER. DESCENT O OTHER CR CRUISE 1 EA 19 941VJ 35344 47054 FLT 366 - PIT-STL - DURING CRUISE AT FL 210, CABIN ALTITUDE CLIMBED TO 11,000 FEET. STOPPED CABIN AT 12,000 FEET, DESCE NDED TO 10,000 FEET. CABIN PRESSURIZATION WORKED IN MANUAL MODE. REPLACED OUTFLOW VALVE ACTUATOR. (M) 2 L 7 2 4F A6WE 1996053000442 19960530 00442 WP 1996 5 30 USAAD96045 1 19960430 A 7931 7938314501 TUBE ASSY DOUG DC9 DC981 3022081 WP NR 1 ENGINE LEAKING A USAA E A ENGINE SHUTDOWN UNSCHED LANDING J K M WARNING INDICATION FLUID LOSS OVER TEMP CR CRUISE 1 EA 19 803US 48035 FLT 254 - PBI-BWI - AT FL 330, MASTER CAUTION LIGHT CAME ON, LOW OIL PRESSURE LIGHT CAME ON, NOTICED LOSS OF ALL OIL QUA NTITY, LOW OIL PRESSURE, AND RISING OIL TEMPERATURE. SHUT DOWN NR 1 ENGINE, DIVERTED TO SAV. REMOVED AND REPLACED NR 1 ENGINE OIL PRESSURE SWITCH LINE. (M) 2 L 7 2 4F A6WE 1996053000443 19960530 00443 WP 1996 5 30 USAAD96047 1 19960501 A 3610 772622 MANIFOLD DOUG DC9 DC981 3022081 WP LT ENGINE CRACKED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 803US 48035 FLT 842 - LAX-PIT - AFTER TAKEOFF, LEVEL AT 5000 FEET, LEFT FIRE WARNING AND BELL CAME ON. AS SOON AS CREW TURNED BELL OFF, THE LIGHT WENT OFF. RETURNED TO LEX. REPLACED LEFT ENGINE 13TH STAGE MANIFOLD AND SENSE LINE. (M) 2 L 7 2 4F A6WE 1996053000444 19960530 00444 EU 1996 5 30 USAAF96037 1 19960428 A 3260 201251224 DNLOCK SENSOR FOKKER F28 F28MK0100 4990807 EU LEFT MLG FAILED A USAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 EA 19 888AU 11357 PIT - FLT 1450 - AFTER GEAR EXTENSION, CAPTAIN RECEIVED ALL THREE GREEN LIGHTS BUT HAD THE LEFT LANDING GEAR DOWNLOCK SW ITCH MESSAGE. CAPTAIN RECYCLED THE GEAR WITH NO CHANGE. LIGHT WENT OUT PRIOR TO TOUCHDOWN. NO EMERGENCY WAS DECLARED AND THE FLIGHT MADE A NORMAL LANDING. MAINTENANCE REPLACED THE LEFT MLG PRIMARY DOWNLOCK SENSOR. (M) 2 L 7 2 4F RT 1996053000445 19960530 00445 1996 5 30 USAAF96038 4 19960428 A 3417 ADC FOKKER F28 F28MK0100 4990807 EU E/E COMPT MALFUNCTIONED A A USAA B EMER. DESCENT G J MULTIPLE FAILURE WARNING INDICATION CR CRUISE 1 EA 19 881US 11333 STL - FL 2129 - AT FL 350, CREW NOTICED THE THRUST WAS BEING REDUCED BY THE AUTOPILOT, THE CAPT'S AIRSPEED WAS DEGRADING DOWNWARD WHILE THE F/O'S WAS GOING TO REDLINE. THE CAPT TOOK CONTROL OF THE A/C, FLYING MANUALLY, AND STARTED A DESCEN T. AT FL 300 THE A/C LOST ONE PACK AND THE CABIN STARTED TO CLIMB TO 10,000 FT. THE CREW DECLARED AN EMERGENCY AND DES CENDED TO 10,000 FT. DURING DESCENT, OTHER PACK FAILED. MASKS DID NOT DEPLOY. UPON REACHING 10,000 FT, CREW CANCELLED THE EMERGENCY AND THE FLT LANDED IN MCI W/O FURTHER INCIDENT. MX REPLACED THE NR 1 AIR DATA COMPUTER, OPERATIONAL CHEC K GOOD. ALSO RESET THE NR 1 AND 2 CABIN PRESS CONTROLLERS, OPS CHECK GOOD. PRESSURIZED A/C, OPS CHECK GOOD. (M) 2 L 7 2 4F RT 1996053000446 19960530 00446 EU 1996 5 30 USAAF96039 1 19960504 A 3340 3021093 STROBE LIGHT FOKKER F28 F28MK0100 4990807 EU LOWER FUSELAGE FAULTY A USAA O OTHER O OTHER LD LANDING 1 EA 19 889US 11964 11358 LGA - FL 866 - UPON LANDING IN LGA, BRAKE PEDALS WENT TO FLOOR, GRABBED AND CYCLED. MAINTENANCE REPLACED THE LOWER FUSE LAGE STROBE LIGHT DUE TO ELECTROMAGNETIC INTERFERENCE WITH THE ANTI-SKID SYSTEM. ANTI-SKID TEST ACCOMPLISHED, CHECKED N ORMAL. (M) 2 L 7 2 4F RT 1996053000447 19960530 00447 NM 1996 5 30 USAASB96074 1 19960503 A 3350 6013211 POWER PACK BOEING 737 737201 1384454 NM GALLEY DOOR FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 257AU 22799 FLT 510 - ROC - MAINTENANCE FOUND THAT THE AFT ENTRY AND SERVICE DOOR EMERGENCY SLIDE LIGHTING SYSTEM WAS INOP. MX REPL ACED THE BATTERY AND THE CHARGER. SYSTEM CHECKED SAT. (M) 2 L 7 2 4F A16WE 1996053000448 19960530 00448 NM 1996 5 30 USAASB96075 1 19960503 A 2611 MICR0300 SMOKE DETECTOR BOEING 737 737201 1384454 NM AFT LAV FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 22754 FLT NR 2359 - LGA - MX FOUND THAT THE AFT LAV SMOKE DETECTOR WAS INOP. MX REPLACED THE SMOKE DETECTOR IN THE AFT LAV. O PS CHECKS SATISFACTORY. (M) 2 L 7 2 4F A16WE 1996053000449 19960530 00449 NM 1996 5 30 USAASB96076 1 19960505 A 2130 7207375 RELIEF VALVE BOEING 737 7374B7 1384702 NM AFT CARGO COMPT FAILED A USAA B G A EMER. DESCENT O2 MASK DEPLOYED UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 433US 24555 FLT 665 - SAV - FLIGHT DIVERTED TO SAV DUE TO RAPID DEPRESSURIZATION AT FL 330. MAINTENANCE REPLACED THE RIGHT PRESSURE RELIEF VALVE. OPS CHECK SAT. (M) 2 L 7 2 4F RT A16WE 1996053000450 19960530 00450 NM 1996 5 30 USAASB96077 1 19960504 A 3350 20121 BATTERY CHARGER BOEING 737 737301 1384611 NM CABIN FAILED A USAA K NONE L NO TEST CR CRUISE 1 EA 19 354US 23557 FLT 1847 - DCA - CABIN EMERGENCY LIGHTS COME ON INTERMITTENTLY IN FLIGHT IN THE WHEN ARMED. MAINTENANCE REPLACED THE CH ARGER ASSEMBLY. OPS CHECKED SATISFACTORY. (M) 2 L 7 2 4F RT A16WE 1996053000451 19960530 00451 NM 1996 5 30 USAASB96078 1 19960504 A 5350 65486995 FAIRING BOEING 737 7372B7 1384560 NM LT WING/BODY NOT SEALED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 270AU 22882 FLT NR 2009 - CLT - HARMONIC SURGE FELT IN AIRFRAME DURING CLIMB-OUT AND TO A LESSER EXTENT IN CRUISE. THIS SURGE FELT MORE PRONOUNCED AT 180 TO 250 KNOTS. MX RESEALED WING TO BODY FAIRING LEFT SIDE. INSPECTED FLIGHT CONTROLS, FUSELAGE, AND GEAR. NO DEFECTS NOTED. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F A16WE 1996053000452 19960530 00452 NM 1996 5 30 USAASB96079 1 19960420 A 2612 667201 FIRE DETECTOR BOEING 737 737301 1384611 NM RT ENGINE FAILED A A USAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 346US 23515 FLT 1021 - PHL - ON CLIMB-OUT AT 2500 FEET, RIGHT ENGINE FIRE WARNING LIGHT AND BELL CAME ON. COMPLETED ENGINE FIRE CHE CK LIST. FIRE WARNING LIGHT DID NOT GO OUT UNTIL ENGINE FIRE SHUTOFF HANDLE WAS PULLED. ENGINE SHUTDOWN FOR 13 MINUTES . MX REPLACED THE RIGHT STRUT DETECTOR. CHECKED SATISFACTORY. (M) 2 L 7 2 4F RT A16WE 1996053000453 19960530 00453 1996 5 30 VTZA96165 4 19960425 A 3418 C771065 SUMMING UNIT BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A VTZA O OTHER N FALSE WARNING AP APPROACH 1 EA 27 497UE 904 FLT 6455 - IAD-PHL - DURING APPROACH, THE STALL WARNING HORN AND STICK SHAKER ACTIVATED. AIRCRAFT LANDED AT PHL WITH NO FURTHER INCIDENTS. AIRCRAFT WAS THEN FERRIED TO IAD WHERE IT LANDED WITH NO INCIDENTS. MAINTENANCE REPLACED THE RIGHT SIGNAL SUMMING UNIT. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996053000454 19960530 00454 EU 1996 5 30 VTZA96166 1 19960423 A 3060 B40610 DE-ICE LEAD JETAIR JETSTM JETSTM4101 1500501 EU LT PROP FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 325UE 41063 FLT 6566 - ROC-JFK - ABORTED THE TAKEOFF, DUE TO THE LEFT PROP HEAT FAILING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MX REPLACED THE LEFT PROP DE-ICE LEAD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996053000455 19960530 00455 NE 1996 5 30 VTZA96167 2 19960422 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE LEFT LOW TORQUE A VTZA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 EA 27 306UE 41020 P75035 FLT 6261 - IAD-EWR - ABORTED THE TAKEOFF DUE TO LOW ENGINE TORQUE INDICATION FROM RIGHT ENGINE. AIRCRAFT RETURNED TO GA TE WITH NO FURTHER INCIDENTS. MX PERFORMED ENGINE RUNS, BUT COULD NOT DUPLICATE THE DISCREPANCIES. AIRCRAFT WAS RELEAS ED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 4 T RT A41NM E18NE 1996053000456 19960530 00456 EU 1996 5 30 VTZA96168 1 19960428 A 3150 TO WARNING JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT ACTIVATED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 312UE 41025 FLT NR 6445 - IAD-CHO - ABORTED TAKEOFF DUE TO THE TAKEOFF CONFIGURATION WARNING SYSTEM ACTIVATING. AIRCRAFT RETURNED T O GATE WITH NO FURTHER INCIDENTS. MAINTENANCE PERFORMED INSPECTION AND OPS CHECK OF SYSTEM, BUT COULD FIND NO DEFECTS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996053000457 19960530 00457 NE 1996 5 30 VTZA96169 2 19960427 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE RIGHT LOW TORQUE A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 EA 27 302UE 2666 41013 P76062 DURING TAKEOFF FROM ROC TO IAD, HAD TO ABORT TAKEOFF DUE TO THE RIGHT ENGINE NOT MAKING THE REQUIRED TORQUE. AIRCRAFT R ETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE PERFORMED INSPECTIONS BUT COULD NOT DUPLICATE DISCREPANCY. AIRC RAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 4 T RT A41NM E18NE 1996053000458 19960530 00458 EU 1996 5 30 VTZA96170 1 19960417 A 5246 14153133501 LAV SERVICE DOOR JETAIR JETSTM JETSTM4101 1500501 EU AFT FUSELAGE MISSING A VTZA O OTHER D INFLIGHT SEPARATION IN INSP/MAINT 1 EA 27 316UE 41055 FLT NR 6150 - IAD-EWR - DURING POST FLIGHT WALK AROUND, DISCOVERED THAT THE TOILET SERVICE DOOR WAS MISSING AFTER LANDIN G. MX OPENED DMI NR 17384 IAW CDL 52-40. MX LATER CLEARED DMI NR 17384 ON APR 25, 1996 BY REPLACING THE TOILET SERVICE DOOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996053000459 19960530 00459 EU 1996 5 30 VTZA96171 1 19960430 A 7712 31024762 TQ SIGNAL COND BAG JETSTM JETSTM3201 1500217 EU RT ENG OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J R WARNING INDICATION PARTIAL RPM/PWR LOSS TO TAKEOFF 1 EA 27 493UE 14118 14118 805 FLT 6467 - PHL-IAD - ABORTED THE TAKEOFF DUE TO THE RIGHT ENGINE ONLY MADE 85 PERCENT TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MX RECALIBRATED THE TORQUE SIGNAL CONDITIONER. AIRCRAFT WAS RELEASED AND APPROVED FOR RETU RN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996053000460 19960530 00460 EU 1996 5 30 VTZA96172 1 19960424 A 2611 72111211000 SMOKE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU COMPT FAILED A A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 308UE 41023 FLT NR 6554 - EWR-BOS - DURING CRUISE, DECLARED AN EMERGENCY AND DIVERTED TO BDL DUE TO THE VENTRAL BAGGAGE BAY SMOKE DE TECTOR WARNING LIGHT ILLUMINATED. AIRCRAFT LANDED AT BDL WITH NO FURTHER INCIDENTS AND ALL PASSENGERS SAFE. MAINTENANC E OPENED DMI NR 18652 IAW MEL 26-3. MX LATER CLEARED DMI NR 18652 ON APRIL 4, 1996, BY REPLACING THE VENTRAL BAGGAGE BA Y SMOKE DETECTOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996053000461 19960530 00461 EU 1996 5 30 VTZA96173 1 19960420 A 5230 32518219 SWITCH STRIKER BAG JETSTM JETSTM3201 1500217 EU BAGGAGE POD OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 495UE 818 FLT 6394 - HVN-IAD - ABORTED TAKEOFF, DUE TO THE POD DOOR WARNING LIGHT ILLUMINATING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MX OPENED DMI NR 55380 IAW MEL 52-1. MX LATER CLEARED DMI NR 55380 ON 4-44-96 BY ADJUSTING THE POD DOOR WARNING SWITCH STRIKER. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996053000462 19960530 00462 EU 1996 5 30 VTZA96174 1 19960501 A 3411 PITOT LINE BAG JETSTM JETSTM3101 1500215 EU LEFT CONTAMINATED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 27 473UE 828 FLT NR 6262 - IAD-GSO - ABORTED THE TAKEOFF DUE TO THE CAPTAINS AIRSPEED INDICATOR READING INCORRECTLY ON THE TAKEOFF RO LL. AN EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MX REMOVED THE WATER FROM THE L EFT PITOT LINE. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996053000463 19960530 00463 EU 1996 5 30 VTZA96176 1 19960501 A 7712 TQ SIG COND BAG JETSTM JETSTM3201 1500217 EU LT/RT ENG FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 485UE 901 FLT 6546 - IAD-ROA - ABORTED THE TAKEOFF DUE TO BOTH ENGINES BEING TEMPERATURE LIMITED DURING THE TAKEOFF ROLL. AIRCRAF T RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE COMPLETED THE FOLLOWING ADJUSTMENTS/REPLACEMENTS, LEFT ADJUST ED THE COMPENSATING RESISTOR, REPLACED THE TORQUE SIGNAL CONDITIONER AND REPLACED THE FLOW CONTROL VALVE. RIGHT ADJUSTE D THE COMPENSATING RESISTOR. PERFORMED ENGINE RUNS, ALL CHECKS GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996053000464 19960530 00464 1996 5 30 VTZA96177 4 19960502 A 3414 3994862236 AIRSPEED IND BAG JETSTM JETSTM3201 1500217 EU RT COCKPIT FAILED A VTZA K NONE N FALSE WARNING CR CRUISE 1 EA 27 485UE 901 FLT NR 6446 - IAD-HVN - DURING CRUISE, THE RIGHT AIRSPEED INDICATOR FAILED. AIRCRAFT LANDED AT HVN WITH NO FURTHER INCI DENTS. AIRCRAFT WAS FERRIED TO IAD AND LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE RIGHT AIRSPEE D INDICATOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996053000465 19960530 00465 EU 1996 5 30 VTZA96182 1 19960505 A 2611 72111211000 SMOKE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU BAGGAGE POD FAILED A VTZA O OTHER N FALSE WARNING LD LANDING 1 EA 27 305UE 41019 FLT 6178 - TYS-IAD - AFTER LANDING WHILE TAXIING UP TO THE GATE, DECLARED AN EMERGENCY DUE TO THE POD SMOKE DETECTOR WAR NING LIGHT ILLUMINATING. AIRCRAFT COMPLETED TAXI TO GATE WITH NO FURTHER INCIDENTS. MX REPLACED THE SMOKE DETECTOR. A IRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996053000466 19960530 00466 EU 1996 5 30 VTZA96183 1 19960506 A 2751 TV176004A POTENTIOMETER JETAIR JETSTM JETSTM4101 1500501 EU RT TE FLAP FAILED A A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 313UE 41026 IAD - DAY - FLT 6292 - DURING CLIMB-OUT, RETURNED DUE TO THE FLAP ASYMMETRY WARNING SYSTEM ACTIVATING IN FLIGHT. AIRCRA FT LANDED AT IAD WITH NO FURTHER INCIDENTS. MX REPLACED THE RT FLAP POSITION TRANSDUCER. AIRCRAFT WAS RELEASED AND APP ROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996053000467 19960530 00467 EU 1996 5 30 VTZA96184 1 19960506 A 5210 HANDLE PLUNGER BAG JETSTM JETSTM3201 1500217 EU PAX DOOR LACK OF LUBE A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 497UE 904 FLT 6307 - BOS-JFK - DURING CLIMB-OUT, RETURNED TO BOS DUE TO THE MAIN PASSENGER DOOR WARNING ILLUMINATING IN FLIGHT. A IRCRAFT LANDED AT BOS WITH NO FURTHER INCIDENTS. MX OPENED DMI NR 55102 IAW MEL 52-2. MX LATER CLEARED DMI NR 55102 ON 05-06-96 BY CLEANING AND LUBING THE PASSENGER DOOR HANDLE PLUNGER. (M) 2 L 7 2 4T RT A56EU 1996053000468 19960530 00468 EU 1996 5 30 VTZA96185 1 19960508 A 3060 B40610 DE-ICE LEAD JETAIR JETSTM JETSTM4101 1500501 EU LT PROP FAILED A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 306UE 41020 FLT NR 6356 - BOS-JFK - DURING CLIMB-OUT, RETURNED TO BOS DUE TO THE LEFT PROP HEAT FAILING. AIRCRAFT LANDED AT BOS WIT H NO FURTHER INCIDENTS. MX REPLACED THE LEFT PROP DE-ICE LEAD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVIC E. (M) 2 L 7 2 4T RT A41NM 1996053000469 19960530 00469 1996 5 30 VTZA96186 4 19960509 A 3425 7010680938 FLGHT DIR COMP JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT FAILED A A VTZA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 27 305UE 41019 FLT NR 6520 - CHS-IAD - DURING CLIMB-OUT, RETURNED TO CHS DUE TO SMOKE IN THE COCKPIT DURING CLIMB. AN EMERGENCY WAS DE CLARED AND FLIGHT CREW NOTICED THAT FLIGHT DIRECTOR FLAG AND SYSTEM WAS FAILED. AIRCRAFT LANDED AT CHS WITH NO FURTHER INCIDENTS. AIRCRAFT WAS THEN FERRIED TO IAS WHERE MX REPLACED THE FLIGHT CONTROL COMPUTER. AIRCRAFT WAS RELEASED AND A PPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996053000470 19960530 00470 WP 1996 5 30 WRLA96020 1 19960503 A 2910 AYG70275019 HYD SYSTEM DOUG DC10 DC1030 3023501 WP NR 3 QUANTITY LOW A WRLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 9MMAS 46955 DURING TAXI, CREW RECEIVED 'ELEVATOR NR 3 HYDRAULIC SYSTEM OFF LIGHT'. FLIGHT CREW ELECTED TO RETURN TO GATE. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL NOTED NR 3 HYDRAULIC RESERVOIR, P/N AYG70275019, LOW. SERVICE TO FULL, ELEVATOR 'OFF LIGHT' EXTINGUISH. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A22WE 1996053000471 19960530 00471 SO 1996 5 30 WTAA960086 1 19960426 A 3234 12038594001 GEAR SELECTOR EMB 120 EMB120RT SO COCKPIT MALFUNCTIONED A WTAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 17 276UE 120067 FAT - RIGHT MAIN LANDING GEAR 'B' SYSTEM INTRANSIT LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MX INSPECTED AND VERIFIED PROPER ADJUSTMENT OF BOTH 'A' AND 'B' PROX SENSORS ON RIGHT MAIN LANDING GEAR. 'A' SYSTEM OPERATIONAL CHECK NORMAL. MAINTENANCE DEFERRED 'B' SYSTEM PER MEL 32-60-1. AIRCRAFT RETURNE D TO SERVICE. MX SUBSEQUENTLY CLEARED DEFERRAL WITH THE REPLACEMENT OF THE LANDING GEAR SELECTOR. (M) 2 L 7 2 4T RT A31SO 1996053000472 19960530 00472 SO 1996 5 30 WTAA960090 1 19960424 A 3350 03091022 CONNECTOR EMB 120 EMB120RT SO CABIN LOOSE A WTAA K NONE L NO TEST IN INSP/MAINT 1 WP 17 454UE 120155 FAT - FORWARD CABIN EMERGENCY LIGHTING REPORTED INOPERATIVE DURING GROUND CHECK. MX DEFERRED EMERGENCY LIGHTING SYSTEM PER MEL 33-50-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL BY REPAIRING ELECTRICAL CONNE CTION AT FORWARD FLOOR TRACK LIGHTING AREA. (M) 2 L 7 2 4T RT A31SO 1996053000473 19960530 00473 SO 1996 5 30 WTAA960092 1 19960429 A 3260 922AA2YA6PZ722 PROX SENSOR EMB 120 EMB120RT SO RT MLG MALFUNCTIONED A WTAA O OTHER N FALSE WARNING CL CLIMB 1 WP 17 276UE 120067 SFO - RIGHT MAIN LANDING GEAR 'B' SYSTEM 'GREEN' LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. MAINTENANCE DEFERRED 'B' SYSTEM PER MEL 32-60-1. AIRCRAFT RETURNED TO SERVICE. MX SUBSEQUENTLY CLEARED DEFERRAL WITH THE REPLACEMENT OF TH E RIGHT MAIN LANDING GEAR 'B' INDICATION SYSTEM PROXIMITY SENSOR. (M) 2 L 7 2 4T RT A31SO 1996053000474 19960530 00474 NE 1996 5 30 WTAA960093A 2 19960427 A 7310 3035681 FUEL FILTER EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE FAILED A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 17 120AM 120012 SFO - LEFT ENGINE FUEL FILTER LIGHT ILLUMINATED ON TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MX REPORTED LEFT EN GINE FUEL FILTER LIGHTS PREVIOUSLY DEFERRED PER MEL 73-33-1. MAINTENANCE ENSURED DEFERRAL 'MAINTENANCE PROCEDURES' HAVE BEEN COMPLIED WITH. AIRCRAFT RETURNED TO SERVICE. MX SUBSEQUENTLY CLEARED DEFERRAL WITH THE REPLACEMENT OF THE LEFT E NGINE FUEL FILTERS. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1996053000475 19960530 00475 NE 1996 5 30 WTAA960093B 2 19960427 A 7310 3035729 FUEL FILTER EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE FAILED A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 17 120AM 120012 SFO - LEFT ENGINE FUEL FILTER LIGHT ILLUMINATED ON TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MX REPORTED LEFT EN GINE FUEL FILTER LIGHTS PREVIOUSLY DEFERRED PER MEL 73-33-1. MX ENSURED DEFERRAL 'MX PROCEDURES' HAVE BEEN COMPLIED WIT H. AIRCRAFT RETURNED TO SERVICE. MX SUBSEQUENTLY CLEARED DEFERRAL WITH THE REPLACEMENT OF THE LEFT ENGINE FUEL FILTERS . (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1996053000476 19960530 00476 SO 1996 5 30 WTAA960094 1 19960426 A 3230 922FSZA6NZ735 PROX SENSOR EMB 120 EMB120RT SO NOSE GEAR FAILED A WTAA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 WP 17 278UE 120083 FAT - LANDING GEAR FAILED TO RETRACT AFTER DEPARTURE. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. FAT MX REMOVED AN D REPLACED RIGHT MAIN LANDING GEAR WEIGHT ON WHEELS PROXIMITY SENSOR. LANDING GEAR RETRACTION CHECK NORMAL DURING GEAR SWING. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996053000477 19960530 00477 1996 5 30 WTAA960095 3 19960505 A 6140 AURAL WARNING EMB 120 EMB120RT SO AUTO FEATHER SYS SOUNDED A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 17 275UE 120058 SFO - AUTOFEATHER AURAL WARNING SOUNDED DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MX UNABLE TO DUPLICATE REPORTED DISCREPANCY DURING ENGINE GROUND RUN. PROPELLER AUTOFEATHER SYSTEM OPERATIONALLY CHECKS NORMAL. AIRCRAFT RETU RNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996053000478 19960530 00478 NM 1996 5 30 UPS96405891 1 19960407 A 2612 FIRE DET BOEING 747 747121 1384871 NM APU COMPT INOPERATIVE A IPXA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 681UP 19661 CREW REPORTED, APU FIRE INDICATION DURING CRUISE. A-LOOP OF FIRE DETECT SYS SELECTED 'B', NO FURTHER INDICATIONS. APU WAS OFF DURING THE ENTIRE EVENT. DEF ITEM PER 26-7, MMOC J SHULTZ ASSIGNED CTRL. NR M-108335, PLACARD A-LOOP SYS INOP A ND SELECTED 'B' LOOP. 2 L 7 4 4F A20WE 1996053000480 19960530 00480 WP 1996 5 30 HAL9632 1 19960329 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 EICBH 47796 HNL - FLT 319 - EMERGENCY LIGHTS - OVERHEAD CEILING LIGHTS OUT AT ROWS 2, 4, 7, 14, 18, 23, 26. REPLACED BATTERIES. OP CHECK OK. (X) 2 L 7 2 4F A6WE 1996053000481 19960530 00481 WP 1996 5 30 HAL9633 1 19960329 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 EICBH 47796 HNL - FLT 319 - LEFT AND RIGHT AFT OVERWING EMERGENCY 'EXIT' LIGHTS OUT. REPLACED BATTERIES. OP CHECK OK. (X) 2 L 7 2 4F A6WE 1996053100001 19960531 00001 WP 1996 5 31 AALA960572 1 19960410 A 5320 99365347 ANGLE DOUG DC9 DC982 3022082 WP BS 160-200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 294AA 49306 TUL - FOUND FLOOR SUPPORT ANGLE HAS CORROSION STATION 160 TO 200 AT NUT PLATE HOLES. REPLACED WITH NEW ANGLE PER SRM. ( M) 2 L 7 2 4F A6WE 1996053100003 19960531 00003 NM 1996 5 31 VNAA9600033 1 19960516 A 2435 8160121 STARTER GEN DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT ENGINE DEFECTIVE A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 424JS 3033 CLIMBING THROUGH FL 160, RT GENERATOR FAILED. CREW WAS THEN ADVISED TO RETURN TO FIELD. AIRCRAFT LANDED WITHOUT FURTHE R INCIDENT. REPLACED THE RT STARTER/GENERATOR IAW MM 24-30-00, GROUND CHECKED GOOD. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996060600001 19960606 00001 WP 1996 6 6 9611529751 1 19960412 A 5320 FITTING DOUG DC9 DC941 302207N WP FS 794 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 751NW 47115 DURING H-CHECK, FOUND CORROSION ON THE LONGERON 30 END FITTING AT FS 794. REPLACED FITTING (P/N 5924878-505) PER EA 97- 109495. 2 L 7 2 4F A6WE 1996060600002 19960606 00002 NM 1996 6 6 9611532295 1 19960506 A 5720 WEB BOEING 727 727251 138408H NM LT WING CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 295US 21506 DURING H-CHECK, FOUND A 3 INCH CRACK AND BUCKLING OF THE RIGHT WING AUXILIARY SPAR NR 5 SPOILER SUPPORT WEB. REPAIRED W EB (P/N 65-16216-150) PER EA 22-105281. 2 L 7 3 4F A3WE 1996060600003 19960606 00003 WP 1996 6 6 9611541145 1 19960507 A 5730 SKIN DOUG DC10 DC1040 3023508 WP WS 611 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 145US 46754 DURING T-CHECK, FOUND A CRACK IN THE LEFT WING LEADING EDGE SKIN AT THE FUELING ACCESS CUT-OUT XOS 611. REPAIRED SKIN ( P/N ARB 2887-501) PER EA 11-105388. 2 L 7 3 4F A22WE 1996060600004 19960606 00004 NM 1996 6 6 9611555524 1 19960507 A 5320 CHORD BOEING 757 757251 1384970 NM FS 1380-1440 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 524US 23618 DURING P-CHECK, FOUND CORROSION IN THE AFT CARGO DOOR LOWER SILL INNER CHORD FS 1380 - FS 1440. REPAIRED CHORD (P/N 146 N8522-52) PER EA 55-102107. 2 L 7 2 4F RT A2NM 1996060600005 19960606 00005 WP 1996 6 6 9611561145 1 19960508 A 5320 JAMB DOUG DC10 DC1040 3023508 WP 3R DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 145US 46754 DURING T-CHECK, FOUND A CRACK IN THE 3R LOWER FORWARD DOOR JAMB WEB. REPAIRED WEB (P/N AEA 0115-2) PER EA 11-105389. 2 L 7 3 4F A22WE 1996060600006 19960606 00006 WP 1996 6 6 9611571145 1 19960508 A 5330 SKIN DOUG DC10 DC1040 3023508 WP FS 1343-1368 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 145US 46754 DURING T-CHECK, FOUND CORROSION ON THE EXTERIOR SKIN FS 1343 - FS 1368, LBL 51 - RBL 51, AT THE POPPET DRAIN PLUGS. REP AIRED SKIN (P/N AYB 7065/NYB 6208) PER EA 11-105372. 2 L 7 3 4F A22WE 1996060600007 19960606 00007 WP 1996 6 6 9611581145 1 19960509 A 5313 LONGERON DOUG DC10 DC1040 3023508 WP FS 1504 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 145US 46754 DURING T-CHECK, FOUND CORROSION ON EXTERNAL LONGERON 31R AT FS 1504. REPAIRED LONGERON (P/N AEA 7136-2) PER EA 11-10539 1. 2 L 7 3 4F A22WE 1996060600008 19960606 00008 WP 1996 6 6 9611591145 1 19960511 A 5347 TRACK DOUG DC10 DC1040 3023508 WP FS 1521-1541 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 145US 46754 DURING T-CHECK, FOUND CORROSION ON THE LEFT OUTBOARD SEAT TRACK FROM FS 1521 - FS 1541, LBL 107. REPAIRED TRACK PER EA 11-099327. 2 L 7 3 4F A22WE 1996060600009 19960606 00009 NM 1996 6 6 9611602295 1 19960513 A 5315 FLOOR BEAM BOEING 727 727251 138408H NM FS 760 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 295US 21506 DURING H-CHECK, FOUND TWO CRACKS IN THE BS 760 FLOOR BEAM WEB AT RBL 60 AND RBL 70. REPAIRED WEB (P/N 65-16325) PER EA 22-102151. 2 L 7 3 4F A3WE 1996060600010 19960606 00010 WP 1996 6 6 9611611145 1 19960513 A 5347 SEAT TRACK DOUG DC10 DC1040 3023508 WP FS 1990-2005 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 145US 46754 DURING T-CHECK, FOUND CORROSION ON THE RIGHT OUTBOARD SEAT TRACK FROM FS 1990 - FS 2005, RBL 67. REPAIRED TRACK (P/N NF A 6222-9) PER EA 11-104266. 2 L 7 3 4F A22WE 1996060600011 19960606 00011 NM 1996 6 6 9611622295 1 19960515 A 5315 FLOOR BEAM BOEING 727 727251 138408H NM FS 1110 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 295US 21506 DURING H-CHECK, FOUND CORROSION ON THE BS 1110 FLOOR BEAM CHORD FROM LBL 70 - RBL 19. REPAIRED CHORD (P/N 65-20837-24) PER EA 22-105312. 2 L 7 3 4F A3WE 1996060600012 19960606 00012 WP 1996 6 6 9611639851 1 19960515 A 5313 LONGERON DOUG DC9 DC951 3022051 WP FS 851 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 760NC 47708 DURING H-CHECK, FOUND CORROSION ON LONGERON 30 AT FS 851. REPAIRED LONGERON (P/N 5924878-503) PER EA 98-108996. 2 L 7 2 4F A6WE 1996060600013 19960606 00013 WP 1996 6 6 9611649851 1 19960516 A 5320 SUPPORT DOUG DC9 DC951 3022051 WP FS 237-264 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 760NC 47708 DURING H-CHECK, FOUND CORROSION ON THE CENTER LINE FLOOR SUPPORT FROM FS 237 - FS 264. REPAIRED SUPPORT (P/N 5910760-11 ) PER EA 98-109085. 2 L 7 2 4F A6WE 1996060600014 19960606 00014 WP 1996 6 6 9611659876 1 19960519 A 5210 ANGLE DOUG DC9 DC951 3022051 WP BS 236.875 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 785NC 48110 DURING H-CHECK, FOUND A CRACK IN THE AFT CABIN DOOR NR 3 BEAM RIGHT ATTACH ANGLE STA Z36.875. REPAIRED ANGLE (P/N 99155 65-29) PER EA 98-109053. 2 L 7 2 4F A6WE 1996060600015 19960606 00015 WP 1996 6 6 9611669905 1 19960520 A 5230 FITTING DOUG DC9 DC931 3022065 WP CARGO DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 955N 47160 DURING H-CHECK, FOUND A CRACK IN THE AFT CARGO DOOR UPPER BEAM END FITTING. REPLACED FITTING. 2 L 7 2 4F A6WE 1996060600016 19960606 00016 WP 1996 6 6 9611679973 1 19960520 A 5312 BULKHEAD T CAP DOUG DC9 DC931 3022065 WP FS 604 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9337 47346 DURING M-CHECK, FOUND CORROSION IN THE FS 604 BULKHEAD T-CAP BETWEEN LONGERONS 29R - 30. REPAIRED T-CAP (P/N 5914865-29 ) PER EA 99-109084. 2 L 7 2 4F A6WE 1996060600017 19960606 00017 WP 1996 6 6 9611689965 1 19960522 A 5320 FITTING DOUG DC9 DC931 3022065 WP FS 598-617 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 911RW 47149 DURING M-CHECK, FOUND CORROSION ON THE RIGHT SIDE FS 598 - FS 617 FRAME TO FUEL TANK FITTING. REPLACED FITTING PER SRM 51-30-4. 2 L 7 2 4F A6WE 1996060600018 19960606 00018 WP 1996 6 6 9611699965 1 19960522 A 5320 FITTING DOUG DC9 DC931 3022065 WP FS 168 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 911RW 47149 DURING M-CHECK, FOUND CORROSION AT THE FS 168 FRAME TO LONGERON 18R DOOR SUPPORT FITTING. REPLACED FITTING PER SRM 51-3 0-4. 2 L 7 2 4F A6WE 1996060600019 19960606 00019 WP 1996 6 6 9611709905 1 19960523 A 5320 FITTING DOUG DC9 DC931 3022065 WP FS 756 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 955N 47160 DURING H-CHECK, FOUND CORROSION ON THE RIGHT MAIN LANDING GEAR WHEELWELL INBOARD AND OUTBOARD FITTINGS FS 756 AT APPROXI MATELY LONGERON 29R. REPLACED FITTINGS PER SRM 51-30 AND DWG 5911418. 2 L 7 2 4F A6WE 1996060600020 19960606 00020 WP 1996 6 6 9611719905 1 19960523 A 5320 FITTING DOUG DC9 DC931 3022065 WP FS 756 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 955N 47160 DURING H-CHECK, FOUND CORROSION IN THE LEFT MAIN LANDING GEAR WHEELWELL INBOARD AND OUTBOARD FITTINGS FS 756. REPLACED FITTINGS PER SRM 51-30 AND DWG 5911418. 2 L 7 2 4F A6WE 1996060600021 19960606 00021 NM 1996 6 6 9611726628 1 19960523 A 5744 FITTING BOEING 747 747251B 1384892 NM RT TE FLAP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 628US 22389 DURING P-CHECK, FOUND CORROSION IN THE RIGHT WING TRAILING EDGE FLAP NR 6 CARRIAGE FITTING BEARING BORE. REPLACED FITTI NG (P/N 65B 08411-6). 2 L 7 4 4F A20WE 1996060600022 19960606 00022 WP 1996 6 6 9611739855 1 19960525 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 764NC 47717 DURING LINE CHECK, FOUND RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996060600023 19960606 00023 WP 1996 6 6 9611749752 1 19960528 A 3350 BATTERY PACK DOUG DC9 DC941 302207N WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 752NW 47116 DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTING FLICKERING ON DIMLY. ALSO, REPORTED AS FLICKERING ON AND OFF IN -FLIGHT. REPLACED BATTERY PACK AND RECYCLED SYSTEM. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996060600024 19960606 00024 WP 1996 6 6 9611751211 1 19960503 A 3350 EMSE299 BATTERY DOUG DC10 DC1030 3023501 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 211NW 46868 DURING LINE INSPECTION, FOUND THE EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE REPLACED THE MID-CABIN BATTERY. 2 L 7 3 4F A22WE 1996060600025 19960606 00025 WP 1996 6 6 9611761225 1 19960510 A 3350 EMSE299 BATTERY PACK DOUG DC10 DC1030 3023501 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 225NW 46582 DURING LINE INSPECTION, FOUND THE EMERGENCY LIGHT INOPERATIVE AT DOOR 1L AND 1R AND THE FIRST CLASS FLOOR LIGHTING INOPE RATIVE. MAINTENANCE REPLACED THE BATTERY PACKS AND TIGHTENED WIRES. 2 L 7 3 4F A22WE 1996060600026 19960606 00026 WP 1996 6 6 9611771211 1 19960527 A 3350 POWER SUPPLY DOUG DC10 DC1030 3023501 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 211NW 46868 DURING LINE INSPECTION, ZONE B, FOUND FLOOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AN D RETURNED TO SERVICE. 2 L 7 3 4F A22WE 1996060600027 19960606 00027 WP 1996 6 6 9611781225 1 19960523 A 3350 EMBS1392 POWER SUPPLY DOUG DC10 DC1030 3023501 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 225NW 46582 DURING LINE INSPECTION, FOUND THE EMERGENCY LIGHT AND STANDBY POWER CIRCUIT BREAKERS TRIPPED. MAINTENANCE REPLACED THE FORWARD BATTERY POWER SUPPLY. 2 L 7 3 4F A22WE 1996060600029 19960606 00029 WP 1996 6 6 9611829944 1 19960529 A 2120 AIR DISTR DOUG DC9 DC931 3022065 WP CABIN SMOKE A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 1309T 47316 DURING INITIAL CLIMB-OUT, FLIGHT ATTENDANT REPORTED SMOKE SMELL IN AFT CABIN. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED COCKPIT, GALLEY, LAVATORIES, AFT ACCESSORY COMPARTMENT, E/E COMPARTMENT, FORWARD ACCES SORY COMPARTMENT, AND BAGGAGE BINS. NO SMELL OF SMOKE OR EVIDENCE OF FIRE WAS DETECTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996060600030 19960606 00030 EU 1996 6 6 9611833201 1 19960529 A 3260 848401 PROX SENSOR AIRBUS 320 A320211 3930320 EU NLG WW FAILED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 301US 31 DURING CLIMB-OUT AFTER LANDING GEAR RETRACTION, RECEIVED L/G GEAR NOT UPLOCKED MESSAGE. CYCLED LANDING GEAR HANDLE AND ALL INDICATIONS NORMAL. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NOSE LANDI NG GEAR PROXIMITY SENSOR 25GA. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996060600031 19960606 00031 WP 1996 6 6 9611849993 1 19960528 A 3260 UPLIMIT SW DOUG DC9 DC931 3022065 WP NLG MALFUNCTIONED A NWAA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 01 8986E 47402 NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE ON APPROACH INTO MSP. COCKPIT OPERATING MANUAL PROCEDURES WERE PERFORM ED AND AIRCRAFT LANDED WITHOUT INCIDENT. NOTE: EMERGENCY EQUIPMENT WAS CALLED OUT ON STANDBY AS A PRECAUTION. MAINTEN ANCE CLEANED TERMINAL STRIP S3-49 AND REPLACED NOSE GEAR UPLIMIT SWITCH S1-91 AND LANDING GEAR LEVER RELAY R2-28. OPERA TIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996060600032 19960606 00032 WP 1996 6 6 9611859940 1 19960528 A 2520 INSULATION DOUG DC9 DC932 3022066 WP CABIN OUT OF POSITION A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 3322L 47031 AIRCRAFT FAILED TO PRESSURIZE AFTER TAKEOFF. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LOO SE INSULATION BLANKET STUCK IN OUTFLOW VALVE. REMOVED INSULATION. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERV ICE. 2 L 7 2 4F A6WE 1996060600033 19960606 00033 WP 1996 6 6 9611869990 1 19960528 A 3260 UNSAFE LIGHT DOUG DC9 DC931 3022065 WP NLG ILLUMINATED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 8950E 47186 NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT . MAINTENANCE PERFORMED SEVERAL GEAR SWINGS. DISCREPANCY COULD NOT BE DUPLICATED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996060600034 19960606 00034 NM 1996 6 6 CALA9600650 1 19960529 A 2722 ACTUATOR BOEING 727 727224 1384076 NM RUDDER LEAKING A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SW 09 79746 22449 AIRCRAFT LOST ALL B-SYSTEM HYDRAULIC QUANTITY AND PRESSURE AFTER TAKEOFF FROM IAH. THE HYDRAULIC LOSS CHECKLIST WAS COM PLIED WITH AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE UPPER RUDDER AC TUATOR SOLENOID O-RING PLATE LEAKING. THE O-RING PLATE WAS REMOVED AND REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD . 2 L 7 3 4F A3WE 1996060600035 19960606 00035 WP 1996 6 6 CALA9600651 1 19960411 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 1997 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68046 47800 INSPECTION FOUND CORROSION ON LOWER FRAME CHORD AT STA 1997, BETWEEN STRINGERS 51R AND 51L. THE AREA WAS REPAIRED IAW E CRA 5330-02386. 2 L 7 3 4F A22WE 1996060600036 19960606 00036 WP 1996 6 6 CALA9600652 1 19960423 A 5320 ADA70269 SHEAR CLIP DOUG DC10 DC1010 3022110 WP BS 1099 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68042 46901 INSPECTION FOUND SHEAR CLIPS CORRODED AT STA 1099, LONGERON 47L TO 49L AND LONGERON 51L TO 52L. REPAIR WAS PERFORMED IA W ECRA 5310-03268. 2 L 7 3 4F A22WE 1996060600037 19960606 00037 WP 1996 6 6 CALA9600653 1 19960423 A 5311 FRAME CAP DOUG DC10 DC1010 3022110 WP BS 1701 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68042 46901 INSPECTION FOUND THE AFT INTERMEDIATE FUSELAGE FRAME CAP CORRODED AT STA 1701. THE AREA WAS REPAIRED IAW ECRA 5310-0326 5. 2 L 7 3 4F A22WE 1996060600038 19960606 00038 WP 1996 6 6 CALA9600654 1 19960423 A 5720 BEAM DOUG DC10 DC1010 3022110 WP LT WING TE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68042 46901 INSPECTION FOUND THE LT WING UPPER CAP TRAILING EDGE BEAM CORRODED. THE BEAM WAS REPAIRED IAW ECRA 5720-01518. 2 L 7 3 4F A22WE 1996060600039 19960606 00039 WP 1996 6 6 CALA9600655 1 19960423 A 5320 DOUBLER DOUG DC10 DC1010 3022110 WP BS 959-979 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68042 46901 INSPECTION FOUND THE FORWARD SKIN DOUBLER AT STA 959 TO 979, LONGERONS 47R AND 46R CORRODED. THE SKIN DOUBLER WAS REPAI RED IAW ECRA 5330-02397. 2 L 7 3 4F A22WE 1996060600040 19960606 00040 WP 1996 6 6 CALA9600656 1 19960424 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 879-1019 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68042 46901 INSPECTION FOUND THE FORWARD INTERMEDIATE FUSELAGE FRAME CAP CORRODED AT STA 899, LONGERON 51L AND 50R; STA 959, LONGERO N S50L AND 50R; AND STA 1019, LONGERON 49L AND 51L. REPAIRS WERE PERFORMED IAW ECRA 5310-03264. 2 L 7 3 4F A22WE 1996060600041 19960606 00041 WP 1996 6 6 CALA9600657 1 19960511 A 3350 EMBS1392 CHARGER DOUG DC10 DC1010 3022110 WP CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 68042 46901 THE EMERGENCY LIGHT TEST IN COCKPIT FAILED TO TEST DURING C-CHECK. THE FAULT ISOLATION PANEL INDICATED MID-POWER PACK F AILURE. THE EMERGENCY LIGHT CHARGER WAS REMOVED AND REPLACED AND EMERGENCY LIGHT TEST CHECKED GOOD. 2 L 7 3 4F A22WE 1996060600042 19960606 00042 NM 1996 6 6 CALA9600658 1 19960516 A 5311 FRAME BOEING 727 727224 1384076 NM BS 1352.46 WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 69736 INSPECTION FOUND WORN AREAS IN FRAME OUTER CHORD ON RT SIDE OF B.S. 1352.46. THE FRAME CHORD WAS REPAIRED IAW ECRA 5310 -03270 AND SRM 51-10-2. 2 L 7 3 4F A3WE 1996060600043 19960606 00043 WP 1996 6 6 CALA9600659 1 19960529 A 2150 CONTROL VALVE DOUG DC9 DC982 3022082 WP RT PACK STUCK OPEN A CALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 09 15820 49480 STRONG FUMES WERE REPORTED IN THE CABIN AFTER TAKEOFF FROM IAH. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOU T INCIDENT. MAINTENANCE PERFORMED A BURN-OUT PROCEDURE PER MM 21-20-02, PARAGRAPH 7C. THE RT CABIN TEMP CONTROL VALVE WAS FOUND STUCK IN THE FULL HOT POSITION. THE VALVE WAS REMOVED AND REPLACED. THE COALESCER BAGS WERE ALSO REPLACED. T HE AIR CONDITIONING SYSTEM CHECKED NORMAL WITH NO FUMES OBSERVED. 2 L 7 2 4F A6WE 1996060600044 19960606 00044 NM 1996 6 6 CALA9600660 1 19960512 A 5330 SKIN BOEING 737 737291 138448W NM BS 827-887 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15255 21069 INSPECTION FOUND FUSELAGE SKIN DENTED AND CREASED FROM STA 827 TO 887 BETWEEN STRINGERS 16L AND 17L. THE DAMAGED AREA W AS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 53-30-3. 2 L 7 2 4F A16WE 1996060600045 19960606 00045 NM 1996 6 6 CALA9600661 1 19960511 A 5512 SKIN BOEING 737 737291 138448W NM HORIZ STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15255 21069 INSPECTION FOUND A 1 INCH CRACK IN RT HORIZONTAL UPPER SKIN. THE CRACK WAS LOCATED APPROXIMATELY 15 INCHES OUTBOARD FRO M FUSELAGE. THE CRACKED AREA WAS REMOVED AND A FIBERGLASS OVERLAY REPAIR WAS INSTALLED IAW SRM 51-40-9 AND 51-20-3. 2 L 7 2 4F A16WE 1996060600046 19960606 00046 NM 1996 6 6 CALA9600662 1 19960509 A 5330 SKIN BOEING 737 737291 138448W NM BS 867 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15255 21069 INSPECTION FOUND FUSELAGE SKIN DENTED AFT OF C-2 DOOR AT B.S. 867 BETWEEN LONGERONS 22R AND 23R. THE DENTED AREA WAS CU T OUT IAW SRM 53-30-3. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 AND 51-30-2. 2 L 7 2 4F A16WE 1996060600047 19960606 00047 WP 1996 6 6 CALA9600663 1 19960510 A 5712 RIB DOUG DC9 DC982 3022082 WP WS 276 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18833 49493 INSPECTION FOUND A .50 INCH CRACK AT LOWER RADIUS OF LEADING EDGE RIB OF LT WING AT STA XRS 276. A DOUBLER REPAIR WAS I NSTALLED IAW ECRA 5720-01521. 2 L 7 2 4F A6WE 1996060600048 19960606 00048 SO 1996 6 6 COMA9610152 1 19960517 A 5522 12002458004 SKIN EMB 120 EMB120RT SO RT ELEVATOR LIGHTNING STRIKE A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 161CA 17482 120143 DURING A LIGHTNING STRIKE INSPECTION FOUND RIGHT ELEVATOR TRAILING EDGE TO HAVE DAMAGE AT THE OUTBOARD TIP. CUT OUT THE DAMAGED AREA OF THE RIGHT ELEVATOR TRAILING EDGE. FABRICATED FILLERS AND DOUBLERS AND INSTALLED IN SERVICEABLE CONDITI ON. ALL WORK DONE I/A/W EMB 120 SRM CHAP 55-20-01 PG 205-206. 2 L 7 2 4T RT A31SO 1996060600049 19960606 00049 SO 1996 6 6 COMA9610153 1 19960524 A 5330 12019230001 SKIN EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 159A 16419 120159 SEVERE CORROSION WAS FOUND DURING INSPECTION ON THE LOWER FUSELAGE SKIN AT FRAME 22 BETWEEN STRINGERS 21R AND 20R. THE CORROSION IS WHERE THE SKIN CONTACTS THE TITANIUM REINFORCING STRAP P/N 120-22409-001. THE DAMAGED AREA WAS REMOVED AND A REPAIR INSTALLED PER EMB-120 SRM 53-00-01 FIGURE 202 SHEET 5. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 1996060600050 19960606 00050 SO 1996 6 6 COMA9610154 1 19960527 A 3231 12012347001 LATCH EMB 120 EMB120RT SO RT MLG DOOR BROKEN A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 247CA 120225 RIGHT MLG OUTBOARD GEAR DOOR WILL NOT CLOSE. REPLACED BROKEN DOOR LATCH ASSY. 2 L 7 2 4T RT A31SO 1996060600051 19960606 00051 1996 6 6 COMA9610155 4 19960524 A 3445 6226190204 TCAS EMB 120 EMB120RT SO AVIONICS MALFUNCTION A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 244CA 12819 118 120217 PILOT'S RED HEADING FLAG LIGHT ON ALONG WITH FAILURE OF TCAS. REPLACED THE AHC-85. PART TOTAL CYCLES, 13,044. 2 L 7 2 4T RT A31SO 1996060600052 19960606 00052 SO 1996 6 6 COMA9610156 1 19960526 A 2751 WARNING SYST EMB 120 EMB120RT SO TE FLAPS ACTIVATED A COMA K NONE N FALSE WARNING AP APPROACH 1 SO 01 179CA 120179 FLAP CONTROL FAULT WARNING WHEN SELECTED TO 25 DEGREES. RESET FLAP SYSTEM - NO FAULT CODES FOUND IN MEMORY. ACFT RETUR NED TO SERVICE. 2 L 7 2 4T RT A31SO 1996060600053 19960606 00053 SW 1996 6 6 COMA9620007 1 19960527 A 3260 2782186057OH INDICATOR SWRNGN SA227 SA227AC 8780603 SW INST PANEL MALFUNCTION A COMA K NONE O OTHER AP APPROACH 1 SO 01 703CA 4587 816 AC703 RIGHT MAIN LANDING GEAR DID NOT INDICATE DOWN AND LOCK UNTIL GEAR WAS CYCLED 3 TIMES. REPLACED THE LANDING GEAR INDICAT OR. PART TOTAL CYCLES, 5,961. 2 L 7 2 4T RT A8SW 1996060600054 19960606 00054 EU 1996 6 6 COMA9630116 1 19960529 A 2916 3800069101 RESERVOIR SAAB SF340 SF340A 7850100 EU NLG LEAKING A COMA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 146CA 17548 340A146 HYDRAULIC FLUID DRIPPING FROM NOSE LANDING GEAR AREA. REPLACED LEAKING HYDRAULIC SYSTEM RESERVOIR. 2 L 7 2 4T RT A52EU 1996060600055 19960606 00055 EA 1996 6 6 COMA9660096 1 19960529 A 3231 NAS620434D BOLT 600861113 CNDAIR CL600 CL6002B19 EA NLG CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 940CA 4341 7048 AIRCRAFT TAXIED TO HANGAR FOR SCHEDULED MAINTENANCE. UPON ARRIVAL MECHANICS NOTICED THE NOSE GEAR DOORS HANGING SLIGHTL Y OPEN WHEN AIRCRAFT WAS POWERED DOWN. FURTHER INVESTIGATION FOUND THE THROUGH-BOLT CORRODED FOR THE NOSE GEAR FORWARD DOOR UPLOCK ROLLER LEVER ASSEMBLY. THE CORROSION WAS NOT ALLOWING THE LEVER TO ROTATE FREELY CAUSING THE ROLLER NOT TO PROPERLY ENGAGE IN THE CAM. THE LEVER AND MOUNT BRACKET WERE CLEANED AND LUBED, THE BOLT WAS REPLACED. AIRCRAFT RETURN ED TO SERVICE. IPC REF: 32-22-00, FIG. 3, SHEET 1, ITEMS NR 310 AND NR 345. 2 L 7 2 4F RT A21EA 1996060600056 19960606 00056 EA 1996 6 6 COMA9660097 1 19960527 A 3231 LINKAGE CNDAIR CL600 CL6002B19 EA NLG DOOR OUT OF ADJUST A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 917CA 7017 NOSE LANDING GEAR DOORS WILL NOT CLOSE WHEN SELECTED TO FIT/NORMAL POSITION. LUBRICATED AND ADJUSTED NOSE LANDING GEAR DOOR LINKAGE. ACFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1996060600057 19960606 00057 EA 1996 6 6 COMA9660098 1 19960528 A 2750 855D1005 BPSU CNDAIR CL600 CL6002B19 EA LT/RT TE FLAPS DEFECTIVE A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 929CA 5788 3812 7035 FLAPS FAILED AT 20 DEGREES DURING RETRACTION. REPLACED THE LT AND RT BRAKE AND POSITON SENSOR UNITS. PART TOTAL CYCLES , 5,181. 2 L 7 2 4F RT A21EA 1996060600058 19960606 00058 NM 1996 6 6 DL72S961311 1 19960522 A 5744 FITTING BOEING 727 727232 1384082 NM FLAP ATTACH FTG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 522DA 21582 AT MID VISIT, THE RT MLG FLAP TRACK ATTACH FITTING WAS FOUND CORRODED. THE FITTING WAS REMOVED, HOLES MACHINED TO REMOV E CORR, BUSHINGS INSTALLED AND FITTING REINSTALLED PER 57-42-0 AND 27-51-31. 2 L 7 3 4F A3WE 1996060600059 19960606 00059 NM 1996 6 6 DL73E961285 1 19960517 A 5330 6545768237 SKIN BOEING 737 737247 138448D NM BS 370-385 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 380DL 23607 FUSELAGE SKIN AT STRINGER 23R FROM STA 370 TO 385 WAS DAMAGED BY A BAG CART. CUT OUT 15 BY 6 IN SKIN AND BONDED DOUBLER . SKIN IS FABRICATED FROM 0.036 CLAD 2024-T3 AND IS BONDED TO A 0.036 CLAD 2024-T3 WAFFLE DOUBLER BENEATH STRINGERS AND FRAMES. IN ADDITION THERE ARE SEVERAL SMALL PILOT HOLES AFT OF THE CUTOUT WHICH WILL NOT BE USED IN THE REPAIR DOUBLER . IN ADDITION, STRINGER 23R HAD A SMALL NICK ON THE INBOARD LWR CORNER AT APPROX STA 385. 2 L 7 2 4F A16WE 1996060600060 19960606 00060 NM 1996 6 6 DL73E961288 1 19960509 A 5312 BULKHEAD WEB BOEING 737 737247 138448D NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 245WA 23519 DURING ACOMPLISHMENT OF SI 3-69482-12, TWO CRACKS WERE DISCOVERED ON THE FWD FACE OF THE STA 178 BULKHEAD WEB. THE FIRS T CRACK IS LOCATED UNDER THE RBL 5.7 VERTICAL STRAP AT APPROX WL 200 AND THE SECOND IS LOCATED UNDER THE LBL 5.7 VERTICA L STRAP AT APPROX WL 198. THE WEB IS MANUFACTURED FROM 0.040 2024-T3 CLAD. 2 L 7 2 4F A16WE 1996060600061 19960606 00061 NM 1996 6 6 DL73S961275 1 19960526 A 5755 SEAL BOEING 737 737232 1384475 NM NR 2 SPOILER MISSING A DALA K NONE D INFLIGHT SEPARATION DE DESCENT 1 SO 27 307DL 23079 SEVERAL PAX REPORTED SOMETHING COMING OFF LT WING WHEN SPOILERS WERE DEPLOYED DURING DESCENT. FOUND NR 2 SPOILER OTBD S EAL MISSING. REPLACED SEAL. 2 L 7 2 4F RT A16WE 1996060600062 19960606 00062 NM 1996 6 6 DL757961292 1 19960517 A 5414 SKIN BOEING 757 757232 1384965 NM NR 1 ENG STRUT FATIGUE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 628DL 22918 THE NR 1 ENGINE NACELLE STRUT SKIN WAS FOUND CRACKED IN THE UPPER FWD CORNER OF 442 AT ACCESS PANEL. THE CRACK LENGTH M EASURED 1 INCH LONG. THE STRUT SKIN IN THIS LOCATION IS THREE LAYERS OF 0.080 CLAD 2024-T3 WHICH ARE STRUCTURALLY BONDE D. AT LETTER CHECK, MTC REPORTS CRACK HAS PROGRESSED PAST THE SECOND STOP DRILL AND IS OUTSIDE THE ALLOWABLE CRACK REGI ON OF FIG 2. ALSO, MTC REPORTS AN ADDITIONAL CRACK EMANATING FROM THE ACCESS HOLE IMMEDIATELY AFT THE 443 AT ACCESS PAN EL, SEE FIG 3 FOR LOCATION AND LENGTHS OF THE 2 CRACKS. 2 L 7 2 4F RT A2NM 1996060600063 19960606 00063 WP 1996 6 6 DLL10961231 1 19960516 A 5711 1505330 SPAR WEB LKHEED 1011 10113851 5265010 WP BS1043/1103/1163 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 722DA 193C1147 THE CENTER WING INTERMEDIATE SPARS AT FS 1043M RBL 116 AND FS 1103M LBL 116 HAD CRACKS IN WEB. ALSO, FS 1103 HAD MULTIP LE CRACKS THROUGH UPPER FASTENER HOLES. REV A ADDED ADDITIONAL CRACK LOCATIONS, REVISED DIRECTIONS AND DRAWINGS TO ACCO MODATE THIS, REV B ADDED FAA APROVAL. 2 L 7 3 4F A23WE 1996060600064 19960606 00064 WP 1996 6 6 DLL10961233 1 19960513 A 5712 RIB CAP LKHEED 1011 10113851 5265010 WP LT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 722DA 193C1147 A 1.0 CRACK WAS FOUND IN THE IWS 555 UPPER CAP BETWEEN STR 19 AND 20. A REPAIR ANGLE WAS SPLICED IN. REV A CHANGES THE FWD CUT LOCATION, REV B REMOVED FWD CUT LOCATION AND EXTENDS SPLICE FROM STR 13 TO THE FWD END OF RIB CAP, REV C CHANGES TIME-LIMIT INSTRUCTINS TO ADD REPAIR FOR MISDRILLED HOLE, REV D ADDS FAA APPROVAL. 2 L 7 3 4F A23WE 1996060600065 19960606 00065 WP 1996 6 6 DLL10961252 1 19960521 A 2560 2462 PANEL LKHEED 1011 10113851 5265010 WP LWR GALLEY INOPERATIVE A DALA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 27 723DA 193C1150 WHILE PERFORMING EMERGENCY EVACUATION TEST PER OPERATION 68111 DURING B-LETTER CHECK, LOWER GALLEY EVAC SIGNAL PANEL FAI LED TO SOUND OR LIGHT. REPLACED PANEL, CHECKS NORMAL. 2 L 7 3 4F A23WE 1996060600066 19960606 00066 WP 1996 6 6 DLL10961262 1 19960523 A 3260 PROX SWITCH LKHEED 1011 10113851 5265010 WP RT MLG DOOR OUT OF ADJUST A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 716DA 193C1095 RIGHT GEAR DOOR LIGHT REMAINED ON AFTER GEAR RETRACTED. FOUND RT GEAR DOOR PROX SW OUT OF ADJUSTMENT. 2 L 7 3 4F A23WE 1996060600067 19960606 00067 WP 1996 6 6 DLL10961263 1 19960522 A 3230 RUN AROUND VLV LKHEED 1011 10113851 5265010 WP RT MLG WW WORN A DALA O OTHER E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 27 716DA 193C1095 AFTER GEAR RETRACTION RT GEAR OR RT DOOR IN TRANS LIGHTS STAYED ON, FELT SLIGHT SHAKING OF A/C AS IF GEAR DOOR OR GEAR H ANGING. CYCLED GEAR DOWN 3 GREENS AND BACK UP WITH LIGHTS COMING BACK ON. WHILE PREPARING TO LAND IN ATL LIGHTS WENT O UT, CONTINUED FLIGHT TO BOS. REPLACED RIGHT MAIN GEAR RUN AROUND VALVE REF FIM 32-30-00 AND MM 32-33-05 LK CK OK, CYCLE D DOOR OPS NORM. ALSO, A/C WENT OUT ON A TEST FLIGHT 9981 AND LANDING GEAR WAS OPS CKD CREW REPORTED ALL OPERATION CHEC KED NORM. 2 L 7 3 4F A23WE 1996060600068 19960606 00068 WP 1996 6 6 DLL10961276 1 19960526 A 2560 MEGAPHONE LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 714DA 193C1090 MEGAPHONE IN FIRST CLASS INOP. 2 L 7 3 4F A23WE 1996060600069 19960606 00069 WP 1996 6 6 DLL10961280 1 19960527 A 3350 10706LD103 SWITCH LKHEED 1011 10113851 5265010 WP CABIN STUCK A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 723DA 193C1150 DURING CK OUT, EMERG LIGHTS WOULD NOT ARM. FOUND LOWER GALLEY EMERG LIGHT SWITCH STUCK. CLEANED AND CYCLED SWITCH, CHE CKS GOOD. 2 L 7 3 4F A23WE 1996060600070 19960606 00070 WP 1996 6 6 DLL13961232 1 19960517 A 5330 SKIN LKHEED 1011 10113851 5265010 WP BS 489-509 DENTED A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 789DL 193A1142 JETWAY HIT A/C CAUSING SKIN DAMAGE 1.5 BY 8 BETWEEN FS 489 AND 509 AND STR 15 AND 15. THE DAMAGE WAS CUT OUT AND A FILL ER WAS INSTALLED AND REINFORCED. REV A REVISED DRAWING TO ACCURATELY REFLECT FILLER CONFIG REV B REVISED REPAIR DESCRIP TION AND DWG TO ACCURATELY REFLECT EXTERNAL SKIN THICKNESS AND REPAIR INSTALLATION. REV C ADDED FAA APPROVAL. 2 L 7 3 4F A23WE 1996060600071 19960606 00071 NM 1996 6 6 DLM11961261 1 19960522 A 3350 BULB DOUG MD11 MD11 3023602 NM CABIN LOOSE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 801DE 48472 EMERGENCY TRACK LIGHTS 43A AND 51G ARE INOP. FOUND BULBS LOOSE. 2 L 7 3 4F RT A22WE 1996060600072 19960606 00072 NM 1996 6 6 DLM11961265 1 19960523 A 3230 TRIM CYLINDER DOUG MD11 MD11 3023602 NM RT MLG MALFUNCTIONED A DALA K NONE J WARNING INDICATION TO TAKEOFF 1 SO 27 804DE 48475 ON FLIGHT 15 OUT OF FRA, ACFT EXPERIENCED AN UNSAFE RT MLG INDICATION WHICH EXTINGUISHED ITSELF AFTER 30 SEC. ON LANDIN G FOUND DAMAGE TO THE RT GEAR WHEEL WELL. FOUND THE RT GEAR TRIM CYLINDER OUT OF ADJ PER THE CMM. THIS COMPONENT WAS R EPLACED ON THE 10TH OF MAY 1996, WITH A HISTORY OF RT GEAR UNSAFE FOLLOWING THAT REPLACEMENT. 2 L 7 3 4F RT A22WE 1996060600073 19960606 00073 NM 1996 6 6 DLM11961277 1 19960526 A 3350 6044113 BATTERY DOUG MD11 MD11 3023602 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 802DE 48473 BATTERY PACK NR 3 FAILS LGT TEST, SHOWS LOW CHARGE. REPLACED BATTERY PACK, CKS GOOD. 2 L 7 3 4F RT A22WE 1996060600074 19960606 00074 NM 1996 6 6 DLM88961260 1 19960522 A 2752 59359731 ACTUATOR ARM DOUG MD88 MD88 3023688 NM LT TE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 940DL 49813 I/B FLAP ACTUATOR ARM CRACKED. REPLACED ARM. 2 L 7 2 4F RT A6WE 1996060600075 19960606 00075 WP 1996 6 6 MWEA96145 1 19960530 A 3350 6011779 POWER SUPPLY DOUG DC9 DC914 3022034 WP RT NACELLE INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 500ME 717 45711 MKE - DURING SERVICE CHECK, FOUND RT EMERGENCY NACELLE LIGHT WOULD NOT ILLUMINATE DURING TEST. REPLACED NACELLE LIGHT P OWER SUPPLY. OPS CHECK GOOD. RETURNED A/C TO SERVICE. (X) 2 L 7 2 4F A6WE 1996060600076 19960606 00076 NM 1996 6 6 P5CA9600235 1 19960529 A 5330 PANEL BOEING 747 747124 1384874 NM FUSELAGE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND PANEL DELAMINATED AFT OF NR 2 PACK HEAT EXCHANGER. REMOVED DELAMINATED SKIN, FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1996060600077 19960606 00077 NM 1996 6 6 P5CA9600236 1 19960529 A 5330 PANEL BOEING 747 747124 1384874 NM FUSELAGE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND PANEL DELAMINATED AFT OF NR 3 PACK HEAT EXCHANGER. REMOVED DELAMINATED SKIN, FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1996060600078 19960606 00078 NM 1996 6 6 P5CA9600237 1 19960529 A 7110 NOSE COWL BOEING 747 747124 1384874 NM NR 3 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND NR 3 ENGINE NOSE COWL DENTED AND CRACKED AT THE 8 O'CLOCK POSITION. POTTED DENT, FABRICATED AND INSTALLED DOUBLER IAW SRM 51-40-06. 2 L 7 4 4F A20WE 1996060600079 19960606 00079 NM 1996 6 6 P5CA9600238 1 19960529 A 5730 PANEL BOEING 747 747124 1384874 NM RT WING LE DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND RIGHT WING TOP LEADING EDGE PANEL AT NR 18 VCF WITH PREVIOUS COMPOSITE REPAIR MISSING TOP SURFACE, EXPOSING CORE M ATERIAL. REPAIRED LEADING EDGE PANEL WITH FIBERGLASS OVERLAYS IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996060600080 19960606 00080 NM 1996 6 6 P5CA9600239 1 19960529 A 5512 PANEL BOEING 747 747124 1384874 NM HORIZ STAB DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND PREVIOUS REPAIR ON UPPER SURFACE LEFT HORIZONTAL STABILIZER TRAILING EDGE PANEL DELAMINATED. REPAIRED IAW SRM 51- 40-06. 2 L 7 4 4F A20WE 1996060600081 19960606 00081 NM 1996 6 6 QXEA9600182 1 19960528 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 811PH 023 SEA - FLOOR PROXIMITY LIGHTING FORWARD LIGHT IS INOPERATIVE. WIRES AT LAMP SOCKET REPAIRED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1996060600082 19960606 00082 EU 1996 6 6 QXEA9600183 1 19960528 A 3350 1315 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 452US 11105 SEA - EMERGENCY LIGHT AT FRONT RIGHT EXIT IS INOPERATIVE. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETUR NED TO SERVICE. 2 L 7 2 4F RT A20EU 1996060600083 19960606 00083 NM 1996 6 6 SWAA960453 1 19960523 A 3350 1000679 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 83SW 22732 DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT LIGHT ABOVE AFT ENTRY DOOR INOPERATIVE. REPLACED BATTERY PACK PER BOEIN G M/M. 2 L 7 2 4F A16WE 1996060600084 19960606 00084 NM 1996 6 6 SWAA960454 1 19960523 A 5230 6546921528 DOOR BOEING 737 7372T4 1384492 NM CARGO COMPT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED C2/C4 CHECK, FOUND AFT CARGO COMPT DOOR WEB CRACKED .75 INCH AND ANGLE CRACKED AT FWD LOWER DOOR STOP. REPLACED CARGO DOOR PER BOEING M/M. 2 L 7 2 4F A16WE 1996060600085 19960606 00085 NM 1996 6 6 SWAA960455 1 19960523 A 5320 WINDOW POST BOEING 737 7373H4 1384600 NM L1/R1 COCKPIT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 312SW 23334 DURING SCHEDULED BC1 CHECK, FOUND R1 AND L1 C-D COCKPIT WINDOW POSTS CRACKED. INSTALLED REPAIR PER SWA RA 1-A53-1156. 2 L 7 2 4F RT A16WE 1996060600086 19960606 00086 NM 1996 6 6 SWAA960456 1 19960524 A 5320 SPLICE BOEING 737 7372H4 138448C NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21722 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, S4R. REPLACED SPLICE PER BOEING SRM. 2 L 7 2 4F A16WE 1996060600087 19960606 00087 NM 1996 6 6 SWAA960457 1 19960524 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 92SW 22964 DURING SCHEDULED A-CHECK, FOUND FUSELAGE SKIN CRACKED, JUST FWD OF WATER SERVICE BAY DOOR. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996060600088 19960606 00088 NM 1996 6 6 SWAA960458 1 19960524 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 92SW 22964 DURING SCHEDULED A-CHECK, FOUND FUSELAGE SKIN CRACKED JUST FWD OF WATER SERVICE BAY DOOR AND ALSO 24 INCHES FWD OF OUTFL OW VALVE. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996060600089 19960606 00089 NM 1996 6 6 SWAA960459 1 19960524 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 747/727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED SV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, AT BS 727B, AND AT BS 747 RT SIDE. REPAIRED ALL PER B OEING SRM. 2 L 7 2 4F RT A16WE 1996060600090 19960606 00090 NM 1996 6 6 SWAA960460 1 19960525 A 5320 ANGLE BOEING 737 7375H4 138449D NM BS 290 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 513SW 24190 DURING SCHEDULED 1/2 D-CHECK, FOUND ANGLE CRACKED AT BS 290, BETWEEN S10 AND S11R. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996060600091 19960606 00091 NM 1996 6 6 SWAA960461 1 19960525 A 5330 SKIN BOEING 737 7375H4 138449D NM SERV DOOR CUTOUT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 513SW 24190 DURING SCHEDULED 1/2 D-CHECK, FOUND FWD SERVICE DOOR CUTOUT CRACKED AT LOWER CORNER AT FASTENER HOLE AND Z-ANGLE. REPAI RED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996060600092 19960606 00092 NM 1996 6 6 SWAA960462 1 19960525 A 5320 STRAP BOEING 737 7375H4 138449D NM BS 311 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 513SW 24190 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM STABILIZING STRAPS CRACKED AT BS 311, BL ZERO, RBL 32, AND AT LBL 14. RE PLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996060600093 19960606 00093 NM 1996 6 6 SWAA960463 1 19960527 A 2120 AIR DISTR BOEING 737 7373H4 1384600 NM CABIN ODOR A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 617SW 27700 IN-FLIGHT, NOTED ELECTRICAL/RUBBER ODOR IN AFT CABIN AREA. NO VISIBLE SMOKE. NO EMERGENCY DECLARED. AIRCRAFT RETURNED TO BUR AND MADE AN UNEVENTFUL LANDING. INSPECTED ALL FLUORESCENT LIGHTING, SIDEWALL LIGHTS, COFFEMAKERS, LAVATORIES, HE ATERS, FLIGHT RECORDER COMPT, CARGO COMPTS, PAX LIGHTS AND PSU'S, E & E COMPT, RAN A/C GASPER FANS, NO EVIDENCE OF SMOKE OR SMELL. 2 L 7 2 4F RT A16WE 1996060600094 19960606 00094 NM 1996 6 6 SWAA960464 1 19960527 A 5320 DOOR FRAME BOEING 737 7373A4 1384585 NM BS 492 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED D-CHECK, FOUND AFT DOOR FRAME CRACKED AT BS 492, RBL 36, WL 162. REPAIRED PER TRAMCO EWO 96-0212. 2 L 7 2 4F RT A16WE 1996060600095 19960606 00095 NM 1996 6 6 SWAA960465 1 19960527 A 5312 BULKHEAD BOEING 737 7373A4 1384585 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKS AT BL ZERO, WL 187, AT RBL 5.7, WL 200, AND AT LBL 5.7, WL 200/20 4. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996060600096 19960606 00096 NM 1996 6 6 SWAA960466 1 19960527 A 5241 SKIN BOEING 737 7373A4 1384585 NM FWD GALLEY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED D-CHECK, FOUND FWD GALLEY DOOR LOWER AFT CORNER INSIDE DOUBLER CRACKED. REPAIRED WITH NEW DOUBLER PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996060600097 19960606 00097 NM 1996 6 6 SWAA960467 1 19960528 A 3350 900542 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 82SW 22731 DURING SCHEDULED A1 CHECK, FOUND FWD CABIN EMERGENCY LIGHTS INOP. REPLACED BATTERY SUPPLY PER BOEING M/M. 2 L 7 2 4F A16WE 1996060600098 19960606 00098 NM 1996 6 6 SWAA960468 1 19960528 A 5330 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 682SW 23496 DURING SCHEDULED BC1 CHECK, FOUND A .5 INCH CRACK AT COOLING DUCT CUTOUT SKIN AFT END. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996060600099 19960606 00099 NM 1996 6 6 SWAA960469 1 19960525 A 7720 EGT BOEING 737 7373H4 1384600 NM NR 1 ENGINE OVERTEMP A SWAA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 SW 07 323SW 23344 ON CLIMB-OUT, NR 1 ENGINE INDICATED EGT OVERTEMP CONDITION FOR 3 SECONDS. AIRCRAFT RETURNED TO ABQ AND MADE AN UNEVENTF UL LANDING. PERFORMED ENGINE INLET AND EXHAUST INSPECTION PER BOEING M/M. NO DEFECTS NOTED. 2 L 7 2 4F RT A16WE 1996060600100 19960606 00100 1996 6 6 SWAA960470 4 19960526 A 3454 NAV RECEIVER BOEING 737 7373H4 1384600 NM COCKPIT DAMAGED A SWAA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 389SW 26592 CHARTER FLIGHT EN ROUTE, AIRCRAFT DIVERTED TO BNA DUE TO FLUID SPILL ONTO NAV/COMM CONTROLS, MAKING BOTH ILS AND NR 1 CO MM INOPERATIVE. AIRCRAFT MADE AN UNEVENTFUL LANDING AT BNA. INSPECTED AREA. REPLACED CAPT AND F/O NAV CONTROL PANELS, BOTH COMM CONTROL PANELS, AND NR 1 NAV RECEIVER PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996060600101 19960606 00101 EA 1996 6 6 SWIA95743 1 19960521 A 3230 PROX SENSOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE NLG OUT OF ADJUST A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 412SW 7101 AFTER LIFT OFF AND GEAR RETRACTION, NOSE GEAR WOULD NOT COME UP. INDICATION REMAINED GREEN. ATTEMPTED TO CYCLE GEAR BU T IT DID NO GOOD. RETURNED TO GATE. REPLACED NOSE GEAR WOW SWITCH BRACKET AND ADJUSTED PROX SENSOR. REFER TO M/M TASK 32-30-00 - 720-901. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 1996060600102 19960606 00102 EA 1996 6 6 SWIA95744 1 19960522 A 3230 DRAG BRACE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE NLG FAILED A SWIA K NONE O OTHER CL CLIMB 1 NM 07 410SW 7066 TAKEOFF BUR, NOSE GEAR WOULD NOT RETRACT. NOSE GEAR REMAINED DOWN WITH NO TRANSIT INDICATION. CYCLED FOUR TIMES TO GET NOSE GEAR UP. REPLACED NOSE GEAR DRAG BRACE IAW CRJ MM 32-21-05 AND SWA RII 32-402. 2 L 7 2 4F 4 F RT A21EA E15NE 1996060600103 19960606 00103 NM 1996 6 6 UPS96220240 1 19960521 A 3350 BATTERIES BOEING 727 72722C 138400F NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 929UP 19092 CREW LEFT EXIT LIGHTS ARMED, A/C SHUT DOWN BY OPERATIONS. REMOVED AND REPLACED BATTERIES. 2 L 7 3 4F A3WE 1996060600104 19960606 00104 NM 1996 6 6 UPS96420224 1 19960516 A 5311 FRAME BOEING 747 747123 1384873 NM BS 1740 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE: C. AT BS 1740 RT STR 14, FRAME FORMED AND OLD FRAME REPAIR CRACKED. REPAIRED AT BS 1740 RT BETWEEN S TR 12 AND STR 14 IAW ETN 747-53-0762. 2 L 7 4 4F A20WE 1996060600105 19960606 00105 NM 1996 6 6 UPS96420225 1 19960515 A 5330 SKIN BOEING 747 747123 1384873 NM BS 987.5 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE: C. FOUND FUSELAGE SKIN CORRODED ON BSTA 987.5 STR 41L AND STR 42L. CUT OUT PIECE OF CORRODED SKIN AN D REPAIRED IAW SRM 53-30-03. 2 L 7 4 4F A20WE 1996060600106 19960606 00106 NM 1996 6 6 UPS96420226 1 19960515 A 5311 FRAME BOEING 747 747123 1384873 NM BS 1600 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE: C. FOUND CRACK IN TOP OF FRAME RT AT BSTA 1600 NEAR FLOOR STUD STR 34. DRILLED OFF CRACK IAW SRM 51- 10-01 AND REPAIRED IAW SRM'S 51-40-03 AND 51-30-02. 2 L 7 4 4F A20WE 1996060600107 19960606 00107 NM 1996 6 6 UPS96420227 1 19960522 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM BS 1720-1740 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE: C. FOUND CROWN AREA FROM SEAT TRACK AT BSTA 1720 - 1740 LBL 25 DAMAGED. REPLACED SEAT TRACK IAW SRM 53-10-23 FIG 5/51-30-02. 2 L 7 4 4F A20WE 1996060600108 19960606 00108 NM 1996 6 6 UPS96420228 1 19960516 A 5320 TORQUE BOX BOEING 747 747123 1384873 NM BS 1840-1860 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE: C. AFT CARGO COMP. WEB ON TOP OF TORQUE BOX IS CRACKED BETWEEN BS 1840/1860, LBL 63. WORKED OUT CRA CK AND REPAIRED IAW SRM'S 51-40-02, 51-30-02. 2 L 7 4 4F A20WE 1996060600109 19960606 00109 NM 1996 6 6 UPS96420229 1 19960515 A 5313 STRINGER BOEING 747 747123 1384873 NM BS 983 CORRDED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE: C. CORROSION FOUND DURING INSP. ON STR 46R BSTA 983 NEAR END FITTING. REPLACED CA. 1 FOOT OF STRINGE R IAW SRM 53-10-01, FIG 1, DETAIL 1. 2 L 7 4 4F A20WE 1996060600110 19960606 00110 NM 1996 6 6 UPS96420230 1 19960520 A 5320 SHEAR TIE BOEING 747 747123 1384873 NM BS 1740 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE: C. FOUND SHEAR TIE CRACKED AT STA 1740 RT SIDE BETWEEN STR 50 AND STR 51. REPAIRED SHEARED TIE IAW S RM 53-10-04, FIG 3. 2 L 7 4 4F A20WE 1996060600111 19960606 00111 NM 1996 6 6 UPS96420231 1 19960516 A 5320 BRACKET BOEING 747 747123 1384873 NM BS 1760 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE: C. AFT CARGO COMPAARTMENT ATTACHMENT BRACKET FOR LOWER SILL JOINT WITH FRAME AT BS 1760 IS CRACKED IN TOP. REPLACED BRACKET IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996060600112 19960606 00112 NM 1996 6 6 UPS96420232 1 19960517 A 5313 STRINGER BOEING 747 747123 1384873 NM BS 2100 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE: C. FOUND CRACK IN FRAME STRINGER CUT-OUT AT BS 2100 S29R. REPAIRED FRAME IAW SRM 53-10-04. 2 L 7 4 4F A20WE 1996060600113 19960606 00113 NM 1996 6 6 UPS96420233 1 19960517 A 5320 SHEAR TIE BOEING 747 747123 1384873 NM BS 2160 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE: C. BULK CARGO COMPARTMENT FOUND CRACKED IN FRAME SHEAR TIE AT STRINGER CUTOUT AT BS 2160, S42/44 LT. REPAIRED SHEAR TIE IAW SRM 53-10-01. 2 L 7 4 4F A20WE 1996060600114 19960606 00114 NM 1996 6 6 UPS96420234 1 19960516 A 5311 FRAME BOEING 747 747123 1384873 NM BS 1960 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE: C. FOUND CRACK IN FRAME INNER FLANGE AT BS 1960, S40L. REPAIRED FRAME INNER FLANGE IAW 53-10-04, FIG 66 DETAIL 3. 2 L 7 4 4F A20WE 1996060600115 19960606 00115 NM 1996 6 6 UPS96420235 1 19960515 A 5311 FRAME BOEING 747 747123 1384873 NM BS 1860 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE: C. AFT CARGO COMPARTMENT, FOUND CRACK IN TOP OF FRAME BETWEEN STR 41/42 LBL 62 NEAR SIDE GUIDE BRACKE T AT BS 1860. REPAIRED CRACK IN FRAME IAW SRM 51-40-03. 2 L 7 4 4F A20WE 1996060600116 19960606 00116 NM 1996 6 6 UPS96420236 1 19960515 A 5320 WEB BOEING 747 747123 1384873 NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE: C. NLG WHEELWELL: WEB FROM PRESSURE PAN AT BULKHEAD STA 400 IS CRACKED. REPLACED WEB IAW SRM 51-30- 02. 2 L 7 4 4F A20WE 1996060600117 19960606 00117 NM 1996 6 6 UPS96420237 1 19960518 A 5311 FRAME BOEING 747 747123 1384873 NM BS 1820 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE: C. AFT CARGO FRAME TOP CAP AT STA 1820, BBL 26L - 42L. REPAIRED IAW SRM 51-40-03. 2 L 7 4 4F A20WE 1996060600118 19960606 00118 NM 1996 6 6 UPS96520239 1 19960521 A 3350 BULB BOEING 757 75724APF 1384969 NM CABIN FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 411UP 23851 INSPECTION TYPE: IN CABIN, EMERGENCY EXIT LIGHT ASSY HAS SEVERAL BURNED OUT BULBS. RELAMPED ASSY. - TESTED NORMALLY. 2 L 7 2 4F RT A2NM 1996060600119 19960606 00119 WP 1996 6 6 UPS96820238 1 19960526 A 2760 276000 SPOILER PUMP DOUG DC8 DC873F 302199F WP MLG WW FAILED A IPXA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 880UP 46080 INSPECTION TYPE: 3+3C. BLOCK TURN BACK, SPOILER PUMP ABNORMAL, LOW PRESSURE. SDN: LOG BOOK PG. 565487. REPLACED SPOILER PUMP AND OPS CHECK GOOD, P/N 27-60-00. 2 L 7 4 4F RT 4A25 1996060600120 19960606 00120 EU 1996 6 6 WWMA9600047 1 19960513 A 2150 1658D000 COOLING TURBINE BAG JETSTM JETSTM3201 1500217 EU LEFT DEFECTIVE A WWMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 15 969AE 346 969 THE CREW REPORTED THAT THE LEFT BLEED WAS PRODUCING A STRONG BURNING HOT OIL SMELL. MAINTENANCE DEFERRED THE LEFT BLEED IAW THE MEL. UPON INVESTIGATION IN SBP ON 5-30-96, THE LEFT COOLING TURBINE AND WATER SOCK WERE REPLACED. GROUND RAN AIRCRAFT AND NO SMELLS WERE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A56EU 1996060600136 19960606 00136 1996 6 6 AALA960426 4 19960320 A 2565 101623303 SLIDE SARGENT BOEING 767 767223 1385123 NM PASSENGER DOOR SCRAPPED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 A3013 LAX - DURING SHOP TEST DEPLOYMENT, EMERGENCY EVACUATION UPPER TUBE HAD POROSITY LEAKS. SCRAPPED EMERGENCY EVACUATION SL IDE. 2 L 7 2 4F RT A1NM 1996060600157 19960606 00157 WP 1996 6 6 96ZZZX2790 1 19960327 A 5720 5932267 CLIPS DOUG DC9 DC931 3022065 WP LT WING CORRODED A A4JA K NONE O OTHER IN INSP/MAINT 1 SO 15 8931E 47140 LEFT WING TEE CAP OUTBOARD HORIZONTAL LEG CORRODED. REMOVED CORROSION, INSTALLED REPAIRS IAW DC-9 SB 57-98 PER DRAWINGS NR 5932267 AND NR 593226 AND DC-9 SRM'S 51-10-3, 51-30-5, AND DC-9 MM 20-30-0. REF: NR 060N1-0001 AND NR 060F1-0002. 2 L 7 2 4F A6WE 1996060600158 19960606 00158 WP 1996 6 6 96ZZZX2791 1 19960327 A 5720 5932267 FILLER DOUG DC9 DC931 3022065 WP LT WING CORRODED A A4JA K NONE O OTHER IN INSP/MAINT 1 SO 15 8931E 47140 LEFT WING TEE CAP OUTBOARD HORIZONTAL LEG CORRODED. REMOVED CORROSION, INSTALLED REPAIRS IAW DC-9 SB 37-98 PER DRAWINGS NR 5932267 AND NR 593226 AND DC-9 SRM'S 51-10-3, 51-30-5, AND DC-9 MM 20-30-0. REF: NR 060N1-0001 AND NR 060F1-0002. 2 L 7 2 4F A6WE 1996060600159 19960606 00159 WP 1996 6 6 96ZZZX2792 1 19960331 A 5521 SPAR DOUG DC9 DC931 3022065 WP LT ELEVATOR CRACKED A A4JA K NONE O OTHER IN INSP/MAINT 1 SO 15 8931E 47140 RADIOGRAPHIC INSPECTION REVEALED CRACK IN LEFT ELEVATOR FRONT SPAR UPPER FLANGE, EMANATING FROM RIVET HOLE IN FORWARD DI RECTION AND TERMINATING AT EDGE OF FLANGE APPROXIMATELY .300 INCH IN LENGTH. REPAIRED AREA IAW DC-9 SRM 55-02, PAGE 31. BALANCED ELEVATOR IAW DC-9 SRM 55-20-1 AND RIGGED ELEVATOR IAW DC-9 MM 27-30-2. 2 L 7 2 4F A6WE 1996060600160 19960606 00160 NM 1996 6 6 96ZZZX2793 1 19960430 A 5330 SKIN BOEING 737 7372H5 138448E NM BS 767 CRACKED A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 220US 20453 GSO - VISUAL INSPECTION FOUND .9 INCH CRACK IN OUTER SKIN AT FS 767, STR 19R DURING WALK-AROUND. INSTALLED DOUBLER USIN G BLIND FASTENERS (OM-7 32938), PER SRM 53-30-3, FIGURE 6. 2 L 7 2 4F A16WE 1996060600161 19960606 00161 GL 1996 6 6 96ZZZX2794 3 19960219 A 6111 E10950PK BLADE BEECH 1900 1900D 1154162 CE HARTZL HCB3T HCB3TN3 GL LT PROPELLER SPLIT A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 171ZV 9477 UE171 HJ437 DURING ROUTINE MAINTENANCE, THE TRAILING EDGE WAS FOUND SPLIT APPROXIMATELY 2.5 INCHES. REPAIRED IAW HARTZELL MM AND FO RM 8110-3. 2 L 7 2 4T RT A24CE 6 C P15EA 1996060600164 19960606 00164 EU 1996 6 6 96ZZZX2797 1 19960408 A 6520 B4554 CHIP PLUG AEROSP SA365 SA365N 8680669 EU T/R GRBOX FAILED A ZYWA K NONE O OTHER IN INSP/MAINT 1 GL 09 365SJ 6018 KNOB ON CHIP PLUG SEPARATED FROM MAGNET. REMOVED AND REPLACED CHIP PLUG. 1 G 7 2 3U H10EU 1996060600165 19960606 00165 1996 6 6 96ZZZX2798 4 19960411 A 3120 APM11200WE CLOCK AEROSP SA365 SA365N 8680669 EU COPILOT FAILED A ZYWA K NONE O OTHER IN INSP/MAINT 1 GL 09 365SJ 689 5652 6018 COPILOT'S CLOCK INOPERATIVE. REMOVED AND REPLACED CLOCK. 1 G 7 2 3U H10EU 1996060600169 19960606 00169 GL 1996 6 6 96ZZZX2802 2 19960319 A 7250 SHEAR PIN BELL 206 206L 1181522 SW ALLSN 250C 250C30P 03013 GL NR 8 BEARING FAILED A A NYBA O OTHER J WARNING INDICATION AP APPROACH 1 EA 11 122NH 45101 CAE821672F PILOT NOTED A HIGH PITCH WHINE EMANATING FROM ENGINE AREA. A VISUAL INSPECTION WAS PERFORMED OF THE ENGINE AND DRIVE TR AIN AREAS. NO DEFECTS NOTED. ENGINE CHIP PLUGS WERE INSPECTED. NO METAL NOTED. APPROXIMATELY 1.50 HOURS AFTER INSPEC TION, THE ENGINE CHIP LIGHT ILLUMINATED WHILE THE PILOT WAS ON FINAL APPROACH. UPON SHUT DOWN, THE MECHANIC INSPECTED E NGINE CHIP PLUGS AND FOUND MODERATE AMOUNTS OF METAL ON THE UPPER PLUG. THE ENGINE ASSY WAS REMOVED FOR REPAIR. UPON T EAR DOWN INSPECTION, NO BINDING NOTED IN THE TURBINE ASSY. THE NR 8 BEARING COVER WAS REMOVED AND THE SHEAR PIN WHICH R ETAINS RETAINER PLATE WAS FOUND LYING IN THE PLATE. IT WAS ALSO NOTED THE NUT RETAINING THE TIE-BOLT HAD LOST TORQUE. 1 G 7 1 3U 3 U H2SW E1GL 1996060600170 19960606 00170 WP 1996 6 6 96ZZZX2803 1 19960505 A 2910 AE2460013J0630 HYDRAULIC HOSE DOUG DC8 DC861 3021952 WP R 3 ENGINE RUPTURED A FXLA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS TO TAKEOFF 1 SO 19 27UA 45942 MIA - ON TAKEOFF, EXPERIENCED LOSS OF HYDRAULIC PRESSURE AND QUANTITY. RETURNED AND LANDED WITHOUT INCIDENT. GROUND IN SPECTION REVEALED A RUPTURED HYDRAULIC HOSE ON NR 3 ENGINE. REPLACED HOSE AND SYSTEM CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4A25 1996060600171 19960606 00171 NM 1996 6 6 AALA960518 1 19960227 A 5314 6518363156 KEEL BEAM BOEING 727 727223 1384074 NM BS 873 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 710AA 22467 DURING CONTRACT MAINTENANCE AT DALA FOR HEAVY C-CHECK, THE RIGHT AND LEFT SIDES OF THE KEEL BEAM JUST AFT OF STA 873 WER E FOUND CRACKED. THE CRACK IN THE LEFT BEAM RESULTED IN THE REMOVAL OF A 0.750 INCH LONG BY 0.380 INCH WIDE BY 0.195 IN CH DEEP SECTION OF THE CHORD BELOW THE CRACKED FLANGE. THE CRACKS WERE CONFINED TO THE UPPER FLANGE OF THE CHORD ONLY A ND WERE REPAIRED PER 727 SB 727-53-0208, REF: DL ERA 303000-14. (X) 2 L 7 3 4F A3WE 1996060600172 19960606 00172 SO 1996 6 6 ASOA96015 1 19960513 A 5330 SKIN EMB 120 EMB120RT SO CARGO DOOR ARM DENTED A ASOA K NONE O OTHER TX TAXI/GRND HDL 1 SO 11 214AS 120009 AIRCRAFT WAS HIT JUST BELOW THE CARGO DOOR BY A BAG CART WHILE PARKED ON THE ATL RAMP. UPON INSPECTION, AIRCRAFT WAS FO UND SAFE FOR A FERRY FLIGHT TO MCN FOR REPAIR. REMOVED DAMAGED AREA AND INSTALLED AN EXTERNAL DOUBLER AND INSTALLED A F ORM DOUBLER OVER THE INTERNAL BRACE PER E.O. 120-053-0038. RII WAS COMPLETED SATISFACTORILY AND THE AIRCRAFT WAS RELEAS ED FOR SERVICE. (X) 2 L 7 2 4T RT A31SO 1996060600174 19960606 00174 WP 1996 6 6 CAL960542 1 19960427 A 4990 OIL TANK VENT DOUG DC9 DC982 3022082 WP APU OIL TANK CLOGGED A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 09 16887 49116 FLT NR 279 - EWR - PRIOR TO PUSH BACK CABIN BEGAN TO FILL WITH SMOKE. DURING T/S FOUND OIL LEAKED ON COALESCER BAGS DUE TO APU OIL TANK BEING OVERSERVICED. REMOVED AND REPLACED COALESCER BAGS CLEANED APU OIL TANK VENT HOLE, DRAINED 2 QTS OF OIL. TANK NOW READS FULL ALSO CLEANED AIR INTAKE BOX. (M) 2 L 7 2 4F A6WE 1996060600175 19960606 00175 NM 1996 6 6 CAL960558 1 19960506 A 3397 PIN BOEING 737 737524 1384721 NM CABIN NOT SEATED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 32626 27530 IAH - FLT 0773 - THE EMERGENCY AISLE PATH LIGHTS AT SEAT 1AB WERE FOUND INOPERATIVE. MAINTENANCE FOUND A PIN PUSHED BAC K ON SEAT WIRING HARNESS. THE PIN WAS RESEATED AND OPERATION OF THE EMERGENCY LIGHTS WAS RESTORED. (X) 2 L 7 2 4F RT A16WE 1996060600176 19960606 00176 NM 1996 6 6 CAL960559 1 19960506 A 3250 CIRCUIT BREAKER BOEING 737 7373T0 1384582 NM NLG STEERING TRIPPED A CALA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 09 69333 23571 PHL - FLT 1755 - TAKEOFF WAS REJECTED AT 50 KNOTS DUE TO LIMITED NOSE WHEEL STEERING. MAINTENANCE FOUND THE NOSE WHEEL STEERING CIRCUIT BREAKER TRIPPED. THE CIRCUIT BREAKER WAS RESET AND STEERING OPERATION WAS NORMAL. (X) 2 L 7 2 4F RT A16WE 1996060600177 19960606 00177 NM 1996 6 6 CAL960560 1 19960506 A 2910 65445101297 HYDRAULIC LINE BOEING 737 737130 1384435 NM LT MLG WW CHAFED A CALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 09 44214 19031 EWR - FLT 0674 - THE B-HYDRAULIC SYSTEM LOW QUANTITY ILLUMINATED ON APPROACH TO DWR. THE 'A' AND 'B' SYSTEMS REMAINED A T 3,000 PSI WITH 2 GALLONS QUANTITY. THE GEAR AND FLAPS EXTENDED NORMALLY. THE QUANTITY WENT TO 1 GALLON WITH T/R ACTI VATED AND RETURNED TO 1.8 GALLONS WHERE IT REMAINED. ACFT LANDED WITHOUT INCIDENT. B-SYSTEM PRESSURE WENT TO ZERO AT T HE GATE. MAINTENANCE FOUND AN A-SYSTEM PRESSURE LINE AND A B-SYSTEM SPOILER LINE, BOTH IN THE LT MLG WHEELWELL, CHAFED. BOTH LINES WERE REPLACED. PRESSURE AND LEAK CHECKS WERE GOOD. THE HYDRAULIC SYSTEM WAS SERVICED TO FULL. (X) 2 L 7 2 4F A16WE 1996060600178 19960606 00178 WP 1996 6 6 CAL960561 1 19960312 A 3397 WIRE DOUG DC10 DC1010 3022110 WP L1 DOOR BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 68044 46903 KUL - THE EMERGENCY LIGHTS AT L-1 DOOR FAILED TO ILLUMINATE DURING TEST. MAINTENANCE FOUND A BROKEN WIRE AT TERMINAL BL OCK. THE WIRE WAS REPAIRED AND OPERATION OF THE EMERGENCY LIGHTS WAS RESTORED. (X) 2 L 7 3 4F A22WE 1996060600179 19960606 00179 WP 1996 6 6 CAL960562 1 19960318 A 5720 BEAM DOUG DC10 DC1010 3022110 WP WS 118-240 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 77961 46903 KUL - THE LEFT WING UPPER TRAILING EDGE BEAM WAS FOUND CORRODED BETWEEN STA XW 118 AND XORS 240. THE AREA WAS REPAIRED IAW ECRA 5720-01514. (X) 2 L 7 3 4F A22WE 1996060600180 19960606 00180 WP 1996 6 6 CAL960563 1 19960405 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1661-1681 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 77961 46903 KUL - THE AFT INTERMEDIATE FUSELAGE SKIN WAS FOUND CORRODED AT STA 1661 AND STA 1681 BETWEEN LONGERON 51L TO LONGERON 52 L. A DOUBLER REPAIR WAS PERFORMED IAW ECRA 5330-02378. (X) 2 L 7 3 4F A22WE 1996060600181 19960606 00181 WP 1996 6 6 CAL960564 1 19960318 A 5720 ARB06361 ANGLE DOUG DC10 DC1010 3022110 WP LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 77961 46903 KUL - THE LEFT WING (MLG SUPPORT INSTALLATION) AUXILIARY SPAR SPLICE ANGLE WAS FOUND CRACKED DUE TO STRESS CORROSION. T HE SPLICE ANGLE WAS REPLACED IAW DRAWING NR ARB06361. (X) 2 L 7 3 4F A22WE 1996060600182 19960606 00182 WP 1996 6 6 CAL960565 1 19960326 A 5753 HNGE BOLT DOUG DC10 DC1010 3022110 WP LT TE FLAP SHEARED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 77961 46903 KUL - THE LEFT INBOARD FLAP OUTBOARD HINGE BOLT WAS FOUND SHEARED AND THE FAIL SAFE BUSHING WAS BROKEN. THE HINGE BEARI NG WAS ALSO CRACKED. THE HINGE BOLT, FAIL SAFE BUSHING, AND HINGE BEARING WERE REPLACED. FLAP INSTALLATION AND RIGGING WAS PERFORMED IAW MM 27-50-01. (X) 2 L 7 3 4F A22WE 1996060600183 19960606 00183 WP 1996 6 6 CAL960566 1 19960405 A 5753 77711626 BOLTS DOUG DC10 DC1010 3022110 WP RT TE FLAP SHEARED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 77961 46903 KUL - THE RIGHT OUTBOARD FLAP, INBOARD HINGE TENSION STAP BOLTS (2 EACH) WERE FOUND SHEARED. THE TENSION STRAP BOLTS WE RE REPLACED IAW STANDARD PRACTICES. (X) 2 L 7 3 4F A22WE 1996060600184 19960606 00184 WP 1996 6 6 CAL960567 1 19960315 A 5712 FORMER DOUG DC10 DC1010 3022110 WP WS 1019/1013 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 77961 46903 KUL - INSPECTION FOUND A 0.75 INCH CRACK AT XOS 1019 AND A 1 INCH CRACK AT XOS 1013 IN LEADING EDGE FORMER. THE FORMER WAS REPAIRED IAW SRM 57-20-00, FIGURE 1. (X) 2 L 7 3 4F A22WE 1996060600185 19960606 00185 WP 1996 6 6 CAL960568 1 19960328 A 5720 FORMER DOUG DC10 DC1010 3022110 WP WS 1089/759 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 77961 46903 KUL - INSPECTION FOUND A 1 INCH CRACK AT XOS 1089 AND A 1.5 INCH CRACK AT XOS 759 IN LEADING EDGE FORMER. THE FORMER WA S REPAIRED IAW SRM 57-00-00, FIGURE 3. (X) 2 L 7 3 4F A22WE 1996060600186 19960606 00186 NM 1996 6 6 CAL960580 1 19960405 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 947 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18350 27296 23588 HOU - INSPECTION FOUND FLOORBEAM INTERCOSTAL CORROSION AT STA 947, LEFT AND RIGHT SIDE. THE INTERCOSTAL WAS REPLACED IA W ECRA 5310-03252. (X) 2 L 7 2 4F RT A16WE 1996060600187 19960606 00187 NM 1996 6 6 CAL960581 1 19960405 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 947-967 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18350 27296 23588 HOU - INSPECTION FOUND FLOORBEAM INTERCOSTAL CORRODED AT STA 947 TO STA 967, RBL 12. THE INTERCOSTAL WAS REPLACED IAW E CRA 5310-03252. (X) 2 L 7 2 4F RT A16WE 1996060600188 19960606 00188 NM 1996 6 6 CAL960582 1 19960405 A 5313 STRINGER BOEING 737 7373T0 1384582 NM BS 500 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18350 27296 23588 HOU - INSPECTION FOUND A .50 INCH CRACK IN STR 16L AT STA 500. A NEW STRINGER SECTION AND SPLICE WAS FABRICATED AND INS TALLED IAW SRM 53-00-03. (X) 2 L 7 2 4F RT A16WE 1996060600189 19960606 00189 NM 1996 6 6 CAL960583 1 19960405 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18350 27296 23588 HOU - INSPECTION FOUND FLOORBEAM CORRODED ON TOP AND BOTTOM SURFACE AT STA 986. THE FLOORBEAM WAS REPLACED IAW SRM 53-0 0-51. (X) 2 L 7 2 4F RT A16WE 1996060600190 19960606 00190 NM 1996 6 6 CAL960584 1 19960404 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 344-360 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18350 27296 23588 HOU - INSPECTION FOUND FLOORBEAM INTERCOSTAL CORRODED BETWEEN STA 344 AND STA 360 AT LBL 15. A NEW INTERCOSTAL WAS FABR ICATED AND INSTALLED IAW ECRA 5310-03252. (X) 2 L 7 2 4F RT A16WE 1996060600191 19960606 00191 NM 1996 6 6 CAL960585 1 19960404 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 294.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18350 27296 23588 HOU - INSPECTION FOUND FLOORBEAM INTERCOSTAL CORRODED JUST AFT OF STA 294.5 AT RBL 15. A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 5310-03252. (X) 2 L 7 2 4F RT A16WE 1996060600192 19960606 00192 WP 1996 6 6 CAL960591 1 19960508 A 3230 GRD SENSE MECH DOUG DC10 DC1010 3022110 WP LANDING GEAR OUT OF ADJUST A CALA O OTHER J WARNING INDICATION TO TAKEOFF 1 SW 09 68046 47800 EWR - FLT 0088 - THE LANDING GEAR HANDLE WOULD NOT RAISE TO UP POSITION AND ON TAKEOFF FROM SFO, THE OVERRIDE BUTTON WAS USED AND THE GEAR RETRACTED. THE AIRCRAFT CONTINUED FLIGHT TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE PERFO RMED A GEAR SWING AND THE GEAR RETRACTED NORMALLY. THE AIRCRAFT WAS OBSERVED TO BE STUCK IN THE AIR MODE WITH AUTO SLAT S EXTENDED AND WOULD NOT RETRACT. A GROUND SENSING CONTROL MECHANISM AND ADJUSTMENT TEST WAS PERFORMED IAW MM 32-24-01, PAGE 202, AND OPERATION CHECKED GOOD. (X) 2 L 7 3 4F A22WE 1996060600193 19960606 00193 NE 1996 6 6 CAL960593 2 19960512 A 7261 775898 OIL TUBE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 1 ENGINE LEAKING A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 16813 48066 708409 MSY - FLT 1865 - THE NR 1 ENGINE BEGAN TO LOSE OIL WHILE EN ROUTE FROM PBI TO IAH. THE AIRCRAFT WAS DIVERTED TO MSY WHE RE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A LEAKING OIL TUBE TO NR 1 ENGINE. THE OIL TUBE WAS REPLACED WITH NEW SEALS INSTALLED. THE ENGINE WAS SERVICED WITH OIL. THE ENGINE WAS RUN AND LEAK CHECKS WERE GOOD. (X) 2 L 7 2 4F 4 F A6WE E9NE 1996060600194 19960606 00194 WP 1996 6 6 CAL960594 1 19960513 A 3230 LATCH ASSY DOUG DC9 DC932 3022066 WP LT MLG BINDING A CALA O OTHER P NO WARNING INDICATION AP APPROACH 1 SW 09 27522 47524 CLE - FLT 1435 - WHEN LANDING GEAR HANDLE WAS MOVED TO THE DOWN POSITION FOR LANDING ON APPROACH TO CLE, THE LT MLG RED UNSAFE LIGHT DID NOT ILLUMINATE. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT MLG UPLOCK LATCH ASSEM BLY ROLLER JAMMED. THE ROLLER WAS ADJUSTED AND A LANDING GEAR SENSOR CHECK WAS PERFORMED IAW MM 32-60-00 AND ALL LIGHTS CHECKED NORMAL. (X) 2 L 7 2 4F A6WE 1996060600195 19960606 00195 WP 1996 6 6 CAL960603 1 19960411 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 1087 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 27509 46350 47798 HOU - INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE SKIN AT STA 1087, LONGERON 1L. THE CRACKED AREA WAS CUT OUT AND A R EPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-04, FIGURE 27. (X) 2 L 7 2 4F A6WE 1996060600196 19960606 00196 WP 1996 6 6 CAL960608 1 19960423 A 5350 CABLES DOUG DC9 DC932 3022066 WP TAILCONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12507 47788 HOU - THE TAILCONE INTERIOR AND EXTERIOR RELEASE SYSTEM PULLED LOW. THE TAILCONE RELEASE SYSTEM CABLES WERE ADJUSTED IA W MM 53-50-3, ITEM B, STEPS 1-17. (X) 2 L 7 2 4F A6WE 1996060600197 19960606 00197 NM 1996 6 6 MALA964976 1 19960430 A 3060 3061K4 RELAY DHAV DHC8 DHC8102 2809003 NM PROP DEICE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 816MA 231 DTW - FLT 3106 - ON CLIMB-OUT, BLADES 2 AND 4 ON THE RIGHT PROPELLER APPEARED TO HEAT CONTINUOUSLY DESPITE SELECTOR POSI TION. THE CREW PULLED THE PROPELLER DEICE CIRCUIT BREAKER AND RETURNED TO DTW. MAINTENANCE REPLACED THE 3061-K4 RELAY. SYSTEM OPERATED SATISFACTORILY. (X) 2 H 7 2 4T RT A13NM 1996060600198 19960606 00198 WP 1996 6 6 MALA964977 2 19960430 A 7200 31025408 ENGINE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP LEFT FAILED A MALA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 15 430MA AC710 TOL/DTW - FLT 3328 - IN CRUISE FLIGHT, THE LEFT ENGINE CHIP DETECTOR LIGHT ILLUMINATED. THE CREW PERFORMED QUICK REFERE NCE PROCEDURES. (X) 2 L 7 2 4T 4 T RT A8SW E4WE 1996060600199 19960606 00199 1996 6 6 MALA964978 4 19960501 A 3442 40010186108 RADAR R/T UNIT SWRNGN SA227 SA227AC 8780603 SW NOSE FAILED A MALA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 425MA AC640 DTW - FLT 3354 - IN CRUISE FLIGHT, WEATHER RADAR SIGNAL BECAME WEAK AND INTERMITTENT. THE RADAR ALSO TILTED 10-15 DEGRE ES DOWN AT VARIOUS RANGES. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE WEATHER RADAR RECEIVER/TRANSCEIVER. SYSTEM OPERATED SATISFACTORILY. (X) 2 L 7 2 4T RT A8SW 1996060600200 19960606 00200 SW 1996 6 6 MALA964979 1 19960503 A 5210 274044010 CORNER SWRNGN SA227 SA227AC 8780603 SW PASSENGER DOOR CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 446MA AC693 MSP - DURING AN INSPECTION, MAINTENANCE PERSONNEL NOTED PASSENGER DOOR LOWER FORWARD CORNER CRACKED AT SNUBBER ATTACH PL ATE. REMOVED AND REPLACED DOOR CORNER, P/N 27-4044-010, AND DOOR CORNER SUPPORT, P/N 27-24150-403, IAW FAC SRM 51-00-00 , PAGE 4, AND SRM 51-40-01. (X) 2 L 7 2 4T RT A8SW 1996060600201 19960606 00201 NM 1996 6 6 MALA964980 1 19960504 A 3230 RETRACT MECH DHAV DHC8 DHC8102 2809003 NM NLG LACK OF LUBE A MALA K NONE J WARNING INDICATION AP APPROACH 1 GL 15 859MA 361 TVC - FLT 3183 - ON APPROACH, THE NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR EXTENSION. THE CREW PERFORMED AN ALTERNATE LANDING GEAR EXTENSION. ALL INDICATIONS WERE NORMAL. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. MAINTENANCE PERFORMED A POST-FLIGHT MEMORY CHECK OF THE PSEU, NO FAULTS RECORDED. THE GEAR WAS CLEANED AND LUBED AS A PRECAUTION. (X) 2 H 7 2 4T RT A13NM 1996060600202 19960606 00202 1996 6 6 MALA964981 4 19960505 A 3442 066308601 RADAR INDICATOR DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A MALA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 864MA 363 DTW - FLT 3338 - IN CRUISE FLIGHT, THE RADAR DISPLAY BEGAN TO PAINT A SOLID GREEN AREA WHEN TURNED ON. THE AIRCRAFT RET URNED TO DTW. MAINTENANCE REPLACED THE WEATHER RADAR INDICATOR. ALL CHECKS SATISFACTORY. (X) 2 H 7 2 4T RT A13NM 1996060600203 19960606 00203 WP 1996 6 6 ORJA9625 1 19960508 A 3233 3937060501 ATTACH BOLT DOUG DC9 DC983 3022083 WP LT MLG ACT SHEARED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 879RA 4752 53185 LEFT LANDING ACTUATOR LOWER LINK ATTACH BOLT SHEARED. REMOVED AND REPLACED LEFT MLG ACTUATOR LOWER LINK LOWER ATTACH BO LT. PART TOTAL CYCLES, 3,685.(X) 2 L 7 2 4F RT A6WE 1996060600204 19960606 00204 EU 1996 6 6 UF6A960403 1 19960409 A 3350 6013211 POWER SUPPLY BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 858AW 8154 2035 ORD - FLT 5733 - FORWARD EMERGENCY EXIT FLOOR TRACK LIGHTING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FORWARD POWE R SUPPLY BATTERY PACK. (X) 2 L 7 2 4T RT A27NM 1996060600205 19960606 00205 WP 1996 6 6 9611799905 1 19960526 A 5320 FITTINGS DOUG DC9 DC931 3022065 WP FS 617-637 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 955N 47160 DURING H-CHECK, FOUND CRACKS ON THE LEFT KEEL FITTINGS AT FORMERS FS 617 AND 637. REPLACED FITTINGS PER SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1996060600206 19960606 00206 WP 1996 6 6 9611809940 1 19960527 A 5320 FITTING DOUG DC9 DC932 3022066 WP FS 598-617 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3322L 47031 DURING M-CHECK, FOUND CORROSION ON THE FRONT SPAR FITTING AT FS 598 TO 617 LBL 66. REPLACED FITTING PER SRM 51-30-0. 2 L 7 2 4F A6WE 1996060600207 19960606 00207 NM 1996 6 6 9611872298 1 19960526 A 3150 T/O WARNING BOEING 727 727251 138408H NM COCKPIT SOUNDED A NWAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 01 298US 22152 DURING TAKEOFF ROLL, AIRCRAFT INDICATED TAKEOFF WARNING. ABORTED TAKEOFF WITHOUT INCIDENT. SECOND TAKEOFF WAS NORMAL. MSP MAINTENANCE PERFORMED TAKEOFF WARNING SYSTEM CHECK, CHECKED OK. 2 L 7 3 4F A3WE 1996060600208 19960606 00208 WP 1996 6 6 9611881159 1 19960530 A 3260 THROTTLE SWITCH DOUG DC10 DC1040 3023508 WP NR 3 BROKEN ARM A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 159US 46768 DURING CLIMB, PLACED THE GEAR HANDLE IN THE UP POSITION, THE WARNING HORN SOUNDED AND ALL FOUR GEAR LIGHTS STAYED RED. G EAR WAS RECYCLED AND VISUALLY CHECKED IN THE UP POSITION WITH THE RED GEAR UNSAFE LIGHT STILL ILLUMINATED. FLIGHT CONTI NUED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 3 THROTTLE ASSEMBLY SWITCH S1-342 AND RETURNED TO SERVICE. 2 L 7 3 4F A22WE 1996060600209 19960606 00209 WP 1996 6 6 9611899936 1 19960523 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 1799U 47370 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY PATH LIGHTING INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996060600210 19960606 00210 WP 1996 6 6 9611909937 1 19960523 A 3350 FUSE DOUG DC9 DC931 3022065 WP CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 908H 47517 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS AT FIRST CLASS CABIN AND GALLEY DOOR INOPERATIVE. REPLACED F USE, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996060600211 19960606 00211 WP 1996 6 6 9611919955 1 19960524 A 3350 6014113 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 922RW 47182 DURING LINE MAINTENANCE INSPECTION, FOUND FIRST CLASS FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PA CK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996060600212 19960606 00212 WP 1996 6 6 9611929966 1 19960526 A 3350 6011779 POWER SUPPLY DOUG DC9 DC931 3022065 WP LT NACELLE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9330 47138 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996060600213 19960606 00213 WP 1996 6 6 9611939969 1 19960524 A 3350 FUSE DOUG DC9 DC931 3022065 WP CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9333 47246 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS AT FIRST CLASS AND GALLEY DOOR INOPERATIVE. REPLACED FUSE, O PERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996060600214 19960606 00214 WP 1996 6 6 9611949972 1 19960526 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9336 47338 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS AT TAIL COMPARTMENT CATWALK INOPERATIVE. REP LACED BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996060600215 19960606 00215 WP 1996 6 6 9611959979 1 19960525 A 3350 FUSE DOUG DC9 DC931 3022065 WP CABIN FAILED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9343 47439 DURING LINE MAINTENANCE INSPECTION, FOUND FIRST CLASS AND GALLEY DOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE AT GA LLEY DOOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996060600216 19960606 00216 WP 1996 6 6 9611969984 1 19960527 A 3350 6011779 POWER SUPPLY DOUG DC9 DC932 3022066 WP LT NACELLE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 984US 47383 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996060600217 19960606 00217 WP 1996 6 6 9611979881 1 19960530 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 676MC 47652 DURING LINE CHECK, FOUND AFT ENTRY DOOR AND TAIL CONE EMERGENCY LIGHTS OUT. REPLACED BATTERIES AND PACKS, OPERATIONAL C HECK OK. 2 L 7 2 4F A6WE 1996060600218 19960606 00218 WP 1996 6 6 9611989605 1 19960524 A 3350 6014113 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 605NW 47223 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS AT ROWS 18 TO 21 AND AFT ENTRY INOPERATIVE. R EPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996060600219 19960606 00219 WP 1996 6 6 9611999154 1 19960530 A 3350 BATTERY PACK DOUG DC9 DC914 3022034 WP CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8913E 45830 DURING LINE CHECK, FOUND RIGHT EMERGENCY OVERWING EXIT LIGHT DOES NOT ILLUMINATE DURING TEST. RESEATED BATTERY PACK, OP ERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996060600220 19960606 00220 WP 1996 6 6 9612009995 1 19960529 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8978E 47327 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996060600221 19960606 00221 WP 1996 6 6 9612019922 1 19960529 A 3350 LIGHTS DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 945N 47664 DURING PREFLIGHT CHECK, FOUND FORWARD CABIN FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. EMERGENCY LIGHTS WERE CHECKED PER MAINTENANCE MANUAL, NO PROBLEMS WERE FOUND. 2 L 7 2 4F A6WE 1996060600222 19960606 00222 WP 1996 6 6 9612029905 1 19960529 A 3350 6011779 BATTERY PACK DOUG DC9 DC931 3022065 WP LT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 955N 47160 DURING PERIODIC CHECK, LEFT NACELLE EMERGENCY LIGHT FAILED TEN MINUTE TEST. REPLACED BATTERY PACK, OPERATIONAL CHECK NO RMAL. 2 L 7 2 4F A6WE 1996060600223 19960606 00223 WP 1996 6 6 9612039915 1 19960529 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 965N 47417 DURING LINE MAINTENANCE INSPECTION, FOUND CABIN CEILING EMERGENCY LIGHTS AT ROWS 14 THROUGH 19 INOPERATIVE. REPLACED BA TTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996060600224 19960606 00224 NM 1996 6 6 96FDEA01037 1 19960528 A 3260 INDICATOR BOEING 727 72722C 138400F NM NLG DOWN MALFUNCTIONED A FDEA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 25 107FE 19202 CYCLED THE GEAR 3 TIMES BEFORE NOSE GEAR IND DOWN. REMOVED AND REPLACED NLG POS PER MM 32-61-21, CYCLED GEAR PER 7-11-0 AND ALL IND NORMAL. 2 L 7 3 4F A3WE 1996060600225 19960606 00225 WP 1996 6 6 96FDEA01038 1 19960529 A 3260 INDICATION DOUG DC10 DC1030F 3023504 WP NLG MALFUNCTIONED A FDEA L ABORTED APPROACH N FALSE WARNING CL CLIMB 1 SO 25 302FE 46801 AFTER GO-AROUND, NOSE GEAR RED LIGHT ON AT BOTH PANELS WITH HANDLE UP, HYD SYS-3 NORMAL. PUT HANDLE DOWN AND BOTH LIGHT S GREEN ON NOSE GEAR. PERFORMED BITE CHECK ON PROXIMITY BOX, FOUND NO DEFECTS. PERFORMED GEAR RETRACTION TEST PER MM 3 2-60-00, UNABLE TO DUPLICATE PROBLEM. SWUNG GEAR 6 TIMES, OPS CK GOOD. 2 L 7 3 4F RT A22WE 1996060600226 19960606 00226 NM 1996 6 6 96FDEA01039 1 19960529 A 5320 691487112 SHEAR TIE BOEING 727 727227 1384078 NM BS 705 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 AFTER REMOVAL OF CRACKED LEVELING COMPOUND AT BS 705 STR 28 RT AND LT, FOUND FRAME SHEAR TIE CORRODED OUT OF LIMITS. RE MOVED CORRODED SHEAR TIE, CLEANED AND TREATED CORROSION ON EXTERNAL SKIN UNDER SHEAR TIE. FOUND SKIN TO BE WITHIN LIMIT S IAW FEDEX SRM 53-30-1, INSTALLED NEW SHEAR TIE. 2 L 7 3 4F A3WE 1996060600227 19960606 00227 NM 1996 6 6 96FDEA01040 1 19960529 A 5320 69144621 ANGLE BOEING 727 72725 1384006 NM BS 870 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 505FE 18276 WHILE WORKING ON NR0488, FOUND CORROSION ON SPLICE ANGLE AT BS 870 TERMINAL FITTING STR 9L FWD SIDE. REMOVED SPLICE ANG LE ON FWD SIDE OF 870 TERMINAL FITTING, STR 9L AND REPLACED PER FEDEX SRM 51-10-1. 2 L 7 3 4F A3WE 1996060600228 19960606 00228 NM 1996 6 6 96FDEA01043 1 19960529 A 5320 SHEAR TIE BOEING 727 727227 1384078 NM BS 950 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 CORROSION (C53-111-01(3), ON SHEAR TIE AT BS 950E LBL 9 WL 138 BETWEEN STR 28 TO 29L. REPAIRED SHEAR TIE PER FEDEX SRM 53-10-4. 2 L 7 3 4F A3WE 1996060600229 19960606 00229 NM 1996 6 6 96FDEA01044 1 19960529 A 5320 65317731 REINFORCE CHORD BOEING 727 727227 1384078 NM BS 1176.9 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 CORROSION ON BS 1176.9 REINFORCEMENT CHORD IS OUT OF LIMITS FROM LBL 47 TO 57 WL 208. REMOVED AND REPLACED DAMAGED REI NFORCEMENT CHORD FROM LBL TO RBL 65 STA 1176.9 WL 208. 2 L 7 3 4F A3WE 1996060600230 19960606 00230 NM 1996 6 6 96FDEA01045 1 19960429 A 5711 SPAR BOEING 727 72725C 138400H NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 120FE 19356 LT WING FRONT SPAR UPPER CHORD CRACKED ABOVE AND O/B OF NR 2 LE FLAP ACTUATOR. REMOVED CRACK, VOID IN CORROSION AND COR ROSION ABOVE AND O/B OF NR 2 LE FLAP ACTUATOR. INSTALLED REPAIR DOUBLER PER FEDEX EA 7-5710-28691 DATE 5-22-96. 2 L 7 3 4F A3WE 1996060600231 19960606 00231 NM 1996 6 6 96FDEA01046 1 19960430 A 5313 STRINGER BOEING 727 72725C 138400H NM BS 848-870 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 120FE 19356 CORROSION STA 6L STA 848 TO 870 UPPER LOBE. CUT CORROSION OUT, INSTALLED STR DOUBLER PER SRM 53-10-3 PG 5 TO 8. 2 L 7 3 4F A3WE 1996060600232 19960606 00232 NM 1996 6 6 96FDEA01048 1 19960528 A 5751 651926012 HINGE CASTING BOEING 727 72725C 138400H NM AILERON BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 136FE 19855 LARGE HINGE ASSEMBLY FOR LEFT HAND O/B AILERON HAS BAR BROKEN OFF. REMOVED HINGE CASTING AND INSTALLED A SERVICEABLE CA STING PER DRAWING NR 65-19260 SHEET 1. 2 L 7 3 4F A3WE 1996060600233 19960606 00233 NM 1996 6 6 96FDEA01049 1 19960528 A 5320 VERT ANGLE BOEING 727 72725C 138400H NM BS 1183 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 136FE 19855 VERT ANGLE CRACKED AT LIGHTENING HOLE AT BS 1183 RBL 26 TO 9 WL 253. PERFORMED 1183 VERTICAL BEAM MOD PER BOEING SERVIC E BULLETIN 727-53-0182 PG 23 SRM 53-10-9. 2 L 7 3 4F A3WE 1996060600234 19960606 00234 NM 1996 6 6 96FDEA01050 1 19960528 A 5320 FLOOR WEB BOEING 727 72725C 138400H NM BS 1178 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 136FE 19855 CABIN CORROSION ON FLOOR WEB STA 1178 APPROX 55 INCHES LBL UPPER SURFACE UNDER CHORD ANGLE. CUT OUT DAMAGED FLOOR WEB A REA, FABRICATED AND INSTALLED DOUBLER REPAIR PER SRM 51-40-2. 2 L 7 3 4F A3WE 1996060600235 19960606 00235 NM 1996 6 6 96FDEA01052 1 19960529 A 5270 DOOR SWITCH BOEING 727 72722 1384002 NM CARGO DOOR FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 189FE 19082 AT FLT LEVEL 310, MCD ANNUNCIATOR LIGHT ILLUMINATED. ACCOMPLISHED CHECKLIST AND DEPRESSURIZED A/C IN DESCENT. LIGHT RE MAINED ILLUMINATED UNTIL 2,000 FEET ABOVE GROUND LEVEL ON APPROACH, THEN WENT OUT. NO OTHER SYMPTOMS WERE NOTED, NO NOI SE OR LOSS OF PRESSURIZATION. A/C RELEASED FOR SERVICE PER MEL 52-4 CATEGORY A EXP 6-1-96. *S/D* FOUND SCREW GROUNDIN G OUT LOCK ROD WARNING SWITCH, FOUND SAME SWITCH BROKEN. REPLACED SCREW AND SWITCH, OPS CK GOOD PER MM 52-70-09. 2 L 7 3 4F A3WE 1996060600236 19960606 00236 NM 1996 6 6 96FDEA01055 1 19960530 A 2910 HYD LINE BOEING 727 72725C 138400H NM A-HYD SYST LEAKING A FDEA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 25 118FE 19300 HYDRAULIC SYSTEM-A FAILURE, QTY DROPPED TO ZERO, MANUALLY CRANKED GEAR DOWN. FLUID SHUTOFF VALVES OFF FOR 30 MINUTES PR IOR TO ENGINE SHUTDOWN. PARTS CATALOG 27-60-00 FIG 20 PG 1, FOUND HYD FLUID LEAKING FROM B-NUT TO T-FITTING NR 60 AND A SMALLER LEAK AT T-FITTING NR 65. REPLACED BOTH T-FITTINGS ALONG WITH HYD LINE NR 11A AND HYD LINE NR 3. REPLACED BOTH ENGINE DRIVEN PUMPS, REPLACED BOTH ASSOCIATED CASE DRAIN FILTERS, LEAK CHECKED HYD PUMPS AND ALL SPOILER RELATED LINES AND B-NUTS LEAK CHECKS GOOD. CYCLED ALL FLT CONTROLS FROM SYS-A AND SERVICED A-SYS HYD QTY. 2 L 7 3 4F A3WE 1996060600237 19960606 00237 NM 1996 6 6 96FDEA1041 1 19960529 A 5320 69144621 SPLICE ANGLE BOEING 727 72725 1384006 NM BS 870 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 505FE 18276 WHILE WORKING NR0488, FOUND CORROSION ON SPLICE ANGLE AFT SIDE BS 870 TERMINAL FITTING, STR 9L. REMOVED SPLICE ANGLE ON AFT SIDE OF BS 870 TERMINAL FITTING STR 9L AND REPLACED PER FEDEX SRM 51-10-1. 2 L 7 3 4F A3WE 1996060600238 19960606 00238 EU 1996 6 6 96UAL900368 1 19960530 A 3350 BATTERY PACK AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 406UA 454 AFT LEFT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. 2 L 7 2 4F RT A28NM 1996060600239 19960606 00239 NE 1996 6 6 96UAL900369 2 19960530 A 7230 55H005 COMPRESSOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 4 ENGINE FAILED A UALA C D F ABORTED TAKEOFF RETURN TO BLOCK ACTIVATE FIRE EXT. B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TO TAKEOFF 1 WP 29 171UA 24322 717692 WHEN TAKEOFF THRUST WAS SET HEARD LOUD BANG FROM RIGHT SIDE OF AIRCRAFT. SMOKE SEEN IN NR 4 ENGINE. FIRED BOTH BOTTLES TO ENGINE. *S/D* HIGH COMPRESSOR STG 5 BLADE FAILURE, NO EVIDENCE OF FIRE. REPLACED ENGINE. 2 L 7 4 4F 4 F RT A20WE E24NE 1996060600240 19960606 00240 NE 1996 6 6 96UAL900371 2 19960530 A 7230 COMPRESSOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT ENGINE FAILED A UALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 544UA 25322 726658 DURING TAKEOFF EXPERIENCED THREE COMPRESSOR STALLS FROM RIGHT ENGINE. AIRCRAFT RETURNED TO FIELD. *S/D* STALLS WERE T HE RESULT OF HIGH PRESSURE COMPRESSOR DAMAGE DUE TO A FAILED 9TH STAGE BLADE. ENGINE REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 1996060600241 19960606 00241 NM 1996 6 6 96UAL900372 1 19960530 A 3350 BATTERY PACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 580UA 26698 EMERGENCY LIGHT ABOVE SEATS 26ABC DOES NOT ILLUMINATE. REPLACED BATTERY PACK AT M10699 MODULE, OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996060600242 19960606 00242 NM 1996 6 6 96UAL900373 1 19960530 A 3350 BATTERY PACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 558UA 26654 EMERGENCY ESCAPE LIGHTS INOP BETWEEN ROWS 16 AND 32. REPLACED BATTERY PACK AT ROW 19, OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996060600243 19960606 00243 NM 1996 6 6 96UAL900374 1 19960530 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CARGO DOOR FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 580UA 26698 EXTERNAL EMERGENCY LIGHT INOP, RIGHT AFT CARGO DOOR. REPLACED LAMP, OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996060600244 19960606 00244 NM 1996 6 6 96UAL900375 1 19960530 A 3350 BATTERY PACK BOEING 737 737322 1384676 NM CABIN DISCHARGED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 337UA 24241 EMERGENCY ESCAPE PATH LIGHTING INOP IN FORWARD CABIN. REPLACED BATTERY PACK, CHECKS OK. 2 L 7 2 4F RT A16WE 1996060600245 19960606 00245 NM 1996 6 6 96UAL900376 1 19960530 A 3244 TIRE BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE LT MLG BLOW OUT A UALA A UNSCHED LANDING O OTHER TO TAKEOFF 1 WP 29 9030U 19068 LEFT OUTBOARD IN TIRE BLEW ON TAKEOFF, DID NOT RETRACT GEAR. REPLACED NUMBER ONE AND NUMBER TWO MAIN TIRES, CHECKS OK. 2 L 7 2 4F 4 F A16WE E2EA 1996060600246 19960606 00246 NM 1996 6 6 96UAL900377 1 19960530 A 2510 COFFEE WARMER BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE COCKPIT DIRTY A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 9002U 19040 CREW REPORT, AN ELECTRIC OVERHEAT SMELL IN THE COCKPIT WITH BOTH PACKS ON, STARTED EIGHT MINUTES AFTER TAKEOFF. *S/D* R EPLACED COALESCER BAGS. FOUND PLASTIC ON FORWARD COFFEE WARMER, REMOVED PLASTIC. RAN PACKS WITH ENGINE AND APU, NO SME LLS NOTED. 2 L 7 2 4F 4 F A16WE E2EA 1996060600247 19960606 00247 1996 6 6 96UAL900378 4 19960530 A 2565 SLIDE PACK AIRCRUISER 62771102 BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE DOOR 1R LOOSE A UALA K NONE O OTHER NR NOT REPORTED 1 WP 29 770UA 0020 26925 DOOR 1R SLIDE PACK FELL OUT AS DOOR 1R WAS OPENED. DOOR WAS IN THE DISARMED POSITION. *S/D* DOOR BEING USED FOR TRAIN ING WHEN SLIDE PACK FELL OFF DOOR AND LANDED ON BOTTLE. SLIDE AND BOTTLE RETURNED TO HOME SHOP FOR OVERHAUL. 2 L 7 2 4F 4 F RT T0001SE E46NE 1996060600248 19960606 00248 WP 1996 6 6 96UAL900379 1 19960530 A 2120 AIR DISTR DOUG DC10 DC1010 3022110 WP CABIN ODOR A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 1828U 46627 STRONG SMELL OF OIL THROUGHOUT THE CABIN. *S/D* RAN ENGINES AND COULD NOT DUPLICATE DISCREPANCY, NO REOCCURANCE. 2 L 7 3 4F A22WE 1996060600250 19960606 00250 NM 1996 6 6 96UAL900381 1 19960530 A 2611 824PTY SMOKE DETECTOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE RT LAV DAMAGED A UALA O OTHER L NO TEST NR NOT REPORTED 1 WP 29 7444U 21898 LAVATORY SMOKE ALARM DISCONNECTED IN FORWARD RIGHT HAND LAVATORY. *S/D* THE CAUSE OF THE FORWARD RIGHT HAND LAVATORY S MOKE DETECTOR BEING DISCONNECTED IS UNKNOWN. A NEW DETECTOR WAS INSTALLED AND IT CHECKED OK. 2 L 7 3 4F 4 F A3WE E2EA 1996060600251 19960606 00251 NM 1996 6 6 96UAL900382 1 19960530 A 3610 HOSE ASSY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 STRUT LEAKS A UALA O OTHER J WARNING INDICATION TO TAKEOFF 1 WP 29 7459U 21913 PER CREW DURING TAKEOFF, AT FULL POWER HAD NR 1 STRUT OVERHEAT LIGHT COME ON. REDUCED POWER AND LIGHT WENT OUT, CRUISE POWER OK. *S/D* REPLACED HOSE ASSEMBLY SECTION 58 STRUT EXHAUST LINE DUE TO LEAK. 2 L 7 3 4F 4 F A3WE E2EA 1996060600252 19960606 00252 NM 1996 6 6 96UAL900383 1 19960530 A 2750 65236132 TRANSMISSION BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE TE FLAPS WORN A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 7255U 21402 DIVERTED TO MIA DUE TO SPLIT FLAP INDICATION ON CLIMBOUT. *S/D* REPLACED RIGHT INBOARD FLAP TRANSMISSION DUE TO BINDIN G. 2 L 7 3 4F 4 F A3WE E2EA 1996060600253 19960606 00253 WP 1996 6 6 ABXA9600498 1 19960529 A 2510 56410321 SEAT DOUG DC8 DC862 3021970 WP FE POSITION UNLOCKED A ABXA K NONE O OTHER CR CRUISE 1 GL 23 802AX 46134 DURING CRUISE, FLIGHT ENGINEER'S SEAT DROPPED FROM THE MID VERTICAL RANGE TO THE LOWEST POSITION. INSPECTED AND LUBED T HE VERTICAL ADJUSTMENT MECHANISM OF THE FLIGHT ENGINEER'S SEAT, OPS CHECK GOOD. 2 L 7 4 4F 4A25 1996060600254 19960606 00254 WP 1996 6 6 ABXA9600499 1 19960529 A 2120 AIR DISTR DOUG DC8 DC863 302198A WP CABIN ODOR A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 23 819AX 45927 DURING CLIMB, AN ELECTRICAL BURNING SMELL WAS EMITTED FROM THE CTC CONTROL PANEL WHEN THE NR 1 AND NR 4 CTC'S WERE TURNE D ON. THE SMELL DISSIPATED AFTER THE CTC'S RAN FOR APPROXIMATELY 30 SECONDS. VISUALLY INSPECTED THE CTC'S AND NO DEFEC TS WERE NOTED. VISUALLY INSPECTED BEHIND THE CTC CONTROL PANEL FOR EVIDENCE OF BURNED WIRING OR SWITCHES AND NO DEFECTS WERE NOTED. OPERATED ALL FOUR CTC'S AND OPS CHECK WAS GOOD. NO EVIDENCE OF AN ELECTRICAL BURNING SMELL. 2 L 7 4 4F 4A25 1996060600255 19960606 00255 WP 1996 6 6 CALA9600664 1 19960510 A 5712 RIB DOUG DC9 DC982 3022082 WP WS 289 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18833 49493 INSPECTION FOUND A .5 INCH CRACK IN LT WING RIB AT XRS 289. A DOUBLER WAS INSTALLED IAW ECRA 5720-01521. 2 L 7 2 4F A6WE 1996060600256 19960606 00256 WP 1996 6 6 CALA9600665 1 19960507 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 100 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18833 49493 INSPECTION FOUND A .3125 INCH CRACK IN FUSELAGE SKIN AT NOSE WHEEL WELL RIGHT AFT DOOR AFT HINGE CUTOUT, STA 100. THE C RACK WAS STOPPED DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 53-05, FIGURE 62. 2 L 7 2 4F A6WE 1996060600257 19960606 00257 WP 1996 6 6 CALA9600666 1 19960510 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 196 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18833 49493 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 196. A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1996060600258 19960606 00258 WP 1996 6 6 CALA9600667 1 19960511 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 1155 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18833 49493 INSPECTION FOUND FLOOR SUPPORT CORRODED BETWEEN CENTER AND INBOARD SEAT TRACK AT STA 1155. A NEW FLOOR SUPPORT WAS FABR ICATED AND INSTALLED IAW SRM 51-10-3 AND 51-30-5. 2 L 7 2 4F A6WE 1996060600259 19960606 00259 WP 1996 6 6 CALA9600668 1 19960424 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1911 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68042 46901 INSPECTION FOUND FLOORBOARD SUPPORT CORRODED THROUGH AT STA 1911, LAV H AND J. THE FLOORBOARD SUPPORTS WERE REMOVED AND REPLACED IAW SRM 53-16-01, FIGURE 5F. 2 L 7 3 4F A22WE 1996060600260 19960606 00260 WP 1996 6 6 CALA9600669 1 19960424 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 879 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68042 46901 INSPECTION FOUND FORWARD CARGO FRAME CORRODED IN CHANNEL AT BASE OF FRAME, STA 879. THE FRAME WAS REPAIRED IAW ECRA 531 0-03264. 2 L 7 3 4F A22WE 1996060600261 19960606 00261 WP 1996 6 6 CALA9600670 1 19960422 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP FWD CARGO DR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68042 46901 INSPECTION FOUND FLOOR SUPPORT BEAM CORRODED AT FORWARD CARGO DOOR FORWARD JAMB. THE FLOOR SUPPORT BEAM WAS REPLACED IA W SRM 53-13-01 FIGURE 7 ITEM 6. 2 L 7 3 4F A22WE 1996060600262 19960606 00262 WP 1996 6 6 CALA9600671 1 19960423 A 5230 DOOR JAMB DOUG DC10 DC1030 3023501 WP FWD CARGO DR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14074 46911 INSPECTION FOUND FORWARD CARGO DOOR JAMB LOWER EDGE CORRODED. THE DOOR JAMB WAS REPAIRED IAW SRM 53-50-00, FIGURE 1. 2 L 7 3 4F A22WE 1996060600263 19960606 00263 NM 1996 6 6 P5CA9600240 1 19960530 A 5730 PANEL BOEING 747 747124 1384874 NM RT WING LE DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND RIGHT WING TOP LEADING EDGE AT NR 19 VARIABLE CAMBER FLAP WITH PREVIOUS COMPOSITE REPAIR CHIPPING AND ERODED. APP LIED NEW FIBERGLASS REPAIR IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1996060600264 19960606 00264 NM 1996 6 6 QXEA9600184 1 19960529 A 2730 8409 TRIM ACTUATORS DORNER DO32 DO328100 2996000 NM ELEVATOR TRIM FREEZING A QXEA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 09 336PH 3014 LEVELING AT FLIGHT LEVEL 310 FOUND ELEVATOR TRIMS INOP, TAT -37C. TRIMS BEGAN TO WORK DURING DESCENT, TAT -7C. AIRCRAF T LANDED IN GEG WITHOUT FURTHER PROBLEMS. LEFT AND RIGHT TRIM ACTUATORS REPLACED IAW MAINTENANCE MANUAL. ELEVATOR TRIM OPS CHECKED GOOD. 2 H 7 2 4T RT A45NM 1996060600265 19960606 00265 WP 1996 6 6 SCNA96150 1 19960523 A 2530 411001131 COFFEE MAKER DOUG DC10 DC1015 3022118 WP AFT GALLEY SMOKING A SCNA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 15 152SY 48289 AFT GALLEY LEFT HAND COFFEE MAKER STARTED SMOKING. PULLED CIRCUIT BREAKER AND SECURED AFT GALLEY BUS. REMOVED AND REPL ACED THE LEFT HAND AFT COFFEE MAKER. 2 L 7 3 4F A22WE 1996060600266 19960606 00266 WP 1996 6 6 9612049928 1 19960602 A 3260 UPLOCK SWITCH DOUG DC9 DC931 3022065 WP RT MLG MALFUNCTIONED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 8921E 45836 RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. RECYCLED GEAR WITH SAME RESULTS, FLIGHT CONT INUED TO DESTINATION AT 10,000 FEET AND 250 KNOTS AIRSPEED. MAINTENANCE PERFORMED GEAR SWING AND PROBLEM COULD NOT BE D UPLICATED. REPLACED RIGHT MAIN GEAR UPLOCK SWITCH AS A PRECAUTION. 2 L 7 2 4F A6WE 1996060600267 19960606 00267 1996 6 6 9612059910 4 19960602 A 3436 WINDSHEAR WARN DOUG DC9 DC931 3022065 WP COCKPIT ACTIVATED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 960N 47256 WINDSHEAR WARNING ACTIVATED DURING TAKEOFF ROLL. ABORTED TAKEOFF AT 110 KNOTS AND RETURNED TO GATE. MAINTENANCE DEFERR ED WINDSHEAR SYSTEM PER MEL 34-44A. 2 L 7 2 4F A6WE 1996060600268 19960606 00268 NM 1996 6 6 9612066628 1 19960601 A 3350 BATTERY PACK BOEING 747 747251B 1384892 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 628US 22389 DURING LINE CHECK, FOUND FOUR RIGHT OVERWING, TWO LEFT OVERWING AND E ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REP LACED BATTERY PACKS, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996060600269 19960606 00269 NM 1996 6 6 96FDEA01056 1 19960531 A 5320 WEB BOEING 727 727225 1384077 NM BS 950 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 468FE 21452 FOUND CORROSION UNDER LOWER DOOR STOP ON THE AFT CARGO DOOR FWD FRAME BS 950E WL 155. REPAIRED CORRODED FRAME AT BS 950 E WL 155 PER FEDEX EA 7-5310-28290. 2 L 7 3 4F A3WE 1996060600270 19960606 00270 NM 1996 6 6 96FDEA01057 1 19960531 A 5330 SKIN BOEING 727 72725 1384006 NM BS 1083-1086 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 505FE 18276 CORROSION (C53-224-04) ON INSIDE SKIN EMANATING FROM WINDOW FRAME AT BS 1083 TO 1086 STR 11L. REMOVED CORROSION FROM WI NDOW DOUBLER FOUND TO BE OUT OF LIMITS. THE SKIN AND FRAME WERE FOUND TO BE IN LIMITS. REPAIRED DOUBLER PER EA 7-5330- 28369. 2 L 7 3 4F A3WE 1996060600271 19960606 00271 NM 1996 6 6 96FDEA01058 1 19960531 A 5330 SKIN BOEING 727 72725 1384006 NM BS 1094 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 505FE 18276 CORROSION (C53-224-04) ON INSIDE OF SKIN EMANATING FROM WINDOW FRAME AT BS 1094, 4 INCHES ABOVE STR 11L. REMOVED CORROS ION FROM WINDOW DOUBLER, FOUND TO BE OUT OF LIMITS. REMOVED CORROSION FROM SKIN AND FRAME FOUND TUBE WITHIN LIMITS. RE PAIRED WINDOW FRAME DOUBLER PER EA 7-5330-28369. 2 L 7 3 4F A3WE 1996060600272 19960606 00272 NM 1996 6 6 96FDEA01059 1 19960531 A 5330 SKIN BOEING 727 727173C 1384059 NM BS 403 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 199FE 19509 DENT IN SKIN BS 403 BETWEEN STR 21 AND 22R. DENT FOUND TO BE OUT OF LIMIT PER FEDEX SRM 53-30-1. CUT OUT DAMAGE, FABRI CATED REPAIR PART, TREATED ALL BARE METAL AND INSTALLED ON SKIN AT BS 403 BETWEEN STR 21 AND 22R PER FEDEX SRM 53-30-3. 2 L 7 3 4F A3WE 1996060600273 19960606 00273 NM 1996 6 6 96FDEA01060 1 19960531 A 5300 SHEAR TIE BOEING 727 727173C 1384059 NM BS 328 CRACK A A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 199FE 19509 SHEAR TIE CRACKED STA 328 WL 231 BETWEEN STR 21 TO 13R, AREA MARKED. REMOVED CRACKED SHEAR TIE, FABRICATED NEW SHEAR TI E, TREATED ALL BARE METAL AND INSTALLED AT BS 328 WL 231 BETWEEN STR 12 TO13R PER FEDEX SRM 53-10-4. 2 L 7 3 4F A3WE 1996060600274 19960606 00274 WP 1996 6 6 CALA9600679 1 19960529 A 4930 M62452060143 FUEL LINE DOUG DC9 DC932 3022066 WP APU FCU LEAKING A CALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 69523 47520 A KEROSENE ODOR WAS SMELLED IN THE COCKPIT AND CABIN AFTER TAKEOFF FROM DFW. THE AIRCRAFT WAS RETURNED TO DFW WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND FUEL LINE TO APU FCU LEAKING. THE FUEL LINE WAS REMOVED AND REPLACED. THE APU WAS RUN WITH NO LEAKS OR ODOR OBSERVED. 2 L 7 2 4F A6WE 1996060600275 19960606 00275 NM 1996 6 6 CALA9600680 1 19960602 A 2612 896768 ELEMENT BOEING 737 7373T0 1384582 NM APU CONTAMINATED A CALA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 09 12327 23457 THE APU FIRE WARNING LIGHT ILLUMINATED WHILE EN ROUTE. THE APU FIRE BOTTLE WAS DISCHARGED AND THE LIGHT EXTINGUISHED. T HE AIRCRAFT WAS DIVERTED TO AUS WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THAT THE ELEVATOR PCU WAS LEAKING F LUID WHICH THEN DRIPPED ONTO FIRE LOOP OF APU EXHAUST DUCT. THE PCU WAS REPAIRED, APU FIRE EXTINGUISHING AND DETECTION SYSTEM WAS PLACARDED INOPERATIVE PENDING REPLACEMENT OF FIRE BOTTLE AND FIRE DETECTION ELEMENT DUE TO CONTAMINATION. 2 L 7 2 4F RT A16WE 1996060600276 19960606 00276 WP 1996 6 6 CALA9600681 1 19960601 A 3230 ROLLER DOUG DC10 DC1010 3022110 WP LG HANDLE BINDING A CALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 09 68046 47800 WHEN LANDING GEAR WAS EXTENDED ON APPROACH, NO GREEN GEAR LIGHTS WOULD ILLUMINATE. ABNORMAL PROCEDURES WERE COMPLIED WI TH AND A VISUAL INSPECTION CONFIRMED GEAR WAS EXTENDED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE GE AR HANDLE ROLLER JAMMED. THE ROLLER AND HANDLE MECHANISM WAS CLEANED AND OPERATION CHECKED GOOD. 2 L 7 3 4F A22WE 1996060600277 19960606 00277 WP 1996 6 6 CALA9600682 1 19960601 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP COCKPIT DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 34838 49634 INSPECTION FOUND COCKPIT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. THE BATTERY AND A BAD TERMINAL END WERE REPLACED AND OP ERATION OF THE LIGHTS WERE RESTORED. 2 L 7 2 4F A6WE 1996060600278 19960606 00278 WP 1996 6 6 CALA9600683 1 19960508 A 5350 CLIPS DOUG DC9 DC982 3022082 WP TAIL CONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18833 49493 THE TAIL CONE INTERIOR HANDLE PULL FROM CLIPS WAS 10 POUNDS. THE CLIPS WERE ADJUSTED IAW MM 53-53-00. 2 L 7 2 4F A6WE 1996060600279 19960606 00279 NM 1996 6 6 CALA9600684 1 19960520 A 5754 SKIN BOEING 737 7373T0 1384582 NM NR 1 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14342 23580 INSPECTION FOUND A 2.875 INCH CRACK IN NR 1 SLAT LOWER SKIN PANEL. A DOUBLER WAS INSTALLED IAW ECRA 5750-01159. 2 L 7 2 4F RT A16WE 1996060600280 19960606 00280 NM 1996 6 6 CALA9600685 1 19960520 A 5347 TRACK BOEING 737 7373T0 1384582 NM AFT CARGO WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14342 23580 INSPECTION FOUND A HOLE WORN THROUGH AFT CARGO FLOORBEAM TRACK ON LT SIDE. THE TRACK WAS REMOVED AND REPLACED IAW SRM 5 1-40-02. 2 L 7 2 4F RT A16WE 1996060600281 19960606 00281 NM 1996 6 6 CALA9600686 1 19960418 A 5330 SKIN BOEING 737 737217 1384464 NM BS 259-360 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND FUSELAGE SKIN DENTED FROM STA 259 TO 360, STRINGER 19R TO 24R. THE SKIN WAS REMOVED AND REPLACED IAW S RM 51-30-2. 2 L 7 2 4F A16WE 1996060600282 19960606 00282 NM 1996 6 6 CALA9600687 1 19960418 A 5330 SKIN BOEING 737 737217 1384464 NM BS 360-447 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND SKIN DENTED FROM STA 360 TO 447 RT SIDE, STRINGER 19R TO 25R. THE SKIN WAS REMOVED AND REPLACED IAW SR M 51-30-2. 2 L 7 2 4F A16WE 1996060600283 19960606 00283 NM 1996 6 6 CALA9600688 1 19960507 A 5313 STRINGER BOEING 737 737217 1384464 NM BS 727 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND STRINGER 22L CORRODED AT STA 727. THE CORRODED SECTION OF STRINGER WAS REMOVED. A NEW STRINGER AND SP LICE ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-10-3 AND 51-30-2. 2 L 7 2 4F A16WE 1996060600284 19960606 00284 NM 1996 6 6 CALA9600689 1 19960515 A 5311 FRAME BOEING 737 737217 1384464 NM BS 480 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND A 1 INCH AND 1.5 INCH CRACK IN FRAME AT STA 480 BETWEEN STRINGER 22L AND 23L. THE CRACKED FRAME SECTIO N WAS REMOVED, A NEW FRAME SECTION WAS FABRICATED AND INSTALLED IAW BOEING DRAWING NR 65C25113. 2 L 7 2 4F A16WE 1996060600285 19960606 00285 NM 1996 6 6 CALA9600690 1 19960423 A 5330 SKIN BOEING 737 737217 1384464 NM BS 328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND FUSELAGE SKIN AND FRAME SHEAR TIES CORRODED AT STA 328, STRINGER 18R. THE CORRODED AREAS OF SKIN AND S HEAR TIES WERE CUT OUT. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, SHEAR TIES WERE FABRICATED AN D INSTALLED IAW SRM 53-10-4. 2 L 7 2 4F A16WE 1996060600286 19960606 00286 NM 1996 6 6 CALA9600691 1 19960424 A 5330 SKIN BOEING 737 737217 1384464 NM BS 500 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 500A BELOW WINDOW BELT ON BOTH LEFT AND RIGHT HAND SIDE OF FUSELAGE. BOTH AREAS WERE REPAIRED IAW SRM 53-30-3. 2 L 7 2 4F A16WE 1996060600287 19960606 00287 NM 1996 6 6 CALA9600692 1 19960422 A 5210 SKIN BOEING 737 737217 1384464 NM L1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND A 1.5 INCH CRACK AT FASTENER HOLE OF L-1 DOOR LOWER SKIN. THE CRACKED SKIN WAS REMOVED, A FILLER AND D OUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 52-00-3 AND 51-30-2. 2 L 7 2 4F A16WE 1996060600288 19960606 00288 NM 1996 6 6 CALA9600693 1 19960506 A 5320 ANGLE BOEING 737 737217 1384464 NM BS 259 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND FRAME UPPER L-ANGLE AND WEB CORRODED AT BS 259, RT SIDE. THE L-ANGLE AND WEB WERE REMOVED AND REPLACED IAW SRM 51-40-2, 51-40-4, 51-30-2, 51-10-6 AND 51-10-2. 2 L 7 2 4F A16WE 1996060600289 19960606 00289 NM 1996 6 6 CALA9600694 1 19960507 A 5313 STRINGER BOEING 737 737217 1384464 NM BS 323 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND A .5 INCH CRACK AND CORROSION AT FASTENER HOLE OF STRINGER 26L, BS 323. THE CRACKED STRINGER WAS REMOV ED AND A NEW PART WAS INSTALLED IAW SRM 51-30-5 AND 51-10-2. 2 L 7 2 4F A16WE 1996060600290 19960606 00290 NM 1996 6 6 CALA9600695 1 19960507 A 5330 SKIN BOEING 737 737217 1384464 NM BS 188-251 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND SEVERAL CRACKS IN SECTION 41 FUSELAGE SKIN ON LT SIDE, BS 188 TO 251, WL 207 TO 234. THE CRACKS RANGED FROM .125 INCH TO .25 INCH IN LENGTH. THE CRACKED AREAS WERE CUT OUT, FILLERS AND DOUBLERS WERE FABRICATED AND INSTALL ED IAW EA 5310-01188 AND SRM 51-30-2. 2 L 7 2 4F A16WE 1996060600291 19960606 00291 NM 1996 6 6 CALA9600696 1 19960424 A 5320 INTERCOSTAL BOEING 737 737217 1384464 NM BS 500-500A CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL BETWEEN STA 500 AND 500A, STRINGER 26L. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW BOEING DRAWING 69-41473. 2 L 7 2 4F A16WE 1996060600292 19960606 00292 NM 1996 6 6 CALA9600697 1 19960429 A 5320 BEAM BOEING 737 737217 1384464 NM BS 540 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND VERTICAL BEAM CRACKED IN HALF AT BS 540, RBL 24.8. THE BEAM WAS REMOVED AND A NEW BEAM WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 57-10-2. 2 L 7 2 4F A16WE 1996060600293 19960606 00293 NM 1996 6 6 CALA9600698 1 19960507 A 5320 SPLICE BOEING 737 737217 1384464 NM BS 360 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND A 1.5 INCH CRACK IN STRINGER SPLICE AT STA 360, STRINGER 21R. THE SPLICE WAS REMOVED AND A NEW SPLICE WAS FABRICATED AND INSTALLED IAW SRM 53-10-3 AND 53-30-2. 2 L 7 2 4F A16WE 1996060600294 19960606 00294 NM 1996 6 6 CALA9600699 1 19960426 A 5311 FRAME BOEING 737 737217 1384464 NM BS 500 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND A 3 INCH CRACK AT NUTPLATE HOLE OF FRAME AT BS 500, LT SIDE. THE CRACKED FRAME SECTION WAS REMOVED AND A NEW FRAME SEGMENT WAS SPLICED IN IAW BOEING DRAWING 65C25113. 2 L 7 2 4F A16WE 1996060600295 19960606 00295 NM 1996 6 6 CALA9600700 1 19960507 A 5311 FRAME BOEING 737 737217 1384464 NM BS 500 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND A 1 INCH CRACK AT TWO NUTPLATE LOCATIONS ON FRAME AT BS 500, RT SIDE. THE CRACKED FRAME SEGMENT WAS RE MOVED AND REPLACED IAW BOEING DRAWING 65C25113. 2 L 7 2 4F A16WE 1996060600296 19960606 00296 SO 1996 6 6 COMA9610157 1 19960529 A 7170 1126005 CHECK VALVE EMB 120 EMB120RT SO RT ENGINE LEAKING A COMA K NONE K FLUID LOSS UK UNKNOWN 1 SO 01 196CA 120196 FUEL LEAKING FROM RT ENGINE NACELLE. REPLACED THE EPA TANK CHECK VALVE. 2 L 7 2 4T RT A31SO 1996060600297 19960606 00297 NE 1996 6 6 COMA9630117 2 19960601 A 7520 HEAT EXCHANGER SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LT ENGINE DIRTY A COMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 359CA 340A053 SMOKE SEEN COMING FROM LEFT ENGINE WHEN HIGH PRESSURE BLEED AIR IN USE. SMOKE CAUSED BY A DIRTY HEAT EXCHANGER. CLEANE D THE HP BLEED HEAT EXCHANGER AND ACFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE6 1996060600298 19960606 00298 EU 1996 6 6 COMA9630118 1 19960530 A 3231 55028J TELESCOPING ROD SAAB SF340 SF340A 7850100 EU RT MLG WORN A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 347CA 340A028 R MLG INBD GEAR DOOR WILL NOT STAY CLOSED. REPLACED THE GEAR DOOR QUICK RELEASE TELESCOPING ROD ASSY. 2 L 7 2 4T RT A52EU 1996060600299 19960606 00299 EA 1996 6 6 COMA9660099 1 19960529 A 3231 NAS620434D BOLT CNDAIR CL600 CL6002B19 EA NLG DOOR CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 940CA 7048 AIRCRAFT TAXIED TO HANGAR FOR SCHEDULED MAINTENANCE. UPON ARRIVAL MECHANICS NOTICED THE NOSE GEAR DOORS HANGING SLIGHTL Y OPEN WHEN AIRCRAFT WAS POWERED DOWN. FURTHER INVESTIGATION FOUND THE THROUGH-BOLT FOR THE NOSE GEAR FORWARD DOOR UPLO CK ROLLER LEVER ASSEMBLY CORRODED. THE CORROSION WAS NOT ALLOWING THE LEVER TO ROTATE FREELY, CAUSING THE ROLLER NOT TO PROPERLY ENGAGE IN THE CAM. THE LEVER AND MOUNT BRACKET WERE CLEANED AND LUBED, THE BOLT WAS REPLACED IPC REF: 32-22- 00, FIG 3 SHEET 1, ITEMS NR 310 AND 345. 2 L 7 2 4F RT A21EA 1996060600300 19960606 00300 WP 1996 6 6 MWEA96147 1 19960601 A 2560 5917689301 EVAC SLIDE COVER DOUG DC9 DC914 3022034 WP GALLEY DOOR FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 800ME 45842 CREW REPORTS, GALLEY DOOR EVACUATION SLIDE COVER FELL OFF. REINSTALLED GALLEY DOOR EVACUATION SLIDE COVER. 2 L 7 2 4F A6WE 1996060600301 19960606 00301 WP 1996 6 6 MWEA96148 1 19960601 A 5230 PAN DOUG DC9 DC932 3022066 WP FWD CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 DURING C-CK, FOUND FWD CARGO DOOR PAN CRACKED ON AFT SIDE AT DOOR LATCH CAM. REPAIRED CRACKED PAN IAW SRM 52-05, FIG 26 A. 2 L 7 2 4F A6WE 1996060600302 19960606 00302 WP 1996 6 6 MWEA96149 1 19960601 A 5522 SKIN DOUG DC9 DC932 3022066 WP RT ELEVATOR MISSING A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 DURING C-CHECK, FOUND 5 INCH BY 2 INCH PIECE OF SKIN MISSING FROM INBD UPPER END OF RT ELEVATOR. INSTALLED FLUSH REPAIR IAW SRM 55-01, PAGE 2. 2 L 7 2 4F A6WE 1996060600303 19960606 00303 WP 1996 6 6 MWEA96150 1 19960601 A 5320 JAMB DOUG DC9 DC932 3022066 WP CARGO DOOR DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 CONDITION 2 DENT ON FWD CARGO DOOR AFT JAMB AREA WHICH WAS ON MAINT CARRY OVER FOR 50 HR. REPAIRED IAW SRM 53-05, FIG 8 2. 2 L 7 2 4F A6WE 1996060600304 19960606 00304 NM 1996 6 6 P5CA9600241 1 19960530 A 5522 PANEL BOEING 747 747124 1384874 NM LT ELEVATOR DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND LEFT OUTBOARD ELEVATOR PANEL DAMAGED. REPAIRED PER SRM 51-40-04. 2 L 7 4 4F A20WE 1996060600305 19960606 00305 NE 1996 6 6 SWAA960471 2 19960527 A 7200 ENGINE BOEING 737 7372H4 138448C NM PWA JT8 JT8D9A 52048 NE NR 1 BIRD STRIKE A SWAA A UNSCHED LANDING C B F.O.D. SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 74SW 22674 IMMEDIATELY AFTER TAKEOFF, FELT AND HEARD LOUD BANG TO AIRCRAFT WITH ASSOCIATED FUMES IN COCKPIT. INSTRUMENTS REMAINED N ORMAL. AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. FOUND EVIDENCE OF BIRDSTRIKE TO NR 1 ENGINE INLET. PE RFORMED BIRDSTRIKE INSPECTION. NO DAMAGE NOTED. REPLACED CSD OIL COOLER AND RIGHT WATER SEPARATOR BAG. PERFORMED ENGIN E POWER ASSURANCE RUN. ALL PER BOEING M/M. 2 L 7 2 4F 4 F A16WE E2EA 1996060600306 19960606 00306 NM 1996 6 6 SWAA960472 1 19960530 A 7933 56B17D OIL TEMP SENSOR BOEING 737 7372H4 138448C NM NR 1 ENGINE MALFUNCTIONED A SWAA D E RETURN TO BLOCK ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SW 07 67SW 22356 EXPERIENCED NR 1 ENGINE HIGH OIL TEMPERATURE. CREW PERFORMED ENGINE SHUTDOWN PROCEDURES. AIRCRAFT RETURNED TO HOU AND MADE AN UNEVENTFUL LANDING. TROUBLESHOT, REPLACED MAIN OIL FILTER, DE-SERVICED OIL TO PROPER LEVEL, REMOVED AND REPLACE D OIL TEMPERATURE SENSOR, AND PERFORMED ENGINE POWER ASSURANCE RUN PER BOEING M/M. 2 L 7 2 4F A16WE 1996060600307 19960606 00307 EU 1996 6 6 96ZZZX2804 1 19960418 A 2730 7227705643 CONTROL CABLES SAAB SF340 340B 7860101 EU RT ELEVATOR CHAFED A PLGA K NONE O OTHER IN INSP/MAINT 1 NE 05 349BE 340B196 DURING ROUTINE C-CHECK INSPECTION, CHAFING WAS FOUND ON LEFT AND RIGHT ELEVATOR CONTROL CABLES BETWEEN FS 292.25 AND FS 630.0. CABLES WERE REPLACED AND RIGGED IAW SAAB MM CHAPTER 21-31-15. REF: OPERATOR CONTROL NR: PLG41896G1. 2 L 7 2 4T RT A52EU 1996060600308 19960606 00308 EU 1996 6 6 96ZZZX2805 1 19960418 A 2720 7227105571 CABLE ASSY SAAB SF340 340B 7860101 EU RUDDER CHAFED A PLGA K NONE O OTHER IN INSP/MAINT 1 NE 05 349BE 340B196 DURING ROUTINE C-CHECK INSPECTION, CHAFING FOUND ON 3 CONTROL CABLES IN RUDDER CIRCUIT 1, DUAL CONTROL RUN. CABLES WERE REPLACED AND RIGGED IAW SAAB MM CHAPTER 27-21-25. REF: OPERATOR CONTROL NR PLG41896G3. 2 L 7 2 4T RT A52EU 1996060600309 19960606 00309 NM 1996 6 6 CAL960556 1 19960505 A 2612 CONNECTOR BOEING 737 7373T0 1384582 NM NR 1 ENGINE CORRODED A CALA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 09 14335 23573 DFW - FLT 0624 - THE NR 1 ENGINE OVERHEAT ANNUNCIATOR LIGHT ILLUMINATED IN CRUISE FLIGHT, BUT EXTINGUISHED AFTER 10 SECO NDS. WHEN LIGHT CAME ON 2ND TIME, CREW DISENGAGED AUTOTHROTTLES AND SPLIT THROTTLE 74 PERCENT N1 AND 92 PERCENT N2. LI GHT CONTINUED TO GO OFF AND ON INTERMITTENTLY. NR 1 ENG WAS SHUT DOWN AND ACFT DIVERTED TO DFW WHERE IT LANDED WITHOUT INCIDENT. MX FND NR 1 ENGINE CORE FIRE LOOP CONNECTORS CORRODED. WIRE SIDE OF BOTH A AND B CONNECTORS CLEANED. UPPER AND LOWER LOOPS TESTED NORMAL. IN ADDITION, AFT CORE FIRE DETECTION LOOP A AND B WAS REMOVED ADN REPLACED. OPERATIONAL AND FUNCTIONAL CHECKS WERE GOOD. (X) 2 L 7 2 4F RT A16WE 1996060600310 19960606 00310 NM 1996 6 6 CAL960587 1 19960404 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18350 27296 23588 HOU - INSPECTION FOUND FLOOR BEAM INTERCOSTAL CORRODED JUST FORWARD OF STA 328 AT RBL 10. A NEW INTERCOSTAL WAS FABRICA TED AND INSTALLED IAW SRM 5310-03252. (X) 2 L 7 2 4F RT A16WE 1996060600311 19960606 00311 WP 1996 6 6 CAL960588 1 19960503 A 7830 5958782503 DRIVE LINK 591029425 DOUG DC9 DC932 3022066 WP LT ENG TR BROKEN A CALA K NONE J WARNING INDICATION LD LANDING 1 SW 09 19504 1525 47638 MTY - FLT 0705 - THE LEFT ENGINE REVERSE UNLOCK LIGHT ILLUMINATED ON LANDING AT MTY. MAINTENANCE FOUND A LEFT ENGINE TH RUST REVERSER DRIVE LINK BROKEN. THE DRIVE LINK REMOVED AND REPLACED. OPERATION CHECKED GOOD PER MM 78-31-5, PAGES 201 -207, FIGURE 201. (X) 2 L 7 2 4F A6WE 1996060600312 19960606 00312 NM 1996 6 6 CAL960589 1 19960404 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 312-328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18350 27296 23588 HOU - INSPECTION FOUND FLOOR BEAM INTERCOSTAL CORRODED BETWEEN STA 312 AND STA 328 AT LBL 10. A NEW INTERCOSTAL WAS FAB RICATED AND INSTALLED IAW ECRA 5310-03252. (X) 2 L 7 2 4F RT A16WE 1996060600313 19960606 00313 NM 1996 6 6 CAL960590 1 19960404 A 5511 SPAR CAP BOEING 737 7373T0 1384582 NM RT HORIZ STAB DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18350 27296 23588 HOU - INSPECTION FOUND IMPACT DAMAGE THREE FEET FROM OUTBOARD END OF RT HORIZONTAL STABILIZER UPPER AND LOWER SPAR CAPS. REPAIRS WERE PERFORMED IAW ECRA 5510-01327. (X) 2 L 7 2 4F RT A16WE 1996060600314 19960606 00314 NM 1996 6 6 CAL960595 1 19960513 A 3350 LIGHT BOEING 737 7373T0 1384582 NM CABIN LOOSE WIRE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14346 23584 IAH - FLT 1677 - INSPECTION FOUND EMERGENCY PATH LIGHTING AT FORWARD FIRST CLASS CLOSET INOPERATIVE. MAINTENANCE RECONN ECTED LOOSE WIRE ON CONNECTOR TO LIGHT ASSEMBLY. (X) 2 L 7 2 4F RT A16WE 1996060600315 19960606 00315 NM 1996 6 6 CAL960596 1 19960430 A 5730 PANEL BOEING 737 737291 138448W NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10251 70772 20361 GSO - INSPECTION FOUND A 1.5 INCH CRACK IN FORWARD OUTBOARD CORNER OF LT WING UPPER TRAILING EDGE PANEL FORWARD OF NR 4 SPOILER. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-30-2. (X) 2 L 7 2 4F A16WE 1996060600316 19960606 00316 NM 1996 6 6 CAL960597 1 19960430 A 5330 SKIN BOEING 737 737291 138448W NM BS 294.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10251 70772 20361 GSO - INSPECTION FOUND LT AFT CORNER OF NOSE WHEELWELL CUT-OUT EXTERNAL SKIN CORRODED AT STA 294.5. THE CORRODED AREA OF SKIN AND BEAR STRAP WERE CUT OUT. STRAP FILLER, SKIN FILLER, AND EXTERNAL DOUBLER WERE FABRICATED AND INSTALLED IAW SR M'S 53-30-3, 53-30-2, 51-30-2, 51-10-2, AND 51-10-6. (X) 2 L 7 2 4F A16WE 1996060600317 19960606 00317 NM 1996 6 6 CAL960598 1 19960428 A 5320 ANGLES BOEING 737 737291 138448W NM LT MLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10251 70772 20361 GSO - INSPECTION FOUND FOUR EACH ATTACH ANGLES CRACKED AT LT MLG STR 18A SHEAR BEAM. THE CRACKS MEASURED FROM 2 TO 5 IN CHES IN LENGTH. THE ANGLES WERE REMOVED AND NEW ANGLES WERE FABRICATED AND INSTALLED IAW ECRA 5310-03254. (X) 2 L 7 2 4F A16WE 1996060600318 19960606 00318 WP 1996 6 6 CAL960605 1 19960429 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 794 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12507 47799 47788 HOU - INSPECTION FOUND SKIN CORRODED IN AFT BAGGAGE BIN AT STA 794, LONGERON 30R. THE SKIN WAS REPAIRED IAW SRM 53-04, FIGURE 12B. (X) 2 L 7 2 4F A6WE 1996060600319 19960606 00319 WP 1996 6 6 CAL960606 1 19960424 A 5720 LE SPLICE DOUG DC9 DC932 3022066 WP WS 198 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12507 47799 47788 HOU - INSPECTION FOUND A 1 INCH CRACK IN RT WING LEADING EDGE SPLICE AT STA XFS 198 BETWEEN NR 3 AND NR 4 SLAT TRACK. T HE AREA WAS REPAIRED IAW ECRA 5710-01726. (X) 2 L 7 2 4F A6WE 1996060600320 19960606 00320 WP 1996 6 6 CAL960607 1 19960425 A 5320 591141237 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 465-484 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12507 47799 47788 HOU - INSPECTION FOUND INTERCOSTAL CORRODED FROM STA 465 TO STA 484 BETWEEN STR 29 AND STR 30L. THE INTERCOSTAL WAS REM OVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-30-2 AND SRM 51-60-0. (X) 2 L 7 2 4F A6WE 1996060600321 19960606 00321 NM 1996 6 6 CAL9690586 1 19960404 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 328-344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18350 27296 23588 HOU - INSPECTION FOUND FLOOR BEAM INTERCOSTAL CORRODED BETWEEN STA 328 AND STA 344 AT LBL 10. A NEW INTERCOSTAL WAS FAB RICATED AND INSTALLED IAW ECRA 5310-03252. (X) 2 L 7 2 4F RT A16WE 1996060600322 19960606 00322 WP 1996 6 6 CKSA96031 1 19960502 A 5730 5611290501 SKIN DOUG DC8 DC862F 3021972 WP LT WING CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 3931A 58215 45961 KOSC - FLT 72016 - DURING 'C-1' CHECK INSPECTION FOUND CARD NR 116L-0551 AREA LEFT WING LEADING EDGE; LEADING EDGE FORWA RD OF OUTBOARD SLOTS INBOARD END, GOUGED AND CORRODED. LEVEL 2 TASK NR 74937. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW DC-8, SRM 57-20. REPAIRED END OF LEADING EDGE OUTBOARD OF OUTBOARD SLOT INBOARD END IAW DC-8, SRM 57-2-1, P AGE 23. (X) 2 L 7 4 4F 4A25 1996060600323 19960606 00323 WP 1996 6 6 CKSA96032 1 19960502 A 5755 56551672 SPOILER DOUG DC8 DC862F 3021972 WP RT WING CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 3931A 58215 45961 KOSC - FLT 72016 - DURING 'C-1' CHECK INSPECTION FOUND NR 121R-0552 AREA RIGHT WING EXTERIOR; NR 3 SPOILER INBOARD END C AP CORRODED. LEVEL 2 TASK NR 59624. REMOVED NR 3 SPOILER IAW DC8 MM CHAPTER 27. REPAIRED AND INSTALLED NR 3 SPOILER P ANEL IAW DC8 MM CHAPTER 27-61-1. RIG AND OPS CHECK DUE. RIG AND OPS CHECK GOOD. (X) 2 L 7 4 4F 4A25 1996060600324 19960606 00324 WP 1996 6 6 CKSA96033 1 19960502 A 5320 3644423509 FITTING DOUG DC8 DC862F 3021972 WP BS 1120 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 3931A 58215 45961 KOSC - FLT 72016 - DURING 'C-1' INSPECTION FOUND CARD NR 559L-0552 AREA, LOWER SURFACE OF LT CUSP; CRACK IN FLOOR SUPPOR T FITTING AT LOWER CUSP LT SIDE STA 1120. LEVEL 2 TASK NR 60892. REMOVED AND REPLACED SHEAR TIE FITTING AS REQUIRED. I NSTALLED IAW SRM 51-1-20D AND SRM 51-1-21. (X) 2 L 7 4 4F 4A25 1996060600325 19960606 00325 WP 1996 6 6 CKSA96034 1 19960502 A 5320 45976431 FITTING DOUG DC8 DC862F 3021972 WP BS 620 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 3931A 58215 45961 KOSC - FLT 72016 - DURING 'C-1' CHECK INSPECTION FOUND, CARD NR 573L-0551 AREA, UPPER SURFACE OF LT CUSP; LT FRAME TO CU SP FITTING AT STA 620 CORRODED. LEVEL 2 TASK NR 73553. REMOVED AND REPLACED FITTING PER DC8 SRM 51-1-20D AND SRM 51-3- 0. (X) 2 L 7 4 4F 4A25 1996060600326 19960606 00326 WP 1996 6 6 CKSA96035 1 19960502 A 5320 45976431 FITTING DOUG DC8 DC862F 3021972 WP BS 600 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 3931A 58215 45961 KOSC - FLT 72016 - DURING 'C-1' CHECK INSPECTION FOUND, CARD NR 573L-0551 AREA, UPPER SURFACE OF LT CUSP, LT FRAME TO CU SP FITTING AT STA 600 CORRODED. LEVEL 2 TASK NR 73552. REMOVED AND REPLACED CUSP FITTING IAW DC-8 SRM'S 53-2-0, 51-1-2 0D, 51-1-3. (X) 2 L 7 4 4F 4A25 1996060600327 19960606 00327 WP 1996 6 6 CKSA96036 1 19960502 A 5320 37534881 FITTING DOUG DC8 DC862F 3021972 WP BS 640 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 3931A 58215 45961 KOSC - FLT 72016 - DURING 'C-1' CHECK INSPECTION FOUND CARD NR 573L-0551 AREA, UPPER SURFACE OF LT CUSP, LT FRAME TO CUS P FITTING AT STA 640 CORRODED. LEVEL 2 TASK NR 73562. REMOVED AND REPLACED FITTING IAW 51-1-20D. (X) 2 L 7 4 4F 4A25 1996060600328 19960606 00328 WP 1996 6 6 CKSA96037 1 19960502 A 5320 36519473 STIFFENER DOUG DC8 DC862F 3021972 WP BS 950 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 3931A 58215 45961 KOSC - FLT 72016 - DURING 'C-1' CHECK INSPECTION FOUND, CARD NR 574L-0551 AREA, LT MLG WHEELWELL, LT MLG WHEELWELL CEILI NG PANEL LONGITUDINAL STIFFENER EXFOLIATING CORROSION APPROXIMATELY STA 950, 3RD STIFFENER OUTBOARD FROM KEEL BEAM LEVE L 2 TASK NR 74823. REMOVED ALL CORROSION, CLEANED, TREATED AND PRIMED WITH REFERENCE TO 53-7-2. REPAIRED IAW SRM 53-2- 0. (X) 2 L 7 4 4F 4A25 1996060600329 19960606 00329 WP 1996 6 6 CKSA96038 1 19960502 A 5330 SKIN DOUG DC8 DC862F 3021972 WP BS 560 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 3931A 58215 45961 KOSC - FLT 72016 - DURING 'C-1' CHECK INSPECTION FOUND, CARD NR 5570-0551 AREA, FORWARD LOWER CARGO BILGE, FS 560 L35L, BULGE IN SKIN. LEVEL 2 TASK NR 59700. REMOVED CORRODED AREA AND INSTALLED REPAIR AS IT REQUIRED IAW DC-8 SRM 51-1-8. S KETCH NR AIA/E/2182 AND 8110-3. (X) 2 L 7 4 4F 4A25 1996060600330 19960606 00330 WP 1996 6 6 CKSA96040 1 19960502 A 5246 5756066 SERVICE PANEL DOUG DC8 DC862F 3021972 WP AFT ACCY COMPT CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 3931A 58215 45961 KOSC - FLT 72016 - DURING 'C-1' CHECK INSPECTION FOUND, CARD NR 5600-0551 AREA, AFT ACCESSORY COMPARTMENT, AFT LAVATORY WASTE DRAIN INNER SERVICE PANEL CORRODED. LEVEL 2 TASK NR 74998. REMOVED AND REPLACED INNER SERVICE PANEL AFT LAVATORY WASTE DRAIN IAW DC-8 SRM 53-2-0, SRM 51-3-0. TREATED AND PAINTED IAW DC-8 SRM 51-1-8. (X) 2 L 7 4 4F 4A25 1996060600331 19960606 00331 WP 1996 6 6 CKSA96041 1 19960502 A 5321 5772721356 FLOOR PLANK DOUG DC8 DC862F 3021972 WP BS 255 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 3931A 58215 45961 KOSC - FLT 72016 - DURING 'C-1' CHECK INSPECTION FOUND, CARD NR 5670-0551 AREA, GALLEY (ANY LOCATION) FS 255 LBL FLOOR P LANK CORROSION LEVEL 2 TASK NR 61938. REMOVED CORROSION, TREATED AND PRIMED AS IT REQUIRED PER IAW DC-8 SRM 51-1-8, AND INSTALLED REPAIR ACCORDING TO IAW DC-8, SRM 53-2-3. (X) 2 L 7 4 4F 4A25 1996060600332 19960606 00332 WP 1996 6 6 CKSA96042 1 19960502 A 5321 5772721207 FLOOR PLANK DOUG DC8 DC862F 3021972 WP BS 255 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 3931A 58215 45961 KOSC - FLT 72016 - DURING 'C-1' CHECK INSPECTION FOUND, CARD NR 5670-0551 AREA, GALLEY (ANY LOCATION) FS 255 LBL 29 FLOO R PLANK CORRODED. LEVEL 2 TASK NR 61940. REMOVED CORROSION, TREATED AND PRIMED AS IT REQUIRED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-8 AND SRM 53-2-3. (X) 2 L 7 4 4F 4A25 1996060600333 19960606 00333 WP 1996 6 6 CKSA96043 1 19960502 A 5532 5647795501 SKIN DOUG DC8 DC862F 3021972 WP VERT STAB CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 3931A 58215 45961 KOSC - FLT 72016 - DURING 'C-1' CHECK INSPECTION FOUND, CARD NR 6000-0551 AREA, AFT FUSELAGE/VERTICAL STABILIZER, VERTIC AL STABILIZER SKIN LEFT SIDE APPROXIMATELY STA XR230 TO XR310 AFT SPAR AREA CORRODED AND SEPARATING. LEVEL 2 TASK NR 61 998. RESEALED BONDED SKIN IAW SRM 51-1-9. REPAIRED CORRODED AREA WITH SCARF DOUBLER IAW SRM 55-2-1. (X) 2 L 7 4 4F 4A25 1996060600334 19960606 00334 WP 1996 6 6 CKSA96044 1 19960502 A 5532 564779637 SKIN DOUG DC8 DC862F 3021972 WP VERT STAB CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 3931A 58215 45961 KOSC - FLT 72016 - DURING 'C-1' CHECK INSPECTION FOUND, CARD NR 6000-0551 AREA, AFT FUSELAGE/VERTICAL STABILIZER SKIN SE PARATING AND CORRODED, VERTICAL STABILIZER RIGHT SIDE APPROXIMATELY STA XR284 TO XR230 AFT SPAR AREA. LEVEL 2 TASK NR 6 1999. REPLACED UPPER RIGHT SKIN PANEL ON VERTICAL STABILIZER IAW SRM 55-2-0. (X) 2 L 7 4 4F 4A25 1996060600335 19960606 00335 WP 1996 6 6 CKSA96045 1 19960502 A 5530 56121618 ANGLE DOUG DC8 DC862F 3021972 WP VERT STAB CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 3931A 58215 45961 DURING 'C-1' CHECK INSPECTION FOUND, CARD NR 6000-0551 AREA, AFT FUSELAGE/VERTICAL STABILIZER. VERTICAL STABILIZER TO F USELAGE ATTACH ANGLE RIGHT SIDE HAS STRESS CRACKS AND CORROSION. LEVEL 2 TASK NR 74799. CLEANED CORROSION AND FOUND TO BE OUT OF LIMITS. NO STRESS CRACKS FOUND. REPAIRED AREAS IN ATTACH ANGLE IAW DC-8 SRM 53-2-5, FIGURE 16A 51-1-20D. T REATED AND PAINTED IAW DC-8 SRM 51-1-8. (X) 2 L 7 4 4F 4A25 1996060600336 19960606 00336 WP 1996 6 6 CKSA96046 1 19960502 A 5530 56121619 ANGLE DOUG DC8 DC862F 3021972 WP VERT STAB CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 3931A 58215 45961 KOSC - FLT 72016 - DURING 'C-1' CHECK INSPECTION FOUND, CARD NR 6000-0551 AREA, AFT FUSELAGE/VERTICAL STABILIZER. VERTI CAL STABILIZER TO FUSELAGE ATTACH LEVEL 2 TASK NR 74798. REPAIRED VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE IAW DC-8 SRM 53-2-5, FIGURE 16A, 51-1-20D. (X) 2 L 7 4 4F 4A25 1996060600337 19960606 00337 WP 1996 6 6 CKSA96047 1 19960502 A 5350 56563502 FILLET PANEL DOUG DC8 DC862F 3021972 WP WING/FUS DELAMINATED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 3931A 58215 45961 DOSC - FLT 72016 - DURING 'C-1' CHECK INSPECTION FOUND, TASK NR 59644 PANEL 262F DELAMINATION. FABRICATED NEW PANEL IAW AIA SKETCH AIA/E/2188 AND INSTALLED. (X) 2 L 7 4 4F 4A25 1996060600338 19960606 00338 WP 1996 6 6 CKSA96048 1 19960502 A 5330 SKIN DOUG DC8 DC862F 3021972 WP BS 490 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 3931A 58215 45961 KOSC - FLT 72016 - DURING 'C-1' CHECK INSPECTION FOUND TASK NR 59699 FS 490 L35R, BULGE IN SKIN. REMOVED FASTENERS AND CUT OUT CORROSION. REPAIRED IAW SKETCH NR A1A/3/2180 PER 8110-3. (X) 2 L 7 4 4F 4A25 1996060600339 19960606 00339 WP 1996 6 6 CKSA96049 1 19960502 A 5540 564411081 STIFFENER DOUG DC8 DC862F 3021972 WP RUDDER CHAFED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 3931A 58215 45961 KOSC - FLT 72016 - DURING 'C-1' CHECK INSPECTION FOUND, TASK NR 61961 RUDDER, STIFFENER CHAFED AT TOP OF NR 2 HINGE CUT -OUT. REPAIRED CHAFED STIFFENER PER AIA SKETCH AIA/E/2315 AND 8110-3. (X) 2 L 7 4 4F 4A25 1996060600340 19960606 00340 1996 6 6 CKSA96050 4 19960406 A 2360 56559422 DOUBLER DOUG DC8 DC861 3021952 WP RT ELEVATOR CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 24UA 42965 45963 SPLP - FLT 73216 - DURING 'C-2' CHECK INSPECTION FOUND, CARD NR 378R-0551 AREA, RT ELEVATOR AND TAB. RT ELEVATOR, STATI C DISCHARGER DOUBLER HAS LEVEL 2 CORROSION. DISCREPANCY RECORD SHEET NR 3009. REMOVED, TREATED AND CONTROLLED CORROSION AT AFFECTED AREA AS REQUIRED PER SRM 51-1-8. (X) 2 L 7 4 4F 4A25 1996060600341 19960606 00341 NM 1996 6 6 EIAA9611644 1 19960510 A 8012 PRESSURE SWITCH BOEING 747 747212B 1384886 NM NR 3 ENGINE FAILED A EIAA E ENGINE SHUTDOWN J WARNING INDICATION IN INSP/MAINT 1 NM 09 485EV 20712 JED - ON CRUISE FLIGHT, NR 3 ENGINE START VALVE LIGHT ILLUMINATED. NR 3 ENGINE SHUT DOWN PER EIA PROCEDURES. CONFIRME D PRESSURE SWITCH AT FAULT. START VALVE OPS CHK OK. DEFERRED PRESSURE SWITCH PER MEL 80-1-1. REPLACED NR 3 ENGINE STAR T VALVE AS A PRECAUTIONARY MEASURE. AT JFK, PRESSURE SWITCH WAS REPLACED. REF: CONTROL NR 96-12. (X) 2 L 7 4 4F A20WE 1996060600342 19960606 00342 NM 1996 6 6 EIAA9611648 1 19960512 A 8012 START VALVE BOEING 747 747212B 1384886 NM NR 3 ENGINE FAILED A EIAA E ENGINE SHUTDOWN J WARNING INDICATION IN INSP/MAINT 1 NM 09 485EV 20712 JFK - FLT 310 - NR 3 START VALVE OPEN LIGHT ILLUMINATED. ACCOMPLISHED ABNORMAL PROCEDURE, ENGINE SHUT-DOWN. WHEN ENGIN E WAS THROTTLED BACK, ENGINE STALLED. NO ABNORMAL EGT EXCURSIONS NOTED. OCCURRED ABOUT 1.20 EPR. REMOVED AND REPLACED ENGINE NR 3 START VALVE AND PRESSURE SWITCH PER MM 80-11-80. OPS CHECK GOOD. PERFORMED ENGINE INSPECTION PER MM 71-00 -43. PERFORMED BORESCOPE INSPECTION PER 72-00-00. PERFORMED WINDMILLING INSPECTION PER 72-00-00. ENGINE OPS CHECK GOO D PER 71-00-00. CHECKED MAIN OIL FILTER AND CHIP DETECTOR. FOUND OK. ENGINE START VALVE LIGHT DEFERRED PER MEL 80-1. REF: CONTROL NR 96-13. (X) 2 L 7 4 4F A20WE 1996060600344 19960606 00344 WP 1996 6 6 HAL9661 1 19960512 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 669HA 47654 HNL - FLT 98 - EMERGENCY OVERHEAD LIGHTS INOPERATIVE AFT OF ROW 22. REPLACED BATTERY. OPS CHECK GOOD. (X) 2 L 7 2 4F A6WE 1996060600345 19960606 00345 WP 1996 6 6 HAL9663 1 19960513 A 2150 PACK DOUG DC9 DC951 3022051 WP CABIN SMOKING A HALA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 13 669HA 47654 HNL - FLT 514 - SMOKE IN COCKPIT AND CABIN. FOUND RT A/C PACK TEMP CONTROL ON FULL HOT POSITION. SELECTED FULL COLD PO SITION, RAN PACKS. OPS CHECK NORMAL. NO SMOKE NOTED. (VAPOR) 2 L 7 2 4F A6WE 1996060600346 19960606 00346 EU 1996 6 6 PLG41396G1 1 19960413 A 3060 666000219 BRUSH BLOCK SAAB SF340 340B 7860101 EU LT PROPELLER WORN A PLGA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 NE 05 352BE 445 DM35 340B239 LGA/PWM - FLT 4796 - RETURNED TO LGA DUE TO FAILURE OF THE LEFT PROPELLER HEAT, LANDING WITHOUT INCIDENT. MAINTENANCE W AS DISPATCHED TO THE AIRCRAFT AND REMOVED AND REPLACED BRUSH BLOCK ASSEMBLY. GROUND RUN CHECKED GOOD, AND AIRCRAFT RETU RNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1996060600347 19960606 00347 EU 1996 6 6 PLG41896G1 1 19960418 A 2730 7227105711 CONTROL CABLES SAAB SF340 340B 7860101 EU LT ELEVATOR CHAFED A PLGA K NONE O OTHER IN INSP/MAINT 1 NE 05 349BE 340B196 DURING ROUTINE C-CHECK INSPECTION, CHAFING WAS FOUND ON LEFT AND RIGHT ELEVATOR CONTROL CABLES BETWEEN FS 292.25 AND FS 630.0. CABLES WERE REPLACED AND RIGGED IAW SAAB MM CHAPTER 21-31-15. REF: OPERATOR CONTROL NR: 96ZZZX2804. (X) 2 L 7 2 4T RT A52EU 1996060600348 19960606 00348 EU 1996 6 6 PLG41896G2 1 19960418 A 2720 7227105581 CABLE ASSY SAAB SF340 340B 7860101 EU RUDDER CHAFED A PLGA K NONE O OTHER IN INSP/MAINT 1 NE 05 349BE 340B196 DURING C-CHECK INSPECTION, CHAFING FOUND ON TWO AFT CABLES IN RUDDER CIRCUIT 1. CABLES WERE REPLACED AND RIGGED IAW SAA B MM CHAPTER 27-21-25. (X) 2 L 7 2 4T RT A52EU 1996060600349 19960606 00349 EU 1996 6 6 PLG41896G3 1 19960418 A 2720 7227105561 CABLE ASSY SAAB SF340 340B 7860101 EU RUDDER CHAFED A PLGA K NONE O OTHER IN INSP/MAINT 1 NE 05 349BE 340B196 DURING ROUTINE C-CHECK INSPECTION, CHAFING FOUND ON 3 CONTROL CABLES IN RUDDER CIRCUIT 1, DUAL CONTROL RUN. CABLES WERE REPLACED AND RIGGED IAW SAAB MM CHAPTER 27-21-25. REF: OPERATOR CONTROL NR 96ZZZX2805. (X) 2 L 7 2 4T RT A52EU 1996060600350 19960606 00350 EU 1996 6 6 PLG41896G4 1 19960418 A 2710 7227105622 CABLE ASSY SAAB SF340 340B 7860101 EU AILERON CHAFED A PLGA K NONE O OTHER IN INSP/MAINT 1 NE 05 349BE 340B196 DURING ROUTINE C-CHECK INSPECTION, CHAFING FOUND ON RIGHT FORWARD CONTROL CABLE IN AILERON CIRCUIT IN FUSELAGE. CABLE W AS REPLACED AND RIGGED IAW SAAB MM CHAPTER 27. (X) 2 L 7 2 4T RT A52EU 1996060600351 19960606 00351 EU 1996 6 6 PLG41896G5 1 19960418 A 5321 FLOOR SAAB SF340 340B 7860101 EU COCKPIT CORRODED A PLGA K NONE O OTHER IN INSP/MAINT 1 NE 05 349BE 340B196 DURING ROUTINE C-CHECK INSPECTION, CORROSION FOUND ON FLOOR UNDER PILOT AND COPILOT'S FLOOR MATS. CORROSION REMOVED AN D DAMAGE REPAIRED IAW SAAB SRM CHAPTER 51. (X) 2 L 7 2 4T RT A52EU 1996060600352 19960606 00352 EU 1996 6 6 PLG41896G6 1 19960418 A 5321 FLOOR SAAB SF340 340B 7860101 EU BS 235-292.25 CORROSION A PLGA K NONE O OTHER IN INSP/MAINT 1 NE 05 349BE 340B196 DURING ROUTINE C-CHECK INSPECTION, CORROSION FOUND ON STRUCTURE UNDER GALLEY FLOOR AREA. MAINTENANCE REMOVED CORROSION AND REPAIRED DAMAGE IAW SAAB SRM CHAPTER 51. MAINTENANCE TREATED AND REPAINTED IAW SAAB SRM CHAPTER 51. (X) 2 L 7 2 4T RT A52EU 1996060600353 19960606 00353 EU 1996 6 6 PLG42296G1 1 19960422 A 3240 7229161027 TUBE SAAB SF340 340B 7860101 EU RT TE FLAP CHAFED A PLGA K NONE K FLUID LOSS IN INSP/MAINT 1 NE 05 362BE 340B291 DURING PRE-FLIGHT INSPECTION, THE CREW NOTED A PUDDLE OF HYDRAULIC FLUID UNDER THE RT MLG (AIRCRAFT HAD BEEN PARKED FOR APPROXIMATELY 2.5 HRS WITH BRAKE SETS). MAINTENANCE WAS CALLED TO THE AIRCRAFT. MAINTENANCE INVESTIGATION DETERMINED T HE FLUID LEAK WAS COMING FROM THE RT NACELLE FLAP COVE AREA. FURTHER INVESTIGATION FOUND A BRAKE LINE WITH A PIN HOLE C HAFE IN AT A PHENOLIC CLAMP. MAINTENANCE REPAIRED THE LINE AND RETURNED THE AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 1996060600354 19960606 00354 EU 1996 6 6 PLG42496G1 1 19960424 A 3150 005W500 WEU SAAB SF340 340B 7860101 EU AVIONICS RACK FAILED A PLGA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NE 05 352BE 1102 340B239 LGA/ROC - FLT 4704 - EXPERIENCED A CONFIG WARNING AND WEU STATUS LIGHT. THE AIRCRAFT RETURNED TO LGA LANDING WITHOUT IN CIDENT. LGA MAINTENANCE REMOVED AND REPLACED THE WEU. ALL CHECKS WERE GOOD, AND AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1996060600355 19960606 00355 EU 1996 6 6 PLG42696G1 1 19960426 A 3030 856ML2 PITOT HEAT SAAB SF340 SF340A 7850100 EU RT FUSELAGE FAILED A PLGA A UNSCHED LANDING O OTHER CR CRUISE 1 NE 05 743BA 81929 340A093 LGA/ROC - FLT 4715 - DURING FLIGHT, THE RIGHT PITOT HEAT FAILED. THE AIRCRAFT RETURNED TO LGA LANDING WTHOUT INCIDENT. LGA MAINTENANCE REMOVED AND REPLACED THE PITOT TUBE AND RETURNED THE AIRCRAFT TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1996060600356 19960606 00356 CE 1996 6 6 PLG4296DG1 1 19960402 A 5270 MS250081 SWITCH BEECH 1900 1900C 1154161 CE PASSENGER DOOR DEFECTIVE A PLGA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NE 05 3068M UB69 BOS - FLT 4532 - AFTER TAKEOFF, CREW NOTICED A FORWARD CABIN DOOR WARNING LIGHT ILLUMINATE. AIRCRAFT RETURNED TO BOS WI THOUT INCIDENT. MAINTENANCE WAS DISPATCHED AND DETERMINED MICROSWITCH ON DOOR TO BE BAD. AFTER ENSURING CABIN DOOR CAN BE CLOSED AND LOCKED, WARNING SYSTEM WAS DEFERRED PER MEL. AIRCRAFT WAS THEN RETURNED TO SERVICE AND OPERATED UNDER ME L. (X) 2 L 7 2 4T RT A24CE 1996060600357 19960606 00357 CE 1996 6 6 PLG51296G1 1 19960501 A 2841 FUEL QTY IND BEECH 1900 1900C 1154161 CE RIGHT FAILED A PLGA O OTHER O OTHER CR CRUISE 1 NE 05 15486 UC131 ALB/LGA - FLT 4652 - IN CRUISE, CREW NOTICED RIGHT FUEL QUANTITY INDICATOR SLOWLY DROPPING. AIRCRAFT DECLARED AN EMERGE NCY AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED AND INSPECTED AIRCRAFT. NO LEAKS WERE NOTED. FUELED AIRCR AFT AND REINSPECTED, NO LEAKS NOTED. MEL'D RIGHT FUEL QUANTITY INDICATOR. AIRCRAFT RETURNED TO SERVICE. THIS SDR IS O PEN PENDING REPAIR. (X) 2 L 7 2 4T RT A24CE 1996060600358 19960606 00358 EU 1996 6 6 PLG5196G1 1 19960501 A 2913 PUMP SAAB SF340 SF340A 7850100 EU HYDRAULIC SYSTEM FAILED A PLGA O OTHER O OTHER AP APPROACH 1 NE 05 340BE 340A062 SYR/BOS - FLT 4372 - ON APPROACH, THE HYDRAULIC SYSTEM FAILED TO PRESSURIZE IN BOTH NORMAL AND OVERRIDE MODES. THE CREW HAND PUMPED THE SYSTEM TO MAINTAIN SYSTEM PRESSURE AND LANDED WITHOUT INCIDENT. BOS MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT AND REPLACED THE HYDRAULIC PUMP AND MOTOR ASSEMBLY AND RETURNED THE AIRCRAFT TO SERVICE. FAILURE OCCURRED IN T HE ELECTRIC MOTOR. THIS SDR WILL REMAIN OPEN PENDING A TEAR DOWN REPORT. (X) 2 L 7 2 4T RT A52EU 1996060600359 19960606 00359 CE 1996 6 6 PLG5696G1 1 19960506 A 3230 571302 POWER PACK MOTOR BEECH 1900 1900C 1154161 CE WING ROOT FAILED A PLGA O OTHER O OTHER CR CRUISE 1 NE 05 31240 UC28 ALB/LGA - FLT 4657 - DURING CRUISE, THE 2-AMP LANDING GEAR RELAY CIRCUIT BREAKER TRIPPED. ON APPROACH, THE CREW RESET T HE CIRCUIT BREAKER, WHICH TRIPPED AGAIN. THE CREW PERFORMED A MANUAL GEAR EXTENSION LANDING IN LGA WITHOUT INCIDENT. M AINTENANCE WAS DISPATCHED TO THE AIRCRAFT. TROUBLESHOOTING DETERMINED THE LANDING GEAR MOTOR HAD SHORTED INTERNALLY. M AINTENANCE REPLACED THE MOTOR AND RETURNED THE AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A24CE 1996060600360 19960606 00360 1996 6 6 TC8A96043 4 19960505 A 3421 CONNECTOR DOUG DC8 DC8F54 3021926 WP LT HORIZON GYRO LOOSE A TC8A K NONE J WARNING INDICATION IN INSP/MAINT 1 GL 23 802CK 45679 SBBG/SBBG - FLR 12403 - ON TAXI, CAPTAIN'S HORIZON GYRO FLAG INDICATED. TROUBLESHOT SYSTEM, FOUND LOOSE CANNON PLUG, RE SET AND RE-TIGHTENED. OPS CHECKS OK. (X) 2 L 7 4 4F 4A25 1996060600361 19960606 00361 EU 1996 6 6 9612073220 1 19960531 A 5220 ACCESS COVER AIRBUS 320 A320211 3930320 EU EMER EXIT DOOR FELL OFF A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 320US 213 DURING TAKEOFF AT 80 KNOTS, THE LEFT FORWARD EMERGENCY EXIT DOOR WARNING LIGHT ILLUMINATED. ABORTED TAKEOFF WITHOUT FUR THER INCIDENT. REINSTALLED THE ACCESS COVER, DOOR WARNING CHECKED OK. 2 L 7 2 4F RT A28NM 1996060600362 19960606 00362 NM 1996 6 6 9612082255 1 19960602 A 8012 START VALVE BOEING 727 727251 138408H NM PWA JT8 JT8D7B 52053 NE NR 1 ENGINE FAILED A NWAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 01 255US 19974 654058 DURING CRUISE FLIGHT, THE NR 1 ENGINE START VALVE LIGHT CAME ON. NR 1 ENGINE SHUT DOWN. AIRCRAFT COMPLETED SCHEDULED F LIGHT TO DTW AND LANDED WITHOUT FURTHER EVENT. ENGINE WINDMILL INSPECTION C/W, MAIN OIL STRAINER AND MAG PLUGS CHECKED OK. STARTER, START CONTROL VALVE, START VALVE PRESSURE SWITCH AND START CONTROL PANEL WERE ALL REPLACED. ENGINE WAS GR OUND RUN AND FOUND SERVICEABLE. 2 L 7 3 4F 4 F A3WE E2EA 1996060600363 19960606 00363 WP 1996 6 6 9612099604 1 19960531 A 3350 FUSE DOUG DC9 DC932 3022066 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 604NW 47222 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN FLOOR PROXIMITY EMERGENCY LIGHTING INOPERATIVE. REPLACED BLOWN FUSE AT RIGHT FORWARD GALLEY DOOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996060600364 19960606 00364 WP 1996 6 6 9612109604 1 19960601 A 3350 FUSE DOUG DC9 DC932 3022066 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 604NW 47222 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD LEFT LOWER EMERGENCY EXIT SIGN INOPERATIVE. REPLACED BLOWN FUSE AT PO WER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996060600365 19960606 00365 WP 1996 6 6 9612119986 1 19960601 A 3350 60030451 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 986US 47480 DURING PERIODIC CHECK, FOUND MID CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996060600366 19960606 00366 WP 1996 6 6 9612129981 1 19960602 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 994Z 47097 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPER ATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996060600367 19960606 00367 WP 1996 6 6 9612139981 1 19960602 A 3350 60030451 POWER SUPPLIES DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 994Z 47097 DURING LINE MAINTENANCE INSPECTION, FOUND AFT CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLIES, OPE RATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996060600368 19960606 00368 WP 1996 6 6 9612149960 1 19960601 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 920RW 47163 DURING PERIODIC CHECK, FOUND FORWARD CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996060600369 19960606 00369 EU 1996 6 6 9612153223 1 19960602 A 2150 757A000009 ACM AIRBUS 320 A320211 3930320 EU FUSELAGE FAILED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 323US 272 DURING CRUISE AT FL390, NOTICED SMOKE AND SMELLED FUMES IN COCKPIT AND CABIN. THE AIRCRAFT DIVERTED TO DEN WHERE AN EME RGENCY WAS DECLARED AND AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE REPLACED THE RIGHT AIR CYCLE MACHINE, OPERA TIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996060600370 19960606 00370 EU 1996 6 6 9612163226 1 19960602 A 3350 321430 BATTERY AIRBUS 320 A320211 3930320 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 326US 282 DURING LINE MAINTENANCE, THE EMERGENCY LIGHTS TEST FAILED THE LEFT FORWARD BATTERY. REPLACED BATTERY PACK, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996060600371 19960606 00371 EU 1996 6 6 9612173227 1 19960601 A 3350 321454 POWER SUPPLY AIRBUS 320 A320211 3930320 EU CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 327NW 11303 6912 297 DURING LINE MAINTENANCE, THE EMERGENCY LIGHTS TEST FAILS THE AFT LEFT POWER SUPPLY UNIT. REPLACED EPSU, OPERATIONAL CHE CK OK. 2 L 7 2 4F RT A28NM 1996060600372 19960606 00372 WP 1996 6 6 ABXA9600500 1 19960531 A 5610 591297756 WINDOW TRIM DOUG DC8 DC862 3021970 WP RT CV WINDOW OUT OF POSITION A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 804AX 45987 FIRST OFFICER'S CLEARVIEW WINDOW WOULD NOT OPEN COMPLETELY. REPOSITIONED WINDOW TRIM AROUND THE FIRST OFFICER'S CLEARVI EW WINDOW, OPS CHECK GOOD. 2 L 7 4 4F 4A25 1996060600373 19960606 00373 WP 1996 6 6 ABXA9600501 1 19960603 A 3260 7000010101 SWITCH DOUG DC8 DC863 302198A WP RT MLG DEFECTIVE A ABXA O OTHER P NO WARNING INDICATION DE DESCENT 1 GL 23 813AX 46136 DURING DESCENT, RIGHT MAIN LANDING GEAR DOWNLOCK LIGHT DID NOT ILLUMINATE AFTER THE LANDING GEAR WAS EXTENDED. RECYCLED THE LANDING GEAR AND RIGHT MAIN LANDING GEAR DOWNLOCK LIGHT ILLUMINATED AFTER APPROXIMATELY TWO MINUTES. REPLACED RIGH T MAIN LANDING GEAR DOWNLOCK SWITCH, CLEANED THE DOWNLOCK SWITCH ELECTRICAL CONNECTOR AND LUBRICATED THE LANDING GEAR. O PS CHECKED LANDING GEAR IAW DC8 MM AND ALL INDICATIONS WERE NORMAL. 2 L 7 4 4F 4A25 1996060600374 19960606 00374 NE 1996 6 6 COMA9610158 3 19960601 A 6110 PROPELLER EMB 120 EMB120RT SO HAMSTD 14RF 14RF9 NE LT ENGINE LEAKING A COMA K NONE K FLUID LOSS TX TAXI/GRND HDL 1 SO 01 205CA 120205 901111 LEFT ENGINE LEAKED A LARGE AMOUNT OF OIL DURING TAXI FROM HANGAR TO GATE. REPLACED THE LT PROPELLER ASSY. 2 L 7 2 4T RT A31SO 6 C P11NE 1996060600375 19960606 00375 SO 1996 6 6 COMA9610159 1 19960601 A 3233 ACTUATOR EMB 120 EMB120RT SO LT MLG OUT OF ADJUST A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 246CA 120223 WHEN LANDING GEAR SELECTED UP, THE LT MLG REMAINED DOWN FOR 5 MINUTES BEFORE RETRACTING. ADJUSTED RETRACT ACTUATOR TO M /M SPECIFICATIONS AND ACFT RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 1996060600376 19960606 00376 SO 1996 6 6 COMA9610160 1 19960531 A 2913 MPEV30082B HYDRAULIC PUMP EMB 120 EMB120RT SO LEFT FAILED A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 241CA 12320 3651 120211 GREEN HYDRAULIC SYSTEM ELECTRIC PUMP, FAILED. REPLACED THE GREEN SYSTEM ELECTRIC HYDRAULIC PUMP. 2 L 7 2 4T RT A31SO 1996060600377 19960606 00377 SO 1996 6 6 COMA9610161 1 19960601 A 5415 12007901001 FITTING EMB 120 EMB120RT SO LT NACELLE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 248CA 120228 LT NACELLE FLAP HINGE ATTACH FITTING FOUND CRACKED DURING INSPECTION. REPLACED CRACKED FITTING. 2 L 7 2 4T RT A31SO 1996060600378 19960606 00378 NE 1996 6 6 COMA9630119 2 19960602 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LEFT FAILED A COMA D RETURN TO BLOCK B K SMOKE/FUMES/ODORS/SPARKS FLUID LOSS TX TAXI/GRND HDL 1 SO 01 347CA 340A028 367513 CONTROL TOWER REPORTED BLUE SMOKE COMING FROM LEFT ENGINE. ACFT RETURNED TO GATE. REPLACED THE LEFT ENGINE. 2 L 7 2 4T 4 T RT A52EU E8NE6 1996060600379 19960606 00379 EA 1996 6 6 COMA9660100 1 19960531 A 2750 601R931057 SENSOR CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTION A COMA K NONE N FALSE WARNING CR CRUISE 1 SO 01 945CA 4898 1753 7069 FLAPS FAILED DURING CRUISE. REPLACED THE FLAP BRAKE AND POSITION SENSOR. 2 L 7 2 4F RT A21EA 1996060600380 19960606 00380 NM 1996 6 6 UPS96220248 1 19960531 A 2170 WATER SEP BAG BOEING 727 72730C 1384009 NM LT PACK DIRTY A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SO 01 919UP 19012 DIRTY WATER SEPARATOR BAG CAUSING ODOR IN FLIGHT DECK. REPLACED BAG. 2 L 7 3 4F A3WE 1996060600381 19960606 00381 WP 1996 6 6 UPS96820247 1 19960519 A 3260 SWITCH DOUG DC8 DC873F 302199F WP LT MLG MALFUNCTIONED A IPXA O OTHER N FALSE WARNING LD LANDING 1 SO 01 819UP 46019 LEFT MLG GEAR SAFE LT INOP. CYCLED GEAR SEVERAL TIMES, NO HELP. RELAMPED AND NO HELP. PERFORMED EMERGENCY PROCEDURES AND LANDED. GEAR WAS PINNED AND AIRCRAFT MOVED OFF TAXIWAY. T/S TO BAD LT MLG DOWN LIMIT SWITCH. SWAPPED PINS TO AUX CONTACTS IN MLG DOWN LIMIT S/W. LIGHT THEN CHECKED NORMAL. PLACED ITEM ON LT MLG DOWN LIMIT SWITCH FOR REPLACEMENT ITE M DEFERRED REF NR D110662. 2 L 7 4 4F RT 4A25 1996060600382 19960606 00382 NE 1996 6 6 96ZZZX2806 2 19960405 A 7250 414129001 ROTOR ASSY BOLKMS 117 BK117A1 5626010 EU LYC LTS101 LTS101650B1 41560 NE POWER TURBINE BLADE SHIFT A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 128HH 486 SC47026 7036 LE45195E FAILED SB LT101-72-10-0153. EXCESSIVE IBPT BLADE SHIFT NR 10, -0.012 INCH. REPLACED WITH USED UNIT CORRECTED PROBLEM. PART TOTAL CYCLES, 1,475.7. 1 G 7 2 3U 3 U H13EU E5NE 1996060600383 19960606 00383 NE 1996 6 6 96ZZZX2807 2 19960501 A 7230 430404701 SEAL BOLKMS 117 BK117A1 5626010 EU LYC LTS101 LTS101650B1 41560 NE NR 1 BEARING LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 128HH 2 6J015 7036 LE45254E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1996060600384 19960606 00384 NE 1996 6 6 96ZZZX2808 2 19960501 A 7230 430150601 SEAL BOLKMS 117 BK117A1 5626010 EU LYC LTS101 LTS101650B1 41560 NE NR 2 BEARING LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 128HH 2 055 7036 LE45254E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1996060600385 19960606 00385 NE 1996 6 6 96ZZZX2809 2 19960501 A 7250 430144801 SEAL BOLKMS 117 BK117A1 5626010 EU LYC LTS101 LTS101650B1 41560 NE NR 3 BEARING LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 128HH 2 8F951363 7036 LE45254E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1996060600386 19960606 00386 NE 1996 6 6 96ZZZX2810 2 19960301 A 7250 414129001 ROTOR ASSY BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE POWER TURBINE BLADE SHIFT A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 420MB 1794 462 SC17081 7077 LE45282E FAILED SB LT101-72-10-0153. EXCESSIVE IBPT BLADE SHIFT NR 25 +0.012 INCH. NR 24 +0.012 INCH. REPLACED WITH USED UNIT, CORRECTED PROBLEM. PART TOTAL CYCLES, 3,601.2. 1 G 7 2 3U 3 U H13EU E5NE 1996060600387 19960606 00387 NE 1996 6 6 96ZZZX2811 2 19960501 A 7230 430124202 BEARING BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE COMP NR 1 PLATING WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 417BK 649 3525 7143 LE45593EF BEARING PLATING WORN OR PEELING OFF. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1996060600388 19960606 00388 NE 1996 6 6 96ZZZX2812 2 19960501 A 7230 430135703 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE NR 2 BEARING LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 417BK 750 549 7143 LE45506EF SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1996060600389 19960606 00389 NE 1996 6 6 96ZZZX2813 2 19960501 A 7250 430144801 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE NR 3 BEARING LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 417BK 70 1190681 7143 LE45506EF SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1996060600390 19960606 00390 NE 1996 6 6 96ZZZX2814 2 19960501 A 7250 410106701 SEAL RING BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE 1ST TURB SHROUD WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 417BK 750 7143 LE45506EF SEAL RING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1996060600391 19960606 00391 EU 1996 6 6 96ZZZX2815 1 19960328 A 6730 AC67246 SERVO DUNLOP SNIAS 350 AS350B2 8680813 EU FORE/AFT LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 96LG 199 29 QN025 2817 SERVO LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996060600392 19960606 00392 NE 1996 6 6 96ZZZX2816 2 19960501 A 7250 410106701 SEAL RING BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE 1ST TURB SHROUD WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 417BK 649 7143 LE45593EF SEAL RING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1996060600393 19960606 00393 NE 1996 6 6 96ZZZX2817 2 19960501 A 7210 430125301 BEARING BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE RED GEARBOX WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 5188B 945 7163 LE45518EF BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW 6 EACH UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1996060600394 19960606 00394 NE 1996 6 6 96ZZZX2818 2 19960501 A 7230 430135703 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE NR 2 BEARING LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 5188B 748 652 7163 LE45518EF SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1996060600395 19960606 00395 EU 1996 6 6 96ZZZX2819 1 19960301 A 5350 350A58010403 COWLING SNIAS 350 AS350B2 8680813 EU M/R GEARBOX CRACKED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 6099P 578 2818 COWLING CRACK AT UPPER REAR OUTBOARD FASTENER HOLE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996060600396 19960606 00396 NE 1996 6 6 96ZZZX2820 2 19960405 A 7250 414129001 ROTOR ASSY BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE POWER TURBINE BLADE SHIFT A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 7060G 720 347 SC47041 7173 LE45511EF FAILED SB LT101-72-10-0153. EXCESSIVE IBPT BLADE SHIFT NR 23, .0105 INCH, NR 15, .0195 INCH. REPLACED WITH USED UNIT, CORRECTED PROBLEM. PART TOTAL CYCLES, 1,423.5. 1 G 7 2 3U 3 U H13EU E5NE10 1996060600397 19960606 00397 NE 1996 6 6 96ZZZX2821 2 19960405 A 7250 430144801 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE NR 3 BEARING LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 7060G 347 33429 7173 LE45511EF SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1996060600399 19960606 00399 NE 1996 6 6 96ZZZX2823 2 19960501 A 7250 43044801 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE NR 3 BEARING LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 71703 327 07901335 7227 LE45509EF SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1996060600400 19960606 00400 NE 1996 6 6 96ZZZX2824 2 19960501 A 7230 430150601 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE NR 2 BEARING LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 71703 327 621 7227 LE45509EF SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1996060600401 19960606 00401 WP 1996 6 6 96ZZZX2825 1 19960309 A 2913 AS6641LS666 HYDRAULIC PUMP DOUG DC9 DC932 3022066 WP LT ENGINE FAILED A VJ6A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 965VV 47202 IAD/IAD - FLT 287 - AIR RETURN, LEFT ENGINE DRIVEN HYDRAULIC PUMP FAILED AFTER TAKEOFF. ABNORMAL PROCEDURES FOLLOWED. R EPLACED LEFT ENGINE DRIVEN HYDRAULIC PUMP PER MM 29-10-05. OPERATIONAL AND LEAK CHECK OK. SERVICED HYDRAULIC SYSTEM. 2 L 7 2 4F A6WE 1996060600402 19960606 00402 NM 1996 6 6 96ZZZX2826 1 19960220 A 3150 EICAS WARNING ELDEC BOEING 767 767216 1385124 NM COCKPIT MALFUNCTIONED A RJEF A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 23 762TA 7038 202 23623 SAL/GUA/LAX - FLT 510 - EN ROUTE, AFTER ONE HOUR AND FORTY MINTUES OF FLIGHT THE EICAS DISPLAYED THE FOLLOWING MESSAGES: PROBE HEAT, LND GEAR MONITOR, NOSE AIR/GND DISAGREE, GROUND SPOILERS. ALSO, THE FOLLOWING LIGHTS CAME ON AT THE UPPER PANEL: AUX PITOT, CAP PITOT, TAT. DUE TO THIS SITUATION, ACFT LANDED IN MEX. DURING GROUND INSPECTION, A BITE TEST W AS PERFORMED SO ALL FAULT MESSAGES WERE RESET PER MM 32-09-03 AND MM 30-31-00. THEREAFTER, AN ENGINE RUNNING WAS PERFOR MED AND VERIFIED NORMAL SYSTEMS OPERATION. AIRPLANE RETURNED TO NORMAL OPERATION THROUGH LAX. 2 L 7 2 2F RT A1NM 1996060600403 19960606 00403 NM 1996 6 6 96ZZZX2827 1 19960207 A 3242 26088127 BRAKE ASSY BOEING 767 7673S1 1385211 NM MLG DEFECTIVE A RJEF K NONE O OTHER IN INSP/MAINT 1 SO 23 769TA 4773 28 B4383 26608 THE BRAKE, PN 2608812-7, SN B4383, CAME FROM AVIALL ON FEBRUARY 5TH, AND INSTALLED THE NEXT DAY ON N769TA. DURING OPERT ION OF FEBRUARY 6TH HERE AT THIS STATION, RECEIVED A FAX MESSAGE FORWARDED FROM AVIALL INFORMING THIS BRAKE HAS A FAILUR E. FAILURE CONSISTED OF A MISSING INSULATOR, PN 2609326, AT ONE OF THE PISTONS ON CONTACT WITH PRESSURE PLATE, PN 26012 466-630. AT LAX, DEFECTIVE BRAKE DEFERRED AND ACFT CONTINUED OPERATION THROUGH SAL. AFTER ACFT ARRIVAL, DAMAGED BRAKE REPLACED BY NEW ON 2-7-96, WHICH WAS SENT AND OVERHAULED BY AVIALL. 2 L 7 2 4F RT A1NM 1996060600404 19960606 00404 NM 1996 6 6 96ZZZX2828 1 19960329 A 3260 DOOR LIGHT BOEING 767 767231 1385131 NM NLG MALFUNCTIONED A TWAA O OTHER N FALSE WARNING CL CLIMB 1 CE 05 604TW 22567 SJU - FLT 11 - DURING CLIMB, A NOSE GEAR DOOR LIGHT FAULT INDICATION WAS OBSERVED. NOSE GEAR PROXIMITY SWITCHES WERE CH ECKED, OPERATION NORMAL. OP-15 - 12-29-95 - SEA. 2 L 7 2 4F RT A1NM 1996060600405 19960606 00405 WP 1996 6 6 96ZZZX2829 1 19960322 A 3260 833703 PROX SWITCH DOUG DC9 DC983 3022083 WP NLG FAILED A TWAA O OTHER N FALSE WARNING CR CRUISE 1 CE 05 9405T 53141 STL FLT 467 - DURING CRUISE, RED NOSE LANDING GEAR UNSAFE LIGHT ILLUMINATED. FOUND INTERNAL MALFUNCTION IN NLG PROXIMI TY SWITCH, MFG PN 8-337-03. REPLACED NLG PROXIMITY SWITCH AND NLG INDICATION, CHECKED NORMAL. CHECK C-1D - 12-4-95 - J FK. 2 L 7 2 4F RT A6WE 1996060600406 19960606 00406 WP 1996 6 6 96ZZZX2830 1 19960215 A 5315 AFA00433 FLOOR BEAM DOUG DC10 DC1010 3022110 WP BS 1701 CRACKED B ZJ4R K NONE O OTHER IN INSP/MAINT 1 SO 13 910SF 46524 DURING CHECK STA 1701 FLOOR BEAM LBL 39, FOUND AFT SIDE UPPER PORTION CORRODED AND CRACKED. INSTALLED NEW FLOOR BEAM IA W LACI E.O. 3523. 2 L 7 3 4F A22WE 1996060600407 19960606 00407 WP 1996 6 6 96ZZZX2831 1 19960227 A 5320 AFA3932 JAMB DOUG DC10 DC1010 3022110 WP FS 1731 CORROSION B ZJ4R K NONE O OTHER IN INSP/MAINT 1 SO 13 910SF 46524 DURING CHECK, LOWER AFT CARGO DOOR LOWER DOOR JAMB FITTING FORWARD SECTION HAS INTERGRANULAR EXFOLIATED CORROSION. REPA IRED IAW LACI E.O. 3538 AND SRM 51-21-0. 2 L 7 3 4F A22WE 1996060600408 19960606 00408 SO 1996 6 6 96ZZZX2832 1 19960501 A 2710 12027655007 CONTROL CABLE EMB 120 EMB120RT 3260202 SO LT WING AILERON WORN A MASA K NONE O OTHER IN INSP/MAINT 1 SW 01 271YV 7495 120271 DURING A 1600-HOUR CONTROL CABLE INSPECTION, FOUND LEFT WING LOWER AILERON CABLE, PN 120-27655-007, WORN WITH BROKEN STR ANDS WHERE CABLE PASSES THROUGH NYLON GROMMET ON BOTH INBOARD AND OUTBOARD NACELLE STRUCTURE. 2 L 7 2 4T RT A31SO 1996060600409 19960606 00409 SO 1996 6 6 96ZZZX2833 1 19960501 A 2710 12027655029 CONTROL CABLE EMB 120 EMB120RT 3260202 SO RT WING AILERON WORN A MASA K NONE O OTHER IN INSP/MAINT 1 SW 01 271YV 7495 120271 DURING A 100-HOUR CONTROL CABLE INSPECTION, FOUND RIGHT WING LOWER AILERON CABLE, PN 120-27655-029, WORN WITH BROKEN STR ANDS WHERE CABLE PASSES THROUGH NYLON GROMMET ON BOTH INBOARD AND OUTBOARD NACELLE STRUCTURE. 2 L 7 2 4T RT A31SO 1996060600410 19960606 00410 SO 1996 6 6 96ZZZX2834 1 19960501 A 2710 12027655005 CONTROL CABLE EMB 120 EMB120RT 3260202 SO LT WING AILERON WORN A MASA K NONE O OTHER IN INSP/MAINT 1 SW 01 271YV 7495 120271 DURING A 1600-HOUR CONTROL CABLE INSPECTION, FOUND LEFT WING LOWER AILERON CABLE, PN 120-27655-005, WORN WITH BROKEN STR ANDS WHERE CABLE PASSES THROUGH NYLON GROMMET ON BOTH INBOARD AND OUTBOARD NACELLE STRUCTURE. 2 L 7 2 4T RT A31SO 1996060600411 19960606 00411 SO 1996 6 6 96ZZZX2835 1 19960501 A 2710 12027655031 CONTROL CABLE EMB 120 EMB120RT 3260202 SO RT WING AILERON WORN A MASA K NONE O OTHER IN INSP/MAINT 1 SW 01 271YV 7495 120271 DURING A 1600-HOUR CONTROL CABLE INSPECTION, FOUND RIGHT WING UPPER AILERON CABLE, PN 120-27655-031, WORN WITH BROKEN ST RANDS WHERE CABLE PASSES THROUGH NYLON GROMMET ON BOTH INBOARD AND OUTBOARD NACELLE STRUCTURE. 2 L 7 2 4T RT A31SO 1996060600418 19960606 00418 1996 6 6 96ZZZX2842 4 19960318 A 3454 5224280101 RECEIVER DOUG DC9 DC921 302205A WP NR 2 NAV INOPERATIVE A VJ6A A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 11 128NK 47307 MEM/MCO - FLT 373 - DIVERTED TO ATL, NR 2 EGT AND NAV REC WENT INOP. EGT CHECKED GOOD ON RUN-UP CHECK FOR SERVICE. REM OVED AND REPLACED NR 2 NAV-REC, OPS CHECK IAW 34-40. 2 L 7 2 4F A6WE 1996060600419 19960606 00419 WP 1996 6 6 96ZZZX2843 1 19960322 A 7722 BALANCE RESISTOR DOUG DC9 DC921 302205A WP NR 2 ENGINE OUT OF TOLERANCE A VJ6A C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 11 128NK 47307 BOS/BOS - FLT 361 - ABORTED TAKEOFF, NR 2 ENGINE EGT WAS ERRATIC. THE NR 2 ENGINE EGT GAUGE STOPS AT APPROXIMATELY 350 DEGREES WHEN TAKEOFF POWER WAS APPLIED. 2 L 7 2 4F A6WE 1996060600420 19960606 00420 WP 1996 6 6 96ZZZX2844 1 19960322 A 3520 90000200712 OXY REGULATOR DOUG DC9 DC932 3022066 WP CABIN FAILED A VJ6A G O2 MASK DEPLOYED O OTHER CR CRUISE 1 SO 11 916VV 47445 ATL/CMH - FLT 274 - ALL THE PASSENGER MASKS DEPLOYED IN-FLIGHT. PERFORMED DROP AND LEAK CHECK, FOUND THE PASSENGER OXYG EN REGULATOR LEAKING. REMOVED AND REPLACED REGULATOR PER MM 35-20, OPS CHECK GOOD, NO LEAKS NOTED. 2 L 7 2 4F A6WE 1996060600422 19960606 00422 WP 1996 6 6 96ZZZX2846 1 19960225 A 3320 CIRCUIT BREAKER DOUG DC9 DC932 3022066 WP CABIN TRIPPED A VJ6A O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 11 939VV 47089 WHILE SITTING AT GATE IN MCO MAKING PA ANNOUNCEMENTS, THE CIRCUIT BREAKER'S FOR PA, INTERPHONE, 'NO SMOKING' AND 'FASTEN SEAT BELT' LIGHTED SIGNS TRIPPED. SMOKE SMELL IN THE CABIN. ACCOMPLISHED VALUJET AIRLINES EO DC-9-3396005, SEAT BELT, NO SMOKING SIGN, PASSENGER WARNING SYSTEM WIRING. 2 L 7 2 4F A6WE 1996060600423 19960606 00423 WP 1996 6 6 96ZZZX2847 1 19960410 A 3230 BYPASS HANDLE DOUG DC9 DC932 3022066 WP LANDING GEAR OUT OF POSITION A VJ6A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 946VV 47226 ATL/ATL - FLT 110 - AIR RETURN, LANDING GEAR WOULD NOT RETRACT. FOUND GEAR BYPASS HANDLE DOWN. REPLACED RIGHT MAIN GEA R DOOR AND LEFT GEAR DOOR BUMPER. RESET BYPASS HANDLE, OPS CHECK NORMAL. 2 L 7 2 4F A6WE 1996060600424 19960606 00424 WP 1996 6 6 96ZZZX2848 1 19960328 A 2912 AC7031H8K1 HYD FILTER DOUG DC9 DC932 3022066 WP RIGHT CUT PACKING A VJ6A O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 SO 11 946VV 47226 MCO/IAD - FLT 470 - ON LANDING, RIGHT HYDRAULIC FLUID WAS LOST. AIRCRAFT TURNED OFF RUNWAY ONTO TAXIWAY, GEAR PINS INST ALLED. REPLACED HYDRAULIC FILTER ASSEMBLY AND CUT PACKING. LEAK CHECKS OK. 2 L 7 2 4F A6WE 1996060600425 19960606 00425 WP 1996 6 6 96ZZZX2849 1 19960229 A 3231 RETRACT MECH DOUG DC9 DC932 3022066 WP NLG DOORS MALFUNCTIONED A VJ6A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 946VV 47226 ATL/ATL - FLT 495 - AIR RETURN, AFTER TAKEOFF, THERE WAS A LOUD WIND NOISE COMING FROM THE NOSE GEAR AREA. RECYCLED GEA R, HAD A RED NOSE GEAR LIGHT ON. LIGHT WENT OUT IN SIXTY SECONDS AND HAD A NORMAL LANDING. JACKED AIRCRAFT, ADJUSTED N OSE GEAR DOORS, CYCLED GEAR. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1996060600426 19960606 00426 WP 1996 6 6 96ZZZX2850 1 19960328 A 2910 AC7031H8K1 O-RING DOUG DC9 DC932 3022066 WP RT HYD SYSTEM CUT A VJ6A O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 SO 11 946VV 47226 MCO/IAD - FLT 470 - ON LANDING, RIGHT HYDRAULIC FLUID WAS LOST. AIRCRAFT TURNED OFF RUNWAY ONTO TAXIWAY, GEAR PINS INST ALLED. REPLACED HYDRAULIC FILTER ASSY AND CUT PACKING. LEAK CHECKS OK. 2 L 7 2 4F A6WE 1996060600427 19960606 00427 WP 1996 6 6 96ZZZX2851 1 19960416 A 3260 0331881001 LIGHT DOUG DC9 DC931 3022065 WP NLG FAILED A VJ6A A UNSCHED LANDING O OTHER CL CLIMB 1 SO 11 960VV 47067 ATL/ATL - FLT 491 - THE CREW EXPERIENCED A GREEN NOSE GEAR INDICATION WITH THE GEAR RETRACTED. REMOVED AND REPLACED NOS E GEAR WARNING LIGHT ASSEMBLY AND OPS CHECKED NOSE GEAR. 2 L 7 2 4F A6WE 1996060600428 19960606 00428 WP 1996 6 6 96ZZZX2852 1 19960410 A 3231 UPLATCH SPRING DOUG DC9 DC931 3022065 WP RT MLG DOOR BROKEN A VJ6A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 960VV 47067 ATL/ATL - FLT 519 - AFTER TAKEOFF, AIR RETURN WHILE EXECUTING THE 'GEAR UPLATCH CHECK', THE 'RIGHT GEAR UNSAFE' LIGHT CA ME ON COUPLED WITH THE 'GEAR DOOR OPEN' LIGHT. FOUND SPRING ON RT MAIN GEAR DOOR UPLATCH BROKEN. REMOVED AND REPLACED SPRING GEAR DOOR AND LIGHTS. OPS CHECK OK. 2 L 7 2 4F A6WE 1996060600429 19960606 00429 WP 1996 6 6 96ZZZX2853 1 19960416 A 3260 0331881001 LIGHT SOCKET DOUG DC9 DC931 3022065 WP NLG FAILED A VJ6A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 11 960VV 47067 ATL/ATL - FLT 491 - THE CREW EXPERIENCED A GREEN NOSE GEAR INDICATION WITH THE GEAR RETRACTED. REMOVED AND REPLACED NOS E GEAR WARNING LIGHT ASSEMBLY AND OPS CHECKED NOSE GEAR. 2 L 7 2 4F A6WE 1996060600430 19960606 00430 EU 1996 6 6 AALA960454 1 19960324 A 3350 A3060698101 CONNECTOR FOKKER F28 F28MK0100 4990807 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1465K 11491 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT PASSENGER SEAT ROW 14 AND AFT FOUND INOPERATIVE. REPLACED BROKE N EMERGENCY FLOOR LIGHT STRIP CONNECTORS AT PASSENGER SEAT ROWS 14 AND 22. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X ) 2 L 7 2 4F RT 1996060600431 19960606 00431 NM 1996 6 6 AALA960608 1 19960418 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7667A 25301 DFW - DURING OVERNIGHT CHECK, SHORT SECTION OF EMERGENCY FLOOR LIGHT AT MID-CABIN FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT FLAT CONDUCTOR WIRE AT MID-CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1996060600432 19960606 00432 NM 1996 6 6 AALA960618 1 19960422 A 3350 1000679 LIGHT GRIMES BOEING 767 767323 1385205 NM COCKPIT DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 391AA 27451 SFO - DURING OVERNIGHT CHECK, COCKPIT DOOR OVERHEAD EXIT LIGHT FOUND INOPERATIVE. REPLACED COCKPIT DOOR OVERHEAD EXIT L IGHT ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1996060600433 19960606 00433 WP 1996 6 6 WRLA96003 1 19960117 A 2840 217003107 INDICATOR DOUG DC10 DC1030 3023501 WP AUXILIARY TANK FAILED A WRLA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 9MMAW 46959 EDAF/KPLH - EN ROUTE DURING CRUISE, FLIGHT CREW RECEIVED 'LOW FUEL PRESSURE INDICATION' FROM AUXILIARY TANK, YET FUEL QU ANTITY INDICATED 7,000 KGS IN TANK. AIRCRAFT HAD 10,500 KGS OF FUEL IN OTHER FUEL TANKS. HOWEVER, DUE TO THE CONFLICTI NG COCKPIT INDICATIONS OF THE AUX TANK (SUSPECTED FUEL QANTITY INDICATION MALFUNCTION), THE FLIGHT CREW ELECTED TO DIVER T TO EINN TO VERIFY FUEL QUANTITY VIA APPROVED ALTERNATE METHOD (DRIP STICKING). AIRCRAFT LANDED AT EINN WITHOUT INCIDE NT. MAINTENANCE PERSONNEL UTILIZED ALTERNATE FUEL QUANTITY CHECK (DRIP STICK) OF AUX TANK AND FOUND AUX TANK EMPTY. CO NFIRMED FUEL QUANTITY INDICATOR MALFUNCTION ON AUX TANK. ITEM DEFERRED PER MEL-28-31. AIRCRAFT RETURNED TO SERVICE.(X) 2 L 7 3 4F A22WE 1996060600434 19960606 00434 NE 1996 6 6 Y2PA96020 2 19960530 A 7261 4003T54P01 SCAVENGE PUMP AMD FALC20 FALCOND 2720304 EU GE CF700 CF7002D2 30010 NE LT ENG FAILED A Y2PA A E F UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. J WARNING INDICATION CL CLIMB 1 GL 23 823AA 228 299G066 YIP - AFTER T/O AT 13,000, CREW OBSERVED LT OIL PRESS WARN LT FLASH. CHECKING OIL PRESS GAUGE SHOWED LESS THAN 25 PSI. A/C RETURNED TO YIP. ENG WAS SHUTDOWN AND ON CLEARING THE RUNWAY THE TWR REPORTED SMOKE AND SOME FLAMES. THE ENG WAS MOTORED, FLAMES WENT OUT BUT SMOKE CONTINUED. RELEASED BOTH FIRE BOTTLES TO THE LEFT ENG. REQUESTED FIRE RESCUE. A/C TAXIED TO USA JET RAMP. FIRE RESCUE ASSIST WAS NOT NEEDED. NO EMERG DECLARED IN FLT. TEAR DOWN REVEALED NR 5 SUMP FIL LED WITH OIL. ALL OIL RETURN TUBES CLEAR, NO OBSTRUCTIONS TO HINDER OIL FLOW. NR 5 SCAVENGE PUMP NOT RETURNING OIL. T EST OF PUMP BY GE STROTHER, AT ROOM TEMP, SHOWED NORM OP. SUSPECT NR 5 SCAVENGE PUMP FAILURE AT ENG OPERATING TEMP. 2 L 7 2 4F 4 F A7EU E7EA 1996060600435 19960606 00435 EU 1996 6 6 Y2PA96023 1 19960425 A 2150 3155ZEQ1 TURBO COMPRESSOR AMD FALC20 FALCON 2720302 EU TAIL COMPARTMENT SMOKING A Y2PA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 23 812AA 150 57 YIP - FLT 14035 - ON TAKEOFF WHEN AIRCRAFT STARTED TO PRESSURIZE, FUEL FUMES AND SMOKE ENTERED THE COCKPIT FROM THE FIRS T OFFICER'S FLOOR VENT. THE CREW RETURNED TO POINT OF DEPARTURE. NO EMERGENCY PRODCEDURES WERE REQUIRED. THE PROBLEM WAS DETERMINED TO BE THE TURBO COMPRESSOR FAILED. REMOVED AND REPLACED UNIT AND SYSTEM OPERATIONAL CHECKED GOOD. (X) 2 L 7 2 4F A7EU 1996060600436 19960606 00436 NM 1996 6 6 96ZZZM884 1 19960314 A 3350 3315235 BATTERY ASSY BOEING 727 727290 138408W NM CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 774AT 21510 MDW - ON DAILY SERVICE CHECK, FOUND FORWARD RIGHT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED FORWARD RIGHT SERVICE DOOR EMERGENCY LIGHT BATTERY, OPS CHECK GOOD. (M) 2 L 7 3 4F A3WE 1996060600437 19960606 00437 NM 1996 6 6 96ZZZM885 1 19960312 A 3350 3322044 CHARGER ASSY BOEING 757 757212 NM CABIN INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 750AT 23126 IND - EMERGENCY LIGHT IN BULLNOSE ABOVE 25ABC INOP. EMERGENCY LIGHT IN BULL NOSE ABOVE 27DEF INOP. REMOVED AND REPLACE D BATTERY CHARGER AT FUSELAGE STATION 1243 LEFT, LIGHT OPS NORMAL. 2 L 7 2 4F RT A2NM 1996060600438 19960606 00438 WP 1996 6 6 96ZZZM886 1 19960310 A 3350 3322037 BATTERY LKHEED 1011 10113851 5265010 WP CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 187AT 036750 193C1077 LAX - 'C' ZONE EGRESS LIGHTING INOP. REMOVED AND REPLACED BATTERY PACK AT R3 DOOR AFT POSITION, OPS CHECK NORMAL. (M) 2 L 7 3 4F A23WE 1996060600439 19960606 00439 NM 1996 6 6 96ZZZM887 1 19960304 A 3350 3315235 BATTERY BOEING 727 727227 1384078 NM CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 778AT 22005 IND - AFT AIRSTAIR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY, OPS CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1996060600440 19960606 00440 NM 1996 6 6 96ZZZM888 1 19960308 A 3350 3314030 LIGHT BOEING 727 727227 1384078 NM CABIN INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 778AT 22005 IND - EMERGENCY LIGHT ABOVE R1 DOOR INOP. REPLACED LIGHT ASSEMBLY, OPS CHECK GOOD. (M) 2 L 7 3 4F A3WE 1996060600441 19960606 00441 1996 6 6 96ZZZM889 4 19960328 A 3413 IVA81A VIS DHAV DHC7 DHC7102 2802708 EA LT COCKPIT FAILED A CICA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 17 234SL 24 FLT 4915 - MIA-PID - PILOT REPORTED THAT DURING TAXI, SMOKE CAME OUT OF THE CAPTAINS INSTRUMENT PANEL. AIRCRAFT WAS FER RIED TO FLL MAINTENANCE BASE. MAINTENANCE REPLACED TCAS/VSI. LEAK AND OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. ( M) 2 H 7 4 4T A20EA 1996060600442 19960606 00442 NE 1996 6 6 96ZZZM890 2 19960307 A 7250 808904 TURBINE BLADE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE NR 2 ENG FAILED A AALA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 SW 07 73444 49470 718479 ORD - FLT 1853 - EN ROUTE ROC/ORD - DURING CRUISE, LOUD BANG FOLLOWED BY LOSS OF POWER FROM NR 2 ENGINE AND NO EPR OR N1 INDICATIONS. ACCOMPLISHED SHUTDOWN OF NR 2 ENGINE AND AIRCRAFT PROCEEDED SINGLE ENGINE TO ORD, LANDING WITHOUT INCIDEN T. REPLACED NR 2 ENGINE AND ACCOMPLISHED LEAK AND GROUND ENGINE RUN CHECKS WITH NO DEFECTS FOUND. ENGINE SHUTDOWN WAS THE RESULT OF 3RD AND 4TH STAGE TURBINE FAILURE. ALL 3RD AND 4TH STAGE TURBINE BLADES WERE BROKEN AT OR NEAR THE AIRFOI L ROOT. NO DEFINITIVE CAUSE OF FAILURE HAS BEEN DETERMINED. ENGINE ROUTED TO SHOP FOR REPAIR AND RETURN TO SERVICE. R EFERENCE AALA960375. 2 L 7 2 4F 4 F A6WE E9NE 1996060600443 19960606 00443 NM 1996 6 6 96ZZZM891 1 19960418 A 2750 ELECTRONIC UNIT BOEING 767 767231 1385131 NM TE FLAPS TRIPPED A TWAA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 603TW 22566 MCI - DURING CLIMB, UNABLE TO RETRACT FLAPS ABOVE ONE DEGREE. RESEATED FLAP/SLAT ELECTRONIC UNIT. OPERATIONAL CHECK AN D BYTE TEST NORMAL. (M) 2 L 7 2 4F RT A1NM 1996060600444 19960606 00444 NE 1996 6 6 96ZZZM892 2 19960424 A 7200 ENGINE LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B NE NR 2 VIBRATION A TWAA E ENGINE SHUTDOWN E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 CE 05 15017 193B1063 4806 MCI - FLT 5034 - DURING CRUISE, SHUT DOWN NR 2 ENGINE DUE TO INCREASE OF VIBRATION ON BOTH A AND B CHANNELS. FOUND FAN OUT OF TRIM BALANCE. PERFORMED ENGINE TRIM BALANCE. ENGINE OPERATION AND INDICATION THEN CHECKED NORMAL. 2 L 7 3 4F 4 F A23WE E12EU 1996060600445 19960606 00445 NM 1996 6 6 96ZZZM893 1 19960416 A 5330 SKIN BOEING 727 727231 1384079 NM FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 52311 19830 MCI - DURING C-CHECK, FOUND CORROSION UNDER SKIN BELOW AFT LAV SERVICE AREA, AND RIVET HEADS POPPED. REMOVED SKIN AND R EPAIRED PER ARA 9917 AND SRM 51-20-1, 51-20-2 AND 51-20-4. (M) 2 L 7 3 4F A3WE 1996060600446 19960606 00446 WP 1996 6 6 96ZZZM894 1 19960416 A 5712 RIB LKHEED 1011 10113851 5265010 WP WS 503.76 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 31013 193B1035 MCI - DURING SPECIAL CHECK, FOUND 1.5 INCH CRACK IN UPPER FORWARD CHORD OF LEFT WING RIB, STATION 503.76. STOP DRILLED AND REPAIRED PER EMLR 66589. 2 L 7 3 4F A23WE 1996060600447 19960606 00447 WP 1996 6 6 96ZZZM895 1 19960418 A 5712 RIB LKHEED 1011 10113851 5265010 WP WS 503 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 15017 193B1063 MCI - DURING SPECIAL CHECK, FOUND 1.25 INCH CRACK IN LEFT WING RIB CASTELLATION FORWARD SIDE OF STRINGER 19, TOP CHORD, WS 503. REPAIRED PER SERVICE BULLETIN 093-57-207, PARA 2B. 2 L 7 3 4F A23WE 1996060600448 19960606 00448 WP 1996 6 6 96ZZZM896 1 19960418 A 5712 RIB LKHEED 1011 10113851 5265010 WP WS 555 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 15017 193B1063 MCI - DURING SPECIAL CHECK, FOUND SEVEN CRACKS IN LEFT WING TOP RIB CASTELLATION, STATION 555. REPAIRED PER SERVICE BUL LETIN 093-57-207, PARA 2B. (M) 2 L 7 3 4F A23WE 1996060600449 19960606 00449 WP 1996 6 6 96ZZZM897 1 19960417 A 7830 TR LIGHT DOUG DC9 DC932 3022066 WP RT ENGINE BROKEN WIRE A TWAA O OTHER N FALSE WARNING CL CLIMB 1 CE 05 932L 47669 STL - DURING CLIMB, RIGHT THRUST REVERSER LIGHT ILLUMINATED. REPAIRED WIRING TO RIGHT THRUST REVERSER. OPERATIONAL CHE CK NORMAL. (M) 2 L 7 2 4F A6WE 1996060600450 19960606 00450 NM 1996 6 6 96ZZZM898 1 19960416 A 5720 VENT BOX BOEING 727 727231 1384079 NM WS 629 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54329 20307 MCI - DURING C-CHECK, FOUND FRONT AND REAR TANGS CRACKED ON FORWARD VENT BOX, WS 629. REPAIRED PER SSRM 52-20-201. 2 L 7 3 4F A3WE 1996060600451 19960606 00451 NM 1996 6 6 96ZZZM899 1 19960411 A 5320 FORMER BOEING 767 767231 1385131 NM BS 1605 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 601TW 22564 MCI - DURING SPECIAL CHECK, FOUND FUSELAGE FORMER, FS 1605, DENTED AND CRACKED, STRINGER 13L TO STRINGER 20L. REPLACED FORMER PER ARA 9958. (M) 2 L 7 2 4F RT A1NM 1996060600452 19960606 00452 WP 1996 6 6 96ZZZM900 1 19960416 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 718 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 977Z 47249 STL - DURING SPECIAL CHECK, FOUND CABIN AREA LONGERON 6L CRACKED AT BOTH ATTACH POINTS, STATION 718. REPAIRED PER SRM 5 3-02, FIGURE 2. (M) 2 L 7 2 4F A6WE 1996060600453 19960606 00453 NM 1996 6 6 96ZZZM901 1 19960411 A 5512 SKIN BOEING 767 767231 1385131 NM HORIZ STAB DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 601TW 22564 MCI - DURING SPECIAL CHECK, FOUND LEFT STABILIZER LOWER SKIN DAMAGED. REPAIRED PER ARA 9959. (M) 2 L 7 2 4F RT A1NM 1996060600454 19960606 00454 NM 1996 6 6 96ZZZM902 1 19960417 A 2780 106788A103 BYPASS VALVE BOEING 727 727231 1384079 NM TE FLAPS MALFUNCTIONED A TWAA O OTHER J WARNING INDICATION DE DESCENT 1 CE 05 54326 20233 FLT 707 - STL - DURING DESCENT, TRAILING EDGE OUTBOARD FLAPS WOULD NOT EXTEND. REMOVED AND REPLACED OUTBOARD TRAILING E DGE FLAP BYPASS VALVE, MFG P/N 106788A103. OPERATIONAL CHECK NORMAL. 2 L 7 3 4F A3WE 1996060600455 19960606 00455 NM 1996 6 6 96ZZZM903 1 19960416 A 2782 1U109592 ACTUATOR BOEING 727 727231 1384079 NM NR 6 LE FLAP FAILED A TWAA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 CE 05 52313 19832 FLT 680 - STL - DURING LANDING, 'A' SYSTEM HYDRAULIC QUANTITY WAS LOST. REMOVED AND REPLACED NR 6 LEADING EDGE SLAT ACT UATOR, MFG P/N 1U1095-9-2. OPERATIONAL CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1996060600456 19960606 00456 NM 1996 6 6 96ZZZM904 1 19960413 A 5712 RIB BOEING 727 727231 1384079 NM WS 546.5 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54325 20232 JFK- DURING C-4D CHECK, FOUND A 1.25 INCH CRACK BETWEEN HOLE AND RADIUS OF RIB LOWER FLANGE AT STRINGER 6, RIB WS 546.5. REPAIRED EPR SERVICE BULLETIN 727-57A159, PAGES 6, 7 AND 8. (M) 2 L 7 3 4F A3WE 1996060600457 19960606 00457 NM 1996 6 6 96ZZZM905 1 19960413 A 5712 RIB BOEING 727 727231 1384079 NM WS 601.5 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54325 20232 JFK - DURING C-4D CHECK, FOUND RIB CRACKED AT RADIUS AREA AT ATTACH POINT TO FIRST STRINGER AFT OF ACCESS HOLE, WL 601.5 . REPAIRED BY STOP DRILLING, FABRICATING AND INSTALLING DOUBLER PER SRM 57-10-05, PAGES 6, 7 AND 8. (M) 2 L 7 3 4F A3WE 1996060600458 19960606 00458 WP 1996 6 6 96ZZZM906 1 19960415 A 3350 58222 BATTERY PACK DOUG DC9 DC934 302207E WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 936L 47711 STL - FLT 501 - DURING CRUISE EMERGENCY EGRESS LIGHT ILLUMINATED. REMOVED AND REPLACED BATTERY PACK, MFG P/N 5822-2, OP ERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 1996060600459 19960606 00459 WP 1996 6 6 96ZZZM907 1 19960415 A 2530 OVENS DOUG DC9 DC932 3022066 WP GALLEY SMOKING A TWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CE 05 996Z 47028 MIA - FLT 492 - WHILE AT THE GATE, OVENS BY L-1 DOOR EMITTED BURING SMELL AND SMOKE. OVENS WERE SHUT DOWN AND CIRCUIT B REAKER PULLED. BURNED PAPER AND FOOD WAS REMOVED FROM OVENS. OVENS WERE OPERATED AT THEIR HIGHEST TEMPERATURE SETTING FOR 30 MINUTES AND NO ABNORMALITIES WERE NOTED. (M) 2 L 7 2 4F A6WE 1996060600460 19960606 00460 NM 1996 6 6 96ZZZM908 1 19960413 A 3350 58223 POWER SUPPLY BOEING 747 747257B 1384853 NM CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 303TW 20116 STL - FLT 16 - DURING LAYOVER, MAINTENANCE EMERGENCY EGRESS LIGHTS ON BOTH AISLES, BETWEEN NR 3 AND NR 4 DOORS, REMAINED ON CONTINUOUSLY. REMOVED AND REPLACED EGRESS LIGHT POWER SUPPLY, MFG P/N 5822-3. OPERATIONAL CHECK NORMAL. (M) 2 L 7 4 4F A20WE 1996060600461 19960606 00461 NM 1996 6 6 96ZZZM909 1 19960415 A 3350 CONNECTOR BOEING 727 727231 1384079 NM CABIN DIRTY A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 54348 21967 FLT 402 - STL - DURING CRUISE, AFT CABIN EMERGENCY EGRESS LIGHTS ILLUMINATED. CLEANED AND DRIED MOISTURE FROM TRACK CON NECTION. OPERATIONAL CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1996060600462 19960606 00462 NM 1996 6 6 96ZZZM910 1 19960418 A 5330 SKIN BOEING 767 767231 1385131 NM BS 1605-1629 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 601TW 22564 MCI - DURING SPECIAL CHECK, FOUND FOD DAMAGE TO LEFT AFT FUSELAGE, FS 1605 TO FS 1629 AND FROM STRINGER 20L TO STRINGER 16L. REPLACED AND REPAIRED SKIN PANEL PER ATA 9958A AND TWA STANDARD PRACTICES. (M) 2 L 7 2 4F RT A1NM 1996060600463 19960606 00463 WP 1996 6 6 96ZZZM911 1 19960422 A 3350 LIGHTS DOUG DC9 DC932 3022066 WP CABIN MALFUNCTIONED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 995Z 47027 STL - FLT 547 - DURING CRUISE, L-1 AND R-1 AND REAR DOOR EMERGENCY LIGHTS ILLUMINATED INTERMITTENTLY. CYCLED EMERGENCY LIGHT SWITCH AT FORWARD FLIGHT ATTENDANTS PANEL. OPERATIONAL CEHCK NORMAL. (M) 2 L 7 2 4F A6WE 1996060600464 19960606 00464 NM 1996 6 6 96ZZZM912 1 19960418 A 5512 SKIN BOEING 767 767231 1385131 NM HORIZ STAB DAMAGED A TWAA K NONE C F.O.D. IN INSP/MAINT 1 CE 05 601TW 22564 MCI - DURING SPECIAL CHECK, FOUND FOD DAMAGE TO LEFT HORIZONTAL STABILIZER LOWER SKIN AND FRONT SPAR, FS 186 TO FS 255. REPAIRED PER ARA 9957 AND TWA AND STANDARD PRACTICES. (M) 2 L 7 2 4F RT A1NM 1996060600465 19960606 00465 NE 1996 6 6 96ZZZM913 2 19960422 A 7261 RD21891 OIL TUBE DOUG DC9 DC915 3022036 WP PWA JT8 JT8D7A 52053 NE NR 2 ENGINE LEAKING A TWAA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION AP APPROACH 1 CE 05 975Z 47035 LNK - FLT 677 - DURING APPROACH, SHUT DOWN NR 2 ENGINE, S/N 3808, DUE TO LOSS OF OIL QUANTITY AND LOW OIL PRESSURE. FOU ND OIL LEAK AT NR 6 BEARING OIL TUBE, MFG P/N RD2189-1. REPLACED OIL TUBE. ENGINE OPERATION AND LEAK CHECK NORMAL. 2 L 7 2 4F 4 F A6WE E2EA 1996060600466 19960606 00466 WP 1996 6 6 96ZZZM914 1 19960423 A 3260 CONNECTOR DOUG DC9 DC932 3022066 WP LT MLG DOOR DIRTY A TWAA O OTHER N FALSE WARNING AP APPROACH 1 CE 05 922L 47108 STL - FLT 284 - DURING APPROACH, AFTER LANDING GEAR EXTENSION, LEFT MAIN LANDING GEAR DOOR LIGHT ILLUMINATED. CYCLED LA NDING GEAR. CLEANED CONNECTOR FOR LEFT LANDING GEAR DOOR SWITCH, MFG P/N H14-6, AND LANDING GEAR DOOR OPERATION AND IND ICATION. 2 L 7 2 4F A6WE 1996060600468 19960606 00468 NM 1996 6 6 96ZZZM916 1 19960413 A 5320 TAB BOEING 727 727231 1384079 NM BS 656.5 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54325 20232 JFK - DURING C-4D CHECK, FOUND A CRACK AT STRINGER 13 VENT BOX FORWARD TAB, STATION 656.5. REPAIRED PER SERVICE BULLETI N 727-57A159. 2 L 7 3 4F A3WE 1996060600469 19960606 00469 WP 1996 6 6 96ZZZM917 1 19960421 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 639 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 992Z 47095 STL - DURING SPECIAL CHECK, FOUND A 1 INCH CRACK IN LONGERON 6R, STATION 639. REPAIRED PER SRM 53-02, PAGE 2A, FIGURE 2 . 2 L 7 2 4F A6WE 1996060600470 19960606 00470 WP 1996 6 6 96ZZZM918 1 19960430 A 3260 7000010101 SWITCH DOUG DC9 DC932 3022066 WP RT MLG FAILED A VJ6A A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 11 921VV 47284 FLT 382 - TPA-BOS - DIVERTED TO ATL, THE RIGHT MAIN GEAR UNSAFE LIGHT ILLUMINATED EN ROUTE, DIVERTED FLIGHT, GEAR EXTEND ED NORMALLY WITH NORMAL INDICATION. FOUND RIGHT MLG UPLIMIT SWITCH BINDING ON THE SWITCH STRIKER. REPLACED STRIKER AND SWITCH IAW MM 32-60-1. 2 L 7 2 4F A6WE 1996060600471 19960606 00471 NE 1996 6 6 96ZZZM919 2 19960428 A 7320 714810 P AND D VALVE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9A 52048 NE NR 2 ENGINE MALFUNCTIONED A VJ6A A UNSCHED LANDING O OTHER CL CLIMB 1 SO 11 913VV 47318 665911 ON FLT 400 - ATL-ATL - AIR RETURN, AFTER TAKEOFF CLIMB POWER WAS SET, THE NR 2 ENGINE BEGAN TO SURGE, EPR 1.5-1.7, F/F P LUS MINUS 1500 LBS/HR, EGT, N1, N2 ALSO FLUCTUATED. REPLACED PRBC AND P AND D VALVES IAW MM 73-10-2 (P AND D) AND 75-31 -1 (PRBC), RAN NR 2 ENGINE IAW MM 71-00 OPS CHECKED GOOD. 2 L 7 2 4F 4 F A6WE E2EA 1996060600472 19960606 00472 NE 1996 6 6 96ZZZM920 2 19960428 A 7532 658385 PBRC DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9A 52048 NE NR 2 ENGINE MALFUNCTIONED A VJ6A A UNSCHED LANDING O OTHER CL CLIMB 1 SO 11 913VV 47318 665911 ON FLT 400 - ATL-ATL - AIR RETURN, AFTER TAKEOFF CLIMB POWER WAS SET, THE NR 2 ENGINE BEGAN TO SURGE. EPR 1.5-1.7, F/F PLUS MINUS 1500 LBS/HR, EGT, N1, N2 ALSO FLUCTUATED. REPLACED PRBC AND P AND D VALVES IAW MM 73-10-2 (P AND D) AND 75-3 1-1 (PRBC), RAN NR 2 ENGINE IAW MM 71-00 OPS CHECKED GOOD. 2 L 7 2 4F 4 F A6WE E2EA 1996060600473 19960606 00473 NE 1996 6 6 96ZZZM921 3 19960423 A 6110 PROP AEROSP ATR42 ATR42300 8680920 EU HAMSTD 14SF 14SF5 NE RT ENGINE OVERTORQUED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 213AT 7854 10483 211 ORD - FLT 4011 - TEN DAYS AFTER OCCURENCE, IN MQT, FDAU READ OUT OVERTORQUE ON BOTH ENGINES. SIMMONS MANAGEMENT GROUNDE D THE AIRCRAFT IN CVG IMMEDIATELY AND DISPATCHED MTX AND INSPECTION TEAM TO INSPECT PROPS AND BOROSCOPE BOTH ENGINES. B OTH ENGINES INSPECTED AS PER PW MANUAL AND THERE WAS NO DANGER EVIDENT. AIRCRAFT WAS FERRIED AS PER HAM STANDARD APPROV AL TO MQT FOR BOTH PROP REPLACEMENT DUE TO RECORDED OVERTORQUE. AIRCRAFT WAS RETURNED TO SERVICE. REFERENCE SIMA961142 . 2 H 7 2 4T RT A53EU 6 C P7NE 1996060600474 19960606 00474 WP 1996 6 6 96ZZZM922 1 19960422 A 5320 INTERCOSTAL LKHEED 1011 10113851 5265010 WP BS 1565/1585 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 302MB 193P1129 FOUND LEVEL 2 CORROSION IN CENTER CARGO COMPARTMENT, STATION 1565, AND 1585, LBL 35 INTERCOSTAL BELOW FLOOR CORRODED. R EMOVED AND REPLACED DAMAGED AREA PER SRM 51-50-04. (M) 2 L 7 3 4F A23WE 1996060600475 19960606 00475 WP 1996 6 6 96ZZZM923 1 19960422 A 5315 FLOORBEAM LKHEED 1011 10113851 5265010 WP BS 1463 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 302MB 193P1129 FOUND LEVEL 2 CORROSION, CENTER CARGO COMPARTMENT, LEFT AND RIGHT SIDES OF FLOOR SUPPORT BEAM UPPER CAP AT STATION 1463 HAD CORROSION. REMOVED AND REPLACED DAMAGED AREA PER SRM 51-50-04. 2 L 7 3 4F A23WE 1996060600476 19960606 00476 WP 1996 6 6 96ZZZM924 1 19960422 A 5312 BULKHEAD BRACKET LKHEED 1011 10113851 5265010 WP BS 1363 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 302MB 193P1129 FOUND LEVEL 2 CORROSION, CENTER CARGO COMPARTENT BELOW FLOOR PANEL AT FORWARD BULKHEAD, STATION 1363, BL 6 ON LEFT SIDE SUPPORT BRACKET HAS CORROSION. REMOVED AND REPLACED DAMAGED BRACKET PER SRM 51-10-5. (M) 2 L 7 3 4F A23WE 1996060600477 19960606 00477 WP 1996 6 6 96ZZZM925 1 19960422 A 5347 FLOOR TRACK LKHEED 1011 10113851 5265010 WP BS 1665-1685 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 302MB 193P1129 FOUND LEVEL 2 CORROSION, AFT CARGO COMPARTMENT LEFT FLOOR TRACK AT STATION 1665-1685, AND STATION 1705. REMOVED AND REP LACED FLOOR TRACK SECTION PER SRM 53-24-00. (M) 2 L 7 3 4F A23WE 1996060600478 19960606 00478 WP 1996 6 6 96ZZZM926 1 19960101 A 5347 SEAT TRACK DOUG DC8 DC863 302198A WP BS 1520-1620 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 4935C 45931 FOUND LEVEL 2 CORROSION, CABIN FLOOR STATION 1520-1620 LEFT SIDE OUTBOARD SEAT TRACK HAS CORROSION. REMOVED DAMAGED ARE A AND SPLICED IN NEW SEAT TRACK PER SRM 51-2-3. (M) 2 L 7 4 4F 4A25 1996060600479 19960606 00479 SW 1996 6 6 96ZZZM927 1 19960413 A 5753 2736015009 RIB SWRNGN SA227 SA227AC 8780603 SW LT TE FLAP CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 60NE AC760B DURING AN INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE LEFT FLAP INBOARD AFT END RIB CHAFED APPROXIMATELY .200 INC H BY .500 INCH, OUTBOARD NOSE END RIB CRACKED IN RELIEF RADIUS AND OUTBOARD HINGE ARM BENT. COMPLETED REPAIR 'PART FOR PART' REPLACEMENT WITH A NEW LEFT INBOARD AFT ENG RIB P/N 27-36003-001, NEW OUTBOARD NOSE END RIB P/N 27-26015-009 AND N EW OUTBOARD HINGE ARM P/N 27-36044-005. ALL WORK DONE IAW FAIRCHILD SRM 51-00-00, PG 4 REV JUNE 1/93, AND 57-90-60 PGS 43-46. FAIRCHILD SRM CHANGERS REFERENCED 51-30-04, REV JUNE 1/93 AND 51-40-00 REV JUNE 1/93. REFERENCE MALA964961. 2 L 7 2 4T RT A8SW 1996060600480 19960606 00480 SW 1996 6 6 96ZZZM928 1 19960413 A 5753 2736044005 HINGE ARM SWRNGN SA227 SA227AC 8780603 SW LT TE FLAP DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 60NE AC760B DURING AN INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE LEFT FLAP INBOARD AFT END RIB CHAFFED APPROXIMATELY .200 IN CH BY .500 INCH, OUTBOARD NOSE END RIB CRACKED IN RELIEF RADIUS AND OUTBOARD HINGE ARM BENT. COMPLETED REPAIR 'PART FOR PART' REPLACEMENT WITH A NEW LEFT INBOARD AFT ENG RIB P/N 27-36003-001, NEW OUTBOARD NOSE END RIB P/N 27-26015-009 AND NEW OUTBOARD HINGE ARM P/N 27-36044-005. ALL WORK DONE IAW FAIRCHILD SRM 51-00-00, PG 4 REV JUNE 1/93, AND 57-90-60 PGS 43-46. FAIRCHILD SRM CHANGERS REFERENCED 51-30-04, REV JUNE 1/93 AND 51-40-00 REV JUNE 1/93. REFERENCE MALA964961. 2 L 7 2 4T RT A8SW 1996060600481 19960606 00481 EU 1996 6 6 AALA96012 1 19960416 A 5320 A53778689200 CASTING AIRBUS 300 A300B4605R 3930308 EU BS 2490-2505 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - FOUND TWO AREAS OF CORROSION ON AFT LEFT SIDE OF AFT MANHOLE. INSTALLED DOUBLER PER ESO 30595, DATED 4-12-96. (M ) 2 L 7 2 4F RT A35EU 1996060600482 19960606 00482 EU 1996 6 6 AALA960129 1 19960124 A 7722 9373M91P03 PROBE AIRBUS 300 A300B4605R 3930308 EU NR 1 ENG LPT BROKEN A A AALA E A ENGINE SHUTDOWN UNSCHED LANDING T ENGINE CASE PENETRATION CL CLIMB 1 SW 07 59081 3539 639 PHL - FLT 1425 - AFTER T/O PHL DURING INITIAL CLIMB, NR 1 ENG EXPERIENCED UNCONTAINED FAILURE RESULTING IN DAMAGE TO LT CORE COWL AND LT AILERON. ACCOMP PROCEDURES AND SHUTDOWN NR 1 ENG. A/C RETURNED TO PHL AND LANDED W/O INCIDENT. REPLA CED NR 1 ENG AND LT CORE COWL. ACCOMP LEAK CHECKS AND GROUND ENG RUN WITH NO DEFECTS FOUND. ACCOMP INTERIM REPAIR TO L T AILERON AND A/C MX FERRY PHL/JFK. REPLACED LT AILERON AT JFK. FOUND 1.6 INCH SECTION OF T49 THERMOCOUPLE PROBE MISSI NG FROM THE 12:00 O'CLOCK PROBE. MISSING SECTION OF PROBE IMPACTED THE LPT STAGE 1 BLADES CAUSING A SUBSEQUENT STAGE 1 BLADE SEPARATION. 10X VISUAL INSPECT OF ALL PROBES HAS BEEN IMPLEMENTED. ENG REPAIRED AND RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A35EU 1996060600483 19960606 00483 1996 6 6 AALA960287 4 19960220 A 2565 D31021107 EVACUATION SLIDE AIRCRUISERS AIRBUS 300 A300B4605R 3930308 EU R3 DOOR DEFECTIVE A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 07 11060 0132 470 JFK - FLT 0587 - AFTER PUSH BACK FROM THE GATE WHEN NR 2 ENGINE STARTED, SMOKE NOTED IN COCKPIT. AIRCRAFT WAS EVACUATED USING SLIDES AND DOOR 3R EMERGENCY EVACUATION SLIDE CAME OUT OF THE CONTAINER AND PARTIALLY UNFOLDED, BUT DID NOT INFLA TE. REPLACED EMERGENCY EVACUATION SLIDE AT DOOR 3R. SLIDE ROUTED TO VENDOR FOR EVALUATION. FINDINGS: ENGINEERING AND NTSB INVESTIGATIONS WERE UNABLE TO ESTABLISH CAUSE FOR SLIDE NON-DEPLOYMENT DUE TO SLIDE DAMAGE SUSTAINED DURING REMOVA L FROM AIRCRAFT. (X) 2 L 7 2 4F RT A35EU 1996060600484 19960606 00484 EU 1996 6 6 AALA960342 1 19960228 A 2170 21D101 COALESCER AIRBUS 300 A300B4605R 3930308 EU ACM BAY DIRTY A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 25071 514 JFK - FLT 1445 - AFTER TAKEOFF DURING CLIMB-OUT, ODOR/FUMES NOTED IN COCKPIT. AIRCRAFT RETURNED TO JFK AND LANDED WITHO UT INCIDENT. ACCOMPLISHED PACK BURN OUT PROCEDURE AND REPLACED ALL COALESCER BAGS. ACCOMPLISHED GROUND ENGINE RUN AND OPERATED APU WITH NO DEFECTS OR ODOR NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996060600485 19960606 00485 EU 1996 6 6 AALA960424 1 19960320 A 5320 SKIN AIRBUS 300 A300B4605R 3930308 EU BS 4740 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND CORROSION AROUND 14 FASTENERS ON AIRCRAFT OUTER SKIN BELOW THRESHOLD. REMOVED CORROSION AS PER AA SRM 51-74 -10-2. TREATED PRIMED AND TOP COATED AREA. (M) 2 L 7 2 4F RT A35EU 1996060600486 19960606 00486 EU 1996 6 6 AALA960435 1 19960320 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU BS 1764-2241 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND CORROSION ON SEAT TRACK JUST INBOARD OF LAV M ON SEAT TRACK NR 8, A PON OPEN UP ENTIRE LENGTH OF SEAT TRACK 8 FROM STATION 1764 TO STATION 2241. INSTALLED NEW SEAT TRACK NR 8 JUST INBOARD OF LAV M, SPLICE TO SPLICE. (M) 2 L 7 2 4F RT A35EU 1996060600487 19960606 00487 EU 1996 6 6 AALA960443 1 19960321 A 5320 5467688 ROLLER TRAY AIRBUS 300 A300B4605R 3930308 EU FRAME 28-35 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND NUMEROUS AREAS OF CORROSION FROM FRAME 28 TO FRAME 35 ON TRAY NR 4. INSTALLED NEW SECTION OF ROLLER TRAY PE R SRM 53-10-10 FIG 202. (M) 2 L 7 2 4F RT A35EU 1996060600488 19960606 00488 EU 1996 6 6 AALA960458 1 19960322 A 5320 ANGLE AIRBUS 300 A300B4605R 3930308 EU BS 1236 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 59081 639 TUL - FOUND FLOORBOARD T-ANGLE CORRODED AT JOGGLE AT FLOORBEAM 15A. CUT OUT CORRODED SECTION AND REPLACED WITH FILLER P IECE ON TOP AND TWO STRAPS UNDERNEATH ONE ON EACH SIDE. REPLACED RIVETS WITH APPROPRIATE HI-LOCKS. (M) 2 L 7 2 4F RT A35EU 1996060600489 19960606 00489 EU 1996 6 6 AALA960459 1 19960323 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU BS 1180-1200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND STRIP ON SEAT TRACK SUPPORT NR 8, 6 INCHES BELOW FORWARD GALLEY MOON MAT IS CORRODED. REMOVED OUT OF LIMITS T-ANGLE AND INSTALLED MANUFACTURED T-ANGLE IAW SRM 53-10-13. (M) 2 L 7 2 4F RT A35EU 1996060600490 19960606 00490 EU 1996 6 6 AALA960485 1 19960325 A 5311 FRAME AIRBUS 300 A300B4605R 3930308 EU FRAME 63 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND CORROSION ON TOP OF FRAME AT LT OUTBOARD ROLLER TRAY ATTACH FRAME 63 AND APPROXIMATELY 5 INCHES OUTBOARD ON VERTICAL ANGLE. REMOVED 1 INCHES SECTION OF ROLLER TRAY, FABRICATED AND INSTALLED NEW SECTION PER SRM 53-10-15, REMOVED CORRODED TOP OF FRAME PER 53-10-13 AND INSTALLED NEW FRAME, ALODINED, PRIMED AND PAINTED ALL NEW PIECES. (M) 2 L 7 2 4F RT A35EU 1996060600491 19960606 00491 EU 1996 6 6 AALA960499 1 19960401 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FR 72-73 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 25071 514 TUL - FOUND SMALL AREA OF CORROSION ON TOP FLANGE OF TEE ANGLE USED PRIMARILY FOR FLOORBOARD SUPPORT. INSTALLED A STRAP .050 THICK 301 CRES .5 HARD OVER TOP FLANGE OF TEE ANGLE WITH 5 (ML 329-5 HI-LOCKS) PAST LAST DAMAGE PER AARD A-300 ESO 30595, DATED 10/10/95. (M) 2 L 7 2 4F RT A35EU 1996060600492 19960606 00492 EU 1996 6 6 AALA960500 1 19960401 A 5320 ANGLE AIRBUS 300 A300B4605R 3930308 EU FR 72-73 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 25071 514 TUL - FOUND SMALL AREA OF CORROSION ON TOP FLANGE OF TEE ANGLE USED PRIMARILY FOR FLOORBOARD SUPPORT. INSTALLED A STRAP .050 THICK 301 CRES .5 HARD OVER TOP FLANGE OF TEE ANGLE WITH 5 (HL 329-5 HI-LOCKS) PAST LAST DAMAGE PER AARD A-300 ESO 30595 DATED 10/10/95. (M) 2 L 7 2 4F RT A35EU 1996060600493 19960606 00493 EU 1996 6 6 AALA960501 1 19960402 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU BS 4574-4627 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 25071 514 TUL - FOUND FLOOR SUPPORT BEAM BETWEEN FRAME 71-72, 3RD FRAME FROM CENTER ON LEFT SIDE HAS CORROSION ON TOP SIDE. INSTA LLED REPAIR ESO 30595. (M) 2 L 7 2 4F RT A35EU 1996060600494 19960606 00494 EU 1996 6 6 AALA960502 1 19960402 A 5320 PLATE AIRBUS 300 A300B4605R 3930308 EU BS 4680 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 25071 514 TUL - FOUND PLATE FORWARD OF L-4 DOOR HAS CORROSION JUST OUTBOARD OF FLOORBOARD 251PG AND FORWARD OF FRAME 73. INSTALLE D DOUBLER PER SRM 53-10-12. (M) 2 L 7 2 4F RT A35EU 1996060600495 19960606 00495 EU 1996 6 6 AALA960503 1 19960401 A 5330 SKIN AIRBUS 300 A300B4605R 3930308 EU FR 61-62 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 70054 461 TUL - FOUND 5 INCH DENT WITH 3 INCH HOLE PUNCTURED THROUGH SKIN IN FIELD, FERRIED TO TUL FOR REPAIR. REPAIRED PER ESO 3 0595, DATED 4-1-96. (M) 2 L 7 2 4F RT A35EU 1996060600496 19960606 00496 EU 1996 6 6 AALA960512 1 19960402 A 5347 5467687 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 25071 514 TUL - FOUND CORROSION IN 2 PLACES ON TOP FLANGE OF SEAT TRACK BLENDED BEYOND LIMITS. REMOVED AND REPLACED WITH A NEW SE CTION OF SEAT TRACK. (M) 2 L 7 2 4F RT A35EU 1996060600497 19960606 00497 EU 1996 6 6 AALA960532 1 19960404 A 5320 A5398019520351 RETAINER AIRBUS 300 A300B4605R 3930308 EU FRAME 74-75 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 25071 514 TUL - FOUND CORROSION ON TOP SIDE OF R4 DOOR LOWER RETAINER 3 PLACES ABOUT 4 INCHES APART BLENDED BEYOND LIMITS (AREA UN DERNEATH TOP LIP OF SCUFF PLATE). REMOVED AND REPLACED RETAINER PER SRM 51-72-10 PAGE 1 AND PAGE 2. (M) 2 L 7 2 4F RT A35EU 1996060600498 19960606 00498 EU 1996 6 6 AALA960533 1 19960404 A 5320 TMS60242 ANGLE AIRBUS 300 A300B4605R 3930308 EU FRAME 74-75 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 25071 514 TUL - FOUND 3 AREAS OF CORROSION AROUND CLIP NUT HOLES FOR FLOORBOARDS, ONE AREA BLENDED BEYOND LIMITS. REMOVED AND REP LACED WITH A NEW SECTION OF 'L' ANGLE PER SRM 51-72-10 PAGE 1 AND PAGE 2. (M) 2 L 7 2 4F RT A35EU 1996060600499 19960606 00499 EU 1996 6 6 AALA960535 1 19960405 A 5400 ANGLE AIRBUS 300 A300B4605R 3930308 EU LT PYLON CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - FOUND T-ANGLE AT TOP OF PYLON HAS CORROSION AT WEB ATTACH AREA. REPLACED ANGLE PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 1996060600500 19960606 00500 EU 1996 6 6 AALA960536 1 19960404 A 5320 ANGLE AIRBUS 300 A300B4605R 3930308 EU BS 4740-4801 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 25071 514 TUL - FOUND CORROSION ON THIRD TO RIGHT OF CENTER FLOOR SUPPORT BETWEEN FRAME 74 AND 75, FIVE PLACES AT FASTENERS HOLES. REPAIRED PER AARD 53-20-00-2. (M) 2 L 7 2 4F RT A35EU 1996060600501 19960606 00501 EU 1996 6 6 AALA960547 1 19960405 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU BS 2559 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 25071 514 TUL - FOUND CORROSION ON TOP FLANGE OF FLOOR SUPPORT 'T' WHERE NR 6 ROLLER TRAY IS SUPPORTED BY 'T'. REPAIRED FLOOR SUP PORT 'T' WHERE NR 6 ROLLER TRAY IS SUPPORTED PER SRM 51-71-50. (M) 2 L 7 2 4F RT A35EU 1996060600502 19960606 00502 EU 1996 6 6 AALA960548 1 19960405 A 5320 ROLLER TRAY AIRBUS 300 A300B4605R 3930308 EU BS 2559 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 25071 514 TUL - FOUND CORROSION UNDER AFT EDGE OF ROLLER TRAY NR 6. REPAIRED NR 6 ROLLER TRAY IAW SRM 53-10-15. (M) 2 L 7 2 4F RT A35EU 1996060600503 19960606 00503 EU 1996 6 6 AALA960549 1 19960408 A 5230 4031409 FITTING AIRBUS 300 A300B4605R 3930308 EU BS 1450 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 25071 514 TUL - LOWER FORWARD CORNER FITTING ON FORWARD CARGO DOOR IS CORRODED. REMOVED AND REPLACED PART. (M) 2 L 7 2 4F RT A35EU 1996060600504 19960606 00504 EU 1996 6 6 AALA960550 1 19960408 A 5230 4031417 FITTING AIRBUS 300 A300B4605R 3930308 EU BS 1711 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 25071 514 TUL - FOUND LOWER AFT CORNER FITTING ON FORWARD CARGO DOOR CORRODED. REMOVED AND REPLACED PART. (M) 2 L 7 2 4F RT A35EU 1996060600505 19960606 00505 EU 1996 6 6 AALA960551 1 19960408 A 5313 LONGERON AIRBUS 300 A300B4605R 3930308 EU BS 4468 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 25071 514 TUL - FOUND LONGERON HAS CORROSION DAMAGE UNDER INTERCOSTAL , BELOW SIDE WALL SUPPORT STRUCTURE. REMOVED AND REPLACED S TRINGER, PER SRM 33-10-14, PG 201. (M) 2 L 7 2 4F RT A35EU 1996060600506 19960606 00506 NM 1996 6 6 AALA960554 1 19960401 A 3232 65267625 ACT FITTING BOEING 727 727227 1384078 NM LT MLG DOOR DEFECTIVE A A AALA O OTHER D INFLIGHT SEPARATION CL CLIMB 1 SW 07 726AA 20733 MIA - 882 - AFTER TAKEOFF SDQ DURING CLIMB, LOUD THUMP NOTED THROUGH OUT AIRCRAFT. SUBSEQUENTLY, BUZZING SOUND NOTED AT SPEEDS ABOVE 280 KNOTS WHICH SEEMED TO COME FROM LOWER LEFT NOSE AREA. NO OTHER ABNORMAL INDICATIONS AND AIRCRAFT PROC EEDED TO MIA AND LANDED WITHOUT INCIDENT. AFTER GATE ARRIVAL, FOUND LEFT MAIN LANDING GEAR STRUT DOOR MISSING. AIRCRAF T MAINTENANCE FERRY MIA/TUL. REPAIRED DOOR ACTUATOR ROD SUPPORT FITTING AND REPLACED LEFT MAIN LANDING GEAR STRUT DOOR. ACCOMPLISHED RIGGING AND LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996060600507 19960606 00507 EU 1996 6 6 AALA960555 1 19960403 A 3230 71540 SEQ VLV FOKKER F28 F28MK0100 4990807 EU NLG DEFECTIVE A AALA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 1413A 11376 DFW - FLT 774 - AFTER TAKEOFF MTY, NOSE LANDING GEAR MESSAGE APPEARED. RECYCLED LANDING GEAR WITH SAME RESULTS. VISUAL LY CONFIRMED NOSE LANDING GEAR RETRACTED BUT DOORS WERE OPEN. CLIMBING THROUGH FL 180, NOSE LANDING GEAR DOORS CLOSED A ND ALL INDICATIONS RETURNED TO NORMAL. AIRCRAFT PROCEEDED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GE AR SEQUENCE VALVE AND FLOW RESTRICTOR. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1996060600508 19960606 00508 EU 1996 6 6 AALA960556 1 19960410 A 5320 CHANNEL AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - FOUND CORROSION ON J-CHANNEL AT FRAME 73 UNDER LAV U. REMOVED AND REPLACED J-CHANNEL PER SRM 51-72-10, PRIMED AND PAINTED AND ALODINED PER SRM 51-21-00. (M) 2 L 7 2 4F RT A35EU 1996060600509 19960606 00509 EU 1996 6 6 AALA960557 1 19960410 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 72-73 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - FOUND FLOORBOARD SUPPORT FLANGE IS HEAVILY CORRODED BETWEEN FRAMES 72 AND 73 AT FLANGE NR 4 FROM LEFT. REPLACED F LOORBOARD SUPPORT NR 4 FROM LEFT AT FRAME 71-5-74-5 PER AARD 51-10-00-3 AND INSTALLED SUPPORT PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 1996060600510 19960606 00510 EU 1996 6 6 AALA960558 1 19960410 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FRAME 73/74 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - FOUND CORROSION ON SEAT TRACK SECTION JUST INSIDE R4 DOOR BETWEEN FRAMES 73 AND 74. REPLACED SEAT TRACK SECTION J UST INSIDE R4 DOOR BETWEEN FRAMES 73 AND 74 AARD 51-10-00 AND INSTALLED SUPPORT PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1996060600511 19960606 00511 EU 1996 6 6 AALA960559 1 19960410 A 5320 CHANNEL AIRBUS 300 A300B4605R 3930308 EU BS 71.5-74.5 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - FOUND CORROSION ON J-CHANNEL BETWEEN FRAME 72 AND 73. REPLACED FLOORBOARD SUPPORT J-CHANNEL UNDER LAV-L FROM FRAM E 71.5 TO 74.5 PER AARD 51-10-00-3 AND INSTALLED SUPPORT PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1996060600512 19960606 00512 EU 1996 6 6 AALA960560 1 19960410 A 5320 CHANNEL AIRBUS 300 A300B4605R 3930308 EU FRAME 72-73 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - FOUND CORROSION ON J-CHANNEL BETWEEN FRAME 72 AND 73. REMOVED AND REPLACED J-CHANNEL PER SRM 51-72-10 AND ALODINE D, PRIMED, PAINTED. (M) 2 L 7 2 4F RT A35EU 1996060600513 19960606 00513 EU 1996 6 6 AALA960561 1 19960410 A 5753 A5794255100160 SKIN AIRBUS 300 A300B4605R 3930308 EU RT TE FLAP CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 25071 514 TUL - FOUND R/W OUTBOARD FLAP OUTBOARD END CORROSION UNDER STATIC WICK BASE. CUT OUT CORRODED AREA AND REPAIRED SKIN PE R SRM 57-50-00 FIG 205. (M) 2 L 7 2 4F RT A35EU 1996060600514 19960606 00514 EU 1996 6 6 AALA960568 1 19960406 A 3260 200444004 DAMPER FOKKER F28 F28MK0100 4990807 EU LT MLG DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 1420D 11403 ORD - FLT 218 - AFTER TAKEOFF ORD WHEN LANDING GEAR RETRACTED, MFDU MESSAGE LEFT MAIN LANDING GEAR WITH NO OTHER ABNORMA L INDICATIONS. AIRCRAFT RETURNED ORD AND LANDED WITHOUT INCIDENT. REPLACED LEFT MAIN LANDING GEAR UPSTOP DAMPER. ACCO MPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1996060600515 19960606 00515 EU 1996 6 6 AALA960576 1 19960410 A 5320 TMS6022457 ANGLE AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 25071 514 TUL - FOUND CORROSION ON TOP FLANGE OF FLOOR SUPPORT T-ANGLE. REMOVED AND REPLACED DAMAGED SECTION OF T-ANGLE AND INSTA LLED A .050 THICK 301 .5 H DOUBLER OVER TOP FLANGE OF T-ANGLE AND OVER FLOORBEAM PER ESO 30595 DATED 4/9/96. (M) 2 L 7 2 4F RT A35EU 1996060600516 19960606 00516 EU 1996 6 6 AALA960577 1 19960411 A 5320 4031567 ANGLE AIRBUS 300 A300B4605R 3930308 EU FS NR 13 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - FOUND Z-ANGLE CORRODED. DUPLICATED Z-ANGLE PER SAMPLE FROM 2024-T3. (M) 2 L 7 2 4F RT A35EU 1996060600517 19960606 00517 EU 1996 6 6 AALA960579 1 19960411 A 3230 71540 SEQ VLV FOKKER F28 F28MK0100 4990807 EU NLG DEFECTIVE A AALA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 1413A 11376 DFW - FLT 851 - AFTER TAKEOFF STL WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR MESSAGE APPEARED ON MFDU WITH AIR NOISE S INDICATING NOSE LANDING GEAR DOORS WERE OPEN. RECYCLED LANDING GEAR AND ALL INDICATIONS RETURNED TO NORMAL WITH NO AI R NOISE. AIRCRAFT PROCEEDED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR SEQUENCE VALVE AND ROD ASSE MBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1996060600518 19960606 00518 EU 1996 6 6 AALA960589 1 19960414 A 5320 A53981919202 ANGLE AIRBUS 300 A300B4605R 3930308 EU FRAME 76-78 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - FOUND ATTACH ANGLE CORRODED ALONG LENGTH AT N/P HOLES. REPLACED ATTACH ANGLE PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 1996060600519 19960606 00519 EU 1996 6 6 AALA960590 1 19960414 A 5320 A53981929201 ANGLE AIRBUS 300 A300B4605R 3930308 EU FRAME 74-76 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - FOUND ATTACH ANGLE CORRODED ALONG ENTIRE LENGTH AT N/P HOLES. REPLACED ATTACH ANGLE PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 1996060600520 19960606 00520 EU 1996 6 6 AALA960591 1 19960413 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - FOUND NR 8 SEAT TRACK CORRODED IN SEVERAL AREAS BETWEEN FRAME 26-31 IN FRONT OF LAV M AND RIGHT SERVICE CTR. INST ALLED SEAT TRACK NR 8 FROM FRAME 25.5 TO 33.5. PER AARD 51-10-00-3 AND SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1996060600521 19960606 00521 EU 1996 6 6 AALA960592 1 19960412 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - FOUND SEAT TRACK NR 3 IS HEAVILY CORRODED AT THRESHOLD TO LAV L BETWEEN FRAME 31L AND 33L. INSTALLED MANUFACTURED SEAT TRACK IAW SRM 51-71 50 PG 201-206. (M) 2 L 7 2 4F RT A35EU 1996060600522 19960606 00522 EU 1996 6 6 AALA960594 1 19960412 A 2750 A5794252620000 PIN AIRBUS 300 A300B4605R 3930308 EU NR 6 TE FLAP CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - FOUND CORROSION ON FAIL/SAFE PIN FOR NR 6 FLAP TRACK FRONT TO REAR CARRIAGE PIN. REPLACED PIN. (M) 2 L 7 2 4F RT A35EU 1996060600523 19960606 00523 EU 1996 6 6 AALA960595 1 19960412 A 5753 A5794252220000 PIN AIRBUS 300 A300B4605R 3930308 EU NR 3 FLAP TRACK CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - FOUND CORROSION ON HOLLOW PIN FOR NR 3 FLAP TRACK FRONT TO REAR CARRIAGE ATTACHMENT. REPLACED PINS. (M) 2 L 7 2 4F RT A35EU 1996060600524 19960606 00524 EU 1996 6 6 AALA960596 1 19960412 A 2750 A5794252620000 PIN AIRBUS 300 A300B4605R 3930308 EU TE FLAPS CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - FOUND FAIL/SAFE PINS FOR NR 3 AND NR 5 FLAP TRACK FRONT TO REAR G CARRIAGE PIN HAS CORROSION. REPLACED PINS. (M) 2 L 7 2 4F RT A35EU 1996060600525 19960606 00525 NM 1996 6 6 AALA960630 1 19960422 A 5347 CPN5628454 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1310-1330 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1755 48490 TUL - FOUND CORROSION AT FORWARD AND AFT INBOARD LAV 'M' ATTACH POINTS AT R-3 DOOR AT TRACK NR 7. INSTALLED NEW SECTION OF SEAT TRACK FROM STATION 1280 TO 1371, TRACK NR 7 PER SRM 53-70-00. (M) 2 L 7 3 4F RT A22WE 1996060600526 19960606 00526 WP 1996 6 6 AALA960631 1 19960423 A 3260 S189 SWITCH DOUG DC9 DC982 3022082 WP GEAR LEVER DEFECTIVE A AALA K NONE N FALSE WARNING CR CRUISE 1 SW 07 407AA 49318 DFW - FLT 1191 - EN ROUTE CLE/DFW - DURING CRUISE, ALL THREE LANDING GEAR RED LIGHTS ILLUMINATED WITH NO OTHER ABNORMAL INDICATIONS. ACCOMPLISHED QRH PROCEDURE WITH SAME RESULTS. AIRCRAFT PROCEEDED TO DFW AND LANDED WITHOUT INCIDENT. REP LACED LANDING GEAR LEVER SWITCH S1-89. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996060600527 19960606 00527 WP 1996 6 6 AALA960632 1 19960423 A 3260 833605A CONTROL UNIT DOUG DC9 DC982 3022082 WP LANDING GEAR DEFECTIVE A AALA K NONE N FALSE WARNING CL CLIMB 1 SW 07 493AA 49731 DFW - FLT 538 - AFTER TAKEOFF SFO DURING CLIMB-OUT, NOSE LANDING GEAR RED LIGHT FLICKERED ON SEVERAL TIMES. LIGHT EXTIN GUISHED AFTER AIRCRAFT WAS LEVEL IN CRUISE. AIRCRAFT PROCEEDED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED LANDING GE AR PROXIMITY SWITCH CONTROL UNIT. ALSO, REPLACED NOSE LANDING GEAR SENSORS. ACCOMPLISHED NOSE LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996060600528 19960606 00528 WP 1996 6 6 AALA960633 1 19960423 A 5313 STRINGER DOUG DC10 DC1010 3022110 WP BS 1085-1110 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 167AA 46930 TUL - FOUND DAMAGED STRINGER FROM CORROSION AT ZONE 120, STRINGER NR 49R, FROM STATION 1085-1110. CUT OUT DAMAGED STRIN GER NR 49R FWD OF CAC ACCESS DOOR AT STATION 1099, REF SRM 53-10-00. (M) 2 L 7 3 4F A22WE 1996060600529 19960606 00529 WP 1996 6 6 AALA960644 1 19960425 A 3350 LIGHT STRIP DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 447AA 49473 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD OVERWING EXIT INOPERATIVE. REPLACED EMERGENCY FLOOR LIG HT STRIP BY EMERGENCY OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996060600530 19960606 00530 NM 1996 6 6 AALA960650 1 19960426 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 626 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 702AA 22460 TUL - FOUND 6 INCHES OF 27R STRINGER REMOVED OF CORROSION, STATION 626. REMOVED CORRODED STRINGER 10 INCH PART, INSTALL ED TWO PARTS OF STRINGER ON EACH SIDE OF FLOOR FRAME STATION 620, FORWARD CARGO. (M) 2 L 7 3 4F A3WE 1996060600531 19960606 00531 NM 1996 6 6 AALA960654 1 19960426 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1177-1180 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 702AA 22460 TUL - FOUND CORROSION INSIDE STRINGER 30, STATION 1177-1180. REPLACED STRINGER BRACKET INSIDE STRINGER 30 WITH NEW PART , TREATED AND PAINTED, SRM 51-10-2. (M) 2 L 7 3 4F A3WE 1996060600532 19960606 00532 NM 1996 6 6 AALA960655 1 19960426 A 2710 65217092 CASTING BOEING 727 727223 1384074 NM WS 243.93 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 6818 19493 TUL - FOUND INBOARD AILERON QUADRANT CASTING AND WEB AT CASTING CRACKED. REMOVED AND INSTALLED NEW WEB AND QUADRANT AND CASTING. (M) 2 L 7 3 4F A3WE 1996060600533 19960606 00533 NM 1996 6 6 AALA960656 1 19960426 A 5320 CASTING BOEING 727 727223 1384074 NM BS 606-610 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 702AA 22460 TUL - FOUND ALUMINUM CASTING AND WEB BEHIND SIL PLATE HAS CORROSION. REPLACED WEB AND CASTING WITH NEW WEB AND CASTING PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1996060600534 19960606 00534 NM 1996 6 6 AALA960657 1 19960426 A 5320 STIFFENER BOEING 727 727223 1384074 NM BS 590 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 702AA 22460 TUL - FOUND SUPPORT (STIFFENER) BEHIND SIL PLATE HAS SURFACE CORROSION. REPLACED SUPPORT STIFFENER WITH NEW STIFFENER P ER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1996060600535 19960606 00535 NM 1996 6 6 AALA960658 1 19960426 A 5320 FITTING BOEING 727 727223 1384074 NM BS 950 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 702AA 22460 TUL - FOUND STATION 950 BUTT SPLICE CORRODED BETWEEN STRINGER 28-29R, AFT CARGO. REPLACED T-FITTING PER SRM 51-10-1. ( M) 2 L 7 3 4F A3WE 1996060600536 19960606 00536 NM 1996 6 6 AALA960659 1 19960426 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 875-685 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 702AA 22460 TUL - FOUND CORROSION IN INSIDE CHANNEL OF STRINGER IN BOTTOM. CUT OUT DAMAGED AREA OF STRINGER SPLICED IN NEW SECTION PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1996060600537 19960606 00537 NM 1996 6 6 AALA960660 1 19960426 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 380-384 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 702AA 22460 TUL - FOUND CREASE ANGLE CORRODED AROUND DRAIN HOLE, RIGHT FORWARD SERVICE DOOR, SILL. REMOVED AND REPLACED CREASE ANGL E, PER AARD 51-20-01-1. (M) 2 L 7 3 4F A3WE 1996060600538 19960606 00538 NM 1996 6 6 AALA960661 1 19960426 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 740 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 702AA 22460 TUL - FOUND CORROSION ON INBOARD SIDE OF STRINGER 27R CHANNEL AT 740 BULKHEAD FITTING. CUT OUT AND REMOVED DAMAGE SECTI ON OF STRINGER. INSTALLED STRINGER SPLICE AS PER SRM 53-10-3 FIG 1. (M) 2 L 7 3 4F A3WE 1996060600539 19960606 00539 NM 1996 6 6 AALA960662 1 19960426 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 580 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 702AA 22460 TUL - FOUND SHEAR TIE HAS CORROSION, STATION 580, BETWEEN STRINGER 26L AND 27L. REMOVED AND REPLACED SHEAR TIE. (M) 2 L 7 3 4F A3WE 1996060600540 19960606 00540 NM 1996 6 6 AALA960663 1 19960426 A 5311 FRAME BOEING 727 727223 1384074 NM BS 985 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 702AA 22460 TUL - FOUND BELL FRAME CORRODED WITH DEEP PITTING. INSTALLED REPLACEMENT BELL FRAME AT STATION 985, BETWEEN STRINGER 29 RT TO 30RT. (M) 2 L 7 3 4F A3WE 1996060600541 19960606 00541 NM 1996 6 6 AALA960664 1 19960426 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 950-970 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 702AA 22460 TUL - FOUND STRINGER 29R CORRODED AT BELL FRAMES FROM STATION 950 TO 970. REPLACED STRINGER 29R, INSTALLED SKIN DOUBLER PER SB 727-53-0179. STRINGER REPLACED FROM 950 TO 1005. (M) 2 L 7 3 4F A3WE 1996060600542 19960606 00542 NM 1996 6 6 AALA960665 1 19960426 A 5315 FLOOR BEAM BOEING 727 727223 1384074 NM BS 1130 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 702AA 22460 TUL - FOUND STATION 1130 FLOORBEAM LOWER SIDE HAS CORROSION UNDER NUT PLATES BL 5R TO 36L, AFTER NUT PLATE AND CUSHION T APE REMOVED. COMPLETED REPAIR PER EOS 11697 DATED 4-17-96. (M) 2 L 7 3 4F A3WE 1996060600543 19960606 00543 NM 1996 6 6 AALA960666 1 19960426 A 5330 SKIN BOEING 727 727223 1384074 NM BS 581 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 702AA 22460 TUL - FOUND CORROSION BELLY SKIN ABOVE STRINGER 27L, STATION 581. REMOVED CORROSION OUT OF LIMITS. CUT OUT AFFECTED AR EA AND INSTALLED EXTERIOR REPAIR ON SKIN IAW SRM 53-30-3 AND SRM 51-10-6. (M) 2 L 7 3 4F A3WE 1996060600544 19960606 00544 NM 1996 6 6 AALA960667 1 19960426 A 5330 SKIN BOEING 727 727223 1384074 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 702AA 22460 TUL - FOUND FUSELAGE SKIN CORROSION ON ACCESS DOOR LANDING. REMOVED CORROSION, FABRICATED AND INSTALLED SHIM, TREATED A ND PRIMED PER ESO 11697 DATED 4-2-06. (M) 2 L 7 3 4F A3WE 1996060600545 19960606 00545 WP 1996 6 6 AALA960669 1 19960426 A 5313 STRINGER DOUG DC10 DC1010 3022110 WP BS 400 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 167AA 46930 TUL - FOUND CORROSION ON LONGERONS FORWARD E/E DOOR AREA. REPLACED LONGERON PER SRM 53-10-00. (M) 2 L 7 3 4F A22WE 1996060600546 19960606 00546 WP 1996 6 6 AALA960670 1 19960426 A 5330 SKIN DOUG DC10 DC1010 3022110 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 167AA 46930 TUL - FOUND SIX RIVET HEADS TO THE RIGHT OF CENTER E/E COMPARTMENT DOOR ARE CUPPED ON FUSELAGE SKIN. REMOVED CORRODED A REA AND INSTALLED DOUBLER PER SRM 53-20-00 PG 6. (M) 2 L 7 3 4F A22WE 1996060600547 19960606 00547 EU 1996 6 6 AALA960671 1 19960426 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FRAME 16 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80058 466 TUL - FOUND CORROSION ON NR 4 SEAT TRACK FROM LEFT APPROXIMATELY FRAME 16, JUST FORWARD OF SEAT LOCKING LUGS. REMOVED A ND REPLACED DAMAGED SECTION OF SEAT TRACK PER SRM 51-21-00-0. (M) 2 L 7 2 4F RT A35EU 1996060600548 19960606 00548 WP 1996 6 6 AALA960673 1 19960426 A 5320 CASTING DOUG DC10 DC1010 3022110 WP BS 1159 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 167AA 46930 TUL - FOUND H-CASTING AT FORWARD SPAR, TO RIGHT CORNER STATION 1159 IS BROKEN THROUGH. REPAIRED H CASTING RIGHT SIDE AS STATION 1159 PER SRM 53-30-00 PAGE 7. (M) 2 L 7 3 4F A22WE 1996060600549 19960606 00549 NE 1996 6 6 AALA960675 2 19960426 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE RIGHT DEFECTIVE A AALA A UNSCHED LANDING A J FLAME/FIRE WARNING INDICATION CL CLIMB 1 SW 07 474 49649 717310 IAD - FLT 217 - ON TAKEOFF FROM DCA, RIGHT ENGINE EGT INCREASED GRADUALLY TO APPROXIMATELY 40 DEGREES CENTIGRADE HIGHER THAN LEFT ENGINE WITH ALL OTHER ENGINE PARAMETERS NORMAL. DURING CLIMB-OUT, TRAILING AIRCRAFT REPORTED NOTING SPARKS IN EXHAUST FROM RIGHT ENGINE. FLIGHT CREW DECLARED EMERGENCY AND AIRCRAFT DIVERTED TO IAD WITH RIGHT ENGINE STILL OPERATI NG. AIRCRAFT LANDED IAD WITHOUT INCIDENT. REPLACED RIGHT ENGINE. ACCOMPLISHED LEAK CHECKS AND GROUND ENGINE RUN WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F 4 F A6WE E9NE 1996060600550 19960606 00550 WP 1996 6 6 AALA960677 1 19960424 A 5313 STRINGER DOUG DC10 DC1010 3022110 WP BS 1139-1159 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 167AA 46930 TUL - FOUND STRINGER CAPS 45, 46 AND 47 HAVE CORROSION UNDERNEATH AT STATION 1139 TO 1159. REMOVED CORROSION PER 53-20- 00. CUT OUT CORROSION AREA INSTALLED REPAIR PER SRM 53-20-00 FIG 6. (M) 2 L 7 3 4F A22WE 1996060600551 19960606 00551 WP 1996 6 6 AALA960678 1 19960429 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 784 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 138AA 46911 TUL - FOUND FLOORBEAM/FLOORBOARD SUPPORT AT STATION 784 AT THRESHOLD OF FORWARD MID SERVICE CENTER IS HEAVILY CORRODED ( UNDER STAINLESS STRIP). REMOVED FLOORBOARD SUPPORT, ANGLE MADE NEW ANGLE ALODINED, PRIMED AND PAINTED. INSTALLED PER A ARD 51-10-00-1. (M) 2 L 7 3 4F A22WE 1996060600552 19960606 00552 WP 1996 6 6 AALA960679 1 19960429 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 784 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 TUL - FOUND STATION 784 CENTER FLOOR SUPPORT HAS CORROSION BETWEEN SEAT TRACKS 4 AND 5. BLENDED OUT CORROSION ALODINED, PRIMED AND PAINTED PER SRM 51-21-01 AND ECO 7349. (M) 2 L 7 3 4F A22WE 1996060600553 19960606 00553 NM 1996 6 6 AALA960680 1 19960426 A 5753 APC73602 VANE DOUG MD11 MD11 3023602 NM RT TE FLAP DELAMINATED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1755 48490 TUL - DURING C-CHECK, FOUND SMALL DELAMINATED AREA ON LOWER SURFACE AND DELAMINATION AT ONE RUB STRIP ON TOP SURFACE OF RT OUTBOARD VANE FLAP. REPAIRED DELAMINATION PER ESO 41000, DATED 4-26-96. (M) 2 L 7 3 4F RT A22WE 1996060600554 19960606 00554 WP 1996 6 6 AALA960681 1 19960429 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 784 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 TUL - FOUND STATION 784 RIGHT FLOOR SUPPORT HAS CORROSION BETWEEN SEAT TRACK 5 AND 6. BLENDED OUT CORROSION ALODINED, P RIMED AND PAINTED PER SRM 51-21-01 AND ECO 7349. (M) 2 L 7 3 4F A22WE 1996060600555 19960606 00555 WP 1996 6 6 AALA960682 1 19960429 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 784 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 TUL - FOUND STATION 784 LT FLOOR SUPPORT HAS CORROSION BETWEEN SEAT TRACK 3 AND 4. BLENDED OUT CORROSION, ALODINED AND PRIMED AND PAINTED PER SRM 51-21-01 AND PER ECO 7349. (M) 2 L 7 3 4F A22WE 1996060600556 19960606 00556 NM 1996 6 6 AALA960683 1 19960426 A 5753 ARC43022 SKIN DOUG MD11 MD11 3023602 NM RT TE FLAP DELAMINATED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1755 48490 TUL - DURING C-CHECK, FOUND DELAMINATION AT SEVERAL AREAS ON TOP AND BOTTOM OF T/E WEDGE ON RIGHT OUTBOARD T/E FLAP. RE PAIRED RIGHT OUTBOARD FLAP T/E DELAMINATION PER ESO 41000 DATED 4-26-96. (M) 2 L 7 3 4F RT A22WE 1996060600557 19960606 00557 NM 1996 6 6 AALA960684 1 19960426 A 5751 SKIN DOUG MD11 MD11 3023602 NM RT AILERON DELAMINATED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1755 48490 TUL - DURING C-CHECK, FOUND TWO PLACES OF DELAMINATION ON UPPER SURFACE OF T/E ON RIGHT OUTBOARD AILERON. REPAIRED DELA MINATION PER ESO 41000 DATED 4-26-96. (M) 2 L 7 3 4F RT A22WE 1996060600558 19960606 00558 WP 1996 6 6 AALA960685 1 19960426 A 5320 AEA01591 ANGLE DOUG DC10 DC1010 3022110 WP BS 1159 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 167AA 46930 TUL - FOUND H-CASTING AT FORWARD SPAR TOP RIGHT CORNER STATION 1159 IS BROKEN THROUGH. REPAIRED H-CASTING RIGHT STATION 1159 PER SRM 53-30-00 FIG 7. (M) 2 L 7 3 4F A22WE 1996060600559 19960606 00559 WP 1996 6 6 AALA960686 1 19960426 A 5347 TIE DOWN TRACK DOUG DC9 DC982 3022082 WP BS 1212-1231 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 466AA 49596 TUL - FOUND CORROSION ON LEFT SIDE OF LEFT TIEDOWN AT SPLICE, BETWEEN FS 1212 AND FS 1231. REPLACED LEFT TIE TRACK FROM SPLICE FS 1212 TO AFT BULKHEAD. (M) 2 L 7 2 4F A6WE 1996060600560 19960606 00560 NM 1996 6 6 AALA960687 1 19960430 A 5310 STRUCTURE BOEING 727 727227 1384078 NM BS 395-402 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 729AA 20736 TUL - FOUND LARGE DENT IN FUSELGE SKIN AND BELT FRAME DAMAGED STATION 395-400, STRINGER 21 AND 22 RT. CUT OUT DAMAGED S KIN AND BELT FRAME AND REPAIR PER SRM 53-104 PAGE 5 AND 53-30-3. (M) 2 L 7 3 4F A3WE 1996060600561 19960606 00561 NM 1996 6 6 AALA960688 1 19960430 A 5720 WING TIP BOEING 727 727223 1384074 NM RT WING DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 880AA 21519 TUL - FOUND RIGHT WING TIP DAMAGED. REMOVED DAMAGED PARTS AND REPLACED WITH NEW PER SRM 51-10-1 PG 1-15. (M) 2 L 7 3 4F A3WE 1996060600562 19960606 00562 WP 1996 6 6 AALA960691 1 19960428 A 2130 21171803 CONTROLLER DOUG DC9 DC982 3022082 WP NR 1 POSITION DEFECTIVE A AALA B G EMER. DESCENT O2 MASK DEPLOYED O OTHER CR CRUISE 1 SW 07 428AA 49340 DTW - FLT 1302 - EN RUOTE DFW/DTW - DURING CRUISE AT FL 330, UNABLE TO MAINTAIN CABIN PRESSURIZATION. ACCOMPLISHED EMER GENCY DESCENT, DROPPED ALL PASSENGER OXYGEN MASKS AND AIRCRAFT PROCEEDED TO DTW, LANDING WITHOUT INCIDENT. REPLACED NR 1 PRESSURIZATION CONTROLLER. ACCOMPLISHED PRESSURIZATION CHECK WITH NO DEFECTS FOUND. PLACARDED PASSENGER OXYGEN SYSTE M AND AIRCRAFT RETURNED TO REVENUE SERVICE WITH ALTITUDE RESTRICTION. SUBSEQUENTLY REPLACED OXYGEN CYLINDERS AND MASKS AT TUL/30. ACCOMPLISHED DROP CHECK AND LEAK CHECKS WITH NO DEFECTS FOUND. OXYGEN SYSTEM PLACARD REMOVED. (M) 2 L 7 2 4F A6WE 1996060600563 19960606 00563 NM 1996 6 6 AALA960692 1 19960430 A 5321 FLOOR BOEING 727 727223 1384074 NM BS 1169 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 887AA 21526 TUL - FOUND CORROSION ON FLOOR AROUND PLUMBING THROUGH FITTINGS FORWARD OF STATION 1183,LEFT LAV. INSTALLED DOUBLER PER SRM 51-40-2. (M) 2 L 7 3 4F A3WE 1996060600564 19960606 00564 NM 1996 6 6 AALA960693 1 19960430 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 1180 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 887AA 21526 TUL - LAV ATTACH ANGLE TO FLOOR, CORROSION ON AND AROUND FITTING, LEFT LAV. CUT OUT CORRODED AREA. INSTALLED NEW ATTAC H ANGLE, SRM 51-10-2. (M) 2 L 7 3 4F A3WE 1996060600565 19960606 00565 NM 1996 6 6 AALA960694 1 19960430 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 380 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 887AA 21526 TUL - FOUND CORROSION ON TOP OF FLOORBEAM STATION 380, RBL 24 TO RBL 56. REPAIRED PER SRM 53-10-8 FIG 1. (M) 2 L 7 3 4F A3WE 1996060600566 19960606 00566 EU 1996 6 6 AALA960695 1 19960430 A 5347 SUPPORT AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80058 466 TUL - FOUND CORROSION ON FLOORBOARD SUPPORT BETWEEN TRACKS 6 AND 7 AND FRAMES 15A AND 16. REPLACED SUPPORT ANGLE PER SR M 51-72-10. (M) 2 L 7 2 4F RT A35EU 1996060600567 19960606 00567 EU 1996 6 6 AALA960696 1 19960430 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80058 466 TUL - FOUND CORROSION IN SEAT TRACK 7 JUST FORWARD OF SEAT LOCKING LUGS APPROX FRAME 15-16. REPLACED SEAT TRACK NR 7 PE R SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 1996060600568 19960606 00568 NM 1996 6 6 AALA960698 1 19960428 A 2420 WIRE DOUG MD11 MD11 3023602 NM AVIONICS C/B PNL SHORTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1755 48490 SDO - FLT 1728 - A/C ARRIVED SDQ WITH FOLLOWING AVIONICS CIRCUIT BREAKERS TRIPPED, F-22, C-9, D-27, D-29 AND C-29. CHEC K OF CIRCUIT BREAKER PANEL REVEALED WIRE BUNDLE CHAFING WITH SHARP EDGE WHICH CUT WIRE INSULATION CAUSING SHORTS. ACCOM PLISHED INTERIM WIRING REPAIRS AND AIRCRAFT MX FERRY SDQ/JFK. REPAIRED WIRING B203-110-24, B203-305-24, B203-816-22 RD BL 4E B203-537-22, B203-50-22, B102-1050-22, B102-2012-18, B102-7013-18N, B102-234-18 AND B102-2015-16N. ACCOMPLISHED G ROUND CHECK OF NR 2 HF, NR 2 DEV MARKER BEACON, ACARS, ENTERTAINMENT SYSTEM, DC BUS 1, 2 AND 3 SLAT POSITION INDICATOR. CIRCUIT BREAKER PANEL LIGHTING AND INTERPHONE CALL. SYSTEMS GROUND CHECKED NORMAL OPS. (M) 2 L 7 3 4F RT A22WE 1996060600569 19960606 00569 WP 1996 6 6 AALA960699 1 19960430 A 5320 SKATE ANGLE DOUG DC9 DC982 3022082 WP BS 1474 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 411AA 49322 TUL - FOUND LEFT VERTICLE SKATE ANGLE DOUBLER CRACKED FS 1474. ACCOMPLISHED REPAIR PER AARD 53-10-00-2. (M) 2 L 7 2 4F A6WE 1996060600570 19960606 00570 WP 1996 6 6 AALA960700 1 19960430 A 5320 3936595501 CLIP DOUG DC9 DC982 3022082 WP BS 1220 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 411AA 49322 TUL - FOUND CLIP CORRODED AFT SIDE OF FRAME BELOW RIGHT TIEDOWN TRACK IN AFT CARGO. REMOVED CLIP. INSTALLED NEW CLIP. (M) 2 L 7 2 4F A6WE 1996060600571 19960606 00571 NM 1996 6 6 AALA960729 1 19960503 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1321-1341 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1756 48491 TUL - FOUND CORROSION ON SEAT TRACK NR 2 UNDER LAV L AFT TIE DOWN FOOT AREA. REPLACED SEAT TRACK SECTION PER SRM 53-70- 00 VOL II. (M) 2 L 7 3 4F RT A22WE 1996060600572 19960606 00572 NM 1996 6 6 AALA960730 1 19960503 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1321-1341 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1756 48491 TUL - FOUND HEAVY CORROSION ON NR 2 SEAT TRACK UNDER MID LAV LEFT. REPLACED SEAT TRACK SECTION PER SRM 53-70-00 VOL 2, TREATED AND PAINTED. (M) 2 L 7 3 4F RT A22WE 1996060600573 19960606 00573 NM 1996 6 6 ASAA9610062 1 19960507 A 3350 8821004 BATTERY PACK BOEING 737 737298C 1384490 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROW 19. ALSO, THE 'EXIT TO REAR' EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED BATTERY PACKS AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996060600574 19960606 00574 NM 1996 6 6 ASAA9640038 1 19960508 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 763AS 25100 SEA - DURING MAINTENANCE CHECK, THE FORWARD TWO EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNE CTED LIGHTS AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996060600575 19960606 00575 NM 1996 6 6 ASAA9640039 1 19960514 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 772AS 25105 ANC - DURING MAINTENANCE CHECK, THE AFT FIVE EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED AFT FIVE EMERGENCY LIGHTS AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996060600576 19960606 00576 WP 1996 6 6 ASAA9680114 1 19960502 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 977AS 3338 53453 SEA - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996060600577 19960606 00577 WP 1996 6 6 CAL960500 1 19960418 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 12538 47218 IAH - FLT 1902 - INSPECTION FOUND FORWARD SECTION OF AISLE PATH LIGHTING INOPERATIVE. THE FORWARD CABIN BATTERY PACK WA S REPLACED AND OPERATION OF THE LIGHTS WAS RESTORED. (M) 2 L 7 2 4F A6WE 1996060600578 19960606 00578 NM 1996 6 6 CAL960530 1 19960316 A 5312 BULKHEAD ANGLE BOEING 727 727227 1384078 NM BS 340 CORROSION A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15774 21242 DURING INSPECTION, FOUND CORROSION AT LOWER L-ANGLE. REMOVED ATTACH ANGLE FROM AFT BLKHD FABRICATED SHIM FOR ANGLE, ALO DINED, PRIMED AND INSTALLED PER IAW 727 SRM 51-30-2, 51-10-1 AND 53-10-2. (M) 2 L 7 3 4F A3WE 1996060600579 19960606 00579 NM 1996 6 6 CAL960531 1 19960315 A 5313 BAC14981312 STRINGER BOEING 727 727227 1384078 NM BS 740 CORROSION A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15774 53819 21242 DURING INSPECTION, FOUND BS 740 FORWARD CARGO COMPARTMENT STRINGER-27L AND ENDING FITTING HAS CORROSION. REMOVED CORROS ION ON END FITTING .002 TO FALL WITHIN LIMITS AT STRINGER 27L BS 740. CUT OUT FABRICATED NEW STRINGER SEC AT STRINGER 2 7L AND STRAP FOR STRINGER REPAIR, TREAT INSTALLED PER SRM 51-10-2, 6 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1996060600580 19960606 00580 NM 1996 6 6 CAL960532 1 19960318 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 422 CORROSION A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15774 53819 21242 DURING INSPECTION, FOUND CORROSION BEYOND LIMITS AT BS 422A STRINGER 26R. REMOVED CORRODED STRINGER IAW SRM 53-10-3, FA BRICATED NEW PART PER IAW B727 SRM 53-10-3 ALODINED AND PRIMED PART PER IAW B727 SRM 51-10-6, INSTALLED PART PER SRM 53- 10-3. (M) 2 L 7 3 4F A3WE 1996060600581 19960606 00581 NM 1996 6 6 CAL960533 1 19960312 A 5320 ANGLE BOEING 727 727227 1384078 NM BS 1130 CORROSION A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15774 53819 21242 DURING INSPECTION, FOUND CORROSION AT BS 1130 WEB BETWEEN STRINGER 30 AND STRINGER 29R. REMOVED CORROSION AND CORRODED REINFORCEMENT ANGLE FABRICATED REPAIR ANGLE FOR WEB AND REINFORCEMENT ANGLE SRM 51-10-6 AND B727 MM 51-20-11 AND INSTALL ED PER SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1996060600582 19960606 00582 NM 1996 6 6 CAL960534 1 19960317 A 5320 ANGLE BOEING 727 727227 1384078 NM BS 580 CORROSION A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15774 53819 21242 DURING INSPECTION, FOUND CORROSION AT BS 580 STRINGER 28R AND STRINGER 28L FORWARD CARGO CIRCUMFERENTIAL SHEAR TIE. CUT OUT CORRODED SHEAR TIE, FABRICATED ANGLE DOUBLER, SHEAR TIE REPAIR, TREATED, PRIMED AND INSTALLED PER IAW B727 SRM 53-1 0-4, 51-10-2 AND MAINTENANCE MANUAL 51-20-31. (M) 2 L 7 3 4F A3WE 1996060600583 19960606 00583 NM 1996 6 6 CAL960535 1 19960318 A 5315 FLOOR BEAM BOEING 727 727227 1384078 NM BS 344 CORROSION A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15774 53819 21242 DURING INSPECTION, FOUND CORROSION AT MAIN CABIN FLOOR BEAM UPPER CAP. REMOVED CORRODED T-CAP, FABRICATED, TREATED, PRI MED. INSTALLED NEW T-CAP PER SRM 51-20-01 AND 53-10-04. (M) 2 L 7 3 4F A3WE 1996060600584 19960606 00584 NM 1996 6 6 CAL960536 1 19960318 A 5347 BAC1520792 SEAT TRACK BOEING 727 727227 1384078 NM BS 340-480 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15774 53819 21242 DURING INSPECTION, FOUND CORRODED SEAT TRACK. REMOVED SEAT TRACK FROM RBL 48 STATION 340 TO 480. FABRICATED AND INSTAL LED NEW SEAT TRACK SEC. (M) 2 L 7 3 4F A3WE 1996060600585 19960606 00585 NM 1996 6 6 CAL960537 1 19960318 A 5347 BAC1520792 SEAT TRACK BOEING 727 727227 1384078 NM BS 380-420 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15774 21242 DURING INSPECTION, FOUND CORROSION AT BS 380 TO 420 BL 24R AND BL 48R SEAT TRACK. FABRICATED SEAT TRACK SEC BS 380 TO 4 20 PER IAW B727 SRM 53-10-5. TREATED AND PRIMED PER SRM 51-10-2. (M) 2 L 7 3 4F A3WE 1996060600586 19960606 00586 NM 1996 6 6 CAL960538 1 19960318 A 5320 617179 SUPPORT BOEING 727 727227 1384078 NM BS 312-344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15774 53819 21242 DURING INSPECTION, FOUND CORROSION AT MAIN CABIN INTERIOR FLOOR SUPPORT. FABRICATED SUPPORT ANGLES, ALODINED, PRIMED AN D INSTALLED PER SRM 51-10-2, 51-30-2 AND 53-10-2. (M) 2 L 7 3 4F A3WE 1996060600587 19960606 00587 NM 1996 6 6 CAL960540 1 19960318 A 5320 ANGLE BOEING 727 727227 1384078 NM DOOR L-1 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15774 21242 DURING INSPECTION, FOUND CORROSION AT L-1 DOOR SILL L-ANGLE. FABRICATED REPAIR ANGLE, CUT OUT CORRODED AREA HEAT TREATE D MATERIAL, DRILLED AND COUNTER SUNK HOLES, ALODINED AND PRIMED, INSTALLED DOUBLER PER SRM 51-40-3 AND INSTALLED FILLER 51-40-3. (M) 2 L 7 3 4F A3WE 1996060600588 19960606 00588 NM 1996 6 6 CAL960547 1 19960325 A 5320 ANGLE BOEING 727 727227 1384078 NM BS 1176 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15774 53819 21242 DURING INSPECTION, FOUND BS 1176 CHORD LBL 27.5 LEFT LAV INBOARD WALL LOWER ATTACH ANGLE HAS CORROSION. REMOVED CORROSI ON FABRICATED, REPAIR INSTALL PER IAW B727 SRM 51-10-2, 51-30-2, MM 51-40-5. (M) 2 L 7 3 4F A3WE 1996060600589 19960606 00589 NM 1996 6 6 CAL960548 1 19960314 A 5210 SKIN BOEING 727 727227 1384078 NM R-1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15774 53819 21242 DURING INSPECTION, FOUND R-1 DOOR SKIN LOWER AFT CORNER HAS APPROX 1 INCH CRACK THROUGH SCREW HOLE. REPAIRED IAW B727 S RM 52-20-2 FABRICATED WITH 2024-T3 .050 CLAD. PRIMED AND TREATED IAW B727 SRM 51-10-2. INSTALLED DOUBLER (4 INCH BY 4 INCH) PER SRM 51-30-2 CRACK STOP DRILLED SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1996060600590 19960606 00590 NM 1996 6 6 CAL960549 1 19960315 A 5210 LINER BOEING 727 727227 1384078 NM L-1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15774 53819 21242 DURING INSPECTION, FOUND NUMEROUS CRACKS AROUND OUTER EDGES AND AROUND ASSISTS HANDLE. FABRICATED INTERNAL DOUBLER ALOD INED, PRIMED, AND INSTALLED PER IAW B727 SRM 52-10-2, 51-30-2 AND 52-20-11, CRACKS STOP DRILLED 51-10-1 EDDY CURRENT REV EALED NO FURTHER CRACKING. (M) 2 L 7 3 4F A3WE 1996060600591 19960606 00591 NM 1996 6 6 CAL960550 1 19960320 A 5320 FLANGE BOEING 727 727227 1384078 NM BS 360 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15774 53819 21242 DURING INSPECTION, FOUND AT BS 360 FORWARD LOWER FUSELAGE S-26R UPPER OUTBOARD FLANGE HAS 1 INCH SECTION CORRODED. REMO VED CORROSION REPAIRED, FABRICATED, ALODINED PRIMED AND INSTALLED PER IAW B727 SRM 51-10-6, 53-10-3, 51-10-2, 53-10-3. ( M) 2 L 7 3 4F A3WE 1996060600592 19960606 00592 WP 1996 6 6 CAL960551 1 19960428 A 5210 SEAL DOUG DC9 DC932 3022066 WP AFT ENTRY DOOR DIRTY A CALA O OTHER O OTHER CR CRUISE 1 SW 09 12538 47218 FLT NR 1198 - MCO - DURING CRUISE, CABIN PRESSURE BEGAN TO CLIMB DESCENDED TO 10,000, WAS ABLE TO GAIN CONTROL IN MANUAL . FOUND AFT ENTRY DOOR HAD TRASH AROUND SEAT. ALSO, FOUND LEAK AT MLG VIEWING PORT DUE TO COLLAR NOT SEATED PROPERLY. REMOVED AND REPLACED COLLAR AND PROPERLY SEATED COLLAR, LEAK CHECK OK. (M) 2 L 7 2 4F A6WE 1996060600593 19960606 00593 EU 1996 6 6 COEA9672001 1 19960418 A 5210 5907047901 BRACKET FOKKER F27 F27MK500 4990629 EU CREW DOOR LOOSE A COEA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 13 720FE 10464 APPROXIMATELY 30 MINUTES AFTER DEPARTURE, THE CREW HEARD A LOUD BANG. PNEUMATIC AND CABIN PRESSURE FLUCTUATED AND DROPP ED SLIGHTLY. THE CREW ELECTED TO TURN BACK TO LAS. ENGINE AUTO FEATHERED WHILE ON APPROACH. AN EMERGENCY WAS DECLARED . A/C LANDED WITHOUT INCIDENT. EMPIRE IS INVESTIGATING ENGINE, PNEUMATIC AND PRESSURIZATION AT THIS TIME. FOUND UPPER AFT CREW DOOR ROLLER BRACKET LOOSE. INSPECTED OIL FILTERS. NO DEFECTS. REPLACED LP FUEL FILTER AND LOW TORQUE SWITCH AS A PRECAUTIONARY MEASURE. ENGINE GROUND RUN FOUND NO FURTHER DISCREPANCIES. ADJUSTED DOOR ROLLER ASSEMBLY, TIGHTENE D ATTACHING BOLTS, PRESSURIZED AIRCRAFT. NO LEAKS NOTED. OPERATIONAL CHECK FLIGHT FOUND SATISFACTORY. (M) 2 H 7 2 4T A817 1996060600594 19960606 00594 NM 1996 6 6 IXKA960027 1 19960508 A 7931 D9798 UNION ORIFICE BOEING 727 727251 138408H NM NR3 ENG PRESS SW CLOGGED A IXKA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 EA 25 267US 20289 FLT NR 72 - TPA-ATL - IN FLIGHT SHUTDOWN, NR 3 ENGINE LOW OIL PRESS OIL FILTER BYPASS LIGHT ILLUMINATED DURING FLIGHT. N R 3 OIL TEMP ROSE FROM 81 TO 110 DEGREES. SHUT DOWN AS PER EMERGENCY CHECK LIST. REMOVED AND REPLACED NR 3 ENGINE OIL PRESSURE UNION ORIFICE AT OIL PRESS MANIFOLD RUNUP AND LEAK CHECK NORMAL PER MM 79-32-00. (M) 2 L 7 3 4F A3WE 1996060600595 19960606 00595 1996 6 6 IXKA960028 4 19960513 A 3456 4573000434 OMEGA RPU LITTON BOEING 727 727225 1384077 NM COCKPIT INOPERATIVE A IXKA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 25 8881Z 21578 FLIGHT NR 2, EWR-BDA - AIR TURN BACK DUE TO OMEGA READING ERROR WITH FLIGHT PLAN. REMOVED AND REPLACED OMEGA RPU, OPS C HECK OK AS PER MM 34-68-01. (M) 2 L 7 3 4F A3WE 1996060600596 19960606 00596 SW 1996 6 6 MALA964971 1 19960420 A 2150 20475546 PACK SWRNGN SA227 SA227AC 8780603 SW RT WING ROOT SEIZED A MALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 436MA AC719B FLIGHT RN 3019 - WHILE TAXIING IN DTW, THE CREW NOTED A SMOKE SMELL IN THE CABIN. THE CREW TURNED THE BLEEDS OFF AND TH E SMOKE DISSIPATED. MAINTENANCE REPLACED THE RIGHT COOLING TURBINE. SYSTEM OPERATED SATISFACTORILY. (M) 2 L 7 2 4T RT A8SW 1996060600597 19960606 00597 NM 1996 6 6 MALA964972 1 19960423 A 3230 10800113 UPLOCK ACTUATOR DHAV DHC8 DHC8102 2809003 NM RT MLG FAILED A MALA O OTHER J WARNING INDICATION CR CRUISE 1 GL 15 826MA 330 FLT 3066 - IN CRUISE FLIGHT TO AZO, THE CREW NOTED THAT THE RIGHT GEAR BEGAN TO CYCLE IN THE WHEEL WELL. MAINTENANCE RE PLACED THE RIGHT MAIN LANDING GEAR UPLOCK ACTUATOR. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2 H 7 2 4T RT A13NM 1996060600598 19960606 00598 NM 1996 6 6 MALA964973 1 19960423 A 3260 841005 PSEU DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A MALA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 15 852MA 349 FLT 3319 - ON APPROACH TO BMI, THE CREW NOTED AN ELECTRICAL SMELLING SMOKE IN THE COCKPIT AND CABIN. MAINTENANCE REPLAC ED THE PSEU. ALL CHECKS SATISFACTORY. (M) 2 H 7 2 4T RT A13NM 1996060600599 19960606 00599 NM 1996 6 6 MALA964974 1 19960424 A 3340 3TC1225 CIRCUIT BREAKER DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A MALA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 15 852MA 349 FLIGHT 3115 - ON APPROACH TO MSP, THE CREW NOTED AN ODOR IN THE COCKPIT, AND THE CAPTAINS LOWER RIGHT CIRCUIT BREAKER WA S HOT. MAINTENANCE REPLACED THE LEFT APPROACH LIGHT JUMPER WIRE (FROM THE BUS BAR TO THE CIRCUIT BREAKER), AND CIRCUIT BREAKER. ALL CHECKS WERE SATISFACTORY. (M) 2 H 7 2 4T RT A13NM 1996060600600 19960606 00600 NM 1996 6 6 MALA964982 1 19960503 A 3350 82420006021 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 832MA 341 FLT 3136 - DURING THE PREFLIGHT WALKAROUND IN DTW, THE EMERGENCY LIGHT ON THE RIGHT SIDE OF ROW 4 WAS PARTIALLY DETACHED AND THE LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. ALL CHECKS WERE SATISFACTORY. (M) 2 H 7 2 4T RT A13NM 1996060600601 19960606 00601 SW 1996 6 6 MALA964983 1 19960507 A 3230 1EN516 SWITCH SWRNGN SA227 SA227AC 8780603 SW NLG OUT OF ADJUST A MALA K NONE J WARNING INDICATION CL CLIMB 1 GL 15 438MA AC721B FLT 3008 - ON CLIMB-OUT FROM MKG, THE NOSE GEAR CYCLED ONCE BEFORE COMING UP AND LOCKED ON GEAR RETRACTION. MAINTENANCE ADJUSTED THE RIGGING OF THE UP POSITION SWITCH. SYSTEM OPERATED SATISFACTORILY. (M) 2 L 7 2 4T RT A8SW 1996060600602 19960606 00602 NM 1996 6 6 MALA964984 1 19960505 A 3350 6104789 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 853MA 353 DURING A PREFLIGHT INSPECTION IN MSP, THE CREW NOTED THAT AN EMERGENCY LIGHT IN THE FRONT AND AFT CABIN AREA WERE INOP. MAINTENANCE REPLACED THE BATTERY PACK IN THE OVERHEAD POSITION AT ROW 3. SYSTEM OPERATED SATISFACTORILY. (M) 2 H 7 2 4T RT A13NM 1996060600603 19960606 00603 NM 1996 6 6 MALA964985 1 19960504 A 2611 CONNECTOR DHAV DHC8 DHC8102 2809003 NM SMOKE DETECTORS LOOSE A MALA K NONE N FALSE WARNING CR CRUISE 1 GL 15 831MA 339 FLT 3059 - IN CRUISE FLIGHT TO DTW, THE SMOKE WARNING LIGHT ILLUMINATED SEVERAL TIMES FOR 3 TO 5 SECONDS. NO EVIDENCE O F SMOKE NOTED. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. MECHANICS CLEANED AND RESECURED THE CANNON PLUGS A T THE SMOKE DETECTOR. THE WARNING CONTROL UNIT WAS REPLACED AS A PRECAUTION. (M) 2 H 7 2 4T RT A13NM 1996060600604 19960606 00604 NM 1996 6 6 RAAAB196003 1 19960308 A 5711 SPAR CAP BOEING 727 72722C 138400F NM WS 410 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 54280 19093 DURING SCHEDULED C-CHECK, INSPECTION OF RIGHT WING FOUND FORWARD LOWER SPAR CAP CORRODED AT WS 410. REPAIRED PER BOEING MSG 7271-96-0571. (M) 2 L 7 3 4F A3WE 1996060600605 19960606 00605 NM 1996 6 6 RAAAB196004 1 19960308 A 5320 WEB BOEING 727 72722C 138400F NM MCD SILL CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 54279 19093 DURING SCHEDULED C-CHECK INSPECTION OF MCD SILL, FOUND WEB CRACKED AND CORRODED AT THE FOLLOWING, BS 487, 499-506, 537-5 48, 552-562, 577-587, 597-607 AND 610-617. REPLACED WEB PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1996060600606 19960606 00606 NM 1996 6 6 RAAAB196005 1 19960308 A 5320 SHEAR TIE BOEING 727 72722C 138400F NM MCD SILL CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 54279 19093 DURING SCHEDULED C-CHECK INSPECTION OF MCD LOWER SILL, FOUND FOLLOWING FRAME SHEAR TIES CRACKED, BS 580, BS 560, BS 540, BS 500. REPAIRED PER SRM 53-10-4, PG 54-57, FIG 14 SHEET 1. (M) 2 L 7 3 4F A3WE 1996060600607 19960606 00607 NM 1996 6 6 RAAAB196006 1 19960308 A 5330 SKIN BOEING 727 72722C 138400F NM BS 235 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 54279 19093 DURING SCHEDULED C-CHECK INSPECTION OF FWD FUSELAGE, FOUND CRACK IN SKIN AT LEFT FORWARD NLG DOOR HINGE CUTOUT. REPAIRE D PER SRM 53-30-3 FIG 3A, SHEET 1. (M) 2 L 7 3 4F A3WE 1996060600608 19960606 00608 NM 1996 6 6 RAAAB196007 1 19960308 A 5312 BULKHEAD BOEING 727 72722C 138400F NM BS 259 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 54279 19093 DURING SCHEDULED C-CHECK INSPECTION OF NLG WHEEL WELL, FOUND LEFT PRESSURE BULKHEAD CRACKED AT BS 259. REPAIRED PER SRM 51-4-2. (M) 2 L 7 3 4F A3WE 1996060600609 19960606 00609 NM 1996 6 6 RAAAB296026 1 19960326 A 3350 8621014 BATTERY PACK 873100212 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 MID CABIN DOOR EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. (M) 2 L 7 3 4F A3WE 1996060600610 19960606 00610 NM 1996 6 6 RAAAB296027 1 19960426 A 5321 PRESS FLOOR BOEING 727 72722C 138400F NM BS 940 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 55140 19098 DURING SCHEDULED INSPECTION OF THE PRESS FLOOR IN THE LEFT WHEEL WELL PER AD 92-19-11, FOUND THE FOLLOWING 5 CRACKS AT S TATION 940, BL 29-1 .375 INCH, BL 31 .625 INCH, BL 36 .375 INCH, BL 38 .75 INCH AND BL 55 1.125 INCH. REPAIRED PER SB 5 3-0149 RV AND DWG 65-89360. (M) 2 L 7 3 4F A3WE 1996060600611 19960606 00611 WP 1996 6 6 RAAAE496003 1 19960402 A 3350 1000553 LIGHT LKHEED 188 188A 5262602 WP CABIN INOPERATIVE A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 9744C 188A1140 RIGHT AFT EMERGENCY EXIT DOOR EMERGENCY LIGHT FAILED SERVICE CHECK. CHANGED LIGHT ASSEMBLY. (M) 2 L 7 4 4T RT 4A22 1996060600612 19960606 00612 WP 1996 6 6 RAAAE496005 1 19960424 A 2915 14050 HYD VALVE LKHEED 188 188A 5262602 WP NR 1 HYD SYS BLOWN GASKET A RAAA H DEACTIVATE SYST/CIRCUITS K FLUID LOSS CL CLIMB 1 AL 03 9744C 188A1140 NR 1 HYD SYSTEM FLUID DRAINED T ZERO AFTER DEPARTURE FROM SDP. SHUT OFF 1 AND 1A PUMPS. REPLACED HYD SYSTEM NR 1 PRIOR ITY VALVE DUE BLOWN CAP GASKET. (M) 2 L 7 4 4T RT 4A22 1996060600613 19960606 00613 SO 1996 6 6 RAAAE896006 1 19960308 A 3350 8621014 BATTERY PACK LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 AFT PASSENGER CABIN EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE . (M) 2 L 7 4 4T 4A22 1996060600614 19960606 00614 SO 1996 6 6 RAAAE96003 1 19960305 A 3350 S102 BATTERY GRIMES 1000553 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 LEFT OVERWING EMERGENCY EXIT PULL DOWN LIGHT WOULD NOT TEST ON SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. ( M) 2 L 7 4 4T 4A22 1996060600615 19960606 00615 WP 1996 6 6 RAAAE96004 1 19960415 A 3230 350511 BUNGEE 8038451 LKHEED 188 188A 5262602 WP RT MLG BROKEN A RAAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 9744C 188A1140 RETURNED TO ANCH DUE TO RIGHT MLG UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION, WHEN GEAR HANDLE PUT TO NEUTRAL RIGHT MLG SHOWED DOWN AND LOCKED. MX FOUND DOOR ACTUATING HOOK ASSY BUNGE BROKEN, CAUSING THE HOOK TO RELAX AND THE DOORS TO CLOSE AHEAD OF THE MLG. (M) 2 L 7 4 4T RT 4A22 1996060600616 19960606 00616 SO 1996 6 6 RAAAE996004 1 19960305 A 3350 1000553 LIGHT LKHEED 188 188C 5262604 SO CABIN FAILED TEST A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 FORWARD PASSENGER ENTRY DOOR EMERGENCY LIGHT FAILED SERVICE CHECK. REPLACED LIGHT ASSEMBLY. (M) 2 L 7 4 4T 4A22 1996060600617 19960606 00617 EU 1996 6 6 RAIA960422 1 19960415 A 5270 SP4594 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU CARGO BAY OUT OF ADJUST A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 03 557HK 41074 BOS - FLT 7725 - CARGO DOOR LIGHT ILLUMINATED DURING TAKEOFF. MAINTENANCE ISSUED DMI 52-3, MAINTENANCE LATER CLEARED DM I BY ADJUSTING DOOR MICROSWITCH, OPERATION CHECK GOOD. (M) 2 L 7 2 4T RT A41NM 1996060600618 19960606 00618 EU 1996 6 6 RAIA960425 1 19960419 A 5270 SP4594 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU CARGO BAY OUT OF ADJUST A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 550HK 3055 41039 ORF - FLT 7754 - BAGGAGE DOOR WARNING ILLUMINATED DURING TAKEOFF. MAINTENANCE ISSUED DMI 52-3, MAINTENANCE LATER CLEARE D DMI BY ADJUSTING DOOR MICRO-SWITCH, OPERATION CHECK GOOD. (M) 2 L 7 2 4T RT A41NM 1996060600619 19960606 00619 EU 1996 6 6 RAIA960426 1 19960417 A 5270 91SE13 SWITCH BAG JETSTM JETSTM3201 1500217 EU PAX DOOR OUT OF ADJUST A RAIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 03 428AM 11017 877 STL - 7420 - PASSENGER DOOR LIGHT ILLUMINATED DURING FLIGHT. MAINTENANCE ISSUED DMI 52-2. MAINTENANCE CLEARED DMI BY A DJUSTING PAX DOOR MICROSWITCH. (M) 2 L 7 2 4T RT A56EU 1996060600620 19960606 00620 WP 1996 6 6 RAIA960428 2 19960418 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LEFT LOW POWER A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CE 03 342TE 7126 954 66317 STL - FLT 7372 - LEFT ENGINE WOULD NOT MAKE TARGET TORQUE. MX REPLACED LEFT ENGINE PERFORMED GROUND RUNS, OPERATIONAL C HECKS GOOD. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996060600621 19960606 00621 EU 1996 6 6 RAIA960429 1 19960422 A 7712 31024766 TQ SIGNAL COND BAG JETSTM JETSTM3201 1500217 EU RT ENG OUT OF ADJUST A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CE 03 428AM 11046 7378 877 STL - FLT 7442 - RIGHT ENGINE DID NOT MAKE TARGET TORQUE. MX ADJUSTED TORQUE SIGNAL CONDITIONER, GROUND RUNS GOOD. (M) 2 L 7 2 4T RT A56EU 1996060600622 19960606 00622 EU 1996 6 6 RAIA960431 1 19960422 A 7933 MS280343 OIL TEMP BULB BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 342TE 9487 954 CMI - FLT NR 7512 - IN FLIGHT LEFT ENGINE OIL TEMPERATURE ROSE TO 140 DEGREES THEN DROPPED TO 130 DEGREES, OIL PRESS APP ROXIMATELY 118 PSI. MX REPLACED LEFT ENGINE OIL TEMP BULB PERFORMED GROUND RUNS OPERATIONAL CHECKS GOOD. (M) 2 L 7 2 4T RT A56EU 1996060600623 19960606 00623 EU 1996 6 6 RAIA960432 1 19960423 A 7722 3036836 ITT WIRE AEROSP ATR42 ATR42300 8680920 EU LT ENGINE BROKEN A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 421TE 14147 102 STL - FLT NR 7398 - LEFT ENGINE ITT GAUGE FLUCTUATES 0-950 DEGREES, ALL OTHER PARAMETERS NORMAL. MAINTENANCE REPAIRED B ROKEN WIRE ON LEFT ENGINE T6 HARNESS, PERFORMED GROUND RUNS OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A53EU 1996060600624 19960606 00624 EU 1996 6 6 RAIA960433 1 19960426 A 5270 91SE13 SWITCH BAG JETSTM JETSTM3201 1500217 EU PAX DOOR OUT OF ADJUST A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 435AM 10669 889 STL - FLT 7390 - PASSENGER DOOR CAPTION ILLUMINATED IN FLIGHT. MX ISSUED DMI 52-2 CAT C. LEFT UPPER MICROSWITCH TO BE ADJUSTED. (M) 2 L 7 2 4T RT A56EU 1996060600625 19960606 00625 EU 1996 6 6 RAIA960434 1 19960426 A 7712 31024766 TQ SIGNAL COND BAG JETSTM JETSTM3201 1500217 EU LT ENG OUT OF ADJUST A RAIA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CE 03 342TE 7907 7907 954 STL - FLT 67 - LEFT ENGINE SHORT ON TARGET TORQUE. MAINTENANCE ADJUSTED TORQUE SIGNAL CONDITIONER. PERFORMED GROUND RU NS OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A56EU 1996060600626 19960606 00626 EU 1996 6 6 RAIA960435 1 19960428 A 2612 2TP17 TEST SWITCH BAG JETSTM JETSTM3201 1500217 EU COCKPIT DIRTY A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 430AM 10925 880 STL - FLT 7080 - LEFT ENGINE FIRE DETECT LIGHT CAME ON. MX INSPECTED SYSTEM, AND CLEANED FIRE DETECT TEST SWITCH. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A56EU 1996060600627 19960606 00627 EU 1996 6 6 RAIA960436 1 19960426 A 5280 137414B426 GEAR DOOR BAG JETSTM JETSTM3201 1500217 EU RT MAIN LOOSE RIVETS A RAIA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 CE 03 971JX 5934 971 LAX - FLT 4789 - VIBRATION IN CONTROL YOKE ABOVE 200 KNOTS. INSPECTION REVEALED THE RIGHT MAIN GEAR DOOR HAD WORKING RI VETS. RIGHT MAIN GEAR DOOR WAS REPAIRED, AND FLIGHT CHECK PERFORMED REVEALING NORMAL OPERATION. (M) 2 L 7 2 4T RT A56EU 1996060600628 19960606 00628 EU 1996 6 6 RAIA960439 1 19960428 A 5610 1379628C402 WINDSCREEN BAG JETSTM JETSTM3201 1500217 EU RT COCKPIT CRACKED A RAIA B EMER. DESCENT C F.O.D. CR CRUISE 1 CE 03 338TE 8602 932 EVV - FLT 7421 - AIRCRAFT EXPERIENCED HAIL DAMAGE IN FLIGHT. REPLACED RIGHT MAIN WINDSCREEN. (M) 2 L 7 2 4T RT A56EU 1996060600629 19960606 00629 EU 1996 6 6 RAIA960440 1 19960429 A 7712 31024766 TQ SIGNAL COND BAG JETSTM JETSTM3201 1500217 EU RT ENGINE INOP A RAIA A UNSCHED LANDING O OTHER AP APPROACH 1 CE 03 435AM 10715 10715 889 STL - FLT 7464 - RIGHT ENGINE INDICATED 60 PERCENT TORQUE AT FLIGHT IDLE DURING APPROACH. MX SWAPPED TO BRIDGE 2 ON THE TORQUE SIGNAL CONDITIONER. PERFORMED GROUND RUNS. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A56EU 1996060600630 19960606 00630 EU 1996 6 6 RAIA960502 1 19960501 A 3350 7012210 LAMP AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 421TE 102 EMERGENCY ESCAPE LIGHT AT SEAT 10A INOP. REPLACED LAMP. (M) 2 H 7 2 4T RT A53EU 1996060600631 19960606 00631 WP 1996 6 6 RAIA960503 2 19960503 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP NR 2 LOW PWR A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CE 03 343TE 955 66201 EVV - FLT 7427 - LOW POWER NR 2 ENGINE. REPLACED ENGINE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996060600632 19960606 00632 EU 1996 6 6 RAIA960504 1 19960503 A 7722 8974694 EGT HARNESS BAG JETSTM JETSTM3201 1500217 EU NR 1 ENG INOPERATIVE A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 424AM 8322 865 STL - FLT 7532 - NR 1 ENGINE EGT FLUCTUATION. REPLACED EGT HARNESS. (M) 2 L 7 2 4T RT A56EU 1996060600633 19960606 00633 EU 1996 6 6 RAIA960505 1 19960503 A 7620 8975481 PROP GOV BAG JETSTM JETSTM3201 1500217 EU NR 1 ENG OUT OF ADJUST A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 430AM 3490 880 STL - FLT 7418 - NR 1 ENGINE LOW TORQUE. ADJUSTED PROP GOV HIGH STOP SCREW. (M) 2 L 7 2 4T RT A56EU 1996060600634 19960606 00634 EU 1996 6 6 RAIA960506 1 19960503 A 2931 HYD PRESS LIGHT AEROSP ATR42 ATR42300 8680920 EU COCKPIT BROKEN WIRE A RAIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 03 424TE 11569 124 STL - FLT 7116 - BLUE HYDRAULIC PRESSURE LIGHT ILLUMINATED. REPAIRED WIRE, P/N BF2419, AND INDICATOR LIGHT. (M) 2 H 7 2 4T RT A53EU 1996060600635 19960606 00635 NE 1996 6 6 SIMA961142 3 19960423 A 6110 PROP AEROSP ATR42 ATR42300 8680920 EU HAMSTD 14SF 14SF5 NE LT ENGINE OVERTORQUED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 213AT 7854 12220 211 ORD - FLT 4011 - TEN DAYS AFTER OCCURENCE, IN MQT, FDAU READ OUT OVERTORQUE ON BOTH ENGINES. SIMMONS MANAGEMENT GROUNDE D THE AIRCRAFT IN CVG IMMEDIATELY AND DISPATCHED MTX AND INSPECTION TEAM TO INSPECT PROPS AND BOROSCOPE BOTH ENGINES. B OTH ENGINES INSPECTED AS PER PW MANUAL AND THERE WAS NO DANGER EVIDENT. AIRCRAFT WAS FERRIED AS PER HAM STANDARD APPROV AL TO MQT FOR BOTH PROP REPLACEMENT DUE TO RECORDED OVERTORQUE. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 6 C P7NE 1996060600636 19960606 00636 EU 1996 6 6 SIMA961241 1 19960503 A 2720 7227200641 RUDDER CONSOLE SAAB SF340 340B 7860101 EU LT/RT CORROSION A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 586MA 15237 340B165 LAW - DURING MAINTENANCE, 'EM-5' CHECK, FOUND THE LEFT/RT RUDDER CONSOLES CORRODED AT THE CASING FLOOR ATTACH POINTS. T HE LT/RT CONSOLES P/N 7227200-641 WERE REPLACED IAW SAAB AMM 27-21-05. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1996060600637 19960606 00637 EU 1996 6 6 SIMA961271 1 19960506 A 3350 3011151 BATTERY AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 424MQ 045 ORD - FLT 4372 - UPPER EMERGENCY EXIT LIGHTS LEFT AND RIGHT SIDES DO NOT WORK WHEN TURNED ON FROM FLIGHT ATTENDANT STATI ON. RAI BATTERY PACK IAW ATR 24-30-10. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996060600638 19960606 00638 GL 1996 6 6 SRAA49605 2 19960425 A 7532 6809125 BLEED VALVE LKHEED 382 382E 526413U SO ALLSN 501D 501D22A 03006 GL NR 2 ENGINE DIRTY A SRAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 23 522SJ 4362 550153 FLIGHT 3904 - REPORTED NR 2 ENGINE FLAME OUT EN ROUTE MOMBASA, SECURED ENGINE PER AOM, PROCEEDED TO DESTINATION AND LAND ED WITHOUT INCIDENT. MX CLEANED DIRTY 5TH STAGE BLEED VALVES, REINSTALLED, ACCOMPLISHED ENGINE PERFORMANCE RUNS AND RET URNED TO SERVICE. (M) 2 H 7 4 4T 4 T A1SO E282 1996060600639 19960606 00639 SO 1996 6 6 SRAA59601 1 19960505 A 2170 COALESCER LKHEED 382 382E 526413U SO AIR COND SYST DIRTY A SRAA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 23 923SJ 4301 ON DESCENT INTO MHZ CARGO AND FLIGHT DECK FILLED UP WITH SMOKE COMING FROM CARGO COMPARTMENT AIR CONDITIONER, ACCOMPLISH ED LANDING WITHOUT INCIDENT. FOUND WATER SEPARATOR SOCK SOAKED WITH OIL FROM BAD EXTERNAL AIR START CART. REMOVED EXCE SS OIL AND REPLACED WATER SEPARATOR SOCK, SYSTEM OPS CHECKED GOOD. (M) 2 H 7 4 4T A1SO 1996060600640 19960606 00640 NM 1996 6 6 TAOA049615 1 19960426 A 2612 65602097 DET CONTL UNIT BOEING 727 727254 138408L NM NR 1 ENGINE MALFUNCTIONED A TAOA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 EA 15 916TS R00056S 20437 FLT NR 6431 - LGA-DCA - ENGINE FIRE WARNING NR 1 CAME ON. PULLED ENGINE DETECTOR 'B' LOOP CIRCUIT BREAKER TO EXTINGUISH LIGHT. ENGINE SHUT DOWN. REPLACED NR 1 ENGINE FIRE WALL LOOP. REPLACE, FIRE DETECTOR CONTROL UNIT. FUNCTIONAL CHECK OF NR 1 ENGINE FIRE WARNING SYSTEM OK, PER MM 26-11-01. (M) 2 L 7 3 4F A3WE 1996060600641 19960606 00641 NE 1996 6 6 TWRA9625 2 19960430 A 7200 ENGINE BOEING 747 747130 1384880 NM PWA JT9 JT9D7A 52054 NE NR 3 FAILED A TWRA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 15 603FF 19746 662616 ENGINE NR 3 IN CRUISE SHUTDOWN FOR LOSS OF OIL, TEMPERATURE RISING AND OIL PRESSURE FLUCTUATING. ENGINE WAS REMOVED AND REPLACED S/N OFF 662616, S/N ON 662867. DUE TO METAL ON MGB CHIP DETECTOR AND SLUDGE/TAR FOUND IN FILTER. (M) 2 L 7 4 4F 4 F A20WE E20EA 1996060600642 19960606 00642 NE 1996 6 6 TWRA9626 2 19960510 A 7250 TURBINE BOEING 747 747121 1384871 NM PWA JT9 JT9D7AH 52054 NE NR 3 ENGINE FAILED A TWRA A E UNSCHED LANDING ENGINE SHUTDOWN X ENGINE FLAMEOUT CL CLIMB 1 EA 15 604FF 19659 685769 AT 13,000 FEET AFTER TAKEOFF LOUD BOOM WAS HEARD AND CONFIRMED ENGINE ON NR 3 ENGINE. AFTER RETURN TO JED INITIAL INSPE CTION FOUND METAL IN TAILPIPE. BORESCOPE INSPECTION FOUND SECOND STAGE TURBINE FAILURE. ENGINE TO BE REPLACED. (M) 2 L 7 4 4F 4 F A20WE E20EA 1996060600643 19960606 00643 NM 1996 6 6 TWRA9627 1 19960509 A 2530 2510003209 OVEN BOEING 747 747124 1384874 NM UPPER DECK FAILED A TWRA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 602FF 19734 DURING CRUISE, CABIN ATTENDANT REPORTED ELECTRICAL SMOKE COMING FROM UPPER DECK OVEN 704 CONTROLLER. PULLED CIRCUIT BRE AKER AND REMOVED OVEN. ITEM WAS DEFERRED TO PAD 3822002, MEL 25-21. OVEN REPLACED. (M) 2 L 7 4 4F A20WE 1996060600644 19960606 00644 NE 1996 6 6 TWRA9628 2 19960513 A 7200 ENGINE BOEING 747 747121 1384871 NM PWA JT9 JT9D7A 52054 NE NR 1 ENG FAILED A TWRA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 EA 15 604FF 19659 662417 DURING CRUISE, NR 1 ENGINE HAD A STEADY STATE STALL AT FLT LEVEL 350 FEET, THRUST WAS REDUCED AND STABILIZED, THEN PUSHE D THROTTLE TO 1.36 EPR WHEN ENGINE STALLED AGAIN. ENGINE POWER WAS MAINTAINED AT IDLE FOR REMAINDER OF FLT. AIRCRAFT D IVERTED TO MANCHESTER. DURING TROUBLESHOOTING, METAL WAS FOUND IN TAILPIPE. ENGINE SCHEDULED TO BE CHANGED. (M) 2 L 7 4 4F 4 F A20WE E20EA 1996060600645 19960606 00645 NM 1996 6 6 UIEA9605 1 19960425 A 5400 13J55200 BOEING 747 747245F 1384897 NM S-DUCT A UIEA A E J UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL J WARNING INDICATION CL CLIMB 1 EA 15 640FE 20826 ATB FLT NR GTI127/ORD/TRN, AFTER TAKEOFF NR 1 ENGINE HAD A FIRE WARNING FOLLOWING INDICATIONS WERE OBSERVED, FIRE WARNIN G LIGHT AND HIGH NACELLE TRMP (ABCLAMPOVE 9.0) ALSO GOT START VALVE OPEN LIGHT. AFTER ENGINE SHUTDOWN GOT OIL FILTER BY PASS LIGHT. DUMPED 90,000 KG FUEL. RETURNED TO ORD, LANDING UNEVENTFUL. FOUND 'S' DUCT CLAMP FAILED CAUSING DAMAGE TO WIRING, FAN COWL AND SEVERAL COMPONENTS. REPLACED DEFECTIVE CLAMP, 'S' DUCT, REVERSER PDU AND REPAIRED WIRING TO REVER SER, START VALVE. ALSO, REPLACED OIL FILTER BYPASS SWITCH AND RIGHT FAN COWL. PERFORMED ENGINE RUNUP. ALL SYSTEMS OPE RATE. (M) 2 L 7 4 4F A20WE 1996060600646 19960606 00646 NM 1996 6 6 USAA960391 1 19960412 A 5347 SEAT TRACK BOEING 737 737201 1384454 NM BS 344-349 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 260AU 34273 22866 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 5 INCH CORROSION SEAT TRACK BS 344 TO BS 349 LBL 22. CUT SEAT TRACK AND SPLICED IN NEW, REPAIRED PER SRM 53-10-5. (M) 2 L 7 2 4F A16WE 1996060600647 19960606 00647 NM 1996 6 6 USAA960392 1 19960412 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 1006-996 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 260AU 34273 22866 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 10 INCH BY 3 INCH CORROSION BS 1006 TO BS 996 STRINGER 26L. INSTALLED R EPLACEMENT STRINGER SECTION, REPAIRED PER SRM 53-10-3. (M) 2 L 7 2 4F A16WE 1996060600648 19960606 00648 NM 1996 6 6 USAA960393 1 19960412 A 5312 BULKHEAD FTG BOEING 737 737201 1384454 NM BS 1156 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 260AU 34273 22866 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK BS 1156 OUTBOARD OF LEFT OUTBOARD PIVOT FITTING BULKHEAD. INSTALLED DOUBLER, REPAIRED PER EO 5391G569. (M) 2 L 7 2 4F A16WE 1996060600649 19960606 00649 WP 1996 6 6 USAA960419 1 19960513 A 5311 S27779306 BELT FRAME DOUG DC9 DC981 3022081 WP BS 1309 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 801US 38909 48037 PIT - DURING Q-5/C5 CHECK INSPECTION, FOUND 2 INCH BY 3 INCH LEVEL 1 CORRODED AREA PREVIOUSLY REWORKED IN BELTFRAME STAT ION 1309 LONGERON 30. CORROSION TASK NR C57-53300. ACCOMPLISHED SPLICE REPAIR PER SRM 53-03 FIG 2. (M) 2 L 7 2 4F A6WE 1996060600650 19960606 00650 WP 1996 6 6 USAA960420 1 19960513 A 5313 2912727 LONGERON DOUG DC9 DC981 3022081 WP BS 446/465 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 801US 38909 48037 PIT - DURING Q-5/C5 CHECK INSPECTION, FOUND 1 INCH BY 4 INCHES OF CORRODED AREA BETWEEN STATION 446 AND 465 LONGERON 26L . LEVEL 2 CORROSION REF TASK NR C-51-53300. REMOVED CORRODED SECTION AND SPLICED IN NEW LONGERON SECTION PER SRM 53-02 FIG 5. (M) 2 L 7 2 4F A6WE 1996060600651 19960606 00651 WP 1996 6 6 USAA960421 1 19960513 A 5330 59364343 SKIN DOUG DC9 DC981 3022081 WP BS 446/465 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 801US 38909 48037 PIT - DURING Q-5/C5 CHECK INSPECTION, FOUND LEVEL 2 CORROSION AREA 4 INCHES BY 4 INCHES AT STATIC PORT HEATING PAD SKIN BETWEEN STATION 446 AND 465 BETWEEN LONGERON 26L AND 27L. CORROSION TASK REF C51-53300. REMOVED DAMAGED AREA AND SPLIC ED IN NEW SKIN SECTION PER USAIR EA NR 32634. (M) 2 L 7 2 4F A6WE 1996060600652 19960606 00652 WP 1996 6 6 USAA960422 1 19960513 A 5313 2777922 LONGERON DOUG DC9 DC981 3022081 WP BS 275/294 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 801US 38909 48037 PIT - DURING Q-5/C5 CHECK INSPECTION, TWO 1 INCH CRACK AT LOWER FLANGE OF LONGERON 17L, STATION 275 AND 294. ACCOMPLISH ED SPLICE REPAIR PER TYPICAL REPAIR 53-10-17. (M) 2 L 7 2 4F A6WE 1996060600653 19960606 00653 WP 1996 6 6 USAA960423 1 19960513 A 5313 2777922 LONGERON DOUG DC9 DC981 3022081 WP BS 408 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 801US 38909 48037 PIT - DURING Q-5/C5 CHECK INSPECTION, FOUND 1 INCH CRACK AT LOWER FLANGE OF LONGERON 17L STATION 408. ACCOMPLISHED SPLI CE REPAIR PER USAIR TYPICAL REPAIR 53-10-17. (M) 2 L 7 2 4F A6WE 1996060600654 19960606 00654 WP 1996 6 6 USAA960424 1 19960513 A 5320 CLIPS DOUG DC9 DC981 3022081 WP BS 1463 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 801US 38909 48037 PIT - DURING Q-5/C5 CHECK INSPECTION, FOUND 3 CLIPS CRACKED RANGING FROM 1.75 INCH TO 2.25 INCH LONG CANTED FRAME STATIO N 1463 LONGERON 7, 9 AND 10. REPAIRED IAW SRM 53-14-4 FIG 3 SHEET NR 7 AND DACO DWG 9911839 AND 9911877. (M) 2 L 7 2 4F A6WE 1996060600655 19960606 00655 WP 1996 6 6 USAA960425 1 19960513 A 5313 27779221 LONGERON DOUG DC9 DC981 3022081 WP BS 228/237 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 801US 38909 48037 PIT - DURING Q-5/C5 CHECK INSPECTION, FOUND TWO 1 INCH CRACKS IN LONGERON 17R LOWER FLANGE STATION 228 AND 237. REMOVED DAMAGED SECTION AND SPLICED IN NEW SECTION PER SRM 53-02 FIG 2 PG 2A. (M) 2 L 7 2 4F A6WE 1996060600656 19960606 00656 WP 1996 6 6 USAA960426 1 19960513 A 5313 27779221 LONGERON DOUG DC9 DC981 3022081 WP BS 256-408 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 801US 38909 48037 PIT - DURING Q-5/C5 CHECK INSPECTION, FOUND 1 INCH CRACK IN LOWER FLANGE IN LONGERON 17R, 4 PLACES AT STATION 256, 408, 370 AND 389. REMOVED DAMAGED SECTION OF LONGERON AND ACCOMPLISHED SPLICE REPAIR PER SRM 53-02 PAGE 2A. (M) 2 L 7 2 4F A6WE 1996060600657 19960606 00657 NM 1996 6 6 USAA960427 1 19960508 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 225US 46572 21667 ROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK FUSELAGE SKIN AT BS 727 A BETWEEN STRINGER 15 AND 16 LEF T. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 PAGE 01. (M) 2 L 7 2 4F A16WE 1996060600658 19960606 00658 WP 1996 6 6 USAA960428 1 19960509 A 5330 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 950VJ 59672 47564 PIT - DURING C-1 CHECK INSPECTION, FOUND .25 INCH CRACK IN MAIN ENTRANCE DOOR TOP AFT DOOR STOP SKIN BOTH LAYERS. INSTA LLED DOUBLER REPAIR PER SRM 53-05 FIG 26A. (M) 2 L 7 2 4F A6WE 1996060600659 19960606 00659 WP 1996 6 6 USAA960429 1 19960509 A 5313 LONGERON DOUG DC9 DC931 3022065 WP STA 756 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 950VJ 59672 47564 PIT - DURING C-1 CHECK INSPECTION, FOUND .5 INCH LONG CRACK IN LONGERON 3L AT STATION 756. INSTALLED SPLICE REPAIR PER SRM 53-02 FIG 2. (M) 2 L 7 2 4F A6WE 1996060600660 19960606 00660 WP 1996 6 6 USAA960430 1 19960510 A 5313 5910130391N STRINGER DOUG DC9 DC931 3022065 WP BS 996 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 972VJ 74491 47052 PIT - DURING C-6 CHECK INSPECTION, FOUND A 1.5 INCH CRACK IN T-CAP AT STATION 996 LONGERON 14L (APBH). SPLICED IN NEW S ECTION OF T-CAP PER SRM 53-03 FIG 37A. (M) 2 L 7 2 4F A6WE 1996060600661 19960606 00661 WP 1996 6 6 USAA960431 1 19960511 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 266/313 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 972VJ 74491 47052 PIT - DURING C-6 AND ACCOMPLISHMENT OF EO 3495X040, FOUND 3 SMALL AREAS OF CORROSION 20 PERCENT OF SKIN THICKNESS IN DEP TH UNDER NR 1 ADF ANTENNA STATION 266 AND ADF ANTENNA STATION 313 LONGERON NR 1. REMOVED AND REPLACED CORRODED SKIN ARE A PER USAIR EA 32324. (M) 2 L 7 2 4F A6WE 1996060600662 19960606 00662 NE 1996 6 6 USAAD96046 2 19960501 A 7313 37820012 FUEL PUMP DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7B 52053 NE RT ENGINE FAILED A USAA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 EA 19 986VJ 28142 7454 47209 657616 FLT 1121 - BOS-DCA - RIGHT ENGINE FAILED AFTER TAKEOFF. NO INDICATION PRIOR TO FAILURE, NO FIRE WARNING. SINGLE ENGINE TIME 5 MINUTES. REPLACED RIGHT ENGINE FUEL PUMP AND FUEL CONTROL UNIT. (M) 2 L 7 2 4F 4 F A6WE E2EA 1996060600663 19960606 00663 WP 1996 6 6 USAAD96048 1 19960502 A 3320 3101364501 TRANSFORMER DOUG DC9 DC931 3022065 WP AFT LAV OVERHEATED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 914VJ 47068 FLT 311 - ATL-PHL - DIVERTED TO BWI DUE TO SMOKE IN AFT LEFT LAV AREA. REPLACED AFT MISC LIGHT CONTROL TRANSFORMER. (M ) 2 L 7 2 4F A6WE 1996060600664 19960606 00664 NE 1996 6 6 USAAD96049 2 19960503 A 7321 7696067 FUEL CONTL UNIT DOUG DC9 DC981 3022081 WP PWA JT8 JT8D217 52053 NE LT ENGINE FAILED A USAA A E UNSCHED LANDING ENGINE SHUTDOWN O OTHER CR CRUISE 1 EA 19 808US 10351 30 48040 696391 BOS - FL 478 - AT TOP OF CLIMB, FL 230, LEFT ENGINE WOULD NOT RESPOND TO THROTTLE MOVEMENT. OIL TEMPERATURE OF LEFT ENG INE WAS THIRTY TO THIRTY-FIVE DEGREES HIGHER THAN THE RIGHT ENGINE TEMPERATURE. FLIGHT RETURNED TO BOS AND SHUT DOWN EN GINE ON FINAL APPROACH. SET: 4 MINUTES. MAINTENANCE REPLACED THE LEFT ENGINE FUEL CONTROL UNIT. (M) 2 L 7 2 4F 4 F A6WE E9NE 1996060600665 19960606 00665 WP 1996 6 6 USAAD96050 1 19960508 A 3350 14597101 BATTERY PACK DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 802US 48036 FLT 7003 - ROC - CEILING MOUNTED EMERGENCY LIGHTS BETWEEN ROWS 5 AND 7 INOP. FOUND DURING OVERNIGHT CHECK. REPLACED BA TTERIES IN POWER PACK. OPERATIONAL CHECK OK. (M) 2 L 7 2 4F A6WE 1996060600666 19960606 00666 WP 1996 6 6 USAAD96051 1 19960510 A 3350 41B030CF00101 PACK BATTERY DOUG DC9 DC931 3022065 WP RT NACELLE DISCHARGED A USAA O OTHER O OTHER IN INSP/MAINT 1 EA 19 971VJ 47051 FLT 1168 - SYR - RIGHT NACELLE EMERGENCY LIGHT INOP. MAINTENANCE REPLACED THE BATTERY PACK FOR RIGHT NACELLE EMERGENCY LIGHT. OPS CHECK SAT. (M) 2 L 7 2 4F A6WE 1996060600667 19960606 00667 WP 1996 6 6 USAAD96052 1 19960509 A 3260 PIN DOUG DC9 DC931 3022065 WP LT MLG DISENGAGED A USAA O OTHER O OTHER AP APPROACH 1 EA 19 969VJ 47421 FLT 517 - YYZ-PHL - LEFT MAIN GEAR DID NOT INDICATE SAFE WITH GEAR DOWN. LEFT MAIN GEAR UNSAFE LIGHT DID NOT ILLUMINATE . FOUND PIN NR 5 AT LEFT MAIN GEAR DOWNLOCK SWITCH PUSHED BACK. REINSTALLED PIN, OPS CHECKS GOOD. TWO TOWER FLY-BY'S WERE CONDUCTED TO VISUALLY ASCERTAIN GEAR POSITION. (M) 2 L 7 2 4F A6WE 1996060600668 19960606 00668 1996 6 6 USAAD96054 4 19960512 A 3454 2587567 RMI DOUG DC9 DC931 3022065 WP RT COCKPIT FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 927VJ 30288 48154 PIT - FL 1036 - UPON REACHING FL 180 OUT OF PIT, CREW NOTED BOTH RIM'S SPINNING AND COULD NOT FIX THE AIRCRAFT POSITION. FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT RMI. (M) 2 L 7 2 4F A6WE 1996060600669 19960606 00669 EU 1996 6 6 USAAF96040 1 19960508 A 2913 40052 ENG DRIVEN PUMP FOKKER F28 F28MK4000 4990810 EU NR 1 ENG FAILED A USAA O OTHER J WARNING INDICATION DE DESCENT 1 EA 19 480AU 8110 11229 CLT - FL 498 - ON DESCENT INTO CLT, CREW LOST UTILITY HYDRAULIC SYSTEM. CAPTAIN EXTENDED THE LANDING GEAR AND FLAPS USI NG ALTERNATE PROCEDURE. NO EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY. MAINTENANCE REPLACED NR 1 ENGINE DRI VEN PUMP AND PRESSURE FILTER. THE HYDRAULIC SYSTEM WAS SERVICED, THE ENGINE WAS RUN AND LEAK TESTED AND ALL FLIGHT CONT ROLS WERE OPS CHECKED AS NORMAL. (M) 2 L 7 2 4F RT A20EU 1996060600670 19960606 00670 EU 1996 6 6 USAAF96041 1 19960512 A 3260 DOOR SENSOR FOKKER F28 F28MK0100 4990807 EU LT MLG OUT OF ADJUST A USAA O OTHER N FALSE WARNING DE DESCENT 1 EA 19 899US 11399 DCA - FL 2286 - ON DESCENT INTO DCA, LEFT LANDING GEAR DOOR SWITCH CAME ON MFDU AFTER THE GEAR WAS LOWERED. CREW HAD TH REE GREEN LIGHTS FOR GEAR BUT AS THEY DESCENED BELOW 900 FEET, THE LANDING GEAR AURAL WARNING CAME ON. CREW RECYCLED GE AR AND LIGHT WENT OUT. FLIGHT LANDED IN DCA WITHOUT FURTHER INCIDENT. MX ADJUSTED THE LEFT NR 2 LANDING GEAR DOOR SENS OR PER THE MM. LANDING GEAR FUNCTIONAL CHECK WAS GOOD. (M) 2 L 7 2 4F RT 1996060600671 19960606 00671 EU 1996 6 6 USAAF96043 1 19960513 A 2750 A83235409 FLAP SYNCHRO FOKKER F28 F28MK0100 4990807 EU LT TE FLAPS FAILED A USAA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 EA 19 886US 11346 PIT - FL 8075 - DURING DESCENT INTO AVP, THE CREW COULD NOT GET THE FLAPS TO EXTEND. A DECISION WAS MADE TO DIVERT TO P IT WHERE MAINTENANCE IS AVAILABLE TO MAKE REPAIRS. THE CAPTAIN DECLARED AN EMERGENCY FOR PRECAUTIONARY MEASURES. THE F LIGHT LANDED WITHOUT INCIDENT. MX REPLACED THE LEFT INBOARD FLAP SYNCHRO. OPERATIONAL CHECK OK. (M) 2 L 7 2 4F RT 1996060600672 19960606 00672 EU 1996 6 6 USAAF96044 1 19960514 A 3260 SWITCH FOKKER F28 F28MK4000 4990810 EU LT MLG DOOR LOOSE A USAA O OTHER N FALSE WARNING CL CLIMB 1 EA 19 484US 11234 TOA - FL 1250 - AFTER TAKEOFF FROM PIT, THE LEFT GEAR RED LIGHT REMAINED ON AFTER GEAR RETRACTION. CREW CYCLED GEAR AND ALL LIGHTS WENT OUT. MAINTENANCE FOUND THE FORWARD LEFT GEAR DOOR SWITCH LOOSE. SWITCH WAS SECURED AND OPS CHECKED (G EAR SWING). CHECKED GOOD. (M) 2 L 7 2 4F RT A20EU 1996060600673 19960606 00673 EU 1996 6 6 USAAF96045 1 19960514 A 3350 6008905 POWER SUPPLY FOKKER F28 F28MK4000 4990810 EU WING FAIRING FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 488US 11240 CLT - MX FOUND THE FORWARD WING TO BODY FAIRING EMERGENCY LIGHTING SYSTEM INOP. MX REPLACED THE FORWARD WING TO BODY FA IRING POWER SUPPLY AND BATTERIES. OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A20EU 1996060600674 19960606 00674 NM 1996 6 6 USAASB96032 1 19960220 A 3350 1000679 LIGHT BOEING 737 737201 1384454 NM CABIN INOPERATIVE A USAA K NONE L NO TEST NR NOT REPORTED 1 EA 19 239US 22354 FLT 2674 - LGA - EMERGENCY EXIT LIGHT AT FORWARD SERVICE DOOR INOP. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERY PACK O VER FORWARD GALLEY SERVICE DOOR. EMERGENCY LIGHTS OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1996060600675 19960606 00675 NM 1996 6 6 USAASB96081 1 19960510 A 3230 RETRACT MECH BOEING 737 737301 1384611 NM LANDING GEAR MALFUNCTIONED A USAA A UNSCHED LANDING O OTHER AP APPROACH 1 EA 19 588US 23933 FLT 1862 - BWI - DURING APPROACH TO DCA, GEAR WAS LOWERED BUT WE HAD NO INDICATION OF SAFE INDICATIONS. DIVERTED TO BWI . EMERGENCY DECLARED. MAINTENANCE CYCLED THE GEAR SEVERAL TIMES, COULD NOT DUPLICATE FAULT. REPLACED THE FOLLOWING IT EMS AS A PRECAUTIONARY MEASURE, L/G AIR GROUND RELAY, LIGHTS C/B, MASTER DIM BUS C/B. GEAR SWING NORMAL. (M) 2 L 7 2 4F RT A16WE 1996060600676 19960606 00676 1996 6 6 USAASB96082 4 19960510 A 3441 HG1050AD05 IRU BOEING 737 737301 1384611 NM E/E COMPT FAILED A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 590US 21606 23935 FLT 84 - SAN - NR 1 IRU FAULT LIGHT ILLUMINATED IN FLIGHT. IN ATT ADI WOULD NOT RECOVER AND HEADING SELECT WAS UNSUCCES SFUL, HEADING SLEWED TO MANUAL SETTING BUT IMMEDIATELY STARTED TO DRIFT. RETURNED TO SAN. MX REPLACED NR 1 IRU. BITE CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 1996060600677 19960606 00677 1996 6 6 USAASB96085 4 19960512 A 3417 HG480B42 ADC BOEING 737 7373B7 1384580 NM E/E COMPT FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 371US 22950 FLT 357 - MCO - ON ROTATION LOST AUTO-THROTTLE AND FLIGHT OFFICERS AIRSPEED WENT TO ZERO. ALSO, FLIGHT OFFICERS ALTITUD E STOPPED AT 1500 FEET, WE WERE CLIMBING TO 10'000. MX REPLACED NR 2 ADC GROUND TEST OK. SYSTEM NOT CERTIFIED FOR CAT IIIA. (M) 2 L 7 2 4F RT A16WE 1996060600678 19960606 00678 NM 1996 6 6 USAASB96086 1 19960514 A 2530 6042H145 RELAY BOEING 737 737301 1384611 NM BEHIND P6 PANEL FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 335US 23232 FLT 1886 - ORF - AT 19,000, THERE WAS AN ACRID, ELECTRICAL ODOR, WITH VERY LIGHT SMOKE, LASTED 3 MINUTES. DIVERTED TO O RF. MX FOUND R-61 RELAY AT L1 TERMINAL BURNED FOR NR 1 GALLEY. REPLACED R-61 RELAY AND L1 TERMINAL END. OPS CHECKS NO RMAL. (M) 2 L 7 2 4F RT A16WE 1996060600679 19960606 00679 NM 1996 6 6 USAASB96087 1 19960509 A 3350 1000679 LIGHT EMERGENCY BOEING 737 737201 1384454 NM COCKPIT FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 237US 22353 FLT 916 - PHL - COCKPIT EMERGENCY LIGHT INOP. MX REPLACED COCKPIT EMERGENCY LIGHT ASSY. OPS CHECK SATISFACTORY. (M) 2 L 7 2 4F A16WE 1996060600680 19960606 00680 EU 1996 6 6 VTZA96187 1 19960510 A 2910 1379305A97 HYD LINE BAG JETSTM JETSTM3201 1500217 EU LT MAIN GEAR LOOSE A VTZA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 27 487UE 906 FLT 6380 - IAD-LGA - DURING CRUISE, DECLARED AN EMERGENCY DUE TO COMPLETE HYDRAULIC PRESSURE LOSS. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MX DISCOVERED THE HYDRAULIC LINE ON THE UP SIDE OF THE LEFT MAIN RETRACTION ACTUATOR WA S LOOSE. MAINTENANCE TIGHTENED LINE AND LEAK CHECKED SYSTEM. COMPLIED WITH INSPECTION FOR HYDRAULIC FLUID LOSS PER J31 MM CHAPTER 05-50. NO OTHER DEFECTS NOTED. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996060600681 19960606 00681 EU 1996 6 6 VTZA96188 1 19960510 A 2435 23079009 STARTER/GEN BAG JETSTM JETSTM3201 1500217 EU LT NACELLE FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 479UE 893 FLT NR 6597 - CRW-IAD - ABORTED THE TAKEOFF DUE TO THE LEFT STARTER/GEN FAILED ON THE TAKEOFF ROLL. AIRCRAFT RETURNED T O GATE WITH NO FURTHER INCIDENTS. MX REPLACED LEFT STARTER/GEN. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVI CE. (M) 2 L 7 2 4T RT A56EU 1996060600682 19960606 00682 EU 1996 6 6 VTZA96189 1 19960511 A 3260 BULB JETAIR JETSTM JETSTM4101 1500501 EU RT MLG IND FAILED A VTZA O OTHER P NO WARNING INDICATION CR CRUISE 1 EA 27 308UE 41023 FLT NR 6523 - JFK-ROC - DURING CRUISE, DECLARED AN EMERGENCY DUE TO THE LEFT MAIN GREEN INDICATION BURNED OUT. AIRCRAFT LANDED AT ROC WITH NO FURTHER INCIDENTS. MX RELAMPED THE STANDBY INDICATION AND OPENED DMI NR 18657 IAW MEL 32-5 ON TH E MAIN GEAR INDICATION. MX LATER CLEARED DMI NR 18657 ON 5-12-96 BY RELAMPING THE MAIN GEAR INDICATION. AIRCRAFT WAS R ELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996060600683 19960606 00683 WP 1996 6 6 VTZA96190 2 19960513 A 7320 8691691 INLET SENSOR BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT ENG OUT OF POSITION A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 474UE 849 P66059 FLT NR 6424 - IAD-BUF - ABORTED TAKEOFF DUE TO THE LEFT ENGINE POWER DROPPING OFF 40 PERCENT DURING THE TAKEOFF ROLL. A IRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPOSITIONED T2 SENSOR. AIRCRAFT WAS RELEASED APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996060600684 19960606 00684 NM 1996 6 6 WRLA96022 1 19960511 A 3244 TIRE DOUG MD11 MD11 3023602 NM MLG LOW PRESSURE A WRLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 273WA 48519 DURING TAXI, FLIGHT CREW NOTED NR 6 MAIN WHEEL ASSY LOW PRESSURE ALERT. FLIGHT CREW ELECTED TO RETURN TO GATE FOR MAINT ENANCE. AIRCRAFT RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE PERSONNEL NOTED NR 6 MAIN WHEEL ASSY WAS 180 PSI. MAI NTENANCE PERSONNEL REMOVED AND REPLACED THE NR 6 MAIN WHEEL ASSY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A22WE 1996060600685 19960606 00685 GL 1996 6 6 HEEA967098 2 19960506 A 7230 23057142 CASE HALVES 6890550 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL 1ST STAGE EXCESS RUB E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8197X CAC41725 S808 CAE831133 ENGINE REMOVED DUE TO N1 LOCKUP. UPON INSPECTION OF COMPRESSOR PARTS NOTED THE FOLLOWING: PLASTIC LIFTING AND EXCESSIV E RUB IN CASE HALVES FIRST STAGE AREA. REPLACED CASE HALVES. 1 G 7 2 3U 3 U H3EU E4CE 1996060600686 19960606 00686 SW 1996 6 6 HEEA967099 1 19960506 A 5210 214070541103 TRACK BELL 214 214ST 1182106 SW DOOR CRACKED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3897N 28106 WHEN EXTRUSION P/N 40-275-6 IS INSTALLED IN TRACK P/N 214-070-541-103 THE TRACK CRACKS 2 G 7 2 4U H10SW 1996060600687 19960606 00687 SW 1996 6 6 HEEA967100 1 19960506 A 6220 412010179105 CONE 412010100193 BELL 412 412 1182202 SW M/R SCORED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893P 3272 A512 33012 LOWER CONE TEFLON COATING SCORED. 1 G 7 2 4U H4SW 1996060600688 19960606 00688 SW 1996 6 6 HEEA967101 1 19960506 A 6220 412010124109 BOLT 412010100193 BELL 412 412 1182202 SW M/R COAT FLAKE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893P 1330 A512 33012 TUNGSTEN COATING FLAKING OFF. SENT TO BELL HELICOPTER TEXTRON FOR INSPECTION AND REPAIR. 1 G 7 2 4U H4SW 1996060600689 19960606 00689 1996 6 6 HEEA967102 4 19960506 A 3452 071119218 CONTROL BELL 214 214ST 1182106 SW XPONDER DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 8045T 28101 XPONDER IDENT SWITCH STICKING IN IDENT POSITION. 2 G 7 2 4U H10SW 1996060600690 19960606 00690 1996 6 6 HEEA967103 4 19960506 A 3452 071119208 CONTROL BELL 212 212 1181420 SW COCKPIT XPONDER DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5736D 31135 CONTROL UNIT HAS BAD DISPLAY AND NEEDS MOD #2. 1 G 7 1 4U H4SW 1996060600691 19960606 00691 1996 6 6 HEEA967104 4 19960506 A 3452 066107100 TRANSPONDER BELL 214 214ST 1182106 SW COCKPIT INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 8045T 28101 TRANSPONDER INOPERATIVE WILL NOT COME ON LINE. 2 G 7 2 4U H10SW 1996060600692 19960606 00692 1996 6 6 HEEA967105 4 19960506 A 3454 071121525 CONTROL UNIT BELL 412 412 1182202 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 22347 36005 CONTROL UNIT HAS MULTIPLE SQUELCH PROBLEMS. 1 G 7 2 4U H4SW 1996060600693 19960606 00693 NE 1996 6 6 HEEA967106 1 19960506 A 5321 7620402021042 PANEL SKRSKY S76 S76A 8143006 NE FLOOR MIS MFG E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 JOGGLE ON PANEL IS 1/16" TOO SHALLOW AND NO EDGE DISTANCE FOR BOLT HOLES. TIME SINCE REPAIR 0:00. 1 G 7 2 3U H1NE 1996060600694 19960606 00694 1996 6 6 HEEA967107 4 19960506 A 3414 412075009105 INDICATOR BELL 412 412 1182202 SW COCKPIT AIRSPEED FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 22347 36005 AIRSPEED NEEDLE WILLNOT GO TO ZERO. 1 G 7 2 4U H4SW 1996060600695 19960606 00695 1996 6 6 HEEA967108 4 19960506 A 3425 1113025 INDICATOR BELL 412 412 1182202 SW COCKPIT HSI FLAG STICKS E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 7128R 36007 HSI DEVIATION VALID FLAG STICKS IN VIEW. 1 G 7 2 4U H4SW 1996060600696 19960606 00696 1996 6 6 HEEA967109 4 19960506 A 3455 066104701 RECEIVER BELL 412 412 1182202 SW COCKPIT ADF INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 22608 33075 ADF IS INOPERATIVE. 1 G 7 2 4U H4SW 1996060600697 19960606 00697 1996 6 6 HEEA967110 4 19960506 A 2370 9806019001 CVR BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 107X 2598 33113 CVR NO AUDIO OR LIGHT WHEN TESTED. 1 G 7 2 4U H4SW 1996060600698 19960606 00698 EU 1996 6 6 HEEA967111 1 19960506 A 5610 1052002 CHIN BUBBLE BOLKMS 105 BO105S 5626006 EU RT FUSELAGE MIS MFG E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5368F S718 R/H CHIN BUBBLE IS TOO SHORT AND WILL NOT REACH CANOPY DOOR POST. 1 G 7 2 3U H3EU 1996060600699 19960606 00699 NE 1996 6 6 HEEA967112 1 19960506 A 6210 7615009043050 TIP CAP SKRSKY S76 S76A 8143006 NE M/R UNBONDED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546G 760076 INBOARD END OF THE TRAILING EDGE STRIP UNBONDED. THE UPPER INTERNAL DOUBLER IS UNBONDED. 1 G 7 2 3U H1NE 1996060600700 19960606 00700 1996 6 6 HEEA967113 4 19960506 A 3453 066402600 LORAN KLN88 BELL 206 206L1 1182107 SW COCKPIT SCREEN DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 21240 45647 LORAN SCREEN LIGHT IS DIM WITH BRIGHTNESS KNOB AT MAXIMUM. 1 G 7 1 3U H2SW 1996060600701 19960606 00701 1996 6 6 HEEA967114 4 19960506 A 2310 4000106010 CONTROL UNIT C10 BOLKMS 105 BO105S 5626006 EU COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 911EB S812 TRANSCEIVER RECEIVES SCRATCHY ON CHANNEL 5. 1 G 7 2 3U H3EU 1996060600702 19960606 00702 NE 1996 6 6 HEEA967115 1 19960506 A 7930 7645001078101 INDICATOR SKRSKY S76 S76A 8143006 NE ENG OIL DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 706AE 760275 ENG OIL INDICATOR HAS NO BACKLIGHTING. 1 G 7 2 3U H1NE 1996060600703 19960606 00703 SW 1996 6 6 HEEA967116 1 19960507 A 3213 206053203101 CROSSTUBE BELL 206 206L1 1182107 SW GEAR CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 CROSS TUBE CORRODED BEYOND LIMITS IN AREA A-4 .014. SCRAPPED CROSSTUBE. 1 G 7 1 3U H2SW 1996060600704 19960606 00704 SW 1996 6 6 HEEA967117 1 19960507 A 3213 206053203103 CROSSTUBE BELL 206 206L1 1182107 SW MAIN GEAR CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 CROSSTUBE CORRODED BEYOND LIMITS IN AREA B-4 .006. SCRAPPED CROSSTUBE. 1 G 7 1 3U H2SW 1996060600705 19960606 00705 SW 1996 6 6 HEEA967118 1 19960507 A 2436 206075447007 REGULATOR BELL 206 206L3 1182108 SW DC VOLTS MALFUNCTION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 4282Z 51499 WHEN VHF IS KEYED, AIRCRAFT VOLTAGE DROPS BY 4 VOLTS. 1 G 7 1 3U H2SW 1996060600706 19960606 00706 SW 1996 6 6 HEEA967119 1 19960507 A 6510 206040370011 SHAFT ASSY BELL 206 206L3 1182108 SW T/R DRIVE BEARING ROUGH E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 41128 51134 DURING INSPECTION FOUND BEARINGS ROUGH. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 1996060600707 19960606 00707 SW 1996 6 6 HEEA967120 1 19960507 A 6330 206033552001 STOP ASSY BELL 206 206L3 1182108 SW XMSN MOUNT UNBONDED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 41128 51134 RUBBER BUMPER ON TOP OF STOP ASSY UNBONDED. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 1996060600708 19960606 00708 SW 1996 6 6 HEEA967121 1 19960507 A 7910 206064515001 SUPPORT ASSY BELL 206 206L3 1182108 SW OIL TANK CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 41128 51134 OIL TANK SUPPORT ASSY CRACKED AND MISSING NUTPLATES. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 1996060600709 19960606 00709 SW 1996 6 6 HEEA967122 1 19960507 A 6330 206033554101 LINK ASSY BELL 206 206L3 1182108 SW XMSN MOUNT BEARING SEPARATE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 41128 51134 LOWER ELASTOMERIC BEARING SEPARATED BEYOND LIMITS. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 1996060600710 19960606 00710 SW 1996 6 6 HEEA967123 1 19960507 A 5520 206023119007 ELEVATOR BELL 206 206L3 1182108 SW ELEV LE OUTBD CHAFED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 41128 51134 ELEVATOR LEADING EDGE CHAFED BEYOND LIMITS AT OUTBOARD END. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 1996060600711 19960606 00711 SW 1996 6 6 HEEA967124 1 19960507 A 5320 206031314045 ANGLE BELL 206 206L3 1182108 SW TAILBOOM MIS LOCATED E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 41128 51134 ANGLE MISLOCATED. SEVERE GAP BETWEEN ANGLE AND TAILBOOM FITTING. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 1996060600712 19960606 00712 SW 1996 6 6 HEEA967125 1 19960507 A 5320 206031314046 ANGLE BELL 206 206L3 1182108 SW TAILBOOM MIS LOCATED E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 41128 51134 ANGLE MISLOCATED. SEVERE GAP BETWEEN ANGLE AND TAILBOOM FITTING. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 1996060600713 19960606 00713 SW 1996 6 6 HEEA967126 1 19960507 A 5320 206031329003 FITTING BELL 206 206L3 1182108 SW TAILBOOM LT MIS LOCATED E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 41128 51134 TAILBOOM FITTING MISLOCATED. FACE OF FITTING NOT PARALLEL WITH TAILBOOM FRAME. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 1996060600714 19960606 00714 SW 1996 6 6 HEEA967127 1 19960507 A 5320 206031329004 FITTING BELL 206 206L3 1182108 SW TAILBOOM RT MISLOCATED E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 41128 51134 TAILBOOM FITTING MISLOCATED. FACE OF FITTING NOT PARALLEL WITH TAILBOOM FRAME. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 1996060600715 19960606 00715 SW 1996 6 6 HEEA967128 1 19960507 A 5311 206032308003 FRAME BELL 206 206L3 1182108 SW TAILBOOM CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 41128 51134 FRAME CRACKED DUE TO MISLOCATED TAILBOOM FITTINGS. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 1996060600716 19960606 00716 SW 1996 6 6 HEEA967129 1 19960507 A 5320 206032308005 ANGLE BELL 206 206L3 1182108 SW TAILBOOM HOLES ELONGATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 41128 51134 RIVET HOLES FOR FITTING IN ANGLE ELONGATED. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 1996060600717 19960606 00717 SW 1996 6 6 HEEA967130 1 19960507 A 5320 206033322003A PANEL ASSY BELL 206 206L3 1182108 SW TAILBOOM MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 41128 51134 RIVET PATTERN ON PANEL DOES NOT ALLOW PROPER EDGE DISTANCE FOR RIVETS ON CHANNEL. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 1996060600718 19960606 00718 1996 6 6 HEEA967131 4 19960507 A 3416 13011001 ALTIMETER 412040002113 BELL 412 412 1182202 SW COCKPIT READS LOW E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2014K ANG00052 33020 NEEDLE INDICATES 140 FEET LOW AT 18,000 FEET. SENT TO B.F. GOODRICH AEROSPACE FOR INSPECTION AND REPAIR. 1 G 7 2 4U H4SW 1996060600719 19960606 00719 SW 1996 6 6 HEEA967141 1 19960508 A 6220 206011149105 YOKE 206011100149 BELL 206 206B3 1181506 SW M/R BEARING FAILURE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2145C 10693 A84 3456 MAIN ROTOR REMOVED FOR 1200 HOUR INSPECTION. (BEARING JOURNALS BREAKING DOWN) REPLACED WITH SERVICEABLE PARTS. 1 G 7 1 3U H2SW 1996060600720 19960606 00720 1996 6 6 HEEA967142 4 19960508 A 3457 0845000000 SKYNAV 5000 BEECH 200 200CBEECH 1152926 CE COCKPIT MALFUNCTION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 39PH BL3 GPS UNIT DOES NOT HOLD ENTERED DATA. 1 L 7 2 4T A24CE 1996060600721 19960606 00721 1996 6 6 HEEA967143 4 19960508 A 3444 071111400 ANTENNA BOLKMS 105 BO105S 5626006 EU RADAR ALT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 90752 S156 RADAR ALTIMETER ANTENNA DEFECTIVE. ERRATIC SIGNAL. 1 G 7 2 3U H3EU 1996060600722 19960606 00722 1996 6 6 HEEA967144 4 19960508 A 3444 071111400 ANTENNA BOLKMS 105 BO105S 5626006 EU RADAR ALT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 131AE S787 RADAR ALT ANTENNA HAS ERRATIC SIGNAL AND IS INTERMITTENT. 1 G 7 2 3U H3EU 1996060600723 19960606 00723 SW 1996 6 6 HEEA967145 1 19960508 A 7714 412075010109 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH NEEDLE SPLIT E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 33008 36004 TRIPLE TACH #1 AND #2 NEEDLE HAVE NEEDLE SPLIT. TIME SINCE REPAIR 6:35. 1 G 7 2 4U H4SW 1996060600725 19960606 00725 1996 6 6 HEEA967147 4 19960508 A 2562 ELT910 ELT NARCO BELL 412 412 1182202 SW COCKPIT MALFUNCTION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 22347 36005 ELT COMES ON INTERMITTENTLY AND DURING ENGINE START. 1 G 7 2 4U H4SW 1996060600726 19960606 00726 SW 1996 6 6 HEEA967148 1 19960508 A 2824 L88010491 VALVE BELL 212 212 1181420 SW FUEL SYS MALFUNCTION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5010F 30936 VALVE INOPERATIVE. CYCLES CONSTANTLY. 1 G 7 1 4U H4SW 1996060600727 19960606 00727 SW 1996 6 6 HEEA967149 1 19960508 A 2435 230321827 STARTER BELL 206 206L1 1182107 SW START/GEN SHORTED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 SHORTED OUT AND GETS VERY HOT. TIME SINCE REPAIR 0:00. 1 G 7 1 3U H2SW 1996060600728 19960606 00728 1996 6 6 HEEA967150 4 19960508 A 2210 117884141 CONTROL UNIT BOLKMS 117 BK117B2 5626013 EU YAW CSAS KICKS E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 132AE 1510 7238 KICKS INTERMITTENTLY.. 1 G 7 2 3U NC H13EU 1996060600729 19960606 00729 SW 1996 6 6 HEEA967151 1 19960508 A 6730 206076062003 CYLINDER BELL 206 206L1 1182107 SW M/R LEAKS E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 16938 4026 45157 LEAKS AT PILOT VALVE AND WEEP HOLE. HIGH PILOT BREAKOUT FORCE. 1 G 7 1 3U H2SW 1996060600730 19960606 00730 SW 1996 6 6 HEEA967152 1 19960508 A 6330 206033554101 LINK ASSY BELL 206 206L1 1182107 SW M/R XMSN BEARING SEPARATE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2249Z 45753 LINK ASSY ELASTOMER BEARINGS SEPARATED. S/N LK0208 &LK7022 1 G 7 1 3U H2SW 1996060600731 19960606 00731 SW 1996 6 6 HEEA967153 1 19960508 A 6330 206033554101 LINK ASSY BELL 206 206L3 1182108 SW XMSN MOUNT DETERIORATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3116L 51529 LINK ASSY DETERIORATED RUBBER. 1 G 7 1 3U H2SW 1996060600732 19960606 00732 SW 1996 6 6 HEEA967154 1 19960508 A 6330 206033554101 LINK ASSY BELL 206 206L3 1182108 SW M/R XMSN DETERIORATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3116L 51529 LINK ASSY DETERIORATED RUBBER. SERIAL NUMBERS REMOVED LK10164, LK7246 AND LK10179. 1 G 7 1 3U H2SW 1996060600733 19960606 00733 SW 1996 6 6 HEEA967155 1 19960508 A 6330 206033554101 LINK ASSY BELL 206 206L1 1182107 SW M/R XMSN DETERIORATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1076T 45373 LINK ASSY RUBBER SEPARATION. 1 G 7 1 3U H2SW 1996060600734 19960606 00734 SW 1996 6 6 HEEA967156 1 19960508 A 6330 206033554101 LINK ASSY BELL 206 206L1 1182107 SW M/R XMSN WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5000K 45167 LINK ASSY WORN ELASTOMER. 1 G 7 1 3U H2SW 1996060600735 19960606 00735 SW 1996 6 6 HEEA967157 1 19960508 A 6330 206033554101 LINK ASSY BELL 206 206L1 1182107 SW M/R XMSN BEARING WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5019F 45244 LINK ASSY TOP BEARING WORN. 1 G 7 1 3U H2SW 1996060600736 19960606 00736 SW 1996 6 6 HEEA967158 1 19960508 A 6330 206033554101 LINK ASSY BELL 206 206L1 1182107 SW M/R XMSN DETERIORATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 LINK ASSY ELASTOMER DETERIORATED. 1 G 7 1 3U H2SW 1996060600737 19960606 00737 SW 1996 6 6 HEEA967159 1 19960508 A 6330 206033554101 LINK ASSY BELL 206 206L1 1182107 SW M/R XMSN WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5012V 45200 LINK ASSY WORN RUBBER. 1 G 7 1 3U H2SW 1996060600738 19960606 00738 SW 1996 6 6 HEEA967160 1 19960508 A 6330 206033554101 LINK ASSY BELL 206 206L1 1182107 SW M/R XMSN DETERIORATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 LINK ASSY ELASTOMER DETERIORATED. SN LK5089 & LK4413 1 G 7 1 3U H2SW 1996060600739 19960606 00739 SW 1996 6 6 HEEA967161 1 19960508 A 6330 206033554101 LINK ASSY BELL 206 206L1 1182107 SW M/R XMSN BEARING SEPARATE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5005F 45176 LINK ASSY BEARING SEPARATED. 1 G 7 1 3U H2SW 1996060600740 19960606 00740 SW 1996 6 6 HEEA967162 1 19960508 A 6330 206033554101 LINK ASSY BELL 206 206L4 1182110 SW M/R XMSN RUBBER SEPARATE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 62127 52023 LINK ASSY RUBBER SEPARATION AT LOWER BEARING. 1 G 7 1 3U NC H2SW 1996060600741 19960606 00741 SW 1996 6 6 HEEA967163 1 19960508 A 6330 206033554101 LINK ASSY BELL 206 206L1 1182107 SW M/R XMSN DETERIORATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5748Q 45499 LINK ASSY DETERIORATED RUBBER. 1 G 7 1 3U H2SW 1996060600743 19960606 00743 CE 1996 6 6 HEEA967166 1 19960508 A 7333 903800097 TRANSMITTER BEECH 200 200CBEECH 1152926 CE PWA PT6 PT6A41 52043 EA FUEL FLOW DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 39PH BL3 ERRATIC FUEL FLOW. 1 L 7 2 4T 4 T A24CE E4EA 1996060600744 19960606 00744 SW 1996 6 6 HEEA967167 1 19960508 A 6320 212075036101 INDICATOR BELL 412 412 1182202 SW GB PRESS/TEMP FLUCTUATES E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 107X 33113 PRESSURE SIDE FLUCTUATES WHEN HOT. 1 G 7 2 4U H4SW 1996060600745 19960606 00745 NM 1996 6 6 9612182767 1 19960601 A 3150 T/O WARNING BOEING 727 7272M7 138407S NM COCKPIT SOUNDED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 727RW 21656 DURING TAKEOFF ROLL, TAKEOFF WARNING HORN SOUNDED WITH THRUST APPLIED, TAKEOFF ABORTED WITH NO INCIDENT. TRIMMED AIRCRA FT, SECOND ATTEMPT WAS NORMAL. MSP MAINTENANCE REPLACED CO-PILOT'S STABILIZER TRIM LIGHT PLATE. PERFORMED TAKEOFF WARN ING CHECK, CHECKED OK. 2 L 7 3 4F A3WE 1996060600746 19960606 00746 NM 1996 6 6 9612192715 1 19960603 A 3244 TIRE BOEING 727 7272S7 138407Z NM NR 1 FAILED A NWAA O OTHER O OTHER LD LANDING 1 GL 01 719RC 22490 DURING LANDING ROLLOUT, THE NR 1 TIRE BLEW OUT. AIRCRAFT STOPPED WITHOUT INCIDENT. MAINTENANCE REPLACED BOTH NR 1 AND NR 2 TIRES, ANTI-SKID TRANSDUCER AND WIRING WITH CONDUIT. PERFORMED ANTI-SKID TEST, CHECKED OK. 2 L 7 3 4F A3WE 1996060600747 19960606 00747 WP 1996 6 6 9612209874 1 19960529 A 2780 ALIGNMENT BLOCKS DOUG DC9 DC951 3022051 WP LE FLAPS OUT OF POSITION A NWAA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 GL 01 783NC 48108 DURING DESCENT INTO GRR, SLAT DISAGREEMENT LIGHT ILLUMINATED. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. FOUN D RIGHT LEADING EDGE SLAT T-DUCT ALIGNMENT BLOCKS BINDING ON TELESCOPIC TUBE. REPOSITIONED UPPER AND LOWER BLOCKS AND C YCLED SLATS NUMEROUS TIMES, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996060600748 19960606 00748 NE 1996 6 6 9612215525 2 19960604 A 7323 TURBINE GOVERNOR BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE NR 1 ENGINE FAILED A NWAA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 GL 01 525US 23619 716460 DURING CLIMB, THE NR 1 ENGINE EXPERIENCED AN UNCOMMANDED SHUTDOWN. AIRCRAFT RETURNED TO SFO AND LANDED WITHOUT FURTHER INCIDENT. REPLACED THE NR 1 ENGINE PERMANENT MAGNET ALTERNATOR STATOR AND ROTOR, CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 1996060600749 19960606 00749 WP 1996 6 6 96UAL900385 1 19960531 A 3350 BATTERY PACK DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1842U 46635 DURING TEST OF EMERGENCY LIGHTS GOT FAULT BALL FOR MID SECTION. LIGHTS INOP FROM 30 LT BACK, OKAY ON RIGHT SIDE. REPLA CED MID CABIN EMERGENCY LIGHTS BATTERY PACK S U1-7106, U1-7108, EEL BATTERY PACK 5822-15 AND MAIN BATTERY PACK 586-1858. 2 L 7 3 4F 4 F A22WE E23EA 1996060600750 19960606 00750 NM 1996 6 6 96UAL900386 1 19960531 A 2751 9660022001 TRANSMITTERS BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE TE FLAP FAILED A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 7264U 21411 PER CREW FLAPS RETRACTED NORMALLY TO FLAPS 5. GOING FROM FLAPS 5 TO FLAPS 2 THE OUTBOARD FLAPS LOCKED OUT AND INBOARD F LAPS CONTINUED UP. USED ALTERNATE FLAP SWITCH TO GET FLAPS UP. *S/D* REPLACED BOTH LEFT AND RIGHT OUTBOARD FLAP TRANS MITTERS DUE TO FAILURE. 2 L 7 3 4F 4 F A3WE E2EA 1996060600751 19960606 00751 NM 1996 6 6 96UAL900387 1 19960531 A 3610 FLANGE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE LOOSE A UALA O OTHER M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 WP 29 7278U 21425 CREW REPORTED A STRUT OVERHEAT NR 3 ENGINE ON TAKEOFF. REDUCED POWER AND SWITCHED PNEUMATICS TO NR 2 ENGINE AND LIGHT S WITCHED OFF. *S/D* AIR LEAK AT FLANGE FOR HP BLEED. FOUND 3 LOOSE BOLTS. SECURED HARDWARE AND RAN ENGINE AGAIN, NO L EAKS PRESENT. 2 L 7 3 4F 4 F A3WE E2EA 1996060600753 19960606 00753 NE 1996 6 6 96UAL900389 2 19960531 A 7261 OIL PUMP SUNDSTRAND 5008437 BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 2 ENGINE CRACKED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 766UA 1760 26917 NUMBER 2 ENGINE LOSING OIL, ENGINE NOT SHUT DOWN. *S/D* OIL LEAK AT MAIN OIL PUMP DUE TO CRACK IN HOUSING. REPLACED M AIN OIL PUMP PER B777 AMM79-21-04. 2 L 7 2 4F 4 F RT T0001SE E46NE 1996060600754 19960606 00754 NM 1996 6 6 96UAL900390 1 19960531 A 3350 RELAY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN FAILED A UALA O OTHER L NO TEST IN INSP/MAINT 1 WP 29 7460U 21914 EMERGENCY EXIT RT CONTROL CIRCUIT BREAKER POPPED. REPLACED R-70 RELAY AND EXIT LIGHT ASSEMBLY IN THE AFT AIRSTAIR. 2 L 7 3 4F 4 F A3WE E2EA 1996060600755 19960606 00755 NM 1996 6 6 96UAL900391 1 19960531 A 2760 BACC63BV14F757 CONNECTOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SPOILER BURNED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 772UA 26930 SPOILERS ADVISORY MESSAGE FAILURE OF ONE OR MORE SPOILER PAIRS. *S/D* FOUND CONNECTOR D2129J BURNED AND REPLACED CONNE CTOR D2129J. 2 L 7 2 4F 4 F RT T0001SE E46NE 1996060600756 19960606 00756 NM 1996 6 6 96UAL900392 1 19960531 A 2780 65176 SWITCH BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 4 LE FLAP WORN A UALA O OTHER O OTHER DE DESCENT 1 WP 29 7446U 21900 INFLIGHT EXTENSION OF FLAPS TO FLAPS 5, LEADING EDGE SLAT NUMBER 4 SLOW TO EXTEND. *S/D* REPLACED NR 4 SLAT EXTEND SWI TCH DUE TO INTERMITTENT OPERATION. 2 L 7 3 4F 4 F A3WE E2EA 1996060600757 19960606 00757 NM 1996 6 6 96UAL900393 1 19960531 A 2820 69186127 VENT TUBE ELBOW BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 FUEL TANK BROKEN A UALA O OTHER K FLUID LOSS CR CRUISE 1 WP 29 7283U 21561 WHILE FEEDING ALL ENGINES FROM TANK NR 2, TANK NR 1 USED APPROXIMATELY 1,000 POUNDS OF FUEL. *S/D* REPLACED BROKEN NR 1 TANK VENT TUBE ELBOW. 2 L 7 3 4F 4 F A3WE E2EA 1996060600758 19960606 00758 NM 1996 6 6 96UAL900394 1 19960531 A 2820 69186127 VENT TUBE ELBOW BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 FUEL TANK BROKEN A UALA O OTHER K FLUID LOSS CR CRUISE 1 WP 29 7295U 21573 CREW REPORTED 500 LBS OF UNWANTED FUEL TRANSFER OUT OF TANK NR 1. *S/D* REPLACED BROKEN NR 1 TANK VENT TUBE ELBOW. 2 L 7 3 4F 4 F A3WE E2EA 1996060600759 19960606 00759 NM 1996 6 6 96UAL900395 1 19960531 A 3350 LAMP BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7256U 21403 LEFT OVERWING EMERGENCY EXIT LIGHT INOP. LAMP BURNED OUT, RELAMPED. 2 L 7 3 4F 4 F A3WE E2EA 1996060600760 19960606 00760 NM 1996 6 6 96UAL900396 1 19960531 A 3350 582214 PWR SUPPLY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7461U 21915 EMERGENCY FLOOR LIGHTING STRIP FROM ROW 5 THROUGH ROW 7 REMAINS ON WITH POWER REMOVED FROM AIRCRAFT. *S/D* POWER SUPPL Y FOR THE AFFECTED EEL SECTION WOULD NOT RESET FOLLOWING AN EEL LIGHTING TEST. REPLACED POWER SUPPLY, OPERATION NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1996060600761 19960606 00761 NM 1996 6 6 96UAL900397 1 19960531 A 7910 372873 LOCK NUT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR2 ENG OIL TANK FAILED A UALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION DE DESCENT 1 WP 29 7280U 21558 700494 NR 2 ENGINE OIL QUANTITY ZERO. ENGINE SHUT DOWN. OIL TANK SUPPORT STRAP NUT FAILED. LOCK NUT CAME OFF STRAP. STUD AN D TANK DROPPED AWAY FROM THE GEARBOX AND DISPLACED THE OIL TRANSFER TUBES. THIS RESULTED IN LOSS OF OIL. 2 L 7 3 4F 4 F A3WE E2EA 1996060600762 19960606 00762 EU 1996 6 6 96UAL900398 1 19960531 A 2932 501310000 SWITCH AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE GREEN HYD SYST LOOSE A UALA K NONE K FLUID LOSS CR CRUISE 1 WP 29 427UA 512 LOST GREEN SYSTEM HYDRAULIC QUANTITY IN CRUISE. BLUE AND YELLOW SYSTEM WERE NORMAL. *S/D* FOUND THE ENGINE PRESSURE S WITCH CAME LOOSE IN FLIGHT. REPLACED SWITCH AND OPERATIONALLY CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 1996060600763 19960606 00763 NM 1996 6 6 96UAL900399 1 19960603 A 3350 LAMP BOEING 737 737322 1384676 NM CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 382UA 24657 EMERGENCY EXIT LIGHT INOP AT DOOR 2L. RELAMPED EMERGENCY EXIT LIGHT AT DOOR 2L, OPERATION CHECKS NORMAL. 2 L 7 2 4F RT A16WE 1996060600765 19960606 00765 NM 1996 6 6 96UAL900401 1 19960603 A 3350 LIGHT BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 9053U 19934 EMERGENCY EXIT LIGHT ABOVE AFT GALLEY DOOR FAILS A-CHECK TEST. REPLACED EMERGENCY LIGHT ASSEMBLY, OPERATION CHECKS NORM AL. 2 L 7 2 4F 4 F A16WE E2EA 1996060600766 19960606 00766 NM 1996 6 6 96UAL900402 1 19960603 A 3350 BATTERY PACK BOEING 757 757222 1384956 NM CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 535UA 25130 EXIT LIGHT ABOVE DOOR 1R WILL NOT ILLUMINATE DURING EMERGENCY LIGHT TEST. REPLACED BATTERY PACK, OPERATION CHECKS NORMA L. 2 L 7 2 4F RT A2NM 1996060600767 19960606 00767 NM 1996 6 6 96UAL900405 1 19960604 A 2820 VALVE CONNECTOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 CROSSFEED LOOSE A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 7461U 21915 NR 1 CROSSFEED VALVE FAILED OPEN, NR 3 FAILED CLOSED. DIVERTED TO DEN. SUPPLEMENTAL DATA UPDATE: FOUND NR 1 CROSSFEED VALVE CONNECTOR DISCONNECTED. RECONNECTED AND OPENED NR 3 CROSSFEED VALVE PER DF794. 2 L 7 3 4F 4 F A3WE E2EA 1996060600768 19960606 00768 NM 1996 6 6 CALA9600701 1 19960429 A 5320 FRAME BOEING 737 737217 1384464 NM E/E DOOR CUTOUT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND A .75 CRACK IN FRAME AT RT SIDE OF E AND E DOOR CUTOUT. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FAB RICATED AND INSTALLED IAW SRM 53-10-2 AND 57-40-3. 2 L 7 2 4F A16WE 1996060600769 19960606 00769 NM 1996 6 6 CALA9600702 1 19960426 A 5330 SKIN BOEING 737 737217 1384464 NM CARGO DR CUTOUT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND A 1.33 CRACK AT FASTENER HOLE IN AFT CARGO DOOR FRAME AFT SKIN. THE CRACKED AREA WAS CUT OUT, A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 AND 51-30-2. 2 L 7 2 4F A16WE 1996060600770 19960606 00770 NM 1996 6 6 CALA9600703 1 19960422 A 5330 SKIN BOEING 737 737217 1384464 NM BS 1040 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND A DENT IN RT FUSELAGE AT STA 1040. THE DENTED AREA WAS CUT OUT. A DOUBLER WAS FABRICATED AND INSTALLE D IAW SRM 53-30-3, FIGURE 1. 2 L 7 2 4F A16WE 1996060600771 19960606 00771 NM 1996 6 6 CALA9600704 1 19960507 A 5315 FLOORBEAM BOEING 737 737217 1384464 NM BS 676 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND A .75 CRACK IN FLOORBEAM AT STA 676, RBL 24. THE BEAM WAS REPAIRED IAW EA 5710-01638. 2 L 7 2 4F A16WE 1996060600772 19960606 00772 NM 1996 6 6 CALA9600705 1 19960502 A 5315 FLOORBEAM BOEING 737 737217 1384464 NM BS 707 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND A 1 INCH CRACK EXTENDING FROM RIVET OF FLOORBEAM AT STA 707, BBL 0. A REPAIR WAS INSTALLED IAW EA 5710 -01322. 2 L 7 2 4F A16WE 1996060600773 19960606 00773 NM 1996 6 6 CALA9600706 1 19960507 A 5311 FRAME BOEING 737 737217 1384464 NM BS 500 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND A 1.5 CRACK AT NUTPLATE HOLE OF FRAME, BS 500A, RT SIDE. THE FRAME SEGMENT WAS REMOVED AND A NEW SECTI ON WAS INSTALLED IAW BOEING DRAWING 65C25113. 2 L 7 2 4F A16WE 1996060600774 19960606 00774 NM 1996 6 6 CALA9600707 1 19960429 A 5730 SKIN BOEING 737 737217 1384464 NM RT WING LE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND A DENT IN RT WING LEADING EDGE SKIN JUST OUTBOARD OF LANDING LIGHT. THE DENTED AREA WAS CUT OUT. A FI LLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-20-1 AND 51-30-2. 2 L 7 2 4F A16WE 1996060600775 19960606 00775 NM 1996 6 6 CALA9600708 1 19960429 A 5330 SKIN BOEING 737 737217 1384464 NM CARGO DR CUTOUT PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND A HOLE IN FUSELAGE SKIN AFT OF AFT CARGO DOOR. A FILLER AND DOUBLER SMALL FLUSH REPAIR WAS INSTALLED I AW SRM 53-30-3. 2 L 7 2 4F A16WE 1996060600776 19960606 00776 NM 1996 6 6 CALA9600709 1 19960429 A 5330 SKIN BOEING 737 737217 1384464 NM BS 887 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 887, STRINGER 25R. THE DENTED AREA OF SKIN WAS CUT OUT, A SKIN SECTION AND SPLICE DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3. 2 L 7 2 4F A16WE 1996060600777 19960606 00777 NM 1996 6 6 CALA9600710 1 19960426 A 5313 STRINGER BOEING 737 737217 1384464 NM BS 383 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND STRINGER 20R CORRODED AT STA 383. THE STRINGER WAS REMOVED AND A NEW STRINGER WAS FABRICATED AND INSTA LLED IAW SRM 51-30-2 AND 51-10-2. 2 L 7 2 4F A16WE 1996060600778 19960606 00778 NM 1996 6 6 CALA9600711 1 19960426 A 5313 STRINGER BOEING 737 737217 1384464 NM BS 360-420 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND STRINGER 26R CORRODED AT STA 360 TO 420. THE STRINGER WAS REMOVED AND A NEW STRINGER WAS FABRICATED AN D INSTALLED IAW SRM 53-10-2 AND 51-30-5. 2 L 7 2 4F A16WE 1996060600779 19960606 00779 NM 1996 6 6 CALA9600712 1 19960426 A 5311 FRAME BOEING 737 737217 1384464 NM BS 400 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND A 1.5 INCH CRACK AT FASTENER HOLE OF FRAME AT STA 400 LOWER LOBE. THE CRACKED AREA WAS REMOVED, A FILL ER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-30-2. 2 L 7 2 4F A16WE 1996060600780 19960606 00780 NM 1996 6 6 CALA9600713 1 19960426 A 5313 STRINGER BOEING 737 737217 1384464 NM BS 355 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND STRINGER 23R CORRODED AT STA 355. THE STRINGER WAS REMOVED AND A NEW STRINGER WAS INSTALLED IAW SRM 53 -10-3. 2 L 7 2 4F A16WE 1996060600781 19960606 00781 NM 1996 6 6 CALA9600714 1 19960505 A 5230 SKIN BOEING 737 737217 1384464 NM FWD CARGO DR DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND IMPACT DAMAGE TO FORWARD CARGO DOOR OUTER SKIN. THE DAMAGED AREA WAS REMOVED AND A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 52-00-3. 2 L 7 2 4F A16WE 1996060600782 19960606 00782 NM 1996 6 6 CALA9600715 1 19960505 A 5751 SKIN BOEING 737 737217 1384464 NM AILERON TAB DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND THE LT WING AILERON TAB SKIN DELAMINATING. THE DELAMINATED AREA WAS REMOVED AND A FIBERGLASS OVERLAY R EPAIR WAS INSTALLED IAW SRM 51-40-9. 2 L 7 2 4F A16WE 1996060600783 19960606 00783 NM 1996 6 6 CALA9600716 1 19960422 A 5330 SKIN BOEING 737 737217 1384464 NM BS 1040 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND RT FUSELAGE SKIN DENTED AT STA 1040. THE DENTED AREA WAS CUT OUT, A DOUBLER WAS FABRICATED AND INSTALL ED IAW SRM 53-30-3, FIGURE 1. 2 L 7 2 4F A16WE 1996060600784 19960606 00784 NM 1996 6 6 CALA9600717 1 19960504 A 5313 STRINGER BOEING 737 737217 1384464 NM BS 294-335 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND CHORD CORRODED AT STA 294 TO 335, STRINGER 26R. THE CHORD SECTION WAS REMOVED AND REPLACED IAW SRM 51- 10-1 AND 51-30-0. 2 L 7 2 4F A16WE 1996060600785 19960606 00785 NM 1996 6 6 CALA9600718 1 19960507 A 5311 FRAME BOEING 737 737217 1384464 NM BS 420 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND A 2 INCH CRACK AT NUTPLATE HOLE OF FRAME, BS 420, STRINGER 22L. THE FRAME SEGMENT WAS REMOVED AND REPL ACED IAW BOEING DRAWING 65C25113. 2 L 7 2 4F A16WE 1996060600786 19960606 00786 NM 1996 6 6 CALA9600719 1 19960507 A 5311 FRAME BOEING 737 737217 1384464 NM BS 440 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND TWO 1 INCH CRACKS AT NUTPLATE HOLES OF FRAME AT BS 440, LT SIDE. THE FRAME WAS REMOVED AND REPLACED IA W BOEING DRAWING 65C25113. 2 L 7 2 4F A16WE 1996060600787 19960606 00787 NM 1996 6 6 CALA9600720 1 19960507 A 5311 FRAME BOEING 737 737217 1384464 NM BS 328 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 328, STRINGER 26L. THE CRACKED AREA WAS REMOVED AND A DOUBLER REPAIR WA S FABRICATED AND INSTALLED IAW SRM 53-40-3 AND 51-30-2. 2 L 7 2 4F A16WE 1996060600788 19960606 00788 NM 1996 6 6 CALA9600721 1 19960507 A 5311 FRAME BOEING 737 737217 1384464 NM BS 328 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND TWO, .5 INCH CRACKS IN FRAME AT BS 328 BETWEEN STRINGER 2OR AND 21R. THE CRACKED AREAS WERE REMOVED, F ILLER AND REPAIR PLATES WERE FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-2. 2 L 7 2 4F A16WE 1996060600789 19960606 00789 NM 1996 6 6 CALA9600722 1 19960426 A 5312 BULKHEAD WEB BOEING 737 737217 1384464 NM BS 664 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND A 7 INCH CRACK IN BULKHEAD PRESSURE WEB AT STA 664, RBL 30. THE WEB WAS REMOVED AND REPLACED IAW SRM 5 1-30-2. 2 L 7 2 4F A16WE 1996060600790 19960606 00790 NM 1996 6 6 CALA9600723 1 19960505 A 5311 FRAME BOEING 737 737217 1384464 NM BS 500 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND TWO, .75 INCH CRACKS IN FRAME AT BS 500B BETWEEN STRINGERS 22R AND 24R. THE FRAME WAS REMOVED AND A NE W FRAME WAS INSTALLED IAW BOEING DRAWING 65C25113. 2 L 7 2 4F A16WE 1996060600791 19960606 00791 WP 1996 6 6 CALA9600724 1 19960501 A 5754 SKIN DOUG DC9 DC982 3022082 WP NR 1 LE FLAP DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 819NY 49479 INSPECTION FOUND TWO DENTS IN NR 1 RT SLAT LEADING EDGE. A REPAIR WAS INSTALLED IAW SRM 57-06, FIGURE 1 AND ECRA 5720-0 1170. 2 L 7 2 4F A6WE 1996060600792 19960606 00792 WP 1996 6 6 CALA9600725 1 19960502 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 256 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 819NY 49479 INSPECTION FOUND THE LT FUSELAGE SKIN DENTED FORWARD OF STA 256 AT LONGERON 17. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-04, FIGURE 38, SHEET 19. 2 L 7 2 4F A6WE 1996060600793 19960606 00793 WP 1996 6 6 CALA9600726 1 19960510 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 256 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 819NY 49479 INSPECTION FOUND THE LT FUSELAGE SKIN DENTED IN TWO PLACES AT STA 256. ONE DENT WAS LOCATED BELOW DOUBLER BETWEEN LONGE RON 17 AND 18. THE OTHER WAS AFT OF DOUBLER BETWEEN LONGERON 17 AND 18. THE DENTED AREAS WERE REMOVED, DOUBLERS WERE F ABRICATED AND INSTALLED IAW SRM 51-30-2 AND ECRA 5330-01203. 2 L 7 2 4F A6WE 1996060600794 19960606 00794 WP 1996 6 6 CALA9600727 1 19960508 A 5320 SUBFLOOR DOUG DC9 DC982 3022082 WP BS 168-200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 819NY 49479 INSPECTION FOUND CABIN SUBFLOOR AT FORWARD SERVICE DOOR CORRODED FROM FS 168 TO 200. A NEW WEB SECTION WAS FABRICATED A ND INSTALLED IAW SRM 51-10-2. 2 L 7 2 4F A6WE 1996060600795 19960606 00795 WP 1996 6 6 CALA9600728 1 19960506 A 5321 FLOOR WEB DOUG DC9 DC982 3022082 WP BS 200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 819NY 49479 INSPECTION FOUND FLOOR WEB CORRODED AT STA 200, LBL 8. THE CORRODED AREA WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTA LLED IAW SRM 53-01. 2 L 7 2 4F A6WE 1996060600796 19960606 00796 WP 1996 6 6 CALA9600729 1 19960502 A 5730 SKIN DOUG DC9 DC982 3022082 WP RT WING LE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 819NY 49479 INSPECTION FOUND A .3125 INCH CRACK IN SKIN AT FORWARD OUTBOARD CORNER OF RIGHT WING FUELING STATION DOOR CUTOUT. THE C RACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-06B. 2 L 7 2 4F A6WE 1996060600797 19960606 00797 NM 1996 6 6 CALA9600730 1 19960419 A 5311 FRAME BOEING 727 727232 1384082 NM BS 215 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16784 20639 INSPECTION FOUND SIDEWALL FRAME IN COCKPIT CORRODED AT BS 215. THE FRAME WAS REMOVED AND A NEW FRAME WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1996060600798 19960606 00798 NM 1996 6 6 CALA9600731 1 19960416 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 303 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16784 20639 INSPECTION FLOOR ATTACH ANGLE CORRODED AT FS 303, LBL 42. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, FIGURE 1. 2 L 7 3 4F A3WE 1996060600799 19960606 00799 NM 1996 6 6 CALA9600732 1 19960416 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 380 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16784 20639 INSPECTION FOUND FLOORBEAM CORRODED AT STA 380, RBL 44 TO 60. A NEW FLOORBEAM WAS FABRICATED AND INSTALLED IAW SRM 53-1 0-8, FIGURE 5. 2 L 7 3 4F A3WE 1996060600800 19960606 00800 NM 1996 6 6 CALA9600733 1 19960416 A 5320 FLOOR SUPPT BOEING 727 727232 1384082 NM BS 418 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16784 20639 INSPECTION FLOOR SUPPORT CORRODED AT STA 418, RBL 24 TO 44. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS FABRICA TED AND INSTALLED IAW SRM 51-40-4. 2 L 7 3 4F A3WE 1996060600801 19960606 00801 NM 1996 6 6 CALA9600734 1 19960420 A 5311 FRAME BOEING 727 727232 1384082 NM BS 1010 GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16784 20639 INSPECTION FOUND OUTBOARD RADIUS OF Z-FRAME GOUGED AT BS 1010, STRINGER 7L. THE GOUGED AREA WAS CUT OUT, A REPAIR WAS F ABRICATED AND INSTALLED IAW SRM 53-10-4, FIGURE 1. 2 L 7 3 4F A3WE 1996060600802 19960606 00802 NM 1996 6 6 CALA9600735 1 19960420 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16784 20639 INSPECTION FOUND FLOORBEAM CORRODED AT STA 312, RBL 12 TO 60. THE FLOORBEAM WAS REMOVED, A T-CAP WAS FABRICATED AND INS TALLED IAW SRM 53-10-8. 2 L 7 3 4F A3WE 1996060600803 19960606 00803 NM 1996 6 6 CALA9600736 1 19960416 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 480 PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16784 20639 INSPECTION FOUND A HOLE IN CABIN FLOORBEAM AT STA 480, RBL 2. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8, FI GURE 3. 2 L 7 3 4F A3WE 1996060600804 19960606 00804 NM 1996 6 6 CALA9600737 1 19960420 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 1110 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16784 20639 INSPECTION FOUND MAIN CABIN FLOORBEAM CORRODED AT BS 1110, RBL 26 TO 36. FOUR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-10-1, FIGURE 1. 2 L 7 3 4F A3WE 1996060600805 19960606 00805 NM 1996 6 6 CALA9600738 1 19960417 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 480 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16784 20639 INSPECTION FOUND FLOORBEAM CORRODED AT BS 480, RBL 44 TO 60. THE CORRODED AREA WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-1, FIGURE 4. 2 L 7 3 4F A3WE 1996060600806 19960606 00806 NM 1996 6 6 CALA9600739 1 19960416 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 340 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16784 20639 INSPECTION FOUND FLOORBEAM CORRODED AT STA 340, RBL 6 TO LBL 31. A REPAIR WAS INSTALLED IAW SRM 53-10-8. 2 L 7 3 4F A3WE 1996060600807 19960606 00807 NM 1996 6 6 CALA9600740 1 19960414 A 5320 DOUBLER BOEING 727 727232 1384082 NM BS 720 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16784 20639 INSPECTION FOUND DOUBLER CORRODED IN FORWARD CARGO PIT AT FS 720D, STRINGER 27L TO 24L. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND MM 51-20-15. 2 L 7 3 4F A3WE 1996060600808 19960606 00808 NM 1996 6 6 CALA9600741 1 19960414 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 620 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16784 20639 INSPECTION FOUND STRINGER 28R CORRODED AT STA 620. THE CORROSION WAS REMOVED AND A STRINGER SPLICE WAS FABRICATED AND I NSTALLED IAW SRM 53-10-3, FIGURE 1. 2 L 7 3 4F A3WE 1996060600809 19960606 00809 NM 1996 6 6 CALA9600742 1 19960415 A 5320 STR SPLICE BOEING 727 727232 1384082 NM BS 625 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16784 20639 INSPECTION FOUND A .75 INCH CRACK IN FORWARD CARGO COMPARTMENT STRINGER SPLICE AT STRINGER 28R, BS 625, RBL 15. THE CRA CKED SPLICE WAS REMOVED, A NEW SPLICE WAS FABRICATED AND INSTALLED IAW SRM 53-10-3, 51-10-2 AND MM 51-20-11. 2 L 7 3 4F A3WE 1996060600810 19960606 00810 NM 1996 6 6 CALA9600743 1 19960415 A 5330 SKIN BOEING 727 727232 1384082 NM BS 700-720 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16784 20639 INSPECTION FOUND SKIN CORRODED IN FORWARD CARGO COMPARTMENT AT STA 700 TO 720, BL 0. THE CORROSION WAS REMOVED, A REPAI R WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 AND 51-30-2. 2 L 7 3 4F A3WE 1996060600811 19960606 00811 NM 1996 6 6 CALA9600744 1 19960419 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 670 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16784 20639 INSPECTION FOUND STRINGER 28L CORRODED AT STA 670. THE CORRODED SECTION WAS CUT OUT. A REPAIR WAS FABRICATED AND INSTA LLED IAW SRM 51-30-2 AND 51-30-3. 2 L 7 3 4F A3WE 1996060600812 19960606 00812 NM 1996 6 6 DHL9670901C 1 19960506 A 5330 SKIN BOEING 727 72782C 1384026 NM BS 1388 BULGED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C-CHECK, FOUND SKIN AT FS 1388 RIGHT SIDE AND FS 1400 RIGHT SIDE. CUT OUT SKIN 4 INCHES BY 4 INCHES, INSTALLED DOUBL ER 6 INCHES BY 6 INCHES, FILLER 4 INCHES BY 4 INCHES PER SRM 54-10-1 AT STA 1388. CLEANED AREA AT FS 1400, NO CORROSION FOUND. 2 L 7 3 4F A3WE 1996060600813 19960606 00813 NM 1996 6 6 DHL9670902C 1 19960502 A 5330 SKIN BOEING 727 72782C 1384026 NM STA 1080 CORROSION A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C-CHECK, FOUND SURFACE CORROSION AT STA 1080 BETWEEN STR 16R AND 18R AFT SKIN OF BUTT SEAM AND ALONG STR 17R STA 1080 TO 1090. REMOVED CORROSION ALONG STR 17R STA 1080 TO 1090, WITHIN LIMITS. INSTALLED FILLER AND EXTERNAL DOUBLER PER S RM 51-30-3 DOUBLER 8 BY 54.5. 2 L 7 3 4F A3WE 1996060600814 19960606 00814 NM 1996 6 6 DHL9670903C 1 19960502 A 5754 SKIN BOEING 727 72782C 1384026 NM NR 6 LE FLAP CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C-CHECK, RIGHT WING LEADING EDGE SLAT O/B HOOK SKIN CRACKED AT RIVET HOLES. REMOVED HOOK FOR ACCESS, FABRICATED AND INSTALLED REPAIR PLATE 4.5 X 3.5 PER SRM 57-30-3. INSTALLED HOOK AND FASTENERS PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996060600815 19960606 00815 NM 1996 6 6 DHL9670904C 1 19960502 A 5400 SKIN BOEING 727 72782C 1384026 NM S-DUCT CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C-CHECK, FOUND S-DUCT HAS CORROSION AROUND FASTENERS AND SKIN BULGE AT 12 O'CLOCK POSITION, 24 FWD OF PRODUCTION BREA K. CUT OUT DAMAGED AREA, INSTALLED DOUBLER 8.5 BY 9.5 PER SRM 54-10-3. 2 L 7 3 4F A3WE 1996060600816 19960606 00816 NM 1996 6 6 DHL9670905C 1 19960512 A 5320 65956002598 FITTING BOEING 727 72782C 1384026 NM BS 1180 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C-CHECK, FOUND CORROSION OF FITTING FWD TOP STA 1180 STR 20L. REMOVED AND REPLACED TIE FITTING PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996060600817 19960606 00817 NM 1996 6 6 DHL9670906C 1 19960509 A 5321 FLOOR BOEING 727 72782C 1384026 NM BS 460 CORROSI0N A A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C-CHECK, FOUND CORROSION ON FLOOR SHEAR AT STA 460 APPROX LBL 51. INSTALLED DOUBLER REPAIR PER SRM 51-40-2, 6.5 INCH BY 5 INCH. 2 L 7 3 4F A3WE 1996060600818 19960606 00818 NM 1996 6 6 DHL9670907C 1 19960508 A 5320 ANGLE BOEING 727 72782C 1384026 NM BS 344 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C-CHECK, FOUND BULGE ON ANGLE AT INTERCOSTAL FS 344 STR 19L. REMOVED AND REPLACED ANGLE PER SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996060600819 19960606 00819 NM 1996 6 6 DHL9670908C 1 19960508 A 5320 BEAM BOEING 727 72782C 1384026 NM BS 1183 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C-CHECK, FOUND CORROSION ON BOTTOM VERTICAL BEAM AT BL 46.93 AT STA 1183. CUT OUT DAMAGED AREA, INSTALLED ANGLE REPA IR AT 1183 PER SRM 51-30-3, 4 BY 1.5 BY 6. 2 L 7 3 4F A3WE 1996060600820 19960606 00820 NM 1996 6 6 DHL9670909C 1 19960507 A 5330 SKIN BOEING 727 72782C 1384026 NM BS 1080 CORROSION A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C-CHECK, FOUND BULGING AROUND FASTENER HEADS AT BS 1080 BUTT JOINT AFT OF PANEL BETWEEN STR 8 AND 4.5 BELOW STR 9. C UT OUT DAMAGED SECTION, INSTALLED REPAIR DOUBLERS AT BS 1080 FROM STR 4 RT TO STR 10 RT IAW S/B 53-109 AND DRAWING 69-62 161, DOUBLERS SIZE 2, 65 BY 7. 2 L 7 3 4F A3WE 1996060600821 19960606 00821 NM 1996 6 6 DHL9670910C 1 19960502 A 5320 DOUBLER BOEING 727 72782C 1384026 NM BS 990-1010 CHAFED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C-CHECK, FOUND SKIN DOUBLER INSIDE B-SYSTEM HYDRAULIC COMPARTMENT, BETWEEN STA 990 AND 1010 CHAFED DEEPLY. INSTALLED DOUBLER PER SRM 53-30-3, 10 BY 6. 2 L 7 3 4F A3WE 1996060600822 19960606 00822 NM 1996 6 6 DHL9670911C 1 19960509 A 5720 ANGLE BOEING 727 72782C 1384026 NM LT WING CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C-CHECK, FOUND CORROSION ON TRAILING EDGE ANGLE AT OUTBOARD HINGE OF OUTBOARD AILERON OF LEFT WING. REMOVED AND REPL ACED LOWER ATTACH ANGLE PER SRM 51-10-1, REPAIR 10 BY 2 BY 1. 2 L 7 3 4F A3WE 1996060600823 19960606 00823 NM 1996 6 6 DHL9670912C 1 19960503 A 2782 ACTUATOR MOUNT BOEING 727 72782C 1384026 NM NR 2 SLAT CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C-CHECK, FOUND NR 2 SLAT ACTUATOR MOUNT CRACKED. FABRICATED DOUBLER REPAIR PER S/B 57-130, DOUBLER 8 BY 3. 2 L 7 3 4F A3WE 1996060600824 19960606 00824 NM 1996 6 6 DHL9670913C 1 19960502 A 5751 SKIN BOEING 727 72782C 1384026 NM AILERON DAMAGED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C-CHECK, OB AILERON OF LEFT WING IB TRAILING EDGE CORNER IS BENT AND OIL CANNING. CUT OUT DAMAGED AREA, FABRICATED N EW SKIN, 14 BY 18 PER SRM 57-50-5. REBALANCED AILERON PER SRM 51-80-4. 2 L 7 3 4F A3WE 1996060600825 19960606 00825 NM 1996 6 6 DHL9670914C 1 19960514 A 5330 SKIN BOEING 727 72782C 1384026 NM BS 1080 DAMAGED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C-CHECK, COMPLY WITH T/A OF S/B 53-109 AT BS 1080 BETWEEN STR 4 LT AND 4 RT. CUT OUT SECTION, FABRICATED SKIN SPLIC E REPAIR DOUBLERS 70 BY 7 PER S/B 53-109. 2 L 7 3 4F A3WE 1996060600826 19960606 00826 NM 1996 6 6 DHL9670915C 1 19960515 A 5330 SKIN BOEING 727 72782C 1384026 NM BS 1080 DAMAGED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C-CHECK, COMPLY WITH TERMINATING ACTION OF S/B 53-109. CUT OUT SECTION FROM STR 4 LT TO 10 LT, BS 1080. INSTALLED R EPAIR DOUBLERS PER S/B 53-109, 67 BY 7. 2 L 7 3 4F A3WE 1996060600827 19960606 00827 NM 1996 6 6 DHL9670916C 1 19960506 A 5330 SKIN BOEING 727 72782C 1384026 NM BS 253 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C-CHECK, FOUND SKIN CRACKED AT FUSE STA 253 STR 10, AFT OF R-3 WINDOW. INSTALLED 10 BY 3 REPAIR DOUBLER PER SRM 53-3 0-3. 2 L 7 3 4F A3WE 1996060600828 19960606 00828 NM 1996 6 6 DHL9670917C 1 19960512 A 5400 STRAP BOEING 727 72782C 1384026 NM S-DUCT CORROSION A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C-CHECK, FOUND NR 2 ENGINE INLET S-DUCT HAS CORROSION ON REINFORCEMENT STRAP AT STA 1203 AT 12 O'CLOCK POSITION. INS TALLED S/S REPLACEMENT STRAP PER AVITAS EO 96PMSI-123RO-6. 2 L 7 3 4F A3WE 1996060600829 19960606 00829 NM 1996 6 6 DHL9670918C 1 19960502 A 5320 DOOR FRAME BOEING 727 72782C 1384026 NM AFT CARGO DR CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C-CHECK, FOUND AFT CARGO DOOR HAS PRESSURIZATION LEAK AT UPPER AFT CORNER. STOP DRILLED CRACKS, INSTALLED REPAIR AT AFT CARGO DOOR FRAME PER AVITAS EO 96PMSI-RO-4, 3.5 BY 9.5. 2 L 7 3 4F A3WE 1996060600830 19960606 00830 NM 1996 6 6 DHL9670919C 1 19960502 A 5330 SKIN BOEING 727 72782C 1384026 NM BS 1166 CORROSION A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C-CHECK, FOUND SKIN BULGE AT STA 1166 BETWEEN STRINGER 21L AND 22L AT AFT LAVATORY SERVICE PANEL. REMOVED CORROSION, INSTALLED DOUBLER REPAIR AT AFT LAVATORY SERVICE PANEL PER AVITAS EO 96PMSI-123RO-5, FILLER PLATE 15.75 BY 14, BACKING PLATE 19 BY 21. 2 L 7 3 4F A3WE 1996060600831 19960606 00831 NM 1996 6 6 DHL9670920C 1 19960503 A 5530 SPAR FORGING BOEING 727 72782C 1384026 NM VERT STAB CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C-CHECK FOUND CORROSION ON VERTICAL FIN FRONT SPAR FORGING BELOW S-DUCT AND LEFT SIDE OF SPLICE PLATE. INSTALLED NEW MODIFIED FRONT SPAR FORGING UPPER SPLICE PLATE BELOW S-DUCT PER AVITAS EO 96PMSI 123D-1, REPAIR 10 BY 3. 2 L 7 3 4F A3WE 1996060600832 19960606 00832 NM 1996 6 6 DHL9670921C 1 19960506 A 5320 WINDOW FRAME BOEING 727 72782C 1384026 NM CABIN CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C-CHECK, FOUND CABIN WINDOW 33L FRAME CRACKED AT BOTH LOWER LEGS. STOP DRILLED CRACK, INSTALLED REPAIR ON FWD AND AF T LOWER LEGS PER AVITAS ENGINEERING ORDER 96PMSI-123D-E, REPAIR SIZE 4, SHIM PLATES 2 LONG. 2 L 7 3 4F A3WE 1996060600833 19960606 00833 NM 1996 6 6 DL72S961326 1 19960531 A 3350 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 400DA 21144 EXIT LIGHT RT AFT INOP, LT WING EMER LIGHT INOP AND RT ENTRY EMER LIGHT INOP. 2 L 7 3 4F A3WE 1996060600834 19960606 00834 NM 1996 6 6 DL72W961308 1 19960528 A 5520 DOUBLER BOEING 727 727247 138408F NM RT ELEVATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2815W 20871 REPAIR DOUBLER CRACKED RT ELEV 3RD FROM O/B HINGE RIB. REPAIRED PER M/M 55-10-31. 2 L 7 3 4F A3WE 1996060600835 19960606 00835 NM 1996 6 6 DL72W961309 1 19960528 A 5532 SKIN BOEING 727 727247 138408F NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2815W 20871 TWO, .75 INCH CRACKS IN VERTICAL STAB SKIN FWD OF SADDLE PANEL RT SIDE ABOVE PANEL 9516. REPAIRED PER M/M 54-30-0. 2 L 7 3 4F A3WE 1996060600836 19960606 00836 NM 1996 6 6 DL72W961310 1 19960528 A 5210 FRAME BOEING 727 727247 138408F NM L2 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2815W 20871 L-2 DOOR FRAME UPPER HINGE CUTOUT CRACKED. REPAIRED PER SRM 52-40-2. 2 L 7 3 4F A3WE 1996060600837 19960606 00837 NM 1996 6 6 DL72W961314 1 19960529 A 3350 RELAY BOEING 727 727247 138408F NM COCKPIT FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2811W 20649 EMERGENCY EXIT LIGHTS WILL NOT GO OUT AFTER TEST. REPLACED R-70 RELAY AND SYSTEM TEST CHECKED NORMAL (P/N 244201154) (M FG 10-60450-3). EVENT OCCURED ON THE GROUND AFTER FLT 1739 ARRIVED FROM TUS\AND THE CREW NOTICED THAT THE EXIT LIGHTS W ERE ON AFTER TESTING. 2 L 7 3 4F A3WE 1996060600838 19960606 00838 NM 1996 6 6 DL72W961315 1 19960529 A 5754 6516221100 SKIN BOEING 727 727247 138408F NM NR 5 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2820W 21058 SKIN CRACKED AT UPPER FWD BOLT HOLE, FENCE ATTACH POINT. REPAIRED PER MM 57-54-0 FIG 813. 2 L 7 3 4F A3WE 1996060600839 19960606 00839 NM 1996 6 6 DL72W961316 1 19960529 A 5754 6516221100 RIB BOEING 727 727247 138408F NM NR 5 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2820W 21058 RIB NR 21 CRACKED. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1996060600840 19960606 00840 NM 1996 6 6 DL73S961296 1 19960514 A 5315 6545410224 FLOOR BEAM BOEING 737 737232 1384475 NM BS 662 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 315DL 23087 THE BL ZERO FLOOR BEAM OF THE WING CENTER SECTION IS CRACKED AT STA 662. NO CRACKS WERE FOUND IN THE WEB. THE CRACK IS TYPICAL PER BOEING SERVICE BULLETIN 737-57-1210. 2 L 7 2 4F RT A16WE 1996060600841 19960606 00841 NM 1996 6 6 DL73S961297 1 19960527 A 2761 SPOILER ACTUATOR BOEING 737 737232 1384475 NM LT WING RUPTURED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 303DL 23075 TOTAL LOSS OF A-SYSTEM HYDRAULICS SYSTEM IN FLIGHT. 2 L 7 2 4F RT A16WE 1996060600842 19960606 00842 NM 1996 6 6 DL73S961327 1 19960531 A 7312 FUEL HEAT VLV BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 311DL 23083 709164 ON CLIMBOUT, NR 1 FUEL HEAT INDICATED FULL OPEN-LOSS OF EPR, SPLIT THROTTLES AND OIL TEMP WENT INTO YELLOW BAND FOR 14 M INS, RETURNED TO MSP. REPLACED FUEL HEAT VALVE PER M/M 73-14-11 PG 402. ALL TEMPERTURES WITHIN LIMITS PER M/M 71-09-10 0 PG 218. FOUND VALVE MISLABLED OLD VALVE. 2 L 7 2 4F 4 F RT A16WE E2EA 1996060600843 19960606 00843 NM 1996 6 6 DL73S961341 1 19960601 A 3397 WIRE BOEING 737 737232 1384475 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 309DL 23081 EMERGENCY LIGHT AT SEAT 19 INOPERATIVE. REPLACED LIGHT ASSY WIRE HARNESS AND LIGHT OPS CK NORMAL. 2 L 7 2 4F RT A16WE 1996060600844 19960606 00844 NM 1996 6 6 DLM88961237 1 19960521 A 4970 OIL PRESS LIGHT DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE APU ILLUMINATED A DALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 SO 27 999DN 2589 53371 APU FAULT LIGHT WITH APU LOW OIL PRESSURE LIGHT CAME ON IN-FLIGHT. (NR 1 GEN ON PREVIOUS MCO). 2 L 7 2 4F 4 F RT A6WE E9NE 1996060600845 19960606 00845 NM 1996 6 6 DLM90961337 1 19960601 A 2450 TRANSFER RELAY DOUG MD90 MD9030 3023690 NM COCKPIT FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 901DA 53381 WHEN THE A/C EMERGENCY PWR IN USE LIGHT CAME ON, PER POM THE EMERGENCY PWR SWITCH WAS PLACED TO THE OFF POSITION. THE E MERGENCY AC BUS OFF LIGHT CAME ON INDICATING THE EMERGENCY AC BUS WAS BEING POWERED FROM THE BATTERY. ACFT WAS DIVERTED TO LAS. REPLACED A/C EMERGENCY POWER TRANSFER RELAY R2-47. 2 L 7 2 4F RT A6WE 1996060600846 19960606 00846 EU 1996 6 6 QXEA9600190 1 19960605 A 3350 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 450US 11101 THE EMERGENCY LIGHT ON THE RIGHT FWD BULKHEAD IS INOPERATIVE. REPLACED DEFECTIVE BULB AND OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996060600847 19960606 00847 WP 1996 6 6 SCNA96151 1 19960517 A 2530 41600011 OVEN DOUG DC10 DC1010 3022110 WP GALLEY SMOKING A SCNA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 15 573SC 46905 WHILE OFF, SMOKE STARTED TO COME OUT OF LATCHING MECHANISM ON OVEN NR 3. CIRCUIT BREAKERS WERE PULLED AND GALLEY POWER WAS TURNED OFF. RESET CIRCUIT BREAKER ON BACK OF OVEN. OPS CHECK NORMAL, NO SIGN OF SMOKE. 2 L 7 3 4F A22WE 1996060600848 19960606 00848 WP 1996 6 6 SCNA96152 1 19960529 A 3230 AYG74155001 CYLINDER DOUG DC10 DC1015 3022118 WP LT MLG INOPERATIVE A SCNA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 152SY 48289 LANDING GEAR FAILED TO RETRACT. DUMPED APPROXIMATELY 28,000 LBS FUEL AND RETURNED TO BASE. REMOVED AND REPLACED BOGIE TRIM INTERLOCK CYLINDER ON LEFT MAIN LANDING GEAR IAW MM 32-31-05, SYSTEM OPS CHECK GOOD. 2 L 7 3 4F A22WE 1996060600849 19960606 00849 NM 1996 6 6 VNAA9606001 1 19960603 A 3234 7178011 SELECTOR HANDLE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LANDING GEAR DEFECTIVE A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 424JS 3033 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF, CREW CYCLED THE GEAR POSITION SELECTOR HANDLE SEVERAL TIMES WITHOUT SUCCES S. CREW EXTENDED THE LANDING MANUALY AND RETURNED TO THE FIELD. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MX REPLACED THE LANDING SELECTOR HANDLE IAW MM 32-30-00. GEAR SWING OPS, CHECKED GOOD. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996060600850 19960606 00850 NE 1996 6 6 WWMA9600048 2 19960604 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LEFT DEFECTIVE A WWMA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 WP 15 247AE 340B247 CREW REPORTED THAT THE LEFT ENGINE OIL PRESSURE WENT TO ZERO. ALSO, THEY HAD A CENTRAL WARNING PANEL LIGHT ON. THE LEF T ENGINE WAS SHUTDOWN AND THE AIRCRAFT LANDED WITHOUT INCIDENT. UPON INVESTIGATION MAINTENANCE FOUND METAL PARTICLES IN THE LEFT ENGINE GEARBOX OIL. THE ENGINE AND GEARBOX WERE REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE 1996060600851 19960606 00851 EU 1996 6 6 WWMA9600049 1 19960604 A 6120 89548120 PROP PITCH CONTL BAG JETSTM JETSTM3201 1500217 EU LT ENGINE DEFECTIVE A WWMA E ENGINE SHUTDOWN O OTHER CL CLIMB 1 WP 15 966AE 966 AFTER TAKEOFF THROUGH 6,000 FEET, THE POWER ROLLED BACK TO 96 PERCENT RPM, IT THEN DECREASED TO 95 PERCENT, EGT WAS AT 6 40 DEGREES AND AT TIMES 650 DEGREES. SPEED LEVER WAS AT HIGH AND THE CREW WAS ABLE TO CONTROL EGT BY PULLING BACK. POW ER HAD NO EFFECT ON POWER SETTING, IT STAYED AT 60 PERCENT. OIL TEMPERATURES WERE CONSTANT AND THE CREW DID NOT NOTE TH E FUEL FLOW. THE LEFT ENGINE WAS SHUT DOWN AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT ENG INE PROP PITCH CONTROL AND PROPELLER. 2 L 7 2 4T RT A56EU 1996061300001 19960613 00001 WP 1996 6 13 9612229753 1 19960604 A 2120 AIR DUCT DOUG DC9 DC941 302207N WP LT CABIN SPLIT A NWAA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 01 753NW 47117 DURING CRUISE, CABIN PRESSURE WOULD NOT HOLD STEADY. SELECTED MANUAL AND STARTED CABIN DOWN MOMENTARILY THEN REVERTED B ACK TO AUTO. RETURNED TO MEM AND LANDED WITHOUT INCIDENT. REPLACED SPLIT DUCT AFT OF ACM ON LEFT SIDE. SYSTEM WAS PLA CED ON MEL. 2 L 7 2 4F A6WE 1996061300002 19960613 00002 WP 1996 6 13 9612239753 1 19960603 A 3320 LIGHT TUBE DOUG DC9 DC941 302207N WP GALLEY OVERHEATED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 753NW 47117 DURING CRUISE TO HOU, FLIGHT ATTENDANT REPORTED SMOKE IN GALLEY AREA. DIVERTED TO GWO AND LANDED WITHOUT INCIDENT. FOU ND GALLEY OVERHEAD FLUORESCENT TUBE NR 3 OVERHEATED AND HERMETIC SEAL FAILED. PLACED LIGHTING SYSTEM ON MEL. ALL ELECT RICAL SYSTEMS OPERATED FOR 30 MINUTES. GALLEY AND OVENS OPERATED FOR 20 MINUTES. ALL OPERATIONAL CHECKS GOOD. 2 L 7 2 4F A6WE 1996061300003 19960613 00003 WP 1996 6 13 9612249878 1 19960603 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 787NC 48149 DURING LINE CHECK, FOUND EMERGENCY EXIT LIGHTS IN AFT STAIRS INOPERATIVE. REPLACED BATTERIES. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996061300004 19960613 00004 WP 1996 6 13 9612259851 1 19960603 A 3350 CONNECTORS DOUG DC9 DC951 3022051 WP CABIN DIRTY A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 760NC 47708 DURING LINE CHECK, FOUND FORWARD ENTRY DOOR ESCAPE PATH EXIT SIGN INOPERATIVE. CLEANED PAINT FROM KNIFE CONNECTORS AT S PLICE JOINT BEHIND ENTRY WAY WALL. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996061300005 19960613 00005 NM 1996 6 13 96FDEA01069 1 19960604 A 3230 RETRACT MECH BOEING 727 7272S2F 1384O81 NM NLG DAMAGED A FDEA K NONE O OTHER LD LANDING 1 SO 25 206FE 22928 UPON LDG AT 147K AND ROLLOUT TO 110K AT WHICH POINT A NOTICEABLE SHIMMY BEGAN AND GOT WORSE. A/C DIRECTION MAINTAINED WITH DIFFERENTIAL BRAKES AND REVERSE. NOSE WHEEL STEERING WAS COMPLETELY INEFFECTIVE. EMERGENCY EQUIPMENT REPORTED TO FLIGHT DECK, AND THAT NO TIRES WERE BLOWN. ****S/D**** INSP NOSE WHEEL STRUT AND DOORS. REPLACED GROUND SHIFT ROD A ND TORQUE LINK PIN. BURNISHED OUT DAMAGE ON LOWER LINK AND REPAINTED. REMOVED AND REPLACED BOTH NOSE WHEEL TIRES PER M M 32-45-11 PG 402 AND MM-15-31, PG 202. A/C OKAY FOR SERVICE. 2 L 7 3 4F A3WE 1996061300006 19960613 00006 NM 1996 6 13 96FDEA01070 1 19960605 A 3610 VALVE BOEING 727 7272S2F 1384O81 NM NR 1 ENGINE LOOSE A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION UK UNKNOWN 1 SO 25 210FE 22932 ENGINE NR 1 STRUT OVERHEAT ILLUMINATED. WHEN NR 1 BLEED WAS CLOSED, LIGHT WENT OUT, FINISHED CHECKLIST RESULTING IN RIG HT PACK AND NR 3 BLEED ONLY USABLE. FOUND SENSE LINE ON NR 1 ENGINE BLEED AIR SHUTOFF VALVE LOOSE, (B-NUT WAS BACKED OF F). TIGHTENED SENSE LINE, RAN ENGINE ON GROUND. NO BLEED LEAKS NOTED. OK FOR SERVICE. 2 L 7 3 4F A3WE 1996061300007 19960613 00007 NM 1996 6 13 96FDEA01071 1 19960604 A 5210 CLOSING MECH BOEING 727 727247 138408F NM PAX DOOR OUT OF ADJUST A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 233FE 21327 ALL MODES OF CABIN PRESSURIZATION SYS FAILED, NO DOOR LIGHT. WHEN A/C BLOCKED IN, FOUND FWD CABIN DOOR IMPROPERLY CLOSE D, AFT PART ADJAR. OPS CHECKED DOOR, DOOR CLOSED PROPERLY. FOUND UPPER AFT PORTION OF DOOR REQ MODERATE PRESSURE WHILE CLOSING TO INSURE UPPER AFT ROLLER RAMPS PROPERLY IN CHANNEL DOOR, SAGS SLIGHTLY. SUSPECT UPPER HINGE BEARING WORN. * S/D* ADJUSTED UPPER ROD LINK ON L-1 DOOR IN ACCORDANCE WITH MAINTENANCE MANUAL 52. 2 L 7 3 4F A3WE 1996061300008 19960613 00008 1996 6 13 ABXA9600502 4 19960603 A 3421 36143091006 EADI DOUG DC9 DC941 302207N WP NR 1 DEFECTIVE A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 965AX 6914 1998 47498 CAPTAIN'S EADI WENT BLANK AND PRODUCED SMOKE AND FUMES IN THE COCKPIT (IN-FLIGHT). REPLACED NR 1 EADI (FOUND SMOKE ODOR IN D.U. FAN) IAW DC-9 M.M. PART TOTAL CYCLES, 3,670. 2 L 7 2 4F A6WE 1996061300009 19960613 00009 NE 1996 6 13 CALA9600745 2 19960603 A 7261 ENGINE BOEING 737 7372C0 1384488 NM PWA JT8 JT8D9 52048 NE NR 2 OIL LEAK A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 09 73243 20072 674329 THE NR 2 ENGINE OIL PRESSURE AND QUANTITY DROPPED ON TAKEOFF. THE DROP IN PRESSURE AND QUANTITY WAS ACCOMPANIED BY ILLU MINATION OF THE LOW OIL PRESSURE LIGHT. THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE COWLING COVERED WITH OIL AND THE OIL STRAINER COVER WAS CRACKED. THE NR 2 ENGINE WAS REMOVED AND REPLACED. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION. *S/D* SHOP FINDINGS REPORTED THAT THE OIL FILTER HOUSING, WHICH HAD BEEN SUSPECT, HAD NO CRACK. THE ENGINE TESTED GOOD AND A BEARING INSPECTION WAS PERFORME D WITH NO DISCREPANCIES NOTED. THE SOURCE OF OIL LEAKAGE WAS NOT CONFIRMED. 2 L 7 2 4F 4 F A16WE E2EA 1996061300010 19960613 00010 WP 1996 6 13 CALA9600746 1 19960605 A 3350 41B004AD073 BATTERIES DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16884 48074 INSPECTION FOUND BOTH THE LEFT AND RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE DURING PRE-DEPARTURE CHECK. TROUBLESHOOTING FOUND THE BATTERIES AT FAULT. THE BATTERIES WERE REPLACED AND OPERATION OF THE OVERWING EMERGENCY EXIT LIGHTS WAS RESTORED. 2 L 7 2 4F A6WE 1996061300011 19960613 00011 NM 1996 6 13 CALA9600747 1 19960504 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 720 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16784 20639 INSPECTION FOUND FORWARD CARGO COMPARTMENT STRINGER 28R CORRODED AT B.S. 720C. THE CORROSION WAS REMOVED. A STRINGER A ND SPLICE WERE FABRICATED AND INSTALLED IAW SRM 53-10-3, FIGURE 1. 2 L 7 3 4F A3WE 1996061300012 19960613 00012 NM 1996 6 13 CALA9600748 1 19960413 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 730-740 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16784 20639 INSPECTION FOUND STRINGER 29R CORRODED AT F.S. 730 TO 740. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-3, 51-30 -10, AND 51-10-7. 2 L 7 3 4F A3WE 1996061300013 19960613 00013 NM 1996 6 13 CALA9600749 1 19960429 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 740 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16784 20639 INSPECTION FOUND FORWARD CARGO COMPARTMENT STRINGER 29L CORRODED AT B.S. 740. THE CORRODED SECTION OF STRINGER WAS REMO VED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-3. 2 L 7 3 4F A3WE 1996061300014 19960613 00014 NM 1996 6 13 CALA9600750 1 19960418 A 5320 FLANGE BOEING 727 727232 1384082 NM BS 1010 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16784 20639 INSPECTION FOUND AFT CARGO CIRCUMFERENTIAL TOP FLANGE, BETWEEN STRINGER 27R AND 28R, STA 1010, MOUNT HOLE FOR SIDEWALL T RANSITION PANEL BROKEN OUT AND WITH A SMALL CRACK. THE CRACKED AREA WAS REMOVED. A CHANNEL WAS FABRICATED AND INSTALLE D IAW SRM 53-10-4, 51-10-3, 51-10-2, AND MM 51-20-0. 2 L 7 3 4F A3WE 1996061300015 19960613 00015 NM 1996 6 13 CALA9600751 1 19960414 A 5753 SKIN BOEING 727 727232 1384082 NM LT TE MID FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16784 20639 INSPECTION FOUND A 3 INCH CRACK IN UPPER SKIN OF LEFT OUTBOARD MID-FLAP AT WBL 442. THE CRACK WAS LOCATED SEVEN INCHES FROM AFT TRAILING EDGE. A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-50-4. 2 L 7 3 4F A3WE 1996061300016 19960613 00016 NM 1996 6 13 CALA9600752 1 19960416 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 740 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16784 20639 INSPECTION FOUND STRINGER 27R IN FAR AFT SECTION OF FORWARD CARGO COMPARTMENT CORRODED NEAR ATTACH ANGLE AT STA 740. THE OLD SPLICE WAS REMOVED. A NEW SPLICE AND ANGLE WERE FABRICATED AND INSTALLED IAW SRM 53-10-3. 2 L 7 3 4F A3WE 1996061300017 19960613 00017 NM 1996 6 13 CALA9600753 1 19960423 A 5744 FITTING BOEING 727 727232 1384082 NM NR 7 SPOILER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16784 20639 INSPECTION FOUND THE NR 7 SPOILER INBOARD WING MOUNTED HINGE FITTING CRACKED OUT OF INBOARD BOLT HOLE. THE INBOARD HING E FITTING WAS REPLACED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996061300018 19960613 00018 NM 1996 6 13 CALA9600754 1 19960430 A 5751 SKIN BOEING 727 727232 1384082 NM AILERON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16784 20639 INSPECTION FOUND A 1 INCH CRACK AT FASTENER HOLE OF LT OUTBOARD AILERON SKIN. A DOUBLER AND FILLER REPAIR WAS FABRICATE D AND INSTALLED IAW SRM 51-30-2 AND 57-50-5. 2 L 7 3 4F A3WE 1996061300019 19960613 00019 NM 1996 6 13 CALA9600755 1 19960416 A 5240 SKIN BOEING 727 727232 1384082 NM RT SERVICE DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16784 20639 INSPECTION FOUND TWO .50 INCH CRACKS IN RT DOOR SIDE SKIN NEXT TO LOWER DOOR STOP FITTINGS. A DOUBLER WAS FABRICATED AN D INSTALLED IAW SRM 51-30-3, 51-10-2, AND 57-40-2. 2 L 7 3 4F A3WE 1996061300020 19960613 00020 NM 1996 6 13 CALA9600756 1 19960413 A 5330 SKIN BOEING 727 727232 1384082 NM BS 1342-1348 LOOSE RIVETS A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16784 20639 INSPECTION FOUND AFT FUSELAGE EXTERNAL SKIN WITH RIVETS LOOSE AND PULLING THROUGH FROM STA 1342 TO 1348, RT SIDE. BULB A NGLES AND A DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 54-30-3 AND 51-40-4. 2 L 7 3 4F A3WE 1996061300021 19960613 00021 NM 1996 6 13 CALA9600757 1 19960413 A 5330 SKIN BOEING 727 727232 1384082 NM BS 1342-1348 LOOSE FASTENERS A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16784 20639 INSPECTION FOUND FASTENERS LOOSE AND PULLING THROUGH EXTERNAL FUSELAGE SKIN AT STA 1342 TO 1348, LT SIDE. A REPAIR CHAN NEL AND SKIN WERE INSTALLED IAW SRM 54-30-3, FIGURE 7. 2 L 7 3 4F A3WE 1996061300022 19960613 00022 NM 1996 6 13 CALA9600758 1 19960420 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 1342 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16784 20639 INSPECTION FOUND A 2 INCH CRACK IN RADIUS OF STRINGER 17R INNER FLANGE AT B.S. 1342. THE STRINGER TIE WAS REMOVED AND T HE CRACK WAS STOP DRILLED. A NEW PART WAS FABRICATED AND INSTALLED IAW SRM 53-10-3, 51-10-2, AND MM 51-20. 2 L 7 3 4F A3WE 1996061300023 19960613 00023 NM 1996 6 13 CALA9600759 1 19960419 A 5712 RIB ATTACH LUG BOEING 727 727232 1384082 NM WS 686 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16784 20639 INSPECTION FOUND A .50 INCH CRACK IN RIB ATTACH LUG ON AFT SIDE OF UPPER VENT STRINGER 12, OUTBOARD SIDE OF W.S. 686 RIB , NR 3 TANK. REPAIR ANGLES, RADIUS BLOCKS, AND VENT PATCHES WERE FABRICATED AND INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996061300024 19960613 00024 NM 1996 6 13 CALA9600760 1 19960414 A 5320 DOOR FRAME BOEING 727 727232 1384082 NM C 2 DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16784 20639 INSPECTION FOUND THE C-2 DOOR FORWARD FRAME CORRODED. A NEW WEB AND T-CAP WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-40-3. 2 L 7 3 4F A3WE 1996061300025 19960613 00025 NM 1996 6 13 CALA9600761 1 19960417 A 5320 STIFFENER BOEING 727 727232 1384082 NM BS 740 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16784 20639 INSPECTION FOUND A .25 INCH CRACK ON TOP OF VERTICAL STIFFENER ON FORWARD INTERNAL WALL OF CENTER FUEL TANK AT STA 740, LBL 15. THE STIFFENER AND TWO T-CLIPS WERE REMOVED AND REPLACED IAW SRM 51-10-1, 51-10-6, 51-30-2, 51-40-4, AND MM 51-2 0-2 AND 51-31-0. 2 L 7 3 4F A3WE 1996061300026 19960613 00026 SO 1996 6 13 COMA9610162 1 19960604 A 5330 12019230001 SKIN EMB 120 EMB120RT SO FRAME 21 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 152CA 17155 120152 DURING AN E9 INSPECTION, FOUND CORROSION ON FUSELAGE LOWER SKIN AT FRAME 21 (FS 6842.6). AT 7 O'CLOCK POSITION, AIRCRAF T HAD A PREVIOUS REPAIR ON FRAME 21 FOR CORROSION AT THE 6 O'CLOCK POSITION. REMOVED PREVIOUS REPAIR DOUBLER, CUT OUT N EW DAMAGED AREA OF FUSELAGE, FABRICATED FILLER AND DOUBLER AS PER SRM 53-00-01. 2 L 7 2 4T RT A31SO 1996061300027 19960613 00027 SO 1996 6 13 COMA9610163 1 19960604 A 2731 ATG120TR SENSOR EMB 120 EMB120RT SO ELEVATOR TRIM DEFECTIVE A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 257CA 120248 TAKEOFF TRIM AURAL WARNING SOUNDED DURING TAKEOFF. TRIM WAS CONFIRMED TO BE PROPERLY SET. REPLACED DEFECTIVE ELEVATOR TRIM PROXIMITY SENSOR. 2 L 7 2 4T RT A31SO 1996061300028 19960613 00028 SO 1996 6 13 COMA9610164 1 19960603 A 5720 12015127001 ANGLE EMB 120 EMB120RT SO LT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 254CA 120233 LEFT WING ROOT FAIRING ATTACH ANGLE IS CRACKED. REPLACED FAIRING ATTACH ANGLE. 2 L 7 2 4T RT A31SO 1996061300029 19960613 00029 1996 6 13 COMA9610165 4 19960603 A 6113 7901891 SPINNER EMB 120 EMB120RT SO LT PROP LOOSE RIVETS A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 1105G 120105 LEFT PROPELLER SPINNER HAS LOOSE RIVETS. REPLACED SPINNER. 2 L 7 2 4T RT A31SO 1996061300030 19960613 00030 SO 1996 6 13 COMA9610166 1 19960604 A 3230 922AA2YA6P2722 SENSOR EMB 120 EMB120RT SO LT MLG DEFECTIVE A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 247CA 120225 WHEN LANDING GEAR SELECTED DOWN, GEAR DID NOT EXTEND. INDICATION WAS 5 RED INTRANSIT AND ONE GREEN DOWNLOCK. EMERGENCY SYSTEM USED TO EXTEND GEAR. REPLACED DEFECTIVE DOWNLOCK PROXIMITY SENSOR ON LEFT MLG. 2 L 7 2 4T RT A31SO 1996061300031 19960613 00031 1996 6 13 COMA9610167 4 19960605 A 3410 39948E2903 AIR SPEED IND EMB 120 EMB120RT SO RT INST PANEL FAILED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 265CA 7262 1732 120257 COPILOT'S AIR SPEED INDICATOR FAILED DURING TAKEOFF. REPLACED THE AIR SPEED INDICATOR. PART TOTAL CYCLES, 7,765. 2 L 7 2 4T RT A31SO 1996061300032 19960613 00032 SO 1996 6 13 COMA9610168 1 19960605 A 7603 CIRCUIT BREAKER EMB 120 EMB120RT SO RT POWER LEVER TRIPPED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 1117H 120117 RIGHT POWER LEVER FLIGHT IDLE STOP SOLENOID CIRCUIT BREAKER TRIPPED. RESET BREAKER - SYSTEM TEST NORMAL. 2 L 7 2 4T RT A31SO 1996061300033 19960613 00033 EU 1996 6 13 COMA9630120 1 19960602 A 8010 WIRE SAAB SF340 SF340A 7850100 EU LT ENGINE CHAFED A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 344CA 340A025 LEFT ENGINE WILL NOT START - NO ROTATION WHEN START SWITCH ENGAGED. REPAIRED CHAFED WIRE AT START RELAY. 2 L 7 2 4T RT A52EU 1996061300034 19960613 00034 EA 1996 6 13 COMA9660101 1 19960602 A 3010 124112450 LEAK DETECTOR CNDAIR CL600 CL6002B19 EA LT WING FAILED A COMA K NONE N FALSE WARNING CR CRUISE 1 SO 01 957CA 390 7109 ANTI-ICE DUCT WARNING MESSAGE ON EICAS. REPLACED 3 DEFECTIVE LEAK DETECTORS IN LEFT WING LEADING EDGE. 2 L 7 2 4F RT A21EA 1996061300035 19960613 00035 EU 1996 6 13 QXEA9600191 1 19960605 A 3350 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 469US 11096 DURING PRE-FLIGHT, CREW FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED BULB AND TESTED GOOD. AIRCRAFT RELEASE D FOR SERVICE. 2 L 7 2 4F RT A20EU 1996061300036 19960613 00036 NM 1996 6 13 QXEA9600192 1 19960605 A 2611 MS25237387 BULB KIDDE 302313 DHAV DHC8 DHC8102 2809003 NM NR 1 SMOKE DET FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 815PH 28265 50 DURING PRE-FLIGHT, CREW FOUND NR 1 CARGO COMPARTMENT WOULD NOT TEST. FOUND DETECTOR BULB BURNED OUT AND RELAMPED, OPS C HECKED GOOD. AIRCRAFT RELEASED FOR SERVICE 2 H 7 2 4T RT A13NM 1996061300037 19960613 00037 NM 1996 6 13 SCNA96153 1 19960604 A 2131 CONTROLLER BOEING 727 727225 1384077 NM E/E COMPT INOPERATIVE A SCNA O OTHER J WARNING INDICATION CR CRUISE 1 GL 15 283SC 22559 DURING TEST FLIGHT, PRESSURIZATION WAS LOST AT ALTITUDE. PLACED AUTO MODE FOR CABIN PRESSURIZATION CONTROLLER ON MEL. R ESEATED CANNON PLUG ON BACK OF CONTROL HEAD. PRESSURIZATION TESTED GOOD IAW MM 21-31-0, CLEARED MEL. 2 L 7 3 4F A3WE 1996061300038 19960613 00038 NM 1996 6 13 VNAA9606002 1 19960606 A 3234 7178011 SELECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LANDING GEAR DEFECTIVE A VNAA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 GL 07 424JS 203 3033 DAY - FLT 4008 - CREW UNABLE TO RETRACT THE LANDING GEAR AFTER TAKEOFF. CYCLED THE SELECTOR HANDLE SEVERAL TIMES WITHO UT SUCCESS. AIRCRAFT RETURNED TO THE FIELD, LANDED WITHOUT INCIDENT. DAY MX REPLACED THE LANDING POSITION SELECTOR HA NDLE I.A.W. M.M.32-30-00, GEAR SWING OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. PART TOTAL CYCLES, 16. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996061300049 19960613 00049 SW 1996 6 13 96ZZZX2917 1 19960520 A 3230 UPLOCK SWRNGN SA226 SA226TC 8780404 SW NLG MALFUNCTIONED A BDHA O OTHER J WARNING INDICATION AP APPROACH 1 GL 15 229AM TC305 NOSE LANDING GEAR DID NOT EXTEND ON THE FIRST TRY AND AIRCRAFT WAS DAMAGED ON LANDING. THE NOSE GEAR DID NOT EXTEND. T HE GEAR WAS NOT CYCLED AND THE EMERGENCY RELEASE WAS NOT PULLED. ALL LIGHT INDICATIONS WERE NORMAL WHEN GEAR RETRACT WA S PERFORMED. COULD NOT BE DUPLICATED. SUSPECT THE UPLOCK HOOK WAS STIFF. 2 L 7 2 4T RT A8SW 1996061300068 19960613 00068 NM 1996 6 13 9612266310 1 19960605 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 670US 24225 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 52C THROUGH 58C. RESECURED WIRES IN SOCKET. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1996061300069 19960613 00069 WP 1996 6 13 9612279905 1 19960605 A 3350 60030451 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 955N 47160 DURING PERIODIC CHECK, FOUND CABIN EMERGENCY LIGHTS DIM. REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996061300070 19960613 00070 WP 1996 6 13 9612289957 1 19960605 A 3350 60030451 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 915RW 47139 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. O PERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996061300071 19960613 00071 WP 1996 6 13 9612299917 1 19960604 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 967N 47573 DURING LINE MAINTENANCE INSPECTION, FOUND INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS AN D BATTERIES. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996061300072 19960613 00072 WP 1996 6 13 9612309922 1 19960604 A 3350 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 945N 47664 DURING PRE-FLIGHT CHECK, FOUND FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. ALSO, REPAIRED WIRES THAT WERE FOUND TO BE SHORTED. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996061300073 19960613 00073 WP 1996 6 13 9612319937 1 19960604 A 3350 FUSE DOUG DC9 DC931 3022065 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 908H 47517 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED FUSE. OPERATIONAL CHECK N ORMAL. 2 L 7 2 4F A6WE 1996061300074 19960613 00074 WP 1996 6 13 9612329937 1 19960604 A 3350 FUSE DOUG DC9 DC931 3022065 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 908H 47517 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED FUSE. OPERATIONA L CHECK NORMAL. 2 L 7 2 4F A6WE 1996061300075 19960613 00075 WP 1996 6 13 9612339973 1 19960603 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9337 47346 DURING PERIODIC CHECK, FOUND OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996061300076 19960613 00076 WP 1996 6 13 9612349978 1 19960604 A 3350 60030451 POWER SUPPLY DOUG DC9 DC931 3022065 WP TAILCONE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9342 47391 DURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE EMERGENCY LIGHTS DIM. REPLACED POWER SUPPLY. OPERATIONAL CHECK NORM AL. 2 L 7 2 4F A6WE 1996061300077 19960613 00077 WP 1996 6 13 9612359984 1 19960603 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 984US 47383 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT OVERWING EMERGENCY EXIT AND AFT CABIN CENTER EMERGENCY EXIT SIGN LIGHTS I NOPERATIVE. REPLACED BATTERY PACK AND BATTERIES. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996061300078 19960613 00078 WP 1996 6 13 9612369959 1 19960605 A 2612 FIRE LOOP DOUG DC9 DC931 3022065 WP B LOOP OUT OF POSITION A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 919RW 47162 FIRE DETECTOR LOOP ANNUNCIATOR ACCOMPANIED BY LOOP B LIGHT ILLUMINATED ON TAKEOFF. ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPOSITIONED LOOP IN NUMEROUS LOCATIONS. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996061300079 19960613 00079 WP 1996 6 13 9612379907 1 19960606 A 2150 SHUT OFF VALVE DOUG DC9 DC931 3022065 WP TAIL COMPT MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 957N 47253 AFTER TAKEOFF FROM PHX, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. AIRCRAFT RETURNED TO PHX AND LANDED WITHOU T INCIDENT. REPLACED LEFT AND RIGHT AIR CONDITIONING PRESSURE REGULATOR AND SHUTOFF VALVES. LEAK AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996061300080 19960613 00080 NM 1996 6 13 96FDEA00972 1 19960513 A 5315 FLOOR BEAM BOEING 727 727227 1384078 NM BS 1070 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 NR 0392 AND NR 005, CORROSION C53-111-01(3) ON LOWER CHORD OF FLOOR BEAM AT NUTPLATE HOLES BS 1070, LBL 41 - RBL 52 WL 200. *****S/D****COMING. REMOVED CORROSION BS 1070, LBL 41 TO RBL 52. AT RBL 12.75, REMOVED 1X1 X .047 INCH BEYOND LI MITS TRIMMED OUT DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED ALL PER SRM 53-10-8, SRM 53-10-1. 2 L 7 3 4F A3WE 1996061300081 19960613 00081 NM 1996 6 13 96FDEA01072 1 19960606 A 2613 652492 OVERHEAT UNIT BOEING 727 7272S2F 1384O81 NM NR 1 ENG STRUT MALFUNCTIONED A FDEA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING UK UNKNOWN 1 SO 25 210FE 22932 DISCREPANCY: ENGINE NR 1 STRUT OVERHEAT LIGHT ILLUMINATED WHEN NR 1 THROTTLE WAS RETARDED, LIGHT WENT OUT. FINISHED CH ECK LIST RESULTING IN RIGHT PACK AND NR 3 BLEED ONLY USABLE. CORRECTIVE ACTION: RAN ENGINE NR 1 AT IDLE POWER, CHECKE D PYLON AREA FOR ANY LEAKS, NONE FOUND. VISUALLY CHECKED TEMPERATURE SENSOR ALL SEEMS OK. REINSTALLED PROPERLY. REPLACE D FIRE OVERHEAT DETECTOR ACCESSORY UNIT FOR PRECAUTION/TROUBLESHOOTING. TESTED OK FOR SERVICE PER MM 26-14-0. INSTALLE D STUB WING PANEL. 2 L 7 3 4F A3WE 1996061300082 19960613 00082 NM 1996 6 13 96FDEA01073 1 19960605 A 5210 507945288 GATE BEAM BOEING 727 727227 1384078 NM FWD ENTRY DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 NR 0177. DISCREPANCY: FWD ENTRY DOOR LOWER GATE BEAM HAS CRACK INDICATION ADJACENT TO LOWER FORWARD STOP PM FITTING IN BOARD FASTENERS. ****S/D ****** COMING. CORRECTIVE ACTION: REMOVED AND REPLACED FORWARD ENTRY DOOR LOWER GATE BEAM IAW OHM 20-50-01. 2 L 7 3 4F A3WE 1996061300083 19960613 00083 WP 1996 6 13 96UAL900406 1 19960605 A 3230 GEAR PINS DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL LANDING GEAR NOT REMOVED A A UALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 WP 29 1831U 46630 ALL LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF, RETURNED TO FIELD. *S/D* GEAR PINS WERE FOUND INSTALLED AFTER AIRCRA FT RETURNED TO FIELD. REMOVED GEAR PINS AND RETURNED AIRCRAFT TO SERVICE. 2 L 7 3 4F 4 F A22WE E23EA 1996061300084 19960613 00084 NM 1996 6 13 96UAL900407 1 19960605 A 2530 80010300331504 SWITCH BOEING 737 737322 1384676 NM OVEN FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 WP 29 317UA 23949 GALLEY OVEN SMOKING, SPARKING WHEN ON. SMOKE COMING FROM HEATER ON LIGHT. *S/D* FOUND SHORT CIRCUIT IN HEATER ON SWIT CH. PROBABLY CAUSED BY MOISTURE IN SWITCH. REPLACED SWITCH, CLEANED OVEN AND CHECKS OK. 2 L 7 2 4F RT A16WE 1996061300085 19960613 00085 NM 1996 6 13 96UAL900408 1 19960605 A 5330 SKIN BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 9023U 19061 THREE RIVETS IN A ROW WITH CRACKS IN FUSELAGE SKIN COMING FROM RIVET HOLES. LOCATION IS APPROXIMATELY ONE FOOT FORWARD AND THREE FEET ABOVE AFT CARGO DOOR. 2 L 7 2 4F 4 F A16WE E2EA 1996061300086 19960613 00086 EU 1996 6 13 96UAL900409 1 19960601 A 5610 WINDOW TRACK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RT COCKPIT CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 410UA 463 FIRST OFFICER'S SLIDING WINDOW LOWER RAIL TRACK FOUND CRACKED. SUPPLEMENTAL DATA UPDATE: REPAIRED TRACK PER STRUCTURAL REPAIR MANUAL SRM-55-11-12. 2 L 7 2 4F 4 F RT A28NM E40NE 1996061300087 19960613 00087 WP 1996 6 13 96UAL900410 1 19960605 A 2150 HEAT EXCHANGER DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 1 PACK CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 1844U 48260 WHILE REPLACING FLEXIBLE DUCT AT COMPRESSOR OUTLET STACK ON NR 1 PACK HEAT EXCHANGER, NOTED CRACK ON OUTLET STACK 12 O'C LOCK POSITION STARTING APPROX 2 INCHES INSIDE OF STACK HEADING DIRECTLY INBD FOR APPROX 1.5 INCHES. *S/D* REPLACED HEA T EXCHANGER. 2 L 7 3 4F 4 F A22WE E23EA 1996061300088 19960613 00088 NM 1996 6 13 96UAL900411 1 19960605 A 3350 BATTERIES BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7258U 21405 AFT STAIR EMERGENCY LIGHT OUT. REPLACED BATTERIES. 2 L 7 3 4F 4 F A3WE E2EA 1996061300089 19960613 00089 NM 1996 6 13 96UAL900412 1 19960605 A 2530 OVEN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE GALLEY BURNT ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 7294U 21572 CREW REPORTED, AFT GALLEY AREA HAS A BURNT SMELL. *S/D* OPERATED COFFEE MAKERS, NO DISCREPANCY OR SMELL NOTED. GALLEY MODULES REMOVED AT LAS. REPLACEMENT OVEN MODULE OPERATED NORMALLY. SUSPECT INBOUND OVEN MODULE, BUT CAUSE UNKNOWN. 2 L 7 3 4F 4 F A3WE E2EA 1996061300090 19960613 00090 NM 1996 6 13 96UAL900413 1 19960605 A 2613 65249203 OVERHEAT DET BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LWR BDY O/H INOPERATIVE A UALA O OTHER L NO TEST IN INSP/MAINT 1 WP 29 7299U 21894 LOWER BODY OVERHEAT DOES NOT TEST. SUPPLEMENTAL DATA UPDATE: REPLACED FIRE AND OVERHEAT DETECTOR. 2 L 7 3 4F 4 F A3WE E2EA 1996061300091 19960613 00091 NM 1996 6 13 96UAL900414 1 19960605 A 2131 CONTROLLER AIRESEARCH 6075103U1 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN MALFUNCTIONED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 WP 29 7286U 10255457 21564 ABORTED TAKEOFF AT DEN. HEARD LOUD AND FREQUENT CHOO CHOOING. FLIGHT ATTENDANT DID NOT REPORT NOISE SO SUSPECT IT WAS NOT ENGINES. CREW FELT VIBRATION. SUSPECT FROM AIR CONDITIONING PACKS. SUPPLEMENTAL DATA UPDATE: CHECKED ENGINE INLE TS AND FOUND NORMAL. RAN PACKS AND FOUND ALL TO BE WORKING NORMALLY. REPLACED LEFT 35 DEGREE CONTROLLER AS PRECAUTIONA RY. 2 L 7 3 4F 4 F A3WE E2EA 1996061300092 19960613 00092 WP 1996 6 13 96UAL900415 1 19960605 A 2781 2A SENSOR DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL LE FLAPS MALFUNCTIONED A UALA O OTHER N FALSE WARNING TO TAKEOFF 1 WP 29 1832U 46631 AFTER THROTTLES ADVANCED FOR TAKEOFF, SLAT DISAGREE LIGHT CAME ON AND TAKEOFF WARNING HORN CAME ON. STOPPED FORWARD MOV EMENT OF THROTTLES AND LIGHT AND HORN STOPPED, THEN CAME ON AGAIN. ABORTED TAKEOFF SLAT LIGHT WENT TO NORMAL. TAKEOFF HORN QUIT. SUPPLEMENTAL DATA UPDATE: BITE CHECK OF PROXIMITY BOX REVEALED FAULT IN SLAT NR 2A SENSOR. FOLLOWING TROUB LESHOOTING, CHAFED WIRE REPAIRED AT WING FEED THROUGH. AS A PRECAUTION, WIRES FROM NR 2A SENSOR TO PROXIMITY BOX WERE R EPLACED LATER. 2 L 7 3 4F 4 F A22WE E23EA 1996061300093 19960613 00093 NM 1996 6 13 96UAL900416 1 19960606 A 2150 ACM AIRESRCH 2040751 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE AFT FUSELAGE FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 7254U 871825 21401 NOISE FROM CONTROL CABIN AIR CONDITIONING GASPER OUTLETS WITH LT PACK ON. LEFT PACK HAS VIBRATIONS AND ODOR AT COLD SET TINGS. SUPPLEMENTAL DATA UPDATE: REPLACED LEFT AIR CYCLE MACHINE DUE TO FROZEN. 2 L 7 3 4F 4 F A3WE E2EA 1996061300094 19960613 00094 1996 6 13 96UAL900417 4 19960606 A 2211 2588812901MOD COMPUTER BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE E/E COMPT CORRODED A UALA O OTHER P O NO WARNING INDICATION OTHER CR CRUISE 1 WP 29 9016U 157 19054 YAW DAMPER ABRUPTLY MOVES RUDDER INTERMITTENTLY FOR NO APPARENT REASON. *S/D* REPLACED YAW COUPLER AND VERTICAL GYRO. FOUND CORROSION ON COMPUTER CONTACTS. REPLACED ROLL COMPUTER, CHECKS OK. 2 L 7 2 4F 4 F A16WE E2EA 1996061300096 19960613 00096 WP 1996 6 13 ABXA9600504 1 19960606 A 3260 AN30213 LEVER NIHON YS11 YS11A500 6310416 WP NLG DEFECTIVE A ABXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 913AX 2053 LANDING GEAR UNSAFE LIGHT ILLUMINATED AND STAYED ON IN-FLIGHT. REPLACED NOSE GEAR UP AND DOWNLOCK SWITCHES AND LEVER IA W YS-11 M.M. 32-61-3. OPS CHECKED GOOD. 2 L 7 2 4T A1PC 1996061300097 19960613 00097 WP 1996 6 13 CALA9600762 1 19960606 A 2842 O-RING DOUG DC9 DC932 3022066 WP LT FUEL PROBES DETERIORATED A CALA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SW 09 27522 47524 A FUEL LEAK FROM THE LT WING UPPER SURFACE WAS DISCOVERED WHILE CRUISING AT FL 260. THE AIRCRAFT WAS DIVERTED TO DFW WH ERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 AND NR 3 FUEL QUANTITY PROBES LEAKING DUE TO DETERIORATED O- RINGS. THE O-RINGS AND BACKUP RINGS WERE REPLACED IAW MM 28-40-1, CODE 3, PAGES 201-203. FURTHER INSPECTION FOUND NO O THER LEAKS. 2 L 7 2 4F A6WE 1996061300098 19960613 00098 WP 1996 6 13 CALA9600763 1 19960606 A 2910 7920134959 HYD LINE DOUG DC9 DC932 3022066 WP WHEEL WELL BROKEN A CALA O OTHER J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SW 09 17531 45847 THE RT HYDRAULIC SYSTEM PRESSURE AND QUANTITY DROPPED TO ZERO IN-FLIGHT. THE LOSS OF PRESSURE AND FLUID WAS ACCOMPANIED BY ILLUMINATION OF THE RT HYD PRESS LOW AND RUDDER CONTROL MANUAL ANNUNCIATOR LIGHTS. THE AIRCRAFT LANDED WITHOUT INCI DENT. MAINTENANCE FOUND A BROKEN HYDRAULIC PRESSURE LINE IN THE RT WHEELWELL. A FLEX LINE WAS INSTALLED AND A DIP WAS ISSUED TO REPLACE THE FLEX LINE WITHIN 1200 HOURS OR 500 FLIGHTS. THE HYDRAULIC SYSTEM WAS SERVICED AND LEAK CHECK WAS GOOD. 2 L 7 2 4F A6WE 1996061300099 19960613 00099 NM 1996 6 13 CALA9600764 1 19960602 A 5312 BULKHEAD WEB BOEING 727 727232 1384082 NM BS 1183 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 27783 20638 INSPECTION FOUND A 1 INCH CRACK IN STA 1183 PRESSURE BULKHEAD AT LBL 8, W.L. 162. THE BULKHEAD WEB WAS REPAIRED IAW ECR A 5310-01473 AND BOEING DRAWING 65C33041. 2 L 7 3 4F A3WE 1996061300100 19960613 00100 WP 1996 6 13 CALA9600765 1 19960527 A 5320 SKIN DOUG DC9 DC982 3022082 WP CARGO DR JAMB DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16804 49246 THE FUSELAGE SKIN AT MID-CARGO DOOR THRESHOLD AREA WAS DAMAGED BY A BELT LOADER. THE DAMAGED AREA WAS REPAIRED IAW ECRA 5330-02404. 2 L 7 2 4F A6WE 1996061300101 19960613 00101 WP 1996 6 13 CALA9600766 1 19960605 A 5350 CABLES DOUG DC9 DC982 3022082 WP TAILCONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35832 49492 THE TAILCONE INTERIOR AND EXTERIOR HANDLES PULLED AT 50 POUNDS TO OPEN LATCHES. THE TAILCONE CABLE PULL TENSION WAS ADJ USTED IAW MM 53-53-00. 2 L 7 2 4F A6WE 1996061300102 19960613 00102 WP 1996 6 13 CALA9600767 1 19960509 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72825 49485 INSPECTION FOUND A .3125 INCH CRACK IN FUSELAGE SKIN AT AFT HINGE CUT-OUT FOR LT NLG STRUT DOOR. THE CRACK WAS STOP DRI LLED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 53-05. 2 L 7 2 4F A6WE 1996061300103 19960613 00103 WP 1996 6 13 CALA9600768 1 19960601 A 5320 DOOR JAMB DOUG DC9 DC982 3022082 WP CARGO COMPT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72825 49485 INSPECTION FOUND MID-CARGO DOOR JAMB LOWER AREA ABOVE SCUFF PLATE CORRODED. THE AREA WAS REPAIRED IAW ECRA 5310-03027. 2 L 7 2 4F A6WE 1996061300104 19960613 00104 NM 1996 6 13 DL72S961357 1 19960604 A 3350 LIGHT BOEING 727 727232 1384082 NM CABIN CORRODED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 520DA 21471 RT EXTERIOR EMERGENCY EXIT LIGHT AT OVERWING HATCH INOP. CLEANED CORROSION ON LIGHT SOCKET CONTACTS. CHECKS NORMAL. 2 L 7 3 4F A3WE 1996061300105 19960613 00105 NM 1996 6 13 DL72S961358 1 19960529 A 5320 TORQUE BOX BOEING 727 727232 1384082 NM BS 1226 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 522DA 21582 AT MID-VISIT, THE AFT STAIRWELL RT TORQUE BOX WAS FOUND CRACKED AT THE UPPER LIGHTENING HOLE AT STA 1226. REPAIRED PER MM 53-11-0. 2 L 7 3 4F A3WE 1996061300106 19960613 00106 NM 1996 6 13 DL72W961352 1 19960529 A 5330 65545661 SKIN BOEING 727 727247 138408F NM BS 540 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2815W 20871 MTC REPORTS CORROSION ON THE FUSELAGE SKIN AT STA 540 AT STR 27R. CUT-OUT RESULTED IN 5.5 INCHES FWD/AFT BY 3.3 INCHES CIRCUM. AN EXISTING REPAIR INBD OF NEW DAMAGE REPAIRS A CUTOUT MEASURING .15 INCH FWD/AFT BY 2.5 INCHES CIRCUM. SKIN IS MACHINED FROM .125 INCH 2024-T3. LOCAL THICKNESS IS .110 INCH. REPAIR WILL INCORPORATE BOTH LOCATIONS INTO ONE REPAIR . 2 L 7 3 4F A3WE 1996061300107 19960613 00107 NM 1996 6 13 DL757961322 1 19960530 A 2530 COFFEE MAKER 811150417 BOEING 757 757232 1384965 NM FWD GALLEY OVERHEATED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 659DL 212 24421 FLIGHT ATTENDANTS REPORTED SMOKE COMING FROM AREA AROUND THE AFT COFFEE MAKER IN THE FIRST CLASS GALLEY. SMOKE DID NOT SEEM TO STOP WHEN THEY PULLED THE CIRCUIT BREAKER IN THE GALLEY. PULLED CIRCUIT BREAKERS S-32 AND S-33 ON THE P-11 PANE L. SMOKE SEEMED TO CEASE. 2 L 7 2 4F RT A2NM 1996061300108 19960613 00108 NM 1996 6 13 DL757961340 1 19960601 A 2530 OVEN 831610401 BOEING 757 757232 1384965 NM MID GALLEY FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 640DL 40 23994 AT CRUISE, F/A REPORT ODOR OF OVERHEATED PLASTIC SMELL AT MID-GALLEY. ODOR PARTICULARLY STRONG AT MID-GALLEY VENT. REM OVED ALL POWER AND ODOR DISSIPATED IN APPROXIMATELY 1 HOUR. INSPECTED AREA FOR SHORTS AND CHAFES - N0NE NOTED. REPLACE D SUSPECTED OVERHEATED/DEFECTIVE FWD FACING MID-GALLEY OVEN. 2 L 7 2 4F RT A2NM 1996061300109 19960613 00109 1996 6 13 DL76L961302 4 19960527 A 3460 FMC 4058650930 BOEING 767 767332 1382001 NM RIGHT FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 173DN 90070899 24800 RT FMC LOCKED UP THEN LEFT FMC LOCKED. AFTER A PERIOD OF TIME, BOTH RESUMED NORMAL OPERATION FOR APPROXIMATELY 2 MINUTE S, THEN RT FMC FAILED. THEN LEFT FMC FAILED. RE-PROGRAMMED ALL DATA IN FMC. AFTER APPROXIMATELY 2 MINUTES, BOTH FMC'S FAILED AGAIN. ON ARRIVAL NYC, REGAINED RT FMC AND THEN LEFT FMC. ON APPROACH, LT FMC FAILED AGAIN. CORRECTIVE ACTION : REPLACED RT MCDU WITH TWA POOL PART. PERFORMED TEST OF FMS SYSTEMS ALL OK. 2 L 7 2 4F RT A1NM 1996061300110 19960613 00110 NM 1996 6 13 DL76L961348 1 19960603 A 5522 183T30018 SKIN BOEING 767 767332 1382001 NM RT ELEVATOR DAMAGED A DALA K NONE C F.O.D. IN INSP/MAINT 1 SO 27 179DN 25144 RT ELEVATOR STRUCK BY STAIR TRUCK CAUSING EXTENSIVE DAMAGE. APPROXIMATELY 4 FOOT SECTION TORN OFF. NO OBVIOUS ADDITIONA L AIRCRAFT STRUCTURAL DAMAGE. REPLACED RIGHT ELEVATOR CONTROL SURFACE. 2 L 7 2 4F RT A1NM 1996061300111 19960613 00111 NM 1996 6 13 DL76P961354 1 19960603 A 3350 20131A BATTERY PACK BOEING 767 767332 1382001 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 140LL 25988 FOUND FLOOR TRACK LIGHTS INOPERATIVE. BOTH LT AND RT SIDES FROM ROW 34 AFT. REPLACED BATTERY PACK 9010. SYSTEM OPERAT ION NORMAL. 2 L 7 2 4F RT A1NM 1996061300112 19960613 00112 NM 1996 6 13 DL76S961342 1 19960601 A 2497 WIRE BOEING 767 767332 1382001 NM E/E COMPT CHAFED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 129DL 24079 FOUND NUMEROUS CIRCUIT BREAKERS TRIPPED ON P6-4 PANEL. REPAIRED WIRES JUST AFT OF CHILLER UNIT IN E/E AREA IN WIRE RUN W272. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A1NM 1996061300113 19960613 00113 WP 1996 6 13 DLL10961350 1 19960524 A 5330 SKIN LKHEED 1011 10113851 5265010 WP FS 469 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 715DA 193C1092 DURING LAYOVER IN ATL, CORROSION WAS FOUND IN THE SKIN JUST AFT OF THE NLG DOOR CUT-OUT. THE CORROSION IS LOCATED BETWE EN STRINGERS 33 AND 34 AT APPROX. FS 469. ALSO, TWO DENTS WERE DISCOVERED BETWEEN FS 469 AND FS 489. THE DAMAGE WAS CL EANED UP, FILLED AND REINFORCED. *** REV B TO ER/A PROVIDES FAA APPROVAL FOR REPAIR *** 2 L 7 3 4F A23WE 1996061300114 19960613 00114 WP 1996 6 13 DLL13961321 1 19960530 A 3350 POWER SUPPLY 5165741 LKHEED 1011 10113851 5265010 WP R4 DOOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 790DL 61442 193A1143 ON LAYOVER, FOUND D-ZONE EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. SYSTEM CHECKS GOOD. 2 L 7 3 4F A23WE 1996061300115 19960613 00115 WP 1996 6 13 DLL13961332 1 19960530 A 3350 08163000710 TRACK LKHEED 1011 10113851 5265010 WP CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 790DL 193A1143 EMERGENCY LIGHT FLOOR TRACK BROKEN AT F/C RT SIDE. FOUND ON LAYOVER. C/A: REPLACED FLOOR TRACK, CKS OK. 2 L 7 3 4F A23WE 1996061300116 19960613 00116 WP 1996 6 13 DLL14961334 1 19960601 A 3350 5165741 BATTERY PACK LKHEED 1011 1011385115 5265015 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 740DA 193C1244 2L AND 2R EMERGENCY EXTERIOR LIGHTS INOP. C/A: REPLACED EMERGENCY BATTERY PACKS FOR 2L AND 2R, CKS OK. 2 L 7 3 4F A23WE 1996061300117 19960613 00117 WP 1996 6 13 DLL14961351 1 19960524 A 5743 1604672101 ATTACH FITTING LKHEED 1011 1011385115 5265015 WP LT MLG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 736DY 193C1227 THE LT MLG RETRACT ACTUATOR RIB FITTING WAS FOUND WITH CORROSION. THE DAMAGE WAS CLEANED UP; SEVERAL FASTENER HOLES WERE SPOT-FACED. THE FITTING WAS EVALUATED AFTER CLEAN-UP AND IT WAS DETERMINED THAT IT COULD STILL CARRY THE INTENDED FLIGHT LOADS. *** REV A PROVIDES FAA APPROVAL TO REPAIR *** 2 L 7 3 4F A23WE 1996061300118 19960613 00118 WP 1996 6 13 DLL17961313 1 19960529 A 3350 P2070003 BATTERY LKHEED 1011 10113853 5265020 WP CABIN MISSING A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 765DA 193H1206 FOUND CAPTAIN'S EMERGENCY FLASHLIGHT SEAL BROKEN AND BATTERY EMPTY DUE LIGHT MOUNTED 180 DEGREES WRONG. REPLACED FLASHL IGHT AND BATTERY. 2 L 7 3 4F A23WE 1996061300119 19960613 00119 NM 1996 6 13 QXEA9600193 1 19960606 A 3350 BULB GRIMES 3017423 DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 828PH 287 DURING PRE-FLIGHT, FOUND LEFT UNDERWING EGRESS LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY, CHECKED GOOD. AIRCRAFT RELEA SED FOR SERVICE. 2 H 7 2 4T RT A13NM 1996061300120 19960613 00120 NE 1996 6 13 SWAA960473 2 19960603 A 7200 ENGINE BOEING 737 7373H4 1384600 NM GE CFM56 CFM563B1 13802 NE NR 1 FAILED A A SWAA D E RETURN TO BLOCK ENGINE SHUTDOWN E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SW 07 313SW 23335 721139 EXPERIENCED NR 1 ENGINE VIBRATION, FOLLOWED BY A/C YAWING TO THE LEFT. N2 RED WARNING LIGHT ILLUMINATED. ENGINE THROTT LE WAS RETARDED TO IDLE, BUT VIBRATION CONTINUED. CREW PERFORMED ENGINE SHUT-DOWN PROCEDURES. AIRCRAFT RETURNED TO OAK AND MADE AN UNEVENTFUL LANDING. REPLACED ENGINE ASSEMBLY PER BOEING M/M. 2 L 7 2 4F 4 F RT A16WE E2GL 1996061300121 19960613 00121 NM 1996 6 13 SWAA960474 1 19960531 A 2120 AIR DISTR BOEING 737 7373H4 1384600 NM CABIN ODOR A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 387SW 26602 FUEL SMELL NOTED IN FORWARD GALLEY AREA. AIRCRAFT RETURNED TO OAK AND MADE AN UNEVENTFUL LANDING. INSPECTED CABIN AND CARGO AREAS, CHECKED A/C PACKS AND PERFORMED ENGINE RUN, NO DEFECTS NOTED. 2 L 7 2 4F RT A16WE 1996061300122 19960613 00122 NM 1996 6 13 SWAA960475 1 19960530 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 520 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN BULGING AT RIVETS AFT OF BS 520C, S28L. REPAIRED PER SWA RA 1-353-1465. 2 L 7 2 4F RT A16WE 1996061300123 19960613 00123 NM 1996 6 13 SWAA960476 1 19960529 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 350 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN DENTED AT BS 350, S18R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996061300124 19960613 00124 NM 1996 6 13 SWAA960477 1 19960602 A 5313 SKIN BOEING 737 7373H4 1384600 NM BS 755 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 330SW 23694 DURING SCHEDULED BC3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 755, S23L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996061300125 19960613 00125 NM 1996 6 13 SWAA960478 1 19960530 A 3350 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 314SW 23336 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY LIGHT AT LEFT OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK PER BOEI NG M/M. 2 L 7 2 4F RT A16WE 1996061300126 19960613 00126 NM 1996 6 13 SWAA960479 1 19960603 A 5330 SKIN BOEING 737 7372T4 1384492 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED TERMINAL CHECK, FOUND FUSELAGE SKIN CRACKED LEFT SIDE AFT OF BS 727 BELOW WINDOW 7TH FROM EMERGENCY EXI T S15. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996061300127 19960613 00127 NM 1996 6 13 SWAA960480 1 19960529 A 5330 SKIN BOEING 737 7372H4 138448C NM PAX DOOR CUTOUT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 95SW 23054 DURING SCHEDULED B-CHECK, FOUND FORWARD ENTRY DOOR LOWER HINGE CUT-OUT CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996061300128 19960613 00128 NM 1996 6 13 SWAA960481 1 19960529 A 5330 SKIN BOEING 737 7372H4 138448C NM SERV DR CUTOUT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 95SW 23054 DURING SCHEDULED B-CHECK, FOUND AFT SERVICE DOOR UPPER HINGE CUT-OUT CRACKED .3750 INCH FROM RADIUS. REPAIRED PER BOEIN G SRM. 2 L 7 2 4F A16WE 1996061300129 19960613 00129 NM 1996 6 13 SWAA960482 1 19960531 A 5230 WEB BOEING 737 7372H4 138448C NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 94SW 23053 DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR OUTER WEB CRACKED 1.5 INCH ON LOWER FWD SIDE. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996061300130 19960613 00130 NM 1996 6 13 SWAA960483 1 19960604 A 3350 6040681 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 85SW 22826 DURING SCHEDULED SERVICE CHECK, FOUND LT AND RT FWD EXTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK P ER BOEING M/M. 2 L 7 2 4F A16WE 1996061300131 19960613 00131 NM 1996 6 13 SWAA960484 1 19960604 A 5320 SPLICE BOEING 737 7372H4 138448C NM BS 907 CRACKED A SWAA K NONE O W OTHER INADEQUATE Q C IN INSP/MAINT 1 SW 07 57SW 21722 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, S4R. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996061300132 19960613 00132 NM 1996 6 13 SWAA960485 1 19960604 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 253 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 20SW 21337 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED TWO PLACES IN R3 WINDOW FRAME .6250 INCH. REPLACED PER BOEING SR M AMD S/B 737-53-1115. 2 L 7 2 4F A16WE 1996061300134 19960613 00134 NM 1996 6 13 SWAA960487 1 19960529 A 5330 SKIN BOEING 737 7373A4 1384585 NM FWD DOOR CUTOUT DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR UPPER HINGE CUT-OUT DAMAGED ON UPPER AND LOWER EDGES. REPAIRED PER BOEIN G SRM. 2 L 7 2 4F RT A16WE 1996061300135 19960613 00135 NM 1996 6 13 SWAA960488 1 19960529 A 5330 SKIN BOEING 737 7373A4 1384585 NM BS 353 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 353, JUST BELOW S17L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996061300136 19960613 00136 NM 1996 6 13 SWAA960489 1 19960529 A 5330 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT THE FOLLOWING LOCATIONS: BS 315 - 318, AT S24 AND 25L, BS 322, S18, BS 921, S19 AND 20. BS 1088, BETWEEN 24 AND 25L, BS 1019, BETWEEN S16 AND 17R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996061300137 19960613 00137 NM 1996 6 13 SWAA960490 1 19960529 A 5312 BULKHEAD CLIP BOEING 737 7373A4 1384585 NM BS 947 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED D-CHECK, FOUND BULKHEAD TO STRINGER CLIP SUPPORT ANGLE CRACKED AT BS 947, S22L. REPLACED PER BOEING SR M. 2 L 7 2 4F RT A16WE 1996061300138 19960613 00138 NM 1996 6 13 SWAA960491 1 19960529 A 5320 BRACKET BOEING 737 7373A4 1384585 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED D-CHECK, FOUND ANGLE BRACKET CRACKED AT BS 727, BL ZERO, WL 154. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996061300139 19960613 00139 NM 1996 6 13 SWAA960492 1 19960529 A 5320 SPLICE BOEING 737 7373A4 1384585 NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED D-CHECK, FOUND FASTENER HOLE CRACKS ON STRINGER SPLICES AT BS 907, S4L AND S4R. REPLACED PER BOEING SR M. 2 L 7 2 4F RT A16WE 1996061300140 19960613 00140 NM 1996 6 13 SWAA960493 1 19960529 A 5311 FRAME BOEING 737 7373A4 1384585 NM BS 787 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME DENTED AT BS 787, S24-25R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996061300141 19960613 00141 NM 1996 6 13 SWAA960494 1 19960529 A 5330 SKIN BOEING 737 7373A4 1384585 NM PNL 3401 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT LOWER CORNER OF PANEL 3401. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996061300142 19960613 00142 NM 1996 6 13 SWAA960495 1 19960529 A 5320 ANGLE BOEING 737 7373A4 1384585 NM BS 291 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED D-CHECK, FOUND WEB ANGLES TO SKIN CRACKED AT BS 291, ABOVE AND BELOW S11R. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996061300143 19960613 00143 NM 1996 6 13 SWAA960496 1 19960529 A 5320 FRAME BOEING 737 7373A4 1384585 NM BS 333 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED D-CHECK, FOUND WEB TO DOOR FRAME CRACKED AT BS 333, S8R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996061300144 19960613 00144 NM 1996 6 13 SWAA960497 1 19960529 A 5330 SKIN BOEING 737 7373A4 1384585 NM BS 371 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED D-CHECK, FOUND CHAFING DAMAGE TO SKIN AT BS 371, BETWEEN S6L AND 5L. INSTALLED REPAIR DOUBLER PER BOEI NG SRM. 2 L 7 2 4F RT A16WE 1996061300145 19960613 00145 NM 1996 6 13 SWAA960498 1 19960529 A 5330 SKIN BOEING 737 7373A4 1384585 NM BS 500 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 500B, BETWEEN S14L AND 15L. INSTALLED REPAIR DOUBLER PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1996061300146 19960613 00146 NM 1996 6 13 VNAA9606003 1 19960603 A 5540 RUDDER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE VERT STAB LIGHTNING STRIKE A VNAA O OTHER C F.O.D. CR CRUISE 1 GL 07 423JS 3032 CREW REPORTED HEARING A LOUD BANG, NO APPARENT CHANGE IN ANY OF THE AIRCRAFT SYSTEMS. AIRCRAFT CONTINUED ON WITH THE FL IGHT AND LANDED IN PIT WITHOUT FURTHER INCIDENT. PIT MX CONDUCTED A LIGHTNING STRIKE INSPECTION AND NOTICED THAT THE RU DDER CAP SHOWED SIGNS OF LIGHTNING STRIKE DAMAGE, BURN MARKS. REPAIRS WERE ACCOMPLISHED IAW MANUFACTURERS RECOMMENDATI ONS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996061300202 19960613 00202 SO 1996 6 13 RAAAE896003 1 19960119 A 3350 8621006 BATTERY PACK 873100212 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 SEAT ROW 15 EGRESS FLOOR PROXIMITY LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. (X) 2 L 7 4 4T 4A22 1996061300203 19960613 00203 SO 1996 6 13 RAAAE896004 1 19960119 A 3350 8621014 BATTERY PACK 873100212 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 LEFT AFT OVERWING EGRESS IDENTIFIER LIGHT ASSY FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. (X) 2 L 7 4 4T 4A22 1996061300205 19960613 00205 SO 1996 6 13 RAAAE906005 1 19960119 A 3350 8621014 BATTERY PACK 873100212 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 RT AFT OVERWING EGRESS IDENTIFIER LIGHT ASSY FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. (X) 2 L 7 4 4T 4A22 1996061300207 19960613 00207 CE 1996 6 13 96ZZZX2925 1 19960126 A 7331 1200106193 FUEL FLOW LINE CESSNA 210 210L 2073448 CE COCKPIT CHAFED A A FPIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 15 93111 21060266 ON JANUARY 26, 1996, PILOT REPORTED ELECTRICAL FAILURE GLOW BEHIND INSTRUMENT PANEL. MAINTENANCE FOUND TRANSPONDER DIMM ER WIRE SHORTED AGAINST PRESSURE LINE. REPLACED FUEL PRESSURE LINE WITH STRATOFLEX III HOSE AND FITTING. INSPECTIONS O N REMAINING FLEET OF CE210'S RESULTING WITH 75 PERCENT HAVING CHAFED FUEL FLOW LINES. ALL LINES ARE BEING REPLACED WITH STRATOFLEX III HOSE AND FITTINGS. REF: OPERATOR CONTROL NR 96ZZZX2926 AND 96ZZZX2927. 1 H 7 1 3O 3A21 1996061300208 19960613 00208 CE 1996 6 13 96ZZZX2926 1 19960126 A 7331 1200106216 FUEL FLOW LINE CESSNA 210 210L 2073448 CE COCKPIT CHAFED A A FPIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 15 93111 21060266 ON JANUARY 26, 1996, PILOT REPORTED ELECTRICAL FAILURE GLOW BEHIND INSTRUMENT PANEL. MAINTENANCE FOUND TRANSPONDER DIMM ER WIRE SHORTED AGAINST PRESSURE LINE. REPLACED FUEL PRESSURE LINE WITH STRATOFLEX III HOSE AND FITTING. INSPECTIONS O N REMAINING FLEET OF CE210'S RESULTING WITH 75 PERCENT HAVING CHAFED FUEL FLOW LINES. ALL LINES ARE BEING REPLACED WITH STRATOFLEX III HOSE AND FITTINGS. REF: OPERATOR CONTROL NR 96ZZZX2925 AND 96ZZZX2927. 1 H 7 1 3O 3A21 1996061300209 19960613 00209 CE 1996 6 13 96ZZZX2927 1 19960126 A 7331 1200106263 FUEL FLOW LINE CESSNA 210 210L 2073448 CE COCKPIT CHAFED A A FPIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 15 93111 21060266 ON JANUARY 26, 1996, PILOT REPORTED ELECTRICAL FAILURE GLOW BEHIND INSTRUMENT PANEL. MAINTENANCE FOUND TRANSPONDER DIMM ER WIRE SHORTED AGAINST PRESSURE LINE. REPLACED FUEL PRESSURE LINE WITH STRATOFLEX III HOSE AND FITTING. INSPECTIONS O N REMAINING FLEET OF CE210'S RESULTING WITH 75 PERCENT HAVING CHAFED FUEL FLOW LINES. ALL LINES ARE BEING REPLACED WITH STRATOFLEX III HOSE AND FITTINGS. REF: OPERATOR CONTROL NR 96ZZZX2925 AND 96ZZZX2926. 1 H 7 1 3O 3A21 1996061300210 19960613 00210 NM 1996 6 13 96ZZZX2928 1 19960330 A 7110 COWL BOEING 727 72723 1384004 NM NR 1 ENGINE DAMAGED A UHVA O OTHER C F.O.D. AP APPROACH 1 SO 11 1910 19385 AIRCRAFT DESCENDING TO MCO AT 13,000 FEET AND 250 KNOTS. ENTERED SCATTERED HAIL. NO FLAPS DOWN, NO LANDING GEAR DOWN. DAMAGE TO NR 2 ENGINE RING COWL, UPPER 180, LEADING EDGE DAMAGE AND ALL OLD REPAIRS TORN LOOSE, WINDOW SEAL TORN BACK, UPPER BEACON BROKE, RADOME DAMAGE (REPLACED). FLT 72 CAK TO MCO AT 3-30-96 - FERRY ACFT TO MOBILE AEROSPACE FOR REPAIRS . STANDARD SRM REPAIRS WERE ACCOMPLISHED, 111 DISCREPANCIES WERE DISCOVERED TO THE SHEET METAL AND REPAIRS WERE MADE. A IRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A3WE 1996061300211 19960613 00211 EU 1996 6 13 96ZZZX2929 1 19960425 A 3260 82301219 ANGLE ISRAEL 1124 1124 4500102 EU NLG BROKEN A DWHA O OTHER N FALSE WARNING AP APPROACH 1 WP 01 1WS 5199 252 ON APPROACH TO LAND AT VNY, THE GEAR WAS SELECTED DOWN. GEAR LIGHTS INDICATED NOSE GEAR UNSAFE. EMERGENCY PROCEDURES W ERE FOLLOWED, A FLY-BY WAS DONE. THE GEAR APPEARED TO BE DOWN AND LOCKED. A SAFE LANDING WAS MADE. INSPECTION FOUND T HE ANGLE BRACKET THAT SUPPORTED GEAR LIGHT SWITCH WAS BROKEN OFF AT THE BEND. BRACKET WAS REPLACED AND RETREAT CHECKS W ERE GOOD. IT APPEARS THAT NORMAL FATIGUE WAS THE CAUSE OF THE BREAK. THIS IS THE ORIGINAL PART. 2 M 7 2 4F A2SW 1996061300212 19960613 00212 EA 1996 6 13 96ZZZX2930 2 19960312 A 7250 GAS GENERATOR BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA LT ENGINE FAILED A A GPPA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 CE 09 132GP UC110 GG32077 TPA - EN ROUTE IN CRUISE FLIGHT, TWO 'POPS' WERE HEARD, LEFT ENGINE. TORQUE DROPPED, PRESSURES DROPPED, PILOT FEATHERED ENGINE AND SHUT DOWN ENGINE. LANDED TPA. PILOT'S INSPECTION NOTED HOLES IN EXHAUST STACKS AND OIL ALL OVER NACELLE AN D FUSELAGE. AIRCRAFT GROUNDED. 2 L 7 2 4T 4 T RT A24CE E4EA 1996061300214 19960613 00214 SO 1996 6 13 96ZZZX2932 1 19960414 A 2710 12027655007 CABLE ASSY EMB 120 EMB120 3260201 SO LT WS 2902-3678 BROKEN STRANDS A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 203YV 120203 WHILE PERFORMING A 1,600 FLIGHT HOUR CABLE INSPECTION, FOUND LT WING UPPER AILERON CONTROL CABLE WORN AND WITH BROKEN ST RANDS AT LT WS Y2902 AND WS Y3678 WHERE THE CABLE PASSES THROUGH THE INBOARD AND OUTBOARD NACELLE WALLS. 2 L 7 2 4T RT A31SO 1996061300215 19960613 00215 SO 1996 6 13 96ZZZX2933 1 19960422 A 5414 1159P2050498 PANEL GULSTM G1159 G1159A 3970109 SO RT PYLON DEBONDED A BTVA K NONE D INFLIGHT SEPARATION IN INSP/MAINT 1 GL 23 911KT 4890 438 DURING POST-FLIGHT INSPECTION, THE BONDED ALUMINUM OUTER SKIN OF THE RT LOWER PYLON BOARD (ALUMINUM HONEYCOMB BONDED PAN EL) WAS FOUND MISSING. SUBMITTER STATED IT APPEARS A BOND FAILURE AT THE LEADING EDGE OF THE PANEL ALLOWED THE AIRSTREA M TO PEEL THE SKIN FROM THE PANEL. PANEL ASSY IS BEING REPLACED. 2 L 7 2 4F A12EA 1996061300216 19960613 00216 GL 1996 6 13 96ZZZX2934 2 19960423 A 7210 406340104101 SEAL BELL 206 206L4 1182110 SW ALLSN 250C 250C30P 03013 GL ENGINE GEARBOX LEAKING A ALGA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SW 03 177AL 3 52157 CAE895834 DURING FLIGHT, THE TRANSMISSION PRESSURE CAUTION LIGHT ILLUMINATED. THE PRESSURE GAUGE INDICATED 30 PSI. DURING FINAL APPROACH, PRESSURE DROPPED TO 20 PSI AND TO 10 PSI DURING HOVER. UPON LANDING, PRESSURE RETURNED TO 25 PSI. AIRCRAFT W AS INSPECTED AND THE TRANSMISSION OIL LEVEL WAS FOUND LOW. THE ENGINE GEARBOX SEAL WAS DETERMINED TO BE LEAKING. SEALS WERE REPLACED. ENGINE OIL AND EXTERNAL FILTER WERE CHANGED. TRANSMISSION CHIP PLUGS WERE ALSO CHECKED. NO DEFECTS NO TED. 1 G 7 1 3U 3 U NC H2SW E1GL 1996061300220 19960613 00220 1996 6 13 96ZZZX2938 4 19960502 A 2312 RT5000 TRANSCEIVER SNIAS 350 AS350B 8680801 EU COMM DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 22UM 140 1065 SUBMITTER STATED TRANSCEIVER HAS NOT WORKED PROPERLY SINCE NEW. UNIT HAS BEEN REPAIRED NUMEROUS TIMES AND UPDATED WITH SEVERAL MODS. NONE OF THOSE REPAIRS OR MODS HAVE WORKED. 1 G 7 1 3U H9EU 1996061300221 19960613 00221 NM 1996 6 13 96ZZZX2939 1 19960327 A 7720 311671201 THERMOCOUPLE DOUG MD900 MD900 3027375 NM RT ENG NR 2 FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 336 90000012 THERMOCOUPLE FAILED RESISTANCE CHECK. REPLACED WITH NEW 2 EACH UNITS, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1996061300222 19960613 00222 1996 6 13 96ZZZX2940 4 19960323 A 3422 071105200 TRANSMITTER KMT112 BOLKMS 105 BO105S 5626006 EU MAG AZIMUTH DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 722MB 13 48806 S754 NOTED 30 TO 35 DEGREE COMPASS VARIATION DURING FLIGHT. SEEMS TO BE MORE OF AN INTERMITTENT PROBLEM THAN CONSTANT. REPL ACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H3EU 1996061300223 19960613 00223 1996 6 13 96ZZZX2941 4 19960506 A 6113 C25317P SPINNER MTSBSI MU2 MU2B60 5780460 CE LT ENGINE CRACKED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 454MA 967 S941 1535SA SPINNER CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 H 7 2 3T RT A10SW 1996061300224 19960613 00224 WP 1996 6 13 CAL60578 1 19960417 A 5230 59101577 PAN DOUG DC9 DC983 3022083 WP BAG BIN DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14879 29047 49526 HOU - INSPECTION FOUND A 2 INCH CRACK IN PAN AT AFT LATCH OF FORWARD BAG BIN DOOR. A DOUBLER REPAIR WAS INSTALLED IAW E CRA 5210-01251. (X) 2 L 7 2 4F RT A6WE 1996061300225 19960613 00225 NM 1996 6 13 CAL960415 1 19960327 A 3350 FUSE BOEING 757 757224 1384958 NM CABIN BLOWN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 12114 27556 LAX - THE OVERHEAD EMERGENCY LIGHT ABOVE AISLEWAY TO COCKPIT WAS FOUND INOPERATIVE WHEN TESTING EMERGENCY LIGHTS. MAINT ENANCE FOUND THE FUSE IN CHARGER POWER PACK BLOWN. THE FUSE WAS REPLACED AND OPERATION OF THE LIGHT WAS RESTORED. (X) 2 L 7 2 4F RT A2NM 1996061300226 19960613 00226 NM 1996 6 13 CAL960502 1 19960419 A 3350 LIGHT BOEING 737 7372C0 1384488 NM R2 DOOR SLIDE INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 10242 20071 GSO - 42 DOOR SLIDE LIGHT BATTERY CHECKS BAD - ZERO VOLTS. REPLACED R2 DOOR SLIDE BATTERY PACK. OPS CHECK GOOD IAW B73 7MM 33-52-63. (X) 2 L 7 2 4F A16WE 1996061300227 19960613 00227 NM 1996 6 13 CAL960503 1 19960419 A 3350 LIGHT BOEING 737 7372C0 1384488 NM L1 DOOR INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 10242 20071 GSO - L1 DOOR SLIDE LIGHT BATTERY CHECKS BAD - ZERO VOLTS. REMOVED AND REPLACED L1 DOOR EVAC SLIDE LIGHT BATTERY PACK A SSY, OPS CHECK GOOD IAW B737 MM 33-51-63. (X) 2 L 7 2 4F A16WE 1996061300228 19960613 00228 NM 1996 6 13 CAL960504 1 19960419 A 3350 BATTERY PACK BOEING 737 7372C0 1384488 NM R1 DOOR SLIDE DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 10242 20071 GSO - R1 DOOR SLIDE LIGHT BATTERY CHECK BAD - LOW VOLTAGE. REPLACED R1 DOOR SLIDE LIGHT BATTERY PACK, OPS CHECK GOOD IA W B737 MX MAN 33-51-63. (X) 2 L 7 2 4F A16WE 1996061300229 19960613 00229 NM 1996 6 13 CAL960529 1 19960425 A 5330 SKIN BOEING 737 737130 1384435 NM BS 192 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16201 65841 19018 GSO - REMOVED DAMAGE AREA AND FABRICATED DOUBLER, INSTALLED DOUBLER AT STRINGER 20R - STATION 192 PER SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1996061300230 19960613 00230 NM 1996 6 13 CAL960555 1 19960504 A 2750 696670835 FOLLOW-UP CABLES BOEING 727 727232 1384082 NM LT TE FLAP BROKEN A A CALA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SW 09 33785 20640 EWR - FLT 0654 - AIRCRAFT REQUIRED 25-30 UNITS RIGHT AILERON TO MAINTAIN LEVEL FLIGHT WHILE ON FINAL APPROACH TO EWR. T HE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LT INBD T/E FLAP FOLLOW-UP CABLES BROKEN WITH RESULTANT DAMAGE T O THE MID-FLAP. THE MID-FLAP AND FOLLOW-UP CABLES WERE REMOVED AND REPLACED. AN ADJUSTMENT TEST OF THE INBOARD MID-FLA P WAS PERFORMED IAW MM 27-51-1, PAGES 409-415. THE FLAPS WERE CYCLED SEVERAL TIMES WITH OPERATION CHECKING GOOD. (X) 2 L 7 3 4F A3WE 1996061300231 19960613 00231 WP 1996 6 13 CAL960569 1 19960502 A 5720 5936838503 SUPPORT DOUG DC9 DC983 3022083 WP WS 91.1547 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14879 29047 49526 HOU - INSPECTION FOUND A 2 INCH CRACK IN UPPER AFT LEG OF LEFT WING CROSS BRACE SUPPORT. THE CRACKED SECTION WAS REMOVE D AND A NEW SECTION WAS SPLICED IN IAW ECRA 5710-01727 AND SRM 51-30-5. (M) 2 L 7 2 4F RT A6WE 1996061300232 19960613 00232 WP 1996 6 13 CAL960570 1 19960423 A 5210 WEB DOUG DC9 DC983 3022083 WP CABIN DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14879 29047 49526 HOU - INSPECTION FOUND A 1.5 INCH CRACK IN MAIN CABIN DOOR WEB BELOW HOLD OPEN HOOK MECHANISM. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 1996061300233 19960613 00233 WP 1996 6 13 CAL960571 1 19960417 A 5230 59101575 WEB DOUG DC9 DC983 3022083 WP BAG BIN DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14879 29047 49526 HOU - INSPECTION FOUND A 2 INCH CRACK IN AFT BAG BIN DOOR WEB AT AFT LATCH. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 52-05. (M) 2 L 7 2 4F RT A6WE 1996061300234 19960613 00234 WP 1996 6 13 CAL960572 1 19960423 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14879 29047 49526 HOU - INSPECTION FOUND A DENT IN FUSELAGE SKIN SIX INCHES AFT AND SIX INCHES ABOVE LEFT AOA VANE. THE SKIN WAS REPAIRED IAW SRM 53-04, FIGURE 38. (M) 2 L 7 2 4F RT A6WE 1996061300235 19960613 00235 WP 1996 6 13 CAL960573 1 19960423 A 5230 DOUBLER DOUG DC9 DC983 3022083 WP BAG BIN DOOR GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14879 29047 49526 HOU - INSPECTION FOUND AFT BAG BIN DOOR DOUBLER GOUGED AT FORWARD LATCH. THE DOUBLER WAS REPLACED PER SRM 52-05, FIGURE 26A. (M) 2 L 7 2 4F RT A6WE 1996061300236 19960613 00236 WP 1996 6 13 CAL960574 1 19960418 A 5320 ANGLE DOUG DC9 DC983 3022083 WP BS 160 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14879 29047 49526 HOU - INSPECTION FOUND FLOOR SUPPORT Z-ANGLE CORRODED AFT OF G-1 GALLEY DRAIN PORT AT STATION 160. THE FLOOR SUPPORT AN GLE WAS REMOVED AND REPLACED IAW SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 1996061300237 19960613 00237 WP 1996 6 13 CAL960575 1 19960419 A 5210 591412161N PAN DOUG DC9 DC983 3022083 WP CABIN DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14879 29047 49526 HOU - INSPECTION FOUND A 2 INCH CRACK JUST ABOVE FORWARD LOWER DOOR STOP OF MAIN CABIN DOOR PAN. THE PAN SECTION WAS RE PLACED IAW SRM 51-30-1, 51-30-2, AND 51-30-4. (M) 2 L 7 2 4F RT A6WE 1996061300238 19960613 00238 WP 1996 6 13 CAL960576 1 19960416 A 5210 INTERCOSTAL DOUG DC9 DC983 3022083 WP CABIN DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14879 29047 49526 HOU - INSPECTION FOUND A 1.25 INCH CRACK IN VERTICAL CHANNEL (INTERCOSTAL) AFT OF DOOR HANDLE SHAFT. THE INTERCOSTAL WA S REPLACED IAW SRM 51-30-2 AND 51-30-5. (M) 2 L 7 2 4F RT A6WE 1996061300239 19960613 00239 WP 1996 6 13 CAL960577 1 19960417 A 5315 FLOORBEAM DOUG DC9 DC983 3022083 WP CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14879 29047 49526 HOU - INSPECTION FOUND CORROSION ON FLOORBEAM BEHIND HOSTESS SEAT AT FORWARD ENTRY AREA. A NEW FLOORBEAM WAS FABRICATED AND INSTALLED IAW SRM 51-30-3. (M) 2 L 7 2 4F RT A6WE 1996061300240 19960613 00240 WP 1996 6 13 CAL960579 1 19960418 A 5320 99363685NC ANGLE DOUG DC9 DC983 3022083 WP BS 946 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14879 29047 49526 HOU - INSPECTION FOUND A .375 INCH CRACK IN KEEL BEAM INTERNAL ANGLE AT STATION 946, SIX INCHES LEFT OF CENTER LINE. TH E AREA WAS REPAIRED IAW SRM 51-30-2 AND 51-30-5. (M) 2 L 7 2 4F RT A6WE 1996061300241 19960613 00241 1996 6 13 CAL960592 4 19960512 A 2565 14611004 SLIDE BOEING 727 727227 1384078 NM PASSENGER DOOR LOW PRESSURE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 74172 2087 21248 LAX - FLT 1840 - INSPECTION FOUND THE AFT RT DOOR SLIDE BOTTLE PRESSURE READING ZERO. THE ESCAPE SLIDE WAS REMOVED AND REPLACED. (X) 2 L 7 3 4F A3WE 1996061300242 19960613 00242 NM 1996 6 13 CAL960600 1 19960502 A 3350 BATTERY PACK BOEING 737 737291 138448W NM PASSENGER DOOR DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 10251 20361 GSO - THE AFT LT ENTRY DOOR SLIDE LIGHT HAD NO VOLTAGE AT TEST JACK WITH LANYARD PULLED AND LIGHTS ON. THE DOOR SLIDE L IGHT BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-63. (X) 2 L 7 2 4F A16WE 1996061300243 19960613 00243 NM 1996 6 13 CAL960601 1 19960502 A 3350 BATTERY PACK BOEING 737 737291 138448W NM SERVICE DOOR DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 10251 20361 GSO - THE FORWARD RT SERVICE DOOR SLIDE LIGHT HAD NO VOTLAGE AT TEST JACK WITH LANYARD PULLED. THE DOOR SLIDE LIGHT BAT TERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-63. (X) 2 L 7 2 4F A16WE 1996061300244 19960613 00244 NM 1996 6 13 CAL960602 1 19960502 A 3350 BATTERY PACK BOEING 737 737291 138448W NM SERVICE DOOR DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 10251 20361 GSO - THE AFT RT SERVICE DOOR SLIDE LIGHT HAD NO VOLTAGE AT TEST JACK WITH LANYARD PULLED. THE DOOR SLIDE LIGHT BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-63. (X) 2 L 7 2 4F A16WE 1996061300245 19960613 00245 WP 1996 6 13 CAL960610 1 19960514 A 3350 41B004AD073 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 43537 47112 CLE - FLT 1144 - THE COCKPIT EMERGENCY LIGHTS WERE FOUND INOPERATIVE. THE POWER SUPPLY BATTERIES WERE FOUND AT FAULT. T HE NICAD BATTERIES IN POWER SUPPLY WERE REPLACED. (X) 2 L 7 2 4F A6WE 1996061300246 19960613 00246 NM 1996 6 13 CAL960611 1 19960418 A 5330 SKIN BOEING 737 737130 1384435 NM BS 360-450 DISBONDING A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14206 67326 19023 GSO - INSPECTION FOUND SKIN PANEL DISBONDING FROM BS 360R TO BS 450R, STR 19R - STR 26R. THE SKIN PANEL WAS REMOVED AND A NEW SKIN AND SPLICE STRAP WERE FABRICATED AND INSTALLED IAW SRM 51-10-2, SRM 51-30-2, AND BOEING DRAWING 67-45768-127 . (X) 2 L 7 2 4F A16WE 1996061300247 19960613 00247 NM 1996 6 13 CAL960612 1 19960417 A 5230 SKIN BOEING 737 737130 1384435 NM C-1 DOOR CREASED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14206 67326 19023 GSO - INSPECTION FOUND SEVERAL CREASES IN LOWER HALF OF C-1 DOOR SKIN PANEL. THE DAMAGED SECTION OF SKIN WAS CUT OUT, A SKIN FILLER AND DOUBLER SPLICE PLATE WERE FABRICATED AND INSTALLED IAW SRM'S 52-30-2, 53-30-3, 51-10-2, AND 51-30-2. ( X) 2 L 7 2 4F A16WE 1996061300248 19960613 00248 NM 1996 6 13 CAL960613 1 19960414 A 5230 SKIN BOEING 737 737130 1384435 NM C-2 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14206 67326 19023 GSO - INSPECTION FOUND AFT EDGE OF C-2 DOOR SKIN BUCKLED AND CRACKED IN TWO PLACES. THE CRACKS WERE .75 INCH LONG. THE DAMAGED AREA WAS CUT OUT. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 52-00-03. (X) 2 L 7 2 4F A16WE 1996061300249 19960613 00249 WP 1996 6 13 CAL960614 1 19960422 A 5320 ADJ70255 CHANNEL DOUG DC10 DC1030 3023501 WP CARGO COMPT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15069 71499 46584 KUL - INSPECTION FOUND FORWARD CARGO COMPARTMENT CHANNEL PUNCTURED AND CORRODED. THE CHANNEL WAS REPAIRED IAW ECRA 5340 -01268. (X) 2 L 7 3 4F A22WE 1996061300250 19960613 00250 NM 1996 6 13 CAL960616 1 19960515 A 3350 BATTERY PACK BOEING 737 737247 138448D NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14246 20129 MCO - FLT 8 - THE EMERGENCY LIGHTS AT RT OVERWING EXIT WERE FOUND INOPERATIVE DURING TEST. THE BATTERY PACK WAS REPLACE D IAW MM 33-51-121 AND MM 33-51-71, AND OPERATION OF THE LIGHTS WAS RESTORED. (X) 2 L 7 2 4F A16WE 1996061300251 19960613 00251 NM 1996 6 13 MZZA96018 1 19960404 A 2612 FIRE DETECTOR BOEING 727 727224 1384076 NM APU MALFUNCTIONED A MZZA F ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 WP 13 642DH 20709 MNL - FLT 877 - AFTER CREW STARTED ALL ENGINES AND TAXIED OUT AND APPROXIMATELY 2 MINUTES AFTER APU SHUT DOWN, APU FIRE WARNING LIGHT AND BELL CAME ON. PULLED APU FIRE HANDLE AND DISCHARGED APU FIRE BOTTLE. AFTER APPROXIMATELY 4 TO 5 MINU TES, THE LIGHT WENT OUT. AFTER ENGINE SHUT DOWN, LIGHT AND BELL WENT OFF ON ITS OWN WITH NO FIRE NOTICED IN THE BAY ARE A. MAINTENANCE INSPECTED APU WITH NO EVIDENCE OF FIRE, CHECKED FIRE DETECTION LOOPS, CLEANED CONNECTORS, AND PEFORMED A PU FIRE TEST, ALL FOUND TO BE NORMAL. RAN APU AND CANNOT DUPLICATE PROBLEM. APU PLACARDED INOPERATIVE PER MEL AND AIRC RAFT DISPATCHED. (X) 2 L 7 3 4F A3WE 1996061300252 19960613 00252 NE 1996 6 13 MZZA96035 2 19960504 A 7261 OIL FILTER STUD BOEING 727 7272F9 138407D NM PWA JT8 JT8D17 52049 NE NR 2 ENGINE PULLED LOOSE A MZZA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 13 75429 21427 GUM - FLT F-925 - AFTER TAKEOFF ON CLIMB-OUT, LOST OIL QUANTITY AND PRESSURE ON NR 2 ENGINE. CREW PRECAUTIONARY SHUT DO WN NR 2 ENGINE AND RETURNED BACK TO GUAM. MAINTENANCE FOUND NR 2 ENGINE MAIN OIL SCREEN COVER PLATE UPPER RIGHT STUD PU LLED OUT OF HELICOIL. MECHANIC REPLACED HELICOIL, STUD, AND MAIN OIL SCREEN. ALSO, PRECAUTIONARY REPLACED OIL PRESSURE TRANSMITTER. NR 2 ENGINE OIL LEAK CHECK AND SYSTEM CHECK GOOD ON ENGINE RUN-UP. (X) 2 L 7 3 4F 4 F RT A3WE E2EA 1996061300254 19960613 00254 SO 1996 6 13 RAAAE895010 1 19960503 A 3350 8621006 BATTERY PACK 873100212 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 SEAT ROW 15 EGRESS FLOOR PROXIMITY LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. (X) 2 L 7 4 4T 4A22 1996061300255 19960613 00255 SO 1996 6 13 RAAAE896001 1 19960106 A 3350 8621006 BATTERY PACK 873100212 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 SEAT ROW 7 EGRESS FLOOR PROXIMITY LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. (X) 2 L 7 4 4T 4A22 1996061300256 19960613 00256 SO 1996 6 13 RAAAE896002 1 19960106 A 3350 8621006 BATTERY PACK 873100212 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 SEAT ROW 15 EGRESS FLOOR PROXIMITY LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. (X) 2 L 7 4 4T 4A22 1996061300266 19960613 00266 SO 1996 6 13 RAAAE996001 1 19960114 A 3350 8621006 BATTERY PACK 873100112 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 EGRESS FLOOR PROXIMITY LIGHT PASSENGER ROW 2 FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. (X) 2 L 7 4 4T 4A22 1996061300267 19960613 00267 SO 1996 6 13 RAAAE996002 1 19960114 A 3350 8621014 BATTERY PACK 873100112 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 LEFT FORWARD OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. REPLACED BATTERY PACK DUE TO LOW CHA RGE. (X) 2 L 7 4 4T 4A22 1996061300268 19960613 00268 EU 1996 6 13 SABA9600012 1 19960322 A 7330 FUEL FILTER IND STBROS SD3 SD360 8100606 EU LT ENGINE ILLUMINATED A SABA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 33 729PC SH3729 CLT/PGV - FLT 5248 - FLIGHT WAS APPROXIMATELY 46 MILES OUT OF CLT WHEN THE LEFT FUEL FILTER CAUTION LIGHT ILLUMINATED DI MLY. THE CAPTAIN CALLED MAINTENANCE CONTROL WITH THE PROBLEM AND HE WAS TOLD TO RETURN TO CLT. UPON THE AIRCRAFT'S RET URN TO CLT, MAINTENANCE PERSONNEL WERE DISPATCHED TO TROUBLESHOOT PROBLEM. LEFT ENGINE FUEL FILTER ELEMENT WAS REMOVED AND INSPECTED FOR CONTAMINATION AND THE FILTER ELEMENT WAS THEN REPLACED AS A PRECAUTIONARY MEASURE. THIS DID NOT FIX T HE INDICATION PROBLEM AND THE INDICATION SYSTEM WAS THEN DEFERRED TO THE MSL PER MEL 28-3 UNDER CONTROL NR 0322-10C. TH E AIRCRAFT WAS THEN RETURNED TO SERVICE. (X) 2 H 7 2 4T A41EU 1996061300269 19960613 00269 NM 1996 6 13 TWRA9622 1 19960413 A 3350 900835A BATTERY PACK BOEING 747 747212B 1384886 NM CABIN DISCHARGED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 620FF 21162 LEFT AND RIGHT SIDE, TWO EMERGENCY EXTERIOR LIGHTS INOPERATIVE. RIGHT SIDE, REPAIRED WIRE AT BATTERY PACK. LEFT SIDE, REPLACED BATTERY PACK. OPS CHECK OK. MM 33-51-00. (X) 2 L 7 4 4F A20WE 1996061300270 19960613 00270 NM 1996 6 13 WRLA96023 1 19960519 A 2822 608432M FUEL PUMP DOUG MD11 MD11 3023602 NM NR 1-3 FUEL TANK LEAKING A WRLA O OTHER K FLUID LOSS LD LANDING 1 EA 27 280WA 48458 AIRCRAFT SUSTAINED A 'HARD-LANDING' WRSJ. DURING MM REQUIRED INSPECTION, FUEL LEAK NOTED AT FUEL BOOST AND TRANSFER PUM PS (4 EACH) ON NR 1 AND NR 3 FUEL TANKS. ALSO, MINOR SKIN WRINKLING NOTED AT BULKHEAD STA 595. AIRCRAFT INSPECTED, AND DAMAGE REPORT FORWARDED TO MCDONNELL DOUGLAS PRODUCT SUPPORT FOR EVALUATION. PER MDC, ACFT FERRIED (UNPRESSURIZED AND GEAR DOWN) TO WIIH FOR REPAIR. MDC STRUCTURAL ENGINEERING EVALUATED AIRCRAFT & DETERMINED THAT STRUCTURAL DAMAGE TO BUL KHEAD 595 WAS NOT SIGNIFICANT & REQUIRED NO REPAIR ACTION. FUEL LEAKS DETERMINED TO BE SEALANT DAMAGE AT FUEL & BOOST P UMP HOUSING/SPAR FAYING SURFACES. BOOST & TRANSFER PUMP HOUSINGS RESEALED. LEAK CHK OK. ACFT RETURNED TO SERVICE.(X) 2 L 7 3 4F RT A22WE 1996061300271 19960613 00271 NM 1996 6 13 WRLA96024 1 19960522 A 2612 61054401 FIRE LOOP DOUG MD11 MD11 3023602 NM NR 1 ENGINE FAILED A WRLA F E ACTIVATE FIRE EXT. ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 EA 27 272WA 48437 DURING INITIAL DESCENT, FLIGHT CREW RECEIVED 'FIRE WARNING' INDICATION ON NR 1 ENGINE. FLIGHT CREW PERFORMED ABNORMAL P ROCEDURES: SHUT DOWN NR 1 ENGINE, DISCHARGED NR 1 FIRE BOTTLE. AT THAT TIME, FIRE WARNING INDICATION EXTINGUISHED. AC FT LANDED WITHOUT FURTHER INCIDENT. ACFT WAS INSPECTED, AND NO EVIDENCE OF FIRE NOTED. CFDS REVIEWED AND NR 1 ENG A-LO OP WITH B-LOOP INOP WOULD CAUSE 'FIRE WARNING' INDICATION. REPLACED 'A' RT REVERSER COWL FIRE LOOP, CLEARING FAULT ON A -LOOP. ADDITIONALLY, CLEARED FAULTS ON B-LOOP BY REPLACING RT REVERSER COWL LOOP AND B-LOOP PYLON HARNESS. BOTH SYSTEM S OPS CHK NORMAL DURING GROUND RUNS. ACFT RETURNED TO SERVICE. (X) 2 L 7 3 4F RT A22WE 1996061300272 19960613 00272 WP 1996 6 13 9612389883 1 19960607 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 671NC 47660 DURING LINE MAINTENANCE, THE EMERGENCY LIGHTS AT ROWS 5 THROUGH 10 INOPERATIVE. REPLACED POWER SUPPLY UNIT, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996061300273 19960613 00273 WP 1996 6 13 9612399860 1 19960606 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 769NC 47757 DURING LINE MAINTENANCE, FOUND LEFT AFT CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK OK . 2 L 7 2 4F A6WE 1996061300274 19960613 00274 NE 1996 6 13 9612405525 2 19960605 A 7323 PMA BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE NR 1 ENGINE MALFUNCTIONED A NWAA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 01 525US 23619 716460 DURING CLIMB, THE NR 1 ENGINE OPERATING PARAMETERS BECAME ERRATIC. AIRCRAFT RETURNED TO SFO AND LANDED WITHOUT FURTHER EVENT. GROUND MAINTENANCE FOUND THE PERMANENT MAGNET ALTERNATOR HAD FAILED DUE TO A LOOSE PMA ROTOR SHAFT IN THE GEAR B OX. MAIN GEAR BOX AND PMA WERE REPLACED. AIRCRAFT WAS GROUND RUN AND FOUND SERVICEABLE. 2 L 7 2 4F 4 F RT A2NM E17NE 1996061300275 19960613 00275 NM 1996 6 13 9612416310 1 19960607 A 2612 FIRE WARNING BOEING 747 747451 1384940 NM APU ACTIVATED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 670US 24225 DURING TAKEOFF, THE APU FIRE WARNING ACTIVATED AT 50 TO 60 KNOTS. ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACED T HE AUTOMATIC FIRE OVERHEAT LOGIC TEST SYSTEM AND RELAY R7692, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1996061300276 19960613 00276 EU 1996 6 13 9612423203 1 19960607 A 3397 WIRE AIRBUS 320 A320211 3930320 EU CABIN DAMAGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 303US 34 DURING LINE MAINTENANCE, FOUND THE EMERGENCY PATH LIGHTS AT ROWS 17 AND 18 INOPERATIVE. REPLACED PIN AT PLUG-TO-SIDEWAL L DISCONNECT AND REPAIRED WIRE, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996061300277 19960613 00277 EU 1996 6 13 9612433231 1 19960609 A 3350 321454 BATTERY PACK AIRBUS 320 A320211 3930320 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 331NW 318 DURING LINE MAINTENANCE, THE EMERGENCY LIGHTS TEST FAULTED INT LOADS L, EXT LOADS FWD L, BATTERY FWD L AND UNIT FWD L. R EPLACED POWER SUPPLY AND BATTERY PACK, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996061300278 19960613 00278 EU 1996 6 13 9612443237 1 19960609 A 3010 SEAL AIRBUS 320 A320211 3930320 EU NR 1 ENG PYLON LEAKING A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 337NW 358 DURING CLIMBOUT, RECEIVED AIR L WING LEAK, FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND MESSAGE CLEARED IMMEDIATELY. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE ANTI-ICE DUCT SLIP JOINT SEALS IN THE LEADING EDGE OF NR 1 ENGINE PYLON, LEAK AND OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996061300279 19960613 00279 NE 1996 6 13 9612459301 2 19960608 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE NR 1 FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 301RC 48054 709916 DURING TAKEOFF, THE NR 1 ENGINE EGT REACHED 800 DEGREES. TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE WITH OUT FURTHER EVENT. MAINTENANCE PERSONNEL FOUND METAL IN THE TAILPIPE. THE ENGINE WAS REMOVED AND REPLACED. 2 L 7 2 4F 4 F A6WE E9NE 1996061300280 19960613 00280 EU 1996 6 13 9612463246 1 19960606 A 2560 SLIDE COVER AIRBUS 320 A320211 3930320 EU LT EMER EXIT DR FELL OFF A NWAA C ABORTED TAKEOFF J WARNING INDICATION IN INSP/MAINT 1 GL 01 346NW 400 DURING TAKEOFF AT 60 KNOTS, THE LEFT AFT EMERGENCY EXIT DOOR WARNING LIGHT ILLUMINATED. ABORTED THE TAKEOFF WITHOUT FUR THER INCIDENT. REINSTALLED THE SLIDE ACCESS COVER. 2 L 7 2 4F RT A28NM 1996061300281 19960613 00281 1996 6 13 ARWA9606001 4 19960531 A 3422 258733511 VERT GYRO DOUG DC8 DC862 3021970 WP E/E COMP FAILED A A ARWA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 19 810BN 45905 AFTER TAKEOFF, CAPT'S ADI INDICATED 15 TO 20 DEGREE BANK IN LEVEL FLIGHT AND INDICATED PITCH 20 DEGREES NOSE-UP IN FLIGH T LEVEL TURN. AIRCRAFT RETURNED TO MIAMI. REMOVED AND REPLACED CAPT'S VERTICAL GYRO, OPS CHECKED NORMAL IAW DAC MM 34- 25-00. 2 L 7 4 4F 4A25 1996061300282 19960613 00282 WP 1996 6 13 CALA9600769 1 19960607 A 3230 PUSHROD DOUG DC9 DC932 3022066 WP NLG GRD SENSE BENT A CALA O OTHER J WARNING INDICATION TO TAKEOFF 1 SW 09 14524 47539 THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE FLIGHT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND PUSHROD AT GROUND SENSE SECTOR BENT. THE PUSHROD WAS REMOVED AND REPLACED. THE NLG GROUND SENSE WAS TESTED IAW MM 32-23-1, PA GE 204A. THE LANDING GEAR WAS SWUNG SEVERAL TIMES AND OPERATION CHECKED GOOD. 2 L 7 2 4F A6WE 1996061300283 19960613 00283 WP 1996 6 13 CALA9600770 1 19960608 A 2910 7936913518 HYD LINE DOUG DC9 DC982 3022082 WP NOSE GEAR LEAKING A A CALA O OTHER J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SW 09 16887 49116 THE RIGHT HYDRAULIC SYSTEM PRESSURE AND QUANTITY DROPPED TO ZERO WHILE EN ROUTE. EMERGENCY GEAR EXTENSION WAS USED PRIO R TO LANDING. THE LT MLG DOOR WAS DAMAGED UPON LANDING AT EWR. MAINTENANCE FOUND THE HYDRAULIC LINE FOR NOSE GEAR UP L EAKING AND THE LINE WAS REPLACED. THE LT MLG DOOR WAS REMOVED AND REPLACED. THE DOOR FORWARD GAP SEAL WAS FILLED IAW E CRA 5280-01136. A DIP WAS ISSUED TO REINSPECT THE SEAL AT 1100 FLIGHT HOUR INTERVALS AND TO REPAIR AT THE NEXT QUARTER- D, HALF-D, OR FULL-D CHECK, WHICHEVER COMES FIRST. A GEAR SWING WAS PERFORMED AND OPERATION CHECKED GOOD. 2 L 7 2 4F A6WE 1996061300284 19960613 00284 WP 1996 6 13 CALA9600771 1 19960609 A 2612 87858201 CONNECTORS DOUG DC9 DC982 3022082 WP NR 1 ENGINE INOPERATIVE A CALA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 09 809NY 49263 THE NR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED WHILE EN ROUTE. THE THROTTLE WAS RETARDED AND THE LIGHT EXTINGUISHED, TH E LIGHT CAME BACK ON DURING APPROACH TO CLE. THE NR 1 ENGINE WAS SHUT DOWN AND THE FIRE BOTTLE WAS DISCHARGED AS A PREC AUTIONARY MEASURE. THE AIRCRAFT LANDED WITHOUT INCIDENT. TWO LOOP CONNECTORS ON LOWER A-LOOP OF NR 1 ENGINE WERE FOUND AT FAULT. THE LOOP CONNECTORS WERE REMOVED AND REPLACED. IN ADDITION, THE FIRE DETECTION UNIT AND A AND B LOOP SWITCH ES WERE REPLACED AS A PRECAUTIONARY MEASURE. ALSO, THE FIRE BOTTLE WAS REPLACED. THE FIRE DETECTION SYSTEM TESTED NORM ALLY. 2 L 7 2 4F A6WE 1996061300285 19960613 00285 NM 1996 6 13 CALA9600772 1 19960608 A 5330 SKIN BOEING 727 727243 138408D NM BS 196/211.5 PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 578PE 21661 INSPECTION FOUND TWO SMALL HOLES IN FUSELAGE SKIN DUE TO GROUND DAMAGE AT STA 196 AND 211.5, RT SIDE. AN INTERIM REPAIR WAS INSTALLED IAW SRM 53-30-3, FIGURE 1, PAGE 5. A DIP WAS ISSUED TO INSPECT REPAIR EVERY 3,000 FLIGHTS AND TO PERFORM A PERMANENT REPAIR AT NEXT FULL D-CHECK, NOT TO EXCEED 10,000 CYCLES. 2 L 7 3 4F RT A3WE 1996061300286 19960613 00286 SO 1996 6 13 COMA9610169 1 19960607 A 2722 12048563001 ECCENTRIC SHAFT EMB 120 EMB120RT SO RUDDER SHEARED A A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 259CA 120252 DURING C-1 INSPECTION, FOUND RUDDER ECCENTRIC SHAFT TO BE SHEARED JUST ABOVE SPLINED SHAFT. INSTALLED SERVICEABLE (P/N 120-48563-001) AND RETURNED AIRCRAFT TO SERVICE. ECCENTRIC SHAFT AND FAIL-SAFE PIN SENT TO EMBRAER FOR ANALYSIS. 2 L 7 2 4T RT A31SO 1996061300287 19960613 00287 NE 1996 6 13 COMA9610170 2 19960608 A 7230 COMPRESSOR EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE DAMAGED A COMA K NONE C F.O.D. IN INSP/MAINT 1 SO 01 265CA 120257 115522 LEFT ENGINE HAS FOD DAMAGE ON COMPRESSOR BLADES. REPLACED ENGINE. 2 L 7 2 4T 4 T RT A31SO E20NE 1996061300288 19960613 00288 SO 1996 6 13 COMA9610171 1 19960608 A 3620 M1160140242 OVERHEAT SWITCH EMB 120 EMB120RT SO RT WING DEFECTIVE A COMA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 SO 01 255CA 120238 RT BLEED AIR DUCT OVERHEAT WARNING CAME ON DURING FLIGHT. REPLACED DEFECTIVE DUCT OVERHEAT SWITCH. 2 L 7 2 4T RT A31SO 1996061300289 19960613 00289 SO 1996 6 13 COMA9610172 1 19960607 A 7603 0881824 SOLENOID EMB 120 EMB120RT SO RT ENGINE SHORTED A COMA K NONE O OTHER CR CRUISE 1 SO 01 1110J 120110 FLIGHT IDLE STOP SOLENOID CIRCUIT BREAKER TRIPPED, WOULD NOT RESET. REPLACED THE FLIGHT IDLE SOLENOID. 2 L 7 2 4T RT A31SO 1996061300290 19960613 00290 EU 1996 6 13 COMA9630121 1 19960608 A 2731 DL3827M157 TRIM ACTUATOR SAAB SF340 SF340A 7850100 EU LT ELEVATOR FAILED A COMA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 361CA 340A056 MAIN PITCH TRIM IS INOP. REPLACED THE TRIM ACTUATOR. 2 L 7 2 4T RT A52EU 1996061300291 19960613 00291 EU 1996 6 13 COMA9630122 1 19960607 A 2910 9302631001 HYDRAULIC LINE SAAB SF340 SF340A 7850100 EU NLG FAILED A COMA H L DEACTIVATE SYST/CIRCUITS ABORTED APPROACH K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 140N 340A140 LOST ALL HYDRAULIC FLUID DURING FLIGHT. LANDING GEAR AND FLAPS LOWERED WITH HAND PUMP. REPLACED FAILED HYDRAULIC LINE FROM SYSTEM PUMP TO FILTER. 2 L 7 2 4T RT A52EU 1996061300292 19960613 00292 EU 1996 6 13 COMA9630123 1 19960607 A 3350 3071BPEGPL BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 158CA 340A158 EMERGENCY FLOOR LIGHTING AT MAIN CABIN DOOR IS INOP. REPLACED LIGHT BULB, ALL LIGHTING OPERATIVE. 2 L 7 2 4T RT A52EU 1996061300293 19960613 00293 EA 1996 6 13 COMA9660102 1 19960608 A 2750 601R571161 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA RT TE FLAPS DEFECTIVE A COMA K NONE O OTHER AP APPROACH 1 SO 01 920CA 7022 FLAPS FAILED AT 20 DEGREES WHEN SELECTED DOWN DURING APPROACH. REPLACED THE RT WING FLAP SYSTEM WIRING HARNESS. 2 L 7 2 4F RT A21EA 1996061300294 19960613 00294 EA 1996 6 13 COMA9660103 1 19960607 A 2750 601R571161 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA RT TE FLAP DEFECTIVE A COMA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 SO 01 945CA 7069 FLAPS FAILED AFTER TAKEOFF. REPLACED THE RT WING FLAP SYSTEM WIRING HARNESS. 2 L 7 2 4F RT A21EA 1996061300295 19960613 00295 NM 1996 6 13 DL72S961370 1 19960529 A 5315 FLOOR BEAM BOEING 727 727232 1384082 NM BS 1070 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 416DA 21258 FOUND CORROSION 0N TOP OF FLOOR BEAM AT STA 1070, RBL 44 TO RBL 58. REPAIRED PER M/M 53-20-11 FIG 804A. 2 L 7 3 4F A3WE 1996061300296 19960613 00296 NM 1996 6 13 DL72S961371 1 19960529 A 5315 FLOOR BEAM BOEING 727 727232 1384082 NM BS 1030 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 416DA 21258 FOUND CORROSION ON FLOOR BEAM, STA 1030 UPPER FLANGE FASTENER HOLES AT LBL 0 AND LBL 9. REPAIRED PER M/M 53-20-11 PG 81 1B. 2 L 7 3 4F A3WE 1996061300297 19960613 00297 NM 1996 6 13 DL733961361 1 19960604 A 5620 PA65457914AR WINDOW BOEING 737 737347 1384647 NM CABIN CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 306WA 23347 SEAT 10A PSGR CABIN WINDOW HAS SEVERAL CIRCULAR CRACKS ON OUTER WINDOW. WINDOW CRACKED AT SEAT 10F DURING PRESSURE CK F OR BROKEN WINDOW AT 10A. CABIN WAS PRESSURIZED TO 4.2 PSI, CABIN RATE OF CLIMB UP AND DOWN NEVER EXCEEDED 1,000 FPM. 2 L 7 2 4F RT A16WE 1996061300298 19960613 00298 1996 6 13 DL73E961345 4 19960602 A 3417 HG480B42 AIR DATA COMP BOEING 737 737247 138448D NM NR 2 INOPERATIVE A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 379DL 23606 ON TAKEOFF ROLL, F/O'S AIRSPEED VSI AND ALTIMETER OFF FLAGS CAME ON, RETURNED TO THE GATE. C/A INSTALLED NEW NR 2 ADC, ALL INDICATIONS ARE NORMAL. 2 L 7 2 4F A16WE 1996061300299 19960613 00299 NM 1996 6 13 DL73E961346 1 19960602 A 2130 DUCT BOEING 737 737247 138448D NM LT AMC RUPTURED A DALA D RETURN TO BLOCK O OTHER CL CLIMB 1 SO 27 237WA 23185 AFTER T/O, A/C WOULD NOT PRESSURIZE, MAIN AND FWD OUTFLOW VALVES CLOSED AND GOOD DUCT PRESSURE. FOUND COMPRESSOR OUTLET DUCT FOR LEFT AMC RUPTURED. 2 L 7 2 4F A16WE 1996061300300 19960613 00300 NM 1996 6 13 DL73S961364 1 19960605 A 2782 654465116 ACTUATOR BOEING 737 737232 1384475 NM NR 4 SLAT FAILED A DALA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 SO 27 312DL 18949 23084 NR 4 SLAT ACTUATOR FAILED TO EXTEND ON APPROACH. REPLACED NR 4 SLAT ACTUATOR, CHECKS OK. 2 L 7 2 4F RT A16WE 1996061300301 19960613 00301 NM 1996 6 13 DLM88961343 1 19960602 A 3320 LIGHT BALLAST DOUG MD88 MD88 3023688 NM CABIN SHORTED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 949DL 49880 BURNING SMELL AND SMOKE COMING FROM AREA OF ROW 26. OVERHEAD LIGHTS FLICKERING AT ROW 26 AT THE SAME TIME SMELL OCCURED . DEACTIVATED BALLAST FOR OVERHEAD AND SIDEWALL LIGHTS FOR ROW 26 E/D. SECURED CONNNECTORS FOR BALLASTS. FOUND BALLAS T SHORTED. REPLACED BALLAST. 2 L 7 2 4F RT A6WE 1996061300302 19960613 00302 NM 1996 6 13 DLM88961347 1 19960601 A 3320 BV040550156 SOCKET DOUG MD88 MD88 3023688 NM CABIN BURNT A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 991DL 53343 ELECTRICAL ODOR IN CABIN AND COCKPIT. FOUND UPPER SIDEWALL LT SOCKET BURNED THROUGH AT SEAT 13ABC. REPLACED SOCKET AND BULB. 2 L 7 2 4F RT A6WE 1996061300304 19960613 00304 NM 1996 6 13 MWEA96152 1 19960607 A 2560 SLIDE PIN DOUG MD88 MD88 3023688 NM GALLEY DOOR FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 601ME 49762 CREW REPORTS FWD GALLEY DOOR EVAC SLIDE COVER PIN CAME OUT. REINSTALLED SLIDE COVER PIN, RETURNED A/C TO SERVICE. 2 L 7 2 4F RT A6WE 1996061300305 19960613 00305 WP 1996 6 13 MWEA96153 1 19960608 A 5730 SKIN DOUG DC9 DC914 3022034 WP LT WING LE DAMAGED A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 500ME 45711 LEADING EDGE OF LT WING SUSTAINED DAMAGE AFTER STRIKING VEHICLE JUST BEFORE PARKING AT JETWAY. INSTALLED DOUBLER REPAIR IAW SRM 57-06, FIG 2. 2 L 7 2 4F A6WE 1996061300306 19960613 00306 WP 1996 6 13 MWEA96154 1 19960608 A 3350 60030431 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 302ME 47102 DURING SERVICE CHECK, FOUND EMER LIGHTS IN AFT ACCESSORY COMPT ILLUMINATE WHEN POWER IS TURNED OFF. REPLACED BATTERY PO WER SUPPLY FOR LIGHTS AFFECTED, OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996061300307 19960613 00307 WP 1996 6 13 MWEA96155 1 19960609 A 2560 5917589103 SLIDE COVER DOUG DC9 DC914 3022034 WP FWD GALLEY FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 80ME 45795 CREW REPORTS GALLEY SERVICE DOOR EVAC SLIDE COVER FELL OFF. REINSTALLED GALLEY SERVICE DOOR EVAC SLIDE COVER. 2 L 7 2 4F A6WE 1996061300308 19960613 00308 NM 1996 6 13 P5CA9600242 1 19960606 A 2710 ACTUATOR BOEING 747 747122 1384872 NM LT AILERON MALFUNCTIONED A P5CA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 WP 23 854FT 19754 AFTER PUSHBACK, DURING FLIGHT CONTROL CHECK, FLIGHT CREW OBSERVED THAT LEFTHAND OUTBOARD AILERON DID NOT MOVE WITH FLAPS DOWN, RETURNED TO BLOCKS. CLEANED ELECTRICAL PLUG ON AILERON LOCKOUT ACTUATOR, OPERATIONAL CHECK SATISFACTORY PER MM 2 7-00-00. 2 L 7 4 4F A20WE 1996061300309 19960613 00309 NM 1996 6 13 9612472294 1 19960521 A 5241 FRAME BOEING 727 727251 138408H NM GALLEY DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 294US 21505 DURING P-CHECK, FOUND A CRACK IN THE FORWARD GALLEY SERVICE DOOR LOWER AFT FRAME AT THE STOP FITTING. REPAIRED FRAME PE R PROJECT 4-52-39963 SEC 2D AND DWG 69-69908-1. 2 L 7 3 4F A3WE 1996061300310 19960613 00310 WP 1996 6 13 9612489905 1 19960528 A 5320 FITTING DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 955N 47160 DURING H-CHECK, FOUND A CRACK IN THE RIGHT KEEL FORMER TO LONGERON 29R FITTING. REPLACED FITTING PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996061300311 19960613 00311 WP 1996 6 13 9612499905 1 19960528 A 5312 BULKHEAD DOUBLER DOUG DC9 DC931 3022065 WP AFT PRESS BLKHD CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 955N 47160 DURING H-CHECK, FOUND A CRACK IN THE AFT PRESSURE BULKHEAD -13 DOUBLER AT THE UPPER LEFT DOOR STOP SUPPORT FITTING PROPA GATING TOWARDS THE LIGHTENING HOLE. REPAIRED PER JO60088 -533, -537 AND SRM 51-30-5. 2 L 7 2 4F A6WE 1996061300312 19960613 00312 WP 1996 6 13 9612509905 1 19960529 A 5330 SKIN DOUG DC9 DC931 3022065 WP FS 598-680 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 955N 47160 DURING H-CHECK, FOUND CORROSION ON THE FUSELAGE SKIN INNER SURFACE FROM FS 598 TO 680, LONGERON 30 TO 27R. REPLACED SKI N PER SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1996061300313 19960613 00313 WP 1996 6 13 9612519902 1 19960529 A 5230 FITTING DOUG DC9 DC931 3022065 WP CARGO DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 952N 47073 DURING H-CHECK, FOUND CRACKS IN THE FORWARD CARGO DOOR AFT SUPPORT ANGLE FITTING AND ANGLE CLIP. REPLACED FITTING AND C LIP. 2 L 7 2 4F A6WE 1996061300314 19960613 00314 WP 1996 6 13 9612529905 1 19960530 A 5320 FITTING DOUG DC9 DC931 3022065 WP FS 600 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 955N 47160 DURING H-CHECK, FOUND CORROSION ON THE FOLLOWING KEEL LONGERON END FITTINGS AT FS 600, 28L, 29L AND 28R. REPLACED END F ITTINGS PER SRM 51-30-2. 2 L 7 2 4F A6WE 1996061300315 19960613 00315 WP 1996 6 13 9612539877 1 19960530 A 5744 FITTING DOUG DC9 DC951 3022051 WP LT SPOILER CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 786NC 48148 DURING B-CHECK, FOUND A .5 INCH CRACK IN THE LEFT OUTBOARD SPOILER INBOARD HINGE FITTING. REPLACED FITTING. 2 L 7 2 4F A6WE 1996061300316 19960613 00316 WP 1996 6 13 9612549902 1 19960530 A 5230 FITTING DOUG DC9 DC931 3022065 WP CARGO DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 952N 47073 DURING H-CHECK, FOUND CRACKS IN THE AFT CARGO DOOR NR 5 BEAM END FITTING, FORWARD SIDE AND IN THE HINGE SPRING BOLT DOOR FITTING. REPLACED FITTINGS. 2 L 7 2 4F A6WE 1996061300317 19960613 00317 WP 1996 6 13 9612559965 1 19960531 A 5230 FITTINGS DOUG DC9 DC931 3022065 WP CARGO DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 911RW 47149 DURING M-CHECK, FOUND TWO CRACKED BEAM END FITTINGS IN THE AFT CARGO DOOR, NR 5 FORWARD END AND NR 2 AFT END. REPLACED FITTINGS. 2 L 7 2 4F A6WE 1996061300318 19960613 00318 NM 1996 6 13 9612562294 1 19960531 A 5744 FITTING BOEING 727 727251 138408H NM NR 8 SPOILER CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 294US 21505 DURING P-CHECK, FOUND A CRACK IN THE RIGHT WING NR 8 SPOILER ACTUATOR SUPPORT FITTING. REPLACED FITTING. 2 L 7 3 4F A3WE 1996061300319 19960613 00319 NM 1996 6 13 9612576628 1 19960601 A 5744 FITTING BOEING 747 747251B 1384892 NM RT TE FLAP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 628US 22389 DURING P-CHECK, FOUND CORROSION IN THE RIGHT WING FLAP NR 6 CARRIAGE FITTING BEARING BORE. REPLACED FITTING (P/N 65B084 11-6). 2 L 7 4 4F A20WE 1996061300320 19960613 00320 WP 1996 6 13 9612581144 1 19960601 A 5743 FITTING DOUG DC10 DC1040 3023508 WP WS 240 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 144JC 46753 DURING T-CHECK, FOUND A CRACK IN THE LEFT WHEEL WELL GEAR SUPPORT FITTING AT THE REAR SPAR XORS 240. REPLACED FITTING ( P/N ARB198-501). 2 L 7 3 4F A22WE 1996061300321 19960613 00321 WP 1996 6 13 9612599907 1 19960601 A 5320 FITTING DOUG DC9 DC931 3022065 WP PAX DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 957N 47253 DURING M-CHECK, FOUND A CRACK IN THE AFT ENTRY DOOR UPPER LEFT DOOR STOP FITTING. REPLACED FITTING PER SRM 51-10-2. 2 L 7 2 4F A6WE 1996061300322 19960613 00322 WP 1996 6 13 9612609902 1 19960602 A 5320 FITTING DOUG DC9 DC931 3022065 WP FS 995 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 952N 47073 DURING H-CHECK, FOUND A CRACK AND CORROSION IN THE LONGERON 22R END FITTING AT FS 995. REPLACED FITTING PER SRM 51-01. 2 L 7 2 4F A6WE 1996061300323 19960613 00323 WP 1996 6 13 9612619941 1 19960602 A 5320 FITTING DOUG DC9 DC932 3022066 WP FS 617 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3324L 47103 DURING H-CHECK, FOUND A CRACK IN THE SUPPORT FITTING AT THE RIGHT INBOARD SEAT TRACK FS 617. REPLACED FITTING PER SRM 5 1-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1996061300324 19960613 00324 WP 1996 6 13 9612629302 1 19960608 A 3250 ANTI-SKID SYST DOUG DC9 DC982 3022082 WP NLG MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 302RC 48055 AT START OF TAKEOFF ROLL, RECEIVED STEADY WHEEL NOT TURNING INDICATION. TAKEOFF WAS ABORTED AT ABOUT 40 KNOTS AND RETUR NED TO THE GATE. INSPECTED WHEELS AND BRAKES, ALL WERE NORMAL. PLACED ANTI-SKID SYSTEM ON MEL. 2 L 7 2 4F A6WE 1996061300326 19960613 00326 WP 1996 6 13 9612649304 1 19960608 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 931MC 48057 DURING LINE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE AT AFT OVERWING EXITS. REPLACED BATTERY PACKS, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996061300327 19960613 00327 WP 1996 6 13 9612659936 1 19960607 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 1799U 47370 DURING LINE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE AT FORWARD ENTRY DOOR AND BOTH AFT OVERWING DOORS INOPERATIVE . REPLACED FUSE AT ENTRY DOOR AND REPLACED BATTERIES IN PACKS AT BOTH OVERWING EXITS, ALL OPERATIONAL CHECKS GOOD. 2 L 7 2 4F A6WE 1996061300328 19960613 00328 WP 1996 6 13 9612669941 1 19960606 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 3324L 47103 DURING LINE CHECK, FOUND OVERHEAD EMERGENCY LIGHTS FROM STA 446 TO 560 WEAK. REPLACED BATTERY PACK B5-32, OPERATIONAL C HECK OK. 2 L 7 2 4F A6WE 1996061300329 19960613 00329 WP 1996 6 13 9612679992 1 19960606 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8960E 45869 DURING LINE CHECK, FOUND OVERHEAD EMERGENCY LIGHT INOPERATIVE IN AFT CABIN. REPLACED BATTERIES, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996061300330 19960613 00330 NM 1996 6 13 96FDEA00440 1 19960305 A 5350 65397349 FAIRING BOEING 727 727233 138408A NM BS 3340 GOUGE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 GOUGE ON FAIRING 3340, 22 INCHES FROM BOTTOM AND 12 AFT OF PANEL. *S/D* REMOVED DAMAGED AREA 3 FT BY 5 FT .040 AND REP AIRED PER SRM 51-40-2. 2 L 7 3 4F RT A3WE 1996061300331 19960613 00331 NM 1996 6 13 96FDEA00441 1 19960305 A 5314 65564416 KEEL BEAM BOEING 727 727233 138408A NM BS 990 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CRACKS IN LOWER I/B AND O/B FLANGE RADIUS IN RT KEEL BEAM BS 990. *S/D* REPAIRED RT KEEL BEAM PER FEDEX EO 7-5310-7-2 356C, PT5 AND FEDEX EA 7-5310-2777B. 2 L 7 3 4F RT A3WE 1996061300332 19960613 00332 NM 1996 6 13 96FDEA00445 1 19960305 A 5347 BAC1520793 SEAT TRACK BOEING 727 727233 138408A NM BS 760-848 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CORROSION AROUND FASTENER HOLES IN SEAT TRACK WELL FROM BS 760 TO 848 LBL 45 WL 208. *S/D* REMOVED CORRODED SEAT TRACK WELL FROM BS 760 TO 848 LBL 45 WL 208, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. INSTALLED NEW SEAT TRACK WELL FROM B S 760 T0 848 RBL WL 208, WET NICK SEALANT AND INSTALLED FASTENERS. 2 L 7 3 4F RT A3WE 1996061300333 19960613 00333 NM 1996 6 13 96FDEA00447 1 19960305 A 5347 BAC1520793 SEAT TRACK BOEING 727 727233 138408A NM BS 760-848 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CORROSION AROUND FASTENER HOLES IN SEAT TRACK WELL FROM BS 760 TO 848 RBL 25 WL 208. *S/D* REMOVED CORRODED SEAT TRACK WELL FROM BS 760 TO 848 RBL 25 WL 208 FOUND TO BE OUT OF LIMITS PER FDE SRM 53-10-1. INSTALLED NEW SEAT TRACK WELL AT BS 760 TO 848 RBL 25 WL 208, WET SEALANT AND INSTALLED FASTENERS. 2 L 7 3 4F RT A3WE 1996061300334 19960613 00334 NM 1996 6 13 96FDEA00454 1 19960307 A 5311 BAC15171080 FRAME BOEING 727 727233 138408A NM BS 760 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 DOUBLE HOLE IN BS 760 FRAME BELOW STR 6L. *S/D* REMOVED DAMAGE, FABRICATED REPAIR PART AND INSTALLED AT BS 760 FRAME B ELOW STR 6L PER SRM 53-10-4. 2 L 7 3 4F RT A3WE 1996061300335 19960613 00335 NM 1996 6 13 96FDEA00499 1 19960311 A 5210 50794543 WEB BOEING 727 727233 138408A NM PAX DOOR GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 NR 0736, FORWARD ENTRY DOOR UPPER HINGE CASTING IN DOOR, LOWER SUPPORT WEB IS GOUGED REQUIRING REPLACEMENT. *S/D* REMO VED AND REPLACED LOWER SUPPORT WEB ON UPPER HINGE CASTING ON FORWARD ENTRY DOOR PER SRM 53-10-2. 2 L 7 3 4F RT A3WE 1996061300336 19960613 00336 NM 1996 6 13 96FDEA01074 1 19960605 A 5315 BAC15034283 FLOOR BEAM BOEING 727 72722 1384002 NM BS 480 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 NR 0548, (001) WHILE WORKING NR0283 FOUND CORROSION ON UPPER SURFACE OF 480 FLOOR BEAM RBL 45. *S/D* REPAIRED FLOOR BE AM BS 480 RBL 45 IAW SRM 53-10-8. 2 L 7 3 4F A3WE 1996061300338 19960613 00338 NM 1996 6 13 96FDEA01076 1 19960608 A 5753 652163480 SKIN BOEING 727 72722 1384002 NM RT TE FLAP DELAMINATION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 467FE 21449 NR 0322, 001 DELAMINATION ON R/W I/B FLAP UPPER SURFACE 48 INCHES FROM I/B END. *S/D* REPAIRED DELAMINATION ON R/W I/B AFT FLAP UPPER SURFACE 48 INCHES FROM I/B END IAW FEDEX SRM 51-40-06, FIG 40 PG 75. 2 L 7 3 4F A3WE 1996061300339 19960613 00339 NM 1996 6 13 96FDEA01077 1 19960608 A 5753 652163092 FORE FLAP BOEING 727 72722 1384002 NM RT TE FLAP DELAMINATION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 467FE 21449 DELAMINATION ON R/W I/B FORE FLAP UPPER SURFACE ABOVE CENTER TRACK. *S/D* REPAIRED R/W I/B FORE FLAP UPPER SURFACE ABO VE CENTER TRACK IAW FEDEX SRM 51-40-6 FIG 36. 2 L 7 3 4F A3WE 1996061300340 19960613 00340 NM 1996 6 13 96FDEA01078 1 19960608 A 5753 652163590 SKIN BOEING 727 72722 1384002 NM RT TE FLAP DELAMINATION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 467FE 21449 NR 0324, 003 DELAMINATION ON R/W O/B AFT FLAP ABOUT 5 INCHES FROM I/B END. *S/D* REPAIRED DELAMINATION ON R/W O/B AFT FLAP 5 INCHES FROM I/B END IAW FEDEX SRM 51-40-06 FIG 40. 2 L 7 3 4F A3WE 1996061300341 19960613 00341 NM 1996 6 13 96FDEA01079 1 19960610 A 5315 652082710 FLOOR BEAM BOEING 727 72722 1384002 NM BS 620 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 NR 0353, 003 CORROSION (C53-224-01) ON FLOOR BEAM TOP CHORD BS 620, LBL 10 TO 21 AND RBL 2 TO 56 WL 208. *S/D* REPAIRE D BS 620 FLOOR BEAM UPPER CHORD LBL 21 TO RBL 56 IAW FEDEX SRM 53-10-8. 2 L 7 3 4F A3WE 1996061300342 19960613 00342 NM 1996 6 13 96FDEA0448 1 19960503 A 5347 BAC1520793 SEAT TRACK BOEING 727 727233 138408A NM BS 760-848 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 NR 0375, 014C CORROSION AROUND FASTENER HOLES IN SEAT TRACK WELL FROM BS 760 TO 848 LBL 25 WL 208. *S/D* SEAT TRACK CO RRODED OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED SEAT TRACK BS 760 TO 848 LBL 25 WL 208. 2 L 7 3 4F RT A3WE 1996061300343 19960613 00343 NM 1996 6 13 96FEA00424 1 19960305 A 5347 652363736 SEAT TRACK BOEING 727 727233 138408A NM BS 480-680 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CORROSION ALONG SEAT TRACK FLANGE AND AROUND FASTENERS IS OUT OF LIMITS BS 480 TO 680 LBL 45 WL 208. *S/D* REMOVED AND REPLACED SEAT TRACK AT BS 480 TO 680 LBL 45 WL 208 SRM 53-10-5. 2 L 7 3 4F RT A3WE 1996061300344 19960613 00344 EU 1996 6 13 96UAL900419 1 19960607 A 3350 LAMP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 424UA 506 CABIN EMERGENCY LIGHT TEST FAILED. RELAMPED EMERGENCY LIGHTS, RESEATED CONNECTOR ON EPSU 11WL, SYSTEM OPERATED NORMALLY . 2 L 7 2 4F 4 F RT A28NM E40NE 1996061300345 19960613 00345 NM 1996 6 13 96UAL900420 1 19960607 A 3350 BATTERIES BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7269U 21416 LEFT FWD OVERWING DOOR EMERGENCY LIGHT DIM. REPLACED BATTERIES, SYSTEM CHECKS OKAY. 2 L 7 3 4F 4 F A3WE E2EA 1996061300346 19960613 00346 WP 1996 6 13 96UAL900421 1 19960607 A 2910 NAS161216 PACKING DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 1 HYD SYST FAILED A UALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 1814U 46613 PER CREW, NR 1 HYDRAULIC SYSTEM LOST FLUID. *S/D* PACKING ON SUCTION/RETURN LINE FITTING FAILED ON REVERSIBLE MOTOR PU MP. REPLACED FITTING AND PACKING. 2 L 7 3 4F 4 F A22WE E23EA 1996061300347 19960613 00347 NM 1996 6 13 96UAL900422 1 19960607 A 2600 285N002838 FIRE WARNING BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE APU ACTIVATED A UALA F ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 WP 29 618UA 21878 61639 CREW REPORTED APU AUTO SHUT DOWN AND FIRE WARNING. FLIGHT CREW DISCHARGED THE FIRE BOTTLE. SUPPLEMENTAL DATA UPDATE: R EPLACED APU FIRE BOTTLE AND SQUIBB PER MM 26-22-02. RAN APU AND CHECKED FOR PNEUMATIC LEAKS, NO LEAKS FOUND. APU RAN F OR SEVERAL HOURS WITH NO SHUT DOWN. VISUALLY CHECKED BOTH UPPER AND LOWER DETECTOR LOOPS AND CLEANED CONNECTORS. REPLA CED CARD M10400, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 1996061300348 19960613 00348 NM 1996 6 13 96UAL900423 1 19960607 A 2421 729825G IDG BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE FAILED A UALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 WP 29 532UA 25072 NR 1 GENERATOR WENT OFF LINE, DIVERTED TO BDL. RESET OK BUT LEFT GENERATOR DRIVE DISCONNECT LIGHT FLASHES INTERMITTENTL Y. PROCEEDED EWR WITH APU OPERATING. *S/D* FOUND THE INTEGRATED DRIVE GENERATOR FAILED. REPLACED INTEGRATED DRIVE GE NERATOR, CHECKS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 1996061300349 19960613 00349 NM 1996 6 13 96UAL900424 1 19960607 A 2421 729825G IDG BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE FAILED A UALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 WP 29 532UA 25072 PER CREW, FELT SUDDEN BUMP IN FLIGHT AND NR 1 GENERATOR DRIVE LIGHT ILLUMINATED AND BREAKER OFF. NUMEROUS EICAS MESSAGE S. DIVERTED TO SLC. *S/D* FOUND INTEGRATED DRIVE GENERATOR FAILED. REPLACED GENERATOR, CHECKS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 1996061300350 19960613 00350 NM 1996 6 13 96UAL900425 1 19960610 A 3350 LIGHT BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 164UA 21657 EXTERIOR EMERGENCY LIGHTS INOPERATIVE AT LEFT SIDE 2ND FIXTURE, 2ND LAMP AND RIGHT SIDE 3RD FIXTURE, 2ND LAMP. 2 L 7 4 4F 4 F A20WE E20EA 1996061300351 19960613 00351 NM 1996 6 13 96UAL900426 1 19960610 A 3350 LIGHT BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 164UA 21657 EMERGENCY CEILING LIGHT AND EEL LIGHT ARE INOPERATIVE IN FORWARD GALLEY BETWEEN DOORS 2R AND 2L. 2 L 7 4 4F 4 F A20WE E20EA 1996061300353 19960613 00353 NM 1996 6 13 96UAL900428 1 19960610 A 2820 69186127 FUEL VENT TUBE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 FUEL TANK CRACKED A UALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 7270U 21417 NR 1 FUEL TANK LOST 800 POUNDS IN 40 MINUTES. SUPPLEMENTAL DATA UPDATE: REPLACED VENT SYSTEM ELBOW IN TANK NR 1. 2 L 7 3 4F 4 F A3WE E2EA 1996061300354 19960613 00354 NE 1996 6 13 96UAL900429 2 19960610 A 7261 54T250 OIL LINE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT ENGINE CRACKED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 660UA 27115 724189 RIGHT ENGINE OIL QUANTITY DECREASED TO ZERO. MADE AN UNSCHEDULED LANDING. *S/D* ANGLE GEAR BOX OIL PRESSURE LINE, LP0 9 CRACKED. REPLACED OIL LINE. 2 L 7 2 4F 4 F RT A1NM E24NE 1996061300355 19960613 00355 NM 1996 6 13 96UAL900430 1 19960610 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 586UA 26710 EMERGENCY LIGHT ROW 24R INOP. RELAMPED EMERGENCY LIGHT ROW 24R, OPERATION NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996061300356 19960613 00356 WP 1996 6 13 ABXA9600505 1 19960606 A 2910 7927176766 HYD LINE DOUG DC9 DC933F 302207A WP RT MLG WW BROKEN A A ABXA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 23 934AX 47462 RIGHT HYDRAULIC SYSTEM FLUID LOSS FAILURE ON CLIMBOUT. CREW PERFORMED ABNORMALS AND CAME TO A FULL STOP ON RUNWAY. MAI NTENANCE SECURED THE GEAR AND STOWED MLG DOORS PRIOR TO TAXI. FOUND ALTERNATE PUMP HYDRAULIC LINE BROKEN IN THE RIGHT W HEEL WELL, REPLACED WITH FLEX LINE AND DEFERRED. ALSO, FOUND GEAR PRESSURE RETURN LINE (7912697-932) IN LEFT WHEEL WELL RUPTURED, REPLACED LINE. REPLACED RIGHT MLG INBD DOOR, BOTH RETURN FILTERS, NR 2 ENGINE DRIVEN HYDRAULIC PUMP AND CASE DRAIN FILTER, LEAK CHECKED AND SERVICED IAW DC9 MM. 2 L 7 2 4F A6WE 1996061300357 19960613 00357 WP 1996 6 13 ABXA9600506 1 19960610 A 3260 0331881003 LIGHT SOCKET DOUG DC9 DC933F 302207A WP RT MLG DEFECTIVE A ABXA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 23 934AX 47462 ON GEAR UPLATCH CHECK, RIGHT LANDING GEAR GREEN LIGHT CAME ON BRIGHT. GEAR RECYCLING WAS NORMAL EXCEPT LIGHT STAYED ON BRIGHT ALL THROUGH RECYCLING. REPLACED THE RIGHT MAIN LANDING GEAR DOWN LIGHT SOCKET. 2 L 7 2 4F A6WE 1996061300358 19960613 00358 WP 1996 6 13 ARWA9606003 1 19960608 A 5230 AE4431300 LOCKING VALVE DOUG DC8 DC862 3021970 WP MAIN CARGO DOOR INOPERATIVE A ARWA O OTHER J WARNING INDICATION TO TAKEOFF 1 SO 19 1803 45895 AFTER TAKEOFF, MAIN CARGO DOOR LIGHT ILLUMINATED AT 8 PSI. INSTALLED THREE GEAR AT DOOR LATCHES, RETURNED TO MIAMI. TR OUBLESHOT SYSTEM, FOUND BAD LOCKING VALVE. REMOVED AND REPLACED LOCKING VALVE IAW 52-30-00, OPS CHECKED NORMAL. 2 L 7 4 4F 4A25 1996061300359 19960613 00359 1996 6 13 CALA9600773 4 19960610 A 3417 HG480B20 ADC BOEING 737 737222 1384473 NM E/E RACK INOPERATIVE A CALA O OTHER O OTHER CR CRUISE 1 SW 09 12235 13965 13929 19758 THE CAPTAIN'S ALTIMETER, COMPASS FLAG IN HSI, OFF FLAG IN ALT SELECT WINDOW, AUTO PILOT, MACH TRIM, GPWS, MODE-C AND CAP TAIN'S DME INSTRUMENTATION ALL WENT INOPERATIVE INTERMITTENTLY WHILE EN ROUTE. THE USABILITY OF THE INSTRUMENTATION WO ULD RETURN EVERY 10 TO 15 MINUTES. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AIR DATA COMPUTER AT FA ULT. THE COMPUTER WAS REMOVED AND REPLACED. A PITOT/STATIC CHECK WAS PERFORMED ON THE COMPUTER IAW MM 34-12-11, PAGES 401 AND 402 AND ALL CHECKED GOOD. 2 L 7 2 4F A16WE 1996061300360 19960613 00360 WP 1996 6 13 CALA9600774 1 19960522 A 5320 JAMB WEB DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35832 49492 INSPECTION FOUND A 2 INCH CRACK IN FORWARD ENTRY DOOR JAMB WEB AT STA 207, LONGERON 15L. A DOUBLER WAS INSTALLED IAW SR M 53-01-01. 2 L 7 2 4F A6WE 1996061300361 19960613 00361 WP 1996 6 13 CALA9600775 1 19960522 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 160-200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35832 49492 INSPECTION FOUND Z-ANGLE FLOOR SUPPORT CORRODED TEN INCHES FROM FORWARD ENTRY DOOR AT STA 160 TO 200. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 53-01-01. 2 L 7 2 4F A6WE 1996061300362 19960613 00362 WP 1996 6 13 CALA9600776 1 19960604 A 5312 BULKHEAD PANELS DOUG DC9 DC982 3022082 WP BS 786.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35832 49492 INSPECTION FOUND BULKHEAD PANELS IN MID BIN CORRODED AT STA 786.5. A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW SRM 53 -01. 2 L 7 2 4F A6WE 1996061300364 19960613 00364 WP 1996 6 13 CALA9600778 1 19960525 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1418 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35832 49492 INSPECTION FOUND A 2 INCH CRACK IN FRAME AT STA 1418, LONGERON 2R AND A 1 INCH CRACK WAS FOUND AT LONGERON 2L. REPAIRS WERE INSTALLED IAW SRM 53-03-32. 2 L 7 2 4F A6WE 1996061300365 19960613 00365 WP 1996 6 13 CALA9600779 1 19960521 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 886 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35832 49492 INSPECTION FOUND A 2.5 INCH CRACK IN KEEL BEAM T-ANGLE SUPPORT FOR ADF PANELS AT STA 886. THE T-ANGLE SUPPORT WAS REMOV ED AND REPLACED IAW SRM 51-30-0. 2 L 7 2 4F A6WE 1996061300366 19960613 00366 SO 1996 6 13 COMA9610173 1 19960609 A 7603 0881824 SOLENOID EMB 120 EMB120RT SO RT ENGINE FAILED A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 267CA 120259 POWER LEVER, FLIGHT IDLE STOP, CIRCUIT BREAKERS WERE TRIPPED. REPLACED THE RT POWER LEVER FLIGHT IDLE STOP SOLENOID, RE SET LT BREAKER. 2 L 7 2 4T RT A31SO 1996061300367 19960613 00367 SO 1996 6 13 COMA9610174 1 19960609 A 2750 12042642507 FLAP SELECTOR EMB 120 EMB120RT SO INST PANEL MALFUNCTION A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 189CA 13994 4257 12089 FLAP CONTROL FAULT WARNING ON CWP. REPLACED FLAP SELECTOR CONTROL. 2 L 7 2 4T RT A31SO 1996061300368 19960613 00368 EU 1996 6 13 COMA9630124 1 19960609 A 3350 6104781 BATTERY SAAB SF340 SF340A 7850100 EU CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 140N 340A140 EMERGENCY LIGHTING IS INOPERATIVE. REPLACED EMERGENCY LIGHTING BATTERIES. 2 L 7 2 4T RT A52EU 1996061300369 19960613 00369 1996 6 13 DHL96724002 4 19960608 A 3421 2588369905 ADI BOEING 727 727228 NM RT COCKPIT FAILED A T DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 724DH 19862 UPON ROTATION, DURING TAKEOFF ROLL, F/O ADI STUCK IN PITCH UP POSITION. RUNWAY FLAG STILL IN VIEW ON LANDING. REMOVED AND REPLACED ADI AND RERACKED INSTRUMENT AMPLIFIER, OPS CHECK OK PER M/M 34-20. 2 L 7 3 4F A3WE 1996061300370 19960613 00370 NM 1996 6 13 QXEA9600194 1 19960608 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT INOPERATIVE A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 102AV 091 COCKPIT EMERGENCY LIGHT WAS INOP. LIGHT ASSY REPLACED AND LIGHT OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 1996061300371 19960613 00371 EU 1996 6 13 QXEA9600195 1 19960609 A 3350 1312 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 466US 11075 RIGHT SIDE EMERGENCY OVERWING EXIT LIGHT INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996061300372 19960613 00372 EU 1996 6 13 QXEA9600196 1 19960610 A 3350 1820 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 452US 11105 EMERGENCY EXIT LIGHT AT SEAT 8E INOP. THE 28V BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996061300373 19960613 00373 EU 1996 6 13 QXEA9600197 1 19960610 A 3350 1312 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 450US 11101 EXIT SIGN AT 8A IS INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996061300374 19960613 00374 EU 1996 6 13 QXEA9600198 1 19960610 A 3350 1315 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 450US 11101 EMERGENCY LIGHT NEAR MAIN CABIN DOOR IS INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996061300375 19960613 00375 WP 1996 6 13 SCNA96154 1 19960603 A 2611 72130000008 SMOKE DETECTOR DOUG DC10 DC1015 3022118 WP FWD RT LAV INOPERATIVE A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 THE SMOKE DETECTOR IN THE LAV JUST AFT OF DOOR R1 WAS FOUND TO BE INOP. REMOVED AND REPLACED THE SMOKE DETECTOR, OPS CH ECK OK. 2 L 7 3 4F A22WE 1996061300376 19960613 00376 EU 1996 6 13 WWMA9600050 1 19960611 A 7712 CTOT SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT ENGINE MALFUNCTIONED A WWMA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 15 313AE 340B313 THE CREW REPORTED, AFTER TAKEOFF THE LEFT ENGINE SPUTTERED 3 TIMES AND OV TEMPERATURE ILLUMINATED BRIEFLY WHILE THE CTOT WAS BEING TURNED OFF. THE AIRCRAFT RETURNED TO FIELD WITHOUT INCIDENT. MAINTENANCE INSPECTED THE LEFT ENGINE COMPRESS ORS FOR CLEANLINESS AND RUB. NO RUB WAS FOUND BUT THE FIRST STAGE COMPRESSOR WAS FOUND TO BE DIRTY. THE AIRCRAFT WAS G ROUND RAN AND THE CTOT WAS FOUND TO BE MALFUNCTIONING. THE COMPRESSOR WASH WAS SCHEDULED AND THE CTOT WAS DEFERRED IAW THE MEL. THE AIRCRAFT WAS RELEASED FOR SERVICE WITH NO FURTHER PROBLEMS. 2 L 7 2 4T 4 T RT A52EU E8NE 1996061300402 19960613 00402 NM 1996 6 13 96ZZZX2968 1 19960326 A 3246 WHEEL BOEING 727 727223 1384074 NM NLG VIBRATION A CKSA C D ABORTED TAKEOFF RETURN TO BLOCK E VIBRATION/BUFFET TO TAKEOFF 1 GL 23 856AA 20997 KHUF - FLT 73304 - ABORTED TAKEOFF AS A RESULT OF SEVERE VIBRATION EMANATING FROM NOSE WHEEL AREA. VIBRATION BEGAN AT A PPROXIMATELY 90 KNOTS AND CONTINUED TO INCREASE WITH AIRSPEEDS. ABORTED AT 110 KNOTS. REMOVED AND REPLACED LEFT NOSE W HEEL. TAXI CHECKED OK. NO OTHER DEFECTS FOUND. 2 L 7 3 4F A3WE 1996061300403 19960613 00403 NM 1996 6 13 96ZZZX2969 1 19960330 A 3260 ACCESSORY UNIT BOEING 727 72722C 138400F NM GEAR WARNING REQUIRED RERACK A CKSA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 23 727CK 19195 KLEX - FLT 73391 - DURING TAKEOFF, STEADY LANDING GEAR UNSAFE HORN SOUNDED IN ALL CONFIGURATIONS. RE-RACK LANDING GEAR ACCESS UNIT. OPS CHECK GOOD ON GROUND. 2 L 7 3 4F A3WE 1996061300416 19960613 00416 GL 1996 6 13 ERAA96205 2 19960301 A 7250 6886407 WHEEL 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL 1ST STAGE BLADE STRETCH A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 125EH 784 CAT25407 562 BLADE STRETCH .005 OVER PRINT SIZE. 1 G 7 2 3U 3 U H3EU E4CE 1996061300417 19960613 00417 EU 1996 6 13 ERAA96206 1 19960301 A 6520 4619310069 ROLLER BEARING 4619002003 BOLKMS 105 BO105S 5626006 EU T/R GR BOX MAKING METAL A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 133EH 17 1285 598 GEARBOX MAKING METAL. ROLLERS ARE ROUGH, METAL CHIPS FOUND ON ROLLERS. 1 G 7 2 3U H3EU 1996061300418 19960613 00418 GL 1996 6 13 ERAA96207 2 19960301 A 7250 23038218 NOZZLE BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL 1ST STAGE MIS OHAUL A ERAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 299EH S807 NOZZLE REC'D BACK FROM OVERHAUL. ROPE PACKING GROOVE IN OUTER BAND TOO NARROW TO SEAT ROPE. 1 G 7 2 3U 3 U H3EU E4CE 1996061300419 19960613 00419 GL 1996 6 13 ERAA96208 2 19960305 A 7250 23034140 NOZZLE BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL 3RD STAGE MIS OHAULED A ERAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 154EH 704 NOZZLE SENT TO OVERHAUL . FLANGE NOT MACHINED TO PROPER DIMENSION CAUSING NOZZLE NOT TO SEAT PROPERLY ON THE SUPPORT DU RING INSTALLATION. 1 G 7 2 3U 3 U H3EU E4CE 1996061300420 19960613 00420 SW 1996 6 13 ERAA96209 1 19960306 A 6220 412018056105 LOWER CONE SEAT BELL 412 412 1182202 SW M/R PITTED A ERAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 LOWER CONE SEAT THAT WAS OVERHAULED WITH ZERO T.S.O. REC'D IN WITH PITTING AROUND DRIVE PIN HOLES. 1 G 7 2 4U H4SW 1996061300421 19960613 00421 SW 1996 6 13 ERAA96210 1 19960308 A 6230 412010182101 BEARING BELL 412 412 1182202 SW M/R EXCESS PLAY A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 167EH 893 33089 BEARING HAS EXCESSIVE RADIAL & AXIAL PLAY. 1 G 7 2 4U H4SW 1996061300422 19960613 00422 GL 1996 6 13 ERAA96211 2 19960308 A 7250 6898731 PT SUPPORT BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL OIL NOZZLE PITTED A ERAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 P T SUPPORT OVERHAULED AND RET'D TO ERA 6/23/95. UPON RECEIVING , INSPECTOR FOUND LARGE PIT IN AREAA11:00 OIL NOZZLE S TRUT. 1 G 7 2 3U 3 U H3EU E4CE 1996061300423 19960613 00423 1996 6 13 ERAA96212 2 19960311 A 7250 A23037413 OUTER SHAFT 6898735 BOLKMS 105 BO105S 5626006 EU TURB ASSY WORN CURVIC A ERAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 151EH 632 CAT25376 S706 OUTER SHAFT WAS INST'D ON TURBINE ASSY 5/11/95 , TT 2793.4. INST'D ON , A/C TT 7234.1 AND HAD TO REMOVE BECAUSE SHAFT HAS WORN CURVIC. 1 G 7 2 3U H3EU 1996061300424 19960613 00424 EU 1996 6 13 ERAA96213 1 19960314 A 6710 10531821 CONTROL ROD ASSY BOLKMS 105 BO105S 5626006 EU PITCH LINK SCORED A ERAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 NEW PITCH LINK ASSY THAT HAS SCORING ON SHAFT. 1 G 7 2 3U H3EU 1996061300425 19960613 00425 GL 1996 6 13 ERAA96214 2 19960320 A 7250 A23001801 COUPLING 6898735 BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL PT OUTER MIS MFG A ERAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 403EH CAT36411 45113 NEW PART WITH PILOT DIAMETER TOO SMALL, WOULD NO FIT DOWN OVER OUTER SHAFT TO REACH THREADS. TURBINE WAS BEING O/H WHEN DESCREPANCY WAS FOUND. PART WAS NEVER INSTALLED. 1 G 7 1 3U 3 U H2SW E4CE 1996061300426 19960613 00426 GL 1996 6 13 ERAA96215 2 19960322 A 7250 6851531 NOZZLE BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL 4TH STAGE MIS OHAULED A ERAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 151EH S706 NOZZLE WAS OVERHAULED AND RETURNED TO ERA 1-11-96. #2-4 SEAL NOT SEATED. 1 G 7 2 3U 3 U H3EU E4CE 1996061300427 19960613 00427 GL 1996 6 13 ERAA96216 2 19960327 A 7323 2524667 GOVERNOR BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20 03013 GL ENGINE MALFUNCTION A ERAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 127EH 7608 571 GOVERNOR WAS OVERHAULED ON 11/6/95. GOVERNOR WILL NOT MAINTAIN RPM UNDER HOOD. 1 G 7 2 3U 3 U H3EU E4CE 1996061300429 19960613 00429 GL 1996 6 13 ERAA96224 2 19960416 A 7323 2524667 GOVERNOR BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20 03013 GL ENGINE DEFECTIVE A ERAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 131EH 401 595 GOVERNOR WAS SENT FOR OVERHAUL 07/18/94 . UNIT NOW HAS 401.3 T.S.O. AND WILL NOT BEEP TO 99%. 1 G 7 2 3U 3 U H3EU E4CE 1996061300430 19960613 00430 GL 1996 6 13 ERAA96225 2 19960416 A 7250 6888547 SUMP COVER BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20 03013 GL PT SUMP LEAK A ERAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 151EH S706 P.T. SUMP COVER WAS SENT FOR OVERHAUL . PART HAS 28.7 HRS T.S.O. AND IS LEAKING AT BOLT HOLE AS MARKED . 1 G 7 2 3U 3 U H3EU E4CE 1996061300431 19960613 00431 GL 1996 6 13 ERAA96226 2 19960417 A 7250 6851531 NOZZLE BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20 03013 GL 4TH STAGE DEFECTIVE A ERAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 292EH S843 NOZZLE SENT FOR O/H AND RET'D 4-3-96 WITH T.I.R. ON SEAL AND BLADE PATH BEYOND ALLOWABLE LIMITS. 1 G 7 2 3U 3 U H3EU E4CE 1996061300432 19960613 00432 SW 1996 6 13 ERAA96227 1 19960422 A 6220 412310400107 BEARING 412010406115 BELL 412 412 1182202 SW M/R EXCESS PLAY A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 417EH 408 A843 33031 BEARINGS HAVE EXCESS RADIAL AND AXIAL PLAY. 1 G 7 2 4U H4SW 1996061300433 19960613 00433 SW 1996 6 13 ERAA96228 1 19960422 A 6220 412310400107 BEARING 412010406115 BELL 412 412 1182202 SW M/R EXCESS PLAY A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 417EH 408 A719 33031 BEARINGS HAVE EXCESS AXIAL & RADIAL PLAY. 1 G 7 2 4U H4SW 1996061300434 19960613 00434 SW 1996 6 13 ERAA96229 1 19960503 A 6230 204011451001 TRUNNION ASSY BELL 412 412 1182202 SW SEAL BEARING DEFECT A ERAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 NEW TRUNNION BEARING THAT HAS DEFECTIVE SEAL. WHILE GREASING TO PREPARE TO INSTALL ON AIRCRAFT, SEAL POPPED OUT OF BEA RING. 1 G 7 2 4U H4SW 1996061300435 19960613 00435 SW 1996 6 13 ERAA96230 1 19960503 A 6220 412310400107 BEARING 412010406115 BELL 412 412 1182202 SW M/R WORN A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 164EH 785 A1439 33004 BEARINGS WORN BEYOND LIMITS. 1 G 7 2 4U H4SW 1996061300436 19960613 00436 SW 1996 6 13 ERAA96231 1 19960503 A 6220 412310400107 BEARING 412010406115 BELL 412 412 1182202 SW M/R WORN A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 164EH 785 A1459 33004 BEARINGS WORN BEYOND LIMITS. 1 G 7 2 4U H4SW 1996061300437 19960613 00437 EU 1996 6 13 ERAA96232 1 19960503 A 6520 4619310071 BEARING 4619002003 BOLKMS 105 BO105S 5626006 EU INTERMED GR BX MAKING METAL A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 133EH 17 1285 598 BEARING WITH 16.7 HRS ROUGH, GEARBOX MAKING METAL. 1 G 7 2 3U H3EU 1996061300438 19960613 00438 EU 1996 6 13 ERAA96233 1 19960506 A 6520 4619310069 ROLLER BEARING 4619002003 BOLKMS 105 BO105S 5626006 EU T/R GR BOX MAKING METAL A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 127EH 613 571 GEARBOX MAKING METAL 1 G 7 2 3U H3EU 1996061300439 19960613 00439 EU 1996 6 13 ERAA96234 1 19960506 A 6520 4619310070 CONICAL ROLLER 4619002003 BOLKMS 105 BO105S 5626006 EU T/R GR BOX MAKING METAL A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 127EH 613 571 GEARBOX MAKING METAL 1 G 7 2 3U H3EU 1996061300440 19960613 00440 EU 1996 6 13 ERAA96235 1 19960506 A 6520 4619310072 ROLLER BEARING 4619002003 BOLKMS 105 BO105S 5626006 EU T/R GR BOX MAKING METAL A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 127EH 613 571 GEARBOX MAKING METAL. 1 G 7 2 3U H3EU 1996061300441 19960613 00441 GL 1996 6 13 ERAA96236 2 19960506 A 7323 2524667 GOVERNOR BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20 03013 GL ENGINE DEFECTIVE A ERAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 293EH 2794 S844 GOVERNOR WAS SENT FOR OVERHAUL AND RETURNED TO ERA 12/19/94. GOVERNOR IS VERY SLOW RESPONDING. 1 G 7 2 3U 3 U H3EU E4CE 1996061300442 19960613 00442 SW 1996 6 13 HEEA967168 1 19960508 A 7931 206075677103 INDICATOR BELL 206 206L3 1182108 SW COCKPIT READS HIGH E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 8591X 51495 INDICATOR PRESSURE SIDE READS HIGH. 1 G 7 1 3U H2SW 1996061300443 19960613 00443 SW 1996 6 13 HEEA967169 1 19960508 A 7714 206075681117 INDICATOR BELL 206 206L3 1182108 SW TURB RPM ERRATIC E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 979BH 51403 TURBINE NEEDLE ERRATIC AT LOW RPM. 1 G 7 1 3U H2SW 1996061300445 19960613 00445 1996 6 13 HEEA967172 4 19960508 A 2210 7660002113103 VERTICAL GYRO SKRSKY S76 S76A 8143006 NE AFCS PITCH DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1545X 760050 KICK IN AFCS PITCH CHANNEL. 1 G 7 2 3U H1NE 1996061300446 19960613 00446 1996 6 13 HEEA967173 4 19960508 A 3444 4014267902 ALTIMETER BELL 412 412 1182202 SW COCKPIT READS HIGH E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 33008 36004 RADAR ALTIMETER DH LIGHT COMES ON TOO SOON AND READS HIGH. 1 G 7 2 4U H4SW 1996061300447 19960613 00447 SW 1996 6 13 HEEA967174 1 19960508 A 6320 206075188005 INDICATOR BELL 206 206L1 1182107 SW XMSN OIL MALFUNCTION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 10814 45415 PRESSURE READS HIGH AND TEMP NEEDLE STICKS. GLASS IS FOGGED 1 G 7 1 3U H2SW 1996061300448 19960613 00448 1996 6 13 HEEA967175 4 19960508 A 2562 ELT10 ELT NARCO BELL 206 206L1 1182107 SW COCKPIT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5006F 45181 DID NOT FUNCTION DURING 30 DAY INSPECTION. 1 G 7 1 3U H2SW 1996061300449 19960613 00449 SW 1996 6 13 HEEA967176 1 19960508 A 2844 206061535007 TRANSDUCER BELL 206 206B 1181511 SW FUEL PRESS DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 22743 3624 FUEL PRESSURE FLUCTUATES BELOW 24 PSI CAUSING HIGH READING. 1 G 7 1 3U H2SW 1996061300450 19960613 00450 SW 1996 6 13 HEEA967177 1 19960508 A 2810 41228200003001 TANK BELL 412 412 1182202 SW LT FUEL DAMAGED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3911L 33023 AFT CROSSTUBE BROKE AND CRACKED FUEL TANK. 1 G 7 2 4U H4SW 1996061300451 19960613 00451 1996 6 13 HEEA967178 4 19960509 A 3416 212070238003 INDICATOR SKRSKY S76 S76A 8143006 NE COCKPIT FRICTION ERROR E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5426U 760167 EXCESSIVE FRICTION ERROR AND 2 YEAR INSPECTION DUE. 1 G 7 2 3U H1NE 1996061300452 19960613 00452 SW 1996 6 13 HEEA967179 1 19960509 A 2436 206075447007 REGULATOR BELL 206 206L1 1182107 SW DC VOLTS MALFUNCTION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2775A 45297 LOAD METER DROPS WHEN VHF IS KEYED. 1 G 7 1 3U H2SW 1996061300453 19960613 00453 1996 6 13 HEEA967180 4 19960509 A 3454 066106701 RECEIVER KN53 BOLKMS 105 BO105S 5626006 EU COCKPIT VOR DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 54191 S804 VOR BEARING OUT OF TOLERANCE. 24 MONTH INSPECTION DUE. 1 G 7 2 3U H3EU 1996061300454 19960613 00454 SW 1996 6 13 HEEA967181 1 19960509 A 7714 8DJ81WBS4 INDICATOR BELL 206 206L1 1182107 SW GP RPM HANGS UP E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5005B 45175 GP INDICATOR GAUGE TENDS TO HANG UP BELOW 20%. 1 G 7 1 3U H2SW 1996061300455 19960613 00455 SW 1996 6 13 HEEA967182 1 19960509 A 7714 8DJ81WBS4 INDICATOR BELL 206 206L1 1182107 SW GP RPM DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 27702 45300 INDICATOR SLOW AND STICKING BETWEEN 0 TO 20%. 1 G 7 1 3U H2SW 1996061300456 19960613 00456 EU 1996 6 13 HEEA967184 1 19960509 A 2824 80030 VALVE AEROSP AS355 AS355F1 8680810 EU FUEL SYS DEFECTIVE E HEEA K NONE K FLUID LOSS NR NOT REPORTED 1 SW 03 5793Z 5142 LEAKING FROM #2 TO #1 ENGINE. 1 G 7 2 3U H11EU 1996061300457 19960613 00457 EU 1996 6 13 HEEA967185 1 19960509 A 2820 HTE9476 SWITCH BOLKMS 105 BO105S 5626006 EU FUEL SYS FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5368F S718 FUEL SWITCH INOPERATIVE. VALVE IS STICKING. 1 G 7 2 3U H3EU 1996061300458 19960613 00458 1996 6 13 HEEA967186 4 19960509 A 3421 222375033103 INDICATOR BELL 412 412 1182202 SW COCKPIT ATTITUDE PRECESSES E HEEA K NONE I FLT. ATTITUDE INST. NR NOT REPORTED 1 SW 03 107X 33113 ATTITUDE INDICATOR PRECESSES IN PITCH AND ROLL. 1 G 7 2 4U H4SW 1996061300459 19960613 00459 1996 6 13 HEEA967187 4 19960509 A 3421 222375033103 INDICATOR BELL 412 412 1182202 SW COCKPIT ATTITUDE MALFUNCTION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 107X 33113 WILL NOT REMAIN ERECT. 1 G 7 2 4U H4SW 1996061300460 19960613 00460 SW 1996 6 13 HEEA967188 1 19960509 A 7722 206075680105 INDICATOR BELL 206 206L1 1182107 SW COCKPIT TOT STICKS E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2251A 45755 INDICATOR STICKS AT ABOUT 530 DEGREES.----MODIFY TO P/N 206-075-680-103. 1 G 7 1 3U H2SW 1996061300461 19960613 00461 EU 1996 6 13 HEEA967189 1 19960509 A 6240 10594575 TRANSMITTER BOLKMS 105 BO105S 5626006 EU MAST MOMENT INTERMITTENT E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 721MB S752 TORQUE INTERMITTENT; NOT FUNCTIONING IN FLIGHT. 1 G 7 2 3U H3EU 1996061300462 19960613 00462 EU 1996 6 13 HEEA967190 1 19960509 A 6240 10594564 INDICATOR BOLKMS 105 BO105S 5626006 EU MAST MOMENT INTERMITTENT E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 721MB S752 MAST MOMENT INDICATOR INTERMITTENT; NOT FUNCTIONING IN FLIGHT. 1 G 7 2 3U H3EU 1996061300463 19960613 00463 SW 1996 6 13 HEEA967191 1 19960509 A 7722 35712519127 INDICATOR BELL 206 206B3 1181506 SW COCKPIT TOT STICKS E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2268W 3606 TOT NEEDLE STICKS THROUGHOUT RANGE. 1 G 7 1 3U H2SW 1996061300464 19960613 00464 EU 1996 6 13 HEEA967194 1 19960509 A 2121 TBL25 MOTOR BRAERO DH125 HS125700A 4230170 EU BLOWER BEARING FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 125CS NA0212 BLOWER MOTOR BEARING BAD. 2 L 7 2 4F A3EU 1996061300465 19960613 00465 EU 1996 6 13 HEEA967195 1 19960509 A 6123 AIR485431 REVERSING VALVE BRAERO DH125 HS125700A 4230170 EU ROD END LEAKS E HEEA K NONE K FLUID LOSS NR NOT REPORTED 1 SW 03 125CS NA0212 REVERSING VALVE LEAKS AT ROD END. 2 L 7 2 4F A3EU 1996061300466 19960613 00466 SW 1996 6 13 HEEA967196 1 19960509 A 6710 214001970111 ACTUATOR ASSY BELL 214 214ST 1182106 SW M/R DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 8045T 28101 MONITOR TEST MALFUNCTION MOTOR OR MAG BREAK DRAGGING. 2 G 7 2 4U H10SW 1996061300467 19960613 00467 SW 1996 6 13 HEEA967197 1 19960509 A 2435 214060056103 STARTER BELL 214 214ST 1182106 SW ENG FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3897N 142 28106 STARTER SPINS, BUT SPLINES DO NOT ENGAGE ENGINE. 2 G 7 2 4U H10SW 1996061300468 19960613 00468 SW 1996 6 13 HEEA967198 1 19960509 A 7722 206075680103 INDICATOR BELL 206 206B3 1181506 SW COCKPIT TOT STICKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 NEEDLE STICKING AT 400 DEGREES. 1 G 7 1 3U H2SW 1996061300469 19960613 00469 1996 6 13 HEEA967199 4 19960509 A 3416 54025100034 ALERTER BEECH 200 200CBEECH 1152926 CE COCKPIT ALTITUDE ERRATIC E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 39PH BL3 ERRATIC ALERTING, IT MIGHT TRIP 1000 FEET ABOVE OR BELOW. OR ANYWHERE IN BETWEEN. TIME SINCE REPAIR 176:40. 1 L 7 2 4T A24CE 1996061300470 19960613 00470 SW 1996 6 13 HEEA967200 1 19960509 A 6710 214001970111 ACTUATOR ASSY BELL 214 214ST 1182106 SW M/R DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 8045T 28101 PISTON HARD TO MOVE WITH BRAKE UNLOCKED. IN MONITOR TEST, PISTON EXTENDS PARTIALLY. 2 G 7 2 4U H10SW 1996061300471 19960613 00471 NE 1996 6 13 HEEA967201 1 19960509 A 3510 10C001616T CONVERTER SKRSKY S76 S76A 8143006 NE OXY SYS DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 911MJ 760231 VENTING LIQUID AND GAS CONTINUOUSLY FROM VENT UNTIL CONVERTOR EMPTIES. 1 G 7 2 3U H1NE 1996061300472 19960613 00472 SW 1996 6 13 HEEA967204 1 19960509 A 7120 206064105101 LEG ASSY BELL 206 206L1 1182107 SW ENG MOUNT BENT E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 LEG ASSEMBLY DOES NOT FITFIXTURE. (BENT) 1 G 7 1 3U H2SW 1996061300473 19960613 00473 1996 6 13 HEEA967205 4 19960509 A 2562 ELT910 ELT BELL 412 412 1182202 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 7128R 36007 SWITCH PANEL INDICATOR LITE GLOWS CONTINUALLY. 1 G 7 2 4U H4SW 1996061300475 19960613 00475 1996 6 13 HEEA967207 4 19960509 A 2312 069102505 TRANSCEIVER BELL 206 206L3 1182108 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 92MT 51175 RECEIVER SENSITIVITY BAD AND CONSTANT SQUELCH. 1 G 7 1 3U H2SW 1996061300476 19960613 00476 SO 1996 6 13 96ZZZM929 1 19960411 A 2752 3203001007 ACTUATOR EMB 120 EMB120RT SO TE FLAPS INOP A A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 267UE 0521 120071 ORD - CREW REPORTED A FLAP AYMMETRY AND CONTROL FAULT AFTER TAKEOFF. THEY ELECTED AN AIR TURN BACK AND MADE AN UNEVENTF UL LANDING. MAINTENANCE REMOVED AND REPLACED FCU AND RT OUTBOARD FLAP ACTUATOR. OPS CHECK WAS GOOD. REFERENCE GLBA960 71. 2 L 7 2 4T RT A31SO 1996061300478 19960613 00478 NM 1996 6 13 96ZZZM931 1 19960508 A 2910 AE2460010H0360 HOSE BOEING 727 72722C 138400F NM RT MLG RUPTURED A RYNA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CE 07 426EX 19089 AFTER TAKEOFF, THE 'A' SYSTEM HYDRAULIC POWER WAS LOST. THE LANDING GEAR WOULD NOT RETRACT. AIRCRAFT MADE AIR TURN BAC K TO IND. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND RIGHT MAIN LANDING GEAR RETRACT ACTUATOR HYDRAULIC FLEX LINE RUPTURE D. REPLACED DAMAGED FLEX LINE PER MM 32-30-00. LEAK CHECK GOOD. INSPECTED 'A' SYSTEM CASE DRAIN FILTERS AND SERVICED HYDRAULICS. 2 L 7 3 4F A3WE 1996061300479 19960613 00479 NM 1996 6 13 96ZZZM932 1 19960510 A 2611 302842 SMOKE DETECTORS BOEING 727 727222 1384073 NM CARGO COMPT FAILED A RYNA O OTHER N FALSE WARNING CR CRUISE 1 CE 07 7639U 19912 DURING CRUISE FROM DAY TO MCI AT FL 310, THE MAIN CARGO SMOKE DETECTOR LIGHT ILLUMINATED. COMPLIED WITH REQUIRED EMERGEN CY CHECKLIST. THE LIGHT EXTINGUISHED AT FL 120. AIRCRAFT LANDED AT MCI WITHOUT INCIDENT. NO EVIDENCE OF FIRE NOTED. R EPLACED SMOKE DETECTORS AT POSITIONS NR 1, NR 3, AND NR 5 PER MM 26-10-0. OPS CHECK GOOD. (M) 2 L 7 3 4F A3WE 1996061300480 19960613 00480 WP 1996 6 13 96ZZZM933 1 19960412 A 5330 SKIN DOUG DC6 DC6B 3021712 WP BS 875 CRACKED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 841TA 41260 44891 FOUND SKIN CRACKED, FS 875, RIGHT LONGERON 4. REWORKED, IAW SRM 12-56. 2 L 7 4 4R 6A4 1996061300481 19960613 00481 WP 1996 6 13 96ZZZM934 1 19960412 A 5330 SKIN DOUG DC6 DC6B 3021712 WP BS 822 CRACKED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 841TA 41260 44891 FOUND SKIN CRACKED, FS 822, LEFT LONGERON 1 TO 2. REWORKED, IAW SRM 12-56. 2 L 7 4 4R 6A4 1996061300482 19960613 00482 WP 1996 6 13 96ZZZM935 1 19960412 A 5330 SKIN DOUG DC6 DC6B 3021712 WP BS 736 CRACKED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 841TA 41260 44891 FOUND SKIN CRACKED, FS 736 RIGHT LONGERON 4 TO 6. REWORKED, IAW SRM 12-56. 2 L 7 4 4R 6A4 1996061300483 19960613 00483 WP 1996 6 13 96ZZZM936 1 19960412 A 5330 SKIN DOUG DC6 DC6B 3021712 WP BS 736 CRACKED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 841TA 41260 44891 FOUND SKIN CRACKED, FS 736 RIGHT LONGERON 4. REWORKED, IAW 12-56. 2 L 7 4 4R 6A4 1996061300484 19960613 00484 WP 1996 6 13 96ZZZM937 1 19960412 A 5330 SKIN DOUG DC6 DC6B 3021712 WP BS 541 CRACKED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 841TA 41260 44891 FOUND SKIN CRACKED, FS 541 LEFT LONGERON 4. REWORKED, IAW SRM 12-56. 2 L 7 4 4R 6A4 1996061300485 19960613 00485 WP 1996 6 13 96ZZZM938 1 19960412 A 5330 SKIN DOUG DC6 DC6B 3021712 WP BS 541 CRACKED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 841TA 44891 FOUND SKIN CRACKED, FS 541 RIGHT LONGEROON 4. REWORKED, IAW SRM 12-55. 2 L 7 4 4R 6A4 1996061300486 19960613 00486 WP 1996 6 13 96ZZZM939 1 19960412 A 5330 SKIN DOUG DC6 DC6B 3021712 WP BS 500 CRACKED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 841TA 41260 44891 FOUND SKIN CRACKED, FS 500 LEFT LONGERON 4. REWORKED, IAW SRM 12-56. 2 L 7 4 4R 6A4 1996061300487 19960613 00487 WP 1996 6 13 96ZZZM940 1 19960412 A 5330 SKIN DOUG DC6 DC6B 3021712 WP BS 380 CRACKED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 841TA 41260 44891 FOUND SKIN CRACKED, FS 380 LEFT LONGERON 4. REWORKED, IAW SRM 12-55. 2 L 7 4 4R 6A4 1996061300488 19960613 00488 WP 1996 6 13 96ZZZM941 1 19960412 A 5330 SKIN DOUG DC6 DC6B 3021712 WP BS 380 CRACKED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 841TA 41260 44891 FOUND SKIN CRACKED, FS 380 RIGHT LONGERON 4. REWORKED, IAW SRM 12-56. 2 L 7 4 4R 6A4 1996061300489 19960613 00489 WP 1996 6 13 96ZZZM942 1 19960412 A 5330 SKIN DOUG DC6 DC6B 3021712 WP BS 360 CRACKED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 841TA 41260 44891 FOUND SKIN CRACKED, FS 360 RIGHT LONGERON 4. REWORKED, IAW SRM 12-55. 2 L 7 4 4R 6A4 1996061300490 19960613 00490 WP 1996 6 13 96ZZZM943 1 19960412 A 5330 SKIN DOUG DC6 DC6B 3021712 WP BS 340 CRACKED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 841TA 41260 44891 FOUND SKIN CRACKED, FS 340 RIGHT LONGERON 4 TO 7. REWORKED, IAW SRM 12-55. (M) 2 L 7 4 4R 6A4 1996061300491 19960613 00491 WP 1996 6 13 96ZZZM944 1 19960412 A 5330 SKIN DOUG DC6 DC6B 3021712 WP BS 295 CRACKED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 841TA 41260 44891 FOUND SKIN CRACKED, FS 295 RIGHT LONGERON 4. REWORKED, IAW SRM 12-56. (M) 2 L 7 4 4R 6A4 1996061300492 19960613 00492 WP 1996 6 13 96ZZZM945 1 19960412 A 5330 SKIN DOUG DC6 DC6B 3021712 WP BS 295 CRACKED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 841TA 41260 44891 FOUND SKIN CRACKED, FS 295 LEFT LONGERON 4. REWORKED, IAW SRM 12-56. 2 L 7 4 4R 6A4 1996061300493 19960613 00493 WP 1996 6 13 96ZZZM946 1 19960412 A 5330 SKIN DOUG DC6 DC6B 3021712 WP BS 200 CRACKED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 841TA 41260 44891 FOUND SKIN CRACKED, FS 200 RIGHT LONGERON 4 TO 5. REWORKED, IAW SRM 12-56. 2 L 7 4 4R 6A4 1996061300494 19960613 00494 WP 1996 6 13 96ZZZM947 1 19960412 A 5330 SKIN DOUG DC6 DC6B 3021712 WP BS 120 CRACKED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 841TA 41260 44891 FOUND SKIN CRACKED, FS 120 RIGHT LONGERON 4. REWORKED, IAW SRM 12-56. 2 L 7 4 4R 6A4 1996061300495 19960613 00495 WP 1996 6 13 96ZZZM948 1 19960412 A 5330 SKIN DOUG DC6 DC6B 3021712 WP BS 99 CRACKED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 841TA 41260 44891 FOUND SKIN CRACKED, FS 99 RIGHT LONGERON 4. REWORKED, IAW SRM 12-56. 2 L 7 4 4R 6A4 1996061300496 19960613 00496 WP 1996 6 13 96ZZZM949 1 19960412 A 5330 SKIN DOUG DC6 DC6B 3021712 WP BS 69 CRACKED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 841TA 41260 44891 FOUND SKIN CRACKS, FS 69 LEFT LONGERON 4 TO 8. REWORKED, IAW SRM 12-56. 2 L 7 4 4R 6A4 1996061300497 19960613 00497 WP 1996 6 13 96ZZZM950 1 19960412 A 5330 SKIN DOUG DC6 DC6B 3021712 WP BS 843 CRACKED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 841TA 41260 44891 FOUND SKIN CRACKED, FS 843 LEFT LONGERON 31. REWORKED, IAW SRM 12-56. 2 L 7 4 4R 6A4 1996061300498 19960613 00498 WP 1996 6 13 96ZZZM951 1 19960412 A 5330 SKIN DOUG DC6 DC6B 3021712 WP BS 540 CORRODED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 841TA 41260 44891 FOUND SKIN BULGED, FS 540 LEFT LONGERON 18 TO 19. REWORKED, IAW SRM 12-56. 2 L 7 4 4R 6A4 1996061300499 19960613 00499 WP 1996 6 13 96ZZZM952 1 19960412 A 5330 SKIN DOUG DC6 DC6B 3021712 WP BS 515 CRACKED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 841TA 41260 44891 FOUND SKIN CRACKED, FS 515 LEFT LONGERON 13. REWORKED, IAW SRM 12-55. 2 L 7 4 4R 6A4 1996061300500 19960613 00500 WP 1996 6 13 96ZZZM953 1 19960412 A 5330 SKIN DOUG DC6 DC6B 3021712 WP BS 381 CORRODED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 841TA 41260 44891 FOUND SKIN BULGED, FS 381 RIGHT LONGERON 21. REWORKED, IAW SRM 12-56. 2 L 7 4 4R 6A4 1996061300501 19960613 00501 WP 1996 6 13 96ZZZM954 1 19960412 A 5313 LONGERON DOUG DC6 DC6B 3021712 WP BS 69 CORRODED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 841TA 41260 44891 FOUND CORROSION, FS 69 RIGHT LONGERON 24 TO 26. REWORKED, IAW SRM 12-56. 2 L 7 4 4R 6A4 1996061300502 19960613 00502 WP 1996 6 13 96ZZZM955 1 19960412 A 5330 SKIN DOUG DC6 DC6B 3021712 WP BS 69 CRACKED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 841TA 41260 44891 FOUND SKIN CRACKED, FS 69 LEFT LONGERON 16. REWORKED, IAW SRM 12-56. 2 L 7 4 4R 6A4 1996061300503 19960613 00503 WP 1996 6 13 96ZZZM956 1 19960412 A 5330 SKIN DOUG DC6 DC6B 3021712 WP BS 69 CRACKED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 841TA 41260 44891 FOUND SKIN CRACKED, FS 69 LEFT LONGERON 20 TO 21. REWORKED IAW SRM 12-56. 2 L 7 4 4R 6A4 1996061300504 19960613 00504 WP 1996 6 13 96ZZZM957 1 19960412 A 5330 SKIN DOUG DC6 DC6B 3021712 WP BS 69 CORRODED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 841TA 41260 44891 FOUND CORROSION, SKIN LAP FS 69 LEFT LONGERON 25 TO 26. REWORKED, IAW SRM 12-56. 2 L 7 4 4R 6A4 1996061300505 19960613 00505 WP 1996 6 13 96ZZZM958 1 19960508 A 2910 31220018CR0360 HYD LINE DOUG DC9 DC932 3022066 WP RT HYD SYST CHAFED A VJ6A O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 11 5342L 47278 FLT NR 340 - JAX-ATL - AT CRUISE ALTITUDE, THE RIGHT HYDRUALIC SYSTEM PRESSURE AND QUANTITY WENT TO ZERO. USED MANUAL G EAR EXTENSION AND ABNORMAL CHECK LIST, LANDED NORMALLY. FOUND HOLE CHAFFED IN AUX PUMP HYDRAULIC LINE. REMOVED AND REP LACED THE HYDRAULIC LINE AND SERVICED RIGHT HYDRAULIC SYSTEM TO PROPER LEVEL WITH SKYDROL, OPS CHECK SYSTEM WITH PRESSUR E ON. 2 L 7 2 4F A6WE 1996061300506 19960613 00506 WP 1996 6 13 96ZZZM959 1 19960410 A 3230 BYPASS HANDLE DOUG DC9 DC932 3022066 WP LANDING GEAR OUT OF POSITION A VJ6A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 946VV 47226 ON FLT 110 - ATL-ATL - AIR RETURN, LANDING GEAR WOULD NOT RETRACT. FOUND GEAR BYPASS HANDLE DOWN. REPLACED RT MAIN GEA R DOOR AND LEFT GEAR DOOR BUMPER. RESET BYPASS HANDLE, OPS CHECK NORMAL. 2 L 7 2 4F A6WE 1996061300507 19960613 00507 WP 1996 6 13 96ZZZM960 1 19960503 A 2120 5216030014 DUCT CONNECTOR DOUG DC9 DC932 3022066 WP TAIL COMPT FAILED A VJ6A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 966VV 47168 FLT 619 - BOS-BOS - AIR RETURN, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT CAME ON AFTER TAKEOFF. REMOVED AND REPLACED BLO WN DUCT CONNECTOR, LEAK CHECK OK. (M) 2 L 7 2 4F A6WE 1996061300508 19960613 00508 1996 6 13 96ZZZM961 4 19960505 A 3442 26071570153 RADAR UNIT DOUG DC9 DC932 3022066 WP FWD FUSELAGE FAILED A A VJ6A A UNSCHED LANDING O OTHER CL CLIMB 1 SO 11 938VV 47442 ON FLT 266 - IAD-CMH - AIR RETURN, THE WEATHER RADAR BEGAN SPOKING. REMOVED AND REPLACED RADAR R/T, SYSTEM OPS CHECKED NORMAL. 2 L 7 2 4F A6WE 1996061300509 19960613 00509 WP 1996 6 13 96ZZZM962 1 19960410 A 3231 UPLATCH SPRING DOUG DC9 DC931 3022065 WP RT MLG DOOR BROKEN A VJ6A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 960VV 47067 AFTER TAKEOFF FOR FLT 519, ATL-ATL, AIR RETURN, WHILE EXECUTING THE 'GEAR UPLATCH CHECK', THE 'RIGHT GEAR UNSAFE' LIGHT CAME ON COUPLED WITH THE 'GEAR DOOR OPEN' LIGHT. FOUND SPRING ON RT MAIN GEAR DOOR UPLATCH BROKEN. REMOVED AND REPLACE D SPRING GEAR DOOR AND LIGHTS. OPS CHECK OK. 2 L 7 2 4F A6WE 1996061300510 19960613 00510 WP 1996 6 13 96ZZZM963 1 19960502 A 7312 320115 FUEL HEAT VLV DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7B 52053 NE RIGHT MALFUNCTIONED A A VJ6A A UNSCHED LANDING O OTHER CL CLIMB 1 SO 11 932VV 47451 FLT NR 533 - ATL-MSY - AIR RETURN, THE FUEL HEAT LIGHT CAME ON SHORTLY AFTER TAKEOFF. THE RIGHT FUEL TEMP WENT TO 80 DE GREES WITHIN 10 MINUTES. THE OIL TEMP WAS 145 DEGREES FOR ONE MINUTE. THE AVERAGE OIL TEMP WAS 130 DEGREES. EXCEEDED 120 DEGREES FOR 15 MINUTES. REMOVED FUEL HEAT VALVE. OIL TEMP LIMITS PER MM 77-01 PG 508. 2 L 7 2 4F 4 F A6WE E2EA 1996061300511 19960613 00511 WP 1996 6 13 96ZZZM964 1 19960426 A 3260 DOOR SWITCH DOUG DC9 DC932 3022066 WP RT MLG OUT OF ADJUST A VJ6A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 11 903VJ 47261 ON FLT 585 - BOS-BOS - AIR RETURN, THE AIRCRAFT RETURNED FROM FLIGHT WITH GEAR DOOR WARNING LIGHT ON WITH GEAR UP. ADJU STED DOOR SWITCH ADJUSTMENT BOLT ON RIGHT MLG IAW MM 32-60-3. SWUNG GEAR, OPS CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 1996061300512 19960613 00512 NE 1996 6 13 96ZZZM965 2 19960510 A 7230 754130176008 IGV RAM LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B NE NR 3 ENG DEFECTIVE A A RIAA A E J UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL J M WARNING INDICATION OVER TEMP CL CLIMB 1 SO 19 764BE 765 193P1113 10628 ON RIA FLT NR 1683 LAS-FLL - DURING ROTATION NR 3 ENGINE HAD A PARTIAL POWER LOSS EPR DROPPED TO 1.160 WITH THROTTLE AT TAKEOFF POSITION, FUEL COMT AMP WAS PLACED TO OVRD AND TGT REACHED 700 DEGREES AT ONE-THIRD THROTTLE WITH N2 OVER 100 PE RCENT. ENGINE WAS THROTTLED BACK TO IDLE, AIRCRAFT DUMPED 35,000 LBS OF FUEL AND RETURNED TO LAS. IN LAS ON GROUND REP LACED MASTER AND SLAVE IGV RAMS AND PERFORMED ENGINE RUN PER MM 71-00-00 PG 515 THROUGH 524. GROUND CHECKED WITHIN LIMI TS. AIRCRAFT RELEASED FOR SERVICE. MASTER IGV RAM P/N 754-1-30176-008 S/N 765, SLAVE IGV RAM P/N 754-1-30175-004 S/N 3 05. 2 L 7 3 4F 4 F A23WE E12EU 1996061300513 19960613 00513 NE 1996 6 13 96ZZZM966 2 19960410 A 7200 ENGINE DOUG DC8 DC863 302198A WP PWA JT3D JT3D7 52039 NE NR 3 FAILED A RIAA E ENGINE SHUTDOWN J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SO 19 4935C 47755 45931 671378 RIA - FLT NR 1700 - LIRN-LICZ - SHUT DOWN NR 3 ENGINE DUE TO LOSS OF OIL PRESSURE. AIRCRAFT LANDED AT LICZ. ON INSPECT ION FOUND METAL IN TAILPIPE. AIRCRAFT WAS THREE ENGINE FERRIED TO MIAMI. NR 3 ENGINE WAS REPLACED. SUBMITTER STATES, SUSPECT 4 1/2 SCAVENGE PUMP FAILURE. 2 L 7 4 4F 4 F 4A25 1E8 1996061300514 19960613 00514 EU 1996 6 13 96ZZZM967 1 19960518 A 3232 125001 ACTUATOR FOKKER F28 F28MK4000 4990810 EU NLG FAILED A USAA O OTHER O OTHER CL CLIMB 1 EA 19 480AU 11229 CLT - FL 568 - NOSE GEAR RED DOOR LIGHT REMAINED ON AFTER GEAR RETRACTION. CREW ACCOMPLISHED ABNORMAL PROCEDURE. LIGHT WENT OUT AFTER GEAR WAS RECYCLED. MAINTENANCE REMOVED AND REPLACED THE FOLLOWING ITEMS; NOSE WHEEL STEERING SELECTOR, P/N 714540 AND NLG DOOR ACTUATOR, P/N 12500-1 AND NLG DOOR SELECTOR VALVE, P/N 71539 AND NLG SELECTOR VALVE, P/N 71538-1 . REFERENCE USAAF96047. 2 L 7 2 4F RT A20EU 1996061300515 19960613 00515 EU 1996 6 13 96ZZZM968 1 19960518 A 3231 71539 SELECTOR VLV FOKKER F28 F28MK4000 4990810 EU NLG DOORS FAILED A USAA O OTHER O OTHER CL CLIMB 1 EA 19 480AU 11229 CLT - FL 568 - NOSE GEAR RED DOOR LIGHT REMAINED ON AFTER GEAR RETRACTION. CREW ACCOMPLISHED ABNORMAL PROCEDURE. LIGHT WENT OUT AFTER GEAR WAS RECYCLED. MAINTENANCE REMOVED AND REPLACED THE FOLLOWING ITEMS; NOSE WHEEL STEERING SELECTOR, P/N 714540 AND NLG DOOR ACTUATOR, P/N 12500-1 AND NLG DOOR SELECTOR VALVE, P/N 71539 AND NLG SELECTOR VALVE, P/N 71538-1 . REFERENCE USAAF96047. 2 L 7 2 4F RT A20EU 1996061300516 19960613 00516 EU 1996 6 13 96ZZZM969 1 19960518 A 3231 71381 SELECTOR VLV FOKKER F28 F28MK4000 4990810 EU NLG DOORS FAILED A USAA O OTHER O OTHER CL CLIMB 1 EA 19 480AU 11229 CLT - FL 568 - NOSE GEAR RED DOOR LIGHT REMAINED ON AFTER GEAR RETRACTION. CREW ACCOMPLISHED ABNORMAL PROCEDURE. LIGHT WENT OUT AFTER GEAR WAS RECYCLED. MAINTENANCE REMOVED AND REPLACED THE FOLLOWING ITEMS; NOSE WHEEL STEERING SELECTOR, P/N 714540 AND NLG DOOR ACTUATOR, P/N 12500-1 AND NLG DOOR SELECTOR VALVE, P/N 71539 AND NLG SELECTOR VALVE, P/N 71538-1 . REFERENCE USAAF96047. 2 L 7 2 4F RT A20EU 1996061300517 19960613 00517 EU 1996 6 13 AALA960714 1 19960501 A 5320 BRACKET AIRBUS 300 A300B4605R 3930308 EU BS 3971 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80058 466 TUL - FOUND CORROSION AT FWD LOWER STOP BRACKET ON DOOR JAMB OF AFT CARGO DOORWAY. INSTALLED NEW SERVICEABLE STOP BRACK ET AT LOWER FWD DOOR JAMB PER SRM 51-74-10. (M) 2 L 7 2 4F RT A35EU 1996061300518 19960613 00518 EU 1996 6 13 AALA960715 1 19960503 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU BS 1870-1923 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80058 466 TUL - FOUND CORROSION ON SEAT TRACK NR 8, MOST RIGHT, ON LUGS AND DOWN INSIDE TRACK STATION 1870-1923. REMOVED AND REPL ACED SEAT TRACK FROM FRAME 25-34 PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 1996061300519 19960613 00519 NM 1996 6 13 AALA960716 1 19960610 A 5330 SKIN BOEING 727 727227 1384078 NM BS 660 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 731AA 20738 TUL - FOUND SKIN BULGED STATION 660 AND STRINGER 28 RT. CUT OUT CORRODED AREA AND INSTALLED SKIN DOUBLER AND STRINGER S ECTION PER SRM 53-30-3 P 1-10 53-10-3 PAGE 1-10. (M) 2 L 7 3 4F A3WE 1996061300520 19960613 00520 EU 1996 6 13 AALA960717 1 19960503 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU BS 1976 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80058 466 TUL - FOUND CORROSION ON SEAT TRACK AND NR 8 AT STATION 1976, MOST RIGHT. REMOVED AND REPLACED SEAT TRACK FROM FRAME 25 -34, PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 1996061300521 19960613 00521 EU 1996 6 13 AALA960718 1 19960503 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU BS 1976-2029 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80058 466 TUL - FOUND CORROSION AND PITS ON NR 8 SEAT TRACK MOST RIGHT STATION 1976-2029. REMOVED AND REPLACED SEAT TRACK FROM FR AME 25-34 PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 1996061300522 19960613 00522 EU 1996 6 13 AALA960726 1 19960505 A 3110 6227477401MOD6 INSTR PANEL FOKKER F28 F28MK0100 4990807 EU COCKPIT DEFECTIVE A AALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 1451N 11460 ORD - FLT 1140 - AFTER TAKEOFF AUS, ELECTRICAL ODOR/SMOKE NOTED AT WINDSHIELD. SHUT OFF BOTH AUTO-THROTTLES AND ODOR/SM OKE DISAPPEARED WITH NO OTHER ABNORMAL INDICATIONS. AIRCRAFT PROCEEDED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED FL IGHT MODE PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION WITH NO ODOR/SMOKE NOTED. (M) 2 L 7 2 4F RT 1996061300523 19960613 00523 EU 1996 6 13 AALA960732 1 19960505 A 5320 A53981929202 ATTACH SECTION AIRBUS 300 A300B4605R 3930308 EU FRAME 76-78 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80058 466 TUL - FOUND CORROSION AT N/P HOLES IN ATTACH SECTION. REPLACED ATTACH SECTION PER SRM 51-71-50. (M) 2 L 7 2 4F RT A35EU 1996061300524 19960613 00524 EU 1996 6 13 AALA960733 1 19960506 A 5754 A57241993202 ANGLE AIRBUS 300 A300B4605R 3930308 EU WS 71 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80058 466 TUL - FOUND RIB ANGLE OUTBOARD OF KRUGER FLAP CRACKED (OUTBOARD OF ACTUATOR). INSTALLED REPAIR DOUBLER PER ESO 30595, D ATED 10-4-95. (M) 2 L 7 2 4F RT A35EU 1996061300525 19960613 00525 EU 1996 6 13 AALA960734 1 19960506 A 5320 FITTING AIRBUS 300 A300B4605R 3930308 EU FRAME 45 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80058 466 TUL - FOUND 1 INCH CRACK RUNS PERPENDICULAR TO FITTING JUST BELOW CENTER TANK. DOUBLER INSTALLED PER ESO 30595. (M) 2 L 7 2 4F RT A35EU 1996061300526 19960613 00526 WP 1996 6 13 AALA960735 1 19960507 A 5320 LAV SERVICE PNL DOUG DC9 DC982 3022082 WP BS 1287-1308 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 288AA 49300 TUL - FOUND HEAVY CORROSION ON INSIDE OF AFT LAV SERVICE PAN. INSTALLED DOUBLER PER ESO80559 DATED 5-3-96. (M) 2 L 7 2 4F A6WE 1996061300527 19960613 00527 WP 1996 6 13 AALA960738 1 19960506 A 5320 ANGLE DOUG DC10 DC1010 3022110 WP WHEEL WELL CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 TUL - FOUND HEAVY CORROSION ON SLANT PANEL ATTACH ANGLE 6 AT LOWER INBOARD CORNER. TREATED PRIMED AND APPLIED DINATSOL AV 40 TO SLANT PANEL ATTACH ANGLE AT LOWER INBOARD CORNER PER ESO 7349 DATED 05-02-96. (M) 2 L 7 3 4F A22WE 1996061300528 19960613 00528 NM 1996 6 13 AALA960741 1 19960506 A 5751 65217097 FITTING BOEING 727 727223 1384074 NM AILERON CONTL CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 882AA 21521 TUL - FOUND INBOARD AILERON QUADRANT HAS HEAVY CORROSION. REMOVED AND INSTALLED NEW QUANDRANT MOUNT CASTING. (M) 2 L 7 3 4F A3WE 1996061300529 19960613 00529 NM 1996 6 13 AALA960742 1 19960506 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 375 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 882AA 21521 TUL - FOUND RIGHT INBOARD SEAT TRACK HAD CORROSION AT AFT TIE DOWN FITTING OF FWD GALLEY. REPLACED SEAT TRACK, STATION 348 TO STATION 400. (M) 2 L 7 3 4F A3WE 1996061300530 19960613 00530 WP 1996 6 13 AALA960752 1 19960503 A 5312 BULKHEAD DOUG DC9 DC982 3022082 WP BS 1309 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 464AA 49594 TUL - FOUND CORROSION ON FWD SIDE OF BULKHEAD STATION 1309 LEFT AT BOTTOM OF BULKHEAD BETWEEN NR 1 AND NR 2 SEAT TRACKS. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-01. (M) 2 L 7 2 4F A6WE 1996061300531 19960613 00531 WP 1996 6 13 AALA960753 1 19960508 A 5320 ROLLER TRAY DOUG DC10 DC1010 3022110 WP BS 630 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 TUL - FOUND CORROSION INSIDE ROLLER TRAY. SPLICE IN NEW SECTION OF ROLLER TRAY FROM 625 TO 640 PER SRM 53-10-00, FIG 17 . (M) 2 L 7 3 4F A22WE 1996061300532 19960613 00532 WP 1996 6 13 AALA960754 1 19960508 A 5320 PANEL DOUG DC10 DC1010 3022110 WP BS 744 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 TUL - FOUND CORROSION ON ROLLER TRACK NR 1 ON SLANTED PANEL LANDING BETWEEN STATION 740-748. FABRICATED ANGLE DOUBLER T REATED, PRIMED PAINTED AND INSTALLED REPAIR PER SRM 53-70-00, PAGE 63. (M) 2 L 7 3 4F A22WE 1996061300533 19960613 00533 WP 1996 6 13 AALA960758 1 19960509 A 5320 ROLLER TRAY DOUG DC10 DC1010 3022110 WP BS 690 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 TUL - FOUND CORROSION INSIDE ROLLER TRAY LEFT NR 1. SPLICED IN NEW SECTION OF ROLLER TRAY FROM A/C STATION 625 TO 730 P ER SRM 53-70-00 PG 63, ALODINED, PRIMED AND PAINTED. (M) 2 L 7 3 4F A22WE 1996061300534 19960613 00534 WP 1996 6 13 AALA960759 1 19960509 A 5320 4933783A SUPPORT DOUG DC10 DC1010 3022110 WP BS 861 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 TUL - INBOARD AFT TIE DOWN FOR THE RIGHT MID LAV IS CORRODED. REPLACED TWO FLOORBOARDS AND THE LAV FLOORBEAM PER SRM 53 -00-01. (M) 2 L 7 3 4F A22WE 1996061300536 19960613 00536 EU 1996 6 13 AALA960761 2 19960509 A 7320 CASC509 REGULATOR FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAYMK65015 EU NR 2 POS DEFECTIVE A AALA E ENGINE SHUTDOWN X ENGINE FLAMEOUT DE DESCENT 1 SW 07 1428D 11413 ORD - FLT 1552 - DURING DESCENT INTO ORD, PASSING THROUGH FL 330 WITH LEFT AIRFRAME/ENGINE ANTI-ICE ON, NR 2 ENGINE ROLL ED BACK WITH CORRESPONDING EICAS MESSAGE. ENGINE RE-START PROCEDURE SUCCESSFUL AND AIRCRAFT LANDED ORD WITHOUT INCIDENT . REPLACED NR 2 ENGINE FUEL FLOW AND AIR FLOW REGULATORS. ACCOMPLISHED ENGINE RIG AND TRIM. ENGINE LEAK AND GROUND CH ECKED NORMAL OPERATION. (M0 2 L 7 2 4F 4 F RT 1996061300537 19960613 00537 EU 1996 6 13 AALA960762 1 19960510 A 3231 715391 VALVE FOKKER F28 F28MK0100 4990807 EU NLG DOOR DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 1436A 11426 DFW - FLT 1139 - AFTER TAKEOFF DFW WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR CONTINUED TO INDICATE AMBER. RECYCLED LANDING GEAR WITH SAME RESULTS. EXTENDED LANDING GEAR AND AIRCRAFT RETURNED TO DFW, LANDING OVERWEIGHT WITHOUT INCIDEN T. REPLACED NOSE LANDING GEAR DOOR SELECTOR VALVE. ACCOMPLISHED LEAK CHECK AND LANDING GEAR RETRACTION CHECK WITH NO D EFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION WITH NO DEFECTS FOUND . (M) 2 L 7 2 4F RT 1996061300538 19960613 00538 WP 1996 6 13 AALA960774 1 19960515 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 1789 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 TUL - FOUND CENTER CARGO AFT BULKHEAD FRAME CORRODED ON TOP FLANGE AT NR 3 ROLLER TRAY ATTACH POINT. REMOVED CORROSION OF BLENDED AREA. ALODINED AND PRIMED BARE AREAS. FABRICATED AND INSTALLED DOUBLER PER SRM 53-60-01. (M) 2 L 7 3 4F A22WE 1996061300539 19960613 00539 WP 1996 6 13 AALA960775 1 19960514 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 886 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 TUL - FOUND LONGERON 52 HAS CORROSION ON SIDES, AT FUSELAGE SKIN ATTACH AREA. INSTALLED NEW SECTION OF LONGERON 52 WITH TWO LONGERON SPLICES PER SRM 53-10-00 FIG 2. (M) 2 L 7 3 4F A22WE 1996061300540 19960613 00540 NM 1996 6 13 ASAA9610050 1 19960411 A 5315 65549051 FLOOR BEAM BOEING 737 737298C 1384490 NM BS 400 CORRODED A ASAA O OTHER O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING C-CHECK, CORROSION WAS FOUND ON THE FLOOR BEAM BS 400, RBL 41 ON THE LOWER SURFACE OF THE AFT UPPER FLANGE. REPAIRED PER EA 5310-01434 AND BOEING TELEX ASA-SEA-960177RR. (M) 2 L 7 2 4F RT A16WE 1996061300541 19960613 00541 WP 1996 6 13 CAL960578 1 19960417 A 5230 59101577 PAN DOUG DC9 DC983 3022083 WP BAG BIN DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14879 29047 49526 HOU - INSPECTION FOUND A 2 INCH CRACK IN PAN AT AFT LATCH OF FORWARD BAG BIN DOOR. A DOUBLER REPAIR WAS INSTALLED IAW E CRA 5210-01251. (M) 2 L 7 2 4F RT A6WE 1996061300542 19960613 00542 NM 1996 6 13 F3LA96013 1 19960521 A 3350 CONNECTOR BOEING 737 737201 1384454 NM CABIN DIRTY A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 207AU 19423 MSP - DURING SERVICE CHECK, MAINTENANCE REPORTED LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. CLEANED LIGH T ASSEMBLY CONTACTS AND CHECKED OK. (M) 2 L 7 2 4F A16WE 1996061300543 19960613 00543 SO 1996 6 13 GLBA96071 1 19960411 A 2750 3472001001 FCU EMB 120 EMB120RT SO TE FLAPS INOP A A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 267UE 0202 120071 ORD - CREW REPORTED A FLAP ASYMMETRY AND CONTROL FAULT AFTER TAKEOFF. THEY ELECTED AND AIR TURN BACK AND MADE AN UNEVEN TFUL LANDING. MAINTENANCE REMOVED AND REPLACED FCU AND RT OUTBOARD FLAP ACTUATOR. OPS CHECK WAS GOOD. (M) 2 L 7 2 4T RT A31SO 1996061300544 19960613 00544 SO 1996 6 13 GLBA96072 1 19960417 A 3233 1959500004 ACTUATOR EMB 120 EMB120RT SO RT MLG OUT OF ADJUST A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 129AM 120119 SAV - CREW REPORTED RIGHT MAIN GEAR WOULD NOT RETRACT FOLLOWING TAKEOFF. THEY MADE AN AIR TURN BACK AND AN UNEVENFUL LA NDING. MAINTENANCE ADJUSTED RIGHT MAIN LANDING GEAR ACTUATOR. OPS CHECK WAS GOOD. (M) 2 L 7 2 4T RT A31SO 1996061300545 19960613 00545 SO 1996 6 13 GLBA96073 1 19960418 A 5230 MS250851 SWITCH EMB 120 EMB120RT SO CARGO DOOR OUT OF ADJUST A GLBA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 01 267UE 120071 ORD - CREW REPORTED, CARGO DOOR ANNUNCIATOR ILLUMINATED DURING TAKEOFF ROLL. CREW ELECTED TO ABORT TAKEOFF AND RETURNED TO GATE. MAINTENANCE ADJUSTED MICROSWITCHES ON CARGO DOOR. OPS CHECK WAS GOOD. (M) 2 L 7 2 4T RT A31SO 1996061300546 19960613 00546 CE 1996 6 13 GLBA96074 1 19960418 A 2460 1013647151 BUS TIE CONTL BEECH 1900 1900C 1154161 CE CENTER AISLE OPEN CIRCUIT A GLBA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 01 130UE UC130 SPI - CREW REPORTED, LEFT GENERATOR ANNUNICATOR ILLUMINATED WHILE TAXIING AND THEY RETURNED TO GATE. MAINTENANCE REMOVE D AND REPLACED BUS TIE CONTROL PRINTED CIRCUIT BOARD. OPS CHECK WAS GOOD. (M) 2 L 7 2 4T RT A24CE 1996061300547 19960613 00547 CE 1996 6 13 GLBA96078 1 19960429 A 7931 OIL PRESS IND BEECH 1900 1900C 1154161 CE RT ENGINE MALFUNCTIONED A GLBA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 01 150UE UC150 TUS - CREW REPORTED RT OIL PRESSURE DROPPED TO 40 PSI AFTER TAKEOFF. THEY PERFORMED AN AIR TURN BACK AND MADE AN UNEVEN TFUL LANDING. MAINTENANCE INSPECTED AIRCRAFT AND MADE GROUND RUN, BUT COULD NOT DUPLICATE OIL PRESSURE FLUCTUATION. (X ) 2 L 7 2 4T RT A24CE 1996061300548 19960613 00548 WP 1996 6 13 GRAA9629 1 19960512 A 3350 6011775 POWER SUPPLY DOUG DC9 DC915 3022036 WP CABIN INOPERATIVE A GRAA K NONE L NO TEST IN INSP/MAINT 1 WP 11 1070T 45784 LINE MAINTENANCE AT RNO, DISCOVERED THAT THE RIGHT NACELLE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REP LACED THE RIGHT NACELLE EMERGENCY BATTERY POWER SUPPLY. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIG HT SYSTEM. NO DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1996061300549 19960613 00549 WP 1996 6 13 HALA9657 1 19960502 A 5330 SKIN DOUG DC9 DC951 3022051 WP BS 1111 DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 420EA 47689 HNL - IN C-CHECK, FOUND 2 FASTENERS PULLED THROUGH ON FUSELAGE SKIN NEAR AFT CARGO DOOR AT STATION 1111 AT LONGERON 28R. SKIN BULGING, CORROSION LEVEL 2. MADE INTERIM REPAIR PER HAL M105, CUT OUT CORROSION, FABRICATED DOUBLER, FILLER AND INSTALLED PER DAC TELEX SVC-HNL-004/KJL DATED APR 25, 1996. PERMANENT REPAIR TO BE ACCOMPLISHED MARCH 25, 1997. (M) 2 L 7 2 4F A6WE 1996061300550 19960613 00550 WP 1996 6 13 HALA9658 1 19960425 A 5330 SKIN DOUG DC9 DC951 3022051 WP FUSELAGE CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 420EA 47689 HNL - IN C-CHECK, FOUND LOWER FUSELAGE SKIN BELOW AND UNDER FORWARD CARGO DOOR SCUFF PLATE HAS MODERATE CORROSION, LEVEL 2. MADE REPAIR PER HAL M105, CUT OUT CORROSION, FABRICATED EXTERNAL AND INTERNAL DOUBLER, FILLER AND INSTALLED PER HNL -SVC-060/RPM DATED APR 19, 1996. (M) 2 L 7 2 4F A6WE 1996061300551 19960613 00551 WP 1996 6 13 HALA9659 1 19960507 A 2923 BOLT DOUG DC10 DC1010 3022110 WP HYDRAULIC PUMP SHEARED A A HALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 13 151AA 46706 LAX - FLT NR 9 - LOSS OF ALL HYDRAULIC FLUID IN SYSTEM 3 ON CLIMB-OUT. RETURNED TO LAX FOR LANDING. FOUND 2 SHEARED BO LTS ON HORIZONTAL STAB TRIM AUX HYD PUMP. REMOVED AND REPLACED HYDRAULIC MOTOR. OPS CHECK, LEAK CHECK OK. SERVICED NR 3 SYSTEM TO REQUIRED LEVEL. (M) 2 L 7 3 4F A22WE 1996061300552 19960613 00552 WP 1996 6 13 HALA9664 1 19960518 A 3260 49319272 UPLOCK GUIDE DOUG DC9 DC951 3022051 WP LT MLG BENT A S HALA O OTHER N FALSE WARNING CL CLIMB 1 WP 13 601AP 47658 HNL - FLT 317 - GEAR UPLATCH FAILED TWICE ON CLIMB-OUT. RED LEFT GEAR UNSAFE LIGHT CAME ON. STRAIGHTENED AND SECURED L EFT GEAR UPLOCK ACTUATOR GUIDE AND SPRING. CLEANED ALL PROX SENSORS. GEAR SWING CHECKED OK. (M) 2 L 7 2 4F A6WE 1996061300553 19960613 00553 WP 1996 6 13 IXXA9678 1 19960508 A 3231 510361 TELESCOPING LINK DOUG DC8 DC871F 302199D WP RT NLG DOOR NOT LATCHED A IXXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 11 828BX 45993 ON DEPARTURE OUT OF BFI, THE RIGHT NLG DOOR DID NOT CLOSE AFTER GEAR RETRACTION. THE GEAR WAS CYCLED, BUT THE PRESENCE OF THE BUFFETING FROM THE DOOR INDICATED THAT IT WAS STILL OPEN. THE AIRCRAFT RETURNED TO BFI FOR MAINTENANCE. AT BFI THE NOSE GEAR DOORS WERE INSPECTED AND OPERATIONALLY CHECKED IAW THE DC-8MM 32-22-1, AND FOUND TO BE NORMAL. THE RIGHT NLG DOOR DID NOT CLOSE ON TAKEOFF EITHER BECAUSE THE TELESCOPING LINK WAS NOT FULLY LATCHED, OR BECAUSE IT WAS NOT LATCH ED AT ALL. (M) 2 L 7 4 4F RT 4A25 1996061300554 19960613 00554 WP 1996 6 13 IXXA9679 1 19960517 A 2120 AIR DISTR DOUG DC8 DC871 302199A WP CABIN ODOR A IXXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 11 829BX 45994 IN CRUISE BETWEEN BFI AND TOL, IT WAS NOTED THAT A SMOKEY OR OILY SMELL WAS COMING OUT OF THE AIR CONDITIONING SYSTEM IN THE COCKPIT AND COURIER AREAS. IN TOL, MAINTENANCE CLEANED THE RECIRC FAN SCREEN, SERVICED THE LAV, AND RAN THE AIR CO NDITIONING PACKS. NO ABNORMAL ODORS WERE NOTED. (M) 2 L 7 4 4F 4A25 1996061300555 19960613 00555 NE 1996 6 13 M3HA96011 2 19960509 A 7261 OIL CAP AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE NR 1 ENG LOOSE A M3HA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 13 4206G 081 HNL - FLT 702 - ON TAKEOFF ROLL FROM HNL, THE CREW NOTICED THAT THE NR 1 ENG OIL PRESSURE WAS LOW. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE MAINTENANCE LINE. UPON INSPECTION OF THE NR 1 ENGINE, THE OIL TANK OIL CAP WAS FOUND TO BE LOOSE. THE ENGINE WAS RESERVICED, AND A ENGINE RUN UP WAS PERFORMED, WITH NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVIC E. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1996061300556 19960613 00556 EU 1996 6 13 M3HA96012 1 19960521 A 3350 POWER SUPPLY AEROSP ATR42 ATR42300 8680920 EU CABIN INOPERATIVE A M3HA K NONE L NO TEST IN INSP/MAINT 1 WP 13 4202G 050 HNL - FLT 721 - EMERGENCY BATTERY LIGHT STAYED ON AFTER SHUT DOWN. REMOVED AND INSTALLED A NEW EMERGENCY POWER SUPPLY U NIT IAW JIC 33-51-21 RAI 1000-001. (M) 2 H 7 2 4T RT A53EU 1996061300557 19960613 00557 SW 1996 6 13 MALA964986 1 19960508 A 3260 1EN516 SWITCH SWRNGN SA227 SA227AC 8780603 SW RT MLG DIRTY A MALA A UNSCHED LANDING P NO WARNING INDICATION AP APPROACH 1 GL 15 428MA AC646 FLT NR 3182 - ON APPROACH TO DTW, THE RIGHT GEAR INTRANSIT LIGHT FAILED TO ILLUMINATE DURING GEAR EXTENSION. ALL OTHER INDICATIONS WERE NORMAL. MX CLEANED AND LUBED THE RIGHT OUTBOARD UPPER POSITION SWITCH. SYSTEM OPERATED SATISFACTORILY . (M) 2 L 7 2 4T RT A8SW 1996061300558 19960613 00558 WP 1996 6 13 MALA964990 2 19960512 A 7230 31011607 COMP SEAL SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE331* 01514 WP RT ENGINE LEAKING A MALA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 15 425MA AC640 FLT NR 3134 - AFTER TAKEOFF FROM MSP, THE CREW NOTED SMOKE IN THE COCKPIT AND CABIN. THE SMOKE DISSIPATED AFTER THE CRE W TURNED OFF THE BLEED AIR SYSTEMS. THE AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE COMPRESSOR SEAL ASSEMBLY. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2 L 7 2 4T 3 T RT A8SW E2WE 1996061300559 19960613 00559 NM 1996 6 13 MZZA96036 1 19960509 A 5610 57176244 SLIDING WINDOW BOEING 727 727224 1384076 NM RT COCKPIT OUT OF ADJUST A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 GUM - DURING TRAINING, FOUND FIRST OFFICERS SLIDING WINDOW WILL NOT OPEN WITH THE EMERGENCY EXTERIOR HANDLE. MAINTENANC E ADJUSTED THE LOWER FORWARD BELLCRANK. OPERATION CHECK GOOD PER MM 56-12-0 AND TESTED PER MM 56-12-11 PG 505 PARA B. ( M) 2 L 7 3 4F A3WE 1996061300560 19960613 00560 NM 1996 6 13 MZZA96037 1 19960428 A 5220 69459345 CABLE ASSEMBLY BOEING 727 727227 1384078 NM EMER EXIT STEP WIRE BROKEN A A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 89427 21365 DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, EXCESSIVE BROKEN WIRES WERE FOUND ON RT OVERWING EMERGENCY ESCAPE , HATCH STEP FORWARD CABLE. THE DAMAGED CABLE ASSEMBLY WAS REMOVED AND REPLACED PER B727 MM 52-21-0. REF HANGAR NON RO UTINE REPAIR ITEM CARD BR 818267 (SEQ NR 02187). (M) 2 L 7 3 4F A3WE 1996061300561 19960613 00561 NM 1996 6 13 MZZA96038 1 19960429 A 3350 EXIT SIGN COVER BOEING 727 727227 1384078 NM CABIN BROKEN A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 89427 21365 TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, BROKEN COVER WERE FOUND ON THE FOLLOWING POSITION 'EXIT' SI GN COVER; AFT ENTRY WAY, LT FORWARD EMERGENCY EXIT, RT AFT EMERGENCY EXIT DOOR. THE DAMAGED 'EXIT' SIGN ASSEMBLIES WERE REMOVED AND REPLCED WITH P/N BR9279-106 PER B727 MM 33-50-11 AN OPERATIONAL CHECK FOUND SATISFACTORY. HANGAR NON ROUTI NE REPAIR ITEM CARD NR 818288, 818289 AND 818291 (SEQ NR 02218, 02219, AND 02221). (M) 2 L 7 3 4F A3WE 1996061300562 19960613 00562 NM 1996 6 13 MZZA96039 1 19960429 A 3350 EXIT SIGN COVER BOEING 727 727227 1384078 NM BROKEN A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 89427 21365 TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, BROKEN COVERS WERE FOUND ON LT AFT EMEREGENCY EXIT DOOR 'EX IT' SIGN. THE DAMAGED 'EXIT' SIGN ASSEMBLY WAS REMOVED AND REPLACED WITH P/N BR9279-105 ASSEMBLY PER B727 MM 33-50-11 A ND OPERATIONAL CHECK FOUND SATISFACTORY. HANGAR NON ROUTINE REPAIR ITEM CARD NR 818290 (SEQ NR 02220) 2 L 7 3 4F A3WE 1996061300563 19960613 00563 NM 1996 6 13 MZZA96040 1 19960429 A 3350 10617891007 EMERGENCY SIGN BOEING 727 727227 1384078 NM EXIT DOOR DIM A MZZA K NONE L NO TEST IN INSP/MAINT 1 WP 13 89427 21365 DURING SELF ILLUMINATION SIGN BRIGHTNESS TEST PER QUARTER D-CHECK WORK CARD 07-1130-1-7301 ON AIRCRAFT AT AIR ASIA, LT/R T AFT EMERGENCY EXIT DOOR 'EMERGENCY' SIGN BRIGHTNESS MEASUREMENT WAS FOUND BELOW THE SPECIFIED LIMIT (100 MICROLAMBERTS ). THE 'EMERGENCY' SIGNS WERE REMOVED AND REPLACED PER B727 MM 33-50-31. HANGAR NON ROUTINE REPAIR ITEM CARD NR 806301 AND 806302 (SEQ NR 02231 AND 02232). 2 L 7 3 4F A3WE 1996061300564 19960613 00564 NM 1996 6 13 MZZA96041 1 19960429 A 3350 10617891008 PULL SIGN BOEING 727 727227 1384078 NM EXIT DOOR DIM A MZZA K NONE L NO TEST IN INSP/MAINT 1 WP 13 89427 21365 TNN - DURING SELF ILLUMINATION SIGN BRIGHTNESS TEST PER QUARTER D-CHECK WORK CARD 07-1130-1-7301 ON AIRCRAFT AT AIR ASIA , RIGHT AFT EMERGECNY EXIT DOOR 'PULL' SIGN BRIGHTNESS MEASUREMENT WAS FOUND BELOW THE SPECIFIED LIMIT (100 MICROLAMBERT S). THE 'PULL' SIGN WAS REMOVED AND REPLACED PER B727 MM 33-50-31. HANGAR NON ROUTINE REPAIR ITEM CARD NR 806302 (SEQ NR 02232) (M) 2 L 7 3 4F A3WE 1996061300565 19960613 00565 NM 1996 6 13 MZZA96042 1 19960430 A 5320 STIFFENER BOEING 727 727227 1384078 NM BS 1050-1070 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 89427 21365 TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT STIFFEN ER UPPER ANGLE AT STRINGER 26L BETWEEN BS 1050 AND BS 1070. THE CORRODED STIFFENER UPPER ANGLE WAS TRIMMED OUT 20 INCH LONG AND REPAIRED PER B72 SRM 51-40-3. HANGAR NON ROUTINE REPAIR ITEM CARD NR 806929 9SEN NR 01061). (M) 2 L 7 3 4F A3WE 1996061300566 19960613 00566 NM 1996 6 13 MZZA96043 1 19960426 A 5320 WEB BOEING 727 727227 1384078 NM AFT AIR STAIR OIL CANNING A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 89427 21365 TNN - DURING 1/4 D-CHECK INSPECTION, ON AIRCRAFT AT AIR ASIA, OIL CANNING WAS FOUND ON AFT AIRSTAIR RT/LT TORQUE BOX INB OARD WEB AT THE FOLLOWING AREA, RT SIDE BETWEEN BS 1243 AND 1253, LEFT SIDE BETWEEN BS 1223 AND 1233, LEFT SIDE BETWEEN BS 1233 AND 1243, LEFT 1243 AND 1253, LEFT SIDE BETWEEN BS 1263 AND 1273. THE AFT AIRSTAIR RT/LT TORQUE BOX INBOARD WEB OIL CANNING AREAS WERE INSTALLED REINFORCEMENT STIFFENER ANGLES PER B727 SRM 51-40-2. HANGAR NON ROUTINE REPAIR ITEM C ARD NR 819449, THROUGH 819453 (SEQ NR 02107, THROUGH 02110 AND 02131) (M) 2 L 7 3 4F A3WE 1996061300567 19960613 00567 NM 1996 6 13 MZZA96044 1 19960424 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 949 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 89427 21365 TNN - DURING 1/4D-CHECK INSPECTION, ON AIRCRAFT AT AIR ASIA, ONE INCH LONG CRACK WAS FOUND ON STRINGER 18A LEFT SIDE HOR IZONTAL FLANGE AT BS 949. THE INTERIM REPAIRED HAD BEEN ACCOMPLISHED PREVIOUSLY PER EC/RA 5310-03095. THE INTERIM REPA IRED WAS REMOVED AND REPLACED WITH PERMANENT REPAIRED PER EC/RA 5310-03096. (M) 2 L 7 3 4F A3WE 1996061300568 19960613 00568 NM 1996 6 13 MZZA96045 1 19960502 A 5713 STRINGER BOEING 727 727227 1384078 NM WS 629 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 89427 21365 TNN - DURING 1/4 D-CHECK, INSPECTION ON AIRCRAFT AT AIR ASIA, .5 INCH LONG CRACK WAS FOUND ON RIGHT OUTER WING UPPER ZEE STRINGER TO RIB ATTACHMENT AT WS 629, STRINGER 9. THE DAMAGED STRINGER WAS REPAIRED PER EA 5762-1050 (SB 727-57A159R5) . HANGAR NON ROUTINE REPAIR ITEM CARD NR 806629 (SEQ NR 06029) 2 L 7 3 4F A3WE 1996061300569 19960613 00569 NM 1996 6 13 MZZA96046 1 19960430 A 5310 FRAME BOEING 727 727227 1384078 NM BS 1166 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 89427 21365 TNN - DURING 1/4D-CHECK, INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FRAME A T BS 1166, STRINGER 27L. THE CORRODED FRAME WAS TREATED AND REPAIRED PER B727 SRM 51-10-6 AND 53-10-4. HANGAR NON ROUT INE REPAIR ITEM CARD NR 806921 (SEQ NR 01054). (M) 2 L 7 3 4F A3WE 1996061300570 19960613 00570 NM 1996 6 13 MZZA96047 1 19960426 A 5330 SKIN BOEING 727 727227 1384078 NM BS 720 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 89427 21365 TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON FUSELAGE SKIN BETWEEN BS 720B AND BS 720C AND BETWEEN STRINGER 28L AND STRINGER 28R FROMING THE MOUNTING FLANGE FOR THE RAM AIR DOOR ACTUATORS ACCESS PANEL. THE CORRODED SKIN WAS TREATED AND REPAIRED PER EC/RA 5330-2394. HANGAR NON ROUTINE REPAIR ITEM CARD NR 819193 (SEQ NR 01025). (M) 2 L 7 3 4F A3WE 1996061300571 19960613 00571 SO 1996 6 13 RAAAE896009 1 19960510 A 3350 1102832 LIGHT LKHEED 188 188C 5262604 SO CABIN FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 2 CHECK, OVERHEAD CENTER WING AFT EMERGENCY LIGHT FAILED TO ILLUMINATE ON TEST. CHANGED LIGHT ASSY. (M) 2 L 7 4 4T 4A22 1996061300572 19960613 00572 SO 1996 6 13 RAAAE896011 1 19960510 A 5312 BLKHD STIFFENER LKHEED 188 188C 5262604 SO BS 200 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 72630 188C2010 DURING SCHEDULED NR 2 CHECK, FOUND FS 200, LBL 7, BULKHEAD VERTICAL STIFFENER CORRODED AT STRINGER 38. REPAIRED PER SRM 51-3-7, FIG 1, SHT 2. (M) 2 L 7 4 4T 4A22 1996061300573 19960613 00573 SO 1996 6 13 RAAAE896012 1 19960510 A 5313 LONGERON LKHEED 188 188C 5262604 SO BS 478 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 72630 188C2010 DURING SCHEDULED NR 2 CHECK, FOUND LEFT BL 13.8 LONGERON CORRODED AT BS 478. REPAIRED PER LAC SWG 841501. (M) 2 L 7 4 4T 4A22 1996061300574 19960613 00574 SO 1996 6 13 RAAAE896013 1 19960510 A 5313 LONGERON LKHEED 188 188C 5262604 SO BS 497 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 72630 188C2010 DURING SCHEDULED NR 2 CHECK, FOUND LEFT BL 13.8 LONGERON CORRODED AT FS 497. REPAIRED PER LAC DWG 841501. (M) 2 L 7 4 4T 4A22 1996061300575 19960613 00575 SO 1996 6 13 RAAAE896014 1 19960510 A 5330 SKIN LKHEED 188 188C 5262604 SO BS 464-530 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 2 CHECK, FOUND FUSELAGE SKIN CORRODED AT FS 490 TO 502 AND STRINGER 39 TO 40. REMOVED AND REPLACED DOUBLER AND SKIN PANEL FS 464-530 AND STRINGER 36 TO 42 PER SRM 53-2-1, FIG 2. (M) 2 L 7 4 4T 4A22 1996061300576 19960613 00576 SO 1996 6 13 RAAAE896015 1 19960510 A 5330 SKIN LKHEED 188 188C 5262604 SO BS 977 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 72630 188C2010 DURING SCHEDULED NR 2 CHECK, FOUND FUSELAGE SKIN CORRODED AT FS 977 AND STRINGER 43 TO 50. REMOVED CORRODED SKIN, INSTA LLED FILLER AND REPAIR PLUTE PER SRM 53-2-1, FIG 2. (M) 2 L 7 4 4T 4A22 1996061300577 19960613 00577 SO 1996 6 13 RAAAE96010 1 19960510 A 5313 LONGERON LKHEED 188 188C 5262604 SO BS 437 DAMAGED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 72630 188C2010 DURING SCHEDULED NR 2 CHECK, FOUND RT BL 13.8 LONGERON DAMAGED AT FS 437. REPAIRED PER SB 651 AND LOCKHEED DWG 841501. (M) 2 L 7 4 4T 4A22 1996061300578 19960613 00578 EU 1996 6 13 RAIA960430 1 19960422 A 7712 MS3122E10 CONNECTOR BAG JETSTM JETSTM3201 1500217 EU COCKPIT DIRTY A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 422AM 856 SPI - FLT 7087 - LEFT ENGINE DID NOT MAKE TARGET TORQUE. CLEANED CANNON PLUG ON SRL COMPUTER. (M) 2 L 7 2 4T RT A56EU 1996061300579 19960613 00579 EU 1996 6 13 RAIA960437 1 19960428 A 3297 GA113 WIRE BAG JETSTM JETSTM3201 1500217 EU NLG BROKEN A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 423AM 858 STL - NR 7290 - LANDING GEAR FAILED TO RETRACT. MAINTENANCE REPAIRED GROUND WIRE FOR WEIGHT ON WHEELS SWITCH ON THE MAI N GROUND BUSS BAR. GEAR SWING CHECK GOOD. (M) 2 L 7 2 4T RT A56EU 1996061300580 19960613 00580 EU 1996 6 13 RAIA960441 1 19960429 A 2611 S5202007SN CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU SMOKE DETECTOR DIRTY A RAIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 03 550HK 3126 41039 BDI - FLT 7655 - MAIN BAGGAGE SMOKE DETECTOR LIGHT ILLUMINATED. CLEANED CANNON PLUG ON DETECTOR. (M) 2 L 7 2 4T RT A41NM 1996061300581 19960613 00581 EU 1996 6 13 RAIA960507 1 19960504 A 2150 F1897P05 DUCT BAG JETSTM JETSTM3201 1500217 EU LT PACK LOOSE A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 03 425AM 11144 870 JLN - FLT 7068 - SMOKE FUMES IN COCKPIT. SECURED DUCT ON ACM PACK. (M) 2 L 7 2 4T RT A56EU 1996061300582 19960613 00582 NE 1996 6 13 RAIA960508 2 19960506 A 7324 3033960 FLOW DIVIDER AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE NR 2 ENG LEAKING A RAIA A UNSCHED LANDING K FLUID LOSS TO TAKEOFF 1 CE 03 425TE 11187 125 120853 STL - FLT 7152 - NR 2 ENGINE POWER, EGT DROPPED OFF ON TAKEOFF. SECURED FUEL SUPPLY FITTING ON FLOW DIVIDER. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1996061300583 19960613 00583 EU 1996 6 13 RAIA960509 1 19960507 A 3246 50068582 WHEEL AEROSP ATR42 ATR42300 8680920 EU NLG OUT OF BAL A RAIA A UNSCHED LANDING E VIBRATION/BUFFET TO TAKEOFF 1 CE 03 EICBF 176 STL - FLT 7398 - VIBRATION IN NOSE DURING TAKEOFF. REPLACED NOSE WHEEL ASSEMBLIES. (M) 2 H 7 2 4T RT A53EU 1996061300584 19960613 00584 EU 1996 6 13 RAIA960510 1 19960507 A 7603 8930823 LINKAGE BAG JETSTM JETSTM3201 1500217 EU NR 1 ENG OUT OF ADJUST A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 03 434AM 6945 887 STL - FLT 7464 - NR 1 ENGINE WOULD NOT PRODUCE TARGET TORQUE. ADJUSTED ENGINE POWER CONTROL LINKAGE. (M) 2 L 7 2 4T RT A56EU 1996061300585 19960613 00585 NE 1996 6 13 RAIA960511 2 19960507 A 7200 ENGINE AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE NR 2 LOW PWR A RAIA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 CE 03 EICBF 15156 4663 176 120530 FYV - FLT 7401 - NR 2 ENGINE WOULD NOT PRODUCE REQUIRED TORQUE. REMOVED AND REPLACED ENGINE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1996061300586 19960613 00586 EU 1996 6 13 RAIA960512 1 19960506 A 3230 C24589000 UPLOCK ASSY AEROSP ATR72 ATR72202 8680940 EU LT MLG FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 723TE 9809 283 MEM - FLT 7145 - LEFT MAIN GEAR UP UNLOCK LIGHT ON FWD PANEL WILL NOT EXTINGUISH, OVERHEAD INDICATION NORMAL. DETERMINE D TO UPLOCK BOX PROX SENSOR. SYSTEM DEFERRED, MEL 32-61-1. (M) 2 H 7 2 4T RT A53EU 1996061300587 19960613 00587 EU 1996 6 13 RAIA960513 1 19960509 A 5210 137968C153 BRACKET BAG JETSTM JETSTM3201 1500217 EU PAX DOOR OUT OF ADJUST A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 427AM 11215 876 STL - FLT 7510 - PAX DOOR LIGHT ILLUMINATED. ADJUSTED DOOR HAND SWITCH STOP BRACKET. (M) 2 L 7 2 4T RT A56EU 1996061300588 19960613 00588 EU 1996 6 13 RAIA960514 1 19960510 A 7712 3104766 TQ SIG COND BAG JETSTM JETSTM3201 1500217 EU NR 1 ENG OUT OF ADJUST A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 342TE 7972 954 STL - FLT 7456 - NR 1 ENGINE LOW TORQUE. CALIBRATED TORQUE SIGNAL CONDITIONER. (M) 2 L 7 2 4T RT A56EU 1996061300589 19960613 00589 EU 1996 6 13 RAIA960516 1 19960512 A 2910 1379305A77 HOSE BAG JETSTM JETSTM3201 1500217 EU NR 1 PUMP LEAKING A RAIA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 CE 03 337TE 8766 929 STL - FLT 7330 - LOST HYDRAULIC PRESSURE IN FLIGHT. EMERGENCY HYDRAULIC SYSTEM FUNCTIONED NORMAL. REPLACED HYDRAULIC P RESSURE HOSE ON NR 1 PUMP. (M) 2 L 7 2 4T RT A56EU 1996061300590 19960613 00590 1996 6 13 RAIA960517 4 19960512 A 2310 CAU2583 RCAU CONTL UNIT AEROSP ATR42 ATR42300 8680920 EU NR 2 FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 421TE 15879 102 STL - FLT 7400 - NR 2 RADIO INTERMITTENT. REPLACED RADIO CONTROL UNIT (RCAU). (M) 2 H 7 2 4T RT A53EU 1996061300591 19960613 00591 EU 1996 6 13 RAIA960518 1 19960510 A 7500 8961153 GASKET BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP NR 1 ENG LEAKING A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 03 429AM 290 879 66321 STL - FLT 7372 - NR 1 ENGINE LOW TORQUE. REPLACED BLEED AIR GASKET. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996061300592 19960613 00592 1996 6 13 RAIA960519 4 19960513 A 3418 C771065 SIG SUMMING UNIT BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 03 429AM 879 STL - FLT 7360 - LEFT STALL CAPTION ILLUMINATED IN FLIGHT. MAINTENANCE REPLACED LEFT STALL SIGNAL SUMMING UNIT. (M) 2 L 7 2 4T RT A56EU 1996061300593 19960613 00593 EU 1996 6 13 REXA96015 1 19960514 A 3241 140041 TRANSDUCER SAAB SF340 SF340A 7850100 EU RT MLG FAILED A REXA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 25 326PX 340A054 BRAKE INOP ON TAXI AFTER LANDING. REMOVED AND REPLACED RHIB ANTI-SKID TRANSDUCER. (M) 2 L 7 2 4T RT A52EU 1996061300594 19960613 00594 EU 1996 6 13 SIMA96131 1 19960510 A 5210 S5217100100200 SKIN AEROSP ATR42 ATR42300 8680920 EU PAX DOOR DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 433MQ 151 MQT - DURING IMBV INSPECTION MAINTENANCE, FOUND DENT IN THE MIDDLE OF THE PASSENGER DOOR OUTER SKIN APPROX 3 INCHES FORW ARD OF THE TRAILING EDGE. DENT WAS 1 INCH LONG BY .375 INCHES WIDE. MAINTENANCE REPAIRED DENT IN PASSENGER DOOR IAW EO E1-5200-053. INITIATED A TDMI OF 1500 CYCLES FOR PERMANENT APPROVAL OF REPAIR BY DGAC. (M) 2 H 7 2 4T RT A53EU 1996061300595 19960613 00595 GL 1996 6 13 SRAA59603 2 19960512 A 7200 ENGINE LKHEED 382 382E 526413U SO ALLSN 501D 501D22A 03006 GL NR 1 DAMAGED A SRAA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 GL 23 923SJ 4301 FLT NR 1 AD08 REPORTED, NR 1 ENGINE BLEED AIR CAUSED AIR CONDITIONING TO EMIT FUMES, CLOSED NR 1 BLEED VALVE TO ELIMINAT E FUMES. ON LANDING, CARGO COMPARTMENT FILLED UP WITH SMOKE AFTER ENGINES WERE REVERSED ON ROLL OUT. FOUND NR 1 ENGINE HAS CRACKED TURBINE REAR BEARING SUPPORT AND INTERNAL LEAK, THE CARGO COMPARTMENT HEAT EXCHANGER WAS ALSO FOUND CRACKED . REPLACED NR 1 ENGINE, CARGO COMP COOLING TURBINE, AND HEAT EXCHANGER, ALL SYSTEMS OPS CHECKED GOOD. (M) 2 H 7 4 4T 4 T A1SO E282 1996061300596 19960613 00596 NM 1996 6 13 TAOA049603 1 19960401 A 2612 894120 FIRE LOOP BOEING 727 727254 138408L NM NR 1 ENG CHAFED A TAOA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 15 916TS 20437 ON TAKEOFF ROLL, NR 1 ENGINE FIRE WARNING LIGHT AND BELL CAME ON. REJECTED TAKEOFF. FOUND 'B' LOOP INSULATION CHAFED T HROUGH APPROX .03125 INCH IN LENGTH. REPAIRED WIRE AND INSTALLED WIRE PROTECTOR. OPERATIONAL CHECK OK. (M) 2 L 7 3 4F A3WE 1996061300597 19960613 00597 NM 1996 6 13 TAOA049604 1 19960404 A 2612 894120 FIRE LOOP BOEING 727 727254 138408L NM NR 3 PYLON MALFUNCTIONED A TAOA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 EA 15 913TS 20250 NR 3 FIRE WARNING LIGHT CAME ON IN CRUISE DISCHARGED BOTH BOTTLES. FOUND 'A' LOOP RESISTANCE LOW. REPLACED 'A' LOOP. ( M) 2 L 7 3 4F A3WE 1996061300598 19960613 00598 NM 1996 6 13 TAOA049614 1 19960429 A 3240 2873 BRAKE BFGOODRICH BOEING 727 727254 138408L NM NLG DRAGGING A TAOA O OTHER O OTHER TO TAKEOFF 1 EA 15 912TS 2816 20438 FLT NR 6480 - DCA-LGA - LOUD NOISE DURING TAKEOFF ROLL, SUSPECT RIGHT BRAKE MAY HAVE BEEN DRAGGING. FOUND RIGHT NOSE BR AKE DRAGGING. REPLACED SAME AND LEFT AND RIGHT NOSE WHEEL ASSY. (M) 2 L 7 3 4F A3WE 1996061300599 19960613 00599 NM 1996 6 13 TAOA059602 1 19960509 A 3350 37067001 BATTERY PACK BOEING 727 727254 138408L NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 914TS 20251 FLT NR 6540 - DCA-LGA - FOUND ON OVERNIGHT L/S SERVICE, AFT RIGHT SERVICE DOOR EMERGENCY EXIT LIGHT DOES NOT TEST. REPL ACED BATTERY PACK IN LIGHT ASSEMBLY. (M) 2 L 7 3 4F A3WE 1996061300600 19960613 00600 NM 1996 6 13 TAOA059603 1 19960515 A 3350 1102833 LIGHT GRIMES BOEING 727 727254 138408L NM CABIN INOPERATIVE A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 914TS 20251 OVERNIGHT L/S SERVICE, DCA - AFT AIRSTAIRS EXTERIOR EMERGENCY EXIT LIGHT INOP. REPLACED EMERGENCY LIGHT ASSEMBLY, AFT A IRSTAIRS. (M) 2 L 7 3 4F A3WE 1996061300601 19960613 00601 WP 1996 6 13 USAA960432 1 19960514 A 5330 SKIN DOUG DC9 DC981 3022081 WP STATION 1437 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 801US 38909 48037 PIT - DURING Q-5/C5 CHECK INSPECTION, FOUND TWO CRACKS .5 INCH LONG EACH, STATION 1437 BETWEEN LONGERON 2L AND 4L, IN AI RCRAFT FUSELAGE SKIN. REPAIRED WITH EXTERNAL DOUBLER PER SRM 53-04 FIG 27 USAIR EA NR 32644 AND EA NR 32647. (M) 2 L 7 2 4F A6WE 1996061300602 19960613 00602 WP 1996 6 13 USAA960433 1 19960514 A 5330 SKIN DOUG DC9 DC981 3022081 WP BS 1437 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 801US 38909 48037 PIT - DURING Q-5/C5 CHECK INSPECTION, FOUND TWO CRACKS .25 INCH EACH, STATION 1437 BETWEEN LONGERON 2R AND 4R IN FUSELAG E SKIN. INSTALLED EXTERNAL DOUBLER PER SRM 53-04 FIG 27. (M) 2 L 7 2 4F A6WE 1996061300603 19960613 00603 NM 1996 6 13 USAA960434 1 19960514 A 5311 FRAME BOEING 737 7372Q9 138448M NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 230AU 43662 21975 INT - DURING Q-4 CHECK EDDY CURRENT, FOUND TWO CRACKS .125 INCH LONG, STATION 727 STRINGER 18A LEFT FRAME. REPLACED FRA ME SECTION AND REPAIRED PER EO 5394G068. (M) 2 L 7 2 4F A16WE 1996061300605 19960613 00605 NM 1996 6 13 USAA960436 1 19960514 A 5320 ANGLE BOEING 737 7372Q9 138448M NM PAX DOOR CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 230AU 43662 21975 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 2 NCH AFT ENTRY THRESHOLD 'Z' ANGLE UPPER LEG. REPL ACED UPPER LEG OF 'Z' ANGLE, REPAIRED PER SRM 51-40-3. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996061300606 19960613 00606 NM 1996 6 13 USAA960437 1 19960514 A 5315 FLOOR BEAM BOEING 737 7372Q9 138448M NM BS 987 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 230AU 43662 21975 INT - DURING Q-4 CHECK, FOUND SEVERAL 1 INCH BY 2 INCH CORRODED AREAS AROUND NUT-PLATES SPANNING A TOTAL OF 86 INCHES, S TATION 987 LBL 36 INCHES TO RBL 50 INCHES FLOOR BEAM. REMOVED T-CAP SECTION OF FLOOR BEAM AND FABRICATED REPLACEMENT SE CTION AND SPLICE BBL 36 TO RBL 50. REPAIRED PER T/R 53-10-05C. (M) 2 L 7 2 4F A16WE 1996061300607 19960613 00607 EU 1996 6 13 USAAF96046 1 19960517 A 3230 RETRACT MECH FOKKER F28 F28MK0100 4990807 EU LANDING GEAR MALFUNCTIONED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 854US 11282 CLT - FL 494 - AFTER TAKEOFF FROM CLT, CAPTAIN COULD NOT RETRACT LANDING GEAR. MANUAL OVERRIDE WAS ATTEMPTED AND UNSUCC ESSFUL. NO EMERGENCY WAS DECLARED AND THE FLIGHT RETURNED TO FIELD IN CLT. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENACNE JACKED THE AIRCRAFT AND SWUNG THE GEAR SEVERAL TIMES. UNABLE TO DUPLICATE. GEAR SWING CHECKS OK. (M) 2 L 7 2 4F RT 1996061300608 19960613 00608 EU 1996 6 13 USAAF96047 1 19960518 A 3250 714540 SELECTOR VLV FOKKER F28 F28MK4000 4990810 EU NLG STEERING MALFUNCTIONED A USAA O OTHER O OTHER CL CLIMB 1 EA 19 480AU 11229 CLT - FL 568 - NOSE GEAR RED DOOR LIGHT REMAINED ON AFTER GEAR RETRACTION. CREW ACCOMPLISHED ABNORMAL PROCEDURE. LIGHT WENT OUT AFTER GEAR WAS RECYCLED. MAINTENANCE REMOVED AND REPLACED THE FOLLOWING ITEMS; NOSE WHEEL STEERING SELECTOR, P/N 714540 AND NLG DOOR ACTUATOR, P/N 12500-1 AND NLG DOOR SELECTOR VALVE, P/N 71539 AND NLG SELECTOR VALVE, P/N 71538-1 . (M) 2 L 7 2 4F RT A20EU 1996061300609 19960613 00609 NM 1996 6 13 USAASB96070 1 19960420 A 2612 667201 FIRE DETECTOR BOEING 737 737301 1384611 NM RT ENG STRUT FAILED A USAA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 346US 23515 FLT NR 1021 - PHL - ON CLIMB-OUT AT 2500 FEET, RIGHT ENGINE FIRE WARNING LIGHT AND BELL CAME ON. COMPLETED ENGINE FIRE CHECK LIST. FIRE WARN LIGHT DID NOT GO OUT UNTIL ENGINE FIRE SHUTOFF HANDLE WAS PULLED. ENGINE SHUTDOWN FOR 13 MINUTES . MX REPLACED THE RIGHT STRUT DETECTOR, CHECKED SAT. (M) 2 L 7 2 4F RT A16WE 1996061300610 19960613 00610 NE 1996 6 13 USAASB96083 2 19960510 A 7311 749965 OIL COOLER BOEING 737 737201 1384454 NM PWA JT8 JT8D9A 52048 NE NR 1 ENG FAILED A USAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 262AU 22868 FLT NR 2316 - RIC - NR 1 ENGINE OIL TEMP REMAINED IN YELLOW ARC FOR MAX 15 MIN RESTRICTION. PRECAUTIONARY ENGINE SHUTDO WN COMPLETED. MAINTENANCE REPLACED LEFT ENGINE FUEL/OIL EXCHANGER. OPS AND LEAK CHECK OK. (M) 2 L 7 2 4F 4 F A16WE E2EA 1996061300611 19960613 00611 NM 1996 6 13 USAASB96084 1 19960511 A 2530 8131 BALLAST BOEING 737 7372B7 1384560 NM NR 3 GALLEY FAILED A USAA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 269AU 22881 FLT NR 1005 - MEM - AT CRUISE ALT AN ELECTRICAL SMELL DEVELOPED IN THE AFT GALLEY. CAPTAIN CONFIRMED UPON INSPECTION AN D DIRECTED FA'S TO PULL ALL AFT GALLEY CIRCUIT BREAKERS. SMELL DISIPATED. DIVERTED TO MEM. MAINTENANCE REMOVED AND RE PLACED BALLAST FOR NR 3 GALLEY WORK LIGHT. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1996061300612 19960613 00612 NM 1996 6 13 USAASB96088 1 19960515 A 2131 7612608 PRESS CONTROLLER BOEING 737 737301 1384611 NM E/E COMPT FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 350US 66730 23553 DCA - FL 1721 - DURING CLIMB AT APPROXIMATELY 6,000 FEET, CREW WAS UNABLE TO MAINTAIN PRESSURIZATION. FLIGHT RETURNED T O FIELD AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE CABIN PRESSURE CONTROLLER. (M) 2 L 7 2 4F RT A16WE 1996061300613 19960613 00613 NM 1996 6 13 USAASB96089 1 19960517 A 3350 FUSE BOEING 737 737401 1384701 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 407US 23877 LGA - MAINTENANCE FOUND THE EMERGENCY EXIT AISLE LIGHTS, IN ROW 24 AND 25, WON'T ILLUMINATE. MAINTENANCE REPLACED FUSE IN BATTERY PACK. (M) 2 L 7 2 4F RT A16WE 1996061300614 19960613 00614 NM 1996 6 13 USAASB96090 1 19960518 A 3350 20121 BATT CHARGER BOEING 737 737401 1384701 NM CABIN FAILED A USAA O OTHER L NO TEST IN INSP/MAINT 1 EA 19 425US 23992 PHL - MAINTENANCE FOUND THE OVERWING MID AISLE EMERGENCY LIGHT INOP. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERY PACK, CHECKS OK. (M) 2 L 7 2 4F RT A16WE 1996061300615 19960613 00615 EU 1996 6 13 WTAA960087 1 19960427 A 3260 INTRANSIT LIGHT BAG JETSTM JETSTM3101 1500215 EU RT MLG ILLUMINATED A WTAA O OTHER N FALSE WARNING AP APPROACH 1 WP 17 431UE 813 LMT - RIGHT MAIN LANDING GEAR INTRANSIT LIGHT ILLUMINATED WITH GEAR EXTENDED. AIRCRAFT FERRIED TO SFO FOR REPAIRS. MX INSPECTED RIGHT MAIN LANDING GEAR UPLOCK AND DOWNLOCK MICROSWITCHES AND ASSOCIATED WIRING. NO DEFECTS NOTED. UNABLE TO DUPLICATE REPORTED DISCREPANCY DURING GROUND CHECK AND SUBSEQUENT TEST FLIGHT. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996061300616 19960613 00616 EU 1996 6 13 WTAA960088 1 19960425 A 3260 9005EN38 UPLOCK SWITCH BAG JETSTM JETSTM3101 1500215 EU RT MLG DIRTY A WTAA O OTHER N FALSE WARNING AP APPROACH 1 WP 17 431UE 813 SBP - RIGHT MAIN LANDING GEAR INTRANSIT LIGHT REMAINS ILLUMINATED WITH GEAR EXTENDED. MAINTENANCE INSPECTED AND CLEANED RIGHT MAIN LANDING GEAR UPLOCK MICROSWITCH. GEAR INDICATIONS NORMAL DURING GROUND CHECK. AIRCRAFT RETURNED TO SERVICE . (M) 2 L 7 2 4T RT A21EU 1996061300617 19960613 00617 EU 1996 6 13 WTAA960089 1 19960425 A 3260 9005EN38 DNLOCK SWITCH BAG JETSTM JETSTM3101 1500215 EU NLG DAMAGED WIRE A WTAA O OTHER N FALSE WARNING AP APPROACH 1 WP 17 424UE 796 PDX - NOSE GEAR 'GREEN' DOWN AND LOCKED LIGHT FAILS TO ILLUMINATE WITH GEAR EXTENDED. CREW CYCLED GEAR WITH NO CHANGE I N INDICATION. AIRCRAFT LANDED WITHOUT INCIDENT. MX REPAIRED DAMAGED WIRE AT NOSE GEAR DOWNLOCK MICROSWITCH. GEAR POSI TION INDICATION SYSTEM OPERATIONAL CHECK NORMAL ON GROUND. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996061300618 19960613 00618 EU 1996 6 13 WTAA960091 1 19960428 A 3260 9005EN38 SWITCH BAG JETSTM JETSTM3101 1500215 EU LT MLG DAMAGED WIRE A WTAA O OTHER N FALSE WARNING TO TAKEOFF 1 WP 17 427UE 811 LAX - LEFT MAIN GEAR INTRANSIT LIGHT REPORTED INOPERATIVE WHEN GEAR RETRACTED. MX REPAIRED DAMAGED WIRING AT LEFT MAIN GEAR UPLOCK MICROSWITCH. GEAR POSITION INDICATIONS OPERATIONAL CHECK NORMAL ON GROUND. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4T RT A21EU 1996061300619 19960613 00619 EU 1996 6 13 WTAA960096 1 19960423 A 7722 9495948 TTL COMPUTER BAG JETSTM JETSTM3101 1500215 EU LT ENGINE INTERMITTENT A WTAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 WP 17 403UE 743 EUG - LEFT ENGINE TORQUE SURGE REPORTED DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. UNABLE TO DUPLICATE REP ORTED DISCREPANCY ON GROUND RUN. SUBSEQUENT TAKEOFF ATTEMPT ABORTED. MAINTENANCE DEFERRED SRL AND TTL SYSTEMS. AIRCRA FT RETURNED TO SERVICE. DISCREPANCY SUBSEQUENTLLY CORRECTED WITH THE REPLACEMENT OF THE LEFT ENGINE TTL COMPUTER. (M) 2 L 7 2 4T RT A21EU 1996061300620 19960613 00620 EU 1996 6 13 WTAA960097 1 19960507 A 3260 622800200 UPLOCK SWITCH BAG JETSTM JETSTM3101 1500215 EU RT MLG FAILED A WTAA O OTHER N FALSE WARNING AP APPROACH 1 WP 17 431UE 813 LAX - RIGHT MAIN LANDING GEAR INTRANSIT LIGHT ILLUMINATED WITH GEAR EXTENDED. AIRCRAFT FERRIED TO FAT FOR REPAIRS. MX REPLACED RIGHT MAIN LANDING GEAR UPLOCK AND DOWNLOCK MICROSWITCHES. SYSTEM OPERATIONAL CHECK NORMAL DURING GEAR RETRACT ION CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996061300621 19960613 00621 EU 1996 6 13 WTAA960098 1 19960508 A 3260 9005EN38 SWITCH BAG JETSTM JETSTM3101 1500215 EU RT MLG FAILED A WTAA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 WP 17 431UE 813 FAT - AFTER RETRACTION RIGHT MAIN LANDING GEAR DOWN AND LOCKED LIGHT REMAINED ILLUMINATED. AIRCRAFT RETURNED TO FAT FOR REPAIRS. MX ADJUSTED RIGHT MAIN LANDING GEAR DOWNLOCK SWITCH. SYSTEM OPERATIONAL CHECK NORMAL DURING GEAR RETRACTION CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996061300622 19960613 00622 SO 1996 6 13 WTAA960099 1 19960509 A 7931 1153P001301 OIL SWITCH EMB 120 EMB120RT SO LT ENGINE FAILED A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 17 278UE 120083 ACV - LEFT ENGINE OIL PRESSURE AURAL WARNING SOUNDED ON TAKEOFF. TAKEOFF ABORTED WITHOUT INCIDENT. MX DEFERRED LEFT EN GINE OIL PRESSURE INDICATION PER MEL 79-32-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL BY REPLACING LEFT ENGINE OIL PRESSURE SWITCH. (M) 2 L 7 2 4T RT A31SO 1996061300623 19960613 00623 EU 1996 6 13 WTAA960100 1 19960509 A 3260 9005EN38 SWITCH BAG JETSTM JETSTM3101 1500215 EU NLG BROKEN WIRE A WTAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 WP 17 424UE 796 SEA - NOSE LANDING GEAR DOWN AND LOCK 'GREEN' INDICATION DID NOT ILLUMINATE AFTER GEAR EXTENSION. AIRCRAFT LANDED WITHO UT INCIDENT. MX REPAIRED GROUND WIRE AT NOSE GEAR DOWNLOCK MICROSWITCH. GROUND POSITION INDICATION NORMAL DURING GROUN D CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996061300624 19960613 00624 EU 1996 6 13 Y2PA96030 1 19960516 A 2130 WARNING SWITCH AMD FALC20 FALCOND 2720304 EU CABIN BROKEN WIRE A Y2PA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 GL 23 823AA 228 MEM - CABIN WENT TO 15,000 FEET DURING CLIMB TO 23,000 FEET. NO HORN OR WARNING LIGHT AT 10,000 FEET. MANUAL PRESSURIZ ATION WAS SELECTED WITH NO RESULT. AIRCRAFT DIVERTED FROM INTENDED DESTINATION AND LANDED IN MEMPHIS,TN. IT WAS DISCOV ERED THAT THE EMERGENCY PRESSURIZATION HANDLE WAS PULLED HALFWAY OUT. RESET THE HANDLE, GROUND RAN AND OPERATIONALLY CH ECKED THE PRESSURIZATION SYSTEM PER MM 21-31-5. OPERATION CHECKED GOOD. THE LACK OF A CABIN ALTITUDE WARNING WAS TRACE D TO A BROKEN WIRE ON THE CABIN ALTITUDE WARNING SWITCH. REPAIR OF THE WIRE RETURNED TO SYSTEM TO NORMAL OPERATION. (M ) 2 L 7 2 4F A7EU 1996061300625 19960613 00625 WP 1996 6 13 Y2PA96031 1 19960519 A 5330 5911401 SKIN DOUG DC9 DC915F 3022037 WP BS 108 CRACKED A Y2PA K NONE O OTHER IN INSP/MAINT 1 GL 23 197US 47154 YIP - FOUND ONE SMALL CRACK IN THE LEFT SIDE OF THE NOSE LANDING GEAR WHEEL WELL SKIN AT STATION 108. REMOVED DAMAGED S KIN AREA. FABRICATED AND INSTALLED REPAIR FILLER AND REPAIR DOUBLER PER USA JET AIRLINES ENGINEERING AUTHORIZATION NR 9 6-53-02R1. (M) 2 L 7 2 4F A6WE 1996061300626 19960613 00626 WP 1996 6 13 ZIAA96010 1 19960513 A 5730 8005171 PLANK 800473501 LKHEED 188 188A 5262602 WP WS 77-82.5 CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 346HA 49667 188A1043 YIP - DURING SCHEDULED CHECK, FUEL LEAK TEST REVEALED FUEL LEAKING FROM NR 2 FUEL TANK UPPER SURFACE AT JOINT BETWEEN PL ANK NRS 6 AND 7. FURTHER INSPECTION REVEALED A 5.5 INCH LONGITUDINAL CRACK IN PLANK 7 AT WS 77 THROUGH 88.5. ROUTED OU T CRACKED AREA FROM WS 77 TO 82.5 PER SB 620. FABRICATED AND INSTALLED REPAIR IAW LAC L-188 SRM 57-2-1, PAGE 33, FIG 3, SHEET 25. (M) 2 L 7 4 4T RT 4A22 1996061300627 19960613 00627 WP 1996 6 13 ZIAA96011 1 19960513 A 5730 800473501 PLANK LKHEED 188 188A 5262602 WP WS 82 CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 346HA 49667 188A1043 YIP - DURING SCHEDULED CHECK, FUEL LEAK TEST REVEALED FUEL LEAKING FROM NR 2 FUEL TANK UPPER SURFACE AT JOINT BETWEEN PL ANK NR 8 AND NR 9. FURTHER INSPECTION WITH SURFACE PROBE EDDY CURRENT REVEALED A .375 INCH CHORDWISE CRACK IN PLANK 9 A T WS 82. CLEANED CRACK PER SRM 51-2-7, PAGE 2. REPAIRED IAW ZIAA DRAWING A57-R01. SEALED AND TOP COATED. LEAK CHECK SATISFACTORY. (M) 2 L 7 4 4T RT 4A22 1996061300628 19960613 00628 WP 1996 6 13 ZIAA96012 1 19960513 A 5730 8339883 PLANK LKHEED 188 188A 5262602 WP WS 264 CRACKED A ZIAA K NONE Z SIGNIFICANT FAILURE REPORT IN INSP/MAINT 1 GL 23 346HA 49667 188A1043 YIP - DURING SCHEDULED CHECK, VISUAL INSPECTION REVEALED CRACK IN LEFT WING LOWER SURFACE PLANK NR 4, WS 264, AT JOINT B ETWEEN PLANK NR 3 AND 4. ROUTED OUT CRACKED AREA, MANUFACTURED AND INSTALLED REPAIR PER SRM 57-2-1, FIG 3, SHEET 15. S EALED REPAIR. LEAK CHECK SATISFACTORY. (M) 2 L 7 4 4T RT 4A22 1996061300629 19960613 00629 WP 1996 6 13 ZIAA96013 1 19960509 A 2612 FIRE WARNING DOUG DC8 DC8F54 3021926 WP NR 4 ENGINE ACTIVATED A ZIAA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 8042U 45676 LAX - DURING CLIMB-OUT, SHUT DOWN NR 4 ENGINE DUE TO FIRE WARNING INDICATION. VISUALLY INSPECTED, OHM'D AND CHECKED FIR E DETECTION LOOPS FOR SHORTS. ALL CHECKS FOUND SATISFACTORY. NO DEFECTS NOTED. NO EVIDENCE OF FIRE FOUND. (M) 2 L 7 4 4F 4A25 1996061300630 19960613 00630 WP 1996 6 13 ZIAA96014 1 19960509 A 7830 530435 TR SEQ VALVE DOUG DC8 DC8F54 3021926 WP NR 4 ENGINE LEAKING A ZIAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 23 8042U 45676 HUF - DURING CRUISE, SHUT DOWN NR 4 ENGINE DUE TO FIRE WARNING INDICATION. FOUND THRUST REVERSER SEQUENCE VALVE LEAKING AND BLOWING HOT AIR ON THE FIRE DETECTION LOOP. REMOVED AND REPLACED SEQUENCE VALVE. OPERATIONAL CHECK GOOD. (M) 2 L 7 4 4F 4A25 1996061300631 19960613 00631 GL 1996 6 13 ZIAA96015 2 19960509 A 7250 6844936 BEARING SUPPORT LKHEED 188 188C 5262604 SO ALLSN 501D 501D13 03004 GL NR 3 ENGINE CRACKED A ZIAA E ENGINE SHUTDOWN J WARNING INDICATION TO TAKEOFF 1 GL 23 289F 188C1110 500889 ANC - DURING TAKEOFF FROM ADQ, HAD FIRE WARNING INDICATION ON NR 3 ENGINE. E-HANDLE PULLED AT 22.37Z. CREW ELECTED TO PROCEED TO ANC. FOUND NR 3 ENGINE REAR TURBINE BEARING SUPPORT COCKED AND CRACKED 75 PERCENT OF ITS CIRCUMFERENCE, THUS DIRECTING EXHAUST GASES/HEAT TO ZONE 4 FIRE DETECTION ELEMENT. REPLACED NR 3 REAR TURBINE BEARING SUPPORT. OPERATIONA L CHECK NORMAL. (M) 2 L 7 4 4T 4 T 4A22 E282 1996061300632 19960613 00632 WP 1996 6 13 9612639965 1 19960605 A 5320 FITTING DOUG DC9 DC931 3022065 WP FS 658 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 911RW 47149 DURING M-CHECK, FOUND A CRACK IN THE FS 658 FLOOR SUPPORT FITTING BELOW THE RIGHT OUTBOARD SEAT TRACK. REPLACED FITTING PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996061300633 19960613 00633 WP 1996 6 13 9612681145 1 19960508 A 5320 JAMB WEB DOUG DC10 DC1040 3023508 WP DOOR 3L CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 145US 46754 DURING T-CHECK, FOUND TWO CRACKS 2.5 AND 1.75 LONG 3L IN THE DOOR 3L AFT LOWER DOOR JAMB WEB. REPAIRED WEB (P/N AEA0112 -1) PER EA 11-105390. 2 L 7 3 4F A22WE 1996061300634 19960613 00634 WP 1996 6 13 9612691145 1 19960513 A 5320 JAMB DOUBLER DOUG DC10 DC1040 3023508 WP CARGO DOOR CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 145US 46754 DURING T-CHECK, FOUND CORROSION IN THE AFT CARGO DOOR JAMB LOWER AFT CORNER DOUBLERS AND RAIL. REPAIRED DOUBLERS (P/N A FA7052-1, AFA7083-501) AND THE RAIL (P/N AFA7029-1) PER EA 11-104264. 2 L 7 3 4F A22WE 1996061300635 19960613 00635 NM 1996 6 13 9612706628 1 19960520 A 5347 SEAT TRACK BOEING 747 747251B 1384892 NM FS 1241 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 628US 22389 DURING P-CHECK, FOUND A CRACK IN THE RBL 96 SEAT TRACK AT BS 1241. REPAIRED TRACK (P/N 65B 13698-1) PER EA 66-101938. 2 L 7 4 4F A20WE 1996061300636 19960613 00636 NM 1996 6 13 9612716628 1 19960522 A 5347 SEAT TRACK BOEING 747 747251B 1384892 NM FS 662 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 628US 22389 DURING P-CHECK, FOUND CORROSION IN THE RBL 11 SEAT TRACK AT BS 662. REPAIRED TRACK PER EA 66-101940. 2 L 7 4 4F A20WE 1996061300637 19960613 00637 WP 1996 6 13 9612729905 1 19960523 A 5313 LONGERON DOUG DC9 DC931 3022065 WP FS 222-225 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 955N 47160 DURING H-CHECK, FOUND A CRACK AND CORROSION IN LONGERON 30 AT FS 222 TO 225. REPAIRED LONGERON (P/N 4912583-501) PER EA 99-108997. 2 L 7 2 4F A6WE 1996061300638 19960613 00638 WP 1996 6 13 9612739905 1 19960524 A 5330 SKIN DOUG DC9 DC931 3022065 WP FS 680-756 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 955N 47160 DURING H-CHECK, FOUND CORROSION ON THE FUSELAGE SKIN UPPER SURFACE IN THE LEFT WHEEL WELL KEEL AREA FS 680 TO 756. REPL ACED SKIN PER (P/N 5911418-111) PER EA 99-109056. 2 L 7 2 4F A6WE 1996061300639 19960613 00639 WP 1996 6 13 9612749905 1 19960525 A 5311 FRAME DOUG DC9 DC931 3022065 WP FS 965 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 955N 47160 DURING H-CHECK, FOUND CORROSION ON THE FS 965 FRAME BETWEEN LONGERON 29L TO 30. REPAIRED FRAME (P/N 9912243-105) PER EA 99-109128. 2 L 7 2 4F A6WE 1996061300640 19960613 00640 NM 1996 6 13 9612752255 1 19960525 A 5311 FRAME BOEING 727 727251 138408H NM FS 870 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 255US 19974 DURING L-CHECK, FOUND A CRACK IN THE BS 870 FRAME BELOW STR 13R. REPAIRED FRAME PER EA B727-53-002. 2 L 7 3 4F A3WE 1996061300641 19960613 00641 WP 1996 6 13 9612769905 1 19960525 A 5330 SKIN DOUG DC9 DC931 3022065 WP FS 464 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 955N 47160 DURING H-CHECK, FOUND A CRACK IN AN EXISTING FUSELAGE SKIN REPAIR AT FS 464 BETWEEN LONGERONS 22L TO 23L. REPAIRED SKIN (P/N 5911410-63) PER EA 99-109147. 2 L 7 2 4F A6WE 1996061300642 19960613 00642 WP 1996 6 13 9612779905 1 19960525 A 5311 FRAME DOUG DC9 DC931 3022065 WP FS 980 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 955N 47160 DURING H-CHECK, FOUND CORROSION ON THE FS 980 FRAME BETWEEN LONGERONS 27R TO 28R. REPAIRED FRAME (P/N 9958238-23) PER E A 99-109127. 2 L 7 2 4F A6WE 1996061300643 19960613 00643 WP 1996 6 13 9612789905 1 19960528 A 5311 FRAME DOUG DC9 DC931 3022065 WP FS 218 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 955N 47160 DURING H-CHECK, FOUND CORROSION ON THE FS 218 FRAME BETWEEN LONGERONS 27L TO 27R. REPAIRED FRAME (P/N 9911520-385) PER EA 99-109117. 2 L 7 2 4F A6WE 1996061300644 19960613 00644 NM 1996 6 13 9612792201 1 19960529 A 5315 FLOOR BEAM BOEING 727 727251 138408H NM FS 1130 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 201US 22154 DURING H-CHECK, FOUND CORROSION ON THE BS 1130 FLOOR BEAM LOWER CHORD FROM LBL 37 TO 28 AND RBL 51. REPAIRED BEAM (P/N 65-20822-3) PER EA 22-105287. 2 L 7 3 4F A3WE 1996061300645 19960613 00645 WP 1996 6 13 9612809982 1 19960603 A 5320 JAMB DOUG DC9 DC932 3022066 WP AFT PAX DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 982US 45790 DURING LINE CHECK, FOUND THREE CRACKS IN THE AFT ENTRY DOOR JAMB, UPPER RIGHT CORNER AT Z=66. REPAIRED JAMB (P/N 591746 3-3) PER EA 99-105424. 2 L 7 2 4F A6WE 1996061300646 19960613 00646 WP 1996 6 13 9612819902 1 19960603 A 5313 LONGERON DOUG DC9 DC931 3022065 WP FS 351 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 952N 47073 DURING H-CHECK, FOUND A CRACK AND CORROSION ON LONGERON 26R AT FS 351. REPAIRED LONGERON (P/N 5911412-113) PER EA 99-10 9059. 2 L 7 2 4F A6WE 1996061300647 19960613 00647 WP 1996 6 13 9612829902 1 19960603 A 5330 SKIN DOUG DC9 DC931 3022065 WP FS 446 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 952N 47073 DURING H-CHECK, FOUND CORROSION ON THE FUSELAGE SKIN DOUBLER BENEATH LONGERON 26L AT FS 446. REPAIRED SKIN (P/N 5925992 -55) PER EA 99-109137. 2 L 7 2 4F A6WE 1996061300648 19960613 00648 WP 1996 6 13 9612839965 1 19960603 A 5230 FITTING DOUG DC9 DC931 3022065 WP CARGO DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 911RW 47149 DURING M-CHECK, FOUND A CRACK IN THE FORWARD CARGO DOOR UPPER DOOR STOP FITTING. REPLACED FITTING. 2 L 7 2 4F A6WE 1996061300649 19960613 00649 WP 1996 6 13 9612849921 1 19960603 A 5313 FITTING DOUG DC9 DC932 3022066 WP FS 980-996 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 943N 47647 DURING M-CHECK, FOUND CORROSION ON THE LONGERON 20L END FITTING AT FS 980 TO 996. REPLACED END FITTING PER SRM 53-11-3, PG 13. 2 L 7 2 4F A6WE 1996061300650 19960613 00650 NM 1996 6 13 9612852294 1 19960604 A 2782 ACT FITTING BOEING 727 727251 138408H NM NR 4 SLAT CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 294US 21505 DURING P-CHECK, FOUND A CRACK IN THE NR 4 SLAT ACTUATOR INBOARD MOUNT FITTING. REPLACED FITTING PER SRM 51-10-01, PG 4. 2 L 7 3 4F A3WE 1996061300651 19960613 00651 WP 1996 6 13 9612861144 1 19960604 A 5320 FITTING DOUG DC10 DC1040 3023508 WP CARGO DR JAMB CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 144JC 46753 DURING T-CHECK, FOUND CORROSION ON THE SPLICE FITTING JUST INBOARD OF THE LOWER FORWARD CORNER OF THE FORWARD CARGO DOOR JAMB. REPLACED FITTING (P/N ADA 7109-501). 2 L 7 3 4F A22WE 1996061300652 19960613 00652 1996 6 13 9612879883 4 19960517 A 3413 4067241860 VSI DOUG DC9 DC951 3022051 WP LT COCKPIT FAILED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 671MC 47660 ON CLIMBOUT, CAPTAIN'S VSI INDICATOR FAILED. DUE TO WEATHER CONDITIONS AT DESTINATION (AZO) DECISION WAS MADE TO DIVERT TO DTW FOR REPAIR. AIRCRAFT LANDED IN DTW WITHOUT INCIDENT. REPLACED CAPTIAN'S VSI INDICATOR, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996061300653 19960613 00653 WP 1996 6 13 9612889155 1 19960611 A 3350 BATTERY PACK DOUG DC9 DC914 3022034 WP LT TAILCONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8914E 45831 DURING LINE CHECK, FOUND LEFT TAILCONE EMERGENCY SLIDE LIGHT AND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BAT TERY PACK IN POWER SUPPLY, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996061300654 19960613 00654 WP 1996 6 13 9612899155 1 19960611 A 3350 BATTERY PACK DOUG DC9 DC914 3022034 WP RT TAILCONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8914E 45831 DURING LINE CHECK, FOUND RIGHT TAILCONE EMERGENCY SLIDE LIGHT AND RIGHT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED B ATTERY PACK IN POWER SUPPLY, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996061300655 19960613 00655 WP 1996 6 13 9612909910 1 19960609 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 960N 47256 DURING LINE CHECK, FOUND OVERWING EMERGENCY EXIT LIGHTS RIGHT SIDE INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK O K. 2 L 7 2 4F A6WE 1996061300656 19960613 00656 WP 1996 6 13 9612919921 1 19960609 A 3350 CONNECTOR DOUG DC9 DC932 3022066 WP CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 943N 47647 DURING LINE CHECK, FOUND EMERGENCY LIGHTS IN GALLEY SERVICE ENTRANCE OVERHEAD LIGHT TO BE TOO DIM TO BE SEEN WITH LENS C LOSED. REINSTALLED CONTACTS IN PLUG P1-4013 PER WIRING MANUAL, ALL EMERGENCY LIGHTS OPERATIONALLY CHECKED GOOD. 2 L 7 2 4F A6WE 1996061300657 19960613 00657 WP 1996 6 13 9612929903 1 19960609 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 953N 47083 DURING LINE CHECK, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996061300658 19960613 00658 EU 1996 6 13 9612933215 1 19960611 A 2910 O-RING AIRBUS 320 A320211 3930320 EU LT SPOILER ACT LEAKING A NWAA O OTHER K FLUID LOSS CR CRUISE 1 GL 01 315US 171 EN ROUTE, RECEIVED HYD G-RSVR LO LVL MESSAGE. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES, DECLARED AN EMERGENCY AND L ANDED WITHOUT INCIDENT AT ORIGINAL DESTINATION. MAINTENANCE REPLACED LEAKING O-RING SEAL ON THE NR 1 SPOILER ACTUATOR F ILTER HOUSING, LEAK AND OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996061300659 19960613 00659 NM 1996 6 13 9612946634 1 19960608 A 2621 34504901M FIRE BOTTLE BOEING 747 747227B 1384888 NM APU COMPARTMENT MALFUNCTIONED A NWAA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 GL 01 634US 22234 DURING CRUISE, THE APU FIRE WARNING SYSTEM ACTIVATED, SYSTEM-A FIRE LOOP DETECTOR FAULTED, FIRE BOTTLE WOULD NOT DISCHAR GE AND PULLED CIRCUIT BREAKER. AIRCRAFT CONTINUED TO SFO AND LANDED WITHOUT INCIDENT. REPLACED FIRE BOTTLE, OPERATIONA L CHECK GOOD. 2 L 7 4 4F A20WE 1996061300660 19960613 00660 EU 1996 6 13 9612983247 1 19960610 A 3260 INDICATION AIRBUS 320 A320211 3930320 EU LDG GEAR DOOR MALFUNCTIONED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 347NW 408 DURING CLIMBOUT AFTER LANDING GEAR RETRACTION, RECEIVED L/G DOORS NOT CLOSED MESSAGE. CYCLED LANDING GEAR HANDLE AND AL L INDICATIONS WERE NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING REVEALED NO DISCREPANCY. 2 L 7 2 4F RT A28NM 1996061300661 19960613 00661 EU 1996 6 13 9612993247 1 19960611 A 3260 201117013 UNLOCK ASSY AIRBUS 320 A320211 3930320 EU LT MLG DOOR MALFUNCTIONED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 347NW 408 DURING CLIMBOUT AFTER LANDING GEAR RETRACTION, RECEIVED L/G DOORS NOT CLOSED MESSAGE. LEFT MAIN LANDING GEAR DOOR INDIC ATED OPEN. CYCLED LANDING GEAR HANDLE WITH NO CHANGE IN INDICATION. AIRCRAFT CONTINUED TO ORIGINAL DESTINATION AND LA NDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR DOOR UPLOCK ASSEMBLY, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996061300662 19960613 00662 NM 1996 6 13 96FDEA00903 1 19960504 A 5315 FLOOR BEAM BOEING 727 72725 1384006 NM BS 620 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 505FE 18276 NR0533 AND 009, CORROSION (C53-224-01, -1) ON UPPER FLANGE FLOOR BEAM PREVIOUS REPAIR BS 620 BETWEEN LBL 22 TO RBL 11 WL 208. *S/D* REMOVED CORRODED UPPER FLANGE FLOORBOARD PREVIOUS REPAIR BS 620 BETWEEN LBL 22 TO RBL 11, WL 208. FABRICA TED NEW CHORD AND REPAIRED ANGLES AND STOPS. FITTED REPAIR PARTS AND DRILLED, DEBURED, CLEANED AND TREATED SEALED FASTE NERS IN PLACE. ALL WORK ACCOMPLISHED PER SRM 53-10-8. 2 L 7 3 4F A3WE 1996061300663 19960613 00663 NM 1996 6 13 96FDEA01080 1 19960611 A 5315 65208371 FLOOR BEAM BOEING 727 72722 1384002 NM BS 1110 DOUBLE HOLE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 NR 0514, 012 DOUBLE HOLE IN FLOOR BEAM TOP CHORD BS 1110, LBL 32, WL 208. *S/D* TRIMMED OUT DOUBLE HOLE IN FLOOR BEAM TO CHORD BS 1110 LB 32 WL 208. FABRICATED REPAIR ANGLES AND FILLER, ALODINED AND PRIMED FLOOR BEAM AND REPAIR ANGLES, I NSTALLED PARTS PER FEDEX EA NR 7-5310-29143. 2 L 7 3 4F A3WE 1996061300664 19960613 00664 NM 1996 6 13 96FDEA01081 1 19960611 A 5320 96116613 WEB BOEING 727 72722 1384002 NM BS 219-227 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 NR 0624 (013) CORROSION (C53-221-01) UNDER WEB BETWEEN STA 219.8 TO 227.8, WL 227, LBL 43. 2 L 7 3 4F A3WE 1996061300665 19960613 00665 NM 1996 6 13 96FDEA01086 1 19960430 A 5311 6516391 FRAME BOEING 727 72725 1384006 NM BS 783.95 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 505FE 18276 STA 783.95 RBL 65 WL 202 WHILE WORKING CARD 7-5310-7-33678 PT 4, FOUND A CRACK ON INSIDE FRAME WEB, STARTING FROM FASTEN ER HOLE, BOTTOM AFT SIDE OF FRAME. REMOVED EXISTING FASTENERS FABRICATED REPAIR PARTS DRILLED AND TREATED MATERIAL PLUG GED REQUIRED FASTENER HOLES. INSTALLED REPAIR PART IAW FEDEX EA 7-5310-29110 AND 7-5310-7-33678 PT 4. 2 L 7 3 4F A3WE 1996061300666 19960613 00666 NM 1996 6 13 96FDEA01087 1 19960501 A 5330 6518219 SKIN BOEING 727 72725 1384006 NM BS 440 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 505FE 18276 BOND DEGRADATION IN THE FORM OF CORROSION AT BS 441 STR 15 AND 16L, .4 BY 8 AREA MARKED. ALSO, BETWEEN STR 17 AND 18L, .3 BY 2 AREA MARKED. FOUND CORROSION TO BE OUT OF LIMITS. REMOVED CORRODED SECTION OF SKIN AND REPAIRED PER FEDEX EA 7 -5330-29115 EA 7-5310-29125 AND EO 7-5330-23196. 2 L 7 3 4F A3WE 1996061300667 19960613 00667 NM 1996 6 13 96FDEA01088 1 19960501 A 5320 6515975 FITTING BOEING 727 72725 1384006 NM BS 870 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 505FE 18276 ON INSPECTION OF BS 870 TERMINAL FITTING LT ROW, 2 NOTED CRACK INDICATIONS IN 2ND AND 3RD HOLE FROM TOP. REMOVED EXISTI NG REPAIR, REMOVED EXISTING FASTENERS IN REPAIR AREA, STOP DRILLED CRACK, BLENDED CORROSION, FABRICATED REPAIR PARTS, TR EATED MATERIAL, INSTALLED REPAIR PARTS IAW FEDEX EA 7-5310-29117. 2 L 7 3 4F A3WE 1996061300668 19960613 00668 NM 1996 6 13 96FDEA01089 1 19960504 A 5320 651854002 WEB BOEING 727 72725 1384006 NM BS 740 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 505FE 18276 WHILE WORKING NR0316, FOUND HOLE TO BE CRACKED UNDER STIFFENER AT BS 740 WEB LBL 55 WL 185. REMOVED BS 740 WEB AND INST ALLED NEW BS 740 WEB PER FEDEX DRAWING 64-18333 AND EA 7-5710-28401. 2 L 7 3 4F A3WE 1996061300669 19960613 00669 NM 1996 6 13 96FDEA01090 1 19960611 A 5311 BELLFRAME BOEING 727 72725C 138400H NM BS 430-450 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 120FE 19356 STR 9L IS CRACKED AT BELLFRAME 440L LWR RIVET. STR FLANGE CRACKED, VIEWED FROM UNDERSIDE AT RIVET BULKTAIL. REMOVED DA MAGED SECTION OF STR 9L FROM STA 430 TO 450. INSTALLED NEW SECTION OF STR 9L STA 430 TO 450 PER SRM 53-10-3 PGS 5, 6, 7 AND 8. 2 L 7 3 4F A3WE 1996061300670 19960613 00670 NM 1996 6 13 96FDEA01091 1 19960611 A 5320 BEAM BOEING 727 72725 1384006 NM BS 1336-1342 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 NR0664 AND 042, CORROSION ON BEAM AT WL 235 RBL 15.5 TO 18.5 LOWER SIDE BS 1336 TO 1342. 2 L 7 3 4F A3WE 1996061300671 19960613 00671 SW 1996 6 13 QXEA9600199 1 19960610 A 2150 20475546 COOLING TURBINE SWRNGN SA227 SA227AC 8780603 SW NR 1 ODOR A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 NM 09 27186 AC707 UPON LANDING AND AFTER USING REVERSE, SMOKE SMELL AND HAZE IN CABIN. NUMBER ONE COOLING TURBINE, HEAT EXCHANGER AND WAT ER SEPARATOR SOCK REPLACED IAW MAINT MANUAL. NUMBER ONE BLEED AIR OPS CHECKED GOOD ON GROUND RUN. 2 L 7 2 4T RT A8SW 1996061300672 19960613 00672 WP 1996 6 13 QXEA9600200 2 19960610 A 7321 8070419 FUEL CONTROL SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111UW 01514 WP NR 1 ENGINE MALFUNCTIONING A A QXEA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 NM 09 2728G 22002 3439 AC731 P44480 NR 1 ENGINE VARYING IN TORQUE AND TEMPRATURE. SWITCHING OFF SRL COMPUTER FAILED TO CORRECT PROBLEM. NR 1 ENGINE SHUTDO WN IN FLIGHT. AIRCRAFT LANDED IN PDX WITHOUT FURTHER PROBLEM. NR 1 FCU AND FUEL PUMP REPLACED. P2 SENSOR LINE CHECKED FOR OBSTRUCTION, NONE NOTED. ENGINE OPS CHECKED GOOD ON GROUND RUN. 2 L 7 2 4T 3 T RT A8SW E3WE 1996061300673 19960613 00673 WP 1996 6 13 SCNA96175 1 19960604 A 2611 13131 SMOKE DET DOUG DC10 DC1015 3022118 WP FWD CARGO INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 151SY 48295 FORWARD CARGO SMOKE DETECTOR WOULD NOT TEST. RELAMPED DETECTOR, OPS CHECK OK. 2 L 7 3 4F A22WE 1996061300674 19960613 00674 NM 1996 6 13 SCNA96176 1 19960605 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM LEFT OVERWING DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 283SC 22559 LEFT OVERWING EMERGENCY EXIT SIGNS WERE BLINKING ON AND OFF. REMOVED AND REPLACED THE BATTERY PACK IN ACCORDANCE WITH M M 33-50-71, SYSTEM OP CHECKS NORMAL. 2 L 7 3 4F A3WE 1996061300675 19960613 00675 NM 1996 6 13 SCNA96177 1 19960609 A 3350 1000677 LIGHT BOEING 727 727225 1384077 NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 283SC 22559 AFT EXIT OVERHEAD EMERGENCY LIGHT ASSEMBLY WAS FOUND INOP. REMOVED AND REPLACED AFT EXIT OVERHEAD EMERGENCY LIGHT ASSEM BLY, OPS CHECK GOOD PER MM 33-50-101. 2 L 7 3 4F A3WE 1996061300676 19960613 00676 NM 1996 6 13 VNAA9606004 1 19960608 A 7810 001A781A1430000 EXHAUST NOZZLE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT ENGINE DEFECTIVE A A VNAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 425JS 3037 CREW REPORTED, A RIGHT HAND ENGINE INLET DE-ICE FAILURE ON APPROACH TO PIT. AIRCRAFT CONTINUED ON AND LANDED WITHOUT IN CIDENT. UPON FURTHER INVESTIGATION BY PIT MX IT WAS DISCOVERED THAT THE MOUNT FLANGE ON THE EXHAUST NOZZLE HAD FAILED A LLOWING HOT EXHAUST GASES TO ESCAPE INTO THE AFT ZONE OF THE ENGINE NACELLE. THESE HOT GASES DAMAGED THE ENGINE INLET D E-ICE EJECTOR FLOW CONTROL VALVE, RENDERING IT INOPERATIVE. PIT MX REPLACED THE RT EXHAUST NOZZLE IAW MM 78-11-00. ALS O, REPLACED THE EFCV CONDUCTED A THROUGH EXAMINATION OF THE AFT NACELLE COULD FIND NO FURTHER EXHAUST GAS HEAT RELATED C OMPONE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996061300680 19960613 00680 NM 1996 6 13 96ZZZX2984 1 19960520 A 3250 588255 SWITCH PIPER PA60 PA60600 7106001 NM NLG STEERING STICKING A DKBA O OTHER O OTHER TO TAKEOFF 1 SO 09 801MA 600433147 DURING TAKEOFF ROLL, AIRCRAFT VEERED TO THE RIGHT. PILOT ABORTED TAKEOFF BRAKING TO KEEP AIRCRAFT ON RUNWAY. PILOT GOT AIRCRAFT STOPPED WITH NO OTHER PROBLEMS. INVESTIGATION REVEALED THE STEERING SWITCH FAILED AND WAS STUCK IN THE RIGHT TURN POSITION AND WOULD NOT SPRING BACK TO THE CENTER OFF POSITION. REPLACED SWITCH, OPS CHECK GOOD. SWITCH SHOULD BE CHECKED FOR GOOD STRONG POSITIVE SPRING BACK TO THE CENTER OFF POSITION. 1 M 7 2 3O RT A17WE 1996061300708 19960613 00708 CE 1996 6 13 96ZZZX3012 1 19960522 A 3242 215304 BRAKE ASSY BFGOODRICH CESSNA 500 500CESSNA 2076602 CE MLG PLATE BROKEN A P MDGA K NONE O OTHER IN INSP/MAINT 1 SO 09 10UH 324 0164 5000304 GOODRICH BRAKE ASSEMBLY - WEAR PIN INDICATOR WAS JUST ABOUT AT POINT TO BE CHANGED. BRAKE WAS REMOVED TO CHANGE AND FOU ND ONE BRAKE PLATE WAS CRACKED IN TWO PLACES, AND BROKEN. WHEN WHEEL WAS REMOVED, PARTS FELL OUT. SUBMITTER RECOMMMEND S 500 LANDING LIMIT ON BRAKE ASSY. PART CYCLES 562. 1 L 7 2 4F A22CE 1996061900011 19960619 00011 NM 1996 6 19 MZZA96023 1 19960321 A 5713 STRINGER BOEING 727 727232 1384082 NM WS 686.5 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING '1/2D' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, 0.5 INCH LONG CRACK FOUND ON LEFT OUTER WING UPPER VENT ST RINGER TO RIB ATTACHMENT AT S12, WS 686.5. THE CRACKED TAB WAS STOP DRILLED AND REPAIRED PER EA 5762-1050 (SB 727-57A15 9R5). REF: HANGAR NON-ROUTINE REPAIR ITEM CARD NR 806515 (SEQ NR 05065). (X) 2 L 7 3 4F A3WE 1996061900012 19960619 00012 NM 1996 6 19 MZZA96024 1 19960325 A 3230 10607441 BALL NUT BOEING 727 727232 1384082 NM NLG NICKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15781 20636 TNN - DURING '1/2D' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, NLG MANUAL EXTENSION BALL NUT AND SCREW ASSEMBLY PATH WAS FOUND NICKED. THE DAMAGED BALL NUT AND SCREW ASSY, PN 10-60744-1, WAS REMOVED AND REPLACED PER B727 MM 32-35-0, AND OPE RATIONAL CHECK FOUND SATISFACTORY. REF: HANGAR NON-ROUTINE REPAIR ITEM CARD NR 819170 (SEQ NR 01154). (X) 2 L 7 3 4F A3WE 1996062000001 19960620 00001 WP 1996 6 20 9600000000 1 19960522 A 7120 R182102T CONEBOLT DOUG DC9 DC9 3022002 WP FWD ENG MOUNT DEFECTIVE A A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 DURING A SHOP OVERHAUL MAGNETIC PARTICLE INSPECTION, THE FORWARD ENGINE MOUNT CONEBOLT WAS FOUND TO HAVE SEVERAL DEFECTS IN ONE END FACE. BOTH THE BOLT (P/N R18210-2T, S/N 15BR124) AND ITS ASSOCIATED ENGINE MOUNT (P/N K2219) ARE MANUFACTUR ED BY BARRY CONTROLS. THE SUBJECT BOLT WAS ROCKWELL HARDNESS TESTED BY NWA AT 37.5 PRIOR TO SHIPMENT BACK TO BARRY CONT ROLS FOR FURTHER ANALYSIS. 2 L 7 2 4F A6WE 1996062000002 19960620 00002 WP 1996 6 20 9612959941 1 19960607 A 5320 FITTING DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3324L 47103 DURING H-CHECK, FOUND A 6 INCH CRACK IN THE FITTING LOCATED AT THE FORWARD END OF THE RIGHT MAIN LANDING GEAR WHEEL WELL ADJACENT TO LONGERON 29R. REPLACED FITTING PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996062000003 19960620 00003 WP 1996 6 20 9612969941 1 19960608 A 5320 FITTING DOUG DC9 DC932 3022066 WP FS 579 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3324L 47103 DURING H-CHECK, FOUND CRACKS IN THE LONGERON 27L END FITTING 8 INCHES LONG AND IN THE LONGERON 28R END FITTING 7 INCHES LONG, BOTH AT FS 579. REPLACED FITTINGS (P/N 3920595-1, -501) PER SRM 51-30-2. 2 L 7 2 4F A6WE 1996062000004 19960620 00004 NM 1996 6 20 9612976612 1 19960609 A 5320 FITTING BOEING 747 747251B 1384892 NM FS 2300-2320 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING PERIODIC CHECK, FOUND CORROSION ON THE UPPER SURFACE OF THE LOWER LAV PAN BS 2300 TO 2320, RBL 10 TO 20. REPLACE D DOUBLER FITTING (P/N 65B04359-1) PER SRM 51-10-01, PAR 9 PG 18. 2 L 7 4 4F A20WE 1996062000005 19960620 00005 WP 1996 6 20 9613009941 1 19960611 A 5320 FITTING DOUG DC9 DC932 3022066 WP FS 579-598 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3324L 47103 DURING H-CHECK, FOUND CRACKS IN THE LONGERON 29R TO 30 END FITTINGS AT APPROXIMATELY FS 579 TO 598. REPLACED FITTINGS P ER SRM 51-30-5. 2 L 7 2 4F A6WE 1996062000006 19960620 00006 WP 1996 6 20 9613019853 1 19960612 A 2933 HYD QTY IND DOUG DC9 DC951 3022051 WP RT HYD SYST MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 762NC 47710 DURING CLIMBOUT, THE RIGHT HYDRAULIC SYSTEM QUANTITY INDICATION WENT TO ZERO. PERFORMED COM AND DIVERTED TO ATL. AIRCR AFT LANDED WITHOUT INCIDENT. FOUND RIGHT HYDRAULIC SYSTEM INDICATOR INOPERATIVE. REPLACED RIGHT HYDRAULIC SYSTEM INDIC ATOR AND TRANSMITTER. LEAK AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996062000007 19960620 00007 WP 1996 6 20 9613029922 1 19960612 A 3260 UNSAFE LIGHT DOUG DC9 DC932 3022066 WP LT MLG ILLUMINATED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 945N 47664 DURING CLIMBOUT, THE LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED WITH GEAR RETRACTED. RECYCLED GEAR WITH N O CHANGE. FLIGHT RETURNED TO SMP AND LANDED WITHOUT INCIDENT. REPLACED GEAR UPLIMIT SWITCH, GEAR DOWN LIMIT SWITCH AND GEAR DOOR SWITCH, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996062000008 19960620 00008 WP 1996 6 20 9613039922 1 19960612 A 3260 UPLATCH ROLLER DOUG DC9 DC932 3022066 WP LT MLG OUT OF ADJUST A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 945N 47664 DURING CLIMBOUT, THE LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTED. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. FOUND UPLATCH ROLLER ON LEFT GEAR NOT ENGAGED PROPERLY IN UPLATCH HOOK. RESHIMMED UPL ATCH ROLLER FOR PROPER LATCH ENGAGEMENT, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996062000009 19960620 00009 NM 1996 6 20 96FDEA01092 1 19960611 A 5315 BAC1505100617 FLOOR BEAM BOEING 727 72722 1384002 NM BS 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 NR0352 AND 004, CORROSION (C53-224-01) ON FLOOR BEAM TOP CHORD BS 600 RBL 10 TO 47 WL 208. *S/D* REMOVED CORROSION ON FLOOR BEAM TOP CHORD BS 600 RBL 10 TO 47 WL 208. FOUND AREA AT RBL 10 TO 17 TO BE OUT OF LIMITS. REPAIRED FLOOR BEAM I AW SRM 53-10-08. 2 L 7 3 4F A3WE 1996062000010 19960620 00010 NM 1996 6 20 96FDEA01093 1 19960611 A 5320 65453132 CLIP BOEING 727 72722 1384002 NM BS 660 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 NR0210 AND 005, DAMAGED STR CLIP AT BS 660 STRS 4R. *S/D* REMOVED DAMAGED CLIP AND INSTALLED NEW STRINGER CLIP AT BS 6 60 STR 4 RT PER SRM 53-10-8. 2 L 7 3 4F A3WE 1996062000011 19960620 00011 NM 1996 6 20 96FDEA01094 1 19960611 A 5320 65453132 CLIP BOEING 727 72722 1384002 NM BS 660 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 NR0211 AND 006, MISSING FASTENERS FROM STR CLIP AT BS 660 STR 3R AND DAMAGED STR CLIP. *S/D* REMOVED AND REPLACED STRI NGER CLIP AT BS 660, STR 3 RT PER SRM 53-10-8. 2 L 7 3 4F A3WE 1996062000012 19960620 00012 NM 1996 6 20 96FDEA01095 1 19960611 A 5320 65453132 CLIP BOEING 727 72722 1384002 NM BS 720 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 NR0212 AND 007, DAMAGED RIVETS AND STR CLIP AT BS 720 STR 4R. *S/D* REMOVED AND REPLACED STRINGER CLIP AT BS 720, STR 4 RT PER SRM 53-10-8. 2 L 7 3 4F A3WE 1996062000013 19960620 00013 NM 1996 6 20 96FDEA01096 1 19960611 A 5754 65973472 FITTING BOEING 727 72722 1384002 NM NR 2 LE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 NR0376 AND 008, NR 2 K-FLAP TO L/E MOUNT FITTING FOR THE CENTER HINGE IS CORRODED (C57-562-01). *S/D* REMOVED AND REPL ACED NR 2 K-FLAP TO LEADING EDGE MOUNT FITTING FOR THE CENTER HINGE IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996062000014 19960620 00014 NM 1996 6 20 96FDEA01097 1 19960611 A 5754 65185331 FITTING BOEING 727 72722 1384002 NM NR 1 LE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 NR 1 K-FLAP TO L/E MOUNT FITTING FOR THE CENTER HINGE IS CORRODED. REMOVED AND REPLACED PER SRM. 2 L 7 3 4F A3WE 1996062000015 19960620 00015 NM 1996 6 20 96FDEA01098 1 19960611 A 5754 65185321 FITTING BOEING 727 72722 1384002 NM NR 5 LE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 NR 5 K-FLAP CENTER HINGE FITTING THAT ATTACHES TO FIXED L/E CORRODED. REMOVED AND REPLACED PER SRM. 2 L 7 3 4F A3WE 1996062000016 19960620 00016 NM 1996 6 20 96FDEA01099 1 19960611 A 5315 65208279 FLOOR BEAM BOEING 727 72722 1384002 NM BS 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 NR0477 AND 011, CORROSION (C53-111-01, -2) ON FLOOR BEAM STA 600 RBL 2, 8, 13, 15, 18 WL 198, FWD BAY. *S/D* BLENDED A ND INSTALLED REPAIR STRAP IAW FED SRM 53-10-1 AND 53-10-8. 2 L 7 3 4F A3WE 1996062000017 19960620 00017 NM 1996 6 20 96FDEA01100 1 19960611 A 5315 652082724 FLOOR BEAM BOEING 727 72722 1384002 NM BS 560 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 NR0481 AND 014, FOUND GOUGE IN FLOOR BEAM STA 560 RBL 6 WL 198, FWD BAY. *S/D* REMOVED DAMAGE, FABRICATED AND INSTALLE D REPAIR PARTS PER SRM 53-10-8. 2 L 7 3 4F A3WE 1996062000018 19960620 00018 NM 1996 6 20 96FDEA01101 1 19960611 A 5311 651766423 FRAME BOEING 727 72722 1384002 NM BS 620 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 NR0499 AND 015, DENT IN FRAME AT BS 620 RBL 39 WL 162. *S/D* REMOVED DENT IN FRAME AT BS 620 RBL 39 WL 162. FABRICATE D REPAIR PARTS AND INSTALLED PER FED EX SRM 51-40-3. 2 L 7 3 4F A3WE 1996062000019 19960620 00019 NM 1996 6 20 96FDEA01102 1 19960611 A 5311 651766415 FRAME BOEING 727 72722 1384002 NM BS 660 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 NR0494 AND 016, DENT IN FRAME AT BS 660 LBL 39 WL 162. *S/D* REPAIRED FRAME AT BS 660 LBL 39 WL 162 AS PER FED EX SRM 51-40-3. 2 L 7 3 4F A3WE 1996062000020 19960620 00020 NM 1996 6 20 96FDEA01103 1 19960611 A 5320 651631510 SHEAR TIE BOEING 727 72722 1384002 NM BS 328 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 NR0646 AND 017, WHILE WORKING NR0348 AFTER REMOVING R/LOWER NOSE CHORD, FOUND CRACKED AND CORRODED SHEAR TIE AT BS 328 W L 148 RBL 15 TO 18. *S/D* REMOVED DAMAGED SHEAR TIE AT BS 328 WL 148 RBL 15 TO 18 IAW FED EX SRM 53-10-4. 2 L 7 3 4F A3WE 1996062000021 19960620 00021 NM 1996 6 20 96FDEA01104 1 19960611 A 5753 652163233 TE WEDGE BOEING 727 72722 1384002 NM LT TE MID FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 NR 0668 AND NR 018. L/W I/B MID FLAP LWR O/B T/E WEDGE DELAMINATED. ****S/D**** REPAIRED L/W I/B MID FLAP IAW FEDEX SRM 51-40-6. 2 L 7 3 4F A3WE 1996062000022 19960620 00022 NM 1996 6 20 96FDEA01105 1 19960611 A 5320 6518015 SHEAR TIE BOEING 727 72722 1384002 NM BS 321 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 NR0671 AND 019, FOUND CRACKED SHEAR TIE BS 321 RBL 15 TO 19 WL 148. *S/D* REPAIRED CRACKED FRAME AND SHEAR TIE AT BS 3 21 RBL 15 TO 19 WL 148 IAW SRM 53-10-4. 2 L 7 3 4F A3WE 1996062000023 19960620 00023 NM 1996 6 20 96FDEA01107 1 19960611 A 2910 AE7040792 HYD LINE DOUG MD11 MD11F 3023600 NM NR 3 HYD SYS FAILED A FDEA E ENGINE SHUTDOWN F K FLT CONT AFFECTED FLUID LOSS CR CRUISE 1 SO 25 602FE 48402 EN ROUTE AT 12.40Z NR 3 HYD SYS LOSS/FAILURE OCCURED ALL FLUID LOST. ALL ABNORMAL CHECKLIST AND PROCEDURES COMPLETED. R EPLACED PRESS LINE THAT GOES FROM THE ENG DRIVEN PUMP TO THE FILTER MODULE. THIS WAS DONE ON EA 1-2910-23270. FINAL FI X WAS DONE IN EWR 6-13-96 WHERE THE HOSE WAS REPLACED. 2 L 7 3 4F RT A22WE 1996062000024 19960620 00024 WP 1996 6 20 96FDEA01108 1 19960612 A 5400 COWL WEB DOUG DC10 DC1010F 3022111 WP NR 2 ENGINE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 SNRM 4206, NR 2 ENG NOSE COWL CRACK AT AFT BULKHEAD AS VIEWED THROUGH ACCESS PANEL 361 KL. *S/D* REMOVED AND REPLACED WEB SECTION AS PER SRM 54-00-01. 2 L 7 3 4F A22WE 1996062000025 19960620 00025 NM 1996 6 20 96FDEA01109 1 19960612 A 5311 651593746 FRAME BOEING 727 727173C 1384059 NM BS 680 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 199FE 19509 NR0535 AND 007, WHILE WORKING NR0032 FOUND FRAME TO BE CRACKED AT BS 680 LBL 30 STR 26L. *S/D* REPAIRED CRACKED FRAME AT BS 680 STR 26L PER SRM 51-40-3. 2 L 7 3 4F A3WE 1996062000026 19960620 00026 WP 1996 6 20 96FDEA01110 1 19960613 A 5312 BULKHEAD FTG DOUG DC10 DC1010F 3022111 WP BS 1156 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 SNRM 1067. CENTER ASSY COMPT - 1156 BULKHEAD - OUTER CAP ANGLE FITTING ON LEFT SIDE HAS A 1.75 INCH CRACK ACROSS THE RA DIUS BETWEEN STR 35 - STR 36L. ***S/D***** NDT VERIFIED END OF CRACK/ACCOMPLISHED REPAIR PER SRM 53-40-00, FIG 8. 2 L 7 3 4F A22WE 1996062000027 19960620 00027 WP 1996 6 20 ABXA9600507 1 19960612 A 3350 5708458503 BATTERY RACK DOUG DC8 DC863 302198A WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 826AX 46061 EMERGENCY EXIT LIGHTS EXTINGUISHED AFTER APPROXIMATELY 3 SECONDS OF OPERATION. REPLACED EMERGENCY LIGHT BATTERY RACK AS SEMBLY IAW DC8 MM, OPS CHECK OF EMERGENCY LIGHTING SYSTEM WAS GOOD. 2 L 7 4 4F 4A25 1996062000028 19960620 00028 1996 6 20 AWRA9606004 4 19960612 A 3422 25883025 DIR GYRO DOUG DC8 DC862 3021970 WP E/E COMPT INOPERATIVE A ARWA K NONE O OTHER TO TAKEOFF 1 SO 19 802BN 45909 NR 1 COMPASS SYSTEM FAILED AFTER TAKEOFF, RETURNED TO MIA. REMOVED AND REPLACED DIRECTIONAL GYRO IAW 34-20-00, OPS CHEC KED NORMAL. 2 L 7 4 4F 4A25 1996062000029 19960620 00029 NM 1996 6 20 CALA9600794 1 19960608 A 3350 30043213 LIGHT BOEING 737 7373T0 1384582 NM L 2 DOOR INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 12349 23587 THE L-2 DOOR EMERGENCY SLIDE EXIT LIGHT WAS FOUND INOPERATIVE. THE EXIT LIGHT WAS REMOVED AND REPLACED. 2 L 7 2 4F RT A16WE 1996062000030 19960620 00030 NM 1996 6 20 CALA9600795 1 19960501 A 5311 FRAME BOEING 737 737217 1384464 NM BS 480 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16232 19886 INSPECTION FOUND A .5 INCH CRACK IN FRAME AT STA 480, BL 0. THE CRACK WAS REMOVED AND A DOUBLER AND FILLER WERE FABRICA TED AND INSTALLED IAW SRM 53-10-4. 2 L 7 2 4F A16WE 1996062000031 19960620 00031 NM 1996 6 20 CALA9600796 1 19960501 A 5320 INTERCOSTAL BOEING 737 737217 1384464 NM BS 500 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16232 19886 INSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO PIT INTERCOSTAL AT STA 500, STRINGER 27L. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 51-20-1, 51-10-2 AND 51-30-2. 2 L 7 2 4F A16WE 1996062000032 19960620 00032 NM 1996 6 20 CALA9600797 1 19960501 A 5320 CHANNEL BOEING 737 737217 1384464 NM BS 500 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16232 19886 THE STRINGER TO FLOOR BEAM ATTACHMENT U-CHANNEL HAD TWO 1 INCH CRACKS AT STA 500A, STRINGER 28R. A REPAIR WAS FABRICATE D AND INSTALLED IAW SRM 51-20-1, FIGURE 7 AND 51-30-2. 2 L 7 2 4F A16WE 1996062000033 19960620 00033 NM 1996 6 20 CALA9600798 1 19960508 A 5320 STRAP BOEING 737 737217 1384464 NM BS 420-500 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16232 19886 INSPECTION FOUND STRAP AT C-1 DOOR THRESHOLD CORRODED, STA 420 TO 500. A NEW STRAP WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-30-2. 2 L 7 2 4F A16WE 1996062000034 19960620 00034 NM 1996 6 20 CALA9600799 1 19960430 A 5312 BLKHD STIFFENER BOEING 737 737217 1384464 NM BS 727 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16232 19886 INSPECTION FOUND A .5 INCH CRACK IN RADIUS OF VERTICAL STIFFENER AT STA 727 BULKHEAD. A DOUBLER WAS FABRICATED AND INST ALLED IAW SRM 51-40-4, 51-10-2 AND 51-21. 2 L 7 2 4F A16WE 1996062000035 19960620 00035 NM 1996 6 20 CALA9600800 1 19960429 A 5720 AUX TRACK BOEING 737 737217 1384464 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16232 19886 INSPECTION FOUND A .5 INCH CRACK IN MID AUXILIARY TRACK OF RT WING ABOVE NR 6 SLAT. A REPAIR WAS INSTALLED IAW SRM 51-3 0-2. 2 L 7 2 4F A16WE 1996062000036 19960620 00036 NM 1996 6 20 CALA9600801 1 19960506 A 5753 SKIN BOEING 737 737217 1384464 NM RT TE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16232 19886 INSPECTION FOUND A 1 INCH CRACK IN UPPER SKIN OF RT WING INBOARD AFT FLAP. THE CRACKED AREA WAS CUT OUT, A FILLER AND D OUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND MM 51-20-0. 2 L 7 2 4F A16WE 1996062000037 19960620 00037 NM 1996 6 20 CALA9600802 1 19960501 A 5530 BRACKET BOEING 737 737217 1384464 NM VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16232 19886 INSPECTION FOUND A 2 INCH CRACK IN RT ANGLE BRACKET AT REAR SPAR OF VERTICAL STABILIZER. THE CRACK WAS STOP DRILLED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2 AND 51-30-2. 2 L 7 2 4F A16WE 1996062000038 19960620 00038 NM 1996 6 20 CALA9600803 1 19960501 A 5530 BRACKET BOEING 737 737217 1384464 NM VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16232 19886 INSPECTION FOUND A 1.5 INCH CRACK IN LT ANGLE BRACKET AT REAR SPAR OF VERTICAL STABILIZER. THE CRACK WAS STOP DRILLED A ND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-00-0, 51-40-3, 51-10-2 AND 51-30-2. 2 L 7 2 4F A16WE 1996062000039 19960620 00039 1996 6 20 CALA9600804 4 19960427 A 2565 11611136 SLIDE BOEING 737 737217 1384464 NM L 1 DOOR INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16232 19886 THE L-1 DOOR EVACUATION SLIDE FAILED DEPLOYMENT TEST. THE COVER LANYARD WOULD NOT RELEASE AND THE SLIDE ONLY PARTIALLY INFLATED. THE SLIDE WAS REMOVED AND REPLACED IAW MM 25-61-30. 2 L 7 2 4F A16WE 1996062000040 19960620 00040 NM 1996 6 20 CALA9600805 1 19960426 A 3397 WIRE BOEING 737 737217 1384464 NM CABIN DAMAGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16232 19886 A SECTION OF FORWARD CABIN EMERGENCY PATH LIGHTS WERE FOUND INOPERATIVE. THE WIRING AT FORWARD TRACK SECTION WAS REPAIR ED IAW MM 33-50-0. 2 L 7 2 4F A16WE 1996062000041 19960620 00041 SO 1996 6 20 COMA9610175 1 19960612 A 3150 ATG120TR PROX SENSOR EMB 120 EMB120RT SO ELEVATOR OUT OF ADJUST A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 462CA 120264 TAKEOFF TRIM WARNING SOUNDED DURING TAKEOFF ROLL. ADJUSTED THE ELEVATOR TRIM TAB PROXIMITY SENSORS. ACFT RETURNED TO S ERVICE. 2 L 7 2 4T RT A31SO 1996062000042 19960620 00042 SO 1996 6 20 COMA9610176 1 19960611 A 3260 922FS2A6N2735 WOW SENSOR EMB 120 EMB120RT SO RT MLG FAILED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 159A 120159 LANDING GEAR HANDLE COULD NOT BE SELECTED TO UP POSITION. REPLACED THE RT MLG, WEIGHT ON WHEELS PROXIMITY SENSOR. 2 L 7 2 4T RT A31SO 1996062000044 19960620 00044 EA 1996 6 20 COMA9660104 1 19960611 A 5210 HANDLE CNDAIR CL600 CL6002B19 EA PAX DOOR NOT STOWED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 929CA 7035 PASSENGER DOOR OUTER HANDLE NOT STOWED MESSAGE ON EICAS. AIRCRAFT WOULD NOT PRESSURIZE. COULD NOT DUPLICATE DISCREPANC Y. DOOR OPERATION AND OUTER HANDLE STOW MECHANISM ALL OPERATE NORMAL. 2 L 7 2 4F RT A21EA 1996062000045 19960620 00045 EA 1996 6 20 COMA9660105 1 19960612 A 3231 601R751461 SELECTOR VALVE CNDAIR CL600 CL6002B19 EA NLG DOOR MALFUNCTION A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 917CA 7017 NOSE LANDING GEAR DOORS REMAINED OPEN AFTER GEAR RETRACTION. REPLACED THE NLG DOORS SELECTOR VALVE. 2 L 7 2 4F RT A21EA 1996062000046 19960620 00046 EA 1996 6 20 COMA9660106 1 19960612 A 3260 172825 TARGET CNDAIR CL600 CL6002B19 EA RT MLG LOOSE A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 952CA 7092 RT MLG DISAGREEMENT MESSAGE WHEN LANDING GEAR RETRACTED. REPLACED LOOSE PROXIMITY SENSOR TARGET ON THE RT MLG UPLOCK AS SY. 2 L 7 2 4F RT A21EA 1996062000047 19960620 00047 EA 1996 6 20 COMA9660107 1 19960612 A 3240 601R752845 VALVE CNDAIR CL600 CL6002B19 EA PARKING BRAKE MALFUNCTION A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 958CA 7111 ANTI-SKID CAUTION MESSAGE ON EICAS. REPLACED THE PARKING BRAKE VALVE. 2 L 7 2 4F RT A21EA 1996062000048 19960620 00048 NM 1996 6 20 P5CA9600243 1 19960607 A 3510 280001 REGULATOR BOEING 747 747123 1384873 NM COCKPIT INOPERATIVE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 SECOND OBSERVER'S O2 REGULATOR HAD NO FLOW. REMOVED AND REPLACED REGULATOR AS PER MM 35-11-07. 2 L 7 4 4F A20WE 1996062000049 19960620 00049 NM 1996 6 20 SWAA960499 1 19960611 A 2121 215201 FAN BOEING 737 7372H4 138448C NM AC BAY FAILED A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 104SW 23110 FLIGHT ATTENDANT NOTED AND REPORTED TO CAPT AN ODOR IN THE CABIN. A UPS PILOT ONBOARD SUGGESTED THAT IT WAS SIMILAR TO THAT OF AN ELECTRICAL SMELL. CREW TURNED GASPER FAN OFF AND SMELL DISSIPATED. THEN SMELL RETURNED, CREW DECLARED AN EM ERGENCY. AIRCRAFT LANDED AT BWI WITHOUT INCIDENT. INSPECTED AND FOUND GASPER FAN TO BE THE FAULT, DEFERRED GASPER FAN OPERATION AND CONTINUED PER MEL 21-26. REPLACED GASPER FAN BER BOEING M/M. 2 L 7 2 4F A16WE 1996062000050 19960620 00050 NM 1996 6 20 SWAA960500 1 19960607 A 5753 FAIRING BOEING 737 7373H4 1384600 NM NR 2 TE FLAP UNSECURED A SWAA D RETURN TO BLOCK D INFLIGHT SEPARATION CL CLIMB 1 SW 07 342SW 24133 IN FLIGHT, NOTED NR 2 FLAP CANOE FAIRING LOOSE FROM MOUNT. AIRCRAFT RETURNED TO STL AND MADE AN UNEVENTFUL LANDING. IN SPECTED, RESECURED FAIRING PIVOT BUSHING BOLT PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996062000051 19960620 00051 NE 1996 6 20 SWAA960501 2 19960608 A 7261 OIL FILTER BOEING 737 7372H4 138448C NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE CONTAMINATED A SWAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SW 07 20SW 21337 NUMBER 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT, THROTTLE RETARDED, NO HELP. CREW PERFORMED ENGINE SHUTDO WN CHECKLIST. AIRCRAFT DIVERTED AND MADE AN UNEVENTFUL LANDING AT BHM. INSPECTED, REMOVED AND REPLACED NR 2 MAIN OIL F ILTER. FOUND MINOR CONTAMINATION, PERFORMED ENGINE RUN, REMOVED AND REPLACED OIL FILTER, NO CONTAMINATION NOTED. ALL E NGINE PARAMETERS NORMAL. 2 L 7 2 4F 4 F A16WE E2EA 1996062000052 19960620 00052 NM 1996 6 20 SWAA960502 1 19960609 A 5330 SKIN BOEING 737 7373H4 1384600 NM FWD FUSELAGE BIRD STRIKE A SWAA A UNSCHED LANDING C F.O.D. CL CLIMB 1 SW 07 334SW 23938 ON CLIMBOUT, EXPERIENCED BIRD STRIKE TO AREA ABOVE AND AFT OF F/O WINDOW. AIRCRAFT RETURNED TO SJC AND MADE AN UNEVENTF UL LANDING. PERFORMED BIRD STRIKE INSPECTION PER BOEING M/M, NO DAMAGE NOTED. 2 L 7 2 4F RT A16WE 1996062000053 19960620 00053 NM 1996 6 20 SWAA960503 1 19960611 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21722 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AROUND FASTENER HEAD AT BS 178, WL 234, LBL 9. REPAIRED PER BOEIN G SRM. 2 L 7 2 4F A16WE 1996062000054 19960620 00054 NM 1996 6 20 SWAA960504 1 19960611 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 1010 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21722 DURING SCHEDULED D-CHECK, FOUND STRINGER CRACKED AT BS 1010, S6R. SPLICED IN NEW SECTION PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000055 19960620 00055 NM 1996 6 20 SWAA960505 1 19960611 A 5320 SPLICE BOEING 737 7372H4 138448C NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21722 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, S4L. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000056 19960620 00056 NM 1996 6 20 SWAA960506 1 19960611 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 360-380 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21722 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AND GOUGED FROM BS 360 TO 380, S3L TO 6L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000057 19960620 00057 NM 1996 6 20 SWAA960507 1 19960611 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 382 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21722 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 382, S17L AND BS 381 BETWEEN S17L AND 16L. ALSO, DAMAGED CRE ASE BEAM WEB AND OUTER CREASE BEAM CHORD AT BS 383, WL 208, LBL 70. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000058 19960620 00058 NM 1996 6 20 SWAA960508 1 19960611 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 907 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21722 DURING SCHEDULED D-CHECK, FOUND O/B SIDE OF STRINGER CORRODED AT BS 907, RBL 15, WL 166, S26R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000059 19960620 00059 NM 1996 6 20 SWAA960509 1 19960611 A 5311 FRAME BOEING 737 7372H4 138448C NM CARGO BAY DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21722 DURING SCHEDULED D-CHECK, FOUND FWD CARGO BAY FRAME DENTED AT BS 500B S22 TO 25R, BS 400 S21 TO 25L, BS 420, S21 TO 25L, BS 480 S 21 TO 22L AND AT BS 500A 21 TO 25L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000060 19960620 00060 NM 1996 6 20 SWAA960510 1 19960611 A 5320 MOPSILL BOEING 737 7372H4 138448C NM BS 959-990 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21722 DURING SCHEDULED D-CHECK, FOUND AFT SERVICE DOOR MOPSILL CORRODED AT BS 959 TO 990, RBL 53 TO 48, WL 209. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000061 19960620 00061 NM 1996 6 20 SWAA960511 1 19960611 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 500 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21722 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME DENTED AT BS 500, RBL 33 AND RBL 26, WL 161 AND 169. REPLACED WITH NEW S ECTION PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000062 19960620 00062 NM 1996 6 20 SWAA960512 1 19960611 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 495 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21722 DURING SCHEDULED D-CHECK, FOUND STRINGER CRACKED AT BS 495, S22R. REPLACED WITH NEW SECTION PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000063 19960620 00063 NM 1996 6 20 SWAA960513 1 19960611 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 500 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21722 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME DENTED AT BS 500A, RBL 44 AND RBL 52 TO 56, WL 168, 179 TO 177. REPLACED WITH NEW SECTION PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000064 19960620 00064 NM 1996 6 20 SWAA960514 1 19960608 A 3350 6104781 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED SV CHECK, FOUND FWD OVERHEAD EMERGENCY EXIT LIGHTS INOP. REPLACED LIGHT BATTERY PACK PER BOEING M/M. 2 L 7 2 4F A16WE 1996062000065 19960620 00065 NM 1996 6 20 SWAA960515 1 19960611 A 5320 CEILING BOEING 737 7372H4 138448C NM NOSE W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 68SW 22357 DURING SCHEDULED 1/4 D-CHECK, FOUND .75 INCH CRACK AT PREVIOUS REPAIR IN NOSE W/W CENTER WEB REPAIR, EXTENDING FROM UNDE R RIVET HEAD. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000066 19960620 00066 NM 1996 6 20 SWAA960516 1 19960611 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 1121 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 68SW 22357 DURING SCHEDULED 1/4 D-CHECK, FOUND STRINGER 14R AT BS 1121 CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000067 19960620 00067 NM 1996 6 20 SWAA960517 1 19960611 A 5512 SKIN BOEING 737 7372H4 138448C NM HORIZ STAB DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 68SW 22357 DURING SCHEDULED 1/4 D-CHECK, FOUND RT HORIZ STAB GOUGED AND DENTED AT 4 PLACES ON LOWER SURFACE, 122 TO 130 O/B FROM FU SELAGE, 10 FWD OF REAR SPAR. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000068 19960620 00068 NM 1996 6 20 SWAA960518 1 19960611 A 5320 GUSSET BOEING 737 7372H4 138448C NM BS 259 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 68SW 22357 DURING SCHEDULED 1/4 D-CHECK, FOUND CRACK IN RADIUS OF NOSE GEAR ACTUATOR AFT SUPPORT FITTING REINFORCING GUSSET AT BS 2 59 NLG W/W CEILING. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000069 19960620 00069 NM 1996 6 20 SWAA960519 1 19960610 A 3350 1000679 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 95SW 23054 DURING SCHEDULED SV CHECK, FOUND EMERGENCY EXIT LIGHT ABOVE FWD ENTRY DOOR INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F A16WE 1996062000070 19960620 00070 NM 1996 6 20 SWAA960520 1 19960607 A 5330 SKIN BOEING 737 7372T4 1384492 NM PAX DOOR CUTOUT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED SV CHECK, FOUND FUSELAGE SKIN CRACKED .5 INCH ON LOWER AFT ENTRY DOOR CUTOUT. REPAIRED PER BOEING SRM AND S/B 737-53-1074. 2 L 7 2 4F A16WE 1996062000071 19960620 00071 NM 1996 6 20 SWAA960521 1 19960607 A 5330 SKIN BOEING 737 7372T4 1384492 NM SERV DR CUTOUT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED SV CHECK, FOUND FUSELAGE SKIN CRACKED .25 INCH ON UPPER HINGE CUTOUT AT AFT SERVICE DOOR. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000072 19960620 00072 NM 1996 6 20 SWAA960522 1 19960607 A 3350 6104781 BATTERY BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED SV CHECK, FOUND LEFT OVERWING EXTERNAL EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M . 2 L 7 2 4F A16WE 1996062000073 19960620 00073 NM 1996 6 20 SWAA960523 1 19960610 A 5512 SKIN BOEING 737 7375H4 138449D NM HORIZ STAB LE DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 511SW 24188 DURING SCHEDULED SV CHECK, FOUND LT HORIZ STAB L/E DENTED 2 PLACES. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996062000074 19960620 00074 NM 1996 6 20 SWAA960524 1 19960608 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 67SW 22356 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 540, LBL 41.5 ON HORIZ CHORD AFT FLANGE. REPAIRED PER SWA RA 1-253-1468. 2 L 7 2 4F A16WE 1996062000075 19960620 00075 NM 1996 6 20 SWAA960525 1 19960608 A 5320 DOOR FRAME BOEING 737 7372H4 138448C NM FWD CARGO CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 67SW 22356 DURING SCHEDULED C2 CHECK, FOUND FWD CARGO DOORWAY AFT FRAME CRACKED ON VERTICAL CHORD AT LOWER STOP FITTING, BETWEEN S2 4 AND 25R. REPAIRED PER SWA RA 1-253-1463. 2 L 7 2 4F A16WE 1996062000076 19960620 00076 NM 1996 6 20 VNAA9606005 1 19960611 A 5350 001A531A0000002 RADOME DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FWD FUSELAGE BIRD STRIKE A VNAA K NONE C F.O.D. TO TAKEOFF 1 GL 07 434JS 3051 SHORTLY AFTER T/O, THE CREW REPORTED STRIKING A BIRD IN THE VICINITY OF THE AIRCRAFT RADOME. CREW CONTINUED ON WITH THE FLIGHT AND LANDED IN PIT WITHOUT FURTHER INCIDENT. PIT MX INSPECTED THE AIRCRAFT AND DISCOVERED THAT THE RADOME HAD BE EN DAMAGED. THEY REPLACED THE RADOME IAW MM 53-10-00. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996062000078 19960620 00078 NM 1996 6 20 96ZZZX3020 1 19960413 A 5720 VENT TUBE BOEING 727 727231 1384079 NM WS 629 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54325 20232 JFK - DURING CHECK C-4D, FOUND A CRACK IN EAR ON VENT TUBE, STA 629, WS ABOVE RIB. INSTALLED AND SECURED REPAIR PER SB 727-57A159. AIRCRAFT TOTAL TIME: 63,700 HOURS; 42,677 CYCLES. 2 L 7 3 4F A3WE 1996062000079 19960620 00079 CE 1996 6 20 96ZZZX3021 1 19960314 A 2910 6000100287 TUBE ASSY LEAR 60 60LEAR 5170707 CE HYDRAULIC SYS CHAFED A OICA K NONE O OTHER IN INSP/MAINT 1 SW 09 799SC 067 DURING ACCESS FOR OTHER MAINTENANCE, THE EXTERNAL HYDRAULIC CART HIGH PRESSURE LINE, PN 6000100-287, WAS FOUND CHAFING O N THE RT HYDRAULIC ACCUMULATOR. A LEAK IN THIS AREA WOULD RESULT IN LOSS OF HYDRAULIC FLUID AS THERE IS NO CHECK VALVE UPSTREAM OF THIS LINE. ESTIMATED DEPTH OF CHAFE 0.008 INCH. THERE WERE ALSO .005 INCH TOOL MARKS AT THE UPPER B-NUT FE RRULE AREA. 2 L 7 2 4F RT A10CE 1996062000080 19960620 00080 1996 6 20 96ZZZX3022 3 19960215 A 6112 E62127 DEICE BOOT DORNER DO32 DO328100 2996000 NM LT PROPELLER DEFECTIVE A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 423JS 3032 FLT 4149 - THE LEFT PROPELLER DEICE FAILED EN ROUTE FROM KAY TO PHL. AIRCRAFT DIVERTED TO PIT. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. LATER THE AIRCRAFT WAS FERRIED TO CAK, WHERE MAINTENANCE REPLACED THE LEFT PROPELLER ASSY IAW MM 61- 00-00. GROUND CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A45NM 1996062000081 19960620 00081 NM 1996 6 20 AALA960516 1 19960327 A 5320 65225475 FITTING BOEING 727 727223 1384074 NM FS 1183 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 708AA 22465 ATL - DURING CONTRACT MAINTENANCE AT DALA FOR HEAVY C-CHECK. C/W AA ROUTINE CARD NR 4189, THE BORE OF THE TENSION TIE B OLT FITTING ON THE OUTBOARD FORWARD RIGHT SIDE OF THE BS 1183 TORQUE BOX STRINGER 3A WAS FOUND CORRODED. THE CORROSION WAS REMOVED BY REAMING THE BORE FROM THE ORIGINAL DIAMETER OF 0.750 INCH TO 0.781 INCH. REPAIR APPROVAL PER DER FORM 81 10-3 DATED 03-18, 1996, REF AD 90-06-09, DL ERA 303314-14AD. ACFT TT, 40,899 HRS. ACFT TC, 21,258. (X) 2 L 7 3 4F A3WE 1996062000082 19960620 00082 NM 1996 6 20 AALA960517 1 19960327 A 5240 65216364 DOOR FRAME BOEING 727 727223 1384074 NM E/E COMPT CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 708AA 22465 ATL - DURING CONTRACT MAINTENANCE AT DALA FOR HEAVY C-CHECK. MAINTENANCE FOUND A CRACK IN THE DOOR FRAME OF THE E/E COM PARTMENT. THE CRACK WAS 1 INCH LONG ON THE RT SIDE AT THE FASTENER HOLE AFT AND ABOVE OF THE LATCH PIN. MTC ALSO FOUND A 1 INCH CRACK IN THE LOWER RADIUS OF THE TRANSVERSE BEAM. REPAIRS WERE ACCOMPLISHED IAW SB 727-52-94, REV 2, REF: DL ERA 303317-14AD. ACFT TT: 40,899 HRS. ACFT TC, 21,258. (X) 2 L 7 3 4F A3WE 1996062000083 19960620 00083 NM 1996 6 20 AALA960519 1 19960404 A 5311 FRAME BOEING 727 727223 1384074 NM FS 784 LOOSE BUSHINGS A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 708AA 22465 ATL - DURING CONTRACT MAINTENANCE AT DALA FOR HEAVY C-CHECK. FUSELAGE OPENING FRAME AT FS 784 RIGHT, HAS LOOSE BUSHINGS IN LOCATIONS PREVIOUSLY INSTALLED PER AAL ESO 1523. NEW BUSHINGS WERE INSTALLED PER DL ERA 303303-14AD. ACFT TT, 40,8 99 HRS. ACFT TC, 21,258. (X) 2 L 7 3 4F A3WE 1996062000084 19960620 00084 NM 1996 6 20 AALA960520 1 19960404 A 5730 65877031 SKIN BOEING 727 727223 1384074 NM LT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 708AA 22465 ATL - DURING CONTRACT MAINTENANCE AT DALA FOR HEAVY C-CHECK. CORROSION DAMAGE WAS FOUND ON THE LOWER WING SKIN CENTER S ECTION BETWEEN S-3C AND S-4C ABOVE THE LT PLENUM CHAMBER. CORROSION WAS CLEANED AND A REPAIR SIMILAR TO SRM 57-30-3, FI GURE 10, WAS INSTALLED. DURING FASTENER REMOVAL, 2 FASTENER HOLES ON S-3C WERE DAMAGED, APPROXIMATELY .1250 INCH OF MAT ERIAL WAS CHIPPED OUT OF THE OUTER SURFACE. THE DAMAGE WAS REMOVED BY COUNTERSINKING THE HOLES. REPAIRS ACCOMPLISHED P ER DL ERA 303272-14 AD. ACFT TT, 40,899 HRS. ACFT TC, 21,258. (X) 2 L 7 3 4F A3WE 1996062000085 19960620 00085 NM 1996 6 20 AALA960721 1 19960402 A 5313 65564415 STRINGER BOEING 727 727223 1384074 NM FS 1000 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 715AA 22470 ATL - DURING CONTRACT MAINTENANCE AT DALA, FOUND STR 29L WITH SEVERAL AREAS OF CORROSION ON THE OUTBOARD SKIN ATTACH FLA NGE. THE DAMAGE WAS LOCATED AT FS 950C TO FS 1000. ACCOMPLISHED REPAIRS PER DL ERA 303390. ACFT TT: 39,457 HRS. ACF T TOTAL CYCLES: 21,587. (X) 2 L 7 3 4F A3WE 1996062000086 19960620 00086 NM 1996 6 20 AALA960722 1 19960411 A 5330 6554574 SKIN BOEING 727 727223 1384074 NM FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 715AA 22470 ATL - DURING CONTRACT MAINTENANCE AT DALA, THE UPPER FORWARD CORNER OF THE C-2 DOOR OPENING HAS HAD DAMAGE REMOVED FROM THE OUTER LAYER OF SKIN. THE RESULTING CUT-OUT IS 1.5 INCHES BY .75 INCH IN THE OUTER LAYER OF SKIN. ACCOMPLISHED REPA IRS PER DL ERA 303435-14. ACFT TT: 39,457 HRS. ACFT TOTAL CYCLES, 21,587. (X) 2 L 7 3 4F A3WE 1996062000087 19960620 00087 NM 1996 6 20 AALA960723 1 19960416 A 5720 651920122 CARRIAGE JOURNAL BOEING 727 727223 1384074 NM LT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 715AA 22470 ATL - DURING CONTRACT MAINTENANCE AT DALA FOR HEAVY C-CHECK, THE OUTBOARD CARRIAGE LARGE JOURNAL OF THE LT INBOARD FLAP WAS FOUND CORRODED. MAINTENANCE MACHINED THE OUTER DIAMETER DOWN TO 2.957 INCH AND THE INNER DIAMETER OUT TO 2.010 INCH ON THE TAPERED SECTION. THE DAMAGE DOES NOT EXTEND INTO THE TAPERED SECTION OF THE CARRIAGE JOURNAL. REPAIR APPROVAL PER DL ERA 357260-14. ACFT TT: 39,457 HRS. ACFT TOTAL CYCLES: 21,587. (X) 2 L 7 3 4F A3WE 1996062000088 19960620 00088 NM 1996 6 20 AALA960724 1 19960409 A 5720 6518522 WING CHORD BOEING 727 727223 1384074 NM BS 760 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 715AA 22470 ATL - DURING CONTRACT MAINTENANCE AT DALA FOR HEAVY C-CHECK, CRACKS WERE DISCOVERED IN THE VERTICAL FLANGE OF THE LBL AN D RBL 70.5 WING CHORD AT FS 760.95. REPAIRS WERE ACCOMPLISHED PER SB 727-57-0112, REV B. ACFT TT: 39,457 HRS. ACFT T OTAL CYCLES: 21,587. (X) 2 L 7 3 4F A3WE 1996062000089 19960620 00089 NM 1996 6 20 AWXA960226 1 19960507 A 5315 FLOOR BEAM BOEING 737 73733A 1384673 NM BS 294.5 CORROSION A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 PAE - FLT 7801 - DURING ROUTINE SCHEDULED C-5 MAINTENANCE CHECK, FOUND CORROSION ON TOP OF HORIZONTAL FLANGE OF FLOOR BE AM BS 294.5, RBL 24-41. REPAIRED IAW SRM 53-10-51. ACFT TT: 36,348. ACFT TC: 22,337. (X) 2 L 7 2 4F RT A16WE 1996062000090 19960620 00090 NM 1996 6 20 AWXA960227 1 19960511 A 5315 FLOOR BEAM BOEING 737 73733A 1384673 NM BS 663 MECH DAMAGE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 172AW 23631 PAE - FLT 7801 - DURING ROUTINE SCHEDULED C-5 MAINTENANCE CHECK, FOUND CUT INTO TOP OF LBL 45 LONGITUDINAL FLOOR BEAM BS 663. REPAIRED BEAM IAW E.R. 3-53-16-33 (TCO-PAN-96-0576RR). ACFT TT: 36,348. ACFT TC: 22,337. (X) 2 L 7 2 4F RT A16WE 1996062000091 19960620 00091 NM 1996 6 20 AWXA960228 1 19960503 A 5753 6546481110 CARRIAGE BOEING 737 7373G7 1384595 NM RT TE FLAP CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 151AW 23219 PAE - FLT 3828 - DURING ROUTINE SCHEDULED C-12 MAINTENANCE CHECK, FOUND RT WING OUTBOARD FLAP INBOARD CARRIAGE THRUST BE ARING CORRODED IN FLAP. NO CORROSION NOTED ON OUTBOARD WING FLAP AND REMOVED AND REPLACED BEARING PER MM 27-51-44. REF ER - CUSTOMER ID NR 00344610 (WINGS 092). ACFT TT: 34,559. ACFT TC: 30,334. (X) 2 L 7 2 4F RT A16WE 1996062000092 19960620 00092 NM 1996 6 20 AWXA960229 1 19960503 A 5753 6546481106 CARRIAGE BOEING 737 7373G7 1384595 NM RT TE FLAP CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 151AW 3183 23219 PAE - FLT 3828 - DURING ROUTINE SCHEDULED C-12 MAINTENANCE CHECK, FOUND RT OUTBOARD FLAP INBOARD CARRIAGE SPINDLE CORROD ED. REMOVED AND REPLACED RT OUTBOARD FLAP INBOARD CARRIAGE PER TASK CARD 13R57057. ACFT TT: 34,559. ACFT TC: 30,334 . (X) 2 L 7 2 4F RT A16WE 1996062000093 19960620 00093 NM 1996 6 20 AWXA960230 1 19960430 A 5315 FLOOR BEAM BOEING 737 7373G7 1384595 NM BS 312 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 151AW 23219 PAE - FLT 3828 - DURING ROUTINE SCHEDULED C-12 MAINTENANCE CHECK, FOUND CORROSION ON UPPER CHORD ON FLOOR BEAM AT STA 31 2, LBL 20 - RBL 22, WL 208. REMOVED DAMAGED UPPER CHORD BS 312, LBL 20, RBL 22, WL 208 AND INSTALLED FABRICATED PART, A LODINED AND PRIMED PER SRM 53-10-51. ACFT TT: 34,561. ACFT TC: 30,335. (X) 2 L 7 2 4F RT A16WE 1996062000094 19960620 00094 NM 1996 6 20 AWXA960231 1 19960501 A 5320 STRINGER BOEING 737 7373G7 1384595 NM BS 500 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 151AW 23219 PAE - FLT 3828 - DURING ROUTINE SCHEDULED C-12 MAINTENANCE CHECK, FOUND CORROSION AROUND NUTPLATE HOLES ON SUB-THESHOLD BS 440 TO BS 491, WL 154. CORRODED BEYOND LIMITS. REMOVED CORRODED SUB-THRESHOLD, FABRICATED AND INSTALLED NEW SUB-THR ESHOLD. ALL PER SRM'S 53-30-15, 51-30-01, 51-10-02. ACFT TT: 34,561. ACFT TC: 30,335. (X) 2 L 7 2 4F RT A16WE 1996062000095 19960620 00095 NM 1996 6 20 AWXA960238 1 19960515 A 5313 STRINGER BOEING 737 737301 1384611 NM BS 500 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 DURING ROUTINE SCHEDULED C-11 MAINTENANCE CHECK, FOUND STR 27R BLOWN AT BS 500D. CUT OUT DAMAGED STR 17R, BS 500D, FABR ICATED PART AND INSTALLED PER SRM 53-00-03. ACFT TT: 34,284. ACFT TC: 22,222. (X) 2 L 7 2 4F RT A16WE 1996062000096 19960620 00096 NM 1996 6 20 AWXA960239 1 19960515 A 5712 RIB BOEING 737 737301 1384611 NM WS 200 GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 PAE - FLT 7805 - DURING ROUTINE SCHEDULED C-11 MAINTENANCE CHECK, FOUND RIGHT WING FIXED LEADING EDGE RIB AT LEADING EDG E STA 208 GOUGED ON LOWER SURFACE FROM SEAL RETAINER ON NR 4 K-FLAP T/R CLOSURE DOOR. REPAIRED RT WING L/E RIB AT L/E S TA 208, IAW ER 3-57-21-14. TCO-PAN-941354RR AND 737-SL-57-27. ACFT TT: 34,284. ACFT TC: 22,222. (X) 2 L 7 2 4F RT A16WE 1996062000097 19960620 00097 NM 1996 6 20 AWXA960240 1 19960516 A 5315 FLOOR BEAM BOEING 737 737301 1384611 NM BS 986 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 PAE - FLT 7805 - DURING ROUTINE SCHEDULED C-11 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM AT STA 986, LBL 46 - RBL 46, WL 208. REMOVED, FABRICATED, INSTALLED REPAIR PARTS PER SRM'S 53-00-51, 51-10-02, 51-40-02. ACFT TT: 34,282. AC FT TC: 22,222. (X) 2 L 7 2 4F RT A16WE 1996062000098 19960620 00098 NM 1996 6 20 AWXA960241 1 19960516 A 5320 WEB BOEING 737 737301 1384611 NM BS 1000 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 324AW 23261 PAE - FLT 7805 - DURING ROUTINE SCHEDULED C-11 MAINTENANCE CHECK, FOUND WEB CRACKED AT STA 1000, LBL 40, WL 208. FABRIC ATED NEW WEB, INSTALLED PER SRM 51-40-02 AND SRM 51-10-02. ACFT TT: 34,261. ACFT TC: 22,222. (X) 2 L 7 2 4F RT A16WE 1996062000099 19960620 00099 CE 1996 6 20 PLG41496G1 1 19960414 A 7120 12991003279 ENGINE TRUSS BEECH 1900 1900C 1154161 CE UPPER INBOARD CRACKED A A PLGA K NONE O OTHER IN INSP/MAINT 1 NE 05 3067X UB67 DURING C/W AD 95-02-18 IAW BEECH SB 2255, RIGHT ENGINE TRUSS WAS FOUND TO HAVE A .50 INCH CRACK EMANATING FROM BOTH SIDE S OF UPPER INBOARD LINSEED OIL RIVET HOLE. TRUSS WAS REPLACED WITH SERVICEABLE ASSEMBLY. (X) 2 L 7 2 4T RT A24CE 1996062000100 19960620 00100 EU 1996 6 20 PLG41496G2 1 19960414 A 3310 4493 POWER SUPPLY SAAB SF340 SF340A 7850100 EU RT INSTR PANEL FAILED A PLGA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NE 05 346BE 9036 340A150 PWM - FLT 4796 - EN ROUTE (10 MILES OUT) REPORTED A SMOKE SMELL IN THE CABIN. THE CREW SHUT OFF THE LT ACM PACK AND LT RECIRC FAN AT WHICH POINT THE SMELL SEEMED TO GO AWAY. UPON LANDING, THE F/O'S INSTRUMENT LIGHTS FAILED FOLLOWED BY SMO KE IN THE COCKPIT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT AND DETERMINED THE RT INSTRUMENT LIGHT POWER SUPPLY HAD F AILED CAUSING THE SMOKE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY. THE NR 2 VSI AND NR 2 PROP OIL PRESSURE GA UGE WERE ALSO REPLACED DUE TO INOPERATIVE LIGHTING. CIRCUIT BREAKER 4LL REPLACED FOR PRECAUTIONARY REASONS. (X) 2 L 7 2 4T RT A52EU 1996062000112 19960620 00112 NM 1996 6 20 RAAAB196002 1 19960115 A 3350 8621006 BATTERY PACK 8731001112 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 ROW 22 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. REPLACED BATTERY PACK DUE TO LOW CHARGE. (X) 2 L 7 3 4F A3WE 1996062000114 19960620 00114 NE 1996 6 20 RAIA960438 3 19960428 A 6111 SFA13M10A BLADE AEROSP ATR42 ATR42300 8680920 EU HAMSTD 14SF 14SF5 NE NR 2 PROPELLER OUT OF BALANCE A RAIA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 CE 03 EICBF 13346 5877 176 8609975 STL - FLT 7230 - AIRCRAFT VIBRATES IN-FLIGHT. MAINTENANCE REPLACED THE NR 2 BLADE ON THE NR 2 PROPELLER. OPS CHECK GOO D. (X) 2 H 7 2 4T RT A53EU 6 C P7NE 1996062000115 19960620 00115 EU 1996 6 20 RAIA960501 1 19960502 A 5270 91SE13 SWITCH BAG JETSTM JETSTM3201 1500217 EU PASSENGER DOOR OUT OF ADJUST A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 436AM 10707 891 STL - FLT 7342 - PASSENGER DOOR WARNING LIGHT ILLUMINATED. VERIFIED DOOR LATCHING PROPERLY, MICROSWITCH REQUIRES ADJUST MENT. SYSTEM DEFERRED PER MEL 52-2. (X) 2 L 7 2 4T RT A56EU 1996062000116 19960620 00116 WP 1996 6 20 USAA960438 1 19960529 A 5530 ANGLE DOUG DC9 DC931 3022065 WP VERTICAL STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 966VJ 69060 47420 PIT - DURING Q-4 CHECK INSPECTION, FOUND 2 INCH CRACK IN DRAG ANGLE RADIUS RT VERTICAL STABILIZER. DRAG ANGLE STA 1089. INSTALLED REPAIR ANGLE PER SRM 53-05, FIGURE 23. (X) 2 L 7 2 4F A6WE 1996062000117 19960620 00117 WP 1996 6 20 USAA960440 1 19960523 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 256 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 823US 35146 49142 PIT - DURING A SCHEDULED Q-2/C-6 CHECK INSPECTION, FOUND A .50 INCH CRACK IN LONGERON 17L LOWER FASTENER TO FRAME AT STA 256, VISUALLY. SPLICED IN NEW SECTION OF LONGERON STA 230 TO STA 273 PER SRM 53-02, FIGURE 2. (X) 2 L 7 2 4F A6WE 1996062000118 19960620 00118 WP 1996 6 20 USAA960464 1 19960523 A 5320 1097198 FITTING DOUG DC9 DC982 3022082 WP VENTRAL DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 823US 35104 49142 PIT - DURING A SCHEDULED Q-2/C-6 CHECK INSPECTION, FOUND VENTRAL DOOR JAMB RIGHT OUTBOARD FITTING CRACKED BETWEEN NR 5 A ND NR 6 RADIAL. FITTING WAS REPLACED PER 53-14-3, FIGURE 2, AND DACO DRAWING 5917579. (X) 2 L 7 2 4F A6WE 1996062000119 19960620 00119 WP 1996 6 20 USAA960466 1 19960524 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 1437 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 816US 38993 48096 PIT - DURING C-1 CHECK INSPECTION, FOUND A 1 INCH SKIN CRACK STA 1437, LONGERON 3L. INSTALLED DOUBLER REPAIR 2024T-3.08 0 INCH PER SRM 53-04, FIGURE 27, PAGE 143. (X) 2 L 7 2 4F A6WE 1996062000120 19960620 00120 NM 1996 6 20 USAABB96016 1 19960519 A 3350 20121 BATTERY CHARGER BOEING 767 7672B7 1385107 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 653US 24894 FRA - FOUND THE FLOOR EMERGENCY LIGHTING SECTION L901 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER, PACK, AND SEVERAL LAMPS. ALSO, REPAIRED TWO WIRE BREAKS. (X) 2 L 7 2 4F RT A1NM 1996062000121 19960620 00121 WP 1996 6 20 USAAD96060 1 19960523 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN LOOSE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 951VJ 47576 CLT - ON GROUND, EMERGENCY LIGHTS ARM AND CHARGE, CIRCUIT BREAKER TRIPS. SECURED LOOSE WIRE IN FLOOR LIGHTING, ROW 20. (X) 2 L 7 2 4F A6WE 1996062000122 19960620 00122 EU 1996 6 20 USAAF96052 1 19960525 A 2131 1026446 CONTROLLER FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 481US 7698 4079 11230 CLT - FLT 2309 - AFTER TAKEOFF, CABIN WOULD NOT PRESSURIZE. THE CAPTAIN LEVELED OFF AT 9,000 FEET AND RETURNED TO THE F IELD WITHOUT INCIDENT. MAINTENANCE REPLACED THE CABIN PRESSURE CONTROLLER. (X) 2 L 7 2 4F RT A20EU 1996062000123 19960620 00123 EU 1996 6 20 USAAF96053 1 19960528 A 2170 COALESCER BAG FOKKER F28 F28MK0100 4990807 EU CABIN CONTAMINATED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 850US 11276 CLT - FLT 1543 - DURING CLIMB-OUT OF CLT, BOTH LAVATORY SMOKE DETECTORS ACTIVATED IN AIRCRAFT. CAPTAIN DECLARED EMERGEN CY AND RETURNED TO FIELD IN CLT. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE RT PACK OIL QUANTITY OV ERSERVICED AND WATER SEPARATOR CONTAMINATED WITH OIL. MAINTENANCE REPLACED WATER SEPARATOR BAG AND DRAINED OIL TO PROPE R LEVEL. RAN PACK. NO SMOKE NOTED FROM PACK. (X) 2 L 7 2 4F RT 1996062000124 19960620 00124 NE 1996 6 20 USAASB96091 2 19960527 A 7200 ENGINE BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE RIGHT BIRD STRIKE A USAA A UNSCHED LANDING C F.O.D. CL CLIMB 1 EA 19 355US 23558 EWR - FLT 1293 - AFTER ROTATION FROM LGA AT APPROXIMATELY 100 FEET, CREW SAW 5 TO 9 SEAGULLS AHEAD OF THE AIRCRAFT. THE RIGHT ENGINE INGESTED ONE LARGE SEAGULL. CREW ELECTED TO MAKE A PRECAUTIONARY LANDING AT EWR ALTHOUGH ENGINE PARAMETER S WERE NORMAL. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED IN EWR WITH NO FURTHER INCIDENT. MAINTENANCE FOUND AND REPLACED THE FOLLOWING ITEMS ON THE RT ENGINE DUE TO BIRD INGESTION: NR 6, NR 7, AND NR 8 FAN BLADES (DAMAGED), CSD OIL COOLER (CLOGGED) AND THE T-2 AND T-12 SENSORS (DAMAGED). NOTE: FAN BLADES NR 25, NR 26, AND NR 27 WERE REPLACED DUE T O REPLACEMENT OF FAN BLADES, NR 6, NR 7, AND NR 8. (X) 2 L 7 2 4F 4 F RT A16WE E2GL 1996062000125 19960620 00125 NM 1996 6 20 USAASB96096 1 19960531 A 3260 189915 SENSOR BOEING 737 737301 1384611 NM RT MLG FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 341US 23510 GSO - FLT 2338 - AFTER DEPARTURE FROM PHL AND GEAR RETRACTED, THE RIGHT MLG DOWNLOCK LIGHT REMAINED ILLUMINATED. FLIGHT DIVERTED TO GSO AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE TROUBLESHOT SYSTEM TO A BAD DOWNLOCK SENSOR. THE RIG HT MLG DOWNLOCK SENSOR WAS REMOVED AND REPLACED. OPS CHECKED GOOD. (X) 2 L 7 2 4F RT A16WE 1996062000126 19960620 00126 NM 1996 6 20 9613042289 1 19960610 A 2133 10328041 OUTFLOW VALVE BOEING 727 727251 138408H NM CABIN MALFUNCTIONED A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 289US 21377 DURING CLIMB, COULD NOT CONTROL CABIN PRESSURIZATION. DESCENDED TO FLIGHT LEVEL 8,000 FEET AND CONTINUED TO GRR. AIRCR AFT LANDED WITHOUT INCIDENT. DTW MAINTENANCE REPLACED BOTH OUTFLOW VALVES AND PERFORMED PRESSURIZATION CHECK, CHECKED O K. 2 L 7 3 4F A3WE 1996062000127 19960620 00127 WP 1996 6 20 9613059178 1 19960613 A 3350 BATTERY PACK DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 3310L 45705 DURING LINE CHECK, FOUND RIGHT NACELLE EMERGENCY LIGHT OUT. REPLACED BATTERY PACK, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996062000128 19960620 00128 WP 1996 6 20 9613069302 1 19960613 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 302RC 48055 DURING LINE CHECK, FOUND EMERGENCY LIGHT BATTERY PACK DEAD AT ROW 6 AND 7. REPLACED BATTERY PACK, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996062000129 19960620 00129 WP 1996 6 20 9613079603 1 19960613 A 3297 WIRE DOUG DC9 DC932 3022066 WP RT MLG CHAFED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 603NW 47101 RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. FLIGHT RETURNED TO MSP AND LANDED WITHOUT IN CIDENT. MAINTENANCE REPAIRED CHAFED WIRES 2G206E24 AND 2G204E24 IN RIGHT WHEEL WELL. OPERATIONAL CHECK NORMAL ON GEAR SWING. 2 L 7 2 4F A6WE 1996062000130 19960620 00130 NM 1996 6 20 9613086638 1 19960613 A 3350 BATTERY PACK BOEING 747 747251B 1384892 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 638US 23549 DURING LINE CHECK, FOUND A ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996062000131 19960620 00131 WP 1996 6 20 9613099308 1 19960613 A 5220 591015931 DOOR DOUG DC9 DC982 3022082 WP CABIN NOT SEALED A NWAA A UNSCHED LANDING J WARNING INDICATION IN INSP/MAINT 1 GL 01 311RC 48089 DURING CLIMB, THE AIRCRAFT FAILED TO PRESSURIZE AND THE RIGHT AFT OVERWING EMERGENCY EXIT DOOR DID NOT APPEAR TO BE FULL Y SEALED, RETURNED TO MSP WITHOUT FURTHER INCIDENT. FOUND THE DOOR NOT SEATED IN THE FRAME. REMOVED AND INSPECTED THE DOOR, NO TROUBLE FOUND. DOOR REINSTALLATION WAS NORMAL. 2 L 7 2 4F A6WE 1996062000132 19960620 00132 NM 1996 6 20 96UAL900268 1 19960417 A 2450 B430 TIE BREAKER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LEFT DAMAGED A UALA H DEACTIVATE SYST/CIRCUITS R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 WP 29 610UA 21871 CREW REPORTS LEFT ENGINE GENERATOR INOPERABLE AND WILL NOT POWER BUS. THE IDG WAS DISCONNECTED. *S/D* A DAMAGED PIN I N LEFT BUS TIE BREAKER CAUSED INTERMITTENT OPENING OF THE LEFT INTEGRATED DRIVE GENERATOR CONTROL BREAKER. THE INTEGRAT ED DRIVE GENERATOR BREAKER WAS REPLACED. 2 L 7 2 4F 4 F RT A1NM E3NE 1996062000133 19960620 00133 NE 1996 6 20 96UAL900404 2 19960604 A 7230 COMPRESSOR BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE NR 1 ENGINE STALLED A A UALA O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 WP 29 606UA 21867 709528 NUMBER ONE ENGINE COMPRESSOR STALLED IN FLIGHT. ENGINE DID NOT SHUTDOWN, IT RECOVERED AND CONTINUED TO CNF UNDER NORMAL CONDITIONS. NO ENGINE PARAMETERS WERE EXCEEDED. *S/D* ENGINE WAS REMOVED AND ANALYZED IN TEST CELL. THE ENGINE MET ALL LIMITS WITHIN THE UAL ENGINE TEST SPECIFICATION. THE AIRCRAFT WAS FLYING THROUGH TURBULENCE. RESULTS OF FLIGHT REC ORDER DATA INDICATE ALTITUDE, TURBULENCE AND AUTO THROTTLE BEING ENGAGED INDUCED THE COMPRESSOR STALL. WE ARE NOW WORKI NG ON NEW FLIGHT PROCEDURES DURING TURBULENCE AND INCREASED TRAINING AWARENESS OF ADVERSE WEATHER PROCEDURES. 2 L 7 2 4F 4 F RT A1NM E3NE 1996062000134 19960620 00134 NM 1996 6 20 96UAL900431 1 19960611 A 3350 POWER CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 657UA 27112 FOUND INOPERABLE EMERGENCY EVACUATION LIGHT STRIP FROM SEAT 11E BACK TO 19E. FOUND SIDEWALL CONNECTOR DAMAGED. REPLACE D COMPLETE POWER CABLE FROM SIDEWALL TO LIGHT STRIPS. OPERATIONS CHECK INDICATES EEL NOW FULLY OPERATIONAL. 2 L 7 2 4F 4 F RT A1NM E24NE 1996062000135 19960620 00135 NM 1996 6 20 96UAL900432 1 19960611 A 3350 STRIP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 659UA 27114 EMERGENCY EVACUATION LIGHTING STRIP AT CLOSET INOPERABLE. REPAIRED EEL STRIP. 2 L 7 2 4F 4 F RT A1NM E24NE 1996062000136 19960620 00136 NM 1996 6 20 96UAL900433 1 19960611 A 2613 355604310 OVERHEAT ELEMENT BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE LT WING/BODY FAILED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 923UA 26643 AFTER TAKEOFF, LEFT WING/BODY OVERHEAT LIGHT CAME ON. ACCOMPLISHED IRREGULAR PROCEDURE, BUT LIGHT STAYED ON. RETURNED TO DEN. *S/D* FOUND OVERHEAT ELEMENT BAD. REPLACED M487 ELEMENT, CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1996062000137 19960620 00137 NM 1996 6 20 96UAL900434 1 19960611 A 2751 1812996 POSITION IND BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE TE FLAPS MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 9052U 19933 TRAILING EDGE FLAPS LOCKED OUT HYDRAULICALLY AT 2.5 DEGREES, NEEDLES WERE MATCHED. CREW SELECTED ALTERNATE FLAPS TO TRY TO GET TO 15 DEGREES. ALTERNATE FLAPS CAUSED BOTH NEEDLES TO INCREASE 1 TO 2 DEGREES. CREW WAS NOT SURE IF FLAPS MOVE D OR IF IT WAS A INDICATION PROBLEM. LANDED WITH FLAPS AT 2 DEGREES. *S/D* TRAILING EDGE FLAP POSITION INDICATOR WAS DETERMINED TO BE THE CAUSE OF THE DISCREPANCY. THE INDICATOR WAS REPLACED AND THE TRAILING EDGE FLAP SYSTEM CHECKED GOO D BOTH HYDRAULICALLY AND ELECTRICALLY. 2 L 7 2 4F 4 F A16WE E2EA 1996062000138 19960620 00138 NM 1996 6 20 96UAL900435 1 19960422 A 3830 AS226B46 O-RING BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE M2 LAV DRAIN CUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 601UA 21862 THE M2 LAVATORY TOILET DRAIN O-RING SEAL WAS PINCHED AND CUT DURING ASSEMBLY OF DRAIN CAUSING WASTE WATER TO LEAK ONTO T HE CENTER WING INTERSPAR UPPER SKIN PANEL. THIS RESULTED IN SEVERE CORROSION DAMAGE TO THE SKIN WITH A ONE INCH DIAMETE R HOLE CORRODED ALL THE WAY THROUGH. *S/D* THE O-RING WAS REPLACED AND THE DAMAGED WING SKIN WAS CUT OUT AND REPAIRED. THIS WAS DISCOVERED DURING A 12C MAINTENANCE VISIT. 2 L 7 2 4F 4 F RT A1NM E3NE 1996062000139 19960620 00139 NM 1996 6 20 96UAL900436 1 19960611 A 3350 60243 LIGHT BOEING 737 737522 138449F NM CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 957UA 26707 FORWARD GALLEY EMERGENCY ESCAPE PATH LIGHTING INOP. REPLACED EMERGENCY ESCAPE PATH LIGHT STRIP. 2 L 7 2 4F RT A16WE 1996062000140 19960620 00140 1996 6 20 96UAL900437 2 19960611 A 7230 1663M24P02 BLADE BOEING 737 737322 1384676 NM NR 2 ENGINE FAILED A UALA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 WP 29 330UA 20928 4855 24191 NUMBER TWO ENGINE FAILED WHILE CLIMBING THROUGH FL310. *S/D* THE NUMBER 16 POSITION FAN BLADE FAILED AT THE BLADE DOVET AIL, RESULTING IN HIGH ROTOR IMBALANCE AND SECONDARY ENGINE DAMAGE. THE CAUSE OF THE BLADE DAMAGE IS BEING INVESTIGATED AT THIS TIME. 2 L 7 2 4F RT A16WE 1996062000141 19960620 00141 NM 1996 6 20 96UAL900438 1 19960611 A 2820 FUEL TANK BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RT MAIN TANK LEAKING A UALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 769UA 26921 FUEL LEAKING FROM RIGHT MAIN TANK INTO CENTER TANK. CENTER TANK AND FUEL IMBALANCE ADVISORY. TAKEOFF FUEL WAS IN BALAN CE AND NO FUEL IN CENTER TANK. FUEL MOVING AT A RATE OF 100 POUNDS EVERY 6 TO 8 MINUTES. 2 L 7 2 4F 4 F RT T0001SE E46NE 1996062000142 19960620 00142 NM 1996 6 20 96UAL900439 1 19960612 A 2730 CONTROLS BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE ELEVATOR STIFF A UALA O OTHER F FLT CONT AFFECTED DE DESCENT 1 WP 29 662UA 27159 UNABLE TO HOLD ALTITUDE AT 10,000 FEET ON AUTO-PILOT. DISCONNECTED AUTO-PILOT AND ELEVATOR WAS STIFF. FLEW FOR 5 TO 10 MINUTES USING STABILIZER FOR PITCH CONTROL. WHILE PUSHING UP AND DOWN SOMETHING LET GO AT 4,000 FEET. AIRCRAFT FLEW N ORMAL FOR THE REST OF THE FLIGHT. *S/D* PERFORMED VISUAL INSPECTION OF CONTROL CABLE SYSTEM PER MM 27-31-00. NO FAULT S WERE FOUND IN MAINTENANCE CONTROL DISPLAY UNIT. CHECKED ELEVATOR WITH EACH HYDRAULIC SYSTEM INDIVIDUALLY AND FOUND NO FAULTS. NO SPECIFIC PARTS FOUND DAMAGED OR FAULTED. 2 L 7 2 4F 4 F RT A1NM E24NE 1996062000143 19960620 00143 NM 1996 6 20 96UAL900440 1 19960612 A 7830 834802 PROX SENSOR BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LT ENG TR UNIT OUT OF ADJUST A UALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 29 608UA 21869 LEFT ENGINE THRUST REVERSER UNLOCKED LIGHT ILLUMINATED DURING TAKEOFF ROLL. TAKEOFF ABORTED AT APPROXIMATELY 100 KNOTS. *S/D* THE LOCK PROXIMITY SENSOR WAS OUT OF ADJUSTMENT. THE SENSOR WAS REPLACED, OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 1996062000144 19960620 00144 WP 1996 6 20 96UAL900441 1 19960612 A 5280 ANB70931 CTR HINGE DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL LT MLG DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 1832U 46631 LEFT HAND MAIN LANDING GEAR DOOR CENTER HINGE CRACKED AT REACTION LINK. REPLACED HINGE. 2 L 7 3 4F 4 F A22WE E23EA 1996062000145 19960620 00145 NE 1996 6 20 96UAL900442 2 19960612 A 7230 BLADE PWA BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE FAILED A UALA A E UNSCHED LANDING ENGINE SHUTDOWN R J Y PARTIAL RPM/PWR LOSS WARNING INDICATION ENGINE STOPPAGE CL CLIMB 1 WP 29 504UA 717962 24625 717962 AFTER TAKEOFF, HEARD A POP. LEFT ENGINE EGT INCREASED. REDUCED THROTTLE POSITION ON LEFT ENGINE. EGT CONTINUED TO INC REASE. SHUT LEFT ENGINE DOWN AND RETURNED TO FIELD. 9TH STAGE BLADE FAILURE. REPLACED ENGINE. OPERATION CHECKS NORMA L. 2 L 7 2 4F 4 F RT A2NM E17NE 1996062000146 19960620 00146 NM 1996 6 20 96UAL900443 1 19960612 A 3230 65B8293116 CONTROL MODULE BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE NLG DIRTY A UALA L ABORTED APPROACH J WARNING INDICATION LD LANDING 1 WP 29 161UA 21352 NOSE GEAR HAD TO BE EXTENDED BY ALTERNATE SYSTEM, HAD A RED GEAR LIGHT AND NO ALTERNATE NOSE GEAR OPEN LIGHT. GPWS SYST EM GAVE AN AURAL GEAR WARNING, CYCLED GEAR. *S/D* DETERMINED THAT GEAR HANDLE WAS NOT MOVING INTO FORWARD DETENT WHEN PUT IN DOWN POSITION. CLEANED SHAFT AND DEBRIS FROM GEAR HANDLE MODULE. CYCLED NOSE GEAR NUMEROUS TIMES, OPS CHECKS OK . 2 L 7 4 4F 4 F A20WE E20EA 1996062000147 19960620 00147 NM 1996 6 20 96UAL900444 1 19960612 A 3397 58631 WIRE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7457U 21911 EMERGENCY EXIT LIGHT FORWARD OF DOOR 1 LT DOES NOT ILLUMINATE WHEN TESTED. *S/D* FEEDER CABLE ASSEMBLY SUPPLYING POWER TO EXIT SIGN FOUND DAMAGED. CABLE ASSEMBLY REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 1996062000149 19960620 00149 NM 1996 6 20 96UAL900446 1 19960612 A 3231 69216674 STOP BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NLG FWD DOOR OUT OF ADJUST A UALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 29 7283U 21561 NOSE GEAR FLUTTER IN FLIGHT. FLICKERING NOSE GEAR DOOR LIGHTS, BOTH CAUTION AMBER ON S/O PANEL AND RED NOSE GEAR LIGHTS ON AT 370 KNOTS IN DESCENT. LIGHT OUT FLUTTER STOPS AT 340 KNOTS. GEAR HANDLE POSITION OFF. *S/D* ADJUSTED FWD NOSE GEAR DOOR AFT STOPS AND ADJUSTED DOOR MECHANISM CABLES. RETRACTION CHECKED NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1996062000150 19960620 00150 1996 6 20 96UAL900447 4 19960613 A 2565 SLIDE DOUG DC10 DC1030 3023501 WP DOOR 3L FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 1854U 47813 DURING SHOP OVERHAUL OF SLIDE/RAFT FROM DOOR 3L, REMOVED FOR TIME EXPIRATION, RAMP PORTION EXPERIENCED INTERNAL BULKHEAD SEPARATION WHEN INFLATED. CAUSE UNDETERMINED. SCRAPPED RAMP PORTION OF SLIDE/RAFT. 2 L 7 3 4F A22WE 1996062000151 19960620 00151 1996 6 20 96UAL900448 4 19960613 A 2565 SLIDE DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL DOOR 3L FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 1828U 46627 DURING SHOP OVERHAUL OF SLIDE/RAFT FROM DOOR 3L, REMOVED FOR OVERHAUL TIME EXPIRATION, RAMP PORTION OF SLIDE EXPERIENCED INTERNAL BULKHEAD SEPARATION WHEN INFLATED. CAUSE UNDETERMINED. SCRAPPED RAMP. 2 L 7 3 4F 4 F A22WE E23EA 1996062000152 19960620 00152 1996 6 20 96UAL900449 4 19960614 A 2565 SLIDE AIRCRUISERS 24D3005193 DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE R3 DOOR FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 1856U 1493 46975 DURING SHOP OVERHAUL OF SLIDE/RAFT FROM DOOR 3L, REMOVED FOR OVERHAUL TIME EXPIRATION, RAMP PORTION OF SLIDE EXPERIENCE D INTERNAL BULKHEAD SEPARATION DURING INFLATION. SUPPLEMENTAL DATA UPDATE: SUBMITTER STATES CAUSE UNDETERMINED. SCRAPP ED RAMP. 2 L 7 3 4F 4 F A22WE E23EA 1996062000153 19960620 00153 NM 1996 6 20 CALA9600806 1 19960612 A 2612 FIRE LOOP BOEING 737 737217 1384464 NM APU BURNED A CALA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 SW 09 12230 19884 THE APU FIRE WARNING LIGHT BEGAN TO FLASH INTERMITTENTLY APPROXIMATELY FIVE MINUTES INTO THE FLIGHT WITH THE APU SHUT DO WN. THE APU FIRE HANDLE WAS PULLED AND THE FIRE LIGHT FLASHING CEASED AFTER 45 SECONDS. THE AIRCRAFT WAS RETURNED TO E WR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE APU TAILPIPE FIRE LOOP WIRES BURNT AND TOUCHING TAILPIPE. T HE BARE WIRES WERE TEMPORARILY TAPED AND THE APU FIRE DETECTION SYSTEM WAS PLACARDED INOPERATIVE PENDING REPAIR OF WIRES . IN ADDITION, THE APU FIRE BOTTLE WAS REMOVED AND REPLACED. 2 L 7 2 4F A16WE 1996062000154 19960620 00154 NM 1996 6 20 CALA9600807 1 19960426 A 3350 602094001 SIGN BOEING 737 737217 1384464 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16232 19886 THE SELF ILLUMINATING EXIT SIGN IN AFT CABIN FAILED ILLUMINOSITY CHECK. THE EXIT SIGN WAS REMOVED AND REPLACED. 2 L 7 2 4F A16WE 1996062000155 19960620 00155 NM 1996 6 20 CALA9600808 1 19960429 A 5330 SKIN BOEING 737 737217 1384464 NM BS 1120 CREASED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16232 19886 INSPECTION FOUND A 3 INCH CREASE IN FUSELAGE SKIN AT STA 1120, BL 0. THE CREASED AREA WAS CUT OUT. A DOUBLER WAS FABRI CATED AND INSTALLED IAW SRM 53-30-3. 2 L 7 2 4F A16WE 1996062000156 19960620 00156 NM 1996 6 20 CALA9600809 1 19960429 A 5230 SKIN BOEING 737 737217 1384464 NM FWD CARGO DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16232 19886 INSPECTION FOUND SEVERAL DENTS IN FORWARD CARGO DOOR SKIN. THE DENTED AREA WAS CUT OUT, A DOUBLER WAS FABRICATED AND IN STALLED IAW SRM 52-00-3, 51-30-2 AND 51-10-2. 2 L 7 2 4F A16WE 1996062000157 19960620 00157 NM 1996 6 20 CALA9600810 1 19960503 A 5315 FLOORBEAM BOEING 737 737217 1384464 NM BS 328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16232 19886 INSPECTION FOUND FLOORBEAM CORRODED AT STA 328. THE FLOORBEAM WAS REMOVED AND A NEW FLOORBEAM WAS FABRICATED AND INSTAL LED IAW SRM 53-10-9 AND MM 51-20. 2 L 7 2 4F A16WE 1996062000158 19960620 00158 NM 1996 6 20 CALA9600811 1 19960504 A 5315 FLOORBEAM BOEING 737 737217 1384464 NM BS 294 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16232 19886 INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 294, RBL 40 TO 55. THE CORRODED SECTION OF CHORD WAS CUT OUT, A REPLACEMENT CHORD AND L-ANGLE DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-10-9, 52-20-1 AND 52-10-2. 2 L 7 2 4F A16WE 1996062000159 19960620 00159 NM 1996 6 20 CALA9600812 1 19960501 A 5311 FRAME BOEING 737 737217 1384464 NM BS 480 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16232 19886 INSPECTION FOUND A 3 INCH CRACK IN FORWARD CARGO FRAME AT STA 480, S21L. THE CRACK WAS STOP DRILLED IAW SRM 51-10-6. R EPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-30-2 AND 51-10-2. 2 L 7 2 4F A16WE 1996062000160 19960620 00160 WP 1996 6 20 CALA9600813 1 19960602 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 1154 BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 INSPECTION FOUND AFT CARGO PIT FLOOR SUPPORT BROKEN AT STA 1154, RBL 6. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 5 3-05. 2 L 7 2 4F A6WE 1996062000161 19960620 00161 WP 1996 6 20 CALA9600814 1 19960531 A 5320 SILL STOP DOUG DC9 DC982 3022082 WP AFT CARGO DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 INSPECTION FOUND CORROSION AT EDGES OF TWO EACH AFT CARGO COMPARTMENT LOWER DOOR SILL STOPS. THE CORROSION WAS REMOVED AND REPAIR DOUBLERS WERE INSTALLED IAW SRM 53-05. 2 L 7 2 4F A6WE 1996062000162 19960620 00162 WP 1996 6 20 CALA9600815 1 19960531 A 5320 TIE CLIP DOUG DC9 DC982 3022082 WP BS 1060 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 INSPECTION FOUND AFT CARGO COMPARTMENT CIRCUMFERENTIAL TIE CLIP CORRODED AT STA 1060 BETWEEN STRINGER 30L AND 3OR. REPA IR DOUBLERS WERE INSTALLED IAW SRM 53-10, PAGE 9. 2 L 7 2 4F A6WE 1996062000163 19960620 00163 WP 1996 6 20 CALA9600816 1 19960530 A 5730 SKIN DOUG DC9 DC982 3022082 WP RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 INSPECTION FOUND A 9 INCH CRACK IN RT WING UPPER COMPOSITE TRAILING EDGE SKIN FORWARD OF INBOARD SPOILER AT INBOARD END. A LAY-UP REPAIR WAS ACCOMPLISHED IAW SRM 51-70-1. 2 L 7 2 4F A6WE 1996062000164 19960620 00164 WP 1996 6 20 CALA9600817 1 19960530 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 617 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 INSPECTION FOUND CORROSION ON RT FLOOR SUPPORT IN MID CARGO COMPARTMENT AT STA 617, STRINGER 28R. A REPLACEMENT BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-00 AND 51-10-3. 2 L 7 2 4F A6WE 1996062000165 19960620 00165 WP 1996 6 20 CALA9600818 1 19960529 A 5230 SKIN DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 INSPECTION FOUND A 4 INCH CRACK IN MID CARGO DOOR SKIN AT HANDLE CUTOUT. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS I NSTALLED IAW SRM 52-05, FIGURE 30. 2 L 7 2 4F A6WE 1996062000166 19960620 00166 WP 1996 6 20 CALA9600819 1 19960530 A 5753 VANE DOUG DC9 DC982 3022082 WP LT TE FLAP DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 INSPECTION FOUND A DENT IN FORWARD INBOARD AREA OF LEFT OUTBOARD FLAP MID VANE. THE DENTED AREA WAS CUT OUT AND A HOT B OND REPAIR WAS INSTALLED IAW SRM 51-70-2. 2 L 7 2 4F A6WE 1996062000167 19960620 00167 NM 1996 6 20 CALA9600820 1 19960602 A 5330 SKIN BOEING 737 737222 1384473 NM L 2 DOOR CUTOUT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12235 19758 INSPECTION FOUND A .75 INCH CRACK IN EXTERNAL SKIN AT FORWARD LOWER CORNER OF L-2 DOOR CUTOUT. THE CRACKED AREA WAS CUT OUT, REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, 51-30-2 AND 51-10-2. 2 L 7 2 4F A16WE 1996062000168 19960620 00168 NM 1996 6 20 CALA9600821 1 19960529 A 5315 FLOORBEAM BOEING 737 737222 1384473 NM BS 665 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12235 19758 INSPECTION FOUND A .5 INCH CRACK IN FLOORBEAM WEB AT STA 665, BBL 0. THE AREA WAS REPAIRED IAW EA 5710-01322, SRM 51-30 -09 AND SRM 51-30-02. 2 L 7 2 4F A16WE 1996062000169 19960620 00169 NM 1996 6 20 CALA9600822 1 19960531 A 5320 DOUBLER BOEING 737 737222 1384473 NM BS 675 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12235 19758 INSPECTION FOUND THREE EACH CRACKS IN T-CHORD AND WEB DOUBLER AT STA 675, RBL 24.8. THE CRACKS WERE .25 INCH OR SMALLER . THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-2. THE EDGE CRACKS ON T-CHORD WERE TRIMMED OUT AND THE REPAIR WAS DETERMINED GOOD IAW SRM 53-10-2. 2 L 7 2 4F A16WE 1996062000170 19960620 00170 NM 1996 6 20 DL72P961393 1 19960610 A 5754 651622199 RIB BOEING 727 727225 1384077 NM LT LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 FOUND LEFT WING SLAT RIB CRACKED AT RADIUS, O/B OF ACTUATOR. REPAIRED PER M/M 57-54-0, FIG 804. 2 L 7 3 4F A3WE 1996062000171 19960620 00171 NM 1996 6 20 DL72S961396 1 19960603 A 5330 65C139132 SKIN BOEING 727 727232 1384082 NM BS 1142-1166 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 522DA 21582 FOUND CORROSION SLIGHTLY AFT OF C-3 DOOR OPENING BEAR STRAP. REPAIRED PER ER/A 303676-14. 2 L 7 3 4F A3WE 1996062000172 19960620 00172 NM 1996 6 20 DL72S961397 1 19960603 A 5311 FRAME BOEING 727 727232 1384082 NM BS 783.95 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 522DA 21582 FOUND CRACKS AT THE LT AND RT FRAMES AT STA 784. REPAIRED BOTH CRACKS PER BAC S/B 727-53-0197, REV 2. 2 L 7 3 4F A3WE 1996062000173 19960620 00173 NM 1996 6 20 DL72S961408 1 19960611 A 5743 TRUNNION BOEING 727 727232 1384082 NM LT MLG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 523DA 21583 FOUND CORROSION ON LEFT GEAR FWD TRUNNION FACE. REPAIRED PER M/M 57-43-0 PG 803. 2 L 7 3 4F A3WE 1996062000174 19960620 00174 NM 1996 6 20 DL72S961409 1 19960611 A 5753 TRACK BOEING 727 727232 1384082 NM NR 4 TE FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 523DA 21583 FOUND CORROSION ON THE NR 4 FLAP TRACK FWD SUPPORT FITTING INSIDE THE BORES. REPAIRED PER M/M 57-42-0. 2 L 7 3 4F A3WE 1996062000175 19960620 00175 NM 1996 6 20 DL72S961410 1 19960611 A 5753 SUPPORT BOEING 727 727232 1384082 NM FLAP TRACK CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 523DA 21583 FOUND CORROSION ON THE FLAP TRACK SUPPORT IN LARGE BEARING BORE. REPAIRED PER M/M 57-42-0, PG 806. 2 L 7 3 4F A3WE 1996062000176 19960620 00176 NM 1996 6 20 DL72S961414 1 19960521 A 5320 TORQUE BOX BOEING 727 727232 1384082 NM BS 1263 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 406DA 21150 THERE IS A CRACK IN THE ANGLE OF THE FWD TRANSVERSE BEAM AND AFT CHANNEL OF THE RT TORQUE BOX AT FS 1263. THIS AREA OF THE TORQUE BOX IS THE SUBJECT OF THE AD 94-07-08 WHICH REQUIRES INSPECTION PER SB 53-0129. THIS ERA WILL REPLACE THE DA MAGED PART IN ACCORDANCE WITH THE S/B. 2 L 7 3 4F A3WE 1996062000177 19960620 00177 NM 1996 6 20 DL72S961416 1 19960517 A 5330 65545661 SKIN BOEING 727 727232 1384082 NM FS 496 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 477DA 20754 CORROSION WAS FOUND IN THE SKIN AT FS 496 AND S-27R. REPAIRED PER ER/A 303236-14. 2 L 7 3 4F A3WE 1996062000178 19960620 00178 NM 1996 6 20 DL72W961369 1 19960606 A 3350 LIGHT BOEING 727 727247 138408F NM AIRSTAIRS INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 293WA 22111 AIRSTAIRS AREA EMERGENCY LIGHT INOP. REPLACED LIGHT. 2 L 7 3 4F A3WE 1996062000179 19960620 00179 NM 1996 6 20 DL72W961411 1 19960519 A 5330 65184203119 SKIN BOEING 727 727247 138408F NM L-1 DOOR CUTOUT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2807W 20579 DURING INSPECTION, FOUND 1 INCH CRACK IN THE UPPER FWD CORNER OF THE L-1 DOOR CUTOUT. REPAIRED PER ER/A 303614-14AD. 2 L 7 3 4F A3WE 1996062000180 19960620 00180 NE 1996 6 20 DL73S961383 2 19960607 A 7200 ENGINE BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE NR 1 MALFUNCTIONED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 323DL 23095 717144 AFTER T/O AND CLIMB THROUGH 18,000 MSL NOTED OIL ODOR FROM AIRCOND, FWD LAV SMOKE ALARM SOUNDED. TURNED OFF LT PACK, AL ARM STOPPED AND OIL SMOKE CEASED. PERFORMED DUCT BURN-OUT PER MM, PERFORMED BREATHER PRESS CK. BREATHER PRESS CHECK, O K. REPLACED NR 2 ENG. 2 L 7 2 4F 4 F RT A16WE E2EA 1996062000181 19960620 00181 NM 1996 6 20 DL757961376 1 19960606 A 3411 851FJ1 PITOT TUBE BOEING 757 757232 1384965 NM LT FUSELAGE DIRTY A DALA D RETURN TO BLOCK C F.O.D. TX TAXI/GRND HDL 1 SO 27 620DL 22910 DURING TAXI OUT AT APPROX 10 KTS, CA AIRSPD IND AND ADI WIND ARROW READ 133 KTS. CHECKED AND FOUND BOTH UPPER AND LWR P ITOT TUBES ON CA SIDE BLOCKED WITH DIRT. REPLACED BOTH TUBES AND PURGED LINES. PUMPED SYS AND LEAK CKD OPS CK GOOD. 2 L 7 2 4F RT A2NM 1996062000182 19960620 00182 NM 1996 6 20 DL76S961390 1 19960609 A 3397 WIRE BOEING 767 767332 1382001 NM CABIN SHORTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 121DE 23435 AFT SECTION OF THE AFT COACH CABIN EMERGENCY FLOOR TRACK LIGHTING WAS INOP ON T/S CHECK. FOUND WIRE SHORTED TO GROUND A T SIDE WALL FEED. REPAIRED WIRE AND REPLACED THE BATTERY PWR SUPPLY M9010, SYSTEM NOW OPERATES NORMAL. 2 L 7 2 4F RT A1NM 1996062000183 19960620 00183 WP 1996 6 20 DLL10961360 1 19960604 A 3350 LIGHT LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 718DA 193C1097 AFT CABIN EMERGENCY TRACK LIGHTS WILL NOT COME ON DURING TEST. FOUND FUSES BLOWN IN AFT RT CONTROL MODULE. REPLACED FU SES, TRACK LIGHTS CKS GOOD. 2 L 7 3 4F A23WE 1996062000184 19960620 00184 WP 1996 6 20 DLL10961366 1 19960605 A 5620 OUTER WINDOW LKHEED 1011 10113851 5265010 WP CABIN BROKEN A DALA K NONE D INFLIGHT SEPARATION CR CRUISE 1 SO 27 1732D 193C1213 OUTER WINDOW ROWS 44 AND 45 ON CAPT'S SIDE, CRACKED AND DEPARTED AIRCRAFT. 2 L 7 3 4F A23WE 1996062000185 19960620 00185 NE 1996 6 20 DLL10961398 2 19960610 A 7200 ENGINE LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B NE NR 3 FAILED A DALA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DE DESCENT 1 SO 27 714DA 193C1090 10653 AT 0340 NUMBER 3 ENGINE APPEARED TO HAVE THE SOUND OF A COMPRESSOR STALL. VIB WENT TO 3.0 OIL, FUEL, TEMPS AND PRESSURE NORMAL, 12000/280 KNOTS A/C YAWED, ENGINE SHUTDOWN, TGT 770 N-2 NORMAL ENGINE SHUT DOWN IN FLIGHT. REPLACED ENGINE. 2 L 7 3 4F 4 F A23WE E12EU 1996062000186 19960620 00186 WP 1996 6 20 DLL17961374 1 19960606 A 2421 IDG LKHEED 1011 10113853 5265020 WP NR 3 ENGINE FAILED A DALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 27 769DL 193H1218 AFTER TAKEOFF, LOST NR THREE GENERATOR WITH ASSOCIATED FLIGHT STATION BUSS FAIL. REPLACED IDG, OPS CK GOOD. 2 L 7 3 4F A23WE 1996062000187 19960620 00187 NM 1996 6 20 DLM88961399 1 19960611 A 2400 EMER POWER SW DOUG MD88 MD88 3023688 NM COCKPIT INOPERATIVE A DALA O OTHER H ELECT. POWER LOSS-50 PC DE DESCENT 1 SO 27 942DL 49815 DURING IDLE DESCENT THROUGH 8,000, CBS K7 AND L8 POPPED OPEN, RESULTING IN LOSS OF A/C EMERGENCY BUS. EMERGENCY POWER O N, WORKED OK. REPLACED EMERGENCY POWER SWITCH. 2 L 7 2 4F RT A6WE 1996062000188 19960620 00188 NM 1996 6 20 P5CA9600244 1 19960612 A 2750 WIRE BOEING 747 747122 1384872 NM TE FLAPS SHORTED A P5CA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 WP 23 850FT 19755 EXPERIENCED FLAP FAILURE/ASYMMETRY LOCKOUT ON CLIMBOUT. RETRACTED T/E FLAPS USING ALTERNATE SYSTEM, DIVERTED TO BIRMING HAM DUE TO ATLANTA WEATHER. TROUBLESHOT SYSTEM, FOUND LOCKOUT PROBLEMS STOPPED WHEN MODE 'S' RELAY CB PULLED. REPAIRED SHORTED WIRE FOUND NEAR P54 PANEL, RELAY 4R914, OPS CHECK NORMAL PER MM 27-58-00. 2 L 7 4 4F A20WE 1996062000189 19960620 00189 NM 1996 6 20 P5CA9600245 1 19960614 A 3610 69B401186 DUCT BOEING 747 747123 1384873 NM LT WING CRACKED A P5CA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 859FT 20326 ON PUSHBACK, NOTED WING LEADING EDGE OVERHEAT ON LEFT WING. WHEN ADP NR 1 WAS SELECTED, LIGHT WENT OUT. RETURNED TO BL OCKS. FOUND DUCT CRACKED AT BOSS FOR NR 2 PYLON BLEED AIR SENSE LINE, BOSS BLOWN OUT. REMOVED AND REPLACED DUCT ASSY, LEAK CHECK NORMAL PER MM 36-11-01. DUCT VERIFIED BY P/N TO BE IN COMPLIANCE WITH AD 91-06-08. 2 L 7 4 4F A20WE 1996062000190 19960620 00190 EU 1996 6 20 QXEA9600201 1 19960612 A 3350 5515800106 LIGHT FOKKER F28 F28MK1000 4990808 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 464US 11063 FORWARD GALLEY LIGHTED EXIT SIGN IS INOP. LIGHT ASSY WAS REPLACED AND SIGN OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996062000191 19960620 00191 EU 1996 6 20 QXEA9600202 1 19960612 A 3350 1315 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 462AU 11054 MAIN CABIN DOOR EMERGENCY EXIT LIGHT IN FORWARD GALLEY IS INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996062000192 19960620 00192 EU 1996 6 20 QXEA9600203 1 19960613 A 3350 1312 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 454US 11107 EMERGENCY EXIT LIGHT AT GALLEY SERVICE/EMERGENCY DOOR IS INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996062000193 19960620 00193 NM 1996 6 20 SCNA96178 1 19960611 A 3350 S106 BATTERY BOEING 727 7272A1 138407F NM CONTROL CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 287SC 21345 CONTROL CABIN PORTABLE EMERGENCY EXIT LIGHT WAS FOUND INOP. REMOVED AND REPLACED BATTERIES IN CONTROL CABIN LIGHT ASSEM BLY AND OPS CHECKED OK IN ACCORDANCE WITH MM 33-50-101. 2 L 7 3 4F A3WE 1996062000194 19960620 00194 1996 6 20 SCNA96179 4 19960607 A 2564 RO202211 LIFERAFT BOEING 727 727227 1384078 NM CABIN RUPTURED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 275AF 22092 DURING FLIGHT ATTENDANT TRAINING, AIRCRAFT RAFT FAILED TO DEPLOY PROPERLY. 2 L 7 3 4F A3WE 1996062000195 19960620 00195 WP 1996 6 20 9613101146 1 19960615 A 4900 APU DOUG DC10 DC1040 3023508 WP TAIL FIRE A A NWAA F ACTIVATE FIRE EXT. A FLAME/FIRE IN INSP/MAINT 1 GL 01 146US 58178 4157 46755 PRIOR TO PUSHBACK, APU TAILPIPE FIRE DEVELOPED. AIRCRAFT APU FIRE BOTTLES WERE DISCHARGED AND FLAMES EXTINGUISHED. THE PASSENGERS WERE DEPLANED THROUGHT THE JETWAY WITHOUT INCIDENT. NO SMOKE WAS PRESENT IN CABIN. MAINTENANCE INSPECTED A PU AND SURROUNDING STRUCTURE, NO DAMAGE FOUND. FIRE BOTTLES WERE REPLACED AND APU PLACED ON MEL. 2 L 7 3 4F A22WE 1996062000196 19960620 00196 NE 1996 6 20 9613111141 2 19960614 A 7230 COMPRESSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20J 52054 NE NR 2 ENGINE STALLED A NWAA O OTHER R PARTIAL RPM/PWR LOSS DE DESCENT 1 GL 01 141US 46750 86141 AT TOP OF DESCENT, THE NR 2 ENGINE COMPRESSOR STALLED WHEN THROTTLE WAS RETARDED. AT THE TIME OF STALL, TEMPERATURE REA CHED 750 DEGREES CELSIUS. FLIGHT CONTINUED TO LGW WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED INSPECTION PER 71-00 -00 AND NO DAMAGE WAS FOUND. 2 L 7 3 4F 4 F A22WE E20EA 1996062000197 19960620 00197 NM 1996 6 20 9613126613 1 19960614 A 3397 WIRE BOEING 747 747251B 1384892 NM CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 613US 20358 DURING LINE CHECK, FOUND DOOR SLIDE AND OVERHEAD EMERGENCY LIGHTS DEFECTIVE AT DOOR 1R. REPAIRED WIRE, OPERATIONAL CHEC K GOOD. 2 L 7 4 4F A20WE 1996062000198 19960620 00198 NM 1996 6 20 9613136301 1 19960615 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 661US 23719 DURING LINE CHECK, FOUND UPPER DECK OVERHEAD EMERGENCY EXIT SIGNS BETWEEN EXIT DOORS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1996062000199 19960620 00199 NM 1996 6 20 9613146305 1 19960616 A 3350 LIGHT BOEING 747 747451 1384940 NM CABIN INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 665US 23820 DURING LINE CHECK, FOUND EMERGENCY LIGHTS AT DOOR 4R AND 2L INOPERATIVE. REPAIRED PIN AND WIRING, OPERATIONAL CHECK GOO D. 2 L 7 4 4F RT A20WE 1996062000200 19960620 00200 1996 6 20 9613159601 4 19960614 A 3442 20671570153 TRANSCEIVER DOUG DC9 DC932 3022066 WP FWD ACCESS COMPT FAILED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 601NW 47038 WEATHER RADAR SYSTEM FAILED AFTER TAKEOFF. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RA DAR TRANSCEIVER, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996062000201 19960620 00201 WP 1996 6 20 9613169604 1 19960613 A 3350 FUSE DOUG DC9 DC932 3022066 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 604NW 47222 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY FUSE, OPERA TIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996062000202 19960620 00202 1996 6 20 9613179965 4 19960616 A 2210 CONNECTOR DOUG DC9 DC931 3022065 WP YAW DAMP ACT LOOSE A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 911RW 47149 AIRCRAFT EXPERIENCED EXCESSIVE YAW AFTER TAKEOFF. YAW DAMPER WAS CYCLED WITH NO HELP. FLIGHT RETURNED TO ATL AND LANDE D WITHOUT INCIDENT. MAINTENANCE RESEATED CANNON PLUG ON YAW DAMPER ACTUATOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996062000203 19960620 00203 1996 6 20 9613189965 4 19960616 A 2211 25878263 AP COMPUTER DOUG DC9 DC931 3022065 WP E/E COMPARTMENT MALFUNCTIONED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 911RW 47149 AIRCRAFT EXPERIENCED EXCESSIVE YAW AFTER TAKEOFF. FLIGHT RETURNED TO ATL AND LANDED WITHOUT INCIDENT. MAINTENANCE REPL ACED STABILIZATION AUGMENTATION COMPUTER, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996062000204 19960620 00204 EU 1996 6 20 9613193247 1 19960614 A 2742 47145121 ACTUATOR AIRBUS 320 A320211 3930320 EU HORIZONTAL STAB MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 347NW 408 DURING CLIMBOUT AT APPROXIMATELY 600 FEET AGL, RECEIVED 'F/CTL ELAC 2 PITCH FAULT' ACCOMPANIED BY UNCOMMANDED 2 TO 3 DEG REE PITCH DOWN INPUTS AND SLUGGISH PITCH RESPONSE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO BOS AND LANDE D WITHOUT INCIDENT. MAINTENANCE REPLACED THE TRIMMABLE HORIZONTAL STABILIZER ACTUATOR, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996062000205 19960620 00205 EU 1996 6 20 9613203249 1 19960615 A 3350 321430 BATTERY AIRBUS 320 A320211 3930320 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 349NW 417 DURING LINE MAINTENANCE, THE FORWARD LEFT EMERGENCY LIGHTS BATTERY PACK FAILED CABIN INTERCOMMUNICATION DATA SYSTEM TEST . REPLACED BATTERY PACK, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996062000206 19960620 00206 NM 1996 6 20 9613212275 1 19960614 A 3244 657276187 TIRE BOEING 727 727251 138408H NM RT MLG FAILED A NWAA K NONE O OTHER LD LANDING 1 GL 01 275US 21154 DURING LANDING, THE NR 4 TIRE HAD A TREAD SEPARATION. MSP MAINTENANCE CHANGED THE NR 4 TIRE AND WHEEL ASSEMBLY PER MAIN TENANCE MANUAL. 2 L 7 3 4F A3WE 1996062000207 19960620 00207 WP 1996 6 20 9613229918 1 19960614 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 940N 47572 DURING LINE MAINTENANCE INSPECTION, FOUND THE RIGHT OVERWING EMERGENCY EXIT LIGHTS WEAK. REPLACED BATTERIES AND REPAIRE D LOOSE LIGHT SOCKET ON FORWARD RIGHT OVERWING LIGHT, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996062000208 19960620 00208 WP 1996 6 20 9613239979 1 19960615 A 3350 FUSE DOUG DC9 DC931 3022065 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9343 47439 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD SERVICE DOOR AND CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE IN POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996062000209 19960620 00209 WP 1996 6 20 9613249907 1 19960612 A 3350 6011779 POWER SUPPLY DOUG DC9 DC931 3022065 WP LT NACELLE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 957N 47253 DURING PERIODIC CHECK, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996062000210 19960620 00210 WP 1996 6 20 9613259925 1 19960611 A 3350 FUSE DOUG DC9 DC932 3022066 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 925US 47472 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE IN RIGHT FORWARD EMERGENCY EXIT DOOR BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996062000211 19960620 00211 WP 1996 6 20 9613269951 1 19960612 A 3350 60030451 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 916RW 47144 DURING PREFLIGHT CHECK, FOUND COCKPIT AND ENTRY DOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL C HECK NORMAL. 2 L 7 2 4F A6WE 1996062000212 19960620 00212 1996 6 20 96UAL900450 4 19960614 A 2565 SLIDE AIRCRUISERS 24D30051103 DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL R3 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 1844U 1526 48260 DURING SHOP OVERHAUL OF SLIDE/RAFT FROM DOOR 3R, REMOVED FOR OVERHAUL TIME EXPIRATION, RAMP PORTION OF SLIDE EXPERIENCED INTERNAL BULKHEAD SEPARATION DURING INFLATION. SUBMITTER STATED CAUSE UNDETERMINED. SCRAPPED RAMP. 2 L 7 3 4F 4 F A22WE E23EA 1996062000213 19960620 00213 NM 1996 6 20 96UAL900451 1 19960614 A 3350 LIGHTS BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 609UA 21870 RIGHT SIDE EXTERIOR EMERGENCY LIGHTS ARE INOPERABLE. 2 L 7 2 4F 4 F RT A1NM E3NE 1996062000214 19960620 00214 1996 6 20 96UAL900452 4 19960614 A 2330 DISCONNECT BOX AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN MIS INSTALLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 405UA 452 FOUND LOCALIZED HEAT DAMAGE AT THE WALL DISCONNECT BOX OF THE PASSENGER ENTERTAINMENT SYSTEM. *S/D* THE DAMAGE WAS CAU SED BY IMPROPER INSTALLATION OF ONE CONNECTOR AND MOISTURE FROM CONDENSATION. THE WALL DISCONNECT BOX WAS REPLACED AND OPERATED NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 1996062000215 19960620 00215 NE 1996 6 20 96UAL900453 2 19960615 A 7321 7202811 BEARING HAMILTON STA 7590002 BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE FUEL CONTROL FLAT SPOT A UALA E A ENGINE SHUTDOWN UNSCHED LANDING M OVER TEMP CR CRUISE 1 WP 29 164UA 76434 21657 685788 NR 4 ENGINE SHUT DOWN DUE TO HIGH EGT. *S/D* REPLACED ENGINE. FOUND FUEL CONTROL UNIT HAD EXCESSIVE WEAR ON ONE SIDE OF THE TT2 PILOT VALVE BEARING. FUEL CONTROL UNIT WAS OVERHAULED. 2 L 7 4 4F 4 F A20WE E20EA 1996062000216 19960620 00216 NM 1996 6 20 96UAL900454 1 19960615 A 5730 65B0808175 SKIN BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE LE WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 4724U 82264 19875 LEFT UPPER SKIN PANEL WAS OBSERVED CRACKED IN-FLIGHT. FOUND PANEL CRACKED AND DELAMINATED ALL THE WAY ACROSS THE INBOAR D-OUTBOARD DIRECTION. REMOVED SKIN PANEL, REPAIRED AND REINSTALLED. 2 L 7 4 4F 4 F A20WE E20EA 1996062000217 19960620 00217 NM 1996 6 20 96UAL900455 1 19960615 A 3350 LAMP BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 4727U 19883 NR 1 RIGHT OVERWING FORWARD EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP ASSY AND REPAIRED BROKEN GROUND WIRE. 2 L 7 4 4F 4 F A20WE E20EA 1996062000218 19960620 00218 WP 1996 6 20 ARWA9606005 1 19960614 A 5313 57501982 LONGERON DOUG DC8 DC863F 302198F WP RT FUSELAGE CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 A 9.5 CRACK STOP HOLE, OLD REPAIR HAS EXTENDED 3 FORWARD ON LONGERON 24R. REMOVED AND REPLACED LONGERON 24R PER DOUGLAS DRAWING 5750198 AND 5615475. 2 L 7 4 4F 4A25 1996062000219 19960620 00219 WP 1996 6 20 ARWA9606006 1 19960614 A 5248 DOOR DOUG DC8 DC863F 302198F WP TAIL CONE CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 TAIL CONE ACCESS DOOR NR 62 FS 19010 CRACKED .5 INCH AT LOWER PART. REPAIRED AREA PER DRAWING OF N441J-15/96, DER APPRO VED. 2 L 7 4 4F 4A25 1996062000220 19960620 00220 WP 1996 6 20 ARWA9606007 1 19960614 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 1540-1723 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 LEVEL 1 CORROSION, SEVERAL SPOTS AT FUSELAGE AFT SECTION, FS 1540 TO FS 1723. 2 L 7 4 4F 4A25 1996062000221 19960620 00221 WP 1996 6 20 ARWA9606008 1 19960614 A 5280 HINGE DOUG DC8 DC863F 302198F WP NLG DOOR CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 NLG LEFT FORWARD DOOR HINGE AFTER WEB CRACKED. REPAIRED IN ACCORDANCE WITH FAUCETT DRAWING, FAA 8110-APPROVED. 2 L 7 4 4F 4A25 1996062000222 19960620 00222 WP 1996 6 20 ARWA9606009 1 19960614 A 5280 HINGE DOUG DC8 DC863F 302198F WP NLG DOOR CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 NLG RIGHT FORWARD DOOR HINGE AFTER WEB CRACKED. REPAIRED IN ACCORDANCE WITH FAUCETT DRAWING, FAA 8110-APPROVED. 2 L 7 4 4F 4A25 1996062000223 19960620 00223 WP 1996 6 20 ARWA9606010 1 19960614 A 5753 FILLET DOUG DC8 DC863F 302198F WP LT TE SLOT BROKEN A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 LEFT WING OUTBOARD SLOT UPPER PART WITH BROKEN FILLET. REMOVED AND REPLACED SEAL AND SPRING IN ACCORDANCE WITH DC-8 MM 27-80-1. 2 L 7 4 4F 4A25 1996062000224 19960620 00224 WP 1996 6 20 ARWA9606011 1 19960614 A 5720 FORMER DOUG DC8 DC863F 302198F WP WS 766.25 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 A 2 INCH CRACK AT LT WING LEADING EDGE FORMER AT XFS 766.250. REPAIRED AREA IN ACCORDANCE WITH CF DRAWING CF-N441J-16/9 6, FAA 8110-APPROVED. 2 L 7 4 4F 4A25 1996062000225 19960620 00225 WP 1996 6 20 ARWA9606012 1 19960614 A 5720 FORMER DOUG DC8 DC863F 302198F WP WS 728.75 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 CRACK AT LT WING LEADING EDGE FORMER AT XFS 728.750 THROUGH 747.500. REPAIRED AREA IN ACCORDANCE WITH CF DRAWING CFN441 J-16/96, FAA 8110-APPROVED. 2 L 7 4 4F 4A25 1996062000226 19960620 00226 WP 1996 6 20 ARWA9606013 1 19960614 A 5720 FORMER DOUG DC8 DC863F 302198F WP WS 766.25 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 CRACK AT LT WING LEADING EDGE FORMER AT XFS 766.250. REPAIRED AREA IN ACCORDANCE WITH CF DRAWING CF-N441J-16/96, FAA 81 10-APPROVED. 2 L 7 4 4F 4A25 1996062000227 19960620 00227 WP 1996 6 20 ARWA9606014 1 19960614 A 5320 FITTING DOUG DC8 DC863F 302198F WP BS 1240-1260 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 AFT LOWER CARGO COMPARTMENT HAS LEVEL 2 CORROSION AT FITTING, FS 1240 THROUGH 1260, LONGERONS 33R AND 34R. FITTING WAS REMOVED AND REPLACED PER DC-8 SRM 51-30. 2 L 7 4 4F 4A25 1996062000228 19960620 00228 WP 1996 6 20 ARWA9606015 1 19960614 A 5320 FITTING DOUG DC8 DC863F 302198F WP BS 160 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 FORWARD CARGO COMPARTMENT AT LONGERON 30R, FS 160, IS CRACKED 1 INCH. REPAIRED LONGERON 30R IN ACCORDANCE WITH DC-8 SRM 53-2-2, FIG 4A; 10. TREATED AND INSTALLED IAW DC-8 SRM 51-1-8 AND 51-1-20D. 2 L 7 4 4F 4A25 1996062000229 19960620 00229 WP 1996 6 20 ARWA9606016 1 19960614 A 5313 5264571612000 LONGERON DOUG DC8 DC863F 302198F WP BS 180 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 FORWARD CARGO COMPARTMENT AT LONGERON 30R, FS 180, CRACKED 2 INCHES. CRACKED SECTION REMOVED AND REPLACED WITH EXTRUSIO N PER DC-8 SRM 51-1-8 AND 51-1-20D. 2 L 7 4 4F 4A25 1996062000230 19960620 00230 WP 1996 6 20 ARWA9606017 1 19960614 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1560 BROKEN A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 LT UPPER SURFACE CUSP EXTRUSION HAS BROKEN FRAME AT LONGERON 21L, FS 1560. REPAIRED FRAME IN ACCORDANCE WITH DC-8 SRM 5 7-2-0. 2 L 7 4 4F 4A25 1996062000231 19960620 00231 WP 1996 6 20 ARWA9606018 1 19960614 A 5311 FRAME DOUG DC8 DC863F 302198F WP FUSELAGE BENT A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 LT UPPER SURFACE CUSP EXTRUSION, FRAME AT LONGERON 21L, IS BENT. REPAIRED FRAME IAW DC-8 SRM 53-2-0, FIG 2. FORMED REP AIR PARTS IAW DC-8 SRM 53-4-1, 51-1-4 AND CLEANED AND TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1996062000232 19960620 00232 WP 1996 6 20 ARWA9606020 1 19960614 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 150-190 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 FORWARD CARGO COMPARTMENT HAS LEVEL 2 CORROSION FROM FS 150 TO 190 AT LONGERON 31R. FORMED STRAP AND TREATED AND INSTAL LED PER DC-8 SRM 53-4-1, 51-1-4, 51-1-8 AND 51-1-21. 2 L 7 4 4F 4A25 1996062000233 19960620 00233 WP 1996 6 20 ARWA9606021 1 19960614 A 5320 DOUBLER DOUG DC8 DC863F 302198F WP BS 215 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 FORWARD CARGO COMPARTMENT HAS LEVEL 2 CORROSION AT FS 215, LONGERON 31R DOUBLER. REMOVED AND REPLACED DOUBLER IAW DC-8 SRM 51-1-8 AND 53-2-0. 2 L 7 4 4F 4A25 1996062000234 19960620 00234 WP 1996 6 20 ARWA9606022 1 19960614 A 5320 DOUBLER DOUG DC8 DC863F 302198F WP BS 400-450 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 FORWARD CARGO COMPARTMENT HAS LEVEL 2 CORROSION AT LONGERON 31R, FS 400 THROUGH 450. REPLACED EXTRUSION AND DOUBLER PER DC-8 SRM 53-2-1, FIG 7, SHEET 1 AND 53-4-1. CLEANED AND TREATED AREA PER DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1996062000235 19960620 00235 WP 1996 6 20 ARWA9606023 1 19960614 A 5320 DOOR FRAME DOUG DC8 DC863F 302198F WP CARGO COMPT CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 FORWARD CARGO COMPARTMENT NR 2 DOOR FRAME AT STA 560 HAS LEVEL 2 CORROSION. FRAME WAS REMOVED AND NEW FRAME FABRICATED IAW DC-8 SRM 52-4-1 AND 51-1-4. TREATED AND INSTALLED PER DC-8 SRM 51-1-8, 51-1-17 AND 51-1-21. 2 L 7 4 4F 4A25 1996062000236 19960620 00236 WP 1996 6 20 ARWA9606024 1 19960614 A 5320 47799401 FITTING DOUG DC8 DC863F 302198F WP BS 440-460 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 FORWARD CARGO COMPARTMENT HAS LEVEL 2 CORROSION BETWEEN FS 440 TO 460 AT LONGERON 31L. REMOVED AND REPLACED FITTING PER DC-8 SRM 51-1-20D AND 51-1-17. 2 L 7 4 4F 4A25 1996062000237 19960620 00237 WP 1996 6 20 ARWA9606025 1 19960614 A 5320 DOUBLER DOUG DC8 DC863F 302198F WP BS 180 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 FORWARD CARGO COMPARTMENT HAS LEVEL 2 CORROSION AT FS 180, LONGERON 31R. REPLACED DOUBLER PER DC-8 SRM 51-1-21 AND 51-1 -20D. CLEANED AND TREATED AREA PER DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1996062000238 19960620 00238 WP 1996 6 20 ARWA9606026 1 19960614 A 5313 LONGERON DOUG DC8 DC863F 302198F WP BS 500 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 FORWARD DECK, LONGERONS 35R AND 36 AT FS 500 HAVE LEVEL 2 CORROSION UNDER FRAME. REPAIRED AREA PER DC-8 SRM 51-1-21, 53 -2-0, 51-1-8 AND 51-1-20D. 2 L 7 4 4F 4A25 1996062000239 19960620 00239 WP 1996 6 20 ARWA9606027 1 19960614 A 5320 ANGLE DOUG DC8 DC863F 302198F WP BS 280/340 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 LEVELS 1 AND 2 CORROSION AT INNER SURFACE STA 340 AND 280, LONGERONS 31L AND 26L. ATTACHMENT ANGLE WAS REMOVED AND REPL ACED. FABRICATED ANGLE IAW DC-8 SRM 53-4-1 AND 51-1-4. TREATED AND INSTALLED IAW DC-8 SRM 51-1-8 AND 51-1-20D. 2 L 7 4 4F 4A25 1996062000240 19960620 00240 WP 1996 6 20 ARWA9606030 1 19960614 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1000 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 AFT CARGO COMPARTMENT HAS LEVEL 2 CORROSION AT FRAME UPPER CAP, FS 1000, LONGERONS 33R AND 34R. CORRODED CAP WAS REMOVE D, FABRICATED, TREATED AND INSTALLED PER DC-8 SRM 53-4-1, 51-1-4, 51-1-8 AND 51-1-21. 2 L 7 4 4F 4A25 1996062000241 19960620 00241 WP 1996 6 20 ARWA9606031 1 19960614 A 5320 3754914501 FITTING DOUG DC8 DC863F 302198F WP BS 1160 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 AFT CARGO COMPARTMENT HAS CORRODED AND BROKEN FITTING AT FS 1160, LONGERON 31R. REMOVED AND REPLACED FITTING PER DC-8 S RM 51-3-0. 2 L 7 4 4F 4A25 1996062000242 19960620 00242 WP 1996 6 20 ARWA9606032 1 19960614 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1324 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 AFT CARGO COMPARTMENT HAS LEVEL 2 CORROSION ON SIDEWALL UPPER AND LOWER FRAMES AT STA 1324. FRAMES WERE REPAIRED, TREAT ED AND INSTALLED PER DC-8 SRM 53-4-1, 51-1-4 , 51-1-8 AND 51-1-20D. 2 L 7 4 4F 4A25 1996062000243 19960620 00243 WP 1996 6 20 ARWA9606033 1 19960614 A 5350 TAIL CONE DOUG DC8 DC863F 302198F WP AFT FUSELAGE CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 TAIL CONE HAS CRACKS OF .5 AND 1.5 AT LONGERONS 7L AND 11L. REPAIRED CRACKS PER DC-8 SRM 53-2-0, FIG 1B, SHEET 3 AND 53 -5-3, FIG 4, SHEETS 1 AND 2. CLEANED AND TREATED AREA PER DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1996062000244 19960620 00244 WP 1996 6 20 ARWA9606034 1 19960614 A 5320 FITTING DOUG DC8 DC863F 302198F WP BS 1220 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 CRACKED FITTING AT FS 1220 BETWEEN CEILING AND FLOOR BEAM. CRACKED FITTING REMOVED AND REPLACED IAW DC-8 SRM 51-1-20D A ND 51-1-21. 2 L 7 4 4F 4A25 1996062000245 19960620 00245 WP 1996 6 20 CALA9600823 1 19960614 A 3350 EA1CS2522D2 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 10801 49127 INSPECTION FOUND EXTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE. THE BATTERY PACK AND LIGHT SOCKET WERE REMOVED AND REPLACE D. 2 L 7 2 4F A6WE 1996062000246 19960620 00246 WP 1996 6 20 CALA9600824 1 19960615 A 7830 7936907608 PRESS LINE DOUG DC9 DC982 3022082 WP RT TR UNIT CRACKED A CALA O OTHER J K WARNING INDICATION FLUID LOSS AP APPROACH 1 SW 09 69803 49229 THE RT HYDRAULIC SYSTEM PRESSURE TEMPORARILY WENT TO ZERO UPON GEAR EXTENSION FOR LANDING AT IAH. THE AIRCRAFT LANDED W ITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC QUANTITY AT ZERO. THE RT THRUST REVERSER CONTROL VALVE HYDRAULIC PRES SURE LINE WAS FOUND CRACKED. AN INTERIM FLEX LINE WAS INSTALLED AND A DIP WAS ISSUED TO REPLACE THE FLEX LINE WITH A PE RMANENT LINE WITHIN 1200 HOURS OR 500 FLIGHTS, WHICHEVER OCCURS FIRST. LEAK CHECKS WERE GOOD. 2 L 7 2 4F A6WE 1996062000247 19960620 00247 WP 1996 6 20 CALA9600825 1 19960615 A 3230 PITCH DAMPER DOUG DC10 DC1010 3022110 WP RT MLG LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 09 68047 47801 THE NR 3 HYDRAULIC SYSTEM QUANTITY DROPPED UPON GEAR EXTENSION FOR LANDING AT HKG. THE AIRCRAFT LANDED WITHOUT INCIDENT . MAINTENANCE FOUND THE NR 3 HYDRAULIC SYSTEM FOUR GALLONS LOW. THE RT MLG PITCH DAMPER WAS FOUND LEAKING. THE RT MLG PITCH DAMPER WAS REPLACED. THE NR 3 HYDRAULIC SYSTEM WAS SERVICED AND LEAK CHECK WAS GOOD. 2 L 7 3 4F A22WE 1996062000248 19960620 00248 NM 1996 6 20 CALA9600826 1 19960616 A 7312 DUCT BOEING 727 727227 1384078 NM PWA JT8 JT8D9 52048 NE FUEL HT VLV BLOWN A CALA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 SW 09 17773 21045 666882 THE NR 3 ENGINE FIRE WARNING BELL AND LIGHT ACTIVATED SHORTLY AFTER TAKEOFF FROM IAH WITH ENGINE AT CLIMB POWER. THE TH ROTTLE WAS RETARDED AND THE FIRE WARNING CEASED. WHEN THE NR 3 THROTTLE WAS ADVANCED TO CLIMB POWER THE FIRE WARNING BE LL AND LIGHT ACTIVATED AGAIN. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO IAH WHERE THE AIRCRAFT LANDED WITHOUT IN CIDENT. MAINTENANCE FOUND THE NR 3 ENGINE FUEL HEAT VALVE DUCT FLANGE BLOWN. THE DUCT WAS REMOVED AND REPLACED. THE N R 3 ENGINE WAS RUN AND NO LEAKS WERE OBSERVED. 2 L 7 3 4F 4 F A3WE E2EA 1996062000249 19960620 00249 NM 1996 6 20 CALA9600827 1 19960616 A 2910 65445101562 HYD LINE BOEING 737 737130 1384435 NM RT REAR SPAR CHAFED A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 77204 19021 THE A-SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO WHILE EN ROUTE. THE HYDRAULIC LOSS CHECKLIST WAS COMPLIED WITH AND THE AIRCRAFT WAS DIVERTED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE A-SYSTEM HYDRAULIC SUPPLY LINE IN THE RT REAR SPAR AREA WITH A HOLE CHAFED THROUGH IT. THE SUPPLY LINE WAS REMOVED AND REPLACED. IN ADDITION, THE HYDRAU LIC LINE IT RUBBED AGAINST WAS REPLACED AS A PRECAUTIONARY MEASURE. LEAK CHECKS WERE GOOD. 2 L 7 2 4F A16WE 1996062000250 19960620 00250 SO 1996 6 20 COMA9610177 1 19960611 A 3246 MS2125005016 BOLT EMB 120 EMB120RT SO RT INBD WHEEL BROKEN A a COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 130G 120130 ON PREFLIGHT INSPECTION, MECHANIC NOTICED TWO BOLTS MISSING FROM THE RIGHT MAIN INBOARD WHEEL ASSEMBLY. BOLTS ARE PRESU MED TO HAVE BROKEN AND FALLEN OUT. WHEEL/TIRE ASSEMBLY WAS REMOVED AND REPLACED. 2 L 7 2 4T RT A31SO 1996062000251 19960620 00251 SO 1996 6 20 COMA9610178 1 19960612 A 6120 7757151 SPLINE EMB 120 EMB120RT SO PWA 118 PW118A NE HAMSTD 14RF 14RF9 NE BALLSCREW SERVO DEFECTIVE A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 164D 1164 115340 910348 WHILE PERFORMING AD-94-22-12 HAMILTON STANDARD S/B 14RF9-61-A53 REV S. FOUND THE SPLINES OF THE BALLSCREW SERVO WORN BE YOND LIMITS PRIMARILY ON THE RIGHT SIDE OF THE SPLINES. SENT PCU OUT TO HAMILTON STANDARD FOR FURTHER EVALUATION. 2 L 7 2 4T 4 T RT A31SO E20NE 6 C P11NE 1996062000252 19960620 00252 SO 1996 6 20 COMA9610179 1 19960614 A 2720 6225734002 SERVO EMB 120 EMB120RT SO RUDDER CONTROLS DEFECTIVE A COMA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 01 179CA 120179 WHEN AUTOPILOT DISENGAGED DURING APPROACH PHASE OF FLIGHT, THE RUDDER CONTROLS JAMMED AND EXCESSIVE FORCE WAS REQUIRED T O MOVE RUDDER CONTROLS. REPLACED DEFECTIVE RUDDER SERVO. 2 L 7 2 4T RT A31SO 1996062000253 19960620 00253 1996 6 20 COMA9610180 4 19960614 A 3418 C818061 COMPUTER EMB 120 EMB120RT SO STALL WARNING DEFECTIVE A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 1110J 120110 COPILOTS STICK SHAKER ACTIVATED DURING TAKEOFF ROLL. REPLACED THE STALL WARNING COMPUTER. 2 L 7 2 4T RT A31SO 1996062000254 19960620 00254 1996 6 20 COMA9610181 4 19960613 A 3418 C818022 SERVO EMB 120 EMB120RT SO CONTROL COLUMN MALFUNCTION A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 164D 120164 PILOTS STICK SHAKER IS ON CONTINUOUSLY. REPLACED THE PILOTS STICK SHAKER. 2 L 7 2 4T RT A31SO 1996062000255 19960620 00255 SO 1996 6 20 COMA9610182 1 19960613 A 5753 KRP138112VT ROLLER EMB 120 EMB120RT SO RT TE FLAP WORN A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 189CA 120189 FLAP DISAGREEMENT WARNING CAME ON DURING LANDING APPROACH. REPLACED THE RT INBD FLAP ROLLERS. 2 L 7 2 4T RT A31SO 1996062000256 19960620 00256 SW 1996 6 20 COMA9620008 1 19960616 A 5320 273000345 ATTACH ANGLE SWRNGN SA227 SA227AC 8780603 SW WS 27.103 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 704CA AC704 WHILE TROUBLESHOOTING OTHER MAINTENANCE PROBLEM, FOUND ATTACH ANGLE THAT ATTACHES THE LEFT AFT WING TO FUSELAGE FAIRING TO THE INBOARD WING RIB AT WS 27.103 TO BE CRACKED. CRACKED ATTACH ANGLE WAS REMOVED AND SERVICABLE ANGLE WAS FABRICATE D AND INSTALLED AS PER AERODESIGN REPORT NR 1930-1 REV IR, 6/16/96. 2 L 7 2 4T RT A8SW 1996062000257 19960620 00257 EU 1996 6 20 COMA9630126 1 19960617 A 7931 TRANSDUCER SAAB SF340 SF340A 7850100 EU LT ENGINE MALFUNCTION A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 320CA 340A064 LEFT ENGINE LOW OIL PRESSURE WARNING SOUNDED DURING CLIMB. REPLACED THE LT ENGINE OIL PRESSURE TRANSDUCER. 2 L 7 2 4T RT A52EU 1996062000258 19960620 00258 WP 1996 6 20 MWEA96158 1 19960615 A 3350 60030431 BATTERY PACK DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 80ME 45795 DURING SERVICE CHECK, FOUND OVERHEAD EMER LIGHTS AT EMER EXIT ROW WOULD NOT EXTINGUISH WHEN POWER REMOVED. REPLACED BAT TERY POWER SUPPLY FOR LIGHTS AFFECTED, OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996062000259 19960620 00259 WP 1996 6 20 MWEA96159 1 19960615 A 5320 DOUBLER DOUG DC9 DC914 3022034 WP ACCESSORY COMPT CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 DURING C-CHECK, FOUND CRACK 1 INCH LONG ON EXISTING REPAIR DOUBLER AT THE VERTICAL STAB RT ATTACH ANGLE IN AFT ACCESSORY COMPT. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 51-30. 2 L 7 2 4F A6WE 1996062000260 19960620 00260 WP 1996 6 20 MWEA96160 1 19960616 A 5311 FRAME DOUG DC9 DC914 3022034 WP BS 880 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 DURING C-CHECK, FOUND FRAME CRACKED AT STA 880 L19R. INSTALLED REPAIR IAW SRM 53-01, FIG 2, SHEET 4. 2 L 7 2 4F A6WE 1996062000261 19960620 00261 WP 1996 6 20 MWEA96161 1 19960616 A 3350 BATTERY DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 800ME 45842 DURING C-CHECK, THE EMERGENCY LIGHTS IN CEILING FROM FWD TO ROW 9 AND OVERHEAD LIGHT IN AFT ACCESSORY COMPT WOULD NOT IL LUMINATE. REPLACED BATTERIES, OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996062000262 19960620 00262 WP 1996 6 20 MWEA96162 1 19960616 A 5210 3917853503 BEAM DOUG DC9 DC932 3022066 WP VENTRAL DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 DURING INSP, FOUND AFT VENTRAL DOOR HAS CRACK IN LT LOWER BEAM. REPLACED BEAM IAW SRM 51-30. 2 L 7 2 4F A6WE 1996062000263 19960620 00263 NM 1996 6 20 P5CA9600246 1 19960617 A 2612 FIRE WARNING BOEING 747 747123 1384873 NM APU ACTIVATED A P5CA F ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 WP 23 858FT 20109 ON CLIMBOUT, FL 28.0 IAS 320 KTS, APU FIRE WARNING LIGHT AND BELL CAME ON. ALSO, ON PILOT'S OVERHEAD PANEL. DISCHARGED APU FIRE BOTTLE, LIGHT WENT OUT IN APPROX 8 SECONDS. ON LANDING, NO EVIDENCE OF FIRE IN APU AREA. WIRES INSPECTED AND FIRE TEST NORMAL PER MM 26-15-00. PLACARDED APU FIRE BOTTLE AND DEFERRED PER MEL 26-8, DUE BOTTLE FIRED. 2 L 7 4 4F A20WE 1996062000264 19960620 00264 EU 1996 6 20 QXEA9600204 1 19960616 A 3350 1315 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 464US 11063 EMERGENCY LIGHTS AT AND ABOVE THE MAIN CABIN DOOR ARE INOP. BULBS WERE REPLACED AND LIGHTS OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996062000265 19960620 00265 EU 1996 6 20 QXEA9600205 1 19960616 A 3350 SPLICE FOKKER F28 F28MK1000 4990808 EU CABIN LOOSE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 457US 11036 FLOOR PROXIMITY LIGHTS ON AISLE SEATS 4, 5 AND 6 ARE INOP. SPLICE REPAIRED AT SEAT 5AB, LIGHTS OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996062000266 19960620 00266 EU 1996 6 20 QXEA9600206 1 19960616 A 3350 5515800104 BULBS FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 457US 11036 EXIT LIGHT AT ROW 8 IS OUT. LIGHT PANEL REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996062000267 19960620 00267 WP 1996 6 20 96ZZZX3023 1 19960515 A 3350 58222 BATTERY PACK DOUG DC9 DC915 3022036 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 491SA 45799 STL - FLT 619 - DURING PRE-FLIGHT, EMERGENCY LIGHTS AND EGRESS LIGHTS WOULD NOT ILLUMINATE. FOUND SWITCH HAD BEEN LEFT IN THE ON POSITION. REPLACED BATTERY POWER PACKS, MFG PN 5822-2 AND VR4D. EMERGENCY LIGHTS AND EGRESS LIGHT SYSTEM OPE RATION CHECKED NORMAL. CHECK C - 5-22-95 - STL. (X) 2 L 7 2 4F A6WE 1996062000268 19960620 00268 WP 1996 6 20 96ZZZX3024 1 19960510 A 5320 FORMER FOOT DOUG DC9 DC982 3022082 WP BS 1452 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 915TW 49186 DURING OP-15, FOUND FORMER FOOT CRACKED AT AFT SIDE OF FORMER, BS 1452, STR 3R AND STR 3L. REPAIRED PER SRM 51-11 AND T WO STANDARD PRACTICES. AIRCRAFT TT: 37,726 HOURS; 19,564 CYCLES. (X) 2 L 7 2 4F A6WE 1996062000269 19960620 00269 WP 1996 6 20 96ZZZX3025 1 19960510 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP BS 1416 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 915TW 49186 DURING OP-15, FOUND CRACK IN AFTERBODY INTERCOSTAL, FS 1416, STR 10L. REPAIRED BY STOP DRILLING AND INSTALLING DOUBLER PER SRM 53-01. AIRCRAFT TT: 37,726 HOURS; 19,564 CYCLES. 2 L 7 2 4F A6WE 1996062000270 19960620 00270 NE 1996 6 20 96ZZZX3026 2 19960519 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE NR 1 FAILED A TWAA E C D ENGINE SHUTDOWN ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 05 956U 49701 SAN - FLT 308 - ON TAKEOFF, SHUT DOWN NR 1 ENGINE, SN 1217, DUE TO LOSS OF EPR AND INCREASE IN EGT. FOUND METAL PARTICL ES IN TAILPIPE. REPLACED ENGINE, ENGINE OPERATION THEN CHECKED NORMAL. ENGINE TOTAL TIME: 22,736 HOURS; 11,408 CYCLES . CHECK C-1D - 3-4-95 - MCI. 2 L 7 2 4F 4 F A6WE E9NE 1996062000271 19960620 00271 WP 1996 6 20 96ZZZX3027 1 19960510 A 5720 ANGLE LKHEED 1011 10113851 5265010 WP WS 503 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 15017 193B1063 MCI - DURING SPECIAL CHECK, FOUND A 2 INCH CRACK AT TOP OF CLOSURE RIB ATTACH ANGLE IN RIGHT WING, IWS 503. REPAIRED BY INSTALLING NEW ATTACHED ANGLE PER SB 093-57-207 AND LOCKHEED DWG NR 1647070, SHEET 2. AIRCRAFT TT: 60,229 HOURS; 22,9 08 CYCLES. 2 L 7 3 4F A23WE 1996062000272 19960620 00272 WP 1996 6 20 96ZZZX3028 1 19960517 A 3230 39140165503 ROD END DOUG DC9 DC931 3022065 WP RT MLG BROKEN A TWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 05 987Z 47137 STL - FLT 609 - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, RT MLG DID NOT RETRACT. EXTENDED ALL LANDING GEARS. FOU ND RT MLG BUNGEE CYLINDER ROD END, MFG PN 3914016-5503, FRACTURED. REPLACED BUNGEE CYLINDER AND RT MLG OPERATION CHECKE D NORMAL. CHECK C - 1-12-96 - STL. 2 L 7 2 4F A6WE 1996062000273 19960620 00273 WP 1996 6 20 96ZZZX3029 1 19960510 A 5712 RIB LKHEED 1011 10113851 5265010 WP WS 555 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 15017 193B1063 MCI - DURING SPECIAL CHECK, FOUND CRACK IN RIB CASTELLATION AT FORWARD SIDE OF STR 13 AND STR 19, TOP IWS 555. REPAIRED PER SB 093-57-207 AND SRM 51-10-01. AIRCRAFT TOTAL TIME: 60,229 HOURS; 22,908 CYCLES. 2 L 7 3 4F A23WE 1996062000274 19960620 00274 WP 1996 6 20 96ZZZX3030 1 19960510 A 5712 1647070 RIB LKHEED 1011 10113851 5265010 WP WS 503 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 15017 193B1063 MCI - DURING SPECIAL CHECK FOUND CRACKS IN TOP WING RIB CASTELLATION OF RT WING, IWS 503, STRINGERS 18, 19, AND 21. REP AIRED PER SB 093-57-207 AND LOCKHEED DWG NR 1647070, SHEET 3. AIRCRAFT TOTAL TIME: 60,229 HOURS; 22,908 CYCLES. 2 L 7 3 4F A23WE 1996062000275 19960620 00275 WP 1996 6 20 96ZZZX3031 1 19960510 A 5712 RIB LKHEED 1011 10113851 5265010 WP WS 555 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 15017 193B1063 MCI - DURING SPECIAL CHECK FOUND CRACK IN RIB CASTELLATION AT FORWARD SIDE OF STR 9, BOTTOM IWS 555. REPAIRED PER SRM 5 1-10-01. AIRCRAFT TOTAL TIME: 60,229 HOURS; 22,908 CYCLES. 2 L 7 3 4F A23WE 1996062000276 19960620 00276 WP 1996 6 20 96ZZZX3032 1 19960513 A 3260 833703 PROX SENSOR DOUG DC9 DC982 3022082 WP NLG FAILED A TWAA O OTHER N FALSE WARNING CL CLIMB 1 CE 05 952U 49266 STL - FLT 24 - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, NLG RED UNSAFE LIGHT REMAINED ILLUMINATED. VERIFIED NLG R ETRACTION BY MECHANICAL INDICATOR. FOUND NLG PROXIMITY SENSOR, MFG PN 8-337-03, FAULTY. REPLACED NLG PROXIMITY SENSOR. NLG INDICATION THEN CHECKED NORMAL. CHECK C-1D - 8-21-95 - MCI. 2 L 7 2 4F A6WE 1996062000277 19960620 00277 WP 1996 6 20 96ZZZX3033 1 19960513 A 3397 0105606003 WIRE DOUG DC9 DC983 3022083 WP CABIN BROKEN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 EICIW 49785 STL - DURING PRE-FLIGHT, FOUND EGRESS LIGHTING INOPERATIVE FROM SEAT ROW 31 AND AFT. FOUND BROKEN WIRE AND BROKEN LENS COVER. REPLACED WIRING MODULE, MFG PN 0105606-003, AND TRACK TOP COVER, MFG PN 0105601-003PA7. EGRESS LIGHT SYSTEM OPE RATION CHECKED NORMAL. CHECK C-1 - 6-27-95 - MCI. 2 L 7 2 4F RT A6WE 1996062000278 19960620 00278 1996 6 20 96ZZZX3034 4 19960601 A 2210 7003180901 COMPUTER BEECH 1900 1900C 1154161 CE YAW DAMPER SHORTED A GUUA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 19 11ZR UB11 MIA/TCB - FLT 381 - PILOT REPORT: ELECTRICAL SMOKE ENTERED CABIN ABOUT 5 MINUTES AFTER TAKEOFF. SUSPECT POSSIBLY BLOWE R MOTOR. AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT INCIDENT. MAINTENANCE REPORT: TROUBLESHOOTING DISCLOSED YAW DAMP COMPUTER INTERNALLY SHORTED AND PRODUCING SMOKE. 2 L 7 2 4T RT A24CE 1996062000279 19960620 00279 EU 1996 6 20 96ZZZX3035 1 19960521 A 3213 200920604 GLAND NUT ROTOL 200920004 STBROS SD3 SD360 8100606 EU RT MLG CRACKED A A DATA L A ABORTED APPROACH UNSCHED LANDING O OTHER LD LANDING 1 GL 13 124CA 12513 9474 DRG599784 SH3652 FSD/OMA - FLT 252 - UPON LANDING IN OMA AS THE AIRCRAFT TOUCHED DOWN, THE PILOT FELT THE RT MAIN GEAR START TO SINK MORE THAN NORMAL, PILOT ELECTED TO MAKE A GO-AROUND. CONTROL TOWER ADVISED THE RT GEAR DID NOT APPEAR TO BE ALL THE WAY DOW N. PILOT USED THE EMERGENCY GEAR EXTENSION SYSTEM AND GEAR STILL SHOWED INTRANSIT. PILOT THEN ELECTED TO RETURN TO FSD TO BURN OFF FUEL AND FSD IS A COMPANY MAINTENANCE BASE. EN ROUTE TO FSD, ALL 3 GREEN GEAR LIGHTS CAME ON. AIRCRAFT LA NDED IN FSD WITHOUT INCIDENT. MAINTENANCE FOUND THE SHOCK STRUT HAD COLLAPSED DUE TO FAILURE OF THE GLAND NUT. SHOCK S TRUT WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T A41EU 1996062000280 19960620 00280 EU 1996 6 20 96ZZZX3036 1 19960201 A 2420 15844000A COOLER AIRBUS 320 A320231 3930325 EU NR 2 CONTAMINATED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 621AW 053 LAS/PHO - FLT 1787 - AIR TURNBACK. ON TAKEOFF, NR 2 GENERATOR DROPPED OFF-LINE FOLLOWED BY ECAM LOW OIL PRESSURE. REMO VED AND REPLACED NR 2 IDG. OPS GOOD ON RUN-UP. REMOVED AND REPLACED COOLER. LEAK CHECK GOOD NO GROUND RUN. REFERENCE : OPERATOR CONTROL NR: AWXA960040. 2 L 7 2 4F RT A28NM 1996062000281 19960620 00281 EU 1996 6 20 AWXA960040 1 19960201 A 2421 740119F GENERATOR AIRBUS 320 A320231 3930325 EU NR 2 FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 621AW 338 053 LAS/PHO - FLT 1787 - AIR TURNBACK. ON TAKEOFF, NR 2 GENERATOR DROPPED OFF-LINE FOLLOWED BY ECAM LOW OIL PRESSURE. REMO VED AND REPLACED NR 2 IDG. OPS GOOD ON RUN-UP. REMOVED AND REPLACED COOLER. LEAK CHECK GOOD NO GROUND RUN. REFERENCE : OPERATOR CONTROL NR: 96ZZZX3036. (X) 2 L 7 2 4F RT A28NM 1996062000282 19960620 00282 NM 1996 6 20 AWXA960182 1 19960412 A 5510 BEAM BOEING 737 73733A 1384673 NM RT HORIZ STAB DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 PAE - FLT 3710 - DURING ROUTINE SCHEDULED C-11 MAINTENANCE CHECK, FOUND DAMAGE AROUND NUTPLATE FASTENER HOLES IN RT HORI ZONTAL LOWER T/E BEAM AT STABILIZER STA 119, STA 144, AND STA 158. REPAIRED DAMAGED AREA AROUND NUTPLATE FASTENER HOLES IAW ER 3-55-12-04. REFERENCE BOEING TELEX TCO-PAN-96-0466RR AND 8110-3. (X) 2 L 7 2 4F RT A16WE 1996062000283 19960620 00283 NM 1996 6 20 AWXA960183 1 19960412 A 5320 STRAP BOEING 737 73733A 1384673 NM BS 1006 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 PAE - FLT 3710 - DURING ROUTINE SCHEDULED C-11 MAINTENANCE CHECK, FOUND CORROSION ON TOP FLOOR PLATE, STA 1006 - STA 101 6, RBL 5. REMOVED AND REPLACED FLOOR PLATE AT BS 1006 - BS 1016, RBL 5 IAW SRM 51-40-2. (X) 2 L 7 2 4F RT A16WE 1996062000284 19960620 00284 NM 1996 6 20 AWXA960184 1 19960412 A 5320 FLOOR PLATE BOEING 737 73733A 1384673 NM BS 1006-1016 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 PAE - FLT 3710 - DURING ROUTINE SCHEDULED C-11 MAINTENANCE CHECK, FOUND CORROSION ON TOP FLOOR PLATE STA 1006 - STA 1016 , LBL 5. REMOVED AND REPLACED FLOOR PLATE SEAL AT BS 1006 - BS 1016, LBL 5 IAW SRM 51-40-2. (X) 2 L 7 2 4F RT A16WE 1996062000285 19960620 00285 NM 1996 6 20 AWXA960185 1 19960412 A 5320 65524577 WEB BOEING 737 73733A 1384673 NM BS 1016-1033 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 PAE - FLT 3710 - DURING ROUTINE SCHEDULED C-11 MAINTENANCE CHECK, FOUND CORROSION ON WEB, STA 1016 - STA 1033, LBL 38 - RBL 38, WL 208. REMOVED AND REPLACED AFT WEBS AT BS 1016 - BS 1033, LBL 38 - RBL 38, WL 208 IAW SRM 51-30-2. (X) 2 L 7 2 4F RT A16WE 1996062000286 19960620 00286 NM 1996 6 20 AWXA960186 1 19960412 A 5315 BAC1505100880 FLOOR BEAM BOEING 737 73733A 1384673 NM BS 986.5 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 PAE - FLT 3710 - DURING ROUTINE SCHEUDLED C-11 MAINTENANCE CHECK, FOUND CORORSION ON FLOOR BEAM TOP CHORD STA 986.5, RLB 22 - RBL 37. REMOVED CORROSION, FOUND OUT OF LIMITS, SUBMITTED FOR ENGINEERING. FABBED PARTS, ALODINE, PRIME AND INST ALLED PER ENGINEERING. ER 3-53-16-14. REFERENCE BOEING TELEX FCO-PAN-96-4566RR AND 8110-3. (X) 2 L 7 2 4F RT A16WE 1996062000287 19960620 00287 NM 1996 6 20 AWXA960188 1 19960412 A 5320 65C105922 INTERCOSTAL BOEING 737 73733A 1384673 NM BS 961 CORROSION A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 PAE - FLT 310 - DURING ROUTINE SCHEDULED C-11 MAINTENANCE CHECK, FOUND CORROSION ON INTERCOSTAL STA 961, RBL 26 - RBL 40 AT NUTPLATE HOLES. FABRICATED AND INSTALLED INTERCOSTAL IAW SRM 51-10-02 AND SRM 51-40-02. (X) 2 L 7 2 4F RT A16WE 1996062000288 19960620 00288 NM 1996 6 20 AWXA960189 1 19960412 A 5320 65C20747 INTERCOSTAL BOEING 737 73733A 1384673 NM BS 986-1006 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 PAE - FLT 3710 - DURING ROUTINE SCHEDULED C-11 MAINTENANCE CHECK, FOUND CORROSION ON INTERCOSTAL STA 986.5 - STA 1006, L BL 21. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW SRM 51-40-02. (X) 2 L 7 2 4F RT A16WE 1996062000289 19960620 00289 NM 1996 6 20 AWXA960190 1 19960412 A 5320 6546812186 INTERCOSTAL BOEING 737 73733A 1384673 NM BS 986-1006 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 PAE - FLT 3720 - DURING ROUTINE SCHEDULED C-11 MAINTENANCE CHECK, FOUND CORROSION ON INTERCOSTAL STA 986.5 - STA 1006, R BL 8 - RBL 17 AT NUTPLATE HOLES. FABRICATED AND REPLACED INTERCOSTAL IAW SRM 51-10-02 AND SRM 51-40-02. (X) 2 L 7 2 4F RT A16WE 1996062000290 19960620 00290 NM 1996 6 20 AWXA960191 1 19960412 A 5330 SKIN BOEING 737 73733A 1384673 NM BS 334-344 GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 PAE - FLT 3710 - DURING ROUTINE SCHEDULED C-11 MAINTENANCE CHECK, FOUND AIRSTAIR CUTOUT IS DAMAGED BS 334 - BS 344, SL 198. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PIECES IAW SRM 53-00-01. (X) 2 L 7 2 4F RT A16WE 1996062000291 19960620 00291 NM 1996 6 20 AWXA960192 1 19960412 A 5320 THRESHOLD BOEING 737 73733A 1384673 NM BS 950 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 PAE - FLT 3710 - DURING ROUTINE SCHEDUED C-11 MAINTENANCE CHECK, FOUND CORROSION ON LT AFT DOOR SILL STA 950, LBL 50. F ABRICATED REPAIR PARTS AND INSTALLED PER SRM 51-70-11. (X) 2 L 7 2 4F RT A16WE 1996062000292 19960620 00292 NM 1996 6 20 AWXA960221 1 19960427 A 5620 691084 WINDOW BOEING 737 73733A 1384673 NM CABIN BROKEN A AWXA K NONE O OTHER CR CRUISE 1 WP 28 165AW 23626 SMF/SNA - FLT 0775 - OUTER CABIN WINDOW PANE AT ROW 4 RT, HAD OUTER PIECE MISSING WITH NO PRESSURIZATION PROBLEMS. REMO VED AND REPLACED WINDOW ASSY AND SEAL. (X) 2 L 7 2 4F RT A16WE 1996062000293 19960620 00293 NE 1996 6 20 AWXA960224 2 19960430 A 7530 BLEED VALVE AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE NR 1 MALFUNCTIONED A A AWXA B G EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 WP 28 628AW 67 CMH - FLT 0266 - BOTH NR 1 AND NR 2 BLEED VALVES FAILED IN-FLIGHT. EMERGENCY DESCENT. ALL CABIN OXYGEN MASKS DROPPED. PERFORMED BLEED SYSTEM INSPECTION ON BOTH ENGINES PER SIL 36-034 AND RAN ENGINES. NO DEFECTS NOTED. REPLACED ALL OXYG EN MASKS EXCEPT ALL LAVS, ROWS 12, 21, 24, AND 25 RIGHT TO 10 AND 17 LEFT. NR 2 BLEED WAS ON MEL 36-11-07, WHEN PILOT I NADVERTENTLY SELECTED ENGINE ANTI-ICE WITHOUT TURNING 1 PACK OFF, THUS CAUSING BLEED FAILURE. (X) 2 L 7 2 4F 4 F RT A28NM E311NE 1996062000294 19960620 00294 NM 1996 6 20 AWXA960236 1 19960519 A 2612 FIRE LOOP BOEING 757 7572S7 1384962 NM LT ENGINE OUT OF POSITION A AWXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 28 906AW 23568 PHX/ATL - FLT 0610 - AIR TURNBACK. LEFT ENGINE OVERHEAT EICAS AND LIGHT AT 20,000 FEET ON CLIMB-OUT. CHECK COMPLETE LI GHTS EXTINGUISHED, LEFT ENGINE AT IDLE AND RETURNED TO PHX. PER FIM 26-11-10, INSPECTED LEFT BLEED DUCTS, NO LEAKS FOUN D. FOUND 3 AREAS OF FIRE LOOP TOUCHING ATTACH TUBE. REPOSITIONED. RAN ENGINE AT HIGH IDLE. (X) 2 L 7 2 4F RT A2NM 1996062000295 19960620 00295 EU 1996 6 20 AWXA960237 1 19960520 A 3350 Z040Y0000110 DEU AIRBUS 320 A320231 3930325 EU NR 4 FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 622AW 17316 054 CHM - FLT 0651 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTING ON WITHOUT POWER FAILURE AT SW COMMAND. RESETS OK. REMOVED AND REPLACED DEU (DECODER ENCODER UNIT) 100RH1. OPS CHECK GOOD. PART TOTAL CYCLES, 8,893. (X) 2 L 7 2 4F RT A28NM 1996062000296 19960620 00296 NM 1996 6 20 AWXA960242 1 19960522 A 3610 312N53217 DUCT BOEING 757 7572S7 1384962 NM NR 1 ENGINE FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 906AW 18221 23568 PHX/EWR - FLT 0684 - AIR TURNBACK. NR 1 ENGINE OVERHEAT IN CLIMB. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED HP6 DUCT. PART TOTAL CYCLES, 7016. (X) 2 L 7 2 4F RT A2NM 1996062000297 19960620 00297 NM 1996 6 20 EIAA9616 1 19960526 A 3244 260356115 TIRE BOEING 747 747212B 1384886 NM NR 5 FAILED A EIAA O OTHER D INFLIGHT SEPARATION LD LANDING 1 NM 09 482EV 94 20713 ANC - UPON LANDING AT ANC, FOUND NR 5 TIRE TREAD SEPARATED, HOWEVER, THE TIRE WAS STILL INFLATED. THE LEFT BODY MLG OUT BOARD DOOR AND ADJACENT AREA SUFFERED DAMAGE AS A RESULT. REMOVED AND REPLACED NR 5 AND NR 6 TIRE ASSEMBLY. TEMPORARY REPAIR ACCOMPLISHED ON THE LT BMLG OUTBOARD DOOR AND ADJACENT AREA PER ECRA 482-52-101-1 TO FLY AIRCRAFT TO JFK, WHERE P ERMANENT REPAIR WAS ACCOMPLISHED. (X) 2 L 7 4 4F A20WE 1996062000298 19960620 00298 NM 1996 6 20 EIAA9617 1 19960529 A 2424 21B731G GCU BOEING 747 747273C 1384896 NM NR 2 ENGINE FAILED A EIAA J A DUMP FUEL UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 NM 09 470EV 20653 HKG - AFTER TAKEOFF (5 MINS INTO FLIGHT) NR 1 AND NR 2 BUS TIE LIGHTS ILLUMINATED. ALSO, SSB OPENED. CONTINUED FLIGHT WITH LIGHTS ON. APPROXIMATELY 20 MINS LATER, NR 2 GENERATOR OPEN LIGHT AND FIELD LIGHT ILLUMINATED. COULD NOT RESET FI ELD OR BUS TIE LIGHTS. GENERATOR PANEL SHOWED CONTROL NR 2 GENERATOR AND CSD NR 1 GENERATOR. NR 1 GENERATOR SHOWED 110 VOLTS AND NORMAL FREQUENCY. DUMPED FUEL AND RETURNED TO HKG. REPLACED LT BCPU AND NR 2 GCU. CHECKED NR 1 AND NR 2 CS D OIL LEVEL. BOTH FOUND NORMAL. CLEANED CANNON PLUG ON NR 1 GCU. PERFORMED ENGINE RUN ON NR 1 AND NR 2. SYSTEM CHECK ED OK. INDICATIONS CHECKED GOOD ON GENERATOR VOLTS, PMG VOLTS, REQ, AND CSD RPM. (X) 2 L 7 4 4F A20WE 1996062000299 19960620 00299 CE 1996 6 20 S2YA960009 1 19960517 A 3500 1145600585 OXY FILL TUBE BEECH 1900 1900D 1154162 CE NLG WW NUT CRACKED A S2YA K NONE O OTHER IN INSP/MAINT 1 GL 13 79SK 5549 UE79 MAINTENANCE WAS TRYING TO SERVICE THE OXYGEN, BUT FOUND A LEAK DUE TO A CRACKED BRASS B-NUT ON THE RT SIDE OF THE CROSS- OVER FILL LINE. THEY ALSO FOUND THE SAME TYPE OF NUT CRACKED ON A SMALLER LINE, PN 129-560047-5, IN THE SAME LOCATION O N AIRCRAFT UE-90, 5/12/96. SUBMITTER SUSPECTS OVERTORQUE OF LINE AT FACTORY INSTALLATION, AND/OR NUT NOT SUITABLE FOR I NSTALLATION. (X) 2 L 7 2 4T RT A24CE 1996062000300 19960620 00300 NM 1996 6 20 TAOA069601 1 19960601 A 8012 97907021 START VALVE BOEING 727 727254 138408L NM NR 1 ENGINE FAILED A TAOA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 EA 15 915TS P582 20252 LGA/MCO - FLT 6653 - DURING DESCENT, NR 1 ENGINE START VALVE OPEN LIGHT CAME ON. NR 1 ENGINE WAS SHUT DOWN IN-FLIGHT. F OUND THE NR 1 ENGINE START VALVE NOT CLOSING PROPERLY. REPLACED NR 1 ENGINE START VALVE PER MM 80-11-11. (X) 2 L 7 3 4F A3WE 1996062000301 19960620 00301 NM 1996 6 20 TAOA069602 1 19960602 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 925TS 11725 21244 BOS/LGA - FLT 6141 - FOUND ON OVERNIGHT CHECK, FORWARD CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PA CK, OPS CHECK OK PER MM 33-50-00. (X) 2 L 7 3 4F A3WE 1996062000302 19960620 00302 1996 6 20 TWRA9631 4 19960529 A 2565 B-NUT FITTING D30440105 BOEING 747 747130 1384880 NM SLIDE RAFT FAILED A TWRA K NONE O OTHER IN INSP/MAINT 1 EA 15 603FF 0199 19746 WHILE PERFORMING A TRAINING SLIDE DEPLOYMENT AT R4 MED, THE AFT ASPIRATOR HOSE B-NUT FITTING FAILED AND THE SLIDE RAFT, PN D30440105, PARTIALLY INFLATED. THE SLIDE/RAFT USED WAS RETAINED FOR TRAINING PURPOSES AFTER REMOVAL FOR OVERHAUL DUE DATE. THE SLIDE RAFT HAS BEEN SENT OUT TO THE REPAIR STATION FOR OVERHAUL. THE ASPIRATOR HOSE ASSY WAS REMOVED AND RO UTED TO THE MANUFACTURER FOR ENGINEERING EVALUATION. (X) 2 L 7 4 4F A20WE 1996062000303 19960620 00303 WP 1996 6 20 USAAD96061 1 19960517 A 3231 RETRACT MECH DOUG DC9 DC931 3022065 WP RT NLG DOOR OUT OF ADJUST A USAA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 EA 19 918VJ 48138 JFK/PIT - FLT 721 - AFTER TAKEOFF, RETRACTING GEAR, NOSE GEAR UNSAFE LIGHT STAYED ON, AND THERE WAS A LOUD VIBRATION. R ECYCLED GEAR, DID SAME THING. ON WALK-AROUND AFTER LANDING, FOUND RT FORWARD NOSE GEAR DOOR OPEN. REPLACED LOCK SENSOR PROXIMITY SWITCH AND CONDUIT AND ADJUSTED CLEARANCE PER MM. SERVICED NOSE STRUT WITH AIR AND OIL PER MM. ALSO, ADJUST ED RT NOSE GEAR DOOR FORWARD BUNGEE TO PROPER TENSION PER MM. (X) 2 L 7 2 4F A6WE 1996062000304 19960620 00304 WP 1996 6 20 USAAD96062 1 19960524 A 2742 1031T10019 TRIM MOTOR DOUG DC9 DC931 3022065 WP HORIZ STAB FAILED A USAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 19 926VJ 32857 252 48146 PIT/EWR - FLT 936 - PRIMARY TRIM DOES NOT TRIM FORWARD. RETURNED TO FIELD. REPLACED PRIMARY TRIM MOTOR AND TRIM BRAKE RELAYS. (X) 2 L 7 2 4F A6WE 1996062000305 19960620 00305 WP 1996 6 20 USAAD96063 1 19960528 A 5610 5912290505 WINDSHIELD DOUG DC9 DC931 3022065 WP LT COCKPIT CRACKED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 937VJ 6171 13396H 48117 PIT/MKE - FLT 410 - CAPTAIN'S WINDSHIELD DEVELOPED SMALL CRACK IN LOWER LEFT CORNER AND SPREAD RAPIDLY. ARCING AND DELA MINATIONS STARTED TO FOLLOW CRACKS. DIVERTED TO LAN. REPLACED CAPTAIN'S WINDSHIELD. (X) 2 L 7 2 4F A6WE 1996062000306 19960620 00306 1996 6 20 USAAD96064 4 19960529 A 3418 80098717 AOA VANE DOUG DC9 DC931 3022065 WP FWD FUSELAGE FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 950VJ 47564 CLT/FAY - FLT 1527 - STALL INDICATION FAILURE WARNING ILLUMINATED ON DEPARTURE. FLIGHT RETURNED TO CLT. ON APPROACH, L IGHT EXTINGUISHED. REPLACED LEFT AND RIGHT AOA VANES. (X) 2 L 7 2 4F A6WE 1996062000307 19960620 00307 WP 1996 6 20 USAAD96065 1 19960516 A 3350 60030451LB BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 997VJ 47336 COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED FORWARD BATTERY PACK. (X) 2 L 7 2 4F A6WE 1996062000308 19960620 00308 WP 1996 6 20 USAAD96066 1 19960530 A 3350 41B030CF00101 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 912VJ 47020 LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED LEFT NACELLE EMERGENCY LIGHT BATTERY PACK. (X) 2 L 7 2 4F A6WE 1996062000309 19960620 00309 WP 1996 6 20 USAAD96067 1 19960531 A 2751 BAN70241 SWITCH DOUG DC9 DC931 3022065 WP LT MLG WW FAILED A USAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 EA 19 936VJ 48116 LGA/RDU - FLT 1507 - ON APPROACH, FLAPS WOULD NOT GO TO 25 DEGREES WITHOUT HORN SOUNDING. GEAR WAS DOWN. REPLACED FLAP SWITCH S1-85. ALSO, REPLACED DISCONNECT P1-227. (X) 2 L 7 2 4F A6WE 1996062000310 19960620 00310 WP 1996 6 20 USAAD96068 1 19960601 A 2130 PRESSURIZATION DOUG DC9 DC982 3022082 WP CABIN MALFUNCTIONED A USAA B EMER. DESCENT O OTHER CR CRUISE 1 EA 19 829US 49429 RIC/CLT - FLT 761 - CABIN ALTITUDE CONTROLLER FAILED TO MAINTAIN ALTITUDE AND CLIMBED AT A HIGH RATE ABOVE 10,000 FEET. DESCENDED TO 8,000 FEET. PERFORMED BITE CHECK ON NR 1 AND NR 2 PRESSURIZATION CONTROLLERS. NO FAULTS FOUND. RAN NR 1 AND NR 2 PACKS, OPS NORMAL. (X) 2 L 7 2 4F A6WE 1996062000311 19960620 00311 WP 1996 6 20 USAAD96069 1 19960530 A 3350 41B030CF00101 BATTERY PACK DOUG DC9 DC931 3022065 WP LT NACELLE DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 912VJ 47020 LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED LEFT NACELLE EMERGENCY LIGHT BATTERY PACK. (X) 2 L 7 2 4F A6WE 1996062000312 19960620 00312 WP 1996 6 20 USAAD96070 1 19960531 A 3350 110049 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 968VJ 47429 FORWARD AISLE EMERGENCY LIGHTS AND EXIT SIGNS INOPERATIVE. REPLACED BATTERY PACK. (X) 2 L 7 2 4F A6WE 1996062000313 19960620 00313 WP 1996 6 20 USAAD96071 1 19960604 A 2120 DUCT DOUG DC9 DC931 3022065 WP RT PACK LOOSE A USAA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 EA 19 966VJ 47420 ORF/CLT - FLT 1139 - TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED AT 11,000 FEET. RETURNED TO FIELD. RECONNECTE D AIR DUCT TO RIGHT PACK. (X) 2 L 7 2 4F A6WE 1996062000314 19960620 00314 NM 1996 6 20 USAASB96100 1 19960604 A 3230 BACC45FN18A14S CONNECTOR BOEING 737 737301 1384611 NM WHEELWELL FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 589US 23934 CLT - FLT 765 - CREW COULD NOT RAISE GEAR OR PRESSURIZE AIRCRAFT AFTER TAKEOFF. FLIGHT RETURNED TO FIELD AND LANDED WIT H NO FURTHER INCIDENT. MAINTENANCE REPLACED PINS 3 AND 4 IN CONNECTOR D4574P. GEAR SWING ACCOMPLISHED. (X) 2 L 7 2 4F RT A16WE 1996062000315 19960620 00315 EU 1996 6 20 VTZA96211 1 19960603 A 2611 7211121100 SMOKE DETECTOR BAG JETSTM JETSTM3201 1500217 EU BAGGAGE BAY MALFUNCTIONED A VTZA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 476UE 884 FLT NR 6377 - IAD-CRW - DURING TAXI, AIRCRAFT RETURNED TO GATE DUE TO THE RED SMOKE CAPTION ILLUMINATING. AIRCRAFT RETU RNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE BAGGAGE BAY SMOKE DETECTOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996062000316 19960620 00316 SO 1996 6 20 WTAA960108 1 19960521 A 3234 12038594001 SELECTOR EMB 120 EMB120RT SO LANDING GEAR MALFUNCTIONED A WTAA O OTHER J WARNING INDICATION CL CLIMB 1 WP 17 276UE 120067 FAT - LANDING GEAR FAILED TO RETRACT ON INITIAL ATTEMPT. GEAR RETRACTION NORMAL ON THIRD ATTEMPT. MAINTENANCE UNABLE T O DUPLICATE DISCREPANCY ON GROUND. SUSPECT FAULTY LANDING GEAR SELECTOR. REPLACED SELECTOR. SYSTEM OPEATIONAL CHECK N ORMAL DURING GEAR RETRACTION CHECK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1996062000317 19960620 00317 NM 1996 6 20 96ZZZX3037 1 19960411 A 5523 65C2638416A TRIM TAB BOEING 737 7373G7 1384595 NM RT ELEVATOR WORN A A AWXA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 28 150AW 48925 23218 PHX/IAH - FLT 0276 - AIR TURNBACK. ENCOUNTERED HIGH SPEED VIBRATION THROUGH RUDDER PEDALS SHORTLY AFTER LIFT OFF AND CO NTINUED THROUGH CRUISE. REMOVED AND REPLACED LEFT AND RIGHT ELEVATOR TRIM TABS. TEST FLIGHT SATISFACTORY, NO VIBRATION NOTED. ACFT TT: 34,607 HRS. ACFT TC: 30,237. REFERENCE: OPERATOR CONTROL NR AWXA960181. 2 L 7 2 4F RT A16WE 1996062000318 19960620 00318 NM 1996 6 20 96ZZZX3038 1 19960511 A 2131 7638101 CONTROLLER BOEING 737 7373G7 1384595 NM CABIN FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 308AW 84011612 24710 LAS/ABQ - FLT 0720 - AIR TURNBACK. AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF IN ANY MODE. REMOVED AND REPLACED PRESS URE CONTROL PANEL AND CABIN PRESSURE CONTROLLER. SYSTEM OPS CHECK GOOD. REFERENCE: OPERATOR CONTROL NR AWXA960225. 2 L 7 2 4F RT A16WE 1996062000319 19960620 00319 EU 1996 6 20 96ZZZX3039 1 19960602 A 2731 SD3456029XA CONTROL CABLE STBROS SD3 SD360 8100606 EU ELEVATOR TRIM BROKEN A A GUUA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 19 826BE SH3745 MIA/MCO - FLT 427A - PILOT REPORT: CLIMBING OUT OF MIA APPROXIMATELY 300 FEET AFTER DEPARTING RUNWAY, LOST ELEVATOR TRI M. DECLARED AN EMERGENCY, RETURNED TO MIA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE: REMOVED AND REPLACED ELEV ATOR TRIM CABLE. 2 H 7 2 4T A41EU 1996062000320 19960620 00320 NE 1996 6 20 96ZZZX3040 2 19960419 A 7310 5905587 FUEL FILTER EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE OBSTRUCTED A GLBA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 01 452UE 120096 SPI - CREW REPORTED RT FUEL FILTER LIGHT ILLUMINATED ON TAKEOFF ROLL AND THEY RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED HIGH AND LOW PRESSURE FUEL FILTERS. OPS CHECK WAS GOOD. REFERENCE: OPERATOR CONTROL NR GLBA96075. 2 L 7 2 4T 4 T RT A31SO E20NE 1996062000321 19960620 00321 NM 1996 6 20 AWXA960174 1 19960404 A 5330 SKIN BOEING 737 7372U9 1384498 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 149AW 22575 PHX - FLT 0275 - DURING ROUTINE MAINTENANCE CHECK, FOUND CRACK IN FUSELAGE RIGHT SIDE OF AIRCRAFT ABOVE AFT WING TO BODY FAIRING APPROXIMATELY 1.5 INCHES. REPAIRED PER SRM 53-30-06. ACFT 44,898 HRS. ACFT TC: 33,583. (X) 2 L 7 2 4F RT A16WE 1996062000322 19960620 00322 NM 1996 6 20 AWXA960180 1 19960409 A 2612 CONNECTORS BOEING 737 737275 1384485 NM NR 2 ENGINE DIRTY A AWXA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 WP 28 CGCPW 20959 PHX/ICT - FLT 0981 - IN-FLIGHT SHUT DOWN. NR 2 ENGINE FIRE WARNING ON FINAL APPROACH INTO ICT. ENGINE SHUT DOWN AND BO TH FIRE BOTTLES ACTIVATED. NO FIRE ON LANDING. CLEANED CONNECTORS D1094 AND D1098. HARD FAULT VANISHED. OPS TEST PER MM 26-11-00, PG 501. OPS TEST GOOD. (X) 2 L 7 2 4F A16WE 1996062000323 19960620 00323 NM 1996 6 20 AWXA960181 1 19960411 A 5523 65C2638416A TRIM TAB BOEING 737 7373G7 1384595 NM LT ELEVATOR WORN A a AWXA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 28 150AW 23218 PHX/IAH - FLT 0276 - AIR TURNBACK. ENCOUNTERED HIGH SPEED VIBRATION THROUGH RUDDER PEDALS SHORTLY AFTER LIFT OFF AND CO NTINUED THROUGH CRUISE. REMOVED AND REPLACED LEFT AND RIGHT ELEVATOR TRIM TABS. TEST FLIGHT SATISFACTORY, NO VIBRATION NOTED. ACFT TT: 34,607 HRS. ACFT TC: 30,237. REFERENCE: OPERATOR CONTROL NR 96ZZZX3037. (X) 2 L 7 2 4F RT A16WE 1996062000324 19960620 00324 NM 1996 6 20 AWXA960187 1 19960412 A 5315 BAC1505100617 FLOOR BEAM BOEING 737 73733A 1384673 NM BS 1016 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 PAE - FLT 3710 - DURING ROUTINE SCHEDULED C-11 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM TOP CHORD AROUND NUTPLAT E HOLES STA 1016, LBL 38 - RBL 38. REMOVED CORRODED CHORD, FABRICATED AND INSTALLED NEW CHORD, WORK PERFORMED IAW ER 3- 53-16-32. REFERENCE BOEING TELEX TCO-PAN-96-454RRR AND 8110-3. ACFT TT: 34,430 HRS. ACFT TC, 20,842. (X) 2 L 7 2 4F RT A16WE 1996062000325 19960620 00325 NM 1996 6 20 AWXA960200 1 19960423 A 2131 7638101 CONTROLLER BOEING 737 737277 1384570 NM CABIN MALFUNCTIONED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 184AW 38560 346 22651 PHX/OAK - FLT 0450 - AIR TURNBACK. PRESSURIZATION WENT TO MAXIMUM DIFFERENTIAL ON CLIMB-OUT. UNCONTROLLABLE IN AUTO MO DE. CREW REPORTED NO ENGINE BLEED PROBLEMS. INSPECTED CARGO DOOR SEALS AND PERFORMED OPERATIONS CHECK OF CABIN PRESSUR E CONTROLLER AND OUTFLOW VALVE. NO DISCREPANCIES NOTED. REMOVED AND REPLACED CPC PER MM 21-31-21 AS PRECAUTION. OPERA TIONS CHECK AND LEAK CHECK OF FIRST AUXILIARY STATIC GOOD. PART TOTAL CYCLES, 31,351. (X) 2 L 7 2 4F RT A16WE 1996062000326 19960620 00326 NM 1996 6 20 AWXA960201 1 19960423 A 5320 6546812186 INTERCOSTAL BOEING 737 73733A 1384673 NM BS 986.5 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 174AW 23633 PAE - FLT 3710 - DURING ROUTINE SCHEDULED C-11 MAINTENANCE CHECK, FOUND CORROSION ON INTERCOSTAL STA 986.5 - STA 1006, L BL 8 - LBL 17 AT NUTPLATE HOLES. FABRICATED AND INSTALLED INTERCOSTAL IAW SRM 51-40-02. ACFT TT: 34,430 HRS. ACFT T C: 20,842. (X) 2 L 7 2 4F RT A16WE 1996062000327 19960620 00327 NM 1996 6 20 AWXA960208 1 19960418 A 5315 65C346882 FLOOR BEAM BOEING 737 737277 1384570 NM BS 520 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 178AW 22645 PAE - FLT 3808 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND UPPER CHORD OF FLOOR BEAM CRACKED IN RADIUS AT SE AT TRACK ATTACH POINT STA 520, LBL 24.45, WL 208. STOP DRILLED CRACK FOR CONTAINMENT AND REPAIR ACCOMPLISHED PER EO 53- 14-12. ACFT TT: 44,382 HRS. ACFT TC: 36,778. (X) 2 L 7 2 4F RT A16WE 1996062000328 19960620 00328 NM 1996 6 20 AWXA960209 1 19960418 A 5315 65C346882 FLOOR BEAM BOEING 737 737277 1384570 NM BS 520 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 178AW 22645 PAE - FLT 3808 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND UPPER CHORD OF FLOOR BEAM CRACKED IN RADIUS AT SE AT TRACK ATTACH POINT, STA 520, RBL 45.5. CRACK CONTAINED AND REPAIR COMPLETED ON FLOOR BEAM CHORD PER EO 53-14-12. A CFT TT: 44,382 HRS. ACFT TC: 36,778. (X) 2 L 7 2 4F RT A16WE 1996062000329 19960620 00329 NM 1996 6 20 AWXA960210 1 19960414 A 5330 SKIN BOEING 737 737277 1384570 NM BS 312 GOUGE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 178AW 22645 PAE - FLT 3808 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 312, STR 4L AND STR 2. REPAIRED IAW SRM 53-30-03. ACFT TT: 44,382 HRS. ACFT TC: 36,778. (X) 2 L 7 2 4F RT A16WE 1996062000330 19960620 00330 NM 1996 6 20 AWXA960211 1 19960417 A 5313 STRINGER BOEING 737 737277 1384570 NM BS 902-917 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 178AW 22645 PAE - FLT 3808 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND CORROSION AT SPLICE OF 27L, STRINGER AT BS 902 - BS 917. REPAIRED IAW SRM 53-10-01, SRM 53-10-03. ACFT TT: 44,382 HRS. ACFT TC: 36,778. (X) 2 L 7 2 4F RT A16WE 1996062000331 19960620 00331 NM 1996 6 20 AWXA960212 1 19960422 A 5330 SKIN BOEING 737 737277 1384570 NM BS 699-697 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 178AW 22645 PAE - FLT 3808 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND CRACK AT BS 699 TO BS 697, LBL WL 148.5 IN KEEL B EAM SKIN. REPAIRED PER ER 2-53-15-23, TCO-PAN-96-0521RR AND 8110-13. ACFT TT: 44,382 HRS. ACFT TC: 36,778. (X) 2 L 7 2 4F RT A16WE 1996062000333 19960620 00333 NM 1996 6 20 AWXA960214 1 19960422 A 5330 SKIN BOEING 737 737277 1384570 NM BS 699-697 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 178AW 22645 PAE - FLT 3808 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND CRACK IN KEEL BEAM SKIN AT BS 699.5 TO BS 697.5, RBL 5 TO WL 148.5. REPAIRED PER ER 2-53-15-23, TCO-PAN-96-0521RR AND 8110-3. ACFT TT: 44,382 HRS. ACFT TC: 36,778. (X) 2 L 7 2 4F RT A16WE 1996062000334 19960620 00334 NM 1996 6 20 AWXA960215 1 19960419 A 5315 FLOOR BEAM BOEING 737 737277 1384570 NM BS 1016-3978 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 178AW 22645 PAE - FLT 3808 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND CORROSION (C53-107-02 PT2) ON BS 1016 UPPER FLOOR BEAM CHORD LBL 5 TO LBL 26, WL 208. REMOVED CORROSION FROM BS 3978 - BS 1016; LBL 5 - RBL 16, WL 208. FOUND OUT OF LI MITS PER SRM 53-10-01 AND REMOVED CHORD AT BS 1016, LBL 40 - RBL 40. FABRICATED NEW CHORD AND INSTALLED PER SRM 53-10-0 1 AND ER NR 3-53-16-32, TCO-PAN-96-0511RR. ACFT TT: 44,382 HRS. ACFT TC: 36,778. (X) 2 L 7 2 4F RT A16WE 1996062000335 19960620 00335 NM 1996 6 20 AWXA960216 1 19960419 A 5315 BAC1505100880 FLOOR BEAM BOEING 737 737277 1384570 NM BS 986 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 178AW 22645 PAE - FLT 3808 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM BS 986, LBL 10 - RBL 18, RBL 30 - RBL 51. REPAIRED FLOOR BEAM PER GR 2-53-1-36, TCO-PAN-96-0510RR. ACFT TT: 44,382 HRS. ACFT TC: 36,778. ( X) 2 L 7 2 4F RT A16WE 1996062000336 19960620 00336 NM 1996 6 20 AWXA960217 1 19960419 A 5315 65498834 FLOOR BEAM BOEING 737 737277 1384570 NM BS 947 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 178AW 22645 PAE - FLT 3808 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM BS 947, LBL 18 TO RBL 18. REPAIRED FLOOR BEAM PER G.R. 2-53-15-35, TCO-PAN-96-0509ER. (X) 2 L 7 2 4F RT A16WE 1996062000337 19960620 00337 NM 1996 6 20 AWXA960218 1 19960413 A 5315 FLOOR BEAM BOEING 737 737277 1384570 NM BS 986 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 178AW 22645 PAE - FLT 3808 - DURING ROUTINE SCHEDULE C-9 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM BS 986, LBL 10 - RBL 18, R BL 30 - RBL 44. REPAIRED PER ER 2-53-15-36 AND TCO-PAN-96-051ORR. ACFT TT: 44,382 HRS. ACFT TC: 36,778. (X) 2 L 7 2 4F RT A16WE 1996062000338 19960620 00338 NM 1996 6 20 AWXA960219 1 19960214 A 5247 SKIN BOEING 737 737277 1384570 NM APU DOOR DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 178AW 22645 PAE - FLT 3808 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND DENT IN APU ACCESS DOOR OUTER SKIN NEAR AFT FLANG E. REPAIRED DENT, IAW SRM 52-00-03. ACFT TT: 44,882 HRS. ACFT TC: 36,778. (X) 2 L 7 2 4F RT A16WE 1996062000339 19960620 00339 NM 1996 6 20 AWXA960220 1 19960414 A 5330 SKIN BOEING 737 737277 1384570 NM BS 802 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 178AW 22645 PAE - FLT 3808 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND SKIN BULGING AROUND FASTENER STA 802, WL 148, RBL 13. REPAIRED SKIN IAW SRM 53-30-03. ACFT TT: 44,382 HRS. ACFT TC: 36,778. (X) 2 L 7 2 4F RT A16WE 1996062000340 19960620 00340 NM 1996 6 20 AWXA960225 1 19960511 A 2130 7110025 PRESS CONTL PNL BOEING 737 7373G7 1384595 NM COCKPIT FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 308AW 8103473 24710 LAS/ABQ - FLT 0720 - AIR TURNBACK. AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF IN ANY MODE. REMOVED AND REPLACED PRESS URE CONTROL PANEL AND CABIN PRESSURE CONTROLLER. SYSTEM OPS CHECK GOOD. REFERENCE: OPERATOR CONTROL PANEL 96ZZZX3038. (X) 2 L 7 2 4F RT A16WE 1996062000341 19960620 00341 NM 1996 6 20 AWXA960232 1 19960501 A 5320 THRESHOLD BOEING 737 7373G7 1384595 NM BS 807-847 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 151AW 23219 PAE - FLT 3828 - DURING ROUTINE SCHEDULED C-12 MAINTENANCE CHECK, FOUND AFT CARGO BAY DOOR SUB-THRESHOLD CORRODED ON THE FORWARD CORNER. FOUND CORROSION BEYOND LIMITS. REMOVED CORRODED SUB-THRESHOLD, FABRICATED AND INSTALLED NEW SUB-THRES OLD. ALL PER 51-20-01, 51-10-02, AND 53-30-15. ACFT TT: 34,561 HRS. ACFT TC: 30,335. (X) 2 L 7 2 4F RT A16WE 1996062000342 19960620 00342 NM 1996 6 20 AWXA960233 1 19960501 A 5320 INTERCOSTAL BOEING 737 7373G7 1384595 NM BS 327 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 151AW 23219 PAI - FLT 3828 - DURING ROUTINE SCHEDULED C-12 MAINTENANCE CHECK, FOUND BS 327, LBL 45, WL 208, INTERCOSTAL CRACKED AT T OP AFT CORNER. REMOVED CRACKED INTERCOSTAL FROM BS 328 TO BS 312. FABRICATED AND INSTALLED NEW INTERCOSTAL PER SRM'S 5 1-10-02, 53-10-02, 53-10-05, 51-30-01. ACFT TT: 34,561 HRS. ACFT TC: 30,335. (X) 2 L 7 2 4F RT A16WE 1996062000343 19960620 00343 NM 1996 6 20 AWXA960234 1 19960508 A 5241 65C340682 HINGE BOEING 737 7373G7 1384595 NM FWD GALLEY DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 151AW 23219 PAI - FLT 3828 - DURING ROUTINE SCHEDLED C-12 MAINTENANCE CHECK, FOUND LOWER GATE HINGE CRACKED ON FORWARD GALLEY DOOR. REMOVED AND REPLACED LOWER GATE HINGE ON R1 GALLEY DOOR PER OHM 52-46-05. ACFT TT: 34,559 HRS. ACFT TC: 30,334. (X ) 2 L 7 2 4F RT A16WE 1996062000344 19960620 00344 NM 1996 6 20 AWXA960235 1 19960509 A 3260 9650648005 GPWS COMPUTER BOEING 737 7373G7 1384595 NM LANDING GEAR MALFUNCTIONED A AWXA O OTHER N FALSE WARNING LD LANDING 1 WP 28 151AW 1659 23219 PAE - FLT 3828 - DURING ROUTINE SCHEDULED C-12 MAINTENANCE CHECK WHILE ATTEMPTING TO LAND, GROUND PROXIMITY COMPUTER CON TINUALLY GAVE FALSE 'GEAR UNSAFE' WARNINGS. TROUBLESHOT AND FOUND G.R.W.S. COMPUTER AT FAULT. REMOVED AND REPLACED COM PUTER AND FUNCTIONAL CHECKED GOOD PER MM 34-42-11. (X) 2 L 7 2 4F RT A16WE 1996062000345 19960620 00345 NM 1996 6 20 AWXA960246 1 19960525 A 5523 65C2638420A TAB BOEING 737 73733A 1384673 NM RT ELEVATOR WORN A a AWXA K NONE E VIBRATION/BUFFET CR CRUISE 1 WP 28 168AW 5323H 23629 PHX/MCI - FLT 0593 - INBOUND, CREW REPORTS HIGH FREQUENCY VIBRATIONS IN-FLIGHT. REMOVED AND REPLACED RT ELEVATOR TAB PE R CARD R6C27007. OPERATES NORMALLY. ACFT TT: 32,297 HRS. ACFT TC: 24,346. X) 2 L 7 2 4F RT A16WE 1996062000346 19960620 00346 NE 1996 6 20 GLBA96075 2 19960419 A 7310 3038454 FUEL FILTER EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE OBSTRUCTED A GLBA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 01 452UE 120096 SPI - CREW REPORTED RT FUEL FILTER LIGHT ILLUMINATED ON TAKEOFF ROLL AND THEY RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED HIGH AND LOW PRESSURE FUEL FILTERS. OPS CHECK WAS GOOD. REFERENCE: OPERATOR CONTROL NR 96ZZZX3040. (X) 2 L 7 2 4T 4 T RT A31SO E20NE 1996062000347 19960620 00347 SO 1996 6 20 GLBA96076 1 19960416 A 5297 WIRE EMB 120 EMB120RT 3260202 SO PASSENGER DOOR BROKEN A GLBA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 01 279UE 120085 RDU - CREW REPORTED FORWARD CABIN DOOR ANNUNCIATOR ILLUMINATED ON TAXI AND THEY RETURNED TO GATE. MAINTENANCE REPAIRED BROKEN WIRE AT FORWARD MICROSWITCH. OPS CHECK WAS GOOD. (X) 2 L 7 2 4T RT A31SO 1996062000348 19960620 00348 EU 1996 6 20 VTZA96209 1 19960531 A 5240 14153133501 SERVICE DOOR JETAIR JETSTM JETSTM4101 1500501 EU L REAR FUSELAGE MISSING A A VTZA O OTHER D INFLIGHT SEPARATION CR CRUISE 1 EA 27 327UE 41080 IAD/DAY - FLT 6292 - DURING CRUISE AT 1330 HRS, THE LAVATORY SERVICE DOOR SEPARATED FROM THE AIRCRAFT. AIRCRAFT CONTINU ED TO DAY WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 46085 IAW MEL 52-4. MAINTENANCE LATER CLEARED DMI NR 46 085 BY REPLACING THE LAVATORY SERVICE DOOR ON 6-10-96. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. SUBMI TTER STATED THIS IS THE 9TH DOOR SEPARATION. AD IS RECOMMENDED. (X) 2 L 7 2 4T RT A41NM 1996062000349 19960620 00349 NE 1996 6 20 9613279858 2 19960617 A 7320 P/D VALVE DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE LT ENGINE MALFUNCTIONED A NWAA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 01 767NC 47724 696737 DURING CLIMB, THE LEFT ENGINE OPERATING PARAMETERS BEGAN TO FLUCTUATE. THE AIRCRAFT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. GROUND MAINTENANCE REPLACED P AND D VALVE AND PERFORMED ENGINE GROUND RUN AND LEAK CHECK. 2 L 7 2 4F 4 F A6WE E2EA 1996062000350 19960620 00350 WP 1996 6 20 9613299152 1 19960616 A 3350 BATTERY PACK DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8911E 45825 DURING LINE CHECK, FOUND TAIL COMPARTMENT OVERHEAD EMERGENCY LIGHTS AND AFT RIGHT AISLE OVERHEAD EMERGENCY LIGHT INOPERA TIVE. REPLACED BATTERY PACK B5-28. ALL EMERGENCY LIGHTS CHECKED OK. 2 L 7 2 4F A6WE 1996062000351 19960620 00351 NM 1996 6 20 9613302710 1 19960617 A 3350 LIGHT BOEING 727 727225 1384077 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 820EA 22557 DURING PREFLIGHT, FOUND EMERGENCY LIGHT IN COCKPIT POSITION INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY, CHECKED OK. 2 L 7 3 4F A3WE 1996062000352 19960620 00352 NM 1996 6 20 9613312283 1 19960616 A 3350 BATTERY PACK BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 283US 21322 DURING PREFLIGHT, FOUND OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY AND POWER SUPPLY, CHECKED OK. 2 L 7 3 4F A3WE 1996062000353 19960620 00353 WP 1996 6 20 9613321141 1 19960615 A 5270 CABLES DOUG DC10 DC1040 3023508 WP DOOR 1L WORN A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 141US 46750 DURING TAKEOFF, DOOR 1L ANNUNCIATOR LIGHT ILLUMINATED, ABORTED TAKEOFF. MAINTENANCE REPLACED BOTH TRANSLATOR CABLES. 2 L 7 3 4F A22WE 1996062000354 19960620 00354 WP 1996 6 20 96138289855 1 19960614 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 764NC 47717 DURING LINE CHECK, FOUND EMERGENCY ESCAPE EXIT SIGNS FOR OVERWING EXITS AT ROW 16 INOPERATIVE. REPLACED BATTERIES, OPER ATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996062000355 19960620 00355 NM 1996 6 20 96FDEA01106 1 19960612 A 5311 691N00065 FRAME BOEING 727 727225 1384077 NM BS 1148 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 467FE 21449 NR0132 AND 004, CRACKED FRAME AROUND NUTPLATE HOLE AT BS 1148 LBL 28 WL 160. *S/D* REMOVED DAMAGED AREA IN FRAME AT BS 114B LBL 28, WL 160, FABRICATED REPAIR PARTS AND INSTALLED IAW FED EX SRM 51-40-2. 2 L 7 3 4F A3WE 1996062000356 19960620 00356 NM 1996 6 20 96FDEA01128 1 19960614 A 5320 651768412 SHEAR TIE BOEING 727 727225 1384077 NM BS 303 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 NR0645 AND 031, WHILE WORKING NRO348 AFTER REMOVAL OF RT LWR NOSE CHORD FOUND SHEAR TIE AT BS 303 WL 148 RBL 15 TO 19 TO BE CRACKED AND CORRODED AND OUT OF LIMITS PER SRM. 2 L 7 3 4F A3WE 1996062000357 19960620 00357 NM 1996 6 20 96FDEA01129 1 19960614 A 5311 651633913 FRAME BOEING 727 727225 1384077 NM BS 970 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 NR0312 AND 032, CORROSION (53-111-01) STA 970, LBL 24 ON TOP FLANGE OF FRAME UNDER STRAP. *S/D* REPAIRED FRAME AT BS 9 70 WL 147 RBL 24 PER FEDEX SRM 51-40-3. 2 L 7 3 4F A3WE 1996062000358 19960620 00358 NM 1996 6 20 96FDEA01130 1 19960614 A 5315 652082724 FLOOR BEAM BOEING 727 727225 1384077 NM BS 560 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 NR0476 AND 033, CORROSION (53-111-01, -2) ON FLOOR BEAM STA 560 LBL 18 WL 198, FWD CARGO BAY. 2 L 7 3 4F A3WE 1996062000359 19960620 00359 NM 1996 6 20 96FDEA01131 1 19960613 A 5312 651596911 BULKHEAD FTG BOEING 727 727225 1384077 NM BS 740 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 NR0090 AND 043, CRACK IN FLANGE OF 740 FORGING LT SIDE FROM STR 19 TO STR 21. *S/D* REMOVED AND REPLACED LT BS 740 BUL KHEAD FITTING IAW FEDEX EA 7-5310-29140. 2 L 7 3 4F A3WE 1996062000360 19960620 00360 NM 1996 6 20 96FDEA01132 1 19960614 A 5313 65562364 STRINGER BOEING 727 727173C 1384059 NM BS 680-700 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 199FE 19509 NR 0032 AND 010. CORROSION (C53-113-10-1) ON STRINGER 26L, BS 680 TO BS 700. REMOVED CORRODED STR 26L, BS 668 - BS 740 . INSTALLED REPAIR STR SECTION IAW FEDEX SRM 53-10-3. 2 L 7 3 4F A3WE 1996062000361 19960620 00361 NM 1996 6 20 96FDEA01133 1 19960614 A 5320 692045B SHEAR TIE BOEING 727 727225 1384077 NM BS 1148 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 467FE 21449 CORROSION (C53-113-10, -2) ON FRAME WEB AND SHEAR TIE AT BS 1148, RBL 1 TO 5 AT WL 150. *S/D* REPAIRED FRAME WEB AND S HEAR TIE AFT AND FWD SIDE AT BS 1148 LBL 1 TO 5 WL 150 IAW FEDEX SRM 53-10-4. 2 L 7 3 4F A3WE 1996062000362 19960620 00362 NM 1996 6 20 96FDEA01134 1 19960614 A 5320 692045B SHEAR TIE BOEING 727 727225 1384077 NM BS 1148 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 467FE 21449 CORROSION (C53-113-10, -2) ON FRAME WEB AND SHEAR TIE AT BS 1148, RBL 9 AT WL 150. *S/D* REPAIRED FRAME WEB AND SHEAR TIE AT BS 1148 RBL 9 WL 150 IAW FEDEX SRM 53-10-4. 2 L 7 3 4F A3WE 1996062000363 19960620 00363 NM 1996 6 20 96FDEA01135 1 19960614 A 5320 692032916 SHEAR TIE BOEING 727 727225 1384077 NM BS 1148 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 467FE 21449 NR0162 007, CORROSION (C53-113-10, -2) ON FRAME WEB AND SHEAR TIE AT BS 1148 RBL 7 TO 13 AT WL 150. 2 L 7 3 4F A3WE 1996062000364 19960620 00364 NM 1996 6 20 96FDEA01136 1 19960614 A 5320 6516347 SHEAR TIE BOEING 727 727225 1384077 NM BS 1130 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 467FE 21449 NR0157 008, CORROSION (C53-113-10, -2) ON FRAME WEB AND SHEAR TIE AT BS 1130, RBL 4 TO 1 AT WL 147. 2 L 7 3 4F A3WE 1996062000365 19960620 00365 WP 1996 6 20 96FDEA01137 1 19960614 A 5720 I BEAM DOUG DC10 DC1010 3022110 WP LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 46705 NR5046, LEFT WING AFT I BEAM DIRECTLY BELOW AND 20 I/B NR 1 SPOILER, EXHIBITS HEAVY INTERGRANDLAR CORROSION. 2 L 7 3 4F A22WE 1996062000366 19960620 00366 NM 1996 6 20 96UAL900456 1 19960617 A 3350 900542U1 BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE BS 800 DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7462U 21916 LT WING AFT EMERGENCY LIGHT IS INOPERATIVE. *S/D* LIGHT INOPERATIVE. REPLACED BATTERY PACK, SYSTEM CHECKS OKAY. 2 L 7 3 4F 4 F A3WE E2EA 1996062000367 19960620 00367 NM 1996 6 20 96UAL900457 1 19960617 A 5610 WINDOW BOEING 141T48354 BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT COCKPIT DEFECTIVE A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 644UA 2708 25094 AIRCRAFT RETURNED TO FIELD DUE TO FIRST OFFICER WINDOW LEAK. *S/D* UPDATE A DEFECTIVE FIRST OFFICER WINDOW CAUSED THE A IR LEAK. REPLACED WINDOW AND PRESSURIZED AIRCRAFT, NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A1NM E24NE 1996062000369 19960620 00369 NM 1996 6 20 CALA9600828 1 19960612 A 5311 FRAME BOEING 727 727243 138408D NM BS 169.8/211.5 DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 578PE 21661 INSPECTION FOUND IMPACT DAMAGE TO FRAMES AT STA 169.8 AND 211.5, WL 170. THE FRAMES WERE REPAIRED IAW SRM 51-40-4, FIGU RE 3. 2 L 7 3 4F RT A3WE 1996062000370 19960620 00370 WP 1996 6 20 CALA9600829 1 19960609 A 5210 INTERCOSTAL DOUG DC9 DC981 3022081 WP PAX CABIN DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13881 48045 INSPECTION FOUND A 1 INCH CRACK IN RADIUS OF MAIN CABIN DOOR INTERCOSTAL. THE CRACK WAS LOCATED AFT OF HANDLE TORQUE SH AFT. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1996062000371 19960620 00371 WP 1996 6 20 CALA9600830 1 19960605 A 5311 FRAME DOUG DC9 DC981 3022081 WP BS 1463 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13881 48045 INSPECTION FOUND A 6 INCH CRACK IN CANTED BELT FRAME AT STA 1463, LONGERON 2L. A REPAIR DOUBLER WAS INSTALLED IAW SRM 5 3-01. 2 L 7 2 4F A6WE 1996062000372 19960620 00372 WP 1996 6 20 CALA9600831 1 19960530 A 5755 5936838503 SUPPORT DOUG DC9 DC981 3022081 WP GRD SPOILER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13881 48045 INSPECTION FOUND A 1 INCH CRACK AT FORWARD ATTACH FASTENER OF RT GROUND SPOILER O/B CROSS BRACE SUPPORT. A CROSS BRACE WAS INSTALLED IAW ECRA 5710-01733. 2 L 7 2 4F A6WE 1996062000373 19960620 00373 WP 1996 6 20 CALA9600832 1 19960528 A 5320 DOUBLER DOUG DC9 DC981 3022081 WP BS 100 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13881 48045 INSPECTION FOUND A .1875 INCH CRACK IN DOUBLER AT NOSE WHEEL WELL LEFT AFT DOOR AFT HINGE CUTOUT, STA 100. A DOUBLER WA S INSTALLED IAW SRM 53-05, FIGURE 62. 2 L 7 2 4F A6WE 1996062000374 19960620 00374 WP 1996 6 20 CALA9600833 1 19960531 A 5320 FLR SUPPORT DOUG DC9 DC981 3022081 WP FWD ENTRY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13881 48045 INSPECTION FOUND FLOOR SUPPORT CORRODED AT FORWARD ENTRY PANEL F. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51 -30-2. 2 L 7 2 4F A6WE 1996062000375 19960620 00375 WP 1996 6 20 CALA9600834 1 19960530 A 5240 DOOR PAN DOUG DC9 DC981 3022081 WP SERVICE DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13881 48045 INSPECTION FOUND FORWARD SERVICE DOOR PAN DENTED AT BAYONET FITTING. A DOUBLER WAS FABRICATED AND INSTALLED AND DOOR ST OP WAS REPLACED IAW SRM 53-05, FIGURE 42. 2 L 7 2 4F A6WE 1996062000376 19960620 00376 WP 1996 6 20 CALA9600835 1 19960531 A 5320 ANGLE DOUG DC9 DC981 3022081 WP BS 984-1003 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13881 48045 INSPECTION FOUND A 1.5 INCH CRACK IN LOWER RADIUS OF EXTERNAL ANGLE AT STA 984 TO 1003, LONGERON 20L. THE AREA WAS REPA IRED IAW ECRA 5310-03277 AND SRM 53-02. 2 L 7 2 4F A6WE 1996062000377 19960620 00377 WP 1996 6 20 CALA9600836 1 19960531 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP BS 148-200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13881 48045 INSPECTION FOUND FLOOR SUPPORT CORRODED AT FORWARD ENTRY BETWEEN PANELS G AND H, STA 148 TO 200. A NEW SUPPORT WAS FABR ICATED AND INSTALLED IAW SRM 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 1996062000378 19960620 00378 WP 1996 6 20 CALA9600837 1 19960531 A 5320 FLOOR SUPPORT DOUG DC9 DC981 3022081 WP BS 718 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13881 48045 INSPECTION FOUND FLOOR SUPPORT AT STA 718 CORRODED AROUND NUTPLATE. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1996062000379 19960620 00379 NM 1996 6 20 CALA9600838 1 19960615 A 5315 FLOOR BEAM BOEING 727 727232 1384082 NM BS 1130/1148 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND FLOOR BEAM CORRODED AT CEILING OF AFT CARGO COMPARTMENT, STA 1130 AND 1148, RT SIDE OF AIRCRAFT. THE F LOOR BEAM WAS REPAIRED IAW ECRA 5310-03288. 2 L 7 3 4F A3WE 1996062000380 19960620 00380 WP 1996 6 20 CALA9600839 1 19960617 A 3320 0398020 BALLAST DOUG DC9 DC982 3022082 WP CABIN OVERHEATED A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 09 10801 49127 CREW CALLED MAINTENANCE WHILE AIRCRAFT WAS AT GATE, STATING THEY SMELLED SMOKE IN THE CABIN. MAINTENANCE FOUND THAT A L IGHT BALLAST ABOVE ROW 19 DEF HAD GOTTEN HOT AND SCORCHED THE OVERHEAD BIN. ALSO, THE PSU CENTER LIGHTING CIRCUIT BREAK ER IN THE COCKPIT WAS FOUND POPPED. MAINTENANCE FOUND THAT A WIRE RUNNING ABOVE THE SAME OVERHEAD BIN HAD GROUNDED. TH E BALLAST WAS REPLACED. ALSO, THE ADJACENT BALLAST WAS REPLACED AS A PRECAUTIONARY MEASURE. THE OVERHEAD BIN WAS PULLE D DOWN AND THE CHARRED WIRING WAS REPLACED AND THE INSULATION WAS REPAIRED. 2 L 7 2 4F A6WE 1996062000381 19960620 00381 WP 1996 6 20 CALA9600840 1 19960616 A 2530 8101220000B OVEN DOUG DC9 DC982 3022082 WP FWD GALLEY CONTAMINATED A CALA F H ACTIVATE FIRE EXT. DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 76823 49483 THE FLIGHT ATTENDANT SAW SMOKE COMING FROM RT OVEN IN FORWARD GALLEY WHILE IN FLIGHT. THE SMOKE CEASED AFTER USING A HA LON AND WATER FIRE EXTINGUISHER AND PULLING THE CIRCUIT BREAKERS FOR THE RIGHT AND LEFT FORWARD OVENS. THE FLIGHT WAS C ONTINUED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND MELTED PLASTIC ON THE HEATING ELEMENTS AND FAN OF THE RT OVEN IN T HE FORWARD GALLEY. THE OVEN WAS REMOVED AND REPLACED, OPERATION OF THE OVEN CHECKED NORMAL. THE HALON AND WATER FIRE E XTINGUISHERS WERE REPLACED. 2 L 7 2 4F A6WE 1996062000382 19960620 00382 SO 1996 6 20 COMA9610183 1 19960617 A 2931 M8372382K204IN CONNECTOR EMB 120 EMB120RT SO LT ENGINE DEFECTIVE A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 159A 120159 LEFT ENGINE LOW HYDRAULIC PRESSURE WARNING DURING CLIMB. REPAIRED WIRING CONNECTOR JO807 IN LT ENGINE NACELLE. 2 L 7 2 4T RT A31SO 1996062000383 19960620 00383 NE 1996 6 20 COMA9630127 2 19960617 A 7250 4074T58P09 O-RING SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LT ENGINE LEAKING A COMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 344CA 340A025 367159 LEFT ENGINE LOW OIL PRESSURE WARNING CAME ON, PRESSURE GAUGE INDICATED 30 PSI. REPLACED THE POWER TURBINE C-SUMP O-RING SEAL. 2 L 7 2 4T 4 T RT A52EU E8NE6 1996062000384 19960620 00384 EU 1996 6 20 COMA9630128 1 19960617 A 2612 72111211000 SMOKE DETECTOR SAAB SF340 SF340A 7850100 EU CARGO MALFUNCTIONED A COMA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SO 01 343CA 340A024 CARGO FIRE LIGHT CAME ON DURING FLIGHT. DISCHARGED FIRE EXTINGUISHER AND FIRE LIGHT WENT OUT. INSPECTED CARGO AREA AND FOUND NO EVIDENCE OF SMOKE OR FIRE. REPLACED THE SMOKE DETECTOR AND FIRE BOTTLE. 2 L 7 2 4T RT A52EU 1996062000385 19960620 00385 EA 1996 6 20 COMA9660108 1 19960617 A 3232 600751363 ACTUATOR CNDAIR CL600 CL6002B19 EA NLG DOOR LEAKING A COMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 918CA 7018 THUMPING NOISE HEARD FROM NLG AREA WHEN LANDING GEAR RETRACTED. REPLACED LEAKING NLG DOOR ACTUATOR. 2 L 7 2 4F RT A21EA 1996062000386 19960620 00386 NM 1996 6 20 DL72K961455 1 19960614 A 5753 6519270 ANTI-FRET STRIPS BOEING 727 727232 1384082 NM TE FLAP TRACK WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 481DA 20861 DURING INSPECTION, FOUND THE MICARTA ANTI FRETSTRIP FOR THE RIGHT WING INBD T/E FLAP, I/B TRACK WORN. REPLACED STRIP IN ACCORDANCE WITH AD 90-07-05. 2 L 7 3 4F A3WE 1996062000387 19960620 00387 NM 1996 6 20 DL72P961428 1 19960614 A 5754 651622187 SLAT BOEING 727 727225 1384077 NM LT WING GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 INNER TAI SKIN GOUGED. REMOVED DAMAGE AND REPAIRED PER M/M 57-54-0 FIG 803A. 2 L 7 3 4F A3WE 1996062000388 19960620 00388 NM 1996 6 20 DL72P961429 1 19960614 A 5753 651622187 SLAT BOEING 727 727225 1384077 NM LT WING WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 OUTER SKIN WORN ALONG FENCE CONTACT AREA. REPAIRED PER M/M 57-54-0 FIG 813. 2 L 7 3 4F A3WE 1996062000389 19960620 00389 NM 1996 6 20 DL72P961430 1 19960614 A 5754 651622187 SKIN BOEING 727 727225 1384077 NM LT LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 SKIN CRACKED AT LOWER FENCE ATTACH HOLE. REPAIRED SKIN PER M/M 57-54-0 FIG 813. 2 L 7 3 4F A3WE 1996062000390 19960620 00390 NM 1996 6 20 DL72P961431 1 19960614 A 5754 651622187 SKIN BOEING 727 727225 1384077 NM LT TE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 SKIN CRACKED AT UPPER TWO FWD FENCE ATTACH HOLES. REPAIRED PER M/M 57-54-0 FIG 813. 2 L 7 3 4F A3WE 1996062000391 19960620 00391 NM 1996 6 20 DL72S961422 1 19960612 A 5743 TRUNNION FITTING BOEING 727 727232 1384082 NM RT MLG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 523DA 21583 FOUND CORROSION ON THE INNER FACE OF THE FWD TRUNNION BEARING SUPPORT FITTING ON THE RT MLG. REPAIRED PER MM 57-43-0. 2 L 7 3 4F A3WE 1996062000392 19960620 00392 NM 1996 6 20 DL72S961423 1 19960614 A 5320 TQ BOX WEB BOEING 727 727232 1384082 NM BS 1223 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 525DA 21585 DURING INSPECTION, FOUND TWO, .5 CRACKS IN LT FWD TORQUE BOX WEB AT UPPER CHORD ATTACH POINT STA 122. REPAIRED PER M/M 53-11-0. 2 L 7 3 4F A3WE 1996062000393 19960620 00393 NM 1996 6 20 DL72S961425 1 19960612 A 2910 SWIVEL BOEING 727 727232 1384082 NM LE SLAT ACTUATOR LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 407DA 21151 DURING CLIMB, A-HYD QTY WENT TO ZERO AND A PUMP LIGHT FLICKERED, RETURNED TO SHV. REPLACED CASE DRAIN FILTERS, NO METAL FOUND. FOUND THE NR 4 SLAT ACTUATOR SWIVEL LEAKING. REPLACED O-RING, REFILLED HYD SYS, RAN ENGINES AND B-PUMPS, OPERA TED ALL FLT CONTROLS TO REMOVE AIR FROM HYD SYS AND SERVICED TO FULL, NO LEAKS NOTED. 2 L 7 3 4F A3WE 1996062000394 19960620 00394 NM 1996 6 20 DL72S961432 1 19960614 A 3260 PROX SENSOR BOEING 727 727232 1384082 NM LT MLG MALFUNCTIONED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 484DA 20864 ON T/O WITH GEAR RETRACTED, HANDLE IN UP POSITION, GOT LT MAIN GEAR RED UNSAFE LIGHT. REPLACED LT MAIN GEAR UP PROX SEN SOR. ALSO, AS A PRECAUTIONARY REPLACED LDG MOD. 2 L 7 3 4F A3WE 1996062000395 19960620 00395 NM 1996 6 20 DL72S961439 1 19960615 A 2910 65178494061 LINE BOEING 727 727232 1384082 NM B-HYDRAULIC SYST BROKEN A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 525DA 21585 THE B-SYS HYD FAILURE IN FLT, RETURNED SLC. FOUND B-SYS PRESS LINE FROM PUMP TO B-PRESS MOD BROKEN. REPLACED LINE, BOT H HYD B-PUMPS AND FILTERS. 2 L 7 3 4F A3WE 1996062000396 19960620 00396 NM 1996 6 20 DL72S961453 1 19960616 A 5330 65C54583 SKIN BOEING 727 727232 1384082 NM BS 1030 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 523DA 21583 DURING INSPECTION, FOUND FUSELAGE SKIN BULGED AT STATION 1030, STRINGER 28R. REPAIRED IN ACCORDANCE WITH B727 SRM 53-30 -3, FIG 1. 2 L 7 3 4F A3WE 1996062000397 19960620 00397 NM 1996 6 20 DL72S961454 1 19960611 A 5230 SKIN BOEING 727 727232 1384082 NM C3 DOOR DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 523DA 21583 FOUND A DEEP, SHARP RADIUS DENT AND GOUGE IN THE C-3 DOOR EXTERIOR SKIN APPROX 15 INCHES LONG, 8 INCHES ABOVE THE HANDLE CUTOUT. REPAIRED PER SRM 52-00-3, FIG 3. 2 L 7 3 4F A3WE 1996062000398 19960620 00398 NM 1996 6 20 DL72W961427 1 19960614 A 2150 1843601 HEAT EXCHANGERS BOEING 727 727247 138408F NM LEFT AND RIGHT LEAKING A DALA B EMER. DESCENT O OTHER CR CRUISE 1 SO 27 297WA 22534 AT 25,000 FT ENG'S AT IDLE, ENG ANTI-ICE ON, LOST CONTROL OF CABIN PRESSURIZATION. DURING EMERGENCY DECENT CABIN CLIMBE D TO 12,000 FT. FOUND BOTH LEFT AND RIGHT HEAT EXCHANGERS LEAKING THROUGH CORE. REPLACED BOTH EXCHANGERS, LEAK AND PRE SSURIZATION CHECKS GOOD. 2 L 7 3 4F A3WE 1996062000399 19960620 00399 NM 1996 6 20 DL72W961435 1 19960614 A 5754 ANGLE BOEING 727 727247 138408F NM NR 6 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 294WA 22112 NR 6 SLAT LOWER COVE SKIN ANGLE CRACKED 1.5 INCH INBD OF ACTUATOR. REPAIRED PER M/M 57-54-0. 2 L 7 3 4F A3WE 1996062000400 19960620 00400 NM 1996 6 20 DL72W961452 1 19960615 A 5320 651751737 CHANNEL BOEING 727 727247 138408F NM BS 1263 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 294WA 22112 DURING INSPECTION, FOUND CHANNEL AT FS 1263 TORQUE BOX CRACKED. CRACK LENGTH WAS APPROXIMATELY 1.5 INCH. REPLACED CHAN NEL PER AD 94-07-08 AND B727 S/B 53-0129, R 4. 2 L 7 3 4F A3WE 1996062000401 19960620 00401 NM 1996 6 20 DL73S961384 1 19960608 A 3260 GPWS BOEING 737 737232 1384475 NM FWD ELECT COMPT INOPERATIVE A DALA L ABORTED APPROACH N FALSE WARNING LD LANDING 1 SO 27 325DL 23097 UPON GEAR EXTENSION GOT ALL THREE GREEN GEAR DOWN LIGHTS. AT 200 AGL THE GPWS 'GEAR UNSAFE MODE' SOUNDED AND THREE RED UNSAFE LIGHTS ILLUMINATED. MISSED APPROACH AND VISUALLY CHECKED GEAR DOWN. NO GPWS SOUNDED ON THE RUNWAY. REPLACED LA NDING GEAR ACCESS UNIT AND GPWS COMPUTER. CHECKED PER M/M 32-09-00, LANDING GEAR WARNING CHECKS OK. 2 L 7 2 4F RT A16WE 1996062000402 19960620 00402 WP 1996 6 20 MWEA96163 1 19960614 A 5320 2024T3 FRAME DOUG DC9 DC932 3022066 WP VENTRAL STAIR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 DURING CERT INSP, FOUND HEAVY CORROSION AT THE BOTTOM OF CANTED FRAME AND AREA SKIN OF LT VENTRAL STAIR JAMB AT STA 1143 . SPLICED IN A SECTION OF REPAIR ANGLE IAW SRM 53-11-4 FIG 5. 2 L 7 2 4F A6WE 1996062000403 19960620 00403 WP 1996 6 20 MWEA96164 1 19960614 A 5320 VENT HOLE DOUG DC9 DC932 3022066 WP BS 945 NOT PLUGGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 DURING CERT MAINTENANCE, VENT HOLE REMAINED AFTER REMOVAL OF AFT GALLEY AT FS 945. REMOVED EXISTING GALLEY VENT AND INS TALLED A PERMANENT REPAIR IAW SRM 53-04, FIG 38. 2 L 7 2 4F A6WE 1996062000404 19960620 00404 WP 1996 6 20 MWEA96165 1 19960614 A 5330 VENT HOLE DOUG DC9 DC932 3022066 WP BS 945 NOT PLUGGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 DURING CERT MAINTENANCE, VENT HOLE REMAINED AFTER REMOVAL OF AFT GALLEY AT FS 945. REMOVED EXISTING GALLEY VENT AND INS TALLED A PERMANENT REPAIR IAW SRM 53-04, FIG 38. 2 L 7 2 4F A6WE 1996062000405 19960620 00405 WP 1996 6 20 MWEA96166 1 19960614 A 5315 FLOOR BEAM DOUG DC9 DC932 3022066 WP BS 229 CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 DURING CERT INSP, A CABIN FLOOR BEAM WAS FOUND CHAFED AT STA 229 UNDER THE LT CENTER FLOOR BOARD. REPAIRED THE FLOOR BE AM IAW 53-05, FIG 20. 2 L 7 2 4F A6WE 1996062000406 19960620 00406 WP 1996 6 20 MWEA96167 1 19960614 A 5315 FLOOR BEAM DOUG DC9 DC932 3022066 WP BS 541 CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 DURING CERT INSP, A CABIN FLOOR BEAM WAS FOUND CHAFED AT STA 541 UNDER LT CENTER FLOORBOARD. REPAIRED THE FLOOR BEAM IA W SRM 53-05, FIG 20. 2 L 7 2 4F A6WE 1996062000407 19960620 00407 WP 1996 6 20 MWEA96168 1 19960614 A 5230 DOOR PAN DOUG DC9 DC932 3022066 WP AFT CARGO DOOR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 57791 DURING CERT INSP, FOUND BOTTOM OF THE AFT CARGO DOOR PAN WITH CORROSION. REPAIRED AFT CARGO DOOR PAN IAW SRM 53-05, FIG 44. 2 L 7 2 4F A6WE 1996062000408 19960620 00408 WP 1996 6 20 MWEA96169 1 19960614 A 5320 99582313 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 908-935 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 DURING CERT INSP, FOUND CORRODED INTERCOSTAL ON UPPER FLANGE IN SEVERAL AREAS AT STA 908 THROUGH 935 LONGERON 29R. REPL ACED INTERCOSTAL IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1996062000409 19960620 00409 WP 1996 6 20 MWEA96170 1 19960614 A 5315 FLOOR BEAM DOUG DC9 DC932 3022066 WP BS 917-965 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 DURING CERT INSP, FOUND CABIN CENTER FLOOR BEAM UPPER CHANNEL WITH MODERATE CORROSION FROM STA 917 TO 965. REPLACED THE SECTION OF FLOOR BEAM IAW SRM 53-01, PG 1 AND 53-11-3, FIG 11. 2 L 7 2 4F A6WE 1996062000410 19960620 00410 WP 1996 6 20 MWEA96171 1 19960614 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 470 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 DURING CERT INSP, REPAIR MOD OF VHF ANTENNA REQUIRES INSTALLATION AT STA 470, LONG 30. INSTALLED PERMANENT REPAIR ON VH F ANTENNA PER SB 53-188 AND SRO 9530005. 2 L 7 2 4F A6WE 1996062000411 19960620 00411 WP 1996 6 20 MWEA96172 1 19960614 A 5312 391016379 BULKHEAD ANGLE DOUG DC9 DC932 3022066 WP BS 996 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 DURING CERT INSP, FOUND AFT CARGO COMPT BULKHEAD ANGLE HAD LIGHT CORRSION ON UNDERSIDE AT STA 996 FROM LONGERONS 25R TO 18R. SPLICED IN A NEW ANGLE IAW THE SRM 53-05, FIG 93. 2 L 7 2 4F A6WE 1996062000412 19960620 00412 NM 1996 6 20 SCNA96180 1 19960615 A 2612 0160007101 FIRE LOOP WIRE BOEING 727 7272J4 1384006 NM NR 3 ENGINE DAMAGED A SCNA A J UNSCHED LANDING DUMP FUEL N FALSE WARNING IN INSP/MAINT 1 GL 15 285SC 21676 THE NUMBER 3 ENGINE FIRE WARNING LIGHT ILLUMINATED AND HORN SOUNDED. PERFORMED ENGINE FIRE/FAILURE CHECKLIST, DECLARED EMERGENCY, DUMPED FUEL TO LANDING WEIGHT AND LANDED. FOUND FRAYED WIRE AT PIN-X OF D400P, REPINNED WIRE AND OPS CHECKS GOOD. 2 L 7 3 4F RT A3WE 1996062000413 19960620 00413 NM 1996 6 20 SCNA96181 1 19960614 A 3350 1000677 LIGHT BOEING 727 727225 1384077 NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 283SC 22559 THE AFT OVERHEAD EMERGENCY LIGHT ASSEMBLY WAS FOUND INOP. REMOVED AND REPLACED THE AFT OVERHEAD EMERGENCY LIGHT ASSEMB LY, OPS CHECK OK. 2 L 7 3 4F A3WE 1996062000414 19960620 00414 NM 1996 6 20 SCNA96182 1 19960611 A 3350 S106 BATTERIES BOEING 727 7272J4 1384006 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 285SC 21676 THE AFT AIRSTAIR OVERHEAD SELF CONTAINED EMERGENCY EXIT LIGHT WAS FOUND INOP. REPLACED BATTERIES AND OPS CHECK OK. 2 L 7 3 4F RT A3WE 1996062000415 19960620 00415 NM 1996 6 20 SWAA960526 1 19960617 A 3397 WIRE BOEING 737 7373H4 1384600 NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 399SW 27693 DURING OVERNIGHT CHECK, FOUND EMERGENCY TRACK LIGHTING INOP BEHIND ROW 6. RECONNECTED WIRING ON TRACK LIGHT. 2 L 7 2 4F RT A16WE 1996062000416 19960620 00416 NM 1996 6 20 SWAA960527 1 19960617 A 2612 FIRE WARNING BOEING 737 7372H4 138448C NM APU ACTIVATED A SWAA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 07 29SW 21340 DIVERTED TO SPS DUE TO APU FIRE WARNING IN FLIGHT. DISCHARGED FIRE BOTTLE. INSPECTED AND FOUND NO EVIDENCE OF FIRE OR OVERHEAT CONDITION. DEFERRED APU FIRE DETECT SYSTEM AND FIRE BOTTLE PER MEL AND CONTINUED. 2 L 7 2 4F A16WE 1996062000417 19960620 00417 NM 1996 6 20 SWAA960528 1 19960616 A 5320 ANGLES BOEING 737 7375H4 138449D NM BS 290 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 514SW 25153 DURING SCHEDULED 1/2 D-CHECK, FOUND ANGLES CRACKED ABOVE S11R AND S12R, BS 290. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996062000418 19960620 00418 NM 1996 6 20 SWAA960529 1 19960616 A 3350 10000679 BASE BOEING 737 7372H4 138448C NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 95SW 23054 DURING OVERNIGHT CHECK, FOUND COCKPIT EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT BASE PER BOEING M/M. 2 L 7 2 4F A16WE 1996062000419 19960620 00419 NM 1996 6 20 SWAA960530 1 19960615 A 4930 FUEL LINE BOEING 737 7372H4 138448C NM APU LEAKING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 80SW 22675 FUEL FUMES NOTED IN CABIN AREA WHILE APU BLEED ON. INSPECTED AND FOUND PRESSURE LINE AT ATOMIZER LEAKING. CONTINUED WI TH APU INOP PER MEL 49-1. 2 L 7 2 4F A16WE 1996062000420 19960620 00420 NM 1996 6 20 SWAA960531 1 19960614 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 847 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 96SW 23055 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN DENTED AT BS 847, AT S7R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000421 19960620 00421 NM 1996 6 20 VNAA9606006 1 19960616 A 3260 870003 PSEU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT AVIONICS RAC DEFECTIVE A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 07 437JS 3055 DURING THE TAKEOFF ROLL AT APPROXIMATELY V1, THE CREW WAS ALERTED BY A TAKEOFF TRIM CONFIGURATION WARNING. CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MX CONTROL ADVISED THE CREW TO CYCLE THE PSEU A AND B-SYSTEM CIRCUIT BREAKERS TO EXTINGUISH THE CAS MESSAGE. CAS MESSAGE EXTINGUISHED, THE CREW THEN CONTINUED ON WITH THE FLIGHT. EN ROUTE THE TAKEOF F TRIM CONFIGURATION WARNING CAS ILLUMINATED AGAIN. CREW CONTINUED ON WITH THE FLIGHT AND LANDED IN PIT WITHOUT FURTHER INCIDENT. PIT MX REPLACED THE PSEU IAW MM 32-60-00, OPS CHECKED GOOD. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996062000445 19960620 00445 WP 1996 6 20 96ZZZM1006 1 19960519 A 3260 D50775 CONNECTOR DOUG DC8 DC8F55 3021928 WP LT/RT MLG SHORTED A CKSA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 809CK 64985 45803 KMIA - LAND GEAR RED UNSAFE LIGHT REMAINS ON AFTER GEAR RETRACTION. CYCLING GEAR NO HELP. FOUND LEFT MAIN SWITCH INOP ALSO FOUND RIGHT MAIN GEAR SWITCH DOOR SWITCH PLUG SHOWING LOW RESISTANCE ACROSS PIN. REPLACED SWITCH ON LEFT SIDE AND PLUG ON RIGHT SIDE. PERFORMED GEAR SWING IAW 32-1-0. CHECKED NORMAL. REFERENCE CKSA96052. 2 L 7 4 4F 4A25 1996062000446 19960620 00446 WP 1996 6 20 96ZZZM1007 1 19960525 A 2570 3716104 COVER DOUG DC8 DC8F54 3021926 WP NLG WW DETACHED A FXLA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 54FA 45637 AFTER TAKEOFF SJU EXPERIENCED RUMBLING NOISE IN NOSE WHEEL WELL. RETURNED TO SJU AND LANDED WITHOUT INCIDENT. INSPECTI ON REVEALED COVER CURTAINS INSIDE NOSE WHEEL WELL WERE DETACHED. SECURED CURTAINS AND RETURNED AIRCRAFT TO SERVICE. (M ) 2 L 7 4 4F 4A25 1996062000447 19960620 00447 CE 1996 6 20 96ZZZM1008 1 19960523 A 3297 WIRE BEECH 1900 1900C 1154161 CE GEAR INDICATION CHAFED A GUUA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 19 198GA UB5 FLT 169 - TPA-MIA - LANDING GEAR INDICATION CIRCUIT BREAKER POPS DURING RETRACTION CYCLED ONLY. REPAIRED CHAFED WIRE UN DER CENTER FLOOR AT PLUG P313. OPS CHECK GOOD ON GEAR SWINGS, OPS CHECK GOOD ON TEST FLIGHT. (M) 2 L 7 2 4T RT A24CE 1996062000448 19960620 00448 NM 1996 6 20 96ZZZM1009 1 19960512 A 5610 001A516A0000205 WINDSHIELD DORNER DO32 DO328100 2996000 NM RT COCKPIT SHATTERED A EQGA O OTHER O OTHER CR CRUISE 1 SW 19 340LS 1371 152 3040 WHILE EN ROUTE FROM CUU TO DFW, THE FLIGHT CREW HEARD A POPPING SOUND AND THE FIRST OFFICERS FRONT WINDSHIELD, OUTER LAY ER SHATTERED. THE AIRCRAFT CONTINUED TO DFW AND LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS FERRIED TO HOT WHERE THE WINDSHIELD WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. DORNIER HAS ISSUED A SERVICE BULLETIN WHICH REPL ACES ALL LIGHT WEIGHT WINDSHIELDS WITH A HEAVIER WINDSHIELD. 2 H 7 2 4T RT A45NM 1996062000449 19960620 00449 EU 1996 6 20 96ZZZM1010 1 19960529 A 7722 HTMASOF2821PW CONNECTOR BAG JETSTM JETSTM3201 1500217 EU RT ENG DIRTY A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 470UE 814 FLT NR 6241 - IAD-PHF - DURING CLIMB, MADE AN UNSCHEDULED LANDING DUE TO RIGHT ENGINE TORQUE AND EGT FLUCTUATED IN FLIGH T. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MX REMOVED AND REPLACED TTL VALVE PLUS CLEANED ZONE 2 CANNON P LUG CONNECTOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. REFERENCE VTZA96206. 2 L 7 2 4T RT A56EU 1996062000450 19960620 00450 NE 1996 6 20 96ZZZM1011 2 19960403 A 8520 ENGINE BEECH 18 D18S 1151004 CE PWA R985 R985AN14B 52008 NE RIGHT CRACKED A GGPA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 01 1827M 8710 1587 A394 JP121391 RIGHT ENGINE OIL LEAK. 1 L 7 2 3R 3 R A765 5E1 1996062000451 19960620 00451 EU 1996 6 20 96ZZZM1012 1 19960521 A 3040 AE5751MK1 TRANSFORMER FOKKER F28 F28MK0100 4990807 EU LT WINDSHIELD FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 885US 11345 MSP - FLT 1140 - WHILE CLIMBING OUT OF MSP, CREW SMELLED AN ODOR OF UNKNOWN ORIGIN. FLIGHT ATTENDANT WAS CALLED TO THE COCKPIT TO VERIFY ODOR. AT THIS TIME, SMOKE WAS SEEN EMITTING FROM THE CENTER WINDSHIELD POST. THE CREW DONNED OXYGEN MASKS AND DECLARED AN EMERGENCY. THEY TURNED OFF THE WINDSHIELD HEAT AND THE SMOKE STOPPED. THE FLIGHT WAS 60 MILES FR OM MSP AND RETURNED TO FIELD LANDING WITHOUT INCIDENT. MX CHECKED WIRING TO LEFT WINDOW AND BENEATH GLARESHIELD AND FOU ND NO EVIDENCE OF SHORTED WIRES. OPERATED SYSTEM, CHECKS OK. MX REPLACED THE FOLLOWING ITEMS PER PRECAUTIONARY MEASURE , LEFT WINDSHIELD TEMP CONTROLLER P/N EAWTC8803-405, LEFT WINDSHIELD TRANSFORMER P/N AE5751MK1. USAAF96050. 2 L 7 2 4F RT 1996062000452 19960620 00452 CE 1996 6 20 96ZZZM970 1 19960411 A 3250 1148201143 BEARING BEECH 1900 1900C 1154161 CE NLG WORN A GLBA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 01 152GL UC152 LAN - CREW REPORTED, THAT LEFT RUDDER PEDAL REQUIRED EXCESSIVE FORCE ON TAKEOFF ROLL. THEY ABORTED THE TAKEOFF AND RETU RNED TO GATE. MAINTENANCE REPLACED MANUAL STEERING BELLCRANK AND ASSOCIATED BEARINGS. OPS CHECK WAS GOOD. REFERENCE G LBA96068. 2 L 7 2 4T RT A24CE 1996062000453 19960620 00453 CE 1996 6 20 96ZZZM971 1 19960411 A 3250 M819341210A010 BUSHING BEECH 1900 1900C 1154161 CE NLG WORN A GLBA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 01 152GL UC152 LAN - CREW REPORTED, THAT LEFT RUDDER PEDAL REQUIRED EXCESSIVE FORCE ON TAKEOFF ROLL. THEY ABORTED THE TAKEOFF AND RETU RNED TO GATE. MAINTENANCE REPLACED MANUAL STEERING BELLCRANK AND ASSOCATED BEARINGS. OPS CHECK WAS GOOD. REFERENCE GL BA96068. 2 L 7 2 4T RT A24CE 1996062000454 19960620 00454 CE 1996 6 20 96ZZZM972 1 19960407 A 3260 MS252531 PEDESTAL SWITCH BEECH 1900 1900C 1154161 CE RT MLG OUT OF ADJUST A GLBA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 01 98GL UC98 SPW - CREW REPORTED, THE 'GEAR INTRANSIT' LIGHT REMAINED ILLUMINATED AFTER GEAR WAS SELECTED UP. THEY ELECTED AN AIR TU RN BACK AND MADE AN UNEVENTFUL LANDING. MAINTENANCE REPLACED RIGHT LANDING GEAR UPLOCK SWITCH AND ADJUSTED LEFT POWER L EVER GEAR WARNING PEDESTAL SWITCH. OPS CHECK WAS GOOD. REFERENCE GLBA96066. 2 L 7 2 4T RT A24CE 1996062000455 19960620 00455 NE 1996 6 20 96ZZZM973 2 19960504 A 7250 TURBINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE NR 1 ENGINE DAMAGED A TWAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 CE 05 913TW 49184 MCI - DURING CRUISE, SHUT DOWN NR 1 ENGINE, S/N 3208, DUE TO RAPID DETERIORATION OF ENGINE PARAMETERS. FOUND TURBINE DA MAGE. CHANGED ENGINE. ENGINE OPERATION THEN CHECKED NORMAL. (M) 2 L 7 2 4F 4 F A6WE E9NE 1996062000456 19960620 00456 WP 1996 6 20 96ZZZM974 1 19960505 A 7331 FFR101MK15 FUEL FLOW REG LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122* 54555 NE NR 3 ENG MALFUNCTIONED A TWAA E ENGINE SHUTDOWN O OTHER AP APPROACH 1 CE 05 11004 193B1016 LAX - DURING APPROACH WHEN THROTTLES WERE RETARDED FROM HIGH POWER, NR 3 ENGINE REMAINED AT HIGH POWER REGARDLESS OF THR OTTLE POSITION. SHUT DOWN ENGINE. REMOVED AND REPLACED FUEL FLOW REGULATOR, MFG P/N FFR101MK15. OPERATIONAL CHECK AND ENGINE RUN NORMAL. 2 L 7 3 4F 4 F A23WE A12EU 1996062000457 19960620 00457 WP 1996 6 20 96ZZZM975 1 19960429 A 5320 BOLT DOUG DC9 DC931 3022065 WP BS 737 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 990Z 47136 STL - DURING SPECIAL CHECK, FOUND A 1.5 INCH CRACK AT FRAME ATTACH BOLT, LONGERON L5, STATION 737. REPAIRED PER SRM 53- 02. 2 L 7 2 4F A6WE 1996062000458 19960620 00458 WP 1996 6 20 96ZZZM976 1 19960503 A 5512 SKIN DOUG DC9 DC932 3022066 WP HORIZ STAB CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 996Z 47028 STL - DURING OP-9, FOUND A .25 INCH CRACK ON ONE SIDE AND A .5 INCH CRACK ON OTHER SIDE OF UPPER AFT SKIN PANEL LEFT HOR IZONTAL STABILIZER INBOARD ATTACH HOLE. REPAIRED PER EMLR 66370. 2 L 7 2 4F A6WE 1996062000459 19960620 00459 NM 1996 6 20 96ZZZM977 1 19960508 A 3260 69B475305 A8 LOGIC CARD BOEING 747 747131 1384881 NM LANDING GEAR MALFUNCTIONED A TWAA O OTHER N FALSE WARNING AP APPROACH 1 CE 05 93109 19675 LAX - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, BOTH RED AND GREEN LIGHTS REMAINED ILLUMINATED. CYCLED LANDING GE AR. FOUND LOGIC CARD A8, MFG P/N 69B4753-5, IN LANDING GEAR LOGIC BOX M93, MALFUNCTIONING. REPLACED A8 LOGIC CARD AND LANDING GEAR INDICATION CHECKED NORMAL. (M) 2 L 7 4 4F A20WE 1996062000460 19960620 00460 WP 1996 6 20 96ZZZM978 1 19960508 A 3350 58222 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 926L 47172 DURING CRUISE EMERGENCY EGRESS LIGHTS ILLUMINATED INTERMITTENTLY. REMOVED AND REPLACED POWER SUPPLY, MFG P/N 5822-2. O PERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996062000461 19960620 00461 NM 1996 6 20 96ZZZM979 1 19960515 A 3350 387 LAMP BOEING 727 727225 1384077 NM CABIN FAILED A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8880Z 21453 RIGHT OVERWING EMERGENCY DOOR HAS EXIT LIGHT OUT. REMOVED AND REPLACED LAMPS. OPS CHECK OK. REFERENCE IXKA960034. 2 L 7 3 4F A3WE 1996062000462 19960620 00462 NM 1996 6 20 96ZZZM980 1 19960514 A 3350 317BPE6DL LAMP BOEING 727 727225 1384077 NM CABIN DAMAGED A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 352PA 20616 CATERER DAMAGED 'E' PATH LIGHTING AT ROW 28 DEF. REMOVED AND REPLACED LIGHT LENS ASSY AT 28 DEF 'E' PATH LIGHT. GROUND CHECK OF 'E' LIGHTING OK PER MM 33-50. REFERENCE IXKA960030. 2 L 7 3 4F A3WE 1996062000463 19960620 00463 EU 1996 6 20 96ZZZM981 1 19960516 A 3350 362624 STRIP STBROS SD3 SD360 8100606 EU CABIN BURNED OUT A GUUA K NONE L NO TEST IN INSP/MAINT 1 SO 19 828BE SH3749 FLT 173 - EYW-MIA - EMERGENCY FLOOR LIGHT AT ROW 11 BURNED OUT. REMOVED AND REPLACED EMERGENCY STRIP LIGHT AT ROW 11. O PS CHECK REMOVAL IAW MM CHAPTER 33-22-20. 2 H 7 2 4T A41EU 1996062000464 19960620 00464 EU 1996 6 20 96ZZZM982 1 19960510 A 2750 BRACKET STBROS SD3 SD360 8100606 EU RT TE FLAP LOOSE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 828BE SH3749 ON A PREFLIGHT CREW, FOUND RIGHT INBOARD FLAP SPLIT AND DOES NOT FULLY RETRACT. DOESN'T TRAVEL CORRECTLY. TROUBLE SHOT , FOUND RIGHT INBOARD FLAP CONTROL BRACKET (UPPER) IN CENTER WING SECTION LOOSE. REMOVED BRACKET, INSPECTED FOUND OK. R EINSTALLED BRACKET AND SAFTIED FLAP SYSTEM OPS CHECK NORMAL IAW MM 27-51-00. (M) 2 H 7 2 4T A41EU 1996062000465 19960620 00465 WP 1996 6 20 96ZZZM983 1 19960516 A 3110 BA171 BALLAST DOUG DC8 DC851 3021920 WP RT COCKPIT SHORTED A FXLA B A EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 19 508DC 45935 DURING CRUISE AT FL 350 MIA-DFW, EXPERIENCED SPARK FOLLOWED BY SMOKE ON THE FLIGHT OFFICERS SIDE OF THE COCKPIT. DONNED MASKS AND GOGGLES AND INITIATED EMERGENCY DESCENT INTO MSY. MADE LANDING WITHOUT INCIDENT. GROUND INSPECTION REVEALED GLARESHIELD LIGHT BALLAST BURNED OUT. PULLED AND COLLARED CIRUIT BREAKER FOR LIGHT AND PLACED ON DEFERRED MAINTENANCE ITEM. AIRCRAFT RELEASED FOR SERVICE PER MEL. UPON ARRIVAL AT MAINTENANCE BASE THE GLARESHIELD LIGHT BALLAST WAS REPLAC ED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4A25 1996062000466 19960620 00466 NM 1996 6 20 96ZZZM984 1 19960510 A 3350 81 LAMPS BOEING 737 7372T4 1384492 NM EXTERIOR FAILED A SPAA K NONE L NO TEST IN INSP/MAINT 1 WP 07 703S 22529 DURING SCHEDULED CHECK, FOUND LEFT LOWER AFT AND UPPER AFT EXTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE. LAMPS WERE REPLA CED AT EACH LOCATION. SUBSEQUENT OPERATIONAL CHECK WAS SATISFACTORY PER BMM 33-51-11. (M) 2 L 7 2 4F A16WE 1996062000467 19960620 00467 WP 1996 6 20 96ZZZM985 1 19960517 A 3220 24085571018 LEVER CVAC 440 440 2422902 WP NOSE DRAG STRUT CRACKED A SPAA O OTHER N FALSE WARNING IN INSP/MAINT 1 WP 07 73166 FL032R3 374 DURING GEAR RETRACTION AFTER TAKEOFF FROM DENVER, THE NOSE GEAR DOWN LIGHT AND GEAR INTRANSIT LIGHT REMAINED ON. AFTER SEVERAL UNSUCCESSFUL ATTEMPTS TO RETRACT THE NOSE GEAR, THE AIRCRAFT RETURNED TO DENVER. UPON INSPECTION OF THE NOSE GE AR ASSEMBLY, THE LEVER, A COMPONENT OF THE DOWN LATCH SYSTEM, WAS FOUND CRACKED AT THE FORWARD MOUNT BOLT HOLE. THE LEV ER WAS REPLACED, THE NOSE GEAR RETRACTION AND EXTENSION SYSTEM WAS OPERATIONALLY CHECKED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4R 6A6 1996062000468 19960620 00468 CE 1996 6 20 96ZZZM986 1 19960522 A 3230 1514818 DRIVE GEAR 958100175 BEECH 58 58 1152740 CE LANDING GEAR STRIPPED A BQTA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 NE 05 577W 10695 TH375 UPON LANDING GEAR ACTUATION, LANDING GEAR CYCLE SLOWER THAN NORMAL AND GRINDING NOISE HEARD. UPON REMOVED OF LANDING GE AR MOTOR, P/N 1514818, STRIPPED OF ALL TEETH EXCEPT FOR 2 OR 3 TEETH REMAINING. 1 L 7 2 3O 3A16 1996062000469 19960620 00469 WP 1996 6 20 96ZZZM987 1 19960509 A 3230 RETRACT MECH DOUG DC9 DC932 3022066 WP NLG LACK OF LUBE A VJ6A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 966VV 47168 ON TAKEOFF WHEN GEAR WAS RAISED, MAIN GEARS CAME UP NORMALLY, NOSE GEAR STAYED DOWN AND LOCKED (GREEN) WITH THE RED NOSE GEAR UNSAFE LIGHT AND GEAR DOOR LIGHT OUT. RECYCLED DOWN NORMAL GEAR DOWN AND LOCKED RAISED GEAR AGAIN W/SAME RESULTS. LOWERED GEAR AND RETURNED FOR LANDING. VISUALLY INSPECTED NLG DRAG BRACES TRUNNION FITTINGS, SUPPORT BULKHEAD LT/RT O VERCTR DOWN LOCK ACTUATOR TORQUE LINKS NO DISCREPANCIES NOTED, JACKED A/C PER VJ WC 0005 AND LUBRICATED NLG FITTINGS PER VJ WC 0223. PERFORMED RET AND EXT CYCLED 5 TIMES AND EXTEND NLG EMERGENCY EXT PER MM 32-30. (M) 2 L 7 2 4F A6WE 1996062000470 19960620 00470 WP 1996 6 20 96ZZZM988 1 19960510 A 3230 BUNGEE CYL DOUG DC9 DC932 3022066 WP LT MLG MALFUNCTIONED A VJ6A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 933VV 47489 AFTER TAKEOFF THE GEAR DOOR OPEN AND LEFT GEAR UNSAFE LIGHT REMAINED ON AFTER RAISING THE GEAR. LOWERED THE GEAR AND GO T AN IMMEDIATE LEFT GREEN, REMAINING TWO LIGHTS ON. REMOVED AND REPLACED GEAR BUNGE CYLINDER PERFROMED LEAK CHECK AND G EAR SWING, OPS CHECK GOOD, NO DEFECTS. (M) 2 L 7 2 4F A6WE 1996062000471 19960620 00471 WP 1996 6 20 96ZZZM989 1 19960512 A 3233 ACTUATOR DOUG DC9 DC932 3022066 WP NLG MALFUNCTIONED A VJ6A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 966VV 47168 ON FLT 404 - ATL-CLT - AIR RETURN, THE NOSE GEAR DID NOT RETRACT AFTER TAKEOFF, LANDED NORMAL. TROUBLE SHOT AND ADJUSTE D DOORS PER DC MM 32-20-0. REMOVED AND REPLACED NOSE GEAR RETRACT CYLINDER PER DC MM 32-32-6. PERFORMED NLG EXTENT, RE TRACT AND EMERGENCY EXTENSION PER DC MM 32-30-0, OPS CHECK NORMAL. (M) 2 L 7 2 4F A6WE 1996062000472 19960620 00472 WP 1996 6 20 96ZZZM990 1 19960509 A 3231 RETRACT MECH DOUG DC9 DC932 3022066 WP NLG DOOR MALFUNCTIONED A VJ6A A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 11 936VV 47397 AFTER RETRACTING LANDING GEAR, THERE WAS A LOUD VIBRATION. UPLATCH CHECK GOOD. VIBRATION AND NOISE INCREASED WITH AIRS PEED. FOUND RIGHT FWD NOSE GEAR DOOR DOWN (DID NOT RETRACT). NO DEFECTS FOUND. FORWARD GEAR UPLOCK AND LOCK NORMAL ON GROUND REF MM 32-20-0. (M) 2 L 7 2 4F A6WE 1996062000473 19960620 00473 1996 6 20 96ZZZM991 4 19960511 A 3421 20852680104 GYRO INDICATOR DOUG DC9 DC932 3022066 WP COCKPIT MALFUNCTIONED A VJ6A A UNSCHED LANDING O OTHER CL CLIMB 1 SO 11 938VV 47442 AIR RETURN RADAR PAINTS ONE LARGE SPOKE AT 10 O'CLOCK POSITION. REPLACED RADAR INDICATOR AND NR 1 VERTICAL GYRO OPS CHE CK GOOD ON GROUND. (M) 2 L 7 2 4F A6WE 1996062000474 19960620 00474 1996 6 20 96ZZZM992 4 19960511 A 3442 25873311 RADAR DOUG DC9 DC932 3022066 WP COCKPIT MALFUNCTIONED A A VJ6A A UNSCHED LANDING O OTHER CL CLIMB 1 SO 11 938VV 47442 AIR RETURN RADAR PAINTS ONE LARGE SPOKE AT 10 O'CLOCK POSITION. REPLACED RADAR INDICATOR AND NR 1 VERTICAL GYRO OPS CHE CK GOOD ON GROUND. (M) 2 L 7 2 4F A6WE 1996062000475 19960620 00475 WP 1996 6 20 96ZZZM993 1 19960516 A 2613 HIGH TEMP LIGHT DOUG DC9 DC932 3022066 WP TAIL COMPT ILLUMINATED A VJ6A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 11 932VV 47451 THE TAIL COMPARTMENT HIGH TEMP LIGHT CAME ON IN FLIGHT. 2 L 7 2 4F A6WE 1996062000476 19960620 00476 WP 1996 6 20 96ZZZM994 1 19960505 A 7722 CONNECTOR DOUG DC9 DC932 3022066 WP NR 2 EGT BROKEN PIN A VJ6A A UNSCHED LANDING O OTHER CL CLIMB 1 SO 11 938VV 47442 FLT 143 - ATL-ATL - AIR RETURN, THE CAPTAIN REPORTED NO INDICATION OF NR 2 EGT GAUGE. REPAIRED BROKEN PIN ON RIGHT EGT CONNECTOR, OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1996062000477 19960620 00477 WP 1996 6 20 96ZZZM995 1 19960516 A 2150 SEAL DOUG DC9 DC932 3022066 WP ACM DUCT LEAKING A VJ6A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 901VJ 47275 ON FLT 642 - ATL-SDF - AIR RETURN, THE TAIL COMPARTMENT HIGH TEMP LIGHT CAME ON IN FLIGHT. REMOVED AND REPLACED LEAKING PERI-SEAL AT DUCT BETWEEN ACM AND FLOW CONTROL VALVE ON RIGHT PACK SYSTEM. OPS CHECK NORMAL PER DC MM 21-20. (M) 2 L 7 2 4F A6WE 1996062000478 19960620 00478 1996 6 20 96ZZZM996 4 19960513 A 3197 WIRE DOUG DC9 DC932 3022066 WP NR 1 ENGINE CHAFED A VJ6A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 11 946VV 47226 ON FLT 157 - ATL-MSY - AIR RETURN, ON CLIMB-OUT BOTH MASTER CAUTION LIGHTS CAME ON INTERMITTENTLY, (FLICKERED DIMLY), NO OTHER INDICATION, ANNUNCIATOR LIGHTS TESTED NORMAL. FOUND WIRE NR E204A18 CHAFED TO NR 1 ENGINE CASE, REPAIRED WIRE PE R DC MM 20 STANDARD WIRING PRACTICE, OPS CHECK GOOD PER DC MM 79-33. (M) 2 L 7 2 4F A6WE 1996062000479 19960620 00479 WP 1996 6 20 96ZZZM997 1 19960422 A 2131 10256852 CONTROLLER DOUG DC9 DC932 3022066 WP CABIN MALFUNCTIONED A A VJ6A B I EMER. DESCENT CABIN DEPRESSURIZATION J WARNING INDICATION CR CRUISE 1 SO 11 911VV 47285 ON FLT 230 - DFW-ATL - THE CABIN ALTITUDE ROSE TO 12000 FEET AND WAS UNCONTROLLABLE AT FLIGHT LEVEL 330 FEET, INITIATED EMERGENCY DESCENT. THE FLIGHT HAD BEEN IN PRECIPITATION AT 33000 FEET FOR APPROXIMATELY 30 MINUTES, CABIN ALTITUDE CONT ROL WAS REGAINED AT 14,000 FEET. PRESSURIZED THE AIRCRAFT TO 7.5 PSI AND HELD FOR 15 MINUTES. OPS CHECKED NORMAL, REMO VED AND REPLACED PRESSURE CONTROLLER, PRECAUTIONARY. (M) 2 L 7 2 4F A6WE 1996062000480 19960620 00480 WP 1996 6 20 96ZZZM998 1 19960422 A 3520 OXYGEN LINE DOUG DC9 DC932 3022066 WP CABIN LOOSE A VJ6A B I EMER. DESCENT CABIN DEPRESSURIZATION J WARNING INDICATION CR CRUISE 1 SO 11 911VV 47285 ON FLT 230 - DFW-ATL - THE CABIN OXYGEN SYSTEM MANUALLY SURGED, OXYGEN MASKS DOORS DID NOT OPEN. CONNECTED SUPPLY LINE TO AFT FLIGHT ATTENDANT PSU AND OPERATED CABIN OXYGEN SYSTEM, ALL PSU DOORS DROPPED, OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996062000482 19960620 00482 WP 1996 6 20 AALA960739 1 19960507 A 3397 WIRE DOUG DC9 DC982 3022082 WP R1 DOOR BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 287AA 49299 ORD - DURING OVERNIGHT CHECK, R1 DOOR EMERGENCY LIGHT INOPERATIVE. REPAIRED BROKEN EMERGENCY LIGHT WIRE AT R1 DOOR. SY STEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996062000483 19960620 00483 WP 1996 6 20 ASAA960118 1 19960517 A 5210 4928806501 HOLD OPEN HOOK DOUG DC9 DC982 3022082 WP L1 DOOR BENT A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 934AS 49235 SEA - PRIOR TO DEPARTURE OF FLIGHT 330, CREW REPORTED THE L1 DOOR BINDS WHEN CLOSING. FOUND THE L1 DOOR HOLD OPEN HOOK BENT, REPLACED THE HOLD OPEN HOOK AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996062000484 19960620 00484 NM 1996 6 20 ASAA9610063 1 19960516 A 3350 20131A BATTERY BOEING 737 737298C 1384490 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 ANC - FLT 22 - DURING CREW PRE-FLIGHT, THE CREW REPORTED THAT THE EMERGENCY EXIT FLOOR TRACK LIGHTS ILLUMINATED AND WOUL D NOT EXTINGUISH. MAINTENANCE REPLACED BATTERY, RECEIVER, AND BULBS. LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996062000485 19960620 00485 NM 1996 6 20 ASAA9610064 1 19960519 A 3350 86210151 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT PALLET 9-6. REPLA CED BATTERY AT PALLET 9-6 AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996062000486 19960620 00486 NM 1996 6 20 ASAA9640040 1 19960514 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 763AS 25100 LAS - FLIGHT 621 - DURING CREW PREFLIGHT, THE FORWARD TWO RED EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERA TIVE. RECONNECTED TRACK LIGHT WIRES AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996062000487 19960620 00487 NM 1996 6 20 ASAA9640041 1 19960518 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 771AS 25104 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 15-18. RECONNECTED LIGHTS AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996062000488 19960620 00488 1996 6 20 ASAA9680116 4 19960512 A 2565 D37013115 INFLATION BOTTLE DOUG DC9 DC983 3022083 WP L1 DOOR LOW PRESSURE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 SEA - DURING MAINTENANCE CHECK, THE L1 DOOR EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. REPLACE D THE L1 DOOR EMERGENCY EVACUATION SLIDE. (M) 2 L 7 2 4F RT A6WE 1996062000489 19960620 00489 WP 1996 6 20 ASAA9680117 1 19960515 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 953AS 49386 SFO - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT NEON CHARGE LAMP DID NOT ILLUMINATE WITH SWITCH IN THE ARMED POSITION. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996062000490 19960620 00490 WP 1996 6 20 ASAA9680119 1 19960518 A 5210 MECHANISM DOUG DC9 DC982 3022082 WP L1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 934AS 49235 LAX - DURING MAINTENANCE CHECK, THE L1 DOOR WAS FOUND TO OVER ROTATE ON THE OUTBOARD PIVOT OF THE HINGE, AND THE HOLD OP EN HOOK DID NOT CATCH THE PIN. RERIGGED THE L1 DOOR, ADJUSTED THE LATCHING CAM AND HOLD OPEN HOOK ACTUATING ARM AND DOO R OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996062000491 19960620 00491 SW 1996 6 20 BDHA9600 1 19960510 A 3233 2751016003 ACTUATOR SWRNGN SA226 SA226TC 8780404 SW NLG FAILED A BDHA O OTHER J WARNING INDICATION AP APPROACH 1 GL 15 229AM TC305 MOT - FLT 421 - THE NOSE LANDING GEAR FAILED TO EXTEND WITH NORMAL EXTENTION. THE EMERGENCY GEAR SELECTOR WAS PULLED AN D THE AIRCRAFT LANDED WITHOUT INCIDENT. THE LEFT NOSE GEAR ACTUATOR WAS RESEALED AND GEAR RETRACTS WERE NORMAL. (M) 2 L 7 2 4T RT A8SW 1996062000492 19960620 00492 SO 1996 6 20 C2XA96IA116 1 19960509 A 3260 922AA2YA6PZ22 PROX SENSOR EMB 120 EMB120RT SO LT NACELLE FAILED A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 16718 120136 IAH - FLT 3795 - PILOT REPORTED, THAT THE LEFT MAIN GEAR WAS SLOW TO RETRACT. THE AIRCRAFT RETURNED TO THE FIELD WITHOU T FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN GEAR PROXIMITY SENSOR. THE LANDING GEAR SYSTEM OPER ATIONALLY CHECKED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996062000493 19960620 00493 SO 1996 6 20 C2XA96IA117 1 19960510 A 3233 1959500007 ACTUATOR EMB 120 EMB120RT SO LT MLG FAILED A C2XA O OTHER O OTHER CL CLIMB 1 SW 09 16718 120136 IAH - FLT NR 3811 - PILOT REPORTED, THAT THE LEFT MAIN LANDING GEAR WAS SLOW TO RETRACT. MAINTENANCE REMOVED AND REPLAC ED THE LEFT MAIN GEAR RETRACT ACTUATOR. THE LANDING GEAR SYSTEM OPERATIONALLY CHECKED GOOD, AND THE AIRCRAFT WAS APPROV ED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996062000494 19960620 00494 EU 1996 6 20 C2XA96IA118 1 19960514 A 5320 S5367800821602 SUPPORT AEROSP ATR42 ATR42320 8680930 EU FS 39-41 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 34817 152 IAH - DURING C-CHECK INSPECTION, THE RIGHT CREASE BEAM FLOORBOARD ATTACH POINT BETWEEN FRAMES 39 AND 41 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE CREASE BEAM AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996062000495 19960620 00495 EU 1996 6 20 C2XA96IA119 1 19960514 A 2710 S2711009100000 BELLCRANK AEROSP ATR42 ATR42320 8680930 EU LT AILERON RUSTED BEARING A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 34817 152 IAH - DURING C-CHECK INSPECTION, THE LEFT AILERON TRANSITION BELLCRANK ABOVE THE TRIM ACTUATOR WAS FOUND TO HAVE A RUSTE D BEARING. MAINTENANCE REMOVED AND REPLACED THE BELLCRANK AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996062000496 19960620 00496 EU 1996 6 20 C2XA96IA120 1 19960514 A 5320 S536713906288 CORNER AEROSP ATR42 ATR42320 8680930 EU SERV DOOR CUTOUT CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 34817 152 IAH - DURING C-CHECK INSPECTION, THE GALLEY SERVICE DOOR CUTOUT WAS FOUND TO BE CRACKED AT THE AFT LOWER CORNER. MAINTE NANCE REMOVED AND REPLACED THE CORNER ASSEMBLY AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996062000497 19960620 00497 EU 1996 6 20 C2XA96IA121 1 19960514 A 5753 S5751021400200 FITTING AEROSP ATR42 ATR42320 8680930 EU RT TE FLAP WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 34817 152 IAH - DURING C-CHECK INSPECTION, THE RIGHT INBOARD FLAP HINGE FITTING AT RIB NR 5 WAS FOUND TO HAVE PLAY AT THE AFT ATTA CH POINT. MAINTENANCE REMOVED, REPAIRED, AND INSTALLED THE HINGE FITTING PER EC5750-01085 AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996062000498 19960620 00498 EU 1996 6 20 C2XA96IA122 1 19960520 A 5753 S5751021400200 FITTING AEROSP ATR42 ATR42320 8680930 EU LT TE FLAP WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 34817 152 IAH - DURING C-CHECK INSPECTION, THE LEFT INBOARD FLAP HINGE FITTING AT RIB NR 5 WAS FOUND TO HAVE PLAY AT THE AFT ATTAC H POINT. MAINTENANCE REMOVED, REPAIRED, AND REINSTALLED THE HINGE FITTING PER EC5750-01085 AND THE AIRCRAFT WAS RETURNE D TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996062000499 19960620 00499 EU 1996 6 20 C2XA96IA123 1 19960514 A 5320 S53971402275 STIFFENER AEROSP ATR42 ATR42320 8680930 EU FR 27-28 CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 34817 152 IAH - DURING C-CHECK INSPECTION, A FRAME STIFFENER BETWEEN FRAMES 27A AND 28 WAS FOUND TO BE CRACKED ON THE AFT END. MA INTENANCE STOP DRILLED THE CRACK AND INSTALLED A DOUBLER PER ATR SRM 51-70-00 AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996062000500 19960620 00500 EU 1996 6 20 C2XA96IA124 1 19960514 A 5320 S2541004120000 THRESHOLD AEROSP ATR42 ATR42320 8680930 EU LAVATORY DOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 34817 152 IAH - DURING C-CHECK INSPECTION, THE LAVATORY DOOR AFT THRESHOLD SECTION WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFT THRESHOLD SECTION AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996062000501 19960620 00501 EU 1996 6 20 C2XA96IA125 1 19960514 A 5320 S2541003900001 FITTING AEROSP ATR42 ATR42320 8680930 EU LAV DOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 34817 152 IAH - DURING C-CHECK INSPECTION, THE LAVATORY DOOR THRESHOLD FITTING ASSEMBLY WAS FOUND TO BE CORRODED. MAINTENANCE REM OVED AND REPLACED THE FITTING ASSEMBLY AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996062000502 19960620 00502 EU 1996 6 20 C2XA96IA126 1 19960514 A 5320 S53971402249 STIFFENER AEROSP ATR42 ATR42320 8680930 EU FR 27 CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 34817 152 IAH - DURING C-CHECK INSPECTION, A FRAME STIFFENER ON FRAME 27A RIGHT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE STIFFENER AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996062000503 19960620 00503 EU 1996 6 20 C2XA96IA127 1 19960514 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FS 39-42 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 34817 152 IAH - DURING C-CHECK INSPECTION, THE FLIGHT ATTENDANTS SEAT TRACKS WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND R EPLACED THE AFT RIGHT SEAT TRACK AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996062000504 19960620 00504 EU 1996 6 20 C2XA96IA128 1 19960513 A 5610 NP1588012 WINDSHIELD AEROSP ATR42 ATR42320 8680930 EU RT COCKPIT CRACKED A C2XA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 09 27806 075 SHV - FLT 3789 - DURING CRUISE THE FIRST OFFICERS WINDSHIELD OUTER PANE CRACKED. THE AIRCRAFT LANDED AT SHV WITHOUT FUR THER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND THE AIRCRAFT WAS FERRIED TO IAH. AT IAH, MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS WINDSHIELD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996062000505 19960620 00505 SO 1996 6 20 C2XA96IA129 1 19960513 A 5530 12015374001 DRAG ANGLE EMB 120 EMB120RT SO VERT STAB CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12715 120125 IAH - DURING C-CHECK INSPECTION, THE LEFT VERTICAL STABILIZER DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED A ND REPLACED THE LEFT DRAG ANGLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996062000506 19960620 00506 WP 1996 6 20 CKSA96052 1 19960519 A 3260 H146 SWITCH DOUG DC8 DC8F55 3021928 WP LT/RT MLG SHORTED A CKSA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 809CK 64985 45803 KMIA - LANDING GEAR RED UNSAFE LIGHT REMAINS ON AFTER GEAR RETRACTION. CYCLING GEAR WAS NO HELP. FOUND LEFT MAIN SWITC H INOP. ALSO, FOUND RIGHT MAIN GEAR SWITCH DOOR SWITCH PLUG SHOWING LOW RESISTANCE ACROSS PIN. REPLACED SWITCH ON LEFT SIDE AND PLUG ON RIGHT SIDE. PERFORMED GEAR SWING IAW 32-1-0. CHECKED NORMAL. (M) 2 L 7 4 4F 4A25 1996062000507 19960620 00507 WP 1996 6 20 CKSA96053 1 19960527 A 3233 57740355508 ACTUATOR DOUG DC8 DC861 3021952 WP RT MLG FAILED A CKSA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 23 816CK 45362 45892 KNGU - UPON GEAR RETRACTION, HYDRAULIC PRESSURE DROPS TO 800 PSI, 'GEAR NOT LATCHED' LIGHT AND 'GEAR DOOR' LIGHT ILLUMIN ATED. (SECONDARY GEAR WARNING LIGHTS SHOW (R) MAIN GEAR AND (R) MAIN GEAR DOOR UNSAFE LIGHTS) AFTER CYCLING GEAR, HYDRA ULIC PRESSURE RECOVERS AND (R) MAIN GEAR RETRACTS SLOWLY. ALL OTHER HYDRAULIC INDICATIONS NORMAL. GEAR PINS INSTALLED AND SAFTIED. INSPECTED AIRCRAFT AND FOUND SAFE FOR INTENDED FERRY FLIGHT. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR RETRACT CYLINDER. CYCLED SYSTEM SEVERAL TIMES. OPS CHECKED AND LEAK CHECKED GOOD IAW DC-8 MM CHAPTER 32-30-0. (M) 2 L 7 4 4F 4A25 1996062000508 19960620 00508 NE 1996 6 20 GLBA96061 2 19960318 A 7320 311703301 HMU EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT ENGINE MALFUNCTIONED A GLBA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 01 299UX 120299 20760 BIS - CREW REPORTED, THE RIGHT EEC FAILED IN FLIGHT. CREW ELECTED AN AIR TURN BACK AND MADE AN UNEVENTFUL LANDING. MAI NTENANCE REMOVED AND REPLACED RIGHT HMU. LEAK AND OPS CHECKS WERE GOOD. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1996062000509 19960620 00509 CE 1996 6 20 GLBA96063 1 19960403 A 6120 BETA COLLAR BEECH 1900 1900D 1154162 CE RT PROP WORN A GLBA K NONE O OTHER AP APPROACH 1 CE 01 100UX UE100 SPW - CREW REPORTED, THE RIGHT PROP WENT INTO GROUND FINE DURING FLAIR, MAINTENANCE REMOVED AND REPLACED RIGHT PROP AND ADJUSTED ENGINE RIGGING FOR TORQUE. OPS CHECKS WERE GOOD. (M) 2 L 7 2 4T RT A24CE 1996062000510 19960620 00510 CE 1996 6 20 GLBA96064 1 19960403 A 3610 BLEED AIR BEECH 1900 1900C 1154161 CE RT ENGINE FAILED A GLBA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 01 159GL UC159 CIU - CREW REPORTED, A RIGHT BLEED AIR FAIL AFTER TAKEOFF AND ELECTED AN AIR TURN BACK WITH UNEVENTFUL LANDING. MX REPL ACED GASKET ON TEMP SENSOR AND DAMAGED EVA TUBING IN RIGHT LEADING EDGE. OPS CHECKS WERE GOOD. (M) 2 L 7 2 4T RT A24CE 1996062000511 19960620 00511 CE 1996 6 20 GLBA96066 1 19960407 A 3260 H111541 UPLOCK SWITCH BEECH 1900 1900C 1154161 CE RT MLG BENT A GLBA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 01 98GL UC98 SPW - CREW REPORTED, THE 'GEAR INTRANSIT' LIGHT REMAINED ILLUMINATED AFTER GEAR WAS SELECTED UP. THEY ELECTED AN AIR TU RN BACK AND MADE AN UNEVENTFUL LANDING. MAINTENANCE REPLACED RIGHT LANDING GEAR UPLOCK SWITCH AND ADJUSTED LEFT POWER L EVER GEAR WARNING PEDESTAL SWITCH. OPS CHECK WAS GOOD. (M) 2 L 7 2 4T RT A24CE 1996062000512 19960620 00512 EA 1996 6 20 GLBA96067 2 19960409 A 7310 3038419 FUEL LINE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA LT ENGINE LOOSE A GLBA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 CE 01 67UE UC67 GRI - CREW REPORTED LEFT ENGINE LOST POWER WHILE AIRBORNE. CREW ELECTED AN AIR TURN BACK AND MADE AN UNEVENTFUL LANDING . MAINTENANCE TIGHTENED AND SAFTIED FUEL LINE AT LEFT AFT FIRE SEAL. LEAK CHECK AND GROUND POWER CHECKS WERE GOOD. (M ) 2 L 7 2 4T 4 T RT A24CE E4EA 1996062000513 19960620 00513 CE 1996 6 20 GLBA96068 1 19960411 A 3250 1148200363 BELLCRANK BEECH 1900 1900C 1154161 CE NLG WORN A GLBA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 01 152GL UC152 LAN - CREW REPORTED, THAT LEFT RUDDER PEDAL REQUIRED EXCESSIVE FORCE ON TAKEOFF ROLL. THEY ABORTED THE TAKEOFF AND RETU RNED TO GATE. MAINTENANCE REPLACED MANUAL STEERING BELLCRANK AND ASSOCATED BEARINGS. OPS CHECK WAS GOOD. (M) 2 L 7 2 4T RT A24CE 1996062000514 19960620 00514 SO 1996 6 20 GLBA96087 1 19960510 A 5240 MS250851 SWITCH EMB 120 EMB120RT SO SERVICE DOOR OUT OF ADJUST A GLBA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 01 128AM 120109 RDU - CREW REPORTED SERVICE DOOR ANNUNCIATOR ILLUMINATED AND THEY RETURNED TO THE GATE. MAINTENANCE ADJUSTED SERVICE DO OR MICROSWITCHES. SYSTEM OPS CHECK WAS GOOD. (M) 2 L 7 2 4T RT A31SO 1996062000515 19960620 00515 CE 1996 6 20 GLBA96088 1 19960512 A 3260 1003810061 DN LOCK SWITCH BEECH 1900 1900C 1154161 CE NLG MALFUNCTIONED A GLBA O OTHER N FALSE WARNING CR CRUISE 1 CE 01 79GL UC79 SPW - CREW REPORTED GEAR 'INTRANSIT' LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE REMOVED AND REPLACED NOSE GEAR DOWNLOCK S WITCH. SYSTEM OPS CHECK WAS GOOD. (M) 2 L 7 2 4T RT A24CE 1996062000516 19960620 00516 CE 1996 6 20 GLBA96089 1 19960513 A 3260 1148200773 BRACKET BEECH 1900 1900C 1154161 CE NOSE BENT A GLBA O OTHER P NO WARNING INDICATION LD LANDING 1 CE 01 141UE UC141 LAN - CREW REPORTED, NOSE GEAR GREEN LIGHT DOES NOT ILLUMINATE WITH GEAR SELECTED DOWN. MAINTENANCE STRAIGHTENED NOSE D OWNLOCK SWITCH CONTACT BRACKET. SYSTEM OPS CHECK WAS GOOD. (M) 2 L 7 2 4T RT A24CE 1996062000517 19960620 00517 CE 1996 6 20 GLBA96090 1 19960512 A 5751 1181300001 AILERON BEECH 1900 1900C 1154161 CE LT AILERON DAMAGED A GLBA K NONE O OTHER IN INSP/MAINT 1 CE 01 122GL 655 UC122 ORD -CREW FOUND DAMAGE ON TRAILING EDGE OF LEFT AILERON DURING WALK AROUND INSPECTION. MAINTENANCE REMOVED AND REPLACED LEFT AILERON. FLIGHT TEST WAS GOOD. (M) 2 L 7 2 4T RT A24CE 1996062000518 19960620 00518 EA 1996 6 20 GLBA96092 2 19960514 A 7397 WIRE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA RT FUEL PRESS CHAFED A GLBA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 01 105GL UC105 MSP - CREW REPORTED RIGHT FUEL PRESSURE ANNUNCIATOR ILLUMINATED. DURING TAXI AND THEY RETURNED TO GATE. MX FOUND CHAFE D WIRE AT PCB. WIRE WAS REPAIRED AND OPS CHECK WAS GOOD. (M) 2 L 7 2 4T 4 T RT A24CE E4EA 1996062000519 19960620 00519 SO 1996 6 20 GLBA96093 1 19960517 A 3260 922AAZYA6A2722A PROX SENSOR EMB 120 EMB120ER 3260203 SO LT MLG OUT OF ADJUST A GLBA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 CE 01 297UX 120297 CIE - CREW REPORTED, LEFT MAIN GEAR 'A' AND 'B' SYSTEM RED LIGHTS REMAINED ILLUMINATED AFTER GEAR RETRACTION. THEY MADE AN AIR TURN BACK AND LANDED UNEVENTFULLY. MAINTENANCE ADJUSTED LEFT GEAR 'A' AND 'B' SYSTEM PROXIMITY SENSORS. OPS CH ECK WAS GOOD. (M) 2 L 7 2 4T RT A31SO 1996062000520 19960620 00520 NM 1996 6 20 IXKA9600036 1 19960527 A 3350 CONNECTOR BOEING 727 727225 1384077 NM CABIN DIRTY A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8882Z 21579 ON POST FLIGHT CHECK, FOUND LEFT AND RIGHT FORWARD OVERWING EMERGENCY LIGHTS INOP. CLEANED CONTACTS TO BOTH LEFT AND RI GHT FORWARD OVERWING LIGHTS. OPS CHECK OK. (M) 2 L 7 3 4F A3WE 1996062000521 19960620 00521 NM 1996 6 20 IXKA960029 1 19960501 A 5241 6556975502 LOWER GATE BOEING 727 727225 1384077 NM GALLEY DOOR DAMAGED A IXKA K NONE O OTHER IN INSP/MAINT 1 EA 25 352PA 20616 FLT 56 - CXL - FORWARD GALLEY SERVICE DOOR (R1) WILL NOT OPEN. FOUND LOWER GATE ASSY ON DOOR DAMAGED. REMOVED AND REPL ACED FOWARD GALLEY SERVICE DOOR (R1) LOWER GATE ASSY PER MM 52-10-10. OP CHECK OK. (M) 2 L 7 3 4F A3WE 1996062000522 19960620 00522 NM 1996 6 20 IXKA960030 1 19960514 A 3350 17023 LENS BOEING 727 727225 1384077 NM CABIN DAMAGED A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 352PA 20616 CATERER DAMAGED 'E' PATH LIGHTING AT ROW 28 DEF. REMOVED AND REPLACED LIGHT LENS ASSY AT 28 DEF 'E' PATH LIGHT. GROUND CHECK OF 'E' LIGHTING OK PER MM 33-50. (M) 2 L 7 3 4F A3WE 1996062000523 19960620 00523 NM 1996 6 20 IXKA960031 1 19960514 A 3350 327 LAMP BOEING 727 727225 1384077 NM CABIN DIM A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 352PA 20616 OVERWING EXIT SIGNS DIM, FORWARD RIGHT, FORWARD LEFT, AFT LEFT. REPLACED LAMPS AT FWD RIGHT, FWD LEFT AND AFT LEFT OVER WING EXIT SIGNS. (M) 2 L 7 3 4F A3WE 1996062000524 19960620 00524 NM 1996 6 20 IXKA960032 1 19960515 A 3350 08199000111 TRACK BOEING 727 727225 1384077 NM CABIN WORN A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 352PA 20616 'E' PATH LIGHT LOOSE AT 4D TO 5D. REMOVED AND REPLACED 'E' PATH FLOOR TRACK. OPS CHECKED OK. (M) 2 L 7 3 4F A3WE 1996062000525 19960620 00525 NM 1996 6 20 IXKA960033 1 19960515 A 3350 1000679 POWER PACK BOEING 727 727251 138408H NM CABIN INOPERATIVE A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 267US 5721 20289 ON POST FLIGHT INSPECTION, FOUND L1 DOOR PORTABLE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED INOP BATTERY POWER PA CK. OPS CHECK OK. (M) 2 L 7 3 4F A3WE 1996062000526 19960620 00526 NM 1996 6 20 IXKA960034 1 19960515 A 3350 328 LAMP BOEING 727 727225 1384077 NM CABIN FAILED A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8880Z 21453 RIGHT OVERWING EMERGENCY DOOR HAS EXIT LIGHT OUT. REMOVED AND REPLACED LAMPS. OPS CHECK OK. (M) 2 L 7 3 4F A3WE 1996062000527 19960620 00527 NM 1996 6 20 IXKA960035 1 19960516 A 3350 LENSE BOEING 727 727225 1384077 NM CABIN LOOSE A IXKA K NONE O OTHER IN INSP/MAINT 1 EA 25 352PA 20616 RED COVER LENS IN TRACK FOR PATH LIGHTING NOT SECURED. SECURED RED COVER LENS IN TRACK, OPS CHECK LIGHTS OK. (M) 2 L 7 3 4F A3WE 1996062000528 19960620 00528 EU 1996 6 20 M3HA96013 1 19960526 A 7712 TQ GAUGE AEROSP ATR42 ATR42300 8680920 EU NR 2 ENGINE MALFUNCTIONED A M3HA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 13 4206G 081 HNL - FLT 442 - AIRCRAFT WAS HALF WAY TO OGG, WHEN THE NR 2 TORQUE GAUGE WENT TO 120 PERCENT AND REMAINED. AIRCRAFT WAS DIVERTED BACK TO HNL, AN UNEVENTFUL LANDING WAS MADE. AIRCRAFT WAS TAKEN OFF LINE FOR THE REMAINDER OF THE DAY. REMOV ED AND INSTALLED SERVICEABLE TORQUE GAUGE NR 2 ENGINE IAW JIC 77-13-81 RAI 10000-001, OPS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1996062000529 19960620 00529 EU 1996 6 20 M3HA96014 1 19960529 A 3411 PITOT PROBE AEROSP ATR42 ATR42300 8680920 EU RT FUSELAGE MALFUNCTIONED A M3HA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 13 4208G 086 HNL - FLT 211 - FROM PREVIOUS PAGE ON DEPARTURE FLIGHT OFFICERS AIRSPEED INDICATOR DID NOT COME UP TO SPEED AS INDICATED ON CAPTAINS AND STANDBYS. REMOVED AND INSTALLED SERVICEABLE FLIGHT OFFICERS PITOT PROBE IAW JIC 34-11-11-RA-10000-001 SEC GOOD LEAK CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1996062000530 19960620 00530 SW 1996 6 20 MALA964991 1 19960513 A 5230 WARNING LIGHT SWRNGN SA227 SA227AC 8780603 SW CARGO DOOR ILLUMINATED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 426MA AC645 FLT NR 3355 - AFTER ROTATION, THE CARGO DOOR WARNING LIGHTS ILLUMINATED. THE AIRCRAFT RETURNED TO YNG. MAINTENANCE INS PECTED THE DOOR MECHANISMS. THE DISCREPANCY COULD NOT BE DUPLICATED. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2 L 7 2 4T RT A8SW 1996062000531 19960620 00531 SW 1996 6 20 MALA964992 1 19960515 A 5330 SKIN SWRNGN SA227 SA227AC 8780603 SW BS 512.81 DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 442MA AC725 DURING AN INSPECTION IN MSP, MAINTENANCE NOTED SKIN DENTING AND OIL CANNING AT FS 512.810. REPAIRS WERE COMPLETED BY FA BRICATING AND INSTALLING A REPAIR DOUBLER IAW FAC SRM 53-90-20 PAGES 61-63. (M) 2 L 7 2 4T RT A8SW 1996062000532 19960620 00532 SW 1996 6 20 MALA964993 1 19960515 A 5280 2755009108 DOOR SWRNGN SA227 SA227AC 8780603 SW RT NLG BENT A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 60NE AC760B FLT 3060 - THE NOSE GEAR BEGAN TO CYCLE AFTER GEAR RETRACTION. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE FOUND THE LOW ER FORWARD CORNER OF THE NLG DOOR BENT OUT INTO THE SLIP STREAM, CAUSING THE DOOR TO NOT CLOSE COMPLETELY. AFTER REPLAC EMENT, THE DOOR WAS RERIGGED. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2 L 7 2 4T RT A8SW 1996062000533 19960620 00533 NM 1996 6 20 MALA964994 1 19960516 A 2720 PIN DHAV DHC8 DHC8102 2809003 NM RUDDER IND LOOSE A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 859MA 361 FLT NR 3311 - AFTER TAKEOFF FROM DTW, THE RUD PRESS AND RUD FULL PRESS CAUTION LIGHTS ILLUMINATED ABOVE 140 KTS. THE AI RCRAFT RETURN DTW. MAINTENANCE RESET A LOOSE PIN AT TERMINAL BLOCK 2721-FB1. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2 H 7 2 4T RT A13NM 1996062000534 19960620 00534 SW 1996 6 20 MALA964995 1 19960516 A 3240 BRAKE LINE SWRNGN SA227 SA227AC 8780603 SW LT MLG OUT OF POSITION A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 15 159MC AC728B FLT N3393 - ON CLIMB-OUT FROM MSP, THE CREW NOTED A LIGHT RUBBER BURNING SMELL THAT DISSIPATED IN APPROXIMATELY 5 MINUTE S. UPON POST FLIGHT INSPECTION, THE LEFT MAIN GEAR INBOARD BRAKE LINE WAS FOUND TO BE RUBBING ON THE TIRE. MX INSPECTE D THE LINE AND FOUND CHAFFING TO BE NEGLIGIBLE. THE LINE WAS REPOSITIONED. ALL CHECKS SATISFACTORY. (M) 2 L 7 2 4T RT A8SW 1996062000535 19960620 00535 SW 1996 6 20 MALA964996 1 19960516 A 5753 2736000039 SKIN SWRNGN SA227 SA227AC 8780603 SW LT TE FLAP CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 424MA AC639 DURING A SCHEDULED INSPECTION IN MSP, THE LEFT FLAP UPPER INBOARD SKIN HAD A HOLE CHAFED THROUGH IT. REPAIRS WERE COMPL ETED TO THE AIRCRAFT BY REPLACING THE LEFT FLAP ASSEMBLY. REPAIRS WERE COMPLETED TO THE FLAP BY FABRICATING AND INSTALL ING A REPAIR DOUBLER AND REPLACEMENT SKIN IAW FAC SRM 57-90-60 REPAIR NR 8. (M) 2 L 7 2 4T RT A8SW 1996062000536 19960620 00536 SW 1996 6 20 MALA964997 1 19960515 A 3233 2752010003 ACTUATOR SWRNGN SA227 SA227AC 8780603 SW NLG MALFUNCTIONED A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 60NE AC760B FLT NR 3301 - ON CLIMB-OUT FROM DTW, THE NOSE GEAR CONTINUED TO CYCLE IN THE WHEEL WELL AFTER GEAR RETRACTION. THE RECY CLED THE GEAR, AND THE PROBLEM REMAINED. THE AIRCRAFT RETURNED TO DTW. MX REPLACED THE LEFT AND RIGHT NOSE LANDING GEA R ACTUATORS IAW SA227 MM 32-30-00. SYSTEM OPERATED SATISFACTORILY DURING A TEST FLIGHT. (M) 2 L 7 2 4T RT A8SW 1996062000537 19960620 00537 NM 1996 6 20 MALA964998 1 19960517 A 3350 6104781 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 833MA 343 FLT NR 3066 - DURING THE PREFLIGHT INSPECTION IN DTW, THE CREW NOTED SEVERAL INOPERATIVE FLOOR TRACK EMERGENCY LIGHTS. M AINTENANCE REPLACED THE RIGHT AFT BATTERY PACK. ALL CHECKS SATISFACTORY. (M) 2 H 7 2 4T RT A13NM 1996062000538 19960620 00538 NM 1996 6 20 MALA964999 1 19960518 A 3350 100055111 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT MALFUNCTIONED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 848MA 346 FLT 3051 - DURING THE POST FLIGHT INSPECTION IN DTW, THE CREW NOTED THAT THE COCKIPT OVERHEAD EMERGENCY LIGHT WOULD INTE RMITTENTLY ILLUMINATE. MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM OPERATED SATISFACTORILY. (M) 2 H 7 2 4T RT A13NM 1996062000539 19960620 00539 NM 1996 6 20 MALA965000 1 19960518 A 3350 6104781 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 859MA 361 FLT 3043 - DURING AN MAINTENANCE INSPECTION IN DTW, THE LEFT AIRSTAIR DOOR EGRESS LIGHT WAS INOPERATIVE. MX REPLACED TH E UPPER WARDROBE BATTERY PACK. ALL CHECKS SATISFACTORY. (M) 2 H 7 2 4T RT A13NM 1996062000540 19960620 00540 SW 1996 6 20 MALA965001 1 19960520 A 2431 MS326E835 CONNECTOR SWRNGN SA227 SA227AC 8780603 SW LT BATTERY BOX WATER CONTAM A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 160MC AC733B FLT NR 3467 - ON CLIMB-OUT FROM YXU, THE LEFT BATTERY AMBER AND RED LIGHTS ILLUMINATED AND THE BATTERY TEMP INDICATION W AS HIGH. THE CREW TURNED OFF THE BATTERY AND RETURNED TO YXU. MAINTENANCE REPLACED THE BATTERY TEMP SENSOR CANNON PLUG . ALL CHECKS SATISFACTORY. (M) 2 L 7 2 4T RT A8SW 1996062000541 19960620 00541 SW 1996 6 20 MALA965002 1 19960520 A 5311 FRAME SWRNGN SA227 SA227AC 8780603 SW BS 242.27 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 2692P AC658B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND TWO CRACKS IN THE LOWER RIGHT BELT FRAME FLANGE AT FS 242.27. R EPAIRS WERE COMPLETED BY STOP DRILLING THE CRACKS AND INSTALLING A REPAIR DOUBLER IAW AEROTECH DESIGNS EA01-96040. (M) 2 L 7 2 4T RT A8SW 1996062000542 19960620 00542 WP 1996 6 20 ORJA9626 1 19960517 A 3241 DRIVE STUDS DOUG DC9 DC982 3022082 WP ANTI-SKID TRANS INOP A ORJA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 11 823RA 49889 WHEEL NOT TURNING LIGHT CAME ON SHORTLY AFTER BEGINNING TO ROLL. RETURNED TO GATE. REINSTALLED DRIVE COUPLING STUDS ON NR 3 ANTI-SKID TRANSDUCER. OPS CHECK NORMAL. (M) 2 L 7 2 4F A6WE 1996062000543 19960620 00543 WP 1996 6 20 ORJA9627 1 19960502 A 3246 26088911 WHEEL DOUG DC9 DC983 3022083 WP LT MLG MISSING BOLT A A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 834RA 5314 53124 POST FLIGHT WALKAROUND, BOLT MISSING ON NR 1 MAIN WHEEL. REMOVED AND REPLACED NR 1 WHEEL ASSEMBLY PER 32-40-01. (M) 2 L 7 2 4F RT A6WE 1996062000544 19960620 00544 WP 1996 6 20 ORJA9628 1 19960502 A 3350 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 822RA 49932 CEILING EMERGENCY LIGHTS ROW 11-16 WILL NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY BATTERIES FOR ROWS 11-16. OPS C HECK NORMAL. (M) 2 L 7 2 4F A6WE 1996062000545 19960620 00545 WP 1996 6 20 ORJA9629 1 19960508 A 3246 26088911 WHEEL ASSEMBLY DOUG DC9 DC983 3022083 WP NR 3 MLG BROKEN A A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 879RA 53185 ON WALK AROUND, FOUND BROKEN THROUGH BOLT ON NR 3 MAIN WHEEL. REPLACED NR 3 MAIN IN AW MM CHAPTER 32. (M) 2 L 7 2 4F RT A6WE 1996062000546 19960620 00546 WP 1996 6 20 ORJA9630 1 19960523 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 824RA 53017 EMERGENCY EXIT FLOOR TRACK LIGHTS AT SEAT ROW 12 TO 16 INOP. REPLACED BATTERY PACK AT SEAT ROW 12. OPS GOOD. (M) 2 L 7 2 4F A6WE 1996062000547 19960620 00547 NM 1996 6 20 ORJA9631 1 19960523 A 2130 PRESSURIZATION DOUG MD90 MD9030 3023690 NM CABIN MALFUNCTIONED A ORJA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 11 902RA 53490 AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. PERFORMED SYSTEM NR 1 AND NR 2 PRESSURIZATION TEST. SYSTEMS NR 1 AND NR 2 OPERATIONAL CHECK NORMAL. LEAK CHECKED CABIN AND CARGO ENTRY DOORS. NO LEAKS NOTED AS PER MM 21-30-00. AIRCRAFT OK F OR SERVICE. (M) 2 L 7 2 4F RT A6WE 1996062000548 19960620 00548 WP 1996 6 20 ORJA9632 1 19960527 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 872RA 49793 OVERWING EMERGENCY LIGHTS REMAIN ILLUMINATED IN 'OFF' POSITION. REMOVED AND REPLACED OVERWING EMERGENCY LIGHTS' BATTERY PACK, IAW MM 33-53-00. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 1996062000549 19960620 00549 SO 1996 6 20 RAAAE896007 1 19960319 A 3350 1000553 LIGHT LKHEED 188 188C 5262604 SO CABIN FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 AFT PAX COMPARTMENT EMERGENCY EXIT EMERGENCY LIGHT FAILED SERVICE CHECK. CHANGED LIGHT ASSY. (M) 2 L 7 4 4T 4A22 1996062000550 19960620 00550 SO 1996 6 20 RAAAE896008 1 19960319 A 3350 1000553 LIGHT LKHEED 188 188C 5262604 SO CABIN FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 LEFT AFT OVERWING EXIT EMERGENCY LIGHT FAILED SERVICE CHECK. CHANGED LIGHT ASSY. (M) 2 L 7 4 4T 4A22 1996062000551 19960620 00551 SO 1996 6 20 RAAAE896016 1 19960510 A 5330 SKIN LKHEED 188 188C 5262604 SO BS 996 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 72630 188C2010 DURING SCHEDULED NR 2 CHECK, FOUND FUSELAGE SKIN CORRODED AT FS 996 AND STR 43 TO 50. REMOVED CORRODED SKIN, INSTALLED FILLER AND REPAIR PLATE PER SRM 53-2-1, FIG 2. (M) 2 L 7 4 4T 4A22 1996062000552 19960620 00552 SO 1996 6 20 RAAAE896017 1 19960510 A 5320 DOUBLER LKHEED 188 188C 5262604 SO BS 181 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 2 CHECK, FOUND REPAIR DOUBLER CRACKED AT FS 181 AND STRINGER 41. REPAIRED PER SRM 53-2-1, FIG 2, SH EET 2 AND 3. (M) 2 L 7 4 4T 4A22 1996062000553 19960620 00553 SO 1996 6 20 RAAAE896018 1 19960510 A 5311 FRAME LKHEED 188 188C 5262604 SO BS 891.5 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 72630 188C2010 DURING SCHEDULED NR 2 CHECK, FOUND FS 891.5 CORRODED AT STRINGER 47 TO 48. REPAIRED PER SRM 53-2-3. (M) 2 L 7 4 4T 4A22 1996062000554 19960620 00554 SO 1996 6 20 RAAAE896019 1 19960510 A 5313 STRINGER LKHEED 188 188C 5262604 SO BS 891.5 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 72630 188C2010 DURING SCHEDULED NR 2 CHECK, FOUND STRINGER 47 CORRODED AT FS 891.5. REPAIRED PER SRM 53-2-2. (M) 2 L 7 4 4T 4A22 1996062000555 19960620 00555 SO 1996 6 20 RAAAE96020 1 19960510 A 5753 SKIN LKHEED 188 188C 5262604 SO RT TE FLAP CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 2 CHECK, FOUND RIGHT FLAP TRAILING EDGE, UPPER SURFACE SKIN CRACKED AT FLAP STATION 241. REPAIRED P ER SRM 57-4-1, FIG 2 AND 51-3-4, FIG 1. (M) 2 L 7 4 4T 4A22 1996062000556 19960620 00556 NE 1996 6 20 S2YA960007 2 19960502 A 7210 310820701 PLANET GEAR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RED GEARBOX DAMAGED A A S2YA K NONE O OTHER TX TAXI/GRND HDL 1 GL 13 841SK 5260 UE84 THE FLIGHT CREW FOUND THE LEFT PROP WOULD NOT FEATHER DURING A GROUND AUTOFEATHER TEST, THEY ALSO NOTICED LEFT ENGINE LO W OIL PRESSURE INDICATION WAS ILLUMINATED. AN ENGINE SHUTDOWN WAS MADE AND MAINTENANCE FOUND METAL PARTICLES IN THE OIL . THE ENGINE WAS REPLACED AND SENT TO PW AND C. INITIAL INVESTIGATION FOUND ONE FIRST STAGE REDUCTION PLANETARY GEAR H AD TURNED ON THE BEARING RACE, SEVERELY SCORING IT. THE SUN GEAR WAS ALSO SPALLING, P/N 3108356-01. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 1996062000557 19960620 00557 CE 1996 6 20 S2YA960008 1 19960523 A 2121 1143800283 BLOWER BEECH 1900 1900D 1154162 CE CABIN FAILED A S2YA G A O2 MASK DEPLOYED UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 13 148SK 2320 UE148 FLT 1199 - IND-MKE - EN ROUTE THE FLIGHT CREW REPORTED SMOKE IN THE CABIN. THEY MADE AN AIR TURN BACK TO IND TAKING EME RGENCY PRECAUTIONS DURING AND AFTER LANDING. MX WAS CALLED TO INSPECT THE AIRCRAFT AND FOUND THE FWD VENT BLOWER SEIZED , BURNED OR BURNED SMELLING, EXTERNAL WIRING SHOWED NO DEFECTS. THIS WAS OUR FIRST INSTANCE OF A BLOWER CAUSING SMOKE I N THE CABIN. (M) 2 L 7 2 4T RT A24CE 1996062000558 19960620 00558 GL 1996 6 20 SRAA59604 2 19960516 A 7250 6871175 TURBINE BLADE LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL NR 2 ENG DAMAGED A SRAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 23 905SJ 9506 4472 550263 DURING CRUISE TO ARI FLT NR 1204, NR 2 ENGINE HAD LOW TORQUE AND HIGH FUEL FLOW, ACCOMPLISHED ENGINE SHUT DOWN AS PRECAU TIONARY PRIOR TO LANDING, AIRCRAFT LANDED WITHOUT INCIDENT. FOUND NR 2 ENGINE HAD TURBINE BLADES DAMAGED. REPLACED NR 2 ENGINE AND PERFORMED ENGINE RUN UP, OPS CHECKED GOOD PER JOB CARDS 7101 AND 7101-2. (M) 2 H 7 4 4T 4 T A1SO E282 1996062000559 19960620 00559 NM 1996 6 20 TAOA059604 1 19960516 A 2913 371380 HYD PUMP VICKERS BOEING 727 727225 1384077 NM NR 1 ENGINE FAILED A TAOA O OTHER J WARNING INDICATION CR CRUISE 1 EA 15 919TS MX484364 20447 FLT 6100- LGA-BOS - NR 1 'A' SYSTEM HYD PUMP LOW PRESSURE LIGHT APPEARED EN ROUTE, TURNED PUMP OFF, PRESSURE REMAINED NO RMAL FOR 5-10 MINUTES. PRESSURE THEN DECREASED SLOWLY TO RED GAUGE BAN WHEN NR 2 'A' LOW PRESSURE APPEARED. REPLACED N R 1 A ENGINE DRIVEN PUMP AND NR 2 'A' ENGINE DRIVEN PUMP. (M) 2 L 7 3 4F A3WE 1996062000560 19960620 00560 NE 1996 6 20 TAOA059605 2 19960516 A 7230 C1 BEARING BOEING 727 727254 138408L NM PWA JT8 JT8D7B 52053 NE NR 3 ENG FAILED A TAOA C D E ABORTED TAKEOFF RETURN TO BLOCK ENGINE SHUTDOWN J WARNING INDICATION TO TAKEOFF 1 EA 15 915TS 655189 20252 654489 FLT NR 6011 - LGA-BOS - VERY LOUD NOISE OCCURRED, TAKEOFF WAS REJECTED, NR 3 ENGINE SHUT DOWN, DUE C1 BEARING FAILURE. R EPLACED NR 3 ENGINE. (M) 2 L 7 3 4F 4 F A3WE E2EA 1996062000561 19960620 00561 NM 1996 6 20 TAOA059606 1 19960517 A 3350 0L3071BPEGPL0791 LENS LAMP BOEING 727 727254 138408L NM CABIN MISSING A TAOA K NONE O OTHER IN INSP/MAINT 1 EA 15 912TS 20438 FLT NR 6121 - BOS-LGA - E-PATH LIGHTING LENS AND LAMP MISSING ROW 26. INSTALLED LENS AND LAMP P/N, 0L3071BPEGPL07912. ( M) 2 L 7 3 4F A3WE 1996062000562 19960620 00562 NE 1996 6 20 TAOA059607 2 19960523 A 7200 ENGINE BOEING 727 727227 1384078 NM PWA JT8 JT8D7B 52053 NE NR 2 FAILED A A TAOA E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION CR CRUISE 1 EA 15 924TS 21041 648862 FLT NR 6151 - BOS-LGA - OIL TEMP WENT INTO YELLOW GAUGE BAN, PROCEDURE FOLLOWED. ONLY ADDITIONAL THROTTLE WOULD KEEP IN DICATION OUT OF YELLOW OR RED GAUGE BAN. SHORTLY, THEREAFTER OIL QUANTITY DECREASED, LOW OIL PRESSURE LIGHT ILLUMINATED , NR 2 ENGINE SHUT DOWN. WINDMILL TIME 20 MINUTES, OIL PRESSURE 15 PSI. REPLACED NR 2 ENGINE, S/N ON 648765. PRELIMIN ARY CAUSE OF FAILURE UNKNOWN, WILL ADVISE AFTER TEAR DOWN. (M) 2 L 7 3 4F 4 F A3WE E2EA 1996062000563 19960620 00563 NM 1996 6 20 TAOA069603 1 19960605 A 3350 900835A BATTERY PACK GRIMES BOEING 727 727225 1384077 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 923TS VA4809 20441 FLT 6540 - DCA-LGA - FOUND ON OVERNIGHT CHECK, EMERGENCY EXIT LAMP AT ROW 28 CEILING INOP. REPLACED BATTERY PACK, OPS C EHCKED OK, PER MM 33-50-00. (M) 2 L 7 3 4F A3WE 1996062000564 19960620 00564 NM 1996 6 20 TWRA9630 1 19960520 A 2560 65B096337 GIRT BAR LIFTER BOEING 747 747212B 1384886 NM PAX DOOR BROKEN A A TWRA K NONE O OTHER IN INSP/MAINT 1 EA 15 620FF 21162 L-2 MED AFT END OF GIRT BAR SLIDE WOULD NOT FULLY ENGAGE IN FLOOR FITTING AND FELL OUT OF LIFTER. FOUND AFT GIRT BAR LI FTER BROKEN. REPLACED LIFTER PER MM 52-11-07. OPS CHECK OK 52-11-00. (M) 2 L 7 4 4F A20WE 1996062000565 19960620 00565 NM 1996 6 20 UIEA9606 1 19960516 A 3230 65B015409 DNLOCK ACTUATOR BOEING 747 747245F 1384897 NM LT MLG MISINSTALLED A A UIEA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 EA 15 640FE 20826 AFTER TAKEOFF DURING GEAR RETRACTION, LEFT BODY GEAR DOOR STAYED OPEN. ALL GEARS WERE UP. RED DOOR/GEAR LIGHTS ON, ALS O PRIM/ALT DOOR OPEN LIGHTS ON. RECYCLED GEAR AND NO HELP. WHEN GEAR HANDLE PLACED TO OFF, LEFT BODY GEAR WENT DOWN/LO CKED. WITH GEAR HANDLE DOWN FOR LANDING, ALL INDICATIONS WERE NORMAL. RETURNED TO LUX, LANDING UNEVENTFUL. FOUND THAT INCORRECT DOWNLOCK ACTUATOR INSTALLED AT LEFT BODY GEAR POSITION DURING 'A' CHECK. REPLACED WITH CORRECT ACTUATOR. OP ERATION RESTORED TO NORMAL. (M) 2 L 7 4 4F A20WE 1996062000566 19960620 00566 NM 1996 6 20 USAA960439 1 19960522 A 5320 CHORD BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 227AU 44671 21816 CLT - INSPECTION FOUND TWO APPROXIMATELY .375 INCH CRACK BY ULTRASONIC AND EDDY CURRENT LOCATED AT STATION 727 AT STRING ER 18A RIGHT CHORD. INSTALLED CHORD SECTION, AUX CHORD AND LOWER SPLICE PER EO NR 9394G068. (M) 2 L 7 2 4F A16WE 1996062000567 19960620 00567 NM 1996 6 20 USAA960441 1 19960521 A 5315 FLOOR BEAM BOEING 737 7374B7 1384702 NM BS 987 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 428US 19542 24550 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH TO 2 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES BS 987 LEFT SIDE TO RIGHT SIDE OF CABIN TOP OF FLOOR BEAM. CUT OFF TOP CHORD OF FLOOR BEAM AND INSTALLED T-CAP REPAIR. REPAIRED PE R EA 4116. (M) 2 L 7 2 4F RT A16WE 1996062000568 19960620 00568 NM 1996 6 20 USAA960442 1 19960521 A 5315 FLOOR BEAM BOEING 737 7374B7 1384702 NM BS 294.5 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 428US 19542 24550 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY 2 INCH CORRODED AREAS, BS 294.5 RBL 8, RBL 39, RBL 44 .5 INCH FLOOR BEAM. CUT OUT CORRODED AREA SPLICED IN FLOOR BEAM, COMPLETED REPAIR. REPAIRED PER SRM 53-10-51 FIG 205. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996062000569 19960620 00569 NM 1996 6 20 USAA960443 1 19960521 A 5315 FLOOR BEAM BOEING 737 7374B7 1384702 NM BS 312 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 428US 19542 24550 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED FLOOR BEAM, BS 312 LBL .5 INCH LBL 7.5 INCH LB L 21 INCH. REMOVED CORROSION, SPLICED T-CAP AND COMPLETED REPAIR. REPAIRED PER TR 53-10-03. CORROSION TASK NR C53-107 -02, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996062000570 19960620 00570 NM 1996 6 20 USAA960444 1 19960521 A 5315 FLOOR BEAM BOEING 737 7374B7 1384702 NM BS 947 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 428US 19542 24550 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER CORRODED AREAS AROUND NUT PLATE HOLES BS 947 LBL 12 FLOO R BEAM. INSTALLED T-CAP AND REPAIR ANGLES AND STRAPS. REPAIRED PER SRM 51-00-53 AND EA 41119. CORROSION TASK NR C53-1 07-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996062000571 19960620 00571 NM 1996 6 20 USAA960445 1 19960521 A 5315 BAC1505100246 FLOOR BEAM BOEING 737 7374B7 1384702 NM BS 328 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 428US 19542 24550 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY 1 INCH CORRODED AREAS BS 228 RBL 14 TO RBL 58 FLOOR BE AM. CUT OUT CORRODED AREA FABRICATED AND INSTALLED REPAIR PARTS COMPLETED REPAIR PER SRM 53-10-51 FIG 205. CORROSION T ASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996062000572 19960620 00572 NM 1996 6 20 USAA960446 1 19960521 A 5320 SUPPORT BEAM BOEING 737 7374B7 1384702 NM BS 270 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 428US 19542 24550 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND APPROX 1 INCH BY 1 INCH OF SURFACE CORROSION STATION 270 AT RBL 11, WL 2 08, COCKPIT ENTRANCE FLOOR SUPPORT BEAM. CUT OUT AFFECTED AREA AND INSTALLED DOUBLER REPAIR. REPAIRED PER SRM 51-70-12 . CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996062000573 19960620 00573 NM 1996 6 20 USAA960447 1 19960521 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM BS 344 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 428US 19542 24550 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER SPOT CORROSION BS 344 LBL 43 TO RBL 8 FLOORBEAM. INSTAL LED T-CAP AND REPAIR ANGLES AND STRAPS. (M) 2 L 7 2 4F RT A16WE 1996062000574 19960620 00574 NM 1996 6 20 USAA960448 1 19960521 A 5311 FRAME BOEING 737 7374B7 1384702 NM BS 294.5 CRACK A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 428US 19542 24550 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK STATION 294.5 RBL 48 FRAME. INSTALLED DOUBLER, REPAIRED PER SRM 51-70-11. (M) 2 L 7 2 4F RT A16WE 1996062000575 19960620 00575 NM 1996 6 20 USAA960449 1 19960521 A 5311 FRAME BOEING 737 7374B7 1384702 NM BS 296 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 428US 19542 24550 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK BS 296 WL 209 RIGHT SERVICE DOORWAY FRAME. INSTALLED DOU BLER, REPAIRED PER SRM 51-70-11. (M) 2 L 7 2 4F RT A16WE 1996062000576 19960620 00576 WP 1996 6 20 USAAD96053 1 19960512 A 3260 1D32245771 HARNESS DOUG DC9 DC931 3022065 WP LT MLG FAULTY A USAA A L UNSCHED LANDING ABORTED APPROACH N FALSE WARNING AP APPROACH 1 EA 19 969VJ 47421 SYR - FLT 856 - LEFT MAIN GEAR LIGHT (GREEN) DID NOT ILLUMINATE WHEN GEAR EXTENDED. FLIGHT DIVERTED TO SYR AND LANDED W ITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT DOWN LIMIT SWITCH HARNESS. (M) 2 L 7 2 4F A6WE 1996062000577 19960620 00577 WP 1996 6 20 USAAD96055 1 19960516 A 3350 60030451 BATTERY PACK DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 826US 48026 SAV - OVERHEAD EMERGENCY LIGHTS INOPERATIVE AT ROWS 3-7 AND 17-20. MX REPLACED THE APPLICABLE BATTERY PACKS. (M) 2 L 7 2 4F A6WE 1996062000578 19960620 00578 WP 1996 6 20 USAAD96056 1 19960504 A 3241 406256 TRANSDUCER DOUG DC9 DC981 3022081 WP OUTBOARD RT FAILED A USAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 19 809US 48041 FLT NR 1846 - MCO-PIT - 'WHEEL NOT TURNING' LIGHT CAME ON AT 85 KNOTS. REPLACED OUTBOARD RIGHT WHEEL TRANSDUCER. (M) 2 L 7 2 4F A6WE 1996062000579 19960620 00579 NE 1996 6 20 USAAD96057 2 19960519 A 7200 ENGINE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9A 52048 NE RT ENGINE FAILED A USAA E A ENGINE SHUTDOWN UNSCHED LANDING M OVER TEMP CR CRUISE 1 EA 19 926VJ 48146 707366 FLIGHT NR 8001 - CLT-GSP - RIGHT ENGINE OIL TEMP DURING CRUISE WENT TO 130 DEGREES. WENT TO 155 DEGREES AT IDLE. SHUT DOWN ENGINE. REPLACED ENGINE. (M) 2 L 7 2 4F 4 F A6WE E2EA 1996062000580 19960620 00580 WP 1996 6 20 USAAD96058 1 19960519 A 3222 16606A0191 O-RING DOUG DC9 DC931 3022065 WP NOSE GEAR BROKEN A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 934VJ 48114 FLT 345 - ATL-BWI - UPON GEAR RETRACTION, NOSE GEAR UNSAFE LIGHT REMAINED ON. CYCLED GEAR AND CONDITION REMAINED. RETU RNED TO FIELD. FOUND SCHRAEDER VALVE O-RING BROKEN. REPLACED SCHRAEDER VALVE AND O-RING. (M) 2 L 7 2 4F A6WE 1996062000581 19960620 00581 WP 1996 6 20 USAAD96059 1 19960520 A 3610 1D36227321 DUCT DOUG DC9 DC931 3022065 WP LEFT CRACKED A USAA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 EA 19 930VJ 45868 FLT NR 447 - DCA-BOS - TAIL COMPARTMENT HIGH TEMP LIGHT CAME ON DURING INITIAL CLIMB. RETURNED TO FIELD. REPLACED 8TH STAGE PNEUMATIC DUCT. (M) 2 L 7 2 4F A6WE 1996062000582 19960620 00582 EU 1996 6 20 USAAF96042 1 19960513 A 3260 201251224 DNLOCK SENSOR FOKKER F28 F28MK0100 4990807 EU LT MLG FAILED A USAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 EA 19 899US 11399 PIT - FL 8076 - ON DESCENT INTO PIT, CREW LOWERED GEAR AND RECEIVED THREE GREEN LIGHTS WHILE BLUE LIGHTS IN GEAR HANDLE REMAINED ON AND A MFDU MESSAGE THAT READ 'LEFT LG DOWNLOCK SWITCH'. AT 400 FEET THE THE AURAL WARNING FOR THE GEAR CAME ON. CREW RECYCLED GEAR AND LIGHT EXTINGUISHED. FLIGHT LANDED IN PIT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED T HE LEFT MLG PRIMARY DOWNLOCK SENSOR. (M) 2 L 7 2 4F RT 1996062000583 19960620 00583 EU 1996 6 20 USAAF96048 1 19960513 A 3350 6008905 POWER SUPPLY FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 493US 11161 CLT - MX FOUND THE AFT EXTERIOR EMERGENCY LIGHTS INOP. MAINTENANCE REPLACED THE AFT EXTERIOR POWER SUPPLY UNIT. (M) 2 L 7 2 4F RT A20EU 1996062000584 19960620 00584 EU 1996 6 20 USAAF96049 1 19960520 A 2150 220348024 AIR COND PACK FOKKER F28 F28MK0100 4990807 EU RIGHT FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 892US 11372 CHA - FLT 1421 - CREW HEARD A RUMBLING NOISE FROM RIGHT PACK EN ROUTE TO MSY. FIFTEEN MINUTES AFTER NOISE, SMOKE ALARMS WENT OFF. CREW SHUT PACK OFF, DECLARED AN EMERGENCY AND DIVERTED TO CHA. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE RIGHT AIRCO PACK ACM OIL SEAL FAILED. THE RIGHT AIRCO PACK WAS REPLACED. OPS CHECKED NORMAL. ( M) 2 L 7 2 4F RT 1996062000585 19960620 00585 EU 1996 6 20 USAAF96050 1 19960521 A 3040 EAWTC8803405 TEMP CONTROLLER FOKKER F28 F28MK0100 4990807 EU LT WINDSHIELD FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 885US 11345 MSP - FLT 1140 - WHILE CLIMBING OUT OF MSP, CREW SMELLED AN ODOR OF UNKNOWN ORIGIN. FLIGHT ATTENDANT WAS CALLED TO THE COCKPIT TO VERIFY ODOR. AT THIS TIME, SMOKE WAS SEEN EMITTING FROM THE CENTER WINDSHIELD POST. THE CREW DONNED OXYGEN MASKS AND DECLARED AN EMERGENCY. THEY TURNED OFF THE WINDSHIELD HEAT AND THE SMOKE STOPPED. THE FLIGHT WAS 60 MILES FR OM MSP AND RETURNED TO FIELD LANDING WITHOUT INCIDENT. MX CHECKED WIRING TO LEFT WINDOW AND BENEATH GLARESHIELD AND FOU ND NO EVIDENCE OF SHORTED WIRES. OPERATED SYSTEM, CHECKS OK. MX REPLACED THE FOLLOWING ITEMS PER PRECAUTIONARY MEASURE , LEFT WINDSHIELD TEMP CONTROLLER P/N EAWTC8803-405, LEFT WINDSHIELD TRANSFORMER P/N AE5751MK1. (M) 2 L 7 2 4F RT 1996062000586 19960620 00586 EU 1996 6 20 VTZA96191 1 19960510 A 7722 SG3106E14S52S CONNECTOR BAG JETSTM JETSTM3201 1500217 EU LT SLR FAILED A VTZA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 477UE 890 FLT NR 6379 - IAD-SYR - ABORTED THE TAKEOFF DUE TO THE LEFT SRL CAP LIGHT ILLUMINATING ON THE TAKEOFF ROLL. AIRCRAFT RE TURNED TO GATE WITH NO FURTHER INCIDENT. MX OPENED DMI NR 03301 IAW MEL 76-1. MX LATER CLEARED DMI NR 03301 ON 5-14-96 BY REPLACING THE T2 CONNECTOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996062000587 19960620 00587 EU 1996 6 20 VTZA96192 1 19960510 A 5270 S2902014 RESET SWITCH JETAIR JETSTM JETSTM4101 1500501 EU PAX DOOR WARNING NOT ACTIVATED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 315UE 41033 FLT 6599 - IAD-EWR - DURING CLIMB-OUT, DECLARED AN EMERGENCY AND RETURNED TO IAD DUE TO THE MAIN PASSENGER DOOR WARNING LIGHT ILLUMINATING AND AIRCRAFT NOT PRESSURIZING. AIRCRAFT LANDED WITH NO FURTHER INCIDENTS. MX OPENED DMI NR 08051 IA W MEL 53-3. MX LATER CLEARED DMI NR 08051 ON BY RESETTING THE DOOR WARNING RESET SWITCH. AIRCRAFT WAS RELEASED AND APP ROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996062000588 19960620 00588 EU 1996 6 20 VTZA96193 1 19960515 A 3260 ATG135022 UPLOCK SWITCH JETAIR JETSTM JETSTM4101 1500501 EU RT MLG FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 320UE 41043 FLT NR 6433 - IAD-EWR - DURING CLIMB-OUT, RETURNED TO IAD DUE TO THE RED GEAR HANDLE LIGHT REMAINING ILLUMINATED AFTER G EAR SELECTED UP. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENT. MX REPLACED RIGHT MAIN LANDING GAR UPLOCK SWITCH. A IRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996062000589 19960620 00589 EU 1996 6 20 VTZA96194 1 19960514 A 3260 ATG135022 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU LT MLG FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 321UE 41045 IAD-DAY - FLT 6290 - DURING CLIMB-OUT, RETURNED TO IAD DUE TO THE LEFT MAIN GEAR INTRANSIT LIGHT REMAINED ILLUMINATED AF TER LANDING GEAR SELECTED UP. A PRECAUTIONARY EMERGENCY WAS DECLARED AND GEAR WAS SELECTED DOWN WITH BOTH MAIN AND STAN DBY INDICATORS CONFIRMING GEAR DOWN AND LOCKED. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE PERFORME D SEVERAL GEAR SWINGS AND REPLACED THE LEFT MAIN UPLOCK SWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVIC E. (M) 2 L 7 2 4T RT A41NM 1996062000590 19960620 00590 EU 1996 6 20 VTZA96195 1 19960519 A 7712 31024762 TQ SIGNAL COND BAG JETSTM JETSTM3101 1500215 EU LT ENGINE OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 27 473UE 828 FLT NR 6407 - IAD-LGA - ABORTED THE TAKEOFF DUE TO THE LEFT ENGINE NOT MAKING TAKEOFF TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED THE TORQUE SIGNAL CONDITIONER. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996062000591 19960620 00591 EU 1996 6 20 VTZA96196 1 19960517 A 3150 TO WARNING JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT ACTIVATED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 306UE 41020 FLT NR 6483 - IAD-CHS - ABORTED TAKEOFF DUE TO THE TAKEOFF CONFIGURATION WARNING SYSTEM ACTIVATING DURING THE TAKEOFF RO LL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE PERFORMED OPS CHECKS, BUT COULD NOT DUPLICATE DIS REPANCIES. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996062000592 19960620 00592 EU 1996 6 20 VTZA96197 1 19960519 A 7600 21188408 EGT COMPENSATORS JETAIR JETSTM JETSTM4101 1500501 EU LT/RT ENG OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK M OVER TEMP TO TAKEOFF 1 EA 27 315UE 41033 FLT NR 6551 - IAD-CLE - ABORTED THE TAKEOFF DUE TO BOTH ENGINE EGT EXCEEDING VRL. AIRCRAFT RETURNED TO GATE WITH NO FUR THER INCIDENTS. MX ADJUSTED BOTH EGT COMPENSATORS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996062000593 19960620 00593 EU 1996 6 20 VTZA96198 1 19960519 A 7712 31024762 TQ SIGNAL COND BAG JETSTM JETSTM3201 1500217 EU LT/RT ENGINE OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 27 474UE 849 FLT NR 6172 - LYH-IAD - ABORTED TAKEOFF DUE TO BOTH ENGINES NOT MAKING TAKEOFF TORQUE. AIRCRAFT RETURNED TO GATE WITH N O FURTHER INCIDENTS. MX ADJUSTED THE TORQUE SIGNAL CONDITIONERS ON BOTH ENGINES. AIRCRAFT WAS RELEASED AND APPROVED FO R RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996062000594 19960620 00594 EU 1996 6 20 VTZA96199 1 19960521 A 2120 BAS2022315 SEAL JETAIR JETSTM JETSTM4101 1500501 EU RT WING ROOT FAILED A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 301UE 41012 FLT 6205 - IAD-MHT - DURING CLIMB-OUT, RETURNED TO IAD DUE TO THE DUCT FAIL CAP LIGHT ILLUMINATING. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MX REPLACED THE RIGHT DUCT O-RINGS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SE RVICE. (M) 2 L 7 2 4T RT A41NM 1996062000595 19960620 00595 EU 1996 6 20 VTZA96200 1 19960523 A 3150 PIN JETAIR JETSTM JETSTM4101 1500501 EU TO CONNECTOR LOOSE A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 306UE 41020 FLT NR 6532 - IAD-ORF - ABORTED TAKEOFF DUE TO THE TAKEOFF CONFIGURATION WARNING SYSTEM ACTIVATING DURING THE TAKEOFF RO LL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MX FOUND PIN AT CONNECTOR PR58R LOOSE. REINSTALLED PIN A INT O CONNECTOR, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996062000596 19960620 00596 1996 6 20 VTZA96201 4 19960523 A 3417 7000700966 ADC JETAIR JETSTM JETSTM4101 1500501 EU NR 1 FAILED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 318UE 41041 FLT NR 6485 - IAD-JFK - DURING CRUISE MADE A UNSCHEDULED LANDING BECAUSE OF A NR 1 ADC FAILED. AIRCRAFT LANDED WITH NO FURTHER INCIDENTS. MX REPLACED NR 1 ADC. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996062000597 19960620 00597 1996 6 20 VTZA96203 4 19960527 A 3416 ALTIMETER SYSTEM BAG JETSTM JETSTM3201 1500217 EU NR 1 REQ'D SERVICE A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 482UE 897 FLT NR 6332 - IAD-PIT - DURING CLIMB, AN UNSCHEDULED LANDING DUE TO NR 1 ALTIMETER FLUCTUATED PLUS/- 200 FEET IN CRUISE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE TIGHTENED FITTING AND DRAINED MOISTURE FROM SYSTEM, OPS AND LEAK CHECKED GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996062000598 19960620 00598 EU 1996 6 20 VTZA96204 1 19960527 A 2770 GUSTLOCK SWITCH JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 306UE 41020 FLT NR 6261 - IAD-EWR - ABORTED TAKEOFF DUE TO THE TAKEOFF CONFIGURATION WARNING SYSTEM ACTIVATING DURING THE TAKEOFF RO LL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MX ADJUSTED GUSTLOCK MICROSWITCH, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996062000599 19960620 00599 1996 6 20 VTZA96205 4 19960526 A 3442 7008470922 RT UNIT JETAIR JETSTM JETSTM4101 1500501 EU RADAR SYSTEM FAILED A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 327UE 41080 FLT 6416 - IAD-CHS - DURING CLIMB-OUT, RETURNED TO IAD DUE TO WEATHER RADAR INOP AND FORECASTED THUNDERSTORMS. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MX REPLACED WEATHER RADAR R/T. AIRCRAFT WAS RELEASED AND APPROVED FOR RET URN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996062000600 19960620 00600 EU 1996 6 20 VTZA96206 2 19960529 A 7320 8974575 BYPASS VALVE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RT ENG FUEL FAILED A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 470UE 814 FLT NR 6241 - IAD-PHF - DURING CLIMB, MADE AN UNSCHEDULED LANDING DUE TO RIGHT ENGINE TORQUE AND EGT FLUCTUATED IN FLIGH T. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MX REMOVED AND REPLACED TTL VALVE PLUS CLEANED ZONE 2 CANNON P LUG CONNECTOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996062000601 19960620 00601 EU 1996 6 20 VTZA96207 1 19960529 A 7722 HTMASOF2821PW CONNECTOR BAG JETSTM JETSTM3201 1500217 EU LT ENGINE DIRTY A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 489UE 908 FLT NR 6170 - IAD-EWR - ABORTED TAKEOFF DUE TO LEFT ENGINE EGT FLUCTUATION. AIRCRAFT RETURNED TO GATE WITH NO FURTHER I NCIDENTS. MAINTENANCE CLEANED ZONE 2 CANNON PLUG CONNECTOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996062000602 19960620 00602 EU 1996 6 20 VTZA96208 1 19960529 A 3260 AIR135668 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU RT MLG FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 302UE 41013 FLT NR 5531 - IAD-ORF - MADE AN UNSCHEDULED LANDING DUE TO RED GEAR HANDLE LIGHT REMAINED ILLUMINATED WITH GEAR UP. AIR CRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED RIGHT UPLOCK MICROSWITCH. OPS CHECK AND GEAR SWING OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996062000603 19960620 00603 EU 1996 6 20 WTAA960101 1 19960515 A 3260 622800200 SWITCH BAG JETSTM JETSTM3101 1500215 EU RT LANDING GEAR FAILED A WTAA O OTHER P NO WARNING INDICATION AP APPROACH 1 WP 17 401UE 729 ACV - RIGHT MAIN LANDING GEAR INTRANSIT LIGHT FAILED TO ILLUMINATE. AIRCRAFT FERRIED TO FAT FOR REPAIRS. MAINTENANCE R EPLACED RIGHT MAIN LANDING GEAR UPLOCK AND DOWNLOCK MICROSWITCHES. GEAR INDICATION NORMAL DURING GROUND CHECK. AIRCRAF T RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996062000604 19960620 00604 SO 1996 6 20 WTAA960103 1 19960517 A 3260 922AA2YA6P2722A PROX SENSOR EMB 120 EMB120RT SO RT LANDING GEAR FAILED A WTAA O OTHER N FALSE WARNING AP APPROACH 1 WP 17 454UE 120155 FAT - RIGHT MAIN LANDING GEAR 'B' SYSTEM INTRANSIT LIGHT REMAINS ILLUMINATED WITH GEAR DOWN. MX DEFERRED 'B' INDICATION SYSTEM PER MEL 32-60-1. AIRCRAFT RETURNED TO SERVICE. MX SUBSEQUENTLY CLEARED DEFERRAL BY REPLACING THE RIGHT MAIN LA NDING GEAR 'B' DOWNLOCK PROXIMITY SENSOR. (M) 2 L 7 2 4T RT A31SO 1996062000606 19960620 00606 SO 1996 6 20 WTAA960105 1 19960516 A 3040 2SC1175A CURRENT SENSOR EMB 120 EMB120RT SO LT WINDSHIELD FAILED A WTAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 17 454UE 120155 SFO - PILOT REPORTED STRONG ELECTRICAL BURNING SMELL IN COCKPIT. MX REPLACED LEFT WINDSHIELD CURRENT SENSOR. SYSTEM OP ERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996062000607 19960620 00607 SO 1996 6 20 WTAA960106 1 19960521 A 3240 BRAKES EMB 120 EMB120RT SO LANDING GEAR MALFUNCTIONED A WTAA O OTHER O OTHER LD LANDING 1 WP 17 251YV 120251 SMF - NORMAL BRAKES FAILED DURING LANDING ROLL AND TAXI. MAINTENANCE CHECKED ANTI-SKID BRAKE TRANSDUCERS. NO DEFECTS N OTED. UNABLE TO DUPLICATE DISCREPANCY. BRAKE SYSTEMS CHECK NORMAL ON LOW SPEED AND HIGH SPEED TAXI BRAKE TESTS. AIRCR AFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996062000608 19960620 00608 EU 1996 6 20 Y2PA96032 1 19960520 A 2130 MY20721205 SENSE LINE AMD FALC20 FALCOND 2720304 EU RT OUTFLOW VLV CRUSHED A a Y2PA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 823AA 228 YIP - AIRCRAFT DEPRESSURIZED ON CLIMB THROUGH 18,000 FEET. AIRCRAFT DESCENDED TO 16,000 FEET AND WAS UNABLE TO CONTROL CABIN MANUALLY. AIRCRAFT DESCENDED TO BELOW 10,000 FEET AND RETURNED, UNPRESSURIZED, TO POINT OF DEPARTURE AT YIP. UNS CHEDULED LANDING MADE AT YIP WITHOUT INCIDENT. THE RIGHT OUTFLOW VALVE SENSE LINE WAS FOUND CRUSHED. THE LINE WAS REPL ACED WITH A SERVICEABLE UNIT. THE AIRCRAFT WAS GROUND PRESSURIZED AND SYSTEM OPERATED NORMALLY. NO DEFECTS NOTED. (M) 2 L 7 2 4F A7EU 1996062000609 19960620 00609 EU 1996 6 20 Y2PA96033 1 19960521 A 5270 H20248021 SWITCH AMD FALC20 FALCOND 2720304 EU CARGO DOOR INOPERATIVE A Y2PA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 821AA 203 ELP - UNSCHEDULED LANDING, AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. AIRCRAFT RETURNED TO POINT OF DEPARTURE AT ELP. THE CARGO DOOR DOWN SWITCH WAS FOUND TO BE INOPERATIVE AND APPEARED DAMAGED. THE SWITCH WAS REPLACED AND RIGGED PER T HE AVTEC CARGO DORO MAINTENANCE MANUAL. THE AIRCRAFT WAS GROUND PRESSURIZED AND SYSTEM OPERATED NORMALLY. NO DEFECTS N OTED. (M) 2 L 7 2 4F A7EU 1996062000610 19960620 00610 EU 1996 6 20 Y2PA96036 1 19960523 A 5270 WARNING LIGHT AMD FALC20 FALCOND 2720304 EU CARGO DOOR ILLUMINATED A Y2PA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 23 817AA 233 ROA - LEVELING AT 23,000 FEET, DOOR WARNING ANNUNCIATOR LIGHT CAME ON ALONG WITH DOOR WARNING HORN AND LIGHT. CABIN NOR MAL NO LOSS OF PRESSURIZATION. AIRCRAFT DIVERTED AND MADE AN UNSCHEDULED LANDING AT ROA. CARGO DOOR WARNING SYSTEM DEF ERRED UNDER MEL TO RETURN TO YIP FOR MAINTENANCE. CARGO DOOR LATCHING MECHANISM RIGGING WAS CHECKED IAW AVCON CARGO DOO R MM WITH NO DEFECTS NOTED. DOOR WAS OPERATED SEVERAL TIMES ON GROUND WITH NO DEFECTS NOTED IN WARNING LIGHT SYSTEM. A IRCRAFT WAS RUN AND PRESSURIZED WITH NO DEFECTS NOTED IN DOOR WARNING SYSTEM. PROBLEM COULD NOT BE DUPLICATED ON GROUND . (M) 2 L 7 2 4F A7EU 1996062000611 19960620 00611 WP 1996 6 20 Y2PA96037 1 19960521 A 3260 POSITION SWITCH DOUG DC9 DC915F 3022037 WP LT MLG OUT OF ADJUST A Y2PA O OTHER N FALSE WARNING AP APPROACH 1 GL 23 195US 47017 YIP - INBOUND TO YIP THE LANDING GEAR WAS SELECTED DOWN. INDICATION WAS 3 GREEN LIGHTS WITH A GEAR DOOR UNSAFE LIGHT. T HE LANDING GEAR WAS RECYCLED AND THE GEAR DOOR UNSAFE LIGHT WENT OUT. THE AIRCRAFT LANDED AT ITS INTENDED DESTINATION A T YIP. CHECKED AND ADJUSTED THE LEFT GEAR DOOR POSITION SWITCH. OPS CHECKS OK. WORK PERFORMED IAW DC9 MM CHAPTER 32-6 0-3. (M) 2 L 7 2 4F A6WE 1996062000612 19960620 00612 1996 6 20 96DHL708005 4 19960614 A 3425 522307300 CDI BOEING 727 72725 1384006 NM LT COCKPIT FAILED A T DHLA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 708DH 18275 CAPT'S NR 1 VOR CDI IS STUCK IN THE CENTER. REMOVED AND REPLACED NR 1 CDI. 2 L 7 3 4F A3WE 1996062000613 19960620 00613 WP 1996 6 20 96UAL900384 1 19960530 A 3030 851DK AUX PITOT HEAT DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL AUX PITOT TUBE INOPERATIVE A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 1832U 46631 AUXILIARY PITOT HEAT IS COMPLETELY INOPERATIVE. BREAKER WILL NOT STAY IN. RETURNED TO SFO. SUPPLEMENTAL DATA UPDATE: HEATER INOPERATIVE. REPLACED AUX PITOT TUBE. 2 L 7 3 4F 4 F A22WE E23EA 1996062000614 19960620 00614 NM 1996 6 20 96UAL900459 1 19960618 A 2150 PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LEFT OVERHEATED A UALA O OTHER M J OVER TEMP WARNING INDICATION IN INSP/MAINT 1 WP 29 7278U 21425 LEFT PACK OVERHEATED IN AUTO MODE ON GROUND. OUTBOUND QUICK GROUND CHECK SHOWED LEFT COOLING FAN WORKING WITH RAM DOOR SHUT. STILL HAD VERY NOTICEABLE BURNT SMELL FROM RAM AIR INLET. WITH BOTH PACKS RUNNING, RIGHT PACK TEMP GAGE JUST BEL OW GREEN BAND WHILE LEFT PACK TEMP STEADILY RISING INTO YELLOW TERRITORY AFTER 30 SECONDS OF RUNNING. *S/D* MAINTENANC E GROUND CHECKED THE OPERATION OF BOTH PACKS AND THE LEFT PACK SEPARATELY AND FOUND WITHIN LIMITS. 2 L 7 3 4F 4 F A3WE E2EA 1996062000615 19960620 00615 NE 1996 6 20 96UAL900460 2 19960618 A 7261 AS3209135 O-RING SEAL BOEING 737 737291 138448W NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE DETERIORATED A UALA A E UNSCHED LANDING ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 978UA 4087 21509 687809 ON TAKEOFF, NR ONE ENGINE OIL PRESSURE WENT TO 85 POUNDS PER SQUARE INCH. IN CLIMB, OIL TEMPERATURE INCREASED. REDUCED POWER AND OIL QUANTITY WENT TO ZERO . LOW OIL PRESSURE LIGHT FLASHED. RETURNED TO FIELD. SMOKE FROM ENGINE REPORTED BY TOWER. SHUT DOWN ENGINE ON TAXI IN. OIL APPEARED TO HAVE OVERTEMPTED. 4 1/2-6 TRUMPET SEALS WERE HARD, DETERIORATE D AND LEAKING. MAIN OIL PUMP HOUSING DISTORTED AND SEVERELY WORN DUE TO EXCESSIVE HEAT. INDICATIONS OF LOW GRADE OIL F IRE. SUSPECT FIRE HEATED OIL DISTORTED PUMP AND CAUSED OIL DRAIN-BACK. OIL LOSS DUE TO LACK OF SCAVENGE AND OIL GOING OUT BREATHER. ISOLATED CASE. REPAIRED OR REPLACED PARTS AS NECESSARY. PART TOTAL CYCLES, 3,080. 2 L 7 2 4F 4 F A16WE E2EA 1996062000616 19960620 00616 NM 1996 6 20 96UAL900461 1 19960618 A 5522 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LT ELEV CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7269U 21416 T-SHAPED CRACK IN BOTTOM SURFACE OF LEFT ELEVATOR APPROXIMATELY 2.5 BY 3 INCHES, MID POINT LOCATION. *S/D* CRACK IN LT ELEVATOR LOWER SKIN REPAIRED PER UA 727 MM 55-24-01 INCLUDING INSTALLATION OF ONE BALANCE WEIGHT TO ADJUST FOR REPAIR W EIGHT BALANCE MOVEMENT. 2 L 7 3 4F 4 F A3WE E2EA 1996062000617 19960620 00617 NM 1996 6 20 96UAL900462 1 19960618 A 3350 1315 LAMP BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LT OVERWING INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7262U 21409 LEFT OVERWING MIDDLE EMERGENCY LIGHT INOPERATIVE. *S/D* CLEANED LAMP SOCKETS AND REPLACED BULBS. LIGHT OPERATION CHEC KED OKAY. 2 L 7 3 4F 4 F A3WE E2EA 1996062000618 19960620 00618 NM 1996 6 20 96UAL900463 1 19960618 A 3350 60243 LIGHT LOCTITE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 303UA 23644 EMERGENCY ESCAPE PATH LIGHT STRIP INOP FROM ROW 17 THROUGH 22 AND IN FRONT OF LEFT HAND GALLEY. RELAMPED TWO STRIPS. C HECKS O.K. 2 L 7 2 4F 4 F RT A16WE E2GL 1996062000619 19960620 00619 WP 1996 6 20 ABXA9600509 1 19960615 A 3350 43 BULB DOUG DC9 DC931 3022065 WP CABIN FAILED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 937AX 47074 DURING SERVICE CHECK FOUND BULB OUT IN OVERHEAD EMERGENCY LIGHTS IN COCKPIT. REPLACED BULB, OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1996062000620 19960620 00620 WP 1996 6 20 CALA9600841 1 19960618 A 3244 TIRE DOUG DC9 DC932 3022066 WP RT MLG CAP SEPARATED A CALA H DEACTIVATE SYST/CIRCUITS D INFLIGHT SEPARATION CR CRUISE 1 SW 09 18544 47219 THE RT HYDRAULIC QUANTITY WENT TO ZERO IN FLIGHT AND THE PRESSURE STARTED DROPPING. THE RIGHT ENGINE PUMP WAS TURNED OF F. THE PRESSURE STAYED AT ZERO AND RIGHT QUANTITY ROSE TO 6. THE GEAR AND FLAPS WERE LOWERED USING THE LEFT SYSTEM AND THE AIRCRAFT LANDED NORMALLY. MAINTENANCE FOUND THE NR 3 TIRE CAP HAD SEPARATED RESULTING IN DAMAGE TO FOUR HYDRAULIC LINES. THE NR 3 TIRE AND HYDRAULIC LINES WERE REMOVED AND REPLACED. THE NR 3 AND NR 4 BRAKE LIMITERS WHICH THE DAMAGED HYDRAULIC LINES WENT TO WERE REPLACED AS A PRECAUTIONARY MEASURE. THE HYDRAULIC SYSTEM WAS SERVICED AND LEAK CHECKS WE RE GOOD. 2 L 7 2 4F A6WE 1996062000621 19960620 00621 WP 1996 6 20 CALA9600842 1 19960618 A 2530 8101280000B OVEN DOUG DC9 DC982 3022082 WP FWD GALLEY CONTAMINATED A CALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 819NY 49479 SMOKE WAS OBSERVED COMING FROM THE FORWARD GALLEY WHILE EN ROUTE. THE FORWARD OUTBOARD OVEN WAS FOUND TO BE EXTREMELY H OT. THE OVEN CIRCUIT BREAKERS WERE DEACTIVATED AND THE SMOKE CEASED. THE AIRCRAFT WAS DIVERTED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BURNED PLASTIC MATERIAL IN RACK OF FORWARD GALLEY OUTBOARD OVEN. THE OVEN WAS PLAC ARDED INOPERATIVE, NO OTHER DEFECTS WERE FOUND. 2 L 7 2 4F A6WE 1996062000622 19960620 00622 NM 1996 6 20 CALA9600844 1 19960527 A 5330 SKIN BOEING 737 737130 1384435 NM BS 410 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 24213 19030 INSPECTION FOUND SKIN CORRODED AT BS 410, STRINGER 18L. THE CORRODED SKIN WAS CUTOUT. A REPAIR DOUBLER AND FILLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 6. 2 L 7 2 4F A16WE 1996062000623 19960620 00623 NM 1996 6 20 CALA9600845 1 19960527 A 5315 FLOORBEAM BOEING 737 737130 1384435 NM BS 294.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 24213 19030 INSPECTION FOUND CORROSION ON AFT UPPER FLANGE OF FLOORBEAM AT BS 294.5, RBL 20 TO RBL 40. THE CORRODED SECTION OF FLOO RBEAM WAS REMOVED, A NEW SECTION OF FLOORBEAM AND SPLICES WERE FABRICATED AND INSTALLED IAW SRM 51-40-4 FIGURE 1. 2 L 7 2 4F A16WE 1996062000624 19960620 00624 NM 1996 6 20 CALA9600846 1 19960527 A 5330 SKIN BOEING 737 737130 1384435 NM BS 228-360 CREASED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 24213 19030 INSPECTION FOUND SKIN CREASED FROM BS 228 TO 360, JUST ABOVE STRINGER 19R. THE DAMAGED SKIN WAS CUT OUT, REPAIR DOUBLER S AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 16. 2 L 7 2 4F A16WE 1996062000625 19960620 00625 NM 1996 6 20 CALA9600847 1 19960527 A 5313 STRINGER BOEING 737 737130 1384435 NM BS 390-410 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 24213 19030 INSPECTION FOUND CORROSION OVER AN 18 INCH SECTION OF STRINGER 22R BETWEEN BS 390 AND 410. THE CORRODED SECTION OF STRI NGER WAS REMOVED. REPAIR CHANNEL AND ANGLES WERE INSTALLED IAW SRM 53-10-3 FIGURE 1. 2 L 7 2 4F A16WE 1996062000626 19960620 00626 NM 1996 6 20 CALA9600848 1 19960527 A 5313 STRINGER BOEING 737 737130 1384435 NM BS 416 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 24213 19030 INSPECTION FOUND A 3 INCH SECTION OF STRINGER 21R CORRODED AT BS 416. THE CORRODED SECTION OF STRINGER WAS REMOVED AND REPAIR CHANNEL AND ANGLES WERE INSTALLED IAW SRM 53-10-3 FIGURE 1. 2 L 7 2 4F A16WE 1996062000627 19960620 00627 NM 1996 6 20 CALA9600849 1 19960527 A 5330 SKIN BOEING 737 737130 1384435 NM BS 394 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 24213 19030 INSPECTION FOUND SKIN DENTED BETWEEN STRINGER 23R AND 24R AT BS 394. THE DAMAGED SECTION OF SKIN WAS CUT OUT, A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 FIGURE 6. 2 L 7 2 4F A16WE 1996062000628 19960620 00628 NM 1996 6 20 CALA9600850 1 19960527 A 5330 SKIN BOEING 737 737130 1384435 NM BS 394 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 24213 19030 INSPECTION FOUND SKIN DENTED BETWEEN STRINGER 23R AND 24R AT BS 394. THE DAMAGED SECTION OF SKIN WAS CUT OUT, A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 FIGURE 6. 2 L 7 2 4F A16WE 1996062000629 19960620 00629 WP 1996 6 20 CKSA96058 1 19960607 A 2612 57775621 FIRE LOOP DOUG DC8 DC8F55 3021928 WP NR 2 ENGINE OUT OF POSITION A CKSA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 6161M 45762 KMIA - FLT 75568 - NR 2 ENGINE FIRE WARNING CAME ON CLIMBING THROUGH 12,000 FEET LIGHT AND BELL STOPPED IMMEDIATELY AFTE R RETARDING THROTTLE TO IDLE. FIRE TEST OK. ADJUSTED LOOP. SYSTEM CHECKS NORMAL PER MM CHAPTER 26-10-0. (M) 2 L 7 4 4F 4A25 1996062000630 19960620 00630 WP 1996 6 20 CKSA96059 1 19960614 A 2612 4W15H24 FIREWIRE DOUG DC8 DC863F 302198F WP NR 3 ENGINE DAMAGED A CKSA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 GL 23 811CK 46147 KMIA - FLT 75848 - SHUTDOWN NR 3 ENGINE AT 1132Z DUE TO FIREWARNING. FIRE WARNING STOPPED WHEN FUEL SHUTOFF. REPAIRED AND REROUTEDDAMAGED WIRE ON RIGHT SIDE LOOP CONNECTOR ON ENGINE. RAN ENGINE AT TAKEOFFPOWER. CHECKS GOOD ON GROUND. N O EVIDENCE OF FIRE FOUND. (M) 2 L 7 4 4F 4A25 1996062000631 19960620 00631 WP 1996 6 20 CKSA96060 1 19960612 A 2612 3777644 FIRE CONNECTOR DOUG DC8 DC8F55 3021928 WP NR 2ENGINE DIRTY A CKSA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 6161M 45762 KMIA- FLT 75794 - NR 2 ENGINE FIRE WARNING INDICATION ON CLIMB-OUT.FIRE LIGHT WENT OUT IMMEDIATELY UPON RETARDING THROTT LE. LIGHT REMAINED OUTAFTER RETURNING THROTTLE CRUISE POWER. ALL OTHER ENGINE INDICATIONS NORMALAND NR 2 ENGINE FIRE W ARNING TEST CHECKED GOOD. CLEANED CANNON PLUGS TO NR2 FIRE LOOP SYSTEM AND CHECKED ALL LOOPS. OPS CHECKED NORMAL PER C HAPTER26-00. (M) 2 L 7 4 4F 4A25 1996062000632 19960620 00632 1996 6 20 DHL96741003 4 19960617 A 3417 ADC BOEING 727 7272Q9 138448M NM NR 2 MALFUNCTIONED A DHLA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 741DH 21931 AT TAKEOFF, FIRST OFFICERS AIRSPEED, ALTITUDE AND RATE OF CLIMB INDICATORS FLAGGED. FOUND AIR DATA NR 2 COMPUTER CIRCUI T BREAKER POPPED AND WOULD NO RESET. FOUND METAL SHAVINGS ON BENCH PLUG. CLEANED WITH CONTACT CLEANER AND BLEW OUT BEN CH PLUG WITH NITROGEN, TESTED SYSTEM, OPS CHECKS NORMAL MM 34-12-0. 2 L 7 3 4F RT A3WE 1996062000633 19960620 00633 WP 1996 6 20 DHL96804009 1 19960612 A 3411 A4144710027 PITOT SYST DOUG DC8 DC873F 302199F WP LEFT MALFUNCTIONED A T DHLA O OTHER O OTHER CL CLIMB 1 SO 01 804DH 46124 ON CLIMBOUT, CAPTAINS AIRSPEED AND ALTIMETER INDICATORS READ LOW AT CRUISE FL250, 1200FT. LOWER AT 300KTS, 20KTS SLOWER . REMOVED AND REPLACED CAPTAINS AIRSPEED INDICATOR PITOT, SYS OPS NORMAL MM 34-10. 2 L 7 4 4F RT 4A25 1996062000634 19960620 00634 NM 1996 6 20 SWAA960532 1 19960617 A 5311 FRAME BOEING 737 7372H4 138448C NM FWD CARGO DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21721 DURING SCHEDULED D-CHECK, FOUND FWD CARGO BAY FRAME DENTED BEYOND LIMITS. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000635 19960620 00635 NM 1996 6 20 SWAA960533 1 19960617 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 492 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21721 DURING SCHEDULED D-CHECK, FOUND UPPER FLANGE OF FUSE FRAME CRACKED AT BS 492, RBL 36, WL 162. REPAIRED PER TRAMCO EWO 9 6-0249. 2 L 7 2 4F A16WE 1996062000636 19960620 00636 NM 1996 6 20 SWAA960534 1 19960617 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 420 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21721 DURING SCHEDULED D-CHECK, FOUND FUSE FRAME CRACKED AT BS 420 AT S26L, ABOVE STRINGER CLIP. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000637 19960620 00637 NM 1996 6 20 SWAA960535 1 19960617 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21721 DURING SCHEDULED D-CHECK, FOUND FUSE FRAMES CRACKED IN RADIUS AT BS 178, WL 207, RBL 29 AND LBL 29. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000638 19960620 00638 NM 1996 6 20 SWAA960536 1 19960617 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 188 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21721 DURING SCHEDULED D-CHECK, FOUND FUSE FRAME CRACKED IN RADIUS AT BS 188, S16R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000639 19960620 00639 NM 1996 6 20 SWAA960537 1 19960617 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 344 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21721 DURING SCHEDULED D-CHECK, FOUND FUSE FRAME CRACKED AT BS 344, LBL 45, WL 170. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000640 19960620 00640 NM 1996 6 20 SWAA960538 1 19960617 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 188 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21721 DURING SCHEDULED D-CHECK, FOUND FUSE FRAME CRACKED AT BS 188, WL 207, LBL 28. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000641 19960620 00641 NM 1996 6 20 SWAA960539 1 19960617 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 328 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21721 DURING SCHEDULED D-CHECK, FOUND FUSE FRAMES CRACKED AT BS 328, RBL 54, WL 183 AND AT BS 360, RBL 55, WL 184. REPLACED P ER BOEING SRM. 2 L 7 2 4F A16WE 1996062000642 19960620 00642 NM 1996 6 20 SWAA960540 1 19960617 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 597 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21721 DURING SCHEDULED D-CHECK, FOUND FUSE FRAME CRACKED AT BS 597, S17R, WL 208. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000643 19960620 00643 NM 1996 6 20 SWAA960541 1 19960617 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21721 DURING SCHEDULED D-CHECK, FOUND FUSE SKIN CRACKED AT BS 178, AT S17R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000644 19960620 00644 NM 1996 6 20 SWAA960542 1 19960617 A 5320 CREASE BEAM BOEING 737 7372H4 138448C NM BS 639 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21721 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM I/B CHORD CRACKED AT BS 639, RBL 65, WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000645 19960620 00645 NM 1996 6 20 SWAA960543 1 19960617 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 380-400 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21721 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 380 TO 400, BELOW S19R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000646 19960620 00646 NM 1996 6 20 SWAA960544 1 19960617 A 5320 SHEAR TIE BOEING 737 7372H4 138448C NM BS 1104 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21721 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 1104, BELOW S5L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000647 19960620 00647 NM 1996 6 20 SWAA960545 1 19960617 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 827 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21721 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 827, S27R, WL 155. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000648 19960620 00648 NM 1996 6 20 SWAA960546 1 19960617 A 5320 SPLICE BOEING 737 7372H4 138448C NM BS 907 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21721 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CORRODED AT BS 907, S26L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000649 19960620 00649 NM 1996 6 20 SWAA960547 1 19960617 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21721 DURING SCHEDULED D-CHECK, FOUND STRINGER CRACKED AT BS 727B, S9R. REPLACED STRINGER SECTION PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000650 19960620 00650 NM 1996 6 20 SWAA960548 1 19960617 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 921 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21721 DURING SCHEDULED D-CHECK, FOUND FUSELAGE DENTED AT BS 921, BETWEEN S22 AND 23R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000651 19960620 00651 NM 1996 6 20 SWAA960549 1 19960617 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 912-921 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21721 DURING SCHEDULED D-CHECK, FOUND FUSELAGE DENTED AT BS 912 TO 921, RBL 0 TO 19, FROM S24R TO S27R. REPAIRED PER BOEING S RM. 2 L 7 2 4F A16WE 1996062000652 19960620 00652 NM 1996 6 20 SWAA960550 1 19960617 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 850-865 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21721 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED FROM BS 850 TO 865, S25 TO 27R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000653 19960620 00653 NM 1996 6 20 SWAA960551 1 19960617 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21721 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727B PLUS 2, AT S18L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000654 19960620 00654 NM 1996 6 20 SWAA960552 1 19960617 A 5320 STRAP BOEING 737 7372H4 138448C NM BS 1138 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21721 DURING SCHEDULED D-CHECK, FOUND FUSELAGE STRAP CRACKED AT BS 1138, S12L. REPAIRED PER BOEING SRM AND BOEING DRAWING 65C 35132. 2 L 7 2 4F A16WE 1996062000655 19960620 00655 NM 1996 6 20 SWAA960553 1 19960617 A 5320 SHEAR TIE BOEING 737 7372H4 138448C NM BS 1138 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21721 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 1138, LBL 27, WL 261. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000656 19960620 00656 NM 1996 6 20 SWAA960554 1 19960617 A 5320 CHORD BOEING 737 7372H4 138448C NM BS 1154 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21721 DURING SCHEDULED D-CHECK, FOUND LOWER CHORD CRACKED AT BS 1154, AT S5L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000657 19960620 00657 NM 1996 6 20 SWAA960555 1 19960617 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 1178 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21721 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 1178, LBL 4. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000658 19960620 00658 NM 1996 6 20 SWAA960556 1 19960617 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 1134 PUNCTURES A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21721 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN PUNCTURED AT BS 1134. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000659 19960620 00659 NM 1996 6 20 SWAA960557 1 19960617 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 354 DAMAGE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21721 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN LIGHTNING STRIKE DAMAGE AT BS 354, S17 TO 18. REPAIRED PER TRAMCO EWO 96- 0279. 2 L 7 2 4F A16WE 1996062000660 19960620 00660 NM 1996 6 20 SWAA960558 1 19960617 A 5320 WEB BOEING 737 7372H4 138448C NM BS 135 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21721 DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AT BS 135, LBL 8, WL 187. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000661 19960620 00661 NM 1996 6 20 SWAA960559 1 19960617 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 440 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21721 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, AT S21L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000662 19960620 00662 NM 1996 6 20 SWAA960560 1 19960617 A 5320 MOPSILL BOEING 737 7372H4 138448C NM BS 304-360 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21721 DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR MOPSILL CORRODED AT BS 304 TO 360, WL 208, LBL 56. REPAIRED PER BOEING S RM. 2 L 7 2 4F A16WE 1996062000663 19960620 00663 NM 1996 6 20 SWAA960561 1 19960617 A 5315 FLOOR BEAM BOEING 737 7372H4 138448C NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21721 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 344, LBL 50 TO RBL 8. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996062000664 19960620 00664 NM 1996 6 20 SWAA960562 1 19960617 A 5330 SKIN BOEING 737 7372H4 138448C NM SERV DR CUTOUT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21721 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SERVICE DOOR LOWER HINGE CUTOUT. REPAIRED PER TRAMCO 96-02 70. 2 L 7 2 4F A16WE 1996062000665 19960620 00665 NM 1996 6 20 SWAA960563 1 19960617 A 5320 SPLICE BOEING 737 7372H4 138448C NM BS 907 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21721 DURING SCHEDULED D-CHECK, FOUND I/B SIDE OF STRINGER SPLICE CORRODED AT BS 907, LBL 12, WL 166 AT S26L. REPLACED PER BO EING SRM. 2 L 7 2 4F A16WE 1996062000666 19960620 00666 NM 1996 6 20 SWAA960564 1 19960618 A 2131 7638101 CONTROLLER BOEING 737 7373G7 1384595 NM E/E BAY INOPERATIVE A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 683SW 24008 AFTER TAKEOFF, CREW WAS UNABLE TO PRESSURE AIRCRAFT, RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. REPLACED PRESSURE CONTROLLER AND OP CHECKED SYSTEM PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996062000667 19960620 00667 WP 1996 6 20 TC8A046 1 19960616 A 2424 WIRE DOUG DC8 DC851 3021920 WP NR 4 ENGINE BROKEN A TC8A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 805CK 45649 NR 1, 2, 3 GENERATOR WILL NOT STAY PARALLELED UNDER LOAD. REPAIRED BROKEN WIRE ON NR 4 ENGINE POWER RELAY AND GENERATOR IAW 24-50, FUNCTIONAL CHECKED AND OPS CHECK NORMAL. 2 L 7 4 4F 4A25 1996062000668 19960620 00668 WP 1996 6 20 TC8A96044 1 19960603 A 2130 FLOW CONTL VLV DOUG DC8 DC8F55 3021928 WP CABIN MALFUNCTIONED A TC8A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 808CK 45817 AFTER TAKEOFF, UNABLE TO PRESSURIZE THE SYSTEM DUE FLOW CONTROL VALVES WEREN'T WORKING PROPERLY. CHECKED FLOW CONTROL V ALVES, CONNECTIONS, RESEATED C/B'S AND TESTED ON GROUND OK. 2 L 7 4 4F 4A25 1996062000669 19960620 00669 WP 1996 6 20 TC8A96045 1 19960613 A 2410 688228B CSD DOUG DC8 DC851 3021920 WP PWA JT3D JT3D3B 52039 NE NR 4 ENGINE LEAKING A TC8A E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 23 805CK 45649 645762 PRECAUTIONARY ENGINE SHUTDOWN NR 4, ERRATIC OIL PRESSURE, OIL PRESSURE LIGHT, GOOD OIL QUANTITY AND TEMP. TROUBLESHOT A ND FOUND NR CSD DISCONNECT LEAKING. REMOVED AND REPLACED NR 4 CSD DISCONNECT. ALSO, PULLED NR 4 ENGINE OIL SCREEN, NO DEFECTS NOTED. INSTALLED OIL SCREEN ASSEMBLY AS PER MM 72-00, ENGINE RUN, OIL PRESSURE, TEMP AND QUANTITY WITHIN LIMITS , NO LEAKS NOTED. 2 L 7 4 4F 4 F 4A25 1E8 1996062000670 19960620 00670 NM 1996 6 20 VASI9606001 1 19960526 A 3350 20131 BATTERY PACK BOEING 737 737204 1384458 NM CABIN DISCHARGED A VSTA K NONE L NO TEST IN INSP/MAINT 1 WP 07 313VA 19711 SEVERAL EMERGENCY ESCAPE TRACK LIGHTS INOP, FWD CABIN. REMOVED AND REPLACED EMERGENCY ESCAPE LIGHT BATTERY PACK, OPS CH ECK GOOD. 2 L 7 2 4F A16WE 1996062000671 19960620 00671 NE 1996 6 20 WWMA9600051 2 19960614 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LEFT FLAMED OUT A A WWMA O OTHER X ENGINE FLAMEOUT DE DESCENT 1 WP 15 231LN 340B231 DURING DESCENT FROM 17000 FT TO 15000 FT WITH TORQUE AT 60 PERCENT AND BEING SLIGHTLY RETARDED TO 55 PERCENT, THE LEFT E NGINE FLAMED OUT WITH A LOUD BANG. ALL GAUGES INDICATED FLAME-OUT. AUTO RELIGHT ENGAGED AND THE ENGINE RELIT AND RETUR NED TO NORMAL. DURIING THE RETARDATION OF LEFT POWER LEVER AT 55 PERCENT TO 50 PERCENT THE CREW REPORTED A TORQUE SURG E OF APPROXMATELY 5 PERCENT WITH AUDIBLE ENGINE FULX. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED THE LE FT ANTI-ICE VALVE AND PERFORMED AN ENGINE COMPRESSOR WASH. THE ENGINE WAS BORESCOPE, INSPECTED WITH NO DEFECTS FOUND. T HE AIRCRAFT WAS RETURNED TO SERVICE WITH NO FURTHER PROBLEMS REPORTED. 2 L 7 2 4T 4 T RT A52EU E8NE 1996062000672 19960620 00672 EU 1996 6 20 WWMA960052 1 19960618 A 2540 17000375 TANK ASSY BAG JETSTM JETSTM3201 1500217 EU CABIN DISLOCATED A WWMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 15 949AE 949 THE CREW REPORTED A STRONG SMELL OF LAVATORY FLUSHING CHEMICAL IN THE CABIN. THEY NOTED IT SEEMED LIKE EITHER A CHEMICA L WAS LEAKING INTO THE CABIN OR THE LAV KEPT ON FLUSHING ON ITS OWN. MAINTENANCE FOUND THE TANK TO BE POSITIONED ON THE LIP OF ITS TRAY AND A SLIGHT AMOUNT OF FLUID IN THE TRAY ONLY. THE TANK WAS REPOSITIONED AND THE FLUID WAS CLEANED. P ERFORMED OPERATIONAL CHECKS AND ALL WERE NORMAL. 2 L 7 2 4T RT A56EU 1996062000673 19960620 00673 EU 1996 6 20 HCMA9620 1 19960604 A 6520 350A33215300 HINGE LAMINATE SNIAS 350 AS350B2 8680813 EU T/R CRACKED E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 992BH 477 2889 REAR ROTOR LAMIFICATION IS CRACKED. 1 G 7 1 3U H9EU 1996062000674 19960620 00674 EU 1996 6 20 HCMA9621 1 19960605 A 6520 350A33215300 HINGE LAMINATE SNIAS 350 AS350B2 8680813 EU T/R CRACKED E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 972BH 462 2804 REAR ROTOR LAMIFICATION IS CRACKED. 1 G 7 1 3U H9EU 1996062000675 19960620 00675 EU 1996 6 20 HCMA9623 1 19960605 A 6520 350A33215300 LAMIFFCATION SNIAS 350 AS350BA 8680817 EU T/R CRACKED E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 532BH 610 2494 REAR ROTOR LAMIFICATION IS CRACKED. 1 G 7 1 3U NC H9EU 1996062000676 19960620 00676 EU 1996 6 20 HCMA9624 1 19960605 A 6520 350A33215300 LAMIFICATION SNIAS 350 AS350BA 8680817 EU T/R CRACKED E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 532BH 213 2494 REAR ROTOR LAMIFICATION IS CRACKED. 1 G 7 1 3U NC H9EU 1996062000677 19960620 00677 EU 1996 6 20 HCMA9625 1 19960605 A 6230 EMRL8RSP3D BEARING SNIAS 350 AS350BA 8680817 EU M/R WORN EXCESS E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 532BH 456 2494 BEARING WORN EXCESSIVELY. 1 G 7 1 3U NC H9EU 1996062000678 19960620 00678 EU 1996 6 20 HCMA9626 1 19960606 A 2840 31896450 TRANSMITTER SNIAS 350 AS350BA 8680817 EU FUEL SYS DEFECTIVE E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 532BH 329 2494 PRESSURE TRANSMITTER FLUCTUATES AND READS LOW. 1 G 7 1 3U NC H9EU 1996062000679 19960620 00679 1996 6 20 HCMA9627 4 19960606 A 3414 3839949002 INDICATOR SNIAS 350 AS350B2 8680813 EU COCKPIT AIR SPD DEFECTIVE E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 992BH 757 2889 INDICATOR DOES NOT ZERO. WILL NOT READ BELOW 63 KTS. 1 G 7 1 3U H9EU 1996062000680 19960620 00680 EU 1996 6 20 HCMA9628 1 19960606 A 6520 350A33215300 BEARING SNIAS 350 AS350BA 8680817 EU T/R WORN EXCESS E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 642BH 977 2495 PART IS WORN EXCESSIVELY. 1 G 7 1 3U NC H9EU 1996062000681 19960620 00681 EU 1996 6 20 HCMA9629 1 19960606 A 6520 350A33215300 BEARING SNIAS 350 AS350BA 8680817 EU T/R WORN EXCESS E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 642BH 736 2495 PART IS WORN EXCESSIVELY. 1 G 7 1 3U NC H9EU 1996062000682 19960620 00682 EU 1996 6 20 HCMA9630 1 19960607 A 6410 355A09103601 BEARING SNIAS 350 AS350B2 8680813 EU T/R CRACKED E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 972BH 862 2804 BEARING IS CRACKED BEYOND LIMITS. 1 G 7 1 3U H9EU 1996062000683 19960620 00683 EU 1996 6 20 HCMA9631 1 19960610 A 6520 350A33215300 LAMIFICATION SNIAS 350 AS350BA 8680817 EU T/R WORN EXCESS E HCMA K NONE O OTHER NR NOT REPORTED 1 WP 13 312B 672 2243 PART IS WORN EXCESSIVELY. REMOVED AND REPLACED. 1 G 7 1 3U NC H9EU 1996062000684 19960620 00684 SW 1996 6 20 HEEA967208 1 19960509 A 6730 206076062003 CYLINDER BELL 206 206L3 1182108 SW M/R LEAKING E HEEA K NONE K FLUID LOSS NR NOT REPORTED 1 SW 03 3116P 14929 51530 AFT BEARING COMING UNSTAKED-LEAKING. 1 G 7 1 3U H2SW 1996062000685 19960620 00685 SW 1996 6 20 HEEA967210 1 19960509 A 5510 206023119151 STABILIZER ASSY BELL 206 206L1 1182107 SW LT & RT SIDE SEPARATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2125M 45649 SEPARATED ON L/H AND R/H SIDE AT BOTTOM EDGE. 1 G 7 1 3U H2SW 1996062000686 19960620 00686 SW 1996 6 20 HEEA967211 1 19960509 A 7722 212075067105 INDICATOR BELL 412 412 1182202 SW COCKPIT ITT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2298Z 33077 ITT INDICATOR INTERNAL LIGHT INOPERATIVE. 1 G 7 2 4U H4SW 1996062000687 19960620 00687 SW 1996 6 20 HEEA967212 1 19960509 A 2436 206075447007 VOLT REGULATOR BELL 206 206L3 1182108 SW DC SYS DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 4282Z 51499 GENERATOR WILL NOT COME ON LINE. 1 G 7 1 3U H2SW 1996062000688 19960620 00688 1996 6 20 HEEA967213 4 19960509 A 3416 1003511326 ALTIMETER BELL 412 412 1182202 SW COCKPIT CASE LEAK E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2298Z 33077 EXCESSIVE CASE LEAK AND 12 MONTH INSPECTION DUE. 1 G 7 2 4U H4SW 1996062000689 19960620 00689 NE 1996 6 20 HEEA967214 1 19960509 A 7810 7630507003044 EJECTOR SKRSKY S76 S76A 8143006 NE EXHAUST CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5426U 760167 EJECTOR IS CRACKED. 1 G 7 2 3U H1NE 1996062000691 19960620 00691 SW 1996 6 20 HEEA967216 1 19960509 A 6320 206040156101 SEAL ASSY BELL 206 206L3 1182108 SW M/R GR BOX CRACKED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 6603X 51412 FOUND CRACK ACROSS CARBON SEAL. SENT TO MAGNETIC SEAL CORP. FOR INSPECTION AND REPAIR. 1 G 7 1 3U H2SW 1996062000692 19960620 00692 SW 1996 6 20 HEEA967217 1 19960509 A 6710 214001347005 ACTUATOR BELL 412 412 1182202 SW M/R CONTROL STICKING E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3893P 33012 ROTARY ACTUATOR NOT RELEASING INTERMITTENTLY. 1 G 7 2 4U H4SW 1996062000693 19960620 00693 SW 1996 6 20 HEEA967218 1 19960509 A 6710 214001347005 ACTUATOR BELL 412 412 1182202 SW M/R MALFUNCTION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3893P 33012 ROTARY ACTUATOR INOPERATIVE. BINDING CYCLIC STICK AND NOT RELEASING FULLY WITH FORCE TRIM ON. 1 G 7 2 4U H4SW 1996062000694 19960620 00694 1996 6 20 HEEA967220 4 19960509 A 2370 9806019001 CVR SKRSKY S76 S76A 8143006 NE COCKPIT FAIL TEST E HEEA K NONE L NO TEST NR NOT REPORTED 1 SW 03 1547D 2644 760077 CVR WILL NOT COMPLETE TEST SEQUENCE AUDIOS AND NO TEST LIGHT. 1 G 7 2 3U H1NE 1996062000695 19960620 00695 1996 6 20 HEEA967222 4 19960509 A 3120 JB15307 CLOCK BOLKMS 105 BO105S 5626006 EU COCKPIT BROKEN E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 624MB S751 STOPPER FOR WINDER IS BROKEN. 1 G 7 2 3U H3EU 1996062000696 19960620 00696 1996 6 20 HEEA967223 4 19960509 A 3421 1113034 INDICATOR SKRSKY S76 S76A 8143006 NE COCKPIT ATTITUDE DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 911MJ 760231 INDICATOR RATCHETS IN ROLL. 1 G 7 2 3U H1NE 1996062000697 19960620 00697 SW 1996 6 20 HEEA967224 1 19960509 A 6720 412001304101 SERVO ASSY BELL 412 412 1182202 SW AUTO FLIGHT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2261D 33076 SERVO KICKING IN FLIGHT. 1 G 7 2 4U H4SW 1996062000699 19960620 00699 EU 1996 6 20 HEEA967226 1 19960509 A 2422 SPS1607A STATIC INVERTER BOLKMS 117 BK117B2 5626013 EU AC SYS FAN MISSING E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 136AE 1953 7234 INVERTER BLOWER FAN IS MISSING AT END OPPOSITE FROM CANNON PLUG. 1 G 7 2 3U NC H13EU 1996062000700 19960620 00700 GL 1996 6 20 HEEA967227 2 19960514 A 7250 23007238 NOZZLE 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL NR 1 VANES CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911FL CAT25377 S717 CAE822238F ENGINE REMOVED DUE TO EXCESSIVE SMOKE ON SHUTDOWN. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: CRACKED AND B OWED BEYOND SERVICEABLE LIMITS ON #1 NOZZLE VANES. REPLACED DISCREPANT PART. 1 G 7 2 3U 3 U H3EU E4CE 1996062000701 19960620 00701 GL 1996 6 20 HEEA967228 2 19960514 A 7250 23038218 NOZZLE VANES 6898735 BELL 206 206B3 1181506 SW ALLSN 250C 250C20B 03013 GL 1ST STAGE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2268V CAT40337 3605 CAE834648 ENGINE REMOVED DUE TO STRIPPED THREADS IN OIL OUT PORT. TURBINE DISASSEMBLED DUE TO LOW POWER ON TEST CELL. UPON INSPE CTION OF TURBINE PARTS NOTED THE FOLLOWING: CRACKED BEYOND SERVICEABLE LIMITS ON NR 1 NOZZLE VANES. REPLACED DISCREPAN T PART. 1 G 7 1 3U 3 U H2SW E4CE 1996062000702 19960620 00702 GL 1996 6 20 HEEA967229 2 19960514 A 7250 23031938 NOZZLE 6898735 BELL 206 206B3 1181506 SW ALLSN 250C 250C20B 03013 GL NR 2 CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 CAT33392 TURBINE REMOVED DUE TO LOW POWER ON TEST CELL. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: CRACKED BEYOND SE RVICEABLE LIMITS ON #2 NOZZLE BRAZEMENT BETWEEN DIAPHRAGM AND VANE INNER BAND. REPLACED DISCREPANT PART. 1 G 7 1 3U 3 U H2SW E4CE 1996062000703 19960620 00703 SW 1996 6 20 HEEA967230 1 19960514 A 6520 212040144101 BEARING 412040002113 BELL 412 412 1182202 SW T/R DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2258F 2385 ANG00052 33073 DUPLEX BEARING CAGES SQUEEZE ON INNER RACE OF BEARING CAUSING A BIND ON INNER RACE AND DOESN'T TURN FREELY. 1 G 7 2 4U H4SW 1996062000704 19960620 00704 SW 1996 6 20 HEEA967231 1 19960514 A 6410 206010765001 BEARING 206016201127 BELL 206 206L1 1182107 SW T/R BLADE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 83MT 663 SEEMEMO 45492 INBOARD BEARINGS CRACKED ON BOTH BLADES S/N CS5188 AND CS5190. 1 G 7 1 3U H2SW 1996062000705 19960620 00705 EU 1996 6 20 HEEA967232 1 19960514 A 6730 704A34240015 ACCUMULATOR SNIAS 350 AS350B2 8680813 EU SERVICE VALVE DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 3017 2771 TAIL ROTOR SERVO ACCUMULATOR SERVICING VALVE HAS STUCK STEM, UNABLE TO CHARGE WITH NITROGEN. 1 G 7 1 3U H9EU 1996062000706 19960620 00706 GL 1996 6 20 HEEA967233 2 19960515 A 7313 6899001 FUEL NOZZLE BELL 230 230 1182149 SW ALLSN 250C 250C30G2 03013 GL ENGINE DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 4981 23009 CAE898226 REMOVED FUEL NOZZLE DUE TO CAUSING HUNG STARTS AND DELAYED LIGHT OFF. UPON INSPECTION OF FUEL NOZZLE FOUND MODERATE STR EAKS IN SPRAY PATTERN, FOUND EXCESSIVE CARBON BUILD UP BETWEEN INNER TIP AND TIP NUT UNDER MAGNIFICATION AFTER ACCUMULAT ING 8:05SINCE LAST CLEANING AND INSPECTION. CLEANED, BENCH CHECKED, CALIBRATED AND FOUND ACCEPTABLE FOR RETURN TO SERVI CE. 1 G 7 2 3U 3 U NC H9SW E1GL 1996062000708 19960620 00708 GL 1996 6 20 HEEA967235 2 19960515 A 7230 23056634 GEARSHAFT 23051643 BELL 206 206L3 1182108 SW ALLSN 250C 250C30S 03013 GL SPUR ADAPTER STEPWEAR E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3207Q 933 CAC90059 51540 CAE890166 ENGINE REMOVED DUE TO TURBINE CYCLED OUT #2 WHEEL AND CRACKED SCROLL. UPON INSPECTION OF COMPRESSOR PARTS NOTED THE FOL LOWING: STEP WEAR BEYOND SERVICEABLE LIMITS ON SPUR ADAPTER GEARSHAFT FORWARD SPLINES. REPLACED DISCREPANT PARTS. 1 G 7 1 3U 3 U H2SW E1GL 1996062000709 19960620 00709 GL 1996 6 20 HEEA967236 2 19960515 A 7230 230052712 SPLINE ADAPTER 23051643 BELL 206 206L3 1182108 SW ALLSN 250C 250C30S 03013 GL COMPRESSOR STEPWEAR E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3207Q 933 CAC90059 51540 CAE890166 ENGINE REMOVED DUE TO TURBINE CYCLED OUT #2 WHEEL AND CRACKED SCROLL. UPON INSPECTION OF COMPRESSOR PARTS NOTED THE FOL LOWING: STEP WEAR BEYOND SERVICEABLE LIMITS ON SPLINE ADAPTER INTERNAL SPLINES. REPLACED DISCREPANT PARTS. 1 G 7 1 3U 3 U H2SW E1GL 1996062000710 19960620 00710 GL 1996 6 20 HEEA967237 2 19960515 A 7230 23004513 CARBON SEAL 23051643 BELL 206 206L3 1182108 SW ALLSN 250C 250C30S 03013 GL COMPRESSOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3207Q 933 CAC90059 51540 CAE890166 ENGINE REMOVED DUE TO TURBINE CYCLED OUT #2 WHEEL AND CRACKED SCROLL. UPON INSPECTION OF COMPRESSOR PARTS NOTED THE FOL LOWING: WORN BEYOND SERVICEABLE LIMITS ON CARBON SEAL ASSY. TANGS AND TANG SLOTS. REPLACED DISCREPANT PARTS. 1 G 7 1 3U 3 U H2SW E1GL 1996062000711 19960620 00711 SW 1996 6 20 HEEA967238 1 19960515 A 6320 206040021005 GEAR 206040004107 BELL 206 206L3 1182108 SW M/R GEAR BOX CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6161A 4477 A109 51611 AT NORMAL OVERHAUL FOUND CRACK INDICATIONS. 1 G 7 1 3U H2SW 1996062000712 19960620 00712 SW 1996 6 20 HEEA967239 1 19960515 A 6320 400040041103 SHAFT 206040004107 BELL 206 206L3 1182108 SW M/R GR BOX CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6161A 4477 A109 51611 AT NORMAL OVERHAUL FOUND CRACK INDICATIONS. 1 G 7 1 3U H2SW 1996062000713 19960620 00713 SW 1996 6 20 HEEA967240 1 19960515 A 6320 NAS66051 BOLT 206040004107 BELL 206 206L3 1182108 SW M/R GR BOX CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6161A 4477 A109 51611 AT NORMAL OVERHAUL FOUND MR GEAR BOX BOLT WITH CRACK INDICATIONS. 1 G 7 1 3U H2SW 1996062000714 19960620 00714 NE 1996 6 20 HEEA967241 1 19960515 A 6410 7610105101041 BLADE SKRSKY S76 S76A 8143006 NE T/R DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 8348 760035 RATTLING NOISE IN OUTER END OF BLADE. 1 G 7 2 3U H1NE 1996062000715 19960620 00715 NE 1996 6 20 HEEA967242 2 19960515 A 7314 108600A5 FUEL PUMP BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE ENGINE PITTED SPLINE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8765J 7054 FUEL PUMP HAS PITTED SPLINES. 1 G 7 2 3U 3 U H13EU E5NE 1996062000716 19960620 00716 SW 1996 6 20 HEEA967243 1 19960515 A 6220 412010179105 CONE 412010100193 BELL 412 412 1182202 SW M/R HUB COATING SCORED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2258F 3155 AAD00024 33073 TEFLON COATING SCORED. SENT TO BELL HELICOPTER TEXTRON FOR INSPECTION AND REPAIR. 1 G 7 2 4U H4SW 1996062000717 19960620 00717 1996 6 20 HEEA967244 4 19960515 A 3442 RADAR RT BELL 230 230 1182149 SW RADAR MALFUNCTION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 230UN 23009 RT UNIT INTERMITTENT OPERATION. 1 G 7 2 3U NC H9SW 1996062000718 19960620 00718 1996 6 20 HEEA967245 4 19960515 A 3451 066106901 INDICATOR BELL 230 230 1182149 SW COCKPIT DME INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 230UN 2966 23009 INDICATOR READ OUT INOPERATIVE 1 G 7 2 3U NC H9SW 1996062000719 19960620 00719 NE 1996 6 20 HEEA967246 1 19960515 A 6220 7610308014102 BRACKET SKRSKY S76 S76A 8143006 NE M/R HUB WEIGHT BROKE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545X 760050 DURING THE PROCESS OF LOOSENING M/R WEIGHT BOLT FOR ROUTINE M/R TRACK AND BALANCE, HUB BALANCE BRACKET BROKE IN TWO PIEC ES. BREAK WAS IN AREA OF 90 DEGREE BEND APPROX. 10% OF FRACTURE AREA APPEARS TO BE A FRESH BREAK. INSPECTED M/R WEIGHT STICK-UPAND FOUND TO BE INSTALLED PROPERLY. 1 G 7 2 3U H1NE 1996062000720 19960620 00720 SW 1996 6 20 HEEA967247 1 19960517 A 3210 222036050104 FAIRING ASSY BELL 230 230 1182149 SW GEAR ASSY CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 3077 23009 FAIRING ASSY IS CRACKED AND WORN. 1 G 7 2 3U NC H9SW 1996062000721 19960620 00721 SW 1996 6 20 HEEA967248 1 19960517 A 3210 222036050103 FAIRING ASSY BELL 230 230 1182149 SW GEAR ASSY CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 3077 23009 FAIRING ASSY IS CRACKED AND WORN. 1 G 7 2 3U NC H9SW 1996062000722 19960620 00722 SW 1996 6 20 HEEA967249 1 19960517 A 5302 206033412119A HANGAR BRACKET 206033004003 BELL 206 206L1 1182107 SW TAILBOOM MIS MFG E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 AOKP00756 NEW HANGER BEARING SUPPORT BRACKET AFT VERTICAL LEG IS BOWED AND BRACKET IS TOO WIDE BETWEEN VERTICAL FLANGES. 1 G 7 1 3U H2SW 1996062000723 19960620 00723 GL 1996 6 20 HEEA967251 2 19960521 A 7230 6893612 BLADES 6890550 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL 2ND & 3RD STAGE BROKEN E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 81832 2522 CAC39370 S828 CAE831098 ENGINE REMOVED DUE TO OIL LEAK FROM #1 BEARING AREA AND SMOKING. UPON INSPECTION OF COMPRESSOR PARTS NOTED THE FOLLOWIN G: 2 EACH BLADES BROKEN OFF .250 AND .365 FROM 2ND-3RD STAGE WHEEL BLADE ROOT AREA. FRONT SUPPORT EXHIBITS 5 EACH VANE S DISLODGED FROM HUB AT BRAZEMENT. COMPRESSOR EXHIBITS EXCESSIVE F.O.D. 1 G 7 2 3U 3 U H3EU E4CE 1996062000724 19960620 00724 GL 1996 6 20 HEEA967252 2 19960521 A 7250 23038218 NOZZLE 6898735 BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL 1ST STAGE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2268X CAT23430 3607 CAE820964F ENGINE REMOVED DUE TO LOW POWER AND SMOKING. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: CRACKED BEYOND SERV ICEABLE LIMITS ON 1ST STAGE NOZZLE VANE. REPLACED DISCREPANT PART. PHI REQUESTING 100% WARRANTY REPAIR. PART OVERHAUL ED ON DALLAS AIRMOTIVE WO# EP1229 DATED 1-24-96. 1 G 7 1 3U 3 U H2SW E4CE 1996062000725 19960620 00725 SW 1996 6 20 HEEA967254 1 19960521 A 5260 212075418103 ACTUATOR BELL 412 412 1182202 SW STEP DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 33008 36004 VERY WEAK AND STICKS. INSPECTED BY ACCESSORY OVERHAUL SHOP AND FOUND SWITCH NOT SET CORRECTLY FROM VENDOR. OUTPUT SHAF T MOVEMENT WAS VERY STIFF, SOME MOISTURE IN UNIT AND SOME INTERNAL CORROSION. REPAIRED ACTUATOR AND RETURNED TO SERVICE. 1 G 7 2 4U H4SW 1996062000726 19960620 00726 SW 1996 6 20 HEEA967256 1 19960522 A 6410 206310105101 BEARING 206016201131 BELL 206 206L1 1182107 SW T/R CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2124Z 1394 CS161 45646 T/R ASSY S/N AFS6743 REMOVED DUE TO 2500 HOUR OVERHAUL. AT INSPECTION OF BLADE S/N CS161 FOUND OUTBOARD BEARING SCRAPPE D DUE TO CORROSION ON BALL. REPLACED WITH SERVICEABLE BEARING. 1 G 7 1 3U H2SW 1996062000727 19960620 00727 1996 6 20 HEEA967257 4 19960522 A 2312 40001452501 TRANSCEIVER RT138F BELL 212 212 1181420 SW COCKPIT MIS WIRED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1079U 31122 HUM ON LINE AND AUDIO CUTS OUT WHEN POWER SUPPLY IS DECREASED BELOW +280. FOUND THE INPUT AND OUTPUT OF U2 WAS WIRED WRO NG. REWIRED U2 CORRECTLY AND UNIT MEETS MANUFACTURERS SPECS. REPAIRED. 1 G 7 1 4U H4SW 1996062000728 19960620 00728 1996 6 20 HEEA967258 4 19960522 A 2312 40001452500 TRANSCEIVER RT138F BOLKMS 117 BK117B1 5626012 EU COCKPIT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 911TL 7198 UNABLE TO RECEIVE. 1 G 7 2 3U H13EU 1996062000730 19960620 00730 1996 6 20 HEEA967260 4 19960522 A 3457 0845000000 SKYNAV 5000 BOLKMS 117 BK117A3 5626015 EU COCKPIT GPS DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 401PH 7050 DOES NOT RETAIN USER WAYPOINT MEMORY. 1 G 7 2 3U H13EU 1996062000731 19960620 00731 1996 6 20 HEEA967261 4 19960522 A 3454 066107800 RECEIVER BELL 412 412 1182202 SW COCKPIT NAV INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 108X 33115 INOPERATIVE. REPLACED F101 AND C101 CAPACITOR. PERFORMED HEADER MODIFICATION AND HUMISEALED HEADERS. LOCALIZER RECEIVE R SENSE WEAK. ADJUSTED NAV RECEIVER BOARD. 1 G 7 2 4U H4SW 1996062000732 19960620 00732 1996 6 20 HEEA967262 4 19960522 A 2312 071121612 CONTROL UNIT BELL 412 412 1182202 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 21498 36003 DIGITS WEAK AND HARD TO TUNE. FOUND PHOTOCELL BAD. REPLACED PHOTOCELL V101 AND LENS COVER. BENCH CHECK GOOD. 1 G 7 2 4U H4SW 1996062000733 19960620 00733 1996 6 20 HEEA967263 4 19960522 A 3453 25410038 CDU BELL 412 412 1182202 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2261D 33076 7000 CDU BOTTOM LED BURNT OUT. 1 G 7 2 4U H4SW 1996062000734 19960620 00734 1996 6 20 HEEA967264 4 19960522 A 3453 066402600 LORAN KLN88 BELL 206 206L1 1182107 SW COCKPIT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5014Y 45219 LORAN WILL NOT NAVIGATE. 1 G 7 1 3U H2SW 1996062000735 19960620 00735 1996 6 20 HEEA967265 4 19960522 A 3457 0110014700 ANTENNA GA56 BRAERO DH125 HS125700A 4230170 EU GPS FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 125CS NA0212 ANTENNA WILL NOT PICKUP SATELLITES. 2 L 7 2 4F A3EU 1996062000736 19960620 00736 1996 6 20 HEEA967266 4 19960522 A 2312 064101701 TRANSCEIVER KAC952 BELL 214 214ST 1182106 SW COCKPIT VHF FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 8045T 28101 WILL NOT TUNE AND DRAWS EXCESSIVE CURRENT WHEN KEYED. SENT TO ALLIED SIGNAL AVIONICS FOR INSPECTION AND REPAIR. 2 G 7 2 4U H10SW 1996062000737 19960620 00737 NE 1996 6 20 HEEA967267 1 19960522 A 6320 SB2559101 BEARING 763510950004 SKRSKY S76 S76A 8143006 NE M/R GR BOX PITTED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546K 243 A08100122 760082 EXCESSIVE PITTING ON ROLLERS AND OUTER RACE. 1 G 7 2 3U H1NE 1996062000738 19960620 00738 EU 1996 6 20 HEEA967268 1 19960522 A 6520 350A33105803 LEVER SNIAS 350 AS350B2 8680813 EU T/R GR BOX WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 2990 2771 TR GR BOX CONTROL LEVER SMALL BORE WORN. 1 G 7 1 3U H9EU 1996062000739 19960620 00739 SW 1996 6 20 HEEA967269 1 19960522 A 6300 214040260105 ADAPTER ASSY BELL 214 214ST 1182106 SW M/R DRIVE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5748M 28102 ADAPTER ASSY CRACKED AROUND 90% OF CIRCUMFERENCE ON LOWER OR BOTTOM. SURFACE CRACK VISIBLE ON TOP SURFACE AS MARKED IN BLACK. 2 G 7 2 4U H10SW 1996062000740 19960620 00740 GL 1996 6 20 HEEA967270 2 19960529 A 7230 23039791 SPLINE ADAPTER 6890550 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL COMPRESSOR FRETTED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4294R 630 CAC41624 S860 CAE835871 ENGINE REMOVED DUE TO COMPRESSOR OVERHAUL. UPON INSPECTION OF COMPRESSOR PARTS NOTED THE FOLLOWING: FRETTING BEYOND OV ERHAUL LIMITS ON SPLINED ADAPTER O.D. REPLACED DISCREPANT PART. 1 G 7 2 3U 3 U H3EU E4CE 1996062000741 19960620 00741 SW 1996 6 20 HEEA967271 1 19960529 A 3340 214175127103 POWER SUPPLY BELL 214 214ST 1182106 SW LIGHT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 8045T 28101 POWER SUPPLY WILL NOT WORK. POPS CIRCUIT BREAKER TIME SINCE REPAIR 39:55. 2 G 7 2 4U H10SW 1996062500001 19960625 00001 SO 1996 6 25 GLBA96070 1 19960408 A 7712 MS3476L1418SY CONNECTOR EMB 120 EMB120ER 3260203 SO LEFT LOOSE A GLBA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 01 297UX 120297 DEN - CREW ABORTED TAKEOFF WHEN RIGHT NP INDICATOR FLUCTUATED FROM 0 TO 100 PERCENT BEFORE SETTLING BELOW 10 PERCENT. M AINTENANCE TIGHTENED LOOSE CONNECTOR ON LEFT NP SENSOR AND PERFORMED SENSOR RESISTANCE CHECK. OPS CHECK WAS GOOD. (M) 2 L 7 2 4T RT A31SO 1996062500002 19960625 00002 NM 1996 6 25 W8PA960011 1 19960414 A 5320 SUPPORT BOEING 737 7373K9 138447L NM BS 500 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 945WP 24212 DURING C-CHECK, FOUND CORROSION ON Z-ANGLE FLOOR SUPPORT AT BS 500A PLUS 10, RBL 21, WL 156.5. REMOVED CORRODED Z-ANGLE FLOOR SUPPORT, FABRICATED REPLACEMENT AND REINSTALLED. (M) 2 L 7 2 4F RT A16WE 1996062500003 19960625 00003 NM 1996 6 25 W8PA960012 1 19960414 A 5753 SKIN BOEING 737 7373K9 138447L NM LT TE FLAP DELAMINATED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 945WP 24212 LEFT OUTBOARD AFT FLAP HAS DELAMINATION ON OUTBOARD CORNER. REPAIRED IAW SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 1996062500004 19960625 00004 NM 1996 6 25 W8PA960013 1 19960414 A 5320 ANGLE BOEING 737 7373K9 138447L NM BS 725 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 945WP 24212 DURING C-CHECK, FOUND CORRODED 'L' ANGLE AT BS 725, LBL 63, WL 190. REMOVED AND REPLACED 'L' ANGLE IAW SRM 51-40-02. C ORROSION DAMAGE .002 INCH THROUGH .040 INCH IN A I INCH BY 2 INCH AREA. (M) 2 L 7 2 4F RT A16WE 1996062500005 19960625 00005 NM 1996 6 25 W8PA960014 1 19960414 A 5230 SKIN BOEING 737 7373K9 138447L NM FWD CARGO DOOR DENTED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 945WP 24212 FOUND DENT BELOW FORWARD CARGO DOOR AT STRINGER 27 BETWEEN BS 460 AND BS 500. REPAIRED IAW SRM 53-00-01 AND 51-40-02. ( M) 2 L 7 2 4F RT A16WE 1996062500006 19960625 00006 NM 1996 6 25 W8PA960016 1 19960414 A 5320 FLOOR SUPPORT BOEING 737 7373K9 138447L NM BS 727 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 945WP 24212 DURING C-CHECK, FOUND CORROSION UNDER NUT PLATES AT BS 727 PLUS 6 INCHES, LBL 7.5 AND LBL 11.5, WL 155. REPLACED CORROD ED AREAS OF FLOOR SUPPORT. (M) 2 L 7 2 4F RT A16WE 1996062500007 19960625 00007 NM 1996 6 25 W8PA960017 1 19960414 A 5312 BULKHEAD BRACKET BOEING 737 7373K9 138447L NM BS 727 BROKEN A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 945WP 24212 DURING C-CHECK, FOUND AFT BAY BULKHEAD ATTACH BRACKET BROKEN. INSTALLED NEW BRACKET AND DOUBLER. (M) 2 L 7 2 4F RT A16WE 1996062500008 19960625 00008 NM 1996 6 25 W8PA960018 1 19960414 A 5320 SUPPORTS BOEING 737 7373K9 138447L NM AFT CARGO BAY CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 945WP 24212 DURING C-CHECK, FOUND CORROSION UNDER NUT PLATES, BS 727-947, LBL 22, IN AFT CARGO BAY. REPLACED SIDEWALL SUPPORTS. (M ) 2 L 7 2 4F RT A16WE 1996062500009 19960625 00009 NM 1996 6 25 W8PA960019 1 19960414 A 5313 STRINGER BOEING 737 7373K9 138447L NM BS 900 DEFORMED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 945WP 24212 DURING C-CHECK, FOUND DENT IN SKIN BS 900, STRINGER 15 LEFT. REPAIRED DAMAGED STRINGER, REMOVED DENT. (M) 2 L 7 2 4F RT A16WE 1996062500010 19960625 00010 NM 1996 6 25 W8PA960020 1 19960414 A 5522 SKIN BOEING 737 7373K9 138447L NM RT ELEV STA 98 DELAMINATED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 945WP 24212 DURING C-CHECK, FOUND RIGHT ELEVATOR LOWER SURFACE DELAMINATED. REPAIRED AND BALANCED ELEVATOR. (M) 2 L 7 2 4F RT A16WE 1996062500011 19960625 00011 NM 1996 6 25 W8PA960021 1 19960414 A 5511 RIB BOEING 737 7373K9 138447L NM RT HORIZ STAB CHAFED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 945WP 24212 DURING C-CHECK, FOUND RIGHT HORIZONTAL STABILIZER TRAILING EDGE RIB CHAFED, ELEVATOR STATIONS 66.54 AND 94.07. REPAIRED RIB. (M) 2 L 7 2 4F RT A16WE 1996062500012 19960625 00012 NM 1996 6 25 W8PA960022 1 19960414 A 5511 RIB BOEING 737 7373K9 138447L NM LT HORIZ STAB CHAFED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 945WP 24212 DURING C-CHECK, FOUND LEFT HORIZONTAL STABILIZER TRAILING EDGE RIB CHAFFED, ELEVATOR STATIONS 121.59 AND 94.07. REPAIRED RIB. (M) 2 L 7 2 4F RT A16WE 1996062500013 19960625 00013 NM 1996 6 25 W8PA960023 1 19960414 A 5542 TE SKIN BOEING 737 7373K9 138447L NM RUDDER DELAMINATED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 945WP 24212 FOUND RUDDER TRAILING EDGE DELAMINATED. REPAIRED DAMAGE IAW SRM 51-70-17. (M) 2 L 7 2 4F RT A16WE 1996062500014 19960625 00014 NM 1996 6 25 W8PA960024 1 19960414 A 5512 SKIN BOEING 737 7373K9 138447L NM LT HORIZ STAB LE DENTED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 945WP 24212 FOUND 2 INCH DENT IN LEFT HORIZONTAL STABILIZER LEADING EDGE. REPAIRED DENT IAW SRM 55-10-01. (M) 2 L 7 2 4F RT A16WE 1996062500015 19960625 00015 NM 1996 6 25 W8PA960025 1 19960414 A 5755 SKIN BOEING 737 7373K9 138447L NM NR 2 SPOILER DENTED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 945WP 24212 FOUND DENT ON NR 2 SPOILER. REPAIRED IAW SRM 57-10-01. (M) 2 L 7 2 4F RT A16WE 1996062600001 19960626 00001 NM 1996 6 26 96FDEA01047 1 19960430 A 5320 DOOR FRAME BOEING 727 72725C 138400H NM CARGO DR CUTOUT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 136FE 19855 CRACK IN LWR FWD CORNER OF DOOR FRAME OF FWD LWR CARGO APPROX 1 INCH LONG. STOP DRILLED CRACK AND INSTALLED 7075-6, 0.9 0 DOUBLER ANGLE PER SRM 53-10-4 PG 39 TO 41. 2 L 7 3 4F A3WE 1996062700001 19960627 00001 WP 1996 6 27 9613289855 1 19960614 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 764NC 47717 DURING LINE CHECK, FOUND EMERGENCY ESCAPE EXIT SIGNS FOR OVERWING EXITS AT ROW 16 INOPERATIVE. REPLACED BATTERIES. OPER ATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996062700002 19960627 00002 NE 1996 6 27 9613336614 2 19960617 A 7230 COMPRESSOR BOEING 747 747251B 1384892 NM PWA JT9 JT9D7F 52054 NE NR 1 ENGINE STALLED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 GL 01 614US 20359 62730 THE NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL AND FLAMES OUT THE TAILPIPE. BOTH EGT AND EPR PEGGED FOR 5 SECONDS. THE NR 1 ENGINE WAS SHUT DOWN AND THE FLIGHT DIVERTED TO ANC WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND METAL IN THE NR 1 ENGINE TAILPIPE. AIRCRAFT HAS BEEN SCHEDULED FOR NR 1 ENGINE CHANGE. 2 L 7 4 4F 4 F A20WE E20EA 1996062700003 19960627 00003 NE 1996 6 27 9613346303 2 19960616 A 7230 COMPRESSOR BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE NR 3 ENGINE STALLED A NWAA C E ABORTED TAKEOFF ENGINE SHUTDOWN R M PARTIAL RPM/PWR LOSS OVER TEMP TO TAKEOFF 1 GL 01 663US 23818 717516 DURING TAKEOFF ROLL-OUT (KIX), THE NR 3 ENGINE EXPERIENCED SEVERAL COMPRESSOR STALLS. THE ENGINE WAS SUBSEQUENTLY SHUT DOWN AND ABORTED TAKEOFF AT 120 KTS. EGT TEMPERATURE WENT TO 790 DEGREES INSTANTLY. BORESCOPE REVEALED INTERNAL DAMAGE OF THE HPC. THE NR 3 ENGINE WAS CHANGED AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 1996062700004 19960627 00004 NM 1996 6 27 9613355501 1 19960615 A 2421 CONNECTOR BOEING 757 757251 1384970 NM RT IDG LOOSE A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 501US 23190 DURING TAKEOFF ROLL, THE RIGHT IDG FELL OFF LINE. TAKEOFF WAS ABORTED WITHOUT INCIDENT. MSP MAINTENANCE FOUND CANNON P LUG BACK SHELL LOOSE. TIGHTENED BACK SHELL. ALSO, FOUND IDG LOW ON OIL. SERVICED PER MAINTENANCE MANUAL. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A2NM 1996062700005 19960627 00005 NE 1996 6 27 9613365501 2 19960617 A 7200 ENGINE BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE NR 2 FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 GL 01 501US 23190 716337 DURING TAKEOFF, THE NR 2 ENGINE EGT INDICATION REACHED 880 DEGREES FOR TWO SECONDS. TAKEOFF WAS ABORTED AT 90 KTS. AIR CRAFT RETURNED TO THE GATE. GROUND MAINTENANCE REPLACED THE NR 2 ENGINE. GROUND RUN AND LEAK CHECK GOOD. AIRCRAFT RET URNED TO SERVICE. 2 L 7 2 4F 4 F RT A2NM E17NE 1996062700006 19960627 00006 NM 1996 6 27 9613376624 1 19960615 A 3260 TERMINAL BLOCK BOEING 747 747251B 1384892 NM NLG INDICATION FAILED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 624US 21706 DURING CLIMB, THE RED NOSE LANDING GEAR LIGHT ILLUMINATED AFTER LANDING GEAR RETRACTION. RECYCLED LANDING GEAR AND LIGH T EXTINGUISHED. AIRCRAFT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. REPAIRED WIRE AT TERMINAL STUD AND REPLACED TER MINAL BLOCK. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996062700007 19960627 00007 WP 1996 6 27 9613389862 1 19960618 A 3010 GASKET DOUG DC9 DC951 3022051 WP RT PACK FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 771NC 47769 DURING CLIMBOUT OF DTW, THE TAIL COMPARTMENT TEMPERATURE ANNUNCIATOR AND MASTER WARNING LIGHT ILLUMINATED. REDUCED POWE R AND WENT TO HP BLEED OFF ON PACKS AND LIGHTS WENT OUT. RESUMED POWER AND MASTER WARNING CAME ON MOMENTARILY AFTER ABO UT 5 MINUTES. RETURNED TO DTW AND LANDED WITHOUT INCIDENT. FOUND RIGHT AC TEMPERATURE HIGH SENSOR GASKET DETERIORATED. REPLACED GASKET AND PERFORMED LEAK CHECK DURING DUAL ENGINE RUN. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996062700008 19960627 00008 WP 1996 6 27 9613399862 1 19960617 A 3010 AUGMENTATION VLV DOUG DC9 DC951 3022051 WP LEFT ANTI ICE MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 01 771NC 47769 DURING CRUISE WITH LEFT ANTI-ICE ON, THE LEFT ICE PROTECTION TEMPERATURE ANNUNCIATOR LIGHT ILLUMINATED. PERFORMED COM AN D LIGHT WENT OUT. WHEN RIGHT SYSTEM WAS LATER SHUT DOWN BEFORE CROSSFEED CLOSED, THE RIGHT ICE PROTECTION TEMPERATURE A NNUNCIATOR LIGHT ILLUMINATED. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. CHANGED THE LEFT AND RIGHT AUGMENTATI ON VALVE, ANTICIPATOR, AND THERMOSTAT. PERFORMED ICE PROTECTION SYSTEM OPERATINAL CHECK. CHECKED OK. 2 L 7 2 4F A6WE 1996062700009 19960627 00009 WP 1996 6 27 9613409910 1 19960617 A 2612 FIRE LOOP DOUG DC9 DC931 3022065 WP RT ENG PYLON CHAFED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 960N 47256 RIGHT ENGINE FIRE SHUT-OFF HANDLE LIGHT BEGAN BLINKING ON TAKEOFF ROLL. ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINT ENANCE FOUND RIGHT PYLON FIRE DETECTOR ELEMENT CONNECTER WIRE CHAFED. REPLACED PYLON AND ENGINE FIRE DETECTOR LOOPS. O PERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996062700010 19960627 00010 NM 1996 6 27 9613412710 1 19960618 A 3350 BATTERIES BOEING 727 727225 1384077 NM COCKPIT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 820EA 22557 DURING PRE-FLIGHT, FOUND COCKPIT EMERGENCY LIGHT WOULD NOT ILLUMINATE. REPLACED BATTERIES. CHECK OK. 2 L 7 3 4F A3WE 1996062700011 19960627 00011 EU 1996 6 27 9613423218 1 19960618 A 3350 BATTERY AIRBUS 320 A320211 3930320 EU CABIN DISCHARGED A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 318US 206 AFT AISLE EMERGENCY EXIT AND DOOR 4L EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996062700012 19960627 00012 NM 1996 6 27 9613436310 1 19960620 A 3350 POWER SUPPLY BOEING 747 747451 1384940 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 670US 24225 DURING LINE CHECK, FOUND 2 RIGHT AFT OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. OPERATIONAL CHECK G OOD. 2 L 7 4 4F RT A20WE 1996062700013 19960627 00013 NM 1996 6 27 9613446305 1 19960619 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 665US 23820 DURING LINE CHECK, FOUND EMERGENCY FLOOR LIGHTS INOPERATIVE AT DOORS 3L AND 2L. REPAIRED BROKEN WIRE. OPERATIONAL CHEC K GOOD. 2 L 7 4 4F RT A20WE 1996062700014 19960627 00014 WP 1996 6 27 9613459998 1 19960618 A 3231 RETRACT MECH DOUG DC9 DC931 3022065 WP NLG DOOR OUT OF ADJUST A NWAA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 01 8934E 47143 DURING APPROACH INTO DTW, NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR WAS EXTENDED. GEAR WAS RECYCLED W ITH SAME RESULTS. CREW PERFORMED EMERGENCY GEAR EXTENSION PROCEDURES AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LEFT NOSE GEAR DOOR OUT OF ADJUSTMENT. ADJUSTED DOOR TO PROPER RIGGING. ALSO, LUBRICATED NOSE GEAR ASSEMBLY. OP ERATIONAL CHECK NORMAL ON TEST FLIGHT. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996062700015 19960627 00015 WP 1996 6 27 9613461226 1 19960620 A 3350 B59005 POWER SUPPLY DOUG DC10 DC1030 3023501 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 226NW 46583 DURING LINE INSPECTION, FOUND THE SEAT MOUNTED EMERGENCY ESCAPE LIGHT INOPERATIVE AT ROWS 31-39. REPLACED BATTERY PACK AND POWER SUPPLY. 2 L 7 3 4F A22WE 1996062700016 19960627 00016 NM 1996 6 27 9613472204 1 19960620 A 3350 BATTERY PACK BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 204US 22544 DURING PRE-FLIGHT, FOUND EMERGENCY LIGHTS INOPERATIVE AT BOTTOM OF AFT AIRSTAIRS. REPLACED BATTERY PACK. OPERATIONAL C HECK OK. 2 L 7 3 4F A3WE 1996062700017 19960627 00017 NE 1996 6 27 9613483239 2 19960618 A 7310 1754M36P01 GASKET AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE NR 1 ENGINE FAILED A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 339NW 367 731729 DURING CLIMB, PILOTS NOTICED A FUEL DISCREPANCY. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT FURTHER EVENT. GROUND MAI NTENANCE FOUND THE NR 1 ENGINE LEAKING FUEL DUE TO A CUT/TORN SEAL BETWEEN THE HYDRO MECHANICAL UNIT AND THE FUEL PUMP. INSTALLED NEW SEAL. 2 L 7 2 4F 4 F RT A28NM E29NE 1996062700018 19960627 00018 NM 1996 6 27 96FDEA00422 1 19960305 A 5320 6540270 L ANGLE BOEING 727 727233 138408A NM BS 720 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CRACKED L-ANGLE ON FLOOR SUPPORT AT BS 720B + 10, RBL 14 WL 155. **S/D*** REMOVED CRACKED L-ANGLE ON FLOOR SUPPORT A T BS 720B + 10, RBL 14, WL 155. FABRICATED REPAIR PART, DRILLED, ALODINED, PRIMED, AND INSTALLED IAW FEDEX SRM 51-20-1. 2 L 7 3 4F RT A3WE 1996062700019 19960627 00019 NM 1996 6 27 96FDEA00429 1 19960305 A 5311 6516342 FRAME BOEING 727 727233 138408A NM BS 1030 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 DOUBLE AND TRIPLE HOLES IN FRAME STA 1030 BETWEEN STR 8 AND 9R. ***S/D *** ACCESSED AREA, TRIMMED OUT DAMAGED AREA, F ABRICATED DOUBLER, INSTALLED FASTENERS AT BS 130 BETWEEN STR 8 AND STR 9R PER EWO 96-2135. 2 L 7 3 4F RT A3WE 1996062700020 19960627 00020 NM 1996 6 27 96FDEA00430 1 19960305 A 5320 6515940 FAIRING FORMERS BOEING 727 727233 138408A NM BS 740-846 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CORROSION (C53-132-01) ON FAIRING FORMERS BS 740 - 846, WL 138.5, LBL - RBL 10. **S/D *** REMOVED DAMAGED SECTION AN D REPLACED WITH NEW PARTS USING OLD PARTS AS A TEMPLATE AT BS 740 - 846, WL 138.5, LBL - RBL 10 IAW FEDEX SRM 51-10-1. 2 L 7 3 4F RT A3WE 1996062700021 19960627 00021 NM 1996 6 27 96FDEA00435 1 19960305 A 5311 6515936 FRAME BOEING 727 727233 138408A NM BS 680 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 DENT ON TOP FLANGE OF FRAME AT BS 680, RBL 39, WL 163. *** S/D *** REPAIRED DENT ON FRAME AT BS 680, RBL 39, WL 163 , IAW FEDEX SRM 51-40-3. 2 L 7 3 4F RT A3WE 1996062700022 19960627 00022 NM 1996 6 27 96FDEA00436 1 19960305 A 5320 6515936 FRAME BOEING 727 727233 138408A NM BS 660 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 DENT ON TOP FLANGE OF FRAME AT BS 660, RBL 33, WL 160. ***S/D*** REPAIRED DENT ON TOP FLANGE PER FEDEX SRM 53-40-03. 2 L 7 3 4F RT A3WE 1996062700023 19960627 00023 NM 1996 6 27 96FDEA00437 1 19960305 A 5311 6515936 FRAME BOEING 727 727233 138408A NM BS 660 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 DENT ON TOP FLANGE OF FRAME AT BS 660, LBL 42, WL 165. ***S/D *** REPAIRED DENTED FRAME AT BS 660, LBL 42, WL 165 IA W FEDEX SRM 51-40-3. 2 L 7 3 4F RT A3WE 1996062700024 19960627 00024 NM 1996 6 27 96FDEA00439 1 19960305 A 5311 6513928 FRAME BOEING 727 727233 138408A NM BS 500 TORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 AT FRAME 500 ABOVE STR 24L THERE IS A 1 INCH BY .50 INCH HOLE TORN THROUGH TOP OF FRAME. *** S/D *** REPAIRED PER FED EX SRM 51-40-03. 2 L 7 3 4F RT A3WE 1996062700025 19960627 00025 NM 1996 6 27 96FDEA00443 1 19960305 A 5330 6554580 SKIN BOEING 727 727233 138408A NM BS 1030 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 BULGE IN SKIN LAP BS 1030, STR 26R. *** S/D **** REMOVED FASTENERS FROM SKIN STA 1020 - 1040, STR 26R. REMOVED SHIM , TRIMMED SHIM TO FIT, ALODINED AND PRIMED PER FEDEX SRM 51-10-1. FAY SEALED PER FEDEX SRM 51-20-04. INSTALLED FASTENE R PER FEDEX SRM 51-30-2. 2 L 7 3 4F RT A3WE 1996062700026 19960627 00026 NM 1996 6 27 96FDEA00450 1 19960305 A 5330 65C25328 SKIN BOEING 727 727233 138408A NM BS 400 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 TWO DENTS IN FUSELAGE SKIN BS 400, STR 17L. ****S/D **** REPAIRED DENTS PER FEDEX SRM 53-30-03, FIG 1. 2 L 7 3 4F RT A3WE 1996062700027 19960627 00027 NM 1996 6 27 96FDEA00455 1 19960307 A 5315 6540272 FLOOR BEAM BOEING 727 727233 138408A NM BS 1030 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 CORROSION ON FLOOR BEAM UPPER CHORD, BS 1030, LBL 9, RBL 10 AND 21, WL 208. *** S/D **** REMOVED DAMAGE, FABRICATED A ND INSTALLED REPAIR PARTS ON FLOOR BEAM UPPER CHORD BS 1030, RBL 10, WL 203 PER FEDEX SRM 53-10-8, FIG 8. REMOVED .011 INCH OF ORIGINAL .125 INCH AT LBL 9 AND .006 INCH AT RBL 21 OF ORIGINAL .125 INCH. BOTH WITHIN LIMITS PER FEDEX SRM 53- 10-1. ALODINED AND PRIMED AREAS. 2 L 7 3 4F RT A3WE 1996062700028 19960627 00028 NM 1996 6 27 96FDEA00493 1 19960311 A 5230 6557203 SKIN BOEING 727 727233 138408A NM NR 3 CARGO DOOR CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 (NR 0168) CORROSION (C53-111-02-(2)), NR 3 CARGO DOOR INNER SKIN HAS CORROSION AROUND A RIVNUT 12 INCHES FROM THE AFT, EDGE 10 INCHES FROM THE BOTTOM. ***S/D *** REMOVED CORROSION FROM NR 3 CARGO DOOR INNER SKIN AROUND RIVNUTS. FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-01. REPAIRED DAMAGED AREA PER FEDEX SRM 51-40-02. 2 L 7 3 4F RT A3WE 1996062700029 19960627 00029 NM 1996 6 27 96FDEA00496 1 19960311 A 5315 6516316 FLOOR BEAM BOEING 727 727233 138408A NM BS 344 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 (NR 0626) CORROSION C53-224-01, BS 344 FLOOR BEAM FROM LBL 60 TO RBL 30 WL 208. CORRECTIVE ACTION: *** S/D*** REMOVE D DAMAGED FLOOR BEAM, BS 344, LBL 1 - 60, WL 208 AND REPLACED WITH NEW IAW FEDEX STANDARD REPAIR DRAWING SRM 27-53-007. 2 L 7 3 4F RT A3WE 1996062700030 19960627 00030 NM 1996 6 27 96FDEA00498 1 19960311 A 5230 6525326 SKIN BOEING 727 727233 138408A NM MAIN CARGO DOOR DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 (NR 0685) MAIN CARGO DOOR HAS TWO BULGES IN THE OUTER SKIN AT FORWARD AND AFT LIFT ACTUATORS. CORRECTIVE ACTION: REWOR KED BULGES ON MCD OUTER SKIN AT FORWARD AND AFT LIFT ACTUATORS TO WITHIN LIMITS AS PER DRAWING 52FX1435. ADJUSTED CLEAR ANCES BETWEEN MCD OUTER SKIN AND FORWARD AND AFT LIFT ACTUATOR ROD ENDS IAW FEDEX MM 52-34-9. 2 L 7 3 4F RT A3WE 1996062700031 19960627 00031 NM 1996 6 27 96FDEA00501 1 19960309 A 5210 6519145 END CAP BOEING 727 727233 138408A NM AFT AIRSTAIR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 (NR 0748) FT AIRSTAIR FORWARD END CAP IS CORRODED BEYOND LIMITS, REQUIRES REPLACEMENT. CORRECTIVE ACTION: ***S/D*** R EMOVED AND REPLACED AFT AIRSTAIR FORWARD END CAP PER FEDEX SRM 51-40-2. 2 L 7 3 4F RT A3WE 1996062700032 19960627 00032 NM 1996 6 27 96FDEA00503 1 19960310 A 5330 6556113 SKIN BOEING 727 727233 138408A NM BS 720 MISSING A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 (NR 0751) CORROSION ON SKIN AROUND BLIND FASTENERS UNDER FAIRING STRUCTURE AT BS 720A + 10, 1 INCH BELOW STR 29/L. CORR ECTIVE ACTION: ***S/D*** REPAIRED SKIN AROUND BLIND FASTENERS UNDER FAIRING STRUCTURE AT BS 710, 1 INCH BELOW STR 28L PER FEDEX SRM'S 53-30-1, 53-30-3, 53-10-1, 53-10-3 AND 51-20-1. 2 L 7 3 4F RT A3WE 1996062700033 19960627 00033 NM 1996 6 27 96FDEA01118 1 19960613 A 5320 6543801 T-FITTING BOEING 727 72722 1384002 NM BS 360 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 NR 0417 AND NR 025. T-FITTING AT BS 360, STR 20L IS CORRODED BEYOND LIMITS. ****S/D**** REMOVED AND REPLACED T-FITT ING. REF: FEDEX SRM 51-30-2. 2 L 7 3 4F A3WE 1996062700034 19960627 00034 NM 1996 6 27 96FDEA01138 1 19960615 A 5320 651634429 SHEAR TIE BOEING 727 72722 1384002 NM BS 1070 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 NR 0321 AND NR 034. BS 1070, LBL 51, STR 22L SHEAR TIE IS CRACKED AT FASTENER. ****S/D**** REPAIRED SHEAR TIE AT BS 1070, LBL 51, STR 22L PER FEDEX SRM 53-10-4, FIG 11. 2 L 7 3 4F A3WE 1996062700035 19960627 00035 WP 1996 6 27 96FDEA01157 1 19960619 A 5210 DOOR DOUG DC10 DC1030F 3023504 WP CABIN OUT OF ADJUST A FDEA A UNSCHED LANDING O OTHER UK UNKNOWN 1 SO 25 302FE 46801 VCP: BOTH CABIN DOORS DID NOT SEAL AND A/C WOULD NOT PRESSURIZE. ADJUSTED DOORS PER MM 52-11-00, PG 520. PRESSURED A/ C USING APU, LEAK CHECKED OK. 2 L 7 3 4F RT A22WE 1996062700036 19960627 00036 NM 1996 6 27 96FDEA01158 1 19960620 A 7930 CONNECTOR BOEING 727 727233 138408A NM NR 2 ENG DIRTY A FDEA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 25 223FE 20935 SCL: ENG NR 2 OIL FILTER BYPASS LIGHT CAME ON AT FLT LEVEL 310, 1 HOUR INTO SECOND LEG. ENGINE SHUTDOWN PER PROCEDURES . NORMAL OIL QUANTITY AND PRESSURE. REMOVED CANNON PLUG FROM LOW OIL PRESSURE SWITCH AND OIL FILTER BYPASS SWITCH AND CLEANED WITH CONTACT CLEANER. REPLACED BOTH CANNON PLUGS. RAN ENG NR 2 AND ACCOMP B727 MEL. MX PROCEDURE 79-2. MX CO NTROL NOTIFIED A/C OK FOR SERVICE. 2 L 7 3 4F RT A3WE 1996062700037 19960627 00037 NM 1996 6 27 96FDEA01159 1 19960618 A 2121 215201 GASPER FAN BOEING 727 7272S2F 1384O81 NM AIR COND BAY FAILED A FDEA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SO 25 212FE 22934 FLIGHT CREW SMELLED ELECTRICAL INSULATION BURNING IN THE COCKPIT. WE NOTICED THE GASPER FAN CIRCUIT BREAKER OPENED. A FEW MINUTES LATER THE SMELL SUBSIDED. GASPER FAN CIRCUIT BREAKER WAS LEFT OPEN AND GASPER FAN SWITCH TURNED OFF. A/C R ELEASED FOR SERVICE PER MEL 21-24 CAT D EXP 10-16-96. REMOVED AND REPLACED GASPER FAN AS PER MM 21-33-11, ALL CKS GOOD. 2 L 7 3 4F A3WE 1996062700038 19960627 00038 NM 1996 6 27 96FDEA01160 1 19960620 A 5315 6515940 FLOOR BEAM BOEING 727 72725 1384006 NM BS 740 ELONGATED HOLE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 NR0669 AND 046, WHILE WORKING NR0553 SEAT TRACK DISCOVERED 740 FLOOR BEAM TO HAVE ELONGATED HOLE AT WL 208 LBL 25. *S/D * REAMED HOLE ON FLOOR BEAM AT BS 740 LBL 25 TO A SIZE OF .4195. INSTALLED FREEZE PLUG WITH SEALANT AND INSTALLED PERM ANENT STRAP IAW FEDEX SRM 51-10-7. 2 L 7 3 4F A3WE 1996062700039 19960627 00039 SO 1996 6 27 COMA9610184 1 19960618 A 2752 3431001001 ACTUATOR EMB 120 EMB120RT SO RT NACELLE DAMAGED A COMA K NONE K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 01 243CA 14066 120212 THE BLUE HYDRAULIC SYSTEM QUANTITY FELL TO ZERO DURING FLIGHT. THE RIGHT NACELLE FLAP ACTUATOR WAS THE CAUSE OF THE HYD RAULIC LEAK. TWO OF THE 4 NAS 1351-3H8P SCREWS THAT SECURE THE SOLENOID VALVE SHEARED ALLOWING THE ACTUATOR TO LEAK PRO FUSELY. REPLACED ACTUATOR. 2 L 7 2 4T RT A31SO 1996062700040 19960627 00040 NE 1996 6 27 COMA9630129 2 19960619 A 7240 HOT SECTION SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RT ENGINE DAMAGED A COMA K NONE O OTHER TO TAKEOFF 1 SO 01 356CA 3289 340A034 367154 RIGHT ENGINE ITT REACHED 931 DEGREES FOR APROXIMATELY 2 SECONDS DURING TAKEOFF. HOT SECTION INSPECTION AND REPAIR. TIM E SINCE LAST HOT SECTION INSP - 3289 HOURS. 2 L 7 2 4T 4 T RT A52EU E8NE6 1996062700041 19960627 00041 EA 1996 6 27 COMA9660109 1 19960616 A 2750 ECU CNDAIR CL600 CL6002B19 EA TE FLAPS TRIPPED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 951CA 7091 FLAPS FAILED AT 30 DEGREES WHEN SELECTED DOWN FOR LANDING. RESET THE FLAP ELECTRONIC CONTROL UNIT. SYSTEM TEST NORMAL. ACFT CONTINUED SERVICE. 2 L 7 2 4F RT A21EA 1996062700042 19960627 00042 EA 1996 6 27 COMA9660110 1 19960618 A 2420 756652 ADG CNDAIR CL600 CL6002B19 EA FUSELAGE FWD BLADE DAMAGE A COMA K NONE O OTHER CR CRUISE 1 SO 01 934CA 5003 50 7042 A COKE WAS SPILLED ON THE COCKPIT CENTER PEDESTAL AND THE A.D.G. AUTO-DEPLOYED. COKE SPILL WAS CLEANED UP AND THE AIR D RIVEN GENERATOR WAS REPLACED DUE TO DAMAGED BLADE. 2 L 7 2 4F RT A21EA 1996062700043 19960627 00043 EU 1996 6 27 DL31J961391 1 19960610 A 7830 SWITCH MODULE AIRBUS 310 A310324 3930206 EU PWA 4152 PW4152 NE NR 2 ENGINE INTERMITTENT A DALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 27 841AB 6416 686 724922 REVERSE UNLOCK ECAM WARNING ACCOMPANIED BY REV (GREEN) AT FL 350, NR 2 ENGINE. FLIGHT DIVERTED TO MIA. NO BUFFET OR BA NK EXPERIENCED. ECAM WARN DISAPPEARS AND RECURS A FEW TIMES DURING DIVERSION. LOCKED OUT NR 2 T/R PER MEL 78-30-01. R EPLACED RVDT/STOW SWITCH MODULE S301. OPS CHECK GOOD. 2 L 7 2 4F RT A35EU E24NE 1996062700044 19960627 00044 EU 1996 6 27 DL31J961479 1 19960618 A 3350 09102110 CAP COVER AIRBUS 310 A310324 3930206 EU CABIN MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 840AB 682 EMERGENCY LIGHT PATH MISSING END CAP FORWARD OF SEAT 13AB, 13GH, AND AT SEAT 33DF, RT SIDE. EMERGENCY LIGHT PATH MISSI NG COVERS AT SEATS 3D, 12GH, 13GH, 18GH, 29AB, AND 29GH. REPLACED END CAPS AND COVERS AT THE ABOVE LOCATIONS. 2 L 7 2 4F RT A35EU 1996062700045 19960627 00045 EU 1996 6 27 DL31J961480 1 19960618 A 3350 321440 PWR SUPPLY AIRBUS 310 A310324 3930206 EU CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 840AB 682 EMERGENCY EXIT SIGN AT 1L DOOR AND EMERGENCY LIGHT F/C RT SIDE OVERHEAD STAYS ON WHEN EMERGENCY TEST SWITCH IS DEPRESSED AT 1L DOOR WILL NOT GO OUT. REPLACED POWER SUPPLY AT 1L DOOR BITE TEST AND OPS CK GOOD. 2 L 7 2 4F RT A35EU 1996062700046 19960627 00046 NM 1996 6 27 DL73E961412 1 19960522 A 5312 BULKHEAD WEB BOEING 737 737247 138448D NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 245WA 23519 DURING ACCOMPLISHMENT OF S.I. 3-69482-12 AT HMV, 2 CRACKS WERE DISCOVERED ON THE FORWARD FACE OF THE B.S. 178 BULKHEAD W EB. FIRST CRACK IS LOCATED AT RBL 5.7, WL 200. THE SECOND CRACK IS LOCATED AT LBL 5.7, WL 198. A .050 INCH DOUBLER WI LL BE INSTALLED. 2 L 7 2 4F A16WE 1996062700047 19960627 00047 NM 1996 6 27 DL767961466 1 19960618 A 2421 IDG BOEING 767 767232 1385132 NM NR 1 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 SO 27 113DA 10503 22225 FORTY-FIVE MINUTES OUT OF SAN JUAN, GOT LEFT GENERATOR DRIVE LIGHT WITH 'L' IDG OIL TEMP STATUS MSG. DISCONNECTED CSD. STARTED APU, BUT APU GENERATOR BREAKER WOULD NOT PUT GENERATOR ON LINE. RETURNED TO SJU. REPLACED LEFT GCU AND IDG. L EAK AND OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 1996062700048 19960627 00048 NM 1996 6 27 DL76L961467 1 19960618 A 2421 755359 IDG 755359 BOEING 767 767332 1382001 NM NR 2 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 SO 27 175DN LOI29 24803 FLIGHT OUT OF FRA - RT IDG DRIVE LIGHT CAME ON STEADY. APU STARTED AND RT IDG DISCONNECTED. APPROXIMATELY 1 HR LATER - APU OIL QTY - EICAS STATUS MSG. APPROXIMATELY 45 MINUTES LATER - APU AUTO SHUTDOWN. FLIGHT DIVERTED TO SNN. REPLACED RT IDG. 2 L 7 2 4F RT A1NM 1996062700049 19960627 00049 NM 1996 6 27 DLM88961405 1 19960612 A 3260 D132 SWITCH DOUG MD88 MD88 3023688 NM NLG INOPERATIVE A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 901DE 53378 AFTER GEAR RETRACTION AT 10,000 FEET, NOSE UNSAFE RED LIGHT ILLUMINATED. RETURNED TO ATL. REPLACED NOSE GEAR LOCKSW ITCH. 2 L 7 2 4F RT A6WE 1996062700050 19960627 00050 NM 1996 6 27 DLM88961436 1 19960615 A 3320 BALLAST D77311001 DOUG MD88 MD88 3023688 NM CABIN SHORTED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 937DL 49810 FLIGHT ATTENDANTS NOTICED SMOKE ABOVE OVERHEAD ROW 31. SECURED LIGHTS AND SMOKE DISAPPEARED. FOUND BALLAST AT ROW 31ED OVERHEAD SHORTED. REMOVED BALLAST BECAUSE OF SMELL. ITEM NIS CVG. FORWARD TO MCO. NEEDS P/N 339101626. 2 L 7 2 4F RT A6WE 1996062700051 19960627 00051 EU 1996 6 27 QXEA9600207 1 19960617 A 2424 914F5696 GCU FOKKER F28 F28MK1000 4990808 EU NR 1 FAILED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 09 450US 25 11101 SEA - ELECTRICAL SMELL IN COCKPIT DURING FLIGHT. NR ONE AC BUS AND NR ONE AC GENERATOR INDICATED FAILURE. NR ONE GCU A ND GENERATOR REPLACED I/A/W MAINT. MANUAL. NR ONE AC BUS AND GENERATOR, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVIC E. 2 L 7 2 4F RT A20EU 1996062700052 19960627 00052 EU 1996 6 27 QXEA9600208 1 19960618 A 3350 5515800104 CIRCUIT BOARD FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 469US 11096 SEA - EMERGENCY EXIT LIGHTS OVER COCKPIT DOOR AND FORWARD PASSENGER CABIN BULKHEAD ARE INOPERATIVE. LIGHT CIRCUIT BOARD S REPLACED AND SIGNS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996062700053 19960627 00053 NM 1996 6 27 QXEA9600209 1 19960618 A 3320 BA08006281 BALLAST DHAV DHC8 DHC8102 2809003 NM CABIN OVERHEATED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 09 840PH 74 SEA - BURNING INSULATION SMELL IN CABIN. TWO OVERHEAD LIGHT BALLASTS REPLACED FOR INDICATION OF OVERHEATING. LAMPS WER E REPLACED AS A PRECAUTIONARY MEASURE ALSO. LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1996062700054 19960627 00054 NM 1996 6 27 UPS96220367 1 19960618 A 3350 BATTERIES BOEING 727 72727C 138400J NM COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 909UP 19115 INSPECTION TYPE: N/A. ROBBED EMERGENCY EXIT LIGHT ASSEMBLY FROM OVER COCKPIT DOOR AND CREW ENTRY DOOR NOTE: DEAD BATT ERIES ON REQ. NR A452588. REPLACED BATTERIES ON COCKPIT EMERGENCY LIGHT ASSEMBLY. REINSTALLED, OPS CHECK GOOD. REPLA CED BATTERIES ON CREW ENTRY, EMERGENCY LIGHT ASSY REINSTALLED, OPS CHECK GOOD. OK FOR SERVICE. 2 L 7 3 4F A3WE 1996062700055 19960627 00055 NM 1996 6 27 UPS96420349 1 19960604 A 5311 FRAME BOEING 747 747121 1384871 NM BS 2100 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE: C. BULK CARGO COMP: FOUND CRACK IN FRAMEWEB AT STRINGER CUTOUT AT BS 2100, S-29 RT. REPAIRED FRAME WEB AT STRINGER CUTOUT IAW SRM 53-10-04, FIG 39. 2 L 7 4 4F A20WE 1996062700056 19960627 00056 NM 1996 6 27 UPS96420350 1 19960610 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1635-1640 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE: C. FOUND CRACK IN STRINGER 31 LT BSTA 1635 TO 1640. STRINGER 31 LT REPLACED BETWEEN STA 1635 - 1650. REPAIR CARRIED OUT IAW SRM 53-10-03, FIG 1. 2 L 7 4 4F A20WE 1996062700057 19960627 00057 NM 1996 6 27 UPS96420351 1 19960606 A 5311 FRAME BOEING 747 747121 1384871 NM BS 1560 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE: C. FRAME STA 1560. FOUND DENT IN WEB AT LBL 57. DENT OUT OF LIMITS IAW SRM 53-10-01. REPAIRED IAW SRM 51-40-02. 2 L 7 4 4F A20WE 1996062700058 19960627 00058 NM 1996 6 27 UPS96420352 1 19960604 A 5320 FRAME BOEING 747 747121 1384871 NM BS 2220 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE: C. FOUND CRACK IN FRAME LOWER FLANGE AT SKIN ATTACHMENT BS 2220. STR 42 LT, JUST BEHIND LEFT OUTFLO W VALVE. FRAME LOWER FLANGE REPAIRED IAW SRM 51-40-03, FIG. 1. 2 L 7 4 4F A20WE 1996062700059 19960627 00059 NM 1996 6 27 UPS96420353 1 19960603 A 5311 FRAME BOEING 747 747121 1384871 NM BS 2040 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE: C. FOUND CRACK IN FRAME WEB AT STRINGER CUTOUT AT BS 2040, S29 LT. FRAME WEB REPAIRED IAW SRM 53-10- 04, FIG 39. 2 L 7 4 4F A20WE 1996062700060 19960627 00060 NM 1996 6 27 UPS96420354 1 19960614 A 5311 FRAME BOEING 747 747121 1384871 NM BS 500 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE: C. FORWARD CARGO COMP: FOUND TWO CRACKS IN TOP FLANGE FROM FRAME STA 500 LT ABOVE STR 38. REPAIRED FRAME IAW SRM 53-10-04, FIG 57. 2 L 7 4 4F A20WE 1996062700061 19960627 00061 NM 1996 6 27 UPS96420355 1 19960605 A 5310 FRAME BOEING 747 747121 1384871 NM BS 1540 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE: C. AFT CARGO COMP: FOUND CRACKS ON FRAME BS 1540 LT AT UPPER FLANGE AT S29 AND S32. REMOVED DAMAGED SECTIONS FROM FRAME INNERFLANGES AT S29 AND S32, AND REPAIRED FRAME INNERFLANGES IAW SRM 51-40-03, FIG 1. 2 L 7 4 4F A20WE 1996062700062 19960627 00062 NM 1996 6 27 UPS96420356 1 19960605 A 5311 FRAME BOEING 747 747121 1384871 NM BS 1500 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE: C. AFT CARGO COMP: FOUND CRACKS IN FRAME BS 1500 LT AT S35 CUTOUT AND ON UPPERFLANGE OF FRAME AT S-3 7. REPAIRED FRAME AT STRINGER CUTOUT IAW SRM 53-10-04, FIG 4. REPAIRED FRAME UPPERFLANGE IAW SRM 51-40-03, FIG 1. 2 L 7 4 4F A20WE 1996062700063 19960627 00063 NM 1996 6 27 UPS96420357 1 19960605 A 5311 FRAME BOEING 747 747121 1384871 NM BS 600 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE: C. AFT CARGO COMP: FOUND CRACK ON FRAME BS 1600 LT ON UPPERFLANGE S-35. REMOVED DAMAGED SECTION FRO M FRAME INNERFLANGE AND REPAIRED FRAME INNERFLANGE IAW SRM 51-40-03, FIG 1. 2 L 7 4 4F A20WE 1996062700064 19960627 00064 NM 1996 6 27 UPS96420358 1 19960605 A 5311 FRAME BOEING 747 747121 1384871 NM BS 1560 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE: C. AFT CARGO COMP. FOUND CRACK IN FRAME BS 1560 LT AT S-35 LT CUTOUT. REPAIRED FRAME WEB AT STRINGE R CUTOUT IAW SRM 53-10-04, FIG 4. 2 L 7 4 4F A20WE 1996062700065 19960627 00065 NM 1996 6 27 UPS96420359 1 19960604 A 5400 REPAIR DOUBLER BOEING 747 747121 1384871 NM NR 3 PYLON INCORRECT REPAIR A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE: C. PYLON NR 3, FOUND REPAIR DOUBLER ON NAC STA 180 LT NOT INSTALLED IAW SRM (EDGE MARGINS ON MID SPAR TOO SMALL). FOUND DURING REMOVAL OF DOUBLER THAT DOUBLER WAS MADE FROM SOFT STEEL MAT: REWORK MID SPAR STIFFENER AND REPLACED GUSSET APPROVED BY TLX UPS-AMS 96-0137RE AND KLM DFX 96 117, ISSUE NR 2. INSTALLED NEW DOUBLER IAW S.B. 747 54 -2034R4, FIGURES 3 AND 6. 2 L 7 4 4F A20WE 1996062700066 19960627 00066 NM 1996 6 27 UPS96420370 1 19960605 A 5311 FRAME BOEING 747 747121 1384871 NM BS 1660 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE: C. AFT CARGO COMP: BS 1660 RT, TOP FLANGE CRACKED JUST ABOVE AND JUST BELOW FLOOR SUPPORT POST. REM OVED DAMAGED SECTIONS FROM FRAME INNERFLANGE AND REPAIRED FRAME INNERFLANGES IAW SRM 51-40-03, FIG 1. 2 L 7 4 4F A20WE 1996062700067 19960627 00067 NM 1996 6 27 UPS96420371 1 19960607 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 2180 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE: C. AFT CARGO COMP: AT STA 2180, STR 46 RT, STRINGER END CRACKED JUST IN FRONT OF SPLICE. STA 2180, STR 46, REPAIRED IAW SRM 53-10-03. 2 L 7 4 4F A20WE 1996062700068 19960627 00068 NM 1996 6 27 UPS96420372 1 19960605 A 5311 FRAME BOEING 747 747121 1384871 NM BS 2180 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE: C. AREA AFT OF BULK CARGO COMP: FOUND CRACK IN FRAME WEB BSTA 2180, RBL 32 UNDER FLOOR SUPPORT. FRA ME WEB REPAIRED IAW SRM 51-40-02, FIG 1. 2 L 7 4 4F A20WE 1996062700069 19960627 00069 NM 1996 6 27 UPS96420373 1 19960618 A 5320 FLANGE BOEING 747 747121 1384871 NM BS 1580 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE: C. AFT CARGO COMP: STA 1580 RT FLANGE CRACKED JUST AFT OF FLOOR SUPPORT. REPAIRED FRAME IAW SRM 51- 40-03, FIG 1. 2 L 7 4 4F A20WE 1996062700070 19960627 00070 NM 1996 6 27 UPS96420374 1 19960612 A 5311 FRAME BOEING 747 747121 1384871 NM BS 1520 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE: C. AFT CARGO COMP: FOUND CRACKS ON FRAME STA 1520 LT AT STR 35 CUTOUT AND SHEAR TIE BETWEEN STR 34 A ND 35. REPAIRED SHEAR TIE IAW SRM 53-10-04, FIG 3. REPAIRED UPPER FLANGE FRAME IAW SRM 51-40-03, FIG 1. 2 L 7 4 4F A20WE 1996062700071 19960627 00071 NM 1996 6 27 UPS96420375 1 19960607 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 2140 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE: C. BULK CARGO COMP: STA 2140 LT, FRAME STRINGER CUTOUT CRACKED AT STR 45. FRAME STR CUTOUT REPAIRED IAW SRM 53-10-04, FIG 41. 2 L 7 4 4F A20WE 1996062700072 19960627 00072 NM 1996 6 27 UPS96420376 1 19960614 A 5320 BRACKET BOEING 747 747121 1384871 NM BS 1980 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE: C. FORWARD CARGO COMP: FOUND CARGO FLOOR STIFFENER ATTACHMENT BRACKET CRACKED AT BS 1980, RBL 54. R EPLACED BRACKET IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996062700073 19960627 00073 NM 1996 6 27 UPS96420377 1 19960618 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1000 ELONGATED HOLES A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE: C. FORWARD CARGO COMP: FOUND DURING LOWER CHORD REPLACEMENT AT BS 1000, ELONGATED HOLES IN STR 46 RT . REPAIRED IAW TELEX UPS-AMS-95-0144RE / ATA 5321/20. 2 L 7 4 4F A20WE 1996062700074 19960627 00074 NM 1996 6 27 UPS96420378 1 19960605 A 5311 FRAME BOEING 747 747121 1384871 NM BS 1500 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE: C. AFT CARGO COMP: FOUND CRACK IN FRAME WEB NEAR INSULATION HOLE AT BS 1500, S-42 RT. STOP DRILLED CRACK AND REPAIRED FRAME WEB IAW KLM-DFX-96-127. REPAIRED APPROVED PER EFN-53-0767. 2 L 7 4 4F A20WE 1996062700075 19960627 00075 NM 1996 6 27 UPS96420379 1 19960606 A 5311 FRAME BOEING 747 747121 1384871 NM BS 1620 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE: C. AFT CARGO COMP. FOUND CRACK IN FRAME AT BS 1620 LT ON UPPER FLANGE S-34. REMOVED DAMAGED SECTION FROM FRAME INNERFLANGE AND REPAIRED FRAME INNERFLANGE IAW SRM 51-40-03, FIG 1. 2 L 7 4 4F A20WE 1996062700076 19960627 00076 NM 1996 6 27 UPS96420380 1 19960606 A 5311 FRAME BOEING 747 747121 1384871 NM BS 1780 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE: C. AFT CARGO COMP: FOUND CRACKS ON FRAME BS 1780 LT ON UPPER FLANGE AT S-37 AND S-40. REMOVED DA MAGED SECTIONS FROM FRAME INNERFLANGE AND REPAIRED FRAME FLANGES AT S-37 AND S-40 IAW SRM 51-40-03, FIG 1. 2 L 7 4 4F A20WE 1996062700077 19960627 00077 NM 1996 6 27 UPS96420381 1 19960603 A 5311 FRAME BOEING 747 747121 1384871 NM BS 2020 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE: C. BULK CARGO COMP: FOUND CRACK IN FRAME WEB AT STRINGER CUTOUT AT BS 2020, S-29 RT. REPAIRED FRAM E WEB AT STRINGER CUTOUT IAW SRM 53-10-04, FIG 39. 2 L 7 4 4F A20WE 1996062700078 19960627 00078 NM 1996 6 27 UPS96420382 1 19960604 A 5311 FRAME BOEING 747 747121 1384871 NM BS 2120 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE: C. BULK CARGO COMP: FOUND CRACK IN FRAME WEB AT STRINGER CUTOUT AT BS 2120, S-29 LT. REPAIRED FRAME WEB AT STRINGER CUTOUT IAW SRM 53-10-04, FIG 39. 2 L 7 4 4F A20WE 1996062700079 19960627 00079 NM 1996 6 27 UPS96420383 1 19960603 A 5311 FRAME BOEING 747 747121 1384871 NM BS 2060 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE: C. BULK CARGO COMP: FOUND CRACK IN FRAME WEB AT STRINGER CUTOUT AT BS 2060, S-29 LT. REPAIRED FR AME WEB AT STRINGER CUTOUT IAW SRM 53-10-04, FIG 39. 2 L 7 4 4F A20WE 1996062700080 19960627 00080 NM 1996 6 27 UPS96420384 1 19960607 A 5320 SHEAR TIE BOEING 747 747121 1384871 NM BS 2000 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE: C. BULK CARGO COMP: BS 2000 LT SHEAR TIE CRACKED AT S-45. REPAIRED SHEAR TIE IAW SRM 53-10-04, FIG 3. 2 L 7 4 4F A20WE 1996062700081 19960627 00081 NM 1996 6 27 UPS96420385 1 19960606 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 2060 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE: C. BULK CARGO COMP: DURING ACCOMPLISHMENT OF FRAME REPAIR AT BS 2060, S-29 LT, FOUND CORROSION IN ST RINGER AT FRAME/STRINGER-CLIP ATTACHMENT. REMOVED DAMAGED SECTION OF STRINGER FROM BS 2050 TO BS 2070 AND REPAIRED STRI NGER IAW SRM 53-20-03, FIG 1. 2 L 7 4 4F A20WE 1996062700082 19960627 00082 NM 1996 6 27 UPS96420386 1 19960604 A 5312 BULKHEAD BOEING 747 747121 1384871 NM BS 1000 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE: C. FORWARD CARGO COMP: FOUND CRACKS IN BS 1000 BULKHEAD LOWER CHORD, BETWEEN S-47/46 LT AND RT. REP LACED LOWER CHORD PARTLY ACCORDING TO SB 747-53-2316R1. 2 L 7 4 4F A20WE 1996062700083 19960627 00083 NM 1996 6 27 UPS96420387 1 19960605 A 5312 BULKHEAD BOEING 747 747121 1384871 NM BS 140 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE: C. SEVERAL CRACKS AT BS 140 FORWARD PRESSURE BULKHEAD, CRACKS AROUND FASTENERS AT INNER RING. WEB CR ACKS AT INNER RING CHORD REPAIRED IAW EO B747-5310-3279, APPENDIX B, FIG 3. 2 L 7 4 4F A20WE 1996062700084 19960627 00084 NM 1996 6 27 UPS96420388 1 19960605 A 5320 SHEAR TIE BOEING 747 747121 1384871 NM BS 2180 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE: C. AREA AFT OF BULK CARGO COMP: FOUND CRACK IN SHEAR TIE AT STRINGER CUTOUT BS 2180, BETWEEN S-44/42 RT. REPAIRED SHEAR TIE AT STRINGER CUTOUT IAW SRM 53-10-04, FIG 4. 2 L 7 4 4F A20WE 1996062700085 19960627 00085 NM 1996 6 27 UPS96420389 1 19960606 A 5320 INTERCOSTAL BOEING 747 747121 1384871 NM BS 1850 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE: C. AFT CARGO COMP: FOUND UNDER TWO ANCHOR NUTS, CORROSION, (ACCESS PANEL CUTOUT, TORQUE BOX) ON INTE RCOSTAL AT BS 1850, RBL 7. REMOVED CORROSION ACC. SRM 51-10-01. DAMAGE OUT OF LIMITS IAW SRM 53-10-01. REPAIRED INTERC OSTAL IAW SRM 51-60-03. INSTALLED NEW ANCHOR NUTS IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996062700086 19960627 00086 NM 1996 6 27 UPS96420390 1 19960619 A 5311 FRAME BOEING 747 747121 1384871 NM BS 2160 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE: C. BULK CARGO COMP: STA 2160 LT FRAME STRINGER CUTOUTS CRACKED AT STR 42 AND STR 44. REPAIRED FRAME IAW SRM 53-10-04, FIG 11. 2 L 7 4 4F A20WE 1996062700087 19960627 00087 NM 1996 6 27 UPS96420391 1 19960619 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 2160 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE: C. BULK CARGO COMP: AT STA 2160, STR 46 LT CRACKED AT STRINGER CLIP. REPAIRED STRINGER IAW SRM 53-1 0-03, FIG 1. 2 L 7 4 4F A20WE 1996062700088 19960627 00088 NM 1996 6 27 UPS96420392 1 19960619 A 5311 FRAME BOEING 747 747121 1384871 NM BS 1860 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE: C. AFT CARGO COMP: FOUND CRACK ON FRAME STA 1860 LT ON UPPER FLANGE STR'S 40 AND 41. REPAIRED FRAME IAW KLM DFX96-122 ISSUE 2, APPRROVED PER EFN 747-53- 0769. 2 L 7 4 4F A20WE 1996062700089 19960627 00089 NM 1996 6 27 UPS96420393 1 19960619 A 5311 FRAME BOEING 747 747121 1384871 NM BS 1640 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE: C. AFT CARGO COMP: FOUND CRACK IN FRAME AT STA 1640 LT ON UPPER FLANGE BETWEEN STR 31 AND 32. RE PAIRED FRAME IAW KLM DFX96-129 ISSUE 5, APPROVED PER UPS EFN 747-53-0766 IN COMBINATION WITH NCR 70660. 2 L 7 4 4F A20WE 1996062700090 19960627 00090 NM 1996 6 27 UPS96420394 1 19960619 A 5311 FRAME BOEING 747 747121 1384871 NM BS 1640 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE: C. AFT CARGO COMP: FOUND DURING FRAME REPAIR BS 1640 LT STR 31/32 INNERFLANGE REINFORCEMENT CHORD DA MAGED AT SAME LOCATION. REPAIRED CHORD IAW KLM DFX96-129 ISSUE 5, APPROVED PER UPS EFN 747- 53-0766 IN COMBINATION WITH NCR 706450. 2 L 7 4 4F A20WE 1996062700091 19960627 00091 NM 1996 6 27 UPS96420395 1 19960619 A 5311 FRAME BOEING 747 747121 1384871 NM BS 2040 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE: C. AFT CARGO COMP: FOUND CRACK IN FRAME WEB AT FRAME SPLICE, BS 2040, STR 34 RT. REPAIRED FRAME IAW SRM 51-40-03, FIG 1. 2 L 7 4 4F A20WE 1996062700092 19960627 00092 NM 1996 6 27 UPS96520396 1 19960619 A 3350 BPS73 POWER SUPPLY BOEING 757 75724APF 1384969 NM CREW ENTRY DOOR INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 410UP 23732 INSPECTION TYPE: N/A. ON PRE-DEPARTURE CHECK, THE EMERGENCY EXIT LIGHTS FAILED TO ILLUMINATE WITH THE SWITCH IN THE ON POSITION. REPLACED THE BATTERY ASSY, POWER SUPPLY. 2 L 7 2 4F RT A2NM 1996062700093 19960627 00093 NM 1996 6 27 UPS96520402 1 19960615 A 5321 FLOOR BOEING 757 75724APF 1384969 NM BS 255-297 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 401UP 23723 INSPECTION TYPE: C. CORROSION ON CONTROL CABIN FLOOR AT BS STA 255-297 FROM BL ZERO-RBL 10, BL ZERO-BL 15 AND LBL 15-L BL 30. REMOVED CORROSION PER SRM 51-20-01. FOUND TO BE OUT OF LIMITS PER SRM 53-00-01 AT BS 297, LBL 15 TO LBL 30. RE PAIRED PER SRM 51-70-13. 2 L 7 2 4F RT A2NM 1996062700094 19960627 00094 WP 1996 6 27 UPS96820360 1 19960618 A 2910 000AE506D0301 HOSE ASSY DOUG DC8 DC871F 302199D WP LT MLG LEAKING A IPXA K NONE K FLUID LOSS TX TAXI/GRND HDL 1 SO 01 708UP 46048 LEFT MLG BOGIE TRIM EXTEND HOSE REPLACED, LINE SECURED. THE FLEX LINE IS LONGER AND NEEDS REPLACING. 2 L 7 4 4F RT 4A25 1996062700095 19960627 00095 WP 1996 6 27 UPS96820361 1 19960603 A 5320 T FITTING DOUG DC8 DC871F 302199D WP KEEL BEAM CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE: C. KEEL BEAM LOWER SURFACE 3 EA T-FITTINGS CRACKED AT FS 900, FS 940 AND FS 950. REPLACED FITTINGS P ER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996062700096 19960627 00096 WP 1996 6 27 UPS96820362 1 19960601 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE: CS2. RT WING LEADING EDGE 6 EA UPPER RIBS CRACKED AT STA XFS728, XFS766, XFS772, XFS804, XFS810, XFS8 16. REPAIRED PER MM 57-00-00, PG 801. 2 L 7 4 4F RT 4A25 1996062700097 19960627 00097 WP 1996 6 27 UPS96820363 1 19960601 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE: CS2. RT WING LEADING EDGE 3 EA LOWER RIBS CRACKED AT STA XFS672, XFS804 AND XFS822. REPAIRED PER MM 57-00-00, PG 801. 2 L 7 4 4F RT 4A25 1996062700098 19960627 00098 WP 1996 6 27 UPS96820364 1 19960601 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE: CS2. RT WING LEADING EDGE 5 EA UPPER RIBS CRACKED AT STA XFS635, XFS641, XFS654, XFS660 AND XFS672. R EPAIRED RIBS PER MM 57-00-00, PG 801. 2 L 7 4 4F RT 4A25 1996062700099 19960627 00099 WP 1996 6 27 UPS96820365 1 19960603 A 5542 SKIN DOUG DC8 DC871F 302199D WP RUDDER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE: CS2. RUDDER LEADING EDGE LT SIDE CRACKED AT SECOND HINGE POINT CUTOUT LOWER SKIN. REPLACED RUDDER AS SY PER T/C S55-682-44. 2 L 7 4 4F RT 4A25 1996062700100 19960627 00100 WP 1996 6 27 UPS96820366 1 19960603 A 5542 SKIN DOUG DC8 DC871F 302199D WP RUDDER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE: CS2. RUDDER RT SIDE AT LEADING EDGE SKIN CRACKED AT SECOND HINGE POINT CUTOUT LOWER SKIN. REPLACED R UDDER ASSY PER T/C S55-682-44. 2 L 7 4 4F RT 4A25 1996062700101 19960627 00101 WP 1996 6 27 UPS96820368 1 19960618 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP FLIGHT DECK DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE: N/A. EMERGENCY LIGHT DOES NOT WORK. REPLACED EMERGENCY BATTERY PACK, OPS CHECKED NORMAL. 2 L 7 4 4F RT 4A25 1996062700102 19960627 00102 WP 1996 6 27 UPS96820397 1 19960605 A 5320 SHEAR TIE DOUG DC8 DC871F 302199D WP FS 1600 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE: CS2. FS 1600 BETWEEN LONGERONS 32L-33L, SHEAR TIE CRACKED. REPLACED SHEAR TIE PER SRM 53-2-0. 2 L 7 4 4F RT 4A25 1996062700103 19960627 00103 WP 1996 6 27 UPS96820398 1 19960602 A 5511 RIB DOUG DC8 DC871F 302199D WP LT HOR STAB LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE: CS2. LT HORIZONTAL STABILIZER LEADING EDGE INBOARD UPPER RIB IS CRACKED. REPAIRED RIB PER SRM 55-2-0 . 2 L 7 4 4F RT 4A25 1996062700104 19960627 00104 WP 1996 6 27 UPS96820399 1 19960531 A 5320 DOUBLER DOUG DC8 DC871F 302199D WP AFT FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE: CS2. DOUBLER CRACKED AT FUSELAGE SKIN MAIN CARGO DOOR AFT JAMB 20 FROM AFT UPPER CORNER. REPLACED DO UBLER PER SRM 51-1-21A. 2 L 7 4 4F RT 4A25 1996062700105 19960627 00105 EA 1996 6 27 96ZZZX3095 2 19960507 A 7200 ENGINE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA LEFT FAILED A MASA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SW 01 157YV 13557 6303 UC157 32512 EN ROUTE FROM DENVER TO PUEBLO, LEFT ENGINE FAILED. AIRCRAFT DIVERTED TO COLORADO SPRINGS. 2 L 7 2 4T 4 T RT A24CE E4EA 1996062700106 19960627 00106 1996 6 27 96ZZZX3096 4 19960515 A 3421 6229681001 EADI BEECH 1900 1900D 1154162 CE LT INSTR PANEL SHORTED A MASA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 01 116ZV UE116 SITTING AT THE GATE IN PORTLAND, OREGON, CAPTAIN'S EADF FADED OUT AND REPORTED SEEING SMOKE FROM INSTRUMENT PANEL. FBO INSPECTED AND FOUND SMELL COMING FROM EADI. (X) 2 L 7 2 4T RT A24CE 1996062700107 19960627 00107 GL 1996 6 27 96ZZZX3097 3 19960103 A 6111 BLADE BEECH 1900 1900D 1154162 CE HARTZL HCB3T HCB3TN3 GL PROPELLER SPLIT A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 174YV 548 UE174 HJ456 DURING ROUTINE MAINTENANCE, THE TRAILING EDGE OF BLADE, SN 1733, WAS FOUND TO HAVE A 3 INCH SPLIT. REPAIRED IAW HARTZEL L MM AND FAA FORM 8110-3 FROM HARTZELL. (X) 2 L 7 2 4T RT A24CE 6 C P15EA 1996062700108 19960627 00108 NM 1996 6 27 96ZZZX3098 1 19960508 A 2431 31920002 TEMP SENSOR MARATHON DORNER DO32 DO328100 2996000 NM NR 2 BATTERY CORRODED A EQGA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 SW 19 350AD 3050 DFW/ACT - ON APPROACH, NR 2 BATTERY OVERTEMP LIGHT STARTED GOING ON AND OFF. THE CAPTAIN DECLARED AN EMERGENCY AND LAND ED WITHOUT FURTHER INCIDENT. THE BATTERY TEMP SENSOR WAS FOUND CORRODED. THE TEMP SENSOR WAS CHANGED AND AIRCRAFT RETU RNED TO SERVICE. (X) 2 H 7 2 4T RT A45NM 1996062700109 19960627 00109 EU 1996 6 27 AALA960414 1 19960318 A 5320 ANGLE AIRBUS 300 A300B4605R 3930308 EU BS 1163-1236 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 59081 639 TUL - FLOOR SUPPORT T-ANGLE HAS CORROSION ON UPPER SURFACE JUST INSIDE L1 DOOR BETWEEN FRAMES 14 AND 15A. REMOVED T-ANG LE SECTION. MANUFACTURED AND INSTALLED T-ANGLE REPAIR PER ESO 30595. TST: 10,275.10 HRS. CYCLES, 4,129. (X) 2 L 7 2 4F RT A35EU 1996062700110 19960627 00110 EU 1996 6 27 AALA960416 1 19960319 A 5320 A53980186204 WEB AIRBUS 300 A300B4605R 3930308 EU L1 DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - CORROSION ON WEB INBOARD L1 DOOR SILL AFT FORWARD GIRT BAR FITTING. REPAIRED AREA PER ESO 3095. CORROSION REMOVE D, INHIBITED, AND PAINTED. TST: 21,374.47 HRS. CYCLES, 8,539. (X) 2 L 7 2 4F RT A35EU 1996062700111 19960627 00111 EU 1996 6 27 AALA960417 1 19960319 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU BS 1180-1230 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - CORROSION ON FLOOR SUPPORT INBOARD R1 DOOR. REMOVED AND INSTALLED NEW T-ANGLE FLOOR SUPPORT AND DOUBLER PER SRM 5 3-10-16. (X) 2 L 7 2 4F RT A35EU 1996062700112 19960627 00112 EU 1996 6 27 AALA960497 1 19960329 A 5230 A5247123100000 BRACKET AIRBUS 300 A300B4605R 3930308 EU BS 5262 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - BRACKET THAT HOLDS THE CARGO DOOR HOLD-OPEN ROD SEVERELY CORRODED. NO OTHER CORROSION FOUND IN SURROUNDING AREA. REPLACED PER SRM 52-30-14-11. TST: 21,374.47 HRS. CYCLES, 8,539. (X) 2 L 7 2 4F RT A35EU 1996062700113 19960627 00113 NM 1996 6 27 AALA960651 1 19960426 A 5320 FLOOR PAN BOEING 727 727223 1384074 NM BS 1177 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 702AA 22460 TUL - CORROSION 1 INCH BELOW FLOORBOARD, STA 1177, LBL 12 INCHES TO 16 INCHES, IN AFT CARGO. REMOVED FLOOR WEB AND INST ALLED NEW FLOOR WEB PER SRM 51-30-2, SRM 51-20-4. TST: 42,325 HRS. CYCLES, 22,016. (X) 2 L 7 3 4F A3WE 1996062700114 19960627 00114 NM 1996 6 27 AALA960652 1 19960426 A 5320 SILL PLATE BOEING 727 727223 1384074 NM BS 568-572 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 702AA 22460 TUL - CORROSION ON SILL PLATE WEB ON FORWARD CARGO DOOR AND CASTING. REPLACED SILL AND CASTING WITH NEW PARTS PER SRM 5 1-10-1, PAGE 4. TST: 42,325 HRS. CYCLES, 22,016. (X) 2 L 7 3 4F A3WE 1996062700115 19960627 00115 NM 1996 6 27 AALA960653 1 19960426 A 5320 SUPPORT BOEING 727 727223 1384074 NM BS 1172-1181 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 702AA 22460 TUL - CORROSION ON LOWER LAVATORY PAN SUPPORT ABOVE STR 221, STA 1172 TO STA 1176. CORROSION ON LAVATORY PAN, STA 1179 AFT OF WATER HOSE CONNECTION JUST BELOW STR 21L. REMOVED CORRODED LAVATORY PAN AND SUPPORT. INSTALLED NEW LAVATORY PAN AND SUPPORT HOSE FITTINGS AND PUMP VALVE PER SRM 51-10-1. TST: 42,325 HRS. CYCLES, 22,016. (X) 2 L 7 3 4F A3WE 1996062700116 19960627 00116 WP 1996 6 27 AALA960751 1 19960503 A 3213 PISTON DOUG DC9 DC982 3022082 WP LT MLG CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7531A 49923 TUL - LEFT MLG PISTON, LEFT LUG CRACKED. NDT PROCEDURE MD-80/PT/002. REPLACED WITH SERVICEABLE MLG PISTON. TST: 16,4 54.22 HRS. CYCLES, 9,103. (X) 2 L 7 2 4F A6WE 1996062700117 19960627 00117 NM 1996 6 27 CAL960557 1 19960505 A 3234 LEVER LATCH ASSY BOEING 737 737524 1384721 NM COCKPIT OUT OF ADJUST A CALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 09 18622 27526 IAH - FLT 1691 - THE LANDING GEAR HANDLE WOULD NOT RAISE TO THE UP POSITION AFTER TAKEOFF FROM IAH. THE AIRCRAFT WAS RE TURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. A GEAR RETRACTION WAS PERFORMED AND THE PROBLEM COULD NOT BE DUPLICATE D. ADJUSTMENT OF THE GROUND SAFETY SENSOR CHECKED GOOD PER MM 32-09-01. THE LEVER LATCH ASSY WAS CLEANED AND LUBRICATE D. IN ADDITION, THE R276 RELAY WAS REPLACED AS A PRECAUTIONARY MEASURE. (X) 2 L 7 2 4F RT A16WE 1996062700118 19960627 00118 WP 1996 6 27 CAL960609 1 19960319 A 7110 FORMER DOUG DC10 DC1030 3023501 WP NR 1 ENGINE COWL CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14074 46911 MAN - INSPECTION FOUND THE NR 1 ENGINE NOSE COWL FORWARD FORMER CRACKED FROM APPROXIMATELY THE 11 O'CLOCK TO 2 O'CLOCK P OSITIONS ALONG INNER SEATING ANGLE. THE CRACK WAS 26 INCHES LONG. A HOLE 2 INCHES IN DIAMETER WAS ALSO FOUND IN THE AR EA. THE NOSE COWL WAS REMOVED. THE COWL WAS REPAIRED IN SHOP AND REFITTED IAW WORK ORDER 1528 AND WORK CARD 02-7100-1- 0003. (X) 2 L 7 3 4F A22WE 1996062700119 19960627 00119 WP 1996 6 27 CKSA96015 1 19960420 A 3310 BA170 BALLAST DOUG DC8 DC862F 3021972 WP COCKPIT BURNED A CKSA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 3931A 58215 45961 KOSC - FLT 72016 - SMOKE OF UNKNOWN ORIGIN ESCAPING FROM F/O PNEUMATIC RAIN REMOVAL LEVER. INSPECTED AND FOUND ORIGIN O F SMOKE COMING FROM LIGHT BALLAST AT F/O RT CONSOLE. FOUND BALLAST AT FAULT, DISCONNECT BALLAST AND TRANSFERRED TO DMI NR 22 IAW AIA MEL 33-1 CAT. 'C' SWITCH PLACARDED. REMOVED AND REPLACED BALLAST TRANSFORMER. OPS CHECK GOOD IAW DC8 MM 33-12-0. DMI CLEARED. PLACARDS REMOVED. (X) 2 L 7 4 4F 4A25 1996062700120 19960627 00120 NM 1996 6 27 CKSA96029 1 19960409 A 2612 CA06KE16S8P CONNECTOR BOEING 727 727223 1384074 NM NR 2 ENGINE FAILED A CKSA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 723CK 71270 665162 20191 KHUF - FLT 73729 - AT CRUISE, ENGINE FIRE WARNING BELL CAME ON VERY WEAK WITHOUT ANY FIRE WARNING LIGHTS. SILENCED THE BELL AND TESTED FIRE WARNING SYSTEM. TESTED OK, BUT WHEN ATTEMPTED RE-TEST, NR 2 FIRE LIGHT WOULD NOT TEST. AFTER SEVE RAL ATTEMPTS, NR 2 FIRE LIGHT TESTED OK. POSSIBLE SHORT. REPAIRED NR 2 ENGINE FIREWALL FIRE WARNING CONNECTOR, SYSTEM OPS CHECK GOOD IAW MM 26-11-03. (X) 2 L 7 3 4F A3WE 1996062700121 19960627 00121 NM 1996 6 27 PCAA9600285 1 19960423 A 2497 WIRE DHAV DHC8 DHC8102 2809003 NM LT/RT ENGINE CHAFED A PCAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 13 EICHP 258 AUXILIARY INVERTER, NR 1 AND NR 2 DC GENERATOR, RUD FULL PRES, GPWS CAUTION LIGHTS, NR 1 STALL WARNING WITH HORN, MASTER WARNING AND CAUTION LIGHTS FLICKERING THROUGHOUT FLIGHT, BATTERIES SHOWING DISCHARGE, BAGGAGE AND PASSENGER DOOR WARNIN G ILLUMINATED. LOST NR 1 ADF, NR 1 ALTITUDE, NR 1 ID802 PANEL, NR 1 TRANSPONDER, NR 1 VSI, NR 1 ATTITUDE, AND NR 1 FUEL FLOW. AIRCRAFT LANDED WITHOUT INCIDENT. TROUBLESHOT ELECTRICAL SYSTEM, FOUND CHAFED WIRES ROUTED ALONG THE LT AND RT ENGINE MOUNT STRUTS FOR THE DC GENERATOR FIELD. INSULATED AFFECTED WIRES AND GROUND CHECKED AIRCRAFT. ALL SYSTEMS CHEC KED GOOD. ACFT RETURNED TO SERVICE. ACTC: 13,229. (X) 2 H 7 2 4T RT A13NM 1996062700122 19960627 00122 NE 1996 6 27 WRLA96021 2 19960503 A 7230 COMPRESSOR DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 2 ENGINE STALLED A WRLA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 EA 27 117WA 48318 DURING TAKEOFF AT ROTATION, FLIGHT CREW EXPERIENCED COMPRESSOR STALL ON NR 2 ENGINE. FLIGHT ENGINEER NOTED A 6 PERCENT DROP IN N-1 SPEED. DURING INITIAL CLIMB-OUT, CREW NOTED SECOND COMPRESSOR STALL. AIRCRAFT RETURNED TO POINT OF DEPARTU RE, LANDING WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED BORESCOPE WITH NO FAULTS FOUND. AS A PRECAUTION, THE MAIN ENGINE CONTROL AND COMBUSTION INLET TEMPERATURE SENSOR WERE REPLACED. GROUND RUN PERFORMED AND ALL PARAMETERS NORMAL. A CFT RETURNED TO SERVICE. (X) 2 L 7 3 4F 4 F A22WE E23EA 1996062700123 19960627 00123 EU 1996 6 27 Y2PA96025 1 19960501 A 5311 SKIN AMD FALC20 FALCON 2720302 EU FUSELAGE DENTED A Y2PA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AA 11525 26 YIP - DENT IN LEFT FORWARD FUSELAGE SKIN, 45 INCHES AFT OF FRAME NR ZERO (1 INCH BY 1 INCH). REMOVED DAMAGED AREA. FAB RICATED AND INSTALLED FILLER AND REPAIR DOUBLER PER F20 SRM 51-10-21 AND USA JET ENGINEERING AUTHORIZATION NR 96-53-03. PART TOTAL CYCLES, 9,307. (X) 2 L 7 2 4F A7EU 1996062700124 19960627 00124 EU 1996 6 27 Y2PA96026 1 19960508 A 5753 MY20124138111 FLAP TRACK AMD FALC20 FALCON 2720302 EU NR 3 TE FLAP CRACKED A A Y2PA K NONE O OTHER IN INSP/MAINT 1 GL 23 812AA 57 YIP - NR 3 RIGHT FLAP RAIL CRACKED. CRACK IS APPROXIMATELY .75 INCH LONG AND IS 2.25 INCHES FORWARD OF THE AFT END OF T HE RAIL ON THE UPPER SURFACE. REMOVED AND REPLACED NR 3 RIGHT WING FLAP RAIL. (X) 2 L 7 2 4F A7EU 1996062700125 19960627 00125 EU 1996 6 27 Y2PA96027 1 19960508 A 5753 MY20114138111 FLAP TRACK AMD FALC20 FALCON 2720302 EU NR 3 TE FLAP CRACKED A Y2PA K NONE O OTHER IN INSP/MAINT 1 GL 23 812AA 57 YIP - NR 3 LEFT FLAP RAIL CRACKED. CRACK IS 0.154 INCHES LONG AND IS 3.334 INCHES FORWARD OF THE AFT END OF THE RAIL ON THE UPPER SURFACE. ESTABLISHED A 'CARRY OVER ITEM' TO RE-INSPECT EACH 300 HOURS OR 6 MONTHS DURING EACH A-CHECK IAW FA LCON MM 12-30-6, CHAPTER 5, ITEM NR 12-30-6. NO FURTHER ACTION REQUIRED AT THIS TIME. A NEW REPORT WILL BE SUBMITTED S HOULD THE CRACK PROPAGATE BEYOND LIMITS. (X) 2 L 7 2 4F A7EU 1996062700126 19960627 00126 EU 1996 6 27 Y2PA96028 1 19960508 A 2520 TYPE263 CREW SEAT AMD FALC20 FALCON 2720302 EU RT COCKPIT CRACKED A Y2PA K NONE O OTHER IN INSP/MAINT 1 GL 23 812AA 153 57 YIP - FIRST OFFICER'S SEAT CRACKED ON RIGHT TOP SEAT FRAME RAIL. REMOVED AND REPLACED SEAT. (X) 2 L 7 2 4F A7EU 1996062700127 19960627 00127 EU 1996 6 27 Y2PA96029 1 19960508 A 2810 L84A13603 NONRETURN VALVE AMD FALC20 FALCON 2720302 EU RT FEEDER TANK DIRTY A A Y2PA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 23 812AA 247 H2450 57 YIP - FLT 14593 - DURING CLIMB AFTER DEPARTURE AT YIP, FUEL FUMES WERE DETECTED IN THE CABIN BY CREW. BLEED AIR SOURCES WERE ALTERNATED WITH NO EFFECT. FUMES SEEMED TO STOP WITH BLEEDS TURNED OFF. CREW USED OXYGEN DURING THIS TIME. PRIO R TO LANDING, NR 1 BLEED AS SELECTED ON WITH RETURN OF STRONG FUEL FUMES. FOUND RIGHT FEEDER TANK PRESSURIZATION CHECK VALVE OFF ITS SEAT. REMOVED, CLEANED, AND REINSTALLED IN FEEDER. PERFORMED DECONTAMINATION PROCEDURE IN FALCON 20 MM 2 8-10-40, PAGES 101 AND 102. ALSO, PERFORMED OPERATIONAL CHECK OF REAR COMPARTMENT TANK REFUELING IAW 38-20-0, PAGE 502, ITEM 6B WITH NO DEFECTS NOTED AT THIS TIME. (X) 2 L 7 2 4F A7EU 1996062700128 19960627 00128 WP 1996 6 27 9613499851 1 19960517 A 5313 LONGERON DOUG DC9 DC951 3022051 WP FS 470 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 760NC 47708 DURING H-CHECK, FOUND CORROSION ON LONGERON 30 AT APPROXIMATELY FS 470. REPAIRED LONGERON (P/N 5924819-558) PER EA 98-1 09078. 2 L 7 2 4F A6WE 1996062700129 19960627 00129 WP 1996 6 27 9613501144 1 19960604 A 5311 FRAME DOUG DC10 DC1040 3023508 WP FS 1841 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 144JC 46753 DURING T-CHECK, FOUND A 3.625 INCH CRACK IN THE FS 1841 FRAME BETWEEN LONGERON 12L TO 13L EXTENDING COMPLETELY THROUGH T HE INBOARD FLANGE AND 2.25 INCH INTO THE FRAME WEB. REPAIRED FRAME (P/N AGA 3783-501) PER EA 11-105412. 2 L 7 3 4F A22WE 1996062700130 19960627 00130 WP 1996 6 27 9613511144 1 19960604 A 5312 BULKHEAD DOUG DC10 DC1040 3023508 WP FS 1156 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 144JC 46753 DURING T-CHECK, FOUND CORROSION ON THE CENTER ACCESSORY PRESSURE BULKHEAD WEB AT FS 1156, LBL 9. REPAIRED WEB (P/N NPB 6280-3) PER EA 11-105414. 2 L 7 3 4F A22WE 1996062700131 19960627 00131 WP 1996 6 27 9613521144 1 19960604 A 5730 SKIN DOUG DC10 DC1040 3023508 WP WS 603 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 144JC 46753 DURING T-CHECK, FOUND A .9 INCH CRACK IN THE RIGHT WING LEADING EDGE SKIN AT XOS 603. REPAIRED SKIN (P/N ARB 2887-502) PER EA 11-105398. 2 L 7 3 4F A22WE 1996062700132 19960627 00132 NM 1996 6 27 9613535507 1 19960605 A 5321 DECK PLATE BOEING 757 757251 1384970 NM FS 1681-1720 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 507US 23196 DURING P-CHECK, FOUND CORROSION ON THE AFT GALLEY FLOOR STRUCTURE DECK PLATE, SHEAR WEB BS 1681 TO 1720. REPAIRED PLATE (P/N 146N5318-3) PER EA 55-106091. 2 L 7 2 4F RT A2NM 1996062700133 19960627 00133 WP 1996 6 27 9613541144 1 19960606 A 5730 SKIN DOUG DC10 DC1040 3023508 WP WS 290 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 144JC 46753 DURING T-CHECK, FOUND CRACKS IN BOTH THE LEFT AND RIGHT WING LEADING EDGE SKIN XOS 290 AND 330. REPAIRED SKIN (P/N ARB 2984-501, -502) PER EA 11-105409. 2 L 7 3 4F A22WE 1996062700134 19960627 00134 WP 1996 6 27 9613551144 1 19960606 A 5311 FRAME DOUG DC10 DC1040 3023508 WP FS 1561 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 144JC 46753 DURING T-CHECK, FOUND CORROSION ON LONGERON 43R AT FS 1561. REPAIRED LONGERON (P/N AFA 7070-1) PER EA 11-105418. 2 L 7 3 4F A22WE 1996062700135 19960627 00135 WP 1996 6 27 9613561144 1 19960606 A 5311 FRAME DOUG DC10 DC1040 3023508 WP FS 1561 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 144JC 46753 DURING T-CHECK, FOUND A 4.625 INCH CRACK IN THE FS 1561 FRAME SPLICE AT LONGERON 44L. REPAIRED SPLICE (P/N AEA 7296-11) PER EA 11-102166. 2 L 7 3 4F A22WE 1996062700136 19960627 00136 WP 1996 6 27 9613571144 1 19960609 A 5311 FRAME DOUG DC10 DC1040 3023508 WP FS 1360 CORROSION A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 144JC 46753 DURING T-CHECK, FOUND CORROSION ON THE FS 1360 FRAME FROM LONGERON 51L TO 51R. REPAIRED FRAME (P/N AYB 7031-3) PER EA 1 1-105407. 2 L 7 3 4F A22WE 1996062700137 19960627 00137 WP 1996 6 27 9613581144 1 19960611 A 5312 BULKHEAD DOUG DC10 DC1040 3023508 WP FS 1369 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 144JC 46753 DURING T-CHECK, FOUND CORROSION ON THE PRESSURE BULKHEAD CAP FS 1369 IN THE CENTER MAIN LANDING GEAR WHEEL WELL. REPAIR ED CAP (P/N AYB 7080-5) PER EA 11-105427. 2 L 7 3 4F A22WE 1996062700139 19960627 00139 WP 1996 6 27 9613609915 1 19960614 A 5312 BULKHEAD FITTING DOUG DC9 DC931 3022065 WP AFT PRESS BLKHD CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 965N 47417 DURING LINE CHECK, FOUND A .5 INCH CRACK IN THE AFT PRESSURE BULKHEAD UPPER LEFT DOOR STOP FITTING. REPLACED FITTING. 2 L 7 2 4F A6WE 1996062700140 19960627 00140 WP 1996 6 27 9613619953 1 19960616 A 5320 FITTING DOUG DC9 DC931 3022065 WP FS 980-995 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 918RW 47158 DURING LINE CHECK, FOUND CORROSION ON THE LONGERON 23L END FITTING AT FS 980 TO 995. REPLACED FITTING PER SRM 51-30-2, 51-30-5. 2 L 7 2 4F A6WE 1996062700141 19960627 00141 WP 1996 6 27 9613629867 1 19960617 A 5230 FITTING DOUG DC9 DC951 3022051 WP CARGO DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 776NC 47786 DURING H-CHECK, FOUND CRACKS IN THE AFT CARGO DOOR END FITTINGS, NR 1 AFT, NR 2 AFT AND NR 5 FORWARD. REPLACED ALL THRE E END FITTINGS. 2 L 7 2 4F A6WE 1996062700142 19960627 00142 NE 1996 6 27 9613631152 2 19960618 A 7261 OIL FILL LINE DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 1 ENGINE LOOSE A NWAA E A ENGINE SHUTDOWN UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CL CLIMB 1 GL 01 152US 46761 86114 THE NR 1 ENGINE OIL QUANTITY BEGAN TO DECREASE AND AT FIVE GALLONS, THE ENGINE WAS SHUT DOWN. CREW FOLLOWED COM PROCEDU RE AND RETURNED TO HNL. ALSO, ON TAXIING TO GATE, APU FIRE WARNING LIGHT ILLUMINATED. CREW FOLLOWED COM PROCEDURE AND FIRED BOTTLE. INSPECTION FOUND OIL FILL LINE LOOSE. FOUND NO DAMAGE TO THE APU. TIGHTENED FILL LINE AND PERFORMED LEA K CHECK. REPLACED APU BOTTLE AND RETURNED TO SERVICE. 2 L 7 3 4F 4 F A22WE E20EA 1996062700143 19960627 00143 NM 1996 6 27 9613646627 1 19960620 A 3350 BATTERY PACK BOEING 747 747251B 1384892 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 627US 21709 DURING LINE CHECK, FOUND ZONE-A EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK GO OD. 2 L 7 4 4F A20WE 1996062700144 19960627 00144 NM 1996 6 27 9613652703 1 19960605 A 3150 T/O WARNING BOEING 727 727225 1384077 NM COCKPIT SOUNDED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 8878Z 21451 DURING TAKEOFF ROLL, TAKEOFF WARNING HORN SOUNDED. ABORTED TAKEOFF WITHOUT INCIDENT AND PERFORMED TAKEOFF WARNING CHECK . ADJUSTED SWITCHES S196 AND S294, OPERATIONAL CHECK OF SYSTEM OK. 2 L 7 3 4F A3WE 1996062700145 19960627 00145 1996 6 27 9613669763 4 19960620 A 3421 VERTICAL GYRO DOUG DC9 DC941 302207N WP E/E COMPT FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 01 763NW 47396 DURING CRUISE, WEATHER RADAR BECAME INOPERATIVE. DUE TO EN ROUTE WEATHER, FLIGHT DIVERTED TO ATL AND LANDED WITHOUT INC IDENT. REPLACED NR 1 VERTICAL GYRO, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996062700146 19960627 00146 WP 1996 6 27 ABXA9600510 1 19960619 A 2730 01537053 BOLT NIHON YS11 YS11A500 6310416 WP ELEVATOR SHEARED A ABXA K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 GL 23 910AX 2050 DISCOVERED A BINDING ELEVATOR DURING PREFLIGHT. FOUND ELEVATOR DOWN SPRING ROD ATTACH BOLT SHEARED. REPLACED BOLT AND CHECKED DOWN SPRING INSTALLATION IAW YS-11 MM CHAPTER 27-31-3, NO DEFECTS NOTED. 2 L 7 2 4T A1PC 1996062700147 19960627 00147 WP 1996 6 27 ABXA9600511 1 19960614 A 3241 420531B CONTROL BOX DOUG DC8 DC861 3021952 WP ANTI-SKID SYST DEFECTIVE A ABXA O OTHER O OTHER LD LANDING 1 GL 23 850AX 402 45894 BRAKES FAILED WITH ANTI-SKID SYSTEM ARMED WITH AIRCRAFT BELOW 15 KIAS ON LANDING. REPLACED ANTI-SKID CONTROL BOX IAW DC 8 MM CHAPTER 32-43-6 AND OPS CHECK WAS GOOD. 2 L 7 4 4F 4A25 1996062700149 19960627 00149 1996 6 27 CALA9600851 4 19960619 A 2565 D29984109 SLIDE DOUG DC9 DC982 3022082 WP TAILCONE LOW PRESSURE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69826 49486 INSPECTION FOUND AFT TAILCONE SLIDE BOTTLE PRESSURE LOW. THE TAILCONE SLIDE WAS REMOVED AND REPLACED IAW MM 25-62-02. 2 L 7 2 4F A6WE 1996062700150 19960627 00150 NM 1996 6 27 CALA9600852 1 19960524 A 5330 SKIN BOEING 737 737130 1384435 NM BS 344-380 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 24213 19030 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 344 TO 380, STRINGER 20R TO 22R. THE DENTED AREA OF SKIN WAS CUT OUT AND N EW SKIN, FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 1 AND 9, SRM 51-10-2 AND 51-30-2. 2 L 7 2 4F A16WE 1996062700151 19960627 00151 NM 1996 6 27 CALA9600853 1 19960529 A 5320 FRAME BOEING 737 737130 1384435 NM C-1 DOORWAY CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 24213 19030 INSPECTION FOUND A 3 INCH CRACK IN UPPER FLANGE OF C-1 DOORWAY AFT FRAME. THE CRACKED FRAME WAS REMOVED AND A NEW FRAME SECTION WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-2 AND BOEING DRAWING 65C35242. 2 L 7 2 4F A16WE 1996062700152 19960627 00152 NM 1996 6 27 CALA9600854 1 19960529 A 5320 ANGLE BOEING 737 737130 1384435 NM NLG WW CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 24213 19030 INSPECTION FOUND NOSE WHEEL WELL CEILING SUPPORT I BEAM AND ATTACHING ANGLES CORRODED. THE BEAM AND ANGLES WERE REMOVED . A NEW BEAM AND ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-30-5, 51-30-2 AND 51-10-2. 2 L 7 2 4F A16WE 1996062700153 19960627 00153 NM 1996 6 27 CALA9600855 1 19960529 A 5313 STRINGER BOEING 737 737130 1384435 NM BS 351.5-360 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 24213 19030 INSPECTION FOUND STRINGER CHANNEL CORRODED AT STA 351.2 TO 360, S20L. THE STRINGER CHANNEL WAS REMOVED AND A NEW CHANNE L WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2 AND BOEING DRAWING 69-48934. 2 L 7 2 4F A16WE 1996062700154 19960627 00154 NM 1996 6 27 CALA9600856 1 19960529 A 5330 SKIN BOEING 737 737130 1384435 NM BS 1016 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 24213 19030 INSPECTION FOUND FUSELAGE SKIN DENTED IN TWO PLACES AT STA 1016, S29R. THE DENTED AREAS WERE CUT OUT, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 1 SRM 51-30-2 AND 51-10-2. 2 L 7 2 4F A16WE 1996062700155 19960627 00155 WP 1996 6 27 MWEA96249 1 19960614 A 5320 BRACKET DOUG DC9 DC932 3022066 WP BS 996 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 DURING CERT INSP, FOUND AN AFT RT BRACKET CRACKED ON RT INTERCOSTAL AT STA 996.0. FABRICATED A NEW BRACKET IAW SRM 53-0 1, PAGE 1 AND INSTALLED IAW SRM 53-01, PAGE 1. 2 L 7 2 4F A6WE 1996062700156 19960627 00156 WP 1996 6 27 MWEA96250 1 19960614 A 5711 SPAR DOUG DC9 DC932 3022066 WP WS 69/91 CORROSION A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 026ME 47791 DURING CERT INSP, LT WING INTERIOR AFT SPAR FOUND WITH MILD CORROSION ON REAR SPAR HORIZONTAL SURFACE AT STA XRS 69.000 AND XRS 91.000. REMOVED CORROSION IAW SRM 51-03-3, SHOT PEENED AFFECTED AREA OF SPAR, TREATED, PRIMED AND INSTALLED STR AP PER DAC TELEX SVC-MSP-0311/AJC. 2 L 7 2 4F A6WE 1996062700157 19960627 00157 WP 1996 6 27 MWEA96251 1 19960619 A 5247 59150817 APU ACCESS DOOR DOUG DC9 DC932 3022066 WP AFT FUSELAGE UNLATCHED A MWEA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 31 301ME 47190 PILOT REPORTS, VIBRATION FELT IN RUDDER PEDALS AT 240 KTS. A/C RETURNED TO MKE. FOUND LT APU ACCESS DOOR HAD COME OPEN TO CAUSE VIBRATION. REPLACED DOOR, NO OTHER DAMAGE NOTED. 2 L 7 2 4F A6WE 1996062700158 19960627 00158 NM 1996 6 27 P5CA9600247 1 19960620 A 2923 AIR DRIVEN PUMP BOEING 747 747122 1384872 NM NR 1 ENGINE PRESS FLUX A P5CA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 850FT 19755 ON TAXI OUT, NR 1 ADP INOP, PRESSURE FLUCTUATION 0 TO 2500 PSI, RETURNED TO BLOCKS. CLEANED FILTERS, RESET OVERSPEED SW ITCH AND LUBED REGULATOR SHUTOFF VALVE AND OPERATIONAL CHECK GOOD IAW MM 29-11-05. 2 L 7 4 4F A20WE 1996062700159 19960627 00159 NM 1996 6 27 P5CA9600248 1 19960620 A 2915 373703 PRESS MODULE BOEING 747 747122 1384872 NM NR 3 SYSTEM CRACKED A P5CA K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 WP 23 852FT 19757 ON ARRIVAL, FOUND HYDRAULIC LEAK FROM NR 3 HYDRAULIC SYSTEM IN SAILBOAT AREA. FOUND NR 3 HYDRAULIC SYSTEM PRESSURE MODU LE HOUSING CRACKED. REMOVED AND REPLACED SAME, OPS AND LEAK CHECK NORMAL IAW MM 29-11-23. 2 L 7 4 4F A20WE 1996062700160 19960627 00160 NM 1996 6 27 QXEA9600210 1 19960620 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT INOPERATIVE A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 827PH 275 PORTABLE EMERGENCY LIGHT IN COCKPIT IS INOP. LIGHT REPLACED AND LIGHT OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 1996062700161 19960627 00161 NM 1996 6 27 QXEA9600211 1 19960620 A 3350 82410162007 CONTROL BOX DHAV DHC8 DHC8102 2809003 NM CABIN MALFUNCTIONED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 818PH 58 UNABLE TO RESET EMERGENCY LIGHTING. EMERGENCY LIGHTING CONTROL BOX REPLACED AND EMERGENCY LIGHTS OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 1996062700162 19960627 00162 EU 1996 6 27 QXEA9600212 1 19960620 A 3350 0L3071BPE BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 466US 11075 SEAT 6AB FLOOR PROXIMITY LIGHT IS INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996062700163 19960627 00163 EU 1996 6 27 QXEA9600213 1 19960620 A 3350 1315 BULB FOKKER F28 F28MK1000 4990808 EU LT UNDER WING FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 466US 11075 LEFT HAND UNDER WING EMERGENCY EXIT LIGHT INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996062700164 19960627 00164 EU 1996 6 27 QXEA9600214 1 19960620 A 3350 1312 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 452US 11105 LEFT WING EMERGENCY EXIT LIGHT IS INOP. BULBS WERE REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996062700165 19960627 00165 EU 1996 6 27 QXEA9600215 1 19960620 A 3350 MGG1280 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 450US 11101 MID CABIN OVERHEAD EXIT SIGN ISN'T ILLUMINATED ON THE BACK SIDE. BULBS WERE REPLACED AND SIGN OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996062700166 19960627 00166 SW 1996 6 27 QXEA9600216 1 19960619 A 3230 27192480001 SPRING SWRNGN SA227 SA227AC 8780603 SW LT MLG WEAK A QXEA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 NM 09 2727B AC730 FAILED TO GET A LEFT MAIN GEAR DOWN AND LOCKED INDICATION ON APPROCH. GEAR WAS RECYCLED AND STILL NO INDICATION. AFTER INITIATION OF A GO-ROUND THE LIGHT ILLUMINATED. AIRCRAFT LANDED WITHOUT FURTHER PROBLEMS. LEFT MAIN GEAR INSPECTED AN D AIRCRAFT FERRIED TO PDX FOR REPAIR. LEFT MAIN GEAR INBOARD BELL CRANK SPRING REPLACED AND GEAR OPS CHECKED GOOD ON GE AR SWING. 2 L 7 2 4T RT A8SW 1996062700167 19960627 00167 NM 1996 6 27 SWAA960565 1 19960617 A 2612 FIRE WIRE BOEING 737 7372H4 138448C NM APU SHORTED A SWAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 29SW 21340 DIVERSION DUE TO APU FIRE WARNING IN FLIGHT. FIRE BOTTLE WAS DISCHARGED. INSPECTED AND FOUND NO EVIDENCE OF FIRE OR OV ERHEAT CONDITION. DEFERRED FIRE DETECT SYSTEM PER MEL, FOUND AND REPAIRED SHORTED WIRE PER BOEING M/M. 2 L 7 2 4F A16WE 1996062700168 19960627 00168 NM 1996 6 27 SWAA960566 1 19960618 A 5330 SKIN BOEING 737 7372H4 138448C NM AFT ENTRY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 62SW 22060 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR UPPER HINGE CUTOUT CRACKED .5 INCH LONG ON OUTER SKIN. REPAIRED PER BOE ING SRM. 2 L 7 2 4F A16WE 1996062700169 19960627 00169 NM 1996 6 27 SWAA960567 1 19960618 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 780 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED TERMINAL CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 780, AT S20R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996062700170 19960627 00170 NM 1996 6 27 SWAA960568 1 19960618 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 370/936/980 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 86SW 22827 DURING SCHEDULED HD CHECK, FOUND FUSELAGE SKIN DENTED AT BS 370, S25L, AT BS 980, S22L AND AT BS 936 AT S19L. REPAIRED ALL PER BOEING SRM. 2 L 7 2 4F A16WE 1996062700171 19960627 00171 NM 1996 6 27 SWAA960569 1 19960620 A 5320 ANGLE BOEING 737 7375H4 138449D NM BS 290 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 514SW 25153 DURING SCHEDULED 1/2 CHECK, FOUND ANGLE CRACKED ABOVE STRINGER 10R, FWD OF SERVICE DOOR, BS 290. REPLACED PER BOEING SR M. 2 L 7 2 4F RT A16WE 1996062700172 19960627 00172 NM 1996 6 27 SWAA960570 1 19960620 A 5230 WEB BOEING 737 7372H4 138448C NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 26SW 21117 DURING SCHEDULED B2 CHECK, FOUND FWD CARGO DOOR LOWER WEB CRACKED ORIGINATING FROM RIVET HOLE, ADJACENT TO AFT/LOWER STO P FITTING. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996062700173 19960627 00173 NM 1996 6 27 SWAA960571 1 19960620 A 5330 SKIN BOEING 737 7373H4 1384600 NM FWD FUSELAGE DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 373SW 26581 DURING SCHEDULED TERM CHECK, FOUND FUSELAGE SKIN DENTED 30 BELOW CAPT WINDOW. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996062700174 19960627 00174 NM 1996 6 27 SWAA960572 1 19960620 A 5230 FRAME BOEING 737 7373H4 1384600 NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED B/C1 CHECK, FOUND FWD CARGO DOOR FRAME CRACKED BELOW CEILING HOOK. REPAIRED PER SWA RA 1-A52-198. 2 L 7 2 4F RT A16WE 1996062700175 19960627 00175 NE 1996 6 27 9613676717 2 19960621 A 7200 ENGINE BOEING 747 747251F 1384898 NM PWA JT9 JT9D7F 52054 NE NR 1 MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 GL 01 617US 21121 89562 DURING TAKEOFF ROLL, THE NR 1 ENGINE EGT WENT INTO THE YELLOW RANGE FOR APPROXIMATELY FIVE MINUTES. THE EGT THEN SETTLE D AT 910 DEGREES AT FL250. ALSO, THE NR 1 ENGINE NACELLE TEMPERATURE 'B' LOOP WENT TO TOP OF GREEN FOR FIVE MINUTES, WI TH NR 1 ENGINE OIL PRESSURE OSCILLATING AT 3 PSI. CREW MADE THE DECISION TO DIVERT FLIGHT TO MSP FOR INSPECTION. THE E NGINE WAS CHANGED AND CHECK WAS NORMAL. 2 L 7 4 4F 4 F A20WE E20EA 1996062700176 19960627 00176 NE 1996 6 27 9613685530 2 19960621 A 7230 COMPRESSOR BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE NR 2 ENGINE STALLED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 01 530US 23845 716457 DURING CLIMB, NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL. THE ENGINE OIL PRESSURE DROPPED AND ENGINE WAS SHUT DOWN. AI RCRAFT RETURNED TO MSP. GROUND MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 1996062700177 19960627 00177 NM 1996 6 27 9613692768 1 19960622 A 3241 40835 TRANSDUCER BOEING 727 7272M7 138407S NM LT MLG MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 01 728RW 21741 DURING CRUISE FLIGHT, THE INBOARD ANTI-SKID INDICATED INOPERATIVE. AIRCRAFT DIVERTED TO JFK AND LANDED WITHOUT INCIDENT . MAINTENANCE PERFORMED CAPACITANCE CHECK OF WIRING FROM ANTI-SKID CONTROL BOX TO TRANSDUCERS AND ANTI-SKID VALVES, WIR ING CHECKED OK. REPLACED INBOARD TRANSDUCER AND BOTH ANTI-SKID VALVES. 2 L 7 3 4F A3WE 1996062700178 19960627 00178 1996 6 27 9613706632 4 19960623 A 3414 ADC BOEING 747 747251B 1384892 NM LEFT MALFUNCTIONED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 632US 23112 DURING CLIMB, BOTH CAPTAIN'S AND FIRST OFFICER'S AIRSPEED INDICATIONS WERE INACCURATE. AIRCRAFT RETURNED TO TPE AND LAN DED WITHOUT INCIDENT. REPLACED THE NR 1 AIR DATA COMPUTER, CAPTAIN'S AIRSPEED INDICATOR AND RECONNECTED THE FIRST OFFIC ER'S AIRSPEED INDICATOR'S STATIC PORT, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996062700179 19960627 00179 NM 1996 6 27 9613716601 1 19960623 A 2613 OVERHEAT WIRE BOEING 747 747151 1384891 NM NR 3 HYD BAY FAILED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 601US 19778 DURING CLIMB, THE NR 3 HYDRAULIC SYSTEM OVERHEAT LIGHT ILLUMINATED. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND LI GHT REMAINED ILLUMINATED. AIRCRAFT RETURNED TO NRT AND LANDED WITHOUT INCIDENT. REPAIRED WIRE FOR OVERHEAT INDICATION IN THE NR 3 HYDRAULIC BAY, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996062700180 19960627 00180 NM 1996 6 27 96FDEA00873 1 19960430 A 5320 6540273 SHEAR TIE BOEING 727 72725 1384006 NM BS 1050 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 NR0520 AND 019, CORROSION ON FRAME SHEAR TIE AT BS 1050 LBL 10 WL 141. *S/D* BLENDED OUT CORROSION FOUND TO BE OUT OF LIMITS AS PER FEDEX SRM 53-10-1, FABRICATED AND INSTALLED REPAIR PART AS PER FEDEX SRM 53-10-4 FIG 11. 2 L 7 3 4F A3WE 1996062700181 19960627 00181 NM 1996 6 27 96FDEA01113 1 19960613 A 5320 65229592 CHORD BOEING 727 72722 1384002 NM BS 914.5 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 NR0545 AND 020, CRACK IN I/B FLANGE OF STR 18A REINFORCEMENT CHORD BS 914.5 RBL 63.7 WL 189. *S/D* REPAIRED CRACK IN I /B FLANGE OF STR 18A REINFORCEMENT CHANNEL BS 914.5 RBL 63.7 WL 189 FEDEX EA 7-5310-29176, FUNCTIONALLY TEST GOOD PER FE DEX MM 32-30-0. 2 L 7 3 4F A3WE 1996062700182 19960627 00182 NM 1996 6 27 96FDEA01120 1 19960613 A 5320 5717752009 WEB BOEING 727 72722 1384002 NM BS 234-259 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 NR0610 AND 027, CORROSION (C53-224-01) UNDER WEB BETWEEN STA 234 TO 259 WL 227 LBL 48. 2 L 7 3 4F A3WE 1996062700183 19960627 00183 NM 1996 6 27 96FDEA01146 1 19960616 A 5315 6518420 FLOOR BEAM BOEING 727 72725 1384006 NM BS 1130 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 NR0440 AND 044, CORROSION (C53-111-01) ON LOWER FLOOR BEAM FLANGE AT BS 1130 RBL 29, 36 LBL 8 AND 20 WL 200. *S/D* REM OVED CORROSION FROM LOWER FLOOR BEAM FLANGE AT BS 1130 RBL 29, 36 LBL 8 AND 20 WL 200. REPAIRED IAW FEDEX SRM 53-10-08 FIG 8 AND EX EA 7-5310-28354. 2 L 7 3 4F A3WE 1996062700184 19960627 00184 NM 1996 6 27 96FDEA01147 1 19960619 A 5315 BAC1505100617 FLOOR BEAM BOEING 727 72725 1384006 NM BS 1110 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 NR0485 AND 045, CORROSION ON FLOOR BEAM BS 1110 AROUND NUTCLIP HOLES WL 208 RBL 25 TO 54. *S/D* REMOVED CORROSION AND REPAIRED TOP CHORD OF FLOOR BEAM BS 1110 WL 208 RBL 10 TO 65 PER FEDEX SRM 53-10-8. 2 L 7 3 4F A3WE 1996062700185 19960627 00185 NM 1996 6 27 96FDEA01148 1 19960619 A 5313 651851149 STRINGER BOEING 727 72722 1384002 NM BS 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 NR0587 AND 035, WHILE WORKING NRO213 FOUND CRACK AND GOUGE IN STR 4R BS 600 IN U-CHANNEL. *S/D* REMOVED DAMAGE AT BS 6 00 STR 4R, REPAIRED PER FEDEX SRM 53-10-1 FIG 1. 2 L 7 3 4F A3WE 1996062700186 19960627 00186 NM 1996 6 27 96FDEA01149 1 19960619 A 5315 65208277 FLOOR BEAM BOEING 727 72722 1384002 NM BS 680 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 NR0354 AND 036, CORROSION (C53-224-01) ON FLOOR BEAM TOP CHORD BS 680 RBL 2 TO 25 WL 208. *S/D* REPAIRED TOP CHORD OF FLOOR BEAM AT BS 680 RBL 2 TO 25 WL 208.1 PER FEDEX SRM 53-10-8 FIG 3. 2 L 7 3 4F A3WE 1996062700187 19960627 00187 NM 1996 6 27 96FDEA01150 1 19960619 A 5330 6518420 SKIN BOEING 727 727225 1384077 NM BS 189 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 467FE 21449 NR0447 AND 010, DENT AT BS 189 STR 28L WAS FOUND TO BE OUT OF LIMITS. *S/D* REPAIRED SKIN AT BS 189 STR 28L PER FEDEX SRM 53-30-3. 2 L 7 3 4F A3WE 1996062700188 19960627 00188 NM 1996 6 27 96FDEA01151 1 19960619 A 5330 65C135472 SKIN BOEING 727 727225 1384077 NM BS 720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 467FE 21449 NR0228 AND 011, CORROSION (C53-113-01, -1) ON INNER SURFACE OF SKIN BS 720B TO 720B PLUS 3 LBL 3 TO RBL 3 WL 148.5. *S/ D* REMOVED CORROSION FROM INNER SURFACE OF SKIN PANEL NR 3363. FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. FABRI CATED TREATED AND INSTALLED PANEL NR 3363 IAW FEDEX SRM 53-30-1. 2 L 7 3 4F A3WE 1996062700189 19960627 00189 NM 1996 6 27 96FDEA01154 1 19960619 A 5320 69208135 SHEAR TIE BOEING 727 727225 1384077 NM BS 1130 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 467FE 21449 NR0158 AND 014, CORROSION (C53-113-10, -2) ON FRAME WEB AND SHEAR TIE AT BS 1130 RBL 8 TO 11 WL 147. *S/D* REMOVED COR ROSION FROM FRAME WEB AND FOUND TO BE IN LIMITS PER FEDEX SRM 51-10-1. REMOVED, FABRICATED AND INSTALLED SHEAR TIE IAW FEDEX SRM 51-10-6 AND 53-10-1. 2 L 7 3 4F A3WE 1996062700190 19960627 00190 NM 1996 6 27 96FDEA01156 1 19960614 A 5320 69298134 SHEAR TIE BOEING 727 727225 1384077 NM BS 1130 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 467FE 21449 NR0159 AND 009, CORROSION (C53-113-10, -2) ON FRAME WEB AND SHEAR TIE AT BS 1130 LBL 1 TO 4 WL 147. *S/D* REMOVED CORR OSION ON FRAME WEB, FOUND TO BE WITHIN LIMITS PER FEDEX SRM 53-10-1. REMOVED AND REPLACED SHEAR TIE IAW FEDEX SRM 51-10 -1 AND 51-20-1. 2 L 7 3 4F A3WE 1996062700191 19960627 00191 1996 6 27 96FDEA01161 4 19960620 A 3454 066106048 VOR RECEIVER BOEING 727 727233 138408A NM E/E COMPT MALFUNCTIONED A FDEA L A ABORTED APPROACH UNSCHED LANDING I FLT. ATTITUDE INST. AP APPROACH 1 SO 25 265FE 21671 IN STABILIZED APPROACH, AUTO PILOT VERY UNSTABLE IN PITCH AXIS A SERVO. AUTO PILOT PTICHES UP AND DOWN WITH ASSOCIATED TRIM RUNS TO TRY AND CAPTURE GLIDE SLOPE. A/C RELEASED FOR SERVICE PER MEL 22-1G CATEGORY C EXP 6-30-96 AUTO PILOT GLI DE SLOPE FUNCTIONS INOPERATIVE. REPLACED VOR/ILS RECEIVER, PER MM 34-31-21. 2 L 7 3 4F RT A3WE 1996062700192 19960627 00192 NM 1996 6 27 96FDEA01162 1 19960621 A 2750 652661457 TRANSMISSION BOEING 727 7272D4 138407U NM LT TE FLAP FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 SO 25 287FE 21849 INBOARD T/E FLAPS SPLIT. REMOVED AND REPLACED L/FLAP I/B TRANSMISSION PER MM 27-51-41, OPS CK GOOD. REQ ITEM INSP COMP LIED WITH. 2 L 7 3 4F A3WE 1996062700193 19960627 00193 NM 1996 6 27 96FDEA01163 1 19960622 A 3260 CONNECTOR BOEING 727 727277 138408S NM LT MLG DOOR DIRTY A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 246FE 20268 LT MGD RED LIGHT REMAINED ON AFTER RAISING GEAR. ACCOMPLISHED RED PAGES PROCEDURES, LIGHT WENT OUT AFTER RECYCLING GEAR . LIGHT FLICKERED AGAIN IN CRUISE, SLOWED TO 270 KNOTS LIGHT CONTINUED TO FLICKER THROUGHOUT FLIGHT. FOUND PLUG FOR DO OR SWITCH UNLOCKED. CLEANED AND RESECURED TESTED PER MM 32-62-11. 2 L 7 3 4F RT A3WE 1996062700194 19960627 00194 NM 1996 6 27 96FDEA01164 1 19960621 A 5754 65162261 BONDING JUMPER BOEING 727 72722 1384002 NM NR 2 LE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 NRO0684 AND 037, NR 2 K-FLAP HAS CORROSION AROUND I/B BONDING JUMPER UPPER AND LOWER ATTACH POINTS. *S/D* BLENDED CORR OSION AND REPAIRED RIB IAW FEDEX SRM 57-50-3 AND FEDEX DRAWING SR 27-57-010 REV B. 2 L 7 3 4F A3WE 1996062700195 19960627 00195 NM 1996 6 27 96FDEA01165 1 19960621 A 5320 6540273 SHEAR TIE BOEING 727 72725 1384006 NM BS 970 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 NR0516 AND 047, CORROSION (C53-111-01-3), (C53-113-01-2) ON FRAME SHEAR TIE AT BS 970 LBL 12 WL 139. *S/D* BLENDED COR ROSION ON SHEAR TIE, FOUND TO BE OUT OF LIMITS. REPAIRED PER FEDEX SRM 53-10-4. 2 L 7 3 4F A3WE 1996062700196 19960627 00196 NM 1996 6 27 96FDEA01166 1 19960621 A 5320 652427635 T-CLIP BOEING 727 727225 1384077 NM BS 1177 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 467FE 21449 NR0151 AND 016, CORROSION (C53-113-10, -2) ON T-CLIP AT BS 1177 RBL 32 WL 170. *S/D* REMOVED AND REPLACED T-CLIP AT BS 1177 RBL 32 WL 170 IAW FEDEX SRM 53-10-4. 2 L 7 3 4F A3WE 1996062700197 19960627 00197 NE 1996 6 27 CALA9600857 2 19960621 A 7530 575157 STATOR VANE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 1 ENGINE FAILED A CALA O OTHER O OTHER DE DESCENT 1 SW 09 14816 49370 709832 THE NR 1 ENGINE COMPRESSOR STALLED AT 37,000 FEET WHEN POWER WAS REDUCED FOR DESCENT. THE STALL WAS ACCOMPANIED BY TWO BANGS AND SUBSEQUENT YAW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED. THE SDR WIL L REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION. SHOP TEARDOWN FINDINGS REVEALED FAILURE OF A C-7 STATOR VANE. 2 L 7 2 4F 4 F A6WE E9NE 1996062700198 19960627 00198 NE 1996 6 27 CALA9600858 2 19960621 A 7510 320115CAL FUEL HEAT VALVE BOEING 737 737130 1384435 NM PWA JT8 JT8D7 52053 NE NR 1 ENGINE INOPERATIVE A CALA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SW 09 59207 19024 654112 THE NR 1 ENGINE OIL TEMPERATURE WENT INTO THE YELLOW BAND AFTER DEPARTURE FROM EWR. THE ENGINE WAS SHUT DOWN AND THE AI RCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE FUEL HEAT VALVE NOT SEATING PROPERLY . THE FUEL HEAT VALVE WAS REPLACED, ALL CHECKS WERE GOOD DURING A HIGH POWER ENGINE RUN. 2 L 7 2 4F 4 F A16WE E2EA 1996062700199 19960627 00199 NE 1996 6 27 CALA9600859 2 19960622 A 7260 GEARBOX BOEING 737 737130 1384435 NM PWA JT8 JT8D7 52053 NE NR 1 ENGINE LEAKING A CALA A E UNSCHED LANDING ENGINE SHUTDOWN J K WARNING INDICATION FLUID LOSS CL CLIMB 1 SW 09 59207 19024 654112 THE NR 1 ENGINE OIL PRESSURE ROSE TO OVER 60 PSI AFTER TAKEOFF. WHEN THE NR 1 THROTTLE WAS RETARDED, THE OIL TEMPERATUR E ROSE BEYOND THE RED LINE. THE NR 1 ENGINE WAS SHUTDOWN AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT I NCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED DUE TO OIL LEAKAGE. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PE NDING INVESTIGATION. *S/D* SHOP FINDINGS REPORTED THE GEARBOX WAS REMOVED AND REPLACED AND SUBSEQUENT TESTING WAS GOOD . 2 L 7 2 4F 4 F A16WE E2EA 1996062700200 19960627 00200 NM 1996 6 27 CALA9600860 1 19960620 A 5315 FLOOR BEAM BOEING 727 727243 138408D NM BS 1130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 571PE 21264 INSPECTION FOUND CORROSION ON FLOOR BEAM AT STA 1130, RT SIDE OF AIRCRAFT. THE FLOOR BEAM WAS REPAIRED IAW ECRA 5310-03 297. 2 L 7 3 4F RT A3WE 1996062700201 19960627 00201 WP 1996 6 27 CALA9600861 1 19960621 A 5350 S2274640 CLIPS DOUG DC9 DC932 3022066 WP TAILCONE WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14534 47110 THE TAILCONE INTERIOR RELEASE HANDLE CLIPS WERE FOUND WORN AND THE HANDLE PULLED FROM CLIPS AT 5 POUNDS. THE CLIPS WERE REMOVED AND REPLACED. 2 L 7 2 4F A6WE 1996062700202 19960627 00202 WP 1996 6 27 CALA9600862 1 19960621 A 5350 3913359547 CABLE DOUG DC9 DC932 3022066 WP TAILCONE TWISTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14534 47110 INSPECTION FOUND TAILCONE RELEASE CABLE ON LEFT HAND SIDE AT TIMING BLOCK DAMAGED AND TWISTED. THE CABLE WAS REMOVED AN D REPLACED. 2 L 7 2 4F A6WE 1996062700203 19960627 00203 WP 1996 6 27 CKSA96061 1 19960620 A 2612 FIRE LOOP LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB211524B02 54555 NE NR 2 ENGINE MALFUNCTIONED A CKSA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 103CK 293C1212 14525 NR 2 ENGINE A-FIRE DETECTION LOOP CAME ON STEADY IN CLIMB. SWITCHED TO B-LOOP AND TEST IAW OPS MANUAL CHECKED GOOD. APP ROXIMATELY 5 MINUTES LATER FIRE WARNING SOUNDED ON B-LOOP, SHUT NR 2 ENGINE DOWN IAW OPS MANUAL. INSPECTED NR 2 ENGINE, NO DEFECTS FOUND. SWAPPED APU AND NR 2 ENGINE FIRE DETECTOR CONTROL UNITS FOR FURTHER TROUBLESHOOTING. APU FIRE DETEC TION SWITCH CHECKS NORMAL AND PERFORMED HIGH POWER RUN ON NR 2 ENGINE, CHECKS NORMAL ON GROUND AT THIS TIME. 2 L 7 3 4F 4 F A23WE E12EU 1996062700204 19960627 00204 SO 1996 6 27 COMA9610185 1 19960619 A 2913 63163 HYD PUMP EMB 120 EMB120RT SO LT ENGINE FAILED A COMA K NONE O OTHER CR CRUISE 1 SO 01 159A 120159 LEFT ENGINE DRIVEN HYDRAULIC PUMP FAILED. REPLACED HYDRAULIC PUMP. 2 L 7 2 4T RT A31SO 1996062700205 19960627 00205 SO 1996 6 27 COMA9610186 1 19960622 A 3610 44E202A SEPARATOR EMB 120 EMB120RT SO LT WING CRACKED A COMA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 254CA 120233 LT BLEED AIR DUCT LEAK WARNING CAME ON AFTER TAKEOFF. REPLACED THE LT BLEED AIR WATER SEPARATOR. 2 L 7 2 4T RT A31SO 1996062700206 19960627 00206 SO 1996 6 27 COMA9610187 1 19960621 A 6120 78249012 PCU EMB 120 EMB120RT SO LT ENGINE MALFUNCTION A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 249CA 120230 LEFT ENGINE PROPELLER RPM WAS ONLY 98 PERCENT WHEN SET FOR MAX RPM. REPLACED THE LT PROPELLER CONTROL UNIT. 2 L 7 2 4T RT A31SO 1996062700207 19960627 00207 NE 1996 6 27 COMA9630130 2 19960621 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RIGHT OVER TEMP A COMA C D ABORTED TAKEOFF RETURN TO BLOCK M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 SO 01 357CA 340A044 367438 RT ENGINE ITT REACHED 945 DEGREES DURING TAKEOFF. REPLACED THE RT ENGINE. 2 L 7 2 4T 4 T RT A52EU E8NE6 1996062700209 19960627 00209 WP 1996 6 27 MWEA96252 1 19960623 A 2560 5917683003 EVAC SLIDE COVER DOUG DC9 DC932 3022066 WP GALLEY DOOR FELL OFF A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 CREW REPORTS, GALLEY DOOR EVACUATION SLIDE COVER FELL OFF. REINSTALLED GALLEY DOOR SLIDE COVER. 2 L 7 2 4F A6WE 1996062700210 19960627 00210 NM 1996 6 27 P5CA9600249 1 19960615 A 3510 80080103 OXY CONTROL UNIT BOEING 747 747123 1384873 NM COCKPIT LEAKING A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 DURING MAINTENANCE, DISCOVERED LEAK IN CREW OXYGEN SYSTEM. REMOVED AND REPLACED CONTROL UNIT IAW MM 35-11-00, LEAK CHEC K OK. 2 L 7 4 4F A20WE 1996062700211 19960627 00211 NM 1996 6 27 P5CA9600250 1 19960615 A 3520 80132107 COUPLING BOEING 747 747123 1384873 NM PAX OXY SYSTEM LEAKING A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 DURING MAINTENANCE, FOUND LEAK IN PASSENGER OXYGEN SYSTEM. REMOVED AND REPLACED COUPLING IAW MM 35-21-00, LEAK CHECK NO RMAL. 2 L 7 4 4F A20WE 1996062700212 19960627 00212 NM 1996 6 27 QXEA9600217 1 19960621 A 3350 82410162007 CONTORL BOX DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 818PH 58 EMERGENCY LIGHTS WILL NOT RESET. EMERGENCY LIGHT CONTROL BOX REPLACED AND LIGHTS OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 1996062700213 19960627 00213 EU 1996 6 27 QXEA9600218 1 19960622 A 3350 6008903 BATTERY PACK FOKKER F28 F28MK1000 4990808 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 450US 11101 RIGHT SIDE OVERWING EMERGENCY EXIT LIGHT AND EXIT SIGN DO NOT ILLUMINATE. BATTERY PACK REPLACED IAW MAIINT MANUAL, LIGH TS OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996062700214 19960627 00214 NE 1996 6 27 VNAA9606007 3 19960619 A 6111 E6212 PROPELLER ASSY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT ENGINE DEFECTIVE A A VNAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 07 429JS 3043 HL190 THE RIGHT ENGINE OIL PRESSURE BEGAN TO FLUCUATE SHORTLY AFTER TAKEOFF. F/O OBSERVED OIL COMING FROM THE FORWARD NACELLE AREA, AFT OF THE PROP. CREW SECURED THE RIGHT ENGINE, CONTACTED ATC TO REPORT THE SITUATION RETURNED TO THE FIELD AND LANDED WITHOUT FURTHER INCIDENT. MECHANICS WERE DISPATCHED FROM DAY TO CMH. INITIAL INSPECTION REVEALED A MISSING O-RI NG FROM THE PROPELLER SPINNER BULKHEAD AND A CAP MISSING FROM THE PROPELLER HUB ASSEMBLY. MX REPLACED THE RIGHT HAND PR OPELLER ASSEMBLY IAW 61-10-00 SERVICE THE ENGINE OIL, GROUND RUNS CHECKED GOOD. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996062700215 19960627 00215 EU 1996 6 27 96ZZZX3099 1 19960515 A 2120 AIR DIST BAG BAE146 BAE146100A 1500260 EU CABIN ODOR A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 31 463AP E1063 ORD - PREVIOUS CREW REPORTS VISUAL SMOKE AND OIL SMELL IN CABIN DURING IN-FLIGHT PORTION OF THE FLIGHT. GROUND RAN ENGI NES AND APU, TEST FLIGHT C/W. NO DUPLICATE. 2 H 7 4 4F RT A49EU 1996062700216 19960627 00216 EU 1996 6 27 96ZZZX3100 1 19960417 A 5312 BULKHEAD BAG BAE146 BAE146300A 1500267 EU RT MLG WW GOUGED A A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 616AW E3145 ATW - RT MLG BAY FRAME 29 BULKHEAD HAS A GOUGE APPROXIMATELY 8.50 INCHES LONG WITH 4 DAMAGED RIVET HEADS AND IS APPROXIM ATEY .009 INCH DEEP. AFTER REMOVAL OF PAINT, RE-MEASURED DEPTH FOUND TO BE .007 INCH DEEP AND REPORTED TO BAE. NDT WAS ACCOMPLISHED ON WC NR 1063. BLENDED, REPLACED 7 RIVETS AND FINISHED, AND TOP COATED AS DESCRIBED IN BAE FAX REF DJR/RJ 0498-96 ALLOWABLE PER FAX DJR/RJ0498. 2 H 7 4 4F RT A49EU 1996062700218 19960627 00218 EU 1996 6 27 96ZZZX3102 1 19960410 A 5260 RAIL BAG BAE146 BAE146300A 1500267 EU FWD AIRSTAIR CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 616AW E3145 ATW - FORWARD AIRSTAIR INBOARD RAIL IS CORRODED AT FORWARD END. REMOVED AND REPLACED INBOARD RAIL AS NEEDED IAW MM. 2 H 7 4 4F RT A49EU 1996062700219 19960627 00219 EU 1996 6 27 96ZZZX3103 1 19960410 A 5310 STRUCTURE BAG BAE146 BAE146300A 1500267 EU FWD LAVATORY CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 616AW E3145 ATW - SEVERAL PLACES CORRODED ON FLOOR STUCTURE UNDER FWD LAV MODULE. REMOVED SURFACE CORROSION ON FLOOR STRUCTURE UNDE R LAV MODULE, TREATED, PRIMED AND PAINTED. 2 H 7 4 4F RT A49EU 1996062700220 19960627 00220 EU 1996 6 27 96ZZZX3104 1 19960410 A 5540 HINGE BAG BAE146 BAE146300A 1500267 EU RUDDER CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 616AW E3145 ATW - VISIBLE PORTION OF RUDDER HINGE BOLTS AT RIBS 20 AND 29 ARE CORRODED. REMOVED NUTS FROM BOLTS, REMOVED MINOR CORR OSION, RE-INSTALLED AND SAFETY NUTS. 2 H 7 4 4F RT A49EU 1996062700221 19960627 00221 EU 1996 6 27 96ZZZX3105 1 19960410 A 2710 CONTROL CABLE BAG BAE146 BAE146300A 1500267 EU AILERON CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 616AW E3145 ATW - AILERON INTERCONNECT CABLES ARE CORRODED AT WING ROOT PULLEYS. REMOVED AND REPLACED BOTH CENTER SECTION AILERON I NTERCONNECT CABLES. REF W/C 2079 FOR FUNCTIONAL TEST OF AILERON CONTROLS. 2 H 7 4 4F RT A49EU 1996062700222 19960627 00222 EU 1996 6 27 96ZZZX3106 1 19960410 A 5320 SILL BAG BAE146 BAE146300A 1500267 EU PASSENGER DOOR CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 616AW E3145 ATW - FORWARD PASSENGER DOOR SILL PLATE CORRODED AND HAS CORNER PIECE BROKEN OFF. REMOVED AND REPLACED FORWARD PASSENGE R DOOR SILL PLATE PER SRM. 2 H 7 4 4F RT A49EU 1996062700223 19960627 00223 EU 1996 6 27 96ZZZX3107 1 19960409 A 5312 BULKHEAD STRIP BAG BAE146 BAE146300A 1500267 EU FRAME 18 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 616AW E3145 ATW - FRAME 18 RT BULKHEAD FLOOR STRIP HAS SURFACE CORROSION. REMOVED SURFACE CORROSION, ALODINED, PRIMED AND PAINTED A LLOWABLE PER SRM. 2 H 7 4 4F RT A49EU 1996062700224 19960627 00224 EU 1996 6 27 96ZZZX3108 1 19960416 A 5320 ANGLE STRIP BAG BAE146 BAE146300A 1500267 EU CABIN FLOOR CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 616AW E3145 ATW - CABIN FLOOR ANGLE STRIP ON LT SIDE OF CABIN BETWEEN FRAMES 19A AND 20 HAS SEVERAL SPOTS OF SURFACE CORROSION - MAR KED WITH BLACK PEN. REMOVED CORROSION, ALODINED, PRIMED AND PAINTED AS REQUIRED ABOVE MENTIONED AREAS. 2 H 7 4 4F RT A49EU 1996062700225 19960627 00225 EU 1996 6 27 96ZZZX3109 1 19960416 A 5320 GUSSET BAG BAE146 BAE146300A 1500267 EU FRAME 20 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 616AW E3145 ATW - TWO GUSSET PLATES ON FRAME 20, LT SIDE, FOR AIRSTAIR RAILS HAVE SPOTS OF SURFACE CORROSION. OUTBOARD GUSSET HAS S POT ON UNDERSIDE TOO. REMOVED ALL CORROSION ON GUSSET PLATES ON FRAME 20. TREATED, PRIMED AND PAINTED. 2 H 7 4 4F RT A49EU 1996062700226 19960627 00226 EU 1996 6 27 96ZZZX3110 1 19960415 A 5320 RIVET BAG BAE146 BAE146300A 1500267 EU SEAT RAIL MISSING A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 616AW E3145 ATW - SEAT RAIL IN CABIN AT FRAME 30, LT OUTBOARD, IS MISSING A RIVET. LOCATED UNDER FLOOR PANEL NR 231NF FORWARD END. (MARKED WITH BLACK PEN). INSTALLED RIVET AT ABOVE MENTIONED LOCATION IAW SRM. 2 H 7 4 4F RT A49EU 1996062700227 19960627 00227 EU 1996 6 27 96ZZZX3111 1 19960415 A 5320 RIVET BAG BAE146 BAE146300A 1500267 EU FLOOR SUPPORT NOT INSTALLED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 616AW E3145 ATW - FLOOR SUPPORT BEAM IN CABIN AT FRAME 24, RT MOST OUTBOARD END, HAS A RIVET THAT HAS NOT BEEN BUCKED. (MARKED WITH BLACK PEN). BUCKED ABOVE MENTIONED RIVET IAW SRM. 2 H 7 4 4F RT A49EU 1996062700228 19960627 00228 EU 1996 6 27 96ZZZX3112 1 19960412 A 5320 JO BOLT BAG BAE146 BAE146300A 1500267 EU STR 12 BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 616AW E3145 ATW - FRAME 29, LEFT FWD FACE AT STR 12, HAS JO BOLT WITH NUT SPINNING. FOUND BOLT HEAD BROKEN. INSTALLED NEW BOLT AND NUT FRAME 29 LEFT FWD FACE, SEALED WITH WITCOBOND 776 PER SRM. 2 H 7 4 4F RT A49EU 1996062700229 19960627 00229 EU 1996 6 27 96ZZZX3113 1 19960412 A 5720 JO BOLTS BAG BAE146 BAE146300A 1500267 EU CENTER TANK LOOSE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 616AW E3145 ATW - DURING DV INSPECTION OF THE CENTER TANK, EVIDENCE OF LOOSE JO BOLTS WERE NOTED. UPON EVALUATION, NO CORROSION NOT ED AND ALL ACCESSIBLE JO BOLTS IN CENTER TANK RIB ON AND LEFT/RIGHT WING TANK RIB 2 WERE TORQUE CHECKED TO 15. DETAILS REPORTED TO AVRO RDO FOR ACCESS. LOOSE JO BOLTS REPORTED AT RIB 2 AND ZERO TO AVRO RDO IS ACCEPTABLE NOW, WITH FUTURE D V INSPECTION AND TIME LIMITED UNTIL REPLACEMENT NO LATER THAN 240. 2 H 7 4 4F RT A49EU 1996062700230 19960627 00230 EU 1996 6 27 96ZZZX3114 1 19960412 A 5712 RIB BAG BAE146 BAE146300A 1500267 EU LT WING LOOSE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 616AW E3145 ATW - LEFT WING, CENTER LIFT SPOILER INBOARD JACK RIBS, HAS LOOSE ATTACH BOLTS (UPPER AFT). SECURED AND SAFTIED BOLTS A T CENTER LIFT SUPPLIER INBOARD JACK-RIB UPPER AFT END. 2 H 7 4 4F RT A49EU 1996062700231 19960627 00231 EU 1996 6 27 96ZZZX3115 1 19960417 A 2710 CONTROL CABLE BAG BAE146 BAE146300A 1500267 EU LT AILERON CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 616AW E3145 ATW - LEFT AILERON INTERCONNECT OUTBOARD CABLE NEEDS TO BE REPLACED DUE TO CORROSION. REMOVED AND REPLACED LEFT AILERON INTERCONNECT OUTBOARD CABLE ASSY IAW 27-11-44. 2 H 7 4 4F RT A49EU 1996062700232 19960627 00232 EU 1996 6 27 96ZZZX3116 1 19960417 A 2710 CONTROL CABLE BAG BAE146 BAE146300A 1500267 EU RT AILERON WORN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 616AW E3145 ATW - RIGHT AILERON INTERCONNECT OUTBOARD CABLE WORN THROUGH TUBING. REMOVED AND REPLACED RIGHT AILERON INTERCONNECT OU TBOARD CABLE ASSY IAW MM 27-11-44. 2 H 7 4 4F RT A49EU 1996062700233 19960627 00233 EU 1996 6 27 96ZZZX3117 1 19960416 A 5320 RIVETS BAG BAE146 BAE146300A 1500267 EU FRAME 26 MISSING A A6WA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 616AW E3145 ATW - FLOOR SUPPORT BEAM AT FRAME NR 26, MOST OUTBOARD LEFT, HAS 2 RIVETS MISSING THAT ATTACH THE ANGLE STRIP TO FRAME U NDER PANEL 231JF. REPLACED 2 EACH RIVETS AT ABOVE MENTIONED LOCATION IAW SRM. 2 H 7 4 4F RT A49EU 1996062700234 19960627 00234 EU 1996 6 27 96ZZZX3118 1 19960411 A 5320 CHANNEL BAG BAE146 BAE146300A 1500267 EU FRAME 15 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 616AW E3145 ATW - UNDER FLOOR STRUCTURE, CHANNEL IS CORRODED THROUGH, LOCATED FORWARD OF FRAME 15 BETWEEN COCKPIT AND FORWARD LAV WA LL ON LEFT SIDE OF AVIONICS ACCESS PANEL. REPLACED UNDER FLOOR CHANNEL BY AVIONICS HATCH, LEFT SIDE, FRAME 12 TO FRAME 15 PER SRM. 2 H 7 4 4F RT A49EU 1996062700235 19960627 00235 EU 1996 6 27 96ZZZX3119 1 19960411 A 5260 RAIL BAG BAE146 BAE146300A 1500267 EU FORWARD AIRSTAIR DIRTY A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 616AW E3145 ATW - FORWARD AIRSTAIR, OUTBOARD RAIL, AND 2 SUPPORT BRACKETS NEED CLEANING, INSP'D AND CORROSION TREATED AS NEEDED. RE MOVED AND REPLACED OUTBOARD RAIL AND CLEANED. INSPECTED SUPPORT BRACKETS AS NEEDED IAW MM. 2 H 7 4 4F RT A49EU 1996062700236 19960627 00236 EU 1996 6 27 96ZZZX3120 1 19960411 A 5321 FLOOR BAG BAE146 BAE146300A 1500267 EU CABIN CORRODED A A6WA K NONE L NO TEST IN INSP/MAINT 1 GL 31 616AW E3145 ATW - FLOOR PLATE OUTBOARD OF FORWARD AIRSTAIR CLOSET HAS SEVERAL PLACES WITH SURFACE CORROSION. REMOVED SURFACE CORROS ION AIRSTAIR CLOSET OUTBOARD SILL AREA, TREATED, PRIMED AND PAINTED. 2 H 7 4 4F RT A49EU 1996062700237 19960627 00237 EU 1996 6 27 96ZZZX3121 1 19960411 A 5320 GUSSET BAG BAE146 BAE146300A 1500267 EU FRAME 15 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 616AW E3145 ATW - FORWARD VEST, FRAME 15 TO FLOOR BEAMS, HAS 3 GUSSET PLATES CORRODED. REMOVED AND REPLACED GUSSET PLATES AS NEEDED IAW SRM. 2 H 7 4 4F RT A49EU 1996062700238 19960627 00238 NM 1996 6 27 BJNA96601 1 19960604 A 3397 WIRE BOEING 737 737214 138446R NM CABIN BROKEN A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 457TM 20156 ROWS 10 AND 15, EMERGENCY EXIT LIGHTS INOPERATIVE. REPAIRED BROKEN WIRES AS REQUIRED. (X) 2 L 7 2 4F A16WE 1996062700239 19960627 00239 EU 1996 6 27 PLGA9606031 1 19960603 A 2613 CONNECTOR SAAB SF340 SF340A 7850100 EU LT TAIL PIPE DIRTY A PLGA A E UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 NE 05 343BE 340A101 JFK - FLT 4960 - ON CLIMB-OUT OF JFK, THE LT TAIL PIPE HOT LIGHT ILLUMINATED. THE CREW SECURED THE ENGINE AND RETURNED TO JFK LANDING WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT AND FOUND MOISTURE IN THE CANNON PLUG (RAIN ING AT THE TIME) TO THE TAIL PIPE TEMPERATURE SENSORS. MAINTENANCE CLEANED THE CANNON PLUG, RESEALED THE CONNECTIONS AT BOTH SENSORS AND RETURNED THE AIRCRAFT TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1996062700240 19960627 00240 CE 1996 6 27 PLGA9606071 1 19960607 A 3230 1143880007 POWER PACK BEECH 1900 1900C 1154161 CE LANDING GEAR DEFECTIVE A PLGA A UNSCHED LANDING O OTHER AP APPROACH 1 NE 05 6929M MX400555A UB27 ISP - FLT 4499 - ON APPROACH TO ISP, NLG DOWN AND LOCKED LIGHT FAILED TO ILLUMINATE. BOTH MAIN GEAR LIGHTS ILLUMINATED AND HYD POWER PACK SHUT OFF WITHOUT TRIPPING CIRCUIT BREAKER. ALL APPROPRIATE CHECK LIST PROCEDURES FAILED TO OBTAIN A GREEN SAFE INDICATION. DUE TO WEATHER CONDITIONS IN ISP, AIRCRAFT DIVERTED TO BDL. AIRCRAFT PERFORMED A FLY-BY WHERE G EAR WAS OBSERVED TO BE EXTENDED. ACFT LANDED IN BDL WITHOUT INCIDENT (ON TOUCH DOWN, DOWN AND LOCKED LIGHT ILLUMINATED) . ACFT INSP AND FERRIED TO ALB WITH GEAR DOWN. ALB MX FND HYD POWER PACK DEFECTIVE. MX REMOVED AND REPLACED POWER PAC K, INSPECTED NOSE GEAR FOR PROPER ADJUST (NO DEFECTS FND), PERFORMED 10 SUCCESSFUL GEAR SWINGS, RTND ACFT TO SERVICE.(X) 2 L 7 2 4T RT A24CE 1996062700241 19960627 00241 EU 1996 6 27 PLGA9606091 1 19960609 A 2421 31342001 AC GENERATOR SAAB SF340 SF340A 7850100 EU LT ENGINE FAILED A PLGA H F DEACTIVATE SYST/CIRCUITS ACTIVATE FIRE EXT. J A WARNING INDICATION FLAME/FIRE LD LANDING 1 NE 05 343BE 1303 340A101 BOS - FLT 4341 - EN ROUTE TO BOS (25 NM SOUTH OF PWN), LT AC GENERATOR FAIL LIGHT ILLUMINATED. ABNORMAL CHECK LIST PROC EDURES FOLLOWED AND AC GENERATOR WAS SELECTED OFF. ON SHORT FINAL INTO BOS, CAPTAIN OBSERVED FLAMES FROM GEN EXHAUST. C REW DECLARED EMERGENCY, LANDED, FIRED BOTH ENG FIRE BOTTLES (ENGINE FIRE WARNING WAS NOT ILLUMINATED) AND EVACUATED ACFT WITHOUT INJURY. MAINTENANCE WAS DISPATCHED TO ACFT AND FOUND THE AC GENERATOR HAD FAILED INTERNALLY. ALL DAMAGE CONTA INED TO THE GEN AND THE COWL EXHAUST SCREEN. MAINTENANCE REMOVED AND REPLACED AC GENERATOR, PROPELLER GEARBOX CARBON SE AL, AND COWL DOOR, RETURNING AIRCRAFT TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1996062700242 19960627 00242 NE 1996 6 27 REXA96018 2 19960528 A 7320 6068T72P09 HMU WOODWARD SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE FAILED A REXA E ENGINE SHUTDOWN X ENGINE FLAMEOUT DE DESCENT 1 SO 25 362PX 91090 340B258 GEE785323 RIGHT ENGINE MADE A VOLUNTARY IN-FLIGHT SHUT DOWN. NO ABNORMAL INDICATIONS OBSERVED PRIOR, DURING, OR AFTER SHUT DOWN. (CRUISE 11,000 MSL, CLEAR WEATHER.) FOUND HMU SHAFT SEIZED. REMOVED AND REPLACED HMU IAW SAAB AMM. RAN RT ENGINE, NO DEFECTS NOTED. (X) 2 L 7 2 4T 4 T RT A52EU E8NE 1996062700243 19960627 00243 EU 1996 6 27 WTAA960112 1 19960530 A 3260 9005EN38 SWITCH BAG JETSTM JETSTM3101 1500215 EU RT MLG LACK OF LUBE A WTAA O OTHER P NO WARNING INDICATION AP APPROACH 1 WP 17 428UE 806 SFO - RT MLG UNSAFE LIGHT DID NOT COME ON DURING GEAR EXTENSION. MAINTENANCE LUBED RT UPLOCK MICROSWITCH. INDICATION N ORMAL DURING GROUND CHECK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A21EU 1996062700244 19960627 00244 SO 1996 6 27 WTAA960113 1 19960530 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A WTAA K NONE L NO TEST IN INSP/MAINT 1 WP 17 280UE 120090 FAT - FLOOR PROXIMITY EMERGENCY LIGHT PATH MARKING SYSTEM INOPERATIVE. DEFERRED BATTERY PACK PER MEL 33-30-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL BY REPLACING AFT EMERGENCY BATTERY PACK. SYSTEM OPERAT IONAL CHECK NORMAL. (X) 2 L 7 2 4T RT A31SO 1996062700245 19960627 00245 SO 1996 6 27 WTAA960116 1 19960602 A 3234 120385894001 SELECTOR EMB 120 EMB120RT SO LANDING GEAR MALFUNCTIONED A WTAA O OTHER N FALSE WARNING CR CRUISE 1 WP 17 284UE 120145 FAT - LT MLG AND NLG GEAR B-LIGHT ILLUMINATES INTERMITTENTLY IN-FLIGHT. MAINTENANCE DEFERRED B-INDICATION SYSTEM PER ME L 32-60-1. AIRCRAFT RETURNED TO SERVICE. SUBSEQUENTLY, CLEARED DEFERRAL BY REPLACMENT OF GEAR HANDLE ASSEMBLY. (X) 2 L 7 2 4T RT A31SO 1996062700246 19960627 00246 EU 1996 6 27 WTAA960117 1 19960602 A 3260 622800200 SWITCH BAG JETSTM JETSTM3101 1500215 EU RT MLG DAMAGED WIRE A WTAA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 WP 17 428UE 806 LAX - RT MLG INTRANSIT LIGHT INOPERATIVE. MAINTENANCE REPAIRED WIRE ON RT LANDING GEAR UPLOCK MICROSWITCH. SYSTEM OPER ATIONAL CHECK NORMAL DURING GEAR RETRACTION CHECK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A21EU 1996062700247 19960627 00247 EU 1996 6 27 WTAA960118 1 19960602 A 3260 622800200 SWITCH BAG JETSTM JETSTM3101 1500215 EU LT MLG OUT OF ADJUST A WTAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 17 428UE 806 LAX - LT MLG INTRANSIT LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. AIRCRAFT RETURNED TO LAX FOR REPAIR. MAINTENA NCE FOUND LT MAIN BRAKE LINE CLAMP HITTING LT MAIN GEAR UPLOCK MICROSWITCH. REPOSITIONED LT MAIN BRAKE LINE CLAMP AND R EADJUSTED MICROSWITCH. SYSTEM OPERATIONAL CHECK NORMAL DURING GEAR RETRACTION CHECK. AIRCRAFT R4ETURNED TO SERVICE. ( X) 2 L 7 2 4T RT A21EU 1996062700248 19960627 00248 EU 1996 6 27 WTAA960120 1 19960603 A 3260 622800200 SWITCH BAG JETSTM JETSTM3101 1500215 EU RT MLG DAMAGED WIRE A WTAA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 WP 17 418UE 780 SEA - RT MLG INTRANSIT LIGHTS INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE ON RT MAIN GEAR UPLOCK MICROSWITCH. SYSTEM OPERATIONAL CHECK NORMAL DURING GEAR RETRACTION CHECK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A21EU 1996062700249 19960627 00249 EU 1996 6 27 WTAA960121 1 19960603 A 3020 8943822 ANTI ICE TUBE BAG JETSTM JETSTM3101 1500215 EU LT ENGINE CRACKED A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 17 429UE 807 IPL - LT ENGINE WOULD NOT PROVIDE MINIMUM TORQUE FOR TAKEOFF. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE REPLACED I NLET ANTI-ICE PLUMBING TUBE ASSY. ENGINE NORMAL DURING GROUND RUN. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A21EU 1996062700250 19960627 00250 EU 1996 6 27 WTAA960122 1 19960604 A 3260 622800200 SWITCH BAG JETSTM JETSTM3101 1500215 EU LT MLG FALSE INDICATION A WTAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 17 331CA 793 FAT - DURING CLIMB-OUT, LT MLG INTRANSIT LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. AIRCRAFT RETURNED TO FAT WIT HOUT INCIDENT. MAINTENANCE REPLACED UPLOCK MICROSWITCH. SYSTEM OPERATIONAL CHECK NORMAL DURING GEAR RETRACTION CHECK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A21EU 1996062700251 19960627 00251 EU 1996 6 27 WTAA960123 1 19960609 A 5610 WINDSHIELD BAG JETSTM JETSTM3101 1500215 EU CENTER COCKPIT BIRD STRIKE A WTAA O OTHER C F.O.D. CR CRUISE 1 WP 17 428UE 806 MOD - BIRD STRIKE REPORTED ON CENTER WINDSHIELD. MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECTION ON WINDOW, CENTER PANE , NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A21EU 1996062700252 19960627 00252 SO 1996 6 27 WTAA960124 1 19960609 A 7331 M8372386R1002N FUEL FILTER IND EMB 120 EMB120RT SO RT ENGINE ILLUMINATED A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 17 250YV 120250 SBA - RT ENGINE FUEL FILTER LIGHT ILLUMINATED ON TAKEOFF. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE REMOVED AND IN SPECTED RIGHT ENGINE HIGH PRESSURE FUEL FILTER. FUEL FILTER LIGHT INDICATED NORMAL DURING ENGINE GROUND RUN. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1996062700253 19960627 00253 WP 1996 6 27 WTAA960125 2 19960609 A 7320 8070429 FUEL CNTRL UNIT BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110U 01514 WP LT ENGINE OUT OF ADJUST A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 17 429UE 807 FAT - LT ENGINE WOULD NOT PROVIDE MINIMUM TORQUE FOR TAKEOFF. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE ADJUSTED M AXIMUM FUEL FLOW. ENGINE NORMAL DURING GROUND RUN. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T 4 T RT A21EU E4WE 1996062700254 19960627 00254 EU 1996 6 27 WTAA960126 1 19960609 A 5101 STRUCTURE BAG JETSTM JETSTM3101 1500215 EU AIR FRAME BIRD STRIKE A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK C F.O.D. TO TAKEOFF 1 WP 17 430UE 784 SNA - CREW REPORTED BIRD STRKE ON TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECTION. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A21EU 1996062700255 19960627 00255 NM 1996 6 27 9613722287 1 19960622 A 3260 656021132 LDG GEAR MODULE BOEING 727 727251 138408H NM LT MLG MALFUNCTIONED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 2287U 21375 DURING GEAR EXTENSION, THE LEFT GEAR DID NOT INDICATE DOWN AND LOCKED. CYCLED GEAR HANDLE, ON SECOND GEAR EXTENSION IND ICATION WAS NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR ELECTRONIC MODULE AND CHECKED LEFT GEAR SE NSOR GAP. PERFORMED LANDING GEAR INDICATION CHECK PER MAINTENANCE MANUAL, CHECKED OK. 2 L 7 3 4F A3WE 1996062700256 19960627 00256 NM 1996 6 27 9613732204 1 19960624 A 2824 CROSSFEED VALVE BOEING 727 727251 138408H NM NR 1 MALFUNCTIONED A NWAA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CR CRUISE 1 GL 01 204US 22544 DURING CRUISE, THE NR 1 FUEL CROSSFEED VALVE WOULD NOT OPEN. AIRCRAFT DIVERTED TO MEM, FUEL WAS DUMPED AND AIRCRAFT LAN DED WITHOUT INCIDENT. LOCKED OPEN NR 1 FUEL CROSSFEED VALVE AND PLACED ON MEL. 2 L 7 3 4F A3WE 1996062700257 19960627 00257 WP 1996 6 27 9613741160 1 19960624 A 3260 DNLOCK SWITCH DOUG DC10 DC1040 3023508 WP LT MLG FAILED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 160US 46769 DURING CLIMB, THE LEFT MAIN GEAR UNSAFE LIGHT REMAINED ON WITH THE GEAR HANDLE UP. RECYCLED GEAR AND VERIFIED LEFT MAIN GEAR DOOR WAS UP AND LOCKED. FLIGHT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE DOWNLOCK P ROXIMITY SWITCH. 2 L 7 3 4F A22WE 1996062700258 19960627 00258 NM 1996 6 27 9613756626 1 19960621 A 3350 BATTERY PACK BOEING 747 747251B 1384892 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 626US 21708 DURING LINE CHECK, FOUND EMERGENCY LIGHTS BY DOORS 1L, 4L, 5L AND 5R INOPERATIVE. REPLACED TWO BATTERY PACKS AND TWO LI GHT ASSEMBLIES, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996062700259 19960627 00259 WP 1996 6 27 9613769304 1 19960623 A 3350 POWER PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 931MC 48057 DURING LINE CHECK, FOUND EMERGENCY EXIT SIGN AT ROW 20 RIGHT INOPERATIVE. REPLACED POWER PACK AND LIGHT ASSEMBLY, OPERA TIONAL CHECK OK. 2 L 7 2 4F A6WE 1996062700260 19960627 00260 WP 1996 6 27 9613779858 1 19960621 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 767MC 47724 DURING LINE CHECK, FOUND OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996062700261 19960627 00261 WP 1996 6 27 9613789955 1 19960619 A 3350 60030451 BATTERY PACK DOUG DC9 DC931 3022065 WP COCKPIT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 922RW 47182 DURING PREFLIGHT CHECK, FOUND COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996062700262 19960627 00262 WP 1996 6 27 9613799921 1 19960618 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 943N 47647 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHT BATTERY PACKS WITH LOW VOLTAGE. REPLACED BATTERY PACK, OPERAT IONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996062700263 19960627 00263 WP 1996 6 27 9613809905 1 19960618 A 3350 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 955N 47160 DURING LINE MAINTENANCE INSPECTION, FOUND AFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996062700264 19960627 00264 WP 1996 6 27 9613819979 1 19960616 A 3040 TERMINAL BLOCK DOUG DC9 DC931 3022065 WP LEFT WINDSHIELD FAILED A NWAA O OTHER A FLAME/FIRE LD LANDING 1 GL 01 9343 47439 UPPER LEFT CORNER OF LEFT WINDSHIELD HAD SPARKS AND FLAMES ON LANDING. WINDSHIELD HEAT WAS SHUT OFF AND SPARKS/FLAMES C EASED. MAINTENANCE FOUND R920 TERMINAL BLOCK TO WINDSHIELD HEAT HAD FAILED. REPLACED TERMINAL BLOCK R920, CAPTAIN'S WI NDSHIELD AND HEAT CONTROLLER. 2 L 7 2 4F A6WE 1996062700265 19960627 00265 WP 1996 6 27 9613829950 1 19960618 A 3260 SWITCH DOUG DC9 DC932 3022066 WP RT MLG DOWNLOCK MALFUNCTIONED A NWAA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 01 9346 47376 RIGHT MAIN GEAR GREEN LIGHT DID NOT ILLUMINATE ON APPROACH. RECYCLED GEAR AND NORMAL INDICATIONS WERE ACHIEVED. AIRCRA FT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT MAIN GEAR DOWNLOCK SWITCH. CYCLED GEAR SEVERAL TIMES, OPERATION AL CHECK NORMAL. 2 L 7 2 4F A6WE 1996062700266 19960627 00266 WP 1996 6 27 9613839905 1 19960622 A 3230 RETRACT MECH DOUG DC9 DC931 3022065 WP LANDING GEAR MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 955N 47160 LANDING GEAR HANDLE WOULD NOT RAISE AFTER TAKEOFF. AIRCRAFT FAILED TO SHIFT FROM GROUND MODE TO FLIGHT MODE. FLIGHT RE TURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED GROUND SHIFT MECHANISM AND ACTUATED LINKAGE SEVERAL TI MES. DISCREPANCY COULD NOT BE DUPLICATED, SYSTEM CHECKED NORMAL. 2 L 7 2 4F A6WE 1996062700267 19960627 00267 WP 1996 6 27 9613849864 1 19960624 A 3610 CROSSFEED VALVE DOUG DC9 DC951 3022051 WP TAIL COMPT LEAKING A NWAA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 GL 01 773NC 47775 ON TAKEOFF JUST AFTER ROTATION, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. PERFORMED COM PROCEDURE BUT LIGHT REMAINED ON. FLIGHT RETURNED TO MIA AND LANDED WITHOUT INCIDENT. FOUND LEFT PNEUMATIC CROSSFEED VALVE LEAKING. REPLAC ED CROSSFEED VALVE, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996062700268 19960627 00268 WP 1996 6 27 9613851144 1 19960620 A 3350 POWER SUPPLY DOUG DC10 DC1040 3023508 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 144JC 46753 DURING LINE INSPECTION, FOUND THE OVERWING EMERGENCY LIGHT POWER SUPPLY FAULTED. MAINTENANCE REPLACED THE OVERWING EMER GENCY POWER SUPPLY AND BATTERY. 2 L 7 3 4F A22WE 1996062700269 19960627 00269 WP 1996 6 27 9613869906 1 19960624 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 956N 47252 DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT AFT OVERWING EMERGENCY LIGHTS VERY DIM. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996062700270 19960627 00270 WP 1996 6 27 9613879955 1 19960624 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 922RW 47182 DURING PREFLIGHT CHECK, FOUND FORWARD CABIN AND GALLEY DOOR EXIT FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. REPAIRED WIRING TO EMERGENCY POWER SUPPLY CONNECTOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996062700271 19960627 00271 WP 1996 6 27 9613889936 1 19960623 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 1799U 47370 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS JUST AFT OF FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996062700272 19960627 00272 WP 1996 6 27 9613899967 1 19960623 A 3350 FUSE DOUG DC9 DC931 3022065 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9331 47263 DURING LINE MAINTENANCE, FOUND EMERGENCY EXIT SIGN AT MAIN CABIN DOOR INOPERATIVE. REPLACED FUSE, OPERATIONAL CHECK NOR MAL. 2 L 7 2 4F A6WE 1996062700273 19960627 00273 WP 1996 6 27 9613909930 1 19960621 A 3350 60030451 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 89S 47042 DURING PERIODIC CHECK, FOUND AFT OVERWING EMERGENCY EXIT LIGHT BATTERY PACK WITH NO OUTPUT. REPLACED BATTERY PACK, OPER ATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996062700274 19960627 00274 WP 1996 6 27 9613919979 1 19960615 A 3350 FUSE DOUG DC9 DC931 3022065 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9343 47439 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD SERVICE DOOR AND FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. REPLACED P OWER SUPPLY FUSE, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996062700275 19960627 00275 1996 6 27 9613929919 4 19960624 A 3418 STALL WARN COMP DOUG DC9 DC932 3022066 WP LEFT MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 941N 47450 STALL WARNING SYSTEM ACTIVATED ON ROTATION. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED L EFT STALL WARNING COMPUTER AND RIGHT AOA TRANSDUCER, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996062700276 19960627 00276 NM 1996 6 27 96FDEA00842 1 19960425 A 5330 6518386 SKIN BOEING 727 72725 1384006 NM BS 1148-1166 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 NR0435 AND 008, SKIN INTERNAL BONDED DOUBLER IS DELAMINATED AT BS 1148 TO 1166 BETWEEN STR 23 TO 25R. *S/D* REPAIRED P ER FEDEX EA 7-5330-28332. 2 L 7 3 4F A3WE 1996062700277 19960627 00277 NM 1996 6 27 96FDEA01167 1 19960625 A 5311 651631470 FRAME BOEING 727 72725 1384006 NM BS 312 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 NR 0543 AND 048. CORROSION ON FRAME AND FAIL-SAFE, BS 312, LBL 49, WL 180. ******S/D***** (MFG PART NUMBER 65-163 14-71.) REMOVED AND REPLACED FRAME AND FAIL-SAFE, BS 312, LBL 49, WL 180, IAW FEDEX SRM 53-10-8, SRM 53-10-1. 2 L 7 3 4F A3WE 1996062700278 19960627 00278 NM 1996 6 27 96FDEA01168 1 19960625 A 5330 65C25337 SKIN BOEING 727 72725 1384006 NM BS 693 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 NR 0512 AND 049. SKIN CHAFED AT LAP, STR 19L, BS 693. ****S/D**** REPAIRED SKIN CHAFED AT LAP STR 19L, BS 693 - BS 7 30, IAW FEDEX EA 7-5330-29190. 2 L 7 3 4F A3WE 1996062700279 19960627 00279 NM 1996 6 27 96FDEA01169 1 19960625 A 5230 6518625114 ANGLE BOEING 727 72722 1384002 NM AFT CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 NR 0405 AND NR 038, AFT CARGO DOOR HAS CRACK INDICATION IN RADIUS OF NR 4 (FROM TOP) OUTBOARD L-ANGLE, 20 INCHES AFT OF FWD EDGE. *****S/D**** COMING. 2 L 7 3 4F A3WE 1996062700280 19960627 00280 NM 1996 6 27 96FDEA01170 1 19960625 A 5754 65162261 LUG BOEING 727 72722 1384002 NM NR 2 LE FLAP CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 MR 0681 AND NR 039. NR 2 K-FLAP HAS CORROSION AROUND OUTBOARD LUG UPPER BOLT HOLE. ****S/D*** REMOVED CORROSION FR OM NR 2 K-FLAP, OUTBOARD LUG UPPER HOLE AND REPAIRED PER FEDEX DRAWING SR 27-57-010, REV B. 2 L 7 3 4F A3WE 1996062700281 19960627 00281 WP 1996 6 27 ABXA9600513 1 19960621 A 5610 5613217508 WINDOW ASSY DOUG DC9 DC931 3022065 WP RT COCKPIT LACK OF LUBE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 FIRST OFFICERS CLEAR VIEW WINDOW HARD TO OPEN AND OCCASIONALLY BINDS. LUBED FIRST OFFICERS CLEAR VIEW WINDOW ASSEMBLY. 2 L 7 2 4F A6WE 1996062700282 19960627 00282 WP 1996 6 27 ABXA9600514 1 19960621 A 2170 21D101 COALESCER BAGS DOUG DC9 DC931 3022065 WP LT/RT DIRTY A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 947AX 47004 UNUSUAL SMELL FROM AIR CONDITIONING VENTS. INSPECTED RAM AIR AND HEAT EXCHANGER DUCTS, NOTHING FOUND. REPLACED THE WAT ER SEPARATOR COALESCER BAGS. 2 L 7 2 4F A6WE 1996062700283 19960627 00283 WP 1996 6 27 ABXA9600515 1 19960622 A 3350 60030431 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 946AX 47003 EMERGENCY LIGHTS STAY ON WITH POWER OFF. REPLACED EMERGENCY LIGHTS POWER SUPPLY. 2 L 7 2 4F A6WE 1996062700284 19960627 00284 WP 1996 6 27 ABXA9600516 1 19960624 A 3350 14597101 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 907AX 47203 DURING PREDEPARTURE CHECK, FOUND EMERGENCY LIGHTS DIM. REPLACED EMERGENCY LIGHT BATTERIES. 2 L 7 2 4F A6WE 1996062700285 19960627 00285 WP 1996 6 27 CALA9600863 1 19960619 A 5314 KEEL PLANK DOUG DC10 DC1010 3022110 WP BS 2007 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68043 46902 INSPECTION FOUND AFT BODY KEEL PLANK CORRODED AT STA 2007 BETWEEN LONGERON 41L AND 43L. THE AREA WAS REPAIRED IAW ECRA 5330-02411. 2 L 7 3 4F A22WE 1996062700286 19960627 00286 WP 1996 6 27 CALA9600864 1 19960619 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1781-1821 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68043 46902 INSPECTION FOUND DENTS AND DEFORMATION IN SKIN AFT OF THE CENTER CARGO DOOR BETWEEN STA 1781 AND 1821, LONGERONS 38R AND 42R. THE AREA WAS REPAIRED IAW ECRA 5330-02412. 2 L 7 3 4F A22WE 1996062700287 19960627 00287 WP 1996 6 27 CALA9600865 1 19960620 A 5312 BULKHEAD T-CAP DOUG DC10 DC1010 3022110 WP BS 1156 GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68043 46902 INSPECTION FOUND TWO GOUGES AT TWO BOLT HOLES OF STA 1156 BULKHEAD T-CAP. THE AREA WAS REPAIRED IAW ECRA 5340-01272. 2 L 7 3 4F A22WE 1996062700288 19960627 00288 WP 1996 6 27 CALA9600866 1 19960619 A 5315 FLOORBEAM DOUG DC10 DC1010 3022110 WP BS 1741 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68043 46902 INSPECTION FOUND CORROSION IN THE UPPER HORIZONTAL FLANGE OF THE LOWER FLOORBEAM AT FUSELAGE STA Y= 1741 BETWEEN X= 40 A ND 50. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-03294. 2 L 7 3 4F A22WE 1996062700289 19960627 00289 WP 1996 6 27 CALA9600867 1 19960620 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 1701-1781 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68043 46902 INSPECTION FOUND CORROSION IN FRAME CAPS AT FUSELAGE STATIONS 1721, 1741, 1761, 1701 AND 1781. REPAIRS WERE PERFORMED I AW ECRA 5310-03295. 2 L 7 3 4F A22WE 1996062700290 19960627 00290 WP 1996 6 27 CALA9600868 1 19960620 A 5320 DOOR SILL DOUG DC10 DC1010 3022110 WP BS 1835 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68043 46902 INSPECTION FOUND CORROSION IN THE AFT CARGO DOOR SILL AT STA 1835 AND THE SILL ANGLE SUPPORT AT STA 1840 WAS CORRODED. R EPAIR WAS PERFORMED IAW ECRA 5310-03296. 2 L 7 3 4F A22WE 1996062700291 19960627 00291 WP 1996 6 27 CALA9600869 1 19960619 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 1641-1701 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68043 46902 INSPECTION FOUND A 7 INCH CRACK IN LONGERON 44R BETWEEN STA 1641 AND 1701. THE LONGERON WAS REPAIRED IAW ECRA 5310-0329 2. 2 L 7 3 4F A22WE 1996062700292 19960627 00292 WP 1996 6 27 CALA9600870 1 19960618 A 5320 FITTING DOUG DC10 DC1010 3022110 WP BS 1551 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68043 46902 INSPECTION FOUND CORROSION IN LONGERON 50L SPLICE FITTING AT STA 1551. REPAIR WAS PERFORMED IAW ECRA 5310-03293. 2 L 7 3 4F A22WE 1996062700293 19960627 00293 NM 1996 6 27 DL72S961450 1 19960617 A 5320 ANGLE BOEING 727 727232 1384082 NM UNDER STAIR ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 494DA 21074 A 2 INCH AND 1.5 INCH CRACK IN TORQUE BOX WEB AT UPPER CHORD RT END. REPAIRED PER M/M 53-11-0. 2 L 7 3 4F A3WE 1996062700294 19960627 00294 NM 1996 6 27 DL72S961451 1 19960617 A 5320 WEB BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 494DA 21074 A .5 INCH CRACK IN TORQUE BOX WEB EXTENDING FROM RT FWD LIGHTENING HOLE. REPAIRED PER M/M 53-11-0. 2 L 7 3 4F A3WE 1996062700295 19960627 00295 NM 1996 6 27 DL72W961459 1 19960602 A 5330 SKIN BOEING 727 727247 138408F NM BELOW LAV PANEL CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2811W 20649 THE SKIN JUST BELOW FWD LAV SERVICE PANEL WAS FOUND CRACKED. THE SKIN IS MADE FROM 0.040 2024-T3 AND THE_FINAL CUTOUT D IMENSIONS WERE 1.375 FWD/AFT AND 2.5 ABOVE/BELOW. THIS ERA GIVES INSTRUCTIONS TO REPAIR THE DAMAGE WITH A 0.050 2024-T3 DOUBLER. 2 L 7 3 4F A3WE 1996062700296 19960627 00296 NM 1996 6 27 DL72W961462 1 19960518 A 5330 6554590 SKIN BOEING 727 727247 138408F NM BS 720 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2809W 20581 SKIN CORROSION AT FS 720F AT STR 27R. REMOVED A 1.75 INCH BY 5 INCH CUTOUT JUST FWD OF AN EXISTING REPAIR AT STA 730. E RA WILL INCORPORATE BOTH REPAIRS INTO ONE REPAIR. 2 L 7 3 4F A3WE 1996062700297 19960627 00297 NM 1996 6 27 DL73E961481 1 19960619 A 3350 337701962 BATTERY PACK BOEING 737 737247 138448D NM REAR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 381DL 23608 ON MAINTS CHECK FOUND REAR MOST SECTION OF EMERGENCY TRACK LIGHTING INOP. REPLACED BATTERY SUPPLY, OPS CK GOOD. 2 L 7 2 4F A16WE 1996062700298 19960627 00298 NM 1996 6 27 DL73E961483 1 19960615 A 3350 BATTERY PACK BOEING 737 737247 138448D NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 380DL 23607 RT OVERWING EMERGENCY LIGHT IS INOP. REPLACED BATTERY PACK AND BATTERY. 2 L 7 2 4F A16WE 1996062700299 19960627 00299 NM 1996 6 27 DL73S961461 1 19960603 A 5312 BULKHEAD WEB BOEING 737 737232 1384475 NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 329DL 23101 DURING SPECIAL INSPECTION 3-69482-12, CRACKS WERE DISCOVERED ON THE FWD FACE OF THE FS 178 BULKHEAD WEB. THE FIRST CRAC K IS LOCATED NEAR THE LBL 5.7 VERTICAL STRAP AT APPROX WL 203. THE SECOND IS NEAR THE RBL 5.7 VERTICAL STRAP AT APPROX WL 203. THE 3RD IS LOCATED NEAR BL 0 AT APPROX WL 195 AND THE FOURTH IS LOCATED NEAR RBL 14 AT WBL 184.5. CUTOUTS RESU LTED IN 4 CUTOUTS MEASURING 1 BY 2.5, 1 BY 4.5, 2.5 BY 2.5 AN 1 DIA HOLE. THE ERA WILL REPAIR THE WEB WITH 2 REPAIR DOU BLERS, ONE INTERNAL AND ONE EXTERNAL BAC15 05-100361 7075-T6 EXTRUSION. 2 L 7 2 4F RT A16WE 1996062700300 19960627 00300 NM 1996 6 27 DL73S961474 1 19960611 A 5312 BULKHEAD WEB BOEING 737 737232 1384475 NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 302DL 23047 THREE CRACKS FOUND ON THE FWD FACE OF THE STA 178 BLKHD WEB. THE FIRST CRACK WAS LOCATED NEAR LBL 5.7 VERTICAL STRAP AT APPROX WL 195, THE SECOND CRACK WAS LOCATED NEAR RBL 5.7 VERTICAL STRAP AT APPROX WL 200 AND THE THIRD CRACK WAS LOCATE D NEAR BL 0 AT APPROX WL 190. THE WEB WAS REPAIRED WITH A DOUBLER IN ACCORDANCE WITH FAA/DER FORM 3110-3 BY SO-831, DTD 06-11-96. 2 L 7 2 4F RT A16WE 1996062700301 19960627 00301 NM 1996 6 27 DL76S961440 1 19960616 A 3397 WIRE BOEING 767 767332 1382001 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 129DL 24079 EMERGENCY FLOOR LIGHT AT SEAT 13 F/G TO MID LAV INOP. FOUND DAMAGE WIRE, RESPLICED WIRES AND CKS OK. 2 L 7 2 4F RT A1NM 1996062700302 19960627 00302 NM 1996 6 27 DL76S961493 1 19960619 A 3350 POWER SUPPLY BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 139DL 25984 A SECTION OF EMERGENCY LIGHTS FAILED TO ILLUMINATE DURING TEST. REPLACED POWER SUPPLY M738, OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 1996062700303 19960627 00303 NM 1996 6 27 DL76S961494 1 19960619 A 2421 IDG BOEING 767 767332 1382001 NM NR 2 ENGINE OVERHEATED A DALA A F UNSCHED LANDING ACTIVATE FIRE EXT. A J FLAME/FIRE WARNING INDICATION CL CLIMB 1 SO 27 136DL 23146 ON CLIMBOUT, HAD RT ENG STARTER EICAS MSG. ACCOMPLISHED STARTER CUTOUT PROCEDURE WITH NO AVAIL. WITHIN A COUPLE OF MIN UTES HAD RT ENG FIRE ANNUNICATED. ENGINE SHUTDOWN FIRE BOTTLES, BOTH USED. RT ENG IDG OVERHEATED CAUSING ENGINE FIRE. 2 L 7 2 4F RT A1NM 1996062700304 19960627 00304 NM 1996 6 27 DLM90961500 1 19960621 A 3222 MS288892 SCHRADER VALVE DOUG MD90 MD9030 3023690 NM NLG FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 904DA 53384 ON GEAR RETRACTION, NOSE GEAR UNSAFE LIGHT REMAINED ON WITH HANDLE UP. NLG INDICATOR WAS FLUSH, RECYCLED IN ACCORDANCE WITH POM BUT LIGHT STAYED ON WHEN ANOTHER RETRACTION WAS ATTEMPTED. REPLACED NOSE STRUT SCHRADER VALVE AND O-RING. SER VICED STRUT IN ACCORDANCE WITH MAINT MANUAL. PERFORMED NOSE GEAR RETRACT CHECK, OPERATION NORMAL. 2 L 7 2 4F RT A6WE 1996062700305 19960627 00305 NM 1996 6 27 P5CA9600251 1 19960620 A 3520 80080208 FLOW CONTL UNIT BOEING 747 747123 1384873 NM PAX OXY SYSTEM LEAKING A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 DURING MAINTENANCE, FOUND PASSENGER O2 LOW. FOUND ELECTRO-PNEUMATIC FLOW CONTROL UNIT LEAKING INTERNALLY. REPLACED SAM E IAW MM 35-21-00. ALSO, REPLACED AFT PASSENGER O2 BOTTLE, (P/N 801307-00), (S/N 962110) NO LEAKS NOTED. 2 L 7 4 4F A20WE 1996062700306 19960627 00306 NM 1996 6 27 VNAA9606008 1 19960617 A 3260 OL6839 BULB DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT MLG FAILED A VNAA L ABORTED APPROACH P NO WARNING INDICATION LD LANDING 1 GL 07 441JS 3059 ON APPROACH AFTER SELECTING GEAR DOWN, THE CREW REPORTED LEFT MAIN LANDING GEAR DID NOT INDICATE DOWN AND LOCKED. CREW SHOT A MISSED APPROACH WHILE THE FIRST OFFICER REPLACED THE BULB IN THE LANDING GEAR POSITION INDICATOR. AFTER BULB REP LACEMENT LEFT MIAN GEAR INDICATED DOWN AND LOCKED. ATC HAD ALREADY NOTIFIED THE AIRPORT AUTHORITIES AND EMERGENCY EQUIP MENT WAS CALLED OUT. THE AIRCRAFT LANDED WITHOUT INCIDENT. NO FUTHER ACTION WAS REQUIRED, AIRCRAFT REMAINED IN SERVIC E. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996062700307 19960627 00307 NE 1996 6 27 VNAA9606009 3 19960619 A 6110 E62127 PROPELLER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE LIGHTNING STRIKE A VNAA K NONE C F.O.D. CR CRUISE 1 GL 07 328JS 3030 HL206 EN ROUTE, FLYING AT FL160 THROUGH LIGHT RAIN, CREW REPORTED HEARING A LOUD BANG FOLLOWED IMMEDIATELY BY A BRIGHT FLASH O F LIGHT. CREW CONTINUED ON WITH THE FLIGHT AND LANDED IN PIT WITHOUT FURTHER INCIDENT. PIT MX CONDUCTED A LIGHTNING ST RIKE INSPECTION IAW MM 05-51-12. DURING THE INSPECTION MX DISCOVERED ONE BLADE ON THE LEFT PROPELLER HAD SUFFERED LIGH TNING STRIKE DAMAGE. MX REPLACED THE LEFT PROPELLER ASSEMBLY IAW MM 61-10-00, GROUND RUNS CHECKED GOOD. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996062700309 19960627 00309 NM 1996 6 27 96ZZZX3123 1 19960127 A 2421 IDG BOEING 767 767259 1385136 NM LT ENGINE FAILED W ANCF A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC NR NOT REPORTED 1 SO 23 986AN 24835 CTG/MAD - FLT 010 - EICAS MSG 01=L GEN DRIVE DISPLAYED. GEN DRIVE LIGHT ILLUMINATED, GEN DRIVE DISCONNECTED. CHANGED I DG. CYCLES, 4,257. HOURS, 22,648. 2 L 7 2 4F RT A1NM 1996062700310 19960627 00310 NE 1996 6 27 96ZZZX3124 2 19960312 A 7200 ENGINE BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE NR 2 FAILED A A6WA F E ACTIVATE FIRE EXT. ENGINE SHUTDOWN Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 GL 31 606AW 722 E2033 LF05220 DEN - FLT 604 - NR 2 ENGINE FAILED IN-FLIGHT, NR 1 BOTTLE BLOWN. ENGINE CHECK LIST C/W. REMOVED AND REPLACED NR 2 ENGI NE IAW MM, PAGE 28412/3 FOR REMOVAL AND REPLACMEENT OF BOTTLE. S/N OFF, LF-05220. S/N ON LF-05076. 2 H 7 4 4F 4 F RT A49EU E6NE 1996062700312 19960627 00312 NE 1996 6 27 96ZZZX3126 2 19960407 A 7260 501113775006 MOUNTING PAD BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE NR 4 GEARBOX SEPARATED A A6WA K NONE K FLUID LOSS IN INSP/MAINT 1 GL 31 606AW 18211 201 TA761 E2033 MKE - FLT 548 - NR 4 ENGINE OIL LEAK. FOUND STARTER MOUNTING PAD SEPARATING FROM ACCESSORY GEARBOX. THREE-ENGINE FERRY TO ATW FOR GEARBOX CHANGE. REMOVED AND REPLACED STARTER MOTOR. 2 H 7 4 4F 4 F RT A49EU E6NE 1996062700313 19960627 00313 NE 1996 6 27 96ZZZX3127 2 19960526 A 7200 ENGINE BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE NR 1 & 2 MALFUNCTIONED A A6WA E A ENGINE SHUTDOWN UNSCHED LANDING J R WARNING INDICATION PARTIAL RPM/PWR LOSS CR CRUISE 1 GL 31 608AW E2049 DSM - FLT 558 - IN ICE ABOVE 26,000 FEET, ALL 4 ENGINES ROLLED BACK TO 40-45 PERCENT. CREW SHUT DOWN NR 1 AND NR 2 DUE TO RISING TGT (APPROXIMATELY 900 DEGREES CELSIUS). NR 2 WAS RE-STARTED. NR 2, NR 3, AND NR 4 RECOVERED. LANDED WITHOU T INCIDENT DSM. MAINTENANCE TO CHARTER THE A/C IN AM. 2 H 7 4 4F 4 F RT A49EU E6NE 1996062700314 19960627 00314 NM 1996 6 27 96ZZZX3128 1 19960326 A 7920 900P3650106103 HOSE DOUG MD900 MD900 3027375 NM OIL SYSTEM WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 458 90000012 HOSE WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1996062700319 19960627 00319 NM 1996 6 27 96ZZZX3133 1 19960108 A 7332 369A840215 SWITCH DOUG MD900 MD900 3027375 NM RT IPS BYPASS INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 298 90000012 PCE206017 RIGHT IPS BYPASS PRESSURE SWITCH INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1996062700322 19960627 00322 NM 1996 6 27 96ZZZX3136 1 19960330 A 6320 900D3409034101 TRANSDUCER DOUG MD900 MD900 3027375 NM M/R GEARBOX DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 62 48156148 90000012 TRANSDUCER UNIT CAUSES PRESSURE GAUGE TO FLUCTUATE 4 PERCENT TO 8 PERCENT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1996062700323 19960627 00323 1996 6 27 96ZZZX3137 4 19960104 A 3160 900A3720002105 DISPLAY DOUG MD900 MD900 3027375 NM INST PANEL INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 311 008251007 90000012 INSTRUMENT DISPLAY UNIT INOPERATIVE. DISPLAY WILL NOT ILLUMINATE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1996062700324 19960627 00324 NM 1996 6 27 96ZZZX3138 1 19960321 A 6720 CEKP3AR112 BEARING DOUG MD900 MD900 3027375 NM T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 445 90000012 THRUST BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1996062700325 19960627 00325 NM 1996 6 27 96ZZZX3139 1 19960321 A 6720 CEKP3AR112 BEARING DOUG MD900 MD900 3027375 NM T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 445 90000012 THRUST BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1996062700326 19960627 00326 NM 1996 6 27 96ZZZX3140 1 19960501 A 6720 CEKP3AR112 BEARING DOUG MD900 MD900 3027375 NM T/R FLAT SPOTS A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 100 90000012 THRUST BEARING HAS FLAT SPOTS. REPLACED WITH 6 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1996062700327 19960627 00327 NM 1996 6 27 96ZZZX3141 1 19960108 A 6210 900R115000109 BLADE DOUG MD900 MD900 3027375 NM M/R DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 298 0111 90000012 M/R BLADE LOOSING PAINT. JOINT FILLER ERODING. ABRASION STRIP DEBONDING AT JOINTS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1996062700328 19960627 00328 NM 1996 6 27 96ZZZX3142 1 19960321 A 7931 900P3650009101 SENSOR DOUG MD900 MD900 3027375 NM ENGINE OIL FLUCTUATES A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 197 53581143 90000012 PRESSURE SENSOR CAUSES PRESSURE GAUGE TO FLUCTUATE 10 PERCENT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1996062700330 19960627 00330 NM 1996 6 27 96ZZZX3144 1 19960108 A 6210 900R115000109 BLADE DOUG MD900 MD900 3027375 NM M/R DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 298 0114 90000012 M/R BLADE LOOSING PAINT. JOINT FILLER ERODING. ABRASION STRIP DEBONDING AT JOINTS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1996062700331 19960627 00331 NM 1996 6 27 96ZZZX3145 1 19960108 A 6210 900R115000109 BLADE DOUG MD900 MD900 3027375 NM M/R DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 298 0113 90000012 M/R BLADE LOOSING PAINT. JOINT FILLER ERODING. ABRASION STRIP DEBONDING AT JOINTS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1996062700332 19960627 00332 NM 1996 6 27 96ZZZX3146 1 19960108 A 6210 900R115000109 BLADE DOUG MD900 MD900 3027375 NM M/R DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 298 0106 90000012 M/R BLADE LOOSING PAINT. JOINT FILLER ERODING. ABRASION STRIP DEBONDING AT JOINTS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1996062700333 19960627 00333 NM 1996 6 27 96ZZZX3147 1 19960108 A 6210 900R115000109 BLADE DOUG MD900 MD900 3027375 NM M/R DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 298 0105 90000012 M/R BLADE LOOSING PAINT. JOINT FILLER ERODING. ABRASION STRIP DEBONDING AT JOINTS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1996062700335 19960627 00335 NM 1996 6 27 96ZZZX3149 1 19960321 A 6200 900R1103001111 FLEX BEAM DOUG MD900 MD900 3027375 NM M/R DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 445 0088 90000012 FLEX BEAM BUMPER ASSY WRAPPING EXCESSIVELY SLIPPED IN THE AREA OF THE OUTBOARD APEX. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1996062700336 19960627 00336 NM 1996 6 27 96ZZZX3150 1 19960321 A 6200 900R1103001111 FLEX BAM DOUG MD900 MD900 3027375 NM M/R DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 445 0109 90000012 FLEX BEAM BUMPER ASSY WRAPPING EXCESSIVELY SLIPPED IN THE AREA OF THE OUTBOARD APEX. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1996062700337 19960627 00337 NM 1996 6 27 96ZZZX3151 1 19960321 A 6200 900R1103001111 FLEX BEAM DOUG MD900 MD900 3027375 NM M/R DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 445 0087 90000012 FLEX BEAM BUMPER ASSY WRAPPING EXCESSIVELY SLIPPED IN THE AREA OF THE OUTBOARD APEX. REPLACED WIH NEW UNIT, CORRECTED P ROBLEM. 1 G 7 2 3U NC H19NM 1996062700338 19960627 00338 NM 1996 6 27 96ZZZX3152 1 19960321 A 6200 900R1103001111 FLEX BEAM DOUG MD900 MD900 3027375 NM M/R DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 445 0111 90000012 FLEX BEAM BUMPER ASSY WRAPPING EXCESSIVELY SLIPPED IN THE AREA OF THE OUTBOARD APEX. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1996062700339 19960627 00339 NM 1996 6 27 96ZZZX3153 1 19960321 A 6200 900R1103001111 FLEX BEAM DOUG MD900 MD900 3027375 NM M/R DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 445 0110 90000012 FLEX BEAM BUMPER ASSY WRAPPING EXCESSIVELY SLIPPED IN THE AREA OF THE OUTBOARD APEX. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1996062700340 19960627 00340 NM 1996 6 27 96ZZZX3154 1 19960321 A 7931 900P3650009101 SENSOR DOUG MD900 MD900 3027375 NM ENGINE OIL DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 247 53581152 90000012 PRESSURE SENSOR CAUSES PRESSURE GAUGE TO FLUCTUATE 10 PERCENT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1996062700341 19960627 00341 NM 1996 6 27 96ZZZX3155 1 19960301 A 6320 900D3409034101 TRANSDUCER DOUG MD900 MD900 3027375 NM GB OIL DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 402 4439657 90000012 PRESSURE TRANSDUCER CAUSES PRESSURE GAUGE TO FLUCTUATE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1996062700348 19960627 00348 1996 6 27 96ZZZX3162 4 19960508 A 2312 064105430 TRANSCEIVER KY196A BELL 206 206L4 1182110 SW INSTRUMENT PANEL BURNED SMELL A ALGA O OTHER B SMOKE/FUMES/ODORS/SPARKS HO HOVERING 1 SW 03 170AL 6602 52063 WHEN VHF CIRCUIT BREAKERS WERE PUSHED IN, THE FREQUENCY INDICATOR LIGHTS FLASHED ON/OFF. DURING HOVER TO THE MAINTENANC E PAD FROM THE BACK ROW, PILOT SMELLED FUMES. REMOVED VHF RADIO AND INSTALLED SERVICEABLE RADIO AND REMOVED BURNED SMEL L. VISUALLY INSPECTED BEHIND INSTRUMENT PANEL AND FOUND NO DISCREPANCIES. VISUALLY INSPECTED BEHIND CIRCUIT BREAKER PA NEL AND FOUND NO DEFECTS. 1 G 7 1 3U NC H2SW 1996062700352 19960627 00352 SW 1996 6 27 96ZZZX3167 1 19960529 A 3213 412050010107 CROSSTUBE BELL 412 412 1182202 SW LT AFT FAILED A A HEEA O OTHER O OTHER LD LANDING 1 SW 03 2148K 6114 A148 36001 AFTER LANDING AND ROLLING THROTTLES BACK TO GROUND IDLE WITH CREW AND 10 PASSENGERS ON BOARD, AIRCRAFT'S CROSSTUBE FRACT URED IN TWO RESULTING IN AIRCRAFT ROLLING TO THE LEFT. BROKEN SECTION OF TUBE CONTACTED HELIPORT PREVENTING AIRCRAFT FR OM ROLLING OVER. FORWARD CROSSTUBE WAS DEFORMED DURING INCIDENT. 1 G 7 2 4U H4SW 1996062700359 19960627 00359 NE 1996 6 27 96ZZZX3174 2 19960508 A 7421 9560136490 IGNITER AEROSP SA365 SA365N 8680669 EU TMECA ARRIEL ARRIEL1C 60030 NE ENGINE TIP WORN A ZYWA K NONE O OTHER IN INSP/MAINT 1 GL 09 365SJ 18708 6018 2256 IGNITER TIPS WORN. REPLACED 3 EACH. REMOVED AND REPLACED IGNITERS. 1 G 7 2 3U 3 U H10EU E19EU 1996062700360 19960627 00360 NE 1996 6 27 96ZZZX3175 2 19960508 A 7421 9560136490 IGNITER AEROSP SA365 SA365N 8680669 EU TMECA ARRIEL ARRIEL1C 60030 NE ENGINE TIP WORN A ZYWA K NONE O OTHER IN INSP/MAINT 1 GL 09 365SJ 14004 6018 2256 IGNITER TIPS WORN. REPLACED 3 EACH. REMOVED AND REPLACED IGNITERS. 1 G 7 2 3U 3 U H10EU E19EU 1996062700361 19960627 00361 NE 1996 6 27 96ZZZX3176 2 19960508 A 7421 9560136490 IGNITER AEROSP SA365 SA365N 8680669 EU TMECA ARRIEL ARRIEL1C 60030 NE ENGINE TIP WORN A ZYWA K NONE O OTHER IN INSP/MAINT 1 GL 09 365SJ 14037 6018 2256 IGNITER TIPS WORN. REPLACED 3 EACH. REMOVED AND REPLACED IGNITERS. 1 G 7 2 3U 3 U H10EU E19EU 1996062700362 19960627 00362 EU 1996 6 27 96ZZZX3177 1 19960528 A 2810 365A55302301 CELL AEROSP SA365 SA365N 8680669 EU FUEL SYSTEM LEAKS A ZYWA K NONE K FLUID LOSS IN INSP/MAINT 1 GL 09 365SJ 3043 1164 6018 FUEL CELL LEAKS. REMOVED AND REPLACED FUEL CELL. 1 G 7 2 3U H10EU 1996062700363 19960627 00363 EU 1996 6 27 96ZZZX3178 1 19960529 A 2810 365A55302200 CELL AEROSP SA365 SA365N 8680669 EU FUEL SYSTEM LEAKS A ZYWA K NONE K FLUID LOSS IN INSP/MAINT 1 GL 09 365SJ 3043 433 6018 FUEL CELL LEAKS. REMOVED AND REPLACED FUEL CELL. 1 G 7 2 3U H10EU 1996062700378 19960627 00378 NM 1996 6 27 USAA960453 1 19960525 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 328 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 279AU 35210 22891 INT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND 1 INCH BY 2.50 INCH CORRODED AREA BS 328, RLB 21, FLOOR BEAM CAP. INSTA LLED DOUBLER, REPAIRED PER TR 53-10-01 A. (X) 2 L 7 2 4F A16WE 1996062700379 19960627 00379 NM 1996 6 27 USAA960454 1 19960525 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 294.5 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 279AU 35210 22891 INT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND CORROSION AT NUTPLATE ON T-CAP .50 INCH BY 1 INCH, STA 294.5 AT BL ZERO, T-CAP OF FLOOR BEAM. REMOVED CORRODED SECTION OF T-CAP, FABRICATED AND SPLICED IN NEW SECTION PER TR 53-10-04 B. (X) 2 L 7 2 4F A16WE 1996062700380 19960627 00380 NM 1996 6 27 USAA960455 1 19960525 A 5330 SKIN BOEING 737 7372B7 1384560 NM SERV DOOR CUTOUT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 279AU 35210 22891 INT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND 2.5 INCH LONG CRACK IN FUSELAGE SKIN AT LOWER AFT CORNER OF FORWARD SERV ICE DOOR CUT OUT. STOP DRILLED CRACK AND INSTALLED DOUBLER PER TR 53-10-19, REV A. (X) 2 L 7 2 4F A16WE 1996062700381 19960627 00381 NM 1996 6 27 USAA960458 1 19960525 A 5240 SKIN BOEING 737 7372B7 1384560 NM AFT SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 279AU 35210 22891 INT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND 1 INCH CRACK AT LOWER HINGE CUT OUT ON A/C AFT SERVICE DOOR SKIN. INSTA LLED FUSELAGE SKIN REPAIR AND REPAIRED PER SRM 53-30-3. (X) 2 L 7 2 4F A16WE 1996062700382 19960627 00382 NM 1996 6 27 USAA960459 1 19960525 A 5311 FRAME BOEING 737 7372B7 1384560 NM BS 312 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 279AU 35210 22891 INT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND .50 INCH CRACKED FRAME, STA 312, STR 5L. INSTALLED DOUBLER, REPAIRED PE R SRM 53-40-3, FIGURE 1. (X 2 L 7 2 4F A16WE 1996062700383 19960627 00383 NM 1996 6 27 USAA960460 1 19960525 A 5314 KEEL BEAM BOEING 737 7372B7 1384560 NM BS 663-727 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 279AU 35210 22891 INT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND 1 INCH BY 64 INCHES OF EROSION/FRETTING CORROSION ON LT/RT KEEL BEAM BS 663 - BS 727 W/W CUT OUT PANEL ATTACH FLANGES. INSTALLED REINFORCING/CHAFE STRIPS. REPAIRED PER EA 41139 SRM 51-10-1. (X) 2 L 7 2 4F A16WE 1996062700384 19960627 00384 NM 1996 6 27 USAA960461 1 19960525 A 5313 STRINGER BOEING 737 7372B7 1384560 NM BS 727L OUT OF LIMITS A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 279AU 35210 22891 INT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND FASTENER HOLE EDGE DISTANCE OUT OF LIMITS (SHORT EDGE MARGIN) STR 18A, S TA 727L, AFT LOWER HOLE. INSTALLED REPAIR ANGLE, REPAIRED PER EA 41124. (X) 2 L 7 2 4F A16WE 1996062700385 19960627 00385 NM 1996 6 27 USAA960462 1 19960525 A 5230 SKIN BOEING 737 7372B7 1384560 NM AFT CARGO DOOR CREASE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 279AU 35210 22891 INT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND CREASE IN EXTERIOR DOOR SKIN 6 INCHES LONG AFT CARGO DOOR (NEAR HANDLE). INSTALLED EXTERIOR SKIN REPAIR, REPAIRED PER TR 52-10-01 A. (X) 2 L 7 2 4F A16WE 1996062700390 19960627 00390 SW 1996 6 27 HEEA967272 1 19960529 A 3340 214175127103 POWER SUPPLY BELL 214 214ST 1182106 SW STROBE INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5748M 22 28102 POWER SUPPLY INOPERATIVE. 2 G 7 2 4U H10SW 1996062700391 19960627 00391 EU 1996 6 27 HEEA967273 1 19960530 A 2822 D107318D1 PUMP BOLKMS 105 BO105S 5626006 EU FUEL BOOST INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7062X S793 INOPERATIVE. NO PRESSURE AND POPPING CB. RECEIVED INSTALLED ON AIRCRAFT. 1 G 7 2 3U H3EU 1996062700392 19960627 00392 EU 1996 6 27 HEEA967274 1 19960530 A 2510 350A77125805 SEAT SNIAS 350 AS350B2 8680813 EU COCKPIT CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6095S 483 2777 SEAT IS CRACKED. (CRACKED IN TWO PLACES) 1 G 7 1 3U H9EU 1996062700393 19960627 00393 SW 1996 6 27 HEEA967275 1 19960530 A 7120 206064105102 LEG ASSY BELL 206 206L1 1182107 SW ENG MOUNT MIS MFG E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 LEG ASSEMBLY DOES NOT FIT FIXTURE PROPERLY. (HAS ABOUT 3/8" TO 1/4" BEND) 1 G 7 1 3U H2SW 1996062700394 19960627 00394 SW 1996 6 27 HEEA967276 1 19960530 A 6320 214040002119S TRANMISSION BELL 214 214ST 1182106 SW M/R MAKING METAL E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 835 28106 TRANSMISSION HAS METAL IN OIL. 2 G 7 2 4U H10SW 1996062700395 19960627 00395 SW 1996 6 27 HEEA967277 1 19960530 A 7712 206075739105 INDICATOR BELL 206 206L3 1182108 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 108PH 51334 INDICATES 3% HIGH OUT OF TOLERANCE AND SLUGGISH OPERATION. 1 G 7 1 3U H2SW 1996062700396 19960627 00396 SW 1996 6 27 HEEA967280 1 19960530 A 3340 214175127103 POWER SUPPLY BELL 214 214ST 1182106 SW STROBE INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 4 28101 POWER SUPPLY INOPERATIVE. 2 G 7 2 4U H10SW 1996062700397 19960627 00397 SW 1996 6 27 HEEA967281 1 19960530 A 7810 206064300005 EXHAUST ASSY BELL 206 206L1 1182107 SW ENG CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5007Y 80 45192 EXHAUST ASSY IS CRACKED. (CRACK 3/4" LONG AT BASE MOUNTING FLANGE AND 1 1/4" LONG VERTICAL CRACK AT WELDED SEAM INTERSE CTING EACH OTHER IN FORM OF REVERSED "T". 1 G 7 1 3U H2SW 1996062700398 19960627 00398 SW 1996 6 27 HEEA967282 1 19960530 A 7810 206064300005 EXHAUST ASSY BELL 206 206L1 1182107 SW ENG CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 16938 29 45157 EXHAUST ASSY IS CRACKED. (CRACK 1 1/8" LONG AT WELDED SEAM ON BACK SIDE OF STACK WELD LOOKS TO BE UNDERCUT.) 1 G 7 1 3U H2SW 1996062700399 19960627 00399 SW 1996 6 27 HEEA967283 1 19960530 A 6520 212040462001 SHAFT 212040004009 BELL 212 212 1181420 SW T/R GR BOX DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 27805 AHT51288 31106 BOLT HOLES DO NOT ALIGN PROPERLY WITH THREADED HOLES OF BEVEL GEAR. 1 G 7 1 4U H4SW 1996062700400 19960627 00400 GL 1996 6 27 HEEA967286 2 19960530 A 7240 23008614 COMBUSTION LINER 23033185 BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL TURBINE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 16938 CAT70113 45157 CAE860015 ENGINE REMOVED DUE TO LOW POWER. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: CRACKED BEYOND SERVICEABLE LIMI TS ON COMBUSTION LINER I.D. IN DOUBLE LIP AREA. REPLACED DISCREPANT PART. 1 G 7 1 3U 3 U H2SW E1GL 1996062700401 19960627 00401 1996 6 27 HEEA967288 4 19960530 A 3457 0110005400 GPS 150 BOLKMS 105 BO105S 5626006 EU COCKPIT INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 4294R S860 GPS INOPERATIVE. 1 G 7 2 3U H3EU 1996062700402 19960627 00402 1996 6 27 HEEA967289 4 19960530 A 2312 064101501 TRANSCEIVER KTR953 BELL 412 412 1182202 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2258F 33073 TX AND RX BREAKS UP DURING ENGINE RUN-UP. 1 G 7 2 4U H4SW 1996062700403 19960627 00403 NE 1996 6 27 HEEA967290 2 19960530 A 7260 STARTER DRIVE SKRSKY S76 S76A 8143006 NE TMECA ARRIEL ARRIEL1S 60030 NE ENG GEAR BOX FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 117WB 98 760092 3509TEC REMOVED STARTER GEN STARTER; DRIVE PULLED OUT OF ENGINE GEARBOX NUT INSIDE GEARBOX HOUSING. 1 G 7 2 3U 3 U H1NE E19EU 1996062700404 19960627 00404 1996 6 27 HEEA967291 4 19960530 A 3457 0110005400 GPS 150 BELL 206 206L3 1182108 SW COCKPIT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 141BH 51303 GPS UNIT DOES NOT PICKUP SATELLITE STATIONS AT ALL. 1 G 7 1 3U H2SW 1996062700405 19960627 00405 EU 1996 6 27 HEEA967292 1 19960530 A 6210 117150081 BLADE BOLKMS 117 BK117A3 5626015 EU M/R SEPARATION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8765J 1595 7054 LEADING EDGE SEPARATION ON THE INBOARD END UPPER AND LOWER SURFACE BEYOND LIMITS. 1 G 7 2 3U H13EU 1996062700406 19960627 00406 NE 1996 6 27 HEEA967293 1 19960530 A 6410 7610105101041 BLADE SKRSKY S76 S76A 8143006 NE T/R UNBONDED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 117WB 3708 760092 ABRASION STRIP CRACKED, TIP WEIGHT COVER DEBONDING AND SPAR PLUG UNBONDING. 1 G 7 2 3U H1NE 1996062700407 19960627 00407 NE 1996 6 27 HEEA967294 1 19960530 A 6410 7610105101041 BLADE SKRSKY S76 S76A 8143006 NE T/R STRIP CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 117WB 3708 760092 SKIN VOID, ABRASION STRIP CRACKED AND ELIPTICAL PLUG UNBONDED. 1 G 7 2 3U H1NE 1996062700408 19960627 00408 NE 1996 6 27 HEEA967295 1 19960530 A 6410 7610105001045 BLADE SKRSKY S76 S76A 8143006 NE T/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8316 BLADE IS CRACKED. (CRACK ON THE LEADING EDGE ABRASION STRIP ON PADDLE "B". 1 G 7 2 3U H1NE 1996062700409 19960627 00409 NE 1996 6 27 HEEA967296 1 19960530 A 6210 7615009100051A BLADE SKRSKY S76 S76A 8143006 NE M/R SEPARATION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22342 11738 760096 SEPARATION ON THE NICKEL STRIP AND ON THE INBOARD SECTION OF THE TRAILING EDGE. 1 G 7 2 3U H1NE 1996062700411 19960627 00411 1996 6 27 HEEA967298 4 19960531 A 3416 D120P2T ANEROID BELL 412 412 1182202 SW ALTIMETER ERRATIC E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2258F 33073 BAROMETRIC ANEROID UNIT HAS AN INCONSISTANT OUTPUT. 1 G 7 2 4U H4SW 1996062700412 19960627 00412 NE 1996 6 27 HEEA967299 1 19960531 A 7933 7645001078101 INDICICATOR SKRSKY S76 S76A 8143006 NE ENG OIL INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1545X 760050 ENGINE TEMP INDICATOR INOPERATIVE. 1 G 7 2 3U H1NE 1996062700413 19960627 00413 SW 1996 6 27 HEEA967300 1 19960531 A 5320 206031302191 PANEL ASSY BELL 206 206L1 1182107 SW AIR FRAME MIS MFG E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5 DOUBLERS INSTALLED IN WRONG SPOTS. 1 G 7 1 3U H2SW 1996062700414 19960627 00414 1996 6 27 HEEA967301 4 19960531 A 3452 066106200 TRANSPONDER KT76 BOLKMS 117 BK117B1 5626012 EU COCKPIT MALFUNCTION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 911TL 7198 ATC UNABLE TO RECEIVED MODE C. FOUND LOW POWER OUT. TRIED ADJUSTING POEWR TO SPECS. REPLACED CAVITY TUBE V101. REPAIR ED. ADJUSTED FREQUENCY. BENCH CHECK GOOD. 1 G 7 2 3U H13EU 1996062700415 19960627 00415 SW 1996 6 27 HEEA967302 1 19960531 A 5511 206020120011 SPAR ASSY BELL 206 206B 1181511 SW HORIZ STAB CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 21431 3452 SPAR ASSY IS CORRODED. (PITTING CORROSION BEYOND LIMITS) SCRAPPED SPAR ASSEMBLY. 1 G 7 1 3U H2SW 1996062700416 19960627 00416 SW 1996 6 27 HEEA967303 1 19960531 A 6330 206033505003 ARM ASSY BELL 206 206L1 1182107 SW NODAL BEAM CHAFED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2246Q 45752 ARM ASSY IS CHAFED. NOTE: THE BEAM AT POINT WHERE CHAFFING OCCURRED IS 1/16" TOO THICK. REPLACED WITH SERVICEABLE NOD AL BEAM. 1 G 7 1 3U H2SW 1996062700417 19960627 00417 SW 1996 6 27 HEEA967304 1 19960531 A 5320 205030710007 FITTING BELL 212 212 1181420 SW FUSELAGE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5736D 31135 FITTING IS CRACKED. (VERTICAL ANGLE CRACKED AT 3RD RIVET HOLES FROM THE TOP IN THE JOGGLE AREA. ANGLE WAS INSTALLED UN DER PRELOAD. REPLACED WITH SERVICEABLE ANGLE. 1 G 7 1 4U H4SW 1996062700418 19960627 00418 EU 1996 6 27 HEEA967305 1 19960531 A 2822 R1110900A5 FUEL PUMP BOLKMS 117 BK117B2 5626013 EU BOOST LEAKAGE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 134AE 7237 FUEL PUMP SEAL LEAKAGE. 1 G 7 2 3U NC H13EU 1996062700419 19960627 00419 SW 1996 6 27 HEEA967306 1 19960531 A 2822 3881005 FUEL PUMP BELL 206 206L1 1182107 SW BOOST WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 50182 45242 PUMP WORN INTERNAL DRIVE SPLINES. 1 G 7 1 3U H2SW 1996062700420 19960627 00420 EU 1996 6 27 HEEA967307 1 19960531 A 7722 TM42739 INDICATOR BOLKMS 105 BO105S 5626006 EU COCKPIT ERRATIC E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 54191 S804 NEEDLE HAS AN ERRATIC INDICATION. TIME SINCE REPAIR 0:00. 1 G 7 2 3U H3EU 1996062700421 19960627 00421 EU 1996 6 27 HEEA967308 1 19960531 A 6700 10541488 CONTROL ROD BOLKMS 105 BO105S 5626006 EU FLT CONTROL CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5421E S806 CONTROL ROD IS CORRODED. (CORROSION UNDER CONTROL ROD NUT) REPLACED WITH SERVICEABLE CONTROL ROD. 1 G 7 2 3U H3EU 1996062700422 19960627 00422 EU 1996 6 27 HEEA967309 1 19960531 A 6700 SK279L279441 CONTROL ROD BOLKMS 105 BO105S 5626006 EU FLT CONTROL DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5421E 6168 S806 NUT END OF CONTROL ROD DAMAGED. REPLACED WITH SERVICEABLE CONTROL ROD. 1 G 7 2 3U H3EU 1996062700423 19960627 00423 GL 1996 6 27 HEEA967310 2 19960604 A 7230 6871259 TIE BOLT 6890550 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL 1ST STAGE WHEEL MIS MFG E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81832 CAC35165 S828 CAE830473 UPON INSTALLATION NOTED THE FOLLOWING: UNABLE TO ENGAGE THREADS INTO 1ST STAGE WHEEL. UPON INSPECTION OF PART NOTED TH E FOLLOWING: IMPROPERLY MACHINED THREADS ON TIE BOLT FWD END. 1 G 7 2 3U 3 U H3EU E4CE 1996062700424 19960627 00424 SW 1996 6 27 HEEA967311 1 19960604 A 5230 1000404 HANDLE ASSY BELL 230 230 1182149 SW DOOR CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 3110 23009 HANDEL IS CRACKED. (HOUSING IS CRACKED) 1 G 7 2 3U NC H9SW 1996062700425 19960627 00425 EU 1996 6 27 HEEA967312 1 19960604 A 6720 10543079 CONTROL ROD BOLKMS 105 BO105S 5626006 EU T/R CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5421E S806 ROD IS CORRODED. (CORROSION FOUND UNDERNEATH BLACK HEAT SHRINK. REPLACED WITH SERVICEABLE CONTROL TUBE. 1 G 7 2 3U H3EU 1996062700426 19960627 00426 EU 1996 6 27 HEEA967313 1 19960604 A 3340 A413AHDADF1428 POWER SUPPLY BOLKMS 105 BO105S 5626006 EU STROBE FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 7136H S833 NO POWER COMING OUT OF POWER SUPPLY. SENT TO WHELAN ENGINE CO. FOR INSPECTION AND REPAIR. 1 G 7 2 3U H3EU 1996062700427 19960627 00427 EU 1996 6 27 HEEA967314 1 19960604 A 5610 350A2500000107 CANOPY SNIAS 350 AS350B2 8680813 EU FWD CORNER CHANNEL BROKE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 2857 2771 CANOPY FRAME U CHANNELS WERE BROKEN AT FORWARD UPPER AND LOWER CORNERS. REPAIRED WITH MESH COMPOSITE SYSTEM AND RETURNED TO SERVICE. 1 G 7 1 3U H9EU 1996062700428 19960627 00428 EU 1996 6 27 HEEA967315 1 19960604 A 6420 704A33633078C LAMINATE BEARING SNIAS 350 AS350B2 8680813 EU T/R FLAPPING WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100R 2862 TAIL ROTOR LAMINATE FLAPPING BEARINGS ARE WORN AND SPLIT. REPLACED WITH SERVICEABLE BEARING. 1 G 7 1 3U H9EU 1996062700429 19960627 00429 NE 1996 6 27 HEEA967316 1 19960604 A 2435 200SGL15Q STARTER SKRSKY S76 S76A 8143006 NE START/GEN FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 706AE 2245 760275 WHEN FIRST PRESSURE STARTING BUTTON - STARTER MAKES LOUD CLUNK/GRINDING NOISE. REPLACED WITH SERVICEABLE STARTER GENERAT OR. 1 G 7 2 3U H1NE 1996062700430 19960627 00430 NE 1996 6 27 HEEA967317 1 19960604 A 6210 7615009043050 TIP CAP SKRSKY S76 S76A 8143006 NE M/R BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31219 760230 TIP CAP OUTER TRAILING EDGE BROKEN OFF. 1 G 7 2 3U H1NE 1996062700431 19960627 00431 NE 1996 6 27 HEEA967318 1 19960604 A 6210 7615009100051 BLADE SKRSKY S76 S76A 8143006 NE M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1547D 8245 760077 BLADE IS CRACKED. (SPAR CRACK NEAR THE ROOT END.) SCRAPPED, 1 G 7 2 3U H1NE 1996062700432 19960627 00432 1996 6 27 HEEA967319 4 19960604 A 3442 MI5852221 RADAR RT3002 BEECH 200 200CBEECH 1152926 CE COCKPIT INTERMITTENT E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 500PH BL29 RADAR INTERMITTENT. 1 L 7 2 4T A24CE 1996062700433 19960627 00433 1996 6 27 HEEA967321 4 19960604 A 3416 B4553110004 ALTIMETER BOLKMS 117 BK117B1 5626012 EU COCKPIT LEAKS E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 191BK 7146 ALTIMETER LEAKS AT BAROMETRIC KNOB. 1 G 7 2 3U H13EU 1996062700434 19960627 00434 1996 6 27 HEEA967322 4 19960604 A 3416 A30 ENCODER BELL 206 206L3 1182108 SW ENCODER DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 6603X 51412 ENCODER OUTPUT READS 9000 FEET AT STATIC AND WILL NOT CALIBRATE. 1 G 7 1 3U H2SW 1996062700435 19960627 00435 1996 6 27 HEEA967323 4 19960604 A 3416 A30 ENCODER BELL 206 206L1 1182107 SW COCKPIT ERRATIC E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1077A 45382 ENCODER INCONSISTENT OUTPUT. 1 G 7 1 3U H2SW 1996062700436 19960627 00436 1996 6 27 HEEA967324 4 19960604 A 3416 5035P2P42 ALTIMETER BOLKMS 105 BO105S 5626006 EU COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 7170D S840 ENCODER IS OFF 80 FEET AT 5000 FEET AND NEEDLE HAS STICKY INDICATION. 1 G 7 2 3U H3EU 1996062700437 19960627 00437 1996 6 27 HEEA967325 4 19960604 A 3416 D120P2T ANEROID BELL 206 206L 1181522 SW ENCODER ERRATIC E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 8094L 1 52125 ENCODER HAS AN ERRATIC OUTPUT. 1 G 7 1 3U H2SW 1996062700438 19960627 00438 1996 6 27 HEEA967326 4 19960604 A 3416 D120P2T ANEROID BELL 206 206L3 1182108 SW ENCODER ERRATIC E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 141BH 51303 UNIT HAS AN ERRATIC OUTPUT. SENT TO TRANS CAL INDUSTRIES FOR WARRANTY REPAIR. 1 G 7 1 3U H2SW 1996062700439 19960627 00439 1996 6 27 HEEA967327 4 19960604 A 2210 7611133 AMPLIFIER SKRSKY S76 S76A 8143006 NE ROLL SLICE DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 22342 760096 #1 ROLL AFCS KICKING IN FLIGHT. SENT TO HELICOPTER SUPPORT, INC. FOR EXCHANGE. 1 G 7 2 3U H1NE 1996062700440 19960627 00440 EU 1996 6 27 HEEA967328 1 19960604 A 7722 TM42040 GAUGE BOLKMS 105 BO105S 5626006 EU COCKPIT TOT FRICTION ERROR E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 EXCESSIVE FRICTION ERROR AND WILL NOT RETURN TO ZERO. SENT TO MASCO FOR INSPECTION AND REPAIR. 1 G 7 2 3U H3EU 1996062700441 19960627 00441 1996 6 27 HEEA967329 4 19960604 A 3416 B4553110004 ALTIMETER BOLKMS 117 BK117A4 5626017 EU COCKPIT FRICTION ERROR E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 911RZ 7092 NEEDLE HAS EXCESSIVE FRICTION ERROR. 1 G 7 2 3U H13EU 1996062700445 19960627 00445 SW 1996 6 27 HEEA967333 1 19960604 A 7722 206075678103 INDICATOR BELL 206 206L3 1182108 SW COCKPIT MALFUNCTION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 979BH 51403 INDICATOR DROPS TO ZERO INTERMITTENTLY. 1 G 7 1 3U H2SW 1996062700446 19960627 00446 1996 6 27 HEEA967334 4 19960604 A 3416 212070238007 INDICATOR BELL 412 412 1182202 SW COCKPIT STICKS E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2258F 33073 INDICATOR NEEDLE STICKS THROUGHOUT SCALE. 1 G 7 2 4U H4SW 1996062700447 19960627 00447 SW 1996 6 27 HEEA967335 1 19960604 A 6320 206040190005 PUMP BELL 206 206L3 1182108 SW M/R GR BOX DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3207Q 51540 PUMP HOUSING DAMAGED AND SHAFT WORN IN SEAL AREA. 1 G 7 1 3U H2SW 1996062700448 19960627 00448 SW 1996 6 27 HEEA967336 1 19960604 A 6320 206040190005 PUMP BELL 206 206L1 1182107 SW M/R GR BOX SHAFT WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5019F 45244 PUMP HOUSING DAMAGED AND SHAFT WORN IN SEAL AREA. 1 G 7 1 3U H2SW 1996062700449 19960627 00449 1996 6 27 HEEA967337 4 19960604 A 3422 258719342 GYRO SKRSKY S76 S76A 8143006 NE COCKPIT MALFUNCTION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5128 760181 GYRO CAUSES COMPASS CORD TO SPIN INTERMITTENTLY. 1 G 7 2 3U H1NE 1996062700450 19960627 00450 NE 1996 6 27 HEEA967338 2 19960605 A 7210 3024780 GEARBOX BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE COMBINING FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 108X 9920 33115 NR 2 ENGINE FAILED TO ENGAGE AFTER START, THEN ENGAGED WITH LOUD BANG AT N1 64 PERCENT. 1 G 7 2 4U 4 U H4SW E22EA 1996062700451 19960627 00451 SW 1996 6 27 HEEA967339 1 19960605 A 7714 8DJ81WBS4 INDICATOR BELL 206 206L1 1182107 SW COCKPIT ERRATIC E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1076Y 45380 ERRATIC OPERATION FROM 0 TO 65%. SENT TO PRECISION AVIONICS & INST., INC. FOR INSPECTION AND REPAIR. 1 G 7 1 3U H2SW 1996062700452 19960627 00452 1996 6 27 HEEA967340 4 19960605 A 3414 8000 INDICATOR BELL 206 206B3 1181506 SW COCKPIT AS FLUCTUATION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2268W 3606 NEEDLE HAS A 10 KT. FLUCTUATION DURING FLIGHT. SENT TO PRECISION AVIONICS & INST., INC. FOR INSPECTION AND REPAIR. 1 G 7 1 3U H2SW 1996062700453 19960627 00453 SW 1996 6 27 HEEA967341 1 19960605 A 7930 1241153 INDICATOR BELL 212 212 1181420 SW ENG OIL PRESS MALFUNCTION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3131S 30953 TEMP. NEEDLE STICKS AND PRESSURE READS HIGH. SENT TO MASCO FOR INSPECTION AND REPAIR. 1 G 7 1 4U H4SW 1996062700454 19960627 00454 1996 6 27 HEEA967342 4 19960605 A 3457 0845000000 SKYNAV 5000 BOLKMS 117 BK117A3 5626015 EU COCKPIT MALFUNCTION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 8765J 7054 SHOWS ERRONEOUS SYMBOLS AT START-UP. 1 G 7 2 3U H13EU 1996062700455 19960627 00455 1996 6 27 HEEA967343 4 19960605 A 2562 ELT910 ELT NARCO BELL 206 206L3 1182108 SW COCKPIT MALFUNCTION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 206LS 51070 ELT TURNS ON BY ITSELF. 1 G 7 1 3U H2SW 1996062700456 19960627 00456 NE 1996 6 27 HEEA967344 2 19960605 A 7321 214060325103 FUEL CONTR BELL 214 214ST 1182106 SW GE CT7TS CT72A 30030 NE NR 1 ENG DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 8045T 28101 #1 ENGINE SURGES. SENT FUEL CONTROL FOR INSPECTION AND REPAIR. 2 G 7 2 4U 4 U H10SW E8NE 1996062700457 19960627 00457 SW 1996 6 27 HEEA967345 1 19960605 A 7712 206075739113 TORQUEMETER BELL 206 206L 1181522 SW COCKPIT ERRATIC E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 7077B 52037 ERRATIC AND RATCHETY MOVEMENT. TIME SINCE REPAIR :25. 1 G 7 1 3U H2SW 1996062700458 19960627 00458 EU 1996 6 27 HEEA967346 1 19960605 A 2150 20475591 TURBINE BOLKMS 105 BO105S 5626006 EU ECU SEIZED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 911FL S717 TURBINE SEIZED. 1 G 7 2 3U H3EU 1996062700459 19960627 00459 1996 6 27 HEEA967347 4 19960605 A 3421 4021541671 HORIZON GYRO BOLKMS 117 BK117A3 5626015 EU COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 8765J 7054 ARTIFICAL HORIZON GYRO SLOW TO ERECT AND CAUSING PITCH KICKING. 1 G 7 2 3U H13EU 1996062700460 19960627 00460 WP 1996 6 27 96ZZZM1013 1 19960523 A 3260 TERMINAL STRIP DOUG DC8 DC861 3021952 WP LANDING GEAR BROKEN WIRE A FXLA O OTHER P NO WARNING INDICATION AP APPROACH 1 SO 19 29UA 46159 ON ARRIVAL AT FL 574 - GUA-MIA - LANDING GEAR WAS EXTENDED. THE LEFT LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE. WHEN FLAPS WERE SELECTED TO 35 DEGREES THE LANDING GEAR HORN WENT OFF. UPON ARRIVAL REPAIRED WIRE AT TERMINAL STRIP S-5 IAW MM 20-50-1 AND PERFORMED SWING IAW MM 32-60-0. OPERATIONAL CHECKS NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4A25 1996062700461 19960627 00461 NM 1996 6 27 96ZZZM1014 1 19960531 A 3230 65461083 WALKING BEAM BOEING 737 737298C 1384490 NM LT MLG BROKEN A ASAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 01 745AS 20794 ANC - TEST FLT - CREW REPORTED, LEFT MAIN LANDING GEAR RED LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. CYCLED MAI N LANDING GEAR SEVERAL TIMES AND INDICATION REMAINED THE SAME. DURING RETURN, THE LEFT GREEN DOWN LIGHT ILLUMINATED WIT H THE GEAR IN THE OFF POSITION LANDED WITHOUT INCIDENT. FOUND LEFT MAIN LANDING GEAR WALKING BEAM BROKEN. REPLACED BEA M AND MAIN GEAR ACTUATOR, ACCOMPLISHED GEAR EXTEND/RETRACT ADJUSTMENT TEST AND RELEASED AIRCRAFT FOR TEST FLIGHT. REFER ENCE ASAA9610071. 2 L 7 2 4F RT A16WE 1996062700462 19960627 00462 NM 1996 6 27 96ZZZM1015 1 19960530 A 2133 7110033 OUTFLOW VLV BOEING 737 7372B7 1384560 NM CABIN MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 271AU 22883 PIT - FLT 1297 - AT 31,000 FEET, CREW RECEIVED A PRESSURIZATION WARNING HORN ON THE AUTOMATIC SYSTEM. CREW SWITCHED TO MANUAL PRESSURIZATION CONTROL AND DESCENDED TO 10,000 FEET. NO EMERGENCY WAS DECLARED. FLIGHT RETURNED TO FIELD AND LA NDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE CABIN PRESSURIZATION CONTROLLER (P/N 7638102) AND THE AFT CABIN PRESSURIZATION OUTFLOW VALVE (P/N 7110033). OPERATIONAL CHECK GOOD. REFERENCE USAASB96094 2 L 7 2 4F A16WE 1996062700463 19960627 00463 NM 1996 6 27 96ZZZM1016 1 19960605 A 3230 BACR13CG2AB R432 RELAY BOEING 737 737301 1384611 NM E/E COMPT MALFUNCTIONED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 589US 23934 CLT - FL 1405 - CREW COULD NOT RAISE GEAR USING NORMAL PROCEDURES. ALTERNATE PROCEDURES WORKED, HOWEVER, THE TAKEOFF WA RNING HORN SOUNDED. FLIGHT RETURNED TO CLT AND LANDED WITH NO FURHTER INCIDENT. MAINTENANCE REPLACED THE R432 AND R276 RELAYS AND PERFORMED A GEAR SWING. REFERENCE USAASB96101. 2 L 7 2 4F RT A16WE 1996062700464 19960627 00464 EU 1996 6 27 96ZZZM1017 1 19960607 A 7830 189188002 TR CABLES FOKKER F28 F28MK0100 4990807 EU NR 1 ENG BROKEN A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 893US 11373 PIT - FLT 1672 - CREW COULD NOT ADVANCE THROTTLES PAST 34 UNITS DURING CLIMB. FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE NR 1 THROTTLE FEEDBACK CABLES FROZEN AND BROKEN. CABLES WERE REPLACED. REFER ENCE USAAF96057. 2 L 7 2 4F RT 1996062700465 19960627 00465 NM 1996 6 27 96ZZZM1018 1 19960530 A 3230 65446915 MODULE BOEING 737 737298C 1384490 NM LT MLG INOP A ASAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 01 745AS 20794 ANC-ATB - FLT 145 - ON DEPARTURE FROM ANC, THE LT MLG RED LIGHT REMAINED ILLUMINATED WITH THE GEAR HANDLE IN THE UP POSI TION, BOTH THE GREEN AND RED LIGHTS ILLUMINATED WITH THE GEAR HANDLE IN THE OFF POSITION. ALL INDICATIONS WERE NORMAL W ITH THE GEAR SELECTED DOWN. AIRCRAFT RETURNED TO ANC AND LANDED WITHOUT INCIDENT. MX JACKED AIRCRAFT AND CYCLED GEAR, UNABLE TO DUPLICATE THE PROBLEM ON THE GROUND. REMOVED AND REPLACED MAIN GEAR UPLOCK ACTUATOR AND MODULE PACKAGE AS PRE CAUTIONARY. COMPLETED GEAR EXTENSION AND RETRACTION ADJUSTMENT AND TEST. OPERATIONAL AND LEAK CHECKS GOOD. REFERENCE ASAA9610067. 2 L 7 2 4F RT A16WE 1996062700466 19960627 00466 EU 1996 6 27 96ZZZM1019 1 19960520 A 5730 1379336B401 SKIN BAG JETSTM JETSTM3201 1500217 EU LT WING CORRODED B AY55 K NONE O OTHER IN INSP/MAINT 1 SO 03 844JX 9238 844 DURING THE COURSE OF PERFORMING A 2000 HOUR INSPECTION, FOUND LEFT UPPER WING SKIN CORRODED IN THE AREA OF ENGINE NACELL E BETWEEN THE MAIN AND REAR SPARS. CORROSION REMOVED EXCEEDING SRM LIMITS, AND REPAIRS WERE PERFORMED IAW WITH BRITISH AEROSPACE REPAIR SCHEME NR 13711084R. THERE IS NOT A CURRENT SERVICE BULLETIN OR AIRWORTHINESS DIRECTIVE THAT ADDRESSES THIS PROBLEM. 2 L 7 2 4T RT A56EU 1996062700467 19960627 00467 EA 1996 6 27 96ZZZM1020 1 19960409 A 5755 75770001042 SPOILER ASSY DHAV DHC7 DHC7102 2802708 EA RT WING DAMAGED A A CICA K NONE O OTHER IN INSP/MAINT 1 SO 17 234SL 1400 FI373 24 ON PRE-FLIGHT, FLIGHT CREW REPORTED 'RIGHT INBOARD ROLL SPOILER IN NEED OF REPAIR.' INVESTIGATION BY MX FOUND RIGHT INB OARD ROLL SPOILER WAS MISSING 95 PERCENT OF THE SPOILER. ATTACH ARMS AND APPROXIMATELY ONE FOOT OF THE ROLL SPOILER REM AINED. MX REPLACED ROLL SPOILER AND AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 4 4T A20EA 1996062700468 19960627 00468 WP 1996 6 27 96ZZZM1021 2 19960528 A 7260 31033336 BEARING FRCHLD SA227 SA227DC 3377521 SW GARRTT TPE331 TPE33112UHR WP RT GEARBOX FAILED A EQGA E ENGINE SHUTDOWN J WARNING INDICATION LD LANDING 1 SW 19 847LS 5922 DC847B P70152 AFTER LANDING AT ROW, THE CHIP DETECTOR LIGHT CAME ON. THE PILOT COMPLETED A NORMAL SHUTDOWN WITH NO FURTHER INDICATION S. AFTER INSPECTING THE CHIP DETECTOR, IT WAS DETERMINED A FAILURE HAD TAKEN PLACE IN THE GEARBOX. AFTER INSPECTING TH E GEARBOX, IT WAS FOUND THAT THE MAIN COMPRESSOR BEARING HAD FAILED. THE BEARING WAS REPLACED AND THE ENGINE REASSEMBLE D. ENGINE GROUND RUNS AND TEST FLIGHTS CHECKED OK AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A18SW E4WE 1996062700469 19960627 00469 WP 1996 6 27 96ZZZM1022 2 19960526 A 7260 31035992 IDLER DRIVE ASSY FRCHLD SA227 SA227DC 3377521 SW GARRTT TPE331 TPE33112UHR WP RT GEARBOX STRIPPED A A EQGA E D ENGINE SHUTDOWN RETURN TO BLOCK Y ENGINE STOPPAGE TX TAXI/GRND HDL 1 SW 19 853LS 4444 DC853B P70183 AFTER STARTING ENGINES AND TAXIING FOR TAKEOFF, THE RIGHT ENGINE SHUTDOWN WITHOUT WARNING. THE AIRCRAFT TAXIED BACK TO THE GATE. UPON INSPECTION OF THE GEARBOX, THE ACCESSORY GEAR ASSEMBLY WAS FOUND TO BE STRIPPED IN THE CENTER OF THE GEA R. THIS GEAR, P/N 3103601-6, S/N P435C, AS WELL AS THE IDLER GEAR ASSEMBLY, P/N 3103599-2, WHICH WAS STRIPPED, WERE REP LACED. ALL GROUND RUNS CHECKED SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A18SW E4WE 1996062700470 19960627 00470 WP 1996 6 27 96ZZZM1023 2 19960526 A 7260 31036016 GEAR ASSY FRCHLD SA227 SA227DC 3377521 SW GARRTT TPE331 TPE33112UHR WP RT GEARBOX STRIPPED A A EQGA E D ENGINE SHUTDOWN RETURN TO BLOCK Y ENGINE STOPPAGE TX TAXI/GRND HDL 1 SW 19 853LS 4444 P435C DC853B P70183 AFTER STARTING ENGINES AND TAXIING FOR TAKEOFF, THE RIGHT ENGINE SHUTDOWN WITHOUT WARNING. THE AIRCRAFT TAXIED BACK TO THE GATE. UPON INSPECTION OF THE GEARBOX, THE ACCESSORY GEAR ASSEMBLY WAS FOUND TO BE STRIPPED IN THE CENTER OF THE GEA R. THIS GEAR, P/N 3103601-6, S/N P435C, AS WELL AS THE IDLER GEAR ASSEMBLY, P/N 3103599-2, WHICH WAS STRIPPED, WERE REP LACED. ALL GROUND RUNS CHECKED SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A18SW E4WE 1996062700471 19960627 00471 NM 1996 6 27 96ZZZM1024 1 19960519 A 2782 1U109592 ACTUATOR BOEING 727 72722C 138400F NM NR 2 SLAT MALFUNCTIONING A RYNA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 CE 07 429EX 19100 THE NR 2 LEADING EDGE SLAT FAILED TO RETRACT AFTER TAKEOFF FROM IND. AIRCRAFT MADE AIR TURN BACK TO IND AND LANDED WITH OUT INCIDENT. REPLACED THE NR 2 SLAT ACTUATOR PER MM 27-81-32. OPS CHECK GOOD. (M) 2 L 7 3 4F A3WE 1996062700472 19960627 00472 NM 1996 6 27 96ZZZM1025 1 19960518 A 3610 39271611 SHUTOFF VLV BOEING 727 727222 1384073 NM NR 3 ENG AIR LEAK A RYNA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 CE 07 7639U 19912 AFTER TAKEOFF FROM BDL, THE NR 3 ENGINE STRUT OVERHEAT WARNING LIGHT ILLUMINTED. THE AIRCRAFT RETURNED TO BDL WITHOUT I NCIDENT. LIGHT EXTINGUISHED WITH REDUCED POWER. FOUND BLEED AIR LEAK AT THE JUNCTION OF THE PNEUMATIC DUCT TO THE NR 3 MODULATING AND SHUT OFF VALVE. REPOSITIONED AND RECLAMPED PNEUMATIC DUCT A MODULATING AND SHUT OFF VALVE PER MM 36-12- 00. LEAK CHECKS GOOD. (M) 2 L 7 3 4F A3WE 1996062700473 19960627 00473 NM 1996 6 27 AALA960765 1 19960512 A 3350 A3060698101 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 659AA 24617 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS FROM PAX SEAT ROW 18F AND AFT INOPERATIVE. RESEATED LOOSE EMERGENC Y FLOOR LIGHT STRIP CONNECTOR BY PAX SEAT ROW 18F. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1996062700474 19960627 00474 EU 1996 6 27 AALA960767 1 19960511 A 3350 STRIP AIRBUS 300 A300B4605R 3930308 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 90070 513 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS INOPERATIVE AT LEFT AISLE OF FIRST CLASS CABIN, AT RIGHT AISLE BETW EEN PAX SEAT ROWS 12 THROUGH 14 AND AT RIGHT AISLE BETWEEN PAX SEAT ROWS 21 THROUGH 23. REPLACED EMERGENCY FLOOR LIGHT STRIPS AT LEFT AISLE OF FIRST CLASS CABIN, AT RIGHT AISLE BETWEEN PAX SEAT ROWS 12 THROUGH 14 AND AT RIGHT AISLE BETWEEN PAX SEAT ROWS 21 THROUGH 23. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996062700475 19960627 00475 NM 1996 6 27 AALA960770 1 19960513 A 3350 1703643 CONTACT PIN BOEING 767 767223 1385123 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 335AA 22333 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 34H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONTACT P IN AT PAX SEAT 34H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1996062700476 19960627 00476 WP 1996 6 27 AALA960776 1 19960516 A 5347 593056675 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1195 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 283AA 49296 TUL - FOUND CORROSION ON SEAT TRACK NR 3 AT STATION 1195. INSTALLED PLUG IN SEAT TRACK AT STATION 1195 PER SRM 53-05 FI G 4A. (M) 2 L 7 2 4F A6WE 1996062700477 19960627 00477 WP 1996 6 27 AALA960777 1 19960516 A 5347 593056675 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1212-1250 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 283AA 49296 TUL - FOUND CORROSION ON TOP OF TRACK NR 1 AND GALLEY TIE DOWNS HAS INTERGRANULAR CORROSION IS FROM STATION 1212-1250. C UT OUT AREA THAT WAS BEYOND LIMITS AND INSTALLED PLUG PER SRM 53-05 FIG 4A AND TREATED AND PRIMED. (M) 2 L 7 2 4F A6WE 1996062700478 19960627 00478 WP 1996 6 27 AALA960778 1 19960516 A 5347 593056675 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1210 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 283AA 49296 TUL - FOUND GALLEY TIE DOWN IN SEAT TRACK NR 1 HAS INTERGRANULAR CORROSION AT STATION 1210. CUT OUT AREA THAT WAS BEYON D LIMITS AND INSTALLED PLUG PER SRM 53-05 FIG 4A AND TREATED AND PRIMED. (M) 2 L 7 2 4F A6WE 1996062700479 19960627 00479 NM 1996 6 27 AALA960782 1 19960508 A 5311 143T10601 FRAME BOEING 767 767323 1385205 NM BS 654 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 354AA 24035 AFW - FOUND AREA OF CORROSION BEYOND SRM LIMITS. BLEND OUT DAMAGE PER ENGINEERING MRB 767-1232. (M) 2 L 7 2 4F RT A1NM 1996062700480 19960627 00480 NM 1996 6 27 AALA960783 1 19960510 A 5753 11372311 SKIN BOEING 767 767323 1385205 NM LT TE FLAP WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 382AN 25451 AFW - FOUND LEFT WING INBOARD AFT FLAP LEADING EDGE SKIN WORN FROM CONTACT WITH SEAL RETAINER. FOUND WEAR TO BE BEYOND SRM ALLOWABLE LIMITS, BLENDED WEAR. ACCOMPLISHED EDDY CURRENT CHECK. NO CRACKS FOUND. FILLED AND RESTORED SURFACE FIN ISH. ADJUSTED SEAL TO PREVENT CHAFING. APPROVED BY ENGINEERING PER MRB 767-1225. 2 L 7 2 4F RT A1NM 1996062700481 19960627 00481 WP 1996 6 27 AALA960788 1 19960517 A 5320 99365347 SUPPORT DOUG DC9 DC982 3022082 WP BS 160-200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 283AA 49296 TUL - FOUND CORROSION ALONG FLOOR SUPPORT STATION 160 TO 200 AT CLIP NUT AREAS, CORROSION BEYOND LIMITS. REPLACED ANGLE SUPPORT. (M) 2 L 7 2 4F A6WE 1996062700482 19960627 00482 WP 1996 6 27 AALA960789 1 19960520 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1871-1880 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 FOUND CORROSION ON FUSELAGE SKIN INTERIOR ABOVE PREVIOUSLY INSTALLED DOUBLER LEFT SIDE STATION 1871, LONGERON 45 AND 46L . TRIMMED OUT CORRODED SKIN AREA AND REMOVED CORROSION FROM SURROUNDING SKIN AREA. TREATED AND PAINTED INSTALLED REPAI R DOUBLER AS PER SRM 53-20-00 FIG 6. (M) 2 L 7 3 4F A22WE 1996062700483 19960627 00483 WP 1996 6 27 AALA960790 1 19960520 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1326 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 TUL - FOUND CORROSION AROUND FUEL SHROUD DRAIN IN LOWER FUSELAGE SKIN, STATION 1326. REMOVED CORROSION AND BLENDED, TRE ATED AND PAINTED. INSTALLED DOUBLER PER SRM 53-40-00 FIG 20. (M) 2 L 7 3 4F A22WE 1996062700484 19960627 00484 WP 1996 6 27 AALA960791 1 19960520 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1481-1491 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 TUL - FOUND TWO FUSELAGE SKINS LOWER DRAINS CORRODED AROUND FLUID OUTLET HOLES. REMOVED CORROSION AND BLENDED AREA. TR EATED AND PAINTED INSTALLED DOUBLER PER SRM VOL 53-40-00 FIG 20. (M) 2 L 7 3 4F A22WE 1996062700485 19960627 00485 NM 1996 6 27 AALA960795 1 19960516 A 5280 113T831610 FITTING BOEING 767 767323 1385205 NM RT DOOR FIG WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 351AA 24032 AFW - FOUND INBOARD SIDE OF RIGHT TRUNNION DOOR FITTING BEYOND SRM LIMITS AFTER BLENDING. ROTOPEENED, ALODINED AND PAIN TED WORN AREA. APPROVED BY ENGINNERING PER MRB 767-1220. (M) 2 L 7 2 4F RT A1NM 1996062700486 19960627 00486 NM 1996 6 27 AALA960796 1 19960516 A 5311 146T1250 FRAME BOEING 767 767323 1385205 NM BS 1417 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 351AA 24032 AFW - FOUND FUSELAGE FRAME WEB IN AFT CARGO CORRODED AROUND NUT PLATE HOLE HAS DAMAGE BEYOND SRM LIMITS. REMOVED CORROS ION, ALODINED AND PRIMED DAMAGED AREA. APPROVED BY ENGINEERING PER MRB 767-1225. (M) 2 L 7 2 4F RT A1NM 1996062700487 19960627 00487 NM 1996 6 27 AALA960797 1 19960516 A 5320 143T501416 WEB BOEING 767 767323 1385205 NM BS 611 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 351AA 24032 AFW - FOUND SMALL AREA OF CORROSION ON WEB. FOUND BEYOND SRM LIMITS AFTER BLENDING. ALODINED, PRIMED AND BLENDED AREA. APPROVED BY ENGINEERING PER MRB 767-1224. (M) 2 L 7 2 4F RT A1NM 1996062700488 19960627 00488 NM 1996 6 27 AALA960798 1 19960516 A 5320 146T80482 CHORD BOEING 767 767323 1385205 NM BS 127.6 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 351AA 24032 AFW - FOUND INTERGRANULAR CORROSION AROUND OUTBOARD FASTENER HOLE. FOUND TWO CORROSION AREAS BEYOND SRM LIMITS AFTER BL ENDING. COUNTERBORED REAMED AND INSTALLED FREEZE PLUG IN AREA OF INTERGRANULAR CORROSION. ALODINED AND REFINISHED TWO BLENDOUTS. (M) 2 L 7 2 4F RT A1NM 1996062700489 19960627 00489 NM 1996 6 27 AALA960799 1 19960516 A 5320 143T82053 CHORD BOEING 767 767323 1385205 NM BS 568-570 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 351AA 24032 AFW - FORWARD CARGO LOWER DOOR CHORD CORRODED AROUND TWO HOLES ON INBOARD SIDE, FOUND BEYOND SRM LIMITS AFTER BLENDING. ALODINED AND REFINISHED BLENDED AREAS. APPROVED BY ENGINEERING PER MRB 767-1222. (M) 2 L 7 2 4F RT A1NM 1996062700490 19960627 00490 NM 1996 6 27 AALA960800 1 19960516 A 5320 143T82042 STRAP BOEING 767 767323 1385205 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 351AA 24032 AFW - FOUND FAIL/SAFE STRAP CORRODED. AFTER BLENDING FOUND 7 BLENDOUTS BEYOND SRM LIMITS. ALODINED AND REFINISHED DAMA GED AREA. APPROVED BY ENGINEERING PER MRB 767-1221. (M) 2 L 7 2 4F RT A1NM 1996062700491 19960627 00491 NM 1996 6 27 AALA960801 1 19960515 A 5320 143T1582 STRAP BOEING 767 767323 1385205 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 351AA 24032 AFW - FOUND FORWARD CARGO DOOR FRAME FAIL/SAFE STRAP CORRODED BEYOND SRM LIMITS AFTER BLENDING. ALODINED AND PRIMED BLE NDED AREA. APPROVED BY ENGINEERING PER MRB 767-1217. (M) 2 L 7 2 4F RT A1NM 1996062700492 19960627 00492 NM 1996 6 27 AALA960802 1 19960516 A 5320 146T80472 STRAP BOEING 767 767323 1385205 NM BS 1244-1305 NOTCHED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 351AA 24032 AFW - FOUND AFT CABIN CARGO STRAP NOTCHED IN 3 PLACES. BLENDED CUT NOTCHES. ROTOPEENED, ALODINED AND PRIMED. APPROVED BY ENGINEERING PER MRB 767-1227. (M) 2 L 7 2 4F RT A1NM 1996062700493 19960627 00493 NM 1996 6 27 AALA960803 1 19960516 A 5330 146T3330 SKIN BOEING 767 767323 1385205 NM PAX DOOR CUTOUT GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 351AA 24032 AFW - FOUND TWO GOUGES ON SKIN LAP AFT APPROX 7 INCHES OF L-2 DOOR. FOUND BEYOND SRM LIMITS AFTER BLENDING. EDDY CURRE NT CHECKED. NO CRACKS FOUND. COUNTERSINKED AND REPLACED FASTENERS. APPROVED BY ENGINEERING PER MRB 767-1219. (M) 2 L 7 2 4F RT A1NM 1996062700494 19960627 00494 WP 1996 6 27 AALA960811 1 19960520 A 5347 593056687 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1060-1182 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 283AA 49296 TUL - FOUND SEAT TRACK CORROSION BLENDED BEYOND MANUAL LIMITS FROM STATION 1060 TO STATION 1182, REF E58-4A 0095459, 009 5471, 0095483. SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05. (M) 2 L 7 2 4F A6WE 1996062700495 19960627 00495 NM 1996 6 27 AALA960813 1 19960521 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 385AM 27059 SFO - DURING OVERNIGHT CHECK, EMERGNCY EXIT LIGHT AT PAX SEAT 26B INOPERATIVE. REPAIRED BROKEN EMERGENCY EXIT LIGHT AT PAX SEAT 26B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1996062700496 19960627 00496 WP 1996 6 27 AALA960816 1 19960624 A 5320 FLOOR SUPPORT DOUG DC10 DC1030 3023501 WP BS 422 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 137AA 47847 TUL - FOUND FLOOR SUPPORT AFT OF G2 BETWEEN INBOARD AND OUTBOARD GALLEY MOUNTS CORRODED AT BOTH ENDS. REMOVED AND FABRI CATED NEW FLOOR SUPPORTS PER SRM 53-00-01, INSTALLED SAME AND TREATED AND PAINTED PER SRM 51-21-01. (M) 2 L 7 3 4F A22WE 1996062700497 19960627 00497 WP 1996 6 27 AALA960817 1 19960521 A 5320 39363631 FITTING DOUG DC9 DC982 3022082 WP BS 786 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 475AA 49650 TUL - FOUND CRACK 4 INCHES LONG ON FITTING AT FORWARD END OF LEFT KEEL BEAM. REMOVED AND REPLACED SPLICE FITTING. (M) 2 L 7 2 4F A6WE 1996062700498 19960627 00498 WP 1996 6 27 AALA960820 1 19960515 A 5320 JAMB DOUG DC9 DC982 3022082 WP BS 160-200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 283AA 49296 TUL - FOUND CORROSION LEFT CUSP AT FORWARD ENTRY STATION 160 TO 200. INSTALLED DOUBLER PER ESO 80559, DATED 5-17-96. ( M) 2 L 7 2 4F A6WE 1996062700499 19960627 00499 NM 1996 6 27 AALA960827 1 19960526 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 369AA 25196 JFK - DURING OVERNIGHT CHECK, FOUND ARROWED EMERGENCY EXIT LIGHT AT LEFT FORWARD OVERWING DOOR INOPERATIVE. REPAIRED PO WER WIRE AT TERMINAL ON LIGHT L-322. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1996062700500 19960627 00500 NM 1996 6 27 AALA960828 1 19960526 A 2420 8044012005 TRANSFORMER HAMSTD BOEING 767 767323 1385205 NM E/E COMPT FAILED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 358AA 91029036 24039 JFK - DURING CRUISE, THE COCKPIT EXPERIENCED SMOKE FOR A SHORT DURATION. SMOKE APPEARED TO BE COMING FROM THE CENTER CO NSOLE ON THE FIRST OFFICER SIDE. LANDED JFK WITHOUT FURTHER INCIDENT. REPLACED BLEED AIR BITE MODULE TRANSFORMER. SYS TEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1996062700501 19960627 00501 NM 1996 6 27 AALA960829 1 19960527 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 643AA 24601 MIA - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTING IN FIRST CLASS SECTION TO COACH CLASS INOPERATIVE . REPAIRED WIRE SPLICE CONNECTOR AT COACH CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1996062700502 19960627 00502 NM 1996 6 27 AALA960833 1 19960509 A 5315 11175008 FLOOR BEAM BOEING 767 767323 1385205 NM BS 894-999 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 366AA 25193 AFW - FLOOR BEAM AT LBL 33 HAD CORROSION AT TWO LOCATIONS BEYOND SRM LIMITS. REPAIRED PER MRB NBR 767-1229. (M) 2 L 7 2 4F RT A1NM 1996062700503 19960627 00503 NM 1996 6 27 ASAA9610065 1 19960528 A 3230 ACTUATOR BOEING 737 737210C 1384459 NM NLG LEAKING A ASAA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 NM 01 744AS 21822 ANC-ATB - FLT 122 - ON TAKEOFF FROM ANC, NOSE LANDING GEAR FAILED TO RETRACT. AIRCRAFT RETURNED TO ANC AND LANDED WITHO UT INCIDENT. MAINTENANCE FOUND 'B' NUT ON NLG LOCK ACTUATOR LEAKING. TIGHTENED 'B' NUT, PERFORMED RETRACTION CHECK AND GEAR OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1996062700504 19960627 00504 NM 1996 6 27 ASAA9610066 1 19960530 A 3230 RETRACT MECH BOEING 737 737298C 1384490 NM LT MLG MALFUNCTIONED A ASAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 01 745AS 20794 ANC-ATB - FLT 123 - ON DEPARTURE FROM ANC, THE LT MLG EXTENDED AND LOCKED DOWN WHEN THE GEAR HANDLE MOVED TO THE OFF POS ITION. THE LT MLG RED UNSAFE LIGHT ILLUMINATED WITH THE GEAR HANDLE UP. AIRCRAFT RETURNED TO ANC AND LANDED WITHOUT IN CIDENT. MAINTENANCE JACKED THE AIRCRAFT AND CYCLED THE GEAR SEVERAL TIMES, COULD NOT DUPLICATE ON GROUND. COMPLETED IN SPECTION OF THE UPLOCK/DOWNLOCK ASSY, NO DEFECTS NOTED. LUBED GEAR AND RELEASED AIRCRAFT. (M) 2 L 7 2 4F RT A16WE 1996062700505 19960627 00505 NM 1996 6 27 ASAA9610067 1 19960530 A 3233 69774969 ACTUATOR BOEING 737 737298C 1384490 NM LT MLG INOP A ASAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 01 745AS 20794 ANC-ATB - FLT 145 - ON DEPARTURE FROM ANC, THE LT MLG RED LIGHT REMAINED ILLUMINATED WITH THE GEAR HANDLE IN THE UP POSI TION, BOTH THE GREEN AND RED LIGHTS ILLUMINATED WITH THE GEAR HANDLE IN THE OFF POSITION. ALL INDICATIONS WERE NORMAL W ITH THE GEAR SELECTED DOWN. AIRCRAFT RETURNED TO ANC AND LANDED WITHOUT INCIDENT. MX JACKED AIRCRAFT AND CYCLED GEAR, UNABLE TO DUPLICATE THE PROBLEM ON THE GROUND. REMOVED AND REPLACED MAIN GEAR UPLOCK ACTUATOR AND MODULE PACKAGE AS PRE CAUTIONARY. COMPLETED GEAR EXTENSION AND RETRACTION ADJUSTMENT AND TEST. OPERATIONAL AND LEAK CHECKS GOOD. (M) 2 L 7 2 4F RT A16WE 1996062700506 19960627 00506 NM 1996 6 27 ASAA9610069 1 19960531 A 3233 69774969 RETRACT ACUATOR BOEING 737 737298C 1384490 NM LT MLG MALFUNCTIONED A ASAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 01 745AS 20794 ANC - TEST FLT - CREW REPORTED, LEFT MAIN LANDING GEAR RED LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. CYCLED MAI N LANDING GEAR SEVERAL TIMES AND INDICATION REMAINED THE SAME. DURING RETURN, THE LEFT GREEN DOWN LIGHT ILLUMINATED WIT H THE GEAR IN THE OFF POSITION, LANDED WITHOUT INCIDENT. FOUND LEFT MAIN LANDING GEAR WALKING BEAM BROKEN. REPLACED BE AM AND MAIN GEAR ACTUATOR, ACCOMPLISHED GEAR EXTEND/RETRACT ADJUSTMENT TEST AND RELEASED AIRCRAFT FOR TEST FLIGHT. (M) 2 L 7 2 4F RT A16WE 1996062700507 19960627 00507 NM 1996 6 27 ASAA9610070 1 19960531 A 3230 RETRACT MECH BOEING 737 737298C 1384490 NM LT MLG OUT OF ADJUST A ASAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 01 745AS 20794 ANC - TEST FLT 9300 - CREW REPORTED, LEFT MAIN LANDING GEAR DOES NOT STAY RETRACTED; EXTENDS OUT OF WHEEL WELL WHEN GEAR HANDLE MOVED TO OFF. LOCKS IN DOWN POSITION AFTER EXTENDING. LANDED WITHOUT INCIDENT. FOUND MANUAL EXTENSION LINKAGE OUT OF RIG. ADJUSTED PER THE MM AND ACCOMPLISHED GEAR EXTEND/RETRACT ADJUSTMENT TEST. (M) 2 L 7 2 4F RT A16WE 1996062700508 19960627 00508 NM 1996 6 27 ASAA9610071 1 19960601 A 3233 69774969 ACTUATOR BOEING 737 737298C 1384490 NM LT MLG MALFUNCTIONED A ASAA K NONE J WARNING INDICATION NR NOT REPORTED 1 NM 01 745AS 20794 ANC - TEST FLT 9300 - CREW REPORTED, LEFT MAIN LANDING GEAR DOES NOT STAY RETRACTED, EXTENDS OUT OF WHEEL WELL WHEN GEAR HANDLE MOVED TO OFF. LANDED WITHOUT INCIDENT. REPLACED LEFT MAIN LANDING GEAR TRANSFER CYLINDER; HOWEVER, PROBLEM REM AINED. FERRIED AIRCRAFT TO SEA. ON ARRIVAL SEA, FOUND RETRACT CYLINDER HITTING HARD ON WING DOOR STABILIZER LINK. REP LACED RETRACT ACTUATOR AND STABILIZER LINK. SYSTEM OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996062700509 19960627 00509 WP 1996 6 27 ASAA9680120 1 19960522 A 3350 20131A BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 936AS 49363 SFO - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHT IN THE FORWARD CABIN WERE FOUND DIM. REPLACED THE BATTE RIES AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996062700510 19960627 00510 WP 1996 6 27 ASAA9680121 1 19960524 A 5240 HOLD OPEN HOOK DOUG DC9 DC983 3022083 WP L2 DOOR OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 LAX - DURING MAINTENACNE CHECK, THE L2 DOOR HOLD OPEN HOOK WOULD NOT ENGAGE IN LATCH. ADJUSTED HOLD OPEN HOOK MECHANISM AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996062700511 19960627 00511 WP 1996 6 27 ASAA9680122 1 19960524 A 5347 TMS6019943 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1204 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 954AS 28629 49387 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON SEAT TRACK AT Y1204, X PLUS 42, Z PLUS 1. REMOVED DAMAGED AREA AND INSTA LLED NEW PIECES IAW DC-9 SRM. (M) 2 L 7 2 4F A6WE 1996062700512 19960627 00512 WP 1996 6 27 ASAA9680123 1 19960524 A 5347 TMS6019943 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1281-1295 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 954AS 28629 49387 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON SEAT TRACK AT Y1281 TO Y1295, X PLUS 42, Z PLUS 1. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM. (M) 2 L 7 2 4F A6WE 1996062700513 19960627 00513 NE 1996 6 27 ASOA96016 2 19960523 A 7320 3038044 P3 LINE EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE BROKEN A A ASOA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 11 127AM 120103 115213 LEVELING OFF AT 2000 FEET DEPARTING DFW, LEFT ENGINE SURGED SLIGHTLY AND SHUTDOWN COMPLETELY WITH AUTOFEATHER. NO LIMIT ATIONS WERE EXCEEDED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW WHERE A LANDING WAS MADE WITHOUT INCID ENT. UPON INSPECTION FOUND P3 LINE BROKEN AT LEFT ENGINE OVERSPEED GOVERNOR. REPLACED P3 LINE AT HMU TO OVERSPEED GOVE RNOR. OPS CHECKS GOOD ON GROUND RUN-UP. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1996062700514 19960627 00514 NE 1996 6 27 ASOA96017 2 19960523 A 7261 4171322 OIL CAP EMB 120 EMB120RT SO PWA 118 PW118 NE ENGINE WORN A ASOA A E UNSCHED LANDING ENGINE SHUTDOWN J K WARNING INDICATION FLUID LOSS CL CLIMB 1 SO 11 227AS 120023 115260 FLT 7925 - ON CLIMB-OUT GOT AURAL WARNING (3 BELLS), ENGINE OIL. OIL PRESSURE WAS FLUCTUATING BETWEEN 55 AND 30 PSID. S HUT ENGINE NR 2 DOWN. AN EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED TO DFW. THE AIRCRAFT WAS LANDED WITHOUT INCIDENT . CLEANED AND INSPECTED RIGHT ENGINE. SERVICED WITH 8 QUARTS OF OIL. GROUND RAN ENGINE AT ALL POWER SETTING. NO LEAK S NOTED. AS A PRECAUTIONARY MEASURE REPLACED ENGINE OIL CAP. SUSPECT OIL CAP SEAL WORN. OPS AND LEAK CHECKS WERE SATI SFACTORY. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1996062700515 19960627 00515 SO 1996 6 27 ASOA96018 1 19960530 A 5230 12023348005 SEAL EMB 120 EMB120RT SO CARGO DOOR DEFECTIVE A ASOA A B UNSCHED LANDING EMER. DESCENT J WARNING INDICATION DE DESCENT 1 SO 11 232AS 120036 IN FLT ATL-CRW - WHILE DESCENDING FROM 25,000 TO 24,00 FEET, CABIN RAPIDLY DEPRESSURIZED FOLLOWING A THUMP HEARD BY ALL 3 CREW MEMBERS. CAPTAIN DECLARED AN EMERGENCY, DESCENDED TO 10,000 FEET AND DIVERTED INTO TRI WHERE LANDING WAS MADE SA FELY AND WITHOUT INCIDENT. FBO MECH INSPECTED AND FOUND SAFE FOR UNPRESSURIZED FERRY FLIGHT TO ATL. REMOVED AND REPLAC ED CARGO DOOR SEAL. OPERATIONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996062700516 19960627 00516 EU 1996 6 27 C2XA961A131 1 19960602 A 5347 NTA44768 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 42836 200 IAH - DURING C-CHECK INSPECTION, LEFT AND RT FLIGHT ATTENDANT SEAT TRACKS FOUND TO HAVE CORROSION BEYOND LIMITS. MX REM OVED FABRICATED AND INSTALLED NEW TRACKS, FRAMES 36 TO FRAME 39. (M) 2 H 7 2 4T RT A53EU 1996062700517 19960627 00517 SO 1996 6 27 C2XA961A132 1 19960601 A 3246 31446 RIM BFGOODRICH EMB 120 EMB120RT SO NR MLG WHEEL CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 27707 1089 120095 IAH - DURING PILOT PRE-FLIGHT, FOUND THE NR 2 MAIN WHEEL ASSEMBLY OUTER HALF WHEEL RIM CRACKED AND SEPARATING. MX REMOV ED AND REPLACED WHEEL ASSY. (M) 2 L 7 2 4T RT A31SO 1996062700518 19960627 00518 SO 1996 6 27 C2XA961A133 1 19960531 A 3350 AGC1 FUSE EMB 120 EMB120RT SO CABIN FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 26714 120118 IAH - DURING 1A, 3A INSPECTION, BOTH LEFT AND RIGHT LOWER EXTERIOR EMERGENCY EXIT LIGHTS FOUND TO BE INOPERATIVE. MX RE MOVED AND REPLACED THE AFT EMERGENCY EXIT LIGHT POWER SUPPLY FUSE. (M) 2 L 7 2 4T RT A31SO 1996062700519 19960627 00519 SO 1996 6 27 C2XA961A134 1 19960604 A 5347 12016000003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 57734 120199 IAH - DURING C-CHECK INSPECTION, FOUND PASSENGER LEFT AND RIGHT SEAT TRACKS TO HAVE CORROSION BEYOND LIMITS. MX REMOVED AND REPLACED SEAT TRACKS, FRAME 29 TO FRAME 39. (M) 2 L 7 2 4T RT A31SO 1996062700520 19960627 00520 NE 1996 6 27 C2XA96IA130 2 19960515 A 7261 S931000600000 OIL LINE AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE NR 2 ENGINE SPLIT A C2XA A E UNSCHED LANDING ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 17831 185 IAH - FLT NR 3779 - PILOT REPORTED, THAT THE NR 2 ENGINE LOST OIL PRESSURE, THE CREW ELECTED TO SHUT DOWN THE ENGINE AND RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MX REMOVED AND REPLACED THE AUX GENERATOR SEAL, AND THE AIRCRAFT RETUR NED TO THE GATE ON THE NEXT FLIGHT REPORTING THE NR 2 OIL PRESSURE LOW. MX REMOVED AND REPLACED THE OIL PRESSURE SWITCH LINE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1996062700521 19960627 00521 SO 1996 6 27 C2XA96IA135 1 19960604 A 5400 12041441002 CHANNEL EMB 120 EMB120RT SO RT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 57734 120199 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT MAIN LANDING INBOARD LOWER NACELLE CHANNEL DEFORMED AND CRACKED BETWEEN NAC ELLE FRAME 14 AND FRAME 15. MAINTENANCE REMOVED AND REPLACED NACELLE CHANNEL. (M) 2 L 7 2 4T RT A31SO 1996062700522 19960627 00522 SO 1996 6 27 C2XA96IA136 1 19960604 A 5320 12006647001 T-CAP EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 57734 120199 IAH - DURING C-CHECK INSPECTION, FOUND FRAME 36 LEFT OUTBOARD T-CAP TO HAVE CORROSION BEYOND LIMITS. MX REMOVED AND REP LACED FRAME 36 LEFT OUTBOARD T-CAP. (M) 2 L 7 2 4T RT A31SO 1996062700523 19960627 00523 SO 1996 6 27 C2XA96IA137 1 19960604 A 5320 12006158002 BUTTSTRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 57734 120199 IAH - DURING C-CHECK INSPECTION, FOUND FRAME 37 TO FRAME 41.5 RIGHT INBOARD BUTTSTRAP TO HAVE CORROSION BEYOND LIMITS. M X REMOVED AND REPLACED RT INBOARD BUTTSTRAP FRAME 37 TO FRAME 41.5. (M) 2 L 7 2 4T RT A31SO 1996062700524 19960627 00524 SO 1996 6 27 C2XA96IA138 1 19960604 A 5320 12006158003 BUTTSTRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 57734 120199 IAH - DURING C-CHECK INSPECTION, FOUND FUSELAGE CENTER BUTTSTRAP FRAME 39 TO FRAME 44 TO HAVE CORROSION BEYOND LIMITS. M X REMOVED AND REPLACED CENTER BUTTSTRAP FROM FRAME 37 TO FRAME 44. (M) 2 L 7 2 4T RT A31SO 1996062700525 19960627 00525 SO 1996 6 27 C2XA96IA139 1 19960604 A 5320 12004449001 T-CAP EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 57734 120199 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT INBOARD T-CAP FRAME 38 TO HAVE CORROSION BEYOND LIMITS. MX REMOVED AND REP LACED RT INBOARD T-CAP FRAME 38. (M) 2 L 7 2 4T RT A31SO 1996062700526 19960627 00526 SO 1996 6 27 C2XA96IA140 1 19960604 A 5320 12006647001 T-CAP EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 57734 120199 IAH - DURING C-CHECK INSPECTION, FOUND FRAME 38 LEFT AND RIGHT OUTBOARD T-CAPS TO HAVE CORROSION BEYOND LIMITS. MX REMO VED AND REPLACED LEFT AND RIGHT OUTBOARD T-CAPS FRAME 38. (M) 2 L 7 2 4T RT A31SO 1996062700527 19960627 00527 NM 1996 6 27 CAL960599 1 19960429 A 5320 DOOR FRAME BOEING 737 737291 138448W NM CARGO COMPT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10251 70772 20361 GSO - INSPECTION FOUND A 3 INCH CRACK IN AFT CARGO COMPARTMENT DOOR CUTOUT FORWARD FRAME. THE FRAME SECTION WAS REMOVED AND REPLACED IAW EA 5310-02555. (M) 2 L 7 2 4F A16WE 1996062700528 19960627 00528 NM 1996 6 27 CAL960615 1 19960514 A 2720 65448619 PWR CONTL UNIT BOEING 737 7373T0 1384582 NM RUDDER INOPERATIVE A CALA O OTHER F FLT CONT AFFECTED CL CLIMB 1 SW 09 17356 24453 24453 23942 THE AIRCRAFT EXPERIENCED AN UNCOMMANDED ROLL AFTER TAKEOFF. RIGHT RUDDER INPUT WAS USED TO COUNTER ACT THE MOVEMENT. T HE YAW DAMPER SWITCH WAS CONFIRMED ON. THE FLIGHT WAS CONTINUED TO BOS WHERE IT LANDED WITHOUT FURTHER EVENT. MAINTENA NCE REMOVED AND REPLACED THE YAW DAMP COUPLER. THE MAIN RUDDER PCU WAS REPLACED AS A PRECAUTIONARY MEASURE. AN ECRA FO R UNCOMMANDED ROLL INSPECTION WAS ISSUED AND COMPLIED WITH AND NO DEFECTS WERE FOUND. IN ADDITION, THE RUDDER TRIM SWIT CH WAS REPLACED PER ECRA 2726-01001 AND THE NR 3 SPOILER ACTUATOR WAS REPLACED DUE TO LEAKAGE. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION. *S/D* VENDOR TEARDOWN FOUND NO FAULTS WITH THE YAW DAMP COUPLER. TEARDOW 2 L 7 2 4F RT A16WE 1996062700529 19960627 00529 WP 1996 6 27 CAL960620 1 19960517 A 3260 833702 DOWNLOCK SENSOR DOUG DC9 DC982 3022082 WP LT MLG INOPERATIVE A CALA O OTHER N FALSE WARNING AP APPROACH 1 SW 09 14890 49114 FLT 1105 - CLE - THE LEFT MLG UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR EXTENSION ON APPROACH TO CLE. CYCLING THE GE AR DID NOT HELP. THE GEAR WAS MANUALLY EXTENDED, BUT THE LIGHT REMAINED ON. THE GEAR WAS VISUALLY VERIFIED DOWN THROUG H THE VIEW PORT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT MLG DOWNLOCK SENSOR AT FAULT. THE D OWNLOCK SENSOR WAS REMOVED AND REPLACED. A GEAR SWING WAS PERFORMED AND ALL OPERATION AND INDICATIONS CHECKED GOOD. (M ) 2 L 7 2 4F A6WE 1996062700530 19960627 00530 WP 1996 6 27 CAL960621 1 19960520 A 7931 SEALS DOUG DC9 DC982 3022082 WP OIL PRESS TRANSM LEAKING A CALA E A ENGINE SHUTDOWN UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SW 09 57837 49582 FLT NR 1891 - MSY - THE NR 2 ENG OIL QTY INDICATOR DROPPED TO ZERO WHILE EN ROUTE FROM TPA TO IAH. THE OIL PRESSURE DRO PPED BELOW 35 SPI. THE NR 2 ENGINE WAS SHUTDOWN AS A PRECAUTIONARY MEASURE AND THE AIRCRAFT WAS DIVERTED TO MSY WHERE I T LANDED WITHOUT INCIDENT. MX FOUND A STATIC OIL LEAK OF OIL PRESSURE TRANSMITTER VENT RESTRICTOR BOLT AT GEARBOX. THE SEALS WERE REPLACED. THE OIL FILTER AND STRAINER COVER WERE ALSO REPLACED. THE ENGINE WAS RUN AND NO LEAKS WERE NOTED . (M) 2 L 7 2 4F A6WE 1996062700531 19960627 00531 NM 1996 6 27 CAL960622 1 19960430 A 5320 ANGLE BOEING 737 7373T0 1384582 NM L-1 DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69351 27168 23589 HOU - INSPECTION CORROSION ON Z-ANGLE AT L-1 DOOR. THE ANGLE WAS REPLACED IAW SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1996062700532 19960627 00532 NM 1996 6 27 CAL960623 1 19960430 A 5320 ANGLE BOEING 737 7373T0 1384582 NM R-1 DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69351 27168 23589 HOU - INSPECTION FOUND Z-ANGLE CORRODED AT R-1 DOOR. THE CORROSION WAS REMOVED IAW SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1996062700533 19960627 00533 NM 1996 6 27 CAL960624 1 19960430 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69351 27168 23589 HOU - INSPECTION FOUND FLOORBEAM CORRODED AT BS 344 ON LEFT AND RIGHT SIDE. A NEW FLOORBEAM WAS FABRICATED AND INSTALLE D IAW SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1996062700534 19960627 00534 NM 1996 6 27 CAL960625 1 19960430 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 986.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69351 27168 23589 HOU - INSPECTION FOUND FLOORBEAM CORRODED AT STATION 986.5. THE FLOORBEAM WAS REPLACED IAW SRM 53-00-51. (M) 2 L 7 2 4F RT A16WE 1996062700535 19960627 00535 NM 1996 6 27 CAL960626 1 19960430 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 950 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69351 27168 23589 HOU - INSPECTION FOUND FLOORBEAM INTERCOSTAL CORRODED AT STATION 950 BETWEEN RBL 8 AND 18. THE INTERCOSTAL WAS REPLACED IAW ECRA 5310-03258. (M) 2 L 7 2 4F RT A16WE 1996062700536 19960627 00536 NM 1996 6 27 CAL960627 1 19960430 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 950 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69351 27168 23589 HOU - INSPECTION FOUND FLOORBEAM INTERCOSTAL CORRODED AT STATION 950 BETWEEN RBL 47 AND 55. THE INTERCOSTAL WAS REPLACE D IAW ECRA 5310-03258. (M) 2 L 7 2 4F RT A16WE 1996062700537 19960627 00537 NM 1996 6 27 CAL960628 1 19960430 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 950 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69351 27168 23589 HOU - INSPECTION FOUND FLOORBEAM INTERCOSTAL CORRODED AT STATION 950 FROM LBL 17 TO 25. THE INTERCOSTAL WAS REPLACED IA W ECRA 5310-03258. (M) 2 L 7 2 4F RT A16WE 1996062700538 19960627 00538 NM 1996 6 27 CAL960629 1 19960430 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM BS 291-312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69351 27168 23589 HOU - INSPECTION FOUND FLOOR SUPPORT CORRODED BETWEEN BS 291 AND 312, 12 INCHES RIGHT OF CENTERLINE. AN INTERCOSTAL WAS FABICATED AND INSTALLED IAW ECRA 5310-03258. (M) 2 L 7 2 4F RT A16WE 1996062700539 19960627 00539 NM 1996 6 27 CAL960630 1 19960430 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM BS 312-328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69351 27168 23589 HOU - INSPECTION FOUND FLOOR SUPPORT CORRODED BETWEEN BS 312 AND 328, 12 INCHES LEFT OF CENTERLINE. AN INTERCOSTAL WAS FABRICATED AND INSTALLED IAW ECRA 5310-03258. (M) 2 L 7 2 4F RT A16WE 1996062700540 19960627 00540 NM 1996 6 27 CAL960631 1 19960430 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM BS 328-344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69351 27168 23589 HOU - INSPECTION FOUND FLOOR SUPPORT CORRODED BETWEEN BS 328 AND 344, 12 INCHES LEFT OF CENTERLINE. AN INTERCOSTAL WAS FABRICATED AND INSTALLED IAW ECRA 5310-03258. (M) 2 L 7 2 4F RT A16WE 1996062700541 19960627 00541 NM 1996 6 27 CAL960632 1 19960430 A 5320 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM BS 344-360 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69351 27168 23589 HOU - INSPECTION FOUND FLOOR SUPPORT CORRODED BETWEEN BS 344 AND 360, 14 INCHES LEFT OF CENTERLINE. AN INTERCOSTAL WAS FABRICATED AND INSTALLED IAW ECRA 5310-03258. (M0 2 L 7 2 4F RT A16WE 1996062700542 19960627 00542 NM 1996 6 27 CAL960633 1 19960430 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 950 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69351 27168 23589 HOU - INSPECTION FOUND FLOORBEAM INTERCOSTAL CORRODED AT STATION 950 BETWEEN RBL 25 AND RBL 40. AN INTERCOSTAL WAS FABR ICATED AND INSTALLED IAW ECRA 5310-03258. (M) 2 L 7 2 4F RT A16WE 1996062700543 19960627 00543 NE 1996 6 27 CAL960641 2 19960521 A 7200 447243 BEARING DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 2 ENGINE FAILED A CALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 09 69826 49486 717374 THE NR 2 ENGINE FAILED WHILE EN ROUTE FROM IAH TO TUS. A MUFFLED BANG WAS HEARD WITH THE EPR AND RPM DROPPING TO ZERO. THE AIRCRAFT WAS DIVERTED TO ELP WHERE IT LANDED WITHOUT INCIDENT. THE NR 2 ENGINE WAS REMOVED AND REPLACED. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION. SHOP TEARDOWN FINDINGS REVEALED FAILURE OF UPPER TOWER SHA FT BEARING. 2 L 7 2 4F 4 F A6WE E9NE 1996062700544 19960627 00544 NE 1996 6 27 CAL960643 2 19960523 A 7321 7436025 FUEL CONTROL BOEING 737 737130 1384435 NM PWA JT8 JT8D7 52053 NE NR 1 ENGINE INOPERATIVE A CALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 09 14212 19029 654090 FLT NR 324 - EWR - THE NR 1 ENGINE BEGAN TO SURGE SEVERELY AFTER TAKEOFF FROM EWR. ALL ENGINE GAUGES WERE SHOWING SURGE AND IT COULD BE FELT. THE ENGINE WAS NOT SHUTDOWN. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE FUEL CONTROL UNIT AT FAULT. THE NR 1 ENGINE FCU WAS REMOVED AND REPLACED. ALL ENGI NE PARAMETERS CHECKED GOOD. (M) 2 L 7 2 4F 4 F A16WE E2EA 1996062700545 19960627 00545 EU 1996 6 27 COEA9674101 1 19960603 A 5330 SKIN FOKKER F27 F27MK600 4990706 EU BS 407-581 CRACKED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 741FE 10387 FUSELAGE STATION 407 TO STATION 581 INCHES WL 30.5 BL RIGHT OML, NUMEROUS CRACKS ALONG THIS SECTION OF SKIN. THE LONGES T IS 17 INCHES. THERE ARE TWO PREVIOUS SMALL REPAIRS IN WHICH THE CRACKS PROCEEDED PAST THE REPAIR. THE ENTIRE LENGTH OF SKIN WAS REMOVED STATION 407 TO 581 STRINGER 44 TO 45 WAS REPLACED IAW FOKKER SRM 53-01-02, FIGURE 22. (M) 2 H 7 2 4T A817 1996062700546 19960627 00546 EU 1996 6 27 COEA9674102 1 19960603 A 5330 SKIN FOKKER F27 F27MK600 4990706 EU BS 407-546 CRACKED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 741FE 10387 FUSELAGE STATION 407 INCHES TO STATION 546 INCHES WL 30.5 STRINGER 44 TO 45 BL LEFT OML, NUMEROUS CRACKS ALONG THE CHINE LINE FASTENER HOLES WITH PREVIOUS REPAIRS. THE ENTIRE LENGTH OF SKIN FUSELAGE STATION 407-546 INCHES WAS REMOVED AND R EPLACED IAW FOKKER SRM 53-01-02, FIGURE 22. (M) 2 H 7 2 4T A817 1996062700547 19960627 00547 EU 1996 6 27 CXXA96BT003 1 19960529 A 3220 D227030006 DRAG BRACE AEROSP ATR42 ATR42320 8680930 EU NLG BROKEN A A C2XA O OTHER E J VIBRATION/BUFFET WARNING INDICATION AP APPROACH 1 SW 09 17810 093 EWR - ON APPROACH INTO NEWARK FLIGHT 3397 - CREW NOTED LOUD BANG, SHUDDERING AND LARGE VIBRATION DURING DESCENT. CREW D ECLARED AN EMERGENCY AND REQUESTED A PRIORITY APPROACH INTO EWR. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND BROKEN BRACKE T ON NOSE LANDING GEAR DRAG BRACE FOR LEFT FORWARD GEAR DOOR. FORWARD DOOR REMOVED. AIRCRAFT RELEASED IAW CDL 32-2 PLA CARD NR 893144. AIRCRAFT RON BTV AND NOSE GEAR DRAG BRACE ASSY WAS REMOVED AND REPLACED IAW ATR 42MM JIC 32-21-12. OPE RATIONAL AND LEAK CHECKS IAW ATR-42 MM JIC 32-31-00. RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996062700548 19960627 00548 CE 1996 6 27 GLBA96079 1 19960502 A 3230 RETRACT MECH BEECH 1900 1900C 1154161 CE LANDING GEAR MALFUNCTIONED A GLBA O OTHER J WARNING INDICATION LD LANDING 1 CE 01 167GL UC167 ORF - CREW REPORTED LANDING GEAR WOULD NOT EXTEND WHEN SELECTED DOWN. ON THE SECOND TRY, GEAR OPERATED NORMALLY. MX PE RFORMED SEVERAL GEAR RETRACTIONS AFTER INSPECTING SYSTEM BUT COULD NOT DUPLICATE DISCREPANCY. (M) 2 L 7 2 4T RT A24CE 1996062700549 19960627 00549 SO 1996 6 27 GLBA96081 1 19960506 A 3233 1959500007 ACTUATOR EMB 120 EMB120RT SO RT MLG MALFUNCTIONED A GLBA O OTHER J WARNING INDICATION CL CLIMB 1 CE 01 129AM 294 120119 RDU - CREW REPORTED, THE RIGHT MAIN GEAR TOOK APPROX 25 SECONDS TO RETRACT WHEN SELECTED UP. MAINTENANCE REMOVED AND RE PLACED THE RIGHT MAIN GEAR ACTUATOR. LEAK AND OPS CHECKS WERE GOOD. (M) 2 L 7 2 4T RT A31SO 1996062700550 19960627 00550 CE 1996 6 27 GLBA96083 1 19960506 A 3230 1013880083 SERVICE VALVE BEECH 1900 1900C 1154161 CE LANDING GEAR MALFUNCTIONED A GLBA O OTHER J WARNING INDICATION LD LANDING 1 CE 01 159GL 1519 UC159 CIU - CREW REPORTED, THE LANDING GEAR FAILED TO EXTEND WHEN SELECTED DOWN. A MANUAL GEAR EXTENTION WAS PERFORMED AND AN UNEVENTFUL LANDING WAS MADE. MX REMOVED AND REPLACED SERVICE VALVE BECAUSE OF AN INTERMITTENT MICROSWITCH. OPS CHECK WAS GOOD. (M) 2 L 7 2 4T RT A24CE 1996062700551 19960627 00551 CE 1996 6 27 GLBA96085 1 19960509 A 3297 WIRE BEECH 1900 1900C 1154161 CE GEAR WARNING CHAFED A GLBA O OTHER N FALSE WARNING CR CRUISE 1 CE 01 123UE UC123 DEN - CREW REPORTED, THE GEAR 'UNSAFE' LIGHT ILLUMINATED AND HORN SOUNDED WITH GEAR UP IN FLIGHT AND WITH GEAR EXTENDED. MX REPAIRED CHAFED WIRE IN ZONE 131. SYSTEM OPS CHECK WAS GOOD. (M) 2 L 7 2 4T RT A24CE 1996062700552 19960627 00552 CE 1996 6 27 GLBA96086 1 19960509 A 3260 INTRANSIT LIGHT BEECH 1900 1900C 1154161 CE LANDING GEAR ILLUMINATED A GLBA O OTHER N FALSE WARNING LD LANDING 1 CE 01 101UE UC101 MSP - CREW REPORTED, THE GEAR 'INTRANSIT' LIGHT ILLUMINATED WITH GEAR DOWN. MX INSPECTED SYSTEM AND PERFORMED NUMEROUS GEAR SWINGS BUT COULD NOT DUPLICATE DISCREPANCY ON THE GROUND OR ON TEST FLIGHT. (M) 2 L 7 2 4T RT A24CE 1996062700553 19960627 00553 WP 1996 6 27 GRAA9630 1 19960512 A 3350 LIGHTS DOUG DC9 DC987 3022087 WP CABIN INOPERATIVE A GRAA K NONE L NO TEST IN INSP/MAINT 1 WP 11 1074T 49727 LINE MAINTENANCE AT ENV, DISCOVERED THAT THE EMERGENCY FLOOR TRACK LIGHTS AT ROW 18 WAS INOP AND MISSING ONE RED LENS. M AINTENANCE RELAMPED AND REPLACED THE MISSING RED LENS. MAINTENANCE PERFORMED AND OPERATIONAL CHECK OF THE EMERGENCY LIG HT SYSTEM. NO DEFECTS WERE NOTED. SYSTEM CHECKED NORMAL. AIRCRAFT WAS RETURNED TO SERVICED. (M) 2 L 7 2 4F RT A6WE 1996062700554 19960627 00554 WP 1996 6 27 HALA9674 1 19960608 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 674MC 47735 HNL - FLT 502 - ON PREFLIGHT, FOUND EMERGNCY LIGHTS IN COCKPIT AND FORWARD AISLE WERE INOP. REPLACED BATTERIES. OPS CH ECK GOOD. (M) 2 L 7 2 4F A6WE 1996062700555 19960627 00555 NM 1996 6 27 HNAA9691036 1 19960603 A 3350 6013211X BATTERY PACK DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 910HA 022 FLT 3040 - FLL-TPA - DURING PREFLIGHT CHECKS, FOUND THE EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY P ACK. (M) 2 H 7 2 4T RT A13NM 1996062700556 19960627 00556 NM 1996 6 27 HNAA9693535 1 19960601 A 3350 40005130003 SWITCH DHAV DHC8 DHC8102 2809003 NM F/A PANEL FAILED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 935HA 19901 142 FLT 3040 - FLL-TPA - DURING PREFLIGHT CHECKS, FOUND THE INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOP. MX FREED THE FLIGH T ATTENDANTS EMERGENCY LIGHT SWITCH. AT RON, THE FLIGHT ATTENDANTS EMERGENCY LIGHT SWITCH WAS REPLACED. (M) 2 H 7 2 4T RT A13NM 1996062700557 19960627 00557 EU 1996 6 27 M3HA96015 1 19960604 A 3397 WIRE AEROSP ATR42 ATR42300 8680920 EU CABIN BROKEN A M3HA K NONE L NO TEST IN INSP/MAINT 1 WP 13 4208G 086 HNL - DURING PREFLIGHT, EMERGENCY EXIT LIGHT CABIN DOOR AND SERVICE DOOR INOP. FOUND WIRING ON SERVICE DOOR EXIT LIGHT BROKEN, REPAIRED AS NECESSARY. WIRING ON EXIT LIGHT ON CABIN DOOR, BROKEN. REPAIRED AS NECESSARY. OPS CHECK GOOD, OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 1996062700558 19960627 00558 SW 1996 6 27 MALA965003 1 19960522 A 3260 INTRANSIT LIGHT SWRNGN SA227 SA227AC 8780603 SW LT MLG FAILED A MALA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 15 27465 AC755B FLT 3135 - ON APPROACH TO MSP, THE LEFT GEAR INTRANSIT LIGHT FAILED TO ILLUMINATE. ALL OTHER INDICATIONS WERE NORMAL. M AINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. THE GEAR POSITION SWITCHES WERE CLEANED AND LUBED. ALL CHECKS SATI SFACTORY. (M) 2 L 7 2 4T RT A8SW 1996062700559 19960627 00559 EU 1996 6 27 PLG51796G1 1 19960517 A 2450 A2042C PDU SAAB SF340 SF340A 7850100 EU LEFT FAILED A PLGA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 NE 05 743BA 351 CJ58182 340A093 FLT 4626 - LGA-BTV - IN CRUISE THE LEFT MAIN BUS AND LEFT AVIONICS BUS FAILED. THE AIRCRAFT DIVERTED TO ALB. THE CREW HAD TO PUMP THE GEAR DOWN DUE TO THE BUS FAILURE, LANDING WITHOUT INCIDENT. ALB MAINTENANCE REMOVED AND REPLACED THE LE FT HAND POWER DISTRIBUTION UNIT AND RETURNED THE AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1996062700569 19960627 00569 WP 1996 6 27 RAIA960531 2 19960523 A 7320 1379287L405 P3 LINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RT ENGINE LEAKING A A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 337TE 8831 929 P66131 JLN - FLT 7026 - RIGHT ENGINE DID NOT MAKE TARGET TORQUE. MAINTENACNE REPLACED RT P3 LINE. PERFORMED GROUND RUNS, OPS CHECK GOOD. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996062700570 19960627 00570 1996 6 27 RAIA960532 4 19960524 A 3442 MI585353 ANTENNA DRIVE AEROSP ATR42 ATR42300 8680920 EU RADAR INOP A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 424TE 9669 124 STL - FLT 7176 - WEATHER RADAR HAS SOLID RED BAND BLOCKING PICTURE. REMOVED AND REPLACED RADAR ANTENNA DRIVE. (M) 2 H 7 2 4T RT A53EU 1996062700571 19960627 00571 WP 1996 6 27 RAIA960533 2 19960524 A 7530 8961153 GASKET BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP NR 2 ENG LEAKING A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 431AM 7219 881 66317 STL - FLT 7282 - NR 2 ENGINE BETA LIGHT ILLUMINATED ON TAKEOFF ROLL. REMOVED AND REPLACED BLEED AIR GASKET. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996062700572 19960627 00572 EU 1996 6 27 RAIA960534 1 19960527 A 6120 6345039001 RESTRICTOR BAG JETSTM JETSTM3201 1500217 EU NR 2 ENGINE DIRTY A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 339TE 10684 935 COU - FLT 7030 - NR 2 BETA LIGHT ILLUMINATED ON TAKEOFF. REMOVED CLEANED AND REINSTALLED BETA SWITCH RESTRICTOR. (M) 2 L 7 2 4T RT A56EU 1996062700573 19960627 00573 1996 6 27 RAIA960535 4 19960529 A 6122 89741016 PROP GOVERNOR BAG JETSTM JETSTM3201 1500217 EU NR 2 ENG FAILED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 428AM 7312 877 STL - FLT 7092 - NR 2 ENGINE WOULD NOT PRODUCE REQUIRED TORQUE. REMOVED AND REPLACED PROP GOVERNOR. (M) 2 L 7 2 4T RT A56EU 1996062700574 19960627 00574 EU 1996 6 27 REXA96016 1 19960522 A 2121 EVCTA465 RECIR FAN SAAB SF340 SF340A 7850100 EU RT COCKPIT FAILED A REXA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 25 327PX 1966 802 340A059 INBOUND TO INL, PILOT REPORTED SMOKE IN COCKPIT. MECHANIC FOUND RIGHT RECIRCULATIN AT FAULT, AND DEFERRED IT PER MEL 5/ 20/96. REMOVED AND REPLACED RIGHT RECIRCULATION FAN IAW SAAB AMM 21-22-10. OPS CHECK GOOD 5/22/96. (M) 2 L 7 2 4T RT A52EU 1996062700575 19960627 00575 EU 1996 6 27 REXA96017 1 19960523 A 3240 140041 TRANSDUCER SAAB SF340 SF340A 7850100 EU LT MLG BRAKE INOP A REXA K NONE O OTHER LD LANDING 1 SO 25 344AM 266 340A030 ANTI-SKID LIGHT ON SHORTLY AFTER TOUCHDOWN, NO BRAKING ACTION WHEN BRAKES ARE APPLIED. PUT PUMP IN OVERRIDE TO GET BRAK ING ACTION. REMOVED LEFT OUTBOARD WHEEL SPEED TRANSDUCER IAW AMM. PERFORMED A HIGH SPEED RUN/TAXI. OPS CHECK GOOD. A IRCRAFT FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1996062700576 19960627 00576 EU 1996 6 27 REXA96019 1 19960526 A 2611 CONNECTOR SAAB SF340 340B 7860101 EU CARGO COMPT DISCONNECTED A REXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 360PX 13822 340B220 PASSING THROUGH 400 FEET, ON CLIMB-OUT, BOTH AVIONICS AND CARGO SMOKE LIGHTS CAME ON. FOUND CARGO HOOKED TO CARGO SMOKE DETECTOR WIRING HARNESS. UNHOOKED CARGO NET. RETERMINATED CANNON PLUG AND RESECURED. GROUND RUNS AND OPS CHECK GOOD. OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1996062700577 19960627 00577 EU 1996 6 27 SIMA961421 1 19960521 A 2752 NAS16126 O-RING AEROSP ATR72 ATR72212 EU RT TE FLAP ACT FAILED A SIMA K NONE J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SW 21 414WF 414 HOU - FLT 3545 - BLUE SYSTEM HYD LOW LEVEL INDICATION, CRUISE FLIGHT. FOUND FLUID LEAKING ON RIGHT OUTBOARD FLAP ACTUAT OR. REPLACED O-RING ON FLAP ACTUATOR AND SERVICE RESERVOIR, OPS AND LEAK CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVIC E. (M) 2 H 7 2 4T RT A53EU 1996062700578 19960627 00578 EU 1996 6 27 SIMA961422 1 19960521 A 3350 3011210 LIGHT AEROSP ATR72 ATR72212 EU AIRSTAIR FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 448AM 1144 448 RAI'D LIGHT ASSY OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996062700579 19960627 00579 EU 1996 6 27 SIMA961441 1 19960523 A 3350 30012000 POWER SUPPLY AEROSP ATR72 ATR72202 8680940 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 252AM 461 253 ORD - FLT 4001 - FORWARD CABIN FLOOR EMERGENCY LIGHTING INOP. REPLACED EMERGENCY LIGHTING POWER SUPPLY. AIRCRAFT WAS R ETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996062700580 19960627 00580 EU 1996 6 27 SIMA961471 1 19960526 A 3350 3011160 LIGHT AEROSP ATR72 ATR72212 EU SERVICE DOOR FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 447AM 447 ORD - FLT 4132 - RAI LIGHT ASSEMBLY. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996062700581 19960627 00581 EU 1996 6 27 SIMA961581 1 19960606 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 274AT 307 274 LAN - FLT 4371 - FORWARD EMERGENCY LIGHTS INOP. RAI POWER SUPPLY 6WL. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996062700582 19960627 00582 EU 1996 6 27 SIMA961631 1 19960611 A 3350 3011210 LIGHT AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 242AT 242 DFW - FLT 3610 - REMOVED AND REPLACED LIGHT SOCKET ASSY. OPS CHECK GOOD. AIRCRFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996062700583 19960627 00583 NM 1996 6 27 TSAA9653037 1 19960606 A 5320 SHEAR BEAM BOEING 737 7372S5C 1384499 NM BS 727 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 802AL 22148 DURING SCHEDULED INSPECTION AT STRINGER 18A SHEAR BEAM (REF AD 93-08-04 AMDT 39-8551), FOUND LEFT BS 727 STRINGER 18A SH EAR BEAM CRACKED APPROX 2 INCHES IN LENGTH. REPAIRED PER ECO 1732R4 PART III STEP E PER DRAWING 65C29228 WITH KIT 65C29 228 3. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1996062700584 19960627 00584 NE 1996 6 27 TWRA9632 2 19960530 A 7200 ENGINE BOEING 747 747282B 1384860 NM PWA JT9 JT9D7A 52054 NE LEFT MALFUNCTIONED A TWRA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 15 611FF 20502 663020 ON APPROACH AND DURING TAXI IN TO PARKING SPOT, A SMELL OF SMOKE WAS DETECTED COCKPIT GALLEY POWER WAS OFF SMELL MOSTLY CAME FROM CAPTAINS SIDE (EYEBALL VENTS). NR 2 ENGINE WAS REPLACED AND R/U CHECK OK, ALL 3 PACKS WERE RUN. OPS CHECK OK . NO SMOKE IN COCKPIT OR CABIN. (M) 2 L 7 4 4F 4 F A20WE E20EA 1996062700585 19960627 00585 NM 1996 6 27 TWRA9633 1 19960531 A 3340 8906K15597100 SWITCH BOEING 747 747282B 1384860 NM COCKPIT SHORTED A TWRA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 15 611FF 20502 ON APPROACH, ELECTRICAL BURNING SMELL WAS NOTICED IN COCKPIT AFTER LEFT OUTBOARD LANDING LIGHT WAS TURNED ON DURING TAXI , LIGHT COULD NOT BE TURNED OFF WITH SWITCH. INSPECTED AREA AND FOUND SWITCH SHORTED AND FIRST INCH OF WIRE TO SWITCH B URNED. CIRCUIT BREAKER ON P6 PULLED AND COLLARED MEL 33-8-C. ON 6/2/96 THE SWITCH WAS REPLACED AND WIRE REPAIRED. OPS CHECK OF LANDING LIGHTS OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 4 4F A20WE 1996062700586 19960627 00586 NM 1996 6 27 USAA960450 1 19960525 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 986.5 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 279AU 35210 22891 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORRODED AREA BS 986.5 FLOOR BEAM T-CAP 44 INCH LBL. I NSTALLED STRAP REPAIR, REPAIRED PER TR 53-10-01A. (M) 2 L 7 2 4F A16WE 1996062700587 19960627 00587 NM 1996 6 27 USAA960451 1 19960525 A 5210 WEB BOEING 737 7372B7 1384560 NM AFT ENTRY DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 279AU 35210 22891 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK AFT ENTRY DOOR 3RD STOP FROM BOTTOM AFT END WEB. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-3. (M) 2 L 7 2 4F A16WE 1996062700588 19960627 00588 NM 1996 6 27 USAA960452 1 19960525 A 5230 CARGO DOOR BOEING 737 7372B7 1384560 NM BS 807 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 279AU 35210 22891 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCH DENT BS 807 STRINGER 20R SKIN ON CARGO DOOR. INSTALLED DOUBLER R EPAIRED PER SRM 52-00-3. (M) 2 L 7 2 4F A16WE 1996062700589 19960627 00589 NM 1996 6 27 USAA960456 1 19960525 A 5313 STRINGER BOEING 737 7372B7 1384560 NM BS 948 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 279AU 35210 22891 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 10 INCH CORRODED AREA STRINGER 27L BS 948. CUT OUT CORRODED SECTION OF STRINGER FABRICATED NEW SECTION AND SPLICED BACK IN, REPAIRED PER SRM 53-10-3. (M) 2 L 7 2 4F A16WE 1996062700590 19960627 00590 NM 1996 6 27 USAA960457 1 19960525 A 5313 STRINGER BOEING 737 7372B7 1384560 NM BS 967-987 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 279AU 35210 22891 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 9 INCH CORRODED AREA AFT CARGO BS 967-987 STRINGER 25L. INSTA LLED STRINGER SPLICE AND REPAIRED PER SRM 53-10-3. (M) 2 L 7 2 4F A16WE 1996062700591 19960627 00591 NM 1996 6 27 USAA960463 1 19960525 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 877 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 279AU 35210 22891 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND TWO 3 INCH DIAMETER DENTS IN EXT FUSELAGE SKIN BS 877-STRINGER 18R. INS TALLED DOUBLER, REPAIRED PER SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1996062700592 19960627 00592 NM 1996 6 27 USAA960465 1 19960528 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727A CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 223US 47251 21665 ROA - DURING 'A' CHECK VISUAL INSPECTION, FOUND 2 CRACKS .875 INCH AND .125 INCH IN LENGTH AT FUSELAGE SKIN AT STRINGER 16L BS 727A. CONTAINED CRACKS AND INSTALLED DOUBLER, REPARIED PER SRM 53-30-3 FIG 1. (M) 2 L 7 2 4F A16WE 1996062700593 19960627 00593 NM 1996 6 27 USAA960467 1 19960601 A 5330 SKIN BOEING 737 737201 1384454 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 228US 44842 21817 ROA - DURING 'TRANSIT CHECK' VISUAL INSPECTION VERIFIED WITH HFEC, FOUND TWO .75 INCH CRACK IN FUSELAGE SKIN JUST ABOVE STRINGER 18L, FORWARD OF BS 787. INSTALLED DOUBLER REPAIR, REPAIRED PER SRM 53-30-3 FIG 6. (M) 2 L 7 2 4F A16WE 1996062700594 19960627 00594 NM 1996 6 27 USAA960468 1 19960601 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 986.5 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 228US 44842 21817 ROA - DURING 'BX TRANSIT' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 3 INCH CORROSION STRINGER 27L BS 986.5. INSTALLED DO UBLER AND STRINGER, REPAIRED PER SRM 53-10-3. (M) 2 L 7 2 4F A16WE 1996062700595 19960627 00595 WP 1996 6 27 USAAD96072 1 19960607 A 3350 41B030CF00101 BATTERY PACK DOUG DC9 DC931 3022065 WP LT NACELLE DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 983VJ 48159 LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK. (M) 2 L 7 2 4F A6WE 1996062700596 19960627 00596 WP 1996 6 27 USAAD96073 1 19960608 A 2421 COOLING SCREEN DOUG DC9 DC982 3022082 WP APU DIRTY A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 817US 48097 FLT 985 - BDL-TPA - WITH RIGHT GENERATOR ON MEL AND APU RUNNING FOR ELECTRICAL POWER, GOT APU OIL TEMP HI CAUTION LIGHT AT FL 350. DESCENDED TO FL 250, AND LIGHT WENT OUT. FLIGHT DIVERTED TO CLT DUE TO FUEL AND WEATHER CONSIDERATIONS AT N EW ALTITUDE. FOUND COOLING PLENUM SCREEN PLUGGED. CLEANED SCREEN. CHECKS GOOD. (M)` 2 L 7 2 4F A6WE 1996062700597 19960627 00597 WP 1996 6 27 USAAD96074 1 19960609 A 2130 1500P0228 SWITCH DOUG DC9 DC981 3022081 WP CABIN FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 805US 48053 FLT NR 8004 - FLL-PHL - AIRCRAFT FERRY FROM FLL-PHL, WOULD NOT PRESSURIZE. DIVERTED TO MCO. REPLACED BLOWN COUPLING AT RIGHT CAU. REPLACED BOTH SECOND SEGMENT CLIMB SWITCHES. CLEANED SENSE LINES AT BOTH AUGMENTATION VALVES. (M) 2 L 7 2 4F A6WE 1996062700598 19960627 00598 EU 1996 6 27 USAAF96051 1 19960522 A 5230 D28630003 DOOR SEAL FOKKER F28 F28MK0100 4990807 EU FWD CARGO DOOR FAILED A USAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 19 869US 11314 PHL - FLT 328 - CREW LOST PRESSURIZATION AT 33,OOO FEET. CREW DESCENDED TO 10,000 FEET. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE FORWARD CARGO DOOR SEAL LEAKING. THE DOOR SEAL WAS REPLACED. AIRCRAFT WAS PRESSURIZED WITH LEAK RATE CHECKING OK AND DOOR CHECKING OK. (M) 2 L 7 2 4F RT 1996062700599 19960627 00599 EU 1996 6 27 USAAF96054 1 19960607 A 3350 6104781 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 862US 11300 BOTH LAVATORY EMERGENCY LIGHTS INOP. REPLACED NR 8 BATTERY PACK. (M) 2 L 7 2 4F RT 1996062700600 19960627 00600 EU 1996 6 27 USAAF96055 1 19960607 A 3350 D42153 INVERTER FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 881US 11333 FIRST CLASS FLOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED INVERTER. (M) 2 L 7 2 4F RT 1996062700601 19960627 00601 EU 1996 6 27 USAAF96056 1 19960609 A 3350 59177 EXIT SIGN FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 481US 11230 FORWARD CABIN EMERGENCY EXIT SIGN INOPERATIVE. REPLACED EMERGENCY EXIT SIGN. (M) 2 L 7 2 4F RT A20EU 1996062700602 19960627 00602 EU 1996 6 27 USAAF96057 1 19960607 A 7830 1159SCP4099 T/R CABLES FOKKER F28 F28MK0100 4990807 EU NR 1 ENGINE BROKEN A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 893US 11373 PIT - FLT 1672 - CREW COULD NOT ADVANCE THROTTLES PAST 34 UNITS DURING CLIMB. FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT. MX FOUND THE NR 1 THRUST REVERSER FEEDBACK CABLES FROZEN AND BROKEN. CABLES WERE REPLACED. (M) 2 L 7 2 4F RT 1996062700603 19960627 00603 NE 1996 6 27 USAASB96092 2 19960527 A 7200 ENGINE BOEING 737 737201 1384454 NM PWA JT8 JT8D15 52051 NE LEFT FAILED A A USAA E ENGINE SHUTDOWN E M VIBRATION/BUFFET OVER TEMP DE DESCENT 1 EA 19 254AU 37955 22796 700282 PHL - FL 945 - DESCENDING FROM 20,000 FEET, NR 1 ENGINE BEGAN BANGING SEVERELY. CREW REDUCED POWER, PARAMETERS LOOKED G OOD. CREW THEN ADVANCED POWER, BANGING RETURNED. AS POWER WAS REDUCED TO IDLE, EGT CLIMBED TO RED. NR 1 ENGINE WAS SH UT DOWN IN FLT. TOTAL SINGLE ENGINE TIME WAS 15 MINUTES. MAINTENANCE REPLACED THE NR 1 ENGINE ASSY PER JOB CARD. OPER ATIONAL CHECK AND LEAK CHECK NORMAL. (M) 2 L 7 2 4F 4 F A16WE E2EA 1996062700604 19960627 00604 NM 1996 6 27 USAASB96094 1 19960530 A 2131 7638102 CONTROLLER BOEING 737 7372B7 1384560 NM CABIN MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 271AU 22883 PIT - FLT 1297 - AT 31,000 FEET, CREW RECEIVED A PRESSURIZATION WARNING HORN ON THE AUTOMATIC SYSTEM. CREW SWITCHED TO MANUAL PRESSURIZATION CONTROL AND DESCENDED TO 10,000 FEET. NO EMERGENCY WAS DECLARED. FLIGHT RETURNED TO FIELD AND LA NDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE CABIN PRESSURIZATION CONTROLLER (P/N 7638102) AND THE AFT CABIN PRESSURIZATION OUTFLOW VALVE (P/N 7110033). OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1996062700605 19960627 00605 NE 1996 6 27 USAASB96095 2 19960530 A 7230 ENGINE BOEING 737 7372B7 1384560 NM PWA JT8 JT8D15A 52051 NE RIGHT BIRD STRIKE A USAA A UNSCHED LANDING C F.O.D. CL CLIMB 1 EA 19 266AU 22878 MCI - FL 800 - FLIGHT WAS CLIMBING OUT OF MCI WHEN THE A/C STRUCK A DUCK AT 3,500 FEET WITH THE RIGHT ENGINE. FLIGHT RE TURNED TO FIELD AS A PRECAUTIONARY MEASURE. ALL ENGINE INDICATIONS WERE NORMAL. NO EMERGENCY WAS DECLARED AND THE FLIG HT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE INSPECTED AIRCRAFT PER MM 5-51-201 (BIRD STRIKE INSPECTION). FOUND THR EE N1 FAN BLADES NICKED AND BENT ON NR 2 ENGINE. DRESSED AFFECTED BLADES PER PW MM 72-00. (M) 2 L 7 2 4F 4 F A16WE E2EA 1996062700606 19960627 00606 NM 1996 6 27 USAASB96097 1 19960601 A 2781 189915 SENSOR BOEING 737 7372B7 1384560 NM RT WING LE FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 281AU 23114 PIT - FLT 1898 - AT APPROXIMATELY 8,000 FEET, THE NR 4 LE SLAT GREEN LIGHT CYCLED ON AND OFF AFTER FLAPS WERE RETRACTED. CREW RECYCLED FLAPS WITH NO CHANGE. CAPTAIN DECIDED TO RETURN TO FIELD. FLT LANDED IN PIT WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 4 LE SLAT MID EXTEND SENSOR. OPS CHECK OF LE INDICATION TESTED GOOD. (M) 2 L 7 2 4F A16WE 1996062700607 19960627 00607 NM 1996 6 27 USAASB96101 1 19960605 A 3230 BACR13CG2AB R278 RELAY BOEING 737 737301 1384611 NM E/E COMPT MALFUNCTIONED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 589US 23934 CLT - FL 1405 - CREW COULD NOT RAISE GEAR USING NORMAL PROCEDURES. ALTERNATE PROCEDURES WORKED, HOWEVER, THE TAKEOFF WA RNING HORN SOUNDED. FLIGHT RETURNED TO CLT AND LANDED WITH NO FURHTER INCIDENT. MAINTENANCE REPLACED THE R432 AND R276 RELAYS AND PERFORMED A GEAR SWING. (M) 2 L 7 2 4F RT A16WE 1996062700608 19960627 00608 NM 1996 6 27 USAASB96102 1 19960610 A 3350 AD20131A BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 427US 24549 PHL - MX FOUND SECTION OF EMERGENCY LIGHTING INOP. MX REPLACED THE NR 8 BATTERY PACK. (M) 2 L 7 2 4F RT A16WE 1996062700609 19960627 00609 EU 1996 6 27 VTZA96202 1 19960524 A 5270 91SE16 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAG DOOR OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 303UE 41015 FLT NR 6477 - IAD-CHS - ABORTED THE TAKEOFF DUE TO THE BAG DOOR CAP ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FUR THER INCIDENTS. MAINTENANCE DEFERRED BAG DOOR LIGHT (DMI 18532, MEL 52-3, CATC). AIRCRAFT WAS RELEASED AND APPROVED FO R RETURN TO SERVICE. MAINTENANCE LATER CLEARED DMI NR 18532 ON 5-29-96 BY CLEANING AND ADJUSTING THE MICROSWITCH. AIRC RAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996062700610 19960627 00610 EU 1996 6 27 VTZA96210 1 19960603 A 5246 14153133501 LAV SERVICE DOOR JETAIR JETSTM JETSTM4101 1500501 EU LT REAR FUSELAGE MISSING A A VTZA K NONE D INFLIGHT SEPARATION CR CRUISE 1 EA 27 325UE 41063 FLT NR 6539 - BOS-EWR - DURING PREFLIGHT WALKAROUND, DISCOVERED THAT THE LAVATORY SERVICE DOOR WAS MISSING. MX OPENED D MI NR 17779 IAW MEL 52-4. MX LATER CLEARED DMI NR 17779 ON 6-7-96 BY REPLACING THE LAV SERVICE DOOR. AIRCRAFT WAS RELE ASED AND APPROVED FOR RETURN TO SERVICE. SUBMITTER STATES, THIS IS THE 10TH DOOR SEPARATION. AD IS RECOMMENDED. (M) 2 L 7 2 4T RT A41NM 1996062700611 19960627 00611 EU 1996 6 27 VTZA96212 1 19960603 A 5270 WARNING LIGHT BAG JETSTM JETSTM3201 1500217 EU PAX DOOR ILLUMINATED A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 491UE 911 FLT 6351 - IAD-SWF - DURING CRUISE, DIVERTED TO AVP DUE TO THE PAX DOOR WARNING LIGHT ILLUMINATING DURING TURBULANCE. A IRCRAFT LANDED AT AVP WITH NO FURTHER INCIDENTS. MX PERFORMED INSPECTIONS AND ALL OPS CHECKS WERE GOOD. AIRCRAFT WAS R ELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996062700612 19960627 00612 WP 1996 6 27 VTZA96214 2 19960606 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LEFT POWER LOSS A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J R WARNING INDICATION PARTIAL RPM/PWR LOSS TO TAKEOFF 1 EA 27 493UE 805 P66016 FLT NR 6363 - LYH-IAD - ABORTED THE TAKEOFF DUE TO THE LEFT ENGINE TORQUE ROLLING BACK. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MX PERFORMED CHECKS BUT COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996062700613 19960627 00613 EU 1996 6 27 VTZA96215 1 19960607 A 7600 21188406 IEC COMPUTER JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT MALFUNCTIONED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 305UE 41019 FLT 6294 - EWR-IAD - ABORTED TAKEOFF DUE TO IEC LIGHT. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MX RESET I EC. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996062700614 19960627 00614 1996 6 27 VTZA96216 3 19960607 A 6140 14191003 BETA PRESS SW JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE FAILURE A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 315UE 41033 FLT NR 6271 - RIC-IAD - DURING TAKEOFF, HAD THE RIGHT ENGINE (RED) BETA LIGHT ON WITH POWER LEVER FORWARD. AIRCRAFT LAN DED AND RETURNED TO GATE WITH NO FURTHER INCIDENTS. MX REMOVED AND REPLACED PRESSURE SWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996062700615 19960627 00615 EU 1996 6 27 VTZA96217 1 19960607 A 2611 7211121100 SMOKE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU BAGGAGE POD FAILED A VTZA K NONE N FALSE WARNING DE DESCENT 1 EA 27 318UE 41041 FLT NR 6265 - IAD-BTV - DURING APPROACH, MADE A SCHEDULED LANDING BUT HAD THE POD SMOKE LIGHT ON DESCENT. AIRCRAFT LAND ED WITH NO FURTHER INCIDENTS. MX OPENED DMI 210004 ON LOG PAGE 832331. MX LATER CLEARED DMI KNR21004 ON 6/7/96 BY REPL ACING THE POD SMOKE DETECTOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996062700616 19960627 00616 EU 1996 6 27 VTZA96218 1 19960608 A 5240 GPU DOOR JETAIR JETSTM JETSTM4101 1500501 EU FUSELAGE NOT CLOSED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 325UE 41063 FLT NR 6270 - IAD-EWR - ABORTED TAKEOFF DUE TO GPU ACCESS DOOR LIGHT. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDEN T. MX INSPECTED AND CLOSED GPU ACCESS DOOR. AIRCRAFT WAS RELEASED AND APPROVED FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1996062700617 19960627 00617 EU 1996 6 27 VTZA96219 1 19960609 A 3150 TO WARNING JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT ACTIVATED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 306UE 41020 FLT NR 6433 - IAD-EWR - ABORTED TAKEOFF DUE TO THE TAKEOFF CONFIGURATION WARNING SYSTEM ACTIVATING DURING THE TAKEOFF RO LL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MX PERFORMED OPS CHECKS, BUT COULD NOT DUPLICATE DISCREPANCIE S. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996062700618 19960627 00618 EU 1996 6 27 VTZA96220 1 19960610 A 2611 7211121100 SMOKE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU BAGGAGE BAY MALFUNCTIONED A VTZA K NONE N FALSE WARNING LD LANDING 1 EA 27 324UE 41017 FLT 6203 - IAD-MHT - DURING APPROACH, AN EMERGENCY WAS DECLARED DUE TO THE BAGGAGE POD SMOKE WARNING LIGHT ILLUMINATING. A/C COMPLETED LANDING WITH NO FURTHER INCIDENTS. FLT CREW EVACUATED CREW ON RUNWAY. CREW, PASSENGERS AND FIRE DEPART MENT NOTICED AN ELECTRICAL SMELL FROM THE COCKPIT/CABIN, BUT NO VISIBLE SMOKE. FIRE DEPARTMENT DISCONNECTED BATTERIES A ND A/C WAS TOWED TO THE GATE. ON CALL MAINTENANCE INSPECTED ELECTRICAL BAY, PDU'S BATTERIES AND OPS CHECKED ALL ELECTRI CAL SYSTEMS, RAN A/C. COULD NOT FIND ANY PROBLEMS. SENT IAD MECHANIC TO MHT. CHECKED ALL SYSTEMS AGAIN AND REPLACED T HE POD SMOKE DETECTOR AS A PRECAUTION. A/C WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996062700619 19960627 00619 SO 1996 6 27 WTAA960109 1 19960502 A 5610 WINDSHIELD EMB 120 EMB120RT SO RT COCKPIT BIRDSTRIKE A WTAA O OTHER C F.O.D. NR NOT REPORTED 1 WP 17 454UE 120155 LAX - BIRD STRIKE REPORTED ON FIRST OFFICERS WINDSHIELD. MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECTION, NO DAMAGE NOT ED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996062700620 19960627 00620 SO 1996 6 27 WTAA960111 1 19960529 A 3260 6839 BULB EMB 120 EMB120RT SO NLG IND FAILED A WTAA L ABORTED APPROACH N FALSE WARNING NR NOT REPORTED 1 WP 17 216YV 120216 LAX - NOSE LANDING GEAR DOWN AND LOCK 'GREEN' INDICATION DID NOT ILLUMINATE. MX REPLACED 4 BULBS. INDICATION NORMAL DU RING GROUND CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996062700621 19960627 00621 SO 1996 6 27 WTAA960114 1 19960530 A 7312 10718F FUEL HEATER EMB 120 EMB120RT SO PWA 118 PW118 NE NR 2 ENG FAILED A WTAA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 17 120AM 120012 RDD - RIGHT ENGINE OIL LIGHT ILLUMINATED IN FLIGHT. CREW SECURED NR 2 ENGINE AND DECLARED AN EMERGENCY. AIRCRAFT LANDE D WITHOUT INCIDENT. MX SUSPECTS POSSIBLE INTERNAL LEAKAGE IN FUEL/OIL HEATER. MX REPLACED FUEL/OIL HEATER. OIL QUANTI TY AND PRESSURES NORMAL DURING ENGINE GROUND RUN. NO LEAKS DETECTED. AIRCRAFT RELEASED FOR TEST FLIGHT. SUBSEQUENT TE ST FLIGHT NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1996062700622 19960627 00622 WP 1996 6 27 WTAA960115 2 19960601 A 7200 ENGINE BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110U 01514 WP LEFT MALFUNCTIONED A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 17 430UE 784 P63184 FAT - LEFT ENGINE WOULD NOT MAKE RATED POWER, DROPPED TO 80 PERCENT ON TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MX REPLACED LEFT ENGINE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A21EU E4WE 1996062700623 19960627 00623 EU 1996 6 27 WTAA960119 1 19960603 A 5730 SKIN BAG JETSTM JETSTM3101 1500215 EU LT WING BIRDSTRIKE A WTAA O OTHER C F.O.D. NR NOT REPORTED 1 WP 17 401UE 729 LAX - CREW REPORTED, BIRD STRIKE ON LEADING EDGE OF LEFT INBOARD WING NEXT GO FUSELAGE. ACCOMPLISHED BIRD STRIKE INSPEC TION ON AIRCRAFT. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996062700624 19960627 00624 EU 1996 6 27 WTAA960529 1 19960529 A 3260 9005EN38 SWITCH BAG JETSTM JETSTM3101 1500215 EU LT MLG FAILED A WTAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 17 331CA 793 LAX - DURING CLIMB-OUT LEFT MAIN LANDING GEAR INTRANSIT LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. MX INSPECTED AND CLEANED UPLOCK MICROSWITCH. SYSTEM OPERATIONAL CHECK NORMAL DURING GEAR RETRACTION CHECK. AIRCRAFT RETURNED TO SER VICE. (M) 2 L 7 2 4T RT A21EU 1996062700625 19960627 00625 WP 1996 6 27 Y2PA96034 1 19960521 A 2150 179945022 HEAT EXCHANGER DOUG DC9 DC915F 3022037 WP CABIN COOL SYS MALFUNCTIONED A Y2PA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 197US 47154 YIP - UNSCHEDULED LANDING WHEN AIRCRAFT WOULD NOT HOLD CABIN AT 16,000 FEET WITH ONLY LEFT PACK. FLIGHT OFFICER NOTICED LACK OF PRESSURIZATION AT 4,000 FEET. MANUAL PRESSURIZATION APPEARED TO HELP BUT NOT ADEQUATE. AIRCRAFT RETURNED TO P OINT OF DEPARTURE AT YIP. THE RIGHT PACK HAD BEEN DEFERRED IAW USA JET MEL ITEM 21-1. REPAIRED NUMEROUS LEAKS IN THE C ABIN PRESSURE VESSEL AND ADJUSTED OUTFLOW VALVE, IAW DC9 MM 21-34-0, SYSTEM OPS CHECK GOOD. REMOVED AND REPLACED RIGHT PRIMARY AND SECONDARY HEAT HEAT EXCHANGERS IAW DC9 MM 21-51-5. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1996062700626 19960627 00626 EU 1996 6 27 Y2PA96035 1 19960523 A 5270 602EN16 SWITCH AMD FALC20 FALCOND 2720304 EU CARGO DOOR MALFUNCTIONED A Y2PA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 821AA 203 ELP - AIRCRAFT RETURNED TO POINT OF DEPARTURE WHEN DOOR LIGHT CAME ON IN FLIGHT AND CABIN WOULD NOT PRESSURIZE. UNSCHED ULED LANDING AT POINT OF DEPARTURE AT ELP. THE CARGO DOOR HANDLE 'CLOSED POSITION' SWITCH IS INTERMITTENT CAUSING DOOR WARNING LIGHT TO ILLUMINATE AND PREVENTING THE CABIN FROM PRESSURIZING. THE SWITCH WAS REPLACED AND RIGGED PER THE AVTE C CARGO DOOR MX MANUAL. THE AIRCRAFT WAS GROUND PRESSURIZED AND SYSTEM OPERATED NORMALLY. NO DEFECTS NOTED. THIS AN A DDITIONAL DIFFICULTY TO A PREVIOUSLY NOTED DISCREPANCY. REFERENCE MISR Y2PA-96-033. (M) 2 L 7 2 4F A7EU 1996062700685 19960627 00685 EU 1996 6 27 96ZZZX3238 1 19960515 A 6520 350A33215300 LAMINATED HINGE AEROSP AS355 AS355F1 8680810 EU T/R GR BOX YOKE BEARING FAILED A M3XA K NONE O OTHER IN INSP/MAINT 1 WP 07 911TM 69 5059 PREMATURE FAILURE OF LAMINATED TEETERING BEARING. T/R YOKE REMOVED AND REPLACED. 1 G 7 2 3U H11EU 1996062700691 19960627 00691 WP 1996 6 27 9614079178 1 19960622 A 3350 LIGHTS DOUG DC9 DC914 3022034 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 3310L 45705 DURING LINE CHECK, FOUND ESCAPE PATH LIGHTING INOPERATIVE AT ROW 5. REPLACED SOCKET, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996062700692 19960627 00692 WP 1996 6 27 9614099928 1 19960625 A 2130 10256861 CONTROLLER DOUG DC9 DC931 3022065 WP COCKPIT MALFUNCTIONED A NWAA G B O2 MASK DEPLOYED EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 01 8921E 45836 LOSS OF CABIN PRESSURIZATION OCCURRED AT 29,000 FEET. OXYGEN MASKS WERE DEPLOYED THROUGHOUT THE CABIN AND EMERGENCY DES CENT WAS MADE TO 11,000 FEET. CABIN PRESSURE WAS REGAINED AND THE AIRCRAFT CONTINUED TO DESTINATION. AN UNEVENTFUL LAN DING WAS ACCOMPLISHED IN MSP. MAINTENANCE REPLACED THE CABIN PRESSURE CONTROLLER, OPERTIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996062700693 19960627 00693 NM 1996 6 27 9614102284 1 19960625 A 2550 CARGO NET BOEING 727 727251 138408H NM CARGO DOOR OUT OF POSITION A NWAA A G B UNSCHED LANDING O2 MASK DEPLOYED EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 01 284US 21323 DURING CRUISE FLIGHT AT 32,000 FEET, AIRCRAFT HAD COMPLETE CABIN DEPRESSURIZATION. OXYGEN MASKS WERE DEPLOYED AND THE A IRCRAFT MADE AN EMERGENCY DESCENT. FLIGHT DIVERTED TO MKE AND LANDED WITHOUT INCIDENT. MKE MAINTENANCE FOUND AFT FORWA RD CARGO NET LODGED IN FORWARD CORNER OF DOOR SILL. PERFORMED VESSEL LEAK CHECK, CHECKED OK. STOWED OXYGEN MASKS, MADE VISUAL INSPECTION OF ALL AIRCRAFT COMPARTMENTS AND OUTFLOW VALVES. 2 L 7 3 4F A3WE 1996062700694 19960627 00694 NM 1996 6 27 96FDEA01172 1 19960626 A 5754 65162256A FLAP BOEING 727 727225 1384077 NM NR 4 LE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 467FE 21449 NR0078 AND 018, NR 4 K-FLAP O/B HINGE LUGS CORRODED UNDER FASTENERS. *S/D* REMOVED CORRODED NR 4 K-FLAP AND INSTALLED NEW NR 4 K-FLAP IAW FEDEX MM 27-81-1, FUNCTIONAL CHECK GOOD IAW FEDEX MM 27-81-11. 2 L 7 3 4F A3WE 1996062700695 19960627 00695 NM 1996 6 27 96FDEA01173 1 19960626 A 5320 692032922 TEAR STRAP BOEING 727 727225 1384077 NM BS 1148 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 467FE 21449 NR0156 AND 019, CORROSION (C53-113-10, -2) BETWEEN SKIN AND FRAME SHEAR TIE AT BS 1148 RBL 23 WL 154. *S/D* REPAIRED T EAR STRAP PER FEDEX SRM 53-30-04, REPAIRS FWD AND AFT SHEAR TIES PER FEDEX SRM 53-10-04. 2 L 7 3 4F A3WE 1996062700696 19960627 00696 NM 1996 6 27 96FDEA01174 1 19960626 A 5230 655714016 BEAM BOEING 727 727225 1384077 NM NR1 CARGO DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 467FE 21449 NR0402 AND 020, NR 1 CARGO DOOR LWR TRANSVERSE BEAM I/B EXTRUSION IS CORRODED BEYOND LIMITS ABOVE LWR LIGHT ASSY. *S/D* REMOVED NR 1 CARGO DOOR LOWER TRANSVERSE BEAM INBOARD, FABRICATED NEW BEAM AND INSTALLED PER FEDEX SRM 51-10-1, 51-30- 2. 2 L 7 3 4F A3WE 1996062700697 19960627 00697 WP 1996 6 27 ARWA9606035 1 19960614 A 5320 3754914501 FITTING DOUG DC8 DC863F 302198F WP FS 1220 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 AFT CARGO COMPARTMENT HAS BROKEN FITTING AT LONGERON 31R AT FS 1220. REMOVED AND REPLACED FITTING PER DC-8 SRM 51-3-0. 2 L 7 4 4F 4A25 1996062700698 19960627 00698 WP 1996 6 27 ARWA9606036 1 19960614 A 5320 97540242 FITTING DOUG DC8 DC863F 302198F WP FS 1160 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 AFT CARGO COMPARTMENT, LOWER VERTICAL STRUT CRACKED AT LONGERON 27R AT FS 1160. REMOVED AND REPLACED NEW FITTING PER DC -8 SRM 51-3-0. 2 L 7 4 4F 4A25 1996062700699 19960627 00699 WP 1996 6 27 ARWA9606037 1 19960614 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 1160-1220 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 LEVEL 2 CORROSION FOUND AT EXTERIOR UPPER SKIN C-3, UPPER DOOR JAMB, AT FS 1160 TO 1220. REMOVED CORRODED SKIN. FABRIC ATED AND TREATED DOUBLERS IAW ARROW AIR SKETCH AND DC-8 SRM 51-1-4 AND 51-1-8. INSTALLED PER DC-8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1996062700700 19960627 00700 WP 1996 6 27 ARWA9606038 1 19960614 A 5730 PLATE DOUG DC8 DC863F 302198F WP RT WINGS CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 RIGHT WING, LOWER SURFACE, PYLON LATERAL REINFORCEMENT PLATE CRACKED. REMOVED CRACKED PLATE, FABRICATED NEW DOUBLER PER DC-8 SRM 54-3-3 AND 51-1-4. TREATED AND INSTALLED PER DC-8 SRM 51-1-8, 51-1-17 AND 51-1-21. 2 L 7 4 4F 4A25 1996062700701 19960627 00701 WP 1996 6 27 ARWA9606039 1 19960614 A 5753 576174814 TRACK DOUG DC8 DC863F 302198F WP RT WING CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 RIGHT WING FLAP, NR 3 HINGE SLIDING COVER EXTERIOR TRACK IS BROKEN IN 2 PLACES. BROKEN TRACK REMOVED AND REPLACED IAW D C-8 MM 27-51-3. 2 L 7 4 4F 4A25 1996062700702 19960627 00702 WP 1996 6 27 ARWA9606040 1 19960614 A 5320 ANGLE DOUG DC8 DC863F 302198F WP FS 200 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 FORWARD CARGO COMPARTMENT HAS LEVEL 2 CORROSION ON ANGLE AT LONGERON 31R AT FS 200. REMOVED ANGLE AND FABRICATED NEW AN GLE IAW DC-8 SRM 53-4-1 AND 51-1-4. TREATED AND INSTALLED ANGLE PER DC-8 SRM 51-1-8 AND 51-1-20D. 2 L 7 4 4F 4A25 1996062700703 19960627 00703 WP 1996 6 27 ARWA9606041 1 19960614 A 5753 SKIN DOUG DC8 DC863F 302198F WP RT TE FLAP DAMAGED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 TEMPORARY REPAIR ON RIGHT WING INBOARD FLAP AT STA XW 60.000. INSTALLED PERMANENT REPAIR PER DC-8 SRM 57-2-1, FIG 2Q. W ING INBOARD FLAP PLATING CLEANED, TREATED AREA PER DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1996062700704 19960627 00704 WP 1996 6 27 ARWA9606042 1 19960614 A 5720 FILLET DOUG DC8 DC863F 302198F WP WS 289 BROKEN A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 RIGHT WING UPPER SURFACE TRAILING EDGE HAS BROKEN FILLET AT STA XRS 289.000. FABRICATED FILLET IAW DC-8 SRM 57-3-3 AND 51-1-4. REMOVED AND REPLACED FILLET IAW DC-8 SRM 51-1-15. 2 L 7 4 4F 4A25 1996062700705 19960627 00705 WP 1996 6 27 ARWA9606043 1 19960614 A 7830 ANGLE DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 3 ENGINE CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 NR 3 ENGINE TRANSLATING RING UPPER ANGLE CRACKED. REPAIRED IAW DRAWING ARW 015713-1184 FAA FORM 8110 APPROVED. 2 L 7 4 4F 4 F 4A25 1E8 1996062700706 19960627 00706 WP 1996 6 27 ARWA9606044 1 19960614 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 55 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 EXTERIOR FUSELAGE HAS 1 CRACK AT LONGERON 33R STA 55, C3 DOOR. REPAIRED AREA PER DRAWING ARW 015713-0315, DER APPROVED. 2 L 7 4 4F 4A25 1996062700707 19960627 00707 WP 1996 6 27 ARWA9606045 1 19960614 A 5712 FORMER DOUG DC8 DC863F 302198F WP WS 747.5 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 A .75 INCH CRACK ON RIGHT WING LEADING EDGE FORMER AT STA XFS 747.500. REPAIRED AREA IAW DRAWING ARW 015713-0305 FAA FO RM 8110 APPROVED. 2 L 7 4 4F 4A25 1996062700708 19960627 00708 WP 1996 6 27 ARWA9606046 1 19960614 A 5712 FORMER DOUG DC8 DC863F 302198F WP WS 347.75 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 A 1 INCH CRACK FOUND IN RIGHT WING LEADING EDGE FORMER AT STA XFS 347.750. REPAIRED AREA IAW DRAWING ARW 015713-0309, F AA FORM 8110 APPROVED. 2 L 7 4 4F 4A25 1996062700709 19960627 00709 WP 1996 6 27 ARWA9606047 1 19960614 A 5712 FORMER DOUG DC8 DC863F 302198F WP WS 766.25 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 A 1 INCH CRACK FOUND ON RIGHT WING LEADING EDGE FORMER AT STA XFS 766.250. REPAIRED AREA IAW DRAWING ARW 015713-0304, F AA FORM 8110 APPROVED. 2 L 7 4 4F 4A25 1996062700710 19960627 00710 WP 1996 6 27 ARWA9606048 1 19960614 A 5712 FORMER DOUG DC8 DC863F 302198F WP WS 723 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 A 1 INCH CRACK ON RIGHT WING LEADING EDGE FORMER AT STA XFS 723.000. REPAIRED AREA IAW DRAWING ARW 015713-0307, FAA FOR M 8110 APPROVED. 2 L 7 4 4F 4A25 1996062700711 19960627 00711 WP 1996 6 27 ARWA9606049 1 19960614 A 5712 FORMER DOUG DC8 DC863F 302198F WP WS 733 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 A 1 CRACK FOUND ON RIGHT WING LEADING EDGE FORMER AT STA XFS 733.000. REPAIRED AREA IAW DRAWING ARW 015713-0306, FAA FO RM 8110 APPROVED. 2 L 7 4 4F 4A25 1996062700712 19960627 00712 WP 1996 6 27 ARWA9606050 1 19960614 A 5712 FORMER DOUG DC8 DC863F 302198F WP WS 845.5 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 A .75 INCH CRACK FOUND ON RIGHT WING LEADING EDGE FORMER AT STA XFS 845.500. REPAIRED AREA IAW DRAWING ARW 015713-0303, FAA FORM 8110 APPROVED. 2 L 7 4 4F 4A25 1996062700713 19960627 00713 WP 1996 6 27 ARWA9606051 1 19960614 A 5712 FORMER DOUG DC8 DC863F 302198F WP WS 852 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 A 1 INCH CRACK FOUND ON RIGHT WING LEADING EDGE FORMER AT STA XFS 852. REPAIRED AREA IAW DRAWING ARW 015713-0302, FAA F ORM 8110 APPROVED. 2 L 7 4 4F 4A25 1996062700714 19960627 00714 WP 1996 6 27 ARWA9606052 1 19960614 A 5712 FORMER DOUG DC8 DC863F 302198F WP WS 324 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 A 1 INCH CRACK FOUND ON RIGHT WING LEADING EDGE FORMER AT STA XFS 324.000. REPAIRED AREA IAW DRAWING ARW 015713-0310, F AA FORM 8110 APPROVED. 2 L 7 4 4F 4A25 1996062700715 19960627 00715 WP 1996 6 27 ARWA9606054 1 19960614 A 5330 SKIN DOUG DC8 DC863F 302198F WP FS 920 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 WING CENTER SECTION HAS LEVEL 2 CORROSION BETWEEN SKIN AND FILLER AT LONGERON 22L, FS 920 THROUGH 980. REPAIRED AREA AC CORDING TO DACO ROD SKETCH NR 96-05-20-003. 2 L 7 4 4F 4A25 1996062700716 19960627 00716 WP 1996 6 27 ARWA9606055 1 19960614 A 5230 CARGO DOOR DOUG DC8 DC863F 302198F WP NR 3 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 NR 3 LOWER CARGO DOOR HAS 1 INCH CRACK IN LEFT UPPER CORNER. REPAIRED NR 3 CARGO DOOR IAW DC-8 SRM 52-2-2 AND 52-4-1. F ABRICATED AND TREATED DOUBLER IAW DC-8 SRM 51-1-4 AND 51-1-8. INSTALLED DC-8 IAW SRM 51-1-21. 2 L 7 4 4F 4A25 1996062700717 19960627 00717 WP 1996 6 27 ARWA9606056 1 19960614 A 5313 LONGERON DOUG DC8 DC863F 302198F WP BS 960 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 LONGERON 24L HAS 3.5 INCH CRACK AT STA 960. LONGERON 24L WAS REPAIRED IAW DC-8 SRM 53-2-2, FIG 5. FABRICATED DOUBLERS PER DC-8 SRM 51-1-1. TREATED AND INSTALLED DOUBLERS IAW DC-8 SRM 51-1-8 AND 51-1-20D. 2 L 7 4 4F 4A25 1996062700718 19960627 00718 WP 1996 6 27 ARWA9606057 1 19960614 A 5320 FILLET DOUG DC8 DC863F 302198F WP BS 940 BROKEN A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 MAIN CARGO COMPARTMENT HAS LEVEL 2 CORROSION AT STA 940, RT UPPER PART, ALONG WITH BROKEN FILLET. REPAIRED AREA ACCORDI NG TO DACO ROD SKETCH NR 96-05-20-003. 2 L 7 4 4F 4A25 1996062700719 19960627 00719 WP 1996 6 27 ARWA9606058 1 19960614 A 5313 LONGERON DOUG DC8 DC863F 302198F WP BS 960-980 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 RIGHT WING CENTER SECTION AT STA 960 THROUGH 980, LONGERON 22R, HAS CORROSION, CRACKS AND SHEARED RIVETS. REPAIRED AREA ACCORDING TO DACO ROD SKETCH NR 96-05-20-003. 2 L 7 4 4F 4A25 1996062700720 19960627 00720 WP 1996 6 27 ARWA9606059 1 19960614 A 5315 FLOOR BEAM DOUG DC8 DC863F 302198F WP BS 1723 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 SUPPORT ANGLE AT FLOOR BEAM HAS LEVEL 2 CORROSION AT FS 1723. REMOVED ANGLE, FABRICATED, TREATED AND INSTALLED ANGLE IA W DC-8 SRM 53-7-3, 51-1-4, 51-1-8 AND 51-1-21. 2 L 7 4 4F 4A25 1996062700721 19960627 00721 WP 1996 6 27 ARWA9606060 1 19960614 A 5241 GALLEY DOOR DOUG DC8 DC863F 302198F WP BS 1220-1240 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 AFT GALLEY DOOR AT LONGERON 21R, FS 1220 TO 1240 HAS 2.5 INCH CRACK. REPAIRED CRACK PER DC-8 SRM 53-2-0, FIG 2. 2 L 7 4 4F 4A25 1996062700722 19960627 00722 WP 1996 6 27 ARWA9606061 1 19960614 A 5220 DOOR BASE DOUG DC8 DC863F 302198F WP EMER EXIT CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 LEFT AFT EMERGENCY DOOR BASE HAS LEVEL 1 CORROSION AND 4 INCH CRACK AT LONGERON 21L. REMOVED CORROSION AND REPAIRED ARE A PER DC-8 SRM 53-2-0, FIG 1B, SHEET 3 AND 51-1-8. 2 L 7 4 4F 4A25 1996062700723 19960627 00723 WP 1996 6 27 ARWA9606063 1 19960614 A 7830 TRANSLATING RING DOUG DC8 DC863F 302198F WP NR 3 ENGINE CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 NR 3 ENGINE TRANSLATING RING HAS 2 INCH CRACK IN RT FORWARD UPPER STRINGER. REPAIRED UPPER STRINGER IAW DC-8 SRM 78-3-3 . 2 L 7 4 4F 4A25 1996062700724 19960627 00724 WP 1996 6 27 ARWA9606065 1 19960614 A 5320 DOOR CUTOUT DOUG DC8 DC863F 302198F WP BS 280 DAMAGED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 TEMPORARY REPAIR IN FORWARD LOWER CARGO COMPARTMENT DOOR CUTOUT, FORWARD CORNER, AT STA 280. REPAIRED FORWARD LOWER COR NER PER DC-8 SRM 53-2-0, FIG 22, CLEANED AND TREATED AREA PER DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1996062700725 19960627 00725 WP 1996 6 27 ARWA9606067 1 19960614 A 5730 PLATE DOUG DC8 DC863F 302198F WP WS 22.75-50 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 RIGHT WING INNER TOP PANEL PLATE SHOWS LEVEL 2 CORROSION FROM XRS 22.750 TO XRS 50.000. REPAIRED AND TREATED AREA PER D C-8 SRM 57-2-1 AND 51-1-8. 2 L 7 4 4F 4A25 1996062700726 19960627 00726 WP 1996 6 27 ARWA9606070 1 19960618 A 2110 CLAMP DOUG DC8 DC862 3021970 WP TURBO COMPRESSOR LOOSE A ARWA K NONE O OTHER CL CLIMB 1 SO 19 802BN 45909 DURING CLIMB, UNABLE TO MAINTAIN PRESSURIZATION WITH FOUR T/C'S OPERATING AT 24,000 FT. CABIN DIFFERENTIAL KEPT CLIMBIN G, RETURNED TO JFK. FOUND LEFT SIDE TURBO COMPRESSOR HOT AIR DUCT CLAMP LOOSE BY BULKHEAD IN UNPRESSURIZED AREA. RETIG HTENED CLAMP, PRESSURIZED AIRCRAFT TO 8.6 AND NO LEAK NOTED. 2 L 7 4 4F 4A25 1996062700727 19960627 00727 1996 6 27 ARWA9606071 4 19960621 A 3420 25883625 DIR GYRO DOUG DC8 DC862 3021970 WP NR 2 COMPASS INOPERATIVE A ARWA K NONE O OTHER CR CRUISE 1 SO 19 1803 45895 AFTER TAKEOFF, NR 2 COMPASS SYSTEM OFF FLAG INTERMITTENT. RETURNED TO MIAMI. REMOVED AND REPLACED DIRECTIONAL GYRO. S YSTEM OPS CHECKED NORMAL IAW 34-20-00. 2 L 7 4 4F 4A25 1996062700728 19960627 00728 WP 1996 6 27 CALA9600871 1 19960625 A 2450 CKT BREAKER DOUG DC9 DC981 3022081 WP COCKPIT FAILED A CALA K NONE O OTHER CR CRUISE 1 SW 09 37882 48027 THE RT AC BUS 50 AMP CIRCUIT BREAKER, AFT CENTER AND LEFT FUEL BOOST PUMP CIRCUIT BREAKERS POPPED WHILE EN ROUTE. CREW ATTEMPTED TO RESET CIRCUIT BREAKERS WITHOUT SUCCESS. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT AC BUS 50 AMP CIRCUIT BREAKER B1-276 AT FAULT. THE CIRCUIT BREAKER WAS REMOVED AND REPLACED. THE OTHER POPPED CIRCUIT BREAKERS WERE RESET. BOTH ENGINES WERE RUN WITH FULL ELECTRICAL LOAD AND ALL OPERATION CHECK ED GOOD WITH NO CIRCUIT BREAKERS POPPING. 2 L 7 2 4F A6WE 1996062700729 19960627 00729 WP 1996 6 27 CALA9600872 1 19960526 A 5754 RIB DOUG DC9 DC982 3022082 WP LE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33817 49371 INSPECTION FOUND A 1.25 INCH CRACK AT INBOARD ROOT RIB OF RT WING SLAT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 5 7-02, FIGURE 2. 2 L 7 2 4F A6WE 1996062700730 19960627 00730 WP 1996 6 27 CALA9600873 1 19960526 A 5720 ANGLE DOUG DC9 DC982 3022082 WP WS 270 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33817 49371 INSPECTION FOUND A .5 INCH CRACK IN RIB SUPPORT ANGLE INSIDE LEADING EDGE, 13 INCHES OUTBOARD OF NR 8 SLAT TRACK AT XRS 270. A SUPPORT ANGLE AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 57-01. 2 L 7 2 4F A6WE 1996062700731 19960627 00731 WP 1996 6 27 CALA9600874 1 19960526 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 219-229 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33817 49371 INSPECTION FOUND LT FUSELAGE SKIN DENTED IN THREE PLACES ABOVE CUSP LINE BETWEEN STA 219 TO 229, LONGERON 17L AND 18L. T HE DAMAGED AREA WAS CUT OUT AND A FLUSH REPAIR WAS INSTALLED IAW ECRA 5330-02410. 2 L 7 2 4F A6WE 1996062700732 19960627 00732 WP 1996 6 27 CALA9600875 1 19960526 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 229-237 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33817 49371 INSPECTION FOUND LT FUSELAGE SKIN DENTED IN THREE PLACES ABOVE CUSP LINE AT STA 229 TO 237. THE DAMAGED AREA WAS CUT OU T AND A FLUSH REPAIR WAS INSTALLED IAW ECRA 5330-02410. 2 L 7 2 4F A6WE 1996062700733 19960627 00733 WP 1996 6 27 CALA9600876 1 19960527 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 262 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33817 49371 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 262 BETWEEN LONGERONS 23 AND 24L. THE DAMAGED AREA WAS CUT OUT AND A FILLE R AND DOUBLER REPAIR WAS INSTALLED IAW SRM 53-04, PAGE 218. 2 L 7 2 4F A6WE 1996062700734 19960627 00734 WP 1996 6 27 CALA9600877 1 19960527 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 207 GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33817 49371 INSPECTION FOUND FUSELAGE SKIN GOUGED AT STA 207, LONGERON 13L. A DOUBLER WAS INSTALLED IAW SRM 53-04, PAGE 218F. 2 L 7 2 4F A6WE 1996062700735 19960627 00735 WP 1996 6 27 CALA9600878 1 19960527 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 1316 GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33817 49371 INSPECTION FOUND RT FUSELAGE SKIN GOUGED AT STA 1316, 8 INCHES BELOW CUSP LINE. NEW PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-04. 2 L 7 2 4F A6WE 1996062700736 19960627 00736 WP 1996 6 27 CALA9600879 1 19960527 A 5753 VANE DOUG DC9 DC982 3022082 WP LT TE FLAP GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33817 49371 INSPECTION FOUND LT INBOARD FLAP VANE LOWER SURFACE GOUGED AND DENTED. THE DAMAGED AREA WAS CUT OUT AND A HOT BOND REPA IR WAS INSTALLED IAW SRM 51-70-2. 2 L 7 2 4F A6WE 1996062700737 19960627 00737 WP 1996 6 27 CALA9600880 1 19960528 A 5753 FLAP VANE DOUG DC9 DC982 3022082 WP RT TE FLAP GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33817 49371 INSPECTION FOUND RT WING OUTBOARD FLAP MIDDLE VANE LOWER LEADING EDGE SKIN GOUGED. THE DAMAGED AREA WAS CUT OUT AND A H OT BOND REPAIR WAS INSTALLED IAW SRM 51-70-2. 2 L 7 2 4F A6WE 1996062700738 19960627 00738 WP 1996 6 27 CALA9600881 1 19960528 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 160-200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33817 49371 INSPECTION FOUND FLOORBOARD SUPPORT CORRODED AT STA 160 TO 200, LBL 60. THE FLOORBOARD SUPPORT WAS REMOVED AND A NEW SU PPORT WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-10-3. 2 L 7 2 4F A6WE 1996062700739 19960627 00739 WP 1996 6 27 CALA9600882 1 19960528 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 140-200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33817 49371 INSPECTION FOUND FLOORBOARD SUPPORT CORRODED AT STA 140 TO 200, BL 0. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS FAB RICATED AND INSTALLED IAW SRM 53-05, 53-00 AND 51-10-3. 2 L 7 2 4F A6WE 1996062700740 19960627 00740 WP 1996 6 27 CALA9600883 1 19960529 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 522 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33817 49371 INSPECTION FOUND A .25 INCH CRACK IN RADIUS OF VERTICAL ANGLE AT AFT SIDE OF STA 522 BULKHEAD ABOVE LONGERON 24L. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-20 AND 51-10-3. 2 L 7 2 4F A6WE 1996062700741 19960627 00741 WP 1996 6 27 CALA9600884 1 19960529 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 522 PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33817 49371 INSPECTION FOUND LOWER FRAME AT AFT SIDE OF STA 522 BULKHEAD PUNCTURED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-01. 2 L 7 2 4F A6WE 1996062700742 19960627 00742 WP 1996 6 27 CALA9600885 1 19960530 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 198 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33817 49371 INSPECTION FOUND MAIN ENTRY FLOOR WEB CRACKED AT STA 198, LBL 60 WITH CORROSION UNDER CIRCUMFERENTIAL FRAME AT STA 200L. THE CORRODED AREA WAS CUT OUT, A FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW ECRA 5310-03285. 2 L 7 2 4F A6WE 1996062700743 19960627 00743 WP 1996 6 27 CALA9600886 1 19960530 A 5320 FITTING DOUG DC9 DC982 3022082 WP DOOR CUTOUT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33817 49371 INSPECTION FOUND CORNER FITTING CORRODED AT LOWER FORWARD CORNER OF CENTER PIT DOOR CUTOUT. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-5 AND 51-10-3. 2 L 7 2 4F A6WE 1996062700744 19960627 00744 WP 1996 6 27 CALA9600887 1 19960531 A 5320 SILL DOUG DC9 DC982 3022082 WP AFT CARGO DR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33817 49371 INSPECTION FOUND THE AFT CARGO DOOR SILL FORWARD FACE CORRODED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-05, FI GURE 63. 2 L 7 2 4F A6WE 1996062700745 19960627 00745 WP 1996 6 27 CALA9600888 1 19960531 A 5320 FITTING DOUG DC9 DC982 3022082 WP BS 1155 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33817 49371 INSPECTION FOUND AFT CARGO FITTING CRACKED AND CORRODED AT STA 1155, LONGERON 29R TO 30R. A REPLACEMENT FITTING WAS FAB RICATED AND INSTALLED IAW SRM 51-00 AND 51-10-3. 2 L 7 2 4F A6WE 1996062700746 19960627 00746 WP 1996 6 27 CALA9600889 1 19960605 A 5311 CIRCUMFERENTIAL DOUG DC9 DC982 3022082 WP BS 1231 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33817 49371 INSPECTION FOUND CIRCUMFERENTIAL CORRODED AT STA 1231 BETWEEN LONGERON 27R AND 27L. THE CORRODED AREA WAS REMOVED. A R EPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-03, FIGURE 2A. 2 L 7 2 4F A6WE 1996062700747 19960627 00747 WP 1996 6 27 CALA9600890 1 19960606 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1380 WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33817 49371 INSPECTION FOUND FRAME WEB REPAIR DOUBLER WORN IN TAIL COMPARTMENT AT STA 1380, LONGERON 5L. THE DOUBLER WAS REMOVED AND REPLACED IAW SRM 53-01. 2 L 7 2 4F A6WE 1996062700748 19960627 00748 NM 1996 6 27 P5CA9600253 1 19960622 A 5240 SERVICE PANEL BOEING 747 747123 1384873 NM NLG CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 FOUND NOSE LANDING GEAR SERVICE PANEL CRACKED ALONG LOWER EDGE. SANDED DAMAGED AREA, APPLIED FIBERGLASS REPAIR IAW SRM 51-40-08. 2 L 7 4 4F A20WE 1996062700749 19960627 00749 NM 1996 6 27 P5CA9600254 1 19960622 A 2612 LEFT SQUIB BOEING 747 747123 1384873 NM NR 2 ENGINE NO TEST A P5CA K NONE L NO TEST IN INSP/MAINT 1 WP 23 859FT 20326 NR 2 ENGINE LEFT HAND SQUIB WOULD NOT TEST. REPAIRED BROKEN WIRE, OPS CHECK GOOD IAW MM 26-10-00. 2 L 7 4 4F A20WE 1996062700750 19960627 00750 NM 1996 6 27 P5CA9600255 1 19960622 A 5730 PANEL BOEING 747 747123 1384873 NM LEFT WING LE PUNCTURED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 FOUND HOLE IN LEFT WING LEADING EDGE, LOWER SURFACE AT OUTBOARD HINGE OF VARIABLE CAMBER FLAP. REPAIRED IAW SRM 51-24-1 1. 2 L 7 4 4F A20WE 1996062700751 19960627 00751 NM 1996 6 27 P5CA9600256 1 19960622 A 5730 TE PANEL BOEING 747 747123 1384873 NM LT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 FOUND LEFT WING TRAILING EDGE PANEL DELAMINATED AT OUTBOARD END OF INBOARD FLAP WELL. APPLIED FIBERGLASS REPAIR IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1996062700752 19960627 00752 NM 1996 6 27 P5CA9600257 1 19960622 A 5730 PANEL BOEING 747 747123 1384873 NM LT WING PUNCTURED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 FOUND HOLE IN LEFT WING PANEL, FORWARD OF INBOARD AILERON, OUTBOARD OF NR 2 PYLON. REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996062700753 19960627 00753 NM 1996 6 27 P5CA9600258 1 19960622 A 5753 PANEL BOEING 747 747123 1384873 NM LT TE FOREFLAP DISBONDING A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 FOUND LEFT HAND OUTBOARD FOREFLAP UPPER SURFACE REPAIR DISBONDING ABOVE NR 1 FLAP TRACK. REPAIRED DAMAGED AREA IAW SRM 51-40-06. 2 L 7 4 4F A20WE 1996062700754 19960627 00754 NM 1996 6 27 P5CA9600259 1 19960622 A 5753 PANEL BOEING 747 747123 1384873 NM LT TE MIDFLAP WORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 FOUND HOLE WORN IN LEFT HAND OUTBOARD MIDFLAP LEADING EDGE, OUTBOARD END. REPAIRED DAMAGE IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996062700755 19960627 00755 NM 1996 6 27 P5CA9600260 1 19960622 A 5753 PANEL BOEING 747 747123 1384873 NM LT TE FOREFLAP WORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 FOUND HOLE IN LEFT HAND OUTBOARD FOREFLAP LEADING EDGE, OUTBOARD END. REPAIRED DAMAGE IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996062700756 19960627 00756 NM 1996 6 27 P5CA9600261 1 19960622 A 5753 PANEL BOEING 747 747123 1384873 NM RT TE FOREFLAP DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 FOUND HOLE IN RIGHT HAND OUTBOARD FOREFLAP LEADING EDGE, OUTBOARD END. REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996062700757 19960627 00757 NM 1996 6 27 P5CA9600262 1 19960622 A 5321 FLOOR PANEL BOEING 747 747123 1384873 NM BS 1720-1740 DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 FOUND FLOOR DAMAGED ON MAIN CARGO DECK STA 1720-1740 LT. REMOVED AND REPLACED FLOOR PANELS IAW SRM 51-32-01. 2 L 7 4 4F A20WE 1996062700758 19960627 00758 NE 1996 6 27 P5CA9600263 2 19960622 A 7250 S RAIL BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE NR 2 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 58582 1680 20326 685982 FOUND NR 2 ENGINE AFT S-RAIL CRACKED AT 2 O'CLOCK POSITION. STRESS RELIEVED IAW MM 72-53-01, WELDED IAW P AND W 72-53-0 1. 2 L 7 4 4F 4 F A20WE E20EA 1996062700759 19960627 00759 NM 1996 6 27 P5CA9600264 1 19960622 A 7800 EXH SLEEVE SKIN BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE NR 2 ENGINE PEELED BACK A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 58582 1680 20326 685982 FOUND NR 2 ENGINE AFT EXHAUST SLEEVE LEADING EDGE SKIN PEELED BACK AND DAMAGED FROM 2 O'CLOCK TO 7 O'CLOCK POSITION. RE PAIRED AREA IAW SRM 54-30-03. 2 L 7 4 4F 4 F A20WE E20EA 1996062700760 19960627 00760 NM 1996 6 27 P5CA9600265 1 19960622 A 3610 ATTACH BRACKET BOEING 747 747123 1384873 NM NR 4 PRECOOLER CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 FOUND NR 4 ENGINE LEFT HAND PRECOOLER TOP ATTACH BRACKET CRACKED. REMOVED BROKEN BRACKET AND BUSHINGS IAW MM 36-12-04. INSTALLED NEW BRACKET AND BUSHINGS IAW MM 36-12-04. 2 L 7 4 4F A20WE 1996062700761 19960627 00761 NM 1996 6 27 P5CA9600266 1 19960622 A 7800 EXH SLEEVE SKIN BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE NR 4 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 68766 2860 20326 662318 FOUND NR 4 ENGINE EXHAUST SLEEVE EXTERNAL LEADING EDGE SKIN PULLED BACK, CRACKED AND PARTLY MISSING, RIGHT SIDE. REMOVE D DAMAGED SKIN IAW SRM 54-30-03. INSTALLED REPAIR PLATE IAW SRM 51-30-02. ENGINE TOTAL CYCLES, 16,359. 2 L 7 4 4F 4 F A20WE E20EA 1996062700762 19960627 00762 NM 1996 6 27 P5CA9600267 1 19960622 A 7110 SKIN BOEING 747 747123 1384873 NM NR 4 CORE COWL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 NR 4 OUTBOARD CORE COWL TOP AFT INSIDE SKIN CRACKED DUE TO EXCESSIVE HEAT. INSTALLED REPAIR DOUBLER IAW SRM 54-30-02. 2 L 7 4 4F A20WE 1996062700763 19960627 00763 NM 1996 6 27 P5CA9600268 1 19960622 A 5730 PANEL BOEING 747 747123 1384873 NM LT WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 FOUND LEFT WING AILERON LOCKOUT ACCESS PANEL CRACKED AT FORWARD INBOARD CORNER. REPAIRED AREA IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996062700764 19960627 00764 NM 1996 6 27 P5CA9600269 1 19960622 A 5522 PANEL BOEING 747 747123 1384873 NM LT ELEVATOR DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 FOUND LEFT HAND INBOARD ELEVATOR DAMAGED AT TRAILING EDGE. REMOVED DAMAGED AREA, REPAIRED IAW SRM 51-10-09. 2 L 7 4 4F A20WE 1996062700765 19960627 00765 NM 1996 6 27 P5CA9600270 1 19960527 A 7110 CORE COWL BOEING 747 747124 1384874 NM NR 1 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND OLD REPAIR CRACKED AND BROKEN ON NR 1 ENGINE OUTBOARD CORE COWL, AFT TOP END. REMOVED OLD REPAIR, FABRICATED AND INSTALLED NEW REPAIR IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996062700766 19960627 00766 NM 1996 6 27 P5CA9600271 1 19960524 A 7110 COWL BOEING 747 747124 1384874 NM NR 4 ENGINE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND NR 4 ENGINE OUTBOARD FAN COWL DELAMINATED AT 2 O'CLOCK POSITION. REMOVED AND REPLACED OUTBOARD FAN COWL IAW MM 71 -11-04. 2 L 7 4 4F A20WE 1996062700767 19960627 00767 NM 1996 6 27 P5CA9600272 1 19960525 A 7110 FLANGE BOEING 747 747124 1384874 NM NR 2 CORE COWL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND NR 2 ENGINE INBOARD CORE COWL MATING FLANGE ON T/R TRAILING EDGE CRACKED AND WORN. REMOVED AND REPLACED FLANGE IA W SRM 51-10-01. 2 L 7 4 4F A20WE 1996062700768 19960627 00768 NM 1996 6 27 P5CA9600273 1 19960525 A 5414 TE TIP BOEING 747 747124 1384874 NM NR 2 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND NR 2 ENGINE OUTBOARD PYLON TRAILING EDGE TIP HAD FASTENER MISSING AND CRACKED END. REMOVED PART, WELDED ON TRAVEL ER, INSTALLED PART IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996062700769 19960627 00769 NM 1996 6 27 P5CA9600274 1 19960525 A 5245 DOOR BOEING 747 747124 1384874 NM RT AC BAY DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FOUND HOLE IN HONEYCOMB PANEL ON INTERIOR SURFACE OF LOWER FUSELAGE RIGHT HAND AIR CONDITIONING BAY DOOR, THIRD ONE AFT. REPAIRED DOOR IAW SRM 51-40-15 AND SRM 51-40-09. 2 L 7 4 4F A20WE 1996062700770 19960627 00770 NM 1996 6 27 P5CA9600275 1 19960604 A 3610 EXH DUCT BOEING 747 747122 1384872 NM PWA JT9 JT9D7F 52054 NE NR 2 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 61657 253 19753 662991 FOUND NR 2 ENGINE 3.5 BLEED AIR LOWER RIGHT HAND EXHAUST DUCT CRACKED. REMOVED DUCT, WELDED IAW BAC5975, REINSTALLED DU CT IAW MM 75-32-06. 2 L 7 4 4F 4 F A20WE E20EA 1996062700771 19960627 00771 NE 1996 6 27 P5CA9600276 2 19960602 A 7250 R RAIL BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 1 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 66775 2009 19753 662231 FOUND NR 1 ENGINE R-RAIL CRACKED AT 10 O'CLOCK POSITION UNDER PRECOOLER DOOR. REMOVED DOOR, STRESS RELIEVED IAW MM 72-5 3-01, FLAP PEENED R-RAIL IAW SRM 51-10-07, REINSTALLED DOOR IAW MM 36-12-01. 2 L 7 4 4F 4 F A20WE E20EA 1996062700772 19960627 00772 NM 1996 6 27 P5CA9600277 1 19960602 A 5753 PANEL BOEING 747 747122 1384872 NM RT TE MIDFLAP BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND RIGHT WING OUTBOARD MIDFLAP OUTBOARD LOWER CORNER BROKEN OFF. REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996062700773 19960627 00773 NM 1996 6 27 P5CA9600278 1 19960611 A 5753 PANEL BOEING 747 747122 1384872 NM RT TE MIDFLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND RIGHT WING INBOARD MIDFLAP OUTBOARD END CRACKED. REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996062700774 19960627 00774 NM 1996 6 27 P5CA9600279 1 19960608 A 3232 FITTING BOEING 747 747122 1384872 NM RT MLG DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND RIGHT HAND BODY GEAR OUTBOARD DOOR ACTUATOR CONNECTING ROD FITTING ON UPPER DOOR CRACKED. REPLACED ROD FITTING PE R MM 32-33-28. OPS CHECK GOOD PER MM 32-33-00. 2 L 7 4 4F A20WE 1996062700775 19960627 00775 NM 1996 6 27 P5CA9600280 1 19960605 A 5753 BOLTS BOEING 747 747122 1384872 NM FLAP TRACKS CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND ALL FLAP TRACK FAIL SAFE BOLTS CORRODED. REMOVED AND REPLACED OUTBOARD TRACK FAIL SAFE BOLTS IAW MM 27-51-04. RE MOVED AND REPLACED INBOARD TRACK FAIL SAFE BOLTS IAW MM 27-51-01. 2 L 7 4 4F A20WE 1996062700776 19960627 00776 NM 1996 6 27 P5CA9600281 1 19960605 A 5753 MOUNTING PIN BOEING 747 747122 1384872 NM NR 7 FLAPTRACK CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND NR 7 FLAP TRACK AFT LINK MOUNTING PIN CORRODED. REPLACED PIN IAW OHM 27-51-75. 2 L 7 4 4F A20WE 1996062700777 19960627 00777 NM 1996 6 27 P5CA9600282 1 19960605 A 5753 MOUNTING BOLTS BOEING 747 747122 1384872 NM NR 1 AFT CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND NR 1 AFT LINK MOUNTING BOLTS CORRODED. REMOVED AND REPLACED NR 1 TRACK AFT LINK MOUNTING BOLTS IAW OHM 27-51-75/S B 27-2280. 2 L 7 4 4F A20WE 1996062700778 19960627 00778 NM 1996 6 27 P5CA9600283 1 19960606 A 5753 PANEL BOEING 747 747122 1384872 NM RT TE FOREFLAP PUNCTURED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND RIGHT HAND INBOARD FOREFLAP PUNCTURED ON LOWER SURFACE NEAR CENTER. REMOVED DAMAGED AREA AND APPLIED FIBERGLASS R EPAIRS IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1996062700779 19960627 00779 NM 1996 6 27 P5CA9600284 1 19960605 A 5753 PANEL BOEING 747 747122 1384872 NM LT OB FOREFLAP PUNCTURED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND LEFT OUTBOARD FOREFLAP PUNCTURED ON UNDERSIDE AT OUTBOARD END. REPAIRED IAW SRM 51-40-06. 2 L 7 4 4F A20WE 1996062700780 19960627 00780 NM 1996 6 27 P5CA9600285 1 19960605 A 5321 FLOOR PANEL BOEING 747 747122 1384872 NM BS 500 DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND MAIN DECK BS 500, RBL 20, FLOOR PANEL ASSEMBLY DELAMINATED. REMOVED AND REPLACED FLOOR PANEL IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996062700781 19960627 00781 NM 1996 6 27 P5CA9600286 1 19960605 A 5350 PANEL BOEING 747 747122 1384872 NM LT WING FAIRING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND LEFT WING UPPER FIXED FAIRING PANEL JUST AFT OF R/S FORWARD OF MLG BEAM ASSEMBLY CRACKED. CRACK APPROXIMATELY 12 INCHES LONG. REPAIRED WITH FIBERGLASS OVERLAYS IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996062700782 19960627 00782 NM 1996 6 27 P5CA9600287 1 19960605 A 5753 PANEL BOEING 747 747122 1384872 NM LT TE AFT FLAP PUNCTURED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND LEFT OUTBOARD AFT FLAP PANEL PUNCTURED ON UNDERSIDE APPROXIMATELY 1 FOOT FROM OUTBOARD END. REMOVED DAMAGED AREA AND APPLIED FILLER AND DOUBLER IAW SRM 51-40-06. 2 L 7 4 4F A20WE 1996062700783 19960627 00783 NM 1996 6 27 P5CA9600288 1 19960605 A 5753 PANEL BOEING 747 747122 1384872 NM LT TE AFT FLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND LEFT OUTBOARD AFT FLAP DELAMINATED ON UNDERSIDE AT INBOARD END. REMOVED DELAMINATED SKIN, FABRICATED AND INSTALLE D FILLERS AND DOUBLERS IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1996062700784 19960627 00784 NM 1996 6 27 P5CA9600289 1 19960605 A 5753 PANEL BOEING 747 747122 1384872 NM LT TE MID FLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND LEFT INBOARD MID FLAP LEADING EDGE DELAMINATED APPROXIMATELY 6 FEET FROM INBOARD EDGE. REMOVED DAMAGED SKIN, FABR ICATED FILLERS AND DOUBLERS, REPAIRED AREA IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1996062700785 19960627 00785 NM 1996 6 27 P5CA9600290 1 19960604 A 5753 PANEL BOEING 747 747122 1384872 NM RT TE AFT FLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND RIGHT WING INBOARD AFT FLAP OUTBOARD UPPER STRESS PANEL DELAMINATED. REMOVED AND REPLACED STRESS PANEL IAW SRM 51 -30-02. 2 L 7 4 4F A20WE 1996062700786 19960627 00786 NM 1996 6 27 P5CA9600291 1 19960604 A 5350 FAIRING BOEING 747 747122 1384872 NM WING/BODY DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND AFT WING-TO-BODY FAIRING 194BR DELAMINATED. REPAIRED FAIRING IAW SRM 51-40-14. 2 L 7 4 4F A20WE 1996062700787 19960627 00787 NM 1996 6 27 P5CA9600292 1 19960603 A 7110 ANGLE BOEING 747 747122 1384872 NM NR 1 ENG COWLING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND CRACKED BRACKET AND DAMAGED PIN AREA AT NR 1 INBOARD COWLING LOWER INSIDE CORNER AT ALIGN PIN. REPAIRED CRACKED A NGLE IAW SRM 51-40-04. 2 L 7 4 4F A20WE 1996062700788 19960627 00788 NM 1996 6 27 P5CA9600293 1 19960603 A 7110 CHAFE STRIP BOEING 747 747122 1384872 NM NR 1 ENG COWLING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND NR 1 INBOARD COWLING LOWER AFT CORNER (INSIDE) HAS CHAFE STRIP CRACKED. REMOVED AND REPLACED CHAFE STRIP IAW SRM 51-10-01 AND SRM 51-30-02. 2 L 7 4 4F A20WE 1996062700789 19960627 00789 NM 1996 6 27 P5CA9600294 1 19960603 A 7110 BRACKET BOEING 747 747122 1384872 NM NR 1 ENG COWLING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND NR 1 INBOARD ENGINE COWLING LOWER FORWARD CORNER INSIDE BRACKETS AT FORWARD FRAME STIFFENER CRACKED AND DAMAGED. R EPAIRED CORNER BRACKETS AND FRAME STIFFENER IAW SRM 54-14-03. 2 L 7 4 4F A20WE 1996062700790 19960627 00790 NM 1996 6 27 P5CA9600295 1 19960603 A 7110 SKIN BOEING 747 747122 1384872 NM NR 1 ENG COWLING PUNCTURED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND NR 1 OUTBOARD MAIN COWL SKIN PUNCTURED BETWEEN FIRST AND SECOND RIB. REPAIRED COWLING IAW SRM 54-30-03. 2 L 7 4 4F A20WE 1996062700791 19960627 00791 NM 1996 6 27 P5CA9600296 1 19960603 A 5730 SKIN REPAIR BOEING 747 747122 1384872 NM LT WING DISBONDING A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND UPPER LEFT WING COMPOSITE REPAIR DISBONDING JUST BELOW L-3 DOOR. REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996062700792 19960627 00792 NM 1996 6 27 P5CA9600297 1 19960602 A 3350 SIGN BOEING 747 747122 1384872 NM CABIN INOPERATIVE A P5CA K NONE L NO TEST IN INSP/MAINT 1 WP 23 853FT 19753 FOUND CREW ENTRY EMERGENCY EXIT SIGN INOPERABLE. RELAMPED LIGHT FIXTURE, OPS CHECK GOOD IAW MM 33-51-13. 2 L 7 4 4F A20WE 1996062700793 19960627 00793 NM 1996 6 27 P5CA9600298 1 19960602 A 5400 SKIN BOEING 747 747122 1384872 NM NR 2 ENG FAIRING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND NR 2 ENGINE FORWARD FAIRING HAS CRACK IN SKIN ON INBOARD SIDE. REMOVED PREVIOUS REPAIR IAW SRM 51-30-02, INSTALLE D DOUBLER AND FILLER IAW SRM 51-10-01. 2 L 7 4 4F A20WE 1996062700794 19960627 00794 NM 1996 6 27 P5CA9600299 1 19960602 A 5320 SILL PROTECTOR BOEING 747 747122 1384872 NM CARGO DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND AFT SILL PROTECTOR IN FRONT OF MAIN DECK CARGO DOOR HAS CRACK IN CENTER PORTION. FOUND CRACK IN SILL PROTECTOR WE B ALSO, UPON REMOVAL OF SILL PROTECTOR. REMOVED SILL PROTECTOR AND WEB IAW SRM 51-10-01. INSTALLED NEW PROTECTOR AND W EB IAW SRM 51-10-01 AND SRM 51-10-02. 2 L 7 4 4F A20WE 1996062700795 19960627 00795 NM 1996 6 27 P5CA9600300 1 19960602 A 5400 LATCH MOUNT BOEING 747 747122 1384872 NM NR 2 ENGINE DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND NR 2 ENGINE OUTBOARD COWL NR 3 LATCH MOUNT DAMAGED. REMOVED AND REPLACED LATCH MOUNT ANGLE IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996062700796 19960627 00796 NM 1996 6 27 UPS96220408 1 19960528 A 5755 SKIN BOEING 727 72722C 138400F NM NR 10 SPOILER DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, NR 10 SPOILER IS DELAMAMINATED AT THE CENTER HINGE UPPER SURFACE. REMOVED DELAMAMINATED AREA, REMOV ED CENTER HINGE TO ACCESS AREA, IMPREGNATED GLASS CLOTH, SEALED REPAIR, REINSTALLED CENTER HINGE AND WORK DONE IAW SRM 5 1-40-06, MM 20-50-01, AND 51-30-2. 2 L 7 3 4F A3WE 1996062700797 19960627 00797 NM 1996 6 27 UPS96220409 1 19960528 A 5755 DOWNSTOP FITTING BOEING 727 72722C 138400F NM NR 14 SPOILER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, NR 14 SPOILER O/B DOWNSTOP FITTING IS CORRODED. REMOVED AND REPLACED NR 14 SPOILER O/B DOWNSTOP FIT TING IAW SRM 51-30-02. 2 L 7 3 4F A3WE 1996062700798 19960627 00798 NM 1996 6 27 UPS96220410 1 19960529 A 5752 TAB HINGE FTG BOEING 727 72722C 138400F NM LT INBD AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, L/W I/B AILERON TAB HAS ALL THREE HINGE FITTINGS CORRODED, TAB SIDE. REMOVED L/W AILERON TAB I/B RE MOVED FITTINGS AND INSTALLED NEW FITTINGS IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996062700799 19960627 00799 NM 1996 6 27 UPS96220411 1 19960529 A 5755 PANEL BOEING 727 72722C 138400F NM NR 5 SPOILER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, NR 5 SPOILER PANEL IS DELAMINATED AT THE CENTER HINGE FITTING UPPER SURFACE. REMOVED CENTER HINGE F ITTING, REPLACED DELAMINATED AREA, FOUND CENTER HINGE FITTING TO BE CRACKED AND WILL REPLACE ON OTHER NRC, WORK DONE IAW SRM 57-50-06. 2 L 7 3 4F A3WE 1996062700800 19960627 00800 NM 1996 6 27 UPS96220412 1 19960529 A 5754 CENTER HINGE BOEING 727 72722C 138400F NM LE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, BULLNOSE CENTER HINGE UPPER ATTACH POINT ON NR 3 K-FLAP B-CORRODED UNDER BOLT HEADS. REMOVED K-FLAP AND REPLACED WITH NEW K-FLAP. 2 L 7 3 4F A3WE 1996062700801 19960627 00801 NM 1996 6 27 UPS96220413 1 19960529 A 5751 HINGE FITTING BOEING 727 72722C 138400F NM RT INBD AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, RT I/B AILERON CENTER WING SIDE HINGE FITTING IS CORRODED. REMOVED CORRODED CENTER HINGE FITTING, F OUND BEARING BLOCK TO HAVE BLOWN DUST SEAL. REPLACED WITH NEW BEARING BLOCK AND REPLACED HINGE FITTING IAW OHM 57-50-01 . 2 L 7 3 4F A3WE 1996062700802 19960627 00802 NM 1996 6 27 UPS96220414 1 19960529 A 5752 TAB HINGE FTG BOEING 727 72722C 138400F NM RT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, R/W I/B AILERON SIDE TAB HINGE FITTINGS ARE CORRODED. REMOVED CORRODED HINGE FITTINGS, LOCATED NEW ONES AND INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996062700803 19960627 00803 NM 1996 6 27 UPS96220415 1 19960530 A 5320 INTERCOSTAL BOEING 727 72722C 138400F NM BS 313-327 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON FLOORBOARD SUPPORT INTERCOSTAL STA 313 TO 327, WL 208, LBL 30 AREAS MARKED. CLEANED AN D EVALUATED AREA 2.3 BY 14, OUT OF LIMITS WITH .040 REMOVED ON ORIG THICKNESS OF .078, ORDERED NEW PART RECEIVED AND INS TALLED IAW SRM 51-10-6, SRM 51-30-2. 2 L 7 3 4F A3WE 1996062700804 19960627 00804 NM 1996 6 27 UPS96220416 1 19960530 A 2782 ACT SUPPORT WEB BOEING 727 72722C 138400F NM NR 5 LE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, NR 5 K-FLAP ACTUATOR O/B TRUNNION SUPPORT WEB IS CRACKED. REMOVED CRACKED SUPPORT WEB, FABRICATED N EW SUPPORT WEB AND INSTALLED ON A/C IAW SRM 51-30-2, SRM 51-10-2. 2 L 7 3 4F A3WE 1996062700805 19960627 00805 NM 1996 6 27 UPS96220417 1 19960530 A 5754 RIB BOEING 727 72722C 138400F NM NR 4 LE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, 2ND AND 3RD RIB CRACKED ON NR 4 SLAT. REMOVED BOTH 2ND AND 3RD RIB FROM SLAT DRILLED UP NEW RIBS AN D INSTALLED IN SLAT PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996062700806 19960627 00806 NM 1996 6 27 UPS96220418 1 19960530 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 405 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON RT STRINGER NR 7 STA 405. REMOVED CORROSION, 1 BY .025 BY .025 OF ORIGINAL .032 OUT OF LIMITS, FABRICATED REPAIR PARTS AND INSTALLED ON A/C AFTER TREATING AFFECTED AREA IAW SRM 51-10-6, 53-10-2 AND SRM 53-1 0-3. 2 L 7 3 4F A3WE 1996062700807 19960627 00807 NM 1996 6 27 UPS96220419 1 19960530 A 5320 STRINGER TIE BOEING 727 72722C 138400F NM BS 950 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON STRINGER TIE STA 950 STR 1 WL 302. REMOVED CORROSION FROM STR TIE STA 950 STR 1 WL 302 , REMOVED .035 FROM ORIGINAL .163 OUT OF LIMITS. REMOVED OLD STRINGER TIE AND INSTALLED NEW TIE IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996062700808 19960627 00808 NM 1996 6 27 UPS96220420 1 19960530 A 5320 WEB FINGER BOEING 727 72722C 138400F NM BS 500 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CRACKED WEB FINGER STA 500, LBL 7 WL 302. REMOVED DAMAGED SECTION OF WEB, FABRICATED REPAIR PARTS A ND INSTALLED PER SRM 51-30-02. 2 L 7 3 4F A3WE 1996062700809 19960627 00809 NM 1996 6 27 UPS96220421 1 19960531 A 2510 SEAT PEDESTAL BOEING 727 72722C 138400F NM BS 226 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON CAPTAINS SEAT PEDESTAL STA 226, LBL 13 TO 31, WL 208. REMOVED CORROSION WAS OUT OF LIM ITS, REMOVED BAD CHANNEL RECEIVED NEW CHANNEL AND INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996062700810 19960627 00810 NM 1996 6 27 UPS96220422 1 19960531 A 5522 BALANCE PANEL BOEING 727 72722C 138400F NM RT ELEVATOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION RT NR 5 BALANCE PANEL AT MATING SURFACES OF BALANCE PANEL HINGE AND WEIGHT ASSM. REMOVED PANEL NR 5 BALANCE BAY, DRILLED OUT FASTENERS, REMOVED CORROSION FROM DOUBLER AND FOUND DOUBLER TO BE OUT OF LIMITS. FA BRICATED NEW DOUBLER AND INSTALLED PANEL, BALANCE PANEL AND HINGE IN A/C PER MM 27-30-21, SRM 51-36-5 AND SRM 55-20-2. 2 L 7 3 4F A3WE 1996062700811 19960627 00811 NM 1996 6 27 UPS96220423 1 19960531 A 5320 MOP SILL BOEING 727 72722C 138400F NM BS 294-300 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, MOP SILL IS CRACKED STA 294 TO 300 LBL 53 WL 208. REMOVED CRACKED MOP SILL AND REPLACED WITH NEW IA W SRM 51-30-02 SRM 51-30-05, SRM 51-10-01, SRM 51-20-04. 2 L 7 3 4F A3WE 1996062700812 19960627 00812 NM 1996 6 27 UPS96220424 1 19960531 A 5347 SEAT TRACK BOEING 727 72722C 138400F NM BS 760-848 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON TOP AND BOTTOM OF FLANGES ON SEAT TRACK STA 760 TO 848 LBL 45, WL 208. REMOVED CORROSI ON FOUND OUT OF LIMITS, REPLACED WITH FABRICATED ONE IAW SRM 53-10-01, SRM 51-30-02. 2 L 7 3 4F A3WE 1996062700813 19960627 00813 NM 1996 6 27 UPS96220425 1 19960601 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 428.5 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, FOUND STR 22L TO BE CORRODED AT BS 428.5. REMOVED CORROSION, SPLICE SECTION AT BS 440, CUT DAMAGED STRINGER, FOUND STR 22L AT BS 412 TO BE CORRODED BEYOND LIMITS AS WELL. CUT STRINGER AT BS 407, FABRICATED REPAIR PARTS AND INSTALLED NEW STRINGER AND REPAIR PARTS IN A/C PER SRM 51-30-02, SRM 53-10-02, 53-10-3. 2 L 7 3 4F A3WE 1996062700814 19960627 00814 NM 1996 6 27 UPS96220426 1 19960602 A 3221 TRUNNION FITTING BOEING 727 72722C 138400F NM NLG CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON LT AND RT NLG TRUNNION FITTING BORES. MACHINED LT AND RT TRUNNION ATTACH POINTS TO REM OVE CORROSION, FABRICATED NEW OVER SIZE BUSHINGS AND INSTALLED IAW SRM 53-40-01 AND BOEING DWG 65-7676. 2 L 7 3 4F A3WE 1996062700815 19960627 00815 NM 1996 6 27 UPS96220427 1 19960603 A 5320 SHEAR TIE BOEING 727 72722C 138400F NM BS 328 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CRACKED SHEAR TIE AT BS 328 RBL 62 WL 191. REPAIRED BS 328 FRAME SHEAR TIE AT RBL 62 WL 191 IAW SRM 53-10-4, 51-30-2, 51-10-2 AND MM 51-20-151. 2 L 7 3 4F A3WE 1996062700816 19960627 00816 NM 1996 6 27 UPS96220428 1 19960604 A 5320 SEAT TRACK WELL BOEING 727 72722C 138400F NM BS 680-695 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION AND MECHANICAL DAMAGE IN SEAT TRACK WELL RBL 45 680 TO 695 WL 208. CORROSION AND MECHANIC AL DAMAGE OUT OF LIMITS IAW SRM 53-10-01, SEAT TRACK WILL BE REPLACED ON UPS NRC 567976. 2 L 7 3 4F A3WE 1996062700817 19960627 00817 NM 1996 6 27 UPS96220429 1 19960601 A 5320 SHEAR TIE BOEING 727 72722C 138400F NM BS 277 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CRACKED SHEAR TIE AT BS 277 LBL 59 WL 194. REPAIRED FRAME SHEAR TIE AT STA 277 LBL 59 WL 194 IAW SR M 53-10-04 AND 53-30-02. 2 L 7 3 4F A3WE 1996062700818 19960627 00818 NM 1996 6 27 UPS96220430 1 19960604 A 5220 CASTING BOEING 727 72722C 138400F NM RT EMER EXIT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON RT HAND OVERWING EXIT, HANDLE SEAL CASTING. REMOVED CORRODED CASTING, RECEIVED NEW DRI LLED UP PART, SEALED AND INSTALLED ON DOOR IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996062700819 19960627 00819 NM 1996 6 27 UPS96220431 1 19960604 A 5754 BONDING JUMPER BOEING 727 72722C 138400F NM NR 4 LE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, NR 4 K-FLAP IS CORRODED AT I/B BONDING JUMPER ATTACH POINT ON RIB. REMOVED CORROSION, REMOVED .085 FROM .170 1 BY 1 AREA OUT OF LIMITS. REMOVED CORRODED AREA, FABRICATED REPAIR PARTS AND INSTALLED RELOCATED JUMPER WIRE TO ANOTHER ATTACH POINT, ALL WORK DONE IAW SRM 57-50-01 AND 51-30-02. 2 L 7 3 4F A3WE 1996062700820 19960627 00820 NM 1996 6 27 UPS96220432 1 19960604 A 5320 SEAT TRACK WELL BOEING 727 72722C 138400F NM BS 540-610 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION AND MECHANICAL DAMAGE IN SEAT TRACK WELL STA 540 TO 610 RBL 45 WL 208. CORROSION AND MECH ANICAL DAMAGE OUT OF LIMITS IAW SRM 53-10-1 SEAT TRACK WILL BE REPLACED ON UPS NRC 567976. 2 L 7 3 4F A3WE 1996062700821 19960627 00821 NM 1996 6 27 UPS96220433 1 19960605 A 5320 T-STIFFENER BOEING 727 72722C 138400F NM BS 740 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON HORIZONTAL T-STIFFENER ON AFT SIDE OF BS 740 WEB BL 0 WL 160. CORROSION MECHANICALLY REMOVED REWORK DEEMED TO BE OUT OF LIMITS IAW SRM 53-10-01. REPLACED STIFFENER IAW SRM 51-10-1, 51-30-2 AND 51-30-5. 2 L 7 3 4F A3WE 1996062700822 19960627 00822 NM 1996 6 27 UPS96220434 1 19960605 A 5752 UPPER TAB BOEING 727 72722C 138400F NM LT AILERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, S-13 UPPER TAB IS CRACKED AT LWS 656. REPAIRED S-13 AT LWS 656 IAW UPS EO B727-5710-0314F. 2 L 7 3 4F A3WE 1996062700823 19960627 00823 NM 1996 6 27 UPS96220435 1 19960605 A 5241 CORNER REVEAL BOEING 727 72722C 138400F NM GALLEY DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON MID GALLEY DOOR FWD UPPER CORNER REVEAL CORRODED. REMOVED OLD FWD UPPER REVEAL CLAMPED NEW PART IN PLACE, BACK DRILLED THROUGH EXITING FASTENER HOLES AND INSTALLED PART IAW SRM 57-30-02. 2 L 7 3 4F A3WE 1996062700824 19960627 00824 NM 1996 6 27 UPS96220436 1 19960606 A 5320 UPLOCK SUPPORT BOEING 727 72722C 138400F NM BS 870-880 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON LEFT MLG UPLOCK SUPPORT STRUCUTRE BS 872 TO 880 LBL 66 TO 70 WL 189 TO 192 ON HORIZONTA L WEB, VERTICAL WEB AND SUPPORT WEB L-ANGLE AND AT BS 889 ON WEB AND FLANGE. REMOVED CORROSION, REWORK ON WEB SUPPORT A NGLE DEEMED OUT OF LIMITS, ONLY REPLACED L-ANGLE IAW SRM 53-10-1, 53-10-2, 51-30-2, 51-30-5 MM 51-20-21, 51-20-31. 2 L 7 3 4F A3WE 1996062700825 19960627 00825 NM 1996 6 27 UPS96220437 1 19960530 A 2720 CENTERING CRANK BOEING 727 72722C 138400F NM RUDDER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, RUDDER AFT CONTROL CENTERING CRANK ASSM HOUSING IS CRACKED AT LEFT SPRING MOUNT FLANGE. REMOVED AND REPLACED RUDDER CENTERING MECHANISM IAW MM 27-20-91. 2 L 7 3 4F A3WE 1996062700826 19960627 00826 NM 1996 6 27 UPS96220438 1 19960606 A 5320 FLOORBOARD SUPRT BOEING 727 72722C 138400F NM BS 649/658 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON FLOORBOARD SUPPORT HAT CHANNEL STA 649 AND STA 658 WL 207.5 RBL BOTTOM SIDE OF NUT CLIP HOLES. MECHANICALLY REMOVED CORROSION, REWORK DEEMED OUT OF LIMITS IAW SRM 53-10-1, REPLACED CHANNEL STA 620 TO 680 IA W SRM 51-30-02, 51-30 -5, 51-30-3, 51-10-2 AND MM 51-20-151. 2 L 7 3 4F A3WE 1996062700827 19960627 00827 NM 1996 6 27 UPS96220439 1 19960606 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 330-400 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON STRINGER 1 STA 330 TO 400. MECHANICALLY REMOVED CORROSION, REWORK AREA AT STR 1 STA 38 0 TO 400 DEEMED OUT OF LIMITS IAW SRM 53-10-1. REPAIRED STR 1 IAW 53-10-3. 2 L 7 3 4F A3WE 1996062700828 19960627 00828 NM 1996 6 27 UPS96220440 1 19960606 A 5315 FLOORBEAM BOEING 727 72722C 138400F NM BS 312 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON FLOORBEAM STA 312 WL 208 LBL 19, 20 LBL 40. CORROSION MECHANICALLY REMOVED FROM STA 31 2 FLOORBEAM LBL 19, 20, 40, REWORK AT LBL 19 DEEMED OUT OF LIMITS IAW SRM 53-10-1. REPAIRED FLOORBEAM AT LBL 19 STA 19 STA 312 IAW SRM 53-10-8 FIG 7. 2 L 7 3 4F A3WE 1996062700829 19960627 00829 NM 1996 6 27 UPS96220441 1 19960607 A 5320 INTERCOSTAL BOEING 727 72722C 138400F NM BS 211 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON INTERCOSTAL BETWEEN BS 211 AND 219 WL 174 RBL 27. REMOVED FAB'D AND INSTALLED REPLACEM ENT INTERCOSTAL IAW SRM 51-30-2 AND 53-10-1. 2 L 7 3 4F A3WE 1996062700830 19960627 00830 NM 1996 6 27 UPS96220442 1 19960607 A 5312 BULKHEAD BRACKET BOEING 727 72722C 138400F NM BS 745 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION AT EXPANSION LINK LBL 7 BS 745 WL 165 ON DELTA BEAM BOX. REMOVED AND REPLACED EXPANSION L INK FORK ASSM, BULKHEAD BRACKET AND BUSHING IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996062700831 19960627 00831 NM 1996 6 27 UPS96220443 1 19960610 A 5320 WEB BOEING 727 72722C 138400F NM BS 1135 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, FOUND CORROSION ON WEB AT STA 1135 LBL 62 WL 208. REMOVED CORROSION 10 BY 3 UP TO .027 ON .063 ORIG INAL THICKNESS OUT OF LIMITS, FABRICATED REPAIR DOUBLER AND INSTALLED PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996062700832 19960627 00832 NM 1996 6 27 UPS96220444 1 19960617 A 5320 INTERCOSTAL BOEING 727 72722C 138400F NM BS 313-327 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON FLOOR SUPPORT INTERCOSTAL STA 313 TO 327 WL 208 RBL 47 AREA MARKED. FOUND SUPPORT OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-30-5 AND 51-30-2. 2 L 7 3 4F A3WE 1996062700833 19960627 00833 NM 1996 6 27 UPS96220445 1 19960617 A 5347 SEAT TRACK BOEING 727 72722C 138400F NM BS 520 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON SEAT TRACK AT BS 520 RBL 15 WL 150. REMOVED AND REPLACED SEAT TRACK FROM 480 TO 530 RB L 15 WL 15 IAW SRM 53-10-05. 2 L 7 3 4F A3WE 1996062700834 19960627 00834 NM 1996 6 27 UPS96220446 1 19960531 A 5347 SEAT TRACK BOEING 727 72722C 138400F NM BS 700-730 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON TOP OF SEAT TRACK AND INSIDE WALL STA 700 TO 730 RBL 62, WL 208. REMOVED CORROSION OUT OF LIMITS, FABRICATED NEW SEAT TRACK, REMOVED OLD SEAT TRACK, INSTALLED NEW SEAT TRACK PER SRM 51-30-2, 53-10-5. 2 L 7 3 4F A3WE 1996062700835 19960627 00835 NM 1996 6 27 UPS96220447 1 19960611 A 5320 WEB BOEING 727 72722C 138400F NM BS 257 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON WEB STA 257 RBL 46 WL 208 TO 229. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS, FAB RICATED NEW WEB IAW SRM 51-10-2, ALODINED AND PRIMED IAW MM 51-20-31 AND INSTALLED PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996062700836 19960627 00836 NM 1996 6 27 UPS96220448 1 19960611 A 5315 FLOORBEAM BOEING 727 72722C 138400F NM BS 328 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON FLOORBEAM AT STA 328, WL 208, LBL 35, 31. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 53 -10-8. 2 L 7 3 4F A3WE 1996062700837 19960627 00837 NM 1996 6 27 UPS96220449 1 19960611 A 5522 SKIN BOEING 727 72722C 138400F NM LT ELEVATOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, LEFT ELEVATOR 2ND FROM O/B STATIC WICK BASE IS LOOSE. FOUND CORRODED SKIN UNDER BASE AND REPAIRED I AW SRM 55-20-01. 2 L 7 3 4F A3WE 1996062700838 19960627 00838 NM 1996 6 27 UPS96220450 1 19960611 A 5315 FLOORBEAM BOEING 727 72722C 138400F NM BS 420 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON FLOORBEAM STA 420 WL 206 IN NUTCLIP HOLES LBL 46 TO 60, LBL 24, RBL 24 AREAS MARKED. F OUND CORROSION OUT OF LIMITS FOR SRM 53-10-1, FABRICATED REPAIR PARTS PER SRM 53-10-8 AND INSTALLED REPAIR PARTS PER SRM 53-10-8. 2 L 7 3 4F A3WE 1996062700839 19960627 00839 NM 1996 6 27 UPS96220451 1 19960611 A 5330 SKIN BOEING 727 72722C 138400F NM BS 553 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON INTERNAL SKIN STA 553 LBL 6 WL 306. CUTOUT DAMAGED AREA, FABRICATED AND INSTALLED REPA IR IAW SRM 53-30-3 AND 53-30-2. 2 L 7 3 4F A3WE 1996062700840 19960627 00840 NM 1996 6 27 UPS96220452 1 19960611 A 5320 FAIL-SAFE STRAP BOEING 727 72722C 138400F NM BS 351 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON TOP OF FAIL-SAFE STRAP STA 351, WL 178, RBL 14 TO 20. REMOVED AND REPLACED FAIL-SAFE S TRAP IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996062700841 19960627 00841 NM 1996 6 27 UPS96220453 1 19960531 A 5347 SEAT TRACK BOEING 727 72722C 138400F NM BS 760-848 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION AROUND NUTPLATES ON BOTTOM SIDE OF SEAT TRACK STA 760 TO 848 RBL 65 WL 208. REMOVED CORRO SION OUT OF LIMITS, REMOVED SEAT TRACK, FABRICATED NEW AND INSTALLED IAW SRM 51-30-2, 53-10-2, 53-10-5. 2 L 7 3 4F A3WE 1996062700842 19960627 00842 NM 1996 6 27 UPS96220454 1 19960612 A 5320 ANGLE BOEING 727 72722C 138400F NM BS 300-342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON VARIOUS ARES OF L-ANGLE BETWEEN BS 300 TO 342, RBL 58 TO 61, WL 208. FOUND AREAS OF CO RROSION TO BE OUT OF LIMITS PER SRM 53-10-1, REMOVED AND REPLACED L-ANGLE IAW SRM 51-40-3. 2 L 7 3 4F A3WE 1996062700843 19960627 00843 NM 1996 6 27 UPS96220455 1 19960612 A 5314 KEEL BEAM BOEING 727 72722C 138400F NM BS 762-772 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON KEEL BEAM OF ELECTRICAL GROUND WIRES BS 762 TO 772, LBL 7 WL 155. FOUND CORROSION OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED CHORD IAW SRM 51-40-4, REINSTALLED GROUND POST AND WIRES IAW WPM 20-20- 00. 2 L 7 3 4F A3WE 1996062700844 19960627 00844 NM 1996 6 27 UPS96220456 1 19960612 A 5510 SUPPORT BOEING 727 72722C 138400F NM RT HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, RT HORIZONTAL STABILIZER SIDE RIB PAD IS PILLOWING. REMOVED RUB PLATE FROM SUPPORT AND FOUND CORROS ION TO BE OUT OF LIMITS PER SRM 55-50-01. INSTALLED NEW RUB PLATE AND SUPPORT PER SRM 51-30-02, MATERIAL LOSS WAS 1OO P ERCENT OF SUPPORT. 2 L 7 3 4F A3WE 1996062700845 19960627 00845 NM 1996 6 27 UPS96220457 1 19960612 A 5510 SUPPORT BOEING 727 72722C 138400F NM LT HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, LT HORIZONTAL STABILIZER SIDE RUB PAD IS PILLOWING. REMOVED RUB PLATE FROM SUPPORT AND FOUND CORROS ION TO BE OUT OF LIMITS PER SRM 55-50-01. INSTALLED NEW RUB PLATE AND SUPPORT PER SRM 51-30-02 MATERIAL LOSS WAS 100 PE RCENT OF SUPPORT. 2 L 7 3 4F A3WE 1996062700846 19960627 00846 NM 1996 6 27 UPS96220458 1 19960612 A 5755 FITTING BOEING 727 72722C 138400F NM NR 7 SPOILER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, NR 7 SPOILER CENTER SUPPORT FITTING IS CORRODED. REMOVED AND REPLACED NR 7 SPOILER CENTER SUPPORT F ITTING IAW MM 27-62-81. 2 L 7 3 4F A3WE 1996062700847 19960627 00847 NM 1996 6 27 UPS96220459 1 19960612 A 5320 WEB BOEING 727 72722C 138400F NM BS 259 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON WEB STA 259 LBL 46 TO 49 WL 208 TO 222. FOUND CORROSION OUT OF LIMITS PER SRM 51-10-6. REMOVED AND REPLACED WEB IAW SRM 51-40-2, 51-30-2, 51-20-04 AND 51-10-02. 2 L 7 3 4F A3WE 1996062700848 19960627 00848 NM 1996 6 27 UPS96220460 1 19960613 A 5320 HAT CHANNEL BOEING 727 72722C 138400F NM BS 1140 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON HAT CHANNEL STA 1140 LBL 35 TO 55 WL 208. REPLACED HAT CHANNEL PER SRM 51-30-2, 51-10- 2. 2 L 7 3 4F A3WE 1996062700849 19960627 00849 NM 1996 6 27 UPS96220461 1 19960613 A 5347 SEAT TRACK BOEING 727 72722C 138400F NM BS 1090-1130 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON SEAT TRACK TOP AND BOTTOM OF FLANGES STA 1090 TO 1130 LBL 55 WL 208. FOUND CORROSION O UT OF LIMITS PER SRM 53-10-01, REMOVED AND REPLACED SEAT TRACK IAW SRM 51-10-2, 51-30-02 AND 51-30-05. 2 L 7 3 4F A3WE 1996062700850 19960627 00850 NM 1996 6 27 UPS96220462 1 19960614 A 5320 INTERCOSTAL BOEING 727 72722C 138400F NM BS 327-343 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON FLOORBOARD SUPPORT INTERCOSTAL STA 327 TO 343, WL 208 LBL 30, AREAS MARKED. FOUND CORR OSION TO BE OUT OF LIMITS IAW SRM 51-10-6. REMOVED AND REPLACED SUPPORT IAW SRM 51-30-02. 2 L 7 3 4F A3WE 1996062700851 19960627 00851 NM 1996 6 27 UPS96220463 1 19960614 A 5320 INTERCOSTAL BOEING 727 72722C 138400F NM BS 257-277 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON FLOOR SUPPORT STA 257 TO 277 LBL 13 TO 15 WL 208. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-01. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-20-04 AND 51-30-02. 2 L 7 3 4F A3WE 1996062700852 19960627 00852 NM 1996 6 27 UPS96220464 1 19960615 A 5320 STIFFENER BOEING 727 72722C 138400F NM BS 344 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON HORIZONTAL STIFFENER AT BS 344, LBL 12 WL 183. REMOVED AND REPLACED STIFFENER IAW SRM 51-30-2, 51-10-5 AND 51-10-01. 2 L 7 3 4F A3WE 1996062700853 19960627 00853 NM 1996 6 27 UPS96220465 1 19960615 A 2550 CARGO PUCK BOEING 727 72722C 138400F NM BS 460 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON CARGO PUCK STA 460, WL 208, LBL 40. REMOVED AND REPLACED CARGO TIE DOWN FITTING IAW SR M 51-30-02 AND 51-10-01. 2 L 7 3 4F A3WE 1996062700854 19960627 00854 NM 1996 6 27 UPS96220466 1 19960615 A 2550 CARGO PUCK BOEING 727 72722C 138400F NM BS 700 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON CARGO PUCK STA 700, WL 208, LBL 57. REMOVED AND REPLACED CARGO TIE DOWN FITTING IAW SR M 51-30-02 AND 51-10-01. 2 L 7 3 4F A3WE 1996062700855 19960627 00855 NM 1996 6 27 UPS96220467 1 19960615 A 2550 CARGO PUCK BOEING 727 72722C 138400F NM BS 720 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON CARGO PUCK STA 720, WL 208, LBL 57. REMOVED AND REPLACED CARGO TIE DOWN FITTING IAW SR M 51-30-02 AND 51-10-01. 2 L 7 3 4F A3WE 1996062700856 19960627 00856 NM 1996 6 27 UPS96220468 1 19960615 A 5320 ANGLE BOEING 727 72722C 138400F NM BS 870 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION AT BS 870 VERTICAL SUPPPORT AND TIE ANGLE LBL 12 WL 199 LEFT MLG WHEEL WELL. FOUND CORROS ION TO BE OUT OF LIMITS PER SRM 53-10-01. REMOVED AND REPLACED SUPPORT AND TIE ANGLE IAW SRM 53-30-02, 51-40-04, MM 51- 20-31, 51-30-00. 2 L 7 3 4F A3WE 1996062700857 19960627 00857 NM 1996 6 27 UPS96220469 1 19960615 A 2550 CARGO PUCK BOEING 727 72722C 138400F NM BS 580 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON CARGO PUCK STA 580, WL 208, LBL 40 AREA MARKED. REMOVED AND REPLACED CARGO PUCK IAW SR M 51-30-02 AND 51-10-01. 2 L 7 3 4F A3WE 1996062700858 19960627 00858 NM 1996 6 27 UPS96220471 1 19960616 A 5320 STRINGER TIE BOEING 727 72722C 138400F NM BS 360 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, FOUND CORROSION ON FRAME AT STA 360, WL 50, LBL 25 TO RBL 25 AND STRINGER TIE AT RT STR NR 22, STA 3 60. CORROSION REMOVAL WAS BEYOND LIMITS ON STRINGER TIE AT STR 22R. REPLACED STR TIE PER 53-10-02, 53-10-03, 51-10-06, MM 51-20-151. 2 L 7 3 4F A3WE 1996062700859 19960627 00859 NM 1996 6 27 UPS96220473 1 19960616 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 351.2-360 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, FOUND CORROSION ON STRINGER 22 RT BETWEEN STA 351.2 AND STA 360. CORROSION REMOVAL WAS OUT OF LIMIT S PER SRM 53-10-01. REMOVED DAMAGED SECTION OF STRINGER, LOCATED AND DRILLED STRINGER REPAIR PARTS, INSTALLED PER SRM 5 3-10-03, 51-30-02, 51-20-04, MM 51-20-151. 2 L 7 3 4F A3WE 1996062700860 19960627 00860 NM 1996 6 27 UPS96220474 1 19960616 A 5312 BULKHEAD ANGLE BOEING 727 72722C 138400F NM BS 480 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON BULKHEAD ANGLE AT BS 480, WL 155, LBL 12, RBL 12. REMOVED AND REPLACED ANGLE IAW 51-30 -02, 51-10-05 AND MM 51-20-151. 2 L 7 3 4F A3WE 1996062700861 19960627 00861 NM 1996 6 27 UPS96220475 1 19960616 A 5315 FLOOR BEAM BOEING 727 72722C 138400F NM BS 344 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON FLOOR BEAM STA 344, WL 208 HAS NUMEROUS AREAS OF CORROSION FROM LBL 60 TO RBL 20. REMO VED AND REPLACED UPPER CHORD OF FLOOR BEAM IAW SRM 53-10-08. 2 L 7 3 4F A3WE 1996062700862 19960627 00862 NM 1996 6 27 UPS96220480 1 19960616 A 5320 FLOOR SUPPORT BOEING 727 72722C 138400F NM BS 480 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON FLOOR SUPPORT AT BS 480 WL 155 LBL 9. REMOVED DAMAGED SECTON OF FLOOR SUPPORT AND SPLI CED A REPLACEMENT SECTION IN IAW SRM 53-10-5 AND 51-30-2. 2 L 7 3 4F A3WE 1996062700863 19960627 00863 NM 1996 6 27 UPS96220481 1 19960531 A 5321 FLOOR BOEING 727 72722C 138400F NM BS 460 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON FLOOR WEB STA 460 WL 208, LBL 52 AREA MARKED. REMOVED CORROSION, FOUND TO BE OUT OF LI MITS PER SRM 53-10-1, CUT OUT DAMAGED AREA AND REPAIRED PER SRM 51-40-02. 2 L 7 3 4F A3WE 1996062700864 19960627 00864 NM 1996 6 27 UPS96220482 1 19960531 A 5751 SUPPORT FITTING BOEING 727 72722C 138400F NM LT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, L/W O/B AILERON, O/B SUPPORT FITTING ON WING IS PITTED AND CORRODED ON LOWER SURFACE AND AROUND BUSH INGS. REMOVED CORRODED PART, ORDERED NEW PART, RECEIVED DRILLED UP FITTING AND INSTALLED NEW FITTING IAW SRM 51-30-2, S RM 51-30-05. 2 L 7 3 4F A3WE 1996062700865 19960627 00865 NM 1996 6 27 UPS96220483 1 19960619 A 5751 FITTING BOEING 727 72722C 138400F NM RT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, R/W O/B AILERON O/B WING SIDE HINGE FITTING IS CORRODED. FOUND R/W O/B AILERON O/B WING SIDE HINGE FITTING OUT OF LIMITS PER SRM 57-40-00. REMOVED AND REPLACED R/W O/B AILERON O/B WING SIDE HINGE FITTING PER SRM 51-30- 02. 2 L 7 3 4F A3WE 1996062700866 19960627 00866 NM 1996 6 27 UPS96220484 1 19960603 A 5321 FLOOR BOEING 727 72722C 138400F NM BS 296 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CRACKED FLOOR AT HYLOCK BS 296, RBL 21, WL 208. REMOVED HYLOCK NDI LOCATED AND MARKED FOR STOP DRIL LING NOTED. CRACK INDICATION STOP DRILLED CRACKS FOUND CRACKS TO BE CONTAINED. FABRICATED AND INSTALLED REPAIR DOUBLER IAW 51-10-02 SRM 51-30-2, SRM 51-20-4. 2 L 7 3 4F A3WE 1996062700867 19960627 00867 NM 1996 6 27 UPS96220485 1 19960619 A 5315 FLOOR BEAM BOEING 727 72722C 138400F NM BS 600 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION IN NUTPLATE HOLES ON FLOOR BEAM BOTTOM SIDE OF UPPER FLANGE STA 600 WL 207.5 RBL 47 TO 63 AREAS MARKED. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-01, REPAIRED FLOOR BEAM AT BS 600 RBL 47 TO 63 PER UPS 727-53-1769. 2 L 7 3 4F A3WE 1996062700868 19960627 00868 NM 1996 6 27 UPS96220486 1 19960619 A 5752 HINGE FITTING BOEING 727 72722C 138400F NM RT AILERON TAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, R/W O/B AILERON TAB SIDE HINGE FITTINGS ARE CORRODED. FOUND HINGE FITTINGS TO BE OUT OF LIMITS PER SRM 57-40-00. REMOVED AND REPLACED R/W O/B AILERON TAB HINGE FITTINGS PER MM 27-10-41. 2 L 7 3 4F A3WE 1996062700869 19960627 00869 NM 1996 6 27 UPS96220487 1 19960619 A 5751 HINGE FTG BOEING 727 72722C 138400F NM LT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, L/W O/B AILERON O/B CENTER HINGE SUPPORT FITTING IS CORRODED. REMOVED CORRODED HINGE FITTING, DRILL ED NEW FITTING AND INSTALLED IAW SRM 51-30-02. 2 L 7 3 4F A3WE 1996062700870 19960627 00870 NM 1996 6 27 UPS96220488 1 19960626 A 3350 1000679 LIGHT BOEING 727 727172C 1384058 NM CABIN LOOSE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 916UP 19808 INSPECTION TYPE N/A, EMERGENCY EXIT LIGHT ILLUMINATED MULTIPLE TIMES IN FLIGHT W/O LOSS OF POWER SOURCES, FLIGHT CONDITI ONS SMOOTH. FOUND EMERGENCY EXIT LIGHT ASSY LOOSE IN THE SOCKET, CLEANED CONTACTS AND RESECURED LIGHT ASSY INTO SOCKET, GRND CHK GOOD. NO NEW PART INSTALLED, OLD PART WORKS FINE. 2 L 7 3 4F A3WE 1996062700871 19960627 00871 NM 1996 6 27 UPS96420405 1 19960621 A 3350 135610A LIGHTS BOEING 747 747123 1384873 NM MAIN DECK INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE N/A REF D111137, EMERGENCY LIGHT AT STA 580 LT CEILING MAIN DECK DIM. REPLACED EMERGENCY LIGHT ASSM (P/ N 1356837) (S/N 19732) ON, (P/N 1356-10A) (S/N UPS 5) OFF, ILLUMINATION CHECKS GOOD. 2 L 7 4 4F A20WE 1996062700872 19960627 00872 NM 1996 6 27 UPS96520406 1 19960622 A 3350 233N3219 SWITCH BOEING 757 75724APF 1384969 NM CABIN BROKEN A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 426UP 25457 INSPECTION TYPE N/A, EMERGENCY LIGHTS UNARMED LIGHT IS BROKEN. REMOVED AND REPLACED UNARMED SWITCH PANEL ASSY, OPS CKD OK. (P/N 233N3219) (S/N D00005) ON, (S/N D00036) OFF. 2 L 7 2 4F RT A2NM 1996062700873 19960627 00873 WP 1996 6 27 UPS96820403 1 19960621 A 2120 AIR DISTR DOUG DC8 DC871F 302199D WP COCKPIT ODOR A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 01 779UP 45979 INSPECTION TYPE N/A, AT TOP OF DECENT CREW SMELLED FUMES, SUSPECT RIGHT PACK. RAN RT PACK, OPS CHECKED NORMALLY. CHECK ED LEFT PACK, OPS CHECK NORMAL. COULD NOT DUPLICATE. PACKS OPS CHECKED NORMAL IAW 21-55-00. 2 L 7 4 4F RT 4A25 1996062700874 19960627 00874 WP 1996 6 27 UPS96820404 1 19960614 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 70-80 DAMAGED A IPXA K NONE O OTHER UK UNKNOWN 1 SO 01 819UP 46019 INSPECTION TYPE N/A, TEAR IN SIDE OF FUSELAGE FWD OF PIT 31 STA 70 TO 80. REPAIRED PER SRM 53-1-2, E0 DC8-5310-8335 AND EO DC8-5310-8335A. 2 L 7 4 4F RT 4A25 1996062700875 19960627 00875 WP 1996 6 27 UPS96820407 1 19960622 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE N/A, EMERGENCY EXIT LIGHTS ARE DIM DURING PREFLIGHT. CLEANED BATTERY PACK CONNECTION, CHANGED BATTERY P ACK, OPERATIONAL TEST NORMAL. 2 L 7 4 4F RT 4A25 1996062700876 19960627 00876 WP 1996 6 27 UPS96820470 1 19960601 A 5542 5644210 SKIN DOUG DC8 DC871F 302199D WP RUDDER CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE CS2, RUDDER LT SIDE HEAVY CORROSION JUST ABOVE THE TAB. REPLACED RUDDER ASSY ON N/R TASK NR 463759 AND ROUTINE T/C NR S55- 682-44. 2 L 7 4 4F RT 4A25 1996062700877 19960627 00877 WP 1996 6 27 UPS96820472 1 19960601 A 5320 5773311 DOUBLER DOUG DC8 DC871F 302199D WP BS 1644 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE CS2, HEAVY CORROSION ON FUSELAGE SKIN STA 1644 BETWEEN LONGERONS 29R AND 30R ON INNER DOUBLER. REPLACED INNER DOUBLER PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1996062700878 19960627 00878 WP 1996 6 27 UPS96820476 1 19960604 A 5320 56122983 FINGER DOUBLER DOUG DC8 DC871F 302199D WP SUBFLOOR CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE CS2, HEAVY CORROSION ON FINGER DOUBLER PANEL SUBFLOOR FS 131 TO 135 RBL 15 TO 25. REPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996062700879 19960627 00879 WP 1996 6 27 UPS96820477 1 19960603 A 5320 46143971N END FITTING DOUG DC8 DC871F 302199D WP FS 70 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE CS2, HEAVY CORROSION ON END FITTING, LONGERON 31R FS 70, FWD END. REPLACED FITTING PER SRM 51-1-20D AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1996062700880 19960627 00880 WP 1996 6 27 UPS96820478 1 19960603 A 5320 4611067 END FITTING DOUG DC8 DC871F 302199D WP FS 70 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE CS2, MODERATE CORROSION ON END FITTING, LONGERON 33R, FS 70 FWD END. REPLACED FITTING PER SRM 51-1-21 A ND 51-1-20D. 2 L 7 4 4F RT 4A25 1996062700881 19960627 00881 WP 1996 6 27 UPS96820479 1 19960604 A 5312 3644359 BULKHEAD FITTING DOUG DC8 DC871F 302199D WP FS 980-1000 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE CS2, FS 980 TO 1000, LONGERON 30R, BULKHEAD FITTING HAS CORROSION CRACK. REPLACED FITTING PER SRM 51-1- 20D. 2 L 7 4 4F RT 4A25 1996062700882 19960627 00882 NM 1996 6 27 VNAA9606011 1 19960624 A 3150 FUEL PRESS WARN DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT ACTIVATED A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 433JS 3047 CREW ABORTED TAKEOFF AFTER BEING ALERTED BY A FUEL LOW PRESSURE CAS MESSAGE. AIRCRAFT RETURNED TO THE TAXI WAY. CREW C LEARED THE CAS MESSAGE, CONDUCTED ENGINE FULL POWER CHECKS IAW AFM, CAS MESSAGE DID NOT ILLUMINATE. ALL SYSTEMS CHECKE D GOOD CREW CONTINUED ON WITH THE FLIGHT. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996062700883 19960627 00883 NM 1996 6 27 VSTA9606002 1 19960625 A 3397 087021038 WIRE HARNESS BOEING 737 737247 138448D NM CABIN BROKEN A VSTA K NONE L NO TEST IN INSP/MAINT 1 WP 07 304VA 19617 EMERGENCY PATH LIGHTING SYSTEM INOP FROM ROW 9 TO REAR. REPAIRED BROKEN WIRE. 2 L 7 2 4F A16WE 1996070200001 19960702 00001 SW 1996 7 2 GXPA96001 1 19960328 A 3240 BRAKE SWRNGN SA226 SA226TC 8780404 SW LT MLG MALFUNCTION A GXPA O OTHER O OTHER LD LANDING 1 GL 23 165GA TC396 UPON LANDING, COPILOT APPLIED BRAKES, LEFT BRAKE GRABBED. RELEASED BRAKE, APPLIED AGAIN, AND AIRCRAFT PULLED TO LEFT AN D COULD NOT RELEASE. AIRCRAFT STOPPED ON SIDE OF RUNWAY. TOWED AIRCRAFT TO HANGAR. MAINTENANCE REPLACED NR 1 AND NR 2 BRAKES AND WHEELS. OPS CHECK GOOD. BRAKES WERE NOT LOCKED WHEN AIRCRAFT WAS TOWED TO HANGAR. (X) 2 L 7 2 4T RT A8SW 1996070200002 19960702 00002 EU 1996 7 2 GXPA96002 1 19960513 A 3320 173016 TRANSFORMER AMD FALC20 FALCON20C5 2730107 EU CABIN DEFECTIVE A GXPA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 23 613GA 104 77 ON 5-13-96, AIRCRAFT DECLARED AN EMERGENCY AND LANDED. THE CREW REPORTED THEY WERE GETTING SMOKE IN THE CABIN. (X) 2 L 7 2 4F RT A7EU 1996070200003 19960702 00003 EU 1996 7 2 VTZA96213 1 19960605 A 3150 TO WARNING JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT ACTIVATED A VTZA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 27 311UE 41029 FLT NR 6341 - IAD-LGA - ABORTED THE TAKEOFF DUE TO THE TAKEOFF CONFIGURATION WARNING SYSTEM ACTIVATING. AIRCRAFT RETURN ED TO GATE WITH NO FURTHER INCIDENTS. MX PERFORMED OPS CHECK BUT COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT WAS RELEASE D AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996070300001 19960703 00001 WP 1996 7 3 9614119925 1 19960624 A 7711 JF298H1 EPR INDICATOR DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9 52048 NE COCKPIT MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 925US 61570 15106 47472 666904 NR 1 ENGINE EPR INDICATION FROZE AT 1.45 ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE . MAINTENANCE REPLACED THE EPR INDICATOR WITH A SERVICEABLE UNIT. SYSTEM OPERATION RETURNED TO NORMAL. 2 L 7 2 4F 4 F A6WE E2EA 1996070300002 19960703 00002 WP 1996 7 3 9614121159 1 19960624 A 3350 POWER SUPPLY DOUG DC10 DC1040 3023508 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 159US 46768 DURING LINE CHECK, FOUND THE FORWARD 'B' ZONE AND AFT ZONE EMERGENCY FLOOR LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES AND POWER SUPPLY. 2 L 7 3 4F A22WE 1996070300003 19960703 00003 WP 1996 7 3 9614139302 1 19960620 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 302RC 48055 DURING LINE CHECK, FOUND CEILING MOUNTED EMERGENCY LIGHTS AT ROW 13 - ROW 18 WOULD NOT TEST. REPLACED BATTERY PACK AND POWER SUPPLY 85-72. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996070300004 19960703 00004 WP 1996 7 3 9614149880 1 19960624 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 675MC 47651 DURING LINE CHECK, FOUND OVERHEAD EMERGENCY LIGHT DIM IN MAIN CABIN. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996070300005 19960703 00005 WP 1996 7 3 9614159861 1 19960624 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 770MC 47758 DURING LINE CHECK, FOUND OVERHEAD EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHEC K OK. 2 L 7 2 4F A6WE 1996070300006 19960703 00006 WP 1996 7 3 9614169851 1 19960624 A 3350 LIGHT DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 760MC 47708 DURING LINE CHECK, FOUND LEFT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED POWER SUPPLY AND BATTERIES. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996070300007 19960703 00007 NM 1996 7 3 9614172276 1 19960621 A 2781 SWITCH BOEING 727 727251 138408H NM NR 2 LE FLAP FAILED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 276US 21155 DURING CLIMBOUT, THE LEADING EDGE SLAT NR 2 INDICATED NO RETRACTION. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDE NT. REPLACED NR 2 LEADING EDGE SWITCH. OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996070300008 19960703 00008 WP 1996 7 3 9614181150 1 19960626 A 7830 UNLOCK LIGHT DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20J 52054 NE NR 3 ENGINE TR ILLUMINATED A NWAA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 GL 01 150US 46759 86174 EN ROUTE DTW-MSP, THE NR 3 ENGINE REVERSER UNLOCK LIGHT ILLUMINATED. CREW FOLLOWED COM PROCEDURE, SHUT DOWN THE ENGINE, AND CONTINUED TO MSP WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED VIBRATION AND WINDMILLING CHECKS. REVERSER WAS AL SO CHECKED FOR STOW AND PROPER LOCKOUT. ALL CHECKS WERE NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A22WE E20EA 1996070300009 19960703 00009 NM 1996 7 3 96FDEA01121 1 19960613 A 5320 651758866 BEAM BOEING 727 72722 1384002 NM BS 268 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 NR 0650 AND 028. CORROSION C53-221-01 ON 25G BEAM STA 268, LBL 2, WL 208. ****S/D**** REMOVED AND REPLACED 25 G-BEAM, STA 268, LB 2, WL 208 PER FEDEX SRM 51-10-1. 2 L 7 3 4F A3WE 1996070300010 19960703 00010 NM 1996 7 3 96FDEA01153 1 19960619 A 5313 6554577 STRINGER BOEING 727 727225 1384077 NM BS 720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 467FE 21449 NR 0225 AND 013. CORROSION C53-113-01(1) AROUND FASTENERS INSIDE CHANNEL OF STR 27R AT BS 720F + 17. ****S/D***** FOUN D TO BE OUT LIMITS. REMOVED CORRODED SECTION OF STR 27B. FABRICATED AND INSTALLED REPAIR PARTS IAW FEDEX SRM 53-10-3. 2 L 7 3 4F A3WE 1996070300011 19960703 00011 NM 1996 7 3 96FDEA01171 1 19960625 A 5313 6554577 STRINGER BOEING 727 727225 1384077 NM BS 720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 467FE 21449 NR0224 AND 017, CORROSION (C53-113-01) AROUND FASTENERS INSIDE CHANNEL OF STR 27L AT BS 720F PLUS 17. 2 L 7 3 4F A3WE 1996070300012 19960703 00012 NM 1996 7 3 96FDEA01175 1 19960623 A 5313 STRINGER BOEING 727 727233 138408A NM BS 720 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 257FE 20939 UPPER LOBE, BL 9, 720C, STR 15L CRACKED. REMOVED DAMAGE AND INSTALLED STR SPLICE PER SRM 53-10-3. 2 L 7 3 4F RT A3WE 1996070300013 19960703 00013 NM 1996 7 3 96FDEA01176 1 19960623 A 5315 FLOOR BEAM BOEING 727 727233 138408A NM BS 870 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 257FE 20939 FLOOR BEAM UPPER CHORD UPPER SURFACE CORRODED STA 870, LB 25 - 45, WL 208. REMOVED CORROSION, INSTALLED REPAIR DOUBLER PER 53-10-07-02. 2 L 7 3 4F RT A3WE 1996070300014 19960703 00014 NM 1996 7 3 96FDEA01177 1 19960624 A 5315 FLOOR BEAM BOEING 727 727233 138408A NM BS 344 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 257FE 20939 FLOOR BEAM UPPER CHORD UPPER SURFACE CORRODED AT STA 344 BL ZERO - LBL 60. REMOVED CORROSION ON UPPER CHORD SURFACE - BEYOND LIMITS PER SRM 51-10-6. REMOVED AND REPLACED TOP TEE ANGLE PER SRM 51-10-1. FLOOR BEAM REPAIRED USING FEDEX E ND DRAWING SR 27-53-007. 2 L 7 3 4F RT A3WE 1996070300015 19960703 00015 NM 1996 7 3 96FDEA01178 1 19960618 A 5320 SUPPORT BOEING 727 727233 138408A NM BS 758-848 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 257FE 20939 SEAT TRACK SUPPORT UPPER CHORD UPPER SURFACE CORRODED STA 758-848, LBL 45. REMOVED AND REPLACED SEAT TRACK SUPPORT PER SRM 51-10-01, STA 758 - 848. 2 L 7 3 4F RT A3WE 1996070300016 19960703 00016 NM 1996 7 3 96FDEA01179 1 19960625 A 5320 GUSSET BOEING 727 727123 138404G NM FS 783.5 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 168FE 18865 CABIN INTERIOR - FS 783.5 RIB SUPPORT GUSSET BELOW FLOOR LEVEL, IS CRACKED AT LOWER INBOARD CORNER, JUST ABOVE WING SKIN , CRACK APPROX 1 INCH. CRACKED GUSSET REMOVED, DOUBLER INSTALLED AS PER BOEING SB 727-53-0197. 2 L 7 3 4F A3WE 1996070300017 19960703 00017 NM 1996 7 3 96FDEA01180 1 19960624 A 5315 FLOOR BEAM BOEING 727 72722 1384002 NM BS 344 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 168FE 18865 MAIN CARGO CORROSION ON FLOOR BEAM AT SCREW HOLES FROM LBL 45 - 54, STA 344. REMOVED CORROSION PER SRM 53-10-1. INSTA LLED FLOOR BEAM REPAIR PER SRM 53-10-8 AND EA 7-5310-28760, DATE 6-24-96. 2 L 7 3 4F A3WE 1996070300018 19960703 00018 NM 1996 7 3 96FDEA01181 1 19960624 A 5311 BELL FRAME BOEING 727 727123 138404G NM BS 680 CRACK A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 168FE 18865 FORWARD CARGO CRACK IN BELL FRAME, STA 680 BETWEEN STR 26-27L. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-40-4 , PG 12-17. 2 L 7 3 4F A3WE 1996070300019 19960703 00019 NM 1996 7 3 96FDEA01182 1 19960627 A 5753 652163133 TE WEDGE BOEING 727 72725 1384006 NM LT TE MID FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 NR0707, 050, LEFT WING I/B MID FLAP T/E WEDGE HAS SEVERAL AREAS OF DELAMINATION. *S/D* REPAIRED DAMAGED SKIN TO LEFT W ING I/B MID FLAP IAW FEDEX SRM 51-40-6. 2 L 7 3 4F A3WE 1996070300020 19960703 00020 NM 1996 7 3 96UAL900465 1 19960619 A 3320 61482 BALLAST BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN BURNED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 7295U 21573 RAMP SERVICE REPORTED ELECTRICAL SMELL IN AFT CABIN AND LEFT AFT LAV SMOKE ALARM SOUNDED. *S/D* RIGHT AFT MIRROR BALLAS T BURNED AND REPLACED BALLAST. 2 L 7 3 4F 4 F A3WE E2EA 1996070300021 19960703 00021 WP 1996 7 3 CALA9600893 1 19960605 A 5230 STOP PAD DOUG DC9 DC982 3022082 WP CARGO DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33817 49371 INSPECTION FOUND MID CARGO DOOR LOWER AFT STOP PAD CORRODED. THE CORRODED AREA WAS CUT OUT. A DOUBLER WAS FABRICATED A ND INSTALLED IAW SRM 52-05. 2 L 7 2 4F A6WE 1996070300022 19960703 00022 WP 1996 7 3 CALA9600894 1 19960526 A 5730 9936820508 PANEL DOUG DC9 DC982 3022082 WP RT WING TE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33817 49371 INSPECTION FOUND A 10 INCH CRACK AT OUTBOARD END OF RT WING UPPER TRAILING EDGE PANEL LOWER SURFACE, AFT OF RIGHT GEAR. THE PANEL WAS REMOVED AND REPLACED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1996070300023 19960703 00023 WP 1996 7 3 CALA9600895 1 19960610 A 3350 41B001TD051 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 33817 49371 INSPECTION FOUND OVERWING EMERGENCY LIGHTS INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED. 2 L 7 2 4F A6WE 1996070300024 19960703 00024 NM 1996 7 3 CALA9600896 1 19960522 A 5315 FLOOR BEAM BOEING 727 727232 1384082 NM BS 335 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND A .3750 INCH CRACK AND A .50 INCH CRACK IN FLOORBEAM U-CHANNEL AT B.S. 335, LBL 25, WL 200. THE CHANNE L WAS REMOVED. A NEW CHANNEL WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 53-40-3, AND MM 51-20-11. 2 L 7 3 4F A3WE 1996070300025 19960703 00025 NM 1996 7 3 CALA9600897 1 19960523 A 5315 FLOOR BEAM BOEING 727 727232 1384082 NM BS 380 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 380, RBL 28 TO 59. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10 -8. 2 L 7 3 4F A3WE 1996070300026 19960703 00026 NM 1996 7 3 CALA9600898 1 19960522 A 5315 FLOOR BEAM BOEING 727 727232 1384082 NM BS 1110 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND FLOORBEAM CORRODED AT STA 1110, BL ZERO TO RBL 66. ANGLES, STRAPS, AND CORDS WERE FABRICATED AND INSTA LLED IAW SRM 53-10-8, 51-30-2, AND 51-10-2. 2 L 7 3 4F A3WE 1996070300027 19960703 00027 NM 1996 7 3 CALA9600899 1 19960523 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 1010-1030 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1010-1030, RBL 65. A REPAIR WAS FABRICATED AND INSTALLED IAW 51-30-2, 51 -10-2, AND 51-40-3. 2 L 7 3 4F A3WE 1996070300028 19960703 00028 NM 1996 7 3 CALA9600900 1 19960524 A 5315 FLOOR BEAM BOEING 727 727232 1384082 NM BS 1130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND FLOORBEAM CORRODED AT B.S. 1130, LBL 25. NEW PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-1, 53-10 -8, AND MM 51-20-11. 2 L 7 3 4F A3WE 1996070300029 19960703 00029 NM 1996 7 3 CALA9600901 1 19960605 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 685 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND STRINGER 28R FLANGE CORRODED AT F.S. 685. THE CORRODED SECTION OF STRINGER WAS REMOVED. A NEW STRINGE R AND SPLICE WERE FABRICATED AND INSTALLED IAW SRM 53-10-3. 2 L 7 3 4F A3WE 1996070300030 19960703 00030 NM 1996 7 3 CALA9600902 1 19960525 A 5320 ANGLES BOEING 727 727232 1384082 NM BS 580 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND SKIN ATTACH ANGLES(2) AT BILGE, STA 580, BL ZERO CORRODED. ANGLE DOUBLERS WERE FABRICATED AND INSTALLE D IAW SRM 51-40-3, 51-10-2, 51-30-2, AND MM 51-20-0. 2 L 7 3 4F A3WE 1996070300031 19960703 00031 NM 1996 7 3 CALA9600903 1 19960519 A 5320 GUSSET BOEING 727 727232 1384082 NM BS 950 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND CORRODED GUSSET AT ATTACH STRINGER 30 TO CIRCUMFERENTIAL AT CENTERLINE, STA 950B. A NEW GUSSET WAS FAB RICATED AND INSTALLED IAW SRM 51-10-6, 51-10-3, 51-40-3, 51-30-2, AND 53-10-1. 2 L 7 3 4F A3WE 1996070300032 19960703 00032 NM 1996 7 3 CALA9600904 1 19960519 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 950 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND FLOORBOARD SUPPORT CORRODED AT CENTERLINE ABOVE STRINGER 30, STA 950F AND STA 950E. A REPAIR WAS FABRI CATED AND INSTALLED IAW SRM 51-40-3, 51-30-2, 51-10-2, AND 51-20-2. 2 L 7 3 4F A3WE 1996070300033 19960703 00033 NM 1996 7 3 DHL96724003 1 19960619 A 3510 OXY BOTTLE BOEING 727 727228 NM COCKPIT EMPTY A T DHLA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 724DH 19862 AT ALTITUDE FOUND OXYGEN DEPLETED, FOUND NO REGULATORS VENTING OXYGEN. SERVICED OXYGEN TO FULL, LEAK OPS CHECKS GOOD IA W MM 35-10. 2 L 7 3 4F A3WE 1996070300034 19960703 00034 EU 1996 7 3 QXEA9600219 1 19960624 A 3350 6008905 POWER SUPPLY FOKKER F28 F28MK1000 4990808 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 454US 11107 SEA - RIGHT OVERWING EMERGENCY EXIT LIGHT IS INOP. POWER SUPPLY REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996070300035 19960703 00035 EU 1996 7 3 QXEA9600220 1 19960624 A 3350 MGG1280 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 466US 11075 SEA - EMERGENCY EXIT LIGHT OUT ABOVE COCKPIT ENTRANCE. BULBS WERE REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURN ED TO SERVICE. 2 L 7 2 4F RT A20EU 1996070300036 19960703 00036 NM 1996 7 3 QXEA9600221 1 19960624 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT INOPERATIVE A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 817PH 288 56 BOI - COCKPIT EMERGENCY LIGHT IS INOP. LIGHT WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1996070300037 19960703 00037 NM 1996 7 3 QXEA9600222 1 19960624 A 2121 011189500 FAN DORNER DO32 DO328100 2996000 NM NR 1 MALFUNCTIONED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 09 328PH 1049 3006 SEA - CAS MESSAGE, NR 1 HX FAN INOP AND SMOKE IN CABIN. NR 1 HX FAN REPLACED AND FAN OPS CHECKED GOOD. AIRCRAFT RETURN ED TO SERVICE. 2 H 7 2 4T RT A45NM 1996070300038 19960703 00038 EU 1996 7 3 QXEA9600223 1 19960625 A 3350 5515800106 SIGN FOKKER F28 F28MK1000 4990808 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 452US 11105 GEG - EMERGENCY EXIT SIGN ABOVE ROW 8 IS PARTIALLY ILLUMINATED. SIGN AT ROW 8 REPLACED AND SIGN OPS CHECKED GOOD. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996070300039 19960703 00039 EU 1996 7 3 QXEA9600224 1 19960626 A 3350 MGG1280 BULBS FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 452US 11105 SEA - LIGHT IS INOP INSIDE EXIT SIGN ABOVE COCKPIT DOOR. BULBS WERE REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETU RNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996070300040 19960703 00040 NM 1996 7 3 SWAA960582 1 19960624 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 95SW 23054 DURING WALKAROUND CHECK, FOUND A 2.25 INCH FUSELAGE SKIN CRACK, RIGHT SIDE AFT OF T/E FLAP, NEXT TO BODY FAIRING. REPAI RED PER BOEING SRM. 2 L 7 2 4F A16WE 1996070300041 19960703 00041 NM 1996 7 3 SWAA960583 1 19960624 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 86SW 22827 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN DENTED AT THE FOLLOWING LOCATIONS: BS 823, AT S26L, BS 341 AT S25R, BS 50 4, BETWEEN 21R AND 22R, BS 203, 4 INCHES ABOVE S23L, BS 947, AT S19L AND AT BS 891, S25R. REPAIRED ALL PER BOEING SRM. 2 L 7 2 4F A16WE 1996070300042 19960703 00042 NM 1996 7 3 SWAA960584 1 19960624 A 5320 CLIP BOEING 737 7372H4 138448C NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 86SW 22827 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 727B, S18R AND S20R. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996070300043 19960703 00043 NM 1996 7 3 SWAA960585 1 19960624 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 86SW 22827 DURING SCHEDULED D CHECK, FOUND BULKHEAD SUPPORT ANGLE CRACKED AT BS 727+8, WL 156 BL ZERO-LBL 5. REPAIRED PER BOEING S RM. 2 L 7 2 4F A16WE 1996070300044 19960703 00044 NM 1996 7 3 SWAA960586 1 19960624 A 5312 BULKHEAD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 86SW 22827 DURING SCHEDULED D CHECK, FOUND BULKHEAD BS 178 CRACKED AT WL 218, RBL 7 TO 12, AND AT RBL 9.5 TO 12. REPAIRED PER BOEI NG SRM. 2 L 7 2 4F A16WE 1996070300045 19960703 00045 NM 1996 7 3 SWAA960587 1 19960624 A 5315 FLOOR BEAM BOEING 737 7372H4 138448C NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 86SW 22827 DURING SCHEDULED D CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 344, LBL 7 TO 10, AND AT RBL 2 TO 31. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996070300046 19960703 00046 NM 1996 7 3 SWAA960588 1 19960624 A 5320 SPLICE BOEING 737 7372H4 138448C NM BS 907 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 86SW 22827 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CORRODED AT BS 907+5. REPAIRED PER BOEING SRM AND BOEING T1-A51-004. 2 L 7 2 4F A16WE 1996070300047 19960703 00047 NM 1996 7 3 SWAA960589 1 19960624 A 5315 FLOOR BEAM BOEING 737 7372H4 138448C NM BS 1006-1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 86SW 22827 DURING SCHEDULED D CHECK, FOUND FLOORBEAM CHORD CORRODED AROUND FASTENER HOLES BETWEEN BS 1006 AND 1016, WL 208, UNDER W EB. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996070300048 19960703 00048 NM 1996 7 3 SWAA960590 1 19960624 A 5320 CHORD BOEING 737 7372H4 138448C NM BS 986.6-1006 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 86SW 22827 DURING SCHEDULED D CHECK, FOUND FLOORBEAM ANGLED CHORD CORRODED AROUND FASTENER HOLES BETWEEN BS 1006 AND 986.5, WL 208, LBL 10 TO 19. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996070300049 19960703 00049 EA 1996 7 3 SWIA95746 1 19960615 A 7931 OIL PRESS SWITCH CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LT ENGINE FAILED A SWIA D RETURN TO BLOCK O OTHER CL CLIMB 1 NM 07 412SW 7101 LEFT ENGINE OIL PRESSURE INDICATION DROPPED TO 0 ON CLIMBOUT. OIL TEMPERATURE REMAINED NORMAL AND NO EICAS MESSAGES APP EARED. REPLACED LEFT ENGINE OIL PRESSURE SWITCH, RAN ENGINE. OPS CHECK GOOD, NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A21EA E15NE 1996070300050 19960703 00050 NM 1996 7 3 UPS96220489 1 19960618 A 5347 SEAT TRACK BOEING 727 72751C 1384015 NM BS 1130-1136 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 903UP 18945 INSPECTION TYPE: C. STA 1130-1136, RBL 62 SEAT TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED, AND INSTALLED SEAT TRA CK PER SRM 51-10-01 AND 51-30-02. 2 L 7 3 4F A3WE 1996070300051 19960703 00051 NM 1996 7 3 UPS96220490 1 19960612 A 5320 TORQ BOX WEB BOEING 727 72751C 1384015 NM FS 1256 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 903UP 18945 INSPECTION TYPE: C. LOWER TORQUE BOX INBD WEB (RT) BS 1256 IS CRACKED AT THE LOWER LIGHTENING HOLE APPROXIMATELY .2 IN CH LONG. REMOVED DAMAGE PER SRM 51-40-02, FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 51-40-02 AND 51-30-02. 2 L 7 3 4F A3WE 1996070300052 19960703 00052 NM 1996 7 3 UPS96220491 1 19960618 A 5754 SKIN BOEING 727 72751C 1384015 NM NR 6 LE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 903UP 18945 INSPECTION TYPE: C. RT WING NR 6 K-FLAP IS CORRODED BEYOND ALLOWABLE LIMITS, L/E STA 286.667. REMOVED CORROSION FOUND BEYOND LIMITS. REPAIR IAW 57-50-03. 2 L 7 3 4F A3WE 1996070300053 19960703 00053 NM 1996 7 3 UPS96220492 1 19960618 A 5311 FRAME BOEING 727 72751C 1384015 NM BS 351 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 903UP 18945 INSPECTION TYPE: C. FS 351 BETWEEN STR 26R AND 26L FRAME LOWER TEE WAS FOUND TO BE BEYOND LIMITS. AFTER CORROSION REM OVAL ON NR 571011. REMOVED AND REPLACED LOWER TEE FRAME AT STA 351 BETWEEN STR 26R AND 26L PER SRM 57-30-02. 2 L 7 3 4F A3WE 1996070300054 19960703 00054 NM 1996 7 3 UPS96220493 1 19960620 A 5320 SHEAR WEB BOEING 727 72751C 1384015 NM BS 1174-1180 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 903UP 18945 INSPECTION TYPE: C. MAIN CABIN EXFOLIATED CORROSION ON SHEAR WEB STA 1174-1180, RBL 25. CUT OUT DAMAGED AREA AND REPA IRED WEB PER SRM 51-40-2. 2 L 7 3 4F A3WE 1996070300055 19960703 00055 NM 1996 7 3 UPS96220494 1 19960613 A 5754 STIFFENERS BOEING 727 72751C 1384015 NM NR 2 SPOILER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 903UP 18945 INSPECTION TYPE: C. LEFT WING AFT SPAR HOLES WORN IN VERTICLE STIFFENERS AT NR 2 SPOILER ACTUATOR FITTING LOWER ATTACH BOLTS. REMOVED AND REPLACED STIFFENERS IAW SRM 57-10-2 51-10-1, AND 51-30-2. 2 L 7 3 4F A3WE 1996070300056 19960703 00056 NM 1996 7 3 UPS96220495 1 19960614 A 5754 ANGLE BOEING 727 72751C 1384015 NM NR 3 SLAT SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 903UP 18945 INSPECTION TYPE: C. LT WING FRONT SPAR VERTICAL STIFFENER L/E RIB ATTACH ANGLE CRACKED AT NR 3 SLAT O/B TRACK O/B ROLL ER MOUNT RIB. REMOVED VERTICAL STIFFENER ON NR 3 SLAT TRACK ATTACH ANGLE. REPLACED PER SRM 51-10-1, 51-30-2. 2 L 7 3 4F A3WE 1996070300057 19960703 00057 NM 1996 7 3 UPS96220496 1 19960614 A 5754 ANGLE BOEING 727 72751C 1384015 NM NR 3 SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 903UP 18945 INSPECTION TYPE: C. LT WING FRONT SPAR VERTICAL STIFFENER/RIB ATTACH ANGLE IS CRACKED AT NR 3 SLAT O/B TRACK I/B ROLLE R MOUNT RIB. REMOVED AND REPLACED STIFFENER ANGLE IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996070300058 19960703 00058 NM 1996 7 3 UPS96220497 1 19960621 A 5751 ROD FITTING BOEING 727 72751C 1384015 NM OUTBD AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 903UP 18945 INSPECTION TYPE: C. RT O/B AILERON BUSS ROD FITTING ON AILERON L/E IS CRACKED. INSTALLED REPLACEMENT FITTING IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996070300059 19960703 00059 NM 1996 7 3 UPS96220498 1 19960614 A 5754 ANGLE BOEING 727 72751C 1384015 NM N 3 SLAT TRACK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 903UP 18945 INSPECTION TYPE: C. LT WING FRONT SPAR VERTICLE STIFFENER/RIB ATTACH ANGLE CRACKED AT NR 3 SLAT I/B TRACK I/B ROLLER M OUNTING RIB. REMOVED AND REPLACED STIFFENER ANGLE IAW DWG 65-16200 AND SRM 57-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 1996070300060 19960703 00060 NM 1996 7 3 UPS96220499 1 19960614 A 5320 DOOR FRAME CLIP BOEING 727 72751C 1384015 NM BS 550 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 903UP 18945 INSPECTION TYPE: C. MAIN CARGO DOOR AT STA 550 UPPER END STR 3L. FRAME TO DOOR FRAME CLIP IS CRACKED. REMOVED AND RE PLACED CLIP IAW SRM 51-30-2 AND 51-10-1. 2 L 7 3 4F A3WE 1996070300061 19960703 00061 NM 1996 7 3 UPS96220500 1 19960614 A 5320 DOOR FRAME CLIP BOEING 727 72751C 1384015 NM BS 550 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 903UP 18945 INSPECTION TYPE: C. MCD STA 540, UPPER END AT SBL, THE BELT FRAME TO DOOR FRAME CLIP IS CRACKED. REMOVED, FABRICATED, AND INSTALLED CLIP PER DWG 69-24114 AND 51-30-2. 2 L 7 3 4F A3WE 1996070300062 19960703 00062 NM 1996 7 3 UPS96220501 1 19960622 A 5315 FLOOR BEAM BOEING 727 72751C 1384015 NM BS 344 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 903UP 18945 INSPECTION TYPE: C. CORROSION ON FLOOR BEAM UPPER CAP, STA 344, BL ZERO TO LBL 30. REMOVED CORRODED STA 344 FLOOR BEA M UPPERCAP FROM RBL 8 TO LBL 66 AND REPAIRED FLOOR BEAM IAW SRM 53-10-8, FIG 9. 2 L 7 3 4F A3WE 1996070300063 19960703 00063 NM 1996 7 3 UPS96220502 1 19960622 A 5754 ATTACH ANGLE BOEING 727 72751C 1384015 NM NR 4 SLAT TRACK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 903UP 18945 INSPECTION TYPE: C. LT WING FROM SPAR VERTICAL STIFFENER/RIB ATTACH ANGLE IS CRACKED AT RT SLAT O/B TRACK I/B ROLLER M OUNTING RIB. REMOVED, FABRICATED, AND INSTALLED NEW STIFFENER IAW DWG 65-16200 AND SRM 51-30-2 AND 57-10-3. 2 L 7 3 4F A3WE 1996070300064 19960703 00064 NM 1996 7 3 UPS96220503 1 19960617 A 5347 SEAT TRACK BOEING 727 72751C 1384015 NM BS 552 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 903UP 18945 INSPECTION TYPE: C. MAIN CABIN SEAT TRACK STA 552, RBL 62 TRACK WAS FOUND BEYOND LIMITS DUE TO CORROSION REMOVAL. REMO VED DAMAGED SECTION OF SEAT TRACK AND INSTALLED NEW SECTION IAW SRM 53-10-5 FIG 1 AND 51-30-2. 2 L 7 3 4F A3WE 1996070300065 19960703 00065 NM 1996 7 3 UPS96220504 1 19960614 A 5754 ATTACH RIB BOEING 727 72751C 1384015 NM NR 4 SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 903UP 18945 INSPECTION TYPE: C. NR 4 SLAT O/B ACTUATOR ATTACH RIB CRACKED IN THREE PLACES. STOP DRILLED CRACKS AND INSTALLED DOUB LER PER SRM 51-40-2 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996070300066 19960703 00066 NM 1996 7 3 UPS96220505 1 19960617 A 5347 SEAT TRACK BOEING 727 72751C 1384015 NM BS 378 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 903UP 18945 INSPECTION TYPE: C. CORROSION ON SEAT TRACK IN 3 AREAS THAT ARE OUT OF LIMITS AT STR 378, LBL 45.5. REMOVED AND REPLA CED SEAT TRACK FROM STA 344-390 IAW SRM 53-10-5 AND 51-30-2. 2 L 7 3 4F A3WE 1996070300067 19960703 00067 NM 1996 7 3 UPS96220506 1 19960621 A 5730 SKIN BOEING 727 72751C 1384015 NM WS 870 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 903UP 18945 INSPECTION TYPE: C. CENTER WING SKIN RT AFT CORNER ADJACENT TO STA 870 SEAL DEPRESSOR HAD CORROSION. REPAIRED AREA IA W DHC SK 903-060 AN DSRM 57-00-00. 2 L 7 3 4F A3WE 1996070300068 19960703 00068 1996 7 3 VNAA9606012 4 19960624 A 2360 SB30134 STATIC WICK DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT WING DAMAGED A VNAA K NONE O OTHER CR CRUISE 1 GL 07 426JS 3038 CREW REPORTED ENCOUNTERING TWO LIGHTNING STRIKES WHILE EN ROUTE FROM PIT TO IPT. AIRCRAFT CONTINUED ON AND LANDED IPT W ITHOUT FURTHER INCIDENT. AIRCRAFT LATER FERRIED TO PIT WHERE MX INSPECTED THE AIRCRAFT I.A.W. M.M. 05-51-12. DETECTED SMALL BURN MARKS ON RADOME RIVETS AND TWO STATIC WICKS MISSING FROM LEFT WING TIP. CLEANED BURN MARKS FROM THE RADOME ( NO FURTHER DAMAGE DETECTED) AND REPLACED THE STATIC WICKS. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996070300086 19960703 00086 NM 1996 7 3 96ZZZX3262 1 19960108 A 6322 900D3448004103 IMPELLER DOUG MD900 MD900 3027375 NM BLOWER WORN A S R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 298 90000012 IMPELLER WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1996070300087 19960703 00087 NM 1996 7 3 96ZZZX3263 1 19960523 A 3350 P4010020 BATTERY PACK GRIMES P4010020 BOEING 727 727231 1384079 NM R1 DOOR DISCHARGED A P9IA K NONE L NO TEST IN INSP/MAINT 1 SO 03 74318 2473 20051 R1 DOOR SLIDE LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPS CHECKS GOOD. MM 33-50-00. 2 L 7 3 4F A3WE 1996070300088 19960703 00088 EA 1996 7 3 96ZZZX3264 1 19960418 A 2750 12251 GEARBOX DHAV DHC7 DHC7102 2802708 EA LT TE FLAP WORN A A CICA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SO 17 25AG 25 MIA/PID - FLT 4925 - DURING TAXI, PILOT REPORTED FORE FLAP CAUTION LIGHT ILLUMINATED. THE AIRCRAFT WAS INSPECTED AND FO UND SAFE FOR FERRY FLIGHT TO FLL MAINTENANCE BASE. FLAPS WERE SET AT 15 DEGREES AND AIRCRAFT FERRIED. MAINTENANCE FOUN D BOTH 90 DEGREE BOXES (LT FWD AND LT AFT) TO HAVE EXCESSIVE PLAY. BOTH 90 DEGREE BOXES WERE REMOVED AND REPLACED. LOA D SENSOR GEARBOX ALSO WAS REMOVED AND REPLACED DUE TO PLAY. OPERATIONAL CHECK GOOD AND AIRCRAFT RETURNED TO SERVICE. 2 H 7 4 4T A20EA 1996070300089 19960703 00089 NM 1996 7 3 96ZZZX3265 1 19960320 A 3350 3314025 BATTERY PACK BOEING 727 727227 1384078 NM CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 783AT 011802 22000 IND - 1L EMERGENCY BATTERY PACK OK IN MANUAL, INOP IN AUTO. REMOVED AND REPLACED 1L DOOR EMERGENCY LIGHTS BATTERY PACK IAW MM CHAPTER 33, OPS CHECK OK. 2 L 7 3 4F A3WE 1996070300090 19960703 00090 NM 1996 7 3 96ZZZX3266 1 19960529 A 2910 65445815 VALVE BOEING 737 737201 1384454 NM A HYD SYSTEM FAILED A F3LA O OTHER J WARNING INDICATION LD LANDING 1 NM 03 205AU 19421 DEN - FLT 546 - AFTER TOUCHDOWN, FLIGHT CREW REPORTED A-SYSTEM HYDRAULIC PRESSURE FLUCTUATING AND LOSS OF NOSE WHEEL STE ERING. TOWED AIRCRAFT TO GATE. REPLACED LEFT HYDRAULIC SHUT OFF VALVE, CASE DRAIN FILTER AND PRESSURE FILTER AND SYSTE M CHECKED OKAY. TOTAL TIME AIRFRAME, 69,487.3 HRS. 2 L 7 2 4F A16WE 1996070300091 19960703 00091 WP 1996 7 3 96ZZZX3267 1 19960506 A 5350 FLAPPER DOOR DOUG DC9 DC932 3022066 WP TAIL COMPT DIRTY A VJ6A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 945VV 47238 ATL/ATL - FLT 233 - AIR RETURN, THE TAIL COMPARTMENT HIGH LIGHT ILLUMINATED INTERMITTENTLY AFTER TAKEOFF. CLEANED TAIL VENT FLAPPER DOOR. 2 L 7 2 4F A6WE 1996070300092 19960703 00092 WP 1996 7 3 96ZZZX3268 1 19960523 A 2170 21D101 COALESCER BAG DOUG DC9 DC983 3022083 WP CABIN DIRTY A TWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 05 9305N 49395 MCI - FLT 667 - DURING CLIMB WHEN ENGINE ANTI-ICE WAS TURNED ON, A BURNING ODOR WAS NOTICED IN THE CABIN. TURNED OFF EN GINE ANTI-ICE. FOUND DIRTY COALESCER, MFG PN 21D10-1. REPLACED BOTH COALESCERS. AIR CONDITIONING SYSTEM THEN CHECKED NORMAL. OP-16 - 2-16-96 - TUS. 2 L 7 2 4F RT A6WE 1996070300093 19960703 00093 NM 1996 7 3 96ZZZX3269 1 19960413 A 5712 RIB BOEING 727 727231 1384079 NM WS 629 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54325 20232 DURING CHECK C-4D, FOUND A .75 INCH CRACK IN RT WING LOWER AFT END OF RIB, WS 629. INSTALLED AND SECURED RIB REPAIR PER SRM 57-10-05, PAGES 6, 7, AND 8. AIRCRAFT TOTAL TIME: 63,700 HOURS; 42,677 CYCLES. 2 L 7 3 4F A3WE 1996070300094 19960703 00094 NM 1996 7 3 96ZZZX3270 1 19960413 A 5313 STRINGER BOEING 727 727231 1384079 NM BS 656.5 BROKEN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54325 20232 DURING CHECK C-4D, FOUND ATTACHED LEG BROKEN OFF STR 13, STA 656.5. REPAIRED PER SB 727-57A159. AIRCRAFT TOTAL TIME: 6 3,700 HOURS; 42,677 CYCLES. 2 L 7 3 4F A3WE 1996070300095 19960703 00095 NM 1996 7 3 96ZZZX3271 1 19960413 A 5712 RIB BOEING 727 727231 1384079 NM WS 738.5 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54325 20232 DURING CHECK C-4D, FOUND A 1 INCH CRACK IN RIGHT WING LOWER FORWARD END OF RIB AT RADIUS, WS 738.5. REPAIRED PER SRM 57 -10-05. AIRCRAFT TOTAL TIME: 63,700 HOURS; 42,677 CYCLES. 2 L 7 3 4F A3WE 1996070300096 19960703 00096 NM 1996 7 3 96ZZZX3272 1 19960413 A 5712 RIB BOEING 727 727231 1384079 NM WS 656.5 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54325 20232 DURING CHECK C-4D, FOUND RIB CRACKED AT SECOND HOLE ON BOTTOM, STA 656.5. REPAIRED PER SRM 57-10-05, PAGE 6, FIGURE 2. AIRCRAFT TOTAL TIME: 63,700 HOURS; 42,677 CYCLES. 2 L 7 3 4F A3WE 1996070300097 19960703 00097 NM 1996 7 3 96ZZZX3273 1 19960413 A 5712 RIB BOEING 727 727231 1384079 NM WS 656.5 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54325 20232 DURING CHECK C-4D, FOUND A 1.50 INCH CRACK IN LEFT WING LOWER AFT END OF RIB, WS 656.5. REPAIRED PER SRM 57-10-05, FIGU RE 2, SHEET 3. AIRCRAFT TOTAL TIME: 63,700 HOURS; 42,677 CYCLES. 2 L 7 3 4F A3WE 1996070300098 19960703 00098 WP 1996 7 3 96ZZZX3274 1 19960322 A 7722 BAL RESISTOR DOUG DC9 DC921 302205A WP NR 2 ENGINE OUT OF ADJUST A VJ6A C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 11 128NK 47307 BOS/BOS - FLT 361 - ABORTED TAKEOFF, NR 2 ENGINE EGT WAS ERRATIC. THE NR 2 ENGINE EGT GAUGE STOPS AT APPROXIMATELY 350 DEGREES WHEN TAKEOFF POWER WAS APPLIED. FOUND THE BALANCING RESISTOR OUT OF TOLERANCE. ADJUSTED IAW MM 77-20-0, PAGE 2 01. RAN ENGINES TO TAKEOFF POWER, CHECKS NORMAL. 2 L 7 2 4F A6WE 1996070300099 19960703 00099 WP 1996 7 3 96ZZZX3275 1 19960502 A 8110 259115 BLOWER DOUG DC6 C118A 3021710 WP PWA R2800 R280052W 52026 NE NR 4 ENGINE WORN A X5CA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SW 11 351CE 16982 1946 44599 NK510222 ABORTED TAKEOFF, NR 4 MANIFOLD PRESSURE ONLY 28 INCHES. 2 L 7 4 4R 4 R 6A3 5E8 1996070300100 19960703 00100 NE 1996 7 3 96ZZZX3276 2 19960413 A 7414 10884501 DISTRIBUTOR DOUG DC6 C118A 3021710 WP PWA R2800 CB16 52026 NE NR 2 ENGINE MALFUNCTIONED A X5CA E ENGINE SHUTDOWN E VIBRATION/BUFFET CR CRUISE 1 SW 11 351CE 1156 44599 35863 SHUT DOWN NR 2 ENGINE DUE TO ROUGHNESS (21172). 2 L 7 4 4R 4 R 6A3 E264 1996070300101 19960703 00101 WP 1996 7 3 AALA960642 1 19960425 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1309 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 279AA 49295 TUL - NR 3 SEAT TRACK HAS CORROSION AT STA 1309. INSTALLED SEAT TRACK PLUG PER SRM 53-05, FIGURE 4A. TST: 32,944 HRS . CYCLES, 18,910. (X) 2 L 7 2 4F A6WE 1996070300102 19960703 00102 WP 1996 7 3 AALA960643 1 19960425 A 5320 3957317501 BRACKET DOUG DC9 DC982 3022082 WP BS 1155 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 279AA 49295 TUL - CORROSION FLOORBOARD BRACKET. REPLACED BRACKET. TST: 32,944 HRS. CYCLES, 18,910. (X) 2 L 7 2 4F A6WE 1996070300103 19960703 00103 WP 1996 7 3 AALA960676 1 19960429 A 5347 500201 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1203-1212 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 279AA 49295 TUL - CORROSION ON NR 3 SEAT TRACK BELOW GALLEY 4A AND 4B. CORROSION WAS BLENDED OUT AND FOUND TO BE OUT OF LIMITS. SE AT TRACK PLUG WAS INSTALLED PER SRM 53-05, FIGURE 4A, TREATED WITH ALODINE WHERE APPLICABLE AND FRAME PRIMED. TST: 32, 944 HRS. CYCLES, 18,910. (X) 2 L 7 2 4F A6WE 1996070300104 19960703 00104 WP 1996 7 3 AALA960690 1 19960429 A 3260 INDICATION LIGHT DOUG DC9 DC983 3022083 WP LANDING GEAR MALFUNCTIONED A AALA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 433AA 49451 SFO - FLT 1801 - DURING APPROACH TO SFO WHEN LANDING GEAR EXTENDED, UNSAFE INDICATION ON ALL 3 LANDING GEARS. ACCOMPLIS HED EMERGENCY GEAR EXTENSION CHECKLIST AND OBTAINED 3 GREEN LIGHTS FOLLOWED BY LIGHTS RETURNING TO RED WHEN EMERGENCY GE AR EXTENSION LEVER WAS STOWED. AIRCRAFT LANDED SFO WITHOUT INCIDENT WITH GEAR EXTENSION LEVER NOT STOWED. CHECKED LAND ING GEAR PROXIMITY SENSORS AND BITE CHECKED PROXIMITY SWITCH CONTROL UNIT WITH NO DEFECTS FOUND. CHECKED S1-89 SWITCH A ND THROTTLE SWITCHES S1-319 AND S1-320 WITH NO DEFECTS FOUND. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECT S FOUND. SYSTEM GROUND CHECKED, NORMAL OPER. UNABLE TO DUPLICATE PROBLEM AND ACFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A6WE 1996070300105 19960703 00105 WP 1996 7 3 AALA960697 1 19960429 A 5320 CLIP DOUG DC9 DC982 3022082 WP BS 1212-1217 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 279AA 49295 TUL - CORROSION ON CLIP ATTACHED TO SKIN (BOTTOM LEG OF INTERCOSTAL) STA 1212 TO STA 1217. TST: 32,944 HRS. CYCLES, 1 8,910. (X) 2 L 7 2 4F A6WE 1996070300106 19960703 00106 WP 1996 7 3 AALA960737 1 19960506 A 2170 21D101 COALESCER DOUG DC9 DC982 3022082 WP ACM BAY DIRTY A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 459AA 49564 ORD - FLT 0333 - AFTER TAKEOFF LGA DURING INITIAL CLIMB-OUT, LIGHT SMOKE AND FUMES NOTED IN CABIN. CONDITION CLEARED WI THIN SEVERAL MINUTES WITH NO CREW ACTION REQUIRED. AIRCRAFT PROCEEDED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED AIR CYCLE MACHINE COALESCER BAGS. ACCOMPLISHED PACK BURN-OUT PROCEDURE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1996070300107 19960703 00107 WP 1996 7 3 AALA960764 1 19960512 A 3260 368658188117 ANNUNCIATOR KORRY DOUG DC9 DC983 3022083 WP RT MLG DEFECTIVE A AALA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 SW 07 438AA 49456 MIA - FLT 0725 - DURING APPROACH TO MIA WHEN LANDING GEAR EXTENDED, RT MLG HAD NO INDICATION. ACCOMPLISHED TOWER FLY-BY AND VISUALLY CONFIRMED RT MLG EXTENDED. AIRCRAFT LANDED MIA WITHOUT INCIDENT. REPLACED LANDING GEAR ANNUNCIATOR PANEL . ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A6WE 1996070300108 19960703 00108 CE 1996 7 3 COEA9696501 1 19960503 A 2842 GF550082 SENSOR CESSNA 208 208B 2073701 CE FUEL RESERVOIR FAILED A COEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 13 965FE 208B0084 FUEL RESERVOIR LOW LEVEL LIGHT ILLUMINATED IN CRUISE. AIRCRAFT DECLARED EMERGENCY, RETURNED TO MTY, AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT SYSTEM IAW CESSNA FIELD SERVICE NOTE 95-21 DATED JUNE 22, 1995, AND FOUND FUEL RESERV OIR LOW LEVEL SENSOR HAD FAILED. MAINTENANCE REMOVED AND REPLACED SENSOR. SYSTEM OPERATION CHECKS GOOD. (X) 1 H 7 1 3T A37CE 1996070300109 19960703 00109 CE 1996 7 3 GLBA96065 1 19960403 A 3233 11238002223 ACTUATOR BEECH 1900 1900C 1154161 CE NLG MALFUNCTIONED A GLBA O OTHER P NO WARNING INDICATION LD LANDING 1 CE 01 130UE 193 UC130 SPI - CREW OBSERVED NOSE GEAR POSITION LIGHT WAS NOT ILLUMINATED WITH GEAR SELECTED DOWN. THEY MADE AN UNEVENTFUL LANDI NG. MAINTENANCE REMOVED AND REPLACED NOSE LANDING GEAR ACTUATOR. LEAK CHECK AND OPS CHECK WERE GOOD. (X) 2 L 7 2 4T RT A24CE 1996070300110 19960703 00110 SW 1996 7 3 MALA964988 1 19960510 A 2730 2743042001 BUSHING SWRNGN SA227 SA227AC 8780603 SW RT ELEVATOR LOOSE A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 863MA AC650B MSP - DURING INSPECTION, MAINTENANCE FOUND THE RT BUSHING LOOSE IN ELEVATOR AFT SPAR FITTING, PN 27-43042-001. REPAIRS WERE COMPLETED BY REAMING BUSHING HOLE IN FITTING, FABRICATING AND INSTALLING BUSHING MADE TO NAS75 STANDARDS. ALL WORK DONE IAW EA 01-96034. (X) 2 L 7 2 4T RT A8SW 1996070300111 19960703 00111 NE 1996 7 3 RAIA960515 2 19960510 A 7510 39702022 VALVE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE NR 2 ENG AI FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 567HK 190 41085 76104 STL - FLT 7213 - NR 2 ENGINE ANTI-ICE FAULT. REPLACED ANTI-ICE VALVE. (X) 2 L 7 2 4T 4 T RT A41NM E18NE 1996070300112 19960703 00112 EU 1996 7 3 RAIA960520 1 19960512 A 2422 PC125123B STATIC INVERTER JETAIR JETSTM JETSTM4101 1500501 EU NOSE FAILED A RAIA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 CE 03 560HK 878 41076 JFK - FLT 7792 - INVERTER FAILED IN-FLIGHT. MAINTENANCE REPLACED THE INVERTER CIRCUIT BREAKER, AND REPLACED THE MAIN ST ATIC INVERTER. (X) 2 L 7 2 4T RT A41NM 1996070300113 19960703 00113 EU 1996 7 3 SIMA961151 1 19960424 A 3350 330151 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 375AE 1100 340B375 DFW - FLT 3589 - EMERGENCY LIGHT IN MIDDLE OF AISLE IS INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY 20LN. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1996070300114 19960703 00114 EU 1996 7 3 SIMA961312 1 19960510 A 3350 LIGHTS SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 375AE 340B375 DFW - FLT 3582 - FLOOR LIGHTING AT SEAT 8A NOT ATTACHED AND LIGHTS INOPERABLE. MEL'D PER 33-15-3. (X) 2 L 7 2 4T RT A52EU 1996070300115 19960703 00115 NE 1996 7 3 SIMA961361 2 19960515 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LEFT FAILED A SIMA E ENGINE SHUTDOWN J WARNING INDICATION LD LANDING 1 SW 21 388AE 296 340B388 GEE785630 FYV - FLT 3687 - DURING LANDING ROLL-OUT, CAPTAIN REPORTED GETTING LEFT OVERTEMP, CHIP DETECTOR, AND OIL PRESSURE WARNIN GS. ENGINE SHUT DOWN. REMOVED AND REPLACED ENGINE. AIRCRAFT WAS RETURNED TO SERVICE. PART TOTAL CYCLES, 288. (X) 2 L 7 2 4T 4 T RT A52EU E8NE 1996070300116 19960703 00116 EU 1996 7 3 SIMA961472 1 19960526 A 3350 3012001 BATTERY PACK AEROSP ATR72 ATR72202 8680940 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 252AM 232 253 DFW - FLT 3716 - WITH BOTH ENGINES RUNNING, F/A REPORTS HALF THE EMERGENCY LIGHTS (PATH LIGHTING EXIT LIGHTS) ON. AFT P ART OF THE CABIN CAME ON WITH EMERGENCY LIGHT SWITCH IN COCKPIT IN ARM POSITION. IT TAKES REPEATED CYCLES OF THE SWITCH TO GET THE LIGHTS TO STAY OFF IN THE ARM POSITION. THIS OCCURRED WHILE TAXIING. REPAIRED EMERGENCY BATTERY AT 62WL. A IRCRAFT WAS RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1996070300117 19960703 00117 EU 1996 7 3 SIMA961561 1 19960604 A 3350 330150 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 375AE 1094 340B375 DFW - FLT 3911 - EMERGENCY LIGHT AT ROW 8 INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1996070300138 19960703 00138 WP 1996 7 3 96ZZZX3297 1 19960509 A 2822 BOOST PUMP DOUG DC9 DC982 3022082 WP CENTER FUEL TANK DEFECTIVE A ASAA O OTHER X ENGINE FLAMEOUT DE DESCENT 1 NM 01 953AS 49386 SEA - DURING DESCENT OF FLT 557, THE LT ENGINE SHUT DOWN. THE LT FUEL TANK TRANSFERRED FUEL INTO THE CENTER TANK WITH T HE CENTER TANK FUEL BOOST PUMPS OFF. THE CENTER TANK FUEL BOOST PUMPS WERE TURNED ON AND FUEL TRANSFERRED BACK INTO THE LT TANK. THE LT ENGINE WAS RESTARTED AND OPERATED NORMALLY. REFERENCE: OPERATOR CONTROL ASAA9680115. 2 L 7 2 4F A6WE 1996070300139 19960703 00139 NM 1996 7 3 96ZZZX3298 1 19960613 A 3350 BPS73 BATTERY CHARGER BOEING 737 7374Q8 NM CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 771AS 25104 JNU - DURING MAINTENANCE CHECK, SECTIONS OF THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPAIRED BROK EN WIRING, REPLACED LAMP BASE ASSEMBLIES, REPLACED BATTERY CHARGER AND ALL LIGHTS OPERATED NORMALLY. REFERENCE: OPERAT OR CONTROL NR ASAA9640045. 2 L 7 2 4F RT A16WE 1996070300140 19960703 00140 1996 7 3 AALA9680126 4 19960529 A 2565 D29982121 EMERG EVAC SLIDE DOUG DC9 DC982 3022082 WP R1 DOOR FAILED TEST A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 957AS 49126 OAK - DURING 15K CHECK, THE R1 DOOR EMERGENCY EVACUATION SLIDE EMERGENCY LIGHTS FAILED TEST. REPLACED THE R1 DOOR EMERG ENCY EVACUATION SLIDE. (X) 2 L 7 2 4F A6WE 1996070300141 19960703 00141 NM 1996 7 3 ASAA9610068 1 19960531 A 3350 6005401 BATTERY BOEING 737 737298C 1384490 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 ANC - DURING MAINTENANCE CHECK, THE RT OVER WING EXTERIOR EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. REPLACED BATTER Y AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1996070300142 19960703 00142 NM 1996 7 3 ASAA9610072 1 19960608 A 3350 883200312 BATTERY PACK BOEING 737 737290C 138448V NM PALLET 8-7 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS ON PALLET 8-7 WERE FOUND INOPERATIVE. REPLACED RE CEIVER AND BATTERY PACK HOUSING AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F A16WE 1996070300143 19960703 00143 NM 1996 7 3 ASAA9610073 1 19960610 A 3350 86210144 BATTERY BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING MAINTENANCE CHECK, THE TRACK AND EMERGENCY LIGHTING WAS FOUND INOPERATIVE IN SEGMENTS. REPLACED BATTERY AT SMOKE BARRIER EMERGENCY EXIT LIGHT ASSEMBLY AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F A16WE 1996070300144 19960703 00144 NM 1996 7 3 ASAA9640042 1 19960530 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 771AS 25104 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 15-18. RECONNECTED LOOSE WIRES AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1996070300145 19960703 00145 NM 1996 7 3 ASAA9640043 1 19960528 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 772AS 25105 SEA - FLT 8 - CREW REPORTED AFT SECTION OF EMERGENCY EXIT FLOOR TRACK LIGHTS WAS DAMAGED AND INOPERATIVE. RECONNECTED L OOSE TRACK WIRES AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1996070300146 19960703 00146 NM 1996 7 3 ASAA9640044 1 19960613 A 3397 WIRE BOEING 737 7374Q8 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 765AS 25102 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE FROM ROW 27 AFT. RECONNECT ED LOOSE WIRE AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1996070300147 19960703 00147 NM 1996 7 3 ASAA9640045 1 19960613 A 3350 S417N50914 LAMP BASE ASSY BOEING 737 7374Q8 NM CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 771AS 25104 JNU - DURING MAINTENANCE CHECK, SECTIONS OF THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPAIRED BROK EN WIRING, REPLACED LAMP BASE ASSEMBLIES, REPLACED BATTERY CHARGER AND ALL LIGHTS OPERATED NORMALLY. REFERENCE: OPERAT OR CONTROL NR 96ZZZX3298. (X) 2 L 7 2 4F RT A16WE 1996070300148 19960703 00148 NM 1996 7 3 ASAA9640046 1 19960613 A 3350 BAS23 BATTERY BOEING 737 737490 1384715 NM L2 DOOR SLIDE DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 767AS 27081 SEA - DURING DEPLOYMENT OF L2 DOOR SLIDE FOR TRAINING, THE EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REMOVED AND REPLACE D BATTERY AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1996070300149 19960703 00149 WP 1996 7 3 ASAA9680115 1 19960509 A 2820 712081 CHECK VALVE DOUG DC9 DC982 3022082 WP CENTER FUEL TANK DEFECTIVE A ASAA O OTHER X ENGINE FLAMEOUT DE DESCENT 1 NM 01 953AS 49386 SEA - DURING DESCENT OF FLT 557, THE LT ENGINE SHUT DOWN. THE LT FUEL TANK TRANSFERRED FUEL INTO THE CENTER TANK WITH T HE CENTER TANK FUEL BOOST PUMPS OFF. THE CENTER TANK FUEL BOOST PUMPS WERE TURNED ON AND FUEL TRANSFERRED BACK INTO THE LT TANK. THE LT ENGINE WAS RESTARTED AND OPERATED NORMALLY. REFERENCE: OPERATOR CONTROL NR 96ZZZX3297. (X) 2 L 7 2 4F A6WE 1996070300150 19960703 00150 WP 1996 7 3 ASAA9680125 1 19960527 A 3350 41B004AD07G3 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 966AS 49104 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE BAT TERIES AND OPERATED NORMALLY. (X) 2 L 7 2 4F A6WE 1996070300151 19960703 00151 WP 1996 7 3 ASAA9680127 1 19960531 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 960AS 16879 2972 53074 PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT NEON CHARGE LAMP DID NOT ILLUMINATE WITH SWITCH IN THE ARMED POSITION. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 1996070300152 19960703 00152 WP 1996 7 3 ASAA9680128 1 19960601 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 969AS 53063 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. RECONNECT ED WIRING AT ROW 2 AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 1996070300153 19960703 00153 WP 1996 7 3 ASAA9680129 1 19960603 A 3350 RPS1B BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 946AS 49658 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE AFT CABIN WERE FOUND DIM. REPLACED THE BATTERY PACK AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 1996070300154 19960703 00154 WP 1996 7 3 ASAA9680130 1 19960604 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 957AS 24746 49126 SEA - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (X) 2 L 7 2 4F A6WE 1996070300155 19960703 00155 WP 1996 7 3 ASAA9680132 1 19960606 A 3350 S103 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 931AS 49232 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 29 TO 31 WERE FOUND INOPERATIVE. REPLACED THE B ATTERIES AND OPERATED NORMALLY. (X) 2 L 7 2 4F A6WE 1996070300156 19960703 00156 WP 1996 7 3 ASAA9680133 1 19960608 A 3350 014597101 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 932AS 49233 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 7 TO 12 WERE FOUND INOPERATIVE. REPLACED THE BA TTERIES AND OPERATED NORMALLY. (X) 2 L 7 2 4F A6WE 1996070300157 19960703 00157 WP 1996 7 3 ASAA9680134 1 19960609 A 3350 S103 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 945AS 49643 PDX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 1 TO 7 WERE FOUND INOPERATIVE. REPLACED THE BAT TERIES AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 1996070300158 19960703 00158 WP 1996 7 3 ASAA9680135 1 19960610 A 3350 41B004AD07G3 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 940AS 49825 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 14 TO 16 WERE FOUND INOPERATIVE. REPLACED THE B ATTERIES AND OPERATED NORMALLY. (X) 2 L 7 2 4F A6WE 1996070300159 19960703 00159 1996 7 3 ASAA9680136 4 19960613 A 2565 D29984103 EMERG EVAC SLIDE DOUG DC9 DC983 3022083 WP TAILCONE FAILED TEST A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 963AS 53077 OAK - DURING 15K CHECK, THE TAILCONE EMERGENCY EVACUATION SLIDE EMERGENCY LIGHTS FAILED TEST. REPLACED THE TAILCONE EME RGENCY EVACUATION SLIDE. (X) 2 L 7 2 4F RT A6WE 1996070300160 19960703 00160 SO 1996 7 3 GLBA96080 1 19960503 A 4940 32540 START CONTACTOR EMB 120 EMB120ER 3260203 SO RT COCKPIT FAILED A GLBA O OTHER B M SMOKE/FUMES/ODORS/SPARKS OVER TEMP CR CRUISE 1 CE 01 292UX 120292 SUX - CREW REPORTED A 'HOT' SMELL COMING FROM COPILOT'S SIDE PANEL (PANEL WAS HOT). MAINTENANCE REMOVED AND REPLACED AP U START CONTACTOR AND ASSOCIATED ELECTRICAL CONNECTORS WHICH HAD BEEN DAMAGED BY HEAT. OPS CHECK WAS GOOD. (X) 2 L 7 2 4T RT A31SO 1996070300161 19960703 00161 CE 1996 7 3 GLBA96082 1 19960506 A 2612 24412886 FIRE LOOP BEECH 1900 1900C 1154161 CE RT FWD MALFUNCTIONED A GLBA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 01 150UE UC150 TUS - CREW REPORTED RT FIRE LIGHT ILLUMINATED WHILE TAXIING, SO THEY RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED RT FORWARD FIRE LOOP. OPS CHECK WAS GOOD. (X) 2 L 7 2 4T RT A24CE 1996070300162 19960703 00162 SO 1996 7 3 GLBA96084 1 19960508 A 7712 3039242 NP SENSOR EMB 120 EMB120ER 3260203 SO RT ENGINE LOOSE A GLBA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 01 292UX 120292 CIU - CREW REPORTED A 30 PERCENT TORQUE LOSS ON RT ENGINE WITH EEC ON. THEY MADE AN AIR TURN-BACK AND LANDED UNEVENTFUL LY. MAINTENANCE TIGHTENED RT NP SENSOR. OPS CHECK WAS GOOD. (X) 2 L 7 2 4T RT A31SO 1996070300163 19960703 00163 NE 1996 7 3 GLBA96094 2 19960517 A 7200 ENGINE EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE LEFT BIRD STRIKE A GLBA A UNSCHED LANDING C F.O.D. CL CLIMB 1 CE 01 293UX 120293 BIS - CREW REPORTED A BIRD STRIKE TO LT ENGINE INTAKE AREA AFTER TAKEOFF. THEY MADE AN AIR TURN-BACK AND LANDED UNEVENT FULLY. MAINTENANCE PERFORMED BORESCOPES OF LT ENGINE. NO DISCREPANCIES FOUND. (X) 2 L 7 2 4T 4 T RT A31SO E20NE 1996070300164 19960703 00164 SO 1996 7 3 GLBA96095 1 19960519 A 5230 MS250851 SWITCH EMB 120 EMB120ER 3260203 SO CARGO DOOR OUT OF ADJUST A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 293UX 120293 DEN - CREW REPORTED THE CARGO DOOR ANNUNCIATOR ILLUMINATED IN-FLIGHT. THEY MADE AN AIR TURN-BACK AND LANDED UNEVENTFULL Y. MAINTENANCE ADJUSTED CARGO DOOR MICROSWITCH. OPS CHECK WAS GOOD. (X) 2 L 7 2 4T RT A31SO 1996070300165 19960703 00165 CE 1996 7 3 GLBA96096 1 19960520 A 6120 310047501 BETA CABLE BEECH 1900 1900C 1154161 CE RT PROPELLER OUT OF ADJUST A GLBA O OTHER O OTHER LD LANDING 1 CE 01 89UE UC89 MSP - CREW REPORTED THE RT PROPELLER DROPPED TO LOW IDLE IN FLAIR. AFTER UNEVENTFUL LANDING, MAINTENANCE RIGGED RT PROP ELLER BETA CABLES. OPS CHECK WAS GOOD. (X) 2 L 7 2 4T RT A24CE 1996070300166 19960703 00166 SO 1996 7 3 GLBA96097 1 19960523 A 7712 311694201 TORQUE SENSOR EMB 120 EMB120ER 3260203 SO RT ENGINE FAILED A GLBA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 01 295UX 7537 120295 SPI - CREW REPORTED RT TORQUE GAUGE INOPERATIVE (READS ZERO). THEY RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED RT TORQUE SENSOR. OPS CHECK WAS GOOD. (X) 2 L 7 2 4T RT A31SO 1996070300167 19960703 00167 CE 1996 7 3 GLBA96098 1 19960523 A 5751 1181300003 AILERON BEECH 1900 1900C 1154161 CE RIGHT CRACKED A GLBA O OTHER F FLT CONT AFFECTED IN INSP/MAINT 1 CE 01 152GL UC152 MSP - CREW REPORTED A CRACK IN RT AILERON END CAP FOUND DURING POST-FLIGHT WALK-AROUND. MAINTENANCE REMOVED, REPAIRED, AND REINSTALLED RT AILERON. TEST FLIGHT CHECKED GOOD. (X) 2 L 7 2 4T RT A24CE 1996070300168 19960703 00168 CE 1996 7 3 GLBA96099 1 19960524 A 3260 404EN16 DOWNLOCK SWITCH BEECH 1900 1900C 1154161 CE LT MLG FAILED A GLBA O OTHER N FALSE WARNING LD LANDING 1 CE 01 122GL UC122 ORD - CREW SELECTED GEAR DOWN, BUT RECEIVED NO 'DOWN AND LOCKED' INDICATION ON LT GEAR. ON SECOND ATTEMPT, LT GEAR LIGH T ILLUMINATED AND CREW LANDED UNEVENTFULLY. MAINTENANCE REMOVED LT GEAR DOWNLOCK SWITCH. OPS CHECK WAS GOOD. (X) 2 L 7 2 4T RT A24CE 1996070300169 19960703 00169 CE 1996 7 3 GLBA96100 1 19960524 A 3260 35133790007 ANNUNCIATOR PANE BEECH 1900 1900C 1154161 CE COCKPIT MALFUNCTIONED A GLBA O OTHER N FALSE WARNING LD LANDING 1 CE 01 130UE UC130 SPI - CREW REPORTED THAT GEAR POSITION LIGHTS REMAINED GREEN AFTER SELECTING GEAR UP. THEY MADE AN AIR TURN-BACK AND LA NDED UNEVENTFULLY. MAINTENANCE REMOVED AND REPLACED 'DOWN AND LOCKED' ANNUNCIATOR ASSY. OPS CHECK WAS GOOD. (X) 2 L 7 2 4T RT A24CE 1996070300170 19960703 00170 CE 1996 7 3 GLBA96102 1 19960530 A 3260 1003810061 DOWNLOCK SWITCH BEECH 1900 1900C 1154161 CE NLG DIRTY A GLBA O OTHER P NO WARNING INDICATION LD LANDING 1 CE 01 167GL UC167 SAV - CREW SELECTED GEAR DOWN, BUT NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE. THEY PERFORMED A MANUAL GEAR EXTENSION AND STILL DID NOT GET GREEN LIGHT. THEY MADE AN UNEVENTFUL LANDING AND WHEN AIRCRAFT TOUCHED DOWN, NOSE GEAR GREEN LIGHT I LLUMINATED. MAINTENANCE CLEANED NOSE GEAR DOWNLOCK SWITCH AND CHECKED ADJUSTMENT. OPS CHECK WAS GOOD. (X) 2 L 7 2 4T RT A24CE 1996070300171 19960703 00171 CE 1996 7 3 GLBA96103 1 19960530 A 2130 1183800043 SOLENOID VALVE BEECH 1900 1900D 1154162 CE LEFT FAILED A GLBA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 01 100UX UE100 DEN - LEFT ENVIRONMENTAL FAIL ANNUNCIATOR ILLUMINATED ON TAKEOFF ROLL AND CREW RETURNED TO GATE. MAINTENANCE REMOVED AN D REPLACED LEFT SOLENOID VALVE. OPS CHECK WAS GOOD. (X) 2 L 7 2 4T RT A24CE 1996070300172 19960703 00172 SO 1996 7 3 GLBA96105 1 19960530 A 2752 3203001007 ACTUATOR EMB 120 EMB120RT SO LT TE FLAP FAILED A A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 128AM 708 120109 MYR - CREW REPORTED A FLAP DISAGREEMENT FAULT AFTER TAKEOFF. THEY MADE AN AIR TURN-BACK AND LANDED UNEVENTFULLY. MAINT ENANCE REPLACED LEFT OUTBOARD FLAP ACTUATOR. OPS CHECK WAS GOOD. (X) 2 L 7 2 4T RT A31SO 1996070300173 19960703 00173 SW 1996 7 3 MALA964987 1 19960510 A 5532 SKIN SWRNGN SA227 SA227AC 8780603 SW VERTICAL STAB CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 863MA AC650B MSP - DURING AN INSPECTION, MAINTENANCE FOUND 3 CRACKS IN RT VERTICAL STABILIZER SKIN ALONG FORWARD AUXILIARY SPAR RIVET S MEASURING .380 INCH AT WL 140.0, .880 INCH AT WL 144.0, .750 INCH AT WL 148.0. REPAIRS WERE COMPLETED BY STOP DRILLIN G CRACKS AND INSTALLING A 2024 T-3 .032 INCH DOUBLER MEASURING 4.0 INCHES BY 12.0 INCHES. COMPLETED IAW AEROTECH DESIGN S EO NR 01-96033. (X) 2 L 7 2 4T RT A8SW 1996070300174 19960703 00174 WP 1996 7 3 9614199935 1 19960626 A 3320 SOCKETS DOUG DC9 DC931 3022065 WP SIDEWALL LTS ARCING A NWAA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 GL 01 1332U 47404 PASSENGER REPORTED THAT SIDEWALL LIGHTS ABOVE WINDOWS AT ROWS 8, 9 AND 10 RIGHT WERE ARCING DURING TAXI-OUT. CREW WAS N OTIFIED AFTER TAKEOFF. FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND FL AMES COMING FROM SIDEWALL FLUORESCENT LAMP HOLDERS. REPLACED THREE LAMP HOLDERS AND RELAMPED DUE TO MELTED LAMP PINS. 2 L 7 2 4F A6WE 1996070300175 19960703 00175 WP 1996 7 3 9614209950 1 19960627 A 3350 LIGHTS DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9346 47376 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS AT SEATS 1CD INOPERATIVE. DEFERRED PER MEL 3 3-24B. DAMAGED WIRE FROM FLOOR TO SEAT 1D NEEDS REPAIR. 2 L 7 2 4F A6WE 1996070300176 19960703 00176 WP 1996 7 3 9614219917 1 19960626 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 967N 47573 DURING PREFLIGHT CHECK, FOUND SEVERAL SECTIONS OF CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES AND BURNED OUT BULB. 2 L 7 2 4F A6WE 1996070300177 19960703 00177 WP 1996 7 3 9614229992 1 19960626 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8960E 45869 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS BETWEEN ROWS 5 THROUGH 10 AND 17 THROUGH 19 I NOPERATIVE. RELAMPED AND REPLACED BATTERIES IN PACK. 2 L 7 2 4F A6WE 1996070300178 19960703 00178 WP 1996 7 3 9614239762 1 19960626 A 3397 WIRE DOUG DC9 DC941 302207N WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 762NW 47395 DURING LINE CHECK, FOUND OVERHEAD EMERGENCY LIGHTS ARE DIM OR NOT ON. REPLACED BATTERIES AND REPAIRED BROKEN GROUND WIR E TO CONNECTOR AT SEATS 10 AND 11. ALL EMERGENCY LIGHT OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F A6WE 1996070300179 19960703 00179 WP 1996 7 3 ABX9600517 1 19960626 A 3241 421396 CONTROL BOX DOUG DC9 DC931 3022065 WP ANTI-SKID SYST DEFECTIVE A ABXA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 944AX 47550 ON TAXI OUT WITH ANTI-SKID IN ARMED POSITION, BRAKES FAILED THREE TIMES. REPLACED THE ANTI-SKID CONTROL BOX. 2 L 7 2 4F A6WE 1996070300180 19960703 00180 WP 1996 7 3 ABXA9600518 1 19960627 A 3233 47783031 ACTUATOR PIN DOUG DC8 DC863 302198A WP RT MLG BROKEN A A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 RIGHT MAIN LANDING GEAR RETRACT ACTUATOR ATTACH PIN WAS FOUND BROKEN DURING POST FLIGHT INSPECTION. REPLACED RIGHT MAIN LANDING GEAR RETRACT ACTUATOR ATTACH PIN IAW DC8 MM, COMPLETED RETRACTION/EXTENSION CHECKS AND NO DEFECTS WERE NOTED, OPS CHECKED GOOD. BOLT WAS INSPECTED IAW AD 71-25-09, 11,358.2 HOURS PRIOR TO FAILING. 2 L 7 4 4F 4A25 1996070300181 19960703 00181 WP 1996 7 3 ABXA9600519 1 19960621 A 3246 685 BEARING GOODYEAR A9560892 DOUG DC9 DC931 3022065 WP 1 BRAKE DEFECTIVE A ABXA K NONE O OTHER TX TAXI/GRND HDL 1 GL 23 948AX FEB9011606 47065 THE NR 1 BRAKE WAS DRAGGING AND OVERHEATED. REPLACED WHEEL AND BRAKE ASSEMBLIES. BLED AND LEAK CHECKED BRAKE IAW DC-9 MM 32-40-2 AND 32-41-1. SHOP FINDINGS INDICATED WHEEL INBOARD BEARING FAILURE. 2 L 7 2 4F A6WE 1996070300182 19960703 00182 NM 1996 7 3 CALA9600905 1 19960627 A 2910 HYD LINE BOEING 737 7373T0 1384582 NM NR 4 BRAKE LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 09 71314 23365 THE A-HYDRAULIC SYSTEM FLUID WAS LOST ON FINAL APPROACH TO EWR. THE LANDING GEAR WAS MANUALLY EXTENDED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 4 BRAKE LINE LEAKING. THE BRAKE LINE WAS REMOVED AND REPLACED AND T HE BRAKES WERE BLED, LEAK CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 1996070300183 19960703 00183 NM 1996 7 3 CALA9600906 1 19960627 A 2720 65C370523 PCU BOEING 737 737217 1384464 NM RUDDER INOPERATIVE A CALA O OTHER F FLT CONT AFFECTED TO TAKEOFF 1 SW 09 16232 25940 6640 19886 THE AIRCRAFT HAD AN UNCOMMANDED ROLL TO THE RIGHT ON TAKEOFF. FIFTEEN TO TWENTY DEGREES OF LEFT AILERON WAS REQUIRED TO MAINTAIN LEVEL FLIGHT. ALL OTHER INDICATIONS WERE NORMAL. THE AIRCRAFT CONTINUED TO CLE WHERE IT LANDED WITHOUT FURTH ER PROBLEM. THE YAW DAMP COUPLER WAS REMOVED AND REPLACED. THE YAW DAMPER WAS PLACED ON PLACARD. THE SDR WILL REMAIN OPEN PENDING INVESTIGATION. *S/D* MAINTENANCE FOUND THAT THE RUDDER PCU TRANSFER VALVE HAD AN OPEN AT PIN 5 AND 6. TH E RUDDER PCU WAS REMOVED AND REPLACED AND THE PLACARD ON YAW DAMPER WAS REMOVED. VENDOR TEARDOWN FOUND NO TROUBLE WITH THE YAW DAMP COUPLER. VENDOR TEARDOWN OF THE RUDDER PCU FOUND THE SERVO VALVE DEFECTIVE. ADDITIONAL TEARDOWN FINDINGS 2 L 7 2 4F A16WE 1996070300184 19960703 00184 NM 1996 7 3 CALA9600907 1 19960521 A 5730 SKIN BOEING 727 727232 1384082 NM WS 555 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND A 1.5 INCH CRACK IN LEADING EDGE SKIN ABOVE NR 6 SLAT OUTBOARD TRACK OF RT WING, WS 555. THE CRACK WAS STOPPED DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30 AND MM 51-20-2. 2 L 7 3 4F A3WE 1996070300185 19960703 00185 NM 1996 7 3 CALA9600908 1 19960521 A 5730 SKIN BOEING 727 727232 1384082 NM WS WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND TWO .5 INCH CRACKS IN SKIN OF RT WING TIP LOWER LEADING EDGE. THE CRACKS WERE STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 57-30-4 AND 51-10-2. 2 L 7 3 4F A3WE 1996070300186 19960703 00186 NM 1996 7 3 CALA9600909 1 19960523 A 5730 SKIN BOEING 727 727232 1384082 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND A .5 INCH CRACK IN RT WING LEADING EDGE SKIN FORWARD OF OUTBOARD SLAT CARRIAGE, NR 5 SLAT. A DOUBLER W AS FABRICATED AND INSTALLED IAW SRM 51-10-2, 57-30-4, FIG 4 AND 9, MM 51-20-11. 2 L 7 3 4F A3WE 1996070300187 19960703 00187 NM 1996 7 3 CALA9600910 1 19960517 A 5330 PANEL BOEING 727 727232 1384082 NM BS 273.5 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND A .375 INCH CRACK AT FASTENER HOLE IN TOP LEFT PANEL AT BS 273.5, LBL 14.5. A DOUBLER WAS FABRICATED A ND INSTALLED IAW SRM 51-10-2, 51-40-2, 51-20-4 AND MM 51-20-11. 2 L 7 3 4F A3WE 1996070300188 19960703 00188 NM 1996 7 3 CALA9600911 1 19960520 A 5522 SKIN BOEING 727 727232 1384082 NM LT ELEVATOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND FOUR CRACKS IN THE LT ELEVATOR LOWER SKIN BETWEEN STA 17.2 AND 37. THE CRACKS RANGED IN LENGTH FROM 1. 12 FT TO 6. THE CRACKED SKIN WAS REMOVED AND A Z-ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-20-1 AND 51-10-2. 2 L 7 3 4F A3WE 1996070300189 19960703 00189 NM 1996 7 3 CALA9600912 1 19960523 A 5530 WEB BOEING 727 727232 1384082 NM BS 1348 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND A FOUR INCH CRACK IN STIFFENER WEB INSIDE VERTICAL FIN ABOVE S-DUCT AT STA 1348. THE CRACK WAS STOPPED DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-30-2 AND MM 51-20-11. 2 L 7 3 4F A3WE 1996070300190 19960703 00190 NM 1996 7 3 CALA9600913 1 19960610 A 5320 SHEAR TIE BOEING 727 727232 1384082 NM BS 580 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND SHEAR TIE CORRODED AT STA 580 BETWEEN STRINGER 27R AND 28R. THE SHEAR TIE WAS REMOVED AND A NEW SHEAR TIE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 53-10-4, FIG 15 AND MM 51-20-2, 51-20-15. 2 L 7 3 4F A3WE 1996070300191 19960703 00191 NM 1996 7 3 CALA9600914 1 19960526 A 5330 SKIN BOEING 727 727232 1384082 NM BS 720 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND SKIN LAP CORRODED AT STA 720D TO 720E, STRINGER 27R. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53- 30-3 AND 51-30-2. 2 L 7 3 4F A3WE 1996070300192 19960703 00192 NM 1996 7 3 CALA9600915 1 19960528 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 535 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND THE FORWARD CARGO COMPARTMENT FLOOR SUPPORT CORRODED AT STA 535, S28L TO S29L. A REPAIR ANGLE WAS FABR ICATED AND INSTALLED IAW SRM 51-10-6, 51-40-4, 51-10-2, 53-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996070300193 19960703 00193 NM 1996 7 3 CALA9600916 1 19960520 A 5320 SHEAR TIE BOEING 727 727232 1384082 NM BS 720 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND SHEAR TIE CORRODED AT BS 720A, STRINGER 29R. A NEW SHEAR TIE WAS FABRICATED AND INSTALLED IAW SRM 51-3 0-2, 51-10-2 AND MM 51-20-11. 2 L 7 3 4F A3WE 1996070300194 19960703 00194 NM 1996 7 3 CALA9600917 1 19960508 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 480 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND STRINGER 21L CORRODED AT STA 480. NEW PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-3, FIGURE 3 AN D 51-30-2. 2 L 7 3 4F A3WE 1996070300195 19960703 00195 NM 1996 7 3 CALA9600918 1 19960518 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 480 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND STRINGER 27R CORRODED AT STA 480. THE CORROSION WAS REMOVED AND A NEW STRINGER WAS FABRICATED AND INST ALLED IAW SRM 51-10-2, 53-10-1 AND MM 51-20-11. 2 L 7 3 4F A3WE 1996070300196 19960703 00196 NM 1996 7 3 CKSA96062 1 19960627 A 2120 AIR DISTR BOEING 727 727223 1384074 NM CABIN ODOR A CKSA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 6812 19487 INFLIGHT EXPERIENCED A BURNING ODOR IRRITATING TO THE EYES, APPEARS TO BE COMING FROM THE AC PACKS. OPERATED APU AND PA CKS FOR 15 MINUTES. VISUALLY INSPECTED PNEUMATIC DUCTS ACM COMPARTMENTS BLEED SYSTEM HEAT EXCHANGER TAIL SECTION AND EL ECTRIC COMPARTMENT. NO EVIDENCE OF FIRE OR SMOKE. 2 L 7 3 4F A3WE 1996070300197 19960703 00197 NM 1996 7 3 P5CA9600301 1 19960627 A 3231 65B13002013 ATTACH FITTING BOEING 747 747122 1384872 NM LT MLG DOOR BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 ON ARRIVAL, FOUND LEFT HAND BODY GEAR DOOR FOLLOW-UP ROD ATTACH FITTING BROKEN. REMOVED AND REPLACED FITTING IAW MM 32- 14-01. INSPECTION REVEALED NO SIGN OF CORROSION. SUSPECT FATIGUE CRACK/WEAR OF BUSHINGS FOR ROD END BOLT. 2 L 7 4 4F A20WE 1996070300198 19960703 00198 NM 1996 7 3 9614246716 1 19960627 A 2611 215610B DETECTOR BOEING 747 747251F 1384898 NM CARGO COMPART MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 01 616US 24041 3724 21120 DURING CRUISE, THE NR 2 MAIN DECK CARGO SMOKE DETECTOR ACTIVATED. AIRCRAFT DIVERTED TO YEG AND LANDED WITHOUT INCIDENT. REPLACED DETECTOR, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996070300199 19960703 00199 NM 1996 7 3 9614256304 1 19960625 A 3350 LIGHT BOEING 747 747451 1384940 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 664US 23819 DURING LINE CHECK, FOUND EMERGENCY FLOOR LIGHTS FROM ROW 42 LEFT TO 66 LEFT INOPERATIVE. RECONNECTED LIGHT ASSEMBLY AND REPLACED LIGHT ASSEMBLY FORWARD OF LAVATORY 4L, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1996070300200 19960703 00200 NM 1996 7 3 9614266635 1 19960625 A 3350 BATTERY BOEING 747 747227B 1384888 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 635US 21682 DURING LINE CHECK, FOUND 4L OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996070300201 19960703 00201 1996 7 3 9614275504 4 19960629 A 3442 20412170414 TRANSCEIVER BOEING 727 727251 138408H NM FWD FUSELAGE MALFUNCTIONED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 504US 25886 6543 23193 DURING CRUISE, WEATHER RADAR DISPLAY ERRATIC AND UNRELIABLE. AIRCRAFT DIVERTED TO DTW AND LANDED WITHOUT INCIDENT. REP LACED THE LEFT TRANSCEIVER, PERFORMED MAINTENANCE BITE TEST, CHECKED OK. 2 L 7 3 4F A3WE 1996070300202 19960703 00202 NM 1996 7 3 96FDEA00869 1 19960430 A 5754 65162251 FLAP BOEING 727 72725 1384006 NM NR 3 LE FLAP CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 NR0151 AND 015, DUE TO NUMEROUS AREAS OF CORROSION NR 3 K-FLAP REQUIRES REPLACEMENT. *S/D* REMOVED AND REPLACED NR 3 K -FLAP IAW FED EX MM 27-81-1 AND MM 27-81-11. 2 L 7 3 4F A3WE 1996070300203 19960703 00203 NM 1996 7 3 96FDEA00870 1 19960430 A 5754 65162267A FLAP BOEING 727 72725 1384006 NM NR 2 LE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 NR0152 AND 016, DUE TO NUMEROUS AREAS OF CORROSION NR 2 K-FLAP REQUIRES REPLACEMENT. *S/D* REMOVED AND REPLACED NR 2 K -FLAP IAW FEDEX MM 27-81-1 AND MM 27-81-11. 2 L 7 3 4F A3WE 1996070300204 19960703 00204 NM 1996 7 3 96FDEA00871 1 19960430 A 5754 651622715 FLAP BOEING 727 72725 1384006 NM NR 1 LE FLAP CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 NR0153 AND 017, DUE TO NUMEROUS AREAS OF CORROSION NR 1 K-FLAP REQUIRES REPLACEMENT. *S/D* REMOVED NR 1 K-FLAP AND SEN T OUT FOR REPAIR. RECEIVED SERVICEABLE REPAIRED NR 1 K-FLAP AND INSTALLED IAW FEDEX MM 27-81-1 AND MM 27-81-11. 2 L 7 3 4F A3WE 1996070300205 19960703 00205 NM 1996 7 3 96FDEA00872 1 19960430 A 5754 65162262 BULLNOSE BOEING 727 72725 1384006 NM NR 5 LE FLAP CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 NR0154 AND 018, DUE TO NUMEROUS AREAS OF CORROSION NR 5 BULLNOSE REQUIRES REPLACEMENT. *S/D* REMOVED AND REPLACED NR 5 K-FLAP BULLNOSE IAW FEDEX OHM 57-51-11, MM 27-81-1, AND MM 27-81-11. 2 L 7 3 4F A3WE 1996070300206 19960703 00206 NM 1996 7 3 96FDEA00886 1 19960502 A 5312 651596911 BULKHEAD FITTING BOEING 727 72725 1384006 NM BS 740 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 NR0089 AND 027, CRACK IN FLANGE OF 740 FORGING RT SIDE FROM STR 19R TO INTERCOSTAL. *S/D* REPLACED 740 FORGING RT SIDE PER FEDEX EA 7-5310-29171. 2 L 7 3 4F A3WE 1996070300207 19960703 00207 NM 1996 7 3 96FDEA01152 1 19960618 A 5320 6518747 SPLICE PLATE BOEING 727 727225 1384077 NM BS 481 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 467FE 21449 NR0227 AND 012, CORROSION (C53-113-01, -1) ON BUTT SPLICE DOUBLER BS 481 BETWEEN STR 28L AND R. *S/D* BLENDED CORROSIO N DOUBLER, FOUND TO BE OUT OF LIMITS. FABRICATED DOUBLER AND FILLER AND INSTALLED PER FEDEX EA 7-5310-29235. 2 L 7 3 4F A3WE 1996070300208 19960703 00208 NM 1996 7 3 96FDEA01155 1 19960616 A 5230 655720416 ANGLE BOEING 727 727225 1384077 NM CARGO DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 467FE 21449 NR0307 AND 015, NR 2 CARGO DOOR SECOND TRANSVERSE BEAM FROM BOTTOM OF DOOR I/B L-ANGLE IS CORRODED. *S/D* REMOVED TRAN SVERSE BEAM, FABRICATED NEW AND INSTALLED IAW FEDEX DRAWING 65-57204. 2 L 7 3 4F A3WE 1996070300209 19960703 00209 NM 1996 7 3 96FDEA01183 1 19960626 A 5720 ARB3216502 FITTING DOUG MD11 MD11 3023602 NM NR 2 FUEL TANK CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 586FE 48487 DISCREPANCY: CENTER FUEL TANK NR 2 RT COMPARTMENT STA XORS 230, 600, RIB REAR SPAR ATTACH FITTING IS CRACKED APPROXIMAT ELY 1.5 INCHES AT TOP (REF N0432). REMOVED AND REPLACED ARB3216-502 WITH NEW PART PER N/R 0432. 2 L 7 3 4F RT A22WE 1996070300210 19960703 00210 NM 1996 7 3 96FDEA01184 1 19960626 A 5754 65162261 HINGE LUGS BOEING 727 727225 1384077 NM NR 2 LE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 467FE 21449 NR0088 AND 021, NR 2 K-FLAP CENTER HINGE LUGS UPPER AND LOWER FASTENERS HAVE CORROSION. *S/D* REMOVED K-FLAP AND REPLA CED IAW FEDEX MM 27-81-1. 2 L 7 3 4F A3WE 1996070300211 19960703 00211 WP 1996 7 3 96FDEA01185 1 19960629 A 5311 65162261 FRAME DOUG DC10 DC1010CF 3023502 WP BS 1781 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 STA 1781 LONGERONS 49 TO 52R BILGE SUMP FRAM/LONGERONS HAVE EXFOLIATION CORROSION AT AFT END OF CTR CARGO COMPARTMENT. * S/D* REMOVED AND REPLACED FRAME SECTION AND SPLICE PER SRM 53-30-00. 2 L 7 3 4F RT A22WE 1996070300212 19960703 00212 NM 1996 7 3 96FDEA01186 1 19960629 A 5320 6516348 SHEAR TIE BOEING 727 727173C 1384059 NM BS 1148 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 199FE 19509 NR0526 AND 012, SHEAR TIE DAMAGED AT BS 1148 BETWEEN STA 19 TO 20 RT ON FWD SIDE OF FRAME. *S/D* REPAIRED DAMAGED SHEA R TIE AT BS 1148 BETWEEN STR 19 AND 20 RT FWD SIDE OF FRAME IAW FEDEX SRM 53-10-4. 2 L 7 3 4F A3WE 1996070300213 19960703 00213 WP 1996 7 3 ARWA9606019 1 19960614 A 5320 DOOR HOUSING DOUG DC8 DC863F 302198F WP FS 280-340 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 FORWARD CARGO COMPARTMENT HAS LEVEL 2 CORROSION AT UPPER SURFACE AT DOOR HOUSING, FS 280 PLUS 340. REPAIRED UPPER SURFA CE IAW DC-8 SRM 53-2-0, FIG 1D. FABRICATED DOUBLER IAW DC-8 SRM 53-4-1, 51-1-1. TREATED AND INSTALLED IAW DC-8 SRM 51- 1-8, 51-1-20D. 2 L 7 4 4F 4A25 1996070300214 19960703 00214 WP 1996 7 3 ARWA9606028 1 19960614 A 5312 97504283 PRESS DOME DOUG DC8 DC863F 302198F WP LEFT CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 LT DOME WITH EXFOLIATE CORROSION ON LOWER INNER RADIUS. REMOVED AND REPLACED DOME PER DRAWING NR 9750428. 2 L 7 4 4F 4A25 1996070300215 19960703 00215 WP 1996 7 3 ARWA9606029 1 19960614 A 5312 97504285 PRESS DOME DOUG DC8 DC863F 302198F WP RIGHT CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 RT DOME CRACKED AT LOWER INNER RADIUS. REMOVED AND REPLACED DOME PER DRAWING NR 9750428. 2 L 7 4 4F 4A25 1996070300216 19960703 00216 WP 1996 7 3 ARWA9606053 1 19960614 A 5320 FITTING DOUG DC8 DC863F 302198F WP BS 780 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 MAIN CARGO COMPARTMENT HAS 3 INCH CRACK IN FITTING AT STA 780, LONGERON 22L. REPAIRED AREA PER ROD SKETCH NR 96-04-25-0 07, DOUGLAS-APPROVED ACTION NR 296570. FABRICATED AND TREATED DOUBLER PER DC-8 SRM 51-1-4, 51-1-8. INSTALLED DOUBLER P ER DC-8 SRM 51-3-0, 51-1-20D. 2 L 7 4 4F 4A25 1996070300217 19960703 00217 WP 1996 7 3 ARWA9606062 1 19960614 A 7830 TRANSLATING RING DOUG DC8 DC863F 302198F WP NR 3 ENG TR CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 NR 3 ENGINE TRANSLATING RING, AFT UPPER CORNER IS CRACKED. REPAIRED IAW ARROW AIR DRAWING NR ARW 015713-1182, FAA 8110- APPROVED. 2 L 7 4 4F 4A25 1996070300218 19960703 00218 WP 1996 7 3 ARWA9606064 1 19960614 A 5343 TRAPEZOID FTG DOUG DC8 DC863F 302198F WP RT MLG CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 RT MLG FITTING ASSEMBLY TO FUSELAGE, TRAPEZOID SHOWS 3 INCH CRACK AT 9, 10 AND 3 O'CLOCK. TRAPEZOID FITTING WAS REMOVED AND REPLACED IAW DC-8 SRM 51-1-21, 51-1-20D AND 51-3-0 AND DOUGLAS TRAP FITTING REPLACEMENT GUIDE. 2 L 7 4 4F 4A25 1996070300219 19960703 00219 WP 1996 7 3 ARWA9606066 1 19960614 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 600-680 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 PERMANENT REPAIR OF LOWER FUSELAGE AT LONGERON 36 FROM FS 600 TO 680 ACCOMPLISHED PER DRAWING ARW 015713-0013, FAA FORM 8110-APPROVED. 2 L 7 4 4F 4A25 1996070300220 19960703 00220 WP 1996 7 3 ARWA9606068 1 19960614 A 5730 PANEL DOUG DC8 DC863F 302198F WP WS 22.75-50 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 RT WING, INNER WING TOP PANEL PLATE SHOWS LEVEL 2 CORROSION FROM XRS 22.750 THROUGH XRS 50.000. REPAIRED WING TOP PANEL IAW DC-8 SRM 57-2-1, FIG 15. TREATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-8, 51-1-17 AND 51-1-20D. 2 L 7 4 4F 4A25 1996070300221 19960703 00221 WP 1996 7 3 ARWA9606069 1 19960614 A 5730 PLATE DOUG DC8 DC863F 302198F WP WS 50-74.869 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 RT WING, INNER WING TOP PANEL PLATE SHOWS LEVEL 2 CORROSION FROM XRS 50.000 THROUGH XRS 74.869. REPAIRED WING TOP PANEL IAW DC-8 SRM 57-2-1, FIG 10, SHEET 2. TREATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-8, 51-1-17 AND 51-1-20D. 2 L 7 4 4F 4A25 1996070300222 19960703 00222 NM 1996 7 3 CALA9600919 1 19960526 A 5320 SHEAR TIE BOEING 727 727232 1384082 NM BS 265 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND SHEAR TIE CORRODED AT STA 265, S25R. A REPAIR WAS PERFORMED IAW SRM 53-10-4, 51-10-2, 51-30-2 AND MM 5 1-20-21. 2 L 7 3 4F A3WE 1996070300223 19960703 00223 NM 1996 7 3 CALA9600920 1 19960522 A 5320 INTERCOSTAL BOEING 727 727232 1384082 NM BS 312-340 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND INTERCOSTAL CORRODED AT STA 312 TO 340, RBL 55. AN INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 51 -20-1, 51-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 1996070300224 19960703 00224 NM 1996 7 3 CALA9600921 1 19960522 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 308-312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 308 TO 312, LBL 30. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-30-2 AND MM 51-20-151. 2 L 7 3 4F A3WE 1996070300225 19960703 00225 NM 1996 7 3 CALA9600922 1 19960522 A 5315 FLOOR BEAM BOEING 727 727232 1384082 NM BS 1070 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND UPPER FLANGES OF FLOORBEAM CORRODED AT BS 1070, RBL 9 TO 12. THE CORRODED AREA WAS REMOVED. AN UPPER CHORD, SUPPORT ANGLES, FILLER AND STRAPS WERE FABRICATED AND INSTALLED IAW 53-10-8, FIGURE 1. 2 L 7 3 4F A3WE 1996070300226 19960703 00226 NM 1996 7 3 CALA9600923 1 19960523 A 5315 FLOOR BEAM BOEING 727 727232 1384082 NM BS 312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND FLOORBEAM CORRODED AT STA 312, LBL 30. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-8, 51- 10-2, 51-30-4 AND MM 51-20-11. 2 L 7 3 4F A3WE 1996070300227 19960703 00227 1996 7 3 CALA9600924 4 19960628 A 3460 4051600913 FLT CONTL COMP BOEING 737 7373T0 1384582 NM NR 1/2 INOPERATIVE A CALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 09 39343 23581 THE AUTOPILOT DISENGAGED FOLLOWED BY ILLUMINATION OF STAB OUT OF TRIM LIGHT, SPEED TRIM FAIL LIGHT, MACH TRIM FAIL LIGHT , OFF FLAGS IN CAPTAIN'S AIRSPEED, ALTITUDE AND VVI INDICATORS AND CAPTAIN'S FLIGHT DIRECTOR V-BARS VIBRATING DURING CRU ISE FLIGHT. TROUBLESHOOTING BY MAINTENANCE FOUND BOTH FLIGHT CONTROL COMPUTERS AT FAULT. BOTH THE NR 1 AND NR 2 FLIGHT CONTROL COMPUTERS WERE REMOVED AND REPLACED, BITE TEST WAS GOOD. LAND VERIFY TEST WAS PERFORMED IAW MM 22-03-00 AND NO FAULTS WERE NOTED. 2 L 7 2 4F RT A16WE 1996070300228 19960703 00228 WP 1996 7 3 CALA9600925 1 19960629 A 2780 SLAT HANDLE DOUG DC9 DC982 3022082 WP COCKPIT BINDING A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 83870 48056 THE SLATS WOULD NOT RETRACT AFTER TAKEOFF FROM DEN. THE SLAT HANDLE WOULD NOT GO INTO RETRACTED DETENT PAST ZERO DEGREE FLAP DETENT. RECYCLING WAS OF NO HELP. THE AIRCRAFT WAS RETURNED TO DEN WHERE IT LANDED WITHOUT INCIDENT. THE FLAP/S LAT HANDLE WAS LUBRICATED AND OPERATION CHECKED GOOD. 2 L 7 2 4F A6WE 1996070300229 19960703 00229 NM 1996 7 3 CALA9600926 1 19960630 A 2913 HYD PUMP BOEING 737 7373T0 1384582 NM NR 2 ENGINE LEAKING A CALA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SW 09 17345 23583 THE B-SYSTEM HYDRAULIC QUANTITY DROPPED TO 1/2 ACCOMPANIED BY ILLUMINATION OF THE B-ENGINE HYDRAULIC PUMP LOW PRESSURE L IGHT WHILE EN ROUTE. THE B-ENGINE HYDRAULIC PUMP WAS SHUT OFF AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITH OUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP LEAKING AND THE FILTER HOUSING FOR ELECTRIC DRIVE N B-PUMP CRACKED. THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP AND B-SYSTEM FILTER WERE REMOVED AND REPLACED. THE HYDRAULIC S YSTEM WAS SERVICED AND OPERATIONAL AND LEAK CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 1996070300230 19960703 00230 NM 1996 7 3 CALA9600927 1 19960630 A 2910 BACH8A06NN0336T HYD LINE BOEING 737 7373T0 1384582 NM NLG ACTUATOR LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 09 14358 23943 THE A-SYSTEM HYDRAULIC FLUID QUANTITY WENT TO ZERO WHILE ON FINAL APPROACH TO EWR. THE AIRCRAFT LANDED WITHOUT INCIDENT . MAINTENANCE FOUND THE NOSE GEAR ACTUATOR HYDRAULIC PRESSURE LINE LEAKING. THE HYDRAULIC PRESSURE LINE WAS REMOVED AN D REPLACED. THE GEAR HANDLE WAS CYCLED SEVERAL TIMES AND NO LEAKS WERE NOTED. 2 L 7 2 4F RT A16WE 1996070300231 19960703 00231 NM 1996 7 3 CALA9600928 1 19960522 A 5315 FLOOR BEAM BOEING 727 727232 1384082 NM BS 1070 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND UPPER FORWARD FLANGE OF FLOORBEAM CORRODED AT BS 1070, RBL 47.25 TO 50.25. THE UPPER CHORD WAS REMOVED AND REPLACED IAW SRM 53-10-8. AN UPPER CHORD, SUPPORT ANGLES, FILLERS, STRAPS AND WEB DOUBLERS WERE FABRICATED AND INS TALLED IAW SRM 53-10-8. 2 L 7 3 4F A3WE 1996070300232 19960703 00232 NM 1996 7 3 CALA9600929 1 19960518 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 700 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND CORROSION ON STRINGER 27R AT STA 700. A NEW STRINGER AND ANGLE WERE FABRICATED AND INSTALLED IAW SRM 5 3-10-3, 51-10-2 AND 51-20-11. 2 L 7 3 4F A3WE 1996070300233 19960703 00233 NM 1996 7 3 CALA9600930 1 19960519 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 540 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND FORWARD CARGO STRINGER 28R AT STA 540 CORRODED. A STRINGER WAS FABRICATED AND INSTALLED IAW SRM 53-10- 3. 2 L 7 3 4F A3WE 1996070300234 19960703 00234 NM 1996 7 3 CALA9600931 1 19960518 A 5320 SHEAR TIE BOEING 727 727232 1384082 NM BS 680 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND CORROSION ON FRAME SHEAR TIE AT STA 680, STRINGER 28L. A NEW SHEAR TIE WAS FABRICATED AND INSTALLED IA W SRM 51-30-2. 2 L 7 3 4F A3WE 1996070300235 19960703 00235 NM 1996 7 3 CALA9600932 1 19960520 A 5320 STRINGER SPLICE BOEING 727 727232 1384082 NM BS 740 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND CORROSION ON STRINGER 27R SPLICE AT BS 740. A NEW STRINGER SPLICE WAS FABRICATED AND INSTALLED IAW SRM 53-10-3 AND 51-30-2. 2 L 7 3 4F A3WE 1996070300236 19960703 00236 NM 1996 7 3 CALA9600933 1 19960520 A 5315 FLOOR BEAM BOEING 727 727232 1384082 NM BS 400 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND FLOORBEAM CORRODED AT STA 400, RBL 10. A NEW FLOORBEAM WAS FABRICATED AND INSTALLED IAW SRM 53-10-8. 2 L 7 3 4F A3WE 1996070300237 19960703 00237 NM 1996 7 3 CALA9600934 1 19960525 A 5311 FRAME BOEING 727 727232 1384082 NM BS 540 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND STA 540 FRAME ASSEMBLY CORRODED. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-4, PAGE 43. 2 L 7 3 4F A3WE 1996070300238 19960703 00238 NM 1996 7 3 CALA9600935 1 19960525 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 540 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND ATTACH ANGLE CORRODED AT STA 540, S29R. THE ATTACH ANGLE WAS REMOVED. A REPAIR PART WAS FABRICATED IA W SRM 53-10-4, 53-10-1 AND 51-20-4. 2 L 7 3 4F A3WE 1996070300239 19960703 00239 NM 1996 7 3 CALA9600936 1 19960602 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 520-540 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND STRINGER 28R CORRODED AT STA 520 T0 540. THE CORRODED STRINGER SECTION WAS REMOVED. A NEW STRINGER AN D SPLICE WERE FABRICATED AND INSTALLED IAW SRM 53-10-3 AND 51-30-2. 2 L 7 3 4F A3WE 1996070300240 19960703 00240 NM 1996 7 3 CALA9600937 1 19960522 A 5315 FLOOR BEAM BOEING 727 727232 1384082 NM BS 328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 328, LBL 30. THE CORRODED AREA WAS CUT OUT, A REPAIR ANGLE WAS FABRICA TED AND INSTALLED IAW SRM 53-10-8, FIGURE 9. 2 L 7 3 4F A3WE 1996070300241 19960703 00241 NM 1996 7 3 CALA9600938 1 19960529 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 580 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND CORROSION ON SKIN ATTACH ANGLE AT STA 580, STRINGER 27L. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-4, 51-30-2 AND MM 51-20-11. 2 L 7 3 4F A3WE 1996070300242 19960703 00242 SO 1996 7 3 COMA9610193 1 19960624 A 3230 18190003 VALVE EMB 120 EMB120RT SO HYD BAY MALFUNCTION A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 246CA 7469 420 120223 WHEN LANDING GEAR SELECTED DOWN, BOTH LT A AND B SYSTEM INTRANSIT LIGHTS REMAINED ON. WHEN LANDING GEAR CYCLED, THE RT A AND B INTRANSIT LIGHTS REMAINED ON. REPLACED THE LANDING GEAR SOLENOID VALVE. PART TOTAL CYCLES, 7,283. 2 L 7 2 4T RT A31SO 1996070300243 19960703 00243 SO 1996 7 3 COMA9610194 1 19960625 A 3230 12043270501 RELAY BOX EMB 120 EMB120RT SO LANDING GEAR MALFUNCTION A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 258CA 25 21 120247 LANDING GEAR WILL NOT RETRACT. REPLACED THE LANDING GEAR RELAY BOX. PART TOTAL CYCLES, 32. 2 L 7 2 4T RT A31SO 1996070300244 19960703 00244 SO 1996 7 3 COMA9610195 1 19960627 A 5330 12019230001 SKIN EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 164D 16803 120164 DURING C-1 INSPECTION, FOUND LOWER FUSELAGE SKIN AT FRAME 21 TO SHOW SIGNS OF CORROSION (SKIN BULGING). FURTHER INVESTI GATION FOUND THAT SMALL AREA BETWEEN SKIN AND TITANIUM STRAP WAS, IN FACT, CORRODED BETWEEN STRINGERS 2DL AND 2DR. REPA IR WAS DONE BY CUTTING OUT DAMAGE, INSTALLING FILLER AND EXTERNAL DOUBLER PER STRUCTURAL REPAIR MANUAL, CHAPTER 53-00-01 , FIGURE 202, SHEET 6. 2 L 7 2 4T RT A31SO 1996070300245 19960703 00245 SO 1996 7 3 COMA9610196 1 19960630 A 2751 FLAP WARNING EMB 120 EMB120RT SO COCKPIT ACTIVATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 162CA 120150 FLAP CONTROL FAULT WARNING AFTER TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. NO DEFECTS FOUND WITH FLAP SYSTEM. 2 L 7 2 4T RT A31SO 1996070300246 19960703 00246 NE 1996 7 3 COMA9610197 2 19960627 A 7313 7944441 SEALS EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENG LEAKING A COMA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 162CA 120150 FUEL DRIPPING FROM RT ENGINE NACELLE. REPLACED THE O-RING SEALS ON THE ENGINE FUEL NOZZLES. 2 L 7 2 4T 4 T RT A31SO E20NE 1996070300247 19960703 00247 SO 1996 7 3 COMA9610198 1 19960626 A 7312 10718D FUEL HEATER EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENG LEAKING A COMA K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 SO 01 259CA 15340 688 120252 FUEL LEAK RT ENGINE. REPLACED LEAKING FUEL TO OIL HEAT EXCHANGER. PART TOTAL CYCLES, 16,641. 2 L 7 2 4T 4 T RT A31SO E20NE 1996070300248 19960703 00248 SO 1996 7 3 COMA9610199 1 19960627 A 2750 3472001001 FLAP CONTL UNIT EMB 120 EMB120RT SO TE FLAPS MALFUNCTION A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 161CA 7748 205 120143 FLAP CONTROL FAULT WARNING DURING TAKEOFF. REPLACED THE FLAP CONTROL UNIT. PART TOTAL CYCLES, 8,211. 2 L 7 2 4T RT A31SO 1996070300249 19960703 00249 SO 1996 7 3 COMA9610200 1 19960627 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 164D 120164 EMERGENCY LIGHTING AT THE CABIN MID SECTION IS DIM. REPLACED EMERGENCY BATTERY. 2 L 7 2 4T RT A31SO 1996070300250 19960703 00250 NE 1996 7 3 COMA9620009 3 19960627 A 6110 PROPELLER SWRNGN SA227 SA227AC 8780603 SW MCAULY 4HFR34 4HFR34C652 NE LT ENGINE LEAKING A COMA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 702M 604 AC702 881161 OIL IS DRIPPING FROM THE LEFT ENGINE PROPELLER. REPLACED PROPELLER. 2 L 7 2 4T RT A8SW 6 C 3PNE 1996070300251 19960703 00251 WP 1996 7 3 COMA9620010 2 19960627 A 7313 31032359 FUEL NOZZLE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP LT ENGINE MALFUNCTIONED A A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 703CA AC703 TAKEOFF ABORTED BECAUSE OF TORQUE ROLL BACK LT ENGINE. REPLACED THE LEFT ENGINE FUEL NOZZLES. 2 L 7 2 4T 4 T RT A8SW E4WE 1996070300252 19960703 00252 1996 7 3 COMA9630131 3 19960625 A 6140 522792 INDICATOR SAAB SF340 SF340A 7850100 EU RT PROPELLER DEFECTIVE A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 158CA 22956 1232 340A158 RIGHT PROPELLER RPM IS INDICATING 1150 AT GROUND IDLE. REPLACED THE RT PROPELLER INDICATOR. PART TOTAL CYCLES, 26,067. 2 L 7 2 4T RT A52EU 1996070300253 19960703 00253 EU 1996 7 3 COMA9630132 1 19960625 A 7603 C821452 CONTROL CABLE SAAB SF340 SF340A 7850100 EU LT ENGINE BINDING A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 140N 340A140 LEFT ENGINE CONDITION CONTROL IS BINDING. REPLACED THE LT CONDITION CABLE SECTION BETWEEN HMU AND PCU. 2 L 7 2 4T RT A52EU 1996070300254 19960703 00254 EU 1996 7 3 COMA9630133 1 19960627 A 3530 4566M37B PBE SAAB SF340 SF340A 7850100 EU GALLEY DEFECTIVE A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 344CA 19989 340A025 THE GALLEY AREA P.B.E. DOES NOT APPEAR TO BE SERVICEABLE. REPLACED THE P.B.E. PART TOTAL CYCLES, 22036. 2 L 7 2 4T RT A52EU 1996070300255 19960703 00255 1996 7 3 COMA9660113 4 19960620 A 3410 6229819004 AIR DATA REF PNL CNDAIR CL600 CL6002B19 EA COCKPIT MALFUNCTION A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 914CA 7012 AURAL WARNING CONTINUOUSLY ACTIVATED DURING TAKEOFF. REPLACED THE ARP-4000. 2 L 7 2 4F RT A21EA 1996070300256 19960703 00256 EA 1996 7 3 COMA9660114 1 19960625 A 3231 RETRACT MECH CNDAIR CL600 CL6002B19 EA NLG DOORS OUT OF ADJUST A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 940CA 4547 7048 NOSE LANDING GEAR DISAGREE MESSAGE ON EICAS WHEN LANDING GEAR SELECTED DOWN. AFTER 25 SECONDS, NLG LOCKED DOWN. ADJUST ED NLG DOORS AND ACFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1996070300257 19960703 00257 EA 1996 7 3 COMA9660115 1 19960627 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 952CA 1344 7092 FLOOR EMERGENCY LIGHTING IS INOP BETWEEN ROWS 2 AND 5. REPAIRED WIRING CONNECTIONS AT STRIP LIGHTING. 2 L 7 2 4F RT A21EA 1996070300258 19960703 00258 NM 1996 7 3 P5CA9600252 1 19960622 A 5246 ACCESS DOOR BOEING 747 747123 1384873 NM FUELING PANEL PUNCTURED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 FOUND HOLE IN FUELING PANEL ACCESS DOOR, RIGHT WING. SANDED DAMAGED AREA, REPAIRED IAW SRM 51-40-08. 2 L 7 4 4F A20WE 1996070300259 19960703 00259 NM 1996 7 3 P5CA9600302 1 19960630 A 2613 OVERHEAT SENSOR BOEING 747 747122 1384872 NM NR 2 PYLON BARE WIRE A P5CA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 WP 23 851FT 19756 DURING TAXI OUT, LEFT WING OVERHEAT LIGHT ILLUMINATED. RETURNED TO BLOCKS. FOUND NR 4 LED GROUP WITH AN AIR LEAK, REPL ACED SEAL IAW MM 36-11-01. FOUND SENSOR NR 2 INBOARD OF NR 2 PYLON WITH A BARE WIRE. REPAIRED SAME IAW MM 26-18-02. L /E OVERHEAT SYSTEM CHECKS GOOD IAW MM 26-18-01. 2 L 7 4 4F A20WE 1996070300260 19960703 00260 NM 1996 7 3 QXEA9600225 1 19960628 A 2121 011389500 FAN DORNER DO32 DO328100 2996000 NM NR 2 PACK INOP A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 329PH 3007 PDX - RIGHT PACK OVERHEAT CAS MESSAGE. A HOT PACK SMELL WAS ASSOCIATED WITH CAS MESSAGE. GROUND COOLING FAN REPLACED A ND SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A45NM 1996070300261 19960703 00261 SW 1996 7 3 QXEA9600226 1 19960628 A 2440 2682241019 RECEPTACLE SWRNGN SA227 SA227AC 8780603 SW FUSELAGE SMOKING A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 26959 AC662 MWH - GPU PLUG-IN BEGAN SMOKING WHILE AIRCRAFT WAS PARKED AT THE GATE WITH GROUND POWER PLUGGED IN. GPU RECEPTACLE REPL ACED AND SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A8SW 1996070300262 19960703 00262 NM 1996 7 3 QXEA9600227 1 19960629 A 3350 82410162007 CONTROL BOX DHAV DHC8 DHC8102 2809003 NM CABIN MALFUNCTIONED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 813PH 32 FCA - CABIN EMERGENCY LIGHTS WILL NOT SHUT OFF WHEN SELECTED OFF. EMERGENCY LIGHT CONTROL BOX REPLACED AND LIGHTS OPS C HECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1996070300263 19960703 00263 NE 1996 7 3 96ZZZM1026 2 19960523 A 7510 577957 DUCT DOUG DC9 DC941 302207N WP PWA JT8 JT8D15 52051 NE NR 1 ENG RUPTURED A TWAA F ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 CE 05 934L 47618 BDL - DURING CLIMB SHUT DOWN NR 1 ENGINE, S/N 1607, DUE TO FIRE WARNING ON BOTH LOOPS. DISCHARGED FIRE EXTINGUISHER BOT TLE. FOUND ANTI-ICE HEAT DUCT, MFG P/N 577957, RUPTURED. REPLACED ANTI-ICE FUEL HEAT DUCT AND FIRE EXTINGUISHER BOTTLE . ENGINE OPERATION THEN CHECKED NORMAL. (M) 2 L 7 2 4F 4 F A6WE E2EA 1996070300264 19960703 00264 NM 1996 7 3 96ZZZM1027 1 19960523 A 2913 3508807 HYD PUMP BOEING 747 747131 1384881 NM NR 1 FAILED A TWAA O OTHER J WARNING INDICATION LD LANDING 1 CE 05 93108 19674 HNL - ON LANDING, NR 1 HYDRAULIC SYSTEM FAILED. REMOVED AND REPLACED NR 1 HYDRAULIC PUMP, MFG P/N 350880-7. RAN ENGINE S, OPERATIONAL CHECK NORMAL. (M) 2 L 7 4 4F A20WE 1996070300265 19960703 00265 WP 1996 7 3 96ZZZM1028 1 19960510 A 5315 FLOOR BEAM DOUG DC9 DC982 3022082 WP BS 1153 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 901TW 49166 MCI - DURING OP-16, FOUND CORROSION ON CABIN FLOOR BEAM AT FASTENER HOLES BETWEEN CHAIR TRACKS NR 2 AND 3, FS 1153. REP LACED SECTION PER SRM 51-01, PAGE 1 AND TWA STANDARD PRACTICES. (M) 2 L 7 2 4F A6WE 1996070300266 19960703 00266 WP 1996 7 3 96ZZZM1029 1 19960510 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 1155-1212 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 915TW 49186 MCI - DURING OP-15, FOUND CORROSION AROUND SCREW HOLE OF FLOOR SUPPORT TEE ANGLE, FS 1155 TO FS 1212, RBL 8. REPLACED T EE ANGLE PER SRM 57-01. (M) 2 L 7 2 4F A6WE 1996070300267 19960703 00267 NE 1996 7 3 96ZZZM1030 2 19960510 A 7530 BLEED CONTROL BOEING 767 767231 1385131 NM PWA JT9 JT9D7R4D 52054 NE NR 1 ENG OUT OF ADJUST A TWAA O OTHER O OTHER CR CRUISE 1 CE 05 605TW 22568 CDG - DURING CRUISE, NR 1 ENGINE SURGED AT CONSTANT THRUST. ENGINE PARAMETERS WERE NORMAL AFTER THE SURGE. CHECKED ENG INE INLET, EXHAUST, 3.5 BLEED VALVE SCREENS AND OIL MAGNETIC CHIP DETECTORS. ALL CHECKS WERE NORMAL. ADJUSTED ENGINE V ANE BLEED CONTROL. 2 L 7 2 4F 4 F RT A1NM E3NE 1996070300268 19960703 00268 WP 1996 7 3 96ZZZM1031 1 19960510 A 5321 FLOOR DOUG DC9 DC982 3022082 WP BS 1174 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 915TW 49186 MCI - DURING OP-15, FOUND CORROSION ON TOP AND BOTTOM OF FLOOR MEMBRANE, FS 1174, LBL 48 TO LBL 60. REMOVED CORROSION P ER SRM 51-10-3, INSTALLED WEB REPAIR PER SRM 53-01, FIGURE 2 AND 51-30-0, FIGURE 2. (M) 2 L 7 2 4F A6WE 1996070300269 19960703 00269 1996 7 3 96ZZZM1032 4 19960509 A 3442 6225132009 RT UNIT DOUG DC9 DC982 3022082 WP FWD FUSELAGE FAILED A TWAA O OTHER O OTHER CR CRUISE 1 CE 05 909TW 49170 MCI - DURING CRUISE, WEATHER RADAR WOULD NOT PAINT KNOWN WEATHER. REMOVED AND REPLACED RECEIVER/TRANSMITTER UNIT, MFG P /N 622-5132-009, AND RADAR ANTENNA, MFG P/N 622-5136-201. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F A6WE 1996070300270 19960703 00270 1996 7 3 96ZZZM1033 4 19960509 A 3442 6225136201 ANTENNA DOUG DC9 DC982 3022082 WP FWD FUSELAGE FAILED A TWAA O OTHER O OTHER CR CRUISE 1 CE 05 909TW 49170 MCI - DURING CRUISE WEATHER RADAR WOULD NOT PAINT KNOWN WEATHER. REMOVED AND REPLACED RECEIVER/TRANSMITTER UNIT, MFG P/ N 622-5132-009, AND RADAR ANTENNA, MFG P/N 622-5136-201. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F A6WE 1996070300271 19960703 00271 NM 1996 7 3 96ZZZM1034 1 19960512 A 5610 CONNECTORS BOEING 727 727231 1384079 NM R1 WINDOW LOOSE A TWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 54334 20461 STL - DURING CRUISE, R-1 WINDOW ARCED AND EMITTED PUFFS OF SMOKE. TURNED OFF WINDOW HEAT. FOUND LOOSE WIRE AT R-1 WIND OW TERMINAL. CLEANED TERMINAL AND SECURED WIRE. WINDOW HEAT OPERATION CHECKED NORMAL. (M) 2 L 7 3 4F A3WE 1996070300272 19960703 00272 NM 1996 7 3 96ZZZM1035 1 19960512 A 2530 OVEN BOEING 727 727231 1384079 NM FWD GALLEY DIRTY A TWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 54337 20491 STL - DURING CRUISE, FORWARD GALLEY OVEN OVERHEATED AND EMITTED SMOKE. TURNED OFF OVEN. FOUND DEBRIS AND SPILLED FOOD IN OVEN, MFG P/N 5616E. CLEANED OVEN AND OPERATION NORMAL. 2 L 7 3 4F A3WE 1996070300273 19960703 00273 WP 1996 7 3 96ZZZM1036 1 19960514 A 3610 LK75573 DUCT LKHEED 1011 1011385115 5265015 WP NR 1 ENGINE CRACKED A TWAA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 CE 05 31029 193B1109 STL - ON TAKEOFF SHUT DOWN NR 1 ENGINE, S/N 4416, DUE TO NACELLE OVERHEAT LIGHT ILLUMINATION. FOUND STUB DUCT ELBOW, MF G P/N LK75573, CRACKED. REPLACED STUB DUCT. PERFORMED HIGH POWER RUNUP, NO LEAKS NOTED, AND OVERHEAT INDICATION CHECKE D NORMAL. 2 L 7 3 4F A23WE 1996070300274 19960703 00274 WP 1996 7 3 96ZZZM1037 1 19960510 A 5347 TIEDOWN TRACK DOUG DC9 DC982 3022082 WP BS 1212-1322 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 915TW 49186 MCI - DURING OP-15, FOUND CORROSION ON RIGHT TIEDOWN TRACK, FS 1212 TO FS 1322. REPAIRED PER SRM 51-01, PAGE 1, ITEM C, AND TWA STANDARD PRACTICES. 2 L 7 2 4F A6WE 1996070300275 19960703 00275 NM 1996 7 3 96ZZZM1038 1 19960515 A 3232 731414 ACTUATOR BOEING 727 727231 1384079 NM RT MLG DOOR MALFUNCTIONED A TWAA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 54352 21984 MCI - AFTER TAKEOFF, RIGHT MAIN LANDING GEAR DOOR DID NOT CLOSED. CYCLED LANDING GEAR. FOUND LANDING GEAR DOOR ACTUATO R, MFG P/N 7-3141-4, MALFUNCTIONING. REPLACED DOOR ACTUATOR AND DOOR OPERATION AND INDICATION CHECKED NORMAL. (M) 2 L 7 3 4F A3WE 1996070300276 19960703 00276 WP 1996 7 3 96ZZZM1039 1 19960524 A 3260 368658188117 LIGHT SOCKET DOUG DC9 DC982 3022082 WP LT MLG FAILED A TWAA O OTHER P NO WARNING INDICATION AP APPROACH 1 CE 05 909TW 49170 JFK - ON LANDING APPROACH, FOLLOWING GEAR EXTENSION THERE WAS NO LEFT GEAR DOWN AND LOCKED INDICATION. REMOVED AND REPL ACED LEFT GEAR DOWNLOCK LIGHT SOCKET, MFG P/N 368-658-1881-17. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996070300277 19960703 00277 NM 1996 7 3 96ZZZM1040 1 19960521 A 2530 8201110000 OVEN BOEING 767 767205 1385121 NM GALLEY DIRTY A TWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 651TW 23058 JFK - DURING CRUISE E6 OVEN EMITTED SMOKE. TURNED OFF OVEN. FOUND DEBRIS IN OVEN. REPLACED OVEN, MFG P/N 8201-11-0000 . OVEN OPERATION THEN CHECKED NORMAL. 2 L 7 2 4F RT A1NM 1996070300278 19960703 00278 WP 1996 7 3 96ZZZM1041 1 19960522 A 3350 58222 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 951U 49245 STL - DURING PREFLIGHT, EGRESS LIGHT IN FIRST CLASS DID NOT FUNCTION PROPERLY. FOUND POWER SUPPLY, MFG P/N 5822-2, MALF UNCTIONING. REPLACED POWER SUPPLY AND EGRESS LIGHT OPERATION CHECKED NORMAL. 2 L 7 2 4F A6WE 1996070300279 19960703 00279 NE 1996 7 3 96ZZZM1042 2 19960528 A 7230 TURBINE DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE NR 2 ENGINE DAMAGED A TWAA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 CE 05 410EA 47731 STL - DURING APPROACH SHUT DOWN NR 2 ENGINE, S/N 1722, DUE TO INCREASING EGT. ACCOMPLISHED NORMAL LANDING. FOUND TURBI NE DAMAGE AND METAL PARTICLES IN TAILPIPE. REPLACED ENGINE. ENGINE OPERATION THEN CHECKED NORMAL. 2 L 7 2 4F 4 F A6WE E2EA 1996070300280 19960703 00280 NE 1996 7 3 96ZZZM1043 2 19960521 A 7321 7898426009 EEC DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 ENG FAILED A HNAA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 EA 07 982HA 13392 380 FLT 3091 - PHL-DCA - WHILE IN CRUISE, AT 5000 FEET, THE NR 2 ENGINE ROLLED BACK LOSING TORQUE, ITT AND FUEL FLOW. NH ST ABILIZED AT 54 PERCENT. ENGINE WAS OPERATED IN FEATHER UNIT TOUCHDOWN IN ORDER TO RETAIN ELECTRIC AND HYDRAULIC POWER. THE CAPTAIN DECLARED AN EMERGENCY, DIVERTED TO BWI AND LANDED WITHOUT INCIDENT. INSPECTED NR 2 ENGINE, NO DEFECTS NOTE D. REMOVED AND REPLACED THE NR 2 PRPM INDICATOR AND THE NR 2 ELECTRONIC CONTROL UNIT (EEC). REFERENCE HNAA9698232. 2 H 7 2 4T 4 T RT A13NM E20NE 1996070300281 19960703 00281 WP 1996 7 3 96ZZZM1044 1 19960517 A 3260 D50775 CONNECTORS DOUG DC8 DC8F55 3021928 WP RT MLG FAILED A CKSA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 809CK 64985 45803 KMIA - ON THE CLIMB-OUT OF MNMG, THE LANDING GEAR UNSAFE LIGHT REMAINED ON, THE APPROPRIATE CHECKLIST WAS COMPLETED AND THE LANDING GEAR WAS RECYCLED. PERIODICALLY DURING CLIMB-OUT AND IN CRUISE THE LIGHT WENT OUT ONLY TO COME ON AGAIN A S HORT TIME LATER. ALSO, THE INTENSITY OF THE LIGHT VARIED OVER THE COURSE OF THE FLIGHT. THE APPROPRIATE SPEED WAS OBSE RVED AND THE FLIGHT CONTINUED ON TO MIAMI. REMOVED AND REPLACED THE UPLATCH (RT) SWITCH AND CANNON PLUG PER MM 32-60-0. PERFORMED A GEAR RETRACTION PER DC8 MM 32-30-0. OPS CHECK OK. REFERENCE CKSA96051. 2 L 7 4 4F 4A25 1996070300282 19960703 00282 NM 1996 7 3 96ZZZM1045 1 19960416 A 5711 SPAR BOEING 747 747121 1384871 NM LT WING CRACKED A S IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 691UP 19641 DURING PYLON MODIFICATION ON THIS A/C, AN INSPECTION OF THE LEFT WING FRONT SPAR REVEALED CRACKS AT FOUR LOCATIONS AT WI NG STATION 669.5. REF ATTACHED QUERY NOTE S/N 16/95 FOR DETAILS. 2 L 7 4 4F A20WE 1996070300283 19960703 00283 NM 1996 7 3 96ZZZM1046 1 19960610 A 5610 141T48049 WINDOW BOEING 757 75723APF 1384966 NM LT COCKPIT CRACKED A CLCA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 19 572CA 24868 FLT 39 - KMIA-MNMG - DURING FLIGHT, THE L1 WINDOW CRACKED. AIRCRAFT RETURNED TO MIAMI, FLORIDA. REMOVED AND REPLACED W INDOW. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 1996070300284 19960703 00284 SO 1996 7 3 96ZZZM1047 1 19960612 A 5713 12016079002 STRINGER EMB 120 EMB120RT SO RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 227AS 120023 DURING INSPECTION, FOUND THE LEFT WING NR 10 STRINGER INBOARD OF NACELLE AND RIGHT WING STRINGER NR 8 INBOARD OF NACELLE CRACKED. DETERMINED TO BE A MAJOR REPAIR IAW SP663 AND FAR 43 APPENDIX A. REPAIRS WILL BE MADE IAW SRM 57-20-03, FIGU RE 201. REFERENCE ASOA96019. 2 L 7 2 4T RT A31SO 1996070300285 19960703 00285 NM 1996 7 3 96ZZZM1048 1 19960612 A 3230 694614112 UPLOCK ASSY BOEING 737 737301 1384611 NM RT MLG MALFUNCTIONED A USAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 19 300AU 23228 PIT - FL 1595 - AFTER TAKEOFF, RIGHT MAIN GEAR SHOWED RED WHEN GEAR WAS RETRACTED WITH HANDLE IN UP POSITION. CREW SELE CTED OFF POSITION AND RIGHT MAIN GEAR CAME DOWN. CREW THEN POSITIONED GEAR HANDLE TO UP POSITION AND GEAR RETRACTED BUT RED GEAR LIGHT REMAINED ILLUMINATED. FLIGHT LANDED WITH NO FURTHER INCIDENT. MX REPLACED THE RIGHT MAIN LANDING GEAR UPLOCK ACTUATOR, UPLOCK ASSEMBLY AND UPLOCK COLLAR. OPERATIONAL CHECK, LEAK CHECK, GEAR SWING AND FREE FALL CHECKED NOR MAL. REFERENCE USAASB96105. 2 L 7 2 4F RT A16WE 1996070300286 19960703 00286 NM 1996 7 3 96ZZZM1049 1 19960612 A 3230 69518383 UPLOCK COLLAR BOEING 737 737301 1384611 NM RT MLG MALFUNCTIONED A USAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 19 300AU 23228 PIT - FL 1595 - AFTER TAKEOFF, RIGHT MAIN GEAR SHOWED RED WHEN GEAR WAS RETRACTED WITH HANDLE IN UP POSITION. CREW SELE CTED OFF POSITION AND RIGHT MAIN GEAR CAME DOWN. CREW THEN POSITIONED GEAR HANDLE TO UP POSITION AND GEAR RETRACTED BUT RED GEAR LIGHT REMAINED ILLUMINATED. FLIGHT LANDED WITH NO FURTHER INCIDENT. MX REPLACED THE RIGHT MAIN LANDING GEAR UPLOCK ACTUATOR, UPLOCK ASSEMBLY AND UPLOCK COLLAR. OPERATIONAL CHECK, LEAK CHECK, GEAR SWING AND FREE FALL CHECKED NOR MAL. REFERENCE USAASB96105. 2 L 7 2 4F RT A16WE 1996070300287 19960703 00287 NM 1996 7 3 96ZZZM1050 1 19960611 A 3260 655825029 CIRCUIT CARD BOEING 737 737301 1384611 NM RT MLG MALFUNCTIONED A USAA O OTHER N FALSE WARNING CL CLIMB 1 EA 19 300AU 23228 PHL - FLT 1868 - ON GEAR RETRACTION, RIGHT MAIN GEAR RED LIGHT STAYED ON WITH HANDLE IN UP POSITION. CREW RECYCLED BREA KERS AND THEN THE GEAR RED LIGHT WENT OUT APPROXIMATELY TWO MINUTES LATER. FLIGHT LANDED WITH NO FURTHER INCIDENTS. MX REPLACED PROX CARDS M982 AND M986. OPS CHECK PER MX MANUAL GOOD. REFERENCE 655825029. 2 L 7 2 4F RT A16WE 1996070300288 19960703 00288 EU 1996 7 3 96ZZZM1051 1 19960607 A 7830 189188002 T/R CABLES FOKKER F28 F28MK0100 4990807 EU NR 1 ENGINE BROKEN A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 893US 11373 PIT - FLT 1672 - CREW COULD NOT ADVANCE THROTTLES PAST 34 UNITS DURING CLIMB. FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT. MX FOUND THE NR 1 THRUST REVERSER FEEDBACK CABLES FROZEN AND BROKEN. CABLES WERE REPLACED. (M) 2 L 7 2 4F RT 1996070300289 19960703 00289 CE 1996 7 3 96ZZZM1052 1 19960606 A 7931 1143800097 OIL PSI GAUGE BEECH 1900 1900D 1154162 CE RT ENGINE MALFUNCTIONED A S2YA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 13 801SK 5508 UE80 THE FLIGHT CREW NOTICED THE RIGHT ENGINE OIL PRESSURE INDICATION HAD DROPPED TO 27 PSI, BUT NO 'LOW PRESSURE' LIGHT. TH EY TURNED BACKED TO MKE (FLT NR 1162 MKE-SBN) AND TOOK PRECAUTION TO SAVE THE ENGINE BY FEATHERING IT ON FINAL APPROACH. MX REPLACED THE RIGHT OIL PRESSURE INDICATOR AND THE OIL PRESSURE TRANSDUCER P/N NR 101-3899023-5 S/N 4614-1-73. (M) 2 L 7 2 4T RT A24CE 1996070300290 19960703 00290 NM 1996 7 3 96ZZZM1053 1 19960607 A 3350 0791R LENS BRUCE BOEING 727 727254 138408L NM CABIN MISSING A TAOA K NONE O OTHER IN INSP/MAINT 1 EA 15 915TS 20252 FLT 6181 - BOS/LGA - EMERGENCY PATH LIGHTING COVER AND LAMP MISSING AREA ROW 14. FOUND ON OVER NIGHT CHECK. REPLACED LAMP AND INSTALLED NEW LAMP COVER, OPS CHECKS OK. REFERENCE TAOA069605. 2 L 7 3 4F A3WE 1996070300291 19960703 00291 WP 1996 7 3 96ZZZM1054 1 19960420 A 2910 2337926 HYDRAULIC LINE 5333641 DOUG DC6 DC6B 3021712 WP LT MLG CHAFED A NACA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 AL 03 434TA 44434 FLIGHT 601 - RETURNED TO FAI DUE TO NO HYDRAULIC PRESSURE AND NO HYDRAULIC QUANTITY. MX REPLACED HYDRAULIC LINE ON LEFT MLG RETRACT STRUT. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 4 4R 6A4 1996070300292 19960703 00292 NE 1996 7 3 96ZZZM1055 2 19960510 A 8530 327627 CYLINDER ASSY DOUG DC6 DC6B 3021712 WP PWA R2800 CB3 52026 NE NR 3 ENGINE RINGLAND FAILURE A NACA E A ENGINE SHUTDOWN UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 AL 03 434TA 1598 44434 P28433 FLT 601 - SHUT DOWN NR 3 ENGINE AT 2030Z DUE TO BACKFIRING. AIRCRAFT RETURNED TO ANC. MX REPLACED NR 18 CYLINDER ASSY DUE TO RINGLAND FAILURE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 4 4R 4 R 6A4 E264 1996070300293 19960703 00293 NE 1996 7 3 96ZZZM1056 2 19960515 A 8530 327628 CYLINDER ASSY DOUG DC6 DC6A 3021706 WP PWA R2800 CB3 52026 NE NR 1 ENGINE CRACKED A NACA E ENGINE SHUTDOWN E VIBRATION/BUFFET CR CRUISE 1 AL 03 779TA 45529 P35160 FLT 312 - SHUTDOWN NR 1 ENGINE AT 1830Z DUE TO BACKFIRING IN RICH AND MANUAL LEAN. AIRCRAFT FERRIED TO ANC FROM ENM. M X REPLACED NR 13 CYLINDER ASSY DUE TO CRACKED HEAD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 4 4R 4 R 6A3 E264 1996070300294 19960703 00294 1996 7 3 96ZZZM1057 4 19960529 A 3442 20671570153 RT UNIT DOUG DC9 DC932 3022066 WP RADAR MALFUNCTIONED A VJ6A A UNSCHED LANDING O OTHER CL CLIMB 1 SO 11 946VV 47226 ON FLT 537 - ATL-TPA - AIR RETURN, WEATHER RADAR HAS 'NO RETURNS' IN FLIGHT, GROUND TEST NORMAL. REMOVED AND REPLACED R /T AND ANTENNA, OPS CHECK NORMAL PER MM 34-40. (M) 2 L 7 2 4F A6WE 1996070300295 19960703 00295 1996 7 3 96ZZZM1058 4 19960529 A 3442 20871790501 ANTENNA DOUG DC9 DC932 3022066 WP RADAR MALFUNCTIONED A VJ6A A UNSCHED LANDING O OTHER CL CLIMB 1 SO 11 946VV 47226 ON FLT 537 - ATL-TPA - AIR RETURN, WEATHER RADAR HAS 'NO RETURNS' IN FLIGHT, GROUND TEST NORMAL. REMOVED AND REPLACED R /T AND ANTENNA, OPS CHECK NORMAL PER MM 34-40. 2 L 7 2 4F A6WE 1996070300296 19960703 00296 WP 1996 7 3 96ZZZM1059 1 19960515 A 2421 GENERATOR DOUG DC9 DC932 3022066 WP LEFT TRIPPED A VJ6A A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 11 920VV 47674 ON FLT 510 - ATL-BNA - AIR RETURN, AT 20,000 FEET THE LEFT GENERATOR TRIPPED WITH A/C X-TIE LOCK OUT, RESET GENERATOR, V OLTS AND FREQS NORMAL, BUT TRIPPED AGAIN WHEN PUT ON LINE. CHECKED LEFT ENGINE GENERATOR CABLE FROM GENERATOR TO RELAY, CHECKS OK. RAN ENGINES PERFORMED CROSS TIE CHECK, OPS CHECK GOOD PER MM 24-20-00. (M) 2 L 7 2 4F A6WE 1996070300298 19960703 00298 GL 1996 7 3 AALA960689 2 19960429 A 7320 PB3 LINE DOUG MD11 MD11 3023602 NM GE CF6 CF6* 30020 GL NR 1 ENG LOOSE A A AALA E ENGINE SHUTDOWN X ENGINE FLAMEOUT CR CRUISE 1 SW 07 1762B 48552 BOS - FLT 86 - EN ROUTE ORD/LHR DURING CRUISE AT FL 290, NR 1 ENGINE SPOOLED DOWN. ATTEMPTED RESTART WAS UNSUCCESSFUL. AIRCRAFT DESCENDED TO FL250 AND RESTART WAS SUCCESSFUL, HOWEVER, ENGINE WOULD NOT ADVANCE PAST IDLE. AIRCRAFT DIVERTED TO BOS AND LANDED WITHOUT INCIDENT. ACCOMPLISHED CFDS, ECU AND FCC FAULT REVIEW WITH NO FAULTS FOUND. RESECURED NR 1 ENGINE PB3 LINE FOUND LOOSE AT ECU AND PRECAUTIONARY CHANGED NR 1 ENGINE FUEL FILTER. ACCOMPLISHED LEAK CHECK AND GROUN D ENGINE RUN WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. ACCOMPLISHED FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS FOUND. SYSTEM OPS CHECK NORMAL. (M) 2 L 7 3 4F 4 F RT A22WE E23EA 1996070300299 19960703 00299 EU 1996 7 3 AALA960719 1 19960503 A 3397 WIRE AIRBUS 300 A300B4605R 3930308 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77080 626 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT AT LEFT AISLE OF MAIN CABIN INOPERATIVE. REPAIRED BROKEN EMERGENCY FLOOR LIGHT WIRE AT LEFT AISLE OF MAIN CABIN BY PAX SEAT ROW 21. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996070300300 19960703 00300 NM 1996 7 3 AALA960763 1 19960510 A 3350 A3060698101 CONNECTOR DOUG MD11 MD11 3023602 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1764B 48554 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 8D TO 12D INOPERATIVE. REPLACED CORRODED EME RGENCY FLOOR LIGHT STRIP CONNECTOR BY PAX SEAT ROW 12D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1996070300301 19960703 00301 EU 1996 7 3 AALA960766 1 19960507 A 3350 STRIP AIRBUS 300 A300B4605R 3930308 EU CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7082A 643 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 12 AND 14 INOPERATIVE. REPLACED DAMAGED EMER GENCY FLOOR LIGHT STRIP BETWEEN PAX SEAT ROWS 12 AND 14. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996070300302 19960703 00302 EU 1996 7 3 AALA960771 1 19960513 A 3350 A3060833101 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7062A 474 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT STRIP AT L2/R2 CROSS AILSE INOPERATIVE. REPLACED BROKEN EMERGENCY F LOOR LIGHT STRIP CONNECTOR AT L2/R2 CROSS AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996070300303 19960703 00303 EU 1996 7 3 AALA960772 1 19960514 A 3350 STRIP AIRBUS 300 A300B4605R 3930308 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 50051 459 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PAX SEAT ROWS 27AB AND 28AB INOPERATIVE. REPLACED EMERGENCY FLO OR LIGHT STRIP BY PAX SEAT ROWS 27AB AND 28AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996070300304 19960703 00304 WP 1996 7 3 AALA960773 1 19960514 A 2133 20219742 OUTFLOW VLV ACT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A A AALA B G A EMER. DESCENT O2 MASK DEPLOYED UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 553AA 53083 PHX - FLT 1172 - AFTER TAKEOFF PHX DURING CLIMB-OUT, UNABLE TO PRESSURIZE A/C IN EITHER AUTO OR MANUAL MODE. ACCOMP EME RGENCY DESCENT AND ALL PAX OXYGEN MASKS SUCCESSFULLY DEPLOYED. A/C RETURNED TO PHX AND LANDED W/O INCIDENT. REPLACED N R 1 PRESSURIZATION CONTROLLER AND GROUND CONTROL RELAYS R2-4 AND R2-106. SYSTEM GROUND CHECKED NORMAL OPERATION. A/C M AINTENANCE FERRY PHX/TUL. RESTOWED ALL PAX OXYGEN MASKS AND SERVICED PAX OXYGEN SYS. ACCOMPLISHED FUNCTIONAL CHECK FLI GHT AND PRESSURIZATION PROBLEM REPEATED. REPLACED OUTFLOW VALVE ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPS. ACCOMP FU NCTIONAL CHECK/FERRY FLIGHT WITH NO DEFECTS FOUND. SYS OPS CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 1996070300305 19960703 00305 NM 1996 7 3 AALA960779 1 19960502 A 5311 143T10601 FRAME BOEING 767 767323 1385205 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 354AA 24035 AFW - FOUND AREA OF CORROSION BEYOND SRM LIMITS. BLENDED OUT DAMAGE PER ENGINEERING MRB 767-1230. (M) 2 L 7 2 4F RT A1NM 1996070300306 19960703 00306 NM 1996 7 3 AALA960780 1 19960510 A 5311 143T10601 FRAME BOEING 767 767323 1385205 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 354AA 24035 AFW - FOUND AREA OF CORROSION BEYOND SRM LIMITS. BLENDED OUT DAMAGE PER ENGINEERING MRB 767-1231. (M) 2 L 7 2 4F RT A1NM 1996070300307 19960703 00307 NM 1996 7 3 AALA960781 1 19960508 A 5320 143TB2042 STOP BOEING 767 767323 1385205 NM BS 568-570 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 354AA 24035 AFW - ROLLOUT STOP ATTACH BOLT HOLES CORRODED BEYOND SRM LIMITS. INSTALLED 1 INCH DIAMETER FREEZE PLUGS PER ENGINEERING MRB 767-1233. (M) 2 L 7 2 4F RT A1NM 1996070300308 19960703 00308 NM 1996 7 3 AALA960784 1 19960516 A 3350 1000679 LIGHT BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 355AA 24036 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT OVER COCKPIT DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT OVER CO CKPIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1996070300309 19960703 00309 EU 1996 7 3 AALA960785 1 19960519 A 3350 STRIP AIRBUS 300 A300B4605R 3930308 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 14077 612 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS FROM PAX SEAT ROW 37B AND AFT INOPERATIVE. REPLACED EMERGENCY FLOO R LIGHT STRIP FROM PAX SEAT ROW 37B AND AFT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996070300310 19960703 00310 WP 1996 7 3 AALA960786 1 19960517 A 3260 PSEU DOUG DC9 DC982 3022082 WP LANDING GEAR MALFUNCTIONED A AALA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 7544A 53026 ORD - FLT 1774 - DURING APPROACH TO ORD WHEN LANDING GEAR EXTENDED, NOSE LANDING GEAR RED LIGHT REMAINED ILLUMINATED WIT H 4 ANTI-SKID LIGHTS ON. CONFIRMED NOSE LANDING GEAR WAS FULLY EXTENDED AND AIRCRAFT LANDED ORD WITHOUT INCIDENT. WHIL E AIRCRFT WAS BEING TOWED TO GATE, NOSE LANDING GEAR LIGHT CHANGED TO GREEN INDICATION BUT ANTI-SKID WOULD NOT ARM. ACC OMPLISHED LANDING GEAR RETRACTION CHECK FOR SEVERAL CYCLED BUT UNABLE TO DUPLICATE PROBLEM. ALL LANDING GEAR INDICATION S AND ANTI-SKID FUNCTION CHECKED NORMAL. PRECAUTIONRAY RESEATED LANDING GEAR PSEU AND AIRCRAFT RETURNED TO SERVICE. (M ) 2 L 7 2 4F A6WE 1996070300311 19960703 00311 NM 1996 7 3 AALA960812 1 19960521 A 3350 STRIP DOUG MD11 MD11 3023602 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1752K 48421 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN LAV B AND RIGHT AISLE GALLEY NR 3 INOPERATIVE. REPLACED EM ERGENCY FLOOR LIGHT STRIP BETWEEN LAV B AND RIGHT AISLE GALLEY NR 3 SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1996070300312 19960703 00312 EU 1996 7 3 AALA960814 1 19960522 A 3350 STRIP AIRBUS 300 A300B4605R 3930308 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7083A 645 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEEN PAX SEAT ROWS 20AB. SYSTEM GROUND CHECKED NORMAL OPERATIO N. (M) 2 L 7 2 4F RT A35EU 1996070300313 19960703 00313 WP 1996 7 3 AALA960822 1 19960523 A 3260 S1412 SWITCH DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 574AA 53151 SFO - FLT 483 - DURING APPROACH TO SFO, WHEN LANDING GEAR EXTENDED, NOSE LANDING GEAR UNSAFE LIGHT ILLUMINATED. RECYCLE D LANDING GEAR AND NO UNSAFE OR GREEN LIGHT ILLUMINATED. AIRCRAFT PERFORMED TOWER FLY-BY AND VISUALLY CONFIRMED NOSE LA NDING GEAR EXTENDED AND DURING SECOND LANDING APPROACH, NOSE LANDING GEAR GREEN LIGHT ILLUMINATED. AIRCRAFT LANDED SFO WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR SWITCH S1-412. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996070300314 19960703 00314 WP 1996 7 3 AALA960824 1 19960524 A 2613 5890966 TEMP SENSOR DOUG DC9 DC982 3022082 WP TAIL COMPT DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 439AA 49457 DFW - FLT 2016 - ON ROTATION OUT OF DFW, THE TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. RETURNED TO LAND DFW AND LIGHT EXTINGUISHED WITH POWER REDUCTION. LIGHT ILLUMINATED AGAIN WITH POWER INCREASE. LANDED DFW WITHOUT INCIDENT AND NORMAL WEIGHT. REPLACED BOTH TAIL COMPARTMENT HIGH TEMPERATURE SENSOR AND ACCOMPLISHED DUCT LEAK CHECK DURING ENGIN E RUN UP AT HIGH POWER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996070300315 19960703 00315 EU 1996 7 3 AALA960825 1 19960525 A 3350 STRIP AIRBUS 300 A300B4605R 3930308 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 80084 675 JFK - DURING OVERNIGHT CHECK, FOUND BROKEN EMERGENCY EXIT FLOOR PATH LIGHT STRIP ON LEFT SIDE OF AIRCRAFT. REPLACED EME RGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996070300316 19960703 00316 EU 1996 7 3 AALA960830 1 19960527 A 3397 WIRE AIRBUS 300 A300B4605R 3930308 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 14077 612 MIA - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT ROW 24R INOPERATIVE. REPAIRED EMERGENCY EXIT FLO OR PATH LIGHTS AT SEAT ROW 24R. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996070300317 19960703 00317 WP 1996 7 3 AALA960834 1 19960525 A 7110 AAP2936 NOSE COWL DOUG DC9 DC982 3022082 WP LT ENG CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 480AA 49298 49655 SAT - DURING ROUTINE MAINTENANCE, FOUND A CRACK AT THE 6 O'CLOCK POSITION ON THE LEFT ENGINE NOSE COWL. CRACK IS LOCATE D 1.5 INCHES AFT OF NOSE COWL LIP SEAM AND ABOUT 3 INCHES OUTBOARD OF NOSE COWL INSPECTION PANEL. APPLIED SPEED TAPE TO DAMAGED AREA, APPROVED FOR ONE TIME FLIGHT FROM SAT TO DFW FOR NOSE COWL REPLACEMENT. FLEW FROM SAT TO DFW AND LANDED WITHOUT INCIDENT. REPLACED LEFT ENGINE COWL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996070300318 19960703 00318 SO 1996 7 3 ASOA96019 1 19960612 A 5713 12016085001 STRINGER EMB 120 EMB120RT SO LT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 227AS 120023 DURING INSPECTION, FOUND THE LEFT WING NR 10 STRINGER INBOARD OF NACELLE AND RIGHT WING STRINGER NR 8 INBOARD OF NACELLE CRACKED. DETERMINED TO BE A MAJOR REPAIR IAW SP663 AND FAR 43 APPENDIX A. REPAIRS WILL BE MADE IAW SRM 57-20-03, FIGU RE 201. (M) 2 L 7 2 4T RT A31SO 1996070300319 19960703 00319 EU 1996 7 3 AWXA960243 1 19960523 A 3350 LIGHTS AIRBUS 320 A320231 3930325 EU CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 629AW 076 PHX - FLT 522 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS INOP ON SEVERAL CABIN SEATS. RESET BATTERY POW ER SUPPLY UNITS. (M) 2 L 7 2 4F RT A28NM 1996070300320 19960703 00320 NM 1996 7 3 AWXA960245 1 19960524 A 7714 WL101EED3 N1 INDICATOR BOEING 737 7373G7 1384595 NM NR 1 ENGINE FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 302AW 28173 AD555116 24009 PHX - FLT 52 - PHX-SJD - AIR TURNBACK, NR 1 ENGINE N1 INDICATOR INOP DIGITAL AND ANALOG. REPLACED N1 INDICATOR. (M) 2 L 7 2 4F RT A16WE 1996070300321 19960703 00321 NM 1996 7 3 AWXA960248 1 19960531 A 2913 3508807 HYD PUMP BOEING 757 7572S7 1384962 NM RT ENGINE FAILED A AWXA K NONE J WARNING INDICATION CR CRUISE 1 WP 28 906AW 23568 ATL - FLT 610 - PHX-ATL - RIGHT ENGINE DRIVE HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATED AT CRUISE ALTITUDE. RIGHT HY DRAULIC ENGINE PUMP EICAS MESSAGE DISPLAYED. REPLACED RIGHT ENGINE DRIVE HYDRAULIC PUMP, REPLACED CASE DRAIN AND PRESSU RE AND RETURN FILTERS. OPERATES OK GOOD ON RUN. REPLACED FILTERS AGAIN. LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 1996070300322 19960703 00322 NE 1996 7 3 AWXA960257 2 19960602 A 7200 ENGINE BOEING 737 737277 1384570 NM PWA JT8 JT8D15 52051 NE NR 2 BIRD STRIKE A AWXA A UNSCHED LANDING C F.O.D. CL CLIMB 1 WP 28 185AW P708905B 22652 MDW-CMH - FLT 828 - AIR TURN BACK, BIRD STRIKE IN THE NR 2 ENGINE. ALL FAN BLADES IN THE INLET WERE DAMAGED. ENGINE HA D SEVERAL COMPRESSOR STALLS AFTER THE BIRD STRIKE. CAPTAIN DECLARED AN EMERGENCY BUT DID NOT SHUT ENGINE DOWN UNTIL AFT ER LANDING. REMOVED AND REPLACED NR 2 ENGINE. (M) 2 L 7 2 4F 4 F RT A16WE E2EA 1996070300323 19960703 00323 EU 1996 7 3 AWXA960264 1 19960609 A 3397 WIRE AIRBUS 320 A320231 3930325 EU CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 633AW 082 PHX - FLT 2851 - DURING ROUTINE MX CHECK, FOUND ROW 22 EMERGENCY EXIT LIGHT INOP ON END OF LEFT SEAT ROW. REPAIRED BROK EN WIRE AT CANNON PLUG. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A28NM 1996070300324 19960703 00324 NE 1996 7 3 AWXA960265 2 19960610 A 7530 658385 PRBC ASSEMBLY BOEING 737 737277 1384570 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE FAILED A AWXA C D ABORTED TAKEOFF RETURN TO BLOCK J R WARNING INDICATION PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 28 185AW 6158721 22652 PHX-OMA - ABORTED TAKEOFF, NR 1 ENGINE HAD COMPRESSOR STALL ONCE WHEN POWER ADVANCED ABOVE IDLE. REMOVED AND REPLACED N R 1 ENGINE PRESSURE RATIO BLEED CONTROL ASSEMBLY, IAW BMM 75-31-11. ALSO, LUBRICATED INTERNAL BLEEDS PER EB 72-006. RA N ENGINES AND OPERATES NORMALLY. (M) 2 L 7 2 4F 4 F RT A16WE E2EA 1996070300325 19960703 00325 NM 1996 7 3 AWXA960267 1 19960608 A 7711 EPR INDICATION BOEING 737 737277 1384570 NM NR 1 ENGINE MALFUNCTIONED A AWXA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 28 184AW 22651 ONT - FLT 2110 - ONT-LAS - ABORTED TAKEOFF, AUTO THROTTLE ENGAGED. DURING TAKEOFF ROLL NR 1 ENGINE EPR DID NOT INDICATE MORE THAN 1.8. PERFORMED TAKEOFF POWER RUN SEVERAL TIMES. NO DEFECT NOTED IN EPR SYSTEM NR 1 ENGINE. (M) 2 L 7 2 4F RT A16WE 1996070300326 19960703 00326 NM 1996 7 3 AWXA960271 1 19960613 A 3233 273N20062 ACTUATOR BOEING 757 757225 1384959 NM RT MLG FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 914AW 37117 SA00100 22208 PHX-ORD - AIR TURN BACK, EICAS MESSAGE GEAR DOORS AND GEAR DISAGREE DIPLAYED WITH GEAR HANDLE UP. DOOR AND GEAR AMBER L IGHTS ILLUMINATED ALL GREEN. DOWN LIGHT EXTINGUISHED WITH GEAR HANDLE OFF. RIGHT GEAR DOWN LIGHT ILLUMINATED. REMOVED AND REPLACED RIGHT MLG ACTUATOR PER BOEING MM REF 32-32-01. PERFORMED GEAR SWING SEVERAL TIMES AND OPS CHECKED GOOD. ( M) 2 L 7 2 4F RT A2NM 1996070300327 19960703 00327 SO 1996 7 3 C2XA96IA141 1 19960607 A 6120 7902015 PROP ACTUATOR EMB 120 EMB120RT SO RT PROP SEIZED A A C2XA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 09 57734 12104 120199 IAH - FLT 3830 - DURING TAKEOFF ROLL, THE NR 2 ENGINE PRODUCED ONLY 22 PERCENT TORQUE. AIRCRAFT RETURNED, MX FOUND THE RIGHT PROPELLER ACTUATOR PITCH CHANGE MECHANISM SEIZED. THE RIGHT PROPELLER ACTUATOR WAS REMOVED AND REPLACED GROUND OPE RATIONAL, LEAK CHECKS GOOD. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996070300328 19960703 00328 NE 1996 7 3 C2XA96IA142 2 19960605 A 7200 ENGINE AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE NR 2 FAILED A A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 09 14832 16222 187 120436 FLT 3965 - IAH-HRL - DIVERTED TO CPR DECLARED CREW PRECAUTIONARY WITH LOW OIL PRESSURE INDICATION ON NR 2 ENGINE. MX SE RVICED NR 2 ENGINE WITH 12 PT OF OIL, GROUND RAN ENGINE AT 80 PERCENT NH CABIN FILLED WITH SMOKE. AIRCRAFT FERRIED CPR TO IAH RIGHT BLEED OFF. MX REMOVED AND REPLACED NR 2 ENGINE GROUND OPERATIONAL, LEAKS CHECKS GOOD. AIRCRAFT WAS APPROV ED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1996070300329 19960703 00329 SO 1996 7 3 C2XA96IA143 1 19960606 A 3260 M610627023 WOW CONTROL EMB 120 EMB120RT SO NLG FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 40717 120133 IAH - FLT 3866 - AFTER TAKEOFF AND GEAR RETRACTION HAD CONTINOUS AURAL WARNING, BRAKES, TRIM, FLAPS, AUTOFEATHER. AIRCR AFT EXECUTED AIR RETURN TO IAH. MX REMOVED, CLEANED AND RESECURED WOW CANNON PLUGS. AURAL WARNINGS OPS CHECKED GOOD. A IRCRAFT AIR RETURNED SECOND TIME WITH DUPLICATE PROBLEM. MX REMOVED AND REPLACED NOSE LANDING GEAR WOW CONTROL RELAY, O PS CHECKED GOOD. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996070300330 19960703 00330 EU 1996 7 3 C2XA96IA145 1 19960613 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FR 36-39 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15816 105 IAH - DURING C-CHECK INSPECTION, THE RIGHT FLIGHT ATTENDANT SEAT TRACK WAS FOUND TO BE CORRODED. MX REMOVED AND REPLACE D THE RIGHT SEAT TRACK AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996070300331 19960703 00331 EU 1996 7 3 C2XA96IA146 1 19960613 A 2710 ABS0345N04 BEARING AEROSP ATR42 ATR42320 8680930 EU LT AILERON RUSTED BEARING A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15816 105 IAH - DURING C-CHECK INSPECTION, THE LEFT AILERON BELLCRANK INSIDE PANEL 544AB WAS FOUND TO HAVE A RUSTED AFT BEARING. M X REMOVED AND REPLACED THE BELLCRANK AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996070300332 19960703 00332 EU 1996 7 3 C2XA96IA147 1 19960613 A 2710 S2718141700200 LEVER ASSY AEROSP ATR42 ATR42320 8680930 EU AILERON BEARINGS BAD A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15816 105 IAH - DURING C-CHECK INSPECTION, THE AILERON INTERCONNECT ROD WAS FOUND TO HAVE STIFF BEARINGS ON THE LEFT END. MX REMO VED AND REPLACED THE LEFT LEVER ASSEMBLY AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996070300333 19960703 00333 EU 1996 7 3 C2XA96IA148 1 19960613 A 5313 S53671200218 STRINGER AEROSP ATR42 ATR42320 8680930 EU FRAME 36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15816 105 IAH - DURING C-CHECK INSPECTION, STRINGER 16 RIGHT AT FRAME 36 WAS FOUND TO BE CORRODED. MX REMOVED THE DAMAGED PORTION OF THE STRINGER AND INSTALLED A REPAIR DOUBLER PER ATR 42 SRM 53-00-00 AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996070300334 19960703 00334 EU 1996 7 3 C2XA96IA149 1 19960613 A 5311 FRAME AEROSP ATR42 ATR42320 8680930 EU FRAME 35 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15816 105 IAH - DURING C-CHECK INSPECTION, FRAME 35 AT STRINGER 17 RIGHT WAS FOUND TO BE CORRODED. MX REMOVED THE DAMAGED PORTION OF THE FRAME AND FABRICATED AND INSTALLED A REPAIR DOUBLER PER ATR SRM 53-00-00 AND THE AIRCRAFT WAS RETURNED TO SERVIC E. (M) 2 H 7 2 4T RT A53EU 1996070300335 19960703 00335 EU 1996 7 3 C2XA96IA150 1 19960613 A 5315 S5367240620802 FLOOR BEAM AEROSP ATR42 ATR42320 8680930 EU FRAME 36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15816 105 IAH - DURING C-CHECK INSPECTION, THE FLOOR SUPPORT BEAM AT FRAME 36 WAS FOUND TO BE CORRODED. MX REMOVED AND REPLACED T HE FLOOR BEAM AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996070300336 19960703 00336 EU 1996 7 3 C2XA96IA151 1 19960613 A 5230 S5237611420501 FITTING AEROSP ATR42 ATR42320 8680930 EU CARGO DOOR CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15816 105 IAH - DURING C-CHECK INSPECTION, THE CARGO DOOR ACTUATOR FITTING ON THE CARGO DOOR WAS FOUND TO BE CRACKED. MX REMOVED AND REPLACED THE FITTING AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996070300337 19960703 00337 WP 1996 7 3 CKSA96051 1 19960517 A 3260 H146 SWITCH DOUG DC8 DC8F55 3021928 WP RT MLG FAILED A CKSA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 809CK 64985 45803 KMIA - ON THE CLIMB-OUT OF MNMG, THE LANDING GEAR UNSAFE LIGHT REMAINED ON, THE APPROPRIATE CHECKLIST WAS COMPLETED AND THE LANDING GEAR WAS RECYCLED. PERIODICALLY DURING CLIMB-OUT AND IN CRUISE, THE LIGHT WENT OUT ONLY TO COME ON AGAIN A SHORT TIME LATER. ALSO, THE INTENSITY OF THE LIGHT VARIED OVER THE COURSE OF THE FLIGHT. THE APPROPRIATE SPEED WAS OBS ERVE AND THE FLIGHT CONTINUED ON TO MIAMI. REMOVED AND REPLACED THE UPLATCH (RT) SWITCH AND CANNON PLUG PER MM 32-60-0. PERFORMED A GEAR RETRACTION PER DC8 MM 32-30-0. OPS CHECK OK. (M) 2 L 7 4 4F 4A25 1996070300338 19960703 00338 EA 1996 7 3 HNAA9690531 1 19960518 A 3230 166805 UPLOCK CYL MENASCO DHAV DHC7 DHC7102 2802708 EA NLG FAILED A HNAA K NONE J WARNING INDICATION AP APPROACH 1 EA 07 905HA 1241 MC140 070 FLT NR 3332 - PHL-DCA - ON APPROACH INTO DCA, THE NOSE WHEEL ATTEMPTS TO CYCLE DOWN WITH GEAR HANDLE IN THE UP POSITION. INDICATIONS ARE A RED NOSE UNSAFE LIGHT FOLLOWED BY A HANDLE LIGHT AT WHICH TIME THE HYDRAULIC SYSTEM TAKES OVER AND F ORCES THE GEAR BACK INTO THE COMMANED POSITION. THE AIRCRAFT LANDED IN DCA WITHOUT INCIDENT. REMOVED AND REPLACED THE NOSE LANDING GEAR UPLOCK BUNGEE ASSEMBLY. (M) 2 H 7 4 4T A20EA 1996070300339 19960703 00339 NE 1996 7 3 HNAA9691729 2 19960515 A 7200 ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 FAILED A HNAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 917HA 075 FLT NR 3461 - MIA-MCO - ON CLIMB-OUT, THE NR 1 ENGINE LOW OIL PRESSURE WARNING LIGHT CAME ON, PRESSURE DECREASED, AND TH E CREW SHUT THE ENGINE DOWN. THE AIRCRAFT TURNED BACK TO MIA AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE NR 1 ENGINE. (M) 2 H 7 2 4T 4 T RT A13NM E20NE 1996070300340 19960703 00340 NM 1996 7 3 HNAA9694328 1 19960515 A 2910 AE2460501E0240 HYD FLEX LINE DHAV DHC8 DHC8102 2809003 NM NR 2 HYD SYSTEM LEAKING A HNAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 07 943HA 18535 167 FLT 3154 - BWI-GSO - DURING FLIGHT, THE NR 2 SYSTEM HYDRAULIC FLUID QUANTITY BEGAN DROPPING. THE CAPTAIN DECLARED AN EM ERGENCY AND RETURNED TO BWI, LANDING WITHOUT INCIDENT. FOUND THE PRESSURE LINE TO INBOARD GROUND SPOILER ACTUATOR LEAKI NG. INSTALLED A TEMPORARY FLEX LINE TO THE RIGHT INBOARD GROUND SPOILER FROM THE CENTER WING AREA. (M) 2 H 7 2 4T RT A13NM 1996070300341 19960703 00341 1996 7 3 HNAA9698232 3 19960521 A 6140 SEL0C29DF PRPM INDICATOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE COCKPIT FAILED A HNAA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 EA 07 982HA 17006 380 FLT 3091 - PHL-DCA - WHILE IN CRUISE, AT 5000 FEET, THE NR 2 ENGINE ROLLED BACK LOSING TORQUE, ITT AND FUEL FLOW. NH ST ABILIZED AT 54 PERCENT. ENGINE WAS OPERATED IN FEATHER UNIT TOUCHDOWN IN ORDER TO RETAIN ELECTRIC AND HYDRAULIC POWER. THE CAPTAIN DECLARED AN EMERGENCY, DIVERTED TO BWI AND LANDED WITHOUT INCIDENT. INSPECTED NR 2 ENGINE, NO DEFECTS NOTE D. REMOVED AND REPLACED THE NR 2 PRPM INDICATOR AND THE NR 2 ELECTRONIC CONTROL UNIT (EEC). (M) 2 H 7 2 4T 4 T RT A13NM E20NE 1996070300342 19960703 00342 WP 1996 7 3 IXXA9682 1 19960525 A 2611 303261 CONTROL AMP DOUG DC8 DC862 3021970 WP COCKPIT INTERMITTENT A IXXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 11 51CX 46027 EN ROUTE BETWEEN ELP AND TOL IN CRUISE FLIGHT AT FL 37, THE MAIN CARGO COMPARTMENT SMOKE DETECTOR LIGHT ILLUMINATED. AT C WAS ADVISED, AND THE AIRCRAFT DIVERTED TO OKC. ON THE GROUND IN OKC, AND AIRCRAFT WAS CHECKED FOR SIGNS OF FIRE, SMOK E, OR ODORS OF COMBUSITON. NONE WERE FOUND IN THE MAIN CARGO COMPARTMENT OR THE BELLY COMPARTMENTS. TROUBLESHOOTING OF THE SMOKE DETECTOR SYSTEM REVEALED A SMOKE DETECTOR CONTROL AMPLIFIER WHICH INTERMITTENTLY PRODUCES A FALSE WARNING LIG HT ON THE GROUND. THE AMPLIFIER WAS REPLACED, AND THE AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 4 4F 4A25 1996070300343 19960703 00343 WP 1996 7 3 IXXA9687 1 19960609 A 2120 AIR DISTR DOUG DC8 DC871 302199A WP CABIN ODOR A IXXA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 11 829BX 45994 EN ROUTE TOL-BFI - A STRONG SMELL OF HOT ELECTRICAL EQUIPMENT WAS NOTED IN THE VICINITY OF THE CIRCUIT BREAKER PANEL BUL KHEAD. MX POWERED UP ALL EQUIPMENT ON THE GROUND WITH NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 4 4F 4A25 1996070300344 19960703 00344 NM 1996 7 3 MZZA96048 1 19960522 A 5330 SKIN BOEING 727 727232 1384082 NM BS 530 MISDRILLED A MZZA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 13 15790 20644 TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, TWO RIVET SPACING WAS FOUND BELOW THE SPECIFIED LIMIT ON BS 5 30, STRINGER 27L THE DAMAGED SKIN WAS REPAIRED PER B727 SRM 53-30-3. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 80683 5. (SEQ NR 01084) (M) 2 L 7 3 4F A3WE 1996070300345 19960703 00345 NM 1996 7 3 MZZA96049 1 19960523 A 5320 FRAME BOEING 727 727232 1384082 NM C2 CARGO DOOR CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15790 20644 TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON C3 CARGO DOOR LOWER FRAME FORME D, SECTION. THE CORRODED FORMED SECTION WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-3. REF, HANGAR NON ROUTINE REP AIR ITEM CARD NR 806982 (SEQ NR 01086). (M) 2 L 7 3 4F A3WE 1996070300346 19960703 00346 NM 1996 7 3 MZZA96050 1 19960520 A 5330 SKIN BOEING 727 727232 1384082 NM BS 950 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15790 20644 DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON C2 CARGO DOOR LOWER CUTOUT SKIN INTER IOR DOUBLER AT BS 950F. THE CORRODED SKIN WAS TREATED AND REPAIRED PER EC/RA NR 5330-02403. REF: HANGAR NON ROUTINE I TEM CARD NR 806983 (SEQ NR 01092) (M) 2 L 7 3 4F A3WE 1996070300347 19960703 00347 NM 1996 7 3 MZZA96052 1 19960517 A 5320 INBOARD WEB BOEING 727 727232 1384082 NM BS 1218 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15790 20644 TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, 1 INCH LONG CRACK WAS FOUND ON RIGHT TORQUE BOX INBOARD WEB L IGHTENING HOLE CUTOUT AT BS 1218. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM 51-40-2. REF: HANGAR NON ROUTIN E REPAIR ITEM CARD NR 806372 (SEQ NR 02068). (M) 2 L 7 3 4F A3WE 1996070300348 19960703 00348 NM 1996 7 3 MZZA96053 1 19960517 A 5320 INBOARD WEB BOEING 727 727232 1384082 NM BS 1213-1223 OIL CANNING A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15790 20644 TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING WAS FOUND ON AFT AIRSTAIR LEFT TORQUE BOX INBOARD WEB AT THE FOLLOWING AREAS; BETWEEN BS 1213 AND 1223, BETWEEN BS 1223 AND 1233. THE DAMAGED WEB WAS INSTALLED REINFORC EMENT STIFFENER ANGLES PER B727 SRM 51-40-2. REF: HANGAR NON ROUTINE REPAIR ITEM CARD NR 806374 AND 806375, (SEQ NR 020 70 AND 02071). (M) 2 L 7 3 4F A3WE 1996070300349 19960703 00349 NM 1996 7 3 MZZA96054 1 19960520 A 5510 BEAM BOEING 727 727232 1384082 NM HORIZ STAB TE CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15790 20644 TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON LEFT HORIZONTAL STABILIZER TE B EAM AT ELEV STATION 17. THE CORRODED TRAILING EDGE BEAM WAS TREATED AND REPAIRED PE B727 SRM 51-10-6 AND 55-10-6. REF: HANGAR NON ROUTINE REPAIR ITEM CARD NR 806962, (SEQ NR 03020). (M) 2 L 7 3 4F A3WE 1996070300350 19960703 00350 NM 1996 7 3 MZZA9651 1 19960520 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 950-1010 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 15790 20644 TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON STRINGER 27R BETWEEN BS 950E AN D 1010. THE CORRODED STRINGER WAS TREATED AND REPAIRED PER EC/RA 5310-03275, A DIP HAS BEEN ISSUED TO REPLACE THE REPAI RED STRINGER S-27R AT NEXT D-CHECK. REF: HANGAR NON ROUTINE REPAIR ITEM CRD NR 806984 (SEQ NR 01093). (M) 2 L 7 3 4F A3WE 1996070300351 19960703 00351 NM 1996 7 3 PCAA9600288 1 19960507 A 3234 5352011 SELECTOR VALVE DHAV DHC8 DHC8102 2809003 NM LANDING GEAR FAILED A PCAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 13 EICHP 258 NOSE GEAR FAILED TO EXTEND WHEN SELECTED DOWN. PERFORMED ALTERNATE EXTENSION, GEAR CAME DOWN AND LOCKED. INDICATION NO RMAL. INSPECTED NOSE GEAR SEQUENCE VALVE RIGGING IAW MM 32-30-31. LUBED PIVOT POINTS. REMOVED AND REPLACED GEAR SELEC T HANDLE, CYCLED GEAR SEVERAL TIMES, CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1996070300352 19960703 00352 NM 1996 7 3 PCAA9600290 1 19960513 A 3234 574205 SELECTOR VALVE DHAV DHC8 DHC8102 2809003 NM LANDING GEAR FAILED A PCAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 13 807EX 292 DURING NORMAL GEAR EXTENSION, LANDING GEAR INOP LIGHT ILLUMINATED. PERFORMED ALTERNATE GEAR EXTENSION, GEAR CAME DOWN N ORMALLY. LANDED WITHOUT INCIDENT. TROUBLESHOT AND FOUND THE LANDING GEAR SELECTOR VALVE TO BE INOPERATIVE IN THE DOWN POSITION. REMOVED AND REPLACED VALVE. SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1996070300353 19960703 00353 NM 1996 7 3 PCAA9600291 1 19960630 A 5320 MS21250H06022 BOLT DHAV DHC8 DHC8102 2809003 NM FUSELAGE CRACKED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 801MX 008 DHC TASK 5310/08F DUE. PERFORMED ULTRASONIC TEST OF RIGHT BOLT, TEST REVEALED 30 PERCENT BACK REFLECTION. REMOVED AND REPLACED BOTH LEFT AND RIGHT FORWARD BOLTS. SUBSEQUENT ULTRASONIC TEST ON BOLT REMOVED FROM LEFT SIDE REVEALED 10 PERCE NT BACK REFLECTION. MAGNETIC PARTICLE INSPECTION REVEALED A CRACK INDICATION MID SHANK. BATHTUB FITTING INSPECTIONS RE VEALED NO DEFECTS. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1996070300354 19960703 00354 CE 1996 7 3 PLGA9606141 1 19960614 A 3260 1003810061 SWITCH BEECH 1900 1900C 1154161 CE NLG MALFUNCTIONED A PLGA O OTHER P NO WARNING INDICATION AP APPROACH 1 NE 05 6929M UB27 MHT - FLT 4537 - ON APPROACH TO MHT, THE NLG DOWN AND LOCKED LIGHT FAILED TO ILLUMINATE AND THE HYDRAULIC POWER PACK SHU T OFF WITHOUT POPPING THE CIRCUIT BREAKER. ALL APPROPRIATE CHECKLIST PROCEDURES FAILED TO OBTAIN A GREEN SAFE INDICATIO N. THE AIRCRAFT LANDED IN MHT WITHOUT INCIDENT (ON TOUCHDOWN THE NLG DOWN AND LOCKED LIGHT ILLUMINATED). THE AIRCRAFT WAS INSPECTED AND FERRIED TO ALB WITH THE GEAR DOWN. MX TROUBLESHOOTING WAS UNABLE TO DUPLICATE THE DISCREPANCY. MX RE MOVED AND REPLACED THE NLG DRAG BRACE SWITCH AS A PRECAUTIONARY MEASURE AND RETURNED THE AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1996070300355 19960703 00355 EU 1996 7 3 PLGA9606153 1 19960615 A 2421 31342001 AC GENERATOR LUCAS 03600912 SAAB SF340 340B 7860101 EU RT ENGINE FAILED A PLGA O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION TX TAXI/GRND HDL 1 NE 05 353BE 1346 1293 340B242 JFK - FLT 4528 - UPON LANDING IN JFK, THE CREW REPORTED THE RIGHT AC GENERATOR AS INOP. MX INSPECTED THE GENERATOR AND FOUND THAT THE DRIVE SHAFT HAD SHEARED. THE SYSTEM WAS MEL'D AND THE AIRCRAFT RETURNED TO SERVICE. UPON ARRIVAL IN BOS , MAINTENANCE REPLACED THE GENERATOR. INSPECTION OF THE GENERATOR FOUND FAILURE OF THE ANTI-DRIVE END BEARING. (M) 2 L 7 2 4T RT A52EU 1996070300356 19960703 00356 EU 1996 7 3 PLGA9606192 1 19960619 A 7110 COWL DOOR SAAB SF340 340B 7860101 EU RT ENG NOT LATCHED A PLGA A UNSCHED LANDING O OTHER CL CLIMB 1 NE 05 358BE 340B279 PIT - FLT 4382 - AFTER TAKEOFF FROM PIT, THE RIGHT ENGINE FWD OUTBOARD COWLING DOOR OPENED. THE AIRCRAFT RETURNED TO PI T, LANDING WITHOUT INCIDENT. THE COWLING WAS TEMPORARILY REPAIRED AND THE AIRCRAFT THEN FERRIED TO PSM FOR PERMANENT RE PAIR. (M) 2 L 7 2 4T RT A52EU 1996070300357 19960703 00357 1996 7 3 S2YA960011 4 19960609 A 2350 1183400921 MIC-SWITCH BEECH 1900 1900D 1154162 CE CONTROL YOKE STUCK A S2YA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 13 891SK UE89 THE CREW OF FLT 1906 MKE-SDF, FOUND THEY HAD A STUCK CAPTAINS MIC-SWITCH IN THE 'ON' POSITION. THEY DECIDED TO TURNBACK TO MKE AND HAVE MX LOOK AT IT. THEY DEFERRED THE SWITCH BY DISABLING IT PER MEL GUIDELINES. THE SWITCH WAS LATER REPL ACED. (M) 2 L 7 2 4T RT A24CE 1996070300358 19960703 00358 EU 1996 7 3 SIMA961652 1 19960613 A 3350 3611210 LIGHT AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 209AT 259 0209 ORD - FLT 4059 - AIRSTAIR EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996070300359 19960703 00359 NE 1996 7 3 SIMA961681 2 19960616 A 7321 350A53000100 MFC AEROSP ATR72 ATR72212 EU PWA PW120 PW124B NE NR 2 ENGINE FAILED A A SIMA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 448AM 486 448 LBB - FLT 3818 - DURING BOARDING, CREW NOTICED AND SMELLED SMOKE IN CABIN, FOLLOWED BY AVIONICS SMOKE WARNING. CREW SHU TDOWN NR 2 ENGINE AND DEPLANED. REMOVED AND REPLACED NR 2 MFC AND OPS CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE . (M) 2 H 7 2 4T 4 T RT A53EU E2ONE 1996070300360 19960703 00360 SO 1996 7 3 SRAA69601 1 19960607 A 5753 34862712AD ATTACH FITT LKHEED 382 382G 526414U SO LT WING CRACKED A A SRAA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 23 905SJ 4472 ON APPROACH TO YIP, FLIGHT 9003 - HAD TO USE FULL RIGHT AILERON TRIM AND 10 DEGREE RIGHT RUDDER TO FLY LEVEL. FOUND LHS FLAP TRACK ATTACH FITTING CRACKED AT FS 241.60, REPLACED FLAP TRACK. SYSTEM OPS CHECKED GOOD PER MM CH 57-10 AND CH 27 . (M) 2 H 7 4 4T A1SO 1996070300361 19960703 00361 SO 1996 7 3 SRAA69602 1 19960608 A 6120 7143253 VALVE HSG LKHEED 382 382G 526414U SO NR 1 PROP BAD BEARING A SRAA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 GL 23 918SJ 4208 ON CLIMB-OUT FROM AVB TO AAB - NR 1 ENGINE RPM FLUCTUATED FROM 105 PERCENT TO 95 PERCENT IN LESS THAN ONE SECOND, NO LOW OIL LIGHT AND MECHANICAL GOVERNING HAD NO EFFECT ON CONDITION, SHUT DOWN NR 1 ENGINE AS PRECAUTIONARY, AIRCRAFT LANDED SAFELY AT AAB. FOUND NR 1 VALVE HOUSING HAD BAD BEARING, REPLACED VALVE HOUSING AND PERFORMED ENGINE RUN, OPS CHECKED G OOD PER J/C 7101, 7101-2, 6101-1, AND 6103. (M) 2 H 7 4 4T A1SO 1996070300362 19960703 00362 SO 1996 7 3 SRAA69603 1 19960607 A 2910 PRESSURIZE SLEEV LKHEED 382 382G 526414U SO BS 245 FAILED A A SRAA D RETURN TO BLOCK J K WARNING INDICATION FLUID LOSS TX TAXI/GRND HDL 1 GL 23 909SJ 4763 DURING TAXIING OUT OF ANC, HYDRAULIC LINE (BETWEEN THE 245 BULKHEAD AND COMBI MODULE) BLEW, CAUSING FUMES AND HYDRAULIC MIST TO ENTER THE CABIN, FOLLOWED BY UTILITY HYD SYSTEM PRESSURE LOSS. SHUT DOWN HYDRAULIC SYSTEM AND DE-PLANED ALL PAS SENGERS. FOUND UTILITY SYSTEM PRESSURE LINE SLEEVE INCORRECTLY TORQUED, REPLACED PRESSURE LINE SLEEVE, SERVICED RESERVO IR AND FLUSHED BELLY OF AIRCRAFT. ALL WORK ACCOMPLISHED PER MM CH 29. (M) 2 H 7 4 4T A1SO 1996070300363 19960703 00363 NM 1996 7 3 TAOA069604 1 19960608 A 3397 WIRE BOEING 727 727254 138408L NM CABIN BROKEN A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 915TS 20252 BOS-LGA - EMERGENCY PATH LIGHTING HAS BROKEN WIRE AT ROW 28D, FOUND ON OVER NIGHT CHECK. REPAIRED BROKEN WIRE. (M) 2 L 7 3 4F A3WE 1996070300364 19960703 00364 NM 1996 7 3 TAOA069605 1 19960607 A 3350 0L3071BPEGPL LAMP BRUCE BOEING 727 727254 138408L NM CABIN MISSING A TAOA K NONE O OTHER IN INSP/MAINT 1 EA 15 915TS 20252 FLT 6181 - BOS/LGA - EMERGENCY PATH LIGHTING COVER AND LAMP MISSING IN AREA OF ROW 14, FOUND ON OVER NIGHT CHECK. REPL ACED LAMP AND INSTALLED NEW LAMP COVER, OPS CHECKS OK. (M) 2 L 7 3 4F A3WE 1996070300365 19960703 00365 NM 1996 7 3 TAOA069606 1 19960607 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 925TS 23240 21244 BOS/LGA - FLT 6091 - FORWARD EMERGENCY LIGHT CEILING AT ROW 3 ABC INOP. REPLACED BATTERY PACK, OPS CHECKED OK. (M) 2 L 7 3 4F A3WE 1996070300366 19960703 00366 NM 1996 7 3 TSAA9653047 1 19960613 A 5320 CLIP BOEING 737 7372S2C 138448G NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 806AL 21927 DURING HEAVY MX VISIT, FOUND CRACKED TIE CLIP AT, BS 747 STRINGER 3L, BS 747 STRINGER 7R, BS 767 STRINGER 4R, BS 787 STR INGER 2L, BS 787 STRINGER 3L, BS 787 STRINGER 5R, BS 807 STRINGER 4R AND BS 727B STRINGER 5R. REPLACED TIE CLIPS PER SR M 51-10-1. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1996070300367 19960703 00367 NM 1996 7 3 TSAA965740 1 19960612 A 5350 FAIRING SEAL BOEING 737 7372T4 1384492 NM RT WING/FUS MISSING A TSAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 13 807AL 23443 FLT 257 - HNL-LIH - RECURRING VIBRATION, LOUD HIGH FREQUENCY VIBRATIONS FROM RIGHT SIDE WING ROOT AREA. STARTED AT 11,0 00 FEET DURING CLIMB AND STOPPED AT 9,000 FEET. DURING DESCENT, VIBRATION FELT IN NR 2 THRUST LEVER AND CABIN FLOOR. V IBRATION NOTICED WITH HIGHER SPEED ONLY, STARTED AT 310 KNOTS AND STOPPED AT 270 KNOTS. FOUND AERODYNAMIC MOISTURE SEAL PORTION MISSING FROM RT FORWARD WING-TO-BODY FAIRING. COVERED AREA WITH SPEED TAPE. (M) 2 L 7 2 4F A16WE 1996070300368 19960703 00368 NM 1996 7 3 TWRA9634 1 19960606 A 2560 65B51382595P BUSTLE SEAL BOEING 747 747212B 1384886 NM L2 DOOR OUT OF ADJUST A TWRA K NONE O OTHER IN INSP/MAINT 1 EA 15 620FF 21162 AT DEPARTURE TIME FLIGHT 24 OUT OF OAK, FLIGHT ATTENDANT HAD DIFFICULTY PUTTING L2 MEL INTO AUTO. REQUIRED THE ASSISTAN CE OF THE FLIGHT ENGINEER. UPON ARRIVAL AT JFK, FOUND LOWER BUSTLE SEAL LOOSE AND INTERFERRING WITH GIRT BAR OPERATION. ADJUSTED SEAL, PERFORMED OPS CHECK OF GIRT BAR OK. (M) 2 L 7 4 4F A20WE 1996070300369 19960703 00369 NM 1996 7 3 TWRA9635 1 19960612 A 2560 GIRT BAR BOEING 747 747212B 1384886 NM LT PAX DOOR DIRTY A TWRA K NONE O OTHER IN INSP/MAINT 1 EA 15 620FF 21162 AT DEPARTURE TIME, FLIGHT ATTENDANT REPORTED L4 MED WAS HARD TO SELECT INTO AUTO. GIRT BAR IS NOT ENGAGING CORRECTLY. L OG ITEM 35056. DURING MAINTENANCE CHECK OF DOOR, FOUND BUSTLE SEAL FOULING GIRT BAR MECHANISM, SECURED SEAL. DOOR AND GIRT BAR OPERATION OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 4 4F A20WE 1996070300370 19960703 00370 EU 1996 7 3 UF6A960404 1 19960415 A 2612 BAEREFJ8539 CONNECTOR BAG ATP ATP EU LT ENG DIRTY A UF6A K NONE N FALSE WARNING TX TAXI/GRND HDL 1 GL 31 851AW 7840 2020 ORD - FLT 5755 - FIRE LOOP CWP ILLUMINATED ON NR 1 SIDE. MAINTENANCE CLEANED CANNON PLUG 'G'. SYSTEM OPS CHECK GOOD. ( M) 2 L 7 2 4T RT A27NM 1996070300371 19960703 00371 EU 1996 7 3 UF6A960406 1 19960421 A 2612 JD007J2281000 FIRE WIRE BAG ATP ATP EU NR 1 ENG FAILED A UF6A O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 GL 31 851AW 10503 2020 ORD - FLT 5701 - NR 1 FIRE LOOP CWP ILLUMINATED ON TAXI. MX REMOVED AND REPLACED LOOP 'B' FIRE DETECTOR. SYSTEM OPS CH ECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1996070300372 19960703 00372 EU 1996 7 3 UF6A960407 1 19960425 A 2612 1WA259 WIRE BAG ATP ATP EU NR 1 ENGINE CHAFED A UF6A O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 GL 31 851AW 10532 2020 ORD - FLT 5710 - FIRE LOOP NR 1 CWP ILLUMINATED WITH FAULT ON FIRE LOOP 'B'. MX FOUND CHAFED SPOT ON WIRE 1WA 259. COV ERED AND PROTECTED CHAF. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1996070300373 19960703 00373 EU 1996 7 3 UF6A960408 1 19960424 A 3251 201075005 CONTROL UNIT BAG ATP ATP EU NLG STEERING FAILED A UF6A C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 31 854AW 3019 2028 CWA - FLT 5714 - SEVERE VIBRATION ON TAKEOFF ROLL. MX REMOVED AND REPLACED STEERING CONTROL MOTOR AND STEERING VALVE. S YSTEM OPS CHECK GOOD. (M) 2 L 7 2 4T RT A27NM 1996070300374 19960703 00374 NE 1996 7 3 UF6A960501 2 19960507 A 7320 3034989 PY LINE BAG ATP ATP EU PWA PW120 PW126A NE NR 2 ENGINE LOOSE A UF6A O OTHER R PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 31 855AW 8298 2029 124242 ORD - FLT 5715 - RIGHT ENGINE ON CLIMB-OUT FELL OFF TO 65 PERCENT AND REMAINED, WOULD NOT INCREASE, POWER LEVER WORKED W ELL BELOW 65 PERCENT. MX FOUND PY LINE LOOSE, TIGHTENED AND SECURED. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T 4 T RT A27NM E2ONE 1996070300375 19960703 00375 EU 1996 7 3 UF6A960502 1 19960510 A 3350 6013211 POWER SUPPLY BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 859AW 3011 22 19415 2036 ORD - ON DAILY INSPECTION OF EMERGENCY LIGHTS, ROWS 6 AND FORWARD WOULD NOT ILLUMINATE. MX REMOVED AND REPLACED FORWARD CEILING BATTERY PACK. (M) 2 L 7 2 4T RT A27NM 1996070300376 19960703 00376 EU 1996 7 3 UF6A960503 1 19960510 A 3350 58674 INVERTER BAG ATP ATP EU NR 1 POSITION FAILED A UF6A K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 856AW 2032 ORD - FLT 5708 - FIRST THREE SECTIONS OF EMERGENCY PATH LIGHTING INOP. MX REMOVED AND REPLACED NR 1 POWER STRIP INVERTE R. (M) 2 L 7 2 4T RT A27NM 1996070300377 19960703 00377 NE 1996 7 3 UF6A960504 2 19960517 A 7200 ENGINE BAG ATP ATP EU PWA PW120 PW126A NE RIGHT MALFUNCTIONED A UF6A C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 31 855AW 2029 124423 ORD - FLT 51-5 - DURING INITIAL POWER UP RIGHT NP DECREASED TO 5 PERCENT, RIGHT GENERATOR CWP CAME ON AND RIGHT TORQUE I NCREASING THEN DECREASING WITH RIGHT POWER LEVER 1 INCH SHEAD OF LEFT. DURING REDUCTION ALL ABNOMALITIES WERE CLEARING. MX PERFORMED GROUND RUN. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4T 4 T RT A27NM E2ONE 1996070300378 19960703 00378 NE 1996 7 3 UF6A960505 2 19960519 A 7532 7857194 HP BLEED VLV BAG ATP ATP EU PWA PW120 PW126A NE NR 2 ENG FAILED A A UF6A A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 GL 31 858AW 683 2035 124451 SBN - FLT 5730 - DURING CLIMB NR 2 ENGINE ITT SURGED TO 860 DEGREES AND TORQUE DROPPED TO 40 PERCENT. MX FOUND NR 2 HP BLEED VALVE WOULD NOT CLOSE AT ELEVATED TORQUE. REMOVED AND REPLACED NR 2 HP BLEED VALVE. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4T 4 T RT A27NM E2ONE 1996070300379 19960703 00379 EU 1996 7 3 UF6A960506 1 19960518 A 3350 363624 LIGHT BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 852AW 10403 2021 CWA - FLT 5718 - FLOOR EMERGENCY LIGHT INOP. MX REMOVED AND REPLACED LIGHT STRIP. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4T RT A27NM 1996070300380 19960703 00380 EU 1996 7 3 UF6A960507 1 19960521 A 3350 363674 LIGHT BAG ATP ATP EU CABIN FAILED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 856AW 9181 2032 SBN - FLT 5757 - EMERGENCY FLOOR EXIT LIGHTING DOES NOT WORK. MX REMOVED AND REPLACED EMERGENCY LIGHTING STRIP. (M) 2 L 7 2 4T RT A27NM 1996070300381 19960703 00381 EU 1996 7 3 UF6A960509 1 19960525 A 3350 363674 LIGHT BAG ATP ATP EU CABIN FAILED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 851AW 2020 SBN - FLT 5751 - EMERGENCY LIGHT NEXT TO LEFT REAR EXIT DOOR INOP. MX REMOVED AND REPLACED LIGHT STRIP. (M) 2 L 7 2 4T RT A27NM 1996070300382 19960703 00382 EU 1996 7 3 UF6A960510 1 19960525 A 3350 6013211 POWER SUPPLY BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 851AW 7788 2020 SBN - EMERGENCY LIGHTS POWER LIGHT SUPPLY INOP. MX REMOVED AND REPLACED POWER SUPPLY. (M) 2 L 7 2 4T RT A27NM 1996070300383 19960703 00383 NM 1996 7 3 USAABB96017 1 19960610 A 5610 WINDSHIELD BOEING 757 757225 1384959 NM RT COCKPIT FAILED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 602AU 35913 22196 DEN - FL 93 - EN ROUTE SAN AT FL 390, R1 WINDSHIELD SHATTERED. FLIGHT DIVERTED TO DEN AND LANDED WITH NO FURTHER INCIDE NT. MX REPLACED THE WINDOW AND HEAT CONTROLLER, (P/N 6240664). (M) 2 L 7 2 4F RT A2NM 1996070300384 19960703 00384 WP 1996 7 3 USAAD96075 1 19960613 A 3350 41B030CF00101 BATTERY PACK DOUG DC9 DC931 3022065 WP LT NACELLE DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 956VJ 47588 LEFT NACELLE EMERGNCY LIGHT INOPERATIVE. REPLACED BATTERY PACK. (M) 2 L 7 2 4F A6WE 1996070300385 19960703 00385 WP 1996 7 3 USAAD96076 1 19960614 A 3350 AD20131A BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 952VJ 47574 FORWARD SECTION OF FLOOR EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK. (M) 2 L 7 2 4F A6WE 1996070300386 19960703 00386 NM 1996 7 3 USAASB96104 1 19960611 A 3260 806002 PROX SWITCH CARD BOEING 737 737301 1384611 NM RT MLG MALFUNCTIONED A USAA O OTHER N FALSE WARNING CL CLIMB 1 EA 19 300AU 23228 PHL - FLT 1868 - ON GEAR RETRACTION, RIGHT MAIN GEAR RED LIGHT STAYED ON WITH HANDLE IN UP POSITION. CREW RECYCLED BREA KERS AND THEN THE GEAR. RED LIGHT WENT OUT APPROXIMATELY TWO MINUTES LATER. FLIGHT LANDED WITH NO FURTHER INCIDENTS. M X REPLACED PROX CARDS M982 AND M986. OPS CHECK PER MX MANUAL GOOD. (M) 2 L 7 2 4F RT A16WE 1996070300387 19960703 00387 NM 1996 7 3 USAASB96105 1 19960612 A 3230 69355005 UPLOCK ACTUATOR BOEING 737 737301 1384611 NM RT MLG MALFUNCTIONED A USAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 19 300AU 23228 PIT - FL 1595 - AFTER TAKEOFF, RIGHT MAIN GEAR SHOWED RED WHEN GEAR WAS RETRACTED WITH HANDLE IN UP POSITION. CREW SELE CTED OFF POSITION AND RIGHT MAIN GEAR CAME DOWN. CREW THEN POSITIONED GEAR HANDLE TO UP POSITION AND GEAR RETRACTED BUT RED GEAR LIGHT REMAINED ILLUMINATED. FLIGHT LANDED WITH NO FURTHER INCIDENT. MX REPLACED THE RIGHT MAIN LANDING GEAR UPLOCK ACTUATOR, UPLOCK ASSEMBLY AND UPLOCK COLLAR. OPERATIONAL CHECK, LEAK CHECK, GEAR SWING AND FREE FALL CHECKED NOR MAL. (M) 2 L 7 2 4F RT A16WE 1996070300388 19960703 00388 NM 1996 7 3 USAASB96110 1 19960615 A 3230 806002 AIR SENSING CARD BOEING 737 7373B7 1384580 NM NLG WW FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 527AU 23862 DCA - FLT 1764 - AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT. THE LANDING GEAR HANDLE WOULD NOT MOVE PAST THE OFF POSITION. FLIGHT RETURNED TO FIELD AT DCA. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE RESET THE LATCH AND CIRCUIT BREAKER AND REPLACED THE AIR SENSING SQUAT SWITCH CARD M991. PERFORMED INTEGRI TY CHECK ON GEAR HANDLE SYSTEM. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996070300389 19960703 00389 NE 1996 7 3 W8PA960027 2 19960620 A 7260 3353107030600U GARLOCK SEAL BOEING 737 7373L9 1384470 NM GE CFM56 CFM563B1 13802 NE RT GEARBOX LEAKING A W8PA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION DE DESCENT 1 NM 03 960WP 23331 720190 FLT CREW NOTICED A STEADY DECREASE IN ENGINE OIL QUANTITY ON THE RIGHT ENGINE FOLLOWED BY FLUCTUATING OIL PRESSURE, THEN A STEADY DROP IN OIL PRESSURE. RIGHT ENGINE WAS SHUTDOWN WHEN PRESSURE WENT BELOW THE RED RADIAL. REPLACED STARTER GA RLOCK SEAL. (M) 2 L 7 2 4F 4 F RT A16WE E2GL 1996070300399 19960703 00399 NE 1996 7 3 96ZZZX3328 2 19960603 A 7314 2PR600CWT PUMP PESCO BEECH 18 G18S 1151010 CE PWA R985 R985AN14B 52008 NE ENGINE FUEL LEAK A A KVJA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 SW 05 9312Y PE80327W BA550 42112135 ENGINE DRIVEN FUEL PUMP DEVELOPED A LEAK FROM A MACHINED ORIFACE AND WAS IGNITED BY EXHAUST FLAME DURING TAXI. SUSPECT INTERNAL FAILURE OF PUMP, NO LOSS OF FUEL PRESSURE NOTED BY CREW. NO DAMAGE TO AIRCRAFT OR OTHER COMPONENTS. 1 L 7 2 3R 3 R A765 5E1 1996070300408 19960703 00408 SO 1996 7 3 96ZZZX3337 1 19960521 A 8010 487769 SOLENOID PIPER PA32 PA32R300 7103213 SO STARTER FAILED A CHRA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 GL 03 4451X 32R7680018 THE PILOT REPORTED ALL ELECTRICAL POWER WAS LOST AFTER THE LANDING GEAR WAS RETRACTED DURING DEPARTURE. AIRCRAFT SUSTAI NED MINOR DAMAGE WHEN THE NOSE GEAR FOLDED. AN INSPECTION REVEALED THE STARTER SOLENOID FAILED. FAILURE CAUSED A SHORT TO GROUND ON THE BATTERY SIDE (PN 487769). SUBMITTER RECOMMENDS A CURRENT LIMITER BE INSTALLED ON BATTERY FEED TO SOLE NOID. 1 L 7 1 3O A3SO 1996070300430 19960703 00430 SW 1996 7 3 HEEA967320 1 19960604 A 5230 206513211 ACTUATOR BELL 407 407 SW BAG DOOR DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407PH 53003 UPON INSTALLATION, FOUND THAT THE BAGGAGE DOOR WOULD NOT CLOSE COMPLETELY. INSPECTED AND FOUND THAT GAS STRUT WOULD NOT COMPRESS COMPLETELY. 1 G 7 1 3U O H2SW 1996070300431 19960703 00431 1996 7 3 HEEA967348 4 19960605 A 3444 7001840903 TRANSCEIVER BELL 212 212 1181420 SW COCKPIT DEFECTIVE E HEEA K NONE J WARNING INDICATION NR NOT REPORTED 1 SW 03 3131S 30953 VALID LIGHT FLASHES OFF AND ON. 1 G 7 1 4U H4SW 1996070300432 19960703 00432 EU 1996 7 3 HEEA967349 1 19960605 A 7160 350A54108004 DUCT SNIAS 350 AS350B2 8680813 EU INTAKE AIR CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6097Z 1673 2820 INTAKE AIR DUCT IS CRACKED. (CRACK IS NEAR MOUNT FLANGE) 1 G 7 1 3U H9EU 1996070300433 19960703 00433 1996 7 3 HEEA967350 4 19960605 A 3444 071111401 ANTENNA BOLKMS 105 BO105S 5626006 EU RADAR ALT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 131AE 10 S787 TROUBLESHOOTING ;ANTENNA INTERMITTENTLY INOPERATIVE. 1 G 7 2 3U H3EU 1996070300434 19960703 00434 NE 1996 7 3 HEEA967351 1 19960605 A 6730 7630103902102 ACTUATOR SKRSKY S76 S76A 8143006 NE SERVO SYS TRIPS BREAKER E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1546K 760082 MOTOR POPS CIRCUIT BREAKER. 1 G 7 2 3U H1NE 1996070300435 19960703 00435 EU 1996 7 3 HEEA967352 2 19960605 A 7510 1092T1002W SERVOMOTOR BOLKMS 105 BO105S 5626006 EU SERVO SYS INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB S737 WHEN ACTUATOR WAS HEATED UP IT BECAME INOPERATIVE. 1 G 7 2 3U H3EU 1996070300436 19960703 00436 SW 1996 7 3 HEEA967353 1 19960605 A 2435 230321827 FIELD ASSY BELL 206 206L 1181522 SW START/GEN SHORTED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5005B 45175 START/GEN SHORTED OUT. 1 G 7 1 3U H2SW 1996070300437 19960703 00437 1996 7 3 HEEA967354 4 19960605 A 3120 B1894522282A CLOCK SNIAS 350 AS350B2 8680813 EU COCKPIT INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 60951 2771 CLOCK INOPERATIVE. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H9EU 1996070300438 19960703 00438 1996 7 3 HEEA967355 4 19960605 A 3421 7926694001 GYRO BEECH 200 200CBEECH 1152926 CE COCKPIT VG DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 39PH BL3 WAIT AND ANT LIGHT COMES ON WHEN STABILIZATION MODE IS SELECTED. 1 L 7 2 4T A24CE 1996070300440 19960703 00440 1996 7 3 HEEA967357 4 19960605 A 3421 222375033103 INDICATOR BELL 412 412 1182202 SW COCKPIT ATTITUDE PRECESSES E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 107X 33113 PRECESSES IN PITCH AND ROLL. 1 G 7 2 4U H4SW 1996070300441 19960703 00441 1996 7 3 HEEA967358 4 19960605 A 3421 222375033103 INDICATOR BELL 412 412 1182202 SW COCKPIT ATTITUDE FAULTY E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 107X 33113 ATTITUDE INDICATOR WILLNOT REMAIN ERECT. 1 G 7 2 4U H4SW 1996070300442 19960703 00442 CE 1996 7 3 HEEA967359 1 19960605 A 2422 PC17 INVERTER BEECH 200 200BEECH 1152920 CE AC SYS MALFUNCTION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 30PH BB635 INVERTER CYCLES FLUCTUATING IN FLIGHT. 1 L 7 2 4T A24CE 1996070300443 19960703 00443 SW 1996 7 3 HEEA967360 1 19960605 A 3212 214073929107 VALVE BELL 214 214ST 1182106 SW FLOAT LEAKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 FLOAT VALVE LEAKS. TIME SINCE REPAIR 20:25. 2 G 7 2 4U H10SW 1996070300445 19960703 00445 1996 7 3 HEEA967362 4 19960605 A 3453 453105004 LORAN R501 SKRSKY S76 S76A 8143006 NE COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5435V 760158 ENTER BUTTON DOES NOT WORK. 1 G 7 2 3U H1NE 1996070300446 19960703 00446 SW 1996 7 3 HEEA967363 1 19960605 A 7931 209070262009 INDICATOR BELL 412 412 1182202 SW ENG OIL STICKS E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 21498 36003 INDICATOR STICKS ON PRESSURE AT 45 PSI. 1 G 7 2 4U H4SW 1996070300447 19960703 00447 SW 1996 7 3 HEEA967364 1 19960605 A 7714 206075682107 INDICATOR BELL 206 206L3 1182108 SW GAS PROD STICKS E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 363BH 51345 N1 NEEDLE STICKS BELOW 10% NORTH. 1 G 7 1 3U H2SW 1996070300448 19960703 00448 1996 7 3 HEEA967365 4 19960605 A 3452 066106200 TRANSCEIVER KT76 BELL 206 206B 1181511 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 22743 3624 NO IDENT LIGHT AND NO LIGHT ON TEST. REPLACED PHOTOCELL V201. REPAIRED. REPLACED DETERIORATED RESISTOR R477. ADJUSTED POWER OUT AND FREQUENCY TO SPECS. BENCH CHECK GOOD. 1 G 7 1 3U H2SW 1996070300449 19960703 00449 SW 1996 7 3 HEEA967366 1 19960605 A 5512 206023119159 SKIN BELL 206 206L3 1182108 SW RT STAB CHAFED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8589X 51487 HOLES IN SKIN; SKIN CHAFED. CORRODED AND HAS DEFECTIVE RIVETS. 1 G 7 1 3U H2SW 1996070300450 19960703 00450 SW 1996 7 3 HEEA967367 1 19960605 A 5512 206023119157 SKIN BELL 206 206L3 1182108 SW LT STAB CHAFED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8589X 51487 HOLES IN SKIN; SKIN CHAFED. CORRODED AND HAS DEFECTIVE RIVETS. 1 G 7 1 3U H2SW 1996070300451 19960703 00451 SW 1996 7 3 HEEA967368 1 19960605 A 2622 P1251211A EXTINGUISHER BELL 206 206L1 1182107 SW LABEL DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 83MT 45492 EXTINGUISHER LABEL NOT LEGIBLE. 1 G 7 1 3U H2SW 1996070300452 19960703 00452 SW 1996 7 3 HEEA967369 1 19960605 A 2844 APTE139KBS100015 TRANSMITTER BELL 412 412 1182202 SW FUEL SYS FLUCTUATES E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2298Z 33077 TRANSMITTER FLUCTUATES. 1 G 7 2 4U H4SW 1996070300454 19960703 00454 SW 1996 7 3 HEEA967372 1 19960605 A 6310 406040548101 CONE SET 406040500113 BELL 206 206L 1181522 SW FREEWHEEL DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 62127 A1552 52023 MECHANICAL DAMAGE. REPLACED WITH SERVICEABLE CONE SET. 1 G 7 1 3U H2SW 1996070300455 19960703 00455 SW 1996 7 3 HEEA967373 1 19960605 A 2820 205060612003 VALVE ASSEMBLY BELL 212 212 1181420 SW FUEL SYS DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5736J 31140 LEAKING INTERNALLY WHEN CLOSED. 1 G 7 1 4U H4SW 1996070300456 19960703 00456 SW 1996 7 3 HEEA967374 1 19960605 A 5530 206023126101 FIN ASSY BELL 206 206L1 1182107 SW VERT STAB CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2125M 45649 FIN ASSY IS CORRODED. (RIV-NUT IMPROPERLY INSTALLED AND CORRODED) SEPARATED AT AFT LOWER EDGE. 1 G 7 1 3U H2SW 1996070300457 19960703 00457 EU 1996 7 3 HEEA967375 1 19960605 A 5210 350A25109324 STRIKER SNIAS 350 AS350B2 8680813 EU COPILOT DOOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 2771 CO-PILOT'S DOOR UPPER LATCH PIN STRIKER WORN. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H9EU 1996070300458 19960703 00458 EU 1996 7 3 HEEA967376 1 19960605 A 2930 806966 ELEMENT SNIAS 350 AS350B2 8680813 EU OIL SYS DEFECTIVE E HEEA K NONE J WARNING INDICATION NR NOT REPORTED 1 SW 03 60951 2771 FILTER BYPASS POPPED. REPLACED WITH SERVICEABLE FILTER. 1 G 7 1 3U H9EU 1996070300459 19960703 00459 EU 1996 7 3 HEEA967377 1 19960605 A 6520 350A27191004 ROD SNIAS 350 AS350B2 8680813 EU T/R GR BOX BEARING WORN E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 60951 2771 BEARING WORN. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H9EU 1996070300460 19960703 00460 1996 7 3 HEEA967378 4 19960605 A 2312 TFM1388 RADIO BELL 206 206L3 1182108 SW COCKPIT SMOKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 141BH 51303 RADIO STARTED TO SMOKE AFTER INITIAL CHECK. 1 G 7 1 3U H2SW 1996070300461 19960703 00461 GL 1996 7 3 HEEA967380 2 19960605 A 7250 6886407 WHEEL 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL 1ST STAGE BLADE ERODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7136H 1199 CAT32012F S833 CAE836387 ENGINE REMOVED DUE TO HIGH CYCLED 1ST,2ND AND 3RD STAGE WHEEL. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: M INOR SULFIDATION ON 7 EACH 1ST STAGE WHEEL BLADES AND ERODED LEADING EDGES. SCRAPPED 1ST STAGE WHEEL. 1 G 7 2 3U 3 U H3EU E4CE 1996070300462 19960703 00462 GL 1996 7 3 HEEA967382 2 19960605 A 7250 23001977 WHEEL 23033185 BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL 3RD STAGE DAMAGED E HEEA K NONE O OTHER LD LANDING 1 SW 03 123 CAT70674 CAE860408 ENGINE REMOVED DUE TO HARD LANDING AND SUDDEN STOPPAGE. REMOVED 3RD STAGE WHEEL PER LETTER C1281F-RMG-1295/CEB A 72-217 6. REPLACED DISCREPANT PART. 1 G 7 1 3U 3 U H2SW E1GL 1996070300463 19960703 00463 GL 1996 7 3 HEEA967383 2 19960605 A 7261 6871311 TUBE ASSY 23033185 BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL OIL PRESS BENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 CAT70287 UPON INSPECTION OF PART NOTED THE FOLLOWING: BENT BEYOND SERVICEABLE LIMITS ON TUBE OIL PRESSURE NOZZLE. REPLACED DISCR EPANT PART. 1 G 7 1 3U 3 U H2SW E1GL 1996070300464 19960703 00464 EU 1996 7 3 HEEA967384 1 19960605 A 2435 23032048 STARTER BOLKMS 105 BO105S 5626006 EU START/GEN FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7062X S793 WOULD NOT START AIRCRAFT. BRUSHES ARE WORN. RECEIVED INSTALLED ON N7062X ON 7-12-95. 1 G 7 2 3U H3EU 1996070300465 19960703 00465 EU 1996 7 3 HEEA967385 1 19960605 A 6520 350A33215300 BEARING SNIAS 350 AS350B2 8680813 EU T/R FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100U 2863 BEARING SEPARATED. ORIGINAL EQUIPMENT RECEIVED INSTALLED ON N6100U ON 8-17-95. 1 G 7 1 3U H9EU 1996070300467 19960703 00467 GL 1996 7 3 HEEA967387 2 19960606 A 7250 23031426 NOZZLE 23035128 BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL NR 4 DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 CAT90623 UPON INSPECTION OF PART NOTED THE FOLLOWING: 2-4 SEAL RUN OUT .011 WITH GOOD RUNOUT IN THE TIP PATH. TIP PATH RUNOUT . 010 WITH A GOOD 2-4 SEAL RUNOUT. REPLACED DISCREPANT PART. 1 G 7 1 3U 3 U H2SW E1GL 1996070300468 19960703 00468 EU 1996 7 3 HEEA967388 1 19960606 A 7930 642790041 TRANSMITTER SNIAS 350 AS350B2 8680813 EU OIL PRESS DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 350BZ 1686 2653 PRESSURE SLOWLY DROPS TO ZERO. 1 G 7 1 3U H9EU 1996070300469 19960703 00469 EU 1996 7 3 HEEA967389 1 19960606 A 2930 806966 ELEMENT SNIAS 350 AS350B2 8680813 EU HYD SYS DEFECTIVE E HEEA K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 03 60951 2771 ON DAILY INSPECTION FOUND BY-PASS BUTTON POPPED ON HYDRAULIC FILTER. 1 G 7 1 3U H9EU 1996070300470 19960703 00470 EU 1996 7 3 HEEA967390 1 19960606 A 6240 430106202 SPEED PICK UP BOLKMS 117 BK117B1 5626012 EU NR TACH DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 117BK 7229 NR TACH FLUCTUATING IN FLIGHT. 1 G 7 2 3U H13EU 1996070300471 19960703 00471 EU 1996 7 3 HEEA967391 1 19960606 A 2823 857A1641 VALVE SNIAS 350 AS350B2 8680813 EU FUEL SYS DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100U 915 2863 VALVE HARD TO TURN AND RATCHETY WHEN IT DOES TURN. 1 G 7 1 3U H9EU 1996070300472 19960703 00472 EU 1996 7 3 HEEA967392 1 19960606 A 5610 04011341990 WINDOW SNIAS 350 AS350B2 8680813 EU CP DOOR CRACKED TRIM E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6097Z 39 2820 REPLACED C.P. DOOR WINDOW FOR CRACKED TRIM. 1 G 7 1 3U H9EU 1996070300473 19960703 00473 EU 1996 7 3 HEEA967394 1 19960607 A 6220 350A31190700 STARFLEX SNIAS 350 AS350B2 8680813 EU M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 2045 2771 STARFLEX HAS CRACK IN ONE ARM. 1 G 7 1 3U H9EU 1996070300474 19960703 00474 SW 1996 7 3 HEEA967395 1 19960610 A 6310 406040548101 CONE SET 406040500113 BELL 206 206L 1181522 SW FREEWHEEL DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 62127 A1552 52023 MECHANICAL DAMAGE. PART SCRAPPED LOCALLY. 1 G 7 1 3U H2SW 1996070300475 19960703 00475 EU 1996 7 3 HEEA967396 1 19960610 A 6210 10515141 BLADE BOLKMS 105 BO105S 5626006 EU M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81992 2336 S827 CRACKS IN THE NOSE AND NECK SHELL AT THE ROOT END. 1 G 7 2 3U H3EU 1996070300476 19960703 00476 EU 1996 7 3 HEEA967397 1 19960610 A 6210 10515141 BLADE BOLKMS 105 BO105S 5626006 EU M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81992 2336 S827 CRACKS IN THE NOSE AND NECK SHELL AT THE ROOT END. 1 G 7 2 3U H3EU 1996070300477 19960703 00477 EU 1996 7 3 HEEA967398 1 19960610 A 6210 10515141 BLADE BOLKMS 105 BO105S 5626006 EU M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8197X 3307 S808 BLADE HAS A HOLE IN THE OUTBOARD LEADING EDGE STRIP. 1 G 7 2 3U H3EU 1996070300478 19960703 00478 NE 1996 7 3 HEEA967399 1 19960610 A 6210 7615009100041 BLADE SKRSKY S76 S76A 8143006 NE M/R WATER CONTAM E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 117WB 3708 760092 BLADE IS SUSPECTED TO HAVE WATER INGRESSION. (BLADE IS CUSTOMER PROPERTY) 1 G 7 2 3U H1NE 1996070300479 19960703 00479 WP 1996 7 3 9613939965 1 19960523 A 5730 SKIN DOUG DC9 DC931 3022065 WP WS 59 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 911RW 47149 DURING M-CHECK, FOUND CORROSION ON THE RIGHT WING UPPER FORWARD SKIN AT XCW 58.5. REPAIRED SKIN (P/N 5910464-4) PER EA 99-110504. 2 L 7 2 4F A6WE 1996070300480 19960703 00480 WP 1996 7 3 9613949965 1 19960523 A 5312 BULKHEAD TEE DOUG DC9 DC931 3022065 WP FS 756 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 911RW 47149 DURING M-CHECK, FOUND CORROSION ON THE FS 756 BULKHEAD UPPER T-CHORD LBL 7 TO RBL 7. REPAIRED T-CHORD PER EA DC9-53-001 . 2 L 7 2 4F A6WE 1996070300481 19960703 00481 WP 1996 7 3 9613959940 1 19960527 A 5320 SILL DOUG DC9 DC932 3022066 WP FS 389-408 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3322L 47031 DURING M-CHECK, FOUND CORROSION ON THE LEFT HAND WINDOW FRAME SILL, UPPER SIDE, BETWEEN FS 389 TO 408. REPAIRED SILL PE R EA 99-108554. 2 L 7 2 4F A6WE 1996070300482 19960703 00482 WP 1996 7 3 9613969940 1 19960527 A 5311 FRAME DOUG DC9 DC932 3022066 WP FS 756 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3322L 47031 DURING M-CHECK, FOUND THREE CRACKS ON THE FS 756 FRAME INBOARD FLANGE OF THE LOWER PRODUCTION SPLICE POCKET. REPAIRED F RAME (P/N 9919620-501) PER EA 99-108562. 2 L 7 2 4F A6WE 1996070300483 19960703 00483 WP 1996 7 3 9613971144 1 19960604 A 5311 FRAME DOUG DC10 DC1040 3023508 WP FS 895 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 144JC 46753 DURING T-CHECK, FOUND CORROSION ON THE FORWARD CARGO DOOR JAMB FRAME AT THE LOWER FORWARD CORNER FS 895, LONGERON 41R. R EPAIRED FRAME (P/N ADA 0233) PER EA 11-105379. 2 L 7 3 4F A22WE 1996070300484 19960703 00484 NM 1996 7 3 9613985507 1 19960606 A 5315 FLOOR BEAM BOEING 757 757251 1384970 NM FS 1661 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 507US 23196 DURING P-CHECK, FOUND CORROSION ON THE BS 1661 FLOOR BEAM ON THE UPPER CHORD LBL 58 TO RBL 59. REPAIRED CHORD (P/N 146N 5090) PER EA 55-106081. 2 L 7 2 4F RT A2NM 1996070300485 19960703 00485 WP 1996 7 3 9613999907 1 19960606 A 5312 BULKHEAD DOUG DC9 DC931 3022065 WP FS 996 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 957N 47253 DURING M-CHECK, FOUND CORROSION ON THE FS 996 AFT PRESSURE BULKHEAD T-ANGLE AT LONGERON 18R. REPAIRED AFT PRESSURE BULK HEAD PER EA DC9-53-009. 2 L 7 2 4F A6WE 1996070300486 19960703 00486 WP 1996 7 3 9614009905 1 19960607 A 5711 SPAR DOUG DC9 DC931 3022065 WP RT WING CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 955N 47160 DURING H-CHECK, FOUND A .75 INCH CRACK IN THE RIGHT WING REAR SPAR AT THE NR 2 FLAP HINGE LOWER INBOARD FASTENER HOLE. R EPAIRED SPAR PER EA 99-110507. 2 L 7 2 4F A6WE 1996070300487 19960703 00487 NM 1996 7 3 9614015507 1 19960611 A 5315 FLOOR BEAM BOEING 757 757251 1384970 NM FS 377 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 507US 23196 DURING P-CHECK, FOUND CORROSION IN THE BS 377 FLOOR BEAM UPPER CHORD LBL 63 TO BL 0. REPAIRED CHORD (P/N 141N5113) PER EA 55-106085. 2 L 7 2 4F RT A2NM 1996070300488 19960703 00488 WP 1996 7 3 9614029975 1 19960613 A 5330 SKIN DOUG DC9 DC931 3022065 WP PAX DOOR CUTOUT CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9339 47382 DURING M-CHECK, FOUND CRACKS IN THE MAIN CABIN DOOR CUTOUT SKIN AT THE NR 3 AND NR 6 STOPS. REPAIRED SKIN (P/N 5911406- 7) PER EA 99-108568, -108569. 2 L 7 2 4F A6WE 1996070300489 19960703 00489 WP 1996 7 3 9614039907 1 19960616 A 5311 FRAME DOUG DC9 DC931 3022065 WP FS 965 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 957N 47253 DURING M-CHECK, FOUND CORROSION ON THE FS 965 FRAME FROM LONGERON 29L TO 29R. REPAIRED FRAME (P/N 9912243-105) PER EA 9 9-110803. 2 L 7 2 4F A6WE 1996070300490 19960703 00490 WP 1996 7 3 9614049907 1 19960618 A 5411 RIB DOUG DC9 DC931 3022065 WP LT PYLON CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 957N 47253 DURING M-CHECK, FOUND A CRACK IN THE LEFT PYLON CLOSING RIB LOWER CAP. REPAIRED CAP (P/N 9958159-57) PER EA 99-109067. 2 L 7 2 4F A6WE 1996070300491 19960703 00491 WP 1996 7 3 9614059918 1 19960621 A 5744 FITTING DOUG DC9 DC932 3022066 WP NR 2 TE FLAP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 940N 47572 DURING H-CHECK, FOUND CORROSION IN THE LEFT WING NR 2 FLAP FORWARD HINGE FITTING FASTENER HOLES. REPLACED HINGE (P/N 59 19218-505) PER CITEXT 09-5740-1-9800. 2 L 7 2 4F A6WE 1996070300492 19960703 00492 WP 1996 7 3 9614069305 1 19960622 A 5320 FITTING DOUG DC9 DC982 3022082 WP FS 1212 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 307RC 48086 DURING H-CHECK, FOUND CORROSION ON THE AFT CARGO DOOR JAMB FITTING AFT LOWER CORNER FS 1212. REPLACED FITTING PER SRM 5 3-10, FIG 1. 2 L 7 2 4F A6WE 1996070300493 19960703 00493 NE 1996 7 3 9614289858 2 19960623 A 7321 FUEL CONTROL DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE NR 1 ENGINE MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 767MC 47724 696737 NR 1 ENGINE EPR, N1 AND FUEL FLOW INDICATORS WERE UNSTABLE DURING CLIMB. THE FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FUEL CONTROL UNIT WITH A SERVICEABLE UNIT. 2 L 7 2 4F 4 F A6WE E2EA 1996070300494 19960703 00494 1996 7 3 9614293220 4 19960629 A 3160 ECAM AIRBUS 320 A320211 3930320 EU COCKPIT MALFUNCTION A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 320US 213 DURING CLIMBOUT, RECEIVED NUMEROUS SPURIOUS ECAM MESSAGES. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. 2 L 7 2 4F RT A28NM 1996070300495 19960703 00495 EU 1996 7 3 9614303231 1 19960701 A 3830 DRAIN AIRBUS 320 A320211 3930320 EU AFT GALLEY PLUGGED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 331NW 318 DURING CLIMBOUT, FLIGHT ATTENDANT HEARD A LOUD NOISE IN THE AFT GALLEY AREA. NOISE STOPPED WHEN THE AFT GALLEY DRAIN WA S USED. AIRCRAFT RETURND TO LAX AND LANDED WITHOUT INCIDENT. THE AFT GALLEY DRAIN WAS BLOCKED OFF AND DEFERRED. 2 L 7 2 4F RT A28NM 1996070300496 19960703 00496 NM 1996 7 3 9614312293 1 19960701 A 3350 POWER SUPPLY BOEING 727 727251 138408H NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 293US 21504 DURING PREFLIGHT, FOUND AFT OVERSTAIR EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY PACK, CHECKED OK. 2 L 7 3 4F A3WE 1996070300497 19960703 00497 NM 1996 7 3 9614326627 1 19960701 A 3350 POWER SUPPLY BOEING 747 747251B 1384892 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 627US 21709 DURING LINE CHECK, FOUND C-ZONE EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY PACK, OPERA TIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996070300498 19960703 00498 WP 1996 7 3 9614331148 1 19960630 A 3260 JV304 SWITCH DOUG DC10 DC1040 3023508 WP COCKPIT BROKEN A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 148US 46757 DURING CLIMB, PLACED THE GEAR HANDLE IN THE UP POSITION. THE 4 UNSAFE LIGHTS REMAINED ILLUMINATED. FOLLOWED COM 2.32.1 6 AND VERIFIED GEAR UP. MAINTENANCE REPLACED THE S1-342 SWITCH. 2 L 7 3 4F A22WE 1996070300499 19960703 00499 NE 1996 7 3 9614349903 2 19960627 A 7230 COMPRESSOR DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7B 52053 NE NR 2 ENGINE STALLED A NWAA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 01 953N 47083 653954 DURING TAKEOFF, THE NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL ACCOMPANIED BY HIGH EGT AND A DECREASE IN EPR OF 0.1. EN GINE RECOVERED AND THE AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT INCIDENT. ENGINE WAS TESTED PER PWA MANUAL, ENGINE P ERFORMANCE WAS WITHIN PRESCRIBED LIMITS. 2 L 7 2 4F 4 F A6WE E2EA 1996070300500 19960703 00500 WP 1996 7 3 9614359304 1 19960629 A 2520 CEILING PANEL DOUG DC9 DC982 3022082 WP TAILCONE AREA OUT OF POSITION A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 931MC 48057 DURING A-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO DEPLOY THE TAILCONE USING THE AFT ENTRY DOOR. ALSO, FOUND TH AT THE CEILING PANEL INTERFERED WITH THE DOOR ARM PIN MOVEMENT. TRIMMED LOWER EDGE OF PANEL AND RETESTED SYSTEM WITHOUT FURTHER CORRECTIVE ACTION. PULL FORCE WITHIN LIMITS. 2 L 7 2 4F A6WE 1996070300501 19960703 00501 NM 1996 7 3 96FDEA00323 1 19960222 A 5330 6554578 SKIN BOEING 727 72722 1384002 NM BS 945 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 GOUGE IN EXTERIOR SKIN BS 945 STR 9R. REMOVED DAMAGED SKIN, BS 945, STR 9 RT FABRICATED AND INSTALLED REPAIR DOUBLER IA W FEDEX SRM 53-30-3. 2 L 7 3 4F A3WE 1996070300502 19960703 00502 NM 1996 7 3 96FDEA00379 1 19960228 A 5320 6516343 INTERCOSTAL BOEING 727 72722 1384002 NM BS 1055 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 DENTED INTERCOSTAL BS 1055 BETWEEN STR 23 TO 25L LBL 36 TO 48 WL 156. *S/D* REMOVED AND REPLACED OUT OF LIMITS INTERCO STEL PER FEDEX SRM 53-10-1. 2 L 7 3 4F A3WE 1996070300503 19960703 00503 NM 1996 7 3 96FDEA00383 1 19960301 A 5320 6573100 DOUBLER BOEING 727 72722 1384002 NM BS 178 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 194FE 19143 WHILE WORKING CARD NR 71C102-01, FOUND RADOME TO BE MISALIGNED AT BS 178, ALLOWING RADOME TO CATCH DOUBLER WHICH CRACKED DOUBLER AND CHIPPED RADOME WL 235 LBL 4. *S/D* REPLACED RADOME WL 235, LBL 4 PER FEDEX SRM 53-50-4 AND REPAIRED SKIN DOUBLER BS 178, WL 235, LBL 4 PER FEDEX EA 7-5310-27737. 2 L 7 3 4F A3WE 1996070300504 19960703 00504 NM 1996 7 3 96FDEA00845 1 19960425 A 5311 6515932 FRAME BOEING 727 72725 1384006 NM BS 580 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 NR0396 AND 005, CRACKED FRAME AT BS 580 WL 154 RBL 18 UNDER FLOOR SUPPORT. *S/D* REMOVED DAMAGED AT BS 580, WL 154, RB L 18, FABRICATED REPAIR DOUBLER AND INSTALLED IAW FEDEX SRM 51-40-3 UNDER FLOOR SUPPORT. 2 L 7 3 4F A3WE 1996070300505 19960703 00505 NM 1996 7 3 96FDEA01187 1 19960701 A 5320 69782441 FITTING BOEING 727 727173C 1384059 NM BS 740 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 199FE 19509 NR0019 AND 013, FOUND CRACKS IN STA 740 FORGING RT BETWEEN STR 18 TO 20 RT, FWD BAY. *S/D* REPAIRED CRACKS IN STA 740 FORGING RT BETWEEN STR 18 TO 20 RT IAW FEDEX EA 7-5310-29123. 2 L 7 3 4F A3WE 1996070300506 19960703 00506 WP 1996 7 3 ABXA9600520 1 19960701 A 3350 0145971010995 BATTERIES DOUG DC9 DC933F 302207A WP COCKPIT DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 931AX 47384 COCKPIT EMERGENCY LIGHTS ARE DIM. REPLACED COCKPIT EMERGENCY LIGHT BATTERIES. 2 L 7 2 4F A6WE 1996070300507 19960703 00507 WP 1996 7 3 CALA9600939 1 19960701 A 2421 976J2526 GENERATOR DOUG DC9 DC982 3022082 WP APU INOPERATIVE A CALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 SW 09 57837 49582 THE APU GENERATOR FAILED, WHILE OPERATING THE APU WITH THE NR 1 GENERATOR PLACARDED INOPERATIVE, EN ROUTE. THE FAILURE WAS ACCOMPANIED BY ILLUMINATION OF THE FEEDER FAULT AND AC CROSSTIE LOCKOUT LIGHTS. THE AIRCRAFT WAS DIVERTED TO EWR WH ERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE APU GENERATOR AT FAULT. THE GENERATOR WAS REMOVED AND REPLACED I AW MM 24-20-02. THE APU WAS RUN WITH FULL ELECTRICAL LOAD AND OPERATION CHECKED GOOD. 2 L 7 2 4F A6WE 1996070300508 19960703 00508 NM 1996 7 3 CALA9600940 1 19960701 A 2910 HYD LINE BOEING 737 737217 1384464 NM NLG ACTUATOR LEAKING A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 09 13234 19888 THE NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM RDU. ALL GEAR WERE LOWERED AND VERIFIED DOWN. THE AIRCRAFT WAS RETURNED TO RDU WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR LOCK ACTUATOR HYDRAULIC FLEX LINE LEAKING. THE LINE WAS REPLACED USING AN INTERIM FLEX LINE. A DIP WAS ISSUED TO REPLACE THE FLEX LINE WITHIN 500 FLIGH TS OR 1200 FLIGHT HOURS. 2 L 7 2 4F A16WE 1996070300509 19960703 00509 WP 1996 7 3 CALA9600941 1 19960606 A 5320 DOUBLER DOUG DC10 DC1010 3022110 WP BS 1801 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68043 46902 INSPECTION FOUND AFT CARGO FINGER DOUBLER CORRODED THROUGH AT STA 1801, STRINGER 47L. THE AREA WAS REPAIRED IAW SRM 53- 20-00, FIGURE 6. 2 L 7 3 4F A22WE 1996070300510 19960703 00510 WP 1996 7 3 CALA9600942 1 19960602 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 1701 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68043 46902 INSPECTION FOUND LONGERON 48L CORRODED AT STA 1701 TO 1721. A REPAIR WAS PERFORMED IAW ECRA 5310-03291. 2 L 7 3 4F A22WE 1996070300511 19960703 00511 WP 1996 7 3 CALA9600943 1 19960602 A 5320 DOUBLER DOUG DC10 DC1010 3022110 WP BS 1761-1781 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68043 46902 INSPECTION FOUND FINGER DOUBLER CORRODED AT STA 1761 TO 1781, LONGERON 46L TO 48L. THE AREA WAS REPAIRED IAW SRM 53-20- 00, FIGURE 6. 2 L 7 3 4F A22WE 1996070300512 19960703 00512 WP 1996 7 3 CALA9600944 1 19960531 A 5330 DOUBLER DOUG DC10 DC1010 3022110 WP STA 1997-2007 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68043 46902 INSPECTION FOUND DOUBLER AND TRANSVERSE SPLICE CORRODED AT STA 1997 TO 2007, LONGERON 38L TO 43L. A REPAIR WAS PERFORME D IAW ECRA 5330-02411. 2 L 7 3 4F A22WE 1996070300513 19960703 00513 WP 1996 7 3 CALA9600945 1 19960602 A 5320 WEB DOUG DC10 DC1010 3022110 WP BS 1258 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68043 46902 INSPECTION FOUND A 3 INCH CRACK IN WEB AT STA 1258, LONGERON 15R. THE AREA WAS REPAIRED IAW SRM 53-00-01, FIGURE 4. 2 L 7 3 4F A22WE 1996070300514 19960703 00514 WP 1996 7 3 CALA9600946 1 19960602 A 5320 WEB DOUG DC10 DC1010 3022110 WP BS 1258 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68043 46902 INSPECTION FOUND A 3 INCH CRACK IN WEB AT STA 1258, LONGERON 15L. THE AREA WAS REPAIRED IAW SRM 53-00-01, FIGURE 4. 2 L 7 3 4F A22WE 1996070300515 19960703 00515 WP 1996 7 3 CALA9600947 1 19960530 A 5320 CHANNEL DOUG DC10 DC1010 3022110 WP CARGO COMPT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68043 46902 INSPECTION FOUND SECOND LEFT FROM CENTERLINE CENTER CARGO CHANNEL CORRODED. A NEW CHANNEL WAS FABRICATED AND INSTALLED IAW SRM 53-70-00, FIGURE 7. 2 L 7 3 4F A22WE 1996070300516 19960703 00516 WP 1996 7 3 CALA9600948 1 19960531 A 5720 DOUBLER DOUG DC10 DC1010 3022110 WP RT WING CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68043 46902 INSPECTION FOUND CORROSION ON RT WING LOWER MAIN LANDING GEAR SUPPORT DOUBLER. THE AREA WAS REPAIRED IAW ECRA 5730-0144 8. 2 L 7 3 4F A22WE 1996070300517 19960703 00517 SO 1996 7 3 COMA9610201 1 19960623 A 2910 62000001 CHECK VALVE EMB 120 EMB120RT SO GREEN HYD SYST FAILED A COMA O OTHER K FLUID LOSS AP APPROACH 1 SO 01 168CA 120168 THE GREEN SYSTEM AUX HYD PUMP CYCLES ON AND OFF WITH MAIN PRESSUE AT 0 PSI. SUSPECT THE ENGINE PUMP CHECK VALVE TO BE A T FAULT LETTING AUX HYD PRESSURE TO REACH THE HIGH PRESSURE SWITCH CAUSING THE AUX HYD PUMP TO CYCLE ON AND OFF. THE RE SERVIOR ASSY WHERE THE CHECK VALVE WAS INSTALLED WAS REMOVED FOR ANALYSIS PER NTSB INVESTIGATOR. 2 L 7 2 4T RT A31SO 1996070300518 19960703 00518 SO 1996 7 3 COMA9610202 1 19960623 A 3231 SV14H11004 VALVE EMB 120 EMB120RT SO LANDING GEAR DR FAILED A COMA O OTHER K FLUID LOSS AP APPROACH 1 SO 01 168CA 120168 EMERGENCY EXTENSION PROCEDURE FAILED, AIRCRAFT MADE GEAR UP LANDING. SUSPECT LANDING GEAR DOORS STAYED CLOSED RESTRICTI NG EXTENSION OF LANDING GEAR. REMOVED LANDING GEAR DOOR SOLENOID VALVE PER NTSB INVESTIGATOR. 2 L 7 2 4T RT A31SO 1996070300519 19960703 00519 SO 1996 7 3 COMA9610203 1 19960623 A 2910 12040350001 HYD HOSE EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE CHAFED A COMA O OTHER K FLUID LOSS AP APPROACH 1 SO 01 168CA 120168 115325 LANDING GEAR FAILED TO EXTEND FOR LANDING. EMERGENCY EXTENSION PROCEDURES FAILED, AIRCRAFT MADE GEAR UP LANDING. INSPE CTION REVEALED THE LEFT GREEN HYD SYSTEM RESERVOIR WAS EMPTY. FOUND LEFT ENGINE DRIVEN HYD PUMP PRESSURE HOSE CHAFED TH ROUGH CAUSING HYD FLUID LEAKAGE. SUSPECT PRESSURE HOSE WAS CHAFED AGAINST THE LEFT OTBD COWLING DOOR SUPPORT ROD HOLDER . 2 L 7 2 4T 4 T RT A31SO E20NE 1996070300520 19960703 00520 SO 1996 7 3 COMA9610204 1 19960615 A 5347 12015995007 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 130G 120130 DURING 2C INSPECTION, FOUND SEAT TRACKS FOR LEFT HAND SIDE PASSENGER SEATS TO BE CORRODED. REMOVED CORRODED SEAT TRACKS AND REPLACED WITH SERVICEABLE TRACKS. 2 L 7 2 4T RT A31SO 1996070300521 19960703 00521 SO 1996 7 3 COMA9610205 1 19960615 A 5315 12020530001 FLOOR BEAM EMB 120 EMB120RT SO UNDER GALLEY CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 130G 120130 DURING 2C INSPECTION, FOUND SURFACE CORROSION ON FLOOR BEAM THAT GALLEY FLOOR ATTACHMENT TRACK MOUNTS TO. REMOVED SURFA CE CORROSION TREATED AREA AND PAINTED TO SERVICEABLE CONDITION. 2 L 7 2 4T RT A31SO 1996070300522 19960703 00522 SO 1996 7 3 COMA9610206 1 19960615 A 5347 12047507001 TRACK EMB 120 EMB120RT SO GALLEY FLOOR CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 130G 120130 DURING 2C INSPECTION, FOUND GALLEY FLOOR ATTACHMENT TRACK TO BE CORRODED. REMOVED CORRODED TRACK AND REPLACED WITH A SE RVICEABLE TRACK. 2 L 7 2 4T RT A31SO 1996070300523 19960703 00523 SO 1996 7 3 COMA9610207 1 19960615 A 2571 NAS620413D BOLT EMB 120 EMB120RT SO NLG RUSTED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 130G 120130 DURING 2C INSPECTION, FOUND FORWARD INBOARD CORNER OF BATTERY COMPARTMENT AT FRAME 4 TO HAVE SIGNS OF CORROSION. FURTHE R INSPECTION FOUND NOSE GEAR FORWARD DOOR, AFT HINGE, HARDWARE TO BE CORRODED. REPLACED HARDWARE AND CLEANED BATTERY CO MPARTMENT. 2 L 7 2 4T RT A31SO 1996070300524 19960703 00524 SO 1996 7 3 COMA9610208 1 19960615 A 5320 12005806003 BUTT STRAP EMB 120 EMB120RT SO FWD FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 130G 120130 DURING 2C INSPECTION, FOUND BUTT STRAPS TO HAVE SURFACE CORROSION. CLEANED, TREATED AND PAINTED AREA PER EMB M/M 51-21- 04. 2 L 7 2 4T RT A31SO 1996070300525 19960703 00525 SO 1996 7 3 COMA9610209 1 19960615 A 5313 12005144006 STRINGER EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 130G 120130 DURING 2C INSPECTION, FOUND STRINGERS IN LOWER FUSELAGE AREA BELOW LAV TO HAVE SURFACE CORROSION. CLEANED LIGHT CORROSI ON, TREATED AND PAINTED PER M/M 51-20-04. 2 L 7 2 4T RT A31SO 1996070300526 19960703 00526 SO 1996 7 3 COMA9610210 1 19960615 A 5347 12016000003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 130G 120130 DURING 2C INSPECTION, FOUND SEAT TRACKS FOR RIGHT HAND SIDE PASSENGERS SEATS TO BE CORRODED. REMOVED CORRODED SEAT TRAC KS AND REPLACED WITH SERVICEABLE TRACKS. 2 L 7 2 4T RT A31SO 1996070300527 19960703 00527 SO 1996 7 3 COMA9610211 1 19960615 A 5320 12013133001 SUPPORT SECTION EMB 120 EMB120RT SO CABIN CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 130G 120130 DURING 2C INSPECTION, FOUND PASSENGER SEAT RIGHT HAND SIDE WALL SEAT TRACK SUPPORT SECTION CORRODED ON SURFACE. CLEANED , TREATED, PAINTED CORRODED AREA PER EMB 120 M/M 51-21-04, OK FOR SERVICE. 2 L 7 2 4T RT A31SO 1996070300528 19960703 00528 SO 1996 7 3 COMA9610212 1 19960615 A 5320 12013136001 SUPPORT SECTION EMB 120 EMB120RT SO CABIN CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 130G 120130 DURING 2C INSPECTION, FOUND PASSENGER SEAT LEFT HAND SIDE WALL SEAT TRACK SUPPORT SECTION CORRODED ON SURFACE. CLEANED, TREATED, PAINTED CORRODED AREA PER EMB 120 M/M 51-21-04, OK FOR SERVICE. 2 L 7 2 4T RT A31SO 1996070300529 19960703 00529 SO 1996 7 3 COMA9610213 1 19960615 A 5320 12006962001 CROSS BEAM EMB 120 EMB120RT SO FLOOR SUPPORT CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 130G 120130 DURING 2C INSPECTION, FOUND PASSENGER FLOOR SUPPORT CROSSBEAM T-SECTION CORRODED AT FUSELAGE FRAME 16. REMOVED CORRODED T-SECTION, LOCATED, DRILLED AND INSTALLED NEW PART PER EMB 120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1996070300530 19960703 00530 SO 1996 7 3 COMA9610214 1 19960615 A 5320 12027289001 BUTT STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 130G 120130 DURING 2C INSPECTION, SEVERAL RIVETS WERE FOUND LOOSE OR WITH CORROSION AT ENTRY FLOOR, LT BUTT STRAP. REMOVED AND REPL ACED WITH ORIGINAL TYPE AND SIZE RIVETS, 19 TOTAL PER EMB 120 SRM CHAPTER 51. 2 L 7 2 4T RT A31SO 1996070300531 19960703 00531 SO 1996 7 3 COMA9610215 1 19960615 A 5315 12025029001 FLOOR BEAM EMB 120 EMB120RT SO FWD FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 130G 120130 DURING 2C INSPECTION, THE FLOOR BEAM NEXT TO THE ELEVATOR CONTROL COLUMN RIGHT WAS FOUND WITH SURFACE CORROSION. CLEANE D, TREATED AND PAINTED AREA PER M/M 51-21-04. 2 L 7 2 4T RT A31SO 1996070300532 19960703 00532 SO 1996 7 3 COMA9610216 1 19960615 A 5315 12005023001 FLOOR BEAM EMB 120 EMB120RT SO FWD FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 130G 120130 DURING 2C INSPECTION, THE FLOOR BEAM NEXT TO THE ELEVATOR CONTROL COLUMN LEFT WAS FOUND WITH SURFACE CORROSION. CLEANED , TREATED AND PAINTED AREA PER M/M 51-21-04. 2 L 7 2 4T RT A31SO 1996070300533 19960703 00533 SO 1996 7 3 COMA9610217 1 19960701 A 7603 0881824 SOLENOID EMB 120 EMB120RT SO RT ENGINE FAILED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 267CA 120259 RT ENGINE POWER LEVER, FLIGHT IDLE STOP SYSTEM, WAS INOP. REPLACED THE RT FLIGHT IDLE STOP SOLENOID. 2 L 7 2 4T RT A31SO 1996070300534 19960703 00534 EU 1996 7 3 COMA9630134 1 19960627 A 5610 7256100502 WINDSHIELD SAAB SF340 SF340A 7850100 EU RT COCKPIT AIR LEAK A COMA K NONE O OTHER CR CRUISE 1 SO 01 140N 340A140 NOTICEABLE WHISTLE IN COCKPIT WHEN BETWEEN 6000 AND 8000 FEET. REPLACED COCKPIT WINDSHIELD. 2 L 7 2 4T RT A52EU 1996070300535 19960703 00535 NE 1996 7 3 COMA9660116 2 19960629 A 7321 6078T55P05 FCU CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RT ENGINE MALFUNCTION A A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 940CA 7048 807170 AFTER STARTING THE RT ENGINE AND RPM STABILIZED FOR 30 TO 60 SECONDS THERE WAS AN UNCOMMANDED THRUST INCREASE. N1 EXCEE DED CHART SETTINGS. REPLACED THE ENGINE FUEL CONTROL UNIT. 2 L 7 2 4F 4 F RT A21EA E15NE 1996070300536 19960703 00536 WP 1996 7 3 DHL96804010 1 19960626 A 2611 303264 AMPLIFIER DOUG DC8 DC873F 302199F WP SMOKE DETECTORS MALFUNCTIONED A T DHLA A J UNSCHED LANDING DUMP FUEL N FALSE WARNING CR CRUISE 1 SO 01 804DH 46124 AFTER TAKEOFF, THE SMOKE DETECTORS ON NR 8, 10, 12 AND NR 14 CAME ON INTERMITTENTLY. REMOVED AND REPLACED SMOKE DETECTI ON SYSTEM AMPLIFIER AND RELAMPED NR 4 SMOKE DETECTOR MM 26-10. 2 L 7 4 4F RT 4A25 1996070300537 19960703 00537 WP 1996 7 3 SCNA96184 1 19960625 A 3350 EMBS1392 POWER SUPPLY DOUG DC10 DC1010 3022110 WP CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 572SC 46977 EMERGENCY LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY IAW MM 33-50-00. 2 L 7 3 4F A22WE 1996070300538 19960703 00538 NM 1996 7 3 UPS96220519 1 19960605 A 5320 653414422 EXPANSION LINK BOEING 727 72722C 138400F NM BS 848-870 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, FOUND CORRODED EXPANSION LINK STA 848 TO 870 RBL 45 WL 208 AND SUPPORT FITTING AT 870. REMOVED CORR ODED EXPANSION LINK AND SUPPORT FITTING AND REPLACED WITH NEW PARTS IAW SRM 51-30-5, 51-21-1, 51-30-2. 2 L 7 3 4F A3WE 1996070300539 19960703 00539 NM 1996 7 3 UPS96220520 1 19960529 A 5320 653414423 EXPANSION LINK BOEING 727 72722C 138400F NM BS 748-760 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON EXPANSION LINK STA 740 TO 760 RBL 45 WL 208. FOUND CORROSION TO BE OUT OF LIMITS IAW S RM 53-10-1. REMOVED CORRODED EXPANSION LINK AND REPLACED WITH NEW PART IAW OHM 20-41-05, 20-50-01, 20-50-03, 20-50-02. 2 L 7 3 4F A3WE 1996070300540 19960703 00540 NM 1996 7 3 UPS96220521 1 19960530 A 5320 ANGLE BOEING 727 72722C 138400F NM BS 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION IN RADIUS OF L-ANGLE AT BS 300, RBL 14 TO RBL 58 WL 208. ALSO, FOUND L-ANGLE TO BE CRACKE D ALONG RADIUS. REMOVED AND REPLACED L-ANGLE WITH NEW IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996070300541 19960703 00541 NM 1996 7 3 UPS96220522 1 19960529 A 5315 FLOOR BEAM BOEING 727 72722C 138400F NM BS 760-850 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION AROUND NUTPLATE ON FLANGE OF FLOOR BEAM STA 768 TO 858 RBL 45 WL 28. FOUND CORROSION TO B E OUT OF LIMITS IAW SRM 53-10-1, FABRICATED NEW PART AND INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996070300542 19960703 00542 NM 1996 7 3 UPS96220523 1 19960530 A 5320 BAC1510335 HAT CHANNEL BOEING 727 72722C 138400F NM BS 342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON HAT CHANNEL AT BS 342 RBL 16 TO RBL 61, WL 208. REMOVED CORROSION FOUND TO BE OUT OF L IMITS. REMOVED HAT CHANNEL, FABRICATED NEW HAT CHANNEL PER BOEING DWG 65-26173-3. INSTALLED NEW HAT CHANNEL, WORK DONE IAW SRM 51-30-2 SRM 53-10-1. 2 L 7 3 4F A3WE 1996070300543 19960703 00543 NM 1996 7 3 UPS96220524 1 19960620 A 5320 654661111 CHANNEL BOEING 727 72722C 138400F NM BS 850 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON INTERCOSTAL STA 850 LBL 45 TO 65 WL 208. REMOVED CORROSION AND FOUND TO BE OUT OF LIMI TS PER SRM 53-10-1. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-10-1. 2 L 7 3 4F A3WE 1996070300544 19960703 00544 NM 1996 7 3 UPS96220527 1 19960621 A 5320 SUPPORT BOEING 727 72722C 138400F NM BS 304 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON COCKPIT ENTRY SUPPORT STA 304 WL 208 LBL 4,9 RBL 3,8 AREA MARKED. FOUND CORROSION TO B E OUT OF LIMITS PER SRM 53-10-1, FARICATED REPLACEMENT SUPPORT PER SRM 51-20-1, 51-30-8 AND 51-30-5. REPLACED FLOOR SUP PORT AT BS 304 LBL 15 PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996070300545 19960703 00545 NM 1996 7 3 UPS96220528 1 19960620 A 5754 65162251 BULLNOSE BOEING 727 72722C 138400F NM NR 3 LE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, BULLNOSE CENTER HINGE LOWER ATTACH POINT ON NR 3 K-FLAP IS CORRODED UNDER BOLT HEAD. REMOVED AND RE PLACED NR 3 K-FLAP IAW MM 27-81-01. 2 L 7 3 4F A3WE 1996070300546 19960703 00546 NM 1996 7 3 UPS96220529 1 19960621 A 5320 WEB BOEING 727 72722C 138400F NM BS 480 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CRACK ON FLOOR WEB STA 480 WL 208 LBL 55 AREA MARKED. WHILE WORKING CRACK FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 51-10-1. REPAIRED PER SRM 51-40-2, 51-10-2 AND M/M 51-21-151. 2 L 7 3 4F A3WE 1996070300547 19960703 00547 NM 1996 7 3 UPS96220530 1 19960620 A 5754 65296219 TRACK BOEING 727 72722C 138400F NM NR 4 LE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, NR 4 SLAT TRACKS, BOTH HAVE CORROSION ON FWD ENDS AND BOTH SIDES. REMOVED AND REPLACED SLAT TRACKS IAW OHM 57-51-61. 2 L 7 3 4F A3WE 1996070300548 19960703 00548 NM 1996 7 3 UPS96220531 1 19960620 A 5320 653414423 LINK BOEING 727 72722C 138400F NM BS 740-760 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON EXPANSION LINK IN CENTER CHANNEL STA 740 TO 760 BL 0 WL 208. REMOVED CORROSION AND FOU ND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED EXPANSION LINK IAW 51-10-2, 51-10-6, 51-30-2, 51-30-4 AND 51-30-8. 2 L 7 3 4F A3WE 1996070300549 19960703 00549 NM 1996 7 3 UPS96220532 1 19960620 A 5320 6517593 SUPPORT BOEING 727 72722C 138400F NM BS 294-303 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON FLOOR SUPPORT STA 294 TO 303 LBL 13 TO 15 WL 208 ON BOTTOM OF SUPPORT. REMOVED CORROSI ON AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED SUPPORT IAW SRM 51-30-02, 51-20-4, 53-10-1. 2 L 7 3 4F A3WE 1996070300550 19960703 00550 NM 1996 7 3 UPS96220533 1 19960620 A 5320 693779915 ANGLE BOEING 727 72722C 138400F NM BS 365 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, GOUGE AND CRACK ON BARRIER NET SUPPORT ANGLES AT STA 365 STR 7 AND 8 LT. REMOVED AND REPLACED BARRI ER SUPPORT ANGLES AND CHANNEL IAW SRM 51-30-2, 51-10-2, 51-10-1. 2 L 7 3 4F A3WE 1996070300551 19960703 00551 NM 1996 7 3 UPS96220534 1 19960620 A 5320 FLOOR SUPPORT BOEING 727 72722C 138400F NM BS 315 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON LAV FLOOR SUPPORT STA 315 WL 208 RBL 17, 20, 24, 27, 30, 39 AREAS MARKED. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-10-1, 51-30-2, 53-10-1, 51-30-5. 2 L 7 3 4F A3WE 1996070300552 19960703 00552 NM 1996 7 3 UPS96220535 1 19960627 A 5311 FRAME BOEING 727 72722C 138400F NM BS 304 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, FOUND CORROSION ON FRAME AT BS 304 WL 175 LBL 44. CLEANED AND REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED PER EO 96-2371. 2 L 7 3 4F A3WE 1996070300553 19960703 00553 NM 1996 7 3 UPS96220536 1 19960529 A 5531 MID SPAR BOEING 727 72722C 138400F NM VERT STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, RT VERT FIN MID SPAR CHORD IS CHAFED AND FRETTING AT ACCESS PANEL 9602. REMOVED CORROSION FOUND OUT OF LIMITS, FABRICATED REPAIR PARTS AND INSTALLED ON A/C SRM 51-30-2 EWO 96-2333. 2 L 7 3 4F A3WE 1996070300554 19960703 00554 NM 1996 7 3 UPS96220537 1 19960529 A 5531 MID SPAR BOEING 727 72722C 138400F NM VERT STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION VERTICAL FIN MID SPAR CHORD IS CHAFED AND FRETTING AT ACCESS PANEL 9601. REMOVED CORROSIO N FOUND TO BE OUT OF LIMITS, FABRICATED REPAIR PARTS AND INSTALLED ON A/C IAW SRM 51-30-2 AND EWO 96-2334. 2 L 7 3 4F A3WE 1996070300555 19960703 00555 NM 1996 7 3 UPS96220538 1 19960626 A 5320 69246212 EXPANSON LINK BOEING 727 72722C 138400F NM BS 850-870 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON EXPANSION LINK STA 850 TO 870 LBL 45 WL 208. REMOVED CORROSION, FOUND TO BE OUT OF LIM ITS PER SRM 53-10-1, REPLACED EXPANSION LINK PER SRM 51-10-1, 51-30-5, 51-30-8, 51-30-2, 51-20-4. 2 L 7 3 4F A3WE 1996070300556 19960703 00556 NM 1996 7 3 UPS96220539 1 19960626 A 5320 65224010502 EXPANSION LINK BOEING 727 72722C 138400F NM BS 740-760 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON EXPANSION LINK STA 740 TO 760 LBL 25 WL 208. REMOVED CORROSION, FOUND TO BE OUT OF LIM ITS PER SRM 53-10-1, REPAIRED EXPANSION LINK PER SRM 51-10-1, 51-30-2. 2 L 7 3 4F A3WE 1996070300557 19960703 00557 NM 1996 7 3 UPS96220540 1 19960620 A 5320 INTERCOSTAL BOEING 727 72722C 138400F NM BS 219.8-227 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON BOTTOM OF INTERCOSTAL STA 219.8 TO STA 227 LBL 42 WL 227. REMOVED INTERCOSTAL, FABRICA TED AND INSTALLED NEW INTERCOSTAL IAW SRM 51-10-2, 51-30-2, 51-20-4. 2 L 7 3 4F A3WE 1996070300558 19960703 00558 NM 1996 7 3 UPS96220541 1 19960620 A 5753 651732214 RIB BOEING 727 72722C 138400F NM NR 8 LE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, NR 8 SLAT I/B TRACK SUPPORT STRUCTURE O/B RIB IS CRACKED IN 2 PLACES. REMOVED AND REPLACED NR 8 SLA T I/B TRACK SUPPORT FITTINGS AND WEBS PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996070300559 19960703 00559 NM 1996 7 3 UPS96220542 1 19960620 A 5320 65317731 CREASE BEAM BOEING 727 72722C 138400F NM BS 1176 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORRROSION ON STA 1176 CREASE BEAM FROM LBL 25 TO 55 WL 208. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 51-10-1. REMOVED CREASE BEAM CHORD AND REPLACED PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996070300560 19960703 00560 NM 1996 7 3 UPS96220543 1 19960620 A 5320 651631790 STIFFENER BOEING 727 72722C 138400F NM BS 351 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON DOGHOUSE FLOOR SUPPORT AT BS 351, RBL 20 AND RBL 30, WL 170. REMOVED AND REPLACED STIF FENER/FLOOR SUPPORT IAW SRM 51-30-2, 53-10-1, 51-30-5. 2 L 7 3 4F A3WE 1996070300561 19960703 00561 NM 1996 7 3 UPS96220544 1 19960620 A 5311 65225896 FRAME BOEING 727 72722C 138400F NM BS 351 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON BS 351 WEB AT RBL 37 AND 47, WL 168 BELOW DOGHOUSE FLOOR. REMOVED DAMAGED WEB SECTION AND INSTALLED NEW SECTION IAW SRM 51-40-2. ALSO, REPLACED CORRODED SHEAR TIE AT STR 24R DUE TO CORROSION OUT OF LIMITS. 2 L 7 3 4F A3WE 1996070300562 19960703 00562 NM 1996 7 3 UPS96220545 1 19960620 A 5311 FRAME BOEING 727 72722C 138400F NM BS 312 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON FRAME CHORD STA 312, RBL 43, WL 178. REMOVED AND REPLACED CHORD IAW SRM 53-10-1, 51-40 -3, 51-30-2. 2 L 7 3 4F A3WE 1996070300563 19960703 00563 NM 1996 7 3 UPS96220546 1 19960620 A 5711 SPAR BOEING 727 72722C 138400F NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION R/W UPPER REAR SPAR CHORD AT WBL 86 JUST ABOVE NR 3 ENGINE FUEL SHUTOFF VALVE. REPAIRED U PPER REAR SPAR CHORD IAW SB 727-57-0145, SRM 57-10-6 AND BOEING DRAWING 65-C19647. 2 L 7 3 4F A3WE 1996070300564 19960703 00564 NM 1996 7 3 UPS96220547 1 19960620 A 5320 CHANNEL BOEING 727 72722C 138400F NM BS 300-342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON HAT CHANNEL FROM BS 300 TO 342, RBL 12, WL 208. REMOVED AND REPLACED HAT CHANNEL IAW S RM 51-30-2, 53-10-1, 51-40-4. 2 L 7 3 4F A3WE 1996070300565 19960703 00565 NM 1996 7 3 UPS96220548 1 19960611 A 5751 6521773501 HINGE FTTNG BOEING 727 72722C 138400F NM LT INBD AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, L/W I/B AILERON TAB HAS ALL THREE HINGE FITTINGS CORRODED ON THE AILERON SIDE. REMOVED CORRODED HIN GE FITTINGS, INSTALLED NEW HINGE FITTINGS IAW SRM 51-30-2, MM 27-10-11. 2 L 7 3 4F A3WE 1996070300566 19960703 00566 NM 1996 7 3 UPS96220549 1 19960529 A 2710 65742845 PULLEY FITTINGS BOEING 727 72722C 138400F NM LT INBD AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, L/W I/B AILERON TURN AROUND PULLEY FITTING IS CORRODED ON LOWER SURFACE. REMOVED CORRODED FITTING W HICH WAS FOUND TO BE OUT OF LIMITS IAW SRM 57-40, INSTALLED NEW FITTING IAW SRM 51-30-2, MM 27-10-00 MM 27-61-00. 2 L 7 3 4F A3WE 1996070300567 19960703 00567 NM 1996 7 3 UPS96220550 1 19960529 A 2760 41460610 SPOILER MIXER BOEING 727 72722C 138400F NM RT WHEEL WELL CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON THE SPOILER MIXER INPUT QUADRANT. FOUND CORROSION TO BE OUT OF LIMITS SRM 57-40. REMO VED CORRODED SPOILER MIXER AND REPLACED WITH SERVICABLE UNIT MM 27-62-00, MM 27-61-31. 2 L 7 3 4F A3WE 1996070300568 19960703 00568 NM 1996 7 3 UPS96220551 1 19960531 A 5330 SKIN BOEING 727 72722C 138400F NM BS 1120-1130 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION BS 1120 TO 1130 BTWN STR 19R AND 20R INTERIOR FUSELAGE SKIN BTWN SKIN DOUBLER AND SKIN AT LAP JOINT, ONE RIVET HAS BUCKTAIL POPPED OFF. REMOVED FASTENERS BS 1108 TO 1142 COMMON TO STR 20R AND SKIN LAP FOR ACCE SS, FOUND DOUBLER TO BE CRACKED, INSTALLED SHORING FOUND TWO AREAS OF CORROSION ON TEAR STRAP, OUT OF LIMITS. SENT TO E NGINEERING RECEIVED RESPONSE AND REPAIRED PER EWO 96-2369 AND SRM 51-10-2 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996070300569 19960703 00569 NM 1996 7 3 UPS96220552 1 19960613 A 5320 ANGLE BOEING 727 72722C 138400F NM BS 760.95 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE-C, CORROSION ON FLOOR SUPPORT ANGLE AT BS 760.95 AND U/S OF CASTING AT 870 RT. CORROSION ON FLOOR SUPPO RT ANGLE REMOVED AND TREATED AND CASTING REPAIRED PER SRS EO 96-27-06. 2 L 7 3 4F A3WE 1996070300570 19960703 00570 NM 1996 7 3 UPS96220553 1 19960613 A 5320 SILL BOEING 727 72722C 138400F NM CARGO DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE-C, CARGO DOOR SILL CORRODED. REPLACED SILL. 2 L 7 3 4F A3WE 1996070300571 19960703 00571 NM 1996 7 3 UPS96220554 1 19960613 A 5753 FLAP TRACK BOEING 727 72722C 138400F NM LT TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE-C, L/W I/B FLAP TRACK CORRODED AND CORROSION ON BOLT HOLE IN LG BEAM FOR FLAP TRACK ATTACH. REPAIRED PE R UPS EO B727-5742-0651-1 AND SRS EO 96-27-011. 2 L 7 3 4F A3WE 1996070300572 19960703 00572 NM 1996 7 3 UPS96220555 1 19960613 A 5753 SUPPRT BRACKET BOEING 727 72722C 138400F NM TE MID FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE-C, MID FLAP INTERNAL STRUCTURE LT AND RT INB CRACKING IN RIB SUPPORT BRACKETS. BRACKETS REPLACED AS NEC ESSARY. 2 L 7 3 4F A3WE 1996070300573 19960703 00573 NM 1996 7 3 UPS96220556 1 19960613 A 5320 DOOR SILL BOEING 727 72722C 138400F NM MAIN CARGO DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE-C, SEVERAL AREAS OF CORROSION AS WELL AS A NUMBER OF HOLES DUE TO CORROSION IN MAIN CARGO DOOR SILL. RE PLACED SILL. 2 L 7 3 4F A3WE 1996070300574 19960703 00574 NM 1996 7 3 UPS96220557 1 19960613 A 5230 HINGES BOEING 727 72722C 138400F NM MAIN CARGO DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE-C, FORWARD AND AFT MAIN CARGO DOOR HINGES SEVERLY CORRODED. REPLACED HINGES. 2 L 7 3 4F A3WE 1996070300575 19960703 00575 NM 1996 7 3 UPS96220558 1 19960613 A 3210 SUPPORT BEAM BOEING 727 72722C 138400F NM MLG CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE-C, INCORRECT BOLTS PITTED. CORROSION FOUND IN MLG SUPPORT BEAM WHEN BOLTS REMOVED. REWORKED IAW UPSEO 727-5740-0727, SRS EO 96-27-011, EO 96-27-012. 2 L 7 3 4F A3WE 1996070300576 19960703 00576 NM 1996 7 3 UPS96220559 1 19960613 A 7110 LINING BOEING 727 72722C 138400F NM NR 2 ENG INTAKE WEAR DAMAGE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE-C, DAMAGE TO ATTENUATION LINING ON NR 2 ENGINE (S/N 81058). REPAIRED IAW UPS EO TAY 7230-8339-A. 2 L 7 3 4F A3WE 1996070300577 19960703 00577 NM 1996 7 3 UPS96220560 1 19960613 A 5330 SKIN BOEING 727 72722C 138400F NM BS 936 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE-C, CRACK FOUND IN SKIN BEHIND STR 18A AT RT BS 936. REPAIRED IAW UPS EO B727-5330-3815-A. 2 L 7 3 4F A3WE 1996070300578 19960703 00578 NM 1996 7 3 UPS96220561 1 19960613 A 5230 LATCH FITTINGS BOEING 727 72722C 138400F NM CARGO DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE-C, MAIN CARGO DOOR LATCH FITTINGS PINS SEIZED. ALL LATCH FITTINGS REPLACED SRS EO 96-27-005. 2 L 7 3 4F A3WE 1996070300579 19960703 00579 NM 1996 7 3 UPS96220562 1 19960613 A 5230 LOWER BEAM BOEING 727 72722C 138400F NM CARGO DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE-C, CRACK IN LOWER BEAM OF MAIN CARGO DOOR AT BS 580. REPAIRED IAW SRS EO 96-27-007. 2 L 7 3 4F A3WE 1996070300580 19960703 00580 NM 1996 7 3 UPS96220563 1 19960613 A 5330 SKIN BOEING 727 72722C 138400F NM BS 441 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE-C, CORROSON ON SKIN AT BUTT JOINT BS 441 54L TO 53R. REPAIRED PER APPENDIX 8.5 OF B727-5310-1371E. 2 L 7 3 4F A3WE 1996070300581 19960703 00581 NM 1996 7 3 UPS96220564 1 19960613 A 5311 FRAME BOEING 727 72722C 138400F NM BS 940 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE-C, CRACKS FOUND IN BS 940 FRAME. FRAME REPLACED PER UPS EO B727-5310-4501. 2 L 7 3 4F A3WE 1996070300582 19960703 00582 NM 1996 7 3 UPS96220565 1 19960613 A 5315 FLOOR BEAM BOEING 727 72722C 138400F NM BS 370 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE-C, CRACK FOUND ON FLOOR BEAM UPPER FLANGE AT BS 870 AT ATTACH POINT TO BS 870 FITTING RT SIDE. REPAIRED IAW SRS EO 96-27-012. 2 L 7 3 4F A3WE 1996070300583 19960703 00583 NM 1996 7 3 UPS96220566 1 19960613 A 5320 ATTACH FITTING BOEING 727 72722C 138400F NM BS 870 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE-C, CORROSION FOUND ON LOWER SURFACE OF THE AFT UPPER FLANGE OF THE BS 870 FITTING AT FLOOR BEAM ATTACH. REPAIR IAW SRS EO 96-27-006. 2 L 7 3 4F A3WE 1996070300584 19960703 00584 NM 1996 7 3 UPS96420567 1 19960629 A 3350 LIGHTS BOEING 747 747SR46 NM MAIN DECK INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 689UP 21033 INSPECTION TYPE N/A, EMERGENCY LIGHTS AT MAIN DECK STA 600 AND 750 ARE INOP. DEFERRED PER MEL 33-13, TRANSFERRED TO MEL LIST. 2 L 7 4 4F A20WE 1996070300585 19960703 00585 NM 1996 7 3 UPS96420568 1 19960628 A 2612 FIRE DETECTOR BOEING 747 747123 1384873 NM CARGO COMP MALFUNCTIONED A IPXA O OTHER N FALSE WARNING IN INSP/MAINT 1 SO 01 673UP 20325 INSPECTION TYPE N/A, THE AFT LOWER CARGO FIRE PROTECTION WAS GIVING FALSE INDICATIONS PERIODICALLY DURING FLIGHT. PERFO RM AFT CARGO LWR FIRE PROTECTION TEST PER MM 26-16-00, OPS CK NORMAL. 2 L 7 4 4F A20WE 1996070300586 19960703 00586 NM 1996 7 3 UPS96420569 1 19960628 A 2611 2156646 SMOKE DETECTOR BOEING 747 747121 1384871 NM CARGO COMPT DEFECTIVE A IPXA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 683UP 20353 INSPECTION TYPE PIRE, NR 5 MAIN DECK CARGO SMOKE DETECTOR ILLUMINATED. REPLACED NR 5 SMOKE DETECTOR (P/N 2156-646) (S/N 140) OFF. 2 L 7 4 4F A20WE 1996070300587 19960703 00587 WP 1996 7 3 UPS96820507 1 19960530 A 2760 56551682 SKIN DOUG DC8 DC871F 302199D WP NR 4 SPOILER DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE CS2, RT WING NR 4 SPOILER DELAMINATED ON LOWER INBD AFT CORNER. REPLACED SPOILER ASSY PER MM 27-61-01. 2 L 7 4 4F RT 4A25 1996070300588 19960703 00588 WP 1996 7 3 UPS96820508 1 19960605 A 5230 57542604 PAN DOUG DC8 DC871F 302199D WP X-SLIDE DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE CS2, A X-SLIDE DOOR FWD LOWER PAN CRACKED. REPLACED PAN ASSY PER DOUGLAS DRAWING 575384. 2 L 7 4 4F RT 4A25 1996070300589 19960703 00589 WP 1996 7 3 UPS96820509 1 19960603 A 5512 56545006 SKIN DOUG DC8 DC871F 302199D WP HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE CS2, RT HORIZONTAL STAB LEADING EDGE SKIN CRACKED AT DOUBLER STA XFS21 6. REPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996070300590 19960703 00590 WP 1996 7 3 UPS96820510 1 19960611 A 5520 5654970 MOUNTING FLANGE DOUG DC8 DC871F 302199D WP RT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE CS2, RT ELEVATOR TOADSTOOL UPPER ACCESS PANEL MOUNTING FLANGE IS CRACKED. REPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996070300591 19960703 00591 WP 1996 7 3 UPS96820511 1 19960606 A 5330 5613855143 SKIN DOUG DC8 DC871F 302199D WP BS 161 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE CS2, FUSELAGE SKIN CRACKED AT LT RADOME HINGE CUTOUT STA 161. REPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996070300592 19960703 00592 WP 1996 7 3 UPS96820512 1 19960602 A 5315 7753795504 FLOOR BEAM DOUG DC8 DC871F 302199D WP BS 1280 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE CS2, HEAVY CORROSION ON FLOOR BEAM FS 1280, LEFT TUNNEL AREA LBL 57. REPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996070300593 19960703 00593 WP 1996 7 3 UPS96820513 1 19960602 A 5320 526155112000 ANGLE DOUG DC8 DC871F 302199D WP BS 1625 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE CS2, MAIN CABIN HEAVY INTERGRANULAR CORROSION ON LONG 21R, FS 1625 ON ANGLE. REPLACED ANGLE PER SRM 51- 1-20D. 2 L 7 4 4F RT 4A25 1996070300594 19960703 00594 WP 1996 7 3 UPS96820514 1 19960603 A 5311 BELTFRAME DOUG DC8 DC871F 302199D WP BS 70 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE CS2, CORROSION CRACK ON BELTFRAME, FS 70 FWD SIDE, LONGERON 30R. REPAIRED FRAME PER SRM 53-2-5. 2 L 7 4 4F RT 4A25 1996070300595 19960703 00595 WP 1996 7 3 UPS96820515 1 19960605 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 640 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE CS2, HEAVY CORROSION ON BELTFRAME FS 640, LONGERONS 34L AND 34R. REPLACED FRAME SECTION PER SRM 51-1-20 D AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1996070300596 19960703 00596 WP 1996 7 3 UPS96820516 1 19960602 A 5311 5772958 BELTFRAME DOUG DC8 DC871F 302199D WP BS 1400 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE CS2, HEAVY CORROSION ON BELTFRAME AT FS 1400 ABOVE LONGERON 35R. REPAIRED FRAME PER SRM 53-2-0. 2 L 7 4 4F RT 4A25 1996070300597 19960703 00597 WP 1996 7 3 UPS96820517 1 19960611 A 5711 5892075 SPAR DOUG DC8 DC871F 302199D WP WS 64.76 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE CS2, HEAVY CORROSION ON HOLE CENTER WING UPPER INBOARD FRONT SPAR AT STA XFS64.76 RIB. REPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996070300598 19960703 00598 WP 1996 7 3 UPS96820518 1 19960608 A 5313 5750198 LONGERON DOUG DC8 DC871F 302199D WP BS 879-902 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE CS2, HEAVY CORROSION AND CRACKED LONGERON 24R FITTING BETWEEN FS 879 TO 902. REPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996070800009 19960708 00009 1996 7 8 96UAL900418 4 19960606 A 2210 4030952906 COUPLER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE E/E COMPT FAILED A UALA O OTHER E F VIBRATION/BUFFET FLT CONT AFFECTED CR CRUISE 1 WP 29 305UA 23666 SEVERAL UNCOMMANDED RUDDER MOVEMENTS, DESCENDED TO LOWER ALTITUDE. *S/D* YAW COUPLER WAS REPLACED. SHOP FOUND YAW COU PLER RATE GYRO FAULTY, CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1996070800010 19960708 00010 WP 1996 7 8 HAL9638 1 19960329 A 5240 5910084191 BEAM DOUG DC9 DC951 3022051 WP FWD SERVICE DOOR CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 EICBH 47796 HNL - FORWARD SERVICE DOOR SN 47786 CRACKED ON NR 2 BEAM AT LOWER HINGE ATTACH AREA. REPAIRED CRACKED BEAM PER SRO DWG NR 5936446. INSTALLED AND RIGGED DOOR PER MM 52-41-0. LEAK CHECKED OK. (X) 2 L 7 2 4F A6WE 1996070800011 19960708 00011 EU 1996 7 8 HCMA9622 1 19960605 A 6520 350A33215300 LAMIFICATION SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE T/R RUBBER TORN E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 982BH 651 2876 9389 LAMIFICATION RUBBER IS TORN BEYOND LIMITS. 1 G 7 1 3U 3 U H9EU E19EU 1996070900001 19960709 00001 NM 1996 7 9 DL73S961353 1 19960527 A 5315 FLOOR BEAM BOEING 737 737232 1384475 NM BS 660 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 302DL 23047 THE BL .07 FLOOR BEAM OF THE WING CENTER SECTION IS CRACKED AT FS 660. NO CRACKS WERE FOUND IN THE WEB. THE CRACK IS T YPICAL PER BACO SB 737-57-1210. THIS ERA WILL INSTALL THE SERVICE BULLETIN REPAIR FOR THIS CONDITION. 2 L 7 2 4F RT A16WE 1996071000014 19960710 00014 CE 1996 7 10 96ZZZX3372 1 19960602 A 3260 63210075 SWITCH CESSNA 402 402C 207590R CE NLG UPLOCK FAILED A SQFA O OTHER N FALSE WARNING CL CLIMB 1 SO 17 2651Y 402C0343 PILOT REPORTED THE RED UNSAFE GEAR LIGHT STAYED ON WITH GEAR UP AND LOCKED. CYCLED GEAR THREE TIMES, STILL THE SAME. O N TROUBLESHOOTING, FOUND FAULTY NOSE GEAR UPLOCK SWITCH. OPERATED GEAR 6 TIMES AFTER SWITCH CHANGED PER CESSNA MM, CHAP TER 27. TAKEOFF FROM FLL AND RETURNED TO FLL. 1 L 7 2 3O A7CE 1996071000019 19960710 00019 SO 1996 7 10 96ZZZX3377 2 19960413 A 8520 629340 ROD BOLT CESSNA 310 310R 2074245 CE CONT O520 IO520M 17032 SO NR 3 FAILED A A NTLA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 EA 23 17FA 310R0011 236360R TAKEOFF FROM BUF TO UTICA, NY, PILOT REPORTED FLUX IN OIL PRESSURE LT ENGINE, FOLLOWED BY ZERO OIL PRESSURE. UNEVENTFUL DIVERT TO ROC. INVESTIGATION FOUND .75 INCH HOLE IN CRANKCASE JUST UNDER THE DATA PLATE. CYLINDER REMOVAL FOUND THE N R 3 ROD AND CAP SEPARATED FROM THE CRANK THROW. FOUND ONE BOLT SHEARED AND OTHER BOLT SHOWED SECONDARY DAMAGE. NO SIGN S OF OVERHEATING, OVERSTRESS, OVERBOOST, OR OVERSPEED, OR MISASSEMBLY TECHNIQUE. CRANK AND CASES DAMAGED BEYOND REPAIR. 1 L 7 2 3O 3 O 3A10 E5CE 1996071000026 19960710 00026 SO 1996 7 10 96ZZZX3384 2 19960520 A 8530 SPRING CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO VALVES BROKEN A BAJA K NONE O OTHER IN INSP/MAINT 1 AL 01 3246M 325 402C0294 519128 DURING A SCHEDULED INSPECTION, A CYLINDER WAS IN THE PROCESS OF BEING CHANGED DUE TO LOW COMPRESSION. UPON REMOVAL OF T HE ROCKER COVER, ALL 4 VALVE SPRINGS WERE FOUND BROKEN. AFTER REMOVAL OF ALL ROCKER COVERS, ONLY ONE VALVE SPRING WAS I NTACT. THERE WERE NO DISCREPANCIES NOTED BY THE PILOT AS TO AN ABNORMAL RUNNING ENGINE. 1 L 7 2 3O 3 O A7CE E8CE 1996071000032 19960710 00032 CE 1996 7 10 96ZZZX3390 1 19960607 A 5210 5511232130 TUBE CESSNA 500 560CESSNA 2076750 CE DOOR LINKAGE MISADJUSTED A S A DXTA K NONE O OTHER IN INSP/MAINT 1 GL 07 336QS 585 5600336 CABIN ENTRY DOOR FAILED TO OPEN UPON ARRIVAL. CREW HAD TO EGRESS THROUGH ESCAPE HATCH. FOUND LOWER FORWARD 3 PINS FAIL ING TO RETRACT FULLY. SUBMITTER STATED CAUSE, FOUND EVIDENCE OF PIN CONTACT WITH CABIN DOOR FRAME. THIS CAUSED THE ABO VE TUBE TO BEND SLIGHTLY WHICH RESTRICTED FULL TRAVEL. 2 L 7 2 4F RT A22CE 1996071000040 19960710 00040 CE 1996 7 10 96ZZZX3398 1 19960601 A 2820 RELIEF VALVE BEECH 200 200BEECH 1152920 CE RT NAC TANK FAILED A GONA K NONE O OTHER IN INSP/MAINT 1 SW 01 131PA BB161 ON INTERIM INSPECTION, FOUND BULGING SKIN AND BENT HAT CHANNELS IN THE WHEELWELL LOWER NACELLE TANK LINER. INSPECTION F OUND BAD PRESSURE RELIEF VALVE. REPLACED LINER AND HAT CHANNELS. REPLACED BOTH RELIEF VALVES. SUGGEST 600-HOUR INSPEC TION ON VALVES. 1 L 7 2 4T A24CE 1996071000046 19960710 00046 NM 1996 7 10 9614366612 1 19960603 A 5315 FLOOR BEAM BOEING 747 747251B 1384892 NM FS 1720 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING P-CHECK, FOUND CORROSION ON THE BS 1720 FLOOR BEAM UPPER CHORD AT RBL 87. REPAIRED CHORD (P/N 65B06360-63) PER E A 66-101950. 2 L 7 4 4F A20WE 1996071000047 19960710 00047 NM 1996 7 10 9614376612 1 19960603 A 5315 FLOOR BEAM BOEING 747 747251B 1384892 NM FS 1740 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING P-CHECK, FOUND CORROSION ON THE BS 1740 FLOOR BEAM UPPER CHORD AT RBL 74. REPAIRED CHORD (P/N 65B06370-22) PER E A 66-101951. 2 L 7 4 4F A20WE 1996071000048 19960710 00048 NM 1996 7 10 9614386307 1 19960610 A 5315 FLOOR BEAM BOEING 747 747451 1384940 NM FS 980 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 667US 24222 DURING P-CHECK, FOUND CORROSION ON THE UPPER DECK FLOOR BEAM UPPER CHORD AT BS 980, RBL 20 TO RBL 30. REPAIRED BEAM (P/ N 65B25643-4) PER EA 63-101956. 2 L 7 4 4F RT A20WE 1996071000049 19960710 00049 NM 1996 7 10 9614396612 1 19960614 A 5312 BULKHEAD BOEING 747 747251B 1384892 NM FS 1251 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING P-CHECK, FOUND A CRACK AND CORROSION ON THE CANTED PRESSURE BULKHEAD DOUBLER AT BS 1251, LBL 84. REPAIRED DOUBLE R (P/N 65B07992-105) PER EA 66-101891. 2 L 7 4 4F A20WE 1996071000050 19960710 00050 NM 1996 7 10 9614406612 1 19960616 A 5711 SPAR BOEING 747 747251B 1384892 NM WS 1517 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING P-CHECK, FOUND CORROSION ON THE RIGHT WING FORWARD SPAR UPPER CHORD FS 1517. REPAIRED CHORD (P/N 65B10849-2) PER EA 66-101949. 2 L 7 4 4F A20WE 1996071000051 19960710 00051 NM 1996 7 10 9614416612 1 19960618 A 5312 BULKHEAD BOEING 747 747251B 1384892 NM FS 2360 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING P-CHECK, FOUND CORROSION ON THE AFT PRESSURE BULKHEAD LOWER FACEPLATE AT BS 2360, LBL 11. REPAIRED FACEPLATE, EX TRUDED Y-SECTION, (P/N 65B02634-13) PER EA 66-101888. 2 L 7 4 4F A20WE 1996071000052 19960710 00052 WP 1996 7 10 9614429867 1 19960620 A 5315 FLOOR BEAM DOUG DC9 DC951 3022051 WP FS 1108 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 776NC 47786 DURING H-CHECK, FOUND CORROSION ON THE FS 1108 FLOOR BEAM AT RBL 14. REPAIRED BEAM (P/N 9958186-1) PER EA 98-110807. 2 L 7 2 4F A6WE 1996071000053 19960710 00053 WP 1996 7 10 9614439867 1 19960620 A 5315 FLOOR BEAM DOUG DC9 DC951 3022051 WP FS 1136 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 776NC 47786 DURING H-CHECK, FOUND CORROSION ON THE FS 1136 FLOOR BEAM RIGHT SIDE. REPAIRED BEAM (P/N 9912243-59) PER EA 98-110806. 2 L 7 2 4F A6WE 1996071000054 19960710 00054 WP 1996 7 10 9614449867 1 19960620 A 5320 CUSP DOUG DC9 DC951 3022051 WP FS 1136-1167 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 776NC 47786 DURING H-CHECK, FOUND CORROSION ON THE RIGHT CUSP FROM FS 1136 TO 1167. REPAIRED CUSP (P/N 2777976) PER EA 98-110533. 2 L 7 2 4F A6WE 1996071000055 19960710 00055 NM 1996 7 10 9614456612 1 19960620 A 5313 LONGERON BOEING 747 747251B 1384892 NM FS 2150-2170 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING P-CHECK, FOUND CORROSION ON STR 50L AT BS 2150 AND 2170. REPAIRED STRINGER (P/N 65B04369-87) PER EA 66-101895. 2 L 7 4 4F A20WE 1996071000056 19960710 00056 NM 1996 7 10 9614466612 1 19960622 A 5313 LONGERON BOEING 747 747251B 1384892 NM FS 1708-1718 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING P-CHECK, FOUND CORROSION ON STR 47L AT BS 1708 AND 1718. REPAIRED STRINGER PER EA 66-101898. 2 L 7 4 4F A20WE 1996071000057 19960710 00057 NM 1996 7 10 9614476612 1 19960625 A 5313 LONGERON BOEING 747 747251B 1384892 NM FS 1851-1853 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING P-CHECK, FOUND CORROSION ON STR 49L FROM BS 1851 TO 1853. REPAIRED STRINGER PER EA 66-101889. 2 L 7 4 4F A20WE 1996071000058 19960710 00058 WP 1996 7 10 9614489105 1 19960627 A 5311 FRAME DOUG DC9 DC915 3022036 WP FS 180 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 95S 47205 DURING LINE CHECK, FOUND A CRACK EXTENDING APPROXIMATELY HALF WAY THROUGH THE FS 180 FRAME BETWEEN LONGERONS 6L TO 7L. R EPAIRED FRAME PER SRM 53-03 FIG 36, SHEETS 1 AND 2. 2 L 7 2 4F A6WE 1996071000059 19960710 00059 WP 1996 7 10 9614499305 1 19960628 A 5320 FITTING DOUG DC9 DC982 3022082 WP FS 197 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 307RC 48086 DURING H-CHECK, FOUND CRACKS IN BOTH THE FS 197 GIRT BAR ATTACH FITTINGS AT RBL 55. REPLACED FITTINGS. 2 L 7 2 4F A6WE 1996071000060 19960710 00060 WP 1996 7 10 9614509909 1 19960629 A 5320 FITTING DOUG DC9 DC931 3022065 WP CABIN DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 959N 47255 DURING M-CHECK, FOUND A .5 INCH CRACK IN THE AFT CABIN DOOR LOWER LEFT DOOR STOP FITTING. REPLACED FITTING PER SRM 51-3 0-2. 2 L 7 2 4F A6WE 1996071000061 19960710 00061 WP 1996 7 10 9614511154 1 19960701 A 3350 BATTERY DOUG DC10 DC1040 3023508 WP FUSELAGE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 154US 46763 DURING LINE INSPECTION, FLOOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED FOUR BATTERIES. 2 L 7 3 4F A22WE 1996071000062 19960710 00062 NM 1996 7 10 9614526622 1 19960702 A 3350 POWER SUPPLY BOEING 747 747251B 1384892 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 622US 21704 DURING LINE CHECK, FOUND LEFT OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996071000063 19960710 00063 WP 1996 7 10 9614539301 1 19960701 A 3350 BATTERIES DOUG DC9 DC982 3022082 WP TAIL COMPT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 301RC 48054 DURING LINE CHECK, FOUND EMERGENCY LIGHTS IN TAIL COMPARTMENT INOPERATIVE. REPLACED BATTERIES AT CHARGER R5 TO 28, OPER ATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996071000064 19960710 00064 WP 1996 7 10 9614549150 1 19960701 A 3350 LIGHT DOUG DC9 DC914 3022034 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8908E 45749 DURING LINE CHECK, FOUND TAIL COMPARTMENT OVERHEAD EMERGENCY LIGHTS INOPERATIVE AT STA 996. REWIRED LIGHT ASSEMBLY, OPE RATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996071000065 19960710 00065 WP 1996 7 10 9614559856 1 19960629 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 765MC 47718 DURING LINE CHECK, FOUND AFT STAIR EMERGENCY LIGHTS WILL NOT ILLUMINATE. REPLACED BATTERIES, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996071000066 19960710 00066 WP 1996 7 10 9614569862 1 19960701 A 2131 CONTROLLER DOUG DC9 DC951 3022051 WP CABIN MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 771MC 47769 ON CLIMBOUT, CABIN PEGGED AT 2,000 FPM DOWN, OUTFLOW FULLY CLOSED. COULD NOT CONTROL IN AUTO. PLACED OUTFLOW IN MANUAL TO CONTROL CABIN TO LANDING. RETURNED TO DTW AND LANDED WITHOUT INCIDENT. FOUND PRESSURIZATION CONTROLLER WOULD NOT P ASS BITE TEST. REPLACED CABIN PRESSURE CONTROLLER, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996071000067 19960710 00067 EU 1996 7 10 9614573228 1 19960626 A 3350 BATTERY PACK AIRBUS 320 A320211 3930320 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 328NW 298 DURING LINE MAINTENANCE, THE LEFT AND RIGHT AFT DOORS EMERGENCY LIGHTS WILL NOT ILLUMINATE. REPLACED BATTERY PACK, OPER ATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996071000068 19960710 00068 NE 1996 7 10 9614589910 2 19960701 A 7530 12356241 BLEED CK VLV DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9A 52048 NE NR 2 ENGINE LEAKING A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 960N 47256 666150 NR 2 ENGINE FIRE WARNING ILLUMINATED SEVERAL TIMES DURING TAKEOFF AND CLIMB. THE FLIGHT RETURNED TO DTW AND LANDED WITH OUT INCIDENT. MAINTENANCE REPLACED A LEAKING 8TH STAGE BLEED CHECK VALVE WITH A SERVICEABLE UNIT. 2 L 7 2 4F 4 F A6WE E2EA 1996071000069 19960710 00069 WP 1996 7 10 9614599602 1 19960701 A 3231 DOOR DOUG DC9 DC932 3022066 WP NLG OPEN A NWAA A UNSCHED LANDING E P VIBRATION/BUFFET NO WARNING INDICATION CL CLIMB 1 GL 01 602NW 47046 VIBRATION WAS COMING FROM NOSE GEAR AREA AFTER TAKEOFF. GEAR INDICATION WAS NORMAL. RECYCLED GEAR BUT VIBRATION CONTIN UED. FLIGHT RETURNED TO MDT AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND RIGHT FORWARD NOSE LANDING GEAR DOOR OPEN. 2 L 7 2 4F A6WE 1996071000070 19960710 00070 WP 1996 7 10 9614609919 1 19960701 A 3260 DT2RA7 SWITCH DOUG DC9 DC932 3022066 WP GEAR LEVER MALFUNCTIONED A NWAA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 01 941N 47450 DURING APPROACH, LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. RECYCLED GEAR AND NORMAL INDICATIONS WERE ACHIEVED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LANDING GEAR LEVER WARNING SWITCH, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996071000071 19960710 00071 WP 1996 7 10 9614619986 1 19960630 A 3350 60030451 POWER SUPPLY DOUG DC9 DC932 3022066 WP AFT FUSELAGE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 986US 47480 DURING PERIODIC CHECK, FOUND AFT STAIRWAY AND OVERHEAD TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SU PPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996071000072 19960710 00072 WP 1996 7 10 9614629611 1 19960701 A 3350 60030451 BATTERY PACK DOUG DC9 DC932 3022066 WP FWD CABIN MALFUNCTIONED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 611NW 47435 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERAT IONAL CHECK OK. 2 L 7 2 4F A6WE 1996071000073 19960710 00073 WP 1996 7 10 9614639917 1 19960701 A 3397 WIRE DOUG DC9 DC932 3022066 WP CABIN SHORTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 967N 47573 FLIGHT ATTENDANT REPORTED FORWARD CABIN FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPAIRED SHORTED WIRE AT ROW 10, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996071000074 19960710 00074 1996 7 10 9614643239 4 19960702 A 2330 VIDEO DISP UNIT AIRBUS 320 A320211 3930320 EU RT CABIN MALFUNCTIONED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 339NW 367 DURING CRUISE, NOTICED UNIDENTIFIABLE FUMES IN THE AREA OF THE FIRST CLASS COAT CLOSET. AN EMERGENCY WAS DECLARED AND A IRCRAFT DIVERTED TO ATL AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RIGHT HAND SIDE FIRST CLASS VIDEO DISPLAY UN IT AT FAULT AND REMOVED IT. THE CIRCUIT BREAKER FOR THE UNIT WAS PULLED. 2 L 7 2 4F RT A28NM 1996071000075 19960710 00075 NM 1996 7 10 96FDEA00380 1 19960228 A 5315 6540145 FLOOR BEAM BOEING 727 72722 1384002 NM BS 580 DOUBLE DRILLED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 194FE 19143 WHILE WORKING NR0308 FOUND HOLE IN RADIUS OF FLOOR BEAM LOWER CHORD BS 580 BL 0 WL 200. *S/D* REPAIRED FLOOR BEAM PER SRM 53-10-8. 2 L 7 3 4F A3WE 1996071000076 19960710 00076 NM 1996 7 10 96FDEA00843 1 19960425 A 5315 6540145 FLOOR BEAM BOEING 727 72725 1384006 NM BS 680 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 NR0400 AND 007, DAMAGED LOWER FLOOR BEAM DUE TO SCREW PROTRUSION CHAFING AT BS 680 LBL TO RBL 18 WL 200. *S/D* REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, DRILLED AND INSTALLED WORKED IAW FEDEX SRM 53-10-8 FIG 2. 2 L 7 3 4F A3WE 1996071000077 19960710 00077 NM 1996 7 10 96FDEA00846 1 19960425 A 5311 BAC1511966 FRAME BOEING 727 72725 1384006 NM BS 1148 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 NR0386 AND 004, CORROSION ON FRAME BS 148 BETWEEN STR 14 TO 15R. *S/D* REMOVED DAMAGED FRAME DOUBLER AND FAIL-SAFE, RE PLACED WITH FABRICATED REPAIR PARTS AT BS 1130 BETWEEN STR 14R AND 15R IAW FEDEX SRM 51-40-3 FIG 1 53-10-2. 2 L 7 3 4F A3WE 1996071000078 19960710 00078 WP 1996 7 10 96FDEA01127 1 19960613 A 5720 FITTING DOUG DC10 DC1010F 3022111 WP LT MLG CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 SNRM 5054, LEFT MLG FITTING EXHIBITS EXFOLIATION CORROSION APPROX 2 SQ IN AT LEFT LWR INTERNAL SURFACE. *S/D* CLEAN AN D TREAT CORROSION, REMOVED AND REPLACED LT LWR FWD AUX SPAR SPLICE PER EA 8-5710-28974. 2 L 7 3 4F A22WE 1996071000079 19960710 00079 NE 1996 7 10 96FDEA01188 2 19960703 A 7200 ENGINE AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680C2A5 NE NR 1 FAILED A FDEA E ENGINE SHUTDOWN X ENGINE FLAMEOUT DE DESCENT 1 SO 25 650FE 745 NR 1 ENGINE FAILED ON ARRIVAL DURING THE DESCENT WHILE AT IDLE POWER. A RELIGHT WAS ATTEMPTED AND A RELIGHT IE EGT ROSE FOR ABOUT 5 SECONDS AND THERE WAS A SHUTDOWN AGAIN. 2 L 7 2 4F 4 F RT A35EU E13NE 1996071000080 19960710 00080 NM 1996 7 10 96FDEA01189 1 19960702 A 5313 6561477 STRINGER BOEING 727 727173C 1384059 NM BS 1057 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 199FE 19509 NR0557 AND 014, WHILE WORKING NR0540, FOUND STR 28R AT BS 1057 TO BE CRACKED AND CORRODED. *S/D* REMOVED DAMAGE STRING ER SECTION AT BS 1057 AND INSTALLED REPAIRED PER SRM 53-10-3. 2 L 7 3 4F A3WE 1996071000081 19960710 00081 NM 1996 7 10 96FDEA01190 1 19960703 A 5330 6518420 SKIN BOEING 727 727173C 1384059 NM BS 358-360 NO EDGE DISTANCE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 199FE 19509 NR0548 AND 015, SKIN HAS INSUFFICIENT EDGE DISTANCE AT BS 358 TO 360 AT STR 27L EXTERNAL SIDE OF SKIN. 2 L 7 3 4F A3WE 1996071000082 19960710 00082 NM 1996 7 10 96UAL900236 1 19960404 A 2421 729825G IDG BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE FAILED A UALA H DEACTIVATE SYST/CIRCUITS H E J ELECT. POWER LOSS-50 PC VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 WP 29 550UA 25398 LEFT GENERATOR FAILED, IDG DRIVE DISCONNECTED ACCOMPANIED WITH INCREASED VIBRATION. *S/D* FOUND INTEGRATED DRIVE GENER ATOR FAILED. REPLACED GENERATOR, CHECKS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 1996071000083 19960710 00083 NM 1996 7 10 96UAL900468 1 19960624 A 3350 920542U1 BATTERY PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7286U 21564 OVERWING EXIT SIGNS ON RIGHT SIDE DO NOT ILLUMINATE DURING EMERGENCY LIGHT TEST. *S/D* CAUSE WAS LOW VOLTAGE. REPLACED BATTERY/POWER SUPPLY. 2 L 7 3 4F 4 F A3WE E2EA 1996071000084 19960710 00084 NE 1996 7 10 96UAL900469 2 19960624 A 7200 ENGINE BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE NR 4 MALFUNCTIONED A UALA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 29 155UA 20104 663085 AFTER TAKEOFF, NR 4 ENGINE EPR DROPPED FROM 1.44 TO 1.26, FUEL FLOW LOW, NR 4 GENERATOR BREAKER TRIPPED, BOTH NR 4 FIRE INDICATIONS APPROACHED FIRE RANGE. SHUT DOWN ENGINE. *S/D* ENGINE WAS REMOVED AND TESTED. TEST CELL PERSONNEL WERE U NABLE TO DUPLICATE THE CONDITION. THE AIRCRAFT HAS NOT EXPERIENCED ANY RECURRING PROBLEMS WITH A DIFFERENT ENGINE INSTA LLED. 2 L 7 4 4F 4 F A20WE E20EA 1996071000085 19960710 00085 NE 1996 7 10 96UAL900470 2 19960624 A 7314 500991D FUEL PUMP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ENGINE FAILED A UALA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 WP 29 433UA 589 V10167 AT CRUISE FL330, RECEIVED AN ECAM MESSAGE 'COMPRESSOR VANE'. SHORTLY AFTER ENGINE 2 BEGAN FLUCTUATING AND THEN SHUT IT SELF DOWN. *S/D* FOUND ALUMINUM CHIPS IN FUEL FILTER, IMPELLER STAGE AND HOUSING OF FUEL PUMP HAD EXTENSIVE DAMAGE CAU SED BY A BOLT IN FUEL SYSTEM. ENGINE FUEL FILTER, FUEL METERING UNIT AND FUEL PUMP WERE REPLACED AND OPERATIONALLY CHEC KED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 1996071000086 19960710 00086 EU 1996 7 10 96UAL900471 1 19960624 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAILED TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 402UA 439 EMERGENCY ESCAPE LIGHTS FAIL OPERATIONAL TEST. 2 L 7 2 4F 4 F RT A28NM E40NE 1996071000087 19960710 00087 NM 1996 7 10 96UAL900472 1 19960624 A 2131 CONTROLLER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 7443U 21897 MADE AN UNPLANNED LAS STOP DUE TO PARTIAL LOSS OF CABIN PRESSURE. CABIN STARTED TO CLIMB, SWITCHED TO MANUAL. WHILE CO NTROLLING IN MANUAL AUTO STARTED TO CONTROL THE OUTFLOW VALVE. *S/D* REMOVED AND RERACKED THE CABIN PRESSURE CONTROLLE R AND THE SYSTEM OPERATIONALLY CHECKED GOOD. 2 L 7 3 4F 4 F A3WE E2EA 1996071000088 19960710 00088 WP 1996 7 10 ABXA9600521 1 19960418 A 5313 27779223 LONGERON DOUG DC9 DC941 302207N WP BS 160 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX 47499 DURING C-CHECK INSPECTION, FOUND LONGERON 2L CRACKED AT STA 160. REPAIRED IAW DC-9 SRM 53-02, FIGURE 2. 2 L 7 2 4F A6WE 1996071000089 19960710 00089 WP 1996 7 10 ABXA9600522 1 19960416 A 5313 27779223 LONGERON DOUG DC9 DC941 302207N WP BS 160/200 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX 47499 DURING C-CHECK INSPECTION, FOUND LONGERON 4L CRACKED AT STA 160, 200. REPAIRED IAW DC-9 SRM 51-30-2, 51-30-5 AND 53-02 FIGURE 2. 2 L 7 2 4F A6WE 1996071000090 19960710 00090 WP 1996 7 10 ABXA9600523 1 19960406 A 7830 5958782503 TR LINK PWA 4310001 DOUG DC9 DC931 3022065 WP RT ENGINE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX DL125 47551 DURING COMPLIANCE OF AD'S 75-14-06, 90-18-03 SB'S 78-36, 78-38, 78-40 AND 78-66, FOUND RIGHT THRUST REVERSER OUTBOARD UP PER DRIVER LINK HAD A CRACK INDICATION. REPLACED RIGHT THRUST REVERSER OUTBOARD UPPER DRIVER LINK IAW DC-9 MM 78-31-5. LINK FOUND TO BE CRACKED AND WAS SCRAPPED. 2 L 7 2 4F A6WE 1996071000091 19960710 00091 WP 1996 7 10 ABXA9600524 1 19960423 A 3231 3923159505 LINK DOUG DC9 DC931 3022065 WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 943AX 47528 DURING COMPLIANCE WITH AD 91-22-07 ASB 32-244 R2, FOUND THE LEFT MAIN LANDING GEAR FLYING DOOR IDLER LINK WORN. REPLACE D LINK IAW DC-9 MM 20-16-0. 2 L 7 2 4F A6WE 1996071000092 19960710 00092 WP 1996 7 10 ABXA9600525 1 19960428 A 5280 HB218600 BUSHING DOUG DC9 DC941 302207N WP RT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 979AX 47492 DURING COMPLIANCE OF AD 91-22-07 ASB 32-244, FOUND RIGHT MAIN LANDING GEAR OUTBOARD DOOR WING MOUNTED HINGE WORN. REPLA CED HINGE BUSHINGS IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1996071000093 19960710 00093 WP 1996 7 10 ABXA9600526 1 19960428 A 5280 29244721 PIN DOUG DC9 DC941 302207N WP RT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 979AX 47492 DURING COMPLIANCE OF AD 91-22-07 ASB 32-244, FOUND RIGHT MAIN LANDING GEAR OUTBOARD DOOR WING MOUNTED HINGE WORN. REPLA CED HINGE PINS IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1996071000094 19960710 00094 WP 1996 7 10 ABXA9600527 1 19960428 A 3233 S10266145802 BUSHING DOUG DC9 DC941 302207N WP LT MLG ACTUATOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 979AX 47492 DURING COMPLIANCE OF AD 91-22-07 ASB 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD ACTUATOR ROD END BUSHINGS WORN. REPL ACED SPACERS IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1996071000095 19960710 00095 WP 1996 7 10 ABXA9600528 1 19960517 A 5240 49157581 CRANK ASSY DOUG DC9 DC931 3022065 WP FWD SERV DOOR BROKEN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47165 DURING COMPLIANCE OF AD'S 81-10-10 AND 90-18-03 SB'S 52-125 REV 5 AND SB 52-127, REV 2, FOUND CRANK ASSEMBLY SERVICE DOO R OPEN LATCH BROKEN. REPLACED CRANK ASSEMBLY IAW DC-9 MM. 2 L 7 2 4F A6WE 1996071000096 19960710 00096 WP 1996 7 10 ABXA9600529 1 19960517 A 5240 39137492 FITTING DOUG DC9 DC931 3022065 WP FWD SERV DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47165 DURING COMPLIANCE OF AD 81-10-10, AD 90-18-03, SB'S 52-125, REV 5 AMD SB 52-127 REV 2, FOUND SERVICE DOOR TORQUE TUBE UP PER ATTACH FITTING HOUSING ASSEMBLY CRACKED. REPLACED UPPER ATTACH FITTING IAW DC-9 MM. 2 L 7 2 4F A6WE 1996071000097 19960710 00097 WP 1996 7 10 ABXA9600530 1 19960506 A 5280 5910557504 DOOR DOUG DC9 DC933F 302207A WP RT WING WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK AND COMPLIANCE OF AD 91-22-07 ASB 32-244, FOUND THE RIGHT FLYING DOOR LINKAGE WORN AND THE SEAL CRACKED. REPLACED DOOR IAW DC-9 MM. 2 L 7 2 4F A6WE 1996071000098 19960710 00098 WP 1996 7 10 ABXA9600531 1 19960506 A 5320 992240591 PAN DOUG DC9 DC933F 302207A WP BS 176 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK INSPECTION, FOUND CRACKED CUP ASSEMBLY AT STA 176, LBL 44. FABRICATED PAN IAW DOUGLAS DRAWING NR 9922405 AND INSTALLED IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 1996071000099 19960710 00099 WP 1996 7 10 ABXA9600532 1 19960506 A 5320 922405103 PAN DOUG DC9 DC933F 302207A WP BS 176 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK INSPECTION, FOUND CRACKED CUP ASSEMBLY AT STA 176, BL 0. FABRICATED PAN IAW DOUGLAS DRAWING NR 922405 AN D INSTALLED IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 1996071000100 19960710 00100 WP 1996 7 10 ABXA9600533 1 19960506 A 5320 992240595 PAN DOUG DC9 DC933F 302207A WP BS 176 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK INSPECTION, FOUND CRACKED CUP ASSEMBLY AT STA 176, RBL 22. FABRICATED PAN IAW DOUGLAS DRAWING NR 922405 AND INSTALLED IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 1996071000101 19960710 00101 WP 1996 7 10 ABXA9600534 1 19960429 A 5320 991050131 CUSP DOUG DC9 DC933F 302207A WP BS 218 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK INSPECTION, FOUND CUSP WEB CRACKED AT STA 218 RIGHT. REPAIRED IAW DC-9 SRM 53-01, FIGURE 2. 2 L 7 2 4F A6WE 1996071000102 19960710 00102 WP 1996 7 10 ABXA9600535 1 19960506 A 5320 992240593 PAN DOUG DC9 DC933F 302207A WP BS 176 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK INSPECTION, FOUND CRACKED CUP ASSEMBLY AT STA 176, RBL 44. FABRICATED PAN IAW DOUGLAS DRAWING NR 9922405 AND INSTALLED IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 1996071000103 19960710 00103 WP 1996 7 10 ABXA9600536 1 19960615 A 3231 BLFR5112T2 BEARING DOUG DC9 DC941 302207N WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 DURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND THE LEFT MAIN LANDING GEAR DOOR ROD ASSEMBLY BEARING WORN AT WELL ON OUTBOARD MAIN LANDING GEAR DOOR. REPLACED BEARING IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1996071000104 19960710 00104 WP 1996 7 10 ABXA9600537 1 19960430 A 5313 27779224 LONGERON DOUG DC9 DC933F 302207A WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK INSPECTION, FOUND LONGERON 17L CRACKED AT STA 980. REPAIRED IAW DC-9 SRM 53-02, FIGURE 2. 2 L 7 2 4F A6WE 1996071000105 19960710 00105 WP 1996 7 10 ABXA9600538 1 19960501 A 5320 99105037 CUSP DOUG DC9 DC933F 302207A WP BS 870 - 889 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK INSPECTION, FOUND CUSP WEB CRACKED AT STA 870 TO 889 LEFT. REPAIRED IAW DC-9 SRM 53-01, PAGE 11. 2 L 7 2 4F A6WE 1996071000106 19960710 00106 WP 1996 7 10 ABXA9600539 1 19960430 A 5311 9923454501 FRAME DOUG DC9 DC933F 302207A WP BS 696 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK INSPECTION, FOUND CRACKED FRAME AT STA 696 AT LEFT CANTED KEEL. REPAIRED IAW DC-9 SRM 53-03, FIGURE 12. 2 L 7 2 4F A6WE 1996071000107 19960710 00107 WP 1996 7 10 ABXA9600540 1 19960430 A 5311 992345311 FRAME DOUG DC9 DC933F 302207A WP BS 675 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK INSPECTION, FOUND CRACKED FRAME AT STA 675 AT LEFT CANTED KEEL. REPLACED DOUBLER IAW DC-9 SRM 53-03, FIG URE 12. 2 L 7 2 4F A6WE 1996071000108 19960710 00108 WP 1996 7 10 ABXA9600541 1 19960514 A 3231 S24312157A016 LINKAGE DOUG DC9 DC933F 302207A WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK INSPECTION AND COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND LEFT FLYING DOOR LINKAGE WORN. REPLACED WORN PARTS IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1996071000109 19960710 00109 WP 1996 7 10 ABXA9600542 1 19960514 A 3231 S24312155A017 LINKAGE DOUG DC9 DC933F 302207A WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK INSPECTION AND COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND LEFT FLYING DOOR LINKAGE WORN. REPLACED WORN PARTS IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1996071000110 19960710 00110 WP 1996 7 10 ABXA9600543 1 19960514 A 3231 NAS104 LINKAGE DOUG DC9 DC933F 302207A WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK INSPECTION AND COMPLIANCE OF AD 91-220-7, ASB 32-244, FOUND LEFT FLYING DOOR LINKAGE WORN. REPLACED WORN PARTS IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1996071000111 19960710 00111 WP 1996 7 10 ABXA9600544 1 19960514 A 3231 DREMS5085 LINKAGE DOUG DC9 DC933F 302207A WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK INSPECTION AND COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND LEFT FLYING DOOR LINKAGE WORN. REPLACED WORN PART IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1996071000112 19960710 00112 WP 1996 7 10 ABXA9600545 1 19960503 A 5320 99105014 CUSP DOUG DC9 DC933F 302207A WP BS 237 - 242 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK INSPECTION, FOUND CUSP WEB CRACKED AT STA 237 TO 242 RIGHT. REPLACED CUSP IAW DC-9 SRM 51-30-1 AND 51-30 -2. 2 L 7 2 4F A6WE 1996071000113 19960710 00113 WP 1996 7 10 ABXA9600546 1 19960501 A 5311 27779305 FRAME DOUG DC9 DC933F 302207A WP BS 465 DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK INSPECTION, FOUND FRAME 465 HAD A HOLE IN THE RADIUS AT LONGERON 16L. REPAIRED IAW DC-9 SUPP SRM K05159. 2 L 7 2 4F A6WE 1996071000114 19960710 00114 WP 1996 7 10 ABXA9600547 1 19960430 A 5320 99105014 CUSP DOUG DC9 DC933F 302207A WP BS 256 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK INSPECTION, FOUND CUSP WEB CRACKED AFT OF STA 256 RIGHT. REPAIRED IAW DC-9 SRM 53-01 FIGURE 2, SHEET 2 A ND 51-10-3. 2 L 7 2 4F A6WE 1996071000115 19960710 00115 WP 1996 7 10 ABXA9600548 1 19960501 A 5313 29248741 LONGERON DOUG DC9 DC933F 302207A WP BS 408 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK INSPECTION, FOUND LONGERON 17R CRACKED AT STA 408. REPAIRED IAW DC-9 SRM 53-02, FIGURE 2. 2 L 7 2 4F A6WE 1996071000116 19960710 00116 WP 1996 7 10 ABXA9600549 1 19960430 A 5313 27779224 LONGERON DOUG DC9 DC933F 302207A WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK INSPECTION, FOUND LONGERON 17R CRACKED AT PYLON BULKHEAD. REPAIRED IAW DC-9 SRM 53-02, FIGURE 2. 2 L 7 2 4F A6WE 1996071000117 19960710 00117 WP 1996 7 10 ABXA9600550 1 19960429 A 5320 99105014 CUSP DOUG DC9 DC933F 302207A WP BS 275 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK INSPECTION, FOUND CUSP WEB CRACKED AT STA 275, LONGERON 18R. REPAIRED IAW DC-9 SRM 53-01, FIGURE 2. 2 L 7 2 4F A6WE 1996071000118 19960710 00118 WP 1996 7 10 ABXA9600551 1 19960507 A 5312 591142717 BULKHEAD TEE DOUG DC9 DC933F 302207A WP BS 996 TRIMMED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK INSPECTION AND AFT PRESSURE BULKHEAD T-CAP CHANGE, LONGERON 25 LEFT TEE WAS TRIMMED FOR ACCESS. REPAIRED IAW ABX REA D953-15276-MR. 2 L 7 2 4F A6WE 1996071000119 19960710 00119 WP 1996 7 10 ABXA9600552 1 19960503 A 5320 992240615 WEB DOUG DC9 DC933F 302207A WP BS 218 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK INSPECTION, FOUND EXFOLIATION CORROSION THROUGH SUBFLOOR AT STA 218, RBL 22 TO RBL 44. REPAIRED IAW ABX REA D953-15251-MR. 2 L 7 2 4F A6WE 1996071000120 19960710 00120 WP 1996 7 10 ABXA9600553 1 19960505 A 5320 9910155105 PANEL DOUG DC9 DC933F 302207A WP BS 737 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK INSPECTION, FOUND CORROSION ON UPPER SURFACE OF THE AFT CENTER PRESSURE PANEL. REPAIRED IAW ABX REA D953 -15270-MR. 2 L 7 2 4F A6WE 1996071000121 19960710 00121 WP 1996 7 10 ABXA9600554 1 19960430 A 5320 991050111 CUSP DOUG DC9 DC933F 302207A WP BS 332 - 351 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK INSPECTION, FOUND RIGHT SIDE CUSP WEB CORRODED FROM STA 332 TO 351. REPAIRED IAW DC-9 SRM 53-01, FIGURE 2. 2 L 7 2 4F A6WE 1996071000122 19960710 00122 WP 1996 7 10 ABXA9600555 1 19960506 A 5320 992240615 SUBFLOOR DOUG DC9 DC933F 302207A WP BS 160 - 200 DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK INSPECTION, FOUND SUBFLOOR DAMAGED AT STA 160 TO 200. REPAIRED IAW DC-9 SRM 53-01 FIGURE 2, SHEET 3. 2 L 7 2 4F A6WE 1996071000123 19960710 00123 WP 1996 7 10 ABXA9600556 1 19960506 A 5320 922405105 PAN DOUG DC9 DC933F 302207A WP BS 176 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK INSPECTION, FOUND CRACKED CUP ASSEMBLY AT STA 176, LBL 22. FABRICATED PAN IAW DOUGLAS DRAWING NR 922405 AND INSTALLED IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 1996071000124 19960710 00124 WP 1996 7 10 ABXA9600557 1 19960514 A 3231 3923158501 LINKAGE DOUG DC9 DC933F 302207A WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 91-22-07, ASB 32-244, FOUND LEFT FLYING DOOR LINKAGE WORN. REPLACED WO RN PARTS IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1996071000125 19960710 00125 WP 1996 7 10 ABXA9600558 1 19960510 A 3231 S2272677F HINGE DOUG DC9 DC933F 302207A WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK INSPECTION AND COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND LEFT FLYING DOOR ARTICULATING DOOR HINGE WORN . REPLACED HINGE IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 1996071000127 19960710 00127 WP 1996 7 10 ABXA9600560 1 19960510 A 5321 99578263 FLOOR PANEL DOUG DC9 DC933F 302207A WP COCKPIT PUNCTURED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK INSPECTION, FOUND COCKPIT FLOOR PANEL PUNCTURED AFT OF THE PILOT'S CONTROL COLUMN. REPAIRED IAW DC-9 SRM 53-21-0, FIGURE 2B. 2 L 7 2 4F A6WE 1996071000128 19960710 00128 WP 1996 7 10 ABXA9600561 1 19960523 A 5753 99576003 BRACKET DOUG DC9 DC931 3022065 WP RT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK INSPECTION, FOUND RIGHT FLAP BRACKETS CRACKED AT STA 353. REPLACED IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 1996071000129 19960710 00129 WP 1996 7 10 ABXA9600562 1 19960523 A 5753 99576007 BRACKET DOUG DC9 DC931 3022065 WP RT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK INSPECTION, FOUND RIGHT FLAP BRACKETS CRACKED AT STA 353. REPLACED IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 1996071000130 19960710 00130 WP 1996 7 10 ABXA9600563 1 19960522 A 5510 9918401171 SCRAPER DOUG DC9 DC931 3022065 WP HORIZ STAB WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER TRAILING EDGE ICE SCRAPER HAD A HOLE IN IT. REPAIRED IAW D C-9 SRM 55-01 FIGURE 2, SHEET 2. 2 L 7 2 4F A6WE 1996071000131 19960710 00131 WP 1996 7 10 ABXA9600564 1 19960530 A 5320 9915558239 BULKHEAD DOUBLER DOUG DC9 DC931 3022065 WP AFT FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK INSPECTION, FOUND CRACKED AFT PRESSURE BULKHEAD STIFFENER DOUBLER BETWEEN LONGERONS 15L AND 16L. REPLACE D IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 1996071000132 19960710 00132 WP 1996 7 10 ABXA9600565 1 19960524 A 5312 9915558236 BULKHEAD CLIP DOUG DC9 DC931 3022065 WP AFT FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK INSPECTION, FOUND AFT PRESSURE BULKHEAD STIFFENER ATTACH CLIP CRACKED AT LONGERON 14R. REPLACED IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 1996071000134 19960710 00134 WP 1996 7 10 ABXA9600567 1 19960524 A 5330 592032339 SKIN DOUG DC9 DC931 3022065 WP BS 332 GOUGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK INSPECTION, FOUND GOUGE IN THE FUSELAGE SKIN AT STATION 332, LONGERON 23R. REPAIRED IAW ABX REA D953-153 70-MR. 2 L 7 2 4F A6WE 1996071000135 19960710 00135 WP 1996 7 10 ABXA9600568 1 19960612 A 5753 99576007 FITTING DOUG DC9 DC931 3022065 WP LT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK INSPECTION, FOUND ATTACH FITTINGS INSIDE THE LEFT FLAP CRACKED. REPLACED IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 1996071000136 19960710 00136 WP 1996 7 10 ABXA9600570 1 19960611 A 5711 5911300501 SPAR DOUG DC9 DC931 3022065 WP LT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK INSPECTION, FOUND CORROSION ON THE LEFT WING UPPER SPAR. REPAIRED IAW ABX REA D957-15400-MR. 2 L 7 2 4F A6WE 1996071000137 19960710 00137 WP 1996 7 10 ABXA9600571 1 19960611 A 5711 5911301501 SPAR DOUG DC9 DC931 3022065 WP LT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK INSPECTION, FOUND CORROSION ON THE LEFT WING LOWER SPAR. REPAIRED IAW ABX REA D957-15400-MR. 2 L 7 2 4F A6WE 1996071000138 19960710 00138 WP 1996 7 10 ABXA9600572 1 19960530 A 5330 59525624 SKIN DOUG DC9 DC931 3022065 WP BS 996 - 1019 OIL CANNING A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN OIL CANNING BELOW THE NR 2 PYLON AT STA 996 TO 1019. REPAIRED IAW ABX RE A D953-15411-MR. 2 L 7 2 4F A6WE 1996071000139 19960710 00139 WP 1996 7 10 ABXA9600573 1 19960615 A 5720 99193497 TEE CAP DOUG DC9 DC931 3022065 WP WS 69 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK INSPECTION, FOUND CORROSION ON STA XRS 69 T-CAP IN THE LEFT WING. REPAIRED IAW ABX REA D957-15418-MR. 2 L 7 2 4F A6WE 1996071000140 19960710 00140 WP 1996 7 10 ABXA9600574 1 19960530 A 5312 5910130373 BULKHEAD DOUBLER DOUG DC9 DC931 3022065 WP BS 996 DOUBLE DRILLED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK INSPECTION, FOUND A DOUBLE DRILLED HOLE ON THE AFT PRESSURE BULKHEAD ABOVE THE RIGHT UPPER CORNER OF THE VENTRAL DOOR. REPAIRED IAW ABX REA D953-15423-MR. 2 L 7 2 4F A6WE 1996071000141 19960710 00141 WP 1996 7 10 ABXA9600575 1 19960605 A 5311 99196181 FRAME DOUG DC9 DC931 3022065 WP BS 718 ELONGATED HOLES A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK INSPECTION, FOUND HOLES ELONGATED ON THE FRAMES AT STA 718 LEFT AND RIGHT. REPAIRED IAW ABX REA D953-154 34-MR. 2 L 7 2 4F A6WE 1996071000142 19960710 00142 WP 1996 7 10 ABXA9600576 1 19960605 A 5311 99196182 FRAME DOUG DC9 DC931 3022065 WP BS 718 ELONGATED HOLES A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK INSPECTION, FOUND HOLES ELONGATED ON THE FRAMES AT STA 718 LEFT AND RIGHT. REPAIRED IAW ABX REA D953-154 34-MR. 2 L 7 2 4F A6WE 1996071000143 19960710 00143 WP 1996 7 10 ABXA9600577 1 19960605 A 5713 59192372 STRINGER DOUG DC9 DC931 3022065 WP RT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK INSPECTION, FOUND STRINGER NR 12 IN THE RIGHT WING CORRODED. REPAIRED IAW ABX REA D957-15435-MR. 2 L 7 2 4F A6WE 1996071000144 19960710 00144 WP 1996 7 10 ABXA9600578 1 19960416 A 5313 591140617 LONGERON DOUG DC9 DC941 302207N WP BS 200 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX 47499 DURING C-CHECK INSPECTION, FOUND LONGERON 4L CRACKED AT STA 200. REPAIRED IAW DC-9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1996071000145 19960710 00145 WP 1996 7 10 ABXA9600579 1 19960416 A 5313 591140617 LONGERON DOUG DC9 DC941 302207N WP BS 160 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX 47499 DURING C-CHECK INSPECTION, FOUND LONGERON 4L CRACKED AT STA 160. REPAIRED IAW DC-9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1996071000146 19960710 00146 WP 1996 7 10 ABXA9600580 1 19960412 A 5730 99574992 PANEL DOUG DC9 DC941 302207N WP RT WING DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX 47499 DURING C-CHECK INSPECTION, FOUND PANEL 1604 DELAMINATED ON THE RIGHT WING. REPLACED PANEL IAW DC-9 SRM 51-30-1 AND 51-3 0-2. 2 L 7 2 4F A6WE 1996071000147 19960710 00147 WP 1996 7 10 ABXA9600581 1 19960424 A 5320 99155613 WEB DOUG DC9 DC941 302207N WP BS 1072 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX 47499 DURING C-CHECK INSPECTION, FOUND CORROSION AT STA 1072 IN THE AFT LOWER CARGO COMPARTMENT. REPAIRED IAW ABX REA D953-15 067-MR. 2 L 7 2 4F A6WE 1996071000148 19960710 00148 WP 1996 7 10 ABXA9600582 1 19960424 A 5320 991556153 WEB DOUG DC9 DC941 302207N WP BS 1072 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX 47499 DURING C-CHECK INSPECTION, FOUND CORROSION AT STA 1072 IN THE AFT LOWER CARGO COMPARTMENT. REPAIRED IAW ABX REA D953-15 067-MR. 2 L 7 2 4F A6WE 1996071000149 19960710 00149 WP 1996 7 10 ABXA9600583 1 19960418 A 5313 591140613 LONGERON DOUG DC9 DC941 302207N WP BS 160 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX 47499 DURING C-CHECK INSPECTION, FOUND LONGERON 2L CRACKED AT STA 160. SPLICED LONGERON IAW DC-9 SRM 53-02, FIGURE 2. 2 L 7 2 4F A6WE 1996071000150 19960710 00150 WP 1996 7 10 ABXA9600584 1 19960607 A 5280 29242891 HINGE DOUG DC9 DC933F 302207A WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 934AX 47462 DURING COMPLIANCE OF AD 91-22-07, ASB 32-244 R2, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR HINGE WORN. REBUSHED HINGE IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1996071000151 19960710 00151 WP 1996 7 10 ABXA9600585 1 19960607 A 5280 591055741 HINGE DOUG DC9 DC933F 302207A WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 934AX 47462 DURING COMPLIANCE OF AD 91-22-07, ASB 32-244 R2, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR ARTICULATING DOOR HINGE WORN . REPLACED HINGE IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 1996071000152 19960710 00152 WP 1996 7 10 ABXA9600586 1 19960607 A 5280 29242891 BUSHING DOUG DC9 DC933F 302207A WP RT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 934AX 47462 DURING COMPLIANCE OF AD 91-22-07, ASB 32-244 R2, FOUND RIGHT MAIN LANDING GEAR OUTBOARD DOOR HINGE WORN. REBUSHED HINGE HALF IAW DC-9 OVERHAUL MANUAL 32-10-16. 2 L 7 2 4F A6WE 1996071000153 19960710 00153 WP 1996 7 10 ABXA9600587 1 19960615 A 5280 BLFR5112T2 BEARING DOUG DC9 DC941 302207N WP RT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 DURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND RIGHT MAIN LANDING GEAR DOOR ROD ASSEMBLY BEARING WORN. REPLACED BE ARING IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1996071000154 19960710 00154 WP 1996 7 10 ABXA9600588 1 19960702 A 3350 14597010 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 943AX 47528 UPON PREDEPARTURE CHECK, FOUND EMERGENCY LIGHTS OUT. REPLACED EMERGENCY LIGHT BATTERIES. 2 L 7 2 4F A6WE 1996071000155 19960710 00155 NM 1996 7 10 CALA9600949 1 19960701 A 5230 SEAL BOEING 737 737524 1384721 NM AFT CARGO DOOR LOOSE A CALA G O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 SW 09 37615 27328 CABIN PRESSURIZATION WAS LOST WHILE AT CRUISE. INITIAL ATTEMPTS TO CONTROL CABIN WITH STANDBY OR MANUAL WERE UNSUCCESSF UL. THE OXYGEN MASKS WERE DEPLOYED AND CABIN CONTROL WAS REGAINED USING MANUAL DC. THE ACFT LANDED WITHOUT FURTHER PRO BLEM. MAINTENANCE PRESSURIZED THE ACFT TO 5 PSI TWICE, ONCE IN AC MANUAL AND ONCE IN DC MANUAL. PRESSURIZATION WAS SUC CESSFUL. THE AFT CARGO DOOR SEAL WAS FOUND COMING LOOSE AT THE FORWARD LOWER CORNER. THE AFT CARGO DOOR SEAL WAS REMOV ED AND REPLACED. THE ACFT WAS PRESSURIZED AGAIN AND LEAK CHECK WAS GOOD. IT WAS OBSERVED THAT ALL OXYGEN MASKS HAD DEP LOYED. THE OXYGEN GENERATORS WERE REMOVED AND REPLACED IAW MM 35-22-11. 2 L 7 2 4F RT A16WE 1996071000156 19960710 00156 WP 1996 7 10 CALA9600950 1 19960620 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 37 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14534 47110 INSPECTION FOUND A 3.5 CRACK IN FORWARD ACCESSORY COMPARTMENT INTERCOSTAL AT STA 37. A NEW INTERCOSTAL WAS FABRICATED A ND INSTALLED IAW SRM 53-10-1. 2 L 7 2 4F A6WE 1996071000157 19960710 00157 WP 1996 7 10 CALA9600951 1 19960620 A 5210 BEAM DOUG DC9 DC932 3022066 WP CABIN DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14534 47110 INSPECTION FOUND A .5 CRACK IN FORWARD END OF MAIN CABIN DOOR NR 8 BEAM. A DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 31. 2 L 7 2 4F A6WE 1996071000158 19960710 00158 WP 1996 7 10 CALA9600952 1 19960613 A 5320 TEE CAP DOUG DC9 DC932 3022066 WP BS 110 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14534 47110 INSPECTION FOUND T-CAP CORRODED IN NOSE WHEEL WELL AT STA 110, LT SIDE. REPAIR DOUBLERS AND FILLER WERE FABRICATED AND INSTALLED IAW ECRA 5310-03289. 2 L 7 2 4F A6WE 1996071000159 19960710 00159 WP 1996 7 10 CALA9600953 1 19960612 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 160 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14534 47110 INSPECTION FOUND TWO 1 INCH CRACKS IN LONGERON 3L AT STA 160. THE LONGERON WAS REPAIRED IAW SRM 53-02. 2 L 7 2 4F A6WE 1996071000160 19960710 00160 WP 1996 7 10 CALA9600954 1 19960629 A 5350 CLIPS DOUG DC9 DC982 3022082 WP TAILCONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18835 49439 EXCESSIVE PULL WAS REQUIRED TO RELEASE TAILCONE EXTERIOR HANDLE FROM CLIPS. THE EXTERIOR HANDLE CLIPS WERE ADJUSTED IAW MM 53-53-00. 2 L 7 2 4F A6WE 1996071000161 19960710 00161 WP 1996 7 10 CALA9600955 1 19960629 A 5350 LATCHES DOUG DC9 DC982 3022082 WP TAILCONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18835 49439 THE PULL REQUIRED TO RELEASE TAILCONE USING THE EXTERIOR HANDLE WAS LOW. THE TAILCONE LATCHES WERE ADJUSTED IAW MM 53-5 3-10. 2 L 7 2 4F A6WE 1996071000162 19960710 00162 NM 1996 7 10 CALA9600956 1 19960630 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 1130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND THE FLOORBEAM CORRODED AT STA 1130, RBL 34 DURING FLIGHT PHONE INSTALLATION. THE FLOORBEAM WAS REPAIRE D IAW SRM 5310-03300. 2 L 7 3 4F A3WE 1996071000163 19960710 00163 WP 1996 7 10 CALA9600957 1 19960619 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP AFT SERV DR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18835 49439 INSPECTION FOUND FLOOR SUPPORT AT AFT SERVICE DOOR CORRODED. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-30-5 AND 51-10-3 . 2 L 7 2 4F A6WE 1996071000164 19960710 00164 WP 1996 7 10 CALA9600958 1 19960619 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP BS 180-195 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18835 49439 INSPECTION FOUND CORROSION ON FLOOR SUPPORT INBOARD OF FORWARD ENTRY DOOR AT STA 180 TO 195. A NEW FLOOR SUPPORT WAS FA BRICATED AND INSTALLED IAW SRM 51-10-1. 2 L 7 2 4F A6WE 1996071000165 19960710 00165 WP 1996 7 10 CALA9600959 1 19960702 A 3610 1555M14G04 DUCT DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 1 ENGINE SEPARATED A CALA O OTHER J WARNING INDICATION TO TAKEOFF 1 SW 09 14063 47864 530343 THE 1 ENGINE FIRE WARNING LIGHT ILLUMINATED ON TAKEOFF ROLL AT APPROXIMATELY 120 KNOTS. THE ENGINE FAIL/FIRE CHECKLIST WAS ACCOMPLISHED. THE FIRE LIGHT WENT OUT APPROXIMATELY 10 SECONDS AFTER RETARDING THE NR 1 THROTTLE. THE NR 1 ENGINE B-LOOP LIGHT WAS STILL ILLUMINATED. THE SYSTEM TESTED VALID WHEN SWITCHED TO A. MAINTENANCE FOUND THE NR 1 ENGINE HIGH STAGE PNEUMATIC DUCT SEPARATED WITH RESULTING DAMAGE TO BOTH THRUST REVERSER COWLS. REMOVED AND REPLACED THE PNEUMATIC DUCT, THE LT AND RT FAN REVERSERS. A POWER ASSURANCE RUN WAS PERFORMED, OPERATION CHECKED GOOD. 2 L 7 3 4F 4 F A22WE E23EA 1996071000166 19960710 00166 NM 1996 7 10 CALA9600960 1 19960703 A 5522 657278417J SKIN BOEING 727 727232 1384082 NM LT ELEVATOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND A 6 INCH CRACK ON LEFT ELEVATOR BOTTOM SKIN, INBOARD. THE LT ELEVATOR WAS REMOVED AND REPLACED IAW MM 27-30-1. AN ADJUSTMENT/TEST WAS PERFORMED ON ELEVATOR AND CONTROL TAB SYSTEM PER MM 27-30-0, PAGE 501 TO 532 AND OPERAT ION CHECKED GOOD. 2 L 7 3 4F A3WE 1996071000167 19960710 00167 NM 1996 7 10 CALA9600961 1 19960703 A 2761 ACTUATOR BOEING 737 737217 1384464 NM RT FLT SPOILER LEAKING A CALA O OTHER J K WARNING INDICATION FLUID LOSS DE DESCENT 1 SW 09 12231 19885 THE A-SYSTEM HYDRAULIC FLUID WAS LOST WHILE ON DESCENT INTO CHS. THE FLUID LOSS WAS ACCOMPANIED BY ILLUMINATION OF THE A-SYSTEM HYDRAULIC PUMP LIGHTS. THE LANDING GEAR WAS LOWERED MANUALLY AND THE FLAPS WERE EXTENDED ELECTRICALLY. THE AI RCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT INBOARD FLIGHT SPOILER ACTUATOR LEAKING. THE ACTUATOR WAS REM OVED AND REPLACED IAW MM 27-61-51. IN ADDITION, A SPOILER PRESSURE LINE IN RIGHT GEAR WELL WAS FOUND LEAKING. THE LINE WAS REPAIRED AND LEAK CHECK WAS GOOD. 2 L 7 2 4F A16WE 1996071000168 19960710 00168 WP 1996 7 10 CALA9600962 1 19960704 A 2913 41003106 HYD PUMP DOUG DC9 DC981 3022081 WP LT HYD SYST LEAKING A CALA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CL CLIMB 1 SW 09 14880 48044 THE LEFT HYDRAULIC SYSTEM QUANTITY DECREASED SHORTLY AFTER TAKEOFF FROM EWR. WHILE COMPLYING WITH ABNORMAL PROCEDURES T HE LT HYDRAULIC PRESSURE LOW LIGHT ILLUMINATED. THE LEFT HYDRAULIC PUMP AND TRANSFER PUMP WERE SECURED. THE AIRCRAFT W AS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC REVERSIBLE PUMP LEAKING. THE PUMP WAS REMOVED AND REPLACED PER MM 29-10-07, LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F A6WE 1996071000169 19960710 00169 NM 1996 7 10 CALA9600963 1 19960704 A 3260 434093003 CIRCUIT MODULE BOEING 757 757224 1384958 NM RT MLG IND INOPERATIVE A CALA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 SW 09 14102 27292 THE RT MAIN LANDING GEAR DOWN LIGHT DID NOT ILLUMINATE WHEN GEAR WAS EXTENDED ON APPROACH TO EWR. THERE WAS NO ASSOCIAT ED EICAS MESSAGE. THE APPROACH WAS ABORTED AND THE GEAR WAS CONFIRMED DOWN DURING A TOWER FLY-BY. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT MLG INDICATION CIRCUIT MODULE AT FAULT. THE CIRCUIT MODULE WAS REMOVED AND REPLACED. A SENSOR/TARGET BITE CHECK WAS PERFORMED ON THE PROXIMITY SWITCH ELECTRONICS UNIT AND NO DEFECTS WERE NOTED. 2 L 7 2 4F RT A2NM 1996071000170 19960710 00170 NM 1996 7 10 CALA9600964 1 19960704 A 2910 6517843328 HYD LINE BOEING 727 727243 138408D NM RT MLG WW LEAKING A A CALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 17407 21270 THE A-SYSTEM HYDRAULIC FLUID QUANTITY DECREASED FROM FOUR GALLONS TO .2 GALLONS DURING FLIGHT. THE GEAR AND FLAPS WERE LOWERED NORMALLY AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC A-SYSTEM RETURN LINE FROM WI NG TANK HEAT EXCHANGER TO RIGHT WHEEL WELL AFT BULKHEAD LEAKING. THE LINE WAS REPLACED USING FLEX LINE AND A DIP WAS IS SUED TO REPLACE THE LINE WITHIN 1200 HOURS OR 500 FLIGHTS, WHICHEVER COMES FIRST. THE HYDRAULIC SYSTEM WAS SERVICED TO FULL. 2 L 7 3 4F RT A3WE 1996071000171 19960710 00171 WP 1996 7 10 CKSA96063 1 19960629 A 2612 FIRE WIRE DOUG DC8 DC8F55 3021928 WP PWA JT3D JT3D3B 52039 NE NR 2 ENGINE BROKEN A CKSA O OTHER N FALSE WARNING DE DESCENT 1 GL 23 6161M 45762 669641 AT TOP OF DESCENT NR 2 ENGINE FIRE WARNING CAME ON. WHEN THROTTLE WAS RETARDED TO IDLE LIGHT WENT OUT. SYSTEM TESTED O K. LEFT ENGINE AT IDLE. REPAIRED BROKEN WIRE DOING FALSE CONTACT, OPS CHECK NORMAL ON GROUND, POWER RUN IAW MM CHAPTER 26-00. 2 L 7 4 4F 4 F 4A25 1E8 1996071000172 19960710 00172 SO 1996 7 10 COMA9610218 1 19960702 A 2751 FLAP WARNING EMB 120 EMB120RT SO COCKPIT ACTIVATED A COMA O OTHER N FALSE WARNING LD LANDING 1 SO 01 189CA 120189 FLAP CONTROL FAULT WARNING DURING LANDING ROLL. COULD NOT DUPLICATE DISCREPANCY. NO DEFECTS FOUND IN FLAP SYSTEM. 2 L 7 2 4T RT A31SO 1996071000173 19960710 00173 SW 1996 7 10 COMA9620011 1 19960702 A 2150 20475546 ACM SWRNGN SA227 SA227AC 8780603 SW LEFT FAILED A COMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 704C AC704 LIGHT SMOKE IN AIRCRAFT AND HOT AIR FROM AIR CONDITIONING VENTS. REPLACED THE LT AIR CYCLE MACHINE AND THE RT BLEED AIR CONTROL VALVE. 2 L 7 2 4T RT A8SW 1996071000174 19960710 00174 NM 1996 7 10 DL72K961463 1 19960309 A 5312 BULKHEAD WEB BOEING 727 727232 1384082 NM BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 491DA 21060 THE BS 1183 BULKHEAD WEB WAS FOUND CRACKED AT RBL 26. THERE IS A 1 INCH CRACK AT WL 166.5. REPAIRED PER ER/A 303276-14 . 2 L 7 3 4F A3WE 1996071000175 19960710 00175 NM 1996 7 10 DL72S961469 1 19960526 A 5312 BLKHD STIFFENER BOEING 727 727232 1384082 NM BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 522DA 21582 CRACKS WERE FOUND EMANATING FROM THE BOTTOM OF THE FLANGE ON THE VERTICAL STIFFENERS LOCATED AT THE BOTH LBL AND RBL 8. REPAIRED PER B727 S/B 727-53-0175, REV 2. 2 L 7 3 4F A3WE 1996071000176 19960710 00176 NM 1996 7 10 DL72S961470 1 19960522 A 5330 65C139132 SKIN BOEING 727 727232 1384082 NM BS 1044 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 537DA 22073 THE SKIN AT STA 1044 AND ST 28L WAS FOUND CORRODED. REPAIRED PER B727 SRM 53-30-3, FIGURE 3. 2 L 7 3 4F A3WE 1996071000177 19960710 00177 NM 1996 7 10 DL72S961471 1 19960518 A 5520 HINGE FTG BOEING 727 727232 1384082 NM LT ELEVATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 538DA 22076 THE REAR SPAR OF THE LT ELEVATOR WAS FOUND CRACKED ON THE I/B SIDE OF THE THIRD FROM O/B HINGE FITTING. MODIFIED PER B7 27 S/B 727-55-0087, REV 1. 2 L 7 3 4F A3WE 1996071000178 19960710 00178 NM 1996 7 10 DL72S961472 1 19960612 A 5330 65545905 SKIN BOEING 727 727232 1384082 NM BS 700 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 421DA 21274 FUSELAGE SKIN JUST AFT OF FUSELAGE STA 700 HAD CORROSION DAMAGE AT STRINGER 28L AND STR 28R. REPAIRED PER B727 SRM 53-3 0-3, FIGURE 1 IN ACCORDANCE WITH B727 S/B 727-53A0203, REV 2. 2 L 7 3 4F A3WE 1996071000179 19960710 00179 NM 1996 7 10 DL72S961473 1 19960612 A 5311 651632639 FRAME BOEING 727 727232 1384082 NM BS 784 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 523DA 21583 FOUND CRACK IN THE INBOARD FLANGE OF STA 784 FRAME JUST ABOVE THE MAIN CABIN FLOOR. REPAIRED PER B727 S/B 727-53-0197. 2 L 7 3 4F A3WE 1996071000180 19960710 00180 NM 1996 7 10 DL72S961482 1 19960619 A 3350 BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 539DA 22385 RT FWD OVERWING EMERGENCY LIGHT IS INOP. REPLACED BATTERY PACK (P/N 9008-3-58), (S/N 8751). 2 L 7 3 4F A3WE 1996071000181 19960710 00181 NM 1996 7 10 DL72S961484 1 19960522 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 1263 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 537DA 22073 FOUND A CRACK IN ANGLE OF THE FWD TRANSVERSE BEAM AND AFT CHANNEL OF THE RT TORQUE BOX AT FS 1263. REPAIRED PER DELTA E R/A 303623-14AD. 2 L 7 3 4F A3WE 1996071000182 19960710 00182 NM 1996 7 10 DL72S961485 1 19960618 A 5320 651751737 CHANNEL BOEING 727 727232 1384082 NM BS 1263 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 494DA 21074 FOUND A .875 INCH CRACK IN THE CHANNEL AT FS 1263. REPAIRED PER DELTA ER/A 303744-14AD. 2 L 7 3 4F A3WE 1996071000183 19960710 00183 NM 1996 7 10 DL72S961486 1 19960617 A 5330 65C139132 SKIN BOEING 727 727232 1384082 NM BS 1060 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 523DA 21583 FOUND CRACK AT STA 1060, ON STRINGER 28R. REPAIRED PER DELTA ER/A 303739-14. 2 L 7 3 4F A3WE 1996071000184 19960710 00184 NM 1996 7 10 DL72S961496 1 19960620 A 5320 WEB BOEING 727 727232 1384082 NM BS 1223 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 496DA 21076 ONE CRACK 48 SECTION TORQUE BOX WEB AT UPPER EDGE STA 1223 LT. REPAIRED PER M/M 53-11-0. 2 L 7 3 4F A3WE 1996071000185 19960710 00185 NM 1996 7 10 DL72S961497 1 19960620 A 5754 STIFFENER BOEING 727 727232 1384082 NM NR 3 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 496DA 21076 A 1.5 INCH CRACK WING FRONT SPAR VERTICAL STIFFENER AT NR 3 SLAT INBD TRACK CUTOUT. REPLACED SPAR STIFFENER PER M/M 57- 20-21. 2 L 7 3 4F A3WE 1996071000186 19960710 00186 NM 1996 7 10 DL72S961515 1 19960624 A 5320 WEB BOEING 727 727232 1384082 NM BS 1213 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 536DA 22049 A 1.25 IN CRACK IN TORQUE BOX WEB UPPER RT CORNER AT STA 1213 AT UPPER CORD. INSTALLED DOUBLER PER MM 53-11-0 PG 832. 2 L 7 3 4F A3WE 1996071000187 19960710 00187 NM 1996 7 10 DL72S961528 1 19960625 A 5754 RIB BOEING 727 727232 1384082 NM NR 6 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 404DA 21148 FOUND A .5 INCH CRACK IN RADIUS OF NOSE RIB INBD SIDE OF INBD TRACK, NR 6 SLAT. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1996071000188 19960710 00188 NM 1996 7 10 DL72S961529 1 19960611 A 5320 ANGLE BOEING 727 727232 1384082 NM FWD CARGO CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 523DA 21583 FOUND CORROSION AT ANGLE UNDER AND AROUND THE HINGES FOR PANEL 3348. REPAIRED PER MM 53-30-1, PG 807 TO 808. 2 L 7 3 4F A3WE 1996071000189 19960710 00189 NM 1996 7 10 DL72S961532 1 19960626 A 2730 PWR CONTL UNIT BOEING 727 727232 1384082 NM ELEVATOR MALFUNCTIONED A DALA O OTHER F FLT CONT AFFECTED CL CLIMB 1 SO 27 541DA 22387 A/C PORPOISED AND VIBRATES ON CLIMB/CRUISE WITH A/P OFF. FEELS LIKE THERE IS PLAY IN CONTROL COLUMN IN PITCH. CONTROL COLUMN KICKS BACK OCCASIONALLY. REPLACED ELEVATOR POWER CONTROL UNIT, PERFORMED AUTO-PILOT AUTH CHECK, ALL INDICATIONS NORMAL. 2 L 7 3 4F A3WE 1996071000190 19960710 00190 NM 1996 7 10 DL72S961537 1 19960626 A 5520 DOUBLER BOEING 727 727232 1384082 NM RT ELEVATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 545DA 22494 PREVIOUS DOUBLER CRACKED 1.5 INCH AT FASTENER. LOWER RT ELEVATOR I/B END. REPAIRED PER SRM 55-20-3 FIG 4. 2 L 7 3 4F A3WE 1996071000191 19960710 00191 NM 1996 7 10 DL72W961468 1 19960524 A 5330 6554590 SKIN BOEING 727 727247 138408F NM BS 700 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2809W 20581 THE SKIN JUST FWD OF STA 700 BETWEEN STR 28L AND 28R NEAR BL 0 WAS FOUND CRACKED AND CORRODED. REPAIRED WITH A DOUBLER AND TRIPLER PER FAA/DER FORM 8110-3, DER DESIGNATION SO-9-57. 2 L 7 3 4F A3WE 1996071000192 19960710 00192 NM 1996 7 10 DL72W961488 1 19960523 A 5312 BULKHEAD BOEING 727 727247 138408F NM BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2813W 20869 A .5 INCH CRACK WAS FOUND IN THE 1183 BULKHEAD AT RBL 8 AND WL 172. REPAIRED PER DELTA ER/A 303629-14AD. 2 L 7 3 4F A3WE 1996071000193 19960710 00193 NM 1996 7 10 DL72W961489 1 19960522 A 5320 651751737 CHANNEL BOEING 727 727247 138408F NM FS 1263 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2813W 20869 FOUND A CRACK IN THE ANGLE OF THE FWD TRANSVERSE BEAM AND AFT CHANNEL OF THE RT TORQUE BOX AT FS 1263. REPAIRED PER DEL TA ER/A 303628-14AD. 2 L 7 3 4F A3WE 1996071000194 19960710 00194 NM 1996 7 10 DL72W961509 1 19960622 A 3350 LIGHT BOEING 727 727247 138408F NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2807W 20579 R2 ABOVE DOOR EXIT EMERGENCY LIGHT INOP. REPLACED EXIT LIGHT AND BATTERIES, CKS NORMAL. 2 L 7 3 4F A3WE 1996071000195 19960710 00195 NM 1996 7 10 DL72W961518 1 19960624 A 3350 81 BULB BOEING 727 727247 138408F NM AFT RT SLIDE FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2819W 21057 ON LAYOVER, FOUND RIGHT AFT SLIDE LIGHT INOP. RELAMPED SAME, CHECKS GOOD. 2 L 7 3 4F A3WE 1996071000196 19960710 00196 NM 1996 7 10 DL72W961520 1 19960624 A 5210 DOOR BOEING 727 727247 138408F NM R1 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2807W 20579 THE R-1 DOOR WAS FOUND CRACKED AT THE UPPER FWD CORNER. REPAIRED PER 52-12-0, FIG 805. 2 L 7 3 4F A3WE 1996071000197 19960710 00197 NM 1996 7 10 DL733961531 1 19960626 A 2600 FIRE WIRE BOEING 737 737347 1384647 NM NR 2 ENGINE SHORTED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 27 305WA 23346 AT 100 KTS ON T/O ROLL, FIRE DETECTOR FAULT LIGHT CAME ON ABORTED T/O. REPAIRED SHORTED FIRE WARNING WIRE IN CORE SECTI ON OF NR 2 ENG NEAR D1208-B-LOOP. 2 L 7 2 4F RT A16WE 1996071000198 19960710 00198 NM 1996 7 10 DL73S961536 1 19960627 A 7430 IGNITION WIRES BOEING 737 737232 1384475 NM COCKPIT FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 322DL 23094 WHEN STOWING STBY COMPASS INSTRUMENT ARCED ACCOMPANIED BY A TRACE OF SMOKE AND ELECTRICAL SMELL. FOUND WIRES IN IGNITIO N SWITCH FOR NR 1 ENGINE BURNED AND MAKING CONTACT WITH STANDBY COMPASS. REPAIRED ALL WIRES, OPS CHECK NORMAL. 2 L 7 2 4F RT A16WE 1996071000199 19960710 00199 NM 1996 7 10 DL757961417 1 19960612 A 3350 767 BULB BOEING 757 757232 1384965 NM 3L DOOR FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 626DL 22916 3L DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED SAME, OP CK GOOD. 2 L 7 2 4F RT A2NM 1996071000200 19960710 00200 NM 1996 7 10 DL757961447 1 19960616 A 3350 767 BULB BOEING 757 757232 1384965 NM L-4 DOOR FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 615DL 22822 L-4 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE DURING TEST. RELAMPED LIGHT ASSEMBLY AND OPERATION NOW NORMAL DURING TEST . 2 L 7 2 4F RT A2NM 1996071000201 19960710 00201 NM 1996 7 10 DL757961476 1 19960616 A 5414 311N3450 SKIN BOEING 757 757232 1384965 NM NR 2 ENGINE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 636DL 23763 THE NR 2 ENGINE NACELLE STRUT SKIN WAS FOUND CRACKED JUST AFT OF NAC 107.7 ON THE I/B SIDE. THE CRACK WAS 1.5 INCH LONG AND EMANATES FROM THE UPPER FWD CORNER OF AN ACCESS HOLE BTW BULKHEADS AT STA 107.700 AND 116.050. THIS ER/A AUTHORIZE S THE CRACK TO BE STOP DRILLED AND INSPECTED ON A TIME LIMITED BASIS. THE PERMANENT REPAIR WILL BE ACCOMPLISHED AT NEXT HMV. THE REPAIR IS ACCOMPLISHED IN ACCORDANCE WITH BAC TWX DAL-ATL-93-1337RR, DTD 04 DEC 93, B757 SRM 54-51-01, FIG 20 3 AND 204. 2 L 7 2 4F RT A2NM 1996071000202 19960710 00202 NE 1996 7 10 DL757961501 2 19960621 A 7230 COMPRESSOR FAN BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 ENGINE BIRD STRIKE A DALA A UNSCHED LANDING C F.O.D. CL CLIMB 1 SO 27 647DL 24218 716303 RT ENG FAILED AT APPROX 800 FT DUE TO INGESTION OF LARGE BIRD. REQUIRES ENG CHANGE, HEAVY FAN AND NOSE COWL DAMAGE. 2 L 7 2 4F 4 F RT A2NM E17NE 1996071000203 19960710 00203 NM 1996 7 10 DL757961502 1 19960621 A 3350 LIGHT BOEING 757 757232 1384965 NM L2 DOOR FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 601DL 22808 L-2 EXTERIOR EMERGENCY LIGHT FAILED TO ILLUMINATE ON SYSTEM TEST. RELAMPED LIGHT ASSY, NOW CKS NORMAL. 2 L 7 2 4F RT A2NM 1996071000204 19960710 00204 NE 1996 7 10 DL757961504 2 19960622 A 7250 TURBINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 ENGINE DAMAGED A DALA O OTHER X ENGINE FLAMEOUT LD LANDING 1 SO 27 657DL 24419 716527 NR 1 ENG TURBINE SECTION DAMAGED. 2 L 7 2 4F 4 F RT A2NM E17NE 1996071000205 19960710 00205 NM 1996 7 10 DL757961521 1 19960624 A 3350 OL3071BP BULB BOEING 757 757232 1384965 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 674DL 25979 EMERGENCY TRACK LIGHT AT ROW 39 INOP DURING MAINTENANCE TEST. RELAMPED AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A2NM 1996071000206 19960710 00206 NM 1996 7 10 DL757961522 1 19960624 A 3350 OL3071BP BULB BOEING 757 757232 1384965 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 674DL 25979 EMERGENCY TRACK LIGHT AT ROW 34 INOP DURING MAINTENANCE TEST. RELAMPED AND INSTALLED A NEW LENS, OPERATION NOW NORMAL. 2 L 7 2 4F RT A2NM 1996071000207 19960710 00207 NM 1996 7 10 DL767961449 1 19960617 A 2150 32027261 CHECK VALVE BOEING 767 767232 1385132 NM RT PACK INOPERATIVE A A DALA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 SO 27 110DL 22222 AFTER T/O, A/C WOULD NOT COOL. HOT AIR ENTERED PASSENGER CABIN AND COCKPIT UNABLE TO STOP HOT AIR ISOLATED BOTH SIDES, NO HELP. REPLACED RT PACK TRIM AIR CK VALVE (P/N 211102808) (MFG/NR 3202726-1) (S/N 2347). 2 L 7 2 4F RT A1NM 1996071000208 19960710 00208 NM 1996 7 10 DL767961519 1 19960624 A 3397 MILW227591618 WIRE BOEING 767 767232 1385132 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 101DA 22213 AFT GALLEY EMERGENCY TRACK LIGHTS ARE OUT. REPAIRED BROKEN WIRE ON TRACK, CHECKS GOOD. 2 L 7 2 4F RT A1NM 1996071000209 19960710 00209 NM 1996 7 10 DL76L961525 1 19960625 A 2710 CONTROL CABLE BOEING 767 767332 1382001 NM AILERON BROKEN A DALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 27 185DN 27961 ON CLIMBOUT THROUGH 5000 FT, LOST RIGHT GENERATOR. NO EICAS MESSAGES. ALMOST CONCURRENT WITH GEN LOSS, EXPERIENCED LEF T AILERON HARD OVER WITH NO ASSOCIATED EICAS CAUTION OR STATUS MESSAGE. REPLACED A2B-3 AILERON CONTROL CABLE. 2 L 7 2 4F RT A1NM 1996071000210 19960710 00210 NM 1996 7 10 DL76S961534 1 19960626 A 3350 LIGHT BOEING 767 767332 1382001 NM OVERWING EXIT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 128DL 24078 LEFT AFT EMERGENCY OVERWING LIGHT INOP. RELAMPED LEFT AFT EMERGENCY LIGHT, CHECKS GOOD. 2 L 7 2 4F RT A1NM 1996071000211 19960710 00211 WP 1996 7 10 DLL10961446 1 19960616 A 3350 POWER SUPPLY LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 735D 193C1226 F/C EMERGENCY TRACK LIGHTS INOP. REPLACED POWER SUPPLY ASSBLY. FOUND DURING ROUTINE CHECK ON NR 2 SERVICE CHECK. 2 L 7 3 4F A23WE 1996071000212 19960710 00212 WP 1996 7 10 DLL10961477 1 19960606 A 5730 SKIN LKHEED 1011 10113851 5265010 WP RIGHT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 721DA 193C1139 DURING LETTER CHECK, THE LOWER WING SKIN ON THE RT WING AT STR 18 RUNOUT WAS FOUND CRACKED. CRACK WAS REPAIRED PER DAL EO 7-70043-3. 2 L 7 3 4F A23WE 1996071000213 19960710 00213 WP 1996 7 10 DLL10961478 1 19960606 A 5311 FRAME LKHEED 1011 10113851 5265010 WP BS 629/1605/1645 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 721DA 193C1139 DURING LETTER CHECK, CRACKS WERE FOUND AT WL 280.6. THE CRACKS WERE REPAIRED PER SI 7-69003-12AD. 2 L 7 3 4F A23WE 1996071000214 19960710 00214 WP 1996 7 10 DLL10961507 1 19960623 A 2150 PACK LKHEED 1011 10113851 5265010 WP NR 2 PACK ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 735D 193C1226 ON DESCENT, ALL AFT LAV SMOKE DETECTORS SOUNDED. ALCOHOL LIKE SMELL REPORTED BY F/A. MAINT RESET AND CHECKED LAV SMOKE DETECTORS. SUSPECT NR 2 PACK AS CAUSE WHEN POWER REDUCED. 2 L 7 3 4F A23WE 1996071000215 19960710 00215 WP 1996 7 10 DLL10961510 1 19960623 A 3350 LIGHT LKHEED 1011 10113851 5265010 WP EXTERIOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 725DA 193C1162 EXTERIOR LIGHT AT L3 DOOR INOP. 2 L 7 3 4F A23WE 1996071000216 19960710 00216 WP 1996 7 10 DLL10961511 1 19960623 A 3350 LIGHT LKHEED 1011 10113851 5265010 WP EXTERIOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 725DA 193C1162 EXTERIOR LIGHT AT L4 DOOR INOP. RELAMPED, CK GOOD. 2 L 7 3 4F A23WE 1996071000217 19960710 00217 NE 1996 7 10 DLL10961512 2 19960624 A 7261 OIL PUMP PACKING LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B02 54555 NE NR 2 ENGINE FAILED A DALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DE DESCENT 1 SO 27 735D 193C1226 10427 FLT ATTENDENTS REPORTED SMOKE AND HAZE IN CABIN ON APPROACH. AFT LAV SMOKE DET WENT OFF. REPLACED OIL PUMP PACKING, CK S GOOD. 2 L 7 3 4F 4 F A23WE E12EU 1996071000218 19960710 00218 WP 1996 7 10 DLL13961426 1 19960613 A 3350 LIGHT LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 782DL 193A1006 14874 EMERGENCY TRACK LIGHTING AT 31 H/J INOP. RELAMPED AND REPLACED CAPS. 2 L 7 3 4F A23WE 1996071000219 19960710 00219 WP 1996 7 10 DLL13961508 1 19960623 A 2530 OVEN LKHEED 1011 10113851 5265010 WP GALLEY FIRE A DALA F ACTIVATE FIRE EXT. A FLAME/FIRE CR CRUISE 1 SO 27 786DL 193A1123 CUP COVERING EGGS IN OVEN CAUGHT FIRE IN NR 1 OVEN. FIRE EXT WITH HALON EXT. 2 L 7 3 4F A23WE 1996071000220 19960710 00220 NM 1996 7 10 DLM11961441 1 19960615 A 3350 6044113 BATTERY PACK DOUG MD11 MD11 3023602 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 812DE 48601 14874 BATTERY PACK NR 6 FAILED PWR UP TEST. REPLACED BATTERY PACK, TEST OK. 2 L 7 3 4F RT A22WE 1996071000221 19960710 00221 NM 1996 7 10 DLM90961530 1 19960626 A 3320 LIGHT WIRES DOUG MD90 MD9030 3023690 NM AFT GALLEY FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 911DA 53391 BRIEF SPARKS, NO ACTUAL FIRE, ABOVE BALLAST IN CEILING AT AFT LEFT GALLEY. AREA WAS COOL TO TOUCH. FOUND SIXTEEN BURNE D WIRES. REPAIRED ALL WIRES, ALL LIGHTS OPS CHECK. 2 L 7 2 4F RT A6WE 1996071000222 19960710 00222 WP 1996 7 10 MWEA96256 1 19960703 A 3350 60030431 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 202ME 47672 DURING SERVICE CHECK, FOUND EMERGENCY CEILING LIGHTS, ROW 4 TO 9 INOP. REPLACED CEILING BATTERY POWER SUPPLY, OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996071000223 19960710 00223 NM 1996 7 10 P5CA9600303 1 19960701 A 5321 FLOOR PANEL BOEING 747 747132 1384882 NM AFT CARGO COMPT DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 FOUND AFT CARGO COMPARTMENT RIGHT HAND WALKWAY HAS A HOLE JUST FWD OF ENTRY DOOR. REPAIRED HOLE IN CARGO FLOOR IAW SRM 51-40-02. 2 L 7 4 4F A20WE 1996071000224 19960710 00224 NM 1996 7 10 P5CA9600304 1 19960701 A 3610 DUCT CLAMP BOEING 747 747132 1384882 NM NR 1 ENGINE BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 NR 1 ENGINE STARTER PNEUMATIC DUCT HAS A BROKEN 'V' BAND CLAMP AT STARTER. REMOVED AND REPLACED 'V' CLAMP AT STARTER IA W MM 36-11-01. 2 L 7 4 4F A20WE 1996071000225 19960710 00225 NM 1996 7 10 P5CA9600305 1 19960701 A 5730 ACCESS PANEL BOEING 747 747132 1384882 NM RT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 FOUND LOWER RIGHT WING ACCESS PANEL DELAMINATED JUST OUTBOARD OF NR 5 FLAP TRACK FAIRING. REMOVED DAMAGED AREA AND APPL IED FIBERGLASS OVERLAYS IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1996071000226 19960710 00226 NM 1996 7 10 P5CA9600306 1 19960701 A 5730 PANEL BOEING 747 747132 1384882 NM LT WING L/E ERODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 FOUND TOP OF LEFT WING ERODED ALONG LEADING EDGE OF FIBERGLASS PANELS, SEVERAL AREAS AT LEADING EDGE OF WING. REPAIRED LEADING EDGE IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1996071000227 19960710 00227 NM 1996 7 10 P5CA9600307 1 19960701 A 3610 PRECOOLER BOEING 747 747132 1384882 NM NR 2 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 FOUND NR 2 ENGINE PRECOOLER CRACKED AT FORWARD LOWER INBOARD CORNER. REMOVED WELD REPAIR IAW BAC 5975, USING 34755 TIG ROD AND REPLACED SAME. LEAK CHECKED ENGINE IAW MM 36-21-01. 2 L 7 4 4F A20WE 1996071000228 19960710 00228 NM 1996 7 10 P5CA9600308 1 19960701 A 5230 SHIELD BOEING 747 747132 1384882 NM AFT CARGO DOOR BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 FOUND AFT CARGO DOOR AFT FIBERGLASS SHIELD FOR PRESSURE DOOR BROKEN AWAY. INSTALLED NEW SHIELD IAW MM 52-34-00. 2 L 7 4 4F A20WE 1996071000229 19960710 00229 NM 1996 7 10 P5CA9600309 1 19960701 A 5321 FLOOR PANEL BOEING 747 747132 1384882 NM CARGO COMPT PUNCTURED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 FOUND HOLE IN BULK CARGO PIT AT FORWARD RIGHT HAND END. REPAIRED HOLE IN FLOOR IAW SRM 51-40-02. 2 L 7 4 4F A20WE 1996071000230 19960710 00230 NE 1996 7 10 P5CA9600310 2 19960701 A 7260 CHIP DETECTOR BOEING 747 747132 1384882 NM PWA JT9 JT9D7A 52054 NE NR 3 ENGINE BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 662376 FOUND NR 3 ENGINE ANGLE GEARBOX CHIP DETECTOR BROKEN. REPLACED CHIP DETECTOR IAW MM 72-61-01. 2 L 7 4 4F 4 F A20WE E20EA 1996071000231 19960710 00231 NM 1996 7 10 P5CA9600311 1 19960701 A 5280 CHANNEL BOEING 747 747132 1384882 NM RT MLG DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 FOUND RIGHT HAND BODY GEAR FLYING DOOR AFT ATTACH HINGE AND BOLTS LOOSE AND STRUCTURE CRACKED. REMOVED DOOR, FABBED NEW CHANNEL, INSTALLED IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996071000232 19960710 00232 NM 1996 7 10 P5CA9600312 1 19960701 A 2550 ROLLER TRAY BOEING 747 747132 1384882 NM BS 1800 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 AT APPROX STA 1800 FOUND 2 ROLLER TRAYS CRACKED, RBL 30 AND RBL 48. REMOVED AND REPLACED CRACKED TRAYS IAW SRM 51-30-02 . 2 L 7 4 4F A20WE 1996071000233 19960710 00233 NM 1996 7 10 P5CA9600313 1 19960701 A 2550 RAIL SUPPORT BOEING 747 747132 1384882 NM BS 560 TORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 FOUND FORWARD CARGO COMPARTMENT SIDE RAIL SUPPORT TORN AT STA 560. REMOVED AND REPLACED SUPPORT IAW SRM 51-30-02 AND 51 -10-01. 2 L 7 4 4F A20WE 1996071000234 19960710 00234 NM 1996 7 10 P5CA9600314 1 19960701 A 5753 SKIN BOEING 747 747132 1384882 NM LT TE MIDFLAP LOOSE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEFT WING INBOARD FLAP MIDFLAP LOWER SURFACE HAS FILLER PULLING LOOSE INBOARD OF INBOARD CANOE. REMOVED DAMAGED AREA, P OTTED SAME AND APPLIED FIBERGLASS OVERLAYS IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996071000235 19960710 00235 NM 1996 7 10 P5CA9600315 1 19960701 A 5753 SKIN BOEING 747 747132 1384882 NM LT TE MIDFLAP LOOSE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEFT WING INBOARD FLAP MID FLAP FIBERGLASS PEELING LOOSE ON LOWER SURFACE AT FRONT SPAR APPROX 2 FEET FROM INBOARD END. REMOVED DAMAGED AREA, POTTED SAME AND APPLIED FIBERGLASS OVERLAYS IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996071000236 19960710 00236 NM 1996 7 10 P5CA9600316 1 19960701 A 5320 SUPPORT BOEING 747 747132 1384882 NM CARGO COMPT BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 AFT CARGO COMPARTMENT LEFT SIDE FORWARD FRAME SUPPORTS ARE BROKEN AWAY FROM FRAME ON ANGLED SIDEWALL. REMOVED AND REPLA CED TENSION STRAP SUPPORTS IAW SRM 51-30-03. 2 L 7 4 4F A20WE 1996071000237 19960710 00237 NM 1996 7 10 P5CA9600317 1 19960701 A 5350 FAIRING BOEING 747 747132 1384882 NM RT PACK DOOR MISSING A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 RIGHT HAND PACK LOUVER DOOR ACCESS PANEL SECTION OF FAIRING MISSING AT FORWARD INBOARD END OF DOOR. INSTALLED NEW FAIRI NG IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996071000238 19960710 00238 NM 1996 7 10 P5CA9600318 1 19960701 A 5330 ACCESS PANEL BOEING 747 747132 1384882 NM FUSELAGE DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 FOUND HOLE IN FUSELAGE ACCESS PANEL FORWARD OF RIGHT HAND PACK LOUVER DOOR. REMOVED DAMAGED AREA, POTTED SAME AND APPLI ED DOUBLERS IAW SRM 51-40-02. 2 L 7 4 4F A20WE 1996071000239 19960710 00239 NM 1996 7 10 P5CA9600319 1 19960701 A 5320 DOOR CUTOUT BOEING 747 747132 1384882 NM BULK CARGO DOOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 INSPECTION OF BULK CARGO DOOR CUTOUT REVEALED EVIDENCE OF LEVEL 2 CORROSION AT AFT LOWER CORNER. REMOVED EXISTING DOUBL ER AND SKIN, FABRICATED FILLER AND TRIPLER, INSTALLED SAME, ALL IAW POLAR AIR CARGO MAINTENANCE AUTHORIZATION 5330-07:01 . PERFORMED HFEC INSPECTION TO ASSURE STRUCTURE CORROSION AND DAMAGE FREE IAW SRM 51-10-01. 2 L 7 4 4F A20WE 1996071000240 19960710 00240 NM 1996 7 10 P5CA9600320 1 19960701 A 2550 LINING BOEING 747 747132 1384882 NM CARGO COMPT DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 BULK CARGO INTERIOR CORNER DAMAGED AT FORWARD LOWER SIDE OF OPENING. REPAIRED DOOR CORNER IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996071000241 19960710 00241 NM 1996 7 10 P5CA9600321 1 19960701 A 5400 FAIRING BOEING 747 747132 1384882 NM NR 3 PYLON MISSING TIP A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 NUMBER 3 ENGINE FORWARD FAIRING LEADING EDGE TIP IS MISSING. REPLACED MISSING TIP IAW MM 54-51-01. 2 L 7 4 4F A20WE 1996071000242 19960710 00242 NM 1996 7 10 P5CA9600322 1 19960702 A 3246 260356115 TIRE BOEING 747 747123 1384873 NM NR 9 WHEEL RUPTURED A P5CA K NONE O OTHER TX TAXI/GRND HDL 1 WP 23 859FT 20326 NUMBER 9 MAIN TIRE RUPTURED DURING TAXI INTO GATE. REMOVED AND REPLACED NR 9 TIRE IAW MM 32-45-01, REPLACED NR 10 AS PR ECAUTIONARY IAW MM 32-45-01. FUSELAGE, WHEEL WELLS AND GEAR DOORS INSPECTED PER BURST TIRE INSPECTION, MM 05-51-34, SAT ISFACTORY. NO EVIDENCE OF FLAT SPOTTING OR LOCKED BRAKES. 2 L 7 4 4F A20WE 1996071000243 19960710 00243 NM 1996 7 10 P5CA9600323 1 19960701 A 5320 DOOR CUTOUT BOEING 747 747132 1384882 NM CARGO COMPT CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 INSPECTION OF THE AFT CARGO DOOR CUTOUT REVEALED LEVEL 2 CORROSION AT THE AFT LOWER CORNER. REMOVED EXISTING FASTENERS AND SKIN, FABRICATED FILLER AND DOUBLER, INSTALLED REPAIR PARTS IAW POLAR AIR CARGO MAINTENANCE AUTHORIZATION 5330-08:01 . PERFORMED HFEC INSPECTION TO ASSURE STRUCTURE CORROSION AND DAMAGE FREE IAW SRM 51-10-01. 2 L 7 4 4F A20WE 1996071000244 19960710 00244 NM 1996 7 10 P5CA9600324 1 19960701 A 7110 FRAME BOEING 747 747132 1384882 NM NR 2 ENGINE COWL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 NR 2 ENGINE INBOARD CORE COWL LOWER FRAME CRACKED AND TORN AT NR 5 LATCH U-BOLT, GUIDE PIN PUSHED BACK. REMOVED AND REP LACED SECTION OF FRAME IAW SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1996071000245 19960710 00245 NM 1996 7 10 P5CA9600325 1 19960701 A 5330 SKIN BOEING 747 747132 1384882 NM BS 1840 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LOWER FUSELAGE SKIN BULGED WITH TWO FASTENERS POPPED, STA 1840 AT STR 44. REMOVED AND CLEANED LEVEL TWO CORROSION FROM SKIN AND SURROUNDING STRUCTURE IAW SRM 51-10-06. REPAIRED IAW SRM 53-30-03. 2 L 7 4 4F A20WE 1996071000246 19960710 00246 NM 1996 7 10 P5CA9600326 1 19960701 A 5330 SKIN BOEING 747 747132 1384882 NM BS 1960 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LOWER FUSELAGE SKIN BULGED AND SEVERAL PULLED RIVETS FS 1960 BETWEEN S-42R AND 43R. REMOVED LEVEL TWO CORROSION IAW SRM 51-10-01. REPAIRED FUSELAGE SRM 53-30-03. 2 L 7 4 4F A20WE 1996071000247 19960710 00247 EU 1996 7 10 QXEA9600228 1 19960630 A 3350 1820 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 454US 11107 LEFT SIDE PASSENGER OVERWING EMERGENCY LIGHT DOES NOT ILLUMINATE IN ARMED POSITION. BULB WAS REPLACED AND LIGHT OPS CHE CKED GOOD. 2 L 7 2 4F RT A20EU 1996071000248 19960710 00248 EU 1996 7 10 QXEA9600229 1 19960630 A 3232 1252515 ACTUATOR FOKKER F28 F28MK1000 4990808 EU LT MLG LEAKING A QXEA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 NM 09 457US 11036 HYDRAULIC SYSTEM UTILITY MASTER WARNING LIGHT ILLUMINATED AND UTILITY SYSTEM HYDRAULIC QUANITITY DROPPED TO ZERO. ALTER NATE GEAR EXTENSION PERFORMED AND AIRCRAFT LANDED WITHOUT FURTHER PROBLEMS. LEFT MAIN GEAR AFT DOOR ACTUATOR REPLACED I AW MAINT MANUAL. SERVICED UTILITY SYSTEM AND SYSTEM OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996071000249 19960710 00249 EU 1996 7 10 QXEA9600230 1 19960630 A 2913 40052 HYD PUMP FOKKER F28 F28MK1000 4990808 EU NR 1 POSITION LEAKING A QXEA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 NM 09 803PH 11031 UTILITY SYSTEM HYDRAULIC QUANITY DROPPED TO ZERO. ALTERNATE GEAR EXTENSION PERFORMED AND AIRCRAFT LANDED WITHOUT FURTHE R PROBLEMS. NR 1 HYDRAULIC PUMP REPLACED AND SYSTEM OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996071000250 19960710 00250 NM 1996 7 10 QXEA9600231 1 19960702 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 812PH 26 THE TWO FORWARD EMERGENCY LIGHTS AND LEFT HAND EXTERIOR EMERGENCY LIGHT ARE INOP. BATTERY PACK PS1 AND PS3 WERE REPLACE D AND LIGHTS OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 1996071000251 19960710 00251 NM 1996 7 10 QXEA9600232 1 19960702 A 3350 P401021 BATTERY DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 816PH 54 FORWARD EMERGENCY FLASHLIGHT BATTERY PACK IS WEAK. BATTERY PACK REPLACED AND LIGHT OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 1996071000252 19960710 00252 WP 1996 7 10 SCNA96185 1 19960630 A 2621 89524001 FIRE BOTTLE DOUG DC10 DC1010 3022110 WP NR 2 ENGINE DISCHARGED A SCNA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 15 571SC 46645 NUMBER 2 ENGINE AGENT LOW LIGHT CAME ON IN FLIGHT. FOUND NUMBER 2 BOTTLE THERMAL DISCHARGED. REMOVED AND REPLACED BOTT LE PER MM 26-21-02, FOUND NO AIR LEAKS. 2 L 7 3 4F A22WE 1996071000253 19960710 00253 NM 1996 7 10 SWAA960591 1 19960625 A 2130 PRESSURIZATION BOEING 737 7372H4 138448C NM CABIN MALFUNCTIONED A SWAA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 82SW 22731 ON CLIMBOUT, PRESSURIZATION FAILED IN AUTO MODE, WENT STANDBY MODE, BUT CABIN PRESSURE CONTINUED TO CLIMB. SWITCHED TO MANUAL MODE AND DESCENDED TO 10,000 FT. AIRCRAFT MADE AN UNEVENTFUL LANDING AT MCI. INSPECTED AND OPERATION CHECKED PR ESSURIZATION SYSTEM NORMAL PER BOEING M/M. 2 L 7 2 4F A16WE 1996071000254 19960710 00254 NM 1996 7 10 SWAA960592 1 19960625 A 5210 ANGLE BOEING 737 7372H4 138448C NM FWD ENTRY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21722 DURING SCHEDULED TERMINAL CHECK, FOUND FWD ENTRY DOOR, INNER FRAME SKIN CRACKED BELOW LOWER HINGE. REPLACED FRAME ANGL E PER BOEING SRM. 2 L 7 2 4F A16WE 1996071000255 19960710 00255 NM 1996 7 10 SWAA960593 1 19960625 A 5330 SKIN BOEING 737 7375H4 138449D NM FUSELAGE GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 511SW 24188 DURING SCHEDULED B/C1 CHECK, FOUND FUSELAGE SKIN GOUGED 14 INCHES BELOW AFT ENTRY. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996071000256 19960710 00256 NM 1996 7 10 SWAA960594 1 19960626 A 5330 SKIN BOEING 737 7372K6 NM PWR DOOR CUTOUT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED C1 CHECK, FOUND EXTERNAL POWER DOOR CUTOUT SKIN CRACKED AT T/E. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996071000257 19960710 00257 NM 1996 7 10 SWAA960595 1 19960627 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING WALKAROUND, FOUND FUSELAGE SKIN CRACKED BELOW FWD SERVICE DOOR. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996071000258 19960710 00258 NM 1996 7 10 SWAA960596 1 19960627 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 757 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 61SW 21970 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE HAD 2 SKIN CRACKS AT BS 757 STRINGER 17L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996071000259 19960710 00259 NM 1996 7 10 SWAA960597 1 19960627 A 5210 FRAME BOEING 737 7372H4 138448C NM AIRSTAIRS CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 61SW 21970 DURING SCHEDULED SERVICE CHECK, FOUND AIRSTAIR DOOR FRAME CRACKED UNDER FWD UPPER STOP. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996071000260 19960710 00260 NM 1996 7 10 SWAA960598 1 19960627 A 3350 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 73SW 22673 DURING SCHEDULED C2/C4 CHECK, FOUND OVERHEAD CENTER AISLE EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F A16WE 1996071000261 19960710 00261 NM 1996 7 10 SWAA960599 1 19960627 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 86SW 22827 DURING SCHEDULED D-CHECK, FOUND STRINGER 25R AT BS 947 CORRODED. REPLACED CORRODED SECTION PER BOEING SRM. 2 L 7 2 4F A16WE 1996071000262 19960710 00262 NM 1996 7 10 SWAA960600 1 19960627 A 5312 BULKHEAD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 86SW 22827 DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT WL 218, LBL 7 TO 10. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996071000263 19960710 00263 NM 1996 7 10 SWAA960601 1 19960627 A 5320 WEB BOEING 737 7372H4 138448C NM BS 492/490 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 86SW 22827 DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR SEAL WEB CORRODED AT BS 492 AND 490, WL 166, RBL 32. REPLACED WEB PER BO EING SRM. 2 L 7 2 4F A16WE 1996071000264 19960710 00264 NM 1996 7 10 SWAA960602 1 19960627 A 5315 SUPPORT BOEING 737 7372H4 138448C NM BS 504 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 86SW 22827 DURING SCHEDULED D-CHECK, FOUND FWD CARGO BAY FLOOR SUPPORT CORRODED AT BS 504, FROM S25L TO 26R. REPAIRED PER BOEING S RM. 2 L 7 2 4F A16WE 1996071000265 19960710 00265 NM 1996 7 10 SWAA960603 1 19960627 A 5330 SKIN BOEING 737 7373A4 1384585 NM BS 1024 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED QD-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 1024, RIGHT SIDE AT S17 AND AT BS 1064, RBL 7, WL 203. INST ALLED REPAIR DOUBLERS PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996071000266 19960710 00266 NM 1996 7 10 SWAA960604 1 19960627 A 3350 POWER SUPPLY BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 510SW 24187 DURING SCHEDULED TERMINAL CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REPLACED LEFT POWER SUPPLY HOUSING P ER BOEING M/M. 2 L 7 2 4F RT A16WE 1996071000267 19960710 00267 NM 1996 7 10 SWAA960605 1 19960701 A 7830 TR UNIT BOEING 737 7372H4 138448C NM ENGINE INOPERATIVE A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 61SW 21970 AFTER TAKEOFF, CREW EXPERIENCED T/R ISOLATION VALVE LIGHT ILLUMINATING. AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING. REPLACED ENGINE ACCESSORY UNIT AND BOTH PRESSURE SWITCHES PER BOEING M/M. 2 L 7 2 4F A16WE 1996071000268 19960710 00268 NM 1996 7 10 UPS96220525 1 19960621 A 5320 653414423 STIFFENER BOEING 727 72722C 138400F NM BS 740-760 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON EXPANSION LINK STA 740 TO 760 RBL 25 WL 208 IN CENTER CHANNEL AT FWD END. FOUND EXPANS ION LINK TO BE OUT OF LIMITS PER SRM 53-10-01. REMOVED AND REPLACED EXPANSION LINK AT BS 740 TO 760 RBL 25 WL 208 PER S RM 51-10-1, 51-30-4, 51-30-8, 51-10-6, 51-10-2. 2 L 7 3 4F A3WE 1996071000269 19960710 00269 NM 1996 7 10 UPS96220526 1 19960620 A 5314 KEEL BEAM BOEING 727 72722C 138400F NM BS 870 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, APU SIDE WEBS ARE CRACKED AT BS 870, LBL 5.5 AND RBL 5.5 WL 156. CUTOUT DAMAGE AND REPAIRED KEEL BE AM IAW UPS IAW EO B727-5330-1995-B AND BOEING DRAWING 65-88832. 2 L 7 3 4F A3WE 1996071000270 19960710 00270 NM 1996 7 10 UPS96220571 1 19960629 A 5311 FRAME BOEING 727 72722C 138400F NM BS 870 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, LT 870 FORGING STR 9 HAS ONE CRACKED HOLE AND CRACK IN RADIUS ON FWD FLANGE. INSTALLED EXTERNAL DOU BLERS AND REPAIRED IAW EO B727-5310-3057E AND EO B727-5310-8080A. 2 L 7 3 4F A3WE 1996071000271 19960710 00271 NM 1996 7 10 UPS96220572 1 19960629 A 5311 FRAME BOEING 727 72722C 138400F NM BS 870 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, RT 870 FORGING SPLICE AT STR 9 HAS 5 CRACKED HOLES AND ONE 2 TO 3 INCH CRACK IN RADIUS OF AFT FLANGE . REPAIRED BS 870 FORGING BY REMOVING DAMAGED SECTION AND SPLICING A NEW SECTION IN PLACE IAW B727-5310-3057 AND B727-5 310-8080A. 2 L 7 3 4F A3WE 1996071000272 19960710 00272 NM 1996 7 10 UPS96220573 1 19960628 A 5315 FLOOR BEAM BOEING 727 72722C 138400F NM BS 640 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION AT NUTPLATES IN FLOOR BEAM BOTTOM SIDE OF UPPER FLANGE STA 640 WL 207.5 LBL 38 AREAS MARKE D. FOUND FLOOR BEAM AT BS 640 LBL 38 TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED FLOOR BEAM AT BS 640 LBL 38 PER UPS EO 727-53-1780. 2 L 7 3 4F A3WE 1996071000273 19960710 00273 NM 1996 7 10 UPS96220574 1 19960628 A 5315 FLOOR BEAM BOEING 727 72722C 138400F NM BS 1110 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, DOUBLE HOLES IN LOWER FLANGE OF THE 1110 FLOOR BEAM LBL 19 RBL 45 WL 201. DURING REMOVAL OF CEILING SUPPORT FOUND FLOOR BEAM TO BE CORRODED OUT OF LIMITS PER SRM 53-10-01. REPAIRED PER EO 96-2357. 2 L 7 3 4F A3WE 1996071000274 19960710 00274 NM 1996 7 10 UPS96220575 1 19960628 A 5315 FLOOR BEAM BOEING 727 72722C 138400F NM BS 680 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON FLOOR BEAM BOTTOM SIDE OF UPPER FLANGE AT NUTCLIP HOLES STA 680 WL 207.5 LBL 5, 29, 33, 35 RBL 4, 37, 59, 60, AREAS MARKED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-1, REPAIRED PER EO 9 6-2363. 2 L 7 3 4F A3WE 1996071000275 19960710 00275 NM 1996 7 10 UPS96220576 1 19960628 A 5321 FLOOR BOEING 727 72722C 138400F NM BS 209-231 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE SI, CORROSION ON FLOOR STA 209 TO 231 LBL 6 TO 18 WL 208. REMOVED CORROSION AND FOUND TO BE OUT OF LIMI TS PER SRM 53-10-1. REPLACED FLOOR PANEL PER SRM 51-40-2, 51-10-2 MM 51-20-151, SRM 51-30-02. 2 L 7 3 4F A3WE 1996071000276 19960710 00276 NM 1996 7 10 UPS96420570 1 19960625 A 5320 STIFFENER BOEING 747 747123F NM BS 2200 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE-C, OUTFLOW VALVE AREA, FOUND CORROSION ON FRAME STIFFENER AT BS 2200, S-42 RT. REPLACED FRAME STIFFENER IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996071000277 19960710 00277 NM 1996 7 10 UPS96420577 1 19960702 A 3350 LIGHT BOEING 747 747121 1384871 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE N/A, PRIMARY UPPER DECK DOOR EMERGENCY LIGHT INOP ON PREFLIGHT. DEFERRED PER MEL 33-15 M112004 ASSIGNED . 2 L 7 4 4F A20WE 1996071000278 19960710 00278 NM 1996 7 10 VNAA9606014 1 19960630 A 7603 POWER LEVER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE QUADRANT LACK OF LUBE A VNAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 424JS 3033 CREW REPORTED, WHEN ADVANCING THE POWER LEVERS, THE LEFT POWER LEVER JAMMED JUST ABOVE THE FLIGHT IDLE GATE. AIRCRAFT R ETURNED TO THE GATE. MX LUBRICATED THE LEFT POWER LEVER PRIMARY FLIGHT IDLE LOCK OUT MECHANISM IAW MM 76-10-00 AND STD MX PRACTICES, GROUND CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996071000279 19960710 00279 NM 1996 7 10 VNAA9607003 1 19960704 A 5610 001A561A0000206 DV WINDOW DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT COCKPIT CRACKED A VNAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 437JS 3055 EN ROUTE, CREW REPORTED A CRACK IN THE CAPTAIN'S DIRECT VISION WINDOW. REPORTED THE PROBLEM TO DISPATCH, WAS THEN INSTR UCTED TO RETURN TO PIT. NO EMERGENCY DECLARED, AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MX REPLACED CAPTAIN'S DV WIND OW IAW MM 56-10-00. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996071000280 19960710 00280 1996 7 10 VSTA9607001 4 19960703 A 3442 MI5910161 RT UNIT BOEING 737 737204 1384458 NM RADAR BAY DEFECTIVE A VSTA K NONE O OTHER CL CLIMB 1 WP 07 313VA 19711 RADAR INDICATOR SHOW R/T FAULT. REMOVED AND REPLACED R/T RADAR. 2 L 7 2 4F A16WE 1996071000282 19960710 00282 GL 1996 7 10 96ZZZX3405 2 19960515 A 7310 355A64302020 UNION AEROSP AS355 AS355F1 8680810 EU ALLSN 250C 250C20F 03013 GL FUEL DIST CRACKED D A M3XA K NONE O OTHER IN INSP/MAINT 1 WP 07 911TM 5059 REMOVED FOR A FUEL PUMP BYPASS CHECK DUE TO DELAYED LIGHT-OFFS ON A C20F ENGINE. UNION WAS FOUND CRACKED AFTER LOOSENIN G B-NUT. BYPASS CHECK COMPLETED AND CHECK PASSED, STILL HAD NO RESOLVE TO DELAYED LIGHT-OFFS. INSTALLED UNION AND FUEL TUBE ASSEMBLY AND TIGHTENED B-NUT, THE INSIDE FLARE BROKE-OFF WITH B-NUT. AFTER INSPECTING THE UNION, SIGNS OF FRETTIN G WERE PRESENT AND THERE WAS A CRACK PRIOR TO IT FAILING. REPLACED UNION WITH NEW ONE. THE DELAYED LIGHT-OFFS PROBLEM WAS CORRECTED. 1 G 7 2 3U 3 U H11EU E4CE 1996071000284 19960710 00284 WP 1996 7 10 96ZZZX3407 1 19960501 A 7920 269A8327155 LINE HUGHES 269 269C 4470504 WP OIL COOLER CHAFED A S HIAA K NONE K FLUID LOSS NR NOT REPORTED 1 WP 27 1105B 411030 'THE INCIDENT OF HELICOPTER HAVING AN ENGINE FAILURE WAS CAUSED BY AN OIL LEAK FROM THE OIL LINE FROM THE ACCESSORY SECT ION OF THE AFT OIL COOLER. THE LINE CHAFED THROUGH ON AN ADJACENT LINE.' SUBMITTER STATED THIS COULD HAVE BEEN PREVENT ED BY BETTER SECURING OF THE OIL LINE WITH A CLAMP IN THIS AREA OF THE ACCESSORY SECTION. 1 G 7 1 3O 4H12 1996071000290 19960710 00290 GL 1996 7 10 96ZZZX3413 2 19960515 A 7210 23030917 BEARING 23035178 BELL 206 206L4 1182110 SW ALLSN 250C 250C30P 03013 GL NR 4 PINION FAILED A L ALGA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 03 177AL 513 JJ00464 52157 THE ENGINE CHIP DETECTOR LIGHT ILLUMINATED IN CRUISE FLIGHT OVER THE GULF OF MEXICO. THE PILOT LANDED THE HELICOPTER ON NEAREST OFFSHORE PLATFORM, APPROXIMATELY 7 MILES AWAY. MAINTENANCE INSPECTED THE CHIP DETECTOR PLUGS AND FOUND THE LOW ER PLUG COVERED WITH METAL SHAVINGS AND A PIECE OF METAL .50 INCH LONG BY .25 INCH WIDE. THE ENGINE WAS REPLACED ON THE OFFSHORE PLATFORM. SUBSEQUENT EXAMINATION OF THE ENGINE REVEALED THE NR 4 PINION BEARING ROLLER CAGE HAD FRACTURED. A LARGE PIECE OF THE ROLLER CAGE WAS MISSING. 1 G 7 1 3U 3 U NC H2SW E1GL 1996071000293 19960710 00293 EU 1996 7 10 96ZZZX3416 1 19960503 A 2150 060018 BELT 3500001 SNIAS 350 AS350B 8680801 EU AIR COND SYSTEM FAILED A A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 21UM 1674 INSTALLED 2 NEW BELTS (1 SPARE) ON AIRCRAFT, FIRST PROBLEM, NO DIRECTION OF ROTATION OR ARROW ON BELT. SECOND PROBLEM W AS BELT BROKE OR DELAMINATED AT GLUE JOINT (SEAM) ON FIRST RUN. AFTER INVESTIGATING, DETERMINED BELT WAS INSTALLED PROP ERLY. SUBMITTER RECOMMENDATION: DIRECTION OF ROTATION ARROW PRINTED ON BELT. ALSO, RECOMMEND TRACKING BATCH. 1 G 7 1 3U H9EU 1996071000295 19960710 00295 EA 1996 7 10 96ZZZX3418 1 19960318 A 2420 DH10301153 CONTROL BOX DHAV DHC7 DHC7102 2802708 EA DC ELECT SYST INOPERATIVE A CICA K NONE J WARNING INDICATION CR CRUISE 1 SO 17 4860J 19 MIA/TPA - FLT 4938 - PILOT REPORTED SECONDARY INVERTER LIGHT ILLUMINATED. AIRCRAFT WAS FERRIED TO FLL MAINTENANCE BASE. MAINTENANCE REPLACED PARALELLING CONTROL BOX. TEST FLIGHT SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 4 4T A20EA 1996071000296 19960710 00296 NM 1996 7 10 95FDEA00763 1 19960412 A 5313 6516344 STRINGER BOEING 727 727277 138408S NM BS 1098-1070 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 242FE 21178 CORROSION (C53-113-01) BS 1098 TO 1070 STR 24R. *S/D* REMOVED AND REPLACED CHANNEL AT BS 1070 TO 1098 AT STR 29R. ALL WORK DONE IAW FEDEX SRM 51-30-2. 2 L 7 3 4F RT A3WE 1996071000297 19960710 00297 NM 1996 7 10 9614652287 1 19960705 A 2750 CONRTOL MECH BOEING 727 727251 138408H NM TE FLAPS OUT OF ADJUST A NWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 01 287US 21375 DURING CLIMBOUT, VIBRATION WAS FELT PASSING THROUGH 15,000 FEET. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED INBOARD FLAP RIGHT AND LEFT AFT ECCENTRICS AND LEFT OUTBOARD FLAP ECCENTRICS. PERFORMED RIG CHECK OF FLIGHT SYSTEM, CHECKED OK. 2 L 7 3 4F A3WE 1996071000298 19960710 00298 WP 1996 7 10 9614669928 1 19960703 A 3260 SWITCH DOUG DC9 DC931 3022065 WP RT MLG MALFUNCTIONED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 8921E 45836 AFTER TAKEOFF, RIGHT MAIN GEAR UNSAFE LIGHT REMAINED ILLUMINATED. RECYCLED GEAR AND LIGHT REMAINED ON. CLIMBING THROUG H FL260, GEAR DOOR LIGHT CAME ON. POSITIONED ENGINE PUMPS TO HIGH. NO AIR NOISE OR VIBRATION. FLIGHT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT MAIN GEAR ACTUATOR AND DOOR SWITCH, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996071000299 19960710 00299 WP 1996 7 10 9614679756 1 19960704 A 2612 FIRE LOOP DOUG DC9 DC941 302207N WP LT ENGINE MALFUNCTIONED A NWAA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 756NW 47180 DURING CLIMBOUT, THE LEFT ENGINE FIRE WARNING SOUNDED. FOLLOWED ENGINE FIRE PROCEDURE AND FIRE INDICATION CONTINUED. D ISCHARGED BOTH FIRE BOTTLES, RETURNED TO MSP AND LANDED WITHOUT INCIDENT. FOUND BOTH LOOPS SHORTED. REPLACED FIRE DETE CTION LOOP, RUNUP AND OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996071000300 19960710 00300 NM 1996 7 10 9614686309 1 19960704 A 3350 PIN BOEING 747 747451 1384940 NM CABIN DISCONNECTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 669US 24224 DURING LINE CHECK, FOUND THAT THE EMERGENCY FLOOR PROXIMITY LIGHTS WERE INOPERATIVE FOR SEATS 11 TO 14JK. RECONNECTED A PIN AT 11JK, CHECKED OK. 2 L 7 4 4F RT A20WE 1996071000301 19960710 00301 NM 1996 7 10 9614696719 1 19960703 A 7722 80J200LWN1 EGT INDICATOR BOEING 747 747251F 1384898 NM PWA JT9 JT9D7F 52054 NE NR 3 ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 169US 21321 62643 DURING TAKEOFF ROLLOUT, THE NR 3 ENGINE EGT OVERTEMPED. TAKEOFF WAS ABORTED AND THE ENGINE WAS SHUT DOWN WHILE STILL IN REVERSE. MAINTENANCE INSPECTED ENGINE INLET, EXHAUST AND ALL 3.5 BLEED PORTS, NO DISCREPANCIES NOTED. REPLACED EGT IN DICATOR AND PERFORMED RUNUP CHECK. CHECK WAS NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4 F A20WE E20EA 1996071000302 19960710 00302 NM 1996 7 10 96FDEA00382 1 19960301 A 5753 652163586 AFT FLAP BOEING 727 727233 138408A NM RT TE AFT FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 275FE 22040 RT WING I/B AFT FLAP HAS A 2 INCH DELAMINATED DENT 14 INCHES FROM I/B END UPPER SURFACE. ROUGH DAMAGE IS 5.5 BY 8.25. R EPAIRED RT WING I/B AFT FLAP 14 INCHES FROM I/B END UPPER SURFACE IAW SRM 51-40-6. 2 L 7 3 4F RT A3WE 1996071000303 19960710 00303 NM 1996 7 10 96FDEA00417 1 19960307 A 5330 6518420 SKIN BOEING 727 72722 1384002 NM BS 277.2 GOUGE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 BS 277.2 STR 21R WL 180, THERE IS A DEEP GOUGE IN SKIN. *S/D* BLENDED GOUGE IN SKIN AT BS 277.2 STR, WL 180. ORIGINAL SKIN THICKNESS WAS 040, AREA REMOVED WAS 030 IN A 1 BY 5 INCH AREA AND WAS FOUND TO BE OUT OF LIMITS PER SRM 53-30-1. D AMAGED AREA WAS REPAIRED PER FEDEX SRM 53-30-3. 2 L 7 3 4F A3WE 1996071000304 19960710 00304 NM 1996 7 10 96FDEA00504 1 19960311 A 5330 6554572 SKIN BOEING 727 72722 1384002 NM BS 660.3 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 NR 0071, BS 660-3 STR 20R, WL 181, THERE IS A DEEP GOUGE IN SKIN. BLENDED GOUGE, OUT OF LIMITS PER SRM 53-30-1. *S/D* REMOVED GOUGE IN SKIN AT BS 660.3 STR 20R, WL 181, FABRICATED REPAIR DOUBLER IAW SRM 53-30-3. 2 L 7 3 4F A3WE 1996071000305 19960710 00305 NM 1996 7 10 96FDEA00505 1 19960311 A 5320 65242581 THRESHOLD WEB BOEING 727 72722 1384002 NM BS 540/560 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 22040 NR 0078, (C53-113-01) ON THRESHOLD VERTICAL WEB UNDER NUTPLATES BS 540 AND 560, RBL 21, WL 156. *S/D* REMOVED AND REIN STALLED VERTICAL WEB IAW SRM 53-10-1. 2 L 7 3 4F A3WE 1996071000306 19960710 00306 NM 1996 7 10 96FDEA00506 1 19960311 A 5313 6515927 STRINGER BOEING 727 72722 1384002 NM BS 540 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 NR 0078 (C53-113-01) ON THRESHOLD VERTICAL WEB UNDER NUTPLATES BS 540 AND 560, RBL 21, WL 156. *S/D* REMOVED DAMAGED P ORTION OF STRINGER AT BS 480, STR 27R, WL 157. REPAIRED STRINGER IAW FEDEX SRM 53-10-3. 2 L 7 3 4F A3WE 1996071000307 19960710 00307 NM 1996 7 10 96FDEA00510 1 19960311 A 5320 6519862 CHORD BOEING 727 72722 1384002 NM BS 318/335 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 NR 400, CORROSION (C53-111-03) ON RT MID NOSE CHORD VERTICAL FLANGE EMANATING FROM BENEATH A VERTICAL STIFFENER BS 518 A ND TWO BULGES IN FLOOR WEB ON CHORDS HORIZONTAL FLANGE BS 318 AND 335, RBL 15, WL 159, ACCESS REQUIRED. *S/D* REMOVED AND REPLACED RT MID CHORD STA 294 TO 351 WL 159, RBL 15. ALL WORK IAW BAC BRW NR 65-18415. 2 L 7 3 4F A3WE 1996071000308 19960710 00308 NM 1996 7 10 96FDEA00595 1 19960318 A 5311 6516344 FRAME BOEING 727 72722 1384002 NM BS 1166 DOUBLE DRILLED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 187FE 19079 NR0473, DOUBLE DRILLED HOLES ON NESTLED FLANGE OF FRAME AT BS 1166 LBL 20 WL 159. *S/D* TRIMMED DAMAGE AND INSTALLED D OUBLER PER SRM 51-40-3. 2 L 7 3 4F A3WE 1996071000309 19960710 00309 NM 1996 7 10 96FDEA00729 1 19960401 A 5313 BAC1498146 STRINGER BOEING 727 72725 1384006 NM BS 1055 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 NR 0623, 042 CORROSION (C53-113-01, -2) FOUND WHILE WORKING NR0602 STA 1055 STR 28R IN STRINGER. *S/D* FOUND CORROSION TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1, REMOVED DAMAGED AREA REPAIRED STR 28R IAW FEDEX SRM 53-10-3. 2 L 7 3 4F A3WE 1996071000310 19960710 00310 NM 1996 7 10 96FDEA00764 1 19960412 A 5230 6525326 FRAME BOEING 727 727277 138408S NM BS 480 GOUGE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 242FE 21178 MCD FWD SIDE FRAME IS GOUGED 56 INCHES UP FROM THE BOTTOM OF THE DOOR. *S/D* REPAIRED FRAME PER EA 7-5230-28057. 2 L 7 3 4F RT A3WE 1996071000311 19960710 00311 NM 1996 7 10 96FDEA00765 1 19960412 A 5230 6525326 FRAME BOEING 727 727277 138408S NM BS 620 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 242FE 21178 MCD AFT SIDE FRAME IS GOUGED ON PREVIOUS REPAIR DOUBLER 17 INCHES UP FROM THE BOTTOM OF DOOR. *S/D* REPLACED REPAIR DO UBLER PER DWG SR 27-52-009. 2 L 7 3 4F RT A3WE 1996071000312 19960710 00312 NM 1996 7 10 96FDEA00841 1 19960425 A 5330 6518420 SKIN BOEING 727 727233 138408A NM BS 205 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 270FE 22035 NR0183 004, BULGE IN SKIN BS 205 RBL 12 WL 168. *S/D* REPAIRED BULGE IN SKIN AT BS 205, RBL 12, WL 168 IAW SRM 53-30-3 . 2 L 7 3 4F RT A3WE 1996071000313 19960710 00313 EU 1996 7 10 96FDEA01191 1 19960701 A 2913 PUMP AIRBUS 310 A310203 EU NR 1 ENGINE INOPERATIVE A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 425FE 264 ENG NR 1 GREEN HYD PUMP INOP. FAILURE OCCURRED IMMEDIATELY AFTER TAKEOFF. REMOVED AND REPLACED NR 1 GREEN SYSTEM PUMP, SHAFT AND CASE RETURN FILTER, OPS CHECK GOOD. 2 L 7 2 4F RT A35EU 1996071000314 19960710 00314 EU 1996 7 10 96FDEA01192 1 19960704 A 3260 INDICATION AIRBUS 300 A300F4605R 3930327 EU NLG MALFUNCTIONED A FDEA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 25 656FE 745 ON APPOACH AFTER LG EXTENDED NR 1 SYS IND 3 GREEN SYS 1 SELECTED ON SHORT FINAL TOO LOW GEAR WARNING INITIATED, SYS 2 OV ERHEAD SHOWED NOSE GEAR NOT DOWN. LANDING GEAR CHECKED VISUALLY DOWN AND LOCKED ON SYS DETECTION 2. ALSO, SELECTED GAV E THE SAME WARNING. 2 L 7 2 4F RT A35EU 1996071000315 19960710 00315 NM 1996 7 10 96FDEA01193 1 19960702 A 5320 6516306130 CHORD BOEING 727 7272D4 138407U NM BS 227.8 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 287FE 21849 DISCREPANCY: NR 0186 (002) CORROSION (C53-100-01) IN FORWARD NOSE COMPARTMENT ON CIRCUMFERENTIAL CHORD AND SURROUNDING STRUCTURE AT BS 227.8, RBL 7 TO LBL 7, WL 156. REMOVED CORRODED CIRCUMFERENTIAL CHORD BS 227.8, LBL 37 - RBL 37. FABRI CATED AND INSTALLED CIRCUMFERENTIAL CHORD BS 227.8 LBL - RBL 37. ALL WORK DONE PER FEDEX DWG 65-16306 AND SRM 51-40-4. 2 L 7 3 4F A3WE 1996071000316 19960710 00316 NM 1996 7 10 96FDEA01194 1 19960702 A 5320 65175861 INTERCOSTAL BOEING 727 72722 1384002 NM BS 277-295 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 DISCREPANCY: NR 0563 (007) CORROSION (C53-221-01) ON INTERCOSTAL BS 277-295, LBL 13 WL 208 ***S/D*** REMOVED AND REPLAC ED UPPER CHORD OF INTERCOSTAL, FLOOR SUPPORT BS 277 TO 295, LBL 13, WL 208. CORROSION FOUND TO BE OUT OF LIMITS. 2 L 7 3 4F A3WE 1996071000317 19960710 00317 NM 1996 7 10 96FDEA01195 1 19960702 A 5753 652165527 SKIN BOEING 727 7272D4 138407U NM LT TE MID FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 287FE 21849 DISCREPANCY: NR 0224 (003) LEFT WING, OUTBOARD MID-FLAP, UPPER SURFACE, TRAILING EDGE HAS 6 INCHES BY 1 INCH DISBOND FR OM INBOARD END. REPAIRED LEFT WING OUTBOARD MID-FLAP UPPER SURFACE TRAILING EDGE 74 INCHES FROM INBOARD END IAW SRM 51- 40-06. 2 L 7 3 4F A3WE 1996071000318 19960710 00318 NM 1996 7 10 96FDEA01196 1 19960702 A 5753 65175861 TE WEDGE BOEING 727 7272D4 138407U NM LT TE MIDFLAP DISBONDED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 287FE 21849 DISCREPANCY: NR 0223 (004) LEFT WING, OUTBOARD MIDFLAP, LOWER SURFACE, TRAILING EDGE WEDGE DISBOND OUTBOARD OF OUTBOARD AFT FLAP TRACK. ***S/D*** REPAIRED LEFT WING O/B MIDFLAP LOWER SURFACE T/E WEDGE OUTBOARD OF OUTBOARD AFT FLAP TRACK IAW SRM 57-40-06. 2 L 7 3 4F A3WE 1996071000319 19960710 00319 NM 1996 7 10 96FDEA01197 1 19960703 A 5320 69208134 SHEAR TIE BOEING 727 7272D4 138407U NM BS 1130 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 287FE 21849 NR 0145, 005, CORROSION (C53-113-01) IN AFT CARGO BAY ON FRAME SHEAR TIE BS 1130, WL 138, RBL 5. *S/D* REMOVED SHEAR T IE CROWN BS 1130, WL 138 RBL 5, FABRICATED SHEAR TIE PER FEDEX SRM 53-20-1. ALODINED, PRIMED, SEALED AND INSTALLED SHEA R TIE AT BS 1130, WL 138, RBL 5. 2 L 7 3 4F A3WE 1996071000320 19960710 00320 WP 1996 7 10 96FDEA01198 1 19960708 A 5245 WARNING LIGHT DOUG DC10 DC1030F 3023504 WP AIR COND DOORS ILLUMINATED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 305FE 47870 DURING CLIMBOUT, AIR COND DOORS LIGHT ILLUMINATED INTERMITTENTLY. AS AIRSPEED INCREASED TO 300 KTS LIGHT ILLUM, STEADY ON DESCENT, LIGHT EXTINGUISHED BELOW 250 KTS. AIRCRAFT RELEASED FOR SERVICE PER MEL/CDL 52-4 CATEGRORY C EXPIRATION, 17 JULY 96. INSPECTED ALL DOOR LATCHES AND DIMENSIONS FOUND SERVICEABLE. ADJUSTED 2 AND 3 DOOR LIMITS SWITCHES PER MM 52 -42-01 PRECAUTIONARY. 2 L 7 3 4F RT A22WE 1996071000321 19960710 00321 NM 1996 7 10 96FDEA01199 1 19960702 A 5311 651593230 FRAME BOEING 727 72722 1384002 NM BS 580 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 NR 0256, 001, CORROSION (C53-111-01) ON FRAME STR 580 BETWEEN STR 22 TO 25 LT FWD BAY 8. *S/D* CORROSION ON FRAME BS 5 80, BETWEEN STR 22 TO 25 LT IS OUT OF LIMITS PER SRM 53-10-01. REPAIRED FRAME PER SRM 51-40-3, ALODINED AND PRIMED ALL BARE METAL. 2 L 7 3 4F A3WE 1996071000322 19960710 00322 NM 1996 7 10 96FDEA01200 1 19960702 A 5315 654027612 FLOOR BEAM BOEING 727 72722 1384002 NM BS 1110 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 DISCREPANCY: NR 0301 (002) CORROSION (53-113-01-27 ) ON LOWER FLANGE OF FLOORBEAM, BS 1110, BBL 50 TO LBL 30 AT THE NUT PLATE HOLES. ***S/D*** REMOVED CORROSION AND REPAIRED LOWER FLANGE OF FLOOR BEAM AT BS 1110, RBL 50 TO LBL 30, REFEREN CE SRM 53-10-8, FIG 2. 2 L 7 3 4F A3WE 1996071000323 19960710 00323 NM 1996 7 10 96FDEA01201 1 19960702 A 5320 654027612 CLIP BOEING 727 72722 1384002 NM BS 910 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 DISCREPANCY: NR 0274 (003) GOUGE IN STRING CLIP BS 910 STR 11 RT. ***S/D*** REMOVED STR CLIP AT BS 910, STR 11 RT, AN D FOUND GOUGE TO BE OUT OF LIMITS PER SRM 53-10-1. REPLACED WITH NEW STRINGER CLIP. 2 L 7 3 4F A3WE 1996071000324 19960710 00324 NM 1996 7 10 96FDEA01202 1 19960702 A 5330 65182192 SKIN PANEL BOEING 727 72722 1384002 NM BS 395 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 NR 0110, 004, BS 380 PLUS 15 WL 160, STR 23 TO 24R THERE IS A SHARP PROTRUDING DENTS IN SKIN. *S/D* REPAIRED DENT AT B S 380 PLUS 15 BETWEEN STR 23 AND 24 RIGHT PER SRM 53-30-3 FIG 3. 2 L 7 3 4F A3WE 1996071000325 19960710 00325 NM 1996 7 10 96FDEA01203 1 19960702 A 5320 651759321 INTERCOSTAL BOEING 727 72722 1384002 NM BS 268-277 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 NR 0572, 006, CORROSION (53-221-01) ON INTERCOSTAL BS 268 TO 277 RBL 13 WL 208. *S/D* REMOVED AND REPLACED INTERCOSTAL BS 268 TO 277 RBL 13 WL 208, DUE TO CORROSION BEING OUT OF LIMITS IAW FED-EX SRM 53-10-1. 2 L 7 3 4F A3WE 1996071000326 19960710 00326 NM 1996 7 10 96FDEA01204 1 19960702 A 5330 65183868 SKIN BOEING 727 72722 1384002 NM BS 1080 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 DISCREPANCY: NR 0205 (005). CORROSION (53-100-01). BS 1080 STR 26R, RBL 30 ON EXTERIOR SKIN AT LAP RBL 13, WL 208. R EPAIRED DAMAGED AREA BS 1060 - 1080, STR 26R, RBL 30 ON EXTERIOR SKIN IAW FEDEX EA 7-5330-29612. 2 L 7 3 4F A3WE 1996071000327 19960710 00327 WP 1996 7 10 CALA9600965 1 19960704 A 3220 LOCKING BOLT DOUG DC9 DC982 3022082 WP NLG SCISSORS SHEARED A A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND THE HEAD SHEARED OFF OF THE LOWER LOCKING BOLT FOR THE NOSE GEAR SCISSORS. THE NOSE GEAR LOWER TORQUE LINK, PIN AND LOCKING BOLT WERE REMOVED AND REPLACED IAW MM 32-21-04, PAGE 201 TO 206. 2 L 7 2 4F A6WE 1996071000328 19960710 00328 WP 1996 7 10 CALA9600966 1 19960705 A 3220 GROUND SHIFT ROD DOUG DC9 DC982 3022082 WP NLG BROKEN A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 16808 49262 THE AIR/GROUND SHIFT MECHANISM WOULD NOT COME OUT OF GROUND MODE AFTER TAKEOFF FROM IAH. THE AIRCRAFT WAS RETURNED TO I AH. MAINTENANCE FOUND GROUND SHIFT ROD ON NOSE GEAR BROKEN. THE GROUND SHIFT ROD WAS REMOVED AND REPLACED. 2 L 7 2 4F A6WE 1996071000329 19960710 00329 NE 1996 7 10 CALA9600967 2 19960706 A 7250 80901401 AIRSEAL DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE NR 1 ENGINE WORN A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 12811 7360 49265 709893 THE NR 1 ENGINE SPOOLED DOWN ACCOMPANIED BY A LOUD EXPLOSION WHILE CLIMBING THROUGH FL 310. ABNORMAL PROCEDURES WERE CO MPLIED WITH AND THE AIRCRAFT WAS RETURNED TO SFO WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPL ACED. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION. *S/D* SHOP FINDINGS REVEALED A WORN T2 INN ER AIRSEAL. 2 L 7 2 4F 4 F A6WE E9NE 1996071000330 19960710 00330 WP 1996 7 10 CALA9600968 1 19960706 A 2910 AE1006037E0260 HYD LINE DOUG DC9 DC932 3022066 WP PRESS TRANS RUPTURED A CALA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CL CLIMB 1 SW 09 27522 47524 THE LEFT HYDRAULIC SYSTEM QUANTITY WAS LOST SHORTLY AFTER TAKEOFF FROM IAH. ABNORMAL PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC PRESSURE LINE GOING TO THE LEFT SYSTEM PRESSURE TRANSMITTER BLOWN. THE LINE WAS REPLACED USING FLEX HOSE AND A DIP WAS ISSUED TO REPLACE TH E LINE WITHIN 1200 HOURS OR 500 FLIGHTS, WHICHEVER OCCURS FIRST. THE LEFT HYDRAULIC SYSTEM WAS SERVICED AND LEAK CHECKS WERE GOOD. 2 L 7 2 4F A6WE 1996071000331 19960710 00331 NM 1996 7 10 CALA9600969 1 19960706 A 2752 MS9391130ZE4C MOTOR BOEING 727 727224 1384076 NM FLAP ACTUATOR LEAKING A A CALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 69736 69736 THE A-SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO WHILE EN ROUTE. THE LOSS WAS ACCOMPANIED BY ILLUMINATION OF THE LOW PRE SSURE LIGHT AND LEADING EDGE FLAP AMBER LIGHT. THE NR 1 KREUGER FLAP WAS SHOWING UNLOCKED ON AUX PANEL. MAINTENANCE FO UND THE OUTBOARD HYDRAULIC FLAP ACTUATOR MOTOR LEAKING. THE FLAP ACTUATOR MOTOR WAS REMOVED AND REPLACED, LEAK AND OPER ATIONAL CHECKS WERE GOOD. IN ADDITION, BOTH THE NR 1 AND NR 2 HYDRAULIC ENGINE DRIVEN PUMPS WERE REMOVED AND REPLACED A S A PRECAUTIONARY MEASURE. 2 L 7 3 4F A3WE 1996071000332 19960710 00332 NM 1996 7 10 CALA9600970 1 19960706 A 2782 1U1110 ACTUATOR BOEING 727 727232 1384082 NM NR 2 LE FLAP LEAKING A A CALA A J UNSCHED LANDING DUMP FUEL K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 09 10791 41613 642 20645 THE A-SYSTEM HYDRAULIC QUANTITY WAS LOST DURING CLIMBOUT. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 LEADING EDGE FLAP ACTUATOR LEAKING. THE ACTUATOR WAS REMOVED AND REPLACED. IN ADDITION, BOTH ENGINE DRIVEN HYDRAULIC PUMPS WERE REMOVED AND REPLACED. THE HYDRAULIC SYSTEM WAS SERVICED , LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 3 4F A3WE 1996071000333 19960710 00333 WP 1996 7 10 CALA9600971 1 19960707 A 3350 41B004AD073 BATTERIES DOUG DC9 DC982 3022082 WP COCKPIT DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 809NY 49263 THE OVERHEAD EMERGENCY LIGHTS IN COCKPIT WOULD ONLY ILLUMINATE FOR FIVE SECONDS WHEN SELECTED. THE BATTERIES FOR COCKPI T EMERGENCY LIGHTS WERE REPLACED AND OPERATION OF LIGHTS WAS RESTORED. 2 L 7 2 4F A6WE 1996071000334 19960710 00334 NE 1996 7 10 CKSA96064 2 19960703 A 7200 ENGINE BOEING 727 727223 1384074 NM PWA JT8 JT8D9A 52048 NE NR 2 FLAMED OUT A CKSA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 GL 23 858AA 21085 666098 NR 2 ENGINE FLAMED OUT AT FL370 WHILE CROSS FEEDING FROM ENGINES NR 1 AND NR 3. NR 2 ENGINE BOOST PUMPS OFF, NORMAL INF LIGHT RESTART WITH BOOST PUMPS ON. INSPECTED ENGINE IAW MM CHAPTER 72-00, OPS CHECKED GOOD ON ENGINE RUN. 2 L 7 3 4F 4 F A3WE E2EA 1996071000335 19960710 00335 SO 1996 7 10 COMA9610219 1 19960703 A 2752 3203001005 ACTUATOR EMB 120 EMB120RT SO RT TE FLAP MALFUNCTION A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 161CA 7534 5171 120143 FLAP CONTROL FAULT WARNING DURING TAKEOFF ROLL. REPLACED THE RT INBD FLAP ACTUATOR. 2 L 7 2 4T RT A31SO 1996071000336 19960710 00336 EU 1996 7 10 COMA9630135 1 19960707 A 7600 5308211C QUADRANT SAAB SF340 SF340A 7850100 EU COCKPIT DEFECTIVE A COMA K NONE O OTHER DE DESCENT 1 SO 01 347CA 18388 223 340A028 DURING DESCENT THE POWER LEVERS CAME THROUGH THE FLIGHT IDLE GATE AND INTO BETA RANGE WITHOUT LIFTING THE POWER LEVER TR IGGERS. REPLACED ENGINE CONTROL QUADRANT. 2 L 7 2 4T RT A52EU 1996071000337 19960710 00337 EU 1996 7 10 COMA9630136 1 19960703 A 5610 WINDSHIELD SAAB SF340 SF340A 7850100 EU COCKPIT BIRD STRIKE A COMA A UNSCHED LANDING C F.O.D. CL CLIMB 1 SO 01 347CA 340A028 BIRD STRIKE, LOWER WINDSHIELD AREA, JUST AFTER TAKEOFF. ACFT RETURNED TO CHA. BIRD STRIKE INSPECTION C/W AND NO DAMAGE NOTED. 2 L 7 2 4T RT A52EU 1996071000338 19960710 00338 EA 1996 7 10 COMA9660117 1 19960706 A 5610 NP1393211 WINDSHIELD CNDAIR CL600 CL6002B19 EA LT COCKPIT CRACKED A COMA K NONE O OTHER CR CRUISE 1 SO 01 951CA 7091 PILOTS WINDSHIELD CRACKED DURING FLIGHT. REPLACED WINDSHIELD. 2 L 7 2 4F RT A21EA 1996071000339 19960710 00339 NM 1996 7 10 P5CA9600327 1 19960707 A 2910 O-RINGS BOEING 747 747122 1384872 NM NR 1 CHK VALVE CUT A P5CA O OTHER K FLUID LOSS CL CLIMB 1 WP 23 853FT 19753 NR 1 HYDRAULIC SYSTEM FLUID LOSS AFTER TAKEOFF. LEAK STOPPED WHEN PUMPS SHUT OFF, SYSTEM QUANTITY STABLE AT 2.5 GALLONS . EXTENDED GEAR AND FLAPS BY ALTERNATE SYSTEM. UPON APPROACH TO MIAMI HAD BODY GEAR AND NOSE GEAR STEERING AVAILABLE F OR TAXI IN. FLUID LOSS CONTINUED TO LESS THAN 1 GALLON DURING TAXI. FOUND NR 1 HYDRAULIC SYSTEM PRESSURE MODULE CHECK VALVE LEAKING. REMOVED CHECK VALVE AND FOUND O-RINGS DAMAGED VISUALLY CHECKED INNER MATING AREA, FOUND OK. REPLACED O- RINGS, OPERATIONAL AND LEAKED CHECKED OK PER BOEING MAINTENANCE MANUAL 29-11-13 AND 29-11-00. 2 L 7 4 4F A20WE 1996071000340 19960710 00340 NM 1996 7 10 P5CA9600328 1 19960708 A 5230 SEAL RETAINER BOEING 747 747122 1384872 NM CARGO DR CUTOUT BENT A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 FWD LOWER CARGO COMPARTMENT CUTOUT SEAL RETAINER AFT EDG BENT AND DEFORMED. FABRICATED NEW SEAL RETAINER PER BOEING SRM 51-32-01, INSTALLED PER BOEING SRM 51-10-01. 2 L 7 4 4F A20WE 1996071000341 19960710 00341 NM 1996 7 10 P5CA9600329 1 19960708 A 5400 BRACKET BOEING 747 747122 1384872 NM NR 4 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 CRACKED SUPPORT BRACKET NR 4 PYLON, GENERATOR LEAD SUPPORT. REMOVED, FABRICATED AND REPLACED BRACKET PER BOEING SRM 51- 30-02 AND 51-10-01. 2 L 7 4 4F A20WE 1996071000342 19960710 00342 NM 1996 7 10 P5CA9600330 1 19960708 A 5400 ANGLE BRACKET BOEING 747 747122 1384872 NM NR 4 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 NR 4 ENGINE PYLON, ANGLE BRACKET BENT AND CRACKED INBD AFT. REMOVED, FABRICATED AND INSTALLED BRACKET PER BOEING SRM 51 -32-01 AND 51-10-02. 2 L 7 4 4F A20WE 1996071000343 19960710 00343 NM 1996 7 10 P5CA9600331 1 19960708 A 5320 DOOR SILL BOEING 747 747122 1384872 NM CARGO COMPT CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 BULK CARGO DOOR SILL CRACKED 2 PLACES. WELD REPAIRED PER BAC59755905 USING TITANIUM TIG ROD, INSTALLED PER BOEING SRM 5 1-10-01. 2 L 7 4 4F A20WE 1996071000344 19960710 00344 NM 1996 7 10 P5CA9600332 1 19960708 A 7110 COWL BOEING 747 747122 1384872 NM NR 4 ENGINE TORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 NR 4 ENGINE CORE COWL FRONT LATCH AREA TORN AND DEFORMED. REMOVED, FABRICATED AND INSTALLED U-CHANNEL PER BOEING SRM 51 -30-02 AND 51-10-01. 2 L 7 4 4F A20WE 1996071000345 19960710 00345 NM 1996 7 10 P5CA9600333 1 19960708 A 5400 ANGLE BOEING 747 747122 1384872 NM NR 4 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 NR 4 ENGINE PYLON UPPER END OF SUPPORT ANGLE CRACKED IN RADIUS INBOARD AND OUTBOARD STATION 221.9 ABOVE AFT ENGINE MOUNT INSIDE PANEL. INSTALLED DOUBLERS IAW BOEING SRM 54-10-03 FIG 19. 2 L 7 4 4F A20WE 1996071000346 19960710 00346 NM 1996 7 10 P5CA9600334 1 19960708 A 5414 SKIN BOEING 747 747122 1384872 NM NR 4 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 NR 4 PYLON INBOARD SIDE LOWER SKIN FLANGE CRACKED. REMOVED, FABRICATED AND INSTALLED SKIN FLANGE IAW BOEING SRM 51-30-0 2 AND 54-12-01. 2 L 7 4 4F A20WE 1996071000347 19960710 00347 NM 1996 7 10 P5CA9600335 1 19960708 A 5280 SKIN BOEING 747 747122 1384872 NM LT MLG DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEFT BODY GEAR INBOARD DOOR LOWER INNER SKIN LEADING EDGE MID SECTION CRACKED AND DEFORMED. REPAIRED PER BOEING SRM 52- 80-02. 2 L 7 4 4F A20WE 1996071000348 19960710 00348 NM 1996 7 10 P5CA9600336 1 19960708 A 5320 BRACKET BOEING 747 747122 1384872 NM NLG WW CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 HORIZONTAL ANGLE CRACKED ON VERTICAL BEAM RIGHT SIDE OF NOSE LANDING GEAR WHEEL WELL BS 320. REMOVED, FABRICATED AND IN STALLED ANGLE PER BOEING SRM 51-10-01, 51-10-02 AND 51-40-03. 2 L 7 4 4F A20WE 1996071000349 19960710 00349 NM 1996 7 10 P5CA9600337 1 19960708 A 5414 SKIN BOEING 747 747122 1384872 NM NR 1 NACELLE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 NR 1 ENGINE INBOARD FAN COWL, TOP FORWARD HINGE HAS CRACK IN SKIN TOP SURFACE. WORKED AND BLENDED OUT CRACK IAW BOEING SRM 51-10-06, TREATED AND PRIMED IAW SRM 51-40-02. 2 L 7 4 4F A20WE 1996071000350 19960710 00350 NM 1996 7 10 P5CA9600338 1 19960708 A 5400 ANGLE BOEING 747 747122 1384872 NM NR 1 NACELLE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 NR 1 OUTBOARD CORE COWL HAS CRACKED REPAIR ANGLE INSIDE TO EDGE AT BEND. REMOVED, FABRICATED AND INSTALLED ANGLE IAW BO EING SRM 51-30-02 AND 51-10-01. 2 L 7 4 4F A20WE 1996071000351 19960710 00351 NM 1996 7 10 SWAA960616 1 19960706 A 3350 6104781 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 86SW 22827 DURING SCHEDULED A1 CHECK, FOUND ALL ENTRY SERVICE DOOR EMERGENCY EXIT LIGHT BATTERY PACKS WEAK. REPLACED BATTERY PACKS PER BOEING M/M. 2 L 7 2 4F A16WE 1996071000352 19960710 00352 NM 1996 7 10 SWAA960617 1 19960705 A 5730 SKIN BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 325SW 23689 DURING SCHEDULED C3 CHECK, FOUND RT WING LOWER SKIN AT NR 6 SLAT CRACKED JUST O/B OF PREVIOUS REPAIR AND A CRACK AT EXTR EME O/B END OF SLAT. REPAIRED PER SWA RA 1-357-259 AND BOEING DRAWING 65C30133. 2 L 7 2 4F RT A16WE 1996071000353 19960710 00353 NM 1996 7 10 SWAA960618 1 19960705 A 3350 BATTERY BOEING 737 7373H4 1384600 NM BS 756 DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 314SW 23336 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT BS 756. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996071000354 19960710 00354 NM 1996 7 10 SWAA960619 1 19960704 A 3350 BATTERY BOEING 737 7375H4 138449D NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 515SW 25154 DURING SCHEDULED C4 CHECK, FOUND EMERGENCY EXIT LIGHTS INOP IN CABIN BETWEEN ROWS 15 AND 18. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996071000355 19960710 00355 NM 1996 7 10 SWAA960620 1 19960705 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 869 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 325SW 23689 DURING SCHEDULED C3 CHECK, FOUND FUSLAGE SKIN CRACKED AT BS 869, S24R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996071000356 19960710 00356 NM 1996 7 10 SWAA960621 1 19960704 A 5330 SKIN BOEING 737 7372H4 138448C NM AFT ENTRY AREA CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 29SW 21340 DURING SCHEDULED A CHECK, FOUND AFT ENTRY DOOR UPPER HINGE SKIN CUTOUT CRACKED AT LOWER RADIUS. REPAIRED PER SWA RA T1- A52-005. 2 L 7 2 4F A16WE 1996071000357 19960710 00357 NM 1996 7 10 SWAA960622 1 19960704 A 3397 WIRE BOEING 737 7373H4 1384600 NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 366SW 26577 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOP IN CABIN BETWEEN ROWS 4 AND 7. RECONNECTED WIRE S AND OPERATION CHECKED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996071000358 19960710 00358 NM 1996 7 10 SWAA960623 1 19960702 A 3350 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 628SW DURING PREFLIGHT, FOUND LEFT OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996071000359 19960710 00359 NM 1996 7 10 SWAA960624 1 19960702 A 3350 WIRE BOEING 737 7375H4 138449D NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 510SW 24187 DURING PREFLIGHT, FOUND EMERGENCY EXIT LIGHTS INOP AT ROW 12. FOUND AND RECONNECTED WIRE AT SOCKET PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996071000360 19960710 00360 NM 1996 7 10 SWAA960625 1 19960702 A 5315 FLOOR BEAM BOEING 737 7373H4 1384600 NM BS 294 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORROSION AT BS 294, LBL 10 AND AT RBL 35, WL 208. REPLACED FLOOR BEAM CHORD PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996071000361 19960710 00361 NM 1996 7 10 SWAA960626 1 19960702 A 5315 FLOOR BEAM BOEING 737 7373H4 1384600 NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORROSION AT BS 328, LBL 11, WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996071000362 19960710 00362 NM 1996 7 10 SWAA960627 1 19960702 A 5315 FLOOR BEAM BOEING 737 7373H4 1384600 NM BS 967 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 967, RBL 28, WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996071000363 19960710 00363 NM 1996 7 10 SWAA960628 1 19960702 A 5320 65516989 SPLICE BOEING 737 7373H4 1384600 NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICES CRACKED AT BS 907, S4L AND S4R. REPLACED BOTH PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996071000364 19960710 00364 NM 1996 7 10 SWAA960629 1 19960702 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 995 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 995, RBL 11, WL 226. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996071000365 19960710 00365 NM 1996 7 10 SWAA960630 1 19960702 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 807/847 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 807 AND 847, AT STRINGER 9L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996071000366 19960710 00366 NM 1996 7 10 SWAA960631 1 19960707 A 5320 STRAP BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 89SW 22904 DURING SCHEDULED 1/2 D-CHECK, FOUND CRACK UNDER VERTICAL STRAP AT RBL 5, WL 192, BS 178. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996071000367 19960710 00367 NM 1996 7 10 SWAA960632 1 19960707 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 967 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 89SW 22904 DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER 25L DAMAGED AT BS 967. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996071000368 19960710 00368 NM 1996 7 10 SWAA960633 1 19960707 A 5315 FLOOR BEAM BOEING 737 7372H4 138448C NM BS 344/294 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 89SW 22904 DURING SCHEDULED 1/2 D-CHECK, FOUND FWD GALLEY FLOOR BEAM UPPER SURFACE CORRODED AT BS 344, RBL 3 TO 10. ALSO, BS 294, 294.5. REPLACED T-CAP PER BOEING SRM. 2 L 7 2 4F A16WE 1996071000369 19960710 00369 NM 1996 7 10 SWAA960634 1 19960707 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 294.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 89SW 22904 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR SUPPORT ANGLE AT FWD GALLEY CORRODED AT BS 294.5. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996071000370 19960710 00370 NM 1996 7 10 SWAA960635 1 19960707 A 5315 FLOOR BEAM BOEING 737 7372H4 138448C NM BS 294.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 89SW 22904 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM AT FWD GALLEY CORRODED AT BS 294.5, LBL 11 AND LBL 19. REPLACED T-CAP PE R BOEING SRM. 2 L 7 2 4F A16WE 1996071000371 19960710 00371 NM 1996 7 10 UPS96220583 1 19960706 A 2613 OVERHEAT DETECT BOEING 727 727185C 138406N NM NR 1 ENGINE DEFECTIVE A IPXA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 954UP 19827 INSPECTION TYPE NA, NR 1 ENG FIRE DETECTION GROUND FAULT LIGHT STEADY IN FLIGHT, FIRE WARNING BELL SOUNDED. GROUND FAUL T WAS EXTINGUISHED. REMOVED AND REPLACED NR 1 ENG FIRE OVERHEAT DETECTOR, OPS CHK GOOD PER M/M 26-11-00. 2 L 7 3 4F A3WE 1996071000372 19960710 00372 NM 1996 7 10 UPS96220584 1 19960507 A 5311 FRAME BOEING 727 72725C 138400H NM BS 760 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE-C, RIGHT SIDE FRAME 760, FWD EDGE OF RT FWD EMERGENCY EXIT HAS TWO SMALL AREAS OF INTERGRANULAR CORROSIO N ON INNER FLANGE STRAP AT STRINGERS 16R AND 17R. REMOVED FASTENERS AND CORROSION PER SRM 51-30-2 AND 51-10-6, BLENDED AREA AND FINISHED PER DHC SK 946-750 AND SRM 51-10-2, INSTALLED FASTENERS PER SRM 57-30-2. 2 L 7 3 4F A3WE 1996071000373 19960710 00373 NM 1996 7 10 UPS96220585 1 19960521 A 5315 FLOOR BEAM BOEING 727 72725C 138400H NM FS 480 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE-C, FLOOR BEAM CORRODED AT STA 480 FROM BL 0 TO RBL 48. CUT OUT DAMAGED AREA AT STA 480, FROM LBL 12 TO RBL 65 PER SRM 53-10-8, FAB'D AND INSTALLED UPPER CAP REPAIR PER SRM 53-10-8 FIG 5 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996071000374 19960710 00374 NM 1996 7 10 UPS96220586 1 19960520 A 5220 SKIN BOEING 727 72725C 138400H NM RT AFT EMER EXT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE-C, RT AFT EMERGENCY EXIT HAS TWO OPEN HOLES AND ONE HOLE IS CRACKED OUT TO THE EDGE OF SKIN. CUT OUT DA MAGE ON RT AFT EXIT DOOR PER SRM 52-40-2 FIG 1, FAB'D DOUBLER AND INSTALLED IAW SRM 52-40-11, 52-40-2 FIG 1 AND SRM 51-3 0-2. 2 L 7 3 4F A3WE 1996071000375 19960710 00375 NM 1996 7 10 UPS96220587 1 19960508 A 5751 SPAR BOEING 727 72725C 138400H NM LT OUTBD AILERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE-C, LT O/B AILERON SPAR UPPER CHORD IS CRACKED O/B OF NR 2 HINGE. REMOVED AND REPLACED UPPER CHORD IAW S RM 51-10-1, 51-30-2 AND BOEING DWG 65-21723. 2 L 7 3 4F A3WE 1996071000376 19960710 00376 NM 1996 7 10 UPS96220588 1 19960509 A 5751 SPAR WEB BOEING 727 72725C 138400H NM LT OUTBD AILERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE-C, LT O/B AILERON SPAR WEB IS CRACKED AT O/B TAB ROD AREA THROUGH HOLE. TRIMMED OUT DAMAGED AREA, FABRI CATED REPAIR AND INSTALLED IAW SRM 51-40-2 FIG 1. 2 L 7 3 4F A3WE 1996071000377 19960710 00377 NM 1996 7 10 UPS96220589 1 19960509 A 5320 FITTING BOEING 727 72725C 138400H NM BS 870 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE-C, RT FUSELAGE TERMINAL FITTING BS 870 HAS A 1 INCH CRACK EXTENDING BETWEEN TWO FASTENERS FWD, OUTER FLA NGE, SIX INCHES ABOVE STR 13R. REMOVED AND REPLACED RT 870 TERMINAL FITTING PER BOEING DWG 65C-23231 AND UPS EO 727-531 0-3056. 2 L 7 3 4F A3WE 1996071000378 19960710 00378 NM 1996 7 10 UPS96420590 1 19960626 A 5315 FLOOR BEAM BOEING 747 747123F NM BS 1580 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE-C, FLOOR BEAM UPPER CHORD BS 1580 CORRODED AT LBL 70 TO 85. CORROSION AT FLOOR BEAM UPPER CHORD BS 1580 LBL 70 TO 85 OUT OF LIMITS IAW SRM 53-10-01. REPAIRED FLOOR BEAM UPPER CHORD BS 1580 LBL 70 TO 85 IAW SRM 51-40-04 FIG 1. 2 L 7 4 4F A20WE 1996071000379 19960710 00379 NM 1996 7 10 UPS96420591 1 19960626 A 5315 FLOOR BEAM BOEING 747 747123F NM BS 500 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE-C, FLOOR BEAM UPPER CHORD BS 1500 CORRODED AT LBL 85. CORROSION AT FLOOR BEAM UPPER CHORD BS 1500 LBL 8 5 OUT OF LIMITS IAW SRM 53-10-01. REPAIRED FLOOR BEAM UPPER CHORD BS 1500 LBL 85 IAW SRM 51-40-04 FIG 1. 2 L 7 4 4F A20WE 1996071000380 19960710 00380 NM 1996 7 10 UPS96420592 1 19960626 A 5315 FLOOR BEAM BOEING 747 747123F NM BS 400 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE-C, UPPER CHORD CORRODED BS 400 BETWEEN RBL 11 TO 57. CORROSION REWORKED IAW SRM 51-10-01, REWORKED STRU CTURALLY ACCEPTABLE IAW APPROVAL: UPS AMS-96-0153RE. 2 L 7 4 4F A20WE 1996071000381 19960710 00381 NM 1996 7 10 UPS96420593 1 19960704 A 5751 WEB BOEING 747 747123F NM RT INBD AILERON DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE-C, RT INB AILERON, TWO FASTENERS OF OUTBD WEB MISSING AND TWO FASTENERS ARE LOSE. REPAIRED WEB OF INB A ILERON IAW SRM 51-40-02. 2 L 7 4 4F A20WE 1996071000382 19960710 00382 NM 1996 7 10 UPS96420594 1 19960704 A 5720 WEB BOEING 747 747123F NM WS 1140 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE-C, RT WING LE FOUND CRACK IN WEB OF D-BEAM AT WS 1140. REPAIRED WEB OF D-BEAM IAW SRM 51-40-02. 2 L 7 4 4F A20WE 1996071000383 19960710 00383 NM 1996 7 10 UPS96420595 1 19960627 A 5320 FITTING BOEING 747 747123F NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE-C, FOUND CRACK IN LOWER FLANGE FROM AFT LATCH TRUSS FITTING POS 13 OF AFT CARGO DOORSILL. REPAIRED AFT LATCH TRUSS FITTING IAW B747-5310-0191, APPENDIX E. 2 L 7 4 4F A20WE 1996071000384 19960710 00384 NM 1996 7 10 UPS96420596 1 19960628 A 5315 FLOOR BEAM BOEING 747 747123F NM BS 2240 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE-C, FLOOR BEAM UPPER CHORD CORRODED AT BS 2240 BETWEEN 33 TO 98. CORRODED UPPER CHORD OUT OF LIMITS IAW SRM 53-10-01, REPLACED CHORD IAW SRM 51-40-03 FIG 1. 2 L 7 4 4F A20WE 1996071000385 19960710 00385 WP 1996 7 10 UPS96820578 1 19960705 A 5320 3758519501 FITTING DOUG DC8 DC871F 302199D WP BS 793 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE: BCK. KEEL CAP BATHTUB FITTING AT FS 793 RT HAS VERTICAL CRACK, NEED AOG TO REMOVE 4 BOLTS IN KEEL BEA M FOR REMOVAL AND REPLACEMENT OF FITTING. NOTE: BOLTS ARE IN FUEL TANK. REMOVED AND REPLACED 4 BOLTS IN KEEL BEAM FIT TING AT FS 793 RT. CLEANED AND SEALED IAW 28-10-01. MM LEAK CHECK DUE, LEAK CHECK GOOD. 2 L 7 4 4F RT 4A25 1996071000386 19960710 00386 WP 1996 7 10 UPS96820579 1 19960706 A 5220 2707316 STOP DOUG DC8 DC871F 302199D WP LT EMER EXIT BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE-N/A, LT OVERWING EMERGENCY EXIT HATCH STOP BROKEN FROM BOTTOM OF HATCH, REQ NR A475379. 2 L 7 4 4F RT 4A25 1996071000387 19960710 00387 WP 1996 7 10 UPS96820580 1 19960705 A 2910 57155A STANDBY PUMP DOUG DC8 DC871F 302199D WP RUDDER LEAKING A IPXA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 706UP 46056 INSPECTION TYPE-N/A, AT FL35 HYD SYS PRESS WENT TO ZERO, HYD QTY DROPPED TO JUST ABOVE THE X-POSITION AND THE RUDDER AND AILERON MANUAL CONTROL LIGHTS ILLUMINATED. HYD FAILURE CHKLIST ACCOMPLISHED. FLUID BEGAN TO DECREASE RAPIDLY WITH AUX PUMP ON. FOUND STANDBY RUDDER PUMP LEAKING FROM DRAIN LINE. REPLACED STANDBY RUDDER PUMP AND TAGGED, REMOVED PART HOL D FOR EVALUATION. 2 L 7 4 4F RT 4A25 1996071000388 19960710 00388 WP 1996 7 10 UPS96820582 1 19960705 A 2121 FAN DOUG DC8 DC873F 302199F WP AIR COND BAY FAILED A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE-A+, RECIR FAN FAILED, FILLED AIR COND BAY WITH SMOKE. FLT CREW AND JUMP SEATERS EVACUATED TILL LOCATION OF SMOKE WAS FOUND. PULLED AND COLLARED RECIRC, FAN, C/IS DEFERRED RECIRC FAN PER MEL 21-16 M-112173. 2 L 7 4 4F RT 4A25 1996071000390 19960710 00390 NE 1996 7 10 HEEA967434 1 19960621 A 6210 7615009043050 TIP CAP SKRSKY S76 S76A 8143006 NE M/R TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31219 760230 TIP CAP HAS THE SKIN TORN NEXT TO THE ABRASION STRIP ON THE LOWER SIDE. 1 G 7 2 3U H1NE 1996071000391 19960710 00391 SW 1996 7 10 HEEA967436 1 19960621 A 2436 206075447007 REGULATOR BELL 206 206L1 1182107 SW DC SYS FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1078C 45392 GENERATOR WOULD NOT COME ON LINE AND FAILED START BENCH TEST. 1 G 7 1 3U H2SW 1996071000392 19960710 00392 SW 1996 7 10 HEEA967437 1 19960621 A 6220 412010190103 SPINDLE 412010100193 BELL 412 412 1182202 SW M/R DEBONDED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 5728 AAD00099 33113 DAMPER BEARING UNBONDED. 1 G 7 2 4U H4SW 1996071000393 19960710 00393 SW 1996 7 10 HEEA967438 1 19960621 A 7931 90093003 INDICATOR BELL 206 206B 1181511 SW ENG OIL MALFUNCTION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2275Q 3625 PRESSURE READS LOW AND TEMP READS HIGH. 1 G 7 1 3U H2SW 1996071000394 19960710 00394 SW 1996 7 10 HEEA967439 1 19960621 A 7931 206075677103 INDICATOR BELL 206 206L3 1182108 SW ENG OIL READS HIGH E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 6610E 51424 PSI READS HIGH AT HIGH RANGE. 1 G 7 1 3U H2SW 1996071000395 19960710 00395 SW 1996 7 10 HEEA967440 1 19960621 A 7931 206075187003 INDICATOR BELL 206 206B 1181511 SW ENG OIL STICKS E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2275Q 3625 PSI NEEDLE STICKS AT 90 PSI. SENT TO MASCO FOR WARRANTY REPAIR. 1 G 7 1 3U H2SW 1996071000397 19960710 00397 SW 1996 7 10 HEEA967442 1 19960621 A 5512 206023119151A SKIN BELL 206 206L1 1182107 SW STAB ASSY DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 DURING PAINT PREPARATION FOUND THAT EXISTING PRIMER COAT WAS PEELING OFF STABILIZER AND THAT OUR PRIMER COAT WOULD NOT A DHERE TO EXISTING PRIMER COAT. BLASTED STABILIZER ASSY TO REMOVE EXISTING PRIMER COAT. FOUND THAT STABILIZER SKIN HAD SEVERALSMALL DENTS. AREA WHERE SKIN WAS SANDED ON WITH HEAVY GRIT PAPER AND A DEEP SCRATCH COMING FROM AN INSERT FOR R/ H LOWER SUPPORT PLATE. 1 G 7 1 3U H2SW 1996071000398 19960710 00398 SW 1996 7 10 HEEA967443 1 19960621 A 6330 206033554101 LINK ASSY BELL 206 206L3 1182108 SW XMSN MOUNT GALLED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8589X 51487 INSIDE BEARING GALLED. 1 G 7 1 3U H2SW 1996071000399 19960710 00399 SW 1996 7 10 HEEA967444 1 19960621 A 6330 206033554101 LINK ASSY BELL 206 206L1 1182107 SW XMSN MOUNT WORN EXCESS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2245Y 45751 BUSHING IS WORN. SENT TO LORD MANUFACTURING FOR EXCHANGE. 1 G 7 1 3U H2SW 1996071000400 19960710 00400 SW 1996 7 10 HEEA967445 1 19960621 A 6330 206033554101 LINK ASSY BELL 206 206L1 1182107 SW XMSN MOUNT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5748Q 45499 BEARING IS BAD AND RUBBER IS MISSING. 1 G 7 1 3U H2SW 1996071000401 19960710 00401 SW 1996 7 10 HEEA967446 1 19960621 A 6330 206033554101 LINK ASSY BELL 206 206L1 1182107 SW XMSN MOUNT DETERIORATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3892R 45594 RUBBER IS DETERIORATED. 1 G 7 1 3U H2SW 1996071000402 19960710 00402 SW 1996 7 10 HEEA967447 1 19960621 A 6330 206033554101 LINK ASSY BELL 206 206L1 1182107 SW XMSN MOUNT BEARING SEPARATE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2761X 45283 BEARING IS SEPARATED. 1 G 7 1 3U H2SW 1996071000403 19960710 00403 SW 1996 7 10 HEEA967448 1 19960621 A 6330 206033554101 LINK ASSY BELL 206 206L3 1182108 SW XMSN MOUNT BEARING FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8589X 51487 BEARING IS DETERIORATED. 1 G 7 1 3U H2SW 1996071000404 19960710 00404 SW 1996 7 10 HEEA967449 1 19960621 A 6330 206033554101 LINK ASSY BELL 206 206L1 1182107 SW XMSN MOUNT DETERIORATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2764F 45279 BEARING RUBBER IS DETERIORATED. 1 G 7 1 3U H2SW 1996071000405 19960710 00405 SW 1996 7 10 HEEA967450 1 19960621 A 6330 206033554101 LINK ASSY BELL 206 206L 1181522 SW XMSN MOUNT WORN RUBBER E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7077B 52037 WORN RUBBER. 1 G 7 1 3U H2SW 1996071000406 19960710 00406 SW 1996 7 10 HEEA967451 1 19960621 A 6330 206033503001 LINK ASSY BELL 206 206L1 1182107 SW XMSN MOUNT UNBONDED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2125M 45649 RUBBER UNBONDED. 1 G 7 1 3U H2SW 1996071000407 19960710 00407 SW 1996 7 10 HEEA967452 1 19960621 A 6330 206033554101 LINK ASSY BELL 206 206L1 1182107 SW XMSN MOUNT UNBONDED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2125M 45649 RUBBER UNBONDED. 1 G 7 1 3U H2SW 1996071000408 19960710 00408 SW 1996 7 10 HEEA967453 1 19960621 A 6330 206033554101 LINK ASSY BELL 206 206L1 1182107 SW XMSN MOUNT WORN EXCESS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2251Z 45756 WORN BEARING. 1 G 7 1 3U H2SW 1996071000409 19960710 00409 SW 1996 7 10 HEEA967454 1 19960621 A 6330 206033554101 LINK ASSY BELL 206 206L3 1182108 SW XMSN MOUNT CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31073 51519 CORROSION IN UPPER BEARING. 1 G 7 1 3U H2SW 1996071000410 19960710 00410 SW 1996 7 10 HEEA967455 1 19960621 A 6330 206033554101 LINK ASSY BELL 206 206L1 1182107 SW XMSN MOUNT CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2250U 45754 ELASTOMER BEARING DETERIORATED. 1 G 7 1 3U H2SW 1996071000411 19960710 00411 1996 7 10 HEEA967457 4 19960621 A 2562 ELT10 ELT NARCO BOLKMS 105 BO105S 5626006 EU COCKPIT WONT TEST E HEEA K NONE L NO TEST NR NOT REPORTED 1 SW 03 911HM S683 WILL NOT TEST. SENT TO NARCO AVIONICS FOR INSPECTION AND REPAIR. 1 G 7 2 3U H3EU 1996071000412 19960710 00412 1996 7 10 HEEA967458 4 19960621 A 2562 ELT10 ELT NARCO BELL 206 206L1 1182107 SW COCKPIT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 10761 45381 CAME ON IN FLIGHT AND WOULD NOT TURN OFF WITH REMOTE SWITCH. SENT 1 G 7 1 3U H2SW 1996071000413 19960710 00413 SW 1996 7 10 HEEA967460 1 19960621 A 7712 412075008113 INDICATOR BELL 412 412 1182202 SW ENG TORQUE FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 108X 33115 #2 NEEDLE WON'T COME UP. 1 G 7 2 4U H4SW 1996071000414 19960710 00414 SW 1996 7 10 HEEA967461 1 19960621 A 3212 214073929103 VALVE BELL 230 230 1182149 SW EMERG FLOAT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 3115 23009 VALVE IS DEFECTIVE. (DEFECTIVE PART NUMBER INSTALLED AS PER BELL HELICOPTERS) 1 G 7 2 3U NC H9SW 1996071000415 19960710 00415 NE 1996 7 10 HEEA967462 1 19960621 A 2432 6013211 EMERGENCY POWER SKRSKY S76 S76A 8143006 NE CELLS DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 UNIT HAS 6 DEFECTIVE CELLS. SENT TO MATHEWS RECHARGEABLE BATTERY FOR INSPECTION AND REPAIR. 1 G 7 2 3U H1NE 1996071000416 19960710 00416 EU 1996 7 10 HEEA967463 1 19960621 A 6520 350A33215300 BEARING SNIAS 350 AS350B2 8680813 EU T/R GR BOX SEPARATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4000L 152 2873 RUBBER SEPARATED. 1 G 7 1 3U H9EU 1996071000417 19960710 00417 1996 7 10 HEEA967464 4 19960621 A 3417 214175421101 COMPUTER BELL 214 214ST 1182106 SW COCKPIT INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 AIR DATA COMPUTER INOPERATIVE. 2 G 7 2 4U H10SW 1996071000418 19960710 00418 NE 1996 7 10 HEEA967465 2 19960621 A 7421 4053T22P01 IGNITOR BELL 214 214ST 1182106 SW GE CT7TS CT72A 30030 NE ENG CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5748M 28102 IGNITOR IS CRACKED. (WORN AND CRACKED) 2 G 7 2 4U 4 U H10SW E8NE 1996071000419 19960710 00419 NE 1996 7 10 HEEA967467 1 19960621 A 6730 7630103902102 ACTUATOR SKRSKY S76 S76A 8143006 NE SERVO SYS INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 4253S 760035 INOPERATIVE. 1 G 7 2 3U H1NE 1996071000427 19960710 00427 NM 1996 7 10 9614706310 1 19960705 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 670US 24225 DURING LINE CHECK, FOUND TWO AFT RIGHT OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1996071000428 19960710 00428 NM 1996 7 10 9614716608 1 19960708 A 3350 POWER SUPPLY BOEING 747 747151 1384891 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 608US 19765 DURING LINE CHECK, FOUND EMERGENCY EXIT LIGHTS BY DOOR 1L INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996071000429 19960710 00429 WP 1996 7 10 9614729995 1 19960706 A 3350 60030451 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8978E 47327 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, O PERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996071000430 19960710 00430 WP 1996 7 10 9614739923 1 19960707 A 3260 DOWNLOCK SWITCH DOUG DC9 DC932 3022066 WP LT MLG CORRODED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 927RC 47469 DURING APPROACH INTO YEG, THE LEFT MAIN LANDING GEAR RED UNSAFE LIGHT REMAINED ON AFTER GEAR WAS EXTENDED. GO-AROUND PR OCEDURES WERE EXECUTED AND CREW REQUESTED EMERGENCY EQUIPMENT ON STANDBY AS A PRECAUTION. GEAR WAS VISUALLY CONFIRMED T HROUGH PERISCOPE TO BE DOWN AND LOCKED. AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE FOUND MOISTURE AND SLIGHT PIN CORROSION ON LEFT MAIN GEAR DOWNLOCK SWITCH. CLEANED SWITCH, OPERATIONAL CHECK NORMAL ON SYSTEM CHECK. 2 L 7 2 4F A6WE 1996071000431 19960710 00431 WP 1996 7 10 9614749604 1 19960707 A 2130 DUCT DOUG DC9 DC932 3022066 WP ACM DISCHARGE FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 GL 01 604NW 47222 LOSS OF CABIN PRESSURIZATION OCCURRED EN ROUTE. FLIGHT DIVERTED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND RIGHT AIR CYCLE MACHINE DISCHARGE DUCT BLOWN. REPLACED DUCT, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996071000432 19960710 00432 WP 1996 7 10 9614759947 1 19960705 A 3620 GASKET DOUG DC9 DC931 3022065 WP RT AC DUCT BLOWN A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 8938E 47161 TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BLOWN GASKET AT RIGHT AIR CONDITIONING HIGH TEMPERATURE SENSOR. REPLACED GASKET AND LEFT HIGH TEMPER ATURE SENSOR AS A PRECAUTION, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996071000433 19960710 00433 NM 1996 7 10 9614842275 1 19960705 A 3260 656021132 ACCESSORY BOX BOEING 727 727251 138408H NM LT MLG MALFUNCTIONED A A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 275US 21154 DURING GEAR RETRACTION, THE LEFT GEAR ON SAFE INDICATOR REMAINED ILLUMINATED. GEAR WAS CYCLED DOWN AND UP, ALL GEAR IND ICATIONS WERE NORMAL. REPLACED LANDING GEAR ACCESSORY BOX AND ADJUSTED LEFT MAIN LANDING GEAR SENSOR. PERFORMED GEAR O PERATIONAL CHECK, CHECKED OK. 2 L 7 3 4F A3WE 1996071000434 19960710 00434 WP 1996 7 10 9614859911 1 19960705 A 3350 6011779 BATTERY PACK DOUG DC9 DC931 3022065 WP LT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 961N 47405 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AND BATTERIES , OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996071000435 19960710 00435 WP 1996 7 10 9614869911 1 19960705 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 961N 47405 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS IN MID CABIN INOPERATIVE. REPLACED BATTERIES , OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996071000436 19960710 00436 WP 1996 7 10 9614879954 1 19960707 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP TAIL COMPT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 921RW 47164 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS IN TAIL COMPARTMENT INOPERATIVE. REPLACED BA TTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996071000437 19960710 00437 WP 1996 7 10 9614889991 1 19960705 A 3350 DWG41B004AD07G3 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8957E 47215 DURING PERIODIC CHECK, FOUND FORWARD OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996071000438 19960710 00438 NE 1996 7 10 96FDEAO1188 2 19960708 A 7321 ECU AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680C2A5 NE NR 1 ENGINE FAILED A A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 650FE 726 NR 1 ENGINE FAILED ON ARRIVAL TO MEM SOMEWHERE DURING THE DECENT. WHILE AT IDLE POWER A RELIGHT WAS ATTEMPTED AND A REL IGHT IE EGT NOSE FOR ABOUT 5 SECONDS THEN THERE WAS A SHUTDOWN AGAIN. REMOVED AND REPLACED NR 1 ENGINE ECU IAW A300-600 MM SUPPLEMENT 73-21-01, NR 1 ECU OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A35EU E13NE 1996071000439 19960710 00439 NM 1996 7 10 96FDEAO1205 1 19960702 A 5330 SKIN BOEING 727 72725C 138400H NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 116FE 19298 FUSE AFT/LWR CORNER OF PILOTS NR 3 WINDOW SKIN CRACKED. DOUBLER INSTALLED PER SRM 53-30-3. 2 L 7 3 4F A3WE 1996071000440 19960710 00440 NM 1996 7 10 96FDEAO1206 1 19960702 A 5330 SKIN BOEING 727 72725C 138400H NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 116FE 19298 FUSE SKIN CRACKED I/B LWR CORNER OF PILOTS NR 4 WINDOW. DOUBLER INSTALLED AT LWR I/B CORNER OF PILOTS NR 4 WINDOW PER S RM 53-30-3. 2 L 7 3 4F A3WE 1996071000441 19960710 00441 NM 1996 7 10 96FDEAO1208 1 19960705 A 5315 FLOOR BEAM BOEING 727 727233 138408A NM BS 870 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 276FE 22041 UPPER LOBE BS 870, RBL 49 TO 51 CORROSION ON TOP FLANGE OF FLOOR BEAM. REMOVED CORROSION PER SRM 51-10-6, THICKNESS REA DINGS ORIG 0.225, READING AFTER CORROSION REMOVAL 0.019. TREATED, PRIMED AND REWORKED AREA. 2 L 7 3 4F RT A3WE 1996071000442 19960710 00442 NM 1996 7 10 96FDEAO1209 1 19960702 A 5320 CENTER POST BOEING 727 72725C 138400H NM COCKPIT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 116FE 19298 FUSE CENTER POST BETWEEN PILOT AND COPILOTS NR 1 WINDOWS CRACKED RT 2RD SCREW DOWN PILOTS NR 4 WINDOW. 2 L 7 3 4F A3WE 1996071000443 19960710 00443 1996 7 10 ABXA9600589 2 19960705 A 7261 81196501 OIL LINE DOUG DC9 DC931 3022065 WP NR 2 ENG GEARBOX DEFECTIVE A ABXA K NONE K J FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 23 937AX 47074 AT 100 FEET AGL ON APPROACH, RIGHT OIL PRESSURE LOW LIGHT ILLUMINATED AND RIGHT OIL PRESSURE GAUGE INDICATED 23 PSI. OI L QUANTITY DROPPED TO ZERO AND ENGINE WAS SHUTDOWN ON ROLLOUT. REPLACED A LEAKING OIL LINE AT THE NR 2 ENGINE GEARBOX. GROUND RAN ENGINE AND NO LEAKS WERE NOTED. 2 L 7 2 4F A6WE 1996071000444 19960710 00444 WP 1996 7 10 ABXA9600590 1 19960702 A 3520 101571 OXY FLEX LINE DOUG DC8 DC863 302198A WP COCKPIT RUPTURED A ABXA B EMER. DESCENT O OTHER CR CRUISE 1 GL 23 812AX 46126 OBSERVER'S FLEXIBLE OXYGEN LINE TO THE REGULATOR RUPTURED INFLIGHT. CREW INITIATED DESCENT TO 21,000 FEET. REPLACED OB SERVER'S FLEXIBLE OXYGEN LINE TO THE REGULATOR. 2 L 7 4 4F 4A25 1996071000445 19960710 00445 WP 1996 7 10 ABXA9600591 1 19960705 A 2170 21D101 COALESCER BAG DOUG DC9 DC931 3022065 WP RIGHT DEFECTIVE A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 23 906AX 47072 STRONG SMELL OF HOT PLASTIC IN CABIN AND COCKPIT ON CLIMBOUT, SMELL WENT AWAY ABOVE 18,000 FEET AND RETURNED ON DESCENT BELOW 18,000 FEET. REPLACED RIGHT COALESCER BAG, GROUND RAN PACK AND NO ODORS WERE NOTED. 2 L 7 2 4F A6WE 1996071000446 19960710 00446 NM 1996 7 10 CALA9600972 1 19960706 A 2612 899321 FIRE LOOP BOEING 737 7373T0 1384582 NM APU INOPERATIVE A CALA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SW 09 12327 23457 THE APU FIRE WARNING LIGHT ILLUMINATED DURING AN INFLIGHT START SHORTLY BEFORE TOUCHDOWN. THE APU FIRE BOTTLE WAS DISCH ARGED AND THE FIRE LIGHT EXTINGUISHED. INSPECTION PLACARD THE APU FIRE DETECTION SYSTEM AND FIRE EXTINGUISHER INOPERAT IVE. THE WARNING WITH FIRE BELL WAS REPEATED DURING CLIMB ON A SUBSEQUENT FLIGHT. THE APU FIRE DETECTION CIRCUIT BREAK ERS WERE PULLED, SINCE THE APU WAS ON PLACARD AND NOT OPERATING. THE WARNING CEASED AND THE FLIGHT WAS CONTINUED WITHOU T FURTHER PROBLEM. THE APU FIRE LOOP ELEMENT AND FIRE BOTTLE WAS REMOVED AND REPLACED. THE APU FIRE DETECTION SYSTEM T ESTED GOOD. 2 L 7 2 4F RT A16WE 1996071000447 19960710 00447 WP 1996 7 10 CALA9600973 1 19960706 A 3610 9787344 FAN AIR VLV DOUG DC10 DC1030 3023501 WP NR 2 PNEU SYS INOPERATIVE A CALA A D J UNSCHED LANDING RETURN TO BLOCK DUMP FUEL J WARNING INDICATION CL CLIMB 1 SW 09 14063 12768 10833 47864 THE NR 2 PNEUMATIC SUPPLY TEMP HIGH LIGHT ILLUMINATED DURING CLIMBOUT OF FRA NR 1 PNEUMATIC SYSTEM WAS PLACARD INOPERATI VE. THE NR 2 PNEUMATIC SUPPLY WAS SHUT OFF AND THE LIGHT EXTINGUISHED. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED T O FRA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 FAN AIR VALVE AT FAULT. THE FAN AIR VALVE WAS REPLA CED. AN ENGINE POWER ASSURANCE RUN WAS PERFORMED AND ALL TEMPERATURE INDICATIONS WERE NORMAL. 2 L 7 3 4F A22WE 1996071000448 19960710 00448 NM 1996 7 10 CALA9600974 1 19960708 A 3260 LOGIC CARDS BOEING 737 737291 138448W NM LOGIC SHELF INOPERATIVE A CALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 17252 20362 THE RED NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED WHEN GEAR WAS RETRACTED AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. A NOSE GEAR SWING WAS PERFORMED IAW MM 32-61-00, PAGE 501 TO 504 AND ALL GEAR OP ERATION AND INDICATIONS WERE NORMAL. THE M983 AND M1215 LOGIC CARDS WERE REMOVED AND REPLACED AS A PRECAUTIONARY MEASUR E PER MM 32-09-20. BOTH CARDS TESTED NORMAL. ANOTHER GEAR SWING WAS PERFORMED AFTER CARD REPLACEMENT WITH NO FAULTS NO TED. 2 L 7 2 4F A16WE 1996071000449 19960710 00449 NM 1996 7 10 CALA9600975 1 19960614 A 5330 SKIN BOEING 737 737291 138448W NM BS 500-510 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17252 20362 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 500 TO 510 BETWEEN STRINGER 3L AND 4L. THE DENTED AREA WAS REMOVED, FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, 51-10-2 AND 51-30-2. 2 L 7 2 4F A16WE 1996071000450 19960710 00450 NM 1996 7 10 CALA9600976 1 19960612 A 5330 SKIN BOEING 737 737291 138448W NM CARGO DR AREA CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17252 20362 INSPECTION FOUND FUSELAGE SKIN CORRODED AROUND FASTENERS BELOW AFT CARGO DOOR. THE CORRODED AREA WAS CUT OUT, A SKIN SE CTION, FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, 51-10-6 AND 51-10-2. 2 L 7 2 4F A16WE 1996071000451 19960710 00451 NM 1996 7 10 CALA9600977 1 19960617 A 5313 STRINGER BOEING 737 737291 138448W NM BS 400 DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17252 20362 INSPECTION FOUND FUSELAGE SKIN DENTED AND STRINGER DAMAGED AT STA 400, STRINGER 18L. THE DAMAGED AREA OF STRINGER WAS R EMOVED IAW SRM 53-10-3. THE SKIN WAS RETURNED TO ORIGINAL CONTOUR IAW SRM 51-70, FIGURE 4. REPAIR PARTS FOR STRINGER W ERE FABRICATED AND INSTALLED IAW SRM 53-10-3, 51-10-2 AND 51-30-2. 2 L 7 2 4F A16WE 1996071000452 19960710 00452 NM 1996 7 10 CALA9600978 1 19960619 A 5330 SKIN BOEING 737 737291 138448W NM BS 992 CREASED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17252 20362 INSPECTION FOUND FUSELAGE SKIN CREASED AT STA 992 BETWEEN STRINGER 27L AND 27R. THE DAMAGED SECTION OF SKIN WAS REMOVED , A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 6, 51-10-2 AND 51-30-2. 2 L 7 2 4F A16WE 1996071000453 19960710 00453 NM 1996 7 10 CALA9600979 1 19960612 A 5330 SKIN BOEING 737 737291 138448W NM GALLEY DR AREA CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17252 20362 INSPECTION FOUND A CRACK IN SKIN AT FORWARD GALLEY DOOR FORWARD LOWER CUTOUT. THE CRACK WAS STOP DRILLED IAW SRM 51-10- 1, FILLER, DOUBLER AND TRIPLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, 51-10-2 AND 51-30-2. 2 L 7 2 4F A16WE 1996071000454 19960710 00454 NM 1996 7 10 CALA9600980 1 19960619 A 5311 FRAME BOEING 737 737291 138448W NM BS 460 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17252 20362 INSPECTION FOUND FORWARD CARGO PIT FRAME CRACKED AT STA 460 BETWEEN STRINGER 20L AND 21L. THE CRACKED SECTION OF FRAME WAS REMOVED IAW SRM 51-30-2 AND A NEW FRAME WAS INSTALLED IAW BOEING DRAWING NR 65C25113. 2 L 7 2 4F A16WE 1996071000455 19960710 00455 NM 1996 7 10 CALA9600981 1 19960621 A 5713 STRINGER BOEING 737 737291 138448W NM WBL 92.5 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17252 20362 INSPECTION FOUND A CRACK IN LT WING STRINGER 13 AT RIB MOUNTING POINT, FIRST RIB OUTBOARD OF WING ROOT, WBL 92.5. THE C RACK WAS STOP DRILLED IAW BOEING DRAWING NR 65C34533. A STRINGER REPAIR WAS FABRICATED AND INSTALLED IAW BOEING DRAWING NR 65C34533. THE SKIN FASTENERS WERE SEALED IAW MM 28-11-0. LEAK CHECK WAS GOOD IAW MM 28-11-0. 2 L 7 2 4F A16WE 1996071000456 19960710 00456 NM 1996 7 10 CALA9600982 1 19960702 A 3350 BATTERY BOEING 737 737291 138448W NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17252 20362 INSPECTION FOUND EMERGENCY LIGHT OVER L-2 DOOR INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED, OPERATION OF THE LIGHT WAS RESTORED. 2 L 7 2 4F A16WE 1996071000457 19960710 00457 NM 1996 7 10 CALA9600983 1 19960702 A 3350 BATTERY BOEING 737 737291 138448W NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17252 20362 INSPECTION FOUND EMERGENCY LIGHT OVER R-2 DOOR INOPERATIVE. THE BATTERY WAS REMOVED, RECHARGED AND REINSTALLED IAW MM 3 3-50-42. OPERATION OF THE LIGHT CHECKED GOOD. 2 L 7 2 4F A16WE 1996071000458 19960710 00458 NM 1996 7 10 CALA9600984 1 19960702 A 3350 BATTERY BOEING 737 737291 138448W NM AFT ENTRY DR DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17252 20362 THE SLIDE LIGHT VOLTAGE AT AFT ENTRY DOOR WAS FOUND LOW AND THE BULB WAS BURNED OUT. THE BATTERY PACK AND BULB WERE REM OVED AND REPLACED. 2 L 7 2 4F A16WE 1996071000459 19960710 00459 NM 1996 7 10 CALA9600985 1 19960702 A 3350 BATTERY BOEING 737 737291 138448W NM FWD ENTRY DR DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17252 20362 INSPECTION FOUND LOW VOLTAGE AT THE FORWARD ENTRY DOOR SLIDE LIGHT. THE BATTERY PACK WAS REMOVED AND REPLACED, OPERATIO N OF THE LIGHT CHECKED GOOD. 2 L 7 2 4F A16WE 1996071000460 19960710 00460 NM 1996 7 10 CALA9600986 1 19960702 A 5315 FLOOR BEAM WEB BOEING 737 737291 138448W NM BS 294.5 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17252 20362 INSPECTION FOUND A CRACK IN FLOOR BEAM WEB AT STA 294.5, RBL 47. THE CRACKED SECTION WAS REMOVED AND A NEW REPAIR DOUBL ER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-30-2. 2 L 7 2 4F A16WE 1996071000461 19960710 00461 NE 1996 7 10 CKSA96065 2 19960630 A 7320 591058 FUEL TUBE DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3B 52039 NE NR3 FUEL CONTROL CRACKED A CKSA O OTHER K FLUID LOSS LD LANDING 1 GL 23 818CK 45961 645987 FUEL LEAK NR 3 ENGINE ON LANDING. REMOVED AND REPLACED FUEL CONTROL FUEL PRESSURE RETURN LINE. OPS CHECKS NORMAL PER M M CHAPTER 73-0, NO LEAKS NOTED DURING RUNUP. 2 L 7 4 4F 4 F 4A25 1E8 1996071000462 19960710 00462 WP 1996 7 10 CKSA96066 1 19960705 A 5730 SKIN DOUG DC8 DC863 302198A WP WS 74.8 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 781AL 45926 DURING B-CHECK INSPECTION, FOUND TOP OF LEFT WING STA 74.8 HAS 2 CRACKS AT FASTENER NEAR LEADING EDGE. REPAIRED CRACKS AT LEFT WING STA 74.8 PER DC-8 SRM 57-2-1 FIG 10, TASK NR 79693. 2 L 7 4 4F 4A25 1996071000463 19960710 00463 WP 1996 7 10 CKSA96067 1 19960705 A 5753 57511841 HINGE BASE DOUG DC8 DC863 302198A WP WS 219 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 781AL 45926 DURING B-CHECK INSPECTION, FOUND STATION 219 FLAP HINGE BASE HAS LARGE CRACK, 6 INCHES LONG. REMOVED AND REPLACED STA 2 19 FLAP HINGE BASE IAW DC-8 SRM 57-1-0. REMOVED AND REINSTALLED FLAP DRIVE LINKS IAW DC-8 MM CHAPTER 27-51-4, OPS CHECK ED GOOD. TASK NR 79662. 2 L 7 4 4F 4A25 1996071000464 19960710 00464 WP 1996 7 10 CKSA96068 1 19960705 A 5342 ANGLE DOUG DC8 DC863 302198A WP BS 1766 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 781AL 45926 DURING B-CHECK INSPECTION, FOUND CARD NR 6820-0551 AREA RUDDER AND TAB EXTERIOR, VERTICAL STAB TO FUSELAGE ATTACH ANGLE CORRODED AT FS 1766. REPAIRED IAW DOUGLAS SRM 53-2-5. TASK NR 79743. 2 L 7 4 4F 4A25 1996071000465 19960710 00465 WP 1996 7 10 CKSA96069 1 19960705 A 5310 STRUCTURE DOUG DC8 DC863 302198A WP PAX DOOR AREA CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 781AL 45926 DURING B-CHECK INSPECTION, FOUND CRACK IN SKIN STRUCTURE AT FWD ENTRY DOOR LOWER AFT CORNER MIGRATING UNDER KICK PLATE. REPAIRED IAW DC-8 SRM 53-2-0 FIG 15. TASK NR 79733. 2 L 7 4 4F 4A25 1996071000466 19960710 00466 WP 1996 7 10 CKSA96070 1 19960705 A 5753 5769581502 SLOT PANEL DOUG DC8 DC863 302198A WP RT TE FLAP CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 781AL 45926 DURING B-CHECK INSPECTION, FOUND RIGHT HAND INBD SLOT PANEL CRACKED TWO PLACES. INSTALLED NEW RIGHT HAND INBOARD SLOT P ANEL IAW DC-8 SRM 51-3-0, 57-2-0. TASK NR 79753. 2 L 7 4 4F 4A25 1996071000467 19960710 00467 WP 1996 7 10 CKSA96071 1 19960705 A 5753 5769583IN SLOT PANEL DOUG DC8 DC863 302198A WP LT TE FLAP CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 781AL 45926 DURING B-CHECK INSPECTION, FOUND LEFT HAND OUTBOARD SLOT PANEL CRACKED. INSTALLED NEW LEFT HAND OUTBOARD SLOT PANEL IAW DC-8 SRM 51-3-0, 57-2-0. TASK NR 79758. 2 L 7 4 4F 4A25 1996071000468 19960710 00468 WP 1996 7 10 CKSA96072 1 19960705 A 5753 5769581501 SLOT PANEL DOUG DC8 DC863 302198A WP LT TE FLAP CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 781AL 45926 DURING B-CHECK INSPECTION, FOUND LEFT HAND INBOARD SLOT PANEL CRACKED. INSTALLED NEW LEFT HAND INBOARD SLOT PANEL IAW S RM 51-3-0, 57-2-0. TASK NR 79759. 2 L 7 4 4F 4A25 1996071000469 19960710 00469 SO 1996 7 10 COMA9610220 1 19960707 A 7312 10718G FUEL HEATER EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENG LEAKING A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 1117H 11013 2972 120117 STRONG FUEL SMELL IN AIRCRAFT DURING TAXI. REPLACED THE LEFT ENGINE FUEL/OIL HEAT EXCHANGER. 2 L 7 2 4T 4 T RT A31SO E20NE 1996071000470 19960710 00470 SO 1996 7 10 COMA9610221 1 19960708 A 6120 7944441 SEALS EMB 120 EMB120RT SO LT PROP LEAKING A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 161CA 120143 THE GROUND FEATHER TEST REQUIRED 11 SECONDS FOR PROP TO TRANSITION FROM FEATHER TO BETA RANGE. REPLACED THE LT PROPELLE R TRANSFER TUBE OIL SEALS. 2 L 7 2 4T RT A31SO 1996071000471 19960710 00471 EA 1996 7 10 COMA9660118 1 19960706 A 3240 5010520 BRAKE ASSY CNDAIR CL600 CL6002B19 EA LT MLG OVERHEAT A COMA D RETURN TO BLOCK M OVER TEMP TX TAXI/GRND HDL 1 SO 01 933CA 3891 8 7040 DURING TAXI, THE LT MLG OUTBD BRAKE OVER HEATED CAUSING WHEEL FUSE LUGS TO MELT AND DEFLATE TIRE. REPLACED THE LT MLG B RAKE ASSY AND WHEEL ASSY. 2 L 7 2 4F RT A21EA 1996071000472 19960710 00472 NM 1996 7 10 DHL9670601C 1 19960619 A 5347 SEAT TRACK BOEING 727 72722C 138400F NM BS 700 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, FOUND SEAT TRACK CORRODED AT STA 700 TO 740 AT LBL 45. REMOVED AND REPLACED TRACK PER SRM 51-10-5. 2 L 7 3 4F A3WE 1996071000473 19960710 00473 NM 1996 7 10 DL72E961566 1 19960701 A 5330 SKIN BOEING 727 727247 138408F NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831WA 21483 FOUND ON D2 LETTER CK, AFT AIRSTAIR DOOR CUTOUT RT FWD RADIUS CRACKED. REPAIRED PER MM 53-30-0. 2 L 7 3 4F A3WE 1996071000474 19960710 00474 NM 1996 7 10 DL72E961567 1 19960701 A 5330 SKIN BOEING 727 727247 138408F NM PAX DOOR AREA CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831WA 21483 FOUND ON D2 LETTER CK, .4687 INCH CRACK IN FUSELAGE SKIN AT FWD ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED PER MM 53-30-0. 2 L 7 3 4F A3WE 1996071000475 19960710 00475 NM 1996 7 10 DL72E961629 1 19960709 A 5330 65C139133 SKIN BOEING 727 727247 138408F NM BS 1050 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2829W 21481 THE FUSELAGE SKIN HAS A 2 BY 2 CUTOUT AT FS 1050, NEAR STR 28R. THE SKIN IS MANUFACTURED FROM CLAD 2024-T3 CHEM-MILLED WITH A LOCAL THICKNESS OF 0.050 AND 0.070. UPON REMOVAL OF TIME-LIMITED REPAIR AT HMV, ADDITIONAL DAMAGE HAS BEEN DISCO VERED, STR 28R AT FS 1050 HAS EXTENSIVE CORROSION AND WILL REQUIRE INSTALLATION OF A SPLICE SECTION. ADDITIONAL CORROSI ON DAMAGE IS LOCATED APPROXIMATELY 2 INCHES INBOARD AND 2 INCHES FWD OF THE EXISTING CUTOUT. THE RESULTING CUTOUT IS 4 BY 5 INCH, 0.050 AND 0.070 2024-T3 CLAD SKIN. 2 L 7 3 4F A3WE 1996071000476 19960710 00476 NM 1996 7 10 DL72L961546 1 19960620 A 5320 FRAME BOEING 727 727232 1384082 NM SERV DOOR AREA CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 508DA 21310 FOUND ON MV1 CHECK, 1 CRACK IN LT AFT SERVICE DOOR CUTOUT FWD FRAME AT INBD RADIUS ADJACENT TO UPPER STOP PAD CASTING. REPAIRED PER SRM REPAIR REF LIA ENG 06/26/96, 53-13-0. 2 L 7 3 4F A3WE 1996071000477 19960710 00477 NM 1996 7 10 DL72L961547 1 19960621 A 5315 FLOOR BEAM BOEING 727 727232 1384082 NM BS 1070 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 508DA 21310 FOUND ON MV1 CHECK, CORROSION ON TOP SIDE OF FLOOR BEAM STA 1070 O/B OF RT O/B SEAT TRACK. REPAIRED PER M/M 53-20-11. 2 L 7 3 4F A3WE 1996071000478 19960710 00478 NM 1996 7 10 DL72L961582 1 19960627 A 5530 65174638 STRINGER BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 508DA 21310 VERTICAL STABILIZER STRINGER 9R WAS FOUND CRACKED OUTSIDE RIB 7 AT STA 133.8 DURING EXECUTION OF EO 4-59253-12 AD. EO C ALLS FOR A REPAIR PER B727 SRM 55-30-4, HOWEVER STR 9R CANNOT BE REPAIRED PER THIS SRM PROCEDURE DUE TO SPACE LIMITATION S ON IBOARD FLANGE. STRINGER WILL BE REPAIRED PER DAL B727 MM 55-30-00, FIGURE 803. 2 L 7 3 4F A3WE 1996071000480 19960710 00480 NM 1996 7 10 DL72L961647 1 19960624 A 5330 65545905 SKIN BOEING 727 727232 1384082 NM BS 700 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 508DA 21310 FUSELAGE SKIN AFT OF FS 700 FOUND TO BE WITH CORROSION DAMAGE BETWEEN STR 28L AND 28R. A 3.25 BY .375 INCH LONG CUTOUT WAS REQUIRED TO REMOVE THE DAMAGE BETWEEN STR 28R AND 28L. SKIN MACHINED FROM 2024-T3 WITH A LOCAL THICKNESS OF 0.050. 2 L 7 3 4F A3WE 1996071000481 19960710 00481 NM 1996 7 10 DL72P961627 1 19960507 A 5312 6516350344 BULKHEAD WEB BOEING 727 727225 1384077 NM BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8889Z 21858 THE FS 1183 BULKHEAD WEB WAS FOUND CRACKED AT RBL 27. THERE IS A .125 VERTICAL CRACK AND A .5 HORIZONTAL CRACK AT WL 17 0. THE WEB IS A BONDED ASSEMBLY OF CLAD 2024-T3 WITH A LOCAL THICKNESS OF 0.050. THE CRACK LOCATION IS OUTSIDE OF THE INSPECTION AREA SPECIFIED BY BOEING S/B 727-53-171. THE CRACKS WILL BE CUTOUT AND A REPAIR DOUBLER INSTALLED. 2 L 7 3 4F A3WE 1996071000482 19960710 00482 NM 1996 7 10 DL72S961562 1 19960619 A 5260 6517510310 DOUBLER BOEING 727 727232 1384082 NM BS 1263 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 523DA 21583 THE AFT VENTRAL STAIRWAY TORQUE BOX RIGHT HAND HORIZONTAL WEB HAS A .5 INCH CRACK IN A PREVIOUS REPAIR DOUBLER INSTALLED BY ER/A 06896-14, AT STA 1263 ON APPROXIMATELY BL 20.5. THIS DOUBLER WILL BE REMOVED AND THE WEB WILL BE TRIMMED IN A RECTANGULAR FASHION. A NEW DOUBLER WILL BE INSTALLED. THE WEB IS MANUFACTURED FROM 0.032 CLAD 7075-T6. 2 L 7 3 4F A3WE 1996071000483 19960710 00483 NM 1996 7 10 DL72S961563 1 19960622 A 5330 65C139132 SKIN BOEING 727 727232 1384082 NM BS 1058 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 529DA 21703 CORROSION WAS DISCOVERED IN THE FUSELAGE SKIN AT STA 1050, STR 28L. THE RESULTING DAMAGE CUTOUT IS 10 INCH FWD/AFT, BY 4.75 INCH I/B AND O/B AND IS CENTRALLY LOCATED AT THE INTERSECTION OF THE FRAME AT STA 1050 AND STR 28L. ALSO, STR 28L IS CORRODED AND WILL BE SPLICED FWD AND AFT OF THE DAMAGE CUTOUT. THE SKIN AT THIS LOCATION IS MANUFACTURED FROM 0.140 2024-T3 CLAD, MACHINED LOCALLY TO 0.070 AND 0.050. THE STRINGER IS MANUFACTURED FROM BAC1498-145, 7075-T6 EXTRUSION. 2 L 7 3 4F A3WE 1996071000484 19960710 00484 NM 1996 7 10 DL72S961573 1 19960627 A 5320 WEB BOEING 727 727232 1384082 NM BS 1323 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 519DA 21470 WEB IS CRACKED AT LIGHTENING HOLE LT SIDE STA 1323. REPAIRED PER M/M 53-11-0 PG 828 NR 15. 2 L 7 3 4F A3WE 1996071000485 19960710 00485 NM 1996 7 10 DL72S961579 1 19960307 A 5320 65175186 ANGLE BOEING 727 727232 1384082 NM BS 1273 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 531DA 21814 THERE IS A ONE INCH CRACK IN THE ANGLE OF THE AFT TRANSVERSE BEAM OF THE RT TORQUE BOX AT FS 1273. THE REPAIR REPLACES THE DAMAGED PARTS IN ACCORDANCE WITH S/B 53-0129. 2 L 7 3 4F A3WE 1996071000486 19960710 00486 NM 1996 7 10 DL72S961580 1 19960628 A 5720 570367002 STIFFENER BOEING 727 727232 1384082 NM NR 2 LE SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 519DA 21470 THE OUTBOARD ACTUATOR ATTACH RIB STIFFENER ON THE NR 2 SLAT ACTUATOR WAS FOUND CRACKED. THE DAL MFG PART NUMBER FOR THE INBOARD AND OUTBOARD STIFFENERS IS (57-0367-002). THE ERA REPLACED BOTH THE INBOARD AND OUTBOARD ATTACH RIB STIFFENERS PER EO 4-59271-3AD. 2 L 7 3 4F A3WE 1996071000487 19960710 00487 NM 1996 7 10 DL72S961601 1 19960627 A 5320 69678811 TRANSVERSE BEAM BOEING 727 727232 1384082 NM BS 1273 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 545DA 22494 A CRACK WAS FOUND IN THE UPPER FWD TRANSVERSE BEAM ANGLE AT STA 1273. THIS AREA OF THE TORQUE BOX IS THE SUBJECT OF AN AIRWORTHINESS DIRECTIVE 94-07-08 WHICH REQUIRES INSPECTION PER S/B 53-0129. THIS ER/A WILL REPLACE THE DAMAGED PART IN ACCORDANCE WITH THE SERVICE BULLETIN. 2 L 7 3 4F A3WE 1996071000488 19960710 00488 NM 1996 7 10 DL72S961632 1 19960704 A 5620 6556703 WINDOW BOEING 727 727232 1384082 NM CABIN FAILED A DALA O OTHER D INFLIGHT SEPARATION CL CLIMB 1 SO 27 535DA 22048 ON CLIMBOUT, AT 27,000 PASSENGER CABIN WINDOW AT ROW 2A CRACKED AND CABIN PRESSURE WAS MAINTAINED AT 7.6 PSI. FLT WAS C ONTINUED AT FL200 AND CABIN PRESS AT 6.0 PSI. ON ARRIVAL PBI FOUND OUTER WINDOW PANE BROKEN, INNER PANE INTACT. REPLAC ED 2A WINDOW, INSPECTED SURROUNDING AREA, NO PROBLEMS FOUND. 2 L 7 3 4F A3WE 1996071000489 19960710 00489 NM 1996 7 10 DL72S961641 1 19960706 A 8000 START DUCT BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE FAILED A A DALA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 27 401DA 21145 695368 NUMBER ONE ENGINE FIRE INDICATION AT CRUISE, WHEN THROTTLE WAS MOVED TO IDLE, INDICATION EXTINGUISHED. ENGINE WAS SHUT DOWN PRECAUTIONARY. ENGINE WINDMILLED FOR APPROX 20 MINUTES N-2 RPM WAS APPROX 15 PERCENT, OIL PRESSURE WAS APPROX 20 P SI, ON APPROACH. FOUND START DUCT AND STARTER FLANGE FAILED. REPLACING STARTER GARLOCK SEAL PRECAUTIONARY. STARTER DU CT, (P/N 804101151) REF IPC 80-10-0 FIG 2 ITEM 135, ARRIVING FROM CONTENTIAL AIRLINES. STARTER (P/N 804001312) IN STOCK. NO DAMAGE NOTED TO GEARBOX/STARTER DRIVE PAD. 2 L 7 3 4F 4 F A3WE E2EA 1996071000490 19960710 00490 NM 1996 7 10 DL72S961650 1 19960706 A 3350 3174981 LIGHT BOEING 727 727232 1384082 NM R1 DOOR CRACKED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 405DA 21149 R1 DOOR SLIDE LIGHT INOP. REPLACED REFLECTOR LIGHT ASSEM. 2 L 7 3 4F A3WE 1996071000491 19960710 00491 NM 1996 7 10 DL72W961544 1 19960627 A 5320 WEB BOEING 727 727247 138408F NM BS 1220 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2810W 20648 TORQUE BOX WEB CRACKED .5 INCH IN ADJACENT RT HAND RAIL STA 1233. INSTALLED DOUBLER PER MM 53-11-0. 2 L 7 3 4F A3WE 1996071000492 19960710 00492 NM 1996 7 10 DL72W961557 1 19960629 A 2433 TR UNIT BOEING 727 727247 138408F NM E/E COMPT BURNT A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 2815W 20871 VISIBLE SMOKE EXHAUSTING FROM E/E COMP WITH ESS TR C/B POPPED, SMELLS ELECTRICAL. FOUND AND REMOVED ESS T/R AND REPLACE D NR 3 TR, OPS OK. 2 L 7 3 4F A3WE 1996071000493 19960710 00493 NM 1996 7 10 DL72W961565 1 19960701 A 2421 976J4981 GENERATOR BOEING 727 727247 138408F NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE FAILED A DALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 27 2820W 21058 687520 NR 1 GEN ALREADY ON MCO NR 2 GEN FAILED. NR 2 ENGINE CSD/ GEN CHANGE IN PROGRESS. 2 L 7 3 4F 4 F A3WE E2EA 1996071000494 19960710 00494 NE 1996 7 10 DL72W961597 2 19960703 A 7200 ENGINE BOEING 727 727247 138408F NM PWA JT8 JT8D15 52051 NE NR 1 FLAME-OUT A DALA C D ABORTED TAKEOFF RETURN TO BLOCK X ENGINE FLAMEOUT TO TAKEOFF 1 SO 27 295WA 22532 665742 NR 1 ENGINE SHUTDOWN ON T/O ROLL AT AT 40 KTS. REPLACED NR 1 ENGINE FUEL PUMP. 2 L 7 3 4F 4 F A3WE E2EA 1996071000495 19960710 00495 NM 1996 7 10 DL72W961598 1 19960703 A 2782 BRACKET BOEING 727 727247 138408F NM NR 2 LE FLAP ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 290WA 22108 FOUND ON B-1 LETTER CK, NR 2 L/E FLAP ACTUATOR I/B MOUNT BRACKET CRACKED AT THE UPPER CORNER. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1996071000496 19960710 00496 NM 1996 7 10 DL72W961599 1 19960703 A 2782 BRACKET BOEING 727 727247 138408F NM NR 1 LE SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 290WA 22108 FOUND ON B1 LETTER CK, NR 1 SLAT ACT INBD MOUNT BRACKET CRACKED. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1996071000499 19960710 00499 NM 1996 7 10 DL767961571 1 19960701 A 5350 FAIRING BOEING 767 767232 1385132 NM LT WING MISSING A DALA K NONE D INFLIGHT SEPARATION IN INSP/MAINT 1 SO 27 107DL 22219 ON ARRIVAL, FOUND FAIRING PANEL 195CL MISSING AND PANEL 195DL LEFT WING DAMAGED. INSPECTED AIRCRAFT FOR ADDITIONAL DAMA GE. REPLACED PANELS PER ERA 359898-14. REPAIRED FUSLAGE DAMAGE BETWEEN FS 1219 AND FS 1241 AND ABOVE S-22 AND S-23 PER SRM. 2 L 7 2 4F RT A1NM 1996071000500 19960710 00500 1996 7 10 DL767961630 2 19960704 A 7320 ECU CB BOEING 767 767232 1385132 NM NR 1 ENGINE TRIPPED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 114DL 28432 22226 GOT STRONG ELECTRICAL SMELL 30 MINUTES AFTER T/O, SMELL GREW FAINT AND WAS GONE IN 15 MIN. FOUND LEFT ENG CONTROL IDLE C/B OUT, LEFT IT OUT. INSPECTED COCKPIT CIRCUIT BREAKER PANELS, INSTRUMENT PANELS, GENERAL AREA AND E AND E COMPARTMENT , NO EVIDENCE OF BURNS OR SMELLS. 2 L 7 2 4F RT A1NM 1996071000501 19960710 00501 1996 7 10 DL76L961555 4 19960628 A 3460 CDU BOEING 767 767332 1382001 NM RIGHT DEFECTIVE A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 186DN 27962 RIGHT CDU FAILED ON CLIMBOUT, LEFT CDU FAILED SHORTLY THERE AFTER. REPLACED LT AND RT CDU, CHECKS OK. CHECKED EQUIPMNT COOLING, ALL NORMAL. 2 L 7 2 4F RT A1NM 1996071000502 19960710 00502 GL 1996 7 10 ERA96001 2 19960701 A 7250 6843648 CONE ASSY CVAC 440 440 2422902 WP ALLSN 501D 501D13H 03004 GL RT ENGINE MISSING A ERAA K NONE D INFLIGHT SEPARATION LD LANDING 1 AL 03 566EA 381 501216 REAR TURBINE SCAVENGE INSULATOR CONE MISSING FROM NR 2 ENGINE. INSPECTED TURBINE AND TAILPIPE FOR DAMAGE AND REPLACED T HE INSULATOR CONE. 2 L 7 2 4R 4 T 6A6 E282 1996071000503 19960710 00503 NE 1996 7 10 ERA96002 2 19960708 A 7260 311169301 SPUR GEAR DHAV DHC8 DHC8103 1386005 NM PWA PW121 PW121 52124 NE RT ENGINE FAILED A A ERAA A E UNSCHED LANDING ENGINE SHUTDOWN X ENGINE FLAMEOUT CR CRUISE 1 AL 03 881EA 2360 2360 233 120210 ENGINE NR 2 FLAME-OUT IN CRUISE AT 20,000 FT. SECURED ENGINE AND DIVERTED TO HOM. ENGINE NR 2 FUEL PUMP DRIVE SPUR GEA R FAILURE RESULTING IN LOSE OF FUEL AND OIL PRESSURE. POST-MOD SB 20195, ACCESSORY DRIVE SPUR GEAR REPLACEMENT, POST-MO D SB 21178, AGB BEARING RETENTION IMPROVEMENT, POST-MOD SB 21060, STIFF FUEL PUMP SHAFT. ENGINE REMOVED FROM SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 1996071000504 19960710 00504 NM 1996 7 10 P5CA9600340 1 19960709 A 5350 65B114741 FAIRING BOEING 747 747122 1384872 NM FUSELAGE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 DELAMINATED BODY FAIRING PANEL LOCATED BETWEEN LEADING EDGE OF MAIN LANDING GEAR CENTER DOORS. REPLACED PANEL PER BOEIN G SRM 51-30-02 AND 51-24-11. 2 L 7 4 4F A20WE 1996071000505 19960710 00505 NM 1996 7 10 P5CA9600341 1 19960709 A 7110 CHANNEL BOEING 747 747122 1384872 NM NR 1 CORE COWL BENT A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 NR 1 ENGINE OUTBOARD CORE COWL LOWER EDGE CHANNEL VERY BENT, WITH PULLED RIVETS AND LOST DOUBLERS. REMOVED FABRICATED A ND INSTALLED CHANNEL PER BOEING SRM 51-40-03. 2 L 7 4 4F A20WE 1996071000506 19960710 00506 NM 1996 7 10 P5CA9600342 1 19960709 A 5414 PANEL BOEING 747 747122 1384872 NM NR 4 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 NR 4 ENGINE PYLON LOWER EDGE PANEL CRACKED. REMOVED FABRICATED AND INSTALLED PANEL PER BOEING SRM 51-10-01. 2 L 7 4 4F A20WE 1996071000507 19960710 00507 NM 1996 7 10 P5CA9600343 1 19960709 A 7110 COWL BOEING 747 747122 1384872 NM NR 3 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 NR 3 LEFT FAN COWL LOWER EDGE IS CRACKED BETWEEN THE AFT AND MIDDLE U-BOLTS. REPAIRED CRACK PER BOEING SRM 51-40-06. 2 L 7 4 4F A20WE 1996071000508 19960710 00508 NM 1996 7 10 P5CA9600344 1 19960709 A 5280 65B1145911 ANGLE BOEING 747 747122 1384872 NM LT MLG STRUT DR WORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEFT BODY GEAR STRUT DOOR OUTER AFT ANGLE WORN WITH A HOLE. REPLACED ANGLE PER BOEING SRM 51-30-02. 2 L 7 4 4F A20WE 1996071000509 19960710 00509 NM 1996 7 10 P5CA9600345 1 19960709 A 2520 R30F8 PULLEY BOEING 747 747122 1384872 NM MAIN DECK BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 MAIN DECK TO UPPER DECK LADDER PULLEY BROKEN. REPLACED PULLEY I/A/W MAINTENANCE MANUAL 25-50-01. 2 L 7 4 4F A20WE 1996071000510 19960710 00510 NM 1996 7 10 P5CA9600346 1 19960709 A 5280 DOOR BOEING 747 747122 1384872 NM RT MLG STRUT CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 RIGHT WING LANDING GEAR STRUT LOWER DOOR LEADING EDGE AREA CRACKED ALONG FAIRING ASSEMBLY. REPAIRED PER BOEING SRM 51-4 0-05. 2 L 7 4 4F A20WE 1996071000511 19960710 00511 NM 1996 7 10 QXEA9600233 1 19960704 A 3350 321430 POWER SUPPLY DORNER DO32 DO328100 2996000 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 328PH 3006 EMERGENCY LIGHT BATTERY PACKS ARE DEAD. AIRCRAFT FERRIED TO PDX FOR REPAIR, POWER SUPPLIES REPLACED AND LIGHTS OPS CHEC KED GOOD. 2 H 7 2 4T RT A45NM 1996071000512 19960710 00512 NM 1996 7 10 QXEA9600234 1 19960703 A 7714 3039242 NP PROBE DORNER DO32 DO328100 2996000 NM NR 1 ENGINE MALFUNCTIONING A A QXEA O OTHER O OTHER AP APPROACH 1 NM 09 330PH 3008 NR 1 ENGINE BEGAN SURGING 20 TO 80 PERCENT ON APPROCH TO SEA. ALL ENGINE INSTRUMENTS INDICATED THE SURGING ALONG WITH A IRCRAFT YAW. NR 1 ENGINE BROUGHT TO IDLE AND PROP WAS FEATHERED. AIRCRAFT LANDED IN SEA WITHOUT FURTHER PROBLEM. NR 1 NP PROBE REPLACED AND ENGINE OPS CHECKED GOOD ON GROUND RUN. 2 H 7 2 4T RT A45NM 1996071000513 19960710 00513 EU 1996 7 10 QXEA9600235 1 19960708 A 3350 1820 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 802PH 11017 EMERGENCY EXIT LIGHTS OVER FORWARD CABIN ARE INOP. BULBS WERE REPLACED AND LIGHTS OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996071000514 19960710 00514 EU 1996 7 10 QXEA9600236 1 19960708 A 3350 MGG1280 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 802PH 11017 EMERGENCY EXIT LIGHTS OVER SEAT ROW 8 ARE INOP. BULBS WERE REPLACED, SIGN OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996071000515 19960710 00515 NM 1996 7 10 96ZZZM1060 1 19960531 A 2910 506849471 HYD LINE BOEING 707 707321C 138367B NM LT MLG WW CRACKED A MIRA H DEACTIVATE SYST/CIRCUITS K FLUID LOSS DE DESCENT 1 SO 19 722GS 19373 OXO- FLT 504 - SKBO-MIA - UTILITY HYD SYSTEM LEAKING, NOSE GEAR PIN WAS INSTALLED, FLAPS 50 DEGREES WERE USED FOR TAG AP PROACH AND 2.5 GALLONS ARE REMAINING AFTER LANDING. PERFORMED TROUBLESHOOTING, FOUND HYDRAULIC LEAK BY AUX HYD PUMP RET URN LINE, REMOVED AND REPLACED LINE. OPS CHECK FOUND GOOD AS PER BMM 29-00. (M) 2 L 7 4 4F 4A26 1996071000516 19960710 00516 EU 1996 7 10 96ZZZM1061 1 19960509 A 5230 DOOR FRAME AMD FALC20 FALCOND 2720304 EU CARGO DOOR CRACKED A DKAA K NONE O OTHER IN INSP/MAINT 1 GL 23 226R 226 ONE SMALL CRACK NOTED IN CARGO DOOR FRAME DURING SSIP X-RAY INSPECTION. (AD 92-17-05 REQUIREMENT). (M) 2 L 7 2 4F A7EU 1996071000517 19960710 00517 WP 1996 7 10 96ZZZM1062 1 19960609 A 3230 LEVELING CYL LKHEED 1011 10113851 5265010 WP LT MLG REQ'D SERV A RIAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 765BE 193P1105 RIA - FLT 608 - OUT OF CAI, AFTER TAKEOFF AND GEAR RETRACTION, BRAKE TEMP AMBER LIGHT ILLUMINATED. GEARS WERE LOWERED T O COOL BRAKES. BRAKE TEMP LIGHT EXTINGUISHED, BUT TRUCK LIGHT ILLUMINATED. AIRCRAFT AIR RETURNED TO CAI. AT CAI, MAIN TENANCE ACCOMPLISHED TROUBLESHOOTING PER MM 32-61-00, BLED LEFT TRUCK LEVELING CYLINDER. AIRCRAFT CHECKED OUT NORMAL. A IRCRAFT RELEASED FOR FLIGHT. (M) 2 L 7 3 4F A23WE 1996071000518 19960710 00518 EU 1996 7 10 96ZZZM1063 1 19960604 A 2421 MICROSWITCH STBROS SD3 SD360 8100606 EU LT GENERATOR OUT OF ADJUST A DATA O OTHER J H WARNING INDICATION ELECT. POWER LOSS-50 PC NR NOT REPORTED 1 GL 13 151CA SH3653 AT CVG, CAPTAIN REPORTED THAT THE LEFT GENERATOR WOULD NOT COME ON LINE. AT THE REQUEST OF MAINTENANCE, ANOTHER ATTEMPT WAS MADE, AT THIS TIME THE GENERATOR CAME ON LINE AND REMAINED ON LINE. PILOT ALSO REPORTED THAT THIS HAD BEEN A PRIOR PROBLEM. AIRCRAFT WAS BROUGHT TO MKE FOR TROUBLESHOOTING. MX FOUND THAT THE STARTER/GENERATOR LINE CONTACTOR WAS INTE RMITTENT. THE CONTACTOR WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. THE CONTACTOR OPEN INVESTIGATION FOUND THAT THE MICROSWITCH ACTUATOR WAS OUT OF ADJUSTMENT, WOULD NOT MAKE SAME TIME WHEN PLACED INTO GENERATOR POSITION. 2 H 7 2 4T A41EU 1996071000519 19960710 00519 EA 1996 7 10 96ZZZM1064 2 19960614 A 7261 AS3209224 O-RING BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA LT ENGINE PINCHED A A GUUA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SO 19 198GA UB5 FLT - 477 - FLL/NAS - LEFT ENGINE LOST OIL PRESSURE THEN THE ENGINE SHUTDOWN ITSELF. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO MIA AND LANDED WITHOUT INCIDENT. INSPECTED AND DETERMINED THAT THE LEFT OIL FILTER COVER O-RING WA S PINCHED ALLOWING LEAKAGE. REMOVED AND REPLACED O-RING. LEAK CHECK AND POWER ASSURANCE RUNS GOOD. AIRCRAFT RELEASED T O SERVICE. 2 L 7 2 4T 4 T RT A24CE E4EA 1996071000520 19960710 00520 WP 1996 7 10 96ZZZM1065 1 19960521 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 410-412 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 985Z 47491 STL - DURING OP-15, FOUND A FOUR INCH CRACK IN LONGERON 30, STATION 410 TO 412. REPLACED LONGERON 30 PER SRM 53-02, FIG URE 15. (M) 2 L 7 2 4F A6WE 1996071000521 19960710 00521 WP 1996 7 10 96ZZZM1066 1 19960604 A 5314 KEEL BEAM DOUG DC9 DC931 3022065 WP RT MLG WW CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 985Z 47491 STL - DURING OP-15, FOUND .5 INCH CRACK IN WHEEL WELL, AFT END OF KEEL BEAM AT GEAR DOOR PIN HINGE LOCKPLATE, RLMG. REP AIRED PER SRM 53-04, FIGURE 42, SHEET 3. 2 L 7 2 4F A6WE 1996071000522 19960710 00522 NM 1996 7 10 96ZZZM1067 1 19960601 A 2530 953000119 SERVING CART BOEING 747 747131 1384881 NM GALLEY FAILED A TWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 93109 19675 JFK - DURING CRUISE, SINGLE SERVING CART NR 412, OVERHEATED AND EMITTED SMOKE. DISCONNECTED ELECTRICAL POWER. FOUND DE FECTIVE HEATING PAD. REPLACED SERVING CART, MFG P/N 953000-119. NEW SERVING CART OPERATION CHECKED NORMAL. 2 L 7 4 4F A20WE 1996071000523 19960710 00523 WP 1996 7 10 96ZZZM1068 1 19960602 A 3222 B050762 SCHRADER VLV DOUG DC9 DC983 3022083 WP NLG FAILED A TWAA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 9305N 49395 MSY - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, NOSE LANDING GEAR DID NOT RETRACT. FOLOWED ORH PROCEDURES. FOUND NOSE LANDING GEAR STRUT DEFLATED AND A DEFECTIVE SCHRADER VALVE. SERVICED NOSE LANDING GEAR STRUT WITH HYDRAULIC FLUID AND REPLACED SCHRADER VALVE, MFG P/N B050762, AND DRY NITROGEN. NOSE LANDING GEAR OPERATION THEN CHECKED NORMAL. 2 L 7 2 4F RT A6WE 1996071000524 19960710 00524 WP 1996 7 10 96ZZZM1069 1 19960602 A 2170 1794601 COALESCER BAG DOUG DC9 DC982 3022082 WP CABIN CONTAMINATED A TWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 05 956U 49701 STL - AFTER TAKEOFF, HAD SMOKE ENTERING CABIN. TURNED OFF LEFT AIR CONDITIONING PACK AND SMOKE SUBSIDED. FOUND OIL CON TAMINATION ON WATER SEPARATOR, MFG P/N 179460-8-1. REPLACED WATER SEPARATOR, PERFORMED AIR CONDITIONING DUCT CLEANOUT. AIR CONDITIONING SYSTEM OPERATION THEN CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 1996071000526 19960710 00526 WP 1996 7 10 96ZZZM1071 1 19960604 A 3260 833703 SENSOR DOUG DC9 DC982 3022082 WP NLG DIRTY A TWAA O OTHER N FALSE WARNING CL CLIMB 1 CE 05 950U 49230 STL - ON TAKEOFF AFTER LANDING GEAR RETRACTION, NOSE LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED. FOUND TARGET AND S ENSOR DIRTY. CLEANED TARGET AND SENSOR, MFG P/N 8-337-03, AND NOSE LANDING GEAR INDICATION CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 1996071000527 19960710 00527 NM 1996 7 10 96ZZZM1072 1 19960618 A 3241 40817 TRANSDUCER BOEING 737 7374B7 1384702 NM LT ANTI SKIN SYS MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 EA 19 446US 24873 BWI - FLT 1257 - ON APPROACH TO DCA, ANTI-SKID INOP LIGHT CAME ON. FLIGHT DIVERTED TO BWI AND LANDED WITH NO FURTHER IN CIDENT. MAINTENANCE REPLACED THE RIGHT MLG STRUT HARNESS AND THE LEFT INBOARD ANTI-SKID TRANSDUCER. OPS CHECK GOOD. R EFERENCE USAASB96113. 2 L 7 2 4F RT A16WE 1996071000528 19960710 00528 EU 1996 7 10 96ZZZM1073 1 19960619 A 2750 TY176004A TRANSDUCER JETAIR JETSTM JETSTM4101 1500501 EU FLAPS OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 307UE 41021 FLT 6202 - MHT-IAD - ABORTED THE TAKEOFF DUE TO THE TAKEOFF CONFIGURATION WARNING SYSTEM ACTIVATING WITH THE SPOILER CAP TION LIGHT ILLUMINATING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE INSPECTED SPOILER SYSTEM BUT COULD NOT FIND ANY DEFECTS. FOR THE TAKEOFF CONFIGURATION WARNING SYSTEM DISCREPANCY MX ADJUSTED THE GUSTLOCK MICROSWI TCHES AND THE FLAP POSITION TRANSDUCERS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. REFERENCE VTZA96225. 2 L 7 2 4T RT A41NM 1996071000529 19960710 00529 NM 1996 7 10 AALA960815 1 19960528 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 340-350 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 874AA 21386 TUL - FOUND CREASE ANGLE FORWARD ENTRY DOOR CORRODED. INSTALLED NEW CREASE ANGLE AND SEALED, TREATED AND PRIMED PER SRM 51-10-6-20. (M) 2 L 7 3 4F A3WE 1996071000530 19960710 00530 WP 1996 7 10 AALA960837 1 19960517 A 5320 9936534199 CUSP DOUG DC9 DC982 3022082 WP BS 160-200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 283AA 49296 TUL - FOUND CORROSION ON RIGHT CUSP AT FORWARD SERVICE DOOR AREA STATION 160 TO 200 (CORROSION REMOVED AND BEYOND LIMITS FOR THICKNESS). INSTALLED DOUBLER PER SRM 53-01 PAGE 2 SHEET 3. (M) 2 L 7 2 4F A6WE 1996071000531 19960710 00531 WP 1996 7 10 AALA960838 1 19960517 A 5320 9936534199 CUSP FITTING DOUG DC9 DC982 3022082 WP BS 200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 283AA 49296 TUL - FOUND CORROSION AT CUSP FITTING JUST AFT OF FORWARD SERVICE DOOR CUTOUT, (CORROSION REMOVAL BEYOND LIMITS). INSTA LLED DOUBLER PER ESO NR 80559. (M) 2 L 7 2 4F A6WE 1996071000532 19960710 00532 WP 1996 7 10 AALA960862 1 19960528 A 5320 CUSP DOUG DC9 DC982 3022082 WP BS 160-200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 283AA 49296 TUL - FOUND CORROSION ON RIGHT CUSP AT FORWARD SERVICE DOOR. INSTALLED DOUBLER PER SRM 53-01 PAGE 2, SHEET 3, PER ESO 8 0554, DATED 5-21-96. (M) 2 L 7 2 4F A6WE 1996071000533 19960710 00533 WP 1996 7 10 AALA960863 1 19960603 A 5320 CLIP DOUG DC10 DC1010 3022110 WP BS 879 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 129AA 46996 TUL - FOUND RIGHT ATTACH CLIP CORRODED AT STATION 879R AFT OF OUTBOARD ROLLER TRAY. REPLACED CORRODED ATTACH CLIP PER S RM 51-01-00. (M) 2 L 7 3 4F A22WE 1996071000534 19960710 00534 NM 1996 7 10 AALA960864 1 19960530 A 5315 146N5300 DECK PLATE BOEING 757 757223 1384957 NM BS 1680 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 647AM 24605 AFW - FOUND DECK PLATE HAS CORROSION REMOVED IN VARIOUS LOCATION AREAS ARE BEYOND SRM LIMITS. PER MRB 757-849. (M) 2 L 7 2 4F RT A2NM 1996071000535 19960710 00535 NM 1996 7 10 AALA960865 1 19960530 A 5315 146N5089 FLOOR BEAM BOEING 757 757223 1384957 NM BS 1640 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 647AM 24605 AFW - FOUND FLOOR BEAM AT STATION 1640 HAD CORROSION REMOVED BEYOND SRM LIMITS AT LBL 37, 39, 40, 50 AND 55. PER MRB 75 7-848. (M) 2 L 7 2 4F RT A2NM 1996071000536 19960710 00536 NM 1996 7 10 AALA960866 1 19960530 A 5315 141N5113 FLOOR BEAM BOEING 757 757223 1384957 NM BS 377 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 647AM 24605 AFW - FOUND ON UPPER SURFACE OF FLOOR BEAM, AT STATION 377, HAD CORROSION REMOVED BEYOND SRM LIMITS. PER MRB 757-846. ( M) 2 L 7 2 4F RT A2NM 1996071000537 19960710 00537 NM 1996 7 10 AALA960867 1 19960530 A 5315 141N5112 FLOOR BEAM BOEING 757 757223 1384957 NM BS 365 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 647AM 24605 AFW - FOUND FLOOR BEAM, AT STATION 365, HAS CORROSION REMOVED ON UPPER SURFACE, MATERIAL REMAINING IS BEYOND SRM LIMITS. PER MRB 757-845. (M) 2 L 7 2 4F RT A2NM 1996071000538 19960710 00538 NM 1996 7 10 AALA960868 1 19960530 A 5210 146N62015 PAN BOEING 757 757223 1384957 NM L-4 DOOR GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 647AM 24605 AFW - FOUND L-4 DOOR PAN HAS GOUGE BLENDED BEYOND SRM LIMITS. PER MRB 757-844. (M) 2 L 7 2 4F RT A2NM 1996071000539 19960710 00539 WP 1996 7 10 AALA960872 1 19960606 A 5320 PAN DOUG DC10 DC1010 3022110 WP BS 879 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 129AA 46996 TUL - FOUND SLIDING DOOR PAN HAS INTERGRANNULAR CORROSION STATION 879. REMOVED AND REPLACED PART PER AARD 51-01-00-05 P G 01. (M) 2 L 7 3 4F A22WE 1996071000540 19960710 00540 NM 1996 7 10 AALA960887 1 19960608 A 5400 ENG INLET BOEING 727 727223 1384074 NM NR 2 ENGINE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 705AA 22462 TUL - NR 2 ENGINE INLET CORRODED AT 11:00 POSITION. REMOVED CORRODED AREA AND MADE FLUSH REPAIR PER SRM 54-30-3 PAGE 2A AND 2B. (M) 2 L 7 3 4F A3WE 1996071000541 19960710 00541 NM 1996 7 10 AALA960889 1 19960608 A 5330 SKIN BOEING 727 727223 1384074 NM BS 580 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 705AA 22462 TUL - FOUND STRINGER 28 LEFT HAS CORROSION AND SKIN CORRODED STATION 580 TO 595. REMOVED AND REPLACED SECTION OF STRING ER AND SKIN AT STRINGER 28 LEFT STATION 580 TO 660 SRM 53-30-3 PAGE 12 - PG 14A. (M) 2 L 7 3 4F A3WE 1996071000542 19960710 00542 NM 1996 7 10 AALA960890 1 19960608 A 5330 SKIN BOEING 727 727223 1384074 NM BS 680-684 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 705AA 22462 TUL - FOUND CORROSION ON BELLY SKIN AND CIRCUMFERENTIAL STRAP, STATION 680 TO 684, INBOARD OF STRINGER 27R. INSTALLED D OUBLER AND FILLER ALODINED, PRIMED, PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 1996071000543 19960710 00543 NM 1996 7 10 AALA960891 1 19960608 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 701 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 705AA 22462 FOUND CORROSION IN STRINGER 27R AT STATION 701. REMOVED OUT OF LIMITS STRINGER AND REPAIRED PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1996071000544 19960710 00544 NM 1996 7 10 AALA960898 1 19960612 A 5315 146N5087 FLOOR BEAM BOEING 757 757223 1384957 NM BS 1600 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 649AA 24607 AFW - FOUND FLOOR BEAM AT STATION 1600 LBL 13 HAD A GOUGE BLENDED BEYOND SRM LIMITS. PER MRB 757-857. (M) 2 L 7 2 4F RT A2NM 1996071000545 19960710 00545 NM 1996 7 10 AALA960899 1 19960612 A 5315 141N5112 FLOOR BEAM BOEING 757 757223 1384957 NM BS 365 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 649AA 24607 AFW - FOUND FLOOR BEAM AT STATION 365 RBL 61 HAD CORROSION BLENDED BEYOND SRM LIMITS. PER MRB 757-856. (M) 2 L 7 2 4F RT A2NM 1996071000546 19960710 00546 NM 1996 7 10 AALA960900 1 19960612 A 5315 141N2910 FLOOR BEAM BOEING 757 757223 1384957 NM BS 324 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 649AA 24607 AFW - FOUND FLOOR BEAM AT STATION 324 HAS CORROSION REMOVED BEYOND SRM LIMITS. PER MRB 757-861. (M) 2 L 7 2 4F RT A2NM 1996071000547 19960710 00547 WP 1996 7 10 AALA960906 1 19960614 A 3350 A3060698101 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 491AA 49684 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS FROM FORWARD PART OF MAIN CABIN TO OVERWING EXIT INOPERATIVE. REPL ACED BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTOR AT FORWARD PART OF MAIN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION . (M) 2 L 7 2 4F A6WE 1996071000548 19960710 00548 NM 1996 7 10 AALA960909 1 19960616 A 3350 A3060698101 CONNECTOR BOEING 727 727227 1384078 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 728AA 20735 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN AFT SECTION OF FIRST CLASS CABIN INOPERATIVE. REPAIRED BROKEN E MERGENCY FLOOR LIGHT WIRING AND REPLACED BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTOR AT AFT SECTION OF FIRST CLASS CABI N. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996071000549 19960710 00549 NM 1996 7 10 AALA960920 1 19960616 A 2613 358050 CONTROL UNIT FENWAL BOEING 727 727227 1384078 NM E/E COMPT DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 727AA 20734 RDU - FLT 1880 - EN ROUTE MIA/DTW DURING CRUISE, LOWER AFT BODY OVERHEAT LIGHT BEGAN TO FLICKER. SHORTLY AFTER BEGINNIN G QRH PROCEDURE, LIGHTS STOPPED FLICKERING AND SYSTEM WOULD NOT TEST. AIRCRAFT DIVERTED TO RDU AND LANDED WITHOUT INCID ENT. REPLACED FIRE DETECTION ACCESSORY CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996071000550 19960710 00550 NM 1996 7 10 AWXA960268 1 19960613 A 2910 69522501 FLEX LINE BOEING 757 7572S7 1384962 NM RT MLG RUPTURED A AWXA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CR CRUISE 1 WP 28 902AW 23322 PHX - FLT 2068 - PHX-LAS - AIR TURNBACK, HYDRAULIC QUANTITY LOSS. RIGHT GEAR DOWNLINE RUPTURED. INSTALLED TEMPORARY FL EX LINE AND SERVICED SYSTEM. PLACED ON 106, DMI NR 28375 TO BE REPLACED BY PERMANENT LINE WITHIN 25 DAYS. (M) 2 L 7 2 4F RT A2NM 1996071000551 19960710 00551 NM 1996 7 10 EISA96040 1 19960429 A 5532 SKIN BOEING 727 727223 1384074 NM LT ELEVATOR T/E DEBONDED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 LEFT ELEVATOR INBOARD TRAILING EDGE IS STARTING TO SEPARATE. CLEANED AREA BONDED WITH A-B STRUCTURAL ADHESIVE REPAIR PE R 51-40-06. (M) 2 L 7 3 4F A3WE 1996071000552 19960710 00552 NM 1996 7 10 EISA96041 1 19960424 A 5280 BRACKET BOEING 727 727223 1384074 NM BS 870 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 FOUND LEFT GEAR WELL DOOR ACTUATOR OUTBOARD SUPPORT FRAME CRACKED, WHERE IT ATTACHES TO STATION 870 BULKHEAD. REMOVED, FABRICATED AND INSTALLED NEW SUPPORT FRAME PER SRM 51-30-02. (M) 2 L 7 3 4F A3WE 1996071000553 19960710 00553 NM 1996 7 10 EISA96042 1 19960424 A 5330 SKIN BOEING 727 727223 1384074 NM LOWER FUSELAGE CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 LOWER FUSELAGE, JUST AFT OF ROTATING BEACON, HAS BULGED AREA. REMOVED OLD REPAIR, FABRICATED AND INSTALLED NEW DOUBLER PER SRM 51-40-01. (M) 2 L 7 3 4F A3WE 1996071000554 19960710 00554 NM 1996 7 10 EISA96043 1 19960424 A 5320 BRACKET BOEING 727 727223 1384074 NM BS 870 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 RIGHT MAIN GEAR DOOR ACTUATOR LINK SUPPORT BRACKET CRACKED, WHERE IT ATTACHES TO STATION 870 WALL. FABRICATED AND INSTA LLED NEW SUPPORT BRACKET. (M) 2 L 7 3 4F A3WE 1996071000555 19960710 00555 NM 1996 7 10 EISA96044 1 19960507 A 5712 RIB BOEING 727 727223 1384074 NM LT WING CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 LEFT WING TRAILING EDGE COVE STIFFENER RIB CRACKED, JUST OUTBOARD OF NR 4 FLAP TRACK. FABRICATED AND INSTALLED NEW RIB PER SRM 51-40-03. (M) 2 L 7 3 4F A3WE 1996071000556 19960710 00556 NM 1996 7 10 EISA96045 1 19960507 A 5720 ANGLE BOEING 727 727223 1384074 NM LT WING CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 LEFT WING SKATE ANGLE CRACKED AT AFT HOLE, JUST OUTBOARD OF NR 4 FLAP TRANSMISSION, WING LOWER SURFACE. STOP DRILLED CR ACK, FABRICATED AND INSTALLED DOUBLER PER SRM 51-40-03. (M) 2 L 7 3 4F A3WE 1996071000557 19960710 00557 NM 1996 7 10 EISA96046 1 19960429 A 5720 ANGLE BOEING 727 727223 1384074 NM LT WING CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 LEFT WING TRAILING EDGE ANGLE CRACKED WHERE IT ATTACHES TO UPPER TRAILING EDGE JUST FORWARD OF INBOARD AILERON INBOARD L EADING EDGE. FABRICATED AND INSTALLED NEW BRACKET PER SRM 51-10-01 AND 51-30-02. (M) 2 L 7 3 4F A3WE 1996071000558 19960710 00558 NM 1996 7 10 EISA96047 1 19960429 A 5720 ANGLE BOEING 727 727223 1384074 NM LT WING CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 LEFT WING STIFFENER ANGLE CRACKED AT UPPER TE JUST OUTBOARD OF NR 5 SPOILER. REMOVED CRACKED ANGLE, FABRICATED AND INST ALLED NEW ANGLE PER SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1996071000559 19960710 00559 NM 1996 7 10 EISA96048 1 19960429 A 5730 SKIN BOEING 727 727223 1384074 NM WS 477 TORN A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 LEFT WING LEADING EDGE SKIN TORN .4375 INCH AT CUTOUT FOR NR 3 SLAT, WHERE INBOARD TRACK GOES INTO WS 477. REMOVED EXIS TING REPAIR, FABRICATED AND INSTALLED NEW REPAIR PER SRM 57-30-04. (M) 2 L 7 3 4F A3WE 1996071000560 19960710 00560 NM 1996 7 10 EISA96049 1 19960514 A 5315 FLOOR BEAM BOEING 727 727223 1384074 NM FB 480 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 FOUND CORROSION AROUND FASTENERS ON FLOOR BEAM STATION 480 RBL 50, E/E SLIDE. REMOVED DAMAGED SECTION OF FLOOR BEAM. F ABRICATED AND INSTALLED REPAIR PER SRM 53-10-08. (M) 2 L 7 3 4F A3WE 1996071000561 19960710 00561 NM 1996 7 10 EISA96050 1 19960424 A 5720 DOUBLER BOEING 727 727223 1384074 NM LT WING CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 LEFT WING INBOARD LEADING EDGE STIFFENER, ATTACHED TO LEADING EDGE RIB, HAS DOUBLER CRACKED AT LOWER FASTENER ACCESS THR OUGH PANEL 6301, JUST OUTBOARD OF FORWARD BOTTLE BOLT. REMOVED OLD REPAIR, FABRICATED AND INSTALLED NEW REPAIR PER SRM 51-40-2. (M) 2 L 7 3 4F A3WE 1996071000562 19960710 00562 NM 1996 7 10 EISA96051 1 19960509 A 5754 RIB BOEING 727 727223 1384074 NM NR 3 SLAT CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 LEFT WING NR 3 SLAT INTERNAL 14TH RIB FROM INBOARD END CRACKED. STOP DRILLED CRACK. FABRICATED AND INSTALLED DOUBLER P ER SRM 51-10-03 AND 57-50-03. (M) 2 L 7 3 4F A3WE 1996071000563 19960710 00563 NM 1996 7 10 EISA96052 1 19960509 A 5754 RIB BOEING 727 727223 1384074 NM NR 3 SLAT CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 LEFT WING, NR 3 SLAT INTERNAL RIB 7TH FROM INBOARD END CRACKED. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER PER SRM 51-10-2 AND 57-50-03. (M) 2 L 7 3 4F A3WE 1996071000564 19960710 00564 NM 1996 7 10 EISA96053 1 19960509 A 5754 RIB BOEING 727 727223 1384074 NM NR 4 SLAT CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 FOUND LEFT WING, NR 4 SLAT INTERNAL 5TH RIB FROM INBOARD END, CRACKED. FABRICATED AND INSTALLED DOUBLER PER SRM 57-50-0 3. (M) 2 L 7 3 4F A3WE 1996071000565 19960710 00565 NM 1996 7 10 EISA96054 1 19960424 A 5320 SUPPORT BOEING 727 727223 1384074 NM BS 700 BROKEN A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 FOUND CABIN LEFT SIDE CIRCUMFERENTIAL SUPPORT BRACKET, AT BS 700 STRINGER 15, BROKEN. (M) 2 L 7 3 4F A3WE 1996071000566 19960710 00566 NM 1996 7 10 EISA96055 1 19960509 A 5320 FRAME BOEING 727 727223 1384074 NM RT COCKPIT DAMAGED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 RIGHT NR 3 COCKPIT WINDOW FRAME HAS FASTENER HOLE DAMAGED. ACCOMPLISHED REPAIR IAW BOEING DRW NR COM 25445-5243. (M) 2 L 7 3 4F A3WE 1996071000567 19960710 00567 NM 1996 7 10 EISA96056 1 19960429 A 5320 SPLICE BOEING 727 727223 1384074 NM BS 1010 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 AFT CARGO COMPARTMENT, INTERGRANNULAR CORROSION AT STRINGER 25L SPLICE AT STATION 1010. REMOVED DAMAGED PARTS, FABRICAT ED AND INSTALLED REPAIR PARTS PER SRM 53-10-03. (M) 2 L 7 3 4F A3WE 1996071000568 19960710 00568 NM 1996 7 10 EISA96080 1 19960510 A 5320 CLIP BOEING 727 727223 1384074 NM BS 1050 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 STRINGER CLIP CRACKED AT BS 1050 STRINGER 28R. REPLACED CLIP PER SRM 51-10-02. (M) 2 L 7 3 4F A3WE 1996071000569 19960710 00569 NM 1996 7 10 EISA96081 1 19960510 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 950B CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 FOUND MAIN CABIN BS 950B STRINGER 9R, HAS CRACK AROUND RIVET. STOP DRILLED CRACK. FABRICATED AND INSTALLED DOUBLER PER SRM 51-30-03. (M) 2 L 7 3 4F A3WE 1996071000570 19960710 00570 NM 1996 7 10 EISA96082 1 19960510 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 990 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 AFT CARGO COMPARTMENT BS 990 BETWEEN STRINGER 24L AND 25L, SHEAR TIE CORRODED. FABRICATED AND INSTALLED NEW SHEAR TIE A ND DOUBLER PER SRM 53-10-04. (M) 2 L 7 3 4F A3WE 1996071000571 19960710 00571 NM 1996 7 10 EISA96083 1 19960510 A 5347 TRACK BOEING 727 727223 1384074 NM BS 680-740 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 FOUND NR 4 FLOOR TRACK CORRODED BETWEEN STATION 680-740. REMOVED CORRODED SECTION OF TRACK. INSTALLED NEW SECTION OF T RACK PER SRM 51-30-02. (M) 2 L 7 3 4F A3WE 1996071000572 19960710 00572 NM 1996 7 10 EISA96084 1 19960514 A 5713 STRINGER BOEING 727 727223 1384074 NM WS 601.5 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 FOUND TOP FORWARD STRINGER CRACKED, LEFT WING STATION 601.5. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 57-10-4. (M) 2 L 7 3 4F A3WE 1996071000573 19960710 00573 NM 1996 7 10 EISA96085 1 19960524 A 5313 STRINGER BOEING 727 727223 1384074 NM CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 FOUND FORWARD CARGO, AFT OF DOOR BETWEEN STATION 620 AND STATION 640 STRINGER 26R, CORRODED. REMOVED STRINGER FROM STAT ION 620 TO STATION 650, FABRICATED AND INSTALLED REPAIR PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1996071000574 19960710 00574 NM 1996 7 10 EISA96086 1 19960521 A 5712 RIB BOEING 727 727223 1384074 NM WS 686.5 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 FOUND RIGHT WING STATION 686.5 RIB CRACKED AT SECOND LOWER STRINGER AFT. REMOVED EXISTING REPAIR. FABRICATED AND INSTA LLED REPAIR PER SRM 52-10-05. (M) 2 L 7 3 4F A3WE 1996071000575 19960710 00575 NM 1996 7 10 EISA96087 1 19960524 A 5320 CHANNEL BOEING 727 727223 1384074 NM BS 400-720 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 FOUND FOURTEEN AREAS OF CORROSION IN FWD BAGGAGE BIN ON FLOOR SUPPORT STRUCTURE, FROM FS 480-720D. ALL AREAS OF CORROSI ON REMOVED. SUPPORT STRUCTURE REPAIRED ON SECTIONS, REPLACED AS NECESSARY PER SRM 51-40-4 AND 51-10-2. (M) 2 L 7 3 4F A3WE 1996071000576 19960710 00576 NM 1996 7 10 EISA96088 1 19960612 A 3397 WIRE BOEING 727 727221 1384071 NM EXTERIOR BROKEN A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 363PA 22535 RIGHT EXTERIOR EMERGENCY LIGHT AFT OVERWING INOP. REPAIRED BROKEN WIRE AT LAMP IAW MM 33-20-00. OPS CHECK GOOD. (M) 2 L 7 3 4F A3WE 1996071000577 19960710 00577 1996 7 10 EISA96089 4 19960612 A 2565 22D226967 EVAC SLIDE BOEING 727 727221 1384071 NM R-1 DOOR FAILED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 363PA 22535 R-1 DOOR SLIDE DID NOT DEPLOY AUTOMATICALLY WHEN DOOR WAS OPENED FOR MINIEVACUATION DEMONSTRATION. REMOVED AND REPLACED R-1 DOOR SLIDE IAW MM 25-10-11. (M) 2 L 7 3 4F A3WE 1996071000578 19960710 00578 NM 1996 7 10 F3LA96016 1 19960621 A 3350 6104781 BATTERY PACK BOEING 737 737201 1384454 NM CABIN DISCHARGED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 212US 20212 DEN - DURING AN A-6 CHECK, MAINTENANCE REPORTED THE RIGHT WING EMERGENCY EXIT LIGHT ABOVE INBOARD FLAPS INOPERATIVE. RE PLACED THE RIGHT BATTERY PACK AND CHECKED OK. (M) 2 L 7 2 4F A16WE 1996071000579 19960710 00579 NM 1996 7 10 F3LA96017 1 19960621 A 3350 6013211 POWER SUPPLY BOEING 737 737201 1384454 NM CABIN INOPERATIVE A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 212US 20212 DEN - DURING AN A-6 CHECK, MX REPORTED THE RIGHT EMERGENCY EXIT LIGHT FORWARD OF AFT CARGO DOOR INOPERATIVE. REPLACED T HE RIGHT BATTERY POWER SUPPLY AND CHECKED OK. (M) 2 L 7 2 4F A16WE 1996071000580 19960710 00580 NM 1996 7 10 GAIA9610 1 19960513 A 3230 RETRACT MECH BOEING 727 727251 138408H NM NLG LACK OF LUBE A GAIA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SW 07 278US 21157 FLT 725 - TOL-IAH - WHEN GEAR DOWN WAS SELECTED DURING APPROACH TO IAH, NOSE LANDING GEAR DID NOT EXTEND AND MANUAL EXTE NSION WAS EMPLOYED TO EXTEND GEAR. AIRCRAFT WAS FLOWN TO DFW ON SPECIAL FLIGHT PERMIT FOR INSPECTION PER MM CH 32-33-0. INSPECTION REVEALED NOTHING AMISS, GEAR WAS LUBED AND CYCLED SUCCESSFULLY NUMEROUS TIMES. AIRCRAFT RETURNED TO SERVIC E. (M) 2 L 7 3 4F A3WE 1996071000581 19960710 00581 NM 1996 7 10 GAIA9611 1 19960514 A 3230 65404675 LOCK ACTUATOR 6516368 BOEING 727 727251 138408H NM NLG FAILED A A GAIA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SW 07 278US 272 DASS300992 21157 WHEN GEAR DOWN WAS SELECTED DURING APPROACH TO TOL, NOSE LANDING GEAR DID NOT EXTEND, GEAR WAS CYCLED AND EXTEDNED SUCCE SSFULLY. INVESTIGATION REVEALED HISSING SOUND INDICATIVE OF BYPASSING OF LOCK ACTUATOR. ACTUATOR CHANGED, AIRCRAFT TES T FLOWN SATISFACTORILY AND RETURNED TO SERVICE. A RESUMPTION OF DIFFICULTY WITH NOSE GEAR THE FOLLOWING DAY WOULD TEND TO EXONERATE THE LOCK ACTUATOR. DOOR WAS RE-RIGGED AND GEAR CYCLED 10 TIMES BY NORMAL METHOD AND 3 TIMES MANUALLY. AIR CRAFT WAS RETURNED TO SERVICE AND NO FURTHER TROUBLE REPORTED AS OF THIS DATE MAY 24, 1996. (M) 2 L 7 3 4F A3WE 1996071000582 19960710 00582 NM 1996 7 10 GAIA9612 1 19960517 A 3230 RETRACT MECH BOEING 727 727251 138408H NM NLG MALFUNCTIONED A GAIA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SW 07 278US 21157 WHEN GEAR DOWN WAS SELECTED DURING APPROACH TO TOL, NOSE LANDING GEAR DID NOT EXTEND AND GEAR WAS CYCLED AND EXTENDED SU CCESSFULLY. DOOR WAS RE-RIGGED AND GEAR CYCLED 10 TIMES BY NORMAL METHOD AND 3 TIMES MANUALLY. AIRCRAFT WAS RETURNED T O SERVICE AND NO FURTHER TROUBLE REPORTED. (M) 2 L 7 3 4F A3WE 1996071000583 19960710 00583 NM 1996 7 10 GAIA9613A 1 19960520 A 3230 DOOR MECH BOEING 727 727251 138408H NM NLG OUT OF ADJUST A GAIA O OTHER O OTHER IN INSP/MAINT 1 SW 07 278US 21157 FLT 724 - TOL-PHX - NOSE GEAR DOOR LIGHT ON DURING FLIGHT, DOOR WAS RE-RIGGED AND GEAR CYCLED 10 TIMES BY NORMAL METHOD AND 3 TIMES MANUALLY. AIRCRAFT WAS RETURNED TO SERVICE AND NO FURTHER TROUBLE REPORTED AS OF THIS DATE, MAY 24, 1996. T HIS SDR CLOSES 96-11, 96-12, AND 96-13. (M) 2 L 7 3 4F A3WE 1996071000584 19960710 00584 WP 1996 7 10 GAIA9614 1 19960523 A 3297 WIRE DOUG DC9 DC915F 3022037 WP LT MLG BROKEN A GAIA O OTHER P NO WARNING INDICATION AP APPROACH 1 SW 07 562PC 45348 47012 FLT NR 770 - RFD-BWI - ON APPROACH TO BWI, AFTER EXTENDING THE LANDING GEAR, THE LEFT MAIN GEAR DOWN AND LOCKED GREEN LI GHT WOULD NOT COME ON. ABNORMAL PROCEDURES WERE FOLLOWED TO EXTEND THE LANDING GEAR. AN UNEVENTFUL LANDING WAS MADE. T HE AIRCRAFT WAS FERRIED TO YIP. INSPECTION REVEALED A BROKEN WIRE ON THE LEFT MLG DOWNLOCK SWITCH CONNECTOR. REPAIRED WIRE AND OPS CHECKED SYSTEM PER DC9 MM. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1996071000585 19960710 00585 WP 1996 7 10 GAIA9615 1 19960604 A 5320 9922042 ATTACH FITTING DOUG DC9 DC915F 3022037 WP LWR FUSELAGE. CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 561PC 47014 DURING C-CHECK INSPECTION, REVEALED TEN CRACKED STRUT FRAME ATTACH FITTINGS IN THE LOWER FUSELAGE CARGO COMPARTMENTS. C LOSER INSPECTION REVEALED THE CRACKS TO BE CORROSION CRACKS ALONG GRAIN LINES. SEVEN FRAMES WERE REPLACED IAW THE DOUGL AS SRM AND THREE OF THE FRAMES WERE REPAIRED IAW KITTY HAWK EA D9-53-030. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1996071000586 19960710 00586 WP 1996 7 10 GAIA9616 1 19960604 A 5311 99581981 FRAME DOUG DC9 DC915F 3022037 WP BS 503 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 561PC 44572 47014 DURING C-CHECK INSPECTION, FOUND A CRACK ON THE LEFT FUSELAGE FRAME AT STATION 503, JUST BELOW THE FLOOR LINE. REMOVED AND REPLACED THE CRACKED FRAME IAW DOUGLAS SERVICE BULLETIN 53-117. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1996071000587 19960710 00587 WP 1996 7 10 GAIA9617 1 19960604 A 5313 LONGERON DOUG DC9 DC915F 3022037 WP BS 256-275 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 561PC 44572 47014 DURING C-CHECK INSPECTION, REVEALED CORROSION ON THE RIGHT LONGERON 18 CUSP MEMBRANE BETWEEN FUSELAGE STATION 256 TO 275 . REPAIRED FLOOR IAW KITTY HAWK EA D9-53-032. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1996071000588 19960710 00588 WP 1996 7 10 GAIA9618 1 19960604 A 5330 5910228 SKIN DOUG DC9 DC915F 3022037 WP BS 942 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 561PC 44572 47014 DURING C-CHECK INSPECTION, FOUND CORROSION ON THE FUSELAGE SKIN JUST AFT OF STATION 942, BETWEEN LONGERON 15 AND 18 LEFT . REPAIRED FUSELAGE SKIN IAW KITTY HAWK EA D9-53-031. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1996071000589 19960710 00589 WP 1996 7 10 GAIA9619 1 19960604 A 5330 5911428 SKIN DOUG DC9 DC915F 3022037 WP BS 817-850 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 561PC 44572 47014 DURING C-CHECK INSPECTION, FOUND CORROSION ON THE FUSELAGE SKIN FROM STATION 817 TO 850, BETWEEN LONGERON 20 AND 23 RIGH T. REPAIRED FUSELAGE SKIN IAW KITTY HAWK EA D9-53-026. THE AIRCRAFT WAS RETUREND TO SERVICE. (M) 2 L 7 2 4F A6WE 1996071000590 19960710 00590 WP 1996 7 10 GAIA9620 1 19960604 A 5330 59114113 SKIN DOUG DC9 DC915F 3022037 WP BS 229-313 DENTED A GAIA O OTHER O OTHER IN INSP/MAINT 1 SW 07 561PC 44572 47014 DURING C-CHECK INSPECTION, REVEALED SEVERAL DENTS ON THE FUSELAGE SKIN FROM STATION 220 TO 313, BETWEEN LONGERON 23 AND 27 RIGHT. REPAIRED FUSELAGE SKIN IAW KITTY HAWK EA D9-53-022. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1996071000591 19960710 00591 WP 1996 7 10 GRAA9631 1 19960513 A 3350 6011775 POWER SUPPLY DOUG DC9 DC915 3022036 WP CABIN INOPERATIVE A GRAA K NONE L NO TEST IN INSP/MAINT 1 WP 11 1070T 45784 LINE MAINTENANCE AT RNO, DISCOVERED THAT THE LEFT EMERGENCY NACELLE LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPL ACED THE EMERGENCY POWER PACK. MAINTENANCE PERFORMED AND OPERATIONAL CHECK OF THE SYSTEM. NO DEFECTS WERE NOTED. AIRC RAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1996071000592 19960710 00592 WP 1996 7 10 GRAA9632 1 19960513 A 3350 6011775 POWER PACK DOUG DC9 DC915 3022036 WP CABIN INOPERATIVE A GRAA K NONE L NO TEST IN INSP/MAINT 1 WP 11 1070T 45784 LINE MAINTENANCE AT RNO, DISCOVERED THAT THE RIGHT EMERGENCY NACELLE LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REP LACED THE EMERGENCY POWER PACK. MAINTENANCE PERFORMED AND OPERATIONAL CHECK OF THE SYSTEM. NO DEFECTS WERE NOTED. AIR CRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1996071000593 19960710 00593 WP 1996 7 10 GRAA9633 1 19960530 A 5248 APB DOOR DOUG DC9 DC915 3022036 WP CABIN DEFECTIVE A GRAA B EMER. DESCENT J WARNING INDICATION DE DESCENT 1 WP 11 1068T 45782 DESCENDING INTO BOS WHEN THE CABIN PRESSURE BECAME ERRATIC. THE CAPTIAN REQUESTED A MORE RAPID DESCENT AND THE TOWER AL ERTED THE AIRPORT EMERGENCY EQUIPMENT TO STANDBY. THE AIRCRAFT LANDED AT BOS WITHOUT FURTHER INCIDENT. MX REALIGNED AF T PRESSURE BULKHEAD DOOR, CLEANED SEAL AREA AND REMOVED EXCESS VELCRO FROM AREA. MAINTENANCE PERFORMED AN OPERATIONAL C HECK OF THE PRESSURE SYSTEM. AIRCRAFT PRESSURIZED NORMAL. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1996071000594 19960710 00594 WP 1996 7 10 GRAA9634 1 19960603 A 5248 DOOR SEAL DOUG DC9 DC915 3022036 WP AFT PRESS BULKHD DIRTY A GRAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 11 1068T 45782 AIRCRAFT WOULD NOT PRESSURIZE IN FLIGHT. THE AIRCRAFT RETURNED TO MYR WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE AFT PRESSURE BULKHEAD DOOR NOT SEALING. MAINTENANCE REMOVED THE AFT PRESSURE BULKHEAD DOOR AND CLEANED THE SEAL. MAINT ENANCE REINSTALLED THE AFT PRESSURE BULKHEAD DOOR AND PRESSURIZED THE AIRCRAFT. NO DEFECTS WERE NOTED. AIRCRAFT WAS RE TURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1996071000595 19960710 00595 WP 1996 7 10 GRAA9635 1 19960603 A 2130 PRESSURIZATION DOUG DC9 DC915 3022036 WP CABIN MALFUNCTIONED A GRAA G A O2 MASK DEPLOYED UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 11 1068T 45782 AIRCRAFT WAS CLIMBING THROUGH 26,000 FEET, WHEN THE CABIN ALTITUDE BEGAN TO INCREASE. THE FLIGHT CREW WAS UNABLE TO CON TROL THE PRESSURE IN MANUAL. THE OXYGEN MASKS DEPLOYED AND THE FLIGHT CREW COMPLIED WITH THE RAPID DECOMPRESSION CHECKL IST AND RETURNED TO MYR WITHOUT FURTHER INCIDENT. MAINTENANCE PRESSURIZED THE AIRCRAFT TO 7.5 PSI. MX INSPECTED ALL DOO RS AND WINDOW SEALS AND FOUND NO DEFECTS. MAINTENANCE REINSTALLED THE OXYGEN MASKS. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1996071000596 19960710 00596 WP 1996 7 10 GRAA9636 1 19960603 A 3350 079123 LENS DOUG DC9 DC987 3022087 WP CABIN MISSING A GRAA K NONE O OTHER IN INSP/MAINT 1 WP 11 1074T 49727 AT ENV, MAINTENANCE DISCOVERED THAT THE EMERGENCY FLOOR TRACK LIGHT LENS (RED) WAS MISSING. MAINTENANCE REPLACED THE LE NS AND PEFORMED AN OPERATIONAL CHECK OF THE EMERGENCY FLOOR TRACK SYSTEM. NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO S ERVICE. (M) 2 L 7 2 4F RT A6WE 1996071000597 19960710 00597 WP 1996 7 10 GRAA9637 1 19960529 A 3350 0816300609 TRACK LIGHT DOUG DC9 DC915 3022036 WP CABIN MISSING A GRAA K NONE O OTHER IN INSP/MAINT 1 WP 11 1070T 45784 AT RNO, WHILE PERFORMING AN A-CHECK, MAINTENANCE DISCOVERED THE EMERGENCY FLOOR TRACK LIGHT BELOW SEAT 10 MISSING. MAIN TENANCE REPLACED THE MISSING FLOOR TRACK LIGHT AND PERFORMED AN OPERATIONAL CHECK OF THE SYSTEM. NO DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1996071000598 19960710 00598 WP 1996 7 10 GRAA9638 1 19960529 A 3350 0816300609 TRACK LIGHT DOUG DC9 DC915 3022036 WP CABIN BROKEN A GRAA K NONE L NO TEST IN INSP/MAINT 1 WP 11 1070T 45784 AT RNO, WHILE PERFORMING AN A-CHECK, MAINTENANCE DISCOVERED AT SEAT 5, THE EMERGENCY FLOOR TRACK BROKEN. MAINTENANCE RE PLACED TO EMERGENCY FLOOR TRACK AND PERFORMED AN OPERATIONAL CHECK OF THE SYSTEM. NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1996071000599 19960710 00599 WP 1996 7 10 GRAA9639 1 19960603 A 3350 0816901 SOCKET DOUG DC9 DC987 3022087 WP CABIN DEFECTIVE A GRAA K NONE L NO TEST IN INSP/MAINT 1 WP 11 1074T 49727 LINE MAINTENANCE AT ENV, DISCOVERED THAT THE EMERGENCY FLOOR TRACK LIGHT SOCKET WAS DETECTIVE. MAINTENANCE REPLACED THE EMERGENCY FLOOR TRACK PIGTAIL SOCKET AND PERFORMED AN OPERATIONAL CHECK OF THE SYSTEM. NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A6WE 1996071000600 19960710 00600 1996 7 10 HALA9672 4 19960606 A 3417 2587400436 ADC DOUG DC9 DC951 3022051 WP E/E COMPT MALFUNCTIONED A HALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 EICBG 0981212 47742 FLT 128 - HNL - ON TAKEOFF FLIGHT OFFICERS ALTIMETER AN ALTITUDE ALERT HAD RED FLAGS. CAPTAINS VSI/TCAS SCREEN WENT BLA NK. REPLACED FLIGHT OFFICERS ELECTRIC ALTIMETER AND NR 2 ADC. OPS AND LEAK CHECK OK. REPLACED CAPTAINS VSI/TCAS INDIC ATOR. TEST AND LEAK CHECK OK. (M) 2 L 7 2 4F A6WE 1996071000601 19960710 00601 WP 1996 7 10 HALA9675 1 19960612 A 3320 BALLAST DOUG DC10 DC1010 3022110 WP CABIN OVERHEATED A A HALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 13 122AA 46522 FLT NR 22 - SEA - FLUORESCENT LIGHT BALLAST FIRE AT SEAT 2A BEGAN TO SMOKE HEAVILY AT CRUISE. POWER REMOVED AND ASSOCIA TED CIRCUIT BREAKERS PULLED, SMOKE DISSIPATED. REPLACED BOTH BALLAST ABOVE 2A. OPS CHECKED NORMAL. NO INDICATION OF F IRE. (M) 2 L 7 3 4F A22WE 1996071000602 19960710 00602 WP 1996 7 10 HALA9676 1 19960612 A 3320 FUSE HOLDER DOUG DC10 DC1010 3022110 WP LAV 1B ARCING A A HALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 13 122AA 46522 FLT NR 22 - SEA - NR 5 LAVATORY LIGHT FUSE ARCING IN FUSE HOLDER. POOR SOLDER CONNECTION. INSULATING TAPE FOUND SMOLDE RING. FUSE REMOVED AND LAVATORY SECURED. RESOLDERED NR 5 LAV 1B LIGHT FUSE HOLDER. OPS CHECKED NORMAL. (M) 2 L 7 3 4F A22WE 1996071000603 19960710 00603 NE 1996 7 10 HNAA9692237 2 19960602 A 7200 ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 FAILED A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 922HA 18902 094 FLT 3402 - LYH-PIT - AFTER TAKEOFF, THE NR 1 ENGINE AUTOFEATHERED AND THE TORQUE INDICATION DROPPED TO ZERO. THE AIRCRA FT TURNED BACK TO LYH AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 ENGINE AND THE TORQUE SENSOR CONTROL UNIT. (M) 2 H 7 2 4T 4 T RT A13NM E20NE 1996071000604 19960710 00604 NM 1996 7 10 IXKA9600037 1 19960610 A 2150 PACK SWITCH BOEING 727 727224 1384076 NM COCKPIT OUT OF POSITION A IXKA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 25 32719 20388 FLT NR 38 - TPA-MDW - UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF. TRIED STANDBY AND MANUAL MODE, NO HELP. EVENTUALLY RT PACK TRIP LIGHT ON. RESET NO HELP. SPLIT IN DUCT PSI RT APPROX 80, LEFT 40. NO INDICATION OF PACK TEMP RISE WITH C OOL AIR BEING SELECTED FROM MIX VALVE. AIR TURN BACK TO TPA. OPS CHECK OF SYSTEM ON GROUND WITH SYSTEM SWITCHED TO AIR MODE, OPS CHECK NORMAL AS PER MM 21-31-0. (M) 2 L 7 3 4F A3WE 1996071000605 19960710 00605 NM 1996 7 10 IXKA9600038 1 19960610 A 2750 M59391130ZC POWER UNIT MOTOR VICKERS M59391130ZC BOEING 727 727230 1384080 NM TE FLAPS SEAL LEAKING A A IXKA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 25 357KP MX210106C 20675 FLT NR 24 - MCO-MDW - DIVETED TO ATL AFTER 'A' SYSTEM HYDRAULIC QUANTITY AND PRESSURE WENT TO ZERO IN FLIGHT. FOUND HYD RAULIC MOTOR SHAFT SEAL BLOWN ON RIGHT OUTBOARD FLAP POWER UNIT. REMOVED AND REPLACED RIGHT FLAP POWER UNIT HYDRAULIC M OTOR AND OPS CHECK OK, NO LEAK AS PER MM 27-51-62. REMOVED AND REPLACED NR 1 ENGINE 'A' SYSTEM HYDRAULIC PUMP AND CASE DRAIN FILTER PRECAUTIONARY AS PER MM 29-11-33 AND 29-11-41 AND REMOVED AND REPLACED NR 2 ENGINE HYD PUMP AND CASE DRAIN FILTER PRECAUTIONARY PER ABOVE MM REF. (M) 2 L 7 3 4F A3WE 1996071000606 19960710 00606 WP 1996 7 10 IXXA9683 1 19960530 A 2612 FIRE WARNING DOUG DC8 DC871 302199A WP NR 4 ENGINE SHORTED A IXXA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SW 11 824BX 45946 EN ROUTE FROM DEN-TOL - THE NR 4 ENGINE FIRE WARNING SHORT CIRCUIT LIGHT CAME ON INTERMITTENTLY, FOLLOWED BY A STEADY LI GHT. AFTER THREE MINUTES, THE SYSTEM WOULD NO LONGER TEST. SHORTLY THEREAFTER, THE FIRE WARNING LIGHT ILLUMINATED AND THE ENGINE WAS SHUT DOWN. THE AIRCRAFT PROCEEDED TO TOL UNEVENTFULLY, WHERE TROUBLESHOOTING DETERMINED THAT A FIRE SENS ING ELEMENT HAD AN INTERMITTENT SHORT. THE SENSING ELEMENT WAS REMOVED AND REPLACED, AND THE AIRCRAFT WAS RETURNED TO S ERVICE AFTER A FUNCTIONAL TEST OF THE NEW ELEMENT. (M) 2 L 7 4 4F 4A25 1996071000607 19960710 00607 NE 1996 7 10 IXXA9684 2 19960601 A 7510 ENG ANTI-ICE DOUG DC8 DC871 302199A WP GE CFM56 CFM562C1 13802 NE NR 2 ODOR A IXXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 11 829BX 45994 EN ROUTE BETWEEN DFW AND TOL, THE USE OF THE NR 2 ENGINE ANTI-ICE PRODUCED AN ODOR SIMILAR TO A BURNED MATCH, BUT THE OD OR DISSIPATED OVER THE COURSE OF THE FLIGHT. IN TOL, A GROUND RUN WAS ACCOMPLISHED WITH THE AIRCRAFT CLOSED. BOTH AIR CONDITIONING PACKS WERE OPERATED AS WELL AS ALL FOUR ENGNE ANTI-ICE SYSTEMS. ALL SYSTEMS OPERATED NORMALLY WITH NO ODOR BEING PRODUCED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 4 4F 4 F 4A25 E2GL 1996071000608 19960710 00608 WP 1996 7 10 IXXA9685 1 19960601 A 2120 AIR DISTR DOUG DC8 DC871 302199A WP COCKPIT ODOR A IXXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 11 829BX 45994 EN ROUTE FROM TOL-DFW - THE FLIGHT CREW NOTED A FAINT SULPHUR LIKE ODOR PRESENT AT TIMES IN COCKPIT, POSSIBLY COMING FRO M THE COCKPIT LIGHTING. ON THE GROUND IN DFW, THE COCKPIT LIGHTS WERE OPERATED AND INSPECTED. THE COCKPIT LIGHTING SYS TEMS OPERATED NORMALLY AND DID NOT PRODUCE AN ODOR. (M) 2 L 7 4 4F 4A25 1996071000609 19960710 00609 NE 1996 7 10 IXXA9686 2 19960618 A 7510 735138 CLAMP DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3 52039 NE NR 4 ENG BROKEN A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 51CX 46027 INVESTIGATION OF THIS EVENT FOUND AN ENGINE ANTI-ICE DUCT CLAMP BOLT HAD FAILED ALLOWING BLEED AIR TO ENTER THE ENGINE C OWLING. THE HOT AIR DAMAGED THE ENGINE WIRING HARNESS WHICH CAUSED SEVERAL ENGINE INDICATION SYSTEM MALFUNCTIONS. INSP ECTION OF THE REMAINING CLAMP FOUND A CRACKED FLANGE. OVERTORQUE OF THE BOLT AND CLAMP ARE SUSPECTED TO BE THE FAILURE MODE OF THIS ASSEMBLY. THE CLAMP ASSY, ANTI-ICE DUCT, WIRING HARNESS AND SEVERAL ASSOCIATED COMPONENTS WERE REPLACED AN D THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 4 4F 4 F 4A25 1E8 1996071000610 19960710 00610 EU 1996 7 10 M3HA96016 1 19960619 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A M3HA K NONE L NO TEST IN INSP/MAINT 1 WP 13 4206G 530 081 HNL - AFT SECTION OF EMERGENCY LIGHTS REMAIN ILLUMINATED WHEN POWERING DOWN. REMOVED AND INSTALLED EMERGENCY BATTERY PA CK. (M) 2 H 7 2 4T RT A53EU 1996071000611 19960710 00611 SW 1996 7 10 MALA965010 1 19960530 A 5330 SKIN SWRNGN SA227 SA227AC 8780603 SW BS 227.271 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 438MA AC721B DURING SCHEDULED MAINTENANCE IN MSP, MAINTENANCE NOTED A FUSELAGE CONSTANT SECTION SKIN CRACK AT FS 227.271. REPAIRS WE RE COMPLETED BY INSTALLING A REPAIR DOUBLER IAW FAC SRM 51-50-02 AND ARP 51-70-9132. (M) 2 L 7 2 4T RT A8SW 1996071000612 19960710 00612 SW 1996 7 10 MALA965011 1 19960530 A 5330 SKIN SWRNGN SA227 SA227AC 8780603 SW BS 189.06 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 438MA AC721B DURING SCHEDULED MAINTENANCE IN MSP, MAINTENANCE FOUND A FUSELAGE CONSTANT SECTION SKIN CRACKED ON THE RIGHT SIDE AT FS 189.06. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING A REPAIR DOUBLER IAW FAC SRM 51-90-02 PAGES 4-5 AND ARP 51 -70-9132. (M) 2 L 7 2 4T RT A8SW 1996071000613 19960710 00613 SW 1996 7 10 MALA965012 1 19960530 A 5330 SKIN SWRNGN SA227 SA227AC 8780603 SW BS 212.27. (M) CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 438MA AC721B DURING SCHEDULED MAINTENANCE IN MSP, MAINTENANCE FOUND A CONSTANT SECTION SKIN CRACK AT FS 212.27 ON THE LEFT SIDE. REP AIRS WERE COMPLETED BY FABRICATING AND INSTALLING A REPAIR DOUBLER IAW FAC SRM 51-90-02 PAGES 4-5 AND ARP 51-70-9132. ( M) 2 L 7 2 4T RT A8SW 1996071000614 19960710 00614 SW 1996 7 10 MALA965013 1 19960530 A 5720 ANGLE SWRNGN SA227 SA227AC 8780603 SW WING/NACELLE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 438MA AC721B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE LEFT INBOARD LOWER WING TO NACELLE TRANSIT ANGLE CRACKED AT THE LEADING EDGE AREA. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING A REPAIR DOUBLER IAW EA-01-96043. (M) 2 L 7 2 4T RT A8SW 1996071000615 19960710 00615 SW 1996 7 10 MALA965018 1 19960606 A 5320 SUPPORT SWRNGN SA227 SA227AC 8780603 SW BS 107 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 424MA AC639 DURING SCHEDULED MAINTENANCE IN MSP, MAINTENANCE FOUND PILOTS SIDE SEAT TRACK SUPPORT CHANNEL AT FS 107 CRACKED BETWEEN RIVETS ON NUT PLATE. FABRICATED AND INSTALLED DOUBLER PER ARP 53-10-9322. (M) 2 L 7 2 4T RT A8SW 1996071000616 19960710 00616 SW 1996 7 10 MALA965020 1 19960609 A 5270 WARNING LIGHT SWRNGN SA227 SA227AC 8780603 SW CARGO COMPT ILLUMINATED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 26906 AC654B FLT 3352 - ON CLIMB-OUT FROM DTW, THE CARGO DOOR WARNING LIGHT ILLUMINATED. THE CREW PERFORMED QUICK REFERENCE PROCEDUR ES AND RETURNED TO DTW. MAINTENANCE FOUND THE PASSENGER BAGS AGAINST THE CARGO DOOR. THE BAGS WERE REARRANGED, AND ALL CHECKS WERE SATISFACTORY. (M) 2 L 7 2 4T RT A8SW 1996071000617 19960710 00617 SW 1996 7 10 MALA965021 1 19960607 A 2150 PACK SWRNGN SA227 SA227AC 8780603 SW LEFT SMOKING A MALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 422MA AC635 FLT NR 3283 - WHILE TAXIING TO THE GATE IN DTW, SMOKE BEGAN TO COME THROUGH THE BLEED AIR VENTS. THE CREW TURNED OFF TH E BLEEDS AND THE SMOKE DISSIPATED. MAINTENANCE DEFERRED THE LEFT AIR CONDITIONING SYSTEM. (M) 2 L 7 2 4T RT A8SW 1996071000618 19960710 00618 NM 1996 7 10 MZZA96007 1 19960201 A 5241 65C1990119 LATCH BOEING 727 7272F9 138407D NM R1 GALLEY DOOR DAMAGED A A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 75429 21427 TNN - DURING 1/4D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, EXCESSIVE BROKEN WIRES WERE FOUND ON R1 GALLEY DOOR ESCAPE S LIDE LATCH CABLE. THE DAMAGED ESCAPE SLIDE LATCH ASSEMBLY WAS REMOVED AND REPLACED PER B727 MM 25-60-15. REF: HANGAR N ON ROUTINE REPAIR ITEM CARD NR 0724976 (SEQ 02086). (M) 2 L 7 3 4F RT A3WE 1996071000619 19960710 00619 NM 1996 7 10 MZZA96008 1 19960207 A 5220 69459345 CABLE BOEING 727 7272F9 138407D NM EMER EXIT STEP DAMAGED A A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 75429 21427 TNN - DURING 1/4D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, EXCESSIVE BROKEN WIRES WERE FOUND ON RIGHT AFT OVERWING EMER GENCY ESCAPE HATCH STEP AFT CABLE. THE DAMAGED CABLE ASSEMBLY WAS REMOVED AND REPLACED PER B727 MM 52-21-0. REF: HANGA R NON ROUTINE REPAIR ITEM CARD NR 0724983. (SEQ NR 02093) (M) 2 L 7 3 4F RT A3WE 1996071000620 19960710 00620 NM 1996 7 10 MZZA96009 1 19960204 A 3350 LIGHT BOEING 727 7272F9 138407D NM CABIN MISSING A MZZA K NONE L NO TEST IN INSP/MAINT 1 WP 13 75429 21427 TNN - DURING 1/4D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, NR 4 GALLEY EMERGENCY 'EXIT' LIGHT LENS WAS FOUND MISSING. T HE DAMAGED 'EXIT' LIGHT ASSEMBLY WAS REMOVED AND REPLACED WITH P/N BS 9279-103 ASSEMBLY PER B727 MM 33-50-11 AND OPERATI ONAL CHECK FOUND SATISFACTORY. REF: HANGAR NON ROUTINE REPAIR ITEM CARD NR 832771 (SEQ NR 02201). (M) 2 L 7 3 4F RT A3WE 1996071000621 19960710 00621 NM 1996 7 10 MZZA96010 1 19960203 A 3350 COVER BOEING 727 7272F9 138407D NM CABIN BROKEN A MZZA K NONE L NO TEST IN INSP/MAINT 1 WP 13 75429 21427 TNN - DURING 1/4D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, BROKEN COVERS WERE FOUND ON AFT ENTRY DOOR AND NEAR L1 ENTRY DOOR 'EXIT' SIGN. THE DAMAGED 'EXIT' SIGN ASSEMBLIES WERE REMOVED AND REPLACED WITH BR9279-105 ASSEMBLIES PER B 727 MM 33-50-11 AND OPERATIONAL CHECK FOUND SATISFACTORY. REF: HANGAR NON ROUTINE REPAIR ITEM CARD NR 832772 AND 832999 (SEQ NR 02199, 02202) (M) 2 L 7 3 4F RT A3WE 1996071000622 19960710 00622 NM 1996 7 10 MZZA96011 1 19960203 A 3350 COVER BOEING 727 7272F9 138407D NM CABIN BROKEN A MZZA K NONE L NO TEST IN INSP/MAINT 1 WP 13 75429 21427 TNN - DURING 1/4D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, BROKEN COVER WAS FOUND ON L2 GALLEY SERVICE DOOR 'EXIT' SIGN . THE DAMAGED 'EXIT' SIGN ASSEMBLY WAS REMOVED AND REPLACED WITH P/N BR9279-106 ASSEMBLY PER B727 MM 33-50-11 AND OPERA TIONAL CHECK FOUND SATISFACTORY. REF; HANGAR NON ROUTINE REPAIR ITEM CARD NR 833000 (SEQ NR 02200). (M) 2 L 7 3 4F RT A3WE 1996071000623 19960710 00623 WP 1996 7 10 ORJA9633 1 19960522 A 3246 26088911 BOLT DOUG DC9 DC983 3022083 WP NR 2 WHEEL/TIRE MISSING A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 833RA 4553 53045 NR 2 MAIN TIRE THROUGH-BOLT MISSING. CHANGED NR 2 W/T ASSEMBLY. (M) 2 L 7 2 4F RT A6WE 1996071000624 19960710 00624 WP 1996 7 10 ORJA9634 1 19960602 A 3210 3935373501 BOLT DOUG DC9 DC983 3022083 WP LT MLG SHEARED A A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 832RA 160 53044 LEFT MAIN LANDING GEAR LOWER TORQUE LINK ASSEMBLY BOLT SHEARED. REMOVED AND REPLACED LOWER TORQUE LINK PIN, LOCK BOLT A ND OUTBOARD BULKING. OPS CHECK GOOD AS PER MM 32-11-04. (M) 2 L 7 2 4F RT A6WE 1996071000625 19960710 00625 WP 1996 7 10 ORJA9635 1 19960606 A 7930 OIL SCREEN LIGHT DOUG DC9 DC982 3022082 WP RT ENGINE ILLUMINATED A ORJA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 11 842RA 49604 ON CLIMB-OUT FROM SEA-ANC - 25,000, R OIL STRAINER CLOG LIGHT CAME ONE. REFERRED TO AOM AND PERFORMED IN FLIGHT AIR RET URN. NO OTHER INDICATIONS WERE ABNORMAL. LIGHT NEVER WENT OUT UNTIL TURNING OFF RUNWAY. OVERWEIGHT LANDING WAS MADE AT 131.7 LBS. REMOVED AND REPLACED RIGHT ENGINE OIL SCREEN. RAN ENGINE APPROX 15 MINUTES. RE-CHECKED OIL SCREEN. NO CLOGGING NOTED. SCREEN LEAK CHECKS NORMAL. SCREEN REPLACED PER RENO AIR MM 110/79-20 PAGE 202. ACCOMPLISHED OVERWEIGH T LANDING INSPECTION PER RENO AIR MM 05-51-04. (M) 2 L 7 2 4F A6WE 1996071000626 19960710 00626 NE 1996 7 10 ORJA9636 2 19960609 A 7200 ENGINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE RIGHT FAILED A A ORJA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 11 871RA 49788 NR 2 ENGINE FAILURE. PERFORMED ENGINE IN FLIGHT SHUTDOWN PROCEDURES IAW FCOM. AIR RETURN TO RENO. FOUND MASSIVE LPT F AILURE. REMOVED AND REPLACED NR 2 ENGINE IAW MM 71-00-00 AND WORK CARD 0099. PERFORMED HI POWER TRIM IAW MM 71-00-00. ALL PARAMETERS CHECK GOOD. NO LEAKS NOTED. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 1996071000627 19960710 00627 EU 1996 7 10 RAIA960521 1 19960515 A 3610 S3611009700000 BLEED LINE AEROSP ATR42 ATR42300 8680920 EU RT ENGINE LEAKS A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 421TE 17579 102 STL - FLT 7402 - RIGHT ENGINE WOULD NOT MAKE TARGET TORQUE. MX REPLACED THE RIGHT ENGINE NACELLE BLEED LINE. GROUND RU NS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1996071000628 19960710 00628 WP 1996 7 10 RAIA960522 2 19960516 A 7320 8974575 BYPASS VALVE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP NR 2 ENG FUEL STICKING A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 862AE 6818 3540 862 66107 MRY - FLT 4760 - ON CLIMB, NR 2 ENGINE FUEL FLOW, TORQUE AND EGT DROPPED OFF. MX REPLACED FUEL BYPASS VALVE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996071000629 19960710 00629 WP 1996 7 10 RAIA960523 2 19960517 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP NR 2 MALFUNCTIONED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 429AM 9605 3516 879 66157 STL - FLT 7050 - NR 2 ENGINE LOW TORQUE. REMOVED AND REPLACED ENGINE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996071000630 19960710 00630 EU 1996 7 10 RAIA960524 1 19960518 A 2121 125220011 FAN BLOWER JETAIR JETSTM JETSTM4101 1500501 EU CABIN OVERHEAT A RAIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 562HK 631 41078 DCA - FLT 7742 - SMOKE IN CABIN DURING TAXI. REPLACED AIRCONDITIONING BLOWER FAN MOTOR. (M) 2 L 7 2 4T RT A41NM 1996071000631 19960710 00631 EU 1996 7 10 RAIA960525 1 19960519 A 7722 8972052 EGT RESISTOR BAG JETSTM JETSTM3201 1500217 EU NR 1 ENG OUT OF ADJUST A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 423AM 6865 858 STL - FLT 7473 - NR 1 ENGINE WOULD NOT PRODUCE TARGET TORQUE. RESET EGT COMP RESISTOR. (M) 2 L 7 2 4T RT A56EU 1996071000632 19960710 00632 WP 1996 7 10 RAIA960526 2 19960520 A 7320 1379287L405 P3 TUBE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP NR 1 ENG CRACKED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 433AM 10751 885 66163 STL - FLT 7094 - NR 1 ENGINE FUEL PRESSURE AND OIL TEMP IND. CIRCUIT BREAKERS TRIPPED AND WOULD NOT RESET. REPLACED P3 BLEED AIR TUBE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996071000633 19960710 00633 EU 1996 7 10 RAIA960527 1 19960520 A 2910 7445B HYD RELEASE VLV BAG JETSTM JETSTM3201 1500217 EU HYD BAY REQ'D RESET A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 860AE 860 LAX - FLT 4735 - GEAR INTRANSIT LIGHTS WOULD NOT EXTINGUISH WITH GEAR UP. RESET HYDRAULIC RELEASE VALVE. (M) 2 L 7 2 4T RT A56EU 1996071000634 19960710 00634 EU 1996 7 10 RAIA960528 1 19960521 A 7722 8974764L EGT COMPENSATOR BAG JETSTM JETSTM3201 1500217 EU LT ENG FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 972JX 5886 972 FAT - FLT 4724 - LEFT ENGINE EGT AN TORQUE FLUCTUATED. MX REPLACED LEFT EGT COMPENSATOR. PERFORMED GROUND RUNS CHECK G OOD. (M) 2 L 7 2 4T RT A56EU 1996071000635 19960710 00635 EU 1996 7 10 RAIA960530 1 19960523 A 3260 0L8562BPEGPL BULB JETAIR JETSTM JETSTM4101 1500501 EU RT MLG FAILED A RAIA B EMER. DESCENT P NO WARNING INDICATION LD LANDING 1 CE 03 557HK 1234 41074 JFK - FLT 7749 - RIGHT MAIN GEAR DOWN AND LOCK INDICATOR INOP. MAINTENANCE REPLACED BULBS FOR THE RIGHT MAIN GEAR INDIC ATION. (M) 2 L 7 2 4T RT A41NM 1996071000636 19960710 00636 EU 1996 7 10 RAIA960601 1 19960601 A 3234 8662C SELECTOR VALVE BAG JETSTM JETSTM3201 1500217 EU LANDING GEAR FAILED A RAIA B EMER. DESCENT O OTHER LD LANDING 1 CE 03 433AM 10826 885 PAH - FLT 7365 - LANDING GEAR WOULD NOT EXTEND. MX REPLACED THE LANDING GEAR SELECTOR VALVE. PERFORMED GEAR SWING OPS CHECK GOOD. (M) 2 L 7 2 4T RT A56EU 1996071000637 19960710 00637 WP 1996 7 10 RAIA960602 2 19960603 A 7320 8974575 BYPASS VALVE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RT ENG FUEL STUCK A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 860AE 4586 4586 860 70001R FAT - FLT 4752 - RIGHT ENGINE DID NOT ACHIEVE TARGET TORQUE. MX REPLACED THE FUEL BYPASS VALVE. PERFORMED STATIC RUNS, OPS CHECK GOOD. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996071000638 19960710 00638 EU 1996 7 10 RAIA960603 1 19960604 A 3610 311282504 BLEED VLV AEROSP ATR72 ATR72202 8680940 EU LT NACELLE STUCK A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 721TE 217 STL - FLT 7110 - LEFT PACK FAULTED, WOULD NOT RESET. MX FOUND THE LEFT BLEED VALVE STUCK CLOSED. DEFERRED LEFT PACK ME L 21-50-1. (M) 2 H 7 2 4T RT A53EU 1996071000639 19960710 00639 WP 1996 7 10 RRXA96021 1 19960412 A 5311 2751960 FRAME DOUG DC8 DC863F 302198F WP BS 879 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 959R 46143 KMCN - DURING C-CHECK, FOUND HOLES DRILLED IN FRAME AT Y=879 ABOVE LONGERON 21 LEFT. FABRICATED AND INSTALLED REPAIR IA W DER APPROVED COTNEY ENGINEERING SKETCH A46-R06 AND DC-8 SRM 51-1-20D. (M) 2 L 7 4 4F 4A25 1996071000640 19960710 00640 WP 1996 7 10 RRXA96022 1 19960412 A 5311 2751960 FRAME DOUG DC8 DC863F 302198F WP BS 759 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 959R 46143 ZIAD - DURING C-CHECK, FOUND HOLE DRILLED IN FRAME AT Y=759 ABOVE LONGERON 21 LEFT. FABRICATED AND INSTALLED REPAIR IAW DER APPROVED COTNEY ENGINEERING SKETCH A46-R07 AND IAW DC-8 SRM 53-2-0, 53-7-3. (M) 2 L 7 4 4F 4A25 1996071000641 19960710 00641 WP 1996 7 10 RRXA96026 1 19960412 A 5320 PRESSURE WEB DOUG DC8 DC863F 302198F WP BS 879.375 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 959R 46143 KMCN - DURING C-CHECK, FOUND CORROSION ON UPPER WHEEL WELL WEB AT Y=879.375, FROM X=57 TO X=66 AND Z=10. CORROSION REMO VED, REQUIRED CUTTING PRESSURE WEB CUSP ANGLE AND HAT CHANNEL. REMOVED DAMAGE AREAS OF PRESS WEB, FABRICATED AND INSTAL LED REPAIRS TO WEB CUSP ANGLE AND HAT SECTION IAW DER APPROVED COTNEY ENGINEERING SKETCH A46-R04, 1 THROUGH 5 REV A AND TREATED AREA IAW DC-8 SRM 51-1-8. (M) 2 L 7 4 4F 4A25 1996071000642 19960710 00642 WP 1996 7 10 RRXA96027 1 19960414 A 5320 WEB DOUG DC8 DC863F 302198F WP BS 902 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 959R 46143 KMCN - DURING C-CHECK, FOUND CORROSION BULGE AND LONGITUDINAL STIFFENER CRACKED TOP RIGHT WHEEL WELL AT Y=902, X-25 AND Z=10. REMOVED CORROSION AND 6 INCH SECTION OF STIFFENER (CUT OUT 5.250 INCH BY 6.75 INCH). REMOVED SECTION OF PRESS WE B. FABRICATED AND INSTALLED REPAIR TO PRESS WEB STIFFENER IAW DER APPROVED COTNEY ENGINEERING SKETCH A46-R01 AND TREATE D AREA IAW DC-8 SRM 51-1-8. (M) 2 L 7 4 4F 4A25 1996071000643 19960710 00643 WP 1996 7 10 RRXA96028 1 19960414 A 5753 PLATING DOUG DC8 DC863F 302198F WP WS 207 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 959R 46143 KMCN - DURING C-CHECK, FOUND SKIN CRACKED THROUGH RIVET INBOARD SLOT L/E UPPER, OUTBOARD FORWARD RIGHT WING. FABRICATED DOUBLER FROM 7075T6 AL AND INSTALLED IAW DER APPROVED COTNEY ENGINEERING SKETCH A46-R02 AND IAW DC-8 SRM 51-1-21, 51-1- 20C. (M) 2 L 7 4 4F 4A25 1996071000644 19960710 00644 WP 1996 7 10 RRXA96029 1 19960411 A 5743 5893936505N FITTING DOUG DC8 DC863F 302198F WP LT MLG CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 959R 46143 KMCN - DURING C-CHECK, FOUND LEFT MLG SUPPORT FITTING CRACKED. CONFIRMED WITH DYE CHECK AND EDDY CURRENT. REMOVED REPL ACED LEFT MLG SUPPORT FITTING IAW DC-8 SRM 51-3-0 AND DACO MLG FITTING REPLACEMENT GUIDE. (M) 2 L 7 4 4F 4A25 1996071000645 19960710 00645 WP 1996 7 10 RRXA96030 1 19960414 A 5730 PLATING DOUG DC8 DC863F 302198F WP WS 210 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 959R 46143 KMCN - DURING C-CHECK, FOUND LEADING EDGE SKIN CRACK THROUGH HI-LOCK LOWER RIGHT AT XFS 210 BELOW INBOARD END OF ACCESS 583C. FABRICATED AND INSTALLED REPAIR IAW DER APPROVED COTNEY ENGINEERING SKETCH A46-R03. (M) 2 L 7 4 4F 4A25 1996071000646 19960710 00646 EU 1996 7 10 SABA9600014 1 19960315 A 2750 SD3452605XA CABLE STBROS SD3 SD360 8100606 EU LT TE FLAP BROKEN A A SABA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 33 153CC SH3753 FLT 5097 - PGV-CLT - ON DEPARTURE, THE FLAPS WERE RETRACTED AND THE LT SIDE FAILED TO RETRACT CORRECTLY. THE CAPT DECID ED TO MAKE A PRECAUTIONARY LANDING IN ISO. THE ASYMMETRIC FLAP CHECKLIST WAS FOLLOWED AND THE A/C MADE AN UNEVENTFUL LA NDING. A MECH AND INSPECTOR WERE DISPATCHED TO ISO. THE A/C FLAP SYS WAS INSPECTED AND THE LT LWR O/B FLAP CABLE WAS F OUND BROKE APPROX 18 IN FROM THE INNER TURNBUCKLE. THE FLAPS WERE RETRACTED, PINNED IN THE RETRACTED POSITION, AND THE A/C FERRIED BACK TO CLT SO REPAIRS COULD BE MADE. ONCE THE A/C ARRIVED IN CLT, THE LT LWR O/B FLAP CABLE WAS REPLACED. THE FLAP SYS WAS THEN GIVEN A FULL OPS TEST. AFTER SATIS COMPLETING THE FLAP SYS TEST, A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T A41EU 1996071000647 19960710 00647 NE 1996 7 10 SIMA961691 2 19960617 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RIGHT FAILED A SIMA A E UNSCHED LANDING ENGINE SHUTDOWN O OTHER CL CLIMB 1 SW 21 371AE 340B371 GEE7085602 SGF - FLT 3654 - DURING CLIMB-OUT, CREW REPORTED A BANG FOLLOWED BY NR 2 ENGINE SHUTDOWN. AIRCRAFT LANDED WITHOUT INCID ENT IN SGF. MX REPLACED ENGINE. OPS CHECKS AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. FAIL ED ENGINE BEING SENT TO STROTHERS FOR TEARDOWN AND EVALUATION. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 1996071000648 19960710 00648 NM 1996 7 10 TSAA9653041 1 19960613 A 5312 BULKHEAD CHORD BOEING 737 7372S2C 138448G NM BS 727 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 806AL 21927 DURING HEAVY MAINTENANCE VISIT, DISCOVERED BS 727 BULKHEAD RIGHT CUTBOARD CHORD CRACKED APPROX 6 INCHES. REPAIRED PER E CO 1785R1. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1996071000649 19960710 00649 NM 1996 7 10 TSAA9653043 1 19960613 A 5313 STRINGER BOEING 737 7372S2C 138448G NM BS 907 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 806AL 21927 DURING HEAVY MAINTENANCE VISIT, FOUND STRINGER 26L EXFOLIATED AT BS 907. REPAIRED PER ECO 2599R1. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1996071000650 19960710 00650 NM 1996 7 10 TSAA9653044 1 19960613 A 5311 FRAME BOEING 737 7372S2C 138448G NM BS 400 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 806AL 21927 DURING HEAVY MAINTENANCE VISIT, FOUND FRAME CRACK, BS 400 STRINGER 21L. REPAIRED PER SRM 53-10-4. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1996071000651 19960710 00651 NM 1996 7 10 TSAA9653045 1 19960613 A 5311 FRAME BOEING 737 7372S2C 138448G NM BS 480 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 806AL 21927 DURING HEAVY MAINTENANCE VISIT, FOUND FRAME CRACK BS 480 STRINGER 22L. REPAIRED PER SRM 53-10-4. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1996071000652 19960710 00652 NM 1996 7 10 TSAA9653046 1 19960613 A 5320 CLIPS BOEING 737 7372S2C 138448G NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 806AL 21927 DURING HEAVY MAINTENANCE VISIT, FOUND CRACKED TIE CIP AT BS 639 STRINGER 3L, BS 685 STRINGER 3R, BS 685 STRINGER 4R, BS 706 STRINGER 3R, BS 706 STRINGER 9L, BS 727A STRINGER 4L, BS 727A STRINGER 6R, BS 706 STRINGER 4R, BS 727B STRINGER 6R, AND BS 727B STRINGER 4L. REPLACED TIE CLIPS PER SRM 51-10-1. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1996071000653 19960710 00653 NM 1996 7 10 TSAA9657042 1 19960613 A 5711 SPAR CAP BOEING 737 7372S2C 138448G NM FSS 280/300/416 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 806AL 21927 DURING HEAVY MAINTENANCE VISIT, FOUND RIGHT WING FRONT SPAR LOWER CAP FORWARD LOWER SIDE. EXFOLIATION CORROSION AT FSS 280, 300, AND 416.8. REPAIRED PER ECO 2135. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1996071000654 19960710 00654 NE 1996 7 10 TWRA9640 2 19960617 A 7260 SNF62433 MAIN GEAR BOX BOEING 747 747136 1384883 NM PWA JT9 JT9D7A 52054 NE NR 2 ENG FAILED A A TWRA B E F EMER. DESCENT ENGINE SHUTDOWN ACTIVATE FIRE EXT. J M WARNING INDICATION OVER TEMP DE DESCENT 1 EA 15 606FF 75430 11040 20273 662938 DURING CRUISE FLIGHT 22 FROM LAX TO JFK, THE NR 2 ENGINE CSD OIL LIGHT AND GENERATOR OPEN LIGHT ILLUMINATED, THE CSD COU LD NOT BE DISCONNECTED. PMG INDICATION WAS 8000 RPM. THE ENGINE WAS BEING SHUT DOWN DUE TO CSD FAILURE, AT THIS TIME T HE NR 2 ENGINE LOST OIL PRESSURE AND THE LIGHT ILLUMINATED. THE NR 2 ENGINE HAD FIRE WARNING INDICATION. BOTH FIRE BOT TLES WERE USED AND THE FIRE WARNING LIGHT REMAINED ILLUMINATED THROUGH FLIGHT TO BLOCKS. AN EMERGENCY WAS DECLARED. UP ON ARRIVAL AT JFK, THE MAIN GEAR BOX WAS FOUND TO HAVE FAILED. THE ENGINE S/N 662938 WAS REMOVED AND REPLACED. (M) 2 L 7 4 4F 4 F A20WE E20EA 1996071000655 19960710 00655 NM 1996 7 10 TWRA9641 1 19960613 A 2611 CONNECTOR BOEING 747 747121 1384871 NM SMOKE ALARM LOOSE A TWRA K NONE N FALSE WARNING CR CRUISE 1 EA 15 604FF 19659 CREW REPORTED UPPER DECK SMOKE ALARM SOUNDS INTERMITTENTLY WITH NO INDICATION OF SMOKE PRESENT. DURING TROUBLESHOOTING, MAINTENANCE FOUND LOOSE CANNON PLUG CONNECTOR AT DETECTOR. SECURED CONNECTOR, OK. (M) 2 L 7 4 4F A20WE 1996071000656 19960710 00656 WP 1996 7 10 USAA960471 1 19960612 A 5330 SKIN DOUG DC9 DC931 3022065 WP PAX DOOR CUTOUT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 941VJ 47054 PIT - DURING C-4 INSPECTION, FOUND TWO .25 INCH CRACKS IN MAIN ENTRANCE STAIRWELL DOOR CUTOUT IN THE FUSELAGE SKIN BOTTO M AFT CORNER. VISUAL EDDY CURRENT CONFIRMED. INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 57A. (M) 2 L 7 2 4F A6WE 1996071000657 19960710 00657 NM 1996 7 10 USAA960472 1 19960614 A 5315 FLOOR BEAM BOEING 737 7373B7 1384580 NM BS 967 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 515AU 29143 23701 CLT - INSPECTION VISUALLY FOUND LEVEL 2 CORROSION, AT NUT PLATE HOLES ACROSS FLOORBEAM, LOCATED AT STATION 967. INSTALL ED NEW CHORD AND REPAIR ANGLES PER T/R 53-15-91A. (M) 2 L 7 2 4F RT A16WE 1996071000658 19960710 00658 NM 1996 7 10 USAA960473 1 19960614 A 5315 FLOOR BEAM BOEING 737 7373B7 1384580 NM B 986.5 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 515AU 29143 23701 CLT - INSPECTION VISUALLY FOUND LEVEL 2 CORROSION AT NUT PLATE HOLES, ACROSS FLOORBEAM LOCATED AT STATION 986.5. INSTAL LED NEW CHORD AND REPAIR ANGLES AS PER T/R 53-10-05. (M) 2 L 7 2 4F RT A16WE 1996071000659 19960710 00659 NM 1996 7 10 USAA960474 1 19960614 A 5315 FLOOR BEAM BOEING 737 737301 1384611 NM BS 986.5 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 351US 26400 23554 CLT - INSPECTION VISUALLY FOUND LEVEL 2 CORROSION ON TOP OF FLOORBEAM LOCATED AT STATION 986.5 RBL 12 AND RBL 14. INSTA LLED NEW CHORD AND REPAIR ANGLES AS PER T/R 53-10-05. (M) 2 L 7 2 4F RT A16WE 1996071000660 19960710 00660 NM 1996 7 10 USAA960497 1 19960622 A 5414 SKIN BOEING 737 7374B7 1384702 NM PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 431US 19428 24553 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK LOWER AFT CORNER OF PYLON SKIN ACCESS OPENING STRINGER 727 L. CUT OUT CRACK, INSTALLED FILLER AND DOUBLER. REPAIRED PER EA 41241. (M) 2 L 7 2 4F RT A16WE 1996071000661 19960710 00661 WP 1996 7 10 USAAD96077 1 19960614 A 3222 733A9FT160P3 STRUT SEAL DOUG DC9 DC931 3022065 WP NLG FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 914VJ 47068 FLT 1541 - PIT-ATL - AFTER TAKEOFF, NOSE GEAR UNSAFE LIGHT REMAINED ON. NOISE INDICATED NOSE GEAR WAS STILL DOWN. GEAR HANDLE PUT DOWN, AND NOSE GEAR INDICATION REMAINED UNSAFE UNTIL NOSE STEERING WHEEL MOVED. THEN A THUNK WAS HEARD, AND ALL GEAR INDICATIONS GREEN. FOUND NOSE GEAR STRUT FLAT AND LEAKING FLUID. REPLACED NOSE GEAR STRUT SEAL. (M) 2 L 7 2 4F A6WE 1996071000662 19960710 00662 1996 7 10 USAAD96078 4 19960614 A 2565 D29984109 SLIDE DOUG DC9 DC981 3022081 WP TAILCONE MALFUNCTIONED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 809US 48041 CLEANING DEPARTMENT AT SRQ DEPLOYED TAILCONE AND AFT SLIDE. SLIDE UNROLLED, BUT DID NOT INFLATE. REPLACED SLIDE ASSEMB LY. (M) 2 L 7 2 4F A6WE 1996071000663 19960710 00663 NE 1996 7 10 USAAD96079 2 19960615 A 7200 ENGINE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7B 52053 NE LEFT FAILED A USAA A UNSCHED LANDING Y ENGINE STOPPAGE DE DESCENT 1 EA 19 984VJ 47207 657475 FLT 490 - SDF-CLT - DURING DESCENT LEFT ENGINE FAILED. 13 MINUTES SINGLE ENGINE TIME. REPLACED LEFT ENGINE. (M) 2 L 7 2 4F 4 F A6WE E2EA 1996071000664 19960710 00664 WP 1996 7 10 USAAD96080 1 19960616 A 7932 8TJ92GAA2 OIL QTY TRANSM DOUG DC9 DC931 3022065 WP NR 2 ENG FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 923VJ 48143 FLT 476 - ELM-PIT, AFTER TAKEOFF, NR 2 ENGINE OIL QUANTITY STARTED TO DECREASE APPROXIMATELY 2 QUARTS/ 10 SECONDS. QUAN TITY STAYED AT 3 QUARTS. RETURNED TO FIELD. ENGINE OIL QUANTITY CHECKED AND FOUND FULL. AIRCRAFT RELEASED PER MEL 79- 3. REPLACED THE NR 2 OIL QUANTITY TRANSMITTER. (M) 2 L 7 2 4F A6WE 1996071000665 19960710 00665 WP 1996 7 10 USAAD96081 1 19960616 A 3350 685551 LIGHT DOUG DC9 DC931 3022065 WP ESCAPE SLIDE INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 943VJ 47058 EMERGENCY LIGHT SLIDE COVER LIGHT INOPERATIVE. REPLACED LIGHT AND INSTALLED NEW BATTERY. (M) 2 L 7 2 4F A6WE 1996071000666 19960710 00666 WP 1996 7 10 USAAD96082 1 19960618 A 5280 5936706506N SUPPORT FITTING DOUG DC9 DC931 3022065 WP RT NLG DOOR CRACKED A USAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 19 977VJ 48155 FLIGHT 8002 - MDT-CLT - AFTER GEAR RETRACTION, CREW NOTED WIND NOISE FROM NOSE GEAR AREA. RETURNED TO FIELD. FOUND CRA CK IN RIGHT NOSE LANDING GEAR DOOR HINGE SUPPORT FITTING. RELEASED FOR SERVICE PER EA 32998. INSPECTED GLIDESLOPE ANTE NNA, NO FAULTS FOUND. (M) 2 L 7 2 4F A6WE 1996071000667 19960710 00667 EU 1996 7 10 USAAF96058 1 19960612 A 3230 200498005 DOWNLOCK ACT FOKKER F28 F28MK4000 4990810 EU RT MLG FAILED A USAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 19 481US 10572 993 11230 CLT - FLT 1147 - AFTER LANDING GEAR EXTENSION, CREW HAD ONE RED LIGHT AND NO GREEN LIGHT ON THE RIGHT MAIN LANDING GEAR. CREW RECYCLED THE GEAR AND NOTED SAME INDICATIONS. TOWER FLYBY WAS CONDUCTED. GEAR WAS MANUALLY EXTENDED. FLIGHT LA NDED WITH NO FURTHER INCIDENT. MX REPLACED THE RIGHT GEAR DOWNLOCK ACTUATOR DUE TO INCOMPLETE EXTENSION. (M) 2 L 7 2 4F RT A20EU 1996071000668 19960710 00668 EU 1996 7 10 USAAF96059 1 19960612 A 3230 SEQ VALVE FOKKER F28 F28MK4000 4990810 EU LANDING GEAR MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 EA 19 480AU 11229 CLT - FLT 799 - ON GEAR EXTENSION, CREW RECEIVED RED GEAR DOOR LIGHT. CREW RECYCLED THE GEAR TWICE WITH SAME INDICATION . GEAR WAS MANUALLY EXTENDED AND TOWER FLYBY CONDUCTED. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE DOOR UP STOP LOOSE AND ADJUSTED IT. THE GEAR DOWN SEQUENCE VALVE WAS REPLACED AS A PRECAUTION. (M) 2 L 7 2 4F RT A20EU 1996071000669 19960710 00669 EU 1996 7 10 USAAF96060 1 19960619 A 3260 SK3852 GEAR INDICATOR FOKKER F28 F28MK0100 4990807 EU COCKPIT FAILED A USAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 EA 19 896US 11391 MCI - FLT 1193 - UPON GEAR EXTENSION, CREW RECEIVED NOSE GEAR GREEN LIGHT AND THEN THE LIGHT EXTINGUISHED. ALL OTHER GE AR INDICATION WERE EXTINGUISHED. CREW PERFORMED ALTERNATE GEAR EXTENSION PROCEDURE AND TWO TOWER FLY BYS. FLIGHT LANDE D WITH NO FURTHER INCIDENT. MX REPLACED THE LANDING GEAR INDICATOR. (M) 2 L 7 2 4F RT 1996071000670 19960710 00670 NM 1996 7 10 USAASB96103 1 19960610 A 2840 20150129Y SENSOR TUBE BOEING 737 7374B7 1384702 NM AUX FUEL TANK FAILED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 438US 24560 LAS - FL 9 - AFT AUXILLIARY TANK FUEL INDICATION WAS ERRACTIC FROM 0 TO 3,300 POUNDS DURING FLIGHT. CREW WAS UNALE TO T RANSFER FUEL DURING FLIGHT. FLIGHT DIVERTED TO LAS AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED LENGTH OF COAX AND SENSOR TUBE. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996071000671 19960710 00671 NM 1996 7 10 USAASB96108 1 19960615 A 2425 BACC45FN2255S7 CONNECTOR BOEING 737 7374B7 1384702 NM COCKPIT SHORTED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 775AU 24933 BWI - FLT 1969 - CREW REPORTED, THAT AFTER STOWING AN OXYGEN MASK, A FOUL ODOR WAS DETECTED IN THE CABIN AND COCKPIT. A DECISION WAS MADE TO RETURN TO FIELD AT BWI. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED CONNECTOR D4074J WHERE TWO PINS WERE FOUND SHORTED. (M) 2 L 7 2 4F RT A16WE 1996071000672 19960710 00672 NM 1996 7 10 USAASB96111 1 19960616 A 5210 SEAL BOEING 737 7374B7 1384702 NM PAX DOOR NOT SEALED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 448US 24892 TPA - FLT 984 - AFTER TAKEOFF, CAPTAIN WAS UNABLE TO PRESSURIZE AIRCRAFT. FORWARD ENTRY DOOR WAS NOT SEALING PROPERLY I N CLOSED POSITION. FLIGHT RETURNED TO FIELD AT TPA. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITH NO FURTHER IN CIDENT. MAINTENANCE CHECKED AND OPERATED FORWARD ENTRY DOOR SEVERAL TIMES. OPS CHECK NORMAL. LUBED DOOR SEAL AS PRECA UTION. CHECKED PROXIMITY SWITCH. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 1996071000673 19960710 00673 NM 1996 7 10 USAASB96113 1 19960618 A 3213 65475317 WIRE HARNESS BOEING 737 7374B7 1384702 NM RT MLG STRUT FAILED A USAA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 EA 19 446US 24873 BWI - FLT 1257 - ON APPROACH TO DCA, ANTI-SKID INOP LIGHT CAME ON. FLIGHT DIVERTED TO BWI AND LANDED WITH NO FURTHER IN CIDENT. MAINTENANCE REPLACED THE RIGHT MLG STRUT HARNESS AND THE LEFT INBOARD ANTI-SKID TRANSDUCER. OPS CHECK GOOD. ( M) 2 L 7 2 4F RT A16WE 1996071000674 19960710 00674 1996 7 10 VTZA96222 4 19960619 A 3442 CONNECTOR BAG JETSTM JETSTM3101 1500215 EU RADAR SCREEN LOOSE A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 473UE 828 FLT NR 6586 - IAD-ISP - DURING CRUISE, RETURNED TO IAD DUE TO THE WEATHER RADAR FAILING IN FLIGHT. AIRCRAFT LANDED AT I AD WITH NO FURTHER INCIDENTS. MX RESECURED THE CONNECTOR ON THE RADAR SCREEN (P/N 6225941001). AIRCRAFT WAS RELEASED A ND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996071000675 19960710 00675 EU 1996 7 10 VTZA96223 1 19960619 A 7712 897457 TTL VALVE BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A VTZA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 27 493UE 805 FLT NR 6376 - CRW-IAD - ABORTED TAKEOFF DUE TO THE RIGHT ENGINE TORQUE ROLLING BACK TO 78 PERCENT ON THE TAKEOFF ROLL. A IRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MX REPLACED THE RIGHT ENGINE TTL VALVE. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996071000676 19960710 00676 EU 1996 7 10 VTZA96225 1 19960619 A 2770 91SE16 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU GUSTLOCK OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 307UE 41021 FLT 6202 - MHT-IAD - ABORTED THE TAKEOFF DUE TO THE TAKEOFF CONFIGURATION WARNING SYSTEM ACTIVATING WITH THE SPOILER CAP TION LIGHT ILLUMINATING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE INSPECTED SPOILER SYSTEM BUT COULD NOT FIND ANY DEFECTS. FOR THE TAKEOFF CONFIGURATION WARNING SYSTEM DISCREPANCY MX ADJUSTED THE GUSTLOCK MICROSWI TCHES AND THE FLAP POSITION TRANSDUCERS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996071000677 19960710 00677 EU 1996 7 10 VTZA96227 1 19960620 A 5400 14171176416 FILLET JETAIR JETSTM JETSTM4101 1500501 EU RT NACELLE DAMAGED A VTZA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 27 301UE 41012 FLT NR 6193 - IAD-JFK - DURING CLIMB-OUT, RETURNED TO IAD DUE TO AN AIRFRAME/ENGINE VIBRATION FOR THE RIGHT SIDE OF THE AIRCRAFT. AIRCRAFT DECLARED AN EMERGENCY AND LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE PERFORMED AN INSPECT ION AND FOUND THE RIGHT OUTBOARD NACELLE TO WING FILLET PANEL DAMAGED. MX REPAIRED DAMAGED PANEL ON 6-20-96. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996071000678 19960710 00678 1996 7 10 WRLA96026 4 19960614 A 3460 4059001905 FCC DOUG MD11 MD11 3023602 NM NR 1 SPURIOUS SIGNAL A WRLA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 273WA 48519 DURING TAXI, FLIGHT CREW NOTED, RT OUTBOARD FLAP DISAGREE INDICATION ON EAD. FLIGHT CREW ELECTED TO RETURN TO GATE FOR CORRECTIVE ACTION. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL PULLED AND RESET CIRCUIT BREAKERS FOR NR 1 FLIGHT CONTROL COMPUTER FAULT CORRECTED. FAULT IS CONSIDERED A 'NUISANCE SPURIOUS' DIGITAL FAULT. NO FURTHER ACTION REQUIRED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A22WE 1996071000679 19960710 00679 SO 1996 7 10 WTAA960127 1 19960611 A 3260 6839 BULBS EMB 120 EMB120RT SO RT MLG FAILED A WTAA O OTHER N FALSE WARNING AP APPROACH 1 WP 17 250YV 120250 PSP - RIGHT MAIN LANDING GEAR INDICATOR 'A' AND 'B' SYSTEM FAILED DURING APPROACH. CREW DECLARED EMERGENCY, LANDED WITH OUT INCIDENT. MAINTENANCE REPLACED 4 BULBS IN RIGHT MAIN LANDING GEAR INDICATOR. BOTH 'A' AND 'B' SYSTEM INDICATION NO RMAL DURING GROUND CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996071000680 19960710 00680 SO 1996 7 10 WTAA960129 1 19960614 A 5610 WINDSHIELD EMB 120 EMB120RT SO LT COCKPIT BIRDSTRIKE A WTAA O OTHER C F.O.D. LD LANDING 1 WP 17 216YV 120216 SBA - CREW REPORTED, BIRD STRIKE ON CAPTAINS WINDSHIELD LOWER CENTER. MX ACCOMPLISHED BIRD STRIKE INSPECTION. NO DAMAG E NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996071000681 19960710 00681 SO 1996 7 10 WTAA960131 1 19960618 A 5330 SKIN EMB 120 EMB120RT SO LT FUSELAGE BIRD STRIKE A WTAA O OTHER C F.O.D. NR NOT REPORTED 1 WP 17 120AM 120012 FAT - CREW REPORTED, BIRD STRIKE BELOW CAPTAINS WINDOW. MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECTION. NO DAMAGE NOT ED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996071100001 19960711 00001 NM 1996 7 11 CALA9600843 1 19960618 A 4970 3804286 OIL PRESS IND BOEING 737 7373T0 1384582 NM APU OUT OF ADJUST A CALA O OTHER N FALSE WARNING DE DESCENT 1 SW 09 12319 23370 THE APU LOW OIL PRESSURE LIGHT NEVER WENT OUT WHEN APU GEN OFF BUS LIGHT WAS ON DURING APU START ON DESCENT INTO EWR. T HE APU THEN AUTO SHUTDOWN. THE AIRCRAFT LANDED WITHOUT INCIDENT. ONE QUART OF OIL WAS ADDED TO THE APU. THE APU START ED NORMALLY ON THE SECOND ATTEMPT, BUT THE APU WOULD NOT COME ON LINE. THE APU OIL PRESSURE WAS FOUND AT 110 PSI DURING TROUBLESHOOTING USING THE APU TEST BOX. THE OIL PRESSURE WAS ADJUSTED TO 100 PSI. NO EXTERNAL LEAKS WERE NOTED, ALL P ARAMETERS WERE WITHIN LIMITS. 2 L 7 2 4F RT A16WE 1996071100004 19960711 00004 NM 1996 7 11 TWRA9629 1 19960515 A 2520 60B4005212 SEAT ELEC CABLE BOEING 747 747212B 1384886 NM SEAT 3B CHAFED A TWRA K NONE B F SMOKE/FUMES/ODORS/SPARKS FLT CONT AFFECTED CR CRUISE 1 EA 15 619FF 21316 UPON DESCENT, FLIGHT ATTENDANT NOTICED A SPARK UNDER SEAT 3B. FLIGHT ATTENDANT NOTIFIED THE FLIGHT ENGINEER AND TECHNIC AL REP, ONE FIRE BOTTLE WAS USED TO EXTINGUISH THE SPARK. CANNON PLUG WAS DISCONNECTED TO SEAT ELECTRONICS BOX. REPAIR TO WIRE ACCOMPLISHED. NO FURTHER PROBLEMS FOR REMAINDER OF FLIGHT. UPON LANDING, SEAT ELECTRONICS BOX CABLE WAS REPAI RED. OPS CHECK OK. MM 23-32-00. (X) 2 L 7 4 4F A20WE 1996071700001 19960717 00001 NM 1996 7 17 DL73S961415 1 19960514 A 5315 FLOOR BEAM 6545410224 BOEING 737 737232 1384475 NM BS 662 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 315DL 23087 THE BL ZERO FLOOR BEAM OF THE WING CENTER SECTION IS CRACKED AT STA 662. NO CRACKS WERE FOUND IN THE WEB. THE CRACK IS TYPICAL PER BACO S/B 737-57-1210. THIS ERA WILL INSTALL THE S/B REPAIR FOR THIS CONDITION. 2 L 7 2 4F RT A16WE 1996071700002 19960717 00002 WP 1996 7 17 ABXA9600569 1 19960612 A 5753 995760015 FITTING DOUG DC9 DC931 3022065 WP LT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK INSPECTION, FOUND ATTACH FITTINGS INSIDE THE LEFT FLAP CRACKED. REPLACED IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 1996071700003 19960717 00003 WP 1996 7 17 96FDEA01207 1 19960708 A 5400 COWL STIFFENER DOUG DC10 DC1010CF 3023502 WP NR 2 ENGINE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 SNRM NR 4225, NR 2 ENGINE NOSE COWL BLKHD STIFFENER ON DUCT WEB CRACKED 10 O'CLOCK POS AS SEEN THROUGH PANEL 361 KL. 2 L 7 3 4F RT A22WE 1996071700004 19960717 00004 WP 1996 7 17 Y2PA96038 1 19960603 A 5280 H146 HINGE DOUG DC9 DC915F 3022037 WP LT MLG DOOR OUT OF POSITION A Y2PA O OTHER J WARNING INDICATION LD LANDING 1 GL 23 195US 47017 YIP - GEAR DOOR LIGHT ON WITH GEAR DOWN INDICATION. FOUND RIGHT HAND HINGE PIN PROTRUDING OUT OF HINGE. REINSTALLED HI NGE PIN. DOOR SYSTEM OPS CHECK IAW MM 32-32-0. (M) 2 L 7 2 4F A6WE 1996071700005 19960717 00005 NM 1996 7 17 EISA96090 1 19960510 A 5532 TRAILING EDGE BOEING 727 727223 1384074 NM VERT STAB SEPARATION A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 VERTICAL STABILIZER TRAILING EDGE, JUST ABOVE RUDDER TAB, AREA STARTING TO SEPARATE. CUT OUT DAMAGE AND ACCOMPLISHED FI BERGLASS REPAIR PER SRM 51-40-06. (M) 2 L 7 3 4F A3WE 1996071700006 19960717 00006 WP 1996 7 17 RRXA96035 1 19960412 A 5311 2751960 FRAME DOUG DC8 DC863F 302198F WP BS 940 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 959R 46143 KMCN - DURING C-CHECK, FOUND HOLES DRILLED IN MAIN FRAME AT Y=940 ABOVE LONGERON 21 LEFT SIDE. FABRICATED, INSTALLED RE PAIR IAW APPROVED COTNEY ENGINEERING SKETCH A46-R06 AND IAW DC8 SRM 51-1-20D. (M) 2 L 7 4 4F 4A25 1996071700007 19960717 00007 WP 1996 7 17 RRXA96036 1 19960412 A 5311 2750825 FRAME DOUG DC8 DC863F 302198F WP BS 1040 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 959R 46143 KMCN - DURING C-CHECK, FOUND HOLE DRILLED THROUGH FRAME AT Y=1040 ABOVE LONGERON 21 LEFT. FABRICATED INSTALLED REPAIR I AW DER APPROVED COTNEY ENGINEERING SKETCH A46-R-5 AND IAW DC-8 SRM 51-1-20D. (M) 2 L 7 4 4F 4A25 1996071700008 19960717 00008 WP 1996 7 17 RRXA96037 1 19960412 A 5311 2750825 FRAME DOUG DC8 DC863F 302198F WP BS 660 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 959R 46143 KMCN - DURING C-CHECK, FOUND HOLE DRILLED THROUGH FRAME AT Y=660 ABOVE LONGERON 21 LEFT. FABRICATED AND INSTALLED REPAI R IAW DER APPROVED COTNEY ENGINEERING SKETCH A46-R05 AND IAW DC-8 SRM 53-2-0. (M) 2 L 7 4 4F 4A25 1996071700009 19960717 00009 WP 1996 7 17 RRXA96038 1 19960412 A 5311 2750825 FRAME DOUG DC8 DC863F 302198F WP BS 300 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 959R 46143 KMCN - DURING C-CHECK, FOUND HOLE DRILLED THROUGH FRAME AT Y=300 ABOVE LONGERON 21 LEFT. FABRICATED AND INSTALLED REPAI R IAW DER APPROVED COTNEY ENGINEERING SKETCH A46-R05 AND IAW DC-8 SRM 51-1-20D. (M) 2 L 7 4 4F 4A25 1996071700010 19960717 00010 WP 1996 7 17 DLL14961490 1 19960619 A 7603 TELEFLEX CABLE LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB211524B4 54555 NE NR 3 ENGINE BROKEN A DALA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 27 1739D 193C1237 NR 3 ENG WOULD NOT REACH T/O EPR. THROTTLE BINDIND AT MAX T/O PWR. ABORTED T/O AT 80 KTS. TELEFLEX CABLE BROKEN. REP LACED CABLE, RAN ENG TO PWR PER PFHB. 2 L 7 3 4F 4 F A23WE E12EU 1996071700011 19960717 00011 WP 1996 7 17 9614089153 1 19960626 A 3350 BATTERY PACK DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8912E 45829 DURING LINE CHECK, FOUND RIGHT ENGINE NACELLE EMERGENCY ILLUMINATION LIGHT INOPERATIVE. REPLACED RIGHT NACELLE LIGHT BA TTERY PACK, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996071800001 19960718 00001 WP 1996 7 18 IXXA96114 1 19960514 A 2611 SMOKE DETECTOR DOUG DC8 DC862 3021970 WP NR 4 CARGO COMPT MALFUNCTIONED A L IXXA A UNSCHED LANDING J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 11 51CX 46027 EN ROUTE BETWEEN ELP AND TOL IN CRUISE FLT AT FL 37, THE MAIN CARGO SMOKE DETECTOR LIGHT ILLUMINATED, FOLLOWED BY AN ACR ID SMELL. THE FE DONNED A PBE AND ENTERED THE MAIN CARGO COMPARTMENT, BUT SAW NO VISIBLE SMOKE. THE A/C DIVERTED TO OK C, DETAILED INSPECTIONS ACCOMPLISHED. THE SMOKE DETECTOR SYSTEM WAS SMOKE TESTED AND FOUND OPERATIONAL. NO ACRID SMELL COULD BE DETECTED. DURING CARGO OFF LOAD, IT WAS NOTED THAT A RESIDUAL ACRID SMELL WAS PRESENT IN THE NR 4 BELLY CARGO COMPARTMENT. WHEN THAT CARGO WAS TRANSFERRED TO A CONTAINER, THE RESIDUAL ACRID SMELL FOLLOWED. AN INSPECTION OF THAT CARGO REVEALED NO VISIBLE SIGN OF COMBUSTION. REFERENCE IXXA9682. (M) 2 L 7 4 4F 4A25 1996071800003 19960718 00003 NM 1996 7 18 TWRA9636 1 19960617 A 3350 PLUG BOEING 747 747212B 1384886 NM CABIN LOOSE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 619FF 21316 DURING WALK THROUGH OF CABIN, INSPECTION FOUND 5R MED EMERGENCY LIGHT INOPERATIVE. MX FOUND PLUG LOOSE AND SECURED PLUG . OPS CHECK OK. (M) 2 L 7 4 4F A20WE 1996071800004 19960718 00004 NM 1996 7 18 TWRA9637 1 19960617 A 3350 S1356B37 LIGHT BOEING 747 747212B 1384886 NM CABIN MISSING A TWRA K NONE O OTHER IN INSP/MAINT 1 EA 15 619FF 21316 DURING WALK THROUGH OF MAIN CABIN OF AIRCRAFT PRIOR TO MILITARY DEPARTURE, INSPECTION FOUND EMERGENCY LIGHT ASSEMBLY NOT INSTALLED AT SEAT 24H AND 31C. INSTALLED EMERGENCY LIGHT ASSEMBLY. OPS CHECK OK. (M) 2 L 7 4 4F A20WE 1996071800005 19960718 00005 NM 1996 7 18 TWRA9638 1 19960617 A 3397 WIRE BOEING 747 747212B 1384886 NM CABIN CHAFED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 619FF 21316 DURING WALK THROUGH OF CABIN PRIOR TO MILITARY DEPARTURE, INSPECTION FOUND 2R MED EMERGENCY LIGHT INOPERATIVE. DURING T ROUBLESHOOTING, MAINTENANCE FOUND SHORTED WIRE. REPLACED SECTION OF WIRE. OPS CHECK OK. ALSO, REPLACED BUSTLE LIGHT A SSEMBLY. (M) 2 L 7 4 4F A20WE 1996071800006 19960718 00006 NM 1996 7 18 TWRA9639 1 19960617 A 3350 900835A BATTERY PACK BOEING 747 747212B 1384886 NM CABIN DISCHARGED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 619FF 21316 DURING WALK THROUGH OF AIRCRAFT PRIOR TO MILITARY DEPARTURE, THE CREW SERVICE DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPER ATIVE. MAINTENANCE FOUND NO VOLTAGE AT EXIT SIGN. REPLACED BATTERY PACK AND 'E' LIGHT ASSEMBLY AT CREW DOOR, OPS CHECK OK, PER MM 35-51-00. (M) 2 L 7 4 4F A20WE 1996071800011 19960718 00011 SO 1996 7 18 96ZZZX3423 1 19960628 A 2436 B002861 REGULATOR LAMAR PIPER PA31 PA31350 7103110 SO DC SYSTEM OVERVOLTAGE A DQFA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 NM 07 27354 66099 317752180 REGULATOR OVERVOLTAGED. BOTH ALTERNATORS DROPPED OFF-LINE. PILOT FAILED TO RESET, CONSEQUENTLY, THE BATTERY DISCHARGED AND A TOTAL ELECTRICAL SHUT DOWN OCCURRED. THE AIRCRAFT LANDED WITHOUT INCIDENT. 1 L 7 2 3O A20SO 1996071800046 19960718 00046 SO 1996 7 18 BTHA96001 1 19960626 A 5412 6821202 FIREWALL PIPER PA32 PA32300 7103212 SO ENG MT ATTACH CRACKED A S BTHA K NONE O OTHER IN INSP/MAINT 1 AL 01 4811T 7020 327240086 DURING INSPECTION FIREWALL WAS FOUND CRACKED BETWEEN LOWER RIGHT ENGINE MOUNT ATTACH POINT AND COWLING FLANGE. CRACK WA S 2.50 INCHES LONG AND RAN HORIZONTALLY. SUBMITTER SPECULATES CAUSE WAS AGE OF PART. RECOMMEND CLOSE AND DETAILED INSP ECTION OF THIS AREA OF THE FIREWALL ON REGULAR BASIS. (X) 1 L 7 1 3O A3SO 1996071800047 19960718 00047 NE 1996 7 18 96ZZZX3458 1 19960426 A 2910 7665009801104 MODULE SKRSKY S76 S76A 8143006 NE HYDRAULIC BYPASS TRIPPED A A ALGA O OTHER J WARNING INDICATION CR CRUISE 1 SW 03 709AL 5470 408 0615B 760278 DURING LEVEL FLIGHT, NR 2 HYDRAULIC PRESSURE GAUGE DROPPED TO ZERO, NO NOISE WAS HEARD, AIRSPEED WAS REDUCED TO 80 KNOTS . LANDING GEAR HANDLE WAS MOVED TO THE EXTEND POSITION. GEAR DID NOT EXTEND. EMERGENCY CHECK LIST WAS UTILIZED TO EXT END GEAR. LANDING GEAR EXTENDED AND LANDED WITHOUT FURTHER INCIDENT. INSPECTED AIRCRAFT, FOUND NR 2 FILTER BYPASS BUTT ON POPPED ON HYDRAULIC MODULE. FLUID LEVEL INDICATED FULL. REMOVED NR 2 HYDRAULIC PUMP, FOUND SHAFT SHEARED, REPLACED PUMP. REMOVED AND REPLACED NR 2 HYDRAULIC MODULE. SERVICED SYSTEM AND PURGED AIR FROM SYSTEM. GROUND RUN, LEAK CHECK, PINNED LANDING GEAR. 1 G 7 2 3U H1NE 1996071800048 19960718 00048 NE 1996 7 18 96ZZZX3459 1 19960426 A 2913 7668009808101 PUMP SKRSKY S76 S76A 8143006 NE HYDRAULIC SHAFT SHEARED A A ALGA O OTHER J WARNING INDICATION CR CRUISE 1 SW 03 709AL 5470 408 0190356 760278 DURING LEVEL FLIGHT, NR 2 HYDRAULIC PRESSURE GAUGE DROPPED TO ZERO, NO NOISE WAS HEARD, AIRSPEED WAS REDUCED TO 80 KNOTS . LANDING GEAR HANDLE WAS MOVED TO THE EXTEND POSITION. GEAR DID NOT EXTEND. EMERGENCY CHECK LIST WAS UTILIZED TO EXT END GEAR. LANDING GEAR EXTENDED AND LANDED WITHOUT FURTHER INCIDENT. INSPECTED AIRCRAFT, FOUND NR 2 FILTER BYPASS BUTT ON POPPED ON HYDRAULIC MODULE. FLUID LEVEL INDICATED FULL. REMOVED NR 2 HYDRAULIC PUMP, FOUND SHAFT SHEARED, REPLACED PUMP. REMOVED AND REPLACED NR 2 HYDRAULIC MODULE. SERVICED SYSTEM AND PURGED AIR FROM SYSTEM. GROUND RUN, LEAK CHECK, PINNED LANDING GEAR. 1 G 7 2 3U H1NE 1996071800053 19960718 00053 EU 1996 7 18 AALA960740 1 19960508 A 5730 SKIN AIRBUS 300 A300B4605R 3930308 EU WS 539 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80058 466 TUL - CORROSION ON LEFT WING SKIN PANEL NR 2 AT AN AREA OUTBOARD AND ADJACENT TO THE AFT PYLON FAIRING ATTACH ANGLE. RE PAIRED PER ESO 3595 DATED 5-3-96. TST: 21,695.01 HOURS. CYCLES, 8,681. (X) 2 L 7 2 4F RT A35EU 1996071800054 19960718 00054 EU 1996 7 18 AALA960755 1 19960507 A 5210 A5211134600000 CONNECT LINK AIRBUS 300 A300B4605R 3930308 EU R1 DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80058 466 TUL - LOWER CONNECTION LINK ON R1 DOOR HAS EXFOLIATION IN CENTER OF LINK. INSTALLED NEW PART PER SRM 51-71-10-0. TST: 21,695.01 HOURS. CYCLES, 8,681. (X) 2 L 7 2 4F RT A35EU 1996071800055 19960718 00055 EU 1996 7 18 AALA960768 1 19960513 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU CARGO COMPT CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80058 466 TUL - CORROSION ON STR 52L, STR 54L, AND STR 55L, AFT CARGO COMPARTMENT. FABRICATED NEW STRINGER SECTIONS AND INSTALLED PER SRM 53-10-14. TST: 21,695.01 HOURS. CYCLES, 8,681. (X) 2 L 7 2 4F RT A35EU 1996071800056 19960718 00056 EU 1996 7 18 AALA960769 1 19960513 A 5330 SKIN AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80058 466 TUL - CORROSION ON FUSELAGE SKIN UNDER FRAME 59, STR 55L. REMOVED CORROSION, INSTALLED DOUBLER PER SRM 53-10-12. TST: 21,695.01 HOURS. CYCLES, 8,681. (X) 2 L 7 2 4F RT A35EU 1996071800057 19960718 00057 EU 1996 7 18 AALA960831 1 19960523 A 5400 195461119050002 ANGLE AIRBUS 300 A300B4605R 3930308 EU NR 2 PYLON CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - CORRODED AT CENTER OF ANGLE 2 INCHES OF A 20 INCH PIECE. REMOVED AND REPLACED WTIH NEW ANGLE PER AARD 51-01-00-05 , PAGE 1, PARAGRAPH 2. TST: 20,962 HOURS. CYCLES 8,396. (X) 2 L 7 2 4F RT A35EU 1996071800058 19960718 00058 EU 1996 7 18 AALA960844 1 19960529 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU BS 4650 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - CENTER FLOORBOARD SUPPORT CORRODED IN SEVERAL AREAS BETWEEN FRAME 71 AND FRAME 78. REMOVED AND REPLACED CENTER FL OORBOARD SUPPORT BETWEEN FRAMES 71 AND 78 PER MM 51-12-10-0. TST: 20,962.17 HOURS. CYCLES 8,396. (X) 2 L 7 2 4F RT A35EU 1996071800059 19960718 00059 EU 1996 7 18 AALA960845 1 19960529 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU BS 2029 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 41063 506 TWO AREAS OF CORROSION ON SEAT TRACK UPPER FLANGE AT NUT CLIP AREA FOR FLOORBOARDS. REMOVED SECTION OF SEAT TRACK AND I NSTALLED A NEW SECTION OF SEAT TRACK PER SRM 51-72-10, P. 1. TST: 20,963.17 HOURS. CYCLES 8,396. (X) 2 L 7 2 4F RT A35EU 1996071800060 19960718 00060 EU 1996 7 18 AALA960860 1 19960531 A 5311 FRAME AIRBUS 300 A300B4605R 3930308 EU BS 2390 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - FRAME 46 CRACKED RIGHT AND LEFT SIDES JUST BELOW CENTER WING BOX. REPAIRED PER ESO 30595. TST: 20,962.17 HOURS. CYCLES 8,396. (X) 2 L 7 2 4F RT A35EU 1996071800061 19960718 00061 EU 1996 7 18 AALA960861 1 19960529 A 5230 SEAL RETAINER AIRBUS 300 A300B4605R 3930308 EU CARGO DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - CORROSION ON SEAL RETAINERS, FORWARD AND AFT LOWER RADII OF FORWARD CARGO DOOR. REPLACED FORWARD AND AFT LOWER DO OR INTERNAL SUPPORT AND FORWARD LOWER DOOR CORNER CAP PER SRM 51-72-10. TST: 20,962.17 HOURS. CYCLES 8,396. (X) 2 L 7 2 4F RT A35EU 1996071800062 19960718 00062 EU 1996 7 18 AALA960882 1 19960607 A 5230 SKIN AIRBUS 300 A300B4605R 3930308 EU CARGO DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - INSIDE FORWARD CARGO 3 INCHES UP FROM BOTTOM INNER SKIN HAS CORROSION ABOVE SEAL RETAINER BETWEEN FRAME 24 AND FRA ME 25. REPAIRED PER ESO 30595. REMOVED CORROSION, PROTECT AREA PER A300 SRM. APPLY CORROSION INHIBITOR. TST: 20,962 HOURS. CYCLES, 8,346. (X) 2 L 7 2 4F RT A35EU 1996071800063 19960718 00063 EU 1996 7 18 AALA960895 1 19960611 A 3230 A252801B SEQUENCE VALVE MESSIER AIRBUS 300 A300B4605R 3930308 EU RT MLG DEFECTIVE A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 07 59081 639 SJU - FLT 0602 - DURING APPROACH SJU WHEN LANDING GEAR EXTENDED, RT MLG DID NOT EXTEND USING SYSTEMS 1 OR 2. RECYCLED L DNG GEAR WITH SAME RESULTS. INDUCED GEAR EXT USING G-LOADING AND ACFT LANDED WITHOUT INCIDENT. LUBRICATED AND FREED OP ER OF RT MLG UPLOCK ROLLER. LUBRICATED RT MLG. PINNED LDNG GEARS AND GND GEAR RETRACT CHK WITH DOORS OPER NORMAL. ACF T MAINT FERRY SJU/JFK AND PROBLEM REPEATED DURING APPR JFK. INDUCED RT GEAR EXT USING G-LOADING AND ACFT LANDED JFK WIT HOUT INCIDENT. REPLACED RT MLG UPLOCK, ROLLER AND PIN, AND PROBLEM PERSISTED. REPLACED RT MLG SEQ VALVE. ACCOMPLISHED LNDG GEAR RETRACT CHK WITH NO DEFECTS FND. SYS GND CHKD, NORMAL OPER. FUNCTION CHK FLT AND SYS OPER CHKD NORMAL. (X) 2 L 7 2 4F RT A35EU 1996071800064 19960718 00064 EU 1996 7 18 AALA960911 1 19960614 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU CARGO COMPT CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - FLOORBOARD SUPPORT CORRODED BETWEEN TRAYS 4 AND 5. INSTALLED NEW SECTION PER SRM 53-10-15. TST: 20,904 HOURS. C YCLES, 8,714. (X) 2 L 7 2 4F RT A35EU 1996071800065 19960718 00065 EU 1996 7 18 AALA960913 1 19960617 A 5320 TMS6018793 ANGLE AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - CORROSION ON TOP OF FLOOR SUPPORT, CENTER FLOOR SUPPORT BETWEEN FRAME 72 AND FRAME 73. REMOVED AND REPLACED CENTE R FLOOR SUPPORT PER SRM 51-72-10-0. TST: 20,904.02 HOURS. CYCLES, 8,714. (X) 2 L 7 2 4F RT A35EU 1996071800066 19960718 00066 EU 1996 7 18 AALA960915 1 19960617 A 5320 TMS6018793 ANGLE AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - THREE AREAS OF CORROSION ON TOP OF LAVATORY SUPPORT ANGLE BETWEEN CENTER AND FIRST FLOOR SUPPORT TO THE RIGHT BETW EEN FRAME 71 AND FRAME 72. REMOVED AND REPLACED LAVATORY SUPPORT ANGLE PER SRM 51-70-00-3. TST: 20,904.02 HOURS. C YCLES, 8,714. (X) 2 L 7 2 4F RT A35EU 1996071800067 19960718 00067 EU 1996 7 18 AALA960917 1 19960617 A 5320 TMS6018793 ANGLE AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - CORROSION ON TOP OF FLOOR SUPPORT ON CENTER TEE ANGLE BETWEEN FRAME 73 AND FRAME 74. REMOVED AND REPLACED CENTER FLOOR SUPPORT PER SRM 51-21-10-0. TST: 20,904.02 HOURS. CYCLES, 8,714. (X) 2 L 7 2 4F RT A35EU 1996071800068 19960718 00068 EU 1996 7 18 AALA960921 1 19960616 A 2612 900045 CONTROL UNIT SYSTRONDONNR FOKKER F28 F28MK0100 4990807 EU APU DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1431B 11416 RDU - FLT 1826 - DURING APPROACH TO RDU, APU FIRE INDICATION ILLUMINATED FOR APPROXIMATELY 2 SECONDS AND THEN EXTINGUISH ED. SIMULTANEOUSLY, APU AUTO-SHUTDOWN. APU FIRE BOTTLE DISCHARGED AND AIRCRAFT LANDED RDU WITHOUT INCIDENT. REPLACED APU FIRE BOTTLE AND PLACARDED APU INOPERATIVE. SUBSEQUENTLY, REPLACED APU FIRE DETECTION CONTROL UNIT AT ORD/17. SYSTE M GROUND CHECKED NORMAL OPERATION. APU OPERATION WITH AIR AND ELECTRIC CHECKED NORMAL. (X) 2 L 7 2 4F RT 1996071800069 19960718 00069 EU 1996 7 18 AALA960922 1 19960619 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - SEAT TRACK NR 9 HAS CORROSION IN CHANNEL. REPLACED SEAT TRACK PER AARD 51-10-00-3 AND INSTALLED PER SRM 51-72-10- 0. TST: 21,904 HOURS. CYCLES, 8,714. (X) 2 L 7 2 4F RT A35EU 1996071800070 19960718 00070 EU 1996 7 18 AALA960923 1 19960619 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU NR 8 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - SEAT TRACK NR 8 HAS CORROSION ON INBOARD FLANGE. REPLACED SEAT TRACK PER AARD 51-10-00-3, AND NSTALLED PER SRM 51 -72-10-0. TST: 21,904 HOURS. CYCLES, 8,714. (X) 2 L 7 2 4F RT A35EU 1996071800071 19960718 00071 EU 1996 7 18 AALA960924 1 19960619 A 5330 SKIN AIRBUS 300 A300B4605R 3930308 EU BS 995 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - DENT AT STA 995, FRAME 10A, RIGHT SIDE OF FUSELAGE. INSTALLED DOUBLER PER SRM 53-10-12. TST: 21,904 HOURS. C YCLES, 8,714. (X) 2 L 7 2 4F RT A35EU 1996071800072 19960718 00072 EU 1996 7 18 AALA960925 1 19960619 A 5330 SKIN AIRBUS 300 A300B4605R 3930308 EU FUSELAGE GOUGES A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - TWO DENTS WITH GOUGES FORWARD OF FRAME 78, 3 INCHES AFT OF LEFT REAR PASSENGER DOOR. CUT OUT DAMAGE AND REPAIRED PER SRM 53-10-12-02. TST: 21,904 HOURS. CYCLES, 8,714. (X) 2 L 7 2 4F RT A35EU 1996071800073 19960718 00073 EU 1996 7 18 AALA960926 1 19960619 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - CORROSION ON TOP OF FLOOR SUPPORT, THE FIRST SUPPORT LEFT OF CENTER, AROUND FASTENER HOLE. REMOVED CORROSION PER SRM 51-74-10-2. TREATED AND PRIMED, WORKED AREA AND INSTALLED DOUBLER PER SRM 53-20-00-2. TST: 21,904.02 HOURS. CY CLES, 8,714. (X) 2 L 7 2 4F RT A35EU 1996071800074 19960718 00074 EU 1996 7 18 AALA960928 1 19960619 A 5320 A53980195200 SEAL RETAINER AIRBUS 300 A300B4605R 3930308 EU R4 DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - CORROSION ON R4 DOOR JAMB SEAL LANDING AT CLIP NUT HOLES. INSTALLED NEW SEAL LANDING PER SRM 51-72-10-0. TST: 2 1,904.02. CYCLES, 8,714. (X) 2 L 7 2 4F RT A35EU 1996071800075 19960718 00075 EU 1996 7 18 AALA960930 1 19960619 A 5320 606377 ANGLE AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - CORROSION ON TOP LEG OF ANGLE INBOARD OF R4 DOOR AT FRAME 75. REPLACED ANGLE PER SRM 51-72-10-0. TST: 21,904.02 . CYCLES, 8,714. (X) 2 L 7 2 4F RT A35EU 1996071800076 19960718 00076 EU 1996 7 18 AALA960931 1 19960619 A 5320 606377 ANGLE AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - CORROSION ON TOP OF FLOORBOARD SUPPORT INBOARD AND AFT OF R4 DOOR THRESHOLD AT FRAME 75A. INSTALLED NEW ANGLE PER SRM 51-72-10-0. TST: 21,904.02. CYCLES, 8,714. (X) 2 L 7 2 4F RT A35EU 1996071800077 19960718 00077 EU 1996 7 18 AALA960932 1 19960619 A 5320 6022457 ANGLE AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - CORROSION ON TOP OF FLOOR SUPPORT, CENTER SUPPORT AT FRAME 77. INSTALLED NEW TEE ANGLE PER SRM 51-72-10-0. TST: 21,904.02. CYCLES, 8,714. (X) 2 L 7 2 4F RT A35EU 1996071800078 19960718 00078 NM 1996 7 18 AALA960934 1 19960617 A 3350 S1196 SWITCH DOUG MD11 MD11 3023602 NM L1 DOOR DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1759 48481 JFK - DURING OVERNIGHT CHECK, CABIN EMERGENCY LIGHTS DO NOT ILLUMINATE WHEN SWITCH AT LEFT FORWARD F/A (L1) POSITION IS TURNED ON. REPLACED EMERGENCY LIGHT SWITCH S1-196 AT L1 DOOR F/A POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION. (X ) 2 L 7 3 4F RT A22WE 1996071800079 19960718 00079 NM 1996 7 18 AALA960935 1 19960618 A 3350 A3060698101 CONNECTOR BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 878AA 21390 ATL - DURING OVERNIGHT CHECK, FOUND EMERGENCY FLOOR LIGHTS IN AFT SECTION OF MAIN CABIN INOPERATIVE. REPLACED BROKEN EM ERGENCY FLOOR LIGHT STRIP CONNECTOR AT AFT SECTION OF MAIN CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1996071800080 19960718 00080 EU 1996 7 18 AALA960939 1 19960618 A 3230 7310SE010500 RESTRICTOR LUCAS AIRBUS 300 A300B4605R 3930308 EU LT MLG DEFECTIVE A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 07 7082A 643 BOS - FLT 1292 - DURING APPROACH TO BOS WHEN LANDING GEAR EXTENDED, LT MLG WOULD NOT EXTEND AND GEAR DOOR AMBER AND GEAR RED LIGHT WERE ILLUMINATED. CONDITION CONTINUED FOR APPROXIMATELY 3 MINUTES AFTER WHICH LT MLG EXTENDED WITH NORMAL GE AR LOCK INDICATIONS. AIRCRAFT LANDED BOS WITHOUT INCIDENT. AIRCRAFT GEAR DOWN MAINTENANCE FERRY BOS/JFK. REPLACED LT MLG HIGH PRESSURE RESTRICTOR. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A35EU 1996071800081 19960718 00081 SO 1996 7 18 GLBA96091 1 19960509 A 2750 FAULT INDICATION EMB 120 EMB120RT SO TE FLAPS ACTIVATED A GLBA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 01 128AM 120109 RDU - ON MAY 9 AND MAY 12, CREW REPORTED A FLAP ASYMMETRY FAULT FOLLOWING TAKEOFF. THEY MADE AIR TURNBACKS AND UNEVENTF UL LANDINGS ON BOTH DATES. MAINTENANCE CLEANED FLAP TRACKS AND PERFORMED BIT TESTS, BUT COULD NOT DUPLICATE DISCREPANCY . (X) 2 L 7 2 4T RT A31SO 1996071800082 19960718 00082 CE 1996 7 18 S2YA960005 1 19960513 A 3610 1013810159 INSTR AIR VALVE BEECH 1900 1900D 1154162 CE RIGHT INOPERATIVE A S2YA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 13 891SK 5080 1454 UE89 MKE - FLT 1906 - AFTER FLIGHT CREW DEPARTED, THEY NOTICED THE LEFT BLEED AIR FAIL ANNUNCIATOR ILLUMINATED AND STAYED ON. THE RIGHT BLEED AIR FAIL ANNUNCIATOR WAS ALREADY DEFERRED SO THEY TURNED BACK TO MKE. MAINTENANCE COULD NOT DUPLICATE THE LEFT BLEED FAIL, BUT THEY CLEARED THE RIGHT BLEED FAIL MEL BY REPLACING THE RIGHT INSTRUMENT AIR VALVE. (X) 2 L 7 2 4T RT A24CE 1996071800083 19960718 00083 1996 7 18 S2YA960006 4 19960513 A 6122 3039550 PROP GOVERNOR BEECH 1900 1900D 1154162 CE RT ENGINE FAILED A A S2YA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 13 831SK 5373 2491488 UE83 GRR - FLT 1123 - THE FLIGHT CREW EXPERIENCED TORQUE FLUCTATIONS OF THE RIGHT ENGINE IN-FLIGHT, TURNED BACK TO GRR. THRO UGH TROUBLESHOOTING, MAINTENANCE FOUND THE PRIMARY GOVERNOR FAILED AND REPLACED IT. DURING A RUN-UP CHECK, THE RIGHT AU TOFEATHER WAS TESTED ON THE GROUND AND THE RIGHT PROPELLER STAYED IN FEATHER. MAINTENANCE CHANGED THE OVERSPEED GOVERNO R CLEARING THAT PROBLEM. PN, 122-389037-3, SN 2699964A, TSN: 5,372.6 HOURS. (X) 2 L 7 2 4T RT A24CE 1996071800084 19960718 00084 NE 1996 7 18 SIMA961412 2 19960520 A 7320 5034T91P06 HMU SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE NR 1 ENGINE FAILED A A SIMA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 SW 21 388AE WA27841 340B388 GEE785240 IAH - FLT 3671 - DURING DESCENT FROM 12,000 FEET, A LOUD POP WAS HEARD FROM NR 1 ENGINE FOLLOWED BY A DECREASE IN TEMPER ATURE, TORQUE, AND ENGINE SPEED. IGNITION LIGHT CAME ON BUT ENGINE DID NOT RE-LIGHT. THE CREW FOLLOWED THE ENGINE FAIL URE CHECK LIST AND LANDED WITH NR 1 ENGINE SHUT DOWN WITHOUT ANY FURTHER INCIDENT. EXTENSIVE TROUBLESHOOTING BY MAINTEN ANCE SHOWED FUEL MANAGEMENT PROBLEMS. THE HMU WAS REPLACED AND A COMPLETE CONTROL RIGGING AND ADJUSTMENT WAS ACCOMPLISH ED. OPS CHECK AND LEAK CHECK WERE GOOD. THE AIRCRAFT PERFORMED A FUNCTIONAL CHECK FLIGHT WITH SATISFACTORY RESULTS. ( X) 2 L 7 2 4T 4 T RT A52EU E8NE 1996071800085 19960718 00085 EU 1996 7 18 SIMA961641 1 19960612 A 3350 330151 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 375AE 1098 340B375 DFW - FLT 3576 - FORWARD EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. OPS CHECK GOOD. AIRCRAFT WAS RETURNED T O SERVICE. (X) 2 L 7 2 4T RT A52EU 1996071800086 19960718 00086 EU 1996 7 18 96ZZZX3464 1 19960125 A 6410 134617P BUSHING BOLKMS 105 BO105S 5626006 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 722MB 751 S754 TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U H3EU 1996071800087 19960718 00087 EU 1996 7 18 96ZZZX3465 1 19960210 A 6210 11715856 BUSHING BOLKMS 117 BK117A3 5626015 EU M/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 117NY 330 7110 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 8 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996071800090 19960718 00090 EU 1996 7 18 96ZZZX3468 1 19960122 A 6420 1053170023 BEARING BOLKMS 117 BK117B1 5626012 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 5194C 7169 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW 2 EACH UNITS, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996071800091 19960718 00091 EU 1996 7 18 96ZZZX3469 1 19960329 A 6420 1053170023 BEARING BOLKMS 117 BK117A4 5626017 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 586BH 375 7129 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996071800092 19960718 00092 EU 1996 7 18 96ZZZX3470 1 19960208 A 6420 1053170023 BEARING BOLKMS 117 BK117A4 5626017 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911BY 7127 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996071800093 19960718 00093 EU 1996 7 18 96ZZZX3471 1 19960418 A 6420 1053170023 BEARING BOLKMS 117 BK117A3 5626015 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 527SF 412 7111 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996071800098 19960718 00098 EU 1996 7 18 96ZZZX3476 1 19960125 A 6420 ABWT82008 BEARING BOLKMS 105 BO105CBS 5626008 EU T/R HEAD WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911BH 685 WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U NC H3EU 1996071800099 19960718 00099 EU 1996 7 18 96ZZZX3477 1 19960207 A 6500 551253 BEARING BOLKMS 105 BO105LSA3 5626020 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 203LF 228 2015 BEARING WORN BEYOND SERVICEABLE LIMITS. MAKES LOUD CLICKING SOUND ONCE EVERY REVOLUTION. REPLACED WITH NEW UNIT, CORRE CTED PROBLEM. 1 G 7 2 3U H3AU 1996071800100 19960718 00100 EU 1996 7 18 96ZZZX3478 1 19960423 A 6420 1053170023 BEARING BOLKMS 117 BK117B1 5626012 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 17SJ 420 7230 WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996071800101 19960718 00101 EU 1996 7 18 96ZZZX3479 1 19960108 A 7930 DK040 TRANSMITTER BOLKMS 105 BO105S 5626006 EU ENGINE DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 722MB 331 7412 S754 TRANSMITTER LOW PRESSURE READING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H3EU 1996071800102 19960718 00102 EU 1996 7 18 96ZZZX3480 1 19960419 A 2840 DK042 TRANSMITTER BOLKMS 105 BO105S 5626006 EU FUEL SYSTEM DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 722MB 441 11625 S754 UNIT CAUSES PRESSURE GAUGE TO FLUCTUATE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H3EU 1996071800103 19960718 00103 EU 1996 7 18 96ZZZX3481 1 19960417 A 6340 IPT20RT1100080G TRANSMITTER BOLKMS 117 BK117A3 5626015 EU M/R GRBOX FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 117MA 92 51612B31 7107 UNIT STAYED AT FULL SCALE ON RUN-UP. RMH PERFORMED NO OFF-WING TESTING OF UNIT. REPLACED WITH NEW UNIT, CORRECTED PROB LEM. 1 G 7 2 3U H13EU 1996071800104 19960718 00104 EU 1996 7 18 96ZZZX3482 1 19960410 A 6340 IPT20RT1100080G TRANSMITTER BOLKMS 117 BK117B1 5626012 EU M/R GEARBOX ERRATIC A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 7060G 722 50372126 7173 ERRATIC SIGNALS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996071800105 19960718 00105 EU 1996 7 18 96ZZZX3483 1 19960110 A 6210 1051585403 BUSHING BOLKMS 117 BK117A4 5626017 EU M/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 586BH 47 7129 BUSHING TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNITS 2 EACH, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996071800110 19960718 00110 NM 1996 7 18 96ZZZX3488 1 19960414 A 5320 SHEAR TIE BOEING 727 727232 1384082 NM BS 720 CORROSION B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 17789 20643 LEVEL 2 CORROSION ON SHEAR TIE AT STA 720C BETWEEN STR 27 AND STR 28R. REMOVED AND REPLACED SHEAR TIE ANGLE PER SRM 53- 10-4 AND SRM 51-10-2. FABRICATED SHEAR TIE PER SRM 53-10-4, TREATED PER SRM 50-10-2. (X) 2 L 7 3 4F A3WE 1996071800111 19960718 00111 NM 1996 7 18 96ZZZX3489 1 19960413 A 5230 T-ANGLE BOEING 727 727232 1384082 NM CARGO DOOR CRACKED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 17789 20643 T-ANGLE, 5TH RIB, FORWARD CARGO DOOR IS CORRODED AND CRACKED. FABRICATED REPAIR ANGLE AND INSTALLED PER SRM 53-30-1 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996071800112 19960718 00112 NM 1996 7 18 96ZZZX3490 1 19960424 A 5320 ANTENNA PLATE BOEING 727 727232 1384082 NM BS 720-740 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 17789 20643 LEFT A/C BAY, LEFT ACCESS BAY DOOR NR 3340L HAS LEVEL 2 CORROSION ON INBOARD SIDE OF STRUCTURE LBL=12 INCHES, STA 720E T O STA 740. REMOVED CORROSION PER SRM 51-10-2. ALODINES ANTENNA PLATE PER SRM 51-10-2. PRIMED PER SRM 51-10-6. FABRIC ATED NEW ANTENNA BASE PLATE PER SRM 51-10-1. CORROSION REMOVED, MATERIAL LOSS WITHIN LIMITS PER SRM 53-10-1, FIGURE 1. ALL PANELS CLOSED COMPLETE. 2 L 7 3 4F A3WE 1996071800113 19960718 00113 NM 1996 7 18 96ZZZX3491 1 19960410 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 720-740 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 17789 20643 SUPPORT AT STA 720E TO STA 740 RBL 6 HAS LEVEL 2 CORROSION. FABRICATED SUPPORT PER OLD PER PART PER SRM 51-20-2. INSTA LLED SUPPORT PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996071800114 19960718 00114 NM 1996 7 18 96ZZZX3492 1 19960410 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 720-740 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 17789 20643 SUPPORT AT STA 720E TO 740 LBL 6 HAS LEVEL 2 CORROSION. FABRICATED SUPPORT ANGLE PER SRM 51-10-2 AND SRM 51-20-2. INST ALLED SUPPORT ANGLE PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996071800115 19960718 00115 NM 1996 7 18 96ZZZX3493 1 19960410 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 700-720 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 17789 20643 SUPPORT AT STA 700 TO STA 720 RBL HAS LEVEL 2 CORROSION. FABRICATED SUPPORT PER OLD PART PER SRM 51-10-2. INSTALLED SU PPORT PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996071800116 19960718 00116 NM 1996 7 18 96ZZZX3494 1 19960408 A 5320 U-CHANNEL BOEING 727 727232 1384082 NM BS 720 CRACKED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 17789 20643 STA 720F UPPER CHORD OF INTERCOSTAL, STRAP CRACKED WITH LEVEL 2 CORROSION. ALSO, 2 EACH, U-CHANNELS CRACKED LBL 12 AND RBL 12 AND 1 EACH L-ANGLE. FABRICATED AND INSTALLED 1 EACH L-ANGLE AND 2 EACH CHANNELS PER SRM 51-30-2 AND SRM 51-20-2. 2 L 7 3 4F A3WE 1996071800117 19960718 00117 NM 1996 7 18 96ZZZX3495 1 19960410 A 5320 WEB BOEING 727 727232 1384082 NM BS 720 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 17789 20643 WEB AT STA 720F IS CORRODED BEYOND LIMITS - KEEL BEAM CBL. REMOVED WEB, FABRICATED AND INSTALLED NEW WEB PER SRM 51-20- 2. CUT WEB, FABRICATED WEB DOUBLER, AND INSTALLED PER SRM 51-40-2. 2 L 7 3 4F A3WE 1996071800118 19960718 00118 NM 1996 7 18 96ZZZX3496 1 19960408 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 344-440 CORROSION B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 17789 20643 LEVEL 2 SURFACE CORROSION THROUGHOUT SEAT TRACK AT STA 344 TO STA 440 RBL 45.5. REMOVED DAMAGED SEAT TRACK, FABRICATED NEW SEAT TRACK PER SRM 53-10-5, FIGURE 1. TREATED AND PRIMED SEAT TRACK PER SRM 51-10-2. REPAIR SEAT TRACK INSTALLED S TA 380 TO STA 440. SEAT TRACK REPLACED STA 344 TO STA 380 PER DRAWING AE 5134. 2 L 7 3 4F A3WE 1996071800119 19960718 00119 NM 1996 7 18 96ZZZX3497 1 19960408 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 344 CORROSION B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 17789 20643 EXFOLIATING CORROSION ON SEAT TRACK AT STA 344 LBL 45. REMOVED DAMAGED SEAT TRACK, FABRICATED NEW SEAT TRACK PER SRM 53 -10-5, FIGURE 1. TREATED AND PRIMED PER SRM 51-10-2. REPAIRED SEAT TRACK STA 380 TO STA 480, REPLACED SEAT TRACK STA 3 44 TO STA 380 PER DRAWING AE 5134. 2 L 7 3 4F A3WE 1996071800120 19960718 00120 NM 1996 7 18 96ZZZX3498 1 19960413 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 675 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 17789 20643 LEVEL 2 CORROSION ON STRINGER SPLICE AT STA 675, STR 27R. REMOVED CORRODED STRINGER AND INSTALLED STRINGER SPLICE PER S RM 53-10-1 AND SRM 53-10-3. 2 L 7 3 4F A3WE 1996071800121 19960718 00121 NM 1996 7 18 96ZZZX3499 1 19960412 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 720-740 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 17789 20643 STRINGER 28R FROM STA 720F TO STA 740 HAS LEVEL 2 CORROSION ON INSIDE. REMOVED AND REPLACED CORRODED STRINGER SECTION A ND REPAIRED PER SRM 53-10-3. 2 L 7 3 4F A3WE 1996071800122 19960718 00122 NM 1996 7 18 96ZZZX3500 1 19960404 A 5320 SHEAR TIE BOEING 727 727232 1384082 NM BS 720 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 17789 20643 PREVIOUS SHEAR TIE REPAIR ON STATION FRAME AT STA 720F HAS LEVEL 2 CORROSION BETWEEN STR 29R AND STR 28R. REMOVED AND R EPLACED SHEAR TIE PER SRM 53-10-3. 2 L 7 3 4F A3WE 1996071800123 19960718 00123 NM 1996 7 18 96ZZZX3501 1 19960414 A 5320 SHEAR TIE BOEING 727 727232 1384082 NM BS 720 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 17789 20643 FORWARD CARGO, STA 720F, STATION FRAME BETWEEN 28L-27L HAS LEVEL 2 CORROSION ON FORWARD SIDE. REMOVED CORRODED SHEAR TI E, FABRICATED AND INSTALLED REPLACEMENT PER SRM 53-10-4. 2 L 7 3 4F A3WE 1996071800124 19960718 00124 NM 1996 7 18 96ZZZX3502 1 19960421 A 5320 CHORD BOEING 727 727232 1384082 NM BS 740 CORROSION B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 17789 20643 FORWARD CARGO, LEVEL 2 CORROSION ON LOWER CHORD OF STA 740 BULKHEAD FROM STR 27L - STR 27R (FORWARD SIDE OF BULKHEAD). R EMOVED CORROSION AND TREATED AT STR 27R - STR 27L (RC2186) STA 740 PER SRM 51-10-6, SRM 51-10-2. REMOVED AND REPLACED S KIN SUPPORT ANGLE PER BOEING M727-96-1774, STR 27L - STR 28L. 2 L 7 3 4F A3WE 1996071800125 19960718 00125 NM 1996 7 18 96ZZZX3503 1 19960422 A 5320 SPLICE BOEING 727 727232 1384082 NM BS 740 CORROSION B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 17789 20643 FORWARD CARGO, STR 28L AT STA 740 BULKHEAD HAS LEVEL 2 CORROSION. FABRICATED STRINGER, SPLICES, AND END CLIPS PER SRM 5 3-10-3. TREATED AND PRIMED PER SRM 51-10-2. INSTALLED STRINGER, SPLICE, AND END CLIPS PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996071800126 19960718 00126 NM 1996 7 18 96ZZZX3504 1 19960411 A 5330 SKIN BOEING 727 727232 1384082 NM BS 720 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 17789 20643 LEVEL 2 CORROSION ON SKIN DOUBLER AND RAM AIR DOOR ACTUATOR CABLE ASSEMBLY AT STA 720B TO STA 720C LBL 4 - RBL 4. CUT O UT DAMAGED SKIN, FABRICATED DOUBLER AND FILLERS, AND INSTALLED PER SRM 53-30-3, FIGURE 1, SRM 51-30-2, SRM 51-10-2. 2 L 7 3 4F A3WE 1996071800127 19960718 00127 NM 1996 7 18 96ZZZX3505 1 19960413 A 5230 CHANNEL BOEING 727 727232 1384082 NM FWD CARGO DOOR GOUGED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 17789 20643 LOWER EDGE OF FORWARD CARGO DOOR HAS 4 EACH HEAVY GOUGES (BEYOND LIMITS). FABRICATED REPAIR CHANNEL PER SRM 51-20-2 AND INSTALLED LOWER BEAM CHANNEL PER SRM 52-30-1 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996071800128 19960718 00128 NM 1996 7 18 96ZZZX3506 1 19960418 A 5315 BAC1518338 FLOOR BEAM BOEING 727 727232 1384082 NM BS 1164 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 17789 20643 AFT LEFT LAVATORY HAS LEVEL 2 CORROSION AROUND PUMBING FITTINGS ON FLOOR. REMOVED DAMAGED AREA OF FLOOR, FABRICATED AND INSTALLED FLOOR BEAM REPAIR PER ENGR SKETCH M000118N00156. 2 L 7 3 4F A3WE 1996071800129 19960718 00129 NM 1996 7 18 96ZZZX3507 1 19960408 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 340-460 CORROSION B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 17789 20643 SEAT TRACK STA 340 TO STA 460 RBL 24 HAS LEVEL 2 CORROSION ON FLANGES AT NUMEROUS LOCATIONS. REMOVED DAMAGED SEAT TRACK , FABRICATED NEW SEAT TRACK PER SRM 53-10-5, FIGURE 1. TREATED AND PRIMED PER SRM 51-10-2. REPAIRED SEAT TRACK STA 380 TO STA 460, REPLACED SEAT TRACK STA 344 TO STA 380 PER DRAWING AE 5134. 2 L 7 3 4F A3WE 1996071800130 19960718 00130 NM 1996 7 18 96ZZZX3508 1 19960410 A 5540 651684512 WEB BOEING 727 727232 1384082 NM RUDDER TORN B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 17789 20643 BOTTOM FACE OF LOWER RUDDER, SKIN TORN AWAY AT LEFT SIDE. REMOVED SKIN PANEL, ORDERED AND INSTALLED NEW SKIN PER SRM'S 51-10-1, 51-10-2, 51-30-2. INSTALLED RUDDER PER MM 27-20-1, AND TESTED RUDDER PER MM 27-20-1. 2 L 7 3 4F A3WE 1996071800132 19960718 00132 NM 1996 7 18 96ZZZX3510 1 19960419 A 7110 NOSE COWL BOEING 727 727232 1384082 NM NR 1 ENGINE CRACKED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 17789 20643 NR 1 ENGINE NOSE COWL, 5 O'CLOCK POSITION SKIN IS PULLED UP 0.10 INCH BY 3 INCHES LONG, 0.5 INCH FORWARD WITH A 0.15 INC H CRACK IN UPPER EDGE. STOP DRILLED CRACK PER SRM 51-10-6. INSTALLED DOUBLER PER SRM 54-30-3 AND SRM 51-10-2. 2 L 7 3 4F A3WE 1996071800133 19960718 00133 NM 1996 7 18 96ZZZX3511 1 19960422 A 5320 SHEAR TIE BOEING 727 727232 1384082 NM BS 680 CRACKED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 17789 20643 FUSELAGE STATION 680 BETWEEN RIGHT STR 15 AND STR 16, THERE IS A 5 INCH CRACK IN THE FRAME SHEAR TIE THROUGH ATTACH FAST ENER. FABRICATED AND INSTALLED REPAIR SHEAR TIE PER SRM 53-10-4 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996071800134 19960718 00134 EU 1996 7 18 AALA960941 1 19960620 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - SEAT TRACK 3 HAS CORROSION ON INBOARD FLANGE. REMOVED AND REPLACED SEAT TRACK PER SRM 51-72-10-0. TST: 21,904 H OURS. CYCLES: 8,714. (X) 2 L 7 2 4F RT A35EU 1996071800135 19960718 00135 EU 1996 7 18 AALA960943 1 19960620 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - THREE AREAS OF CORROSION ON SEAT TRACK A ON TOP FLANGE. REMOVED AND REPLACED SEAT TRACK PER SRM 51-72-10-0. TST: 21,904 HOURS. CYCLES, 8,714. (X) 2 L 7 2 4F RT A35EU 1996071800136 19960718 00136 EU 1996 7 18 AALA960944 1 19960620 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - CORROSION ON TOP OF FLOOR SUPPORT, FIRST FLOOR SUPPORT RIGHT OF CENTER BETWEEN FRAME 71 AND FRAME 72. TST: 21,90 4 HOURS. CYCLES, 8,714. (X) 2 L 7 2 4F RT A35EU 1996071800137 19960718 00137 EU 1996 7 18 AALA960945 1 19960620 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - CORROSION ON TOP OF FLOOR SUPPORT, FIRST FLOOR SUPPORT LEFT OF CENTER BETWEEN FRAME 72 AND FRAME 73. INSTALLED S TRAP REPAIR PER AARD 53-20-00-2. TST: 21,904.02 HOURS. CYCLES, 8,714. (X) 2 L 7 2 4F RT A35EU 1996071800138 19960718 00138 EU 1996 7 18 AALA960946 1 19960620 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - CORROSION TOP OF FLOOR SUPPORT, FOURTH FLOOR SUPPORT LEFT OF CENTER. INSTALLED STRAP REPAIR PER AARD 53-20-00-2. TST: 21,904.02 HOURS. CYCLES, 8,714. (X) 2 L 7 2 4F RT A35EU 1996071800139 19960718 00139 EU 1996 7 18 AALA960947 1 19960620 A 5320 6022457 SUPPORT AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - CORROSION ON TOP OF FLOOR SUPPORT, FIRST FLOOR SUPPORT RIGHT OF CENTER AT FRAME 77. INSTALLED NEW FLOOR SUPPORT P ER SRM 51-72-10-0. TST: 21,904.02 HOURS. CYCLES, 8,714. (X) 2 L 7 2 4F RT A35EU 1996071800140 19960718 00140 EU 1996 7 18 AALA960948 1 19960620 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - CORROSION ON TOP OF FLOOR SUPPORT, FIRST SUPPORT RIGHT OF CENTER AT FRAME 73. INSTALLED STRAP PER AARD 53-20-00-2 . TST: 21,904.02 HOURS. CYCLES, 8,714. (X) 2 L 7 2 4F RT A35EU 1996071800141 19960718 00141 EU 1996 7 18 AALA960949 1 19960620 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - CORROSION ON TOP OF SUPPORT, SECOND SUPPORT RIGHT OF CENTER 6 INCHES AFT OF FRAME 73. REPLACED FLOOR SUPPORT PER SRM 51-22-10-0. TST: 21,904.02 HOURS. CYCLES, 8,714. (X) 2 L 7 2 4F RT A35EU 1996071800142 19960718 00142 EU 1996 7 18 AALA960950 1 19960621 A 5320 A53274618202 SUPPORT AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - CORROSION ON TOP OF FLOOR SUPPORT, THIRD SUPPORT LEFT OF CENTER BETWEEN FRAME 71, 6 INCHES AFT. INSTALLED NEW SEC TION OF FLOOR SUPPORT PER SRM 51-72-10-0. TST: 21,904.02 HOURS. CYCLES, 8,714. (X) 2 L 7 2 4F RT A35EU 1996071800143 19960718 00143 EU 1996 7 18 AALA960951 1 19960621 A 5320 A53279208200 SUPPORT AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - CORROSION ON TOP OF FLOOR SUPPORT, THIRD FLOOR BEAM LEFT OF CENTER BETWEEN FRAME 71 AND FRAME 72. INSTALLED NEW S ECTION OF FLOOR SUPPORT PER SRM 51-72-10-0. TST: 21,904.02 HOURS. CYCLES, 8,714. (X) 2 L 7 2 4F RT A35EU 1996071800144 19960718 00144 NM 1996 7 18 9614765513 1 19960621 A 5315 FLOOR BEAM BOEING 757 757251 1384970 NM FS 1661 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 513US 23201 DURING P-CHECK, FOUND CORROSION ON THE BS 1661 FLOOR BEAM UPPER CHORD AT LBL 16 AND RBL 32. REPAIRED BEAM (P/N 146N5090 ) PER EA 55-106106. 2 L 7 2 4F RT A2NM 1996071800145 19960718 00145 NM 1996 7 18 9614776612 1 19960624 A 5313 LONGERON BOEING 747 747251B 1384892 NM FS 2163 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING P-CHECK, FOUND CORROSION ON STR 51R AT BS 2163. REPAIRED STRINGER (P/N 65B04369-176) PER EA 66-101900. 2 L 7 4 4F A20WE 1996071800146 19960718 00146 WP 1996 7 18 9614781224 1 19960624 A 5330 SKIN DOUG DC10 DC1030 3023501 WP FS 1146 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 224NW 46581 DURING L-CHECK, FOUND CORROSION ON THE FUSELAGE SKIN DOUBLER AT FS 1146 BETWEEN LONGERONS 51L TO 52L. REPAIRED SKIN (P/ N AAA7058-1) PER EA 12-105442. 2 L 7 3 4F A22WE 1996071800147 19960718 00147 NM 1996 7 18 9614795513 1 19960625 A 5321 PLATE BOEING 757 757251 1384970 NM FS 1681 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 513US 23201 DURING P-CHECK, FOUND CORROSION ON THE AFT GALLEY DECK PLATE AT BS 1681 BETWEEN LBL 54 TO RBL 54. REPAIRED PLATE (P/N 1 46N5318-3) PER EA 55-106107. 2 L 7 2 4F RT A2NM 1996071800148 19960718 00148 NM 1996 7 18 9614802285 1 19960626 A 5315 FLOOR BEAM BOEING 727 727251 138408H NM FS 1130 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 285US 21324 DURING H-CHECK, FOUND CORROSION ON THE BS 1130 FLOOR BEAM BETWEEN RBL 3 TO RBL 31. REPAIRED BEAM (P/N 65-20838-16) PER EA 22-102133. 2 L 7 3 4F A3WE 1996071800149 19960718 00149 NM 1996 7 18 9614812285 1 19960627 A 5313 LONGERON BOEING 727 727251 138408H NM FS 970-990 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 285US 21324 DURING H-CHECK, FOUND CORROSION ON STR 29L BETWEEN BS 970 TO 990. REPAIRED STRINGER (P/N 65-56441) PER EA 22-102131. 2 L 7 3 4F A3WE 1996071800150 19960718 00150 WP 1996 7 18 9614829940 1 19960702 A 5720 FITTING DOUG DC9 DC932 3022066 WP WNG 69 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3322L 47031 DURING M-CHECK, FOUND CORROSION ON THE FITTING LOCATED AT WING STR 15 AND THE RIGHT WS 69 FRAME. REPLACED FITTING PER S RM 51-30-5. 2 L 7 2 4F A6WE 1996071800151 19960718 00151 WP 1996 7 18 9614839305 1 19960702 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FS 994 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 307RC 48086 DURING H-CHECK, FOUND A CRACK ON LONGERON 20L AT FS 994. REPAIRED LONGERON (P/N 5936034-501) PER EA 93-105330. 2 L 7 2 4F A6WE 1996071800152 19960718 00152 WP 1996 7 18 9614899925 1 19960702 A 7711 LG80A2 TRANSMITTER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9A 52048 NE NR 1 MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 925US 47794 1408 47425 666904 NR 1 EPR INDICATION FROZE AT 1.55 ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAIN TENANCE REPLACED THE EPR TRANSMITTER WITH A SERVICEABLE UNIT. 2 L 7 2 4F 4 F A6WE E2EA 1996071800153 19960718 00153 NM 1996 7 18 9614902703 1 19960709 A 3241 ANTI-SKID IND BOEING 727 727225 1384077 NM COCKPIT ILLUMINATED A NWAA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 GL 01 8878Z 21451 DURING APPROACH, ANTI-SKID INDICATION ILLUMINATED. AIRCRAFT DIVERTED TO LAN AND LANDED WITHOUT INCIDENT. ANTI-SKID SYS TEM WAS PLACED ON MEL NR 459969 PER MAINTENANCE CONTROL. 2 L 7 3 4F A3WE 1996071800154 19960718 00154 WP 1996 7 18 9614919609 1 19960704 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 609NW 47234 DURING LINE CHECK, FOUND RIGHT HAND OVERWING NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CH ECK OK. 2 L 7 2 4F A6WE 1996071800155 19960718 00155 WP 1996 7 18 9614929609 1 19960704 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 609NW 47234 DURING LINE CHECK, FOUND LEFT HAND OVERWING NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHE CK OK. 2 L 7 2 4F A6WE 1996071800156 19960718 00156 WP 1996 7 18 9614939305 1 19960706 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN BROKEN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 307RC 48086 DURING LINE CHECK, FOUND AFT EMERGENCY LIGHT BROKEN. REPLACED LIGHT ASSEMBLY, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996071800157 19960718 00157 WP 1996 7 18 9614949103 1 19960708 A 3350 BATTERY PACK DOUG DC9 DC915 3022036 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 93S 47078 DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTS BACK TO ROW 2 AND FORWARD CABIN DOOR EXIT SIGNS INOPERATIVE. REPL ACED BATTERY PACK IN POWER SUPPLY B5-901, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996071800158 19960718 00158 WP 1996 7 18 9614959983 1 19960704 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 983US 47282 DURING LINE CHECK, FOUND NACELLE AND TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS, OPERATIONAL CHECK O K. 2 L 7 2 4F A6WE 1996071800159 19960718 00159 WP 1996 7 18 9614969979 1 19960703 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9343 47439 DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTS IN TAILCONE AREA INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996071800160 19960718 00160 WP 1996 7 18 9614979926 1 19960703 A 3350 CONNECTOR DOUG DC9 DC932 3022066 WP CABIN DISCONNECTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 926NW 47425 DURING LINE CHECK, FOUND EMERGENCY LIGHTS AT ROWS 8, 9 AND 10 INOPERATIVE. FOUND CONNECTOR BEHIND WALL PANEL AT 10R DIS CONNECTED. RECONNECTED, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996071800161 19960718 00161 NM 1996 7 18 96FDEA00868 1 19960430 A 5754 65162258 FLAP BOEING 727 72725 1384006 NM NR 4 LE FLAP CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 NR0150, 014, DUE TO NUMEROUS AREAS OF CORROSION NR 4 K-FLAP REQUIRES REPLACEMENT. *S/D* REMOVED AND REPLACED NR 4 K-FL AP IAW FED-EX MM 27-81-1, FUNCTIONAL TEST GOOD IAW MM 27-81-1. 2 L 7 3 4F A3WE 1996071800162 19960718 00162 NM 1996 7 18 96FDEA01210 1 19960708 A 5315 65208276 FLOOR BEAM BOEING 727 72722 1384002 NM BS 660 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 NR 0719, 010, CORROSION (C53-111-01) ON FLOOR BEAM STA 660 RBL 24 WL 198. *S/D* REPAIRED FLOOR BEAM PER SRM 53-10-8. 2 L 7 3 4F A3WE 1996071800163 19960718 00163 NM 1996 7 18 96FDEA01211 1 19960708 A 5311 65207231 FRAME BOEING 727 72722 1384002 NM BS 572 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 DISCREPANCY: NR 0255 (011) CORROSION (C53-111-01) ON WEB/FRAME, BS 572, RBL 24-26 WL 157 FORWARD BAY. CORRECTIVE ACTIO N: REPAIRED WEB/FRAME BS 572, RBL 24-26, WL 157 IAW FEDEX EA 7-5310-29271. 2 L 7 3 4F A3WE 1996071800164 19960718 00164 NM 1996 7 18 96FDEA01213 1 19960709 A 7930 1163P182 SWITCH BOEING 727 727233 138408A NM NR 2 ENGINE FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 223FE 20935 NR 2 OIL FILTER BYPASS LIGHT ON AFTER TAKEOFF. SHUT DOWN AND RETURNED OIL PRESSURE 45, TEMPERATURE 90, QUANTITY 3.8. A IRCRAFT RELEASED FOR SERVICE PER MINIMUM EQUIPMENT LIST 79-4 CATEGORY B EXPIRATION 12 JUL 96. REF NR 2 OIL FILTER BY PA SS INOPERATIVE, CHECKED WIRE INTEGRITY FOUND OK. CHECKED OIL FILTER BY PASS FOUND CLEAN DRAINED OIL TANK AND OIL PRESS SWITCH. REMOVED AND REPLACED SWITCH, RAN ENGINE TO TAKEOFF AND CHECKED NORMAL. 2 L 7 3 4F RT A3WE 1996071800165 19960718 00165 NM 1996 7 18 96FDEA01214 1 19960701 A 5320 5717752012 WEB BOEING 727 72722 1384002 NM BS 224-259 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 DISCREPANCY: NR 0574 (012) CORROSION (C53-221-01) ON UNDERSIDE OF HORIZONTAL WEB AND L-ANGLES BS 224-259, LBL 42-54, W L 224-236 CORRECTIVE ACTION: REPAIRED HORIZONTAL WEB BS 237 TO 259, LBL 42-54, WL 224-232, AND REPLACED L-ANGLES IAW SR M 51-40-2, DUE TO CORROSION BEING OUT OF LIMITS IAW SRM 53-10-1. 2 L 7 3 4F A3WE 1996071800166 19960718 00166 NM 1996 7 18 96FDEA01215 1 19960704 A 5313 65271326 STRINGER BOEING 727 72722 1384002 NM BS 530-550 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 DISCREPANCY: NR 00250 (013) CORROSION (C53-111-01) ON STR 27L CHANNEL STR 536-546 LT FORWARD BAY. CORRECTIVE ACTION: * *S/D** REMOVED CORRODED SECTION OF STR FROM BS 530-550 STR 27L. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-3, FIG 1. 2 L 7 3 4F A3WE 1996071800167 19960718 00167 NM 1996 7 18 96FDEA01216 1 19960708 A 5311 651630611 FRAME BOEING 727 72722 1384002 NM BS 227.8 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 DISCREPANCY: NR 0579 (014) CORROSION (C53-221-01) ON FRAME BS 227.8 WL 226 AND 233 RBL 41-43 5. CORRECTIVE ACTION: **S /D** REPAIRED FRAME BS 227.8 W/L 226 AND 283 RBL 41 - 43.5 PER SRM 51-40-2. 2 L 7 3 4F A3WE 1996071800168 19960718 00168 NM 1996 7 18 96FDEA01217 1 19960708 A 5754 65162261 BONDING JUMPER BOEING 727 72722 1384002 NM NR 2 LE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 DISCREPANCY: NR 0551 (015) CORROSION (C57-562-01) NR 2 K-FLAP TO BULLNOSE INBOARD BONDING JUMPER UPPER ATTACH POINT. C ORRECTIVE ACTION: CORRODED AREA FOUND TO BE OUT OF LIMITS PER FEDEX DWG R 27-57-010. REPAIRED NR 2 K-FLAP TO BULLNOSE INBOARD BONDING JUMPER ATTACH POINT PER FEDEX DWG 27-57-010 AND SRM 57-50-3. 2 L 7 3 4F A3WE 1996071800169 19960718 00169 NM 1996 7 18 96FDEA01218 1 19960702 A 5751 65217662 TE SKIN BOEING 727 72722 1384002 NM RT AILERON DISBONDED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 NR 0464, 016, RIGHT WING O/B AILERON IS DELAMINATED AT O/B TRAILING EDGE. *S/D* REPAIRED O/B AILERON AT O/B TRAILING E DGE IAW FEDEX SRM 51-40-06. 2 L 7 3 4F A3WE 1996071800170 19960718 00170 NM 1996 7 18 96FDEA01219 1 19960707 A 5754 65162262 BONDING JUMPER BOEING 727 72722 1384002 NM NR 5 LE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 NR 0547, 007, CORROSION (C57-562-01) AT BOTH ATTACH POINTS ON THE O/B BONDING JUMPER ON THE NR 5 K-FLAP BULLNOSE. *S/D* REPAIRED UPPER ATTACH POINT PER FEDEX SRM 57-50-3 FIG 3, LOWER ATTACH POINT WITHIN LIMITS AFTER CORROSION REMOVAL PER FEDEX DWG R 27-57-010. 2 L 7 3 4F A3WE 1996071800171 19960718 00171 NM 1996 7 18 96FDEA01220 1 19960705 A 5330 6518216 SKIN BOEING 727 7272D4 138407U NM BS 416 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 287FE 21849 NR 0104, 006, SKIN DENT BS 416 RBL 40 WL 168. *S/D* REPAIRED SKIN DENT AT BS 416, RBL 40, WL 168 FOUND TO BE OUT OF LI MITS PER SRM 53-10-01. REMOVED DAMAGE, FABRICATED FILLER AND DOUBLER AND INSTALLED IAW 53-30-01. 2 L 7 3 4F A3WE 1996071800172 19960718 00172 NM 1996 7 18 96FDEA01221 1 19960705 A 5330 6556115 SHEAR TIE BOEING 727 7272D4 138407U NM BS 720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 287FE 21849 NR 0149, 007, CORROSION (C53-113-01) IN THE FWD CARGO BAY ON FRAME SHEAR TIE BS 720D, LBL 16, WL 148. 2 L 7 3 4F A3WE 1996071800173 19960718 00173 NM 1996 7 18 96FDEA01222 1 19960702 A 5754 6516222717A SKIN BOEING 727 7272D4 138407U NM NR 1 LE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 287FE 21849 NR 0181, 008, NR 1 K-FLAP DATA PLATE AREA HAS CORROSION. *S/D* REMOVED CORROSION BY CUTTING OUT DAMAGED AREA AND INSTA LLING FILLER AND REPAIR PLATES IAW SRM 29-57-010 AND 51-10-06. 2 L 7 3 4F A3WE 1996071800174 19960718 00174 NM 1996 7 18 96FDEA01223 1 19960701 A 5320 65198616 CHORD BOEING 727 7272D4 138407U NM BS 322-336 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 287FE 21849 DISCREPANCY: NR 0189 (009) CORROSION (C53-100-01) ON UPPER SURFACE OF THE HORIZONTAL FLANGE OF RT LOWER NOSE CHORD BETW EEN BS 322 AND 336, RBL 16, WL 148. CORRECTIVE ACTION: REMOVED CORRODED RT LOWER NOSE CHORD AND INSTALLED NEW RT LOWER NOSE CHORD BS 282 - 360, RBL 16, WL 148. 2 L 7 3 4F A3WE 1996071800175 19960718 00175 NM 1996 7 18 96FDEA01225 1 19960710 A 3610 65208276 CLAMP BOEING 727 7272S2F 1384O81 NM NR 1 STRUT LOOSE A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 210FE 22932 ENGINE NR 1 STRUT OVERHEAT LIGHT ILLUMINATED IN FLIGHT DURING CLIMBOUT AT 15,000 MSL. FOLLOWED APPROPRIATE CHECK LIST A ND LIGHT WENT OUT CONTINUED TO GEG. TIGHTENED LEAKING CLAMPS BOTH SIDES OF MODULATING SHUTOFF VALVE IN NR 1 ENGINE STUB WING TO STOP LEAKS NEAR SENSING ELEMENT. 2 L 7 3 4F A3WE 1996071800176 19960718 00176 NM 1996 7 18 96FDEA01229 1 19960709 A 5311 651630919 FRAME BOEING 727 72722 1384002 NM BS 251.6, CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 DISCREPANCY: NR 0581(021) CORROSION (C53-221-01) ON FRAME BS 251.6, WL 223, LBL 48. CORRECTIVE ACTION *****S/D***** R EPAIRED FRAME STA 251.6, WL 223, LBL 48 IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1996071800177 19960718 00177 WP 1996 7 18 CALA9600987 1 19960709 A 3260 833703 DNLOCK SENSOR DOUG DC9 DC982 3022082 WP NLG INOPERATIVE A CALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 83870 48056 THE NOSE LANDING GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. CHECKLIST PROCEDURES WERE COMPLIED W ITH AND THE AIRCRAFT WAS RETURNED. MAINTENANCE FOUND THE NOSE GEAR DOWNLOCK SENSOR AT FAULT. THE DOWNLOCK SENSOR WAS R EMOVED AND REPLACED. THE NOSE GEAR WAS CYCLED SEVERAL TIMES WITH OPERATION AND INDICATIONS CHECKING GOOD PER MM 32-60-0 0. 2 L 7 2 4F A6WE 1996071800179 19960718 00179 NM 1996 7 18 CALA9600989 1 19960621 A 3350 38931002 BATTERY BOEING 727 727227 1384078 NM AFT ENTRY DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17773 21045 INSPECTION FOUND EMERGENCY LIGHT AT AFT ENTRY INOPERATIVE. THE BATTERY PACK WAS CHARGED AND REINSTALLED. 2 L 7 3 4F A3WE 1996071800180 19960718 00180 NM 1996 7 18 CALA9600990 1 19960621 A 5311 CIRCUMFERENTIAL BOEING 727 727227 1384078 NM BS 950 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17773 21045 INSPECTION FOUND CIRCUMFERENTIAL CORRODED IN AFT CARGO COMPARTMENT AT STA 950A, STRINGER 30R. THE CORRODED TEE WAS REMO VED, A NEW TEE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996071800181 19960718 00181 NM 1996 7 18 CALA9600991 1 19960621 A 5730 SKIN BOEING 727 727227 1384078 NM RT WING LE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17773 21045 INSPECTION FOUND A .5 INCH CRACK IN RT WING LEADING EDGE SKIN AT AFT END OF OUTBOARD HOOK CUTOUT FOR NR 6 SLAT. THE CRA CK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 57-30-4. 2 L 7 3 4F A3WE 1996071800182 19960718 00182 NM 1996 7 18 CALA9600992 1 19960622 A 5730 SKIN BOEING 727 727227 1384078 NM RT WING DEBONDED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17773 21045 INSPECTION FOUND UPPER AND LOWER SKIN OF RT WING LOWER FIXED PANEL DEBONDING FORWARD OF WHEEL WELL DOOR RELEASE HANDLE. THE PANEL WAS REMOVED, REPAIRED IAW SRM 51-40-05 AND REINSTALLED. 2 L 7 3 4F A3WE 1996071800183 19960718 00183 NM 1996 7 18 CALA9600993 1 19960622 A 5720 ANGLE BOEING 727 727227 1384078 NM NR 7 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17773 21045 INSPECTION FOUND A 1.5 INCH CRACK IN RADIUS OF ANGLE AT INBOARD UPSTOP BLOCK ON NR 7 LEADING EDGE SLAT. THE CRACKED ANG LE WAS REMOVED AND NEW PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-40-4 AND 51-30-2. 2 L 7 3 4F A3WE 1996071800184 19960718 00184 NM 1996 7 18 CALA9600994 1 19960622 A 5720 ANGLE BOEING 727 727227 1384078 NM NR 8 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17773 21045 INSPECTION FOUND A 1.5 INCH CRACK IN RADIUS OF ANGLE AT OUTBOARD UPSTOP BLOCK ON NR 8 LEADING EDGE SLAT. A 1.5 INCH CRA CK WAS ALSO FOUND IN RADIUS OF ANGLE AT INBOARD UPSTOP BLOCK ON NR 8 LEADING EDGE SLAT. THE CRACKED AREAS WERE CUT OUT, REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 51-10-4. 2 L 7 3 4F A3WE 1996071800185 19960718 00185 NM 1996 7 18 CALA9600995 1 19960622 A 5330 SKIN BOEING 727 727227 1384078 NM BS 350 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17773 21045 INSPECTION FOUND A DENT IN LT FUSELAGE SKIN JUST BELOW AND AFT OF FORWARD ENTRANCE DOOR AREA AT STA 350 BETWEEN STRINGER 17L AND 18L. THE DENTED AREA WAS CUT OUT, A FILLER AND DOUBLER WERE INSTALLED IAW SRM 53-30-3, FIGURE 1. 2 L 7 3 4F A3WE 1996071800186 19960718 00186 WP 1996 7 18 DHL96801010 1 19960706 A 7722 65003603 EGT IND DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C1 13802 NE NR 2 MALFUNCTIONED A T DHLA A J UNSCHED LANDING DUMP FUEL N FALSE WARNING CL CLIMB 1 SO 01 801DH 46033 692540 ENGINE NR 2 EGT 900 ON TAKEOFF. REMOVED AND REPLACED NR 2 EGT INDICATOR AND EGT THERMOCOUPLE AND HARNESS. ACCOMPLISHED HIGH EGT CHECK PER M/M 71-00, ALL WITHIN LIMITS. 2 L 7 4 4F 4 F RT 4A25 E2GL 1996071800187 19960718 00187 WP 1996 7 18 DHL9680109 1 19960706 A 7722 65003003 EGT IND DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C1 13802 NE NR 1 MALFUNCTIONED A T DHLA A J UNSCHED LANDING DUMP FUEL N FALSE WARNING CL CLIMB 1 SO 01 801DH 46033 692440 NR 1 ENGINE OVERTEMP ON TAKEOFF 905 PLUS 910 FOR 10 TO 15 SEC. REMOVED AND REPLACED NR 1 EGT IND, ACCOMPLISHED HIGH EGT CHECK PER MM 71-00, ALL WITHIN LIMITS. 2 L 7 4 4F 4 F RT 4A25 E2GL 1996071800188 19960718 00188 WP 1996 7 18 MWEA96257 1 19960708 A 3350 100865 POWER SUPPLY DOUG DC9 DC914 3022034 WP CABIN INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 800ME 45842 DURING INSPECTION, FOUND AFT TWO LIGHTS ON EMERGENCY FLOOR TRACK LIGHTING INOP. REPLACED BATTERY POWER SUPPLY, OPS CHEC K GOOD. 2 L 7 2 4F A6WE 1996071800189 19960718 00189 WP 1996 7 18 MWEA96258 1 19960703 A 2560 5917689103 SLIDE COVER DOUG DC9 DC932 3022066 WP GALLEY SERV DOOR FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 302ME 47102 CREW REPORTS, GALLEY SERVICE DOOR SLIDE COVER FELL OFF. REINSTALLED GALLEY DOOR SLIDE COVER. 2 L 7 2 4F A6WE 1996071800190 19960718 00190 WP 1996 7 18 MWEA96259 1 19960703 A 3350 100865 POWER SUPPLY DOUG DC9 DC932 3022066 WP AFT CABIN INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 206ME 47791 DURING INSPECTION, FOUND AFT SECTION OF EMERGENCY FLOOR TRACK LIGHTING INOP. REPLACED AFT BATTERY POWER SUPPLY, OPS CHE CK GOOD. 2 L 7 2 4F A6WE 1996071800191 19960718 00191 WP 1996 7 18 SCNA96186 1 19960701 A 2621 89524001 FIRE BOTTLE DOUG DC10 DC1010 3022110 WP NR 2 DISCHARGED A SCNA O OTHER J WARNING INDICATION IN INSP/MAINT 1 GL 15 572SC 46977 NUMBER 2 ENGINE AGENT LOW LIGHT WAS FOUND ON. REMOVED AND REPLACED FIRE EXTINGUISHER BOTTLE IAW MAINTENANCE MANUAL CHAP TER 26-20-02 AND 26-21-06, OPS CHECK NORMAL. 2 L 7 3 4F A22WE 1996071800192 19960718 00192 WP 1996 7 18 SCNA96187 1 19960705 A 2621 89524001 FIRE BOTTLE DOUG DC10 DC1010 3022110 WP NR 2 RT DISCHARGED A SCNA O OTHER J WARNING INDICATION IN INSP/MAINT 1 GL 15 572SC 46977 NUMBER 2 ENGINE AGENT LOW LIGHT WAS FOUND ON. REMOVED AND REPLACED FIRE EXTINGUISHING BOTTLE IAW MAINTENANCE MANUAL 26- 20-01, OPS AND LEAK CHECKED OK. 2 L 7 3 4F A22WE 1996071800193 19960718 00193 NM 1996 7 18 SWAA960636 1 19960708 A 3350 20121 BATTERY BOEING 737 7375H4 138449D NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 525SW 26567 DURING SCHEDULED A-CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996071800194 19960718 00194 NM 1996 7 18 SWAA960637 1 19960708 A 3397 WIRE BOEING 737 7375H4 138449D NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 511SW 24188 DURING WALK-AROUND, FOUND EMERGENCY EXIT LIGHTING WIRES BROKEN, 4 WHITE LIGHTS INOP AT ROW FWD OF OVERWING EXIT. REPAIR ED AND OP CHECKED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996071800195 19960718 00195 NM 1996 7 18 SWAA960638 1 19960708 A 3397 WIRE BOEING 737 7375H4 138449D NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 505SW 24182 DURING WALK-AROUND, FOUND SIX WHITE EMERGENCY TRACK LIGHTS INOP. INSPECTED AND FOUND WIRE PULLED FROM LIGHT ASSEMBLY AT ROW 18. REPAIRED AND OP CHECKED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996071800196 19960718 00196 NM 1996 7 18 SWAA960639 1 19960708 A 3350 LIGHT BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 526SW 26568 DURING WALK-AROUND, FOUND FLOOR TRACK LIGHTING LOOSE AT MID CABIN AREA. REPAIRED AND OP CHECKED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996071800197 19960718 00197 NM 1996 7 18 SWAA960640 1 19960708 A 3397 WIRE BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 367SW 26578 DURING WALK-AROUND, FOUND FLOOR TRACK LIGHTING INOP AT LEFT OVERWING EXIT. FOUND BROKEN WIRE. REPAIRED AND OP CHECKED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996071800198 19960718 00198 NM 1996 7 18 SWAA960641 1 19960708 A 5314 KEEL BEAM BOEING 737 7373H4 1384600 NM BS 500+2 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED D-CHECK, FOUND CORROSION ON KEEL BEAM AT BS 500 PLUS 2, LBL 8, WL 149. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996071800199 19960718 00199 NM 1996 7 18 SWAA960642 1 19960708 A 5312 BULKHEAD WEB BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED D-CHECK, FOUND BS 178 PRESSURE BULKHEAD WEB CRACKED AT WL 199.5. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996071800200 19960718 00200 NM 1996 7 18 SWAA960643 1 19960708 A 5312 BULKHEAD WEB BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED D-CHECK, FOUND BS 178 PRESSURE BULKHEAD WEB CRACKED AT WL 200, LBL 4.7. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996071800201 19960718 00201 NM 1996 7 18 SWAA960644 1 19960708 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 318 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 318, RBL 43, WL 173. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996071800202 19960718 00202 NM 1996 7 18 SWAA960645 1 19960708 A 5315 FLOOR BEAM BOEING 737 7373H4 1384600 NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORRODED AT BS 312, BL 0, WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996071800203 19960718 00203 NM 1996 7 18 SWAA960646 1 19960708 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 480 CREASED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CREASE AT BS 480, S28L TO 29L, WL 264. INSTALLED REPAIR DOUBLER PER BOEIN G SRM. 2 L 7 2 4F RT A16WE 1996071800204 19960718 00204 NM 1996 7 18 SWAA960647 1 19960708 A 2782 654465111 ACTUATOR BOEING 737 7372H4 138448C NM NR 1 LE SLAT FAILED A SWAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 07 51SW 21448 AFTER TAKEOFF, NUMBER 1 L/E SLAT WOULD NOT RETRACT. AIRCRAFT RETURNED TO MCO AND MADE AN UNEVENTFUL LANDING. REPLACED SLAT ACTUATOR AND LEAK CHECKED PER BOEING M/M. 2 L 7 2 4F A16WE 1996071800205 19960718 00205 NM 1996 7 18 VNAA9607005 1 19960706 A 3244 26107012 TIRE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT MLG FLAT A VNAA O OTHER E VIBRATION/BUFFET TX TAXI/GRND HDL 1 GL 07 458PS 120 3068 DURING TAXI OUT, CREW REPORTED HEARING A LOUD THUMPING SOUND FROM THE LEFT SIDE OF THE AIRCRAFT, ASSOCIATED WITH THE AIR CRAFT SLOWING ALMOST TO A STOP. CREW ELECTED TO SHUT DOWN BOTH ENGINES AND CALL MX. UPON ARRIVING AT THE AIRCRAFT, MX NOTICED THAT THE LEFT OUTBOARD MAIN LANDING GEAR TIRE WAS FLAT. MX REPLACED THE LEFT MAIN LANGING GEAR TIRE/WHEEL ASSEM BLY IAW MM 32-40-00. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996071800240 19960718 00240 NM 1996 7 18 9614982276 1 19960710 A 2782 1U1095 ACTUATOR BOEING 727 727251 138408H NM NR 1 LE SLAT FAILED A NWAA A J UNSCHED LANDING DUMP FUEL F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 01 276US 21155 DURING FLAP RETRACTION, THE NR 1 SLAT AMBER LIGHT ILLUMINATE ON SECOND OFFICER'S PANEL. VISUAL CHECK SHOWED NR 1 SLAT D ID NOT RETRACT. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED NR 1 SLAT ACTUATOR, PERFORMED FLAP/SLAT LEAK AND OPERATIONAL CHECK, CHECKED OK. 2 L 7 3 4F A3WE 1996071800241 19960718 00241 WP 1996 7 18 9614999969 1 19960709 A 7331 FUEL FLOW IND DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9A 52048 NE LT ENGINE MALFUNCTIONED A NWAA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 GL 01 9333 47246 DURING CRUISE FLIGHT, LEFT ENGINE FUEL FLOW BEGAN ERRATIC FLUCTUATIONS BETWEEN 4,000 LBS AND 6,000 LBS. A PRECAUTIONARY ENGINE SHUTDOWN WAS ACCOMPLISHED AND FLIGHT CONTINUED TO DESTINATION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE D EFERRED LEFT ENGINE FUEL FLOW INDICATION PER MEL 73-1A. 2 L 7 2 4F 4 F A6WE E2EA 1996071800242 19960718 00242 NE 1996 7 18 9615001159 2 19960709 A 7200 ENGINE DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 3 MALFUNCTIONED A NWAA E ENGINE SHUTDOWN J WARNING INDICATION LD LANDING 1 GL 01 159US 46768 86156 DURING LANDING ROLLOUT, THE NR 3 ENGINE EXPERIENCED REVERSE STALL. WITH EGT INCREASING TO 1,000 DEGREES, CREW FOLLOWED COM PROCEDURE AND SHUT DOWN THE ENGINE WHILE STILL IN REVERSE. AIRCRAFT WAS TAXIED TO THE GATE WITHOUT FURTHER INCIDENT . BORESCOPE INSPECTION REVEALED NO DAMAGE. THE NR 3 ENGINE WAS PLACED ON AN 80 HOUR MAXIMUM FLYBACK. 2 L 7 3 4F 4 F A22WE E20EA 1996071800243 19960718 00243 EU 1996 7 18 9615013244 1 19960711 A 2421 740119D IDG AIRBUS 320 A320211 3930320 EU NR 1 INOPERATIVE A NWAA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS M J OVER TEMP WARNING INDICATION NR NOT REPORTED 1 GL 01 344NW 19125 11422 388 DURING FLIGHT, RECEIVED AN OVERHEAT INDICATION ON THE NR 1 INTEGRATED DRIVE GENERATOR. DISCONNECTED SAME PER THE COCKPI T OPERATING MANUAL. APU STARTED NORMALLY, HOWEVER AFTER APPROXIMATELY 10 MINUTES AN APU AUTO SHUTDOWN OCCURRED. DIVERT ED TO RNO WITHOUT FURTHER INCIDENT. REPLACED THE NR 1 INTEGRATED DRIVEN GENERATOR AND FLUSHED THE EXTERNAL COOLING SYST EM. LEAK, OPERATIONAL AND FUNCTIONAL DISCONNECT CHECKS WERE ALL OK. APU OPERATED NORMALLY ON THE GROUND. 2 L 7 2 4F RT A28NM 1996071800244 19960718 00244 WP 1996 7 18 9615029971 1 19960711 A 3350 60030451 POWER SUPPLY DOUG DC9 DC931 3022065 WP AFT FUSELAGE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9335 47337 DURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHE CK NORMAL. 2 L 7 2 4F A6WE 1996071800245 19960718 00245 WP 1996 7 18 9615039945 1 19960711 A 4950 BLEED AIR DOUG DC9 DC931 3022065 WP APU LEAKING AIR A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 8925E 45840 DURING CLIMBOUT, PASSENGERS REPORTED A FUEL LIKE SMELL IN CABIN. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. M AINTENANCE FOUND THAT APU WAS BLEEDING RESIDUAL OIL INTO AIR CONDITIONING SYSTEM, APU WAS CHANGED ON 10JUL96. REPLACED COALESCER BAGS, LEAK AND OPERATIONAL CHECK WAS NORMAL. 2 L 7 2 4F A6WE 1996071800246 19960718 00246 WP 1996 7 18 9615049917 1 19960710 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 967N 47573 DURING LINE MAINTENANCE INSPECTION, FOUND OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL C HECK NORMAL. 2 L 7 2 4F A6WE 1996071800247 19960718 00247 WP 1996 7 18 9615059968 1 19960711 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9332 47264 DURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996071800248 19960718 00248 NM 1996 7 18 96FDEA01212 1 19960709 A 3260 DOWNLOCK SWITCH BOEING 727 72727C 138400J NM NLG DIRTY A FDEA O OTHER N FALSE WARNING AP APPROACH 1 SO 25 146FE 1911O AFTER INITIAL EXTENSION OF LANDING GEAR, NOSE GEAR LIGHT DID NOT ILLUMINATE GREEN LIGHT TESTED OKAY. LANDING GEAR RETRA CTED AND EXTENDED AGAIN WITH SAME RESULT OF UNSAFE NOSE GEAR INDICATION. ACCOMPLISHED CHECK LIST, RAISED AND LOWERED GE AR AGAIN. NOSE GEAR INDICATION GREEN ON THIRD ATTEMP AND ON ALL ATTEMPTS FELT NOSE GEAR EXTEND. CHECKED FOR WATER IN E AND E BAY AROUND LANDING GEAR MODULE, CHECKED ALL WIRING AND RIGGING ON NOSE GEAR DOWN LOCK SWITCH. CLEANED SWITCH WIT H CONTACT CLEANER AND LUBED LINKAGE. 2 L 7 3 4F A3WE 1996071800249 19960718 00249 NM 1996 7 18 96FDEA01224 1 19960701 A 5320 691487114 SHEAR TIE BOEING 727 7272D4 138407U NM BS 700 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 287FE 21849 DISCREPANCY: NR 0157 (010) CORROSION (C53-113-01) IN THE FORWARD CARGO BAY ON FRAME SHEAR TIE BS 700, WL 148, RBL 10. C ORRECTIVE ACTION: REMOVED CORRODED SHEAR-TIE AT BS 700, WL 148, RBL 10. FABRICATED NEW SHEAR-TIE AND INSTALLED REF SRM 53-10-4. 2 L 7 3 4F A3WE 1996071800250 19960718 00250 NM 1996 7 18 96FDEA01226 1 19960707 A 5754 6521715A BONDING JUMPER BOEING 727 72722 1384002 NM NR 3 LE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 NR 0552, 018, CORROSION (C57-562-01) NR 3 K-FLAP TO BULLNOSE O/B BONDING JUMPER, UPPER LOWER ATTACH POINTS. *S/D* REPL ACED NR 3 K-FLAP BULLNOSE, REPAIRED K-FLAP RIB AT O/B BONDING JUMPER UPPER ATTACH POINT IAW MM 27-81-1, SRM 57-50-3. 2 L 7 3 4F A3WE 1996071800251 19960718 00251 NM 1996 7 18 96FDEA01227 1 19960704 A 5754 65162252 UPPER LUG BOEING 727 72722 1384002 NM NR 4 LE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 NR 0549, 019, CORROSION (C57-562-01) ON THE O/B UPPER LUG O/B HINGE NR 4 K-FLAP. *S/D* REMOVED AND REPLACED K-FLAP PER MM 27-81-1. 2 L 7 3 4F A3WE 1996071800252 19960718 00252 NM 1996 7 18 96FDEA01228 1 19960709 A 5330 6517530101 SKIN BOEING 727 72722 1384002 NM BS 1243 OIL CANNED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 NR 0177, 020, OIL CANNED SKIN AT 1243 TO 1253 STR 22 TO 23 LT. *S/D* REPAIRED PER SRM 53-30-3 FIG 1. 2 L 7 3 4F A3WE 1996071800253 19960718 00253 NM 1996 7 18 96FDEA01230 1 19960710 A 5320 6516330 RIB BOEING 727 727173C 1384059 NM BS 870 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 199FE 19509 NR 0479, 016, CRACK ON LT INTERNAL RIB STR 13 AFT SIDE OF BS 870 TERMINAL FITTING AREA, APPROX 4 INCHES IN LENGTH. *S/D * REPAIRED CRACK ON LT INTERNAL RIB STR 13 AFT SIDE OF BS 870 TERMINAL FITTING IAW FED EX EA 7-53-10-29173. 2 L 7 3 4F A3WE 1996071800254 19960718 00254 NM 1996 7 18 96FDEA01231 1 19960707 A 5313 6554577 STRINGER BOEING 727 7272D4 138407U NM BS 720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 287FE 21849 DISCREPANCY: NR 00157 (011) CORROSION (C53-113-01 )(1) IN FORWARD CARGO BAY ON STR 27 AROUND BOLTS WL 148, BS 720C. CO RRECTIVE ACTION: REPAIRED CRACK ON LEFT INTERNAL RIB, STR 13, AFT SIDE BS 870 TERMINAL FITTING IAW FEDEX EA 7-5310-291 73. 2 L 7 3 4F A3WE 1996071800255 19960718 00255 NM 1996 7 18 96FDEA01232 1 19960709 A 5320 655457 SHEAR TIE BOEING 727 7272D4 138407U NM BS 720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 287FE 21849 NR 0348, 012, WHILE WORKING NR 0148 FOUND SHEAR TIE CORRODED BS 720, LBL 11, WL 148. *S/D* CORROSION FOUND TO BE OUT O F LIMITS. REMOVED OLD SHEAR TIE AND INSTALLED NEW IAW SRM 53-10-4. 2 L 7 3 4F A3WE 1996071800256 19960718 00256 NM 1996 7 18 96FDEA01233 1 19960709 A 5320 65562385 TEARSTRAP BOEING 727 7272D4 138407U NM BS 680 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 287FE 21849 DISCREPANCY: (NR 0137) (013) CORROSION (C53-113-01)(1) IN THE FORWARD CARGO BAY STRAP AND SKIN BS 680, WL 148, RBL 10. CORRECTIVE ACTION: CORROSION ON SKIN AND TEARSTRAP FOUND TO BE OUT OF LIMITS. ACCOMPLISHED SKIN AND TEAR STRAP REPAIR AT BS 680, RBL 10, WL 148, IAW SRM 53-30-4 AND SRM 53-10-04. 2 L 7 3 4F A3WE 1996071800257 19960718 00257 NM 1996 7 18 96FDEA01234 1 19960710 A 5320 6525995 SHEAR TIE BOEING 727 7272D4 138407U NM BS 1148 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 287FE 21849 DISCREPANCY: (NR 0147) (014) CORROSION (C53-113-01(2) IN THE AFT CARGO BAY FRAME SHEAR TIE BS 1148, WL 138, BLB 5, CORRO SION FOUND TO BE OUT OF LIMITS. REMOVED CORRODED SHEAR TIE, FABRICATED AND INSTALLED NEW SHEAR TIE AT BS 1148, WL 138, BLB 5, IAW 53-10-4. 2 L 7 3 4F A3WE 1996071800258 19960718 00258 1996 7 18 96FDEA01235 4 19960710 A 3417 ADC AIRBUS 310 A310203 EU NR 1 FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 403FE 230 AFTER GEAR RETRACTION CAPTAIN RED SPEED TAPE APPEARED RENDERING SPEED INFO INOP. SWITCHED ADC INSTRUMENT TO SYS, TWO SP EED INFO RECOVERED. NR 1 AND 2 AUTO THROTTLE TRIPPED, NR 2 ONLY RESET, BOTH LOWER ACCESS DOOR SHOW AMBER WITH CHIME. C ABIN RATE OF CLIMB ABOUT THE SAME AS A/C RATE OF CLIMB, ECAM DOOR PAGE SHOWS GREEN PRIOR TO BLOCKOUT ELECTED TO RETURN T O IAH. REMOVED AND REPLACED NR 1 ADC AND C/W PITOT STASTIC CHECKS NORMAL, RED SPEED LIMIT LIGHT OK. FOUND ACCESS DOOR HANDLE TRIPPED, RESET OK. 2 L 7 2 4F RT A35EU 1996071800259 19960718 00259 NM 1996 7 18 96FDEA01236 1 19960710 A 5312 65AUG1327 BULKHEAD TEE BOEING 747 747245F 1384897 NM BS 1480 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 641FE 20827 AFT CARGO BS 1480 RBL 33 BULKHEAD UPPER CHORD FOUND CRACKED APPROX 3 INCH. *S/D* BS 1480 BULKHEAD UPPER T-CHORD REPLAC ED AS PER EA NR 310-96 WITH BSB 747-53-2282 REV 01 WORK INSTRUCTION. 2 L 7 4 4F A20WE 1996071800260 19960718 00260 WP 1996 7 18 96FDEA01237 1 19960710 A 5412 BULKHEAD DOUG DC10 DC1010F 3022111 WP BS 31.8 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 NR 2 ENGINE INTAKE FWD BULKHEAD STA 31.8 HAS SEVERAL CRACKS AT THE FOLLOWING POS; 5 O'CLOCK, 5:45, 6:15, 8:30 AND 9 O'CL OCK POSITION. REMOVED AND REPLACED LEFT AND LOWER WEB SECTIONS PER SRM 54-10-00. 2 L 7 3 4F A22WE 1996071800261 19960718 00261 EU 1996 7 18 96FDEA01238 1 19960711 A 2910 HYD LINE AIRBUS 310 A310221 3930310 EU LT WING LEAKING A FDEA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 25 418FE 343 STA KHH LOST GREEN HYD SYS DURING DESCENT PERFOMED ECAM ITEMS. WHEN A/C ARRIVED CK'D GREEN RSVR QTY AND FOUND LOWER THA N HAT ARC. T/S FOUND HYD FLUID LEAKING FROM LT INSIDE WING SPAR BETWEEN PYLON AND 1ST FLAP TRACK IT IS A RIDGID LINE FO R AILERON DROOP RUBBING AND HAD A CUT HYD TUBE FABRICATED BY CAL PER MM 20-23-11 NEW TUBE INSTALLED AND LEAK CHECKED GOO D. 2 L 7 2 4F RT A35EU 1996071800262 19960718 00262 WP 1996 7 18 96FDEA01239 1 19960712 A 7120 MOUNT BOLTS DOUG DC10 DC1010F 3022111 WP NR 3 PYLON LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 059 46907 NR 4316, WHILE INSPECTING NR 3 PYLON FORWARD MOUNT BULKHEAD, 3 LT AND 3 RT FORWARD MOUNT TRUSS FITTING, FOUND 7 MOUNT BO LTS LOOSE, PYLON STATION YN 222-227 AT LOWER FORWARD HORIZONTAL SPAR CAPS LT AND FWD SIDES REF LAX C-02-SNRM NR 4316. 2 L 7 3 4F A22WE 1996071800263 19960718 00263 WP 1996 7 18 96FDEA01240 1 19960712 A 7120 BOLTS DOUG DC10 DC1010F 3022111 WP NR 1 PYLON LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 DISCREPANCY: NR 4110, WHILE INSPECTING NR 1 PYLON FORWARD MOUNT BULKHEAD LT AND RT FORWARD MOUNT TRUSS FITTING, FOUND 1 EA TRUSS MOUNT BOLT LOOSE ON LT LOWER SPAR CAP, FOUND MORE MOUNT BOLTS LOOSE, PYLON STA YN 222-227. BOLTS REMOVED, HOL ES INSPECTED AND FOUND OK. BOLTS REPLACED IAW SB 54-95. 2 L 7 3 4F A22WE 1996071800264 19960718 00264 NM 1996 7 18 96FDEA01241 1 19960707 A 5312 651633070 BULKHEAD WEB BOEING 727 72722 1384002 NM BS 870 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 DISCREPANCY: NR 0711. FOUND CRACK ON WHEELWELL BULKHEAD STA 870, WL 190, LBL 50 (CENTER TANK). CORRECTIVE ACTION: REP AIRED PER SRM 53-10-9, FIG 4. 2 L 7 3 4F A3WE 1996071800265 19960718 00265 NM 1996 7 18 96FDEA01242 1 19960707 A 5320 65163169 CHORD BOEING 727 72722 1384002 NM BS 344 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 DISCREPANCY: NR 0622 023 CORROSION ON UPPER CHORD BS 344, RBL 7 TO LBL 55, WL 208. ***S/D *** REMOVED AND REPLACED UP PER CHORD OF FLOOR AT STATION 344, RBL 65 TO LBL 65 IAW FED EX SRM 27-53-007. 2 L 7 3 4F A3WE 1996071800266 19960718 00266 NM 1996 7 18 96FDEA01243 1 19960707 A 5320 65183834 TRIPLER BOEING 727 72722 1384002 NM BS 1110-1130 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 NR 0717 024, BS 1110 TO 1130, STR 26R, WL 152. SKIN IS BULGED. *S/D* OPENED SKIN LAP REMOVED THE CORROSION BY BLENDIN G .002 FROM AN AREA OF 6 BY 12 ON THE SKIN. REMOVED THE TRIPLER REINSTALLED FASTENERS, AREA IS WITHIN LIMITS AS PER SRM 53-30-1. 2 L 7 3 4F A3WE 1996071800267 19960718 00267 NM 1996 7 18 96UAL900480 1 19960624 A 2910 BACH8B04NN0157 HOSE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LT ELEV ACT LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 7261U 21408 TOTAL A-SYSTEM HYDRAULIC FLUID QUANTITY LOSS ON DEPARTURE. FEATHERED PUMPS AND RETURNED TO ORD. *S/D* FOUND FLEX LINE LEAKING AT LEFT ELEVATOR ACTUATOR. REPLACED LINE AND CHECKED FOR LEAKS. 2 L 7 3 4F 4 F A3WE E2EA 1996071800268 19960718 00268 NM 1996 7 18 96UAL900481 1 19960624 A 2820 69186127 FUEL VENT TUBE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 FUEL TANK BROKEN A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 7444U 21898 NUMBER 1 MAIN FUEL QUANTITY INOPERATIVE, GAUGE ERRATIC, ROLLS UP AND DOWN. CROSS-FEED OPEN, NR 2 MAIN PUMPS ON AND NR 1 PUMPS OFF. *S/D* MAINTENANCE REMOVED BROKEN VENT ELBOW IN NR 1 TANK, HAD ELBOW WELDED AND IT WAS REINSTALLED AND LEAK CHECKED OKAY. 2 L 7 3 4F 4 F A3WE E2EA 1996071800269 19960718 00269 NM 1996 7 18 96UAL900485 1 19960625 A 2820 69186128 FUEL VENT TUBE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 FUEL TANK BROKEN A UALA O OTHER O OTHER CR CRUISE 1 WP 29 7263U 21410 WHILE CROSS-FEEDING ALL ENGINES FROM NUMBER 2 TANK NUMBER 3 FUEL QUANTITY DECREASED 700 LBS. *S/D* FUEL VENT TUBE ELBOW CRACKED AT FLANGE. REPLACED TUBE ELBOW, LEAKED CHECKED OKAY AND NO TRANSFER NOTED. 2 L 7 3 4F 4 F A3WE E2EA 1996071800270 19960718 00270 NM 1996 7 18 96UAL900491 1 19960627 A 3251 651781410 ACTUATOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NLG STEERING BYPASSING A UALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 29 7456U 21910 ON THE RUNWAY LINE UP THE NOSE WHEEL STEERING FAILED, LOCKED WITH TILLER BOW FULL RIGHT. MAINTENANCE TOWED AIRCRAFT BAC K TO GATE. *S/D* REPLACED NLG STEERING CYLINDER DUE TO BYPASSING. 2 L 7 3 4F 4 F A3WE E2EA 1996071800271 19960718 00271 NM 1996 7 18 96UAL900496 1 19960702 A 3350 60243 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 568UA 26674 EMERGENCY ESCAPE LIGHT STRIP AT THRESHOLD OF AFT LAV INOP. REPLACED EMERGENCY ESCAPE LIGHT STRIP AT AFT LAV THRESHOLD W ITH NEW LIGHT ASSEMBLY, OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996071800272 19960718 00272 NM 1996 7 18 96UAL900497 1 19960702 A 5330 SKIN BOEING 737 737322 1384676 NM CARGO DR CUTOUT CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 312UA 23673 SKIN CRACKED IN V-SHAPE 4 INCHES AFT OF REAR CARGO DOOR CUTOUT AT STATION 847 FROM STRINGER 20R TO 23R. SOME RIVETS PUL LED ALONG WITH SOME DOUBLER BONDING SEPARATION. BONDED DOUBLER AND BEAR STRAP STILL INTACT. 2 L 7 2 4F RT A16WE 1996071800273 19960718 00273 NM 1996 7 18 96UAL900498 1 19960702 A 2560 GIRT BAR AIR CRUISERS 62772201 BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE DOOR 2L SLIDE OUT OF POSITION A UALA K NONE O OTHER NR NOT REPORTED 1 WP 29 774UA 26936 DOOR 2 LEFT SLIDE UNRAVELED, DOOR ASSIST BOTTLE BLOWN. *S/D* THE SLIDE GIRT MATERIAL WAS DISLODGED FROM ITS RETAINING TRAY FORCING THE MODE SELECT HANDLE TO THE DOOR ARM POSITION UPON DOOR OPENING. INSTALLED NEW SLIDE AND CHECK FOR PROPE R STOWAGE OF GIRT MATERIAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 1996071800274 19960718 00274 NM 1996 7 18 96UAL900499 1 19960703 A 3350 LIGHT BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 106UA 26474 EMERGENCY EXIT LIGHTING CROSS AISLE BETWEEN DOOR 2L AND 2R ARE INOP. REPAIRED EMERGENCY EXIT LIGHTING STRIP. 2 L 7 4 4F 4 F RT A20WE E24NE 1996071800275 19960718 00275 NM 1996 7 18 96UAL900500 1 19960703 A 2612 FIRE WIRE BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE APU CHAFED A UALA F ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 WP 29 156UA 20105 APU FIRE WARNING CAME ON DURING LANDING ROLL OUT WITH INTERMITTENT FAULT LIGHT. DISCHARGED FIRE BOTTLE, NO EVIDENCE OF FIRE. *S/D* INVESTIGATION REVEALED A CHAFED FIRE DETECTION WIRE. CORRECTIVE ACTION WAS TAKEN TO INSULATE CHAFFED WIR E. THIS IS CONSIDERED AN ISOLATED EVENT. 2 L 7 4 4F 4 F A20WE E20EA 1996071800276 19960718 00276 NM 1996 7 18 96UAL900501 1 19960703 A 2130 PRESS SYSTEM BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN MALFUNCTIONED A UALA O OTHER O OTHER CL CLIMB 1 WP 29 7283U 21561 LOST CONTROL OF CABIN PRESSURE AT TOP OF CLIMB. THROTTLES AT IDLE, CABIN CLIMBED AT 1300 TO 1500 FPM UNTIL POWER WAS AD DED. 2 L 7 3 4F 4 F A3WE E2EA 1996071800278 19960718 00278 EU 1996 7 18 96UAL900503 1 19960705 A 2150 NSA5532612 CLAMP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 PACK BROKEN A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 432UA 587 UNPLANNED STOP AT PDX DUE TO LOSS OF CABIN PRESSURIZATION. *S/D* FOUND CLAMP ON THE OUTLET OF THE NR 1 PACK CONDENSER BROKEN CAUSING AIRCRAFT TO SLOWLY REPRESSURIZE. REPLACED CLAMP AND SYSTEM OPERATED NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 1996071800279 19960718 00279 NE 1996 7 18 96UAL900504 2 19960705 A 7313 6840023MS FUEL NOZZLE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE LEAKING A UALA F ACTIVATE FIRE EXT. A FLAME/FIRE IN INSP/MAINT 1 WP 29 921UA 25388 726363 NUMBER ONE ENGINE HAD A TAIL PIPE FIRE DURING START. FIRE BOTTLES WERE USED AND PASSENGERS WERE EVACUATED. ENGINE STAR T ABORTED AND GROUND CREW ADVISED OF THE ENGINE FIRE. *S/D* REPLACED ENGINE. THE FUEL NOZZLES WERE SENT TO AN OUTSIDE VENDOR FOR TESTING. SEVEN OF THE TWENTY NOZZLES HAD MINOR CHECK VALVE LEAKAGE. THIS CONDITION CONTRIBUTED TO THE TAIL PIPE FIRE. 2 L 7 2 4F 4 F RT A16WE E2GL 1996071800280 19960718 00280 NM 1996 7 18 96UAL900505 1 19960705 A 5242 652163137 DOOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE E/E DOOR OUT OF RIG A UALA O OTHER E VIBRATION/BUFFET CL CLIMB 1 WP 29 7291U 21569 VIBRATION AND THUMPING UNDER COCKPIT FLOOR. *S/D* FOUND ELECTRONICS ACCESS DOOR OUT OF RIG AND HANGING UP ON DOOR FRAM E. SUSPECT DOOR POPPED OFF OF FRAME CAUSING NOISE WHEN PRESSURIZED. ACCOMPLISHED DOOR RIG PER THE MM. 2 L 7 3 4F 4 F A3WE E2EA 1996071800281 19960718 00281 NE 1996 7 18 96UAL900506 2 19960705 A 7200 ENGINE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 MALFUNCTIONED A UALA O OTHER E VIBRATION/BUFFET CL CLIMB 1 WP 29 7461U 21915 AIRFRAME VIBRATION ON CLIMB-OUT AND CRUISE. CAN DUPLICATE VIBRATION BY ROLLING TO THE LEFT. CAN ELIMINATE VIBRATION BY PUTTING SMALL AMOUNT OF SPOILERS ON. PERFORMED DIAGNOSTIC TEST FLIGHT AND FOUND VIBRATION RELATED TO NR 1 ENGINE. REP LACED ENGINE. BORESCOPED OKAY. PRE-REPAIR RUN VERIFIED A MAX VIBRATION OF 3.4 MILS ON INLET AND 2.4 MILS ON EXHAUST. T RIM BALANCED ENGINE AT THE FAN TO 1.9 MILS ON INLET AND 1.9 ON EXHAUST. NO DEFINITE CAUSE FOUND FOR THE VIBRATION REPOR TED. 2 L 7 3 4F 4 F A3WE E2EA 1996071800282 19960718 00282 NM 1996 7 18 96UAL900507 1 19960705 A 2751 FLAP INDICATOR HAROWE SERVO 2061131 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE TE FLAPS MALFUNCTIONED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 7460U 21914 UNABLE TO RETRACT FLAPS FULLY, RETURNED TO LAS. *S/D* REPLACED INBOARD FLAP INDICATOR PER MM 27-54-18. 2 L 7 3 4F 4 F A3WE E2EA 1996071800283 19960718 00283 WP 1996 7 18 ABXA9600592 1 19960710 A 3231 RETRACT MECH DOUG DC8 DC861 3021952 WP RT MLG DOOR OUT OF ADJUST A ABXA K NONE J WARNING INDICATION CL CLIMB 1 GL 23 847AX 46031 LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION ON CLIMBOUT. RIGHT MAIN LANDING GEAR DOOR NOT LATC HED LIGHT WAS FOUND TO BE ILLUMINATED. LANDING GEAR WAS RECYCLED SEVERAL TIMES. ALL INDICATIONS WERE NORMAL WITH GEAR DOWN AND ALL ABNORMAL INDICATIONS EXTINGUISHED DURING FINAL APPROACH. RIGGED RIGHT MAIN LANDING GEAR DOOR FOLLOW-UP SYS TEM IAW DC8 MM, CHAPTER 32-31-5. PERFORMED RETRACTION CHECK AND ALL INDICATIONS WERE GOOD. 2 L 7 4 4F 4A25 1996071800284 19960718 00284 WP 1996 7 18 ABXA9600593 1 19960711 A 2510 56410311ABX1 SEAT DOUG DC8 DC861 3021952 WP LT COCKPIT DEFECTIVE A ABXA O OTHER O OTHER TO TAKEOFF 1 GL 23 852AX 46016 CAPTAIN'S AND FLIGHT ENGINEER'S SEATS SLIPPED OUT OF THE LOCKED POSITIONS DURING TAKEOFF. CLEANED FLIGHT ENGINEER'S SEA T TRACKS AND LUBED SEAT LOCKING PINS. REPLACED CAPTAIN'S SEAT IAW DC8 MM. OPS CHECK GOOD FOR CAPTAIN'S AND FLIGHT ENGI NEER'S SEATS LOCKING IN POSITION. 2 L 7 4 4F 4A25 1996071800285 19960718 00285 NM 1996 7 18 CALA9600996 1 19960624 A 5753 TRACK BOEING 727 727227 1384078 NM NR 4 TE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17773 21045 INSPECTION FOUND A .75 INCH CRACK IN OUTBOARD SIDE OF NR 4 FLAP TRACK TO MAIN LANDING GEAR BEAM ATTACH BOLT AREA. THE F LAP TRACK WAS REMOVED AND REPLACED IAW SRM 57-10-0 AND MM 27-51-0. 2 L 7 3 4F A3WE 1996071800286 19960718 00286 NM 1996 7 18 CALA9600997 1 19960702 A 5312 BULKHEAD BOEING 737 7373T0 1384582 NM BS 178-180 DAMAGED A CALA K NONE C F.O.D. IN INSP/MAINT 1 SW 09 18350 23588 THE AIRCRAFT EXPERIENCED A BIRD STRIKE RESULTING IN DAMAGE TO FUSELAGE SKIN AND BS 178 BULKHEAD WEB AT APPROXIMATELY RBL 20, WL 190. THE BULKHEAD WEB WAS REPAIRED IAW ECRA 5310-03301. THE SKIN AT STA 180 WAS REPAIRED PER SRM 53-00-01, FIG URE 27. 2 L 7 2 4F RT A16WE 1996071800287 19960718 00287 NM 1996 7 18 CALA9600998 1 19960709 A 5330 SKIN BOEING 727 727232 1384082 NM BS 520 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A 5 INCH CRACK WITH CORROSION IN SKIN LAP JOINT AT STA 520, S24L. REPAIRED IAW SRM 53-30-03, FIGURE 5. 2 L 7 3 4F A3WE 1996071800288 19960718 00288 NM 1996 7 18 CALA9600999 1 19960705 A 5720 STIFFENER BOEING 737 737130 1384435 NM WS 180.36 DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 408PE 19025 TWO STIFFENERS AND AFT SIDE OF WEB ON RT WING AT STA 180.36 SUSTAINED DAMAGE FROM TOOLING. THE STIFFENERS WERE REMOVED AND THE DAMAGED AREA WAS BLENDED IAW SRM 51-30-2 AND 57-10-1. STIFFENERS AND REPAIR PLATES WERE FABRICATED AND INSTALLE D IAW SRM 57-10-2 ANS 57-10-6. 2 L 7 2 4F A16WE 1996071800289 19960718 00289 NM 1996 7 18 CALA9601000 1 19960705 A 5330 SKIN BOEING 737 737130 1384435 NM BS 312-328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 408PE 19025 INSPECTION FOUND LOWER FUSELAGE SKIN AND STRINGER CORRODED WITH RIVETS POPPED AT STA 312 TO 328, STRINGER 27L TO 26R. T HE CORRODED AREA OF SKIN WAS CUT OUT, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-2. STRINGER 28 WAS RE MOVED AND REPLACED IAW SRM 53-30-2 AND 51-30-2. 2 L 7 2 4F A16WE 1996071800290 19960718 00290 NM 1996 7 18 CALA9601001 1 19960704 A 5330 SKIN BOEING 737 737130 1384435 NM BS 400 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 408PE 19025 INSPECTION FOUND A DENT IN FUSELAGE SKIN AT STA 400, S18L. THE DENTED AREA WAS CUT OUT, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 AND 51-10-2. 2 L 7 2 4F A16WE 1996071800291 19960718 00291 NM 1996 7 18 CALA9601002 1 19960704 A 5330 SKIN BOEING 737 737130 1384435 NM BS 277 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 408PE 19025 INSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN AT STA 277, STRINGER 26R. THE CRACKED AREA WAS CUT OUT, A REPAIR DOUBL ER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-2, 53-30-3 AND 51-10-2. 2 L 7 2 4F A16WE 1996071800292 19960718 00292 NM 1996 7 18 CALA9601003 1 19960705 A 5230 SKIN BOEING 737 737130 1384435 NM C 2 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 408PE 19025 INSPECTION FOUND A .5 INCH CRACK AT LIGHTENING HOLE OF C-2 DOOR INTERIOR SKIN. THE CRACK WAS STOP DRILLED, A WEB REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-2, 51-30-2 AND 51-40-2. 2 L 7 2 4F A16WE 1996071800293 19960718 00293 NM 1996 7 18 CALA9601004 1 19960704 A 5730 SKIN BOEING 737 737130 1384435 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 408PE 19025 INSPECTION FOUND TWO .25 INCH CRACKS IN RT WING LEADING EDGE SKIN AT ANTI-ICE DUCT CUTOUT, NR 5 SLAT. THE CRACKED AREA WAS CUT OUT, REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 57-30-4 AND 51-10-2. 2 L 7 2 4F A16WE 1996071800294 19960718 00294 NM 1996 7 18 CALA9601005 1 19960705 A 5720 STIFFENER BOEING 737 737130 1384435 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 408PE 19025 INSPECTION FOUND A .25 INCH CRACK IN RT WING VERTICAL STIFFENER AT LEADING EDGE UNDER PANEL 6526. THE STIFFENER WAS REM OVED AND REPLACED IAW SRM 51-30-2 AND 51-10-5. 2 L 7 2 4F A16WE 1996071800295 19960718 00295 NM 1996 7 18 CALA9601006 1 19960704 A 5315 FLOOR BEAM BOEING 737 737130 1384435 NM BS 660 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 408PE 19025 INSPECTION FOUND A .5 INCH CRACK IN FLOOR BEAM UPPER CHORD AT STA 660, BL 07. THE FLOORBEAM WAS REPAIRED IAW EA 5710-01 322, OPERATION 2 AND ECRA 5710-01743. 2 L 7 2 4F A16WE 1996071800296 19960718 00296 1996 7 18 CKSA96073 2 19960711 A 7530 BLEED AIR DOUG DC8 DC855 3021927 WP NR 2 ENGINE ODOR A CKSA O OTHER O OTHER CL CLIMB 1 GL 23 801CK 45816 OPERATING ALL 4 BLEEDS ON CLIMBOUT DETECTED AN ODOR. EYES BURNED COULD TASTE OILY SUBSTANCE IN MOUTH. PROBLEM REDUCED WITH NR 2 BLEED TURNED OFF. PERFORMED ENGINE RUN AND OPS CHECK AND ALL ENGINE BLEEDS NOTICED ODOR ONLY WITH NR 2 BLEED ON, CLOSED NR 2 BLEED AND ENTERED ON DMI NR 96 IAW AIA MEL CHAPTER 36-1 CAT C PLACARDS INSTALLED. RAN ALL ENGINES TO TA KEOFF POWER WITH BLEEDS ON, COULD NOT DUPLICATE ON GROUND AND OPS CHECKED NORMAL IAW 72-00. 2 L 7 4 4F 4A25 1996071800297 19960718 00297 SO 1996 7 18 COMA9610222 1 19960710 A 5280 12036136001 BRACKET EMB 120 EMB120RT SO LT MLG DOOR BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 196CA 120196 LT MLG AFT GEAR DOOR BRACKET IS BROKEN. REPLACED BRACKET. 2 L 7 2 4T RT A31SO 1996071800298 19960718 00298 NM 1996 7 18 DHL96740004 1 19960709 A 3510 10608872 OXY REGULATOR BOEING 727 7272Q9 138448M NM COCKPIT LEAKING A T DHLA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 740DH 21930 AFTER TAKEOFF CHECKLIST, CREW OXYGEN WAS READING 100 LBS. SWAPPED CAPTAINS AND SECOND OBSERVERS REGULATOR, REPLACED OXY GEN REGULATOR, NO LEAKS NOTED MM 35-10 2 L 7 3 4F RT A3WE 1996071800299 19960718 00299 NE 1996 7 18 DHL96801011 2 19960709 A 7260 3505154211 STARTER PAD DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C1 13802 NE NR 4 ENGINE DAMAGED A T DHLA A E J UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL J WARNING INDICATION CR CRUISE 1 SO 01 801DH 46033 692365 NR 4 ENGINE WAS SHUT DOWN DURING FLIGHT. OIL PRESSURE STARTED FLUXUATING AND OIL QTY WENT TO ZERO. REMOVED AND REPLACE D NR 4 ENGINE FOR STARTER PAD DAMAGE. 2 L 7 4 4F 4 F RT 4A25 E2GL 1996071800303 19960718 00303 NM 1996 7 18 DL72K961603 1 19960515 A 5753 652179612 FAIRING BOEING 727 727232 1384082 NM TE FLAP TRACK CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 491DA 21060 DURING A ROUTINE INSPECTION, A CRACK WAS DISCOVERED ON THE LEFT HAND OUTBOARD FLAP TRACK FAIRING. THE CRACK IS .75 IN L ENGTH AND IS LOCATED ON THE OUTBOARD SIDE OF THE FAIRING. THE FAIRING SKIN IS MANUFACTURED FROM 0.040 7075-T6. REPAIRE D PER ERA 303601-14. 2 L 7 3 4F A3WE 1996071800307 19960718 00307 NM 1996 7 18 DL72L961614 1 19960418 A 5320 65175186 TRANSVERSE BEAM BOEING 727 727232 1384082 NM BS 1273 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 509DA 21311 THERE IS A 2.5 INCH CRACK IN THE ANGLE OF BOTH THE TRANSVERSE BEAM AND THE GUSSET OF THE TORQUE BOX AT FS 1273. THESE A REAS OF THE TORQUE BOX ARE THE SUBJECT OF AD 94-07-08, WHICH REQUIRES INSPECTION PER S/B 53-0129. THIS REPLACEMENT DOES NOT TERMINATE THE REPETITIVE INSPECTION REQUIREMENTS. TERMINATING ACTION WILL BE PROVIDED BY EO 4-61071-3. 2 L 7 3 4F A3WE 1996071800308 19960718 00308 NM 1996 7 18 DL72P961613 1 19960430 A 5320 651751738 TRANSVERSE BEAM BOEING 727 727225 1384077 NM BS 1263 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8873Z 21291 THERE IS A CRACK IN THE ANGLE OF THE FWD TRANSVERSE BEAM OF THE RT TORQUE BOX AT FS 1263. THIS AREA OF THE TORQUE BOX I S THE SUBJECT OF AD 94-07-08, WHICH REQUIRES INSPECTION PER S/B 53-0129. THIS REPLACEMENT DOES NOT TERMINATE THE REPETI TIVE INSPECTION REQUIREMENTS. TERMINATING ACTION WIL BE PROVIDED BY EO 4-61071-3. 2 L 7 3 4F A3WE 1996071800309 19960718 00309 NM 1996 7 18 DL72S961589 1 19960201 A 5320 651751738 TRANSVERSE BEAM BOEING 727 727232 1384082 NM FS 1263 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 418DA 21271 THERE IS A CRACK IN THE ANGLE OF THE FWD TRANSVERSE BEAM OF THE RT TORQUE BOX AT FS 1263. THIS AREA OF THE TORQUE BOX I S THE SUBJECT OF AIRWORTHINESS DIRECTIVE 94-07-08, WHICH REQUIRES INSPECTION PER S/B 53-0129. THIS ER/A WILL REPLACE TH E DAMAGED PART IN ACCORDANCE WITH THE S/B. 2 L 7 3 4F A3WE 1996071800310 19960718 00310 NM 1996 7 18 DL72S961602 1 19960117 A 5320 65175186 TRANSVERSE BEAM BOEING 727 727232 1384082 NM BS 1273 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 408DA 21152 THERE IS A .5 INCH CRACK IN THE ANGLE OF BOTH THE FWD AND AFT TRANSVERSE BEAMS OF THE RT TORQUE BOX AT FS 1273. THESE A REAS OF THE TORQUE BOX ARE THE SUBJECT OF AIRWORTHINESS DIRECTIVE 94-07-08, WHICH REQUIRES INSPECTION PER S/B 53-0129. 2 L 7 3 4F A3WE 1996071800311 19960718 00311 NM 1996 7 18 DL72S961604 1 19960120 A 5311 FRAME BOEING 727 727232 1384082 NM FS 1166 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 419DA 21272 THE BS 1166 FRAME WAS FOUND CORRODED NEAR STRINGER 29R. THE REMOVED SECTION OF FRAME WAS TOO LARGE TO REPAIR PER THE B7 27 SRM. THE FRAME WEB IS MANUFACTURED FROM 0.063 CLAD 7075-T6. ALSO, THERE IS A FACTORY INSTALLED 0.050 CLAD 7075-T6 B ONDED DOUBLER INSTALLED AT THIS LOCATION. THE REPAIR WILL REQUIRE INSTALLATION OF TWO 0.040 TI-6AL-4V DOUBLERS AND ONE 0.071 CLAD 7075-T6 REPAIR ANGLE. THIS REPAIR MAINTAINS THE PREVENTATIVE MODIFICATION PREVIOUSLY ACCOMPLISHED AT STR 28R PER EO 4-59823-3AD, WHICH PROVIDES TERMINATING ACTION FOR THE REPETITIVE INSPECTIONS MANDATED BY AD 92-12-03. 2 L 7 3 4F A3WE 1996071800312 19960718 00312 NM 1996 7 18 DL72S961606 1 19960227 A 5320 651751738 TRANSVERSE BEAM BOEING 727 727232 1384082 NM BS 1263 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 467DA 20744 THERE IS A CRACK IN THE ANGLE OF THE FWD TRANSVERSE BEAM AND AFT CHANNEL OF THE RT TORQUE BOX AT FS 1263. THIS AREA OF THE TORQUE BOX IS THE SUBJECT OF AIRWORTHINESS DIRECTIVE 94-07-08, WHICH REQUIRES INSPECTION PER S/B 53-0129. REPAIRED PER ERA 303225-14AD. 2 L 7 3 4F A3WE 1996071800313 19960718 00313 NM 1996 7 18 DL72S961607 1 19960227 A 5320 651841483 WEB BOEING 727 727232 1384082 NM BS 284.5-285.5 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 476DA 20753 THE LT SIDEWALL WEB OF THE NOSE WHEEL WELL HAS A 2.5 INCH CRACK BETWEEN STA 294.5 AND 285.5 APPROXIMATELY AT WL 170. TH E WEB AT THIS LOCATION IS 0.040 CLAD 2024-T3. THE DAMAGED PORTION OF THE WEB WILL BE TRIMMED OUT AND A REPAIR DOUBLER A ND TWO STRAPS WILL BE INSTALLED. THE REPAIR IS ACCOMPLISHED PER S/B 727-53-0145. THIS REPAIR DOES NOT PROVIDE TERMINAT ING ACTION FOR EO 4-59270-3AD. 2 L 7 3 4F A3WE 1996071800316 19960718 00316 NM 1996 7 18 DL72S961615 1 19960321 A 2782 BRACKET BOEING 727 727232 1384082 NM NR 1-2-8 LE FLAP MISINSTALLED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 520DA 21471 THE NR 1, NR 2 AND NR 8 SLAT ACTUATOR MOUNT BRACKETS WERE FOUND WITH GAPS EXCEEDING THE 0.01 LIMIT SET BY SI 4-59271-12. THE GAPS AT THE MOUNT BRACKETS ARE THE SUBJECT OF S/B 727-57-0130. SHIMS WILL BE INSTALLED IN ACCORDANCE WITH THE SER VICE BULLETIN. THE BRACKETS WERE NOT FOUND TO BE CRACKED. THIS ER/A DOES NOT TERMINATE THE INSPECTION REQUIREMENTS OF SI 4-59271-12. ACCOMPLISHMENT OF EO 4-59271-3AD IS STILL MANDATORY PRIOR TO THE ACCUMULATION OF 60,000 FLIGHT CYCLES. 2 L 7 3 4F A3WE 1996071800317 19960718 00317 NM 1996 7 18 DL72S961616 1 19960321 A 2782 STIFFENER BOEING 727 727232 1384082 NM NR 8 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 520DA 21471 THE INBOARD ACTUATOR ATTACH RIB STIFFENER ON THE NR 8 SLAT ACTUATOR WAS FOUND CRACKED. THE DAL MFG PART NUMBER FOR THE INBOARD AND OUTBOARD STIFFENERS IS (57-0367-002). BOTH THE INBOARD AND OUTBOARD ATTACH RIB STIFFENERS WILL BE REPLACED PER EO 4-59271-3AD. THIS ER/A DOES NOT PROVIDE TERMINATING ACTION FOR EO 4-59271-3AD. OPERATIONS 570 AND 590 HAVE BEEN COMPLIED WITH FOR THE NR 8 SLAT ONLY. 2 L 7 3 4F A3WE 1996071800319 19960718 00319 NM 1996 7 18 DL72W961585 1 19960118 A 5320 65175186 TRANSVERSE BEAM BOEING 727 727247 138408F NM FS 1273 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 292WA 22110 THERE IS A 1 INCH CRACK IN THE ANGLE OF BOTH THE FWD AFT TRANSVERSE BEAMS OF THE RT TORQUE BOX AT FS 1273. THESE AREAS OF THE TORQUE BOX ARE THE SUBJECT OF AIRWORTHINESS DIRECTIVE 94-07-08, WHICH REQUIRES INSPECTION PER S/B 53-0129. THIS ER/A WILL REPLACE THE DAMAGED PARTS IN ACCORDANCE WITH TJE S/B. 2 L 7 3 4F A3WE 1996071800320 19960718 00320 NM 1996 7 18 DL72W961626 1 19960422 A 7120 65187228 MOUNT FITTING BOEING 727 727247 138408F NM NR 3 ENGINE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 290WA 22108 THE NR 3 ENGINE FORWARD MOUNT FITTING WAS FOUND CRACKED AND REQUIRED REPLACEMENT. THE CRACK EXTENDED FROM THE TOP OF TH E FITTING TO THE BOTTOM OF THE FITTING APPROXIMATELY 2 INCHES OUTBOARD OF THE FUSELAGE SKIN. THE CRACK FOLLOWED THE BLE ND LINE BETWEEN PLANE 'A' AND AUXILIARY PLANE 'A' AS NOTED IN BOEING DRQWING 65-18722, SHEET 2, ZONE 4A. THERE ARE NO 6 5-18722-8 FITTINGS PRESENTLY AVAILABLE AND IT IS REQUIRED THAT A 65-18722-4 FITTING FROM A RETIRED AIRCRAFT BE INSTALLED . INSTALLATION OF THE 65-18722-4 FITTING REQUIRES MODIFICATION IN ORDER TO REPLACE THE FITTING. 2 L 7 3 4F A3WE 1996071800321 19960718 00321 NM 1996 7 18 DL733961622 1 19960222 A 5330 SKIN BOEING 737 737347 1384647 NM BS 870-890 WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 309WA 23442 FUSELAGE SKIN (0.036 CLAD 2024-T3) UNDERNEATH THE VERTICAL STABILIZER FORWARD FAIRING FROM FS 870 TO 890 WAS FOUND WORN BEYOND B737-300 SRM 53-00-01 LIMITATIONS. THE WEAR WAS FOUND TO HAVE A MAXIMUM DEPTH OF APPROXIMATELY 0.012. ER/A WILL REPAIR THE DAMAGED AREA BY INSTALLING AN EXTERNAL DOUBLER. IT IS NOT NECESSARY TO CUTOUT THE DAMAGED AREA DUE TO MAXIM UM DAMAGED AREA OF 0.012 STILL LEAVES 66 PERCENT OF SKIN THICKNESS. 2 L 7 2 4F RT A16WE 1996071800322 19960718 00322 NM 1996 7 18 DL733961628 1 19960406 A 5330 654576972 SKIN BOEING 737 737347 1384647 NM BS 379 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 302WA 23182 THE SKIN AT THE COOLING DUCT CUTOUT, FS 379 BL 0, WAS FOUND CRACKED AT THE AFT EDGE OF THE CUTOUT. THE CRACK IS APPROX .5 IN LENGTH AND IS TYPICAL OF CRACKS DESCRIBED IN BACO S/B 737-53-1117 R-1. THE CRACK WILL BE STOP DRILLED AND A PERMA NENT REPAIR WILL BE INSTALLED PER THE BACO S/B. DURING ACCOMPLISHEMENT OF REPAIR, SKIN WAS DAMAGED JUST FORWARD OF FS 3 80, AT STR 27L, REQUIRING A SMALL CUTOUT. THE S/B DOUBLER WILL BE INCREASED IN SIZE TO ACCOUNT FOR THE ADDTIONAL DA MAGE. 2 L 7 2 4F RT A16WE 1996071800323 19960718 00323 NM 1996 7 18 DL73E961584 1 19960627 A 5312 BULKHEAD WEB BOEING 737 737247 138448D NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 373DL 23520 DURING ACCOMP OF SI 3-69482-12, TWO CRACKS WERE DISCOVERED ON THE FORWARD FACE OF THE BS 178 BULKHEAD WEB. FIRST CRACK IS LOCATED UNDER THE RBL 5.7 VERTICAL STRAP AT APPROXIMATELY WL 202 AND THE SECOND IS LOCATED UNDER THE LBL 5.7 VERTICAL STRAP, RANGING BETWEEN WL 198 AND WL 202. THE WEB IS MANUFACTURED FROM 0.040 2024-T3 CLAD. 2 L 7 2 4F A16WE 1996071800324 19960718 00324 NM 1996 7 18 DL73E961648 1 19960623 A 5753 BOLT BOEING 737 7372S3 NM NR 2 TE FLAP WORN THREADS A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 369DL 21776 WHILE ACCOMPLISHING TORQUE CHECK OF CENTER ATTACH BOLT OF NR 2 FLAP O/B TRACK ATTACH FITTING, THE CENTER BOLT WAS FOUND TO HAVE DAMAGED THREADS. IN ACCORDANCE WITH SB 737-57A1130, THE PREVENTATIVE MOD WILL BE INSTALLED. ADDITIONALLY, THE FLAP TRACK BUSHING WAS FOUND TO HAVE MINOR FRETTING ON THE INNER BORE. IN ACCORDANCE WITH FIGURE 4 OF SB 737-57A1130, T HE BUSHING HOLE CAN BE ENLARGED TO 0.5015 MAX DIAMETER. 2 L 7 2 4F RT A16WE 1996071800325 19960718 00325 NM 1996 7 18 DL73S961581 1 19960702 A 5330 6545769545 SKIN BOEING 737 737232 1384475 NM BS 373 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 303DL 23075 THE SKIN AT THE COOLING DUCT CUTOUT, BS 373 LBL 3, FOUND CRACKED AT THE AFT EDGE OF THE CUTOUT. THE CRACK IS APPROX 2 INCH LENGHTH AND IS TYPICAL OF CRACKS DESCRIBED IN BACO S/B 737-53-1117 R1. THE CRACK WILL BE STOP DRILLED AND A P ERMANENT REPAIR WILL BE INSTALLED PER BACO. 2 L 7 2 4F RT A16WE 1996071800326 19960718 00326 NM 1996 7 18 DL73S961583 1 19960627 A 5312 BULKHEAD WEB BOEING 737 737232 1384475 NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 323DL 23095 CRACKS DISCOVERED ON FORWARD FACE OF FS 178 BULKHEAD WEB. THE FIRST CRACK IS LOCATED NEAR THE RBL 5.7 VERTICAL STRAP AT APROX WL 200. THE SECOND IS LOCATED NEAR THE RBL 5.7 VERTICAL STRAP AT APROX WL 203. THE THIRD IS LOCATED NEAR LBL 5. 7 AT APPROXIMATELY WL 188. THE LBL 5.7 VERTICAL STIFFENER LOCATED ON THE AFT SIDE OF THE BULKHEAD IS ALSO CRACKED IN TH E RADIUS AT APPROXIMATELY WL 184.5. ENGINEERING REPAIR AUTHORIZATION REPAIRED CRACK WITH ONE EXT DOUBLER. THE STIFFENE R WILL BE REPAIRED WITH TWO ANGLES AND A STRAP. 2 L 7 2 4F RT A16WE 1996071800327 19960718 00327 NM 1996 7 18 DL73S961624 1 19960323 A 5312 BULKHEAD WEB BOEING 737 737232 1384475 NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 301DL 23073 DURING INSPECTION PER SI 3-69482-12, THE WEB OF FS 178 BULKHEAD WAS FOUND WITH FOUR CRACKS, EACH MEASURING APPROX 1 INCH , AT LBL 5.7 AND WL 195 AND RBL 5.7 AND WL 195. THE WEB IS MANUFACTURED FROM 0.040 CLAD 2024-T3, ER/A ISSUED FOR REPAIR . 2 L 7 2 4F RT A16WE 1996071800328 19960718 00328 NM 1996 7 18 DL757961465 1 19960618 A 2121 FAN BOEING 757 757232 1384965 NM CARGO COMPT FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 602DL 22809 ELECT SMELL IN AIRCRAFT AND SHORTLY AFTER AN EQUIPMENT COOLING MESSAGE. REPLACED FAN, OPS CHECK GOOD. 2 L 7 2 4F RT A2NM 1996071800329 19960718 00329 NE 1996 7 18 DL757961549 2 19960628 A 7200 ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 FAILED A DALA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 SO 27 608DA 22815 727102 LEFT ENG FAILURE ON CLIMBOUT PASSING 5,000 FT, PERFORMED ENG FAILURE PROCEDURE. REPLACED SVC. 2 L 7 2 4F 4 F RT A2NM E17NE 1996071800330 19960718 00330 NM 1996 7 18 DL757961560 1 19960629 A 2530 COFFEE MAKER BOEING 757 757232 1384965 NM AFT GALLEY FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 654DL 24394 ACFT DIVERTED INTO ABQ DUE TO ELECTRICAL SMELL IN THE AFT GALLEY. MTC FOUND COFFEE MAKER AT FAULT AND RENDERED INOP. 2 L 7 2 4F RT A2NM 1996071800331 19960718 00331 NM 1996 7 18 DL757961605 1 19960213 A 5754 114N4005157 SKIN BOEING 757 757232 1384965 NM NR 4 LE FLAP PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 635DL 23762 A .25 INCH HOLE WAS FOUND ON THE LOWER SKIN AND PARTIALLY INTO THE CORE ON THE NR 4 LEADING EDGE SLAT. THE HOLE IS LOCA TED 3 FT OUTBOARD OF THE INBOARD EDGE OF THE SLAT. THE TRAILING EDGE WEDGE IS AN ALUMINUM/HONEYCOMB PANEL WITH THE ALUM INUM SKIN MADE FROM 0.016 2024-T81 SHEET. 2 L 7 2 4F RT A2NM 1996071800332 19960718 00332 NM 1996 7 18 DL757961623 1 19960214 A 5320 146N53183 WEB BOEING 757 757232 1384965 NM BS 1681-1720 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 659DL 24421 THE AFT FUSELAGE SUBFLOOR WEB WAS FOUND CORRODED ON THE LEFT HAND SIDE FROM FS 1681-1720. THE WEB IS MANUFACTURED FROM 0.071 CLAD 2024-T3. THE DAMAGED SECTION WILL BE REMOVED AND REPLACED WITH A NEW SECTION. THE TWO WEBS WILL BE SPLICED TOGETHER WITH UPPER AND LOWER 0.080 CLAD 2024-T3 DOUBLERS AT LBL 4. 2 L 7 2 4F RT A2NM 1996071800333 19960718 00333 NM 1996 7 18 DL757961652 1 19960708 A 3350 767 BULB BOEING 757 757232 1384965 NM L2 DOOR FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 684DA 27104 ON LAYOVER, FOUND L2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. FOUND LAMP BURNT. RELAMPED SAME AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A2NM 1996071800334 19960718 00334 NM 1996 7 18 DL757961653 1 19960708 A 3350 767 BULB BOEING 757 757232 1384965 NM L4 DOOR FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 684DA 27104 ON LAYOVER, FOUND L4 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. FOUND BULB BURNT. RELAMPED SAME AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A2NM 1996071800335 19960718 00335 NM 1996 7 18 DL76L961651 1 19960625 A 2710 A2B3 CONTROL CABLE BOEING 767 767332 1382001 NM RT AILERON SEVERED A A DALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 27 185DN 27961 DURING CLIMB, FLIGHT CREW HEARD A CRACK FOLLOWED BY A/C ROLL TO THE LEFT. TEMPORARILY LOST LEFT IDG BUT QUICKLY RETURNE D. FOUND AILERON CONTROL CABLE A2B-3 SEVERED AND RIGHT GENERATOR FEEDER CABLE WORN JUST FORWARD AND RIGHT OF THE FORWAR D CARGO COMPARTMENT WALL APPROX STA 340, WL 190, RBL 67.5. REPLACED A2B-3 CABLE, RIGGED AND OPS CHECKED SAME, ALL OK. S PLICED RIGHT GENERATOR FEEDER CABLE FROM P-32 PANEL TO FORWARD CARGO COMPARTMENT WALL, OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 1996071800336 19960718 00336 WP 1996 7 18 DLL10961535 1 19960626 A 3530 PBE LKHEED 1011 10113851 5265010 WP LOWER GALLEY BUTTON POPPED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 720DA 193C1136 PBE IN LOWER GALLEY HAS BUTTON POPPED. REPLACED PBE, OK FOR SERVICE. 2 L 7 3 4F A23WE 1996071800337 19960718 00337 WP 1996 7 18 DLL10961540 1 19960624 A 5742 1527807101 FITTING LKHEED 1011 10113851 5265010 WP WS 503 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 729DA 193C1180 LT WING PYLON BACKUP FITTING BULKHEAD BETWEEN IWS 503 AND IWS 529 FOUND WITH A 6 INCH CRACK ORIGINATING AT THE I/B RAD O F THE SKIN ATTACH TAB, TRAVELING THROUGH THE INTEGRAL FLANGE AND PROCEEDED ACROSS THE WEB TOWARD THE CENTER RING INNER C AP AT45 DEG. THE FITTING M/F 7075-T6 FORGING. REPLACED FITTING. 2 L 7 3 4F A23WE 1996071800338 19960718 00338 WP 1996 7 18 DLL10961541 1 19960625 A 5711 1528363247 REAR SPAR LKHEED 1011 10113851 5265010 WP WS 0.0 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 729DA 193C1180 REAR SPAR WEB CRACKED AT WS 0.00 BEGINNING AT THE LOWER END OF WEB AND EXTENDING UP THROUGH TWO ATTACHMENTS TO THE LOWER SPAR ANGLE FOR 2. THE REAR SPAR WEB IS M/F .150 7075-T6511 PLATE. REPAIRED PER ERA273915-14. 2 L 7 3 4F A23WE 1996071800339 19960718 00339 WP 1996 7 18 DLL10961542 1 19960627 A 5330 SKIN LKHEED 1011 10113851 5265010 WP FS 629 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 727DA 193C1167 SEVERAL CRACKS WERE FOUND FROM A FASTENER. CUTOUT RESULTS WERE A 1.125 DIA HOLE. DAMAGE LOCATED AT FS 629 I/B OF STR 3 4, SKIN M/F .068 2024-T3 CLAD SHEET. REPAIRED PER ERA273975-14. 2 L 7 3 4F A23WE 1996071800340 19960718 00340 WP 1996 7 18 DLL10961548 1 19960628 A 3230 1516207121 CONTROL MODULE LKHEED 1011 10113851 5265010 WP RT MLG BINDING A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 716DA 193C1095 RIGHT GEAR WILL NOT RETRACT AFTER T/O. JACKED A/C, RIGHT GEAR WOULD NOT RAISE. REPLACED RIGHT MAIN LANDING GEAR PHASE CONTROL MODULE PER M/M. CYCLED GEAR SEVERAL TIMES, NOW OP AND LEAK CHECKS NORMAL. 2 L 7 3 4F A23WE 1996071800341 19960718 00341 WP 1996 7 18 DLL10961574 1 19960630 A 2100 1628962101 BRACKET LKHEED 1011 10113851 5265010 WP NR 2 RAM AIR DR MISSING A DALA K NONE D INFLIGHT SEPARATION IN INSP/MAINT 1 SO 27 1732D 193C1213 NR 2 ECS RAM AIR DOOR WAS FOUND MISSING ON ARRIVAL IN BOS. THE DOOR MOUNT BRACKETS HAD FAILED DUE TO CORROSION. UPON I NSP FOUND ALL THREE ECS RAM AIR DOOR MOUNTS CORRODED. 2 L 7 3 4F A23WE 1996071800344 19960718 00344 WP 1996 7 18 DLL10961600 1 19960603 A 5350 1505713103 FAIRING SUPPORT LKHEED 1011 10113851 5265010 WP BS 983 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 727DA 193C1167 LOWER FUSELAGE FAIRING ATTACH ANGLE WAS REPLACED DUE TO A 20 INCH CRACK FROM LBL 14 TO RBL 15 AT FS STA 983. 2 L 7 3 4F A23WE 1996071800345 19960718 00345 WP 1996 7 18 DLL10961636 1 19960705 A 3350 2233 LIGHT LKHEED 1011 10113851 5265010 WP L 2 DOOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 712DA 193C1088 L2 EXIT DOOR OVERWING SLIDE LIGHT INOP. RELAMPED. 2 L 7 3 4F A23WE 1996071800346 19960718 00346 WP 1996 7 18 DLL10961646 1 19960701 A 5320 1521397105 TRIPLER LKHEED 1011 10113851 5265010 WP FWD OUTFLOW VLV CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 729DA 193C1180 CORROSION WAS FOUND ON THE SURFACE OF THE INTERNAL TRIPLER SURROUNDING THE FWD OUTFLOW VALVE CUTOUT. THE CORROSION WILL BE REMOVED AND TREATED. 2 L 7 3 4F A23WE 1996071800347 19960718 00347 WP 1996 7 18 DLL13961550 1 19960627 A 5330 SKIN LKHEED 1011 10113851 5265010 WP BS 699/729 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 785DL 193A1121 THE BELLY SKIN AT FS 669 AND FS 729 AND STR 33 TO 35 WERE FOUND WITH SEVERAL AREAS OF CORROSION DURING RETIREMENT IN ATL . THE CORROSION WAS CUT OUT AND A FILLER/DOUBLER REPAIR WAS INSTALLED. 2 L 7 3 4F A23WE 1996071800348 19960718 00348 WP 1996 7 18 DLL13961577 1 19960703 A 3350 337001090 POWER SUPPLY LKHEED 1011 10113851 5265010 WP GALLEY INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 789DL 193A1142 G-CK, OPN78100 OVERHEAD EMERGENCY LIGHTS BATT PACK DOES NOT TEST PROPERLY WITH SW ON PACK, COMES ON BUT GOES DIM IMMEDIA TELY. REPLACED PWR SUPPLY, TEST GOOD PER OPN 78100. 2 L 7 3 4F A23WE 1996071800349 19960718 00349 WP 1996 7 18 DLL13961578 1 19960703 A 3350 337001090 POWER SUPPLY LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 789DL 193A1142 OVERHEAD EMERGENCY LIGHTS BATT PACK ADJACENT TO L4 DOOR DOES NOT TEST PROPERLY WITH SW ON BATT PACK, LIGHTS COMES ON BUT GOES DIM IMMEDIATELY. REPLACED PWR SUPPLY, TEST OK PER OPN 78100. 2 L 7 3 4F A23WE 1996071800350 19960718 00350 WP 1996 7 18 DLL13961644 1 19960701 A 5330 SKIN LKHEED 1011 10113851 5265010 WP R1 DOOR CORNER CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 789DL 193A1142 DURING A LETTER CHECK INSPECTION, A SMALL CRACK WAS FOUND IN THE UPPER AFT CORNER OF THE R1 DOOR. THE CONDITION WILL BE REPAIRED PER L1011 SRM 53-15-00, FIG 806 AND WILL ALSO INCORPORATE PREVIOUSLY ISSUED ER/A 266553-14. 2 L 7 3 4F A23WE 1996071800351 19960718 00351 WP 1996 7 18 DLL13961645 1 19960701 A 5330 SKIN LKHEED 1011 10113851 5265010 WP R1 DOOR CUTOUT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 789DL 193A1142 AN EXISITNG REPAIR WAS REMOVED FOR INSPECTION AND FOUND TO HAVE FURTHER DAMAGE. THIS REPAIR HAS BEEN INCORPORATED INTO ER/A 359868-14. NO FURTHER WORK IS ACCOMPLISHED PER THIS ER/A. 2 L 7 3 4F A23WE 1996071800352 19960718 00352 WP 1996 7 18 DLL14961596 1 19960514 A 5330 SKIN LKHEED 1011 1011385115 5265015 WP BS 1361-1453 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 736DY 193C1227 DURING HMV, THE BELLY SKIN FROM FS 1363 TO 1453 BETWEEN STR 31 AND 32 AND BETWEEN STR 34 AND 35 WAS FOUND TO BE CORRODED . THE CORROSION WAS CUT OUT AND A REPAIR FILLER/DOUBER WAS INSTALLED. 2 L 7 3 4F A23WE 1996071800353 19960718 00353 WP 1996 7 18 DLL14961631 1 19960704 A 3350 5165741 POWER SUPPLY LKHEED 1011 1011385115 5265015 WP L2 DOOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1739D 193C1237 FOUND ON L/O, EMERGENCY EXIT LIGHTS AT L2 DOOR AND LOWER GALLEY INOP. REPLACED EMERGENCY LIGHTS PWR SUPPLY AT L2 DOOR. 2 L 7 3 4F A23WE 1996071800354 19960718 00354 WP 1996 7 18 DLL15961538 1 19960626 A 3230 CONTROL VLV LKHEED 1011 10113853 5265020 WP RT MLG WW FAILED A DALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 27 752DA 193W1172 LOSS C-SYS HYD QTY IMMEDIATELY AFTER LANDING GEAR LOWERED. REPLACED LANDING GEAR PHASE CONTROL VALVE, OPERATED LANDING GEAR AND OPS CKS GOOD. 2 L 7 3 4F A23WE 1996071800355 19960718 00355 WP 1996 7 18 DLL15961558 1 19960629 A 3350 081691 LIGHTS LKHEED 1011 10113853 5265020 WP CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 755DL 193Y1184 ON L/O, FOUND EMERGENCY FLOOR TRACK LIGHTS 1B, 12E, 24G INOP. REPLACED LAMP HOLDERS ON 1B, 12E, 24G, EMERGENCY LIGHTS C K GOOD. 2 L 7 3 4F A23WE 1996071800357 19960718 00357 WP 1996 7 18 DLL16961649 1 19960708 A 3350 5165741 POWER SUPPLY LKHEED 1011 10113853 5265020 WP CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 759DA 193Y1176 AFT LT CEILING EMERGENCY LIGHTS FAIL TO TEST. REPLACED AFT LT POWER SUPPLY, LIGHTS CHECK NORMAL. 2 L 7 3 4F A23WE 1996071800358 19960718 00358 NM 1996 7 18 DLM88961594 1 19960213 A 5330 SKIN DOUG MD88 MD88 3023688 NM C-1 DOOR CUTOUT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 946DL 49819 DURING C-2 CHECK, THE FUSELAGE SKIN AT THE AFT EDGE OF THE C-1 DOOR WAS FOUND WITH AN EXISTING STOP DRILL HOLE. HOLE WA S TRIMMED OUT AND A FILLER/DOUBLER REPAIR WAS INSTALLED. 2 L 7 2 4F RT A6WE 1996071800359 19960718 00359 NM 1996 7 18 DLM88961643 1 19960707 A 3240 26088921 BRAKE DOUG MD88 MD88 3023688 NM NR 1 LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 999DN 53371 IN FLIGHT, LT HYD WENT TO 4 QTS. COMPLETED PROCEDURES, QUANTITY INCREASED. RESTORED SYSTEM ON FINAL, MAINTAINED 4 QUAR TS AND GOOD PRESSURE. FOUND NR 1 BRAKE ASSY LEAKING. REPLACED SAME AND SERVICED HYDRAULICS, NO LEAKS. 2 L 7 2 4F RT A6WE 1996071800360 19960718 00360 WP 1996 7 18 MWEA96260 1 19960710 A 3350 LIGHT DOUG DC9 DC914 3022034 WP CABIN INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 800ME 45842 DURING INSP, FOUND LT AND RT OVERWING WING EMERGENCY LIGHTS INOP. CHANGED AND ARMED THE SYSTEM, OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996071800361 19960718 00361 NM 1996 7 18 P5CA9600348 1 19960707 A 5753 SKIN BOEING 747 747122 1384872 NM RT TE MIDFLAP WORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 RIGHT HAND INBOARD MIDFLAP TRAILING EDGE HAS EXPOSED HONEYCOMB. POTTED SMALL PUNCTURE, APPLIED FILLER AND OVERLAY IAW S RM 51-40-09. 2 L 7 4 4F A20WE 1996071800362 19960718 00362 NM 1996 7 18 P5CA9600349 1 19960707 A 5753 PANEL BOEING 747 747122 1384872 NM LT TE MIDFLAP PUNCTURED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEFT WING INBOARD MIDFLAP INBOARD UPPER STRESS PANEL PUNCTURED. INSTALLED FILLER AND DOUBLER IAW SRM 51-40-06. 2 L 7 4 4F A20WE 1996071800363 19960718 00363 NM 1996 7 18 P5CA9600350 1 19960630 A 3250 COVER BOEING 747 747122 1384872 NM NLG STEERING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 NOSE GEAR STEERING CABLE HOUSING COVER CRACKED. SANDED OUT CRACK, COLD BOND PLY LAYUP BONDED AND SEALED IAW SRM 51-40-0 9. 2 L 7 4 4F A20WE 1996071800364 19960718 00364 NM 1996 7 18 P5CA9600351 1 19960702 A 7110 CHANNEL BOEING 747 747122 1384872 NM NR 3 COWL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 NR 3 INBOARD CORE COWL LOWER EDGE CHANNEL CRACKED AND BENT. REMOVED CHANNEL, FABRICATED CHANNEL AND SPLICE AND INSTALLE D IAW SRM 51-40-03. 2 L 7 4 4F A20WE 1996071800365 19960718 00365 NM 1996 7 18 P5CA9600352 1 19960703 A 5753 69B109211 BOGIE PIN BOEING 747 747122 1384872 NM NR 7 FLAP TRACK PITTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 FOUND NR 7 FLAP TRACK BOGIE PINS PITTED. REMOVED AND REPLACED PINS IAW MM 27-51-04. 2 L 7 4 4F A20WE 1996071800366 19960718 00366 NM 1996 7 18 P5CA9600353 1 19960702 A 5753 65B166206 BRACE BOEING 747 747122 1384872 NM NR 4 TE FLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 FOUND NR 4 MOVEABLE CANOE FORWARD SUPPORT FITTING CRACKED. REMOVED AND REPLACED BRACE IAW MM 27-51-00 AND MM 27-51-45. 2 L 7 4 4F A20WE 1996071800367 19960718 00367 NM 1996 7 18 P5CA9600354 1 19960705 A 5415 69B910541 FITTING BOEING 747 747122 1384872 NM NR 4 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 FOUND NR 4 PYLON FORWARD FAIRING OUTBOARD LATCH 'U' FITTING CRACKED. REMOVED AND REPLACED FORWARD FAIRING RETAINER FITT ING IAW SRM 54-10-03 AND MM 54-32-01. 2 L 7 4 4F A20WE 1996071800368 19960718 00368 NM 1996 7 18 P5CA9600355 1 19960703 A 5753 65B08424202 PANEL BOEING 747 747122 1384872 NM RT TE MIDFLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 RIGHT HAND INBOARD MIDFLAP TOP SURFACE CENTER PANEL HAS LARGE AREAS OF DELAMINATION. REMOVED PANEL AND INSTALLED NEW PA NEL IAW SRM 51-10-01. 2 L 7 4 4F A20WE 1996071800369 19960718 00369 NM 1996 7 18 P5CA9600356 1 19960709 A 5753 COVE PANEL BOEING 747 747122 1384872 NM LT TE MIDFLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEFT WING OUTBOARD MIDFLAP TRAILING EDGE COVE PANEL CRACKED AT MIDPOINT. REMOVED DAMAGED PANEL AND CORE, FABRICATED COR E, FILLER AND DOUBLERS AND INSTALLED IAW SRM 51-40-09 AND 51-40-12. 2 L 7 4 4F A20WE 1996071800370 19960718 00370 NM 1996 7 18 P5CA9600357 1 19960709 A 5753 SKIN BOEING 747 747122 1384872 NM LT TE FOREFLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEFT WING OUTBOARD FOREFLAP HAS PREVIOUS GOUGE AND DELAMINATION AT OUTBOARD LEADING EDGE. REMOVED DAMAGED SKIN, POTTED CORE, FABRICATED FILLER AND DOUBLERS AND INSTALLED IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1996071800371 19960718 00371 NM 1996 7 18 P5CA9600358 1 19960709 A 5753 SKIN BOEING 747 747122 1384872 NM LT TE AFT FLAP PUNCTURED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEFT WING OUTBOARD AFT FLAP UPPER SURFACE HAS SMALL PUNCTURE. REMOVED DAMAGED SKIN, POTTED CORE, FABRICATED FILLER AND DOUBLERS AND INSTALLED REPAIR IAW SRM 51-40-11 AND 51-40-15. 2 L 7 4 4F A20WE 1996071800372 19960718 00372 NM 1996 7 18 P5CA9600359 1 19960710 A 5753 FAIRING BOEING 747 747122 1384872 NM NR 4 FLAP TRACK PUNCTURE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 NR 4 FLAP TRACK CANOE FAIRING HAS PUNCTURE IN LOWER AFT END. REMOVED DAMAGED SKIN, POTTED CORE, FABRICATED FILLER AND D OUBLERS AND INSTALLED REPAIR IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1996071800373 19960718 00373 NM 1996 7 18 P5CA9600360 1 19960703 A 5753 65B141611 SUPPORT BOEING 747 747122 1384872 NM NR 1 TE FLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 NR 1 FLAP TRACK SEQUENCE TOGGLE ROLLER SUPPORT LINK CRACKED. REMOVED AND REPLACED SUPPORT LINK IAW MM 27-51-00. 2 L 7 4 4F A20WE 1996071800374 19960718 00374 NM 1996 7 18 P5CA9600361 1 19960622 A 5340 STOP FITTING BOEING 747 747122 1384872 NM AFT CARGO DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 AFT CARGO DOOR FRAME STRUCK BY PALLET AND DAMAGED DURING LOADING. FOUND WEB DAMAGE AT BS 1820 AT LOWER STOP FITTING, FI TTING CRACKED. REPAIRED WEB AND FITTING IAW SRM 53-10-04. 2 L 7 4 4F A20WE 1996071800375 19960718 00375 NE 1996 7 18 SCNA96188 2 19960706 A 7200 ENGINE BOEING 727 727225 1384077 NM PWA JT8 JT8D15A 52051 NE NR 3 FAILED A A SCNA C D ABORTED TAKEOFF RETURN TO BLOCK Y T ENGINE STOPPAGE ENGINE CASE PENETRATION TO TAKEOFF 1 GL 15 283SC 22559 DURING TAKEOFF ROLL, THE NUMBER THREE ENGINE EXPERIENCED A CONTAINED FAILURE AND ENGINE PARTS WERE REPORTED DEPARTING TH E AIRCRAFT. ABORTED TAKEOFF AND RETURNED TO THE GATE. THE ENGINE WAS REPLACED IN ACCORDANCE WITH MM 71-95-17 AND TRIMM ED IN ACCORDANCE WITH 71-95-18. SHOP FINDINGS WILL BE REPORTED WHEN AVAILABLE. 2 L 7 3 4F 4 F A3WE E2EA 1996071800376 19960718 00376 NM 1996 7 18 SCNA96189 1 19960703 A 5400 S-DUCT BOEING 727 7272J4 1384006 NM NR 2 ENGINE CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 288SC 20765 DURING MAINTENANCE INSPECTION, CORROSION WAS FOUND IN THE INLET OF THE S-DUCT ON ENGINE 2. REMOVED CORROSION, FABRICATE D AND INSTALLED A REPAIR IN ACCORDANCE WITH B727 SRM 54-10-03 FIGURE 8. 2 L 7 3 4F RT A3WE 1996071800377 19960718 00377 WP 1996 7 18 SCNA96190 1 19960703 A 5330 SKIN DOUG DC10 DC1015 3022118 WP BS 890 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING MAINTENANCE INSPECTION, CORROSION WAS FOUND IN THE FUSELAGE SKIN AT BS 890, NEAR STRINGER 44L. CUT OUT CORROSION , FABRICATED AND INSTALLED A REPAIR IN ACCORDANCE WITH SRM 52-20-00. 2 L 7 3 4F A22WE 1996071800378 19960718 00378 NM 1996 7 18 UPS96220599 1 19960710 A 2613 CONNECTOR BOEING 727 72751C 1384015 NM NR 3 ENGINE CHAFED A IPXA E ENGINE SHUTDOWN N FALSE WARNING LD LANDING 1 SO 01 904UP 18946 INSPECTION TYPE N/A, ENG 3 STRUT OVERHEAT LIGHT CAME ON JUST PRIOR TO LANDING. EXTINGUISHED AFTER ENGINE WAS SHUT DOWN. ENGINE SHUTDOWN DURING LANDING ROLL. *S/D* REPAIRED CHAFED WIRE AT FIRE WALL. REMOVED AND REPLACED CONNECTOR ON STA RT STRUT, CONNECTOR ON START STRUT OVERHEAT 1OO DEG IN AFT AIRSTAIR AREA AND OPS CK NORMAL. 2 L 7 3 4F A3WE 1996071800379 19960718 00379 NM 1996 7 18 UPS96420607 1 19960706 A 3350 5136B37 LIGHT BOEING 747 747121 1384871 NM AFT FLGHT DECK INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 691UP 19641 INSPECTION TYPE N/A, ONE OF THE OVERHEAD LIGHTS ON THE AFT FLIGHT DECK IS BURNED OUT, WILL NOT ILLUMINATE WITH THE EMERG ENCY LIGHT SWITCH ON. REMOVED AND REPLACED AFT FLT DECK OVERHEAD EMERGENCY LIGHT PACK, CHECKS OK PER MM 33-51-00 (P/N 5 136B37), (S/N 10006-372) ON, OFF (S/N 18363) OFF. 2 L 7 4 4F A20WE 1996071800380 19960718 00380 WP 1996 7 18 UPS96820608 1 19960701 A 5751 SPAR DOUG DC8 DC871F 302199D WP RT AILERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE N/A, RT INB AILERON, INB AILERON ATTACH HINGE, INB SET OF HOLES 2 HAVE CRACK INDICATIONS. INB HOLES ALL LAYERS CRACKED, 1ST 3 LAYERS INDICATIONS ON INB SIDE, AFT LAYER OUTB SIDE. OUTB HOLE FIRST 2 LAYERS HAVE CRACK INDICAT IONS INB SIDE OF HOLE. OUTB SET OF HOLES, NO CRACKS NOTED. REPAIRED RT I/B AILERON HINGE ATTACH FITTING, I/B SET OF HO LES ON LOWER SPAR IAW REO-02070. TORQUED 6 AILERON STUD MOUNT BOLTS IAW DC8 SRM 51-3-1. INSTALLED WEB IAW DC8 SRM 51-3 -6, 51-1-20D. 2 L 7 4 4F RT 4A25 1996071800381 19960718 00381 NM 1996 7 18 VNAA9607006 1 19960707 A 3244 26107012 TIRE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT MLG FAILED A VNAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 431JS 3028 DURING TAXI OUT, CREW REPORTED THAT BOTH RT MLG TIRES FAILED. CREW WAS UNABLE TO MOVE THE AIRCRAFT. CREW CALLED MX TO THE AIRCRAFT. MX REPLACED BOTH RT MLG WHEEL AND TIRE ASSEMBLIES IAW MM 32-40-00. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996071800382 19960718 00382 EU 1996 7 18 96FDEA01244 1 19960713 A 7931 CIRCUIT BREAKER AIRBUS 300 A300F4605R 3930327 EU CB PANEL TRIPPED A FDEA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SO 25 660FE 759 ON TAKEOFF, RECEIVED ECAM WARNING FOR ADC NR 2 FAULT PITCH TRIM NR 2 TRIPPED YAW DAMP NR 2 TRIPPED, THEN GOT LOW IPIL PR ESS ON NR 2 ENG ECAM AND ANALOG GAUGE WAS ZERO, RETURNED TO LANDING PDX. R7R OIL PRESS TRANSMITTER NO HELP AT ALL. FINA LLY DISCOVERED THE CB CONTROLLING BUSS BAR 231XP POPPED. RESET AND OIL PRESSURE NOW OK AND ALL OTHER ADC SUFF BACK TO N ORMAL. 2 L 7 2 4F RT A35EU 1996071800383 19960718 00383 WP 1996 7 18 96FDEA01245 1 19960713 A 5320 AFA005511 CAP ANGLE DOUG DC10 DC1010CF 3023502 WP BS 1761 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68056 47810 BELL FRAME CORRODED AT BS 1761. REMOVED BELL FRAME AND INSTALLED A NEW BELLFRAME AND SPLICE ANGLE DOUBLER PER SRM 53-40 -00 FIG 1L. 2 L 7 3 4F RT A22WE 1996071800384 19960718 00384 NM 1996 7 18 96FDEA01246 1 19960708 A 5311 6542531 FRAME BOEING 727 72722 1384002 NM BS 540 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 DISCREPANCY: NR 0235 (025) FOUND DENT IN FRAME STA 540 BETWEEN STRINGERS 23 TO 24 LT FORWARD BAY. CORRECTIVE ACTION: R EPAIRED DENT IN FRAME STA 540 BETWEN STR 23 - STR 24L, FWD BAY PER FEDEX SRM 51-40-3. 2 L 7 3 4F A3WE 1996071800385 19960718 00385 NM 1996 7 18 96FDEA01247 1 19960703 A 5330 6518420 SKIN BOEING 727 72722 1384002 NM BS 182-192 LIGHTNING STRIKE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19144 NR 0430, 026, 4 LIGHTNING STRIKES BS 182 TO 192, LT WL 225 TO 227. 2 L 7 3 4F A3WE 1996071800386 19960718 00386 NM 1996 7 18 96FDEA01248 1 19960711 A 5311 652072630 FRAME BOEING 727 72722 1384002 NM BS 540 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 DISCREPANCY: NR 0235 (027) CORROSION ON C-CHANNEL, STATION 532, RBL 26, WL 155. CORRECTIVE ACTION: REPAIRED DENT IN F RAME BS 540 BETWEEN STR 23 AND STR 24L, SRM 51-40-3. 2 L 7 3 4F A3WE 1996071800387 19960718 00387 NM 1996 7 18 96FDEA01249 1 19960712 A 5730 6516286 SKIN BOEING 727 727173C 1384059 NM BS 7604 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 199FE 19509 DISCREPANCY: NR 0593 (017) FRETTING CORROSION AT FUEL CELL CUTOUT 7604 RT WING. CORRECTIVE ACTION: REPAIRED PER FEDEX EA 7-5710-29614. ALSO, CHANGED MODEL FROM 7272D4 TO 727173C AND S/N FROM 21849 TO 19509. 2 L 7 3 4F A3WE 1996071800388 19960718 00388 NM 1996 7 18 96FDEA01250 1 19960712 A 5730 657271311 SKIN BOEING 727 7272D4 138407U NM BS 825 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 287FE 21849 NR 0462, 015 CORROSION (C53-224-05) UPPER EXTERIOR SKIN ON CENTER WING FUEL TANK BS 825 RBL 65, WL 199. *S/D* REPAIRED UPPER EXTERIOR SKIN ON CENTER WING FUEL TANK AT BS 825 RBL 65 WL 199 PER FEDEX EA NR 7-5710-29704. 2 L 7 3 4F A3WE 1996071800389 19960718 00389 NM 1996 7 18 96FDEA01251 1 19960712 A 5313 655848817 STRINGER BOEING 727 7272D4 138407U NM BS 945-950 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 287FE 21849 DISCREPANCY: NR 0430 (016) WHILE WORKING 7-5310-7-432913 PT3 CORRECTIVE ACTION: ****S/D**** REPAIRED STR 18A AT BS 945 - 950, LBL 67, WL 109 PER EA 7-5310-29607. 2 L 7 3 4F A3WE 1996071800390 19960718 00390 NM 1996 7 18 96FDEA01252 1 19960712 A 5320 HFAB5351011 SHEAR TIE BOEING 727 7272D4 138407U NM BS 700 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 287FE 21849 DISCREPANCY: NR 0155 (017) CORROSION (C53-113-01(1) IN THE FWD CARGO BAY ON FRAME SHEAR TIE BS 700, WL 148, LBL 10. CO RRECTIVE ACTION: ***S/D *** REMOVED OLD SHEAR TIE BS 700, WL 148, LBL 10. FABRICATED AND INSTALLED NEW SHEAR TIE BS 7 00 PER SRM 51-20-01. 2 L 7 3 4F A3WE 1996071800391 19960718 00391 NM 1996 7 18 96FDEA01253 1 19960715 A 5313 65271325 STRINGER BOEING 727 72722 1384002 NM BS 459 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 DISCREPANCY: NR 0222 (028) CORROSION (C53-111-01 (2) ON STR FLANGE, STR 23 RT, STA 489 RT, FORWARD BAY. CORRECTIVE AC TION: REPAIRED STR AT BS 489, STR 23R PER FEDEX SRM 53-10-3, FIG 2. 2 L 7 3 4F A3WE 1996071800392 19960718 00392 NM 1996 7 18 96FDEA01254 1 19960715 A 5315 65208277 FLOORBEAM BOEING 727 72722 1384002 NM BS 680 GOUGE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 DISCREPANCY: NR 0245 (029) FOUND GOUGES IN FLOORBEAM, STR 680 RBL 25, LBL 25 WL 198 (FORWARD BAY). CORRECTIVE ACTION: BLENDED GOUGES, ONE WAS OUT OF LIMITS IN FLOOR BEAM STA 600 RBL 4.75 WL 198 PER FEDEX SRM 53-10-1. REMOVED DAMAGED AR EA, FABRICATED REPAIR PARTS, ALODINED AND PRIMED REPAIR PARTS. INSTALLED REPAIR PARTS PER FEDEX SRM 53-10-8. 2 L 7 3 4F A3WE 1996071800393 19960718 00393 NM 1996 7 18 96FDEA01255 1 19960715 A 5320 65208277 SHEAR TIE BOEING 727 72722 1384002 NM BS 540 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 DISCREPANCY: NR 0225 (030) CORROSION ON SHEAR TIE STA 540 LT BETWEEN STR 24-25, LT FORWARD BAY. CORRECTIVE ACTION: RE PAIRED SHEAR TIE, STA 540 LT BETWEEN STR 24-25 LT PER SRM 53-10-4. 2 L 7 3 4F A3WE 1996071800394 19960718 00394 NM 1996 7 18 96FDEA01256 1 19960715 A 5320 65207282 SHEAR TIE BOEING 727 72722 1384002 NM BS 540 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 DISCREPANCY: NR 0225 (031) CORROSION ON SHEAR TIE STA 540 LT BETWEEN STR 24-25 LT FWD BAY. CORRECTIVE ACTION: *****S/ D*****. 2 L 7 3 4F A3WE 1996071800395 19960718 00395 NM 1996 7 18 CALA9601007 1 19960608 A 5330 SKIN BOEING 737 737217 1384464 NM BS 1020-1044 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12231 19885 INSPECTION FOUND FUSELAGE SKIN DENTED BETWEEN STA 1020 AND 1044, STRINGER 25R. THE DENTED AREA WERE CUT OUT IAW SRM 53- 30-8. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 AND 51-30-2. 2 L 7 2 4F A16WE 1996071800396 19960718 00396 NM 1996 7 18 CALA9601008 1 19960608 A 5330 SKIN BOEING 737 737217 1384464 NM BELOW R1 DOOR GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12231 19885 INSPECTION FOUND A GOUGE IN FUSELAGE SKIN BELOW R-1 DOOR AT STRINGER 18R. THE GOUGED AREA WAS CUT OUT IAW SRM 53-30-3. A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. 2 L 7 2 4F A16WE 1996071800397 19960718 00397 NM 1996 7 18 CALA9601009 1 19960609 A 5730 SKIN BOEING 737 737217 1384464 NM WBL 165 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12231 19885 INSPECTION FOUND A 3 INCH CRACK IN RT WING UPPER SURFACE SKIN AT REAR SPAR, WBL 165, AFT OF INBOARD DRY BAY PANEL. THE CRACKED SECTION WAS CUT OUT AND A DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5730-01449. 2 L 7 2 4F A16WE 1996071800398 19960718 00398 NM 1996 7 18 CALA9601010 1 19960626 A 5330 SKIN BOEING 737 737217 1384464 NM WINDOW BELT DISBONDING A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12231 19885 INSPECTION FOUND ONE AREA OF RT WINDOW BELT SKIN DISBONDING. THE WINDOW BELT SKIN WAS REPAIRED IAW SRM 53-30-08. 2 L 7 2 4F A16WE 1996071800399 19960718 00399 NM 1996 7 18 CALA9601011 1 19960610 A 5330 SKIN BOEING 737 737217 1384464 NM BS 188-251 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12231 19885 INSPECTION FOUND A .5 INCH CRACK IN LT FUSELAGE SKIN BETWEEN BS 188 AND 251, WL 207 TO 234. THE CRACKED AREA WAS CUT OU T, DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW EA 5310-01188. 2 L 7 2 4F A16WE 1996071800400 19960718 00400 NM 1996 7 18 CALA9601012 1 19960626 A 5330 SKIN BOEING 737 737217 1384464 NM BS 188-251 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12231 19885 INSPECTION FOUND A 1.75 INCH AND 5.75 INCH CRACK IN RT FUSELAGE SKIN BETWEEN BS 188 AND 251, WL 207 TO 234. THE CRACKED AREA WAS CUT OUT. A FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW EA 5310-01188. 2 L 7 2 4F A16WE 1996071800401 19960718 00401 NM 1996 7 18 CALA9601013 1 19960620 A 5320 WEB BOEING 737 737217 1384464 NM BS 358 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12231 19885 INSPECTION FOUND A 1.5 INCH CRACK IN WEB AT STA 358, STRINGER 17L. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW 51-4 0-3, 51-10-2 AND 53-10-2. 2 L 7 2 4F A16WE 1996071800402 19960718 00402 NM 1996 7 18 CALA9601014 1 19960627 A 5315 FLOOR BEAM BOEING 737 737217 1384464 NM BS 675-685 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12231 19885 INSPECTION FOUND FLOOR BEAM LOWER CHORD AND TRANSVERSE BEAM CRACKED AT STA 675, BL 0. THE TRANSVERSE BEAM AT STA 685, B L 0 WAS ALSO CRACKED. THE BEAMS WERE REPAIRED IAW ECRA 5710-01740 AND SRM 51-40-4. 2 L 7 2 4F A16WE 1996071800404 19960718 00404 WP 1996 7 18 CALA9601016 1 19960714 A 2433 6RW176YN3 TRANS RECT DOUG DC9 DC981 3022081 WP FWD E/E COMPT INOPERATIVE A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 13881 22085 803 48045 AN ELECTRICAL ODOR WAS MOMENTARILY OBSERVED IN THE FORWARD GALLEY WHILE IN FLIGHT. UPON INVESTIGATION THE RIGHT DC TRAN SFER RELAY WAS FOUND TRIPPED AND THE RIGHT DC LOAD METER READ ZERO. THE TRANSFER CIRCUIT BREAKER WAS NOT RESET AND THE ODOR WENT AWAY. THE AIRCRAFT LANDED AT EWR WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND THE RIGHT NR 1 TRANSFORMER RECTI FIER AT FAULT. THE TRANSFORMER RECTIFIER WAS REMOVED AND REPLACED. 2 L 7 2 4F A6WE 1996071800405 19960718 00405 NM 1996 7 18 CALA9601017 1 19960713 A 3244 TIRE BOEING 737 737130 1384435 NM RT MLG FAILED A CALA O OTHER O OTHER TO TAKEOFF 1 SW 09 33202 19019 A LOUD BANG WAS HEARD AFTER TAKEOFF, WHILE CLIMBING THROUGH 3,000 FEET. THE FLIGHT CONTINUED TO BOS WHERE IT LANDED SAF ELY. MAINTENANCE FOUND THAT THE NR 3 TIRE HAD BLOWN RESULTING IN DAMAGE TO RT OUTBOARD SIDE OF WHEEL WELL. THE RT I/B FLAP TRACK FAIRING AND THREE HYDRAULIC LINES WERE ALSO DAMAGED. THE RT O/B SIDE OF WHEEL WELL WAS REPAIRED IAW ECRA 535 0-01273. THE RT I/B FLAP TRACK FAIRING WAS REPLACED IAW MM 27-51-141, FIGURE 401. THE THREE DENTED HYDRAULIC LINES WER E REMOVED AND REPLACED. IN ADDITION, THE NR 3 MAIN TIRE ASSEMBLY WAS REPLACED. THE NR 3 BRAKE AND NR 4 MAIN TIRE ASSEM BLY WERE REMOVED AND REPLACED AS A PRECAUTION. 2 L 7 2 4F A16WE 1996071800406 19960718 00406 1996 7 18 COMA9610223 4 19960712 A 3452 6226523005 CONTROLLER EMB 120 EMB120RT SO AVIONICS BAY FAILED A COMA D RETURN TO BLOCK O OTHER CL CLIMB 1 SO 01 247CA 120225 TRANSPONDER NR 1 AND NR 2 REPORTED INOPERATIVE BY AIR TRAFFIC CONTROL. REPLACED CTL-92. 2 L 7 2 4T RT A31SO 1996071800407 19960718 00407 SW 1996 7 18 COMA9620012 1 19960712 A 3260 IEN516 DOWNLOCK SWITCH SWRNGN SA227 SA227AC 8780603 SW RT MLG FAILED A COMA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 702M AC703 THE RIGHT MLG WOULD NOT INDICATE DOWN AND LOCKED UNTIL CYCLED 3 TIMES. REPLACED THE RIGHT MLG OUTBOARD DOWNLOCK SWITCH. 2 L 7 2 4T RT A8SW 1996071800408 19960718 00408 EA 1996 7 18 COMA9660119 1 19960713 A 3260 16227101 SPRING CNDAIR CL600 CL6002B19 EA NLG BINDING A COMA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 940CA 7048 RECEIVED GEAR DISAGREE AND NOSE DOORS MESSAGE WHEN GEAR WAS SELECTED DOWN, GEAR LOWERED 1 MIN AFTER GO-AROUND. ADJUSTED NOSE GEAR DOWNLOCK ASSIST SPRING TO ALLOW MOVEMENT AT SPRING PIVOT POINTS. 2 L 7 2 4F RT A21EA 1996071800409 19960718 00409 NM 1996 7 18 P5CA9600362 1 19960711 A 2810 COUPLING BOEING 747 747132 1384882 NM NR 2 PYLON LOOSE A P5CA K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 WP 23 857FT 20246 DURING MAINTENANCE, FOUND FUEL LEAK INBOARD NR 2 PYLON. INSPECTED DRY BAY AREA ABOVE NR 2 PYLON PER MM 28-11-00. FOUND FUEL FEED MANIFOLD COUPLING LOOSE AT SPAR. TIGHTENED AND SECURED COUPLING, PRESSURE CHECK GOOD. 2 L 7 4 4F A20WE 1996071800410 19960718 00410 NM 1996 7 18 P5CA9600363 1 19960713 A 3244 260190260 TIRE BOEING 747 747122 1384872 NM NR 2/3 MLG BLOWN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 NR 2 AND 3 MAIN TIRES FOUND BLOWN ON ARRIVAL. NR 1 MAIN TIRE HAD FLAT SPOT AND THERMAL RELIEF AT BLOCKS. NR 4 MAIN TIR E HAD FLAT SPOT BUT RETAINED AIR. REMOVED AND REPLACED NR 1, 2, 3, 4 WHEEL ASSEMBLIES IAW MM 32-45-01. REMOVED AND REP LACED NR 4 BRAKE ASSEMBLY DUE TO BROKEN DISC FOUND WHEN WHEEL ASSEMBLY REMOVED, IAW MM 32-41-15. COMPLIED WITH BLOWN TI RE INSPECTION PER MM 5-51-34, ANTI-SKID BITE CHECKS NORMAL. 2 L 7 4 4F A20WE 1996071800411 19960718 00411 NE 1996 7 18 P5CA9600364 2 19960527 A 7250 TURBINE EXH BOEING 747 747124 1384874 NM PWA JT9 JT9D7A 52054 NE NR 3 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 695757 NR 3 ENGINE 'R' AND 'S' RAILS CRACKED IN PREVIOUS WELDED AREAS AT 12 O'CLOCK POSITION. THE 'S' FLANGE CLEVIS PIN HAS PI NHOLE CRACK, THE 'R' FLANGE 12 O'CLOCK RACETRACK SLOT RADIAL CRACK TO RAIL. INSPECTED TURBINE EXHAUST CASE AT 1,000 HR INTERVALS FOLLOWING DISCOVERY OF INITIAL CRACK INDICATION TO ENSURE ABOVE LIMITS HAVE NOT BEEN EXCEEDED. 2 L 7 4 4F 4 F A20WE E20EA 1996071800412 19960718 00412 SO 1996 7 18 SRAA960703 1 19960715 A 2841 FUEL QTY IND LKHEED 382 382B 5264104 SO NR 1/2 INOPERATIVE A SRAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 916SJ 4134 AFTER TAKEOFF, FOUND NR 1 AND 2 FUEL QUANTITY INOP ALONG WITH ALL FUEL FLOW INDICATIONS. ACCOMPLISHED AIR TURNBACK AND LANDED WITHOUT INCIDENT, ITEM IS UNDER INVESTIGATION. 2 H 7 4 4T A1SO 1996071800413 19960718 00413 NE 1996 7 18 TC8A96047 2 19960627 A 7320 PS4 LINE DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3B 52039 NE NR 4 ENGINE LOOSE A TC8A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 181SK 45910 669585 ADVANCING NR 4 THROTTLE FOR T/O, COULD ONLY REACH 75 PERCENT N1 89.5 PERCENT N2 AND EPR OF 1.24. FOUND PS4 LINE LOOSE, TIGHTENED AND SECURED, OPS CKD ASPER MM 71-00 NORMAL. 2 L 7 4 4F 4 F 4A25 1E8 1996071800414 19960718 00414 WP 1996 7 18 TC8A96048 1 19960627 A 7603 3766216505 THROTTLE DRUM DOUG DC8 DC8F55 3021928 WP PWA JT3D JT3D3B 52039 NE NR 2 ENGINE LACK OF LUBE A TC8A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 808CK 45817 645142 NR 2 POWER LEVER BINDING, ENGINE WOULD NOT DEVELOP MAX POWER. CLEANED AND LUBED THROTTLE DRUM, OPS CHECK NORMAL AT ALL POWER SETTINGS IAW 71-00. 2 L 7 4 4F 4 F 4A25 1E8 1996071800416 19960718 00416 SO 1996 7 18 96ZZZX3548 1 19960624 A 3246 16203500 WHEEL PARKERHANFIN PIPER PA31 PA31350 7103110 SO RT MLG BROKEN A S APCA K NONE O OTHER IN INSP/MAINT 1 NM 01 36PB 12210 317405128 A 6 INCH PIECE OF THE OUTBOARD WHEEL HALF WAS FOUND BROKEN OFF. 1 L 7 2 3O A20SO 1996071800444 19960718 00444 WP 1996 7 18 9615069955 1 19960712 A 3350 60030451 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN MALFUNCTIONED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 922RW 47182 DURING LINE MAINTENANCE, EMERGENCY LIGHTS OVER ROWS 12, 14 AND AFT OVERWING EXITS INOPERATIVE. REPLACED BATTERY PACKS F OR OVERWING EXIT AND CEILING EMERGENCY LIGHTS, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996071800445 19960718 00445 1996 7 18 9615072761 4 19960713 A 3442 20412151102 RADAR INDICATOR BOEING 727 7272M7 138407S NM COCKPIT FAILED A NWAA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 01 721RW 21200 DURING CRUISE, AIRCRAFT WEATHER RADAR BECAME INOPERATIVE. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLAC ED RADAR INDICATOR AND PERFORMED SYSTEM TEST, CHECKED OK. 2 L 7 3 4F A3WE 1996071800446 19960718 00446 NE 1996 7 18 9615086637 2 19960713 A 7230 COMPRESSOR BOEING 747 747251B 1384892 NM PWA JT9 JT9D7R4G2 52054 NE NR 2 ENGINE STALLED A NWAA O OTHER R PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 01 637US 23548 15244 DURING CLIMB, THE NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL. WITH NO SPIKE IN EGT AND ALL ENGINE INDICATIONS BEING NOR MAL, CREW FOLLOWED COM PROCEDURES AND CONTINUED TO AMS WITHOUT FURTHER INCIDENT. BORESCOPE INSPECTION OF HIGH PRESSURE COMPRESSOR REVEALED NO DISCREPANCIES. EVBC REPLACEMENT AND PRECISION TRIM OF EVBC/FUEL CONTROL WILL BE DONE WITHIN FIVE CYCLES. 2 L 7 4 4F 4 F A20WE E3NE 1996071800447 19960718 00447 1996 7 18 9615096631 4 19960713 A 2211 788270002 GYRO BOEING 747 747251B 1384892 NM E/E COMPT MALFUNCTIONED A NWAA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 01 631US 23111 DURING CRUISE, THE AIRCRAFT EXPERIENCED A SUDDEN ROLL AND PITCH UP CONDITION. AIRCRAFT DIVERTED TO ANC AND LANDED WITHO UT FURTHER INCIDENT. REPLACED THE NR 1 INERTIAL NAVIGATION SYSTEM COMPUTER AND AUTO-PILOT ROLL COMPUTER. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996071800448 19960718 00448 WP 1996 7 18 9615109302 1 19960710 A 3350 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 302RC 48055 DURING LINE CHECK, FOUND SEVERAL TAIL INTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY POWER SUPPLY PACK AT B5-2 8, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996071800449 19960718 00449 WP 1996 7 18 9615111162 1 19960713 A 2934 VT0107F TRANSMITTER DOUG DC10 DC1040 3023508 WP NR 2 HYD SYS LEAKING A NWAA A J UNSCHED LANDING DUMP FUEL K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 162US 44629 4753 46771 DURING CLIMB, THE NR 2 HYDRAULIC SYSTEM SHOWED A SLOW LEAK. RETURNED TO HNL, DUMPED 38,000 LBS OF FUEL AND LANDED WITHO UT INCIDENT. MAINTENANCE REPLACED THE NR 2 PRESSURE TRANSMITTER. 2 L 7 3 4F A22WE 1996071800450 19960718 00450 WP 1996 7 18 9615121227 1 19960713 A 3620 CONNECTOR DOUG DC10 DC1030 3023501 WP NR 2 PNEU SYST DIRTY A NWAA A J UNSCHED LANDING DUMP FUEL N FALSE WARNING CR CRUISE 1 GL 01 227NW 46969 DURING CRUISE, THE NR 2 PNEUMATIC TEMPERATURE HIGH LIGHT ILLUMINATED. DIVERTED TO NRT, DUMPED 100,000 LBS OF FUEL AND L ANDED WITHOUT INCIDENT. MAINTENANCE CLEANED INDICATOR TEMPERATURE SENSOR CANNON PLUG. 2 L 7 3 4F A22WE 1996071800451 19960718 00451 WP 1996 7 18 9615139926 1 19960713 A 3397 WIRE DOUG DC9 DC932 3022066 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 926NW 47425 DURING LINE MAINTENANCE INSPECTION, FOUND AFT STAIRWELL EMERGENCY LIGHTS INOPERATIVE. REPAIRED BROKEN WIRES L795G18 AND L795K18 AT FEED THROUGH P3-13, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996071800452 19960718 00452 WP 1996 7 18 9615149941 1 19960712 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 3324L 47103 DURING PERIODIC CHECK, FOUND FORWARD AND AFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONA L CHECK NORMAL. 2 L 7 2 4F A6WE 1996071800453 19960718 00453 WP 1996 7 18 9615159978 1 19960712 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9342 47391 DURING LINE MAINTENANCE INSPECTION, FOUND AFT EMERGENCY LIGHTS IN TAILCONE INOPERATIVE. REPLACED BATTERY PACK AND SECUR ED LOOSE PIN AT CHARGER ASSEMBLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996071800454 19960718 00454 WP 1996 7 18 9615169980 1 19960713 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9344 47440 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD OVERHEAD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES AND P OWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996071800455 19960718 00455 WP 1996 7 18 9615179609 1 19960714 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 609NW 47234 DURING LINE MAINTENANCE INSPECTION, FOUND CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES AT ROWS 1 TO 4 AND ROW S 14 TO 17, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996071800456 19960718 00456 WP 1996 7 18 9615189150 1 19960713 A 2420 914F5674 RELAY DOUG DC9 DC914 3022034 WP LT GENERATOR FAILED A NWAA O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION AP APPROACH 1 GL 01 8908E 53791 7516 45749 DURING APPROACH, ALL COCKPIT LIGHTS BEGAN FLASHING ACCOMPANIED BY LEFT GENERATOR OFF, LEFT AC BUS OFF AND CROSSTIE LOCKO UT ANNUNCIATOR LIGHTS FLASHING RAPIDLY. LEFT GENERATOR WAS TURNED OFF AND APU WAS STARTED TO POWER LEFT BUS. CREW REQU ESTED EMERGENCY EQUIPMENT ON STANDBY AS A PRECAUTION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUN D THAT THE LEFT GENERATOR WOULD NOT COME ON LINE. REPLACED THE LEFT AC GENERATOR POWER RELAY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996071800457 19960718 00457 WP 1996 7 18 9615199905 1 19960713 A 2750 ST12BC TRANSMITTER DOUG DC9 DC931 3022065 WP RT TE FLAP MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 955N 2893 212 47160 STALL WARNING INDICATION FAILURE LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. M AINTENANCE REPLACED RIGHT FLAP POSITION TRANSMITTER, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996071800458 19960718 00458 WP 1996 7 18 9615209611 1 19960712 A 3260 SWITCHES DOUG DC9 DC932 3022066 WP MLG DOOR FAILED A NWAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 01 611NW 47435 LANDING GEAR DOOR OPEN LIGHT ILLUMINATED IN CRUISE FLIGHT. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTEN ANCE REPLACED BOTH LEFT AND RIGHT GEAR DOOR SWITCHES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996071800459 19960718 00459 NE 1996 7 18 ABXA9600594 2 19960712 A 7321 71128726 FCU DOUG DC8 DC861 3021952 WP PWA JT3D JT3D3B 52039 NE NR 4 ENGINE DEFECTIVE A ABXA C D ABORTED TAKEOFF RETURN TO BLOCK X ENGINE FLAMEOUT TO TAKEOFF 1 GL 23 852AX 2780 46016 669523 NR 4 ENGINE FLAMED OUT DURING TAKEOFF ROLL. REPLACED FUEL TEMPERATURE PROBE, FUEL CONTROL UNIT AND FUEL PUMP FILTERS. C HECKED FUEL CONTROL UNIT LINKAGE AND RIGGING. CHECKED RIGGING OF EMERGENCY SHUTOFF VALVE. CHECKED PS4 LINE AND BORESCO PED ENGINE. REPLACED MAIN FUEL PUMP FOR PRECAUTIONARY MEASURES. GROUND RAN ENGINE AND NO DEFECTS WERE NOTED. 2 L 7 4 4F 4 F 4A25 1E8 1996071800460 19960718 00460 NM 1996 7 18 CALA9601018 1 19960621 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 951 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70353 23591 INSPECTION FOUND INTERCOSTAL CORRODED AT BS 951, LBL 20. THE INTERCOSTAL WAS REPLACED IAW ECRA 5310-03298. 2 L 7 2 4F RT A16WE 1996071800461 19960718 00461 NM 1996 7 18 CALA9601019 1 19960620 A 5320 WEB BOEING 737 7373T0 1384582 NM BS 1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70353 23591 INSPECTION FOUND LEFT AND RIGHT AFT LAV FLOOR WEB CORRODED FROM STA 1016 TO AFT PRESSURE BULKHEAD. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-20-2. 2 L 7 2 4F RT A16WE 1996071800462 19960718 00462 NM 1996 7 18 CALA9601020 1 19960621 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM BS 1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70353 23591 INSPECTION FOUND THREE LEFT AFT LAV FLOOR SUPPORTS CORRODED AT STA 1016. FLOOR SUPPORTS WERE FABRICATED AND INSTALLED I AW BOEING DRAWING NR 65-46812. 2 L 7 2 4F RT A16WE 1996071800463 19960718 00463 NM 1996 7 18 CALA9601021 1 19960620 A 5320 ANGLE BOEING 737 7373T0 1384582 NM BS 945-1000 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70353 23591 INSPECTION FOUND R-2 DOOR FLOOR THRESHOLD Z-ANGLE CORRODED AT STA 945 TO 1000. THE ANGLE WAS REPLACED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 1996071800464 19960718 00464 NM 1996 7 18 CALA9601022 1 19960620 A 5320 ANGLE BOEING 737 7373T0 1384582 NM BS 945-1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70353 23591 INSPECTION FOUND L-2 DOOR FLOOR THRESHOLD Z-ANGLE CORRODED AT STA 945 TO 1016. THE ANGLE WAS REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 1996071800465 19960718 00465 NM 1996 7 18 CALA9601023 1 19960621 A 5320 WEB BOEING 737 7373T0 1384582 NM BS 1006-1026 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70353 23591 INSPECTION FOUND FLOOR WEB SUPPORT CORRODED AT STA 1006 TO 1026. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-20-2. 2 L 7 2 4F RT A16WE 1996071800466 19960718 00466 NM 1996 7 18 CALA9601024 1 19960621 A 5320 WEB BOEING 737 7373T0 1384582 NM BS 986-1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70353 23591 INSPECTION FOUND RIGHT AFT LAV OUTBOARD FLOOR WEB CORRODED AT STA 986 TO 1016. THE WEB WAS REPLACED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 1996071800467 19960718 00467 NM 1996 7 18 CALA9601025 1 19960620 A 5315 FLOOR BEAM BOEING 737 7373T0 1384582 NM BS 312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70353 23591 INSPECTION FOUND FLOOR BEAM CORRODED AT BS 312. DOUBLERS WERE INSTALLED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 1996071800468 19960718 00468 NM 1996 7 18 CALA9601026 1 19960621 A 5315 FLOOR BEAM BOEING 737 7373T0 1384582 NM BS 986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70353 23591 INSPECTION FOUND FLOOR BEAM UPPER CHORD CORRODED AT STA 986. THE CORRODED CHORD WAS REMOVED AND A NEW CHORD WAS FABRICA TED AND INSTALLED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 1996071800469 19960718 00469 NM 1996 7 18 CALA9601027 1 19960621 A 5320 ANGLE BOEING 737 7373T0 1384582 NM BS 344-360 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70353 23591 INSPECTION FOUND Z-ANGLE CORRODED BETWEEN BS 344 AND 360. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 1996071800470 19960718 00470 NM 1996 7 18 CALA9601028 1 19960620 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 294-312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70353 23591 INSPECTION FOUND INTERCOSTAL CORRODED AT BS 294 TO 312. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS FABRICATE D AND INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F RT A16WE 1996071800471 19960718 00471 NM 1996 7 18 CALA9601029 1 19960620 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 312-328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70353 23591 INSPECTION FOUND INTERCOSTAL CORRODED AT BS 312 TO 328. THE INTERCOSTAL WAS REPLACED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 1996071800472 19960718 00472 NM 1996 7 18 CALA9601030 1 19960620 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 328-344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70353 23591 INSPECTION FOUND INTERCOSTAL CORRODED AT BS 328 TO 344. A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW ECRA 5310-03 298. 2 L 7 2 4F RT A16WE 1996071800473 19960718 00473 NM 1996 7 18 CALA9601031 1 19960620 A 5320 ANGLE BOEING 737 7373T0 1384582 NM R1 DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70353 23591 INSPECTION FOUND Z-ANGLE AT R-1 DOOR CORRODED. THE ANGLE WAS REPLACED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 1996071800474 19960718 00474 NM 1996 7 18 CALA9601032 1 19960621 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 993 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70353 23591 INSPECTION FOUND THE RIGHT AFT LAV WALL FLOOR SUPPORT INTERCOSTAL CORRODED AROUND SCREW HOLES AT STA 993. A FLOOR SUPPO RT WAS INSTALLED IAW SRM 51-10-02 AND 5310-03298. 2 L 7 2 4F RT A16WE 1996071800475 19960718 00475 NM 1996 7 18 CALA9601033 1 19960621 A 5315 FLOOR BEAM BOEING 737 7373T0 1384582 NM BS 947.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70353 23591 INSPECTION FOUND AFT CABIN FLOOR BEAM CHORD AT STA 947.5 CORRODED AROUND SCREW HOLES NEAR CENTERLINE. THE CHORD WAS REM OVED AND REPLACED IAW SRM 53-00-51. 2 L 7 2 4F RT A16WE 1996071800476 19960718 00476 NM 1996 7 18 CALA9601034 1 19960621 A 5315 FLOOR BEAM BOEING 737 7373T0 1384582 NM BS 344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70353 23591 INSPECTION FOUND FLOOR BEAM CORRODED AT SCREW HOLES, STA 344. THE CORRODED AREA WAS CUT OUT AND A FLOOR BEAM WAS INSTAL LED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 1996071800477 19960718 00477 NM 1996 7 18 CALA9601035 1 19960620 A 5315 FLOOR BEAM BOEING 737 7373T0 1384582 NM BS 328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70353 23591 INSPECTION FOUND CORROSION ON FLOOR BEAM AT BS 328, RBL 18. THE CORRODED AREA WAS CUT OUT, A CHORD REPAIR INSTALLED IAW SRM 53-10-51, FIGURE 205. 2 L 7 2 4F RT A16WE 1996071800478 19960718 00478 SO 1996 7 18 COMA9610224 1 19960711 A 2750 FLAP WARNING EMB 120 EMB120RT SO TE FLAP SYST ACTIVATED A COMA K NONE O OTHER LD LANDING 1 SO 01 152CA 120152 FLAP CONTROL FAULT WARNING AFTER LANDING. INSPECTED FLAP SYSTEM AND FOUND TO OPERATE NORMALLY. COULD NOT DUPLICATE DIS CREPANCY. 2 L 7 2 4T RT A31SO 1996071800479 19960718 00479 NE 1996 7 18 COMA9610225 2 19960711 A 7313 3035191 FUEL NOZZLE EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE LEAKING A COMA K NONE K FLUID LOSS NR NOT REPORTED 1 SO 01 247CA 120225 FUEL LEAKING FROM RT ENGINE NACELLE. REPLACED THE RT ENGINE FUEL NOZZLES. 2 L 7 2 4T 4 T RT A31SO E20NE 1996071800480 19960718 00480 EU 1996 7 18 COMA9630137 1 19960709 A 6120 8210163C OVER SPEED GOV SAAB SF340 SF340A 7850100 EU RT PROPELLER MALFUNCTION A COMA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SO 01 356CA 340A034 RT ENGINE PROPELLER OVER SPEED TEST FUNCTION IN INOP. REPLACED THE PROPELLER OVER SPEED GOVERNOR. 2 L 7 2 4T RT A52EU 1996071800481 19960718 00481 EA 1996 7 18 COMA9660120 1 19960711 A 5297 601R57689101 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR BROKEN A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 912CA 7011 DOOR INDICATION CIRCUIT BREAKER TRIPPED WHEN POWER ADVANCED FOR TAKEOFF. REPLACED THE CARGO DOOR WARNING SYSTEM WIRING HARNESS. 2 L 7 2 4F RT A21EA 1996071800482 19960718 00482 EA 1996 7 18 COMA9660121 1 19960711 A 2751 601R930301 FLAP POS SENSOR CNDAIR CL600 CL6002B19 EA LT TE FLAP MALFUNCTION A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 951CA 7091 HYDRAULIC PUMP 3B AND 2B FAIL CAUTION MESSAGE ON EICAS. FLAP INDICATION WENT FROM GREEN TO WHITE. REPLACED THE LT FLAP POSITION SENSOR. 2 L 7 2 4F RT A21EA 1996071800483 19960718 00483 EA 1996 7 18 COMA9660122 1 19960711 A 2910 NAS1602904 HYD SEAL CNDAIR CL600 CL6002B19 EA LT MLG LEAKING A COMA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 937CA 7044 HYDRAULIC FLUID LEAK AT LT MLG. REPLACED THE QUICK DISCONNECT SEAL AT THE LT I/B BRAKE HYDRAULIC LINE. 2 L 7 2 4F RT A21EA 1996071800484 19960718 00484 NM 1996 7 18 P5CA9600365 1 19960713 A 5730 FASTENER BOEING 747 747132 1384882 NM LT/RT WING SHEARED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 INSPECTION PER AD 95-02-15 SB 57A2266, FOUND 49 SHEARED FASTENERS AT RIGHT WING FRONT SPAR FS 575.81 TO 684.18, AND 36 SHEARED FASTENERS AT LEFT WING FRONT SPAR FS 575.81 TO 668.18. PERFORMED HFEC INSPECTION, NO CRACKS FOUND. MODIFIED AN D INSTALLED FASTENERS PER SB 57A2266. 2 L 7 4 4F A20WE 1996071800485 19960718 00485 NM 1996 7 18 SCNA96191 1 19960711 A 3350 90052 POWER SUPPLY BOEING 727 7272J4 1384006 NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 288SC 29765 THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND INOP. REPLACED BATTERY POWER SUPPLY ASSEMBLY AND OPS CHECKED OK. 2 L 7 3 4F RT A3WE 1996071800486 19960718 00486 1996 7 18 SWAA960648 4 19960710 A 2210 4030952906 YAW DAMPER BOEING 737 7373H4 1384600 NM AUTO-PILOT MALFUNCTIONED A SWAA O OTHER F FLT CONT AFFECTED CL CLIMB 1 SW 07 395SW 27689 EN ROUTE, EXPERIENCED UNCOMMANDED YAW INPUT AFTER TAKEOFF. CREW CONTINUED AND LANDED WITHOUT INCIDENT AT OAK. REPLACED YAW DAMPER AND RUDDER PCU PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996071800487 19960718 00487 NM 1996 7 18 SWAA960649 1 19960714 A 8012 97910231 START VALVE BOEING 737 7372H4 138448C NM NR 1 MALFUNCTIONED A SWAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SW 07 64SW 22062 EN ROUTE, NUMBER 1 ENGINE START VALVE LIGHT ILLUMINATED. PERFORMED ENGINE SHUTDOWN AS PRECAUTIONARY. LANDED WITHOUT IN CIDENT AT HOU. REPLACED ENGINE START PRESSURE SWITCH, START VALVE AND OPERATION CHECKED PER BOEING M/M. 2 L 7 2 4F A16WE 1996071800488 19960718 00488 NM 1996 7 18 SWAA960650 1 19960710 A 3350 6104789 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 82SW 22731 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F A16WE 1996071800489 19960718 00489 NM 1996 7 18 SWAA960651 1 19960711 A 5330 SKIN BOEING 737 7372H4 138448C NM PAX DOOR AREA CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 87SW 22903 DURING SCHEDULED B2 CHECK, FOUND AFT ENTRY DOOR UPPER HINGE CUTOUT CRACKED .125 INCH. REPAIRED PER TYPICAL REPAIR NR T1 -A52-005. 2 L 7 2 4F A16WE 1996071800490 19960718 00490 NM 1996 7 18 SWAA960652 1 19960711 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 1152 CREASED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 87SW 22903 DURING SCHEDULED B2 CHECK, FOUND UPPER FUSELAGE SKIN CREASED AT BS 1152, BETWEEN S5 AD 6R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996071800491 19960718 00491 NM 1996 7 18 SWAA960653 1 19960711 A 5311 BELT FRAME BOEING 737 7372H4 138448C NM BS 1100 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 87SW 22904 DURING SCHEDULED 1/2 D-CHECK, FOUND BELT FRAME CRACKED AT LEFT SIDE OF APU COMPARTMENT, BS 1100 TO 1106. REPLACED PER B OEING SRM. 2 L 7 2 4F A16WE 1996071800492 19960718 00492 NM 1996 7 18 SWAA960654 1 19960711 A 5315 FLOOR BEAM BOEING 737 7372H4 138448C NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 87SW 22904 DURING SCHEDULED 1/2 D-CHECK, FOUND FWD GALLEY FLOOR BEAM T-CAP CORRODED AT BS 312 BL 0. REPLACED T-CAP PER TYPICAL REP AIR TI-353-012. 2 L 7 2 4F A16WE 1996071800493 19960718 00493 NM 1996 7 18 SWAA960655 1 19960711 A 5315 FLOOR BEAM BOEING 737 7372H4 138448C NM BS 986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 87SW 22904 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM CORRODED AT BS 986.5, RBL 16, 20, 22, 24, 26, 32 AND 36. REPAIRED PER BO EING SRM. 2 L 7 2 4F A16WE 1996071800494 19960718 00494 NM 1996 7 18 SWAA960656 1 19960711 A 5320 WEB BOEING 737 7372H4 138448C NM BS 1000 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 87SW 22904 DURING SCHEDULED 1/2 D-CHECK, FOUND WEB CORROSION AROUND NUTPLATE AT BS 1000, RBL 44. REPLACED WEB PER BOEING SRM. 2 L 7 2 4F A16WE 1996071800495 19960718 00495 NM 1996 7 18 SWAA960657 1 19960711 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 990 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 87SW 22904 DURING SCHEDULED 1/2 D-CHECK, FOUND Z-ANGLE CORROSION AT AFT GALLEY DOOR BETWEEN BS 990 TO 927. REPLACED ANGLE PER BOEI NG SRM. 2 L 7 2 4F A16WE 1996071800496 19960718 00496 NM 1996 7 18 SWAA960658 1 19960711 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 813 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23338 DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT LOWER FLANGE CRACKED AT BS 813, LBL 17, WL 156. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996071800497 19960718 00497 NM 1996 7 18 SWAA960659 1 19960711 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 639 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23338 DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AT BS 639, S15L. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996071800498 19960718 00498 NM 1996 7 18 SWAA960660 1 19960711 A 5320 TIE BOEING 737 7373H4 1384600 NM BS 344 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23338 DURING SCHEDULED D-CHECK, FOUND STRINGER TIE CRACKED AT BS 344, S10R. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996071800499 19960718 00499 NM 1996 7 18 SWAA960661 1 19960711 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 470 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23338 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 470 BETWEEN S23 AND 22L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996071800500 19960718 00500 NM 1996 7 18 SWAA960662 1 19960711 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 350SW 24409 DURING SCHEDULED TERMINAL CHECK, FOUND AFT CEILING EMERGENCY EXIT LIGHT SIGN INOP. REPLACED BATTERY PACK PER BOEING M/M . 2 L 7 2 4F RT A16WE 1996071800501 19960718 00501 NM 1996 7 18 SWAA960663 1 19960709 A 3350 20131A BATTERY PACK BOEING 737 7373Q8 1384670 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED SERVICE CHECK, FOUND AFT OVERHEAD EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996071800502 19960718 00502 NM 1996 7 18 SWAA960664 1 19960709 A 3350 20121 CHARGER BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 510SW 24187 DURING SCHEDULED C3 CHECK, FOUND FWD SERVICE DOOR EXIT LIGHT INOP. REPLACED BATTERY CHARGER PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996071800503 19960718 00503 NM 1996 7 18 SWAA960665 1 19960712 A 5220 DOOR FRAME BOEING 737 7372H4 138448C NM BS 294 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 55SW 21593 DURING SCHEDULED B2 CHECK, FOUND FWD SERVICE DOOR FRAME CRACKED AT BS 294, 8 INCHES ABOVE FLOOR LEVEL. REPAIRED PER TYP ICAL REPAIR AND BOEING SRM. 2 L 7 2 4F A16WE 1996071800504 19960718 00504 NM 1996 7 18 SWAA960666 1 19960712 A 5240 WEB BOEING 737 7372H4 138448C NM FWD SERV DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 55SW 21593 DURING SCHEDULED B2 CHECK, FOUND FWD SERVICE DOOR WEB ON FWD SIDE OF LOWER SUPPORT CASTING CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996071800505 19960718 00505 NM 1996 7 18 SWAA960667 1 19960712 A 3350 LIGHT BOEING 737 7373Q8 1384670 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 662SW 23255 DURING SCHEDULED A-CHECK, FOUND EMERGENCY LIGHT AT AFT SERVICE DOOR INOP. REPLACED AND OP CHECKED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996071800506 19960718 00506 NM 1996 7 18 SWAA960668 1 19960712 A 5315 FLOOR BEAM BOEING 737 7372H4 138448C NM BS 986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 89SW 22904 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM CORROSION IN AND AROUND FWD FLANGE AT RBL 15 AND 45, BS 986.5. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996071800507 19960718 00507 NM 1996 7 18 SWAA960669 1 19960712 A 5315 FLOOR BEAM BOEING 737 7372H4 138448C NM BS 294 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 89SW 22904 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM CORROSION AT UPPER FLANGE, BS 294, LBL 1, 8 AND 11. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996071800508 19960718 00508 NM 1996 7 18 SWAA960670 1 19960712 A 5315 FLOOR BEAM BOEING 737 7372H4 138448C NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 89SW 22904 DURING SCHEDULED 1/2 D-CHECK, FOUND UPPER AND LOWER SURFACES OF FLOOR BEAM UPPER T-CHORD AFT FLANGE CORRODED, BS 312, LB L 1. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996071800509 19960718 00509 NM 1996 7 18 SWAA960671 1 19960714 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING WALKAROUND CHECK, FOUND FUSELAGE SKIN CRACKED NEAR WATER SERVICE PANEL. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996071800510 19960718 00510 NM 1996 7 18 SWAA960672 1 19960714 A 3350 900835A BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 96SW 23055 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY LIGHTS ABOVE OVERWING EXITS INOP. REPLACED BATTERY PACK AND POWER SUPPL Y PER BOEING M/M. 2 L 7 2 4F A16WE 1996071800511 19960718 00511 NM 1996 7 18 SWAA960673 1 19960713 A 3397 WIRE BOEING 737 7375H4 138449D NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 506SW 24183 DURING WALKAROUND CHECK, FOUND FLOOR EMERGENCY LIGHTS AT ROW 16 INOP. REPAIRED WIRE TO CONNECTOR AT LIGHT PER BOEING M/ M. 2 L 7 2 4F RT A16WE 1996071800512 19960718 00512 EA 1996 7 18 SWIA95745 1 19960624 A 5610 NP1393212 WINDSHIELD CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RT COCKPIT FAILED A SWIA B EMER. DESCENT O OTHER CR CRUISE 1 NM 07 409SW 7056 RT WINDSHIELD SHATTERED AT 33,000 FEET. REMOVED AND REPLACED CO-PILOT'S WINDSHIELD WITH NEW UNIT IAW MM 56-12-01 AND RT NR 56-10. 2 L 7 2 4F 4 F RT A21EA E15NE 1996071800513 19960718 00513 NM 1996 7 18 UPS96220617 1 19960716 A 3260 H1010262 SWTCH BOEING 727 72751C 1384015 NM RT MLG DEFECTIVE A IPXA O OTHER P NO WARNING INDICATION AP APPROACH 1 SO 01 904UP 18946 WHEN GEAR LOWERED FOR LANDING, RIGHT MAIN GREEN LIGHT DID NOT ILLUMINATE, WARNING HORN SOUNDED WHEN FLAPS SELECTED TO 30 DEGREES. RECYCLED GEAR PER AMO PROCEDURE. NO CHANGE. ACCOMPLISHED ALTERNATE EXTENSION PROCEDURE, REMOVED AND REPLACE D GEAR GREEN LIGHT SWITCH RT. PERFORMED OPERATIONAL CHECK OF LANDING GEAR WITH PLANE ON JACKS. OPERATIONAL INDICATION NORMAL. 2 L 7 3 4F A3WE 1996071800514 19960718 00514 NM 1996 7 18 UPS96220619 1 19960703 A 5320 65453132 CLIP BOEING 727 727180C 138406G NM BS 970-990 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE-C, MAIN CABIN AT STR 9R, THE STRINGER TO FRAME TIE CLIPS ARE CRACKED AT FOLLOWING STA 970 TO 990. REMOV ED, FABRICATED AND INSTALLED CLIPS IAW SRM 51-30-2 AND 51-10-1. 2 L 7 3 4F A3WE 1996071800515 19960718 00515 NM 1996 7 18 UPS96220620 1 19960703 A 5320 65453132 CLIP BOEING 727 727180C 138406G NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE-C, MAIN CABIN AT STR 7R, THE STRINGER TO FRAME TIE CLIPS ARE CRACKED AT FOLLOWING STA 970 TO 1010, 1030, 1070. REMOVED, FABRICATED AND INSTALLED CLIPS IAW SRM 51-30-2 AND 51-10-1. 2 L 7 3 4F A3WE 1996071800516 19960718 00516 NM 1996 7 18 UPS96220621 1 19960706 A 5320 65453132 CLIP BOEING 727 727180C 138406G NM BS 970-1010 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE-C, MAIN CABIN AT STR 6R, THE STRINGER TO FRAME TIE CLIPS ARE CRACKED AT FOLLOWING STA 970 TO 1010. REMO VED, FABRICATED AND INSTALLED CLIPS IAW SRM 51-30-2 AND 51-10-1. 2 L 7 3 4F A3WE 1996071800517 19960718 00517 NM 1996 7 18 UPS96220622 1 19960708 A 5320 CLIP BOEING 727 727180C 138406G NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE-C, MAIN CABIN AT STR 7L, THE STRINGER TO FRAME TIE CLIPS ARE CRACKED AT FOLLOWING STA 970, 1010, 1030, 1 050. REMOVED, FABRICATED AND INSTALLED CLIPS IAW SRM 51-30-2 AND 51-10-1. 2 L 7 3 4F A3WE 1996071800518 19960718 00518 NM 1996 7 18 UPS96220623 1 19960708 A 5320 65453135 CLIP BOEING 727 727180C 138406G NM BS 970-990 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE-C, MAIN CABIN AT STR 8L, THE STRINGER TO FRAME TIE CLIPS ARE CRACKED AT FOLLOWING STA 970, 990. REMOVED , FABRICATED AND INSTALLED CLIPS IAW SRM 51-30-2 AND 51-10-1. 2 L 7 3 4F A3WE 1996071800519 19960718 00519 NM 1996 7 18 UPS96220624 1 19960708 A 5320 654531313 CLIP BOEING 727 727180C 138406G NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE-C, MAIN CABIN AT STR 9L, THE STRINGER TO FRAME TIE CLIPS ARE CRACKED AT FOLLOWING STA 970, 990, 1010, 10 30. REMOVED, FABRICATED AND INSTALLED CLIPS IAW SRM 51-30-2 AND 51-10-1. 2 L 7 3 4F A3WE 1996071800520 19960718 00520 NM 1996 7 18 UPS96220625 1 19960703 A 5320 65453132 CLIP BOEING 727 727180C 138406G NM BS 1010-1050 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE-C, MAIN CABIN AT STR 5L, THE STRINGER TO FRAME TIE CLIPS ARE CRACKED AT FOLLOWING STA 1010, 1050. REMOV ED, FABRICATED AND INSTALLED CLIPS IAW SRM 51-30-2 AND 51-10-1. 2 L 7 3 4F A3WE 1996071800521 19960718 00521 NM 1996 7 18 UPS96220626 1 19960703 A 5320 65453132 CLIP BOEING 727 727180C 138406G NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE-C, MAIN CABIN AT STR 8R, THE STRINGER TO FRAME TIE CLIPS ARE CRACKED AT FOLLOWING STA 970, 990, 1030 AND 1050. REMOVED, FABRICATED AND INSTALLED CLIPS IAW SRM 51-30-2 AND 51-10-1. 2 L 7 3 4F A3WE 1996071800522 19960718 00522 NM 1996 7 18 UPS96220627 1 19960701 A 5754 RIB BOEING 727 727180C 138406G NM NR 4 LE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE-C, LT WING, NR 4 SLAT L/E RIB IS CRACKED AT BOTTOM 8 INCHES I/B OF O/B END. REMOVED DAMAGED AREA PER SR M 57-50-3, FIG 9, FAB AND INSTALLED DOUBLER PER SRM 57-50-3 FIG 9. 2 L 7 3 4F A3WE 1996071800523 19960718 00523 NM 1996 7 18 UPS96220628 1 19960703 A 5320 65453132 CLIP BOEING 727 727180C 138406G NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE-C, FRAME TIE CLIPS CRACKED AT STR 6L, STATIONS 970, 990, 1010 AND 1030. REMOVED THE DAMAGED CLIPS, FAB' D REPLACEMENT PARTS AND INSTALLED PER SRM 51-10-1, 51-30-2 AND 53-10-2. 2 L 7 3 4F A3WE 1996071800524 19960718 00524 NM 1996 7 18 UPS96220629 1 19960702 A 5320 SHEAR TIE BOEING 727 727180C 138406G NM BS 328 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE-C, SHEAR TIE CRACKED AT BS 328 AT NOSE LOWER LOBE AREA STR 28L. FAB'D SHEAR TIE AND INSTALLED PER SRM 5 1-40-02 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996071800525 19960718 00525 NM 1996 7 18 UPS96220630 1 19960704 A 5311 FRAME BOEING 727 727180C 138406G NM BS 328 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE-C, FRAME WEB CRACKED FS 328 STR 28L. STOP DRILLED CRACK PER SRM 51-40-2, NDT INSP FAB'D AND INSTALLED D OUBLER REPAIR PER SRM 51-40-2 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996071800526 19960718 00526 NM 1996 7 18 UPS96220631 1 19960701 A 5720 ANGLE BOEING 727 727180C 138406G NM WS 127 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE-C, RT WING L/E RIB TO SPAR ANGLE WS 127 CRACKED. REMOVED, FAB'D AND INSTALLED ANGLE PER SRM 57-10-2, 57 -10-3, 51-30-2, 51-10-2 AND DRAWING 69-20117. 2 L 7 3 4F A3WE 1996071800527 19960718 00527 NM 1996 7 18 UPS96220632 1 19960702 A 5313 STRINGER BOEING 727 727180C 138406G NM BS 600 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE-C, HEAVY CORROSION ON STR 26L AT STA 600. FAB'D AND INSTALLED STRINGER SECTION PER SRM 53-10-3 AND 51-3 0-2. 2 L 7 3 4F A3WE 1996071800528 19960718 00528 NM 1996 7 18 UPS96220633 1 19960704 A 5313 STRINGER BOEING 727 727180C 138406G NM BS 620 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE-C, FS 620 STR 26L HAS HEAVY CORROSION. FAB'D AND INSTALLED STRINGER SECTION PER SRM 53-10-3 AND 51-30-2 . 2 L 7 3 4F A3WE 1996071800529 19960718 00529 NM 1996 7 18 UPS96220634 1 19960630 A 5313 STRINGER BOEING 727 727180C 138406G NM BS 1333 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE-C, BS 1333 STR 16L IS CRACKED AT THE PRESS RELIEF DOOR. REPAIRED IAW SRM 53-10-3 AND 51-30-2. 2 L 7 3 4F A3WE 1996071800530 19960718 00530 NM 1996 7 18 UPS96220635 1 19960712 A 2782 MOUNT ANGLE BOEING 727 727180C 138406G NM NR 4 LE FLAP ACT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE-C, LT WING NR 4 SLAT ACTUATOR ROD END MOUNT ANGLE O/B AND I/B SIDES ARE CRACKED. REMOVED CRACKED FLANGE FROM I/B AND O/B RIBS, FAB'D AND INSTALLED REPAIR ANGLE IAW SRM 51-40-3. 2 L 7 3 4F A3WE 1996071800531 19960718 00531 NM 1996 7 18 UPS96220636 1 19960712 A 5754 ANGLE BOEING 727 727180C 138406G NM NR 2 LE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE-C, LT WING NR 2 SLAT, RIB TO RIB ATTACH ANGLE HAS 5 INCH CRACK AT O/B HOOK. REMOVED ANGLE, FAB'D REPLAC E ANGLE AND INSTALLED IAW SRM 57-50-2, 51-30-2. 2 L 7 3 4F A3WE 1996071800532 19960718 00532 NM 1996 7 18 UPS96220637 1 19960710 A 5720 ANGLE BOEING 727 727180C 138406G NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE-C, LT WING ANGLE FOR PANEL 8107 CRACKED. REMOVED FAB'D AND INSTALLED ANGLE PER BOEING DWG NR 65-19275 A ND 51-30-2. 2 L 7 3 4F A3WE 1996071800533 19960718 00533 NM 1996 7 18 UPS96220638 1 19960706 A 5330 SKIN BOEING 727 727180C 138406G NM BS 360 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE-C, STA 360 BELOW SKIN LAP STR 19R TO 20R IS BEYOND ALLOWABLE LIMITS. CUT OUT DAMAGE AND INSTALLED DOUBL ER REPAIR IAW SRM 53-30-3, 51-10-2. 2 L 7 3 4F A3WE 1996071800534 19960718 00534 NM 1996 7 18 UPS96220639 1 19960701 A 5347 CARGO TRACK BOEING 727 727180C 138406G NM BS 517 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE-C, CORROSION ON LEFT CARGO TRACK, STA 517 LWR CARGO COMPT. REMOVED AND REPLACED TRACK PER SRM 51-30-2 ( P/N 65-23410-4). 2 L 7 3 4F A3WE 1996071800535 19960718 00535 NM 1996 7 18 UPS96220641 1 19960705 A 5320 ANGLE BOEING 727 727180C 138406G NM BS 940-950 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE-C, LT WHEEL WELL O/B ANGLE BETWEEN 940 AND 950 FITTINGS AT STR 18A IS CRACKED. FAB'D AND INSTALLED NEW CHORD ANGLE IAW SRM 53-10-02 AND 51-30-2. 2 L 7 3 4F A3WE 1996071800536 19960718 00536 NM 1996 7 18 UPS96220642 1 19960715 A 5320 WEB BOEING 727 727180C 138406G NM BS 940-950 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE-C, LT WHEEL WELL O/B ANGLE BETWEEN 940 AND 950 FITTINGS AT STR 18A IS CRACKED IN TWO PLACES. REMOVED ST R 18A SILL WEB, FAB'D AND INSTALLED NEW WEB PER SRM 51-10-1, 51-30-2 AND DWG 65-22419. 2 L 7 3 4F A3WE 1996071800537 19960718 00537 NM 1996 7 18 UPS96220643 1 19960715 A 5320 FITTING BOEING 727 727180C 138406G NM BS 740 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 921UP 19874 INSPECTION TYPE-C, FS 740 BETWEEN STR 19R TO 20R FITTING WAS CRACKED BEYOND STOP DRILL. REPAIRED BS 740 RT FITTING PER EO B727-5310-8420-A 2 L 7 3 4F A3WE 1996071800538 19960718 00538 NM 1996 7 18 UPS96420601 1 19960709 A 3350 LIGHTS BOEING 747 747123 1384873 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE DLY, MAIN DECK TWO EMERGENCY EXIT LIGHTS INOP, FWD AISLE LIGHT AND FWD LIGHT IN L1 DOOR SILL. PERFORMED OPS CHK OF EMERGENCY LIGHTS, LIGHTS CHECK GOOD. 2 L 7 4 4F A20WE 1996071800539 19960718 00539 NM 1996 7 18 UPS96420610 1 19960714 A 5330 SKIN BOEING 747 747123 1384873 NM BS 2726-2733 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE DLY, EMPENNAGE LEFT SIDE 8 TO 9 INCH CRACK ABOUT MIDDLE OF EXHAUST SECTION, CRACKED COMPLETELY THROUGH I NTO APU SECTION, AFT OF HORIZONTAL STABILIZER BETWEEN FS 2726 TO 2733 WL 320. REPAIRED APU HOUSING SECTION SKIN SECTION , SEALED AND PAINTED PER SRM 53-30-03 FIG 1A. 2 L 7 4 4F A20WE 1996071800540 19960718 00540 NM 1996 7 18 UPS96420611 1 19960716 A 2611 215680 SMOKE DETECTOR BOEING 747 747123 1384873 NM CARGO COMPT INOPERATIVE A IPXA F ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 SO 01 673UP 20325 INSPECTION TYPE-N/A, LOWER AFT CARGO FIRE WARNING DURING CLIMB, BOTH FIRE BOTTLES DISCHARGED AS PER AOM. AIR TURNBACK T O SEL. REMOVED AND REPLACED NR 4 SMOKE DETECTOR IN AFT LWR CARGO COMP, OPS CHK NORMAL PER B747 M/M. REMOVED AND REPLAC ED BOTH FIRE BOTTLES IAW MM 26-23-01, OPS SQUIB AND PRESS SYSTEM CHECK GOOD. 2 L 7 4 4F A20WE 1996071800541 19960718 00541 NM 1996 7 18 UPS96520612 1 19960713 A 5755 113N550139A SPOILER BOEING 757 75724APF 1384969 NM NR 1 WATER DAMAGE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 405UP 23727 INSPECTION TYPE 3C, NR 1 SPOILER REQUIRES REMOVAL AND REPLACEMENT DUE TO CLASS 4 WATER DAMAGE. REMOVED AND REPLACED NR 1 SPOILER IAW MM 27-61-01. FUNCTIONAL CHECK GOOD IAW MM 27-61-00. 2 L 7 2 4F RT A2NM 1996071800542 19960718 00542 NM 1996 7 18 UPS96520613 1 19960713 A 5712 RIB BOEING 757 75724APF 1384969 NM LT TE WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 405UP 23727 INSPECTION TYPE 3C, WHILE WORKING ROLLER RIB EO B757-5750-2093-1 SMALL CRACK MEASURING .3125 INCH LONG BY .125 INCH WIDE WAS DICOVERED 30.625 INCHES INBD FROM NEW ROLLER RIB AND 12.5 INCHES FORWARD OF TRAILING EDGE LEFT SIDE INBD AFT FLAP. REPAIRED PER SRM 51-70-4 AND SRM 57-53-01. 2 L 7 2 4F RT A2NM 1996071800543 19960718 00543 NM 1996 7 18 UPS96520614 1 19960713 A 5755 113N550140A SPOILER BOEING 757 75724APF 1384969 NM NR 12 WATER DAMAGE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 405UP 23727 INSPECTION TYPE 3C, NR 12 SPOILER REQUIRES REMOVAL AND REPLACEMENT DUE TO CLASS 4 WATER DAMAGE. REMOVED AND REPLACED NR 12 SPOILER IAW MM 27-61-01. FUNCTIONAL CHECKED GOOD IAW MM 27-61-00. 2 L 7 2 4F RT A2NM 1996071800544 19960718 00544 NM 1996 7 18 UPS96520615 1 19960713 A 5755 113N460136A SPOILER BOEING 757 75724APF 1384969 NM NR 7 WATER DAMAGE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 405UP 23727 INSPECTION TYPE 3C, NR 7 SPOILER REQUIRES REMOVAL AND REPLACEMENT DUE TO CLASS 4 WATER DAMAGE. REMOVED AND REPLACED NR 7 SPOILER IAW MM 27-61-01. FUNCTIONAL TEST GOOD ON NR 7 SPOILER IAW MM 27-61-00. 2 L 7 2 4F RT A2NM 1996071800545 19960718 00545 NM 1996 7 18 UPS96620640 1 19960710 A 2421 IDG BOEING 767 76734AF 1385212 NM ENGINE REQUIRED SERVICE A IPXA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 304UP 27242 INSPECTION, REJECTED TAKEOFF DUE TO GEN OFF LIGHT ILLUMINATED AND ACCOMPANIED BY GEN DRIVE LIGHT ILLUMINATED AS WELL. C HECKED AND SERVICED IDG, RAN ENGINE AND CHECKS NORMAL. 2 L 7 2 4F RT A1NM 1996071800546 19960718 00546 NE 1996 7 18 HEEA967400 1 19960610 A 6210 7615009100041 BLADE SKRSKY S76 S76A 8143006 NE M/R WATER CONTAM E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 117WB 3708 760092 BLADE IS SUSPECTED TO HAVE WATER INGRESSION. 1 G 7 2 3U H1NE 1996071800547 19960718 00547 NE 1996 7 18 HEEA967401 1 19960610 A 6210 7615009100041 BLADE SKRSKY S76 S76A 8143006 NE M/R WATER CONTAM E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 117WB 3708 760092 BLADE IS SUSPECTED TO HAVE WATER INGRESSION. 1 G 7 2 3U H1NE 1996071800548 19960718 00548 NE 1996 7 18 HEEA967402 1 19960610 A 6210 7615009100041 BLADE SKRSKY S76 S76A 8143006 NE M/R WATWER CONTAM E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 117WB 3708 760092 BLADE IS SUSPECTED TO HAVE WATER INGRESSION. 1 G 7 2 3U H1NE 1996071800549 19960718 00549 EU 1996 7 18 HEEA967403 1 19960610 A 7712 9580113720 TRANSMITTER SNIAS 350 AS350B2 8680813 EU ENG TORQUE READS HIGH E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 2771 TORQUE READING HIGH AND NORMAL T4 FOUND TORQUE TRANSMITTER INDICATING 8% HIGH. 1 G 7 1 3U H9EU 1996071800550 19960718 00550 EU 1996 7 18 HEEA967404 1 19960611 A 6220 350A31190703 STARFLEX AEROSP AS355 AS355F1 8680810 EU M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5796S 489 5164 CRACKED STARFLEX ARM BEYOND LIMITS. 1 G 7 2 3U H11EU 1996071800551 19960718 00551 NE 1996 7 18 HEEA967405 1 19960611 A 6210 7615009043050 TIP CAP SKRSKY S76 S76A 8143006 NE M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22342 760096 CRACKED FIBERGLASS SKIN BETWEEN THE INNER AND OUTER DOUBLER. 1 G 7 2 3U H1NE 1996071800552 19960718 00552 1996 7 18 HEEA967406 4 19960611 A 3457 S67157539 ANTENNA BELL 206 206B 1181511 SW COCKPIT GPS DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2268X 3607 GPS ANTENNA NOT PICKING UP SIGNAL STRENGTH FROM SATELLITES. 1 G 7 1 3U H2SW 1996071800553 19960718 00553 1996 7 18 HEEA967407 4 19960611 A 3457 0845000000 SKYNAV 5000 BELL 206 206L1 1182107 SW COCKPIT GPS DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2775A 272 45297 WILL NOT TRACK SATELLITES. TIME SINCE REPAIR 110:15. 1 G 7 1 3U H2SW 1996071800554 19960718 00554 SW 1996 7 18 HEEA967408 1 19960611 A 6210 206010200133 BLADE BELL 206 206B3 1181506 SW M/R CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2497 HAS EXCESSIVE AMOUNT OF EXFOLIATION ON UPPER LEADING EDGE NEAR THE TIP WITH PIECE MISSING. 1 G 7 1 3U H2SW 1996071800555 19960718 00555 SW 1996 7 18 HEEA967409 1 19960612 A 6520 214040011119 GEARBOX BELL 214 214ST 1182106 SW T/R CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 PART IS CORRODED. (OUTPUT SHAFT SPLINES CORROSION PITTED OR FRETTING DUE TO TAIL ROTOR BLADE ASSEMBLY RETAINING NUT LOS ING TORQUE. 2 G 7 2 4U H10SW 1996071800556 19960718 00556 EU 1996 7 18 HEEA967410 1 19960612 A 6210 10515141 BLADE BOLKMS 105 BO105S 5626006 EU M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8197X 3307 S808 CRACKS IN THE NOSE AND NECK SHELL AT THE CUFF AREA. 1 G 7 2 3U H3EU 1996071800557 19960718 00557 EU 1996 7 18 HEEA967411 1 19960612 A 6210 10515141 BLADE BOLKMS 105 BO105S 5626006 EU M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7170D 2320 S840 CRACKS IN THE NOSE SHELL NEAR THE CUFF AREA. 1 G 7 2 3U H3EU 1996071800558 19960718 00558 EU 1996 7 18 HEEA967412 1 19960612 A 6210 10515170 BLADE BOLKMS 105 BO105S 5626006 EU M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7170D 2320 S840 THE NOSE SHELL CRACKED AND SEPARATED. 1 G 7 2 3U H3EU 1996071800559 19960718 00559 EU 1996 7 18 HEEA967413 1 19960612 A 6210 10515141 M/R BLADE BOLKMS 105 BO105S 5626006 EU M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8197X 3147 S808 THE NOSE SHELL AND NECK SHELL CRACKED. 1 G 7 2 3U H3EU 1996071800560 19960718 00560 1996 7 18 HEEA967414 4 19960613 A 3452 066106200 TRANSCEIVER KT76 BELL 206 206L3 1182108 SW COCKPIT ATC DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 31077 51520 R/H KNOB BROKEN. REPLACED KNOB. REPAIRED. UNIT HAS LOW POWER OUT AND CANNOT ADJUST POWER UP TO SPECS. REPLACED CAVITY OSCILLATOR V101. REPAIRED. ADJUSTED PULSE WIDTH. BENCH CHECK GOOD. 1 G 7 1 3U H2SW 1996071800561 19960718 00561 1996 7 18 HEEA967415 4 19960613 A 3444 066104802 INDICATOR SKRSKY S76 S76A 8143006 NE RADAR ALTIMETER FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 22342 760096 RADAR ALTIMETER INDICATOR SPINNING. NEEDLE ON INDICATOR SPINS CONSTANTLY. FOUND OPEN FOIL ON POWER SUPPLY BOARD DUE TO CORROSION. RE-SOLDERED OVER OPEN RUN AND REPLACED CORRODED CAPACITOR C102. REPAIRED PROBLEM. REPLACED RESISTORS R518, R519, R534 AND R260 TO INCORPORATE MOD 10 ASPER SERVICE BULLETIN KING KRA405-10. PERFORMED TOTAL CALIBRATION AND ALIGN MENT. BENCH CHECK GOOD. 1 G 7 2 3U H1NE 1996071800562 19960718 00562 1996 7 18 HEEA967416 4 19960614 A 2370 9806019001 CVR BELL 412 412 1182202 SW COCKPIT INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3893S 33022 CVR INOPERATIVE. 1 G 7 2 4U H4SW 1996071800563 19960718 00563 1996 7 18 HEEA967417 4 19960614 A 2370 9806019001 CVR BELL 412 412 1182202 SW COCKPIT WONT TEST E HEEA K NONE L NO TEST NR NOT REPORTED 1 SW 03 22347 36005 CVR WILL NOT TEST. 1 G 7 2 4U H4SW 1996071800564 19960718 00564 1996 7 18 HEEA967418 4 19960614 A 2370 9806019001 CVR BELL 412 412 1182202 SW COCKPIT CVR DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 33008 36004 TRANSCRIPTION OF CVR TAPES UNSATISFACTORY. 1 G 7 2 4U H4SW 1996071800565 19960718 00565 GL 1996 7 18 HEEA967419 2 19960617 A 7250 6886407 ENGINE 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL TURBINE WHEEL LOW POWER E HEEA K NONE R PARTIAL RPM/PWR LOSS IN INSP/MAINT 1 SW 03 7136H 585 CAT36772 S833 CAE836456 ENGINE REMOVED DUE TO LOW POWER. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: MINOR SULFIDATION ON ALL 1ST ST AGE WHEEL BLADES. SCRAPPED 1ST STAGE WHEEL. 1 G 7 2 3U 3 U H3EU E4CE 1996071800566 19960718 00566 GL 1996 7 18 HEEA967420 2 19960617 A 7250 23055430 NOZZLE 23033185 BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL 1ST STAGE CRACKED E HEEA K NONE R PARTIAL RPM/PWR LOSS IN INSP/MAINT 1 SW 03 2251Z 728 CAT70546 45756 CAE860213 ENGINE REMOVED DUE TO CRACKED FIRST STAGE NOZZLE AND LOW POWER ON TEST CELL. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: EXCESSIVE RUN OUT (.007) BEYOND SERVICEABLE LIMITS ON #2 NOZZLE TIP PATHS. REPLACED DISCREPANT PART. 1 G 7 1 3U 3 U H2SW E1GL 1996071800567 19960718 00567 GL 1996 7 18 HEEA967421 2 19960617 A 7250 23060450 NOZZLE 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL NR 1 NOZ VANE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7136H 585 CAT36772 S833 CAE836456 ENGINE REMOVED DUE TO LOW POWER. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: CRACKED BEYOND SERVICEABLE LIMI TS ON #1 NOZZLE VANES. REPLACED DISCREPANT PART. 1 G 7 2 3U 3 U H3EU E4CE 1996071800568 19960718 00568 GL 1996 7 18 HEEA967422 2 19960617 A 7250 23008054 NOZZLE 23033185 BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL NR 1 NOZ VANE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5742H 441 CAT70741 45476 CAE860112 ENGINE REMOVED DUE TO HIGH OIL CONSUMPTION. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: CRACKED AND BOWED B EYOND SERVICEABLE LIMITS ON #1 NOZZLE VANES. REPLACED DISCREPANT PART. 1 G 7 1 3U 3 U H2SW E1GL 1996071800569 19960718 00569 GL 1996 7 18 HEEA967427 2 19960621 A 7240 6899081 LINER 23035128 SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL FUEL NOZ BORE MIS MFG E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 CAT90574 UPON ATTEMPTING ASSEMBLY FOUND THE IGNITER AND FUEL NOZZLE BORE DO NOT ALIGN WITH NUMEROUS COMB. CASES. REPLACED DISCREP ANT PART. 1 G 7 2 3U 3 U H1NE E1GL 1996071800570 19960718 00570 SW 1996 7 18 HEEA967428 1 19960621 A 6420 214011802111 YOKE 214011801117 BELL 214 214ST 1182106 SW T/R BEARING WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 3484 A407 28106 COMPLY WITH OSN 214ST-96-08, ALSO BLADE BEARINGS ARE WORN. 2 G 7 2 4U H10SW 1996071800571 19960718 00571 1996 7 18 HEEA967429 4 19960621 A 2312 071127401 TRANSCEIVER KFS594 BELL 412 412 1182202 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3893S 33022 DISPLAY DIM AND LENS FADED. 1 G 7 2 4U H4SW 1996071800572 19960718 00572 1996 7 18 HEEA967430 4 19960621 A 3455 066107700 RECEIVER BELL 214 214ST 1182106 SW COCKPIT ADF FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 8045T 28101 DOES NOT WORK. REPLACED HEADERS J302, J306, J307 AND APPLIED HUMISEAL TO HEADERS FOR CORROSION CONTROL. REPLACED CRACKE D RESISTOR R339 AND CRACKED SPACER FOR BNC. REPLACED BROKEN HEX NUT ON POWER SUPPLY AND INSTALLED MISSING WASHER, NUT A ND SPACER. TESTED.BENCH CHECK GOOD. 2 G 7 2 4U H10SW 1996071800573 19960718 00573 1996 7 18 HEEA967431 4 19960621 A 3452 066106200 TRANSCEIVER KT76 BELL 206 206B 1181511 SW COCKPIT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2269A 3608 WILL NOT REPORT. FOUND UNIT DRAWS EXCESSIVE CURRENT. REPLACED CAVITY OSCILLATOR V101. REPAIRED. ADJUSTED PULSE WIDTH AND FREQUENCY. BENCH CHECK GOOD. 1 G 7 1 3U H2SW 1996071800574 19960718 00574 1996 7 18 HEEA967432 4 19960621 A 3453 066402600 LORAN KLN88 BELL 206 206L1 1182107 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 50046 45173 TAKES 15-20 MINUTES TO WARM UP AND LOSES ITSELF INTERMITTENTLY. 1 G 7 1 3U H2SW 1996071800575 19960718 00575 SW 1996 7 18 HEEA967433 1 19960621 A 2930 41003285 INDICATOR BELL 214 214ST 1182106 SW HYD BYPASS WONT TEST E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5748M 28102 HYD BYPASS LIGHT WON'T TEST. 2 G 7 2 4U H10SW 1996071800576 19960718 00576 NE 1996 7 18 HEEA967468 1 19960621 A 6730 7630103902102 ACTUATOR SKRSKY S76 S76A 8143006 NE SERVO SYS STICKS E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1546G 760076 INTERMITTENTLY STICKS; BUT STARTS WHEN TAPPED ON. 1 G 7 2 3U H1NE 1996071800577 19960718 00577 SW 1996 7 18 HEEA967469 1 19960621 A 6220 412010124109 BOLT BELL 412 412 1182202 SW M/R COAT FLAKE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 108X 2097 33115 BOLTS HAVE COATING FLAKING. SERIAL NUMBERS REMOVED ARE A701, A746, AND A603. 1 G 7 2 4U H4SW 1996071800578 19960718 00578 SW 1996 7 18 HEEA967470 1 19960621 A 6320 212070116009 INDICATOR BELL 412 412 1182202 SW XMSN OIL ERRATIC E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2149S 36002 PILOT REPORTED TEMPERATURE FLUX OF 40 DEGREE IN FLIGHT. 1 G 7 2 4U H4SW 1996071800579 19960718 00579 EU 1996 7 18 HEEA967471 1 19960621 A 6320 4638201005 UPPER HOUSING BOLKMS 105 BO105S 5626006 EU M/R GR BOX WORN EXCESS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 721MB S752 PART IS WORN EXCESSIVELY. (BUSHING BORE WORN BEYOND LIMITS) 1 G 7 2 3U H3EU 1996071800580 19960718 00580 1996 7 18 HEEA967472 4 19960621 A 2200 7690001802106 ACTUATOR SKRSKY S76 S76A 8143006 NE AFCS CHATTERS E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 31217 6507 760229 ACTUATOR CHATTERS WHEN SWITCHED ON. 1 G 7 2 3U H1NE 1996071800581 19960718 00581 SW 1996 7 18 HEEA967473 1 19960624 A 7722 206375007101 INDICATOR BELL 206 206L3 1182108 SW COCKPIT TOT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 129MR 51129 INDICATES OVER 10 DEGREES LOW IN EXPANDED SCALE ON INITIAL START. 1 G 7 1 3U H2SW 1996071800582 19960718 00582 1996 7 18 HEEA967474 4 19960624 A 2200 7690001802106 ACTUATOR SKRSKY S76 S76A 8143006 NE AFCS MALFUNCTION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1546K 760082 ACTUATOR INTERMITTENTLY FALLS OFF LINE. 1 G 7 2 3U H1NE 1996071800583 19960718 00583 EU 1996 7 18 HEEA967475 1 19960624 A 7170 0174078010 VALVE SNIAS 350 AS350B2 8680813 EU START DRAIN LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 350BZ 1684 2653 START DRAIN VALVE LEAKING FUEL. 1 G 7 1 3U H9EU 1996071800584 19960718 00584 SW 1996 7 18 HEEA967476 1 19960624 A 2810 206061661101 CELL BELL 206 206B 1181511 SW FUEL SYS PEELED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2272V 3621 FUEL CELL IS PEELED. (UNBONED FLANGE AND PEELING) 1 G 7 1 3U H2SW 1996071800585 19960718 00585 SW 1996 7 18 HEEA967477 1 19960624 A 6320 206040531001 CASE ASSY BELL 206 206L1 1182107 SW OIL PASSAGE CLOGGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2133X 45634 CASE ASSY CLOGGED OIL PASSAGE. 1 G 7 1 3U H2SW 1996071800586 19960718 00586 NE 1996 7 18 HEEA967478 1 19960624 A 7810 7630507003044 EJECTOR SKRSKY S76 S76A 8143006 NE EXH SYS CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31217 760229 EJECTOR IS CRACKED. 1 G 7 2 3U H1NE 1996071800587 19960718 00587 EU 1996 7 18 HEEA967479 1 19960624 A 6420 105317381 INNER SLEEVE BOLKMS 117 BK117B2 5626013 EU T/R HEAD WORN EXCESSIVELY E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 132AE 7238 INNER SLEEVE IS WORN EXCESSIVELY. (SEAL RIDE AREA WORN) 1 G 7 2 3U NC H13EU 1996071800588 19960718 00588 EU 1996 7 18 HEEA967480 1 19960624 A 6240 10594575 TRANSMITTER BOLKMS 105 BO105S 5626006 EU M/R MAST WONT TEST E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 50293 S677 TRANSMITTER WILL NOT TEST PROPERLY. 1 G 7 2 3U H3EU 1996071800589 19960718 00589 EU 1996 7 18 HEEA967481 1 19960624 A 6240 10594565 INDICATOR BOLKMS 105 BO105S 5626006 EU MAST MOMENT WONT TEST E HEEA K NONE L NO TEST NR NOT REPORTED 1 SW 03 50293 S677 INDICATOR WILL NOT TEST PROPERLY. 1 G 7 2 3U H3EU 1996071800590 19960718 00590 1996 7 18 HEEA967482 4 19960624 A 3421 1113034 INDICATOR SKRSKY S76 S76A 8143006 NE COCKPIT ATTITUDE DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 911MJ 760231 INDICATOR SHORTED AND POPS CIRCUIT BREAKER. 1 G 7 2 3U H1NE 1996071800591 19960718 00591 SW 1996 7 18 HEEA967483 1 19960624 A 7722 206375007103 INDICATOR BELL 206 206L 1181522 SW COCKPIT TOT STICKS E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 7074W 52033 NEEDLE STICKS AT ZERO. 1 G 7 1 3U H2SW 1996071800592 19960718 00592 SW 1996 7 18 HEEA967484 1 19960624 A 6240 206070265101 INDICATOR BELL 206 206L1 1182107 SW DUAL TACH STICKS E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 50034 45167 NEEDLE STICKS AT ZERO. 1 G 7 1 3U H2SW 1996071800593 19960718 00593 SW 1996 7 18 HEEA967485 1 19960624 A 2841 206075189101 INDICATOR BELL 206 206B3 1181506 SW FUEL QTY DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2268W 3606 OIL INSIDE OF GLASS. 1 G 7 1 3U H2SW 1996071800594 19960718 00594 1996 7 18 HEEA967486 4 19960624 A 3417 214175421101 COMPUTER BELL 214 214ST 1182106 SW AIR DATA INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 AIR DATA COMPUTER INOPERATIVE. PART IS BURNT. TIME SINCE REPAIR 15:45. 2 G 7 2 4U H10SW 1996071800595 19960718 00595 SW 1996 7 18 HEEA967489 1 19960627 A 6520 214040011119 GEARBOX BELL 214 214ST 1182106 SW T/R CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5748M 4271 28102 PART IS CORRODED. (CORROSION ON DRIVE SPLINES) REMOVED FROM MAST S/N A13-01164, T.T. 4271:05. 2 G 7 2 4U H10SW 1996071800596 19960718 00596 SW 1996 7 18 HEEA967490 1 19960627 A 2435 214060056103 STARTER BELL 214 214ST 1182106 SW ENGINE BURNT E HEEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 03 3897N 857 28106 STARTER SMOKING ON ENGINE START; UNIT IS BURNT. 2 G 7 2 4U H10SW 1996071800598 19960718 00598 GL 1996 7 18 HEEA967493 2 19960628 A 7250 23031938 NOZZLE 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL NR 2 CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 205UC CAT25464 S668 CAE833145 ENGINE DISASSEMBLED DUE TO LOW POWER ON TEST CELL. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: CRACKS BEYOND LIMITS ON #2 NOZZLE BRAZED AREA BETWEEN DIAPHRAGM AND VANE INNER BAND. REPLACED DISCREPANT PART. 1 G 7 2 3U 3 U H3EU E4CE 1996071800599 19960718 00599 GL 1996 7 18 HEEA967494 2 19960702 A 7230 6871259 TIE BOLT 6890550 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENG COMP DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7136J CAC41763 S830 CAE270055 UPON ASSEMBLY OF COMPRESSOR NOTED THE FOLLOWING: UNABLE TO ENGAGE THREADS INTO 1ST STAGE WHEEL. UPON INSPECTION OF PAR T NOTED THE FOLLOWING: IMPROPERLY MACHINED THREADS ON TIE BOLT FWD END. REPLACED DISCREPANT PART. 1 G 7 2 3U 3 U H3EU E4CE 1996071800600 19960718 00600 SW 1996 7 18 HEEA967495 1 19960702 A 3213 412050010107 CROSSTUBE BELL 412 412 1182202 SW MLG FAILED E HEEA K NONE O OTHER LD LANDING 1 SW 03 3893P 6277 33012 UPON LANDING AT OFFSHORE PLATFORM, AS COLLECTIVE WAS BEING LOWERED, LOUD CRACK WAS HEARD AND AIRCRAFT SETTLED RIGHT, REA R. POWER WAS APPLIED (COLLECTIVE), IN A HOVER MECHANIC ON PLATFORM CONFIRMED BROKEN CROSSTUBE. AIRCRAFT RETURNED TO SH ORE BASEAND LANDED ON JACKS PRIOR TO SHUTDOWN. CROSSTUBE IN THREE PIECES. 1 G 7 2 4U H4SW 1996071800601 19960718 00601 GL 1996 7 18 HEEA967496 2 19960702 A 7250 6886407 WHEEL 6898735 BELL 206 206B3 1181506 SW ALLSN 250C 250C20B 03013 GL 1ST STAGE ERODED BLADES E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2275Q 779 CAT33006 3625 CAE836429 ENGINE REMOVED DUE TO CYCLED OUT WHEELS. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: SEVERE EROSION ON #1 AN D #2 WHEEL BLADES LEADING EDGES. SCRAPPED 1ST STAGE WHEEL. 1 G 7 1 3U 3 U H2SW E4CE 1996071800602 19960718 00602 GL 1996 7 18 HEEA967497 2 19960702 A 7250 6898782 WHEEL 6898735 BELL 206 206B3 1181506 SW ALLSN 250C 250C20B 03013 GL 2ND STAGE ERODED BLADES E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2275Q 779 CAT33006 3625 CAE836429 ENGINE REMOVED DUE TO CYCLED OUT WHEELS. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: SEVERE EROSION ON #1 AN D #2 WHEEL BLADES LEADING EDGES. SCRAPPED 1ST STAGE WHEEL. 1 G 7 1 3U 3 U H2SW E4CE 1996071800603 19960718 00603 SW 1996 7 18 HEEA967498 1 19960705 A 3340 6035571 POWER SUPPLY BELL 214 214ST 1182106 SW STROBE INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5748M 141 28102 POWER SUPPLY INOPERATIVE. 2 G 7 2 4U H10SW 1996071800604 19960718 00604 GL 1996 7 18 HEEA967499 2 19960705 A 7230 6851574 SCROLL ASSY 6890550 BELL 206 206B3 1181506 SW ALLSN 250C 250C20B 03013 GL PROBE ELBOW OVERSIZE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2269A CAC41691 3608 CAE835389 UPON PRE-ASSEMBLY INSPECTION OF PART NOTED THE FOLLOWING: I.D. OVERSIZED ON SCROLL PROBE ELBOW BORE AS MARKED. REPLACED DISCREPANT PART. PART RETURNED TO DALLAS AIRMOTIVE FOR 100% WARRANTY REPAIR PER ROB HALDEMEN'S INSTRUCTIONS. 1 G 7 1 3U 3 U H2SW E4CE 1996071800605 19960718 00605 GL 1996 7 18 HEEA967500 2 19960705 A 7230 23056634 GEARSHAFT 23033191 BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL SPUR ADAPTER STEP WEAR E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1078G 482 CAC70280 45398 CAE860166 ENGINE REMOVED DUE TO SMOKE ON SHUTDOWN. UPON VISUAL INSPECTION OF COMPRESSOR NOTED THE FOLLOWING: STEP WEAR BEYOND SE RVICEABLE LIMITS ON SPUR ADPATER GEARSHAFT AFT SPLINES. REPLACED DISCREPANT PART. 1 G 7 1 3U 3 U H2SW E1GL 1996071800606 19960718 00606 GL 1996 7 18 HEEA967502 2 19960705 A 7230 230052712 SPLINE ADAPTER 23033191 BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL GEARSHAFT WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5748Q 683 CAC70080 45499 CAE860100 ENGINE REMOVED DUE TO TURBINE OVERHAUL AND COMPRESSOR N1 SHAFTING INSPECTION. UPON INSPECTION OF COMPRESSOR PARTS NOTED THE FOLLOWING: STEP WEAR BEYOND SERVICEABLE LIMITS ON SPUR ADAPTER GEARSHAFT AFT SPLINES AND STEP WEAR BEYOND SERVICEA BLE LIMITSON SPLINE ADAPTER INTERNAL SPLINES. REPLACED DISCREPANT PART. 1 G 7 1 3U 3 U H2SW E1GL 1996071800607 19960718 00607 GL 1996 7 18 HEEA967503 2 19960705 A 7250 23038218 NOZZLE 6898735 BELL 206 206B3 1181506 SW ALLSN 250C 250C20B 03013 GL 1ST STAGE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2268A CAT33392 3602 TURBINE DISASSEMBLED DUE TO LOW POWER ON TEST CELL. UPON INSPECTION OF TURBINE PARTS FOUND CRACKED 1ST STAGE NOZZLE VAN ES AND INNER BARREL. REPLACED DISCREPANT PART. 1 G 7 1 3U 3 U H2SW E4CE 1996071800608 19960718 00608 EU 1996 7 18 HEEA967504 1 19960705 A 7722 50061036 INDICATOR BOLKMS 105 BO105S 5626006 EU EXH TEMP WONT CALIB E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5421E S806 WILL NOT CALIBRATE. 1 G 7 2 3U H3EU 1996071800609 19960718 00609 EU 1996 7 18 HEEA967505 1 19960705 A 7722 50061036 INDICATOR BOLKMS 105 BO105S 5626006 EU EXH TEMP FRICTION ERROR E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 7170D S840 EXCESSIVE FRICTION ERROR. 1 G 7 2 3U H3EU 1996071800610 19960718 00610 EU 1996 7 18 HEEA967506 1 19960705 A 7722 50061036 INDICATOR BOLKMS 105 BO105S 5626006 EU EXH TEMP READS HIGH E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 91070 S145 READS 20 DEGREES HIGH AND WON'T CALIBRATE. 1 G 7 2 3U H3EU 1996071800611 19960718 00611 NE 1996 7 18 HEEA967507 1 19960705 A 7931 7645001078101 INDICATOR SKRSKY S76 S76A 8143006 NE ENG OIL READS HIGH E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 4253S 760035 HIGH OIL PRESSURE. 1 G 7 2 3U H1NE 1996071800612 19960718 00612 NM 1996 7 18 HEEA967508 1 19960705 A 6230 900C2010188105 SWASHPLATE DOUG MD900 MD900 3027375 NM M/R BEARING FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 9214U 58 90000014 SWASHPLATE BEARING INNER RACE IS SPINNING. 1 G 7 2 3U NC H19NM 1996071800613 19960718 00613 SW 1996 7 18 HEEA967509 1 19960705 A 6330 206033506101 RESTRAINT BELL 206 206L3 1182108 SW XMSN WORN EXCESS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8592X 51508 TRANSMISSION RESTRAINT IS WORN EXCESSIVELY. (WORN BEARING) 1 G 7 1 3U H2SW 1996071800614 19960718 00614 SW 1996 7 18 HEEA967510 1 19960705 A 6330 206033506101 RESTRAINT BELL 206 206L1 1182107 SW XMSN WORN EXCESS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 27766 45312 RESTRAINT IS WORN EXCESSIVELY. (UNSTAKED BEARING) 1 G 7 1 3U H2SW 1996071800615 19960718 00615 SW 1996 7 18 HEEA967511 1 19960705 A 6330 206033506101 RESTRAINT BELL 206 206L1 1182107 SW XMSN WORN BEARING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5005F 45176 RESTRAINT WORN BEARING AND EDGE SEPARATION. 1 G 7 1 3U H2SW 1996071800616 19960718 00616 SW 1996 7 18 HEEA967512 1 19960705 A 6320 206040156101 SEAL ASSY BELL 206 206L3 1182108 SW M/R GR BOX PITTED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 32041 51539 SEAL IS PITTED. 1 G 7 1 3U H2SW 1996071800618 19960718 00618 1996 7 18 HEEA967514 2 19960705 A 7412 49522 EXCITER BOLKMS 105 BO105S 5626006 EU ENG IGN DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 54197 S805 EXCITER WILL NOT START ENGINES AND NEW IGNITER PLUG POPS VERY SLOWLY. 1 G 7 2 3U H3EU 1996071800619 19960718 00619 1996 7 18 HEEA967515 4 19960705 A 2210 5485020 ACTUATOR BEECH 200 200CBEECH 1152926 CE AUTO PILOT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 39PH BL3 SPIRAL DISC SWITCH LEVER HAS EXCESSIVE PLAY. 1 L 7 2 4T A24CE 1996071800620 19960718 00620 1996 7 18 HEEA967516 4 19960705 A 2200 7690001802106 ACTUATOR SKRSKY S76 S76A 8143006 NE AFCS FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 911MJ 760231 AFCS INDICATOR PEGGED TO THE LEFT SIDE. 1 G 7 2 3U H1NE 1996071800622 19960718 00622 1996 7 18 HEEA967520 4 19960705 A 2564 214070943107 LIFE RAFT BELL 214 214ST 1182106 SW CABIN STRAPS BROKE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 LIFE RAFT STRAPS BROKE UPON INSTALLATION. (REPACK AND RETURN) 2 G 7 2 4U H10SW 1996071800623 19960718 00623 SW 1996 7 18 HEEA967522 1 19960705 A 6320 204040386001 CASE ASSY BELL 412 412 1182202 SW M/R GR BOX CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 33008 36004 PART IS CORRODED. (CORROSION IN LARGE BOLT HOLES AND PITTING ON MOUNTING SURFACE. 1 G 7 2 4U H4SW 1996071800624 19960718 00624 SW 1996 7 18 HEEA967523 1 19960705 A 2422 412075101101 INVERTER BELL 412 412 1182202 SW AC SYS TRIPS BREAKER E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 22608 33075 POPS CIRCUIT BREAKER. 1 G 7 2 4U H4SW 1996071800625 19960718 00625 1996 7 18 HEEA967524 4 19960705 A 2370 9806019001 CVR SKRSKY S76 S76A 8143006 NE COCKPIT WONT TEST E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 792CH 760193 PILOT SIDE NOT TESTING CORRECTLY. 1 G 7 2 3U H1NE 1996071800626 19960718 00626 SW 1996 7 18 HEEA967525 1 19960705 A 2437 209070264003 DUAL AMMETER BELL 412 412 1182202 SW COCKPIT FLUCTUATES E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 7128R 36007 #1 NEEDLE FLUCTUATES WHEN VIBRATED & INTERMITTENTLY STICKS AT ZERO. TIME SINCE REPAIR 29:35. 1 G 7 2 4U H4SW 1996071800627 19960718 00627 SW 1996 7 18 HEEA967526 1 19960709 A 3212 214073929107 VALVE BELL 214 214ST 1182106 SW FLOAT LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 FLOAT VALVE SUSPECT LEAKING. 2 G 7 2 4U H10SW 1996071800628 19960718 00628 SW 1996 7 18 HEEA967527 1 19960709 A 2842 206364601101 TRANSMITTER BELL 206 206L3 1182108 SW FUEL QTY ERRATIC E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 6160Z 51610 FUEL QUANTITY READING ERRATIC. 1 G 7 1 3U H2SW 1996071800629 19960718 00629 1996 7 18 HEEA967528 4 19960709 A 3424 INDICATOR BELL 412 412 1182202 SW COCKPIT T&B INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2149S 36002 RATE TURN INDICATOR INOPERATIVE. 1 G 7 2 4U H4SW 1996071800630 19960718 00630 NE 1996 7 18 HEEA967532 1 19960709 A 7334 7645001078118 TRANSMITTER SKRSKY S76 S76A 8143006 NE FUEL PRESS DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 911MJ 760231 CAUSING ERONEOUS PRESSURE READINGS. 1 G 7 2 3U H1NE 1996071800631 19960718 00631 1996 7 18 HEEA967533 4 19960709 A 2230 7611123 AMPLIFIER SKRSKY S76 S76A 8143006 NE PITCH SLICE INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5427S 760168 PITCH CHANNEL INOPERATIVE. 1 G 7 2 3U H1NE 1996071800632 19960718 00632 NE 1996 7 18 HEEA967539 1 19960709 A 6410 7610105101041 BLADE SKRSKY S76 S76A 8143006 NE T/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 4167 760035 THE ABRASION STRIP ON PADDLE "B" HAS A CHIP MISSING ON THE INBOARD SECTION. PADDLE "A" IS ALSO CRACKED. 1 G 7 2 3U H1NE 1996071800633 19960718 00633 NE 1996 7 18 HEEA967545 1 19960709 A 6410 7610105101041 BLADE SKRSKY S76 S76A 8143006 NE T/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 706AE 5456 760275 PART IS CRACKED. (THE ABRASION STRIP ON PADDLE "A" HAS A CRACK WITH MULTIPLE BRANCHES. 1 G 7 2 3U H1NE 1996071800634 19960718 00634 NE 1996 7 18 HEEA967549 1 19960709 A 6210 7615009043051 TIP CAP SKRSKY S76 S76A 8143006 NE M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 706AE 760275 TIP CAP IS CRACKED. (TIP CAP HAS THE ABRASION STRIP CRACK AND SEPARATED. ALSO HAS SEPARATION ON THE OUTER AND INNER DO UBLER. 1 G 7 2 3U H1NE 1996071800635 19960718 00635 NE 1996 7 18 HEEA967551 1 19960709 A 6210 7615009100051A BLADE SKRSKY S76 S76A 8143006 NE M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 15460 7237 760223 BLADE IS CRACKED. (SEVERAL CRACKS ON THE TITANIUM STRIP WITH SEPARATION. THE CRACK AT STA. 123" HAS MULTIPLE BRANCHES. 1 G 7 2 3U H1NE 1996071800636 19960718 00636 1996 7 18 HEEA967568 4 19960710 A 3444 066104800 ALTIMETER KRA405 SKRSKY S76 S76A 8143006 NE COCKPIT RAD ALT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5426U 760167 RADAR ALTIMETER READS 50 FEET ON GROUND. (NEEDLE ON INDICATOR SPINS CONSTANTLY AND FLUCTUTATES INTERMITTENTLY) 1 G 7 2 3U H1NE 1996071800637 19960718 00637 1996 7 18 HEEA967570 4 19960710 A 3442 MI5852013 INDICATOR P4001 SKRSKY S76 S76A 8143006 NE RADAR FAIL;ED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 707AE 760276 TARGET ALERT DOESN'T FUNCTION PROPERLY (BROKEN CRT AND NO DISPLAY) 1 G 7 2 3U H1NE 1996071800639 19960718 00639 1996 7 18 HEEA967573 4 19960710 A 3453 25410038 LORAN 7000CDU SKRSKY S76 S76A 8143006 NE COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1545K 760047 SEVERAL LED SEGMENTS UNREADABLE. 1 G 7 2 3U H1NE 1996071800640 19960718 00640 1996 7 18 HEEA967574 4 19960710 A 2312 4000106010 CONTROL UNIT SKRSKY S76 S76A 8143006 NE COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 707AE 760276 DISPLAY WILL NOT DIM. REPLACED PHOTOCELL RT1. REPAIRED. ALSO REPLACED INTERMITTENT THUMBWHEEL ASSY. FOUND WITH TRANSM ITTER MANUAL/GD SWITCH TO GD, AND TRYING TO LOAD A FREQUENCY INTO THE RECEIVE PRESET POSITION, DISPLAY WOULD BLANK. FOU ND SOLDER BRIDGE ON PINS OFSELECTOR SWITCH S2. REMOVED SOLDER BRIDGE. REPAIRED PROBLEM. BENCH CHECK GOOD. 1 G 7 2 3U H1NE 1996071800641 19960718 00641 1996 7 18 HEEA967575 4 19960710 A 3451 066106600 TRANSCEIVER SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 707AE 760276 TRANSCEIVER WILL NOT RECEIVE ON ANY CHANNEL. 1 G 7 2 3U H1NE 1996071800642 19960718 00642 1996 7 18 HEEA967580 4 19960710 A 3453 27098292 ANTENNA SKRSKY S76 S76A 8143006 NE LORAN WEAK E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1545X 760050 LORAN ANTENNA WEAK SIGNAL STRENGTH. 1 G 7 2 3U H1NE 1996071800643 19960718 00643 EU 1996 7 18 KCDA962 1 19960610 A 2822 6404284 CONNECTOR AEROSP AS355 AS355F1 8680810 EU BOOST PUMP WIRE FAILED E KCDA K NONE O OTHER IN INSP/MAINT 1 SO 15 5802X 7456 5225 PILOT REPORTED LH FUEL BOOST PUMP INOPERATIVE. FOUND ELECTRICAL CONNECTOR AT 15 ALPHA PANEL TO BE BLACKENED AND DEFORMED DUE TO APPARENT ELECTRICAL SHORT. ONE WIRE IN CONNECTOR HAD BURNED ITSELF WHICH CAUSED PUMP TO GO INOP. FUSE IN CIRCUIT DID NOTOPEN. THIS IS A SECOND OCCURENCE. FIRST OCCURENCE WAS ON RH SYSTEM. REMOVED AND REPLACED CONNECTOR. PUMP OPERATE S NORMALLY. 1 G 7 2 3U H11EU 1996071800644 19960718 00644 EU 1996 7 18 96ZZZX3577 1 19960302 A 5210 1172428111 CATCHER BOLKMS 117 BK117B1 5626012 EU LT DOOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 17SJ 405 7230 CATCHER WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996071800647 19960718 00647 EU 1996 7 18 96ZZZX3580 1 19960307 A 6320 6607A2114 SWITCH BOLKMS 105 BO105LSA3 5626020 EU GEARBOX FAILED A R7MA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 NM 11 203LF 175 T16986 2015 GEARBOX OIL PRESSURE SWITCH INOPERATIVE. LOW PRESSURE WARNING LIGHT WILL NOT COME ON AT SHUT-DOWN. REPLACED WTIH NEW U NIT, CORRECTED PROBLEM. 1 G 7 2 3U H3AU 1996071800648 19960718 00648 EU 1996 7 18 96ZZZX3581 1 19960401 A 6320 6607A2114 SWITCH BOLKMS 105 BO105LSA3 5626020 EU GEARBOX MALFUNCTION A R7MA K NONE N FALSE WARNING IN INSP/MAINT 1 NM 11 203LF 62 T16987 2015 GEARBOX OIL PRESSURE SWITCH INOPERATIVE. CAUSES LOW PRESSURE WARNING LIGHT AT FLIGHT IDLE. REPALCED WITH NEW UNIT, COR RECTED PROBLEM. 1 G 7 2 3U H3AU 1996071800649 19960718 00649 EU 1996 7 18 96ZZZX3582 1 19960329 A 5210 F4154 SPRING BOLKMS 105 BO105LSA3 5626020 EU DOOR WEAK A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 203LF 348 2015 DOOR GAS SPRING WEAK. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H3AU 1996071800650 19960718 00650 EU 1996 7 18 96ZZZX3583 1 19960217 A 6420 1053170023 BEARING BOLKMS 117 BK117B1 5626012 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 417BK 149 7143 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996071800651 19960718 00651 EU 1996 7 18 96ZZZX3584 1 19960324 A 7712 G555674 TRANSDUCER BOLKMS 117 BK117B1 5626012 EU COCKPIT TORQUE DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 5194C 546 836 7169 TRANSDUCER SENDING FALSE SIGNALS TO TORQUE METER. REPLACED WTIH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996071800652 19960718 00652 EU 1996 7 18 96ZZZX3585 1 19960103 A 6410 134617P BUSHING BOLKMS 117 BK117B1 5626012 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 5194C 535 7169 TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996071800653 19960718 00653 EU 1996 7 18 96ZZZX3586 1 19960103 A 6410 134616P BUSHING BOLKMS 117 BK117B1 5626012 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 5194C 535 7169 TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996071800654 19960718 00654 EU 1996 7 18 96ZZZX3587 1 19960110 A 5210 1172428112 CATCHER BOLKMS 117 BK117B1 5626012 EU RT DOOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 5194C 771 7169 RIGHT CATCHER WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996071800656 19960718 00656 EU 1996 7 18 96ZZZX3589 1 19960227 A 3243 01005101 MASTER CYLINDER PARKERHANFIN BOLKMS 117 BK117A4 5626017 EU BRAKE LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 586BH 3 7129 MASTER CYLINDER LEAKING BEYOND SERVICEABLE LIMITS. REPALCED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996071800657 19960718 00657 EU 1996 7 18 96ZZZX3590 1 19960328 A 6210 10513103505 BLADE PIN BOLKMS 117 BK117B1 5626012 EU M/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 7060G 827 180663 7173 BLADE PIN WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996071800658 19960718 00658 EU 1996 7 18 96ZZZX3591 1 19960328 A 6210 10513103505 BLADE PIN BOLKMS 117 BK117B1 5626012 EU M/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 7060G 752 181330 7173 BLADE PIN WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996071800659 19960718 00659 EU 1996 7 18 96ZZZX3592 1 19960328 A 6210 10513103505 BLADE PIN BOLKMS 117 BK117B1 5626012 EU M/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 7060G 752 181284 7173 BLADE PIN WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996071800660 19960718 00660 EU 1996 7 18 96ZZZX3593 1 19960328 A 6210 10513103505 BLADE PIN BOLKMS 117 BK117B1 5626012 EU M/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 7060G 752 181251 7173 BLADE PIN WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996071800661 19960718 00661 NM 1996 7 18 96ZZZX3594 1 19960617 A 2913 900H3821501103 PUMP DOUG MD900 MD900 3027375 NM HYD DUAL SYS LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 901CF 65 0066380039 90000012 PUMP LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH USED UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1996071800662 19960718 00662 NM 1996 7 18 96ZZZX3595 1 19960617 A 6310 900D1400528101 PINION ASSY DOUG MD900 MD900 3027375 NM ENG/XMSN LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 901CF 656 0062190077 90000012 PINION ASSY LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1996071800663 19960718 00663 NM 1996 7 18 96ZZZX3596 1 19960617 A 6310 900D1400528101 PINION ASSY DOUG MD900 MD900 3027375 NM ENG/XMSN LEAKING A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 457 0062190015 90000012 PINION ASSY LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1996071800664 19960718 00664 EU 1996 7 18 96ZZZX3597 1 19960208 A 6420 1053170018 BOLT BOLKMS 117 BK117A4 5626017 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911BY 543 7127 BOLT WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996071800668 19960718 00668 EU 1996 7 18 96ZZZX3601 1 19960125 A 6410 134616P BUSHING BOLKMS 105 BO105S 5626006 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 722MB 751 S754 TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U H3EU 1996071800670 19960718 00670 SW 1996 7 18 96ZZZX3603 1 19960616 A 6310 222044607003 COUPLING BELL 230 230 1182149 SW ENG/XMSN CORRODED B TI1R K NONE O OTHER IN INSP/MAINT 1 SW 05 230JP 870 A739 23019 PITTING, CORROSION INSIDE COUPLING DUE TO APPARENT LACK OF COATING. 1 G 7 2 3U NC H9SW 1996071800671 19960718 00671 SW 1996 7 18 96ZZZX3604 1 19960616 A 6310 222044607003 COUPLING BELL 230 230 1182149 SW ENG/XMSN CORRODED B TI1R K NONE O OTHER IN INSP/MAINT 1 SW 05 230JP 870 23019 PITTING, CORROSION INSIDE COUPLING DUE TO APPARENT LACK OF COATING. 1 G 7 2 3U NC H9SW 1996071800672 19960718 00672 SW 1996 7 18 96ZZZX3605 1 19960617 A 6310 222044607003 COUPLING BELL 230 230 1182149 SW ENG/XMSN CORRODED B TI1R K NONE O OTHER IN INSP/MAINT 1 SW 05 230JP 870 A995 23019 PITTING, CORROSION INSIDE COUPLING DUE TO APPARENT LACK OF COATING. 1 G 7 2 3U NC H9SW 1996071800673 19960718 00673 SW 1996 7 18 96ZZZX3606 1 19960617 A 6310 222044607003 COUPLING BELL 230 230 1182149 SW ENG/XMSN CORRODED B TI1R K NONE O OTHER IN INSP/MAINT 1 SW 05 230JP 870 A813 23019 PITTING, CORROSION INSIDE COUPLING DUE TO APPARENT LACK OF COATING. 1 G 7 2 3U NC H9SW 1996071800688 19960718 00688 WP 1996 7 18 96ZZZX3622 1 19960611 A 3234 4501001 CONTROL HANDLE LKHEED 1011 1011385115 5265015 WP COCKPIT DEFECTIVE A RIAA K NONE J WARNING INDICATION AP APPROACH 1 SO 19 306GB 193U1138 RIA - FLT 103 - JSJ/MIA - DURING LANDING APPROACH WITH GEAR LEVER IN NEUTRAL POSITION, GEAR INTRANSIT (PILOTS PANEL). A LL 3 GEAR DOOR LIGHTS AND TAIL SKID LIGHTS ON (F/E PANEL) WITH GEAR LEVER UP, ALL LIGHTS OUT. ON LANDING, REMOVED AND R EPLACED LANDING GEAR CONTROL HANDLE. OPS CHECKED GOOD PER MM 32-61-00 (CYCLED LANDING GEAR). AIRCRAFT RELEASED TO SERV ICE. 2 L 7 3 4F A23WE 1996071800689 19960718 00689 SO 1996 7 18 96ZZZX3623 2 19960306 A 8550 SEPARATOR SCREEN CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO LT/RT ENGINE FROZE UP A BSAA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CL CLIMB 1 NM 05 2718Y 402C0232 BIL - ON TAKEOFF (AIRBORNE), OIL PRESSURE AT RED LINE, FUEL FLOW ERRATIC, MANIFOLD PRESS VERY SENSITIVE AND ERRATIC, FUE L PRESS EXCEEDED RED LINE. AIRCRAFT RETURNED AND LANDED UNEVENTFULLY. ALL TEMPS IN GREEN AT TAKEOFF. BOTH ENGINES NOT ED COVERED WITH OIL, BUT ENGINES STILL HAD OIL AND PRESS. AIR/OIL SEPARATORS FROZE UP BOTH ENGINES. CLEANED BOTH ENGIN ES AND COWLING. REMOVED AND CLEANED SEPARATOR SCREEN, HOUSING, AND DRAIN LINES BOTH ENGINES. DRAINED OIL AND INSPECTED MAGNETIC PLUGS BOTH ENGINES - NOTED CLEAN AND NORMAL. REMOVED BOTH ENGINE OIL FILTERS AND INSPECTED - CLEAN AND NORMAL . INSTALLED NEW FILTERS AND SERVICED BOTH ENGINES WITH OIL. GROUND RUN, OPS CHKD, AND LEAK CHKD NORMAL BOTH ENGINES. 1 L 7 2 3O 3 O A7CE E8CE 1996071800690 19960718 00690 WP 1996 7 18 96ZZZX3624 1 19960507 A 3350 58222 POWER SUPPLY DOUG DC9 DC941 302207N WP CABIN INOPERATIVE A TWAA K NONE L NO TEST CR CRUISE 1 CE 05 935L 47603 STL - FLT 661 - DURING CRUISE, EMERGENCY EGRESS LIGHTS ILLUMINATED. REMOVED AND REPLACED EMERGENCY EGRESS LIGHT POWER S UPPLY, MFG PN 5822-2. OPERATIONAL CHECK NORMAL. CHECK C - 8-27-95 - STL. 2 L 7 2 4F A6WE 1996071800691 19960718 00691 CE 1996 7 18 C2XA96IA144 1 19960611 A 3097 H31A8 WIRE BEECH 1900 1900D 1154162 CE RT WINDSHIELD CHAFED A C2XA A UNSCHED LANDING A FLAME/FIRE CR CRUISE 1 SW 09 81538 UE199 LAN - FLT 3123 - PILOT REPORTED THAT A FIRE AND SMOKE WERE NOTED COMING JUST BELOW THE COPILOT'S WINDSHIELD. THE CREW W AS ABLE TO EXTINGUISH THE FIRE AND LANDED AT LAN WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS INSPECTED AND FERRIED TO CL E WHERE MAINTENANCE FOUND THE POWER LEAD TO THE FIRST OFFICER'S WINDSHIELD TO HAVE BEEN CHAFING ON THE AIRFRAME. MAINTE NANCE REMOVED AND REPLACED THE WIRE AND ALL OTHER COMPONENTS AFFECTED BY THE DEFECTIVE WIRE AND THE AIRCRAFT WAS APPROVE D FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1996071800750 19960718 00750 NE 1996 7 18 96UAL900493 2 19960627 A 7200 ENGINE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE WING OUT OF BALANCE A UALA O OTHER E VIBRATION/BUFFET AP APPROACH 1 WP 29 945UA 26684 NUMBER TWO ENGINE HAD MAJOR VIBRATION. LANDED UNDER AMBER ALERT WITH EMERGENCY EQUIPMENT. *S/D* NUMBER TWO ENGINE WAS OUT OF BALANCE. ACCOMPLISHED A TRIM BALANCE. INITIAL OUT OF BALANCE CONDITION WAS, FAN 6 MILS AND TURBINE 3 MILS. AF TER TRIM, FAN .5 MILS AND TURBINE 1 MIL. 2 L 7 2 4F 4 F RT A16WE E2GL 1996071800751 19960718 00751 NM 1996 7 18 96UAL900508 1 19960708 A 2910 109661116 O-RING BOEING 65C163001 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 2 SPOILER LEAKING A UALA O OTHER J K WARNING INDICATION FLUID LOSS CR CRUISE 1 WP 29 7287U 21565 SYSTEM A-HYDRAULIC LEAK EN ROUTE. LANDED UNDER AMBER ALERT. *S/D* FOUND LEAKING O-RING ON NR 2 SPOILER FILTER. REPLA CED O-RING AND RESERVICED THE RESERVOIR, LEAK CHECKED OK. 2 L 7 3 4F 4 F A3WE E2EA 1996071800752 19960718 00752 NM 1996 7 18 96UAL900509 1 19960708 A 2530 27212110 TERMINAL STRIP BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE GALLEY DAMAGED A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 614UA 21875 AN ELECTRICAL SMOKE ODOR OCCURRED IN THE AFT GALLEY. *S/D* A LOOSE TERMINAL CAUSED THIS DISCREPANCY. THE TERMINAL STR IP FOR THE AFT CART CABLE ON RIGHT SIDE WAS REPLACED, OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 1996071800753 19960718 00753 WP 1996 7 18 96UAL900510 1 19960708 A 3250 4913802BW03110 FOLLOW-UP CABLE DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NLG BROKEN A UALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 29 1841U 46634 ON TAXI OUT NOSE STEERING FOLLOW-UP CABLE SNAPPED. *S/D* REPLACED LEFT HAND STEERING FOLLOW-UP CABLE. 2 L 7 3 4F 4 F A22WE E23EA 1996071800755 19960718 00755 NM 1996 7 18 96UAL900512 1 19960709 A 3350 M10699 POWER SUPPLY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 511UA 24799 CEILING EMERGENCY EXIT LIGHT INOP AT SEAT 17ABC. CHANGED POWER SUPPLY ITEM, EMERGENCY LIGHTS OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996071800756 19960718 00756 NM 1996 7 18 96UAL900513 1 19960709 A 2613 OVERHEAT LIGHT BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE BODY ILLUMINATED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 926UA 26648 BODY OVERHEAT LIGHT CAME ON, RETURNED TO SMF. 2 L 7 2 4F 4 F RT A16WE E2GL 1996071800757 19960718 00757 NM 1996 7 18 96UAL900514 1 19960709 A 3350 20131 BATTERY BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN DISCHARGED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 203UA 24718 EMERGENCY ESCAPE PATH LIGHTING INOPERABLE FROM ROW 16 AFT. REPLACED CABLE AND PLUG AND BATTERY PACK. CHECKS O.K. 2 L 7 2 4F 4 F RT A16WE E2GL 1996071800758 19960718 00758 NM 1996 7 18 96UAL900515 1 19960709 A 3397 58781 WIRE BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 9002U 19040 EMERGENCY ESCAPE PATH LIGHTING INOPERABLE FROM ROW 10 TO ROW 13. REPLACED POWER CABLE. CHECKS O.K. 2 L 7 2 4F 4 F A16WE E2EA 1996071800759 19960718 00759 NM 1996 7 18 96UAL900516 1 19960709 A 3350 20131 BATTERY BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN DISCHARGED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 335UA 24230 EMERGENCY ESCAPE PATH LIGHTING INOP FROM ROW 3 TO ROW 9 AND LEFT WING OVERWING EXIT LIGHT INOP. *S/D* REPLACED BATTERY PACK, CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1996071800760 19960718 00760 NM 1996 7 18 96UAL900517 1 19960710 A 2150 9131B506 RELAY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE GROUND COOLING FAILED A UALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 7459U 21913 RIGHT PACK OVER TEMPERATURE ON GROUND, SMOKE IN THE CABIN. ACFT RETURNED TO GATE. *S/D* REPLACED GROUND COOLING FAN A ND COOLING FAN RELAY. 2 L 7 3 4F 4 F A3WE E2EA 1996071800761 19960718 00761 NM 1996 7 18 96UAL900518 1 19960710 A 3220 162N1136 PIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NLG FAILED A UALA O OTHER E B VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 WP 29 584UA 10596 26706 AIRCRAFT EXPERIENCED HEAVY VIBRATION AND UNDER FUSELAGE SMOKE DURING LANDING SFO. AIRCRAFT TOWED TO GATE. NOSE LANDING GEAR LOWER TORSION LINK PIN FRACTURED CAUSING THE NOSE GEAR TO ROTATE 90 DEGREES AND THE AIRPLANE TO SKID DOWN THE RUNW AY TO A STOP. REPLACED PIN, LOWER TORSION LINK, AND INNER CYLINDER. TESTED AND OPERATION CHECKS NORMAL. PIN SENT TO B OEING FOR EVALUATION 7/14/96. EXPECT RESPONSE BY 10/15/96. 2 L 7 2 4F 4 F RT A2NM E17NE 1996071800762 19960718 00762 NM 1996 7 18 96UAL900519 1 19960711 A 3350 LIGHT BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE CABIN MALFUNCTIONED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 9012U 19050 EMERGENCY ESCAPE PATH LIGHTING INOP ROW 19. *S/D* THIS IS AN AREA THAT THE LIGHT STRIP MAKES A JOG AND THE STRIP IS NO T SUPPOSE TO LIGHT UP, SYSTEM IS OK. 2 L 7 2 4F 4 F A16WE E2EA 1996071800763 19960718 00763 NM 1996 7 18 96UAL900520 1 19960711 A 2612 FIRE WARNING BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE NR 2 ENGINE ACTIVATED A UALA A E F UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 WP 29 984UA 21642 NUMBER TWO ENGINE SHUT DOWN IN FLIGHT DUE TO FIRE WARNING, FIRE BOTTLE DISCHARGED. 2 L 7 2 4F 4 F A16WE E2EA 1996071800764 19960718 00764 NM 1996 7 18 96UAL900521 1 19960711 A 2822 BOOST PUMP CB BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE RT CTR TANK TRIPPED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 995UA 22399 THE LEFT HAND CENTER TANK FUEL BOOST PUMP PREVIOUSLY INOP ON CLIMB DUE TO POPPED CIRCUIT BREAKER, THE RIGHT CENTER TANK BOOST PUMP CIRCUIT BREAKER POPPED. RETURNED TO FIELD. 2 L 7 2 4F 4 F A16WE E2EA 1996071800765 19960718 00765 NM 1996 7 18 96UAL900522 1 19960711 A 3350 20131 BATTERY BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE CABIN DISCHARGED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 9011U 19049 LEFT OVERWING EMERGENCY EXIT LIGHT INOP. *S/D* REPLACED BATTERY IN OVERWING EMERGENCY LIGHT, CHECKS OK. 2 L 7 2 4F 4 F A16WE E2EA 1996071800766 19960718 00766 NM 1996 7 18 96UAL900523 1 19960711 A 2910 HYD FLUID BOEING 737 737291 138448W NM PWA JT8 JT8D9A 52048 NE A-HYD SYST LOST A UALA K NONE K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 983UA 21641 CREW REPORTS, AIRCRAFT EXPERIENCED THE LOSS OF 'A' SYSTEM HYDRAULICS ON FLAP RETRACTION AFTER TAKEOFF. RECEIVED LEADING EDGE AMBER INTRANSIT LIGHT AND NUMBER THREE FLAP LIGHT ON OVERHEAD PANEL. 2 L 7 2 4F 4 F A16WE E2EA 1996071800767 19960718 00767 NM 1996 7 18 96UAL900524 1 19960711 A 2120 AIR DISTR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE L2 DOOR FUEL ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 773UA 26929 FLIGHT ATTENDANT AT DOOR 2 LEFT REPORTS FUEL SMELL AFTER LIFT OFF AND ON FINAL DESCENT, NORMAL OTHER TIMES. 2 L 7 2 4F 4 F RT T0001SE E46NE 1996071800768 19960718 00768 NM 1996 7 18 96UAL900525 1 19960711 A 3350 EA1619 LAMP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE DOOR 1L INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 383UA 24658 EMERGENCY EXIT SLIDE LIGHT AT DOOR ONE LEFT INOP. RELAMPED, CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1996071800769 19960718 00769 NM 1996 7 18 96UAL900526 1 19960712 A 3350 LIGHT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7299U 21894 RIGHT HAND OVERWING EMERGENCY LIGHTS INOPERATIVE. 2 L 7 3 4F 4 F A3WE E2EA 1996071800770 19960718 00770 NM 1996 7 18 96UAL900527 1 19960712 A 2910 HYD FLUID BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE A-HYD SYST LOST A UALA O OTHER K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 WP 29 7264U 21411 LOST HYDRAULIC FLUID FROM A-SYSTEM DURING TAKEOFF. 2 L 7 3 4F 4 F A3WE E2EA 1996071800771 19960718 00771 WP 1996 7 18 96UAL900528 1 19960712 A 3397 558791 WIRE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1852U 47811 EEL LEFT SIDE FIRST CLASS AT FWD END PULLED LOOSE AND PIN BROKEN. *S/D* REPLACED EEL POWER FEEDER STRIP AT DOOR ONE LE FT. 2 L 7 3 4F 4 F A22WE E23EA 1996071800772 19960718 00772 WP 1996 7 18 96UAL900529 1 19960712 A 3350 362624 LIGHT DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1812U 46611 LAST THREE EEL LIGHT STRIPS INOPERATIVE IN FIRST CLASS RIGHT SIDE. REPLACED LIGHT ASSEMBLIES. 2 L 7 3 4F 4 F A22WE E23EA 1996071800773 19960718 00773 NM 1996 7 18 96UAL900530 1 19960712 A 2910 HYD FLUID BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE B-HYD SYST LOST A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 WP 29 7456U 21910 LOST ALL OF B-SYSTEM HYDRAULIC FLUID ON DEPARTURE, RETURNED TO SEA. 2 L 7 3 4F 4 F A3WE E2EA 1996071800774 19960718 00774 NM 1996 7 18 96UAL900531 1 19960712 A 2820 FUEL DISTR SYS BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1/3 TANKS MALFUNCTIONED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 7271U 21418 FUEL TANKS 1 AND 3 LOST 800 AND 500 POUNDS WHEN FEEDING FROM NR 2. 2 L 7 3 4F 4 F A3WE E2EA 1996071800775 19960718 00775 NM 1996 7 18 96UAL900532 1 19960712 A 2150 PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN SMOKING A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 7463U 21917 RIGHT PACK TRIPS IN MANUAL AND AUTO MODES WITH SMOKE IN THE AFT CABIN. 2 L 7 3 4F 4 F A3WE E2EA 1996071800776 19960718 00776 WP 1996 7 18 ABX9600595 1 19960712 A 3260 DOOR IND DOUG DC9 DC941 302207N WP LT/RT MLG MALFUNCTIONED A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 973AX 47511 AFTER TAKEOFF, WHEN THE GEAR WAS RETRACTED, THE GEAR DOOR OPEN AND LEFT AND RIGHT GEAR UNSAFE LIGHTS REMAINED ILLUMINATE D. RECYCLED, GEAR INDICATION NORMAL. PERFORMED LANDING GEAR TEST IAW DC-9 MM, THE INDICATION SYSTEM TEST NORMAL. 2 L 7 2 4F A6WE 1996071800777 19960718 00777 WP 1996 7 18 ABXA9600596 1 19960715 A 3231 39567851 LINKAGE DOUG DC9 DC932 3022066 WP RT NLG DOOR DEFECTIVE A ABXA K NONE J WARNING INDICATION AP APPROACH 1 GL 23 909AX 47148 FORWARD NOSE GEAR DOORS WILL NOT RETRACT. RECYCLED GEAR, NO HELP. REPLACED RIGHT NOSE GEAR LINKAGE IAW DC-9 MM. 2 L 7 2 4F A6WE 1996071800778 19960718 00778 WP 1996 7 18 ABXA9600597 1 19960716 A 2822 11230311 BOOST PUMP DOUG DC8 DC861 3021952 WP PWA JT3D JT3D3B 52039 NE NR4 ENGINE DEFECTIVE A ABXA K NONE X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 GL 23 845AX 5244 46157 669579 NR 4 ENGINE FEED PUMP PRESSURE LIGHT ILLUMINATED WHILE CLIMBING THROUGH 24,000 FEET AND ENGINE FLAMED OUT. CHECKLIST PR OCEDURES WERE ACCOMPLISHED AND THE ENGINE HAD RELIGHT. REPLACED BOOST AND FEED PUMPS FOR THE NR 4 ENGINE IAW DC8 MM, CH APTER 28-20-00. GROUND RAN ENGINE AND NO DEFECTS NOTED. NASH PUMP FILTER WAS REMOVED AND FOUND CLEAN. 2 L 7 4 4F 4 F 4A25 1E8 1996071800779 19960718 00779 WP 1996 7 18 CALA9601036 1 19960627 A 5350 LATCH DOUG DC9 DC932 3022066 WP TAILCONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 THE TAILCONE EXTERIOR RELEASE HANDLE PULLED LOW AT 20 POUNDS. TAILCONE LATCH WAS ADJUSTED AND THE EXTERIOR RELEASE HAND LE PULL TESTED WITHIN SPECIFICATIONS AT 34 POUNDS PER MM 53-50-3. 2 L 7 2 4F A6WE 1996071800780 19960718 00780 NM 1996 7 18 CALA9601037 1 19960711 A 5320 FRAME BOEING 737 737222 1384473 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12235 19758 INSPECTION FOUND A 3.75 INCH CRACK BELOW UPPER STOP FITTING OF FORWARD CARGO DOOR AFT FRAME. THE CRACKED SECTION OF FRA ME WAS CUT OUT, A FRAME SPLICE REPAIR WAS INSTALLED IAW ECRA 5365-01042. 2 L 7 2 4F A16WE 1996071800781 19960718 00781 WP 1996 7 18 MWEA96265 1 19960716 A 3350 1001591 FLASHLIGHT DOUG DC9 DC932 3022066 WP FWD ENTRY DOOR BROKEN SWITCH A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 202ME 47672 DURING INSP, FOUND FWD ENTRANCE DOOR EMERGENCY FLASHLIGHT ON AND OFF SWITCH BROKEN. REPLACED FLASHLIGHT ASSY, OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996071800782 19960718 00782 NM 1996 7 18 P5CA9600366 1 19960716 A 5280 65B1091728 SKIN BOEING 747 747124 1384874 NM RT MLG DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 RIGHT HAND BODY GEAR DOOR INNER SKIN CRACKED UNDER ATTACH ROD FITTING SUPPORT FRAME. REMOVED DAMAGED SECTION OF SKIN, I NSTALLED DOUBLER REPAIR ON INNER FRAME, INSTALLED DOUBLER ON DOOR INNER SKIN IAW SRM 51-40-02. 2 L 7 4 4F A20WE 1996071800783 19960718 00783 EU 1996 7 18 QXEA9600247 1 19960714 A 4900 APU FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 487US 11238 APU AUTO SHUTDOWN CABIN AND COCKPIT FILLED WITH SMOKE. AIRCRAFT WAS PARKED AT THE GATE. PROBLEM TRACED TO APU, APU PLA CED ON MEL 49-1. 2 L 7 2 4F RT A20EU 1996071800784 19960718 00784 EU 1996 7 18 QXEA9600248 1 19960714 A 2120 AIR DISTR FOKKER F28 F28MK4000 4990810 EU COCKPIT SMOKE A QXEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 09 487US 11238 AFTER TAKEOFF, VISUAL SMOKE WAS OBSERVED IN THE COCKPIT AND CABIN COMING FROM AIR CONDITIONING VENTS. AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT FURTHER PROBLEM. PROBLEM COULD NOT BE DUPLICATED ON GROUND. TEST FLIGHT CONDUCTED AND FLI GHT WAS SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. NO FURTHER PIREPS THROUGH 071796. APU WAS PLACED ON MEL, THE PREV IOUS FLIGHT FOR THE SAME PROBLEM. 2 L 7 2 4F RT A20EU 1996071800785 19960718 00785 NM 1996 7 18 QXEA9600249 1 19960714 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 826PH 214 LEFT HAND AFT EMERGENCY EXIT EGRESS LIGHT AND THIRD AND FOURTH FORWARD RED FLOOR PROXIMITY PATH LIGHTS ARE INOP. POWER SUPPLY, BATTERY PACKS REPLACED AND LIGHTS OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 1996071800786 19960718 00786 EU 1996 7 18 QXEA9600250 1 19960714 A 3350 MGG1280 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 462AU 11054 FORWARD CABIN EXIT SIGN HAS 6 OF 7 BULBS INOP. BULBS WERE REPLACED AND LIGHTS OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996071800787 19960718 00787 EU 1996 7 18 QXEA9600251 1 19960716 A 3350 MGG1280 BULB FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 478US 11227 EXIT SIGN OVER COCKPIT DOOR IS DIM 28V. BULBS WERE REPLACED AND SIGN OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996071800788 19960718 00788 EU 1996 7 18 QXEA9600252 1 19960716 A 3350 MGG1280 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 469US 11096 MID CABIN EMERGENCY LIGHT FACING AFT HAS SEVERAL BULBS INOP. BULBS WERE REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996071800789 19960718 00789 EU 1996 7 18 QXEA9600253 1 19960716 A 3350 1315 BULB FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 487US 11238 EMERGENCY LIGHT OVER EXIT 9E IS OUT. BULBS WERE REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996071800790 19960718 00790 WP 1996 7 18 RRXA96033 1 19960711 A 2612 CONNECTOR DOUG DC8 DC871F 302199D WP NR4 ENG FIRE DET FAILED A RRXA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 15 500MH 45812 NR 4 ENGINE IN CRUISE HAD AN INTERMITTENT FIRE WARNING, THROTTLE WAS RETARDED TO IDLE, BLEED AND GENERATOR WERE TURNED O FF. LIGHT WENT OUT, LATER FIRE WARNING CAME ON AGAIN STEADY. ENGINE WAS SHUTDOWN AND FIRE BOTTLES DISCHARGED. REMOVED AND REPLACED NR 4 ENGINE FIRE BOTTLES, INSTALLED 4 SQUIBS ON SAME. ACCOMPLISHED A COMPLETE ELECTRICAL WIRING SHAKE OF NR 4 ENGINE FIRE WARNING SYSTEM. REMOVED AND REPLACED CONNECTOR ON FWD END OF RT FAN FIRE LOOP NR 4 ENGINE. RECONNECTE D NR 4 ENG CSD, FIRE WARNING AND GENERATOR OPS NORMAL ON NR 1 AND NR 4 ENGINE RUN. 2 L 7 4 4F RT 4A25 1996071800791 19960718 00791 NE 1996 7 18 RRXA96034 2 19960711 A 7200 ENGINE DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C1 13802 NE NR 4 FLAMED OUT A RRXA O OTHER X ENGINE FLAMEOUT DE DESCENT 1 WP 15 8087U 45977 NR 4 ENGINE FLAMED OUT DURING DESCENT. RAN ENGINE FLAME-OUT CHECKLIST, ENGINE RELIT AND OPERATED NORMAL FOR REST OF TRI P. COMPLIED WITH ENGINE FLAME-OUT CHECKLIST IAW CFM56-2C CHAPTER 71-00-00. FOUND MOISTURE IN NR 4 MAIN TANK, RETURNED NR 4 ENGINE TO SERVICE. 2 L 7 4 4F 4 F RT 4A25 E2GL 1996071800792 19960718 00792 WP 1996 7 18 SCNA96192 1 19960715 A 3350 LIGHT DOUG DC10 DC1010 3022110 WP CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 571SC 46645 EMERGENCY TRACK LIGHTING IS INOPERATIVE AT ROW 6, BOTH SIDES. REPAIRED BROKEN WIRE IN TRACK ON BOTH SIDES. TRACK LIGHTI NG CHECKED GOOD PER 33-50-00. 2 L 7 3 4F A22WE 1996071800793 19960718 00793 NM 1996 7 18 SCNA96193 1 19960714 A 2910 65178444440 HYDRAULIC LINE BOEING 727 7272J4 1384006 NM A-HYD SYSTEM LEAKING A SCNA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 15 285SC 21676 ON FINAL, LOST SYSTEM-A FLUID. MANUALLY EXTENDED GEAR AND LANDED NORMALLY. REMOVED AND REPLACED HYDRAULIC LINE, PERFOR MED OPERATIONAL AND LEAK CHECK. 2 L 7 3 4F RT A3WE 1996071800794 19960718 00794 NM 1996 7 18 SCNA96194 1 19960710 A 3350 S106 BATTERY BOEING 727 7272J4 1384006 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 284SC 21438 FOUND AFT ENTRY OVERHEAD EMERGENCY PORTABLE AREA LIGHTING INOP. REMOVED AND REPLACED BATTERY PACK IN ACCORDANCE WITH MM 33-50-101, SYSTEM OPS CHECKS NORMAL. 2 L 7 3 4F RT A3WE 1996071800795 19960718 00795 NM 1996 7 18 SCNA96195 1 19960710 A 3350 6105771 BATTERY BOEING 727 7272J4 1384006 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 284SC 21438 FOUND L2 AND R2 EMERGENCY DOOR SLIDE LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK IN ACCORDANCE WITH MM 33-50-51, SYS TEM OPS CHECKS NORMAL. 2 L 7 3 4F RT A3WE 1996071800796 19960718 00796 WP 1996 7 18 SCNA96196 1 19960714 A 2150 7012505 CHECK VALVE DOUG DC10 DC1015 3022118 WP NR 2 PACK INOPERATIVE A SCNA A J UNSCHED LANDING DUMP FUEL O OTHER NR NOT REPORTED 1 GL 15 151SY 48295 UNABLE TO PRESSURIZE CABIN, DUMPED APPROXIMATELY 30,000 POUNDS OF FUEL AND RETURNED TO LAS. FOUND CHECK VALVE (P/N 7012 -505) TO BE INOP IN NUMBER 2 PACK AND A BLOWN AIR CONDITIONING DUCT (P/N 7009-605). REMOVED AND REPLACED BOTH PARTS IAW MM 21-30-0. DUCT LEAK AND CHECK VALVE OPERATIONAL CHECKS WERE PERFORMED. 2 L 7 3 4F A22WE 1996071800797 19960718 00797 SO 1996 7 18 SRAA960705 1 19960715 A 3230 8430M2 BALLSCREW LKHEED 382 382G 526414U SO RT MLG WORN A SRAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 909SJ 4763 AFTER TAKEOFF, NOTICED RIGHT MLG WAS SLOW TO RETRACT. RECYCLED GEAR AND ACCOMPLISHED AIR TURNBACK, LANDING WITHOUT INCI DENT. CONTINUED A SERIES OF 3 FLIGHTS WITH GEARS DOWN, AT ANC THE FINAL DESTINATION THE RIGHT MLG WAS INSPECTED AND FOU ND THE FORWARD BALLSCREW WORN. REPLACED UNIT AND PERFORMED OPS CK PER MM CH 32. 2 H 7 4 4T A1SO 1996071800798 19960718 00798 NE 1996 7 18 96ZZZM1074 2 19960609 A 7230 COMPRESSOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 2 ENGINE STALLED A TWAA O OTHER R PARTIAL RPM/PWR LOSS CL CLIMB 1 CE 05 902TW 49153 3227 SLC - DURING CLIMB, SHUT DOWN NR 2 ENGINE DUE TO COMPRESSOR STALLS. FOUND METAL PARTICLES IN ENGINE BLEED AIR DUCT AND CAPS. CHANGED ENGINE. ENGINE OPERATION THEN CHECKED NORMAL. (M) 2 L 7 2 4F 4 F A6WE E9NE 1996071800799 19960718 00799 WP 1996 7 18 96ZZZM1075 1 19960625 A 2400 CONDUIT DOUG DC9 DC932 3022066 WP WS 115 CUT A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 906VJ 68239 47379 DURING MAINTENANCE, WHILE VERIFYING FLAP FOLLOW-UP CABLES FOR PROPER INSTALLATION PER FLEET CAMPAIGN 2296. FOUND LT AIL ERON UP CABLE NR 35 IN LEFT WHEEL WELL CHAFING THROUGH ELECTRICAL CONDUIT APPROX ONE INCH LONG BY .1875 INCH DEEP. 2 L 7 2 4F A6WE 1996071800800 19960718 00800 NE 1996 7 18 96ZZZM1076 2 19960617 A 7261 793651 OIL PRESS TUBE BOEING 727 727225 1384077 NM PWA JT8 JT8D15A 52051 NE NR 2 ENG FRACTURED A MYWA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 19 804MA 22435 IN CRUISE AT FL 330, NR 2 ENGINE, AFTER ONE AND ONE QUARTER HOURS OF FLIGHT, LOW OIL/FILTER LIGHT CAME ON. OIL QUANTITY DROPPED TO HALF GALLON. OIL PRESSURE DROPPED TO 20-30 PSI. SHUTDOWN IN FLIGHT WITH CUTOFF SWITCH. FOR REMAINING 30 M INUTES OF FLIGHT WHILE WINDMILLING MAINTAINED POSITIVE OIL PRESSURE. AN OPERATIONAL DECISION WAS MADE TO REPLACE THE EN GINE. IN THE SHOP, ISOLATED THE CAUSE OF THE OIL LOSS TO A BROKEN NR 6 BEARING OIL PRESSURE TUBE. (M) 2 L 7 3 4F 4 F A3WE E2EA 1996071800801 19960718 00801 WP 1996 7 18 96ZZZM1077 2 19960618 A 7321 21011445 EEC BRAERO DH125 HS125700A 4230170 EU GARRTT TFE731 TFE7313 01518 WP LT ENG FAILED A KKYA O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 NE 03 270KA 9 NA0307 EN ROUTE FROM HOU TO APA WHILE CRUISING AT 35,000 FEET, THE LEFT ENGINE ROLLED BACK TO FLIGHT IDLE WITH NO PILOT INPUT. THE ENGINE WAS SWITCHED TO MANUAL MODE AND OPERATION WAS RESTORED TO NORMAL. THE AIRCRAFT LANDED WITHOUT INCIDENT. TH E ELECTRONIC ENGINE COMPUTER WAS CHANGED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F A3EU E6WE 1996071800802 19960718 00802 1996 7 18 96ZZZM1078 4 19960529 A 3442 20671570153 RT UNIT DOUG DC9 DC932 3022066 WP WEATHER RADAR MALFUNCTIONED A VJ6A A UNSCHED LANDING O OTHER CL CLIMB 1 SO 11 946VV 47226 ON FLT 537 - ATL-TPA - AIR RETURN, WEATHER RADAR HAS 'NO RETURNS' IN FLIGHT GROUND TEST NORMAL. REMOVED R/T AND ANTENNA , OPS CHECK NORMAL PER MM 34-40. (M) 2 L 7 2 4F A6WE 1996071800803 19960718 00803 1996 7 18 96ZZZM1079 4 19960529 A 3442 20871790501 ANTENNA DOUG DC9 DC932 3022066 WP WEATHER RADAR MALFUNCTIONED A VJ6A A UNSCHED LANDING O OTHER CL CLIMB 1 SO 11 946VV 47226 ON FLT 537 - ATL-TPA - AIR RETURN, WEATHER RADAR HAS 'NO RETURNS' IN FLIGHT GROUND TEST NORMAL. REMOVED R/T AND ANTENNA , OPS CHECK NORMAL PER MM 34-40. (M) 2 L 7 2 4F A6WE 1996071800804 19960718 00804 WP 1996 7 18 96ZZZM1080 1 19960610 A 2730 92747813 TRIM BRAKE RELAY DOUG DC9 DC932 3022066 WP PRIMARY TRIM FAILED A VJ6A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 930VV 47723 OFN FLT 396 - ATL-RDU - THE PRIMARY TRIM STOPPED WORKING APPROXIMATELY 5 MINUTES AFTER TAKEOFF. REMOVED AND REPLACED TH E PRIMARY TRIM BRAKE RELAY, OPS CK IAW 27-40. (M) 2 L 7 2 4F A6WE 1996071800805 19960718 00805 WP 1996 7 18 96ZZZM1081 1 19960516 A 3610 460300 SEAL DOUG DC9 DC932 3022066 WP TAIL COMPT FAILED A VJ6A D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SO 11 932VV 47451 ON FLT 498 - ATL-PHF - GATE RETURN, THE TAIL COMPARTMENT HIGH TEMP LIGHT CAME ON DURING TAXI. REPLACED LEAKING SLIP JOI NT SEAL. (M) 2 L 7 2 4F A6WE 1996071800806 19960718 00806 WP 1996 7 18 96ZZZM1082 1 19960516 A 2150 4667761 ACM DOUG DC9 DC932 3022066 WP LEFT FAILED A VJ6A O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 11 919VV 47260 THE LEFT ACM OVERHEATED AND FILLED THE CABIN WITH SMOKE, EVACUATED THE AIRCRAFT AT THE GATE. REMOVED AND REPLACED LEFT ACM, IAW MM 21-50-2, OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1996071800807 19960718 00807 WP 1996 7 18 96ZZZM1083 1 19960521 A 2150 ACM DOUG DC9 DC932 3022066 WP LEFT OVERHEATED A VJ6A O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 11 919VV 47260 LEFT ACM OVERHEATED, FILLED CABIN WITH SMOKE, EVACUATED AIRCRAFT. AIRCRAFT WAS AT GATE. SECURED SENSE LINE ON LEFT FLO W CONTROL VALVE, OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1996071800808 19960718 00808 WP 1996 7 18 96ZZZM1084 1 19960516 A 2613 HIGH TEMP LIGHT DOUG DC9 DC932 3022066 WP TAIL COMPT ILLUMINATED A VJ6A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 932VV 47451 THE TAIL COMPARTMENT HIGH TEMP LIGHT CAME ON IN FLIGHT. (M) 2 L 7 2 4F A6WE 1996071800809 19960718 00809 WP 1996 7 18 96ZZZM1085 1 19960610 A 2613 TEMP SENSOR DOUG DC9 DC932 3022066 WP TAIL COMPT AIR LEAK A VJ6A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 930VV 47723 ON FT 396 - ATL-RDU - THE TAIL COMPARTMENT HIGH LIGHT CAME ON APPROXIMATELY 4-5 MINUTES AFTER TAKEOFF. FOUND A/C TEMP H IGH SENSOR LEAKING AIR, REMOVED AND REPLACED THE TEMP SENSOR AND SEAL PER MM 36-00. OPS CHECK AND LEAK CHECK OK. (M) 2 L 7 2 4F A6WE 1996071800811 19960718 00811 WP 1996 7 18 96ZZZM1087 1 19960429 A 5330 SKIN REPAIR DOUG DC9 DC932 3022066 WP BS 242 CRACKED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 916VV 47445 DURING C-CHECK, FOUND TEMPORARY REPAIR INSTALLED ON LEFT SIDE OF FUSELAGE FS 242 AT LONGERONS 17 AND 18, ALSO FINGER DOU BLER CRACKED SAME AREA. REMOVED TEMPORARY REPAIR, FABRICATED AND INSTALLED PERMANENT REPAIR TO PLATING AND FINGER DOUBL ER IAW EA 12-5304-29-C0918R1. (M) 2 L 7 2 4F A6WE 1996071800812 19960718 00812 WP 1996 7 18 96ZZZM1088 1 19960506 A 5311 2779306 FRAME DOUG DC9 DC932 3022066 WP BS 965 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 914VV 47486 DURING C-CHECK, FOUND CORROSION ON AFT SIDE OF FLOOR FRAME F/S 965 AT LONGERONS 23 TO 30 LEFT. REMOVED CORROSION AND FO UND TO BE BEYOND LIMITS, FABRICATED FRAME AND SPLICE REPAIRS IAW SRM 53-03 AND HEAT TREATED IAW SRM 51-10-2A. INSTALLED REPAIR IAW SRM 51-30-2 PARA 1-12 FIG 1-23 AND 53-03 PARA 1 FIG 1-7. (M) 2 L 7 2 4F A6WE 1996071800813 19960718 00813 WP 1996 7 18 96ZZZM1089 1 19960527 A 5311 99196181N FRAME DOUG DC9 DC932 3022066 WP BS 718 CRACKED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 905VJ 47378 DURING 'A' CHECK, FOUND CRACK IN LEFT WHEEL WELL AT STATION 718 ON FRAME FITTING ABOVE TRAPIZOID PANEL. REMOVED STATION 718 FRAME, INTERCOSTALS AND SEAT TRACK IAW DC-9 SB 53-131. INSTALLED NEW FRAME AND ATTACHMENTS DRILLED HOLE IAW DC-9 S RM 51-10-4. INSTALLED FASTENERS IAW DC-9 SRM 51-30-5, 51-30-2, 51-30-8 AND 51-30-1. SPLICED IN SEAT TRACK IAW DC-9 SRM 53-05 FIG 4. INSTALLED MAIN FRAME AND INTERCOSTALS. (M) 2 L 7 2 4F A6WE 1996071800814 19960718 00814 EU 1996 7 18 96ZZZM1090 1 19960619 A 7712 KJA6T11F35S CONNECTOR BAG JETSTM JETSTM3201 1500217 EU LT ENGINE DIRTY A VTZA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 27 489UE 908 FLT 6407 - LGA-IAD - ABORTED TAKEOFF DUE TO THE LEFT EGT FLUCTUATING. EGT FLUCTUATIONS STABILIZED WITH SRL SELECTED OFF . MX OPENED DMI NR 55614 IAW MEL 76-1. MX LATER CLEARED DMI NR 55614 ON 6-20-96 BY CLEANING ZONE 2 CANNON PLUG AND THE STRAIN GAUGE CANNON PLUG. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. REFERENCE VTZA96224. 2 L 7 2 4T RT A56EU 1996071800815 19960718 00815 EU 1996 7 18 96ZZZM1091 1 19960624 A 5210 137968C HANDLE ASSY BAG JETSTM JETSTM3201 1500217 EU PAX DOOR OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 491UE 911 FLT NR 6314 - IAD-BUF - ABORTED TAKEOFF DUE TO THE PASSENGER DOOR WARNING LIGHT ILLUMINATING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MX ADJUSTED DOOR HANDLE, CLEANED AND LUBED MICROSWITCHES AND PLUNGERS. REPLACED WORN DOOR BUSHING. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. REFERENCE VTZA96228. 2 L 7 2 4T RT A56EU 1996071800816 19960718 00816 EU 1996 7 18 96ZZZM1092 1 19960624 A 5210 1371382C401 DRAW BOLT ASSY BAG JETSTM JETSTM3201 1500217 EU PAX DOOR DIRTY A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 491UE 911 FLT NR 6314 - IAD-BUF - ABORTED TAKEOFF DUE TO THE PASSENGER DOOR WARNING LIGHT ILLUMINATING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MX ADJUSTED DOOR HANDLE, CLEANED AND LUBED MICROSWITCHES AND PLUNGERS. REPLACED WORN DOOR BUSHING. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. REFERENCE VTZA96228. 2 L 7 2 4T RT A56EU 1996071800817 19960718 00817 EU 1996 7 18 96ZZZM1093 1 19960624 A 5270 91SE16 SWITCH BAG JETSTM JETSTM3201 1500217 EU PAX DOOR DIRTY A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 491UE 911 FLT NR 6314 - IAD-BUF - ABORTED TAKEOFF DUE TO THE PASSENGER DOOR WARNING LIGHT ILLUMINATING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MX ADJUSTED DOOR HANDLE, CLEANED AND LUBED MICROSWITCHES AND PLUNGERS. REPLACED WORN DOOR BUSHING. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. REFERENCE VTZA96228. 2 L 7 2 4T RT A56EU 1996071800818 19960718 00818 NM 1996 7 18 96ZZZM1094 1 19960404 A 5320 DOUBLER BOEING 727 727232 1384082 NM BS 724-728 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 17789 20643 LEVEL 2 CORROSION ON SKIN DOUBLER AT STATION 724A TO 728A BL0. REMOVED EXISTING DOUBLER AND REPLACED WITH NEW PER SRM 5 3-30-3 FIG 1. (M) 2 L 7 3 4F A3WE 1996071800819 19960718 00819 NM 1996 7 18 96ZZZM1095 1 19960404 A 5320 SHEAR TIE BOEING 727 727232 1384082 NM BS 720 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 17789 20643 LEVEL 2 CORROSION ON SHEAR TIE AT STATION 720A STRINGER 28L. REMOVED AND REPLACED SHEAR TIE PER SRM 53-10-4 FIG 15. 2 L 7 3 4F A3WE 1996071800820 19960718 00820 NM 1996 7 18 96ZZZM1096 1 19960319 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM CABIN CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 17789 20643 AFT MAIN CABIN HAS LEVEL 2 CORROSION ON SEAT TRACK RBL 24 INCHES STATION 1050 TO 1110. REMOVED CORROSION PER SRM 51-10- 16 AND REPLACED SEAT TRACK FROM STATION 1070 TO 1132 PER SRM 53-10-5. 2 L 7 3 4F A3WE 1996071800821 19960718 00821 NM 1996 7 18 96ZZZM1097 1 19960229 A 5543 SKIN BOEING 727 727232 1384082 NM RUDDER TAB DELAMINATED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 17789 20643 UPPER RUDDER TAB HAS DELAM AT UPPER TRAILING EDGE AND AT LOWER FACE. INSTALLED FILLER/DOUBLER AND HONEY COMB TO UPPER R UDDER TAB. INSTALLED HONEY COMB TO LOWER RUDDER TAB PER SRM 51-40-6. FIBERGLASS HOT BOND REPAIRS. (M) 2 L 7 3 4F A3WE 1996071800828 19960718 00828 NM 1996 7 18 AALA960743 1 19960503 A 5315 141N5113 FLOOR BEAM BOEING 757 757223 1384957 NM BS 377 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 645AA 24603 AFW - FOUND FLOOR BEAM AT STATION 377 HAD 6 AREAS OF CORROSION BLENDED BEYOND SRM LIMITS, PER MRB 757-822. (M) 2 L 7 2 4F RT A2NM 1996071800829 19960718 00829 NM 1996 7 18 AALA960744 1 19960503 A 5315 146N5089 FLOOR BEAM BOEING 757 757223 1384957 NM BS 1640 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 645AA 24603 AFW - FOUND FLOOR BEAM AT STATION 1640 HAS CORROSION REMOVED BEYOND SRM LIMITS, PER MRB 757-826. (M) 2 L 7 2 4F RT A2NM 1996071800830 19960718 00830 NM 1996 7 18 AALA960745 1 19960503 A 5230 146N8522 SILL BOEING 757 757223 1384957 NM CARGO DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 645AA 24603 AFW - FOUND LOWER MAIN SILL, UPPER CHORD, NR 2 CARGO DOOR CUTOUT HAS CORROSION REMOVED ON UPPER AND LOWER SURFACES. COR ROSION REMOVED IS BEYOND SRM LIMITS, PER MRB 757-831. (M) 2 L 7 2 4F RT A2NM 1996071800831 19960718 00831 NM 1996 7 18 AALA960746 1 19960503 A 5315 141N5112 FLOOR BEAM BOEING 757 757223 1384957 NM BS 365 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 645AA 24603 AFW - FOUND FLOOR BEAM AT STATION 365 HAS CORROSION ON UPPER SURFACE BLENDED BEYOND SRM LIMITS, PER MRB 757-821. (M) 2 L 7 2 4F RT A2NM 1996071800832 19960718 00832 NM 1996 7 18 AALA960747 1 19960503 A 5315 141N5111 FLOOR BEAM BOEING 757 757223 1384957 NM BS 345 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 645AA 24603 AFW - FOUND FLOOR BEAM AT STATION 345 HAS CORROSION REMOVED ON UPPER SURFACE. MATERIAL REMAINING IS BEYOND SRM LIMITS, PER MRB 757-820. (M) 2 L 7 2 4F RT A2NM 1996071800833 19960718 00833 NM 1996 7 18 AALA960748 1 19960503 A 5315 141N2910 FLOOR BEAM BOEING 757 757223 1384957 NM BS 342 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 645AA 24603 AFW - FOUND FLOOR BEAM AT STATION 324 HAS CORROSION REMOVED ON UPPER SURFACE. MATERIAL REMOVED IS BEYOND SRM LIMITS, PE R MRB 757-819. (M) 2 L 7 2 4F RT A2NM 1996071800834 19960718 00834 NM 1996 7 18 AALA960749 1 19960503 A 5315 146N5089 FLOOR BEAM BOEING 757 757223 1384957 NM BS 1640 CUT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 645AA 24603 AFW - WHILE CUTTING THE TOP CAP OFF FLOOR BEAM 1640 FOR SRM REPAIR, EO WAS LOST ON THE 5 MOST OUTBOARD RIGHT FASTENERS A T FRAME, PER MRB 757-827. (M) 2 L 7 2 4F RT A2NM 1996071800835 19960718 00835 NM 1996 7 18 AALA960750 1 19960503 A 5321 146N5300 DECK PLATE BOEING 757 757223 1384957 NM BS 1720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 645AA 24603 AFW - FOUND DECK PLATE HAS SEVERAL AREAS OF CORROSION BLENDED BEYOND SRM LIMITS, PER MRB 757-824. (M) 2 L 7 2 4F RT A2NM 1996071800836 19960718 00836 NM 1996 7 18 AALA960793 1 19960521 A 3350 A3060733101 CONNECTOR BOEING 727 727227 1384078 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 728AA 20735 MIA - DURING OVERNIGHT CHECK, FIRST CLASS CABIN EMERGENCY FLOOR LIGHTS INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIG HT STRIP CONNECTOR AT FORWARD AREA OF FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996071800837 19960718 00837 NM 1996 7 18 AALA960794 1 19960520 A 3350 1000679 LIGHT GRIMES BOEING 727 727227 1384078 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 729AA 20736 DFW - DURING OVERNIGHT CHECK, COCKPIT DOOR OVERHEAD EXIT LIGHT INOPERATIVE. REPLACED COCKPIT DOOR OVERHEAD EXIT LIGHT A SSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996071800838 19960718 00838 NM 1996 7 18 AALA960804 1 19960515 A 5210 146N6201 PAN BOEING 757 757223 1384957 NM R-4 DOOR GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 646AA 24604 AFW - FOUND R-4 DOOR HANDLE PAN HAS GOUGE BLENDED, AREA BLEND IS BEYOND SRM LIMITS, PER MRB 757-842. (M) 2 L 7 2 4F RT A2NM 1996071800839 19960718 00839 NM 1996 7 18 AALA960805 1 19960515 A 5320 141N5161 INTERCOSTAL BOEING 757 757223 1384957 NM BS 405 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 646AA 24604 AFW - FOUND INTERCOSTAL AT STATION 405 AND RBL 58 HAS CORROSION ON UPPER SURFACE, MATERIAL REMOVED IS BEYOND SRM LIMITS, PER MRB 757-841. (M) 2 L 7 2 4F RT A2NM 1996071800840 19960718 00840 NM 1996 7 18 AALA960806 1 19960515 A 5315 141N5112 FLOOR BEAM BOEING 757 757223 1384957 NM BS 365 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 646AA 24604 AFW - FOUND FLOOR BEAM AT STATION 365 HAS CORROSION REMOVED BEYOND SRM LIMITS, PER MRB 757-840. (M) 2 L 7 2 4F RT A2NM 1996071800841 19960718 00841 NM 1996 7 18 AALA960807 1 19960515 A 5321 146N5300 DECK PLATE BOEING 757 757223 1384957 NM BS 1720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 646AA 24604 AFW - FOUND DECK PLATE HAS CORROSION REMOVAL ON UPPER SURFACE AT VARIOUS LOCATIONS. MATERIAL REMOVED IS BEYOND SRM LIMI TS, PER MRB 757-839. (M) 2 L 7 2 4F RT A2NM 1996071800842 19960718 00842 NM 1996 7 18 AALA960808 1 19960515 A 5210 146N6201 PAN BOEING 757 757223 1384957 NM L-4 DOOR GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 646AA 24604 AFW - FOUND L-4 DOOR HANDLE PAN HAS A SMALL GOUGE, AFTER BLENDING AREA IS BEYOND SRM LIMITS, PER MRB 757-838. (M) 2 L 7 2 4F RT A2NM 1996071800843 19960718 00843 NM 1996 7 18 AALA960809 1 19960515 A 5320 141N51911 SUPPORT BOEING 757 757223 1384957 NM BS 345 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 646AA 24604 AFW - FLOOR PANEL SUPPORT AT STATION 345 AND BL 0 HAS CORROSION REMOVED ON UPPER SURFACE, MATERIAL REMAINING IS BEYOND S RM LIMITS, PER MRB 757-837. (M) 2 L 7 2 4F RT A2NM 1996071800844 19960718 00844 NM 1996 7 18 AALA960810 1 19960515 A 5315 141N5111 FLOOR BEAM BOEING 757 757223 1384957 NM BS 345 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 646AA 24604 AFW - FOUND FLOOR BEAM AT STATION 345 HAS CORROSION REMOVED ON UPPER SURFACE. MATERIAL REMAINING IS BEYOND SRM LIMITS, PER MRB 757-836. (M) 2 L 7 2 4F RT A2NM 1996071800845 19960718 00845 NM 1996 7 18 AALA960821 1 19960522 A 2120 AIR DISTR BOEING 757 757223 1384957 NM CABIN ODOR A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 650AA 24608 SFO - FLT 1376 - AFTER T/O SFO DURING INITIAL CLIMB-OUT, ELECTRICAL ODOR NOTED IN CABIN AND COCKPIT. A/C RETURNED TO SF O AND LANDED W/O INCIDENT. CHECKED OPERATION OF ALL PACKS AND CABIN/COCKPIT LIGHTING WITH NO DEFECTS FOUND. ACCOMP FUN CTIONAL CHECK FLT AND PROBLEM REPEATED. REPEATED CHECK OF COCKPIT/CABIN LIGHTING INCLUDING FULL BRIGHT OPERATION WITH N O DEFECTS FOUND. CLEANED HYDRAULIC RESERVOIR PRESSURE MODULE CHECK VALVES AND REPLACED FILTER. CHECKED EQUIP COOLING S YSTEM WITH NO DEFECTS FOUND. ACCOMP PACK BURN OUT PROCEDURE ON BOTH PACKS. ACCOMP SECOND FUNCTIONAL CHECK FLT WITH NO DEFECTS FOUND. SYSTEMS OPERATIONAL CHECKED NORMAL WITH NO ODOR NOTED NOTED. A/C RETURNED TO SERV. (M) 2 L 7 2 4F RT A2NM 1996071800846 19960718 00846 NM 1996 7 18 AALA960823 1 19960524 A 2910 6517844239 LINE BOEING 727 727223 1384074 NM 'A' HYD SYSTEM DEFECTIVE A AALA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 712AA 22468 DFW - FLT 1178 - DURING CRUISE WHILE EN ROUTE MEX-DFW, LOST 'A' HYDRAULIC SYSTEM QUANTITY AND PRESSURE ACCOMPLISHED MANU AL GEAR EXTENSION AND LANDED DFW WITHOUT INCIDENT. LANDING WAS NOT OVERWEIGHT. REPLACED HYDRAULIC 'A' SYSTEM PRESSURE LINE AT 'A' SYSTEM HYDRAULIC MODULE AND 'A' SYSTEM FILTERS. ACCOMPLISHED LEAK CHECK AND GEAR SWING. SYSTEM GROUND CHEC KED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996071800847 19960718 00847 NM 1996 7 18 AALA960826 1 19960525 A 3350 1000679 LIGHT GRIMES BOEING 727 727233 138408A NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 866AA 21371 DFW - DURING OVERNIGHT CHECK, FOUND EMERGENCY OVERHEAD LIGHT AT ROW 25 INOPERATIVE. REPLACED EMERGENCY OVERHEAD LIGHT A SSEMBLY AT ROW 25. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A3WE 1996071800848 19960718 00848 EU 1996 7 18 AALA960839 1 19960529 A 3230 715391 SEQ VALVE FOKKER F28 F28MK0100 4990807 EU NLG DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 1441A 602G 11436 DFW - FLT 1591 - DURING TAKEOFF FROM DFW, THE NOSE GEAR DOOR DID NOT CLOSE. CYCLED GEAR WITH SAME RESULTS. RETURNED DF W AND LANDED WITHOUT FURTHER INCIDENT. REPLACED SEQUENCING VALVE. ACCOMPLISHED THREE GEAR SWINGS, AND LEAK CHECK. SYS TEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1996071800849 19960718 00849 NM 1996 7 18 AALA960841 1 19960529 A 3350 900542 BATTERY BOEING 727 727223 1384074 NM CABIN DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 894AA 22010 RDU - DURING OVERNIGHT CHECK, FOUND THE AFT STAIR EMERGENCY EXIT LIGHTS INOPERATIVE. CLEANED BATTERY CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996071800850 19960718 00850 NM 1996 7 18 AALA960842 1 19960529 A 3350 LAMP BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 898AA 22014 DFW - DURING OVERNIGHT CHECK, FOUND RIGHT AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOPERATIVE. RESEATED LAMP HOUSING. SY STEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996071800851 19960718 00851 WP 1996 7 18 AALA960843 1 19960530 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 271AA 49293 DFW - FLT 2273 - DURING PREFLIGHT, FOUND THE FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. REPAIRED WIRING FOR FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996071800852 19960718 00852 NM 1996 7 18 AALA960852 1 19960530 A 3397 WIRE DOUG MD11 MD11 3023602 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1765B 48596 DFW - DURING OVERNIGHT CHECK, FOUND THE LEFT AISLE EMEGENCY EXIT FLOOR PATH LIGHTING AT SEAT ROWS 20 THROUGH 28 INOPERAT IVE. REPLACED WIRING BETWEEN SEAT ROW 20C AND S3-1234TE. REPAIRED CONNECTOR AT SEAT 28C, AND REPLACED CONNECTOR. SYST EM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1996071800853 19960718 00853 WP 1996 7 18 AALA960854 1 19960601 A 3260 833605A PROX SWI UNIT DOUG DC9 DC982 3022082 WP E/E COMPT DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 488AA 49681 DFW - FLT 853 - AFTER TAKEOFF DFW WHEN LANDING GEAR HANDLE RAISED, THREE RED LIGHTS ILLUMINATED WITH NO YELLOW GEAR DOOR LIGHT. SELECTED LANDING GEAR DOWN AND GOT THREE GREEN INDICATION. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDEN T. REPLACED LANDING GEAR PROXIMITY SWITCH UNIT. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYS TEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996071800854 19960718 00854 EU 1996 7 18 AALA960855 1 19960531 A 3350 CONDUCTOR AIRBUS 300 A300B4605R 3930308 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 34078 615 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 12AB AND 20AB INOPERATIVE. REPLACED EMERGENC Y FLOOR LIGHT FLAT CONDUCTOR BETWEEN PAX SEAT ROWS 12AB AND 20AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996071800855 19960718 00855 NM 1996 7 18 AALA960857 1 19960602 A 3350 1000679 LIGHT GRIMES BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 701AA 22459 RDU - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT OVER FORWARD GALLEY DOORS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT OVER FORWARD GALLEY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996071800856 19960718 00856 NM 1996 7 18 AALA960858 1 19960603 A 3350 1000679 LIGHT BOEING 767 767223 1385123 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 330AA 22330 SFO - DURING OVERNIGHT CHECK, COCKPIT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED COCKPIT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1996071800857 19960718 00857 WP 1996 7 18 AALA960869 1 19960605 A 3350 CONDUCTOR DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 406A 49317 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT FLAT CONDUCTOR BY FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996071800858 19960718 00858 NE 1996 7 18 AALA960870 2 19960603 A 7250 BLADE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D209 52053 NE TURBINE SECTION FAILED A A AALA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 SW 07 562AA 49344 ORD - FLT 1671 - AFTER TAKEOFF ORD DURING CLIMB-OUT, RIGHT ENGINE FAILED. ACCOMPLISHED SHUTDOWN OF RIGHT ENGINE AND AIR CRAFT RETURNED TO ORD, LANDING OVERWEIGHT WITHOUT INCIDENT. REPLACED RIGHT ENGINE DUE TO TURBINE BLADE FAILURE. ACCOMP LISHED LEAK CHECKS AND GROUND ENGINE RUN WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. ACCOMPLISHED O VERWEIGHT LANDING INSPECTION WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. REMOVED ENGINE ROUTED TO S HOP FOR REPAIR AND RETURN TO SERVICE. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 1996071800859 19960718 00859 NM 1996 7 18 AALA960871 1 19960606 A 2750 240863 DRIVE MOTOR BOEING 727 727227 1384078 NM LT TE FLAP DEFECTIVE A AALA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SW 07 716AA 20608 IAD - FLT 1089 - AFTER TAKEOFF PHL DURING CLIMB-OUT, SYSTEM A HYDRAULIC LOW LEVEL LIGHT ILLUMINATED AND SYSTEM A QUANTIT Y DECREASED TO LESS THAN 1 GALLON. AIRCRAFT DIVERTED TO IAD, LANDING GEAR MANUALLY LOWERED, AND AIRCRAFT LANDED IAD WIT HOUT INCIDENT. REPLACED LEFT FLAP DRIVE MOTOR AND SERVICED HYDRAULIC SYSTEM A. ACCOMPLISHED LEAK AND GROUND CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996071800860 19960718 00860 NM 1996 7 18 AALA960873 1 19960606 A 3320 8721 BALLAST DAYRAY DOUG MD11 MD11 3023602 NM CABIN OVERHEATED A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 1755 48490 DFW - FLT 0051 - EN ROUTE DFW DURING CRUISE, ELECTRICAL ODOR NOTED IN CABIN WITH NO ABNORMAL INDICATIONS. AIRCRAFT PROC EEDED TO DFW AND LANDED WITHOUT INCIDENT. PLACARDED CABIN LIGHT BALLAST AT ROW 9CD. BALLAST SUBSEQUENTLY CHANGED AT EZ E/08 AND PLACARD REMOVED. SYSTEM GROUND CHECKED NORMAL OPERATION WITH NO ELECTRICAL ODOR NOTED. (M) 2 L 7 3 4F RT A22WE 1996071800861 19960718 00861 NM 1996 7 18 AALA960874 1 19960607 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 313AA 22316 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 29AB INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT C ONNECTOR ON BACK OF LIGHT ASSEMBLY AT PAX SEAT 29AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1996071800862 19960718 00862 EU 1996 7 18 AALA960875 1 19960608 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1454D 11466 DFW - DURING OVERNIGHT CHECK, L1 DOOR EMERGENCY EXIT SIGN INOPERATIVE. REPAIRED BROKEN WIRE AT L1 DOOR EMERGENCY EXIT L IGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1996071800863 19960718 00863 WP 1996 7 18 AALA960876 1 19960608 A 3350 STRIP DOUG DC10 DC1010 3022110 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 128AA 46984 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PAX SEAT ROW 17B INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT ST RIP BY PAX SEAT ROW 17B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A22WE 1996071800864 19960718 00864 WP 1996 7 18 AALA960880 1 19960612 A 3350 A3060698101 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 476AA 49651 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN MAIN CABIN FORWARD OF PAX SEAT ROW 20 INOPERATIVE. RESECURED LO OSE EMERGENCY FLOOR LIGHT STRIP CONNECTOR BY PAX SEAT ROW 20. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996071800865 19960718 00865 NM 1996 7 18 AALA960883 1 19960612 A 5330 SKIN BOEING 727 727223 1384074 NM BS 380 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 868AA 21373 TUL - FOUND SKIN BULGED, CRACKED AT FASTENER HOLE STATION 380 STRINGER 21 TO 22R. REMOVED CRACKED AREA AND INSTALLED DO UBLER PER SRM 53-30-3 PAGE 5-8. (M) 2 L 7 3 4F A3WE 1996071800866 19960718 00866 NM 1996 7 18 AALA960884 1 19960612 A 5330 SKIN BOEING 727 727223 1384074 NM BS 305 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 868AA 21373 TUL - FOUND FUSELAGE SKIN HAS .5 INCH CRACK AT FORWARD END OF FUEL ENTRY DOOR LOWER HINGE CUTOUT. ROUTED OUT CRACK, INS TALLED DOUBLER PER SB 727-53-0198. (M) 2 L 7 3 4F A3WE 1996071800867 19960718 00867 NM 1996 7 18 AALA960885 1 19960608 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 950 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 705AA 22462 TUL - FOUND CORROSION ON OUTBOARD SIDE STRINGER 29R TWO INCHES AFT OF 950E. REPLACED AFT SECTION OF STRINGER 29RT STATI ON 950D PLUS 10 INCHES TO STATION 990 PLUS 10 INCHES PER ESO 11697. (M) 2 L 7 3 4F A3WE 1996071800868 19960718 00868 NM 1996 7 18 AALA960886 1 19960608 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 344-352 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 705AA 22462 TUL - FOUND FORWARD E/E STATION 344 TO STATION 352, UNDER RIGHT NOSE GEAR WALKWAY, LOWER CHORD ANGLE AT ATTACH TO NOSE G EAR W/W HAS BEARING CORROSION JUST AFT OF NOSE GEAR DRAG BRACKET, FORWARD SUPPORT BEAM. INSTALLED NEW RIGHT LOWER CHORD ANGLE PER SRM 51-10-01. (M) 2 L 7 3 4F A3WE 1996071800869 19960718 00869 NM 1996 7 18 AALA960888 1 19960608 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 514-525 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 705AA 22462 TUL - FOUND STRINGER 27 LEFT HAS CORROSION STATION 514 TO STATION 525. CUT OUT CORROSION AND REPLACED STRINGER 27L FROM STATION 513 TO STATION 525, PER SRM 53-10-3 PG 3-4B. (M) 2 L 7 3 4F A3WE 1996071800870 19960718 00870 NM 1996 7 18 AALA960892 1 19960608 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 700 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 705AA 22462 TUL - FOUND CORROSION ON SHEAR TIE NEAR DOME NUTS, STATION 700 STRINGER 28L TO 28R. REMOVED SHEAR TIE AND INSTALLED NEW ONE PER SRM 57-10-3 PG 4. (M) 2 L 7 3 4F A3WE 1996071800871 19960718 00871 NM 1996 7 18 AALA960893 1 19960608 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 705AA 22462 TUL - FOUND STRINGER END CRACKED STRINGER 15R AT THE LIGHT BOX FORWARD SIDE STATION 720B PLUS 4. REMOVED CRACK STRINGER AND SPLICED NEW STRINGER AS PER SRM 53-10-3 FIG 1. (M) 2 L 7 3 4F A3WE 1996071800872 19960718 00872 NM 1996 7 18 AALA960894 1 19960608 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1096 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 705AA 22462 TUL - FOUND CRACK IN FUSELAGE SKIN ON CROWN AT STATION 1096, RIGHT SIDE OF STRINGER NR 1 AT FASTENER FOR NR 2 ENG INLET FORWARD ATTACH. INSTALLED DOUBLER PER SB 727-53A0204 SRM 53-30-3 FIG 3 PAGE 12-14. (M) 2 L 7 3 4F A3WE 1996071800873 19960718 00873 WP 1996 7 18 AALA960896 1 19960612 A 3222 SPACERS DOUG DC9 DC983 3022083 WP NLG STRUT MISINSTALLED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 76201 53291 TUL - FLT 1404 - AFTER T/O TUL WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR DID NOT RETRACT. EXTENDED LANDING GEAR AN D A/C RETURNED TO TUL, LANDING OVERWEIGHT WITHOUT INCIDENT. SERVICED NOSE LANDING GEAR STRUT WITH OIL AND NITROGEN AND ACCOMP OVERWEIGHT LANDING INSPECTION WITH NO DEFECTS FOUND. A/C REDEPARTED AND PROBLEM REPEATED. A/C RETURNED TO TUL A ND LANDED OVERWEIGHT WITHOUT INCIDENT. REMOVED NOSE LANDING GEAR INNER CYLINDER AND CORRECTED INSTALLATION RETRACTION C HECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION WITH NO DEFECTS FOUND. ACCOMP FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS FOUND. SYSTEM OPS CHECKED NORMAL. (M) 2 L 7 2 4F RT A6WE 1996071800874 19960718 00874 NM 1996 7 18 AALA960901 1 19960612 A 5315 146N5089 FLOOR BEAM BOEING 757 757223 1384957 NM BS 1640 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 649AA 24607 AFW - FOUND FLOOR BEAM AT STATION 1640 HAS CORROSION REMOVED BEYOND SRM LIMITS. PER MRB 757-860. (M) 2 L 7 2 4F RT A2NM 1996071800875 19960718 00875 NM 1996 7 18 AALA960902 1 19960612 A 5320 146N8522 SILL BOEING 757 757223 1384957 NM BS 1410 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 649AA 24607 AFW - FOUND UPPER CHORD ON LOWER MAIN SILL, NR 2 CARGO DOOR CUTOUT HAS CORROSION REMOVED BEYOND LIMITS. PER MRB 757-862 . (M) 2 L 7 2 4F RT A2NM 1996071800876 19960718 00876 NM 1996 7 18 AALA960903 1 19960612 A 5321 146N5300 DECK PLATE BOEING 757 757223 1384957 NM BS 1720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 649AA 24607 AFW - FOUND DECK PLATE HAS CORROSION REMOVED IN VARIOUS LOCATIONS, CORROSION REMOVED IS BEYOND SRM LIMITS. PER MRB 757- 855. (M) 2 L 7 2 4F RT A2NM 1996071800877 19960718 00877 WP 1996 7 18 AALA960904 1 19960614 A 3240 26088921 BRAKE BENDIX DOUG DC9 DC982 3022082 WP NR 2 MLG LOCKED UP A AALA K NONE O OTHER LD LANDING 1 SW 07 464AA 49594 ORD - FLT 1931 - DURING LANDING AT ORD, LEFT NR 2 MAIN LANDING GEAR BRAKE LOCKED UP AND FUSE PLUGS BLEW. AIRCRAFT LANDE D WITHOUT INCIDENT AND TAXIED TO GATE. REPLACED LEFT NR 2 MAIN LANDING GEAR BRAKE. ALSO, REPLACED LEFT MAIN NR 1 AND N R 2 WHEEL AND TIRE ASSEMBLIES. SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996071800878 19960718 00878 WP 1996 7 18 AALA960908 1 19960715 A 5312 BULKHEAD TEE DOUG DC10 DC1010 3022110 WP BS 1156 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 166AA 46908 TUL - DURING C-CHECK, FOUND CRACK IN FS 1156 BULKHEAD RIGHT TEE CAP INBOARD OF FIFTH FASTENER IN THE LOWER ROW OF FASTEN ERS FROM THE OUTBOARD END. STOP DRILLED CRACK AND INSTALLED DOUBLER PER ESO 7349 DATE 5-14-97 AND SRM 51-35-01 VOL II, SRM 51-21-01, VOL II, SRM 51-38-01, VOL II. TST: 81,156.07 HRS. CYCLES, 24,004. (X) 2 L 7 3 4F A22WE 1996071800879 19960718 00879 WP 1996 7 18 AALA960912 1 19960617 A 5347 SEAT TRACKS DOUG DC9 DC982 3022082 WP BS 207 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 292AA 49304 TUL - FOUND NR 5 SEAT TRACK CORRODED FORWARD END OUTBOARD SIDE. REPLACED NR 5 SEAT TRACK STATION 207 TO STATION 246. I NSTALLED SPLICE AT STATION 246 IAW SRM 53-05 FIG 4F. TREATED AND PRIMED AREAS AS REQUIRED. (M) 2 L 7 2 4F A6WE 1996071800880 19960718 00880 WP 1996 7 18 AALA960914 1 19960617 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 1155 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 292AA 49304 TUL - FOUND CORROSION ON ANGLE BRACE, FORWARD, INBOARD BOTTOM ANGLE AND CORNER ANGLE OF DOOR FRAME OPENING. REPLACED CO RNER ANGLE. REINSTALLED FASTENERS AND TREATED AND PRIMED AREA. (M) 2 L 7 2 4F A6WE 1996071800881 19960718 00881 WP 1996 7 18 AALA960916 1 19960618 A 5347 TRACK DOUG DC9 DC982 3022082 WP BS 1200-1300 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 292AA 49304 TUL - FOUND CORROSION IN TIE DOWN TRACK NR 2 AT FS 1200 AND FS 1300. REMOVED AND REPLACED TRACK FROM STATION 1180-1307 PER SRM 53-05 FIG 4. (M) 2 L 7 2 4F A6WE 1996071800882 19960718 00882 WP 1996 7 18 AALA960918 1 19960612 A 2780 59388282 BRACKET DOUG DC9 DC982 3022082 WP RT WING BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 215AA 49163 TUL - FOUND PULLEY BRACKET IS BROKEN IN TWO PLACES, UPPER HORIZONTAL LEG AND AFT VERTICAL LEG. REPLACED PULLEY BRACKET. (M) 2 L 7 2 4F A6WE 1996071800883 19960718 00883 WP 1996 7 18 CAL960639 1 19960508 A 5313 LONGERON DOUG DC9 DC932 3022066 WP FS 218 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 67332 47218 HOU - INSPECTION FOUND LONGERON 25L CORRODED AT FS 218. A NEW SECTION OF LONGERON WAS SPLICED IN IAW SRM 51-30-21. (M) 2 L 7 2 4F A6WE 1996071800884 19960718 00884 WP 1996 7 18 CAL960640 1 19960508 A 5320 ANGLE DOUG DC9 DC932 3022066 WP NLG WW CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 67332 47218 HOU - INSPECTION FOUND L-ANGLE AT NOSE WHEEL WELL FORWARD BULKHEAD, STATION 110, LONGERON 25L CORRODED. A DOUBLER WAS I NSTALLED IAW SRM 53-00-01. (M) 2 L 7 2 4F A6WE 1996071800885 19960718 00885 WP 1996 7 18 CKSA96054 1 19960529 A 3260 DC26F1415S CONNECTOR DOUG DC8 DC863 302198A WP RT MLG BROKEN A CKSA O OTHER N FALSE WARNING AP APPROACH 1 GL 23 868BX 57383 46034 ON GEAR EXTENSION, 'GEAR NOT LATCHED' LIGHT CAME ON WITH 3 NORMAL GREEN GEAR LIGHT, CYCLED GEAR SEVERAL TIMES WITH SAME INDICATIONS AS FIRST EXTENSION (WITH EXCEPTION WHEN GEAR HANDLE WAS PLACED DOWN THE RIGHT MAIN LANDING GEAR WENT IMMEDIA TELY TO GREEN INDICATION). REPAIRED WIRE IN CANNON PLUG AT RIGHT GEAR DOWN LIMIT SWITCH IAW MM CHAPTER 32-60. OPS CHEC K NORMAL ON GROUND. (M) 2 L 7 4 4F 4A25 1996071800886 19960718 00886 WP 1996 7 18 CKSA96055R1 1 19960603 A 5320 SR08538003 DOUBLER DOUG DC8 DC855 3021927 WP FS 220 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 801CK 60055 45816 DURING B-D CHECK INSPECTION, FOUND CARD NR 4640-0551 AREA, FLT COMPARTMENT MID AREA FS 220 LEFT OUTBOARD FINGER DOUBLER, HAS CORROSION, LEVEL 2 TASK NR 76881. REPAIRED IAW SKETCH, AIA/E/2316 DATED 5/14/96 AS REQUIRED. (M) 2 L 7 4 4F 4A25 1996071800887 19960718 00887 EU 1996 7 18 COEA9670201 1 19960625 A 7712 10542N02W01 TQ IND FOKKER F27 F27MK600 4990706 EU LT ENGINE FAILED A COEA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 NM 13 702FE 10350 NR 1 LT TORQUE PRESSURE INDICATOR FAILED DURING TAKEOFF ROLL AT RNO. DURING START UP, TAXI AND INITIAL TAKEOFF POWER SE TTING INDICATIONS WERE NORMAL. AFTER INITIAL TAKEOFF POWER WAS SET AND THE ROLL BEGAN, BOTH DIGITAL AND ANALOG TORQUE I NDICATIONS FAILED. TAKEOFF WAS ABORTED. MX REPLACED THE NR 1 TORQUE PRESSURE INDICATOR. OPS CHECK NORMAL. AIRCRAFT R ELEASED. (M) 2 H 7 2 4T A817 1996071800888 19960718 00888 NE 1996 7 18 IXKA9600039 2 19960617 A 7314 378200 FUEL PUMP BOEING 727 727251 138408H NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE FAILED A A IXKA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 25 264US 03357 19983 FLT 81 - TPA-ATL - AFTER GEAR RETRACTION, NR 1 ENGINE SHUT DOWN. RETURNED TO TPA. FOUND FUEL PUMP SHAFT SHEARED. REMO VED AND REPLACED FUEL PUMP AND FUEL CONTROL AS PER MM 73-11-01 PG 401-408 AND MM 73-21-2, PAGE 401-405. INSPECTED, RAN ENGINE AND OPS CHECK OK. ALL INDICATIONS OK. (M) 2 L 7 3 4F 4 F A3WE E2EA 1996071800889 19960718 00889 NM 1996 7 18 IXKA9600040 1 19960525 A 3350 BATTERY PACK BOEING 727 727225 1384077 NM CABIN OUT OF POSITION A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 352PA 20616 EMERGENCY FLOOR LIGHTING INOP, WINDOW EXIT. FOUND BATTERY PACK TILTED IN MODULE. RESECURED AND CHARGED PER MM 33-30-22 . (M) 2 L 7 3 4F A3WE 1996071800890 19960718 00890 NM 1996 7 18 IXKA9600041 1 19960528 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM EXTERIOR DISCHARGED A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 353PA 9826 20622 RIGHT SIDE AFT EMERGENCY LIGHT EXTERIOR INOP. REMOVED AND REPLACED POWER PACK, OPS CHECK OK. (M) 2 L 7 3 4F A3WE 1996071800891 19960718 00891 NM 1996 7 18 IXKA9600042 1 19960605 A 3350 LIGHT BOEING 727 727225 1384077 NM CABIN INOPERATIVE A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 354PA 20624 CEILING EMERGENCY LIGHT AFT GALLEY AREA NEEDS REWIRING. INSTALLED EMERGENCY LIGHT PER MM 33-50-01, ALL LIGHTS CHECKED O K. NO CHAFED OR VISIBLE WIRES. EMERGENCY LIGHTS OK. (M) 2 L 7 3 4F A3WE 1996071800892 19960718 00892 NM 1996 7 18 IXKA9600043 1 19960605 A 2520 PSU BOEING 727 727225 1384077 NM CABIN RED FLAGGED A IXKA K NONE J WARNING INDICATION IN INSP/MAINT 1 EA 25 354PA 20624 RED FLAGS ARE SHOWING AT PSU 29 AND 30 DEF NEEDS TO BE REPACKED. REPACKED 29 AND 30 DEF PSU PER MM 35-21-42. (M) 2 L 7 3 4F A3WE 1996071800893 19960718 00893 NM 1996 7 18 IXKA9600044 1 19960531 A 3397 WIRE BOEING 727 727225 1384077 NM CABIN LOOSE A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 361KP 20627 EMERGENCY FLOOR LIGHTING IS OFF TRACK BY AFT GALLEY AND WIRES ARE EXPOSED. REINSTALLED AND RESECURED. (M) 2 L 7 3 4F A3WE 1996071800894 19960718 00894 NM 1996 7 18 IXKA9600045 1 19960531 A 3350 LIGHT BOEING 727 727225 1384077 NM CABIN FELL OFF A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 361KP 20627 OVERHEAD EMERGENCY LIGHT, BY AFT GALLEY, FELL OFF. RESECURED EMERGENCY LIGHT BY AFT GALLEY AREA. (M) 2 L 7 3 4F A3WE 1996071800895 19960718 00895 NM 1996 7 18 IXKA9600046 1 19960602 A 3350 LIGHT BOEING 727 727225 1384077 NM CABIN INOPERATIVE A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8881Z 21578 AFT CENTER CABIN EMERGENCY EXIT LIGHT INOP. REPLACED AFT CENTER CABIN EMERGENCY EXIT LIGHT PER MM 33-50-91. (M) 2 L 7 3 4F A3WE 1996071800896 19960718 00896 NM 1996 7 18 IXKA9600047 1 19960605 A 3350 900835A POWER PACK BELL 900835A BOEING 727 727224 1384076 NM CABIN INOP A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 32719 B2607 20388 FORWARD PASSENGER OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED POWER PACK ASSY AND OPS CHECK OK AS PER MM 33-50- 51. (M) 2 L 7 3 4F A3WE 1996071800897 19960718 00897 NM 1996 7 18 IXKA9600048 1 19960611 A 3350 P2070003001 BATTERY PACK BOEING 727 727224 1384076 NM AFT FLASH LIGHT INOPERATIVE A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 32719 20388 AFT EMERGENCY FLASH LIGHT INOP. REMOVED AND REPLACED BATTERY. OPS CHECK OK. (M) 2 L 7 3 4F A3WE 1996071800898 19960718 00898 NM 1996 7 18 IXKA9600049 1 19960608 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN INOP A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8883Z N2775 21580 RIGHT FORWARD OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK AND OPS CHECK PER MM 33-50-71. (M) 2 L 7 3 4F A3WE 1996071800899 19960718 00899 NM 1996 7 18 IXKA9600050 1 19960613 A 3350 LIGHT BOEING 727 727225 1384077 NM CABIN DIRTY A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 361KP 20627 LEFT FORWARD OVERWING EMERGENCY LIGHT INOP. TROUBLESHOT SYSTEM AND FOUND CONTACTS CORRODED, CLEANED CONTACTS AND OPS CH ECK OK. (M) 2 L 7 3 4F A3WE 1996071800900 19960718 00900 NM 1996 7 18 IXKA9600051 1 19960613 A 3350 S106 BATTERY BOEING 727 727225 1384077 NM CABIN DISCHARGED A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 361KP 20627 AFT AIRSTAIR OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED NICAD BATTERY CELLS. OPS CHECK OK. (M) 2 L 7 3 4F A3WE 1996071800901 19960718 00901 NM 1996 7 18 IXKA9600052 1 19960620 A 2130 106142618 FLOW CONTL VALVE BOEING 727 727251 138408H NM RIGHT VLV INTERMITTENT A IXKA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 25 259US P539 19978 AFTER TAKEOFF AT ATL, FLT 73, ATL TO MCO, AIR TURN BACK DUE TO UNABLE TO PRESSURIZE ON DEPARTURE IN AUTO OR MANUAL. TRO UBLESHOT PRESSURIZATION TO INTERMITTENT FLOW CONTROL VALVE. REMOVED AND REPLACED FLOW CONTROL VALVE PER MM 36-12-11. P RESSURIZED A/C PER MM 21-30-00. OPS CHECK OK. (M) 2 L 7 3 4F A3WE 1996071800902 19960718 00902 NM 1996 7 18 IXKA9600053 1 19960623 A 3350 BATTERY PACK BOEING 727 727251 138408H NM CABIN DIRTY A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 259US 19978 FORWARD EMERGENCY CEILING LIGHT OUT. REMOVED BATTERY AND CLEANED CONTACTS INSTALLED BATTERY PACK, OPS CHECK OK AS PER M M 33-50-01. (M) 2 L 7 3 4F A3WE 1996071800903 19960718 00903 NM 1996 7 18 IXKA9600054 1 19960627 A 3397 WIRE BOEING 727 727225 1384077 NM CABIN BROKEN A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8881Z 21578 FORWARD 'E' PATH LIGHT INOP. REPAIRED BROKEN WIRE TO LIGHT, CHECK OK AS PER MM 33-50-01. (M) 2 L 7 3 4F A3WE 1996071800904 19960718 00904 NM 1996 7 18 IXKA9600055 1 19960627 A 3350 CM1307BPEGP1 LAMP BOEING 727 727225 1384077 NM CABIN INOP A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8882Z 21579 EMERGENCY LIGHT INOP AT ROW 20. REMOVED AND REPLACED EMERGENCY LIGHT BULB AND LENSE. OPS CHECK OK. (M) 2 L 7 3 4F A3WE 1996071800905 19960718 00905 WP 1996 7 18 IXXA96100 1 19960619 A 5330 PANEL DOUG DC8 DC862 3021970 WP BS 1590 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 31CX 65131 45911 DURING ROUTINE C-CHECK INSPECTION, CORROSION OF THE EXTERIOR PLATING AT FUSELAGE STATION 1590, LONGERON 35 LEFT TO 35 RI GHT WAS IDENTIFIED. THE PANEL WAS REMOVED AND REPLACED FROM STATION 1530 TO 1730, LONGERONS 31 LEFT TO 31 RIGHT. (M) 2 L 7 4 4F 4A25 1996071800906 19960718 00906 WP 1996 7 18 IXXA9688 1 19960611 A 3241 39069B CONTROL VALVE DOUG DC8 DC871 302199A WP RT ANTI-SKID INTERMITTENT A IXXA O OTHER J WARNING INDICATION TO TAKEOFF 1 SW 11 823BX 1474A 46064 ANTI-SKID FAIL LIGHT ILLUMINATED ON TAKEOFF ROLL DEPARTING ICT TO OKC. GEAR WAS RECYCLED AND THE LIGHT EXTINGUISHED. A IRCRAFT LANDING AT OKC WAS UNEVENTFUL. MX REPLACED THE RIGHT OUTBOARD ANTI-SKID DUAL CONTROL SERVO VALVE. THE SYSTEM O PERATIONALLY CHECKED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 4 4F 4A25 1996071800907 19960718 00907 WP 1996 7 18 IXXA9689 1 19960617 A 5270 WIRING HARNESS DOUG DC8 DC863F 302198F WP CARGO DOOR BROKEN A IXXA O OTHER N FALSE WARNING DE DESCENT 1 SW 11 786AL 3319 46121 EN ROUTE MIA TO SJU, CARGO DOOR WARNING LIGHT ILLUMINATED ON DESCENT INTO SJU. FOLLOWING AN UNEVENTFUL LANDING, MX REPA IRED THE WIRING HARNESS OF THE CARGO DOOR WARNING SYSTEM AND RETURNED THE AIRCRAFT TO SERVICE. (M) 2 L 7 4 4F 4A25 1996071800908 19960718 00908 WP 1996 7 18 IXXA9690 1 19960619 A 5512 56408081 PANEL DOUG DC8 DC862 3021970 WP HORIZ STAB CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 31CX 45911 DURING ROUTINE C-CHECK INSPECTION OF THE HORIZONTAL STABILIZER CENTER SECTION, THE FORWARD UPPER PANEL WAS FOUND TO BE C RACKED. THE INSPECTION WAS WITHIN THE SCOPE OF DOUGLAS SERVICE BULLETIN 55-15, USING THE NDT METHODS CALLED OUT. THE P ANEL WAS REPLACED. (M) 2 L 7 4 4F 4A25 1996071800909 19960718 00909 WP 1996 7 18 IXXA9691 1 19960619 A 5512 56408081 PANEL DOUG DC8 DC862 3021970 WP HORIZ STAB CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 31CX 65131 45911 DURING ROUTINE C-CHECK INSPECTION OF THE HORIZONTAL CENTER SECTION, THE LOWER FORWARD PANEL WAS FOUND TO BE CRACKED. TH E INSPECTION WAS ACCOMPLISHED IAW DOUG SERVICE BULLETING 55-15, USING THE NDT METHODS. THE PANEL WAS REPLACED. (M) 2 L 7 4 4F 4A25 1996071800910 19960718 00910 WP 1996 7 18 IXXA9692 1 19960619 A 5512 5640807501 UPPER MID PANEL DOUG DC8 DC862 3021970 WP HORIZ STAB CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 31CX 65131 45911 DURNG ROUTINE C-CHECK INSPECTION OF THE HORIZONTAL STABILIZER CENTER SECTION, THE UPPER MID PANEL WAS FOUND CRACKED. TH E INSPECTION WAS ACCOMPLISHED IAW DOUGLAS SERVICE BULLETIN 55-15, USING THE NDT METHODS. THE PANEL WAS REPLACED. (M) 2 L 7 4 4F 4A25 1996071800911 19960718 00911 WP 1996 7 18 IXXA9693 1 19960619 A 5730 PLATING DOUG DC8 DC862 3021970 WP RT WING LE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 31CX 65131 45911 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND IN THE RIGHT WING LEADING EDGE EXTERNAL PLATING AT STATION XW 761.6 95. THE CRACK WAS REMOVED BY CUT OUT. THE REPAIR WAS ACCOMPLISHED BY FABRICATION AND INSTALLATION OF A REPAIR FILLER A ND EXTERNAL DOUBELR IAW THE DOUGLAS STRUCTURAL REPAIR MANUAL 57-2-1. (M) 2 L 7 4 4F 4A25 1996071800912 19960718 00912 WP 1996 7 18 IXXA9694 1 19960619 A 5530 ANGLE DOUG DC8 DC862 3021970 WP VERT STAB CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 31CX 65131 45911 DURING ROUTINE C-CHECK INSPECTION, THE RIGHT VERTICAL STABILIZER ATTACH ANGLE WAS FOUND CRACKED AND CORRODED AT THE FRON T SPAR. REPAIR OF THE ANGLE WAS ACCOMPLISHED IAW FAA DER APPROVED DRAWING A62-R112. (M) 2 L 7 4 4F 4A25 1996071800913 19960718 00913 WP 1996 7 18 IXXA9695 1 19960619 A 5330 PANEL DOUG DC8 DC862 3021970 WP BS 1583 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 31CX 45911 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS IDENTIFIED IN THE FUSELAGE EXTERNAL PLATING AT FUSELAGE STATION 1583 AND LONGERON 22 LEFT. THE CRACK WAS REMOVED BY CUTOUT, THE REPAIR WAS ACCOMPLISHED BY FABRICATING AND INSTALLING A FILLER A ND EXTERNAL DOUBLER IAW THE DOUGLAS STRUCTURAL MANUAL 53-2-1. (M) 2 L 7 4 4F 4A25 1996071800914 19960718 00914 WP 1996 7 18 IXXA9696 1 19960619 A 5330 PANEL DOUG DC8 DC862 3021970 WP BS 1541 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 31CX 65131 45911 DURING ROUTINE C-CHECK INSPECTION OF THE UPPER AFT FUSELAGE EXTERNAL PLATING, A CRACK WAS IDENTIFIED AT FUSELAGE STATION 1541, LONGERON 17 RIGHT. REPAIR WAS ACCOMPLISHED BY CRACK CUT OUT, FABRICATION AND INSTALLATION OF A REPAIR FILLER AND EXTERNAL DOUBLER IAW THE DOUGLAS STRUCTURAL REPAIR MANUAL 53-2-1. (M) 2 L 7 4 4F 4A25 1996071800915 19960718 00915 WP 1996 7 18 IXXA9697 1 19960619 A 5330 PANEL DOUG DC8 DC862 3021970 WP BS 1559 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 31CX 65131 45911 DURING ROUTINE C-CHECK INSPECTION OF THE UPPER AFT FUSELAGE EXTERIOR PLATING, A CRACK WAS IDENTIFIED AT FUSELAGE STATION 1559, LONGERON 17 RIGHT. THE CRACK WAS REMOVED BY CUT OUT. THE REPAIR FILLER AND EXTERNAL DOUBLER WERE FABRICATED AND INSTALLED IAW THE DOUGLAS STRUCTURAL REPAIR MANUAL 53-2-1. (M) 2 L 7 4 4F 4A25 1996071800916 19960718 00916 WP 1996 7 18 IXXA9698 1 19960619 A 5330 PANEL DOUG DC8 DC862 3021970 WP BS 1529 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 31CX 65131 45911 DURING RUOTINC C-CHECK INSPECTION, AN EXTERNAL FUSELAGE SKIN CRACK WAS IDENTIFIED AT FUSELAGE STATION 1529, LONGERON 17 RIGHT. REPAIR WAS ACCOMPLISHED BY REMOVAL OF THE CRACK, CUT OUT, FABRICATION AND INSTALLATION OF A FILLER AND EXTERNAL DOUBLER IAW THE DOUGLAS STRUCTUAL REPAIR MANUAL 53-2-1. (M) 2 L 7 4 4F 4A25 1996071800917 19960718 00917 WP 1996 7 18 IXXA9699 1 19960619 A 5330 5751702501 PANEL DOUG DC8 DC862 3021970 WP BS 296 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 31CX 65131 45911 DURING ROUTINE C-CHECK AND CPCP INSPECTION, CORROSION OF THE EXTERIOR PLATING WAS IDENTIFIED AT FUSELAGE STATION 296 BET WEEN LONGERONS 34 AND 35 RIGHT. THE CORRODED AREA WAS CUT OUT AND REPAIR WAS ACCOMPLISHED BY FABRICATION AND INSTALLATI ON OF A FILLER AND EXTERNAL DOUBLER IAW DOUGLAS STRUCTURAL REPAIR MANUAL 53-2-1. (M) 2 L 7 4 4F 4A25 1996071800918 19960718 00918 1996 7 18 RAIA960604 4 19960606 A 3442 6227337001 RT UNIT BAG JETSTM JETSTM3201 1500217 EU NOSE FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 430AM 10841 10841 880 STL - FLT 7312 - WEATHER RADAR INOP. MAINTENANCE REPLACED THE RADAR R/T. (M) 2 L 7 2 4T RT A56EU 1996071800919 19960718 00919 EU 1996 7 18 RAIA960605 1 19960620 A 7712 94959411 TTL BAG JETSTM JETSTM3201 1500217 EU RIGHT OUT OF ADJUST A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 431AM 1185 881 STL - FLT 7372 - RIGHT TORQUE DROPPED 20 PERCENT AND STABILIZED. MAINTENANCE ADJUSTED RIGHT TTL COMPUTER. PERFORMED GR OUND RUNS, OPS CHECK GOOD. (M) 2 L 7 2 4T RT A56EU 1996071800920 19960718 00920 EU 1996 7 18 RAIA960606 1 19960609 A 7714 56787048011 NH INDICATOR AEROSP ATR42 ATR42300 8680920 EU INST PANEL STUCK A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 425TE 12206 125 STL - FLIGHT 7462 - RIGHT ENGINE NH WENT TO 106 PERCENT AND STUCK THERE. MAINTENANCE REPLACED THE RIGHT NH INDICATOR. G ROUND RUN CHECKS GOOD. (M) 2 H 7 2 4T RT A53EU 1996071800921 19960718 00921 1996 7 18 RAIA960607 3 19960611 A 6140 8659566 BETA SWITCH BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 433AM 5980 885 COU - FLT 7038 - AT 70 KNOTS RIGHT ENGINE BETA LIGHT ILLUMINATED. BETA LIGHT REMAINED ILLUMINATED UNTIL PLA RETURNED TO TAXI. MAINTENANCE REPLACED RIGHT ENGINE BETA SWITCH. PERFORMED GROUND RUNS. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A56EU 1996071800922 19960718 00922 EU 1996 7 18 RAIA960608 1 19960617 A 7722 CA3108R12S3SF80 CONNECTOR BAG JETSTM JETSTM3201 1500217 EU RT NACELLE BROKE WIRE A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 433AM 10916 885 CMI - FLT 7449 - RIGHT ENGINE EGT INCREASED ON TAKEOFF ROLL. TORQUE AT 60 PERCENT, EGT AT 650. MX REPAIRED BROKEN WIRE AT RIGHT ENGINE T2 CANNON PLUG. GROUND RUNS CHECK GOOD. (M) 2 L 7 2 4T RT A56EU 1996071800923 19960718 00923 EU 1996 7 18 RAIA960609 1 19960617 A 5280 137414B418 GEAR DOOR BAG JETSTM JETSTM3201 1500217 EU LT/RT MLG LOOSE RIVET A RAIA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 CE 03 433AM 10917 885 STL - FLT 7512 - CAPTAIN'S YOKE SHAKING AT 190 KNOTS. EXTENDED FLAPS, VIBRATION WENT AWAY. MX REPLACED RIVETS ON THE L EFT AND RIGHT MAIN GEAR DOORS. PERFORMED IN FLIGHT MX CHECK, NO VIBRATIONS NOTED. (M) 2 L 7 2 4T RT A56EU 1996071800924 19960718 00924 WP 1996 7 18 RAIA960610 2 19960619 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RIGHT MALFUNCTIONED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CE 03 434AM 9680 887 P66105 STL - FLT 7096 - RIGHT ENGINE FAILED TO ACHIEVE TARGET TORQUE. MAINTENANCE REPLACED RIGHT ENGINE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996071800925 19960718 00925 EU 1996 7 18 SABA9600015 1 19960531 A 3230 RELEASE VLV PIN BAG JETSTM JETSTM3101 1500215 EU LANDING GEAR TRIPPED A SABA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 33 158PC 763 FLT 5210 - CHS-RDU - A/C HAD JUST TAKEN OFF WHEN THE CREW SELECTED GEAR UP THE GEAR WOULD ONLY RETRACT HALFWAY. GEAR HA NDLE WAS RECYCLED AND GEAR WOULD NOT RETRACT. GEAR HANDLE WAS SELECTED DOWN, ALL INDICATIONS WERE GREEN AND THE CAPTAIN RETURNED TO CHS, UNEVENTFUL LANDING MADE. AFTER DEPLANING THE PAX'S AT THE GATE, CAPT CALLED MX CONTROL TO NOTIFY THEM OF PROB. THE MGR ON DUTY DECIDED TO FERRY THE A/C BACK TO CLT, SO REPAIRS COULD BE MADE. A/C TAKEN TO THE MX HANGAR F OR T/S. THE LANDING GEAR RELEASE VLV PIN WAS FOUND POPPED. THE PIN WAS RESET AND THE NORM AND EMERGENCY SYS'S WERE FUN CTION CHECKED NUMEROUS TIMES. ALL RETRACTIONS AND EXTENSIONS WERE NORMAL. THE A/C WAS THEN RETURNED TO SERV.(M) 2 L 7 2 4T RT A21EU 1996071800926 19960718 00926 EU 1996 7 18 SIMA961761 1 19960624 A 3350 3011185 POWER SUPPLY AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 135MQ 135 ORD - FLT 4051 - RAI'D EMERGENCY LIGHTING CONTROLLER 3WL. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996071800927 19960718 00927 SO 1996 7 18 SRAA69604 1 19960614 A 6120 582855 VALVE HSG LKHEED 382 382G 526414U SO NR 1 PROP DAMAGED A A SRAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 23 921SJ 4586 ON TAKEOFF ROLL OUT OF GAL NR 1 PROPELLER WENT TO 104 PERCENT RPM (PTICH LOCKED). NR 1 ENGINE WAS SHUT DOWN AND TAKEOFF ABORTED, AIRCRAFT RETURNED TO BLOCKS WITHOUT INCIDENT. FOUND NR 1 PROP VALVE HOUSING HAD METAL SHAVINGS. REPLACED NR 1 PROPELLER ASSEMBLY PER J/C 6101, 6101-1 AND PERFORMED ENGINE RUN UP PER J/C 7101 AND 7101-2 OPS CHECKED GOOD. (M) 2 H 7 4 4T A1SO 1996071800928 19960718 00928 1996 7 18 SRAA69605 4 19960616 A 3413 5L29392A VSI BOEING 747 747246F NM COCKPIT LEAKS A SRAA A J UNSCHED LANDING DUMP FUEL O OTHER CL CLIMB 1 GL 23 741SJ 22063 DURING CLIMB-OUT OF JFK, FOUND CAPTAIN AND FIRST OFFICERS AIRSPEED INDICATORS AND ALTIMETERS IN DISAGREEMENT, DUMPED FUE L AND ACCOMPLISHED AIR TURN BACK TO JFK. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND CAPTAINS VSI LEAKING, AND FIRST OFFIC ERS PITOT TUBE ALSO LEAKING, REPLACED BOTH UNITS. SYSTEM OPS CHECKED GOOD PER MM CH 34-11-00. (M) 2 L 7 4 4F A20WE 1996071800929 19960718 00929 NM 1996 7 18 SRAA69606 1 19960617 A 2611 SMOKE DET BOEING 747 747212B 1384886 NM CARGO DECK MALFUNCTIONED A SRAA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 745SJ 20888 DURING CRUISE NR 2 MAIN DECK SMOKE DETECTOR LIGHT CAME ON, PHYSICALLY INSPECTED MAIN CARGO DECK FOUND NO SIGN OF FIRE OR SMOKE, ABNORMAL PROCEDURE COMPLIED WITH, LIGHT WENT OUT APPROXIMATELY 10 MINUTES LATER. MAINTENANCE PERFORMED OPS CHEC KED ON SMOKE DETECTION SYSTEM PER BMM CH 26-14-00, COULD NOT DUPLICATE PROBLEM, OPS CHECKED GOOD. (M) 2 L 7 4 4F A20WE 1996071800930 19960718 00930 1996 7 18 SRAA69607 4 19960620 A 3421 5223206004 ADI LKHEED 382 382E 526413U SO NR 2 FAILED A SRAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 23 901SJ 4299 DURING FLIGHT 9001 OUT OF YIP, CO-PILOTS GYRO FLAG CAME IN VIEW, ACCOMPLISHED AIR TURN BACK TO YIP WITHOUT INCIDENT. FO UND CO-PILOTS ADI FAILED, REMOVED AND REPLACED NR 2 ADI, SYSTEM OPS CHECKED GOOD PER MM CH 34. (M) 2 H 7 4 4T A1SO 1996071800931 19960718 00931 SW 1996 7 18 SWHA96004 1 19960621 A 3260 6839 BULBS 2782186057 SWRNGN SA227 SA227AC 8780603 SW LT MLG IND FAILED A SWHA A UNSCHED LANDING P NO WARNING INDICATION AP APPROACH 1 SW 17 789C 820 8806051 AC540 ON SCHEDULED FLIGHT 215A, UPON FINAL APPROACH, PILOT REPORTED NO DOWN AND LOCKED INDICATION FOR THE LEFT MAIN LANDING GE AR. PRESS TO TEST FOR THE INDICATOR DID NOT WORK. THE FLIGHT WAS DIVERTED TO AUSTIN. THE PILOT CALLED OUT AN EMERGENC Y AND LANDED WITHOUT INCIDENT. A FLY BY WAS PERFORMED TO CONFIRM THE GEAR WERE ALL DOWN BEFORE THE LANDING. INVESTIGAT ION REVEALED BOTH LIGHT BULBS IN THE LEFT MAIN GEAR DOWN AND LOCKED INDICATOR WERE BURNED OUT. THE BULBS WERE REPLCED A ND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A8SW 1996071800932 19960718 00932 NM 1996 7 18 USAA960491 1 19960622 A 5315 FLOOR BEAM BOEING 737 7374B7 1384702 NM BS 986.5 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 431US 19428 24553 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER AREAS OF CORROSION STATION 986.5 FLOOR BEAM UPPER CHORD LBL 45 TO RBL 45, WL 208. REPAIRED PER EA 41219. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996071800933 19960718 00933 NM 1996 7 18 USAA960492 1 19960622 A 5315 FLOOR BEAM BOEING 737 7374B7 1384702 NM BS 947 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 431US 19428 24553 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 26 INCH CORROSION, STATION 947 FLOOR BEAM RBL 13 INCHES TO LBL 13 INCHES, WL 208. FABRICATED PER EA 41220. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996071800934 19960718 00934 NM 1996 7 18 USAA960493 1 19960622 A 5311 FRAME BOEING 737 7374B7 1384702 NM BS 787 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 431US 19428 24553 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 1 INCH CORRSION AT FRAME AROUND AFT CARGO DOOR CUT OUT BS 787 PLUS 8 INCHES, STRINGER 25R. CUT OUT SECTION OF FRAME AND INSTALLED REPAIR. REPAIRED PER SRM 53-00-07 FIG 201. (M) 2 L 7 2 4F RT A16WE 1996071800935 19960718 00935 NM 1996 7 18 USAA960494 1 19960622 A 5315 FLOOR BEAM BOEING 737 7374B7 1384702 NM BS 312 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 431US 19428 24553 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES BS 312 RBL 8 THROUGH L BL 8. INSTALLED NEW SECTION OF UPPER CHORD, REPAIRED PER SRM 53-10-51 FIG 205. (M) 2 L 7 2 4F RT A16WE 1996071800936 19960718 00936 NM 1996 7 18 USAA960495 1 19960622 A 5315 FLOOR BEAM BOEING 737 7374B7 1384702 NM BS 344 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 431US 19428 24553 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES BS 344 LBL 21 THROUGH RBL 9. INSTALLED NEW SECTION OF T-CAP, REPAIRED PER TR 53-10-03. (M) 2 L 7 2 4F RT A16WE 1996071800937 19960718 00937 NM 1996 7 18 USAA960496 1 19960622 A 5315 FLOOR BEAM BOEING 737 7374B7 1384702 NM BS 328 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 431US 19428 24553 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER AREAS OF CORROSION STATION 328 FLOOR BEAM UPPER CHORD AT NUT PLATE HOLES RBL 13 TO RBL 58. CUT OUT DAMAGED CHORD AND SPLICED IN NEW SECTION PER TR 53-10-03. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996071800938 19960718 00938 EU 1996 7 18 VTZA96221 1 19960618 A 5230 91SE16 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGGAGE DOOR LACK LUBE A VTZA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 27 307UE 41021 FLT 6508 - ROA-IAD - ABORTED THE TAKEOFF DUE TO THE BAGGAGE DOOR WARNING LIGHT ILLUMINATING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MX OPENED DMI NR 41005 IAW MEL 52-3. MX LATER CLEARED DMI NR 41005 AND 6-20-96 BY INSPECTIN G AND LUBING THE DOOR WARNING MICROSWITCHES. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996071800939 19960718 00939 EU 1996 7 18 VTZA96224 1 19960619 A 7712 HTMAS0F2821P CONNECTOR BAG JETSTM JETSTM3201 1500217 EU LT ENGINE DIRTY A VTZA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 27 489UE 908 FLT 6407 - LGA-IAD - ABORTED TAKEOFF DUE TO THE LEFT EGT FLUCTUATING. EGT FLUCTUATIONS STABILIZED WITH SRL SELECTED OFF . MX OPENED DMI NR 55614 IAW MEL 76-1. MX LATER CLEARED DMI NR 55614 ON 6-20-96 BY CLEANING ZONE 2 CANNON PLUG AND THE STRAIN GAUGE CANNON PLUG. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996071800940 19960718 00940 EU 1996 7 18 VTZA96226 1 19960620 A 5270 91SE16 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGGAGE DOOR DIRTY A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 318UE 41041 FLT NR 6417 - CHS-IAD - ABORTED TAKEOFF DUE TO THE MAIN BAGGAGE DOOR WARNING ILLUMINATING DURING TAKEOFF. AIRCRAFT RETU RNED TO GATE WITH NO FURTHER INCIDENTS. MX OPENED DMI NR 21010 IAW MEL 52-3 ON THE BAGGAGE DOOR WARNING. MX LATER CLEA RED DMI NR 21010 ON 6-21-96 BY INSPECTING CLEANING AND LUBING THE DOOR WARNING MICROSWITCHES. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996071800941 19960718 00941 EU 1996 7 18 VTZA96228 1 19960624 A 5210 E1135 BUSHING BAG JETSTM JETSTM3201 1500217 EU PAX DOOR WORN A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 491UE 911 FLT NR 6314 - IAD-BUF - ABORTED TAKEOFF DUE TO THE PASSENGER DOOR WARNING LIGHT ILLUMINATING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MX ADJUSTED DOOR HANDLE, CLEANED AND LUBED MICROSWITCHES AND PLUNGERS. REPLACED WORN DOOR BUSHING. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996071800942 19960718 00942 EU 1996 7 18 VTZA96229 1 19960615 A 2611 111211000 SMOKE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU BAGGAGE COMPT DIRTY A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 311UE 41029 FLT NR 6430 - JFK-IAD - DURING CRUISE, RETURNED TO JFK DUE TO THE POD SMOKE LIGHT ILLUMINATING IN FLIGHT. MX INSPECTED BUT COULD NOT FIND ANY SIGNS OF SMOKE OR FIRE. OPENED DMI NR 08199 IAW MEL 26-3 ON THE SMOKE DETECTOR. MX LATER CLEARE D DMI NR 08199 ON 6-16-96 BY CLEANING THE SMOKE DETECTOR. AIRCRFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996071800943 19960718 00943 EU 1996 7 18 VTZA96230 1 19960616 A 7600 21188406 IEC JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 307UE 41021 FLT 6366 - IAD-CHS - ABORTED THE TAKEOFF DUE TO THE LEFT ENGINE NOT MAKING TAKEOFF TORQUE. AIRCRAFT RETURNED TO GATE WI TH NO FURTHER INCIDENTS. MX OPENED DMI NR 41004 IAW MEL 76-2 ON THE TTL. MX LATER CLEARED DMI NR 41004 BY ADJUSTING TH E EGT COMPENSATION SETTING. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996071800944 19960718 00944 EU 1996 7 18 VTZA96231 1 19960621 A 5270 91SE16 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGGAGE DOOR DIRTY A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 302UE 41013 FLT NR 6445 - BOS-IAD - ABORTED THE TAKEOFF DUE TO THE BAGGAGE DOOR WARNING LIGHT ILLUMINATING. AIRCRAFT RETURNED TO GA TE WITH NO FURTHER INCIDENTS. MX OPENED DMI NR 52845 IAW MEL 52-3. MX LATER CLEARED DMI NR 52845 ON 6-24-96 BY CLEANIN G AND LUBING THE DOOR WARNING MICROSWITCHES. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996071800945 19960718 00945 EU 1996 7 18 VTZA96232 1 19960623 A 7712 31053741 TT2 SENSOR JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE BROKEN WIRE A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 315UE 41033 FLT NR 6403 - IAD-BOS - ABORTED THE TAKEOFF DUE TO THE LEFT ENGINE TORQUE SPOOLING DOWN. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MX REPAIRED A WIRE TO THE TT2 SENSOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996071800946 19960718 00946 1996 7 18 VTZA96233 4 19960621 A 3418 C771065 SIG SUMM UNIT BAG JETSTM JETSTM3201 1500217 EU BS 130 OUT OF ADJUST A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 481UE 895 FLT NR 6424 - IAD-BUF - RETURNED TO IAD DUE TO THE STALL WARNING SYSTEM ACTIVATING. AIRCRAFT LANDED AT IAD WITH NO FURT HER INCIDENTS. MAINTENANCE ADJUSTED BOTH SIGNAL SUMMING UNITS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVIC E. (M) 2 L 7 2 4T RT A56EU 1996071800947 19960718 00947 EU 1996 7 18 VTZA96234 1 19960622 A 2770 91SE16 GUSTLOCK SW JETAIR JETSTM JETSTM4101 1500501 EU CENTER CONSOLE OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 307UE 41021 FLT NR 6150 - IAD-EWR - ABORTED THE TAKEOFF DUE TO THE TAKEOFF CONFIGURATION WARNING SYSTEM ACTIVATING. AIRCRAFT RETURN ED TO GATE WITH NO FURTHER INCIDENTS. MX ADJUSTED THE GUSTLOCK MICROSWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RET URN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996071800948 19960718 00948 EU 1996 7 18 VTZA96235 1 19960625 A 3234 8777701 GEAR HANDLE JETAIR JETSTM JETSTM4101 1500501 EU CENTER CONSOLE FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 311UE 41029 FLT NR 6185 - IAD-RDU - DURING CLIMB-OUT, RETURNED TO IAD DUE TO THE LANDING GEAR NOT RETRACTING WHEN SELECTED UP. AIRC RAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE GEAR HANDLE. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996071800949 19960718 00949 EU 1996 7 18 VTZA96236 1 19960625 A 2770 91SE16 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU GUST LOCK OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 315UE 41033 FLT NR 6290 - IAD-DAY - ABORTED TAKEOFF DUE TO THE TAKEOFF CONFIGURATION WARNING ACTIVATING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MX ADJUSTED THE GUSTLOCK HANDLE MICROSWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996071800950 19960718 00950 EU 1996 7 18 VTZA96237 1 19960626 A 3260 AIR135670 WOW SWITCH JETAIR JETSTM JETSTM4101 1500501 EU LT MLG FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 311UE 41029 FLT NR 6418 - IAD-BOS - DURING CLIMB-OUT RETURNED TO IAD DUE TO THE LANDING GEAR NOT RETRACTING WHEN SELECTED UP AND THE GEAR HANDLE WOULD NOT SELECT UP. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE LEFT WEIG HT ON WHEELS SWITCH. A MAINTENACNE ACCEPTANCE FLIGHT WAS REQUIRED AND PERFORMED SATISFACTORILY. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996071800951 19960718 00951 EU 1996 7 18 VTZA96238 1 19960630 A 7712 31024762 TQ SIGNAL COND BAG JETSTM JETSTM3201 1500217 EU LT ENG OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 471UE 821 FLT 6920 - LYH-IAD - ABORTED THE TAKEOFF DUE TO THE LEFT ENGINE NOT MAKING TAKEOFF TORQUE. AIRCRAFT RETURNED TO GATE WI TH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED THE TORQUE SIGNAL CONDITIONER. AIRCRAFT WAS RELEASED AND APPROVED FOR RE TURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996071800952 19960718 00952 NM 1996 7 18 W8PA960047 1 19960701 A 3350 BATT/CHARGER BOEING 737 7373B7 1384580 NM CABIN FAILED A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 509AU 23384 DURING A3 CHECK, FOUND EMERGENCY EXIT LIGHTS INOP FOR L-1 DOOR EXIT. REPLACED EMERGENCY BATTERY CHARGER/BATTERY ASSEMBL Y. (M) 2 L 7 2 4F RT A16WE 1996071800953 19960718 00953 SO 1996 7 18 WTAA960130 1 19960616 A 7931 OIL PRESS LIGHT EMB 120 EMB120RT SO COCKPIT ILLUMINATED A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 WP 17 285UE 120153 SFO - LOW OIL PRESSURE LIGHT CAME ON DURING TAKEOFF. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE INSPECTED BOTH ENGI NES FOR LEAKS AND CHAFED WIRES. NO DEFECTS NOTED. LOW OIL PRESSURE WARNING LIGHT SYSTEM OPERATIONAL CHECK NORMAL DURIN G ENGINE GROUND RUN. UNABLE TO DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996071800954 19960718 00954 EU 1996 7 18 Y2PA96039 1 19960614 A 2810 FUEL CAP AMD FALC20 FALCOND 2720304 EU RT WING LOOSE A Y2PA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 GL 23 815AA 205 Y2PA - CREW MADE AN UNSCHEDULED LANDING AFTER ANOTHER AIRCRAFT REPORTED FUEL SIPHONING FROM RIGHT WING AFTER DEPARTURE F ROM LGC. THIS WAS VERIFIED BY THE CREW. NO EMERGENCY PROCEDURES NECESSARY. AIRCRAFT RETURNED TO LGC. MECHANIC AT LGC FOUND RIGHT FUEL CAP UNSEATED. CAP WAS REMOVED AND INSPECTED WITH NO FAULTS BEING DISCOVERED. CAP WAS REINSTALLED AND SHOWED NO LEAKAGE OF PRESSURE OF FUEL DURING ENGINE RUN. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A7EU 1996071800955 19960718 00955 EU 1996 7 18 Y2PA96040 1 19960618 A 3260 A223802 SQUAWT SWITCH AMD FALC20 FALCOND 2720304 EU NLG FAILED A Y2PA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 817AA 00213V 233 YIP - LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM YIP. AIRCRAFT RETURNED TO YIP AND MADE AN UNSCHEDULED LANDING. NO EMERGENCY PROCEDURES REQUIRED. PROBLEM WAS DUPLICATED. REPLACED THE NOSE LANDING GEAR SQUAWT SWITCH. LANDING GEAR WAS CYCLED AND OPERATIONALLY CHECK PER FALCON MM 32-60-10 WITH NO DEFECTS NOTED. (M) 2 L 7 2 4F A7EU 1996071800956 19960718 00956 EU 1996 7 18 Y2PA96041 1 19960619 A 2810 350012 FUEL CAP AMD FALC20 FALCOND 2720304 EU RT WING WORN A A Y2PA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 GL 23 817AA 233 YIP - CREW DISCOVERED FUEL VENTING FROM RIGHT WING AFTER TAKEOFF FROM YIP. UNSCHEDULED LANDING MADE, AIRCRAFT RETURNED TO YIP. NO EMERGENCY PROCEDURES REQUIRED. MAINTENANCE FOUND THE FUEL CAP TO BE DEFECTIVE DUE TO A WORN LOCKING PRONG. FUEL CAP WAS REPLACED WITH A SERVICEABLE PART. AIRCRAFT WAS RUN UP AND FUEL CAP SHOWED NO LEAKAGE OF PRESSURE DURING E NGINE RUN. (M) 2 L 7 2 4F A7EU 1996071800957 19960718 00957 EU 1996 7 18 Y2PA96042 1 19960620 A 2810 350012 FUEL CAP AMD FALC20 FALCOND 2720304 EU LT/RT WING LEAKING A A Y2PA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 GL 23 821AA 203 LIT - CREW MADE AN UNSCHEDULED LANDING AFTER OBSERVING FUEL SPRAY FROM BOTH WING FUEL CAPS. AIRCRAFT RETURNED TO POINT OF DEPARTURE AT LIT. NO EMERGENCY PROCEDURES NECESSARY. CAPS REMOVED AND INSPECTED PER FALCON MM 28-00, PG 601. NO DE FECTS NOTED. AIRCRAFT DEPARTED AND RETURNED ONCE AGAIN AFTER FUEL SPRAY OBSERVED FROM LEFT WING. USA JET MECHANIC SENT TO LIT RESOLVE PROBLEM. INSPECTED LEFT FUEL CAP AND REPLACED WITH A SERVICEABLE UNIT. THE RIGHT WING FUEL CAP WAS ALS O INSPECTED, ALTHOUGH IT DID NOT LEAK AND NO DEFECTS WERE NOTED, BUT FOR PRECAUTIONARY REASONS THE CAP WAS REPLACED. (M ) 2 L 7 2 4F A7EU 1996071800958 19960718 00958 EU 1996 7 18 Y2PA96043 1 19960624 A 2810 C381521A FUEL FILTER AMD FALC20 FALCOND 2720304 EU RT WING LEAKING A A Y2PA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 GL 23 817AA 233 YIP - TOWER REPORTED FUEL VENTING FROM RIGHT WING AFTER TAKEOFF FROM YIP. UNSCHEDULED LANDING MADE, AIRCRAFT RETURNED T O YIP. NO EMERGENCY PROCEDURES REQUIRED. MX REPLACED THE FUEL FILTER/FILLER ASSEMBLY IN THE RIGHT WING WITH A SERVICEA BLE PART. AIRCRAFT WAS RUN UP AND FUEL CAP SHOWED NO LEAKAGE OF PRESSURE DURING ENGINE RUN. THIS IS THE SECOND TIME TH AT THIS AIRCRAFT HAS HAD FUEL VENTING FROM RIGHT WING FUEL FILLER. THE FUEL CAP WAS REPLACED THE PRIOR INCIDENT. (M) 2 L 7 2 4F A7EU 1996071800959 19960718 00959 WP 1996 7 18 Y2PA96044 1 19960622 A 3231 RETRACT MECH DOUG DC9 DC915F 3022037 WP LT/RT MLG DOOR OUT OF ADJUST A Y2PA O OTHER J WARNING INDICATION LD LANDING 1 GL 23 195US 47017 GEAR DOOR OPEN LIGHT STAYED ON WITH GEAR DOWN AND LOCKED, FOLLOWED EMERGENCY PROCEDURE 2-32-6. AIRCRAFT FERRIED TO DFW FOR MX BOTH MAIN LANDING GEAR DOORS SCUFFED ON LANDING. ADJUSTED LANDING GEAR PUSH/PULL CABLES, CHECKED DOOR LATCH MECH ANISM CLEARANCES. PERFORMED SRM REPAIRS ON LT/RT GEAR DOORS IAW SRM 52-01 FIG 2. (M) 2 L 7 2 4F A6WE 1996071800960 19960718 00960 WP 1996 7 18 Y2PA96045 1 19960625 A 3233 39136585503 ACTUATOR DOUG DC9 DC915F 3022037 WP RT MLG FAILED A Y2PA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 194US 47016 YIP - WITH GEAR RAISED AFTER TAKEOFF RIGHT GEAR UNSAFE LIGHT AND GEAR DOOR OPEN LIGHT CAME ON, GEAR WAS CYCLED AND LIGHT S REMAINED ON. REMOVED AND REPLACED RT MLG ACTUATOR. FOUND LOOSE RIGHT GEAR DOOR SWITCH, TIGHTENED MOUNTING BOLTS. OP S CHECK GOOD. (M) 2 L 7 2 4F A6WE 1996071800961 19960718 00961 WP 1996 7 18 96006122804 1 19960215 A 5320 DOOR FRAME DOUG DC10 DC1030 3023501 WP FS 1305 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 228NW 7549 70309 46578 R-3 DOOR LOWER AFT FRAME AT FS 1305, STR 27 FOUND CRACKED INSIDE LIGHTING HOLE. REMOVED EXISTING DOUBLER. STOP DRILLED CRACK AND VERIFIED BY NDT CRACK DOES NOT GO PAST STOP DRILL. FABRICATED AND ISNTALLED DOUBLER IAW SRM 53-50-00, FIGURE 19. (X) 2 L 7 3 4F A22WE 1996071800962 19960718 00962 WP 1996 7 18 96007122805 1 19960215 A 5320 DOOR FRAME DOUG DC10 DC1030 3023501 WP FS 1305 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 228NW 75849 20309 46578 L-3 DOOR FRAME, FS 1305, STR 26, CLOSE OUT PANEL HAS 2 EACH ONE INCH LONG CRACKS INSIDE LOWER INSPECTION HOLE. REMOVED EXISITNG DOUBLER, STOP DRILLED CRACKS, AND VERIFIED BY NDT CRACKS DO NOT GO PAST STOP DRILL. FABRICATED DOUBLER AND INS TALLED IAW SRM 53-50-00, FIGURE 19. (X) 2 L 7 3 4F A22WE 1996071800963 19960718 00963 WP 1996 7 18 96008122806 1 19960215 A 5320 DOOR FRAME DOUG DC10 DC1030 3023501 WP FS 1254 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 228NW 75849 20309 46578 L-3 DOOR FRAME, FS 1254, STR 27, CLOSE OUT PANEL HAS 2 EACH ONE INCH LONG CRACKS INSIDE LOWER INSPECTION HOLE. REMOVED EXISITNG DOUBLER, TRIMMED OUT CRACKS, AND VERIFIED BY NDT CRACKS WERE TRIMMED OUT. FABRICATED DOUBLER AND INSTALLED IAW SRM 53-50-00, FIGURE 19. (X) 2 L 7 3 4F A22WE 1996071800964 19960718 00964 WP 1996 7 18 96011122807 1 19960220 A 5320 CLIP DOUG DC10 DC1030 3023501 WP NLG WW CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 228NW 75849 20309 46578 ON NOSE WHEELWELL FORWARD OF PANEL 115AZ BETWEEN LONGERON 51R AND LONGERON 51L IN AVIONICS COMPARTMENT, FOUND 14 EACH CO RRODED HILOC FASTENERS AND 2 EACH CORRODED T-CLIPS. REMOVED AND REPLACED 14 EACH HILOCS. FABRICATED AND INSTALLED 2 EA CH T-CLIPS IAW SRM 53-00-01 AND SRM 51-33-01. (X) 2 L 7 3 4F A22WE 1996071800965 19960718 00965 WP 1996 7 18 96012122808 1 19960220 A 5315 AGA70821 FLOOR BEAM DOUG DC10 DC1030 3023501 WP FS 1880 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 228NW 75849 20309 46578 RIGHT MAIN FLOOR SUPPORT BEAM AT FS 1880 RT, RBL 36 IS CORRODED BEYOND SRM LIMITS. REMOVED AND REPLACED FLOOR SUPPORT B EAM IAW SRM 51-30-00. (X) 2 L 7 3 4F A22WE 1996071800966 19960718 00966 WP 1996 7 18 96013122809 1 19960220 A 5313 AGA30182 LONGERON DOUG DC10 DC1030 3023501 WP FS 1953-1975 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 228NW 75849 20309 46578 LONGERON 15R BETWEEN FS 1953 AND FS 1975 HAS 2 AREAS OF INTERGRANULAR CORROSION. CUT FRAMES AT FS 1953, FS 1964, AND FS 1975 PER SRM 53-30-00, FIGURE 5. REPLACED LONGERON 15R IAW MFG DWG AGA3018-2. FABRICATED SPLICES AND REINSTALLED FRAM ES IAW SRM 53-30-00, FIGURE 5. (X) 2 L 7 3 4F A22WE 1996071800967 19960718 00967 WP 1996 7 18 96014122810 1 19960227 A 5230 DOOR FARME DOUG DC10 DC1030 3023501 WP CARGO DOOR BLEND OUT A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 228NW 75849 20309 46578 FOUND DEEP BLEND-OUT AND NON-SRM REPAIR (KNIFE EDGE BLEND-OUT) ON AFT LOWER CORNER OF FORWARD CARGO DOOR FRAME. FABRICA TED AND INSTALLED DOUBLER AND FILLER REPAIR PER SRM 53-50-00, FIGURE 9, SHEET 1 EXCEPT EXTENDED EXTERNAL DOUBLER AFT TO PICK UP 2 ROWS BEYOND BLEND-OUT (REFERENCE LACI ENGINEERING ORDER NR 3575). (X) 2 L 7 3 4F A22WE 1996071800968 19960718 00968 WP 1996 7 18 96015123001 1 19960312 A 2560 ABA8262501 GIRT BAR HOOK DOUG DC10 DC1030 3023501 WP L1 DOOR CORROSION A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 230NW 46552 L1 DOOR AFT GIRT BAR HOOK HAS EXCESSIVE PITTING CORROSION APPROXIMATELY 6 SQUARE INCHES. REMOVED AND REPLACED AFT GIRT BAR HOOK IAW NR 2162. (X) 2 L 7 3 4F A22WE 1996071800969 19960718 00969 WP 1996 7 18 96016122811 1 19960305 A 5340 TRUNNION FTG DOUG DC10 DC1030 3023501 WP LT MLG WORN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 228NW 75849 20309 46578 LEFT MLG TRUNNION FITTING ATTACHING BORES (AFT TOP AND BOTTOM) (RETRACT ACTUATOR A-FRAME) ARE RE-WORKED BEYOND MAXIMUM L IMITS PER NWA SA5743-01026-5, NOTE 2. OVERSIZED BORES TO 1.0075 INCHES PER STEP 1 NWA SA5743-01026-5. FABRICATED AND I NSTALLED BUSHINGS. ALL REPAIRS ACCOMPLISHED IAW NWA SA5743-01026-5. (X) 2 L 7 3 4F A22WE 1996071800970 19960718 00970 WP 1996 7 18 96017122812 1 19960305 A 3233 ARB380014 ACTUATOR MOUNT DOUG DC10 DC1030 3023501 WP RT MLG CORROSION A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 228NW 75849 20309 46578 FOUND LIGHT PITTING CORROSION ON THE RIGHT MLG RETRACT CYLINDER MOUNTING SURFACE ON TRUNNION WITH LIGHT GALVANIC CORROSI ON IN THE BORES. MECHANICALLY REMOVED CORROSION ON MLG RETRACT CYLINDER MOUNTING SURACE AND ON BORES. FABRICATED AND I NSTALLED FILLER. REPAIRS ACCOMPLISHED IAW LACI ENGINEERING ORDER NR 3594 AND DRW SA5743-01026-2. (X) 2 L 7 3 4F A22WE 1996071800971 19960718 00971 WP 1996 7 18 96018122813 1 19960305 A 3233 ARB380013 ACTUATOR FTG DOUG DC10 DC1030 3023501 WP LT MLG CORROSION A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 228NW 75849 20309 46578 DURING ACCOMPLISHMENT OF CORROSION REWORK OF THE LEFT MLG TRUNNION FITTING (NWA STOCK NR 12-5743-9-0001) PER SA5743-0102 6-5, CORROSION ON THE LOWER AFT MLG ACTUATOR FITTING LUG EXCEEDED THE LIMITS OF SA5743-01026-5. THE REMAINING ATTACH AR EAS WERE BLENDED WITHIN LIMITS. AT LOWER AFT MOUNT PAD LOCATION, REMOVED CORROSION BY SPOTFACING THE CORRODED AREA. FA BRICATED FILLER WASHER WITH THE SAME THICKNESS AS CORROSION REMOVAL DEPTH. INSTALLED PER LACI ENGINEERING ORDER NR 3598 REV A. (X) 2 L 7 3 4F A22WE 1996071800972 19960718 00972 WP 1996 7 18 96019122814 1 19960305 A 5320 ADA34391 JAMB DOUG DC10 DC1030 3023501 WP R2 DOOR CORROSION A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 228NW 75849 20309 46578 CORROSION WAS FOUND ON THE R-2 DOOR JAMB UPPER FLANGE, INBOARD SURFACE. CORROSION REMOVAL WAS BEYOND LIMITS BETWEEN STA 791 AND STA 860. FABRICATED 2 EACH FILLERS AND ANGLES AND INSTALLED IAW LACI ENGINEERING ORDER NR 3617, REV. D (REFERE NCE DAC MESSAGES MISC-0794/JH, MISC-0884/RLT, MISC-1093/JAH, AND MISC-1239/JAH). (X) 2 L 7 3 4F A22WE 1996071800973 19960718 00973 WP 1996 7 18 96ZZZX3637 1 19960608 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 EICBH 47796 HNL - FLT 128 - COCKPIT AND CABIN EMERGENCY LIGHTS WILL NOT ILLUMINATE. REPLACED BATTERIES, OPS CHECK GOOD. (X) 2 L 7 2 4F A6WE 1996071800974 19960718 00974 EU 1996 7 18 96ZZZX3638 1 19960513 A 2760 P308450058 SWITCH BAG BAE146 BAE146100A 1500260 EU NR 2 SPOILER MALFUNCTIONED A TIXA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 19 117TR E1017 SPOILER UNLOCK LIGHT ILLUMINATED IN-FLIGHT. PERFORMED SPOILER SYSTEM TEST PER MM 27-61-11, PAGE 208 - PAGE 212. NR 2 S POILER FAILED ONCE DURING SEVERAL CHECKS OF THE SYSTEM. REPLACED NR 2 SPOILER MICROSWITCH IAW MM 27-61-11, PRECAUTIONAR Y. PERFORMED SATISFACTORY TEST FLIGHT PRIOR TO RELEASING AIRCRAFT FOR REVENUE SERVICE. 2 H 7 4 4F RT A49EU 1996071800975 19960718 00975 SO 1996 7 18 GLBA96062 1 19960317 A 2750 3075001017 CONTROL UNIT EMB 120 EMB120RT SO TE FLAPS MALFUNCTIONED A GLBA O OTHER F FLT CONT AFFECTED AP APPROACH 1 CE 01 279UE 0101 120085 SAV - CREW REPORTED FLAP ASYMMETRY FAULT ON APPROACH. FAULT COULD NOT BE DUPLICATED ON GROUND, BUT LATER RECURRED. MAI NTENANCE AT RDU REMOVED AND REPLACED CONTROL UNIT. SYSTEM CHECKS OK ON GROUND. (X) 2 L 7 2 4T RT A31SO 1996071800976 19960718 00976 SO 1996 7 18 GLBA96069 1 19960411 A 3246 31544 WHEEL ASSY EMB 120 EMB120RT SO RT MLG FAILED A GLBA O OTHER D INFLIGHT SEPARATION LD LANDING 1 CE 01 452UE 2824 120096 ORD - CREW REPORTED THE RIGHT INBOARD MAIN WHEEL BROKE DURING LANDING AND DEPARTED THE AIRCRAFT. WHEEL STRUCK LEFT INBO ARD AFT GEAR DOOR. MAINTENANCE REPLACED RIGHT INBOARD MAIN TIRE AND WHEEL ASSY AND LEFT INBOARD GEAR DOOR. MAINTENANCE ALSO REPAIRED STRUCTURAL DAMAGE TO NACELLE ABOVE LEFT INBOARD AFT GEAR IAW EMBRAER SRM 54-10-01. GEAR SWING, OPS CHECK WAS GOOD. DOOR S/N, 46. (X) 2 L 7 2 4T RT A31SO 1996071800977 19960718 00977 EU 1996 7 18 SIMA961401 1 19960519 A 3350 330150 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 373AE 1081 340B373 DFW - FLT 3689 - OVERHEAD EMERGENCY LIGHT ON 10A AND 12A INOPERATIVE. EMERGENCY EXIT LIGHTS OUT ON OVERWING DOOR. REPL ACED POWER SUPPLY AT 24LN IAW AMM 33-50-10. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1996071800978 19960718 00978 EU 1996 7 18 SIMA961411 1 19960520 A 3350 330150 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 373AE 1063 340B373 DFW - FLT 3726 - EMERGENCY EXIT LIGHTS 8A, B, AND C INOPERATIVE. REPLACED POWER SUPPLY. AIRCRAFT WAS RETURNED TO SERVI CE. (X) 2 L 7 2 4T RT A52EU 1996071800979 19960718 00979 NE 1996 7 18 SIMA961501 2 19960529 A 7261 3022383 GARLOCK SEAL AEROSP ATR72 ATR72212 EU PWA PW120 PW127 NE NR 2 ENGINE TORN A SIMA E ENGINE SHUTDOWN J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SW 21 322AC 320 127065 DFW - FLT 3620 - NR 2 ENGINE LOST OIL PRESSURE WITH ALL WARNINGS. CREW SHUT DOWN ENGINE AND LANDED WITHOUT INCIDENT. R EMOVED AND INSTALLED AC WILD GENERATOR GARLOCK SEAL IAW P AND W MM 72-10-00. AIRCRAFT WAS RETURNED TO SERVICE. PART TO TAL CYCLES 4,692. (X) 2 H 7 2 4T 4 T RT A53EU E20NE 1996072200001 19960722 00001 NM 1996 7 22 DL73S961621 1 19960209 A 5315 6545410223 FLOOR BEAM BOEING 737 737232 1384475 NM BS 664 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 328DL 23100 THE BL 0 FLOOR BEAM OF THE WING CENTER SECTION IS CRACKED AT FS 664. NO CRACKS WERE FOUND ON THE WEB. THE CRACK IS TYP ICAL PER BOEING SERVICE BULLETIN 737-57-1210. 2 L 7 2 4F RT A16WE 1996072500001 19960725 00001 EU 1996 7 25 9615223214 1 19960713 A 3350 321454 POWER SUPPLY AIRBUS 320 A320211 3930320 EU CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 314US 15244 3191 160 DURING LINE MAINTENANCE, FOUND THE CENTER EMERGENCY EXIT LIGHT AND LEFT OVERWING EXIT LIGHT INOPERATIVE. REPLACED POWER SUPPLY UNIT. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996072500002 19960725 00002 EU 1996 7 25 9615233214 1 19960715 A 3350 321454 POWER SUPPLY AIRBUS 320 A320211 3930320 EU CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 314US 12378 1496 160 DURING LINE MAINTENANCE, THE EMERGENCY LIGHTS TEST SHOWED UNIT EMER L. EPSU 11WL FAILED SELF-TEST. REPLACED POWER SUPPL Y UNIT. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996072500003 19960725 00003 NM 1996 7 25 9615246603 1 19960712 A 3350 POWER SUPPLY BOEING 747 747151 1384891 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 603US 19780 DURING LINE CHECK, FOUND EXIT SIGN AND CEILING EMERGENCY LIGHT OUT AT DOOR 1R. ALSO, FOUND FLOOR PATH EMERGENCY LIGHT I NOPERATIVE BY NR 2 GALLEY. REPLACED EXIT SIGN, POWER SUPPLY, AND LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996072500004 19960725 00004 WP 1996 7 25 9615259861 1 19960714 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 770NC 47758 DURING LINE CHECK, FOUND AFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERIES. OPERATIO NAL CHECK GOOD. 2 L 7 2 4F A6WE 1996072500005 19960725 00005 EU 1996 7 25 9615263227 1 19960712 A 2150 757A000008 ACM AIRBUS 320 A320211 3930320 EU NR 1 SEIZED A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 01 327NW 11613 11613 297 FUMES PRESENT IN COCKPIT AND CABIN FOLLOWED BY A PACK ONE OVERHEAT MESSAGE. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURE S AND THE FUMES CEASED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT AT THE ORIGINAL DESTINATION. MAINTENANCE FOUND THE NR 1 PACK AIR CYCLE MACHINE SEIZED AND A CLAMP ON THE PACK OUTLET DUCT BROKEN. REPLACED THE AIR CYCLE MACHINE AND CLAMP. LEAK AND OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996072500006 19960725 00006 NM 1996 7 25 9615272710 1 19960715 A 3260 IND LIGHTS BOEING 727 727225 1384077 NM LANDING GEAR MALFUNCTIONED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 820EA 22557 DURING APPROACH ON GEAR EXTENSION, ALL GEAR INDICATION LIGHTING GREEN AND RED CAME ON. GEAR WAS CYCLED A SECOND TIME. A LL INDICATIONS WERE NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED LANDING GEAR TEST OF SYSTEM. CHEC KED OK. 2 L 7 3 4F A3WE 1996072500007 19960725 00007 WP 1996 7 25 9615289941 1 19960624 A 5711 CHORD DOUG DC9 DC932 3022066 WP WS 58-76 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3324L 47103 DURING H-CHECK, FOUND CORROSION ON THE FORWARD SPAR LOWER CAP, WS 58 - 76, LEFT SIDE. REPAIRED CAP (P/N 5911307-505) PE R EA 99-110530. 2 L 7 2 4F A6WE 1996072500008 19960725 00008 WP 1996 7 25 9615299305 1 19960625 A 5511 SPAR DOUG DC9 DC982 3022082 WP LT HORIZ STAB CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 307RC 48086 DURING H-CHECK, FOUND CORROSION ON THE LEFT HORIZONTAL STABILIZER UPPER AND LOWER SPAR CAPS AT STA 169. REPAIRED CAPS P ER EA 93-105338. 2 L 7 2 4F A6WE 1996072500009 19960725 00009 WP 1996 7 25 9615301161 1 19960627 A 5751 SKIN DOUG DC10 DC1040 3023508 WP LT AILERON CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 161US 46770 DURING LINE CHECK, FOUND A CRACK IN THE LEFT OUTBOARD AILERON UPPER SKIN AT THE NR 5 RIB. REPAIRED PER EA 11-105126. 2 L 7 3 4F A22WE 1996072500010 19960725 00010 WP 1996 7 25 9615319305 1 19960628 A 5320 WEB DOUG DC9 DC982 3022082 WP FS 200 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 307RC 48086 DURING H-CHECK, FOUND CORROSION IN THE FS 200 CUSP WEB, LEFT SIDE. REPAIRED CUSP (P/N 9910078-9) PER EA 93-105341. 2 L 7 2 4F A6WE 1996072500011 19960725 00011 WP 1996 7 25 9615329940 1 19960630 A 5720 SPLICE DOUG DC9 DC932 3022066 WP WS 91 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3322L 47031 DURING M-CHECK, FOUND CORROSION ON THE LOWER FORWARD SPAR CAP SPLICE PLATE AT XRS 91, LEFT SIDE. REPAIRED SPLICE (P/N 3 912208-1) PER EA 99-109071. 2 L 7 2 4F A6WE 1996072500012 19960725 00012 WP 1996 7 25 9615339941 1 19960701 A 5711 SPAR DOUG DC9 DC932 3022066 WP WS 58-112 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3324L 47103 DURING H-CHECK, FOUND CORROSION ON THE LEFT WING LOWER REAR SPAR CAP (XW 58 - XRS 91) AND SPAR CAP SPLICE T (XRS 112). R EPAIRED CAP (P/N 5911305-503) AND T (P/N 5911357-1) PER EA 99-110801, 99-110805. 2 L 7 2 4F A6WE 1996072500013 19960725 00013 WP 1996 7 25 9615349305 1 19960701 A 5347 TRACK DOUG DC9 DC982 3022082 WP FS 408-427 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 307RC 48086 DURING H-CHECK, FOUND CORROSION ON THE FORWARD CARGO TIE DOWN TRACK, LEFT SIDE, FS 408 - 427. REPAIRED TRACK (P/N 59365 94-521N) PER EA 93-105343. 2 L 7 2 4F A6WE 1996072500014 19960725 00014 WP 1996 7 25 9615359305 1 19960701 A 5311 FRAME DOUG DC9 DC982 3022082 WP FS 1418 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 307RC 48086 DURING H-CHECK, FOUND CRACKS IN THE FS 1418 FRAME FROM LONGERON 2L - 2R. REPAIRED FRAME PER EA 93-105348. 2 L 7 2 4F A6WE 1996072500015 19960725 00015 NM 1996 7 25 9615362285 1 19960701 A 5313 LONGERON BOEING 727 727251 138408H NM FS 1000 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 2856S 21324 DURING H-CEHCK, FOUND CORROSION ON STR 29L AT FS 1000. REPAIRED STRINGER (P/N 65-56441) PER EA 22-105471. 2 L 7 3 4F A3WE 1996072500016 19960725 00016 WP 1996 7 25 9615379983 1 19960704 A 5711 SPAR DOUG DC9 DC932 3022066 WP WS 547-554 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 983US 47282 DURING H-CHECK, FOUND CORROSION ON THE LEFT WING FORWARD SPAR LOWER CAP FROM XFS 547 - 554. REPAIRED CAP (P/N 5919153-1 ) PER EA 99-110821. 2 L 7 2 4F A6WE 1996072500017 19960725 00017 WP 1996 7 25 9615389909 1 19960708 A 5320 STOP FITTING DOUG DC9 DC931 3022065 WP PAX DOOR JAMB CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 959N 47255 DURING M-CHECK, FOUND A CRACK IN THE AFT ENTRY DOOR JAMB LOWER RIGHT STOP FITTING. REPLACED FITTING PER SRM 51-30-2. 2 L 7 2 4F A6WE 1996072500018 19960725 00018 WP 1996 7 25 9615399941 1 19960710 A 5713 LONGERON DOUG DC9 DC932 3022066 WP WS 58-98 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3324L 47103 DURING H-CHECK, FOUND CORROSION ON THE LEFT WING STR 15, WS 58 - 72, 88, AND 96 - 98. REPAIRED STRINGER (P/N 5919237-50 1) PER EA 99-109161, 99-110814. 2 L 7 2 4F A6WE 1996072500019 19960725 00019 WP 1996 7 25 9615409961 1 19960711 A 5753 HINGE FITTING DOUG DC9 DC931 3022065 WP LT TE FLAP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 924RW 70238 47185 DURING H-CHECK, FOUND CORROSION IN THE LEFT FLAP NR 4 FORWARD HINGE IN LOWER STUD HOLES. REPLACED FITTING (P/N 5912596- 501) PER CITEXT 90-2750-1-9806. 2 L 7 2 4F A6WE 1996072500020 19960725 00020 WP 1996 7 25 9615419101 1 19960711 A 7120 MOUNT DOUG DC9 DC915 3022036 WP NR 1 ENGINE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 91S 47063 DURING LINE CHECK, FOUND CORROSION IN THE NR 1 ENGINE AFT MOUNT. REPLACED MOUNT. 2 L 7 2 4F A6WE 1996072500021 19960725 00021 WP 1996 7 25 9615429101 1 19960712 A 7120 YOKE DOUG DC9 DC915 3022036 WP NR 1 ENGINE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 91S 47063 DURING LINE CHECK, FOUND CORROSION IN THE NR 1 ENGINE LOWER AFT PYLON YOKE. REPLACED YOKE. 2 L 7 2 4F A6WE 1996072500022 19960725 00022 WP 1996 7 25 9615439154 1 19960712 A 5320 FITTING DOUG DC9 DC914 3022034 WP BS 802 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8913E 45830 DURING H-CHECK, FOUND CORROSION ON THE FS 802 FRAME TO RIGHT CUSP FITTING. REPLACED FITTING PER SRM 51-30. 2 L 7 2 4F A6WE 1996072500023 19960725 00023 WP 1996 7 25 9615449921 1 19960713 A 5230 FITTING DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 943N 47647 DURING H-CHECK, FOUND A CRACK IN THE AFT CARGO DOOR NR 5 BEAM END FITTING FORWARD END. REPLACED FITTING PER SRM 51-30-5 . 2 L 7 2 4F A6WE 1996072500024 19960725 00024 WP 1996 7 25 9615459952 1 19960714 A 5320 FITTING DOUG DC9 DC931 3022065 WP FS 227 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 916RW 47144 DURING M-CHECK, FOUND CORROSION ON THE FS 227 SPLICE FITTING, RIGHT SIDE. REPLACED FITTING PER SRM'S 51-30-5, 51-10-3, AND 51-10-4. 2 L 7 2 4F A6WE 1996072500025 19960725 00025 WP 1996 7 25 9615461159 1 19960716 A 3350 POWER SUPPLY DOUG DC10 DC1040 3023508 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 159US 46768 DURING LINE INSPECTION, FOUND THE ESCAPE EMERGENCY FLOOR LIGHT AT DOOR 3L AND 3R INTERMITTENT. REPLACED BATTERY POWER S UPPLY. 2 L 7 3 4F A22WE 1996072500026 19960725 00026 NE 1996 7 25 9615471143 2 19960716 A 7230 ENGINE DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 2 STALLED A NWAA O OTHER R PARTIAL RPM/PWR LOSS DE DESCENT 1 GL 01 133JC 46752 86135 EN ROUTE LAX-HNL, THE NR 2 ENGINE EXPERIENCED TOP OF DESCENT STALL WHEN POWER WAS RETARDED. CREW FOLLOWED COCKPIT OPERA TING PROCEDURE AND FLIGHT CONTINUED TO HNL WITHOUT FURTHER INCIDENT. VISUAL INSPECTION OF THE NR 2 ENGINE REVEALED NO D ISCREPANCIES. BORESCOPE OF HPC INCLUDING THE 13TH, 15TH STAGE STATOR, COMBUSTION CHAMBER, AND THE HPT WILL BE DONE WITH IN FIVE CYCLES. 2 L 7 3 4F 4 F A22WE E20EA 1996072500027 19960725 00027 WP 1996 7 25 9615489851 1 19960715 A 2130 54447211 ACTUATOR DOUG DC9 DC951 3022051 WP OUTFLOW VALVE MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 760NC 2485 507 47708 AIRCRAFT WOULD NOT PRESSURIZE IN AUTO AFTER TAKEOFF. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE R EPLACED CONTROLLER, PRE-PRESSURE CONTROLLER AND AMPLIFIER; ALL WITH NO HELP. REPLACED OUTFLOW VALVE ACTUATOR. OPERATIO NAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996072500028 19960725 00028 WP 1996 7 25 9615499955 1 19960715 A 3010 SYLZ9885 ELECT CONTROL DOUG DC9 DC931 3022065 WP ANTI-ICE MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 922RW 50935 276 47182 RIGHT ICE PROTECTION TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. AIRFOIL ICE PROTECTION PRESSURE ABNORMAL LIGHT A LSO ILLUMINATED. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAITNENANCE REPLACED RIGHT ANTICIPATOR AND THERMO STAT WITH NO HELP. REPLACED RIGHT ELECTRONIC THERMAL CONTROL UNIT. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SER VICE. 2 L 7 2 4F A6WE 1996072500029 19960725 00029 NM 1996 7 25 96FDEA01257 1 19960701 A 5320 69631561 SHEAR TIE BOEING 727 7272D4 138407U NM BS 700 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 287FE 21849 DISCREPANCY: (NR 0156) (018) CORROSION (C53-115-010) IN THE FORWARD CARGO BAY SHEAR-TIE, BS 700, WL 148, LBL 5. CORREC TIVE ACTION: REMOVED CORRODED SHEAR TIE, FABRICATED AND INSTALLED NEW SHEAR TIE ALL PER SRM 53-10-1 AT BS 700, WL 148, BLB, CORROSION FOUND TO BE OUT OF LIMITS. 2 L 7 3 4F A3WE 1996072500030 19960725 00030 WP 1996 7 25 96FDEA01258 1 19960716 A 2750 CONTROL CABLE DOUG DC10 DC1010CF 3023502 WP TE FLAPS OUT OF POSITION A FDEA O OTHER F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 SO 25 68052 47806 DISCREPANCY: GOT FLAP DISAGREE FLAG ON TOUCHDOWN, DID NOT RETRACT FLAPS. CORRECTIVE ACTION: FOUND LEFT FLAP CABLE OFF TRACK. REMOVED AND REPLACED LEFT BUS CABLES RIGGED PER MM 27-50-00. OPERATION CHECKED OK, I/B O/B OPERATIONALLY CHECK S NORMAL. 2 L 7 3 4F RT A22WE 1996072500031 19960725 00031 NM 1996 7 25 96FDEA01259 1 19960716 A 5320 69174065 GUSSET BOEING 727 72722 1384002 NM BS 825 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 DISCREPANCY: NR 0340 (032) FRAME GUSSET IS CRACKED AT BS 825, LBL 67, WL 197. CORRECTIVE ACTION: REMOVED AND REPLACED GUSSET AT BS 25, LBL 67, WL 197. 2 L 7 3 4F A3WE 1996072500032 19960725 00032 NM 1996 7 25 96FDEA01260 1 19960716 A 5315 65208279 FLOOR BEAM BOEING 727 72722 1384002 NM BS 600 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 DISCREPANCY: NR 0259(033) CORROSION (C53-111-01) AROUND NUTPLATES AROUND EXISTING FLOOR BEAM REPAIR STA 600 RBL 1, 5, 8, 12, 15, 19, 24, WL 198 (FWD BAY). CORRECTIVE ACTION: *****S/D******** COMING. 2 L 7 3 4F A3WE 1996072500033 19960725 00033 NM 1996 7 25 96FDEA01261 1 19960711 A 5313 6527132 STRINGER BOEING 727 72722 1384002 NM BS 540 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 DISCREPANCY: NR 0725 (034) WHILE WORKING NR 0722, FOUND CRACK UNDERNEATH FASTENER AT BS 540, STRINGER 24 LT. REPAIRED CRACK UNDERNEATH FASTENER AT BS 540, STR 24L PER FEDEX SRM 53-10-3. 2 L 7 3 4F A3WE 1996072500034 19960725 00034 NM 1996 7 25 96FDEA01262 1 19960626 A 5720 PL1201336 PL1 WASHER DOUG MD11 MD11 3023602 NM NR 2 FUEL TANK MISINSTALLED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 586FE 48487 DISCREPANCY: WHILE INCREASING MTOGW (SB 57-20) DISCREPANCY WAS FOUND THAT THE PL1-20-1336 WASHER AND PL1-16-1336 WASHER S ON THE UPPER AND LOWER BOLTS (81139-20-99 AND 81139-16-99) HAD BEEN INCORRECTLY INSTALLED PER MM 20-20-01, FIG 201. ( ALSO DPS 1.336). PER FIG 201, WASHER INDEX NR 5 BELONGS BEFORE AND AFTER PL1 WASHER WHERE INSTALLED, IN THIS CASE, WASH ERS WERE INSTALLED BOTH AFTER PL1 WASHER JUST BEFORE NUT INSTALLED. CORRECTIVE ACTION: BOLTS REMOVED FOR NDT TESTING A ND CHECKED GOOD. WASHERS REPLACED AND VERIFIED FOR CORRECT INSTALLATION. 2 L 7 3 4F RT A22WE 1996072500035 19960725 00035 NM 1996 7 25 96FDEA01263 1 19960718 A 3610 CLAMP BOEING 727 727225 1384077 NM NR 1 ENGINE LOOSE A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 SO 25 464FE 21288 DISCREPANCY: SHORTLY AFTER TAKEOFF (APPROXIMATELY 5 MINUTES) ENGINE NR 1 STRUT OVERHEAT LIGHT CAME ON FOR ABOUT 1 MINUT E THEN WENT OUT. COMPLIED WITH RED TABS, TESTED SATISFACTORY. CORRETIVE ACTION: FOUND LOOSE CLAMP BY SENSOR AND WAS B LOWING ON IT, TIGHTEN CLAMP, NO LEAKS NOTED ON SENSOR. OK FOR SERVICE THIS STATION.. 2 L 7 3 4F A3WE 1996072500036 19960725 00036 NM 1996 7 25 96FDEA01264 1 19960718 A 5712 RIB BOEING 727 72725C 138400H NM WS 436.5 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 116FE 19298 DISCREPANCY: NR 1 FUEL TANK RIB AT WING STA 436.5 CRACKED AT LOWER ATTACHMENT POINT FOR STRINGER, JUST AFT OF ACCESS OP ENING. CORRECTIVE ACTION: STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER PER SRM 57-10-5. 2 L 7 3 4F A3WE 1996072500037 19960725 00037 NM 1996 7 25 96FDEA01265 1 19960718 A 5320 FITTING BOEING 727 72725C 138400H NM BS 740 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 116FE 19298 DISCREPANCY: STRINGER END FITTING CRACKED STA 740, AFT SIDE, AT STRINGER 5 RT. CORRECTIVE ACTION: REMOVED AND REPLACE D STRINGER END FITTING PER SRM 51-10-01. 2 L 7 3 4F A3WE 1996072500038 19960725 00038 WP 1996 7 25 CKSA96074 1 19960712 A 3210 5715316 SIDE BRACE DOUG DC8 DC861 3021952 WP LT MLG WORN A CKSA O OTHER J WARNING INDICATION CR CRUISE 1 GL 23 817CK 45887 KORD - FLT 76824: GEAR FAILED UPLATCH CHECK, LEFT GEAR UNSAFE LIGHT STAYED ILLUMINATED, CYCLED GEAR TWICE. AIRCRAFT HAS BEEN INSPECTED AND FOUND SAFE FOR INTENDED FERRY FLIGHT PER AIA GMM REFERENCE 4-6-3. ADJUSTED LOWER LEFT MAIN LANDING GEAR FLYAWAY DOOR, LUBED LEFT MAIN LANDING GEAR UPLATCH, REPLACED LOWER SIDE BRACE ASSEMBLY. CONSISTS OF 2 EACH BOLTS P N 4771388-1, PN 3771403-1, 2 EACH BLOCK ASSEMBLIES PN 5715316, 1 LINK PN 5654774-503. COMPLIED WITH GEAR SWING, SWUNG G EAR SEVERAL TIMES. NO DEFECTS NOTED, GEAR OPS AND LEAK CHECKS GOOD. 2 L 7 4 4F 4A25 1996072500039 19960725 00039 EA 1996 7 25 COMA9660123 1 19960716 A 5230 H34153 HANDLE ASSY CNDAIR CL600 CL6002B19 EA CARGO DOOR CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 933CA 7040 CARGO DOOR LATCH RELEASE DOES NOT SPRING OPEN WHEN LATCH IS OPENED. REPLACED THE CARGO DOOR HANDLE AND HOUSING ASSY. 2 L 7 2 4F RT A21EA 1996072500040 19960725 00040 WP 1996 7 25 RRXA96039 1 19960716 A 5330 PANELS DOUG DC8 DC873F 302199F WP NLG WW LOOSE A RRXA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 15 870TV 46086 LEMD - FLT 362 - UPON GEAR RETRACTION, NOSE WELL AND NOSE GEAR AREA EXCESSIVE LOUD NOISE, RECYCLED GEAR 2 TIMES, NOISE R EMAINED WITH LOUD METALIC THUD, THEN QUIET. VISUAL INSPECTION OF NOSE GEAR REVEALED NO ANNOMALIES OF GEAR OR DOORS, HOW EVER, TWO INSPECTION PANELS WERE LOOSE AND BOTH CURTAINS WERE DOWN. REPLACED CURTAINS AND REPLACED SEVERAL SCREWS IN PA NELS. (M) 2 L 7 4 4F RT 4A25 1996072500041 19960725 00041 WP 1996 7 25 RRXA96040 1 19960716 A 3610 DUCT CLAMP DOUG DC8 DC863 302198A WP NR 2 ENGINE MISSING A RRXA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 WP 15 950R 45903 KDAY - FLT 27 - DURING CLIMB-OUT, NUMEROUS WARNING LIGHTS AND INDICATORS FOR NR 2 ENG CAME ON. GEN DRIVE OIL LIGHT, NR 2 START VLV OPEN LIGHT, GEN FAIL LIGHT, GEN UNPARALLED LIGHT, ENG OIL PRESS FRONT AND BACK AND CB'S OPENED ALL PERTAININ G TO NR 2 ENG, OIL PRESS AND TEMP AND INDICATORS WENT OFF SCALE HIGH THEN LOW. SHUTDOWN ENG NR 2 AT 0443Z, ENGINE OIL P RESS AND TEMP GAUGES AND LIGHTS WERE FAILED AND THERE WAS NO WAY TO MONITOR ENG. FOUND DUCT CLAMP MISSING FROM PNEU DUC T, AND NUMEROUS WIRING HARNESSES MELTED. A/C PREPARED FOR ONE ENG INOP FERRY PERMIT. R/R ALL ENG PYLON WIRING PLUGS AN D CLAMPS IAW DC8 MM 20-50-1. R/R ENG WIRING HARNESS IAW DC8 MM 70-40-1. ALL SYS OPS CHK GOOD ON ENG RUNUP. (M) 2 L 7 4 4F 4A25 1996072500042 19960725 00042 WP 1996 7 25 RRXA96041 1 19960716 A 7931 41800141 OIL PRESS XMITT DOUG DC8 DC863 302198A WP NR 4 ENG FAILED A RRXA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 WP 15 796AL 087844 46054 OBBI - DF8 - PRECAUTIONARY SHUTDOWN OF NR 4 ENGINE DUE TO LOW OIL PRESS READING BELOW 36 PSI (QTY AND TEMP OK). REMOVED AND REPLACED NR 4 ENGINE OIL PRESS X-MITTER PER MM CHAPTER 79. PERFORMED NR 4 ENGINE RUN PER EWWA ENGINE RUNUP MANUAL, NR 4 ENGINE OIL PRESS, OPS CHECKED NORMAL ON GROUND RUN. (M) 2 L 7 4 4F 4A25 1996072500043 19960725 00043 WP 1996 7 25 UPS96820609 1 19960715 A 5210 4613487 FITTING DOUG DC8 DC871F 302199D WP PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 DURING B-CHECK INSPECTION, FOUND FORWARD ENTRY DOOR DRAGGING. DURING TROUBLESHOOTING, FOUND LOWER FUSELAGE MOUNTED FITT ING ASSEMBLY FOR TORQUE TUBE CRACKED FITTING. REPLACEMENT C/W. 2 L 7 4 4F RT 4A25 1996072500044 19960725 00044 1996 7 25 UPS96820644 4 19960718 A 2562 LIFE RAFT ELT DOUG DC8 DC873F 302199F WP CABIN INOP A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 ELT BEACON RECEIVED ON 121.5 FOR ENTIRE FLIGHT. SUSPECT ELT IN AIRCRAFT LIFE RAFTS HAS GONE OFF. REMOVED AND REPLACED BOTH 6 MAN LIFE RAFTS. P/N OFF 600-107RB, S/N OFF 6523, P/N ON 600-107RB, S/N ON E-125, P/N OFF 600-107RB, S/N OFF 6538 , P/N ON 600-107RB, S/N ON F-172. 2 L 7 4 4F RT 4A25 1996072500045 19960725 00045 WP 1996 7 25 UPS96820645 1 19960617 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 1700 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE: C. LONGERON 34L CORRODED AT FS 1700 IN AFT ACCESSORY COMPT, AT TIE FITTING. REMOVED AND REPLACED CO RRODED LONGERON SECTION IAW DC8 SRM 53-3-2, ALODINED AND PRIMED AS REQUIRED IAW DC8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996072500046 19960725 00046 WP 1996 7 25 UPS96820646 1 19960618 A 5320 DOOR JAMB DOUG DC8 DC873F 302199F WP FS 300 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE: C. MAIN CARGO DOOR JAMB HAS A 2 INCH LONG CRACK ON LOWER AFT CORNER. CUT OUT CRACKED SECTION, FABRIC ATED NEW FRAME/JAMB SECTION, NEW SHIMS, ALODINED, AND INSTALLED IAW REO-02036 AND DC8 SRM 51-1-21, AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996072500047 19960725 00047 WP 1996 7 25 UPS96820647 1 19960620 A 5711 SPAR CAP DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE: C. CRACKS IN RIGHT LOWER SPAR CAP IN HOLES 4, 5, 6, 7, AND 10 -XW 454. REAMED HOLE NR 10, ALODINED A ND PRIMED IAW SRM 51-1-8, AND INSTALLED BUSHING IAW DWG J060232 HOLES 4, 5, 6, 7. REAMED HOLES, STRESS COINED HOLES IAW DPS 3.67-56 AND DAC DWG J060232. ALODINED AND PRIMED IAW 51-1-8, INSTALLED BUSHING IAW REO 02038 AND DAC DWG J060232 A ND SRM 51-1-25. FABRICATED REPAIR STRAP IAW REO 02038 AND DWG J060232. ALODINED AND PRIMED IAW 51-1-8. 2 L 7 4 4F RT 4A25 1996072500048 19960725 00048 WP 1996 7 25 UPS96820648 1 19960621 A 5730 PANEL DOUG DC8 DC873F 302199F WP LT/RT WING OUT OF LIMITS A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE: C. ACCOMPLISHED PERMANENT REPAIR TO LEFT AND RIGHT LEADING EDGE UPPER ATTACH HOLES PER SRM WAN NR 193 191. REPAIRED LEADING EDGE SLANT PANEL UPPER CAP IAW TIMCO REO 02029 AND ENGINEERING FILE DC8 57-0695. 2 L 7 4 4F RT 4A25 1996072500049 19960725 00049 WP 1996 7 25 UPS96820649 1 19960621 A 5400 SPAR CAP DOUG DC8 DC873F 302199F WP NR 1 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE: C. CRACKS IN FRONT UPPER SPAR CAP AND 508 BULKHEAD FITTING. REPAIRED FRONT UPPER SPAR CAP AND 508 BUL KHEAD FITTING, NR 1 PYLON POSITION IAW TIMCO REO-02058 AND ENGINEEERING FILE DC8-57-0690. 2 L 7 4 4F RT 4A25 1996072500050 19960725 00050 WP 1996 7 25 UPS96820650 1 19960622 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP NR 1 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE: C. .050 INCH CRACK AT T/E OF TEE DOUBLER. TRIMMED OUT DAMAGE AREA OF TEE DOUBLER, SHOT PEENED EDGE O F TRIM RADIUS, AND AREA OF UPPER AND LOWER SURFACE IN TRIM AREA PER OPS 4.999 CORROSION PROTECT ALL BARE METAL AND REWOR K AREA SRM 51-1-8 AND IAW TIMCO REO-02042. 2 L 7 4 4F RT 4A25 1996072500051 19960725 00051 WP 1996 7 25 UPS96820651 1 19960624 A 5311 FRAME DOUG DC8 DC873F 302199F WP FS 300 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE: C. LEFT CIRCUMFERENTIAL FRAME HAS A 3 INCH CRACK IN RADIUS AT FS 300, IN LOWER AFT CORNER OF MAIN CAR GO DOOR CUT-OUT. CUT OUT DAMAGED SECTION OF FRAME, FABRICATED NEW FRAME SECTION, IAW SRM 51-1-21 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996072500052 19960725 00052 WP 1996 7 25 UPS96820652 1 19960627 A 5400 DRAG ANGLE DOUG DC8 DC873F 302199F WP NR 3 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE: C. NR 3 PYLON DRAG ANGLE HAS SHEARED FASTENER HEAD, AND CRACK INDICATIONS. REPAIRED NR 3 PYLON DRAG ANGLE FASTENER, AND CRACK INDICATIONS IAW REO 02062, REV IR. 2 L 7 4 4F RT 4A25 1996072500053 19960725 00053 WP 1996 7 25 UPS96820653 1 19960709 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP BS 1440-1460 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE: C. INTERCOSTAL, FS 1440-1460 AT L34R IS CORRODED. REMOVED INTERCOSTAL AND J-ANGLE, FABRICATED J-ANGL E PER DAC DWG 5616674 ALODINED AND PRIMED IAW DC8SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996072500054 19960725 00054 WP 1996 7 25 UPS96820654 1 19960713 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 1350 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE: C. LONGERON 34R, FS 1350 IS CRACKED ON SPLICE FITTING. FABRICATED NEW FITTING IAW DAC DWG 3779919-1, INSTALLED FITTING IAW DC8 SRM 51-1-20D. ALODINED AND PRIMED AS REQUIRED IAW DC8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996072500055 19960725 00055 WP 1996 7 25 UPS96820655 1 19960712 A 5753 WEB DOUG DC8 DC873F 302199F WP LT TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE: C. LEFT WING INBOARD END WEB IS CRACKED. REPAIRED LEFT FLAP WEB AT XCW=64.8 IAW TIMCO REO-02088 AND ENGINEERING FILE DC8 57-0697. 2 L 7 4 4F RT 4A25 1996072500056 19960725 00056 WP 1996 7 25 UPS96820656 1 19960716 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 1350-1490 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE: C. L34R, FS 1440-1460, IS CORRODED THROUGH VERTICAL LEG. REMOVED AND REPLACED L34R, FS 1350-1490. 2 L 7 4 4F RT 4A25 1996072500057 19960725 00057 EU 1996 7 25 96ZZZX3639 1 19960218 A 5230 F5202801 LATCH BRACKET AMD FALC20 FALCON 2720302 EU CARGO DOOR CRACKED A DKAA K NONE O OTHER IN INSP/MAINT 1 GL 23 227R 227 TWO CARGO DOOR ROTATING LATCH BRACKETS FOUND CRACKED DURING SSIP DYE-PENETRANT INSPECTION. (AD 92-17-05 REQUIREMENT). 2 L 7 2 4F A7EU 1996072500058 19960725 00058 EU 1996 7 25 96ZZZX3640 1 19960218 A 5230 DOOR FRAME AMD FALC20 FALCON 2720302 EU CARGO DOOR CRACKED A DKAA K NONE O OTHER IN INSP/MAINT 1 GL 23 227R 227 THREE SMALL CRACKS IN CARGO DOOR FRAME NOTES DURING SSIP X-RAY INSPECTION. (AD 92-17-05 REQUIREMENT). 2 L 7 2 4F A7EU 1996072500059 19960725 00059 EU 1996 7 25 96ZZZX3641 1 19960501 A 5230 171605105 DOOR AMD FALC20 FALCON 2720302 EU CARGO COMPT CRACKED A DKAA K NONE O OTHER IN INSP/MAINT 1 GL 23 227R 227 ONE SMALL CRACK NOTED IN CARGO DOOR DURING SSIP X-RAY INSPECTION. (AD 92-17-05 REQUIREMENT) 2 L 7 2 4F A7EU 1996072500060 19960725 00060 EU 1996 7 25 96ZZZX3642 1 19960501 A 5230 DOOR FRAME AMD FALC20 FALCOND 2720304 EU CARGO COMPT CRACKED A DKAA K NONE O OTHER IN INSP/MAINT 1 GL 23 229R 229 ONE SMALL CRACK NOTED IN CARGO DOOR FRAME DURING SSIP X-RAY INSPECTION. (AD 92-17-05 REQUIREMENT). 2 L 7 2 4F A7EU 1996072500061 19960725 00061 EU 1996 7 25 96ZZZX3643 1 19960501 A 5230 F52003 ROTATING LATCH AMD FALC20 FALCOND 2720304 EU CARGO DOOR CRACKED A DKAA K NONE O OTHER IN INSP/MAINT 1 GL 23 229R 229 ONE CARGO DOOR ROTATING LATCH FOUND CRACKED DURING SSIP DYE-PENETRANT INSPECTION. (AD 92-17-05 REQUIREMENT). 2 L 7 2 4F A7EU 1996072500062 19960725 00062 EA 1996 7 25 96ZZZX3644 1 19960516 A 7331 MS3126E1210S CONNECTOR DHAV DHC7 DHC7102 2802708 EA NR 4 FUEL FLOW CORRODED A CICA O OTHER N FALSE WARNING DE DESCENT 1 SO 17 8041D 026 TPA/MIA - FLT 4937 - PILOT REPORTED INDICATOR FOR NR 4 FUEL FLOW WAS FLUCTUATING AND HANGING UP. AIRCRAFT WAS FERRIED F ROM MIA TO FLL AFTER INSPECTION AND MAG STICK CHECKED FOR FUEL QUANTITY. MAINTENANCE REPLACED NR 4 AND NR 5 FUEL TANK P ROBES DUE TO HIGH RESISTANCE READINGS. INSULATION CHECK AT FUEL TANK CHECKED OK, BUT NOT AT COCKPIT INDICATOR. FURTHER TROUBLESHOOTING INDICATED NR 4 FUEL FLOW CANNON PLUG HAD CORROSION AND LOOSE PINS. REPLACED CANNON PLUG AND SYSTEM TES TED OK. CAUSE OF FLUCTUATING DETERMINED TO BE FAULTY CANNON PLUG LOCATED ON TANK NR 4 BEHIND RT LEADING WING EDGE. CHE CKED ALL ASSOCIATED WIRING TO PREVENT RECURRENCE. 2 H 7 4 4T A20EA 1996072500063 19960725 00063 NE 1996 7 25 96ZZZX3645 2 19960325 A 7200 ENGINE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE LEFT SURGED A AMTA O OTHER E VIBRATION/BUFFET CR CRUISE 1 GL 11 516AT 27972 31397 PHX - LEFT ENGINE SURGED DURING DECELERATION AT 38,000 FEET. ENGINE OPERATION ABNORMAL AFTER SURGE, ENGINE WAS NOT SHUT DOWN. EGT 30-50 HIGHER THAN RT ENGINE, VIBES TO 1.8. TROUBLESHOT PER FIM 75-32-00, INSPECTED INLET, EXHAUST, CHIP DET ECTOR ON DEFECTS. ACCOMPLISHED L/P FAN BLADE INSPECTION 75-31-13, NO DEFECTS NOTED. ACCOMPLISHED MAXIMUM TAKEOFF ENGIN E RUN VIBES. 2 L 7 2 4F 4 F RT A2NM E12EU 1996072500064 19960725 00064 NE 1996 7 25 96ZZZX3648 2 19960604 A 7310 3035317 FILTERS EMB 120 EMB120RT SO PWA 118 PW118 NE FUEL SYSTEM CLOGGED A GLBA D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 01 128AM 120109 RDU - FUEL FILTER LIGHT ILLUMINATED ON POWER UP FOR DEPARTURE. REMOVED AND REPLACED FUEL PUMP OUTLET FILTER AND FUEL HE ATER FILTER. AIRCRAFT RETURNED TO SERVICE. REFERENCE: OPERATOR CONTROL NR GLBA96114. 2 L 7 2 4T 4 T RT A31SO E20NE 1996072500065 19960725 00065 EU 1996 7 25 AWXA960269 1 19960611 A 3610 PTB266450 SEAL AIRBUS 320 A320231 3930325 EU LT WING ROOT FAILED A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 628AW 67 LAS - FLT 0146 - ABORTED TAKEOFF. LOW SPEED REJECT FOR AIR LEAK AT LEFT WING. LEAK CHECKED, BLED SYSTEM, AND FOUND BAD SEAL AT SLIP JOINT JUST INBOARD OF WING ROOT. REPLACED SEAL. LEAK CHECK GOOD. (X) 2 L 7 2 4F RT A28NM 1996072500066 19960725 00066 EU 1996 7 25 AWXA960283 1 19960530 A 5347 ASN12223 SEAT TRACK AIRBUS 320 A320231 3930325 EU CABIN CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 620AW 052 PAE - DURING ROUTINE SCHEDULED C-5 MAINTENANCE CHECK, FOUND RT INBOARD SEAT TRACK CORRODED AT AFT FRAME OF R1 DOOR (X807 7, -2540, -Y30). REMOVED, FABRICATED, TREATED, AND INSTALLED PARTS PER SRM 53-00-15. (X) 2 L 7 2 4F RT A28NM 1996072500067 19960725 00067 EU 1996 7 25 AWXA960284 1 19960530 A 5347 SEAT TRACK AIRBUS 320 A320231 3930325 EU CABIN CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 620AW 052 PAE - DURING ROUTINE SCHEDULED C-5 MAINTENANCE CHECK, FOUND RT OUTBOARD SEAT TRACK CORRODED AT AFT FRAME OF R1 DOOR. RE PLACED SEAT TRACK IAW SRM 53-11-14. (X) 2 L 7 2 4F RT A28NM 1996072500068 19960725 00068 EU 1996 7 25 AWXA960285 1 19960601 A 5315 ASNA2247 FLOORBEAM AIRBUS 320 A320231 3930325 EU BS 605 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 620AW 052 PAE - DURING ROUTINE SCHEDULED C-5 MAINTENANCE CHECK, FOUND CORROSION IN NUMEROUS PLACES ON FLOORBOARD SUPPORT BEAM ASSY AT -2540, BS 605 THROUGH BS 709 - YO. REMOVED, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-24-00 AND ER 32-53-12- 07. (X) 2 L 7 2 4F RT A28NM 1996072500069 19960725 00069 NE 1996 7 25 AWXA960289 2 19960624 A 7321 79830015046 EEC AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE NR 1 ENGINE FAILED A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 635AW 11254 2344 25000048 092 PHX/ORD - FLT 0004 - ABORTED TAKEOFF. NR 1 ENGINE DID NOT MAKE TAKEOFF POWER. REPLACED NR 1 ENGINE EEC PER R9373301. O PERATIONS CHECK GOOD. PART TOTAL CYCLES, 5,817. (X) 2 L 7 2 4F 4 F RT A28NM E311NE 1996072500070 19960725 00070 EU 1996 7 25 AWXA960290 1 19960625 A 5230 D5237134000200 DOOR HANDLE AIRBUS 320 A320231 3930325 EU CARGO DOOR OUT OF ADJUST A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 626AW 65 PHX/RNO - AIR TURNBACK. FORWARD CARGO DOOR ECAM MESSAGE INDICATING FORWARD CARGO DOOR OPEN IN-FLIGHT. REMOVED AND REPL ACED FORWARD CARGO DOOR HANDLE PER MM 52-31-21. REWORKED HANDLE PER ENGINEERING REPAIR NR 32-53-30-06. OPERATIONS CHEC K GOOD. (X) 2 L 7 2 4F RT A28NM 1996072500071 19960725 00071 1996 7 25 AWXA960323 4 19960703 A 3441 IRS BOEING 737 7373G7 1384595 NM LEFT MALFUNCTIONED A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 311AW 24712 YVR/PHX - FLT 2278 - AIR TURNBACK. FLIGHT CREW REPORTED LEFT IRS FAILED, GPWS FAILED AND THE NR 6 SLAT INTRANSIT LIGHT ILLUMINATED ON FORWARD AND OVERHEAD. CONTRACT MAINTENANCE REALIGNED IRS'S WITH NO DEFECTS NOTED. GPWS BITE NORMAL. OP ERATED SLATS/FLAPS SEVERAL TIMES WITH NO FAULTY INDICATIONS NOTED. SLATS PHYSICALLY OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1996072500072 19960725 00072 EU 1996 7 25 AWXA960329 1 19960705 A 2700 3945122502 ELAC AIRBUS 320 A320232 3930326 EU NR 1 FAILED A AWXA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CR CRUISE 1 WP 28 639AW 8762 73 1417 471 BOS - FLT 2821 - AIR TURNBACK. ELAC 1 FAILED IN-FLIGHT. RESET NO GOOD. REMOVED AND REPLACED ELAC 1 PER MM 27-93-34. S YSTEM CHECKS GOOD. PART TOTAL CYCLES, 4,501. (X) 2 L 7 2 4F RT A28NM 1996072500073 19960725 00073 NE 1996 7 25 DJSA2396002 2 19960308 A 8530 CYLINDER DOUG DC3 DC3C 3021457 WP PWA R1830 R183094 52020 NE NR 2 ENGINE CRACKED A DJSA A UNSCHED LANDING E VIBRATION/BUFFET NR NOT REPORTED 1 GL 23 8021Z 20444 P144713 RETURNED TO 'TOL' WITH ROUGH RUNNING ENGINE. FOUND NR 1 CYLINDER CRACKED ON NR 2 ENGINE. (X) 2 L 7 2 4R 4 R A669 5E4 1996072500074 19960725 00074 SO 1996 7 25 GLBA96106 1 19960601 A 3231 922AH2YA6P2722A UPLOCK SENSOR EMB 120 EMB120RT SO RT MLG DOORS FAILED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 452UE 120096 LAN - CREW REPORTED GEAR INTRANSIT LIGHTS REMAINED ILLUMINATED AND GEAR DOORS DID NOT RETRACT. THEY MADE AN AIR TURNBAC K AND LANDED UNEVENTFULLY. MAINTENANCE REMOVED AND REPLACED RT MLG UPLOCK SENSOR AND ADJUSTED ALL UPLOCK TARGETS. OPS CHECK WAS GOOD. (X) 2 L 7 2 4T RT A31SO 1996072500075 19960725 00075 EA 1996 7 25 GLBA96108 2 19960605 A 7313 1900008 NOZZLE O-RING BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA LT ENGINE PINCHED A GLBA A E UNSCHED LANDING ENGINE SHUTDOWN K FLUID LOSS CL CLIMB 1 CE 01 60UE UC60 DEC - CREW REPORTED LT ENGINE TORQUE DROPPED WITHOUT POWER LEVER INPUT FOLLOWING TAKEOFF. ENGINE WAS SHUT DOWN AND CREW MADE AIR TURNBACK AND LANDED UNEVENTFULLY. MAINTENANCE REPLACED A PINCHED O-RING ON FUEL NOZZLE. ENGINE RUN AND POWER CHECKS WERE GOOD. (X) 2 L 7 2 4T 4 T RT A24CE E4EA 1996072500076 19960725 00076 EA 1996 7 25 GLBA96109 2 19960605 A 7530 131823E4 EVA TUBING BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA RT ENGINE MELTED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 166GL UC166 RDU - CREW REPORTED A RIGHT BLEED AIR FAIL AFTER TAKEOFF. THEY MADE AN AIR TURNBACK AND LANDED UNEVENTFULLY. MAINTENAN CE REPAIRED BLEED LEAK IN EVA TUBING. OPS CHECK WAS GOOD. (X) 2 L 7 2 4T 4 T RT A24CE E4EA 1996072500077 19960725 00077 CE 1996 7 25 GLBA96110 1 19960601 A 3246 11480013 NOSE WHEEL BEECH 1900 1900C 1154161 CE NLG UNBALANCED A GLBA O OTHER E VIBRATION/BUFFET TO TAKEOFF 1 CE 01 168GL 5442 UC168 RDU - STRONG VIBRATION ON TAKEOFF ROLL, AFTER ROTATION, AND UP TO 12,000 FEET. FOUND BALANCE WEIGHTS HAD FALLEN OFF OF NOSE TIRE ASSY. REMOVED AND REPLACED NOSE WHEEL ASSY. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1996072500078 19960725 00078 CE 1996 7 25 GLBA96111 1 19960603 A 3233 1143800419 ACTUATOR BEECH 1900 1900C 1154161 CE MLG FAILED A GLBA O OTHER J WARNING INDICATION AP APPROACH 1 CE 01 122GL 0450 UC122 ORD - LEFT MLG SLOW TO INDICATE DOWN AND LOCKED. REMOVED AND REPLACED LEFT MLG ACTUATOR. OPS CHECKS GOOD. (X) 2 L 7 2 4T RT A24CE 1996072500079 19960725 00079 CE 1996 7 25 GLBA96112 1 19960603 A 3150 WARNING SWITCH BEECH 1900 1900C 1154161 CE PEDESTAL LOOSE SCREWS A GLBA O OTHER N FALSE WARNING AP APPROACH 1 CE 01 89UE UC89 MSP - GEAR WARNING HORN COMES BACK 'ON' AFTER BEING SILENCED ON APPROACH. SECURED BOTH SCREWS HOLDING WIRE ENDS TO LEFT WARNING SWITCH IN PEDESTAL. OPS CHECKS GOOD. (X) 2 L 7 2 4T RT A24CE 1996072500080 19960725 00080 SO 1996 7 25 GLBA96113 1 19960604 A 2752 3203001007 FLAP ACTUATOR EMB 120 EMB120RT SO RT TE FLAP FAILED A GLBA O OTHER O OTHER AP APPROACH 1 CE 01 128AM 0919 120109 RDU - FLAP DISAGREEMENT, OUTBOARD FLAPS HANG AT ABOUT 10 DEGREES WHEN SELECTED FROM 15 DEGREES TO ZERO DEGREES. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR, OPS CHECKS GOOD. (X) 2 L 7 2 4T RT A31SO 1996072500081 19960725 00081 NE 1996 7 25 GLBA96114 2 19960604 A 7310 5905587 FILTERS EMB 120 EMB120RT SO PWA 118 PW118 NE FUEL SYSTEM CLOGGED A GLBA D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 01 128AM 120109 RDU - FUEL FILTER LIGHT ILLUMINATED ON POWER UP FOR DEPARTURE. REMOVED ADN REPLACED FUEL PUMP OUTLET FILTER AND FUEL HE ATER FILTER. AIRCRAFT RETURNED TO SERVICE. REFERENCE: OPERATOR CONTROL NR 96ZZZX3648. (X) 2 L 7 2 4T 4 T RT A31SO E20NE 1996072500082 19960725 00082 CE 1996 7 25 GLBA96115 1 19960607 A 6120 189894001 SOLENOID BEECH 1900 1900C 1154161 CE RT ENGINE WIRING DAMAGED A GLBA O OTHER O OTHER LD LANDING 1 CE 01 84GL UC84 ORD - CREW REPORTED THE AIRCRAFT PULLS TO THE RIGHT DURING FLARE. MAINTENANCE REPAIRED DAMAGED WIRING AT THE RIGHT LOW PITCH SOLENOID. OPS CHECK WAS GOOD. (X) 2 L 7 2 4T RT A24CE 1996072500083 19960725 00083 CE 1996 7 25 GLBA96116 1 19960610 A 3230 44EN496 SQUAT SWITCH BEECH 1900 1900C 1154161 CE RT MLG LACK OF LUBE A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 96UE UC96 ORD - GEAR WOULD NOT RETRACT. LUBED RIGHT SQUAT SWITCH. PERFORMED TEST FLIGHT WITH NORMAL GEAR RETRACTION. AIRCRAFT R ETURNED TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1996072500084 19960725 00084 CE 1996 7 25 GLBA96117 1 19960615 A 3250 NOSE WHEEL BEECH 1900 1900C 1154161 CE NLG NOT CENTERED A GLBA O OTHER O OTHER LD LANDING 1 CE 01 98GL UC98 SPW - UPON LANDING, NOSE WHEEL IS NOT CENTERED. VEERS TO THE RIGHT ON TOUCHDOWN. ADJUSTED LEFT ENGINE DEAD BAND. OPS CHECK GOOD. (X) 2 L 7 2 4T RT A24CE 1996072500085 19960725 00085 SO 1996 7 25 GLBA96118 1 19960615 A 3230 CONNECTOR EMB 120 EMB120RT SO LANDING GEAR LOOSE PIN A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 451UE 120108 ORD - GEAR HANDLE LOCK WOULD NOT RELEASE AFTER TAKEOFF FROM ORD. COULD NOT RAISE GEAR. FOUND CANNON PLUG ON LANDING GE AR RELAY BOX HAD A LOOSE PIN. SECURED PIN AND RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1996072500086 19960725 00086 SO 1996 7 25 GLBA96119 1 19960606 A 3230 UPLOCK ACTUATOR EMB 120 EMB120ER 3260203 SO LT MLG MALFUNCTIONED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 292UX 120292 SPW - LEFT MAIN A AND B SYSTEMS RED LIGHTS REMAINED ILLUMINATED AFTER RETRACTION. CREW MADE AN AIR TURNBACK AND LANDED UNEVENTFULLY. MAINTENANCE SWAPPED MLG UPLOCK ACTUATORS. TEST FLIGHT SATISFACTORY. (X) 2 L 7 2 4T RT A31SO 1996072500087 19960725 00087 EU 1996 7 25 SIMA961651 1 19960613 A 3350 330151 BATTERY PACK SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 373AE 1071 340B373 DFW - FLT 3891 - FORWARD SECTION OF EMERGENCY LIGHTS WOULD NOT ILLUMINATE. BATTERY PACK FOR EMERGENCY LIGHTS WOULD NOT TAKE CHARGE. REPLACED BATTERY PACK AT STA 21LN, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1996072500088 19960725 00088 EU 1996 7 25 SIMA961661 1 19960614 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 EU CABIN FAILED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 4AE 574 244 ORD - FL 4339 - FORWARD EMERGENCY EXIT LIGHT IN CABIN REMAINS ON WITH THE SWITCH OFF/RESET. REPLACED EMERGENCY POWER SU PPLY 43WL. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1996072500089 19960725 00089 GL 1996 7 25 9615501211 2 19960717 A 7230 COMPRESSOR DOUG DC10 DC1030 3023501 WP GE CF6 CF650C 30018 GL NR 1 ENGINE STALLED A NWAA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 01 211NW 46868 55130 AFTER TAKEOFF AND DURING CLIMB, THE NR 1 ENGINE EXPERIENCED COMPRESSOR STALL AT 6,000 FEET. CREW FOLLOWED COCKPIT OPERA TING PROCEDURE, SHUT DOWN THE ENGINE, DUMPED 12,000 LBS OF FUEL AND RETURNED TO SEA WITHOUT FURTHER INCIDENT. MAINTENAN CE INSPECTION OF THE ENGINE REVEALED METAL IN TAILPIPE. THE ENGINE WAS REPLACED. 2 L 7 3 4F 4 F A22WE A23EA 1996072500090 19960725 00090 NM 1996 7 25 9615512705 1 19960717 A 2781 POSITION SWITCH BOEING 727 727225 1384077 NM NR 4 LE FLAP FAILED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 802EA 22433 DURING CLIMB ON FLAP/SLAT RETRACTION, THE NR 4 LEADING EDGE SLAT STILL INDICATED IN TRANSIT. AIRCRAFT RETURNED TO MSP A ND LANDED WITHOUT INCIDENT. REPLACED NR 4 LEADING EDGE FLAP/SLAT POSITION SWITCH AND FLAP/SLAT ANNUNCIATOR INDICATION P ANEL, SYSTEM CHECKED OK. 2 L 7 3 4F A3WE 1996072500091 19960725 00091 WP 1996 7 25 9615529956 1 19960717 A 3232 ACTUATOR DOUG DC9 DC931 3022065 WP RT NLG DOOR MALFUNCTIONED A NWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 01 923RW 47183 AFTER TAKEOFF, EXCESSIVE VIBRATION WAS COMING FROM NOSE GEAR AREA AFTER GEAR RETRACTION. RECYCLED GEAR WITH SAME RESULT S. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND RIGHT NOSE GEAR DOOR OPEN. REPLACED THE RIGH T NOSE GEAR DOOR ACTUATOR, OPERATIONAL CHECK NORMAL ON GEAR CYCLE. 2 L 7 2 4F A6WE 1996072500092 19960725 00092 WP 1996 7 25 9615539968 1 19960717 A 3320 LIGHT BALLAST DOUG DC9 DC931 3022065 WP CABIN FAILED A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 01 9332 47264 FLIGHT ATTENDANT REPORTED ELECTRICAL BURNING SMELL IN AFT CABN. FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT INCI DENT. MAINTENANCE FOUND BALLAST FOR SIDEWALL LIGHTS AT ROW 16 RIGHT SIDE. DEFERRED LIGHTING PER MEL 33-2 AWAITING PART S FOR REPLACEMENT OF BALLAST. 2 L 7 2 4F A6WE 1996072500093 19960725 00093 WP 1996 7 25 9615549922 1 19960715 A 3320 LIGHT BALLAST DOUG DC9 DC932 3022066 WP CABIN FAILED A NWAA K NONE A FLAME/FIRE IN INSP/MAINT 1 GL 01 945N 47664 DURING LINE MAINTENANCE INSPECTION, FOUND EVIDENCE OF FIRE AT ROW 21DEF AT LOWER SIDEWALL LIGHT AFT BALLAST. DEFERRED L IGHT PER MEL 33-2, AWAITING PARTS FOR REPLACEMENT OF BALLAST ASSEMBLY. 2 L 7 2 4F A6WE 1996072500094 19960725 00094 WP 1996 7 25 9615559925 1 19960715 A 3241 SWITCH DOUG DC9 DC932 3022066 WP LT ANTI-SKID MALFUNCTIONED A NWAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 01 925US 47472 LEFT INBOARD ANTI-SKID LIGHT ILLUMINATED DURING TAKEOFF ROLL. ABORTED TAKEOFF AT 60 KNOTS. PILOT RECYCLED ANTI-SKID SW ITCH, SECOND TAKEOFF ATTEMPT WAS SUCCESSFUL. FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. 2 L 7 2 4F A6WE 1996072500095 19960725 00095 WP 1996 7 25 9615569601 1 19960716 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 601NW 47038 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES AND BULBS, O PERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996072500096 19960725 00096 WP 1996 7 25 9615579998 1 19960715 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8934E 47143 DURING LINE MAINTENANCE INSPECTION, FOUND BOTH AFT OVERWING EMERGENCY EXIT SIGN LIGHTS INOPERATIVE. REPLACED BATTERIES IN BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996072500097 19960725 00097 1996 7 25 9615589941 4 19960715 A 2565 13621228 EVAC SLIDE DOUG DC9 DC932 3022066 WP TAILCONE LOW PRESSURE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3324L 47103 DURING PERIODIC CHECK, FOUND TAILCONE EVACUATION SLIDE PRESSURE LOW. REPLACED SLIDE. 2 L 7 2 4F A6WE 1996072500098 19960725 00098 WP 1996 7 25 9615599976 1 19960715 A 3350 60030451 POWER SUPPLY DOUG DC9 DC931 3022065 WP RT NACELLE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9340 47389 DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY AND BATTERIE S, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996072500099 19960725 00099 1996 7 25 9615609941 4 19960715 A 2565 113317 EVAC SLIDE DOUG DC9 DC932 3022066 WP PAX DOOR LOW PRESSURE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3324L 60445 3696 47103 DURING PERIODIC CHECK, FOUND MAIN CABIN DOOR EVACUATION SLIDE LOW ON PRESSURE. REPLACED SLIDE. 2 L 7 2 4F A6WE 1996072500100 19960725 00100 WP 1996 7 25 9615619931 1 19960715 A 3350 60030451 BATTERY PACK DOUG DC9 DC931 3022065 WP RT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 90S 47244 DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996072500101 19960725 00101 WP 1996 7 25 CALA9601038 1 19960717 A 2540 RAZOR OUTLET DOUG DC9 DC932 3022066 WP LT LAV INOPERATIVE A CALA H DEACTIVATE SYST/CIRCUITS B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 09 33506 47765 SMOKE WAS OBSERVED COMING FROM AREA OF FLUORESCENT LIGHT IN LT LAV AND THE SMOKE DETECTOR WAS SOUNDING WHILE EN ROUTE. L AV CIRCUITS WERE DEACTIVATED AND THE SMOKE CEASED. THE AIRCRAFT LANDED IN OMA WITHOUT INCIDENT. MAINTENANCE FOUND THE LT LAV RAZOR OUTLET CIRCUIT BREAKER POPPED. THE CIRCUIT BREAKER WAS RESET, BUT POPPED AGAIN WHEN OUTLET WAS USED. THE RAZOR OUTLET WAS PLACARDED INOPERATIVE AND THE CIRCUIT BREAKER WAS COLLARED. IN ADDITION, THE LAV LIGHTS AND FLUSH MOTO R WERE CHECKED WITH NO DISCREPANCIES NOTED. 2 L 7 2 4F A6WE 1996072500102 19960725 00102 NM 1996 7 25 CALA9601039 1 19960718 A 3310 SOCKET BOEING 727 727232 1384082 NM GLARESHIELD SHORTED A CALA A J UNSCHED LANDING DUMP FUEL B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TO TAKEOFF 1 SW 09 45793 20647 A SMALL AMOUNT OF SMOKE WAS OBSERVED COMING FROM UNDER GLARESHIELD, ACCOMPANIED BY ILLUMINATION OF SEVERAL WARNING LIGHT S AFTER GEAR WAS RAISED. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTE NANCE FOUND THE NR 2 THRUST REVERSER OPERATING LIGHT SOCKET AT FAULT. THE LIGHT SOCKET WAS REPLACED AND OPERATIONAL CHE CK WAS GOOD. 2 L 7 3 4F A3WE 1996072500103 19960725 00103 WP 1996 7 25 CALA9601040 1 19960718 A 3230 59516395001 BUNGEE CYL DOUG DC9 DC982 3022082 WP NLG INOPERATIVE A CALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 09 92874 23122 23122 49122 THE NLG LIGHT INDICATED UNSAFE DURING APPROACH. THE GEAR WAS CYCLED AND INDICATIONS WERE GOOD. THE AIRCRAFT LANDED WIT HOUT INCIDENT. MAINTENANCE FOUND THE NLG BUNGEE CYLINDER AT FAULT. THE NLG BUNGEE CYLINDER WAS REPLACED. THE GEAR WAS RETRACTED SEVERAL TIMES AND OPERATION CHECKED GOOD. 2 L 7 2 4F A6WE 1996072500104 19960725 00104 NE 1996 7 25 DL73E961719 2 19960717 A 7260 GEARBOX BOEING 737 737247 138448D NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE FAILED A DALA E ENGINE SHUTDOWN Y ENGINE STOPPAGE CR CRUISE 1 SO 27 377DL 23604 709223 NR 2 ENGINE LOSS OIL PRESSURE, NR 2 ENGINE SHUTDOWN. REPLACED ENGINE GEARBOX. 2 L 7 2 4F 4 F A16WE E2EA 1996072500105 19960725 00105 NM 1996 7 25 DL73E961724 1 19960709 A 5312 BULKHEAD WEB BOEING 737 737247 138448D NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 236WA 23184 THREE CRACKS WERE DISCOVERED ON THE FWD FACE OF THE FS 178 BULKHEAD WEB. THE FIRST CRACK IS LOCATED NEAR THE RBL 5.7 VE RTICAL STRAP AT APPROX WL 198. THE SECOND IS LOCATED NEAR THE RBL 5.7 VERTICAL STRAP AT WL 200. THE THIRD IS LOCATED N EAR LBL 5.7 AT APPROX WL 198. THE DAMAGE WAS REPAIRED WITH A DOUBLER APPROVED BY FAA/DER FORM 8110-3, DER DESIGNATION S O-867, DTD 7-9-96. 2 L 7 2 4F A16WE 1996072500106 19960725 00106 1996 7 25 DL76L961673 4 19960710 A 3460 4058650930 CDU BOEING 767 767332 1382001 NM LT COCKPIT FAILED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 173DN 24800 LEFT CDU FAILED 1 HR AFTER T/O. PULLED C/B AND LEFT OUT FOR 20 MINS, RESET AND CDU DID NOT WORK. RETURNED TO JFK. REP LACED LEFT CDU, OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 1996072500107 19960725 00107 NM 1996 7 25 DL76S961661 1 19960709 A 3350 POWER SUPPLY BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 128DL 24078 LEFT AFT CABIN EMERGENCY AISLE LIGHTS DO NOT ILLUMINATE. REPLACED PWR SUPPLY M739, OPN NOW NORMAL. 2 L 7 2 4F RT A1NM 1996072500108 19960725 00108 NM 1996 7 25 DL76S961699 1 19960716 A 2530 COFFEE MAKER BOEING 767 767332 1382001 NM MID GALLEY FAILED A DALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 27 139DL 25984 TEN MINUTES AFTER FLIGHT ATTENDANT REPORTED ELECTRICAL SMOKE SMELL IN RIGHT GALLEY, BOTH MID AND AFT CABIN LAV SMOKE DET ECTORS ACTIVATED IN FLT. NO DETECTABLE SMOKE OR FIRE, TURNED UTILITY BUSES OFF FOR REMAINDER OF FLT. REPLACED INBD CO FFEE MAKER MID GALLEY DUE TO BURNT ELECTRICAL ODOR FROM COFFEE MAKER. IN ADDITION, INSPECTED A/C CEILING AREA RAN REC F ANS, CHECKED ALL VCR'S, OPENED AND INSPECTED ALL MID GALLEY ELECT PANELS AND ALL OK. 2 L 7 2 4F RT A1NM 1996072500109 19960725 00109 NM 1996 7 25 DLM88961656 1 19960709 A 3350 081691 LIGHT DOUG MD88 MD88 3023688 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 911DL 49542 EMERGENCY FLOOR TRACK BULB FWD OF 31D INOP. REPLACED LIGHT FIXTURE, CKS OK. 2 L 7 2 4F RT A6WE 1996072500110 19960725 00110 NM 1996 7 25 DLM88961676 1 19960711 A 3350 LIGHT DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 910DL 49541 FIRST CLASS EMERGENCY AISLE LIGHTS INOP. REPLACED BATTERIES, CHECKS NORMAL. 2 L 7 2 4F RT A6WE 1996072500111 19960725 00111 NM 1996 7 25 P5CA9600367 1 19960718 A 7110 CHANNEL BOEING 747 747122 1384872 NM NR 2 ENG COWL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NR 2 ENGINE INBOARD CORE COWL INNER CHANNEL AFT SECTION IS CRACKED. FABRICATED PARTS AND REPAIRED IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996072500112 19960725 00112 NM 1996 7 25 P5CA9600368 1 19960718 A 7110 CORE COWL BOEING 747 747122 1384872 NM NR 3 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NR 3 ENGINE INBOARD CORE COWL IS CRACKED AT AFT UPPER CORNER. STOP DRILLED CRACK, FABRICATED DOUBLERS AND REPAIRED IAW SRM 54-10-03. 2 L 7 4 4F A20WE 1996072500113 19960725 00113 NE 1996 7 25 P5CA9600369 2 19960718 A 7250 R-RAIL BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 4 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 662736 NR 4 ENGINE R-RAIL IS CRACKED CIRCUMFERENTIALLY, LIGHTENING HOLE TO LIGHTENING HOLE AT THE 5:30 POSITION. WELDED AND ST RESS RELIEVED IAW PRATT AND WHITNEY MM 72-53-01. 2 L 7 4 4F 4 F A20WE E20EA 1996072500114 19960725 00114 NE 1996 7 25 P5CA9600370 2 19960717 A 7250 S-RAIL BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 4 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 662376 NR 4 ENGINE S-RAIL HAS A RADIAL CRACKED AT 1:30 POSITION. WELDED AND STRESS RELIEVED IAW PRATT AND WHITNEY MM 72-53-01. 2 L 7 4 4F 4 F A20WE E20EA 1996072500115 19960725 00115 NE 1996 7 25 P5CA9600371 2 19960717 A 7250 S-RAIL BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 2 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 663048 NR 2 ENGINE S-RAIL HAS A RADIAL CRACK AT THE 2 O'CLOCK POSITION. WELDED AND STRESS RELIEVED IAW PRATT AND WHITNEY MM 72 -53-01. 2 L 7 4 4F 4 F A20WE E20EA 1996072500116 19960725 00116 NM 1996 7 25 P5CA9600372 1 19960717 A 7110 SUPPORT PLATE BOEING 747 747122 1384872 NM NR 2 ENG COWL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NR 2 ENGINE OUTBOARD CORE COWL, LOWER FORWARD CORNER SUPPORT PLATE IS CRACKED IN THE LIGHTENING HOLE. WELDED BRACKET AN D REINSTALLED IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996072500117 19960725 00117 NM 1996 7 25 P5CA9600373 1 19960717 A 7160 AIR DUCT BOEING 747 747122 1384872 NM NR 2 ENG COWL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NR 2 ENGINE INBOARD CORE COWL LOWER FORWARD AIR DUCT IS CRACKED. WELDED AND REINSTALLED IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996072500118 19960725 00118 NM 1996 7 25 P5CA9600374 1 19960717 A 5753 LE FAIRING BOEING 747 747122 1384872 NM LT/RT TE FLAPS DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 ALL EIGHT FLAP TRACK FIXED L/E FAIRINGS HAVE HEAVY EROSION AT FORWARD END WITH SEVERAL AREAS DELAMINATED AND CRACKED. R EPAIRED DELAMINATION WITH FIBERGLASS OVERLAYS AND REPAIRED EROSION IAW SRM 51-40-09 AND 51-40-11. 2 L 7 4 4F A20WE 1996072500119 19960725 00119 NM 1996 7 25 P5CA9600375 1 19960716 A 5280 DOOR BOEING 747 747122 1384872 NM RT MLG GEAR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 RIGHTHAND OUTBOARD BODY GEAR DOOR HAS LARGE AREA OF BARE METAL WITH SURFACE CORROSION. REMOVED LEVEL ONE CORROSION, TRE ATED IAW SRM 51-24-11, 51-10-01. 2 L 7 4 4F A20WE 1996072500120 19960725 00120 NM 1996 7 25 P5CA9600376 1 19960717 A 5415 MOUNT BRACKET BOEING 747 747122 1384872 NM NR 3 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NR 3 ENGINE CLAMP MOUNTING BRACKET IS CRACKED FOUR INCHES FORWARD OF R-RAIL AT 6 O'CLOCK POSITION. FABRICATED NEW BRACK ET AND INSTALLED IAW MM 70-50-00. 2 L 7 4 4F A20WE 1996072500121 19960725 00121 NM 1996 7 25 P5CA9600377 1 19960716 A 7830 TR SLEEVE BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 4 ENGINE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 662736 NR 4 ENGINE HAS SURFACE CORROSION ON THRUST REVERSER SLEEVE AT RT UPPER JACKSCREW BARREL NUT HOLES. REMOVED LEVEL ONE C ORROSION AND TREATED IAW SRM 51-10-01. 2 L 7 4 4F 4 F A20WE E20EA 1996072500122 19960725 00122 NE 1996 7 25 P5CA9600378 2 19960718 A 7230 TIP SHROUD BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 3 ENGINE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 685904 NR 3 ENGINE INLET FAN BLADE TIP SHROUD DELAMINATED AT 5:30 POSITION. REPAIRED DELAMINATION AND APPLIED ADHESIVE IAW SRM 72-33-01. 2 L 7 4 4F 4 F A20WE E20EA 1996072500123 19960725 00123 NM 1996 7 25 P5CA9600379 1 19960716 A 5400 BRACKET BOEING 747 747122 1384872 NM NR 3 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NR 2 ENGINE AIR DUCT MOUNT ANGLE BRACKET IS CRACKED AT THE 6 O'CLOCK POSITION FORWARD OF MAIN GEARBOX. FABRICATED ANGLE AND INSTALLED IAW SRM 51-10-01. 2 L 7 4 4F A20WE 1996072500124 19960725 00124 NM 1996 7 25 P5CA9600380 1 19960717 A 5720 FALSE SPAR BOEING 747 747122 1384872 NM RT WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 RT FALSE SPAR FORWARD SIDE FROM WING GEAR TRUNNION ATTACH I/B TO END HAS BARE METAL WITH MINOR SURFACE CORROSION. REMOV ED LEVEL ONE CORROSION, TREATED IAW SRM 51-10-02. 2 L 7 4 4F A20WE 1996072500125 19960725 00125 NM 1996 7 25 P5CA9600381 1 19960715 A 5320 PRESS DECK BOEING 747 747122 1384872 NM NLG WW CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NOSE WHEEL WELL UPPER PRESSURE DECK HAS NUMEROUS SPOTS OF BARE METAL WITH MINOR SURFACE CORROSION. REMOVED LEVEL ONE CO RROSION, TREATED IAW SRM 51-10-02. 2 L 7 4 4F A20WE 1996072500126 19960725 00126 NE 1996 7 25 96ZZZX3649 2 19960704 A 7260 AS3209158 SEAL DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3B 52039 NE NR 4 ENG GEARBOX DEFECTIVE A RIAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 19 772CA 46131 669446 ON RIA FLT 1712 (CDG/MIA) - DURING CRUISE AT APPROXIMATELY 1830Z, NR 4 ENGINE WAS SHUT DOWN DUE TO OIL PRESSURE LIGHT ON , ENGINE OIL PRESSURE FLUCTUATING AND DECREASING BELOW 35 PSI. AT MIA ON GROUND, MAINTENANCE FOUND LEAKING GEARBOX TOWE R SHAFT SEAL. SEAL WAS REPLACED, AIRCRAFT WAS RUN-UP, LEAK CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 4 4F 4 F 4A25 1E8 1996072500127 19960725 00127 NM 1996 7 25 96ZZZX3650 1 19960612 A 2130 40007B46E STATIC FITTING BOEING 727 727231 1384079 NM NR 1 CONTROLLER LOOSE A MYWA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 808MA 21988 IAH - RETURN FROM FLIGHT - UPON CLIMB-OUT, FOUND CABIN PRESSURIZATION UNCONTROLLABLE IN AUTO AND STANDBY. SWITCHED MANU AL DC. CABIN RATE NOT CONTROLLABLE. SHUT OFF ONE PACK. CABIN STARTED TO RISE UNCONTROLLABLE. CLOSED CARGO HEAT OUTFL OW VALVE. CABIN STARTED TO DESCEND ON DESCENT. ON POST-FLIGHT INSPECTION, FOUND STATIC FITTING ON CABIN PRESSURE CONTR OLLER TO BE LOOSE. TIGHTENED. OPS CHECK IAW MM 21-30-00 NORMAL. (X) 2 L 7 3 4F A3WE 1996072500128 19960725 00128 EU 1996 7 25 96ZZZX3651 1 19960704 A 3350 3011151 POWER SUPPLY AEROSP ATR42 ATR42300 8680920 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 223AT 298 223 DFW - FLT 3623 - EMERGENCY LIGHTS AT PASSENGER ENTRANCE AND 12 WL INOPERATIVE. REPLACED BATTERY POWER SUPPLY AT 30 WL A ND 18 WL. AIRCRAFT WAS RETURNED TO SERVICE. REFERENCE: OPERATOR CONTROL SIMA961861, AND CONTROL NR 96ZZZX3652. 2 H 7 2 4T RT A53EU 1996072500129 19960725 00129 EU 1996 7 25 96ZZZX3652 1 19960704 A 3350 3011180A POWER SUPPLY AEROSP ATR42 ATR42300 8680920 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 223AT 3323 223 DFW - FLT 3623 - EMERGENCY LIGHTS AT PASSENGER ENTRANCE AND 12 WL INOPERATIVE. REPLACED BATTERY POWER SUPPLY AT 30 WL A ND 18 WL. AIRCRAFT WAS RETURNED TO SERVICE. REFERENCE: OPERATOR CONTROL NR SIMA961861, AND CONTROL NR 96ZZZX3651. (X ) 2 H 7 2 4T RT A53EU 1996072500130 19960725 00130 WP 1996 7 25 96ZZZX3653 1 19960503 A 3260 CONNECTOR DOUG DC9 DC931 3022065 WP LANDING GEAR LOOSE A VJ6A O OTHER P NO WARNING INDICATION AP APPROACH 1 SO 11 931ML 47202 ATL/MCO - FLT 505 - WITH GEAR EXTENDED NO GREEN LIGHT INDICATION, RECYCLED GEAR AND LIGHT CAME ON DURING APPROACH. FOUN D MICROSWITCH CONNECTOR HALF WAY OUT, RECONNECTED AND CLEANED CANNON PLUG PER MM 32-60-1. REMOVED SWITCH AND MANUALLY P ERFORMED SATISFACTORY OPS CHECK. 2 L 7 2 4F A6WE 1996072500131 19960725 00131 NM 1996 7 25 AALA960962 1 19960625 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 480-500 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 703AA 22461 TUL - CORROSION ON STR 28L JUST AFT OF STA 480. REPAIRED PER SRM 53-10-3, FIGURE 1, PAGE 4. TST: 42,362 HOURS. CYC LES, 22,280. (X) 2 L 7 3 4F A3WE 1996072500132 19960725 00132 NM 1996 7 25 AALA960964 1 19960625 A 5330 SKIN BOEING 727 727223 1384074 NM BS 214 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 703AA 22461 TUL - UPPER POST BETWEEN CAPTAIN'S SLIDING WINDOW AND WINDSHIELD IS CRACKED (VERIFIED BY DYE PENETRANT CHECK) EXTERNAL S KIN. STOPPED DRILLED CRACK. HFEC SHOWS NO CRACKING PAST STOP DRILL HOLE. DRILLED HOLES IN DOUBLER AND INSTALLED DOUBL ER IAW SRM 53-30-3, FIGURE 8. TST: 42,352 HOURS. CYCLES, 22,280. (X) 2 L 7 3 4F A3WE 1996072500133 19960725 00133 NM 1996 7 25 AALA960965 1 19960625 A 5330 SKIN BOEING 727 727223 1384074 NM BS 480-500 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 703AA 22461 TUL - CORROSION ON FUSELAGE SKIN BELOW STR 28L, ST 480 - STA 500. REPAIRED PER SRM 53-30-3, FIGURE 3A, PAGE 14. TST: 4 2,362 HOURS. CYCLES, 22,280. (X) 2 L 7 3 4F A3WE 1996072500134 19960725 00134 NM 1996 7 25 AALA960980 1 19960629 A 5730 SKIN BOEING 727 727227 1384078 NM WS 825 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - LOWER WING SKIN CORRODED ABOVE LEFT PRIMARY HEAT EXCHANGE. REMOVED CORROSION, INSTALLED DOUBLER AND TRIPLER PER S RM 57-30-3, PAGE 25. TST: 64,997 HOURS. CYCLES, 44,491. (X) 2 L 7 3 4F A3WE 1996072500135 19960725 00135 NM 1996 7 25 AALA960981 1 19960629 A 5711 SPAR BOEING 727 727227 1384078 NM FSS 198 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - CORRODED AND BULGED AROUND RIVETS. REMOVED CORROSION AND INSTALLED DOUBLER PER ESO 11697. REF: E-58 NR 1771442, DATED 6-17-56. TST: 64,997 HOURS. CYCLES, 44,491. (X) 2 L 7 3 4F A3WE 1996072500136 19960725 00136 NM 1996 7 25 AALA960982 1 19960629 A 5720 ANGLE BOEING 727 727227 1384078 NM FSS 190 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - ANGLE, LOWER CORD ANGLE, BADLY CORRODED AROUND RIVETS BELOW LEFT EDGE FUEL TANK PLATE. REMOVED CORROSION AND INST ALLED DOUBLER PER ESO 11697. REF: E-58 NR 1771441, DATED 6-17-96. TST: 64,997 HOURS. CYCLES, 44,491. (X) 2 L 7 3 4F A3WE 1996072500137 19960725 00137 NM 1996 7 25 AALA960983 1 19960629 A 5330 SKIN BOEING 727 727227 1384078 NM BS 416 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - DENT AT STA 416, STR 24L, IN FUSELAGE SKIN. CUT OUT DAMAGED AREA, INSTALLED DOUBLER PER SRM 53-30-3, FIGURE 3. T ST: 64,997 HOURS. CYCLES, 44,491. (X) 2 L 7 3 4F A3WE 1996072500138 19960725 00138 NM 1996 7 25 AALA960984 1 19960629 A 5511 SPAR BOEING 727 727227 1384078 NM LT HORIZ STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - LEFT STABILIZER REAR SPAR CORD HAS CORROSION TOP SIDE OF LEFT STABILIZER AT REAR SPAR CORD INBOARD END. CUT OUT D AMAGED AREA AND INSTALLED DOUBLERS PER ESO 11697, DATED 6-17-96. TST: 64,997 HOURS. CYCLES, 44,491. (X) 2 L 7 3 4F A3WE 1996072500139 19960725 00139 NM 1996 7 25 AALA960985 1 19960629 A 5711 SPAR BOEING 727 727227 1384078 NM RT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - CORROSION LOWER LEADING EDGE WING PANELS OUTBOARD NR 8 SLAT ACTUATOR. REMOVED CORROSION, NDT CHECK, INSTALL DOUBL ER STRAP PER SRM 57-30-00, FIGURE NR 2. TST: 64,997 HOURS. CYCLES, 44,491. (X) 2 L 7 3 4F A3WE 1996072500140 19960725 00140 NM 1996 7 25 AALA960986 1 19960629 A 5311 BELT FRAME BOEING 727 727227 1384078 NM BS 344 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - CORROSION ON BELL FRAME AND ANGLE AT STA 344 AT STR 25R. CUT OUT CORRODED SECTION AND INSTALLED DOUBLERS PER SRM 51-40-3, PAGES 1-6. TST: 64,997 HOURS. CYCLES, 44,491. (X) 2 L 7 3 4F A3WE 1996072500141 19960725 00141 NM 1996 7 25 AALA960987 1 19960629 A 5510 BEAM BOEING 727 727227 1384078 NM HORIZ STAB TE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - LEFT HORIZONTAL STABLIZER TRAILING EDGE BEAM CORRODED INBOARD OF NR 4 ELEVATOR HINGE BEARING. REMOVED CORROSION, REPAIRED PER SRM ESO 11697, DATED 6-20-96. TST: 64,997 HOURS. CYCLES, 44,491. (X) 2 L 7 3 4F A3WE 1996072500142 19960725 00142 NM 1996 7 25 AALA960988 1 19960629 A 5330 SKIN BOEING 727 727227 1384078 NM BS 1342 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - CRACK IN SKIN, LEFT SIDE OF VERTICAL STABILIZER (JUST ABOVE FUSELAGE MATE POINT), STA 1342. STOP DRILLED CRACK AN D INSTALLED DOUBLER PER SB 727-55-82. TST: 64,997 HOURS. CYCLES, 44,491. (X) 2 L 7 3 4F A3WE 1996072500143 19960725 00143 NM 1996 7 25 AALA960989 1 19960629 A 5330 SKIN BOEING 727 727227 1384078 NM BS 415 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - BEAR STRAP CRACKED LOWER AFT CORNER FORWARD GALLEY DOOR. STOP DRILLLED CRACK AND INSTALLED REPAIR AT LOWER AFT CO RNER PER BSB 727-53-0188. TST: 64,997 HOURS. CYCLES, 44,491. (X) 2 L 7 3 4F A3WE 1996072500144 19960725 00144 NM 1996 7 25 AALA960990 1 19960629 A 5330 SKIN BOEING 727 727227 1384078 NM BS 1030 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - CRACK AT RIVET HEAD. FOUND CORROSION UPON SKIN REPAIR. CUT OUT CORRODED SKIN, REPAIRED PER ESO 11697 DATED 6-21- 96. INSTALLED TRIPLE DOUBLER. TST: 64,997 HOURS. CYCLES, 44,491. (X) 2 L 7 3 4F A3WE 1996072500145 19960725 00145 NM 1996 7 25 AALA960991 1 19960629 A 5720 ANGLE BOEING 727 727227 1384078 NM WS 196 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - CORROSION ON FRONT SPAR LOWER CHORD ANGLE, STA 196. REMOVED CORROSION. INSTALLED DOUBLER PER ESO 11697 DATED 6-1 7-96. TST: 64,997 HOURS. CYCLES, 44,491. (X) 2 L 7 3 4F A3WE 1996072500146 19960725 00146 WP 1996 7 25 HAL9667 1 19960531 A 3297 WIRE DOUG DC9 DC951 3022051 WP NLG BROKEN A HALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 13 EICBH 47796 HNL - FLT 504 - UPON TAKEOFF AND GEAR RETRACTION, NOSE GEAR UNSAFE LIGHT AND GEAR DOOR OPEN LIGHT REMAINED ON. RECYCLED , INITIALLY 3 GREEN, THE NOSE GEAR UNSAFE LIGHT ILLUMINATED AGAIN. DID EMERGENCY GEAR EXTENSION, STILL FLUCTUATED BETWE EN RED AND GREEN. GEAR DOOR OPEN LIGHT ON AND OFF ALSO. (RETURNED TO HNL.) INSPECTED NOSE GEAR AND DOORS FOR CONDITIO N AND SECURITY CHECKED OK. CLEANED AND INSPECTED MLG DOOR PROXIMITY SWITCHES, REPLACED PROXIMITY WARNING CONTROL BOX. B ITE CHECK GOOD. FOUND BROKEN WIRE ON NOSE GEAR RPOXIMITY SWITCH HARNESS, REPLACED PROXIMITY SWITCH, AND CONDUIT ON NLG. GEAR SWING CHECK OK. (X) 2 L 7 2 4F RT A6WE 1996072500147 19960725 00147 WP 1996 7 25 HAL9679 1 19960624 A 2150 UNI5021 APU DOUG DC10 DC1010 3022110 WP APU COMPT OIL LEAK A HALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 13 116AA 73094 911 P90132 46516 HNL - FLT 12 - SMOKE AND OIL SMELL IN CABIN ON GROUND PRIOR TO DEPARTURE. *SUPPLEMENTAL SDR TO SHOW FINAL CLOSING ACTIO N*. REMOVED NRS 1, 2, 3 AIR CONDITIONER COALESCER BAGS AND PURGED AIRCRAFT SYSTEM PER MM 21-10-00. REPLACED COALESCER BAGS AND THE OPERATIONAL CHECK AND LEAK CHECK GOOD. THE APU OIL SMOKE AND OIL SMELL RETURNED AND THE APU WAS PLACARDED INOPERATIVE. A NEW APU WAS SENT TO SFO AND AN APU CHANGE IS SCHEDULED FOR JUNE 28, 1996. THE APU WAS CHANGED ON JUNE 2 8 AS SCHEDULED. THE AIRCRAFT IS IN SERVICE. (X) 2 L 7 3 4F A22WE 1996072500148 19960725 00148 WP 1996 7 25 HAL9680 1 19960626 A 3244 TIRE DOUG DC9 DC951 3022051 WP NLG SHIMMY A HALA C D ABORTED TAKEOFF RETURN TO BLOCK E VIBRATION/BUFFET TO TAKEOFF 1 WP 13 601AP 47658 ITO - FLT 121 - VIOLENT NOSE WHEEL SHIMMY AT APPROXIMATELY 75 KNOTS. APPLIED FORWARD YOKE PRESSURE WITH NOSE WHEEL STEE RING INPUT. NO CHANGE. ABORTED THE TAKEOFF. VISUALLY CHECKED NOSE LANDING GEAR AND SURROUNDING AREA. NO DEFECTS NOTE D. REMOVED AND REPLACED NOSE TIRE ASSEMBLIES. (X) 2 L 7 2 4F A6WE 1996072500149 19960725 00149 WP 1996 7 25 HAL9681 1 19960628 A 3350 P4010049 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 699HA 4658 47763 HNL - FLT 113 - FORWARD SIDEWALL EMERGENCY OVERWING EMERGENCY LIGHTS WILL NOT TEST. REPLACED BATTERY. OPS CHECK OK. ( X) 2 L 7 2 4F A6WE 1996072500150 19960725 00150 WP 1996 7 25 HAL9684 1 19960629 A 2131 5037 CONTROLLER DOUG DC10 DC1010 3022110 WP CABIN MALFUNCTIONED A HALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 153AA 121134 46708 LAX - FLT 04 - AIRCRAFT WOULD NOT PRESSURIZE IN AUTO MODE SHORTLY AFTER TAKEOFF FROM LAX. F/A SAID R-4 DOOR AND L-4 DOO R NOT PLUGGING PROPERLY AFTER TAKEOFF. MANUAL MODE WORKED BETTER AFTER REDUCTION OF POWER AND HIGH STAGE BLEED CAME ON. AIRCRAFT RETURNED TO GATE AFTER 20 MINUTES IN THE AIR. (ATB) REPLACED AUTO PRESSURE CONTROL. BITE CHECKED SYSTEM OK . INSPECTED ALL CABIN AND CARGO DOOR SEALS. OK. PRESSURIZED AIRCRAFT AND OPS CHECK NORMAL. (X) 2 L 7 3 4F A22WE 1996072500151 19960725 00151 WP 1996 7 25 HAL9685 1 19960702 A 2612 FIRE LOOP DOUG DC9 DC951 3022051 WP NR 1 ENGINE LOOSE CONNECTOR A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 673MC 47726 HNL - LEFT ENGINE B-LOOP INOPERATIVE. *SUPPLEMENTAL* - CLEANED AND SECURED CONNECTOR. OPS CHECK OK. (X) 2 L 7 2 4F A6WE 1996072500152 19960725 00152 WP 1996 7 25 HAL9686 1 19960629 A 3350 P4010049 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 EICBH 4912 47796 HNL - LEFT SIDEWALL EMERGENCY LIGHTS ON AFT OVERWING EXIT DIM. CHANGED LIGHT SYSTEM, CONDITION SAME. REPLACED BATTERY. OPS CHECKED GOOD. (X) 2 L 7 2 4F A6WE 1996072500153 19960725 00153 WP 1996 7 25 HAL9687 1 19960630 A 3350 P4010049 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 709HA 4990 47764 HNL - FORWARD LEFT OVERWING EMERGENCY EXIT LIGHTS ON SIDEWALL DIM. REPLACED BATTERY. OPS CHECKED GOOD. (X) 2 L 7 2 4F A6WE 1996072500154 19960725 00154 WP 1996 7 25 HAL9688 1 19960701 A 7931 VTO304F OIL PRESS XMTR DOUG DC9 DC951 3022051 WP NR 2 ENGINE MALFUNCTIONED A HALA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 13 420EA 107153 47689 HNL - FLT 540 - DURING TAKEOFF ROLL, RIGHT ENGINE OIL PRESSURE GAUGE DROPPED TO ZERO. ABORTED TAKEOFF. RETURNED TO GAT E. REPLACED OIL PRESSURE TRANSMITTER ON NR 2 ENGINE. CHECKED CONDITION AND SECURITY OF CANNON PLUG AND WIRING ON ENGIN E. OPERATIONAL CHECK GOOD. OK FOR SERVICE. (X) 2 L 7 2 4F A6WE 1996072500155 19960725 00155 WP 1996 7 25 HAL9689 1 19960702 A 2612 FIRE LOOP DOUG DC9 DC951 3022051 WP NR 1 ENGINE INOPERATIVE A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 673MC 47726 HNL - NR 1 ENGINE B-LOOP INOPERATIVE. OK TO CONTINUE PER MEL 26-1. (X) 2 L 7 2 4F A6WE 1996072500156 19960725 00156 WP 1996 7 25 HAL9690 1 19960706 A 2612 FIRE LOOP DOUG DC9 DC951 3022051 WP NR 1 ENGINE FAILED CONNECTOR A HALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 13 673MC 47726 HNL - NR 1 ENGINE B-LOOP INOPERATIVE. *SUPPLEMENTAL* - REPLACED CONNECTOR FOR NR 1 ENGINE APRON B-LOOP. RUN-UP ENGINE CHECK OK. (X) 2 L 7 2 4F A6WE 1996072500157 19960725 00157 WP 1996 7 25 HAL9691 1 19960706 A 2612 FIRE LOOP DOUG DC9 DC951 3022051 WP NR 2 ENGINE DIRTY CONNECTOR A HALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 13 673MC 47726 HNL - NR 2 ENGINE B-LOOP INOPERATIVE. TEST OK. CLEANED NR 2 ENGINE B-LOOP ELEMENT CONNECTORS. RUN-UP ENGINE, OPERATIO N CHECK OK. (X) 2 L 7 2 4F A6WE 1996072500158 19960725 00158 EU 1996 7 25 M3HA96021 1 19960708 A 7714 CONNECTOR AEROSP ATR42 ATR42320 8680930 EU LT ENGINE DIRTY A M3HA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 13 988MA 380 HNL - FLT 301 - DURING CLIMB-OUT, NR 1 NH INDICATOR BECAME INOPERATIVE. AIRCRAFT RETURNED TO HNL. CLEANED CANNON PLUG ON NR 1 NH SENSOR. OPS CHECKED OK. (X) 2 H 7 2 4T RT A53EU 1996072500159 19960725 00159 NE 1996 7 25 RAIA960529 2 19960521 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE RIGHT FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 564HK 630 41081 76097 STL - FLT 7282 - RIGHT ENGINE OIL CONTAMINATION LIGHT CAME ON IN-FLIGHT. MAINTENANCE PERFORMED ENGINE SOAP SAMPLE, AND REPLACED THE RIGHT ENGINE. (X) 2 L 7 2 4T 4 T RT A41NM E18NE 1996072500160 19960725 00160 EU 1996 7 25 SIMA961851 1 19960703 A 2611 FR3222 SMOKE DETECTOR AEROSP ATR72 ATR72212 EU LAVATORY FAILED A SIMA O OTHER N FALSE WARNING AP APPROACH 1 SW 21 420AT 221 420 ICT - FLT 4861- AFT SMOKE WARNING IN COCKPIT. LAVATORY SMOKE INDICATION ON F/A'S PANEL. NO VISUAL INDICATION OF SMOKE IN AIRCRAFT. MAINTENANCE REPLACED DETECTOR AND TESTED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1996072500161 19960725 00161 EU 1996 7 25 SIMA961861 1 19960704 A 3350 3011151 POWER SUPPLY AEROSP ATR42 ATR42300 8680920 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 223AT 3656 223 DFW - FLT 3623 - EMERGENCY LIGHTS AT PASSENGER ENTRANCE AND 12 WL INOPERATIVE. REPLACED BATTERY POWER SUPPLY AT 30 WL A ND 18 WL. AIRCRAFT WAS RETURNED TO SERVICE. REFERENCE: OPERATOR CONTROL NR 96ZZZX3651, AND CONTROL NR 96ZZZX3652. (X ) 2 H 7 2 4T RT A53EU 1996072500162 19960725 00162 EU 1996 7 25 SIMA961881 1 19960706 A 2150 22051201 ACM AEROSP ATR72 ATR72212 EU RIGHT FAILED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 447AM 2755 0435 447 DFW - FLT 3687 - ABOUT TWO MINUTES AFTER TAKEOFF, NR 1 F/A CALLED AND REPORTED SMELL OF SMOKE. SOON AFTER, COULD SMELL IT IN THE COCKPIT. AIRCRAFT RETURNED TO DFW. REPLACED RIGHT ACM DUE TO SEIZURE. (X) 2 H 7 2 4T RT A53EU 1996072500163 19960725 00163 EU 1996 7 25 SIMA961882 1 19960706 A 3350 3012001 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 667 263 GRR - EMERGENCY LIGHTS IN AFT CABIN FOUND INOPERATIVE IN MAINTENANCE CHECK. REPLACED BATTERY PACK. OPS CHECK GOOD. AI RCRAFT WAS RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1996072500164 19960725 00164 NE 1996 7 25 Y2PA96046 2 19960629 A 7200 ENGINE AMD FALC20 FALCOND 2720304 EU GE CF700 CF7002D2 30010 NE AFT FUSELAGE BIRD STRIKE A Y2PA C D ABORTED TAKEOFF RETURN TO BLOCK C F.O.D. TO TAKEOFF 1 GL 23 821AA 10229 3555 203 245G013 YIP - FLT 17211 - BIRD INGESTED DURING TAKEOFF ROLL. CREW ABORTED TAKEOFF AT 110 KNOTS. NO EMERGENCY PROCEDURES BEYOND ABORTED TAKEOFF REQUIRED. AIRCRAFT DID NOT BECOME AIRBORNE. ENGINE FAN ROTOR ASSEMBLY BADLY DAMAGED DUE TO BIRD INGES TION. ALL FAN BLADES APPEAR TO BE SCRAP. ENGINE COMPRESSOR IS ALSO DAMAGED DUE TO FOD, POSSIBLY DUE TO MATERIAL FORCED FORWARD FROM THE FAN ROTOR THROUGH THE BYPASS DUCT AND INTO THE COMPRESSOR INLET. ALL DAMAGE CONTAINED WITHIN THE ENGI NE. ENGINE REMOVED FROM AIRCRAFT AND SENT TO ENGINE SHOP FOR MAJOR REPAIR. PART TOTAL CYCLES, 7,075. (X) 2 L 7 2 4F 4 F A7EU E7EA 1996072500165 19960725 00165 WP 1996 7 25 9615629961 1 19960721 A 2550 PIN DOUG DC9 DC931 3022065 WP CARGO COMPT OUT OF POSITION A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 924RW 47185 AFTER TAKEOFF, THE AFT CARGO DOOR WARNING LIGHT ILLUMINATED. RETURNED TO DTW WITHOUT FURTHER INCIDENT. FOUND THE LOWER CARGO NET PIN BETWEEN THE DOOR AND DOOR JAMB. INSPECTED THE DOOR AND SWITCH, NO TROUBLE FOUND. 2 L 7 2 4F A6WE 1996072500166 19960725 00166 EU 1996 7 25 9615633201 1 19960721 A 3260 DOOR INDICATION AIRBUS 320 A320211 3930320 EU RT MLG MALFUNCTIONED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 301US 31 DURING APPROACH AFTER LANDING GEAR EXTENSION, THE RIGHT MAIN LANDING GEAR DOOR INDICATED APPROXIMATELY ONE FOURTH OPEN. CYCLED LANDING GEAR HANDLE AND INDICATION REMAINED THE SAME. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHO OTING REVEALED NO DISCREPANCIES. 2 L 7 2 4F RT A28NM 1996072500167 19960725 00167 NM 1996 7 25 9615642276 1 19960717 A 3350 BATTERY PACK BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 276US 21155 DURING PREFLIGHT, FOUND EMERGENCY EXIT SIGN BY AFT GALLEY INOPERATIVE. REPLACED BATTERY PACK, CHECKED OK. 2 L 7 3 4F A3WE 1996072500168 19960725 00168 NE 1996 7 25 9615652285 2 19960715 A 7260 STUD BOEING 727 727251 138408H NM PWA JT8 JT8D15 52051 NE NR 2 ENG GEARBOX FAILED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN J K WARNING INDICATION FLUID LOSS CR CRUISE 1 GL 01 265US 21324 696473 NR 2 ENGINE OIL QUANTITY WAS DECREASING DURING CRUISE FLIGHT. ACCOMPLISHED PRECAUTIONARY SHUTDOWN. FLIGHT DIVERTED TO FAR AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED STUD IN GEARBOX AND SERVICED OIL TANK. PERFORMED LEAK AND OPERAT IONAL CHECK, NO LEAKS FOUND. 2 L 7 3 4F 4 F A3WE E2EA 1996072500169 19960725 00169 WP 1996 7 25 ABXA9600598 1 19960717 A 2410 MS17413270 O-RING DOUG DC8 DC863 302198A WP PWA JT3D JT3D7 52039 NE NR 3 CSD LEAKING A ABXA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 23 821AX 46116 671175 NR 3 ENGINE OIL QUANTITY SLOWLY DECREASED AFTER TAKEOFF. THE ENGINE WAS SHUTDOWN WHEN THE OIL QUANTITY REACHED ONE GALL ON. OIL PRESSURE AND OIL TEMPERATURE WAS NORMAL. ENGINE WINDMILLED AT 29 PERCENT N2 AND 16 PERCENT N1 AFTER SHUTDOWN A T 0445Z. ENGINE MAINTAINED AN OIL PRESSURE OF 5 PSI AFTER SHUTDOWN. RESEALED NR 3 ENGINE CSD GARLOCK SEAL AND INSTALLE D AN O-RING SEAL ON THE NR 3 ENGINE CSD. LEAK CHECK AND OPS CHECK GOOD IAW DC8 MM, CHAPTER 24-10-1 AND PRATT AND WHITNE Y MM, CHAPTER 72-00. 2 L 7 4 4F 4 F 4A25 1E8 1996072500170 19960725 00170 WP 1996 7 25 ABXA9600599 1 19960717 A 3260 0080004003 PROX CONTL BOX DOUG DC9 DC941 302207N WP RT MLG DEFECTIVE A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 953AX 47608 RIGHT GEAR UNSAFE LIGHT REMAINS ON WITH GEAR HANDLE IN UP POSITION. REPLACED THE PROXIMITY CONTROL BOX AND PERFORMED A GEAR SWING IAW DC-9 MM 32-6-0. 2 L 7 2 4F A6WE 1996072500171 19960725 00171 WP 1996 7 25 ABXA9600600 1 19960719 A 3350 1820 LAMP DOUG DC8 DC861 3021952 WP CABIN DEFECTIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 845AX 46157 EMERGENCY EXIT LIGHT DOES NOT INDICATE DISARMED. RELAMPED EMERGENCY EXIT LIGHT, OPS CHECK GOOD. 2 L 7 4 4F 4A25 1996072500172 19960725 00172 WP 1996 7 25 ARWA9607001 1 19960721 A 3260 7000010101 SWITCH DOUG DC8 DC863F 302198F WP RT MLG INOPERATIVE A ARWA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 19 441J 45988 ON CLIMB-OUT FROM ATL, GEAR NOT LATCHED. LIGHT CAME ON, RECYCLED GEAR AND NOW GEAR AND DOOR LIGHT ON. DIVERTED TO MIAM I. TROUBLESHOT, FOUND RT MLG UPLATCH SWITCH BAD. REMOVED AND REPLACED SWITCH I.A.W. 32-30-00. OPS CHECKED NORMAL ON G EAR SWING, RETURN ACFT TO SERVICE. 2 L 7 4 4F 4A25 1996072500173 19960725 00173 NM 1996 7 25 CALA9601041 1 19960719 A 3040 6171545 HEAT CONTROL BOEING 747 747230B 1384889 NM R1 WINDOW INOPERATIVE A CALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 78019 18961 4937 20527 CREW OBSERVED A STRONG ELECTRICAL INSULATION ODOR COMING FROM THE MAP AND APPROACH LIGHT CONTROL SWITCHES DURING FLIGHT. THE WIRE LEADING TO R-1 WINDOW WAS ALSO HOT. THE CIRCUIT BREAKERS WERE PULLED AND THE ODOR CEASED. MAINTENANCE CHECK ED BOTH MAP AND APPROACH LIGHT CONTROLS AND NO DEFECTS WERE FOUND. MAINTENANCE FOUND THE R-1 WINDOW HEAT CONTROL AT FAU LT. OPERATION OF THE R-1 WINDOW HEAT CHECKED GOOD IAW MM 30-41-04. MAINTENANCE ALSO FOUND A BAD TERMINAL ON CONTACT A OF WINDOW. THE TERMINAL WAS REPLACED. 2 L 7 4 4F A20WE 1996072500174 19960725 00174 NM 1996 7 25 CALA9601042 1 19960721 A 2910 BACH8B04NN0202T HYD LINE BOEING 737 737214 138446R NM NLG D/L ACT LEAKING A CALA A D UNSCHED LANDING RETURN TO BLOCK J K WARNING INDICATION FLUID LOSS CL CLIMB 1 SW 09 14239 19920 THE A-SYSTEM HYDRAULIC QUANTITY BEGAN TO DROP SHORTLY AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED W ITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR DOWNLOCK ACTUATOR UPPER LINE LEAKING. THE LINE WAS REMOVED AND REPLAC ED, LEAK CHECK WAS GOOD. 2 L 7 2 4F A16WE 1996072500175 19960725 00175 WP 1996 7 25 CALA9601043 1 19960721 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP COCKPIT ENT LOW VOLTAGE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 THE COCKPIT ENTRANCE EMERGENCY LIGHTS WERE FOUND VERY DIM DURING A PREFLIGHT INSPECTION. THE COCKPIT EMERGENCY BATTERY PACK WAS REMOVED AND REPLACED AND THE LIGHTS WERE RESTORED TO NORMAL. 2 L 7 2 4F A6WE 1996072500176 19960725 00176 NM 1996 7 25 CALA9601044 1 19960719 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 967 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14307 23358 INSPECTION FOUND INTERCOSTAL CORRODED AT FS 967, LBL 17.61 AND RBL 17.61. A REPAIR WAS PERFORMED IAW ECRA 5320-01443. 2 L 7 2 4F RT A16WE 1996072500177 19960725 00177 NM 1996 7 25 CALA9601045 1 19960720 A 2150 PACK BOEING 727 727224 1384076 NM CABIN SMOKING A CALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DE DESCENT 1 SW 09 69735 20664 WHILE OPERATING RT PACK IN MANUAL WITH MIX VALVE AT HALF POSITION, THE RIGHT PACK TEMP WENT TO 150 DEGREES AND WAS ACCOM PANIED BY CABIN SMOKE DURING DESCENT INTO EWR. THE SMOKE CLEARED WHEN COOLING DOOR WAS OPENED AND MIX VALVE WAS ADJUST ED. THE AIRCRAFT LANDED AT EWR WITHOUT FURTHER PROBLEM. MAINTENANCE CHECKED THE OPERATION OF BOTH PACKS ON THE GROUND WITH ENGINES RUNNING AND WERE UNABLE TO DUPLICATE THE PROBLEM. THE ENGINE BLEED AIR DISTRIBUTION WAS ALSO CHECKED IAW M M 36-10-0 AND ALL OPERATION CHECKED GOOD. 2 L 7 3 4F A3WE 1996072500178 19960725 00178 SO 1996 7 25 COMA9610226 1 19960717 A 2916 3182001003 RESERVOIR EMB 120 EMB120RT SO LEFT LEAKING A COMA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 246CA 120223 LEFT HYDRAULIC RESERVOIR LOW PRESSURE WARNING ILLUMINATED DURING FLIGHT. REPLACED THE HYDRAULIC RESERVOIR ASSY. 2 L 7 2 4T RT A31SO 1996072500179 19960725 00179 SO 1996 7 25 COMA9610227 1 19960719 A 3241 426871 CONTROL BOX EMB 120 EMB120RT SO AVIONICS MALFUNCTION A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 1110J 16411 14234 120110 ANTI-SKID LIGHT ILLUMINATED WHEN LANDING GEAR RETRACTED. REPLACED THE ANTI-SKID CONTROL BOX. 2 L 7 2 4T RT A31SO 1996072500180 19960725 00180 EA 1996 7 25 COMA9660124 1 19960718 A 7830 22850741115 TR SWITCH CNDAIR CL600 CL6002B19 EA RT ENG MALFUNCTION A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 940CA 7048 RT THRUST REVERSER ICON CAME ON IN FLIGHT. THRUST REVERSER DID NOT DEPLOY. REPLACED THE RT ENGINE THRUST REVERSER STOW SWITCH. 2 L 7 2 4F RT A21EA 1996072500181 19960725 00181 NM 1996 7 25 DL72E961708 1 19960625 A 5754 651622199 RIB BOEING 727 727247 138408F NM LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 282WA 21484 LOWER AFT FLANGE DOUBLER CRACKED, UPPER FWD FLANGE CRACKED PAST STOP DRILL AND LOWER FWD FLANGE DOUBLER CRACKED. REPLAC ED RIB. 2 L 7 3 4F A3WE 1996072500182 19960725 00182 NM 1996 7 25 DL72E961709 1 19960625 A 5754 651622199 RIB BOEING 727 727247 138408F NM NR 4 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 282WA 21484 LOWER AFT FLANGE CRACKED, UPPER FLANGE CRACKED AND STOP DRILLED BUT NO DOUBLER AND FWD FLANGE HAS TEMPORARY REPAIR. REP LACED RIB. 2 L 7 3 4F A3WE 1996072500183 19960725 00183 NM 1996 7 25 DL72E961710 1 19960625 A 5754 651622199 RIB BOEING 727 727247 138408F NM NR 4 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 282WA 21484 LOWER FLANGE OF RIB NR 18 CRACKED IN RADIUS. STOP DRILLED CRACK AND REPAIRED PER SRM 57-54-0. 2 L 7 3 4F A3WE 1996072500184 19960725 00184 NM 1996 7 25 DL72E961711 1 19960625 A 5754 651622199 SPAR WEB BOEING 727 727247 138408F NM NR 4 LE SLAT DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 282WA 21484 UPPER SPAR WEB FLANGE DAMAGED BY STOP DRILLING RIBS NR 11 AND NR 12. MANUFACTURED DOUBLER, REPAIRED PER SRM 57-50-3 FIG 4. 2 L 7 3 4F A3WE 1996072500185 19960725 00185 NM 1996 7 25 DL72K961714 1 19960708 A 5754 COVE SKIN ANGLE BOEING 727 727232 1384082 NM NR 2 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 474DA 20751 FOUND .25 INCH CRACK EXTENDING FROM NR 2 SLAT O/B TRACK UP STOP PAD, IN COVE SKIN ATTACH ANGLE. REPAIRED PER M/M 57-54- 0 PG 816. 2 L 7 3 4F A3WE 1996072500186 19960725 00186 NM 1996 7 25 DL72K961715 1 19960708 A 5720 STIFFENER BOEING 727 727232 1384082 NM LE SPAR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 474DA 20751 FOUND 1.25 INCH CRACKS AT WING L/E SPAR STIFFENERS AFT OF NR 3 SLAT I/B TRACK TWO EACH. REPAIRED BY REPLACING STIFFENER S PER M/M 57-20-21 PG 813. 2 L 7 3 4F A3WE 1996072500187 19960725 00187 NM 1996 7 25 DL72K961716 1 19960708 A 2782 BRACKET BOEING 727 727232 1384082 NM NR 7 LE SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 474DA 20751 FOUND NR 7 SLAT ACTUATOR CRACKED I/B BRACKET UPPER LOBE. REPAIRED PER ERA 303841-14. 2 L 7 3 4F A3WE 1996072500188 19960725 00188 NM 1996 7 25 DL72K961717 1 19960708 A 5720 STIFFENER BOEING 727 727232 1384082 NM LE SPAR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 474DA 20751 FOUND 1 CRACK IN WING L/E SPAR STIFFENERS OF NR 2 O/B TRACK. REPAIRED PER M/M 57-20-21 PG 813. 2 L 7 3 4F A3WE 1996072500189 19960725 00189 NM 1996 7 25 DL72K961728 1 19960718 A 3350 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 474DA 20751 1L EMERGENCY LIGHT INOP. REPLACED LIGHT ASSEMBLY. 2 L 7 3 4F A3WE 1996072500190 19960725 00190 NM 1996 7 25 DL72K961733 1 19960708 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 2 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 474DA 20751 A .25 INCH CRACK EXTENDING FROM NR 2 SLAT O/B TRACK UPSTOP PAD IN COVE SKIN ATTACH ANGLE. INSTALLED DOUBLER PER M/M 57- 54-0 PG 816. 2 L 7 3 4F A3WE 1996072500191 19960725 00191 NM 1996 7 25 DL72K961738 1 19960719 A 3350 OL3071PEGPL LAMP BOEING 727 727232 1384082 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 481DA 20861 AFT EMERGENCY PATH LIGHT INOP DURING TEST. RELAMPED, CKS OK. 2 L 7 3 4F A3WE 1996072500192 19960725 00192 NM 1996 7 25 DL72L961694 1 19960714 A 3350 CONNECTORS BOEING 727 727232 1384082 NM L1 DOR DIRTY A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 502DA 21304 ON LAYOVER, FOUND L-1 DOOR OVERHEAD EMERGENCY EXIT SIGN INOP. CLEANED BATTERY CONNECTORS AND LIGHT ASSY CONTACTS, ALL O PS NORMAL. 2 L 7 3 4F A3WE 1996072500193 19960725 00193 NM 1996 7 25 DL72L961704 1 19960717 A 5754 651622292 RIB BOEING 727 727232 1384082 NM LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 513DA 21315 RIB CRACKED AT RADIUS. REPAIRED RIB PER M/M 57-54-00 PG 813. 2 L 7 3 4F A3WE 1996072500194 19960725 00194 NM 1996 7 25 DL72L961705 1 19960717 A 5754 651622292 RIB BOEING 727 727232 1384082 NM RT LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 513DA 21315 RIB CRACKED AT RADIUS. REPAIRED RIB PER M/M 57-54-00. 2 L 7 3 4F A3WE 1996072500195 19960725 00195 NM 1996 7 25 DL72P961678 1 19960712 A 3350 081691 LIGHT BOEING 727 727225 1384077 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8889Z 21858 EPL LIGHT AT SEAT 5C IS LOOSE FROM MOUNTING AND LIGHT INOP. REPLACED LIGHT ASSY AND CHECKS OK. 2 L 7 3 4F A3WE 1996072500196 19960725 00196 NM 1996 7 25 DL72S961675 1 19960712 A 3350 6104789 BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 542DA 22391 L2 AND R2 SERVICE EXIT DOOR SLIDE LIGHTS INOP. REPLACED BATTERY PACK M983. 2 L 7 3 4F A3WE 1996072500197 19960725 00197 NM 1996 7 25 DL72S961680 1 19960712 A 3350 1619 BULB BOEING 727 727232 1384082 NM CABIN CORRODED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 521DA 21472 ON LAYOVER, FOUND L-1 DOOR EMERGENCY LIGHT INOP. RELAMPED, CHECKS GOOD. 2 L 7 3 4F A3WE 1996072500198 19960725 00198 NM 1996 7 25 DL72S961685 1 19960712 A 3350 BATTERIES BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 497DA 21077 L1 AND COCKPIT DOOR EMERGENCY LIGHTS INOP. REPLACED BATTERIES IN RACKS, BOTH OP CHECK GOOD. 2 L 7 3 4F A3WE 1996072500199 19960725 00199 NM 1996 7 25 DL72S961695 1 19960706 A 5315 FLOOR BEAM BOEING 727 727232 1384082 NM BS 344 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 420DA 21273 FOUND CORROSION ON FLOOR BEAM STA 344 AT SEAT TRACK ATTACH POINT RBL 21. REPAIRED PER SRM 53-10-8 FIG 11. 2 L 7 3 4F A3WE 1996072500200 19960725 00200 NM 1996 7 25 DL72S961696 1 19960716 A 5754 6516221100 SKIN BOEING 727 727232 1384082 NM NR 5 LE SLAT GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 475DA 20752 DEEP GOUGE IN LWR SKIN BY LINE UP SPADE. REPAIRED PER SRM 57-50-3. 2 L 7 3 4F A3WE 1996072500201 19960725 00201 NM 1996 7 25 DL72S961713 1 19960717 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 483DA 20863 DURING SERVICE CHECK, FOUND EMERGENCY EXIT LIGHTS ABOVE OVERWING EXITS ON RT SIDE INOP. REPLACED BATTERY PACK, OPS NORM AL. 2 L 7 3 4F A3WE 1996072500202 19960725 00202 NM 1996 7 25 DL72S961720 1 19960710 A 5330 65545902 SKIN BOEING 727 727232 1384082 NM BS 696 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 519DA 21470 A PUNCTURE REPAIR WAS FOUND CORRODED. THE CORROSION LED TO A 1 BY 2 CUT OUT AT STA 695 OUTBOARD OF STRINGER 28R. DAMAG E WAS REPAIRED PER B727 SRM 53-30-3, FIGURE 1. 2 L 7 3 4F A3WE 1996072500203 19960725 00203 NM 1996 7 25 DL72S961721 1 19960711 A 5330 6518420 SKIN BOEING 727 727232 1384082 NM BS 700/720 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 420DA 21273 THREE AREAS OF CORRODED SKIN WERE FOUND, ONE AT FS 720 STRINGER 28L, ONE AT FS 720, STRINGER 28R AND ONE AT FS 700 STRIN GER 28R. THERE IS AN EXISTING REPAIR AT FS 700 STRINGER 28L. TWO DOUBLERS WILL BE INSTALLED TO REPAIR THE DAMAGE. THE REPAIR DOUBLERS ARE INSTALLED IN ACCORDANCE WITH S/B 727-53A0203, REV 2. 2 L 7 3 4F A3WE 1996072500204 19960725 00204 NM 1996 7 25 DL72S961726 1 19960416 A 5754 651622296 RIB BOEING 727 727232 1384082 NM LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 498DA 21142 RIB NR 8 WAS CRACKED. REPAIRED RIB PER MM 57-54-0 FIG 805. 2 L 7 3 4F A3WE 1996072500205 19960725 00205 NM 1996 7 25 DL72S961727 1 19960416 A 5754 651622296 RIB BOEING 727 727232 1384082 NM LE SLAT DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 498DA 21142 RIB NR 11 WAS CRACKED. INSTALLED RIB REPAIR PER MM 57-54-0 FIG 805. 2 L 7 3 4F A3WE 1996072500206 19960725 00206 NM 1996 7 25 DL72S961729 1 19960416 A 5754 651622296 RIB BOEING 727 727232 1384082 NM LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 498DA 21142 RIB NR 12 WAS CRACKED. INSTALLED REPAIR PER MM 57-54-0 FIG 805. 2 L 7 3 4F A3WE 1996072500207 19960725 00207 NM 1996 7 25 DL72S961730 1 19960416 A 5754 651622296 RIB BOEING 727 727232 1384082 NM LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 498DA 21142 RIB NR 12 WAS CRACKED. REPAIRED RIB PER MM 57-54-0 FIG 805. 2 L 7 3 4F A3WE 1996072500208 19960725 00208 NM 1996 7 25 DL72S961731 1 19960416 A 5754 651622296 RIB BOEING 727 727232 1384082 NM LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 498DA 21142 RIB NR 18 WAS CRACKED. REPAIRED RIB PER MM 57-54-0 FIG 805. 2 L 7 3 4F A3WE 1996072500209 19960725 00209 NM 1996 7 25 DL72S961734 1 19960716 A 5754 BRACKET BOEING 727 727232 1384082 NM NR 2 LE FLAP ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 521DA 21472 FOUND CRACK ON I/B ACTUATOR BRACKET FOR THE NR 2 L/E K-FLAP. REPAIRED PER M/M 57-20-21 FIG 807 AND INSTALLED PER M/M 57 -20-21 PG 811. 2 L 7 3 4F A3WE 1996072500210 19960725 00210 NM 1996 7 25 DL72S961736 1 19960716 A 5754 RIB BOEING 727 727232 1384082 NM NR 3 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 521DA 21472 RIB CRACKED NR 3 L/E SLAT, O/B OF ACTUATOR ATTACH BRACKET O/B RIB. FABRICATED REPAIR PER MM 57-54-0 PG 804. 2 L 7 3 4F A3WE 1996072500211 19960725 00211 NM 1996 7 25 DL72S961742 1 19960720 A 3350 BATTERIES BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 495DA 21075 ON PREFLIGHT, FOUND 1 EMERGENCY FLASHLIGHT AT 1L DOOR LED NOT FLASHING. REPLACED BATTERY AND BULB, NOW OPN NORM. 2 L 7 3 4F A3WE 1996072500212 19960725 00212 NM 1996 7 25 DL72W961723 1 19960709 A 5330 SKIN BOEING 727 727247 138408F NM BS 1095.9 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 297WA 22534 THE FUSELAGE SKIN WAS INITIALLY CRACKED AT STA 1095.9 OUTBOARD OF STR 1. THE DAMAGE WAS REPAIRED WITH A TIME LIMITED DO UBLER. WHEN THE PERMANENT REPAIR WAS BEING INSTALLED, TWO ADDITIONAL DAMAGE LOCATIONS WERE FOUND. A NEW PERMANENT REPA IR DOUBLER WAS INSTALLED IN ACCORDANCE WITH S/B 727-53A0204. 2 L 7 3 4F A3WE 1996072500213 19960725 00213 NM 1996 7 25 DL72W961732 1 19960710 A 5240 FRAME BOEING 727 727247 138408F NM R2 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 297WA 22534 R2 DOOR FWD FRAME CRACKED AT UPPER HINGE CUTOUT. REPAIRED PER SRM 52-40-02 FIG 4. 2 L 7 3 4F A3WE 1996072500214 19960725 00214 NM 1996 7 25 DL757961677 1 19960711 A 3350 LIGHT BOEING 757 757232 1384965 NM AFT RT OVERWING INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 672DL 25977 AFT RIGHT OVERWING EMERGENCY SLIDE LIGHT INOP. RELAMPED, CHECKS NORMAL. 2 L 7 2 4F RT A2NM 1996072500215 19960725 00215 NM 1996 7 25 DL757961689 1 19960713 A 3350 BATTERY PACK BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 635DL 23762 687344 L2 DOOR EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK SYSTEM, CHECKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 1996072500216 19960725 00216 NM 1996 7 25 DL757961690 1 19960713 A 2910 HYD FLUID BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE LEFT LOST A DALA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 670DN 25331 687344 AFTER T/O, LOST ALL LEFT HYD FLUID. UPON ARRIVAL, NECESSARY TO ALTERNATE EXTEND LANDING GEAR, PULLED AIRCRAFT OFF RUNWA Y TO GATE WITH TOW TRACTOR. LEFT HYD SYSTEM QTY READS ZERO. 2 L 7 2 4F 4 F RT A2NM E17NE 1996072500217 19960725 00217 NM 1996 7 25 DL757961718 1 19960717 A 3350 767 LAMP BOEING 757 757232 1384965 NM AFT CARGO DOOR FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 635DL 23762 EXTERIOR EMERGENCY LIGHT ON THE AFT CARGO DOOR INOP. RELAMPED, OP CK GOOD. 2 L 7 2 4F RT A2NM 1996072500218 19960725 00218 NM 1996 7 25 DL757961722 1 19960710 A 5754 114N4005158 TE WEDGE BOEING 757 757232 1384965 NM NR 7 LE SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 656DL 24396 THE TRAILING EDGE WEDGE ON THE NR 7 SLAT WAS FOUND WITH DELAMINATION 20 INCHES FROM THE INBOARD END OF THE SLAT. THE DA MAGE MEASURED 2 INCHES ACROSS AND EXTENDED .25 INCH FWD OF THE AFT END OF THE PART. THIS DAMAGE WAS REPAIRED PER B757 S RM 51-70-10 AS SPECIFIED IN CHAPTER 57-43-02, FIGURE 201. 2 L 7 2 4F RT A2NM 1996072500219 19960725 00219 WP 1996 7 25 DLL10961670 1 19960710 A 3350 081691 LIGHT SOCKET LKHEED 1011 10113851 5265010 WP CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 722DA 193C1147 ON LAYOVER, FOUND EMERGENCY LIGHT SOCKET INOP. REPLACED EMERGENCY LIGHT SOCKET, EMERGENCY LIGHTS OP CHECK GOOD. 2 L 7 3 4F A23WE 1996072500220 19960725 00220 WP 1996 7 25 DLL10961697 1 19960716 A 2612 895695 FIRE LOOP LKHEED 1011 10113851 5265010 WP NR 1 ENGINE MALFUNCTIONED A DALA F E ACTIVATE FIRE EXT. ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SO 27 735D 193C1226 NR 1 ENGINE FIRE LIGHT AND BELLS, WENT THROUGH PROCEDURES AND SHUTDOWN, FIRED FIRE BOTTLES. INSPECTION REVEALED THAT NO FIRE HAD OCCURED. REPLACED ALL FIRE DET LOOPS, CHECKS GOOD ON ENGINE RUN FOR TWO HOURS AT DIFFERENT SETTINGS. 2 L 7 3 4F A23WE 1996072500221 19960725 00221 WP 1996 7 25 DLL13961707 1 19960716 A 3260 701147 PROX LOGIC BOX LKHEED 1011 10113851 5265010 WP E/E BAY FAILED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 784DA 193A1038 ALL WARNING LIGHTS FAILED AS PREVIOUS LOG BOOK ENTRY, LDG GEAR, SLAT REV PRESS AND INTRANSIT LIGHTS, DOOR OPEN LIGHTS. A IR TURNBACK TO SEA, NO GREEN DOWN AND LOCK LIGHT GEAR. 2 L 7 3 4F A23WE 1996072500222 19960725 00222 WP 1996 7 25 DLL15961655 1 19960709 A 3070 1553025115 SWITCH PANEL LKHEED 1011 10113853 5265020 WP COCKPIT FAILED A DALA F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 SO 27 752DA 193W1172 ON GROUND, WASTE/WATER PANEL AFT 1 AND AFT 2 SWITCH LIGHT SHORTED OUT CAUSING FLAME AND SMOKE. USED HALON BOTTLE, SWITC H 217201153 FAULTED. REPLACED PANEL (P/N 3170001240). 2 L 7 3 4F A23WE 1996072500223 19960725 00223 WP 1996 7 25 DLL15961667 1 19960710 A 5210 7424281 CABLE LKHEED 1011 10113853 5265020 WP PAX DOOR BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 752DA 193W1172 DURING MID VISIT, THE L3 DOOR FAILED TO OPERATE IN THE EMERGENCY MODE. FOUND LOCK PIN CABLE BROKEN. REPLACED SAME PER MM 52-12-27. 2 L 7 3 4F A23WE 1996072500224 19960725 00224 NM 1996 7 25 DLM11961664 1 19960710 A 3350 LIGHT DOUG MD11 MD11 3023602 NM PWA JT8 JT8D15A 52051 NE CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 803DE 48474 700015 EMERGENCY FLOOR TRACK LIGHTS INOP FWD OF SEAT 30C AND RT SIDE OF FIRST CLASS GALLEY. CLEANED SOCKETS AND RELAMPED, CHEC KS OK. 2 L 7 3 4F 4 F RT A22WE E2EA 1996072500225 19960725 00225 NM 1996 7 25 DLM11961668 1 19960710 A 3350 6044113 BATTERY DOUG MD11 MD11 3023602 NM COCKPIT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 808DE 48479 EMERGENCY BATT TEST FAILS, BATT 1 LOW. FOUND F/C FLOOR TRACK SHORTED OUT AND BATT MAKING LOUD NOISE WHEN SELECTED ON. R EPLACED BATT AND REPAIRED TRACK. 2 L 7 3 4F RT A22WE 1996072500226 19960725 00226 NM 1996 7 25 DLM88961684 1 19960712 A 3350 LIGHTS DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 952DL 49883 EMERGENCY TRACK LIGHTS INOP FROM ROW 29 TO AFT OF ACFT. 2 L 7 2 4F RT A6WE 1996072500227 19960725 00227 NM 1996 7 25 P5CA9600383 1 19960718 A 7110 COWL BOEING 747 747122 1384872 NM NR 3 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 CRACKED CHAFE STRIP NR 3 INBOARD CORE COWL UPPER EDGE. REMOVED, FABRICATED AND REPLACED CHAFE STRIP PER BOEING SRM 51-3 0-02 AND 51-10-01. 2 L 7 4 4F A20WE 1996072500228 19960725 00228 NM 1996 7 25 P5CA9600384 1 19960718 A 5753 LE SKIN BOEING 747 747122 1384872 NM NR 1 TE FOREFLAP DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 SMALL HOLES IN LEFT WING NR 1 FOREFLAP ON LEADING EDGE INBOARD OF NR 1 FLAP TRACK. REPAIRED PER BOEING SRM 51-40-15 AND 51-40-11. 2 L 7 4 4F A20WE 1996072500229 19960725 00229 NM 1996 7 25 P5CA9600385 1 19960720 A 5280 DOOR BOEING 747 747122 1384872 NM LT/RT MLG DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 DELAMINATED REPAIR ON BOTH THE LEFT AND RIGHT WING LANDING GEAR FLYING DOORS. REPAIRED PER BOEING SRM 51-40-15 AND 51-4 0-06. 2 L 7 4 4F A20WE 1996072500230 19960725 00230 NM 1996 7 25 P5CA9600386 1 19960718 A 7110 CHANNEL BOEING 747 747122 1384872 NM NR 3 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 CRACKED CHANNEL ON NR 3 ENGINE INBOARD CORE COWL LOWER CHANNEL AT THE FORWARD MOST GUIDE PIN. REPAIRED PER BOEING SRM 5 1-10-01 AND 51-30-02. 2 L 7 4 4F A20WE 1996072500231 19960725 00231 NM 1996 7 25 P5CA9600387 1 19960718 A 7110 COWL BOEING 747 747122 1384872 NM NR 4 ENGINE TORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 TEAR AT TRAILING EDGE OF NR 4 ENGINE INBOARD CORE COWL OUTER SKIN. REPAIRED PER BOEING SRM 51-10-01, 51-30-02 AND 51-10 -02. 2 L 7 4 4F A20WE 1996072500232 19960725 00232 NM 1996 7 25 P5CA9600388 1 19960717 A 7110 SLOT SEAL BOEING 747 747122 1384872 NM NR 1 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 CRACKED SKIN AT NR 1 ENGINE RIGHT SLOT SEAL FORWARD END. WELD REPAIRED PER BOEING SRM 51-10-01. 2 L 7 4 4F A20WE 1996072500233 19960725 00233 NM 1996 7 25 P5CA9600389 1 19960717 A 5753 SKIN BOEING 747 747122 1384872 NM NR 4 TE MID FLAP CHAFED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 CHAFED TO CORE MATERIAL UPPER SURFACE RIGHT OUTBOARD MID FLAP NEAR OUTBOARD END. REPAIRED PER BOEING SRM 51-40-06. 2 L 7 4 4F A20WE 1996072500234 19960725 00234 SO 1996 7 25 SRAA960706 1 19960720 A 2424 3S2060DC102D1 GEN CTL PNL LKHEED 382 382G 526414U SO COCKPIT FAILED A SRAA G O2 MASK DEPLOYED B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 905SJ 4472 DURING FLIGHT, AFTER 3.8 HOURS INTO FLIGHT, NR 1 GENERATOR CONTROL PANEL EMITS SMOKE. TURNED OFF NR 1 GENERATOR CONTROL PANEL AND REMOVED FROM RACK, RESUMED NORMAL OPERATION AFTER TWO MINUTES WITH OXYGEN MASK. AIRCRAFT LANDED WITHOUT INCI DENT, NR 1 GENERATOR CONRTOL PANEL TRANSFERRED TO DMI 01469 PER MEL 24-5. 2 H 7 4 4T A1SO 1996072500235 19960725 00235 NM 1996 7 25 SWAA96674 1 19960719 A 5330 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 680AA 23505 DURING SCHEDULED B/C1 CHECK, FOUND LEFT AFT FUSE SKIN DENTED AFT OF AFT ENTRY DOOR, JUST BELOW EMERGENCY EXIT LIGHT. RE PAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996072500236 19960725 00236 NM 1996 7 25 SWAA96675 1 19960719 A 5330 SKIN BOEING 737 7372H4 138448C NM CARGO DR CUTOUT GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 56SW 21721 DURING SCHEDULED C4 CHECK, FOUND FWD CARGO DOOR CUTOUT GOUGED BEYOND SRM LIMITS. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996072500237 19960725 00237 NM 1996 7 25 SWAA96676 1 19960719 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 56SW 21721 DURING SCHEDULED C4 CHECK, FOUND LOWER FUSELAGE SKIN CRACKED FWD OF DME ANTENNA CUTOUT. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996072500238 19960725 00238 NM 1996 7 25 SWAA96677 1 19960719 A 5320 SHEAR TIE BOEING 737 7372H4 138448C NM BS 1104 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 56SW 21721 DURING SCHEDULED C4 CHECK, FOUND A .25 INCH CRACK ON BELTFRAME TO SKIN SHEAR TIE AT BS 1104, BETWEEN STRINGERS 12 AND 13 L AT LEFT SIDE OF APU. REPLACED SHEAR TIE PER BOEING SRM. 2 L 7 2 4F A16WE 1996072500239 19960725 00239 NM 1996 7 25 SWAA96678 1 19960716 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED IN RADIUS CHORD ON LEFT SIDE AT WL 195 TO 196. REPAIRED PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1996072500240 19960725 00240 NM 1996 7 25 SWAA96679 1 19960716 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 847-947.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM TO SIDEWALL SUPPORT PLATE CORRODED AT BS 847 TO 947.5, RBL 21. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996072500241 19960725 00241 NM 1996 7 25 SWAA96680 1 19960716 A 3350 23013 CHARGER BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE B L SMOKE/FUMES/ODORS/SPARKS NO TEST IN INSP/MAINT 1 SW 07 68SW 22357 AT GATE, HAD BURNT SMELL IN COCKPIT. BATTERY CHARGER C/B TRIPS AND WOULD NOT RESET. REPLACED CHARGER PER BOEING M/M. 2 L 7 2 4F A16WE 1996072500242 19960725 00242 NM 1996 7 25 SWAA96681 1 19960717 A 5320 WEB BOEING 737 7372H4 138448C NM BS 711 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AND CHAFED AT BS 711, BL 0, WL 150. REPLACED WEB AT BS 711, BL 0, WL 150 PE R BOEING SRM. 2 L 7 2 4F A16WE 1996072500243 19960725 00243 NM 1996 7 25 SWAA96682 1 19960717 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 947.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED D-CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 947.5, RBL 22, WL 178. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996072500244 19960725 00244 NM 1996 7 25 SWAA96683 1 19960717 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STRINGER 23 TO 25R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996072500245 19960725 00245 NM 1996 7 25 SWAA96684 1 19960717 A 5320 BRACKET BOEING 737 7372H4 138448C NM BS 947 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED D-CHECK, FOUND SUPPORT BRACKET CRACKED AT BS 947, BETWEEN S24 AND 25L. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996072500246 19960725 00246 NM 1996 7 25 SWAA96685 1 19960717 A 5320 CLIPS BOEING 737 7372H4 138448C NM BS 747 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 747, S18R AND AT S20R. REPLACED BOTH PER BOEING SRM. 2 L 7 2 4F A16WE 1996072500247 19960725 00247 NM 1996 7 25 SWAA96686 1 19960717 A 5320 WEB BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED D-CHECK, FOUND BS 178 PRESSURE WEB CRACKED AT WL 219, RBL 11. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996072500248 19960725 00248 NM 1996 7 25 SWAA96687 1 19960717 A 5320 WEB BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED D-CHECK, FOUND 8 CRACKS AT BS 178 PRESSURE WEB BETWEEN WL 190 AND 201, LBL 4.7. REPAIRED PER BOEING SR M. 2 L 7 2 4F A16WE 1996072500249 19960725 00249 NM 1996 7 25 SWAA96688 1 19960719 A 2910 HYD HOSE BOEING 737 7373H4 1384600 NM NLG ACTUATOR LEAKING A SWAA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 07 686SW 23175 AFTER TAKEOFF, NOSE GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO BHM AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOU ND NOSE GEAR MAIN ACTUATOR HYD HOSE LEAKING. REPLACED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996072500250 19960725 00250 NM 1996 7 25 UPS96420657 1 19960720 A 3350 FUSE BOEING 747 747SR46 NM CABIN BLOWN A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 689UP 21033 INSPECTION TYPE W/E, EMERGENCY LIGHT IN UPPER DOOR JAMB OF THE MAIN ENTRY DOOR IS INOP. REPLACED BAD FUSE IN POWER MODU LE M325, OPS CHECK GOOD PER MM 33-51-00. 2 L 7 4 4F A20WE 1996072500251 19960725 00251 WP 1996 7 25 UPS96820658 1 19960718 A 2170 22D10 COALESCER BAG DOUG DC8 DC873F 302199F WP LT PACK CONTAMINATED A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE N/A PIREP, LEFT PACK TRIPPED, RESET AND SELECTED WARMER TEMP, SELECTED LEFT PACK ON AND GOT PACK SMOKE I N COCKPIT. REPLACED CONTAMINATED COALESCER BAG IAW 21-55-03, OPS CHECK GOOD (P/N 22D10). 2 L 7 4 4F RT 4A25 1996072500252 19960725 00252 NM 1996 7 25 VSTA9607002 1 19960720 A 3520 FLOW CONTROL BOEING 737 737204 1384458 NM CABIN NOT RESET A VSTA O OTHER G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 WP 07 312VA 20236 ON CLIMBOUT, OXYGEN MASKS DROPPED WITH ACCOMPANYING PAX O2 LIGHT ILLUM, PAX O2 FLOW CONTROL UNITS NOT PROPERLY RESET AFT ER MAINTENANCE MASK DROP TEST DURING 'C' CHECK. RESET PAX O2 FLOW CONTROL UNITS, RESTOWED MASKS AND SERVICED PAX O2. 2 L 7 2 4F A16WE 1996072500253 19960725 00253 WP 1996 7 25 96003122801 1 19960206 A 5512 ALC72271 SKIN DOUG DC10 DC1030 3023501 WP HORIZ STAB CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 228NW 75849 20309 46578 CRACK 0.9 INCHES LONG AND .650 INCHES DEEP IN LEFT AFT UPPER CENTER SECTION OF HORIZONTAL STABILIZER PANEL AT HOLE NR 5 AND HOLE NR 6. CRACK IS WITHIN FLYABLE LIMITS IAW SA 42248-3. TREATED HOLE AND SURROUNDING AREAS WITH LPS 3 AND NOTIFI ED NWA ENGINEERING OF REQUIREMENT TO ESTABLISH A REPETITIVE INSPECTION AND DOCUMENTATION PROGRAM PER LACI ENGINEERING OR DER NR 3584. INSPECTION ACCOMPLISHED IAW WITH ALERT SB 55-16. MAINTENANCE ACCOMPLISHED BY LOCKHEED AEROMOD CENTER. (X ) 2 L 7 3 4F A22WE 1996072500254 19960725 00254 WP 1996 7 25 96004122802 1 19960206 A 5512 ALC72261 SKIN DOUG DC10 DC1030 3023501 WP HORIZ STAB CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 228NW 75849 20309 46578 CRACK 0.9 INCHES LONG AND .812 INCHES DEEP IN RIGHT FORWARD CENTER SECTION OF HORIZONTAL STABILIZER PANEL AT LOWER HOLE NR 6 AND NR 7. CRACK IS WITHIN FLYABLE LIMITS IAW SA 42248-3. TREATED HOLE AND SURROUNDING AREAS WITH LPS 3 AND NOTIFI ED NWA ENGINEERING OF REQUIREMENT TO ESTABLISH A REPETITIVE INSPECTION AND DOCUMENTATION PROGRAM PER LACI ENGINEERING OR DER NR 3584. INSPECTION ACCOMPLISHED IN C/W ALERT SB 55-16. MAINTENANCE ACCOMPLISHED BY LOCKHEED AEROMOD CENTER. (X) 2 L 7 3 4F A22WE 1996072500255 19960725 00255 WP 1996 7 25 96005122803 1 19960206 A 5320 SR105700227 STRAP DOUG DC10 DC1030 3023501 WP STR 41 REQUIRED REWORK A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 228NW 75849 20309 46578 WING STRINGER 41, STRAP PN SR 10570022-7, REQUIRES REWORK PER NWA ENGINEERING SKETCH SA 5711-01032-7, MACHINED ANGLE. R E-MACHINED ANGLE ON DOUBLER, PN SR 105700227, PER NWA SKETCH SA 5711-01032-7. WORK ACCOMPLISHED IN C/W SB 57-114 AND AD 94-12-05. MAINTENANCE ACCOMPLISHED BY LOCKHEED AEROMOD CENTER. (X) 2 L 7 3 4F A22WE 1996072500256 19960725 00256 WP 1996 7 25 96032122816 1 19960424 A 5730 003001001 COVER DOUG DC10 DC1030 3023501 WP LT WING CORROSION A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 228NW 75849 20309 46578 DURING CHECK, CORROSION WAS FOUND ON 5 FUEL TANK PROBE COVER PLATES ON THE MATING SURFACE. THE PART NUMBERS ARE: 003-0 01-001, 003-001-002, 003-001-006. CORROSION WAS REMOVED TO A MINIMUM THICKNESS OF 0.160 INCH TRANSITION RADIUS BETWEEN HORIZONTAL AND VERTICAL FLANGES KEPT SAME AS ORIGINAL. COVER PLATES WILL BE RE-FINIHSED. MAINTENANCE ACCOMPLISHED BY L OCKHEED AEROMOD CENTER. (X) 2 L 7 3 4F A22WE 1996072500257 19960725 00257 WP 1996 7 25 96034122818 1 19960424 A 5540 TIP DOUG DC10 DC1030 3023501 WP RUDDER LIGHTNING STRIKE A NWAA K NONE C F.O.D. IN INSP/MAINT 1 GL 01 228NW 75849 20309 46578 DURING CHECK, FOUND LIGHTNING STRIKE DAMAGE 1 INCH BY .25 INCH AT UPPER TIP OF UPPER AFT RUDDER. REMOVED DAMAGE IAW SRM 55-41-01, VOLUME III, SRM'S 51-35-01, 51-35-02, 54-41-01. MAINTENANCE ACCOMPLISHED BY LOCKHEED AEROMOD CENTER. (X) 2 L 7 3 4F A22WE 1996072500258 19960725 00258 WP 1996 7 25 96035122819 1 19960424 A 7620 148851 VALVE ASSY DOUG DC10 DC1030 3023501 WP NR 1 ENGINE LEAKING A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 228NW 75849 20309 46578 DURING CHECK, FOUND NR 1 ENGINE FIRE HANDLE HYDRAULIC SHUT-OFF VALVE LEAKS INTERNALLY. REMOVED, REPLACED, AND RIGGED NR 1 ENGINE FIRE HANDLE HYDRAULIC SHUT-OFF VALVE ASSY IAW MM 29-15-1. MAINTENANCE ACCOMPLISHED BY LOCKHEED AEROMOD CENTER . (X) 2 L 7 3 4F A22WE 1996072500259 19960725 00259 WP 1996 7 25 96ZZZX3655 1 19960525 A 2913 566411L5666 HYD PUMP DOUG DC9 DC983 3022083 WP LT ENGINE FAILED A TWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 05 9306T 49567 STL - FLT 134 - DURING CRUISE, LEFT ENGINE HYDRAULIC PUMP FAILED. AIRCRAFT RETURNED TO AIRPORT. REMOVED AND REPLACED L EFT ENGINE HYDRAULIC PUMP DUE TO A SHEARED SHAFT, MFG PN 566411L5666. OPERATIONAL CHECK NORMAL. OP-16 - 4-8-96 - TUS. 2 L 7 2 4F RT A6WE 1996072500260 19960725 00260 WP 1996 7 25 96ZZZX3656 1 19960602 A 3297 WIRE DOUG DC9 DC951 3022051 WP NLG SENSOR BROKEN A TWAA O OTHER N FALSE WARNING AP APPROACH 1 CE 05 411EA 47732 HOU - FLT 639 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, NOSE LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED. CY CLED LANDING GEAR. FOUND BROKEN WIRE AT NOSE LANDING GEAR DOWNLOCK SENSOR. MADE AIRWORTHINESS REPAIR TO WIRING. NOSE LANDING GEAR INDICATION THEN CHECKED NORMAL. CHECK C - 6-2-96 - STL. 2 L 7 2 4F RT A6WE 1996072500261 19960725 00261 NM 1996 7 25 96ZZZX3659 1 19960619 A 3350 6104781 BATTERY PACK BOEING 737 7372L9 1384497 NM CABIN DISCHARGED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 170PL 168 22733 DEN - FLT 443 - UPON ARRIVAL, FLIGHT CREW REPORTED EXTERNAL EXIT LIGHTS INOPERATIVE AT LEFT FORWARD PASSENGER DOOR AND R IGHT AFT SERVICE DOOR. MAINTENANCE REPLACED BATTERY PACKS AND LIGHT SOCKETS FOR BOTH DOORS, AND SYSTEM CHECKED OKAY. A IRFRAME, 34,084.4 HOURS. 2 L 7 2 4F RT A16WE 1996072500262 19960725 00262 NM 1996 7 25 96ZZZX3660 1 19960619 A 3350 30043213 LIGHT SOCKET BOEING 737 7372L9 1384497 NM CABIN INOPERATIVE A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 170PL 168 22733 DEN - FLT 65 - UPON ARRIVAL, FLIGHT CREW REPORTED EXTERNAL EXIT LIGHTS INOPERATIVE AT LEFT FORWARD PASSENGER DOOR AND RI GHT AFT SERVICE DOOR. MAINTENANCE REPLACED BATTERY PACKS AND LIGHT SOCKETS FOR BOTH DOORS, AND SYSTEM CHECKED OKAY. AI RFRAME, 34,084.4 HOURS. 2 L 7 2 4F RT A16WE 1996072500263 19960725 00263 1996 7 25 96ZZZX3661 4 19960608 A 2562 4523050 ELT ARTEX 1104 BEECH 1900 1900D 1154162 CE EMPENNAGE UNSECURED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 843CA 2570 53850 UE43 DURING OTHER MAINTENANCE IN EMPENNAGE, THE ELT ASSEMBLY WAS DISCOVERED UNSECURED. THE UNIT HAD BROKEN FROM ITS MOUNTING BASE AND WAS LODGED BETWEEN RIBS ADJACENT TO MOUNTING PAD. ANTENNA WAS STILL ATTACHED, BUT ELT WAS NOT OPERATIONAL. T HE MOUNTING TRAY WAS BROKEN IN NUMEROUS PIECES OF WHICH WERE LAYING LOOSE IN EMPENNAGE. 2 L 7 2 4T RT A24CE 1996072500269 19960725 00269 SO 1996 7 25 96ZZZX3672 2 19960624 A 8550 CLAMP CESSNA 206 TU206G 2073357 CE CONT O520 TSIO520M 17040 SO OIL DIPSTICK LOOSE A EW7A A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 EA 11 924JD 67 U20606317 291699R AFTER TAKEOFF, PILOT NOTICED OIL COMING OUT OF ENGINE COWLING. AFTER LANDING, FOUND OIL DIPSTICK COUPLING AND CLAMP BEC AME LOOSE FROM ENGINE CASE NIPPLE. REINSTALLED COUPLING AND SECURED CLAMP. RECLAMPED DIP STICK HOUSING WITH SMALLER AD EL CLAMPS. WASHED ENGINE AND GROUND RUN-UP OF ENGINE. NO LEAKS NOTICED. RECOMMEND AT EACH PRE-FLIGHT WHEN CHECKING OI L LEVEL, TO ALSO INCLUDE VISUAL INSPECTION OF DIPSTICK HOUSING SECURITY. AIRCRAFT TOTAL TIME 1,466.7. REFERENCE: AIR CARRIER CERTIFICATE NR EW7A379W. 1 H 7 1 3O 3 O A4CE E8CE 1996072500270 19960725 00270 NE 1996 7 25 AALA960840 2 19960529 A 7320 FFG021BH FUEL GOVERNOR WOODWARD BOEING 757 757223 1384957 NM RROYCE RB211 RB211535E4 54555 NE NR 2 ENGINE DEFECTIVE A AALA O OTHER O OTHER DE DESCENT 1 SW 07 607AM 27058 SJU - FLT 1470 - ON DESCENT TO SJU, THE NR 2 ENGINE WOULD NOT ADVANCE FROM IDLE POSITION. LANDED SJU WITHOUT INCIDENT. REPLACED NR 2 ENGINE FUEL GOVERNOR AND THROTTLE ANGLE TRANSDUCER. RAN ALL NECESSARY RUN-UP CHECKS. SYSTEM GROUND CHEC KED, NORMAL OPERATION. (X) 2 L 7 2 4F 4 F RT A2NM E12EU 1996072500271 19960725 00271 EU 1996 7 25 AALA960905 1 19960615 A 3250 201071682 CAP NUT ROTOL FOKKER F28 F28MK0100 4990807 EU NLG DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1421K 11404 ORD - DURING B-CHECK WHILE LUBRICATING NOSE LANDING GEAR, FOUND NOSE GEAR TURNING TUBE UPPER CAP NUT FAILED. THREADS RE MAINED ON TURNING TUBE, BUT NO THREADS REMAINED ON CAP NUT. REPLACED NOSE LANDING GEAR TURNING TUBE CAP NUT. SYSTEM LE AK AND GROUND CHECKED NORMAL OPERATION. (X) 2 L 7 2 4F RT 1996072500272 19960725 00272 EU 1996 7 25 AWXA960244 1 19960523 A 3350 CONNECTOR AIRBUS 320 A320231 3930325 EU CABIN LOOSE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 643AW 315 DTW - FLT 0051 - DURING ROUTINE MAINTENANCE CHECK, CREW FOUND EMERGENCY EXIT SIGN NOT ILLUMINATED. CONTRACT MAINTENANCE FOUND LOOSE CONNECTOR AND RESECURED. (X) 2 L 7 2 4F RT A28NM 1996072500273 19960725 00273 SO 1996 7 25 BUHA2396001 1 19960425 A 2910 MS21905D4 T FITTING EMB 110 EMB110P1 3260122 SO NLG CRACKED A BUHA K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 GL 23 34A 110350 LOSS OF HYDRAULIC PRESSURE DUE TO CRACKED T-FITTING. (X) 1 L 7 2 4T A21SO 1996072500274 19960725 00274 NM 1996 7 25 CAL960634 1 19960522 A 2913 6500103 HYD PUMP BOEING 737 7373T0 1384582 NM NR 1 ENGINE LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 09 19357 7069 23841 EWR - FLT 1556 - THE AIRCRAFT LOST A-SYSTEM HYDRAULIC FLUID ON APPROACH TO EWR. THE AIRCRAFT LANDED WITHOUT INCIDENT. M AINTENANCE FOUND THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP AT FAULT. THE PUMP WAS REMOVED AND REPLACED. THE ENGINE WAS RUN AND LEAK CHECK WAS GOOD. (X) 2 L 7 2 4F RT A16WE 1996072500276 19960725 00276 NM 1996 7 25 MZZA96055 1 19960606 A 5754 SKIN BOEING 727 727264 138408M NM NR 4 LE FLAP CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 622DH 20896 TNN - DURING SERVICE CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, 1 INCH LONG CRACK WAS FOUND ON RIGHT WING NR 4 LEADING ED GE FLAP INBOARD CORNER UPPER SKIN. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM 57-50-3. HANGAR NON-ROUTINE RE PAIR ITEM CARD NR 807436 (SEQ. 020). (X) 2 L 7 3 4F A3WE 1996072500277 19960725 00277 NM 1996 7 25 P91A096037 1 19960613 A 3350 BATTERY PACK GRIMES BOEING 727 727231 1384079 NM CABIN DIRTY A P9IA K NONE L NO TEST IN INSP/MAINT 1 SO 03 12305 64167 19562 AFT AIR STAIR OVERHAUL EMERGENCY LIGHT DOES NOT ILLUMINATE. CLEANED CONTACTS AT BATTERY PACK. OPS CHECKS GOOD IAW MM 3 3-50-0. (X) 2 L 7 3 4F A3WE 1996072500278 19960725 00278 EU 1996 7 25 PLGA9605301 1 19960530 A 3210 AIR127282 PIN SAAB SF340 340B 7860101 EU RT MLG CORRODED A PLGA K NONE O OTHER IN INSP/MAINT 1 NE 05 359BE 340B285 PSM - DURING A SCHEDULED LANDING GEAR INSPECTION, THE RT MLG TORQUE KNEES WERE FOUND LOOSE. DURING DISASSEMBLY, THE LOW ER PIVOT PIN WAS FOUND CORRODED. REMOVED AND REPLACED THE PIVOT PIN AND BUSHINGS AND RETURNED THE AIRCRAFT TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1996072500279 19960725 00279 EU 1996 7 25 SIMA961782 1 19960625 A 2497 WIRE AEROSP ATR42 ATR42300 8680920 EU COCKPIT FLOOR CHAFED A A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 21 251AE 250 DFW - FLT 3621 - ON APPROACH IN DFW, CREW REPORTED A POPPING SOUND FOLLOWED BY SMELL OF SMOKE AND SEVERAL TRIPPED CIRCUI T BREAKERS. AIRCRAFT LANDED NORMALLY WITHOUT INCIDENT. MAINTENANCE DISCOVERED SEVERAL CHAFED WIRES UNDER THE FLOOR BEH IND THE PILOT SEAT. MAINTENANCE WILL REPLACE A TOTAL OF 28 WIRES. INCIDENT STILL UNDER INVESTIGATION AS TO DIRECT CAUS E OF DISCREPANCY AND IF FAILURE OF COMPONENT IS IN QUESTION. AIRCRAFT REMAINS OUT OF SERVICE. (X) 2 H 7 2 4T RT A53EU 1996072500280 19960725 00280 WP 1996 7 25 WRLA96025 1 19960612 A 2760 AYG70915505 MIXER BRACKET DOUG DC10 DC1030 3023501 WP RT SPOILERS LACK OF LUBE A WRLA H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED DE DESCENT 1 EA 27 9MMAV 48283 DURING INITIAL DESCENT WHEN FLIGHT CREW DEPLOYED SPEED BRAKE, AIRCRAFT HAD TENDENCY TO ROLL TO THE RIGHT. SITUATION WAS CORRECTIBLE WITH NORMAL FLIGHT CONTROL INPUT. AIRCRAFT CONTINUED TO DESTINATION, LANDED WITHOUT FURTHER INCIDENT. MAI NTENANCE PERSONNEL FOUND NRS 1, 4, AND 5 RIGHT SPOILERS DID NOT COMPLETELY DEPLOY ON AILERON OPERATION. CHECKED INTEGRI TY OF PULLEYS, CABLES, AND QUADRANTS TO AFFECTED SPOILERS. FOUND ALL ITEMS NORMAL. CLEANED AND LUBED SPOILERS QUADRANT S. GROUND CHECKED OK. AIRCRAFT RETURNED TO SERVICE. NOTE: AIRCRAFT HAS FLOWN 5 FLIGHTS WITH NO RECURRENCE OF THIS EV ENT. (X) 2 L 7 3 4F A22WE 1996072500281 19960725 00281 1996 7 25 HEEA967565 4 19960710 A 2312 064105430 TRANSCEIVER BELL 206 206L1 1182107 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5007Q 45187 STANDBY LED DIGITS NOT ALL LIGHTING UP. 1 G 7 1 3U H2SW 1996072500282 19960725 00282 1996 7 25 HEEA967566 4 19960710 A 3444 066104800 ALTIMETER KRA405 BOLKMS 117 BK117B1 5626012 EU COCKPIT RAD ALT ERRATIC E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 911TL 7198 ERRATIC RADAR ALT. OPERATION AT ZERO AND ABOVE 2000FT. RESOLDERED ALL WIRES GOING TO STRIP LINE ASSEMBLY. REPAIRED PROB LEM. VIBRATED AND COOKED UNIT TO VERIFY NEEDLE STABILITY. REPLACED BROKEN CAPACITOR C701. REPLACED RESISTORS R518,R51 9,R534 AND R260 TO INCORPORATE MOD 10. BENCH CHECK GOOD. 1 G 7 2 3U H13EU 1996072500283 19960725 00283 1996 7 25 HEEA967567 4 19960710 A 2312 064105430 TRANSCEIVER BOLKMS 117 BK117B1 5626012 EU COCKPIT VHF DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 911TL 7198 MHZ, KHZ FREQUENCY, TRANSFER FREQUENCY AND CHANNEL FREQUENCY UNABLE TO CHANGE. 1 G 7 2 3U H13EU 1996072500284 19960725 00284 1996 7 25 HEEA967569 4 19960710 A 2210 2593996333 TARSYN BELL 412 412 1182202 SW AUTO FLIGHT MALFUNCTION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 107X 33113 TARSYN WON'T SLAVE AND PRECESSES CONSTANTLY. TIME SINCE REPAIR 489:10. 1 G 7 2 4U H4SW 1996072500285 19960725 00285 1996 7 25 HEEA967571 4 19960710 A 3457 0110005400 GPS 150 BELL 206 206L1 1182107 SW COCKPIT GPS FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 22425 45743 GPS WILL NOT FIND SATELLITES. 1 G 7 1 3U H2SW 1996072500286 19960725 00286 SW 1996 7 25 HEEA967576 1 19960710 A 2730 206001191001 TUBE ASSY BELL 206 206L3 1182108 SW ELEV CONTROL CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8588X 51486 TUBE ASSY IS CRACKED. (CRACKS AT CLEVIS END. THREE EACH CRACKS .420" - .515" AND .590" LONG AT CLEVIS END OF TUBE. 1 G 7 1 3U H2SW 1996072500287 19960725 00287 SW 1996 7 25 HEEA967577 1 19960710 A 3213 AB205050403031 CROSSTUBE BELL 412 412 1182202 SW MLG DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 1273 36002 DAMAGE TO AREAS OF CROSSTUBE NOT ALLOWED AS PER BHT 412- CR&O-2 CHAP. 32, FIGURE 32-1, PAGE 7. SENT TO AIRBORNE SUPPLY, INC. FOR WARRANTY REPAIR OR EXCHANGE. 1 G 7 2 4U H4SW 1996072500288 19960725 00288 SW 1996 7 25 HEEA967578 1 19960710 A 5510 206023119151 STABILIZER ASSY BELL 206 206L1 1182107 SW HORZ STAB MIS MFG E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 STABILIZER IS TOO THICK. WILL NOT ALIGN TO STABILIZER SUPPORTS THAT ATTACH TO TAILBOOM. 1 G 7 1 3U H2SW 1996072500289 19960725 00289 SW 1996 7 25 HEEA967579 1 19960710 A 5510 206023119151 STABILIZER ASSY BELL 206 206L1 1182107 SW HORZ STAB MIS MFG E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 STABILIZER INSERTS FOR L/H AND R/H TAILBOOM ATTACHMENT SUPPORTS MISLOCATED. (INSTALLED TOO FAR OFF) 1 G 7 1 3U H2SW 1996072500290 19960725 00290 EU 1996 7 25 HEEA967581 1 19960710 A 2822 P94B12208 PUMP,FUEL SNIAS 350 AS350B2 8680813 EU RT BOOST DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 60951 2771 WHEN RIGHT HAND BOOST PUMP IS TURNED ON, FUSE BLOWS. 1 G 7 1 3U H9EU 1996072500291 19960725 00291 GL 1996 7 25 HEEA967582 2 19960716 A 7250 6886407 WHEEL 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL 1ST STAGE DEFECTIVE E HEEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 03 721MB 750 CAT30507F S752 CAE830726 ENGINE REMOVED DUE TO SMOKE ON SHUTDOWN. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: MINOR SULFIDATION ON AL L 1ST STAGE WHEEL BLADES. SCRAPPED 1ST STAGE WHEEL. 1 G 7 2 3U 3 U H3EU E4CE 1996072500292 19960725 00292 GL 1996 7 25 HEEA967583 2 19960716 A 7250 6886407 WHEEL 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL 1ST STAGE DEFECTIVE E HEEA K NONE R PARTIAL RPM/PWR LOSS IN INSP/MAINT 1 SW 03 50293 1358 CAT32263F S677 CAE821629F ENGINE REMOVED DUE TO LOW POWER. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: MINOR SULFIDATION ON ALL 1ST ST AGE WHEEL BLADES. SCRAPPED 1ST STAGE WHEEL. 1 G 7 2 3U 3 U H3EU E4CE 1996072500293 19960725 00293 GL 1996 7 25 HEEA967584 2 19960716 A 7250 6886407 WHEEL 6898735 AEROSP AS355 AS355F2 8680812 EU ALLSN 250C 250C20F 03013 GL 1ST STAGE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6040U 914 CAT33145 5474 CAE840099 ENGINE REMOVED DUE TO HIGH OIL CONSUMPTION. UPON INSPECTION OF TURBINE PARTS DUE TO LOW POWER ON TEST CELL NOTED THE FO LLOWING: ONSET OF SULPHIDATION ON 20 EACH 1ST STAGE WHEEL BLADES AND CRACKED IN RIM AREA. SCRAPPED 1ST STAGE WHEEL. 1 G 7 2 3U 3 U H11EU E4CE 1996072500294 19960725 00294 SW 1996 7 25 HEEA967585 1 19960716 A 6710 214001371102 BELLCRANK ASSY BELL 214 214ST 1182106 SW M/R CONTROL DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 BEARING BORES WHERE BEARING P/N MS27641-5 ARE INSTALLED ARE MISALIGNED AND BOLT MUST BE HAMMERED IN AND IS SCORED WHEN I NSTALLED. 2 G 7 2 4U H10SW 1996072500295 19960725 00295 EU 1996 7 25 HEEA967586 1 19960716 A 2840 DK040 TRANSMITTER BOLKMS 105 BO105S 5626006 EU FUEL SYS DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 TRANSMITTER BENCH CHECK BAD. DOES NOT DROP TO ZERO AFTER INITIAL RUNUP. ALSO FLUCTUATES. MANUFACTURED IN 1995. 1 G 7 2 3U H3EU 1996072500296 19960725 00296 NE 1996 7 25 9615666729 2 19960720 A 7230 COMPRESSOR BOEING 747 747251F 1384898 NM PWA JT9 JT9D7F 52054 NE NR 4 ENGINE STALLED A NWAA E D ENGINE SHUTDOWN RETURN TO BLOCK J R WARNING INDICATION PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 GL 01 629US 22388 62905 WHILE WAITING FOR TAKEOFF, THE NR 4 ENGINE EXPERIENCED A SILENT COMPRESSOR STALL. AS EGT ROSE TO 950 DEGREES AND OIL PR ESSURE LOW LIGHT ILLUMINATED, CREW FOLLOWED COCKPIT OPERATING PROCEDURE, SHUT DOWN THE ENGINE, AND RETURNED TO THE GATE. MAINTENANCE PERFORMED FIRST STALL PROCEDURE PER MAINTENANCE MANUAL AND NO DISCREPANCIES WERE NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4 F A20WE E20EA 1996072500297 19960725 00297 NM 1996 7 25 9615672702 1 19960722 A 2131 7612608 CONTROLLER BOEING 727 727225 1384077 NM CABIN MALFUNCTIONED A NWAA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 GL 01 8877Z 2561 2561 21450 DURING CLIMBOUT ABOVE 10,000 FEET, UNABLE TO CONTROL CABIN ALTITUDE IN EITHER AUTO OR STANDBY. AIRCRAFT RETURNED TO MSP , FUEL WAS DUMPED, AND LANDED WITHOUT INCIDENT. REPLACED CABIN AUTO PRESSURE CONTROLLER AND PERFORMED OPERATIONAL CHECK . CHECKED OK. ALSO PRESSURIZED AIRFRAME AND CHECKED FOR LEAKS. 2 L 7 3 4F A3WE 1996072500299 19960725 00299 WP 1996 7 25 9615699944 1 19960717 A 7931 OIL PRES REG VLV DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9A 52048 NE LT ENGINE MALFUNCTIONED A NWAA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 GL 01 1309T 47316 666905 DURING DESCENT, THE LEFT ENGINE OIL PRESSURE DECREASED TO 20 PSI AND LOW OIL PRESSURE LIGHT ILLUMINATED. FOLLOWED COCKP IT OPERATING MANUAL PROCEDURES AND PERFORMED A PRECAUTIONARY SHUTDOWN OF LEFT ENGINE. AIRCRAFT CONTINUED TO ORIGINAL DE STINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE OIL PRESSURE REGULATOR VALVE AND OIL FILTER . LEAK AND OPERAITONAL CHECK OK. 2 L 7 2 4F 4 F A6WE E2EA 1996072500300 19960725 00300 WP 1996 7 25 9615709956 1 19960720 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 923RW 47183 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD AND MID-CABIN FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES AND POWER SUPPLIES. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996072500301 19960725 00301 WP 1996 7 25 9615719967 1 19960720 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9331 47263 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. OPERATION AL CHECK NORMAL. 2 L 7 2 4F A6WE 1996072500302 19960725 00302 WP 1996 7 25 9615729975 1 19960719 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9339 47382 DURING PRE-FLIGHT CHECK, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. MAINTENANCE REPAIRED AND RE-POSITIONED WIRE UNDER SEAT 3C. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996072500303 19960725 00303 WP 1996 7 25 9615739609 1 19960721 A 3350 6011779 BATTERY PACK DOUG DC9 DC932 3022066 WP LT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 609NW 47234 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996072500304 19960725 00304 WP 1996 7 25 9615749971 1 19960717 A 3350 60030451 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9335 47337 DURING LINE MAINTENANCE INSPECTION, FOUND AFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACKS. OPER ATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996072500305 19960725 00305 WP 1996 7 25 9615759609 1 19960717 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP COCKPIT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 609NW 47234 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS IN COCKPIT WOULD NOT TEST. REPLACED BATTERIES. OPE RATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996072500306 19960725 00306 WP 1996 7 25 9615769613 1 19960721 A 3320 BALLAST DOUG DC9 DC932 3022066 WP CABIN FAILED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 613NW 47438 DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT SIDEWALL LIGHTS FLICKERING IN BRIGHT AND DIM SETTINGS. MAINTENANCE FOUN D RIGHT SIDEWALL LIGHT BALLAST IN FORWARD CABIN WITH BURNT CONTACTS. ALSO, FOUND AFT PINS IN WIRE HARNESS BURNT. DEACT IVATED SIDEWALL LIGHTS PER FC 3320-01067 AND DEFERRED PER MEL 33-2. 2 L 7 2 4F A6WE 1996072500307 19960725 00307 WP 1996 7 25 9615779940 1 19960718 A 2131 CONTROLLER DOUG DC9 DC932 3022066 WP CABIN MALFUNCTIONED A NWAA B EMER. DESCENT J WARNING INDICATION DE DESCENT 1 GL 01 3322L 47031 LOSS OF CABIN PRESSURIZATION OCCURRED DURING INITIAL DESCENT AT 31,000 FEET. EMERGENCY DESCENT WAS MADE TO 10,000 FEET AND CABIN PRESSURE WAS REGAINED. FLIGHT CONTINUED TO DESTINATION WITHOUT FURTHER INCIDENT. AN UNEVENTFUL LANDING WAS A CCOMPLISHED. REPLACED CABIN PRESSURE CONTROLLER AND RESECURED LOOSE DUCT AT RIGHT ACM. OPERATIONAL CHECK NORMAL ON CAB IN PRESSURE CHECK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996072500308 19960725 00308 WP 1996 7 25 9615789860 1 19960718 A 2150 ACM DUCT DOUG DC9 DC951 3022051 WP LEFT LOOSE A NWAA G B O2 MASK DEPLOYED EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 01 769NC 47757 LOSS OF CABIN PRESSURIZATION OCCURRED DURING CRUISE FLIGHT AT 28,000 FEET. OXYGEN MASKS WERE AUTOMATICALLY DEPLOYED THR OUGHOUT THE CABIN AND EMERGENCY DESCENT WAS MADE TO 10,000 FEET. PRESSURE WAS REGAINED AND AIRCRAFT CONTINUED TO DESTIN ATION. AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE FOUND DUCT AND CLAMP LOOSE AT LEFT ACM AND DOWNSTREAM OF WA TER SEPARATOR. RESECURED DUCT AND CLAMP. OPERATIONAL CHECK NORMAL ON CABIN RPESSURE CHECK. AIRCRAFT RETURNED TO SERVI CE. 2 L 7 2 4F A6WE 1996072500309 19960725 00309 NM 1996 7 25 96FDEA01266 1 19960720 A 2613 OVERHEAT LIGHT BOEING 727 727225 1384077 NM NR 1 ENG STRUT ILLUMINATED A FDEA O OTHER N FALSE WARNING TO TAKEOFF 1 SO 25 464FE 21288 DISCREPANCY: (MOCC 96-137) NR 1 ENGINE STRUT OVERHEAT ILLUMINATED MOMENTARILY ON TAKEOFF. EXTINGUISHED WHEN POWER WAS REDUCED TO QUIET EPR. SYSTEM TESTED OK. CORRECTIVE ACTION: INSPECTED NR 1 ENGINE STUB WING DUCTING FOR LEAKS, NO DEFE CTS NOTED, OK FOR SERVICE. 2 L 7 3 4F A3WE 1996072500310 19960725 00310 WP 1996 7 25 96FDEA01267 1 19960719 A 2740 CHECK VALVE DOUG DC10 DC1010CF 3023502 WP STAB CONTL BROKEN A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 68049 47803 DISCREPANCY: (MOCC 96-138) DURING LEVEL FLIGHT AT 27,000 FEET, NR 1 HYDRAULIC QUANTITY WENT TO ZERO. ACCOMPLISHED APPR OPRIATE CHECK LIST. CORRECTIVE ACTION: FOUND NR 2 STABILIZER CONTROL VALVE CHECK VALVE BROKEN. REMOVED AND REPLACED C HECK VALVE, MOA FILTERS, AND ENGINE NR 1 HYDRAULIC PUMP. 2 L 7 3 4F RT A22WE 1996072500311 19960725 00311 WP 1996 7 25 96FDEA01268 1 19960708 A 5412 BLKHD STIFFENER DOUG DC10 DC1010CF 3023502 WP NR 2 ENGINE CRACKED A FDEA K NONE O OTHER CR CRUISE 1 SO 25 68056 47810 DISCREPANCY: NR 2 ENGINE NOSE COWL BLKHD STIFFENER ON D-DUCT WEB CRACKED AT 10 O'CLOCK POSITION. REFERENCE: FCD 08-55 -005 SNRM 4225. CORRECTIVE ACTION: REMOVED STIFFENER, WELDED CRACK, AND RE-INSTALLED STIFFENER PER SRM 57-00-00. 2 L 7 3 4F RT A22WE 1996072500312 19960725 00312 NM 1996 7 25 96FDEA01269 1 19960719 A 5315 BAC1518338 FLOOR BEAM BOEING 727 72725C 138400H NM BS 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 116FE 19298 DISCREPANCY: (NR 1123) FLOORBEAM CORRODED UPPER CHORD STA 400, LBL 32-41 (MAIN CARGO). CORRECTIVE ACTION: REMOVED DAM AGED SECTION OF UPPER CHORD. INSTALLED FLOORBEAM REPAIR PER SRM 53-10-8, FIG 3. 2 L 7 3 4F A3WE 1996072500313 19960725 00313 NM 1996 7 25 96FDEA01270 1 19960717 A 5313 6561477 STRINGER BOEING 727 7272D4 138407U NM BS 680 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 287FE 21849 DISCREPANCY: (NR 0383)(019) CORROSION (C53-113-01) IN THE FORWARD CARGO BAY ON STR 28R, BS 680, WL 148. CORRECTIVE AC TION: *****S/D******* COMING. 2 L 7 3 4F A3WE 1996072500314 19960725 00314 NM 1996 7 25 96FDEA01271 1 19960719 A 5711 65185384 CTR WING SPAR BOEING 727 7272D4 138407U NM BS 866 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 181FE 21849 NR0702 AND 703, CORROSION CTR WING TANK, STA 866 SPAR AND UPPER CHORD CORRODED FROM LBL 50 TO RBL 50. *S/D* REMOVED AN D REPLACED REAR SPAR UPPER CHORD PER 51-40-4 FIG 1 AND EA 7-5710-28808. 2 L 7 3 4F A3WE 1996072500315 19960725 00315 NM 1996 7 25 96FDEA01272 1 19960719 A 2810 65185373 CTR WING TANK BOEING 727 7272D4 138407U NM BS 866 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 181FE 18868 DISCREPANCY: (NR 0701 ) CORROSION CENTER WING TANK, STA 866 SPAR AND LOWER CHORD CORRODED FROM LBL 20 TO RBL 50. COR RECTIVE ACTION: REMOVED CORROSION FROM LOWER CHORD AND INSTALLED REPAIR PER EA 7-5710-28806. 2 L 7 3 4F A3WE 1996072500316 19960725 00316 NM 1996 7 25 96FDEA01273 1 19960706 A 5315 652082735 FLOORBEAM BOEING 727 72722 1384002 NM BS 540 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 DISCREPANCY: (NR 0743 (035) WHILE WORKING 0251, FOUND CORROSION ON FLOORBEAM LOWER CHORD BS 540 LBL 14 TO RBL 23 WL 200 . CORRECTIVE ACTION: REPAIRED FLOORBEAM LOWER CHORD BS 540 LBL 14 - RBL 23 WL 200 PER FEDEX SRM 53-10-8. 2 L 7 3 4F A3WE 1996072500317 19960725 00317 NM 1996 7 25 96FDEA01274 1 19960721 A 5330 6518386109 SKIN BOEING 727 727173C 1384059 NM BS 1156 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 199FE 19509 DISCREPANCY: (NR 0132) (18) SKIN DOUBLER IS DELAMINATED AT BS 1156, RBL 31, WL 158, BETWEEN STR 25R AND STR 26R. CORRE CTIVE ACTION: REMOVED AND REPLACED SKIN PANEL IAW FEDEX EA 7-5330-29608. 2 L 7 3 4F A3WE 1996072500318 19960725 00318 NM 1996 7 25 96FDEA01275 1 19960721 A 5330 65207282 FRAME BOEING 727 72722 1384002 NM BS 1057.5 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 NR 0321, 037 CORROSION (C53-113-01) AND CRACK AT PREVIOUS REPAIR FRAME AT BS 1057.5 RBL. *S/D* REMOVED AND REPLACED 10 57.6 MAIN FRAME RT SIDE, PER FEDEX SRM 53-10-2 AND BOEING DRAWING 65-20728. 2 L 7 3 4F A3WE 1996072500319 19960725 00319 NM 1996 7 25 96FDEA01276 1 19960721 A 5311 651634430 FRAME BOEING 727 72722 1384002 NM BS 1070 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 DISCREPANCY: (NR 0316)(036) CRACK IN FRAME AT BS 1070, LBL 37, WL 153 ABOVE STR 25L. CORRECTIVE ACTION: *****S/D ** ** COMING. 2 L 7 3 4F A3WE 1996072500320 19960725 00320 NM 1996 7 25 96FDEA01277 1 19960721 A 5754 652163475 SKIN BOEING 727 7272D4 138407U NM LT TE AFT FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 DISCREPANCY: (NR 0026)(O01) LEFT WING INBOARD AFT FLAP IS DELAMINATING ALONG 0113 EDGE UPPER AND LOWER SURFACES. CORRE CTIVE ACTION: ****S/D****** COMING. 2 L 7 3 4F A3WE 1996072500321 19960725 00321 NM 1996 7 25 96FDEA01278 1 19960721 A 5753 652163223 TE WEDGE BOEING 727 7272D4 138407U NM LT TE MID FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 DISCREPANCY: (NR 0027)(O02) LEFT WING INBOARD MID-FLAP TRAILING EDGE WEDGE IS DELAMINATED 6 INCHES FROM INBOARD END UP PER SURFACE. CORRECTIVE ACTION: ****S/D****** COMING. 2 L 7 3 4F A3WE 1996072500322 19960725 00322 NM 1996 7 25 96FDEA01279 1 19960722 A 5330 6516306 SKIN BOEING 727 7272D4 138407U NM BS 267 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 287FE 21849 DISCREPANCY: NR 0103 (20) SKIN DENT BS 267, WL 152, RBL 24. OUT OF LIMITS SRM 53-30-1. CORRECTIVE ACTION: REPAIRED S KIN DENT AT BS 267, WL 152, RBL 24, PER FEDEX SRM 53-30-3. 2 L 7 3 4F A3WE 1996072500323 19960725 00323 NM 1996 7 25 96FDEA01280 1 19960722 A 5720 6516325 CHORD BOEING 727 7272D4 138407U NM BS 760 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 287FE 21849 DISCREPANCY: NR 0305 (21) CRACK IN PLUS CHORD AT BS 760, LBL 70.5, WL 205. CORRECTIVE ACTION: *****S/D *****COMING. 2 L 7 3 4F A3WE 1996072500324 19960725 00324 NM 1996 7 25 96FDEA01281 1 19960723 A 5314 KEEL BEAM BOEING 747 747245F 1384897 NM BS1288 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 641FE 20827 SIN: BS 1288 L/H KEEL BEAM LOWER CHORD FOUND CORRODED AFTER CORROSION BLEND OUT. MATERIAL REMOVED 0.110 OUT OF SRM LI MIT. CHORD ORIGINAL THICKNESS 0.250. ****S/D***** REPAIRED CARRIED OUT AS PER FEDEX ENGINEERING REPAIR AUTHORIZATION ERA # B53-10-336. 2 L 7 4 4F A20WE 1996072500325 19960725 00325 SO 1996 7 25 BIER960034 1 19960723 A 6120 LW1009885 DIFF PRES CNTRL PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA RT ENGINE INOPERATIVE B BIEA K NONE R PARTIAL RPM/PWR LOSS CR CRUISE 1 EA 21 27508 348 348 317852031 L267568A MANIFOLD PRESSURE FOLLOWED PROPELLER PITCH ADJUSTMENT, MAXIMUM PRESSURE OK ON TAKEOFF, BUT DID NOT MAINTAIN CONSTANT MP IN-FLIGHT. FOUND DIFFERENTIAL PRESSURE CONTROLLER TO BE INOPERATIVE. 1 L 7 2 3O 3 O A20SO E14EA 1996072500326 19960725 00326 NM 1996 7 25 CALA9601046 1 19960719 A 3340 300909103 STROBE LIGHT BOEING 737 737291 138448W NM TAIL SECTION LIGHTNING STRIKE A CALA A UNSCHED LANDING B C SMOKE/FUMES/ODORS/SPARKS F.O.D. CR CRUISE 1 SW 09 15255 13326 12204 21069 THE AIRCRAFT WAS STRUCK BY LIGHTNING WHILE AT FL 210 EN ROUTE FROM RDU TO EWR. THE COCKPIT FILLED WITH SMOKE AND A LOUD POP WAS HEARD. THE EXTERNAL LIGHT CIRCUIT BREAKER HAD VISIBLE FLAMES MOMENTARILY AND HAD TRIPPED AND MELTED. BOTH COC KPIT SMOKE HOODS WERE USED, AIRCRAFT WAS DIVERTED TO BWI AND LANDED WITHOUT INCIDENT. INSPECTION PER MM 05-51-151 FOUND THE AFT STROBE LIGHT HAD BEEN STRUCK AND THE RUDDER HAD A BURNED OUT RIVET AND BURNED PAINT. THE BURNED CIRCUIT BREAKE R WAS REPLACED. THE AFT STROBE LIGHT WAS REPLACED AND A NEW WIRE AND PIN FROM J-CANNON PLUG TO GROUND WAS INSTALLED IAW MM 33-40-03. SPEED TAPE WAS APPLIED OVER THE MISSING RIVET. PART TC, 10,152. 2 L 7 2 4F A16WE 1996072500327 19960725 00327 NE 1996 7 25 CALA9601047 2 19960722 A 7530 790762 STATOR SUPPT DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 2 ENGINE BROKEN A CALA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SW 09 937MC 23486 3089 49450 717439 THE NR 2 ENGINE COMPRESSOR BEGAN TO STALL AFTER TAKEOFF AT 13,000 FEET. THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDE D WITHOUT INCIDENT. INSPECTION BY MAINTENANCE FOUND DAMAGE TO THE NR 2 ENGINE 13TH STAGE COMPRESSOR. THE NR 2 ENGINE W AS REMOVED AND REPLACED. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION. *S/D* SHOP FINDINGS REV EALED AN 8TH STAGE STATOR SUPPORT (SHELF) BROKEN. 2 L 7 2 4F 4 F A6WE E9NE 1996072500328 19960725 00328 NE 1996 7 25 CKSA96075 2 19960722 A 7313 MS919806 FUEL NOZZEL FTG BOEING 747 747146 NM PWA JT9 JT9D7A 52054 NE NR 3 ENGINE LOOSE A CKSA F ACTIVATE FIRE EXT. J WARNING INDICATION CL CLIMB 1 GL 23 702CK 20332 662521 VHHH-FLT NR 77068: FULL FIRE WARNING ON NR 3 ENGINE. BOTH FIRE BOTTLES DISCHARGED. INSPECTED NR 3 ENGINE. FOUND LOOS E FITTING ON FUEL NOZZLE AND BLOWN SEAL AT PRECOOLER DUCT COUPLING. RETORQUED AND SEALED AT PRECOOLER DUCT COUPLING - E DP FILTER CARTRIDGE MAGNETIC PLUG INSPECTION SATISFACTORY - RE-PROTECTED ADJACENT ELECTRICAL WIRES. LEAK CHECK OK AT FU EL NOZZLE FITTING DURING ENGINE RUN-UP. NR 3 ENGINE OK FOR SERVICE. REMOVED AND REPLACED LT AND RT NR 3 ENGINE FIRE EXT INGUISHING BOTTLE AND SQUIB CARTRIDGE IAW MM 26-21-03, PAGE 401. 2 L 7 4 4F 4 F A20WE E20EA 1996072500329 19960725 00329 SO 1996 7 25 COMA9610228 1 19960722 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 248CA 12000 1000 120228 EMERGENCY LIGHTING IS INOPERATIVE. REPLACED THE EMERGENCY LIGHTING BATTERIES. PART TOTAL CYCLES, 11,500. 2 L 7 2 4T RT A31SO 1996072500330 19960725 00330 SO 1996 7 25 COMA9610229 1 19960721 A 7603 0881824 SOLENOID EMB 120 EMB120RT SO LT NACELLE FAILED A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 266CA 120258 LEFT POWER LEVER, FLIGHT IDLE STOP SOLENOID CIRCUIT BREAKER, TRIPPED. REPLACED THE FLIGHT IDLE STOP SOLENOID. 2 L 7 2 4T RT A31SO 1996072500331 19960725 00331 WP 1996 7 25 MWEA96266 1 19960722 A 3350 60030451 POWER SUPPLY DOUG DC9 DC915 3022036 WP CABIN INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 300ME 45718 DURING INSPECTION, FOUND EMERGENCY CEILING LIGHTS STAY ON WHEN AIRCRAFT POWER IS TURNED OFF. REPLACED EMERGENCY CEILING LIGHT BATTERY PACK. OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996072500332 19960725 00332 NM 1996 7 25 P5CA9600390 1 19960722 A 5400 DOUBLER BOEING 747 747124 1384874 NM NR 4 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 CRACKED DOUBLER ON NR 4 PYLON LEFT SIDE AFT OF REAR MOUNT AREA. REMOVED DOUBLER, FABRICATED, AND INSTALLLED NEW DOUBLER PER BOEING SRM 54-10-03. 2 L 7 4 4F A20WE 1996072500333 19960725 00333 NM 1996 7 25 P5CA9600391 1 19960722 A 3610 65B401551 DUCT BOEING 747 747124 1384874 NM NR 4 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 CRACKED PNEUMATIC DUCT NR 4 PYLON BY T-CONNECTION FOR PRESSURE ANTICIPATOR ASSEMBLY. REMOVED AND REPLACED DUCT PER BOEI NG MAINTENANCE MANUAL 36-11-01. 2 L 7 4 4F A20WE 1996072500334 19960725 00334 WP 1996 7 25 SCNA96197 1 19960719 A 3350 110049 POWER SUPPLY DOUG DC10 DC1010 3022110 WP CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 572SC 46977 FOUND MID-CABIN RIGHT EMERGENCY FLOOR LIGHT INOPERATIVE. REMOVED AND REPLACED MID-GALLEY EMERGENCY LIGHT BATTERY POWER SUPPLY (P/N 11-0049, S/N 1970) AND BATTERY ASSEMBLY (P/N 2D131A, S/N 43604). OPS CHECK GOOD IN ACCORDANCE WITH 33-51-0 1. 2 L 7 3 4F A22WE 1996072500335 19960725 00335 NM 1996 7 25 SCNA96198 1 19960716 A 3350 1864 LAMP BOEING 727 7272A1 138407F NM OVHD PANEL INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 286SC 21601 FOUND EMERGENCY LIGHTS DISARM AMBER LIGHT INOP. REMOVED AND REPLACED LAMP, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1996072500336 19960725 00336 NM 1996 7 25 SCNA96199 1 19960719 A 3350 328 LAMP BOEING 727 7272J4 1384006 NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 288SC 20765 FOUND RIGHT SERVICE DOOR OVERHEAD EXIT SIGN LIGHTS INTERMITTENT. RELAMPED AND OPS CHECKED NORMAL. 2 L 7 3 4F RT A3WE 1996072500337 19960725 00337 NM 1996 7 25 SCNA96200 1 19960719 A 3350 328 LAMP BOEING 727 7272J4 1384006 NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 288SC 20765 FOUND LEFT FORWARD OVERWING EXIT SIGN INTERMITTENT. RELAMPED AND OPS CHECKED NORMAL. 2 L 7 3 4F RT A3WE 1996072500338 19960725 00338 NM 1996 7 25 SWAA960689 1 19960718 A 2751 WIRE BOEING 737 7373H4 1384600 NM NR 1 TE FLAP BROKEN A SWAA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SW 07 373SW 26581 AFTER TAKEOFF, NR 1 T/E FLAP TRANSIT LIGHTS (FWD AND OVERHEAD) REMAINED ILLUMINATED. AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. INSPECTED AND REPAIRED BROKEN GROUND LUG WIRE PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996072500339 19960725 00339 NM 1996 7 25 SWAA960690 1 19960719 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 470 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 470, BETWEEN S23 AND 22L. INSTALLED DOUBLER REPAIR PER BOEIN G SRM. 2 L 7 2 4F RT A16WE 1996072500340 19960725 00340 NM 1996 7 25 SWAA960691 1 19960719 A 5315 FLOOR BEAM BOEING 737 7372H4 138448C NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 89SW 22904 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 986, RBL 5. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996072500341 19960725 00341 NM 1996 7 25 SWAA960692 1 19960719 A 5320 CHORD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 89SW 22904 DURING SCHEDULED 1/2 D-CHECK, FOUND CHORD CRACKED AT BS 178 BULKHEAD AT LBL 5.7. REPAIRED PER BOEING SRM AND T1-253-031 . 2 L 7 2 4F A16WE 1996072500342 19960725 00342 NM 1996 7 25 SWAA960693 1 19960719 A 5320 WEB BOEING 737 7372H4 138448C NM BS 1000 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 89SW 22904 DURING SCHEDULED 1/2 D-CHECK, FOUND WEB UNDER AFT GALLEY CORRODED AROUND NUTPLATE AT BS 1000, RBL 44. REPLACED WEB PER BOEING SRM. 2 L 7 2 4F A16WE 1996072500343 19960725 00343 NM 1996 7 25 SWAA960694 1 19960719 A 5320 ANGLE BOEING 737 7372H4 138448C NM FWD SERV CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 89SW 22904 DURING SCHEDULED 1/2 D-CHECK, ANGLE BELOW S13R FORWARD OF FORWARD SERVICE DOOR CRACKED AT AFT END. REPLACED ANGLE PER B OEING SRM. 2 L 7 2 4F A16WE 1996072500344 19960725 00344 NM 1996 7 25 SWAA960695 1 19960719 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 1006 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 89SW 22904 DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER 26R CORRODED AT BS 1006. REPLACED STRINGER SECTION PER BOEING SRM. 2 L 7 2 4F A16WE 1996072500345 19960725 00345 NM 1996 7 25 SWAA960696 1 19960718 A 5330 SKIN BOEING 737 7373A4 1384585 NM BS 1183 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 680AA 23505 DURING SCHEDULED B/C1 CHECK, FOUND FUSELAGE SKIN CRACKED 8 INCHES BELOW BS 1183. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996072500346 19960725 00346 NM 1996 7 25 SWAA960697 1 19960718 A 5330 CUTOUT BOEING 737 7373A4 1384585 NM FWD GALLEY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 680AA 23505 DURING SCHEDULED B/C1 CHECK, FOUND FORWARD GALLEY DOOR UPPER AND LOWER HINGE CUT-OUTS CRACKED .25 INCH. REPAIRED PER SW A RA 1-352-0251. 2 L 7 2 4F RT A16WE 1996072500347 19960725 00347 NM 1996 7 25 SWAA960698 1 19960718 A 5320 FRAME BOEING 737 7372H4 138448C NM FWD ENTRY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING WALKAROUND CHECK, FOUND FORWARD ENTRY FRAME CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996072500348 19960725 00348 NM 1996 7 25 SWAA960699 1 19960720 A 3231 LINKAGE BOEING 737 7373H4 1384600 NM NLG DOOR MISADJUSTED A SWAA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 604SW 27955 AFTER TAKEOFF, WHEN GEAR RETRACTED, NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED. RECYCLED GEAR AND RECEIVED SAME INDICA TION. VISUALLY CHECKED NOSE GEAR, UP AND LOCKED. LANDED AT STL WITHOUT INCIDENT, ADJUSTED NLG DOOR LINKAGE AND PERFORME D GEAR RETRACTION TEST PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996072500349 19960725 00349 NM 1996 7 25 SWAA960700 1 19960719 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 277 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 55SW 21593 DURING SCHEDULED B2 CHECK, FOUND FRAME-TO-FRAME INTERCOSTAL CRACKED AT BS 277, AT S14R. REPLACED FRAME PER BOEING SRM. 2 L 7 2 4F A16WE 1996072500350 19960725 00350 NM 1996 7 25 SWAA960701 1 19960719 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 178, WL 234, RBL 10 AROUND FASTENER HEAD. INSTALLED DOUBLER REPAIR PER BOEING SRM. 2 L 7 2 4F A16WE 1996072500351 19960725 00351 NM 1996 7 25 SWAA960702 1 19960721 A 2910 BACH8B04NM0166T LINE BOEING 737 7373H4 1384600 NM NLG WW RUPTURED A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 686SW 23175 AFTER TAKEOFF, NOSE GEAR WOULD NOT RETRACT. RECYCLED GEAR, NO HELP. RETURNED TO BHM AND MADE AN UNEVENTFUL LANDING. I NSPECTED AND FOUND HYDRAULIC FLUID AROUND SWIVEL. REMOVED AND REPLACED RETRACT LINE TO LOCK ACTUATOR, RESERVICED SYSTEM , AND RETRACTION TESTED NOSE GEAR PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996072500352 19960725 00352 NM 1996 7 25 UPS96520618 1 19960716 A 5320 FLOOR BEAM BOEING 757 75724APF 1384969 NM BS 310.5 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 405UP 23727 INSPECTION TYPE: C. FLOORBEAM BS 310.5, LBL 25-30, FOUND TO HAVE CORROSION AROUND NUT CLIP. REMOVED CORROSION BY CUTT ING OUT DAMAGE AREA. FABRICATED REPAIR PARTS. INSTALLED REPAIR PARTS. ALODINED AND PRIMED REPAIR IAW EWO 9 6-4068. 2 L 7 2 4F RT A2NM 1996072500376 19960725 00376 NM 1996 7 25 CA960319101 1 19960303 A 5340 651630086 CHORD ANGLE BOEING 737 737275 1384485 NM FS 178 CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 39969 39969 (CAN)CHORD ANGLE AT STA 178 CRACKED IN TWO PLACES WL 196 AND STRINGER 17. REPAIRED. 2 L 7 2 4F A16WE 1996072500377 19960725 00377 NM 1996 7 25 CA960415012 1 19960330 A 2610 894120 FIRE LOOP WHITTAKER 894120 BOEING 727 7272J4 1384006 NM PWA JT8 JT8D17 52049 NE NR 3 ENG INTERNAL FAILURE W D E RETURN TO BLOCK ENGINE SHUTDOWN N FALSE WARNING TX TAXI/GRND HDL 1 CA 0 700814 (CAN)INTERMITTENT FIRE WARNING ON #3 ENGINE WHILE TAXIING OUT. ENGINE SHUT DOWN AND RETURNED TO GATE. #3 FIRE LOOP AT F AULT. REPLACED. 2 L 7 3 4F 4 F RT A3WE E2EA 1996072500389 19960725 00389 SO 1996 7 25 96ZZZX3684 1 19960619 A 3260 SWITCH PIPER PA31 PA31350 7103110 SO RT MLG REQ LUBE A BSYA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 07 35871 318052123 RIGHT MAIN GEAR NOT SHOWING DOWN AND LOCK INDICATION. CLEANED AND LUBED DOWN AND LOCK SWITCH AND MECHANISM. OPS CHECKS GOOD. 1 L 7 2 3O A20SO 1996072500391 19960725 00391 SO 1996 7 25 96ZZZX3686 1 19960610 A 3230 RETRACT SYSTEM PIPER PA31 PA31350 7103110 SO RT MLG MALFUNCTIONED A BSYA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 07 35871 318052123 RIGHT MAIN GEAR WOULD NOT COME DOWN AND LOCK. CYCLED GEAR 4 TIMES, WORKED OK. AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 3O A20SO 1996072500392 19960725 00392 CE 1996 7 25 96ZZZX3687 1 19960613 A 3230 RELAY BEECH 58 58 1152740 CE BRAKE FAILED A BSYA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 33WC TH170 GEAR WOULD NOT EXTEND. CRANKED GEAR DOWN AND LANDED, NO PROBLEM. FOUND DEFECTIVE LANDING GEAR BRAKE RELAY. REMOVED AN D REPLACED RELAY. OPS CHECKED GOOD. 1 L 7 2 3O 3A16 1996072500399 19960725 00399 NM 1996 7 25 96ZZZX3695 1 19960605 A 3230 EXTEND SYS PIPER PA60 PA60600 7106001 NM MLG MALFUNCTION A BSYA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 07 6892R 600887816125 NO GEAR DOWN AND LOCK INTO CMH. CYCLED CIRCUIT BREAKER WORKED OK. MAINTENANCE JACKED AIRCRAFT, CYCLED GEAR SIX TIMES, COULD NOT DUPLICATE. AIRCRAFT RTURNED TO SERVICE. 1 M 7 2 3O RT A17WE 1996072500423 19960725 00423 WP 1996 7 25 96ZZZM1120 1 19960619 A 3350 6011779 POWER SUPPLY DOUG DC9 DC983 3022083 WP CARGO COMPT DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 963AS 53077 OAK - DURING ENGINE RUN-UP AT 15K CHECK, WHEN THE GENERATOR WAS DROPPED OFF LINE, THE EXTERIOR OVERWING EMERGENCY LIGHTS ILLUMINATED WITH THE EMERGENCY LIGHT SWITCH IN THE OFF POSITION. REPLACED THE POWER SUPPLY AND RELAY R2-271 AND OPERAT ED NORMALLY. REFERENCE ASAA9680139. 2 L 7 2 4F RT A6WE 1996072500424 19960725 00424 NM 1996 7 25 96ZZZM1121 1 19960613 A 3350 20131A BATTERY BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING MAINTENANCE CHECK, THE FORWARD AND AFT EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED FORWARD TRANSMITTER AND FORWARD AND AFT BATTERIES. LIGHTS OPERATED NORMALLY. REFERENCE ASAA9610074. 2 L 7 2 4F A16WE 1996072500425 19960725 00425 NM 1996 7 25 96ZZZM1122 1 19960618 A 3350 86210144 BATTERY BOEING 737 737298C 1384490 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY TRACK LIGHTS PALLET 6-8 WOULD NOT TURN OFF AND THE SMOKE BARRIER EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED BATTERY FOR EMERGENCY TRACK LIGHTS ON PALLET 6-8 AND REPLACED BATTERY FOR SMOKE BARRIER EMERGENCY LIGHT AND ALL LIGHTS OPERATED NORMALLY. REFERENCE ASAA9610076. 2 L 7 2 4F RT A16WE 1996072500426 19960725 00426 NE 1996 7 25 96ZZZM1123 2 19960630 A 7497 311479202 WIRE HARNESS DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE LT ENGINE MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 833MA 343 FLT 3344 - IN CRUISE FLIGHT FROM DTW, THE CREW NOTED INTERMITTENT TORQUE FLUCTUATIONS FROM THE LEFT ENGINE. THE AIRCRAF T RETURNED TO DTW. MAINTENANCE REPLACED THE LEFT HMU, P/N 786391-6, AND THE LEFT ENGINE HARNESS, P/N 3114792-02. THE T SCU WAS REPLACED AS A PRECAUTION. ALL CHECKS WERE SATISFACTORY. REFERENCE MALA965059. 2 H 7 2 4T 4 T RT A13NM E20NE 1996072500427 19960725 00427 SW 1996 7 25 96ZZZM1124 1 19960612 A 5753 2731141003 PLATE SWRNGN SA227 SA227AC 8780603 SW TE FLAP WORN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 425MA AC640 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE RIGHT FLAP ROLLER DOUBLER WORN. COMPLETED REPAIR BY REMOVIN G WORN ROLLER DOUBLER AND INSTALLING NEW ROLLER DOUBLER P/N 27-31141-001 AND ROLLER PLATE P/N 27-31141-003 IAW FAC ARP'S 57-10-9513 AND 57-20-9424. REFERENCE MALA963034. 2 L 7 2 4T RT A8SW 1996072500434 19960725 00434 NM 1996 7 25 AALA960846 1 19960521 A 2530 836900 MOUNT BOEING 767 767323 1385205 NM GALLEY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 39356 24037 AFW - FOUND G6 GALLEY MOUNT HAS CORROSION ON INBOARD VERTICAL AND HORIZONTAL SURFACE BEYOND SRM LIMITS. REMOVE EXISTING CORROSION, FABRICATE REPAIR FITTING PER ENGINEERING MRB 767-1230. 2 L 7 2 4F RT A1NM 1996072500435 19960725 00435 NM 1996 7 25 AALA960847 1 19960524 A 5315 111T5008 FLOOR BEAM BOEING 767 767323 1385205 NM BS 867-921 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 39356 24037 AFW - FOUND CORROSION ON FLOOR BEAM AFTER BLENDING TO BE BEYOND SRM LIMITS. FOUND AND BLENDED OUT CORROSION. ATTACHED A FABRICATED STRAP OF .050 301 1/2 HARD STAINLESS. ALODINED, PRIMED AND PAINTED PER ENGINEERING MRB NR 767-1237. (M) 2 L 7 2 4F RT A1NM 1996072500436 19960725 00436 NM 1996 7 25 AALA960848 1 19960324 A 5320 143T82042 STRAP BOEING 767 767323 1385205 NM BS 524-593 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 361AA 24042 AFW - FOUND AND BLENDED CORROSION ON FORWARD CARGO FAIL/SAFE STRAP IN THREE PLACES. AFTER BLENDING, FOUND EACH AREA TO BE BEYOND SRM LIMITS. ALODINED, PRIMED AND PAINTED EACH AREA. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY E NGINEERING PER MRB 767-1241. (M) 2 L 7 2 4F RT A1NM 1996072500437 19960725 00437 NM 1996 7 25 AALA960849 1 19960524 A 5311 146T1224 FRAME BOEING 767 767323 1385205 NM BS 1197 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 361AA 24042 AFW - FOUND AFT CARGO J CAP FRAME CORRODED. AFTER BLENDING FOUND TO BE BEYOND SRM LIMITS. BLENDOUTS ARE 20:01 RATIO. A LODINED AND PRIMED. APPROVED BY ENGINEERING PER MRB 767-1243. (M) 2 L 7 2 4F RT A1NM 1996072500438 19960725 00438 NM 1996 7 25 AALA960850 1 19960524 A 5311 143T1227 FRAME BOEING 767 767323 1385205 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 361AA 24042 AFW - FOUND FRAME INNER CHORD CORRODED. FOUND BEYOND SRM LIMITS AFTER BLENDING. REFINISHED BLENDED AREAS PER SRM 53-00 -07 FIG 101. APPROVED FOR CONTINUED SERVICE BY ENGINEERING PER MRB 767-1280. (M) 2 L 7 2 4F RT A1NM 1996072500439 19960725 00439 NM 1996 7 25 AALA960851 1 19960524 A 5311 FRAME BOEING 767 767323 1385205 NM BS 1175 WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 361AA 24042 AFW - FOUND WEAR ON AFT CARGO J CAP FRAME. FOUND WEAR TO EXCEED SRM ALLOWABLE LIMITS. BLENDED DAMAGED AREAS, ALODINED AND PRIMED. APPROVED BY ENGINEERING WITH NOTED CONDITION PER MRB 767-1244. (M) 2 L 7 2 4F RT A1NM 1996072500440 19960725 00440 NM 1996 7 25 AALA960877 1 19960607 A 2121 732591A FAN BOEING 767 767223 1385123 NM FWD EQUIP BAY DEFECTIVE A AALA H DEACTIVATE SYST/CIRCUITS J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 320AA 22321 LHR - FLT 0066 - EN ROUTE ORD/LHR DURING CRUISE, ELECTRICAL ODOR NOTED IN COCKPIT FOLLOWED BY EICAS MESSAGE FOR FORWARD EQUIPMENT COOLING SUPPLY FAN. COOLING SUPPLY FAN CIRCUIT BREAKER POPPED AND ODOR DISAPPEARED. AIRCRAFT PROCEEDED LHR A ND LANDED WITHOUT INCIDENT. REPLACED NR 1 FORWARD EQUIPMENT COOLING FAN. SYSTEM GROUND CHECKED NORMAL OPERATION WITH N O ELECTRICAL ODOR NOTED. (M) 2 L 7 2 4F RT A1NM 1996072500441 19960725 00441 NM 1996 7 25 AALA960910 1 19960606 A 2530 8369011 MOUNT BOEING 767 767323 1385205 NM G7 GALLEY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 359AA 24040 AFW - FOUND G-7 GALLEY MOUNT HAD CORROSION BEYOND MM LIMITS. BLENDED CORROSION, FABRICATED REPAIR FITTING PE MRB 767-12 54. (M) 2 L 7 2 4F RT A1NM 1996072500442 19960725 00442 1996 7 25 AALA960919 4 19960615 A 2330 RDAX5352 DECODER DOUG MD11 MD11 3023602 NM CABIN OVERHEAD DEFECTIVE A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 07 1755 48490 LGW - FLT 0050 - ON FINAL APPROACH TO LGW, PUFF OF SMOKE NOTED FROM OVERHEAD BETWEEN 3L AND 3R DOORS WITH ELECTRICAL ODO R. NO OTHER ABNORMAL INDICATIONS AND AIRCRAFT LANDED LGW WITHOUT INCIDENT. REMOVED DECODER FROM ABOVE PAX SEAT 21C AND PLACARDED SYSTEM RENDERING PAX SEATS 20CDE THROUGH 38CDE INOPERATIVE WITH NO READING OR CALL LIGHTS. DECODER SUBSEQUEN TLY REPLACED AT EZE/16. SYSTEM GROUND CHECKED NORMAL OPERATION. READING AND CALL LIGHTS FROM PAX SEATS 20CDE THROUGH 3 8CDE OPERATION NORMAL. (M) 2 L 7 3 4F RT A22WE 1996072500443 19960725 00443 WP 1996 7 25 AALA960927 1 19960620 A 5347 TRACK DOUG DC9 DC982 3022082 WP BS 1211-1231 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 292AA 49304 TUL - FOUND CORROSION ON AFT CARGO TIE DOWN TRACK (RT AFT SIDE TRACK). BLENDED CORROSION (SRM 51-10-03). FOUND TO BE O UT OF LIMITS. INSTALLED NEW TIE DOWN TRACK. (M) 2 L 7 2 4F A6WE 1996072500444 19960725 00444 WP 1996 7 25 AALA960929 1 19960620 A 5320 59366711 STRAP DOUG DC9 DC982 3022082 WP BS 1211 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 292AA 49304 FOUND CORROSION ON TOP OF AFT LOWER DOOR FRAME AT STATION 1211 ABOVE LONGERON 28R (AT L27R). INSTALLED FILLER PER ESO 8 0559. TREATED AND PRIMED AREA. CORROSION WAS REMOVED PER SRM 51-10-3. (M) 2 L 7 2 4F A6WE 1996072500445 19960725 00445 WP 1996 7 25 AALA960936 1 19960618 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN SHORTED A AALA O OTHER L NO TEST CR CRUISE 1 SW 07 7521A 49898 DFW - FLT 352 - EN ROUTE SAN/DFW DURING CRUISE, EMERGENCY FLOOR LIGHTS AT MID-CABIN (ROWS 21 THROUGH 33) ILLUMINATED AND COULD NOT BE EXTINGUISHED FROM F/A SWITCH OR COCKPIT SWITCH. AIRCRAFT PROCEEDED TO DFW AND LANDED WITHOUT INCIDENT. R EPAIRED SHORTED WIRE IN EMERGENCY FLOOR LIGHT FEEDER HARNESS AT MID-CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996072500446 19960725 00446 NM 1996 7 25 AALA960938 1 19960618 A 2530 WARMING CART BOEING 767 767323 1385205 NM GALLEY FAILED A AALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 380AN 25449 LHR - FLT 116 - EN ROUTE JFK/LHR DURING CRUISE, SLIGHT SMOKE NOTED IN B/C GALLEY WHEN WARMING CART AND OVEN TURNED ON. T URNED OFF B/C GALLEY WARMING CART AND OVEN AND AIRCRAFT PROCEEDED TO LHR, LANDING WITHOUT INCIDENT. WARMING CART REPLAC ED BY CATERING AND B/C GALLEY OVEN PLACARDED INOPERATIVE. SUBSEQUENTLY AT SFO/18, B/C GALLEY OVEN OPERATION CHECKED BY RUNNING AT 375 DEGREES FOR ONE HOUR WITH NO SMOKE NOTED. UNABLE TO DUPLICATE PROBLEM AND AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A1NM 1996072500447 19960725 00447 WP 1996 7 25 AALA960940 1 19960610 A 5740 3920342503 FITTING DOUG DC9 DC982 3022082 WP WS 807 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 290AA 49302 FOUND 12 INCH FITTING ON UPPER FORWARD LEFT SIDE OF WING SPAR IS CRACK VERT AT RADIUS. E58 1780872 REPLACED FITTING AND SHIM TO FIT USING GENERAL PROCEDURES SRM 51-10. (M) 2 L 7 2 4F A6WE 1996072500448 19960725 00448 WP 1996 7 25 AALA960942 1 19960620 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 1200-1220 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 442AA 49468 TUL - FOUND WEB CORRODED AT STATION 1211 ABOVE LONG 28R CORROSION EXTENDS UNDER RIGHT TIE DOWN TRACK. CUT OUT OLD WEB A ND FABRICATED NEW WEB SECTION. SPLICED WEB PER SRM 53-01 GUIDELINES AND ESO 80559. (M) 2 L 7 2 4F A6WE 1996072500449 19960725 00449 NE 1996 7 25 AALA960954 2 19960619 A 7200 ENGINE BOEING 757 757223 1384957 NM RROYCE RB211 RB211535E4 54555 NE RIGHT FLAMED OUT A AALA E ENGINE SHUTDOWN J X WARNING INDICATION ENGINE FLAMEOUT DE DESCENT 1 SW 07 663AM 25297 LGA - FLT 732 - DURING DESCENT INTO LGA AT APPROXIMATELY 7000 FEET WITH POWER LEVERS AT IDLE, RIGHT ENGINE FLAMED OUT. A TTEMPTED RE-START SUCCESSFUL AND AIRCRAFT LANDED LGA WITHOUT INCIDENT. REPLACED RT ENGINE BVCU, TPU, IPG SOLENOID AND P LA TRANSDUCER. ACCOMPLISHED SYSTEM LEAK AND GROUND ENGINE RUN CHECKS WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORM AL OPERATION. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 1996072500450 19960725 00450 NM 1996 7 25 AALA960955 1 19960619 A 2530 3111 CHILLER DOUG MD11 MD11 3023602 NM GALLEY DIRTY A AALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 1759 48481 LHR - FLT 142 - EN ROUTE JFK/LHR DURING CRUISE, AFT B-C GALLEY CHILLER MADE NOISES AND SLIGHT SMOKE NOTED. TURNED OFF P OWER TO AFT B-C GALLEY CHILLER AND AIRCRAFT PROCEEDED TO LHR, LANDING WITHOUT INCIDENT. PLACARDED AFT B-C GALLEY CHILLE R INOPERATIVE. SUBSEQUENTLY, AT DFW/22, CLEANED AFT B-C GALLEY CHILLER OUTLET SCREEN. CHILLER OPERATION CHECKED NORMAL WITH NO NOISES OR SMOKE NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION AND PLACARD REMOVED. (M) 2 L 7 3 4F RT A22WE 1996072500451 19960725 00451 WP 1996 7 25 AALA960960 1 19960618 A 5320 SILL DOUG DC9 DC982 3022082 WP BS 200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 290AA 49302 TUL - DURING DETAIL INSPECTION OF CARD 4002. FOUND HEAVY CORROSION ON FORWARD SERVICE DOOR FLOOR PANEL AT LOWER AFT COR NER STATION 200. REPAIRED PER ESO 80559 DATED 6-21-96. (M) 2 L 7 2 4F A6WE 1996072500452 19960725 00452 NM 1996 7 25 AALA960963 1 19960625 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 990 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 703AA 22461 FOUND CORROSION ON STRINGER 29R. CUT AND SPLICED NEW SECTION OF STRINGER PER SRM 53-10-3 PG 11A-11E. (M) 2 L 7 3 4F A3WE 1996072500453 19960725 00453 NM 1996 7 25 AALA960966 1 19960625 A 3260 434093003 BOARD BOEING 767 767223 1385123 NM LT MLG DEFECTIVE A AALA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 SW 07 322AA 22323 BOS - FLT 147 - DURING APPROACH TO BOS WHEN LANDING GEAR EXTENDED, LEFT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE WITH EICAS AND ALL OTHER INDICATIONS NORMAL. ACCOMPLISHED TOWER FLY-BY AND CONFIRMED ALL LANDING GEAR EXTENDED. AIRCR AFT LANDED BOS WITHOUT INCIDENT. REPLACED INTEGRATED CIRCUIT MODULE BOARD FOR LEFT MAIN LANDING GEAR. SYSTEM GROUND CH ECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1996072500454 19960725 00454 NM 1996 7 25 AALA960994 1 19960702 A 5320 SUPPORT BOEING 727 727223 1384074 NM BS 364-380 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 881AA 21520 TUL - FOUND STATION 364 TO 380 RBL 12 FLOOR BOARD SUPPORT BEAM CORRODED ON UPPER FLANGE. REMOVED FLOOR SUPPORT BEAM, IN STALLED NEW FLOOR SUPPORT BEAM. (M) 2 L 7 3 4F A3WE 1996072500455 19960725 00455 NM 1996 7 25 AALA960995 1 19960702 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 344 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 881AA 21520 TUL - FOUND STATION 344, RIGHT INBOARD SEAT TRACK HAS CORROSION AT ATTACH POINT TO FLOOR BEAM UPPER FLANGE OF TRACK, INB OARD AND OUTBOARD SIDES. REMOVED CORRODED SECTION. SPLICED IN NEW SECTION SRM 53-10-5, FIG 7. (M) 2 L 7 3 4F A3WE 1996072500456 19960725 00456 NM 1996 7 25 AALA960996 1 19960702 A 5315 FLOOR BEAM BOEING 727 727223 1384074 NM BS 380 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 881AA 21520 TUL - FOUND STATION 380 FLOOR BEAM HAS CORROSION AT RBL 55-60 (TOP FLANGE). REMOVED CORRODED SECTION. INSTALLED FILLER AND DOUBLER PAINTED AND TREATED SRM 53-10-8 PG 9 C, D, E. (M) 2 L 7 3 4F A3WE 1996072500457 19960725 00457 NM 1996 7 25 AALA960997 1 19960702 A 5315 FLOOR BEAM BOEING 727 727223 1384074 NM BS 380 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 881AA 21520 TUL - FOUND STATION 380 FLOOR BEAM HAS CORROSION AT RBL 32-37. CUT OUT CORRODED SECTION. INSTALLED NEW SECTION SRM 53- 10-8 PAGE 9C-E. (M) 2 L 7 3 4F A3WE 1996072500458 19960725 00458 NM 1996 7 25 AALA960998 1 19960702 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 360 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 881AA 21520 TUL - FOUND STATION 360 RBL 55 SEAT TRACK CORRODED ON INBOARD FLANGE TOP SIDE. INSTALLED NEW SEAT TRACK FROM STATION 34 4-380, RT RBL 55. (M) 2 L 7 3 4F A3WE 1996072500459 19960725 00459 NM 1996 7 25 AALA960999 1 19960702 A 5347 STOP BOEING 727 727223 1384074 NM BS 420 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 881AA 21520 TUL - FOUND STATION 420 RIGHT SIDE OF CABIN SEAT TRACK STOP BLOCK CORRODED ON INBOARD AND OUTBOARD FLANGES IN FRONT OF T HE SHORT 40 INCHES SECTION OF SEAT TRACK JUST INBOARD OF CREASE ANGLE. REMOVED AND DELETED SEAT TRACK STOP BLOCK PER SR M 53-10-2 PG 44N (A). (M) 2 L 7 3 4F A3WE 1996072500460 19960725 00460 NM 1996 7 25 AALA961000 1 19960626 A 5330 141N3431 SKIN BOEING 757 757223 1384957 NM BS 376 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 625AA 24583 AFW - FOUND FUSELAGE SKIN AT STATION 376 AND STRINGER 20R HAS GOUGE BLENDED BEYOND SRM. DYE CHECKED, FOUND NO CRACK, BL ENDED GOUGE PER SRM 53-00-01-1. DIGITAL THICKNESS PARENT .080 PERFORMED EDDY CURRENT INSPECTION, NO CRACKS NOTED. (M) 2 L 7 2 4F RT A2NM 1996072500461 19960725 00461 NM 1996 7 25 AALA961001 1 19960702 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 420-460 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 881AA 21520 TUL - FOUND STATION 420 TO 460, RIGHT SIDE OF CABIN 40 INCHES SHORT SECTION OF SEAT TRACK CORRODING INSIDE CHANNEL, ENTI RE LENGTH. REMOVED AND DELECTED SEAT TRACK FROM STATION 420 TO 460 RT PER SRM 53-10-2 PG 44. (M) 2 L 7 3 4F A3WE 1996072500462 19960725 00462 NM 1996 7 25 AALA961002 1 19960702 A 5320 SUPPORT BOEING 727 727223 1384074 NM BS 418 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 881AA 21520 TUL - FOUND STATION 418 FLOOR SUPPORT CORRODED FROM OUTBOARD SIDE OF OUTBOARD SEAT TRACK TO CREASE ANGLE. REMOVED FLOOR SUPPORT AND INSTALL NEW SUPPORT. (M) 2 L 7 3 4F A3WE 1996072500463 19960725 00463 NM 1996 7 25 AALA961003 1 19960702 A 5330 SKIN BOEING 727 727223 1384074 NM WS 474-494 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 881AA 21520 TUL - FOUND CORROSION ON LOWER LE WING SKIN EXTENSION LFSS 474-LFSS 494. REMOVED CORROSION, TREAT, PRIME AND INSTALLED REPAIR DOUBLER PER AARD 5730 00 2 PAGE 1 FIG 1. (M) 2 L 7 3 4F A3WE 1996072500464 19960725 00464 NM 1996 7 25 AALA961004 1 19960702 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 1110-1130 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 881AA 21520 TUL - FOUND CORROSION ON SEAT TRACK STATION 1110 TO 1130 LEFT OUTBOARD. REPLACED SEAT TRACK, LEFT OUTBOARD STATION 1110 TO 1130. (M) 2 L 7 3 4F A3WE 1996072500465 19960725 00465 NM 1996 7 25 ASAA9610074 1 19960613 A 3350 873203041 TRANSMITTER BOEING 737 737290C 138448V NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING MAINTENANCE CHECK, THE FORWARD AND AFT EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED FORWARD TRANSMITTER AND FORWARD AND AFT BATTERIES. LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1996072500466 19960725 00466 NM 1996 7 25 ASAA9610075 1 19960618 A 5315 65549064 FLOOR BEAM BOEING 737 737210C 1384459 NM BS 520 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 SEA - DURING C-CHECK, FOUND CORROSION ON THE UPPER CHORD FLANGE OF THE FLOOR BEAM AT BS 520, LBL 20 TO RBL 20. REPAIRED PER EA 5310-01445 AND BOEING TELEX ASA-SEA-95-0249RR. (M) 2 L 7 2 4F A16WE 1996072500467 19960725 00467 NM 1996 7 25 ASAA9610076 1 19960618 A 3350 8821004 BATTERY BOEING 737 737298C 1384490 NM CARGO COMPT DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY TRACK LIGHTS PALLET 6-8 WOULD NOT TURN OFF AND THE SMOKE BARRIER EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED BATTERY FOR EMERGENCY TRACK LIGHTS ON PALLET 6-8 AND REPLACED BATTERY FOR SMOKE BARRIER EMERGENCY LIGHT AND ALL LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996072500468 19960725 00468 NM 1996 7 25 ASAA9610077 1 19960619 A 5315 65549072 FLOOR BEAM BOEING 737 737210C 1384459 NM BS 747 CORROSION A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 SEA - DURING C-CHECK, FOUND CORROSION ON THE FLOOR BEAM AT BS 747 ON THE LOWER FORWARD FLANGE BETWEEN RBL 24.5 AND RBL 4 4.5. REPAIRED PER EA 5310-01443 AND BOEING TELEX ASA-SEA-96-0243RR. (M) 2 L 7 2 4F A16WE 1996072500469 19960725 00469 NM 1996 7 25 ASAA9610078 1 19960619 A 5315 65549061 FLOOR BEAM BOEING 737 737210C 1384459 NM BS 500 CORROSION A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 SEA - DURING C-CHECK, FOUND CORROSION ON THE UPPER CHORD FORWARD AND AFT FLAGNE OF THE FLOOR BEAM AT BS 500A BETWEEN LBL 25 TO RBL 25. REPAIRED PER EA 5310-01453 AND BOEING TELEX ASA-SEA-96-2721. (M) 2 L 7 2 4F A16WE 1996072500470 19960725 00470 NM 1996 7 25 ASAA9610079 1 19960619 A 5315 65549071 FLOOR BEAM BOEING 737 737210C 1384459 NM BS 727 CORROSION A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 SEA - DURING C-CHECK, FOUND CORROSION ON THE FLOOR BEAM AT BS 727B, BETWEEN LBL 20.75 AND RBL 55.5 AROUND THE FASTENER H OLES USED TO SECURE THE AFT CARGO COMPARTMENT CEILING PANELS. REPAIRED PER EA 5310-01447 AND BOEING TELEX ASA-SEA-96-02 71. (M) 2 L 7 2 4F A16WE 1996072500471 19960725 00471 NM 1996 7 25 ASAA9610080 1 19960619 A 5315 65671403 FLOOR BEAM BOEING 737 737210C 1384459 NM BS 559-605 CORROSION A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 743AS 21821 SEA - DURING C-CHECK, FOUND CORROSION ON THE LONGITUDINAL FLOOR BEAM INBOARD FLANGE AT BS 559 TO BS 605, BL 0. REPAIRED PER EA 5310-01451, EA 5310-01452 AND BOEING TELEX ASA-SEA-96-0254RR. (M) 2 L 7 2 4F A16WE 1996072500472 19960725 00472 NM 1996 7 25 ASAA9610081 1 19960619 A 3350 S417N5048 SOCKET BOEING 737 737290C 138448V NM CARGO COMPT MISSING A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 ANC - DURING MAINTENANCE CHECK, ONE EMERGENCY EXIT LIGHT SOCKET WAS FOUND MISSING PALLET 9-6. REPLACED SOCKET AND LIGHT S OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1996072500473 19960725 00473 NM 1996 7 25 ASAA9610082 1 19960621 A 3350 1060091101 LIGHT BOEING 737 737210C 1384459 NM CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 SEA - DURING MAINTENANCE CHECK, THE AFT SERVICE DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED LIGHT A SSEMBLY AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1996072500474 19960725 00474 NM 1996 7 25 ASAA9610083 1 19960628 A 3260 H1010154 DNLOCK SENSOR BOEING 737 7372X6C 1384552 NM NLG INTERMITTENT A ASAA O OTHER N FALSE WARNING CL CLIMB 1 NM 01 746AS 23123 SEA - FLT 861 - ON ARRIVAL, CREW REPORTED THE NOSE LANDING GEAR DOWN AND LOCKED (GREEN) LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. RECYCLED GEAR AND LIGHT EXTINGUISHED. LANDED WITHOUT INCIDENT. UNABLE TO DUPLICATE MALFUNCTION ON G ROUND, CYCLED GEAR MULTIPLE TIMES AND OPERATED NORMALLY. REPLACED NOSE LANDING GEAR DOWNLOCK SENSOR AS PRECAUTIONARY ME ASURE. (M) 2 L 7 2 4F RT A16WE 1996072500475 19960725 00475 NM 1996 7 25 ASAA9610084 1 19960629 A 3397 WIRE BOEING 737 737210C 1384459 NM CARGO COMPT BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE ON PALLET 10-1. REPAIRED B ROKEN WIRE ON PALLET AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1996072500476 19960725 00476 NM 1996 7 25 ASAA9640047 1 19960615 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 772AS 25105 SNA - FLT 449 - PRIOR TO DEPARTURE, CREW REPORTED THAT THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIV E. MAINTENANCE RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996072500477 19960725 00477 NM 1996 7 25 ASAA9640048 1 19960617 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 773AS 25106 SEA - DURING MAINTENANCE CHECK, TWO EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROW 15. REMOVED AND REPLACED WIRING AT ROW 15 AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996072500478 19960725 00478 NM 1996 7 25 ASAA9640049 1 19960626 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 763AS 25100 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 14-27. REPLA CED BROKEN WIRE AND LIGHT ASSEMBLY, P/N 5417N5048, AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996072500479 19960725 00479 NM 1996 7 25 ASAA9640051 1 19960628 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 765AS 25102 SEA - DURING MAINTENANCE CHECK, THE AFT TWO EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRIN G AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996072500480 19960725 00480 NM 1996 7 25 ASAA9640052 1 19960629 A 3350 S417N50911 SOCKET BOEING 737 7374Q8 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 756AS 25097 SEA - DURING MAINTENANCE CHECK, THE AFT THREE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED SOCKET FOR WHITE LIGHT AND ALL LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996072500481 19960725 00481 NM 1996 7 25 ASAA9640054 1 19960630 A 3350 1060091101 LIGHT BOEING 737 7374Q8 NM CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 779AS 25111 SEA - DURING MAINTENANCE CHECK, THE L-1 EMERGENCY EXIT IDENTIFIER WAS FOUND TO HAVE ONE LAMP OUT AND A BROKEN LENS. REP LACED LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996072500482 19960725 00482 NM 1996 7 25 ASAA9640055 1 19960701 A 3350 8100022607 LIGHT BOEING 737 7374Q8 NM CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 771AS 25104 ANC - FLT 88 - PRIOR TO DEPARTURE THE EMERGENCY EXIT FLOOR TRACK LIGHT AT ROW 23 WAS FOUND INOPERATIVE. RELEASED PER ME L 33-19B. REPLACED LIGHT ASSEMBLY WITH HARNESS IN SEA ON 7/2/96, AND LIGHT OPERATED NORMALLY. REMOVED PLACARD. (M) 2 L 7 2 4F RT A16WE 1996072500483 19960725 00483 WP 1996 7 25 ASAA9680137 1 19960615 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 948AS 11556 53021 PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996072500484 19960725 00484 WP 1996 7 25 ASAA9680139 1 19960619 A 3350 922710127 RELAY DOUG DC9 DC983 3022083 WP CARGO COMPT DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 963AS 53077 OAK - DURING ENGINE RUN-UP AT 15K CHECK, WHEN THE GENERATOR WAS DROPPED OFF LINE, THE EXTERIOR OVERWING EMERGENCY LIGHTS ILLUMINATED WITH THE EMERGENCY LIGHT SWITCH IN THE OFF POSITION. REPLACED THE POWER SUPPLY AND RELAY R2-271 AND OPERAT ED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996072500485 19960725 00485 WP 1996 7 25 ASAA9680140 1 19960622 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 977AS 10915 53453 SFO - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996072500486 19960725 00486 WP 1996 7 25 ASAA9680141 1 19960630 A 3350 41B004AD07G3 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 956AS 48079 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. REPLACED THE ABTTERIES AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996072500487 19960725 00487 WP 1996 7 25 ASAA9680142 1 19960630 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 956AS 48079 SEA - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT CHARGE LAMP WAS FOUND INOPERATIVE. REPLACED THE LI GHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996072500488 19960725 00488 SW 1996 7 25 MALA963034 1 19960612 A 5753 2731141001 DOUBLER SWRNGN SA227 SA227AC 8780603 SW TE FLAP WORN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 425MA AC640 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE RIGHT FLAP ROLLER DOUBLER WORN. COMPLETED REPAIR BY REMOVIN G WORN ROLLER DOUBLER AND INSTALLING NEW ROLLER DOUBLER P/N 27-31141-001 AND ROLLER PLATE P/N 27-31141-003 IAW FAC ARP'S 57-10-9513 AND 57-20-9424. (M) 2 L 7 2 4T RT A8SW 1996072500489 19960725 00489 1996 7 25 MALA965016 4 19960606 A 3442 066308601 RADAR INDICATOR DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A MALA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 828MA 333 FLT 3173 - IN FLT, THE WEATHER RADAR BECAME INOPERATIVE. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE WEATHE R RADAR INDICATOR. SYSTEM OPERATED SATISFACTORILY. (M) 2 H 7 2 4T RT A13NM 1996072500490 19960725 00490 1996 7 25 MALA965017 4 19960606 A 3442 071131900 RT UNIT DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A MALA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 826MA 330 FLT 3010 - IN FLT, THE WEATHER RADAR FAILED TO PAINT GROUND. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE WE ATHER RADAR RECEIVER/TRANSCEIVER. SYSTEM OPERATED SATISFACTORILY. (M) 2 H 7 2 4T RT A13NM 1996072500491 19960725 00491 SW 1996 7 25 MALA965019 1 19960608 A 2750 SP3082640K COMPENSATOR SWRNGN SA227 SA227AC 8780603 SW TE FLAPS MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 421MA AC634 FLT 3140 - ON CLIMB-OUT FROM DTW, THE SAS FAULT LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE SAS FLAP COMPENSATOR AND THE ANNUNCIATOR PANEL. (M) 2 L 7 2 4T RT A8SW 1996072500492 19960725 00492 SW 1996 7 25 MALA965022 1 19960610 A 3260 1EN516 SWITCH SWRNGN SA227 SA227AC 8780603 SW NLG FAILED A MALA K NONE P NO WARNING INDICATION AP APPROACH 1 GL 15 446MA AC693 FLT 3078 - ON APPROACH TO MSP, THE NOSE GEAR INTRANSIT LIGHT FAILED TO ILLUMINATE UPON GEAR EXTENSION. ALL OTHER INDICA TIONS WERE NORMAL. THE AIRCRAFT CONTINUED TO MSP. MAINTENANCE REPLACED THE LEFT UPPER POSITION SWITCH. ALL CHECKS WER E SATISFACTORY. (M) 2 L 7 2 4T RT A8SW 1996072500493 19960725 00493 SW 1996 7 25 MALA965023 1 19960610 A 5230 CLOSING MECH SWRNGN SA227 SA227AC 8780603 SW CARGO DOOR MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 26906 AC654B FLT 3024 - EN ROUTE FROM DTW TO MKG, THE CARGO DOOR PRIMARY AND SECONDARY WARNING LIGHT ILLUMINATED. THE CREW PERFORMED QUICK REFERENCE PROCEDURES AND DIVERTED TO LAN. MX REPLACED THE CARGO DOOR MAIN SPRING AND OVER CENTERING BELLCRANK HA RDWARE. (M) 2 L 7 2 4T RT A8SW 1996072500494 19960725 00494 SW 1996 7 25 MALA965024 1 19960527 A 5230 SKIN SWRNGN SA227 SA227AC 8780603 SW CARGO DOOR CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 422MA AC635 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE CARGO DOOR SKIN UPPER TABS CRACKED AT FORWARD AND AFT HINGE RECESS. COMPLETED REPAIRS BY REMOVING DAMAGE AND INSTALLING STAINLESS DOUBLERS IAW FAIRCHILD ARP 52-30-9130 DATED 20 JU NE 1991. (M) 2 L 7 2 4T RT A8SW 1996072500495 19960725 00495 SW 1996 7 25 MALA965025 1 19960527 A 5320 2731110 STIFFENER SWRNGN SA227 SA227AC 8780603 SW BL 0.0 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 422MA AC635 DURING A SCHEDULED INSPECTION IN MSP, MX FOUND CRACKS IN STIFFENER, P/N 27-31110, AT BL 0.0. FREPAIRED IAW FAC SRM 57-90 -30 PAGES 3 THROUGH 12, REPAIR NR 1 AND NR 2. FABRICATED AND INSTALLED REPAIR DOUBLERS AND TEE ANGLES. (M) 2 L 7 2 4T RT A8SW 1996072500496 19960725 00496 NM 1996 7 25 MALA965026 1 19960613 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 819MA 251 FLT NR 3183 - DURING THE PREFLIGHT INSPECTION IN DTW, THE OVERHEAD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTEN ANCE REPLACED THE EMERGENCY LIGHT LAMP ASSEMBLY. ALL CHECKS SATISFACTORY. (M) 2 H 7 2 4T RT A13NM 1996072500497 19960725 00497 1996 7 25 MALA965027 4 19960611 A 3422 6226136002 DIR GYRO SWRNGN SA227 SA227AC 8780603 SW NR 1 INTERNAL FAULT A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 445MA AC687 FLT 3310 - AFTER TAKEOFF FROM DTW, THE CAPTAINS DIRECTIONAL GYRO WOULD INTERMITTENTLY FREEZE. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE NR 1 DIRECTIONAL GYRO. ALL CHECKS SATISFACTORY. (M) 2 L 7 2 4T RT A8SW 1996072500498 19960725 00498 1996 7 25 MALA965028 4 19960613 A 3454 066107804 VHF NAV RECEIVER DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 832MA 341 FLT 3420 - EN ROUTE FROM DTW, THE FLIGHT OFFICERS VOR, HEAD, CDI AND TO-FROM BECAME INOPERATIVE. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE NR 2 VHF NAV RECEIVER. SYSTEM OPERATED SATISFACTORILY. (M) 2 H 7 2 4T RT A13NM 1996072500499 19960725 00499 NM 1996 7 25 MALA965029 1 19960609 A 3350 6104781 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 828MA 333 DURING A PREFLIGHT INSPECTION IN DTW, THE FORWARD TO FLOOR TRACK LIGHTS WERE INTERMITTENT. MAINTENANCE DEFERRED THE SYS TEM PER MEL 33-13 (C). THE MEL WAS CLEARED THROUGH REPLACEMENT OF THE BATTERY PACK. SYSTEM OPERATED SATISFACTORILY. ( M) 2 H 7 2 4T RT A13NM 1996072500500 19960725 00500 SW 1996 7 25 MALA965030 1 19960612 A 5400 ANGLE SWRNGN SA227 SA227AC 8780603 SW WING/NACELLE WORN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 425MA AC640 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE RIGHT NACELLE INBOARD LOWER WING SKIN TO NACELLE ATTACH ANGL E REPAIR DOUBLER WORN. REMOVED EXISTING REPAIR AND INSTALLED NEW 6.5 INCH REPAIR DOUBLER OVER AREA IAW FAIRCHILD SRM 51 -00-00 PAGE 4 PART FOR PART REPLACEMENT AND FAC ARP 54-20-9101 REV B DATED MAY 12, 1993. (M) 2 L 7 2 4T RT A8SW 1996072500501 19960725 00501 SW 1996 7 25 MALA965031 1 19960612 A 5753 2736000040 SKIN SWRNGN SA227 SA227AC 8780603 SW TE FLAP CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 425MA AC640 DURNG A SCHEDULED INSPECTION IN MSP, MX FOUND THE INBOARD MOST TRAILING EDGE ON THE RIGHT FLAP TO HAVE CHAFE DAMAGE. CO MPLETED REPAIR TO RT FLAP P/N 27-36000-040 S/N C-135 BY REMOVING DAMAGED AREA TO TOP SKIN IN EXHAUST TRAIL AND INSTALLIN G REPAIR DOUBLER AND SKIN PATCH IAW FAC SRM 57-90-60 REPAIR NR 8. (M) 2 L 7 2 4T RT A8SW 1996072500502 19960725 00502 SW 1996 7 25 MALA965032 1 19960612 A 5320 NUT PLATE SWRNGN SA227 SA227AC 8780603 SW COCKPIT CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 425MA AC640 DURING A SCHEDULED INSPECTION IN MSP, MX FOUND FLIGHT OFFICERS INBOARD SEAT TRACK CENTER NUT PLATE CRACKED OUT TO RIVET. COMPLETED REPAIR BY FABRICATING AND INSTALLING REPAIR FILLER AND DOUBLER IAW EA 01-96049. (M) 2 L 7 2 4T RT A8SW 1996072500503 19960725 00503 SW 1996 7 25 MALA965033 1 19960612 A 5532 SKIN SWRNGN SA227 SA227AC 8780603 SW VERT STAB CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 425MA AC640 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE RIGHT VERTICAL STABILIZER SKIN CRACKED AFT OF THE CUT OUT FO R THE HORIZONTAL STABILIZER SPAR. PERFORMED REPAIR TO RIGHT VERTICAL STAB SKIN BY REMOVAL OF PREVIOUS REPAIR. STOP DRI LLED NEW CRACK. FABRICATED AND WET INSTALLED REPAIR DOUBLER IAW FAC SRM 51-90-04 REPAIR NR 11. (M) 2 L 7 2 4T RT A8SW 1996072500504 19960725 00504 SW 1996 7 25 MALA965035 1 19960527 A 5400 ANGLE SWRNGN SA227 SA227AC 8780603 SW WING/NACELLE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 422MA AC635 DURING A SCHEDULED INSPECTION IN MSP, FOUND LEFT INBOARD LOWER NACELLE TO WING TRANSIT ANGLE FORWARD EDGE CRACKED ON PRE VIOUS REPAIR. REMOVED PREVIOUS REPAIR, FABRICATED AND WET INSTALLED REPAIR DOUBLER IAW ARP 54-20-9101 REV B DATED MAY 1 2, 1993. WHILE COMPLETING REPAIR, NOTED LEFT INBOARD LOWER NACELLE TO WING TRANSIT ANGLE CRACKED FROM RIVET 9.5 INCH BA CK FROM PREVIOUS REPAIR. STOP DRILLED CRACK, FABRICATED AND WET INSTALLED REPAIR DOUBLER IAW ARP 54-20-9101 REV B DATED MAY 12, 1993. (M) 2 L 7 2 4T RT A8SW 1996072500505 19960725 00505 SW 1996 7 25 MALA965036 1 19960527 A 5400 ANGLE SWRNGN SA227 SA227AC 8780603 SW NACELLE/WING CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 422MA AC635 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND LEFT INBOARD UPPER NACELLE TO WING TRANSIT ANGLE FORWARD EDGE CR ACKED. COMPLETED REPAIR BY STOP DRILLING CRACK, FABRICATING AND WET INSTALLING REPAIR DOUBLER IAW ARP 54-20-9101 REV B DATED MAY 12, 1993. (M) 2 L 7 2 4T RT A8SW 1996072500506 19960725 00506 SW 1996 7 25 MALA965037 1 19960612 A 5311 FRAME SWRNGN SA227 SA227AC 8780603 SW BS 377.271 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 425MA AC640 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND AN INTERCOSTAL CRACK. PERFORMED REPAIR TO RT LOWER BELT FRAME A T FS 377-271. STOP DRILLED CRACK, FABRICATED, PREPPED AND INSTALLED REPAIR DOUBLER IAW FAC SRM 53-90-20 PAGES 88-89, DA TED JANUARY 18, 1993. (M) 2 L 7 2 4T RT A8SW 1996072500507 19960725 00507 SW 1996 7 25 MALA965038 1 19960527 A 5320 DOOR FRAME SWRNGN SA227 SA227AC 8780603 SW BS 159.247 SCUFFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 422MA AC635 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE PASSENGER DOOR OPENING ON FUSELAGE FRAME AT FS 159.247 SCUFF ED BY PASSENGER DOOR GUIDES. COMPLETED REPAIR BY FABRICATING AND INSTALLING REPAIR DOUBLER IAW FAC SRM 53-90-20 PAGES 7 5-77 REPAIR NR 17. (M) 2 L 7 2 4T RT A8SW 1996072500508 19960725 00508 SW 1996 7 25 MALA965039 1 19960527 A 5320 DOOR FRAMES SWRNGN SA227 SA227AC 8780603 SW BS 133.873 SCUFFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 422MA AC635 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE PASSENGER DOOR OPENING ON FUSELAGE FRAME AT FS 133.873 SCUFF ED BY PASSENGER DOOR GUIDES. COMPLETED REPAIR BY FABRICATING AND INSTALLING REPAIR DOUBLER IAW FAC SRM 53-90-20 PAGES 7 5-77 REPAIR NR 17. (M) 2 L 7 2 4T RT A8SW 1996072500509 19960725 00509 SW 1996 7 25 MALA965040 1 19960612 A 5311 FRAME SWRNGN SA227 SA227AC 8780603 SW BS 212.271 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 425MA AC640 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERFORMED REPAIR TO CRACK ON THE RIGHT LOWER BELT FRAME AT FS 212.271. STOP DRILLED CRACK, FABRICATED, PREPPED AND INSTALLED REPAIR DOUBLER IAW FAC SRM 53-90-20 PAGES 88-89, DATED JANUARY 1 8, 1993. (M) 2 L 7 2 4T RT A8SW 1996072500510 19960725 00510 SW 1996 7 25 MALA965041 1 19960612 A 5230 MOUNT SWRNGN SA227 SA227AC 8780603 SW BS 491 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 425MA AC640 DURING A SCHEDULED INSPECTION AT MSP, MAINTENANCE FOUND A GAS STRUT MOUNT POST HOLE TO BE CRACKED. PERFORMED REPAIR TO CARGO DOOR FRAME AT FS 491.00 BY REMOVING DAMAGED GAS STRUT MOUNT HOLE. FABRICATED, PREPPED AND INSTALLED A REPAIR ANGL E, REPAIR PLATE, AND FILLER IAW FAIRCHILD ARP 53-20-9503 DATED MARCH 1, 1995. (M) 2 L 7 2 4T RT A8SW 1996072500511 19960725 00511 SW 1996 7 25 MALA965042 1 19960527 A 5311 FRAME SWRNGN SA227 SA227AC 8780603 SW BS 189.060 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 422MA AC635 DURING A SCHEDULED INSPECTION IN MSP, PERFORMED REPAIR TO RIGHT LOWER BELT FRAME AT FS 189.060. STOP DRILLED CRACK, FAB RICATED, PREPPED AND INSTALLED REPAIR DOUBLER IAW FAC SRM 53-90-20 PAGES 87-90, DATED JANUARY 18, 1993. (M) 2 L 7 2 4T RT A8SW 1996072500512 19960725 00512 SW 1996 7 25 MALA965043 1 19960527 A 5321 FLOOR BOARD SWRNGN SA227 SA227AC 8780603 SW BS 227.221 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 422MA AC635 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND A CRACKED OUT RIVET HOLE IN RIGHT CENTER AISLE FLOOR BOARD WEB A T FS 227.221. CRACK LENGTH APPROXIMATELY .300. COMPLETED REPAIR BY STOP DRILLING CRACK, FABRICATING AND INSTALLING A R EPAIR DOUBLER. LENGTH OF REPAIR IS 9.50 INCH. ALL WORK WAS COMPLETED IAW FAIRCHILD SRM 53-90-20 PGS 67-69, REPAIR NR 1 5 REV JANUARY 18, 1993. (M) 2 L 7 2 4T RT A8SW 1996072500513 19960725 00513 SW 1996 7 25 MALA965044 1 19960527 A 5311 FRAME SWRNGN SA227 SA227AC 8780603 SW BS 197.27 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 422MA AC635 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERFORMED REPAIR TO LOWER RIGHT BELT FRAME RELIEF RADIUS AT FS 197.27 AND BL 8. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAIRCHILD SRM REPAIR NR 19, 53-90-20 PAGES 83 -35, REV JANUARY 18, 1993. (M) 2 L 7 2 4T RT A8SW 1996072500514 19960725 00514 SW 1996 7 25 MALA965045 1 19960615 A 3234 7092011 CONTL HANDLE SWRNGN SA227 SA227AC 8780603 SW LANDING GEAR INTERNAL FAULT A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 436MA AC719B FLT NR 3405 - ON CLIMB-OUT FROM MSP, THE LANDING GEAR HANDLE WOULDN'T MOVE TO RETRACT THE GEAR. THE AIRCRAFT RETURNED T O MSP. MX REPLACED THE LANDING GEAR CONTROL HANDLE ASSEMBLY. ALL CHECKS WERE SATISFACTORY. (M) 2 L 7 2 4T RT A8SW 1996072500515 19960725 00515 NM 1996 7 25 MALA965046 1 19960618 A 3350 10005511 LAMP DHAV DHC8 DHC8102 2809003 NM COCKPIT INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 854MA 357 FLT NR 3370 - DURING THE PREFLIGHT INSPECTION IN MSP, THE CREW FOUND THE COCKPIT OVERHEAD EMERGENCY LIGHT INOP. MAINTEN ANCE REPLACED THE EMERGENCY EXIT LAMP ASSEMBLY. ALL CHECKS SATISFACTORY. (M) 2 H 7 2 4T RT A13NM 1996072500516 19960725 00516 SW 1996 7 25 MALA965047 1 19960618 A 3260 SWITCH SWRNGN SA227 SA227AC 8780603 SW RT MLG LACK OF LUBE A MALA O OTHER N FALSE WARNING AP APPROACH 1 GL 15 439MA AC722 FLT 3479 - ON APPROACH TO DTW, THE RIGHT GEAR INTRANSIT LIGHT DID NOT ILLUMINATE DURING GEAR EXTENSION. ALL OTHER INDIC ATIONS WERE NORMAL. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. MX CLEANED AND LUBED THE RIGHT GEARS INDICATI ONS SWITCHES. ALL CHECKS SATISFACTORY. (M) 2 L 7 2 4T RT A8SW 1996072500517 19960725 00517 SW 1996 7 25 MALA965048 1 19960620 A 5210 2724089005 SEAL SWRNGN SA227 SA227AC 8780603 SW PAX DOOR WORN A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 436MA AC719B FLT 2911 - ON CLIMB-OUT FROM DTW, A LOUD SQUEAL WAS HEARD FROM THE PASSENGER DOOR AREA. THE AIRCRAFT RETURNED TO DTW. M X REPLACED THE PASSENGER DOOR SEAL. ALL CHECKS SATISFACTORY. (M) 2 L 7 2 4T RT A8SW 1996072500518 19960725 00518 NM 1996 7 25 MALA965049 1 19960621 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN LOOSE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 853MA 353 FLT 3315 - DURING THE POST FLIGHT IN DTW, TWO FLOOR TRACK LIGHTS WERE INOP. MAINTENANCE RESECURED A TRACK PLUG CONNECTO R AT ROW 10. (M) 2 H 7 2 4T RT A13NM 1996072500519 19960725 00519 NM 1996 7 25 MALA965050 1 19960621 A 3350 6104781 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 831MA 339 FLT 3420 - DURING THE PREFLIGHT IN DTW, THE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS. ALL CHECKS SATISFACTORY. (M) 2 H 7 2 4T RT A13NM 1996072500520 19960725 00520 NM 1996 7 25 MALA965051 1 19960621 A 3350 6104781 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 831MA 339 FLT 3137 - DURING THE PREFLIGHT IN DTW, THE AFT EMERGENCY AISLE LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE CABIN AFT RIGHT BATTERY PACK. ALL CHECKS GOOD. (M) 2 H 7 2 4T RT A13NM 1996072500521 19960725 00521 SW 1996 7 25 MALA965052 1 19960622 A 5400 ANGLE SWRNGN SA227 SA227AC 8780603 SW WING/NACELLE DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 446MA AC693 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND RIGHT OUTBOARD UPPER NACELLE TO WING TRANSIT ANGLE HAD FASTENER PULLING THROUGH SKIN. COMPLETED REPAIR BY FABRICATING AND WET INSTALLING REPAIR DOUBLER IAW ARP 54-20-9101 REV B DATED MAY 12, 1993 AND FAIRCHILD SRM CHAPTERS 51-30-02, 51-40 AND 51-30-03. (M) 2 L 7 2 4T RT A8SW 1996072500522 19960725 00522 SW 1996 7 25 MALA965053 1 19960622 A 5411 FORMER SWRNGN SA227 SA227AC 8780603 SW LT NACELLE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 446MA AC693 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND NACELLE UPPER FORMER CRACKED. STOP DRILLED CRACKS AND INSTALLED REPAIR DOUBLER AS PER FAC SRM 51-90-02 PAGE 5, REF. (M) 2 L 7 2 4T RT A8SW 1996072500523 19960725 00523 SW 1996 7 25 MALA965054 1 19960622 A 2730 274401161 TORQUE TUBE SWRNGN SA227 SA227AC 8780603 SW ELEVATOR DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 446MA AC693 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE ELEVATOR TORQUE TUBE ROD END HOLES TO BE ELONGATED. COMPLET ED REPAIR TO ELEVATOR P/N 27-44001-161 S/N FAC-345 BY REPLACING ELEVATOR TORQUE TUBE WITH SAME P/N 27-44026-007 WITH NEW PART. ALL WORK COMPLETED IAW FAC MM 27-30-00 PAGES 202-203. (M) 2 L 7 2 4T RT A8SW 1996072500524 19960725 00524 NM 1996 7 25 MALA965055 1 19960622 A 2431 68001008010 BATT TEMP IND DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A MALA K NONE O OTHER CL CLIMB 1 GL 15 828MA 333 FLT 3121 - ON CLIMB-OUT FROM MSP, THE BATTERY TEMPERATURE INDICATOR FAILED. THE CREW DISCONNECTED THE AUX AND MAIN BATT ERIES AND RETURNED TO MSP. MAINTENANCE REPLACED THE BATTERY TEMP MONITOR PANEL. (M) 2 H 7 2 4T RT A13NM 1996072500525 19960725 00525 WP 1996 7 25 MALA965056 2 19960625 A 7200 ENGINE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP RIGHT FAILED A MALA A E UNSCHED LANDING ENGINE SHUTDOWN Y ENGINE STOPPAGE CL CLIMB 1 GL 15 2692P AC658B FLT 3253 - EN ROUTE FROM GFK, THE RIGHT ENGINE FAILED. THE AIRCRAFT RETURNED TO GFK AND LANDED WITHOUT FURTHER INCIDENT . DURING THE POST FLIGHT, PROP AND FUSELAGE DAMAGE WAS ALSO NOTED. THE ENGINE WAS REPLACED. AN INVESTIGATION IS CONTI NUING. (M) 2 L 7 2 4T 4 T RT A8SW E4WE 1996072500526 19960725 00526 NM 1996 7 25 MALA965057 1 19960626 A 3350 6104789 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM GALLEY DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 816MA 231 DURING A MAINTENANCE WALKAROUND IN DTW, THE GALLEY OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENAN CE REPLACED THE WARDROBE LOWER BATTERY PACK. ALL CHECKS WERE SATISFACTORY. (M) 2 H 7 2 4T RT A13NM 1996072500527 19960725 00527 NM 1996 7 25 MALA965058 1 19960630 A 3260 841005 PSEU DHAV DHC8 DHC8102 2809003 NM COCKPIT MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 859MA 361 FLT NR 2915 - EN ROUTE TO RVC, THE CREW NOTED THAT THE NOSE GEAR UNSAFE LIGHT WOULD INTERMITTENTLY ILLUMINATE. THE AIRC RAFT RETURNED TO DTW. MAINTENANCE REPLACED THE PSEU. ALL CHECKS SATISFACTORY. (M) 2 H 7 2 4T RT A13NM 1996072500528 19960725 00528 NE 1996 7 25 MALA965059 2 19960630 A 7320 7863916 HMU DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE LT ENGINE MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 833MA 343 FLT 3344 - IN CRUISE FLIGHT FROM DTW, THE CREW NOTED INTERMITTENT TORQUE FLUCTUATIONS FROM THE LEFT ENGINE. THE AIRCRAF T RETURNED TO DTW. MAINTENANCE REPLACED THE LEFT HMU, P/N 786391-6, AND THE LEFT ENGINE HARNESS, P/N 3114792-02. THE T SCU WAS REPLACED AS A PRECAUTION. ALL CHECKS WERE SATISFACTORY. (M) 2 H 7 2 4T 4 T RT A13NM E20NE 1996072500529 19960725 00529 SW 1996 7 25 MALA965060 1 19960630 A 2120 AIR DISTR SWRNGN SA227 SA227AC 8780603 SW COCKPIT SMOKE A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 60NE AC760B FLT 3324 - AFTER LANDING IN LNK, THE CREW NOTED SMOKE COMING OUT OF THE LEFT GASPER VENT. THE SYSTEM WAS DEFERRED PER M EL 21-96. (M) 2 L 7 2 4T RT A8SW 1996072500530 19960725 00530 SW 1996 7 25 MALA965061 1 19960703 A 3260 INTRANSIT LIGHT SWRNGN SA227 SA227AC 8780603 SW RT MLG ILLUMINATED A MALA O OTHER N FALSE WARNING AP APPROACH 1 GL 15 425MA AC640 FLT NR 3376 - ON APPROACH TO ERI, THE RIGHT GEAR INTRANSIT LIGHT REMAINED ILLUMINATED, AND THE DOWN AND LOCKED LIGHT REM AINED EXTINGUISHED. THE CREW CYCLED THE GEAR UNTIL ALL INDICATIONS WERE NORMAL. MAINTENANCE INSPECTED THE GEAR SWITCHE S AND WIRING. ALL CHECKS WERE SATISFACTORY. (M) 2 L 7 2 4T RT A8SW 1996072500531 19960725 00531 NM 1996 7 25 RAAAB296028 1 19960616 A 3350 1000679 LIGHT BOEING 727 72722C 138400F NM CABIN FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 MID CABIN SERVICE DOOR EMERGENCY EXIT LIGHT FAILED SERVICE CHECK. CHANGED LIGHT ASSEMBLY. (M) 2 L 7 3 4F A3WE 1996072500532 19960725 00532 NM 1996 7 25 RAAAB296029 1 19960610 A 5320 65196721 SILL CAP BOEING 727 72722C 138400F NM BS 1030-1130 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 55329 19098 DURING SCHEDULED S3 INSPECTION PER CARD 53-54102, FOUND AFT CARGO DOOR SILL CAP CORRODED AT BS 1063, 1075, 1078, AND 109 3 AND A CRACK RUNNING FROM BS 1057.6 TO 1062.6. INSTALLED NEW CAP STRAP PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1996072500533 19960725 00533 NM 1996 7 25 RAAAB296030 1 19960622 A 5330 SKIN BOEING 727 72722C 138400F NM CABIN CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 55400 19098 DURING SCHEDULED INSPECTION PER SB 53-054, FOUND MID CABIN DOOR UPPER HINGE CUT OUT CRACKED. REPAIRED PER SB 727-53-054 REV 1 AND BOEING MSG M7272-53-2800. (M) 2 L 7 3 4F A3WE 1996072500534 19960725 00534 SO 1996 7 25 RAAAE996005 1 19960528 A 3350 8621014 BATTERY PACK 873100112 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 LEFT FORWARD OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CEHCK. REPLACED BATTERY PACK DUE TO LOW CHA RGE. (M) 2 L 7 4 4T 4A22 1996072500535 19960725 00535 SO 1996 7 25 RAAAE996006 1 19960528 A 3350 8621014 BATTERY PACK 873100112 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 RIGHT FORWARD OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. REPLACED BATTERY PACK DUE TO LOW CH ARGE. (M) 2 L 7 4 4T 4A22 1996072500536 19960725 00536 SO 1996 7 25 RAAAE996021 1 19960528 A 3350 8621014 BATTERY PACK LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 AFT PAX CABIN EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. (M) 2 L 7 4 4T 4A22 1996072500537 19960725 00537 WP 1996 7 25 USAA960499 1 19960624 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 160 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 943VJ 72136 47058 PIT - DURING C-4 CHECK, FOUND 1 INCH LENGTH CRACK EXTENDING THROUGH RIVET AT FORWARD AIRSTAIR CUT OUT, BOTTOM FORWARD CO RNER, STATION 160. INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 57A. (M) 2 L 7 2 4F A6WE 1996072500538 19960725 00538 EU 1996 7 25 USAA960503 1 19960628 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU BS 600-623 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 482US 22238 11231 PIT - DURING UNSCHEDULED MAINTENANCE, FOUND CRACK IN FUSELAGE SKIN, LEFT SIDE 23 INCHES LONG AT STATION 600-623 AT STRIN GER 17. INSTALLED DOUBLER PER EO 5393L023 AND EA 33032. (M) 2 L 7 2 4F RT A20EU 1996072500539 19960725 00539 EU 1996 7 25 USAA960504 1 19960628 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU BS 600-619 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 482US 22238 11231 PIT - DURING UNSCHEDULED MAINTENANCE, FOUND CRACK IN FUSELAGE SKIN RIGHT SIDE 19 INCHES LONG AT STATION 600-619 STRINGER 58. INSTALLED DOUBLER PER EO 5393L023 AND EA 33032. (M) 2 L 7 2 4F RT A20EU 1996072500540 19960725 00540 WP 1996 7 25 USAAD96083 1 19960622 A 3350 AD20131A BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 985VJ 47208 FORWARD EMERGENCY LIGHTS INOPERATIVE. REPLACED FORWARD BATTERY PACK. (M) 2 L 7 2 4F A6WE 1996072500541 19960725 00541 NE 1996 7 25 USAAD96084 2 19960623 A 7200 ENGINE DOUG DC9 DC981 3022081 WP PWA JT8 JT8D217 52053 NE RIGHT FAILED A USAA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 EA 19 809US 48041 709965 FLT 912 - FLL-CLT - DURING CLIMB, CREW HEARD A LOUD BANG AND NOTICED POWER LOSS FROM RIGHT ENGINE. SHUT DOWN ENGINE. R EPLACED RIGHT ENGINE. (M) 2 L 7 2 4F 4 F A6WE E9NE 1996072500542 19960725 00542 WP 1996 7 25 USAAD96085 1 19960624 A 2613 95000011 CIRCUIT BREAKER DOUG DC9 DC982 3022082 WP C/B PANEL FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 817US 48097 FLT 765 - CLT-MSY - ON CLIMB, WHEEL WELL OVERHEAT CIRCUIT BREAKER POPPED. RETURNED TO FIELD. REPLACED CIRCUIT BREAKER. (M) 2 L 7 2 4F A6WE 1996072500543 19960725 00543 WP 1996 7 25 USAAD96086 1 19960624 A 2910 SEAL DOUG DC9 DC931 3022065 WP RUDDER SOV FAILED A USAA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 EA 19 993VJ 47332 FLT 1796 - MCI-BOS - RIGHT SYSTEM HYDARULIC FLUID QUANTITY DECREASING IN FLIGHT. DIVERTED TO CMH. FOUND BAD SEAL ON RU DDER CONTROL SHUTOFF VALVE FITTING. REPLACED SEAL. SERVICED HYDRAULIC SYSTEM. (M) 2 L 7 2 4F A6WE 1996072500544 19960725 00544 WP 1996 7 25 USAAD96087 1 19960622 A 3350 AD20131A BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 985VJ 47208 FORWARD EMERGENCY LIGHTS INOPERATIVE. REPLACED FORWARD BATTERY PACK. (M) 2 L 7 2 4F A6WE 1996072500545 19960725 00545 WP 1996 7 25 USAAD96088 1 19960626 A 2120 DUCT DOUG DC9 DC931 3022065 WP A/C SYSTEM LOOSE A USAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 19 960VJ 47505 FLT 1148 - PIT-BGM - ON CLIMB, EXTREME VIBRATION CAME FROM TAIL. RETURNED TO FIELD. FOUND AIR CONDITIONING DUCT BLOWN OFF THE COOLING AIR TURBINE. REATTACHED DUCT. (M) 2 L 7 2 4F A6WE 1996072500546 19960725 00546 WP 1996 7 25 USAAD96089 1 19960627 A 2910 HYD LINE DOUG DC9 DC931 3022065 WP LT MLG WW OUT OF POSITION A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 916VJ 47023 FLT 1258 - PIT-CAK - ON TAKEOFF, GEAR DOOR OPEN LIGHT CAME ON. AFTER GEAR RETRACTION, DOOR OPEN LIGHT WENT OUT AND LEFT UNSAFE LIGHT CAME ON. CYCLED GEAR, AND UNSAFE LIGHT REMAINED ON. RETURNED TO FIELD. FOUND HYDRAULIC LINE FROM HANDPU MP IN LEFT WHEEL WELL WEDGED BETWEEN LEFT GEAR DOOR AND UPLOCK ASSEMBLY. RE-ATTACHED LINE. OPS CHECKS GOOD. (M) 2 L 7 2 4F A6WE 1996072500547 19960725 00547 WP 1996 7 25 USAAD96090 1 19960628 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN SHORTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 962VJ 47507 EMERGENCY LIGHTS HAVE FAINT GLOW IN CEILING COMPANION WAY AND FIRST CLASS. REPAIRED SHORTED WIRE AT AFT COMPANION WAY E MERGENCY LIGHT, AND REPLACED POWER SUPPLY B5-24. (M) 2 L 7 2 4F A6WE 1996072500548 19960725 00548 WP 1996 7 25 USAAD96091 1 19960629 A 3397 WIRE DOUG DC9 DC931 3022065 WP LAV CEILING CHAFED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 951VJ 47576 EMERGENCY LIGHTS ARM AND CHARGE CIRCUIT BREAKER POPPED ON LANDING, WOULD NOT RESET. REPAIRED TWO CHAFED WIRES ABOVE RIG HT LAV CEILING. (M) 2 L 7 2 4F A6WE 1996072500549 19960725 00549 WP 1996 7 25 USAAD96092 1 19960629 A 3260 DOOR TARGET DOUG DC9 DC931 3022065 WP RT MLG OUT OF ADJUST A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 982VJ 48158 FLT 8560 - PIT-MCO - ON CLIMB, GEAR DOOR OPEN LIGHT ILLUMINATED. DIVERTED TO CLT. ADJUSTED RIGHT GEAR DOOR TARGET. PE RFORMED GEAR SWING, CHECKED GOOD. (M) 2 L 7 2 4F A6WE 1996072500550 19960725 00550 WP 1996 7 25 USAAD96093 1 19960630 A 2810 39205551 ROD DOUG DC9 DC931 3022065 WP FUEL PANEL FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 925VJ 48145 FLT 1200 - DCA-PVD - SLAT DISAGREE LIGHT CAME ON FOLLOWING SLAT RETRACTION. RETURNED TO FIELD. FOUND FUELING DOOR HAD RESTRICTED SLAT RETRACTION. REPAIRED FUELING DOOR, REPLACED ONE LATCH, AND HOLD OPEN ROD ON DOOR. (M) 2 L 7 2 4F A6WE 1996072500551 19960725 00551 WP 1996 7 25 USAAD96094 1 19960701 A 3350 AD20131A BATTERY DOUG DC9 DC931 3022065 WP COCKPIT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 935VJ 48115 COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES. (M) 2 L 7 2 4F A6WE 1996072500552 19960725 00552 EU 1996 7 25 USAAF96067 1 19960627 A 3230 200444004 UPLOCK STOP FOKKER F28 F28MK0100 4990807 EU RT MLG FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 861US 11297 PHL - FLT 701 - AFTER TAKEOFF, CREW HAD RIGHT LANDING GEAR SELECTOR LIGHT ON THE MFDU. FLIGHT RETURNED TO PHL AND LANDE D WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT MAIN LANDING GEAR UPLOCK STOP. (M) 2 L 7 2 4F RT 1996072500553 19960725 00553 EU 1996 7 25 USAAF96068 1 19960627 A 2612 51653027 FIRE DETECTION FOKKER F28 F28MK0100 4990807 EU APU MALFUNCTIONED A USAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 19 880US 12830 11331 MEM - FLT 1229 - ON FINAL TO MEM, CREW STARTED APU. AFTER NORMAL START, THE APU FIRE WARNING SOUNDED. THE APU SHUTDOWN AUTOMATICALLY AND THE FIRE BOTTLE ACTIVATED. CREW CONTINUED APPROACH AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF A FIRE. MAINTENANCE REPLACED THE FIRE DETECTION CONTROLLER. (M) 2 L 7 2 4F RT 1996072500554 19960725 00554 EU 1996 7 25 USAAF96069 1 19960629 A 3350 6104781 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 894US 11379 PIT - FOUND EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE RESET THE EMERGENCY LIGHT CIRCUIT BREAKERS AND REPLACED THE MAIN ENTRANCE DOOR EXIT SIGN BATTERY PACK. (M) 2 L 7 2 4F RT 1996072500555 19960725 00555 EU 1996 7 25 USAAF96070 1 19960630 A 3230 RETRACT MECH FOKKER F28 F28MK0100 4990807 EU NLG LACK OF LUBE A USAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 19 885US 11345 PIT - FL 400 - AFTER TAKEOFF, THE NOSE GEAR DID NOT RETRACT. CREW RECYCLED THE GEAR AND THE GEAR RETRACTED NORMALLY. F LIGHT CONTINUED TO PIT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE JACKED THE AIRCRAFT AND SWUNG THE GEAR SEVERAL TIMES. NO PROBLEMS WERE FOUND. THE GEAR WAS LUBRICATED AND THE AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT 1996072500556 19960725 00556 NM 1996 7 25 USAASB96093 1 19960530 A 3350 500000043 POWER SUPPLY BOEING 737 737201 1384454 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 247US 22754 ROC - MAINTENANCE FOUND THE AFT AISLE BULLNOSE EMERGENCY EXIT SIGN WOULD NOT ILLUMINATE. MAINTENANCE REPLACED THE POWER SUPPLY. (M) 2 L 7 2 4F A16WE 1996072500557 19960725 00557 NM 1996 7 25 USAASB96116 1 19960625 A 2121 6454051 FAN BOEING 737 7374B7 1384702 NM AIR COND BAY FAILED A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 19 429US 19986 24551 MCO - FLT 1981 - ON DESCENT TO MCO, CREW NOTICED A VERY STRONG ODOR. SMELLED LIKE HYDRAULIC FLUID ON A HOT DUCT. NO EM ERGENCY WAS DECLARED AND THE FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT AIR CONDITIONING REC IRCULATING FAN. OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A16WE 1996072500558 19960725 00558 1996 7 25 USSASB96112 4 19960617 A 3442 6225132108 RADAR TR UNIT BOEING 737 7373B7 1384580 NM NOSE COMP FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 530AU 34866 24412 PHL - FLT 164 - AFTER TAKEOFF FROM PHL, CAPTAIN LOST WEATHER RADAR. DUE TO WEATHER, FLIGHT WAS NOT ABLE TO CONTINUE TO BTV AND RETURNED TO PHL. FLIGHT LANDED WITH NO FURTHER INCIDENT. MX REPLACED WEATHER RADAR TRANSCEIVER. OPS CHECKED N ORMAL. (M) 2 L 7 2 4F RT A16WE 1996072500559 19960725 00559 NM 1996 7 25 W8PA960054 1 19960708 A 3350 BULB BOEING 737 7373B7 1384580 NM CABIN FAILED A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 947WP 23376 DURING SERVICE CHECK, FOUND FLOOR TRACK EMERGENCY EXIT LIGHT INOP AT ROW 15. RELAMPED LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A16WE 1996072500560 19960725 00560 EU 1996 7 25 WTAA960128 1 19960613 A 3230 7445B RESET VALVE BAG JETSTM JETSTM3101 1500215 EU LT MLG POPPED A WTAA O OTHER J WARNING INDICATION CL CLIMB 1 WP 17 427UE 811 SFO - LANDING GEAR WOULD NOT RETRACT ON INITIAL ATTEMPT. MAINTENACNE FOUND LANDING GEAR EMERGENCY EXTENSION RESET PIN P OPPED. RESET PIN. LANDING GEAR RETRACTION CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996072500561 19960725 00561 EU 1996 7 25 WTAA960132 1 19960622 A 7933 MS280343 OIL TEMP SENSOR BAG JETSTM JETSTM3101 1500215 EU LT ENGINE FAILED A WTAA O OTHER N FALSE WARNING CR CRUISE 1 WP 17 431UE 813 FAT - DURING FLIGHT, LEFT ENGINE OIL TEMPERATURE INDICATION REPORTED AT RED LINE. ALL OTHER ENGINE PARAMETERS NORMAL. C REW ACCOMPLISHED PRECAUTIONARY SHUTDOWN OF LEFT ENGINE. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPL ACED ENGINE OIL TEMPERATURE SENSOR. LEFT ENGINE INDICATING SYSTEM NORMAL DURING GROUND RUN. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 2 4T RT A21EU 1996072500562 19960725 00562 SO 1996 7 25 WTAA960133 1 19960627 A 3233 2060500005 ACTUATOR EMB 120 EMB120RT SO NLG LEAKING A WTAA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 WP 17 276UE 120067 FAT - NOSE GEAR WILL NOT RETRACT AFTER TAKEOFF. AIRCRAFT RETURNED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED N OSE GEAR RETRACTION JACK ACTUATOR. SYSTEM OPERATIONAL CHECK NORMAL DURING GEAR RETRACTION CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996072500563 19960725 00563 SO 1996 7 25 WTAA960134 1 19960627 A 3233 1959500007 ACTUATOR EMB 120 EMB120RT SO RT MLG OUT OF ADJUST A WTAA O OTHER J WARNING INDICATION TO TAKEOFF 1 WP 17 201YW 120201 SFO - AFTER TAKEOFF RIGHT MAIN LANDING GEAR INTRANSIT LIGHT WOULD NOT EXTINGUISH AFTER GEAR RETRACTION. AIRCRAFT RETURN ED TO STATION WITHOUT INCIDENT. MAINTENANCE ADJUSTED RIGHT MAIN LANDING GEAR ACTUATOR. SYSTEM OPERATIONAL CHECK NORMAL DURING GEAR RETRACTION CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996072500578 19960725 00578 EU 1996 7 25 96ZZZX3732 1 19960606 A 6410 355A12004004 BLADE SNIAS 350 AS350B 8680801 EU T/R PAINT DEPARTED A A FCYA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 WP 13 85GA 1426 3813 2362 AN APPROXIMATE 6 INCH SQUARE PIECE OF PAINT WAS SHED FROM THE POLY ABRASION STRIP TOWARD THE BLADE TIP DURING FLIGHT. A HIGH VIBRATION SET IN AND HELICOPTER LANDED IMMEDIATELY. CAUSE OF PROBLEM WAS DUE TO THE POLYURETHANE SHEET BECOMING S OFT AND GUMMY; THUS, PAINT COMES OFF READILY DUE TO LACK OF ADHESION. THE SOLUTION APPEARS TO BE REPLACEMENT OR REDESIG N OF MATERIAL DUE TO ITS SUSCEPTIBILITY OF THIS OCCURRENCE IN A HUMID ENVIRONMENT. 1 G 7 1 3U H9EU 1996072500580 19960725 00580 WP 1996 7 25 9615799905 1 19960719 A 7711 EPR LINE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D17 52049 NE NR 2 ENGINE BROKEN A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 955N 47160 696742 DURING TAKEOFF, THE LEFT ENGINE EPR INDICATION DROPPED FROM 1.97 TAKEOFF SETTING TO 1.7. CREW ABORTED TAKEOFF AND RETUR NED TO GATE WITHOUT INCIDENT. MAINTENANCE REPLACED BROKEN EPR PROBE LINE FOR NR 2 ENGINE, OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F A6WE E2EA 1996072500581 19960725 00581 WP 1996 7 25 9615809927 1 19960626 A 7332 FUEL PRESS SW DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7 52053 NE LT ENGINE FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 8920E 45835 653519 WHILE APPLYING TAKEOFF POWER, THE LEFT ENGINE FUEL FILTER PRESSURE DROP LIGHT ILLUMINATED. CREW ABORTED TAKEOFF AND RET URNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE REPLACED THE FUEL FILTER AND FUEL DIFFERENTIAL PRESSURE SWITCH. RAN EN GINE TO TAKEOFF POWER AND REINSPECTED FUEL FILTER. OPERATIONAL CHECK OK, NO CONTAMINATION FOUND. 2 L 7 2 4F 4 F A6WE E2EA 1996072500582 19960725 00582 NE 1996 7 25 9615812762 2 19960717 A 7230 COMPRESSOR BOEING 727 7272M7 138407S NM PWA JT8 JT8D17R 52049 NE NR 1 ENGINE STALLED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 01 722RW 21201 689950 WHILE APPLYING POWER FOR TAKEOFF, THE NR 1 ENGINE HAD A COMPRESSOR STALL. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE PERFORMED THE FOLLOWING FUNCTIONS ON NR 1 ENIGNE, REPLACED PRBC, CHECKED ENGINE INLET AN D EXHAUST AND DRAINED FUEL CONTROL MOISTURE TRAP. 2 L 7 3 4F 4 F A3WE E2EA 1996072500583 19960725 00583 NM 1996 7 25 9615832299 1 19960703 A 7603 CONTROL CABLE BOEING 727 727251 138408H NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE BROKEN A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN O OTHER CL CLIMB 1 GL 01 299US 22153 700518 DURING CLIMBOUT, THE NR 1 ENGINE THRUST LEVER CABLE BROKE AS THE CREW WAS DECREASING POWER. THIS CAUSED ENGINE TO INCRE ASE TO FULL POWER. CREW THEN PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT IN CIDENT. MAINTENANCE REPLACED THE NR 1 ENGINE THRUST LEVER CABLE, RIGGED AND OPERATIONAL CHECK OK. 2 L 7 3 4F 4 F A3WE E2EA 1996072500584 19960725 00584 WP 1996 7 25 9615849611 1 19960722 A 3610 AUGMENTATION VLV DOUG DC9 DC932 3022066 WP AFT FUSELAGE FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 611NA 47435 TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT AUGMENTATION VALVE AND BOTH LEFT AND RIGHT OUTBOARD AUGMENTATION VALVE CLAMPS, OPERATIONAL C HECK NORMAL. 2 L 7 2 4F A6WE 1996072500585 19960725 00585 WP 1996 7 25 9615859613 1 19960723 A 3350 LIGHTS DOUG DC9 DC932 3022066 WP CABIN MALFUNCTIONED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 613NW 47438 ALL EMERGENCY LIGHTS, SIGNS AND PATH LIGHTING BEGAN FLICKERING DURING FLIGHT. MAINTENANCE INSPECTED WIRING AT OVERHEAD COCKPIT FORWARD FLIGHT ATTENDANT SWITCH AND AT CONNECTOR P1-4009, ALL CHECKED NORMAL. DISCREPANCY COULD NOT BE DUPLICAT ED. 2 L 7 2 4F A6WE 1996072500586 19960725 00586 NM 1996 7 25 96UAL900476 1 19960624 A 2612 FIRE SENSOR BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE WHEEL WELL MALFUNCTIONED A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 608UA 21869 LANDED UNDER AMBER ALERT DUE TO WHEEL WELL FIRE WARNING INDICATION. *S/D* CAUSE MAY HAVE BEEN A FAULTY SENSOR INDICAT ION, UNABLE TO DUPLICATE THIS DISCREPANCY. DURING MM PROCEDURE 05-51-35, OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 1996072500587 19960725 00587 WP 1996 7 25 96UAL900482 1 19960624 A 3350 CONNECTOR DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1855U 47837 EEL FLOOR LIGHTING INOPERATIVE AT ROWS 9 TO 16. *S/D* SECURED EEL LIGHT CONNECTION AFT OF 2R LAVATORY. 2 L 7 3 4F 4 F A22WE E23EA 1996072500588 19960725 00588 NM 1996 7 25 96UAL900486 1 19960625 A 2820 DEU HONEYWELL S345T000227 BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE RIGHT MALFUNCTIONED A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 619UA 21879 UNWANTED FUEL TRANSFER OCCURRED, THE RIGHT FUEL QUANTITY INCREASED BY AS MUCH AS 1,400 LBS WITH CROSS FEED CLOSED. *S/ D* A DENSITOMETER ELECTRONIC UNIT MALFUNCTIONED AND WAS REPLACED, OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 1996072500589 19960725 00589 NM 1996 7 25 96UAL900489 1 19960626 A 2560 EVAC HORN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FLIGHT DECK MALFUNCTIONED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 FLIGHT DECK EMERGENCY EVACUATION HORN DOES NOT TEST. *S/D* PANEL ASSY WAS REMOVED AND REPLACED. REMOVED UNIT WAS TEST ED IN SHOP AND NO FAULT WAS FOUND. 2 L 7 4 4F 4 F RT A20WE E24NE 1996072500590 19960725 00590 NM 1996 7 25 96UAL900534 1 19960715 A 2421 745329C IDG BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 FAILED A UALA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CR CRUISE 1 WP 29 643UA 25093 THE NUMBER 2 INTEGRATED DRIVE GENERATOR FAILED. AIRCRAFT DIVERTED TO JFK. *S/D* A HYDRAULIC LOG FAILURE OCCURRED IN T HE IDG. HEAVY CYLINDER BLOCK WEAR ALSO CONTRIBUTED TO A LOSS OF OIL CHARGE PRESSURE AND AN INABILITY TO MAINTAIN FREQUE NCY. THE IDG WAS REPLACED. 2 L 7 2 4F 4 F RT A1NM E24NE 1996072500591 19960725 00591 NM 1996 7 25 96UAL900535 1 19960715 A 5270 DOOR LIGHT ELDEC 841502 BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CARGO DOOR ILLUMINATED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 652UA 058 25390 AIRCRAFT RETURNED TO IAD DUE TO CARGO DOOR LIGHT. *S/D* BUILT IN TEST EQUIPMENT INDICATED LOGIC CARD 3 FAILED IN THE P ROXIMITY SWITCH ELECTRONIC UNIT. REPLACED LOGIC CARD, OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 1996072500592 19960725 00592 NM 1996 7 25 96UAL900536 1 19960715 A 5510 BACB30NE3H25 BOLT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LT HORZ STAB SHEARED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7464U 21918 DURING REPLACEMENT OF HORIZONTAL STAB PIVOT BEARINGS, FOUND ANTI-ROTATION PLATE CROSS BOLT SHEARED ON LT STAB FITTING. A NTI-ROTATION PLATES DISLODGED AND PIVOT BUSHING ROTATED IN HINGE FITTING BORE CREATING GOUGE IN OUTBOARD FACE OF LT PIVO T FITTING. ROTATION OF BEARING CAUSED STEPPING OF I/B AND O/B FACES OF LT FITTING. RT FITTING ALSO INCURRED MINOR STEP PING AROUND BORE UNDER BUSHING FLANGES. CAUSED BY SHEARED ANTI-ROTATION PLATE CROSS BOLT. THE GOUGE WAS REMOVED BY MEA NS OF A SPOT FACE AND INSTALLATION OF A PLUG. STEPPING AROUND BORE REMOVED BY INCREASING THE DEPTH OF THE ORIGINAL SPOT FACE. 2 L 7 3 4F 4 F A3WE E2EA 1996072500593 19960725 00593 NE 1996 7 25 96UAL900537 2 19960715 A 7321 FUEL CONTROL HAMSTD 7791005 BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE MALFUNCTIONED A UALA E ENGINE SHUTDOWN J R Y WARNING INDICATION PARTIAL RPM/PWR LOSS ENGINE STOPPAGE DE DESCENT 1 WP 29 551UA F19713 25399 TOP OF DESCENT, LEFT ENGINE VALVE LIGHT ACTIVATED. NO RESPONSE WITH THROTTLE MOVEMENT. RESTARTED LEFT ENGINE. DURING SHORT FINAL APPROACH AGAIN NO RESPONSE FROM LEFT ENGINE. TAXIED TO GATE ON ONE ENGINE. O-RINGS USED TO SEAL THE MINIM UM PRESSURE SHUTOFF VALVE (MPSOV) AGAINST THE FUEL CONTROL HOUSING WERE DAMAGED. FCU WAS REPLACED. OPERATION CHECKS NO RMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996072500594 19960725 00594 NM 1996 7 25 96UAL900538 1 19960715 A 5200 DOOR SEALS BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE DOORS LEAKING A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 9067U 19948 LOUD SQUEAL AT DOOR, TWO RIGHT AND OUTFLOW VALVE IS FULL CLOSED. DUE TO MANY AIR LEAKS AROUND DOORS AND DRAIN VALVES UN ABLE TO PRESSURIZE AIRCRAFT. *S/D* FOUND AIR LEAKS AROUND DOOR ONE LEFT, TWO RIGHT AND LEFT. REPLACED RADIO RACK COOL ING VALVE AND ADJUSTED DOOR SEALS. 2 L 7 2 4F 4 F A16WE E2EA 1996072500595 19960725 00595 NE 1996 7 25 96UAL900539 2 19960715 A 7230 750701 COMPRESSOR BLADE BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE NR 2 ENGINE FAILED A UALA A UNSCHED LANDING R E C PARTIAL RPM/PWR LOSS VIBRATION/BUFFET F.O.D. CR CRUISE 1 WP 29 9040U 1930 19078 655904 AT FLIGHT LEVEL 330, MACH .75 AND 1.85 EPR, NUMBER TWO ENGINE MADE A LOUD THUMP NOISE AND LOST HALF ITS POWER. THERE WA S A STEADY VIBRATION. PULLED NUMBER TWO ENGINE THROTTLE BACK TO IDLE, ELECTED NOT TO SHUT IT DOWN. COCKPIT INDICATIONS WERE NORMAL EXCEPT FOR LOSS OF EPR. *S/D* BIRD INGESTION AND C-1 BLADE AIRFOIL TIP FAILURE RESULTED IN EXTENSIVE DOWN STREAM DAMAGE IN BOTH COMPRESSORS. 2 L 7 2 4F 4 F A16WE E2EA 1996072500596 19960725 00596 NE 1996 7 25 96UAL900540 2 19960715 A 7230 1B6709 COMPRESSOR BLADE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT ENGINE BROKEN A UALA C D ABORTED TAKEOFF RETURN TO BLOCK E J R VIBRATION/BUFFET WARNING INDICATION PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 29 523UA 14453 24932 CREW OBSERVED YELLOW FLASH ACCOMPANIED WITH A LOUD BANG ON RIGHT SIDE OF AIRCRAFT. ABORTED TAKEOFF AT 100 KTS. BORESCO PE REVEALED ENGINE NOT SERVICEABLE. *S/D* FOUR BROKEN 9TH STAGE COMPRESSOR BLADES. SCRAPPED ALL THE 6TH THROUGH 17TH STAGE COMPRESSOR BLADES AND REPLACED WITH NEW. 2 L 7 2 4F 4 F RT A2NM E17NE 1996072500597 19960725 00597 NM 1996 7 25 96UAL900541 1 19960715 A 2750 RETRACT MECH BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE INBD TE FLAP MALFUNCTIONED A UALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 7463U 21917 INBOARD TRAILING EDGE FLAPS WOULD NOT EXTEND. 2 L 7 3 4F 4 F A3WE E2EA 1996072500598 19960725 00598 WP 1996 7 25 96UAL900542 1 19960715 A 3350 58791 JUMPER CHORD DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1857U 46986 EEL LIGHTING INOPERATIVE ON RT SIDE FROM FORWARD GALLEY THROUGH B-SECTION OF COACH. REPLACED JUMPER CHORD FOR RIGHT HAN D SECTION B. 2 L 7 3 4F 4 F A22WE E23EA 1996072500599 19960725 00599 NE 1996 7 25 96UAL900543 2 19960716 A 7230 1B6509 COMPRESSOR BLADE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE BROKEN A UALA A UNSCHED LANDING E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 583UA 12883 26705 ON CLIMBOUT, CREW HEARD LOUD BANG AND DETECTED A SLIGHT YAW AS GEAR RETRACTED. NO ADVERSE ENGINE INDICATIONS. PASSENGE RS ON LEFT OBSERVED FIRE FLASH. *S/D* BROKEN 9TH STAGE COMPRESSOR BLADE. SCRAPPED THE 6TH THROUGH 17TH COMPRESSOR BLA DES AND REPLACED WITH NEW, OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996072500600 19960725 00600 WP 1996 7 25 96UAL900544 1 19960716 A 2170 COALESCER BAG DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN DIRTY A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 1838U 46632 BURNING SMELL AFTER TAKEOFF, RETURNED TO CLE. *S/D* ISOLATED SMELL TO NR 1 PNEUMATIC SYSTEM. FOUND NO RESIDUE IN SYST EM DUCTING OR VALVES. BURNED OUT THE NR 1 SYSTEM AND REPLACED COALESCER BAG, NO REOCCURANCE. 2 L 7 3 4F 4 F A22WE E23EA 1996072500601 19960725 00601 1996 7 25 96UAL900545 4 19960716 A 2565 SLIDE AIR CRUISER D29835103 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN LEAKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7260U 17697778 21407 DURING SHOP OVERHAUL OF SLIDE, REMOVED FOR OVERHAUL TIME EXPIRATION INFLATABLE PORTION DEVELOPED A 3 INCH SEAM LEAK UNDE R THE SLIDE. SCRAPPED SLIDE. 2 L 7 3 4F 4 F A3WE E2EA 1996072500602 19960725 00602 NE 1996 7 25 96UAL900546 2 19960716 A 7230 1B6509 COMPRESSOR BLADE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE BROKEN A UALA A UNSCHED LANDING E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CR CRUISE 1 WP 29 576UA 11874 26690 LEFT ENGINE HAD 2 COMPRESSOR STALLS AT ALTITUDE. FLIGHT DIVERTED TO ICT. *S/D* BROKEN 9TH STAGE COMPRESSOR BLADE. SC RAPPED ALL 6TH THROUGH 17TH STAGE BLADES AND REPLACED WITH NEW. 2 L 7 2 4F 4 F RT A2NM E17NE 1996072500604 19960725 00604 NM 1996 7 25 96UAL900548 1 19960717 A 3244 TIRE BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE LT MLG FAILED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK E VIBRATION/BUFFET TO TAKEOFF 1 WP 29 9068U 19949 ABORTED TAKEOFF AT 115 KNOTS BECAUSE IT FELT LIKE A BLOWN TIRE AND AIRCRAFT YAW TO THE LEFT. 2 L 7 2 4F 4 F A16WE E2EA 1996072500605 19960725 00605 NM 1996 7 25 96UAL900549 1 19960717 A 5270 PSEU ELDEC 849704 BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CARGO DOOR FAILED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 660UA 508 27115 AIRCRAFT RETURNED TO IAD DUE TO A FORWARD CARGO DOOR LIGHT. SUPPLEMENTAL DATA UPDATE: PSEU BITE SHOWED BOTH LOGIC CARD 3 (005) AND DRIVER CARD (007) FAILED. REPLACED THE PSEU. OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 1996072500606 19960725 00606 NM 1996 7 25 96UAL900550 1 19960717 A 2530 OVEN SELL 8055510000 BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE GALLEY SMOKING A UALA F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 652UA 89080138 25390 USED FIRE EXTINGUISHER FOR SMOKE AND FUMES FROM GALLEY OVEN. FOUND MELTED PLASTIC MATERIAL ON HEATING ELEMENT GRILL IN OVEN. OVEN OPERATED NORMALLY AFTER PLASTIC MATERIAL WAS REMOVED. 2 L 7 2 4F 4 F RT A1NM E24NE 1996072500607 19960725 00607 NM 1996 7 25 96UAL900551 1 19960717 A 5310 STRUCTURE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 847-1016 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 331UA 24192 LAVATORY TRUCK BACKED INTO THE AIRCRAFT AND DAMAGED THE FUSELAGE BELLY SKIN, STRINGERS, STRINGER TIES AND FRAMES BETWEEN BODY STATION 847 TO 1016 OF STRINGER 26 LEFT AND 26 RIGHT. ALL DAMAGED PARTS WERE EITHER REPLACED OR REPAIRED PER APPL ICABLE STRUCTURE REPAIR MANUAL AND ENGINEERING VARIANCE AUTHORITY. 2 L 7 2 4F 4 F RT A16WE E2GL 1996072500608 19960725 00608 WP 1996 7 25 96UAL900552 1 19960717 A 2611 CM376AS15 LAMP DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 2 SMOKE DET FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1843U 46636 NR 2 AFT CARGO SMOKE DETECTOR WOULD NOT TEST. *S/D* TEST LAMP WAS BURNED OUT, REPLACED LAMP. 2 L 7 3 4F 4 F A22WE E23EA 1996072500609 19960725 00609 NM 1996 7 25 96UAL900553 1 19960717 A 3350 LIGHT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FLIGHT DECK INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7271U 21418 EMERGENCY LIGHT OUT OVER FLIGHT DECK DOOR. 2 L 7 3 4F 4 F A3WE E2EA 1996072500610 19960725 00610 NE 1996 7 25 96UAL900554 2 19960718 A 7250 761702 T2 BLADE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE FRACTURED A UALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 29 7463U 17624 21917 NR 3 ENGINE FAILED AT 800 FEET ON TAKEOFF. EGT PEGGED, RPM DECAY, OIL QUANTITY DROPPED TO ONE GALLON AND OIL PRESSURE D ROPPED TO ZERO. RETURNED TO DEN. T-2 BLADE FAILURE DUE TO NOTCH BREAK-OUT AND RESULTANT CYCLE FATIGUE. THE BLADE FAIL URE WAS THE CAUSE OF THE DISC BLADE FIR TREE POST-FAILURE. EXTENSIVE DOWN STREAM DAMAGE IN THE N1 TURBINE AND EXHAUST C ASE. UNDER INVESTIGATION. 2 L 7 3 4F 4 F A3WE E2EA 1996072500611 19960725 00611 NM 1996 7 25 96UAL900555 1 19960718 A 2121 FAN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 306UA 23667 EXHAUST COOLING FAN OFF LIGHT ILLUMINATED ON CLIMBOUT. LIGHT STAYED OFF WHEN SWITCHED TO ALT FAN. LIGHT STAYED ON UNTI L DESCENT WHEN BOTH NORMAL AND ALT FANS WORKED OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1996072500612 19960725 00612 NE 1996 7 25 96UAL900556 2 19960718 A 7530 3214446 HI STAGE VALVE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LT ENGINE INOPERATIVE A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 354UA 24360 AIRCRAFT WOULD NOT PRESSURIZE ON ONE PACK, OUTFLOW VALVE SHOWED CLOSED. *S/D* REPLACED LEFT HAND ENGINE HIGH STAGE VAL VE PER MM, HIGH STAGE VALVE FOUND INOP. RAN ENGINES AND PRESSURIZED AIRCRAFT, AIRCRAFT PRESSURE CONTROL SYSTEM CHECKED NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 1996072500613 19960725 00613 NM 1996 7 25 96UAL900557 1 19960719 A 3350 LAMP BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE CABIN NOT SECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 4723U 19882 NR 1 LEFT OVERWING EMERGENCY LIGHT HAS FORWARD LAMP INOP. LAMP FOUND UNSECURED. SECURED LAMP, OPS CHECKS GOOD. 2 L 7 4 4F 4 F A20WE E20EA 1996072500615 19960725 00615 WP 1996 7 25 ABXA9600601 1 19960722 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 903AX 47427 ON PREDEPARTURE CHECK, EMERGENCY LIGHTS DIM. REPLACED EMERGENCY LIGHT BATTERIES IAW DC-9 SUPP M/M 33-50. 2 L 7 2 4F A6WE 1996072500616 19960725 00616 NM 1996 7 25 CALA9601048 1 19960719 A 3397 WIRE BOEING 757 757224 1384958 NM CABIN BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 33103 27293 INSPECTION FOUND SEAT 28 ABC EMERGENCY LIGHT INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE LEADING TO LAMP ASSEMBLY OF S EAT 28 ABC. THE WIRE WAS REPAIRED AND OPERATION CHECKED GOOD. 2 L 7 2 4F RT A2NM 1996072500617 19960725 00617 NM 1996 7 25 CALA9601049 1 19960723 A 3234 S60252 SELECT VALVE BOEING 727 727232 1384082 NM LANDING GEAR INOPERATIVE A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 45793 51644 1015 20647 THE TAIL SKID LIGHT REMAINED ILLUMINATED AFTER TAKEOFF. THE GEAR WAS CYCLED, BUT THE LIGHT WOULD NOT EXTINGUISH. THE LE FT AND RIGHT MLG RED AND GREEN LIGHTS REMAINED ILLUMINATED WITH GEAR HANDLE IN THE OFF POSITION. ALL THREE GEAR DOOR LI GHTS ALSO REMAINED ILLUMINATED. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND T HE MLG SELECT VALVE AT FAULT. THE MLG SELECT VALVE WAS REMOVED AND REPLACED IAW MM 32-31-31, PAGE 401, LEAK AND OPERATI ONAL CHECKS WERE GOOD. 2 L 7 3 4F A3WE 1996072500618 19960725 00618 WP 1996 7 25 CALA9601050 1 19960722 A 3233 39281375001 CYLINDER DOUG DC9 DC982 3022082 WP NLG INOPERATIVE A CALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 09 92874 28159 7794 49122 THE NOSE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED WHEN GEAR WAS EXTENDED FOR LANDING. THE GEAR WAS CYCLED AND THE RED LIGHT EXTINGUISHED WITH THE GREEN INDICATION LIGHT ILLUMINATING. THE AIRCRAFT HAD A BRIEF HISTORY OF THE NLG RED LIGHT REMAINING ILLUMINATED AFTER GEAR EXTENSION. MAINTENANCE REMOVED AND REPLACED THE NLG RETRACT CYLINDER IAW MM 32-32-06, PAGE 201, LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F A6WE 1996072500619 19960725 00619 NM 1996 7 25 DHL96703002 1 19960719 A 3610 39271611 MOD VALVE BOEING 727 72730C 1384009 NM NR 1 ENGINE MALFUNCTIONED A T DHLA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 703DH 19010 AIRCRAFT WOULD ONLY PRESSURIZE TO .5 PSI DIFFERENTIAL 8,500 FEET CABIN ALT AT 10,000 AIRCRAFT ALT, NOTED 26 PSI SPLIT ON DUCT PRESSURE GAUGES. REMOVED AND REINSTALLED LEFT OUTFLOW VALVE. REMOVED AND REPLACED NR 1 ENG 13TH STAGE MOD VALVE AND LEFT PACK 35 DEG CONTROL VALVE. GROUND RAN ENG, OPS CHECK NORM. 2 L 7 3 4F A3WE 1996072500620 19960725 00620 WP 1996 7 25 SCNA96201 1 19960721 A 3260 368658188113 INDICATOR DOUG DC10 DC1030F 3023504 WP CTR GEAR INOPERATIVE A SCNA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 GL 15 601GC 47921 FOUND CENTER LANDING GEAR INDICATION INOP AT PILOTS AND FLIGHT ENGINEERS STATIONS. REPLACED CENTER GEAR ANNUNCIATOR ON FLIGHT ENGINEER PANEL AND RELAMPED FIRST OFFICERS CENTER GEAR LIGHT. 2 L 7 3 4F RT A22WE 1996072500621 19960725 00621 NE 1996 7 25 VSTA9607004 2 19960723 A 7532 754317 BLEED VALVE BOEING 737 737204 1384458 NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE MISSING A VSTA K NONE O OTHER IN INSP/MAINT 1 WP 07 312VA 20236 665632 EPR CHECK READINGS NR 2 ENGINE UNSATISFACTORY, 13TH STAGE COMPRESSOR BLEED VALVE BROKE LOOSE FROM NR 2 ENGINE COMPRESSOR CASE. ENGINE CHANGE REQUIRED. 2 L 7 2 4F 4 F A16WE E2EA 1996072900001 19960729 00001 NM 1996 7 29 RAAAB196008 1 19960529 A 3350 873100112 LIGHT BOEING 727 72722C 138400F NM CABIN FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 RIGHT FWD OVERWING EMERGENCY EXIT EGRESS IDENTIFIER RED TRANSMITTER LIGHT STAYS ON. REPLACED LIGHT ASSY. (M) 2 L 7 3 4F A3WE 1996072900002 19960729 00002 NM 1996 7 29 RAAAB196009 1 19960512 A 2910 6517844333 LINE BOEING 727 72722C 138400F NM A HYD SYST CRACKED A RAAA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 AL 03 831RV 54486 19093 HYD A SYSTEM LOST ALL FLUID INFLIGHT CX1-HL LEG. REPLACED CRACKED NR 1 ENGINE HYD PUMP PRESS SUPPLY LINE AT A SYSTEM MO DULE. (M) 2 L 7 3 4F A3WE 1996072900003 19960729 00003 NM 1996 7 29 RAAAB196010 1 19960628 A 5330 SKIN BOEING 727 72722C 138400F NM NOSE W/W CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 54598 19093 DURING SCHEDULED S1 INSPECTION PER CARD S1-11101, FOUND 2 ADJACENT CRACKS EMANATING FROM HI-LOCK FASTENERS IN NOSE W/W U PPER SKIN BS 259.5, RBL 21 AND 22. REPAIRED PER SRM 53-10-9. (M) 2 L 7 3 4F A3WE 1996072900004 19960729 00004 NM 1996 7 29 RAAAB196011 1 19960628 A 5330 SKIN BOEING 727 72722C 138400F NM NOSE W/W CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 54598 19093 DURING SCHEDULED S1 INSPECTION PER CARD S1-11101, FOUND 2 ADJACENT CRACKS EMANATING FROM HI-LOCK FASTENERS IN NOSE W/W U PPER SKIN BS 259.5, LBL 21 AND 22. REPAIRED PER SRM 53-10-9. (M) 2 L 7 3 4F A3WE 1996072900005 19960729 00005 NM 1996 7 29 DHL96724004 1 19960716 A 7722 EGT INDICATION BOEING 727 727228 NM NR 2 ENGINE MALFUNCTIONED A T DHLA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 724DH 19862 ON DEPARTURE, NR 2 ENGINE REACHED TEMP LIMITS PRIR TO REACHING T/O. THRUST WAS REDUCED TO 1.85 EPR TO MAINTAIN TEMP LIM ITS. ALL OTHER ENGINE INDICATION SHOWED NORMAL. ON CLIMBOUT TEMP STAYED AT MAX, WITH CHARTED CLIMB THRUST. COULD NOT DUPLICATED, SWAPPED NR 2 AND NR 3 INDICATORS FOR TROUBLESHOOTING. RAN AT TAKEOFF POWER FOR 3 MINUTES, MAX EGT WAS 565 D EGREES. 2 L 7 3 4F A3WE 1996080200001 19960802 00001 WP 1996 8 2 9615829301 1 19960720 A 5320 FITTING DOUG DC9 DC982 3022082 WP FS 1338 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 301RC 48054 DURING H-CHECK, FOUND CORROSION IN THE FS 1338 FRAME GUSSET FTTTING AT LBL 58. REPLACED FITTING (P/N 5913700-1) PER SRM 51-01, PAGE 1. 2 L 7 2 4F A6WE 1996080200002 19960802 00002 WP 1996 8 2 9615861141 1 19960703 A 5730 SKIN DOUG DC10 DC1040 3023508 WP WS 467 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 141US 46750 DURING L-CHECK, FOUND A CRACK IN THE LEFT WING LEADING EDGE SKIN AT THE ANTI-ICE DUCT DOOR CUTOUT XOS 467. REPAIRED SKI N PER EA 11-105129. 2 L 7 3 4F A22WE 1996080200003 19960802 00003 NM 1996 8 2 9615875525 1 19960711 A 5315 FLOOR BEAM BOEING 757 757251 1384970 NM FS 365 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 525US 23619 DURING P-CHECK, FOUND CORROSION ON THE BS 365 FLOOR BEAM UPPER CHORD FROM BL ZERO - RBL 52. REPAIRED CHORD (P/N 141N511 2) PER EA 55-074949. 2 L 7 2 4F RT A2NM 1996080200004 19960802 00004 WP 1996 8 2 9615881158 1 19960711 A 5730 SKIN DOUG DC10 DC1040 3023508 WP WS 610 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 158US 46767 DURING L-CHECK, FOUND A CRACK IN THE LEFT WING FIXED LEADING EDGE SKIN AT XOS 610. REPAIRED SKIN (P/N ARB2887-501) PER EA 11-105353. 2 L 7 3 4F A22WE 1996080200005 19960802 00005 WP 1996 8 2 9615891158 1 19960711 A 5730 SKIN DOUG DC10 DC1040 3023508 WP WS 610 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 158US 46767 DURING L-CHECK, FOUND A CRACK IN THE RIGHT WING FIXED LEADING EDGE SKIN AT XOS 610. REPAIRED SKIN (P/N ARB2887-502) PER EA 11-105354. 2 L 7 3 4F A22WE 1996080200006 19960802 00006 NM 1996 8 2 9615902713 1 19960715 A 7120 MOUNT FITTING BOEING 727 7272S7 138407Z NM NR 2 ENGINE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 716RC 22021 DURING H-CHECK, FOUND CORROSION ON THE NR 2 ENGINE AFT MOUNT FITTING. REPLACED FITTING PER MM 71-21-01, PAGE 404. 2 L 7 3 4F A3WE 1996080200007 19960802 00007 WP 1996 8 2 9615919301 1 19960716 A 5320 FITTING DOUG DC9 DC982 3022082 WP FS 826/845/864 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 301RC 48054 DURING H-CHECK, FOUND CORROSION AND CRACKS IN THE RBL 21 SEAT TRACK MOUNT FITTINGS AT FS 826, 845, AND 864. REPLACED FITTINGS (P/N'S 3925817-502, 3925816-502, AND 3925816-2) PER SRM 51-01. 2 L 7 2 4F A6WE 1996080200008 19960802 00008 WP 1996 8 2 9615929921 1 19960718 A 5320 FITTING DOUG DC9 DC932 3022066 WP LT MLG WW CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 943N 47647 DURING H-CHECK, FOUND A 1.50 INCH CRACK IN THE LEFT WHEELWELL KEEL TO SLANTED PRESSURE PANEL SUPPORT FITTING. REPLACED FITTING PER SRM 53-01, PAGE 1. 2 L 7 2 4F A6WE 1996080200009 19960802 00009 WP 1996 8 2 9615939856 1 19960718 A 5210 FITTING DOUG DC9 DC951 3022051 WP PAX DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 765NC 47718 DURING H-CHECK, FOUND A CRACK IN THE MAIN ENTRY DOOR NR 3 BEAM FORWARD END FITTING. REPLACED FITTING. 2 L 7 2 4F A6WE 1996080200010 19960802 00010 WP 1996 8 2 9615949301 1 19960719 A 5320 FITTING DOUG DC9 DC982 3022082 WP FS 1333 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 301RC 48054 DURING H-CHECK, FOUND CORROSION ON THE LONGERON 28L END FITTING AT FS 1333. REPLACED FITTING (P/N 4917650-1) PER SRM 51 -01. 2 L 7 2 4F A6WE 1996080200011 19960802 00011 WP 1996 8 2 9615959995 1 19960719 A 5320 FITTING DOUG DC9 DC931 3022065 WP FS 579 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8978E 47327 DURING M-CHECK, FOUND A CRACK IN THE FS 579 FRAME FITTING LEFT SIDE. REPLACED FITTIN 'G' PER SRM'S 51-10-3 AND 51-30-0. 2 L 7 2 4F A6WE 1996080200012 19960802 00012 WP 1996 8 2 9615969944 1 19960723 A 3310 BA17011 BALLAST DOUG DC9 DC931 3022065 WP COCKPIT FAILED A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 01 1309T 47316 DURING APPROACH INTO ORD, FLIGHT CREW SMELLED AN ELECTRICAL ODOR IN COCKPIT. AN EMERGENCY WAS DECLARED AND OXYGEN MASKS WERE UTILIZED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED FORWARD NOSE COMPARTMENT, E/E COMPARTMENT, AND FORWARD GALLEY FOR EVIDENCE OF ELECTRICAL FIRE OR MELTING WIRE COVERINGS OR SHORTING CONDITIONS. NO PROBLEMS WERE FOUN D. AN ELECTRICAL ODOR WAS FOUND TO BE COMING FROM SIDE PANEL UNDER CAPTAIN'S FLIGHT BAG STORAGE AREA. REPLACED BALLAST FOR GLARESHIELD FLUORESCENT LIGHTS. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996080200013 19960802 00013 EU 1996 8 2 9615973211 1 19960724 A 3350 321454 POWER SUPPLY AIRBUS 320 A320211 3930320 EU CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 311US 125 DURING LINE MAINTENANCE, THE EMERGENCY LIGHTS TEST FAULTS AFT LT BAT CAP. REPLACED POWER SUPPLY UNIT. OPERATIONAL CHEC K OK. 2 L 7 2 4F RT A28NM 1996080200014 19960802 00014 1996 8 2 9615989604 4 19960724 A 3442 20671570153 TRANSCEIVER DOUG DC9 DC932 3022066 WP FWD FUSELAGE FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 604NW 13540 298 47222 WEATHER RADAR SYSTEM FAILED ON TAKEOFF ROLL. ABORTED TAKEOFF BETWEEN 50-60 KNOTS. MAINTENANCE REPLACED RADAR TRANSCEIV ER. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996080200015 19960802 00015 WP 1996 8 2 9615999952 1 19960724 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 916RW 47144 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERIES IN POWER SUPPLY. OP ERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996080200016 19960802 00016 WP 1996 8 2 9616009910 1 19960724 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 960N 47256 DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPAIRED LOOSE GROUND CONNECTION. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996080200017 19960802 00017 NM 1996 8 2 96FDEA01126 1 19960613 A 5711 6516233 SPAR CHORD BOEING 727 727173C 1384059 NM WS 520-526 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 199FE 19509 NR 0490 AND 009. LEFT WING AFT UPPER SPAR CHORD VERTICAL LEG HAS CRACK BETWEEN NR 2 AND NR 3 SPOILERS. REMOVED DAMAGE FROM LEFT WING UPPER REAR SPAR STA 531 - 539. FABRICATED AND INSTALLED REPAIR PER FEDEX SRM 57-10-6, MM 27-61-0, MM 28- 1-0. 2 L 7 3 4F A3WE 1996080200018 19960802 00018 NM 1996 8 2 96FDEA01284 1 19960724 A 5754 65162267A BONDING JUMPER BOEING 727 7272D4 138407U NM NR 2 LE FLAP CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 NR 0261 003. CORROSION AROUND NR 2 K-FLAP OUTBOARD LOWER BONDING JUMPER UPPER ATTACH POINT. REPAIRED NR 2 K-FLAP OUTBO ARD LOWER BONDING JUMPER UPPER ATTACH POINT IAW SRM 57-50-03. MOVED ATTACH POINT IAW SRM 27-57-010C. 2 L 7 3 4F A3WE 1996080200019 19960802 00019 NM 1996 8 2 96FDEA01285 1 19960724 A 5320 651862216 BEAR STRAP BOEING 727 727173C 1384059 NM BS 1075-1160 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 199FE 19509 NR 0540 019. CORROSION C53-113-01(2). FOUND ON BEAR STRAP AND STAINLESS STEEL DOUBLER FROM BS 1075 - 1160, STR 225R W L 148.5. ****S/D***** COMING. 2 L 7 3 4F A3WE 1996080200020 19960802 00020 NM 1996 8 2 96FDEA01286 1 19960724 A 5313 65258113 LONGERON BOEING 727 72722 1384002 NM BS 1110 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 NR 0729 038. WHILE WORKING NR 0312, DISCOVERED CRACK IN FORWARD MOST FASTENER HOLE OF LONGERON AT BS 1110, STR 27R. * **S/D**** COMING. 2 L 7 3 4F A3WE 1996080200021 19960802 00021 NM 1996 8 2 96FDEA01287 1 19960723 A 5320 69463461 INTERCOSTAL BOEING 727 7272D4 138407U NM BS 720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 287FE 21849 NR 01148 022. CORROSION C53-113-01(1) IN THE FORWARD CARGO BAY ON INTERCOSTAL BS 720, WL 148, LBL 10. ****S/D***** C OMING. 2 L 7 3 4F A3WE 1996080200022 19960802 00022 NE 1996 8 2 CALA9601051 2 19960723 A 7250 772203 T3 BLADE DOUG DC9 DC981 3022081 WP PWA JT8 JT8D217A 52053 NE NR 1 ENGINE BROKEN A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 16883 26704 4462 48073 717392 THE NR 1 ENGINE FAILED WITH LOSS OF OIL WHILE EN ROUTE. THE AIRCRAFT WAS DIVERTED TO JAX WHERE IT LANDED WITHOUT INCIDE NT. MAINTENANCE FOUND METAL IN THE NR 1 ENGINE TAILPIPE. THE NR 1 ENGINE WAS REMOVED AND REPLACED. THE SDR WILL REMAI N OPEN FOR PART INFORMATION PENDING INVESTIGATION. *S/D* SHOP FINDINGS REVEALED A BROKEN T-3 BLADE. 2 L 7 2 4F 4 F A6WE E9NE 1996080200023 19960802 00023 NM 1996 8 2 CALA9601052 1 19960724 A 3222 69141067 CYLINDER BOEING 737 7373T0 1384582 NM NLG INOPERATIVE A CALA O OTHER J WARNING INDICATION CL CLIMB 1 SW 09 18350 28053 28053 23588 THE NOSE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION DEPARTING MFE. THE GEAR WAS CYCLED, BUT THE L IGHT DID NOT EXTINGUISH. THE FLIGHT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. THE NLG RETRACT ACTUATOR WAS RE PLACED BASED ON THE REPORTED FAULT. THE GEAR WAS SWUNG, AND THE PROBLEM WAS DUPLICATED. THE NLG CYLINDER WAS REMOVED A ND REPLACED. THE GEAR WAS SWUNG SEVERAL TIMES WITH OPERATION AND INDICATIONS CHECKING GOOD. 2 L 7 2 4F RT A16WE 1996080200024 19960802 00024 WP 1996 8 2 CKSA96076 1 19960725 A 5347 BAC1520792 SEAT TRACK DOUG DC8 DC861 3021952 WP CARGO COMPT CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 SPLP - FLT 74558: DURING C AND AOS INSPECTION WORK CARD NR 006-4: FOUND RT TRACK NR 1, STA 1580, HAS LEVEL 2 CORROSION . INSTALLED TRACK AT AFFECTED AREA PER SRM 53-2-3. 2 L 7 4 4F 4A25 1996080200025 19960802 00025 WP 1996 8 2 CKSA96077 1 19960725 A 5347 BAC1520792 SEAT TRACK DOUG DC8 DC861 3021952 WP CARGO COMPT CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 SPLP - FLT NR 74558: DURING C AND AOS INSPECTION WORK CARD 006-4, FOUND CENTER TRACK, STA 1420 THROUGH STA 1400, HAS LE VEL 2 CORROSION. REMOVED AND REPLACED TRACK AT AFFECTED AREA PER SRM 53-2-3. 2 L 7 4 4F 4A25 1996080200026 19960802 00026 WP 1996 8 2 CKSA96078 1 19960725 A 5347 BAC1520792 SEAT TRACK DOUG DC8 DC861 3021952 WP CARGO COMPT CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 SPLP - FLT NR 74558: DURING C AND AOS INSPECTION WORK CARD 010-10, FOUND CARGO COMPARTMENT FLOOR NR 1 TRACK RIGHT SIDE STA 580 HAS LEVEL 2 CORROSION. INSTALLED TRACK AT AFFECTED AREA AS PER SRM 53-2-3. 2 L 7 4 4F 4A25 1996080200027 19960802 00027 WP 1996 8 2 CKSA96079 1 19960725 A 5320 J0602969 CUSP DOUG DC8 DC861 3021952 WP FS 1600-1620 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 SPLP - FLT NR 74558: DURING C AND AOS INSPECTION WORK CARD 007-1, FOUND FS 1600 THROUGH FS 1620 LT SIDE FRAME-TO-FRAME FORMER HAS LEVEL 2 CORROSION. MADE AND INSTALLED FORMER PER SRM 53-2-5. 2 L 7 4 4F 4A25 1996080200028 19960802 00028 NM 1996 8 2 DL72K961761 1 19960719 A 5320 WINDOW POST BOEING 727 727232 1384082 NM LT COCKPIT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 474DA 20751 FOUND A CRACK IN THE LT SIDE F-N COCKPIT WINDOW POST. REPAIRED PER S/B 737-53-0086, REV 11 IN ACCORDANCE WITH A.D. 93-0 5-17 AND 90-06-09. 2 L 7 3 4F A3WE 1996080200029 19960802 00029 NM 1996 8 2 DL72S961755 1 19960722 A 3350 LIGHT 1000677 BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 476DA 1000 20753 LT AFT SERVICE DOOR OVERHEAD EMERGNECY LIGHT INOPERATIVE. REPLACED LIGHT ASSY AND BATTERIES, CHECKS NORMAL. 2 L 7 3 4F A3WE 1996080200030 19960802 00030 NM 1996 8 2 DL72S961757 1 19960723 A 3350 LIGHT BOEING 727 727232 1384082 NM AFT AIRSTAIR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 475DA 20752 FOUND BOTH EMERGENCY EXIT LIGHTS IN AFT AIRSTAIR INOPERATIVE. CLEANED BATTERY TERMINALS, OPS CK OK. 2 L 7 3 4F A3WE 1996080200031 19960802 00031 NM 1996 8 2 DL72S961770 1 19960718 A 5743 TRUNNION BOEING 727 727232 1384082 NM LT MLG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 521DA 21472 FOUND CORROSION ON LEFT MLG FORWARD TRUNNION BORE AND FACE. REPAIRED PER DELTA ERA 303917-14. 2 L 7 3 4F A3WE 1996080200032 19960802 00032 NM 1996 8 2 DL72W961762 1 19960723 A 5312 6516350339 BULKHEAD WEB BOEING 727 727247 138408F NM BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2819W 21057 FOUND CRACK AT RBL 27 OF BS 1183 BULKHEAD WEB. THE DAMAGE CONSISTED OF A .75 INCH CRACK AT WL 170. THE CRACK LOCATION I S OUTSIDE OF THE INSPECTION AREA SPECIFIED BY S/B 727-53-171. REPAIRED PER B727 SRM 53-10-9, FIG. 4. 2 L 7 3 4F A3WE 1996080200033 19960802 00033 NM 1996 8 2 DL767961743 1 19960720 A 3350 LIGHT 8200008804 BOEING 767 767232 1385132 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 114DL 22226 AISLE EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT FIXTURE. 2 L 7 2 4F RT A1NM 1996080200034 19960802 00034 WP 1996 8 2 DLL10961753 1 19960722 A 2913 3508807 PUMP LKHEED 1011 10113851 5265010 WP NR 2 ENG CRACKED A DALA O OTHER K FLUID LOSS CR CRUISE 1 SO 27 1731D 193C1200 IN CRUISE B-SYSTEM HYDRAULIC RESERVOIR LOW QUANTITY LIGHT ON WITH FLUID LEVEL AT THREE-EIGHTS FULL. AT SAME TIME, NOTED B2 ATM ON PRESSURIZING B-HYDRAULIC SYSTEM AND B-PUMP LOW PRESSURE LIGHT ON FLUID LOSS STOPPED WITH PUMPS TURNED OFF. F OUND B-SYSTEM ENGINE DRIVEN PUMP CASTING CRACKED. REPLACED SAME. OPS CHECK GOOD. 2 L 7 3 4F A23WE 1996080200035 19960802 00035 WP 1996 8 2 DLL13961746 1 19960721 A 3350 BATTERY PACK 5165741 LKHEED 1011 10113851 5265010 WP R4 DOOR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 786DL 37859 193A1123 R4 DOOR BATTERY PACK WILL NOT POWER LIGHTS. REPLACED PACK, CHECKS GOOD. 2 L 7 3 4F A23WE 1996080200036 19960802 00036 NM 1996 8 2 DLM88961739 1 19960719 A 5320 FRAME DOUG MD88 MD88 3023688 NM C-1 DOOR CUTOUT CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DL 49537 FOUND DURING D-1 LETTER CHECK - CORROSION AT C-1 DOOR CUT-OUT LOWER THRESHOLD/FRAME. REPAIRED PER SRM 53-05 FIG 44 AND ERA 359982-14. 2 L 7 2 4F RT A6WE 1996080200037 19960802 00037 NM 1996 8 2 DLM88961740 1 19960719 A 2910 793691342 LINE DOUG MD88 MD88 3023688 NM TAIL COMPARTMENT NOT SECURED A DALA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 SO 27 982DL 53273 LOSS OF RIGHT HYDRAULIC SYSTEM IN-FLIGHT. GEAR EXTENSION HANDLE NOT STOWED AT GATE. FOUND LOOSE B-NUT ON RIGHT ENGINE HYDRAULIC PUMP PRESSURE LINE INSIDE TAIL COMPARTMENT JUST INBOARD OF PYLON. TIGHTENED SAME. RAN ENGINES - LEAK CHECKS GOOD. SERVICED HYDRAULICS. 2 L 7 2 4F RT A6WE 1996080200038 19960802 00038 NM 1996 8 2 P5CA9600392 1 19960724 A 5730 65B1161711 PANEL BOEING 747 747122 1384872 NM WS 420 DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 DELAMINATED PANEL LEFT WING UPPER ABOVE FALSE SPAR AREA WS 420. REPLACED PANEL PER BOEING SRM 51-10-01. 2 L 7 4 4F A20WE 1996080200039 19960802 00039 NM 1996 8 2 P5CA9600393 1 19960724 A 7110 65B0076332 COWLING BOEING 747 747123 1384873 NM NR 3 ENGINE DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 3 ENGINE COWLING AND THRUST REVERSER TRANSLATING SLEEVE DAMAGED WHEN NR 3 THRUST REVERSER OPERATED WITH CORE COWL OPE N. REPLACED CORE COWL AND REPAIRED TRANSLATING SLEEVE PER BOEING SRM 54-30-03 FIG. 21 AND SRM 51-40-06 FIG. 12. 2 L 7 4 4F A20WE 1996080200040 19960802 00040 EU 1996 8 2 QXEA9600254 1 19960718 A 3350 6008905 POWER SUPPLY FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 478US 12 11227 GEG - SEVERAL EVACUATION LIGHTS IN GALLEY AREA ARE INOPERATIVE. POWER SUPPLY REPLACED AND LIGHT OPS CHECKED GOOD. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996080200041 19960802 00041 EU 1996 8 2 QXEA9600255 1 19960718 A 3350 6008905 BATTERY PACK FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 478US 2880 11227 PDX - EMERGENCY LIGHT AT SEAT 4AB IS INOPERATIVE. BATTERY PACK REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996080200042 19960802 00042 EU 1996 8 2 QXEA9600256 1 19960718 A 3350 1820 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 454US 11107 BOI - EMERGENCY EXIT LIGHT AT ROW 8E IS INOPERATIVE. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED T O SERVICE. 2 L 7 2 4F RT A20EU 1996080200043 19960802 00043 NE 1996 8 2 QXEA9600257 2 19960719 A 7530 MS2452333 SWITCH DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 BLEED SYS MALFUNCTIONED A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 829PH 304 PSC - WHEN BLEEDS ARE TURNED ON AFTER ENGINE START A FAIRLY STRONG FUEL SMELL IS PRESENT. SMELL DISAPPEARS AFTER APPROX IMATELY ONE MINUTE. NR 2 HIGH PRESSURE SWITCH REPLACED AND BLEED OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 1996080200044 19960802 00044 NE 1996 8 2 QXEA9600258 2 19960720 A 7532 776863 BLEED VALVE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 BLEED AIR MALFUNCTIONED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 829PH 12651 304 SEA - AFTER NR 2 ENGINE IS STARTED AND BLEED IS SWITCHED ON, FUEL ODOR IS PRESENT FOR ABOUT 1 MINUTE. THEN DISAPPEARS. N R 2 ENGINE HP BLEED VALVE REPLACED I/A/W MAINT. MANUAL. ENGINE GROUND RUN AND SYSYEM OPS CHECKED GOOD. AIRCRAFT RETURN ED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 1996080200045 19960802 00045 EU 1996 8 2 QXEA9600259 1 19960720 A 3350 1820 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 466US 11075 BOI - EMERGENCY LIGHT IS INOPERATIVE IN LEFT OVERWING EXIT HANDLE. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996080200046 19960802 00046 EU 1996 8 2 QXEA9600260 1 19960721 A 3350 1820 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 450US 11101 PDX - LEFT, ROW 8 EXIT LIGHT OUT. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996080200047 19960802 00047 NM 1996 8 2 QXEA9600261 1 19960722 A 3350 OL3071BPEGPL BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 816PH 54 SEA - AFT OVERHEAD AISLE EMERGENCY LIGHT IS INOPERATIVE. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURN ED TO SERVICE. 2 H 7 2 4T RT A13NM 1996080200048 19960802 00048 EU 1996 8 2 QXEA9600262 1 19960723 A 3350 MGG1280 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 466US 11075 PDX - CEILING EXIT LIGHT INOP AT ROW 8 ON THE AFT SIDE. BULBS WERE REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETUR NED TO SERVICE. 2 L 7 2 4F RT A20EU 1996080200049 19960802 00049 NM 1996 8 2 QXEA9600263 1 19960723 A 3350 MS24266R12B12SM CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN DISCONNECTED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 811PH 23 PSC - EMERGENCY STRIP LIGHTS DS1 THROUGH DS4 ARE INOPERATIVE. WIRE CONNECTOR FOUND DISCONNECTED, RECONNECTED AND LIGHTS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1996080200050 19960802 00050 NE 1996 8 2 QXEA9600264 2 19960724 A 7320 7863916 HMU DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 ENGINE MALFUNCTIONED A A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 829PH 2759 304 PCE120430 PDX - NR 2 ENGINE DOES NOT FOLLOW THROTTLE. STRONG SMELL OF FUEL ON FIRST START WITH NR 2 BLEED ON. NR 2 ENGINE HMU RE PLACED I/A/W MAINT. MANUAL. ENGINE GROUND RUNS CHECKED GOOD, NO FUEL SMELL FROM BLEED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 1996080200051 19960802 00051 NM 1996 8 2 RAAA96B2032 1 19960719 A 3350 86210144 BATTERY PACK 873100112 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 RIGHT SERVICE DOOR EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. 2 L 7 3 4F A3WE 1996080200052 19960802 00052 NM 1996 8 2 RAAA96B2033 1 19960719 A 3350 86210066 BATTERY PACK 873100112 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 ROW 7 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. 2 L 7 3 4F A3WE 1996080200053 19960802 00053 WP 1996 8 2 RAAA96E4008 1 19960718 A 5311 FRAME LKHEED 188 188A 5262602 WP BS 264.5 DAMAGED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 49429 188A1140 DURING SCHEDULED NR 1 CHECK, FOUND F.S. 264.5 FRAME DAMAGED DUE CARGO IMPACT AT STRINGERS 22 TO 23. REPAIRED PER SRM 53 -2-3 FIG. 2, PG. 9. 2 L 7 4 4T RT 4A22 1996080200054 19960802 00054 WP 1996 8 2 RAAA96E4009 1 19960718 A 5311 FRAME LKHEED 188 188A 5262602 WP BS 283.5 DAMAGED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 49429 188A1140 DURING SCHEDULED NR 1 CHECK, FOUND F.S. 283.5 FRAME DAMAGED DUE CARGO IMPACT AT STRINGERS 22 TO 23. REPAIRED PER SRM 53 -2-3 FIG. 2, PG. 9. 2 L 7 4 4T RT 4A22 1996080200055 19960802 00055 SO 1996 8 2 RAAA96E9009 1 19960719 A 3350 873100112 LIGHT LKHEED 188 188C 5262604 SO CABIN INOPERATIVE A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 EGRESS FLOOR PROXIMITY LIGHT PASSENGER ROW 21 FAILED SERVICE CHECK. CHANGED LIGHT ASSEMBLY. 2 L 7 4 4T 4A22 1996080200056 19960802 00056 NE 1996 8 2 TC8A96049 2 19960725 A 7200 ENGINE DOUG DC8 DC8F54 3021926 WP PWA JT3D JT3D3B 52039 NE NR 3 FAILED A TC8A A E UNSCHED LANDING ENGINE SHUTDOWN E Y VIBRATION/BUFFET ENGINE STOPPAGE CL CLIMB 1 GL 23 802CK 45679 669735 DISCREPANCY: NR 3 ENGINE VIBRATION ON CLIMB-OUT. AIRCRAFT YAWED AND EPR DROPPED. IN-FLIGHT SHUT DOWN COMPLETED. CSD D ISCONNECTED. CORRECTIVE ACTION: REMOVED AND REPLACED NR 3 ENGINE, CHECK GROUND OPS RUN-UP OK IAW MM 71-00. 2 L 7 4 4F 4 F 4A25 1E8 1996080200057 19960802 00057 NM 1996 8 2 UPS96220664 1 19960724 A 2613 SENSE WIRES BOEING 727 72725C 138400H NM LT AIRSTAIR WALL CHAFED A IPXA K NONE N FALSE WARNING CR CRUISE 1 SO 01 931UP 19858 NR 1 ENGINE STRUT OVERHEAT FLICKERED TWICE DURING CRUISE. FOUND STRUT DETECTOR WIRES WITH MINOR SIGNS OF CHAFING. CORR ECTED ALL CHAFING AREAS. SYSTEM CHECKS NORMAL. OK FOR SERVICE. 2 L 7 3 4F A3WE 1996080200058 19960802 00058 WP 1996 8 2 UPS96820661 1 19960724 A 3350 5708458 LIGHT DOUG DC8 DC873F 302199F WP CABIN INOPERATIVE A IPXA L ABORTED APPROACH O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE-N/A, COCKPIT OVERHEAD DOME EMERGENCY LIGHT AND CABIN EMERGENCY LIGHT INOP. REMOVED AND REPLACED CANNON PLUG AT EMERGENCY BATTERY PACK AND PIN. REMOVED AND REPLACED BATTERY PACK AND CKD OKAY (P/N 5708458-503) (S/N FTL 231) ON, (2054) OFF. 2 L 7 4 4F RT 4A25 1996080200059 19960802 00059 NM 1996 8 2 96ZZZX3734 1 19960603 A 2130 CONNECTOR GARRTT 106142618 BOEING 727 727251 138408H NM FLOW CONTL VALVE LOOSE A FX7A A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 SO 19 266US 43685 5068 P1483 19985 KMIA - AFTER DEPARTURE DURING CLIMB STAGE, UNABLE TO OBTAIN CABIN PRESSURE. DUMPED FUEL AND RETURNED TO KMIA LANDING UN EVENTFULLY. FOUND LOOSE ELECTRICAL CONNECTOR AT THE PNEUMATIC FLOW CONTROL/SHUT-OFF VALVE, P/N 39608831. TIGHTENED THE CONNECTOR, OPERATIONAL TEST NORMAL PER MM21-30-00 P501-P503. RETURNED TO SERVICE. 2 L 7 3 4F A3WE 1996080200060 19960802 00060 NE 1996 8 2 96ZZZX3735 2 19960608 A 7250 539004 TURBINE BOEING 727 727251 138408H NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE DAMAGED A A FX7A E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 19 266US 22374 K93556 19985 KMIA - AFTER DEPARTURE DURING CLIMB STAGE, SEVERE VIBRATION ON NR 2 ENGINE. INITIATED EMERGENCY PROCDURES, SHUT DOWN NR 2 ENGINE, DUMPED FUEL AND RETURNED TO KMIA LANDING UNEVENTFULLY. FOUND NR 2 ENGINE TURBINE DAMAGED. 2 L 7 3 4F 4 F A3WE E2EA 1996080200062 19960802 00062 WP 1996 8 2 96ZZZX3737 1 19960604 A 5330 SKIN DOUG DC6 DC6A 3021706 WP BS 500 CRACKED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 874TA 35686 11624 44641 SKIN CRACKED, STA 500, ABOVE WINDOW LINE, RIGHT. REWORKED IAW SRM 4-29. 2 L 7 4 4R 6A3 1996080200063 19960802 00063 WP 1996 8 2 96ZZZX3738 1 19960604 A 5330 SKIN DOUG DC6 DC6A 3021706 WP BS 720 CRACKED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 874TA 35686 11624 44641 SKIN CRACKED, FS 720, AFT BAGAGE DOOR FRAME. REWORKED - IAW SRM 4-29. 2 L 7 4 4R 6A3 1996080200064 19960802 00064 WP 1996 8 2 96ZZZX3739 1 19960604 A 5330 SKIN DOUG DC6 DC6A 3021706 WP BS 217 CRACKED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 874TA 35686 11624 44641 SKIN CRACKED, FS 217, AFT CORNER OF FORWARD MAIN CARGO DOOR. REWORKED IAW SRM 4-29. 2 L 7 4 4R 6A3 1996080200065 19960802 00065 WP 1996 8 2 96ZZZX3740 1 19960604 A 5330 SKIN DOUG DC6 DC6A 3021706 WP BS 58 CRACKED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 874TA 35686 11624 44641 SKIN CRACKED, STA 58, AFT UPPER CORNER OF CAPTAIN'S WINDOW. REWORKED IAW SRM 4-29. 2 L 7 4 4R 6A3 1996080200066 19960802 00066 WP 1996 8 2 96ZZZX3741 1 19960604 A 5330 SKIN DOUG DC6 DC6A 3021706 WP BS 448 CRACKED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 874TA 35686 11624 44641 SKIN CRACKED, FS 448, RIGHT WING. REWORKED IAW SRM. 2 L 7 4 4R 6A3 1996080200067 19960802 00067 WP 1996 8 2 96ZZZX3742 1 19960604 A 5330 SKIN DOUG DC6 DC6A 3021706 WP BS 490 CRACKED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 874TA 35686 11624 44641 SKIN CRACKED, FS 490, ABOVE WINDOW LINE, LEFT. REWORKED IAW SRM 4-29. 2 L 7 4 4R 6A3 1996080200068 19960802 00068 WP 1996 8 2 96ZZZX3743 1 19960613 A 3350 1001191 LIGHT PANEL DOUG DC9 DC933F 302207A WP COCKPIT INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 933F 47191 OAK - EMERGENCY EXIT LIGHTS WILL NOT TEST. REMOVED AND REPLACED BATTERY PACK AND MAIN ENTRY DOOR EMERGENCY LIGHT PANEL. SYSTEM OPERATIONS CHECK GOOD. REFERENCE OPERATOR CONTROL NR: EIAA9618. 2 L 7 2 4F A6WE 1996080200069 19960802 00069 NM 1996 8 2 AWXA960291 1 19960625 A 7722 EGT BOEING 737 7373G7 1384595 NM NR 2 ENGINE OVERTEMP A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 309AW 24711 PHX/OMA - FLT 2517 - AIR TURNBACK. NR 2 ENGINE OVERTEMP EGT ON TAKEOFF CLIMB-OUT 930 DEGREES FOR LESS THAN 2 SECONDS. P ER MM 72-00-00, PAGE 682, B ITEM AND 3A AND BY PERFORMANCE GROUND RUN SYSTEM. CHECKS OK FOR SERVICE. (X) 2 L 7 2 4F RT A16WE 1996080200070 19960802 00070 NM 1996 8 2 AWXA960326 1 19960706 A 7722 EGT BOEING 737 737277 1384570 NM NR 2 ENGINE OVERTEMP A AWXA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 WP 28 183AW 22650 LAS/SFO - FLT 2603 - AIR TURNBACK. ON TAKEOFF, THE NR 2 ENGINE HAD AN OVERTEMP OF EGT. THE PILOT REPORTED A TEMPERATUR E OF 635 DEGREES FOR A PERIOD OF 20-30 SECONDS. HE SAID IT WAS A BLEEDS-OFF TAKEOFF. PER MM 71-09-100, PAGE 218F, THE ENGINE WILL REQUIRE A BORESCOPE INSPECTION. COMPLIED WITH BORESCOPE INSPECTION PER CARD 15M72014. Q.C. PERFORMED BORES COPE REQUIRED PER 72-00, PAGE 530W-532. TROUBLESHOOTING PRIOR TO BORESCOPE PER P AND W MM 72-00, PAGE 127-139. PERFORM ED TRIM RUN PER F5M71002. TAKEOFF POWER AND EGT GOOD. (X) 2 L 7 2 4F RT A16WE 1996080200071 19960802 00071 NE 1996 8 2 AWXA960327 2 19960705 A 7261 OIL CAP BOEING 737 737277 1384570 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE DAMAGED A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 WP 28 179AW 22646 PHX - FLT 2164 - AIR TURNBACK. ON DEPARTURE ROLL, AIRCRAFT REPORTED FLUID COMING FROM NR 2 ENGINE, NR 2 OIL GAUGE SHOWE D 3 GALLONS DROPPING TO 1 GALLON. REDUCED THRUST ON NR 2 ENGINE AND RETURNED FOR NORMAL LANDING. OIL TEMPERATURE AND P RESSURE REMAINED WITHIN NORMAL LIMITS. AT GATE, FOUND OIL CAP LOCKED AT NR 2 ENGINE, BUT NOT SEATED. FOUND CAP TO BE B AD. REPLACED CAP AND SERVICED ENGINE OIL, RAN ENGINE, OPS NORMAL. (X) 2 L 7 2 4F 4 F RT A16WE E2EA 1996080200072 19960802 00072 NM 1996 8 2 AWXA96040 1 19960713 A 3610 BLEED SYSTEM BOEING 757 7572G7 1384963 NM NR 2 ENGINE MALFUNCTIONED A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 908AW 24233 PHX/JFK - FLT 0292 - AIR TURNBACK. CREW REPORTED NR 2 ENGINE BLEED OFF LIGHT ILLUMINATED AND THE PACK WAS OFF. CREW TR IED CIRCUIT BREAKER RESET TO NO AVAIL. CREW DID SEVERAL RESETS AND BLEED STILL DID NOT COME BACK ON. AIRCRAFT RETURNED TO PHX FOR REPAIR DUE TO POSSIBLE ICING CONDITIONS AT JFK. UNABLE TO DUPLICATE PROBLEM. BLEED SYSTEM CHECKED GOOD ON GROUND WITH ENGINE RUNS. (X) 2 L 7 2 4F RT A2NM 1996080200073 19960802 00073 WP 1996 8 2 CKSA9600057 1 19960531 A 5710 STRUCTURE DOUG DC8 DC861 3021952 WP RT WING DAMAGED A CKSA B EMER. DESCENT O OTHER DE DESCENT 1 GL 23 812CK 45890 SPIM - FLT 74558 - DECLARED EMERGENCY, LANDED AT SPIM. ON POST-FLIGHT INSPECTION, FOUND SEVERE DAMAGE TO RIGHT WING TIP , RIGHT AILERON, NR 1 ENGINE COWLS, NR 2 ENGINE COWLS, LEFT WING LEADING EDGE, LEFT FLAP AND LEFT AILERON. (X) 2 L 7 4 4F 4A25 1996080200074 19960802 00074 WP 1996 8 2 EIAA9618 1 19960613 A 3350 60030431 BATTERY PACK DOUG DC9 DC933F 302207A WP CABIN DISCHARGED A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 933F 47191 OAK - EMERGENCY EXIT LIGHTS WILL NOT TEST. REMOVED AND REPLACED BATTERY PACK AND MAIN ENTRY DOOR EMERGENCY LIGHT PANEL. SYSTEM OPERATIONS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1996080200075 19960802 00075 NE 1996 8 2 EIAA9619 2 19960705 A 7530 FITTING DOUG DC9 DC932F 3022067 WP PWA JT8 JT8D9A 52048 NE NR 2 ENGINE BROKEN A EIAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 935F 47220 665815 KTN - AFTER TAKEOFF, RIGHT ENGINE EPR REDUCED TO 1.6 (FROM 2) AND EGT CLIMBED TO 565 C. N1 DROPPED FROM 95 PERCENT TO 8 5 PERCENT. OIL PRESSURE WAS NORMAL. RETURNED TO PAKT. FOUND PS4 MANIFOLD FITTING ON PRBC BROKEN IN HALF. REPLACED FI TTING. PERFORMED ENGINE RUN PER MM 71-00. ALL CHECKS WERE GOOD. (M) 2 L 7 2 4F 4 F A6WE E2EA 1996080200076 19960802 00076 NM 1996 8 2 TAOA069617 1 19960709 A 3350 013071BPGPL LAMP BOEING 727 727294 1384088 NM CABIN MISSING A TAOA K NONE O OTHER IN INSP/MAINT 1 EA 15 921TS 22043 ESCAPE PATH LIGHTING AT ROW 27 MISSING LAMP. REPLACED LAMP, ROW 27. (X) 0 4 A3WE 1996080200077 19960802 00077 NM 1996 8 2 TAOA069618 1 19960711 A 2611 824PY SMOKE DETECTOR BOEING 727 727225 1384077 NM FORWARD LAV FAILED A TAOA O OTHER N FALSE WARNING CL CLIMB 1 EA 15 922TS 1145 20415 FORWARD LAVATORY SMOKE DETECTOR WARNING WENT OFF ON CLIMB-OUT. REPLACED AND TESTED DETECTOR PER MM 25-60-00. (X) 2 L 7 3 4F A3WE 1996080200078 19960802 00078 NM 1996 8 2 TAOA079601 1 19960714 A 3350 S106 BATTERY MARATHON BOEING 727 727294 1384088 NM AFT AIRSTAIR DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 921TS 22043 AFT AIRSTAIRS EMERGENCY EXIT LIGHTS WILL NOT TEST. REPLACED BATTERIES, OPS CHCK OK. (X) 0 4 A3WE 1996080200079 19960802 00079 NM 1996 8 2 TWRA96126 1 19960704 A 3350 ML7715 BULB BOEING 747 747238B 1384828 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 614FF 20534 DURING DAILY CHECK, FOUND CABIN 'D' ZONE 'E' PATH LIGHT AT SEAT42A, 45A AND 39K INOP. RELAMPED, OPS CHECK OK PER MM 33- 51-00.(M) 2 L 7 4 4F A20WE 1996080200080 19960802 00080 NM 1996 8 2 TWRA96129 1 19960709 A 3350 1317 BULB BOEING 747 747259B NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 EICEO 21730 DURING DAILY CHECK, FOUND 25C CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED 25C CEILING EMERGENCY LIGHT BULB. OPS CHEC K NORMAL PER MM 33-51-00. (X) 2 L 7 4 4F RT A20WE 1996080200081 19960802 00081 NM 1996 8 2 TWRA96136 1 19960710 A 3350 PLUG BOEING 747 747130 1384880 NM R4 DOOR LOOSE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 603FF 19746 DURING DAILY CHECK, FOUND R4 BUSTLE LIGHT INOPERATIVE. FOUND LOOSE CANNON PLUG. SECURED OPS CHECK, NORMAL PER MM 33-51 -00. (X) 2 L 7 4 4F A20WE 1996080200082 19960802 00082 NM 1996 8 2 TWRA96137 1 19960710 A 3350 3004181A LIGHT BOEING 747 747130 1384880 NM 4L DOOR INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 603FF 19746 DURING DAILY CHECK, FOUND 4L DOOR UPPER BUSTLE LIGHT INOPERATIVE. REPLACED BUSTLE LIGHT AT 4L DOOR. OPS CHECK OK PER M M-33-51-00. (X) 2 L 7 4 4F A20WE 1996080200083 19960802 00083 NM 1996 8 2 TWRA96143 1 19960711 A 3350 CONNECTOR BOEING 747 747130 1384880 NM CABIN LOOSE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 603FF 19746 DURING DAILY CHECK, FOUND SIDE WALL EMERGENCY EXIT LIGHT INOPERATIVE FORWARD OF NR 5L AND NR 5R DOOR. REPAIRED LOOSE CO NNECTOR IN CEILING AREA. OPS CHECK GOOD PER MM 33-51-00. (X) 2 L 7 4 4F A20WE 1996080200084 19960802 00084 NM 1996 8 2 USAA960469 1 19960613 A 5330 SKIN BOEING 737 737201 1384454 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 36895 22756 ROA - DURING VISUAL INSPECTION, FOUND 1 INCH CRACK IN FUSELAGE SKIN. INSTALLED DOUBLER PER SRM 53-30-03. (X) 2 L 7 2 4F A16WE 1996080200085 19960802 00085 NM 1996 8 2 USAA960470 1 19960613 A 5330 SKIN BOEING 737 737201 1384454 NM FUSELAGE LIGHTNING STRIKE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 36895 22756 ROA - DURING BX CHECK, FOUND LIGHTNING STRIKE DAMAGE 2 INCHES BY 8 INCHES ON FUSELAGE CROWN SKIN. BURNISHED DAMAGED ARE A AND INSTALLED DOUBLER PER SRM 53-30-3, FIGURE 6. (X) 2 L 7 2 4F A16WE 1996080200086 19960802 00086 1996 8 2 USAABB96018 4 19960706 A 2565 POWER SUPPLY 10121 BOEING 767 767201 1385125 NM RT OVERWING DEFECTIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 648US 6284 23900 CLT - DURING ANNUAL SLIDE DEPLOYMENT CHECK, RIGHT OVERWING ESCAPE SLIDE DID NOT DEPLOY AUTOMATICALLY WHEN ACTUATED. SLI DE WAS SUCCESSFULLY DEPLOYED MANUALLY. MAINTENANCE FOUND A DEFECTIVE FUSE IN POWER SUPPLY M962. POWER SUPPLY WAS REPLA CED. (X) 2 L 7 2 4F RT A1NM 1996080200087 19960802 00087 WP 1996 8 2 USAAD96102 1 19960712 A 7931 811131 RELIEF VALVE DOUG DC9 DC931 3022065 WP RT ENGINE FAILED A USAA A E UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 EA 19 977VJ 48155 PHL/PWM - FLT 2246 - ON CLIMB, 'RT ENGINE OIL PRESS LOW' WARNING LIGHT FLICKERED WITH CORRESPONDING DROP ON OIL PRESSURE GAUGE. SHUT DOWN ENGINE, RETURNED TO FIELD. REPLACED RIGHT ENGINE OIL PRESSURE RELIEF VALVE, AND ADJUSTED PRESSURE PE R MM. (X) 2 L 7 2 4F A6WE 1996080200088 19960802 00088 EU 1996 8 2 USAAF96077 1 19960716 A 3350 5515800106 PANEL FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 482US 11231 PIT - EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE FORWARD, MID AND AFT EMERGENCY PANELS. (X) 2 L 7 2 4F RT A20EU 1996080200089 19960802 00089 NM 1996 8 2 USAASB96098 1 19960610 A 3260 387 LAMP BOEING 737 7372B7 1384560 NM NLG LIGHT BURNED OUT A USAA O OTHER P NO WARNING INDICATION AP APPROACH 1 EA 19 286AU 23133 RSW - FLT 989 - ON APPROACH INTO RSW AT GEAR EXTENSION, CAPTAIN FAILED TO GET NOSE GEAR LIGHT. CAPTAIN DID A GO-AROUND AND RELAMPED NOSE GEAR DOWNLIGHT. GEAR WAS CYCLED WITH NORMAL GEAR INDICATION. RELAMPED NOSE GEAR LIGHT. (X) 2 L 7 2 4F A16WE 1996080200090 19960802 00090 NM 1996 8 2 USAASB96099 1 19960603 A 2740 ELECT TRIM BOEING 737 737201 1384454 NM STABILIZER TRIM ACTIVATED A USAA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 EA 19 257AU 22799 LGA - FLT 2221 - ON APPROACH TO LGA, CREW REPORTED WHILE FLYING WITH AUTOPILOT DISENGAGED, THE ELECTRIC STABILIZER TRIM ACTIVATED FOR 3-5 SECONDS. CREW OVERRODE TRIM AND PERFORMED A GO-AROUND. FLIGHT THEN LANDED WITH NO FURTHER INCIDENT. MAINTENANCE PERFORMED SYSTEMS CHECKS ON BOTH THE AUTOPILOT AND STABILIZER TRIM SYSTEMS. NO FAULTS WERE FOUND. (X) 2 L 7 2 4F A16WE 1996080200091 19960802 00091 NM 1996 8 2 USAASB96109 1 19960615 A 7931 SRL04GM1 OIL PRESS IND BOEING 737 737201 1384454 NM NR 1 ENGINE FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 240AU 51744 24737 22355 BWI - FLT 2539 - ABOUT 50 MILES OUT OF BWI, THE CREW OBSERVED ZERO OIL PRESSURE ON THE NR 1 ENGINE. ALL OTHER INDICATIO NS WERE NORMAL. FLIGHT RETURNED TO FIELD AT BWI. THE ENGINE WAS NOT SHUT DOWN AND NO EMERGENCY EQUIPMENT WAS CALLED OU T. THE FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 ENGINE OIL PRESSURE INDICATOR. (X) 2 L 7 2 4F A16WE 1996080200092 19960802 00092 NM 1996 8 2 USAASB96114 1 19960623 A 2520 STRAP BOEING 737 737201 1384454 NM L2 DOOR OUT OF POSITION A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 265AU 22962 PIT - FLT 1279 - WHILE CLIMBING THROUGH 8,000/9,000 FEET, FLIGHT ATTENDANT ADVISED CAPTAIN OF A NOISE FROM THE REAR OF T HE AIRCRAFT. AFTER LEVELLING OFF AT 11,000 FEET, DISCOVERED THE SAFETY RESTRAINING STRAP WAS CAUGHT IN THE 2L DOOR. TH ERE WAS NO DOOR WARNING INDICATIONS OR ABNORMAL PRESSURE INDICATIONS. FLIGHT DIVERTED TO PIT AND LANDED WTIH NO FURTHER INCIDENT. 2 L 7 2 4F A16WE 1996080200093 19960802 00093 NM 1996 8 2 USAASB96115 1 19960624 A 3230 RETRACT MECH BOEING 737 737201 1384454 NM LANDING GEAR MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 254AU 22796 ORF - FLT 1177 - AFTER TAKEOFF, CREW WAS UNABLE TO RAISE LANDING GEAR. LANDING GEAR INDICATIONS WERE BLANK. CREW ACCOM PLISHED CHECK LIST AND FOUND LIGHTS AND LEVER LATCH CIRCUIT BREAKERS TRIPPED. RESET SAME AND GOT NORMAL INDICATIONS. C APTAIN DECIDED TO RETURN TO FIELD. EMERGENCY WAS DECLARED. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE PERFOR MED OPS CHECK (GEAR SWING) OF LANDING GEAR SYSTEM PER MM. OPS CHECKED GOOD. (X) 2 L 7 2 4F A16WE 1996080200094 19960802 00094 NM 1996 8 2 USAASB96117 1 19960626 A 2612 6937307112 FIRE CONTRL MOD BOEING 737 737296 1384486 NM COCKPIT FAILED A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 238US 27521 16963 22398 LIT - FLT 764 - CAPTAIN REPORTED THE WHEELWELL OVERHEAT DETECTION ILLUMINATED IN CRUISE. EMERGENCY WAS DECLARED. FLIGH T DIVERTED TO LIT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE P8-1 ENGINE AND APU FIRE CONTROL MODULE . OPERATIONAL CHECK NORMAL. (X) 2 L 7 2 4F RT A16WE 1996080200095 19960802 00095 NE 1996 8 2 USAASB96118 2 19960627 A 7261 OIL FILTER STUDS BOEING 737 737201 1384454 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE PULLED OUT A USAA A E UNSCHED LANDING ENGINE SHUTDOWN J K WARNING INDICATION FLUID LOSS CR CRUISE 1 EA 19 241US 22443 CLE - FLT 273 - FLYING AT 27,000 FEET, THE NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. CREW SHUT DOWN NR 2 ENGINE A ND DECLARED AN EMERGENCY. FLIGHT DIVERTED TO CLE AND LANDED WITH NO FURTHER INCIDENT. TOTAL SINGLE ENGINE TIME WAS 10 MINUTES. MAINTENANCE FOUND 2 OIL FILTER STUDS PULLED OUT OF CASTING ON THE NR 2 ENGINE. REPAIR WAS MADE USING HELI-COI LS. REPLACED OIL FILTER. RAN ENGINE, LEAK CHECKED GOOD. (X) 2 L 7 2 4F 4 F A16WE E2EA 1996080200096 19960802 00096 NM 1996 8 2 USAASB96120 1 19960705 A 3260 DOWNLOCK SENSOR BOEING 737 7372B7 1384560 NM NLG OUT OF ADJUST A USAA O OTHER N FALSE WARNING AP APPROACH 1 EA 19 286AU 23133 CLT - FLT 1126 - ON GEAR EXTENSION, NOSE GEAR RED LIGHT REMAINED ILLUMINATED. CREW CYCLED GEAR WITH NO HELP. GEAR VIS UAL CHECK INDICATED GEAR WAS DOWN. RED LIGHT FINALLY WENT OUT AND GREEN LIGHT ILLUMINATED. FLIGHT LANDED WITH NO FURTH ER INCIDENT. MAINTENANCE ADJUSTED THE NLG DOWNLOCK SENSOR PER MM 32-61-51. PERFORMED GEAR SWING, OPS CHECK GOOD. (X) 2 L 7 2 4F A16WE 1996080200097 19960802 00097 NM 1996 8 2 USAASB96124 1 19960709 A 2130 31040 FLOW CONTROL VLV BOEING 737 737201 1384454 NM E/E COMPT FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 226US 21815 MSP - FLT 824 - ON CLIMB-OUT ABOVE 15,000 FEET, A LOUD RUMBLING NOISE BEGAN. CREW DECIDED TO RETURN TO FIELD AT MSP. A LL AIRCRAFT INDICATORS WERE NORMAL. CREW SWITCHED EQUIPMENT COOLING FAN TO ALTERNATE, THEN GASPER FAN TO OFF, NO HELP. NOSE EVENTUALLY DIMINISHED AND QUIT BELOW 10,000 FEET. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE INSPECTED DOORS AND WING-TO-BODY FAIRINGS. NO DEFECTS NOTED. AIRCRAFT WAS PRESSURIZED AND CHEC KED FOR LEAKS. ALL CHECKED GOOD. REPLACED EQUIPMENT COOLING AUTO FLOW CONTROL VALVE. OPS CHECKED GOOD. (X) 2 L 7 2 4F A16WE 1996080200098 19960802 00098 NE 1996 8 2 USAASB96126 2 19960712 A 7321 FUEL CONTROL BOEING 737 7372B7 1384560 NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE OUT OF TRIM A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 281AU 23114 CLT - FLT 560 - TAKEOFF ROLL-OUT OF PIT WAS NORMAL. UPON PASSING 100 KNOTS, THE THROTTLES SPLIT UNTIL CLIMB POWER WAS R EACHED. ALL INDICATIONS SHOWED NORMAL THEN. CREW CONTACTED MAINTENANCE CONTROL VIA ARINC. DECISION WAS MADE TO DIVERT TO CLT WHERE THE FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE TRIMMED THE FUEL CONTROL UNIT ON THE NR 2 ENGINE. (X) 2 L 7 2 4F 4 F A16WE E2EA 1996080200099 19960802 00099 NM 1996 8 2 USAASB96127 1 19960713 A 2120 65C280055 SUPPLY DUCT BOEING 737 737301 1384611 NM A/C DIST BAY BLOWN A USAA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 EA 19 586US 23931 DEN - FLT 600 - DURING CRUISE, CREW REPORTED A FUSELAGE VIBRATION AT ROW 9 A, B, C. CAPTAIN CONTACTED MAINTENANCE CONTR OL VIA ACARS AND TOGETHER THEY COULD NOT PINPOINT A CLEAR CAUSE OF THE VIBRATION. A DECISION WAS MADE TO DIVERT TO DEN WHERE THE FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE CONTROL CABIN SUPPLY DUCT IN THE AIR CONDITIONI NG DISTRIBUTION BAY BLOWN. REPAIRED SAME. LEAK CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1996080200100 19960802 00100 NM 1996 8 2 USAASB96128 1 19960714 A 7921 749965 OIL COOLER BOEING 737 7372Q9 138448M NM NR 1 ENGINE FAILED A A USAA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 EA 19 230AU 25774 21975 BOS - FLT 788 - ON CLIMB-OUT AT APPROXIMATELY 10,000 FEET, THE NR 1 ENGINE OIL TEMPERATURE GAUGE WENT INTO THE YELLOW BA ND. TEMPERATURE DECREASED WITH POWER INCREASE AND INCREASED WITH POWER DECREASE. CREW DECIDED TO RETURN TO FIELD AT BO S. OIL TEMPERATURE WAS IN YELLOW BAND FOR APPROXIMATELY 15 MINUTES. TEMPERATURE RETURNED TO GREEN BAND DURING DESCENT AND LANDING. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED SAFELY WITH NO FURTHER INCIDENT. MAINTENANCE INSPECTED TH E TEMPERATURE BULB CANNON PLUG. CHECKED NORMAL. THEY ALSO REMOVED AND REPLACED THE NR 1 ENGINE OIL COOLER. LEAK CHECK GOOD. POWER RUN GOOD. (X) 2 L 7 2 4F A16WE 1996080200101 19960802 00101 NM 1996 8 2 USAASB96129 1 19960715 A 2820 10608488 FUEL HOSE BOEING 737 7372B7 1384560 NM NR 1 ENG STRUT FAILED A A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 276AU 22888 BWI - FLT 1176 - EN ROUTE FROM MCO TO BDL, CAPTAIN NOTICED WHAT APPEARED TO BE A FUEL LOSS AND SUSPECTED A FUEL LEAK. C APTAIN DECLARED AN EMERENCY AND THE FLIGHT DIVERTED TO BWI. AFTER LANDING SAFELY AND EXITING RUNWAY, FIRE DEPARTMENT TO LD CREW A BAD FUEL LEAK WAS COMING FROM THE NR 1 ENGINE AND RECOMMENDED TO PULL FIRE HANDLE. FIRE HANDLE WAS PULLED WHI CH DISCHARGED FIRE BOTTLE TO NR 1 ENGINE. AIRCRAFT WAS TOWED TO GATE WITH PASSENGERS ON BOARD. MAINTENANCE REPLACED TH E FUEL HOSE ASSY IN THE STRUT FOR THE NR 1 ENGINE. LEAK CHECK GOOD. THEY ALSO REPLACED THE NR 1 ENGINE FIRE BOTTLE AND SQUIB. OPS CHECK SATISFACTORY PER MM. (X) 2 L 7 2 4F A16WE 1996080200102 19960802 00102 NM 1996 8 2 USAASB96130 1 19960716 A 3230 RETRACT MECH BOEING 737 7372B7 1384560 NM NLG LACK OF LUBE A USAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 19 286AU 23133 PIT - FLT 1589 - DURING APPROACH TO PIT AND LANDING GEAR LOWERED, NOSE GEAR RED LIGHT STAYED ON. CREW RECYCLED GEAR, BU T NOSE GEAR RED LIGHT STILL SHOWED RED FOR APPROXIMATELY 20 SECONDS, THEN TURNED GREEN. FLIGHT LANDED SAFELY WITH NO FU RTHER INCIDENT. MAINTENANCE JACKED AIRCRAFT AND LUBRICATED NOSE GEAR. ACCOMPLISHED GEAR RETRACTION/EXTENSION CHECK. O PERATIONAL CHECK AND INDICATION NORMAL. (X) 2 L 7 2 4F A16WE 1996080200103 19960802 00103 WP 1996 8 2 9616011157 1 19960725 A 7931 VT0304C OIL PRESS TRANSM DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 3 ENGINE FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 157US 46766 86170 DURING TAKEOFF, THE NR 3 ENGINE OIL PRESSURE DROPPED TO 20 PSI. THE TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GA TE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 3 ENGINE OIL PRESSURE TRANSMITTER AND OIL PRESSURE INDICATOR. PERFORMED LEAK AND OPERATIONAL CHECK. CHECKS WERE NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A22WE E20EA 1996080200104 19960802 00104 WP 1996 8 2 CALA9601053 1 19960724 A 3350 EMBS1392 CHARGER DOUG DC10 DC1030 3023501 WP CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 68065 46590 THE EMERGENCY LIGHT SYSTEM WOULD NOT TEST DURING A PRE-FLIGHT TEST. INSPECTION FOUND FORWARD, MID, AND AFT BATTERY CHAR GERS INOPERATIVE. THE BATTERY CHARGERS WERE REMOVED AND REPLACED. THE EMERGENCY LIGHT SYSTEM TESTED GOOD. 2 L 7 3 4F A22WE 1996080200105 19960802 00105 WP 1996 8 2 CALA9601054 1 19960724 A 3350 EMSE299 BATTERY PACK DOUG DC10 DC1030 3023501 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 68065 46590 INSPECTION FOUND EMERGENCY EXIT LIGHTS AT L-1, L-2, AND L-4 DOORS INOPERATIVE. THE BATTERY PACKS WERE REMOVED AND REPLA CED AND OPERATION OF THE EMERGENCY EXIT LIGHTS WAS RESTORED. 2 L 7 3 4F A22WE 1996080200106 19960802 00106 WP 1996 8 2 CALA9601055 1 19960725 A 2450 914F5655 BUS GEN CONT DOUG DC9 DC981 3022081 WP EQUIP INSTL INOPERATIVE A CALA O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SW 09 37882 9334 9222 48027 BOTH GENERATOR OFF-LIGHTS ILLUMINATED AND ALL GENERATOR POWER WAS LOST DURING CLIMB AT 9,000 FEET. THE AC CROSSTIE LOCK OUT LIGHT ALSO CAME ON. THE GENERATORS WERE RESET AND OPERATION WAS NORMAL, BUT THE AC CROSSTIE LOCKOUT LIGHT REMAINED ILLUMINATED. THE FLIGHT WAS CONTINUED WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND THE BUS GENERATOR CONTROL UNIT AT FAU LT. THE BUS GENERATOR CONTROL UNIT WAS REMOVED AND REPLACED. THE ENGINES WERE RUN AND OPERATIONAL CHECKS WERE GOOD. P ART TOTAL CYCLES 6,407. 2 L 7 2 4F A6WE 1996080200107 19960802 00107 WP 1996 8 2 CALA9601056 1 19960725 A 3210 LINK DOUG DC9 DC982 3022082 WP LT MLG BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72822 49482 THE CREW FOUND FORWARD UPPER SUPPORT LINK ON LT MLG BROKEN DURING A PREFLIGHT CHECK. THE FORWARD UPPER SUPPORT LINK ON LT MLG WAS REMOVED AND REPLACED IAW MM 32-11-04, PAGE 205-206A. 2 L 7 2 4F A6WE 1996080200108 19960802 00108 NM 1996 8 2 CALA9601057 1 19960711 A 5320 FITTING BOEING 737 7372C0 1384488 NM BS 695 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14245 20074 INSPECTION FOUND A CRACK IN VERTICAL LEG OF FORWARD HALF OF LOWER LT FITTING AT B.S. 695, STRINGER 18A. THE CRACKED FIT TING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW DRAWING NR 65C34490 AND SA008-5310-02456 THROUGH SA0013-5310-02456. 2 L 7 2 4F A16WE 1996080200109 19960802 00109 NM 1996 8 2 CALA9601058 1 19960710 A 5320 CHORD BOEING 737 7372C0 1384488 NM BS 727 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14245 20074 INSPECTION FOUND A CRACK PAST SECOND FASTENER HOLE OF CHORD AT STRINGER 18A ON BOTH THE LT AND RT SIDES OF B.S. 727. TH E CHORD SEGMENTS WERE REMOVED AND REPLACED IAW BOEING DRAWING 65C33722 AND CAL WORK CARD 15-5310-1-0023. 2 L 7 2 4F A16WE 1996080200110 19960802 00110 NM 1996 8 2 CALA9601059 1 19960710 A 5312 BULKHEAD WEB BOEING 737 7372C0 1384488 NM BS 178 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14245 20074 INSPECTION FOUND A 7 INCH CRACK IN PRESSURE BULKHEAD WEB AT WL 218, STA 178 ON BOTH LT AND RT SIDES. BOTH CRACKED AREAS OF BULKHEAD WEB WERE CUT OUT. FILLER AND DOUBLER REPAIRS WERE FABRICATED AND INSTALLED IAW SRM'S 53-10-2, 51-10-2, AND 51-30-2. 2 L 7 2 4F A16WE 1996080200111 19960802 00111 NM 1996 8 2 CALA9601060 1 19960710 A 5330 SKIN BOEING 737 7372C0 1384488 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14245 20074 INSPECTION FOUND FUSELAGE SKIN CORRODED JUST AFT OF AFT CARGO DOOR AFT LOWER CORNER. THE CORRODED SECTION OF SKIN WAS C UT OUT. FILLER AND SPLICE DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-30-3 AND SRM 51-30-2. 2 L 7 2 4F A16WE 1996080200112 19960802 00112 NM 1996 8 2 CALA9601061 1 19960710 A 5330 SKIN BOEING 737 7372C0 1384488 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14245 20074 INSPECTION FOUND FUSELAGE SKIN CORRODED AT OUTFLOW VALVE. THE CORRODED SECTION OF SKIN WAS CUT OUT. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM'S 53-30-3, 51-10-6, AND 51-10-2. 2 L 7 2 4F A16WE 1996080200113 19960802 00113 WP 1996 8 2 CALA9601062 1 19960627 A 5350 LATCH DOUG DC9 DC932 3022066 WP TAILCONE OUT OF RIG A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 THE TAILCONE EXTERIOR RELEASE HANDLE PULLED LOW AT 20 POUNDS. TAILCONE LATCH ADJUSTMENT WAS PERFORMED AND PULL WAS WITH IN SPECIFICATIONS PER MM 53-50-3. 2 L 7 2 4F A6WE 1996080200114 19960802 00114 WP 1996 8 2 CALA9601063 1 19960702 A 5314 KEEL BEAM DOUG DC9 DC932 3022066 WP BS 622 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND A CRACK IN RT SIDE OF KEEL BEAM AT STA 622. A DOUBLER WAS INSTALLED IAW SRM 53-05. 2 L 7 2 4F A6WE 1996080200115 19960802 00115 WP 1996 8 2 CALA9601064 1 19960702 A 5320 FLR SUPPORT DOUG DC9 DC932 3022066 WP CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND FLOOR SUPPORT CORRODED AT FORWARD SIDE OF PANEL NR 7A, FORWARD ENTRY. A NEW FLOOR SUPPORT WAS FABRICAT ED AND INSTALLED IAW SRM 51-30-0. 2 L 7 2 4F A6WE 1996080200116 19960802 00116 NM 1996 8 2 P5CA9600394 1 19960726 A 5314 KEEL BEAM BOEING 747 747122 1384872 NM BS 1000 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 DURING B-CHECK, FOUND LEVEL 1 CORROSION ON RIGHT SIDE OF THE KEEL BEAM BS 1000. REMOVED AND TREATED CORROSION WITHIN LI MITS PER BOEING SRM 51-10-01. 2 L 7 4 4F A20WE 1996080200117 19960802 00117 NM 1996 8 2 P5CA9600395 1 19960726 A 7800 EXHAUST SLEEVE BOEING 747 747122 1384872 NM NR 2 ENGINE PIECE MISSING A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 DURING B-CHECK, FOUND NR 2 ENGINE EXHAUST SLEEVE, LEFT SIDE, MANY FASTENERS LOOSE AND MISSING, LOWER RIGHT LEADING EDGE SKIN PIECE MISSING, REMOVED AND REPLACED FASTENERS, INSTALLED DOUBLERS PER BOEING SRM 54-30-03 AND SRM 51-10-01. 2 L 7 4 4F A20WE 1996080200118 19960802 00118 NM 1996 8 2 P5CA9600396 1 19960726 A 2560 SLIDE BAR BOEING 747 747122 1384872 NM RIGHT WORN THROUGH A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 DURING B-CHECK, FOUND RIGHT BODY GEAR OUTBOARD DOOR SLIDE BAR FORWARD UPPER FLANGE WORN THROUGH. FABRICATED AND INSTALL ED NEW FLANGE CHANNEL PER BOEING SRM 51-10-01. 2 L 7 4 4F A20WE 1996080200119 19960802 00119 NM 1996 8 2 P5CA9600397 1 19960726 A 5522 SKIN BOEING 747 747122 1384872 NM LT ELEVATOR DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 DURING B-CHECK, FOUND LEFT INBOARD ELEVATOR, INBOARD AFT CORNER DELAMINATED. REPAIRED PER BOEING SRM 51-40-15. 2 L 7 4 4F A20WE 1996080200120 19960802 00120 NM 1996 8 2 P5CA9600398 1 19960724 A 5414 SKIN BOEING 747 747122 1384872 NM NR 2 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 DURING B-CHECK, FOUND NR 2 ENGINE PYLON INBOARD AFT LOWER SKIN IS CRACKED AND FASTENERS FORWARD OF CRACK ARE WORKED LOOS E. FABRICATED AND INSTALLED REPAIR DOUBLER PER BOEING SRM'S 51-30-02, 54-30-03, AND 54-50-03. 2 L 7 4 4F A20WE 1996080200121 19960802 00121 NM 1996 8 2 P5CA9600399 1 19960724 A 3211 BUSHING BOEING 747 747122 1384872 NM RT MLG MIGRATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 DURING B-CHECK, FOUND RIGHT BODY GEAR TRUNNION BUSHING MIGRATED BEYOND .050 INCH LIMIT (.075 INCH). RESEATED BODY GEAR TRUNNION BUSHING PER BOEING MAINTENANCE MANUAL 32-13-01. 2 L 7 4 4F A20WE 1996080200122 19960802 00122 NM 1996 8 2 P5CA9600400 1 19960725 A 7810 EXHAUST CASE BOEING 747 747122 1384872 NM NR 2 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 DURING B-CHECK, FOUND NR 2 ENGINE R-RAIL HAS 2 CRACKS AT THE 5:30 AND 7:00 O'CLOCK POSITIONS. WELDED, STRESS RELIEVED, AND SHOT PEENED PER MAINTENANCE MANUAL 72-53-01, AND SRM 51-10-07. 2 L 7 4 4F A20WE 1996080200123 19960802 00123 NM 1996 8 2 P5CA9600401 1 19960725 A 7810 EXHAUST CASE BOEING 747 747122 1384872 NM NR 3 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 DURING B-CHECK, FOUND NR 3 ENGINE R-RAIL HAS 2 CRACKS AT THE 6:00 AND 7:OO O'CLOCK POSITIONS. WELDED, STRESS RELIEVED, AND SHOT PEENED PER MAINTENANCE MANUAL 72-53-01 AND SRM 51-10-07. 2 L 7 4 4F A20WE 1996080200124 19960802 00124 NM 1996 8 2 P5CA9600402 1 19960724 A 5414 SKIN BOEING 747 747122 1384872 NM NR 1 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 DURING B-CHECK, FOUND NR 1 PYLON SKIN CRACKED ON INBOARD SIDE AFT OF LOWER SLOT SEAL. REPAIRED PER BOEING SRM 54-30-03. 2 L 7 4 4F A20WE 1996080200125 19960802 00125 NM 1996 8 2 P5CA9600403 1 19960723 A 7110 COWL BOEING 747 747122 1384872 NM NR 4 ENGINE TORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 DURING B-CHECK, FOUND NR 4 ENGINE OUTBOARD CORE COWL FORWARD UPPER CORNER TORN AND LOOSE FASTENERS ON OUTER SKIN. REPAI RED PER BOEING SRM 51-30-02. 2 L 7 4 4F A20WE 1996080200126 19960802 00126 GL 1996 8 2 RAAA96E4010 2 19960725 A 7210 6874188 RED GEARBOX LKHEED 188 188A 5262602 WP ALLSN 501D 501D13 03004 GL NR 3 ENGINE HIGH OIL PRESS A RAAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 9744C 37016 55 188A1140 500943 NR 3 ENGINE PRECAUTIONARY SHUTDOWN, AT 2026Z WHILE CLIMBING OUT OF ANC, DUE HIGH (244 PSI) REDUCTION GEARBOX OIL PRESSUR E. RETURNED TO ANC. VERIFIED INDICATION SYSTEM. REPLACED RGB OIL PUMP ASSY. DID NOT CORRECT PROBLEM. SUSPECT RGB IN TERNAL OIL SYSTEM RESTRICTION. REPLACED NR 3 ENGINE. 2 L 7 4 4T 4 T RT 4A22 E282 1996080200127 19960802 00127 NM 1996 8 2 SCNA96202 1 19960724 A 3350 1102832 BATTERY PACK BOEING 727 727227 1384078 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 275AF 22092 AFT AIRSTAIR OVERHEAD EMERGENCY LIGHT FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK IN LIGHT ASSEMBLY IN ACCORDANCE WI TH MM 33-50-61. OPS CHECKED GOOD. 2 L 7 3 4F A3WE 1996080200128 19960802 00128 WP 1996 8 2 SRAA960708 1 19960724 A 2620 WIRE DOUG DC8 DC871F 302199D WP NR 2 PYLON FAILED A SRAA A UNSCHED LANDING L NO TEST CR CRUISE 1 GL 23 872SJ 46040 DURING FLIGHT 9829 FROM MIA, NR 2 ENGINE FIRE SHUT-OFF VALVE TRIPS CIRCUIT BREAKER AND WILL NOT RESET. ACCOMPLISHED AIR TURN BACK TO MIA, AIRCRAFT LANDED WITHOUT INCIDENT. REPAIRED WIRING AT NR 2 PYLON SECTION, SYSTEM OPS CHECKED GOOD PER MM CHAPTERS 26-3-1 AND 78-3-1. 2 L 7 4 4F RT 4A25 1996080200129 19960802 00129 1996 8 2 96ZZZX3744 4 19960723 A 2565 11611142 ESCAPE SLIDE BOEING 737 737201 1384454 NM PASSENGER DOOR LOW PRESSURE A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 2944 8 PAA022 19423 DEN - FLT 601 - UPON ARRIVAL, FLIGHT CREW REPORTED THE FORWARD ENTRY DOOR ESCAPE SLIDE BOTTLE PRESSURE AT ZERO. MAINTEN ANCE REPLACED ESCAPE SLIDE. 2 L 7 2 4F A16WE 1996080200130 19960802 00130 EU 1996 8 2 RAIA960701 1 19960628 A 3150 350A23008314 CCAS COMPUTER AEROSP ATR42 ATR42300 8680920 EU COCKPIT OFF LINE A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 03 421TE 11256 8577 102 STL - FLT 7518 - TAKEOFF CONFIGURATION WARNING CAME ON. MAINTENANCE RERACKED THE CCAS COMPUTER, TESTED SYSTEM, OPS CHEC K GOOD. (X) 2 H 7 2 4T RT A53EU 1996080200131 19960802 00131 EU 1996 8 2 RAIA960702 1 19960629 A 3260 9005EN38 SWITCH BAG JETSTM JETSTM3201 1500217 EU MLG DIRTY A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 342TE 954 STL - FLT 7344 - DURING GEAR RETRACTION, RT MAIN STAYED DOWN AND LOCKED. MAINTENANCE CLEANED THE RIGHT MAIN DOWN AND LO CK SWITCH. PERFORMED GEAR SWINGS. OPS CHECK GOOD. AIRCRAFT TT: 8,250.4 HOURS. (X) 2 L 7 2 4T RT A56EU 1996080200132 19960802 00132 EU 1996 8 2 RAIA960703 1 19960630 A 7720 ST3114 TRIM RESISTOR AEROSP ATR42 ATR42300 8680920 EU LT ENGINE BROKEN WIRE A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 421TE 102 STL - FLT 7408 - LEFT ENGINE REACHED MAXIMUM TEMPERATURE BEFORE MEETING TARGET TORQUE. MAINTENANCE REPAIRED WIRE ON THE LEFT T6 TRIM RESISTOR. PERFORMED GROUND RUNS. OPS CHECK GOOD. ENGINE TT: 14,615.6 HRS. (X) 2 H 7 2 4T RT A53EU 1996080200133 19960802 00133 EU 1996 8 2 RAIA960704 1 19960702 A 5230 S533712992088 BOLT AEROSP ATR42 ATR42300 8680920 EU DOOR FRAME OUT OF ADJUST A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 422TE 106 STL - FLT 7176 - AIRCRAFT WOULD NOT PRESSURIZE ABOVE 3 PSI, APPEARS TO BE A CAP AT LOWER EDGE OF CARGO DOOR. ADJUSTED D OOR LATCH RECEPTACLE ECCENTRIC BOLT. AIRCRAFT TT: 17,823.0 HRS. (X) 2 H 7 2 4T RT A53EU 1996080200134 19960802 00134 NE 1996 8 2 RAIA960706 2 19960704 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE RIGHT BIRDSTRIKE A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK C F.O.D. TO TAKEOFF 1 CE 03 567HK 580 41085 76104 STL - FLT 7219 - LEFT AND RIGHT ENGINE BIRD STRIKE. MAINTENANCE PERFORMED BORESCOPE ON LEFT ENGINE, FOUND NO DAMAGE. M AINTENANCE REPLACED RIGHT ENGINE. (X) 2 L 7 2 4T 4 T RT A41NM E18NE 1996080200135 19960802 00135 NE 1996 8 2 RAIA960707 2 19960709 A 7200 ENGINE AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE NR 1 FAILED A A RAIA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 421TE 14706 9142 102 120656 MEM - FLT 7135 - NR 1 ENGINE LOST OIL PRESSURE, ITT WENT TO 850. ENGINE WAS SHUT DOWN AND AIRCRAFT LANDED WITHOUT INCID ENT. MAINTENANCE REPLACED THE NR 1 ENGINE. (X) 2 H 7 2 4T 4 T RT A53EU E20NE 1996080200136 19960802 00136 EU 1996 8 2 RAIA960708 1 19960710 A 3230 IMU5 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU LT MLG OUT OF ADJUST A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 558HK 41071 STL - FLT 7514 - GEAR WOULD NOT RETRACT. MAINTENANCE ADJUSTED LEFT MAIN GEAR AIR/GROUND SQUAT SWITCH. AIRCRAFT TT: 1, 371.0 HRS. (X) 2 L 7 2 4T RT A41NM 1996080200137 19960802 00137 EU 1996 8 2 RAIA960709 1 19960710 A 7603 137907E FRICTION RING BAG JETSTM JETSTM3201 1500217 EU COCKPIT OUT OF ADJUST A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 435AM 889 STL - FLT 7056 - NR 1 ENGINE RPM DROPPING OFF ON TAKEOFF. MAINTENANCE ADJUSTED THE SPEED LEVER FRICTION. AIRCRAFT TT: 11,094.0 HOURS. (X) 2 L 7 2 4T RT A56EU 1996080200138 19960802 00138 EU 1996 8 2 RAIA960710 1 19960720 A 5270 SP4594 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU CARGO DOOR OUT OF ADJUST A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 554HK 2429 41067 JFK - FLT 7789 - CARGO DOOR WARNING CAME ON DURING FLIGHT. MAINTENANCE ADJUSTED AFT POSITION SWITCH. (X) 2 L 7 2 4T RT A41NM 1996080200139 19960802 00139 NM 1996 8 2 TWRA96142 1 19960712 A 2530 TRASH CAN BOEING 747 747130 1384880 NM AFT GALLEY FIRE A TWRA F ACTIVATE FIRE EXT. A FLAME/FIRE CR CRUISE 1 EA 15 603FF 19746 DURING CRUISE, FLIGHT ATTENDANT FIRED L-5 HALON FIRE EXTINGUISHER INTO THE AFT DRY GALLEY TRASH RECEPTACLE DUE TO AN APP ARENT FIRE. IT IS BELIEVED TO BE CAUSED BY A PASSENGER'S CIGARETTE. INSPECTED AREA, FOUND NO DAMAGE. REPLACED FIRE EX TINGUISHER BOTTLE. AIRCRAFT CONTINUED FOR SERVICE. (X) 2 L 7 4 4F A20WE 1996080200140 19960802 00140 NM 1996 8 2 USAA960475 1 19960621 A 5241 SKIN BOEING 737 7372B7 1384560 NM GALLEY DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 287AU 32629 23134 GSO - DURING 'WALKAROUND' VISUAL INSPECTION, FOUND .50 INCH CRACK IN EXTERIOR SKIN FORWARD GALLEY DOOR OUTER SKIN AT THE FORWARD UPPER CORNER OF THE LOWER HINGE CUT OUT. INSTALLED DOUBLER, REPAIRED PER TYPICAL REPAIR 52-10-01 A. (X) 2 L 7 2 4F A16WE 1996080200141 19960802 00141 NM 1996 8 2 USAA960476 1 19960620 A 5312 BULKHEAD BOEING 737 737201 1384454 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 246US 36978 22753 INT - DURING 'Q-6' CHECK VISUAL INSPECTION FOUND 3 CRACKS, 1 INCH, 1 INCH, AND .50 INCH, 178 BULKHEAD. STOP DRILL CRACK S, FABRICATED DOUBLER, FILLERS, AND INSTALLED. REPAIRED PER SRM 51-10-1, TR 53-10-11. (X) 2 L 7 2 4F A16WE 1996080200142 19960802 00142 NM 1996 8 2 USAA960477 1 19960620 A 5312 BULKHEAD BOEING 737 737201 1384454 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 246US 36978 22753 INT - DURING 'Q-6' CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK, 178 BULKHEAD. STOP DRILLED CRACK, FABRICATED DOUBLER, F ILLERS, AND INSTALLED. REPAIRED PER SRM 51-01-1, TR 53-10-11. (X) 2 L 7 2 4F A16WE 1996080200143 19960802 00143 NM 1996 8 2 USAA960478 1 19960620 A 5312 BULKHEAD BOEING 737 737201 1384454 NM BS 1156 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 246US 36978 22753 INT - DURING 'Q-6' CHECK VISUAL INSPECTION, FOUND .50 INCH CRACK BS 1156, WL 380 RT OUTBOARD CHORD OF BULKHEAD. STOP DR ILLED AND INSTALLED REPAIR. REPAIRED PER EO 5391G569. (X) 2 L 7 2 4F A16WE 1996080200144 19960802 00144 NM 1996 8 2 USAA960479 1 19960620 A 5315 FLOOR BEAM BOEING 737 737201 1384454 NM BS 328 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 246US 36978 22753 INT - DURING 'Q-6' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 2 INCH CORROSION FLOOR BEAM, STA 328, LBL 27. FABRICATED TE E-CAP REPAIR, REPAIRED PER TR 53-10-13. (X) 2 L 7 2 4F A16WE 1996080200145 19960802 00145 NM 1996 8 2 USAA960480 1 19960620 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 246US 36978 22753 INT - DURING 'Q-6' CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK, STR 18A SHELF, 1 INCH FORWARD OF STA 727 BULKHEAD AT I NBOARD VERTICAL FASTENER. STOP DRILL CRACK AND INSTALLED REPAIR KIT. REPAIRED PER EO 5393G256. (X) 2 L 7 2 4F A16WE 1996080200146 19960802 00146 NM 1996 8 2 USAA960481 1 19960620 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 246US 36978 22753 INT - DURING 'Q-6' CHECK VISUAL INSPECTION, FOUND 1.6250 INCH CRACK IN OUTER SKIN S18R, BS 727A PLUS 7 INCHES. DOUBLER INSTALLED, REPAIRED PER SRM 53-30-3. (X) 2 L 7 2 4F A16WE 1996080200147 19960802 00147 NM 1996 8 2 USAA960482 1 19960620 A 5320 STIFFENER BOEING 737 737201 1384454 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 246US 22753 INT - DURING 'Q-6' CHECK EDDY CURRENT, FOUND .50 INCH LONG CRACK AT STIFFENER STA 178, LBL 5.7 INCH, WL 184. INSTALLED REPAIR ANGLES AND REPAIRED PER TR 53-10-17. (X) 2 L 7 2 4F A16WE 1996080200148 19960802 00148 NM 1996 8 2 USAA960483 1 19960622 A 5313 STRINGER BOEING 737 7372B7 1384560 NM BS 967-974 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 278AU 35513 22890 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 7 INCH BY 3 INCH CORRODED AREA, STR 25L, BS 967 TO BS 974. INSTALLED REPAIR DOUBLER, REPAIRED PER SRM 53-10-3. CORROSION TASK NR: C53-202-01. CORROSION LEVEL: 2. (X) 2 L 7 2 4F A16WE 1996080200149 19960802 00149 NM 1996 8 2 USAA960484 1 19960622 A 5314 KEEL BEAM BOEING 737 7372B7 1384560 NM BS 672-727 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 278AU 35513 22890 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND FRETTING CORROSION 55 INCHES RIGHT KEEL BEAM LOWER CORD STA 672 TO STA 727. INSTALLED REPAIR STRAP, REPAIRED PER EA 41232. CORROSION TASK NR: C53-212-01. CORROSION LEVEL: 2. (X) 2 L 7 2 4F A16WE 1996080200150 19960802 00150 NM 1996 8 2 USAA960485 1 19960622 A 5320 T-CAP BOEING 737 7372B7 1384560 NM BS 1016 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 278AU 35513 22890 INT - DURING Q-CHECK VISUAL INSPECTION, FOUND T-CAP SURFACE CORROSION AT LBL 15, STA 1016. REMOVED PRE-EXISTING REPAIR, FABRICATED NEW REPAIR AND REPAIRED PER SRM 53-10-9. (X) 2 L 7 2 4F A16WE 1996080200151 19960802 00151 NM 1996 8 2 USAA960486 1 19960622 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 328 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 278AU 35513 22890 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORRODED SCREW HOLES ON FLOOR BEAM BS 328 22 INCHES R BL 36 INCHES RBL AND 42 INCHES RBL. REPLACED SECTION OF FLOOR BEAM AND INSTALLED ANGLES. REPAIRED PER TR 53-10-13. (X ) 2 L 7 2 4F A16WE 1996080200152 19960802 00152 NM 1996 8 2 USAA960487 1 19960622 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 967 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 278AU 35513 22890 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY 1 INCH CORRODED AREAS ON FLOOR BEAM UPPER FLANGE BS 967 LBL 27 INCHES TO RBL 52 INCHES. INSTALLED T-SECTION WITH REPAIR ANGLES AND STRAPS, REPAIRED PER EA NR 41242. (X) 2 L 7 2 4F A16WE 1996080200153 19960802 00153 NM 1996 8 2 USAA960488 1 19960622 A 5313 STRINGER BOEING 737 7372B7 1384560 NM BS 967-972 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 278AU 35513 22890 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 5 INCH BY 3 INCH CORRODED AREA STR 27L BS 967 TO BS 972. INSTALLED ST RINGER SPLICE, REPAIRED PER SRM 53-10-3, FIGURE 1. CORROSION TASK NR: C53-208-01. CORROSION LEVEL: 2. (X) 2 L 7 2 4F A16WE 1996080200154 19960802 00154 NM 1996 8 2 USAA960489 1 19960622 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 947.5 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 278AU 35513 22890 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND SEVERAL CORRODED AREAS 1 INCH BY 1 INCH ON FLOOR BEAM BS 947.5 LBL 37 INCHES TO RBL 35 INCHES. INSTALLED T-CAP WITH REPAIR ANGLES, REPAIRED PER SRM 53-10-9. (X) 2 L 7 2 4F A16WE 1996080200155 19960802 00155 NM 1996 8 2 USAA960490 1 19960622 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 986.5 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 278AU 35513 22890 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY 1 INCH CORRODED AREAS ON FLOOR BEAM UPPER FLANGE BS 986.5 LBL 27 INCHES TO RBL 52 INCHES. INSTALLED T-SECTION WITH REPAIR ANGLES AND STRAPS, REPAIRED PER EA NR 41243. (X) 2 L 7 2 4F A16WE 1996080200156 19960802 00156 NM 1996 8 2 USAA960505 1 19960703 A 5330 SKIN BOEING 737 737201 1384454 NM BS 760 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 227AU 41700 21816 ROA - DURING 'BX' CHECK VISUAL INSPECTION, CONFIRMED WITH HFEC, FOUND .75 INCH FUSELAGE SKIN CRACK S19L, BS 760. STOP D RILLED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3, FIGURE 3. (X) 2 L 7 2 4F A16WE 1996080200157 19960802 00157 NM 1996 8 2 USAA960506 1 19960703 A 5330 SKIN BOEING 737 737201 1384454 NM DOOR CUT OUT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 227AU 41700 21816 ROA - DURING 'BX' CHECK VISUAL INSPECTION, FOUND .4375 INCH CRACK AT AFT ENTRY DOOR CUT OUT FORWARD LOWER HINGE CUT OUT FUSELAGE SKIN. REMOVED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3, FIGURE 34. (X) 2 L 7 2 4F A16WE 1996080200158 19960802 00158 NM 1996 8 2 W8PA960062 1 19960722 A 3350 20131A BATTERY PACK BOEING 737 7373L9 1384470 NM CABIN DISCHARGED A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 960WP 21493 23331 EMERGENCY PATH LIGHT INOPERATIVE IN ONE SECTION OF THE CABIN. REPLACED BATTERY PACK ASSEMBLY AT MID-CABIN AFT. (X) 2 L 7 2 4F RT A16WE 1996080200160 19960802 00160 EU 1996 8 2 9616033206 1 19960728 A 3244 TIRE AIRBUS 320 A320211 3930320 EU NR 1 FLAT A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 306US 60 DURING TAKEOFF ROLL, RECEIVED BRAKES HOT AND DELAY TAKEOFF MESSAGES. TAKEOFF WAS ABORTED BETWEEN 60 AND 70 KNOTS. AIRC RAFT RETURNED TO THE GATE WHERE MAINTENANCE FOUND THE NR 1 TIRE FLAT. REPLACED NR 1 AND NR 2 TIRES. LEAK CHECK OK. 2 L 7 2 4F RT A28NM 1996080200161 19960802 00161 WP 1996 8 2 CALA9601065 1 19960724 A 4940 360452425 IGNITION SYST 38003681 DOUG DC9 DC982 3022082 WP APU INOPERATIVE A CALA O OTHER O OTHER CR CRUISE 1 SW 09 937MC 8679 115 P184C 49450 THE APU SHUT DOWN WHILE EN ROUTE TO EWR. A RESTART ATTEMPT WAS UNSUCCESSFUL. THE APU COMBUSTOR UNIT AND IGNITION EXCIT ER WERE REMOVED AND REPLACED. THE APU WAS OPERATED SEVERAL TIMES AND LEAK AND OPERATIONAL CHECKS WERE GOOD. PART TOTAL CYCLES, 5,593. 2 L 7 2 4F A6WE 1996080200162 19960802 00162 WP 1996 8 2 CALA9601066 1 19960728 A 3230 NCG6001 GRD SENSE DOUG DC10 DC1010 3022110 WP NLG OUT OF RIG A CALA O OTHER J WARNING INDICATION CL CLIMB 1 SW 09 68047 47801 THE LANDING GEAR WOULD NOT RETRACT ON FIRST ATTEMPT AFTER TAKEOFF FROM SPN. THE GEAR HANDLE WOULD NOT GO TO THE UP POSI TION UNTIL THE OVERRIDE BUTTON WAS USED. THE FLIGHT CONTINUED TO GUM WHERE IT LANDED WITHOUT INCIDENT. THE AIRCRAFT HA D A BRIEF HISTORY OF PROBLEMS WITH THE GEAR HANDLE NOT RAISING TO THE UP POSITION. MAINTENANCE FOUND THE GROUND SENSING MECHANISM OUT OF RIG. THE GROUND SENSING MECHANISM WAS ADJUSTED AND TESTED PER MM 32-24-01. THE GEAR WAS CYCLED SEVER AL TIMES AND OPERATION CHECKED GOOD. 2 L 7 3 4F A22WE 1996080200163 19960802 00163 WP 1996 8 2 CALA9601067 1 19960702 A 5320 FLR SUPPORT DOUG DC9 DC932 3022066 WP CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND FORWARD ENTRY FLOOR SUPPORT AT PANEL NR 12 AND NR 13 CORRODED. THE FLOOR SUPPORT WAS REPLACED IAW SRM 53-01. 2 L 7 2 4F A6WE 1996080200164 19960802 00164 WP 1996 8 2 CALA9601068 1 19960701 A 5320 FLR SUPPORT DOUG DC9 DC932 3022066 WP BS 446 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND A 1 INCH CRACK IN FORWARD BAGGAGE BIN FLOOR SUPPORT AT STA 446, LONGERON 29R. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1996080200165 19960802 00165 WP 1996 8 2 CALA9601069 1 19960705 A 5320 39143301 FITTING DOUG DC9 DC932 3022066 WP PAX DOOR JAMB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND A 1.125 INCH CRACK IN MAIN CABIN DOOR JAMB INTERNAL FITTING FOR DOOR STOP. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-00. 2 L 7 2 4F A6WE 1996080200166 19960802 00166 WP 1996 8 2 CALA9601070 1 19960716 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 148-160 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL BETWEEN STA 148-160, LONGERON 11R. THE INTERCOSTAL WAS REPAIRED IAW SRM 53-05, FIGURE 100. 2 L 7 2 4F A6WE 1996080200167 19960802 00167 WP 1996 8 2 CALA9601071 1 19960701 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 756 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND A CRACK IN LONGERON 2L AT STA 756. THE CRACKED SECTION OF LONGERON WAS REMOVED AND A NEW SECTION WAS S PLICED IN IAW SRM 53-02, FIGURE 2. 2 L 7 2 4F A6WE 1996080200168 19960802 00168 WP 1996 8 2 CALA9601072 1 19960701 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 699 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND A .25 INCH CRACK IN LONGERON 1L AT STA 699. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIGURE 4. 2 L 7 2 4F A6WE 1996080200169 19960802 00169 WP 1996 8 2 CALA9601073 1 19960701 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 699 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND LONGERON 5L CRACKED AT STA 699. THE LONGERON WAS REPAIRED IAW SRM 53-02. 2 L 7 2 4F A6WE 1996080200170 19960802 00170 WP 1996 8 2 CALA9601074 1 19960701 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 699 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND A .1250 INCH CRACK IN LONGERON 5R AT STA 699. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIGURE 2. 2 L 7 2 4F A6WE 1996080200171 19960802 00171 WP 1996 8 2 CALA9601075 1 19960701 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 699 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND A CRACK IN LONGERON 6L AT STA 699. A NEW LONGERON WAS INSTALLED IAW SRM 53-02. 2 L 7 2 4F A6WE 1996080200172 19960802 00172 WP 1996 8 2 CALA9601076 1 19960701 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 639 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND A CRACK IN LONGERON 6L AT STA 639. A NEW LONGERON WAS INSTALLED IAW SRM 53-02. 2 L 7 2 4F A6WE 1996080200173 19960802 00173 WP 1996 8 2 CALA9601077 1 19960716 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 658 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND A CRACK IN LONGERON 6L AT STA 658. A NEW LONGERON WAS INSTALLED IAW SRM 53-02. 2 L 7 2 4F A6WE 1996080200174 19960802 00174 WP 1996 8 2 CALA9601078 1 19960715 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 160-200 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND FOUR 1.25 INCH CRACKS IN LONGERON 4L FROM STA 160-200. THE CRACKED AREAS WERE CUT OUT AND A NEW SECTIO N OF LONGERON WAS SPLICED IN IAW SRM 53-02, FIGURE 2. 2 L 7 2 4F A6WE 1996080200175 19960802 00175 WP 1996 8 2 CALA9601079 1 19960715 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 160 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND TWO 1.25 INCH CRACKS IN LONGERON 3L AT STA 160. THE CRACKED SECTION OF LONGERON WAS REMOVED AND A NEW SECTION WAS SPLICED IN IAW SRM 53-02, FIGURE 2. 2 L 7 2 4F A6WE 1996080200176 19960802 00176 WP 1996 8 2 CALA9601080 1 19960715 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 200 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND TWO 1.25 INCH CRACKS IN LONGERON 2L AT STA 200. THE CRACKED SECTION OF LONGERON WAS REMOVED AND A NEW SECTION WAS SPLICED IN IAW SRM 53-02, FIGURE 2. 2 L 7 2 4F A6WE 1996080200177 19960802 00177 SO 1996 8 2 COMA9610230 1 19960612 A 6120 7757151 BALLSCREW SERVO 78249024 EMB 120 EMB120RT SO PWA 118 PW118A NE HAMSTD 14RF 14RF9 NE PROP CONTL UNIT DEFECTIVE A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 164D 908161 120164 115340 910348 AD-94-22-12. WHILE PERFORMING HAMILTON STANDARD SB 14RF-9-61-A53 REV. S, FOUND THE SPLINES OF THE BALLSCREW SERVO WERE WORN BEYOND LIMITS PRIMARILY ON THE RIGHT SIDE OF THE SPLINES. ACTION TAKEN: SENT PCU OUT TO HAMILTON STANDARD FOR FUR THER EVALUATION. 2 L 7 2 4T 4 T RT A31SO E20NE 6 C P11NE 1996080200178 19960802 00178 SW 1996 8 2 COMA9620013 1 19960728 A 2150 COMPRESSOR SWRNGN SA227 SA227AC 8780603 SW FREON AC SYST FAILED A COMA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 703CA AC703 WHEN FREON A/C SYSTEM SWITCHED OFF FOR ENGINE START, SMOKE WAS OBSERVED COMING FROM THE AIR INTAKE ON NOSE COMPARTMENT. FOUND SMOKE TO BE COMING FROM OVERHEATED COMPRESSOR MOTOR. SYSTEM DEACTIVATED AND PLACED ON DEFERRED MAINTENANCE LIST. 2 L 7 2 4T RT A8SW 1996080200179 19960802 00179 EA 1996 8 2 COMA9660125 1 19960727 A 2913 MPEV30122B HYD PUMP CNDAIR CL600 CL6002B19 EA 3A LOW PRESSURE A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 940CA 5767 1868 7048 GEAR DISAGREE WARNING WHEN SELECTED DOWN DURING LANDING APPROACH. SECOND ATTEMPT WAS NORMAL. REPLACED HYDRAULIC PUMP 3 A. PART TOTAL CYCLES, 5,295. 2 L 7 2 4F RT A21EA 1996080200180 19960802 00180 WP 1996 8 2 MWEA96267 1 19960727 A 2560 27500931 GIRT BAR SPRING DOUG DC9 DC932 3022066 WP FWD GALLEY DOOR WEAK A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 DURING C-CHECK, FOUND GALLEY SERVICE DOOR GIRT BAR LATCH SPRINGS WEAK. REPLACED GIRT BAR LATCH COMPRESSION SPRINGS. 2 L 7 2 4F A6WE 1996080200181 19960802 00181 NM 1996 8 2 MWEA96268 1 19960727 A 2560 SLIDE COVER DOUG MD88 MD88 3023688 NM AFT GALLEY DOOR OUT OF ADJUST A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 DURING INSPECTION, FOUND AFT GALLEY SERVICE DOOR EVACUATION SLIDE COVER HITS DOOR JAMB WHEN OPENING AND CLOSING. ADJUST ED SLIDE COVER. OPS CHECK GOOD. RETURNED A/C TO SERVICE. 2 L 7 2 4F RT A6WE 1996080200182 19960802 00182 WP 1996 8 2 MWEA96269 1 19960728 A 5230 DOOR PAN DOUG DC9 DC914 3022034 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 DURING INSPECTION FOUND AFT CARGO DOOR PAN CRACKED AT BEAM 5 AFT END OF DOOR. INSTALLED DOUBLER REPAIR IAW SRM 52-03, F IG. 8, SHEETS 1 AND 2. 2 L 7 2 4F A6WE 1996080200183 19960802 00183 WP 1996 8 2 MWEA96270 1 19960728 A 5230 DOOR PAN DOUG DC9 DC914 3022034 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 DURING INSPECTION, FOUND FORWARD CARGO DOOR INNER PAN CRACKED NEAR AFT LOCKING CAM. INSTALLED REPAIR IAW SRM 52-05, FIG . 26A. 2 L 7 2 4F A6WE 1996080200184 19960802 00184 WP 1996 8 2 MWEA96271 1 19960728 A 5730 SKIN DOUG DC9 DC932 3022066 WP RT WING DEBONDED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 TEMPORARY REPAIR INSTALLED ON RT WING TRAILING EDGE UPPER SKIN IAW SRM 57-01, FIG. 2, SHEET 2. INSTALLED PERMANENT DOUB LER REPAIR IAW SRM 57-01, FIG. 2, SHEET 2. 2 L 7 2 4F A6WE 1996080200185 19960802 00185 WP 1996 8 2 SCNA96203 1 19960724 A 3260 368658188113 GEAR INDICATION DOUG DC10 DC1030F 3023504 WP FE PANEL MALFUNCTIONED A SCNA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 15 602GC 47923 FOUND ENGINEER'S PANEL LANDING GEAR INDICATOR SHOWING UNSAFE ON RIGHT MAIN. GROUND OPS TESTED NORMAL. 2 L 7 3 4F RT A22WE 1996080200211 19960802 00211 NE 1996 8 2 96ZZZM1131 2 19960624 A 7261 OIL FILTER BOEING 727 727231 1384079 NM PWA JT8 JT8D9 52048 NE NR 2 ENGINE DIRTY A TWAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 CE 05 54333 20460 MCO - DURING CRUISE SHUT DOWN NR 2 ENGINE, S/N 1541, DUE TO OIL FILTER BYPASS LIGHT ILLUMINATION. FOUND METAL PARTICLES IN OIL FILTER. REPLACED ENGINE. ENGINE OPERATION THEN CHECKED NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1996080200212 19960802 00212 NE 1996 8 2 96ZZZM1132 2 19960624 A 7320 FFR101MK10 FF REGULATOR LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B NE NR 2 ENG MALFUNCTIONED A TWAA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 CE 05 31023 193B1080 STL - AFTER TAKEOFF SHUTDOWN NR 2 ENGINE, S/N 4413, DUE TO OVERSPEED AND NO RESPONSE TO THRUST LEVER MOVEMENT. FOUND IN TERNAL MALFUNCTION IN FUEL FLOW REGULATOR MFG P/N FFR101MK10. REPLACED FUEL FLOW REGULATOR. ENGINE OPERATION THEN CHEC KED NORMAL. 2 L 7 3 4F 4 F A23WE E12EU 1996080200213 19960802 00213 NE 1996 8 2 96ZZZM1133 2 19960624 A 7261 OIL FILTER BOEING 727 727231 1384079 NM PWA JT8 JT8D9 52048 NE NR 2 ENGINE DIRTY A TWAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 CE 05 54333 20460 JFK - DURING CRUISE SHUT DOWN NR 2 ENGINE, S/N 1541, DUE TO OIL FILTER BYPASS LIGHT ILLUMINATION. FOUND OIL FILTER FULL OF CARBIDE CRYSTALS CHANGED OIL FILTER, DRAINED ENGINE OIL AND RESERVICED OIL TANK. ENGINE OPERATION THEN CHECKED NORM AL. (M) 2 L 7 3 4F 4 F A3WE E2EA 1996080200214 19960802 00214 NE 1996 8 2 96ZZZM1134 2 19960623 A 7310 QAO3403 FUEL FILTER LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB21122B NE NR 3 ENGINE DIRTY A TWAA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 CE 05 7036T 193B1232 DEN - DURING CRUISE NR 3 ENGINE, S/N 4402, SPUN DOWN. DESCEND TO FL 240 AND RESTARTED ENGINE. REPLACED ENGINE FUEL FIL TER, MFG P/N QA03403, PERFORMED TEST 19 OF MM 71-00-00. ENGINE OPERATION CHECKED NORMAL. 2 L 7 3 4F 4 F A23WE E12EU 1996080200215 19960802 00215 1996 8 2 96ZZZM1135 4 19960621 A 2565 100505201 SLIDE DOUG DC9 DC982 3022082 WP L2 DOOR DEPLOYED A TWAA O OTHER O OTHER CR CRUISE 1 CE 05 904TW 49156 STL - DURING CRUISE, L2 DOOR EVACUATION SLIDE, MFG P/N 100505-201, INFLATED. DEFLATED SLIDE. FOUND EVACUATION SLIDE LA NYARD HAD CAUGHT ON FOOD SERVING CART. REPLACED EVACUATION SLIDE. L2 DOOR OPERATION CHECKED NORMAL. 2 L 7 2 4F A6WE 1996080200216 19960802 00216 WP 1996 8 2 96ZZZM1136 1 19960622 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN WEAK A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 985Z 47491 STL - DURING CRUISE, EMERGENCY LIGHTS ILLUMINATED INTERMITTENTLY. FOUND ALL EMERGENCY LIGHT BATTERY POWER SUPPLY WEAK, MFG P/N 5822-2. REPLACED ALL BATTERY POWER SUPPLIES AND THEN EMERGENCY LIGHT SYSTEM OPERATION CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 1996080200217 19960802 00217 WP 1996 8 2 96ZZZM1137 1 19960615 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 756 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 926L 47172 STL - DURING SPECIAL INSPECTION, FOUND .5 INCH CRACK LONGERON 5R STATION 756, REPAIRED PER SRM 53-02 FIGURE 2. 2 L 7 2 4F A6WE 1996080200218 19960802 00218 WP 1996 8 2 96ZZZM1138 1 19960617 A 3350 58222 BATTERY PACK DOUG DC9 DC915 3022036 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 970Z 45772 STL - DURING DESCENT AISLE EGRESS LIGHTS AT SEAT ROWS 15 THROUGH 17 ILLUMINATED. FOUND POWER SUPPLY BATTERY PACK WEAK, MFG P/N 5822-2. REPLACED POWER SUPPLY BATTERY PACK AND EGRESS LIGHT SYSTEM, OPERATION CHECKED NORMAL. 2 L 7 2 4F A6WE 1996080200219 19960802 00219 WP 1996 8 2 96ZZZM1139 1 19960623 A 5313 LONGERON DOUG DC9 DC951 3022051 WP BS 832 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 417EA 47753 STL - DURING AS-2, FOUND .5 INCH CRACK IN LONGERON 5R STATION 832. REPAIRED LONGERON 5R PER SRM 53-02 FIGURE 2. 2 L 7 2 4F A6WE 1996080200220 19960802 00220 NE 1996 8 2 96ZZZM1140 2 19960620 A 8530 327627 CYLINDER ASSY DOUG DC6 DC6B 3021712 WP PWA R2800 CB3 52026 NE NR 1 ENGINE CRACKED A NACA E ENGINE SHUTDOWN K FLUID LOSS DE DESCENT 1 AL 03 867TA 45202 32304 FLT NR 43 - SHUT DOWN NR 1 ENGINE AT 2110Z DUE TO OIL LOSS. AIRCRAFT FERRIED FROM OTZ TO ANC. MAINTENANCE REPLACED NR 2 CYLINDER DUE TO CRACKED HEAD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 4 4R 4 R 6A4 E264 1996080200221 19960802 00221 NM 1996 8 2 96ZZZM1141 1 19960612 A 2131 FITTING BOEING 727 727231 1384079 NM CONTROLLER LOOSE A MYWA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 808MA 21988 IAH - RETURN FROM FLIGHT, UPON CLIMB-OUT, FOUND CABIN PRESSURIZATION UNCONTROLLABLE IN AUTO AND STANDBY. SWITCHED TO MA NUAL DC. CABIN RATE NOT CONTROLLABLE. SHUT OFF ONE PACK. CABIN STARTED TO RISE UNCONTROLLABLE. CLOSED CARGO HEAT OUT FLOW VALVE. CABIN STARTED TO DESCEND ON DESCENT. ON POST FLT INSPECTION, FOUND FITTING ON CABIN PRESSURE CONTROLLER TO BE LOOSE, TIGHTENED. OPS CHECK IAW MM 21-30-00 NORMAL. (M) 2 L 7 3 4F A3WE 1996080200222 19960802 00222 NM 1996 8 2 96ZZZM1142 1 19960607 A 7722 152RL801E EGT IND BOEING 727 727225 1384077 NM NR 2 ENGINE INTERMITTENT A MYWA A UNSCHED LANDING P NO WARNING INDICATION CR CRUISE 1 SO 19 806MA 0145 22437 MIA - RETURN FROM FLIGHT - NR 2 ENGINE EGT READS 200 DEGREES CELSIUS LOWER THAN NR 1 AND NR 3 ENGINES AT 23,000 IN FLIGH T. REMOVED 'J' BOX ON NR 2 ENGINE AND CLEANED CONNECTORS. REMOVED AND REPLACED NR 2 ENGINE EGT INDICATOR IAW 77-20. ( M) 2 L 7 3 4F A3WE 1996080200223 19960802 00223 NM 1996 8 2 96ZZZM1143 1 19960524 A 2750 66258752 COUPLING BOEING 727 727225 1384077 NM NR 2 FLAP TRANS MISSING A MYWA O OTHER J WARNING INDICATION DE DESCENT 1 SO 19 886MA 21855 MIA - ON APPROACH, THE OUTBOARD FLAPS HAD AN ASYMMETRY CONDITION. PERFORMED CHECKLIST 2A114. INSPECTED THE OUTBOARD FL AP DRIVE SYSTEM. FOUND THE LEFT OUTBOARD FLAP DRIVE COUPLING DISCONNECTED AT ITS INBOARD JACKSCREW. INSTALLED MISSING SCREWS AND RIGGED FLAPS AS PER MM 27-51-12. OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996080200224 19960802 00224 EU 1996 8 2 96ZZZM1144 1 19960628 A 3246 AH53352 WHEEL ASSY DUNLOP FOKKER F27 F27MK200 4990620 EU NLG WORN A OIZA O OTHER E VIBRATION/BUFFET TO TAKEOFF 1 WP 19 279MA 11816 KQ048 10297 NOSE GEAR VIBRATION ON TAKEOFF, LANDING AND TAXI NORMAL. REMOVED AND REPLACED NOSE WHEEL ASSY. 2 H 7 2 4T A817 1996080200225 19960802 00225 WP 1996 8 2 96ZZZM1145 1 19960604 A 5330 SKIN DOUG DC6 DC6A 3021706 WP BS 123 CRACKED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 874TA 44641 FOUND SKIN CRACKED, FS 123 AFT OF MAIN CARGO DOOR FRAME. REWORKED IAW 4-29. 2 L 7 4 4R 6A3 1996080200226 19960802 00226 WP 1996 8 2 96ZZZM1146 1 19960604 A 5330 SKIN DOUG DC6 DC6A 3021706 WP BS 123 CRACKED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 874TA 44641 FOUND SKIN CRACKED, FS 123 FWD MAIN CARGO DOOR. REWORKED, IAW SRM 4-29. 2 L 7 4 4R 6A3 1996080200227 19960802 00227 WP 1996 8 2 96ZZZM1147 1 19960604 A 5330 SKIN DOUG DC6 DC6A 3021706 WP BS 801 CRACKED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 874TA 44641 FOUND SKIN CRACKED, FS 801 RIGHT EMERGENCY EXIT. REWORKED IAW SRM 4-29. 2 L 7 4 4R 6A3 1996080200228 19960802 00228 WP 1996 8 2 96ZZZM1148 1 19960604 A 5330 SKIN DOUG DC6 DC6A 3021706 WP BS 111 CRACKED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 874TA 44641 FOUND SKIN CRACKED, FS 111 FORWARD OF LOWER BAGGAGE DOOR. REWORKED, IAW SRM 4-29. 2 L 7 4 4R 6A3 1996080200229 19960802 00229 WP 1996 8 2 96ZZZM1149 1 19960604 A 5330 SKIN DOUG DC6 DC6A 3021706 WP BS 200 CRACKED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 874TA 44641 FOUND SKIN CRACKED, FS 200 AFT LOWER CORNER OF FORWARD MAIN CARGO DOOR. REWORKED IAW SRM 4-29. 2 L 7 4 4R 6A3 1996080200230 19960802 00230 WP 1996 8 2 96ZZZM1150 1 19960611 A 5320 SUPPORT LKHEED 1011 10113851 5265010 WP LWR GALLEY CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 319EA 193A1040 FOUND LEVEL 2 CORROSION, LOWER GALLEY FLOOR SUPPORT CORRODED AT STATION 901 FROM BL 0 TO BL 42 LEFT AND RIGHT. REMOVED AND REPLACED GALLEY FLOOR SUPPORT PER SRM 51-10-00. (M) 2 L 7 3 4F A23WE 1996080200231 19960802 00231 WP 1996 8 2 96ZZZM1151 1 19960611 A 5320 SUPPORT LKHEED 1011 10113851 5265010 WP CABIN CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 319EA 193A1040 FOUND LEVEL 2 CORROSION, AFT CABIN FLOOR PANEL NR 271-TB, PANEL SUPPORT IS CORRODED BELOW L-4 FLIGHT ATTENDANT SEAT. RE MOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR. 2 L 7 3 4F A23WE 1996080200232 19960802 00232 WP 1996 8 2 96ZZZM1152 1 19960611 A 5315 FLOOR BEAM LKHEED 1011 10113851 5265010 WP BS 695 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 319EA 193A1040 FOUND LEVEL 2 CORROSION, FORWARD CARGO COMPARTMENT, LEFT FLOOR BEAM HAS CORROSION, AND CRACKED AT STATION 695. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-21-00. 2 L 7 3 4F A23WE 1996080200233 19960802 00233 WP 1996 8 2 96ZZZM1153 1 19960611 A 5320 BRACKET LKHEED 1011 10113851 5265010 WP CABIN CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 319EA 193A1040 FOUND LEVEL 2 CORROSION, RIGHT PASSENGER COMPARTMENT FLOOR PANEL NR 272GB SUPPORT BRACKET CORRODED. REMOVED AND REPLACE D SUPPORT BRACKET PER SRM 51-10-01. 2 L 7 3 4F A23WE 1996080200234 19960802 00234 WP 1996 8 2 96ZZZM1154 1 19960611 A 5320 SUPPORT LKHEED 1011 10113851 5265010 WP BS 281-313 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 319EA 193A1040 FOUND LEVEL 2 CORROSION, FLOOR SUPPORT UPPER CAP BETWEEN FS 281 AND FS 313 LBL 31 HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 51-10-01. 2 L 7 3 4F A23WE 1996080200235 19960802 00235 WP 1996 8 2 96ZZZM1155 1 19960611 A 5320 SUPPORT LKHEED 1011 10113851 5265010 WP CABIN CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 319EA 193A1040 FOUND LEVEL 2 CORROSION, RIGHT AFT PASSENGER COMPARTMENT FLOOR PANEL NR 272KB, SUPPORT BRACKET CORRODED. REMOVED DAMAGE D AREA, FABRICATED AND INSTALLED REPAIR PER SRM 51-10-01. 2 L 7 3 4F A23WE 1996080200236 19960802 00236 WP 1996 8 2 96ZZZM1156 1 19960611 A 5320 ANGLE LKHEED 1011 10113851 5265010 WP BS 806 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 319EA 193A1040 FOUND LEVEL 2 CORROSION, LOWER GALLEY FLOOR SUPPORT T-ANGLE HAS CORROSION FROM BL 0 TO BL 42 LEFT AND RIGHT AT STATION 8 06. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 51-10-01. 2 L 7 3 4F A23WE 1996080200237 19960802 00237 WP 1996 8 2 96ZZZM1157 1 19960611 A 5347 SEAT TRACK LKHEED 1011 10113851 5265010 WP BS 1746 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 319EA 193A1040 FOUND LEVEL 2 CORROSION, AFT PASSENGER COMPARTMENT SEAT TRACK AT LEFT BL 73 STATION 1746 HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-21-00. 2 L 7 3 4F A23WE 1996080200238 19960802 00238 WP 1996 8 2 96ZZZM1158 1 19960611 A 5320 SUPPORT LKHEED 1011 10113851 5265010 WP BS 901 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 319EA 193A1040 FOUND LEVEL 2 CORROSION, LOWER GALLEY FLOOR SUPPORT CORRODED AT STATION 901 FROM BL 0 TO BL 42 LEFT AND RIGHT. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 51-10-0. 2 L 7 3 4F A23WE 1996080200239 19960802 00239 WP 1996 8 2 96ZZZM1159 1 19960611 A 5315 FLOOR BEAM LKHEED 1011 10113851 5265010 WP BS 1778 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 319EA 193A1040 FOUND LEVEL 2 CORROSION, FLOOR BEAM STATION 1778 FROM BL 82 LEFT AND RIGHT CORRODED. REMOVED DAMAGED AREA, FABRICATED A ND INSTALLED REPAIR PER SRM 53-21-00. (M) 2 L 7 3 4F A23WE 1996080200240 19960802 00240 WP 1996 8 2 96ZZZM1160 1 19960611 A 5320 BRACKET LKHEED 1011 10113851 5265010 WP CABIN CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 319EA 193A1040 FOUND LEVEL 2 CORROSION, R4 FLIGHT ATTENDANT SEAT SUPPORT BRACKET IS CORRODED BELOW FLOOR LEVEL. REMOVED DAMAGED AREA F ABRICATED AND INSTALLED REPAIR PER SRM 51-10-01. 2 L 7 3 4F A23WE 1996080200241 19960802 00241 WP 1996 8 2 96ZZZM1161 1 19960611 A 5315 FLOOR BEAM LKHEED 1011 10113851 5265010 WP BS 329 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 319EA 193A1040 FOUND LEVEL 2 CORROSION, MAIN CABIN FLOOR BEAM UPPER CAP IS CORRODED AT FS 329 TO LBL 64. REMOVED DAMAGED AREA, FABRICA TED AND INSTALLED REPAIR PER SRM 51-10-05. 2 L 7 3 4F A23WE 1996080200242 19960802 00242 WP 1996 8 2 96ZZZM1162 1 19960611 A 5321 DECK LKHEED 1011 10113851 5265010 WP BS 329-349 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 319EA 193A1040 FOUND LEVEL 2 CORROSINO, MAIN CABIN PRESSURE DECK FLOOR CORRODED BETWEEN FS 329L TO FS 349L LBL 110. REMOVED DAMAGED AR EA, FABRICATED AND INSTALLED REPAIR PER SRM 53-11-00. 2 L 7 3 4F A23WE 1996080200243 19960802 00243 WP 1996 8 2 96ZZZM1163 1 19960611 A 5321 DECK LKHEED 1011 10113851 5265010 WP BS 349-369 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 319EA 193A1040 FOUND LEVEL 2 CORROSION, MAIN CABIN PRESSURE DECK FLOOR IS CORRODED BETWEEN FS 349L AND 369L LBL 100. REMOVED DAMAGED A REA FABRICATED AND INSTALLED REPAIR PER SRM 53-11-00. 2 L 7 3 4F A23WE 1996080200244 19960802 00244 WP 1996 8 2 96ZZZM1164 1 19960611 A 5321 DECK LKHEED 1011 10113851 5265010 WP BS 328-349 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 319EA 193A1040 FOUND LEVEL 2 CORROSION, MAIN CABIN PRESSURE DECK FLOOR IS CORRODED FS 328 AND FS 349 TO RBL 51. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-11-00. 2 L 7 3 4F A23WE 1996080200245 19960802 00245 EU 1996 8 2 96ZZZM1165 1 19960622 A 3213 5006227 BEARING SAAB SF340 340B 7860101 EU RT NLG WHEEL FAILURE A NVEA O OTHER D INFLIGHT SEPARATION TO TAKEOFF 1 SO 03 269AE 340B269 ON TAKEOFF THE TOWER CONTACTED THE CREW STATING THAT THEY OBSERVED A TIRE FALLING FROM THE A/C. THE CAUSE HAS BEEN DETE RMINED TO BE A RT NOSE WHEEL BEARING FAILURE. REMOVED AND REPLACED NLG LOWER TQ LINK, AXLE, AND BOTH TIRE ASSYS. 2 L 7 2 4T RT A52EU 1996080200246 19960802 00246 EU 1996 8 2 96ZZZM1166 1 19960612 A 2611 06232855001 SMOKE DET LENS FENWAL 72111211000 SAAB SF340 340B 7860101 EU CARGO COMPT DIRTY A NVEA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SO 03 253AE A2607 340B253 FLT NR 4938 - JFK - SMOKE WARNING INBOUND TO JFK. THE CREW DISCHARGED 1 EXTINGUISHER BOTTLE. INSPECTION OF THE AFT CAR GO COMPARTMENT PROVED IT WAS A FALSE WARNING. CLEANED DETECTOR LENS. ALSO, REMOVED AND REPLACED THE EXTINGUISHER BOTTL E. 2 L 7 2 4T RT A52EU 1996080200247 19960802 00247 EU 1996 8 2 96ZZZM1167 1 19960531 A 7120 09952701 MOUNT BRACKET 9394816 SAAB SF340 340B 7860101 EU RT ENG FRACTURED A NVEA K NONE O OTHER IN INSP/MAINT 1 SO 03 280AE 372 340B280 ALB - DURING SCHEDULED REMOVAL FOR HIGHTIME, RIGHT ENGINE BOTTOM PGB MOUNT WAS FOUND TO BE FAILED. FAILURE OCCURRED DUE TO A FRACTURE OF BONDED CANNISTER SUPPORT FITTING AT ATTACHMENT POINT TO ENGINE MOUNT BRACKET. REF CMM 71-20-20 PG 101 2, ITEM 50. 2 L 7 2 4T RT A52EU 1996080200248 19960802 00248 EU 1996 8 2 96ZZZM1168 1 19960511 A 3230 HP848430621 CONTROL VLV SAAB SF340 340B 7860101 EU NLG WW MALFUNCTIONED A NVEA O OTHER P NO WARNING INDICATION LD LANDING 1 SO 03 280AE 340B280 FLT 4966 - JFK - GEAR UNSAFE WARNING WHEN GEAR SELECTED DOWN FOR LANDING. ALL THREE GREEN LIGHT EXTINGUISHED. CFR EQP WAS CALLED OUT. CYCLED GEAR HANDLE SEVERAL TIMES, AND FINALLY DID ACHIEVE SAFE INDICATIONS. SAFE LANDING IN JFK. INSP ECTED GEAR AND FOUND NO DEFECTS. PERFORMED GEAR SWING AND SYSTEM OPERATED NORMALLY. REPLACED LANDING GEAR CONTROL VALV E AS PRECAUTIONARY MEASURE. 2 L 7 2 4T RT A52EU 1996080200249 19960802 00249 EU 1996 8 2 96ZZZM1169 1 19960422 A 3246 5010488 WHEEL SAAB SF340 340B 7860101 EU NR 3 CRACKED A NVEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 03 201AE 340B201 LSE - NR 3 MAIN WHEEL ASSY HALF FAILED, AN 8 INCH PORTION OF THE BEAD RIM CRACKED OUT. REMOVED AND REPLACED NR 3 WHEEL AND TIRE ASSY. 2 L 7 2 4T RT A52EU 1996080200250 19960802 00250 EU 1996 8 2 96ZZZM1170 1 19960428 A 2460 CIRCUIT BREAKER SAAB SF340 340B 7860101 EU LEFT TRIPPED A NVEA O OTHER H ELECT. POWER LOSS-50 PC DE DESCENT 1 SO 03 259AE 340B259 FLT 4925 - JFK - CAPTAINS SIDE COCKPIT INSTRUMENT/ELECTRICAL POWER FAILED IN FLIGHT. CAPTAIN DECLARED EMERGENCY AND LAN DED SAFELY WITHOUT FURTHER INCIDENT. RESETTING THE LEFT START RELAY CIRCUIT BREAKER. 2 L 7 2 4T RT A52EU 1996080200251 19960802 00251 SW 1996 8 2 96ZZZM1171 1 19960627 A 6120 31039081 OIL PRESS TUBE WOODWARD 89741016 FRCHLD SA227 SA227DC 3377521 SW RT PROP GOV CRACKED A EQGA E ENGINE SHUTDOWN J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SW 19 847LS 6059 2334483 DC847B WHILE EN ROUTE FROM HOT TO DFW, THE CAPTAIN NOTICED THAT THE OIL PRESSURE ON THE RIGHT ENGINE WAS DROPPING RAPIDLY. THE FLIGHT CREW THEN SHUTDOWN AND SECURED THAT ENGINE. THE AIRCRAFT THEN LANDED AT DFW WITHOUT FURTHER INCIDENT. ON INSPE CTION, IT WAS FOUND THAT AN OIL PRESSURE LINE ON THE PROP GOVERNOR HAD CRACKED ALLOWING THE ENGINE OIL SUPPLY TO LEAK OU T. THE LINE WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A18SW 1996080200253 19960802 00253 SW 1996 8 2 96ZZZM1173 1 19960617 A 3297 608AA22 WIRE SWRNGN SA226 SA226TC 8780404 SW LT MLG BROKEN A BDHA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 329BA TC238 RAP - FLT 434 - AFTER DEPARTURE THE LEFT MAIN GEAR INTRANSIT LIGHT STAYED ON. THE GEAR WAS CYCLED AND THE LIGHT REMAINE D ON. THE AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. INSPECTION OF THE SYSTEM FOUND A BROKEN WIRE IN THE LEFT WHEE L WELL. THE WIRE WAS REPAIRED AND SEVERAL RETRACTS PERFORMED. THE AIRCRAFT WAS RELEASED. (M) 2 L 7 2 4T RT A8SW 1996080200254 19960802 00254 SW 1996 8 2 96ZZZM1174 1 19960617 A 2751 2782425031 CONTROL BOX SWRNGN SA226 SA226TC 8780404 SW TE FLAPS WET A BDHA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 329BA 002 TC238 MSP - FLT 434 - ON TAXI, THE FLAP INDICATOR WAS ERRATIC. THE CREW RETURNED AND THE SYSTEM WAS INSPECTED. THE INSPECTIO N FOUND WATER HAD LEAKED THROUGH THE WINDSHIELD WIPER SHAFT AND DRIPPED ON THE GEAR AND FLAP WARNING BOX. THE UNIT WAS REPLACED AND LEAK WAS SEALED. THE AIRCRAFT WAS RELEASED. (M) 2 L 7 2 4T RT A8SW 1996080200255 19960802 00255 NE 1996 8 2 96ZZZM1175 2 19960630 A 7200 ENGINE LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B NE NR 2 FAILED A TWAA E ENGINE SHUTDOWN E VIBRATION/BUFFET CL CLIMB 1 CE 05 31014 193B1036 LAX - FLT 150 - DURING CLIMB, SHUT DOWN NR 2 ENGINE, S/N 4813, DUE TO HIGH VIBRATION MONITORING. FOUND METAL PARTICLES IN TAILPIPE. REPLACED ENGINE. ENGINE OPERATION THEN CHECKED NORMAL. ENGINE TOTAL TIME 49,344, ENGINE CYCLES 16,215. 2 L 7 3 4F 4 F A23WE E12EU 1996080200256 19960802 00256 NE 1996 8 2 96ZZZM1176 2 19960519 A 7250 798157 SHROUD FLANGE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 1 ENGINE WORN A TWAA E ENGINE SHUTDOWN J WARNING INDICATION TO TAKEOFF 1 CE 05 956U 49701 SAN - FLT 308 - ON TAKEOFF, SHUT DOWN NR 1 ENGINE, S/N 1217, DUE TO LOSS OF EPR AND INCREASE IN EGT. FOUND METAL PARTIC LES IN TAILPIPE. REPLACED ENGINE, ENGINE OPERATION THEN CHECKED NORMAL. INVESTIGATION REVEALED SECOND STAGE LOW PRESSUR E TURBINE VANES WORE THROUGH SHROUD, P/N 798157 FLANGE, LIBERATING SHROUD INTO GAS PATH. ENGINE WAS REPAIRED AND RETURN ED TO SERVICE. ENGINE TOTAL TIME 22,736, ENGINE TOTAL CYCLES 11,408. 2 L 7 2 4F 4 F A6WE E9NE 1996080200257 19960802 00257 NE 1996 8 2 96ZZZM1177 2 19960701 A 7321 FUEL CONTROL BOEING 767 767231 1385131 NM PWA JT9 JT9D7R4D 52054 NE NR 1 ENG OUT OF ADJUST A TWAA O OTHER O OTHER CR CRUISE 1 CE 05 605TW 22568 SJU - DURING CRUISE NR 1 ENGINE, S/N 4623, EXPERIENCED A POWER SURGE. ADJUSTED BETA RATE 1/4 TURN CLOCKWISE. ENGINE TH EN CHECKED NORMAL. (M) 2 L 7 2 4F 4 F RT A1NM E3NE 1996080200258 19960802 00258 EA 1996 8 2 96ZZZM1179 1 19960621 A 3230 156017 LWR DRAG STRUT DHAV DHC7 DHC7102 2802708 EA LT MLG FAILED A HNAA K NONE J WARNING INDICATION AP APPROACH 1 EA 07 905HA 15509 152 070 FLT 3254 - DCA-ORF - ON APPROACH INTO DCA, THE LEFT MAIN GEAR WOULD NOT EXTEND UNTIL THE NOSE AND RIGHT MAIN WERE FULLY EXTENDED. THE AIRCRAFT LANDED IN DCA WITHOUT INCIDENT. REMOVED AND REPLACED THE LOCK ACTUATOR AND LOWER DRAG STRUT. R EFERENCE HNAA9690542. 2 H 7 4 4T A20EA 1996080200259 19960802 00259 SO 1996 8 2 ASOA96020 1 19960611 A 2913 PV302229 HYD PUMP EMB 120 EMB120RT SO RT ENGINE DEFECTIVE A A ASOA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CL CLIMB 1 SO 11 243AS 120072 AT APPROXIMATELY 16,000 FEET ON CLIMB-OUT GSO-ATL, SIMULTANEOUS 'LOW LEVEL' AND 'MAIN PUMP LOW PRESSURE' LIGHTS ILLUMINA TED ON HYDRAULIC PANEL AND 'HYD' LIGHT ON MAP. CREW DECLARED AN EMERGENCY AND LANDED SAFELY WITH ZERO FLAPS IN ATL. RE MOVED AND REPLACED RIGHT ENGINE HYDRAULIC PUMP AND PRESSURE LINE. OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAF T WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1996080200260 19960802 00260 SO 1996 8 2 ASOA96021 1 19960618 A 5330 SKIN EMB 120 EMB120RT SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 264AS 120165 UPON INSPECTION, FOUND CORROSION ON FRAMES 21 AND 23 AT STRINGERS 21 RIGHT TO 20 LEFT. REPAIR DETERMINED TO BE A MAJOR REPAIR IAW SP663. REPAIRS MADE IAW THE SRM AND EO 120-53-0043. ALL WAS COMPLETED SATISFACTORILY AND THE AIRCRAFT WAS R ELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1996080200261 19960802 00261 SO 1996 8 2 ASOA96022 1 19960618 A 5330 SKIN EMB 120 EMB120RT SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 261AS 120141 UPON INSPECTION, FOUND CORROSION ON FRAME 21 BETWEEN STRINGERS 21 RT TO 20 LT. REPAIR DETERMINDED TO BE A MAJOR REPAIR IAW SP663. REPAIRS WILL BE MADE IAW THE SRM AND EO 120-53-0044. (M) 2 L 7 2 4T RT A31SO 1996080200262 19960802 00262 SO 1996 8 2 ASOA96023 1 19960620 A 6120 SM600BA60N1 RCCB EMB 120 EMB120RT SO RT RELAY PANEL FAILED A ASOA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 218AS 120015 IN CRUISE FLIGHT OAJ-ATL, CREW ENCOUNTERED AN ELECTRICAL SMELL COMING FROM THE CIRCUIT RELAY CONSOLE ON THE FIRST OFFICE RS SIDE. CREW COMPLIED WITH THE POH PROVISIONS AND DIVERTED INTO FLO. ATL MECHANIC ISOLATED THE PROBLEM TO THE RIGHT P ROP HEAT RCCB AND DEACTIVATED SAME. THE AIRCRAFT WAS THEN FERRIED TO ATL. REMOVED AND REPLACED THE RIGHT PROP HEAT RCC B. THE AIRCRAFT OPERATIONAL CHECKS WERE GOOD AND IT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1996080200263 19960802 00263 NE 1996 8 2 ASOA96024 2 19960623 A 7313 MS9388009 NOZZLE O-RING EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE CUT A A ASOA A E F UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. A J FLAME/FIRE WARNING INDICATION CL CLIMB 1 SO 11 503AS 120275 115609 DURING CLIMB THROUGH 11,500 FEET, PNS-ATL, CREW GOT A FIRE BELL, LIGHT, AND T6 WARNING. THE CREW SHUT DOWN THE RIGHT EN GINE, FEATHERED THE PROP AND PULLED THE FIRE HANDLE. THE FIRE WARNING EXTINGUISHED AND THE CREW RETURNED TO PNS WHERE L ANDING WAS MADE SAFELY AND WITHOUT INCIDENT AND FIRE WAS CONFIRMED TO BE OUT. UPON INSPECTION FOUND ALL FUEL NOZZLE TRA NSFER TUBES TO BE INSTALLED PROPERLY. INSPECTED ALL TRANSFER TUBE O-RINGS, FOUND THE O-RING AT THE 12 O'CLOCK POSITION CUT. REPLACED ALL FUEL NOZZLE O-RINGS. LEAK AND OPERATIONAL CHECKS WERE GOOD. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1996080200264 19960802 00264 SO 1996 8 2 ASOA96025 1 19960628 A 5713 12016085002 STRINGER EMB 120 EMB120RT SO RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 229AS 120042 DURING INSPECTION, FOUND THE RIGHT WING NR 8 AND NR 10 STRINGERS INBOARD OF NACELLE CRACKED. DETERMINED TO BE A MAJOR I AW SP663 AND FAR 43 APPENDIX A. REPAIRS MADE IAW SRM 57-20-03, FIGURE 201 AND EO120-57-0014. (M) 2 L 7 2 4T RT A31SO 1996080200265 19960802 00265 SO 1996 8 2 ASOA96026 1 19960707 A 3000 38E966A DE-ICE PRESS REG EMB 120 EMB120RT SO LT WING DEFECTIVE A A ASOA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 SO 11 258AS 120131 FLT NR 7097 - WHEN DESCENDING INTO GRT, LEFT BLEED LEAK LIGHT ILLUMINATED. THE CREW FOLLOWED THE CHECKLIST, DECLARED AN EMERGENCY, SHUT DOWN THE LEFT ENGINE AND LANDED UNEVENTFULLY IN GTR. THE FOLLOWING MORNING, THE CREW RAN THE ENGINE AT 90 PERCENT TORQUE WITH THE BLEED OFF AND THE LIGHT REMAINED OFF. AN FBO MECHANIC MADE A LOG ENTRY FOR A FERRY FLIGHT T O ATL. REMOVED AND REPLACED THE PRESSURE REGULATOR FOR THE DE-ICE SYSTEM AT THE WATER SEPARATOR. LEAK AND OPERATIONAL CHECKS WERE GOOD, AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M) 2 L 7 2 4T RT A31SO 1996080200266 19960802 00266 SO 1996 8 2 ASOA96027 1 19960707 A 5313 STRINGER EMB 120 EMB120RT SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 240AS 120060 DURING C-CHECK INSPECTION, FOUND CORROSION AT FRAME 20, STRINGER 20R. REMOVED RIVETS, SPLICED STRINGER, CLEANED CORROSI ON FROM FRAME 20, STRINGER 20R AND SEALED AND INSTALLED STRINGER IAW SRM 53-00-03 FIG 201 AND 51-22-00 FIG 5. (M) 2 L 7 2 4T RT A31SO 1996080200267 19960802 00267 SO 1996 8 2 ASOA96028 1 19960707 A 5313 STRINGER EMB 120 EMB120RT SO FUSELGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 240AS 120060 DURING C-CHECK INSPECTION, FOUND SKIN DISTORTED ON BELLY OF AIRCRAFT, RIGHT SIDE OF TRANSPONDER ANTENNA. REMOVED RIVETS , REMOVED STRINGER, CLEANED AREA, SEALED AND INSTALLED SPLICED STRINGER IAW SRM 53-00-03 FIG 201 AND 51-22-00 FIG 5. AL L AREAS WERE TREATED FOR CORROSION. (M) 2 L 7 2 4T RT A31SO 1996080200268 19960802 00268 SO 1996 8 2 ASOA96029 1 19960707 A 5313 STRINGER EMB 120 EMB120RT SO FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 240AS 120060 DURING C-CHECK INSPECTION, FOUND SKIN DISTORTED ON BELLY OF AIRCRAFT, RIGHT SIDE OF MARKER BEACON ANTENNA. REMOVED RIVE TS, INSPECTED AND FOUND CORROSION BETWEEN STRINGER AND BELLY SKIN. SPLICED IN NEW STRINGER, SEALED AND INSTALLED IAW SR M 53-00-03 FIG 201 AND 51-22-00 FIG 5. (M) 2 L 7 2 4T RT A31SO 1996080200269 19960802 00269 NM 1996 8 2 AWXA960262 1 19960525 A 5315 65C346885 FLOOR BEAM BOEING 737 737301 1384611 NM BS 520 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 23260 PAE - DURING ROUTINE SCHEDULED C-11 MAINTENANCE CHECK, FOUND CRACK AT STATION 520, RBL 45 FLOOR BEAM. STOP DRILLED CRAC K, FABRICATED REPAIR ANGLE, DRILLED REPAIR PARTS AND INSTALLED PER GO 53-14-12. (M) 2 L 7 2 4F RT A16WE 1996080200270 19960802 00270 EU 1996 8 2 AWXA960278 1 19960525 A 5310 STRUCTURE AIRBUS 320 A320231 3930325 EU BS 1292 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 620AW 052 PAE - DURING ROUTINE SCHEDULED C-5 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR STRUCTURE FR 68, ST 3257, X-240 Y-1292 RI GHT AROUND NUT PLATE HOLE. REMOVED CORROSION, FABRICATED REPAIR PARTS, INSTALLED WET PER SRM 53-00-14. (M) 2 L 7 2 4F RT A28NM 1996080200271 19960802 00271 EU 1996 8 2 AWXA960279 1 19960525 A 5310 STRUCTURE AIRBUS 320 A320231 3930325 EU BS 3250-3257 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 620AW 052 PAE - DURING ROUTINE C-5 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR STRUCTURE FR 68, STATION 3250-3257, X-240, Y-7292 L EFT AROUND NUT PLATE HOLES. REMOVED CORROSION, FABRICATED REPAIR PARTS, INSTALLED WET PER SRM 53-00-14. (M) 2 L 7 2 4F RT A28NM 1996080200272 19960802 00272 EU 1996 8 2 AWXA960280 1 19960528 A 5320 SUPPORT AIRBUS 320 A320231 3930325 EU BS 718-412 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 620AW 052 PAE - DURING ROUTINE SCHEDULED C-5 MAINTENANCE CHECK, FOUND CORROSION IN NUMEROUS PLACES ON FLOOR BOARD SUPPORT BEAM AT Z-540, BS 718-412. REPAIRED IAW SRM 51-43-12, 53-11-14. (M) 2 L 7 2 4F RT A28NM 1996080200273 19960802 00273 EU 1996 8 2 AWXA960282 1 19960530 A 5315 D53472098000 FLOOR BEAM AIRBUS 320 A320231 3930325 EU BS 765 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 620AW 052 PAE - DURING ROUTINE SCHEDULED C-5 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM FR 66 STH 3165-3167, X-240, Y765 LEF T. REPAIRED IAW SRM 51-32-11, 51-24-00, 51-23-11. (M) 2 L 7 2 4F RT A28NM 1996080200274 19960802 00274 EU 1996 8 2 C2XA96BT004 1 19960702 A 3230 842503 PSEU AEROSP ATR42 ATR42320 8680930 EU LANDIGN GEAR DEFECTIVE A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 09 34817 152 FLT 3286 - SDF - CREW NEEDED TO USE THE GEAR RETRACT OVERRIDE TO RAISE LANDING GEAR. AIRCRAFT ARRIVED CLE UNEVENTUALLY. AIRCRAFT WAS RELEASED IAW MEL NR 32-31-1 CATEGORY 'C' PLACARD 894310. AIRCRAFT CAME TO BTV FOR REPAIRS FOUND DEFECTIV E PSEU OPERATIONALLY CHECKED LANDING GEAR GOOD AND RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996080200275 19960802 00275 EU 1996 8 2 C2XA96BT005 1 19960706 A 3230 E0053R14B19SNE CONNECTOR AEROSP ATR42 ATR42320 8680930 EU NLG WHEELWELL SHORTED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 34817 152 EWR - FLT 3502 - AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO EWR UNEVENTFULLY. AIRCRAFT RELEASE D IAW MEL 32-31-3 PLACARD 894297. AIRCRAFT REPAIRED IN EWR, FOUND A SHORTED CONNECTOR (5004VC) IN NOSE WHEEL WELL WHICH CAUSED THE PSEU TO FAULT. CONNECTOR AND PSEU REPLACED AND CHECKED AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996080200276 19960802 00276 EU 1996 8 2 C2XA96IA153 1 19960624 A 5347 53678001236 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FR 33-36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14833 188 IAH - DURING C-CHECK INSPECTION, THE RIGHT INBOARD SEAT TRACK WAS FOUND TO BE CORRODED FROM FRAME 33 TO FRAME 36. MAINT ENANCE REMOVED THE DAMAGED SECTION OF SEAT TRACK AND REPLACED IT WITH A SERVICEABLE SECTION, REFERENCE ATR SRM 53-00-00 AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996080200277 19960802 00277 EU 1996 8 2 C2XA96IA154 1 19960624 A 5315 S53172158204 FLOOR BEAM AEROSP ATR42 ATR42320 8680930 EU FRAME 7 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14833 188 IAH - DURING C-CHECK INSPECTION, THE FLOOR SUPPORT BEAM AT FRAME 7 UNDER PANEL 211FF WAS FOUND TO BE CORRODED. MAINTENA NCE REMOVED THE DAMAGED SECTION AND INSTALLED A REPAIR DOUBLER PER EC 5310-01070 AND THE AIRCRAFT WAS RETURNED TO SERVIC E. (M) 2 H 7 2 4T RT A53EU 1996080200278 19960802 00278 EU 1996 8 2 C2XA96IA155 1 19960624 A 2133 2095F010800 OUTFLOW VALVE AEROSP ATR42 ATR42320 8680930 EU CABIN MALFUNCTIONED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14833 13011 186 188 IAH - DURING C-CHECK INSPECTION, THE OUTFLOW VALVES WERE FOUND TO BE REMAINING OPEN DURING THE FUNCTIONAL CHECK OF THE A IRCRAFT DITCHING SYSTEM PER ATR JIC 21-30-00 FUT 10010-001. MAINTENANCE REMOVED AND REPLACED THE ELECTROPNEUMATIC OUTFL OW VALVE PER ATR JIC 21-31-22 AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996080200279 19960802 00279 EU 1996 8 2 C2XA96IA156 1 19960624 A 5311 S53671311200 FRAME AEROSP ATR42 ATR42320 8680930 EU FS 37 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14833 188 IAH - DURING C-CHECK INSPECTION, FRAME 37 WAS FOUND TO BE CORRODED ON THE RIGHT SIDE BETWEEN STRINGERS 13 AND 14 JUST AB OVE THE CREASE BEAM. MAINTENANCE REPAIRED THE DAMAGED PER EC5310-01013 AND ATR REPAIR DRAWING 16S536R0054 AND THE AIRCR AFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996080200280 19960802 00280 EU 1996 8 2 C2XA96IA157 1 19960624 A 5530 S5397903200000 ROD ASSY AEROSP ATR42 ATR42320 8680930 EU VERT STAB CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14833 188 IAH - DURING C-CHECK INSPECTION, THE VERTICAL STABILIZER LINK ROD ASSEMBLY WAS FOUND TO BE CORRODED. MAINTENANCE REMOVE D AND REPLACED THE ROD ASSEMBLY PER ATR JIC 55-30-00 RAI 10000-002 AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996080200281 19960802 00281 SO 1996 8 2 C2XA96IA158 1 19960704 A 3234 12038594001 CONTROL HANDLE EMB 120 EMB120RT SO COCKPIT FAILED A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 09 57734 120199 IAH - FLT 3993 - PILOT REPORTED THAT AFTER TAKEOFF, THE GEAR 'A' SYSTEM RED POSITION INDICATION LIGHT REMAINED ON AFTER GEAR RETRACTION. THE AIRCRAFT LANDED AT IAH WITHOUT FURTHER INCIDENT, WHERE MAINTENANCE REMOVED AND REPLACED THE LANDIN G GEAR CONTROL HANDLE. THE AIRCRAFT OPERATIONALLY CHECKED GOOD AND WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996080200282 19960802 00282 NM 1996 8 2 EISA96091 1 19960702 A 5311 FRAME BOEING 727 727223 1384074 NM BS 740 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 311NE 19703 740 FORGING, STATION 26R IS CORRODED AT END FITTING IN AIR COND DISTRIBUTION BAY. CUT OUT DAMAGED AREA. FABRICATED REP AIR PARTS AND INSTALLED PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1996080200283 19960802 00283 NM 1996 8 2 EISA96092 1 19960702 A 5311 CIRCUMFERENTIAL BOEING 727 727223 1384074 NM BS 500 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 311NE 19703 CIRCUMFERENTIAL AT STATION 500, STRINGER 21L HAS CRACK. INSTALLED REPAIR DOUBLER PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1996080200284 19960802 00284 NM 1996 8 2 EISA96093 1 19960702 A 5320 CLIP BOEING 727 727223 1384074 NM BS 500 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 311NE 19703 STRINGER TIE CLIP AT STATION 500, STRINGER 24L IS CRACKED. RPLACED DAMAGED TIE CLIP PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1996080200285 19960802 00285 NM 1996 8 2 EISA96094 1 19960702 A 5220 SKIN BOEING 727 727223 1384074 NM EMER EXIT DOOR CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 311NE 19703 LEFT AFT OVERWING EXIT HAS CRACK ON OUTER SKIN AT LOWER SECTION. INSTALLED DOUBLER PER SRM 52-20-2. (M) 2 L 7 3 4F A3WE 1996080200286 19960802 00286 NM 1996 8 2 EISA96095 1 19960702 A 5730 SKIN BOEING 727 727223 1384074 NM RT WING CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 311NE 19703 RT WING TRAILING EDGE WELL, APPEARANCE OF CRACK AT NR 13 AND NR 14 SPOILER STOP FITTING. INSTALLED NEW FITTING PER SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1996080200287 19960802 00287 NM 1996 8 2 EISA96096 1 19960702 A 5730 SKIN BOEING 727 727223 1384074 NM RT WING DISBONDED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 311NE 19703 RIGHT WING UPPER SURFACE DAMAGED AREAS AT NR 9 SPOILER TRAILING EDGE. CUT OUT DAMAGED AREA, ACCOMPLISHED HOT BOND REPAI R PER SRM 51-40-06. (M) 2 L 7 3 4F A3WE 1996080200288 19960802 00288 NM 1996 8 2 EISA96097 1 19960702 A 5320 CLIP BOEING 727 727223 1384074 NM BS 620 GOUGED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 311NE 19703 FOUND FS 620, STRINGER 24L HAS GOUGED TIE CLIP ON AFT SIDE OF CIRCUMFERENTIAL. REPLACED TIE CLIP PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1996080200289 19960802 00289 1996 8 2 F3LA96018 4 19960714 A 2565 11611142 SLIDE BOEING 737 7372L9 1384497 NM L1 DOOR LOW PRESSURE A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 170PL 22733 MSP - DURING SERVICE CHECK, MAINTENANCE REPORTED L-1 DOOR ESCAPE SLIDE BOTTLE PRESSURE LOW. REPLACED L-1 DOOR ESCAPE SL IDE. (M) 2 L 7 2 4F RT A16WE 1996080200290 19960802 00290 EA 1996 8 2 HNAA9690538 1 19960610 A 2611 824OPY SMOKE DETECTOR DHAV DHC7 DHC7102 2802708 EA LAVATORY FAILED A HNAA K NONE N FALSE WARNING CR CRUISE 1 EA 07 905HA 32999 070 FLT 3170 - HPN-DCA - THE LAVATORY SMOKE DETECTOR SOUNDED IN FLIGHT. THE DETECTOR WAS MEL'D PER MEL 26-15 AND THE AIRCRA FT CONTINUED OPERATION WITHOUT INCIDENT. AT RON, THE SMOKE DETECTOR WAS REMOVED AND REPLACED. (M) 2 H 7 4 4T A20EA 1996080200291 19960802 00291 EA 1996 8 2 HNAA9690542 1 19960621 A 3230 155507 LOCK ACTUATOR DHAV DHC7 DHC7102 2802708 EA LT MLG FAILED A HNAA K NONE J WARNING INDICATION AP APPROACH 1 EA 07 905HA 37905 MMC026 070 FLT 3254 - DCA-ORF - ON APPROACH INTO DCA, THE LEFT MAIN GEAR WOULD NOT EXTEND UNTIL THE NOSE AND RIGHT MAIN WERE FULLY EXTENDED. THE AIRCRAFT LANDED IN DCA WITHOUT INCIDENT. REMOVED AND REPLACED THE LOCK ACTUATOR AND LOWER DRAG STRUT. ( M) 2 H 7 4 4T A20EA 1996080200292 19960802 00292 NM 1996 8 2 HNAA9692440 1 19960612 A 3230 574205 SELECTOR VLV DHAV DHC8 DHC8102 2809003 NM LANDING GEAR FAILED A HNAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 07 924HA 21809 351 105 FLT NR 3260 - HPN-BWI - ON APPROACH INTO BWI, THE LANDING GEAR WOULD NOT EXTEND WHEN SELECTED DOWN. LOWERED GEAR USING ALTERNATE SYSTEM AND LANDED IN BWI WITHOUT INCIDENT. REMOVED AND REPLACED THE LANDING GEAR SELECTOR VALVE. (M) 2 H 7 2 4T RT A13NM 1996080200293 19960802 00293 NM 1996 8 2 HNAA9693634 1 19960529 A 2611 CONNECTOR DHAV DHC8 DHC8102 2809003 NM SMOKE DET WET A HNAA O OTHER N FALSE WARNING CR CRUISE 1 EA 07 936HA 145 FLT 3282 - EWN-CLT - EN ROUTE TO CLT, THE SMOKE WARNING LIGHT CAME ON AND WOULD NOT RESET. AIRCRAFT CONTINUED ON TO CLT AND LANDED WITHOUT INCIDENT. DRIED WATER, AND RESET THE CANNON PLUG ON THE NR 2 SMOKE DETECTOR. (M) 2 H 7 2 4T RT A13NM 1996080200294 19960802 00294 NE 1996 8 2 IXXA96101 2 19960727 A 7261 540618 OIL PUMP DOUG DC8 DC863 302198A WP PWA JT3D JT3D7 52039 NE ENGINE GEARBOX FAILED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 788AL 45999 671251 SUBSEQUENT INVESTIGATION FOUND THE METAL CONTAMINATION OF THE OIL FILTER TO BE ALUMINUM GENERATED FROM THE GEARBOX OIL P UMP. PRECAUTIONARY INSPECTION OF THE NR 5 AND NR 6 BEARINGS REVEALED NO PROBLEMS. OIL SYSTEM WAS FLUSHED AND THE OIL P UMP REPLACED. THE ENGINE SUCCESSFULLY PASSED RUN CHECKS AND WAS RETURNED TO SERVICE. (M) 2 L 7 4 4F 4 F 4A25 1E8 1996080200295 19960802 00295 WP 1996 8 2 IXXA96102 1 19960625 A 3260 7000010202 DOWNLOCK SW DOUG DC8 DC871 302199A WP LT MLG DIRTY A IXXA K NONE N FALSE WARNING DE DESCENT 1 SW 11 826BX 45998 UPON GEAR EXTENTION INTO TOL, LEFT GEAR INDICATION LIGHT ILLUMINATED IMMEDIATELY. ALL GEAR LIGHTS ILLUMINATED WITH GEAR UNSAFE LIGHT. GEAR WAS CYCLED, EXTENTION WAS NORMAL EXCEPT LEFT GEAR LIGHT CAME ON IMMEDIATELY. MAINTENANCE FOUND LEF T GEAR DOWNLOCK SWITCH DIRTY. THE SWITCH WAS CLEANED. INDICATION SYSTEM OPERATIONALLY CHECKED GOOD IAW MM 32-60-06. ( M) 2 L 7 4 4F 4A25 1996080200296 19960802 00296 WP 1996 8 2 IXXA96103 1 19960627 A 3260 7000010202 DOWNLOCK SW DOUG DC8 DC871 302199A WP LT MAIN GEAR INTERMITTENT A IXXA O OTHER N FALSE WARNING DE DESCENT 1 SW 11 826BX 45998 ON DESCENT INTO SAN, LANDING GEAR UNSAFE LIGHT ILLUMINATED ACCOMPANIED BY THE WARNING HORN WHEN FLAPS SELECTED TO 50 DEG REES. GEAR CYCLED SEVERAL TIMES UNTIL SAFE INDICATION WAS OBTAINED. LANDING WAS UNEVENTFUL. MAINTENANCE REPLACED THE LEFT DOWNLOCK SWITCH AND OPERATIONALLY CHECKED THE SYSTEM IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL AND THE AIR CRAFT RETURNED TO SERVICE. (M) 2 L 7 4 4F 4A25 1996080200297 19960802 00297 EU 1996 8 2 M3HA96017 1 19960630 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A M3HA K NONE L NO TEST IN INSP/MAINT 1 WP 13 4209G 2277 129 HNL - PREFLIGHT - FORWARD EMERGENCY LIGHTS, OVER EXITS, DO NOT ILLUMINATE. REMOVED AND INSTALLED SERVICEABLE EMERGENCY BATTERY PACK. (M) 2 H 7 2 4T RT A53EU 1996080200298 19960802 00298 EU 1996 8 2 M3HA96019 1 19960702 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A M3HA K NONE L NO TEST IN INSP/MAINT 1 WP 13 4208G 3455 086 HNL - FLT 709 - PREFLIGHT - FORWARD EMERGENCY LIGHTS OVERHEAD AND NR 1, 2, 5 FLOOR INOP. REMOVED AND INSTALLED SERVICEA BLE EMERGENCY BATTERY PACKS. (M) 2 H 7 2 4T RT A53EU 1996080200299 19960802 00299 NM 1996 8 2 MALA964975 1 19960429 A 2421 GENERATOR DHAV DHC8 DHC8102 2809003 NM LEFT MALFUNCTIONED A MALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 GL 15 819MA 251 FLT 3205 - ON CLIMB-OUT FROM MSP, THE RIGHT AC BUS, STALL WARNING, AND TRU CAUTION LIGHTS ILLUMINATED. THE CREW COMPLET ED QUICK REFERENCE PROCEDURES AND RETURNED TO MSP. MAINTENANCE REPLACED A CORRODED CONNECTOR. THE RIGHT AC GENERATOR, GENERATOR RELAY, AND LEFT AC GENERATOR WERE REPLACED AS A PRECAUTIONARY MEASURE. SYSTEM OPERATED SATISFACTORILY. (M) 2 H 7 2 4T RT A13NM 1996080200300 19960802 00300 SW 1996 8 2 MALA964989 1 19960426 A 3260 1EN516 UPLIMIT SWITCH SWRNGN SA227 SA227AC 8780603 SW NLG OUT OF ADJUST A MALA O OTHER N FALSE WARNING CL CLIMB 1 GL 15 426MA AC645 FLT 3087 - ON CLIMB-OUT FROM YQT, THE CREW NOTED THAT THE NOSE GEAR CYCLED IN THE WHEEL WELL FIVE TIMES BEFORE COMING UP AND LOCKED. THE AIRCRAFT CONTNUED TO MSP WITHOUT FURTHER INCIDENT. MAINTENANCE RE-RIGGED THE UPLIMIT AND UP POSITION SWITCHES. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2 L 7 2 4T RT A8SW 1996080200301 19960802 00301 NM 1996 8 2 MALA965062 1 19960706 A 3350 6104781 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 853MA 353 DLT 3125 - DURING THE PREFLIGHT INSPECTION, TWO EMERGENCY LIGHTS ON THE FORWARD CABIN FLOOR ARE INOPERATIVE. MAINTENANC E REPLACED A BATTERY PACK. ALL CHECKS SATISFACTORY. (M0 2 H 7 2 4T RT A13NM 1996080200302 19960802 00302 SW 1996 8 2 MALA965063 1 19960706 A 5230 MECHANISM SWRNGN SA227 SA227AC 8780603 SW CARGO DOOR OUT OF ADJUST A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 434MA AC717 FLT 3049 - EN ROUTE FROM LNK, THE CARGO DOOR WARNING LIGHT ILLUMINATED IN FLIGHT. THE AIRCRAFT RETURNED TO LNK. MAINTE NANCE ADJUSTED THE CARGO DOOR ROD ENDS ON THE FORWARD BOTTOM BELLCRANK AND THE DOOR HANDLE POSITION SWITCH. ALL CHECKS SATISFACTORY. (M) 2 L 7 2 4T RT A8SW 1996080200303 19960802 00303 NM 1996 8 2 MALA965064 1 19960706 A 3350 10005511 LAMP DHAV DHC8 DHC8102 2809003 NM COCKPIT MISSING A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 864MA 363 FLT 3052 - DURING THE PREFLIGHT INSPECTION IN DTW, THE COCKPIT EMERGENCY EXIT LAMP ASSEMBLY WAS MISSING. MAINTENANCE IN STALLED A NEW LIGHT ASSEMBLY. ALL CHECKS SATISFACTORY. (M) 2 H 7 2 4T RT A13NM 1996080200304 19960802 00304 SW 1996 8 2 MALA965065 1 19960706 A 7933 OIL TEMP SENSOR SWRNGN SA227 SA227AC 8780603 SW RT ENGINE MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 428MA AC646 FLT 3048 - AFTER TAKEOFF FROM DTW, THE RIGHT OIL TEMPERATURE DROPPED TO 40 DEGREES CELSIUS. ALL OTHER ENGINE INDICATION S WERE NORMAL. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. AS A PRECAUTION, TH E RIGHT OIL TEMP BULB WAS REPLACED. ALL CHECKS SATISFACTORY. (M) 2 L 7 2 4T RT A8SW 1996080200305 19960802 00305 SW 1996 8 2 MALA965066 1 19960707 A 5320 2722085 DOOR FRAME SWRNGN SA227 SA227AC 8780603 SW BS 438.06 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 424MA AC639 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERFORMED REPAIR TO A CRACK IN THE CARGO DOOR FRAME, P/N 27-22085, AT FS 438.060 BY REMOVING DAMAGED GAS STRUT MOUNT HOLE (1.625 BY 1.825), FABRICATED, PREPPED AND INSTALLED A REPAIR ANGLE, REPAIR PLATE, AND FILLER IAW FAIRCHILD ARP 53-20-9503 DATED MARCH 1, 1995. (M) 2 L 7 2 4T RT A8SW 1996080200306 19960802 00306 SW 1996 8 2 MALA965067 1 19960707 A 5320 2722085 DOOR FRAME SWRNGN SA227 SA227AC 8780603 SW BS 491 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 424MA AC639 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERFORMED REPAIR TO A CRACK IN THE CARGO DOOR FRAME, P/N 27-22085, AT FS 491, BY REMOVING DAMAGED GAS STRUT MOUNT HOLE (1.625 BY 1.825). FABRICATED, PREPPED AND INSTALLED A REPAIR ANGLE, RE PAIR PLATE, AND FILLER IAW FAIRCHILD ARP 53-20-9503 DATED MARCH 1, 1995. (M) 2 L 7 2 4T RT A8SW 1996080200307 19960802 00307 WP 1996 8 2 ORJA9637 1 19960627 A 3350 5917161509 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 832RA 53044 OVERHEAD EMERGENCY LIGHTS INOP AT ROWS 2-4. FOUND BATTERIES BAD. REMOVED AND REPLACED BATTERIES. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1996080200308 19960802 00308 WP 1996 8 2 ORJA9638 1 19960630 A 3210 3937060501 ATTACH PIN BOLT DOUG DC9 DC983 3022083 WP LT MLG SHEARED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 836RA 53046 LEFT MLG LOWER TORQUE LINK ATTACH PIN BOLT SHEARED. REPLACED LT MLG LOWER TORQUE LINK ATTACH PIN BOLT IAW 32-17-01 DAC COMM. (M) 2 L 7 2 4F RT A6WE 1996080200309 19960802 00309 NM 1996 8 2 PCAA9600293 1 19960604 A 2611 30326E7 SMOKE DET AMP DHAV DHC8 DHC8102 2809003 NM BAGG COMPT MALFUNCTIONED A PCAA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 EA 13 817EX 13306 191 FLT 3534 - AFT BAG COMPARTMENT SMOKE WARNING ILLUMINATED IN TURBULANCE. EMERGENCY DECLARED, AIRCRAFT DIVERTED TO LNS. S MOKE WARNING INDICATION EXTINGUISHED ON LANDING. NO EVIDENCE OF SMOKE OR FIRE. REPLACED SMOKE DETECTOR AMPLIFIER AS A PRECAUTIONARY MEASURE. SYSTEM TEST AND OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1996080200310 19960802 00310 NE 1996 8 2 PCAA9600296 2 19960618 A 7250 TURBINE BLADE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 ENG SEPARATED A A PCAA O OTHER N FALSE WARNING NR NOT REPORTED 1 EA 13 831EX 12501 160 121353 FLT 3859 - EXPERIENCED A TORQUE FLUCTUATION OF THE NR 1 ENGINE AND INCREASE OF ITT TO APPROX 780 DEGREES. TORQUES DROPP ED TO 50 PECENT FOLLOWED BY A LOUD GRINDING NOISE AND ENGINE FIRE INDICATION. INSPECTION VERIFIED NO INDICATION OF FIRE . ENGINE REMOVED AND REPLACED IAW DHC-8 MM. GROUND RUN AND OPERATIONAL CHECKS NORMAL. PRELIMINARY INVESTIGATION INDIC ATES APPARENT LP TURBINE BLADE SEPARATION. INVESTIGATION CONTINUES, AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T 4 T RT A13NM E20NE 1996080200311 19960802 00311 EU 1996 8 2 PLGA9606121 1 19960612 A 2421 31342001 AC GENERATOR SAAB SF340 340B 7860101 EU RT NACELLE FAILED A PLGA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 NE 05 360BE 340B287 BGR - FLT 4964 - AFTER LANDING IN BGR, THE CREW NOTED THE RT AC GENERATOR FAIL LIGHT ILLUMINATED AND OBSERVED SPARKS COM ING FROM THE RT NACELLE. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT. REMOVED AND REPLACED THE AC GENERATOR, GENERATOR CONTROL UNIT, COWL EXHAUST SCREEN AND RETURNED THE AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1996080200312 19960802 00312 EU 1996 8 2 PLGA9606191 1 19960619 A 2913 4018502 HYD PUMP SAAB SF340 SF340A 7850100 EU FWD FUSELAGE FAILED A PLGA O OTHER J WARNING INDICATION AP APPROACH 1 NE 05 340BE DS45 340A062 BOS - FLT 4372 - DURING APPROACH TO BOS, EXPERIENCED FAILURE OF THE HYDRAULIC SYSTEM. THE HYDRAULIC PUMP AND MOTOR ASSE MBLY WERE REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. TEARDOWN OF THE ELECTRIC MOTOR FOUND THE ARMATURE BEARING HAD FAILED. BEARING P/N 102729N1 AND 400431N1 WERE BOTH REPORTED AS HAVING 'WORN GREASE'. THE UNIT WAS REPAIRED AND RETURNE D TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1996080200313 19960802 00313 EU 1996 8 2 PLGA9606194 1 19960619 A 2572 E/E BAY SAAB SF340 SF340A 7850100 EU FWD FUSELAGE DIRTY A PLGA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NE 05 743BA 340A093 LGA - FLT 4778 - AFTER TAKEOFF FROM LGA, THE CREW NOTED SMOKE IN THE COCKPIT. AN EMERGENCY WAS DECLARED AND THE AIRCRAF T RETURNED TO LGA LANDING WITHOUT INCIDENT. MAINTENANCE INSPECTED THE COMPLETE COCKPIT AREA AND PERFORMED ELECTRICAL CH ECKS OF ALL SYSTEMS WITH NO DEFECTS NOTED AND NO ODOR PRESENT. ALL ELECTRICAL CHECKS WERE NORMAL. AN INSPECTION OF THE EQUIPMENT BAY BELOW THE COCKPIT REVEALED A COFFEE SPILL. THE AREA WAS CLEANED AND THE AIRCRAFT RELEASED TO SERVICE. ( M) 2 L 7 2 4T RT A52EU 1996080200314 19960802 00314 EU 1996 8 2 PLGA9606252 1 19960625 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT MALFUNCTIONED A PLGA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING UK UNKNOWN 1 NE 05 362BE 340B291 JFK - FLT 4528 - TWENTY MINUTES OUT OF JFK EN ROUTE TO SYR, THE CREW RECEIVED A CARGO SMOKE WARNING LIGHT. EMERGENCY PR OCEDURES WERE FOLLOWED AND THE FIRE BOTTLE DISCHARGED. THE CREW DECLARED AN EMERGENCY AND DIVERTED BACK TO JFK. THE AI RCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE DETERMINDED THE WARNING TO BE FALSE. THE AIRCRAFT REPOSITIONED TO PSM FOR REPAIRS UNDER MEL 26-22-1. THE TWO CARGO SMOKE DETECTORS WERE CLEANED AND OPS CHECKED GOOD. THE FIRE EXTINQUISHER WAS REPLACED AND THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1996080200315 19960802 00315 WP 1996 8 2 RRXA96032 1 19960622 A 3260 DNLOCK SWITCH DOUG DC8 DC873F 302199F WP LT MLG CORRODED A RRXA K NONE N FALSE WARNING AP APPROACH 1 WP 15 791FT 46045 KMIA - FLT 890 - WHEN EXTENDING LANDING GEAR, LEFT MLG LIGHT STAYED OUT WITH DOORS AND GEAR NOT LATCHED LIGHTS ON WITH F LAPS AT 35 DEGREES WHEN RETARDING THROTTLES LANDING GEAR WARNING HORN SOUNDED. CYCLED GEAR SEVERAL TIMES BEFORE LEFT ML G LIGHT CAME ON AND NO LANDING GEAR HORN. TROUBLE SHOT, FOUND LEFT MLG DOWN LOCK SWITCH PINS CORRODED AND DIRTY CONTACT S, CLEANED CANNON PLUG, REMOVED AND REPLACED DOWNLOCK SWITCH. OPERATIONAL CHECK OK, ALL IAW MM 32-60-06. (M) 2 L 7 4 4F RT 4A25 1996080200318 19960802 00318 CE 1996 8 2 S2YA960012 1 19960625 A 2612 2440915 FIRE LOOP BEECH 1900 1900D 1154162 CE LT ENG MALFUNCTIONED A S2YA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 GL 13 145SK UE145 FLT 1050 - MKE - ON APPROACH, CREW NOTICED THE LT FIRE PULL 'T' HANDLE ILLUMINATED IN FLIGHT, THEY PROCEEDED TO SHUT DOW N THE ENGINE AND DISCHARGED THE FIRE EXTINGUISHER BOTTLE. AN EMERGENCY WAS DECLARED, THEY LANDED AND DISEMBARKED PAX OF F WING. MAINTENANCE REPLACED BOTH FWD AND AFT FIRE LOOPS FOR PRECAUTION (AFT LOOP P/N NR 244-12886) OPERATIONAL CHECKED GOOD ON GROUND. (M) 2 L 7 2 4T RT A24CE 1996080200319 19960802 00319 WP 1996 8 2 SABA9600017 2 19960624 A 7200 ENGINE BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110U 01514 WP LEFT FAILED A A SABA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 33 693JX 693 P63159C FLT 5104 - CLT-HTS - AIRCRAFT HAD JUST TAKEN OFF WHEN THE LEFT EGT STARTED RISING THROUGH 700 DEGREES. THE CAPTAIN REDU CED POWER ON THE LEFT ENGINE TO BRING THE EGT TO AN ACCEPTABLE LEVEL. THE CAPTAIN THEN RETURNED TO THE FIELD WHERE HE M ADE AN UNEVENTFUL LANDING. THE LEFT ENGINE WAS REMOVED AND REPLACED AND THE AIRCRAFT WAS TEST FLOWN AND THEN RETURNED T O SERVICE. THE ENGINE WAS THEN SENT TO GARRETT FOR INSPECTION AND REPAIR. (M) 2 L 7 2 4T 4 T RT A21EU E4WE 1996080200320 19960802 00320 EU 1996 8 2 SABA9600018 1 19960701 A 3260 INDICATION STBROS SD3 SD360 8100606 EU NLG MALFUNCTIONED A SABA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 SO 33 742CC SH3742 FLT 5194 - CLT-AGS - ON APPROACH INTO AGS, WHEN THE LANDING GEAR WAS SELECTED DOWN THE NOSE GEAR INTRANSIT LIGHT DID NOT EXTINGUISH AND THE GREEN LIGHT DID NOT ILLUMINATED. FOLLOWED CHECKLIST PROCEDURES AND DECLARED AN EMERGENCY, DID A FLY -BY OF THE TOWER FOR NLG POSITION. EMERGENCY EQUIP STANDING BY THE AIRCRAFT MADE AN UNEVENTFUL LANDING IN AGS. THE GEA R WAS PINNED AND THE RETRACTION SYSTEM DEFERRED PER MEL 32-3 UNDER CONTROL NR 0701-10C. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. THE MSL WAS CLEARED BY OPS CHECK OF LANDING GEAR SYSTEM NUMEROUS TIMES ON 7-2-96 CCAIR WO NR 34679. NO DEF ECTS NOTED. (M 2 H 7 2 4T A41EU 1996080200321 19960802 00321 EU 1996 8 2 SABA9600019 1 19960705 A 3260 200923203 DNLOCK SWITCH STBROS SD3 SD360 8100606 EU NLG MALFUNCTIONED A SABA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 SO 33 742CC SH3742 TRAINING FLT 9101 - CLT-HKY-CLT - ON APPROACH INTO CLT WHEN THE LANDING GEAR WAS SELECTED DOWN, THE NOSE GEAR INTRANSIT LIGHT (RED) DID NOT EXTINGUISH AND THE NOSE GEAR DOWN LIGHT (GREEN) DID NOT ILLUMINATE. FOLLOWED THE CHECKLIST PROCEDUR ES, DECLARED AN EMERGENCY, AND DID A FLYBY OF THE TOWER FOR NLG POSITION. AN UNEVENTFUL LANDING WAS INTO CLT. THE CAPT AIN THEN NOTIFIED MAINTENANCE CONTROL OF THE PROBLEM. THE LANDING GEAR WAS PINNED AND THE AIRCRAFT WAS TAKEN TO HEAVY M AINTENANCE. THE PROBLEM WAS A FAULTY NLG DOWNLOCK SWITCH. REMOVED AND REPLACED SWITCH. OPS CHECK GOOD. (M) 2 H 7 2 4T A41EU 1996080200322 19960802 00322 EU 1996 8 2 SIMA961781 1 19960626 A 3350 3011210 LIGHT AEROSP ATR72 ATR72212 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 451AT 451 ORD - FLT 4058 - EMERGENCY AIRSTAIR LIGHT INOP. REPLACED EMERGENCY LIGHT ASSEMBLY. OPS CHECK GOOD. AIRCRAFT WAS RETUR NED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996080200323 19960802 00323 EU 1996 8 2 SIMA961901 1 19960708 A 3350 3012001 BATTERY AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 4AE 1322 244 DFW - FLT 3828 - FOUND FORWARD EMERGENCY LIGHTS INOP. RAI'D BATTERY AT POWER SUPPLY LOCATION 43WL. OPS CHECK SATISFACT ORY. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996080200324 19960802 00324 EU 1996 8 2 SIMA961902 1 19960708 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 4AE 482 244 DFW - FLT 3821 - FORWARD CABIN EMERGENCY FLOOR LIGHTS WOULDN'T EXTINGUISH AFTER POWER LOSS. RAI'D FORWARD EMERGENCY POW ER SUPPLY. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996080200325 19960802 00325 SO 1996 8 2 SRAA69608 1 19960620 A 3230 JACKSCREW LKHEED 382 382G 526414U SO RT MLG FAILED A SRAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 921SJ 4586 AFTER TAKING OFF FROM ILL FOR ANC ON FLIGHT 956, FOUND RIGHT MAIN LANDING GEAR WOULD NOT RETRACT, CONTINUED FLIGHT WITH GEARS DOWN AND LANDED IN ANC WITHOUT INCIDENT. FOUND RIGHT MAIN LANDING GEAR JACKSCREW FAILED. REMOVED AND REPLACED JA CKSCREW AT RIGHT AFT POSITION. OPS CHECKED GOOD PER MM CH 32. (M) 2 H 7 4 4T A1SO 1996080200326 19960802 00326 NM 1996 8 2 TAOA069609 1 19960523 A 5343 65176768 TRUNNION BOEING 727 727254 138408L NM RT NLG W/W CRACKED A TAOA K NONE O OTHER IN INSP/MAINT 1 EA 15 914TS 20251 FLT 6530 - DCA-LGA - FOUND ON L/S CHECK, NOSE GEAR RIGHT TRUNNION FITTING CRACKED THREE INCHES AT FWD RADIUS. REPLACED RIGHT TRUNNION FITTING PER SRM 51-30-2. RII ACCOMPLISHED. (M) 2 L 7 3 4F A3WE 1996080200327 19960802 00327 1996 8 2 TAOA069611 4 19960621 A 3440 5224363006 RADIO ALT COLLINS 339H1B BOEING 727 727254 138408L NM LT COCKPIT FAILED A TAOA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 913TS 718 20250 SMOKE CAME FROM CAPTAINS RADIO ALTIMETER IN FLIGHT, PULLED BOTH RADIO ALTIMETERS CIRCUIT BREAKERS AND SMOKE STOPPED. RE PLACED CAPTAINS RADIO ALTIMETER INDICATOR, INSPECTED WIRING AND CANNON PLUG, CHECKS OK IAW MM CHAPTER 34-48-31. (M) 2 L 7 3 4F A3WE 1996080200328 19960802 00328 NM 1996 8 2 TAOA069612 1 19960621 A 3232 731414 ACTUATOR BOEING 727 727294 1384088 NM RT MLG WW DOOR FAILED A TAOA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 921TS 145D 22043 FLT 6161 - EN ROUTE BOS-LGA - FLT ATTENDANT IN THE AFT CABIN REPORTED A STRONG SMELL OF FUEL. FOUND RIGHT MAIN GEAR WHE EL WELL DOOR ACTUATOR CRACKED AND SPRAYING SKYDROL. REPLACED RIGHT WHEEL WELL DOOR ACTUATOR, LEAK AND OPERATIONAL CHECK OK IAW MM CH 32-32-81. (M) 0 4 A3WE 1996080200329 19960802 00329 NM 1996 8 2 TAOA069613 1 19960624 A 3397 WIRE BOEING 727 727254 138408L NM CABIN BROKEN A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 912TS 20438 EMERGENCY FLOOR PATH LIGHTING ROW 25 DEF LIGHT INOP. REPAIRED BROKEN WIRE ON LIGHT BASE. OPS CHECK OK. (M) 2 L 7 3 4F A3WE 1996080200330 19960802 00330 NM 1996 8 2 TAOA069614 1 19960701 A 3350 1102873 LIGHT GRIMES BOEING 727 727227 1384078 NM CABIN BROKEN A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 925TS 286 21244 OVERHEAD AISLE EMERGENCY LIGHT AT ROW 10 INOP. REPLACED LIGHT ASSEMBLY. (M) 2 L 7 3 4F A3WE 1996080200331 19960802 00331 NM 1996 8 2 TAOA069615 1 19960701 A 3350 90052 BATTERY PACK BOEING 727 727225 1384077 NM LT EMERG EXIT DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 918TS UA444022863 20445 LEFT OVERWING EMERGENCY EXIT SIGN INOP. REPLACED BATTERY CHARGER AND BATTERY PACK. (M) 2 L 7 3 4F A3WE 1996080200332 19960802 00332 NM 1996 8 2 TAOA069616 1 19960707 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 923TS 20125 20441 OVERWING AISLE EMERGENCY EXIT SIGNS INOP. REPLACED BATTERY PACK CHECKS OK AS PER MM CHAPTER 33-50. (M) 2 L 7 3 4F A3WE 1996080200333 19960802 00333 NM 1996 8 2 TSAA9653051 1 19960624 A 5313 STRINGER BOEING 737 7372Q9 138448M NM BS 827 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 804AL 21719 DURING HEAVY MAINTENANCE VISIT, FOUND EXFOLIATION CORROSION ON STRINGER 27R BS 827. REPAIRED STRINGER PER SRM 53-10-3 A ND REPAIRED SKIN PER SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1996080200334 19960802 00334 NM 1996 8 2 TSAA9653054 1 19960624 A 5330 SKIN BOEING 737 7372Q9 138448M NM BS 344 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 804AL 21719 DURING HEAVY MAINTENANCE VISIT, FOUND .625 INCH CRACK AT BS 344 LOWER AFT CORNER OF FORWARD AIRSTAIR DOOR CUT OUT. REPA IRED PER ECO 1143. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1996080200335 19960802 00335 NM 1996 8 2 TSAA9653057 1 19960624 A 5330 SKIN BOEING 737 7372Q9 138448M NM BS 727 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 804AL 21719 DURING HEAVY MAINTENANCE VISIT, LOWER FUSELAGE SKIN BULGE BS 727 PLUS 12 INCHES THROUGH BS 727A AT STRINGER 28R. REPAIR ED PER ECO 2726 WITH DEVIATION A, B, C, D, AND E. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1996080200336 19960802 00336 NM 1996 8 2 TSAA9653058 1 19960624 A 5330 SKIN BOEING 737 7372Q9 138448M NM BS 967 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 804AL 21719 DURING HEAVY MAINTENANCE VISIT, FOUND SKIN BULGE AROUND RELIEF VALVE CUT OUT AT BS 967 STRINGER 26R-27R. REPAIRED PER E CO 2203R1. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1996080200337 19960802 00337 NM 1996 8 2 TSAA9653059 1 19960624 A 5330 SKIN BOEING 737 7372Q9 138448M NM BS 400 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 804AL 21719 DURING HEAVY MAINTENANCE VISIT, FOUND LOWER FUSELAGE SKIN CRACK AT BS 400 BL-0. REPAIRED PER ECO 2724R1. AIRCRAFT RETU RNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1996080200338 19960802 00338 NM 1996 8 2 TSAA9655052 1 19960624 A 5531 REAR SPAR BOEING 737 7372Q9 138448M NM VERT STAB CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 804AL 21719 DURING HEAVY MAINTENANCE VISIT, FOUND EXFOLIATION ON RIGHT VERTICAL STABILIZER REAR SPAR AT FS 67 TO 83. REPAIRED PER E CO 2509R2. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1996080200339 19960802 00339 NM 1996 8 2 TWRA9642 1 19960621 A 3350 ML7715 BULB BOEING 747 747212B 1384886 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 EVAC LIGHTS AT SEATS 14 HJK, 51HJK, 53 ABC, 62 HJK, L2 MED, 4H, 11A, 14A, AND 13H. REPLACED BULBS, OPS CHECK OK 53-51-0 0. (M) 2 L 7 4 4F A20WE 1996080200340 19960802 00340 NM 1996 8 2 TWRA9643 1 19960622 A 3350 900835A BATTERY BOEING 747 747212B 1384886 NM CABIN DISCHARGED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING CABIN INSPECTION OF EVAC SYSTEM, MAINTENANCE FOUND UPPER DECK EXIT SIGN INOP. MAINTENANCE REMOVED AND REPLACED B ATTERY PACK. OPS CHECK MM 33-51-00 OK. (M) 2 L 7 4 4F A20WE 1996080200341 19960802 00341 NM 1996 8 2 TWRA9644 1 19960622 A 3397 WIRE BOEING 747 747212B 1384886 NM CABIN BROKEN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 SEAT 28 ABC EVAC LIGHT INOP. MAINTENANCE FOUND BROKEN WIRE, REPAIRED WIRE. OPS CHECK OK MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996080200342 19960802 00342 NM 1996 8 2 TWRA9645 1 19960621 A 3350 6012114 BATTERY PACK BOEING 747 747212B 1384886 NM CABIN DISCHARGED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 R/U OVERWING EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK. OPS CHECK OK MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996080200343 19960802 00343 NM 1996 8 2 TWRA9646 1 19960621 A 3350 086861 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 UPPER DECK, GALLEY FLOOR, EVAC LIGHTS INOPERATIVE. REPLACED LIGHT ASSEMBLY. OPS CHECK OK MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996080200344 19960802 00344 WP 1996 8 2 USAA960500 1 19960708 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 1174 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 824US 35439 49143 PIT - DURING Q3/C5 CHECK, FOUND 3 INCH BY 4 INCH CORROSION IN SKIN AT NR 3 VHF ANTENNA FS 1174 AREA, LONGERON 30. TREAT ED AND INSTALLED DOUBLERS PER EO 32910 (10 INCH BY 20 INCH). CORROSION LEVEL 2, CORROSION TASK NR C50-53300. (M) 2 L 7 2 4F A6WE 1996080200345 19960802 00345 WP 1996 8 2 USAA960501 1 19960708 A 5320 1190403 SKIN CLIP DOUG DC9 DC931 3022065 WP BS 1019 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 971VJ 74890 47051 PIT - DURING AFT PRESSURE BULKHEAD REPAIR, PCI-919, FOUND CRACK APPROX 1.25 INCH LONG AT SKIN CLIP. AFT SIDE OF BELT FR AME 1019 LT SIDE, BELOW AUG VALVE. FILLER AND DOUBLER INSTALLED 2014T6 .050 PER EA NR 32448 SRM 53-03 PG 97 FIG 29. (M ) 2 L 7 2 4F A6WE 1996080200346 19960802 00346 WP 1996 8 2 USAA960502 1 19960708 A 5311 99118594 FRAME DOUG DC9 DC931 3022065 WP BS 1104 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 971VJ 74890 47051 PIT - DURING AFT PRESSURE BULKHEAD REPAIR, PCI-919, FOUND CRACK APPROXIMATELY .5 INCH LONG ON CANTED FRAME STA 1104, ST R 12R. INSTALLED DOUBLER 2024T3, .063 INCH PER SRM 53-03, FIG 30. (X) 2 L 7 2 4F A6WE 1996080200347 19960802 00347 WP 1996 8 2 USAA960507 1 19960708 A 5530 991183381 DRAG ANGLE DOUG DC9 DC982 3022082 WP VERT STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 824US 35439 49143 PIT - DURING Q3/C5 CHECK, FOUND 1 INCH CRACK THROUGH RIVET AT LT VERTICAL STABILIZER DRAG ANGLE AFT SIDE CANTED STATION 1388. INSTALLED REPAIR STRAPS AND ANGLES PER SRM 55-02 FIG 26 CONFIG 7001. (M) 2 L 7 2 4F A6WE 1996080200348 19960802 00348 WP 1996 8 2 USAA960510 1 19960708 A 5320 591359535 SKIN CLIP DOUG DC9 DC931 3022065 WP BS 1076 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 971VJ 47051 PIT - DURING AFT PRESSURE BULKHEAD REPAIR, PCI-919, FOUND 1 INCH LONG CRACK AT STATION 1076 LONGERON 16 LEFT AT SKIN CLI P. REPAIRED MFG CLIP FROM 2024T3 .062 PER EA 31776 AND SRM 53-03 FIG 31. (M) 2 L 7 2 4F A6WE 1996080200349 19960802 00349 NM 1996 8 2 USAA960511 1 19960709 A 5315 FLOOR BEAM BOEING 737 7374B7 1384702 NM BS 986.5 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 19229 24555 CLT - CLT INSPECTION VISUALLY FOUND LEVEL 2 CORROSION 100 BY 4 INCHES LOCATED AT STATION 986.5 FROM RT CREASE BEAM TO LT CREASE BEAM. REPLACED T-CAP AS PER TYPICAL REPAIR 53-10-05. (M) 2 L 7 2 4F RT A16WE 1996080200350 19960802 00350 WP 1996 8 2 USAAD96095 1 19960702 A 2150 600300 SEAL DOUG DC9 DC931 3022065 WP LT ACM FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 956VJ 47588 FLT 551 - RDU-CLT - TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED AFTER TAKEOFF, FLICKERED, THEN EXTINGUISHED WHEN BLEEDS WERE TURNED OFF. FOUND LEAKING PERI-SEALS ON DUCT BELOW LEFT ACM. REPLACED SEALS, RAN BOTH PACKS, CHECKS GOOD. (M) 2 L 7 2 4F A6WE 1996080200351 19960802 00351 WP 1996 8 2 USAAD96096 1 19960702 A 3350 60030451LB BATTERY PACK DOUG DC9 DC982 3022082 WP AFT LAV DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 821US 49138 FLOOR LEVEL EMERGENCY LIGHTS (ROWS 19-27) INOPERATIVE. REPLACED BATTERY PACK, CHECKS GOOD. (M) 2 L 7 2 4F A6WE 1996080200352 19960802 00352 WP 1996 8 2 USAAD96097 1 19960704 A 3350 AD20131A BATTERY PACK DOUG DC9 DC931 3022065 WP AFT LAV DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 987VJ 47210 AFT FLOOR AND CATWALK EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK. (M) 2 L 7 2 4F A6WE 1996080200353 19960802 00353 WP 1996 8 2 USAAD96098 1 19960705 A 3350 110049 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 969VJ 47421 FORWARD FLOOR TRACK EMERGENCY LIGHTS INOPERATIVE. REPLACED FORWARD BATTERY PACK. (M) 2 L 7 2 4F A6WE 1996080200354 19960802 00354 WP 1996 8 2 USAAD96099 1 19960706 A 3610 5958765503 MANIFOLD DOUG DC9 DC931 3022065 WP RT ENGINE CRACKED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 931VJ 47188 FLT 2398 - PHL-BOS - AFTER TAKEOFF, AT 1500 FEET, RIGHT FIRE WARNING LIGHT AND BELL CAME ON. PULLED RIGHT ENGINE BACK T O IDLE, AND WARNING CEASED. RETURNED TO FIELD. FOUND 13TH STAGE CROSSOVER MANIFOLD BLOWN, AND ANTI-ICE CROSSOVER LEAKI NG AND EXPANSION JOINT. REPLACED 13TH STAGE CROSSOVER, AND ANTI-ICE CROSSOVER. (M) 2 L 7 2 4F A6WE 1996080200355 19960802 00355 WP 1996 8 2 USAAD96100 1 19960709 A 3350 110049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 817US 48097 FIRST CLASS FLOOR TRACK LIGHTING INOPERATIVE. REPLACED BATTERY PACK. (M) 2 L 7 2 4F A6WE 1996080200356 19960802 00356 EU 1996 8 2 USAAF96061 1 19960621 A 3244 D07354415M TIRE FOKKER F28 F28MK0100 4990807 EU LT MLG FAILED A USAA A UNSCHED LANDING D E INFLIGHT SEPARATION VIBRATION/BUFFET CL CLIMB 1 EA 19 851US 5672 1218 11278 PIT - FL 1050 - ON TAKEOFF, CREW FELT SLIGHT VIBRATION. VIBRATION INCREASED BEFORE GEAR WAS RETRACTED. PASSENGER REPOR TED SEEING A PIECE OF RUBBER GO BY THE WINDOW. FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE NR 1 TIRE HAD LOST ITS RECAP AND DAMAGED THE LEFT WING UNDERSIDE, LEFT FLAP AND THE LEFT OUTBOARD GEAR DOOR. WHEEL WAS REPLACED AND THE DAMAGE REPAIRED. (M) 2 L 7 2 4F RT 1996080200357 19960802 00357 EU 1996 8 2 USAAF96062 1 19960621 A 3350 60030451LB BATTERY PACK FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 480AU 11229 CLT - THE FORWARD EMERGENCY LIGHTS STAYED ILLUMINATED WITH POWER ON. MAINTENANCE REPLACED THE FORWARD EMERGENCY LIGHT B ATTERY PACK. (M) 2 L 7 2 4F RT A20EU 1996080200358 19960802 00358 EU 1996 8 2 USAAF96063 1 19960621 A 2130 3925308 PRSOV FOKKER F28 F28MK0100 4990807 EU RIGHT FAILED A USAA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 EA 19 869US 7077 11314 PIT - FLT 2049 - CLIMBING THROUGH 12,000 FEET, CREW NOTICED A NOISE FROM LEFT PACK, AFTER WHICH THE OUTPUT TEMPERATURE R OSE TO 150 DEGREES. RIGHT PACK TEMPERATURE WAS RUNNING HOT BUT COOLED WHEN ENGINE POWER WAS REDUCED ON DESCENT. CABIN BECAME VERY WARM. FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT PRSOV WHI CH WAS CAUSING A PRESSURE IMBALANCE AND THE RIGHT AIR CONDITIONING PACK. (M) 2 L 7 2 4F RT 1996080200359 19960802 00359 EU 1996 8 2 USAAF96064 1 19960623 A 2150 22034802 PACKS FOKKER F28 F28MK0100 4990807 EU LEFT/RIGHT FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 853US 11281 ATL - FLT 1184 - EN ROUTE MSY-BWI, FL350, CREW NOTED A GRINDING NOISE FROM BOTH PACKS. CABIN THEN BEGAN TO FILL WITH SM OKE. FLIGHT DIVERTED TO ATL AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED BOTH PACKS DUE TO TURBINE FAILUR ES. (M) 2 L 7 2 4F RT 1996080200360 19960802 00360 EU 1996 8 2 USAAF96065 2 19960624 A 7313 FUEL NOZZLE FOKKER F28 F28MK4000 4990810 EU RROYCE SPEY SPEY55515P 54521 EU LT ENGINE BURNED A A USAA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 EA 19 486US 11237 9165 CLT - FLT 464 - AFTER TAKEOFF, THE NR 1 ENGINE WOULD NOT ADVANCE TO FULL THROTTLE AFTER REACHING 8000 FEET. ENGINE SURG ED AFTER 8000 FEET. FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE PERFORMED A BORESCOPE ON T HE ENGINE. SEVERAL FUEL NOZZLES WERE COKED AND ONE BURNED THROUGH. ENGINE WAS REPLACED. (M) 2 L 7 2 4F 4 F RT A20EU E2EU 1996080200361 19960802 00361 EU 1996 8 2 USAAF96066 1 19960624 A 5220 A20425409 HANDLE FOKKER F28 F28MK0100 4990807 EU EMER EXIT BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 891US 11366 FORWARD LEFT OVERWING EMERGENCY EXIT HANDLE WAS FOUND BROKEN. MAINTENANCE REPLACED THE HANDLE. (M) 2 L 7 2 4F RT 1996080200362 19960802 00362 EU 1996 8 2 USAAF96071 1 19960630 A 3610 BS12966 SEAL FOKKER F28 F28MK4000 4990810 EU LOW PRESS VLV LEAKING A USAA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 EA 19 481US 11230 CLT - FL 425 - AFTER TAKEOFF, THE RIGHT BAY OVERHEAT LIGHT ILLUMINATED. THE LIGHT EXTINGUISHED WHEN THE RIGHT BLEED SYS TEM WAS SECURED. FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE LOWER PRESSURE V ALVE SEALS. (M) 2 L 7 2 4F RT A20EU 1996080200363 19960802 00363 EU 1996 8 2 USAAF96072 1 19960628 A 3260 BULBS FOKKER F28 F28MK0100 4990807 EU COCKPIT FAILED A USAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 EA 19 891US 11366 CLT - FLT 2228 - ON APPROACH TO CLT, CREW DID NOT RECEIVE GREEN LIGHTS WITH GEAR EXTENDED. TOWER FLY-BY WAS CONDUCTED, THEN THE ALTERNATE GEAR PROCEDURE WAS PERFORMED. SECOND TOWER FLY-BY CONDUCTED FOLLOWED BY AN UNEVENTFUL LANDING. MAIN TENANCE REPLACED THE LANDING GEAR INDICATION LIGHTS. (M) 2 L 7 2 4F RT 1996080200364 19960802 00364 EU 1996 8 2 USAAF96073 1 19960628 A 3230 200497005 DNLOCK ACTUATOR FOKKER F28 F28MK4000 4990810 EU LT MLG FAILED A USAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 19 484US 11234 FLT 227 - DAY-CLT - LEFT MAIN GEAR DOWN AND LOCKED INDICATOR DID NOT ILLUMINATE ON GEAR EXTENSION. CYCLED GEAR 5 TIMES, THEN DOWN AND LOCKED LIGHT ILLUMINATED. REPLACED LEFT MAIN GEAR DOWNLOCK ACTUATOR. (M) 2 L 7 2 4F RT A20EU 1996080200365 19960802 00365 EU 1996 8 2 USAAF96074 1 19960707 A 3350 6104781 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 853US 11281 PHL - EMERGENCY LIGHT OVER PASSENGER ENTRANCE DOOR INOPERATIVE. REPLACED BATTERY PACK. (M) 2 L 7 2 4F RT 1996080200366 19960802 00366 EU 1996 8 2 USAAF96075 1 19960708 A 5230 DOOR FOKKER F28 F28MK0100 4990807 EU CARGO COMPT NOT SECURE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 858US 11291 CLT - FLT 1278 - CLIMBING THROUGH 1000 FEET, CREW RECEIVED MID CARGO DOOR UNSAFE LIGHT. FLIGHT RETURNED TO CLT AND LAND ED WITH NO FURTHER INCIDENT. MAINTENANCE RESEATED THE DOOR. (M) 2 L 7 2 4F RT 1996080200367 19960802 00367 EU 1996 8 2 USAAF96076 1 19960707 A 3350 6104781 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 853US 11281 PHL - EMERGENCY LIGHT OVER LEFT OVERWING EXIT, INOPERATIVE. REPLACED BATTERY PACK. (M) 2 L 7 2 4F RT 1996080200368 19960802 00368 NM 1996 8 2 USAASB96106 1 19960614 A 3350 6104781 BATTERY PACK BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 281AU 23114 RDU - MAINTENANCE FOUND THE FORWARD ENTRY AND SERVICE DOOR EMERGENCY LIGHTS INOP. MAINTENANCE REPLACED THE BATTERY PACK . (M) 2 L 7 2 4F A16WE 1996080200369 19960802 00369 NM 1996 8 2 USAASB96107 1 19960614 A 3350 900835A BATTERY PACK BOEING 737 737201 1384454 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 256AU 22798 SYR - MAINTENANCE FOUND THE AFT SET OF AISLE EMERGENCY SEAT LIGHTS BLINKING ON AND OFF. MAINTENANCE REPLACED THE BATTER Y PACK. (M) 2 L 7 2 4F A16WE 1996080200370 19960802 00370 NM 1996 8 2 USAASB96121 1 19960706 A 2613 OVERHEAT LIGHT BOEING 737 7374B7 1384702 NM NR 1 ENGINE ILLUMINATED A USAA A E UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 EA 19 780AU 24997 BDA - FL 1459 - WHILE CLIMBING OUT OF DBA AT 24,000 FEET, THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. REDUCED THRUST TO IDLE, HOWEVER, LIGHT REMAINED ON. CAPTAIN SHUT DOWN THE NR 1 ENGINE AND RETURN TO BDA. TOTAL SINGLE ENGINE TIME WAS 1 6 MINUTES. MAINTENANCE CHECKED FOR AIR LEAKS. NO LEAKS FOUND. PERFORMED ENGINE RUN AT HIGH POWER. CHECKS NORMAL. FO UND B LOOP WOULD NOT TEST ON GROUND. ACCOMPLISHED CONTINUITY CK OF NR 1 ENGINE B LOOP FROM M279 PLUG D1002. FOUND NORM AL. CHECKED ALL B LOOP CONNECTORS FOR DEFECTS, NONE FOUND. PERFORMED B LOOP OPERATIONAL CHECK, CHECKED NORMAL. (M) 2 L 7 2 4F RT A16WE 1996080200371 19960802 00371 NM 1996 8 2 9616046636 1 19960727 A 3350 BATTERY PACK BOEING 747 747251B 1384892 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 636US 23547 DURING LINE CHECK, FOUND THE OVERWING EMERGENCY LIGHTS AT DOOR 4L INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHEC K GOOD. 2 L 7 4 4F A20WE 1996080200372 19960802 00372 NM 1996 8 2 9616052768 1 19960727 A 2410 700842A CSD BOEING 727 7272M7 138407S NM NR 1 ENGINE FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 728RW 21031 995 21741 DURING INITIATION ON TAKEOFF POWER, THE NR 1 CSD LOW PRESSURE LIGHT FLICKERED FOLLOWED BY A GENERATOR TRIP ON NR 1 ENGIN E. REPLACED NR 1 CSD. LEAK AND OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996080200373 19960802 00373 NM 1996 8 2 9616062767 1 19960725 A 5753 TRAILING EDGE BOEING 727 7272M7 138407S NM RT TE AFT FLAP VIBRATION A NWAA A UNSCHED LANDING E F VIBRATION/BUFFET FLT CONT AFFECTED CL CLIMB 1 GL 01 727RW 21656 DURING CLIMB-OUT THROUGH 20,000 FEET, ENCOUNTERED AIRCRAFT VIBRATION. IT APPEARED THE RIGHT INBOARD TRAILING EDGE HAD S TARTED TO FLUTTER. ACCOMPLISHED AIRCRAFT VIBRATION CHECK. ADJUSTED THE RIGHT INBOARD AFT FLAP AND PERFORMED FLIGHT CON TROL SYSTEM CHECK. CHECKED OK. 2 L 7 3 4F A3WE 1996080200374 19960802 00374 WP 1996 8 2 9616079929 1 19960727 A 2822 FUEL LINE DOUG DC9 DC931 3022065 WP RT BOOST PUMP DISCONNECTED A A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION UK UNKNOWN 1 GL 01 8923E 45838 FUEL BEGAN VENTING FROM LEFT WING EN ROUTE DCA-MSP. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT INCIDENT. FORWARD AND AF T RIGHT FUEL PRESSURE LIGHTS WOULD NOT EXTINGUISH AFTER LANDING. MAINTENANCE FOUND FUEL LINE AT FORWARD RIGHT FUEL BOOS T PUMP DISCONNECTED AT UNION. LINE WAS RECONNECTED AND A NEW O-RING WAS INSTALLED. LEAK AND OPERATIONAL CHECK NORMAL, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996080200375 19960802 00375 WP 1996 8 2 9616089859 1 19960721 A 3260 TARGET BOLT DOUG DC9 DC951 3022051 WP RT MLG OUT OF ADJUST A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 768NC 47729 AFTER TAKEOFF ON GEAR RETRACTION, GEAR DOOR OPEN LIGHT REMAINED ON. RECYCLED GEAR AND LIGHT REMAINED ON. RECYCLED GEAR AND GOT LEFT AND RIGHT GEAR UNSAFE LIGHT AND DOOR OPEN LIGHT. DESCENDED TO 18,000 FEET AND SLOWED TO 180 KNOTS. ALL L IGHTS WENT OUT. FLIGHT CONTINUED TO MEM AND LANDED WITHOUT INCIDENT. FOUND RIGHT PROXIMITY SWITCH TARGET THROUGH-BOLT HITTING ON FORWARD DOOR FRAME. ADJUSTED AND SWUNG GEAR FIVE TIMES AND EMERGENCY EXTENSION, ALL CHECKED GOOD. 2 L 7 2 4F A6WE 1996080200376 19960802 00376 1996 8 2 9616099156 4 19960727 A 3442 RADAR TR UNIT DOUG DC9 DC914 3022034 WP FWD FUS FAILED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 8915E 45832 AFTER DEPARTURE, RADAR WOULD NOT PAINT WEATHER OR GROUND RETURNS. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. R EPLACED TRANSCEIVER AND RADAR INDICATOR. SYSTEM CHECKS WERE NORMAL ON GROUND IN TEST PATTERN. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996080200377 19960802 00377 1996 8 2 9616109156 4 19960727 A 3442 RADAR ANTENNA DOUG DC9 DC914 3022034 WP FWD FUS MALFUNCTIONED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 8915E 45832 DURING CLIMB-OUT OF MSP, RADAR PICTURE WAS VERY POOR, PAINTS SOME WEATHER BUT ALWAYS SPOKING. FLIGHT RETURNED TO MSP AN D LANDED WITHOUT INCIDENT. REPLACED RADAR ANTENNA AND TRANSCEIVER. RADAR OPERATIONALLY CHECKED GOOD ON GROUND. 2 L 7 2 4F A6WE 1996080200378 19960802 00378 WP 1996 8 2 9616119153 1 19960727 A 3350 BATTERY PACK DOUG DC9 DC914 3022034 WP COCKPIT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8912E 45829 DURING LINE CHECK, FOUND COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996080200379 19960802 00379 WP 1996 8 2 9616129752 1 19960721 A 3397 WIRE DOUG DC9 DC941 302207N WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 752NW 47116 DURING LINE CHECK, FOUND EMERGENCY EXIT FLOOR LIGHTS INOPERATIVE AT FORWARD OVERWING EXIT. REPAIRED BROKEN WIRE AT RIGH T SIDEWALL. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996080200380 19960802 00380 WP 1996 8 2 9616139874 1 19960724 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 785NC 48108 DURING LINE CHECK, FOUND OVERHEAD EMERGENCY LIGHT FORWARD OF WING INOPERATIVE. REPLACED BATTERIES. OPERATIONAL CHECK O K. 2 L 7 2 4F A6WE 1996080200381 19960802 00381 WP 1996 8 2 9616149302 1 19960725 A 3350 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 302RC 48055 DURING LINE CHECK, FOUND CABIN EMERGENCY CEILING LIGHTS OUT AT ROW 5 THROUGH ROW 10. REPLACED POWER SUPPLY. OPERATIONA L CHECK OK. 2 L 7 2 4F A6WE 1996080200382 19960802 00382 WP 1996 8 2 9616159856 1 19960725 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 765NC 47718 DURING LINE CHECK, FOUND RIGHT AND LEFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996080200383 19960802 00383 WP 1996 8 2 9616169877 1 19960726 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 786NC 48148 DURING LINE CHECK, FOUND CEILING EMERGENCY LIGHTS AT ROWS 20 - 25 AND 7 - 11 FAILED TO TEST. REPLACED BATTERIES IN POWE R SUPPLIES AT ROWS 8 AND B2 - 58. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996080200384 19960802 00384 WP 1996 8 2 9616179752 1 19960726 A 3350 SPLICE DOUG DC9 DC941 302207N WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 752NW 47116 DURING LINE CHECK, FOUND EMERGENCY ESCAPE FLOOR LIGHTING INOPERATIVE AT ROWS 7 - 13. REPAIRED BROKEN SPLICE. OPERATION AL CHECK OK. 2 L 7 2 4F A6WE 1996080200385 19960802 00385 WP 1996 8 2 9616189974 1 19960728 A 3231 RETRACT MECH DOUG DC9 DC931 3022065 WP NLG RT DOOR NOT LATCHED A NWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 01 9338 47347 VIBRATION FROM NOSE GEAR AREA OCCURRED AFTER TAKOEFF. FLIGHT RETURNED TO YUL AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND RIGHT NOSE GEAR DOOR OPEN. RESECURED DOOR. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996080200386 19960802 00386 WP 1996 8 2 9616199968 1 19960722 A 2530 TERMINAL BLOCK DOUG DC9 DC931 3022065 WP COFFEEMAKER MELTED A NWAA K NONE O OTHER UK UNKNOWN 1 GL 01 9332 47264 FLIGHT ATTENDANT REPORTED THAT FORWARD GALLEY COFFEEMAKER HAD NO POWER. MAINTENANCE INSPECTED WIRING AND FOUND WIRING A ND TERMINAL BLOCK TO COFFEEMAKER MELTED. DEFERRED COFFEEMAKER AND COLLARED CIRCUIT BREAKER. AWAITING PARTS FOR TERMINA L BLOCK REPLACEMENT. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996080200387 19960802 00387 WP 1996 8 2 9616209609 1 19960728 A 3350 LIGHTS DOUG DC9 DC932 3022066 WP LT/RT NACELLE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 609NW 47234 DURING LINE MAINTENANCE INSPECTION, FOUND BOTH ENGINE NACELLE EMERGENCY LIGHTS INOPERATIVE IN TEST MODE. REPLACED BOT H POWER SUPPLIES AND BATTERIES. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996080200388 19960802 00388 WP 1996 8 2 9616219601 1 19960725 A 3350 6011779 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 601NW 47038 DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPERATION AL CHECK NORMAL. 2 L 7 2 4F A6WE 1996080200389 19960802 00389 WP 1996 8 2 9616229997 1 19960725 A 3350 LIGHTS DOUG DC9 DC931 3022065 WP TAIL COMPT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8933E 47142 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY EVACUATION TRACK LIGHTING AT CATWALK INOPERATIVE. REPAIRED WIRE HARNESS AND REPLACED ALL THREE LIGHT SOCKETS. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996080200390 19960802 00390 WP 1996 8 2 9616239998 1 19960728 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8934E 47143 DURING LINE MAINTENANCE INSPECTION, FOUND COCKPIT AND FORWARD ENTRY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES. O PERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996080200391 19960802 00391 WP 1996 8 2 9616249955 1 19960726 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 922RW 47182 FORWARD CABIN EMERGENCY EVACUATION LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AT FORWARD SERVICE DOOR. OPERATIONAL CHEC K NORMAL. 2 L 7 2 4F A6WE 1996080200392 19960802 00392 WP 1996 8 2 9616259964 1 19960726 A 3350 GROUND WIRE DOUG DC9 DC931 3022065 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 912RW 47150 DURING PERIODIC CHECK, FOUND MID-CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPAIRED BROKEN GROUND WIRE AT BATTERY P ACK. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996080200393 19960802 00393 WP 1996 8 2 9616269911 1 19960728 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP LT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 961N 47405 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT ENGINE NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERIES. OPERATI ONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996080200394 19960802 00394 1996 8 2 9616279921 4 19960725 A 2565 113317 EVAC SLIDE DOUG DC9 DC932 3022066 WP PAX DOOR WEAK BATTERY A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 943N 10796 54524 47647 DURING PERIODIC CHECK, MAIN CABIN DOOR EVACUATION SLIDE FAILED BATTERY TEST. REPLACED SLIDE. 2 L 7 2 4F A6WE 1996080200395 19960802 00395 WP 1996 8 2 9616289955 1 19960726 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 922RW 47182 FORWARD CABIN FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE, BATTERIES, AND LAMPS. OPERATIONAL CHECK NOR MAL. 2 L 7 2 4F A6WE 1996080200396 19960802 00396 NE 1996 8 2 9616299910 2 19960726 A 7321 FUEL CONTROL DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9 52048 NE RT ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 960N 47256 666150 DURING TAKEOFF, RIGHT ENGINE EPR WOULD NOT REACH TAKEOFF SETTING AND RIGHT ENGINE ALSO HAD FIRE LOOP LIGHT ILLUMINATION. CREW ABORTED TAKEOFF AND RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE REPLACED FUEL CONTROL, PUMP ASSEMBLY, AND PRE SSURE RATIO BLEED CONTROL VALVE. OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F A6WE E2EA 1996080200397 19960802 00397 NM 1996 8 2 96FDEA01139 1 19960614 A 5311 6516346 FRAME BOEING 727 727173C 1384059 NM BS 1110 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 199FE 19509 NR 0546 AND 011. WHILE WORKING NR 0537, FOUND CORROSION ON FRAME BS 1110, WL 150, RBL 29 - RBL 34. BLENDED CORROSION, FOUND TO BE WITHIN LIMITS PER DWG 65-16346. ALODINED AND PRIMED AREAS. 2 L 7 3 4F A3WE 1996080200398 19960802 00398 NM 1996 8 2 96FDEA01288 1 19960726 A 7930 42D107A2 OIL BYPASS SW BOEING 727 727233 138408A NM NR 1 ENGINE FAILED A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 SO 25 222FE 20933 NR 1 OIL BYPASS LIGHT ON IN FLT, OIL PRESS 50, TEMP 90, 3.5 GAL, ALL OK. IT STAYED ON AT IDLE PWR, SHUTDOWN NR 1. A/C RELEASED FOR SERVICE PER MEL 79-2 CAT B EXP 29JUL96. *S/D* REMOVED AND REPLACED NR 1 OIL BYPASS SWITCH. RAN AND OPS CHECK GOOD. 2 L 7 3 4F RT A3WE 1996080200399 19960802 00399 NM 1996 8 2 96FDEA01289 1 19960727 A 3260 WARNING HORN BOEING 727 72725C 138400H NM LANDING GEAR SOUNDED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 119FE 19301 ON TAKEOFF, GEAR WARNING HORN SOUNDED WHEN GEAR RETRACTED WITH FLAPS IN 25 DEGREE POSITION. COULD NOT BE SILENCED WITHO UT LOWERING THE GEAR. PERFORMED LANDING GEAR WARNING SYSTEM TEST IAW MM 31-26-0 STEOS 26-31 FOR SERVICE. 2 L 7 3 4F A3WE 1996080200400 19960802 00400 NM 1996 8 2 96FDEA01290 1 19960726 A 5311 65229592 FRAME BOEING 727 72722 1384002 NM BS 913 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 NR 0370 039. BS 913, WL 194, STR 18A FRAME IS CRACKED IN MAIN WHEELWELL. REPAIRED CRACKED FRAME BS 13, WL 194, STR 18A IAW FEDEX EA 7-5310-29295A. 2 L 7 3 4F A3WE 1996080200401 19960802 00401 NM 1996 8 2 96FDEA01291 1 19960726 A 5311 6582615 FRAME BOEING 727 7272D4 138407U NM BS 950 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 287FE 21849 NR 0386 023. FRAME IS CRACKED UNDER UPPER FLANGE AT STA 950E, 4.50 INCHES INBOARD OF STR 26L FROM HI-LOCK FASTENER HOLE INTO RADIUS OF FLANGE (OVER .25 INCH LONG). REMOVED DAMAGE AND REPAIRED FRAME UNDER UPPER FLANGE AT BS 950E, LBL 7 - 3 5 PER FEDEX SRM 51-40-3. 2 L 7 3 4F A3WE 1996080200402 19960802 00402 NM 1996 8 2 96FDEA01293 1 19960729 A 5720 65185371 CHORD BOEING 727 72722 1384002 NM BS 870 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 NR 0231 042. CORROSION C53-132-02(1) ON STA 870, UPPER CHORD LBL 58-60, 46, 36-38, 26-28, 17-19, RBL 55, 45, 10, 0 WL 1 72. REMOVED AND REPLACED 870 UPPER CHORD LBL 70 - RBL 70, WL 172 PER FEDEX EA 7-5710-29709. 2 L 7 3 4F A3WE 1996080200403 19960802 00403 NM 1996 8 2 96FDEA01294 1 19960722 A 5311 65191601 FRAME BOEING 727 72722 1384002 NM BS 480 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 NR 0757 041. CRACK ON INBOARD FLANGE OF FRAME AT BS 480 STR 26R RBL 24. REMOVED DAMAGE IN FRAME AT BS 480, STR 26R RBL 24. FABRICATED REPAIR PART, ALODINED, PRIMED, PAINTED AND INSTALLED REPAIR PART PER FEDEX SRM 51-40-3. 2 L 7 3 4F A3WE 1996080200404 19960802 00404 NM 1996 8 2 96FDEA01295 1 19960710 A 5210 50794516 GATE BEAM BOEING 727 72722 1384002 NM FWD ENTRY DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 NR 0143 040. FORWARD ENTRY DOOR LOWER GATE BEAM IS CRACKED 2 EACH PLACES ADJACENT TO LOWER FORWARD STOP PIN FITTING. R EMOVED AND REPLACED LOWER GATE BEAM PER FEDEX SRM 51-10-1. 2 L 7 3 4F A3WE 1996080200405 19960802 00405 NM 1996 8 2 CALA9601081 1 19960728 A 3260 SWITCH BOEING 727 727232 1384082 NM RT MLG DOOR INOPERATIVE A CALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 45793 20647 THE RT GEAR DOOR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTON DEPARTING EWR. THE RED DOORS LIGHT WAS ALSO ON. A RET URN TO EWR WAS BEGUN AND BOTH LIGHTS REMAINED ILLUMINATED WHEN GEAR WAS EXTENDED FOR LANDING. THE AIRCRAFT LANDED AT EW R WITHOUT INCIDENT. MAINTENANCE VERIFIED THE RIGHT GEAR DOOR WAS UP AND LOCKED WITH LIGHTS ON. THE LANDING GEAR DOOR W ARNING SWITCH WAS FOUND AT FAULT. THE SWITCH WAS REMOVED AND REPLACED. OPERATION AND INDICATIONS CHECKED GOOD IAW MM 3 2-62-11, PAGE 501. 2 L 7 3 4F A3WE 1996080200406 19960802 00406 WP 1996 8 2 CALA9601082 1 19960729 A 7921 749965 OIL COOLER DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE NR 2 ENGINE INOPERATIVE A A CALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 09 16807 24831 24831 49261 717409 THE NR 2 ENGINE OIL TEMPERATURE APPROACHED REDLINE AFTER TAKEOFF FROM SFO. THE TEMPERATURE INCREASE WAS ACCOMPANIED BY OIL PRESSURE DROP. THE NR 2 ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS RETURNED TO SFO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE OIL COOLER AT FAULT. THE OIL COOLER WAS REMOVED AND REPLACED. THE ENGINE WAS RUN W ITH NO LEAKS NOTED AND ALL ENGINE INDICATIONS WERE NORMAL. PART TOTAL CYCLES, 12,240. 2 L 7 2 4F 4 F A6WE E9NE 1996080200407 19960802 00407 NE 1996 8 2 CALA9601083 2 19960729 A 7510 7958591505 DUCT DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 1 ENGINE BLOWN A CALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 35832 49492 708491 THE NR 1 ENGINE FIRE WARNING LIGHT AND BELL ACTIVATED DURING CLIMB-OUT OF MIA. CHECKLIST PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT WAS RETURNED TO MIA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE ANTI-ICE DUCT FROM NOSE COWL TO SADDLE DUCT BLOWN. THE DUCT WAS REMOVED AND REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F 4 F A6WE E9NE 1996080200408 19960802 00408 WP 1996 8 2 CALA9601084 1 19960713 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 1038 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND A 3 INCH CRACK IN FUSELAGE SKIN AT STA 1038, LT SIDE, ABOVE PYLON. THE AREA WAS REPAIRED IAW SRM 53-04 . 2 L 7 2 4F A6WE 1996080200409 19960802 00409 WP 1996 8 2 CALA9601085 1 19960712 A 5210 591412161 PAN DOUG DC9 DC932 3022066 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND A 1 INCH CRACK IN MAIN CABIN DOOR PAN AT LOWER HINGE AREA. A DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5210-01262. 2 L 7 2 4F A6WE 1996080200410 19960802 00410 WP 1996 8 2 CALA9601086 1 19960702 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND FLOOR SUPPORT CORRODED AT FORWARD SERVICE DOOR. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51- 10-03. 2 L 7 2 4F A6WE 1996080200411 19960802 00411 WP 1996 8 2 CALA9601087 1 19960701 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 370 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT STA 370, LONGERON 26L. THE FLOOR SUPPORT WAS REPAIRED IAW SRM 51-10 -02. 2 L 7 2 4F A6WE 1996080200412 19960802 00412 WP 1996 8 2 CALA9601088 1 19960702 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 935 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND WEB CORRODED AT FORWARD SIDE OF AFT BAGGAGE BIN DOOR CUT OUT, STA 935. THE CORRODED AREA OF WEB WAS CU T OUT AND A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 4. 2 L 7 2 4F A6WE 1996080200413 19960802 00413 WP 1996 8 2 CALA9601089 1 19960711 A 5320 CLIPS DOUG DC9 DC932 3022066 WP BS 996 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND UPPER AND LOWER AFT PRESSURE BULKHEAD CLIPS ON BOTH THE LT AND RT SIDES CRACKED AT Z= 34, STA 996. THE CLIPS WERE REMOVED AND REPLACED IAW SRM 51-60-0 AND DOUGLAS DRAWING 9915558. 2 L 7 2 4F A6WE 1996080200414 19960802 00414 WP 1996 8 2 CALA9601090 1 19960711 A 5312 BULKHEAD CLIPS DOUG DC9 DC932 3022066 WP BS 996 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND UPPER AND LOWER AFT PRESSURE BULKHEAD CLIPS CRACKED ON BOTH LT AND RT SIDES AT Z= 24, STA 996. THE CLI PS WERE REMOVED AND REPLACED IAW DOUGLAS DRAWING 9915558. 2 L 7 2 4F A6WE 1996080200415 19960802 00415 WP 1996 8 2 CALA9601091 1 19960711 A 5312 CLIPS DOUG DC9 DC932 3022066 WP BS 996 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND THE UPPER AND LOWER AFT PRESSURE BULKHEAD CLIPS CRACKED ON BOTH THE LT AND RT SIDES AT Z= 14, STA 996. THE CLIPS WERE REMOVED AND REPLACED IAW DOUGLAS DRAWING 9915558. 2 L 7 2 4F A6WE 1996080200416 19960802 00416 WP 1996 8 2 CALA9601092 1 19960711 A 5312 BULKHEAD CLIPS DOUG DC9 DC932 3022066 WP BS 996 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND UPPER AND LOWER AFT PRESSURE BULKHEAD CLIPS CRACKED ON LT SIDE AT Z= 48, STA 996. THE CLIPS WERE REMOV ED AND REPLACED IAW DOUGLAS DRAWING 9915558. 2 L 7 2 4F A6WE 1996080200417 19960802 00417 WP 1996 8 2 CALA9601093 1 19960711 A 5312 BULKHEAD CLIP DOUG DC9 DC932 3022066 WP BS 996 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND A .50 INCH CRACK IN THE LOWER AFT PRESSURE BULKHEAD CLIP ON RT SIDE AT Z= 48.5, STA 996. THE CLIP WAS REMOVED AND REPLACED IAW DOUGLAS DRAWING 9915558. 2 L 7 2 4F A6WE 1996080200418 19960802 00418 WP 1996 8 2 CALA9601094 1 19960717 A 5320 HAT SECTION DOUG DC9 DC982 3022082 WP FWD ENTRY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16887 49116 INSPECTION FOUND HAT SECTION CORRODED AROUND NUTPLATE HOLE BETWEEN PANEL J AND H AT FORWARD ENTRY. THE HAT SECTION WAS REMOVED AND A NEW HAT SECTION WAS INSTALLED IAW SRM 51-30-1. 2 L 7 2 4F A6WE 1996080200419 19960802 00419 WP 1996 8 2 CALA9601095 1 19960711 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP BS 1309 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16887 49116 INSPECTION FOUND FIVE 1 INCH CRACKS IN INTERCOSTAL IN AFT BAGGAGE BIN AT STA 1309. THE CRACKS WERE STOP DRILLED AND A D OUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2. 2 L 7 2 4F A6WE 1996080200420 19960802 00420 WP 1996 8 2 CALA9601096 1 19960710 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP BS 465-484 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16887 49116 INSPECTION FOUND A 10 INCH CRACK IN FORWARD BAGGAGE BIN INTERCOSTAL AT VHF ANTENNA MOUNT BETWEEN STA 465 AND STA 484. T HE INTERCOSTAL WAS REMOVED AND A NEW ONE WAS INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1996080200421 19960802 00421 WP 1996 8 2 CALA9601097 1 19960712 A 5320 SUB FLOOR DOUG DC9 DC982 3022082 WP BS 1136-1274 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16887 49116 INSPECTION FOUND BOTTOM OF SUB-FLOOR CORRODED OUTBOARD OF LEFT OUTBOARD SEAT TRACK AT STA 1136-1274. THE SUB-FLOOR WAS REPLACED IAW SRM 51-30-02. 2 L 7 2 4F A6WE 1996080200422 19960802 00422 WP 1996 8 2 CALA9601098 1 19960708 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 165 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16887 49116 INSPECTION FOUND FUSELAGE SKIN DENTED BETWEEN LONGERON 21R AND 22R AT STA 165. THE DENT WAS COLD-FORMED AND DYE CHECKED WITH NO CRACKS FOUND. AN INTERNAL DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, PAGE 218. 2 L 7 2 4F A6WE 1996080200423 19960802 00423 WP 1996 8 2 CALA9601099 1 19960711 A 5320 CHANNEL DOUG DC9 DC982 3022082 WP BS 69 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16887 49116 INSPECTION FOUND Z-CHANNEL CRACKED AT STA 69. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2, PAGE 9 AN D SRM 51-30-5. 2 L 7 2 4F A6WE 1996080200424 19960802 00424 WP 1996 8 2 CALA9601100 1 19960708 A 5330 SKIN DOUG DC9 DC982 3022082 WP FWD FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16887 49116 INSPECTION FOUND FUSELAGE SKIN DENTED FORWARD OF PITOT TUBES. THE DENTED SECTION OF SKIN WAS REPLACED IAW SRM 51-30-2 A ND SRM 51-30-5. 2 L 7 2 4F A6WE 1996080200425 19960802 00425 SO 1996 8 2 COMA9610231 1 19960725 A 2150 PACK EMB 120 EMB120RT SO RTGHT SMOKING A COMA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 1117H 120117 RIGHT COOLING PACK FAIL WARNING - SMOKE IN CABIN. COULD NOT DUPLICATE DISCREPANCY. INSPECTION AND OPERATION OF SYSTEM NORMAL. NO DEFECTS FOUND. 2 L 7 2 4T RT A31SO 1996080200426 19960802 00426 SO 1996 8 2 COMA9610232 1 19960725 A 5280 12037521001 HINGE EMB 120 EMB120RT SO RT MLG DOOR BROKEN A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 263CA 120255 RIGHT M.L.G. DID NOT RETRACT WHEN LANDING GEAR WAS SELECTED UP. REPLACED BROKEN LANDING GEAR DOOR AFT HINGE, WHICH DID NOT ALLOW ACTUATION OF THE SEQUENCE VALVE. 2 L 7 2 4T RT A31SO 1996080200427 19960802 00427 SO 1996 8 2 COMA9610233 1 19960729 A 2752 3082001007 ACTUATOR EMB 120 EMB120RT SO LT NACELLE FLAP MALFUNCTION A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 189CA 195 120189 FLAP CONTROL FAULT WARNING DURING APPROACH. REPLACED LT NACELLE FLAP ACTUATOR. PART TOTAL CYCLES, 200. 2 L 7 2 4T RT A31SO 1996080200428 19960802 00428 SO 1996 8 2 COMA9610234 1 19960729 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 179CA 11271 531 120179 MIDDLE SECTION OF FLOOR PATH EMERGENCY LIGHTING IS INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY. PART TOTAL CYCLES, 1 1,171. 2 L 7 2 4T RT A31SO 1996080200429 19960802 00429 1996 8 2 COMA9630138 4 19960729 A 3442 6224022001 R/T UNIT SAAB SF340 SF340A 7850100 EU RADAR MALFUNCTION A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 347CA 18439 6726 340A028 WHEN RADAR IS TILTED ABOVE GROUND RETURN, STORMS DISAPPEAR. REPLACED THE RADAR R/T. PART TOTAL CYCLES, 20,726. 2 L 7 2 4T RT A52EU 1996080200430 19960802 00430 NE 1996 8 2 COMA9630139 2 19960729 A 7261 AC9718F25 FILTER SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LT ENGINE DIRTY A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 344CA 15 340A025 367108 LEFT ENGINE OIL BYPASS INDICATION ILLUMINATED. REPLACED THE ENGINE OIL FILTER. PART TOTAL CYCLES, 15. 2 L 7 2 4T 4 T RT A52EU E8NE6 1996080200431 19960802 00431 EA 1996 8 2 COMA9660126 1 19960728 A 2760 54C54677E01 MANIFOLD ASSY CNDAIR CL600 CL6002B19 EA SPOILER SYST MALFUNCTION A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 940CA 2943 7048 RIGHT OUTBOARD GROUND SPOILER DEPLOY CAUTION MESSAGE ON EICAS. SPOILER WAS VISUALLY CONFIRMED TO BE STOWED. REPLACED T HE SPOILER MANIFOLD ASSY. PART TOTAL CYCLES, 3,599. 2 L 7 2 4F RT A21EA 1996080200432 19960802 00432 NM 1996 8 2 DL73S961752 1 19960703 A 5312 BULKHEAD WEB BOEING 737 737232 1384475 NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 303DL 23075 DURING MID-VISIT, 178 BULKHEAD WAS FOUND TO BE CRACKED IN WEB. DAMAGE WAS REPAIRED WITH AN ALUMINUM DOUBLER IN ACCORDAN CE WITH FAA/DER FORM 8110-3, DER DESIGNATION SO-867. 2 L 7 2 4F RT A16WE 1996080200433 19960802 00433 NM 1996 8 2 DL73S961765 1 19960723 A 3350 BPS73 POWER SUPPLY BOEING 737 737232 1384475 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 309DL 23081 AFT CABIN EMERGENCY FLOOR TRACK INOPERATIVE. C/A: REPAIRED WIRE ON TRACK AND REPLACED BATTERY AND POWER SUPPLY FOR AFT TRACK POWER SUPPLY, MFG NR BPS7-3. BATTERY MFG NR 2013-1A. 2 L 7 2 4F RT A16WE 1996080200434 19960802 00434 NM 1996 8 2 DL757961764 1 19960724 A 3350 BPS73 POWER SUPPLY BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 644DL 23998 ON PRE-DEPARTURE CHECK, FOUND LENS AND BULB MISSING FROM F/C EMERGENCY LIGHT FLOOR TRACK. REPLACED POWER SUPPLY AND REP AIRED WIRES IN FLOOR TRACK. 2 L 7 2 4F RT A2NM 1996080200435 19960802 00435 NM 1996 8 2 DL757961766 1 19960513 A 5720 TE WEDGE 114N4005178 BOEING 757 757232 1384965 NM WING DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 607DL 000031 22814 TRAILING EDGE WEDGE UPPER AND LOWER SKIN DELAMINATED AT INBOARD END. REPLACED TRAILING EDGE WEDGE. REF SRM 57-43-02. 2 L 7 2 4F RT A2NM 1996080200436 19960802 00436 NM 1996 8 2 DL757961787 1 19960630 A 5720 TE WEDGE 114N4002147 BOEING 757 757232 1384965 NM WING DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 644DL A10175 23998 TRAILING EDGE WEDGE DELAMINATED. REPLACED WEDGE PER SRM 57-43-02. 2 L 7 2 4F RT A2NM 1996080200437 19960802 00437 NM 1996 8 2 DL757961792 1 19960723 A 3350 3020424 LIGHT BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 646DL 24217 IRREG: FOUND ON L/O R2 SLIDE LIGHT INOPERATIVE. CORR: REPLACED LIGGT ASSY. SYSTEM CHECKS GOOD. 2 L 7 2 4F RT A2NM 1996080200438 19960802 00438 NM 1996 8 2 DL76L961794 1 19960726 A 3350 FUSE M9009 BOEING 767 767332 1382001 NM CABIN BLOWN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 174DN 24802 ON L/O, FOUND E-PATH LIGHT IN AFT B/C AND FORWARD PART OF Y-CLASS INOPERATIVE ON BOTH SIDES. REPLACED FUSE F1 IN POWER SUPPLY. OPS CKS OK. 2 L 7 2 4F RT A1NM 1996080200439 19960802 00439 NM 1996 8 2 DL76L961803 1 19960728 A 2520 WIRE BOEING 767 767332 1382001 NM PAX SEAT CHAFED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 175DN 24803 WIRING FOR F/C SEAT 2-A AND OTHER SEATS ON CIRCUIT SHORTED AND BURNED THROUGH. PULLED ASSOCIATED CIRCUIT BREAKERS, P-36 AND P-37 IN E/E COMPARTMENT PER MTC CO-ORDINATOR. REPAIRED CHAFED WIRE. SYSTEM OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 1996080200440 19960802 00440 1996 8 2 DL76S961772 4 19960724 A 2565 SLIDE 101651303 BOEING 767 767332 1382001 NM CABIN DOOR DEPLOYED A DALA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 138DL 2561 25409 DOOR 2R SLIDE DEPLOYED, FLIGHT ATTENDANT REPORTED ARMING/DEARMING MECHANISM DIFFICULT TO OPERATE. FORWARD 2R SLIDE TO M CO PER MEL 52-11-04 ARMING MECHANISM CHECKS GOOD. SLIDE REPLACED ON LOG A020745004, FLT 1632 IN BOS, S/N INSTALLED PA13 54, MCO AND PLACARD REMOVED. 2 L 7 2 4F RT A1NM 1996080200441 19960802 00441 WP 1996 8 2 DLL17961776 1 19960725 A 3310 BALLAST LKHEED 1011 10113853 5265020 WP COCKPIT FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 769DL 193H1218 FLUORESCENT LIGHT UNDER CAPTAIN'S GLARESHIELD - BALLAST BECAME VERY HOT AND CAUSES ELECTRICAL OVERHEAT AND SMELL IN THE COCKPIT. REPOSITIONED WIRES AT BALLAST. SYSTEM CHECKS GOOD. 2 L 7 3 4F A23WE 1996080200442 19960802 00442 NM 1996 8 2 DLM88961756 1 19960720 A 5320 JAMB DOUG MD88 MD88 3023688 NM FWD CARGO DOOR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DL 49537 DURING LETTER CHECK, THE FORWARDD CARGO DOOR OPENING WAS FOUND WITH EXTENSIVE CORROSION ON THE LOWER JAMB PAN. A SPLICE REPAIR WAS ACCOMPLISHED PER MD-88, SRM 53-05, FIG 44. 2 L 7 2 4F RT A6WE 1996080200443 19960802 00443 NM 1996 8 2 P5CA9600404 1 19960726 A 4980 EXHAUST DUCT BOEING 747 747122 1384872 NM APU CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 CRACK IN THE APU EXHAUST DUCT AT 12:00 O'CLOCK POSITION. WELDED CRACK PER BAC 5975. 2 L 7 4 4F A20WE 1996080200444 19960802 00444 NM 1996 8 2 P5CA9600405 1 19960726 A 5753 FAIRINGS BOEING 747 747122 1384872 NM FLAP TRACKS DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 NRS 1, 2, 3, 5, AND 8 FLAP TRACK FIXED FAIRINGS HAVE SEVERAL AREAS OF EROSION AND DELAMINATION. REPAIRED PER BOEING SRM 51-40-12. 2 L 7 4 4F A20WE 1996080200445 19960802 00445 NM 1996 8 2 P5CA9600406 1 19960726 A 7110 COWL LOWER RAIL BOEING 747 747122 1384872 NM NR 3 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 NR 3 ENGINE INBOARD CORE COWL LOWER RAIL CRACKED IN 3 PLACES. REMOVED, FABRICATED AND INSTALLED LOWER RAIL PER BOEING S RM 51-10-01 AND SRM 51-30-02. 2 L 7 4 4F A20WE 1996080200446 19960802 00446 NM 1996 8 2 P5CA9600407 1 19960726 A 5280 HINGE BOEING 747 747122 1384872 NM RT MLG DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 RIGHT WING GEAR INBOARD DOOR FORWARD HINGE IS CRACKED. REPLACED HINGE PER BOEING MAINTENANCE MANUAL 32-12-03. 2 L 7 4 4F A20WE 1996080200447 19960802 00447 NM 1996 8 2 P5CA9600408 1 19960727 A 5247 BRACKETS BOEING 747 747122 1384872 NM APU LT DOOR BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 APU LEFT DOOR FORWARD AND AFT FIRE DETECTOR ELEMENT BRACKETS BROKE OFF DOOR. REPAIRED PER BOEING SRM 51-40-03. 2 L 7 4 4F A20WE 1996080200448 19960802 00448 NM 1996 8 2 P5CA9600409 1 19960730 A 5411 FRAME BOEING 747 747123 1384873 NM NR 3 PYLON CHAFED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 3 PYLON UPPER LINK CHAFED AT 12:00 O'CLOCK POSITION. REMOVED DAMAGE AND SHOT PEENED SURFACE, TREATED DEPTH .021 INCH WITHIN LIMITS PER BOEING SRM 54-40-01. 2 L 7 4 4F A20WE 1996080200449 19960802 00449 NM 1996 8 2 P5CA9600410 1 19960730 A 5414 SKIN BOEING 747 747123 1384873 NM NR 3 PYLON GOUGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 3 PYLON GOUGED BY ENGINE SIDE COWL ON LEFT SIDE. REPAIRED PER BOEING SRM 54-30-03. 2 L 7 4 4F A20WE 1996080200450 19960802 00450 NM 1996 8 2 P5CA9600411 1 19960730 A 5414 SKIN BOEING 747 747123 1384873 NM NR 3 PYLON WORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 3 PYLON WORN WHERE HIT BY SIDE COWLING. BLENDED AREA PER BOEING SRM 54-10-01. 2 L 7 4 4F A20WE 1996080200451 19960802 00451 NM 1996 8 2 P5CA9600412 1 19960730 A 5414 SKIN BOEING 747 747123 1384873 NM NR 3 PYLON WORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 3 PYLON RIGHT SIDE RIVETS PULLED THROUGH SKIN. REPLACED RIVETS PER BOEING SRM 51-30-02. 2 L 7 4 4F A20WE 1996080200452 19960802 00452 NM 1996 8 2 P5CA9600413 1 19960730 A 5280 DOOR BOEING 747 747123 1384873 NM RT MLG CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LEVEL 1 CORROSION ON AFT EDGE OF RIGHT BODY GEAR OUTBOARD DOOR. REMOVED CORROSION, TREATED AND FOUND WITHIN LIMITS PER BOEING SRM 51-10-01. 2 L 7 4 4F A20WE 1996080200453 19960802 00453 NM 1996 8 2 P5CA9600414 1 19960730 A 5280 DOOR BOEING 747 747123 1384873 NM RT MLG CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LEVEL 1 CORROSION AT TRAILING EDGE RIGHT BODY GEAR INBOARD WHEELWELL DOOR. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01. 2 L 7 4 4F A20WE 1996080200454 19960802 00454 NM 1996 8 2 QXEA9600265 1 19960726 A 5730 85700001007 PLATE DHAV DHC8 DHC8102 2809003 NM PANEL 521AT CORROSION A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 812PH 26 PDX - FRETTING CORROSION FOUND ON LADDER PLATE 521AT AND MOUNTING SURFACE OF PLATE 521AT DURING TASK 522. BLENDED I/A/W EA 9-57-85. CORROSION DEPTH UNDER 0.011 INCH. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1996080200455 19960802 00455 NM 1996 8 2 QXEA9600266 1 19960726 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 811PH 23 SEA - SOME OF THE EMERGENCY LIGHTS WERE NOTED AS BEING DIM. POWER SUPPLY PS1 REPLACED AND LIGHTS OPS CHECKED GOOD. AIR CRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1996080200456 19960802 00456 EU 1996 8 2 QXEA960267 1 19960727 A 3350 6008903 POWER SUPPLY FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 493US 11161 PDX - FORWARD HALF OF CABIN EVACUATION LIGHTS INOPERATIVE. POWER SUPPLY NRS 2 AND 3 REPLACED AND LIGHTS OPS CHECKED GOO D. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996080200457 19960802 00457 SO 1996 8 2 SWIA95750 1 19960717 A 3230 12038594001 CONTROL UNIT EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LANDING GEAR MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 204SW 120243 RAISED GEAR HANDLE AFTER TAKEOFF AND GEAR DID NOT RETRACT. RED LIGHTS CAME ON (UPPER LEFT ONE CAME ON AND THEN WENT OUT) . GREEN STAYED. CYCLED GEAR HANDLE DOWN. RED LIGHTS WENT OUT. PLACED HANDLE UP AGAIN WITH SAME RESULTS. ONE MORE AT TEMPT, SAME RESULT. RETURNED FOR LANDING. JACKED AIRCRAFT AND CYCLED GEAR SEVERAL TIMES. LANDING GEAR RETRACTED AND E XTENDED NORMALLY EVERY TIME AND INDICATED CORRECTLY. REPLACED LANDING GEAR CONTROL MODULE. CYCLED GEAR SEVERAL TIMES A ND OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1996080200458 19960802 00458 SO 1996 8 2 SWIA95751 1 19960718 A 3297 WIRE HARNESS EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT MLG FAILED A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 204SW 120243 RAISED LANDING GEAR AFTER TAKEOFF AND EXPERIENCED EXACT SAME SITUATION AS OCCURRED ON 7/17/96. RAISED GEAR HANDLE AFTER TAKEOFF AND GEAR DID NOT RETRACT. RED LIGHTS CAME ON (UPPER LT ONE CAME ON AND THEN WENT OUT). GREEN STAYED. CYCLED AND SAME PROBLEM. REPLACED LEFT MAIN LANDING GEAR AND WIRE HARNESS AND SENSOR. REPLACED, ADJUSTED AND SECURED PER EMB MM 32-61-00. OPS CHECKED SEVERAL TIMES AND OPS CHECK GOOD ON GROUND WITH NO PROBLEMS. 2 L 7 2 4T 4 T RT A31SO E20NE 1996080200459 19960802 00459 SW 1996 8 2 SWIA95752 1 19960724 A 3213 STRUT SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP LT MLG WORN A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 26974 AC664 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. INSPECTION OF AIRCRAFT DETECTED A FAULTY OUTBOARD GEAR SWITCH. REPLACED AND ADJUSTED PER 32-00-00, THE LEFT MAIN LANDING GEAR STRUT WAS IN NEED OF REBUILDING. REPLACED THE STRUT SEALS AND INS PECTED AIRCRAFT LANDING GEAR. SYSTEM OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A8SW E4WE 1996080200460 19960802 00460 EU 1996 8 2 WWMA9600059 1 19960727 A 3260 9005EN38 SWITCH BAG JETSTM JETSTM3201 1500217 EU NLG OUT OF ADJUST A WWMA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 WP 15 948AE 948 THE NOSE GEAR UNLOCKED LIGHT ILLUMINATED AND REMAINED ON. MAINTENANCE ADJUSTED THE NOSE GEAR DOWNLOCK SWITCH AND PERFOR MED GEAR SWINGS. THE AIRCRAFT WAS RELEASED FOR SERVICE WITH NO FURTHER PROBLEMS. 2 L 7 2 4T RT A56EU 1996080200529 19960802 00529 NM 1996 8 2 9616302716 1 19960730 A 7931 CONNECTOR BOEING 727 7272S7 138407Z NM PWA JT8 JT8D17 52049 NE NR 3 ENGINE DIRTY A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 720RC 22491 655285 DURING TAKEOFF, THE NR 3 ENGINE OIL PRESSURE WAS 20 PSI. CREW ABORTED TAKEOFF. MAINTENANCE CLEANED CONNECTOR ON THE NR 3 ENGINE OIL PRESSURE INDICATOR. OPERATIONAL CHECK OK. 2 L 7 3 4F 4 F A3WE E2EA 1996080200530 19960802 00530 NM 1996 8 2 9616312285 1 19960728 A 3350 900835A BATTERY BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 285US 21324 DURING LINE CHECK, FOUND THAT THE AFT EMERGENCY AISLE EXIT SIGN WAS INOPERATIVE. REPLACED THE BATTERY PACK. CHECKED OK . 2 L 7 3 4F A3WE 1996080200531 19960802 00531 NM 1996 8 2 9616322292 1 19960729 A 3350 BATTERY BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 292US 21503 DURING LINE CHECK, FOUND THAT THE RIGHT OVERWING EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE BATTERY PACK AND POWER S UPPLY. CHECKED OK. 2 L 7 3 4F A3WE 1996080200532 19960802 00532 NM 1996 8 2 96FDEA01209 1 19960702 A 5320 CTR POST BOEING 727 72725C 138400H NM COCKPIT DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 116FE 19298 FUSE CENTER POST BETWEEN PILOT AND COPILOT NR 1 WINDOWS CRACKED RIGHT 3RD SCREW DOWN, PILOTS NR 4 WINDOW. NDT VERIFIED NO CRACK FOUND WITH HFEC. 2 L 7 3 4F A3WE 1996080200533 19960802 00533 NM 1996 8 2 96FDEA01300 1 19960730 A 5330 651821950 SKIN BOEING 727 72722 1384002 NM BS 360-440 LIGHTNING STRIKE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 NR 0100 044. BS 360 - 440, WL 160, STR 24-26R, THERE ARE SEVERAL LIGHTNING STRIKES (MARKED). ****S/D**** REPAIRED L IGHTNING STRIKES PER FEDEX SRM 53-30-3, FIG 20 AT BS 360 - 440, WL 160, STR 24-26R. 2 L 7 3 4F A3WE 1996080200534 19960802 00534 NM 1996 8 2 96FDEA01301 1 19960730 A 5330 65182151 SKIN BOEING 727 72722 1384002 NM BS 520 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 195FE 19144 NR0171 009. BS 520, STR 25, RBL 30, THERE IS A CRACK IN SKIN. ****S/D**** MECHANICALLY REMOVED CRACK IN SKIN LOCATED AT BS 520, STR 25R, RBL 30. REPAIRED SKIN PER FEDEX EA 7-5310-29202. 2 L 7 3 4F A3WE 1996080200535 19960802 00535 NM 1996 8 2 96FDEA01302 1 19960702 A 5320 CASTING BOEING 727 72725C 138400H NM BS 870 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 116FE 19298 UPPER LOBE MAIN CARGO STA 870 CASTING WL 190 LT HFEC INDICATES CRACK, AREA MARKED. CUT OUT CORROSION AND CRACK PER EA , INSTALLED REPAIR FITTING IAW EA 7-5310-28783. 2 L 7 3 4F A3WE 1996080200536 19960802 00536 NM 1996 8 2 96FDEA1298 1 19960730 A 5320 6586358140 DOORWAY FRAME BOEING 727 7272D4 138407U NM BS 848.95 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 NR 0419 005. RIGHT AFT EMERGENCY EXIT DOORWAY AFT FRAME IS GOUGED 1.5 INCHES LONG AT BS 848.95 RBL 69.5 WL 234 GOUG E IS IN RADIUS. REWORKED GOUGED AREA OF RT AFT EMERGENCY EXIT DOORWAY FRAME IAW FEDEX EA 7-5310-29767. 2 L 7 3 4F A3WE 1996080200537 19960802 00537 NM 1996 8 2 96UAL900533 1 19960715 A 5310 STRUCTURE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE BS 340-450 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7289U 21567 THE RT FUSELAGE BETWEEN B.S. 340 AND 450 WAS DAMAGED WHEN THE TOW TRACTOR PULLING THE PLANE JACK-KNIFED AND THE AIRPLANE RAN OVER THE TRACTOR. THE DAMAGE INVOLVED TORN SKIN, SEVERED FRAMES, DAMAGED STRINGERS, AND MISCELLANEOUS DAMAGE TO IN TERNAL BRACKETS, INTERCOSTALS, ETC. CAUSED BY JACK-KNIFED TRACTOR. ALL DAMAGED PARTS WERE EITHER REPLACED WITH NEW PAR TS OR REPAIRED PER THE APPLICABLE SRM. 2 L 7 3 4F 4 F A3WE E2EA 1996080200538 19960802 00538 NM 1996 8 2 96UAL900559 1 19960722 A 3350 M10699 BATTERY PACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 577UA 26693 EMERGENCY ESCAPE FLOOR LIGHTING INOPERATIVE. FINAL 10 FEET IN AFT SECTION. REPLACE EMERGENCY ESCAPE LIGHTING BATTERY P ACK. OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996080200539 19960802 00539 NE 1996 8 2 96UAL900560 2 19960722 A 7200 ENGINE HAMSTD MR732336 BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 LOST POWER A UALA E ENGINE SHUTDOWN Y J ENGINE STOPPAGE WARNING INDICATION AP APPROACH 1 WP 29 559UA A4460 26657 LOST POWER ON NR 1 ENGINE DURING APPROACH TO ORD. ENGINE INDICATIONS AND CREW ALERT SYSTEM (EICAS) SHOWED TWO HARD FAUL TS AGAINST THE FUEL CONTROL UNIT (FCU). ENGINEERING CONDUCTED AN AS RECEIVED ON THE FUEL CONTROL UNIT, BUT DID NOT FIND ANY MAJOR DEFECTS. THE ROOT CAUSE OF THE IN-FLIGHT SHUTDOWN IS UNDETERMINED. THE FUEL CONTROL UNIT WAS NOT A CONTRIBUT ING FACTOR. 2 L 7 2 4F 4 F RT A2NM E17NE 1996080200540 19960802 00540 NM 1996 8 2 96UAL900561 1 19960722 A 3231 141N093552 CONTROL ROD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NLG DOOR FAILED A UALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 29 531UA 25042 DURING GEAR RETRACTION, HEARD LOUD GEAR DOOR NOISE ACCOMPANIED WITH VIBRATION. RETURNED TO FIELD. NOSE LANDING GEAR DO OR CONTROL ROD FRACTURED DURING GEAR RETRACTION. REPLACE ROD WITH NEW ROD. OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996080200541 19960802 00541 NM 1996 8 2 96UAL900562 1 19960722 A 2150 BACD40D441342 SLEEVE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE AIR COND BAY CUT A UALA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 777UA 26916 AIRCRAFT LOST PRESSURIZATION. CABIN ALTITUDE WENT TO 10,000 FEET WHEN CRUISING AT 37,000 FEET. DESCENDED TO 22,000 FEE T AND CABIN ALTITUDE RECOVERED TO NORMAL. AIRCRAFT DIVERTED TO GANDER, NEWFOUNDLAND. SUPPLEMENTAL DATA UPDATE: CLAMP S AND SLEEVE UPSTREAM OF RIGHT PACK AIR CONDITIONING CHECK VALVE WERE FOUND LOOSE. IN ADDITION, A 4.5 INCH LONG CIRCUMF ERENTIAL CUT WAS FOUND ON THE CORRESPONDING SLEEVE ON THE LEFT PACK SYSTEM. 2 L 7 2 4F 4 F RT T0001SE E46NE 1996080200542 19960802 00542 NM 1996 8 2 96UAL900563 1 19960722 A 3350 20131 BATTERY BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN DISCHARGED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 908UA 25008 FIRST CLASS EMERGENCY ESCAPE PATH LIGHTING INOP AND EMERGENCY EXIT LIGHT INOP AT DOOR ONE RIGHT. *S/D* REPLACED BATTER Y PACK, CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1996080200543 19960802 00543 NE 1996 8 2 96UAL900564 2 19960723 A 7230 COMPRESSOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ENGINE STALLED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 WP 29 190UA 24700 26879 724700 45 SECONDS AFTER TAKEOFF, POWER APPLIED, EXPERIENCED 2 RAPID COMPRESSOR STALLS WITH MAX EPR. IDLED ENGINE FOR ONE MINUT E AND THEN SHUT IT DOWN. RETURNED TO FIELD. ENGINE WAS REPLACED. CAUSE OF COMPRESSOR STALLS WAS GENERAL DETERIORATION OF THE HIGH PRESSURE COMPRESSOR WHICH IN TURN CAUSED LOSS OF SURGE MARGIN. 2 L 7 4 4F 4 F RT A20WE E24NE 1996080200544 19960802 00544 EU 1996 8 2 96UAL900565 1 19960723 A 2710 SERVO CONTROL MR27145 AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LT AILERON LEAKING A UALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 425UA 1993 508 LANDED UNDER AMBER ALERT AT IAD DUE TO LOSS OF HYDRAULIC PRESSURE. *S/D* FOUND LEFT OUTBOARD AILERON SERVO CONTROL LEA KING. REPLACED SERVO CONTROL AND OPERATIONALLY CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 1996080200545 19960802 00545 NM 1996 8 2 96UAL900566 1 19960723 A 3411 PITOT TUBE BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE RIGHT PLUGGED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 WP 29 4727U 19883 FIRST OFFICER'S AIRSPEED INDICATOR INOPERATIVE. READS ZERO ALL THE TIME. ABORTED TAKEOFF AT 100 KNOTS. PROBLEM CAUSE D BY BLOCKED PITOT INPUT. SOURCE OF BLOCKAGE CANNOT BE DETERMINED; HOWEVER, MATERIAL REMOVED FROM PROBE WAS MOST LIKELY A CARBONIZED INSECT. NO COMPONENT FAILURE. 2 L 7 4 4F 4 F A20WE E20EA 1996080200546 19960802 00546 NM 1996 8 2 96UAL900567 1 19960723 A 2820 69186127 FUEL VENT TUBE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 FUEL TANK CRACKED A UALA O OTHER O OTHER CR CRUISE 1 WP 29 7286U 21564 THE NR 1 FUEL QUANTITY GUAGE DECREASED BY 700 POUNDS WHILE CROSS FEEDING FROM NR 2, ALL CROSS FEEDS OPEN. *S/D* FOUND NR 1 FUEL VENT TUBE CRACKED AND IN PRELOAD. REPLACED VENT TUBE, RECLAMPED AND RESHIMMED. 2 L 7 3 4F 4 F A3WE E2EA 1996080200547 19960802 00547 NM 1996 8 2 96UAL900568 1 19960723 A 2820 69186128 FUEL VENT TUBE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 FUEL TANK CRACKED A UALA O OTHER O OTHER CR CRUISE 1 WP 29 7462U 21916 NR 3 FUEL QUANTITY LOST 700 POUNDS WHILE CROSS FEEDING FROM NR 2. *S/D* REPLACED FUEL VENT TUBE IN NR 3 TANK. 2 L 7 3 4F 4 F A3WE E2EA 1996080200549 19960802 00549 NM 1996 8 2 96UAL900570 1 19960724 A 2170 HUMIDIFIER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE COCKPIT FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 178UA 24385 SHORTLY AFTER LEVEL OFF AT CRUISE ALTITUDE, SMOKE APPEARED IN COCKPIT. SMOKE CEASED AFTER LOWER RECIRCULATION FAN SWITC HED OFF. CAUSE UNKNOWN. COULD NOT DUPLICATE CONDITION ON GROUND. HUMIDIFIER WAS REPLACED AS A PRECAUTION. 2 L 7 4 4F 4 F RT A20WE E24NE 1996080200550 19960802 00550 NM 1996 8 2 96UAL900571 1 19960725 A 5330 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE BS 1050 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7460U 21914 AFT LOWER FUSELAGE AFT OF AFT VHF ANTENNA RT SIDE HAS BULGE, A SMALL BUBBLE AND CRACK. SUPPLEMENTAL DATA UPDATE: DISC REPANCY CONFIRMED TO BE CORROSION IN FUSELAGE SKIN AND STRINGER IN TWO PLACES: BS 1050 AT S-28L AND BS 1050 AT 28R. SK IN REPAIRED PER 53-30-3, FIGURE 3. STRINGERS REPAIRED PER SRM 53-10-3, FIGURE 1. 2 L 7 3 4F 4 F A3WE E2EA 1996080200551 19960802 00551 NM 1996 8 2 96UAL900572 1 19960725 A 3260 NAS52965 LINKAGE RIVET BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NLG POS SWITCH SHEARED A UALA O OTHER N FALSE WARNING LD LANDING 1 WP 29 7442U 21896 NOSE GEAR WOULD NOT LOCK DOWN. CRANKED GEAR DOWN MANUALLY AND HAD NORMAL LANDING. DID NOT GET GREEN NOSE GEAR LIGHT, R ED LIGHT STAYED ON. *S/D* FOUND NOSE LANDING GEAR POSITION SWITCH LINKAGE RIVET SHEARED AND LINKAGE BENT. REPLACED PO SITION SWITCH AND LINKAGE. JACKED AIRCRAFT AND OPERATED NLG SEVERAL TIMES. ALSO, TESTED NLG MANUAL EXTENSION SYSTEM, A LL OPERATIONS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1996080200552 19960802 00552 NM 1996 8 2 96UAL900573 1 19960725 A 2781 H1010261 SWITCH BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 2 LE FLAP OUT OF ADJUST A UALA O OTHER O OTHER CR CRUISE 1 WP 29 7286U 21564 UNPLANNED STOP SFO DUE TO LEADING EDGE FLAP TRANSIT LIGHT ON. *S/D* ADJUSTED NR 2 LEADING EDGE FLAP SWITCH, OPERATIONA L CHECK GOOD. 2 L 7 3 4F 4 F A3WE E2EA 1996080200553 19960802 00553 1996 8 2 96UAL900574 4 19960725 A 2565 SLIDE AIRCRUISERS D29835103 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7449U 17447378 21903 DURING SHOP OVERHAUL OF SLIDE REMOVED FOR OVERHAUL TIME EXPIRATION INFLATABLE PORTION DEVELOPED A 3 INCH SEAM LEAK ON TH E TUBE, APPROXIMATELY 4 FEET FROM THE TOE END OF THE UNIT. SCRAPPED SLIDE. 2 L 7 3 4F 4 F A3WE E2EA 1996080200554 19960802 00554 NM 1996 8 2 96UAL900575 1 19960726 A 2781 834403 PROX SENSOR BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE NR 8 LE SLAT OUT OF ADJUST A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 608UA 21869 AIRCRAFT RETURNED TO THE FIELD AT MIA DUE TO A LEADING EDGE SLAT ASYMMETRY MESSAGE. *S/D* THE LEADING EDGE SLAT ASYMME TRY MESSAGE WAS CAUSED BY AN OUT OF LIMIT SENSOR TO TARGET GAP CONDITION ON NUMBER 8 SLAT OUTBOARD PROXIMITY SENSOR S298 . THE SENSOR TO TARGET GAP WAS ADJUSTED PER MM 27-88-01, OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 1996080200555 19960802 00555 NE 1996 8 2 ABXA9600602 2 19960729 A 7200 ENGINE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7B 52053 NE LEFT DEFECTIVE A ABXA A UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 GL 23 941AX 42218 1510 47419 653710 AFTER 23 MINUTES OF FLIGHT, LEFT ENGINE FLAMED OUT. ATTEMPTED RESTART TO NO AVAIL. DECLARED EMERGENCY AND LANDED AT PIT WITHOUT FURTHER INCIDENT. REPLACED NR 1 ENGINE IAW MIP WORK CARD J7001. PART TOTAL CYCLES, 34,936. 2 L 7 2 4F 4 F A6WE E2EA 1996080200556 19960802 00556 WP 1996 8 2 ABXA9600603 1 19960730 A 3230 RETRACT MECH DOUG DC8 DC863 302198A WP LANDING GEAR MALFUNCTIONED A ABXA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 23 815AX 46097 DURING APPROACH WHEN LANDING GEAR HANDLE WAS LOWERED, GEAR STAYED UP. EXECUTED MISSED APPROACH. ON 2ND APPROACH, RECYC LED GEAR AND GEAR CAME DOWN NORMALLY WITH NORMAL INDICATION. PERFORMED ADJUSTMENT TEST IAW DC8 M.M. 32-30-0. OPS CHECK GOOD NUMEROUS TIMES. 2 L 7 4 4F 4A25 1996080200557 19960802 00557 WP 1996 8 2 ABXA9600604 1 19960730 A 3350 5708458503 POWER SUPPLY DOUG DC8 DC863 302198A WP CABIN DEFECTIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 826AX 46061 EMERGENCY LIGHTING TEST FAILED. REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY IAW DC8 M.M. 33-50-2. OPS CHECK GOOD. 2 L 7 4 4F 4A25 1996080200558 19960802 00558 WP 1996 8 2 CALA9601101 1 19960709 A 5350 LATCHES DOUG DC9 DC982 3022082 WP TAILCONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16887 49116 THE FORCE REQUIRED TO DROP TAILCONE USING THE INTERIOR RELEASE HANDLE AND AFT ENTRANCE DOOR RELEASE HANDLE WAS EXCESSIVE . THE TAILCONE LATCHES WERE ADJUSTED IAW MM 53-53-00. 2 L 7 2 4F A6WE 1996080200559 19960802 00559 WP 1996 8 2 CALA9601102 1 19960725 A 5350 CLIPS DOUG DC9 DC982 3022082 WP TAILCONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16887 49116 THE FORCE REQUIRED TO PULL INTERIOR AND EXTERIOR TAILCONE RELEASE HANDLES OUT OF CLIPS WAS EXCESSIVE. THE CLIPS WERE AD JUSTED IAW MM 53-53-00. 2 L 7 2 4F A6WE 1996080200560 19960802 00560 NM 1996 8 2 CALA9601103 1 19960725 A 5320 WEB BOEING 737 7372C0 1384488 NM BS 675 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14241 20070 INSPECTION FOUND A 1.5 INCH CRACK IN PRESSURE WEB AT STA 675, BL ZERO TO LBL 1.5. THE CRACKED WEB AREA WAS REMOVED AND A NEW SECTION OF WEB WAS INSTALLED IAW ECRA 5710-01748. 2 L 7 2 4F A16WE 1996080200561 19960802 00561 NM 1996 8 2 CALA9601104 1 19960725 A 5315 FLOOR BEAM BOEING 737 7372C0 1384488 NM BS 675/685 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14241 20070 INSPECTION FOUND A 2 INCH CRACK IN FLOORBEAM LOWER T-CHORD AT STA 675, BBL ZERO AND A 2 INCH CRACK WAS ALSO FOUND IN CHO RD AT STA 685, BBL ZERO. A REPAIR AT STA 675 WAS PERFORMED IAW BOEING DRAWING 65C17173. A REPAIR ANGLE WAS INSTALLED A T STA 685 IAW ECRA 5710-01746. 2 L 7 2 4F A16WE 1996080200562 19960802 00562 NM 1996 8 2 CALA9601105 1 19960725 A 5330 SKIN BOEING 737 7372C0 1384488 NM BS 259 BULGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14241 20070 INSPECTION FOUND FUSELAGE SKIN BULGED AT STA 259, STRINGER 24L. THE BULGED AREA WAS REMOVED. A FILLER AND DOUBLER REPA IR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. 2 L 7 2 4F A16WE 1996080200563 19960802 00563 NM 1996 8 2 CALA9601106 1 19960717 A 3350 BATTERY PACK BOEING 737 7372C0 1384488 NM CABIN DISCHARGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14241 20070 INSPECTION FOUND THE R-2 DOOR SLIDE LIGHT INOPERATIVE. THE BATTERY PACK WAS REPLACED AND THE LANYARD SWITCH WAS CLEANED . THE LIGHT TESTED GOOD IAW MM 33-51-0. 2 L 7 2 4F A16WE 1996080200564 19960802 00564 1996 8 2 DHL722004 4 19960730 A 3421 158663A VERT GYRO BOEING 727 727228 NM NR 2 INOPERATIVE A T DHLA A UNSCHED LANDING O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 NR 2 VERTICAL GYRO INOPERATIVE. REMOVED AND REPLACED GYRO. OPS CHECK OK PER MM 34-22-21. 2 L 7 3 4F A3WE 1996080200565 19960802 00565 WP 1996 8 2 MWEA96272 1 19960729 A 3030 851AK PITOT HEAT DOUG DC9 DC932 3022066 WP FWD FUSELAGE INOPERATIVE A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 207ME 47794 PILOT REPORTS ON CLIMB-OUT OF MKE, CAPT. PITOT HEAT FAILED. RETURNED TO MKE. REPLACED CAPT. PITOT TUBE. OPS CHECK GOO D. RETURNED A/C TO SERVICE. 2 L 7 2 4F A6WE 1996080200566 19960802 00566 NM 1996 8 2 P5CA9600415 1 19960731 A 5720 HILOCK FASTENER BOEING 747 747122 1384872 NM RT WING HEAD SHEARED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 HEAD SHEARED ON HILOCK RIGHT WING AFT SPAR, LOWER CHORD, JUST OUTBOARD OF WING GEAR AFT TRUNNION. REPLACED HILOCK PER B OEING SRM 51-10-01. 2 L 7 4 4F A20WE 1996080200567 19960802 00567 NM 1996 8 2 P5CA9600416 1 19960730 A 5512 WEDGE BOEING 747 747123 1384873 NM LT HORIZ STAB LOOSE FASTENERS A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LOOSE TRAILING EDGE WEDGE ON LEFT OUTBOARD HORIZONTAL STABILIZER BOTTOM AND TOP. REPLACED FASTENERS PER BOEING SRM 51-3 0-02. 2 L 7 4 4F A20WE 1996080200568 19960802 00568 1996 8 2 P5CA9600417 4 19960730 A 2360 STATIC WICK BOEING 747 747123 1384873 NM LT ELEVATOR LOOSE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 BASE LOOSE ON INBOARD STATIC WICK LEFT OUTBOARD ELEVATOR. REMOVED AND REPLACED FASTENERS PER BOEING SRM 51-30-02. 2 L 7 4 4F A20WE 1996080200569 19960802 00569 GL 1996 8 2 SRAA960709 2 19960730 A 7200 ENGINE LKHEED 382 382E 526413U SO ALLSN 501D 501D22A 03006 GL NR 4 RPM FLUX A SRAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 23 923SJ 4301 ON TAKEOFF ROLL FOR FLIGHT 1205 OUT OF COF, NR 4 ENGINE HAD 2 PERCENT RPM FLUX WITH ALL OTHER PARAMETERS FLUXING ALSO, R EJECTED TAKEOFF WITHOUT FURTHER INCIDENT. 2 H 7 4 4T 4 T A1SO E282 1996080200570 19960802 00570 NM 1996 8 2 UPS96520677 1 19960731 A 3350 BPS73 POWER SUPPLY BOEING 757 75724APF 1384969 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 422UP 25324 INSPECTION TYPE N/A, EMER EXIT LIGHTS DO NOT ILLUMINATE WHEN TURNED ON. REMOVED, REPLACED AND TESTED EMER EXIT LIGHT PW R SUPPLY PER MM 33-51-07. 2 L 7 2 4F RT A2NM 1996080200571 19960802 00571 WP 1996 8 2 UPS96820666 1 19960725 A 3211 ATTACH STUD DOUG DC8 DC873F 302199F WP LT MLG SHEARED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE: DLY. LEFT MLG DOWNLOCK ACTUATOR GEAR ATTACH STUD SHEARED (EXTEND-RETRACT) D113074. TRANSFERRED TO N RC 352009/009N. FABRICATED BUSHING AND INSTALLED BUSHING AND NEW STUD PER XEA-X8-32-1063. REINSTALLED ACTUATOR, ADJUSTE D. OPS CK OK PER M/M 32-32-02. 2 L 7 4 4F RT 4A25 1996080200572 19960802 00572 WP 1996 8 2 UPS96820669 1 19960710 A 5320 SHEAR TIE DOUG DC8 DC871F 302199D WP BS 1600 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-D, SHEAR TIE CRACKED AT FS 1600 BETWEEN LONGERONS 31R AND 30R. REPAIRED SHEAR TIE PER SRM 53-2-0, FIG 2 B. 2 L 7 4 4F RT 4A25 1996080200573 19960802 00573 WP 1996 8 2 UPS96820670 1 19960626 A 5511 RIBS DOUG DC8 DC871F 302199D WP LT HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-D, 3 LOWER RIBS CRACKED ON LT HORIZONTAL STABILIZER LEADING EDGE AT STA XRS35 INBD, XRS29 INBD AND XRS11 2 INBD UPPER RIBS. REPAIRED RIBS PER SRM 55-2-0. 2 L 7 4 4F RT 4A25 1996080200574 19960802 00574 WP 1996 8 2 UPS96820671 1 19960626 A 5511 RIBS DOUG DC8 DC871F 302199D WP LT HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-D, 2 LOWER RIBS ON LT HORIZONTAL STABILIZER LEADING EDGE ARE CRACKED AT STA XRS35 INBD AND XRS29 INBD. R EPAIRED RIBS PER SRM 55-2-0. 2 L 7 4 4F RT 4A25 1996080200575 19960802 00575 WP 1996 8 2 UPS96820672 1 19960701 A 5312 BULKHEAD FTG DOUG DC8 DC871F 302199D WP BS 1800 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-D, BOTH ATTACHMENT FITTINGS TO CANTED BULKHEAD STRUCTURE ARE CRACKED AT FS 1800 LBL AND RBL 9. REPAIRED FITTINGS PER SRM 53-2-0, FIG 1B. 2 L 7 4 4F RT 4A25 1996080200576 19960802 00576 WP 1996 8 2 UPS96820673 1 19960626 A 5712 5770123 RIBS DOUG DC8 DC871F 302199D WP RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-D, RT WING LEADING EDGE HAS 8 RIBS CRACKED AT STA XFS628, XFS616, XFS660, XFS660 LOWER, XFS666, XFS735, XFS800 AND XFS806. REPAIRED RIBS PER SRM 57-2-0 AND MM 57-00-00 FIG 801. 2 L 7 4 4F RT 4A25 1996080200577 19960802 00577 WP 1996 8 2 UPS96820674 1 19960710 A 5320 SHEAR TIE DOUG DC8 DC871F 302199D WP BS 1600 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-D, SHEAR TIE CRACKED AT FS 1600 BETWEEN LONGERONS 26R AND 27R. REPAIRED SHEAR TIE PER SRM 53-2-0, FIG 2 A. 2 L 7 4 4F RT 4A25 1996080200578 19960802 00578 WP 1996 8 2 UPS96820675 1 19960626 A 5712 5770123 RIBS DOUG DC8 DC871F 302199D WP RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-D, 4 RIBS CRACKED ON LEADING EDGE RT WING UPPER AT STA XFS560, XFS5 72, XFS578 AND XFS610. REPAIRED RIB S PER SRM 57-2-0 AND MM 57-00-00 FIG 801. 2 L 7 4 4F RT 4A25 1996080200579 19960802 00579 WP 1996 8 2 UPS96820676 1 19960627 A 5511 RIBS DOUG DC8 DC871F 302199D WP RT HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-D, 2 RT HORIZONTAL STABILIZER LEADING EDGE LOWER RIBS CRACKED AT STA XRS82 AND XRS111. REPAIRED RIBS PE R SRM 55-2-0. 2 L 7 4 4F RT 4A25 1996080200580 19960802 00580 NM 1996 8 2 VNAA9607008 1 19960721 A 3260 INTRANSIT LIGHT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LANDING GEAR ILLUMINATED A VNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 427JS 3039 AFTER TAKEOFF FROM DCA EN ROUTE TO CHS, CREW REPORTED THE NOSE LANDING GEAR INTRANSIT LIGHT WOULD NOT EXTINGUISH. CREW WAS ADVISED TO DIVERT TO PIT. AIRCRAFT LANDED IN PIT WITHOUT FURTHER INCIDENT. MX INSPECTED AIRCRAFT AND CONDUCTED GRO UND CHECKS I.A.W. M.M. 32-21-01. NO DEFECTS NOTED. MX UNABLE TO DUPLICATE THE DISCREPANCY, AIRCRAFT RETURNED TO SERVIC E. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996080500001 19960805 00001 NM 1996 8 5 AALA960856 1 19960601 A 3350 P2010031303 LIGHT BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 658AA 24616 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT SIDE MARKER LIGHT AT DOOR 2R INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT SIDE MARKER LIGHT AT DOOR 2R. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1996080600003 19960806 00003 WP 1996 8 6 96ZZZX3654 1 19960613 A 2424 51511003 GCU LKHEED 1011 10113851 5265010 WP NR 1 ENGINE DEFECTIVE A RIAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 SO 19 302MB 193A1129 ON RIA FLT 118 - SFO/BOS - 2.25 HOURS INTO FLIGHT, AIRCRAFT DIVERTED TO LAS DUE TO NR 1 AND NR 3 GENERATORS INOPERATIVE IN-FLIGHT. NO FREQUENCY OR VOLTAGE IN EITHER ONE. BOTH GENERATORS HAD PMG ON GROUND AT LAST MAINTENANCE. REMOVED AND REPLACED NR 1 ENGINE GCU - OPS CHECKED NORMAL IAW MM 24-20-00. FOUND NR 3 IDG OVERSERVICED (OIL). SERVICED TO CORRECT LEVEL, RAN ENGINE AND PERFORMED COMPLETE AC GENERATION ADJUSTMENT AND TEST, OPS CKS NORMAL, IAW MM 24-20-00. AIRCRAFT R ELEASED TO SERVICE. (X) 2 L 7 3 4F A23WE 1996080600004 19960806 00004 NE 1996 8 6 96ZZZX3657 2 19960329 A 8520 CASE BEECH 18 E18S 1151006 CE PWA R985 R985AN14B 52008 NE LEFT ENGINE CRACKED A GGPA K NONE K FLUID LOSS TX TAXI/GRND HDL 1 NM 01 9001 6813 1273 BA460 226551 LEFT ENGINE OIL LEAK. 1 L 7 2 3R 3 R A765 5E1 1996080600005 19960806 00005 CE 1996 8 6 96ZZZX3658 1 19960522 A 3260 UPLIMIT SWITCH BEECH 18 D18S 1151004 CE RT MLG SHORTED WIRE A OSYA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 354T A91 ON TAKEOFF, TOWER ADVISED THE PILOT THAT MAIN GEAR APPEARED TO BE NOT FULLY RETRACTED. PILOT COCKPIT INDICATION WAS BOT H LANDING GEAR WERE RETRACTED. AFTER CYCLING THE LANDING GEAR AND PLACING THE GEAR LEVER DOWN, INDICATION WAS RED (UP) AND GREEN (DOWN). PILOT PERFORMED EMERGENCY LANDING GEAR EXTENSION PROCEDURE. INDICATION WAS THE SAME, EMERGENCY WAS D ECLARED AND NORMAL LANDING WAS ACCOMPLISHED. FOUND SHORTED WIRE AT RIGHT WHEELWELL. GEAR OPERATIONALLY CHECKED. 1 L 7 2 3R A765 1996080600010 19960806 00010 NM 1996 8 6 UPS96420660 1 19960719 A 3350 CONTROL MODULE BOEING 747 747123 1384873 NM FLIGHT DECK INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE: W/E. EMERGENCY LIGHT DISARMED, INDICATOR LIGHT FAILED TO ILLUMINATE IN DISARM OR ARM POSITION. REMOV ED AND REPLACED EMERGENCY LIGHT CONTROL MODULE. 2 L 7 4 4F A20WE 1996080600012 19960806 00012 WP 1996 8 6 DLL14961741 1 19960720 A 2820 SIG CONDITIONER LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB211524B4 54555 NE NR 1 ENGINE MALFUNCTIONED A DALA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 SO 27 737D 49664 193C1228 014762 WHILE AT CRUISE JUST PRIOR TO DESCENT, NR 1 ENGINE FLAMED OUT, GRAVITY FEED FAILED TO KEEP UP WITH ENGINE NEEDS (TANK TO ENG). BOTH TANK PUMP LOW LIGHTS ILLUMINATED JUST BEFORE FLAMEOUT. RESTART AND SUBSEQUENT OPERATION WAS NORMAL. TANK 1 A TRANSFER VALVE ON MCO AND PLAC 28-27-02A. REPLACED SIGNAL CONDITIONER. OPS CHECK GOOD. 2 L 7 3 4F 4 F A23WE E12EU 1996080600013 19960806 00013 NM 1996 8 6 UPS96220662 1 19960724 A 3350 1000679 LIGHT BOEING 727 727185C 138406N NM FLIGHT CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 940UP 19826 CREW EMERGENCY EXIT LIGHT INOPERATIVE. DEAD BATTERY. REMOVED AND REPLACED EMERGENCY EXIT LITE ASSY IAW M/M 25-60-00, O PS CHECK NORMAL. 2 L 7 3 4F A3WE 1996080600014 19960806 00014 NM 1996 8 6 UPS96220663 1 19960724 A 3350 1000679 LIGHT BOEING 727 727185C 138406N NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 940UP 19826 COCKPIT EMERGENCY LIGHT INOPERATIVE. DEAD BATTERY. REMOVED AND REPLACED EMERERGENCY LIGHT ASSY IAW MM 256000. OPS CK NORMAL. 2 L 7 3 4F A3WE 1996080600015 19960806 00015 CE 1996 8 6 96ZZZM1178 1 19960614 A 3230 6046H39A RELAY BEECH 18 E18S 1151006 CE MLG FAILED A GGPA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NM 01 9001 112 BA460 YKM-BFI - THE MAIN LANDING GEAR CIRCUIT BREAKER POPPED. PILOT DIVERTED TO PAE MAINTENANCE BASE AND CRANKED GEAR DOWN. M AINTENANCE CREW FOUND THE LANDING GEAR RELAY BURNED UP. REPLACED RELAY AND GEAR RETRACTION PERFORMED. AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 3R A765 1996080600019 19960806 00019 NM 1996 8 6 DHL96701007 1 19960727 A 3260 IND LIGHT BOEING 727 72730C 1384009 NM LANDING GEAR MALFUNCTIONED A T DHLA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 01 701DH 19011 GREEN LIGHT WOULD NOT ILLUMINATE WHEN GEAR SELECTED DOWN, GEAR LIGHT WORKED AFTER CYCLING GEAR. PERFORMED LANDING GEAR LOCK AND POSITION INDICATION TEST PER MM 32-61-21, NO DEFECTS NOTED. 2 L 7 3 4F A3WE 1996080600020 19960806 00020 NM 1996 8 6 UPS96420678 1 19960712 A 2612 FIRE WARN BOEING 747 747123 1384873 NM CARGO COMPT MALFUNCTIONED A IPXA O OTHER N FALSE WARNING DE DESCENT 1 SO 01 675UP 20390 INSPECTION TYPE N/A, LOWER CARGO FIRE WARNING CAME ON 4 TO 5 TIMES ON DESCENT. 2 L 7 4 4F A20WE 1996080700001 19960807 00001 NM 1996 8 7 96FDEA01299 1 19960730 A 2750 6521631143 SKIN BOEING 727 7272D4 138407U NM LT TE FOREFLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 NR 0028, 004 LEFT WING O/B FOREFLAP I/B END HAS A LARGE DELAMINATED TEMPORARY REPAIR. *S/D* LEFT WING O/B FOREFLAP I/B END WAS REPAIRED PER FEDEX SRM 51-40-6. 2 L 7 3 4F A3WE 1996080800001 19960808 00001 NM 1996 8 8 9616332287 1 19960730 A 2933 B7111 QTY IND BOEING 727 727251 138408H NM COCKPIT MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 287US 32946 23264 21375 DURING CRUISE LEVEL FLIGHT, 'A' HYDRAULIC SYSTEM QUANTITY DECREASED STEADILY TO 1.6 GALLONS. AIRCRAFT DIVERTED TO GTF A ND LANDED WITHOUT INCIDENT. REPLACED HYDRAULIC QUANTITY INDICATOR AND PERFORMED SYSTEM LEAK CHECK. SYSTEM CHECKED OK. 2 L 7 3 4F A3WE 1996080800002 19960808 00002 WP 1996 8 8 9616349304 1 19960728 A 5241 SEAL DOUG DC9 DC982 3022082 WP GALLEY SVC DOOR FAILED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 931MC 48057 DURING CLIMB MSP-IND, A FLIGHT ATTENDANT HEARD A LOUD BANGING NOISE OUTSIDE OF THE AFT GALLEY SERVICE DOOR. RETURNED TO MSP WITHOUT FURTHER INCIDENT. REPLACED UPPER DOOR SEAL AND RETAINER. 2 L 7 2 4F A6WE 1996080800003 19960808 00003 WP 1996 8 8 9616359752 1 19960729 A 3350 SPLICE DOUG DC9 DC941 302207N WP CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 752NW 47116 DURING LINE CHECK, FOUND EMERGENCY EXIT FLOOR PROXIMITY LIGHTS INOPERATIVE FROM ROWS 6-12 DEF. REPLACED SPLICE BEHIND S IDEWALL-OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996080800004 19960808 00004 WP 1996 8 8 9616369882 1 19960730 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 670MC 47659 DURING LINE CHECK, FOUND EMERGENCY LIGHTS IN TAILCONE AREA AFT CABIN INOPERATIVE. REPLACED BATTERIES. OPERATIONAL CHEC K OK. 2 L 7 2 4F A6WE 1996080800005 19960808 00005 NM 1996 8 8 9616372285 1 19960728 A 3350 BATTERY PACK BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 285US 21324 DURING PREFLIGHT, FOUND AFT EMERGENCY AISLE EXIT SIGN INOPERATIVE ABOVE AFT LAVATORIES. REPLACED BATTERY PACK. CHECKED OK. 2 L 7 3 4F A3WE 1996080800006 19960808 00006 NM 1996 8 8 9616382289 1 19960731 A 3350 BATTERIES BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 289US 21377 DURING PREFLIGHT, FOUND EMERGENCY EXIT SIGN ABOVE LEFT AFT GALLEY SERVICE DOOR INOPERATIVE. REPLACED BATTERIES. CHECKE D OK. 2 L 7 3 4F A3WE 1996080800007 19960808 00007 WP 1996 8 8 9616399763 1 19960726 A 3260 ANNUNCIATOR MOD DOUG DC9 DC941 302207N WP COCKPIT FAILED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 763NW 47396 ON APPROACH, NOSE GEAR LIGHT FAILED TO ILLUMINATE THE FIRST TWO TIMES GEAR WAS LOWERED. ON THE THIRD ATTEMPT, ALL INDIC ATIONS WERE NORMAL. PROBLEM FOUND TO BE IN NOSE GEAR ANNUNCIATOR MODULE. CLEANED ANUNCIATOR, CHANGED BULB, AND SWUNG G EAR TEN TIMES. ALL GEAR POSITION INDICATIONS CHECK GOOD. 2 L 7 2 4F A6WE 1996080800008 19960808 00008 WP 1996 8 8 9616409858 1 19960731 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 767NC 47724 DURING LINE CHECK, FOUND OVERHEAD EMERGENCY LIGHTS INOPERATIVE ROWS 20-24. REPLACED BATTERIES IN POWER PACK. OPERATION AL CHECK OK. 2 L 7 2 4F A6WE 1996080800009 19960808 00009 WP 1996 8 8 9616419918 1 19960731 A 4970 TEMP SENSOR DOUG DC9 DC932 3022066 WP LT PACK MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 940N 47572 AUTO PRESSURIZATION SYSTEM FAILED AFTER TAKEOFF. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLA CED THE LEFT FLOW CONTROL VALVE WITH NO HELP. REPLACED THE LEFT PACK TURBINE INLET TEMPERATURE SENSOR. OPERATIONAL CHE CK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996080800010 19960808 00010 NM 1996 8 8 96FDEA01303 1 19960731 A 5320 6515933 SHEAR TIE BOEING 727 7272D4 138407U NM BS 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 287FE 21849 NR 0141, 024 CORROSION (C53-1113-0141) IN THE FWD CARGO BAY ON FRAME SHEAR TIE BS 600 WL 150 RBL 17. *S/D* REMOVED CO RRODED SHEAR TIE AT BS 600 WL 150 RBL 1. FABRICATED AND INSTALLED NEW SHEAR TIE AT BS 600 WL 150 RBL 17 PER FEDEX SRM 5 3-10-4. 2 L 7 3 4F A3WE 1996080800011 19960808 00011 NM 1996 8 8 96FDEA01304 1 19960801 A 3350 1060091102 LIGHT BOEING 727 72722 1384002 NM BS 328 INOPERATIVE A FDEA K NONE L NO TEST IN INSP/MAINT 1 SO 25 195FE 19144 LP 558749 045C. EMERGENCY EXIT LIGHT OVER FORWARD ENTRY DOOR DOES NOT ILLUMINATE WITH LOSS OF ESSENTIAL AC POWER. REP LACED FORWARD ENTRY LIGHT ASSEMBLY. FUNCTIONAL TEST CHECKS GOOD IAW FEDEX MM 33-50-101. (BS 328, WL 200 LBL 65.) 2 L 7 3 4F A3WE 1996080800012 19960808 00012 NE 1996 8 8 CALA9601107 2 19960730 A 7530 790762 STATOR SUPPT DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 2 ENGINE BROKEN A CALA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SW 09 14816 28171 5809 49370 THE NR 2 ENGINE BEGAN TO VIBRATE ACCOMPANIED BY AN ERRATIC EPR GAGE READING WHILE EN ROUTE. ENGINE POWER WAS REDUCED TO IDLE, ATTEMPTS TO OBTAIN MORE THAN 50 PERCENT POWER CAUSED EXCESSIVE VIBRATION. THE AIRCRAFT WAS DIVERTED TO EWR WHERE IT LANDED WITHOUT INCIDENT. A BORESCOPE INSPECTION FOUND DAMAGE TO THE NR 2 ENGINE. THE NR 2 ENGINE WAS REMOVED AND R EPLACED. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION. *S/D* SHOP FINDINGS REVEALED AN 8TH STA GE STATOR SUPPORT(SHELF) BROKEN. 2 L 7 2 4F 4 F A6WE E9NE 1996080800013 19960808 00013 WP 1996 8 8 CALA9601108 1 19960731 A 3260 833604 PROX CONTROL DOUG DC9 DC982 3022082 WP LANDING GEAR INOPERATIVE A CALA O OTHER N FALSE WARNING CL CLIMB 1 SW 09 72824 40771 4327 49824 ALL THREE RED GEAR UNSAFE LIGHTS REMAINED ILLUMINATED AFTER TAKEOFF. THE GEAR WAS CYCLED, BUT THE LIGHTS DID NOT EXTING UISH. THE LIGHTS WERE INTERMITTENT FOR A WHILE AND WENT OUT AFTER 2O MINUTES. THE FLIGHT WAS CONTINUED WITHOUT FURTHER PROBLEM. TROUBLESHOOTING BY MAINTENANCE FOUND THE PROXIMITY CONTROL UNIT AT FAULT. THE PROXIMITY CONTROL UNIT WAS REP LACED. GEAR INDICATIONS CHECKED NORMAL. PART TOTAL CYCLES, 26,106. 2 L 7 2 4F A6WE 1996080800014 19960808 00014 NM 1996 8 8 CALA9601109 1 19960731 A 2910 6517843345 HYD LINE BOEING 727 727224 1384076 NM LE FLAPS LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 09 69736 69736 THE A-SYSTEM HYDRAULIC FLUID QUANTITY DROPPED TO ZERO ON FINAL APPROACH TO EWR. THE FLUID LOSS WAS ACCOMPANIED BY ILLUMI NATION OF HYDRAULIC SYSTEM LOW PRESSURE LIGHTS. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A LEAK IN THE LEADING EDGE SLAT HYDRAULIC PRESSURE LINE LOCATED IN AC BAY SIDE OF FORWARD WHEELWELL. A FLEX LINE REPAIR WAS INSTALLED PER CONTINENTAL AIRLINES GENERAL MAINTENANCE MANUAL 10-799-78, PAGE 14. A DIP WAS ISSUED TO INSTALL A PERMANENT LINE W ITHIN 1200 HOURS OR 500 FLIGHTS, WHICHEVER COMES FIRST. 2 L 7 3 4F A3WE 1996080800015 19960808 00015 NM 1996 8 8 CALA9601110 1 19960731 A 2450 HARNESS BOEING 737 737130 1384435 NM APU FAILED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14211 19028 MAINTENANCE FOUND FEEDER HARNESS BURNT WHILE TROUBLESHOOTING THE APU. A STRINGER AT BELLY OF AIRCRAFT ABOUT 15 INCHES F ORWARD OF APU COMPARTMENT AFT OF AFT PRESSURE BULKHEAD WAS FOUND BURNED DUE TO THE FEEDER HARNESS ARCING. A NEW HARNESS WAS SPLICED IN AND RECEPTACLE D4800J WAS REPLACED. APU OPERATION CHECKED GOOD. THE BURNED SECTION OF STRINGER WAS REP AIRED IAW SRM 53-10-3, FIGURE 1, SHEET 7. A CONDUCTIVITY TEST WAS PERFORMED ON SURROUNDING FUSELAGE SKIN AND THE CONDUC TIVITY OF THE AREA WAS WITHIN LIMITS PER SRM 51-10-03. 2 L 7 2 4F A16WE 1996080800016 19960808 00016 SO 1996 8 8 COMA9610235 1 19960731 A 5330 12019230001 SKIN EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 137H 18127 120137 DURING INSPECTION, FOUND LOWER FUSELAGE SKIN TO BE CORRODED AT FRAME 22 BETWEEN STRINGERS 20 LT AND 20 RT, CUT OUT CORRO DED AREA OF LOWER FUSELAGE SKIN FABRICATED AND INSTALLED A SERVICEABLE FILLER AND DOUBLER REPAIR. ALL WORK WAS DONE I/A /W EMB 120 S.B. 120-53-0065, S.R.M. 53-00-01, FIG. 202. AIRCRAFT TOTAL CYCLES, 20,085. 2 L 7 2 4T RT A31SO 1996080800017 19960808 00017 SO 1996 8 8 COMA9610236 1 19960731 A 2150 PACK EMB 120 EMB120RT SO RIGHT SMOKING A COMA H D DEACTIVATE SYST/CIRCUITS RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 1117H 120117 CABIN FILLED WITH SMOKE WITH RT COOLING PACK ON. COULD NOT DUPLICATE. OPERATIONAL CHECK OF COOLING SYSTEM NORMAL. 2 L 7 2 4T RT A31SO 1996080800018 19960808 00018 EA 1996 8 8 COMA9660127 1 19960731 A 3520 OXY MASKS CNDAIR CL600 CL6002B19 EA CABIN DEPLOYED A COMA G D O2 MASK DEPLOYED RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 914CA 7012 ALL OF THE PASSENGER CABIN OXYGEN MASKS DEPLOYED DURING TAXI. RESTOWED OXYGEN MASKS. SYSTEM CHECKS SERVICABLE. 2 L 7 2 4F RT A21EA 1996080800019 19960808 00019 NM 1996 8 8 DL72K961802 1 19960727 A 3350 LIGHT 1000677 BOEING 727 727232 1384082 NM COCKPIT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 481DA 3969 20861 COCKPIT EXIT EMERGENCY LIGHT INOPERATIVE DURING TEST. REPLACED LIGHT ASSEMBLY. 2 L 7 3 4F A3WE 1996080800020 19960808 00020 NM 1996 8 8 DL72K961813 1 19960722 A 5320 WEB BOEING 727 727232 1384082 NM BS 1303 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 415DA 21257 FOUND TWO 1.5 INCH CRACKS AT LOWER LT AND RT CORNERS OF VERTICLE WEB AT STA 1303 ABOVE THE 'S' DUCT. REPAIRED PER SRM 5 3-10-4, FIG 17. 2 L 7 3 4F A3WE 1996080800021 19960808 00021 NM 1996 8 8 DL72L961779 1 19960724 A 3350 0L3071BPEGPL BULB BOEING 727 727232 1384082 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 501DA 21303 LAST LIGHT ON EMERGENCY TRACK LIGHTING COPILOT'S SIDE AND AT ROW 17 INOPERATIVE. REPLACED BULB. OPS CHECK NORMAL. 2 L 7 3 4F A3WE 1996080800022 19960808 00022 NM 1996 8 8 DL72S961759 1 19960723 A 2150 PACK FAN 6056751 BOEING 727 727232 1384082 NM RIGHT INOPERATIVE A DALA C D ABORTED TAKEOFF RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 543DA 1181660 22392 REJECTED TAKEOFF AT DFW 18L DUE TO RT PACK TRIPPING OFF AND FILLING THE CABIN WITH SMOKE. REPLACED RIGHT PACK FAN. OPS CHECK NORMAL. 2 L 7 3 4F A3WE 1996080800023 19960808 00023 NM 1996 8 8 DL72S961777 1 19960725 A 2121 215201 FAN BOEING 727 727232 1384082 NM CARGO COMPT INOPERATIVE A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 519DA 21470 AFTER TAKEOFF, FLIGHT ATTENDANT REPORTED SMOKE IN CABIN. COMPLIED WITH P.O.M. AND RETURNED TO SFO. (PACK TEMP NORMAL) REPLACED GASPER FAN. OPS CHECK NORMAL. 2 L 7 3 4F A3WE 1996080800024 19960808 00024 NM 1996 8 8 DL72S961780 1 19960716 A 5530 WEB BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 521DA 21472 FOUND CRACK AT 1303 B/H STR CUTOUT LEFT SIDE INSIDE VERTICAL STABILIZER JUST ABOVE 'S' DUCT. REPAIRED PER SRM 53-10-4. 2 L 7 3 4F A3WE 1996080800025 19960808 00025 NM 1996 8 8 DL72S961782 1 19960725 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 467DA 20744 ON LAYOVER, FOUND CENTER AISLE EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 3. REPLACED BATTERY PACK. OPS NORMAL. 2 L 7 3 4F A3WE 1996080800026 19960808 00026 NM 1996 8 8 DL72S961783 1 19960725 A 3350 90052 POWER SUPPLY BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 467DA 20744 ON LAYOVER, FOUND EMERGENCY EXIT LIGHT ABOVE R-2 DOOR INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY PACK. OPS NORMAL. 2 L 7 3 4F A3WE 1996080800027 19960808 00027 NM 1996 8 8 DL72S961791 1 19960727 A 3350 BULB 1315 BOEING 727 727232 1384082 NM COCKPIT FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 497DA 21077 EMERGENCY EXIT LIGHT OVER COCKPIT DOOR WILL NOT TEST. RELAMPED, OPS CHECKS OK. 2 L 7 3 4F A3WE 1996080800028 19960808 00028 NM 1996 8 8 DL72W961798 1 19960727 A 3350 BATTERIES S106 BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 297WA 22534 ON LAYOVER, FOUND FORWARD CROSS-AISLE CEILING LIGHT FOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, LIGHTS CHECK GOOD. 2 L 7 3 4F A3WE 1996080800029 19960808 00029 NM 1996 8 8 DL73E961767 1 19960724 A 3350 BATTERY PACK 20131A BOEING 737 737247 138448D NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 376DL 23603 EMERGENCY LIGHTS OUT AT LT OVERWING RT SIDE ABOVE WING EXIT HATCH, AND OVERHEAD BINS 13C, 11D, AND 10C. REPLACED BATTER Y PACK. 2 L 7 2 4F A16WE 1996080800030 19960808 00030 NM 1996 8 8 DLM11961778 1 19960724 A 3350 BATTERIES P2070003 DOUG MD11 MD11 3023602 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 810DE 48565 EMERGENCY FLASHLIGHT AT 4R NOT BLINKING. REPLACED FLASHLIGHT, CHECKS NORMAL. 2 L 7 3 4F RT A22WE 1996080800031 19960808 00031 WP 1996 8 8 QXEA9600268 2 19960728 A 7200 ENGINE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111UW 01514 WP ROTOL R321 R321482F8 GL LEFT DAMAGED A QXEA D RETURN TO BLOCK C F.O.D. TX TAXI/GRND HDL 1 NM 09 26959 AC662 P44636 DRG83289 GTF - TAXIING FROM THE RAMP, THE LEFT PROPELLER STRUCK A TRAFFIC CONE. CONE WAS THROWN INTO THE FUSELAGE AT STA 166.5, WL 77. DENT SIZE WAS APPROXIMATELY 12 INCHES BY 12 INCHES AND .50 INCH DEEP. ONE PROP BLADE WAS BENT FROM THE IMPACT. THE PROP WAS REPLACED AND THE ENGINE WAS REPLACED BECAUSE OF THE PROP STRIKE. ENGINE AND PROP REPLACEMENT WAS IAW MM A ND BOTH OPS CHECKED GOOD ON GROUND RUN. AIRCRAFT FERRIED TO PDX FOR REPAIR OF THE FUSELAGE DENT. DAMAGED ICE SHIELD, F USELAGE SKIN, STRINGER SECTION, INTERCOSTAL, AND FRAME SECTION. REPAIRED IAW SRM. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 3 T RT A8SW E3WE 6 C P61GL 1996080800032 19960808 00032 EU 1996 8 8 QXEA9600269 1 19960730 A 3350 MGG1280 BULBS GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 493US 11161 SEA - SEVERAL EMERGENCY BULBS ARE INOPERATIVE IN AISLE EXIT SIGN AT ROW 8. BULBS WERE REPLACED AND SIGN OPS CHECKED GOO D. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996080800033 19960808 00033 NM 1996 8 8 QXEA9600270 1 19960731 A 5220 001A522C0120000 DOOR DORNER DO32 DO328100 2996000 NM CABIN NOT SEATED A QXEA K NONE J WARNING INDICATION CR CRUISE 1 NM 09 332PH 3010 GEG - DOOR WARNING LIGHT ILLUMINATED, SYSTEM PAGE INDICATED EXIT AT 9A. CABIN DIFFERENTIAL PRESSURE LOWERED TO 3.45 PSI D AND LIGHT WENT OUT. AIRCRAFT LANDED WITHOUT FURTHER PROBLEMS. REMOVED AND REINSTALLED EMERGENCY EXIT DOOR AT 9A. AI RCRAFT PRESSURIZED TO 5.5 PSID AND WARNING LIGHT REMAINED OUT. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A45NM 1996080800034 19960808 00034 NM 1996 8 8 QXEA9600271 1 19960731 A 5270 869701 SENSOR ELDEC DORNER DO32 DO328100 2996000 NM EMER EXIT DOOR OUT OF ADJUST A QXEA K NONE N FALSE WARNING CR CRUISE 1 NM 09 332PH 3010 BIL - DOOR WARNING LIGHT ILLUMINATED DURING DESCENT THROUGH 20,000 FEET AT 5.1 PSID, SYSTEM PAGE INDICATED EXIT AT 9A. A IRCRAFT LANDED IN BIL WITHOUT FURTHER PROBLEMS. AIRCRAFT FERRIED TO GEG FOR REPAIR. PROXIMITY SENSOR ADJUSTED AND EXIT AT 9A IAW MM. SENSOR OPS CHECKED GOOD IAW MM. TEST FLIGHT CONDUCTED AND FLIGHT WAS SATISFACTORY. AIRCRAFT RETURNED T O SERVICE. 2 H 7 2 4T RT A45NM 1996080800035 19960808 00035 EU 1996 8 8 QXEA9600272 1 19960731 A 3350 MGG1280 BULB GRIMES 5515800106 FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 802PH 11017 SEA - FORWARD EMERGENCY EXIT SIGN DIM. BULBS WERE REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996080800076 19960808 00076 CE 1996 8 8 96ZZZX3825 1 19960621 A 2133 261950010 VALVE LEAR 35 35A 5170602 CE CABIN PRESSURE FAILED A IJDA C D ABORTED TAKEOFF RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 WP 01 810CC 486 SMOKE IN CABIN AND COCKPIT WITH ACCOMPANYING HEAT. PRESSURIZATION VALVE STUCK 'OPEN' CAUSING FULL CABIN/COCKPIT HEAT. O CCURRED DURING TAKEOFF. VALVE TROUBLESHOT AND REPLACED BY REPAIR STATION AT AWAY-FROM-HOME LOCATION. 2 L 7 2 4F A10CE 1996080800091 19960808 00091 WP 1996 8 8 9616589946 1 19960730 A 3350 60030451 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN MALFUNCTIONED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8926E 45863 DURING LINE MAINTENANCE INSPECTION, FOUND AFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERAT IONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996080800092 19960808 00092 WP 1996 8 8 9616599971 1 19960730 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9335 47337 DURING PERIODIC CHECK, FOUND TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND BATTERIES, OPERATIONAL CH ECK NORMAL. 2 L 7 2 4F A6WE 1996080800093 19960808 00093 WP 1996 8 8 9616609995 1 19960729 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP TAILCONE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8978E 47327 DURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, OPERATI ONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996080800094 19960808 00094 WP 1996 8 8 9616619995 1 19960731 A 3350 FUSE DOUG DC9 DC931 3022065 WP TAIL COMPT BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8978E 47327 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE AT POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996080800095 19960808 00095 WP 1996 8 8 9616629604 1 19960731 A 3350 60030451 POWER SUPPLY DOUG DC9 DC932 3022066 WP TAILCONE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 604NW 47222 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS IN TAILCONE INOPERATIVE. REPLACED POWER SUPP LY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996080800096 19960808 00096 WP 1996 8 8 9616639609 1 19960801 A 3350 6011779 BATTERY PACK DOUG DC9 DC932 3022066 WP RT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 609NW 47234 DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996080800097 19960808 00097 WP 1996 8 8 9616649610 1 19960801 A 3350 FUSE DOUG DC9 DC932 3022066 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 610NW 47432 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996080800098 19960808 00098 NM 1996 8 8 9616652704 1 19960730 A 7711 EPR TRANSMITTER BOEING 727 727225 1384077 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE INOPERATIVE A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 801EA 22432 648996 DURING TAKEOFF, NR 3 ENGINE EPR INDICATOR BECAME INOPERATIVE. CREW ABORTED TAKEOFF AND RETURNED TO GATE WITHOUT INCIDEN T. MAINTENANCE REPLACED NR 3 ENGINE EPR TRANSMITTER, OPERATIONAL CHECK OK. 2 L 7 3 4F 4 F A3WE E2EA 1996080800099 19960808 00099 WP 1996 8 8 9616669876 1 19960801 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 785NC 48110 DURING LINE CHECK, FOUND AFT LEFT AND RIGHT CABIN OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONA L CHECK OK. 2 L 7 2 4F A6WE 1996080800100 19960808 00100 EU 1996 8 8 9616813222 1 19960731 A 2730 ROD ENDS AIRBUS 320 A320211 3930320 EU ELEVATOR SERVO WORN A NWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 01 322US 263 CLIMBING THROUGH 15,000 FEET AT 290 KNOTS, EXPERIENCED AIRFRAME VIBRATION MOST NOTICEABLEY IN THE AFT CABIN. REDUCING S PEED REDUCED VIBTATION. AIRCRAFT RETURNED TO MSP UNDER DIRECTION OF MAINTENANCE CONTROL AND DISPATCH AND ACCOMPLISHED A N UNEVENTFUL LANDING. MAINTENANCE REPLACED FOUR ELEVATOR SERVO CONTROL ROD ENDS. 2 L 7 2 4F RT A28NM 1996080800101 19960808 00101 NM 1996 8 8 96FDEA01305 1 19960728 A 3610 BACH7D01DL DUCT ASSY BOEING 727 727225 1384077 NM NR 1 PYLON LEAKING A FDEA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 25 464FE 21288 SECOND FLT OF DAY ON DEPARTURE, MAXIMUM POWER ENGINE NR 1 STRUT OVERHEAT LIGHT ILLUMINATED. LIGHT WENT OUT UPON RETARDI NG THROTTLES. RETURNED FOR UNEVENTFUL LANDING. FOUND LEAKS AT BALL NUT CONNECTION TO 8TH STAGE CHECK VALVE, FLEX LINE FROM 13TH STAGE TO THRUST REV T-CONNECTION. REMOVED AND REPLACED 8TH STAGE DUCT ASSEMBLY, HP VALVE FLEX LINE, HOSE ASSE MBLY AND RAN ENGINE, LEAK CHECK GOOD. 2 L 7 3 4F A3WE 1996080800102 19960808 00102 NM 1996 8 8 96FDEA01306 1 19960729 A 7930 1163P182 OIL BYPASS SW BOEING 727 727233 138408A NM NR 2 ENGINE MALFUNCTIONED A FDEA A E UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING NR NOT REPORTED 1 SO 25 223FE 20935 NR 2 ENG SHUTDOWN DUE TO NR 2 OIL FILTER BYPASS LIGHT ON IN FLT AND WOULD NOT EXTINGUISH. REMOVED AND REPLACED MAIN OIL SCREEN. FOUND SMALL PIECES OF CARBON. RAN NR 2 ENG TO T/O POWER FOR 5 MINUTES. REMOVED AND REPLACED LOW OIL SCREEN, FOUND IT CLEANED. REMOVED AND REPLACED LOW OIL BYPASS SWITCH, SYS WORKED NORMAL WITH 32 ENG RUNNING. 2 L 7 3 4F RT A3WE 1996080800103 19960808 00103 NM 1996 8 8 96FDEA01307 1 19960731 A 3230 1U10851 SEQUENCE VALVE BOEING 727 72722 1384002 NM LT MLG WW LEAKING A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 190FE 19083 LOSS OF SYS A-HYD ON GEAR RETRACTION. A-PUMPS RAN FOR 7 MINUTES WITHOUT FLUID. REMOVED AND REPLACED NR 1 AND NR 2 ENG HYD PUMPS PER MM 29-11-33. REMOVED AND REPLACED NR 1 AND NR 2 ENG HYD PUMP CASE DRAIN FILTERS PER MM 29-11-41, S-SYS RE TURN FILTER PER MM 29-11-102, LT MLG LOCK OPERATED SEQUENCE VALVE PER MM 32-32-31 AND LEAK CHECK GOOD. RAN ENG PER JET RUN HANDBOOK, OPS CHECK GOOD. UNABLE TO COMPLY WITH LANDING GEAR RETRACTION TEST PER MM. JACKED A/C PER CHAPTER 7 MM A ND SWUNG GEAR SEVERAL TIMES, RESET MANUAL EXTENSION AND OPS CHECK GOOD, NO LEAKS. GEAR SWING GOOD AND GEAR PINS REMOVED AND STOWED. 2 L 7 3 4F A3WE 1996080800104 19960808 00104 NM 1996 8 8 96FDEA01308 1 19960801 A 5320 6969085 STRINGER CLIP BOEING 727 7272D4 138407U NM BS 640 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 FWD CARGO BAY STR CLIP HAS TORN EDGE BS 640 STR 27L. FABRICATED STR CLIP AND INSTALLED AT BS 640 STR 27L PER FEDEX SRM 53-10-1. 2 L 7 3 4F A3WE 1996080800105 19960808 00105 NM 1996 8 8 96FDEA01309 1 19960802 A 3350 1060091101 LIGHT BOEING 727 72722 1384002 NM CABIN INOPERATIVE A FDEA K NONE L NO TEST IN INSP/MAINT 1 SO 25 195FE 19144 NRO774 AND 046, EMERGENCY EXIT LIGHT OVER FWD ENTRY DOOR DOES NOT ILLUMINATE WITH LOSS OF ESSENTIAL AC POWER. *S/D* RE PLACED FWD ENTRY LIGHT ASSEMBLY, FUNCTIONAL TEST CHECKS OK IAW FEDEX MM 33-50-101. 2 L 7 3 4F A3WE 1996080800106 19960808 00106 NM 1996 8 8 96FDEA01310 1 19960802 A 5330 651753057 SKIN BOEING 727 7272D4 138407U NM BS 1220 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 NR0444 AND 007, AFT AIRSTAIR CUTOUT L/FWD CORNER CRACKED PAST RIVET BS 1220 STR 26. *S/D* REPAIRED CRACK AT BS 220 STR 26L IAW FEDEX STANDARD REWORK DRAWING SR 27-53-024. 2 L 7 3 4F A3WE 1996080800107 19960808 00107 NM 1996 8 8 CALA9601111 1 19960730 A 5330 SKIN BOEING 737 737219 1384469 NM FWD FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10248 20344 INSPECTION FOUND A .4375 INCH CRACK IN FUSELAGE SKIN BELOW FIRST OFFICER'S EYEBROW WINDOW. THE SKIN WAS REPAIRED IAW SR M 53-30-3, PAGES 26 TO 28E, REPAIR NR 7. 2 L 7 2 4F A16WE 1996080800108 19960808 00108 1996 8 8 DHL96722004 4 19960730 A 3421 158663A VERT GYRO BOEING 727 727228 NM NR 2 FAILED A T DHLA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 722DH 19861 NUMBER 2 VERTICAL GYRO IS INOPERATIVE. REMOVED AND REPLACED GYRO, OPS CHECK GOOD PER MM 34-22-21. 2 L 7 3 4F A3WE 1996080800109 19960808 00109 NM 1996 8 8 DL72S961827 1 19960730 A 5320 651751738 CHANNEL BOEING 727 727232 1384082 NM BS 1263 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 497DA 21077 FOUND A 1 INCH CRACK IN THE CHANNEL AT FS 1263, TORQUE BOX. REPLACED PER BOEING S/B 53-0129. 2 L 7 3 4F A3WE 1996080800110 19960808 00110 NM 1996 8 8 DL73E961826 1 19960730 A 5320 INTERCOSTAL BOEING 737 737247 138448D NM BS 332 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 374DL 23521 FOUND CRACK AT THE R-1 DOOR FRAME INTERCOSTAL AT STR 8A. REPAIRED PER S/B 737-53A1108, REV 5 IN ACCORDANCE WITH FAA/DER FORM 8110-3, DER DESIGNATION NM-2256, DATED 7/29/96. 2 L 7 2 4F A16WE 1996080800111 19960808 00111 NM 1996 8 8 DL73S961819 1 19960723 A 5330 SKIN BOEING 737 737232 1384475 NM R-2 DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 314DA 23086 FOUND A 2.25 INCH CRACK IN THE R-2 DOORWAY. REPAIRED PER B737-200 SRM 53-30-3, FIG 24. 2 L 7 2 4F RT A16WE 1996080800112 19960808 00112 NM 1996 8 8 DL73S961820 1 19960723 A 5330 6545769545 SKIN BOEING 737 737232 1384475 NM BS 373 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 334DL 23105 THE SKIN AT THE COOLING DUCT CUTOUT, BS 373 LBL 3 WAS FOUND CRACKED AT THE AFT EDGE OF THE CUTOUT. THE CRACK MEASURED A PPROXIMATELY 1.375 INCH LENGTH. REPAIRED PER BOEING S/B 737-53-1117, REV 1. 2 L 7 2 4F RT A16WE 1996080800113 19960808 00113 NM 1996 8 8 DL757961825 1 19960730 A 5220 144N863012 CUB STRAP BOEING 757 757232 1384965 NM RT EMER EXIT CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 627DL 22917 FOUND CORROSION ON THE FWD SIDE OF THE RT OVERWING EXIT DOOR INNER SIDE, CUB STRAP. REPAIRED PER BACO TWX DAL-ATL-96-11 44RR, DATED 7/29/96. 2 L 7 2 4F RT A2NM 1996080800114 19960808 00114 WP 1996 8 8 DLL10961816 1 19960731 A 3350 012 BATTERY PACK LKHEED 1011 10113851 5265010 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 728DA 193C1173 L2 DOOR EMERGENCY LIGHT BATTERY PACK FAILS OPN. REPLACED BATTERY PACK. 2 L 7 3 4F A23WE 1996080800115 19960808 00115 WP 1996 8 8 DLL10961817 1 19960731 A 3350 012 POWER SUPPLY LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 728DA 193C1173 PWR SUPPLY AT R-4 DOOR FAILS FUNCTION TEST. REPLACED POWER SUPPLY, OPS CHECK NORMAL. 2 L 7 3 4F A23WE 1996080800116 19960808 00116 WP 1996 8 8 DLL10961818 1 19960731 A 3350 012 BATTERY PACK LKHEED 1011 10113851 5265010 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 728DA 193C1173 L-1 DOOR EMERGENCY LIGHT BATTERY PACK FAILS OPN. REPLACED BATTERY PACK, OPS CHECK NORMAL. 2 L 7 3 4F A23WE 1996080800117 19960808 00117 WP 1996 8 8 TC8A96051 1 19960802 A 2130 PRESSURIZATION DOUG DC8 DC8F55 3021928 WP CABIN MALFUNCTIONED A TC8A O OTHER J WARNING INDICATION CR CRUISE 1 GL 23 808CK 45817 LOST PRESSURIZATION DURING CRUISE, UNABLE TO OPERATE NASI FLOW CONTROL SYSTEM. CHECKED NASI SYSTEM AND GROUND RUN, SYST EM CHECKED GOOD IAW NASI M/M CHAPTER 21-7-0, PRESSURIZATION OK. 2 L 7 4 4F 4A25 1996080800121 19960808 00121 SW 1996 8 8 96ZZZX3843 1 19960610 A 6322 247821 SHAFT ASSY 222365515105 BELL 222 222U 1182140 SW COOLER BLOWER SHEARED A A NXTA E ENGINE SHUTDOWN M OVER TEMP CR CRUISE 1 SW 19 143CF 47506 DURING FLIGHT, THE PILOT NOTED THE NR 2 ENGINE OIL PRESSURE DROPPING AND THE OIL TEMPRATURE RISING. HE SHUT DOWN THE EN GINE AS A RESULT, AND PERFORMED A SINGLE ENGINE LANDING. WHILE INVESTIGATING THE CAUSE, THE MECHANIC DISCOVERED THE SHA FT OF THE OIL COOLER BLOWER TO HAVE SHEARED NEXT TO THE SPINE ADAPTER. THE IMPELLERS APPEAR TO HAVE SEIZED INSIDE THE H OUSING. 1 G 7 2 3U H9SW 1996080800125 19960808 00125 SW 1996 8 8 96ZZZX3847 1 19960620 A 6230 206010336005 DRIVE LINK BELL 206 206L1 1182107 SW M/R MAST WORN B ZV1R K NONE O OTHER IN INSP/MAINT 1 SW 03 40LP 45233 PLAY IN EXCESS OF .025 INCH AT TWO PLACES. SEE BELL MM L3, FIGURE 62.21. AT TEAR DOWN, FOUND BEARING AND SPACERS WORN. TOTAL TIMES LESS THAN 1,000 HOURS AND 1 YEAR SINCE REPLACED. 1 G 7 1 3U H2SW 1996080800127 19960808 00127 NE 1996 8 8 96ZZZX3849 2 19960618 A 8530 327627 CYLINDER DOUG DC6 DC6A 3021706 WP PWA R2800 CB3 52026 NE NR 2 ENGINE CRACKED A NACA E ENGINE SHUTDOWN E VIBRATION/BUFFET CR CRUISE 1 AL 03 99330 1454 43576 31613 FLT 32 - SHUT DOWN NR 2 ENGINE AT 1245Z DUE TO ROUGH RUNNING AND UNABLE TO LEAN. MAINTENANCE REPLACED NR 16 CYLINDER DU E TO A CRACKED HEAD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4R 4 R 6A3 E264 1996080800128 19960808 00128 NE 1996 8 8 96ZZZX3850 3 19960616 A 6110 PROP ASSY DHAV DHC8 DHC8102 2809003 NM HAMSTD 14SF 14SF7 NE RT PROP FAILED A PCAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 13 808EX 11809 299 BWI - FLT 3530 - ON CLIMB AFTER DEPARTING, EXPERIENCED AN UNCOMMANDED AUTOFEATHER OF THE NR 2 PROPELLER. ENGINE WAS SEC URED AND AIRCRAFT RETURNED TO BWI WITHOUT INCIDENT. C/W UNSCHEDULED FEATHERING CHECKS AS OUTLINED IN PRATT & WHITNEY MM . REMOVED AND REPLACED COMPLETE PROPELLER ASSY IAW MM. ALSO, REMOVED AND REPLACED ENGINE SPIDER HARNESS IAW MM. GROUN D RAN AIRCRAFT. OPS CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. REFERENCE: OPERATOR CONTROL NR PCAA9600295. AIRCRAF T TOTAL CYCLES: 13,253. 2 H 7 2 4T RT A13NM 6 C P7NE 1996080800129 19960808 00129 WP 1996 8 8 96ZZZX3853 1 19960717 A 3350 08163046008 TRACK DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 969AS 53063 PDX - FLT 56 - EMERGENCY EXIT FLOOR TRACK LIGHTING INOPERATIVE ROWS S30 AND 32/33. RELAMPED AND INSTALLED NEW SECTION O F TRACK; LIGHTS OPERATED NORMALLY. REFERENCE: OPERATORS CONTROL NR ASAA9680154. 2 L 7 2 4F RT A6WE 1996080800131 19960808 00131 NE 1996 8 8 96ZZZX3855 2 19960528 A 7200 ENGINE DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE NR 2 FAILED A TWAA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 CE 05 410EA 47731 STL - FLT 564 - DURING APPROACH, SHUT DOWN NR 2 ENGINE, S/N 1722, DUE TO INCREASING EGT. ACCOMPLISHED NORMAL LANDING. F OUND TURBINE DAMAGE AND METAL PARTICLES IN TAILPIPE. REPLACED ENGINE, ENGINE OPERATION THEN CHECKED NORMAL. ENGINE TO TAL TIME: 35,307 HOURS; 32,872 CYCLES. CHECK C-12 - 3-20-96 - STL. INVESTIGATION OF NR 2 ENGINE, S/N 1722, SHUTDOWN R EVEALED ONE EACH VANE CRACKED AT INNER SHROUD AND RELEASED, PRODUCING DAMAGE TO THE HIGH PRESSURE COMPRESSOR AND TURBINE . THE ENGINE WAS REPAIRED AND RETURNED TO SERVICE. 2 L 7 2 4F 4 F A6WE E2EA 1996080800132 19960808 00132 WP 1996 8 8 96ZZZX3856 1 19960716 A 3232 1512449107 ACTUATOR LKHEED 1011 10113851 5265010 WP NLG DOOR DEFECTIVE A RIAA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 SO 19 319EA 193A1040 RIA - FLT 112 - HNL/SFO - AFTER TAKEOFF DURING GEAR RETRACTION, 3 GREEN LIGHTS EXTINGUISHED, DOOR IN-TRANSITION RED LIGH TS REMAINED ON, NOSE GEAR OR DOOR AMBER LIGHT ON, S/O PANEL REMAINED ON 2-3 SECONDS. VIBRATION FELT, GEARS WERE CYCLED WITH NO HELP. ACFT DUMPED FUEL AND RETURNED TO HNL. ON GROUND, MAINTENANCE FOUND FWD LT NLG DOOR ACTUATING CYLINDER DE FECTIVE. ACTUATING CYLINDER REPLACED PER MM 32-35-01, MM 32-22-01, 5 NOSE GEAR RETRACTIONS ACCOMPLISHED, ACFT CHECKED N ORMAL, ACFT RELEASED INTO SERVICE. (X) 2 L 7 3 4F A23WE 1996080800133 19960808 00133 1996 8 8 A21A4983401 4 19960717 A 3416 51828007207 ALTIMETER FOKKER F28 F28MK4000 4990810 EU COCKPIT FAILED A A21A A UNSCHED LANDING O OTHER CL CLIMB 1 WP 17 498US 399 11181 FAT/LAS - DURING CLIMB, CAPTAIN'S ALTIMETER STUCK AT 5,300 FEET. FIRST OFFICER'S ALTIMETER OK. ALTERNATE SOURCE SELECT ED AND NO HELP. CREW REPORTED TO MAINTENANCE CONTROL AND WAS ADVISED TO RETURN TO FAT. CAPTAIN'S ALTIMETER WAS REPLACE D, PITOT STATIC TEST WAS ACCOMPLISHED IAW 34-10-02 AND 34-11-02, AND SYSTEM FUNCTIONED NORMALLY. (X) 2 L 7 2 4F RT A20EU 1996080800134 19960808 00134 NM 1996 8 8 AALA961031 1 19960711 A 5311 FRAME BOEING 727 727223 1384074 NM BS 804.95 DOUBLE DRILLED A AALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 707AA 22464 TUL - DOUBLE HOLE DRILLED IN BELT FRAME. REPAIRED FRAME PER SRM 53-10-4, FIGURE 2. TST: 41,665 HOURS. CYCLES: 21,76 8. (X) 2 L 7 3 4F A3WE 1996080800135 19960808 00135 NM 1996 8 8 AALA961032 1 19960711 A 5720 STIFFENER BOEING 727 727223 1384074 NM WS 255 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 707AA 22464 TUL - LEFT WING FORWARD SPAR, CORROSION ON VERTICAL STIFFENER FSS 255. REPLACED STIFFENER PER SRM 51-10-4. TST: 41,66 5 HOURS. CYCLES: 21,768. (X) 2 L 7 3 4F A3WE 1996080800136 19960808 00136 NM 1996 8 8 AALA961033 1 19960711 A 5720 STIFFENER BOEING 727 727223 1384074 NM WS 245 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 707AA 22464 TUL - LEFT WING FORWARD SPAR, CORROSION ON VERTICAL STIFFENER, FSS 245. REPLACED VERTICAL STIFFENER PER SRM 51-10-4, PA GE 4. TST: 41,665 HOURS. CYCLES: 21,768. (X) 2 L 7 3 4F A3WE 1996080800137 19960808 00137 NM 1996 8 8 AALA961034 1 19960711 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 704 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 707AA 22464 TUL - CORROSION ON STR 28L, STA 704. INSTALLATED NEW SECTION OF STR 28L, STA 680 TO STA 720. TST: 41,665 HOURS. CYCL ES: 21,768. (X) 2 L 7 3 4F A3WE 1996080800138 19960808 00138 NM 1996 8 8 AALA961035 1 19960711 A 5320 WEB BOEING 727 727223 1384074 NM BS 1136-1166 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 707AA 22464 FIVE PLACES OF CORROSION ON RIGHT AFT LAVATORY FLOOR WEB, EACH BEING APPROXIMATELY 2 INCHES BY 6 INCHES IN A 20 SQUARE I NCH AREA WITH 2 PLACES PASSED LIMITS. REMOVED CORROSION SECTION, REPLACED WITH SHIMMED DOUBLER PER SRM 51-40-2. ALODIN ED, PRIMED AND PAINTED. TST: 41,665 HOURS. CYCLES: 21,768. (X) 2 L 7 3 4F A3WE 1996080800139 19960808 00139 NM 1996 8 8 AALA961036 1 19960711 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 680-720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 707AA 22464 TUL - CORROSION ON STR 28R, STA 680 TO STA 720 PLUS 3 INCHES. REMOVED AND INSTALLED NEW STRINGER PER SRM 51-10-1, PAGE 4. ALODINED, PRIMED AND PAINTED PER MM 51-20-0. TST: 41,665 HOURS. CYCLES: 21,768. (X) 2 L 7 3 4F A3WE 1996080800140 19960808 00140 NM 1996 8 8 AALA961037 1 19960711 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 950-1000 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 707AA 22464 TUL - HEAVY CORROSION ON STR 29R FROM STA 950E TO STA 1000. REMOVED AND REPLACED STR 29R, STA 950-STA 1000 IAW SRM 53-1 0-3, AND INSTALLED DOUBLER AND TRIPLER IAW SRM 53-30-3, FIGURE 3, AND ESO 11697, DATED 6-10-96. TST: 41,665 HOURS. CY CLES: 21,768. (X) 2 L 7 3 4F A3WE 1996080800141 19960808 00141 NM 1996 8 8 AALA961040 1 19960711 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 480-488 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 707AA 22464 TUL - CORROSION ON STR 28L, OUTBOARD SIDE. REMOVED CORROSION STA 28L STA 480 - STA 488. REPAIRED STR 28L, STA 484 PER SRM 53-10-3. TST: 41,665 HOURS. CYCLES: 21,768. (X) 2 L 7 3 4F A3WE 1996080800142 19960808 00142 NM 1996 8 8 AALA961041 1 19960711 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 680-710 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 707AA 22464 TUL - CORROSION ON STA 27R. REMOVED STA 27R, STA 680 - STA 710. INSTALLED NEW SECTION OF STRINGER PER 53-10-3. TST: 4 1,665 HOURS. CYCLES: 21,768. (X) 2 L 7 3 4F A3WE 1996080800143 19960808 00143 NM 1996 8 8 AALA961042 1 19960711 A 5320 STRAP BOEING 727 727223 1384074 NM BS 610-620 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 707AA 22464 TUL - CORROSION ON STRAP. REMOVED CORROSION, INSTALLED NEW STRAP FRAME 610-620 PER SRM 53-10-3. TST: 41,665 HOURS. C YCLES: 21,768. (X) 2 L 7 3 4F A3WE 1996080800144 19960808 00144 NM 1996 8 8 AALA961043 1 19960711 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 700 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 707AA 22464 REMOVED SHEAR TIE, REPLACED WITH NEW SHEAR TIE, STA 700, 28LT-28RT PER 53-10-3. TST: 41,665 HOURS. CYCLES: 21,768. ( X) 2 L 7 3 4F A3WE 1996080800145 19960808 00145 NM 1996 8 8 AALA961044 1 19960711 A 5330 SKIN BOEING 727 727223 1384074 NM BS 480-500 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 707AA 22464 TUL - CORROSION ON BELLY SKIN. INSTALLED DOUBLER PER SRM 53-30-3, PAGES 12-14A. REMOVED CORROSION. TST: 41,665 HOURS . CYCLES: 21,768. (X) 2 L 7 3 4F A3WE 1996080800146 19960808 00146 NM 1996 8 8 AALA961045 1 19960711 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 650-680 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 731AA 20738 TUL - STR 28R CORRODED. CUT OUT CORRODED SECTION, INSTALLED STRINGER PER SRM 53-10-3, FIG. 1. TST: 41,665 HOURS. CYC LES: 21,768. (X) 2 L 7 3 4F A3WE 1996080800147 19960808 00147 NM 1996 8 8 AALA961046 1 19960711 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 660-680 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 731AA 20738 TUL - STRINGER CORRODED 27L, STA 650 - STA 680. CUT OUT CORRODED STRINGER SECTION. INSTALLED NEW SECTION, SRM 53-10-3, FIGURE 1. TST: 41,665 HOURS. CYCLES: 21,768. (X) 2 L 7 3 4F A3WE 1996080800148 19960808 00148 NM 1996 8 8 AALA961047 1 19960711 A 5315 FLOOR BEAM BOEING 727 727227 1384078 NM BS 825.95 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 731AA 20738 TUL - CRACK IN FLOOR BEAM WEB AT HOLE, STA 823.95, INBOARD, RT SIDE. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 5 1-40-2, PAGES 1-6. TST: 41,665 HOURS. CYCLES: 21,768. (X) 2 L 7 3 4F A3WE 1996080800149 19960808 00149 NM 1996 8 8 AALA961048 1 19960711 A 5311 FRAME BOEING 727 727223 1384074 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 707AA 22464 TUL - CORROSION ON LOWER BELL FRAME, STA 720. INSTALLED REPAIR ON BELL FRAME PER SRM 53-10-4. TST: 41,665 HOURS. CYC LES: 21,768. (X) 2 L 7 3 4F A3WE 1996080800150 19960808 00150 NM 1996 8 8 AALA961049 1 19960711 A 5311 FRAME BOEING 727 727223 1384074 NM BS 804.95 MISDRILLED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 707AA 22464 TUL - HOLE DRILLED IN RADIUS OF FRAME. REPAIRED FRAME PER SRM 53-10-4, FIGURE 2. TST: 41,665 HOURS. CYCLES: 21,768. (X) 2 L 7 3 4F A3WE 1996080800151 19960808 00151 NM 1996 8 8 AALA961050 1 19960711 A 5311 FRAME BOEING 727 727223 1384074 NM BS 783.95 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 707AA 22464 TL - HOLE AND GOUGE IN RADIUS OF BELT FRAME. REPAIRED FRAME PER SRM 53-10-4, FIGURE 2. TST: 41,665 HOURS. CYCLES: 2 1,768. (X) 2 L 7 3 4F A3WE 1996080800152 19960808 00152 NM 1996 8 8 AALA961051 1 19960711 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 707AA 22464 TUL - CORROSION ON SHEAR TIE, STA 720 FROM STR 28L - STR 28R. REPLACED WITH NEW SHEAR TIE. TST: 41,665 HOURS. CYCLES : 21,768. (X) 2 L 7 3 4F A3WE 1996080800153 19960808 00153 NM 1996 8 8 ASAA9640061 1 19960717 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 773AS 25106 PDX - FLT 106 - EMERGENCY EXIT FLOOR TRACK LIGHTS INOPERATIVE AT ROW 15 (3 RED AND 2 WHITE). RECONNECTED WIRING TO LAMP SOCKETS AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1996080800154 19960808 00154 NM 1996 8 8 ASAA9640062 1 19960724 A 3350 RPS1B CHARGER BOEING 737 7374Q8 NM CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 755AS 25096 SEA - DURING MAINTENANCE CHECK, THE L-2 DOOR EMERGENCY EXIT IDENTIFIER WAS FOUND INOPERATIVE. REPLACED PACK CHARGER AND LIGHT OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1996080800155 19960808 00155 WP 1996 8 8 ASAA9680154 1 19960717 A 3350 303 LAMP DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 969AS 53063 PDX - FLT 56 - EMERGENCY EXIT FLOOR TRACK LIGHTING INOPERATIVE ROWS S30 AND 32/33. RELAMPED AND INSTALLED NEW SECTION O F TRACK; LIGHTS OPERATED NORMALLY. REFERENCE: OPERATORS CONTROL NR 96ZZZX3853. (X) 2 L 7 2 4F RT A6WE 1996080800156 19960808 00156 SO 1996 8 8 ASOA96031 1 19960724 A 2841 10026000002 INDICATOR EMB 120 EMB120RT SO FUEL QUANTITY ERRATIC A ASOA O OTHER O OTHER DE DESCENT 1 SO 11 232AS 17545 557 120036 ON DESCENT ABY-ATL, NOTED LEFT FUEL QUANTITY DOWN BY 600 POUNDS. CREW SUSPECTED FUEL LEAK IN LEFT TANK AND DECLARED AN EMERGENCY FOR DIRECT LANDING IN ATL. INSIDE MARKER, THE FUEL GAUGE RETURNED TO NORMAL. LANDING WAS MADE SAFELY AND WIT HOUT INCIDENT. REMOVED AND REPLACED THE LEFT FUEL QUANTITY INDICATOR. OPERATIONAL LEAK CHECKS WERE GOOD AND THE AIRCRA FT WAS RELEASED FOR FURTHER SERVICE. (X) 2 L 7 2 4T RT A31SO 1996080800157 19960808 00157 SO 1996 8 8 C2XA96IA152 1 19960612 A 3350 12021299001 LIGHT EMB 120 EMB120RT SO LT EXTERIOR INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12703 096 120084 CLE - DURING A ROUTINE CHECK OF EMERGENCY LIGHTING SYSTEM, LEFT AFT EXTERIOR EMERGENCY LIGHT FAILED TO ILLUMINATE. MAIN TENANCE REMOVED AND REPLACED LIGHT ASSEMBLY, OPERATIONAL CHECKED GOOD, AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1996080800158 19960808 00158 NM 1996 8 8 F3LA96019 1 19960721 A 3350 BULB BOEING 737 7372L9 1384497 NM CABIN FAILED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 170PL 11 22733 DEN - FLT 443 - DURING SERVICE CHECK, MAINTENANCE REPORTED THE EMERGENCY AISLE PATH LIGHTING INOPERATIVE. CLEANED CONTA CTS, REPLACED BULBS AND SYSTEM CHECKED OKAY. (X) 2 L 7 2 4F RT A16WE 1996080800159 19960808 00159 NM 1996 8 8 GAIA9621 1 19960604 A 2611 SMOKE DETECTOR BOEING 727 727251 138408H NM CARGO COMPT ILLUMINATED A GAIA O OTHER N FALSE WARNING DE DESCENT 1 SW 07 279US 21158 IAH/TOL - FLT 725 - DURING DESCENT INTO TOL, MAIN CARGO CABIN SMOKE DETECTOR LIGHT CAME ON. CHECKED CABIN, NO SMOKE NOT ED. MAINTENANCE CHECKED SYSTEM, NO DEFECTS NOTED. SYSTEM OPERATIONALLY CHECKED NORMAL. AIRCRAFT RELEASED FOR FLIGHT. (X) 2 L 7 3 4F A3WE 1996080800160 19960808 00160 NM 1996 8 8 GAIA9622 1 19960510 A 3350 BATTERY PACK BOEING 727 727223 1384074 NM BS 328 DISCHARGED A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 854AA 20995 DURING - C-CHECK INSPECTION, FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT FAILED TO TEST. MAINTENANCE FOUND BATTERY PACK DIS CHARGED. CHARGED BATTERY PACK PER B727 MM 33-50-0. CHECK GOOD. (X) 2 L 7 3 4F A3WE 1996080800161 19960808 00161 EU 1996 8 8 M3HA96018 1 19960702 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A M3HA K NONE L NO TEST IN INSP/MAINT 1 WP 13 988MA 2491 380 HNL - FLT 307 - EMERGENCY LIGHTS OVER PASSENGER TYPE EXITS DO NOT WORK WITH POWER OFF. FLOOR TRACK LIGHTS NRS 1, 3, 5, FRONT OF AIRCRAFT DO NOT COME ON WITH MASTER SWITCH OFF. REMOVED AND INSTALLED SERVICEABLE EMERGENCY BATTERY PACKS. LI GHTS OPS GOOD. (X) 2 H 7 2 4T RT A53EU 1996080800162 19960808 00162 NM 1996 8 8 MALA965075 1 19960716 A 3350 6104789 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A MALA O OTHER L NO TEST IN INSP/MAINT 1 GL 15 861MA 362 MSP - DURING A MAINTENANCE WALK-AROUND, SEVERAL EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE LOWER COAT CLOSET AND FORWARD CABIN LEFT BATTERY PACKS. ALL CHECKS SATISFACTORY. (X) 2 H 7 2 4T RT A13NM 1996080800163 19960808 00163 NM 1996 8 8 ORJA9640 1 19960715 A 3260 INDICATOR LIGHT DOUG MD90 MD9030 3023690 NM NLG MALFUNCTIONED A ORJA O OTHER P NO WARNING INDICATION AP APPROACH 1 WP 11 902RA 53490 NOSE GEAR INDICATOR LIGHT DID NOT INDICATE GREEN AFTER EXTENDING GEAR. RECYCLED GEAR AND NOSE GEAR INDICATED GREEN. AD JUSTED NOSE GEAR LOCKED PROXIMITY SENSOR IAW MM 32-61-02. SWUNG NOSE GEAR SEVERAL TIMES; COULD NOT DUPLICATE DISCREPANC Y. OPS CHECK GOOD. (X) 2 L 7 2 4F RT A6WE 1996080800164 19960808 00164 WP 1996 8 8 ORJA9641 1 19960715 A 3350 41B994AD073 POWER SUPPLY DOUG DC9 DC987 3022087 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 752RA 49780 AFT CABIN EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY. OPS CHECK NORMAL. (X) 2 L 7 2 4F RT A6WE 1996080800165 19960808 00165 WP 1996 8 8 ORJA9642 1 19960721 A 3350 41B004AD073 BATTERY PACK EA1DA3D3 DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 842RA 49604 FLOOR TRACK EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROWS 6-11. REPLACED BATTERY PACK. OPS CHECK GOOD. (X) 2 L 7 2 4F A6WE 1996080800166 19960808 00166 NM 1996 8 8 PCAA9600295 1 19960616 A 6120 311195401 HARNESS DHAV DHC8 DHC8102 2809003 NM RT PROP FAILED A PCAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 13 808EX 11809 299 BWI - FLT 3530 - ON CLIMB AFTER DEPARTING, EXPERIENCED AN UNCOMMANDED AUTOFEATHER OF THE NR 2 PROPELLER. ENGINE WAS SEC URED AND AIRCRAFT RETURNED TO BWI WITHOUT INCIDENT. C/W UNSCHEDULED FEATHERING CHECKS AS OUTLINED IN PRATT & WHITNEY MM . REMOVED AND REPLACED COMPLETE PROPELLER ASSY IAW MM. ALSO, REMOVED AND REPLACED ENGINE SPIDER HARNESS IAW MM. GROUN D RAN AIRCRAFT. OPS CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. REFERENCE: OPERATOR CONTROL NR 96ZZZX3850. AIRCRAFT TOTAL CYCLES: 13,253. (X) 2 H 7 2 4T RT A13NM 1996080800167 19960808 00167 EU 1996 8 8 RAIA960711 1 19960717 A 3242 AH54450 BRAKE ASSY BAG JETSTM JETSTM3201 1500217 EU LT MLG OVERHEATED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 971JX 5299 3080 971 LAX - FLT 4763 - DURING TAXI ONTO THE RUNWAY, THE LEFT MAIN TIRE WENT FLAT. MAINTENANCE FOUND LEFT BRAKE TO OVERHEAT CA USING THE WHEEL ASSY THERMAL FUSE TO BLOW. REPLACED LEFT MAIN TIRE AND BRAKE ASSY. (X) 2 L 7 2 4T RT A56EU 1996080800168 19960808 00168 EU 1996 8 8 RAIA960712 1 19960718 A 7712 31024766 TQ SIGNAL COND BAG JETSTM JETSTM3201 1500217 EU LT ENGINE OUT OF ADJUST A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 434AM 10506 6923 887 STL - FLT 7061 - LEFT ENGINE WOULD NOT PRODUCE TARGET TORQUE. MAINTENANCE ADJUSTED THE LEFT TORQUE SIGNAL CONDITIONER. (X) 2 L 7 2 4T RT A56EU 1996080800169 19960808 00169 1996 8 8 RAIA960713 4 19960718 A 3425 7003360946 AHRS COMPUTER AEROSP ATR72 ATR72202 8680940 EU NR 1 LOOSE A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 722TE 10375 220 PAI - FLT 7111 - ADU AND AHRS FAILED. MAINTENANCE RE-RACKED THE NR 1 AHRS COMPUTER. (X) 2 H 7 2 4T RT A53EU 1996080800170 19960808 00170 WP 1996 8 8 RAIA960714 2 19960718 A 7320 8961151 GASKETS BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RT ENGINE LEAKS A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 427AM 300 876 P66085 STL - FLT 7350 - RIGHT ENGINE WOULD NOT PRODUCE TARGET TORQUE. MAINTENANCE REPLACED THE RIGHT ENGINE P3 GASKETS. PERFO RMED GROUND RUNS. ENGINE TT, 9,871.0 HOURS. (X) 2 L 7 2 4T 4 T RT A56EU E4WE 1996080800171 19960808 00171 WP 1996 8 8 RAIA960715 2 19960718 A 7320 137928L405 P3 LINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3312UA 01514 WP RT ENGINE LEAKS A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 03 431AM 9857 881 P66162 STL - FLT 7512 - RIGHT ENGINE WOULD NOT PRODUCE TARGET TORQUE. MAINTENANCE REPLACED THE RT ENGINE P3 LINE. PERFORMED P OWER RUNS. (X) 2 L 7 2 4T 3 T RT A56EU E3WE 1996080800172 19960808 00172 EU 1996 8 8 RAIA960716 1 19960718 A 7720 311429901 T6 THERMOCOUPLE AEROSP ATR42 ATR42300 8680920 EU LT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 03 426TE 15660 228 FYV - FLT 7401 - LEFT ENGINE ITT INCREASED RAPIDLY TO 795. MAINTENANCE REPLACED LEFT ENGINE T6 THERMOCOUPLE. PERFORMED GROUND RUNS. (X) 2 H 7 2 4T RT A53EU 1996080800173 19960808 00173 EU 1996 8 8 RAIA960717 1 19960719 A 7712 31024766 TQ SIGNAL COND BAG JETSTM JETSTM3201 1500217 EU RT ENGINE OUT OF ADJUST A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 339TE 7761 7651 935 STL - FLT 7330 - RIGHT ENGINE WOULD NOT PRODUCE TARGET TORQUE. MAINTENANCE ADJUSTED THE RIGHT TORQUE SIGNAL CONDITIONER . PERFORMED GROUND RUNS. (X) 2 L 7 2 4T RT A56EU 1996080800174 19960808 00174 EU 1996 8 8 RAIA960718 1 19960719 A 7931 KPT06F84S CONNECTOR BAG JETSTM JETSTM3201 1500217 EU LT ENGINE LOOSE A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 862JX 10408 862 LAX - FLT 4761 - LEFT ENGINE OIL PRESSURE ERRATIC. MAINTENANCE REPAIRED THE LEFT OIL PRESSURE TRANSDUCER CANNON PLUG. ( X) 2 L 7 2 4T RT A56EU 1996080800175 19960808 00175 1996 8 8 RAIA960719 4 19960720 A 6122 31057165 PROP GOVERNOR JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE OUT OF ADJUST A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 03 555HK 19539 41072 STL - FLT 7326 - RIGHT ENGINE SLOW TO SPOOL UP TO TARGET TORQUE. MAINTENANCE ADJUSTED THE RIGHT PROPELLER GOVERNOR. PE RFORMED GROUND RUNS. (X) 2 L 7 2 4T RT A41NM 1996080800176 19960808 00176 WP 1996 8 8 RAIA960720 2 19960721 A 7320 8961151 P3 GASKETS BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT ENGINE LEAKS A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 342TE 430 954 SPI - FLT 7092 - LEFT ENGINE WOULD NOT PRODUCE TARGET TORQUE. MAINTENANCE REPLACED THE LEFT ENGINE P3 GASKETS. ENGINE TT, 9,934.5 HOURS. (X) 2 L 7 2 4T 4 T RT A56EU E4WE 1996080800177 19960808 00177 NM 1996 8 8 TAOA079603 1 19960718 A 2130 8844851 SENSE TUBE GARRTT BOEING 727 727225 1384077 NM CABIN PRESS BENT A TAOA O OTHER O OTHER CR CRUISE 1 EA 15 922TS P398 20415 AT ALTITUDE OF 21,000 FEET AS THE THROTTLES WERE RETARDED TO CRUISE, THE CABIN BEGAN TO CLIMB. AS POWER WAS INCREASED, CABIN PRESSURIZATION CONTROL OPERATED NORMALLY. REPLACED BENT SENSE LINE, SYSTEM TESTED NORMAL PER MM, CHAPTER 21-30-0 . REPLACED FLOW CONTROL VALVE, OPS OK PER MM, CHAPTER 21-30-0. (X) 2 L 7 3 4F A3WE 1996080800178 19960808 00178 NM 1996 8 8 TWRA9648 1 19960624 A 5280 DOOR BOEING 747 747121 1384871 NM RT MLG STRUT DAMAGED A TWRA K NONE O OTHER IN INSP/MAINT 1 EA 15 609FF 20354 DURING POST-FLIGHT, FLT 112, MAINTENANCE REPRESENTATIVE FOUND RIGHT WING GEAR STRUT DOOR DAMAGED, UPPER STRUT DOOR HINGE S INTACT, DOOR BROKEN IN TWO, LOWER STRUT DOOR ROD END BROKEN, DOOR INTACT, MINOR DAMAGE TO GULL DOOR, AFT MID-INBD FLAP DAMAGE FROM DEBRIS. DOOR WAS REPLACED. GEAR RETRACTION PERFORMED OK UNDER INVESTIGATION. (X) 2 L 7 4 4F A20WE 1996080800179 19960808 00179 NM 1996 8 8 TWRA9672 1 19960629 A 3350 S1356B37 LIGHT BOEING 747 747124 1384874 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 602FF 19734 DURING DAILY CHECK, MAINTENANCE FOUND CEILING EMERGENCY LIGHT INOPERATIVE IN AISLE OF AFT LAVATORY COMPLEX (N). REPLACE D LIGHT ASSY. OPS CHECK OK MM-33-51-00. (X) 2 L 7 4 4F A20WE 1996080800180 19960808 00180 NM 1996 8 8 W8PA960043 1 19960509 A 5720 FITTING BOEING 737 7373B7 1384580 NM RIGHT PYLON CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 947WP 23376 PITTING DISCOVERED ON OVERWING ATTACH FITTING JUST FORWARD OF FRONT SPAR. BLENDED OUT AND APPLIED PRIMER PER SRM 57-20- 90. (X) 2 L 7 2 4F RT A16WE 1996080800181 19960808 00181 NM 1996 8 8 W8PA960044 1 19960423 A 5313 STRINGER BOEING 737 7373B7 1384580 NM BS 727 CRACKED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 947WP 23376 DURING INSPECTION OF STR 18A WEB PER SB 737-53-1170, FOUND CRACKS IN THE AFT INBOARD LEFT SIDE HOLES. REPAIRED IAW SB 7 37-53-1170. (X) 2 L 7 2 4F RT A16WE 1996080800182 19960808 00182 NM 1996 8 8 W8PA960045 1 19960423 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 360 DENTED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 947WP 23376 FOUND DENT AT STA 360, WL 212L, 1.250 INCH LENGTH, .062 INCH DEPTH. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-00-01. (X) 2 L 7 2 4F RT A16WE 1996080800183 19960808 00183 NM 1996 8 8 W8PA960046 1 19960423 A 5330 SKIN BOEING 737 7373B7 1384580 NM DOOR CUT OUT CRACKED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 947WP 23376 DURING INSPECTION OF THE FORWARD GALLEY DOORWAY CUT-OUT UPPER CORNERS PER SB 737-53-116, FOUND 1 INCH CRACK IN UPPER AFT CORNER AND 2 CRACKS IN UPPER FORWARD CORNER. REPAIRED IAW SB 737-53-1116. (X) 2 L 7 2 4F RT A16WE 1996080800184 19960808 00184 NM 1996 8 8 W8PA960048 1 19960509 A 5320 INTERCOSTAL BOEING 737 7373B7 1384580 NM BS 847-867 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 947WP 23376 FOUND CORROSION ON FLOOR TO SIDE WALL INTERCOSTAL, BOTH TOP AND BOTTOM, AROUND NUTPLATES AT BS 847-867, RBL 22, WL 164. REMOVED AND REPLACED INTERCOSTAL PER SRM 53-60-15. (X) 2 L 7 2 4F RT A16WE 1996080800185 19960808 00185 NM 1996 8 8 W8PA960049 1 19960509 A 5320 FLOOR SUPPORT BOEING 737 7373B7 1384580 NM BS 757 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 947WP 23376 FOUND CORROSION ON FLOOR SUPPORT, BOTH TOP AND BOTTOM, AROUND NUTPLATES AT BS 727 D+5 TO 845, RBL 2.5 AND 7.5, WL 162. R EPAIRED IAW SRM 53-00-53. (X) 2 L 7 2 4F RT A16WE 1996080800186 19960808 00186 NM 1996 8 8 W8PA960050 1 19960509 A 5320 INTERCOSTAL BOEING 737 7373B7 1384580 NM BS 826 CRACKED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 947WP 23376 FOUND CRACK UNDER FLANGE OF INTERCOSTAL AT BS 826, RBL 6, WL 159. REMOVED AND REPLACED INTERCOSTAL. SRM 53-60-15. (X) 2 L 7 2 4F RT A16WE 1996080800187 19960808 00187 NM 1996 8 8 W8PA960052 1 19960509 A 5320 ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A W8PA K NONE O OTHER IN INSP/MAINT 1 WP 05 947WP 23376 FOUND AFT CARGO COMPARTMENT SUPPORT ANGLE CRACKED ON UPPER FLANGE AT BS 772, RBL 20, WL 154. REMOVED AND REPLACED SUPPO RT ANGLE PER SRM 51-30-01. (X) 2 L 7 2 4F RT A16WE 1996080800188 19960808 00188 SO 1996 8 8 WTAA960145 1 19960716 A 3260 120025226501 CONTROL BOX EMB 120 EMB120RT SO LANDING GEAR FAILED A WTAA O OTHER N FALSE WARNING CR CRUISE 1 WP 17 250YV 120250 SFO - INTERMITTENT RED INDICATION ON LEFT MLG AND NLG A-SYSTEM ONLY IN-FLIGHT WITH GEAR HANDLE SELECTED UP. MAINTENANCE SWAPPED SYSTEM 'A' AND SYSTEM 'B' CONNECTORS ON BOTH GEARS AND DEFERRED SYSTEM 'A'. AIRCRAFT RETURNED TO SERVICE. MAI NTENANCE SUBSEQUENTLY CLEARED DEFERRAL BY REPLACING THE LANDING GEAR CONTROL BOX. (X) 2 L 7 2 4T RT A31SO 1996080800189 19960808 00189 EU 1996 8 8 WTAA960146 2 19960718 A 7320 8691691 TQ TEMP SENSOR BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110U 01514 WP LT ENG TTL VALVE CHAFED WIRE A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 17 103XV 747 SEA - POWER LOSS REPORTED ON LEFT ENGINE ON TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE FOUND CHAFED W IRE AT LEFT ENGINE TORQUE TEMP LIMITING VALVE. REPAIRED WIRE. ENGINE GROUND RUN NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T 4 T RT A21EU E4WE 1996080800190 19960808 00190 NE 1996 8 8 9616825523 2 19960802 A 7321 EEC BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE NR 2 ENGINE FAILED A NWAA E ENGINE SHUTDOWN X ENGINE FLAMEOUT CL CLIMB 1 GL 01 523US 23617 716405 DURING CLIMB, THE NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL AND THEN AUTO SHUTDOWN. AIRCRAFT RETURNED TO DEPARTURE AIR PORT AND LANDED WITHOUT FURTHER EVENT. GROUND MAINTENANCE INSPECTED ENGINE, NO DAMAGED NOTED. REPLACED THE NR 2 ENGINE SVA ACTUATOR AND ELECTRONIC ENGINE CONTROL UNIT. ENGINE GROUND RUN AND FOUND SERVICEABLE. 2 L 7 2 4F 4 F RT A2NM E17NE 1996080800191 19960808 00191 NE 1996 8 8 9616839863 2 19960801 A 7230 COMPRESSOR DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE NR 2 ENGINE FOD A NWAA A UNSCHED LANDING C F.O.D. CL CLIMB 1 GL 01 772NC 37509 3745 47774 696729 DURING CLIMB, THE RIGHT ENGINE EXPERIENCED A COMPRESSOR STALL. CREW RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINT ENANCE REPLACED RIGHT ENGINE, OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F RT A6WE E2EA 1996080800192 19960808 00192 NM 1996 8 8 9616846310 1 19960803 A 3350 CONNECTOR BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 670US 24225 DURING LINE CHECK, FOUND FLOOR EMERGENCY LIGHT INOPERATIVE FROM ROWS 21 THROUGH 31. REINSTALLED CONNECTOR, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1996080800193 19960808 00193 WP 1996 8 8 9616859613 1 19960803 A 7711 EPR TRANSMITTER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9A 52048 NE NR 1 ENGINE FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 613NW 47438 655396 DURING TAKEOFF, THE NR 1 ENGINE EPR INDICATOR BECAME INOPERATIVE. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 ENGINE EPR TRANSMITTER, OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F A6WE E2EA 1996080800194 19960808 00194 EU 1996 8 8 9616863218 1 19960802 A 3260 PROX SENSORS AIRBUS 320 A320211 3930320 EU GEAR DOORS DIRTY A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 318US 206 DURING APPROACH AFTER LANDING GEAR EXTENSION, THE GEAR DOORS DID NOT INDICATE CLOSED. CYCLED LANDING GEAR HANDLE AND AL L INDICATIONS WERE NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED LANDING GEAR DOOR PROXIMITY SENSORS, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996080800195 19960808 00195 NM 1996 8 8 9616872708 1 19960801 A 3244 TIRE BOEING 727 727225 1384077 NM NR 2 FAILED A NWAA A J UNSCHED LANDING DUMP FUEL O OTHER TO TAKEOFF 1 GL 01 817EA 22554 DURING TAKEOFF, THE NR 2 TIRE FRAGMENTED, FUEL WAS DUMPED AND RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE NR 1 AND NR 2 TIRES AND INSPECTED FLAPS AND NR 1 ENGINE FOR DAMAGE. 2 L 7 3 4F A3WE 1996080800196 19960808 00196 NM 1996 8 8 9616886304 1 19960803 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 664US 23819 DURING LINE CHECK, FOUND FLOOR EMERGENCY LIGHTS INOPERATIVE FROM LAVATORY DR 4L2 TO ROW 57 AND AT ROWS 72 AND 73. RECON NECTED WIRES, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1996080800197 19960808 00197 NM 1996 8 8 96FDEA01311 1 19960729 A 7600 65225847 BRACKET BOEING 727 7272D4 138407U NM PWA JT8 JT8D15 52051 NE BS 1163 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 287FE 21849 NR0360 AND 025, NR 1 ENG CONTROL QUADRANT SUPPORT CASTING CRACKED JUST FORWARD AND I/B OF THRUST CRACK. *S/D* REMOVED AND REPLACED NR 1 ENG CONTROL QUADRANT SUPPORT CASTING PER FEDEX MM 76-12-0, 71-21-22, 71-21-21, 78-30-15, 76-12-41 AND 71-00. 2 L 7 3 4F 4 F A3WE E2EA 1996080800198 19960808 00198 NM 1996 8 8 96FDEA01312 1 19960805 A 5320 65189154 WEB BOEING 727 7272D4 138407U NM BS 294.5-344 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 NR0447 AND 008, WHILE ACCESSING WEB FOR REPAIR ON NR0052, FOUND WEB TO BE CRACKED AND CORRODED AT BS 294.5 TO 344 WL 170 RBL 34. *S/D* REMOVED CORROSION ON WEB AND FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. FABRICATED WEB, USING OL D WEB AS A TEMPLATE, ALODINED, PRIMED AND PAINTED, INSTALLED WEB. 2 L 7 3 4F A3WE 1996080800199 19960808 00199 NM 1996 8 8 96FDEA1313 1 19960805 A 5753 652163476 SKIN BOEING 727 72722 1384002 NM AFT TE FLAP DELAMINATION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 NR0012 AND 001, RIGHT WING I/B AFT FLAP HAS TEMPORARY REPAIR THAT NEEDS TO BE MADE PERMANENT. *S/D* REPAIRED RIGHT WIN G I/B AFT FLAP IAW FEDEX SRM 51-40-6. 2 L 7 3 4F A3WE 1996080800200 19960808 00200 WP 1996 8 8 CALA9601112 1 19960802 A 2530 OVEN DOUG DC9 DC982 3022082 WP AFT GALLEY FIRE A CALA F ACTIVATE FIRE EXT. A FLAME/FIRE CR CRUISE 1 SW 09 13891 49102 SMOKE BEGAN COMING FROM AFT GALLEY OVENS WHILE EN ROUTE. A FIRE EXTINGUISHER WAS USED TO EXTINGUISH OVEN FIRE. THE AIR CRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AFT GALLEY OVENS AND FOUND PAPER BURN ED INSIDE OF OVENS. THE FIRE HAD BEEN CONTAINED TO INSIDE OF OVENS. THE PAPER WAS REMOVED AND OPERATION OF THE OVENS C HECKED GOOD. THE FIRE EXTINGUISHER WAS REMOVED AND REPLACED. 2 L 7 2 4F A6WE 1996080800201 19960808 00201 NM 1996 8 8 CALA9601113 1 19960803 A 2910 651784414 HYD LINE BOEING 727 727227 1384078 NM PRESS MODULE LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 70755 21366 AIRCRAFT LOST THE A-SYSTEM HYDRAULIC QUANTITY WHILE EN ROUTE. THE LOSS WAS ACCOMPANIED BY ILLUMINATION OF THE NR 1 A-PU MP PRESSURE LIGHT. THE HYDRAULIC QUANTITY LOSS AND HYDRAULIC SYSTEM FAILURE CHECKLISTS WERE ACCOMPLISHED AND THE AIRCRA FT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND HYDRAULIC PRESSURE LINE AT A-SYSTEM PRESSURE MODULE LEAKING. THE LINE WAS REPLACED USING FLEX LINE AND A DIP WAS ISSUED TO REPLACE THE FLEX LINE WITHIN 1200 HOURS OR 500 FLIGHTS. 2 L 7 3 4F A3WE 1996080800202 19960808 00202 WP 1996 8 8 CALA9601114 1 19960730 A 5521 SPAR NUT DOUG DC9 DC932 3022066 WP LT ELEVATOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND, LT ELEVATOR MOST OUTBOARD BOTTOM NUT ON SPAR CRACKED. THE NUT WAS REMOVED AND REPLACED PER MM 20-16-0 . 2 L 7 2 4F A6WE 1996080800203 19960808 00203 WP 1996 8 8 CALA9601115 1 19960713 A 5350 CLIPS DOUG DC9 DC982 3022082 WP TAILCONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15841 49581 THE TAILCONE EXTERIOR RELEASE HANDLE HAD EXCESSIVE PULL OUT OF CLIPS. THE TAILCONE EXTERIOR RELEASE HANDLE CLIPS WERE A DJUSTED IAW MM 53-53-00. 2 L 7 2 4F A6WE 1996080800204 19960808 00204 WP 1996 8 8 CALA9601116 1 19960719 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP BS 148.5-199 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15841 49581 INSPECTION FOUND FORWARD CABIN FLOOR SUPPORT CORRODED AT STA 148.5 TO 199. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 57 -30-0. 2 L 7 2 4F A6WE 1996080800205 19960808 00205 WP 1996 8 8 CALA9601117 1 19960719 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP BS 160-198 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15841 49581 INSPECTION FOUND FORWARD CABIN LT SIDE FLOORBOARD SUPPORT ANGLE CORRODED AT STA 160 TO 198, 5 INCHES INBOARD OF FORWARD ENTRY DOOR CUTOUT. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-2. 2 L 7 2 4F A6WE 1996080800206 19960808 00206 WP 1996 8 8 CALA9601118 1 19960719 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP BS 160-200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15841 49581 INSPECTION FOUND FORWARD CABIN RT SIDE FLOORBOARD SUPPORT CORRODED AT STA 160 TO 200. THE SUPPORT WAS REMOVED AND REPLA CED IAW SRM 51-10-03. 2 L 7 2 4F A6WE 1996080800207 19960808 00207 WP 1996 8 8 CALA9601119 1 19960719 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP BS 200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15841 49581 INSPECTION FOUND FORWARD CABIN FLOORBOARD SUPPORT AT AIRCRAFT CENTERLINE CORRODED AT STA 200. THE FLOOR SUPPORT WAS REM OVED AND REPLACED IAW SRM 51-10-03. 2 L 7 2 4F A6WE 1996080800208 19960808 00208 WP 1996 8 8 CALA9601120 1 19960719 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP BS 200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15841 49581 INSPECTION FOUND FORWARD CABIN RT SIDE FLOORBOARD SUPPORT CORRODED AT STA 200, 9 INCHES RIGHT OF CENTER TO RIGHT CENTER FLOOR TRACK. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-03. 2 L 7 2 4F A6WE 1996080800209 19960808 00209 WP 1996 8 8 CALA9601121 1 19960719 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP BS 148.5-199 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15841 49581 INSPECTION FOUND FORWARD CABIN FLOOR SUPPORT CORRODED AT STA 148.5 TO 199. THE FLOOR SUPPORT WAS REMOVED AND REPLACED I AW SRM 51-10-03. 2 L 7 2 4F A6WE 1996080800210 19960808 00210 WP 1996 8 8 CALA9601122 1 19960719 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP BS 180 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15841 49581 INSPECTION FOUND FORWARD CABIN FLOOR SUPPORT CORRODED, RT SIDE, STA 180. THE FLOOR SUPPORT WAS REMOVED AND REPLACED. 2 L 7 2 4F A6WE 1996080800211 19960808 00211 WP 1996 8 8 CALA9601123 1 19960719 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP BS 198-203 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15841 49581 INSPECTION FOUND FORWARD CABIN LT SIDE FLOORBOARD SUPPORT ANGLE CORRODED AT STA 198 TO 203. THE FLOOR SUPPORT WAS REMOV ED AND REPLACED IAW SRM 51-10-03. 2 L 7 2 4F A6WE 1996080800212 19960808 00212 SO 1996 8 8 COMA9610237 1 19960803 A 2910 HYD SYST EMB 120 EMB120RT SO LEFT REQD SERVICE A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 243CA 120212 LEFT HYDRAULIC RESERVOIR LOW FLUID LEVEL WARNING ILLUMINATED, QUANTITY INDICATOR IN YELLOW ZONE. INSPECTED AIRCRAFT FOR POSSIBLE HYDRAULIC LEAKS AND FOUND NONE. SERVICED HYDRAULIC SYSTEM TO PROPER LEVEL AND ACFT RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 1996080800213 19960808 00213 EU 1996 8 8 COMA9630140 1 19960803 A 6120 8210151 PCU SAAB SF340 SF340A 7850100 EU RT ENGINE MALFUNCTION A COMA K NONE O OTHER LD LANDING 1 SO 01 357CA 340A044 DURING TAKEOFF AND LANDING THE MAX PROPELLER RPM IS 1380. REPLACED THE RT PROPELLER CONTROL UNIT. 2 L 7 2 4T RT A52EU 1996080800214 19960808 00214 NM 1996 8 8 DHL96701008 1 19960730 A 3510 OXY REG VALVE BOEING 727 72730C 1384009 NM COCKPIT NOT OPEN A T DHLA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 701DH 19011 APPROXIMATELY 30 MIN AFTER TAKEOFF, THE O2 QUANITY DROPPED TP 200 PSI. SERVICED O2 PER M/M 12-15-11, FOUND REGULATOR VA LVE NOT FULLY OPEN. LEAK CHECK OK. 2 L 7 3 4F A3WE 1996080800215 19960808 00215 NM 1996 8 8 DHL96703003 1 19960801 A 2742 72970008 ACTUATOR BOEING 727 72730C 1384009 NM HORIZ STAB JAMMED A T DHLA K NONE O OTHER DE DESCENT 1 SO 01 703DH 19010 STABILIZER TRIM JAMMED FROM TOP OF DESCENT, WOULD NOT STRIM NOSE UP. COMPLIED WITH ALTERNATE PROCEDURE. CLEANED AND LU BED STAB TRIM JACKSCREW DUE TO EXCESSIVE MOISTURE. REPLACED MAIN STAM ACTUATOR, ACTUATED STAB TRIM FULL TRAVEL AND NO D EFECTS NOTED. 2 L 7 3 4F A3WE 1996080800216 19960808 00216 NM 1996 8 8 P5CA9600419 1 19960729 A 5320 LONGERON BOX WEB BOEING 747 747122 1384872 NM LT MLG WW DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 DAMAGED WEB AND STRINGER LEFT BODY GEAR WHEEL WELL LONGERON BOX BS 1460 AFT OF BRACKET FOR OVERWING SLIDE BOTTLE, NOT IN STALLED. FOUND ON BLOWN TIRE INSPECTION. REPAIRED PER BOEING SRM 51-40-02 AND 51-10-01. 2 L 7 4 4F A20WE 1996080800217 19960808 00217 NM 1996 8 8 P5CA9600420 1 19960729 A 5320 ANGLE BOEING 747 747122 1384872 NM LT MLG BENT A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 LEFT BODY GEAR HYDRAULIC BULKHEAD OUTBOARD SUPPORT ANGLE BENT FOUND DURING BLOWN TIRE INSPECTION. REMOVED FABRICATED AN D INSTALLED PER BOEING SRM 51-10-01. 2 L 7 4 4F A20WE 1996080800218 19960808 00218 NM 1996 8 8 P5CA9600421 1 19960729 A 3201 TIRE GUARD BOEING 747 747122 1384872 NM LT MLG DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 LEFT BODY GEAR WHEEL WELL VERTICAL TIRE GUARD UPPER WEB DAMAGED. FOUND ON BLOWN TIRE INSPECTION. REMOVED FABRICATED AN D REPLACED PER BOEING SRM 51-40-00. 2 L 7 4 4F A20WE 1996080800219 19960808 00219 NM 1996 8 8 P5CA9600422 1 19960729 A 3230 65B8157383 TORQUE TUBE BOEING 747 747122 1384872 NM LT MLG BENT A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 OUTBOARD FLAP DRIVE TORQUE TUBE BENT, WHIP GUARD BENT AND WHIP GUARD BRACKET BENT, BLOWN TIRE DAMAGE. REPLACED TORQUE T UBE WHIP GUARD AND BRACKET RIGGED FLAPS PER BOEING M/M 27-51-20. 2 L 7 4 4F A20WE 1996080800220 19960808 00220 NM 1996 8 8 P5CA9600423 1 19960729 A 5320 BRACKET BOEING 747 747122 1384872 NM LT MLG BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 SUPPORT BRACKETS BROKEN FOR LEFT BODY GEAR PRIORITY VALVE, FOUND ON BLOWN TIRE INSPECTION. REMOVED FABRICATED AND REPLA CED BRACKETS PER BOEING SRM 51-10-01. 2 L 7 4 4F A20WE 1996080800221 19960808 00221 NM 1996 8 8 P5CA9600424 1 19960729 A 5320 PRESSURE DECK BOEING 747 747122 1384872 NM BS 1355 PUNCTURED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 PUNTURE IN PRESSURE DECK, BENT STIFFENER AND GOUGED SPLICE PLATE LEFT BODY GEAR WHEEL WELL BS 1355 LBL 127.75, FOUND ON BLOWN TIRE INSPECTION. REPAIRED PER MA A5340-02:01. 2 L 7 4 4F A20WE 1996080800222 19960808 00222 NM 1996 8 8 P5CA9600425 1 19960729 A 5320 STIFFENER BOEING 747 747122 1384872 NM BS 1362 BENT A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 BENT PRESSURE DECK STIFFENERS BENT LEFT BODY GEAR WHEEL WELL BS 1362 ABOVE VERTICAL TIRE GUARD, FOUND ON BLOWN TIRE INSP ECTION. REPAIRED PER MA 53:40-01:01. 2 L 7 4 4F A20WE 1996080800223 19960808 00223 NM 1996 8 8 P5CA9600426 1 19960729 A 2613 356412400 OVERHEAT LOOP BOEING 747 747122 1384872 NM LT MLG WW CRIMPED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 CRIMPED OVER HEAT LOOP LEFT BODY GEAR WHEEL WELL PRESSURE DECK INBOARD, FOUND ON BLOWN TIRE INSPECTION. REPLACED LOOP A ND TESTED PER BOEING MAINT MANUAL 26-17-02. 2 L 7 4 4F A20WE 1996080800224 19960808 00224 NM 1996 8 8 P5CA9600427 1 19960729 A 5320 FITTING BOEING 747 747122 1384872 NM BS 1480 BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 BROKEN FITTING FOR LONGERON BOX SUPPORT ROD LEFT BODY GEAR WHEEL WELL BS 1480, FOUND ON BLOWN TIRE INSPECTION. REMOVED FABRICATED AND INSTALLED FITTING PER BOEING SRM 51-10-01. 2 L 7 4 4F A20WE 1996080800225 19960808 00225 NM 1996 8 8 P5CA9600428 1 19960729 A 5320 65B01865833 SUPPORT BOEING 747 747122 1384872 NM BS 1480 DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 DAMAGED FAIRING SUPPORT STRUCTURE FOR THE LEFT HAND WING TO BODY FAIRING BS 1480, FOUND ON BLOWN TIRE INSPECTION. REPLA CED SUPPORT STRUCTURE PER BOEING SRM 51-10-01. 2 L 7 4 4F A20WE 1996080800226 19960808 00226 NM 1996 8 8 P5CA9600429 1 19960729 A 5330 65B105097 PANEL BOEING 747 747122 1384872 NM BS 1480 DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 DAMAGED VERTICAL HONEYCOMB PANEL BS 1480 LEFT BODY GEAR WHEEL WELL, FOUND ON BLOWN TIRE INSPECTION. REPLACED PANEL PER BOEING SRM 51-10-01. 2 L 7 4 4F A20WE 1996080800227 19960808 00227 NM 1996 8 8 P5CA9600430 1 19960729 A 5320 FAIRING SUPPORT BOEING 747 747122 1384872 NM BS 1540 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 BENT FAIRING SUPPORT LEFT WING TO BODY FAIRING BS 1540, FOUND ON BLOWN TIRE INSPECTION. REPAIRED PER BOEING SRM 53-50-0 4, EDDY CURRENT INSPECTION REVEALED NO CRACKS. 2 L 7 4 4F A20WE 1996080800228 19960808 00228 NM 1996 8 8 P5CA9600431 1 19960729 A 5320 65B06755601 SUPPORT BOEING 747 747122 1384872 NM BS 1480-1500 DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 DAMAGED FAIRING SUPPORT STRUCTURE BL 0 FROM 1480 TO 1500, FOUND ON BLOWN TIRE INSPECTION. REPLACED SUPPORT STRUCTURE PE R BOEING SRM 51-10-01. 2 L 7 4 4F A20WE 1996080800229 19960808 00229 NM 1996 8 8 P5CA9600432 1 19960729 A 3232 65B130025 FITTING BOEING 747 747122 1384872 NM LT MLG ACT BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 BROKEN LEFT BODY GEAR INBOARD DOOR ACTUATOR FITTING, FOUND ON BLOWN TIRE INSPECTION. REPLACED FITTING PER BOEING SRM 51 -10-01. 2 L 7 4 4F A20WE 1996080800230 19960808 00230 NM 1996 8 8 P5CA9600433 1 19960729 A 3232 65B109145 ACTUATOR ROD BOEING 747 747122 1384872 NM LT MLG DOOR BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 BROKEN ACTUATOR ROD FOR THE LEFT BODY GEAR INBOARD DOOR, FOUND ON BLOWN TIRE INSPECTION. REPLACED ROD PER BOEING MAINT MANUAL 32-14-05. 2 L 7 4 4F A20WE 1996080800231 19960808 00231 NM 1996 8 8 P5CA9600434 1 19960729 A 3230 65B054201 BRACKET BOEING 747 747122 1384872 NM LT MLG BENT A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 BENT LEFT BODY GEAR LOWER DRAG STRUT SEGMENT BRACKET FOR BUNGEE, FOUND ON BLOWN TIRE INSPECTION. REPLACED BRACKET PER B OEING SRM 51-10-01. 2 L 7 4 4F A20WE 1996080800232 19960808 00232 NM 1996 8 8 P5CA9600435 1 19960729 A 3230 65B088025 BUNGEE BOEING 747 747122 1384872 NM LT MLG DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 DAMAGED BUNGEE ON LEFT BODY LANDING GEAR, FOUND ON BLOWN TIRE INSPECTION. REPLACED BUNGEE PER BOEING MAINT MANUAL 32-33 -16. 2 L 7 4 4F A20WE 1996080800233 19960808 00233 NM 1996 8 8 P5CA9600436 1 19960729 A 5330 65B0673229 PANEL BOEING 747 747122 1384872 NM FUSELAGE DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 DAMAGED PANEL NR 193B ADF PANEL 16.5 BY 18.5 AREA, FOUND ON BLOWN TIRE INSPECTION. REPLACED PANEL PER BOEING SRM 51-10- 01. 2 L 7 4 4F A20WE 1996080800234 19960808 00234 NM 1996 8 8 P5CA9600437 1 19960729 A 5330 65B067313 PANEL BOEING 747 747122 1384872 NM FUSELAGE DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 PANEL NR 193C HAS 2 AREAS OF DAMAGE, ONE IN THE CENTER OF PANEL 20 INCH CRACK, THE OTHER A 6 BY 7 HOLE, FOUND ON BLOWN T IRE INSPECTION. REPLACED PANEL PER BOEING SRM 51-10-01. 2 L 7 4 4F A20WE 1996080800235 19960808 00235 NM 1996 8 8 P5CA9600438 1 19960729 A 5330 65B067449 PANEL BOEING 747 747122 1384872 NM FUSELAGE PUNCTURED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 WING TO FUSELAGE PANEL 193D HAS 2 AREAS OF DAMAGE 1 AFT CENTER 32 BY 31.25, THE OTHER FORWARD LOWER 8 BY 2.5, FOUND ON B LOWN TIRE INSPECTION. REPLACED PANEL PER BOEING SRM 51-10-01. 2 L 7 4 4F A20WE 1996080800236 19960808 00236 NM 1996 8 8 P5CA9600439 1 19960729 A 5330 65B0673011 PANEL BOEING 747 747122 1384872 NM FUSELAGE DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 WING TO FUSELAGE PANEL 193F HAS AREA IN CENTER OF PANEL WITH NUMEROUS DENTS, FOUND ON BLOWN TIRE INSPECTION. REPLACED P ANEL PER BOEING SRM 51-10-01. 2 L 7 4 4F A20WE 1996080800237 19960808 00237 1996 8 8 P5CA9600440 2 19960731 A 7220 INLET PANEL BOEING 747 747123 1384873 NM NR 1 ENGINE DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 1 ENGINE INLET ACOUSTIC PANEL DENTED AT 4 O'CLOCK. REPAIRED PER BOEING SRM 54-34-03. 2 L 7 4 4F A20WE 1996080800238 19960808 00238 NM 1996 8 8 P5CA9600441 1 19960731 A 5414 SKIN BOEING 747 747123 1384873 NM NR 3 PYLON DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 3 PYLON RIGHT SIDE AFT MOUNT AREA SKIN DAMAGED BY SIDE COWLING. INSTALLED DOUBLER AND FILLER PER BOEING SRM 54-30-03 . 2 L 7 4 4F A20WE 1996080800239 19960808 00239 NM 1996 8 8 P5CA9600442 1 19960731 A 5230 SEAL DEPRESSOR BOEING 747 747123 1384873 NM CARGO DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 FORWARD CARGO COMPARTMENT AFT DOOR SEAL DEPRESSOR, PREVIOUS REPAIR CRACKED. REPLACED SEAL DEPRESSOR PER BOEING SRM 51-1 0-01. 2 L 7 4 4F A20WE 1996080800240 19960808 00240 NM 1996 8 8 P5CA9600443 1 19960731 A 5330 SKIN BOEING 747 747123 1384873 NM BS 2700 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 FUSELAGE SKIN CRACKED, LEFT SIDE ABOVE INBOARD ELEVATOR BS 2700. REPAIRED PER BOEING SRM 53-30-03. 2 L 7 4 4F A20WE 1996080800241 19960808 00241 NM 1996 8 8 P5CA9600444 1 19960731 A 5330 SKIN BOEING 747 747123 1384873 NM BS 3266 PUNCTURED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 FUSELAGE SKIN PUNCTURED BELOW AFT JACK PAD BS 2366 WL 220. REPAIRED PER BOEING SRM 53-30-03 FIG 1 A. 2 L 7 4 4F A20WE 1996080800242 19960808 00242 NM 1996 8 8 P5CA9600445 1 19960731 A 5320 BRACKET BOEING 747 747123 1384873 NM FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LEFT BODY GEAR FORWARD DOOR UPPER STOP PAD, BRACKET CRACKED ON FORWARD SIDE. REPLACED BRACKET PER BOEING SRM 51-30-02. 2 L 7 4 4F A20WE 1996080800243 19960808 00243 NM 1996 8 8 P5CA9600446 1 19960731 A 5400 FAIRING BOEING 747 747123 1384873 NM NR 4 PYLON WORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 4 PYLON INBOARD SIDE AFT FAIRING SECTION WORN NAC STA 270. FABRICATED AND INSTALLED NEW PART PER BOEING SRM 54-30-03 . 2 L 7 4 4F A20WE 1996080800244 19960808 00244 NE 1996 8 8 P5CA9600447 2 19960731 A 7270 RACEWAY BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE NR 4 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 662964 NR 4 ENGINE RIGHT SIDE RACEWAY BRACKET CRACKED ALONG WELD JOINT 2 TO 3 O'CLOCK POSITION. WELDED AND STRESS RELIEVED PER PRATT AND WHITNEY MAINT MANUAL 72-53-01. 2 L 7 4 4F 4 F A20WE E20EA 1996080800245 19960808 00245 NE 1996 8 8 P5CA9600448 2 19960731 A 7250 EXHAUST CASE BOEING 747 747123 1384873 NM PWA JT9 JT9D7F 52054 NE NR 1 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 663071 NR 1 ENGINE TURBINE EXHAUST CASE S-RAIL CRACKED AT 10 O'CLOCK. WELDED AND STRESS RELIEVED PER PRATT AND WHITNEY MAINT M ANUAL 72-53-01. 2 L 7 4 4F 4 F A20WE E20EA 1996080800246 19960808 00246 NM 1996 8 8 P5CA9600449 1 19960731 A 3260 CONTACT PLATE BOEING 747 747123 1384873 NM NLG CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NOSE LANDING GEAR SQUAT SWITCH CONTACT PLATE FASTENERS LOOSE AND PLATE BENT. ALSO, REINFORCEMENT PLATE CRACKED. REMOVE D FABRICATED AND REINSTALLED CONTACT PLATE AND REINFORCEMENT PLATE PER BOEING SRM 51-10-01. 2 L 7 4 4F A20WE 1996080800247 19960808 00247 NM 1996 8 8 P5CA9600450 1 19960731 A 5753 SKIN BOEING 747 747123 1384873 NM NR 1 TE MIDFLAP LOOSE RIVETS A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 FASTENERS LOOSE LEFT WING OUTBOARD MIDFLAP UPPER SURFACE LEADING EDGE AREA BY NR 2 FLAP TRACK. REPLACED OR RESET RIVETS PER BOEING SRM 51-30-02. 2 L 7 4 4F A20WE 1996080800248 19960808 00248 NM 1996 8 8 P5CA9600451 1 19960731 A 5330 SKIN BOEING 747 747123 1384873 NM FUSELAGE LOOSE RIVETS A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 FUSELAGE EXTERIOR ABOVE LEFT APU ACESS DOOR WORKING FASTENERS. REPLACED FASTENERS PER BOEING SRM 51-30-02. 2 L 7 4 4F A20WE 1996080800249 19960808 00249 NE 1996 8 8 P5CA9600452 2 19960731 A 7250 TURBINE EXHAUST BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE NR 2 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 662336 NR 2 ENGINE S-RAIL CRACKED 5 TO 7 O'CLOCK. WELDED AND STRESS RELIEVED PER PRATT AND WHITNEY MAINT MANUAL 72-53-01. 2 L 7 4 4F 4 F A20WE E20EA 1996080800250 19960808 00250 NE 1996 8 8 P5CA9600453 2 19960731 A 7250 TURBINE EXHAUST BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE NR 2 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 662336 NR 2 ENGINE TURBINE EXHAUST CASE R-RAIL RADIAL CRACK AT 6 O'CLOCK POSITION. WELDED AND STRESS RELIEVED PER PRATT AND WH ITNEY MAINT MANUAL 72-53-01. 2 L 7 4 4F 4 F A20WE E20EA 1996080800251 19960808 00251 NM 1996 8 8 P5CA9600454 1 19960801 A 7110 65B0072250 NOSE COWL BOEING 747 747123 1384873 NM NR 2 ENGINE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 NR 2 ENGINE NOSE COWL TOP PANEL DELAMINATING. REPLACED NOSE COWL PER BOEING MAINT MANUAL 71-11-02. 2 L 7 4 4F A20WE 1996080800252 19960808 00252 1996 8 8 P5CA9600455 4 19960802 A 2360 STATIC WICK BOEING 747 747123 1384873 NM LT ELEVATOR NOT BONDED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LEFT OUTBOARD ELEVATOR OUTBOARD STATIC WICK NOT BONDED TO ELEVATOR. REPAIRED PER BOEING SRM 51-10-01 AND MAINTENANCE MA NUAL 51-60-00. 2 L 7 4 4F A20WE 1996080800253 19960808 00253 NM 1996 8 8 P5CA9600456 1 19960802 A 5730 PANEL BOEING 747 747123 1384873 NM LT WING PUNCTURED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LEFT WING TRAILING EDGE LOWER SURFACE PUNCTURE IN PANEL 581HB. REPAIRED PER BOEING SRM 51-40-15. 2 L 7 4 4F A20WE 1996080800254 19960808 00254 NM 1996 8 8 P5CA9600457 1 19960802 A 5522 SKIN BOEING 747 747123 1384873 NM RT ELEVATOR DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 DELAMINATION ON RIGHT OUTBOARD ELEVATOR OUTBOARD AFT CORNER. REPAIRED PER BOEING SRM 51-40-15. 2 L 7 4 4F A20WE 1996080800255 19960808 00255 NM 1996 8 8 P5CA9600458 1 19960802 A 7120 NUT BOEING 747 747123 1384873 NM NR 4 ENGINE SLIPPAGE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 4 ENGINE LEFT TANGENTIAL LINK AND RIGHT TANGENTIAL LINK SLIPPAGE MARK NOT IN ALIGNMENT. REPLACED NUT AND RETORQUED P ER P AND W MAINTENANCE MANUAL 71-21-04. 2 L 7 4 4F A20WE 1996080800256 19960808 00256 NM 1996 8 8 P5CA9600459 1 19960802 A 4940 BATTERY COMPT BOEING 747 747123 1384873 NM APU BENT A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 OUTBOARD FLANGE BENT APU BATTERY COMPARTMENT. REPAIRED PER BOEING SRM 51-30-02 AND 51-10-01. 2 L 7 4 4F A20WE 1996080800257 19960808 00257 NM 1996 8 8 P5CA9600460 1 19960801 A 5321 FLOOR BOEING 747 747123 1384873 NM BS 1680 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 CRACKED FLOOR PANEL AFT CARGO COMPARTMENT BS 1680 AT CENTER LOCK. REPAIRED PER BOEING SRM 51-30-02. 2 L 7 4 4F A20WE 1996080800258 19960808 00258 NM 1996 8 8 P5CA9600461 1 19960802 A 5522 SKIN BOEING 747 747123 1384873 NM LT ELEVATOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 CRACK LEFT INBOARD ELEVATOR ON UPPER SURFACE AT OUTBOARD END. REPAIRED PER BOEING SRM 51-40-15. 2 L 7 4 4F A20WE 1996080800259 19960808 00259 NM 1996 8 8 P5CA9600462 1 19960802 A 3250 TORQUE LINK BOEING 747 747123 1384873 NM NLG STEERING GOUGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 GOUGED NOSE LANDING GEAR TORQUE LINK ON RIGHT TOP SIDE. REPAIRED PER BOEING SRM 51-10-02 AND 51-10-01. 2 L 7 4 4F A20WE 1996080800260 19960808 00260 NM 1996 8 8 P5CA9600463 1 19960802 A 5522 TE WEDGE BOEING 747 747123 1384873 NM RT ELEVATOR DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 DELAMINATED TRAILING EDGE WEDGE RIGHT INBOARD ELEVATOR 3 FOOT BY 6 INCH AREA. REPAIRED PER BOEING SRM 51-40-15. 2 L 7 4 4F A20WE 1996080800261 19960808 00261 NM 1996 8 8 P5CA9600464 1 19960802 A 5730 PANEL BOEING 747 747123 1384873 NM LT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 DELAMINATED LEFT WING TRAILING EDGE PANEL AFT OF NR 1 PYLON. REPAIRED PER BOEING SRM 51-40-09. 2 L 7 4 4F A20WE 1996080800262 19960808 00262 NM 1996 8 8 P5CA9600465 1 19960802 A 3610 65B5113410 DUCT BOEING 747 747123 1384873 NM NR 1 ACM CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 CRACKED Y-DUCT AT NR 1 AIR CYCLE MACHINE PACKAGE INBOARD FORWARD. REPLACED DUCT PER BOEING MAINTENANCE MANUAL 36-11-01. 2 L 7 4 4F A20WE 1996080800263 19960808 00263 NM 1996 8 8 P5CA9600466 1 19960802 A 2612 FIRE WIRE BOEING 747 747123 1384873 NM NR 3 ENGINE WORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 WIRES WORN THROUGH ON NR 3 ENGINE FIRE LOOP AT HYDRAULIC LINE BOX FORWARD BRACKET AT 3 O'CLOCK POSITION. REPLACED WIRIN G PER BOEING WIRING STANDARD PRACTICES MANUAL 20-10-13. 2 L 7 4 4F A20WE 1996080800264 19960808 00264 NM 1996 8 8 P5CA9600467 1 19960802 A 3020 65B901827 ANTI-ICE DUCT BOEING 747 747123 1384873 NM NR 3 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 3 ENGINE NOSE COWL ANTI-ICE DUCT CRACKED NEAR PRESSURE SWITCH SENSE LINE ATTACHMENT INSIDE PYLON. REPLACED DUCT PER BOEING MAINTENANCE MANUAL 30-21-06. 2 L 7 4 4F A20WE 1996080800265 19960808 00265 NM 1996 8 8 P5CA9600468 1 19960802 A 5522 ELEVATOR BOEING 747 747123 1384873 NM LT ELEVATOR DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LEFT INBOARD ELEVATOR TRAILING EDGE HAS SMALL DELAMINATION AT PREVIOUS REPAIR. REPAIRED PER BOEING SRM 51-40-09. 2 L 7 4 4F A20WE 1996080800267 19960808 00267 NM 1996 8 8 P5CA9600470 1 19960803 A 2710 CONTROL CABLE BOEING 747 747123 1384873 NM BS 410 FAILED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 RIGHT WHEEL WELL FORWARD BULKHEAD BS 1283 CABLE FOUND LOOSE. UPON INVESTIGATION FOUND CABLE BIRD CAGED BY PULLEY AT BS 410 RBL 90 WL 210. REPLACED CONTROL CABLE PER BOEING MAINTENANCE MANUAL 20-11-03 AND 27-11-00. 2 L 7 4 4F A20WE 1996080800268 19960808 00268 EU 1996 8 8 QXEA9600273 1 19960802 A 3350 1820 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 457US 11036 EMERGENCY LIGHT OVER LEFT WING EXIT INOP. BULBS WERE REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996080800269 19960808 00269 NM 1996 8 8 SCNA96210 1 19960712 A 3350 LIGHT BOEING 727 727251 138408H NM CABIN SHORTED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 280US 21159 EMERGENCY EXIT CIRCUIT BREAKER TRIPPED. CLEARED SHORTED 28 VOLT TAB AT RIGHT FORWARD OVER WING LIGHT ASSEMBLY, OPS CHEC KED OK. 2 L 7 3 4F A3WE 1996080800270 19960808 00270 NM 1996 8 8 SWAA960703 1 19960723 A 5315 FLOOR BEAM BOEING 737 7372H4 138448C NM BS 203 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED D-CHECK, FOUND COCKPIT FLOOR BEAM CORROSION AT BS 203 WL 208 RBL 12 TO 18. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996080800271 19960808 00271 NM 1996 8 8 SWAA960704 1 19960723 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 727 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME DENTED AT BS 727A PLUS 16 TO 19 AT S20L. INSTALLED DOUBLER REPAIR PER BO EING SRM. 2 L 7 2 4F A16WE 1996080800272 19960808 00272 NM 1996 8 8 SWAA960705 1 19960723 A 5320 CHORD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED D-CHECK, FOUND CRACK IN SIDE CHORD FROM WL 194 TO 195, BS 178, LEFT. REPLACED CHORD PER BOEING SRM. 2 L 7 2 4F A16WE 1996080800273 19960808 00273 NM 1996 8 8 SWAA960706 1 19960723 A 5320 CHORD BOEING 737 7372H4 138448C NM BS 616 DAMAGE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED D-CHECK, FOUND FRAME WEB DAMAGED AT BS 616 RBL 170, WL 221. INSTALLED DOUBLER REPAIR PER BOEING SRM. 2 L 7 2 4F A16WE 1996080800274 19960808 00274 NM 1996 8 8 SWAA960707 1 19960723 A 5320 STRAP BOEING 737 7372H4 138448C NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM STRAP CORRODED AT BS 328 RBL 5 WL 208. INSTALLED NEW STRAP PER BOEING SRM. 2 L 7 2 4F A16WE 1996080800275 19960808 00275 NM 1996 8 8 SWAA960708 1 19960723 A 5315 FLOOR BEAM BOEING 737 7372H4 138448C NM BS 294 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORRODED AT BS 294 RBL 15, 27, 39, 44.5 AND 46.5. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996080800276 19960808 00276 NM 1996 8 8 SWAA960709 1 19960723 A 5315 FLOOR BEAM BOEING 737 7372H4 138448C NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORRODED AT BS 312, LBL 7 AND AT BL 0, WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996080800277 19960808 00277 NM 1996 8 8 SWAA960710 1 19960723 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 967 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED D-CHECK, FOUND MOP SILL FLOOR STIFFENER ANGLE BS 967 TO 987.5 RBL 46, WL 207. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996080800278 19960808 00278 NM 1996 8 8 SWAA960711 1 19960723 A 5320 SILL BOEING 737 7372H4 138448C NM BS 967-992.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED D-CHECK, FOUND AFT SERVICE DOOR MOP SILL FLOOR CORRODED AT BS 967 TO 992.5, RBL 49 TO 47, WL 208 AND 20 9. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996080800279 19960808 00279 NM 1996 8 8 SWAA960712 1 19960723 A 5315 FLOOR BEAM BOEING 737 7372H4 138448C NM BS 987.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORRODED AT BS 987,5, LBL 40, WL 208 AT RBL 40, WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996080800280 19960808 00280 NM 1996 8 8 SWAA960713 1 19960723 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 318 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 318, BETWEEN S2L AND S3L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996080800281 19960808 00281 NM 1996 8 8 SWAA960714 1 19960723 A 5313 STRINGERS BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED D-CHECK, FOUND STRINGERS CRACKED AT S16 AT WING ICE LIGHT CUTOUT. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996080800282 19960808 00282 NM 1996 8 8 SWAA960715 1 19960723 A 5320 SPLICE BOEING 737 7372H4 138448C NM BS 359 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED D-CHECK, FOUND STRINGER END SPLICE CRACKED AT BS 359, S14L, UPPER AND LOWER FASTENER HOLES. REPLACED P ER BOEING SRM. 2 L 7 2 4F A16WE 1996080800283 19960808 00283 NM 1996 8 8 SWAA960716 1 19960723 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 303.9 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED D-CHECK, FOUND FRAME WEB CRACKED AT BS 303.9, JUST BELOW S16L. REPLACED WEB PER BOEING SRM. 2 L 7 2 4F A16WE 1996080800284 19960808 00284 NM 1996 8 8 SWAA960717 1 19960723 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 847 DAMAGE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DAMAGE AT BS 847, RBL 12, S26 TO 25R. INSTALLED REPAIR DOUBLER PER BOEING SRM. 2 L 7 2 4F A16WE 1996080800285 19960808 00285 NM 1996 8 8 SWAA960718 1 19960723 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 1016 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 1016, BETWEEN 18 AND 19R. INSTALLED REPAIR DOUBLER PER BOEIN G SRM. 2 L 7 2 4F A16WE 1996080800286 19960808 00286 NM 1996 8 8 SWAA960719 1 19960723 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 328 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 87SW 22903 DURING SCHEDULED 1/2 D-CHECK, FOUND FWD GALLEY WEB UPPER ANGLE CRACKED BS 328, RBL 32. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996080800287 19960808 00287 NM 1996 8 8 SWAA960720 1 19960723 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 87SW 22903 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM UPPER FLANGE CORRODED AT BS 344 LBL 4 TO 22. REPLACED T-CAP PER BOEING S RM. 2 L 7 2 4F A16WE 1996080800288 19960808 00288 NM 1996 8 8 SWAA960721 1 19960723 A 5315 FLOOR BEAM BOEING 737 7372H4 138448C NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 87SW 22903 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM CORRODED AT BS 344, ON LOWER SURFACE OF SCREW HOLES, LBL 25 TO 38. REPLA CED T-CAP PER BOEING SRM. 2 L 7 2 4F A16WE 1996080800289 19960808 00289 NM 1996 8 8 SWAA960722 1 19960723 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 87SW 22903 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM UPPER FLANGE CORRODED AT BS 344 LBL 4 TO 22. REPLACED T-CAP PER BOEING S RM. 2 L 7 2 4F A16WE 1996080800290 19960808 00290 NM 1996 8 8 SWAA960723 1 19960724 A 3350 20121 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 379SW 26586 DURING SCHEDULED SERVICE CHECK, FOUND RIGHT AFT SERVICE EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996080800291 19960808 00291 NM 1996 8 8 SWAA960724 1 19960724 A 5315 FLOOR BEAM BOEING 737 7372H4 138448C NM BS 294 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 87SW 22903 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM UPPER FLANGE SCREW HOLE CORROSION AT BS 294, LBL 25. REPLACED T-CAP PER BOEING SRM AND TI 253-008. 2 L 7 2 4F A16WE 1996080800292 19960808 00292 NM 1996 8 8 SWAA960725 1 19960724 A 5311 BELTFRAME BOEING 737 7372H4 138448C NM BS 639 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 92SW 22964 DURING SCHEDULED B-CHECK, FOUND BELTFRAME CRACKED AT BS 639 AND S17R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996080800293 19960808 00293 NM 1996 8 8 SWAA960726 1 19960724 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 907 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 221811 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CORROSION AT BS 907, RBL 5.5, WL 165. REPLACED CORRODED SECTION PER BOE ING SRM. 2 L 7 2 4F A16WE 1996080800294 19960808 00294 NM 1996 8 8 SWAA960727 1 19960724 A 5320 STRAP BOEING 737 7372H4 138448C NM BS 1138 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 221811 DURING SCHEDULED D-CHECK, FOUND FUSE RT HORIZONTAL STRAPS CRACKED AT BS 1138, S12L AND 12R. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996080800295 19960808 00295 NM 1996 8 8 SWAA960728 1 19960724 A 5320 STRAP BOEING 737 7372H4 138448C NM BS 1138 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 221811 DURING SCHEDULED D-CHECK, FOUND FUSE LT HORZIZONTAL STRAP CRACKED AT BS 1138, S5. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996080800296 19960808 00296 NM 1996 8 8 SWAA960729 1 19960724 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 787 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 221811 DURING SCHEDULED D-CHECK, FOUND STRINGER DAMAGE AT BS 787, S16R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996080800297 19960808 00297 NM 1996 8 8 UPS96220719 1 19960722 A 5753 65192029 CARRIAGE BOEING 727 727180C 138406G NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE SI, CORROSION (C53-581-04.00-03) NR 2 CARRIAGE IS CORRODED AT THRUST WASHER MATING SURFACE. REMOVED AND REPLACED CARRIAGE WITH ROTABLE UNIT. 2 L 7 3 4F A3WE 1996080800298 19960808 00298 NM 1996 8 8 UPS96220721 1 19960722 A 5753 651859929 CARRIAGE BOEING 727 727180C 138406G NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE SI, CORROSION (C57-581-04.00-03) NR 4 CARRIAGE HAS COOROSION ON THRUST WASHER MATING SURFACE. REMOVED A ND REPLACED CARRIAGE 34 WITH ROTOABLE UNIT. 2 L 7 3 4F A3WE 1996080800299 19960808 00299 NM 1996 8 8 UPS96220722 1 19960723 A 5320 CLIP BOEING 727 727180C 138406G NM BS 600 CORRODED A IPXA O OTHER O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE SI, CORROSION (C53-111-01.00-02) ON STRINGER CLIP RBL 64 STA 600 WL 198 STR 18. REMOVED CORROSION, REWO RK DEEMED OUT OF LIMITS IAW SRM 53-10-1. FABRICATED THEN REPLACED STR 18 STA 600 STRINGER CLIP IAW SRM 51-10-2, 51-30-5 , 53-30-3. 2 L 7 3 4F A3WE 1996080800300 19960808 00300 NM 1996 8 8 UPS96220723 1 19960723 A 5315 FLOOR BEAM BOEING 727 727180C 138406G NM BS 312 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE SI, CORROSION (C53-224001.05-01) ON TOP AND BOTTOM FLOOR BEAM AROUND NUTPLATE HOLE AT STA 312 LBL 25 WL 208. MECHANICALLY REMOVED CORROSION, REWORK DEEMED OUT LIMITS IAW SRM 53-10-1. REPAIRED CORROSION DAMAGE REWORK ON STA 312 FLOOR BEAM LBL 25 IAW SRM 53-10-8. 2 L 7 3 4F A3WE 1996080800301 19960808 00301 NM 1996 8 8 UPS96220724 1 19960723 A 5754 RIB BOEING 727 727180C 138406G NM NR 4 SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE SI, NR 4 SLAT 5TH RIB FROM I/B END IS CRACKED AT NUTPLATE. REPAIRED NR 4 SLAT 5TH RIB FROM I/B END SRM 57-50-3. 2 L 7 3 4F A3WE 1996080800302 19960808 00302 NM 1996 8 8 UPS96220725 1 19960723 A 5755 65173481 SKIN BOEING 727 727180C 138406G NM NR 6 SPOILER DISBONDING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE SI, NR 6 SPOILER SHOWS HONEYCOMB SEPARATION ALONG FWD EDGE AND WATER ENTRAPMENT IN VIEW 5. REPAIRED NR 6 SPOILER IAW SRM 57-50-6. 2 L 7 3 4F A3WE 1996080800303 19960808 00303 NM 1996 8 8 UPS96220729 1 19960724 A 5741 69139017 BOTTLE PIN BOEING 727 727180C 138406G NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE SI, CORROSION (C53-100-05-4B) RT WING AFT BOTTLE PIN RUSTED AND PITTED AT INTERNAL MATING SURFACE. REMO VED AND REPLACED BOTTLE PIN IAW T/C C53-100-05-4D. 2 L 7 3 4F A3WE 1996080800304 19960808 00304 NM 1996 8 8 UPS96220730 1 19960724 A 5347 SEAT TRACK BOEING 727 727180C 138406G NM BS 786 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE SI, CORROSION IN SEAT TRACK LBL 25 STA 786 TO 848 WL 208. MECHANICALLY REMOVED CORROSION, REWORK DEEMED OUT LIMITS IAW SRM 53-10-1. REMOVED AND REPLACED SEAT TRACK FROM STA 786 TO 848 LBL 25 IAW 51-30-2, 53-10-5. 2 L 7 3 4F A3WE 1996080800305 19960808 00305 NM 1996 8 8 UPS96220733 1 19960724 A 2730 692149923 RETURN SPRING BOEING 727 727180C 138406G NM ELEVATOR CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE SI, ELEVATOR CONTROL CENTERING UNIT RETURN SPRINGS ARE CORRODED. REMOVED AND REPLACED ELEVATOR CONTROL CENTERING UNIT RETURN SPRINGS PER M/M 27-30-71. 2 L 7 3 4F A3WE 1996080800306 19960808 00306 NM 1996 8 8 UPS96220734 1 19960724 A 5311 FRAME BOEING 727 727180C 138406G NM BS 352 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE SI, CORROSION (C53-111-01.00-01) ON FORWARD SIDE OF FRAME STA 352 RBL 13 TO 32 WL 168. MECHANICALLY REM OVED CORROSION PER SRM 51-10-6 FOUND OUT OF LIMITS PER SRM 53-10-1, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-40- 2, 51-20-1, 51-10-2, 51-10-6, 51-30-2. 2 L 7 3 4F A3WE 1996080800307 19960808 00307 NM 1996 8 8 UPS96220735 1 19960725 A 5320 651862222 INTERCOSTAL BOEING 727 727180C 138406G NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE SI, AFT CARGO DOOR AFT HINGE FUSELAGE INTERCOSTAL IS CRACKED AT HINGE MOUNT. REMOVED AND REPLACED AFT C ARGO DOOR AFT HINGE FRAME INTERCOSTAL IAW SRM 51-10-1, 51-10-2, 51-30-2, 51-20-1. 2 L 7 3 4F A3WE 1996080800308 19960808 00308 NM 1996 8 8 UPS96220736 1 19960720 A 5754 INNER WEB BOEING 727 72751C 1384015 NM NR 3 SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-C, NR 3 SLAT INNER WEB AT ACTUATOR CRACKED ON BOTH SIDES. STOP DRILLED CRACKS PER SRM 51-10-1, FABRICAT ED AND INSTALLED WEB REPAIR PER SRM 51-40-3 AND 57-50-1. 2 L 7 3 4F A3WE 1996080800309 19960808 00309 NM 1996 8 8 UPS96220737 1 19960727 A 5320 WEB BOEING 727 72751C 1384015 NM FS 251.6 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-C, NLG WHEEL WELL LEFT SIDE WEB IS CRACKED AT FS 251.6. REMOVED, FABRICATED AND INSTALLED WEB PER SRM 5 1-40-2 AND 51-30-2. 2 L 7 3 4F A3WE 1996080800310 19960808 00310 NM 1996 8 8 UPS96220738 1 19960722 A 5754 K-FLAP BOEING 727 72751C 1384015 NM NR 1 LE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-C, NR 1 K-FLAP 6 INCHES O/B OF I/B HINGE, WEB L/E INSIDE HAS A 3 INCH CRACK. REMOVED, FABRICATED REPLAC EMENT PART AND INSTALLED IAW 57-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 1996080800311 19960808 00311 NM 1996 8 8 UPS96220739 1 19960726 A 5330 SKIN BOEING 727 72751C 1384015 NM FS 850-870 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-C, MAIN CABIN FS 850 TO 870 BL 0 TO LBL 45 CENTER TANK UPPER PRESSURE SKIN HAS CORROSION. REMOVED AND A REA NOTED WAS SUBMITTED TO ENG FOR REPAIR. FLAP PEENING DAMAGE AREA PER DHC SK 904-400-AND BOEING M/M 20-10-3. ALODINE AND PRIMED STRUCTURE AND REINSTALLED FASTENERS PER SK 904-400 AND SRM 51-20-4. 2 L 7 3 4F A3WE 1996080800312 19960808 00312 NM 1996 8 8 UPS96220740 1 19960726 A 2782 ACTUATOR RIBS BOEING 727 72751C 1384015 NM NR 3 SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-C, NR 3 SLAT INBD AND OTBD ACTUATOR ATTACH RIBS ARE CRACKED. REMOVED, FABRICATED AND INSTALLED RIBS PER SRM 57-50-2, 51-30-2 AND BOEING DWG 65-17240. 2 L 7 3 4F A3WE 1996080800313 19960808 00313 NM 1996 8 8 UPS96220741 1 19960726 A 2782 SUPPORT CHANNEL BOEING 727 72751C 1384015 NM NR 3 SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-C, NR 3 SLAT ACTUATOR SUPPORT CHANNEL BETWEEN I/B AND O/B ACTUATOR. REMOVED, FABRICATED AND INSTALLED C HANNEL PER DWG 65-17294 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996080800314 19960808 00314 NM 1996 8 8 UPS96220742 1 19960717 A 5320 WEB BOEING 727 72751C 1384015 NM BS 1263-1270 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-C, THE RT LWR TORQUE BOX I/B WEB AT STA 1263 TO 1270 HAS 4 CRACKS AT RIVET HOLE AND 3 CRACKS PAST STOOP DRILLS. REPAIRED I/B TORQUE BOX WEB AND INSTALLED THE 65-17510-313 AND 65-175 10-314. 2 L 7 3 4F A3WE 1996080800315 19960808 00315 NM 1996 8 8 UPS96220743 1 19960725 A 5347 SEAT TRACK BOEING 727 72751C 1384015 NM BS 740-760 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-C, SEAT TRACK AT BS 740 TO 760 LBL 44.5 IS CORRODED AND CRACKED. REMOVED AND REPAIRED TRACK PER SRM 51- 30-2. 2 L 7 3 4F A3WE 1996080800316 19960808 00316 NM 1996 8 8 UPS96220745 1 19960703 A 5741 69139017 BOTTLE PIN BOEING 727 72722C 138400F NM LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE-C, SLIGHT SURFACE CORROSION ON INNER SURFACE OF LT REAR BOTTLE PIN. NEW BOTTLE PIN INSTALLED IAW MM 57- 41-01. 2 L 7 3 4F A3WE 1996080800317 19960808 00317 NM 1996 8 8 UPS96220746 1 19960705 A 5311 FRAME BOEING 727 72722C 138400F NM BS 600 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE-C, CORROSION ON FRAME BS 600 ADJACENT TO STR 26L. CORROSION REMOVED AND FOUND TO BE OUT OF LIMITS IAW S RM 51-10-01. FRAME REPAIRED IAW SRM 53-10-4 FIG 1. 2 L 7 3 4F A3WE 1996080800318 19960808 00318 NM 1996 8 8 UPS96220747 1 19960703 A 5330 SKIN BOEING 727 72722C 138400F NM BS 1183 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE-C, CORROSION BETWEEN FUSELAGE SKIN AND FRAME AT BS 1183 BETWEEN 58L AND 59L. AREA PAINT STRIPPED IAW MM 51-20-1, FASTENERS REMOVED IAW SRM 51-30- 2, AREA BETWEEN BS 1183 AND 1166 BETWEEN 510L AND 58L INSPECTED IAW B7 27 NDT MANUAL 51-00-00 FIG 5. INTERNAL FOUND DISBONDED WITH SURFACE CORROSION ON BOTH SKIN AND DOUBLER. AREA REPAIRED IAW SR S EO 96-30-010. 2 L 7 3 4F A3WE 1996080800319 19960808 00319 NM 1996 8 8 UPS96220748 1 19960704 A 5320 WEB BOEING 727 72722C 138400F NM BS 292 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE-C, CRACK IN NOSE WHEEL WELL WEB, BS 292 RBL 30 WL 180 APPROX. HFEC CARRIED OUT TO CONFIRM CONTAINMENT O F CRACK BY STOPDRILL IAW B727 NDT MANUAL PART 6, 51-00-00 FIG 4, NO DEFECTS FOUND. REPAIR TO WEB IN NOSE WHEEL WELL CAR RIED OUT IAW SRS EO 96-30-002. 2 L 7 3 4F A3WE 1996080800320 19960808 00320 NM 1996 8 8 UPS96220749 1 19960703 A 5330 SKIN BOEING 727 72722C 138400F NM BS 1183 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE-C, CORROSION BETWEEN FUSELAGE SKIN AND S17L, BS 1183. REMOVED SKIN PANEL, REPAIRED IAW SRS EO 96-30-015 . 2 L 7 3 4F A3WE 1996080800321 19960808 00321 NM 1996 8 8 UPS96220750 1 19960717 A 5330 SKIN BOEING 727 72722C 138400F NM BS 1183-1080 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE-C, CORROSION AND DISBOND ON FUSELAGE SKIN AND DOUBLER BS 1183 TO 1080 BETWEEN S20R AND 26R. SKIN PANEL DERIVETED IAW SRM 51-30-02. SKIN PANEL AND DOUBLER INSPECTED USING LFEC IAW B727 NDT MANUAL, PART 6 51-00-00 FIG 5, MAT ERIAL LOSS OF 10 TO 30 PERCENT INDICATED ALONG LENGTH INSPECTED. DOUBLER FOUND TO BE BOTH CORRODED AND DISBONDED SKIN P ANEL REPAIRED IAW SRS EO 96-30-13. 2 L 7 3 4F A3WE 1996080800322 19960808 00322 NM 1996 8 8 UPS96220751 1 19960703 A 5330 SKIN BOEING 727 72722C 138400F NM BS 1085 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE-C, CORROSION ON FUSELAGE SKIN BS 1085 BETWEEN STR 12L AND BL AREA PAINT STRIPPED IAW MM 51-20-1, AREA RE INSPECTED FOUND TO BE CORRODED AND DAMAGED. SKIN AT BS 1080 TO 1160 BETWEEN S10L & S14L DERIVETED IAW SRM 51-30-2, SKIN PANEL REPAIRED IAW SRS EO 96-30-004. 2 L 7 3 4F A3WE 1996080800323 19960808 00323 NM 1996 8 8 UPS96220752 1 19960725 A 5712 RIBS BOEING 727 72722C 138400F NM WS 656.5L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE-C, TWO HYDROPRESSED RIBS WERE FOUND CRACKED. CRACKED RIBS REPLACED WITH BUILT-UP RIBS, PER ABOVE EO O/S FASTENERS INSTALLED PER SRS EO 96-30-012. 2 L 7 3 4F A3WE 1996080800324 19960808 00324 NM 1996 8 8 UPS96220753 1 19960703 A 5330 SKIN BOEING 727 72722C 138400F NM BS 1090-1110 DELAMINATION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE-C, DELAMINATION AT BS 1090 TO 1110 BETWEEN STR 11 AND 12 RT SIDE. FOKKER BOND INSP CARRIED OUT ON TWO S USPECT AREAS OF METAL TO METAL DISBOND IAW B727 NDT MANUAL PART 4 51-40-00 FIG 1. BOTH AREAS INDICATE DISBONDING SKIN P ANEL AND DOUBLER INSPECTED. SKIN PANEL REPAIRED IAW SRS EO 96-30-008. 2 L 7 3 4F A3WE 1996080800325 19960808 00325 NM 1996 8 8 UPS96220754 1 19960731 A 5712 RIB BOEING 727 72722C 138400F NM WS 760 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE-C, A PREVIOUS REPAIR WAS DISCOVERED TO THE RBL 70.5 RIB CHORD AT 135 760. HOWEVER, A CRACK HAD PROGRESS ED SINCE THE ORIGINAL REPAIR INSTALLATION. REPAIR PER CARRIED OUT PER SB727-53-0112 (UPS EO 7275710-1271) WITH DEVIATIO NS OUTLINED IN SRS EO 96-30-016. 2 L 7 3 4F A3WE 1996080800326 19960808 00326 NM 1996 8 8 UPS96220755 1 19960711 A 5720 CLAMP RINGS BOEING 727 72722C 138400F NM LT/RT FUEL DOORS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE-C, FRETTING SURFACE CORROION ON LT AND RT WING FUEL TANK DOOR CLAMP RINGS. FUEL TANK DOOR CLAMP RINGS R EPLACED IAW MM 28-11. 2 L 7 3 4F A3WE 1996080800327 19960808 00327 NM 1996 8 8 UPS96220756 1 19960704 A 5751 SKIN BOEING 727 72722C 138400F NM LT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE-C, LT O/B AILERON HAS SKIN BULGE ON TOP SKIN I/B END. RIVETS REMOVED FROM AILERON SKIN I/B END IAW SRM 51-30-2, AILERON HINGE ASSM FOUND CORRODED. REPLACED HINGE ASSM IAW DWG 65-2176 AILERON RIGGED IAW 27-10-00. 2 L 7 3 4F A3WE 1996080800328 19960808 00328 NM 1996 8 8 UPS96220757 1 19960728 A 5320 VERT STRINGER BOEING 727 72722C 138400F NM WS 686.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE-C, VERT STRINGER FOUND CRACKED AT STR 13 TO 14 AT WS 686.5 LT. REPAIRED PER UPS EO B727-5710-0314-F. 2 L 7 3 4F A3WE 1996080800329 19960808 00329 NM 1996 8 8 UPS96220758 1 19960706 A 5320 DOUBLER BOEING 727 72722C 138400F NM PAX DOOR CUTOUT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE-C, FWD ENTRY DOOR CUTOUT HAS DOUBLER CRACK AT TOP FWD CORNER. REPAIR CARRIED OUT IAW EO B727-5330-1460 APPENDIX OPTION 1. 2 L 7 3 4F A3WE 1996080800330 19960808 00330 NM 1996 8 8 UPS96220759 1 19960728 A 5320 BODY JOINT BOEING 727 72722C 138400F NM BS 360 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE-C, BOLTS IN PRODUCTION JOINT AT BS 360 FOUND CORRODED DURING STRUCTURAL SAMPLE BELOW STR 21L AND 21R. B OLTS REPLACED AS REQUIRED BETWEEN STR 21L AND 21R AT BS 360 AND TORQUED IAW MM 553-11-00 PG 601, CRACK IN HOLE AT BS 360 O/B OF STR 28R REPAIRED IAW SRS EO 96-30-005. 2 L 7 3 4F A3WE 1996080800331 19960808 00331 NM 1996 8 8 UPS96220761 1 19960706 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 460-480 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE-D, STR 21R BS 460 TO 480. REPAIRED PER SRM 53-10-3. 2 L 7 3 4F A3WE 1996080800332 19960808 00332 NM 1996 8 8 UPS96220762 1 19960704 A 5320 SHEAR TIE BOEING 727 72722C 138400F NM BS 328 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE-D, SHEAR TIE CORRODED AND CRACKED ON ST 22L AT BS 328 LT SIDE. SHEAR TIE REPLACED SRM 53-10-2. 2 L 7 3 4F A3WE 1996080800333 19960808 00333 NM 1996 8 8 UPS96420744 1 19960710 A 5315 FLOOR BEAM BOEING 747 747123 1384873 NM BS 640 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE-C, MAIN DECK FLOOR BEAM UPPER CHORD CORRODED AT BS 640 BETWEEN RBL 33, 98 UPPER CHORD AT BS 640 BETWEEN RBL 33, 98. REPLACED IAW SRM 53-10-07 FIG 12 AND UPS EFN 747-53-0778, KLM DFX 96-150. 2 L 7 4 4F A20WE 1996080800334 19960808 00334 1996 8 8 UPS96620760 2 19960803 A 7261 9608M12POZ GASKET BOEING 767 76734AF 1385212 NM OIL PUMP MOUNT LEAKING A IPXA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 302UP 27240 INSPECTION TYPE N/A, SIMULATED LOSS OF OIL QUANTITY IN RIGHT ENGINE, ENG OIL PRESS LIGHT ILLUM, ENG OIL PRESS ZERO, ENG OIL QUANTITY ZERO. FOUND GASKET LEAKING AT OIL PUMP MOUNTING GASKET. REMOVED AND REPLACED GASKET IAW MM 79-21-03, NO OIL LEAKS NOTED. SERVICED OIL TANK WITH 18 QUART OF OIL. 2 L 7 2 4F RT A1NM 1996080800335 19960808 00335 WP 1996 8 8 UPS96820763 1 19960629 A 5315 5644657503 FLOOR BEAM DOUG DC8 DC871F 302199D WP BS 920 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-CS2, HEAVY CORROSION ON FS 920 FLOOR BEAM UPPER LEG AFT SIDE LBL 16. REPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996080800336 19960808 00336 WP 1996 8 8 UPS96820764 1 19960702 A 5315 5640915165 BEAM DOUG DC8 DC871F 302199D WP BS 780 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-CS2, HEAVY CORROSION FS 780 FLOOR BEAM UPPER LEG LBL 12. REPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996080800337 19960808 00337 WP 1996 8 8 UPS96820765 1 19960628 A 5320 5612298 DOUBLER DOUG DC8 DC871F 302199D WP BS 19-8 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-CS2, HEAVY CORROSION ON FUSELAGE NOSE SECTION PRESSURE DOUBLER STA 19 TO 8. REPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996080800338 19960808 00338 WP 1996 8 8 UPS96820766 1 19960627 A 5320 561229859 DOUBLER DOUG DC8 DC871F 302199D WP BS 52-42 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-CS2, HEAVY CORROSION ON SUBFLOOR AND FINGER DOUBLER AT LONGERON 24R FS 52 THROUGH 42. REPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996080800339 19960808 00339 WP 1996 8 8 UPS96820767 1 19960701 A 5347 DC853B013501 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 1707 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-CS2, CORROSION OUT OF LIMITS ON SEAT TRACK NR 5, FS 1707. REPLACED SEAT TRACK SECTION FS 1670 TO 1707 P ER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1996080800340 19960808 00340 WP 1996 8 8 UPS96820768 1 19960626 A 5320 3755822505N FITTING DOUG DC8 DC871F 302199D WP BS 340 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-CS2, HEAVY CORROSION ON BATH TUB FITTING AT FS 340, BETWEEN LONGERONS 27L TO 28L. REPLACED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996080800341 19960808 00341 WP 1996 8 8 Y2PA96054 1 19960801 A 5330 591141097 SKIN DOUG DC9 DC915F 3022037 WP BS 392 DENTED A Y2PA K NONE O OTHER IN INSP/MAINT 1 GL 23 567PC 47153 DURING C/D BRIDGING CHECK, FOUND DENT IN FUSELAGE SKIN AT STATION 392 BETWEEN L20 TO 21 LT 3 BY 3 BY.120. INSTALLED DOU BLER REPAIR IAW DC-9 SRM 53-04 FIG 38. N/R CARD 96-0264. 2 L 7 2 4F A6WE 1996080800342 19960808 00342 WP 1996 8 8 Y2PA96055 1 19960801 A 5330 591141097 SKIN DOUG DC9 DC915F 3022037 WP BS 365 CRACKED A Y2PA K NONE O OTHER IN INSP/MAINT 1 GL 23 567PC 47153 DURING C/D BRIDGING CHECK, FOUND CRACK IN FUSELAGE SKIN LT SIDE STATION 365 JUST BELOW CARGO DOOR. REMOVED DAMAGED SECT ION OF FUSELAGE SKIN AND INSTALLED EXTERNAL REPAIR DOUBLERS AS SHOWN IN FIG 1 OF THIS EA NR 53-96154. N/R CARD 96-0267. 2 L 7 2 4F A6WE 1996080800343 19960808 00343 WP 1996 8 8 Y2PA96056 1 19960801 A 5320 4912281IN DOOR FRAME DOUG DC9 DC915F 3022037 WP CARGO DOOR PUNCTURED A Y2PA K NONE O OTHER IN INSP/MAINT 1 GL 23 567PC 47153 DURING C/D BRIDGING CHECK, FOUND PUNCTURE IN LOWER AFT A PIT DOOR FRAME. REPAIRED LOWER AFT DOOR FRAME IAW EA NR 53-961 55 FLIGHT VEHICLES, INC N/R CARD 96-0257. 2 L 7 2 4F A6WE 1996080800344 19960808 00344 WP 1996 8 8 Y2PA96057 1 19960801 A 5330 591141097 SKIN DOUG DC9 DC915F 3022037 WP BS 405 DENTED A Y2PA K NONE O OTHER IN INSP/MAINT 1 GL 23 567PC 47153 DURING C/D BRIDGING CHECK, FOUND DENT IN FUSELAGE SKIN AT STA 405 STRINGER L-19 LT, 4 BY 3.5 BY .035. REPAIRED DENTS IN FUSELAGE SKIN IAW EA NR 53-96154 DATED 7-11-96, N/R CARD 96-0265. 2 L 7 2 4F A6WE 1996080800345 19960808 00345 WP 1996 8 8 Y2PA96058 1 19960801 A 5230 99216961 ATTACH SUPPORT DOUG DC9 DC915F 3022037 WP CARGO DOOR ACT CRACKED A Y2PA K NONE O OTHER IN INSP/MAINT 1 GL 23 567PC 47153 DURING C/D BRIDGING CHECK, FOUND CARGO DOOR FWD ACTUATOR SUPPORT PLATE HAS CRACK UNDER IT ON FUSELAGE SUB STRUCTURE. RE PAIRED CARGO DOOR FWD ACTUATOR SUPPORT PLATE IAW EA NR 53-96156 DATED 7-17-96 AND IAW DC-9 SRM, INTERIM REPAIR TILL NEXT C-CHECK OR 2500 HR PER EA NR 53-96156 FIG 1. N/R CARD 96-0181. 2 L 7 2 4F A6WE 1996080800346 19960808 00346 WP 1996 8 8 Y2PA96059 1 19960801 A 5210 5915901553 DOOR SKIN DOUG DC9 DC915F 3022037 WP FWD AIRSTAIR CORRODED A Y2PA K NONE O OTHER IN INSP/MAINT 1 GL 23 567PC 47153 DURING C/D BRIDGING CHECK, FOUND DOOR CORRODED. INSTALLED REPAIR DOUBLER TO FWD AIRSTAIR DOOR PER ENGR DWG AIA/E/2252. REPAIRED AIRSTAIR DOOR PER ENGR DWG AIA/E/2252 COVERED BY AIA 8110-3, N/R CARD 96-0330. 2 L 7 2 4F A6WE 1996080800347 19960808 00347 NM 1996 8 8 96ZZZM1181 1 19960706 A 3350 8621004 BATTERYPACK BOEING 737 737298C 1384490 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING MAINTENANCE CHECK, THE SMOKE BARRIER AND ROW 12EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATI VE. REPLACEDBATTERY PACKS AND LIGHTS OPERATED NORMALLY. REFERENCE ASAA9610091. 2 L 7 2 4F RT A16WE 1996080800348 19960808 00348 NM 1996 8 8 96ZZZM1182 1 19960705 A 3350 86210151 BATTERY BOEING 737 737210C 1384459 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 SEA - DURING RECONFIGURATION, THE FORWARD EMERGENCY EXIT TRACKLIGHT TRANSMITTER WAS FOUND TO BE INOPERATIVE. REMOVED AN D REPLACEDTRANSMITTER AND BATTERY AND LIGHTS CHECKED NORMAL. REFERENCEASAA9610092. 2 L 7 2 4F A16WE 1996080800349 19960808 00349 NM 1996 8 8 96ZZZM1183 1 19960624 A 3350 900835A BATTERY PACK BOEING 747 747212B 1384886 NM CABIN DISCHARGED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 619FF 21316 DURING DAILY SERVICE, FOUND CEILING MOUNTED EXIT SIGNS AT R4MED, L2 MED L3 MED, AND ADJACENT TO SEAT 12C, 20H AND 52C AR E INOPERATIVE.REPLACED LIGHT ASSEMBLIES AND BATTERY PACKS. OPS CHECK OK. REFERENCETWRA9657. 2 L 7 4 4F A20WE 1996080800350 19960808 00350 NM 1996 8 8 96ZZZM1184 1 19960709 A 7931 41820044 OIL PRESSTRANS BOEING 737 737401 1384701 NM NR 2 ENG MALFUNCTIONED A USAA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 EA 19 422US 23989 CLT - FL 2127 - AT CRUISE, PRIOR TO DESCENT, THE NR 2 ENG OILPRESSURE INDICATED ZERO. ALL OTHER INDICATIONS WERE NORMAL . THE NR 2 ENGOIL PRESSURE SHOWED ZERO FOR ABOUT 60 SECONDS BEFORE IT WAS PLACED AT IDLE.THREE MINUTES LATER, SHUTDOWN THE NR 2 ENGINE FOR CAUTION REASONS. ANEMERGENCY WAS DECLARED AND THE FLT LANDED SAFELY WITH NO FURTHER INCIDENT.TOTAL SINGLE ENGINE TIME WAS TWENTY-FIVE MINUTES. MX REPLACED THE NR 2ENGINE OIL PRESSURE SWITCH AND OIL PRESSURE TRANSMITTER . OPS CHECK WASNORMAL. INSPECTION OF ENGINE AFTER SHUTDOWN SHOWED NO DEFECTS. ALL ENGPARAMETERS CHECKED NORMAL. REFER ENCE USAASB96123 2 L 7 2 4F RT A16WE 1996080800351 19960808 00351 NE 1996 8 8 96ZZZM1185 2 19960216 A 7314 5009986B FUEL PUMP EMB 120 EMB120 3260201 SO PWA 118 PW118A NE RT ENGINE FAILED A A MASA A UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 SW 01 203YV 13874 120203 115491 APPROXIMATELY 50 MILES OUT OF RPD WITH GEAR DOWN AND LOCKED ON FERRY FLIGHT, THE RIGHT ENGINE FLAMED OUT. THE AIRCRAFT RETURNED TO RPD WITHOUT FURTHER INCIDENT. MX DISCOVERED THE CAUSE OF THE FLAMEOUT TO BE FUEL STARVATION AND THE RIGHT E NGINE HIGH PRESSURE PUMP AS WELL AS THE HMU WERE REPLACED. AIRCRAFT WAS OPS CHECKED AND RELEASED TO FERRY FLT TO FARMIN GTON. 2 L 7 2 4T 4 T RT A31SO E20NE 1996080800352 19960808 00352 EA 1996 8 8 96ZZZM1186 2 19960707 A 7200 ENGINE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA LEFT FAILED A GUUA A UNSCHED LANDING J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 19 199GA 9557 1683 UB13 PCE32080 FLT 410 - FPO-MIA - ON CLIMB-OUT FROM FPO, ODORAND SMOKE EMULATING FROM THE FLOOR OF THE COCKPIT. LEFT ENGINE INDICATIO NSWERE ERRATIC, SHUTDOWN LEFT ENGINE. RELIEVED CABIN PRESSURE TO EVACUATERESIDUAL SMOKE. DECLARED AN EMERGENCY, RETURN ED TO FPO AND LANDED WITHOUTFURTHER INCIDENT. REMOVED AND REPLACED THE LEFT POWER PLANT ASSEMBLY ANDROUTED THE REMOVED UNIT TO OVERHAUL VENDER FORANALYSIS. 2 L 7 2 4T 4 T RT A24CE E4EA 1996080800353 19960808 00353 EA 1996 8 8 96ZZZM1187 1 19960711 A 3230 54C546347 SEQVLV DHAV DHC8 DHC8311 1386006 EA NLG FAILED A MASA O OTHER J WARNING INDICATION DE DESCENT 1 SW 01 430AW 279 FLT 7456 - EN ROUTE DEN/RAP - ON DESCENT WHEN THE GEAR WAS SELECTEDDOWN, ALL BUT THE NOSE GEAR EXTENDED, AT WHICH TIME T HE CREW NOTICED THATTHE NR 2 HYD SYSTEM PRESSURE AND QTY WAS ZERO. THE CREW THEN ALTERNATELYEXTENDED THE NOSE GEAR WITH OUT INCIDENT AND LANDED SAFELY. UPONINVESTIGATION IT WAS FOUND THAT THE NOSE LANDING GEAR DOOR SEQUENCE VALVESOLENOID H AD PARTIALLY SEPARATED SHEARING 2 OF 4 BOLTS ATTACHING SOLENOID TOVALVE BODY. THE SEQUENCE VALVE WAS REPLACED, HYDRAULI C SERVICED ALL CHECKEDNORMAL, A TEST FLT PERFORMED AND ACFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1996080800354 19960808 00354 NM 1996 8 8 ASAA9610085 1 19960702 A 3350 1060091101 LIGHT BOEING 737 737210C 1384459 NM L-1DOOR DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 SEA - DURING MAINTENANCE CHECK, THE FORWARD ENTRY DOOR OVERHEADEMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED LIG HT ASSEMBLY ANDOPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1996080800355 19960808 00355 NM 1996 8 8 ASAA9610086 1 19960702 A 3350 8821004 BATTERY BOEING 737 737210C 1384459 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACKLIGHTS WERE FOUND INOPERATIVE AT ROWS 10/11. REPLACED BAT TERY PACK AT ROW11 RECEIVER AND LIGHTS OPERATED NORMALLY.(M) 2 L 7 2 4F A16WE 1996080800356 19960808 00356 NM 1996 8 8 ASAA9610087 1 19960703 A 3397 WIRE BOEING 737 737290C 138448V NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING MAINTENANCE CHECK, THE FORWARD CABIN OVERHEADEMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. RECONNECTED LOOSE WIRE INTERMINAL AT NR 1 CONNECTION AT LIGHT ASSEMBLY AND LIGHT OPERATED NORMALLY.(M) 2 L 7 2 4F A16WE 1996080800357 19960808 00357 NM 1996 8 8 ASAA9610088 1 19960704 A 3350 82210151 BATTERY BOEING 737 737298C 1384490 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING MAINTENANCE CHECK, THE FORWARD EMERGENCY EXITFLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED FORWARD T RACK LIGHTTRANSMITTER BATTERY AND LIGHTS OPERATED NORMALLY.(M) 2 L 7 2 4F RT A16WE 1996080800358 19960808 00358 NM 1996 8 8 ASAA9610089 1 19960704 A 3350 8821004 BATTERY BOEING 737 737298C 1384490 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACKLIGHTS AT ROW 15 WERE FOUND INOPERATIVE. REPLACED TRACK L IGHT BATTERY ANDLIGHTS OPERATED NORMALLY.(M) 2 L 7 2 4F RT A16WE 1996080800359 19960808 00359 NM 1996 8 8 ASAA9610090 1 19960707 A 3350 RPS1B BATTERY PACK BOEING 737 737210C 1384459 NM CARGOCOMPT DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 744AS 21822 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACKLIGHTS WERE FOUND INOPERATIVE ON 1 PALLET. REPLACED BATTERY PA CK AND LIGHTSOPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1996080800360 19960808 00360 NM 1996 8 8 ASAA9610091 1 19960706 A 3350 86210144 BATTERYPACK BOEING 737 737298C 1384490 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING MAINTENANCE CHECK, THE SMOKE BARRIER AND ROW 12EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATI VE. REPLACEDBATTERY PACKS AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996080800361 19960808 00361 NM 1996 8 8 ASAA9610092 1 19960705 A 3350 883200312 TRANSMITTER BOEING 737 737210C 1384459 NM CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 SEA - DURING RECONFIGURATION, THE FORWARD EMERGENCY EXIT TRACKLIGHT TRANSMITTER WAS FOUND TO BE INOPERATIVE. REMOVED AN D REPLACEDTRANSMITTER AND BATTERY AND LIGHTS CHECKED NORMAL.(M) 2 L 7 2 4F A16WE 1996080800362 19960808 00362 NM 1996 8 8 ASAA9610093 1 19960710 A 3350 1060091101 LIGHT BOEING 737 7372X6C 1384552 NM LTOVERWING INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING MAINTENANCE CHECK, THE LEFT OVERWING EMERGENCYEXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED LIGHT ASSEM BLY AND LIGHTOPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996080800363 19960808 00363 NM 1996 8 8 ASAA9640053 1 19960629 A 3350 S417N50911 SOCKET BOEING 737 737490 1384715 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 768AS 27082 JNU - DURING MAINTENANCE CHECK, THE AFT FOUR EMERGENCY EXITFLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED TRACK LI GHT LAMP SOCKETAND ALL LIGHTS OPERATED NORMALLY.(M) 2 L 7 2 4F RT A16WE 1996080800364 19960808 00364 NM 1996 8 8 ASAA9640058 1 19960705 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 771AS 25104 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACKLIGHTS WERE FOUND TO BE INOPERATIVE BETWEEN ROWS 14 THROUG H 18. RECONNECTEDWIRING AT ROW 14 AND LIGHTS OPERATED NORMALLY.(M) 2 L 7 2 4F RT A16WE 1996080800365 19960808 00365 WP 1996 8 8 ASAA9680124 1 19960524 A 3260 833703 SENSOR DOUG DC9 DC983 3022083 WP NLG DEFECTIVE A ASAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 01 962AS 53076 PDX - DIVERTED TO PDX - AFTER DEPARTURE FROM EAX OF FLT 7560 - CREWREPORTED THE NOSE LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEARRETRACTED, INDICATOR BUTTON INDICATED RETRACTED. CYCLED GEAR AND LIGHTREMAINED ILLUMINATED. REPL ACED THE NOSE LANDING GEAR LOCKED SENSOR ANDACCOMPLISHED RETRACTION/EXTENSION TEST AND OPERATED NORMALLY.(M) 2 L 7 2 4F RT A6WE 1996080800366 19960808 00366 WP 1996 8 8 ASAA9680131 1 19960604 A 5210 LINER DOUG DC9 DC982 3022082 WP L1DOOR DETACHED A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 967AS 49103 SEA - AFTER ARRIVAL, OF FLT 397 - CREW REPORTED THE L1 DOORDIFFICULT TO OPEN. FOUND THE FORWARD UPPER EDGE OF DOOR LINE R DETACHED,REATTACHED DOOR LINER AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996080800367 19960808 00367 WP 1996 8 8 ASAA9680138 1 19960616 A 3230 MECHANISM DOUG DC9 DC982 3022082 WP FLT COMPT OUT OF ADJUST A ASAA O OTHER N FALSE WARNING CL CLIMB 1 NM 01 956AS 48079 SEAT - PRIOR TO ARRIVAL OF FLIGHT 511 - CREW REPORTED, THE LANDING GEAR HANDLE COULD NOT BE MOVED TO THE UP POSITION ON THE FIRST ATTEMPT AFTER TAKEOFF FROM SAN. ON THE THIRD ATTEMPT, THE GEAR HANDLE WAS MOVED TO THE UP YPOSITION AND THE L ANDING GEAR RETRACTED NORMALLY. (M) 2 L 7 2 4F A6WE 1996080800368 19960808 00368 1996 8 8 ASAA9680143 4 19960701 A 2565 D37013109 SLIDE BOTTLE DOUG DC9 DC982 3022082 WP R1DOOR LOW PRESSURE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 953AS 49386 PDX - DURING MAINTENANCE CHECK, THE R1 DOOR EMERGENCY EVACUATIONSLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. REPLACED THE R1 DOOREMERGENCY EVACUATION SLIDE. (M) 2 L 7 2 4F A6WE 1996080800369 19960808 00369 WP 1996 8 8 ASAA9680145 1 19960706 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 969AS 53063 LAX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTSFROM ROW 30 AFT WERE FOUND INOPERATIVE. REPAIRED BROKEN WIRE AT ROW 31 ANDOPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996080800370 19960808 00370 WP 1996 8 8 ASAA9680146 1 19960607 A 3350 0105610001 LIGHT DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 972AS 53448 SEA - DURING MAINTENANCE CHECK, THE AFT FOUR EMERGENCY FLOOR TRACKLIGHTS WERE FOUND INOPERATIVE. REPLACED DEFECTIVE LIG HT ASSEMBLY ANDOPERATED NORMALLY.(M) 2 L 7 2 4F RT A6WE 1996080800371 19960808 00371 1996 8 8 ASAA9680147 4 19960707 A 2565 D37013117 SLIDE BOTTLE DOUG DC9 DC983 3022083 WP TAILCONE LOWPRESSURE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 939AS 49657 SEA - DURING MAINTENACNE CHECK, THE TAILCONE EMERGENCY EVACUATIONSLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. REPLACE D THE TAILCONEEMERGENCY EVACUATION SLIDE. (M) 2 L 7 2 4F RT A6WE 1996080800372 19960808 00372 WP 1996 8 8 ASAA9680149 1 19960708 A 3350 014597101 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 966AS 49104 ANC - DURING MAINTENANCE CHECK,THE RIGHT OVERHEAD EMERGENCY LIGHTIN THE TAILCONE AREA WAS FOUND INOPERATIVE. REPLACED T HE BATTERIES ANDOPERATED NORMALLY.(M) 2 L 7 2 4F A6WE 1996080800373 19960808 00373 WP 1996 8 8 ASAA9680150 1 19960709 A 3350 0200335001 LIGHT DOUG DC9 DC982 3022082 WP TAILCONE DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 956AS 48079 SEA - DURING MAINTENANCE CHECK, THE FORWARD OVERHEAD EMERGENCYLIGHT IN THE TAILCONE AREA WAS FOUND INOPERATIVE. REPLACE D THE LIGHTASSEMBLY AND OPERATED NORMALLY.(M) 2 L 7 2 4F A6WE 1996080800374 19960808 00374 WP 1996 8 8 ASAA9680151 1 19960710 A 3350 014597101 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 954AS 49387 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS ATROW 8 WOULD NOT EXTINGUISH WHEN ALL ELECTRICAL POWER WAS REMOVED FROM THEAIRCRAFT. REPLACED THE BATTERIES AND OPERATED NORMALLY.(M) 2 L 7 2 4F A6WE 1996080800375 19960808 00375 WP 1996 8 8 ASAA9680152 1 19960712 A 3350 41B004AD07G3 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 943AS 53018 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROMROWS 13 TO 18 WERE FOUND INOPERATIVE. REPLACED THE BA TTERIES AND OPERATEDNORMALLY.(M) 2 L 7 2 4F RT A6WE 1996080800376 19960808 00376 WP 1996 8 8 ASAA9680153 1 19960714 A 3350 S103 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 955AS 48080 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROMROWS 6 TO 10 WERE FOUND INOPERATIVE. REPLACED THE BAT TERIES AND OPERATEDNORMALLY. (M) 2 L 7 2 4F A6WE 1996080800377 19960808 00377 EU 1996 8 8 AWXA960281 1 19960528 A 5320 SUPPORT AIRBUS 320 A320231 3930325 EU BS 719 CORROSION A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 620AW 052 PAE - DURING ROUTINE SCHEDULED C-5 MAINTENANCE CHECK, FOUNDCORROSION ON FLOOR BOARD SUPPORT BEAM AT 2540, BS 719 AND -18 . REPAIRED IAWSRM 53-11-14. (M) 2 L 7 2 4F RT A28NM 1996080800378 19960808 00378 SO 1996 8 8 C2XA96IA169 1 19960709 A 5400 12030995001 ANGLE EMB 120 EMB120RT SO LT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 27707 120095 IAH - DURING C-CHECK INSPECTION, THE LEFT NACELLE FRAME 2 ATTACHANGLE WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLAC ED THE AFFECTEDANGLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.(M) 2 L 7 2 4T RT A31SO 1996080800379 19960808 00379 SO 1996 8 8 C2XA96IA170 1 19960709 A 5400 12030995002 ANGLE EMB 120 EMB120RT SO RT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 27707 120095 IAH - DURING C-CHECK INSPECTION, THE RIGHT NACELLE FRAME 2ATTACH ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THEAFFECTED ANGLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.(M) 2 L 7 2 4T RT A31SO 1996080800381 19960808 00381 NM 1996 8 8 TWRA96121 1 19960709 A 3350 ML7715 BULB BOEING 747 747212B 1384886 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 616FF 21939 DURING DAILY CHECK, FOUND 36C FLOOR EVAC LIGHT INOP. REPLACEDBULB, OPS CHECK OK 33-51-00.(M) 2 L 7 4 4F A20WE 1996080800382 19960808 00382 NM 1996 8 8 TWRA96122 1 19960705 A 3350 ML7715 BULB BOEING 747 747238B 1384828 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 614FF 20534 DURING DAILY CHECK, FOUND FLOOR EGRESS LAMP SEAT 11C IN 'B' ZONEINOP. RELAMPED OPS CHECK OK PER MM 33-51-00.(M) 2 L 7 4 4F A20WE 1996080800383 19960808 00383 NM 1996 8 8 TWRA96123 1 19960704 A 3350 ML7715 BULB BOEING 747 747238B 1384828 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 614FF 20534 DURING DAILY CHECK, FOUND CABIN 'E' ZONE 4H SIDE 'E' PATH LIGHTSAT 51A AND 58A INOP. RELAMPED, OPS CHECK OK PER MM 33-5 1-00.(M) 2 L 7 4 4F A20WE 1996080800384 19960808 00384 NM 1996 8 8 TWRA96125 1 19960704 A 3350 ML7715 BULB BOEING 747 747238B 1384828 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 614FF 20534 DURING DAILY CHECK, FOUND CABIN 'B' ZONE SEAT 11A, 15K, 16K EVACLIGHTS INOP. RELAMPED OPS CHECK OK PER MM 33-51-00.(M) 2 L 7 4 4F A20WE 1996080800385 19960808 00385 NM 1996 8 8 TWRA96127 1 19960709 A 3350 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 619FF 21316 DURING DAILY CHECK, FOUND NR 4 MED F/A JUMPSEAT EMERGENCY LIGHTIS INOP. RECONNECTED PLUG, OPS CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996080800386 19960808 00386 NM 1996 8 8 TWRA96128 1 19960706 A 3350 S1356B37 LIGHT BOEING 747 747238B 1384828 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 607PE 20011 DURING DAILY CHECK, FOUND MAIN CABIN 'B' ZONE CEILING EMERGENCYLIGHT FWD RIGHT FLUCTUATES. REPLACED OVERHEAD CEILING EM ERGENCY LIGHT. OPSCHECK NORMAL PER MM 33-51-00.(M) 2 L 7 4 4F A20WE 1996080800387 19960808 00387 NM 1996 8 8 TWRA96130 1 19960708 A 3350 LIGHTS BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND EGRESS LIGHTS INOP. OPERATED EGRESSLIGHTS, OPS CHECK OK. (M) 2 L 7 4 4F A20WE 1996080800388 19960808 00388 NM 1996 8 8 TWRA96132 1 19960710 A 3350 S1356B37 BATTERYPACK BOEING 747 747212B 1384886 NM CABIN DISCHARGED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 620FF 21162 DURING DAILY CHECK, FOUND CEILING LIGHT ABOVE SEATS 26GH INOP.REPLACED AISLE BATTERY PACK. OPS CHECK OK PER MM 33-51-00 . (M) 2 L 7 4 4F A20WE 1996080800389 19960808 00389 NM 1996 8 8 TWRA96133 1 19960710 A 3397 WIRE BOEING 747 747212B 1384886 NM CREW EXIT BROKEN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 620FF 21162 DURING DAILY CHECK, FOUND EMERGENCY EXIT LIGHT INOP ON WALLFORWARD OF CREW EXIT DOOR. REPAIRED BROKEN WIRE AT BACK OF S IGN. OPS CHECKOK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996080800390 19960808 00390 NM 1996 8 8 TWRA96134 1 19960703 A 3350 900835A BATTERYPACK BOEING 747 747238B 1384828 NM 2R DOOR DISCHARGED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 607PE 20011 DURING DAILY CHECK, FOUND EMERGENCY LIGHT ABOVE 2R DOOR IS WEAK.REPLACED BATTERY PACK. OPS CHECK OK PER MM 33-51-00. ( M) 2 L 7 4 4F A20WE 1996080800391 19960808 00391 NM 1996 8 8 TWRA96135 1 19960703 A 3350 ML7715 BULB BOEING 747 747238B 1384828 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 607PE 20011 DURING DAILY CHECK, FOUND EMERGENCY LIGHT AT 21ABC, 3AC, 37ABCAND 51ABC INOP. RELAMPED, OPS CHECK OK PER MM 33-51-00.(M ) 2 L 7 4 4F A20WE 1996080800392 19960808 00392 NM 1996 8 8 TWRA96139 1 19960711 A 3350 1317 BULB BOEING 747 747238B 1384828 NM OVERWING FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 614FF 20534 DURING DAILY CHECK, FOUND RIGHT SIDE OF AIRCRAFT OVERWING (EVAC)HAS TWO LIGHTS INOP (BOTTOM TWO). RELAMPED, LIGHTS OPS CHECK NORMAL PER MM33-51-00. (M) 2 L 7 4 4F A20WE 1996080800393 19960808 00393 NM 1996 8 8 TWRA96140 1 19960711 A 3350 ML7715 BULB BOEING 747 747238B 1384828 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 614FF 20534 DURING DAILY CHECK, FOUND L1 DOOR 2 FLOOR (EVAC) LIGHTS OUT.REPAIRED BROKEN WIRE AND LAMPED LIGHTS. OPS CHECK NORMAL PE R MM 33-51-00.(M) 2 L 7 4 4F A20WE 1996080800394 19960808 00394 NM 1996 8 8 TWRA96141 1 19960711 A 3350 ML7715 BULB BOEING 747 747238B 1384828 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 614FF 20534 DURING DAILY CHECK, FOUND SEAT 6K AND 45ABC (EVAC) FLOOR LIGHTINOP. RELAMPED LIGHT, OPS CHECK OK PER MM 33-51-00.(M) 2 L 7 4 4F A20WE 1996080800395 19960808 00395 NM 1996 8 8 TWRA96152 1 19960713 A 3350 ML7715 BULB BOEING 747 747212B 1384886 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 619FF 21316 DURING DAILY CHECK, FOUND SEAT 31K EVAC LIGHT INOP. RELAMPED OPSCHECK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996080800396 19960808 00396 NM 1996 8 8 TWRA96187 1 19960717 A 3350 07912 LIGHT BOEING 747 747238B 1384828 NM CABIN MISSING A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 607PE 20011 DURING DAILY CHECK, FOUND ROW 63H EVAC LIGHT MISSING. REPAIREDWIRING ON LAMP SOCKET. REPLACED CAP AND BULB. OPS CHECK OK PER MM33-51-00. (M) 2 L 7 4 4F A20WE 1996080800397 19960808 00397 NM 1996 8 8 TWRA9649 1 19960624 A 3350 FUSE BOEING 747 747130 1384880 NM CABIN BLOWN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 603FF 19746 DURING PREFLIGHT, FOUND E ZONE EMERGENCY ESCAPE PATH LIGHTING ONLEFT SIDE INOPERATIVE. REPLACED FUSE, OPS CHECK OK.(M) 2 L 7 4 4F A20WE 1996080800398 19960808 00398 NM 1996 8 8 TWRA9650 1 19960625 A 3397 WIRE BOEING 747 747130 1384880 NM CABIN SHORTED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 603FF 19746 DURING DAILY SERVICE, FOUND E ZONE EMERGENCY ESCAPE PATH LIGHTINGON LEFT SIDE INOPERATIVE. REPAIRED WIRE AT SEAT 62, OP S NORMAL.(M) 2 L 7 4 4F A20WE 1996080800399 19960808 00399 NM 1996 8 8 TWRA9651 1 19960622 A 3350 6016123 BATTERY PACK BOEING 747 747282B 1384860 NM CABIN DISCHARGED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 611FF 20502 DURING DAILY SERVICE, FOUND CREW DOOR EMERGENCY EXIT SIGN AND SILLLIGHTS INOPERATIVE DURING OPS CHECK. REPLACED BATTERY AT OVERHEAD CREW DOORFOR SILL LIGHTS AND RELAMPED EXIT SIGN WITH 700 517-14 BULBS. BOTH LIGHTSTEST OK. (M) 2 L 7 4 4F A20WE 1996080800400 19960808 00400 NM 1996 8 8 TWRA9652 1 19960624 A 3350 3001481A LIGHT BOEING 747 747124 1384874 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 602FF 19734 DURING DAILY SERVICE, FOUND EMERGENCY EGRESS LIGHT ON 4L MED UPPERBUSTLE INOPERATIVE. REMOVED AND REPLACED 4L MED UPPER BUSTLE LGIHTASSEMBLY. OPS CHECK OK.(M) 2 L 7 4 4F A20WE 1996080800401 19960808 00401 NM 1996 8 8 TWRA9653 1 19960624 A 3397 WIRE BOEING 747 747124 1384874 NM CABIN BROKEN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 602FF 19734 EMERGENCY EGRESS LIGHTS AT 1L FLIGHT ATTENDANT SEAT AND AT SEAT 31HJK ARE INOPERATIVE. FOUND BORKEN WIRES AND REPAIRED PER 33-51-00. OPSCHECK NORMAL. (M) 2 L 7 4 4F A20WE 1996080800402 19960808 00402 NM 1996 8 8 TWRA9654 1 19960624 A 3350 60B500391 SIGN BOEING 747 747121 1384871 NM CABIN BROKEN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 604FF 19659 DURING DAILY SERVICE, FOUND 5R MED EXIT LIGHT INOPERATIVE.REPLACED BROKEN EXIT SIGN.(M) 2 L 7 4 4F A20WE 1996080800403 19960808 00403 NM 1996 8 8 TWRA9655 1 19960622 A 3350 900835A BATTERY PACK BOEING 747 747212B 1384886 NM CABIN DISCHARGED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY SERVICE, FOUND UPPER DECK EXIT SIGN LIGHT INOP. REMOVED AND REPLACED BATTERY PACK. OPS CHECK NORMAL. (M) 2 L 7 4 4F A20WE 1996080800404 19960808 00404 NM 1996 8 8 TWRA9657 1 19960624 A 3350 S1356837 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 619FF 21316 DURING DAILY SERVICE, FOUND CEILING MOUNTED EXIT SIGNS AT R4 MED,L2 MED L3 MED, AND ADJACENT TO SEAT 12C, 20H AND 52C AR E INOPERATIVE.REPLACED LIGHT ASSEMBLIES AND BATTERY PACKS. OPS CHECK OK.(M) 2 L 7 4 4F A20WE 1996080800405 19960808 00405 NM 1996 8 8 TWRA9658 1 19960624 A 3350 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 619FF 21316 DURING DAILY SERVICE, FOUND R1 AND L5 MED BUSTLE LIGHTSINOPERATIVE. RELAMPED, OPS CHECK OK.(M) 2 L 7 4 4F A20WE 1996080800406 19960808 00406 NM 1996 8 8 TWRA9659 1 19960626 A 3350 S1356B37 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 619FF 21316 DURING DAILY SERVICE, FOUND B ZONE RIGHT SIDE AFT EMERGENCYCEILING LIGHT OUT. REPLACED CEILING LIGHT ASSEMBLY, OPS CHEC K NORMAL.(M) 2 L 7 4 4F A20WE 1996080800407 19960808 00407 NM 1996 8 8 TWRA9667 1 19960628 A 2410 BACC45FS22B19S CSD BOEING 747 747121 1384871 NM NR 2ENGINE FAILED A TWRA E A ENGINE SHUTDOWN UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 15 617FF 19650 DURING CRUISE, NR 4 GENERATOR FIELD TRIPPED, CSD DID NOTDISCONNECT ENGINE WAS SHUT DOWN PER FLIGHT MANUAL A/C DIVERTED T O LIMADURING CRUISE NR 2 CSD INDICATED HI TEMPERATURE, EXCEEDED RED LIMIT. CSD,DISCONNECTED. CSD REPLACED. MAINTENANC E REMOVED CSD AND GENERATOR.INSTALLED BLANKING PLATES. ENGINE R/U PERFORMED NO LEAKS. WINDMILLINSPECTION WAS ACCOMPLIS HED. DURING FURTHER T/S FOUND CSD CANNON PLUG PINSPUSHED BACK. (M) 2 L 7 4 4F A20WE 1996080800408 19960808 00408 NM 1996 8 8 TWRA9670 1 19960626 A 3350 S1356837900083SA BATTERY BOEING 747 747212B 1384886 NM CABIN DISCHARGED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 619FF 21316 EXIT SIGN OVERHEAD AND AISLEWAY OVERHEAD EXIT SIGN INOP BY R2DOOR. BATTERY CHARGED, OPS CHECKED OK PER MM 33-51.(M) 2 L 7 4 4F A20WE 1996080800409 19960808 00409 NM 1996 8 8 TWRA9671 1 19960701 A 3350 086861 LIGHT BOEING 747 747212B 1384886 NM CABIN MISSING A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 619FF 21316 FOUND 14TH EMERGENCY LIGHT IS MISSING. REPLACED LIGHT ASSY ANDCOVER EMERGENCY LGIHT AT 14H. OPS CHECK NORMAL AS PER MM 57-00.(M) 2 L 7 4 4F A20WE 1996080800410 19960808 00410 NM 1996 8 8 TWRA9673 1 19960701 A 3350 CONNECTOR BOEING 747 747212B 1384886 NM CABIN DISCONNECT A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 619FF 21316 NR 5R MED CEILING EMERGENCY LIGHT IS INOP. FOUND PLUG FLOORCEILING LIGHT DISCONNECTED. RECONNECTED PLUG NR 5R MED CEIL ING EMERGENCYLIGHT, OPS CHECK NORMAL.(M) 2 L 7 4 4F A20WE 1996080800411 19960808 00411 NE 1996 8 8 UIEA9607 2 19960624 A 7260 CHIP DETECTOR BOEING 747 747128 1384894 NM PWA JT9 JT9D7A 52054 NE NR 1ENG GB LEAKING A UIEA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION DE DESCENT 1 EA 15 3203Y 19751 685679 FLT NR VR966 - GRU-MEX - NR 1 ENGINE HIGH OILCONSUMPTION AT TOP OF DESCENT QTY SHOWED 2 GALLONS PRESSURE DROPPED TO 30PS I AND WAS FLUCTUATING, SHUTDOWN ENGINE, TOTAL WINDMILLING TIME 28 MINUTES. PERFORMED WINDMILL INSPECTION. NO DAMAGE NOT ED. SERVICED ENGINE OIL.ENGINE RUN REVEALED ACCESSORY GEAR BOX CHIP DETECTOR LEAKING. REPLACED AGBCLIP DETECTOR. ENGI NE RUN OPS CHECKS OK. (M) 2 L 7 4 4F 4 F A20WE E20EA 1996080800412 19960808 00412 WP 1996 8 8 USAA960508 1 19960716 A 5311 27779306 BELTFRAME DOUG DC9 DC982 3022082 WP BS 1322 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 829US 28433 49429 PIT - DURING Q-2/C-5 CHECK, FOUND .5 INCH BY 4 INCH CORRODED AREA,STATION 1322 LONGERON 30 BELTFRAME. SPLICED IN NEW BE LTFRAME PER SRM53-14-3, CORROSION TASK NR C57-53300. CORROSION LEVEL 1.(M) 2 L 7 2 4F A6WE 1996080800413 19960808 00413 WP 1996 8 8 USAA960509 1 19960719 A 5311 591016373 BELTFRAME DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 991VJ 70406 47310 PIT - DURING Q-1/C-3 CHECK, FOUND CORROSION IN BELTFRAME 1 INCH WIDEBY 2 INCH LONG AT BELTFRAME 996 AT LONGERON 18 LT. C UT OUT CORRODEDBELTFRAME, INSTALLED FILLER AND DOUBLERS 7075 T6 PER SRM 53-30 FIG 14 AND53-05 FIG 93. CORROSION TASK NR C58-53300, CORROSION LEVEL 1.(M) 2 L 7 2 4F A6WE 1996080800414 19960808 00414 WP 1996 8 8 USAA960513 1 19960717 A 5312 BLKHD DOUBLER DOUG DC9 DC931 3022065 WP BS996 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 971VJ 74934 47051 PIT - DURING AFT PRESS BULKHEAD MOD, FOUND 4 INCH LONG CRACK AT AFTPRESS BULKHEAD STATION 996 UPPER RT CORNER OF REAR PA X DOORWAY, DOUBLER5910130-11. REPLACED UPPER HALF OF DOUBLER 5910130-11 PER EA 32891A ANDDACO DWG J060088. (M) 2 L 7 2 4F A6WE 1996080800415 19960808 00415 NM 1996 8 8 USAA960514 1 19960718 A 5320 SHEAR BEAM BOEING 737 737201 1384454 NM BS706 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 243US 37825 22445 ROA - DURING BX-CHECK, VISUAL INSPECTION FOUND .75 INCH CRACKSTRINGER 18 A RIGHT SHEAR BEAM AT BS 706. INSTALLED REPAIR KIT, REPAIREDPER EO 5393G256 PART 3 STEP 4. (M) 2 L 7 2 4F A16WE 1996080800416 19960808 00416 NM 1996 8 8 USAA960515 1 19960715 A 5330 SKIN BOEING 737 737201 1384454 NM BS747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 255AU 36194 22797 ROA - DURING 'BX CHECK' VISUAL, CONFIRMED WITH HFEC INSPECTIONFOUND 1 INCH FUSELAGE SKIN CRACK BS 747 STRINGER 18R. REM OVED CRACK ANDINSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 6. (M) 2 L 7 2 4F A16WE 1996080800417 19960808 00417 NM 1996 8 8 USAA960516 1 19960719 A 5311 FRAME BOEING 737 7372B7 1384560 NM BS 990 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 283AU 35101 23116 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCHBY 1 INCH FRAME STATION 990 WL 208. INSTALLED FRAME REP AIR AND REPLACED 'Z'ANGLE, REPAIRED PER SRM 51-40-03, 51-10-2. CORROSION TASK NR 53-107-02,CORROSION LEVEL 1. (M) 2 L 7 2 4F A16WE 1996080800418 19960808 00418 NM 1996 8 8 USAA960517 1 19960719 A 5512 SKIN BOEING 737 7372B7 1384560 NM HORIZSTAB DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 283AU 35101 23116 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH INDENTEDAREA STABILIZER SKIN STATION 111.1 APPROX 12 INCHES FORWA RD OF AFT SPAR.INSTALLED DOUBLER, REPAIRED PER SRM 55-10-3. (M) 2 L 7 2 4F A16WE 1996080800419 19960808 00419 NM 1996 8 8 USAA960518 1 19960719 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS1016 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 283AU 35101 23116 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 4 INCHCORRODED AREA ON TOP OF FLOOR BEAM BS 1016 LBL 16 LBL 5. INSTALLED FLOORBEAM REPAIR, REPAIRED PER SRM 53-10-9. CORROSION TASK NR C53-017-02,CORROSION LEVEL 1. (M) 2 L 7 2 4F A16WE 1996080800420 19960808 00420 NM 1996 8 8 USAA960519 1 19960719 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS720 CHAFFING A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 283AU 35101 23116 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 10 INCHESCHAFFING STATION 720 RHS KEEL BEAM LOWER CORD OUTBOARD FLANGE. INSTALLEDREPAIR STRAP, REPAIRED PER EA 41322. (M) 2 L 7 2 4F A16WE 1996080800421 19960808 00421 NM 1996 8 8 USAA960520 1 19960719 A 5313 STRINGER BOEING 737 7372B7 1384560 NM BS960-967 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 283AU 35101 23116 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 7 INCHCORRODED AREA AT INBOARD SIDE STRINGER BS 960-967 STRING ER 26R. INSTALLEDSTRINGER SPLICE/REPAIR. REPAIRED PER SRM 53-10-3 PAGE 10 FIG 1. CORROSIONTASK NR C53-202-01, CORROSI ON LEVEL 1. (M) 2 L 7 2 4F A16WE 1996080800422 19960808 00422 NM 1996 8 8 USAA960521 1 19960719 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS986 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 283AU 35101 23116 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION 90INCHES AT STATION 986 FLOOR BEAM UPPER CHORD. INSTALLED NEW SECTION WITHREPAIR ANGLES AND STRAPS, REPAIRED EA 41317. CORROSION TASK NR C53-107-02,CORROSION LEVEL 1. (M) 2 L 7 2 4F A16WE 1996080800423 19960808 00423 NM 1996 8 8 USAA960522 1 19960719 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 917 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 283AU 35101 23116 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CRACK .375 INCHSTATION 917 BETWEEN STRINGERS 21L AND 22L SKIN. INSTALLE D DOUBLER, REPAIREDPER SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1996080800424 19960808 00424 NM 1996 8 8 USAA960523 1 19960719 A 5312 BULKHEAD SKIN BOEING 737 7372B7 1384560 NM AFT PRESSBLKHD SCRATCH A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 283AU 35101 23116 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .75 INCH SCRATCHAFT PRESSURE BULKHEAD SKIN 5 O'CLOCK POSITION. INSTALLE D DOUBLER, REPAIREDPER SRM 53-10-4 FIG 3. (M) 2 L 7 2 4F A16WE 1996080800425 19960808 00425 NM 1996 8 8 USAA960524 1 19960719 A 5512 SKIN BOEING 737 7372B7 1384560 NM HORIZ STAB GOUGES A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 283AU 35101 23116 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO GOUGES 1 INCHAND .625 INCH SKIN STABILIZER STATION 226 15 INCHES AND 20 INCHES AFT OFFRONT SPAR. INSTALLED DOUBLER, REPAIRED PER SRM 55-10-3.(M) 2 L 7 2 4F A16WE 1996080800426 19960808 00426 NM 1996 8 8 USAA960525 1 19960719 A 5512 SKIN BOEING 737 7372B7 1384560 NM HORIZ STAB GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 283AU 35101 23116 INT - DURING Q-6 CHECK VISUAL INSPECTION FOUND TWO GOUGES .75INCH AND .625 INCH SKIN STABILIZER STATION 92.7 APPROXIMATE LY 17 INCHES FROMAFT SPAR. INSTALLED DOUBLER, REPAIRED PER SRM 55-10-3.(M) 2 L 7 2 4F A16WE 1996080800427 19960808 00427 NM 1996 8 8 USAA960526 1 19960719 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 360 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 283AU 35101 23116 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCHCORRODED AREA FLOOR BEAM BS 360 RBL 54. INSTALLED REPAI R ANGLE, REPAIREDPER TR 53-10-05 C. CORROSION TASK NR C53-107-02, CORROSION LEVEL 1.(M) 2 L 7 2 4F A16WE 1996080800428 19960808 00428 NM 1996 8 8 USAA960527 1 19960719 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS328 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 283AU 35101 23116 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY1 INCH CORRODED AREAS ON FLOOR BEAM BS 328 RBL 12 INCH TO RBL 45 INCH.INSTALLED NEW T-CAP WITH REPAIR ANGLES, REPAIRED PER TR 53-10-13. CORROSIONTASK NR C53-107-02, CORROSION LEVEL 1. (M) 2 L 7 2 4F A16WE 1996080800429 19960808 00429 NM 1996 8 8 USAA960528 1 19960719 A 5315 FLOORBEAM BOEING 737 7372B7 1384560 NM BS 967 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 283AU 35101 23116 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH CORRODEDAREAS FLOOR BEAM BS 967. INSTALLED DOUBLER REPAIRED PER SRM 53-10-9.CORROSION TASK NR C53-107-02, CORROSION LEVEL 1 (M) 2 L 7 2 4F A16WE 1996080800430 19960808 00430 NM 1996 8 8 USAA960529 1 19960719 A 5313 STRINGER BOEING 737 7372B7 1384560 NM BS947-995 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 283AU 35101 23116 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND SPOTS OFCORROSION ALONG SIDES OF STRINGER BS 947-995 S-27L. REMOVED STR INGERSECTION, FABRICATED NEW SECTION AND INSTALLED, REPAIRED PER SRM 53-10-3.CORROSION TASK NR C53-202-01 CORROSION LEVE L 1. (M) 2 L 7 2 4F A16WE 1996080800431 19960808 00431 NM 1996 8 8 USAA960530 1 19960719 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 947.5 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 283AU 35101 23116 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .33 INCH CORRODEDAREA FLOOR BEAM BS 947.5 RBL 10 TO LBL 36. INSTALLED R EPLACEMENT T-CAP,REPAIRED PER TR 53-10-05C. CORROSION TASK NR C53-107-02, CORROSION LEVEL 1. (M) 2 L 7 2 4F A16WE 1996080800432 19960808 00432 NM 1996 8 8 USAA960531 1 19960719 A 5315 FLOORBEAM BOEING 737 7372B7 1384560 NM BS 1006 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 283AU 35101 23116 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION 3INCHES AT FLOOR BEAM STATION 1006 LBL 8. CUT OFF T-CAP THAT WAS OUT OFLIMITS, FABRICATED REPLACEMENT AND INSTALLED PER SRM 53-10-9 FIG 2.CORROSION TASK NR C53-107-02, CORROSION LEV EL 1. (M) 2 L 7 2 4F A16WE 1996080800433 19960808 00433 NM 1996 8 8 USAA960532 1 19960719 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS312 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 283AU 35101 23116 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO 1 INCH BY 3INCH CORRODED AREAS AT NUT PLATE HOLES T-CAP, BS 312 FLOO R BEAM BBL 0, RBL8. INSTALLED T-CAP REPAIR AND REPAIRED PER SRM 53-10-9. CORROSION TASK NRC53-107-02, CORROSION LEVEL 1. (M) 2 L 7 2 4F A16WE 1996080800434 19960808 00434 NM 1996 8 8 USAA960533 1 19960718 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM BS 1016 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 244US 37900 22752 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 8 INCHCORROSION FLOOR BEAM F/S 1016 BL 0 TO RBL 12. SPLICED I N FLOOR BEAM T-CAPAND DOUBLERS REPAIRED PER SRM 53-10-9 EA 41313. (M) 2 L 7 2 4F A16WE 1996080800435 19960808 00435 NM 1996 8 8 USAA960534 1 19960718 A 5314 KEELBEAM BOEING 737 737201 1384454 NM BS 710-727 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 244US 37900 22752 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH DIAMETERCORRODED AREA PLUS 4 KEEL BEAM RBL 6.4 FS 727 TO FS 710. SPOT FACED HOLESINSTALLED, INSTALLED REPAIR STRAP. REPAIRED PER EA 41303. (M) 2 L 7 2 4F A16WE 1996080800436 19960808 00436 NM 1996 8 8 USAA960535 1 19960718 A 5312 BULKHEAD BOEING 737 737201 1384454 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 244US 37900 22752 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 1INCH CRACK IN 178 BULKHEAD TWO PLACES LEFT SIDE AT LOWER LEFT MOUNT FORRADAR. INSTALLED DOUBLERS, REPAIRED PER TR 53-10-11.(M) 2 L 7 2 4F A16WE 1996080800437 19960808 00437 NM 1996 8 8 USAA960536 1 19960718 A 5312 BULKHEAD BOEING 737 737201 1384454 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 244US 37900 22752 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND APPROX 1 INCHCRACK IN 178 BULKHEAD 2 PLACES RIGHT SIDE AT LOWER RIGHT MO UNT FOR RADAR.INSTALLED DOUBLER AND FILLERS, REPAIRED PER TR 53-10-11.(M) 2 L 7 2 4F A16WE 1996080800438 19960808 00438 NM 1996 8 8 USAA960537 1 19960719 A 5330 SKIN BOEING 737 737296 1384486 NM BS520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 238US 40929 22398 BOS - DURING UNSCHEDULED MAINTENANCE, FOUND 2.4 INCH CRACK LTSIDE OF FUSELAGE S16L AT STATION 520, CONFIRMED BY EDDY CUR RENT. INSTALLEDDOUBLER PER SRM 53-30-3 FIG6 AS PERMANENT REPAIR. (M) 2 L 7 2 4F RT A16WE 1996080800439 19960808 00439 WP 1996 8 8 USAAD96103 1 19960712 A 2913 314195 HYDRAULICPUMP DOUG DC9 DC931 3022065 WP RT ENGINE FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 993VJ 72602 47332 FLT 1240 - PIT-BGM - IN CRUISE, RIGHT HYDRAULIC SYSTEM LOW PRESSURELIGHT AND RUDDER CONTROL MANUAL LIGHT ILLUMINATED. N O QUANTITY LOSS.RETURNED TO PIT. REPLACED NR 2 ENGINE DRIVEN PUMP. (M) 2 L 7 2 4F A6WE 1996080800440 19960808 00440 WP 1996 8 8 USAAD96106 1 19960715 A 3232 39567851 ACTUATOR DOUG DC9 DC981 3022081 WP NLG DOOR WORN A USAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 19 814US 48094 FLT 1448 - PIT-PHL - AFTER TAKEOFF, EXPERIENCED SEVERE NOSE GEARVIBRATION AND UNSAFE INDICATION ON NOSE GEAR. CYCLED GE AR, NO CHANGE.AFTER RETRACTING MAIN GEAR DOORS, GOT DOWN AND LOCKED INDICATION ON NOSEGEAR. RETURNED TO FIELD. REPLACE D LEFT AND RIGHT NOSE GEAR FORWARD DOORACTUATOR LINKS. (M) 2 L 7 2 4F A6WE 1996080800441 19960808 00441 WP 1996 8 8 USAAD96107 1 19960715 A 2150 CLAMP DOUG DC9 DC981 3022081 WP RT PACK DUCT LOOSE A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 813US 48093 FLT 647 - LGA-PBI - UNABLE TO HOLD CABIN ALTITUDE AT FL 350. CABINCLIMBING AT 500-600 FEET PER MINUTE. STILL UNABLE TO CONTROL IN MANUAL.DIVERTED TO CHS. FOUND LOOSE CLAMP ON RIGHT PACK DUCT WORK. RESECUREDDUCT. (M) 2 L 7 2 4F A6WE 1996080800442 19960808 00442 WP 1996 8 8 USAAD96108 1 19960716 A 3260 92743643 RELAY DOUG DC9 DC931 3022065 WP NLG FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 931VJ 47188 FLT 845 - CLT-SDF - NOSE GEAR UNSAFE LIGHT ON WITH GEAR RETRACTION.RECYCLED GEAR WITH SAME RESULT. RETURNED TO FIELD. R EPLACED R2-28 RELAY.GEAR SWING CHECKS GOOD.(M) 2 L 7 2 4F A6WE 1996080800443 19960808 00443 WP 1996 8 8 USAAD96109 1 19960723 A 2910 AC7031H8K1 FILTERASSY DOUG DC9 DC982 3022082 WP RIGHT FAILED A USAA O OTHER K FLUID LOSS AP APPROACH 1 EA 19 821US 49138 FLT 790 - CLT-IND - ON APPROACH, RIGHT HYDRAULIC SYSTEM QUANTITYBEGAN DROPPING. MAIN GEAR LOCKED, BUT HAD TO USE EMERGE NCY EXTENSION TO GETNOSE GEAR LOCKED. REPLACED RIGHT HYDRAULIC FILTER HOUSING ASSY. (M) 2 L 7 2 4F A6WE 1996080800444 19960808 00444 1996 8 8 USAAF96078 4 19960717 A 2213 6227476411 FLT CNTRL COMPTR FOKKER F28 F28MK0100 4990807 EU AVIONICS RACK FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 857US 11289 PIT - FL 1601 - AFTER TAKEOFF, CREW RECEIVED 'NO AUTOLAND'MESSAGE. NEITHER AUTOPILOT WOULD TURN ON. FLIGHT RETURNED TO PIT ANDLANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 FCC.(M) 2 L 7 2 4F RT 1996080800445 19960808 00445 NM 1996 8 8 USAASB96123 1 19960709 A 7931 21SN04211A OIL PRESSSW BOEING 737 737401 1384701 NM NR 2 ENG MALFUNCTIONED A USAA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 EA 19 422US 23989 CLT - FL 2127 - AT CRUISE, PRIOR TO DESCENT, THE NR 2 ENG OILPRESSURE INDICATED ZERO. ALL OTHER INDICATIONS WERE NORMAL . THE NR 2 ENGOIL PRESSURE SHOWED ZERO FOR ABOUT 60 SECONDS BEFORE IT WAS PLACED AT IDLE.THREE MINUTES LATER, SHUTDOWN THE NR 2 ENGINE FOR CAUTION REASONS. ANEMERGENCY WAS DECLARED AND THE FLIGHT LANDED SAFELY WITH NO FURTHERINCIDENT. TO TAL SINGLE ENGINE TIME WAS TWENTY-FIVE MINUTES. MAINTENANCEREPLACED THE NR 2 ENGINE OIL PRESSURE SWITCH AND OIL PRESSUR E TRANSMITTER.OPS CHECK WAS NORMAL. INSPECTION OF ENGINE AFTER SHUTDOWN SHOWED NODEFECTS. ALL ENGINE PARAMETERS CHECKE D NORMAL. (M) 2 L 7 2 4F RT A16WE 1996080800446 19960808 00446 NM 1996 8 8 USAASB96125 1 19960711 A 3350 0L3071BPEGPL LIGHT BOEING 737 7372B7 1384560 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 529AU 24411 LAS - FL 623 - FLOOR TRACK EMERGENCY LIGHTS INOP AT ROW 22 DEF.MAINTENANCE REPLACED THE EMERGENCY LIGHT LENSE P/N 07912 AND BULB P/N0L3071BPEGPL AT ROW 22 DEF. OPS CHECK GOOD.(M) 2 L 7 2 4F A16WE 1996080800447 19960808 00447 NM 1996 8 8 USAASB96131 1 19960716 A 5312 SEALS BOEING 737 7374B7 1384702 NM AFT PRESSBLKHD OUT OF POSITION A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 775AU 24933 BWI - FLT 262 - AFTER TAKEOFF FROM BWI, CAPTAIN WAS UNABLE TOPRESSURIZE AIRCRAFT. FLIGHT RETURNED TO FIELD AT BWI. NO EMERGENCY WASDECLARED AND THE FLIGHT LANDED WITH NO FURTHER INCIDENT. MX CLEANED WATERDRAIN LINES ON BOTH PACKS AND LIN ES TO LEFT AND RIGHT STANDBY TEMPERATURECONTROL VALVES. PACK FLOW CHECKED NORMAL AT MIXING CHAMBER. ALSO, FOUNDLARGE A IR LEAK AT REAR PRESURE BULKHEAD. SEAL WAS FOUND OUT OF THE TRACKWHERE APU DUCT ENTERS THE PRESSURIZED AREA. REPAIRED SAME. ENGINE RUNACCOMPLISHED AT ALL POWER SETTINGS. DUCT PRESSURE, PACK OPERATION ANDPRESSURIZATION OK. (M) 2 L 7 2 4F RT A16WE 1996080800448 19960808 00448 NM 1996 8 8 USAASB96132 1 19960717 A 3260 106122629 DOWNLOCKSENSOR BOEING 737 7372B7 1384560 NM NLG FAILED A USAA O OTHER N FALSE WARNING DE DESCENT 1 EA 19 286AU 23133 MCO - FL 1145 - ON DESCENT INTO MCO, LANDING GEAR WAS LOWERED,NOSE GEAR RED LIGHT FLICKERED ON. CAPTAIN WENT THROUGH MA NUAL GEAREXTENSION PROCEDURE. NOSE GEAR SHOWED DOWN AND LOCKED IN VIEW FINDER.EMERGENCY EQUIPMENT WAS CALLED OUT. ABOU T FOUR MINUTES FROM LANDING GEARLIGHT WENT TO GREEN. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCEREPLACED THE N OSE GEAR DOWNLOCK SENSOR. SYSTEM CHECKS NORMAL. (M) 2 L 7 2 4F A16WE 1996080800449 19960808 00449 NM 1996 8 8 USAASB96134 1 19960719 A 3260 CIRCUIT BREAKER BOEING 737 7374B7 1384702 NM GEARINDICATION TRIPPED A USAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 EA 19 445US 24863 PIT - FL 1211 - ON APPROACH INTO PIT, CREW RECEIVED A REDINDICATION LIGHT WITH THE GEAR DOWN. CAPTAIN REQUESTED A FLYBY OF THE TOWERAND RECEIVED CONFIRMATION OF THE GEAR BEING DOWN. AFTER TALKING WITHMAINTENANCE AND FOLLOWING ABNORMAL PRO CEDURES, THE CREW FOUND THAT A CIRCUITBREAKER WAS THE CAUSE OF THE LIGHT. THE CIRCUIT BREAKER WAS RESTORED ANDTHE LIGHT WENT OUT AS THE FLIGHT WAS EN ROUTE TO A SECOND FLYBY. THE SECONDFLYBY WAS CANCELLED AND THE FLIGHT LANDED SAFELY IN P IT. RESTORED CIRCUITBREAKER. (M) 2 L 7 2 4F RT A16WE 1996080800450 19960808 00450 NM 1996 8 8 USAASB96135 1 19960721 A 3397 WIRE BOEING 737 737301 1384611 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 560AU 23514 TPA - MAINTENANCE FOUND THE EMERGENCY LIGHTS INOP ON LEFT SEATAT EMERGENCY EXIT ROW. MAINTENANCE FOUND BROKEN WIRE. RE PAIRED SAME. OPSCHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996080800451 19960808 00451 NM 1996 8 8 USAASB96136 1 19960722 A 3260 INDICATION BOEING 737 7372Q9 138448M NM LANDING GEAR MALFUNCTIONED A USAA O OTHER N FALSE WARNING DE DESCENT 1 EA 19 231US 21976 CLT - FLT 1979 - ON DESCENT INTO CLT, WHEN LANDING GEAR LOWERED,CREW RECEIVED THREE GEAR RED LIGHTS AND THREE GEAR GREEN LIGHTS. THE GEARHORN SOUNDED AT FLAPS 15. CREW RECYCLED GEAR AND RECEIVED THREE GEAR GREENLIGHTS ONLY. THE FLIGHT LA NDED WITH NO FURTHER INCIDENT. MAINTENANCEJACKED AIRCRAFT AND CYCLED GEAR SEVERAL TIMES. UNABLE TO DUPLICATE.CLEANED A ND LUBED GEAR HANDLE. CYCLED GEAR SEVERAL MORE TIMES AND WAS STILLUNABLE TO DUPLICATE. SYSTEM OPS CHECK GOOD.(M) 2 L 7 2 4F A16WE 1996080800452 19960808 00452 NE 1996 8 8 WRLA96027 2 19960629 A 7320 51D440 EEC DATA PLUG DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE NR 1 ENG MISINSTALLED A WRLA A UNSCHED LANDING J W WARNING INDICATION INADEQUATE Q C TO TAKEOFF 1 EA 27 274WA 48633 DURING TAKEOFF ROLL, FLIGHT CREW NOTED NR 1 ENGINE WOULDNOT PRODUCE REQUESTED POWER (62,000 LB). ALL OTHER ENGINE PARAM ETERS WERENORMAL. FLIGHT CREW CONTINUED TAKEOFF. HOWEVER, AT PIC'S OPTION, AIRCRAFTRETURNED TO POINT OF DEPARTURE (AIR TURN-BACK). AIRCRAFT RETURNED WITHOUTINCIDENT. UPON INVESTIGATION, MX NOTED THE NR 1 ENGINE HAD ELECTRONICENGINE CONT ROL DATA PLUG INSTALLED (60,000 LBS THRUST LIMIT). AIRCRFTRETURNED TO SERVICE (ALL ENGINES RESTRICTED TO 60,000 LB THRU ST LIMIT).(M) 2 L 7 3 4F 4 F RT A22WE E24NE 1996080800453 19960808 00453 WP 1996 8 8 9616429941 1 19960617 A 5713 LONGERON DOUG DC9 DC932 3022066 WP WS 69-137 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3324L 47103 DURING H-CHECK, FOUND CORROSION ON THE RIGHT WING STR 17 FROM STA 69 TO 137. REPAIRED STRINGER (P/N 5919339-2) PER EA 9 9-110809. 2 L 7 2 4F A6WE 1996080800454 19960808 00454 WP 1996 8 8 9616439940 1 19960701 A 5713 LONGERON DOUG DC9 DC932 3022066 WP WS 58-112 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3322L 47031 DURING M-CHECK, FOUND CORROSION ON THE LEFT WING STR 13 TO 15, 17 BETWEEN XW 58 AND XRS 112. REPAIRED STRINGER (P/N 591 9239, 5919237, 5919238) PER EA 99-110827. 2 L 7 2 4F A6WE 1996080800455 19960808 00455 WP 1996 8 8 9616449940 1 19960702 A 5713 LONGERON DOUG DC9 DC932 3022066 WP WS 60/68 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3322L 47031 DURING M-CHECK, FOUND CORROSION ON THE RIGHT WING STR 14 AT XRS 68 AND ON STR 19 AT XRS 60. REPAIRED STRINGERS (P/N 591 9238-502, 5911279-502) PER EA 99-110820, -110876. 2 L 7 2 4F A6WE 1996080800456 19960808 00456 WP 1996 8 8 9616459941 1 19960702 A 5713 LONGERON DOUG DC9 DC932 3022066 WP WS 58-112 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3324L 47103 DURING H-CHECK, FOUND CORROSION ON LEFT WING STR 17 TO 18 BETWEEN XW 58 AND XRS 112. REPAIRED STRINGER (P/N 5919239-1, 5911279-1) PER EA 99-110802, -110871, -110526. 2 L 7 2 4F A6WE 1996080800457 19960808 00457 WP 1996 8 8 9616469964 1 19960705 A 5311 FRAME DOUG DC9 DC931 3022065 WP FS 718 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 912RW 47150 DURING M-CHECK, FOUND A CRACK IN THE FS 718 FRAME, LEFT SIDE, AT THE LOWER FORWARD POCKET. REPAIRED FRAME (P/N 9919618- 1) PER EA 99-108580. 2 L 7 2 4F A6WE 1996080800458 19960808 00458 WP 1996 8 8 9616479941 1 19960709 A 5713 LONGERON DOUG DC9 DC932 3022066 WP WS 69-137 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3324L 47103 DURING H-CHECK, FOUND CORROSION ON THE LEFT WING STR 21 FROM XRS 69 TO 137. REPAIRED STRINGER (P/N 5911280-1) PER EA 99 -110531. 2 L 7 2 4F A6WE 1996080800459 19960808 00459 WP 1996 8 8 9616489961 1 19960711 A 5320 PRESS PANEL DOUG DC9 DC931 3022065 WP FS 105 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 924RW 47185 DURING H-CHECK, FOUND FOUR CRACKS IN THE NOSE LANDING GEAR HORIZONTAL PRESSURE PANEL AT THE LEFT AND RIGHT SIDES AT THE INBOARD AND OUTBOARD VERTICAL STIFFENERS FS 105. REPAIRED PANEL (P/N 9910073-313) PER EA 99-109075. 2 L 7 2 4F A6WE 1996080800460 19960808 00460 WP 1996 8 8 9616499301 1 19960711 A 5320 FITTING DOUG DC9 DC982 3022082 WP FS 1217 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 301RC 48054 DURING H-CHECK, FOUND CORROSION ON THE FS 1217 FLOOR FITTING BETWEEN LONGERON 29R TO 30. REPLACED FITTING PER SRM 51-01 PG 1. 2 L 7 2 4F A6WE 1996080800461 19960808 00461 NM 1996 8 8 9616502713 1 19960717 A 5313 LONGERON BOEING 727 7272S7 138407Z NM FS 950 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 716RC 22021 DURING H-CHECK, FOUND CORROSION ON STR 29L AT BS 950A PLUS 1 AND BS 950F PLUS 8. REPAIRED STRINGER (P/N 65-56441-4) PER EA 27-105355, -105358. 2 L 7 3 4F A3WE 1996080800462 19960808 00462 NM 1996 8 8 9616512713 1 19960718 A 5241 FRAME BOEING 727 7272S7 138407Z NM SERVICE DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 716RC 22021 DURING H-CHECK, FOUND A CRACK IN THE LEFT AFT SERVICE DOOR FORWARD FRAME. REPAIRED FRAME (P/N 65-56992-3) PER EA 27-105 359. 2 L 7 3 4F A3WE 1996080800463 19960808 00463 WP 1996 8 8 9616529921 1 19960722 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 1143 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 943N 47647 DURING H-CHECK, FOUND A CRACK IN THE FS 1143 FRAME AT THE TAILCONE HANDLE LEFT SIDE. REPAIRED FRAME (P/N 9911842-501) P ER EA 99-110966. 2 L 7 2 4F A6WE 1996080800464 19960808 00464 WP 1996 8 8 9616539758 1 19960722 A 5230 FITTING DOUG DC9 DC941 302207N WP CARGO DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 758NW 47286 DURING H-CHECK, FOUND CRACKS IN THE AFT CARGO DOOR FORWARD END FITTINGS ON BEAMS NR 2, 3 AND 5. REPLACED FITTINGS PER S RM 51-30-5. 2 L 7 2 4F A6WE 1996080800465 19960808 00465 WP 1996 8 8 9616549301 1 19960723 A 5320 FITTING DOUG DC9 DC982 3022082 WP FS 1333 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 301RC 48054 DURING H-CHECK, FOUND CORROSION IN THE LONGERON 25L, 26L, AND 29L END FITTINGS AT FS 1333. REPLACED FITTINGS (P/N 39364 40-1N) PER SRM 51-01. 2 L 7 2 4F A6WE 1996080800466 19960808 00466 WP 1996 8 8 9616559856 1 19960723 A 5320 FITTING DOUG DC9 DC951 3022051 WP FS 699 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 765NC 47718 DURING H-CHECK, FOUND A CRACK IN THE KEEL LONGERON 30 END FITTING AT FS 699. REPLACED FITTING PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996080800467 19960808 00467 WP 1996 8 8 9616569856 1 19960723 A 5320 FITTING DOUG DC9 DC951 3022051 WP FS 1067 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 765NC 47718 DURING H-CHECK, FOUND CORROSION IN THE LONGERON 22R END FITTING AT FS 1067. REPLACED END FITTING PER SRM 51-30-2. 2 L 7 2 4F A6WE 1996080800468 19960808 00468 NM 1996 8 8 9616576614 1 19960725 A 5720 FITTING BOEING 747 747251B 1384892 NM BS 1000 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 614US 23059 DURING P-CHECK, FOUND A CRACK IN THE CENTER WING VERTICAL SUPPORT FRAME UPPER TIE FITTING BS 1000 AT LBL 35. REPLACED F ITTING PER SA 5715-01014-3. 2 L 7 4 4F A20WE 1996080800469 19960808 00469 WP 1996 8 8 9616679104 1 19960710 A 5312 BULKHEAD DOUG DC9 DC915 3022036 WP AFT PRESS BLKHD CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 94S 47204 DURING LINE CHECK, FOUND A 4.5 INCH CRACK IN THE AFT PRESSURE BULKHEAD -13 DOUBLER RADIUS, UPPER RIGHT CORNER. REPAIRED BULKHEAD DOUBLER (P/N 5910130-1) PER EA 91-110928. 2 L 7 2 4F A6WE 1996080800470 19960808 00470 WP 1996 8 8 9616689154 1 19960712 A 5320 DOUBLER DOUG DC9 DC914 3022034 WP CARGO DR JAMB CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8913E 45830 DURING H-CHECK, FOUND CORROSION IN THE AFT CARGO DOOR JAMB DOUBLER LOWER FORWARD CORNER. REPAIRED DOUBLER (P/N 5910158- 25) PER EA 91-110856. 2 L 7 2 4F A6WE 1996080800471 19960808 00471 WP 1996 8 8 9616699154 1 19960712 A 5330 SKIN DOUG DC9 DC914 3022034 WP FS 718 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8913E 45830 DURING H-CHECK, FOUND CORROSION ON THE FUSELAGE SKIN AT FS 718 BETWEEN LONGERONS 28R TO 29R. REPAIRED SKIN (P/N 5911425 -3) PER EA 91-109073. 2 L 7 2 4F A6WE 1996080800472 19960808 00472 WP 1996 8 8 9616709154 1 19960713 A 5330 SKIN DOUG DC9 DC914 3022034 WP BS 444-468 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8913E 45830 DURING H-CHECK, FOUND CORROSION ON THE FUSELAGE SKIN AT THE ANTENNA DOUBLERS FS 444 TO 468, LONGERON 29L TO 30. REPAIRE D SKIN (P/N 5911412-3) PER EA 91-110858. 2 L 7 2 4F A6WE 1996080800473 19960808 00473 WP 1996 8 8 9616719154 1 19960718 A 5312 BULKHEAD ANGLE DOUG DC9 DC914 3022034 WP FS 76 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8913E 45830 DURING H-CHECK, FOUND A CRACK IN THE NOSE LANDING GEAR WHEEL WELL RIGHT INBOARD BULKHEAD UPPER ATTACH ANGLE FS 76. REPA IRED ANGLE (P/N 9910073-60) PER EA 91-110861. 2 L 7 2 4F A6WE 1996080800474 19960808 00474 NM 1996 8 8 9616726614 1 19960720 A 5311 FRAME BOEING 747 747251B 1384892 NM FS 500 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 614US 23059 DURING P-CHECK, FOUND A 1.5 INCH CRACK IN THE FS 500 FRAME WEB AND WEB DOUBLER BELOW STR 12R. REPAIRED FRAME (P/N 65B01 718-520) AND DOUBLER (P/N 65B01718-162) PER EA 66-106540. 2 L 7 4 4F A20WE 1996080800475 19960808 00475 WP 1996 8 8 9616739154 1 19960723 A 5311 PRESS PANEL DOUG DC9 DC914 3022034 WP FS 105 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8913E 45830 DURING H-CHECK, FOUND A CRACK IN THE NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL AT THE LEFT OUTBOARD VERTICA L STIFFENER FS 105. REPAIRED PANEL (P/N 9910073-313) PER EA 91-110860. 2 L 7 2 4F A6WE 1996080800476 19960808 00476 WP 1996 8 8 9616749301 1 19960726 A 5320 FITTING DOUG DC9 DC982 3022082 WP FS 1200 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 301RC 48054 DURING H-CHECK, FOUND CORROSION ON THE LONGERON 23L TIE FITTING AT FS 1200. REPLACED FITTING (P/N 3913208-509) PER SRM 51-01 ITEM C PG 1. 2 L 7 2 4F A6WE 1996080800477 19960808 00477 WP 1996 8 8 9616759758 1 19960729 A 5313 LONGERON DOUG DC9 DC941 302207N WP FS 170 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 758NW 47286 DURING H-CHECK, FOUND CORROSION ON LONGERON 29L AND IN ITS END FITTING AT FS 170. REPAIRED LONGERON AND REPLACED FITTIN G PER SRM 53-02 FIG 2 AND 51-30-2 PG 2 FIG 1. 2 L 7 2 4F A6WE 1996080800478 19960808 00478 WP 1996 8 8 9616769996 1 19960729 A 5320 FITTING DOUG DC9 DC931 3022065 WP FS 229 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8932E 47141 DURING M-CHECK, FOUND CORROSION IN THE RIGHT CUSP FITTING AT FS 229, LONGERON 18R. REPLACED FITTING (P/N 4912772-504N) PER SRM 51-30-1. 2 L 7 2 4F A6WE 1996080800479 19960808 00479 WP 1996 8 8 9616779758 1 19960730 A 5320 FITTING DOUG DC9 DC941 302207N WP FS 699 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 758NW 47286 DURING H-CHECK, FOUND A CRACK IN THE KEEL LONGERON 30 RIGHT SIDE END FITTING AT FS 699. REPLACED FITTING (P/N 3924029-5 02N) PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996080800480 19960808 00480 WP 1996 8 8 9616789909 1 19960801 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 633 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 959N 47255 DURING M-CHECK, FOUND CORROSION ON THE FS 633 FRAME FITTING BETWEEN KEEL LONGERONS 29R AND 29.5R. REPLACED FITTING PER SRM 51-30-5 PG 1. 2 L 7 2 4F A6WE 1996080800481 19960808 00481 WP 1996 8 8 9616799758 1 19960801 A 5210 FITTING DOUG DC9 DC941 302207N WP PAX DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 758NW 47286 DURING H-CHECK, FOUND A CRACK IN THE AFT ENTRY DOOR AT THE UPPER LEFT DOOR STOP. REPLACED FITTING. 2 L 7 2 4F A6WE 1996080800482 19960808 00482 WP 1996 8 8 9616899851 1 19960802 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 760NC 47708 DURING LINE CHECK, FOUND ONE SECTION OF OVERHEAD EMERGENCY LIGHTS INOPERATIVE AFT OF OVERWING EXITS. REPLACED BATTERY P ACK B5-58, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996080800483 19960808 00483 WP 1996 8 8 9616909104 1 19960805 A 3350 BATTERY PACK DOUG DC9 DC915 3022036 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 94S 47204 DURING LINE CHECK, FOUND FORWARD AND AFT EMERGENCY CEILING LIGHTS INOPERATIVE. REPLACED BATTERY PACKS BETWEEN GALLEYS A ND RIGHT AFT LAV, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996080800484 19960808 00484 WP 1996 8 8 9616919923 1 19960803 A 3350 60030451 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 927RC 47469 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT NACELLE AND TAILCONE EMERGENCY EVACUATION SLIDE LIGHTS INOPERATIVE. REPL ACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996080800485 19960808 00485 WP 1996 8 8 9616929923 1 19960803 A 3350 6011779 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN MALFUNCTIONED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 927RC 47469 DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT NACELLE AND TAILCONE EVACUATION SLIDE LIGHTS INOPERATIVE. REPLACED POWE R SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996080800486 19960808 00486 WP 1996 8 8 9616939952 1 19960804 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 916RW 47144 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. FOUND BROKEN WIRE IN TRACK. REPAIRED WIRE, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996080800487 19960808 00487 WP 1996 8 8 9616949954 1 19960804 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP TAIL COMPT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 921RW 47164 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY EVACUATION LIGHTS IN TAIL COMPARTMENT INOPERATIVE. REPLACED BATTERI ES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996080800488 19960808 00488 WP 1996 8 8 9616959955 1 19960802 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN PINCHED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 922RW 47182 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD RIGHT CABIN ENTRY DOOR EMERGENCY EXIT SIGN LIGHTS INOPERATIVE. FOUND WIRES PINCHED UNDER SEAT 1D. REPLACED FUSE, REPAIRED AND REPOSITIONED WIRES UNDER SEAT AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996080800489 19960808 00489 WP 1996 8 8 9616969978 1 19960804 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP TAILCONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9342 47391 DURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996080800490 19960808 00490 WP 1996 8 8 9616979603 1 19960804 A 3350 60030451 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 603NW 47101 DURING LINE MAINTENANCE INSPECTION, FOUND OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND BATTERI ES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996080800491 19960808 00491 WP 1996 8 8 9616989955 1 19960804 A 3010 3927102 AUGMENTATION VLV DOUG DC9 DC931 3022065 WP AFT ACCESS CMPT MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 922RW 47182 RIGHT AND LEFT ICE PROTECTION TEMPERATURE HIGH, PRESSURE ABNORMAL AND AIR CONDITIONING SUPPLY TEMPERATURE HIGH LIGHTS IL LUMINATED AFTER TAKEOFF. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT AUGMENTATION V ALVE, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996080800492 19960808 00492 WP 1996 8 8 9616999972 1 19960803 A 2130 RELAY DOUG DC9 DC931 3022065 WP E/E BAY MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 9336 47338 AUTO PRESSURIZATION SYSTEM FAILED AFTER TAKEOFF, OUTFLOW VALVE REMAINED OPEN. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY ON GROUND. REPLACED GROUND SENSE RELAY R2-4 AS A PRECAUTION. 2 L 7 2 4F A6WE 1996080800493 19960808 00493 WP 1996 8 8 9617009972 1 19960803 A 2130 PRESS REGULATOR DOUG DC9 DC931 3022065 WP CABIN FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 9336 47338 AUTO PRESSURIZATION SYSTEM FAILED AFTER TAKEOFF. CABIN ALTITUDE CLIMBED IN CONJUNCTION WITH AIRCRAFT ALTITUDE. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED CABIN PRESSURE RESET REGULATOR AND AMPLIFIER, OPERATI ONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996080800494 19960808 00494 WP 1996 8 8 9617019902 1 19960803 A 3260 LIGHT SOCKET DOUG DC9 DC931 3022065 WP NLG GREEN IND LOOSE A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 952N 47073 NOSE LANDING GEAR GREEN LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NOSE GEAR GREEN LIGHT SOCKET LOOSE CAUSING PRESS TO TEST FUNCTION TO BE ACTIVATED AT ALL TIMES. SEC URED SOCKET AND RELAMPED, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996080800495 19960808 00495 EU 1996 8 8 9617023218 1 19960804 A 3260 PROX SENSOR AIRBUS 320 A320211 3930320 EU LANDING GEAR MALFUNCTIONED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 318US 206 DURING APPROACH AFTER LANDING GEAR EXTENSION, RECEIVED L/G GEAR NOT DOWNLOCKED MESSAGE. CYCLED LANDING GEAR AND ALL IND ICATIONS WERE NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED PROXIMITY SENSOR 25GA, LANDING GEAR SELEC TOR VALVE AND NR 2 LANDING GEAR CONTROL INTERFACE UNIT, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996080800496 19960808 00496 NM 1996 8 8 96DHK72194C 1 19960606 A 5347 SEAT TRACK BOEING 727 727228 NM BS 1110/1130 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND INBD FLANGE OF SEAT TRACK HAS CORROSION CRACK BETWEEN STA 1110 AND 1130 AT RBL 46. FABRICATED AND IN STALLED NEW SEAT TRACK FROM BS 1010 TO BS 1130 PER SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996080800497 19960808 00497 NM 1996 8 8 96DHL721109 1 19960604 A 5730 PANEL BOEING 727 727228 NM RT WING DELAMINATED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, RT UPPER WING APU EXHAUST FIBERGLASS PANEL IS DELAMINATED ON OUTBD SIDE. INSTALLED BONDING REPAIR PER SRM 5 1-40-6, 65 BY 27.25. 2 L 7 3 4F A3WE 1996080800498 19960808 00498 NM 1996 8 8 96DHL721110 1 19960606 A 5712 RIB BOEING 727 727228 NM WS 686.5 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND RIB AT WS 686.5 LOWER CHORD CRACKED AT STR 6 AND STR 8. STOP DRILLED HOLES, INSTALLED REPAIR AT STR 6 PER 57-10-5, 10.5 BY 2. INSTALLED REPAIR AT STR 8 PER SRM 57-10-5, 12.5 BY 2. 2 L 7 3 4F A3WE 1996080800499 19960808 00499 NM 1996 8 8 96DHL721114 1 19960608 A 5315 FLOORBEAM BOEING 727 727228 NM BS 950 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND CABIN FLOORBEAM AT BS 950 RBL 6 TO RBL 19 HAS SEVERE CORROSION. REMOVED AND REPLACED FLOORBEAM 10 FT BY 7 LONG PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996080800500 19960808 00500 NM 1996 8 8 96DHL72185C 1 19960604 A 5330 SKIN BOEING 727 727228 NM BS 1430 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND BULGING UNDER RAIN GUTTER AT BOTH SIDES OF SEAM STA 1430 WL 259 EXT RT SIDE. CUT OUT DAMAGED SKIN, FA BRICATED FILLER 3 BY 4 FT, DOUBLER 6 BY 3 FT; FILLER 2 BY 3 FT AND DOUBLER 4 BY 6, INSTALLED PER SRM 55-30-3. 2 L 7 3 4F A3WE 1996080800501 19960808 00501 NM 1996 8 8 96DHL72187C 1 19960605 A 5311 FRAME BOEING 727 727228 NM BS 760.95 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, BS 760.95 RT SIDE FRAME CRACKED THROUGH INBD FLANGE EXTENDING OUTBD TO OUTER FLANGE. INSTALLED REPAIR KIT O N CABIN FRAME AT FS 760.95 PER S/B 53-197. 2 L 7 3 4F A3WE 1996080800502 19960808 00502 NM 1996 8 8 96DHL72190C 1 19960605 A 5313 BAC1493512 STRINGER BOEING 727 727228 NM BS 300 DENTED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, SMALL DENTS AT FUS STA 300 STR 14, 15, RT. REPAIRED STRINGER AT STA 14 PER SRM 53-10-3, 18. 2 L 7 3 4F A3WE 1996080800503 19960808 00503 NM 1996 8 8 96DHL72193C 1 19960606 A 5315 FLOORBEAM BOEING 727 727228 NM BS 1110 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND HEAVY CORROSION ON FLOORBEAM UPPER FLANGE AT BS 1130 BETWEEN RBL 15 AND RBL 44. CUT OUT DAMAGED AREA, FABRICATED STRAP 9.75 BY 1 AND L-ANGLE 9.75 BY 2.5. INSTALLED REPAIR PER SRM 51-10-2. FABRICATED AND INSTALLED REPAIR AT UPPER FLANGE L-ANGLE 11.5 AND STRAP 11.5 BY 1 PER SRM 51-40-4. 2 L 7 3 4F A3WE 1996080800504 19960808 00504 NM 1996 8 8 96DHL72195C 1 19960606 A 5347 SEAT TRACK BOEING 727 727228 NM BS 1110-1130 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, SEAT TRACK FLANGES CORRODED AT RBL 55 BETWEEN STA 1100 AND1130. REPLACED SEAT TRACK PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996080800505 19960808 00505 NM 1996 8 8 96DHL72197C 1 19960606 A 5313 STRINGER BOEING 727 727228 NM BS 580-600 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, STRINGER 26L HAS CORROSION BETWEEN STA 580 AND 600. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-8 STRINGE R 14 AND SPLICES 2 EA 11 LONG. 2 L 7 3 4F A3WE 1996080800506 19960808 00506 NM 1996 8 8 96DHL72198C 1 19960606 A 5347 SEAT TRACK BOEING 727 727228 NM BS 998-1025 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721SH 19545 AT C-CHECK, SEAT TRACK BL 24 LT CORRODED STA 998 TO 1025. REMOVED AND REPLACED SEAT TRACK FROM STA 970 TO 1110 PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996080800507 19960808 00507 NM 1996 8 8 96FDEA01314 1 19960802 A 5320 FITTING BOEING 727 72722C 138400F NM BS 740 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 STR END FITTING CRACKED STA 740 STR 5R. REMOVED AND REPLACED STR END FITTING PER 51-10-01. 2 L 7 3 4F A3WE 1996080800508 19960808 00508 NM 1996 8 8 96FDEA01315 1 19960805 A 5711 6518538 SPAR CHORD BOEING 727 72722 1384002 NM BS 870 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 181 18868 CENTER WING TANK INTERNAL BS 870 REAR SPAR UPPER CHORD CORRODED FROM RBL 6 TO 48. REMOVED CORROSION, CUT OUT SPAR WEB F ROM RBL 54 TO LBL 51, INSTALLED WEB DOUBLER AND NEW SPAR CHORD. ALL WORK ACCOMPLISHED PER SRM 51-40-4 FIG 1 ESO 11782 D ATE 7-23-96, FAR 8110-3 DATED 7-23-96 AND EA 7-5710-28808 DATED 7-23-96. 2 L 7 3 4F A3WE 1996080800509 19960808 00509 NM 1996 8 8 96FDEA01316 1 19960805 A 5330 SKIN BOEING 727 72722 1384002 NM BS 1140-1183 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 181FE 18868 FUSELAGE SKIN CORROSION BETWEEN SKIN LAYERS FROM BS 1140 TO 1183 STR 15 TO 20R. REMOVED CORROSION AND CUT OUT DAMAGED S KIN BS 1148 TO 1183 STR 14 TO 20R. INSTALLED DOUBLER PER EA 7-5310-28796A AND SRM 53-30-3 FIG 12. 2 L 7 3 4F A3WE 1996080800510 19960808 00510 NM 1996 8 8 96FDEA01317 1 19960802 A 5315 FLOOR BEAM BOEING 727 72722C 138400F NM BS 600 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 NR0436, FWD CARGO BS 600 BL 0 TO RBL 24 HEAVY CORROSION ON LOWER SIDE OF LOWER LEG OF MAIN CARGO FLOOR BEAM. *S/D* INS TALLED FLOOR BEAM REPAIR PER SRM 53-10-8. 2 L 7 3 4F A3WE 1996080800511 19960808 00511 NM 1996 8 8 96FDEA01318 1 19960804 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 720 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 NR0440, FWD CARGO BS 720 STR 23R HEAVY CORROSION INSIDE STR ON LOWER LEG. *S/D* REMOVED CORROSION AND INSTALLED STRING ER REPAIR PER 53-10-3. 2 L 7 3 4F A3WE 1996080800512 19960808 00512 NM 1996 8 8 96FDEA01319 1 19960731 A 5711 SPAR WEB BOEING 727 72722C 138400F NM WS 870 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 CTR FUEL TANK BAY 3, AFT SPAR WEB AT STA 870 BULGED, CRACKED AND CORRODED WITH POPPED RIVETS AT APPROX LBL 40 NEAR UPPER CHORD ANGLE. UPPER CHORD ANGLE HAS POPPED RIVETS IN THIS AREA ALSO. 2 L 7 3 4F A3WE 1996080800513 19960808 00513 NM 1996 8 8 96FDEA01320 1 19960731 A 5320 SPLICE BOLTS BOEING 727 72722C 138400F NM BS 360 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 NR0879 STA 360 STR 26 LT AND RT SEVERAL SPLICE BOLTS ARE HEAVILY CORRODED AND NUTS FOR THE BOLTS ALSO CORRODED. 2 L 7 3 4F A3WE 1996080800514 19960808 00514 NM 1996 8 8 96FDEA01321 1 19960731 A 5320 SKATE ANGLE BOEING 727 72722C 138400F NM BS 294 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 NR0867 AND 0868, STA 294 RT SIDE OF DOGHOUSE BELOW FLOOR PANEL CORROSION IN LWR FWD CORNER BELOW NUT AND BEHIND SEALANT - NR0867 STA 294 R/H SIDE OF DOGHOUSE, BELOW FLOOR PANEL CORROSION ON ANGLE THAT ATTACHS TO DOGHOUSE LWR FWD AREA SK ATE ANGLE NR0868. *S/D* FOR NR0868 REMOVED AND REPLACED SKATE ANGLE WITH NEW SKATE ANGLE PER SRM 53-10-04. 2 L 7 3 4F A3WE 1996080800515 19960808 00515 NM 1996 8 8 96FDEA01322 1 19960731 A 5320 SKATE ANGLE BOEING 727 72722C 138400F NM BS 294-312 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 NR0875 AND 0949, STA 294 TO 312 LT SIDE OF DOGHOUSE NOSE W/W BELOW FLOOR PANEL HAS CORROSION ON SKATE ANGLE LWR I/B SECT ION OF TORQUE BOX NR0875. LT SKATE ANGLE AT STA 294.5 TO 298 HEAVY CORROSION ON VERTICAL SIDE OF SKATE ANGLE NR0949. 2 L 7 3 4F A3WE 1996080800516 19960808 00516 WP 1996 8 8 ABXA9600605 1 19960802 A 3297 320552 WIRE DOUG DC9 DC932 3022066 WP NLG BROKEN A ABXA K NONE P NO WARNING INDICATION LD LANDING 1 GL 23 987AX 47364 WITH THROTTLES AT IDLE, NOSE GEAR UNSAFE LIGHT NOT ON. WHEN GEAR EXTENDED, NOSE GEAR DOWN LIGHT NOT ON. RECYCLED GEAR, ALL THREE GREEN LIGHTS CAME ON. REPAIRED THE BROKEN STRANDS OF WIRE AND REPLACED THE GROUNDING LUG AT WIRE NR G213-24N . THE INDICATION SYSTEM OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996080800517 19960808 00517 WP 1996 8 8 ABXA9600606 1 19960805 A 3350 41B004AD07G3 BATTERIES DOUG DC9 DC915 3022036 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 927AX 45717 EMERGENCY LIGHTS DIM WHEN TESTED. REPLACED BATTERIES IN EMERGENCY LIGHT POWER PACK, OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996080800518 19960808 00518 WP 1996 8 8 ABXA9600607 1 19960802 A 3350 6012233 BATTERY PACK DOUG DC8 DC863 302198A WP CABIN DISCHARGED A ABXA K NONE L NO TEST CR CRUISE 1 GL 23 824AX 46141 AFTER TAKEOFF, EMERGENCY LIGHTS CAME ON. REPLACED EMERGENCY LIGHTING BATTERY PACK, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1996080800519 19960808 00519 WP 1996 8 8 CALA9601124 1 19960802 A 3320 0398030 BALLAST DOUG DC9 DC982 3022082 WP CABIN SIDEWALL FAILED A CALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 09 72825 49485 AN ELECTRICAL SMELL WAS OBSERVED IN THE FIRST CLASS CABIN WHILE AIRCRAFT WAS AT GATE WITH NO PASSENGERS ON BOARD. MAINT ENANCE FOUND CENTER LOWER BALLAST FOR LOWER SIDEWALL LIGHTS AT SEAT 1 A, C BAD. THE CIRCUIT BREAKER WAS PULLED AND COLL ARED AND THE PLUG WAS DISCONNECTED FROM BALLAST. THE LIGHTS WERE PLACARDED INOPERATIVE IAW MEL 33-02. 2 L 7 2 4F A6WE 1996080800520 19960808 00520 WP 1996 8 8 CALA9601125 1 19960805 A 2121 6054577 AIR DIST FAN DOUG DC9 DC982 3022082 WP BS 218 BURNED WIRE A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 09 16802 27273 19150 49222 SMOKE ENTERED THE COCKPIT AFTER ENGINE START AT IAH. THE PACKS WERE TURNED OFF AND THE ENGINES WERE SHUTDOWN. THE SMOK E WAS ACCOMPANIED BY POPPING AND ARCING IN MAIN ENTRANCE OVERHEAD. INSPECTION OF STA 218 OVERHEAD FOUND WIRE FOR RT HEA T EXCHANGER COOLING FAN BURNED. ALL OVERHEAD SPLICES AT STA 218 FOR BOTH THE LEFT AND RIGHT GROUND COOLING FANS WERE RE SPLICED. IN ADDITION, 50 AMP CIRCUIT BREAKERS B1-254, B1-255, B1-256 AND THE LEFT AND RIGHT HEAT EXCHANGER RELAYS R2-53 AND R2-54 WERE REMOVED AND REPLACED. OPERATION OF THE LEFT COOLING FAN CHECKED GOOD. THE RIGHT COOLING FAN WAS PLACAR DED INOPERATIVE PENDING PRECAUTIONARY REPLACEMENT. 2 L 7 2 4F A6WE 1996080800521 19960808 00521 WP 1996 8 8 CALA9601126 1 19960719 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BAGG DOOR JAMB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15841 49581 INSPECTION FOUND Z-ANGLE AT AFT BAGGAGE BIN LOWER DOOR JAMB CORRODED. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10- 03. 2 L 7 2 4F A6WE 1996080800522 19960808 00522 WP 1996 8 8 CALA9601127 1 19960726 A 5210 BEAM DOUG DC9 DC982 3022082 WP MAIN CABIN DR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15841 49581 INSPECTION FOUND A .75 INCH CRACK ON UPPER HORIZONTAL BEAM AT AFT CORNER OF MAIN CABIN DOOR AND A 1 INCH CRACK WAS FOUND ON UPPER HORIZONTAL BEAM AT FORWARD CORNER OF MAIN CABIN DOOR. DOUBLER REPAIRS WERE INSTALLED IAW SRM 52-05, FIGURE 31 , SHEET 10 SECTION T-T AND SECTION U-U. 2 L 7 2 4F A6WE 1996080800523 19960808 00523 WP 1996 8 8 CALA9601128 1 19960717 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 503-541 CREASED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15841 49581 INSPECTION FOUND A CREASE IN FUSELAGE SKIN FROM STA 503 TO 541 AT LONGERON 22R. THE SKIN WAS REPAIRED IAW ECRA 5330-024 21. 2 L 7 2 4F A6WE 1996080800524 19960808 00524 WP 1996 8 8 CALA9601129 1 19960716 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 236 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15841 49581 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 236, LONGERON 17L TO 18L. THE DENTED AREA OF SKIN WAS CUT OUT AND A REPAIR WAS INSTALLED IAW ECRA 5330-02420. 2 L 7 2 4F A6WE 1996080800525 19960808 00525 WP 1996 8 8 CALA9601130 1 19960716 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 227 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15841 49581 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 227. THE AREA WAS REPAIRED IAW SRM 51-10-03. 2 L 7 2 4F A6WE 1996080800526 19960808 00526 WP 1996 8 8 CALA9601131 1 19960730 A 5712 RIB DOUG DC9 DC982 3022082 WP WING LE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15841 49581 INSPECTION FOUND A .25 INCH CRACK IN WING LEADING EDGE RIB OUTBOARD OF NR 8 SLAT TRACK. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5710-01749. 2 L 7 2 4F A6WE 1996080800527 19960808 00527 WP 1996 8 8 CALA9601132 1 19960716 A 5320 DOOR JAMB DOUG DC9 DC982 3022082 WP RT MLG DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15841 49581 INSPECTION FOUND A 1 INCH CRACK IN RT MLG DOOR JAMB. A REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 2. 2 L 7 2 4F A6WE 1996080800528 19960808 00528 WP 1996 8 8 CALA9601133 1 19960717 A 5730 DOUBLER DOUG DC9 DC982 3022082 WP BS 194 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15841 49581 INSPECTION FOUND WING LEADING EDGE SPLICE DOUBLER CRACKED BETWEEN NR 5 AND NR 6 SLAT TRACK, STA 194. THE AREA WAS REPAI RED IAW ECRA 5710-01645. 2 L 7 2 4F A6WE 1996080800529 19960808 00529 SO 1996 8 8 COMA9610238 1 19960805 A 5246 FUEL DOOR EMB 120 EMB120RT SO FUEL COMPT NOT SECURED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 261CA 120254 SERVICE DOOR WARNING LIGHT CAME ON AFTER TAKEOFF. SECURED SINGLE POINT FUEL SERVICE DOOR. 2 L 7 2 4T RT A31SO 1996080800530 19960808 00530 SO 1996 8 8 COMA9610239 1 19960805 A 6120 PROP GOVERNOR EMB 120 EMB120RT SO LEFT MALFUNCTIONED A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 256CA 120245 LT PROPELLER WILL NOT AUTO-FEATHER OR MANUAL FEATHER. COULD NOT DUPLICAE DISCREPANCY, SYSTEM TEST NORMAL AND ACFT RETUR NED TO SERVICE. 2 L 7 2 4T RT A31SO 1996080800531 19960808 00531 SO 1996 8 8 COMA9610240 1 19960803 A 2910 HYD SYST EMB 120 EMB120RT SO RIGHT MOISTURE CONTAM A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 255CA 120238 RT HYDRAULIC RESERVOIR LOW PRESSURE WARNING ILLUMINATED. DRAINED MOISTURE FROM RESERVOIR, SYSTEM CHECK NORMAL. 2 L 7 2 4T RT A31SO 1996080800532 19960808 00532 SO 1996 8 8 COMA9610241 1 19960804 A 2752 3431001001 ACTUATOR EMB 120 EMB120RT SO RT TE FLAP LEAKING A COMA K NONE K FLUID LOSS UK UNKNOWN 1 SO 01 257CA 120248 BLUE HYDRAULIC SYSTEM FAILED. REPLACED THE RT NACELLE FLAP ACTUATOR. 2 L 7 2 4T RT A31SO 1996080800533 19960808 00533 EA 1996 8 8 COMA9660128 1 19960804 A 5240 SERVICE DOORS CNDAIR CL600 CL6002B19 EA CABIN NOT SECURED A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 934CA 7042 OVERBOARD COOL IS INOP. OPENED AND RECLOSED THE CABIN AND SERVICE DOORS. OVERBOARD COOL OPERATES NORMAL. 2 L 7 2 4F RT A21EA 1996080800534 19960808 00534 EA 1996 8 8 COMA9660129 1 19960803 A 3260 864806 PSEU CNDAIR CL600 CL6002B19 EA AVIONICS MALFUNCTION A COMA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 915CA 7013 NOSE LANDING GEAR DOOR OPEN LIGHT ILLUMINATED DURING TAXI AND NOSE WHEEL STEERING FAILED. REPLACED THE PROXIMITY SENSOR ELECTRONIC UNIT. 2 L 7 2 4F RT A21EA 1996080800535 19960808 00535 EA 1996 8 8 COMA9660130 1 19960804 A 3220 16400105 DRAG BRACE CNDAIR CL600 CL6002B19 EA NLG MALFUNCTION A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 916CA 3215 620 7014 LANDING GEAR DISAGREE MESSAGE WITH GEAR UP, WITH GEAR DOWN NLG DOORS REMAIN OPEN. REPLACED THE NLG DRAG BRACE ASSY. 2 L 7 2 4F RT A21EA 1996080800536 19960808 00536 NM 1996 8 8 DHL72160C 1 19960610 A 5347 15201466 SEAT TRACK BOEING 727 727228 NM BS 848 WORN A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, LOCK HOLES WERE ELONGATED ON NR 2 SEAT TRACK LBL 45 STA 848. REMOVED AND REPLACED TRACK PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996080800537 19960808 00537 NM 1996 8 8 DHL9672101C 1 19960609 A 5313 STRINGER BOEING 727 727228 NM BS 720 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND STR 22 LT CRACKED BETWEEN STA 720A AND 720B. FABRICATED AND INSTALLED STRINGER REPAIR 7 INCHES LONG P ER SRM 53-10-3. 2 L 7 3 4F A3WE 1996080800538 19960808 00538 NM 1996 8 8 DHL9672102C 1 19960609 A 5210 SKIN BOEING 727 727228 NM PAX DOOR CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND FWD ENTRY DOOR AFT INNER SKIN HAS CRACK GRIND OUT. STOP DRILLED CRACK, INSTALLED DOUBLER REPAIR 4 INC HES BY 4 FT PER SRM 51-40-2. 2 L 7 3 4F A3WE 1996080800539 19960808 00539 NM 1996 8 8 DHL9672103C 1 19960505 A 5330 SKIN BOEING 727 727228 NM BS 188 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, EXTERIOR FUSELAGE HAS 2 CRACKS AROUND FASTENERS AT BS 188 WL 224 AND WL 219, BS 196 AND WL 222 LEFT SIDE. C UT OUT DAMAGE, INSTALLED DOUBLER 15 BY 18.5 PER SRM 53-30-3. 2 L 7 3 4F A3WE 1996080800540 19960808 00540 NM 1996 8 8 DHL9672104C 1 19960605 A 5330 SKIN BOEING 727 727228 NM BS 227 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND EXTERIOR FUSELAGE WITH CRACK AT BS 227.8 WL 223 AND BS 235.8 AT WL 230 LEFT SIDE. INSTALLED DOUBLER REPAIR PER SRM 53-20-3, REPAIR 15 BY 18.5. 2 L 7 3 4F A3WE 1996080800541 19960808 00541 NM 1996 8 8 DHL9672105C 1 19960606 A 5712 RIB BOEING 727 727228 NM WS 629 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND RIB AT WS 629 LOWER CHORD CRACKED AT STR 8. INSTALLED REPAIR PERSRM 57-10-5, 9 BY 2. 2 L 7 3 4F A3WE 1996080800542 19960808 00542 NM 1996 8 8 DHL9672106C 1 19960607 A 5712 RIB BOEING 727 727228 NM WS 601 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND RIGHT WING RIB LOWER ATTACHMENT CRACK AT WS 601 AT S8 AND S6. STOP DRILLED CRACKS AND INSTALLED REPA IR PER SRM 57-10-5, STR 8 REPAIR 9 BY 5, STR 6 REPAIR 10 BY 5. 2 L 7 3 4F A3WE 1996080800543 19960808 00543 NM 1996 8 8 DHL9672107C 1 19960606 A 5712 RIB BOEING 727 727228 NM WS 686 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND CRACK IN RIB LOWER CHORD WS 686.6 STR 6. STOP DRILLED CRACK, INSTALLED REPAIR PER SRM 57-10-5, 9.5 B Y 2. 2 L 7 3 4F A3WE 1996080800544 19960808 00544 NM 1996 8 8 DHL9672108C 1 19960505 A 5754 ATTACH BOEING 727 727228 NM NR 7 SLAT ACT CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND NR 7 SLAT ACTUATOR ROD END ATTACH IN OUTBD RIB IN SLAT CRACKED. STOP DRILLED CRACK, INSTALLED REPAIR PER SRM 57-50-3, REPAIR 5 BY 4 BY .5. 2 L 7 3 4F A3WE 1996080800545 19960808 00545 NM 1996 8 8 DHL9672109C 1 19960805 A 5347 152729 SEAT TRACK BOEING 727 727228 NM BS 600 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND NR 6 SEAT TRACK RBL 45 HAS CORROSION AND CRACKED AT STA 600 THROUGH 660. REMOVED AND REPLACED SEAT TR ACK PER SRM 51-30-2, 60 INCHES LONG. 2 L 7 3 4F A3WE 1996080800546 19960808 00546 NM 1996 8 8 DHL96721100 1 19960601 A 5315 14902785 FLOORBEAM BOEING 727 727228 NM BS 328 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, CABIN FLOORBEAM BS 328 LBL 30 IS CORRODED AT FLOORBEAM SUPPORT ANGLE ATTACH POINTS. INSTALLLED ANGLE REPAIR S 17 BY 1.5 BY 1.5, 15.25 BY 1.5 BY 1.5 PER SRM 51-40-4. 2 L 7 3 4F A3WE 1996080800547 19960808 00547 NM 1996 8 8 DHL96721101 1 19960605 A 5311 FRAME BOEING 727 727228 NM BS 1166 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, BAGGAGE FRAME CRACKED AND CORRODED AT STA 1166 BETWEEN STR 29 AND 30 RT. CUT OUT DAMAGED AREA 2 BY 4 AND IN STALLED REPAIR PER SRM 53-10-4, 9 BY 8. 2 L 7 3 4F A3WE 1996080800548 19960808 00548 NM 1996 8 8 DHL96721102 1 19960620 A 5330 SKIN BOEING 727 727228 NM BS 600 DENTED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND DENT IN FUSELAGE SKIN AT MCD DOUBLER APPROX STA 600 BELOW STR 17L. INSTALLED DOUBLER REPAIR PER SRM 5 3-30-3, 12 BY 7. 2 L 7 3 4F A3WE 1996080800549 19960808 00549 NM 1996 8 8 DHL96721103 1 19960609 A 5347 SEAT TRACK BOEING 727 727228 NM BS 950 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND SEAT TRACK AT RBL 48 CORRODED AT STA 950C TO 950F. REPLACED TRACK PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996080800550 19960808 00550 NM 1996 8 8 DHL96721104 1 19960611 A 5741 FITTING BOEING 727 727228 NM LT WING GOUGED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, LEFT WING FRONT SPAR TERMINAL FITTING DAMAGED. REAMED DAMAGED AREA, MADE BUSHING SLEEVE PER DRAWING 65C3617 6, INSTALLED PER BOEING TELEX, INSTALLED BOTTLE BUSHING AND PIN PER M/M 57-41-1. 2 L 7 3 4F A3WE 1996080800551 19960808 00551 NM 1996 8 8 DHL96721105 1 19960604 A 5712 6516209159 RIB BOEING 727 727228 NM LT WING LE CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND LEFT WING L/E SKIN SUPPORT RIB CRACKED ON INBD SIDE OF NR 3 LEADING EDGE FLAP WELL ON INBD SIDE, APPRO X 18. REMOVED SUPPORT RIB AND INSTALLED NWE RIB PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996080800552 19960808 00552 NM 1996 8 8 DHL96721106 1 19960609 A 5730 SKIN BOEING 727 727228 NM LT WING DELAMINATED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, LEFT WING UPPER SURFACE PANEL ABOVE OUTBD AILERON OUTBD BALANCE BAY, FWD LEADING EDGE SKIN DELAMINATED. INS TALLED BONDING REPAIR PER SRM 51-40-6, 34 BY 18. 2 L 7 3 4F A3WE 1996080800553 19960808 00553 NM 1996 8 8 DHL96721107 1 19960604 A 5730 PANEL BOEING 727 727228 NM LT WING DELAMINATED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, LEFT WING UPPER SURFACE PANEL 8147, HAS DELAMINATION AND SURFACE CORROSION. INSTALLED BONDING REPAIR PER SR M 51-40-5 AND 51-40-6, 40 BY 20 AND INSTALLED PANEL PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996080800554 19960808 00554 NM 1996 8 8 DHL96721108 1 19960605 A 5730 SKIN BOEING 727 727228 NM WING CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, TOP COVE PANEL FWD OF NR 9 SPOILER CENTER SKIN IS CRACKED AND BROKEN. STOP DRILLED CRACK, INSTALLED DOUBLER REPAIR PER SRM 51-40-2, 3 BY 4 PER SRM 51-40-2. 2 L 7 3 4F A3WE 1996080800555 19960808 00555 NM 1996 8 8 DHL9672110C 1 19960610 A 5347 BAC1520792 SEAT TRACK BOEING 727 727228 NM BS 600 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND NR 5 SEAT TRACK RBL 25 AT STA 600 CENTER CRACKED BETWEEN ATTACH FASTENERS. REMOVED AND REPLACED SEAT TRACK FROM STA 550 TO 690 PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996080800556 19960808 00556 NM 1996 8 8 DHL96721111 1 19960606 A 5712 65C3320224 RIB BOEING 727 727228 NM RT WING CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, RIGHT WING UPPER RIB 70.5 HAS CRACKS AT TWO UPPER FWD AND LOWER FWD HOLES. REMOVED OUTBD ANGLE AND STRAP AN D INBD T-CLIP AND STRAP. HFEC INSPECTED UPPER RIB FASTENER HOLES PER S/B 57-0112 AND INSTALLED REPAIR PER S/B 57-0112, SEALED TANK AND LEAK CHECK PER SRM 51-20-4. 2 L 7 3 4F A3WE 1996080800557 19960808 00557 NM 1996 8 8 DHL96721113 1 19960608 A 5315 FLOORBEAM BOEING 727 727228 NM BS 950 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, CABIN FLOORBEAM CAP AT BS 950 LBL 5 TO LBL 23 HAS SEVERE CORROSION. REMOVED AND REPLACED FLOORBEAM 10 FT BY 7 PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996080800558 19960808 00558 NM 1996 8 8 DHL96721115 1 19960603 A 5320 ANGLE BOEING 727 727228 NM BS 950 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, CORROSION FOUND UNDER FS 950 CASTING SPLICE PLATE ON LEFT W/W AFT WALL 16 BELOW SIDE STRUT AFT BEARING HOUSI NG. REMOVED CORRODED SPLICE ANGLE, CUT OUT CORRODED WEB, INSTALLED WEB REPAIR PER SRM 51-40-2, 9 BY 3.5. REPLACED SPLI CE PLATE ANGLE, INSTALLED ANGLE REPAIR PER SRM 51-40-2, 2 BY 2 BY 11. 2 L 7 3 4F A3WE 1996080800559 19960808 00559 NM 1996 8 8 DHL96721116 1 19960531 A 5530 FORGING BOEING 727 727228 NM VERT STAB CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 VERTICAL FIN FRONT SPAR FORGING HAS INTERIM REPAIR PER AVITAS EO 96PMS I114RO-1. REMOVED INTERM REPAIR PER SRM 51-30-2 , INSTALLED VERTICAL FIN FRONT SPAR FORGING PER AVITALS ENGINEERING DRAWING 96PMSI124D-1. 2 L 7 3 4F A3WE 1996080800560 19960808 00560 NM 1996 8 8 DHL96721117 1 19960607 A 5530 FORGING BOEING 727 727228 NM VERT STAB CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND VERTICAL FIN FRONT SPAR FORGING RT SIDE LOWER HORIZONTAL CHORD HAS CRACK FROM RBL 1.5 TO 4.5. LOWER V ERTICAL WEB CRACKED FROM RBL 1.25 TO 5.75. STOP DRILLED HOLES AND INSTALLED FIN FRONT SPAR FORGING AND WEB REPAIR PER A VITAS ENGINEERING DRAWING 96PMSI124D-1. 2 L 7 3 4F A3WE 1996080800561 19960808 00561 NM 1996 8 8 DHL96721118 1 19960607 A 5530 FORGING BOEING 727 727228 NM VERT STAB CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND VERTICAL FIN FRONT SPAR FORGING LT SIDE LOWER HORIZONTAL CHORD HAS CRACK FROM LBL .5 TO LBL 1.5. STOP DRILLED CRACK, INSTALLED CHORD REPAIR PER AVITAS ENGINEERING DRAWING 96PMSI124R-1. 2 L 7 3 4F A3WE 1996080800562 19960808 00562 NM 1996 8 8 DHL96721119 1 19960605 A 5415 FITTING BOEING 727 727228 NM NR 1 ENGINE CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, NR 1 ENG MOUNT SUPPORT FITTING CRACKED AT LOWER I/B CORNER. REMOVED CRACKED MEMBER ON NR 1 ENGINE AFT MOUNT PER BOEING INSTRUCTIONS 32-9430. 2 L 7 3 4F A3WE 1996080800563 19960808 00563 NM 1996 8 8 DHL9672111C 1 19960611 A 5313 BAC149814C STRINGER BOEING 727 727228 NM BS 680 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND STRINGER 9 RIGHT IS CRACKED AT BS 680. CUT OUT DAMAGED SECTION OF STRINGER AND INSTALLED REPAIR PER SRM 53-10-3, REPAIR 12 INCHES. 2 L 7 3 4F A3WE 1996080800564 19960808 00564 NM 1996 8 8 DHL9672112 1 19960609 A 5315 BAC1505100617 FLOORBEAM BOEING 727 727228 NM BS 950 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND FLOORBEAM AT STA 950 HAS CORROSION ON UPPER SURFACE BL 0 TO RBL 24. REMOVED AND REPLACED BEAM PER SRM 51-10-1, 10 FT BY 17. 2 L 7 3 4F A3WE 1996080800565 19960808 00565 NM 1996 8 8 DHL96721120 1 19960605 A 5754 ANGLE BOEING 727 727228 NM NR 7 LE SLAT CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, NR 7 SLAT ACTUATOR OUTBD TRUNNION ATTACH ANGLE ON FWD SPAR IS CRACKED. FABRICATED NR 7 SLAT ACTUATOR O/B A TTACH ANGLE AND DOUBLER PER S/B 50-0130. INSTALLED ACTUATOR, DOUBLER AND ATTACH ANGLE PER S/B 57-0130. 2 L 7 3 4F A3WE 1996080800566 19960808 00566 NM 1996 8 8 DHL9672112C 1 19960612 A 5313 BAC1498144 STRINGER BOEING 727 727228 NM BS 404 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND STRINGER 18 R AT STA 404 CORRODED AND CRACKED. CUT OUT DAMAGED AREA AND INSTALLED SPLICE 12 LONG PER SRM AND STRINGER 13 LONG. 2 L 7 3 4F A3WE 1996080800567 19960808 00567 NM 1996 8 8 DHL9672113C 1 19960612 A 5311 FRAME BOEING 727 727228 NM BS 304 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND FWD FACE OF FRAME AT STA 304 CORRODED. REMOVED FASTENERS AT FRAME AND REMOVED CORROSION. FABRICATED AND INSTALLED DOUBLER PER SRM 51-40-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996080800568 19960808 00568 NM 1996 8 8 DHL9672114C 1 19960613 A 5315 FLOORBEAM BOEING 727 727228 NM BS 312 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND CABIN FLOORBEAM AT BS 312 LBL 30 CORRODED AT FLOORBEAM ATTACH POINTS. CUT OUT DAMAGED AREAS AND INSTA LLED ANGLE REPAIR 5 BY 7 PER SRM 53-10-8. 2 L 7 3 4F A3WE 1996080800569 19960808 00569 NM 1996 8 8 DHL9672115C 1 19960615 A 5315 FLOORBEAM BOEING 727 727228 NM BS 312 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND CABIN FLOORBEAM BS 312 LBL 4 CORRODED. CUT OUT DAMAGED AREA AND INSTALLED REPAIR 9.75 BY 1.5 BY 1.5 PER SRM 51-40-4. 2 L 7 3 4F A3WE 1996080800570 19960808 00570 NM 1996 8 8 DHL9672116C 1 19960606 A 5712 RIB BOEING 727 727228 NM WS 629 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND LOWER CHORD CRACKED AT RIB AT WS 629 AT STR. INSTALLED REPAIR PER SRM 57-10-5, 12.5 BY 3. 2 L 7 3 4F A3WE 1996080800571 19960808 00571 NM 1996 8 8 DHL9672117C 1 19960603 A 5320 PRESSURE DECK BOEING 727 727228 NM BS 280 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND NOSE W/W PRESSURE DECK CRACKED AT STA 280. FABRICATED AND INSTALLED DOUBLER 19 BY 10 PER SRM 51-40- 2. 2 L 7 3 4F A3WE 1996080800572 19960808 00572 NM 1996 8 8 DHL9672118C 1 19960609 A 5347 BAC15201466 SEAT TRACK BOEING 727 727228 NM BS 680-720 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND CORROSION ON SEAT TRACK FLANGE BS 680 TO 720A. REMOVED AND REPLACED FLOOR TRACK PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996080800573 19960808 00573 NM 1996 8 8 DHL9672119C 1 19960609 A 5320 BAC1518359 SUPPORT BOEING 727 727228 NM BS 360-400 CORROSION A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND CORRODED FLOOR SUPPORT BEAM, BS 360 TO 400 LBL 24. FABRICATED AND INSTALLED CABIN FLOOR SUPPORT PER SRM 51-10-1, REPAIR 20 LONG. 2 L 7 3 4F A3WE 1996080800574 19960808 00574 NM 1996 8 8 DHL9672120C 1 19960609 A 5311 FRAME BOEING 727 727228 NM BS 227.8 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND CORROSION ON FRAME AT STA 227.8 BELOW COCKPIT WINDOW RIGHT SIDE. REMOVED WEB MATERIAL AND INSTALLED FILLER 5 BY 2 AND DOUBLER 5 BY 12 PER SRM 51-40-2. 2 L 7 3 4F A3WE 1996080800575 19960808 00575 NM 1996 8 8 DHL9672121C 1 19960608 A 5313 BAC1498138 STRINGER BOEING 727 727228 NM BS 420 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND STRINGER 4L CRACKED AT STA 420. CUT OUT DAMAGED AREA, INSTALLED REPAIR PER SRM 53-10-3, 20 LONG. 2 L 7 3 4F A3WE 1996080800576 19960808 00576 NM 1996 8 8 DHL9672122C 1 19960608 A 5320 CIRCUMFERENTIAL BOEING 727 727228 NM BS 520 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND CIRCUMFERENTIAL CRACKED AT I/B FLANGE 6 INCHES ABOVE FLOOR AT STA 520 RIGHT SIDE. STOP DRILLED CRACK, FABRICATED DOUBLERS AND INSTALLED PER SRM 53-10-4, DOUBLERS 15 BY 5.5. 2 L 7 3 4F A3WE 1996080800577 19960808 00577 NM 1996 8 8 DHL9672123C 1 19960608 A 5340 BAC15201466 SEAT TRACK BOEING 727 727228 NM BS 857-863 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND CABIN SEAT FLANGE FROM BS 857 TO BS 863 LBL 45 CORRODED. REMOVED AND REPLACED SEAT TRACK PER SRM 51-1 0-1, 20 LONG. 2 L 7 3 4F A3WE 1996080800578 19960808 00578 NM 1996 8 8 DHL9672124C 1 19960606 A 5312 BULKHEAD ANGLE BOEING 727 727228 NM BS 1166 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND AFT BAGGAGE COMP BULKHEAD PANEL SUPPORT ANGLE CORRODED STA 1166 LBL 23 TO RBL 65. REMOVED CORROSION, INSTALLED ANGLE 2 BY 2 BY 130 PER SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996080800579 19960808 00579 NM 1996 8 8 DHL9672125C 1 19960611 A 5313 BAC14981476 STRINGER BOEING 727 727228 NM BS 837 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND CORROSION ON STR 16L STA 837 BELOW EMERGENCY EXIT CUTOUT. REMOVED AND INSTALLED NEW STRINGER FROM BS 830 TO 850 PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996080800580 19960808 00580 NM 1996 8 8 DHL9672126C 1 19960605 A 5320 608128 ANGLE BOEING 727 727228 NM BS 1110 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND CORROSION ON SKIN TIE ANGLE AT STA 110 AT FLOOR LEVEL STRINGER 17L. REMOVED TIE ANGLE, FABRICATED NEW TIE ANGLE 6 LONG AND INSTALLED PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996080800581 19960808 00581 NM 1996 8 8 DHL9672127C 1 19960605 A 5320 BRACKET BOEING 727 727228 NM BS 950 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND STRINGER 4 LEFT TIE BRACKET CRACKED AT STA 950A. REMOVED AND INSTALLED NEW TIE BRACKET PER SRM 51-10 -1, 2 BY 2 BY 1 BY 3. 2 L 7 3 4F A3WE 1996080800582 19960808 00582 NM 1996 8 8 DHL9672128C 1 19960605 A 5320 INTERCOSTAL BOEING 727 727228 NM BS 950 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, AFT BAGGAGE COMPARTMENT INTERCOSTAL IS CRACKED AT STA 950A AND STR 24R. FABRICATED NEW INTERCOSTAL 24 BY 4. 5 AND INSTALLED PER SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996080800583 19960808 00583 NM 1996 8 8 DHL9672129C 1 19960605 A 5320 INTERCOSTAL BOEING 727 727228 NM BS 950 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND INTERCOSTAL CRACKED AT STA 950D TO 950E AT STR 25 TO 26 RIGHT. INSTALLED ANGLE 8 BY .5 PER SRM 51-40 -3, FILLER 1. 2 L 7 3 4F A3WE 1996080800584 19960808 00584 NM 1996 8 8 DHL9672130C 1 19960605 A 5320 WEB BOEING 727 727228 NM BS 1148 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND AFT BAG COMP CRACK IN WEB AT STA 1148 AND STR 25 RT. REMOVED MATERIAL, FABRICATED NEW INTERCOSTAL 13. 5 BY 7.75 FT AND INSTALLED PER SRM 51-40-2. 2 L 7 3 4F A3WE 1996080800585 19960808 00585 NM 1996 8 8 DHL9672131C 1 19960605 A 5311 FRAME BOEING 727 727228 NM BS 970 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FRAME CRACKED IN AFT BAGGAGE COMP AT STA 970 STR 26 LT. STOP DRILLED CRACK, FABRICATED FRAME REPAIR 1 BY 4 BY 15, FILLER 1 BY 1 BY 15 PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996080800586 19960808 00586 NM 1996 8 8 DHL9672132C 1 19960605 A 5320 INTERTCOSTAL BOEING 727 727228 NM BS 950 BENT A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND INTERCOSTAL BENT AT STA 950A TO 950B STR 25 LT. REMOVED AND REPLACED INTERCOSTAL 20 BY 3.5 FT BY 1 F T PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996080800587 19960808 00587 NM 1996 8 8 DHL9672133C 1 19960605 A 5320 INTERCOSTAL BOEING 727 727228 NM BS 950 BENT A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND INTERCOSTAL BENT AT STA 950A TO 950B AT STR 23 LT. FABRICATED NEW INTERCOSTAL PER SRM 51-30-2, 24 BY 4.4 AND INSTALLED PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996080800588 19960808 00588 NM 1996 8 8 DHL9672134C 1 19960609 A 5347 BAC1520792 SEAT TRACK BOEING 727 727228 NM BS 1000 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND CORROSION ON UPPER SURFACE OF SEAT TRACK FLANGE STA 1000 BL 58L. FABRICATED AND INSTALLED NEW SEAT TR ACK 40 LONG PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996080800589 19960808 00589 NM 1996 8 8 DHL9672135C 1 19960609 A 5320 BAC1518359 SUPPORT BOEING 727 727228 NM BS 996 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND FLOOR SUPPORT HAS CORROSION ON UPPER SURFACE AT STA 996 BL 50 LT. FABRICATED NEW SUPPORT 8.5 LONG PE R SRM 51-1-1. 2 L 7 3 4F A3WE 1996080800590 19960808 00590 NM 1996 8 8 DHL9672136C 1 19960617 A 5347 SEAT TRACK BOEING 727 727228 NM BS 720 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND SEAT TRACK CORRODED AT BS 720B TO 720C AT RBL 48. REPLACED SEAT TRACK PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996080800591 19960808 00591 NM 1996 8 8 DHL9672137C 1 19960609 A 5347 SEAT TRACK BOEING 727 727228 NM BS 340-380 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND CORROSION ON SEAT TRACK FLANGE BS 340 TO 380 LBL 45. FABRICATED AND INSTALLED NEW SEAT TRACK PER SRM 51-10-1, 40 LONG. 2 L 7 3 4F A3WE 1996080800592 19960808 00592 NM 1996 8 8 DHL9672138C 1 19960609 A 5347 BAC1520792 SEAT TRACK BOEING 727 727228 NM BS 680 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND CORROSION AROUND HOLES IN SEAT TRACK BS 680 OUTBD RIGHT TRACK. REMOVED AND REPLACED SEAT TRACK BS 48 0 TO 700 PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996080800593 19960808 00593 NM 1996 8 8 DHL9672139C 1 19960609 A 5315 FLOORBEAM BOEING 727 727228 NM BS 480 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND CORROSION TOP OF FLOORBEAM AT BS 480 RBL 0 TO RBL 24. CUT OUT DAMAGED AREA RBL 0 TO 24 AND INSTALLED REPAIR PER SRM 53-10-8. 2 L 7 3 4F A3WE 1996080800594 19960808 00594 NM 1996 8 8 DHL9672140C 1 19960609 A 5320 603338 SPLICE BOEING 727 727228 NM BS 680 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 195454 AT C-CHECK, FOUND CORROSION AT SEAT TRACK SPLICE BS 680 TO 700. REMOVED AND REPLACED SPLICES PER SRM 53-10-5, SPLICES 1 3, STRAP 6 BY 3. 2 L 7 3 4F A3WE 1996080800595 19960808 00595 NM 1996 8 8 DHL9672141C 1 19960609 A 5347 BAC1520792 SEAT TRACK BOEING 727 727228 NM BS 680 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND CORROSION ON SEAT TRACK BS 680 TO 700 RBL 24. REMOVED SEAT TRACK FROM STA 550 TO 690, REMOVED CORROSI ON FROM SEAT TRACK 690 TO 700, WITHIN LIMITS. REPLACED TRACK FROM 550 TO 690 PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996080800596 19960808 00596 NM 1996 8 8 DHL9672142C 1 19960609 A 5315 FLOORBEAM BOEING 727 727228 NM BS 460 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND CORROSION ON TOP OF FLOORBEAM BS 460 RBL 45 TO RBL 63. REMOVED CABIN FLOORBEAM AND REPLACED REPAIR 2 0 BY 3 PER SRM 53-10-8. 2 L 7 3 4F A3WE 1996080800597 19960808 00597 NM 1996 8 8 DHL9672143C 1 19960609 A 5320 STRAP BOEING 727 727228 NM BS 700 CORROSION A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND CORROSION FLOORBEAM STRAP RBL 24 AT STA 700. CUT OUT CORROSION FROM 690 TO 710, FABRICATED NEW STRAP 48 BY 3, PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996080800598 19960808 00598 NM 1996 8 8 DHL9672144C 1 19960609 A 5320 603338 SPLICE BOEING 727 727228 NM BS 680 CORROSION A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND CORROSION ON SEAT TRACK SPLICE BS 680 TO 700 RBL 24. REPLACED SPLICE PER SRM 51-10-1, 12 LONG. 2 L 7 3 4F A3WE 1996080800599 19960808 00599 NM 1996 8 8 DHL9672146C 1 19960609 A 5315 FLOORBEAM BOEING 727 727228 NM BS 480 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND CORROSION BS 480 BL TO RBL 24 FLOORBEAM TOP. REMOVED DAMAGED AREA AND REPLACED PER SRM 53-10-8, BL 0 TO RBL 24. 2 L 7 3 4F A3WE 1996080800600 19960808 00600 NM 1996 8 8 DHL9672147C 1 19960609 A 5347 BAC1520792 SEAT TRACK BOEING 727 727228 NM BS 340-380 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND CORROSION ON SEAT TRACK FLANGE BS 340 TO 380 LBL 59. FABRICATED AND INSTALLED NEW SEAT TRACK 116 PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996080800601 19960808 00601 NM 1996 8 8 DHL9672148C 1 19960609 A 5320 SPLICE BOEING 727 727228 NM BS 680-700 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND CORROSION ON SEAT TRACK SPLICE BS 680 TO 700 RBL 45. REMOVED AND REPLACED SPLICE PER SRM 53-10-5, 2 P IECES 12 AND 15.5. 2 L 7 3 4F A3WE 1996080800602 19960808 00602 NM 1996 8 8 DHL9672149C 1 19960609 A 5320 603338 SPLICE BOEING 727 727228 NM BS 680-700 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND CORROSION BS 680 TO 700 LBL 24 AT SEAT TRACK SPLICE. REMOVED AND REPLACED SPLICE 13 LONG AND STRAP 6 BY 3 PER SRM 53-10-5. 2 L 7 3 4F A3WE 1996080800603 19960808 00603 NM 1996 8 8 DHL9672150C 1 19960610 A 5347 BAC1520792 SEAT TRACK BOEING 727 727228 NM BS 480-700 WORN A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND NR 6 SEAT TRACK WORN FROM BS 480 TO 700 RBL 45. REMOVED AND REPLACED TRACK PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996080800604 19960808 00604 NM 1996 8 8 DHL9672151C 1 19960609 A 5347 15201466 SEAT TRACK BOEING 727 727228 NM BS 720 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND CORROSION AT BS 720A O/B SEAT TRACK ON TOP FLANGE AROUND FASTENER HOLES. REPLACED SEAT TRACK PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996080800605 19960808 00605 NM 1996 8 8 DHL9672152C 1 19960613 A 5315 BAC1505100617 FLOORBEAM BOEING 727 727228 NM BS 344 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND CABIN FLOORBEAM CAP CORRODED ALONG TOP SURFACE AND AT NUT CLIP LOCATION BS 344 LBL 60 TO RBL 14. REPL ACED CAP PER SRM 51-40-4. 2 L 7 3 4F A3WE 1996080800606 19960808 00606 NM 1996 8 8 DHL9672153C 1 19960605 A 5311 FRAME BOEING 727 727228 NM BS 970 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND FRAME CRACKED IN AFT BAG COMPT AT STA 970 STR 26L. STOP DRILLED CRACK AND FABRICATED FRAME REPAIR DOU BLER 1 BY 4 BY 15, FILLER 1 BY 1 BY 15 PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996080800607 19960808 00607 NM 1996 8 8 DHL9672154C 1 19960610 A 5347 BAC1520792 SEAT TRACK BOEING 727 727228 NM BS 540 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, NR 6 SEAT TRACK CRACKED FROM RBL 45 AT STA 540 TO 542. REMOVED AND REPLACED SEAT TRACK BS 480 TO 700 PER SR M 51-30-2. 2 L 7 3 4F A3WE 1996080800608 19960808 00608 NM 1996 8 8 DHL9672155C 1 19960610 A 5347 BAC1520792 SEAT TRACK BOEING 727 727228 NM BS 602 WORN A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, NR 5 SEAT TRACK RBL 25 LOCKING HOLES ELONGATED AT STA 602. REMOVED AND REPLACED SEAT TRACK BS 550 TO BS 69 0 PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996080800609 19960808 00609 NM 1996 8 8 DHL9672156C 1 19960610 A 5347 BAC1520792 SEAT TRACK BOEING 727 727228 NM BS 480-590 WORN A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, NR 3 SEAT TRACK LBL 25 LOCKING HOLES ELONGATED. REMOVED AND REPLACED TRACK BS 480 TO 590 AND INSTALLED SPLI CE BETWEEN 480 TO 600 AT LBL 25, 11 LONG. INSTALLED STRAP 9 BY 3 PER SRM 53-10-5. 2 L 7 3 4F A3WE 1996080800610 19960808 00610 NM 1996 8 8 DHL9672157C 1 19960610 A 5347 BAC1520792 SEAT TRACK BOEING 727 727228 NM BS 720 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, NR 5 SEAT TRACK RBL 25 AT STA 720C CRACKED AT CENTER BETWEEN ATTACHING FASTENERS. REPLACED TRACK PER SRM 5 1-10-1. 2 L 7 3 4F A3WE 1996080800611 19960808 00611 NM 1996 8 8 DHL9672158C 1 19960605 A 5320 BRACKET BOEING 727 727228 NM BS 1010 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND S-4R TIE BRACKET CRACKED STA 1010. REMOVED AND REPLACED BRACKET PER SRM 51-10-1, 2.5 BY 1 BY 2.5 BY 3 . 2 L 7 3 4F A3WE 1996080800612 19960808 00612 NM 1996 8 8 DHL9672159C 1 19960605 A 5320 BRACKET BOEING 727 727228 NM BS 950 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, S-15R TIE BRACKET CRACKED AT STA 950A. REMOVED AND REPLACED BRACKET 2 BY 2 BY 1 BY 4 PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996080800613 19960808 00613 NM 1996 8 8 DHL9672161C 1 19960609 A 5315 FLOORBEAM BOEING 727 727228 NM BS 1070 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FLOORBEAM STA 1070 BL 30R TO 65R HAS MANY AREAS OF CORROSION. INSTALLED CABIN FLOORBEAM REPAIR AT STA 1070, 26 BY 3, PER SRM 53-10-8 AND 53-30-2. 2 L 7 3 4F A3WE 1996080800614 19960808 00614 NM 1996 8 8 DHL9672162C 1 19960610 A 5330 SKIN BOEING 727 727228 NM BS 600 DENTED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, SKIN DENTED AT STA 600 STR 19L. INSTALLED EXTERNAL DOUBLER PER SRM 53-10-3, 12 BY 7. 2 L 7 3 4F A3WE 1996080800615 19960808 00615 NM 1996 8 8 DHL9672163C 1 19960612 A 5741 BOTTLE PIN BOEING 727 727228 NM LT WING CORROSION A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, LEFT HAND BOTTLE PIN HAS CORROSION AND WEAR MARKS IN SIDE WALL. REMOVED DAMAGE PER S/B 57-0175, FABRICATED REPAIR SLEEVES PER SRM 57-10-7, INSTALLED SLEEVES BUSHINGS AND BOTTLE PIN PER SRM 57-10-7 AND MM 57-41-1. 2 L 7 3 4F A3WE 1996080800616 19960808 00616 NM 1996 8 8 DHL9672164C 1 19960606 A 5511 RIB BOEING 727 727228 NM LT HORIZ STAB PUNCTURED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, LT HORIZONTAL STAB HAS RIB WITH PUNCTURE AT STA 14. INSTALLED RIB REPAIR PER SRM 55-10-4, 13 BY 11. 2 L 7 3 4F A3WE 1996080800617 19960808 00617 NM 1996 8 8 DHL9672165C 1 19960607 A 5531 SPAR WEB BOEING 727 727228 NM VERT STAB GOUGED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, VERTICAL STAB HAS GOUGES ON FWD SPAR WEB RT TENSION TIE BEAM. INSTALLED WEB REPAIR PER SRM 51-40-2, 4 BY 3. 2 L 7 3 4F A3WE 1996080800618 19960808 00618 NM 1996 8 8 DHL9672166C 1 19960609 A 5542 SKIN BOEING 727 727228 NM RUDDER WORN A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND UPPER RUDDER LEADING EDGE SKIN HAS WEAR AT TOP RT SIDE. INSTALLED DOUBLER REPAIR PER SRM 55-40-3, 10 BY 14. 2 L 7 3 4F A3WE 1996080800619 19960808 00619 NM 1996 8 8 DHL9672167C 1 19960609 A 5542 SKIN BOEING 727 727228 NM RUDDER WORN A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND UPPER RUDDER LEADING EDGE SKIN WORN AT LT LOWER SIDE. INSTALLED DOUBLER REPAIR PER SRM 55-40-3, 10 BY 10. 2 L 7 3 4F A3WE 1996080800620 19960808 00620 NM 1996 8 8 DHL9672168C 1 19960609 A 5542 SKIN BOEING 727 727228 NM RUDDER WORN A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, LOWER RUDDER LEADING EDGE SKIN IS WORN THROUGH AT RT BOTTOM. INSTALLED DOUBLER REPAIR PER SRM 55-40-3, 21 B Y 13.5. 2 L 7 3 4F A3WE 1996080800621 19960808 00621 NM 1996 8 8 DHL9672169C 1 19960614 A 5522 SKIN BOEING 727 727228 NM RT ELEVATOR CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, RT ELEVATOR SKIN BULGING AND CORRODED AT ELEVATOR TRAILING EDGE STA 173.21 AND 190. INSTALLED FILLER AND DO UBLER REPAIR 15 PER SRM 55-3-3, CALCULATED NEW BALANCE MOMENT AND CHANGED DATA PLATE PER SRM 51-80-7. NO ADDITIONAL WE IGHT REQD. 2 L 7 3 4F A3WE 1996080800622 19960808 00622 NM 1996 8 8 DHL9672170C 1 19960605 A 5312 BULKHEAD WEB BOEING 727 727228 NM BS 1183 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, PRESSURE WEB AT 1183 BULKHEAD CRACKED AT FWD SIDE FLOOR LEVEL RBL 49. INSTALLED DOUBLER REPAIR PER SRM 51-4 0-2, 3 BY 2 AND INSTALLED NEW WEB AT RBL 49 PER SRM 51-40-2, 12.75 BY 6. 2 L 7 3 4F A3WE 1996080800623 19960808 00623 NM 1996 8 8 DHL9672171C 1 19960606 A 5315 FLOORBEAM BOEING 727 727228 NM BS 1070 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 10545 AT C-CHECK, MAIN FLOORBEAM HAS CORROSION AT STA 1070 LBL 50 ON UPPER AFT FLANGE IN BAGGAGE COMP. CUT OUT FLANGE APPROX 24, INSTALLED REPAIR AT STA 1070 UPPER CAP FROM LBL 24 TO LBL 50 PER SRM 53-10-8, SIZE 26 BY 3. 2 L 7 3 4F A3WE 1996080800624 19960808 00624 NM 1996 8 8 DHL9672172C 1 19960608 A 5320 BRACKET BOEING 727 727228 NM BS 680 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, TIE BRACKET CRACKED AFT SIDE OF BS 680. INSTALLED NEW TIE BRACKET AT STR 9, 1.5 BY 1.5 BY 2 PER SRM 51-10-1 . 2 L 7 3 4F A3WE 1996080800625 19960808 00625 NM 1996 8 8 DHL9672173C 1 19960608 A 5241 DOOR BOEING 727 727228 NM GALLEY CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND CORROSION AT AFT UPPER CORNER OF RT GALLEY DOOR CORNER BRACKET AND FRAME. REMOVED CORROSION PER SRM 5 1-10-6 AND INSTALLED NEW BRACKET 4 BY 3. 2 L 7 3 4F A3WE 1996080800626 19960808 00626 NM 1996 8 8 DHL9672174C 1 19960608 A 5320 BRACKET BOEING 727 727228 NM BS 480 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, S-7 L TIE BRACKET CRACKED AT STA 480. INSTALLED NEW BRACKET PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996080800627 19960808 00627 NM 1996 8 8 DHL9672175C 1 19960603 A 5320 ANGLE BOEING 727 727228 NM BS 900 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, ATTACH ANGLE CRACKED AT BS 900 LBL 65 OUTBD SIDE OF PRESSURE DECK, 12 BELOW PRESS DECK. REPLACED ATTACH AN GLE 4 BY 6 PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996080800628 19960808 00628 NM 1996 8 8 DHL9672176C 1 19960609 A 5315 FLOORBEAM BOEING 727 727228 NM BS 720 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND CORROSION ON FLOORBEAM STA 720D LBL 60. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED FLOORBEAM UPPE R CAP PER SRM 53-10-8, 12 LONG. 2 L 7 3 4F A3WE 1996080800629 19960808 00629 NM 1996 8 8 DHL9672177C 1 19960605 A 5320 BRACKET BOEING 727 727228 NM BS 950 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND S-3L TIE BRACKET CRACKED AT STA 950D. REMOVED AND REPLACED TIE BRACKET PER SRM 51-10-1, 1.5 BY 1 FT B Y 1.5. 2 L 7 3 4F A3WE 1996080800630 19960808 00630 NM 1996 8 8 DHL9672178C 1 19960608 A 5320 BRACKET BOEING 727 727228 NM BS 660 TORN A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, S-9L TIE BRACKET TORN AT STA 660. REMOVED AND REPLACED TIE BRACKET PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996080800631 19960808 00631 NM 1996 8 8 DHL9672179C 1 19960608 A 5320 BRACKET BOEING 727 727228 NM BS 700 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, STRINGER 6L, 7L, 8L AND 9L TIE BRACKETS CUTOUT AT UPPER ENDS CHECK FOR LIMITS STA 700. REMOVED TIE BRACKETS , INSTALLED NEW TIE BRACKETS 2 BY 1.5 BY 2 FT BY 3 PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996080800632 19960808 00632 NM 1996 8 8 DHL9672180C 1 19960608 A 5320 BRACKET BOEING 727 727228 NM BS 700 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, S-3L TIE BRACKET UPPER SECTION CUTOUT STA 700 CHECK CUTOUT LIMITS. REMOVED AND REPLACED TIE BRACKET PER SRM 51-30-2, 2 BY 1.5 BY 2 BY 3. 2 L 7 3 4F A3WE 1996080800633 19960808 00633 NM 1996 8 8 DHL9672181C 1 19960608 A 5320 BRACKET BOEING 727 727228 NM BS 700 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND S-5L TIE BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER SRM 51-10-1, 2 BY 1.5 BY 2 BY 3. 2 L 7 3 4F A3WE 1996080800634 19960808 00634 NM 1996 8 8 DHL9672182C 1 19960604 A 5320 FITTING BOEING 727 727228 NM BS 740 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, FOUND CORROSION S-8L END FITTING AT 740. REMOVED CORROSION, FOUND CRACKED END FITTING. REPLACED FITTING PE R SRM 51-10-1. 2 L 7 3 4F A3WE 1996080800635 19960808 00635 NM 1996 8 8 DHL9672183C 1 19960605 A 5754 SKIN BOEING 727 727228 NM NR 6 LE SLAT DENTED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, NR 6 SLAT EXTERIOR SKIN AT L/E HAS DENT. CUT OUT DENT AREA, FABRICATED DOUBLER 8 BY 4 AND FILLER 1 BY 4 AN D INSTALLED PER SRM 57-30-3. 2 L 7 3 4F A3WE 1996080800636 19960808 00636 NM 1996 8 8 DHL9672184C 1 19960607 A 5741 FITTING BOEING 727 727228 NM RT WING CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, RT WING FWD BOTTLE PIN HOLE END FITTING CORRODED. REAMED DAMAGED TERMINAL FITTING, FABRICATED BUSHING SLEEV E PER DRAWING 65C36176, INSTALLED SLEEVE AND INSTALLED BOTTLE PIN AND BUSHING PER MM 57-41-1 AND 57-41-11. 2 L 7 3 4F A3WE 1996080800637 19960808 00637 NM 1996 8 8 DHL9672186C 1 19960603 A 5312 BULKHEAD BOEING 727 727228 NM BS 178 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, BS 178 BULKHEAD WEB CRACKED AT RIVET WL 196 BL 2 RT. STOP DRILLED CRACKS, INSTALLED WEB REPAIR 5 BY 5 PER S RM 51-40-2. 2 L 7 3 4F A3WE 1996080800638 19960808 00638 NM 1996 8 8 DHL9672188C 1 19960605 A 5311 FRAME BOEING 727 727228 NM BS 783.95 CRACKED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, BS 783.95 RT SIDE FRAME CRACKED VERTICALLY FWD FLANGE FROM BOTTOM OF FRAME UP TO SECOND FASTENER HOLE INBD R OW. VERIFIED CRACKS AT FASTENER HOLES, INSTALLED FRAME REPAIR PER S/B 53-0197 AND DRAWING 65C36280. 2 L 7 3 4F A3WE 1996080800639 19960808 00639 NM 1996 8 8 DHL9672189 1 19960609 A 5347 BAC15198342 SEAT TRACK BOEING 727 727228 NM BS 1110 CORROSION A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, SEAT TRACK CORRODED IN SEVERAL PLACES AT LBL 46 AT BS 1110 AND 1130. REMOVED SEAT TRACK AND INSTALLED NEW T RACK PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996080800640 19960808 00640 NM 1996 8 8 DHL9672191C 1 19960606 A 5347 SEAT TRACK BOEING 727 727228 NM BS 1110 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DK 19545 AT C-CHECK, AFT CABIN FLOOR SEAT TRACK HEAVILY CORRODED AT LBL 25, BETWEEN BS 1110 AND 1130. REMOVED AND REPLACED SEAT TRACK 26 LONG PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996080800641 19960808 00641 NM 1996 8 8 DHL9672192C 1 19960606 A 5315 FLOORBEAM BOEING 727 727228 NM BS 1130-1148 CORRODED A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, CORROSION ON AFT CABIN FLOOR SUPPORT UPPER SIDE BETWEEN BS 1130 AND 1148. CUT OUT DAMAGED AREA 3 BY 1, FABR ICATED AND INSTALLED ANGLE REPAIR 6.5 BY 2 BY 2 PER SRM 51-40-4. 2 L 7 3 4F A3WE 1996080800642 19960808 00642 NM 1996 8 8 DHL9672199C 1 19960610 A 5347 BAC152792 SEAT TRACK BOEING 727 727228 NM BS 950 WORN A T DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT C-CHECK, NR 6 SEAT TRACK AT STA 950D RBL 45 WORN. REPLACED SEAT TRACK PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996080800643 19960808 00643 WP 1996 8 8 MWEA96303 1 19960731 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 465 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, FOUND INTERCOSTAL CRACKED FOR CABIN FLOOR CENTER SUPPORT STA 465. INSTALLED DOUBLER REPAIR IAW SRM 53-0 1. 2 L 7 2 4F A6WE 1996080800644 19960808 00644 WP 1996 8 8 MWEA96304 1 19960731 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 917-937 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, FOUND TEMPORARY REPAIR INSTALLED ON SKIN AT STA 917 TO 937 AND LONGERON 25L. INSTALLED PERMANENT FLUSH REPAIR IAW SRM 53-04, FIG 12B. 2 L 7 2 4F A6WE 1996080800645 19960808 00645 WP 1996 8 8 MWEA96305 1 19960731 A 5320 4912772 ANGLE DOUG DC9 DC932 3022066 WP BS 230 EXFOLIATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, A CABIN CUSP ANGLE FITTING WAS FOUND EXFOLIATED AT THE LT SIDE FUS STA 230. INSTALLED NEW ANGLE FITTING S IAW SRM 51-10-4. 2 L 7 2 4F A6WE 1996080800646 19960808 00646 WP 1996 8 8 MWEA96306 1 19960731 A 5320 4914413 FITTING DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, LT AFT EMERGENCY EXIT OVERWING HAS TWO CRACKED PAN TO FRAME ATTACH FITTINGS. REPLACED THE TWO FITTINGS IAW SRM 52-01. 2 L 7 2 4F A6WE 1996080800647 19960808 00647 WP 1996 8 8 MWEA96307 1 19960731 A 5400 4919864 FITTING DOUG DC9 DC932 3022066 WP RT PHLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 510ME 47132 DURING D-CHECK, A CRACKED FITTING WAS FOUND IN RT PYLON. FABRICATED A NEW FITTING IAW DAC SWG 4919864, INSTALLED IAW SR M 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 1996080800648 19960808 00648 WP 1996 8 8 MWEA96308 1 19960731 A 5320 SUPPORT WEB DOUG DC9 DC932 3022066 WP NLG WW CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, CRACK FOUND IN THE NOSE LANDING GEAR DRAG BRACE SUPPORT WEB. REPAIRED DRAG BRACE SUPPORT BY INSTALLING A FILLER AND NESTED ANGLE PER DAC TELEX SVC MSP-0321/PDG DATED 7 MAY 96. 2 L 7 2 4F A6WE 1996080800649 19960808 00649 WP 1996 8 8 MWEA96309 1 19960731 A 5510 STRINGERS DOUG DC9 DC932 3022066 WP LT HORIZ STAB CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, LOWER STRINGERS 5, 6 WERE FOUND CRACKED AT STATION XHS 50 IN LT HORIZ STAB. REPAIRED THE CRACKED STRING ERS IAW SRM 55-02, FIG 16. 2 L 7 2 4F A6WE 1996080800650 19960808 00650 WP 1996 8 8 MWEA96310 1 19960731 A 5522 SKIN DOUG DC9 DC932 3022066 WP LT ELEVATOR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, FOUND CORROSION ON LOWER SKIN OF LT ELEVATOR 15 INCHES FROM OUTBD TIP. REPLACED SKIN IAW ME EA 55-003. 2 L 7 2 4F A6WE 1996080800651 19960808 00651 WP 1996 8 8 MWEA96311 1 19960731 A 5531 RIBS DOUG DC9 DC932 3022066 WP VERTICAL STAB CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, THREE RIBS WERE FOUND CRACKED THROUGH THE AFT FASTENER HOLES IN THE VERTICAL STABILIZER LEADING EDGE. R EPAIRED THE CRACKED RIBS WITH ANGLE DOUBLERS IAW SRM 55-01, FIG 2 SHEET 3. 2 L 7 2 4F A6WE 1996080800652 19960808 00652 WP 1996 8 8 MWEA96312 1 19960731 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 980 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, EXFOLIATION CORRISION WAS FOUND IN ATTACH FITTING, FLOOR BEAM TO CUSP LINE STRUCTURE AT STA 980 LT. FAB RICATED A NEW FITTING IAW SRM 51-10-2 AND INSTALLED IAW SRM 51-30. 2 L 7 2 4F A6WE 1996080800653 19960808 00653 SO 1996 8 8 RAAA96E9010 1 19960806 A 5414 SKIN LKHEED 188 188C 5262604 SO NR 3 NACELLE CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 1968R 188C2007 DURING ENGINE CHANGE PRE-INSTALL INSPECTION, FOUND .25 INCH CRACK AT FASTENER HOLE IN NR 3 NACELLE OUTBD SKIN AT NAC STA 41, AFT OF OUTBD UPPER ENG MOUNT POINT. REPAIRED PER SRM 54-2-1, FIG 3. 2 L 7 4 4T 4A22 1996080800654 19960808 00654 NM 1996 8 8 SWAA960731 1 19960728 A 3241 26066724 WHEEL BOEING 737 7373H4 1384600 NM NR 2 DAMAGED A SWAA K NONE O OTHER TO TAKEOFF 1 SW 07 356SW 25251 NUMBER 2 WHEEL DAMAGED. REMOVED AND REPLACED NUMBERS 1 AND 2 TIRE/WHEEL ASSEMBLIES PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996080800655 19960808 00655 1996 8 8 SWAA960732 4 19960801 A 2565 61620468 SLIDE BOEING 737 7375H4 138449D NM R 1 DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 511SW 24188 INADVERTENT SLIDE DEPLOYMENT AT FWD SERVICE DOOR. REPLACED SLIDE ASSEMBLY PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996080800656 19960808 00656 NM 1996 8 8 SWAA960733 1 19960730 A 3230 GEAR PIN BOEING 737 7373H4 1384600 NM LANDING GEAR NOT REMOVED A SWAA D RETURN TO BLOCK O OTHER TO TAKEOFF 1 SW 07 355SW 25250 AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. INSPECTED AIRC RAFT, REMOVED GEAR PINS. 2 L 7 2 4F RT A16WE 1996080800657 19960808 00657 NM 1996 8 8 SWAA960734 1 19960805 A 2612 FIRE WARNING BOEING 737 7373A4 1384585 NM APU MALFUNCTIONED A SWAA D F RETURN TO BLOCK ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 SW 07 675AA 23253 ON CLIMBOUT, APU FIRE WARNING LIGHT AND BELL SOUNDED, FIRE BOTTLE WAS DISCHARGED. AIRCRAFT RETURNED TO LAS AND MADE AN UNEVENTFUL LANDING. INSPECTED AIRCRAFT AND FOUND NO EVIDENCE OF FIRE OR OVERHEAT CONDITION. DEFERRED FIRE DETECT/EXTIN GUISHING SYSTEMS AND CONTINUED PER MEL. 2 L 7 2 4F RT A16WE 1996080800658 19960808 00658 NM 1996 8 8 SWAA960735 1 19960805 A 2782 ACTUATOR BOEING 737 7372H4 138448C NM NR 3 LE SLAT MALFUNCTIONED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 80SW 22675 ON CLIMBOUT, NR 3 SLAT WOULD NOT FULLY RETRACT. AIRCRAFT RETURNED TO MAF AND MADE AN UNEVENTFUL LANDING. INSPECTED AND LUBED SLAT TRACKS, OPERATION CHECKED SLATS. MX FERRIED TO DAL. REMOVED AND REPLACED NR 3 SLAT ACTUATOR AND OP CHECKED PER BOEING M/M. 2 L 7 2 4F A16WE 1996080800659 19960808 00659 NM 1996 8 8 SWAA960736 1 19960802 A 5530 DOUBLER BOEING 737 7373H4 1384600 NM VERT STAB GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED D-CHECK, FOUND DOUBLER ON LT VERTICAL STAB AFT T-BEAM HAS A DEEP GOUGE, 10 INCHES FROM TOP OF BODY. RE PLACED DOUBLER PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996080800660 19960808 00660 NM 1996 8 8 SWAA960737 1 19960802 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 995 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 995, RBL 611, WL 226. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996080800661 19960808 00661 NM 1996 8 8 SWAA960738 1 19960727 A 3350 6104789 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 26SW 21117 DURING SCHEDULED SERVICE CHECK, FOUND FWD EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F A16WE 1996080800662 19960808 00662 NM 1996 8 8 UPS96220778 1 19960805 A 5330 SKIN BOEING 727 72727C 138400J NM BS 572 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 908UP 19114 INSPECTION TYPE DLY, SKIN CRACK LEFT SIDE OF FUSELAGE STA 572 JUST ABOVE STR 25. REMOVED DAMAGE FROM SKIN AND STRINGER IAW 53-20-3 AND 53-30-3. DAMAGE REMOVED, FABRICATED DOUBLER, PICKED UP HOLES FROM A/C PER 53-30-3. 2 L 7 3 4F A3WE 1996080800663 19960808 00663 NM 1996 8 8 UPS96220785 1 19960730 A 5315 FLOORBEAM BOEING 727 727180C 138406G NM BS 560 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE SI, CORROSION ON BOTTOM FLOOR BEAM AROUND NUTPLATE HOLES AT STA 560 RBL 45 TO 60 WL 208. REMOVED CORROS ION, REWORK DEEMED OUT OF LIMITS IAW SRM 53-10-1. REMOVED AND REPLACED UPPER FLANGES OF FLOOR BEAM IAW 53-10-2. 2 L 7 3 4F A3WE 1996080800664 19960808 00664 NM 1996 8 8 UPS96220786 1 19960730 A 5347 BAC15201432 SEAT TRACK BOEING 727 727180C 138406G NM BS 668 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE SI, CORROSION UNDER NUTPLATE ON SEAT TRACK FLANGE I/B RBL 25 STA 668 WL 207.8. MECHANICALLY REMOVED COR ROSION, REWORK DEEMED OUT OF LIMITS IAW SRM 53-10-1. ALSO, FOUND CORROSION OUT OF LIMITS FROM STA 480 TO 690 RBL 25 SEA T TRACK. REMOVED AND REPLACED SECTION OF SEAT TRACK 480 TO 690 RBL 25 IAW SRM 53-10-5. 2 L 7 3 4F A3WE 1996080800665 19960808 00665 NM 1996 8 8 UPS96220787 1 19960730 A 5753 FLAP TRACK BOEING 727 727180C 138406G NM NR 3 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE SI, WHEN WORKING CARD 266 NRC 577741 FOUND TWO HOLES CORRODED AT AFT MOUNTING BRACKET OF NR 3 FLAP TRACK . REPAIRED NR 3 FLAP TRACK AFT MOUNT POINT ON BEAM IAW UPS EO NR 727-57-1716. 2 L 7 3 4F A3WE 1996080800666 19960808 00666 NM 1996 8 8 UPS96220788 1 19960730 A 5753 65192067 FLAP TRACK BOEING 727 727180C 138406G NM NR 3 RUSTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE SI, RUST EMANATING FROM NR 3 FLAP TRACK AT SPOILER BEAM MOUNT PAD. REPAIRED NR 3 FLAP TRACK IAW TRAMCO EO 96-2443, UPS EO 727-57-1715. WHILE WORKING THIS NRC 577741, FOUND BOTH TRACK SUPPORT TOWERS CORRODED OUT OF LIMITS. REMOVED AND REPLACED TOWERS IAW SRM 51-30-5, 51-30-2, (P/N 65-41301-14, 65-41301-15). 2 L 7 3 4F A3WE 1996080800667 19960808 00667 NM 1996 8 8 UPS96220789 1 19960730 A 5320 SKIN SPLICE BOEING 727 727180C 138406G NM BS 257 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE SI, CRACKED IN EXTERNAL SKIN SPLICE 1 INCH BELOW STR 10 LAP LT STA 257. REPAIRED EXTERNAL SKIN SPLICE I AW SRM 53-30-3. 2 L 7 3 4F A3WE 1996080800668 19960808 00668 NM 1996 8 8 UPS96220790 1 19960731 A 5347 SEAT TRACK BOEING 727 727180C 138406G NM BS 490-502 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE SI, CORROSION ON SEAT TRACK FLANGE LBL 1 INCH STA 490 TO 502 WL 207.8. REMOVED CORROSION, REWORK DEEMED OUT OF LIMITS IAW SRM 53-10-1. REMOVED AND REPLACED SECTION OF SEAT TRACK FROM STA 490 TO 550 BL 0 TRACK IAW TRAMCO EW O 96-2419. 2 L 7 3 4F A3WE 1996080800669 19960808 00669 NM 1996 8 8 UPS96220792 1 19960731 A 5730 SPAR ACCESS DOOR BOEING 727 727180C 138406G NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE SI, CORROSION FRONT SPAR ACCESS DOOR ON RIGHT WING HAS CORROSION ON INNER AND OUTER SURFACE. REMOVED CO RROSION, REWORK DEEMED OUT OF LIMITS IAW SRM 57-10-1. REPAIRED RT WING SPAR FUEL ACCESS CUTOUT IAW TRAMCO EWO 96-2423. 2 L 7 3 4F A3WE 1996080800670 19960808 00670 NM 1996 8 8 UPS96220795 1 19960801 A 5315 FLOORBEAM BOEING 727 727180C 138406G NM BS 620 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE SI, CORROSION ON TOP AND BOTTOM FLOOR BEAM AROUND NUTPLATE HOLE AT STA 620 RBL 60 WL 208. BLENDED OUT D AMAGE, HFEC INSPECTED, FABRICATED AND INSTALLED REPAIR ANGLE IAW TRAMCO EWO 96-2429 UPS ENGINEERING FILE NR 53-1798. 2 L 7 3 4F A3WE 1996080800671 19960808 00671 NM 1996 8 8 UPS96220796 1 19960801 A 5315 FLOOR BEAM BOEING 727 727180C 138406G NM BS 660 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE SI, CORROSION ON FLOOR BEAM AROUND NUTPLATE HOLES STA 660 RBL 50 WL 208. BLENED OUT DAMAGE, HFEC INSPEC T FOR CORROSION REMOVAL, FABRICATED AND INSTALLED REPAIR ANGLE IAW TRAMCO EWO 96-2428 UPS ENGINEERING FILE NR 727-53-179 7. 2 L 7 3 4F A3WE 1996080800672 19960808 00672 NM 1996 8 8 UPS96220797 1 19960801 A 5320 FLOOR SUPPORT BOEING 727 727180C 138406G NM BS 344 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE SI, CORROSION ON HAT CHANNEL AT STA 344 RBL 20 WL 208. REMOVED, FABRICATED, INSTALLED REPLACEMENT HAT C HANNEL IAW SRM 51-10-2, 51-30-1, 51-30-2, 51-30-8. 2 L 7 3 4F A3WE 1996080800673 19960808 00673 NM 1996 8 8 UPS96220798 1 19960801 A 5320 ANGLE BOEING 727 727180C 138406G NM BS 330-360 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE SI, WHILE WORKING NRC 577408 FOUND MOP SEAL AT BS 330 TO 360 RBL 62 TO BE CORRODED. WHILE DRILLING NEW MOP SEAL FOUND WEB AT BS 355 TO BE CORRODED. REMOVED MOP SEAL, FABRICATED AND INSTALLED REPLACEMENT. REPAIRED CORRODED WEB IAW SRM 51-40-2, OTHER WORK IAW SRM 51-30-8, 51-10-2, 51-30-2. BOEING DRAWING 65-17580, SRM 51-20-1. 2 L 7 3 4F A3WE 1996080800674 19960808 00674 NM 1996 8 8 UPS96220799 1 19960801 A 5330 SKIN BOEING 727 727180C 138406G NM BS 1323 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE SI, CRACK IN FUSELAGE SKIN, LOWER FWD CORNER OF BLOW OUT PANEL CUTOUT BS 1323 LBL 50 WL 216. REPAIRED S KIN AT BS 1323 LBL 50 WL 216 IAW SRM 53-30-3. 2 L 7 3 4F A3WE 1996080800675 19960808 00675 NM 1996 8 8 UPS96220800 1 19960801 A 5315 FLOOR BEAM BOEING 727 727180C 138406G NM BS 344 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE SI, CORROSION ON FLOOR BEAM AT STA 344 RBL 50 TO RBL 20 WL 208. REMOVED UPPER CHORD FROM FLOOR BEAM AND PERFORMED FULL SECTION REPAIR AND REPLACEMENT OF CHORD IAW SRM 53-10-8. 2 L 7 3 4F A3WE 1996080800676 19960808 00676 NM 1996 8 8 UPS96220801 1 19960801 A 5315 FLOOR BEAM BOEING 727 727180C 138406G NM BS 640 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE SI, CORROSION ON TOP AND BOTTOM FLOOR BEAM AROUND NUTPLATE HOLES AT STA 640 RBL 25 TO 60 WL 208. REPAIR ED FLOOR BEAM IAW SRM 53-10-8. 2 L 7 3 4F A3WE 1996080800677 19960808 00677 NM 1996 8 8 UPS96220802 1 19960801 A 5311 65224972 FRAME BOEING 727 727180C 138406G NM BS 930 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE SI, WHILE WORKING 578300 FOUND 930 FRAME RIGHT HAND CRACKED BETWEEN WL 211 AND 213 AT FASTENER LOCATION THROUGH SKIN. REMOVED AND REPLACED FRAME IAW SRM 51-30-2, 51-10-2, 51-20-1 BOEING DRAWING 65-16336. 2 L 7 3 4F A3WE 1996080800678 19960808 00678 NM 1996 8 8 UPS96220803 1 19960802 A 5315 FLOOR BEAM BOEING 727 727180C 138406G NM BS 600 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE SI, CORROSION ON TOP AND BOTTOM FLOOR BEAM AROUND NUTPLATES HOLES AT STA 600 RBL 25 TO 60 WL 208. BLEND OUT DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLE IAW TRAMCO EWO 96-2426 UPS ENGINEERING FILE NR 727-53-1801. 2 L 7 3 4F A3WE 1996080800679 19960808 00679 NM 1996 8 8 UPS96220804 1 19960802 A 5315 FLOOR BEAM BOEING 727 727180C 138406G NM BS 680 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE SI, CORROSION ON FLOOR BEAM STA 680 RBL 45 TO 65 WL 208 AROUND NUTPLATE HOLES. BLEND OUT DAMAGE, FABRIC ATED AND INSTALLED REPAIR ANGLE IAW TRAMCO EWO 96-2427, AUTHORIZED BY UPS ENGINEERING FILE NR 727-53-1799. 2 L 7 3 4F A3WE 1996080800680 19960808 00680 NM 1996 8 8 UPS96220805 1 19960802 A 5320 FLOOR SUPPORT BOEING 727 727180C 138406G NM BS 352 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE SI, WHILE WORKING CARD 577368 FOUND FLOOR SUPPORT AT STA 352 RBL 47 TO RBL 14 TO HAVE CORROSION AT WL 17 1. REMOVED FLOOR SUPPORT ANGLE, FABRICATED AND INSTALLED REPLACEMENT PART IAW SRM 53-10-1, 51-20-2, 51-10-1. 2 L 7 3 4F A3WE 1996080800681 19960808 00681 NM 1996 8 8 UPS96220806 1 19960802 A 5532 SKIN BOEING 727 727180C 138406G NM VERT STAB CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE SI, CORROSION AROUND FASTENERS ON LT FIN MIDSPAR AT FIN STA 194 TO FIN STA 210. REPAIRED LT SKIN AT FIN STA 194 TO FIN STA 210. 2 L 7 3 4F A3WE 1996080800682 19960808 00682 NM 1996 8 8 UPS96220807 1 19960802 A 5320 65493981 CASTING BOEING 727 727180C 138406G NM BS 362 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE SI, WHILE WORKING NRC 577316 FOUND CORROSION IN BARRIER NET CASTING WELL NEXT TO DRAIN HOLE STA 362 LBL 4 WL 207. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 51-10-6. REMOVED AND REPLACED BARRIER NET CASTING STA 362 LBL 4 WL 207 IAW SRM 51-30-8, 51-30-2, 5-10-1, 51-20-4. 2 L 7 3 4F A3WE 1996080800683 19960808 00683 NM 1996 8 8 UPS96220808 1 19960803 A 5320 65184176 STIFFENER BOEING 727 727180C 138406G NM BS 315 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE SI, CORROSION ON STIFFENER STA 315 LBL 12 RBL 12 WL 181 AREAS MARKED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED STIFFENER STA 315 LBL 12 TO RBL 12 WL 181 PER SRM 51-30-2, 51-10-1 , 51-10-6, 51-20-150. 2 L 7 3 4F A3WE 1996080800684 19960808 00684 NM 1996 8 8 UPS96220809 1 19960803 A 5347 654197734 SEAT TRACK BOEING 727 727180C 138406G NM BS 360-380 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE SI, CORROSION IN SEAT TRACK RBL 62 STA 360 TO 380 WL 208. REMOVED CORROSION AND FOUND TO BE OUT OF LIMI TS PER SRM 51-10-1. REMOVED AND REPLACED SEAT TRACK AT RBL 62 STA 360 TO 380 WL 208 IAW SRM 51-3-5, 51-20-151, 51-30-2. 2 L 7 3 4F A3WE 1996080800685 19960808 00685 NM 1996 8 8 UPS96420791 1 19960717 A 5720 CHORD BOEING 747 747123 1384873 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE-C, RT WING LOWER CHORD CRACKED AT RT ILES 1117.00 INSIDE L/E AREA. REMOVED BROKEN OFF PIECE AND TRIMMED CHORD. REPAIR ANGLE PLACED, APPROVED UPS AMS 96-0172RE. 2 L 7 4 4F A20WE 1996080800686 19960808 00686 NM 1996 8 8 UPS96420793 1 19960716 A 5730 SKIN BOEING 747 747123 1384873 NM WS 410 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE-C, RT WING T/E, FOUND FIBERGLASS PANEL BULGED AT WS 410. REMOVED AND INSTALLED PANEL IAW 51-30-02, BLEN D OUT CORROSION AND INSPECT THE REWORKED AREA, SHOTPEEN, ALODINE AND REFINISH THE AREA, EDDY CURRENT FASTENER HOLES REPL ACED FASTENERS, UPS AMS 96-0181. 2 L 7 4 4F A20WE 1996080800687 19960808 00687 NM 1996 8 8 UPS96420794 1 19960719 A 5411 FRAME BOEING 747 747123 1384873 NM NR 4 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE-C, PYLON NR 4 FOUND FRAME CRACKED AT NAC STA 160 LT. REPLACED RIB AND DOUBLER IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996080800688 19960808 00688 WP 1996 8 8 UPS96820779 1 19960626 A 5320 SUPPORT ANGLE DOUG DC8 DC871F 302199D WP BS 70 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-CS2, FS 70 SUPPORT ANGLE HAS MODERATE CORROSION AND CRACKED AT LONGERONS 30L TO 35R. REPAIRED SUPPORT A NGLE PER SRM 53-2-0. 2 L 7 4 4F RT 4A25 1996080800689 19960808 00689 WP 1996 8 8 UPS96820780 1 19960627 A 5311 5764343507 FRAME DOUG DC8 DC871F 302199D WP BS 1060 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-CS2, MODERATE CORROSION DAMAGE AT BELTFRAME FS 1060 LONGERON 36. REPAIRED FRAME PER SRM 53-2-0. 2 L 7 4 4F RT 4A25 1996080800690 19960808 00690 WP 1996 8 8 UPS96820781 1 19960627 A 5311 5764343507 FRAME DOUG DC8 DC871F 302199D WP BS 1060 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE CS2, HEAVY CORROSION ON BELTFRAME FS 1060 BETWEEN LONGERONS 35L TO 36 UPPER CAP. REPLACED FRAME SECTION PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996080800691 19960808 00691 WP 1996 8 8 UPS96820782 1 19960711 A 5311 3614944501 FRAME DOUG DC8 DC871F 302199D WP BS 1060 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE CS2, HEAVY CORROSION ON UPPER FWD SIDE OF BELTFRAME FS 1060 LONGERONS 30R TO 32L. REPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996080800692 19960808 00692 WP 1996 8 8 UPS96820783 1 19960710 A 5315 5616795503 FLOOR BEAM DOUG DC8 DC871F 302199D WP BS-12 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE CS2, CORROSION DAMAGE AT FLOOR BEAM LOWER HORIZONTAL FLANGE FS 12 LBL 45. REPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996080800693 19960808 00693 WP 1996 8 8 UPS96820784 1 19960628 A 5711 5615058502 SPAR DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE CS2, RT LOWER AUX SPAR IS CRACKED AT BOLT HOLE. REPLACED AUX SPAR PER TASK CARD NR 1057. 2 L 7 4 4F RT 4A25 1996080800694 19960808 00694 1996 8 8 HEEA967598 4 19960731 A 3450 071121004 CONTROL BOX BELL 412 412 1182202 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2148K 36001 DISPLAY FLICKERS. REPLACED DISPLAY (DS302) P/N 037-0084-00. REPAIRED. BENCH CHECK GOOD. 1 G 7 2 4U H4SW 1996080800695 19960808 00695 1996 8 8 HEEA967599 4 19960731 A 3450 071121004 CONTROL BOX BOLKMS 117 BK117A3 5626015 EU COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 911NC 7026 ON LCD DISPLAY DIGITS ARE NOT COMPLETE IN SQUELCH SPOTS. CLEANED WAFERS AND DISPLAY CONNECTORS. ALSO REPLACED LOCK RING . REPAIRED. BENCH CHECK GOOD. 1 G 7 2 3U H13EU 1996080800696 19960808 00696 1996 8 8 HEEA967600 4 19960731 A 2312 071121540 COMM CONTROL BELL 214 214ST 1182106 SW COCKPIT COMM DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5748M 28102 WILL NOT ALWAYS CHANGE FREQUENCY. FOUND WAFERS AND CONTACTS LOOSE. TIGHTENED WAFERS AND CONTACT. REPAIRED. ALSO REPLA CED RETAINING RING. BENCH CHECK GOOD. 2 G 7 2 4U H10SW 1996080800697 19960808 00697 1996 8 8 HEEA967601 4 19960731 A 2312 071121540 COMM CONTROL BOLKMS 105 BO105S 5626006 EU COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 6607K S841 DIGITAL DISPLAY UNREADABLE. REPLACED DISPLAY LENS AND PHOTOCELL (V101). ALSO REPLACED TRANSFER SWITCH S102. REPAIRED A ND BENCH CHECK GOOD. 1 G 7 2 3U H3EU 1996080800698 19960808 00698 1996 8 8 HEEA967602 4 19960731 A 3452 066106200 TRANSCEIVER KT76 BELL 206 206L3 1182108 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 4180F 51469 RIGHT KNOB BROKEN. REPLACED BROKEN FACEPLATE ASSEMBLY. ALSO REPLACED DEFECTIVE V101 CAVITY OSCILLATOR DUE TO FREQUENCY DRIFT. UNIT BENCH CHECK GOOD. 1 G 7 1 3U H2SW 1996080800699 19960808 00699 1996 8 8 HEEA967603 4 19960731 A 3452 066106200 TRANSCEIVER KT76 BOLKMS 105 BO105S 5626006 EU COCKPIT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 967MB S737 NO OUTPUT POWER. FOUND WHEN UNIT TURNED TO STANDBY, UNIT TURNS OFF. REPLACED SWITCH BOARD ASSEMBLY. REPAIRED PROBLEM. REPLACED PHOTOCELL V301 DUE TO BEING WEAK. REPAIRED. BENCH CHECK GOOD. 1 G 7 2 3U H3EU 1996080800700 19960808 00700 1996 8 8 HEEA967604 4 19960731 A 3452 066106200 TRANSCEIVER KT76 BELL 206 206L1 1182107 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1078G 45398 WOULD NOT TEST. FOUND FREQUENCY TO DRIFT WHEN VIBRATED AND COOKED UNDER HEAT LAMP. REPLACED CAVITY TUBE V101. REPAIRED . HEATED UNIT, VIBRATED AND PUT IN FREEZER. BENCH CHECK GOOD. 1 G 7 1 3U H2SW 1996080800701 19960808 00701 1996 8 8 HEEA967605 4 19960731 A 3452 066106200 TRANSCEIVER KT76 BELL 206 206B3 1181506 SW COCKPIT INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2268G 3603 INOPERATIVE. REPLACED PHOTOCELL V301 DUE TO WEAK REPLY LIGHT. REPAIRED. COOKED UNIT UNDER HEAT, VIBRATED AND PUT IN FR EEZER. BENCH CHECK GOOD. 1 G 7 1 3U H2SW 1996080800702 19960808 00702 1996 8 8 HEEA967606 4 19960731 A 3452 066106200 TRANSCEIVER KT76 BELL 206 206L1 1182107 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2125M 45649 REPLY LIGHT DIM. REPLACED PHOTOCELL V301. REPAIRED. BENCH CHECK GOOD. 1 G 7 1 3U H2SW 1996080800703 19960808 00703 1996 8 8 HEEA967607 4 19960731 A 3452 066106200 TRANSCEIVER KT76 BOLKMS 105 BO105S 5626006 EU COCKPIT WEAK E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 7170D S840 TRANSPONDER WEAK. FOUND FREQUENCY FALLS OFF LINE WHEN VIBRATED. REPLACED CAVITY OSCILLATOR V101. REPAIRED, COOKED UNIT UNDER HEAT LAMP, VIBRATED AND PUT IN FREEZER. BENCH CHECK GOOD. 1 G 7 2 3U H3EU 1996080800704 19960808 00704 1996 8 8 HEEA967608 4 19960731 A 3452 066106200 TRANSCEIVER KT76 BOLKMS 105 BO105S 5626006 EU COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 54197 S805 DOESN'T WORK IN AIRCRAFT USING TEST EQUIPMENT. FOUND FREQUENCY WOULD DROP OFF LINE WHEN VIBRATED. REPLACED V101 CAVITY TUBE. REPAIRED. ALSO REPLACED V301 PHOTOCELL. REPAIRED. BENCH CHECK GOOD. 1 G 7 2 3U H3EU 1996080800705 19960808 00705 1996 8 8 HEEA967609 4 19960731 A 3454 066400900 CONVERTER KN22 BELL 206 206L3 1182108 SW COCKPIT INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 363BH 51345 UNIT INOPERATIVE. (VOR/LOC NOT WORKING) 1 G 7 1 3U H2SW 1996080800706 19960808 00706 1996 8 8 HEEA967610 4 19960731 A 2312 064102300 TRANSCIEVER BOLKMS 117 BK117A3 5626015 EU COCKPIT VHF INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 401PH 7050 RECEIVER INOPERATIVE. 1 G 7 2 3U H13EU 1996080800707 19960808 00707 1996 8 8 HEEA967611 4 19960731 A 3451 066106902 INDICATOR KDI573 BELL 412 412 1182202 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 6559Z 36019 DME INDICATOR DIGITS ON DISPLAY WILL NOT BRIGHTEN UP. 1 G 7 2 4U H4SW 1996080800709 19960808 00709 1996 8 8 HEEA967613 4 19960731 A 2312 071121525 CONTROL UNIT BELL 412 412 1182202 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 108X 33115 DISPLAY BLINK INTERMITTENT. DISPLAY DIM. REPLACED V101 PHOTOCELL. REPAIRED. BENCH CHECK GOOD. 1 G 7 2 4U H4SW 1996080800710 19960808 00710 1996 8 8 HEEA967614 4 19960731 A 2312 064101905 TRANSCEIVER BELL 206 206L1 1182107 SW COCKPIT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5007Y 45192 TRANSCEIVER UNIT WILL NOT LIGHT UP OR TRANSMIT. 1 G 7 1 3U H2SW 1996080800711 19960808 00711 1996 8 8 HEEA967615 4 19960731 A 3455 066107700 RECEIVER BELL 412 412 1182202 SW COCKPIT ADF FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2149S 36002 2182 TO 2189 FREQUENCY NOT IN SPECS IN "ANT" MODE. (NO NEEDLE DEFLECTION) 1 G 7 2 4U H4SW 1996080800712 19960808 00712 1996 8 8 HEEA967616 4 19960731 A 3453 066402600 LORAN KLN88 BELL 206 206L3 1182108 SW COCKPIT INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 6610Y 51419 INOPERATIVE. (GOES OUT WHEN VIBRATED; ALSO DISPLAYS GARBAGE AT ALL TIMES) INSPECTED AND TESTED UNIT AND FOUND IT WOULD GO OUT COMPLETELY WHEN VIBRATED AND LOOSE PRESENT POSITION. ALSO, UNIT WOULD DISPLAY GARBAGE ON DISPLAY AT TIMES. 1 G 7 1 3U H2SW 1996080800713 19960808 00713 1996 8 8 HEEA967617 4 19960731 A 3453 066402600 LORAN KLN88 BELL 206 206L3 1182108 SW COCKPIT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 41791 51465 LORAN INOPERATIVE. (DROPS OFF LINE WHEN VIBRATED) 1 G 7 1 3U H2SW 1996080800714 19960808 00714 1996 8 8 HEEA967618 4 19960731 A 3453 066402600 LORAN KLN88 BELL 206 206L1 1182107 SW COCKPIT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5014Y 45219 LORAN "DIRECT TO" BUTTON DOES NOT WORK. 1 G 7 1 3U H2SW 1996080800715 19960808 00715 1996 8 8 HEEA967619 4 19960731 A 3444 066106103 ALTIMETER BELL 206 206L3 1182108 SW COCKPIT RADAR ERROR E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 8590X 51494 RADAR ALTIMETER READS 50% LOWER THAN PRESSURE ALTIMETER 1 G 7 1 3U H2SW 1996080800716 19960808 00716 GL 1996 8 8 HEEA967620 2 19960802 A 7250 23060450 NOZZLE VANES 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL NR 1 CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 50293 410 CAT32263F S677 CAE821629F ENGINE REMOVED DUE TO LOW POWER. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: CRACKS BEYOND SERVICEABLE LIMIT S ON #1 NOZZLE VANES AND CRACKED BEYOND SERVICEABLE LIMITS ON COMB. LINER SKIRT. REPLACED DISCREPANT PARTS. 1 G 7 2 3U 3 U H3EU E4CE 1996080800717 19960808 00717 GL 1996 8 8 HEEA967621 2 19960802 A 7250 23056108 LINER 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL COMB SKIRT CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 50293 410 CAT32263F S677 CAE821629F ENGINE REMOVED DUE TO LOW POWER. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: CRACKS BEYOND SERVICEABLE LIMIT S ON #1 NOZZLE VANES AND CRACKED BEYOND SERVICEABLE LIMITS ON COMB. LINER SKIRT. REPLACED DISCREPANT PARTS. 1 G 7 2 3U 3 U H3EU E4CE 1996080800718 19960808 00718 GL 1996 8 8 HEEA967622 2 19960802 A 7250 23060450 NOZZLE VANES 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL NR 1 CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 54197 533 CAT23485 S805 CAE836331 ENGINE REMOVED DUE TO CRACKED COMPRESSOR SCROLL. TURBINE DISASSEMBLED DUE TO LOW POWER ON TEST CELL. UPON INSPECTION O F TURBINE PARTS NOTED THE FOLLOWING: CRACKED BEYOND SERVICEABLE LIMITS ON NR 1 NOZZLE VANES AND EXCESSIVE RUNOUT BEYOND SERVICEABLE LIMITS ON NR 2 NOZZLE 1ST STAGE TIP PATH. REPLACED DISCREPANT PARTS. 1 G 7 2 3U 3 U H3EU E4CE 1996080800719 19960808 00719 GL 1996 8 8 HEEA967623 2 19960802 A 7250 23031938 NOZZLE VANES 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL NR 2 CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 54197 533 CAT23485 S805 CAE836331 ENGINE REMOVED DUE TO CRACKED COMPRESSOR SCROLL. TURBINE DISASSEMBLED DUE TO LOW POWER ON TEST CELL. UPON INSPECTION O F TURBINE PARTS NOTED THE FOLLOWING: CRACKED BEYOND SERVICEABLE LIMITS ON NR 1 NOZZLE VANES AND EXCESSIVE RUNOUT BEYOND SERVICEABLE LIMITS ON NR 2 NOZZLE 1ST STAGE TIP PATH. REPLACED DISCREPANT PARTS. 1 G 7 2 3U 3 U H3EU E4CE 1996080800720 19960808 00720 GL 1996 8 8 HEEA967624 2 19960802 A 7250 23060450 NOZZLE VANES 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL NR 1 CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7161J 394 CAT25990 S834 CAE831141 TURBINE REMOVED DUE TO 1750 HOUR INSPECTION. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: CRACKED BEYOND SERVI CEABLE LIMITS ON NR 1 NOZZLE VANES. REPLACED DISCREPANT PART. 1 G 7 2 3U 3 U H3EU E4CE 1996080800721 19960808 00721 GL 1996 8 8 HEEA967627 2 19960802 A 7250 23038218 NOZZLE 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL 1ST STAGE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 9190Y 785 CAT25437 S669 CAE270075 ENGINE REMOVED DUE TO CARBON 6 & 7 OIL PRESSURE STRUT. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: CRACKED B EYOND SERVICEABLE LIMITS ON #1 NOZZLE VANES. REPLACED DISCREPANT PART. 1 G 7 2 3U 3 U H3EU E4CE 1996080800722 19960808 00722 GL 1996 8 8 HEEA967628 2 19960802 A 7250 23038218 NOZZLE 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL 1ST STAGE OUT OF SPEC E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7136J CAT23285 S830 PART INSTALLED IN TURBINE AND TEST CELL RAN PRODUCED -5.9-4.5-4.5 (NOTE TURBINE PRODUCED -1.1,+0.5+0.5 WITH DALLAS AIRMO TIVE OH #1 NOZZLE) UPON INSPECTION OF PART NOTED THE FOLLOWING: OUT OF OVERHAUL SPECS.A,B,E & F. REPLACED DISCREPANT PA RT. 1 G 7 2 3U 3 U H3EU E4CE 1996080800723 19960808 00723 SW 1996 8 8 HEEA967629 1 19960802 A 6420 214011801127 HUB BELL 214 214ST 1182106 SW T/R BUSHING CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 734 28106 INBOARD BUSHING P/N 214-010-766-101 BEING CRACKED ON BOTH GRIP SETS. ( GRIP SET P/N 214-010-822-101, S/N A474 AND S/N A4 77, T.T. 734:45, T.S.O. 734:45. ) 2 G 7 2 4U H10SW 1996080800726 19960808 00726 EU 1996 8 8 96ZZZX3860 1 19960708 A 6520 350A33215300 LAMINATED HINGE AEROSP AS355 AS355E 8680805 EU T/R TEETER BRG WORN A EJYA K NONE O OTHER IN INSP/MAINT 1 WP 07 911TX 125 5073 DURING ROUTINE MAINTENANCE, FOUND TEETERING BEARINGS WORN BEYOND LIMITS. REPLACED WITH NEW BEARINGS. 1 G 7 2 3U H11EU 1996080800727 19960808 00727 EU 1996 8 8 96ZZZX3861 1 19960708 A 6410 355A12004008 BLADE AEROSP AS355 AS355E 8680805 EU TAIL ROTOR COATING PEEL A EJYA K NONE E VIBRATION/BUFFET IN INSP/MAINT 1 WP 07 911TX 207 5073 PROTECTIVE COATING PEELING FROM SURFACE OF TAIL ROTOR BLADES CAUSING AIRCRAFT VIBRATIONS. REPLACED TAIL ROTOR BLADES. 1 G 7 2 3U H11EU 1996080800729 19960808 00729 WP 1996 8 8 96ZZZX3863 2 19960628 A 7230 31013751 BEARING MTSBSI MU2 MU2B20 5780407 SW GARRTT TPE331 TPE3311151A 01514 WP COMPRESSOR FAILED A HGTA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SW 15 89CR 1246 93199148434 233 P34008 ENGINE WAS MAKING A CLICKING NOISE, ENGINE WAS REMOVED AND SENT FOR REPAIR. FOUND THE FIRST STAGE STATOR HEAT DISTRESSE D AND HITTING FIRST STAGE TURBINE WHEEL. REPAIRED. THE ENGINE WAS RE-INSTALLED AND FLOWN THE NEXT DAY. IT WAS MAKING THE NOISE AGAIN, AND THE AIRCRAFT WAS BROUGHT TO TULSA FOR INSPECTION OF THE NOISE AT IJI PER REQUEST. PART 91 TRIP, TH E LEFT ENGINE FAILED. THE NTS SYSTEM WORKED PERFECTLY AND THE AIRCRAFT LANDED WITHOUT INCIDENT. 1 H 7 2 3T 4 T A2PC E3WE 1996080800806 19960808 00806 NE 1996 8 8 9617031229 2 19960805 A 7310 AC9227F1740 FUEL FILTER DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 1 ENGINE CLOGGED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 229NW 46551 55780 DURING TAKEOFF ROLLOUT, THE NR 1 ENGINE FUEL FILTER BYPASS LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE FUEL FILTER AND FOUND SLIGHTLY CLOGGED. REPLACED THE NR 1 FUEL FILTER AND PERFORMED ENGINE RUNUP CHECK. CHECK WAS NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A22WE E23EA 1996080800807 19960808 00807 NM 1996 8 8 9617045530 1 19960806 A 3350 BATTERY PACK BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 530US 23845 FLOOR EMERGENCY LIGHTS BETWEEN ROWS 15 THROUGH 21 INOPERATIVE. REPLACED BATTERY PACK AND POWER SUPPLY AT DOOR 2R, CHECK ED OK. 2 L 7 3 4F A3WE 1996080800808 19960808 00808 NM 1996 8 8 9617052289 1 19960803 A 3350 BATTERY PACK BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 729RW 21377 RIGHT FORWARD EXTERIOR OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, CHECKED OK. 2 L 7 3 4F A3WE 1996080800809 19960808 00809 NM 1996 8 8 9617062768 1 19960806 A 3350 POWER SUPPLY BOEING 727 7272M7 138407S NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 728RW 21741 LEFT FORWARD EXTERNAL OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED POWER SUPPLY M654, CHECKED GOOD. 2 L 7 3 4F A3WE 1996080800810 19960808 00810 1996 8 8 9617072295 4 19960806 A 3442 20704100101 TRANSCEIVER BOEING 727 727251 138408H NM E/E BAY FAILED A NWAA A UNSCHED LANDING L NO TEST CR CRUISE 1 GL 01 295US 21506 DURING FLIGHT RADAR FAILED, NO TEST PATTERN OBSERVED. NO GROUND RETURN IN NORMAL OR CONT/MSP. REPLACED WEATHER RADAR T RANSCEIVER, OPERATIONAL CHECK NORMAL. 2 L 7 3 4F A3WE 1996080800811 19960808 00811 NM 1996 8 8 96FDEA01323 1 19960806 A 5314 65C8000007 KEEL BEAM BOEING 727 72722 1384002 NM BS 1050 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 NR0201 AND 002, BS 1050 STR 29L LBL 6 THERE IS A BULGE IN SKIN. *S/D* REMOVED AND REPLACED LT KEEL BEAM STR 296 FROM B S 960 TO BS 1090 PER SB 727-53-0179. 2 L 7 3 4F A3WE 1996080800812 19960808 00812 NM 1996 8 8 96UAL900474 1 19960624 A 2780 S256T00211 RVDT BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LE SLAT FAILED A UALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 WP 29 608UA 21869 AIRCRAFT RETURNED TO IAD DUE TO LEADING EDGE SLAT INDICATION. *S/D* INDICATION WAS CAUSED BY FLAP SLAT ELECTRONIC UNIT BALL FAULTING M548 OUTBOARD SLAT ROTARY VARIABLE DIFFERENTIAL TRANSFORMER. REPLACED M548 ROTARY VARIABLE DIFFERENTIAL TRANSFORMER PER MM 27-81-11. FLAP OPERATIONS CHECK NORMAL AND FINAL FSEU BITE CHECKS WERE NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 1996080800813 19960808 00813 NM 1996 8 8 96UAL900479 1 19960624 A 2780 256T2710S POWER DRIVE UNIT BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LE FLAPS OUT OF RIG A UALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 WP 29 608UA 21869 RETURNED TO IAD UNDER AMBER ALERT DUE TO LEADING EDGE SLAT FAILED TO RETRACT. *S/D* THE POWER DRIVE UNIT AND M604 ROTA RY VARIABLE DIFFERENTIAL TRANSDUCER WAS MISRIGGED. REPLACED ALL PROXIMITY SWITCH ELECTRONIC UNIT CARDS. ADJUSTED M604 ROTARY VARIABLE DIFFERENTIAL TRANSDUCER PER MM-27-51-26. REPLACED OUTBOARD LEADING EDGE SLAT POWER DRIVE UNIT. FINAL T ROUBLESHOOTING LED TO REPLACING THE FLAP SLAT ELECTRONIC UNIT AS A PRECAUTION. 2 L 7 2 4F 4 F RT A1NM E3NE 1996080800814 19960808 00814 NM 1996 8 8 96UAL900487 1 19960626 A 3350 LIGHT BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 156UA 20105 RIGHT HAND EXTERIOR BODY FAIRING AFT EMERGENCY LIGHTS INOP. *S/D* REPLACED BATTERY PACK. 2 L 7 4 4F 4 F A20WE E20EA 1996080800815 19960808 00815 NM 1996 8 8 96UAL900495 1 19960628 A 2910 S271W8113 CHECK VALVE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE PYLON GALLED A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 776UA 26937 ENGINE DRIVEN PUMP ON NUMBER 2 ENGINE LEAKING HYDRAULIC FLUID AT PUMP OUTLET. *S/D* LEAK WAS AT HYDRAULIC PUMP OUTLINE LINE CHECK VALVE LOCATED IN PYLON. CHECK VALVE WAS REPLACED. DEFECTIVE VALVE SENT TO VENDOR FOR FURTHER ANALYSIS. 2 L 7 2 4F 4 F RT T0001SE E46NE 1996080800816 19960808 00816 NE 1996 8 8 96UAL900576 2 19960729 A 7314 2175221 BEARING ARGOTEC 7203016 BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUEL PUMP FAILED A UALA K NONE J X WARNING INDICATION ENGINE FLAMEOUT CR CRUISE 1 WP 29 172UA 22362 22362 0541 24363 717676 ENGINE FLAMEOUT. UNABLE TO RESTART. FUEL PUMP BEARING FAILURE CAUSED FUEL RUN SOLENOID SCREEN TO BECOME CLOGGED. ENGI NE WAS REPLACED. 2 L 7 4 4F 4 F RT A20WE E24NE 1996080800817 19960808 00817 WP 1996 8 8 96UAL900577 1 19960729 A 3397 58791 WIRE DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1845U 48261 FORWARD GALLEY LT AISLE EMERGENCY LIGHT DOES NOT WORK. *S/D* REPLACED BROKEN LEAD IN, OPERATIONAL CHECKED SATISFACTORY . 2 L 7 3 4F 4 F A22WE E23EA 1996080800818 19960808 00818 NM 1996 8 8 96UAL900578 1 19960729 A 3350 6104781 BATTERY PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7291U 21569 EMERGENCY LIGHTS INOPERATIVE. SUPPLEMENTAL DATA UPDATE: BATTERY DISCHARGED. REPLACED AFT AIRSTAIR EMERGENCY LIGHT BAT TERY PACK. 2 L 7 3 4F 4 F A3WE E2EA 1996080800819 19960808 00819 NM 1996 8 8 96UAL900579 1 19960729 A 7830 65B963011 TR SWITCH BOEING 747 747222B 1384904 NM PWA JT9 JT9D7R4G2 52054 NE NR 2 ENGINE SHORTED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 29 151UA 23736 715240 NR 2 ENGINE REVERSER LIGHT CAME ON DURING TAKEOFF ROLL. TAKEOFF WAS ABORTED. *S/D* THRUST REVERSER STOW POSITION INDI CATOR SWITCH HAD INTERMITTENT SHORT. REPLACED SWITCH. 2 L 7 4 4F 4 F RT A20WE E3NE 1996080800820 19960808 00820 WP 1996 8 8 96UAL900580 1 19960729 A 3350 EMB51392 POWER SUPPLY DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL LAVATORY INOPERATIVE A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 29 1839U 46633 AT START OF DESCENT A STRONG ODOR OF SMOKE CAME FROM 1L LAVATORY. A PASSENGER HAD FLUSHED TOILET. ODOR WAS OF SHORT D URATION. *S/D* REPLACED FORWARD EMERGENCY LIGHT BATTERY AND POWER SUPPLY. 2 L 7 3 4F 4 F A22WE E23EA 1996080800821 19960808 00821 NM 1996 8 8 96UAL900581 1 19960729 A 3350 1317 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 553UA 25277 CABIN EMERGENCY EGRESS LIGHTING INOP ABOVE SEATS 1AB. RELAMPED, OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996080800822 19960808 00822 NM 1996 8 8 96UAL900582 1 19960729 A 2820 69186128 FUEL VENT TUBE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 FUEL TANK BROKEN A UALA K NONE O OTHER CR CRUISE 1 WP 29 7280U 21558 HAD FUEL FROM FUEL TANK 3 TO TANK 2 TO ALL ENGINES SEQUENCE. *S/D* FOUND NR 3 FUEL TANK VENT TUBE ELBOW BROKEN. REPLA CED TUBE. 2 L 7 3 4F 4 F A3WE E2EA 1996080800823 19960808 00823 NM 1996 8 8 96UAL900583 1 19960730 A 3350 LIGHTS BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 937UA 26668 EMERGENCY ESCAPE PATH LIGHT FORWARD OF DOOR TWO LEFT. 2 L 7 2 4F 4 F RT A16WE E2GL 1996080800824 19960808 00824 NM 1996 8 8 96UAL900584 1 19960730 A 2820 69186128 FUEL VENT TUBE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 FUEL TANK BROKEN A UALA K NONE O OTHER CR CRUISE 1 WP 29 7268U 21415 UNWANTED FUEL TRANSFER FROM NR 3 TANK. *S/D* FOUND FUEL VENT TUBE IN NR 3 TANK BROKEN. REPLACED TUBE. 2 L 7 3 4F 4 F A3WE E2EA 1996080800825 19960808 00825 NM 1996 8 8 96UAL900585 1 19960730 A 2782 654476015 ACTUATOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 6 LE FLAP BROKEN A UALA K NONE J WARNING INDICATION NR NOT REPORTED 1 WP 29 345UA 24249 THE LEADING EDGE FLAPS TRANSIT LIGHT IS ON AND THE NR 6 SLAT LIGHT IS ON STEADY. REPLACED SLAT ACTUATOR. SHOP FOUND TH E ACTUATOR ROD END BROKEN. SENT ROD END TO BOEING FOR EVALUATION. 2 L 7 2 4F 4 F RT A16WE E2GL 1996080800826 19960808 00826 NM 1996 8 8 96UAL900586 1 19960731 A 5313 65B00142 STRINGER BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE BS 760-780 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 4717U 19878 FOUND ONE POPPED AND SEVERAL DISHED RIVETS ON BELLY SKIN FROM STATION 760 TO 780. INTERNAL INSPECTION FOUND CORRODED ST RINGERS 47L AND 47R, STATION 760 TO 780. REMOVED STRINGERS 47L AND 47R FROM STATION 740 TO 780. REMOVED LIGHT SURFACE CORROSION ON SKIN, ALODINE, PRIME, SPLICED IN NEW STRINGERS PER SRM 53-10-03 PAGE 1. 2 L 7 4 4F 4 F A20WE E20EA 1996080800827 19960808 00827 NM 1996 8 8 96UAL900587 1 19960731 A 2120 213T21091 DUCT BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE AIR DISTR RUPTURED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 614UA 49236 21875 SHORTLY AFTER TAKEOFF, THE AIRCRAFT EXPERIENCED A LOUD BANG AND RIGHT DUCT LEAK EICAS MESSAGE. THE AIRCRAFT RETURNED TO FIELD. THE INTERCONNECT DUCT BETWEEN THE LEFT AND RIGHT AIR CONDITIONING PACKS RUPTURED AT A PRODUCTION SEAM. HYDROGE N EMBRITTLEMENT AT THE SEAM WELD OF THE DUCT SEGMENT WAS THE CAUSE OF FAILURE. THE DUCT WAS REPLACED. OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 1996080800828 19960808 00828 WP 1996 8 8 96UAL900588 1 19960731 A 5512 SKIN DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL RT HORIZ STAB DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 1839U 46633 AIRPLANE FERRIED TO OAK FOR ENGINEERING EVALUATION OF RT HORIZONTAL STABILIZER SKIN. DUE TO A SUSPECTED APU HOT START T HE LOWER SKIN PANELS OF THE RT HORIZONTAL STABILIZER, DETACHABLE ELEVATOR AND INBOARD ELEVATOR SHOW SIGNS OF EXCESSIVE S KIN WRINKLING AND BUCKLING. IN ADDITION, THE LOWER FAIRING STRUCTURE ALSO HAS SIGNS OF HEAT DAMAGE. UNDER INVESTIGATIO N. A VISUAL INSPECTION WAS ACCOMPLISHED ON THE AFFECTED AREA. THE DAMAGED PANELS AND FAIRING STRUCTURE WERE REMOVED AN D REPLACED. 2 L 7 3 4F 4 F A22WE E23EA 1996080800829 19960808 00829 WP 1996 8 8 96UAL900589 1 19960731 A 3350 EMB51392 BATTERY PACK DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1844U 48260 EMERGENCY LIGHTING BATTERY CHECK WILL NOT TEST. *S/D* REPLACED FORWARD MID BATTERY PACK. 2 L 7 3 4F 4 F A22WE E23EA 1996080800831 19960808 00831 NE 1996 8 8 96UAL900591 2 19960802 A 7230 COMPRESSOR BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 3 ENGINE STALLED A UALA O OTHER E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS DE DESCENT 1 WP 29 4724U 19875 662819 NR 3 ENGINE HAD COMPRESSOR STALL WHEN THROTTLE RETARDED FOR DESCENT. STALL CAUSED STEADY AIRFRAME VIBRATION, EGT CLIMBE D TO 700 DEGREES AND ENGINE SHUTDOWN. 2 L 7 4 4F 4 F A20WE E20EA 1996080800832 19960808 00832 NM 1996 8 8 96UAL900592 1 19960802 A 3350 1315 LAMP BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7467U 21921 EMERGENCY EXIT LIGHT AT DOOR 1R IS INOPERATIVE. *S/D* RELAMPED, SYSTEM CHECKS OKAY. 2 L 7 3 4F 4 F A3WE E2EA 1996080800833 19960808 00833 NM 1996 8 8 96UAL900593 1 19960802 A 2910 HYD VALVE WATERMAN HYD 1121S21072 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE TE FLAPS FAILED A UALA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 7293U 21571 LOST SYSTEM 'A' HYDRAULIC QUANTITY AND PRESSURE AFTER START OF TAXI. REPLACED OUTBOARD FLAP HYDRAULIC FLOW LIMITING VAL VE DUE TO LEAKING. INSPECTED HYD FILTERS, NO METAL FOUND. SERVICED HYD SYSTEM. OPERATED ALL FLIGHT CONTROLS AND CYCLE D GEAR HANDLE WITH GEARS PINNED. OPERATED NR 1 AND NR 2 ENGINES. ALL INDICATIONS NORMAL. NO LEAKS. 2 L 7 3 4F 4 F A3WE E2EA 1996080800834 19960808 00834 1996 8 8 CALA9601134 4 19960802 A 2210 4030952906 COUPLER BOEING 737 737524 1384721 NM AP SYSTEM INOPERATIVE A CALA O OTHER F FLT CONT AFFECTED CL CLIMB 1 SW 09 59630 3738 3738 27534 THE AIRCRAFT EXPERIENCED AN UNCOMMANDED ROLL OF 30 DEGREES LEFT AT 7,000 FEET AND 210 KNOTS. THE AUTOPILOT WAS DISCONNEC TED AND LEVEL FLIGHT WAS REGAINED. WHEN THE AUTOPILOT WAS RECONNECTED THE AIRCRAFT FLEW NORMALLY. THE FLIGHT WAS CONTI NUED WITHOUT FURTHER PROBLEMS. MAINTENANCE TESTED THE AUTOPILOT AND DFC SYSTEMS AND PERFORMED A LAND VERIFY WITH ALL SY STEMS PASSING TEST. THE YAW DAMP COUPLER WAS REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE AND TESTED IAW MM 22-12-31 . THE SDR WILL REMAIN OPEN PENDING SHOP FINDINGS ON YAW DAMP COUPLER. THE YAW DAMP COUPLER VENDOR TEAR-DOWN REPORT STAT ED THAT REJECTION OF THE COMPONENT WAS NOT CONFIRMED. PART TOTAL CYCLES, 2,077. 2 L 7 2 4F RT A16WE 1996080800835 19960808 00835 NE 1996 8 8 CALA9601135 2 19960806 A 7321 8062493 FUEL CONTROL BOEING 737 7373T0 1384582 NM GE CFM56 CFM563B1 13802 NE NR 1 ENGINE INOPERATIVE A CALA K NONE O OTHER AP APPROACH 1 SW 09 69333 31308 2954 23571 721349 THE NR 1 ENGINE FLAMED OUT ON APPROACH TO IAH. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE FUEL CONTROL UNIT. THE FUEL PUMP WAS ALSO REPLACED. THE ENGINE WAS TRIMMED PER MM 71-00-01 AND ALL PAR AMETERS WERE NORMAL WITH NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A16WE E2GL 1996080800836 19960808 00836 WP 1996 8 8 CKSA96080 1 19960803 A 2612 D5020 FIRE LOOP DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3B 52039 NE NR 4 ENGINE CHAFED A CKSA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 23 801MG 45986 669406 NR 4 ENGINE FIRE WARNING CAME ON AT CRUISE ALT 37.0, ALL ENGINE PARAMETERS APPEARED NORMAL. OIL PRESSURE AND TEMPERATUR E MIN OIL 25 PSI. SHUTDOWN ENGINE INFLIGHT IAW AIA FOM PROCEDURES, WINDMILL TIME 47 MINUTES. REMOVED AND REPLACED NR 4 ENGINE FIRE LOOP AND PERFORMED OPS CHECK, OPS CHECK GOOD IAW MM 26-2-0. REMOVED AND REPLACED FIRE BOTTLES IAW MM 26-3- 0. PERFORMED ENGINE INSPECTION PER PRATT AND WHITNEY JT3D-7 MM CHAPTER 72, PAGE 663, SECTION C. PERFORMED ENGINE RUNUP OPS CHECK NORMAL IAW MM 71-00. 2 L 7 4 4F 4 F 4A25 1E8 1996080800837 19960808 00837 WP 1996 8 8 CKSA96081 1 19960803 A 2621 893244 FIRE BOTTLE DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3B 52039 NE NR 4 ENGINE DISCHARGED A CKSA F ACTIVATE FIRE EXT. P NO WARNING INDICATION CR CRUISE 1 GL 23 801MG 45986 669406 NR 4 ENGINE OUTBOARD BOTTLE DID NOT INDICATE LOW PRESSURE WHEN DISCHARGED FOR FIRE WARNING INDICATION. REMOVED AND REPL ACED NR 3 AND NR 4 FIRE BOTTLES. PERFORMED SYSTEM CHECK, SYSTEM CHECKS OUT NORMAL IAW 26-3-0. 2 L 7 4 4F 4 F 4A25 1E8 1996080800838 19960808 00838 WP 1996 8 8 MWEA96313 1 19960731 A 5315 FLOOR BEAM DOUG DC9 DC932 3022066 WP AFT CARGO COMPT CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, LIGHT CORROSION FOUND IN UPPER FLANGE OF CABIN FLOOR BEAM BETWEEN NUTPLATES AT STA 996 ABOVE WASTE DRAIN TUBE ON RT SIDE. REPLACED UPPER CAP ANGLE IAW SRM 53-1. 2 L 7 2 4F A6WE 1996080800839 19960808 00839 WP 1996 8 8 MWEA96314 1 19960731 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 965 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, FITTING FOR FLOOR BEAM ATTACH TO CUSP STRUCTURE FOUND CORRODED/CRACKED AT STA 965. FABRICATED A NEW FIT TING IAW SRM 51-10-2, INSTALLED IAW SRM 51-30. 2 L 7 2 4F A6WE 1996080800840 19960808 00840 WP 1996 8 8 MWEA96315 1 19960731 A 5530 FITTING DOUG DC9 DC932 3022066 WP VERT STAB CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, THE RT FWD VERTICAL STAB ATTACH FITTING WAS FOUND CRACKED BETWEEN BOLT HOLES AT STA 1087. INSTALLED A N EW ATTACH FITTING IAW SRM 55-01, PG 1. 2 L 7 2 4F A6WE 1996080800841 19960808 00841 WP 1996 8 8 MWEA96316 1 19960731 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 1121 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, CORROSION AND POPPED RIVET FOUND IN END FITTING AT STA 1121, LONG 10R. INSTALLED A NEW FITTING IAW SRM 51-10-3 AND 51-30-5. 2 L 7 2 4F A6WE 1996080800842 19960808 00842 WP 1996 8 8 MWEA96317 1 19960731 A 5400 FITTING DOUG DC9 DC932 3022066 WP LT PYLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, LT PYLON ATTACH FITTING WAS FOUND CRACKED IN AFT INBD CORNER OF THE CANNON PLUG COMPARTMENT. REPLACED C RACKED FITTING IAW SRM 51-01 AND 51-30-1. 2 L 7 2 4F A6WE 1996080800843 19960808 00843 WP 1996 8 8 MWEA96318 1 19960731 A 5522 SKIN DOUG DC9 DC932 3022066 WP LT ELEVATOR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, FOUND THAT THE LT ELEVATOR HAD MODERATE CORROSION ON UPPER OUTBD SKIN FROM STA XE171.0 TO XHR 224.0. RE PLACED AFFECTED SKIN IAW ME EA 55-002. 2 L 7 2 4F A6WE 1996080800844 19960808 00844 WP 1996 8 8 MWEA96319 1 19960731 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 1038 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, A FRAME WEB WAS FOUND CRACKED IN AFT ACCESSORY AT STA 1038 INBD OF LONGERON 13L. INSTALLED A REPAIR IAW SRM 53-01, FIG 2 SHEET 3. 2 L 7 2 4F A6WE 1996080800845 19960808 00845 WP 1996 8 8 MWEA96320 1 19960731 A 5711 SPAR CAP DOUG DC9 DC932 3022066 WP WS 506-545 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, THE RT WING LEADING EDGE HAD MODERATE SURFACE CORROSION INSIDE BOTTOM SPAR CAP BETWEEN STATIONS XRS 506 TO XRS 545. COMPLETED REPAIR IAW DAC TELEX SVC-MSP-0427/RMK DATED 6/3/96. 2 L 7 2 4F A6WE 1996080800846 19960808 00846 WP 1996 8 8 MWEA96321 1 19960731 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 1076 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, CRACKED LONGERONS WERE FOUND IN AFT ACCESSORY COMPT LONG 2L AND 2R AT STA 1076. FABRICATED LONGERONS IA W SRM 53-02, FIG 8 AND INSTALLED IAW SRM 53-01, PAGE 1. 2 L 7 2 4F A6WE 1996080800847 19960808 00847 WP 1996 8 8 MWEA96322 1 19960731 A 5753 SKIN DOUG DC9 DC932 3022066 WP NR 5 TE FLAP DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, THE RT FLAP NR 5 TRAILING EDGE WAS FOUND WITH DENTED LOWER SKIN FROM THE 3RD THROUGH 5TH RIB FROM THE OU TBD EDGE. INSTALLED NEW SKIN IAW EA 57-004. 2 L 7 2 4F A6WE 1996080800848 19960808 00848 EU 1996 8 8 QXEA9600274 1 19960805 A 3350 1820 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 462AU 11054 RIGHT OVERWING EMERGENCY LIGHT FOUND INOP DURING PREFLIGHT. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996080800849 19960808 00849 NM 1996 8 8 QXEA9600275 1 19960805 A 5712 RIB DORNER 001B574A1004 DORNER DO32 DO328100 2996000 NM LT WING LE CRACK A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 330PH 3008 LEFT WING LEADING EDGE SECTION 511AL .5 INCH CRACK NOTED IN OUTBOARD RIB UPPER FLANGE AT THE LAST FASTENER LOCATION. CR ACK FOUND DURING C-CHECK. CRACK STOP DRILLED AND DOUBLER INSTALLED PER EA 7-57-49. 2 H 7 2 4T RT A45NM 1996080800850 19960808 00850 SW 1996 8 8 QXEA9600276 1 19960806 A 2612 3219027001 LOGIC MODULE SWRNGN SA227 SA227AC 8780603 SW NR 1 ENGINE MALFUNCTIONED A QXEA K NONE N FALSE WARNING CR CRUISE 1 NM 09 26932 AC660 NR 1 ENGINE FIRE WARNING AMBER LIGHT ILLUMINATED INTERMITTENTLY IN CRUISE. FIRE WARNING LOGIC MODULE REPLACED AND SYSTE M OPS CHECKED GOOD. 2 L 7 2 4T RT A8SW 1996080800851 19960808 00851 SO 1996 8 8 RAAA96E9011 1 19960807 A 2110 2064204 CABIN COMP. LKHEED 188 188C 5262604 SO NO. 3 ENGINE MALFUNCTIONED A RAAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 AL 03 1968R 56 188C2007 DURING POST MAINTENANCE TEST, FLIGHT CABIN AND COCKPIT FILLED WITH SMOKE AFTER 20 MINUTES OF FLIGHT, SOURCE UNKNOWN. A IRCRAFT LANDED WITHOUT INCIDENT, SMOKE NOTED BY FLIGHT CREW AFTER AIRCRAFT PARKED. REPLACED NR 3 ENG'S ENGINE DRIVEN C OMPRESSOR. RUN OPS, CHECK AIR CONDITIONING SYSTEM WITH BOTH EDC'S ON LINE. NO OIL SMOKE NOTED, OPS CHECKED NORMAL. 2 L 7 4 4T 4A22 1996080800852 19960808 00852 NM 1996 8 8 VSTA9608001 1 19960805 A 2613 106109665 OVERHEAT ELEMENT BOEING 737 737247 138448D NM NR 2 ENGINE BROKEN A VSTA E ENGINE SHUTDOWN N FALSE WARNING UK UNKNOWN 1 WP 07 303VA 20125 NR 2 ENG OVERHEAT LIGHT CAME ON. PULLED BACK POWER AND THE LIGHT STAYED ON. FIRED BOTH EXTINGUISHERS AND LIGHT STAYED ON. SHUT DOWN ENGINE, INSP, FOUND LOWER FWD ELEMENT BELOW G/BOX BROKEN. REMOVED AND REPLACED, OPS CHECK GOOD. 2 L 7 2 4F A16WE 1996081200001 19960812 00001 EU 1996 8 12 C2XA96IA183 1 19960612 A 3234 1005383Y00 SELECTOR VALVE AEROSP ATR42 ATR42320 8680930 EU LANDING GEAR FAILED A A C2XA O OTHER J WARNING INDICATION AP APPROACH 1 SW 09 42836 11231 236 200 IAH - FLT 3865 - ON APPROACH TO IAH, LANDING GEAR WOULD NOT EXTEND. CREW FOLLOWED EMERGENCY EXTENSION PROCEDURES AND TH E AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR SELECTOR VALVE AND PERFORMED OPERATIONAL CHEC KS PER ATR-42 MM PROCEDURES, ALL SYSTEM CHECKS NORMAL. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1996081500001 19960815 00001 SO 1996 8 15 SWIA95753 1 19960728 A 2910 1203501525 HYDRAULIC LINE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT ENGINE FAILED A SWIA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 07 288SW 120316 IN-FLIGHT FAILURE OF THE BLUE HYDRAULIC SYSTEM WITH LOSS OF FLUID. FOUND NR 6 HYDRAULIC LINE CHAFING ON ENGINE OIL COOL ER AIR INLET. REPLACED NR 6 LINE AND RIGHT ENGINE DRIVEN HYDRAULIC PUMP. RAN RIGHT ENGINE, OPS CHECK AND LEAK CHECK GO OD. 2 L 7 2 4T 4 T RT A31SO E20NE 1996081500002 19960815 00002 NE 1996 8 15 96ZZZX3857 2 19960717 A 7200 ENGINE LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B NE NR 2 FAILED A RIAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 19 302MB 41209 3394 193A1129 10218 ON RIA, FLT 711A, MIA/YQX - DURING CLIMB-OUT, NR 2 ENGINE EXPERIENCED HIGH AVM ON BOTH CHANNELS (AVM FOLLOWED THROTTLE). ACFT RETURNED TO MIA. ON GROUND, MAINTENANCE FOUND METAL IN CHIP DETECTORS. ENGINE REPLACED, ACFT RELEASED INTO SERV ICE. (X) 2 L 7 3 4F 4 F A23WE E12EU 1996081500003 19960815 00003 EU 1996 8 15 SWAA960730 2 19960803 A 7230 FAN BLADES BOEING 737 7373A4 1384585 NM CFMINT CFM56 CFM563B2 13802 EU NR 1 DAMAGED A SWAA D RETURN TO BLOCK C E F.O.D. VIBRATION/BUFFET TO TAKEOFF 1 SW 07 677AA 23291 EXPERIENCED BIRD STRIKE TO NUMBER 1 ENGINE ON TAKEOFF ACCOMPANIED BY VIBRATION. AIRCRAFT RETURNED TO BHM AND MADE AN UN EVENTFUL LANDING. PERFORMED BIRD STRIKE AND BORESCOPE INSPECTIONS, REPLACED 8 ENGINE FAN BLADES AND PERFORMED ENGINE RU N PER BOEING M/M. 2 L 7 2 4F 4 F RT A16WE E21EU 1996081500006 19960815 00006 NM 1996 8 15 P5CA9600471 1 19960804 A 3231 1411935 ROD END BOEING 747 747123 1384873 NM RT MLG DOOR WRONG PART A P5CA O OTHER J WARNING INDICATION CL CLIMB 1 WP 23 858FT 20109 WITH GEAR RETRACTED AND GEAR HANDLE IN OFF POSITION RED DOOR OPEN LIGHT ON FORWARD PANEL ILLUMINATED AND AMBER BODY DOOR OPEN LIGHT ON FE PANEL ILLUMINATED, IN BOTH PRIMARY AND ALTERNATE POSITIONS. REPLACED RIGHT BODY GEAR DOOR ACTUATOR IA W MM 32-33-27, LEAK CHECKED OK BUT DID NOT FIX PROBLEM. FOUND BODY GEAR DOOR LINKAGE ROD END WRONG PART NUMBER AND WOUL D NOT ALLOW ADJUSTMENT. REPLACED ROD AND RIGGED PER BOEING MAINTENANCE MANUAL 32-33-27 PG 401-405, 32-14-10, 32-14-00. 2 L 7 4 4F A20WE 1996081500007 19960815 00007 NM 1996 8 15 96FDEA01324 1 19960807 A 5311 65207282 FRAME BOEING 727 72722 1384002 NM BS 1057 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 NR 0176 AND 003. CORROSION C53-111-01(3) ON FRAME AT BS 1057, RBL 30, WL 149. ****S/D**** COMING. 2 L 7 3 4F A3WE 1996081500008 19960815 00008 NM 1996 8 15 96FDEA01325 1 19960807 A 5315 6520838 FLOOR BEAM BOEING 727 72722 1384002 NM BS 1110 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 NR0111 AND 004, CORROSION (C53-111-01, -3) ON FLOOR BEAM UNDER NUTPLATES AT BS 1110 WL 200 LBL 32 TO RBL 43 AFT BAY. *S /D* REPAIRED FLOOR BEAM AT BS 1110, WL 200, LBL 32 TO RBL 43 PER FEDEX EA NR 7-5310-29712. 2 L 7 3 4F A3WE 1996081500009 19960815 00009 NM 1996 8 15 96FDEA01326 1 19960807 A 5315 65208346 FLOOR BEAM BOEING 727 72722 1384002 NM BS 1050 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 NR 0114 AND 005. CORROSION C53-111-01(3) ON FLOOR BEAM UNDER NUTPLATES AT BS 1050 FROM LBL 32 - RBL 41, WL 200 (AFT BAY ). *****S/D***** COMING. 2 L 7 3 4F A3WE 1996081500010 19960815 00010 NM 1996 8 15 96FDEA01327 1 19960807 A 5313 6556236 STRINGER BOEING 727 727233 138408A NM BS 720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 219FE 21102 NR0328 AND 001, CORROSION (C53-111-01, -2) ON STR 27L BS 720A PLUS 10 WL 150 LBL 15. *S/D* REMOVED DAMAGED SECTION FRO M 720A PLUS 7 TO 720A PLUS 10. REPAIRED STR SECTION PER FEDEX SRM 53-10-1, 53-10-3 FIG 1. 2 L 7 3 4F RT A3WE 1996081500011 19960815 00011 WP 1996 8 15 96FDEA01329 1 19960807 A 5320 FITTING DOUG DC10 DC1030 3023501 WP BS 2033 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 321FE 47836 SNRM 3063. HORIZONTAL STABILIZER CENTER SECTION FITTING IS CRACKED AT RT FORWARD UPPER TORQUE BOX PLANE, STA 2033, S TR 13R. ****S/D***** VERIFIED CRACK WITH HFEC. FABRICATE REPAIR ANGLE AND DOUBLER. INSTALLED PER EA 8-5310-29041. 2 L 7 3 4F A22WE 1996081500012 19960815 00012 NM 1996 8 15 96FDEA01330 1 19960806 A 2613 OVERHEAT LIGHT BOEING 727 72722 1384002 NM NR 1 STRUT ILLUMINATED A FDEA A E UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 SO 25 195FE 19144 AFTER T/O ON CLIMBOUT, ENG NR 1 STRUT OVERHEAT LITE ON. RAN CHKLST. ENG AT IDLE FOR 3 MIN LITE REMAINED ON. SHUTDOWN E NG PER CHKLST. AFTER 5 MIN LITE STILL ON. PULLED FIRE HANDLE AS PRECAUT. 2 MIN LATER LITE OFF. WINDMILL 20 MIN OIL PR ESS 43. REMD PNLS TO STRUT AREA. RAN NR 1 ENG PER JRH & LEAKING FROM CLAMP AT HEAT EXCHANGER INLET. TIGHTENED CLAMP & SECURED PANELS. RAN ENG & LITE OK UNITL ENG SHUTDOWN & NR 1 ENG STRUT LITE CAME ON STEADY & REMAINED ON. SUSPECT BAD LOOP. NR 1 ENG OIL FILTER REPLACED & RAN ENG FOR 5 MIN PER 72-00. NR 1 ENG STRUT O/H LITE REMAINS ON. LOOP OR WIRING AT FAULT. NO CONTAMINATION FOUND NR 1 ENG. REMOVED & REPLACED NR 1 ENG STRUT O/H DET LOOP PER MM 26-11-31. OPS CK GD. 2 L 7 3 4F A3WE 1996081500013 19960815 00013 NM 1996 8 15 96FDEA01331 1 19960807 A 5280 DOOR BOEING 727 727173C 1384059 NM NLG MISSING A FDEA A J UNSCHED LANDING DUMP FUEL D INFLIGHT SEPARATION CL CLIMB 1 SO 25 199FE 19509 RAISED GEAR HANDLE AND HEARD LOUD BANG. FELT VIBRATIONS AND NOSE GEAR LIGHT REMAINED ILLUMINATED. LOWERED GEAR, DUMP ED FUEL, AND RETURNED TO BASE. ****S/D***** LEFT FORWARD NOSE GEAR DOOR WAS FOUND TO BE MISSING. REPLACED LEFT FO RWARD NOSE GEAR DOOR PER MM 32-22-1. ALL SHEET METAL REPAIRS IAW EA 7-5310-260945. REINSTALLED LEFT AFT NOSE (STRUT) D OOR PER MM 32-22-12. 2 L 7 3 4F A3WE 1996081500014 19960815 00014 NM 1996 8 15 96FDEA1328 1 19960807 A 5330 6572702 SKIN BOEING 727 7272D4 138407U NM BS 303 CREASED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 NR0430 & 009 SHARP CREASE IN SKIN FROM STA 303 - 325 L/H BETWEEN STR 3-4. ****S/D***** REPAIRED CREASE IN SKIN PER FEDEX SRM 53-30-3. DAMAGED AT BS 303 BETWEEN STR 3 & 4L WAS REPAIRED ON NR-0471. 2 L 7 3 4F A3WE 1996081500015 19960815 00015 NM 1996 8 15 CALA9601136 1 19960807 A 2612 FIRELOOP BOEING 737 737130 1384435 NM NR 1 ENGINE MALFUNCTIONED A CALA A E F UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 SW 09 77204 19021 THE NR 1 ENGINE FIRE WARNING LIGHT AND BELL ACTIVATED DURING CLIMB OUT OF EWR. BOTH FIRE BOTTLES WERE DISCHARGED, THE N R 1 ENGINE WAS SHUTDOWN, AND AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE BOTTOM FIRE DETECTOR LOOP AT FAULT. THE FIRE DETECTOR LOOP AND THREE CONNECTORS WERE REMOVED AND REPLACED. BOTH FIRE BOTTLES WERE REMOVED AND REPLACED. THE NR 1 ENGINE WAS RUN AT TAKEOFF POWER AND ALL INDICATIONS WERE NORMAL. 2 L 7 2 4F A16WE 1996081500016 19960815 00016 NE 1996 8 15 CALA9601137 2 19960807 A 7250 798403 T3 BLADE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE NR 1 ENGINE BROKEN A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 16892 25812 493 49391 716747 A LOUD BANG WAS HEARD AND THE AIRCRAFT EXPERIENCED VIBRATION DURING CLIMBOUT.T HE NR 1 ENGINE N1 AND N2 BOTH SPOOLED DO WN AND EGT ROSE TO APPROXIMATELY 630 DEGREES. THE ENGINE THROTTLE WAS REDUCED TO IDLE AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE TURBINE FAILED AND THERE WAS METAL IN THE TAILP IPE. THE NR 1 ENGINE WAS REMOVED AND REPLACED. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION. * S/D* SHOP FINDINGS REVEALED A BROKEN T-3 BLADE. 2 L 7 2 4F 4 F A6WE E9NE 1996081500017 19960815 00017 WP 1996 8 15 CALA9601138 1 19960807 A 2910 7936907669 HYD LINE DOUG DC9 DC982 3022082 WP LT MLG DOOR LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 92874 49122 THE AIRCRAFT LOST RT HYDRAULIC SYSTEM PRESSURE WHILE EN ROUTE TO CLE. THE HYDRAULIC QUANTITY INDICATION FLUCTUATED BETW EEN TWO AND TWELVE QUARTS. THE LANDING GEAR WAS LOWERED USING ALTERNATE EXTENSION HANDLE. WHEN THE AIRCRAFT ARRIVED IN CLE, THE NOSE GEAR STEERING WAS INOPERATIVE. THE AIRCRAFT WAS TOWED TO THE GATE. MAINTENANCE FOUND HYDRAULIC LINE TO LT MLG DOOR LATCH LEAKING. THE LINE WAS REPLACED USING FLEX LINE AND A DIP WAS ISSUED TO REPLACE THE FLEX LINE BEFORE 1 ,200 HOURS OR 500 FLIGHTS. 2 L 7 2 4F A6WE 1996081500018 19960815 00018 SO 1996 8 15 COMA9610242 1 19960807 A 2752 MS3126P1210S CONNECTOR EMB 120 EMB120RT SO RT TE FLAP ACT DEFECTIVE A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 189CA 120189 RIGHT OUTBOARD FLAP IS STUCK AT 45 DEGREES. REPLACED DEFECTIVE WIRING CONNECTOR AT RIGHT OUTBOARD FLAP ACTUATOR. 2 L 7 2 4T RT A31SO 1996081500019 19960815 00019 NM 1996 8 15 DL72L961841 1 19960804 A 3350 1060097126 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 512DA 21314 FORWARD CENTER EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY. 2 L 7 3 4F A3WE 1996081500020 19960815 00020 NM 1996 8 15 DL72L961853 1 19960802 A 5330 65C139132 SKIN BOEING 727 727232 1384082 NM BS 1040-1080 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 509DA 21311 FOUND CORROSION ON THE INTERNAL SKIN BETWEEN STA 1040-1080 AT STR 28L. THE CORROSION WAS BLENDED WITH A MAXIMUM DEPTH OF 0.012 INCH BETWEEN STR 28L AND THE OUTBOARD INTERCOSTAL. STR 28L WAS ALSO FOUND CORRODED. SPLICED NEW SECTIONS IN A T STA'S 1040, 1060, AND 1080 PER B727 SRM 53-10-3, FIG. 1. THE SKIN WILL BE REPAIRED PER B727 SRM 53-30-3, FIG. 4. 2 L 7 3 4F A3WE 1996081500021 19960815 00021 NM 1996 8 15 DL72S961831 1 19960801 A 3350 081691 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 421DA 21274 TRACK LIGHT AT 36D INOPERATIVE. REPLACED SOCKET AND BULB, CHECKS NORMAL. 2 L 7 3 4F A3WE 1996081500022 19960815 00022 NM 1996 8 15 DL72S961835 1 19960803 A 3350 334701744 BATTERY PACK BOEING 727 727232 1384082 NM RT OVERWING DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 489DA 21019 RIGHT OVERWING EMERGENCY LIGHTS INOPERATIVE ON S/C TEST. REPLACED OVERWING BATTERY RACK POWER SUPPLY, TEST OK PER M/M. 2 L 7 3 4F A3WE 1996081500023 19960815 00023 NM 1996 8 15 DL72S961840 1 19960803 A 3350 334701744 POWER SUPPLY BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 498DA 21142 DURING TEST, CENTER EMERGENCY LIGHTS FLICKER. REPLACED POWER SUPPY, OPS CHECK NORMAL. 2 L 7 3 4F A3WE 1996081500024 19960815 00024 NM 1996 8 15 DL72S961852 1 19960802 A 5330 6554583126 SKIN BOEING 727 727232 1384082 NM BS 1166 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 521DA 21472 FOUND CORROSION IN THE AFT LAVATORY SERVICE PANEL CUTOUT. LOCATED JUST AFT OF STA 1166. REPAIRED IN ACCORDANCE WITH FA A/DER FORM 8110-3, DER DESIGNATION SO-831, DATED AUGUST 2, 1996. 2 L 7 3 4F A3WE 1996081500025 19960815 00025 NM 1996 8 15 DL757961837 1 19960803 A 2121 COOLING FAN 731376A BOEING 757 757232 1384965 NM E/E COMPT FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 622DL 0318 22912 10203 ON DESCENT INTO CVG, STRONG SMELL OF SMOKE IN COCKPIT. DECLARED EMERGENCY AND LANDED WITH SMELL OF SMOKE REPORTED BY FL T ATTNS FROM FWD-MID-AND AFT SECTIONS OF CABIN. FIRE DEPT REPORTED STRONG SMELL OF SMOKE IN AVIONICS COMPARTMENT UPON G ROUND INSPECTION. FOUND NR 1 EQUIPMENT COOLING FAN WITH FROZEN BEARING. REPLACED FAN. 2 L 7 2 4F RT A2NM 1996081500026 19960815 00026 NE 1996 8 15 DL76L961849 2 19960805 A 7200 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 MALFUNCTIONED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 172DN 24454 24775 724163 NR 2 ENGINE REPLACED DUE EGT LIMITED ISA 8 PLUS DEGREES. ENGINE TOTAL CYCLES, 4,037. 2 L 7 2 4F 4 F RT A1NM E24NE 1996081500027 19960815 00027 NM 1996 8 15 DL76S961847 1 19960802 A 5754 114T41031 TE WEDGE BOEING 767 767332 1382001 NM LE FLAP DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 123DN 23437 THE NRS 10, 11, 12 LEADING EDGE SLATS' TRAILING EDGE WEDGES WERE FOUND TO HAVE AREAS OF DELAMINATION. THE AREAS MEASURE 4 INCHES BY 6 INCHES, 2 INCHES BY 3 INCHES, AND 10 INCHES BY 6 INCHES, RESPECTIVELY. REPAIRED IN ACCORDANCE WITH B767- 300 SRM, 57-43-02, FIG 201. 2 L 7 2 4F RT A1NM 1996081500028 19960815 00028 WP 1996 8 15 DLL10961832 1 19960802 A 3310 LIGHT PANEL 10648LD1109 LKHEED 1011 10113851 5265010 WP COCKPIT FAILED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 725DA 193C1162 FDAU LIGHT ILLUMINATED DURING TAXI THEN SMOKE WAS OBSERVED COMING OUT FROM BEHIND FLT DATA RECORDER SWITCH. SWITCH ASSY WAS REPLACED, BUT LIGHTS WILL NOT COME ON. ON SWITCH LIGHT. SUSPECT PANEL WAS DAMAGED WHEN SWITCH SHORTED OUT. FDAU W AS FORWARDED TO MCO/PLAC PER MEL 31-31-01. 2 L 7 3 4F A23WE 1996081500029 19960815 00029 WP 1996 8 15 DLL10961845 1 19960626 A 5320 1512169101 FITTING LKHEED 1011 10113851 5265010 WP BS 901 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 727DA 193C1167 THE LOWER DOOR SILL INBOARD CAP FITTINGS, AT FS 901 LT AND RT, WERE FOUND CORRODED AND REQUIRED REPLACEMENT. THE DAMAGE WAS FOUND IN ATLANTA DURING AN HMV IN JUNE, 1996. TO CORRECT THE PROBLEM, NEW FITTINGS WERE MANUFACTURED BY DELTA. 2 L 7 3 4F A23WE 1996081500030 19960815 00030 WP 1996 8 15 DLL10961848 1 19960805 A 5313 1616180101 LONGERON LKHEED 1011 10113851 5265010 WP BS 328 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 728DA 193C1173 THE FUSELAGE NOSE WHEELWELL LONGERON AT LBL 22 WAS FOUND WITH EXTENSIVE CORROSION AT FS 328. DUE TO THE EXTENT OF THE C ORROSION, THE LONGERON WILL BE CUT AT FS 339 AND A NEW REPLACEMENT SECTION WILL BE SPLICED IN. 2 L 7 3 4F A23WE 1996081500031 19960815 00031 WP 1996 8 15 DLL13961834 1 19960803 A 3350 337701962 POWER SUPPLY LKHEED 1011 10113851 5265010 WP BS 827 INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 787DL 193A1126 REF OPN 78102. EMERGENCY LIGHTS WILL NOT TEST FROM POWER SUPPLY. TEST SWITCH AT STA 827L. REPLACED POWER SUPPLY, TEST S GOOD PER OPN. 2 L 7 3 4F A23WE 1996081500032 19960815 00032 WP 1996 8 15 DLL13961842 1 19960804 A 2612 FIRE WARN LKHEED 1011 10113851 5265010 WP NR 1 ENGINE MALFUNCTIONED A DALA E F A ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 786DL 69379 193A1123 NR 1 ENGINE B-LOOP FIRE WARNING PLACED ON MCO BY FLIGHT CREW DURING TAXI OUT DUE TO FLICKERING. AT 17,000 FEET, NR 1 EN GINE A-LOOP STARTED FLICKERING ACCOMPANIED BY WARNING BELL AND LIGHT. ENGINE SHUT DOWN, BOTH BOTTLES DISCHARGED AND AIR CRAFT RETURNED TO JFK. 2 L 7 3 4F A23WE 1996081500033 19960815 00033 WP 1996 8 15 DLL14961830 1 19960801 A 2822 11250804 BOOST PUMP LKHEED 1011 1011385115 5265015 WP NR 1 TANK FAILED A DALA A UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 SO 27 1739D 3043 193C1237 TANK'S NR 1 OUTBOARD FUEL BOOST PUMP CIRCUIT BREAKER TRIPPED AT FL 330 IMMEDIATELY FOLLOWED BY NR 2 ENGINE FLAMEOUT. N ORMAL RESTART FOLLOWED. 2 L 7 3 4F A23WE 1996081500034 19960815 00034 NM 1996 8 15 P5CA9600472 1 19960806 A 3244 49X17 TIRE BOEING 747 747122 1384872 NM NR 5/6 FAILED A P5CA K NONE O OTHER TO TAKEOFF 1 WP 23 850FT 41 19755 DURING INITIAL APPROACH TO JFK, ATC NOTIFIED OF RUBBER SECTIONS FOUND ON RUNWAY AT LCK. AFTER LANDING, FOUND CAP MISSIN G ON NR 6 TIRE AND NR 5 TIRE THERMALLY DEFLATED AFTER TAXI. REPLACED NR 5 AND NR 6 TIRE ASSEMBLIES PER BOEING MAINTENAN CE MANUAL 32-45-01. PERFORMED BURST INSPECTION PER BOEING MM 05-51-25. BLED NRS 5, 6, 7, 8 BRAKES PER BOEING MM 32-41- 00 PRECAUTIONARY. 2 L 7 4 4F A20WE 1996081500035 19960815 00035 WP 1996 8 15 RRXA96065 1 19960806 A 3231 47749321 RETRACT MECH DOUG DC8 DC873F 302199F WP RT MLG DOOR BROKEN A RRXA K NONE J WARNING INDICATION CL CLIMB 1 WP 15 792FT 46046 LANDING GEAR DOORS NOT LATCHED LIGHT STAYED ON AFTER GEAR RETRACTION. DID NOT GO OUT WITH UPLATCH CHECK, GEAR WAS CYCLE D, LIGHT STAYED ON. ALTERNATE GEAR DOOR LIGHTS STAYED OUT. **CORRECTIVE ACTION** CHECKED LT AND RT PROXIMITY SWITCHES , CYCLED GEAR DOORS, COULD NOT DUPLICATE. OPENED PROXIMITY SWITCH PANEL AND CHECKED EACH PROX SWITCH SEPARATELY. REMOV ED ACCESS COVERS AND FOUND BROKEN LINK ASSEMBLY ON RT MLG DOOR UPLOCK MECHANISM AND BROKEN LATCH ASSEMBLY ON LT MLG DOOR UPLOCK MECHANISM. REPLACED LINK ASSEMBLY AND REPAIRED LATCH ASSEMBLY. 2 L 7 4 4F RT 4A25 1996081500036 19960815 00036 NM 1996 8 15 SWAA960739 1 19960730 A 5320 WEB BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 89SW 22904 DURING SCHEDULED 1/2 D CHECK, FOUND CRACK INDICATION UNDER VERTICAL STRAP AT BS 178, LBL 5, WL 196. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996081500037 19960815 00037 NM 1996 8 15 SWAA960740 1 19960730 A 5315 FLOOR BEAM BOEING 737 7372H4 138448C NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 89SW 22904 DURING SCHEDULED 1/2 D CHECK, FOUND FLOORBEAM CORROSION ON FORWARD EDGE OF BEAM, BS 1016, RBL 4.5. REPAIRED PER SWA RA 1-253-1476. 2 L 7 2 4F A16WE 1996081500038 19960815 00038 NM 1996 8 15 SWAA960741 1 19960730 A 5320 WEB BOEING 737 7372H4 138448C NM BS 468 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 89SW 22904 DURING SCHEDULED 1/2 D CHECK, FOUND WEB IN FORWARD CARGO BIN CRACKED APPROX 1.75 INCH AT BS 468, RBL 23. REPAIRED PER B OEING SRM. 2 L 7 2 4F A16WE 1996081500039 19960815 00039 NM 1996 8 15 SWAA960742 1 19960730 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 89SW 22904 DURING SCHEDULED 1/2 D CHECK, FOUND STRINGER 16R CRACKED BETWEEN 500A AND 500B. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996081500040 19960815 00040 NM 1996 8 15 SWAA960743 1 19960730 A 5730 SKIN BOEING 737 7372H4 138448C NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 89SW 22904 DURING SCHEDULED 1/2 D CHECK, FOUND LT WING NR 3 OUTBOARD AUXILIARY TRACK CUTOUT CRACKED APPROXIMATELY .25 INCH. REPAIR ED PER SWA RA 1-257-167. 2 L 7 2 4F A16WE 1996081500041 19960815 00041 NM 1996 8 15 SWAA960744 1 19960727 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 87SW 22903 DURING SCHEDULED 1/2 D CHECK, FOUND RT SIDE FUSELAGE SKIN CRACKED AT BS 907. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996081500042 19960815 00042 NM 1996 8 15 SWAA960745 1 19960727 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 986.5/1006 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 87SW 22903 DURING SCHEDULED 1/2 D CHECK, FOUND AFT GALLEY LOWER LOBE STRINGER 27L CORRODED AT BS 1006, AND AT BS 986.5. REPAIRED P ER BOEING SRM. 2 L 7 2 4F A16WE 1996081500043 19960815 00043 NM 1996 8 15 SWAA960746 1 19960727 A 5315 FLOOR BEAM BOEING 737 7372H4 138448C NM BS 294 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 87SW 22903 DURING SCHEDULED 1/2 D CHECK, FOUND FLOORBEAM CORROSION AT BS 294, RBL 21, AT BS 294, RBL 39, AT BS 294, RBL 27. REPAIR ED PER SWA RA TI 253-08 AND BOEING SRM. 2 L 7 2 4F A16WE 1996081500044 19960815 00044 NM 1996 8 15 SWAA960747 1 19960727 A 5315 FLOOR BEAM BOEING 737 7372H4 138448C NM BS 986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 87SW 22903 DURING SCHEDULED 1/2 D CHECK, FOUND FLOORBEAM CORROSION AT BS 986.5 AT AFT FLANGE AND AT LBL 4. REPLACED PER BOEING SRM . 2 L 7 2 4F A16WE 1996081500045 19960815 00045 NM 1996 8 15 SWAA960748 1 19960727 A 5315 FLOOR BEAM BOEING 737 7372H4 138448C NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 87SW 22903 DURING SCHEDULED 1/2 D CHECK, FOUND FLOORBEAM CORROSION AT BS 312 ON UPPER SURFACE AND AROUND SCREW HOLES, LBL 12 TO RBL 3. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996081500046 19960815 00046 NM 1996 8 15 SWAA960749 1 19960727 A 5315 FLOOR BEAM BOEING 737 7372H4 138448C NM BS 294 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 87SW 22903 DURING SCHEDULED 1/2 D CHECK, FOUND FLOORBEAM CORROSION AT BS 294 ON UPPER SURFACE AND AROUND SCREW HOLES, RBL 1. REPLA CED T-CAP PER BOEING SRM. 2 L 7 2 4F A16WE 1996081500047 19960815 00047 NM 1996 8 15 SWAA960750 1 19960727 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 807 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 87SW 22903 DURING SCHEDULED 1/2 D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 807, AT S22L, JUST AFT AND ABOVE EXIT LIGHT. REPAIRED P ER BOEING SRM. 2 L 7 2 4F A16WE 1996081500048 19960815 00048 NM 1996 8 15 SWAA960751 1 19960727 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 790 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 60SW 21812 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 1.5 INCHES AT BS 790, AT S24L, BOTTOM SIDE OF S24L. REPAIRE D PER BOEING SRM. 2 L 7 2 4F A16WE 1996081500049 19960815 00049 NM 1996 8 15 SWAA960752 1 19960726 A 3230 BACC1873R LATCH LEVER BOEING 737 7375H4 138449D NM LANDING GEAR MALFUNCTIONED A SWAA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 525SW 26567 AFTER TAKEOFF, LANDING GEAR LEVER WOULD NOT PASS OFF POSITION WITHOUT USING OVERRIDE. FLIGHT CONTINUED AND LANDED NORMA LLY. REMOVED AND REPLACED LANDING GEAR LATCH LEVER AND PRESSURE WARNING CIRCUIT BREAKER ON P6-3 PANEL. OPS CHECKED GOOD PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996081500050 19960815 00050 NM 1996 8 15 SWAA960753 1 19960726 A 3610 332A103427 TUBE BOEING 737 7375H4 138449D NM PNEUMATIC SYST FAILED A SWAA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 514SW 25153 AT FL 350, ALTIMETER WARNING HORN SOUNDED. CREW PERFORMED RAPID DESCENT TO 16,000 FEET. LEFT PNEUMATIC DUCT PRESS INDI CATED 45 PSI AND RT, 13 PSI. MAIN OUTFLOW INDICATED FULLY CLOSED AT ALL TIMES. FLIGHT LANDED NORMALLY. REMOVED AND RE PLACED PRSOV PNEUMATIC CONTROL TUBE, AND OPS CHECKED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996081500051 19960815 00051 NM 1996 8 15 SWAA960754 1 19960805 A 5320 CLIPS BOEING 737 7372H4 138448C NM BS 380 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 380, S21L AND S22L. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996081500052 19960815 00052 NM 1996 8 15 SWAA960755 1 19960805 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 948.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED D-CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 947.5, AT S22R. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996081500053 19960815 00053 NM 1996 8 15 SWAA960756 1 19960805 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 495 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED D-CHECK, FOUND STRINGER 22R CRACKED AT BS 495. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996081500054 19960815 00054 NM 1996 8 15 SWAA960757 1 19960805 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 480 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME DENTED AT BS 480, S22L. INSTALLED DOUBLER PER BOEING SRM. 2 L 7 2 4F A16WE 1996081500055 19960815 00055 NM 1996 8 15 SWAA960758 1 19960805 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 379-384 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 379-384, BETWEN S22 AND 23R. INSTALLED DOUBLER REPAIR PER BO EING SRM. 2 L 7 2 4F A16WE 1996081500056 19960815 00056 NM 1996 8 15 SWAA960759 1 19960805 A 5320 STRAP BOEING 737 7372H4 138448C NM BS 436-455 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED D-CHECK, FOUND FUSELAGE TIE STRAP CORRODED AT NUTPLATE HOLES, BS 436-455, RBL 27. INSTALLED REPAIR PER BOEING SRM. 2 L 7 2 4F A16WE 1996081500057 19960815 00057 NM 1996 8 15 SWAA960760 1 19960805 A 5320 SHEAR TIE BOEING 737 7372H4 138448C NM BS 460 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 460 BETWEEN S19 AND 20L. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996081500058 19960815 00058 NM 1996 8 15 SWAA960761 1 19960805 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 420 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED D-CHECK, FOUND FRAME DENTED AND GOUGED AT BS 420, LBL 62. REPLACED FRAME PER BOEING SRM. 2 L 7 2 4F A16WE 1996081500059 19960815 00059 NM 1996 8 15 SWAA960762 1 19960805 A 5311 FRAMES BOEING 737 7372H4 138448C NM BS 440/492 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED D-CHECK, FOUND FORWARD CARGO FRAMES CRACKED IN UPPER FLANGE AT BS 492, RBL 36, WL 167, AT BS 440, RBL 3 5 AND AT RBL 39. INSTALLED DOUBLER REPAIRS PER BOEING SRM. 2 L 7 2 4F A16WE 1996081500060 19960815 00060 NM 1996 8 15 SWAA960763 1 19960805 A 5311 FRAMES BOEING 737 7372H4 138448C NM BS 500 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED D-CHECK, FOUND FRAMES CRACKED AT BS 500B, LBL 34-50, WL 160-169, AND AT BS 500, LBL 35-38, WL 161-168. INSTALLED DOUBLER REPAIRS PER BOEING SRM. 2 L 7 2 4F A16WE 1996081500061 19960815 00061 NM 1996 8 15 SWAA960764 1 19960805 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 402.5 BETWEEN S24 AND 25R AND AT BS 357 AND BS 358, BETWEEN S 24 AND 25R. INSTALLED DOUBLER REPAIRS PER BOEING SRM. 2 L 7 2 4F A16WE 1996081500062 19960815 00062 NM 1996 8 15 SWAA960765 1 19960805 A 5320 CHORD BOEING 737 7372H4 138448C NM BS 338/339 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM INBOARD CHORD CRACKED AT BS 638 AND BS 639, LBL 63, WL 208. INSTALLED REPAI R PER BOEING SRM. 2 L 7 2 4F A16WE 1996081500063 19960815 00063 NM 1996 8 15 SWAA960766 1 19960805 A 5320 WEB BOEING 737 7372H4 138448C NM BS 1138 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED D-CHECK, FOUND CRACKED WEB AT BS 1138, S5L. INSTALLED REPAIR PER BOEING SRM. 2 L 7 2 4F A16WE 1996081500064 19960815 00064 NM 1996 8 15 SWAA960767 1 19960805 A 5241 FRAME BOEING 737 7372H4 138448C NM AFT GALLEY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED D-CHECK, FOUND FOWARD GALLEY DOOR AFT FRAME CRACKED ON FRAME LOWER STOP PIN FITTING AND AT NR 4 STOP FI TTING. INSTALLED REPAIR PER BOEING SRM. 2 L 7 2 4F A16WE 1996081500065 19960815 00065 NM 1996 8 15 UPS96220810 1 19960806 A 2613 CONNECTOR BOEING 727 72731C 1384011 NM TAY AFT STAIRS WET A IPXA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 925UP 19230 ON CLIMB-OUT FROM PHL, NR 1 ENGINE STRUT OVERHEAT LIGHT BEGAN FLICKERING. LIGHT BECAME STEADY UPON LEVEL OFF AT FL 280. ACCOMPLISHED ENGINE STRUT OVERHEAT QF CHECKLIST. LIGHT WENT OUT WHEN NR 1 THROTTLE RETARDED TO NEAR IDLE. AFTER ABOU T 5 MINS, LIGHT RE-ILLUMINATED. ACCOMPLISHED REMAINDER OF CHECKLIST AND SHUTDOWN NR 1 ENGINE IAW CHECKLIST. FOUND WATE R IN PLUG, CLEANED. PUT PLUG IN AFT STAIRWELL BACK TOGETHER PER M/M 20-11-13, SEALED PLUG, NO LEAKS NOTED ON ENGINE RUN -UP, NO FLICKERING OF OVERHEAT LIGHT FOR NR 1 ENGINE. OK FOR SERVICE. 2 L 7 3 4F A3WE 1996081500066 19960815 00066 NM 1996 8 15 UPS96220816 1 19960727 A 5220 65210818 CASTING BOEING 727 727180C 138406G NM EMER EXIT DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE: SI. CORROSION RT FORWARD OVERWING EXIT HANDLE PRESSURE SEAL CASTING. REMOVED CORRODED CASTING, INSTA LLED NEW CASTING. ALL WORK DONE IAW SRM 51-30-2, SRM 52-00-2, AND OHM 52-26-01. 2 L 7 3 4F A3WE 1996081500067 19960815 00067 NM 1996 8 15 UPS96220817 1 19960731 A 5531 177CRES150170K MIDSPAR BOEING 727 727180C 138406G NM VERT STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE: SI. CORROSION RT FIN MID-SPAR HAS FRETTING CORROSION AT ACCESS PANEL 9602 FIN STA 226.7 FIN W.L. 168. 39 AND BS 1495.75. CORROSION REMOVAL OUT OF LIMITS, REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR PARTS PER TRAM CO E.W.O. 96-2402. 2 L 7 3 4F A3WE 1996081500068 19960815 00068 NM 1996 8 15 UPS96220818 1 19960803 A 5330 SKIN BOEING 727 727180C 138406G NM BS 310 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE: SI. CORROSION UNDER STIFFENER AT STA 310 LBL 12 TO RBL 12 WL 181 AREA MARKED. REMOVED CORROSION FROM STIFFENER AND FOUND CORROSION UNDER DOUBLER AND SKIN, ALL OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED STIFFENE R, DOUBLER AND SKIN SECTION AT STA 310-294, WL 181 RBL 12 LBL 12 IAW SRM'S 51-40-2, 51-10-2, 51-20-151, 51-30-2. 2 L 7 3 4F A3WE 1996081500069 19960815 00069 NM 1996 8 15 UPS96220819 1 19960803 A 5320 654939816 BAR NET CASTING BOEING 727 727180C 138406G NM BS 362 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE: SI. WHILE WORKING NRC NR 577416, FOUND CORROSION IN BARRIER NET CASTING WELL NEXT TO DRAIN HOLE STA 3 62 RBL 61 WL 207. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 51-10-6. REMOVED AND REPLACED BARRIER NET CA STING STA 362 RBL 61 WL 207 IAW SRM'S 51-30-5, 51-30-2. 2 L 7 3 4F A3WE 1996081500070 19960815 00070 NM 1996 8 15 UPS96520811 1 19960806 A 5330 SKIN BOEING 757 75724APF 1384969 NM BS 1681/1701 PUNCTURED A IPXA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 427UP 25458 INSPECTION TYPE-N/A, ON T/O ROLL HEARD SOUND, LIKE A CONTAINER WAS ROLLING TOWARD REAR OF ACFT. REJECTED T/O AND RETURN ED TO RAMP. UPON MAINT INSPECTION FOUND 7,000 LB BALLEST PALLET IN POSS 15 AND HOLE IN ACFT SKIN APROX 7 BY 24. RT AND LT STA 1681 AND 1701 HOLE PUNCTURED IN FUSELAGE SKIN AT STA 1701. ACCOMPLISHED AIRWORTHY REPAIR TO LT AND RT FUSELAGE FRAMES AT STA 1681 AND 1701. REPLACED FUSELAGE SKIN FROM STA 1620 TO STA 1720 RT SIDE PER SRM 51-10-01 AND STANDARD PRA CTICES. 2 L 7 2 4F RT A2NM 1996081500071 19960815 00071 NM 1996 8 15 UPS96520826 1 19960806 A 5400 FUSE PIN BOEING 757 75724APF 1384969 NM NR 2 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 427UP 25458 OUTBOARD FUSELAGE ON NR 2 ENGINE PYLON CRACKED. INBOARD AND OUTBOARD FUSELAGE PINS REPLACED. COMPLIED WITH EO B757-544 0-0431-1 APPENDIX F, COMPLIED T/C 5001 (PW) REMOVAL AND INSTALLATION OF NR 2 (RT) ENGINE. 2 L 7 2 4F RT A2NM 1996081500072 19960815 00072 WP 1996 8 15 UPS96820812 1 19960723 A 5320 END FITTING DOUG DC8 DC871F 302199D WP NR 2 ALT TANK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE: C. STRINGER END FITTING CRACKED ON LOWER AFT STRINGER INSIDE NR 2 ALT TANK AT STA 74. REMOVED CRACKE D FITTING, INSTALLED NEW FITTING IAW DC8 SRM 51-1-21D. 2 L 7 4 4F RT 4A25 1996081500101 19960815 00101 SO 1996 8 15 96ZZZX3921 1 19960716 A 2750 95504000 BRACKET PIPER PA34 PA34200T 7103406 SO FLAP LEVER CRACKED A S APCA K NONE O OTHER IN INSP/MAINT 1 NM 01 4490F 6628 347670339 INSPECTION FOUND FLAP LEVER BRACKET IS CRACKED AT BOTH FORWARD BEND RADIUS. 1 L 7 2 3O A7SO 1996081500103 19960815 00103 SO 1996 8 15 96ZZZX3923 2 19960712 A 8530 646020 ELBOW CESSNA 414 414A 2075907 CE CONT O520 TSIO520NB 17040 SO ENG INDUCTION BLOWN OUT A A BMUA O OTHER O OTHER AP APPROACH 1 NM 09 6624C FT082594 414A0034 503082 AIRCRAFT RETURNED FROM FLIGHT ON SHORT FINAL. ENGINE RPM COULD NOT BE REDUCED BELOW 1,400 RPM. SECURED ENGINE WITH MIX TURE TO PREVENT ASYMMETRIC THRUST CONDITION. UPON INSPECTION BY MECHANIC, FOUND BLOWN OUT INDUCTION ELBOW. SECOND OCCU RRENCE IN 6 MONTHS. SUBMITTER RECOMMENDS REVIEW OF MANUFACTURER'S MATERIALS AND ONE-TIME INSPECTION OF ALL INSTALLED HO SES FOR SPLITTING AT SPRING JOINTS. 1 L 7 2 3O 3 O A7CE E8CE 1996081500111 19960815 00111 SO 1996 8 15 96ZZZX3931 2 19960713 A 8520 CRANKCASE CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO BASE FLANGE CRACKED A BAJA K NONE K FLUID LOSS IN INSP/MAINT 1 AL 01 6878L 1114 402C0602 248279R PILOT REPORTED AN OIL LEAK CLIMBING FROM THE RIGHT SIDE OF THE LEFT ENGINE. AFTER INSPECTING THIS AREA OF THE ENGINE, T HE ALTERNATOR BASE GASKET APPEARED TO BE RIPPED AND A PORTION OF IT STICKING OUT OF THE FLANGE AREA. UPON REMOVAL OF TH E ALTERNATOR AND BASE GASKET, DISCOVERED THERE WAS A CRACK IN THE CRANKCASE FROM THE ALTERNATOR BASE FLANGE TRAVELING AF T TOWARDS NR 5 CYLINDER. 1 L 7 2 3O 3 O A7CE E8CE 1996081500124 19960815 00124 NM 1996 8 15 9617092284 1 19960806 A 3244 657276187 TIRE BOEING 727 727251 138408H NM NR 2 FAILED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 284US 21323 DURING WALK AROUND,FOUND NUMBER TWO TIRE BANDAGE RETREAD COMING APART. REPLACED NUMBER TWO TIRE AND INSPECTED FLAPS AND GEAR DOORS FOR DAMAGE. 2 L 7 3 4F A3WE 1996081500125 19960815 00125 NM 1996 8 15 9617102202 1 19960807 A 3244 TIRE BOEING 727 727251 138408H NM NR 3 SEPARATED A NWAA K NONE D INFLIGHT SEPARATION TO TAKEOFF 1 GL 01 202US 22155 DURING TAKEOFF, NUMBER THREE TIRE CAP SEPARATED FROM TIRE. REPLACED NUMBER THREE TIRE AND INSPECTED FLAPS AND GEAR DOOR S FOR DAMAGE. 2 L 7 3 4F A3WE 1996081500126 19960815 00126 EU 1996 8 15 9617113218 1 19960807 A 3260 848401 SENSOR AIRBUS 320 A320211 3930320 EU MLG MALFUNCTIONED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 318US 206 DURING APPROACH AFTER PLACING THE LANDING GEAR HANDLE IN THE DOWN POSITION, THE LANDING GEAR DOORS INDICATED PARTIALLY O PEN. CYCLED LANDING GEAR HANDLE AND ALL INDICATIONS NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED TH E MAIN LANDING GEAR PROXIMITY SENSORS 32GA AND 33GA. LUBED MAIN LANDING GEAR AND NOSE LANDING GEAR STRUTS PRECAUTIONARY , OPS CHECK OK. 2 L 7 2 4F RT A28NM 1996081500127 19960815 00127 EU 1996 8 15 9617123218 1 19960807 A 3260 PROX SENSOR AIRBUS 320 A320211 3930320 EU RT MLG DOOR MALFUNCTIONED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 318US 206 DURING APPROACH AFTER EXTENDING THE LANDING GEAR, RECEIVED 'L/G NOT DOWNLOCKED' MESSAGE WITH NOSE LANDING GEAR INDICATIN G LOCKED AND THE MAIN LANDING GEAR INDICATING UNLOCKED. CYCLED THE LANDING GEAR HANDLE AND ALL INDICATION'S NORMAL. AI RCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT MAIN LANDING GEAR DOOR CLOSED PROXIMITY SENSOR (28GA), O PS CHECK OK. 2 L 7 2 4F RT A28NM 1996081500128 19960815 00128 NE 1996 8 15 9617136603 2 19960807 A 7230 COMPRESSOR BOEING 747 747151 1384891 NM PWA JT9 JT9D7A 52054 NE NR 4 ENGINE STALLED A NWAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DE DESCENT 1 GL 01 603US 19780 62438 AT TOP OF DESCENT, THE NR 4 ENGINE COMPRESSOR STALLED. THE ENGINE WAS THEN SHUTDOWN AS EGT REACHED 950 DEGREES AND N2 W ENT TO 105 PERCENT. CREW FOLLOWED COCKPIT OPERATING PROCEDURE AND MADE THREE ENGINE LANDING WITHOUT FURTHER INCIDENT. T HE A/C WILL BE FERRY TO NRT FOR NR 4 ENGINE CHANGE. 2 L 7 4 4F 4 F A20WE E20EA 1996081500129 19960815 00129 EU 1996 8 15 9617143237 1 19960807 A 2750 RETRACT MECH AIRBUS 320 A320211 3930320 EU TE FLAPS MALFUNCTIONED A A NWAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 01 337NW 358 DURING CLIMBOUT, THE FLAPS WOULD NOT RETRACT. RECEIVED 'F/CTL FLAPS LOCKED' MESSAGE WITH THE WING TIP BRAKE ON. AIRCRA FT DIVERTED TO LAX AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING REVEALED NO DISCREPANCIES. 2 L 7 2 4F RT A28NM 1996081500131 19960815 00131 NM 1996 8 15 96FDEA01332 1 19960808 A 5311 66118081 FRAME SPLICE BOEING 727 727233 138408A NM BS 520 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 219FE 21102 NR0041 & 002 DENT IN FRAME SPLICE BS 520 STR 25L. ****S/D***** REMOVED FRAME CAP FROM BS 520 STR 25L FABRICATE D & INSTALLED FRAME CAP IAW FEDEX SRM 51-20-1 ALODINED & PRIMED. 2 L 7 3 4F RT A3WE 1996081500132 19960815 00132 NM 1996 8 15 96FDEA01333 1 19960808 A 5315 65208379 FLOOR BEAM BOEING 727 727233 138408A NM BS 1110 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 219FE 21102 NR0466 & 003 CORROSION C53-224-04 ON FLOOR BEAM AROUND CLIP NOT HOLE BS 1110 LBL 16 WL 207.9 *****S/D**** REM OVED DAMAGED AREA & FABRICATED REPAIR ANGLES (2 EA) & REPAIR FILLER, INSTALLED & TREATED ON FLOOR BEAM AT BS 1110 LBL 16 WL 207.9 IAW FEDEX SRM 53-10-8. 2 L 7 3 4F RT A3WE 1996081500133 19960815 00133 NM 1996 8 15 96FDEA01334 1 19960808 A 5543 65727372 SKIN BOEING 727 72722 1384002 NM RUDDER TAB DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 NR0577 AND 006, UPPER RUDDER TAB LOWER SURFACE RT AND LT HAS AREAS OF DELAMINATION. *S/D* REPAIRED UPPER RUDDER TAB LO WER SURFACE RT AND LT PER FEDEX SRM 51-40-6. 2 L 7 3 4F A3WE 1996081500134 19960815 00134 NM 1996 8 15 96FDEA01335 1 19960808 A 5315 654027612 FLOOR BEAM BOEING 727 72722 1384002 NM BS 1110 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 NR0560 AND 007, CORROSION (C53-224-01, -3) ON BS 1110 BEAM RBL 26 TO 45 WL 208.1. *S/D* CUT OUT CORROSION AND INSTALLE D REPAIR ON BS 1110 BEAM RBL 26 TO 45 WL 208.1 IAW FEDEX SRM 53-10-8. 2 L 7 3 4F A3WE 1996081500135 19960815 00135 NM 1996 8 15 96FDEA01336 1 19960808 A 5320 WEB BOEING 727 72722 1384002 NM BS 227.8 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 24981 8590 19145 NR0633 AND 008, CORROSION (C53-221-01) ON WEB AND OUTBOARD CF FRAME STA 227.8 RBL 42 WL 211 TO 233. *S/D* REPAIRED WEB AT STA 227 TO 8, RBL 42, WL 227. 2 L 7 3 4F A3WE 1996081500136 19960815 00136 EU 1996 8 15 96FDEA01337 1 19960808 A 5270 SWITCH AIRBUS 310 A310222 3930315 EU RT CABIN DOOR FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 422FE 346 CLIMBING THROUGH 8,000 FEET, RIGHT CABIN DOOR INDICATED UNLOCKED. REMAINED ON UNTIL LANDING ROLL OUT. REPLACED DOOR WA RNING MICROSWITCHES 8WS AND 42WS, ADJUSTED AND FUNCTIONAL TEST ON GROUND SATISFACTORY. 2 L 7 2 4F RT A35EU 1996081500137 19960815 00137 NM 1996 8 15 96FDEA01338 1 19960807 A 5320 WINDOW POST BOEING 727 72722C 138400F NM NR 1 WINDOW CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 CRACK AT F/O'S NR 1 WINDOW O/B POST AT UPPER CORNER. CRACK LENGTH VERIFIED BY NDT HFEC, CRACK WAS STOP DRILLED AND VERI FIED BY NDT HFEC REPAIR DOUBLER INSTALLED PER SRM 53-30-3. 2 L 7 3 4F A3WE 1996081500138 19960815 00138 NM 1996 8 15 96FDEA01339 1 19960808 A 2751 POS TRANSMITTER BOEING 727 727277 138408S NM TE FLAPS MALFUNCTIONED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 246FE 22068 SPLIT FLAP ON T/O, ON RETRACT TO 5 OUTBOARD FLAPS STOPPED AT 15 INBOARD FLAPS TO 5. ACCOMP EMERGENCY PROCED FLAPS EXTEN DED NORMAL TO 30 DEGREE AND RECOVERED AT IND. F/F O/B FLAP POS IND. RAN FLAPS, FOUND O/B NEEDLES SPLIT AND OUT OF BAND AT POSITION EO DEGREE. ADJ RT AND LT O/B FLAP POS TRANSMITTERS OPS CHECKS NORMAL. ALL WORK DONE AS PER MM 27-52-13. 2 L 7 3 4F RT A3WE 1996081500139 19960815 00139 NM 1996 8 15 96FDEA01340 1 19960809 A 5311 6515528 FRAME BOEING 727 727233 138408A NM BS 500 DENTS A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 219FE 21102 NR0470 & 004 DENT IN FRAME AT BS00 BETWEEN STR 15-16R. ****S/D***** REPAIRED DAMAGED FRAME AT BS 500 STR 15-16R AS PER FEDEX SRM 51-40-3. 2 L 7 3 4F RT A3WE 1996081500140 19960815 00140 NM 1996 8 15 96FDEA01341 1 19960806 A 5210 6516477 GATE BOEING 727 7272D4 138407U NM FWD ENTRY DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 NR0486 & 010 WHILE WORKING NR0400 FOUND FWD ENTRY DOOR UPR GATE TO BE CORRODED SEVERELY. ****S/D**** R/R FWD ENTR Y DOOR UPPER GATE. ALL WORK DONE IAW FEDEX SRM 51-30-2. 2 L 7 3 4F A3WE 1996081500141 19960815 00141 WP 1996 8 15 ABXA9600608 1 19960806 A 3350 60030431 POWER SUPPLY DOUG DC9 DC933F 302207A WP CABIN DEFECTIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 931AX 47384 EMERGENCY LIGHTS WILL NOT SHUT OFF. REPLACED BATTERY POWER SUPPLY IAW DC-9 MM 33-50-0, OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996081500142 19960815 00142 WP 1996 8 15 ABXA9600609 1 19960807 A 3260 7000010101 DNLOCK SWITCH DOUG DC9 DC932 3022066 WP RT MLG DEFECTIVE A ABXA K NONE N FALSE WARNING CL CLIMB 1 GL 23 980AX 47176 AFTER TAKEOFF, LANDING GEAR WAS RETRACTED AND RIGHT GEAR UNSAFE LIGHT REMAINED ON. GEAR WAS RECYCLED, LIGHT STAYED ON. UPLATCH CHECK WAS ACCOMPLISHED, GEAR UNSAFE LIGHT WENT OUT. REPLACED RIGHT MAIN GEAR DOWN LOCK SWITCH PER DC-9 SUPP MM 32-60-01, OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996081500143 19960815 00143 WP 1996 8 15 ARWA9608001 1 19960807 A 5230 SKIN DOUG DC8 DC862 3021970 WP BS 480 PUNCTURED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 802BN 45909 WHILE LOADING AIRCRAFT, CARGO PERSONNEL PUNCTURED SKIN APPROXIMATELY 2 FORWARD OF BELLY DOOR. REPAIRED 2 TO 3 HOLE AT F USELAGE STA 480, LONGERON 29/30R IN ACCORDANCE WITH DER DRAWING ARW960173-0001. 2 L 7 4 4F 4A25 1996081500144 19960815 00144 WP 1996 8 15 CALA9601139 1 19960808 A 2420 CIRCUIT BREAKER DOUG DC9 DC982 3022082 WP COCKPIT PNL TRIPPED A CALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 09 18835 49439 WHILE OPERATING THE APU ON TAKEOFF WITH THE LT GENERATOR PLACARDED INOPERATIVE, THE APU GENERATOR WAS LOST AND HAD NO CR OSSTIE. THE APU GENERATOR COULD NOT BE RESET AND THE AIRCRAFT WAS RETURNED TO LAS. MAINTENANCE FOUND THE APU CONTROL C IRCUIT BREAKER POPPED. THE CIRCUIT BREAKER WAS RESET AND OPERATION OF THE APU GENERATOR AND AC CROSSTIE CHECKED GOOD. 2 L 7 2 4F A6WE 1996081500145 19960815 00145 WP 1996 8 15 CALA9601140 1 19960808 A 2910 7936907665 HYD LINE DOUG DC9 DC982 3022082 WP TAIL COMPT LEAKING A CALA O OTHER J K WARNING INDICATION FLUID LOSS CL CLIMB 1 SW 09 14814 49112 THE RT HYDRAULIC SYSTEM QUANTITY BEGAN TO DECREASE DURING CLIMB. THE R/H HYDRAULIC QUANTITY CONTINUED TO DROP SLOWLY WH ILE AT CRUISE. THE TRANSFER PUMP, RT HYDRAULIC PUMP AND AUX PUMP WERE TURNED OFF. THE PUMPS WERE RETURNED TO NORMAL ON APPROACH WITH THE RT HYDRAULIC QUANTITY AT 2 GALLONS. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A PINHO LE LEAK IN RT HYDRAULIC SYSTEM PRESSURE LINE LOCATED IN TAIL COMPARTMENT. THE HYDRAULIC LINE WAS REMOVED AND REPLACED. THE RT HYDRAULIC SYSTEM WAS SERVICED TO FULL AND LEAK CHECKS WERE GOOD. 2 L 7 2 4F A6WE 1996081500146 19960815 00146 WP 1996 8 15 CALA9601141 1 19960725 A 5320 DOOR JAMB DOUG DC9 DC982 3022082 WP MID BAG BIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15841 49581 INSPECTION FOUND MID BAGGAGE BIN DOOR JAMB PAN LOWER SECTION CORRODED AROUND FASTENERS. THE LOWER DOOR JAMB WAS REPAIRE D IAW SRM 53-05-63. 2 L 7 2 4F A6WE 1996081500147 19960815 00147 WP 1996 8 15 CALA9601142 1 19960719 A 5321 FLOORBOARD DOUG DC9 DC982 3022082 WP COCKPIT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15841 49581 INSPECTION FOUND COCKPIT FLOORBOARD AT FIRST OFFICER'S SEAT TRACK CORRODED. THE FLOORBOARD WAS REPLACED IAW SRM 51-10-0 2. 2 L 7 2 4F A6WE 1996081500148 19960815 00148 WP 1996 8 15 CALA9601143 1 19960714 A 5530 ATTACH ANGLE DOUG DC9 DC982 3022082 WP DORSAL FIN CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 98876 49444 INSPECTION FOUND RT DORSAL FIN ATTACH ANGLE CRACKED. THE ANGLE WAS REPAIRED IAW EA 5340-01012. 2 L 7 2 4F A6WE 1996081500149 19960815 00149 WP 1996 8 15 CALA9601144 1 19960730 A 5511 5918000530N SPAR DOUG DC9 DC932 3022066 WP LT HORIZ STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND CORROSION ON UPPER SPAR CAP OF LT HORIZONTAL STABILIZER FORWARD SIDE OF REAR SPAR AT STA XHS 95. THE C ORRODED SECTION OF SPAR CAP WAS CUT OUT AND A NEW SECTION WAS SPLICED IN IAW SRM 55-02, PAGES 85 TO 87. 2 L 7 2 4F A6WE 1996081500150 19960815 00150 WP 1996 8 15 MWEA96323 1 19960731 A 5412 FIREWALL DOUG DC9 DC932 3022066 WP RT PYLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, RT PYLON WAS FOUND TO HAVE SMALL CRACK IN LWR FWD CORNER OF ANGLED FIREWALL INBD OF AFT ENGINE ISOLATOR. FABRICATED A REPAIR AND INSTALLED IAW SRM 51-20-3 AND 54-01, FIG 2 SHEET 4. 2 L 7 2 4F A6WE 1996081500151 19960815 00151 WP 1996 8 15 MWEA96324 1 19960731 A 5400 ANGLE DOUG DC9 DC932 3022066 WP BS 1059 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, RT PYLON FRAME UPPER FLANGE FOUND CRACKED AT STA 1059 OUTBD OF FIREWALL. REPLACED ANGLE IAW SRM 51-302. 2 L 7 2 4F A6WE 1996081500152 19960815 00152 WP 1996 8 15 MWEA96325 1 19960731 A 5711 SPAR DOUG DC9 DC932 3022066 WP WS 513-551 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, LT WING AFT SPAR UPPER AND LOWER CAPS WERE CORRODED FROM STA XRS 513 TO XRS 551. REPAIRED THE SPAR AND CAPS PER DAC TELEX SVC-MSP-0411/PDG DATED 30 MAY, 96 AND SRM 57-09, FIG 24. 2 L 7 2 4F A6WE 1996081500153 19960815 00153 WP 1996 8 15 MWEA96326 1 19960731 A 5230 PAN DOUG DC9 DC932 3022066 WP FWD CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, FWD CARGO DOOR WAS FOUND TO HAVE SMALL CRACK IN AFT OUTER PAN COMING FROM A BN FASTENER HOLE. INSTALLED A REPAIR IAW SRM 52-08, FIG 8 SHEET 1. 2 L 7 2 4F A6WE 1996081500154 19960815 00154 WP 1996 8 15 MWEA96327 1 19960731 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 991 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, AFT FUS SKIN CRACKED AT LT PYLON UPPER ATTACH ANGLE, 1.5 INCH AT STA 991 UNDER LONGERON 15L. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW 53-04, PG 279 FIG 46. 2 L 7 2 4F A6WE 1996081500155 19960815 00155 WP 1996 8 15 MWEA96328 1 19960731 A 5753 HINGE FITTING DOUG DC9 DC932 3022066 WP LT TE FLAP CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, LT FLAP MOUNTED INBD HINGE FITTING WAS FOUND CRACKED AT ACTUATOR INBD LUG. INSTALLED A NEW HINGE FITTIN G IAW OH MANUAL 27-50-1. 2 L 7 2 4F A6WE 1996081500156 19960815 00156 WP 1996 8 15 MWEA96329 1 19960731 A 5753 HINGE FITTING DOUG DC9 DC932 3022066 WP RT TE FLAP CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, RT FLAP MOUNTED INBD HINGE FITTING WAS FOUND CRACKED AT ACTUATOR INBD LUG. INSTALLED NEW HINGE FITTING IAW LH MANUAL 27-50-1. 2 L 7 2 4F A6WE 1996081500157 19960815 00157 WP 1996 8 15 MWEA96330 1 19960731 A 5315 FLOOR BEAM DOUG DC9 DC932 3022066 WP BS 398 GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, FWD CARGO COMPT CEILING LWR FLANGES OF CABIN FLOOR BEAM WERE GOUGED FROM CARGO DOOR HITTING AT STA 389 A ND 408. INSTALLED REPAIR IAW SRM 53-05, FIG 86. 2 L 7 2 4F A6WE 1996081500158 19960815 00158 WP 1996 8 15 MWEA96331 1 19960731 A 5320 FITTING DOUG DC9 DC932 3022066 WP VENT DOOR JAMB CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, VENTRAL DOOR JAMB LT SIDE FITTING 24 INCHES ABOVE FLOOR LINES WAS FOUND CRACKED. FABRICATED NEW FITTING IAW DAC DRAWING 3917624 AND INSTALLED IAW SRM 51-30. 2 L 7 2 4F A6WE 1996081500159 19960815 00159 WP 1996 8 15 MWEA96332 1 19960731 A 5320 BLKHD ANGLES DOUG DC9 DC932 3022066 WP BS 996 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, LT SIDE NR 2, 3 AND 4 T-ANGLES WERE FOUND CRACKED WHERE AFT PRESSURE BULKHEAD MEETS FUS SKIN AT STA 996. FABRICATED AND INSTALLED NEW ANGLES IAW DAC DRAWING J060110. 2 L 7 2 4F A6WE 1996081500160 19960815 00160 WP 1996 8 15 MWEA96333 1 19960731 A 5315 FLOOR BEAM DOUG DC9 DC932 3022066 WP BS 398 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, CABIN FLOOR BEAM CAP AT STA 980 HAD CORROSION ON TOP OF BEAM; FLOOR BEAM UPPER CAP AT STA 996 HAD CORROS ION ON TOP AND BOTTOM OF BEAM. REPAIRED AREAS IAW SRM 53-01, 53-05, FIG 20A PG 31. 2 L 7 2 4F A6WE 1996081500161 19960815 00161 WP 1996 8 15 MWEA96334 1 19960731 A 5312 BLKHD ANGLES DOUG DC9 DC932 3022066 WP AFT FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, RT SIDE T-ANGLES WERE FOUND CRACKED AT NR 1, 2, 3 AND 4 POSITIONS AT STA 996 WHERE RT FUS SKIN MEETS AFT PRESSURE BULKHEAD. FABRICATED NEW ANGLES AND INSTALLED IAW DAC DRAWING J060110. 2 L 7 2 4F A6WE 1996081500162 19960815 00162 WP 1996 8 15 MWEA96335 1 19960731 A 5320 DOOR JAMB DOUG DC9 DC932 3022066 WP VENTRAL DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, VENTRAL DOOR JAMB WEB AT RT UPPER CORNER WAS FOUND CRACKED. FABRICATED REPAIR PARTS IAW SRM 53-05 AND I NSTALLED IAW SRM 53-05, PG 63. 2 L 7 2 4F A6WE 1996081500163 19960815 00163 WP 1996 8 15 MWEA96336 1 19960731 A 5315 FLOOR BEAM DOUG DC9 DC932 3022066 WP BS 980-996 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, TWO CABIN FLOOR BEAMS WERE FOUND WITH CORROSION ON BEAM FROM CENTERLINE TO RT SIDE OF FUSELAGE AT STA 98 0 AND 996. INSTALLED REPAIR ANGLE AND FILLERS IAW SRM 53-04, FIG 20A. 2 L 7 2 4F A6WE 1996081500164 19960815 00164 WP 1996 8 15 MWEA96337 1 19960731 A 5314 KEEL BEAM DOUG DC9 DC932 3022066 WP RT MLG WW CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, CORROSION FOUND ON RT MLG DOOR ATTACH BEAM AND ON A KEEL BEAM END FITTING. INSTALLED A NEW ATTACHING BE AM AND END FITTING IAW SRM 51-30-5. 2 L 7 2 4F A6WE 1996081500165 19960815 00165 WP 1996 8 15 MWEA96338 1 19960731 A 5230 5910157 PAN DOUG DC9 DC932 3022066 WP AFT CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, AFT CARGO DOOR WAS FOUND WITH CRACK IN DOOR PAN AT DOOR STOP BEAM NR 1 FWD SIDE OF DOOR. FABRICATED A N EW PAN SPLICE AND INSTALLED IAW DAC DRAWING 5934142. 2 L 7 2 4F A6WE 1996081500166 19960815 00166 WP 1996 8 15 MWEA96339 1 19960731 A 5230 3914025 CLIP DOUG DC9 DC932 3022066 WP AFT CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, AFT CARGO DOOR NR 4 BEAM END WAS FOUND CRACKED ON AFT END OF DOOR. REPLACED BEAM END CLIP WITH A NEW ON E IAW SRM 52-01. 2 L 7 2 4F A6WE 1996081500167 19960815 00167 WP 1996 8 15 MWEA96340 1 19960731 A 5730 SKIN DOUG DC9 DC932 3022066 WP WS 199-211 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CK, CORROSION FOUND ON LT FLAP INSIDE SURFACE OF UPPER AND LOWER SKINS STA XFLS 199-211 AND ADJOINING RIB AT ST A XFLS 201. ALSO, ON LDG EDGE NOSE RIB SUPPORT AT STA XFLS201. REMOVED CORROSION, INSTALLED NEW RIBS IAW SRM 57-01 PG 1. 2 L 7 2 4F A6WE 1996081500168 19960815 00168 WP 1996 8 15 MWEA96341 1 19960731 A 5753 WEB DOUG DC9 DC932 3022066 WP LT TE FLAP CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, FOUND CORROSION ON INBD AREA OF FLAP INSIDE ON AFT SPAR WEB. REPAIRED AFT SPAR WEB IAW SRM 57-01, FIG 2 . 2 L 7 2 4F A6WE 1996081500169 19960815 00169 WP 1996 8 15 MWEA96342 1 19960731 A 5753 NOSE RIB DOUG DC9 DC932 3022066 WP RT TE FLAP CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, RT FLAP LDG EDGE NOSE CAP RIBS WERE FOUND CORRODED TO EXCESS AT STA XFLS198 AND XFLS210. INSTALLED TWO NEW NOSE CAP RIBS IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1996081500170 19960815 00170 WP 1996 8 15 MWEA96343 1 19960731 A 5753 SKIN DOUG DC9 DC932 3022066 WP LT TE FLAP CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, NUMEROUS AREAS OF LT FLAP HAD CORROSION. REPLACED SKIN IN THESE AREAS IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1996081500171 19960815 00171 WP 1996 8 15 MWEA96344 1 19960731 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 737 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, LT MAIN GEAR INNER DOOR PAN INTERCOSTAL 'Z' ATTACH ANGLE WAS CRACKED AT STA 737. INSTALLED A NEW INNER DOOR PAN INTERCOSTAL IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1996081500172 19960815 00172 WP 1996 8 15 MWEA96345 1 19960731 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 180 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, A-FRAME WAS FOUND CRACKED ABOVE PAX DOOR INTERCOSTAL AT STA 180 AT LONG 6L. FABRICATED AND INSTALLED RE PAIR PARTS IAW SRM 53-03, FIG 36. HEAT TREATED 7075-0 PARTS TO 7075-T6 IAW SRM 53-03 FIG 36. 2 L 7 2 4F A6WE 1996081500173 19960815 00173 WP 1996 8 15 MWEA96346 1 19960731 A 5313 2777922 LONGERON DOUG DC9 DC932 3022066 WP BS 200 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, LONGERON 4L FOUND CRACKED IN FRAME AT STA 200. SPLICED IN NEW SECTION OF LONGERON IAW SRM 53-02 FIG 2. 2 L 7 2 4F A6WE 1996081500174 19960815 00174 WP 1996 8 15 MWEA96347 1 19960731 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 1076 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, AFT ACCESSORY COMPT FRAME WAS FOUND CRACKED AT STA 1076, LONG 3R. FABRICATED FRAME IAW SRM 53-01, PAGE 1. HEAT TREATED IAW SRM 51-10-2A AND INSTALLED IAW SRM 53-03, PG 131. 2 L 7 2 4F A6WE 1996081500175 19960815 00175 WP 1996 8 15 MWEA96348 1 19960731 A 5754 RIBS DOUG DC9 DC932 3022066 WP NR 1 LE FLAP CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, LT WING HAD TWO LEADING EDGE RIBS FOUND CRACKED AT NR 1 SLAT INBD AREA. REPLACED RIBS IAW SRM 57-01, PG 1, 2. 2 L 7 2 4F A6WE 1996081500176 19960815 00176 WP 1996 8 15 MWEA96349 1 19960731 A 5754 9955843 FITTINGS DOUG DC9 DC932 3022066 WP NR 4 LE FLAP CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, NR 4 SLAT INBD FITTING FOUND WITH TWO PREVIOUSLY CORRODED SPOT FACES WHICH ARE PRESENTLY RECORRODED. RE PAIRED FITTINGS IAW DAC TELEX SVC-MSP-0365/PDG DATED 17 MAY 96. 2 L 7 2 4F A6WE 1996081500177 19960815 00177 WP 1996 8 15 MWEA96350 1 19960731 A 5754 9955834 FITTING DOUG DC9 DC932 3022066 WP RT LE FLAP OVERSIZE HOLE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, RT NR 2 SLAT CENTER FITTING FOUND WITH ENLARGED HOLE DIAMETER FOR THE ECCENTRIC ATTACH BOLT. REPAIRED O VERSIZED HOLE IAW DAC TELEX SVC-MSP-0451/PPS DATED 11 JUNE 96. 2 L 7 2 4F A6WE 1996081500178 19960815 00178 WP 1996 8 15 MWEA96351 1 19960731 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 813 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, RT FUSELAGE SIDE SKIN FOUND CHAFED AND CORRODED FROM WING FILLET PANEL AT STA 813 AND LONG 26R. REPAIRE D DAMAGED AREA IAW DAC TELEX SVC-MSP-0335/DLP DATED 6 MAY 96. 2 L 7 2 4F A6WE 1996081500179 19960815 00179 WP 1996 8 15 MWEA96352 1 19960731 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 1155 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, DEEP DENT IN FUSELAGE SKIN WAS FOUND AT APPROX STA 1155 ON AFT RT CANTED STATION AREA. FABRICATED AND I NSTALLED A REPAIR IAW SRM 53-01, FIG 2 SHEET 3. 2 L 7 2 4F A6WE 1996081500180 19960815 00180 WP 1996 8 15 MWEA96353 1 19960731 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 120 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, A-FRAME IN E AND E COMPT WAS FOUND WITH A 2 INCH AREA OF HEAVY CORROSION AT STA 120, LONGERON 25R. FABR ICATED A REPAIR DOUBLER IAW SRM 53-03, FIG 5, SECTION AA AND INSTALLED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 1996081500181 19960815 00181 WP 1996 8 15 MWEA96354 1 19960731 A 5320 SHOVEL CLIP DOUG DC9 DC932 3022066 WP BS 110 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, A SHOVEL CLIP WAS FOUND CORRODED AT STA 110, LONG 21R. INSTALLED A NEW CLIP IAW SRM 51-30-2 AND 51-30-5 . 2 L 7 2 4F A6WE 1996081500182 19960815 00182 WP 1996 8 15 MWEA96355 1 19960731 A 5520 ANGLE DOUG DC9 DC932 3022066 WP LT ELEVATOR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, SEVERE CORROSION WAS FOUND ON LT ELEVATOR T/E 'TEE' ATTACH ANGLE BRACKET AT STA XE 171.5. FABRICATED A NEW TEE AND INSTALLED IAW SRM 51-10 AND 51-30. 2 L 7 2 4F A6WE 1996081500183 19960815 00183 WP 1996 8 15 MWEA96356 1 19960731 A 5754 RIB DOUG DC9 DC932 3022066 WP NR 4 LE FLAP CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, RT WING NR 4 SLAT OUTBD DRIVE FITTING RIB ASSY WAS FOUND CRACKED BETWEEN 2 FASTENERS ON LOWER FLANGE. R EPLACED RIB SET IAW SRM 57-02 PAGE 1, 2. 2 L 7 2 4F A6WE 1996081500184 19960815 00184 WP 1996 8 15 MWEA96357 1 19960731 A 5712 9919325 RIB DOUG DC9 DC932 3022066 WP RT WING CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, RT WING HAD SIX NOSE RIBS CORRODED AND ONE CRACKED ON LOWER FLANGE. REMOVED CORROSION IAW SRM 51-10-3, REPAIRED DAMAGED RIB IAW SRM 57-01, REINSTALLED REPAIR IAW SRM 51-30. 2 L 7 2 4F A6WE 1996081500185 19960815 00185 WP 1996 8 15 MWEA96358 1 19960731 A 5320 3916209 FITTING DOUG DC9 DC932 3022066 WP BS 680 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, TWO SEAT TRACK FITTINGS WERE FOUND CRACKED AT STA 680, ONE UNDER NR 1 AND ONE UNDER NR 4 TRACK. INSTALL ED NEW FITTINGS IAW SRM 51-10-4 AND 51-30-5. 2 L 7 2 4F A6WE 1996081500186 19960815 00186 WP 1996 8 15 MWEA96359 1 19960731 A 5751 SKIN DOUG DC9 DC932 3022066 WP LT AILERON CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, LT AILERON UPPER SKIN FOUND WITH NUMEROUS AREAS OF LIGHT CORROSION. FABRICATED NEW SKIN AND DOUBLER IAW ME EA 57-002, TREATED AND PRIMED IAW SRM 51-10-3 AND INSTALLED IAW EA 57-002. 2 L 7 2 4F A6WE 1996081500187 19960815 00187 WP 1996 8 15 MWEA96360 1 19960731 A 5511 SPAR WEB DOUG DC9 DC932 3022066 WP RT HORIZ STAB CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, A 2 INCH AREA OF CORROSION FOUND ON RT HORIZONTAL STAB AFT SPAR WEB AT STA XMS 32.0. COMPLETED REPAIR I AW DAC TELEX SVC/MSP/0407/SBT. 2 L 7 2 4F A6WE 1996081500188 19960815 00188 WP 1996 8 15 MWEA96361 1 19960731 A 5720 ANGLE DOUG DC9 DC932 3022066 WP LT WING CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, LT WING TRAP PANEL AFT OUTBD FLANGE REPAIR HAD AN ANGLE CRACK AT THE AFT FLANGE. INSTALLED ANGLE REPAIR IAW SRM 57-09, FIG 71 SHEET 2. 2 L 7 2 4F A6WE 1996081500189 19960815 00189 WP 1996 8 15 MWEA96362 1 19960731 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 313-332 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, LONGERON UPPER FLANGE FOUND CRACKED AT STA 313 TO 332 AT LONG 29L. FABRICATED A LONG SECTION AND REPAIR SPLICES AND INSTALLED IAW SRM 53-02 AND 53-02, FIG 14. 2 L 7 2 4F A6WE 1996081500190 19960815 00190 WP 1996 8 15 MWEA96363 1 19960731 A 5320 4916270 FITTING DOUG DC9 DC932 3022066 WP BS 680 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, LT KEEL HORSESHOE BRACKET FOUND CORRODED AT STA 680, LONG 29 LT. FABRICATED A NEW FITTING IAW DAC DWG 4 916270 AND INSTALLED IAW SRM 51-30-03. 2 L 7 2 4F A6WE 1996081500191 19960815 00191 WP 1996 8 15 MWEA96364 1 19960731 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 699 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, RT SIDE KEEL FITTING FOUND CRACKED AT STA 699. FABRICATED A NEW FITTING IAW DAC DWG 4915126 AND INSTALL ED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 1996081500192 19960815 00192 WP 1996 8 15 MWEA96365 1 19960731 A 5753 9957774 RIB DOUG DC9 DC932 3022066 WP RT TE FLAP CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, RT FLAP NOSE RIB FOUND CRACKED AT STA 207. FABRICATED A TEMPORARY REPAIR IAW SRM 57-01, FIG 3 SHEET 3 A ND INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1996081500193 19960815 00193 WP 1996 8 15 MWEA96366 1 19960731 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP BS 996 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, DOUBLER PLATE FOUND CORRODED AT STA 996 FWD OF APB ABOVE LONGERON 30. FABRICATED A NEW DOUBLER IAW SRM 53-03 AND INSTALLED IAW 51-30-5. 2 L 7 2 4F A6WE 1996081500194 19960815 00194 WP 1996 8 15 MWEA96367 1 19960731 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 218 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, FRAME LOWER FLANGE WAS FOUND CORRODED AT STA 218 IN E AND E COMPT FROM LONG 27L TO 27R. INSTALLED FRAME REPAIR IAW SRM 53-03-4A. 2 L 7 2 4F A6WE 1996081500195 19960815 00195 WP 1996 8 15 MWEA96368 1 19960731 A 5712 RIB DOUG DC9 DC932 3022066 WP RT WING CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, RT WING NR 1 SLAT INBD IDLER TRACK OUTBD RIB WAS FOUND CRACKED. REPLACED RIB SET IAW SRM 57-01, PAGE 1 AND 2. 2 L 7 2 4F A6WE 1996081500196 19960815 00196 WP 1996 8 15 MWEA96369 1 19960731 A 5320 DOOR JAMB DOUG DC9 DC932 3022066 WP BS 200 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, GALLEY DOOR JAMB 'T' FITTING WAS FOUND WITH CORROSION AT STA 200 FWD OF LONG 17R. FABRICATED NEW FITTIN G AND INSTALLED IAW SRM 51-10-2 AND 51-30-2. 2 L 7 2 4F A6WE 1996081500197 19960815 00197 WP 1996 8 15 MWEA96370 1 19960731 A 5313 3924809 LONGERON DOUG DC9 DC932 3022066 WP BS 579-604 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, LONG 30 END FITTING WAS FOUND CORRODED FROM STA 579 TO 604. FABRICATED SPLICE FITTING IAW DAC DWG 39248 09 AND INSTALLED IAW SRM 53-01. 2 L 7 2 4F A6WE 1996081500198 19960815 00198 WP 1996 8 15 MWEA96371 1 19960731 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 503 IMPROPER REPAIR A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, FUSELAGE FRAME FOUND WITH PREVIOUS IMPROPER REPAIR AT STA 503, LONGERON 28L TO 28R. INSTALLED REPAIR PE R SRM 53-03, FIG 2A SHEET 1. 2 L 7 2 4F A6WE 1996081500199 19960815 00199 WP 1996 8 15 MWEA96372 1 19960731 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 986-996 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, A SKIN PANEL WAS FOUND CORRODED FROM STA 986 TO 996 LONG 29L TO 29R. INSTALLED EXTERNAL DOUBLER REPAIR IAW 53-04, FIG 9. 2 L 7 2 4F A6WE 1996081500200 19960815 00200 WP 1996 8 15 MWEA96373 1 19960731 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 803-818 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, FUSELAGE SKIN FOUND CORRODED FROM STA 803 TO 818 LONG 27L TO 27R. FABRICATED NEW SKIN PANEL AND INSTALL ED IAW DAC TELEX SVC-MSP-0320/AJC, DATED 7 MAY 96. 2 L 7 2 4F A6WE 1996081500201 19960815 00201 WP 1996 8 15 MWEA96374 1 19960731 A 5315 1414813 FLOOR BEAM DOUG DC9 DC932 3022066 WP BS 160 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, FLOOR BEAM UPPER CAP FOUND EXFOLIATED 15.5 INCHES INBD OF THE CUSP ANGLE AT STA 160. SPLICED IN A NEW S ECTION OF CAP IAW DAC TELEX SVC-SMP-0420/SBT. 2 L 7 2 4F A6WE 1996081500202 19960815 00202 WP 1996 8 15 MWEA96375 1 19960731 A 5320 9958195 SPLICE DOUG DC9 DC932 3022066 WP BS 700 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, LT KEEL SPLICE FOUND CRACKED AT STA 700. INSTALLED NEW KEEL SPLICE IAW SRM 51-30-5. 2 L 7 2 4F A6WE 1996081500203 19960815 00203 WP 1996 8 15 MWEA96376 1 19960731 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 150 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, A PREVIOUS SKIN REPAIR DOUBLER REQUIRED REMOVAL FOR FURTHER EVALUATION AT STA 150 BETWEEN LONG 17R AND 1 8R. COMPLETED REPAIR IAW SRM 53-04, FIG 47. 2 L 7 2 4F A6WE 1996081500204 19960815 00204 WP 1996 8 15 MWEA96377 1 19960731 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 288 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, PREVIOUS REPAIR ON FUSELAGE SKIN WAS REEVALUATED ON FWD LOWER SKIN AT STA 288 AT LONG 20R. REMOVED PREV IOUS REPAIR, FABRICATED AND INSTALLED NEW REPAIR IAW SRM 53-04, FIG 12B SHEET 5. 2 L 7 2 4F A6WE 1996081500205 19960815 00205 WP 1996 8 15 MWEA96378 1 19960731 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 325 GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, VHF ANTENNA SUPPORT L-ANGLE FOUND GOUGED TO EXCESS AT STA 325, LONG 29L AND 30. REPLACED THE ANGLE IAW SRM 53-01 PAGE 1. 2 L 7 2 4F A6WE 1996081500206 19960815 00206 WP 1996 8 15 MWEA96379 1 19960731 A 5320 TEE DOUG DC9 DC932 3022066 WP BS 756 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, LT GEAR WELL TEE HAD DEEP CORROSION PITTING AT STA 756, LONG 29L AND 30. FABRICATED REPAIR AND INSTALLE D IAW SRM 53-03 AND 51-30-5. 2 L 7 2 4F A6WE 1996081500207 19960815 00207 WP 1996 8 15 MWEA96380 1 19960731 A 5730 SKIN DOUG DC9 DC932 3022066 WP WS 84 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, LT WING LEADING EDGE FOUND CORRODED EXCESSIVELY AT STA XIS 84.0. INSTALLED REPAIR DOUBLERS IAW SRM 57-0 6A, FIG 4. 2 L 7 2 4F A6WE 1996081500208 19960815 00208 WP 1996 8 15 MWEA96381 1 19960731 A 5730 SKIN DOUG DC9 DC932 3022066 WP WS 82 BLENDED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, LT WING LEADING EDGE WAS FOUND WITH TWO SMALL BLENDED AREAS AT STA XIS 82.0. REPAIRED BLENDED AREAS IAW SRM 57-06A, FIG 4. 2 L 7 2 4F A6WE 1996081500209 19960815 00209 WP 1996 8 15 MWEA96382 1 19960731 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 218-256 CREASES A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, FWD FUSELAGE LOWER RT SKIN HAD SEVERAL CREASES IN CORNER BETWEEN STA 218 TO 256 AND LONG 24R TO 26R. IN STALLED A REPAIR IAW SRM 53-04, FIG 38 VIEW P. 2 L 7 2 4F A6WE 1996081500210 19960815 00210 WP 1996 8 15 MWEA96383 1 19960731 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 332 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, FWD FUSELAGE LOWER RT SKIN HAD SEVERAL DENTS AND CREASES AT STA 332, LONG 24R. FABRICATED AND INSTALLED REPAIR IAW SRM 53-04, FIG 38 SHEET 18. 2 L 7 2 4F A6WE 1996081500211 19960815 00211 WP 1996 8 15 MWEA96384 1 19960731 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 370 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, FWD CARGO COMPT DOOR JAMB AREA EXTERIOR SKIN CORNER FOUND DAMAGED AT STA 370, LONG 26L. REPAIRED SKIN P ER SRM 53-04, FIG 38 SHEET 20. 2 L 7 2 4F A6WE 1996081500212 19960815 00212 WP 1996 8 15 MWEA96385 1 19960731 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 408 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, INTERCOSTAL FOUND CRACKED ABOVE FWD CARGO DOOR JAMB AT STA 408 ABOVE LONG 19R. FABRICATED NEW INTERCOST AL AND INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1996081500213 19960815 00213 WP 1996 8 15 MWEA96386 1 19960731 A 5711 SPAR DOUG DC9 DC932 3022066 WP WS 380 RT CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, RT WING REAR SPAR UPPER TANG WAS FOUND CORRODED AT STA XRS 380.0 JSUT ABOVE OUTBD FLAP HINGE. FABRICATE D AND INSTALLED REPAIR IAW SRM 57-09, FIG 12. 2 L 7 2 4F A6WE 1996081500214 19960815 00214 WP 1996 8 15 MWEA96387 1 19960731 A 5720 ANGLE DOUG DC9 DC932 3022066 WP WS 380 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, A T/E PANEL RIB UPPER ANGLE CORRODED, RT WING STA XRS 380. FABRICATED AND INSTALLED A NEW ANGLE WITH RI B IAW SRM 51-40-0. 2 L 7 2 4F A6WE 1996081500215 19960815 00215 WP 1996 8 15 MWEA96388 1 19960731 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 436-522 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, LONGERON 29R FOUND WITH CORROSION FROM STA 436 TO 522. FOUND CORROSION OUT OF LIMITS AND REPLACED WITH NEW LONGERON SECTION IAW SRM 53-01. 2 L 7 2 4F A6WE 1996081500216 19960815 00216 WP 1996 8 15 MWEA96389 1 19960731 A 5280 SKIN DOUG DC9 DC932 3022066 WP RT MLG DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, RT MLG INBD DOOR TOP SKIN WAS FOUND CRACKED AT ACTUATOR FITTING APPROX .625 INCH LONG. FABRICATED A REP AIR IAW SRM 52-01 AND INSTALLED IAW SRM 52-01, FIG 2 SHEET 3. 2 L 7 2 4F A6WE 1996081500217 19960815 00217 WP 1996 8 15 MWEA96390 1 19960731 A 5320 RECESS PANELS DOUG DC9 DC932 3022066 WP NOSE SECTION CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, FOUND LT AND RT WINDSHIELD WIPER MOTOR CAVITIES HAVE CRACKS ON INNER RECESS PANELS. INSTALLED REPAIR IA W SRM 53-03, FIG 34 SHEET 1. 2 L 7 2 4F A6WE 1996081500218 19960815 00218 WP 1996 8 15 MWEA96391 1 19960731 A 5753 RIB DOUG DC9 DC932 3022066 WP TE FLAP REQ'D REPAIR A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, DUE TO RECEIPT OF CORRECT PARTS, A TEMPORARY REPAIR NEEDED TO BE REPLACED ON FLAP AT STA XFLS 199.0. IN STALLED REPLACEMENT RIB IAW SRM 57-01, PAGE 1. 2 L 7 2 4F A6WE 1996081500219 19960815 00219 WP 1996 8 15 MWEA96392 1 19960731 A 5753 RIB DOUG DC9 DC932 3022066 WP LT TE FLAP REQ'D REPAIR A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, TEMPORARY REPAIR NEEDED TO BE REPLACED ON FLAP AT STA XFLS 288.0. INSTALLED REPLACEMENT RIB IAW SRM 57- 02, PAGE 1. 2 L 7 2 4F A6WE 1996081500220 19960815 00220 WP 1996 8 15 MWEA96393 1 19960731 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 417-579 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, LONGERON 30 FOUND WITH MILD CORROSION FROM STA 417 T0 579. INSTALLED NEW LONGERON IAW SRM 53-01. 2 L 7 2 4F A6WE 1996081500221 19960815 00221 WP 1996 8 15 MWEA96394 1 19960731 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 229-559 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, LONGERON 29L WAS FOUND TO HAVE VARIOUS AREAS OF CORROSION STA 229 THROUGH 579. INSTALLED NEW LONGERON I AW SRM 53-01. 2 L 7 2 4F A6WE 1996081500222 19960815 00222 WP 1996 8 15 MWEA96395 1 19960731 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 427-446 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, FOUND INTERCOSTAL CRACKED AND CORRODED BETWEEN STA 446 TO 427 AT LONGERON 29LT. FABRICATED AND INSTALLE D INTERCOSTAL IAW SRM 51-10-2. 2 L 7 2 4F A6WE 1996081500223 19960815 00223 WP 1996 8 15 MWEA96396 1 19960731 A 5320 SUPPORT STRUT DOUG DC9 DC932 3022066 WP RT LAV FLOOR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, FOUND CORROSION ON FLOOR BEAM SUPPORT STRUT IN RT LAV AT STA 965. REMOVED CORROSION IAW SRM 51-10-3 AND INSTALLED SUPPORT AND CASTING IAW 51-30. 2 L 7 2 4F A6WE 1996081500224 19960815 00224 WP 1996 8 15 MWEA96397 1 19960731 A 5220 SEAL PAN DOUG DC9 DC932 3022066 WP AFT EMER EXIT CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, CORROSION FOUND ON LT AFT EMERGENCY EXIT DOOR SEAL PAN FWD LOWER CORNER. REPLACED NEW LOWER SEAL PAN IA W SRM 52-01. 2 L 7 2 4F A6WE 1996081500225 19960815 00225 WP 1996 8 15 MWEA96398 1 19960731 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 1104 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, FUSELAGE FRAME WAS EXFOLIATED AT STA 1104 BETWEEN LONGERONS 3L AND 4L. REPLACED FRAME NEW IAW SRM 53-01 , PAGE 1 AND 2. 2 L 7 2 4F A6WE 1996081500226 19960815 00226 WP 1996 8 15 MWEA96399 1 19960731 A 5220 SEAL PAN DOUG DC9 DC932 3022066 WP RT EMER EXIT CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, FOUND CORROSION ON RT AFT EMERGENCY EXIT DOOR SEAL PAN FWD AND AFT LOWER CORNERS. REPLACED SEAL PAN NEW IAW SRM 52-01. 2 L 7 2 4F A6WE 1996081500227 19960815 00227 WP 1996 8 15 MWEA96400 1 19960731 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 965/980 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING D-CHECK, LONGERONS 16L AND 17L WERE FOUND CRACKED AT STA 965 AND LONG 17L CRACKED AT STA 980. INSTALLED REPAIR I AW SRM 53-02, PAGE 2A. 2 L 7 2 4F A6WE 1996081500228 19960815 00228 WP 1996 8 15 MWEA96401 1 19960804 A 5730 TE SKIN DOUG DC9 DC932 3022066 WP LT WING CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 DURING C-CHECK, FOUND LT WING LOWER TRAILING EDGE PANEL CRACKED FWD OF INBD BUTT DOOR. FABRICATED AND INSTALLED TRAILIN G EDGE IAW SRM 53-01, FIG 2 AND 57-31-3, FIG 3. 2 L 7 2 4F A6WE 1996081500229 19960815 00229 WP 1996 8 15 MWEA96402 1 19960807 A 2560 SLIDE COVER DOUG DC9 DC914 3022034 WP FWD GALLEY DOOR FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 800ME 45842 CREW REPORTS, GALLEY SERVICE DOOR EVAC SLIDE COVER FALLING OFF. REINSTALLED GALLEY DOOR SLIDE COVER. 2 L 7 2 4F A6WE 1996081500230 19960815 00230 WP 1996 8 15 MWEA96403 1 19960731 A 2560 SLIDE COVER DOUG DC9 DC932 3022066 WP FWD GALLEY DOOR FELL OFF A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47672 DURING INSP, MAINT REPORTS GALLEY DOOR EVAC SLIDE COVER FELL OFF WHILE CLOSING DOOR. REINSTALLED GALLEY DOOR SLIDE COVE R. 2 L 7 2 4F A6WE 1996081500231 19960815 00231 WP 1996 8 15 PNSA960718 2 19960718 A 7321 FUEL CONTROL WOODWARD 89778015 SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP ENGINE OUT OF ADJUST A PNSA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 AL 03 46NE 2123788 AC746B LOW POWER ON TAKEOFF. ADJUSTED MAX POWER, GROUND RUN AND FLT CHECK OK. 2 L 7 2 4T 4 T RT A8SW E4WE 1996081500232 19960815 00232 SW 1996 8 15 QXEA9600277 1 19960808 A 3260 1EN516 SWITCH SWRNGN SA227 SA227AC 8780603 SW NLG INTERMITTENT A QXEA O OTHER P NO WARNING INDICATION AP APPROACH 1 NM 09 26959 AC662 NOSE GEAR DOWN/LOCKED INDICATOR DID NOT ILLUMINATE ON GEAR EXTINSION. LIGHT ILLUMINATED AFTER ALTERNATE GEAR EXTENSION PROCEDURES. AIRCRAFT LANDED IN FCA WITHOUT FURTHER PROBLEMS. AIRCRAFT FERRIED TO PDX FOR REPAIR. RIGHT HAND NOSE GEAR DOWN/LOCKED SWITCH REPLACED AND NOSE GEAR INDICATION OPS CHECKED GOOD ON GEAR SWING. 2 L 7 2 4T RT A8SW 1996081500233 19960815 00233 NM 1996 8 15 QXEA9600278 1 19960808 A 5270 869701 SENSOR DORNER DO32 DO328100 2996000 NM LT EMER EXIT OUT OF ADJUST A QXEA K NONE J WARNING INDICATION CL CLIMB 1 NM 09 330PH 3008 INTERMITTENT DOOR WARNING CAS MESSAGE AFTER TAKEOFF, LEFT SIDE UNDER WING EMERGENCY EXIT. EMERGENCY EXIT PROXIMITY SENS OR ADJUSTED IAW MAINT MANUAL, DOOR INDICATION OPS CHECKED GOOD. 2 H 7 2 4T RT A45NM 1996081500234 19960815 00234 EU 1996 8 15 QXEA9600279 1 19960807 A 3350 5515800104 BULBS GRIMES 5515800106 FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 803PH 11031 EXIT SIGN OVER COCKPIT DOOR INOP. SIGN REPLACED AND SIGN OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996081500235 19960815 00235 WP 1996 8 15 TC8A96052 1 19960809 A 7722 EGT TEMP IND DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3B 52039 NE NR 3 ENGINE MALFUNCTIONED A TC8A D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 23 181SK 45910 669217 NR 3 ENGINE IDLE EGT 400 DEGREES CELCIUS. CHECKED EGT INDICATION SYSTEM AS PER MM 77-20-0 NORMAL. ALSO, CHECKED THERMO COUPLE PROBES AND HARNESS, NORMAL. CARRIED OUT AN ENGINE TEST AS PER MM 71-00, ENGINE OPERATING LIMITS FOUND NORMAL. 2 L 7 4 4F 4 F 4A25 1E8 1996081500236 19960815 00236 WP 1996 8 15 TC8A96053 1 19960809 A 2910 HYD LINE DOUG DC8 DC8F55 3021928 WP RUDDER FAILED A TC8A A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 GL 23 808CK 45817 HYDRAULIC QUANTITY LOST DURING CLIMBOUT, RETURNED TO SBGR. FOUND HYDRAULIC STANDBY RUDDER PUMP PRESSURE LINE BUSTED. R EMOVED AND REPLACED LINE, OPS CHECKED GOOD IAW DC-8 M/M 29-0. 2 L 7 4 4F 4A25 1996081500237 19960815 00237 1996 8 15 VSTA9608002 4 19960808 A 3442 20671570153 R/T UNIT BENDIX RDR1E BOEING 737 737247 138448D NM FWD ELEC BAY DEFECTIVE A VSTA A UNSCHED LANDING O OTHER UK UNKNOWN 1 WP 07 303VA 6382 20125 WX RADAR RETURNS INTERMITTANT. AIR RETURN TO MIAMI. DEFECTIVE WX RADAR R/T, REMOVED AND REPLACED R/T AND OPS CHECK GOO D. 2 L 7 2 4F A16WE 1996081500238 19960815 00238 EU 1996 8 15 WWMA9600060 1 19960808 A 2611 721112110 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT MALFUNCTIONED A WWMA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 WP 15 354SB 340B354 THE CARGO SMOKE LIGHT ILLUMINATED IN FLIGHT, THE NR 1 CARGO EXTINGUISHER FIRE BOTTLE WAS FIRED. NO SMOKE OR FIRE WAS EV IDENT TO THE FLIGHT CREW. MAINTENANCE REPLACED THE CARGO FIRE BOTTLE AND CLEANED BOTH CARGO SMOKE DETECTORS. THE AIRCR AFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT A52EU 1996081500242 19960815 00242 1996 8 15 96ZZZX3947 4 19960618 A 3416 375002241 ALTIMETER AEROSP SA365 SA365N 8680669 EU COCKPIT OUT OF CALIB A ZYWA K NONE O OTHER IN INSP/MAINT 1 GL 09 365SJ 1416 3860 6018 ALTIMETER OUT OF CALIBRATION. REMOVED AND REPLACED ALTIMETER. 1 G 7 2 3U H10EU 1996081500243 19960815 00243 1996 8 15 96ZZZX3948 4 19960618 A 3416 066306401 ALTIMETER AEROSP SA365 SA365N 8680669 EU COCKPIT ENCODER OUT OF CALIB A ZYWA K NONE O OTHER IN INSP/MAINT 1 GL 09 365SJ 3047 18312 6018 ALTIMETER OUT OF CALIBRATION. REMOVED AND REPLACED ALTIMETER. 1 G 7 2 3U H10EU 1996081500244 19960815 00244 EU 1996 8 15 96ZZZX3949 1 19960618 A 3340 34528H021 POWER SUPPLY AEROSP SA365 SA365N 8680669 EU STROBE DEFECTIVE A ZYWA K NONE O OTHER IN INSP/MAINT 1 GL 09 365SJ 141 1474 6018 STROBE FLASHING SLOWLY. REMOVED AND REPLACED POWER SUPPLY. 1 G 7 2 3U H10EU 1996081500245 19960815 00245 EU 1996 8 15 96ZZZX3950 1 19960701 A 3340 34258H011 LIGHT AEROSP SA365 SA365N 8680669 EU STROBE INOPERATIVE A ZYWA K NONE O OTHER IN INSP/MAINT 1 GL 09 365SJ 144 2462 6018 STROBE INOPERATIVE. REMOVED AND REPLACED LIGHT. 1 G 7 2 3U H10EU 1996081500246 19960815 00246 EU 1996 8 15 96ZZZX3951 1 19960404 A 6410 704A33633171 HINGE SNIAS 350 AS350B2 8680813 EU T/R PINK WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 6099P 242 2818 LAMINATED HINGE HAS ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996081500247 19960815 00247 EU 1996 8 15 96ZZZX3952 1 19960222 A 6410 704A33633171 HINGE SNIAS 350 AS350B 8680801 EU T/R YELLOW WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 779LF 180 1621 LAMINATED HINGE HAS ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996081500248 19960815 00248 EU 1996 8 15 96ZZZX3953 1 19960220 A 6410 704A33633171 HINGE SNIAS 350 AS350B2 8680813 EU T/R YELLOW WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911LR 16 2404 LAMINATED HINGE HAS ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996081500249 19960815 00249 EU 1996 8 15 96ZZZX3954 1 19960529 A 6410 704A33633171 HINGE SNIAS 350 AS350B2 8680813 EU T/R PINK WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 92LG 97 2575 LAMINATED HINGE HAS ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996081500250 19960815 00250 EU 1996 8 15 96ZZZX3955 1 19960221 A 6410 704A33633171 HINGE SNIAS 350 AS350B2 8680813 EU T/R PINK WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 92LG 363 2575 LAMINATED HINGE HAS ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996081500251 19960815 00251 EU 1996 8 15 96ZZZX3956 1 19960517 A 6220 704A33633156 SPHERICAL STOP SNIAS 350 AS350B2 8680813 EU M/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 93LG 503 4318 2654 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996081500252 19960815 00252 EU 1996 8 15 96ZZZX3957 1 19960517 A 6220 704A33633156 SPHERICAL STOP SNIAS 350 AS350B2 8680813 EU M/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 93LG 503 4329 2654 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996081500253 19960815 00253 EU 1996 8 15 96ZZZX3958 1 19960517 A 6220 704A33633156 SPHERICAL STOP SNIAS 350 AS350B2 8680813 EU M/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 93LG 503 4331 2654 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996081500254 19960815 00254 EU 1996 8 15 96ZZZX3959 1 19960517 A 6220 117775P STARFLEX SNIAS 350 AS350B2 8680813 EU M/R BALL JOINT WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 93LG 303 2654 TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 3 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996081500255 19960815 00255 EU 1996 8 15 96ZZZX3960 1 19960701 A 6410 704A33633171 HINGE SNIAS 350 AS350B2 8680813 EU T/R PINK WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 94LG 130 2728 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996081500256 19960815 00256 EU 1996 8 15 96ZZZX3961 1 19960417 A 6410 704A33633116 BEARING SNIAS 350 AS350B2 8680813 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 94LG 389 2728 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 4 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996081500257 19960815 00257 EU 1996 8 15 96ZZZX3962 1 19960608 A 7931 642790041 TRANSMITTER SNIAS 350 AS350B2 8680813 EU ENGINE OIL FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 94LG 224 129 2728 OIL PRESSURE GAUGE NOT GETTING SIGNAL. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996081500258 19960815 00258 EU 1996 8 15 96ZZZX3963 1 19960518 A 7931 642790041 TRANSMITTER SNIAS 350 AS350B2 8680813 EU ENGINE OIL DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 96LG 225 1453 2817 OIL PRESSURE INDICATOR PEGS HIGH. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996081500259 19960815 00259 EU 1996 8 15 96ZZZX3964 1 19960530 A 6220 117775P STARFLEX SNIAS 350 AS350B2 8680813 EU M/R BALL JOINT WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 96LG 610 2817 TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996081500260 19960815 00260 EU 1996 8 15 96ZZZX3965 1 19960419 A 6520 350A33200403 SPIDER SNIAS 350 AS350B2 8680813 EU T/R DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 96LG 551 MA0399 2817 TAIL ROTOR SPIDER ASSEMBLY HAS LOOSE BEARING BAFFLES. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996081500261 19960815 00261 EU 1996 8 15 96ZZZX3966 1 19960328 A 6500 350A35105901 COUPLING SNIAS 350 AS350B2 8680813 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 96LG 525 2817 COUPLING'S OUTER DISK DENTED AND WORN. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996081500262 19960815 00262 SW 1996 8 15 96ZZZX3967 1 19960723 A 6420 206011810151 HUB BELL 206 206L4 1182110 SW T/R STIFF A NYBA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 EA 11 123NH 2013 AG156 52076 PILOT NOTED THAT WITH INCREASED RPM, TAIL ROTOR PEDALS BECAME STIFF. THE T/R BLADE FEATHERING BEARINGS WERE NOT FOUND T O BE CRACKED. TAIL ROTOR HUB ASSY WAS REMOVED AND VISUALLY INSPECTED IAW BELL 206L-4 MM. NO OBVIOUS DEFECTS HAVE BEEN NOTED. A THOROUGH TEAR-DOWN INSPECTION WILL BE ACCOMPLISHED TO DETERMINE THE STIFF PEDAL CONDITION. REPLACED T/R HUB A ND BLADE ASSEMBLY. 1 G 7 1 3U NC H2SW 1996081500263 19960815 00263 SW 1996 8 15 96ZZZX3968 1 19960610 A 6322 247821 SHAFT ASSY 222865515105 BELL 222 222U 1182140 SW COOLER BLOWER SHEARED A A NXTA E A ENGINE SHUTDOWN UNSCHED LANDING M OVER TEMP CR CRUISE 1 SW 19 143CF 47506 DURING FLIGHT, PILOT NOTED NR 2 ENGINE OIL PRESSURE DROPPING AND THE OIL TEMPERATURE RISING. HE SHUT DOWN THE ENGINE AS A RESULT AND PERFORMED A SINGLE ENGINE LANDING. WHILE INVESTIGATING THE CAUSE, MECHANIC DISCOVERED THE SHAFT OF THE OI L COOLER BLOWER TO HAVE SHEARED NEXT TO THE SPLINE ADAPTER. THE IMPELLERS APPEAR TO HAVE SEIZED INSIDE THE HOUSING. 1 G 7 2 3U H9SW 1996081500264 19960815 00264 EU 1996 8 15 96ZZZX3969 1 19960728 A 6320 4638304001 SUN GEAR 438001004 BOLKMS 105 BO105S 5626006 EU M/R XMSN FAILED A L A ALGA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 03 2906T 2630 1591 835 S573 FOLLOWING THE ACCIDENT OF A BO105S, AN INVESTIGATION REVEALED THE SUN GEAR (PN 4638-304-001) IN THE MAIN ROTOR TRANSMISS ION HAD FAILED. THE EXACT CAUSE OF THE FAILURE TO THIS SUN GEAR HAS NOT BEEN DETERMINED. THIS SAME SUN GEAR HAD BEEN I N THE MAIN ROTOR TRANSMISSION OF AN AIRCRAFT THAT WAS INVOLVED IN A CATASTROPHIC ACCIDENT WHERE THE AIRCRAFT HAD IMPACTE D THE GROUND IN AN INVERTED ATTITUDE. PART TOTAL TIME SINCE OVERHAUL, 1,591 HOURS. TRANSMISSION S/N, 1165. 1 G 7 2 3U H3EU 1996081500265 19960815 00265 1996 8 15 96ZZZX3970 4 19960121 A 3460 COMPUTER BAC 146 AVRO146RJ100 1500096 EU E/E COMPARTMENT MALFUNCTIONED W ANCF C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 23 505MM E3242 BOG - FLT 506 - TAKEOFF WAS ABORTED DUE TO THRUST RATING PANEL (TRP) AND FLIGHT GUIDANCE COMPUTER (FGC) DISCONNECTING. F AULT RESET. FAILURE COULD NOT BE DUPLICATED. CYCLES, 2,986. HOURS, 3,209. 2 H 7 4 4F RT A49EU 1996081500267 19960815 00267 NE 1996 8 15 96ZZZX3972 2 19960101 A 7320 HMA BAC 146 AVRO146RJ100 1500096 EU LYC LF507 LF5071F NE NR 4 ENGINE MALFUNCTIONED W A ANCF C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 23 504MM E3221 BOG - FLT 502 - DURING TAKEOFF RUN LIMITED TO MAX POWER DUE TO MAX WEIGHT, THE ENGINE NR 4 FOR 96 N1 REQUIRED, DID NOT R EACH 96. IT SHOWS 94 PERCENT AND DESECNDING, ALTHOUGH THE THRUST LEVER WAS ADVANCED MORE. THE EGT, SAME ENGINE, WAS IN CREASING. THE TAKEOFF WAS DISCONTINUED AT 80 KNOTS. P-11A CONNECTOR WAS CLEANED AND CHECKED. INDICATORS WERE SWAPPED. FAIL DID NOT DUPLICATE, BUT EGT IS 30 DEGREES CENTRIGRADE OVER THE ENGINE NR 2 INDICATOR. HMA WAS CHANGED. TESTING R UN-UP OK. HMA S/N OFF, 1AGV32AB, PN 2-193-330-03. S/N ON AG091AB, PN 2-193-330-05. HOURS, 2,932. CYCLES, 2,799. 2 H 7 4 4F 4 F RT A49EU E6NE 1996081500269 19960815 00269 NE 1996 8 15 96ZZZX3974 2 19960131 A 7230 COMPRESSOR BAC 146 AVRO146RJ100 1500096 EU LYC LF507 LF5071F NE NR 3 ENGINE STALLED W A ANCF O OTHER R E PARTIAL RPM/PWR LOSS VIBRATION/BUFFET CL CLIMB 1 SO 23 507MM E3245 GUA - FLT 503 - AFTER PASSING 1,000 FEET AGL, A COMPRESSOR STALL WAS HEARD, ENG NR 3 PARAMETERS BEGAN TO FLUCTUATE. EGT EXCEEDED THE TAKEOFF LIMIT THROTTLE, NR 3 WAS REDUCED. EVEN THOUGH, ENGINE CONTINUED TO VIBRATE WITH THE ENGINE VIBRAT ION CAUTION LIGHT ILLUMINATED. AT THIS POINT, ENGINE WAS UNCONTROLLABLE. ENGINE FAILURE AND SHUT-DOWN PROCEDURE WAS PE RFORMED, IT WAS INSPECTED. FOUND SMALL METAL PARTICLES IN EXHAUST AREA. CHANGED ENGINE NR 3, TESTED IAW MM 71-00-00. O K. ENGINE S/N ON: LF07323, OFF: LF07314. HOURS, 3,171. CYCLES, 2,868. 2 H 7 4 4F 4 F RT A49EU E6NE 1996081500270 19960815 00270 EU 1996 8 15 96ZZZX3975 1 19960118 A 7931 CONNECTOR BAC 146 AVRO146RJ100 1500096 EU NR 4 ENGINE DIRTY W ANCF E ENGINE SHUTDOWN N FALSE WARNING NR NOT REPORTED 1 SO 23 509MM E3248 SMR/RNG - FLT 161 - IN-FLIGHT, ENGINE NR 4 SHUT DOWN. ACCOMPLISHED DUE OIL LOW PRESSURE. ENGINE NR 4 WAS CHECKED PER L EAK EVIDENCES AND IT IS OK. OIL PRESSURE TRANSMITTER ELECTRICAL CONNECTOR WAS CHECKED AND CLEANED. TEST ON ENGINE OK. NOTE: NO EVIDENCE OF ACTUAL LOW OIL PRESSURE WAS FOUND. HOURS, 3,055. CYCLES, 2,831. 2 H 7 4 4F RT A49EU 1996081500272 19960815 00272 NM 1996 8 15 96ZZZX3977 1 19960624 A 2782 ACTUATOR BOEING 727 727225 1384077 NM NR 8 LE FLAP FAILED A MYWA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 889MA 21854 LOG REPORT: GL521 AT MIA - RETURN FROM FLIGHT. AFTER TAKEOFF WHILE RETRACTING THE FLAPS FROM THE 5-DEGREE TO THE 2-DEG REE POSITIONS, THE LE FLAP AMBER INTRANSIT LIGHT ILLUMINATED ON THE FORWARD AND FE'S PANELS FOR THE NR 8 POSITION. REPL ACED NR 8 SLAT ACTUATOR. OPERATIONAL CHECK OK PER MM 27-80. 2 L 7 3 4F A3WE 1996081500273 19960815 00273 NM 1996 8 15 96ZZZX3978 1 19960712 A 3610 652244117 DUCT BOEING 727 727222 1384073 NM NR 3 ENGINE RUPTURED A RYNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 07 7638U 19911 NR 3 ENGINE FIRE WARNING ACTIVATED AFTER TAKEOFF. REPLACED THE NR 3 ENGINE, 13TH STAGE SADDLE DUCT PER MM 72-00. 2 L 7 3 4F A3WE 1996081500274 19960815 00274 NM 1996 8 15 96ZZZX3979 1 19960627 A 3350 LENSES BOEING 737 7374S3 1384711 NM CABIN MISSING A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 786AS 24795 SEA - FLT 315 - TWO LENS COVERS FOR EMERGENCY EXIT FLOOR TRACK LIGHTING MISSING AT ROW 17. RELAMPED AND INSTALLED MISSI NG LENSES; LIGHTS OPERATED NORMALLY. REFERENCE: OPERATOR CONTROL NR ASAA9640050. 2 L 7 2 4F RT A16WE 1996081500275 19960815 00275 EU 1996 8 15 96ZZZX3980 1 19960617 A 2910 9302631001 HYDRAULIC LINE SAAB SF340 340B 7860101 EU BRAKE SYSTEM FAILED A NVEA K NONE K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 03 235AE 340B235 JFK - FLT 4894 - CREW REPORTS: HYDRAULIC LOW LIGHT ILLUMINATED ONE MINUTE PRIOR TO LANDING. AFTER LANDING, AIRCRAFT HA D MINIMAL BRAKE PRESSURE. FOUND HYDRAULIC LINE LEAKING, REPLACED SAME. 2 L 7 2 4T RT A52EU 1996081500276 19960815 00276 NM 1996 8 15 96ZZZX3981 1 19960605 A 3230 651781914 LOCK ACTUATOR BOEING 737 7373G7 1384595 NM NLG FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 150AW 28985 9427 SC527 23218 PHX/IAH - FLT 0278 - AIR TURNBACK. AFTER RAISING LANDING GEAR AFTER TAKEOFF, NOSE GEAR RED LIGHT REMAINED ILLUMINATED. WHEN GEAR HANDLE PLACED TO OFF, NOSE GEAR WENT DOWN, FAILING TO STAY UP AND LOCKED. REMOVED AND REPLACED NOSE GEAR MOD ULAR PACKAGE PER MM 32-33-31, PAGES 401-403. REMOVED AND REPLACED NOSE LANDING GEAR LOCK ACTUATOR PER R4N32010. REFERE NCE: OPERATOR CONTROL NR AWXA960263. PART TOTAL CYCLES, 18,057. 2 L 7 2 4F RT A16WE 1996081500277 19960815 00277 WP 1996 8 15 AALA960956 1 19960623 A 4990 38005041 APU GARRTT DOUG DC9 DC983 3022083 WP APU COMPARTMENT LEAKING OIL A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 592AA P80119 53255 EWR - FLT 1223 - DURING TAKEOFF FROM EWR, SLIGHT SMOKE NOTED IN CABIN. TURNED OFF BOTH AIR CONDITIONING PACKS AND SMOKE CLEARED. AIRCRAFT RETURNED TO EWR AND LANDED OVERWEIGHT WITHOUT INCIDENT. REPLACED APU DUE TO OIL LEAKAGE. ACCOMPLIS HED PNEUMATIC SYSTEM DUCT BURN-OUT PROCEDURE. SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION WITH NO SMOKE OR SMELL NO TED. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION WITH NO DEFECTS FOUND. ACCOMPLISHED FUNCTIONAL CHECK FLIGHT WITH NO DE FECTS FOUND. SYSTEM OPERATIONAL CHECKED NORMAL. (X) 2 L 7 2 4F RT A6WE 1996081500278 19960815 00278 NM 1996 8 15 ASAA9640050 1 19960627 A 3350 303 LAMPS BOEING 737 7374S3 1384711 NM CABIN FAILED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 786AS 24795 SEA - FLT 315 - TWO LENS COVERS FOR EMERGENCY EXIT FLOOR TRACK LIGHTING MISSING AT ROW 17. RELAMPED AND INSTALLED MISSI NG LENSES; LIGHTS OPERATED NORMALLY. REFERENCE: OPERATOR CONTROL NR 96ZZZX3979. (X) 2 L 7 2 4F RT A16WE 1996081500279 19960815 00279 NM 1996 8 15 AWXA960247 1 19960528 A 2910 HYD LINE BOEING 737 7373G7 1384595 NM LT MLG RUPTURED A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 28 157AW 23779 PHX/RNO - FLT 0536 - AIR TURNBACK. ENGINE NR 1 HYDRAULIC PUMP LOW PRESSURE LIGHT ON HYDRAULIC SYSTEM QUANTITY GAUGE IND ICATED NEAR EMPTY. REPLACED RUPTURED HYDRAULIC LINE AT INBOARD PORT OF LT MLG UPLOCK ACTUATOR. LEAK CHECK GOOD. INSPE CTED ALL A-SYSTEM PRESSURE AND RETURN FILTERS PER MM 29-15. ALL CLEAN. (X) 2 L 7 2 4F RT A16WE 1996081500280 19960815 00280 NM 1996 8 15 AWXA960258 1 19960603 A 2782 ACTUATOR BOEING 737 737275 1384485 NM NR 2 LE FLAP FAILED A AWXA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 WP 28 CGCPW 3583 20966 20959 PHX/OAK - FLT 0577 - AIR TURNBACK. NR 2 SLAT EXTENDED ABOUT 2 INCHES EN ROUTE. REMOVED AND REPLACED NR 2 ACTUATOR PER R3M27020. OPERATION AND LEAK CHECK GOOD. PART TOTAL CYCLES, 35,841. (X) 2 L 7 2 4F A16WE 1996081500281 19960815 00281 NM 1996 8 15 AWXA960261 1 19960524 A 5330 5103971014T3 SKIN BOEING 737 737301 1384611 NM BS 956 DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 23260 PAE - FLT 7819 - DURING ROUTINE SCHEDULED C-11 MAINTENANCE CHECK, FOUND DENT IN SKIN AT BS 956 BETWEEN STR 18 AND STR 19 RT. REMOVED DAMAGE, FABRICATED REPAIR PART, ALODINED, INSTALLED PART IAW SRM 53-00-01 AND SRM 51-40-03. (X) 2 L 7 2 4F RT A16WE 1996081500282 19960815 00282 NM 1996 8 15 AWXA960263 1 19960605 A 3260 65446914 MODULAR BOEING 737 7373G7 1384595 NM NLG FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 150AW 35034 1176 23218 PHX/IAH - FLT 0278 - AIR TURNBACK. AFTER RAISING LANDING GEAR AFTER TAKEOFF, NOSE GEAR RED LIGHT REMAINED ILLUMINATED. WHEN GEAR HANDLE PLACED TO OFF, NOSE GEAR WENT DOWN, FAILING TO STAY UP AND LOCKED. REMOVED AND REPLACED NOSE GEAR MOD ULAR PACKAGE PER MM 32-33-31, PAGES 401-403. REMOVED AND REPLACED NOSE LANDING GEAR LOCK ACTUATOR PER R4N32010. REFERE NCE: OPERATOR CONTROL NR. 96ZZZX3981. PART TOTAL CYCLES, 30,509. (X) 2 L 7 2 4F RT A16WE 1996081500283 19960815 00283 NM 1996 8 15 AWXA960266 1 19960609 A 2782 654476012 ACTUATOR BOEING 737 7373S3 1384711 NM NR 5 LE FLAP FAILED A AWXA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 WP 28 313AW 31378 23712 LAS/SNA - FLT 0806 - AIR TURNBACK. ON TAKEOFF FROM LAS AT 200 FEET, HAD A STICK SHAKER FOR 25 SECONDS AT 170 KIAS. LEA DING EDGE FLAP ANNUNCIATOR LIGHTS FLASHING BETWEEN TRANSIT EXT. AND L/E DEVICES OVERHEAD ANNUNCIATOR PANEL SHOWED NR 5 S LAT GOING BETWEEN EXT. GREEN AND TRANS AMBER. VISUALLY, F/O SAW NR 5 SLAT MOVING ABOUT 2 INCHES FROM EVEN WITH NR 6 TO 2 INCHES EXTENDED. REMOVED AND REPLACED NR 5 SLAT ACTUATOR PER CARD R3M27020. OPS CHECKS NORMAL. PART TOTAL CYCLES, 1 9,667. (X) 2 L 7 2 4F RT A16WE 1996081500284 19960815 00284 1996 8 15 AWXA9960293 4 19960627 A 3460 B398BCM0104 FMGC AIRBUS 320 A320232 3930326 EU NR 2 FAILED A A AWXA O OTHER F FLT CONT AFFECTED TO TAKEOFF 1 WP 28 641AW 15906 805 664 453 PHX/SNA - FLT 2651 - UNCOMMANDED LEFT RUDDER INPUT AT APPROXIMATELY 120 KNOTS ON TAKEOFF ROLL. REMOVED AND REPLACED FMG C. CYCLED RUDDER. NO DEFECTS NOTED AT THIS TIME. BITE TEST OF AFS AND SFCS SYSTEM, ALSO CHECK GOOD. NO FAULTS RECORD ED AT THIS TIME BY EITHER SYSTEM. PART TOTAL CYCLES, 8,172. (X) 2 L 7 2 4F RT A28NM 1996081500285 19960815 00285 EU 1996 8 15 RAIA960705 1 19960630 A 2612 51653151 FIRE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 03 568HK 436 41086 JFK - FLT 7660 - RIGHT ENGINE FIRE WARNING ILLUMINATED IN-FLIGHT. MAINTENANCE INSPECTED FIRE LOOP AND REPLACED RIGHT DI GITAL FIRE DETECTOR. (X) 2 L 7 2 4T RT A41NM 1996081500286 19960815 00286 EU 1996 8 15 SIMA961711 1 19960619 A 5320 S53171101241205 WINDOW FRAME AEROSP ATR42 ATR42300 8680920 EU LT COCKPIT CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 47AE 18779 047 DURING A 24K INSPECTION, CRACK ON CAPTAIN'S SIDE OF WINDOW FRAME NODE 5 WAS FOUND. MAINTENANCE REMOVED CRACK AND REPAIR ED AREA IAW E.O. E1-5300-157. AIRCRAFT WAS RETURNED TO SERVICE. PART TOTAL CYCLES, 23,907. (X) 2 H 7 2 4T RT A53EU 1996081500287 19960815 00287 NM 1996 8 15 W8PA960051 1 19960701 A 3350 LIGHT BULB BOEING 737 7373Q8 1384670 NM CABIN EEL FAILED A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 956WP 24299 FOUND EXTERNAL EMERGENCY EXIT LIGHT INOPERATIVE FOR R-2 DOOR. RELAMPED LIGHT ASSEMBLY. (X) 2 L 7 2 4F RT A16WE 1996081500288 19960815 00288 NM 1996 8 15 W8PA960056 1 19960715 A 3350 BULB BOEING 737 7373S3 1384711 NM CABIN FAILED A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 375TA 23787 FOUND EXTERNAL EMERGENCY EXIT LIGHT INOPERABLE FOR R-1 DOOR. RELAMPED LIGHT ASSEMBLY. (X) 2 L 7 2 4F RT A16WE 1996081500289 19960815 00289 NM 1996 8 15 CALA9601145 1 19960808 A 2612 89931505 DET. MODULE BOEING 737 7373T0 1384582 NM E&E COMPMT INOPERATIVE A CALA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 SW 09 17344 28485 19520 23582 WHILE CLIMBING THROUGH 34,000 FEET, WITH THE APU SHUT OFF, THE APU FIRE LIGHT AND BELL ACTIVATED. THE APU FIRE BOTTLE W AS DISCHARGED AND THE LIGHT EXTINGUISHED WITHIN TWO MINUTES. THE AIRCRAFT WAS DIVERTED TO SDF WHERE IT LANDED WITHOUT I NCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE APU FIRE DETECTION MODULE WAS REMOVED AND REPLACED. AN APU FIRE LOOP WAS ALSO FOUND SHORTED. THE FIRE LOOP WAS REMOVED AND REPLACED, OPERATION OF APU FIRE DETECTION SYSTEM CHECKED GOO D. 2 L 7 2 4F RT A16WE 1996081500290 19960815 00290 NM 1996 8 15 CALA9601146 1 19960807 A 5260 AIRSTAIRS BOEING 727 727232 1384082 NM TAIL SECTION OUT OF ADJUST A A CALA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 09 10791 20645 THE AFT AIRSTAIRS FELL DOWN WHILE TAXIING TO GATE AFTER LANDING AT IAH. THE AIRCRAFT WAS STOPPED AND THE STAIRS WERE SE CURED. WHEN THE AIRSTAIRS WAS EXAMINED FOR DAMAGE ONLY A SKID MARK WAS FOUND ON THE SKID PLATE. THE AIRSTAIR WAS OPERA TED SEVERAL TIMES. MAINTENANCE FOUND THAT THE STAIR HANDLE WAS NOT GOING OVERCENTER EVERY TIME. TROUBLESHOOTING FOUND STOPS ADJUSTED TOO LOW CAUSING CAM ROLLER TO NOT ENGAGE. THE STOPS WERE ADJUSTED AND TESTED PER MM 52-62-01 AND OPERATI ON OF THE STAIRS CHECKED GOOD. 2 L 7 3 4F A3WE 1996081500291 19960815 00291 NE 1996 8 15 CALA9601147 2 19960809 A 7530 7479555 STATOR CONTL BOEING 747 747230B 1384889 NM PWA JT9 JT9D7A 52054 NE #1 ENGINE INOPERATIVE A CALA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 09 78019 16773 2959 20527 662892 TAKEOFF WAS ABORTED AT 115 KNOTS AFTER THE NR 1 ENGINE WOULD NOT MAKE TAKEOFF POWER. THE AIRCRAFT WAS RETURNED TO GATE WHERE SIX TIRES BLEW DUE TO HEAT. MAINTENANCE FOUND THE NR 1 ENGINE COMPRESSOR STATOR CONTROL AT FAULT. THE COMPRESSOR STATOR CONTROL WAS REMOVED AND REPLACED IAW MM 75-31-401 AND GROUND TEST WAS GOOD. THE NR 1 ENGINE WAS BORESCOPED AND ALL CHECKS WERE GOOD. A HIGH ENERGY STOP/HEAT DAMAGE INSPECTION WAS PERFORMED PER MM 05-51-10 AND NO DISCREPANCIES WERE FOUND. IN ADDITION, THE BLOWN TIRES AND WHEEL ASSEMBLIES WERE REMOVED AND REPLACED. 2 L 7 4 4F 4 F A20WE E20EA 1996081500292 19960815 00292 WP 1996 8 15 CALA9601148 1 19960809 A 3260 SWITCH DOUG DC9 DC982 3022082 WP GEAR HANDLE CONTAMINATED A CALA O OTHER J WARNING INDICATION TO TAKEOFF 1 SW 09 72824 49824 ALL THREE RED GEAR UNSAFE LIGHTS REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE GEAR WAS CYCLED AND THE APPROPRIATE CH ECKLIST WAS FOLLOWED, BUT THE LIGHTS REMAINED ON. THE LIGHTS WENT OFF APPROXIMATELY 10 MINUTES AFTER TAKEOFF AND THE FL IGHT WAS CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE PINNED THE GEARS AND CHECKED THE THROTTLE SWITC HES AND GEAR HANDLE SWITCH. DEBRIS WAS FOUND ON THE GEAR HANDLE SWITCH. THE SWITCH WAS CLEANED WITH OPERATION AND INDI CATIONS CHECKING NORMAL. 2 L 7 2 4F A6WE 1996081500293 19960815 00293 NM 1996 8 15 CALA9601149 1 19960811 A 2420 915F2125 GCU BOEING 737 737214 138446R NM P6 PANEL INOPERATIVE A CALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TO TAKEOFF 1 SW 09 14239 15620 15620 19920 THE LEFT BUS OFF LIGHT COME ON SHORTLY AFTER TAKEOFF. THE LIGHT WAS ACCOMPANIED BY AN ELECTRICAL ODOR OR AIR CONDITIONI NG PACK SMELL AND A CLICKING SOUND, LIKE THAT OF A RELAY OPENING AND CLOSING, THE SOUND WAS HEARD COMING FROM BEHIND THE SECOND OFFICER'S SEAT. THE LIGHT EXTINGUISHED AND THE ODOR DISSIPATED ABOUT 10 MINUTES LATER. THE AIRCRAFT LANDED AT ATL WITHOUT INCIDENT. MAINTENANCE CHECKED THE ELECTRICAL OPERATION OF BOTH ENGINE GENERATORS AND FOUND BOTH GOOD. THE LEFT GCU WAS REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE, AN OPERATIONAL CHECK OF THE APU GENERATOR WITH MAXIMUM LOA D GAVE ALL NORMAL PARAMETERS. 2 L 7 2 4F A16WE 1996081500294 19960815 00294 WP 1996 8 15 9617161225 1 19960809 A 3620 PNEUM SYS DOUG DC10 DC1030 3023501 WP MALFUNCTIONED A NWAA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CR CRUISE 1 GL 01 225NW 46582 DURING CRUISE, THE NR 2 MANIFOLD FAIL LIGHT ILLUMINATED. FOLLOWED COM AND SHUT OFF THE PNEUMATIC SUPPLY. DUMPED 15,000 LBS OF FUEL AND RETURNED TO HNL. MAINTENANCE DEFERRED THE NR 2 PNEUMATIC SYSTEM AND REPAIRED THE NR 3 SYSTEM WHICH WAS ON MEL. 2 L 7 3 4F A22WE 1996081500295 19960815 00295 WP 1996 8 15 9617179140 1 19960806 A 3350 LIGHT DOUG DC9 DC914 3022034 WP LT NAC EEL INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 930RC 45729 DURING LINE CHECK, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED LEFT NACELLE EMERGENCY LIGHT BATTERY PACK, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996081500296 19960815 00296 WP 1996 8 15 9617189868 1 19960808 A 3350 LIGHTS DOUG DC9 DC951 3022051 WP INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 777NC 47787 DURING LINE CHECK, FOUND BOTH EXTERIOR OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BOTH OVERWING EMERGENCY BATTERY PACKS, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996081500297 19960815 00297 WP 1996 8 15 9617199955 1 19960807 A 3350 LIGHT DOUG DC9 DC931 3022065 WP CABIN EEL INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 922RW 47182 DURING LINE MAINTENANCE INSPECTION, FOUND CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES AND FUSE, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996081500298 19960815 00298 WP 1996 8 15 9617209995 1 19960807 A 3350 FUSE DOUG DC9 DC931 3022065 WP TAIL BATT PACK BLOWN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8978E 47327 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE IN EMERGENCY BAT TERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996081500299 19960815 00299 WP 1996 8 15 9617219996 1 19960807 A 3350 6011779 POWER SUPPLY DOUG DC9 DC931 3022065 WP LEFT NACELLE MALFUNCTIONED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8932E 47141 DURING PERIODIC CHECK, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996081500300 19960815 00300 WP 1996 8 15 9617229996 1 19960807 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP FWD F/A PANEL MALFUNCTIONED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8932E 47141 DURING PERIODIC CHECK, FOUND EMERGENCY LIGHT SWITCH AT FORWARD FLIGHT ATTENDANT PANEL INTERMITTENT BETWEEN ARM AND ON PO SITION. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996081500301 19960815 00301 WP 1996 8 15 9617239989 1 19960806 A 3350 60030451 BATTERY PACK DOUG DC9 DC931 3022065 WP FWD ENTRY WAY MALFUNCTIONED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8945E 47181 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS DIM IN FORWARD ENTRY WAY. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996081500302 19960815 00302 WP 1996 8 15 9617249995 1 19960804 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP TAILCONE DISCHARGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8978E 47326 DURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE RELEASE HANDLE AND CATWALK EMERGENCY EXIT LIGHTS INOPERATIVE. REPLAC ED BATTERIES, OPEATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996081500303 19960815 00303 WP 1996 8 15 9617259605 1 19960805 A 3397 WIRE DOUG DC9 DC932 3022066 WP FWD CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 605NW 47223 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHT AT SEAT 3C INOPERATIVE. REPAIRED BROKEN WIRE, OPERATIONAL CHE CK NORMAL. 2 L 7 2 4F A6WE 1996081500304 19960815 00304 NM 1996 8 15 9617266718 1 19960809 A 3233 ACTUATOR BOEING 747 747251F 1384898 NM LT MLG MALFUNCTION A NWAA O OTHER O OTHER AP APPROACH 1 GL 01 618US 21122 DURING APPROACH, THE LEFT WING LANDING GEAR WOULD NOT EXTEND. RECYCLED LANDING GEAR AND UTILIZED ALTERNATE LANDING GEAR EXTENSION. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE LEFT WING LANDING GEAR RETRACT ACTUATOR AND DOWNLOCK ACTUAT OR, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996081500305 19960815 00305 WP 1996 8 15 9617279966 1 19960810 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP AFT CABIN DISCHARGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9330 47138 DURING LINE MAINTENANCE INSPECTION, FOUND AFT CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHE CK NORMAL. 2 L 7 2 4F A6WE 1996081500306 19960815 00306 WP 1996 8 15 9617289970 1 19960810 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP FWD CABIN DISCHARGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9334 47247 DURING PREFLIGHT CHECK, FOUND FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN BATTERY PACK, OPERATION AL CHECK NORMAL. 2 L 7 2 4F A6WE 1996081500307 19960815 00307 WP 1996 8 15 9617299971 1 19960811 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP TAILCONE MALFUNCTIONED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9335 47337 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS OVER TAILCONE RELEASE HANDLE INOPERATIVE. REPLACED POWER SUP PLY AND BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996081500308 19960815 00308 WP 1996 8 15 9617309997 1 19960809 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP AFT CABIN DISCHARGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8933E 47142 DURING LINE MAINTENANCE INSPECTION, FOUND AFT SECTION OF CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPER ATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996081500309 19960815 00309 WP 1996 8 15 9617319610 1 19960811 A 3350 FUSE DOUG DC9 DC932 3022066 WP FWD CABIN BLOWN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 610NW 47432 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. REPLACED FUSE IN BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996081500310 19960815 00310 WP 1996 8 15 9617329610 1 19960810 A 3350 FUSE DOUG DC9 DC932 3022066 WP FWD CABIN BLOWN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 610NW 47432 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE IN EMERGENCY POWER PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996081500311 19960815 00311 NM 1996 8 15 9617336611 1 19960811 A 3260 LOGIC CARD BOEING 747 747251B 1384892 NM NLG DEFECTIVE A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 611US 20356 DURING CLIMB, THE RED NOSE LANDING GEAR LIGHT ILLUMINATED AFTER LANDING GEAR RETRACTION. RECYCLED LANDING GEAR AND LIGH T EXTINGUISHED. AIRCRAFT CONTINUED TO SEA AND LANDED WITHOUT INCIDENT. RESEATED GEAR CARDS IN HOLDERS AND GREASED NOSE LANDING GEAR, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996081500313 19960815 00313 SO 1996 8 15 COMA9610244 1 19960809 A 3150 WARNING HORN EMB 120 EMB120RT SO CENTRAL WARNING ACTIVATED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 156CA 120156 TAKE OFF TRIM AURAL WARNING SOUNDED ON TAKEOFF ROLL. COULD NOT DUPLICATE DISCREPANCY. RESET AURAL WARNING UNIT AND ACF T CONTINUED SERVICE. 2 L 7 2 4T RT A31SO 1996081500314 19960815 00314 SO 1996 8 15 COMA9610245 1 19960808 A 6120 78249035 PCU EMB 120 EMB120RT SO L/H LEAKING A COMA C ABORTED TAKEOFF K FLUID LOSS TO TAKEOFF 1 SO 01 266CA 6990 871 120258 LEFT ENGINE LOW OIL PRESSURE WARNING DURING TAKEOFF. OIL LEAKING FROM LEFT NACELLE. 2 L 7 2 4T RT A31SO 1996081500315 19960815 00315 EU 1996 8 15 COMA9630141 1 19960809 A 6120 8542M2 COMPUTER SAAB SF340 SF340A 7850100 EU AVIONICS MALFUNCTION A COMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 359CA 23037 7393 340A053 AUTO COARSEN WARNING ILLUMINATED DURING TAKEOFF. REPLACED THE AUTO COARSEN COMPUTER. 2 L 7 2 4T RT A52EU 1996081500316 19960815 00316 NM 1996 8 15 UPS96220829 1 19960808 A 5530 2024T4 WEB BOEING 727 727180C 138406G NM 3-95 CRACKED A IPXA O OTHER O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE SI. WHILE WORKING RUDDER TRIM ACTUATOR DISCOVERED WEB CRACKED AT CUTOUTS FOR RTA AND RTB CABLES UNDER PR ESSURE SEALS AT FIN STA 87.0 IN FIN TUNNEL. REPAIRED FIN STA 87.0 WEB IN FIN IAW TRAMCO EWO 96-2442, UPS FILE NR 727-5 5-0332. 2 L 7 3 4F A3WE 1996081500317 19960815 00317 NM 1996 8 15 UPS96220830 1 19960809 A 5530 7075T6 MIDSPAR CHORD BOEING 727 727180C 138406G NM 3-95 CORRODED A IPXA O OTHER O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE SI, CORROSION LT FIN MIDSPAR HAS CORROSION AT ACCESS PANEL 9601 FIN STA 226.7, FIN WL 168.39. REAMED HO LES, INSTALLED FREEZE PLUGS, CUTOUT DAMAGED AREA AND REAMED PER ENG FILE NR 727-55-0331. 2 L 7 3 4F A3WE 1996081500318 19960815 00318 NM 1996 8 15 UPS96420827 1 19960801 A 5320 NA FITTING BOEING 747 747123 1384873 NM BS 2060 CRACKED A IPXA O OTHER O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE CPCP, MAIN DECK FLOOR, STRUCTURE FITTING AT BS 2060 RBL 65 IS CRACKED, LENGTH OF CRACK IS 1.5 INCH. REM OVED CRACKED FITTING AND INSTALLED NEW FITTING IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996081500319 19960815 00319 NM 1996 8 15 UPS96420832 1 19960729 A 5310 NA UPPER CHORD BOEING 747 747123 1384873 NM BS 2040 CORRODED A IPXA O OTHER O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE CPCP, MAIN DECK FLOOR STRUCTURE CORROSION AT FLOOR PANEL FASTENER HOLES IN FLOOR BEAM UPPER CHORD AT STA 2040 RBL 75 TO 98.58. REMOVED CORROSION UPPER CHORD BS 2040 BETWEEN RBL 75 TO 108 IAW SRM 51-10-01. UPPER CHORD OUT O F LIMITS IAW SRM 53-10-01. REPAIRED UPPER CHORD IAW SRM 53-10-07. 2 L 7 4 4F A20WE 1996081500320 19960815 00320 WP 1996 8 15 UPS96820831 1 19960808 A 5350 NA TAIL CONE DOUG DC8 DC873F 302199F WP TAIL CONE CRACKED A IPXA O OTHER O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE DLY, 6 TO 8 INCH CRACK IN TAIL CONE BEHIND LEFT ELEVATOR. REPAIRED CRACK IN TAIL CONE PER EO DC-8-5350- 7876-A. 2 L 7 4 4F RT 4A25 1996081500321 19960815 00321 NM 1996 8 15 QXEA9600280 1 19960809 A 5270 869701 SENSOR ELDEC DORNER DO32 DO328100 2996000 NM LEFT AFT EXIT REQ. ADJUSTMENT A QXEA K NONE J WARNING INDICATION CR CRUISE 1 NM 09 330PH 3008 DOOR WARNING CAS MESSAGE IN FLIGHT, SYSTEM INDICATED LEFT REAR UNDERWING EXIT. NO AIR LEAKS OR SOUND COMING FROM EXIT, NO LOSS OF CABIN PRESSURE. AIRCRAFT ALTITUDE WAS 14,000 FT, LIGHT EXTINGUISHED AT 5,000 FT. EXIT PROXIMITY SENSOR ADJU STED IAW MAINT MANUAL AND INDICATION OPS CHECKED GOOD. 2 H 7 2 4T RT A45NM 1996081500322 19960815 00322 EU 1996 8 15 QXEA9600281 1 19960809 A 3350 5515800106 LIGHT ASSY. FOKKER FOKKER F28 F28MK1000 4990808 EU FWD CABIN BURNT OUT BULBS A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 454US 11107 EXIT LIGHT ABOVE MAIN CABIN DOOR INOP. LIGHT ASSY REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996081500323 19960815 00323 NM 1996 8 15 QXEA9600282 1 19960810 A 5270 869701 SENSOR ELDEC DORNER DO32 DO328100 2996000 NM LEFT REAR EXIT MALFUNCTIONING A QXEA K NONE J WARNING INDICATION CR CRUISE 1 NM 09 330PH 3008 LEFT REAR EMERGENCY EXIT DOOR WARNING CAS MESSAGE INFLIGHT AT 17,000 FT. LIGHT WENT OUT AT 4.50 CABIN PSID. PROXIMITY SENSOR REPLACED AND ADJUSTED IAW MAINT MANUAL, WARNING SYSTEM OPS CHECKED GOOD. 2 H 7 2 4T RT A45NM 1996081500324 19960815 00324 NM 1996 8 15 QXEA9600283 1 19960810 A 3350 6038443 POWER SUPPLY DHAV DHAV DHC8 DHC8102 2809003 NM PS4 INOP A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 831PH 328 AFT CEILING EGRESS LIGHT INOP. PS4 POWER SUPPLY REPLACED AND LIGHT OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 1996081500325 19960815 00325 NM 1996 8 15 96FDEA01342 1 19960810 A 2751 2061121 INDICATOR BOEING 727 727233 138408A NM TE FLAPS MALFUNCTIONED A FDEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 25 222FE 20933 DURING TAKEOFF RETRACTING FLAPS FROM 15 DEGREES TO 5 DEGREES, OUTBOARD FLAPS LEFT AND RIGHT NEEDLES SPLIT BY 2 NEEDLE WI DTHS AND OUTBOARD FLAP INDICATOR STOPPED MOVING. COMPLIED WITH ASYMMETRICAL FLAP CHECKLIST. REPLACED OUTBOARD FLAP POS ITION INDICATOR. CHECKED AND CLEANED LEFT OUTBOARD POSITION TRANSMITTER PLUG. FARED FLAPS WITH A HYD SYS AND SAFTIED A LTERNATE FLAP SWITCH OFF. PERFORMED SEVERAL FLAP CYCLES USING STANDARD PROCEDURE. OPS CK GOOD. NO DEFECT NOTED. 2 L 7 3 4F RT A3WE 1996081500326 19960815 00326 NE 1996 8 15 96FDEA01343 2 19960810 A 7310 772443007 LINE BOEING 727 72725 1384006 NM PWA JT8 JT8D7B 52053 NE NR 2 ENGINE LEAKING A FDEA A E UNSCHED LANDING ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 502FE 18271 NR 2 ENGINE WOULD NOT RUN HIGHER THAN EPR 1.02, N1 63.0, EGT 260 DEGREES, N2 74.0, AND FUEL FLOW 2950 POUNDS PER HOUR. POSSIBLE FUEL LEAK. ENGINE SHUT DOWN AS A PRECAUTION. FOUND LEAK ON SECONDARY MANIFOLD TUBE. REMOVED AND REPLACED P ACKING FOR SECONDARY MANIFOLD, TUBE LEAKED CHECK OK. NEEDS MANIFOLD CHANGE. REMOVED AND REPLACED FUEL MANIFOLD AND SEA LS PERFORMED RUN-UP PER JET RUN HANDBOOK. OPS CK NORMAL. LINE P/N 07-72443-0007. 2 L 7 3 4F 4 F A3WE E2EA 1996081500327 19960815 00327 NM 1996 8 15 96FDEA01344 1 19960809 A 5320 6519606178 SHEAR WEB BOEING 727 727233 138408A NM BS 1170- 1176 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 219FE 21102 NR 0467 AND 005. CORROSION C53-224-04 ON BOTTOM SIDE OF WEB BS 1170-1176 RBL - LBL 2 WL 207. REMOVED WEB BS 1170-11 76 RBL - LBL 2 WL 207. FABRICATED AND INSTALLED NEW WEB. REMOVED SEAT TRACK BS 1130 - 1183 BL ZERO WL 207. FABRI CATED AND INSTALLED NEW TRACK. ALL PER FEDEX SRM 51-20-1, 51-10-1. 2 L 7 3 4F RT A3WE 1996081500328 19960815 00328 WP 1996 8 15 96FDEA01345 1 19960810 A 5753 ARB00291 STRAP DOUG DC10 DC1030 3023501 WP LT TE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 321FE 47836 SNRM 5074. LEFT WING - OTBD FLAP INBD HINGE SUPPORT FITTING OTBD TENSION STRAP IS CRACKED LOWER BOLT HOLE EXTERNAL SUR FACE. REMOVED AND REPLACED SUPPORT FITTING TENSION STRAP PER EA 8-5710-29040 AND EO 8-5750-7-4320B3 PT 1. 2 L 7 3 4F A22WE 1996081500329 19960815 00329 WP 1996 8 15 96FDEA01346 1 19960726 A 2700 ARN0052516 BRACKET DOUG DC10 DC1030 3023501 WP R/WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 321FE 47836 SNRM 6004 R/H WING - O/B SLAT DRIVE MECHANISM, OUTER BRKT HAS CRACK INDICATION IN FWD FLANGE FILLET RADIUS. R/R SLAT DRIVE MECHANISM BRACKET PER MM 27-83-02. 2 L 7 3 4F A22WE 1996081500330 19960815 00330 NM 1996 8 15 96FDEA01347 1 19960812 A 5311 6515532 FRAME BOEING 727 727233 138408A NM BS 580 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 219FE 21102 NR0469 AND 006. DENTS IN FRAME AT BS 580 BETWEEN STR 16-17R. REPAIRED DAMAGED FRAME AT BS 580 BETWEEN STR 16-17R PER FEDEX SRM 51-40-3. 2 L 7 3 4F RT A3WE 1996081500331 19960815 00331 NM 1996 8 15 96FDEA01348 1 19960812 A 5311 6510287 FRAME BOEING 727 727233 138408A NM BS 660 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 219FE 21102 NR0042 AND 007. DENTS IN FRAME BS 660 STR 23-25L. DENT IN FRAME AT BS 660 BETWEEN STR 24-25L FOUND TO BE WITHIN LIM ITS PER FEDEX SRM 53-10-1. DENT IN FRAME AT BS 660 BETWEEN 23-24L FOUND OUT OF LIMITS (CRACKED). REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR CAP PER FEDEX SRM 51-40-3. 2 L 7 3 4F RT A3WE 1996081500332 19960815 00332 NM 1996 8 15 96FDEA01349 1 19960812 A 5315 6520834 FLOOR BEAM BOEING 727 727233 138408A NM BS 1050 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 219FE 21102 NR0465 AND 088. CORROSION C53-224-04 ON FLOOR BEAM OUT OF LIMITS BS 1050 RBL 35 WL 208.1. REMOVED DAMAGED AREA, F ABRICATED AND INSTALLED REPAIR ANGLES (2 EA), AND REPLACED FILLER ON FLOOR BEAM AT BS 1050 RBL 35 WL 208.1 AND TREATE D IAW FEDEX SRM 53-10-8. 2 L 7 3 4F RT A3WE 1996081500333 19960815 00333 NM 1996 8 15 96FDEA01350 1 19960806 A 5315 6520833 FLOOR BEAM BOEING 727 727233 138408A NM BS 1070 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 219FE 21102 NR0265 AND 009, CORROSION ON BOTTOM OF FLOOR BEAM BS 1070 LBL 55 TO RBL 65. *S/D* REPAIRED FLOOR BEAM AT 1070 LBL 47 T O RBL 65 IAW FEDEX SRM 53-10-8. 2 L 7 3 4F RT A3WE 1996081500334 19960815 00334 NM 1996 8 15 96FDEA01297 1 19960729 A 5710 ARB0029509N CASTING DOUG MD11 MD11F 3023600 NM L/WING BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 SNRM 5020 THE L/H WING, O/B FLAP, I/B HINGE FITTING SUPPORT CASTING IS BROKEN OUT AT THE WING REAR SPAR, LOWER T ANG, WING STA XORS 560 APPROX. ******S/D ******* REPLACED L/FLAP TENSION STRAP SUPPORT WITH NEW ONE, PER MDC SB 57 -0-10 CONDITION II DATE C.W 8-12-96. 2 L 7 3 4F RT A22WE 1996081500335 19960815 00335 WP 1996 8 15 TC8A96050 1 19960730 A 2130 PRESSURIZATION DOUG DC8 DC8F54 3021926 WP CABIN MALFUNCTION A TC8A A UNSCHED LANDING O OTHER CL CLIMB 1 GL 23 802CK 45679 DISCREPANCY: UNABLE TO MAINTAIN CABINPRESSURIZATION. CORRECTIVE ACTION: FOUND AFT L/H PAX DOOR NOT SECURE.SECURED DOOR OPS CHECK GOOD. 2 L 7 4 4F 4A25 1996081500336 19960815 00336 WP 1996 8 15 CALA9601150 1 19960809 A 4920 3812761 APU DOUG DC9 DC982 3022082 WP ACFT TAIL OIL LEAK A CALA A D UNSCHED LANDING RETURN TO BLOCK B K SMOKE/FUMES/ODORS/SPARKS FLUID LOSS TO TAKEOFF 1 SW 09 17812 23757 8317 49250 A FLIGHT ATTENDANT REPORTED SMOKE ENTERED THE CABIN JUST AFTER TAKEOFF FROM DEN. THE SMOKE SOURCE WAS ISOLATED TO AIR C ONDITIONING PACKS AND THE AIRCRAFT WAS RETURNED TO DEN. MAIINTENANCE FOUND THE APU WAS BLOWING OIL UP THROUGH PLENUM IN TO THE AIR SYSTEM. THE APU WAS REMOVED AND REPLACED PER MM 49-10-00. LEAK AND OPERATIONAL CHECKS WERE GOOD. PART TOTA L CYCLES, 11,261. 2 L 7 2 4F A6WE 1996081500337 19960815 00337 WP 1996 8 15 CALA9601151 1 19960811 A 3260 UP/DNLK SWITCH DOUG DC9 DC931 3022065 WP NLG INOPERATIVE A CALA O OTHER P NO WARNING INDICATION AP APPROACH 1 SW 09 14564 47490 WHEN GEAR WAS EXTENDED ON APPROACH TO BHM NEITHER THE RED TRANSIT OR GREEN DOWN INDICATION LIGHTS FOR THE NOSE GEAR ILLU MINATED. THE GEAR WAS CYCLED WITH NO CHANGE IN INDICATION. EMERGENCY GEAR EXTENSION WAS USED TWICE BEFORE THE GREEN IND ICATION BECAME STEADY. THE AIRCRAFT LANDED AT BHM WITHOUT INCIDENT. THE NOSE GEAR UPLOCK AND DOWNLOCK SWITCHES WERE RE MOVED AND REPLACED IAW MM 32--60-1, CODE 2. BOTH SWITCHES WERE ADJUSTED AND TESTED IAW MM 32-60-0, PAGES 201-203, AND O PERATION CHECKED NORMAL. THE GEAR WAS SWUNG SIX TIMES WITH OPERATION AND INDICATIONS CHECKING GOOD. 2 L 7 2 4F A6WE 1996081500338 19960815 00338 NM 1996 8 15 CALA9601152 1 19960812 A 3350 30043213 LIGHT BOEING 737 7373T0 1384582 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17317 23368 INSPECTION FOUND THE R-1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. THE LIGHT SOCKET WAS FOUND CORRODED. THE R-1 DOOR EXTERIOR EMERGENCY LIGHT WAS REMOVED AND REPLACED. 2 L 7 2 4F RT A16WE 1996081500339 19960815 00339 WP 1996 8 15 CALA9601153 1 19960809 A 5350 CABLES DOUG DC9 DC932 3022066 WP TAILCONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 TAILCONE RELEASE USING INTERIOR HANDLE PULLED LOW AT 15 POUNDS. THE TAILCONE CABLES WERE ADJUSTED IAW MM 53-50-00. 2 L 7 2 4F A6WE 1996081500340 19960815 00340 NM 1996 8 15 CALA9601154 1 19960804 A 5320 COVER PLATE BOEING 727 727224 1384076 NM BS 1090 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND A .25 INCH CRACK IN C-3 DOOR FORWARD FRAME COVER PLATE AT B.S. 1090, STRINGER 27. THE FRAME COVER PLAT E WAS REPAIRED IAW SRM 51-40-2 AND 51-30-0. 2 L 7 3 4F A3WE 1996081500341 19960815 00341 NM 1996 8 15 CALA9601155 1 19960804 A 5532 SKIN BOEING 727 727224 1384076 NM VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND A 2 INCH CRACK IN RT SIDE VERTICAL STABILIZER EXTERNAL SKIN AT FIN STA 180, STRINGER 7. THE CRACKED SEC TION OF SKIN WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 55-30-3, FIGURE 1. 2 L 7 3 4F A3WE 1996081500342 19960815 00342 NM 1996 8 15 CALA9601156 1 19960802 A 5532 SKIN BOEING 727 727224 1384076 NM VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND TWO .25 INCH CRACKS AT FASTENER HOLES IN RIGHT SIDE VERTICAL STABILIZER EXTERNAL SKIN JUST BELOW PANEL 9516. THE PANEL WAS REMOVED FOR ACCESS. THE CRACKED SKIN WAS CUT OUT IAW SRM 54-30-3. REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 54-30-3, FIGURE 6 AND SRM 51-30-2. THE PANEL WAS REINSTALLED. 2 L 7 3 4F A3WE 1996081500343 19960815 00343 NM 1996 8 15 CALA9601157 1 19960803 A 5532 SKIN BOEING 727 727224 1384076 NM VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND A .25 INCH CRACK AT FASTENER HOLE OF LEFT SIDE VERTICAL STABILIZER EXTERNAL SKIN AT FIN STA 157 BETWEEN STRINGER S 4 AND 5. THE CRACKED SECTION OF SKIN WAS REMOVED IAW SRM 55-30-3. A REPAIR WAS FABRICATED AND INSTALLED IA W SRM 55-30-3 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996081500344 19960815 00344 NM 1996 8 15 CALA9601158 1 19960810 A 5320 INTERCOSTAL BOEING 727 727224 1384076 NM BS 1128 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND A .75 INCH CRACK IN THE UPPER AFT RADIUS OF CABIN FLOOR INTERCOSTAL AT B.S. 1128, BL ZERO. A REPAIR AN GLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996081500345 19960815 00345 NM 1996 8 15 CALA9601159 1 19960810 A 5330 SKIN BOEING 727 727224 1384076 NM FWD FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND A 3 INCH CRACK IN FUSELAGE SKIN AFT OF RADOME AT 12 O'CLOCK POSITION. THE SKIN PANEL WAS REMOVED AND A NEW SKIN PANEL WAS FABRICATED AND INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996081500346 19960815 00346 NE 1996 8 15 9617343248 2 19960810 A 7530 VBV AIRBUS 320 A320212 EU CFMINT CFM56 CFM565A3 NE NR 2 ENGINE FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 348NW 410 731773 DURING TAKEOFF ROLL, THE NR 2 ENGINE COMPRESSOR VANE MESSAGE ILLUMINATED. ABORTED TAKEOFF AT 80 KNOTS. AIRCRAFT RETURN ED TO GATE. MAINTENANCE REPLACED THE VBV ASSEMBLY AND 4 VBV DOORS, ENGINE OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A28NM E29NE 1996081500347 19960815 00347 WP 1996 8 15 9617359763 1 19960811 A 3010 HIGH TEMP SENSOR DOUG DC9 DC941 302207N WP LEFT MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 763NW 47396 AFTER TAKEOFF POWER WAS APPLIED, THE LEFT ICE PROTECTION TEMPERATURE HIGH LIGHT ILLUMINATED. NO ICE PROTECTION WAS SELE CTED ON. LIGHT REMAINED ON UNTIL HIGH PRESSURE BLEED SWITCH WAS TURNED OFF. REPLACED THE HIGH TEMPERATURE SENSOR, OPER ATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996081500348 19960815 00348 1996 8 15 9617366636 2 19960810 A 7532 BLEED VALVE BOEING 747 747251B 1384892 NM NR 4 ENGINE FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J M WARNING INDICATION OVER TEMP TO TAKEOFF 1 GL 01 636US 23547 DURING TAKEOFF (AMS), THE NR 4 ENGINE EGT WARNING AND OVERHEAT LIGHT ILLUMINATED FOLLOWED BY A NR 4 ENGINE FIRE WARNING. ABORTED TAKEOFF. REPLACED THE HIGH STAGE BLEED VALVE AND CONTROLLER. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996081500349 19960815 00349 EU 1996 8 15 9617373232 1 19960809 A 2761 31077050 ACTUATOR AIRBUS 320 A320211 3930320 EU NR 3 SPOILER RUPTURED A A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 332NW 14051 319 SHORTLY AFTER LIFT OFF, RECEIVED F/CTL SPLR 3 FAULT MESSAGE FOLLOWED BY THE BLUE HYDRAULIC SYSTEM QUANTITY AND PRESSURE DECREASING TO ZERO. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT HAND NR 3 SPOILER ACTUATOR RUPTURED. REPLACED ACTUATOR. LEAK AND OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996081500350 19960815 00350 WP 1996 8 15 9617381229 1 19960810 A 2751 96010206 TRANSMITTER DOUG DC10 DC1030 3023501 WP LT TE FLAP FAILED A NWAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 01 229NW 1420 1420 46551 DURING TAKEOFF ROLL, THE WARNING HORN SOUNDED WITH 15 DEGREE FLAPS, 21 DEGREE TRIM, AND SPEED BRAKES FULL FORWARD. MAIN TENANCE REPLACED THE LEFT OUTBOARD FLAP POSITION TRANSMITTER. 2 L 7 3 4F A22WE 1996081500351 19960815 00351 EU 1996 8 15 9617393239 1 19960810 A 3251 C20216332292C CONTROL UNIT AIRBUS 320 A320212 EU NLG STEERING FAILED A A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 339NW 7449 2131 367 DURING TAKEOFF ROLL, THE FIRST OFFICER DID NOT RECEIVE ANY RESPONSE FROM THE RUDDER PEDALS OR THE STEERING TILLER. TAKE OFF WAS ABORTED AT SLOW SPEED. AIRCRAFT RETURNED TO GATE WHERE MAINTENANCE REPLACED THE BRAKE STEERING CONTROL UNIT. O PERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996081500352 19960815 00352 EU 1996 8 15 9617403218 1 19960809 A 3230 INTERFACE UNIT. AIRBUS 320 A320211 3930320 EU LANDING GEAR FAILED A A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 318US 206 DURING APPROACH, THE LANDING GEAR DID NOT EXTEND. CYCLED LANDING GEAR HANDLE AND ALL INDICATIONS WERE NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED PROXIMITY SENSORS 35GA, 36GA, 37GA, 38GA, 39GA, AND NR 1 LANDING GEAR CO NTROL INTERFACE UNIT. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996081500353 19960815 00353 WP 1996 8 15 9617419996 1 19960804 A 5220 DOOR DOUG DC9 DC931 3022065 WP EMERGENCY EXITS OUT OF ADJUST A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8932E 47141 DURING M-CHECK, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO OPERATE ALL FOUR OVERWING EMERGENCY EXIT DOORS. ADJUSTED DO ORS PER MM 52-21-0. 2 L 7 2 4F A6WE 1996081500354 19960815 00354 SO 1996 8 15 COMA9610246 1 19960809 A 3397 WIRE EMB 120 EMB120RT 3260202 SO CABIN FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 164D 120164 EMERGENCY FLOOR LIGHTING IS DIM. REPAIRED FLOOR PATH LIGHTING WIRING AT FRAME 24. SYSTEM CHECK SATISFACTORY. 2 L 7 2 4T RT A31SO 1996081500355 19960815 00355 NM 1996 8 15 SWAA960768 1 19960801 A 3350 BATTERY BOEING 737 7373A4 1384585 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 669SW 23752 AT GATE, FOUND FLOOR EMERGENCY TRACK LIGHTS INOPERATIVE AT MID-CABIN AREA. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996081500356 19960815 00356 NM 1996 8 15 SWAA960769 1 19960801 A 3260 1061226211 UPLOCK SENSOR BOEING 737 7375H4 138449D NM RT MLG MALFUNCTIONED A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 506SW 24183 DIVERTED TO PHX DUE TO RIGHT MAIN GEAR UNSAFE LIGHT ILLUMINATING IN-FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTE D AND REPLACED RIGHT GEAR UPLOCK SENSOR PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996081500357 19960815 00357 NM 1996 8 15 SWAA960770 1 19960802 A 3260 SENSOR BOEING 737 7373H4 1384600 NM LANDING GEAR OUT OF ADJUST A SWAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 609SW 27929 AIR RETURN TO PHX DUE TO TAKEOFF WARNING INDICATION SOUNDING IN-FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED AN D ADJUSTED GROUND SHIFT SENSOR AND OPS CHECKED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996081500358 19960815 00358 NM 1996 8 15 SWAA960771 1 19960807 A 3397 WIRE BOEING 737 7372H4 138448C NM AFT GALLEY BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 59SW 21811 AT GATE, FOUND BOTH AFT EMERGENCY EXIT LIGHTS REMAINING ILLUMINATED AT ALL TIMES. REMOVED AFT GALLEY AND REPAIRED BROKE N WIRE. OPS CHECKED OK PER BOEING M/M. 2 L 7 2 4F A16WE 1996081500359 19960815 00359 NM 1996 8 15 SWAA960772 1 19960808 A 3350 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 56SW 21721 AT GATE, FOUND AFT ENTRYWAY EMERGENCY EXIT LIGHTS DIM. REPLACED LIGHT ASSEMBLY PER BOEING M/M. 2 L 7 2 4F A16WE 1996081500360 19960815 00360 NM 1996 8 15 SWAA960773 1 19960808 A 3350 1000679 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED A1 CHECK, FOUND EMERGENCY EXIT AT AFT ENTRY DOOR INOPERATIVE. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F A16WE 1996081500361 19960815 00361 NM 1996 8 15 SWAA960774 1 19960808 A 3397 WIRE BOEING 737 7372H4 138448C NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED A1 CHECK, FOUND BOTH AFT EMERGENCY EXTERIOR LIGHTS REMAINING ILLUMINATED WITH SWITCH IN ARM POSITION. R EPAIRED BROKEN WIRE AT BATTERY PACK PER BOEING M/M. 2 L 7 2 4F A16WE 1996081500362 19960815 00362 NM 1996 8 15 SWAA960775 1 19960806 A 3350 6104791 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED T-CHECK, FOUND AFT ENTRY DOOR AND AFT SERVICE DOOR EXTERIOR EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PER BOEING M/M. 2 L 7 2 4F A16WE 1996081500363 19960815 00363 NM 1996 8 15 SWAA960776 1 19960805 A 3350 900835A BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 60SW 21812 DURING SCHEDULED SV CHECK, FOUND OVERWING EXIT EXTERIOR EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PER BOEING M/M. 2 L 7 2 4F A16WE 1996081500364 19960815 00364 NM 1996 8 15 SWAA960777 1 19960807 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 360-420 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED SV CHECK, FOUND STRINGER CORRODED AROUND FASTENER HOLES FROM BS 360 TO BS 420, WL 305. REPAIRED PER BO EING SRM. 2 L 7 2 4F A16WE 1996081500365 19960815 00365 NM 1996 8 15 SWAA960778 1 19960807 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 767 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED SV CHECK, FOUND STRINGER CRACKED AT BS 767, S10R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996081500366 19960815 00366 NM 1996 8 15 SWAA960779 1 19960807 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 807 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED SV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, WL 236, LBL 68. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996081500367 19960815 00367 NM 1996 8 15 SWAA960780 1 19960807 A 5330 SKIN BOEING 737 7372H4 138448C NM PAX DOOR CUTOUT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED B1 CHECK, FOUND FORWARD ENTRY DOORWAY UPPER FORWARD RADIUS HAS A .5 INCH CRACK FROM RIVET TOWARD DOORWA Y CUT-OUT ON FUSELAGE SKIN. REPAIRED PER SWA RA 1-253-1483. 2 L 7 2 4F A16WE 1996081500368 19960815 00368 NM 1996 8 15 SWAA960781 1 19960802 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 781-800 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 83SW 22732 DURING SCHEDULED SV CHECK, FOUND 2 CRACKS ALONG S24L AND BETWEEN BS 781-800. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996081500369 19960815 00369 NM 1996 8 15 SWAA960782 1 19960804 A 5320 WEB BOEING 737 7372H4 138448C NM BS 470 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 87SW 22903 DURING SCHEDULED 1/2 D-CHECK, FOUND WEB AT BS 470 CRACKED UNDER FORWARD CARGO DOOR THRESHOLD. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996081500370 19960815 00370 NM 1996 8 15 SWAA960783 1 19960804 A 5312 BULKHEAD BOEING 737 7372H4 138448C NM BS 1020 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 87SW 22903 DURING SCHEDULED 1/2 D-CHECK, FOUND PRESSURE BULKHEAD CRACKED AT FLOOR LEVEL FORWARD AT BS 1020, RBL 37. REPAIRED PER B OEING SRM. 2 L 7 2 4F A16WE 1996081500371 19960815 00371 NM 1996 8 15 SWAA960784 1 19960731 A 2432 CA72720 BATTERY BOEING 737 7372H4 138448C NM BATTERY COMPT SHORTED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 07 90SW 22905 DURING FINAL APPROACH, FLIGHT ATTENDANT NOTED A BURNING SMELL IN FORWARD CABIN AREA. INSPECTED AND FOUND MAIN A/C BATTE RY CELLS SHORTED. REPLACED AND OPS CHECKED BATTERY AND CHARGER PER BOEING M/M. 2 L 7 2 4F A16WE 1996081500372 19960815 00372 NM 1996 8 15 SWAA960785 1 19960805 A 5315 FLOOR BEAM BOEING 737 7372H4 138448C NM BS 294.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM UPPER T-CHORD CORRODED AT BS 294.5, BBL ZERO TO LBL 8. REPAIRED PER BOEING S RM. 2 L 7 2 4F A16WE 1996081500373 19960815 00373 NM 1996 8 15 SWAA960786 1 19960805 A 5320 SUPPORTS BOEING 737 7372H4 138448C NM BS 400-520 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED D-CHECK, FOUND FLOOR TO SIDEWALL SUPPORTS CORRODED AT BS 400A TO BS 520, RBL 23, WL 156, AT BS 492, RBL 32, WL 160, AND AT BS 420 TO BS 440, RBL 23, WL 156. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996081500374 19960815 00374 NM 1996 8 15 SWAA960787 1 19960805 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 398 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 398, S24-25R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996081500375 19960815 00375 NM 1996 8 15 SWAA960788 1 19960805 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 960 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 960, S21L. REPAIRED PER TRAMCO EWO 96-0406. 2 L 7 2 4F A16WE 1996081500376 19960815 00376 NM 1996 8 15 SWAA960789 1 19960805 A 5320 DOOR FRAME BOEING 737 7372H4 138448C NM BS 440 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED D-CHECK, FOUND DOOR FRAME CRACKED AT BS 440, RBL 36.5, WL 162. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996081500377 19960815 00377 NM 1996 8 15 SWAA960790 1 19960805 A 5312 BULKHEAD WEB BOEING 737 7372H4 138448C NM BS 178 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED D-CHECK, FOUND PRESSURE BULKHEAD WEB GOUGED AT BS 178, RBL 12, WL 239. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996081500378 19960815 00378 NM 1996 8 15 SWAA960791 1 19960805 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 225 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED D-CHECK, FOUND FUSELAGE DENTED AT BS 225, S25R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996081500379 19960815 00379 NM 1996 8 15 SWAA960792 1 19960805 A 5315 FLOOR BEAM BOEING 737 7372H4 138448C NM BS 947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORRODED AT BS 947, RBL 46 TO 43, WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996081500380 19960815 00380 NM 1996 8 15 SWAA960793 1 19960805 A 5311 FRAMES BOEING 737 7372H4 138448C NM BS 294/616/639 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 616, WL 202, LBL 65, AT BS 294, RBL 54, WL 274, AND AT BS 639, WL 202, LBL 65. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996081500381 19960815 00381 NM 1996 8 15 SWAA960794 1 19960805 A 5315 FLOOR BEAM BOEING 737 7372H4 138448C NM BS 710/712 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM WEB CRACKED TWO PLACES, BS 710 AND BS 712, RBL 25, WL 203. REPAIRED PER BOEI NG SRM. 2 L 7 2 4F A16WE 1996081500382 19960815 00382 NM 1996 8 15 SWAA960795 1 19960805 A 5312 BULKHEAD ANGLE BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED D-CHECK, FOUND T-ANGLE CRACK ON AFT SIDE OF BS 178 BULKHEAD, LBL 5.5, WL 183.5. REPAIRED PER BOEING SR M. 2 L 7 2 4F A16WE 1996081500383 19960815 00383 NM 1996 8 15 SWAA960796 1 19960805 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 947-1012 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED D-CHECK, FOUND STRINGER 27L CORRODED FROM BS 947 TO BS 1012. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996081500384 19960815 00384 NM 1996 8 15 SWAA960797 1 19960805 A 5312 BULKHEAD CHORD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED D-CHECK, FOUND PRESSURE BULKHEAD CHORD CRACK AT BS 178, WL 208.5, TO WL 207, LBL 29. REPAIRED PER BOEI NG SRM. 2 L 7 2 4F A16WE 1996081500385 19960815 00385 NM 1996 8 15 SWAA960798 1 19960805 A 5320 SHEAR TIE BOEING 737 7372H4 138448C NM BS 967 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED D-CHECK, FOUND FRAME SHEAR TIE CORRODED AT BS 967, S25L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996081500386 19960815 00386 NM 1996 8 15 SWAA960799 1 19960805 A 3350 BATTERY PACK BOEING 737 7372K6 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED SV CHECK, FOUND AFT CABIN EMERGENCY TRACK LIGHTING INOPERABLE. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996081500387 19960815 00387 NM 1996 8 15 SWAA960800 1 19960805 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 727/747 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED TERM CHECK, FOUND A 3.5 INCH CRACK ON OUTER SKIN RT SIDE OF FUSELAGE, BETWEEN BS 747 AND BS 727R, AT S1 8R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996081500388 19960815 00388 NM 1996 8 15 SWAA960801 1 19960805 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED SERVICE CHECK, FOUND A 3 INCH FUSELGE SKIN CRACK FORWARD OF WATER SERV PANEL. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996081500389 19960815 00389 NM 1996 8 15 SWAA960802 1 19960805 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 877 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 329SW 23693 DURING SCHEDULED TERM CHECK, FOUND A 2 INCH FUSELAGE SKIN CRACK AT BS 877, JUST AFT OF EMERGENCY LIGHT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996081500390 19960815 00390 NM 1996 8 15 SWAA960803 1 19960805 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED SERV CHECK, FOUND A 2 INCH FUSELAGE SKIN CRACK APPROXIMATELY 10 INCHES FORWARD OF WATER SERV PANEL. R EPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996081500391 19960815 00391 NM 1996 8 15 SWAA960804 1 19960805 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 847 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN DENTED 6 INCHES AFT OF AFT CARGO DOOR AT BS 847, AT S19R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996081500392 19960815 00392 NM 1996 8 15 SWAA960805 1 19960721 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 350SW 24409 DURING SCHEDULED TERM CHECK, FOUND AFT CENTER CEILING EMERGENCY EXIT SIGN INOPERATIVE. REPLACED BATTERY AND OPS CHECKED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996081500393 19960815 00393 NM 1996 8 15 SWAA960806 1 19960803 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 224 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 380SW 26587 DURING SCHEDULED BC1 CHECK, FOUND FUSELAGE SKIN DAMAGED 13 INCHES BELOW R1 WINDOW FRAME AT BS 224. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996081500394 19960815 00394 NM 1996 8 15 SWAA960807 1 19960729 A 5240 SKIN BOEING 737 7373H4 1384600 NM FWD SERV DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 605SW 27596 DURING SCHEDULED C1 CHECK, FOUND FORWARD SERV DOOR OUTER SKIN CRACKED ABOVE SNUBBER AT L/E FORWARD SIDE. REPAIRED PER S WA RA 1-352-0252. 2 L 7 2 4F RT A16WE 1996081500395 19960815 00395 NM 1996 8 15 SWAA960808 1 19960806 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 607SW 27927 DURING SCHEDULED TERM CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE AT AFT ENTRY. RELAMPED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996081500396 19960815 00396 NM 1996 8 15 SWAA960809 1 19960805 A 5320 SHEAR TIE BOEING 737 7373A4 1384585 NM BS 927 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673AA 23251 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CORRODED AT BS 927, BETWEEN S27R AND S27L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996081500397 19960815 00397 NM 1996 8 15 SWAA960810 1 19960806 A 3350 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 507SW 24184 DURING SCHEDULED C1 CHECK, FOUND 2 FLOOR TRACK LIGHTS INOPERATIVE AT EMERGENCY EXIT ROW. RELAMPED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996081500398 19960815 00398 NM 1996 8 15 SWAA960811 1 19960806 A 5315 FLOOR BEAM BOEING 737 737317 138447P NM BS 520 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 693SW 23174 DURING SCHEDULED C2 CHECK, FOUND FLOOR BEAM CRACKED AT BS 520, RBL 26. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996081500399 19960815 00399 NM 1996 8 15 SWAA960812 1 19960806 A 5330 SKIN BOEING 737 737317 138447P NM BS 500/727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 693SW 23174 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKS AT BS 727E, AT S23R, AT 500C, LBL 24.74. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996081500400 19960815 00400 NM 1996 8 15 VNAA9607009 1 19960704 A 5610 001561A0000206 DV WINDOW DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT COCKPIT CRACKED A VNAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 437JS 18192 3055 EN ROUTE FROM PIT TO CHS, CREW REPORTED A CRACK IN THE CAPTAIN'S DIRECT VISION (DV) WINDOW. REPORTED THE PROBLEM TO DIS PATCH, WERE THEN INSTRUCTED TO RETURN TO PIT. NO EMERGENCY DECLARED, AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. PIT MX REPLACED CAPTAIN'S DV WINDOW I.A.W. M.M. 56-10-00. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996081500401 19960815 00401 NM 1996 8 15 VNAA9607010 1 19960731 A 7603 POWER LEVER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LEFT LACK OF LUBE A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 07 431JS 3028 DURING THE TAKEOFF ROLL, CREW REPORTED THAT THE LEFT HAND POWER LEVER WOULD NOT ADVANCE ABOVE THE FLIGHT IDLE GATE, CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. OUT STATION MX CLEANED AND LUBRICATED THE LEFT HAND POWER LEVER PRIMARY LOW PITCH STOP MECHANISM I.A.W. M.M. 76-10-00. GROUND RUNS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996081500402 19960815 00402 NM 1996 8 15 VNAA9607011 1 19960731 A 2931 APTE1331000300BA TRANSDUCER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE HYD PACK DEFECTIVE A VNAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 07 434JS 23585 3051 EN ROUTE FROM PIT TO HUN, CREW REPORTED BEING ALERTED BY A HYDRAULIC LOW PRESSURE C.A.S. MESSAGE. THIS WAS FOLLOWED ALM OST IMMEDIATELY BY A STAND-BY PRESSURE SYSTEM FAIL C.A.S. MESSAGE. AIRCRAFT DIVERTED TO BDL, LANDED WITHOUT FURTHER INC IDENT. AIRCRAFT WAS LATER FERRIED FROM BDL TO CAK. MAINTENANCE REPLACED THE HYDRAULIC PRESSURE TRANSDUCER I.A.W. M.M. 29-31-03, GROUND CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996081500404 19960815 00404 NM 1996 8 15 96FDEA01351 1 19960725 A 5744 ARB00295108 STRAP DOUG MD11 MD11F 3023600 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 601FE 48401 RIGHT WING OUTBOARD FLAP, INBOARD HINGE TENSION STRAP SUPPORT CRACKED AT LOWER ATTACH BOLT HOLE, LOWER SURFACE (EXTERNA L) STA X ODRSX562390. REPLACED RIGHT FLAP TENSION STRAP SUPPORT WITH NEW PART PER MDC SB 57-0-10 CONDITION II AND C/W EA 1-5710-29039. 2 L 7 3 4F RT A22WE 1996081500405 19960815 00405 NM 1996 8 15 96FDEA01352 1 19960812 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 FORWARD CARGO BS 720 STR 23R HEAVY CORROSION INSIDE STRINGER ON LOWER LEG. REMOVED CORROSION AND INSTALLED STRINGER RE PAIR PER SRM 53-10-3. 2 L 7 3 4F A3WE 1996081500406 19960815 00406 NM 1996 8 15 96FDEA01353 1 19960812 A 5315 FLOOR BEAM BOEING 727 72722C 138400F NM BS 312 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 MAIN CARGO CORROSION ON FLOOR BEAM AT STA 312 LBL 19. INSTALLED AND COMPLETED FLOOR BEAM REPAIR STA 312 LBL 19 PER SRM 53-10-8. 2 L 7 3 4F A3WE 1996081500407 19960815 00407 NM 1996 8 15 VNAA9608002 1 19960806 A 3240 ACCUMULATOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE PARKING BRAKE REQD SERVICE A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 434JS 3051 DURING CLIMB-OUT, CREW REPORTED BEING ALERTED BY AN EMERGENCY/PARKING BRAKE ACCUMULATOR PRESS LOW CAS MESSAGE. CREW ELE CTED TO RETURN TO THE FIELD, AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. PIT MX SERVICED THE PARKING BRAKE ACCUMULATOR I. A.W. M.M. 12-00-00. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996081500408 19960815 00408 NM 1996 8 15 P5CA9600473 1 19960807 A 5320 SUPPORT BOEING 747 747122 1384872 NM E/E COMPT BENT A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FORWARD CARGO AFT E AND E COMPARTMENT, RIGHT SIDE 3RD ROW SHELF BURNDY SUPPORT RAIL NEEDS TO BE REALIGNED DUE TO SLIGHT DISTORTION. STRAIGHTENED PER BOEING SRM 51-10-01, PAGE 11. 2 L 7 4 4F A20WE 1996081500409 19960815 00409 NM 1996 8 15 P5CA9600474 1 19960807 A 5320 SUPPORT BOEING 747 747122 1384872 NM E/E COMPT BENT A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FORWARD CARGO AFT E AND E COMPARTMENT 2ND ROW SHELF BURNDY SUPPORT RAIL NEEDS TO BE REALIGNED DUE TO SLIGHT DISTORTION. STRAIGHTENED PER BOEING SRM 51-10-01, PAGE 11. 2 L 7 4 4F A20WE 1996081500410 19960815 00410 NM 1996 8 15 P5CA9600475 1 19960807 A 5320 SUPPORT BOEING 747 747122 1384872 NM E/E COMPT BENT A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FORWARD CARGO AFT E AND E COMPARTMENT, CENTER SECTION 3RD ROW SHELF BURNDY SUPPORT RAIL NEEDS TO BE REALIGNED DUE TO SLI GHT DISTORTION. STRAIGHTENED PER BOEING SRM 51-10-01. 2 L 7 4 4F A20WE 1996081500411 19960815 00411 NM 1996 8 15 P5CA9600476 1 19960807 A 5320 SUPPORT BOEING 747 747122 1384872 NM E/E COMPT BENT A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FORWARD CARGO AFT E AND E COMPARTMENT, LEFT SIDE 2ND ROW BURNDY SUPPORT RAIL NEEDS TO BE REALIGNED DUE TO SLIGHT DISTORT ION. STRAIGHTENED PER BOEING SRM 51-10-01, PAGE 11. 2 L 7 4 4F A20WE 1996081500412 19960815 00412 NM 1996 8 15 P5CA9600477 1 19960807 A 5320 SUPPORT BOEING 747 747122 1384872 NM E/E COMPT BENT A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FORWARD CARGO AFT E AND E COMPARTMENT, LEFT SIDE 3RD ROW BURNDY BLOCK SUPPORT RAIL NEEDS TO BE REALIGNED DUE TO SLIGHT D ISTORTION. STRAIGHTENED PER BOEING SRM 51-10-01, PAGE 11. 2 L 7 4 4F A20WE 1996081500413 19960815 00413 NM 1996 8 15 P5CA9600478 1 19960807 A 5320 SUPPORT BOEING 747 747122 1384872 NM E/E COMPT BENT A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FORWARD CARGO AFT E AND E COMPARTMENT, LEFT SIDE 4 TH ROW BURNDY SUPPORT RAIL NEEDS TO BE REALIGNED DUE TO SLIGHT DISTOR TION. STRAIGHTENED PER BOEING SRM 51-10-01, PAGE 11. 2 L 7 4 4F A20WE 1996081500414 19960815 00414 NM 1996 8 15 P5CA9600479 1 19960807 A 5320 BRACKET BOEING 747 747122 1384872 NM E/E COMPT BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FORWARD CARGO E AND E COMPARTMENT RIB FOR CANNON PLUGS BETWEEN RIGHT AND CENTER SECTION SUPPORT BRACKET BROKEN. REPLACE D PER BOEING SRM 51-10-01. 2 L 7 4 4F A20WE 1996081500415 19960815 00415 NM 1996 8 15 P5CA9600480 1 19960807 A 5320 SUPPORT BOEING 747 747122 1384872 NM E/E COMPT BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FORWARD CARGO E AND E COMPARTMENT MOST OUTBOARD CANNON PLUG RIB SUPPORT RIB BROKEN. REPAIRED VERTICAL SUPPORT PER BOEIN G SRM 51-10-01 AND SRM 51-40-03. 2 L 7 4 4F A20WE 1996081500416 19960815 00416 NM 1996 8 15 P5CA9600481 1 19960807 A 5320 SUPPORT BOEING 747 747122 1384872 NM E/E COMPT CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FORWARD CARGO AFT E AND E COMPARTMENT, RIB WHICH HOLDS CANNON PLUGS BETWEEN LEFT AND CENTER SECTIONS, CRACKED AND BROKEN . REPAIRED PER BOEING SRM 51-10-01 AND SRM 51-40-03. 2 L 7 4 4F A20WE 1996081500417 19960815 00417 NM 1996 8 15 P5CA9600482 1 19960807 A 5320 BRACKET BOEING 747 747122 1384872 NM E/E COMPT BENT A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FORWARD CARGO AFT E AND E COMPARTMENT, LEFT SIDE OUTBOARD RIB FOR CANNON PLUGS SUPPORT BRACKET BENT. REPLACED PER BOEIN G SRM 51-10-01. 2 L 7 4 4F A20WE 1996081500418 19960815 00418 NM 1996 8 15 P5CA9600483 1 19960807 A 5230 SEAL DEPRESSOR BOEING 747 747122 1384872 NM CARGO DOOR DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FORWARD CARGO DOOR, SEAL DEPRESSOR DAMAGED FORWARD LOWER SIDE. REPLACED DAMAGED SECTION PER BOEING SRM 51-10-01. 2 L 7 4 4F A20WE 1996081500419 19960815 00419 NE 1996 8 15 ARWA9608002 2 19960810 A 7250 675803 T3 DISC PWA JT3D7 DOUG DC8 DC862 3021970 WP PWA JT3D JT3D7 52039 NE NR 4 ENGINE CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 810BN 14021 669162 45905 669162 DURING ROUTINE ACCOMPLISHMENT OF AD 82-14-02, ENGINE S/N 669162, NR 4 POSITION, EDDY CURRENT INSPECTION INDICATED T3 DIS K CRACKED THROUGH ONE TIEBOLT HOLE. T3 DISK ASSEMBLY WAS REMOVED AND REPLACED I.A.W. OA 1349 AND JT3D MAINTENANCE MANUA L CHAPTER 72. INSTALLED P/N 797903, S/N MLDAH 1052. PART TOTAL CYCLES, 5,482. 2 L 7 4 4F 4 F 4A25 1E8 1996081500420 19960815 00420 1996 8 15 ARWA9608003 4 19960813 A 3421 2589201901 INSTRUMENT AMP DOUG DC8 DC862 3021970 WP NR 2 GYRO FAILED A ARWA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 19 802BN 45909 EN ROUTE FROM JFK TO SJU, NR 2 ADI GYRO FLAG IN VIEW. RESET CIRCUIT BREAKER, NO HELP. INTERMITTENT FLAG IN CRUISE, FLA G IN VIEW AT ALL TIMES DURING DESCENT, DIVERTED TO MIA. REMOVED AND REPLACED NR 2 INSTRUMENT AMP. SYSTEM OPS NORMAL I. A.W. DC-8 MM 34-25-00. 2 L 7 4 4F 4A25 1996081500421 19960815 00421 SO 1996 8 15 SRAA960806 1 19960813 A 2612 892541100 CONTROL UNIT LKHEED 382 382G 526414U SO NR 3 ENGINE DEFECTIVE A SRAA K NONE N FALSE WARNING IN INSP/MAINT 1 GL 23 909SJ 4763 DURING PRE-FLIGHT, NR 3 FIRE HANDLE AND MASTER DISPLAY FLASHED INTERMITTENTLY WITHOUT NR 3 ENGINE RUNNING. FOUND NR 3 E NGINE FIRE CONTROL UNIT DEFECTIVE, REPLACED FIRE CONTROL UNIT, SYSTEM CHECKED GOOD PER M.M. CH 26. 2 H 7 4 4T A1SO 1996081500422 19960815 00422 NM 1996 8 15 AWXA960270 1 19960612 A 2120 65C256299 CABIN MUFFLER BOEING 737 73733A 1384673 NM AIR DISTR SYSTEM FAILED A A AWXA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 28 164AW 10833 23625 PHX/COS - FLT 2412 - AIR TURNBACK. ON CLIMB-OUT, A/C SYSTEM STARTED BLOWING EXTREMELY HIGH PRESSURE AIR OUT OF ALL AIR DUCTS IN THE COCKPIT. REMOVED AND REPLACED CONTROL CABIN MUFFLER. REMOVED AND REPLACED TURBO FAN. RAN BOTH PACKS WIT H ENGINE BLEEDS. FLIGHT DECK AIR DISTRIBUTION SYSTEM NORMAL. PART TOTAL CYCLES, 8,039. REFERENCE: OPERATOR CONTROL NR 96ZZZX3991. (X) 2 L 7 2 4F RT A16WE 1996081500423 19960815 00423 NM 1996 8 15 96ZZZX3991 1 19960612 A 2121 8012403 TURBO FAN BOEING 737 73733A 1384673 NM AIR DISTR SYSTEM FAILED A AWXA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 28 164AW 10833 42973 23625 PHX/COS - FLT 2412 - AIR TURNBACK. ON CLIMB-OUT, A/C SYSTEM STARTED BLOWING EXTREMELY HIGH PRESSURE AIR OUT OF ALL AIR DUCTS IN THE COCKPIT. REMOVED AND REPLACED CONTROL CABIN MUFFLER. REMOVED AND REPLACED TURBO FAN. RAN BOTH PACKS WIT H ENGINE BLEEDS. FLIGHT DECK AIR DISTRIBUTION SYSTEM NORMAL. PART TOTAL CYCLES, 8,039. REFERENCE OPERATOR CONTROL N R AWXA960270. 2 L 7 2 4F RT A16WE 1996081500424 19960815 00424 NM 1996 8 15 AWXA960272 1 19960610 A 5320 65C807351 MOPSILL BOEING 737 73733A 1384673 NM BS 947-990 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 PAE - FLT 7829 - DURING ROUTINE SCHEDULED C-13 MAINTENANCE CHECK, FOUND CORROSION ON MOPSILL AT ASD STA 947 - STA 990, W L 208. REMOVED AND REPLACED ASD MOPSILL IAW SRM'S 5120-01, 51-40-02, AND 51-40-08. (X) 2 L 7 2 4F RT A16WE 1996081500425 19960815 00425 NM 1996 8 15 AWXA960273 1 19960601 A 5315 FLOOR BEAM BOEING 737 73733A 1384673 NM BS 967 CORROSION A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 PAE - FLT 7829 - DURING ROUTINE SCHEDULED C-13 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM STA 967, LBL 5 - LBL 28, WL 208. REPAIRED TOP CHORD OF FLOOR BEAM AT STA 967, BL ZERO - LBL 36 IAW 737-300, SRM 53-00-51. (X) 2 L 7 2 4F RT A16WE 1996081500426 19960815 00426 NM 1996 8 15 AWXA960274 1 19960610 A 5330 SKIN BOEING 737 73733A 1384673 NM BS 344-380 GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 PAE - FLT 7829 - DURING ROUTINE SCHEDULED C-13 MAINTENANCE CHECK, FOUND FUSELAGE LAP SEAM GOUGED AT BS 344 - BS 380, STR 19R. APPROXIMATE DIMENSIONS 31 INCHES BY 70 INCHES WIDE B .018 INCHES DEEP. REPAIRED AREA IAW SRM 53-00-01. (X) 2 L 7 2 4F RT A16WE 1996081500427 19960815 00427 NM 1996 8 15 AWXA960275 1 19960612 A 5315 FLOOR BEAM BOEING 737 73733A 1384673 NM BS 987 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 PAE - FLT 7829 - DURING ROUTINE SCHEDULED C-13 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM STA 987, LBL 28 - RBL 26 , WL 208. REMOVED, FABRICATED, INSTALLED REPAIR PARTS PER SRM 53-60-51. (X) 2 L 7 2 4F RT A16WE 1996081500428 19960815 00428 NM 1996 8 15 AWXA960276 1 19960604 A 5315 FLOOR BEAM BOEING 737 73733A 1384673 NM BS 1006 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 173AW 23632 PAE - FLT 7829 - DURING ROUTINE SCHEDULED C-13 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM STA 1006, RBL 10, WL 208 . REMOVED CORRODED SECTION AT BS 1006, LBL 15 TO RBL 45, WL 208. FABRICATED PARTS, ALODINED, PRIMED, AND INSTALLED PER SRM 53-00-51, SRM 53-60-5. (X) 2 L 7 2 4F RT A16WE 1996081500429 19960815 00429 NM 1996 8 15 AWXA960277 1 19960607 A 5330 SKIN BOEING 737 73733A 1384673 NM BS 262 LIGHTNING STRIKE A AWXA K NONE C F.O.D. IN INSP/MAINT 1 WP 28 173AW 23632 PAE - FLT 7829 - DURING ROUTINE SCHEDULED C-13 MAINTENANCE CHECK, FOUND LIGHTNING STRIKE ON SKIN AT BS 262 BETWEEN STR 6 AND STR 7 LT. CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND FILLER, ALODINED AND PRIMED PER SRM 53-00-01. (X) 2 L 7 2 4F RT A16WE 1996081500430 19960815 00430 NM 1996 8 15 AWXA960286 1 19960614 A 5315 FLOOR BEAM BOEING 737 7373G7 1384595 NM BS 967 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 311AW 24712 PAE - FLT 7807 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM AT STA 967, WL 208. REMO VED CORRODED FLOOR BEAM AND REPAIRED BEAM PER SRM 53-00-51, BS 767, LBL 1.5 - LBL 56. (X) 2 L 7 2 4F RT A16WE 1996081500431 19960815 00431 NM 1996 8 15 AWXA960287 1 19960613 A 5315 BAC1505100880 FLOOR BEAM BOEING 737 7373G7 1384595 NM BS 987 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 311AW 24712 PAE - FLT 7807 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM STA 987, WL 208, LBL ZERO , 20, 46, AND RBL 22. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIRED PARTS PER E.R. 3-53-15-07. (X) 2 L 7 2 4F RT A16WE 1996081500432 19960815 00432 NM 1996 8 15 AWXA960288 1 19960612 A 5315 FLOOR BEAM BOEING 737 7373G7 1384595 NM BS 294.5 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 311AW 24712 PAE - FLT 7807 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CORROSION ON TOP CHORD OF FLOOR BEAM BS 294.5, RL B 28 - RBL 35, WL 208. REMOVED CORRODED SECTION OF FLOOR BEAM, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-51. (X) 2 L 7 2 4F RT A16WE 1996081500433 19960815 00433 NM 1996 8 15 AWXA960292 1 19960626 A 2761 65449617 ACTUATOR BOEING 737 737277 1384570 NM NR 8 SPOILER CRACKED A AWXA O H OTHER DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 WP 28 185AW 43044 1883 22652 PHX/SFO - FLT 2604 - PRESSURE AND QUANTITY DROPPED TO ZERO SHORTLY AFTER LANDING AND DURING TAXI. NR 1 AND NR 2 ENGINE DRIVEN HYDRAULIC LOW PRESSURE LIGHTS ILLUMINATED THEN BOTH PUMPS WERE TURNED OFF WITHIN APPROXIMATELY 30 SECONDS. NR 2 ENGINE WAS SHUT DOWN. FOUND NR 8 GROUND SPOILER ACTUATOR HOUSING CRACKED. SENT TECHNICIANS AND PARTS FROM PHX. REMOVE D AND REPLACED NR 8 GROUND SPOILER ACTUATOR PER AWA TASK CARD R3M27016. OPERATIONS AND LEAK CHECKS GOOD. PARTS TOTAL CYCLES, 36,944. (X) 2 L 7 2 4F RT A16WE 1996081500434 19960815 00434 NM 1996 8 15 AWXA960294 1 19960624 A 3610 39266411 PRECOOLER VALVE BOEING 737 737112 1384412 NM NR 1 ENGINE FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 708AW 13322 19771 PHX/SJC - FLT 2886 - AIR TURNBACK. UNABLE TO PRESSURIZE AIRCRAFT WITH SINGLE PACK ON CLIMB-OUT. BLEED AIR LEAK UNDER B LOW-OUT DOOR NR 1, ENGINE NR 1 KRUGER FLAP AT DUCT CLAMP. RETORQUED CLAMP.4 REMOVED AND REPLACED NR 2 ENGINE PRE-COOLE R VALVE PER MM 36-00-00. REMOVED AND REPLACED NR 1 ENGINE 13TH STAGE REGULATOR PER MM 21-11-31. CABIN AIR LEAK AFT LEF T FUSELAGE AT LAP JOINT 2 PLACES ADJACENT TO PORTABLE WATER SERVICE PANEL. REMOVED PREVIOUS REPAIR, REPAIRED PER SRM 53 -30-3 F. 16. E/E COOLING EXHAUST VALVE NOT CLOSING ALLTHE WAY. REMOVED AND REPLACED COOLING EXHAUST VALVE. REFERENCE: OPERATOR CONTROL NR 96ZZZX3992. (X) 2 L 7 2 4F A16WE 1996081500435 19960815 00435 NM 1996 8 15 96ZZZX3992 1 19960624 A 3610 39268631 REGULATOR BOEING 737 737112 1384412 NM 13TH STAGE FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 708AW 19771 PHX/SJC - FLT 2886 - AIR TURNBACK. UNABLE TO PRESSURIZE AIRCRAFT WITH SINGLE PACK ON CLIMB-OUT. BLEED AIR LEAK UNDER B LOW-OUT DOOR NR 1, ENGINE NR 1 KRUGER FLAP AT DUCT CLAMP. RETORQUED CLAMP. REMOVED A4ND REPLACED NR 2 ENGINE PRE-COOLE R VALVE PER MM 36-00-00. REMOVED AND REPLACED NR 1 ENGINE 13TH STAGE REGULATOR PER MM 21-11-31. CABIN AIR LEAK AFT LEF T FUSELAGE AT LAP JOINT 2 PLACES ADJACENT TO PORTABLE WATER SERVICE PANEL. REMOVED PREVIOUS REPAIR, REPAIRED PER SRM 53 -30-3 F. 16. E/E COOLING E4XHAUST VALVE NOT CLOSING ALLTHE WAY. REMOVED AND REPLACED COOLING EXHAUST VALVE. TOTAL CYC LES, 2,757. REFERENCE: OPERATOR CONTROL NR AWXA960294. 2 L 7 2 4F A16WE 1996081500436 19960815 00436 NM 1996 8 15 AWXA960296 1 19960629 A 2120 S210N7012 LOW FLOW SENSOR BOEING 737 73733A 1384673 NM EQUIP COOLING FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 175AW 1780 23634 PHX/MCI - FLT 2590 - AIR TURNBACK. EQUIPMENT COOLING EXHAUST OFF LIGHT ILLUMINATED ABOVE 8,000 FEET. REMOVED AND REPLA CED LOW FLOW SENSOR T464, IAW 21-58-45. OPS CHECK GOOD IAW 21-58-03. REMOVED AND REPLACED AIR FLOW SENSOR M10. OPS CH ECKS GOOD. REFERENCE: OPERATOR CONTROL NR 96ZZZX3993. (X) 2 L 7 2 4F RT A16WE 1996081500437 19960815 00437 NM 1996 8 15 96ZZZX3993 1 19960629 A 2120 S210N7012 AIR FLOW SENSOR BOEING 737 73733A 1384673 NM EQUIP COOLING FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 175AW 1803 23634 PHX/MCI - FLT 2590 - AIR TURNBACK. EQUIPMENT COOLING EXHAUST OFF LIGHT ILLUMINATED ABOVE 8,000 FEET. REMOVED AND REPLA CED LOW FLOW SENSOR T464, IAW 21-58-45. OPS CHECK GOOD IAW 21-58-03. REMOVED AND REPLACED AIR FLOW SENSOR M10. OPS CH ECKS GOOD. REFERENCE: OPERATOR CONTROL NR AWXA960296. 2 L 7 2 4F RT A16WE 1996081500438 19960815 00438 NM 1996 8 15 AWXA960297 1 19960629 A 2700 FLIGHT CNTRL SYS BOEING 737 7373G7 1384595 NM WINGS MALFUNCTIONED A A AWXA O OTHER F FLT CONT AFFECTED DE DESCENT 1 WP 28 303AW 24010 BUR/PHX - FLT 2545 - UNCOMMANDED ROLL TO LEFT ON DESCENT. 1,800 FEET AUTOPILOT ON VNAV AND LNAV JUST STOWED SPEED BRAKE AND ACFT ROLLED VIOLENTLY TO LEFT. HAPPENED 2ND TIME WITH A/P OFF HAND FLYING. C/W BITE AND FUNCTION CHECK, NO DEFECT S NOTED. C/W BOTH A8M27001 AND A8M27002, RUDDER PCU FUNCTION CHECKS, NO DEFECTS. RUDDER PCU CYCLE TEST, NO DEFECTS NOT ED. RUDDER PCU INTERNAL LEAK CHECK FOR T/S. NO DEFECTS. VISUALLY INSPECTED AILERONS, SPOILERS, AND FLAPS. NO PHYSICA L DEFECTS NOTED. ALL OPS NORMAL AT THIS TIME. CONDUCTED TEST FLIGHT AS REQUIRED. CONTROL AND SPOILERS NORMAL ALL MODE S. NO DEFECTS NOTED. FLT CHK CONDUCTED UNDER FAR 91. (X) 2 L 7 2 4F RT A16WE 1996081500439 19960815 00439 NM 1996 8 15 AWXA960298 1 19960701 A 3230 CIRCUIT BREAKER BOEING 737 73733A 1384673 NM LANDING GEAR TRIPPED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 175AW 23634 PHX/LAX - FLT 2039 - AIR TURNBACK. AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. USED OVERRIDE TO RETRACT GEARS. (LE VER LATCH CIRCUIT BREAKER WAS FOUND POPPED OUT ON ARRIVAL PHX.) JACKED AIRCRAFT AND CYCLED GEAR 4 TIMES, NO FAULTS NOTE D. (X) 2 L 7 2 4F RT A16WE 1996081500440 19960815 00440 NE 1996 8 15 AWXA960320 2 19960705 A 7200 ENGINE BOEING 737 7372M8 1384483 NM PWA JT8 JT8D9A 52048 NE NR 1 OVERTEMP A A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 141AW 44314 3159 21955 687715 PHX/ONT - FLT 2622 - AIR TURNBACK. NR 1 ENGINE OIL TEMPERATURE CLIMBED TO 118 DEGREES AT CRUISE, 123 CELSIUS ON DESCENT , 140 CELSIUS FOR 10 MINUTES AT 110 FEET. POWER UP TEMPERATURE NORMAL. REMOVED AND REPLACED NR 1 ENGINE PER R5M71003, RIGGED PER CARD F5M76001 AND TRIMMED PER CARD F5M71002. ENGINE TOTAL CYCLES, 51,823. (X) 2 L 7 2 4F 4 F A16WE E2EA 1996081500441 19960815 00441 NM 1996 8 15 AWXA960321 1 19960705 A 2913 5718607 HYDRAULIC PUMP BOEING 737 7373G7 1384595 NM 'A' SYSTEM FAILED A AWXA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 28 158AW 30166 9131 182894 23780 PHX - FLT 2830 - GATE RETURN. A-SYSTEM ELECTRIC PUMP FAILED ON TAXI OUT. OVERHEAT AND LOW PRESSURE LIGHTS ILLUMINATED. REMOVED AND REPLACED A-SYSTEM ELECTRIC HYDRAULIC PUMP PER CARD R4M29002. OPS AND LEAK CHECK GOOD. PART TOTAL CYCLES, 24,482. (X) 2 L 7 2 4F RT A16WE 1996081500442 19960815 00442 NM 1996 8 15 AWXA960322 1 19960703 A 2782 654465114 ACTUATOR BOEING 737 737275 1384485 NM NR 2 LE FLAP DAMAGED A AWXA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 28 CGAPW 40057 0137 20922 ICT/PHX - FLT 1103 - LOSS OF A-SYSTEM HYDRAULIC FLUID. CONTRACT MAINTENANCE FOUND NR 2 LEADING EDGE SLAT ACTUATOR DAMAG ED. REMOVED AND REPLACED ACTUATOR PER R3M27020. OP CHECK NORMAL. INSPECTED HYDRAULIC FILTERS PER MM 2911-0. NO CONTA MINATION FOUND. PHX MAINTENANCE RE-INSPECTED INSTALLATION PER BMM 27. OK FOR SERVICE. PART TOTAL CYCLES, 34,587. (X) 2 L 7 2 4F A16WE 1996081500443 19960815 00443 NM 1996 8 15 AWXA960324 1 19960703 A 5755 654645161B SKIN BOEING 737 737277 1384570 NM NR 7 SPOILER DELAMINATION A A AWXA O OTHER F FLT CONT AFFECTED CR CRUISE 1 WP 28 186AW MA5407 22653 LAS - FLT 2022 - AIRCRAFT ROLLS LEFT WITH FLAPS EXTENDED. REQUIRES 10-15 UNITS OF AILERON FOR LEVEL FLIGHT. ALL POSITI ONS INDICATE NORMAL. FOUND NR 7 FLIGHT SPOILER TO HAVE 50 PERCENT SURFACE DELAMINATION. REMOVED AND REPLACED NR 7 SPOI LER PANEL, IAW BMM 27-61-11. (X) 2 L 7 2 4F RT A16WE 1996081500444 19960815 00444 NM 1996 8 15 AWXA960325 1 19960703 A 2721 RUDDER TRIM BOEING 737 737277 1384570 NM VERTICAL STAB OUT OF ADJUST A A AWXA K NONE F FLT CONT AFFECTED CL CLIMB 1 WP 28 186AW 22653 PHX - FLT 2450 - AIRCRAFT ROLLS LEFT ALL FLIGHT REGIMES - CLIMB. RUDDER TRIM ZERO 5-8 DEGREES AILERON NEEDED. .75 DEGR EES RIGHT RUDDER CORRECTION AILERON ZERO BALL DISPLACEMENT. LEFT CRUISE RUDDER TRIM ZERO 5 DEGREES. AILERON RIGHT TRIM 15-20 RIGHT AILERON ON APROACH. VISUAL CHECKED SPOILERS FOR DELAMINATION, FIT AND FARE. NO DEFECTS NOTED VISUALLY. C HECKED RUDDER, NO DEFECTS NOTED. CHECKED FLAPS FOR SECURITY AND DELAMINATION. (X) 2 L 7 2 4F RT A16WE 1996081500445 19960815 00445 NM 1996 8 15 AWXA960328 1 19960706 A 3244 TIRES BOEING 737 737277 1384570 NM NR 1 MLG BLEW OUT A AWXA O OTHER O OTHER LD LANDING 1 WP 28 184AW 43055 22651 PHX/SFO - FLT 2605 - SFO REPORTED AIRCRAFT INBOUND HAD BLOWN BOTH NR 1 AND NR 2 MLG TIRES ON LANDING. ACFT SUSTAINED DA MAGE TO INBD FLAPS AND TO LT GEAR DOORS. UNITED INSPECTED ACFT AND REPLACED TIRES. ACFT FERRIED TO PHX. REMOVED AND R EPLACED NR 2 L/E TAIL GATE ASSY. OTBD AND T/E AND INBD AND T/E FLAPS INSTALLED. REMOVED AND REPLACED NR 2 FLAP FAIRING SEQ TRACK. REMOVED AND REPLACED LOWER PIE PANEL. REMOVED AND REPLACED ALL 3 GEAR DOORS. REMOVED AND REPLACED NR 1 BR AKE METERING VALVE. REMOVED AND REPLACED BRAKE VALVE ACTUATOR. PART TC: 36,637. (X) 2 L 7 2 4F RT A16WE 1996081500446 19960815 00446 CE 1996 8 15 96ZZZM1188 1 19960715 A 7810 11495000033 EXHAUST STACK BEECH 1900 1900C 1154161 CE LT ENGINE CRACKED A GUUA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 19 11ZR UB11 FLT 460 - TCB-MIA - LEFT FIRE HANDLE ILLUMINATED DURING TAXI, STAYED ILLUMINATED FOR APPROXIMATELY 4 MINUTES THEN WENT O UT. NO OTHER INDICATION OF FIRE. DETERMINED EXHAUST STACK TO BE CRACKED. REMOVED AND REPLACED EXHAUST. (M) 2 L 7 2 4T RT A24CE 1996081500447 19960815 00447 CE 1996 8 15 96ZZZM1189 1 19960719 A 3260 IEN516 DNLOCK SW BEECH 1900 1900C 1154161 CE RT MLG CHATTERING A GUUA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 19 259AF UB55 GEAR SHOWS THREE GREEN, BUT GEAR HANDLE LIGHTS IS ILLUMINATED. REMOVED AND REPLACED RIGHT DOWNLOCK SWITCH. 2 L 7 2 4T RT A24CE 1996081500448 19960815 00448 NM 1996 8 15 96ZZZM1190 1 19960717 A 2611 303268 AMPLIFIER BOEING 747 747124 1384874 NM CARGO COMPT MALFUNCTION A TWRA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 EA 15 602FF 30950 19734 IN CRUISE AT FL 390, LOWER FWD CARGO FIRE WARNING (BELL/LIGHTS) CAME ON. WHEN FIRE BOTTLE NR 1 WAS DISCHARGED, FIRE WAR NING LIGHTS WENT OUT IMMEDIATELY. FM VOL, 1 PAGE 2.12.2 PROCEDURE WAS ACCOMPLISHED SUSPECTED FAULTY WARNING SYSTEM. F/ E MADE PHYSICAL INSPECTION OF CARGO COMPARTMENT IN FLIGHT AND FOUND NO EVEIDENCE OF HEAT, FIRE OR SMOKE. MAINTENANCE IN SPECTED THE AREA, FOUND NO EVIDENCE OF HEAT, FIRE OR SMOKE. FOUND TO BE AN INDICATION PROBLEM. REMOVED AND REPLACED DE TECTOR, SMOKE DETECTOR AMPLIFIER. OPS CHECK NORMAL PER MM 26-16-11. AIRCRAFT RETURNED TO SERVICE. REFERENCE TWRA96178 . 2 L 7 4 4F A20WE 1996081500449 19960815 00449 NM 1996 8 15 96ZZZM1191 1 19960717 A 3350 ML7715 BULB BOEING 747 747238B 1384828 NM CABIN MISSING A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 607PE 20011 DURING DAILY CHECK, FOUND ROW 58C EVAC LIGHT MISSING. REPLACED LENS AND BULB, OPS CHECK OK PER MM 33-51-00. REFERENCE TWRA96186. 2 L 7 4 4F A20WE 1996081500450 19960815 00450 NM 1996 8 15 96ZZZM1192 1 19960715 A 3350 ML7715 BULB BOEING 747 747212B 1384886 NM CABIN BROKEN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 620FF 21162 DURING DAILY CHECK, FOUND BROKEN EVAC LIGHTS AT SEAT 27C. REPLACED EMERGENCY LIGHT CAP AND BULB. OPS CHECK OK PER MM 3 3-51-00. REFERENCE TWRA96194. 2 L 7 4 4F A20WE 1996081500451 19960815 00451 NM 1996 8 15 96ZZZM1193 1 19960713 A 3350 ML7715 BULB BOEING 747 747212B 1384886 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND EVAC FLOOR LIGHT OUT. FORWARD OF L2 JUMP SEAT (2ND LIGHT). REPLACED EMERGENCY LIGHT CAP AND BULB. OPS CHECK OK PER MM 33-51-00. REFERENCE TWRA96149. 2 L 7 4 4F A20WE 1996081500452 19960815 00452 NM 1996 8 15 96ZZZM1194 1 19960716 A 3350 ML7715 BULB BOEING 747 747212B 1384886 NM SEAT FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND SEAT 53ABC LENS AND BULB MISSING. REPLACED LENS AND BULB, OPS CHECK NORMAL PER MM 33-51-00. R EFERENCE TWRA96168. 2 L 7 4 4F A20WE 1996081500453 19960815 00453 NM 1996 8 15 96ZZZM1195 1 19960716 A 3350 ML7715 BULB BOEING 747 747212B 1384886 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND EVAC FLOOR CAP AND BULB INOP SEAT 50H. REPLACED CAP AND BULB, OPS CHECK OK PR MM 33-51-00. R EFERENCE TWRA96171. 2 L 7 4 4F A20WE 1996081500454 19960815 00454 WP 1996 8 15 96ZZZM1196 1 19960708 A 5347 SEAT TRACK DOUG DC9 DC934 302207E WP BS 200-206 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 936L 47711 STL - DURING OP-19, FOUND CORROSION ON LEFT INBOARD SEAT TRACK, STATION 200-206. REPLACED SEAT TRACK PER SRM 53-03, PAG E 10G, SHEET 1, FIGURE 4F. (M) 2 L 7 2 4F RT A6WE 1996081500455 19960815 00455 WP 1996 8 15 96ZZZM1197 1 19960706 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 89 DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 STL - DURING SPECIAL CHECK, FOUND DENT ABOVE EXTERNAL POWER DOOR, STATION 89, LONGERON 17L. CUT OUT DAMAGED SKIN AND RE PAIRED PER SRM 53-04, FIGURE 12B. TOTAL AIRCRAFT TIME 71,703, TOTAL CYCLES 77,896. 2 L 7 2 4F A6WE 1996081500456 19960815 00456 WP 1996 8 15 96ZZZM1198 1 19960703 A 3260 PROX ELECT UNIT DOUG DC9 DC982 3022082 WP NLG FAILED A TWAA O OTHER N FALSE WARNING CR CRUISE 1 CE 05 915TW 49186 STL - DURING CRUISE, NOSE GEAR UNSAFE LIGHT ILLUMINATED. REMOVED AND REPLACED PROXIMITY ELECTRONICS UNIT. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996081500457 19960815 00457 WP 1996 8 15 96ZZZM1199 1 19960704 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 989Z 47135 STL - DURING CRUISE, FLOOR EGRESS LIGHTING STRIP ILLUMINATED AT ROWS 14 TO 20. DISCONNECTED, CLEANED AND RECONNECTED BA TTERY PACK AT ROWS 14 TO 20. OPERATIONAL CHECK OF EGRESS LIGHTING SYSTEM NORMAL. (M) 2 L 7 2 4F A6WE 1996081500458 19960815 00458 WP 1996 8 15 96ZZZM1200 1 19960630 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 756 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 921L 47107 STL - DURING SPECIAL CHECK, FOUND A CRACK IN LONGERON 1L, STATION 756. REPAIRED PER SRM 53-02, FIGURE 4, PAGE 5. (M) 2 L 7 2 4F A6WE 1996081500459 19960815 00459 WP 1996 8 15 96ZZZM1201 1 19960412 A 5313 LONGERON DOUG DC9 DC951 3022051 WP BS 1151 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 409EA 47728 STL - DURING OP-15, FOUND CRACK APPROXIMATELY ONE INCH LONG IN LONGERON 17R, STATION 1151, TOP AND BOTTOM LEGS. REPAIRE D PER SRM 53-02. AIRCRAFT TOTAL TIME 41,764, TOTAL CYCLES 37,652. 2 L 7 2 4F A6WE 1996081500460 19960815 00460 WP 1996 8 15 96ZZZM1202 1 19960710 A 3260 BULB DOUG DC9 DC982 3022082 WP RT MLG FAILED A TWAA O OTHER P NO WARNING INDICATION AP APPROACH 1 CE 05 914TW 49185 SFO - DURING GEAR EXTENSION RIGHT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE. REMOVED AND REPLACED LIGHT BULB IN LIGHT ASSEMBLY. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F A6WE 1996081500461 19960815 00461 WP 1996 8 15 96ZZZM1203 1 19960710 A 3350 BULB DOUG DC9 DC983 3022083 WP CABIN LOOSE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9307R 49663 STL - DURING LAYOVER MAINTENANCE, EMERGENCY LIGHTS WOULD NOT TEST. REMOVED AND RE-SEATED BULBS IN SOCKETS. OPERATIONAL TEST NORMAL. (M) 2 L 7 2 4F RT A6WE 1996081500462 19960815 00462 WP 1996 8 15 96ZZZM1204 1 19960708 A 3260 H146 DNLOCK SWITCH DOUG DC9 DC931 3022065 WP LT MLG FAILED A TWAA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 CE 05 990Z 47136 STL - DURING CLIMB, LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON. FLIGHT RETURNED TO STL. REMOVED AND REPLACED DOWN LOCK SWITCH, MFG P/N H14-6. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996081500463 19960815 00463 WP 1996 8 15 96ZZZM1205 1 19960708 A 3350 58222 POWER SUPPLY DOUG DC9 DC934 302207E WP CABIN INOPERATIVE A TWAA K NONE L NO TEST CR CRUISE 1 CE 05 927L 48123 STL - DURING CRUISE EGRESS LIGHTS AT ROWS 8-12 ILLUMINATED. REMOVED AND REPLACED POWER SUPPLY, MFG P/N 5822-2. OPERATI ONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 1996081500464 19960815 00464 WP 1996 8 15 96ZZZM1206 1 19960709 A 3350 58222 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A TWAA K NONE L NO TEST CR CRUISE 1 CE 05 982PS 47251 STL - DURING CRUISE, EMERGENCY EGRESS LIGHT ILLUMINATED. REMOVED AND REPLACED BATTERY PACK, MFG P/N 5822-2. OPERATIONA L CHECK NORMAL. (M) 2 L 7 2 4F A6WE 1996081500465 19960815 00465 WP 1996 8 15 96ZZZM1207 1 19960709 A 3350 58222 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A TWAA K NONE L NO TEST CR CRUISE 1 CE 05 412EA 47733 STL - DURING CRUISE, COACH EMERGENCY LIGHTS ILLUMINATED. REMOVED AND REPLACED BATTERY PACK, MFG P/N 5822-2. OPERATIONA L CHECK NORMAL. (M) 2 L 7 2 4F A6WE 1996081500466 19960815 00466 WP 1996 8 15 96ZZZM1208 1 19960709 A 3350 58222 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 986Z 47589 STL - DURING LAYOVER, MAINTENANCE FOUND EMERGENCY LIGHTS INOPERATIVE. FEEDER CABLES WERE CHECKED FOR SECURITY AND BATTE RY PACK, MFG P/N 5822-2, WAS CHANGED. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F A6WE 1996081500467 19960815 00467 WP 1996 8 15 96ZZZM1209 1 19960708 A 3350 58222 BATTERY PACK DOUG DC9 DC915 3022036 WP CABIN DISCHARGED A TWAA K NONE L NO TEST CR CRUISE 1 CE 05 973Z 47033 STL - DURING CRUISE, EGRESS LIGHTING ILLUMINATED IN LAST THREE ROWS. REMOVED AND REPLACD BATTERY PACK, MFG P/N 5822-2. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F A6WE 1996081500468 19960815 00468 WP 1996 8 15 96ZZZM1210 1 19960710 A 3350 58222 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A TWAA K NONE L NO TEST CR CRUISE 1 CE 05 982PS 47251 STL - DURING CRUISE, EMERGENCY LIGHTS FLASHED ON AND OFF. REMOVED AND REPLACED POWER SUPPLY, MFG P/N 5822-2. OPERATION AL CHECK NORMAL. 2 L 7 2 4F A6WE 1996081500469 19960815 00469 WP 1996 8 15 96ZZZM1211 1 19960713 A 3350 58222 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A TWAA K NONE L NO TEST CR CRUISE 1 CE 05 989Z 47135 STL - DURING CRUISE, EGRESS LIGHTS AT SEAT ROW 15 TO 20 ILLUMINATED. FOUND POWER SUPPLY, MFG P/N 5822-2, WEAK. REPLACE D POWER SUPPLY. OPERATION THEN CHECKED NORMAL. 2 L 7 2 4F A6WE 1996081500470 19960815 00470 WP 1996 8 15 96ZZZM1212 1 19960710 A 3244 TIRE LKHEED 1011 1011385115 5265015 WP RT MLG FAILED A TWAA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 31031 193B1115 LAX - AFTER GEAR RETRACTION, RIGHT REAR BRAKE OVERHEAT LIGHT ILLUMINATED. LANDING GEAR WAS EXTENDED IN ORDER TO COOL TH E BRAKE AND THEN RETRACTED. NR 4 RIGHT TIRE, NR 4R, BRAKE ASSEMBLY, MFG P/N 2-1367-10PT-1, AND ANTI-SKID VALVE, MFG P/N 6000006, WERE REMOVED AND REPLACED. OPERATIONAL CHECK NORMAL. 2 L 7 3 4F A23WE 1996081500471 19960815 00471 WP 1996 8 15 96ZZZM1213 1 19960710 A 3242 2136710PT1 BRAKE LKHEED 1011 1011385115 5265015 WP RT MLG FAILED A TWAA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 31031 193B1115 LAX - AFTER GEAR RETRACTION, RIGHT REAR BRAKE OVERHEAT LIGHT ILLUMINATED. LANDING GEAR WAS EXTENDED IN ORDER TO COOL TH E BRAKE AND THEN RETRACTED. NR 4 RIGHT TIRE, NR 4R, BRAKE ASSEMBLY, MFG P/N 2-1367-10PT-1, AND ANTI-SKID VALVE, MFG P/N 6000006, WERE REMOVED AND REPLACED. OPERATIONAL CHECK NORMAL. 2 L 7 3 4F A23WE 1996081500472 19960815 00472 WP 1996 8 15 96ZZZM1214 1 19960710 A 3241 6000006 ANTI-SKID VLV LKHEED 1011 1011385115 5265015 WP RT MLG FAILED A TWAA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 31031 193B1115 LAX - AFTER GEAR RETRACTION, RIGHT REAR BRAKE OVERHEAT LIGHT ILLUMINATED. LANDING GEAR WAS EXTENDED IN ORDER TO COOL TH E BRAKE AND THEN RETRACTED. NR 4 RIGHT TIRE, NR 4R, BRAKE ASSEMBLY, MFG P/N 2-1367-10PT-1, AND ANTI-SKID VALVE, MFG P/N 6000006, WERE REMOVED AND REPLACED. OPERATIONAL CHECK NORMAL. 2 L 7 3 4F A23WE 1996081500473 19960815 00473 NM 1996 8 15 96ZZZM1215 1 19960713 A 3231 26702887 SEQ VALVE BOEING 747 747131 1384881 NM NLG DOOR MALFUNCTIONED A TWAA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 93108 19674 HNL - DURING CLIMB, NOSE LANDING GEAR DOORS CAME OPEN WITH LANDING GEAR SELECTED TO UP. CYCLED LANDING GEAR. FOUND NOS E LANDING GEAR DOOR SEQUENCE VALVE. NOSE GEAR DOOR OPERATION CHECKED NORMAL. 2 L 7 4 4F A20WE 1996081500474 19960815 00474 NM 1996 8 15 96ZZZM1216 1 19960714 A 2530 888011 SERVING CART BOEING 767 767231 1385131 NM GALLEY FAILED A TWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 607TW 22570 STL - DURING CRUISE, SINGLE SERVING CART CONNECTOR EMITTED SMOKE AND CIRCUIT BREAKER POPPED. TURNED OFF SERVICING CART AND DISCONNECTED CONNECTOR. FOUND INTERNAL MALFUNCTION IN SERVING CART, MFG P/N 88801-1, CONNECTOR. REPLACED SERVING C ARGO AND OPERATION THEN CHECKED NORMAL. 2 L 7 2 4F RT A1NM 1996081500475 19960815 00475 WP 1996 8 15 96ZZZM1217 1 19960702 A 5210 BEAM FITTING DOUG DC9 DC915 3022036 WP PAX DOOR CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 490SA 45798 STL - DURING OP-15, FOUND .25 INCH CRACK IN FORWARD LOWER DOOR BEAM FITTING RIVET HOLE. REPAIRED PER SRM 51-00 AND TWA STANDARD PRACTICES. AIRCRAFT TOTAL TIME 63,299, AIRCRAFT TOTAL CYCLES 77,392. 2 L 7 2 4F A6WE 1996081500476 19960815 00476 NE 1996 8 15 96ZZZM1218 2 19960707 A 7200 ENGINE BOEING 747 747156 1384884 NM PWA JT9 JT9D7AH 52054 NE NR 2 FAILED A A TWAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 05 134TW 19958 HNL - DURING CLIMB NR 2 ENGINE, S/N 4115, FIRE WARNING ILLUMINATED. ENGINE WAS SHUTDOWN IN FLIGHT AND AIRCRAFT RETURNED TO HNL WHERE ENGINE WAS CHANGED. ENGINE TOTAL TIME 78,187, CYCLES 14,251. 2 L 7 4 4F 4 F A20WE E20EA 1996081500477 19960815 00477 NE 1996 8 15 96ZZZM1219 2 19960706 A 7250 TURBINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 2 ENG FAILED A TWAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 CE 05 911TW 49182 OMA - DURING CRUISE NR 2 ENGINE, S/N 3225, WAS SHUTDOWN DUE TO TURBINE FAILURE. ENGINE TOTAL TIME 34,212, CYCLES 17,878 . 2 L 7 2 4F 4 F A6WE E9NE 1996081500478 19960815 00478 NE 1996 8 15 96ZZZM1220 2 19960714 A 7200 ENGINE BOEING 747 747143 1384901 NM PWA JT9 JT9D7A 52054 NE NR 4 FAILED A A TWAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 CE 05 17010 19729 4266 CDG - DURING CRUISE SHUT DOWN NR 4 ENGINE, S/N 4266, DUE TO LOW OIL PRESSURE. FOUND ANGLE GEARBOX AND ACCESSORY GEARBO X CHIP DETECTORS WITH METAL PARTICLES. REPLACED ENGINE AND THEN ENGINE OPERATION CHECKED NORMAL. ENGINE TOTAL TIME 55, 441, TOTAL CYCLES 13,504. 2 L 7 4 4F 4 F A20WE E20EA 1996081500479 19960815 00479 WP 1996 8 15 96ZZZM1221 1 19960610 A 5313 LONGERON DOUG DC9 DC951 3022051 WP BS 813 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 412EA 47733 STL - DURING OP-15, FOUND .25 INCH CRACK IN LONGERON 2R, STATION813, UNDER OUTBOARD BOLT. REPAIRED PER SRM 53-02, FIGUR E 2 AND TWA STANDARDPRACTICES. AIRCRAFT TOTAL TIME 41,166, AIRCRAFT TOTAL CYCLES36,801. 2 L 7 2 4F A6WE 1996081500480 19960815 00480 NE 1996 8 15 96ZZZM1222 2 19960720 A 7200 ENGINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D217C 52053 NE NR 2 FAILED A TWAA E ENGINE SHUTDOWN E J VIBRATION/BUFFET WARNING INDICATION DE DESCENT 1 CE 05 9409F 53121 1213 STL - DURING DESCENT, SHUT DOWN NR 2 ENGINE, S/N 1213, DUE TO VIBRATION AND OIL FILTER BYPASS LIGHT ILLUMINATION. FOUND METAL PARTICLES ON OIL SYSTEM CHIP DETECTORS. REPLACED ENGINE, ENGINE OPERATION THEN CHECKED NORMAL. ENGINE TOTAL TIM E 22,333, ENGINE TOTAL CYCLES 11,261. 2 L 7 2 4F 4 F RT A6WE E9NE 1996081500481 19960815 00481 NM 1996 8 15 96ZZZM1223 1 19960716 A 2133 7207375 OUTFLOW VALVE BOEING 737 7372L9 1384497 NM CABIN MALFUNCTIONED A ZZDA A B G UNSCHED LANDING EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CL CLIMB 1 SO 15 464AT 21278 FLT NR 501 - ALB-MCO - EXPERIENCED PRESSURIZATION PROBLEMS AT FL 350 (MAX PRESS DIFF) CABIN BEGAN CLIMBING AT 1,000 PLUS . OUTFLOW WAS FULL CLOSED AND UNABLE TO CONTROL CABIN PRESSURE. OXYGEN MASKS DEPLOYED. ACCOMPLISHED EMERGENCY DESCENT TO 10,000 AND PERFORMED AND UNSCHEDULED LANDING AT ORF. AIRCRAFT WAS FERRIED TO MCO. TROUBLESHOT PRESSURIZATION FAILU RE TO SAFETY RELIEVE VALVES. REMOVED AND REPLACED VALVES IAW 737MM 21-32-21. OPS CHECK NORMAL. 2 L 7 2 4F RT A16WE 1996081500482 19960815 00482 NM 1996 8 15 96ZZZM1224 1 19960713 A 3240 26010425 BRAKE BENDIX BOEING 737 7372P6 NM NR 2 MALFUNCTIONED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW BC692 21355 DURING POST FLIGHT INSPECTION, PILOT FOUND NR 1 TIRE FLAT. MAINTENANCE INSPECTION REVEALED THAT THE THERMAL FUSE HAD ME LTED DURING BRAKE OVERHEAT. PILOT REPORTED THAT NO HIGH ENERGY STOP HAD BEEN MADE. SUSPECT DRAGGING BRAKE. PERFORMED BRAKE OVERHEAT INSPECTION PER BOEING MM 5-51-11. NO DISCREPANCIES NOTED DURING INSPECTION. REPLACED THE NR 1 BRAKE ASS Y AND THE NR 1 AND NR 2 MAIN WHEEL ASSEMBLIES. RETURNED AIRCRAFT TO SERVICE. BRAKE ASSEMBLY WAS OVERHAULED BY AVIALL O N 4/4/96. ASSEMBLY HAD ACCUMILATED 228 CYCLES. 2 L 7 2 4F RT A16WE 1996081500483 19960815 00483 NM 1996 8 15 96ZZZM1225 1 19960723 A 7930 42D107A1 BYPASS SWITCH BOEING 737 737214 138446R NM NR 1 ENG DIRTY A ZZDA A B UNSCHED LANDING EMER. DESCENT J WARNING INDICATION CL CLIMB 1 SO 15 460AT 20158 FLT 670 - MCO-GSO - AFTER REACHING FL 250, THE NR 1 ENG OIL FILTER BYPASS LIGHT BEGAN FLICKERING. THE NR 1 ENG WAS SHUT DOWN AND AN EMERGENCY WAS DECLARED INTO DAYTONA. AIR TRAN MECHANICS REMOVED THE ENG OIL FILTER AND INSPECTED. ENG OIL FILTER WAS CLEAN. MECH REPLACED THE FILTER AND RAN THE ENG. FILTER LIGHT CONTINUED TO FLICKER. OIL PRESS SWITCH WAS P LACED ON MEL AND THE A/C WAS RELEASED FOR FLT. PRIOR TO ASSUMING FLT 670, THE A/C HAD ARRIVED IN MCO FROM FLT 721 WITH THE NR 1 ENG OIL FILTER BYPASS LIGHT FLICKERING DURING TAXI. MECH T/S SYSTEM AND FOUND THE OIL FILTER BYPASS SWITCH CON NECTOR DIRTY. THE CONNECTOR WAS CLEANED AND POST MX ENG RUN WAS NORMAL. NR 1 ENG OIL FILTER BYPASS LIGHT REMAINS MEL. 2 L 7 2 4F A16WE 1996081500484 19960815 00484 NM 1996 8 15 96ZZZM1226 1 19960705 A 2612 894406 FIRE LOOP BOEING 737 737214 138446R NM APU OUT OF POSITION A ZZDA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 15 460AT 20158 MCO-GSO - FLT 670 - IN FLT, THE APU FIRE WARNING CAME ON (AUDIBLE AND VISUAL). APU WAS NOT IN USE AT TIME. CREW PULLED THE FIRE HANDLE AND DISCHARGED THE FIRE BOTTLE, THE WARNING SYSTEM REMAINED ON. EMERGENCY WAS DECLARED, EMERGENCY DESC ENT MADE. AFTER LANDING, MECH OPENED THE APU ACCESS DOOR AND INSPECTED THE AREA FOR EVIDENCE OF FIRE OR O/H, NONE FOUND . PLACED APU AND APU FIRE DET SYS ON MEL. MECH PERFORMED CLOSE VISUAL INSPECTION OF FIRE LOOP AND FOUND LOOP BENT IN T WO PLACES AND TOUCHING METAL. REPOSITIONED LOOP AND PERFORMED A RESISTANCE CHECK. RESISTANCE CHECK WAS NORMAL. PERFOR MED A TEST OF THE APU FIRE DETECTION SYSTEM. ALL TESTS WERE NORMAL. RETURNED APU TO SERVICE. 2 L 7 2 4F A16WE 1996081500485 19960815 00485 EU 1996 8 15 AALA960972 1 19960621 A 2130 566920 VALVE FOKKER F28 F28MK0100 4990807 EU AVIONICS COMPT DEFECTIVE A AALA A B G UNSCHED LANDING EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 SW 07 1423A 11406 ADF - FLT 1788 - EN ROUTE ORD-ATL - DURING CRUISE AT FL 290, UNABLE TO CONTROL CABIN PRESSURIZATION AND CABIN ALTITUDE I NCREASED. ACCOMPLISHED EMERGENCY DESCENT AND ALL PAX OXYGEN MASKS DROPPED SUCCESSFULLY. AIRCRAFT DIVERTED TO SDF AND L ANDED WITHOUT INCIDENT. REPLACED PREVIOUSLY PLACARDED AVIONICS COOLING OUTLET VALVE. ACCOMPLISHED LEAK AND GROUND CHEC KS WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION AND PLACARD REMOVED. ACCOMPLISHED FUNCTIONAL CHECK FL IGHT AND AIRCRAFT MAINTENANCE FERRY SDF/TUL FOR PAX OXYGEN MASK RESTOW AND OXYGEN SYSTEM SERVICING TO BE ACCOMPLISHED IN CONJUNCTION WITH C-CHECK. (M) 2 L 7 2 4F RT 1996081500486 19960815 00486 WP 1996 8 15 AALA960977 1 19960627 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 420 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 164AA 46950 TUL - G2 GALLEY SUPPORT CORRODED IN NUMEOUS LOCATIONS AT MOUNTING FLANGES AROUND BOSSES. REPLACED ENTIRE UNIT PER SRM 5 1-21-01 VOL II. (M) 2 L 7 3 4F A22WE 1996081500487 19960815 00487 WP 1996 8 15 AALA960979 1 19960628 A 5720 BRACKET DOUG DC10 DC1030 3023501 WP WS 264 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 164AA 46950 TUL - FOUND HYD LINE SUPPORT BRACKET HAD LIGHT CORROSION WHEN CLEANED .5 INCH CRACK WAS FOUND. NEW BRACKET WAS DUPLICAT ED AND INSTALLED IN PLACE OF CRACKED PART PER DC-10 SRM 51-10-00. (M) 2 L 7 3 4F A22WE 1996081500488 19960815 00488 WP 1996 8 15 AALA960992 1 19960701 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 791-808 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 164AA 46950 TULE - FOUND CORROSION ON FLOOR BOARD SUPPORT BETWEEN TRACK AND GALLEY SUPPORT BEAM. REMOVED OH SUPPORT AND MANUFACTURE D NEW BEAM PER SRM 53-00-01 PAGE 1. (M) 2 L 7 3 4F A22WE 1996081500489 19960815 00489 WP 1996 8 15 AALA960993 1 19960701 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 460 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 164AA 46950 TUL - G3 GALLEY SUPPORT OUTBOARD OF NR 3 SEAT TRACK CORRODED. REMOVED AND REPLACED OUTBOARD GALLEY SUPPORT PER SRM 53-0 0-01. (M) 2 L 7 3 4F A22WE 1996081500490 19960815 00490 WP 1996 8 15 AALA961006 1 19960703 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 296AA 49308 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT STRIP BY FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BY FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996081500491 19960815 00491 WP 1996 8 15 AALA961013 1 19960705 A 3350 A3060698101 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 237AA 49523 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS FROM PAX SEAT ROW 21 AND AFT INOPERATIVE. RESECURED LOOSE EMERGENC Y FLOOR LIGHT STRIP CONNECTOR BY PAX SEAT ROW 21. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996081500492 19960815 00492 WP 1996 8 15 AALA961014 1 19960705 A 3350 A3060698101 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7549A 53031 BOS - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS FROM AFT GALLEY DOOR TO AFT CABIN INOPERATIVE. REPLACED BROKEN EME RGENCY FLOOR LIGHT STRIP CONNECTOR BY AFT GALLEY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996081500493 19960815 00493 EU 1996 8 15 AALA961016 1 19960706 A 3397 WIRE AIRBUS 300 A300B4605R 3930308 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 14068 511 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PAX SEAT ROW 27 CENTER BULKHEAD INOPERATIVE. REPAIRED BROKEN EM ERGENCY FLOOR LIGHT WIRE BY PAX SEAT ROW 27 CENTER BULKHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996081500494 19960815 00494 EU 1996 8 15 AALA961017 1 19960706 A 5610 D20543405 WINDSHIELD FOKKER F28 F28MK0100 4990807 EU L1 DEFECTIVE A A AALA H DEACTIVATE SYST/CIRCUITS O OTHER DE DESCENT 1 SW 07 1416A 11395 DFW - FTL 1542 - DURING DESCENT INTO DFW, L1 WINDSHIELD ARCED FROM CENTER LOWER PORTION OF WINDOW. CREW TURNED OFF LEFT WINDOW HEAT AND CONTINUED DESCENT. AT 9,000 FT AND 250 KTS, L1 WINDSHIELD OUTER PANEL SHATTERED. AIRCRAFT PROCEEDED T O DFW AND LANDED WITHOUT INCIDENT. REPLACED L1 WINDSHIELD. ALSO, REPLACED L1 WINDOW HEAT CONTROLLER. SYSTEM GROUND CH ECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1996081500495 19960815 00495 EU 1996 8 15 AALA961021 1 19960708 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 70073 516 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 21H THROUGH 25H MISSING. REPLACED EMERGENCY FLOOR LIGHT STRIP BETWEEN PAX SEAT ROWS 21H THROUGH 25H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996081500496 19960815 00496 WP 1996 8 15 AALA961022 1 19960710 A 7714 COVER DOUG DC9 DC982 3022082 WP LT ENGINE CRACKED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 454AA 49559 IAD - FLT 845 - WHILE EN-ROUTE EWR-DFW - DIVERTED TO IAD DUE TO FUMES IN CABIN. LEFT ENGINE HAD AN UNUSUAL NOISE DURING FLIGHT. LANDED OVERWEIGHT AT IAD WITHOUT INCIDENT. REPLACED N1 TACH ACCESSORY HOUSING ACCESS COVER AND AIR CONDITIONI NG PACK FILTERS. PERFORMED OVERWEIGHT LANDING AND PERFORMED ENGINE RUN UP. NO EXCESSIVE NOISE, VIBRATION, OR SMELL NOT ED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996081500497 19960815 00497 WP 1996 8 15 AALA961023 1 19960710 A 3397 WIRE DOUG DC9 DC982 3022082 WP AFT STAIRWAY CORRODED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 216AA 49167 DFW - DURING OVERNIGHT CHECK, FOUND AFT STAIRWAY SIDEWALL EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED CORRO DED WIRE TO LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996081500498 19960815 00498 NM 1996 8 15 AALA961038 1 19960711 A 5330 SKIN BOEING 727 727223 1384074 NM BS 480-500 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 707AA 22464 TUL - FOUND CORROSION ON SKIN STATION 480 TO 500, STATION 28 LEFT. INSTALLED REPAIR PER SRM 53-30-3, STATION 480 TO 500 , STRINGER 28 LEFT. (M) 2 L 7 3 4F A3WE 1996081500499 19960815 00499 NM 1996 8 15 AALA961039 1 19960711 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 495-500 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 707AA 22464 TUL - FOUND CORROSION ON STRINGER 27R . REPAIRED STRINGER PER SRM 53-10-3 PG 3-4. REMOVED CORROSION PER SRM 51-10-6. ( M) 2 L 7 3 4F A3WE 1996081500500 19960815 00500 NM 1996 8 15 AALA961053 1 19960711 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 877AA 21389 MIA - DURING OVERNIGHT MAINTENANCE, FOUND THE FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. SECURED FIRST C LASS EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996081500501 19960815 00501 NM 1996 8 15 AALA961054 1 19960711 A 3260 GEAR INDICATION BOEING 767 767323 1385205 NM LT MLG MALFUNCTIONED A AALA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 388AA 27448 MIA - FLT 26 - ON APPROACH TO MIA DURING NORMAL GEAR EXTENSION, THE LEFT MAIN LANDING GEAR DID NOT INDICATE DOWN AND LOC KED. PERFORMED ALTERNATE GEAR EXTENSION, LEFT MAIN GEAR DID NOT INDICATE DOWN AND LOCKED. PUT ADP TO ON POSITION AND R ETURNED ALTERNATE GEAR SWITCH TO OFF POSITION, THIS GAVE A DOWN AND LOCKED INDICATION. LANDED MIA WITHOUT INCIDENT. TR OUBLESHOT LANDING GEAR SYSTEM BY SWINGING GEAR SEVERAL TIMES. ALSO, CHECKED ALTERNATE GEAR EXTENSION SYSTEM. PERFORMED LEAK CHECK. COULD NOT DUPLICATE ON GROUND. SYSTEM GROUND CHECKED NORMAL OPERATION. AIRCRAFT RELEASED FOR SERVICE. ( M) 2 L 7 2 4F RT A1NM 1996081500502 19960815 00502 NM 1996 8 15 AALA961055 1 19960711 A 2781 FLAP WARNING BOEING 767 767323 1385205 NM LE FLAPS ACTIVATED A AALA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 369AA 25196 MIA - FLT 111 - ON APPROACH TO MIA, WHILE EXTENDING FLAPS TO 20 DEGREES A LEADING EDGE SLAT ASYMMETRIC EICAS MESSAGE. D ECLARED AN EMERGENCY AND LANDED AT MIA WITHOUT INCIDENT. PERFORMED BITE CHECK OF FFU WITH NO FAULTS NOTED. CYCLED FLAP S SEVERAL TIMES WITH NO FAULTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. COULD NOT DUPLICATE ON GROUND, AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A1NM 1996081500503 19960815 00503 WP 1996 8 15 AALA961058 1 19960712 A 5315 FLOOR BEAM DOUG DC10 DC1030 3023501 WP BS 1781 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 164AA 46950 TULE - FOUND CORROSION ON FLOOR BEAM AT AFT LWR CORNER OF CENTER CARGO DOORWAY AREA. REPAIRED PER ESO 7349 DATED 7-9-96 FABRICATED AND INSTALLED STACK DOUBLER. (M) 2 L 7 3 4F A22WE 1996081500504 19960815 00504 WP 1996 8 15 AALA961059 1 19960712 A 5330 SKIN DOUG DC10 DC1030 3023501 WP BS 1681 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 164AA 46950 TULE - FOUND CORROSION ON OUTER FUSELAGE SKIN UNDERNEATH LOWER BEACON. INSTALLED AN INTERNAL DOUBLER PER ESO 7349 DATED 7-11-96. (M) 2 L 7 3 4F A22WE 1996081500505 19960815 00505 WP 1996 8 15 AALA961060 1 19960712 A 5400 SPAR WEB DOUG DC10 DC1030 3023501 WP NR 1 PYLON GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 164AA 46950 TULE - FOUND GOUGE IN LOWER AFT SPAR WEB. REPAIRED PER ESO 7349 DATED 7-11-96. (M) 2 L 7 3 4F A22WE 1996081500506 19960815 00506 WP 1996 8 15 AALA961064 1 19960715 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 70504 49798 DFW - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE, FORWARD OF FIRST CLASS TO MID-COACH SE CTION. REPLACED TWO JUMPER WIRES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996081500507 19960815 00507 WP 1996 8 15 AALA961065 1 19960715 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 429AA 49341 DFW - DURING OVERNIGHT CHECK, FOUND THE AFT STAIR SIDE WALL EMERGENCY EXIT LIGHT MARKERS INOPERATIVE. REPLACED WIRE SEC TION FROM POWER LEADS TO AFT STAIR AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996081500508 19960815 00508 NM 1996 8 15 AALA961072 1 19960716 A 5315 FLOOR BEAM BOEING 727 727227 1384078 NM BS 825.95 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 731AA 20738 TULE - FOUND CRACK IN FLOOR BEAM WEB STATION 826.95 BELOW RIGHT LIGHTING HOLE CUTOUT. CRACKS ENDS IN RIVET HOLE. INSTA LLED REPAIR PER SRM 61-40-2 PG 1-66. (M) 2 L 7 3 4F A3WE 1996081500509 19960815 00509 NM 1996 8 15 AALA961073 1 19960716 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 53-680 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 731AA 20738 TULE - FOUND STRINGER CORROSION FS 530-680, STRINGER 28L. REPLACED STRINGER. (M) 2 L 7 3 4F A3WE 1996081500510 19960815 00510 NM 1996 8 15 AALA961074 1 19960716 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 650-680 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 731AA 20738 TUL - FOUND STRINGER 27L CORRODED BETWEEN OUTER SKIN AND STRINGER. INSTALLED NEW STRINGER SECTION FROM STATION 640 TO 6 80, PER SRM 53-10-3 FIG 1. (M) 2 L 7 3 4F A3WE 1996081500511 19960815 00511 NM 1996 8 15 AALA961075 1 19960716 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 650 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 731AA 20738 TULE - FOUND STRINGER 28R CORRODED, STATION 650-680. INSTALL STRINGER REPAIR PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1996081500512 19960815 00512 NM 1996 8 15 AALA961083 1 19960718 A 3350 MODULE BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 892AA 22008 DFW - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT LIGHT, OVER RIGHT WING, INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT M ODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996081500513 19960815 00513 NM 1996 8 15 AALA961085 1 19960708 A 5320 143T8510 DOOR SILL BOEING 767 767223 1385123 NM BS 615.5 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 315AA 22317 AFW - FOUND AND BLENDED OUT CORROSION ON THE UPPER SURFACE OF FWD CARGO DOOR LOWER MAIN SILL INNER CHORD. THE BLENDOUT EXCEEDED SRM MAX ALLOWABLE LIMITS. ROTO PEENED AREA, INSTALLED FILLER FABRICATED FROM 7075-T6 ALUMINUM. ALODINED AND P RIMED AREA. APPROVED BY ENGINEERING PER MRB 767-1269. CHORD WILL BE REPLACED ON OR BEFORE NEXT MBV. (M) 2 L 7 2 4F RT A1NM 1996081500514 19960815 00514 NM 1996 8 15 AALA961086 1 19960708 A 5315 11175008 FLOOR BEAM BOEING 767 767223 1385123 NM BS 855 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 315AA 22317 AFW - FOUND AND BLENDED GOUGE ON THE UPPER SURFACE OF THE MAIN CABIN FLOOR BEAM. BLEND EXCEEDS SRM MAX ALLOWABLE LIMITS . ROTO PEENED, ALODINED AND PRIMED APPROVED BY ENGINEERING PER MRB 767-1270. (M) 2 L 7 2 4F RT A1NM 1996081500515 19960815 00515 NM 1996 8 15 AALA961087 1 19960702 A 5730 111T3013 SKIN BOEING 767 767223 1385123 NM CTR WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 315AA 22317 AFW - FOUND AND REMOVED HEAVY CORROSION ON CENTER WING UPPER SKIN AT AFT DRAIN LOCATIONS STA 955 LBL 71 AND RBL 7L. ALS O, THE LOWER CHORD TO FLOOR BEAM T-EXTRUSION WAS CUT AND REMOVED. REINSTALLED T-CHORD WITH 'I' EXTRUSION ON EACH SIDE O F THE CHORD WITH 5 FASTENERS ON EACH SIDE OF THE CUT. CORRODED AREAS WERE CLEANED, SHOT PEENED, ALODINED AND PRIMED. A PPROVED BY ENGINEERING PER MRB 767-1268. (M) 2 L 7 2 4F RT A1NM 1996081500516 19960815 00516 NM 1996 8 15 AALA961088 1 19960708 A 5315 111T5007 FLOOR BEAM BOEING 767 767223 1385123 NM BS 850-870 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 315AA 22317 AFW - FOUND AND BLENDED CORROSION IN 2 AREA OF THE UPPER SURFACE OF THE CABIN FLOOR BEAMS. THE BLENDOUTS EXCEEDED SRM A LLOWABLE LIMITS. CUT EACH FLOOR BEAM OF STATION 843.5 AND 876.8. SPLICED NEW SECTIONS OF FLOOR BEAM. ACCOMPLISHED PER APPROVED ENGINEERING INSTRUCTIONS OF MRB 767-1264. (M) 2 L 7 2 4F RT A1NM 1996081500517 19960815 00517 NM 1996 8 15 AALA961089 1 19960709 A 5320 146T1008 TEAR STRAPS BOEING 767 767223 1385123 NM BS 1540-1562 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 315AA 22317 AFW - FOUND TEAR STRAPS DAMAGED BEYOND SRM LIMITS. MANUFACTURED .080 2.2A-T3 BARE DOUBLER, INSTALLED USING FILLER BETWE EN DOUBLER AND TEAR STRAPS PER ENGINEERING MRB 767-1265. (M) 2 L 7 2 4F RT A1NM 1996081500518 19960815 00518 WP 1996 8 15 AALA961094 1 19960720 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 510AM 49804 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PAX SEAT ROWS 32 AND 33 INOPERATIVE. REPLACED EMERGENCY FLOOR L IGHT STRIP BY PAX SEAT ROWS 32 AND 33. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996081500519 19960815 00519 EU 1996 8 15 AALA961096 1 19960719 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 14065 508 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 21HJ TO 23HJ INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BETWEEN PAX SEAT ROWS 21 HJ TO 23 HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996081500520 19960815 00520 EU 1996 8 15 AALA961097 1 19960719 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 90070 513 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT PAX SEAT 20B FOUND DAMAGED AND INOPERATIVE. REPLACED DAMAGED EM ERGENCY FLOOR LIGHT STRIP BY PAX SEAT 20B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996081500521 19960815 00521 WP 1996 8 15 AALA961101 1 19960719 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7533A 49987 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRI P BY FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996081500522 19960815 00522 WP 1996 8 15 ASAA9680148 1 19960707 A 7312 780956 FUEL HEAT DUCT DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE RT ENGINE BROKEN A ASAA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 NM 01 946AS 49658 SEA - AIR TURN BACK OF FLT 300, CREW REPORTED THE RIGHT ENGINE FIRE WARNING LIGHT ILLUMINATED DURING INITIAL CLIMB, LIGH T EXTINGUISHED WHEN POWER BROUGHT TO IDLE. LIGHT REMAINED OFF AT APPROACH POWER OF 1.4 EPR. REPLACED BROKEN FUEL HEAT DUCT ON RIGHT ENGINE, ACCOMPLISHED RUN UP AND OPERATED NORMALLY. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 1996081500523 19960815 00523 SO 1996 8 15 C2XA96IA 1 19960709 A 5730 12042999003 SKIN EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 27707 120095 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING LOWER SKIN SURFACE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REP LACED THE AFFECTED PORTION OF SKIN, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996081500524 19960815 00524 SO 1996 8 15 C2XA96IA160 1 19960709 A 5347 1204599601 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 27707 120095 IAH - DURING C-CHECK INSPECTION, THE RIGHT UPPER SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996081500525 19960815 00525 SO 1996 8 15 C2XA96IA161 1 19960709 A 5347 12026864007 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 27707 120095 IAH - DURING C-CHECK INSPECTION, THE LEFT AFT LOWER SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLAC ED THE AFFECTED SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996081500526 19960815 00526 SO 1996 8 15 C2XA96IA162 1 19960709 A 5347 12015995603 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 27707 120095 IAH - DURING C-CHECK INSPECTION, THE LEFT LOWER FORWARD SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND RE PLACED THE AFFECTED SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996081500527 19960815 00527 SO 1996 8 15 C2XA96IA163 1 19960709 A 5347 12015995603 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 27707 120095 IAH - DURING C-CHECK INSPECTION, THE LEFT UPPER FORWARD SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND RE PLACED THE AFFECTED PORTION OF SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996081500528 19960815 00528 SO 1996 8 15 C2XA96IA164 1 19960709 A 5347 12016000003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 27707 120095 IAH - DURING C-CHECK INSPECTION, THE RIGHT LOWER AFT SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLA CED THE AFFECTED PORTION OF SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996081500529 19960815 00529 SO 1996 8 15 C2XA96IA165 1 19960709 A 5347 12016000001 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 27707 120095 IAH - DURING C-CHECK INSPECTION, THE RIGHT LOWER FORWARD SEAT TRACK WAS FOUND TO BE CORRODED. MX REMOVED AND REPLACED T HE AFFECTED PORTION OF SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996081500530 19960815 00530 SO 1996 8 15 C2XA96IA166 1 19960709 A 5347 12015997003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 27707 120095 IAH - DURING C-CHECK INSPECTION, THE RIGHT SIDE WALL SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLA CED THE AFFECTED PORTION OF SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996081500531 19960815 00531 SO 1996 8 15 C2XA96IA167 1 19960709 A 5320 12064449001 BUTTSTRAP EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 27707 120095 IAH - DURING C-CHECK INSPECTION, THE BUTT STRAP BETWEEN FRAME 38 TO 40, WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED A ND REPLACED THE AFFECTED BUTT STRAP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996081500532 19960815 00532 SO 1996 8 15 C2XA96IA168 1 19960709 A 5320 12006489001 BUTTSTRAP EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 27707 120095 IAH - DURING C-CHECK INSPECTION, THE BUTT STRAP BETWEEN FRAMES 40 AND 44 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996081500533 19960815 00533 CE 1996 8 15 COEA9685001 1 19960717 A 3240 MS28775224 O-RING CESSNA 208 208B 2073701 CE RT MLG BRAKE LEAKING A COEA F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 NM 13 850FE 208B0164 DURING PILOT'S TAXI TO PARKING AFTER LANDING IN PHX, THE RIGHT BRAKE CAUGHT FIRE REQUIRING A FIRE EXTINGUISHER TO EXTING UISH THE FLAME. THE FIRE LASTED FOR APPROX 2 MINUTES. UPON INSPECTION MX FOUND EVIDENCE THAT ONE BRAKE PISTON WAS LEAK ING FLUID AROUND A FAILED O-RING. THIS WAS A CONTRIBUTING FACTOR TO THE CAUSE OF THE FIRE. NO DAMAGE WAS DONE TO THE A IRCRAFT. MX REPLACED THE COMPLETE WHEEL AND BRAKE ASSY IAW CESSNA MM. THE REMOVED WHEEL AND BRAKE ASSY ARE SCRAP. THE BRAKE ASSY WAS OVERHAULED IN DEC 1994 AND HAD A TOTAL TIME OF 510.3 HRS WHEN REMOVED ON THIS DATE. (M) 1 H 7 1 3T A37CE 1996081500534 19960815 00534 SO 1996 8 15 GLBA96120 1 19960614 A 3230 RETRACT MECH EMB 120 EMB120RT SO LANDING GEAR MALFUNCTIONED A GLBA O OTHER O OTHER CL CLIMB 1 CE 01 451UE 120108 SPI - LANDING GEAR WOULD NOT RETRACT UNTIL TILLER WAS DEPRESSED AND RELEASED. MAINTENANCE COMPLETED SEVERAL GEAR SWINGS AND COULD NOT DUPLICATE. (M) 2 L 7 2 4T RT A31SO 1996081500535 19960815 00535 CE 1996 8 15 GLBA96121 1 19960614 A 2750 1005240731 GEAR BOX ASSY BEECH 1900 1900D 1154162 CE TE FLAPS FAILED A GLBA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 CE 01 169GL 1329 UE169 RDU - AFTER TAKEOFF, FLAPS WOULD NOT RETRACT. MAINTENANCE MEL'D FLAPS AND THEN REMOVED AND REPLACED THE FLAP MOTOR GEAR BOX ASSY. (M) 2 L 7 2 4T RT A24CE 1996081500536 19960815 00536 SO 1996 8 15 GLBA96122 1 19960623 A 3010 EJECTORS EMB 120 EMB120ER 3260203 SO WING DE-ICE BOOT CROSS WIRED A GLBA O OTHER W INADEQUATE Q C TX TAXI/GRND HDL 1 CE 01 297UX 120297 DEN - LEFT AND RIGHT OUTBOARD WING DE-ICE BOOTS INFLATED WITHOUT COMMAND AND WOULD NOT DEFLATE WHILE TAXIING OUT. MX CO RRECTED TWO EJECTORS THAT WERE CROSS WIRED AND PATCHED BOOTS. (M) 2 L 7 2 4T RT A31SO 1996081500537 19960815 00537 SO 1996 8 15 GLBA96123 1 19960623 A 3231 12032943001 SEQUENCE VLV EMB 120 EMB120RT SO RT MLG DOOR DIRTY A GLBA O OTHER J WARNING INDICATION CL CLIMB 1 CE 01 267UE 120071 CIU - GEAR WILL NOT RETRACT. CLEANED RT FORWARD OUTBOARD GEAR DOOR SEQUENCE VALVE PLUNGER WHICH WAS STUCK. CYCLED GEAR SEVERAL TIMES. (M) 2 L 7 2 4T RT A31SO 1996081500538 19960815 00538 CE 1996 8 15 GLBA96124 1 19960624 A 2612 FIRE LIGHT BEECH 1900 1900C 1154161 CE RT ENGINE ILLUMINATED A GLBA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 CE 01 101UE UC101 MUN - RIGHT ENGINE 'FIRE PULL' LIGHT ILLUMINATED DURING SINGLE ENGINE TURN. MAINTENANCE INSPECTED FIRE ZONE AND FOUND N O DAMAGE, COULD NOT DUPLICATE PROBLEM. (M) 2 L 7 2 4T RT A24CE 1996081500539 19960815 00539 EA 1996 8 15 GLBA96125 2 19960621 A 7530 EVA TUBE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA LT BLEED AIR DAMAGED A GLBA O OTHER N FALSE WARNING CL CLIMB 1 CE 01 141UE UC141 MSP - LEFT BLEED AIR FAIL ANNUNCIATOR ILLUMINATED DURING CLIMB-OUT. MX REPAIRED HOLE IN EVA TUBING. (M) 2 L 7 2 4T 4 T RT A24CE E4EA 1996081500540 19960815 00540 CE 1996 8 15 GLBA96126 1 19960626 A 3230 RETRACT MECH BEECH 1900 1900C 1154161 CE LANDING GEAR MALFUNCTIONED A GLBA O OTHER J WARNING INDICATION CL CLIMB 1 CE 01 96UE UC96 ALO - GEAR WOULD NOT RETRACT. MX CYCLED GEAR SEVERAL TIMES AND TEST FLIGHT COULD NOT DUPLICATE PROBLEM. (M) 2 L 7 2 4T RT A24CE 1996081500541 19960815 00541 CE 1996 8 15 GLBA96128 1 19960630 A 3230 571302 MOTOR BEECH 1900 1900C 1154161 CE LANDING GEAR FAILED A GLBA O OTHER J WARNING INDICATION CL CLIMB 1 CE 01 96UE 172A UC96 BRL - GEAR WOULD NOT RETRACT AFTER TAKEOFF. MX REMOVED AND REPLACED LANDING GEAR MOTOR. (M) 2 L 7 2 4T RT A24CE 1996081500542 19960815 00542 CE 1996 8 15 GLBA96129 1 19960619 A 3246 114800121 WHEEL ASSY BEECH 1900 1900C 1154161 CE NLG UNBALANCED A GLBA O OTHER E VIBRATION/BUFFET CL CLIMB 1 CE 01 125GL UC125 ORD - NOSE WHEEL CAUSES VIBRATION DURING CLIMB-OUT UP TO 2500 FEET. MAINTENANCE REMOVED AND REPLACED NOSE WHEEL ASSY. ( M0 2 L 7 2 4T RT A24CE 1996081500543 19960815 00543 CE 1996 8 15 GLBA96130 1 19960619 A 3230 571302 MOTOR BEECH 1900 1900C 1154161 CE LANDING GEAR FAILED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 141UE 724A UC141 GFK - GEAR WILL NOT RETRACT. MX REMOVED AND REPLACED LANDING GEAR POWER PACK MOTOR. (M) 2 L 7 2 4T RT A24CE 1996081500544 19960815 00544 CE 1996 8 15 GLBA96131 1 19960619 A 6120 SOLENOID BEECH 1900 1900C 1154161 CE PROP CONTL DIRTY A GLBA O OTHER O OTHER LD LANDING 1 CE 01 104GL UC104 SPI - ON LANDING, FLARE AIRCRAFT YAWED VIOLENTLY LEFT AS IF LEFT PROP HAD DROPPED INTO REVERSE. MX CLEANED AND ADJUSTED LOW PITCH SOLENOID. (M) 2 L 7 2 4T RT A24CE 1996081500545 19960815 00545 CE 1996 8 15 GLBA96132 1 19960618 A 2121 1143800283 BLOWER MOTOR BEECH 1900 1900C 1154161 CE AFT FAILED A GLBA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 01 150UE UC150 TUS - ELECTRICAL SMOKE IN COCKPIT AFTER ONE HOUR EN ROUTE. FLEW WITH RIGHT GENERATOR AND INVERTER OFF. MX REMOVED AND REPLACED AFT VENT BLOWER MOTOR ASSY WHICH WAS SEIZED AND BURNED. (M) 2 L 7 2 4T RT A24CE 1996081500546 19960815 00546 CE 1996 8 15 GLBA96133 1 19960628 A 3297 WIRE BEECH 1900 1900D 1154162 CE RT MLG CHAFED A GLBA O OTHER O OTHER LD LANDING 1 CE 01 97UX UE97 AIA - LANDING GEAR INDICATOR CIRCUIT BREAKER POPPED WHEN GEAR EXTENDED. MX REPAIRED BROKEN AND CHAFFED WIRES TO RIGHT M AIN GEAR UPLOCK SWITCH. (M) 2 L 7 2 4T RT A24CE 1996081500547 19960815 00547 CE 1996 8 15 GLBA96134 1 19960621 A 3230 RETRACT MECH BEECH 1900 1900C 1154161 CE LANDING GEAR MALFUNCTIONED A GLBA O OTHER N FALSE WARNING CL CLIMB 1 CE 01 166GL UC166 RDU - GEAR WOULD NOT COME UP AFTER TAKEOFF. MX PERFORMED SEVERAL GEAR SWINGS AND COULD NOT DUPLICATE. RETURNED AIRCRAF T TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1996081500548 19960815 00548 SO 1996 8 15 GLBA96135 1 19960614 A 5400 DRAIN LINE EMB 120 EMB120RT SO RT ENGINE OUT OF POSITION A GLBA K NONE O OTHER TO TAKEOFF 1 CE 01 267UE 120071 ORD - RIGHT POWER LEVER HANGS UP DURING TAKEOFF. MAINTENANCE FOUND LOOSE DRAIN LINE CAUSING LINKAGE TO HANG-UP. SECURE D LINE AND OPS GOOD. (M0 2 L 7 2 4T RT A31SO 1996081500549 19960815 00549 WP 1996 8 15 RRXA96042 1 19960725 A 3231 57156105501 VALVE DOUG DC8 DC873F 302199F WP MLG DOOR MALFUNCTIONED A RRXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 15 870TV 528X 46086 KOAK - FLT 1 - AFTER GEAR RETRACTION, THREE GREEN LIGHTS EXTINGUISHED, DOORS NOT LATCHED AND GEAR NOT LATCHED RED LIGHTS ILLUMINATED. ON POST FLIGHT INSPECTION, FOUND TIRE MARKS ON DOOR. INDICATING RIGHT MLG DOOR IS NOT OPENING. RETURNED TO KOAK. MAINTENANCE REMOVED AND REPLACED THE RIGHT MLG DOOR CONTROL VALVE AND RIGGED PER MAINTENANCE MANUAL 32-31-5 S WUNG GEAR, OPS CHECKS NORMAL. (M) 2 L 7 4 4F RT 4A25 1996081500550 19960815 00550 NM 1996 8 15 TWRA95110 1 19960706 A 3350 S1356B37 LIGHT BOEING 747 747238B 1384828 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 607PE 20011 DURING DAILY CHECK, FOUND MAIN CABIN 'B' ZONE CEILING EMERGENCY LIGHT FORWARD RIGHT FLUCTUATES. REPLACED OVERHEAD CEILI NG EMERGENCY LIGHT, OPS CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500551 19960815 00551 NM 1996 8 15 TWRA96100 1 19960703 A 3350 ML7715 BULB BOEING 747 747212B 1384886 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND THE FLOORING FLOOR MOUNTED EVAC LIGHT ARE LOOSE INOP OR LENSES MISSING (ADJACENT OT SEATS 1H, 11C, 14C, 31H, 35H, 39H, 45H, 62H). REPLACED ALL LIGHTS LENSES AND RELAMPED 1H, 11C, 14C 31H, 39H, 45H. OPS CHECK PER MM 33-51-00 PAGE 501. (M) 2 L 7 4 4F A20WE 1996081500552 19960815 00552 NM 1996 8 15 TWRA96101 1 19960703 A 3350 30041801 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND 1L DOOR BUSTLE EVAC LIGHT INOP. REMOVED AND REPLACED BUSTLE LIGHT AT L1 DOOR, OPS CHECK NORMA L AS PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500553 19960815 00553 NM 1996 8 15 TWRA96102 1 19960703 A 3350 S1356B37 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND CEILING EVAC LIGHT INOP IN AISLE AT SEAT ROW 64AC. REMOVED AND REPLACED OVERHEAD LIGHT AT SEA T 64AC. OPS CHECK OK AS PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500554 19960815 00554 NM 1996 8 15 TWRA96103 1 19960703 A 3350 S1356A36 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND CEILING EVAC LIGHT INOP IN AISLE AT SEAT ROW 51ABC. REMOVED AND REPLACED EVAC LIGHT AT O/H 51 ABC. OPS CHECK NORMAL AS PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500555 19960815 00555 NM 1996 8 15 TWRA96104 1 19960703 A 3350 90084 POWER SUPPLY BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND OVERHEAD AISLE EXIT LIGHT INOP AT SEAT ROW 31ABC AND 35ABC. REMOVED AND REPLACED POWER SUPPLY AND PERFORMED OPS CHECK, OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500556 19960815 00556 NM 1996 8 15 TWRA96105 1 19960703 A 3350 S1356B37 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND CEILING EVAC LIGHT INOP IN AISLE AT SEAT ROW 51HJK. REMOVED AND REPLACED O/H EVAC LIGHT AT 52 HJK. OPS CHECKED NORMAL AS PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500557 19960815 00557 NM 1996 8 15 TWRA96106 1 19960703 A 3350 58541 STRIP BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND 3 FLOOR MOUNTED EVAC LIGHTS ARE INOPERATIVE, LOOSE, MISSING LENSES BETWEEN SEAT ROW 28ABC AND 30ABC. REPLACED LIGHT STRIP AND MISSING CAPS AND LIGHTS BULBS. OPS CHECK NORMAL PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500558 19960815 00558 NM 1996 8 15 TWRA96107 1 19960706 A 3350 ML7715 BULB BOEING 747 747212B 1384886 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURIG DAILY CHECK, FOUND 62H, 58H, 50H, 40H, FLOOR EMERGENCY LIGHTS INOP, ALSO 12C 28C, 64C. RELAMPED, OPS CHECK OK PER MM 33-51-00 PAGE 501. (M) 2 L 7 4 4F A20WE 1996081500559 19960815 00559 NM 1996 8 15 TWRA96108 1 19960706 A 3397 WIRE BOEING 747 747212B 1384886 NM CABIN BROKEN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND NR 1 R MED 'EXIT' EMERGENCY LIGHT INOP. REPAIRED BROKEN WIRE. OPS CHECK OK PER MM 33-51-00 P AGE 501. (M) 2 L 7 4 4F A20WE 1996081500560 19960815 00560 NM 1996 8 15 TWRA96109 1 19960706 A 3397 WIRE BOEING 747 747212B 1384886 NM CABIN BROKEN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND BETWEEN 1KH AND 6KH FLOOR EMERGENCY LIGHTS INOP. REPAIRED WIRE UNDER SEAT. OPS CHECK OK PER MM 33-51-00 PAGE 501. (M) 2 L 7 4 4F A20WE 1996081500561 19960815 00561 NM 1996 8 15 TWRA96111 1 19960706 A 3350 CONNECTOR BOEING 747 747136 1384883 NM CABIN LOOSE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 606FF 20273 DURING DAILY CHECK, FOUND UPPER DECK EXIT LIGHT, STAIRWAY SIDEWALL EMERGENCY LIGHT BETWEEN 1L MED AND 1R MED GALLEY FLOO R EMERGENCY LIGHT AND 'A' ZONE 4AB TO 6AB FLOOR EMERGENCY LIGHT INOP. REPAIRED CONNECTOR COMING FROM POWER SUPPLY TO ST AIRWAY E PATH. OPS CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500562 19960815 00562 NM 1996 8 15 TWRA96112 1 19960705 A 3397 WIRE BOEING 747 747121 1384871 NM CABIN LOOSE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 604FF 19659 DURING DAILY CHECK, FOUND EVAC LIGHTS INOP, MOUNTED ON SEAT SIDE PANEL BETWEEN 41H AND 35H. FOUND LOOSE WIRE, SECURED W IRE ON SEATS BETWEEN 41H AND 35H. OPS CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500563 19960815 00563 NM 1996 8 15 TWRA96113 1 19960705 A 3350 276001 FUSE BOEING 747 747212B 1384886 NM CABIN BLOWN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND 'Z' ZONE ENTIRE RIGHT SIDE 'E' PATH LIGHT STRIP INOP. REPLACED FUSE, LIGHT. OPS CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500564 19960815 00564 NM 1996 8 15 TWRA96114 1 19960705 A 3350 ML7715 BULB BOEING 747 747212B 1384886 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND 'C' ZONE SEAT 31K, 'B' ZONE 12A, 14A (EVAC) LIGHT INOP. REPLACED LENS, BULB AND LIGHT. OPS C HECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500565 19960815 00565 NM 1996 8 15 TWRA96115 1 19960705 A 3350 ML7715 BULB BOEING 747 747212B 1384886 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND 'D' ZONE 'E' PATH LIGHT, RIGHT SIDE SEAT 45H, INOP. REPLACED BULB, OPS CHECK OK PER MM 33-51- 00. (M) 2 L 7 4 4F A20WE 1996081500566 19960815 00566 NM 1996 8 15 TWRA96116 1 19960705 A 3350 ML7715 BULB BOEING 747 747212B 1384886 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND 'E' ZONE, 'E' PATH LIGHTS AT RIGHT SIDE SEATS 50H AND 58K INOP. REPLACED LENS, BULB, AND LIGH T. OPS CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500567 19960815 00567 NM 1996 8 15 TWRA96117 1 19960706 A 3350 ML7715 BULB BOEING 747 747212B 1384886 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND MAIN CABIN CROSSOVER EXIT LIGHT INOP 'B' ZONE FORWARD RIGHT. RELAMPED, OPS CHECK OK PER MM 33 -51-00. (M) 2 L 7 4 4F A20WE 1996081500568 19960815 00568 NM 1996 8 15 TWRA96118 1 19960706 A 3350 TERMINAL BOEING 747 747212B 1384886 NM CABIN LOOSE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND MAIN CABIN CROSSOVER LIGHT INOP 'A' ZONE RIGHT. FOUND LOOSE TERMINAL. RESECURED, OPS CHECK O K PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500569 19960815 00569 NM 1996 8 15 TWRA96119 1 19960706 A 3397 WIRE BOEING 747 747212B 1384886 NM CABIN BROKEN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND MAIN CABIN CROSSOVER 'EXIT' LIGHT INOP 'E' ZONE AFT RIGHT. FOUND WIRE BROKEN. REPAIRED, OPS CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500570 19960815 00570 NM 1996 8 15 TWRA96120 1 19960705 A 3350 ML7715 BULB BOEING 747 747212B 1384886 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND 'C' ZONE PATH LIGHT LEFT SIDE LAST RED LIGHT INOP. REPLACED BULB, OPS CHECK OK PER MM 33-51-0 0. (M) 2 L 7 4 4F A20WE 1996081500572 19960815 00572 NM 1996 8 15 TWRA96138 1 19960710 A 3350 276005 FUSE BOEING 747 747130 1384880 NM CABIN BLOWN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 603FF 19746 DURING DAILY CHECK, FOUND 'E' ZONE R/S 'E' PATH LIGHT INOP. REPLACED FUSE AND REPAIRED CHAFED WIRE AT SEAT TRACK. OPS CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500573 19960815 00573 NM 1996 8 15 TWRA96144 1 19960714 A 3350 S1356B37 BATTERY PACK BOEING 747 747130 1384880 NM CABIN DISCHARGED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 603FF 19746 DURING DAILY CHECK, FOUND EGRESS LIGHT LEFT SIDE 'E' ZONE ENTIRE COLUMN INOP. REPAIRED CHAFED WIRE AND REPLACED BATTERY PACK, OPS CHECK NORMAL PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500574 19960815 00574 NM 1996 8 15 TWRA96145 1 19960710 A 3350 ML7715 BULB BOEING 747 747212B 1384886 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND EVAC LIGHTS INOP AT ROW 14C, 40H, 53C AND 58H. REPLACED BULB, OPS CHECK OK PER MM 33-51-00. ( M) 2 L 7 4 4F A20WE 1996081500575 19960815 00575 NM 1996 8 15 TWRA96146 1 19960710 A 3397 WIRE BOEING 747 747212B 1384886 NM CABIN LOOSE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND EVAC LIGHT INOP AT NR 2L MED JUMP SEAT. REWIRED AND CHANGED TRACK COVER, OPS CHECK OK MM 33-5 1-00. (M) 2 L 7 4 4F A20WE 1996081500576 19960815 00576 NM 1996 8 15 TWRA96147 1 19960710 A 3350 387 SWITCH BOEING 747 747212B 1384886 NM 1L DOOR INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND NR 1 MED CONTROL PANEL EVAC INDICATOR LIGHT INOP. REPLACED EVAC EMERGENCY SWITCH, OPS CHECK O K PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500577 19960815 00577 NM 1996 8 15 TWRA96148 1 19960713 A 3350 1317 BULB BOEING 747 747212B 1384886 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND L1 MED EVAC EXIT SIGN BULB OUT. REPLACED BULB, OPS CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500578 19960815 00578 NM 1996 8 15 TWRA96149 1 19960713 A 3350 07912 CAP BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURNG DAILY CHECK, FOUND EVAC FLOOR LIGHT OUT, FORWARD OF L2 JUMP SEAT (2ND LIGHT). REPLACED EMERGENCY LIGHT CAP AND BU LB. OPS CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500579 19960815 00579 NM 1996 8 15 TWRA96150 1 19960713 A 3350 ML7715 BULB BOEING 747 747212B 1384886 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND EVAC LIGHT OUT (FLOOR) SEAT 11C, 11 HJK, 12C, 14C, 36C AND 36 HJK. REPLACED EMERGENCY LIGHT L ENS AND BULB. OPS CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500580 19960815 00580 NM 1996 8 15 TWRA96151 1 19960713 A 3350 S1356B37 BATTERY CHARGER BOEING 747 747212B 1384886 NM CABIN MALFUNCTIONED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND EXIT SIGN ABOVE SEAT 10 C (EVAC) ALL LIGHTS OUT. REPLACED EMERGENCY LIGHT BATTERY CHARGER. L IGHT OPS CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500581 19960815 00581 NM 1996 8 15 TWRA96153 1 19960712 A 3350 RP51B BATTERY PACK BOEING 747 747130 1384880 NM CABIN DISCHARGED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 603FF 19746 DURING DAILY CHECK, FOUND 'E' ZONE LEFT ROW EMERGENCY LIGHTS OUT. RELAMPED, EMERGENCY PACK. OPS CHECK OK PER MM 33-51- 00. (M) 2 L 7 4 4F A20WE 1996081500582 19960815 00582 NM 1996 8 15 TWRA96154 1 19960712 A 3350 RP51B BATTERY PACK BOEING 747 747130 1384880 NM CABIN DISCHARGED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 603FF 19746 DURING DAILY CHECK, FOUND 'E' ZONE RIGHT SIDE EMERGENCY LIGHTS OUT. REPLACED EMERGENCY PACKS. OPS CHECK PER MM 33-51-0 0. (M) 2 L 7 4 4F A20WE 1996081500583 19960815 00583 NM 1996 8 15 TWRA96155 1 19960714 A 3350 900835A BATTERY PACK BOEING 747 747130 1384880 NM CABIN DISCHARGED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 603FF 19746 DURING DAILY CHECK, FOUND EGRESS LIGHTS LEFT SIDE 'E' ZONE ENTIRE COLUMN INOP. REPAIRED CHAFED WIRE AND REPLACED BATTER Y PACK. OPS CHECK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500584 19960815 00584 NM 1996 8 15 TWRA96156 1 19960712 A 3350 LIGHT BOEING 747 747212B 1384886 NM CABIN LOOSE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND 4R MED EVAC EXIT LIGHT OUT. RECONNECTED LIGHT ASSY. OPS CHECK OK PER MM 33-51-00 PAGE 501. ( M) 2 L 7 4 4F A20WE 1996081500585 19960815 00585 NM 1996 8 15 TWRA96157 1 19960712 A 3350 CM7715 BULB BOEING 747 747212B 1384886 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND FIRST THREE EVAC LIGHTS OUT AFT OF 4R MED. RELAMPED, OPS CHECK OK PER MM 33-51-00 PAGE 501. ( M) 2 L 7 4 4F A20WE 1996081500586 19960815 00586 NM 1996 8 15 TWRA96158 1 19960712 A 3350 CM7715 BULB BOEING 747 747212B 1384886 NM CABIN BLOWN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND FIRST THREE FLOOR EVAC LIGHTS OUT AFT OF 4L MED. RELAMPED, OPS CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500587 19960815 00587 NM 1996 8 15 TWRA96159 1 19960712 A 3350 276005 FUSE BOEING 747 747212B 1384886 NM CABIN BLOWN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND BETWEEN 3R MED AND 4R MED ALL EVAC LIGHTS ARE OUT (FLOOR). REPLACED FUSE, OPS CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500588 19960815 00588 NM 1996 8 15 TWRA96160 1 19960712 A 3350 276005 FUSE BOEING 747 747212B 1384886 NM CABIN BLOWN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND BETWEEN 3L MED AND 4L MED ALL EVAC LIGHTS ARE OUT (FLOOR). REPLACED FUSE. OPS CHECK OK PER M M 33-51-00 PAGE 501. (M) 2 L 7 4 4F A20WE 1996081500589 19960815 00589 NM 1996 8 15 TWRA96161 1 19960712 A 3350 LIGHT BOEING 747 747212B 1384886 NM CABIN DISCONNECTED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND 3L MED EMERGENCY EXIT SIGN LIGHTS OUT. FOUND DISCONNECTED LIGHT ASSEMBLY. RECONNECTED. OPS CHECK OK PER MM 33-51-00 PAGE 501. (M) 2 L 7 4 4F A20WE 1996081500590 19960815 00590 NM 1996 8 15 TWRA96162 1 19960712 A 3350 07912CM7715 LIGHT BOEING 747 747212B 1384886 NM CABIN MISSING A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND SEAT 14C FLOOR EMERGENCY LIGHT HAS CAP AND LIGHT MISSING. REPLACED LIGHT AND CAP. OPS CHECK OK PER MM 33-51-00 PAGE 501. (M) 2 L 7 4 4F A20WE 1996081500591 19960815 00591 NM 1996 8 15 TWRA96163 1 19960715 A 3350 PLUG BOEING 747 747212B 1384886 NM CABIN LOOSE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 620FF 21162 DURING DAILY CHECK, FOUND EMERGENCY CEILING LIGHT INOP ABOVE SEAT 52C. RESET PLUG ON LIGHT ASSY, OPS CHECK OK PER MM 33 -51-00. (M) 2 L 7 4 4F A20WE 1996081500592 19960815 00592 NM 1996 8 15 TWRA96165 1 19960713 A 2760 HANDLE BOEING 747 747212B 1384886 NM AUTO SPOILER OUT OF ADJUST A TWRA O OTHER N FALSE WARNING DE DESCENT 1 EA 15 618FF 21937 DURING DESCENT, AUTO SPOILER WOULD NOT ARM (JAMMED) ON LANDING, AUTO SPOILER LIGHT CAME ON IN PEDESTAL. FOUND ARMING PA WL ON TIP OF HANDLE STOP. ADJUSTED PAWL. PERFORMED OPS CHECK PER MM 27-61-00. OPS CHECK NORMAL ON SEVERAL ATTEMPTS. A IRCRAFT CONTINUED IN SERVICE. (M) 2 L 7 4 4F A20WE 1996081500593 19960815 00593 NM 1996 8 15 TWRA96166 1 19960715 A 3350 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 620FF 21162 DURING DAILY CHECK, FOUND R1 MED UPPER BUSTLE DOOR LIGHT INOP. OPERATED LIGHTS, FOUND TO BE NORMAL OPERATION. (M) 2 L 7 4 4F A20WE 1996081500594 19960815 00594 NM 1996 8 15 TWRA96167 1 19960714 A 3350 1317 BULB BOEING 747 747121 1384871 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 604FF 19659 DURING DAILY CHECK, FOUND EMERGENCY LIGHTS AT5R DOOR THRESHOLD BOTH INOP. RELAMPED, OPS CHECK NORMAL PER MM 33-51-00. ( M) 2 L 7 4 4F A20WE 1996081500595 19960815 00595 NM 1996 8 15 TWRA96168 1 19960716 A 3350 07912 LENS BOEING 747 747212B 1384886 NM CABIN MISSING A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND SEAT 53ABC LENS AND BULB MISSING. REPLACED LENS AND BULB, OPS CHECK NORMAL PER MM 33-51-00. ( M) 2 L 7 4 4F A20WE 1996081500596 19960815 00596 NM 1996 8 15 TWRA96169 1 19960716 A 3350 BULB BOEING 747 747212B 1384886 NM CABIN LOOSE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND 5L MED EVAC EXIT SIGN INOP. RESEATED BULB, OPS CHECK NORMAL PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500597 19960815 00597 NM 1996 8 15 TWRA96170 1 19960716 A 3350 ML7715 BULB BOEING 747 747212B 1384886 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND EVAC FLOOR LIGHT OUT SEAT 5H. RELAMPED SEAT 5H. OPS CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500598 19960815 00598 NM 1996 8 15 TWRA96171 1 19960716 A 3350 07912 LENS BOEING 747 747212B 1384886 NM CABIN MISSING A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND EVAC FLOOR CAP AND BULB INOP SEAT 50H. REPLACED CAP AND BULB, OPS CHECK OK PR MM 33-51-00. ( M) 2 L 7 4 4F A20WE 1996081500599 19960815 00599 NM 1996 8 15 TWRA96172 1 19960716 A 3350 07912 LENS BOEING 747 747212B 1384886 NM CABIN MISSING A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND EVAC FLOOR CAP AND LIGHT OUT SEAT 40H. PLACED LENS AND REPAIRED WIRE. OPS CHECK NORMAL PER M M 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500600 19960815 00600 NM 1996 8 15 TWRA96173 1 19960716 A 3350 07912 CAP BOEING 747 747212B 1384886 NM CABIN MISSING A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND EVAC FLOOR LIGHT AND CAP OUT SEAT 12C. REPLACED FLOOR EVAC CAP. OPS CHECK NORMAL PER MM 33-5 1-00. (M) 2 L 7 4 4F A20WE 1996081500601 19960815 00601 NM 1996 8 15 TWRA96174 1 19960716 A 3350 ML7715 BULB BOEING 747 747212B 1384886 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND U/D CREW DOOR EXIT SIGN EVAC (E) LIGHT OUT. RELAMPED EXIT SIGN (E). OPS CHECK OK PER MM 33-5 1-00. (M) 2 L 7 4 4F A20WE 1996081500602 19960815 00602 NM 1996 8 15 TWRA96175 1 19960716 A 3350 S1356B37 LIGHT BOEING 747 747130 1384880 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 603FF 19746 DURING DAILY CHECK, FOUND CEILING EVAC LIGHT INOP JUST FWD OF SPIRAL STAIRWAY ON L/S IN 'A' ZONE. REPLACE CEILING EVAC LIGHT, OPS CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500603 19960815 00603 NM 1996 8 15 TWRA96176 1 19960717 A 3350 1317 BULB BOEING 747 747238B 1384828 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 614FF 20534 DURING DAILY CHECK, FOUND RIGHT OVERWING EVAC LIGHT UOT FIRST FROM BOTTOM. RELAMPED, OPS CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500604 19960815 00604 NM 1996 8 15 TWRA96177 1 19960717 A 3350 1317 BULB BOEING 747 747238B 1384828 NM CABIN MISSING A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 607PE 20011 DURING DAILY CHECK, FOUND OUTSIDE WALL OF LAV 'K' EVAC LIGHT BULB MISSING AND LENS MISSING. REPLACED BULB AND COVER, OP S CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500605 19960815 00605 NM 1996 8 15 TWRA96178 1 19960717 A 2611 30231A7 SMOKE DETECTOR BOEING 747 747124 1384874 NM CARGO COMPT MALFUNCTION A TWRA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 EA 15 602FF 837 19734 IN CRUISE AT FL 390, LOWER FWD CARGO FIRE WARNING (BELL/LIGHTS) CAME ON. WHEN FIRE BOTTLE NR 1 WAS DISCHARGED, FIRE WAR NING LIGHTS WENT OUT IMMEDIATELY. FM VOL, 1 PAGE 2.12.2 PROCEDURE WAS ACCOMPLISHED SUSPECTED FAULTY WARNING SYSTEM. F/ E MADE PHYSICAL INSPECTION OF CARGO COMPARTMENT IN FLIGHT AND FOUND NO EVEIDENCE OF HEAT, FIRE OR SMOKE. MAINTENANCE IN SPECTED THE AREA, FOUND NO EVIDENCE OF HEAT, FIRE OR SMOKE. FOUND TO BE AN INDICATION PROBLEM. REMOVED AND REPLACED DE TECTOR, SMOKE DETECTOR AMPLIFIER. OPS CHECK NORMAL PER MM 26-16-11. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 4 4F A20WE 1996081500606 19960815 00606 NM 1996 8 15 TWRA96179 1 19960718 A 3350 276005 FUSE BOEING 747 747130 1384880 NM CABIN BLOWN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 603FF 19746 DURING DAILY CHECK, FOUND R/S 'E' ZONE EVAC LIGHT OUT. REPLACED FUSE ON BATTERY PACK. OPS CHECK OK PER MM 33-51-00. ( M) 2 L 7 4 4F A20WE 1996081500607 19960815 00607 NM 1996 8 15 TWRA96180 1 19960718 A 3350 RP51B BATTERY CHARGER BOEING 747 747238B 1384828 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 614FF 20534 DURING DAILY CHECK, FOUND 'B' ZONE RIGHT FLOOR EVAC LIGHTS INOP. REPLACED BATTERY CHARGER, OPS CHECK OK PER MM 33-51-00 . (M) 2 L 7 4 4F A20WE 1996081500608 19960815 00608 NM 1996 8 15 TWRA96181 1 19960718 A 3350 S1356A36 LIGHT BOEING 747 747238B 1384828 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 614FF 20534 DURING DAILY CHECK, FOUND NR 5 RIGHT AND NR 5 LEFT MED CEILING SILL EMERGENCY LIGHT INOP, (AFT SIDE). REPLACED CEILNG L IGHT, OPS CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500609 19960815 00609 NM 1996 8 15 TWRA96182 1 19960718 A 3350 RP51B BATTERY CHARGER BOEING 747 747238B 1384828 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 614FF 20534 DURING DAILY CHECK, FOUND UPPER DECK RIGHT FLOOR EVAC LIGHTS INOP (ENTIRE STRIP). REPLACED BATTERY CHARGER, OPS CHECK O K PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500610 19960815 00610 NM 1996 8 15 TWRA96183 1 19960718 A 3350 ML7715 BULB BOEING 747 747212B 1384886 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND 'E' ZONE LEFT FLOOR EVAC LIGHT INOP AT SET 58C. RELAMPED, OPS CHECK OK PR MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500611 19960815 00611 NM 1996 8 15 TWRA96184 1 19960718 A 3350 ML7715 BULB BOEING 747 747212B 1384886 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND B-ZONE FLOOR LEFT STRIP HAS TWO LIGHTS INOP, 10C AND 12C. REPLACED BULB, OPS CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500612 19960815 00612 NM 1996 8 15 TWRA96185 1 19960718 A 3350 ML7715 BULB BOEING 747 747212B 1384886 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND 'E' ZONE AFT LEFT CROSSOVER EXIT SIGN INOP. RELAMPED, OPS CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500613 19960815 00613 NM 1996 8 15 TWRA96186 1 19960717 A 3350 07912 LENS BOEING 747 747238B 1384828 NM CABIN MISSING A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 607PE 20011 DURING DAILY CHECK, FOUND ROW 58C EVAC LIGHT MISSING. REPLACED LENS AND BULB, OPS CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500614 19960815 00614 NM 1996 8 15 TWRA96188 1 19960717 A 3350 BATTERY BOEING 747 747238B 1384828 NM CABIN DISCHARGED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 607PE 20011 DURING DAILY CHECK, FOUND SPIRAL STAIRWAY (EXIT LIGHTS) INOP. RECHARGED BATTERY, OPS CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500615 19960815 00615 NM 1996 8 15 TWRA96189 1 19960717 A 3350 ML7715 BULB BOEING 747 747238B 1384828 NM DOOR FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 607PE 20011 DURING DAILY CHECK, FOUND NR 1 MED AUX BAR FLOOR EVAC LIGHT INTERMITTENT. REPLACED BULB AND SECURED STRIP. CHECKED OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500616 19960815 00616 NM 1996 8 15 TWRA96190 1 19960718 A 3350 1317 BULB BOEING 747 747121 1384871 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 609FF 20354 DURING DAILY CHECK, FOUND 7ABC SEAT EVAC LGHT INOP. RELAMPED 7ABC. OPS CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500617 19960815 00617 NM 1996 8 15 TWRA96191 1 19960718 A 3397 WIRE BOEING 747 747121 1384871 NM CABIN BROKEN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 609FF 20354 DURING DAILY CHECK, FOUND 30ABC, 40ABC, 58ABC SEAT EVAC LIGHT INOP. REPAIRED BROKEN WIRE UNDER SEAT, OPS CHECK OK PR MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500618 19960815 00618 NM 1996 8 15 TWRA96192 1 19960720 A 3350 58541 STRIP BOEING 747 747282B 1384860 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 611FF 20502 DURING DAILY CHECK, FOUND UPPER DECK EGRESS LIGHT IS INOP AND LEFT OF 'Z' ZONE EGRESS LIGHTS ARE INOP. REMOVED AND REPL ACED STRIP IN UPPER DECK AND REPAIRED BROKEN WIRE IN 'A' ZONE PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500619 19960815 00619 NM 1996 8 15 TWRA96194 1 19960723 A 3350 S1356B37 LIGHT BOEING 747 747124 1384874 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 602FF 19734 DURING DAILY CHECK, FOUND EVAC CEILING LIGHT INOP BY SEATS 54HJK. REPLACED LIGHT ASSY AT SEAT 54HJK EMERGENCY LIGHT. OP S CHECK NORMAL PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500620 19960815 00620 NM 1996 8 15 TWRA9660 1 19960626 A 3350 FUSE BOEING 747 747130 1384880 NM CABIN BLOWN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 603FF 19746 DURING DAILY SERVICE CHECK, FOUND EVAC LIGHTS ON ALL SEATS IN 'E' ZONE RIGHT SIDE INOP. FOUND FUSE BLOWN REPLACED 5 AMP FUSE. OPS CHECK OK MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500621 19960815 00621 NM 1996 8 15 TWRA9668 1 19960628 A 2611 8240PY SMOKE DETECTOR BOEING 747 747238B 1384828 NM LAVATORY WIRE BROKEN A TWRA K NONE O OTHER IN INSP/MAINT 1 EA 15 614FF 20534 DURING DAILY SERVICE, FOUND 'J' AND 'Q' LAV SMOKE DETECTOR INOP. FOUND BROKEN WIRE, REPAIRED WIRING, OPS CHECK OK. (M) 2 L 7 4 4F A20WE 1996081500622 19960815 00622 NM 1996 8 15 TWRA9674 1 19960628 A 3350 276001 FUSE BOEING 747 747121 1384871 NM CABIN BLOWN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 609FF 20354 DURING DAILY CHECK, FOUND LEFT EXTERIOR 3RD EVAC LIGHT IS INOP. REPLACED FUSE FOR EXTERIOR LIGHT ASSEMBLY. OPS CHECK O K MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500623 19960815 00623 NM 1996 8 15 TWRA9675 1 19960628 A 3350 ML7715 BULB BOEING 747 747212B 1384886 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 'EVAC' LIGHT ON SEAT 39H IS INOPERATIVE. (FOUND DURING DAILY SERVICE.) ALSO, SEAT 60C AND SEAT 61C. REPLACED LIGHT BU LBS. OPS CHECK OK, MM-33-41-00. (X) 2 L 7 4 4F A20WE 1996081500624 19960815 00624 NM 1996 8 15 TWRA9676 1 19960628 A 3350 1356B37 BATT CHARGER BOEING 747 747121 1384871 NM CABIN MALFUNCTIONED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 609FF 20354 DURING DAILY SERVICE, FOUND 'EVAC' CEILING LIGHT INOP AJACENT TO SEAT 71C. FOUND BATTERY PACK LOW VOLTS, REPLACED CHARG ER, OPS CHECK OK. (M) 2 L 7 4 4F A20WE 1996081500625 19960815 00625 NM 1996 8 15 TWRA9678 1 19960628 A 3350 BULB BOEING 747 747238B 1384828 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 614FF 20534 FLOOR EVAC EMERGENCY LIGHTS ARE INOP AT 44C, 15H. RELAMP LIGHT. OPS CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500626 19960815 00626 NM 1996 8 15 TWRA9679 1 19960628 A 3350 S1356B37 LIGHT BOEING 747 747238B 1384828 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 614FF 20534 CEILING EMERGENCY LIGHTS ARE INOP AT 25C, 54H. RELAMP LIGHT ASSY, OPS CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500627 19960815 00627 NM 1996 8 15 TWRA9680 1 19960628 A 3350 LIGHT BOEING 747 747238B 1384828 NM CABIN BROKEN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 614FF 20534 AFT OF NR 3 L MED EXIT EMERGENCY LIGHT IS INOP. FOUND BROKE ASSY, OPS CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500628 19960815 00628 NM 1996 8 15 TWRA9681 1 19960701 A 3350 LIGHT BOEING 747 747136 1384883 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 606FF 20273 DURING DAILY CHECK, FOUND 'E' ZONE, AFT GALLEY WHOLE FLOOR EMERGENY LIGHT IS INOP. FOUND AFT GALLEY STRIP WET, DRIED ST RIP AND CHECKED OPERATION OF EMERGENCY LIGHTS. CHECKS OK PER 33-51-00 PG 501. (M) 2 L 7 4 4F A20WE 1996081500629 19960815 00629 NM 1996 8 15 TWRA9682 1 19960629 A 3350 S1356B37 BATTERY CHARGER BOEING 747 747130 1384880 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 603FF 19746 DURING DAILY CHECK, FOUND LEFT SEAT ROW EMERGENCY LIGHTS INOP THROUGH OUT 'E' ZONE. REPLACED CHARGER OPERATION CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500630 19960815 00630 NM 1996 8 15 TWRA9683 1 19960629 A 3350 1317 BULB BOEING 747 747130 1384880 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 603FF 19746 DURING DAILY CHECK, FOUND BUSTLE LIGHT INOP L1 MED. RELAMPED LIGHT, OPERATION CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500631 19960815 00631 NM 1996 8 15 TWRA9684 1 19960703 A 3350 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 620FF 21162 DURING DAILY CHECK, FOUND CEILING EMERGENCY LIGHT INOP, BETWEEN 4R AND 4L MAIN ENTRY DOOR FWD GALLEY. ITEM DEFERRED AS PER MEL 33-13-C. (M) 2 L 7 4 4F A20WE 1996081500632 19960815 00632 NM 1996 8 15 TWRA9686 1 19960703 A 3350 980084 POWER PACK BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY SERVICE, FOUND OVERHEAD EXIT LIGHT INOP AT SEAT ROW 31 ABC-35 ABC. REMOVED AND REPLACED POWER PACK ASSY, O PS CHECK OK MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500633 19960815 00633 NM 1996 8 15 TWRA9687 1 19960703 A 3350 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY SERVICE, FOUND FLOOR MOUNTED 'EVAC' LIGHT LOOSE, LENSE COVER MISSING AND INOP. ADJACENT TO SEAT 1H, 1C, 14 C, 31H, 39H, 45H AND 62H. RELAMPED AS NEEDED AND REPLACED LENSE COVERS MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500634 19960815 00634 NM 1996 8 15 TWRA9688 1 19960703 A 3350 31356A36 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY SERVICE, FOUND CEILING 'EVAC' LIGHTS INOP AT SEAT ROW 51 ABC AND 52 HJK. (M) 2 L 7 4 4F A20WE 1996081500636 19960815 00636 NM 1996 8 15 TWRA9691 1 19960704 A 3397 WIRE BOEING 747 747124 1384874 NM CABIN BROKEN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 602FF 19734 DURING DAILY CHECK, FOUND 65H SEAT EMERGENCY LIGHT INOP. REPAIRED BROKEN WIRE, OPS CHECK NORMAL MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500637 19960815 00637 NM 1996 8 15 TWRA9692 1 19960704 A 3350 1317 BULB BOEING 747 747130 1384880 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 603FF 19746 DURING DAILY CHECK, FOUND LEFT SIDE CEILINGS (EVAC LIGHT) NEXT TO ROW 37 ABC INOP. RELAMPED, OPS CHECK OK PER MM 33-51- 00. (M) 2 L 7 4 4F A20WE 1996081500638 19960815 00638 NM 1996 8 15 TWRA9693 1 19960704 A 3350 1317 BULB BOEING 747 747130 1384880 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 603FF 19746 DURING DAILY CHECK, FOUND 4L MED UPPER BUSTLE LIGHT INOP. RELAMPED, OPS CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500639 19960815 00639 NM 1996 8 15 TWRA9694 1 19960704 A 3350 ML7715 BULB BOEING 747 747238B 1384828 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 614FF 20534 DURING DAILY CHECK, FOUND CABIN 'B' ZONE RIGHT SIDE 'E' PATH LIGHTS AT SEAT 16K AND 15K INOP. RELAMP, OPS CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500640 19960815 00640 NM 1996 8 15 TWRA9695 1 19960604 A 3350 ML7715 BULB BOEING 747 747238B 1384828 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 614FF 20534 DURING DAILY CHECK, FOUND CABIN 'B' ZONE LEFT SIDE 'E' PATH LIGHT AT SEAT 11A INOP. RELAMPED, OPS CHECK OK PER MM 33-51 -00. (M) 2 L 7 4 4F A20WE 1996081500641 19960815 00641 NM 1996 8 15 TWRA9696 1 19960704 A 3350 ML7715 BULB BOEING 747 747238B 1384828 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 614FF 20534 DURING DAILY CHECK, FOUND CABIN LEFT 'D' ZONE 'E' PATH LIGHT AT 42A TWO LIGHTS INOP AND 45A ONE LIGHT. RELAMPED, OPS CH ECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500642 19960815 00642 NM 1996 8 15 TWRA9697 1 19960704 A 3350 ML7715 BULB BOEING 747 747238B 1384828 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 614FF 20534 DURING DAILY CHECK, FOUND CABIN RIGHT 'D' ZONE 'E' PATH LIGHT AT SEAT 39K INOP. RELAMP, OPS CHECK OK AS PER MM 33-51-00 . (M) 2 L 7 4 4F A20WE 1996081500643 19960815 00643 NM 1996 8 15 TWRA9698 1 19960704 A 3350 ML7715 BULB BOEING 747 747238B 1384828 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 614FF 20534 DURING DAILY CHECK, FOUND CABIN 'E' ZONE LEFT SIDE 'E' PATH LIGHTS INOP AT 51A AND 58A. RELAMP, OPS CHECK OK PER MM 33- 51-00. (M) 2 L 7 4 4F A20WE 1996081500644 19960815 00644 NM 1996 8 15 TWRA9699 1 19960704 A 3350 ML7715 BULB BOEING 747 747238B 1384828 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 614FF 20534 DURING DAILY CHECK, FOUND CABIN 'E' RIGHT SIDE 'E' PATH LIGHT STRIP BETWEEN 50 TO 51 NOT SECURED. RELAMPED AND SECURED. OPS CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500645 19960815 00645 EU 1996 8 15 VTZA96253 1 19960712 A 3412 102AU1AG HEATER JETAIR JETSTM JETSTM4101 1500501 EU TAT PROBE FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 309UE 41022 FLT NR 6160 - IAD-TYS - DURING CRUISE, RETURNED TO IAD DUE TO TAT PROBE HEATER FAILED IN FLIGHT. AIRCRAFT RETURNED TO G ATE WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED TAT PROBE, OPS CHECKS OK. AIRCRAFT WAS RELEASED AND AP PROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996081500646 19960815 00646 EU 1996 8 15 VTZA96254 1 19960715 A 2770 GUST LOCK JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT NOT SET A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 309UE 41022 FLT NR 6517 - IAD-BOS - ABORTED TAKEOFF DUE TO TAKEOFF CONFIGURATION WARNING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE RESET GUSTLOCK HANDLE, OPS CHECKS OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE . (M) 2 L 7 2 4T RT A41NM 1996081500647 19960815 00647 EU 1996 8 15 VTZA96255 1 19960712 A 7722 6100116 EGT GAUGE BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A VTZA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 490UE 909 FLT NR 6243 - IAD-PHF - DURING TAXI, RETURNED TO GATE DUE TO LEFT EGT GAUGE DROPPED TO ZERO AND THEN WENT BACK UP. MAIN TENANCE REMOVED AND REPLACED EGT GAUGE, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996081500648 19960815 00648 EU 1996 8 15 VTZA96256 1 19960713 A 7712 PROC732201 TQ LIMITER VLV BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A VTZA A UNSCHED LANDING O OTHER TO TAKEOFF 1 EA 27 470UE 814 FLT NR 6250 - ABE-IAD - DURING TAKEOFF, MADE AN UNSCHEDULED LANDING AT ABE DUE TO LEFT ENGINE NOT MAKING TARGET TORQUE. AIRCRAFT RETURNED AND LANDED AT ABE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED TTL VALVE, OPS CHECKS OK. AIRCRAF T WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996081500649 19960815 00649 1996 8 15 VTZA96257 4 19960714 A 3422 258719343 DIRECTIONAL GYRO BAG JETSTM JETSTM3201 1500217 EU NR 2 FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK I FLT. ATTITUDE INST. TO TAKEOFF 1 EA 27 470UE 814 FLT NR 6261 - IAD-EWR - ABORTED TAKEOFF DUE TO NR 2 HSI FLAGGED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. M AINTENANCE REPLACED NR 2 DG, OPS CHECKS OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996081500650 19960815 00650 EU 1996 8 15 VTZA96258 1 19960714 A 5230 A1424D SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGG DOOR LOOSE A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 27 302UE 41013 FLT NR 6567 - BOS-EWR - ABORTED THE TAKEOFF DUE TO THE BAGGAGE DOOR WARNING LIGHT ILLUMINATING. AIRCRAFT RETURNED TO GA TE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 52857 IAW MEL 52-3. MAINTENANCE CLOSED DMI 52857 ON 7-16-96 BY RESECURING MICROSWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996081500651 19960815 00651 EU 1996 8 15 VTZA96259 1 19960718 A 5230 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGG DOOR OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 302UE 41013 FLT NR 6547 - IAD-ROA - ABORTED TAKEOFF DUE TO BAGGAGE DOOR LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHE R INCIDENTS. MAINTENANCE OPENED DMI 52680, IAW MEL 52-3. MAINTENANCE CLOSED DMI 52860 ON 7-2-96 BY ADJUSTING FWD BAGGA GE DOOR MICROSWITCH, OP CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996081500652 19960815 00652 1996 8 15 VTZA96260 4 19960715 A 3442 6222502001 ANTENNA BAG JETSTM JETSTM3201 1500217 EU NOSE FAILED A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 483UE 898 IAD-HVN - FLT 6173 - DURING CLIMB, MADE UNSCHEDULED LANDING AT IAD DUE TO RADAR FAILED IN FLIGHT. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED ANTENNA DRIVE. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996081500653 19960815 00653 EU 1996 8 15 VTZA96261 1 19960715 A 7712 31024766 TQ SIGNAL COND BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 27 470UE 814 FLT NR 6363 - LYH-IAD - ABORTED TAKEOFF DUE TO LEFT ENGINE WOULD NOT MAKE REQUIRED TAKEOFF TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED TORQUE SIGNAL CONDITIONER AND PERFORMED RECOMPUTATION OF LEFT ENGINE. OPS CHECKS OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996081500654 19960815 00654 EU 1996 8 15 VTZA96262 1 19960717 A 7930 696225 TRIPLE GAUGE BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A VTZA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 EA 27 488UE 907 FLT NR 6383 - IAD-CMH - DURING CLIMB, MADE A UNSCHEDULED LANDING DUE TO THE LEFT ENGINE HIGH OIL TEMP INDICATION. MAINT ENANCE REMOVED AND REPLACED LEFT ENGINE OIL TEMP INDICATOR, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996081500655 19960815 00655 EU 1996 8 15 VTZA96263 1 19960717 A 7722 CONNECTOR BAG JETSTM JETSTM3201 1500217 EU LT ENGINE LOOSE A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 479UE 893 PIT - IAD - FLT NR 6580 - DURING TAKEOFF DUE TO LEFT EGT FLUCTUATION. AIRCRAFT RETURNED TO GATE AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI 04160, MEL 76-10. MAINTENANCE ON 7-17-96 CLOSED DMI 04160 BY REPAIRING WIRE IN EGT C ANNON PLUG. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996081500656 19960815 00656 EU 1996 8 15 VTZA96264 1 19960719 A 7931 1241012 TRANSDUCER JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE FAILURE A VTZA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 301UE 41012 FLT NR 6324 - IAD-RDU - DURING TAXI, RETURNED TO GATE DUE TO LOW OIL PRESSURE CAP LIGHT. MAINTENANCE REMOVED AND REPLAC ED OIL PRESSURE TRANSDUCER, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996081500657 19960815 00657 EU 1996 8 15 VTZA96265 1 19960719 A 3260 AIR135022 UPLOCK SWITCH JETAIR JETSTM JETSTM4101 1500501 EU RT MLG FAILURE A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 310UE 41028 FLT 6222 - JFK-IAD - DURING CLIMB-OUT, RETURNED TO IAD DUE TO RED GEAR HANDLE LIGHT REMAINED ILLUMINATED AFTER GEAR SELE CTED UP. AIRCRAFT LANDED AT JFK WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED RIGHT GEAR UPLOCK SWITCH. AIRCRAFT WA S RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996081500658 19960815 00658 EU 1996 8 15 VTZA96266 1 19960719 A 7722 CONNECTOR BAG JETSTM JETSTM3201 1500217 EU RT ENG EGT DIRTY A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 493UE 805 FLT NR 6243 - IAD-PHF - ABORTED THE TAKEOFF DUE TO THE RIGHT ENGINE EGT FLUX. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE CLEANED ZONE 2 CANNON PLUG, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SER VICE. (M) 2 L 7 2 4T RT A56EU 1996081500659 19960815 00659 1996 8 15 VTZA96267 4 19960719 A 3425 7003360948 AHRS COMPUTER JETAIR JETSTM JETSTM4101 1500501 EU NR 1 FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 314UE 41027 FLT 6598 - IAD-RUD - ABORTED TAKEOFF DUE TO NR 1 EADI FAILURE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MX REMOVED AND REPLACED NR 1 AHRS COMPUTER, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996081500660 19960815 00660 NM 1996 8 15 W8PA960057 1 19960716 A 3350 BULB BOEING 737 7373B7 1384580 NM CABIN FAILED A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 947WP 23376 FOUND FLOOR TRACK EMERGENCY EXIT LIGHT MISSING AFT OF OVERWING EXIT ROW. RELAMPED AND REPLACED MISSING LENS. (M) 2 L 7 2 4F RT A16WE 1996081500661 19960815 00661 SO 1996 8 15 WTAA960135 1 19960707 A 3230 12038594001 CONTROL BOX EMB 120 EMB120RT SO RT MLG INTERMITTENT A WTAA O OTHER J WARNING INDICATION CL CLIMB 1 WP 17 216YV 120216 SMF - RIGHT MAIN LANDING GEAR FAILED TO RETRACT ON INITIAL ATTEMPT. GEAR RETRACTED NORMALLY ON SECOND ATTEMPT. AIRCRAF T FERRIED TO FAT FOR MAINTENANCE. MAINTENANCE REPLACED LANDING GEAR CONTROL BOX. SYSTEM OPERATIONAL CHECK NORMAL DURIN G GEAR RETRACTION CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996081500662 19960815 00662 EU 1996 8 15 WTAA960136 1 19960707 A 3260 622800200 SWITCH BAG JETSTM JETSTM3101 1500215 EU LT MLG DAMAGED WIRE A WTAA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 17 103XV 747 MCE - EN ROUTE MCE TO VIS, LEFT MAIN GEAR INDICATES DOWN AND LOCKED WITH GEAR RETRACTED. AIRCRAFT DIVERTED TO FAT. MX FOUND LEFT MAIN GEAR MICROSWITCH WIRES CHAFED. REPAIRED AS NECESSARY. SYSTEM OPERATIONAL CHECK NORMAL DURING GEAR RETR ACTION CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996081500663 19960815 00663 EU 1996 8 15 WTAA960137 1 19960707 A 3260 622800200 DOWNLOCK SW BAG JETSTM JETSTM3101 1500215 EU LT MLG FAILED A WTAA O OTHER N FALSE WARNING TO TAKEOFF 1 WP 17 103XV 747 MCE - LEFT MAIN GEAR INDICATES DOWN AND LOCK LIGHT CAME ON IN FLIGHT. WHEN GEAR WAS EXTENDED GREEN LIGHTS WENT OUT AND RED LIGHTS ILLUMINATED. WHEN GEAR LOCKED DOWN ALL RED LIGHTS WENT OUT AND GREEN LIGHTS ILLUMINATED. MAINTENANCE REPLAC ED LEFT MAIN GEAR DOWNLOCK MICROSWITCH. SYSTEM OPERATIONAL CHECK NORMAL DURING GEAR RETRACTION CHECK. AIRCRAFT RETURNE D TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996081500664 19960815 00664 EU 1996 8 15 WTAA960138 1 19960707 A 3260 1847F RADIUS ROD BAG JETSTM JETSTM3101 1500215 EU LT MLG INTERMITTENT A WTAA O OTHER N FALSE WARNING CL CLIMB 1 WP 17 103XV 747 FAT - LEFT MAIN GEAR INDICATES DOWN AND LOCKED WITH GEAR RETRACTED. INDICATION NORMAL AFTER GEAR WAS CYCLED. MAINTENAN CE REPLACED LEFT MAIN LANDING GEAR RADIUS ROD. SYSTEM OPERATIONAL CHECK NORMAL DURING GEAR RETRACTION CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996081500665 19960815 00665 EU 1996 8 15 WTAA960139 1 19960701 A 7931 APT79100080D OIL PRESS TRANS BAG JETSTM JETSTM3101 1500215 EU RT ENGINE CHAFED WIRE A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 17 401UE 729 LAX - RIGHT ENGINE OIL PRESSURE INDICATED 150 PSI, TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE FOUND CHAFING ON WIRE GOING TO OIL PRESSURE TRANSMITTER. RE-ROUTED AND INSULATED WIRE. SYSTEM OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SE RVICE. (M) 2 L 7 2 4T RT A21EU 1996081500666 19960815 00666 EU 1996 8 15 WTAA960140 1 19960701 A 2435 23079009 STARTER/GEN BAG JETSTM JETSTM3101 1500215 EU LT ENGINE FAILED A WTAA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION NR NOT REPORTED 1 WP 17 420UE 788 SEA - LEFT GENERATOR FAILED IN FLIGHT. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MX REPLACED LEFT STARTER GENERAT OR. OPERATIONAL CHECK NORMAL DURING GROUND RUN. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996081500667 19960815 00667 EU 1996 8 15 WTAA960141 1 19960712 A 5330 SKIN BAG JETSTM JETSTM3101 1500215 EU FUSELAGE BIRD STRIKE A WTAA K NONE C F.O.D. AP APPROACH 1 WP 17 103XV 747 FAT - CREW REPORTED, BIRD STRIKE ON LOWER FUSELAGE ON FINAL APPROACH. MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECTION. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996081500668 19960815 00668 SO 1996 8 15 WTAA960142 1 19960712 A 3230 1204370001 RELAY BOX EMB 120 EMB120RT SO LANDING GEAR FAILED A WTAA O OTHER J WARNING INDICATION AP APPROACH 1 WP 17 122AM 120013 SFO - LANDING GEAR WOULD NOT EXTEND WITH NORMAL EXTENSION. ABNORMAL GEAR EXTENSION PROCEDURES USED. AIRCRAFT FERRIED T O FAT. MAINTENANCE REMOVED AND REPLACED LANDING GEAR RELAY BOX. SYSTEM OPERATIONAL CHECK NORMAL DURING GEAR RETRACTION CHECK. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1996081500669 19960815 00669 SO 1996 8 15 WTAA960142B 1 19960714 A 3233 1959500003 RETRACTION JACK EMB 120 EMB120RT SO RT MLG OUT OF ADJUST A WTAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 17 284YV 120284 SFO - RIGHT MAIN LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. AIRCRAFT WAS FERRIED TO FAT. MAINTENANCE ADJUSTED RIGHT MAIN LANDING GEAR RETRACTION JACK AND UPLOCK PROXIMITY SENSOR. SYSTEM OPERATIONAL CHECK NORMAL DURING GEAR RETRACTION CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996081500670 19960815 00670 SO 1996 8 15 WTAA960143A 1 19960714 A 3260 922FS2A6NZ735A PROXIMITY SENSOR EMB 120 EMB120RT SO RT MLG OUT OF ADJUST A WTAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 17 284YV 120284 SFO - RIGHT MAIN LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. AIRCRAFT WAS FERRIED TO FAT. MAINTENANCE ADJUSTED RIGHT MAIN LANDING GEAR RETRACTION JACK AND UPLOCK PROXIMITY SENSOR. SYSTEM OPERATIONAL CHECK NORMAL DURING GEAR RETRACTION CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996081500671 19960815 00671 SO 1996 8 15 WTAA960144 1 19960713 A 3241 140043 TRANSDUCER EMB 120 EMB120RT SO LANDING GEAR DIRTY A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 WP 17 271YV 120271 FAT - BRAKE WARNING LIGHT ILLUMINATED DURING TAXI ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE UNABLE TO DUPLIC ATE DISCREPANCY. DEFERRED ANTI-SKID AS PRECAUTION. AIRCRAFT RELEASED FOR SERVICE. MX SUBSEQUENTLY CLEARED DEFERRAL BY INSPECTING AND CLEANING WHEEL SPEED TRANSDUCER CONNECTORS AND MECHANICAL ENGAGEMENTS. (M) 2 L 7 2 4T RT A31SO 1996081500672 19960815 00672 EU 1996 8 15 Y2PA96047 1 19960702 A 5270 SWITCH AMD FALC20 FALCOND 2720304 EU CABIN DOOR OUT OF ADJUST A Y2PA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 823AA 228 ELP - ABOUT 1 MINUTE AFTER TAKEOFF FROM ELP, THE CABIN DOOR WARNING LIGHT ILLUMINATED (FLICKERED ON AND OFF). AIRCRAFT RETURNED TO ELP AND MADE AN UNSCHEDULED LANDING. NO EMERGENCY PROCEDURES REQUIRED. FOUND AFT FUSELAGE COMPARTMENT DOOR CLOSED/LATCHED SWITCH OUT OF RIGG. ADJUSTED DOOR CLOSED/LATCHED SWITCH ON FUSELAGE AFT COMPARTMENT DOOR IAW FALCON MM 52-31-1. OPERATION OF DOOR WARNING SYSTEM ON GROUND CHECKS GOOD. (M) 2 L 7 2 4F A7EU 1996081500673 19960815 00673 WP 1996 8 15 Y2PA96048 1 19960809 A 3260 H146 DOOR SWITCH DOUG DC9 DC915F 3022037 WP RT MLG FAILED A Y2PA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 194US 47016 LRD - GEAR DOOR OPEN LIGHT REMAINING ON IN FLIGHT AFTER PERFORMING UPLATCH CHECK. REPLACED RIGHT MAIN GEAR DOOR SWITCH, AND ADJUSTED DOOR STOP BOLT ON GEAR DOOR IAW DC9 MM 32-70-0, 32-31-4. GEAR CYCLED AND CHECKED OK. (M) 2 L 7 2 4F A6WE 1996081500674 19960815 00674 NE 1996 8 15 Y2PA96049 2 19960813 A 7200 ENG AMD FALC20 FALCON 2720302 EU GE CF700 CF7002D2 30010 NE RIGHT FLAMED OUT A Y2PA A UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 GL 23 819AA 26 304207B YIP - THE RT ENG FLAMED OUT DURING PERFORMANCE OF A MAX ALT ACCELERATION TEST. TEST FLT TO PERFORM THIS CHK ON THE RT E NG WAS BEING DONE TO DETERMINE IF PREVIOUS FLAME OUT PROBLEM HAD BEEN RESOLVED, REF MRR Y2PA-96-008. NO EMERG PROCEDURE S REQUIRED. A/C RETURNED. REF ORIG MRR DATED 7-15-96 FOR PREVIOUS REWORK. STG 1/2 TURBINE AIR NOZZLE AND FAN NOZZLE W ERE REPLACED WITH UNITS OF LARGER AREA. ENG GROUND RUN INDICATED MAIN FUEL CNTRL TRIMMING PROPERLY, RESULTING IN REPLAC EMENT WITH .0 TSO MAIN FUEL PUMP AND MAIN FUEL CNTRL. ENG GRD RUN SUCCESSFUL AND RESULTING TEST FLT AS 35,000 FT TO PER FORM MAX ALT ACCELERATION TEST ALSO WAS SUCCESSFUL ON FALCON. NO PARTS DEFECT, ONLY RT COMB OF AREAS WERE NECESSARY. (M) 2 L 7 2 4F 4 F A7EU E7EA 1996081500675 19960815 00675 GL 1996 8 15 HEEA967630 2 19960808 A 7260 23007248 GEARSHAFT 23035178 BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL ACCESSORY DRV MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 6610L CAG95565 51423 CAE895559 UPON INSPECTION OF PART NOTED THE FOLLOWING: IMPROPERLY FINISHED MACHINING ON GEARSHAFT FWD ID FACE AS MARKED. REPLACED DISCREPANT PART. 1 G 7 1 3U 3 U H2SW E1GL 1996081500676 19960815 00676 GL 1996 8 15 HEEA967631 2 19960808 A 7260 6899402 PTO GEAR 6894171 BELL 206 206B3 1181506 SW ALLSN 250C 250C20B 03013 GL ACCESSORY DRV DEFECTIVE E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 2275Y CAG23022 3626 CAE821700F RECEIVING INSPECTION REVEALED COPPER COATING LIFTING ON P.T.O. GEAR FWD SIDE. REPLACED DISCREPANT PART. 1 G 7 1 3U 3 U H2SW E4CE 1996081500677 19960815 00677 EU 1996 8 15 HEEA967632 1 19960808 A 6310 4638202007 CLUTCH 4638001004 BOLKMS 105 BO105S 5626006 EU FREEWHEEL WORN EXCESS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB 2756 965 S737 INNER CAGE WORN BEYOND LIMITS. REPLACED WITH SERVICEABLE CLUTCH S/N 3617, T.T. 2513:45, T.S.I. 0:00. 1 G 7 2 3U H3EU 1996081500678 19960815 00678 EU 1996 8 15 HEEA967633 1 19960808 A 6210 355A11002011 BLADE SNIAS 350 AS350B2 8680813 EU M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 1788 2771 M/R BLADE IS CRACKED. (CRACK IS ABOUT 4 1/2" LONG. 1 G 7 1 3U H9EU 1996081500679 19960815 00679 SW 1996 8 15 HEEA967634 1 19960808 A 6710 204011121009A GRIP 204012101143 BELL 212 212 1181420 SW PITCH HORN DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1082G 6757 ABG7406 31109 THREADS ON PITCH HORN BORE ARE TO DAMAGED TO ACCEPT NEW THREAD INSERT. ALSO REPLACE BLADE BOLT BUSHING AND DRAG BRACES BUSHING AND INSTALL BUSHING IN PITCH HORN BORE. 1 G 7 1 4U H4SW 1996081500680 19960815 00680 1996 8 15 HEEA967635 4 19960808 A 3416 5035P2P42 ALTIMETER BOLKMS 105 BO105S 5626006 EU COCKPIT ENCODER ERROR E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 911PF 84 S718 ENCODER IS OFF 100 FEET AT 10,000 FEET AND ABOVE. 1 G 7 2 3U H3EU 1996081500681 19960815 00681 SW 1996 8 15 HEEA967636 1 19960808 A 7722 206375007103 INDICATOR BELL 206 206L4 1182110 SW COCKPIT TOT STUCK E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 62127 52023 TOT NEEDLE STUCK ON ZERO, WON'T INDICATE. 1 G 7 1 3U NC H2SW 1996081500682 19960815 00682 1996 8 15 HEEA967637 4 19960808 A 3457 0110005400 GPS 150 BOLKMS 105 BO105S 5626006 EU COCKPIT GPS DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 4294R S860 RIGHT HAND OF DISPLAY SCREEN DISPLAYS ILLEGAL CHARACTERS. 1 G 7 2 3U H3EU 1996081500683 19960815 00683 1996 8 15 HEEA967638 4 19960808 A 3457 0110005400 GPS 150 BELL 206 206L1 1182107 SW COCKPIT GPS MALFUNCTION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2246Q 45752 GPS "ENT" AND "DIRECT TO" BUTTONS UNREADABLE, ALSO NAV BUTTON LIGHT FLICKERS INTERMITTENTLY. 1 G 7 1 3U H2SW 1996081500684 19960815 00684 EU 1996 8 15 HEEA967639 1 19960808 A 6210 10515141 BLADE BOLKMS 105 BO105S 5626006 EU M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 724MB 7408 S756 M/R BLADE IS CRACKED. (NOSE AND NECK SHELL CRACKED AND SMALL AREAS OF SEPARATION ON THE LEADING EDGE STRIPS. 1 G 7 2 3U H3EU 1996081500685 19960815 00685 SW 1996 8 15 HEEA967640 1 19960808 A 6210 412015300109 BLADE BELL 412 412 1182202 SW M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 33008 6216 36004 BLADE IS CRACKED. (SPANWISE CRACK ON THE TRAILING EDGE STRIP CENTER AT STATION 242" APPROXIMATELY 1 1/4" IN LENGTH. SEN T TO COMPOSITE TECHNICS FOR INSPECTION AND REPAIR. 1 G 7 2 4U H4SW 1996081500686 19960815 00686 EU 1996 8 15 HEEA967641 1 19960808 A 6210 10515141 BLADE BOLKMS 105 BO105S 5626006 EU M/R SEPARATION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 54191 6235 S804 M/R BLADE SEPARATION ON THE LEADING EDGE ABRASION STRIPS BEYOND LIMITS. THE SEPARATION ARE ON THE INBOARD STRIP AND THE TWO CENTER STRIPS. 1 G 7 2 3U H3EU 1996081500687 19960815 00687 1996 8 15 HEEA967642 4 19960808 A 2370 9806019001 CVR BELL 412 412 1182202 SW COCKPIT WONT TEST E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 22347 2799 36005 CVR DOES NOT TEST. 1 G 7 2 4U H4SW 1996081500753 19960815 00753 NM 1996 8 15 CALA9601160 1 19960808 A 5713 STRINGER BOEING 727 727224 1384076 NM WS 656.50 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND NR 1 FUEL TANK STRINGER CRACKED ON HORIZONTAL FLANGE AT WS 656.50. THE CRACK WAS STOP DRILLED IAW SB 7 27-57A159. A REPAIR WAS FABRICATED AND INSTALLED IAW SB 727-57A159 AND EA 5762-01050, REV J. 2 L 7 3 4F A3WE 1996081500754 19960815 00754 NM 1996 8 15 CALA9601161 1 19960808 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM BS 1130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND FLOOR BEAM LOWER CHORD CORRODED AT STA 1130, RBL 1 TO RBL 40. A REPAIR WAS FABRICATED AND INSTALLED IA W SRM 51-40-04, FIGURE 1 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996081500755 19960815 00755 NM 1996 8 15 CALA9601162 1 19960805 A 5330 SKIN BOEING 727 727224 1384076 NM BS 1183 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND FUSELAGE SKIN CORRODED AROUND AFT LAV SERVICE PANEL AT STA 1183, STRINGER 20L TO 23L. THE CORRODED ARE A OF SKIN AND STRINGER WERE REMOVED, SKIN AND STRINGER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 12 AND SRM 53-10-3, FIGURE 1. 2 L 7 3 4F A3WE 1996081500756 19960815 00756 NM 1996 8 15 CALA9601163 1 19960806 A 5540 RUDDER BOEING 727 727224 1384076 NM VERT STAB CHAFED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND LOWER LEFT LEADING EDGE OF UPPER RUDDER CHAFED. THE ACCESS PANELS WERE REMOVED, THE AREA WAS CLEANED A ND THE FASTENERS WERE REMOVED IAW SRM 51-30-2. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-40-3, FIGURE 1. THE A CCESS PANELS WERE REINSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996081500757 19960815 00757 NM 1996 8 15 CALA9601164 1 19960805 A 5320 FITTING BOEING 727 727224 1384076 NM BS 1183 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND STRINGER 22L ATTACH FITTING CORRODED AT STA 1183. THE FITTING WAS REMOVED AND REPLACED IAW SRM 53-10-3 , 51-10-1, AND 51-30-2. 2 L 7 3 4F A3WE 1996081500758 19960815 00758 NM 1996 8 15 CALA9601165 1 19960805 A 5523 TAB BOEING 727 727224 1384076 NM LT ELEVATOR DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND LT ELEVATOR TAB DELAMINATED ALONG TRAILING EDGE. THE ELEVATOR TAB WAS REPAIRED IAW SRM 51-40-6 AND 51- 40-10. THE ELEVATOR TAB WAS REBALANCED IAW SRM 51-80-9. 2 L 7 3 4F A3WE 1996081500759 19960815 00759 NM 1996 8 15 CALA9601166 1 19960804 A 5414 SKIN BOEING 727 727224 1384076 NM NR 3 PYLON WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND NR 3 ENGINE PYLON TOP PORTION OF APRON INBOARD CENTER SECTION WORN THROUGH. THE WORN SKIN AND LONGERON WERE REMOVED. REPLACEMENT SKIN AND LONGERON WERE FABRICATED AND INSTALLED IAW SRM 54-30-2, FIGURE 1 AND 51-30-2. 2 L 7 3 4F A3WE 1996081500760 19960815 00760 NM 1996 8 15 9617686637 1 19960812 A 3610 Y-DUCT BOEING 747 747251B 1384892 NM NR 3 PYLON CRACKED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 637US 23548 DURING TAKEOFF, THE NR 3 FIRE WARNING LIGHT ILLUMINATED ACCOMPANIED BY HIGH NACELLE TEMPERATURE INDICATIONS. AIRCRAFT A BORTED TAKEOFF AND RETURNED TO GATE. FOUND CRACK IN Y-DUCT AT PYLON AREA. REPAIRED DUCT AND REPLACED HIGH STAGE VALVE AND CONTROLLER, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996081500761 19960815 00761 NM 1996 8 15 9617696718 1 19960813 A 3230 658051792 UPLOCK ACT BOEING 747 747251B 1384892 NM RT MLG FAILED A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 618US 14782 14782 21122 DURING APPROACH, THE RIGHT WING LANDING GEAR WOULD NOT EXTEND DURING LANDING GEAR EXTENSION. RECYCLED LANDING GEAR AND LANDING GEAR EXTENDED. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE RIGHT WING GEAR UPLOCK ACTUATOR, OPERATIONAL CHE CK GOOD. 2 L 7 4 4F A20WE 1996081500762 19960815 00762 WP 1996 8 15 9617709886 1 19960808 A 2613 OVERHEAT SENSOR DOUG DC9 DC951 3022051 WP TAIL COMPT MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 6001R 47783 UPON APPLYING TAKEOFF POWER, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. ACFT RETURNED TO THE GATE. AT GATE W ITH APU ON AND LEFT PACK ON LIGHT CAME ON AGAIN. LIGHT WENT OUT WHEN LEFT PACK WAS SECURED. REPLACED BOTH LEFT AND RIG HT TAIL COMPARTMENT OVERHEAT SENSORS. 2 L 7 2 4F A6WE 1996081500763 19960815 00763 NM 1996 8 15 9617716303 1 19960813 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 663US 23818 DURING LINE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE FROM ROWS 29 TO 31. REPAIRED BROKEN WIRE AND LIGHT ASSEMBLY, OPER ATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1996081500764 19960815 00764 WP 1996 8 15 9617429758 1 19960725 A 5320 SUPPORT DOUG DC9 DC941 302207N WP VENTRAL STAIRWAY CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 758NW 47286 DURING H-CHECK, FOUND A CRACK IN THE VENTRAL STAIRWAY PRESSURE DOME DOOR SUPPORT. REPAIRED SUPPORT (P/N 9915565-29) PER EA 97-110982. 2 L 7 2 4F A6WE 1996081500765 19960815 00765 WP 1996 8 15 9617439301 1 19960725 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 1174 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 301RC 48054 DURING H-CHECK, FOUND CORROSION ON THE GALLEY ATTACH FITTING SUPPORT FS 1174 AT LBL 56. REPAIRED SUPPORT (P/N 3952122-1 ) PER EA 93-105370. 2 L 7 2 4F A6WE 1996081500766 19960815 00766 WP 1996 8 15 9617449301 1 19960725 A 5320 FITTING DOUG DC9 DC982 3022082 WP BS 886 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 301RC 48054 DURING H-CHECK, FOUND A CRACK IN THE FLOOR BEAM SUPPORT FITTING AT FS 886, LBL 21. REPAIRED FITTING (P/N 3925817-1) PER EA 93-106194. 2 L 7 2 4F A6WE 1996081500767 19960815 00767 WP 1996 8 15 9617459856 1 19960726 A 5315 FLOOR BEAM DOUG DC9 DC951 3022051 WP BS 1136 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 765NC 47718 DURING H-CHECK, FOUND CORROSION ON THE FS 1136 FLOOR BEAM UPPER CHORD AT RBL 20. REPAIRED CHORD (P/N 9912243-55) PER EA 98-110969. 2 L 7 2 4F A6WE 1996081500768 19960815 00768 WP 1996 8 15 9617469856 1 19960726 A 5315 FLOOR BEAM DOUG DC9 DC951 3022051 WP BS 1078-1136 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 765NC 47718 DURING H-CHECK, FOUND CORROSION ON THE CENTER LINE FLOOR CAP BL 0 FROM FS 1078 TO 1136. REPAIRED CAP (P/N 5910760-11) P ER EA 98-110985. 2 L 7 2 4F A6WE 1996081500769 19960815 00769 WP 1996 8 15 9617479964 1 19960726 A 5312 BULKHEAD DOUBLER DOUG DC9 DC931 3022065 WP AFT PRESS BLKHD CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 912RW 47150 DURING M-CHECK, FOUND A 3 INCH CRACK IN THE AFT PRESSURE BULKHEAD UPPER CORNER DOUBLER AND WEB SKINS. REPAIRED SAME (P/ N 5910130-13, -111, -113) PER EA DC9 53-023. 2 L 7 2 4F A6WE 1996081500770 19960815 00770 WP 1996 8 15 9617489856 1 19960728 A 5320 CUSP DOUG DC9 DC951 3022051 WP BS 1151-1167 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 765NC 47718 DURING H-CHECK, FOUND CORROSION ON THE RIGHT CUSP T-ANGLE FS 1151 TO 1167 AT LONGERON 18R. REPAIRED CUSP (P/N 9910701-1 0) PER EA 98-110974. 2 L 7 2 4F A6WE 1996081500771 19960815 00771 NM 1996 8 15 9617496614 1 19960731 A 5313 LONGERON BOEING 747 747251B 1384892 NM BS 1300 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 614US 23059 DURING P-CHECK, FOUND CORROSION IN THE LEFT OVERWING LONGERON AT BS 1300. REPAIRED LONGERON (P/N 65B10097-11) PER EA 66 -101907. 2 L 7 4 4F A20WE 1996081500772 19960815 00772 NM 1996 8 15 9617506614 1 19960731 A 5330 SKIN BOEING 747 747251B 1384892 NM BS 1750 1791 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 614US 23059 DURING P-CHECK, FOUND CORROSION ON THE FUSELAGE SKIN AND INTERNAL DOUBLER/TRIPLER BS 1750 TO 1791, STR 42R TO 43R. REPA IRED SKIN (P/N 65B07002-1) PER EA 66-106554. 2 L 7 4 4F A20WE 1996081500773 19960815 00773 WP 1996 8 15 9617519154 1 19960731 A 5713 LONGERON DOUG DC9 DC914 3022034 WP WS 73 - 76 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8913E 45830 DURING H-CHECK, FOUND CORROSION ON THE LEFT WING STRINGER 14 BETWEEN XRS 73 TO 76. REPAIRED STRINGER (P/N 5911277-501) PER EA 91-110852. 2 L 7 2 4F A6WE 1996081500774 19960815 00774 WP 1996 8 15 9617529154 1 19960731 A 5713 LONGERON DOUG DC9 DC914 3022034 WP WS 79 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8913E 45830 DURING H-CHECK, FOUND CORROSION IN THE LEFT WING STRINGER 15 AT XRS 79. REPAIRED STRINGER (P/N 5911276-501) PER EA 91-1 10874. 2 L 7 2 4F A6WE 1996081500775 19960815 00775 WP 1996 8 15 9617539154 1 19960731 A 5713 LONGERON DOUG DC9 DC914 3022034 WP WS 69 - 91 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8913E 45830 DURING H-CHECK, FOUND CORROSION IN THE LEFT WING STRINGER 17 BETWEEN XRS 69 TO 91. REPAIRED STRINGER (P/N 5911278-1) PE R EA 91-110877. 2 L 7 2 4F A6WE 1996081500776 19960815 00776 WP 1996 8 15 9617549758 1 19960801 A 5320 PRESS WEB DOUG DC9 DC941 302207N WP BS 105 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 758NW 47286 DURING H-CHECK, FOUND CRACKS IN THE NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE WEB FS 105 AT BL 25 AND 37 LEFT AND RIGHT. REPAIRED WEB (P/N 9910073-313) PER EA 97-110964. 2 L 7 2 4F A6WE 1996081500777 19960815 00777 WP 1996 8 15 9617559909 1 19960802 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 580 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 959N 47255 DURING M-CHECK, FOUND A 10 INCH CRACK IN THE LONGERON 30 END FITTING AT FS 580. REPLACED FITTING PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996081500778 19960815 00778 WP 1996 8 15 9617569758 1 19960803 A 5315 FLOOR BEAM DOUG DC9 DC941 302207N WP BS 218 - 237 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 758NW 47286 DURING H-CHECK, FOUND CORROSION IN THE CENTER LINE FLOOR CAP BL 0 FROM FS 218 TO 237. REPAIRED CAP (P/N 5910137-9) PER EA 97-110704. 2 L 7 2 4F A6WE 1996081500779 19960815 00779 WP 1996 8 15 9617579909 1 19960804 A 5320 PRESS WEB DOUG DC9 DC931 3022065 WP BS 105 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 959N 47255 DURING M-CHECK, FOUND CRACKS IN THE NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE WEB FS 105 AT LBL 25 AND RBL 25. R EPAIRED WEB (P/N 9910073-313) PER EA 99-110706 AND -110719. 2 L 7 2 4F A6WE 1996081500780 19960815 00780 WP 1996 8 15 9617589996 1 19960804 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 889 BROKEN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8932E 47141 DURING M-CHECK, FOUND THE EAR BROKEN OFF OF THE FS 889 FRAME TO FLOOR BEAM ATTACH FITTING BENEATH THE LEFT CUSP WEB. RE PLACED FITTING (P/N 3919749-1) PER SRM 51-10-2. 2 L 7 2 4F A6WE 1996081500781 19960815 00781 WP 1996 8 15 9617599104 1 19960804 A 5312 BULKHEAD DOUBLER DOUG DC9 DC915 3022036 WP AFT PRESS BLKHD CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 94S 47204 DURING LINE CHECK, FOUND A .25 INCH CRACK IN THE AFT PRESSURE BULKHEAD UPPER CORNER DOUBLER AND WEB SKIN. REPAIRED SAME (P/N 5910130-13, -111, -113) PER EA DC9-53-024, SB53-166, AND DWG J060110. 2 L 7 2 4F A6WE 1996081500782 19960815 00782 WP 1996 8 15 9617609996 1 19960804 A 5315 FLOOR BEAM DOUG DC9 DC931 3022065 WP BS 237 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8932E 47141 DURING M-CHECK, FOUND A CRACK IN THE FS 237 FLOOR BEAM AT LBL 27. REPAIRED BEAM PER EA DC9-53-025. 2 L 7 2 4F A6WE 1996081500783 19960815 00783 NM 1996 8 15 9617616309 1 19960806 A 5744 FITTING BOEING 747 747451 1384940 NM NR 3 TE FLAP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 669US 24224 DURING P-CHECK, FOUND CORROSION IN THE NR 3 FLAP TRACK OUTBOARD SIDE FITTING AT WBL 353. REPLACED FITTING. 2 L 7 4 4F RT A20WE 1996081500784 19960815 00784 WP 1996 8 15 9617629984 1 19960806 A 5343 FITTING DOUG DC9 DC932 3022066 WP LT/RT MLG CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 984US 47383 DURING H-CHECK, FOUND CRACKS IN THE LEFT AND RIGHT MAIN LANDING GEAR WHEEL WELL BANANA FITTINGS AT THE BOTTOM OF THE CEN TER TANK. REPAIRED FITTINGS PER DACO SR5932450. 2 L 7 2 4F A6WE 1996081500785 19960815 00785 NM 1996 8 15 9617636309 1 19960806 A 5744 FITTING BOEING 747 747451 1384940 NM LT TE FORE FLAP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 669US 24224 DURING P-CHECK, FOUND CORROSION IN THE LEFT WING OUTBOARD FORE FLAP, INBOARD SEQUENCE CARRIAGE ATTACH FITTING LONG BORE. REPLACED FITTING. 2 L 7 4 4F RT A20WE 1996081500786 19960815 00786 WP 1996 8 15 9617649909 1 19960807 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 637- 667 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 959N 47255 DURING M-CHECK, FOUND CORROSION ON THE UNDERWING FUSELAGE SKIN FROM FS 637 TO 667, LONGERONS 27R TO 29R. REPAIRED SKIN (P/N 5911418-119) PER EA 99-110716. 2 L 7 2 4F A6WE 1996081500787 19960815 00787 WP 1996 8 15 9617659996 1 19960807 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 905 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8932E 47141 DURING M-CHECK, FOUND CORROSION ON LONGERON 19L AT FS 905. REPAIRED LONGERON PER EA DC9-53-028. 2 L 7 2 4F A6WE 1996081500788 19960815 00788 WP 1996 8 15 9617669912 1 19960810 A 5320 FITTING DOUG DC9 DC931 3022065 WP PAX DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 962N 47406 DURING M-CHECK, FOUND A CRACK IN THE AFT ENTRY DOOR STOP FITTING, LOWER RIGHT SIDE. REPLACED FITTING (P/N 3917624-517) PER SRM 51-30-2. 2 L 7 2 4F A6WE 1996081500789 19960815 00789 WP 1996 8 15 9617679138 1 19960810 A 5320 FITTING DOUG DC9 DC915 3022036 WP BS 468-475 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9348 45787 DURING H-CHECK, FOUND A 7 INCH CRACK IN THE LONGERON 30 END FITTING FROM FS 468 TO 475. REPLACED FITTING (P/N 5916064-1 N) PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996081500790 19960815 00790 EU 1996 8 15 QXEA9600284 1 19960813 A 7603 A75322401 CONTROL CABLE FOKKER F28 F28MK4000 4990810 EU QUADRANT NR2 ENG CORROSION A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 NR 2 ENGINE CONTROL CABLE QUADRANT AND SUPPORT BRACKET FOUND WITH NUMEROUS AREAS OF CORROSION IN THE AREA OF THE SUPPORT SHAFT BEARINGS, THE QUADRANT CABLE GROOVE AND CABLE END BALL SOCKET. ITEM FOUND DURING C-CHECK NR050-16, CORROSION REM OVED IAW EA 4-76-01. 2 L 7 2 4F RT A20EU 1996081500791 19960815 00791 EU 1996 8 15 QXEA9600285 1 19960813 A 2510 A75831001 PEDESTAL FOKKER F28 F28MK4000 4990810 EU COCKPIT CORROSION A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PEDESTAL MOUNTING POINTS HAVE CORROSION .030 TO .200 ON THE UPPER SIDE AT BOLT HEAD MATING SURFACES. CORROSION FOUND DU RING C-CHECK NR100-17,43,49, CORROSION REMOVED AND TREATED IAW EA 4-53-36. 2 L 7 2 4F RT A20EU 1996081500792 19960815 00792 EU 1996 8 15 QXEA9600286 1 19960813 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 STRINGER 1B IS CRACKED AT AFT RIVET FORWARD OF FORWARD PRESSURE BULKHEAD. CRACK NOTED DURING C-CHECK NR170-24, CRACK R EPAIRED IAW SRM 53-02-05. 2 L 7 2 4F RT A20EU 1996081500793 19960815 00793 EU 1996 8 15 QXEA9600287 1 19960813 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 STRINGER 74B IS CRACKED AT AFT RIVET AND CREASED 3 INCHES FORWARD OF CRACK, FORWARD OF FORWARD PRESSURE BULKHEAD. CRACK NOTED DURING C-CHECK NR170-25, CRACK AND CREASE REPAIRED IAW SRM 53-02-01 AND EA 4-53-43. 2 L 7 2 4F RT A20EU 1996081500794 19960815 00794 EU 1996 8 15 QXEA9600288 1 19960813 A 5230 A28410405 HINGE FOKKER F28 F28MK4000 4990810 EU FWD CARGO DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 FORWARD CARGO DOOR, DOOR MOUNTED HINGE HALF CRACKS NOTED ON AFT LUG AND 5TH LUG FROM FORWARD END. CRACKS NOTED DURING C -CHECK NR250-75, HINGE REPLACED IAW EO 4-52-05A. 2 L 7 2 4F RT A20EU 1996081500795 19960815 00795 EU 1996 8 15 QXEA9600289 1 19960813 A 5311 FRAME STRIP FOKKER F28 F28MK4000 4990810 EU BS 3820 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 AFT OF NOSE GEAR WHEEL BAY AT STA 3820 INNER FRAME STRIP CRACK TYPE 2 NOTED, INNER FRAME STRIP LT AND RT SIDE. CRACKS N OTED DURING C-CHECK NR230-85, CRACKS REPAIRED IAW EO 4-53-33, SB F28/53-123 INCORPORATED. 2 L 7 2 4F RT A20EU 1996081500796 19960815 00796 EU 1996 8 15 QXEA9600290 1 19960813 A 5320 COVER FOKKER F28 F28MK4000 4990810 EU BS 2550 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 NOSE GEAR BAY TOP COVER CRACK NOTED DURING HFEC, CRACK AT STATION 2550 APPROX 1.062 FROM RT EDGE OF BAY TOP COVER, CRACK LENGTH APPROX .687. CRACK IS PARALLEL TO DOF, CRACK NOTED DURING C-CHECK NR213-109,-270, CRACK REPAIRED IAW SRM 53-02- 18. 2 L 7 2 4F RT A20EU 1996081500797 19960815 00797 EU 1996 8 15 QXEA9600291 1 19960813 A 5320 COVER FOKKER F28 F28MK4000 4990810 EU BS 2623 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 NOSE GEAR BAY TOP COVER CRACK NOTED DURING HFEC. CRACK IS LOCATED AT STA 2623 APPROX 1.125 FROM RT EGE OF BAY TOP COVER , CRACK LENGTH APPROX .625, CRACK IS PARALLEL TO DOF. CRACK NOTED DURING C-CHECK NR213-110,-269, CRACK REPAIRED IAW SRM 53-02-18. 2 L 7 2 4F RT A20EU 1996081500798 19960815 00798 EU 1996 8 15 QXEA9600292 1 19960813 A 5312 BULKHEAD BEAM FOKKER F28 F28MK4000 4990810 EU REAR PRESS BLKHD CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 REAR PRESSURE BULKHEAD BELOW CABIN FLOOR IN AFT CARGO BAY HORIZONTAL BEAM II TOP RADIUS RT EDGE AT BL 1050R IS CRACKED A PPROX .500. CRACK NOTED DURING C-CHECK NR290-111, CRACK REPAIRED IAW EA 4-53-38. 2 L 7 2 4F RT A20EU 1996081500799 19960815 00799 EU 1996 8 15 QXEA9600293 1 19960813 A 5312 BULKHEAD BEAM FOKKER F28 F28MK4000 4990810 EU REAR PRESS BLKHD CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 REAR PRESSURE BULKHEAD BELOW FLOOR IN AFT CARGO BAY HORIZONTAL BEAM III TOP RADIUS RT EDGE OUTBOARD OF BL 1050R IS CRACK ED APPROX .375. CRACK NOTED DURING C-CHECK NR290-112, CRACK REPAIRED IAW EA 4-53-35. 2 L 7 2 4F RT A20EU 1996081500800 19960815 00800 EU 1996 8 15 QXEA9600294 1 19960813 A 5320 TIE STRAPS FOKKER F28 F28MK4000 4990810 EU CARGO COMPT CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 FORWARD CARGO BAY GILL LINER STRINGER TO FRAME TIE STRAPS 5 EACH, ARE ALL CRACKED AT FRAME 4900. CRACKS NOTED DURING C- CHECK NR200-234. REPLACED FRAME TIE STRAPS IAW SRM 51-31-05. 2 L 7 2 4F RT A20EU 1996081500801 19960815 00801 EU 1996 8 15 QXEA9600295 1 19960813 A 5330 STRINGER FOKKER F28 F28MK4000 4990810 EU CARGO COMPT CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 FORWARD CARGO BAY GILL LINER FLOOR SUPPORT STRINGER CRACKED ABOVE STRINGER NR 3 AT FRAME 8305. CRACK NOTED DURING C-CHE CK NR 200-257. STRINGER REPLACED IAW SRM 51-31-07. 2 L 7 2 4F RT A20EU 1996081500802 19960815 00802 EU 1996 8 15 QXEA9600296 1 19960813 A 5230 SKIN FOKKER A28400815 FOKKER F28 F28MK4000 4990810 EU CARGO DOOR TORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 CENTER CARGO DOOR INNER SKIN HAS A 2 INCH TEAR IN THE SKIN LOCATED 10 INCHES ABOVE LOWER SILL. TEAR NOTED DURING C-CHEC K NR250-277, TEAR REPAIRED IAW EA 4-52-15. 2 L 7 2 4F RT A20EU 1996081500803 19960815 00803 EU 1996 8 15 QXEA9600297 1 19960813 A 5230 SKIN FOKKER A28400813 FOKKER F28 F28MK4000 4990810 EU CARGO DOOR TORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 FORWARD CARGO DOOR INNER SKIN HAS A RIP AT THE LOWER EDGE 1 INCH LONG. RIP NOTED DURING C-CHECK NR250-278. RIP REPAIRE D IAW EA 4-52-14. 2 L 7 2 4F RT A20EU 1996081500804 19960815 00804 EU 1996 8 15 QXEA9600298 1 19960813 A 5311 RIB FOKKER F28 F28MK4000 4990810 EU NLG WW DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 8 BY 4 INCH DENT NOTED IN NOSE WHEEL BAY AND RIB 15, 40 AND 20 DAMAGED. DAMAGE NOTED DURING C-CHECK NR252-282, DAMAGE R EPAIRED IAW EA 4-53-54. 2 L 7 2 4F RT A20EU 1996081500805 19960815 00805 EU 1996 8 15 QXEA9600299 1 19960813 A 3350 23531 POWER SUPPLY FOKKER FOKKER F28 F28MK4000 4990810 EU CARGO BAY INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 487US 11238 AFT WING EVAC LIGHTS ARE INOP. POWER SUPPLY IN CARGO BAY REPLACED AND LIGHTS OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996081500806 19960815 00806 EU 1996 8 15 QXEA9600300 1 19960813 A 3350 23531 POWER SUPPLY FOKKER FOKKER F28 F28MK4000 4990810 EU CABIN LOW BATTERY A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 487US 26 11238 BOTH LEFT OVERWING EXIT LIGHTS ARE DIM. POWER SUPPLY AT SEAT 9A REPLACED AND LIGHTS OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996081500807 19960815 00807 NM 1996 8 15 QXEA9600301 1 19960813 A 3260 864202 SENSOR DHAV DHAV DHC8 DHC8102 2809003 NM NLG CRACKED A QXEA O OTHER N FALSE WARNING CL CLIMB 1 NM 09 813PH 32 ON CLIMBOUT THROUGH 12,000 FT, A THUMP WAS HEARD FOLLOWED BY NOSE GEAR INTRANSIT LIGHT. INTRANSIT LIGHT EXTINGUISHED ON ITS OWN AFTER AWHILE. AIRCRAFT LANDED IN PDX WITHOUT FURTHER PROBLEM. NLG DRAG STRUT PROXIMITY SENSOR FOUND CRACKED. SENSOR REPLACED AND ADJUSTED IAW MAINT MANUAL, NOSE GEAR INDICATION OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 1996081500808 19960815 00808 NM 1996 8 15 VNAA9608003 1 19960812 A 3243 S4340200001 BRAKE VLE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT MLG W/W DEFECTIVE A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 434JS 3051 SHORTLY AFTER T/O DURING CLIMB OUT, THE FLIGHT CREW WAS ALERTED BY AN EMERGENCY/PARK BRAKE CAS MESSAGE. CREW ELECTED TO RETURN TO THE FIELD AND AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. PIT MX REPLACED THE EMERGENCY/PARK BRAKE VALVE IAW M M 32-43-02, GROUND CHECKED GOOD. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996081500809 19960815 00809 NM 1996 8 15 96FDEA01354 1 19960813 A 5330 6518216 SKIN BOEING 727 7272D4 138407U NM BS 720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 288FE 21850 NR0236 AND 011, CORROSION (71C208-02) FWD CARGO BAY SKIN AT BS 720C PLUS 13 JUST I/B OF STR 28L. *S/D* REPAIRED CORRO SION DAMAGE IN FWD CARGO BAY SKIN AT BS 720C PLUS 3 IAW FEDEX SRM 53-30-3. 2 L 7 3 4F A3WE 1996081500810 19960815 00810 NM 1996 8 15 96FDEA01355 1 19960813 A 5320 65198622 NOSE CHORD BOEING 727 72722 1384002 NM BS 294-351 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 NR0610 AND 009, CORROSION (C53-111-01, -1) ON RT UPPER NOSE CHORD STA 312, 318, 330 RT WL 168 DOG HOUSE. *S/D* REMOVED AND REPLACED RT MID NOSE CHORD BS 294 TO 351 WL 169 RBL 15 AND REINSTALLED ALL ITEMS REMOVED FOR ACCESS. 2 L 7 3 4F A3WE 1996081500811 19960815 00811 NM 1996 8 15 96FDEA01356 1 19960813 A 5314 65184072 KEEL BEAM BOEING 727 72722 1384002 NM BS 1010 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 NR0647 AND 010, CORROSION (C53-100-3) BETWEEN SKIN AND KEEL BEAM BS 1062 STR 29R. *S/D* REMOVED AND REPLACED RT KEEL B EAM STR 29R FROM BS 960 TO BS 1090 PER SB 727-53-0179. 2 L 7 3 4F A3WE 1996081500812 19960815 00812 NM 1996 8 15 96FDEA01357 1 19960813 A 5320 65317731 CHORD BOEING 727 72722 1384002 NM BS 1176 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 NR0562 AND 011, CORROSION (C53-224-08) ON 1176.9 REINFORCEMENT CHORD AT LBL 63 WL 208.1 OUT OF LIMITS PER FEDEX SRM 53- 10-01. 2 L 7 3 4F A3WE 1996081500813 19960815 00813 NM 1996 8 15 96FDEA01358 1 19960813 A 5720 ARB0029509N CASTING DOUG MD11 MD11F 3023600 NM WS 562 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 608FE 48548 NR 5002, LT WING O/B FLAP I/B HINGE TENSION TIE SUPPORT STRAP CRACKED AT LOWER ATTACH BOLT HOLE AS SEEN FROM LWR EXTERNA L SURFACE STA XORS562, VERIFIED BY HFEC. 2 L 7 3 4F RT A22WE 1996081500814 19960815 00814 NM 1996 8 15 96FDEA1359 1 19960812 A 5320 DOUBLER BOEING 727 72722C 138400F NM BS 870 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 RT 870 INTERGRAL RIB FWD CRACKED FROM O/B HOLE TO EDGE. THE 2ND CRACK O/B OF O/B HOLE CRACKED FROM EDGE THROUGH RADIUS INTO AFT LWR HOLE OF O/B FLANGE. INSTALLED DOUBLER PER EZ 7-5310-28831. 2 L 7 3 4F A3WE 1996081500815 19960815 00815 NM 1996 8 15 96FDEA01360 1 19960813 A 5320 FLANGE BOEING 727 72722C 138400F NM BS 1148-1166 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 NR0176, MAIN CARGO HAS CORR ON STR 5L STA 1148 TO 1166. REMOVED CORR SRM 51-10-6 OUT OF LIMITS, CUT REPAIR PARTS FOR IN SIDE FLANGE REPAIR PER SRM 53-10-3. 2 L 7 3 4F A3WE 1996081500816 19960815 00816 NM 1996 8 15 96FDEA01361 1 19960813 A 5320 DOUBLER BOEING 727 72722C 138400F NM PAX DR CUTOUT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 FOUND CRACK AT FWD ENTRY DOOR CUT OUT FRAME UPPER HINGE AREA. INSTALLED DOUBLER AS PER SRM 53-10-4 FIG 2. 2 L 7 3 4F A3WE 1996081500817 19960815 00817 WP 1996 8 15 MWEA96404 1 19960809 A 3350 60030431 BALLAST DOUG DC9 DC914 3022034 WP CABIN FAILED A MWEA K NONE L NO TEST UK UNKNOWN 1 GL 31 400ME 45727 EMERGENCY LIGHTS WOULD NOT EXTINGUISH WITH ALL POWER OFF ON A/C. REPLACED LIGHT BALLAST, REPLACED LOANER UNIT 8/10/96. 2 L 7 2 4F A6WE 1996081500818 19960815 00818 WP 1996 8 15 MWEA96405 1 19960811 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 602ME 48133 FIRST SECTION OF CABIN OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERY IN NR 2 EMERGENCY BATTERY PACK POWER SUPPLY. 2 L 7 2 4F A6WE 1996081500819 19960815 00819 WP 1996 8 15 MWEA96406 1 19960811 A 2560 5917689103 COVER DOUG DC9 DC932 3022066 WP PAX DOOR SLIDE FELL OFF A MWEA K NONE O OTHER UK UNKNOWN 1 GL 31 207ME 47794 FWD ENTRY DOOR SLIDE COVER CAME OFF. REINSTALLED FWD ENTRY DOOR SLIDE AND COVER. 2 L 7 2 4F A6WE 1996081500820 19960815 00820 WP 1996 8 15 MWEA96407 1 19960811 A 3350 R2215 RELAY DOUG DC9 DC914 3022034 WP CABIN INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 400ME 45727 DURING OPS TEST OF EMERGENCY LIGHTS, FOUND FOUR FWD CABIN CEILING LIGHTS INOP AND LT NACELLE LIGHT INOP. REPLACED TWO B ATTERIES IN POWER SUPPLY AND R2-215 RELAY FOR LT EMERGENCY NACELLE FLOODLIGHT. 2 L 7 2 4F A6WE 1996081500821 19960815 00821 WP 1996 8 15 MWEA96408 1 19960812 A 3350 6003043 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 501ME 48132 AFT F/A STATION OVERHEAD CEILING EMERGENCY LIGHT STAYS ON CONSTANTLY AFTER EXTERNAL POWER AND GROUND SERVICE BUS IS OFF. REPLACED BATTERY PACK. 2 L 7 2 4F A6WE 1996081500822 19960815 00822 WP 1996 8 15 MWEA96409 1 19960813 A 3350 6011775 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 501ME 48132 BOTH AFT NACELLE EMERGENCY LIGHTS STAY ON WHEN SWITCH IS SELECTED OFF. REPLACED BOTH AFT NACELLE EMERGENCY LIGHT BATTER Y PACKS. 2 L 7 2 4F A6WE 1996081500823 19960815 00823 WP 1996 8 15 MWEA96410 1 19960814 A 5210 2712074 SEAL DOUG DC9 DC932 3022066 WP CABIN DOOR UNSECURED A MWEA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 31 301ME 47190 DURING CLIMBOUT, CREW HEARD LOUD NOISE COMING FROM PAX ENTRANCE, RETURNED TO MKE. FOUND SECONDARY SEAL HANGING OUTSIDE OF PAX DOOR. RESECURED SEAL, NO OTHER DEFECTS NOTED. 2 L 7 2 4F A6WE 1996081500824 19960815 00824 WP 1996 8 15 MWEA96411 1 19960814 A 2560 5917689103 COVER DOUG DC9 DC932 3022066 WP CABIN DOOR LOOSE A MWEA K NONE O OTHER UK UNKNOWN 1 GL 31 207ME 47794 MAIN CABIN DOOR SLIDE FELL OFF. REINSTALLED LATCH ASSY ON SLIDE COVER. 2 L 7 2 4F A6WE 1996081500825 19960815 00825 NM 1996 8 15 P5CA9600484 1 19960715 A 5320 ANGLE BOEING 747 747132 1384882 NM BS 1340 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 DIAGONAL SUPPORT CRACKED AT L3 DOOR AFT CUTOUT BS 1340 APPROX S21L. REPLACED SUPPORT ANGLE PER BAC SRM 51-10-01 PG 18. 2 L 7 4 4F A20WE 1996081500826 19960815 00826 NM 1996 8 15 P5CA9600485 1 19960715 A 5210 SKIN BOEING 747 747132 1384882 NM R1 DOOR DETACHED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 EXTERIOR SKIN DETACHED ON R1 DOOR AT LOWER HINGE AREA. REFORMED SKIN PER BAC SRM 51-40-1. 2 L 7 4 4F A20WE 1996081500827 19960815 00827 NM 1996 8 15 P5CA9600486 1 19960715 A 5320 65B1135218 THRESHOLD BOEING 747 747132 1384882 NM R5 DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACK IN THRESHOLD R5 DOOR FORWARD LOWER CORNER. REPAIRED PER BOEING SRM 51-30-02. 2 L 7 4 4F A20WE 1996081500828 19960815 00828 NM 1996 8 15 P5CA9600487 1 19960715 A 5314 KEEL BEAM BOEING 747 747132 1384882 NM BS 1220 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION KEEL BEAM BOX LOWER EXTERIOR SURFACE BS 1220 TO 1230. CORROSION REMOVED AND REPROTECTED AS PER BOEING SRM 51-10-01 AND 02. 2 L 7 4 4F A20WE 1996081500829 19960815 00829 NM 1996 8 15 P5CA9600488 1 19960715 A 5210 BACB107I01 BEARING BOEING 747 747132 1384882 NM R1 DOOR DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 DAMAGED LOWER BEARING AT UPPER HINGE ON R1 DOOR TORQUE TUBE. UPPER HINGE BEARING REPLACED AND DOOR RIG CK'D PER BAC MM 52-11-01. 2 L 7 4 4F A20WE 1996081500830 19960815 00830 NM 1996 8 15 P5CA9600489 1 19960715 A 5330 SKIN BOEING 747 747132 1384882 NM BS 1480 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION FUSELAGE SKIN BS 1480 AT STRINGER S46L AND S47L. REMOVED AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1996081500831 19960815 00831 NM 1996 8 15 P5CA9600490 1 19960715 A 5313 LONGERON BOEING 747 747132 1384882 NM BS 980-990 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION LONGERON OUTBOARD SURFACE AT BS 980 TO 990 S50R TO S51R. REMOVED CORROSION PER BOEING SRM 51-10-01 AN D 51-10-02. 2 L 7 4 4F A20WE 1996081500832 19960815 00832 NM 1996 8 15 P5CA9600491 1 19960715 A 5210 BACB10A7DDH BEARING BOEING 747 747132 1384882 NM R1 DOOR DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 BEARING PROTRUDING AT R1 DOOR TORQUE TUBE LWR GUIDE ARM. LWR GUIDE ARM BEARING REPLACED AND DOOR RIG CK'D PER BAC MM 52 -11-01. 2 L 7 4 4F A20WE 1996081500833 19960815 00833 NM 1996 8 15 P5CA9600492 1 19960715 A 5320 65B10098148 SUPPORT BOEING 747 747132 1384882 NM BS 987 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 2 CORROSION/CRACK ON BODY FAIRING SUPPORT BS 987 LBL 10 TO RBL 60. REPLACED SUPPORT PER BOEING SRM 51-10-01. 2 L 7 4 4F A20WE 1996081500834 19960815 00834 NM 1996 8 15 P5CA9600493 1 19960715 A 5210 BACB10FU01 BEARING BOEING 747 747132 1384882 NM L2 DOOR DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 DAMAGED UPPER BEARING AT L2 DOOR TORQUE TUBE LWR HINGE. BEARING REPLACED AND DOOR RIG CK'D PER BAC MM 52-11-01. 2 L 7 4 4F A20WE 1996081500835 19960815 00835 NM 1996 8 15 P5CA9600494 1 19960715 A 5330 SKIN BOEING 747 747132 1384882 NM BS 840-850 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION ON BELLY SKIN AND BODY FAIRING SUPPORT STRUCTURE BS 840 AND 850. REMOVED CORROSION AND REPROTECTED PE R BOEING SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1996081500836 19960815 00836 NM 1996 8 15 P5CA9600495 1 19960715 A 5320 SUPPORT BOEING 747 747132 1384882 NM BS 1280 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION KEEL BEAM PANEL SUPPORT AT BS 1280 LBL 10 TO RBL 10. REMOVED CORROSION AND TREATED PER BOEING SRM 51- 10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1996081500837 19960815 00837 NM 1996 8 15 P5CA9600496 1 19960715 A 5210 BACB10FU01 BEARING BOEING 747 747132 1384882 NM R2 DOOR DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 DAMAGED UPPER BEARING AT R2 DOOR TORQUE TUBE LWR HINGE. BEARING REPLACED AND DOOR RIG CK'D PER BAC MM 52-11-01. 2 L 7 4 4F A20WE 1996081500838 19960815 00838 NM 1996 8 15 P5CA9600497 1 19960715 A 5314 KEEL BEAM BOEING 747 747132 1384882 NM BS 1350 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION KEEL BEAM BOX EXTERIOR LOWER SURFACE AT BS 1350 LBL 10 TO RBL 10. REMOVED CORROSION AND REPROTECTED PER BOEING SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1996081500839 19960815 00839 NM 1996 8 15 P5CA9600498 1 19960715 A 5320 SCUFF PLATE BOEING 747 747132 1384882 NM CARGO DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 DAMAGED AFT SCUFF PLATE AT BULK CARGO DOOR. WELD REPAIR MADE PER BAC SRM 51-30-02. 2 L 7 4 4F A20WE 1996081500840 19960815 00840 NM 1996 8 15 P5CA9600499 1 19960715 A 5311 FRAME BOEING 747 747132 1384882 NM BS 2368 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION FRAME 2638 AT WL 219 LBL 12 TO RBL 12. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53 -10-02, TREATED PER 51-10-02. 2 L 7 4 4F A20WE 1996081500841 19960815 00841 NM 1996 8 15 P5CA9600500 1 19960715 A 5244 DOOR BOEING 747 747132 1384882 NM EMPENANGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION APU BATTERY COMPARTMENT DOOR INNER SURFACE. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS P ER 52-00-02, TREATED PER 51-10-02. 2 L 7 4 4F A20WE 1996081500842 19960815 00842 NM 1996 8 15 P5CA9600501 1 19960715 A 5320 FLOOR SUPPORT BOEING 747 747132 1384882 NM BS 782 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACK AT SCREW HOLE BS 782 MOST OUTBOARD FLOOR SUPPORT. REPAIRED PER BOEING SRM 51-40-04. 2 L 7 4 4F A20WE 1996081500843 19960815 00843 NM 1996 8 15 P5CA9600502 1 19960715 A 5320 SUPPORT BOEING 747 747132 1384882 NM BS 1440 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CORROSION MAIN DECK BS 1440 LATERAL FLOOR SUPPORT AT LBL 75 TO 97. CORROSION REMOVED AND REPROTECTED PER BOEING SRM 51- 10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1996081500844 19960815 00844 NM 1996 8 15 P5CA9600503 1 19960715 A 5320 65B0500065 FRAME BOEING 747 747132 1384882 NM L5 DOOR CUTOUT CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACK AT MID REVEAL AREA OF L5 DOOR CUTOUT AT APPROX S19 TO 20L. CUTOUT REVEAL REPAIRED PER BAC SRM 51-10-01 AND DOOR R IG CK'D PER BAC MM 52-11-01. 2 L 7 4 4F A20WE 1996081500845 19960815 00845 NM 1996 8 15 P5CA9600504 1 19960715 A 5313 STRINGER BOEING 747 747132 1384882 NM BS 1000-1020 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACK STRINGER 1R BETWEEN BS 1000 AND 1020. REPAIRED STRINGER AS PER HAECO REPAIR SCHEME 53-00-32968 REFERENCE BOEING F AX PAO-HKG-96-0001TE, 0003RE, 0006RE. 2 L 7 4 4F A20WE 1996081500846 19960815 00846 NM 1996 8 15 P5CA9600505 1 19960715 A 5220 FRAME BOEING 747 747132 1384882 NM L5 DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACK AT AFT LWR CORNER AREA LWR AFT LATCH ROLLER OF L5 DOOR INTERIOR FACE. CRACK REPAIRED PER BAC SRM 51-40-02 FIG 1. 2 L 7 4 4F A20WE 1996081500847 19960815 00847 NM 1996 8 15 P5CA9600506 1 19960715 A 5313 STRINGER BOEING 747 747132 1384882 NM BS 1000-1020 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACKED STRINGER S6R BETWEEN BS 1000 AND 1020. REPAIRED PER HAECO REPAIR SCHEME 53-00-32968 REFERENCE BOEING FAX PAO-HK G-96-0001TE, 0003RE,0006RE. 2 L 7 4 4F A20WE 1996081500848 19960815 00848 NM 1996 8 15 P5CA9600507 1 19960715 A 5320 FRAME BOEING 747 747132 1384882 NM L5 DOOR CUTOUT CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACK AT FRAME ATTACH SHEAR TIE OF L5 DOOR CUTOUT AT BS 2300 A18-19L. SHEAR TIE REPAIRED PER BAC SRM 53-10-04 FIG 3. 2 L 7 4 4F A20WE 1996081500849 19960815 00849 NM 1996 8 15 P5CA9600508 1 19960715 A 5320 SHEAR TIE BOEING 747 747132 1384882 NM BS 2300 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACK AT FRAME ATTACH SHEAR TIE AT R5 DOOR CUTOUT BS 2300, BETWEEN S18 TO 9R. SHEAR TIE REPAIRED PER BAC SRM 53-10-04 F IG 3. 2 L 7 4 4F A20WE 1996081500850 19960815 00850 NM 1996 8 15 P5CA9600509 1 19960715 A 5320 65B050498 THRESHOLD BOEING 747 747132 1384882 NM R5 DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACK AT AFT LWR CORNER THRESHOLD OF R5 DOOR. REPLACED CORNER THRESHOLD PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1996081500851 19960815 00851 NM 1996 8 15 P5CA9600510 1 19960715 A 5330 SKIN BOEING 747 747132 1384882 NM BS 1240-1260 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION ON FUSELAGE SKIN BETWEEN S8R AND S9R BS 1240 TO 1260. REMOVED CORROSION AND TREATED PER BOEING SRM 51 -10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1996081500852 19960815 00852 NM 1996 8 15 P5CA9600511 1 19960715 A 5320 FLOOR SUPPORT BOEING 747 747132 1384882 NM BS 863 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION MAIN DECK BS 863 RIGHT OUTBOARD LONGITUDINAL FLOOR SUPPORT UPPER SURFACE. REMOVED CORROSION AND TREAT ED PER BOEING SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1996081500853 19960815 00853 NM 1996 8 15 P5CA9600512 1 19960715 A 5320 65B0969919 FITTING BOEING 747 747132 1384882 NM BS 1720 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACK AT S19R END FITTING, BS 1720. REPLACED END FITTING PER BAC SRM 51-10-01 PG 18. 2 L 7 4 4F A20WE 1996081500854 19960815 00854 NM 1996 8 15 P5CA9600513 1 19960715 A 5313 STRINGER BOEING 747 747132 1384882 NM BS 1460-1480 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACKED STRINGER S2R BETWEEN BS 1480 AND 1460. REPAIRED PER HAECO REPAIR SCHEME 53-00-32968 REFERENCE BOEING FAX PAO-HK G-0001TE, 003RE, 0006RE. 2 L 7 4 4F A20WE 1996081500855 19960815 00855 NM 1996 8 15 P5CA9600514 1 19960715 A 5315 FLOOR BEAM BOEING 747 747132 1384882 NM BS 980 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION MAIN DECK FLOOR BEAM UPPER CHORD LOWER SURFACE BS 980 RBL 110. REMOVED CORROSION AND TREATED PER BOEI NG SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1996081500856 19960815 00856 NM 1996 8 15 P5CA9600515 1 19960715 A 5210 FRAME BOEING 747 747132 1384882 NM R4 DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACK AT R4 DOOR FWD FRAME UPPER CORNER. TRIMMED FRAME TO REMOVE CRACK PER BAC SRM 52-00-01 FIG 1. 2 L 7 4 4F A20WE 1996081500857 19960815 00857 NM 1996 8 15 P5CA9600516 1 19960715 A 5320 DOUBLER BOEING 747 747132 1384882 NM R4 DOOR CUTOUT CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACK AT INTERIOR DOUBLER IN LWR LATCH FITTING AREA OF FWD LWR R4 DOOR CUTOUT. REPAIRED DOUBLER PER BAC SRM 53-10-04 FI G 84. 2 L 7 4 4F A20WE 1996081500858 19960815 00858 NM 1996 8 15 P5CA9600517 1 19960715 A 7110 NOSE COWL BOEING 747 747132 1384882 NM NR 1 ENGINE DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 DENT IN NR 1 ENGINE NOSE COWL 7 O'CLOCK POSITION. METAL FILLER REPAIRED AS PER BOEING SRM 51-40-06 PARA 2L. 2 L 7 4 4F A20WE 1996081500859 19960815 00859 NM 1996 8 15 P5CA9600518 1 19960715 A 5315 FLOOR BEAM BOEING 747 747132 1384882 NM BS 860 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 2 CORROSION BS 860 FLOOR BEAM RIGHT END REFORCING FLOOR SUPPORT AT SCREW HOLES. FABRICATED AND REPLACED FLOOR SUP PORT PER BOEING SRM 51-10-01 PAGE 18. 2 L 7 4 4F A20WE 1996081500860 19960815 00860 NM 1996 8 15 P5CA9600519 1 19960715 A 5347 TIE DOWN TRACK BOEING 747 747132 1384882 NM BS 862 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 COROSION BS 862, RBL 98 TIE DOWN TRACK OUTBOARD. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01 AND 51-1 0-02. 2 L 7 4 4F A20WE 1996081500861 19960815 00861 NM 1996 8 15 P5CA9600520 1 19960715 A 5320 REVEAL BOEING 747 747132 1384882 NM R4 DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACK AT FWD REVEAL UPPER HINGE AREA OF R4 DOOR CUTOUT. CUTOUT REVEAL REPAIRED PER BAC SRM 51-40-03. 2 L 7 4 4F A20WE 1996081500862 19960815 00862 NM 1996 8 15 P5CA9600521 1 19960715 A 7110 NOSE COWL BOEING 747 747132 1384882 NM NR 1 ENGINE DEBONDED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 DEBONDED PANEL NR 1 ENGINE NOSE COWL TOP PANEL 12 O'CLOCK POSITION. REPAIRED PANEL PER BOEING SRM 54-30-03. 2 L 7 4 4F A20WE 1996081500863 19960815 00863 NM 1996 8 15 P5CA9600522 1 19960715 A 5320 SUPPORT BOEING 747 747132 1384882 NM BS 770-800 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION RIGHT MOST OUTBOARD LONGITUDINAL FLOOR SUPPORT UPPER SURFACE BETWEEN BS 770 AND BS 800. REPLACED FLOO R SUPPORT PER BOEING SRM 51-10-01 PG 18. 2 L 7 4 4F A20WE 1996081500864 19960815 00864 NM 1996 8 15 P5CA9600523 1 19960715 A 7110 PANEL BOEING 747 747132 1384882 NM NR 4 ENGINE DEBONDED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 DEBONDED PANEL NR 4 ENGINE NOSE COWL 6 O'CLOCK POSITION. REPAIRED PER BOEING SRM 54-30-03 FIG 28. 2 L 7 4 4F A20WE 1996081500865 19960815 00865 NM 1996 8 15 P5CA9600524 1 19960715 A 5320 FRAME BOEING 747 747132 1384882 NM R4 DOOR CUTOUT CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACK AT FWD FRAME UPPER CORNER OF R4 DOOR CUTOUT. TRIMMED FRAME TO REMOVE CRACK PER BAC SRM 53-10-01. 2 L 7 4 4F A20WE 1996081500866 19960815 00866 NM 1996 8 15 P5CA9600525 1 19960715 A 5320 REVEAL BOEING 747 747132 1384882 NM L4 DOOR CUTOUT CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACK AT BS 1670 BETWEEN S17 TO 18L, L4 DOOR CUTOUT FWD UPPER CORNER REVEAL. TRIMMED REVEAL TO REMOVE CRACK PER BAC SRM 53-10-01 FIG 1. 2 L 7 4 4F A20WE 1996081500867 19960815 00867 NM 1996 8 15 P5CA9600526 1 19960715 A 5210 BACB10FU01 BEARING BOEING 747 747132 1384882 NM R4 DOOR DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 DAMAGED LWR BEARING AT R4 DOOR TORQUE TUBE UPPER HINGE. REPLACED BEARING AND CK'D DOOR RIG PER BAC MM 52-11-01. 2 L 7 4 4F A20WE 1996081500868 19960815 00868 NM 1996 8 15 P5CA9600527 1 19960715 A 5210 BACB10FU33 BEARING BOEING 747 747132 1384882 NM L4 DOOR DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 DAMAGED BEARING AT L4 DOOR TORQUE TUBE MID SUPPORT. BEARING REPLACED AND DOOR RIG CK'D PER BAC MM 52-11-01. 2 L 7 4 4F A20WE 1996081500869 19960815 00869 NM 1996 8 15 P5CA9600528 1 19960715 A 5512 SKIN BOEING 747 747132 1384882 NM HORIZ STAB LE CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 MINOR SURFACE CORROSION ON LEFT HORIZ STAB LEADING EDGE STA 200. SURFACE CORROSION REMOVED AND AREA REPROTECTED PER BAC MM 51-21-03 AND BAC SRM 51-10-02. 2 L 7 4 4F A20WE 1996081500870 19960815 00870 NM 1996 8 15 P5CA9600529 1 19960715 A 5210 BACB10FU21 BEARING BOEING 747 747132 1384882 NM L4 DOOR DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 DAMAGED LWR BEARING AT L4 TORQUE TUBE UPPER HINGE. REPLACED UPPER HINGE BEARING AND CK'D RIG OF DOOR PER BAC MM 52-11-0 1. 2 L 7 4 4F A20WE 1996081500871 19960815 00871 NM 1996 8 15 P5CA9600530 1 19960715 A 5315 FLOOR BEAM BOEING 747 747132 1384882 NM BS 800 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION MAIN DECK BS 800 FLOOR BEAM RIGHT END REINFORCING PLATE IN BOTH UPPER AND LOWER SURFACE. REMOVED CORR OSION AND REPROTECTED AREA PER BOEING 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1996081500872 19960815 00872 NM 1996 8 15 P5CA9600531 1 19960715 A 7110 NOSE COWL BOEING 747 747132 1384882 NM NR 4 ENGINE DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 DENT IN NR 4 ENGINE NOSE COWL 9 O'CLOCK POSITION. REPAIRED PER BOEING SRM 51-40-06 PARA 2L. 2 L 7 4 4F A20WE 1996081500873 19960815 00873 NM 1996 8 15 P5CA9600532 1 19960715 A 5320 SUPPORT BOEING 747 747132 1384882 NM BS 520-560 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION RIGHT MOST OUTBOARD LONGITUDINAL FLOOR SUPPORT LOWER SURFACE BS 520 TO BS 560. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1996081500874 19960815 00874 NM 1996 8 15 P5CA9600533 1 19960715 A 5210 BACB10CF10PP BEARING BOEING 747 747132 1384882 NM L4 DOOR DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 DAMAGED BEARINGS AT L4 TORQUE TUBE GUIDE ARM. REPLACED BEARINGS AND CK'D RIG OF DOOR PER BAC MM 52-11-01. 2 L 7 4 4F A20WE 1996081500875 19960815 00875 NM 1996 8 15 P5CA9600534 1 19960715 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 640-645 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION MAIN DECK RBL 98 SEAT TRACK OUTBOARD FLANGE BETWEEN BS 640 AND 645. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1996081500876 19960815 00876 NM 1996 8 15 P5CA9600535 1 19960715 A 5320 SUPPORT BOEING 747 747132 1384882 NM BS 827 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 2 CORROSION BS 827 LEFT MOST OUTBOARD LONGITUDINAL FLOOR SUPPORT. REPLACED FLOOR SUPPORT PER BOEING SRM 51-10-01 PAGE 18. 2 L 7 4 4F A20WE 1996081500877 19960815 00877 NM 1996 8 15 P5CA9600536 1 19960715 A 5320 SCUFF PLATE BOEING 747 747132 1384882 NM L3 DOOR CUTOUT CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION ON EXTERNAL SKIN AT L3 DOOR SCUFF PLATE. CORROSION REMOVED AND AREA RETREATED PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1996081500878 19960815 00878 NM 1996 8 15 P5CA9600537 1 19960715 A 5753 FAIRING BOEING 747 747132 1384882 NM NR 4 FLAP TRACK DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 DAMAGE AT NR 4 FLAP TRACK FORWARD FIXED FAIRING EXTERNAL SURFACE. REPAIRED PER BOEING SRM 51-40-15. 2 L 7 4 4F A20WE 1996081500879 19960815 00879 NM 1996 8 15 P5CA9600538 1 19960715 A 5753 FAIRING BOEING 747 747132 1384882 NM NR 5 FLAP TRACK DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 DAMAGE AT NR 5 FLAP TRACK FORWARD FIXED FAIRING AT EXTERNAL SURFACE. REPAIRED PER BOEING SRM 51-40-15. 2 L 7 4 4F A20WE 1996081500880 19960815 00880 NM 1996 8 15 P5CA9600539 1 19960715 A 5753 FAIRING BOEING 747 747132 1384882 NM NR 6 FLAP TRACK DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 DAMAGE AT NR 6 FLAP TRACK FORWARD FIXED FAIRING EXTERNAL SURFACE. REPAIRED PER BOEING SRM 51-40-15. 2 L 7 4 4F A20WE 1996081500881 19960815 00881 NM 1996 8 15 P5CA9600540 1 19960715 A 5210 BACB10AB6M BEARING BOEING 747 747132 1384882 NM R1 DOOR DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 DAMAGED LWR BEARING AT R1 DOOR BODY TORQUE TUBE. REPLACED BEARING AND CK'D DOOR RIG PER BAC MM 52-10-01. 2 L 7 4 4F A20WE 1996081500882 19960815 00882 NM 1996 8 15 P5CA9600541 1 19960715 A 5753 FAIRING BOEING 747 747132 1384882 NM NE 3 FLAP TRACK DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 DAMAGE NR 3 FLAP TRACK FORWARD FIXED FAIRING EXTERNAL SURFACE. REPAIRED PER BOEING SRM 51-40-15. 2 L 7 4 4F A20WE 1996081500883 19960815 00883 NM 1996 8 15 P5CA9600542 1 19960715 A 5320 SUPPORT BOEING 747 747132 1384882 NM BS 880 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 2 CORROSION BODY FAIRING SUPPORT SURFACE BS 880 LBL 25 TO RBL 25. REPAIRED PER BOEING SRM 53-50-04. 2 L 7 4 4F A20WE 1996081500884 19960815 00884 NM 1996 8 15 P5CA9600543 1 19960715 A 5320 BRACKET BOEING 747 747132 1384882 NM BS 2020 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACKED BULK CARGO FLOOR PANEL SUPPORT ATTACH BRACKET AT BS 2020 RBL 55. REPAIRED PER BOEING SRM 51-40-05. 2 L 7 4 4F A20WE 1996081500885 19960815 00885 NM 1996 8 15 P5CA9600544 1 19960715 A 5320 THRESHOLD BOEING 747 747132 1384882 NM L5 DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACK AT FWD LWR CORNER THRESHOLD ON L5 DOOR. WELD REPAIR MADE TO THRESHOLD PER BAC5975 HAECO TECHNICAL ASSISTANCE REQ UISITION 059055 AND INSTALLED PER BAC SRM 51-30-02. 2 L 7 4 4F A20WE 1996081500886 19960815 00886 NM 1996 8 15 P5CA9600545 1 19960715 A 5330 PANEL BOEING 747 747132 1384882 NM FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION KEEL BEAM ACCESS PANEL 193P INNER SURFACE SEVERAL PLACES. REMOVED CORROSION AND TREATED PER BOEING SR M 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1996081500887 19960815 00887 NM 1996 8 15 P5CA9600546 1 19960715 A 5320 SUPPORT BOEING 747 747132 1384882 NM BS 1500-1520 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION MAIN DECK LEFT MOST OUTBOARD LONGITUDIINAL FLOOR SUPPORT UPPER AND LOWER SURFACE BS 1500 TO 1520. REM OVED CORROSION AND TREATED PER BOEING SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1996081500888 19960815 00888 NM 1996 8 15 P5CA9600547 1 19960715 A 5315 FLOOR BEAM BOEING 747 747132 1384882 NM BS 1660 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION MAIN DECK BS 1660 FLOOR BEAM LEFT END REINFORCING PLATE AT SCREW HOLE AREA. REMOVED CORROSION PER BOE ING SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1996081500889 19960815 00889 NM 1996 8 15 P5CA9600548 1 19960715 A 5753 FAIRING BOEING 747 747132 1384882 NM NR 6 TE FLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 DELAMINATION, EROSION AND PAINT CHIPPING NR 6 FLAP TRACK MOVABLE FAIRING. REPAIRED PER BOEING SRM 51-40-15. 2 L 7 4 4F A20WE 1996081500890 19960815 00890 NM 1996 8 15 P5CA9600549 1 19960715 A 5320 BRACKET BOEING 747 747132 1384882 NM BS 1773 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACKED AFT CARGO TIE DOWN TRACK ATTACH BRACKET AT BS 1773 RBL 30. REPAIRED PER BOEING SRM 51-10-01. 2 L 7 4 4F A20WE 1996081500891 19960815 00891 NM 1996 8 15 P5CA9600550 1 19960715 A 5321 FLOOR PLATE BOEING 747 747132 1384882 NM BS 1850 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION AFT CARGO FLOOR PLATE UPPER SURFACE BS 1850 RBL 7 TO RBL 14. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1996081500892 19960815 00892 NM 1996 8 15 P5CA9600551 1 19960715 A 5321 FLOOR PLATE BOEING 747 747132 1384882 NM BS 1980-2040 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION AFT BULK CARGO DOOR SILL ENTRY FLOOR PLATE UNDER SCUFF PLATE UPPER SURFACE AT BS 1980 TO 2040. CORROS ION REMOVED AND TREATED PER BOEING SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1996081500893 19960815 00893 NM 1996 8 15 P5CA9600552 1 19960715 A 5320 SUPPORT BOEING 747 747132 1384882 NM BS 1940-1960 BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 BROKEN AFT CARGO SLOPE PANEL SUPPORT AT BS 1940 TO 1960. REPLACED SLOPE PANEL SUPPORT PER BOEING SRM 51-10-01. 2 L 7 4 4F A20WE 1996081500894 19960815 00894 NM 1996 8 15 P5CA9600553 1 19960715 A 5320 SUPPORT BOEING 747 747132 1384882 NM BS 1660-1720 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION MAIN DECK BS 1660 TO BS 1720 RIGHT MOST OUTBOARD LONGITUDINGAL FLOOR SUPPORT UPPER SURFACE. CORROSION REMOVED AND TREATED PER BOEING SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1996081500895 19960815 00895 NM 1996 8 15 P5CA9600554 1 19960715 A 5315 FLOOR BEAM BOEING 747 747132 1384882 NM BS 1720 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION MAIN DECK BS 1720 FLOOR BEAM UPPER CHORD UPPER SURFACE. CORROSION REMOVED AND TREATED PER BOEING SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1996081500896 19960815 00896 NM 1996 8 15 P5CA9600555 1 19960715 A 5347 TIE DOWN TRACK BOEING 747 747132 1384882 NM BS 1670 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION MAIN DECK BS 1670 RBL 98 TIE DOWN TRACK OUTBOARD FLANGE. REMOVED CORROSION AND TREATED PER BOEING SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1996081500897 19960815 00897 NM 1996 8 15 P5CA9600556 1 19960715 A 5315 FLOOR BEAM BOEING 747 747132 1384882 NM BS 1660 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION MAIN DECK BS 1660 FLOOR BEAM UPPER CHORD AT RBL 100 RIGHT END REINFORCING PLATE. REMOVED CORROSION AN D TREATED PER BOEING SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1996081500898 19960815 00898 WP 1996 8 15 RRXA96066 1 19960813 A 2910 TEE FITTING DOUG DC8 DC873F 302199F WP RT HYD SYST FAILED A RRXA A J UNSCHED LANDING DUMP FUEL K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 15 795FT 46103 SHUTDOWN HYDRAULIC SYSTEM DUE STEADY SLOW QTY LOSS, WITH SYSTEM SHUTDOWN QTY LOSS STOPPED. THEN RT GEAR DOOR LIGHT CAME ON WITH A LOUD RUMBLE FROM THE NOSE GEAR DOOR. ELECTED TO RETURN TO EINN, DUMPED FUEL TO MAX LANDING WEIGHT. REPOWERE D HYDRAULIC SYSTEM FOR NORMAL LANDING. REPLACED TEE FITTING RT MAIN RESERVOIR AND LEAK CHECKED GOOD. CHECKED AND ADJUS TED UPLOCK RIGGING ON MAIN LANDING GEAR DOORS AND GROUND OPS CHECKED GOOD PER 32-10-00. 2 L 7 4 4F RT 4A25 1996081500899 19960815 00899 WP 1996 8 15 ARWA9608004 1 19960814 A 2720 NAS16128 O-RING DOUG DC8 DC863F 302198F WP RUDDER CONTL DAMAGED A ARWA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 19 441J 45988 INFLIGHT AT FL 350, HYDRAULIC QUANTITY SUDDENLY STARTED DESCENDING AND CONTINUED DESCENDING. ISOLATED HYDRAULIC SYSTEM. RETURNED TO MIAMI AND FOUND RUDDER SELECTOR VALVE PLUG LEAKING. REPLACED O-RING, NO LEAKS NOTED IAW DC-8 MM 29-00-00. 2 L 7 4 4F 4A25 1996081900001 19960819 00001 NM 1996 8 19 AALA961076 1 19960716 A 5330 SKIN BOEING 727 727227 1384078 NM BS660 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 731AA 20738 TUL - FOUND SKIN BULGED STATION 660 AND STRINGER 28 RT. CUT OUTCORRODED AREA AND INSTALLED SKIN DOUBLER AND STRINGER SE CTION PER SRM53-30-3 P 1-10 53-10-3 PAGE 1-10. (M) 2 L 7 3 4F A3WE 1996082000001 19960820 00001 NM 1996 8 20 EISA96098 1 19960703 A 3610 CLAMP BOEING 727 727221 1384071 NM NR 1 ENG LOOSE A EISA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SW 07 363PA 22535 ENGINE NR 1 FIRE WARNING LIGHT ILLUMINATED AFTER TAKEOFF. ENGINE NR 1 SHUTDOWN, LIGHT EXTINGUISHED UPON THROTTLE CLOSIN G. FOUND CLAMP ON 8TH STAGE DUCT LEAKING AIR ON FIRE WALL LOOP. REMOVED AND INSPECTED CLAMP AND DUCT FOR CRACKS, NO DE FECTS NOTED. RAN ENGINE NO LEAKS NOTED. (M) 2 L 7 3 4F A3WE 1996082000002 19960820 00002 NM 1996 8 20 UPS96420813 1 19960729 A 5412 FIRE WALL BOEING 747 747123 1384873 NM NR 3 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE: C. PYLON NR 3, FOUND VERTICAL FIRE WALL AT NAC STA 180 CRACKED AT LT TOP CORNER (CRACK IS 1.5 INCHES LONG). REPLACED FIRE WALL IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996082000003 19960820 00003 NM 1996 8 20 UPS96420814 1 19960718 A 5411 FRAME BOEING 747 747123 1384873 NM NR 3 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE: C. PYLON NR 3, FOUND LT FORWARD FRAME OF BULKHEAD NAC STA 222 CRACKED AT TOP SIDE (CRACKS 2X RUNNING FROM AFT TOP FASTENER TO FRAME EDGE). PERFORMED REPAIR IAW KLM DFX 96-153 ISSUE NR 2 UPS EFN NR 747-54-0128. 2 L 7 4 4F A20WE 1996082000004 19960820 00004 NM 1996 8 20 UPS96420815 1 19960802 A 5312 BULKHEAD WEB BOEING 747 747123 1384873 NM BS 400 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE: C. MAIN DECK BS 400 BULKHEAD WEB CRACKED JUST BELOW LT STR 26, BS 400 LT BULKHEAD WEB CRACK REPAIRED IAW SRM 53-10-04, FIG 78. 2 L 7 4 4F A20WE 1996082000005 19960820 00005 NM 1996 8 20 UPS96420820 1 19960719 A 5414 SKIN BOEING 747 747123 1384873 NM NR 1 PYLON WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE: C. PYLON NR 1, WEAR DAMAGE IN PYLON LEADING EDGE SKIN LT NAC STA 211/216 AND WEAR DAAMAGE IN PYLON SK IN LT TOP SIDE NAC 220/225. REPAIRED LEADING EDGE SKIN IAW UPS EFN 747-54-0129, KLM 96-160. REPAIRED PYLON SKIN LT TOP SIDE IAW SRM 51-30-03, FIG 17A. 2 L 7 4 4F A20WE 1996082000006 19960820 00006 NM 1996 8 20 UPS96420821 1 19960722 A 5315 FLOOR BEAM BOEING 747 747123 1384873 NM BS 1580 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE: C. MAIN DECK FLOORBEAM: FOUND FLOOR BEAM UPPER CHORD CORRODED AT BS 1580 RBL 69/88. CORROSION REMOV ED ON UPPER CHORD BS 1580 RBL 69/88 IAW SRM 51-10-01. UPPER CHORD OUT OF LIMITS IAW SRM 53-10-01, REPAIRED UPPER CHORD BETWEEN RBL 69/88 IAW SRM 53-10-07. 2 L 7 4 4F A20WE 1996082000007 19960820 00007 NM 1996 8 20 UPS96420822 1 19960718 A 5315 FLOOR BEAM BOEING 747 747123 1384873 NM BS 680 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE: C. MAIN DECK FLOOR BEAM UPPER CHORD CORRODED AT BS 680 BETWEEN 11 RT/LT. CORROSION REMOVED ON UPPER CHORD AT BS 680 BETWEEN 11 RT/LT. UPPER CHORD OUT OF LIMITS IAW SRM 53-10-01. REPAIRED UPPER CHORD AT BS 680 BETWEEN 11 RT/LT IAW SRM 51-40-04, FIG 1. 2 L 7 4 4F A20WE 1996082000008 19960820 00008 NM 1996 8 20 UPS96420823 1 19960726 A 5320 FITTING BOEING 747 747123 1384873 NM BS 1960 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE: C. MAIN DECK FLOOR STRUCTURE, FITTING AT STA 1960 RBL 57 IS CRACKED. LENGTH OF CRACK IS 1.5 INCHES. REMOVED CRACKED FITTING AND INSTALLED NEW FITTING AT BS 1960 RBL 57 IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996082000009 19960820 00009 NM 1996 8 20 UPS96420824 1 19960719 A 5414 SKIN BOEING 747 747123 1384873 NM NAC STA 208 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE: C. CRACK IN PYLON SKIN AT ACCESS PANEL CUTOUT LT NAC STA 208. REPAIRED SKIN IAW SRM 54-30-03, FIG 17 B. 2 L 7 4 4F A20WE 1996082000010 19960820 00010 NM 1996 8 20 UPS96420825 1 19960806 A 3350 LIGHT BOEING 747 747121 1384871 NM CREW SERV DOOR INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE: DLY. EMERGENCY EXIT LIGHT ON CREW SERVICE DOOR INOP. EXIT DOOR LIGHT OPERATIONAL. OPS CHK GOOD. 2 L 7 4 4F A20WE 1996082000011 19960820 00011 NM 1996 8 20 UPS96420828 1 19960724 A 5315 UPPERCHORD BOEING 747 747123 1384873 NM BS 1000 CRACKED A IPXA O OTHER O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE CPCP, MAIN DECK FLOOR BEAM UPPER CHORD CORRODED AT BS 1000 BETWEEN RBL 70 TO 100. REMOVED CORROSION IAW SRM 51-10-01, UPPER CHORD OUT OF LIMITS IAW SRM 53-10-01. REPAIRED UPPER CHORD AT BS 1000 FROM RBL 70 TO RBL 108 IAW S RM 53-10-07. 2 L 7 4 4F A20WE 1996082000012 19960820 00012 NE 1996 8 20 9617089104 2 19960808 A 7261 7578679 OIL FILTER DOUG DC9 DC915 3022036 WP PWA JT8 JT8D7 52053 NE RT ENGINE CLOGGED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 94S 47204 653404 DURING TAKEOFF ROLL, RIGHT ENGINE OIL STRAINER CLOGGING LIGHT ILLUMINATED. CREW ABORTED TAKEOFF AND RETURNED TO GATE WI THOUT INCIDENT. MAINTENANCE REPLACED RIGHT ENGINE OIL FILTER, OPS AND LEAK CHECK OK. 2 L 7 2 4F 4 F A6WE E2EA 1996082200001 19960822 00001 NE 1996 8 22 CALA9601167 2 19960813 A 7250 835601 T1 BLADE BOEING 737 737219 1384469 NM PWA JT8 JT8D9 52048 NE NR 1 ENGINE FRACTURED A CALA A E UNSCHED LANDING ENGINE SHUTDOWN E VIBRATION/BUFFET CL CLIMB 1 SW 09 10248 20344 666932 THE NR 1 ENGINE ROLLED BACK TO 1.4 EPR AND AIRCRAFT VIBRATION WAS FELT AFTER GEAR RETRACTION. THE NR 1 ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS RETURNED TO CAE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE DAMAGED. THE NR 1 ENGINE WAS REMOVED AND REPLACED. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION. *S/D* SHOP FINDINGS REPORTED T1 BLADE FRACTURE DUE TO OVERTEMP AT POINT OF FRACTURE. 2 L 7 2 4F 4 F A16WE E2EA 1996082200002 19960822 00002 NM 1996 8 22 CALA9601168 1 19960815 A 3231 2670112 SAFETY VALVE BOEING 757 757224 1384958 NM RT MLG DOOR INOPERATIVE A CALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 09 14107 7863 7863 27297 THE GEAR DOOR LIGHT ILLUMINATED AFTER GEAR EXTENSION ON APPROACH. CHECKLIST PROCEDURES WERE COMPLIED WITH AND THE AIRCR AFT LANDED AT EWR. THE AIRCRAFT ARRIVED AT GATE WITH RIGHT GEAR DOOR DOWN. MAINTENANCE FOUND THE RT MLG DOOR SAFETY VA LVE AT FAULT. THE RT MLG DOOR SAFETY VALVE WAS REMOVED AND REPLACED PER MM 32-35-05 AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A2NM 1996082200003 19960822 00003 NM 1996 8 22 CALA9601169 1 19960815 A 2750 RETRACT MECH BOEING 737 737524 1384721 NM TE FLAPS LACK OF LUBE A A CALA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SW 09 17614 27327 YHE FLAPS WOULD NOT EXTEND BEYOND 15 DEGREES DURING APPROACH. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BOTH OUTBOARD FLAP'S JACKSCREW GIMBALS DRY OF LUBRICATION. THE GIMBALS WERE LUBRICATED AND OPERATION OF THE FLAPS CHECK ED GOOD. 2 L 7 2 4F RT A16WE 1996082200004 19960822 00004 WP 1996 8 22 CALA9601170 1 19960815 A 3350 60030451 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 33817 49371 INSPECTION FOUND FORWARD OVERWING EMERGENCY LIGHTS INOPERATIVE. THE BATTERIES WERE REMOVED AND REPLACED AND THE OPERATI ON OF THE LIGHTS WAS RESTORED. 2 L 7 2 4F A6WE 1996082200005 19960822 00005 WP 1996 8 22 CALA9601171 1 19960815 A 4920 3812761 APU COMPRESSOR DOUG DC9 DC982 3022082 WP AFT FUSELAGE DAMAGED A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 14890 21823 4788 49114 THERE WAS A STRONG PUNGENT ODOR IN THE AIRCRAFT CABIN SHORTLY AFTER TAKEOFF. NO ODOR WAS NOTICED DURING CRUISE PORTION OF FLIGHT WITH BOTH PACKS OPERATING. MAINTENANCE FOUND THE APU COMPRESSOR DAMAGED AND SEAL LEAKING. THE APU WAS PLACAR DED INOPERATIVE FOR FUTURE REPLACEMENT. IN ADDITION, BOTH PACK WATER SEPARATOR BAGS WERE REMOVED AND REPLACED. THE ENG INES WERE RUN AND LEAK CHECKS WERE GOOD WITH NO ODOR OBSERVED. 2 L 7 2 4F A6WE 1996082200006 19960822 00006 WP 1996 8 22 CALA9601172 1 19960730 A 5522 SKIN DOUG DC9 DC982 3022082 WP LT ELEVATOR TORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10834 49494 INSPECTION FOUND A 2 INCH TEAR IN SKIN AT LT ELEVATOR LEADING EDGE INBOARD NR 1 HINGE. THE TORN SECTION OF SKIN WAS REM OVED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-30 AND 55-20-0, ITEM 1. 2 L 7 2 4F A6WE 1996082200007 19960822 00007 WP 1996 8 22 CALA9601173 1 19960731 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP BS 905 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10834 49494 INSPECTION FOUND FLOOR SUPPORT CRACKED AT STA 905 LEFT. A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1996082200008 19960822 00008 WP 1996 8 22 CALA9601174 1 19960801 A 5210 SKIN DOUG DC9 DC982 3022082 WP PAX DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10834 49494 INSPECTION FOUND SKIN DENTED ALONG BOTTOM OF MAIN CABIN DOOR. THE DENTED SKIN WAS CUT OUT, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 52-05, FIGURE 37. 2 L 7 2 4F A6WE 1996082200009 19960822 00009 WP 1996 8 22 CALA9601175 1 19960730 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10834 49494 A TEMPORARY REPAIR DOUBLER HAD BEEN INSTALLED DUE TO SKIN DAMAGE AFT OF LT FORWARD WATER SERVICE PANEL. A PERMANENT CLA SS I REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-04, FIGURE 12B. 2 L 7 2 4F A6WE 1996082200010 19960822 00010 WP 1996 8 22 CALA9601176 1 19960731 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 313 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10834 49494 A TEMPORARY REPAIR DOUBLER HAD BEEN INSTALLED DUE TO DENTED FUSELAGE SKIN AT STA 313 LEFT. A PERMANENT CLASS I REPAIR W AS FABRICATED AND INSTALLED IAW SRM 53-04, FIGURE 12B. 2 L 7 2 4F A6WE 1996082200011 19960822 00011 WP 1996 8 22 CALA9601177 1 19960727 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 198-200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10834 49494 INSPECTION FOUND FLOOR SUPPORT ANGLE AT AFT LOWER CORNER OF FORWARD ENTRY DOOR STA 198 TO 200 CORRODED. THE SUPPORT ANG LE WAS REMOVED AND REPLACED IAW SRM 53-30-5. 2 L 7 2 4F A6WE 1996082200012 19960822 00012 WP 1996 8 22 CALA9601178 1 19960730 A 5320 CUSP MEMBRANE DOUG DC9 DC982 3022082 WP BS 1174 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10834 49494 INSPECTION FOUND CUSP MEMBRANE CORRODED FORWARD AND AFT OF STA 1174 IN AFT BAGGAGE BIN. THE AREA WAS REPAIRED IAW SRM 5 3-01. 2 L 7 2 4F A6WE 1996082200013 19960822 00013 WP 1996 8 22 CALA9601179 1 19960730 A 5320 CUSP MEMBRANE DOUG DC9 DC982 3022082 WP BS 1134/1135 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10834 49494 INSPECTION FOUND CORROSION ON CUSP MEMBRANE AT STA 1134 AND 1135, LT SIDE IN AFT BAGGAGE BIN. THE AREA WAS REPAIRED IAW SRM 53-01. 2 L 7 2 4F A6WE 1996082200014 19960822 00014 WP 1996 8 22 9617741160 1 19960815 A 2132 AW2835AF01 INDICATOR DOUG DC10 DC1040 3023508 WP COCKPIT FAILED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 160US 33227 33227 46769 DURING CLIMB, CABIN WOULD NOT PRESSURIZE. FLIGHT RETURNED TO SEA. MAINTENANCE REPLACED THE CABIN DIFFERENTIAL PRESSURE INDICATOR, OPERATIONAL CHECK OK. 2 L 7 3 4F A22WE 1996082200015 19960822 00015 WP 1996 8 22 9617759852 1 19960814 A 3260 DNLOCK SENSOR DOUG DC9 DC951 3022051 WP LT MLG MALFUNCTIONED A NWAA K NONE N FALSE WARNING DE DESCENT 1 GL 01 761NC 47709 DURING DESCENT ON GEAR EXTENSION, THE LEFT GEAR UNSAFE LIGHT CAME ON AND THE LEFT GEAR GREEN LIGHT WAS OUT. RECYCLED GE AR AND GOT NORMAL DOWN AND GREEN INDICATION. FLIGHT LANDED WITHOUT INCIDENT. PERFORMED TEST OF SYSTEM, REPLACED DOWN L OCK SENSOR AND OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996082200016 19960822 00016 WP 1996 8 22 9617769961 1 19960814 A 3260 SWITCH DOUG DC9 DC931 3022065 WP NLG MALFUNCTIONED A NWAA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 01 924RW 47185 DURING APPROACH, NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR WAS EXTENDED. BULBS WERE CHANGED WITH NO H ELP. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NOSE LANDING GEAR SWITCH, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996082200017 19960822 00017 WP 1996 8 22 9617779609 1 19960812 A 3350 BATTERY PACKS DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 609NW 47234 DURING LINE MAINTENANCE INSPECTION, FOUND EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BOTH BATTERY PACKS, OPERATION AL CHECK NORMAL. 2 L 7 2 4F A6WE 1996082200018 19960822 00018 WP 1996 8 22 9617789984 1 19960813 A 3397 WIRE DOUG DC9 DC932 3022066 WP CABIN DAMAGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 984US 47383 DURING PERIODIC CHECK, FOUND EMERGENCY LIGHTS AT ROWS 11 THROUGH 13 INOPERATIVE. MAINTENANCE REPAIRED PINCHED WIRE AT R OW 12 AND REPLACED FUSE AT LEFT AFT BATTERY PACK AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996082200019 19960822 00019 WP 1996 8 22 9617799916 1 19960812 A 3350 FUSE DOUG DC9 DC932 3022066 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 949N 47566 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN EMERGENCY AND FORWARD SERVICE DOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BLOWN FUSE, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996082200020 19960822 00020 WP 1996 8 22 9617809984 1 19960813 A 3350 BATTERY PACKS DOUG DC9 DC932 3022066 WP NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 984US 47383 DURING PERIODIC CHECK, FOUND NACELLE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996082200021 19960822 00021 WP 1996 8 22 9617819604 1 19960812 A 3231 UPLATCH ASSY DOUG DC9 DC932 3022066 WP LT MLG DOOR LOOSE A NWAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 01 604NW 47222 DURING APPROACH, LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS EXTENDED. GO-AROUND PROCEDURES WERE EXECUTED A ND AN UNEVENTFUL LANDING WAS ACCOMPLISHED ON SECOND ATTEMPT. MAINTENANCE FOUND THE LEFT MAIN GEAR DOOR UPLATCH MECHANIS M LOOSE. TIGHTENED UPLATCH MECHANISM. ALSO, REPLACED BOTH MAIN GEAR DOOR SKID PLATES DUE TO DAMAGE ON LANDIND. NO SHE ETMETAL DAMAGE WAS INCURRED. 2 L 7 2 4F A6WE 1996082200022 19960822 00022 NM 1996 8 22 9617826636 1 19960815 A 3350 BATTERY PACK BOEING 747 747251B 1384892 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 636US 23547 DURING LINE CHECK, FOUND ZONE-B EMERGENCY FLOOR PATH LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996082200023 19960822 00023 NM 1996 8 22 9617832709 1 19960815 A 7933 OIL TEMP IND BOEING 727 727225 1384077 NM PWA JT8 JT8D15A 52051 NE RT ENGINE MALFUNCTIONED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 GL 01 818EA 22555 695266 DURING CLIMBOUT, THE RIGHT ENGINE OIL TEMPERATURE BEGAN STEADILY RISING. CREW PERFORMED A PRECAUTIONARY SHUTDOWN OF THE RIGHT ENGINE. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED THE FOLLOWING FUNCTIONS ON THE RIGHT ENGINE, INSPECTED MAG PLUGS, OIL SCREEN, FUEL HEAT VALVE, REPLACED OIL TEMPERATURE INDICATOR AND OIL TEMPERATU RE BULB. LEAK AND OPERATIONAL CHECK OK. 2 L 7 3 4F 4 F A3WE E2EA 1996082200024 19960822 00024 NM 1996 8 22 SWAA960813 1 19960812 A 2612 FIRE DET MODULE BOEING 737 7372H4 138448C NM NR 2 ENGINE MALFUNCTIONED A SWAA A E F UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 07 61SW 21970 DIVERTED TO DTW DUE TO NUMBER 2 ENGINE FIRE WARNING SOUNDING IN FLIGHT AND FIRE BOTTLES ACTIVATED. CREW PERFORMED ENGI NE SHUTDOWN PROCEDURES. AIRCRAFT LANDED AT DTW WITHOUT INCIDENT. INSPECTED AND FOUND NO EVIDENCE OF FIRE OR OVERHEAT CONDITION. REPLACED FIRE DETECT MODULE, FIRE CONTROL PANEL, FIRE BOTTLES AND OP CHECKED SYSTEM PER BOEING M/M. 2 L 7 2 4F A16WE 1996082200025 19960822 00025 1996 8 22 SWAA960814 4 19960808 A 3418 AOA BOEING 737 7375H4 138449D NM STALL WARNING DAMAGED A SWAA A K UNSCHED LANDING NONE F FLT CONT AFFECTED TO TAKEOFF 1 SW 07 521SW 25320 AFTER TAKEOFF, EXPERIENCED CAPT STICK SHAKER ACTIVATION. RESETING C/B, NO HELP. AIRCRAFT RETUNED TO MDW AND MADE AN UNE VENTFUL LANDING. INSPECTED AND FOUND AOA VANE DAMAGED. REPLACED STALL WARNING VANE PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996082200026 19960822 00026 1996 8 22 SWAA960815 4 19960810 A 3417 HG480B42 ADC BOEING 737 7373Q8 1384670 NM LT COCKPIT MALFUNCTIONED A SWAA A O UNSCHED LANDING OTHER F FLT CONT AFFECTED CL CLIMB 1 SW 07 672SW 23406 AFTER TAKEOFF, CAPT AIRSPEED INDICATOR ROLLED BACK CAUSING STALL AND WINDSHEAR WARNING. AIRSPEED THEN WENT TO MAX SCAL E WITH STICK SHAKER ACTIVATION. AIRCRAFT RETUNED TO PHX AND MADE AN UNEVENTFUL LANDING. INSPECTED AND REPLACED CAPT AD C, PERFORMED PITOT STATIC LEAK CHECK AND DFCS BITE CHECK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996082200027 19960822 00027 EU 1996 8 22 QXEA9600316 1 19960815 A 3350 312003 FUSES FOKKER F28 F28MK1000 4990808 EU CABIN BLOWN A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 454US 11107 EVAC SIGN ABOVE COCKPIT ENTRY WAY AND SINGLE BULB EVAC LIGHT ABOVE CABIN ENTRY WAY ARE INOP. REPLACED TWO BLOWN FUSES, BULB IN EXIT SIGN ABOVE COCKPIT DOOR AND SIGNS OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996082200028 19960822 00028 EU 1996 8 22 QXEA9600317 1 19960815 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU CABIN CORROSION A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 RIGHT HAND OUTBOARD SEAT TRACK HAS CORROSION ON INBOARD FLOOR SUPPORT AT FRAME 12405, 13365 AND 13875A. CORROSION NOTED DURING C-CHECK NR300-35-36-37. TRACK REPLACED I/A/W SRM 530215. 2 L 7 2 4F RT A20EU 1996082200029 19960822 00029 EU 1996 8 22 QXEA9600318 1 19960815 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 A .25 INCH CRACK AT FRAME 15205, FRAME TO SKIN ANGLE ABOVE LOWER DIAGONAL BETWEEN STRINGERS 53A AND 51. CRACK NOTED DUR ING C-CHECK NR300-103. CRACK REPAIRED I/A/W SRM 530213 PG 4. 2 L 7 2 4F RT A20EU 1996082200030 19960822 00030 EU 1996 8 22 QXEA9600319 1 19960815 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 CRACKED CLIP AT FRAME 15205 BELOW LOWER DIAGONAL BETWEEN STRINGERS 53A AND 51. CRACK NOTED DURING C-CHECK NR300-104. C RACK REPAIRED I/A/W SRM 530213 PG 4. 2 L 7 2 4F RT A20EU 1996082200031 19960822 00031 EU 1996 8 22 QXEA9600320 1 19960815 A 5320 GUSSET FOKKER F28 F28MK4000 4990810 EU FRAME 6305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 GUSSET CRACKED AT FRAME 6305 AND AFT OF STRINGER 45. CRACK NOTED DURING C-CHECK NR300-124. CRACK REPAIRED I/A/W SRM 51 3101. 2 L 7 2 4F RT A20EU 1996082200032 19960822 00032 NM 1996 8 22 96FDEA01369 1 19960815 A 2760 RETURN HYD LINE BOEING 727 72725C 138400H NM A-HYD SYSTEM BROKEN A FDEA O OTHER K FLUID LOSS CR CRUISE 1 SO 25 136FE 19855 TOTAL LOSS OF A-SYS HYD AT FLT LEVEL 280. GEAR MANUALLY EXTENDED AND FLAPS WERE EXTENDED THROUGH ALTERNATE FLAP MASTER. REMOVED AND REPLACED SPOILER RETURN LINE RT. FOUND 2 BROKEN BRACKETS AT SPOILER CLOSE OUT PANEL, REMOVED AND REPLACED SAME (P/N 65-21658-36) AND (B27-57-001-13). PER CREW, PUMPS WERE SHUT OFF IMMEDIATELY WHEN A-SYS HYD WENT DOWN. REMOV ED AND REPLACED A-SYS CASE DRAIN FILTERS PRECAUTIONARY, THEY WERE CLEAN. RAN ENG 1 AND 2 PER JET RUN HANDBOOK, LEAK CK OK, SERVICED AND BLEED HYD SYS. 2 L 7 3 4F A3WE 1996082200033 19960822 00033 NM 1996 8 22 96FDEA01370 1 19960815 A 2130 RELAY BOEING 727 72722 1384002 NM CABIN PRESS SYST DIRTY A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 187FE 19079 CLIMBING OUT AT APPROX FLT LVL 250, HIGH PITCHED HOWL STARTED, FOLLOWED BY LOSS OF CABIN PRESS. UNABLE TO CONTROL CABI N PRESSURE USING BOTH PACKS. REMOVED AND REPLACED SAFETY RELAY, CLEANED AND OPS CK'D, OUTFLOW VALVES PER ENGINE RUN TO STEADY 4 PSI. 2 L 7 3 4F A3WE 1996082200034 19960822 00034 NM 1996 8 22 96FDEA01371 1 19960815 A 5315 FLOOR BEAM BOEING 727 727233 138408A NM BS 1148 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 219FE 21102 NR0054 AND 012, CORROSION (C53-111-01, -3) ON BOTTOM OF FLOOR BEAM BS 1148 RBL 10. 2 L 7 3 4F RT A3WE 1996082200035 19960822 00035 NM 1996 8 22 96FDEA01372 1 19960816 A 5315 65163161 FLOOR BEAM BOEING 727 72722 1384002 NM BS 344 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 NR0550 AND 017, CORROSION (C53-224-01, -1) ON FLOOR BEAM UPPER CHORD BS 344 LBL 65 RBL 17 WL 208. 2 L 7 3 4F A3WE 1996082200036 19960822 00036 NM 1996 8 22 96FDEA01362 1 19960814 A 5320 65453132 CLIP BOEING 727 727233 138408A NM BS 680 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 219FE 21102 NR 0471 AND 010. STRINGER CLIP IS CRACKED AT BS 680 STR 3L. ***S/D***** COMING. 2 L 7 3 4F RT A3WE 1996082200037 19960822 00037 NM 1996 8 22 96FDEA01366 1 19960815 A 5315 652082724 FLOOR BEAM BOEING 727 72722 1384002 NM BS 560 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 NR 0627 AND 015. CORROSION C53-224-01(1) AND BARE METAL ON BS 560 BEAM FROM LBL 62 - RBL 24 WL 208.1. ******S/D** ** COMING. 2 L 7 3 4F A3WE 1996082200038 19960822 00038 NM 1996 8 22 96FDEA01368 1 19960815 A 5313 BAC1498138 STRINGER BOEING 727 727233 138408A NM BS 390 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 219FE 21102 NR 0511 AND 011. CRACK IN STR 23L BETWEEN STR 380 AND STR 400. ****S/D***** COMING. 2 L 7 3 4F RT A3WE 1996082200039 19960822 00039 WP 1996 8 22 MWEA96412 1 19960815 A 3350 100865 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 206ME 47791 AFT STATION OF FLOOR EMERGENCY LIGHT INOP. REPLACED FLOOR TRACK BATTERY PACK. 2 L 7 2 4F A6WE 1996082200040 19960822 00040 NM 1996 8 22 DL72K961854 1 19960806 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 474DA 20751 LT OVERWING EMERGENCY EXIT LIGHT SIGNS INOP. REPLACED BATTERY PACK, CKS NORMAL. 2 L 7 3 4F A3WE 1996082200041 19960822 00041 WP 1996 8 22 DLL14961857 1 19960808 A 3350 TRACK LKHEED 1011 1011385115 5265015 WP CABIN DAMAGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 741DA 193C1245 EMERGENCY LIGHT TRACK AT MID GALLEY DAMAGED. REPLACED SECTION OF EMERGENCY LIGHT TRACK, CHECKS GOOD. 2 L 7 3 4F A23WE 1996082200042 19960822 00042 NM 1996 8 22 DL72S961859 1 19960808 A 3350 BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 538DA 22076 BOTH AFT DOOR SLIDE LIGHTS INOP. REPLACED BATTERY PACK, CKS GOOD. 2 L 7 3 4F A3WE 1996082200043 19960822 00043 NM 1996 8 22 DLM88961864 1 19960808 A 3213 5935347507 PISTON DOUG MD88 MD88 3023688 NM LT MLG CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 990DL 53342 FOUND ON E1 LTR CK, LT MLG PISTON CRACKED IN LOWER RADIUS REPAIR. REPLACED PISTON. 2 L 7 2 4F RT A6WE 1996082200044 19960822 00044 NM 1996 8 22 DLM88961865 1 19960808 A 3213 593534750707 PISTON DOUG MD88 MD88 3023688 NM RT MLG CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 990DL 53342 FOUND ON E1 LTR CK, RT MLG CRACKED AT AFT LUG INBD END. REPLACED PISTON. 2 L 7 2 4F RT A6WE 1996082200045 19960822 00045 NM 1996 8 22 DL73E961874 1 19960811 A 3350 LIGHT BOEING 737 737247 138448D NM R2 DOOR INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 243WA 23517 R2 DOOR EMERGENCY ESCAPE SLIDE LIGHT INOP. 2 L 7 2 4F A16WE 1996082200046 19960822 00046 NE 1996 8 22 DLM88961894 2 19960706 A 7230 500050101 FAN HUB ASSY DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE CRACKED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK T ENGINE CASE PENETRATION TO TAKEOFF 1 SO 27 927DA 49714 726984 DURING TAKEOFF ROLL, NR 1 ENGINE ENCOUNTERED AN UNCONTAINED FAILURE OF THE 1ST STAGE FAN HUB ASSEMBLY. ENGINE DEBRIS PE NETRATED THE FUSELAGE. TWO FATALITIES OCCURRED. UNDER NTSB INVESTIGATION. 2 L 7 2 4F 4 F RT A6WE E9NE 1996082200047 19960822 00047 NM 1996 8 22 DL72E961901 1 19960813 A 3350 1001141 LIGHT BOEING 727 727247 138408F NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 830WA 21482 FOUND AFT STAIR OVERHEAD EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY, OPS CHECK NORMAL. 2 L 7 3 4F A3WE 1996082200048 19960822 00048 NM 1996 8 22 P5CA9600600 1 19960815 A 2910 HYD LINE BOEING 747 747124 1384874 NM NR 4 PYLON LOOSE A P5CA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 23 855FT 19733 NR 4 HYDRAULIC SYSTEM LOW QUANTITY LIGHT CAME ON AFTER TAKEOFF. DEPRESSURIZED ADP AND EDP QUANTITY STABILIZED AT 1.6 GA LLONS. AFTER SYSTEM USED FOR LANDING QUANTITY RAISED TO 4.0 GALLONS THEN DROPPED TO 3 GALLONS AFTER LANDING. TIGHTENED LOOSE B-NUT ON SUPPLY LINE AT TOP OF PYLON, LEAK CHECK OK PER BOEING MAINTENANCE MANUAL 29-11-00. 2 L 7 4 4F A20WE 1996082200049 19960822 00049 NE 1996 8 22 P5CA9600601 2 19960815 A 7261 ENGINE BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 4 MALFUNCTIONED A P5CA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 23 853FT 52914 21 19753 686076 NR 4 ENGINE OIL QUANTITY DECREASED INFLIGHT, WHEN OIL PRESSURE BEGAN TO FLUCTUATE AND LOW OIL PRESSURE CAUTION LIGHT FLI CKERED. COMPLETED THE PRECAUTIONARY ENGINE SHUT DOWN. ON GROUND RUN FOUND OIL LEAKING FROM BREATHER PORT. REMOVED AND REPLACED ENGINE PER BOEING MAINTENANCE MANUAL 71-00-02. 2 L 7 4 4F 4 F A20WE E20EA 1996082200050 19960822 00050 NM 1996 8 22 P5CA9600602 1 19960805 A 5330 PANEL BOEING 747 747121 1384871 NM BS 540-560 DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FOUND DISTORTION ON PANEL AT FUS SKIN RT BETWEEN STA 540 AND 560 AND BETWEEN STRINGERS 35 TO 36. STRAIGHTENED AND SMOOT HED PANEL IAW SRM 51-40-01. 2 L 7 4 4F A20WE 1996082200051 19960822 00051 NM 1996 8 22 P5CA9600603 1 19960805 A 5400 BRACKET BOEING 747 747121 1384871 NM NR 2 PYLON CHAFED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FOUND TRIANGLE BRACKET UNDER NR 2 PYLON AFT FAIRING CHAFED. INSTALLED NEW BRACKET WITH RIVET AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 1996082200052 19960822 00052 NM 1996 8 22 P5CA9600604 1 19960805 A 5330 SKIN BOEING 747 747121 1384871 NM BS 720-820 DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FOUND DENTS, SCRATCHES AND CORROSION ON HEAD OF RIVETS AT FUS SKIN BETWEEN STA 720 TO 820, BETWEEN STRINGERS 26 TO 28 LT . STRAIGHTENED AND SMOOTHED PANEL, REMOVED LEVEL ONE CORROSION IAW SRM 51-10-01. CORROSION WITHIN LIMITS OF SRM 53-10- 01. 2 L 7 4 4F A20WE 1996082200053 19960822 00053 NM 1996 8 22 P5CA9600605 1 19960805 A 5330 SKIN BOEING 747 747121 1384871 NM BS 2180 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FOUND SURFACE CORROSION ON LOWER FUSELAGE SKIN AT STA 2180 BETWEEN STR 46 RT TO 46 LT. REMOVED LEVEL ONE CORROSION FROM SKIN, TREATED AREA IAW SRM 51-10-01. CORROSION FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996082200054 19960822 00054 NM 1996 8 22 P5CA9600606 1 19960805 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1980-2000 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FOUND CORROSION ON STRINGER 42 BETWEEN STA 1980 TO 2000 RT SIDE. REMOVED LEVEL ONE CORROSION AND TREATED AREA AS PER SR M 51-10-01. CORROSION FOUND TO BE WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996082200055 19960822 00055 NM 1996 8 22 P5CA9600607 1 19960805 A 5320 TIE CLIPS BOEING 747 747121 1384871 NM BS 1940 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FOUND CORROSION ON TIE CLIPS STATION 1940 RT SIDE AT STRINGERS 28, 29, 30, 31, 32. REMOVED LEVEL ONE CORROSION AND TREA TED IAW SRM 51-10-01. CORROSION FOUND TO BE WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996082200056 19960822 00056 NM 1996 8 22 P5CA9600608 1 19960805 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1940-1960 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FOUND CORROSION ON STRINGER 51 BETWEEN STA 1940 TO 1960 RT SIDE. REMOVED LEVEL ONE CORROSION AND TREATED AREA IAW SRM 5 1-10-01. CORROSION FOUND TO BE WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996082200057 19960822 00057 NM 1996 8 22 P5CA9600609 1 19960805 A 5320 SUPPORT BOEING 747 747121 1384871 NM BS 840 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FOUND CORROSION ON FAIRING SUPPORT AT LOWER FUSELAGE STATION 840 BETWEEN AREA LBL 15 TO RBL 30 AND SHEARED RIVET AT AREA . REMOVED LEVEL ONE CORROSION FROM FAIRING SUPPORT IAW SRM 51-10-01. CORROSION FOUND TO BE WITHIN LIMITS OF SRM 53-10- 01. 2 L 7 4 4F A20WE 1996082200058 19960822 00058 NM 1996 8 22 P5CA9600610 1 19960805 A 5711 SPAR BOEING 747 747121 1384871 NM WS 669 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FOUND CRACK ON UPPER CHORD AT STATION 669 NEAR THE FRONT SPAR. REMOVED AND REPLACED CHORD IAW SB 57-2273. 2 L 7 4 4F A20WE 1996082200059 19960822 00059 NM 1996 8 22 B4MR96001 1 19960812 A 5330 SKIN BOEING 727 727191 1384063 NM FUSELAGE CRACKED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 503MG 19392 DURING C1 CHECK, INSPECTION FOUND AD94-07-08 AGING AIRCRAFT REFERENCE SB 727-53-0183: HFEC INSPECTION REVEALED FIVE CRAC K INDICATIONS AT FASTENERS MARKED ON RIGHT HAND SECTION 41 FUSELAGE SKIN BS 219.8 TO BS 251.6 BETWEEN S15R TO S17R. REP AIRED CRACK RIGHT HAND SECTION 41 FUSELAGE SKIN BS 219.8 TO BS 251.6 BETWEEN S15R TO S17R IN ACCORDANCE WITH BOEING SB 7 27-53-0183 AND PART 1 OF STRUCTURAL REPAIR MANUAL 727-53-30-3 FIGURE 3. REPORT GENERATED BY AMERICAN INTERNATIONAL AIRW AYS (B4MR), DOING WORK FOR COOK AIRCRAFT LEASING (PART 91). 2 L 7 3 4F A3WE 1996082200060 19960822 00060 WP 1996 8 22 TC8A96054 1 19960814 A 3244 TIRE DOUG DC8 DC8F54 3021926 WP NR 6 BLEW A TC8A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 802CK 45679 NR 6 TIRE BLEW DURING TAXI, AIRCRAFT NOT MOVED AFTER TIRE BLEW. REMOVED AND REPLACED NR 6 TIRE IAW DC-8 MM 32-40-1. BR AKE INSPECTED FOR FREEDOM OF MOVEMENT AND BLED. TIRE BLEW DUE TO BRAKE DRAGGING. 2 L 7 4 4F 4A25 1996082200079 19960822 00079 CE 1996 8 22 96ZZZX4036 1 19960726 A 2130 VALVE LEAR 35 35A 5170602 CE CABIN PRESSURE MALFUNCTION A FKVA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 34TB 285 DESTINATION FROM BIRMINGHAM (BHM TO TRI-CITIES (TRI). ON ROTATION OUT OF BIRMINGHAM, BLEED AIR VALVES WENT INTO EMERGEN CY PRESSURIZATION MODE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO BIRMINGHAM AND LANDED WITHOUT INCIDENT. PILOT, THEREFORE, NOTIFIED THE DIRECTOR OF OPS AND THE DIRECTOR OF MAINTENANCE OF THE PROBLEM. DOM RESEARCHED THE PROB LEM AND NOTIFIED THE PIC TO RE-CYCLE THE BLEED AIR SWITCHES. CHECKS WERE THEN ACCOMPLISHED BY THE PIC AND THE SYSTEM OP ERATED NORMALLY. THE AIRCRAFT WAS THEN RETURNED TO MEMPHIS AND LANDED WITHOUT INCIDENT. CHECKS THEN WERE MADE BY THE D OM AND COULD NOT DUPLICATE THE PROBEM. 2 L 7 2 4F A10CE 1996082200083 19960822 00083 NM 1996 8 22 CALA9601180 1 19960816 A 2910 AE2463513J0604 HYD LINE BOEING 727 727227 1384078 NM NR 2 ENGINE LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 79754 21363 AIRCRAFT LOST A-SYSTEM HYDRAULICS WHILE EN ROUTE. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND THE N R 2 ENGINE A-HYDRAULIC SYSTEM RETURN FLEX LINE LEAKING IN S-DUCT AREA. THE FLEX LINE WAS REMOVED AND REPLACED AND LEAK CHECK WAS GOOD. IN ADDITION, THE NR 1 AND NR 2 ENGINE DRIVEN HYDRAULIC PUMPS WERE REMOVED AND REPLACED AS A PRECAUTIONA RY MEASURE. 2 L 7 3 4F A3WE 1996082200084 19960822 00084 NM 1996 8 22 CALA9601181 1 19960818 A 2782 269002911 ACTUATOR BOEING 727 727227 1384078 NM NR 7 LE FLAP LEAKING A A CALA A UNSCHED LANDING F K J FLT CONT AFFECTED FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 09 76752 19061 9209 21248 THE NR 7 LEADING EDGE SLAT WOULD NOT RETRACT AFTER TAKEOFF. THE FLAPS WERE CYCLED AND THE LEADING EDGE DEVICE RETRACTIO N FAILURE CHECKLIST WAS COMPLIED, BUT THE NR 7 SLAT WOULD NOT RETRACT. SOME LOSS OF THE A-SYSTEM HYDRAULIC QUANTITY WAS ALSO OBSERVED. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 7 LEADING EDGE SLAT ACTUATOR PISTON END CAP BLOWN OFF. THE NR 7 SLAT ACTUATOR WAS REMOVED AND REPLACED. LEAK AND OPERATIONAL CHE CKS WERE GOOD. 2 L 7 3 4F A3WE 1996082200085 19960822 00085 WP 1996 8 22 CALA9601182 1 19960801 A 5510 HINGE PLATES DOUG DC9 DC982 3022082 WP LT HOR STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10834 49494 INSPECTION FOUND INBOARD AND OUTBOARD HINGE PLATES FOR LT HORIZONTAL STABILIZER CORRODED. THE HINGE PLATES WERE REMOVED AND NEW PLATES WERE INSTALLED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 1996082200086 19960822 00086 WP 1996 8 22 CALA9601183 1 19960731 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 160-200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10834 49494 INSPECTION FOUND FLOOR Z-ANGLE CORRODED INBOARD OF FLOOR PANEL-K AT STA 160 TO 200. A NEW ANGLE WAS FABRICATED AND INST ALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1996082200087 19960822 00087 WP 1996 8 22 CALA9601184 1 19960727 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10834 49494 INSPECTION FOUND FLOOR PANEL SUPPORT Z-ANGLE CORRODED AT FLOOR PANEL-H, STA 200. THE Z-ANGLE WAS REMOVED AND REPLACED I AW SRM 51-30-2. 2 L 7 2 4F A6WE 1996082200088 19960822 00088 WP 1996 8 22 CALA9601185 1 19960730 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP BS 1287 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10834 49494 INSPECTION FOUND CRACKS AT NUTPLATE HOLES OF INTERCOSTAL IN AFT BAGGAGE BIN, BOTH FORWARD AND AFT OF STA 1287. THE AREA WAS REPAIRED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1996082200089 19960822 00089 WP 1996 8 22 CALA9601186 1 19960805 A 5350 CLIPS DOUG DC9 DC982 3022082 WP TAILCONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13891 49102 MORE THAN 30 POUNDS OF FORCE WAS REQUIRED TO PULL THE INTERIOR TAILCONE RELEASE HANDLE FROM CLIPS. THE RETAINING CLIPS WERE ADJUSTED TO SPECIFICATIONS PER MM 53-53-00. 2 L 7 2 4F A6WE 1996082200090 19960822 00090 NE 1996 8 22 9617946623 2 19960815 A 7230 FAN BLADE BOEING 747 747251B 1384892 NM PWA JT9 JT9D7Q 52054 NE NR 2 ENGINE FAILED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 01 623US 21705 02449 DURING CLIMBOUT OF NRT, THE NR 2 ENIGNE EXPERIENCED A COMPRESSOR STALL AND SUBSEQUENT VIBRATION OF THE ENGINE. CREW SHU T DOWN THE ENGINE AND RETURNED TO NRT WITHOUT FURTHER INCIDENT. INSPECTION OF THE ENGINE REVEALED NR 5 FAN BLADE BROKEN BELOW THE MID SPAN SHROUD AND THE LIBERATED PIECE EXITED THROUGH THE NOSE COWL AND DOG HOUSE. THE ENGINE, FORWARD FAIR ING COVER AND NOSE COWL WERE REPLACED. 2 L 7 4 4F 4 F A20WE E3NE 1996082200091 19960822 00091 WP 1996 8 22 9617951146 1 19960815 A 3260 802527 PROXIMITY BOX DOUG DC10 DC1040 3023508 WP MLG FAILED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 146US 40649 36429 46755 DURING TAKEOFF, ALL RED GEAR POSITION LIGHTS ILLUMINATED AND THE WARNING HORN SOUNDED WITH THE GEAR HANDLE UP. RECYCLED GEAR BUT LIGHT REMAINED ILLUMINATED UNITL PASSING 10,000 FEET. MAINTENANCE REPLACED THE MAIN LANDING GEAR PROXIMITY BOX . 2 L 7 3 4F A22WE 1996082200092 19960822 00092 WP 1996 8 22 9617961146 1 19960815 A 3260 POSITION IND DOUG DC10 DC1040 3023508 WP LANDING GEAR MALFUNCTIONED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 146US 46755 DURING TAKEOFF, THE GEAR RETRACTED BUT THE RED GEAR POSITIONS INDICATORS REMAINED ILLUMINATED. RECYCLED GEAR AND THE LI GHT WENT OUT. MAINTENANCE PERFORMED INSPECTIONS AND BITE TESTS, OPERATIONAL CHECK OK. 2 L 7 3 4F A22WE 1996082200093 19960822 00093 WP 1996 8 22 9617979912 1 19960815 A 3350 6011779 BATTERY PACK DOUG DC9 DC931 3022065 WP RT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 962N 47406 DURING LINE MAINTENANCE INSPECTION, FOUND THE RIGHT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATI ONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996082200094 19960822 00094 WP 1996 8 22 9617999612 1 19960816 A 3260 DOWNLOCK SWITCH DOUG DC9 DC932 3022066 WP NLG MALFUNCTIONED A NWAA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 01 912NW 47436 ON APPROACH, NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR WAS EXTENDED. RECYCLED GEAR AND NORMAL INDICATIONS WER E ACHIEVED. MAINTENANCE REPLACED THE NOSE GEAR DOWNLOCK SWITCH, OPERATIONAL CHECK NORMAL ON GEAR SWING. 2 L 7 2 4F A6WE 1996082200095 19960822 00095 NE 1996 8 22 9618002284 2 19960816 A 7230 COMP BLADES BOEING 727 727251 138408H NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE FOD A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 284US 21323 700793 DURING ENGINE RUNUP FOR TAKEOFF, THE NR 2 ENGINE EXPERIENCED SEVERAL COMPRESSOR STALLS. CREW ABORTED TAKEOFF AND RETURN ED TO THE GATE WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 ENGINE DUE TO FOD, OPERATIONAL CHECK OK. 2 L 7 3 4F 4 F A3WE E2EA 1996082200096 19960822 00096 NE 1996 8 22 9618019921 2 19960814 A 7230 P/D VALVE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D15 52051 NE LT ENGINE OUT OF ADJUST A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 01 943N 47647 656971 DURING TAKEOFF WHEN THROTTLES WERE ADVANCED, THE LEFT ENGINE EXPERIENCED SEVERAL COMPRESSOR STALLS. CREW ABORTED TAKEOF F AND RETURNED TO THE GATE. MAINTENANCE ADJUSTED P AND D VALVE, RUNUP AND OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F A6WE E2EA 1996082200097 19960822 00097 WP 1996 8 22 9618029602 1 19960818 A 3220 DOOR DOUG DC9 DC932 3022066 WP NLG NOT LATCHED A NWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 01 602NW 47046 EXCESSIVE NOISE AND VIBRATION WAS COMING FROM NOSE GEAR AREA AFTER GEAR RETRACTION ON DEPARTURE. RECYCLED GEAR WITH SAM E RESULTS. FLIGHT RETURNED TO MCI AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LEFT NOSE GEAR DOOR OPEN. SECURED GE AR DOORS. 2 L 7 2 4F A6WE 1996082200098 19960822 00098 WP 1996 8 22 9618039603 1 19960818 A 3350 6011779 POWER SUPPLY DOUG DC9 DC932 3022066 WP LT NACELLE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 603NW 47101 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996082200099 19960822 00099 WP 1996 8 22 9618049978 1 19960817 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9342 47391 DURING LINE MAINTENANCE INSPECTION, FOUND CABIN EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERIES IN FORWARD AISLE CEILIN G AND AFT RIGHT LAVATORY OVERHEAD, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996082200100 19960822 00100 WP 1996 8 22 9618059964 1 19960817 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 912RW 47150 DURING LINE MAINTENANCE INSPECTION, FOUND AFT TAILCONE AND CATWALK EMERGENCY LIGHTS DIM. REPLACED BATTERIES, OPERATIONA L CHECK NORMAL. 2 L 7 2 4F A6WE 1996082200101 19960822 00101 SO 1996 8 22 COMA9610247 1 19960816 A 5270 MS250851 SWITCH EMB 120 EMB120RT SO AVIONICS DOOR OUT OF ADJUST A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 162CA 120150 SERVICE DOOR WARNING LIGHT ILLUMINATED DURING FLIGHT. ADJUSTED THE AVIONICS DOOR MICROSWITCH. 2 L 7 2 4T RT A31SO 1996082200102 19960822 00102 EA 1996 8 22 COMA9660132 1 19960816 A 2613 356024310 OVERHEAT DET CNDAIR CL600 CL6002B19 EA RT PYLON MALFUNCTIONED A COMA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 916CA 7014 14TH STAGE BLEED AIR DUCT FAIL MESSAGE. ENGINE SHUT DOWN AND RETURN TO FIELD. REPLACED DEFECTIVE BLEED LEAK DETECTOR L OOP AT RT ENGINE PYLON. 2 L 7 2 4F RT A21EA 1996082200103 19960822 00103 NM 1996 8 22 SWAA960816 1 19960814 A 3350 CONNECTOR BOEING 737 7372H4 138448C NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 51SW 21448 DURING SCHEDULED A1 CHECK, FOUND EXTERIOR EMERGENCY LIGHTING INOP AT FWD SERVICE DOOR. REPAIRED CONNECTOR AT SOCKET AND OP CHECKED PER BOEING M/M. 2 L 7 2 4F A16WE 1996082200104 19960822 00104 NM 1996 8 22 SWAA960817 1 19960815 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 965-969 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 74SW 22674 DURING SCHEDULED D-CHECK, FOUND STR 27L CORRODED AT BS 965 TO 969 AND AT BS 1003. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996082200105 19960822 00105 NM 1996 8 22 SWAA960818 1 19960815 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 792 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 74SW 22674 DURING SCHEDULED D-CHECK, FOUND STRINGER SUPPORT CORRODED AT BS 792, AT S20L, WL 181. REPAIRED PER BOEING SRM AND TI-A5 1-002. 2 L 7 2 4F A16WE 1996082200106 19960822 00106 NM 1996 8 22 SWAA960819 1 19960815 A 5320 WEB BOEING 737 7372H4 138448C NM BS 492 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 74SW 22674 DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AT BS 492, RBL 28, WL 159. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996082200107 19960822 00107 NM 1996 8 22 SWAA960820 1 19960815 A 5320 WEB BOEING 737 7372H4 138448C NM BS 782 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 74SW 22674 DURING SCHEDULED D-CHECK, FOUND WEB AT DOOR FRAME CUTOUT CRACKED AT FASTENER HOLE, BS 782, RBL 29, WL 161. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996082200108 19960822 00108 NM 1996 8 22 SWAA960821 1 19960815 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 74SW 22674 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKS AT BS 178, BETWEEN RBL 7.7 AND 11.7. REPAIRED PER BOEING SRM AND T RAMCO EWO 96-0395. 2 L 7 2 4F A16WE 1996082200109 19960822 00109 NM 1996 8 22 SWAA960822 1 19960815 A 5330 SKIN BOEING 737 7372H4 138448C NM AFT GAL CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED B2 CHECK, FOUND FUSELAGE SKIN CRACKED .625 INCH FROM UPPER CUTOUT AT AFT GALLEY DOOR. REPLACED PER BOE ING SRM. 2 L 7 2 4F A16WE 1996082200110 19960822 00110 NM 1996 8 22 SWAA960823 1 19960815 A 5210 SKIN BOEING 737 7372H4 138448C NM AFT ENTRY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 20SW 21337 DURING SCHEDULED SERV CHECK, FOUND AFT ENTRY DOOR OUTER SKIN UPPER HINGE CUTOUT CRACKED AT LOWER RADIUS PROGRESSING DOWN WARD. REPAIRED PER TYPICAL REPAIR T1-A52-005. 2 L 7 2 4F A16WE 1996082200111 19960822 00111 NM 1996 8 22 SWAA960824 1 19960815 A 5330 SKIN BOEING 737 7372H4 138448C NM AFT FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 20SW 21337 DURING SCHEDULED SERV CHECK, FOUND AIRSTAIRS CUTOUT, FWD UPPER SUPPORT STRUCTURE FOR FWD DOOR STOP CRACKED AND EXTENDING OUT FROM UNDER STOP. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996082200112 19960822 00112 NM 1996 8 22 SWAA960825 1 19960814 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 383 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 344SW 24152 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN DENTED AT BS 383, BELOW S24R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996082200113 19960822 00113 NM 1996 8 22 SWAA960826 1 19960814 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 356 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 344SW 24152 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 356, BELOW S18R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996082200114 19960822 00114 NM 1996 8 22 SWAA960827 1 19960813 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 95SW 23054 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR LOWER HINGE CUTOUT ON DOOR .125 INCH CRACKED EXTENDING OUT FROM AFT LOWE R CORNER. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996082200115 19960822 00115 NM 1996 8 22 SWAA960828 1 19960814 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED B-CHECK, FOUND AFT CARGO DOOR HANDLE CUTOUT UPPER CORNER CRACKED ON OUTER SKIN. REPAIRED PER SWA RA 1- A50-020. 2 L 7 2 4F A16WE 1996082200116 19960822 00116 NM 1996 8 22 SWAA960829 1 19960810 A 3350 LIGHT BOEING 737 7372H4 138448C NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 52SW 21533 FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSEMBLY PER BOEING M/M. 2 L 7 2 4F A16WE 1996082200117 19960822 00117 NM 1996 8 22 SWAA960830 1 19960812 A 3350 1000679 LIGHT BOEING 737 7372H4 138448C NM COCKPIT INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 52SW 21533 FOUND COCKPIT EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSEMBLY PER BOEING M/M. 2 L 7 2 4F A16WE 1996082200118 19960822 00118 NM 1996 8 22 SWAA960831 1 19960812 A 5312 BULKHEAD BOEING 737 7375H4 138449D NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 515SW 25154 DURING SCHEDULED D-CHECK, FOUND CRACK INDICATION AT UPPER RADAR MOUNT AT BS 178 BULKHEAD LBL 6.7, WL 212.3. REPAIRED CR ACK PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996082200119 19960822 00119 NM 1996 8 22 SWAA960832 1 19960812 A 5315 FLOOR BEAM BOEING 737 7375H4 138449D NM BS 312 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 515SW 25154 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 312, LBL 1 AND RBL 7, WL 208. REPAIRED CRACK PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996082200120 19960822 00120 NM 1996 8 22 SWAA960833 1 19960812 A 5320 SUPPORT BOEING 737 7375H4 138449D NM BS 295-353 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 515SW 25154 DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CORROSION FROM BS 295 TO 353, RBL 52, WL 208. REPAIRED CRACK PER BOEING S RM. 2 L 7 2 4F RT A16WE 1996082200121 19960822 00121 NM 1996 8 22 SWAA960834 1 19960812 A 5320 ANGLE BOEING 737 7375H4 138449D NM BS 295 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 515SW 25154 DURING SCHEDULED D-CHECK, FOUND FLOOR WEB ANGLE CRACKED AT BS 295, RBL 55, WL 208. REPAIRED CRACK PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996082200122 19960822 00122 EU 1996 8 22 WWMA9600066 1 19960816 A 2611 72111121000 SMOKE DET SAAB SF340 340B 7860101 EU CARGO COMPT DIRTY A WWMA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 WP 15 326AE 340B326 THE CARGO SMOKE LIGHT ILLUMINATED WHEN THE CARGO DOOR WAS OPENED TO REMOVE BAGS. MAINTENANCE COULD NOT DUPLICATE PROBLE M. BOTH CARGO SMOKE DETECTORS WERE CLEANED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 1996082200123 19960822 00123 EU 1996 8 22 WWMA9600065 1 19960816 A 2150 7769105 ACM SAAB SF340 340B 7860101 EU RIGHT OUT OF OIL A WWMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 15 354SB 340B354 CREW REPORTED A SMELL IN THE COCKPIT AFTER THE ENGINES WERE RUNNING. MAINTENANCE FOUND THE RIGHT ACM OUT OF OIL AND REP LACED IT. AIRCRAFT WAS RUN WITH NO ODORS NOTED. 2 L 7 2 4T RT A52EU 1996082200124 19960822 00124 EU 1996 8 22 WWMA9600064 1 19960813 A 2611 72111211000 SMOKE DETECTORS SAAB SF340 340B 7860101 EU CARGO BAY DIRTY A WWMA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 WP 15 354SB 340B354 AT THE GATE WITH BOTH ENGINES SHUT DOWN AND EXTERNAL POWER ON THE AIRCRAFT THE CARGO SMOKE WARNING ILLUMINATED WHEN THE CARGO DOOR WAS OPENED. MAINTENANCE INSPECTED THE WIRING SYSTEM WITH NO DISCREPANCIES FOUND, BOTH CARGO SMOKE DETECTORS WERE REPLACED. 2 L 7 2 4T RT A52EU 1996082200125 19960822 00125 EU 1996 8 22 WWMA9600063 1 19960811 A 2121 VENT FAN SAAB SF340 340B 7860101 EU AVIONICS BAY ODOR A WWMA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 15 332AE 340B332 PILOT REPORTED A FUNNY NOISE AND ELECTRICAL SMELL IN THE AVIONICS VENT FAN. MAINTENANCE OPERATED THE FAN FOR 20 MINUTES AND COULD NOT DUPLICATE ANY PROPLEMS. 2 L 7 2 4T RT A52EU 1996082200126 19960822 00126 EU 1996 8 22 WWMA9000062 1 19960812 A 3330 2LA00510400 LIGHTS SAAB SF340 340B 7860101 EU CARGO COMPT DIRTY A WWMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 15 354SB 340B354 THE CARGO SMOKE INDICATOR ILLUMINATED ON GROUND, WHEN THE CARGO BAY WAS UNLOADED AN ELECTRICAL BURN SMELL WAS DETECTED. MAINTENANCE FOUND BOTH CARGO LIGHTS TO BE DIRTY AND BURNED. BOTH LIGHTS WERE REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE WITH NO FURTHER PROBLEMS. 2 L 7 2 4T RT A52EU 1996082200127 19960822 00127 WP 1996 8 22 96FDEA01373 1 19960817 A 3260 PROX BOX DOUG DC10 DC1030 3023501 WP NLG MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 302FE 46801 ON T/O, NOSE GEAR INDICATED NO RETRACT, BOTH INDICATIONS. ON LANDING NR 2 T/R WOULD NOT DEPLOY. RAN APPROPRIATE CHECKL IST, DUMPED FUEL AND RETURNED TO ANC. INSPECTED NOSE GEAR, PROX ELECTRONIC UNIT FROM A/C 315, INSTALLED IN A/C 302. JA CKED NOSE GEAR, CYCLED NOSE GEAR SEVERAL TIMES. ALL INDICATION NORMAL, OK FOR SERVICE SEE AML 603806 FOR T/R NR 2. 2 L 7 3 4F A22WE 1996082200128 19960822 00128 NM 1996 8 22 96FDEA01374 1 19960819 A 5320 651634031 SHEAR TIE BOEING 727 72722 1384002 NM BS 990 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 NR0690 AND 019, CORROSION ON SHEAR TIE AT BS 990 BETWEEN STR 29 TO 30L. *S/D* REPAIRED SHEAR TIE AT BS 990 BETWEEN ST RINGER 29 LEFT AND 30 LEFT AS PER FEDEX SRM 51-30-2. 2 L 7 3 4F A3WE 1996082200129 19960822 00129 NM 1996 8 22 96FDEA01375 1 19960819 A 5320 651634430 SHEAR TIE BOEING 727 72722 1384002 NM BS 1070 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 NR0689 AND 020, CORROSION ON SHEAR TIE AT BS 170 BETWEEN STR 28 TO 29R. 2 L 7 3 4F A3WE 1996082200130 19960822 00130 NM 1996 8 22 96FDEA01376 1 19960819 A 5320 651634031 SHEAR TIE BOEING 727 72722 1384002 NM BS 990 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 NR0683 AND 021, CRACKED SHEAR TIE AT BS 990 BETWEEN STR 29 TO 30R. 2 L 7 3 4F A3WE 1996082200131 19960822 00131 NM 1996 8 22 96FDEA01377 1 19960819 A 5320 651633920 SHEAR TIE BOEING 727 72722 1384002 NM BS 970 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 NR0682 AND 022, CRACKED SHEAR TIE AT BS 970 BETWEEN STR 28 TO 29R. *S/D* REMOVED CRACKED SHEAR TIE AND REPLACED IAW FE DEX SRM 51-30-2. 2 L 7 3 4F A3WE 1996082200132 19960822 00132 NM 1996 8 22 96FDEA01378 1 19960819 A 5320 651633937 SHEAR TIE BOEING 727 72722 1384002 NM BS 970 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 NR0681 AND 023, CRACKED SHEAR TIE AT BS 970 BETWEEN STR 29 TO 30R. 2 L 7 3 4F A3WE 1996082200133 19960822 00133 NM 1996 8 22 96FDEA01379 1 19960819 A 5313 651838727 STRINGER BOEING 727 72722 1384002 NM BS 1082 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 NR0672 AND 024, WHILE WORKING NR201 FOUND STR TO BE CRACKED AT BS 1082 WL 138 STR 29L. 2 L 7 3 4F A3WE 1996082200134 19960822 00134 NM 1996 8 22 96FDEA01380 1 19960819 A 5313 65181135 STRINGER BOEING 727 72722 1384002 NM BS 680-700 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 NR0129 AND 025, CORROSION (C53-224-02, -1) ON STR 6L BS 700 TO 680. *S/D* CORROSION ON STR NR 6L BS 700 TO 680 WAS FO UND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. REPAIRED STRINGER PER FEDEX SRM 53-10-3 FIG 3. 2 L 7 3 4F A3WE 1996082200135 19960822 00135 NM 1996 8 22 96FDEA01381 1 19960819 A 5320 651838714 DOUBLER BOEING 727 72722 1384002 NM BS 1080 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 NR0696 AND 002, CORROSION ON SKIN SPLICE DOUBLER AT BS 1080 FROM RBL 23 TO LBL 32 WL 140. ALSO, (P/N 65-18387-15). *S/ D* REMOVED CORROSION ON SKIN SPLICE DOUBLER AT BS 1080 RBL 23 TO LBL 32 WL 140, FOUND TO BE OUT OF LIMITS. REMOVED FAB RICATED SKIN SPLICE DOUBLER AND INSTALLED. 2 L 7 3 4F A3WE 1996082200136 19960822 00136 NM 1996 8 22 96FDEA01382 1 19960819 A 2710 65217227419 FITTING BOEING 727 72722 1384002 NM LT AILERON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 NR0360 AND 027, CORROSION (C57-581-01-1) LT WING O/B AILERON CONTROL ROD FITTING ON AILERON IS CORRODED. *S/D* REMOVED AND REPLACED LT WING O/B AILERON CONTROL ROD FITTING ON AILERON IAW FEDEX SRM 51-30-2. 2 L 7 3 4F A3WE 1996082200137 19960822 00137 NM 1996 8 22 96FDEA01383 1 19960819 A 5320 69206899 SHEAR TIE BOEING 727 72722 1384002 NM BS 1030 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 NR0673 AND 028, WHILE WORKING NR0668 FOUND BULGE IN BETWEEN SKIN AND FRAME AT BS 1030 BETWEEN STR 18 TO 19L. 2 L 7 3 4F A3WE 1996082200138 19960822 00138 NM 1996 8 22 96FDEA01384 1 19960816 A 5320 9086043 CLIP BOEING 727 72722 1384002 NM BS 970 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 NR0119 AND 018, CRACKED STR CLIP AT BS 970 STR 16R. *S/D* REMOVED CRACKED STRINGER CLIP AT BS 970 STRINGER 16 RT AND R EPLACED WITH NEW IAW FEDEX SRM 51-30-2. 2 L 7 3 4F A3WE 1996082200139 19960822 00139 NM 1996 8 22 96FDEA01364 1 19960814 A 5320 65184176 STIFFENER BOEING 727 72722 1384002 NM BS 314 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 NR 0607 AND 013. CORROSION C53-111-01(1) ON HORIZONTAL STIFFENER STA 314 RBL 12 WL 178. ****S/D***** COMING. 2 L 7 3 4F A3WE 1996082200140 19960822 00140 NM 1996 8 22 96FDEA01365 1 19960814 A 5320 65184175 STIFFENER BOEING 727 72722 1384002 NM BS 310 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 NR 0611 AND 014. CORROSION C53-111-01 ON HORIZONTAL STIFFENER STA 310 RBL 12 WL 178. ****S/D****** COMING. 2 L 7 3 4F A3WE 1996082200141 19960822 00141 1996 8 22 VNAA9608004 4 19960817 A 3417 7014700911 AIR DATA COMP DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT AVIONIC RACK DEFECTIVE A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 07 426JS 3038 DURING THE TAKEOFF ROLL, CREW REPORTED BEING ALERTED BY A FLIGHT GUIDANCE COMPUTER FAIL CAS MESSAGE. CREW ABORTED THE T AKEOFF AND RETURNED TO THE GATE. MX REPLACED THE NR 2 MINI AIR DATA COMPUTER IAW MM 34-11-01, GROUND CHECKED GOOD. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996082200142 19960822 00142 WP 1996 8 22 MWEA96413 1 19960817 A 3350 60030431 POWER SUPPLY DOUG DC9 DC915 3022036 WP CABIN INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 900ME 45841 DURING A-CHECK, FOUND SEVERAL EMER POWER CEILING LIGHTS INOP IN AFT CABIN. REPLACED BATTERY POWER SUPPLY, OPS CHECK GOO D. 2 L 7 2 4F A6WE 1996082200143 19960822 00143 WP 1996 8 22 SCNA96212 1 19960730 A 2611 13131 LAMP DOUG DC10 DC1010 3022110 WP NUMBER 3 INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 573SC 46905 CARGO SMOKE DETECTOR FAILED TEST ON THE NUMBER 3 POSITION. RELAMPED NUMBER 3 SMOKE DETECTOR AND OPERATIONAL CHECKED NOR MAL. 2 L 7 3 4F A22WE 1996082200144 19960822 00144 NE 1996 8 22 SCNA96213 2 19960805 A 7532 PRBC BOEING 727 727225 1384077 NM PWA JT8 JT8D17R 52049 NE NR 1 ENGINE MALFUNCTIONED A SCNA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 GL 15 283SC 22559 NUMBER 1 ENGINE EGT WENT TO 670 ON CLIMBOUT. RETURNED TO LAS. INSPECTED INLET AND EXHAUST, INSPECTED AND BLEW OUT PT2 AND PT7 LINES AND CHANGED THE PRESSURE RATIO BLEED CONTROL, OPS CHECKED ENGINE. 2 L 7 3 4F 4 F A3WE E2EA 1996082200145 19960822 00145 WP 1996 8 22 SCNA96214 1 19960807 A 2913 O-RING DOUG DC10 DC1030F 3023504 WP NR 2 ENGINE CUT A A SCNA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 15 603GC 47922 DURING FLIGHT NOTICED THAT THE NUMBER 2 ENGINE OIL QUANTITY WAS AT 0 AND THE OIL PRESSURE WAS FLUCTUATING BETWEEN 20 PSI AND 40 PSI. AFTER MONITORING, THE OIL PRESSURE DROPPED BELOW RED LINE AND NUMBER 2 OIL PRESSURE LIGHT ILLUMINATED. NU MBER 2 ENGINE WAS SHUT DOWN AND DIVERTED TO MSP. REMOVED AND REPLACED O-RINGS ON LEFT HAND HYDRAULIC PUMP SHAFT. PERFO RMED AN OPERATIONAL CHECK OF NUMBER 2 ENGINE AND ALL PARAMETERS INDICATED NORMAL IN ACCORDANCE WITH 71-00-00 AND 29-11-0 1. 2 L 7 3 4F RT A22WE 1996082200146 19960822 00146 NM 1996 8 22 SCNA96215 1 19960810 A 3350 S106 BATTERY BOEING 727 727225 1384077 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 283SC 22559 FOUND EMERGENCY LIGHT INOP ABOVE AFT EXIT DOOR. REPLACED BATTERIES IN THE LIGHT ASSEMBLY, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1996082200147 19960822 00147 NM 1996 8 22 SCNA96216 1 19960809 A 2611 PU90421S SMOKE DETECTOR BOEING 727 7272J4 1384006 NM AFT LAVATORY INOPERATIVE A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 288SC 20765 RIGHT AFT LAV SMOKE DETECTOR WILL NOT SHUT OFF. REMOVED AND REPLACED THE RIGHT AFT LAV SMOKE DETECTOR, OPS CHECKED GOOD . 2 L 7 3 4F RT A3WE 1996082200148 19960822 00148 NM 1996 8 22 SCNA96217 1 19960810 A 3350 10617844 BATTERY PACK BOEING 727 7272J4 1384006 NM CABIN LOOSE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 285SC 21676 RIGHT EXTERIOR OVERWING EMERGENCY LIGHT INOP. FOUND BATTERY PACK LOOSE, RESEATED AND SECURED BATTERY PACK, OPS CHECK GO OD. 2 L 7 3 4F RT A3WE 1996082200149 19960822 00149 NM 1996 8 22 SCNA96218 1 19960813 A 3350 S106 BATTERY PACK BOEING 727 727227 1384078 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 275AF 22092 AFT AIRSTAIR OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1996082200150 19960822 00150 NM 1996 8 22 SCNA96219 1 19960813 A 3350 6013211 BATTERY PACK BOEING 727 727227 1384078 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 275AF 22092 L-1 ENTRY DOOR, R-1 SERVICE DOOR AND FWD FLOOR TRACK EMERGENCY LIGHTS VERY DIM. REMOVED AND REPLACED FWD FLOOR TRACK BA TTERY POWER SUPPLY, OPS CHECKED GOOD. 2 L 7 3 4F A3WE 1996082200151 19960822 00151 NM 1996 8 22 SCNA96220 1 19960801 A 3260 MS250111 WARNING SWITCH BOEING 727 727225 1384077 NM NLG DOOR OUT OF ADJUST A SCNA O OTHER J WARNING INDICATION CL CLIMB 1 GL 15 283SC 22559 WHEN FLYING FROM 26,000 TO 28,000 FT IN TURBULANCE. ABOVE MACH 0.80, NOSE GEAR DOOR LIGHT FLICKERED ON AND OFF, FOLLOWE D BY A LOUD BANGING NOISE. JACKED NOSE LANDING GEAR. PERFORMED ADJUSTMENT, TEST OF NOSE WHEEL WELL DOORS PER MM 32-22- 1. PERFORMED ADJUSTMENT TEST OF LANDING GEAR DOOR WARNING SWITCH PER MM 32-62-11. ALL OPERATIONAL CHECKS NORMAL ON GRO UND. 2 L 7 3 4F A3WE 1996082200152 19960822 00152 NM 1996 8 22 SCNA96221 1 19960813 A 3350 FLOOR LIGHT BOEING 727 7272J4 1384006 NM CABIN SPLIT A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 288SC 20765 SECTION OF EMERGENCY FLOOR TRACK LIGHTING SPLIT FROM GALLEY CART TRAFFIC, NEAR AFT GALLEY AREA FORWARD OF 33D. REPLACED BAD SECTION OF TRACK LIGHTING IN AFT GALLEY, OPS CHECKED OK. 2 L 7 3 4F RT A3WE 1996082200153 19960822 00153 NM 1996 8 22 SCNA96222 1 19960813 A 3350 LIGHT BOEING 727 7272J4 1384006 NM CABIN DAMAGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 288SC 20765 EMERGENCY FLOOR TRACK LIGHTING SPLIT IN SECTION NEXT TO SEAT 5D. REPLACED BAD SECTION OF TRACK LIGHTING. OPS CHECKED O K. 2 L 7 3 4F RT A3WE 1996082200154 19960822 00154 WP 1996 8 22 SCNA96223 1 19960805 A 2612 24402534 CONNECTOR DOUG DC10 DC1015 3022118 WP ENGINE 3 LOOP A DIRTY A SCNA O OTHER N FALSE WARNING CR CRUISE 1 GL 15 152SY 48289 ENGINE 3 LOOP-A LIGHT ILLUMINATED IN-FLIGHT WITHOUT FIRE WARNING. FOLLOWED COM PROCEDURE AND LOOP-B TESTED SATISFACTORY . LOOP-A LIGHT WENT OUT WHILE PERFORMING COM PROCEDURE. CONTINUED FLIGHT USING LOOP-B DETECTION SYSTEM. REMOVED, IN SPECTED, AND CLEANED CANNON PLUGS. OPS CHECKED GOOD. 2 L 7 3 4F A22WE 1996082200155 19960822 00155 WP 1996 8 22 SCNA96224 1 19960807 A 2612 24402534 LOOP B ASSY DOUG DC10 DC1015 3022118 WP ENGINE 3 LOOP A FAULT A SCNA O OTHER J WARNING INDICATION CL CLIMB 1 GL 15 152SY 48289 ENGINE 3 LOOP-A LIGHT ILLUMINATED IN-FLIGHT WITHOUT FIRE WARNING. FOLLOWED COM PROCEDURE AND LOOP-B TESTED SATISFACTORY . LOOP-A LIGHT WENT OUT WHILE PERFORMING COM PROCEDURE. CONTINUED FLIGHT USING LOOP-B DETECTION SYSTEM. REMOVED, IN SPECTED, AND CLEANED CANNON PLUGS. OPS CHECKED GOOD. 2 L 7 3 4F A22WE 1996082200156 19960822 00156 WP 1996 8 22 SCNA96225 1 19960809 A 2612 24402534 FIRE WIRE DOUG DC10 DC1015 3022118 WP ENGINE 3 LOOP A CHAFFED A SCNA O OTHER J WARNING INDICATION CL CLIMB 1 GL 15 152SY 48289 ENGINE 3 LOOP-A LIGHT ILLUMINATED IN-FLIGHT WITHOUT FIRE WARNING. FOLLOWED COM PROCEDURE AND LOOP-B TESTED SATISFACTORY . LOOP-A LIGHT WENT OUT WHILE PERFORMING COM PROCEDURE. CONTINUED FLIGHT USING LOOP-B DETECTION FOUND CHAFED WIRE BY PYLON DETECTORS. PROTECTED AND WRAPPED WIRING SYSTEM. OPS CHECKED NORMAL IN ACCORDANCE WITH MM 26-10-00. 2 L 7 3 4F A22WE 1996082200157 19960822 00157 GL 1996 8 22 HEEA967643 2 19960813 A 7240 6899081 LINER 23035128 BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL COMBUSTION SEC DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8588X CAT95381 51486 CAE895475 COMBUSTION LINER REMOVED FROM TURBINE DUE TO -2 LOW POWER ON TEST CELL. TURBINE PRODUCED +1.6 WITH OH REPLACEMENT LIN ER. REPLACED DISCREPANT PART. 1 G 7 1 3U 3 U H2SW E1GL 1996082200158 19960822 00158 GL 1996 8 22 HEEA967644 2 19960813 A 7230 23007196 REAR SUPPORT 23033191 BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL COMPRESSOR MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 2245Y CAC70023 45751 CAE860583 RECEIVING INSPECTION REVEALED: IMPROPERLY MACHINED REAR SUPPORT RETAINING RING GROOVE. REPLACED DISCREPANT PART. 1 G 7 1 3U 3 U H2SW E1GL 1996082200159 19960822 00159 GL 1996 8 22 HEEA967645 2 19960813 A 7230 23051137 SHROUD HOUSING 23033193 BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL COMPRESSOR DISTORTED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8588X CAC91513 51486 CAE895475 COMPRESSOR DISASSEMBLED DUE TO LOW POWER ON TEST CELL (-11.1). UPON INSPECTION OF COMPRESSOR PARTS NOTED THE FOLLOWING: DISTORTED FINISH ON SHROUD HOUSING COATING AS MARKED. (NOTE: ENGINE POWER +1.6 WITH OH REPLACEMENT PART) REPLACED D ISCREPANT PART. 1 G 7 1 3U 3 U H2SW E1GL 1996082200160 19960822 00160 GL 1996 8 22 HEEA967646 2 19960813 A 7250 23051646 SHAFT 23033185 BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL OUTER PT DEFECTIVE E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 2250U CAT70603 45754 CAE860662 RECEIVING INSPECTION REVEALED: PLATING MISSING ON THE OUTER PT SHAFT SEALING SURFACE. REPLACED DISCREPANT PART. 1 G 7 1 3U 3 U H2SW E1GL 1996082200161 19960822 00161 GL 1996 8 22 HEEA967647 2 19960813 A 7240 23056130 LINER 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL COMBUSTION SEC DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7136J CAT23285 S830 CAE836413 ENGINE REMOVED DUE TO TURBINE OVERHAUL. TURBINE DISASSEMBLED DUE TO LOW POWER ON TEST CELL (-1.1). TURBINE PRODUCED (+ 3.2) POWER WITH OVERHAULED REPLACEMENT COMB LINER. REPLACED DISCREPANT PART. 1 G 7 2 3U 3 U H3EU E4CE 1996082200162 19960822 00162 GL 1996 8 22 HEEA967648 2 19960813 A 7250 6888547 INTERNAL SUMP 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL TURBINE LEAKING E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 7136J CAT23285 S830 CAE836413 RECEIVING INSPECTION REVEALED: LEAKING THROUGH INTERNAL SUMP GRAPHITE DURING PRESSURE CHECK. REPLACED DISCREPANT PART. 1 G 7 2 3U 3 U H3EU E4CE 1996082200163 19960822 00163 GL 1996 8 22 HEEA967649 2 19960813 A 7250 6870992 CASE 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL OUTER ASSY DEFECTIVE E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 5421E CAT30372F S806 UPON TURBINE ASSEMBLY NOTED THE FOLLOWING: UNABLE TO FIT AIR TUBE RETAINING RING INTO COMB CASE RING GROOVE. REPLACED D ISCREPANT PART. 1 G 7 2 3U 3 U H3EU E4CE 1996082200167 19960822 00167 GL 1996 8 22 HEEA967654 2 19960815 A 7250 23031938 NOZZLE 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL NR 2 DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 721MB CAT30507F S752 CAE830726 ENGINE REMOVED DUE TO SMOKE ON SHUTDOWN. TURBINE DISASSEMBLED DUE TO LOW POWER ON TEST CELL (-8.4). TURBINE PRODUCED - 0- POWER WITH OVERHAULED REPLACEMENT NOZZLE. REPLACED DISCREPANT PART. 1 G 7 2 3U 3 U H3EU E4CE 1996082200168 19960822 00168 SW 1996 8 22 HEEA967655 1 19960815 A 6220 214010248101 SEAL 214010100207 BELL 214 214ST 1182106 SW M/R DETERIORATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 1624 A529 28106 RUBBER UNBONDED FROM METAL RING. RUBBER BOOT APPEARS TO BE DRY ROTTED. PARTS SCRAPPED LOCALLY. REPLACED WITH SERVICEAB LE PARTS. 2 G 7 2 4U H10SW 1996082200170 19960822 00170 SW 1996 8 22 HEEA967657 1 19960816 A 5302 206032308103S FRAME BELL 206 206L1 1182107 SW TAILBOOM GOUGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2133X 45634 PART IS GOUGED. (TAILBOOM RING HAS GOUGES INNER AREA OF OUTER FLANGE. 1 G 7 1 3U H2SW 1996082200171 19960822 00171 SW 1996 8 22 HEEA967658 1 19960816 A 6220 412010190103 SPINDLE 412010100193 BELL 412 412 1182202 SW M/R HUB UNBONDED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3893P 2977 AAD00032 33012 SPINDLE UNBONDED. 1 G 7 2 4U H4SW 1996082200172 19960822 00172 SW 1996 8 22 HEEA967659 1 19960816 A 6220 412010190103 SPINDLE 412010100193 BELL 412 412 1182202 SW M/R HUB BEARING FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3893P 5288 AAD00032 33012 SPINDLE NEEDS BEARING REPLACEMENT. 1 G 7 2 4U H4SW 1996082200173 19960822 00173 NE 1996 8 22 HEEA967660 1 19960816 A 6210 7615009043054 TIP CAP SKRSKY S76 S76A 8143006 NE M/R BLADE TEAR E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2743E 760155 INSPECTED BOTTOM SIDE ON M/R BLUE BLADE TIP CAP AND FOUND TEAR ON TIP CAP. SUSPECT AIR BUBBLE IN PAINT MATERIAL CAUSING TEAR. AIR BUBBLE IS NOTABLE. 1 G 7 2 3U H1NE 1996082200174 19960822 00174 SW 1996 8 22 HEEA967661 1 19960816 A 7722 206375007103 INDICATOR BELL 206 206L3 1182108 SW COCKPIT TOT STICKS E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 4180F 51469 INDICATOR NEEDLE STICKS AT ZERO AND WON'T INDICATE ON FIRST START. 1 G 7 1 3U H2SW 1996082200175 19960822 00175 1996 8 22 HEEA967662 4 19960816 A 2370 9806019001 CVR BELL 412 412 1182202 SW COCKPIT INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 21498 2914 36003 CVR WILL NOT WORK. 1 G 7 2 4U H4SW 1996082200176 19960822 00176 1996 8 22 HEEA967663 4 19960816 A 3442 MI5853013 INDICATOR P500 BELL 230 230 1182149 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 236X 23015 NO COLOR ON DISPLAY. 1 G 7 2 3U NC H9SW 1996082200177 19960822 00177 SW 1996 8 22 HEEA967664 1 19960816 A 3213 AB205050403031 CROSSTUBE BELL 412 412 1182202 SW CROSSTUBE DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2014K 142 33020 CUT MARKS AROUND MOUNTING PADS. NO DAMAGE ALLOWED IN THIS AREA. 1 G 7 2 4U H4SW 1996082200178 19960822 00178 SW 1996 8 22 HEEA967665 1 19960816 A 3213 206053201103 CROSSTUBE BELL 206 206L3 1182108 SW LT SIDE AFT MIS DRILLED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 108PH 51334 TWO HOLES ON LEFT SIDE AFT ARE MISSED DRILLED. REPLACED WITH SERVICEABLE CROSSTUBE. 1 G 7 1 3U H2SW 1996082200179 19960822 00179 1996 8 22 HEEA967666 4 19960816 A 2312 4000106010 CONTROL UNIT C10 BOLKMS 105 BO105S 5626006 EU COCKPIT VHF DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5031U S678 VOLUME ON RECEIVE IS LOW TO NONE AT ALL. REPLACED BAD PHOTOCELL RT1 AND BAD SWITCH S6. TOUCHED UP FACEPLATE. CLEANED T HUMBWHEEL ASSY WITH ALCOHOL. BENCH CHECK GOOD. 1 G 7 2 3U H3EU 1996082200180 19960822 00180 1996 8 22 HEEA967667 4 19960816 A 2312 4000106010 CONTROL UNIT BOLKMS 105 BO105S 5626006 EU COCKPIT VHF FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 9190Y S669 CONTROL WILL NOT POWER UP. 1 G 7 2 3U H3EU 1996082200181 19960822 00181 1996 8 22 HEEA967668 4 19960816 A 2312 40001452502 TRANSCEIVER RT138F BOLKMS 105 BO105S 5626006 EU COCKPIT INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 137AE S851 TRANSCEIVER INOPERATIVE. (MULTIPLE INTERMITTENT PROBLEMS) 1 G 7 2 3U H3EU 1996082200183 19960822 00183 1996 8 22 HEEA967670 4 19960816 A 3442 MI5851352 TRANSCEIVER P40 SKRSKY S76 S76A 8143006 NE COCKPIT INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1545X 760050 TRANSCEIVER INOPERATIVE AFTER WARM UP. TIME SINCE REPAIR 0:00. 1 G 7 2 3U H1NE 1996082200184 19960822 00184 SW 1996 8 22 HEEA967671 1 19960816 A 5610 206B2003 CHIN BUBBLE BELL 206 206L1 1182107 SW FWD FUSELAGE MIS MFG E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2246Q 45752 POSITIONED NEW CHIN BUBBLE TO AIRCRAFT. FOUND CHIN BUBBLE NOT FORMED CORRECTLY AT AFT OUTBOARD UPPER EDGE OF BUBBLE. 1 G 7 1 3U H2SW 1996082200185 19960822 00185 1996 8 22 HEEA967672 4 19960816 A 3453 27098292 ANTENNA BELL 214 214ST 1182106 SW LORAN DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 8045T 28101 LORAN SHOWS NO SIGNAL FROM THIS ANTENNA. 2 G 7 2 4U H10SW 1996082200186 19960822 00186 SW 1996 8 22 HEEA967673 1 19960816 A 7722 212075067109 INDICATOR BELL 412 412 1182202 SW COCKPIT ITT STICKS E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 33008 36004 ITT INDICATOR NEEDLE STICKS ON ZERO DURING START. 1 G 7 2 4U H4SW 1996082200187 19960822 00187 SW 1996 8 22 HEEA967674 1 19960816 A 7722 212075067109 INDICATOR BELL 412 412 1182202 SW COCKPIT ITT STUCK E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3893P 33012 ITT NEEDLE STUCK ON ZERO, WON'T INDICATE. 1 G 7 2 4U H4SW 1996082200188 19960822 00188 1996 8 22 HEEA967675 4 19960816 A 3416 D120P2T ANEROID BELL 206 206L3 1182108 SW COCKPIT BARO LEAKS E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 6251V 51404 CASE LEAKS 2000 FEET PER MINUTE. 1 G 7 1 3U H2SW 1996082200189 19960822 00189 SW 1996 8 22 HEEA967676 1 19960816 A 2435 230321586 CLAMP BELL 206 206L4 1182110 SW START/GEN FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8094L 52125 DURING VISUAL CHECK OF START/GENERATOR FOUND HEAD OF "T" BOLT BROKEN OFF AND LAYING IN ENGINE PAN. CLAMP HAD REMAINED O N STARTER GEN BUT WAS UNCOUPLED. REPLACED WITH SERVICEABLE CLAMP. 1 G 7 1 3U NC H2SW 1996082200190 19960822 00190 SW 1996 8 22 HEEA967677 1 19960816 A 2730 205001017001 TUBE ASSY BELL 212 212 1181420 SW ELEV LOOSE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5736J 31140 ELEVATOR CONTROL TUBE, ATTACHED BELOW SWASHPLATE, CLEVIS END LOOSE IN TUBE AND WORKING. REPLACED WITH SERVICEABLE TUBE. 1 G 7 1 4U H4SW 1996082200191 19960822 00191 1996 8 22 HEEA967678 4 19960816 A 3453 25410036 7000 RCU BELL 412 412 1182202 SW COCKPIT LORAN DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3893P 33012 LORAN WARNING ADVISORY LIGHT 5 AND DID NOT SELF TEST. 1 G 7 2 4U H4SW 1996082200192 19960822 00192 SW 1996 8 22 HEEA967679 1 19960816 A 7931 212075036101 INDICATOR BELL 412 412 1182202 SW GR BOX OIL PRESS READS LOW E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3893N 33010 GEAR BOX TEMP/ PRESS INDICATES LOW PRESSURE. 1 G 7 2 4U H4SW 1996082200193 19960822 00193 NE 1996 8 22 AWXA960330 2 19960708 A 7200 ENGINE BOEING 737 737277 1384570 NM PWA JT8 JT8D15 52051 NE NR 2 OVERTEMP A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 183AW 43986 2567 22650 P702874B PHX - FLT 1195 - AIR TURNBACK FOR ENGINE NR 2 OVERTEMP. REMOVED AND REPLACED ENGINE NR 2 FOR HIGH EGT. PART TOTAL CY CLES: 33,896. (X) 2 L 7 2 4F 4 F RT A16WE E2EA 1996082200194 19960822 00194 NE 1996 8 22 AWXA960331 2 19960708 A 7200 ENGINE BOEING 737 7372M8 1384483 NM PWA JT8 JT8D9A 52048 NE NR 1 BIRD STRIKE A AWXA C D ABORTED TAKEOFF RETURN TO BLOCK C F.O.D. TO TAKEOFF 1 WP 28 141AW 21955 LAS - FLT 0981 - ABORTED TAKEOFF. BIRD STRIKE ON TAKEOFF ROLL. LEFT HAND FORWARD PART OF A/C. C/W AWA FORM 382 FOD IN SPECTION PARAGRAPH A, SECTIONS 1 AND 2. FOD DID NOT ENTER ENGINE AND NO DAMAGE NOTED. (X) 2 L 7 2 4F 4 F A16WE E2EA 1996082200195 19960822 00195 NM 1996 8 22 AWXA960332 1 19960618 A 5315 FLOOR BEAM BOEING 737 73733A 1384673 NM BS 294 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 PAE - FLT 7827 - DURING ROUTINE SCHEDULED C-12 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM UPPER CHORD AT BS 294, W L 208, RBL 33. REMOVED FLOOR BEAM BS 294, RBL 25-60, WL 208. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 52-10-51. A IRCRAFT TOTAL TIME: 34,246 HOURS. AIRCRAFT TOTAL CYCLES, 20,589. (X) 2 L 7 2 4F RT A16WE 1996082200196 19960822 00196 NM 1996 8 22 AWXA960333 1 19960618 A 5315 FLOOR BEAM BOEING 737 73733A 1384673 NM BS 312 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 PAE - FLT 7827 - DURING ROUTINE SCHEDULED C-12 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM UPPER CHORD AT BS 312, W L 208, LBL 16. REPAIRED FLOOR BEAM AT BS 312, WL 208, LBL 16 - RBL 60 BY REPLACING UPPER TEE CHORD IAW SRM 53-10-51. A IRCRAFT TOTAL TIME, 34,246 HOURS. AIRCRAFT TOTAL CYCLES, 20,589. (X) 2 L 7 2 4F RT A16WE 1996082200197 19960822 00197 NM 1996 8 22 AWXA960335 1 19960620 A 5330 SKIN BOEING 737 73733A 1384673 NM BS 339 DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 PAE - FLT 7827 - DURING ROUTINE SCHEDULED C-12 MAINTENANCE CHECK, FOUND DENT AT BS 339 BETWEEN STR 23R AND STR 24R. REM OVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 53-00-01. AIRCRAFT TOTAL TIME, 34,246 HOURS. AIRCRAFT TOT AL CYCLES, 20,589. (X) 2 L 7 2 4F RT A16WE 1996082200198 19960822 00198 EU 1996 8 22 AWXA960341 1 19960712 A 3520 AJ5L3425 CONTAINER ASSY AIRBUS 320 A320231 3930325 EU CABIN FAILED A AWXA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 28 632AW 00432 81 CMH/EWR - FLT 2686 - AIR TURNBACK. LOSS OF CABIN PRESSURE, OXYGEN MASKS DID NOT DEPLOY AT ROW 8, A, B, AND C. REMOVED AND REPLACED ROW 8, A, B, AND C OVERHEAD OXYGEN MASK ASSEMBLY IAW 35-42-41. (X) 2 L 7 2 4F RT A28NM 1996082200199 19960822 00199 NM 1996 8 22 AWXA960343 1 19960706 A 5315 FLOOR BEAM BOEING 737 7373G7 1384595 NM BS 328 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 PAE - FLT 7803 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND FLOOR BEAM CORRODED AT BS 328, RBL 18, WL 208. F ABRICATED REPAIR PARTS, ALODINED AND PRIMED PER SRM 53-10-51. AIRCRAFT TOTAL TIME: 29,886 HOURS. AIRCRAFT TOTAL CYCLE S, 23,179. (X) 2 L 7 2 4F RT A16WE 1996082200200 19960822 00200 NM 1996 8 22 AWXA960344 1 19960706 A 5315 FLOOR BEAM BOEING 737 7373G7 1384595 NM BS 294.5 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 PAE - FLT 7803 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND BEAM CORRODED AT BS 294.5, RBL 12, WL 208. REMOV ED, FABRICATED AND REPLACED FLOOR BEAM PER SRM 53-10-51. AIRCRAFT TOTAL TIME, 29,886 HRS. AIRCRAFT TOTAL CYCLES, 23,17 9. (X) 2 L 7 2 4F RT A16WE 1996082200201 19960822 00201 NM 1996 8 22 AWXA960345 1 19960709 A 5330 SKIN BOEING 737 7373G7 1384595 NM BS 450 DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 PAE - FLT 7803 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND DENT IN SKIN AT BS 450 BETWEEN STR 27 AND STR 26 RT. REPAIRED IAW 53-00-01. AIRCRAFT TT, 29,886 HOURS. AIRCRAFT TC: 23,179. (X) 2 L 7 2 4F RT A16WE 1996082200202 19960822 00202 NM 1996 8 22 AWXA960346 1 19960708 A 5315 FLORO BEAM BOEING 737 7373G7 1384595 NM BS 312 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 PAE - FLT 7803 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND FLOOR BEAM CORRODED AT BS 312, LBL ZERO - RBL 12, WL 208. REMOVED DAMAGED PART AND INSTALLED FABRICATED FLOOR BEAM AT BS 312, WL 208, LBL 21 - RBL 21 PER SRM 53-10-51. AIRCRAFT TOTAL TIME, 29,886 HOURS. AIRCRAFT TOTAL CYCLES, 23, 179. (X) 2 L 7 2 4F RT A16WE 1996082200203 19960822 00203 NM 1996 8 22 AWXA960347 1 19960706 A 5315 FLOOR BEAM BOEING 737 7373G7 1384595 NM BS 344 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 PAE - FLT 7803 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND FLOOR BEAM CORRODED AT BS 344, LBL 26, WL 208. F ABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR PARTS PER SRM 53-10-51. ACFT TT: 29,886 HOURS. ACFT TC: 23,719. (X ) 2 L 7 2 4F RT A16WE 1996082200204 19960822 00204 NM 1996 8 22 AWXA960348 1 19960706 A 5315 FLOOR BEAM BOEING 737 7373G7 1384595 NM BS 312 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 155AW 23777 PAE - FLT 7803 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND FLOOR BEAM CORRODED AT BS 312, BL ZERO, RBL 12, W L 208. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-51. AIRCRAFT TOTAL TIME 29,886. AIRCRAFT TC 23,179. (X) 2 L 7 2 4F RT A16WE 1996082200205 19960822 00205 WP 1996 8 22 RRXA9605 1 19960730 A 2910 O-RINGS DOUG DC8 DC871 302199A WP HYD FITTING FAILED A RRXA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 WP 15 811AL 46099 KONT/KDAY - FLT 023 - EN ROUTE, MAIN HYDRAULIC QUANTITY DROPPED TO STANDPIPE LEVEL APPROXIMATELY 4.8 GALLONS. MAINTENAN CE FOUND FITTING ON LINE GOING TO AILERON SHUT-OFF VALVE LEAKING. INSTALLED NEW O-RING, OPS CHECK AND LEAK CHECK GOOD. (X) 2 L 7 4 4F 4A25 1996082200206 19960822 00206 SO 1996 8 22 RAAAE896022 1 19960711 A 3350 8621014 BATTERY PACK 873100212 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 AFT PASSENGER CABIN EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE . (X) 2 L 7 4 4T 4A22 1996082200207 19960822 00207 SO 1996 8 22 RAAAE996007 1 19960701 A 3350 8621014 BATTERY PACK 873100112 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 FORWARD AFT CABIN ENTRY DOOR EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. (X) 2 L 7 4 4T 4A22 1996082200208 19960822 00208 SO 1996 8 22 RAAAE996008 1 19960701 A 3350 8612006 BATTERY PACK 873100112 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 EGRESS FLOOR PROXIMITY LIGHT PASSENGER ROW 17 FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. (X) 2 L 7 4 4T 4A22 1996082200209 19960822 00209 NM 1996 8 22 RAAAB296031 1 19960701 A 3350 86210144 BATTERY PACK 873100112 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 RIGHT AFT OVERWING EXIT EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. (X) 2 L 7 3 4F A3WE 1996082200210 19960822 00210 WP 1996 8 22 RAAA496007 1 19960711 A 3350 S103 BATTERIES GRIMES 1000553 LKHEED 188 188A 5262602 WP CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 9744C 188A1140 RIGHT OVERWING EMERGENCY EXIT PULL DOWN EMERGENCY LIGHT FAILED SERVICE TEST. (X) 2 L 7 4 4T RT 4A22 1996082200211 19960822 00211 WP 1996 8 22 RAAAE496006 1 19960708 A 3350 1000553 LIGHT LKHEED 188 188A 5262602 WP CABIN FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 9744C 188A1140 RIGHT AFT EMERGENCY EXIT DOOR EMERGENCY LIGHT FAILED SERVICE CHECK. CHANGED LIGHT ASSEMBLY. (X) 2 L 7 4 4T RT 4A22 1996082200212 19960822 00212 NM 1996 8 22 TWRA96193 1 19960717 A 3350 S1356B37 LIGHT BOEING 747 747136 1384883 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 606FF 7225271 20273 DURING DAILY CHECK, FOUND EMERGENCY CEILING LIGHT INOPERATIVE ABOVE SEAT 36 HJK. REPLACED LIGHT ASSY. OPS CHK OK PER M M 33-51-00. (X) 2 L 7 4 4F A20WE 1996082200213 19960822 00213 NM 1996 8 22 TWRA96195 1 19960721 A 3350 ML1755 BULB BOEING 747 747212B 1384886 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND EVAC FLOOR LIGHT AT SEAT 18H, 40H, AND 50H INOPERATIVE. REPLACED BULB. OPS CHK OK PER MM 33- 51-00. (X) 2 L 7 4 4F A20WE 1996082200214 19960822 00214 NM 1996 8 22 TWRA96196 1 19960722 A 3350 07912 LENS BOEING 747 747212B 1384886 NM CABIN MISSING A TWRA K NONE O OTHER IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND EVAC LIGHT INOPERATIVE SEATS 28C, 53C, AND 58C. REPLACED LENS AND LIGHT BULB. OPS CHECK OK P ER MM 33-51-00. REFERENCE: OPERATOR CONTROL NR 96ZZZX4040. (X) 2 L 7 4 4F A20WE 1996082200215 19960822 00215 NM 1996 8 22 96ZZZX4040 1 19960722 A 3350 ML1755 BULB BOEING 747 747212B 1384886 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND EVAC LIGHT INOPERATIVE SEAT 28C, 53C, AND 58C. REPLACED LENS AND LIGHT BULB. OPS CHECK OK PE R MM 33-51-00. REFERENCE: OPERATOR CONTROL NR TWRA96196. 2 L 7 4 4F A20WE 1996082200216 19960822 00216 NM 1996 8 22 TWRA96197 1 19960719 A 3350 1317 BULB BOEING 747 747238B 1384828 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 607PE 20011 DURING DAILY CHECK, FOUND EVAC LIGHT EXTERIOR LEFT SIDE INOPERATIVE. RELAMPED. OPS CHECK OK PER MM 33-51-00. (X) 2 L 7 4 4F A20WE 1996082200217 19960822 00217 NM 1996 8 22 TWRA96198 1 19960720 A 3350 A3060698101 CONNECTOR BOEING 747 747282B 1384860 NM CABIN DEFECTIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 611FF 20502 DURING DAILY CHECK, FOUND ENTIRE U/D EVAC LIGHT INOPERATIVE. FOUND BAD CONNECTOR FOR FEEDER. REPLACED CONNECTOR. EMER GENCY LIGHT OPS CHECK NORMAL PER MM 33-51-00. (X) 2 L 7 4 4F A20WE 1996082200218 19960822 00218 NM 1996 8 22 TWRA96200 1 19960721 A 3350 PLUG BOEING 747 747136 1384883 NM CABIN LOOSE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 606FF 20273 DURING DAILY CHECK, FOUND STAIRCASE EVAC INOPERATIVE. REPAIRED LOOSE CONNECTION ON STAIRCASE PLUG. OPS CHECK NORMAL PE R MM 33-51-00. (X) 2 L 7 4 4F A20WE 1996082200219 19960822 00219 NM 1996 8 22 TWRA96201 1 19960720 A 3350 CONNECTOR BOEING 747 747282B 1384860 NM CABIN LOOSE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 611FF 20502 DURING DAILY CHECK, FOUND RIGHT AISLE WITH NO EVAC LIGHTS FROM 22 KJA THROUGH 26 KJH. FOUND LOOSE CONNECTOR. TIGHTEN C ONNECTOR. LIGHT OPS CHECK OK PER MM 33-51-00. (X) 2 L 7 4 4F A20WE 1996082200221 19960822 00221 NE 1996 8 22 96ZZZX4043 2 19960701 A 7260 230307203 SEAL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE CSD LIP LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 911BY 726 7127 LE45038E CSD LIP SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1996082200222 19960822 00222 NE 1996 8 22 96ZZZX4044 2 19960701 A 7260 430101501 SEAL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE GOVERNOR LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 911BY 726 7127 LE45038E GOVERNOR/STARTER/FCU SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH 4 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1996082200223 19960822 00223 NE 1996 8 22 96ZZZX4045 2 19960701 A 7260 430101301 SEAL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE ALTERNATOR LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 911BY 726 7127 LE45038E ALTERNATOR AFT SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1996082200224 19960822 00224 NE 1996 8 22 96ZZZX4046 2 19960701 A 7260 430101201 SEAL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE ALTERNATOR LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 911BY 726 7127 LE45038E ALTERNATOR FORWARD SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1996082200225 19960822 00225 NE 1996 8 22 96ZZZX4047 2 19960701 A 7250 414144001 BEARING BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE RT ENG NR 2 FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911BY 726 31069 7127 LE45038E BEARING HAS EXCESSIVE SCORING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1996082200226 19960822 00226 NE 1996 8 22 96ZZZX4048 2 19960701 A 7230 4101000641 ROTOR BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE COMPRESSOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911BY 726 104663 7127 LE45038E COMPRESSOR AXIAL ROTOR WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. PART TOTAL CYCLES, 1 04,663. 1 G 7 2 3U 3 U H13EU E5NE 1996082200227 19960822 00227 EU 1996 8 22 96ZZZX4049 1 19960701 A 2430 WIRE BOLKMS 105 BO105CBS 5626008 EU GENERATOR DETACHED A R7MA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 11 105NC 790 SMOKE IN CABIN. WIRE CAME LOOSE ON GENERATOR CAUSING AN OVER VOLTAGE TAKING OUT REGULATOR, DC, AND COMM NR 1 RADIO WHIC H CAUSED THE SMOKE AND SMELL. WIRE WAS REPAIRED, REPLACED REGULATOR, DG, AND COMM NR 1 RADIO. PROBLEM CORRECTED. 1 G 7 2 3U NC H3EU 1996082200228 19960822 00228 NM 1996 8 22 TWRA9677 1 19960628 A 3350 900835A BATTERY PACK BOEING 747 747121 1384871 NM CABIN DISCHARGED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 609FF 20354 DURING DAILY SERVICE, FOUND OVERHEAD 'EVAC' LIGHTS IN AREA OF SEAT ROW 32K AND EMERGENCY EXIT SIGN INOPERATIVE. REPLACE D BATTERY PACK, OPS CHECK OK. MM 33-51-00. (X) 2 L 7 4 4F A20WE 1996082200329 19960822 00329 NM 1996 8 22 CALA9601188 1 19960819 A 2913 6500103 HYD PUMP BOEING 737 737217 1384464 NM NR 2 ENGINE LEAKING A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 16232 5104 3643 19886 THE A-SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO FOLLOWED BY LOSS OF PRESSURE ON NR 2 ENGINE WHILE EN ROUTE. AIRCRAFT W AS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP LEAKING. T HE PUMP WAS REMOVED AND REPLACED, THE HYDRAULIC RESERVOIR WAS SERVICED, THE ENGINE WAS RUN AND ALL OPERATION AND LEAK CH ECKS WERE GOOD. 2 L 7 2 4F A16WE 1996082200330 19960822 00330 NE 1996 8 22 CALA9601189 2 19960817 A 7250 775404 T4 BLADE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 1 ENGINE BROKEN A CALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 09 10801 26187 10702 49127 717364 THE NR 1 ENGINE FAILED WHILE EN ROUTE. THE AIRCRAFT WAS RETURNED TO LAS WHERE IT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS TAKEN OUT OF SERVICE FOR ENGINE REPLACEMENT. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION. *S/D* SHOP FINDINGS REVEALED A BROKEN T-4 BLADE. 2 L 7 2 4F 4 F A6WE E9NE 1996082200331 19960822 00331 WP 1996 8 22 9617849909 1 19960723 A 5312 BULKHEAD DOUG DC9 DC931 3022065 WP AFT PRESS BLKHD CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 959N 47255 DURING M-CHECK, FOUND A 1.1 INCH CRACK IN THE AFT PRESSURE BULKHEAD UPPER INBOARD CORNER IN THE 9 DOUBLER. ALSO, FOUND A 4 INCH CRACK IN THE RIGHT SIDE VENTRAL DOOR JAMB. REPAIRED BOTH PER EA DC9-53-022. 2 L 7 2 4F A6WE 1996082200332 19960822 00332 WP 1996 8 22 9617859984 1 19960808 A 5320 PRESS WEB DOUG DC9 DC932 3022066 WP BS 105 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 984US 47383 DURING H-CHECK, FOUND CRACKS IN THE NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE WEB FS 105 AT LBL 25 AND RBL 25 AT THE INBOARD AND OUTBOARD VERTICAL SUPPORT FITTINGS. REPAIRED WEB (P/N 9910073-313) PER EA 99-110720. 2 L 7 2 4F A6WE 1996082200333 19960822 00333 WP 1996 8 22 9617869984 1 19960812 A 5312 BULKHEAD CAP DOUG DC9 DC932 3022066 WP BS 598 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 984US 47383 DURING H-CHECK, FOUND CORROSION IN THE FS 598 BULKHEAD T-CAP FROM LONGERON 28L TO 28R. REPAIRED CAP (P/N 5914865-29) PE R EA 99-110725. 2 L 7 2 4F A6WE 1996082200334 19960822 00334 WP 1996 8 22 9617879984 1 19960812 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 676-685 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 984US 47383 DURING H-CHECK, FOUND CORROSION ON LONGERON 29L FROM FS 676 TO 685. REPAIRED LONGERON (P/N 5911418-99) PER EA 99-110723 . 2 L 7 2 4F A6WE 1996082200335 19960822 00335 WP 1996 8 22 9617889984 1 19960812 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 690 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 984US 47383 DURING H-CHECK, FOUND CORROSION ON THE KEEL CENTER SECTION (LONGERON 29R) AT FS 690. REPAIRED KEEL (P/N 5911418-101) PE R EA 99-110728. 2 L 7 2 4F A6WE 1996082200336 19960822 00336 WP 1996 8 22 9617899138 1 19960813 A 5210 FITTINGS DOUG DC9 DC915 3022036 WP AFT ENTRY DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9348 45787 DURING H-CHECK, FOUND CRACKS IN THE AFT ENTRY DOOR NR 3 BEAM UPPER AND LOWER END FITTINGS. REPLACED FITTINGS. 2 L 7 2 4F A6WE 1996082200337 19960822 00337 WP 1996 8 22 9617901151 1 19960813 A 5730 SKIN DOUG DC10 DC1040 3023508 WP WS 610 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 151US 46760 DURING T-CHECK, FOUND A CRACK IN THE RIGHT WING FIXED LEADING EDGE SKIN AT XOS 610. REPAIRED SKIN (P/N ARB2887-501) P ER EA 11-106298. 2 L 7 3 4F A22WE 1996082200338 19960822 00338 NM 1996 8 22 9617912715 1 19960813 A 5744 FITTING BOEING 727 7272S7 138407Z NM LT TE FLAP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 719RC 22490 DURING H-CHECK, FOUND CORROSION ON THE LEFT WING INBAORD FLAP NR 3 FLAP CARRIAGE BEARING SUPPORT FITTING. REPLACED FI TTING PER SRM 51-10-01. 2 L 7 3 4F A3WE 1996082200339 19960822 00339 WP 1996 8 22 9617921151 1 19960814 A 5330 SKIN DOUG DC10 DC1040 3023508 WP BS 1509-1531 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 151US 46760 DURING T-CHECK, FOUND CORROSION ON THE UNDER WING BARREL SKIN FROM FS 1509 TO 1531, LONGERONS 49L TO 49R AND ON THE BULK HEAD T-ANGLE. REPAIRED THE SKIN (P/N AYB7065-1) AND T-ANGLE (P/N AEA7079-1) PER EA 11-106295. 2 L 7 3 4F A22WE 1996082200340 19960822 00340 WP 1996 8 22 9617939863 1 19960815 A 5320 FITTING DOUG DC9 DC951 3022051 WP BS 1167 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 772NC 47774 DURING H-CHECK, FOUND A CRACK IN THE FS 1167 INTERCOSTAL END FITTING BETWEEN LONGERONS 27L TO 28L. REPAIRED PER SRM 51- 30-5. 2 L 7 2 4F A6WE 1996082200341 19960822 00341 1996 8 22 9618069759 4 19960816 A 3442 RADAR ANTENNA DOUG DC9 DC941 302207N WP FWD FUSELAGE OUT OF ADJUST A NWAA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 01 759NW 47287 DURING CRUISE, WEATHER RADAR IMAGES CELLS THAT MOVE 20 TO 30 MILES AFTER EACH SWEEP DUE TO EN ROUTE WEATHER. FLIGHT RET URNED TO DTW AND LANDED WITHOUT INCIDENT. TESTED THE RADAR TRANSCEIVER PER 34-41-4. ADJUSTED ANTENNA/TRANSCEIVER SYNC HRONIZATION, OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996082200342 19960822 00342 1996 8 22 9618073225 4 19960815 A 3442 RADAR TR UNIT AIRBUS 320 A320211 3930320 EU FWD FUSELAGE INOPERATIVE A NWAA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 01 325US 281 DURING CRUISE WHILE APPROACHING THUNDERSTORM CELLS AT APPROXIMATELY 50 MILES, THE WEATHER RADAR DID NOT PAINT. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE WEATHER RADAR TRANSCEIVER, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996082200343 19960822 00343 NM 1996 8 22 9618086718 1 19960818 A 3230 DNLOCK ACTUATOR BOEING 747 747251B 1384892 NM RT MLG FAILED A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 618US 21122 DURING APPROACH, THE RIGHT WING LANDING GEAR WOULD NOT EXTEND DURING LANDING GEAR EXTENSION. RECYCLED LANDING GEAR AND LANDING GEAR EXTENDED. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE RIGHT WING GEAR DOWNLOCK ACTUATOR, OPERATIONAL C HECK GOOD. 2 L 7 4 4F A20WE 1996082200344 19960822 00344 NM 1996 8 22 9617986310 1 19960819 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 670US 24225 DURING LINE CHECK, FOUND TWO RIGHT AFT EXTERIOR FUSELAGE EMERGENCY LIGHTS INOPERATIVE. REPELACED BATTERY PACK, OPERATIO NAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1996082200345 19960822 00345 1996 8 22 COMA9660133 4 19960817 A 2210 6229968001 YAW DAMPER CNDAIR CL600 CL6002B19 EA NR 1 INOPERATIVE A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 956CA 7105 YAW DAMPER NR 1 INOP MESSAGE ON EICAS DURING TAXI. REPLACED THE NR 1 YAW DAMPER. 2 L 7 2 4F RT A21EA 1996082200346 19960822 00346 EU 1996 8 22 WWMA9600061 1 19960811 A 2611 721112110 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT DEFECTIVE A WWMA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 WP 15 354SB 340B354 THE CARGO SMOKE LIGHT ILLUMINATED IN FLIGHT, THE NR 1 CARGO EXTINGUISHER FIRE BOTTLE WAS FIRED. EMERGENCY GROUND EVACUA TION WAS CONDUCTED INCLUDING PULLING BOTH FIRE HANDLES AND FIRING BOTH ENGINE FIRE BOTTLES. MAINTENANCE REPLACED BOTH C ARGO SMOKE DETECTORS AND ALL BLOWN FIRE BOTTLES. 2 L 7 2 4T RT A52EU 1996082200347 19960822 00347 EU 1996 8 22 WWMA9600067 1 19960812 A 2611 MS90311271 TEST SWITCH SAAB SF340 340B 7860101 EU COCKPIT SHORTED A WWMA F ACTIVATE FIRE EXT. N FALSE WARNING NR NOT REPORTED 1 WP 15 354SB 340B354 THE CARGO SMOKE LIGHT ILLUMINATED, THE CREW DISCHARGED THE NR 1 CARGO BOTTLE. MAINTENANCE FOUND A SHORT ON SMOKE PANEL TEST SWITCH 15WK. REPLACED SWITCH AND RIGHT FIRE BOTTLE, RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 1996082200348 19960822 00348 EU 1996 8 22 QXEA9600333 1 19960819 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 32-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 CLIP CRACKED AT FRAME 32-2 AND STRINGER 23, TWO CRACKS NOTED. CRACKS NOTED DURING C-CHECK (NR400-93). CRACK REPAIRED I /A/W SRM 530213. 2 L 7 2 4F RT A20EU 1996082200349 19960822 00349 EU 1996 8 22 QXEA9600334 1 19960819 A 5533 WEB FOKKER F28 F28MK4000 4990810 EU BS 23570 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 TWO INCH CRACK NOTED IN THE INNER WEB FLANGE, FORWARD SECTION OF THE RIGHT HAND SIDE OF THE BULLET FAIRING. CRACK NOTED DURING C-CHECK (NR400-99), CRACK REPAIRED IAW EA 4-55-13. 2 L 7 2 4F RT A20EU 1996082200350 19960822 00350 EU 1996 8 22 QXEA9600335 1 19960819 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 50-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 CRACKED CLIP AT FRAME 50-2 FROM STRINGER 53 TO 51, CRACK HAD PROGRESSED BEYOND 2ND STOP DRILL. CRACK NOTED DURING C-CHE CK (NR400-101), REPAIRED IAW SRM 530213. 2 L 7 2 4F RT A20EU 1996082200351 19960822 00351 EU 1996 8 22 QXEA9600336 1 19960819 A 3350 MGG1280 BULBS FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 454US 11107 AFT EXIT SIGN HAS SEVERAL BULBS INOP. BULBS WERE REPLACED AND SIGN OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996082200352 19960822 00352 EU 1996 8 22 QXEA9600337 1 19960819 A 3350 1820 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU GALLEY FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 466US 11075 EMERGENCY LIGHT NEAR FORWARD SERVICE/EMERGENCY DOOR IS INOP. BULBS WERE REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996082200353 19960822 00353 EU 1996 8 22 QXEA9600338 1 19960819 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 A 1 INCH CRACK IN LEFT WING TRAILING EDGE SKIN NEXT TO SHROUD DOOR 81L FORWARD MOUNT FOR SPRING BOX BRACKET. CRACK NOTE D DURING C-CHECK (NR810-13), REPAIRED IAW EA 4-57-12. 2 L 7 2 4F RT A20EU 1996082200354 19960822 00354 NM 1996 8 22 96FDEA01385 1 19960819 A 5320 66126391 ANGLE BOEING 727 72722 1384002 NM BS 961 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 NR0698 AND 029, CORROSION ON KEEL BEAM SUPPORT ANGLE AT BS 950 LBL TO RBL 5 WL 138. 2 L 7 3 4F A3WE 1996082200355 19960822 00355 NE 1996 8 22 96FDEA01386 2 19960817 A 7200 ENGINE BOEING 727 727227 1384078 NM PWA JT8 JT8D17 52049 NE NR 1 ENGINE DAMAGED A FDEA C D E ABORTED TAKEOFF RETURN TO BLOCK ENGINE SHUTDOWN E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 25 480FE 21462 ADVANCED POWER FOR TAKEOFF AND HAD LARGE AIRFRAME VIBRATION. THROTTLES RETARDED AND TAKEOFF ABORTED. EPR MADE IT AS FA R AS 1.3, BUT NOT UP TO 1.4. SUBSEQUENT POST FLIGHT INSPECTION REVEALED DAMAGE TO THE NUMBER ONE ENGINE. REMOVED AND R EPLACED THE NUMBER ONE ENGINE PER WORK CARD 70T0001, 70T0003 AND 70T0301. OPERATIONS AND LEAK CHECK GOOD ON GROUND RUNS . REQUIRED INSPECTION ITEMS HAVE BEEN COMPLIED WITH. 2 L 7 3 4F 4 F A3WE E2EA 1996082200356 19960822 00356 WP 1996 8 22 ABXA9600611 1 19960818 A 2910 O-RING DOUG DC8 DC861 3021952 WP NR 3 HYD SYST CUT A ABXA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 23 845AX 46157 LOST HYDRAULIC QUANTITY DOWN TO THE N, RAN HYDRAULIC PRESS/LOSS CHECKLIST. THE QUANTITY STAYED AT THE N. VISUALLY INSP ECTED AIRCRAFT, NO LEAKS NOTED. SERVICED HYDRAULIC SYSTEM, RAN NR 2 AND NR 3 ENGINES, CYCLED ALL SYSTEMS, FOUND NR 3 E NGINE HYDRAULIC PUMP PRESSURE LINE UNION LEAKING AT PUMP. REPLACED O-RING AND LEAK CHECKED GOOD IAW DC-8 MM 29-10-1. 2 L 7 4 4F 4A25 1996082200357 19960822 00357 WP 1996 8 22 ABXA9600612 1 19960818 A 2720 57155A RUDDER PUMP DOUG DC8 DC861 3021952 WP RUDDER LEAKING A A ABXA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 23 845AX 46157 ONE HOUR INTO FLIGHT NOTICED HYDRAULIC QUANTITY SLOWLY DECREASING. MARKED GAUGE AND CONTINUED TO DECREASE VERY SLOWLY. APPROXIMATELY ONE NEEDLE WIDTH ABOVE STANDPIPE PERFORMED HYDRAULIC FLUID LOSS CHECKLIST. ONCE HYDRAULICS DEPRESSURIZED AND ISOLATED, QUANTITY STABILIZED. ON DESCENT AT FL 180 REPOWERED HYDRAULICS AND QUANTITY DECREASED TO STANDPIPE. PER FORMED ABNORMAL CHECKLIST, QUANTITY AT STANDPIPE, PRESSURE AT 3,000 PSI QUANTITY REMAINED AT STANDPIPE FOR LANDING AND TAXI IN. FOUND STANDBY RUDDER PUMP TO BE LEAKING AT CASE DRAIN. REPLACED STANDBY RUDDER PUMP IAW DC-8 MM CHAPTER 29. S ERVICED MAIN HYDRAULIC SYSTEM, PERFORMED OPERATIONAL CHECK OF ALL SYSTEMS. HYDRAULIC SYSTEM WORKING NORMAL. 2 L 7 4 4F 4A25 1996082200358 19960822 00358 WP 1996 8 22 DLL15961870 1 19960811 A 3350 TRACK LKHEED 1011 10113853 5265020 WP CABIN DAMAGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 756DR 193Y1185 SECTION OF EMERGENCY LIGHT TRACK INOP RT SIDE MID CABIN. FOUND WIRE BROKEN. REPAIRED WIRE, CHECKS GOOD. 2 L 7 3 4F A23WE 1996082200359 19960822 00359 NM 1996 8 22 DL757961871 1 19960811 A 3350 20131A BATTERY PACK BOEING 757 757232 1384965 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 630DL 22920 ON L/O, FOUND 1ST CLASS EMERGENCY PATH LIGHTS INOP. REPLACED BATT PACK, CHECKS GOOD. 2 L 7 2 4F RT A2NM 1996082200360 19960822 00360 WP 1996 8 22 DLL10961872 1 19960811 A 3350 5165741 POWER SUPPLY LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 714DA 193C1090 R3 EMERGENCY LIGHT INOP. REPLACED PWR SUPPLY, CHECKS GOOD. 2 L 7 3 4F A23WE 1996082200361 19960822 00361 WP 1996 8 22 DLL15961873 1 19960811 A 3350 0L3071BPEGPL BULB LKHEED 1011 10113853 5265020 WP CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 754DL 193Y1181 AFT SECTION E PASS LIGHTS ARE INOP. RELAMPED 2 AFT LIGHTS, CKS GOOD. 2 L 7 3 4F A23WE 1996082200362 19960822 00362 WP 1996 8 22 DLL13961876 1 19960809 A 5312 BULKHEAD WEB LKHEED 1011 10113851 5265010 WP BS 449 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 787DL 193A1126 DURING LTR CHECK, THE 449 BLKHD AT RBL 10 WAS FOUND TO BE CRACKED. THE BLKHD WEB WAS CUTOUT AND A NEW SECTION WAS SPLIC ED IN. 2 L 7 3 4F A23WE 1996082200363 19960822 00363 WP 1996 8 22 DLL10961877 1 19960711 A 5320 CAP FITTING LKHEED 1011 10113851 5265010 WP BS 901 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 727DA 193C1167 DURING HMV, THE LOWER DOOR SILL AT FS 901 INBD CAP FITTINGS WERE FOUND TO BE CORRODED. THE DAMAGED FITTING WAS REMOVED AND REPLACED. 2 L 7 3 4F A23WE 1996082200364 19960822 00364 WP 1996 8 22 DLL10961878 1 19960711 A 5711 SPAR CAP LKHEED 1011 10113851 5265010 WP WS 1163 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 727DA 193C1167 DURING HMV, THE INTERMEDIATE SPAR UPPER CAP AT WS 1163 WAS FOUND IN NEED OF REPAIR. THE DAMAGE WAS REMOVED AND A NEW PA RT WAS SPLICED IN. 2 L 7 3 4F A23WE 1996082200365 19960822 00365 WP 1996 8 22 DLL10961879 1 19960702 A 5312 BULKHEAD WEB LKHEED 1011 10113851 5265010 WP BS 449 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 729DA 193C1180 DURING HMV, THE FS 449 BLKHD WAS FOUND CRACKED. THE BLKH WEB WAS CUTOUT AND A NEW SECTION WAS SPLICED IN. 2 L 7 3 4F A23WE 1996082200366 19960822 00366 WP 1996 8 22 DLL10961880 1 19960731 A 5330 SKIN LKHEED 1011 10113851 5265010 WP BS 819 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 728DA 193C1173 DURING LTR CHK, THE FUSELAGE SKIN AT FS 819, BL 0 WAS FOUND CORRODED. THE DAMAGED SKIN WAS CUT OUT AND A FILLER/DOUBLER REPAIR WAS INSTALLED. 2 L 7 3 4F A23WE 1996082200367 19960822 00367 WP 1996 8 22 DLL13961881 1 19960702 A 5312 BULKHEAD LKHEED 1011 10113851 5265010 WP BS 1809 BUCKLED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 789DL 193A1142 DURING LTR CHK, THE AFT PRESSURE BLKH AT FS 1809 WAS FOUND TO BE BUCKLED. THE DAMAGED SECTION WAS CUT OUT AND A NEW PAR T WAS SPLICED IN. 2 L 7 3 4F A23WE 1996082200368 19960822 00368 WP 1996 8 22 DLL10961882 1 19960712 A 5320 PRESSURE DECK LKHEED 1011 10113851 5265010 WP BS 378-385 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 727DA 193C1167 DURING HMV, THE HORIZONTAL PRESSURE DECK AT FS 378 TO 385 WAS FOUND TO BE CRACKED. THE DAMAGE WAS CUT OUT AND A FILLER/ DOUBLER REPAIR WAS INSTALLED. 2 L 7 3 4F A23WE 1996082200369 19960822 00369 WP 1996 8 22 DLL10961887 1 19960731 A 5743 RIB LKHEED 1011 10113851 5265010 WP RT MLG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 727DA 193C1167 THE RT MLG ATTACH RIB WAS FOUND CORRODED ON THE AFT OUTBOARD FLANGE. THE CORRODED AREA IS LOCATED UNDER THE AFT LOWER L UG BACKUP CHANNEL. THE CORROSION WILL BE REMOVED AND THE THE RIB WILL BE REWORKED. 2 L 7 3 4F A23WE 1996082200370 19960822 00370 WP 1996 8 22 DLL10961888 1 19960731 A 5712 RIB CAP LKHEED 1011 10113851 5265010 WP WS 555 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 715DA 193C1092 DURING THE ACCOMPLISHMENT OF SI 7-59208-12AD ON THE RT WING, CRACKS WERE FOUND ON THREE UPPER RIB CAP CASTELATIONS. THE CRACKS WILL BE TREATED TEMPORARILY AND PERMANENT REPAIR WILL BE ACOMPLISHED AT THE NEXT HMV LIMIT. 2 L 7 3 4F A23WE 1996082200371 19960822 00371 NM 1996 8 22 DLM11961890 1 19960813 A 3350 BATTERIES 61020 DOUG MD11 MD11 3023602 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 802DE NONE 48473 FLASHLIGHT AT L2 INB SEAL BROKEN RED DIODE NOT FLASHING. REPLACED BATTERY AND INSTALLED NEW SEAL. 2 L 7 3 4F RT A22WE 1996082200372 19960822 00372 NM 1996 8 22 DL757961895 1 19960813 A 5754 114N4005157 TE WEDGE BOEING 757 757232 1384965 NM NR 4 LE SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 644DL 23998 T/E WEDGE HAD SEVERAL DELAMINATED AREAS. REPLACED DAMAGED WEDGE PER SRM 57-43-02, FIGURE 2. 2 L 7 2 4F RT A2NM 1996082200373 19960822 00373 NE 1996 8 22 DLM88961897 2 19960813 A 7230 COMP BLADE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE DAMAGED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 917DL 725944 49573 725944 FLT ATTN IN AFT OF ACFT REPORTED LOUD EXCESSIVE NOISE FROM ENGINES. PERFORMED BORESCOPE ON NR 1 ENGINE 6TH AND 7TH STAG E COMPRESSOR DUE TO N1 FAN BLADE DAMAGE FOUND. DAMAGE TO 7TH STAGE OUT OF M/M LIMITS. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A6WE E9NE 1996082200374 19960822 00374 WP 1996 8 22 DLL10961899 1 19960814 A 3350 5165741 POWER SUPPLY LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1734D 193C1225 CABIN EMERGENCY EXIT SIGNS AT 2L AND LT CLASS DIVIDER INOP. REPLACED PWR SUPPLY, TESTS OK. 2 L 7 3 4F A23WE 1996082200375 19960822 00375 NM 1996 8 22 DL767961900 1 19960814 A 3350 333780100 BATTERY PACK BOEING 767 767232 1385132 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 103DA 22215 FOUND ON L/O, AFT THREE EXTERIOR EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY M738 AND BATTERY PACK, LIGHT OPS NORMAL. 2 L 7 2 4F RT A1NM 1996082200376 19960822 00376 WP 1996 8 22 DLL10961902 1 19960814 A 3350 BATTERY 61020 LKHEED 1011 10113851 5265010 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 725DA NONE 193C1162 EMERGENCY FLASHLIGHT DOES NOT INDICATE CHARGING. REPLACED FLASHLIGHT. 2 L 7 3 4F A23WE 1996082200377 19960822 00377 NE 1996 8 22 DL76L961904 2 19960814 A 7200 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 MALFUNCTIONED A DALA O OTHER O OTHER IN INSP/MAINT 1 SO 27 182DN 25987 723834 NR 1 ENG PARAMETERS SHIFTED. REPLACED NR 1 ENGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 1996082200378 19960822 00378 WP 1996 8 22 DLL10961905 1 19960814 A 3350 POWER PACK 516741 LKHEED 1011 10113851 5265010 WP PWA 4060 PW4060 52119 NE CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 725DA 65532 193C1162 723834 EXT LIGHT AT L4 DOOR INOP. REPLACED POWER PACK, CHECKS GOOD. 2 L 7 3 4F 4 F A23WE E24NE 1996082200379 19960822 00379 WP 1996 8 22 DLL10961906 1 19960815 A 3830 WASTE WATER PNL 10648LD1111 LKHEED 1011 10113851 5265010 WP PWA 4060 PW4060 52119 NE FE PANEL MOISTURE CONTAM A DALA D RETURN TO BLOCK B H SMOKE/FUMES/ODORS/SPARKS ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 SO 27 728DA UNK 193C1173 723834 ON TAXI OUT, FLT RCDR WASTE WATER PANEL BEGAN SPARKING DUE TO MOISTURE. PULLED CBS, RETURNED TO GATE. 2 L 7 3 4F 4 F A23WE E24NE 1996082200380 19960822 00380 NM 1996 8 22 DLM88961908 1 19960816 A 4990 OIL SYST DOUG MD88 MD88 3023688 NM APU LEAKING A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 997DL 53364 CABIN AND COCKPIT FILLED WITH SMOKE AFTER T/O. PERFORMED HIGH PRESS PNEU DUCT BURN OUT PER MM 21-00-02 PGS 209 TO 216. 2 L 7 2 4F RT A6WE 1996082200381 19960822 00381 NE 1996 8 22 DL72K961909 2 19960816 A 7314 FUEL PUMP BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE FAILED A DALA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 SO 27 474DA 20751 700467 NR 3 ENGINE LOST THRUST SHORTLY AFTER GEAR RETRACTION. THERE WERE NO ACCOMPANYING SOUNDS HEARD IN COCKPIT. ENGINE INST RUMENTS INDICATED ENGINE FAILURE. NORMAL DESCENT, APPROACH AND LANDING. REPLACED FUEL PUMP, OPS CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1996082200382 19960822 00382 NM 1996 8 22 DL76L961913 1 19960817 A 3350 20131 BATTERY PACK BOEING 767 767332 1382001 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 186DN 27962 THREE AFT EXTERIOR EMERGENCY LIGHTS OUT ON LEFT SIDE OF A/C. REPLACED BATTERY PACK, SYSTEM OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 1996082200383 19960822 00383 NM 1996 8 22 DL76L961916 1 19960818 A 2121 GASPER FAN 6054578 BOEING 767 767332 1382001 NM CABIN FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 177DN 25122 OUT OF 15,000 FT, FLT ATTENDANTS REPORTED FUMES IN FIRST CLASS. RETURNED TO JFK. ISOLATED PROBLEM TO GASPER FAN FAILED . DEACTIVATED SAME PER MEL 21-24-01. PACKS AND RECIRC FANS OPS OK. 2 L 7 2 4F RT A1NM 1996082200384 19960822 00384 NM 1996 8 22 DL73E961917 1 19960808 A 5312 BULKHEAD WEB BOEING 737 737247 138448D NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 374DL 23521 DURING INSPECTION, MAINTENANCE DISCOVERED 5 CRACKS ON THE FWD FACE OF THE 178 BULKHEAD WEB. IN ACCORDANCE WITH FAA FORM 8110-3 DTD 8-8-96 BY DER SO-889, EACH OF THE CRACKS WERE CUT OUT AND A REPAIR DOUBLER AND FILLERS WERE INSTALLED. 2 L 7 2 4F A16WE 1996082200385 19960822 00385 NM 1996 8 22 DL73S961919 1 19960816 A 5315 65498841 FLOOR BEAM BOEING 737 737232 1384475 NM BS 967 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 305DL 23077 DURING INSPECTION, BS 967 FLOOR BEAM HAD CORROSION BLENDED AWAY AT 2 NUTPLATE LOCATIONS. IN ACCORDANCE WITH BACOTWX DA L-ATL-96-124RR, DATED 14 AUG 1996, THE BEAM REPAIRED USING A REPAIR STRAP. 2 L 7 2 4F RT A16WE 1996082200386 19960822 00386 NM 1996 8 22 DL73S961920 1 19960807 A 5330 SKIN BOEING 737 737232 1384475 NM GALLEY DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 312DL 23084 THE R-1 DOORWAY CRACKED AT THE LOWER AFT CORNER APPROX 1.4 INCH LENGTH. THE CRACK WILL BE REPAIRED PER B737-200, SRM 53 -30-3 FIG 26 WITH THE EXCEPTION OF BLIND FASTENER SUBSTITUTION TO FACILITATE MTC. ALSO, FOUND THAT THE CRACK ENDED I N A NUTPLATE HOLE WHICH WILL BE PLUGGED PER THE SRM. SINCE THE NUTPLATE HOLE IS AN ATTACH POINT FOR THE SCUFF PLATE, TH E SCUFF PLATE WILL BE TRIMMED TO DELETE THE HOLE LOCATION. ALSO, THERE IS A PREVIOUS REPAIR APPROX 2 INCHES OUTBD OF WHERE THIS REPAIR WILL EXTEND. 2 L 7 2 4F RT A16WE 1996082200387 19960822 00387 NM 1996 8 22 DL72K961921 1 19960810 A 5312 6516350315 BLKHD STIFFENER BOEING 727 727232 1384082 NM BS 1883 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 414DA 21256 DURING INSPECTION, THE BL 0 VERTICAL STIFFENER OF THE FUSELAGE STATION 1183 BULKHEAD WAS FOUND CRACKED AT WL 190. THE C RACK IS 1.75 INCH LONG IN THE AFT RT FLANGE WHERE A BRACKET ATTACHES. IN ACCORDANCE WITH B727 SRM 51-40-1 FIG 1, THE CR ACK WAS STOP DRILLED AND 2 REPAIR ANGLES WERE INSTALLED. 2 L 7 3 4F A3WE 1996082200388 19960822 00388 NM 1996 8 22 DL73E961922 1 19960809 A 5312 BULKHEAD WEB BOEING 737 737247 138448D NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 239WA 23187 DURING INSPECTION, 2 CRACKS WERE DISCOVERED ON THE FWD FACE OF BS 178 BULKHEAD WEB. CRACKS WERE LOCATED UNDER THE LBL 5 .7 AND RBL 5.7 VERTICAL STRAPS. IN ACCORDANCE WITH FAA/DER FORM 8110-3, DER DESIGNATION SO-957, DATED 9 AUG 1996, THE CRACKS WERE TRIMMED OUT AND A REPAIR DOUBLER WAS INSTALLED. 2 L 7 2 4F A16WE 1996082200389 19960822 00389 NM 1996 8 22 P5CA9600611 1 19960817 A 2410 705117L CSD BOEING 747 747122 1384872 NM NR 1 ENGINE OVERHEATED A P5CA O OTHER J M WARNING INDICATION OVER TEMP CL CLIMB 1 WP 23 854FT 19754 DURING CLIMB AT FL 310, NR 1 ENGINE HAD DUAL FIRE WARNING LIGHTS ILLUM WITH PEGGED NACELLE INDICATORS. PULLED THROTTLE BACK TO IDLE AND LIGHTS WENT OUT, INDICATIONS NORMAL AND CONTINUED FLIGHT. ON GROUND FOUND CSD OVERHEATED AND BODY CRAC KED WIRING BURNT ON CSD. REPLACED CSD PER BOEING MAINTENANCE MANUAL 24-11-01. 2 L 7 4 4F A20WE 1996082200390 19960822 00390 NM 1996 8 22 P5CA9600612 1 19960818 A 2910 3637033 MODULE HOUSING BOEING 747 747122 1384872 NM NR 3 HYD SYST CRACKED A P5CA K NONE K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 853FT 19753 NR 3 HYDRAULIC SYSTEM FLUID LOSS AFTER PUSHBACK. FOUND NR 3 HYDRAULIC SYSTEM PRESSURE MODULE HOUSING CRACKED. REMOVED AND REPLACED MODULE PER BOEING MAINTENANCE MANUAL 29-11-23. 2 L 7 4 4F A20WE 1996082200391 19960822 00391 NM 1996 8 22 P5CA9600613 1 19960816 A 2910 HYD LINE BOEING 747 747122 1384872 NM LT WING CRACKED A P5CA K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 WP 23 852FT 19757 NR 1 HYDRAULIC QUANTITY LOW. FOUND CRACKED LINE NR 1 HYDRAULIC SYSTEM FROM T-FITTING INBOARD OF NR 1 PYLON TO T-FITTING OUTBOARD OF NR 1 PYLON. INSTALLED TEMPORARY FLEX LINE PER BOEING MAINTENANCE MANUAL 29-00-00 PAGE 5. 2 L 7 4 4F A20WE 1996082200392 19960822 00392 SO 1996 8 22 SRAA960808 1 19960819 A 3230 RETRACT MECH LKHEED 382 382G 526414U SO LT MLG MALFUNCTIONED A SRAA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 GL 23 921SJ 4586 ON APPROACH, LEFT MAIN LANDING GEAR WOULD NOT EXTEND, DIVERTED TO FAI AND PREPARED TO HAND CRANK THE LANDING GEAR ON APP ROACH. LOWERED GEAR HANDLE AND ALL GEARS CAME DOWN AND LOCKED NORMALLY. ACCOMPLISHED LANDING WITHOUT INCIDENT AND ITEM IS UNDER INVESTIGATION. 2 H 7 4 4T A1SO 1996082200393 19960822 00393 NE 1996 8 22 96ZZZM1227 2 19960717 A 7260 220309004 CHIP DETECTOR BAC 146 146200A 1500266 EU LYC ALF502 ALF502R 41580 NE NR 4 ENGINE MISINSTALLED A TIXA E ENGINE SHUTDOWN W INADEQUATE Q C NR NOT REPORTED 1 WP 19 156TR E2156 LF05526A NR 4 ENGINE SHUT DOWN IN FLIGHT DUE TO LOW OIL PRESSURE LIGHT ILLUMINATION AND INDICATION. INSPECTION OF THE ENGINE UPO N ARRIVAL, REVEALED FULL FLOW CHIP DETECTOR HAD LOOSENED AND FALLEN OUT OF ITS HOUSING. INVESTIGATION HAS SHOWN MAINTEN ANCE HAD REPLACED THE MAIN OIL FILTER AND CHECKED THE FULL FLOW DETECTOR. IMPROPER INSTALLATION OF THE DETECTOR IS UNDE R REVIEW. (M) 2 H 7 4 4F 4 F A49EU E6NE 1996082200394 19960822 00394 WP 1996 8 22 96ZZZM1230 1 19960709 A 2751 SRDL12C INDICATOR DOUG DC9 DC933F 302207A WP RT TE FLAP FAILED A EIAA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 09 933F 47191 DEN - AUTO PILOT PORPOISES VIOLENTLY IN PITCH WHILE COUPLED ON ILS, BEGINNING AT 500 FEET RADAR ALTITUDE. REPLACED RIGH T FLAP POSITION TRANSMITTER AND GAUGE IAW THE DC9 MM. OPERATIONS CHECK GOOD. REFERENCE EIAA9621. 2 L 7 2 4F A6WE 1996082200395 19960822 00395 WP 1996 8 22 96ZZZM1231 1 19960613 A 3350 1001191 LIGHT DOUG DC9 DC933F 302207A WP CABIN INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 933F 47191 OAK - EMERGENCY EXIT LIGHTS WILL NOT TEST. REMOVED AND REPLACED BATTERY PACK AND MAIN ENTRY DOOR EMERGENCY LIGHT PANEL. SYSTEM OPERATIONS CHECK GOOD. REFERENCE EIAA9618. 2 L 7 2 4F A6WE 1996082200396 19960822 00396 GL 1996 8 22 96ZZZM1232 3 19960711 A 6110 EROSION SHIELD BEECH 1900 1900C 1154161 CE HARTZL HCB4M HCB4M GL LEFT PROP DEBONDED A GPPA K NONE O OTHER IN INSP/MAINT 1 CE 09 32018 UC38 LEFT PROP EROSION SHIELD DELAMINATION NEAR TRAILING EDGE, DETECTED ON PRE-FLIGHT INSPECTION. MAINTENANCE DETERMINED OUT OF LIMITS DUE TO, TOO WIDE AND TOO CLOSE TO TRAILING EDGE PER 1900 CAMP MM. FERRIED AIRCRAFT TO CRAIG AND REMOVED AND REPLACED PROP. 2 L 7 2 4T RT A24CE 6 C P56GL 1996082200397 19960822 00397 CE 1996 8 22 96ZZZM1233 1 19960709 A 5610 1143840201 WINDSHIELD BEECH 1900 1900C 1154161 CE LT COCKPIT CRACKED A GPPA O OTHER O OTHER CR CRUISE 1 CE 09 39019 UC39 EN ROUTE TO JAX, CAPTAINS WINDSHIELD CRACKED (APPROX 5 PLACES NEAR UPPER EDGE), OUTER PLY ONLY. LANDED JAX. MX DETERMI NED UNAIRWORTY PER PILOT VISIBILITY AND INTERFERENCE WITH WIPER OPS. FERRIED A/C TO CRG UNPRESSURIZED AND REMOVED AND R EPLACED WINDSHIELD. 2 L 7 2 4T RT A24CE 1996082200398 19960822 00398 1996 8 22 96ZZZM1234 4 19960604 A 3442 6225941001 RADAR INDICATOR COLLINS BEECH 1900 1900C 1154161 CE COCKPIT FAILED A GPPA A I UNSCHED LANDING CABIN DEPRESSURIZATION B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 09 129GP 597 UC114 PLANE IN CRUISE FLT AT 18,000, SMOKE IS NOTICED COMING FROM CENTER OF AVIONICS PANEL. DESCENDED TO 6,000 FEET AND DUMPE D CABIN PRESSURE WHILE TURNING OFF SYSTEMS, SMOKE DISSIPATES, IT SEEMS TO HAVE COME FROM WEATHER RADAR INDICATOR TOP ARE A AND ABOVE ALTITUDE ALERTER. PLANE DECLARES EMERGENCY AND LANDS AT BLUE FIELD W. VA. MAINTENANCE FOUND THE RADAR INDI CATOR WEATHER HAD AN INTERNAL SHORT. (M) 2 L 7 2 4T RT A24CE 1996082200399 19960822 00399 NM 1996 8 22 96ZZZM1235 1 19960603 A 3040 2312 WINDOW HEAT CONT 10618331 BOEING 737 7372P6 NM E/E BAY FAILED A ZZDA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 15 EICJW 2045 21355 DURING DESCENT INTO BHM FLT, CREW EXPERIENCED SMOKE IN COCKPIT. SMOKE PROCEDURES WERE ADHERED TO, WHICH INCLUDE WINDOW HEAT OFF AND ALTERNATE BLOWER ON. CONTRACT MAINTENANCE WAS DISPATCHED UPON LANDING. TROUBLESHOOTING REVEALED R1 WINDOW HEAT INOP. HEAT CONTROLLER SMELLED AND APPEARED BURNT. PLACED WINDOW HEAT ON MEL 30-11. UPON ARRIVAL TO MCO, HEAT CO NTROLLER WAS REPLACED WITH SERVICEABLE UNIT AND OPERATIONALLY CHECKED. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996082200400 19960822 00400 EU 1996 8 22 96ZZZM1236 2 19960728 A 7200 ENGINES BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU NR 1/NR 2 OVERTEMPED A W8PA O OTHER M J OVER TEMP WARNING INDICATION CL CLIMB 1 NM 03 951WP 22951 OVERTEMPED ENGINE DURING WINDSHEAR RECOVERY, NR 1 - 968 DEGREES, NR 2 972 DEGREES. DURATION APPROX 3 SECONDS AT 500 FEE T AGL, AIR RETURN. REPLACED BOTH ENGINES DUE TO OVERTEMP. 2 L 7 2 4F 4 F RT A16WE E21EU 1996082200401 19960822 00401 NM 1996 8 22 96ZZZM1239 1 19960701 A 3610 1947924 PRECOOLER BOEING 737 7373S3 1384711 NM NR 2 ENGINE CRACKED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 314AW 23733 DEN - FLT 2484 - AIR TURNBACK, AIRCRAFT DEPARTED DEN AND WOULD NOT PRESSURIZE ON ONE BLEED (NR 2 BLEED ON MEL). AIRCRAF T FERRIED TO PHX. ENGINE NR 1 HIGH STAGE VALVE TEST FAILED. REMOVED AND REPLACED NR 1 HIGH STAGE VALVE. REFERENCE MEL 36-05. FOUND CRACKED PRECOOLER. REMOVED AND REPLACED PRECOOLER AND SENSE LINES. REFERENCE AWXA960299. 2 L 7 2 4F RT A16WE 1996082200402 19960822 00402 WP 1996 8 22 96ZZZM1241 1 19960724 A 5210 4928806501 HOLD OPEN HOOK DOUG DC9 DC982 3022082 WP L1 DOOR BENT A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 934AS 49235 SEA - AFTER ARRIVAL OF FLT 371, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN AND LATCH IN OPEN POSITION. FOUND HOLD OPEN HOOK BENT AND DOOR CONTROL ROD LOCK LOOSE. REPLACED DOOR HOLD OPEN HOOK, TIGHTENED AND SAFTIED CONTROL ROD LOCK AN D DOOR OPERATED NORMALLY. REFERENCE ASAA9680156 2 L 7 2 4F A6WE 1996082200403 19960822 00403 EU 1996 8 22 96ZZZM1242 1 19960725 A 3060 ANN50 DE-ICE FUSE JETAIR JETSTM JETSTM4101 1500501 EU PROP DE-ICE FAILURE A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 312UE 41025 FLT NR 6578 - IAD-PWM - DURING CRUISE, MADE UNSCHEDULED LANDING AT IAD DUE TO PROP DE-ICE FAILURE, ELEVATOR HORN ICE FAI LURE, AND STALL WARNING TAPE SHOWS STALL INDICATION. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED ELEV HORN, DE-ICE FUSE AND INSPECTED STALL WARNING. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPRO VED FOR RETURN TO SERVICE. REFERENCE VTZA96275. 2 L 7 2 4T RT A41NM 1996082200405 19960822 00405 WP 1996 8 22 96ZZZM1244 1 19960424 A 2910 61105340534 HYD HOSE DOUG DC8 DC8F54 3021926 WP RUDDER ACCUM RUPTURED A FXLA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 19 54FA 45637 ON TAKEOFF MIA, NOTED LOSS OF HYDRAULIC QUANTITY. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED A R UPTURED HOSE ON THE RUDDER ACCUMULATOR. REPLACED HOSE, SERVICED HYD SYSTEM AND RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 4 4F 4A25 1996082200406 19960822 00406 EU 1996 8 22 96ZZZM1245 1 19960430 A 3260 INDICATOR LIGHT STBROS SD3 SD360 8100606 EU RT MLG MALFUNCTIONED A GUUA O OTHER N FALSE WARNING AP APPROACH 1 SO 19 831BE SH3757 FLT NR 436 - MCO-MIA - RIGHT LANDING GEAR GREEN DOWN LIGHT DOES NOT LIGHT WITH GEAR DOWN, FILAMENT TEST OK. AIRCRAFT LA NDING GEAR SYSTEM WAS DEFERRED WITH GEAR PINS SAFETIED IN PLACE. PERFORMED GEAR SWING IAW SD3 MM CHAPTER 32, OPS CHECK GOOD. (M) 2 H 7 2 4T A41EU 1996082200407 19960822 00407 CE 1996 8 22 96ZZZM1246 1 19960426 A 3260 H111541 UPLOCK SW BEECH 1900 1900C 1154161 CE LANDING GEAR OUT OF ADJUST A GUUA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 SO 19 195GA UB65 FLT 393 - MIA-DAB - LANDING GEAR HANDLE LIGHTS CAME ON IN FLIGHT, GEAR CAME UP ABOUT 1/2 WHEEL. EXTENDED GEAR HAD THREE GREEN. AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT INCIDENT. PLACED AIRCRAFT ON JACKS CYCLED GEAR. GEAR STAYED UP. A DJUSTED BOTH MAIN UP-POSITION SWITCHES. CYCLED GEAR 4 TIMES. OPS CHECK GOOD. AIRCRAFT RELEASED TO SERVICE (M) 2 L 7 2 4T RT A24CE 1996082200408 19960822 00408 NM 1996 8 22 ASAA9610094 1 19960715 A 5315 654581252 FLOOR BEAM BOEING 737 737290C 138448V NM BS 328 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING D-CHECK, THE UPPER CHORD FLANGE OF STATION 328 FLOOR BEAM (CABIN) WAS FOUND CORRODED. REPLACED CHORD AND S PLICED AT LBL 33 PER EA 5310-01454 AND BOEING TELEX ASA-SEA-94-0292RR. (M) 2 L 7 2 4F A16WE 1996082200409 19960822 00409 NM 1996 8 22 ASAA9640060 1 19960712 A 5330 SKIN BOEING 737 7374Q8 NM BS 884-937 SCRAPED A ASAA K NONE O OTHER LD LANDING 1 NM 01 754AS 25095 SEA - ON ARRIVAL OF FLT 105, CREW REPORTED POSSIBLE TAIL SKID CONTACT WITH RUNWAY DURING LANDING. PERFORMED HARD LANDIN G AND TAIL DRAG INSPECTIONS. FOUND DAMAGE TO LOWER FUSELAGE SKIN PANELS BS 884-937, STR 28L-28R. INSTALLED PERMANENT R EPAIR PER EA 5330-01259 AND BOEING TELEX ASA-SEA-96-0312RR DATED 7/15/96. (M) 2 L 7 2 4F RT A16WE 1996082200410 19960822 00410 SO 1996 8 22 ASOA96030 1 19960721 A 3240 214791 BRAKE EMB 120 EMB120RT SO LT MLG INOPERATIVE A ASOA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 11 235AS 120047 DURING TAXI OUT DFW-ICT, FOOT PEDAL BRAKING ACTION WAS LOST. CREW USED THE EMERGENCY BRAKE TO STOP THE AIRCRAFT. MAINT ENANCE ADVISED THE CREW TO TURN THE ANTI-SKID SWITCHES OFF, AT WHICH TIME FOOT PEDAL BRAKING WAS REGAINED. CREW THEN TA XIIED THE AIRCRAFT BACK TO THE GATE. REMOVED AND REPLACED THE LEFT OUTBOARD BRAKE ASSEMBLY AND THE LEFT BRAKE CONTROL V ALVE. OPERATIONAL AND LEAK CHECKS WERE GOOD. MAINTENANCE PERFORMED A TAXI CHECK WITH THE ANTI-SKID ON AND OFF, AND ACH IEVED BRAKING WITH EVERY COMMAND. (M) 2 L 7 2 4T RT A31SO 1996082200411 19960822 00411 NM 1996 8 22 AWXA960249 1 19960514 A 5315 FLOOR BEAM BOEING 737 7372M8 1384483 NM BS 986.5 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 141AW 21955 PAE - FLT 7812 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM BS 986.5, RBL 41, RBL 50, WL 208. REMOVED CORROSION BS 986.5, RBL 37, RBL 39 AND FOUND OUT OF LIMIT PER SRM 53-10-1 AND REPAIR. INSTALLED IAW E R 2-53-15-42 (TCO-PAN-96-061SRR.) (M) 2 L 7 2 4F A16WE 1996082200412 19960822 00412 NM 1996 8 22 AWXA960250 1 19960514 A 5315 FLOOR BEAM BOEING 737 7372M8 1384483 NM BS 1006 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 141AW 21955 PAE - FLT 7812 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM BS 1006, LBL 11, WL 208. REMOVED CORROSION BS 1006, LBL 11, WL 208. OUT OF LIMIT PER SRM 53-10-1. REPAIRED IAW ER 2-53-15-43 (TCO-PAN-96-0612R R) (M) 2 L 7 2 4F A16WE 1996082200413 19960822 00413 NM 1996 8 22 AWXA960251 1 19960515 A 5320 6545895U3 SPLICE BOEING 737 7372M8 1384483 NM BS 905 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 141AW 21955 FLT 7812 - PAE - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CORROSION ON STRINGER 27, RIGHT SPLICE BS 905. R EMOVED STRINGER SPLICE AT BS 905 AND STRINGER 27R. FABRICATED REPAIR PARTS IAW SRM 53-10-3, FIG 1. ALODINED, PRIMED AN D INSTALLED. (M) 2 L 7 2 4F A16WE 1996082200414 19960822 00414 NM 1996 8 22 AWXA960253 1 19960515 A 5315 FLOOR BEAM BOEING 737 7372M8 1384483 NM BS 967 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 141AW 21955 PAE - FLT 7812 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM BS 967, LBL 21-19, WL 208 . REMOVED DAMAGED AREA AT BS 967, LBL 21-29, WL 208. FABRICATED PART AND INSTALLED PER SRM 53-10-9. (M) 2 L 7 2 4F A16WE 1996082200415 19960822 00415 NM 1996 8 22 AWXA960254 1 19960515 A 5315 FLOOR BEAM BOEING 737 7372M8 1384483 NM BS 947 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 141AW 21955 PAE - FLT 7812 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM BS 947, LBL 0-4, WL 208. REMOVED STRAP AND REPAIRED PER ER 2-53-15-44 (TCO-PAN 96-0624RR). (M) 2 L 7 2 4F A16WE 1996082200416 19960822 00416 NM 1996 8 22 AWXA960255 1 19960518 A 5330 SKIN BOEING 737 7372M8 1384483 NM FUSELAGE DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 141AW 21955 PAE - FLT 7812 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND SMALL DENT AFT OF L-2 DOOR (CENTER OF DOOR, 2 INC H AFT). REFERENCE FORM 106 NR 23581. REPLACED SKIN PER ER 2-53-35-06. ENGINEERING REFERENCE TCO-PAN-95-0605RR-621RR. (M) 2 L 7 2 4F A16WE 1996082200417 19960822 00417 NM 1996 8 22 AWXA960256 1 19960515 A 5330 SKIN BOEING 737 7372M8 1384483 NM BS 1047 DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 141AW 21955 PAE - FLT 7812 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND SKIN DENTED STATION 1047-1063, STRINGER 18 RT, WL 206. REMOVED DAMAGED SKIN, FABRICATED REPAIR DOUBLER, INSTALLED REPAIR PARTS PER SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1996082200418 19960822 00418 NM 1996 8 22 AWXA960259 1 19960522 A 5320 MS29754 WEB BOEING 737 737301 1384611 NM BS 1016 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 23260 PAE - FLT 7819 - DURING ROUTINE SCHEDULED C-11 MAINTENANCE CHECK, FOUND WEB CORRODED ON UPPER SURFACE BS 1016, WL 208, R BL 16. REMOVED CORROSION FROM BS 1016, WL 208, RBL 16. FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-60-51. (M) 2 L 7 2 4F RT A16WE 1996082200419 19960822 00419 NM 1996 8 22 AWXA960260 1 19960522 A 5320 INTERCOSTAL BOEING 737 737301 1384611 NM BS 748 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 325AW 23260 PAE - FLT 7819 - DURING ROUTINE SCHEDULED C-11 MAINTENANCE CHECK, FOUND CRACK ON INTERCOSTAL BS 748 IN BETWEEN 25 AND 26 RIGHT STRINGERS. REMOVED AND REPLACED INTERCOSTAL BS 748 IN BETWEEN 25 AND 26 RIGHT STRINGERS. ALL WORK DONE IAW SRM 51-10-02, 51-20-01 AND 51-30-01. (M) 2 L 7 2 4F RT A16WE 1996082200420 19960822 00420 NM 1996 8 22 AWXA960299 1 19960701 A 3610 32144463 HIGH STAGE VLV BOEING 737 7373S3 1384711 NM NR 1 ENGINE FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 314AW 23733 DEN - FLT 2484 - AIR TURNBACK, AIRCRAFT DEPARTED DEN AND WOULD NOT PRESSURIZE ON ONE BLEED (NR 2 BLEED ON MEL). AIRCRAF T FERRIED TO PHX. ENGINE NR 1 HIGH STAGE VALVE TEST FAILED. REMOVED AND REPLACED NR 1 HIGH STAGE VALVE. REFERENCE MEL 36-05. FOUND CRACKED PRECOOLER. REMOVED AND REPLACED PRECOOLER AND SENSE LINES. (M) 2 L 7 2 4F RT A16WE 1996082200421 19960822 00421 NM 1996 8 22 AWXA960300 1 19960425 A 5330 SKIN BOEING 737 7372E3 NM BS 1014 CORROSION A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 138AW 22792 PAE - FLT 3819 - DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND CORROSION ON INTERIOR SKIN AT BS 1014, BLO, WL 1 48. REMOVED CORROSION FROM SKIN. FOUND OUT OF LIMITS. FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-30-3. (M) 2 L 7 2 4F RT A16WE 1996082200422 19960822 00422 NM 1996 8 22 AWXA960301 1 19960425 A 5330 SKIN BOEING 737 7372E3 NM BS 1006 CORROSION A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 138AW 22792 PAE - FLT 3819 - DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND BULGING SKIN AT BS 1006, STRINGER 28 RT. REPAIR ED AREA PER ER NR 2-53-36-19 (FAA/DER TCO-PAN-96-0552RR). (M) 2 L 7 2 4F RT A16WE 1996082200423 19960822 00423 NM 1996 8 22 AWXA960302 1 19960425 A 5330 SKIN BOEING 737 7372E3 NM BS 984 CORROSION A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 138AW 22792 PAE - FLT 3819 - DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND BULGING SKIN AT BS 984, 3 INCH BELOW STRINGER 18 RIGHT. REPAIRED AREA PER ER NR 2-53-36-19 (FAA/DER TCO-PAN-96-0552RR). (M) 2 L 7 2 4F RT A16WE 1996082200424 19960822 00424 NM 1996 8 22 AWXA960303 1 19960425 A 5320 694957411 ANGLE BOEING 737 7372E3 NM BS 1016 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 138AW 22792 PAE - FLT NR 3819 - DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND BUTT JOINT SPLICE ANGLE AT BS 1016, BL0 WL 19 4 IS CORRODED. REMOVED SPLICE ANGLE AT BS 1016, BLO, WL 194. CLEANED AREA, ALODINED, PRIMED AND FABRICATED PART AND IN STALLED PER SRM 51-30-2 AND OHM 20-50-11. (M) 2 L 7 2 4F RT A16WE 1996082200425 19960822 00425 NM 1996 8 22 AWXA960304 1 19960425 A 5313 STRINGER BOEING 737 7372E3 NM BS 1006 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 138AW 22792 DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND STRINGER 27L AT BS 1006 CORRODED AT STRINGER CLIP. REMOVED, FABRI CATED AND REPLACED REPAIR PARTS PER SRM 53-10-3. (M) 2 L 7 2 4F RT A16WE 1996082200426 19960822 00426 NM 1996 8 22 AWXA960305 1 19960425 A 5312 6549914545 BULKHEAD FITTING BOEING 737 7372E3 NM FUSELAGE CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 138AW 22792 PAE - FLT 3819 - DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND BULKHEAD SUPPORT FITTING CORRODED BEYOND LIMITS. REPLACED FITTING PER IAW SCM 51-10-1. (M) 2 L 7 2 4F RT A16WE 1996082200427 19960822 00427 NM 1996 8 22 AWXA960306 1 19960430 A 5315 FLOOR BEAM BOEING 737 7372E3 NM BS 967 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 138AW 22792 PAE - FLT NR 3819 - DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND CORROSION AROUND NUT PLATE HOLE ON FLOOR BEAM STATION 967, WL 208, RBL 28. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-10-9. (M) 2 L 7 2 4F RT A16WE 1996082200428 19960822 00428 NM 1996 8 22 AWXA960307 1 19960430 A 5313 BAC1498156 STRINGER BOEING 737 7372E3 NM BS 1004-1016 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 138AW 22792 PAE - FLT 3819 - DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND CORROSION ON THE STRINGER 26R, BS 1004-1016, RBL 12, WL 148. REMOVED AND REPLACED STRINGER 26 PER SRM 53-10-2. (M) 2 L 7 2 4F RT A16WE 1996082200429 19960822 00429 NM 1996 8 22 AWXA960308 1 19960430 A 5315 FLOOR BEAM BOEING 737 7372E3 NM BS 1016 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 138AW 22792 PAE - FLT 3819 - DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND CORROSION ON STATION 1016 FLOOR BEAM UPPER CHORD RBL 5 TO LBL 28, WL 208. FABRICATED REPAIR PARTS AND INSTALLED PER ER 2-53-15-41 (TC-PAN-960551RR). (M) 2 L 7 2 4F RT A16WE 1996082200430 19960822 00430 NM 1996 8 22 AWXA960309 1 19960430 A 5315 FLOOR BEAM BOEING 737 7372E3 NM BS 947 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 138AW 22792 PAE - FLT NR 3819 - DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND CORROSION UNDERSIDE OF FLOOR BEAM AROUND NUT PLATES STATION 947, RBL 48 TO LBL 5, WL 208. FABRICATED REPAIR PARTS AND INSTALLED PER ER 2-53-15-40 (TC-PAN-96-0541RR) . (M) 2 L 7 2 4F RT A16WE 1996082200431 19960822 00431 NM 1996 8 22 AWXA960310 1 19960430 A 5320 65C807351 MOP SILL BOEING 737 7372E3 NM BS 957-987 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 138AW 22792 PAE - FLT 3819 - DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND CORROSION ON RIGHT AFT SERVICE DOOR MOP SILL STA TION 957-987, RBL 50, WL 208. REMOVED AND REPLACED MOP SILL PER SRM 51-30-2. (M) 2 L 7 2 4F RT A16WE 1996082200432 19960822 00432 NM 1996 8 22 AWXA960311 1 19960430 A 5312 BLKHD DOUBLER BOEING 737 7372E3 NM BS 1156 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 138AW 22792 PAE - FLT 3819 - DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND BULKHEAD DOUBLER AT BS 1156 CRACKED BETWEEN TWO FASTENERS. STOP DRILLED CRACK, NDI VERIFIED CRACK CONTAINMENT. REPAIRED WIT MOD PER SB 53-1086 R3. (M) 2 L 7 2 4F RT A16WE 1996082200433 19960822 00433 NM 1996 8 22 AWXA960312 1 19960430 A 5510 CLEVIS BOEING 737 7372E3 NM HORIZ STAB CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 138AW 22792 PAE - FLT 3819 - DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND CORROSION ON LEFT UPPER CHORD ATTACH CLEVIS AND BOTTOM CHORD ATTACH LUG OF HINGE HOUSING. REMOVED CORROSION FROM LEFT UPPER/LOWER LUG CLEVIS .018 INCH, .005 INCH, .013 INCH AND .006 INCH FROM ORIGINAL THICKNESS .433 INCH MATERIAL AND LOWER LUG ORIGINAL THICKNESS .894 INCH. FLAP PEENED AREA, ALODINED AND PRIMED PER ER NR 2-55-12-07 (TCO-PAN 95-05499RR). (M) 2 L 7 2 4F RT A16WE 1996082200434 19960822 00434 NM 1996 8 22 AWXA960313 1 19960430 A 5712 69449039 RIB BOEING 737 7372E3 NM LT WING LE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 138AW 22792 PAE - FLT 3819 - DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND LEFT L/E RIB CRCKED AT WBL 183.4. REPAIRED RIB IAW 51-40-4, 51-10-12 AND 51-30-2. (M) 2 L 7 2 4F RT A16WE 1996082200435 19960822 00435 NM 1996 8 22 AWXA960314 1 19960501 A 5511 RIB BOEING 737 7372E3 NM HORIZ STAB CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 138AW 22792 DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND RIGHT HORIZONTAL STAB L/E RIB CRACKED AT STATION 123.85. FABRICA TED REPAIR PARTS AND INSTALLED PER SRM 51-40-3, 55-10-2, 51-10-2, 51-20-1 AND 51-30-2. (M) 2 L 7 2 4F RT A16WE 1996082200436 19960822 00436 NM 1996 8 22 AWXA960315 1 19960501 A 5511 RIB BOEING 737 7372E3 NM HORIZ STAB CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 138AW 22792 PAE - FLT 3819 - DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND RIGHT HORIZONTAL STAB L/E RIB CRACKED AT STATION 151.75. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-40-3, 55-10-2, 51-10-2, 51-20-1 AND 51-30-2. (M) 2 L 7 2 4F RT A16WE 1996082200437 19960822 00437 NM 1996 8 22 AWXA960316 1 19960501 A 5511 RIB BOEING 737 7372E3 NM HORIZ STAB CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 138AW 22792 PAE - FLT NR 3819 - DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND RIGHT HORIZONTAL STABILIZER L/E RIB CRACKED A T STATION 170.34. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-40-3, 55-10-2, 51-10-2, 51-20-1 AND 51-30-2. (M) 2 L 7 2 4F RT A16WE 1996082200438 19960822 00438 NM 1996 8 22 AWXA960317 1 19960501 A 5511 RIB BOEING 737 7372E3 NM HORIZ STAB CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 138AW 22792 DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND RIGHT HORIZONTAL STABILIZER L/E RIB CRACKED AT STATON 114.55. FA BRICATED AND INSTALLED REPAIR PARTS PER SRM 51-40-3, 55-10-2, 51-10-2, 51-20-1 AND 51-30-2. (M) 2 L 7 2 4F RT A16WE 1996082200439 19960822 00439 NM 1996 8 22 AWXA960318 1 19960501 A 5313 STRINGER BOEING 737 7372E3 NM BS 967 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 138AW 22792 DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND CORROSION ON STRINGER 17L, BL 967. FABRICATED AND INSTALLED REPA IR STRINGER PER SRM 53-30-02. (M) 2 L 7 2 4F RT A16WE 1996082200440 19960822 00440 NM 1996 8 22 AWXA960319 1 19960501 A 5315 FLOOR BEAM BOEING 737 7372E3 NM BS 987 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 138AW 22792 PAE - FLT 3819 - DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM BS 987, LBL TO RBL 45, W L 208. REMOVED CORROSION, OUT OF LIMITS. FABRICATED NEW TOP CHORD PER SRM 51-30-2 AND INSTALLED PER SRM 51-10-2 AND ER 2-53-15-39 (TC-PAN 96-0538RR). (M) 2 L 7 2 4F RT A16WE 1996082200441 19960822 00441 NM 1996 8 22 AWXA960334 1 19960618 A 5320 ANGLE BOEING 737 73733A 1384673 NM BS 294 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 175AW 23634 PAE - FLT 7827 - DURING ROUTINE SCHEDULED C-12 MAINTENANCE CHECK, FOUND CORROSION ON REINFORCEMENT ANGLE UNDER FLOOR BEA M AT BS 294, RBL 44, WL 207. REMOVED DAMAGED REINFORCEMENT FROM FLOOR BEAM UPPER CHORD BS 294, RBL 30 TO RBL 60, WL 207 . FABRICATED AND INSTALLED REPAIR PARTS, IAW SRM 51-30-01. (M) 2 L 7 2 4F RT A16WE 1996082200442 19960822 00442 EU 1996 8 22 AWXA960339 1 19960712 A 2780 SLAT LOCK AIRBUS 320 A320231 3930325 EU LE FLAP FAILED A AWXA O OTHER N FALSE WARNING CR CRUISE 1 WP 28 635AW 092 RNO - LAS - EMERGENCY DECLARED, SLAT LOCK FAULT SHORTLY AFTER TAKEOFF FROM PHX. COMPLIED WITH CIRCUIT BREAKER RESET CFD S, SFCC, 1 AND 2 TEST, WING TIP BRAKE RESET WITH NO FAULTS FOUND AND NORMAL OPS CHECK OF FLAP/SLATS SYSTEM. (M) 2 L 7 2 4F RT A28NM 1996082200443 19960822 00443 NM 1996 8 22 AWXA960350 1 19960724 A 2520 SEAT BOEING 737 7372M8 1384483 NM CABIN NOT SECURED A AWXA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 28 141AW 21955 PHX - FLT 2890 - AIR TURNBACK, SEAT ROW 6 A, B, C, NOT SECURED. SECURED SEAT ROW 6 A, B, C IN SEAT TRACK AS NEEDED. (M ) 2 L 7 2 4F A16WE 1996082200444 19960822 00444 EU 1996 8 22 C2XA96IA171 1 19960718 A 5753 S5751000502100 SKIN AEROSP ATR42 ATR42320 8680930 EU RT TE FLAP DELAMINATED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15827 175 IAH - DURING C-CHECK INSPECTION, THE RIGHT INBOARD FLAP WAS FOUND TO BE DELAMINATED ON THE UPPER SURFACE. MAINTENANCE R EMOVED AND REPLACED THE FLAP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996082200445 19960822 00445 EU 1996 8 22 C2XA96IA172 1 19960718 A 5753 S5751000501200 SKIN AEROSP ATR42 ATR42320 8680930 EU LT TE FLAP DELAMINATED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15827 175 IAH - DURING C-CHECK INSPECTION, THE LEFT INBOARD FLAP WAS FOUND TO BE DELAMINATED. MAINTENANCE REMOVED AND REPLACED TH E FLAP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996082200446 19960822 00446 EU 1996 8 22 C2XA96IA173 1 19960718 A 5311 S53672407200 FRAME AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15827 175 IAH - DURING C-CHECK INSPECTION, FRAME 38 WAS FOUND TO BE CORRODED. MAINTENANCE REPAIRED THE AFFECTED FRAME SECTION USI NG A DOUBLER REPAIR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996082200447 19960822 00447 EU 1996 8 22 C2XA96IA174 1 19960718 A 5311 S53672406200 FRAME AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15827 175 IAH - DURING C-CHECK INSPECTION, FRAME 36 WAS FOUND TO BE CORRODED. MAINTENANCE REPAIRED THAT AFFECTED PORTION OF FRAME USING A DOUBLER REPAIR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996082200448 19960822 00448 SO 1996 8 22 C2XA96IA175 1 19960726 A 5347 12016000003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12703 120084 IAH - DURING C-CHECK INSPECTION, THE RIGHT FORWARD FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND R EPLACED THE SEAT TRACK AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996082200449 19960822 00449 SO 1996 8 22 C2XA96IA176 1 19960726 A 5347 12015995003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12703 120084 IAH - DURING C-CHECK INSPECTION, THE LEFT FORWARD FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND RE PLACED THE SEAT TRACK AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996082200450 19960822 00450 SO 1996 8 22 C2XA96IA177 1 19960726 A 5347 12026864007 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12703 120084 IAH - DURING C-CHECK INSPECTION, THE LEFT AFT FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLAC ED THE SEAT TRACK AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996082200451 19960822 00451 SO 1996 8 22 C2XA96IA178 1 19960726 A 5400 12030995001 ANGLE EMB 120 EMB120RT SO RT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12703 120084 IAH - DURING C-CHECK INSPECTION, THE ATTACH ANGLE ON THE NR 2 FRAME OF THE RIGHT NACELLE WAS FOUND TO BE CRACKED. MAINT ENANCE REMOVED AND REPLACED THE ANGLE AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996082200452 19960822 00452 SO 1996 8 22 C2XA96IA179 1 19960726 A 5400 12030995001 ANGLE EMB 120 EMB120RT SO LT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12703 120084 IAH - DURING C-CHECK INSPECTION, THE ATTACH ANGLE ON THE LEFT ENGINE NACELLE FRAME 2 WAS FOUND TO BE CRACKED. MAINTENAN CE REMOVED AND REPLACED THE ATTACH ANGLE AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996082200453 19960822 00453 EU 1996 8 22 C2XA96IA180 1 19960730 A 5755 S5771000002001 SKIN AEROSP ATR42 ATR42320 8680930 EU LT SPOILER CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14822 163 IAH - DURING C-CHECK INSPECTION, THE LEFT SPOILER WAS FOUND TO BE CRACKED ON THE UPPER AND LOWER SURFACES AND THE LOWER SURFACE TO BE SEPARATING. MAINTENANCE REMOVED AND REPLACED THE SPOILER PER ATR JIC 57-71-00 RAI 10000-003, AND THE AIRC RAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996082200454 19960822 00454 EU 1996 8 22 C2XA96IA181 1 19960730 A 5347 NTA44768 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14822 163 IAH - DURING C-CHECK INSPECTION, THE LEFT FLIGHT ATTENDANT SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996082200455 19960822 00455 EU 1996 8 22 C2XA96IA182 1 19960730 A 5240 H33343 LATCH AEROSP ATR42 ATR42320 8680930 EU DOCUMENT DOOR CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14822 163 IAH - DURING C-CHECK INSPECTION, THE DOCUMENT DOOR LATCH MECHANISM WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REP LACED THE LATCH MECHANISM, AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996082200456 19960822 00456 NM 1996 8 22 CAL960604 1 19960502 A 3397 WIRE BOEING 757 757224 1384958 NM CABIN BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 12109 27299 LAX - THE EMERGENCY AISLE LIGHTS AT ROWS 3-5 A, B WERE FOUND INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT SEAT TRACK 5A, B. THE WIRE WAS SPLICED AND OPERATION OF THE LIGHTS WAS RESTORED. (M) 2 L 7 2 4F RT A2NM 1996082200457 19960822 00457 WP 1996 8 22 EIAA9620 1 19960627 A 2730 ROD END NUT DOUG DC9 DC933F 302207A WP ELEVATOR LOOSE A A EIAA O OTHER F FLT CONT AFFECTED DE DESCENT 1 NM 09 933F 47191 SEA - DURING DESCENT THROUGH 16,000 FEET, ELEVATOR CONTROL JAMMED UNTIL 15 LBS FORWARD FORCE APPLIED, THEN ABRUPTLY FREE D. INSPECTED ELEVATOR SYSTEM IAW MM. NO FAULTS FOUND. UNABLE TO DUPLICATE. CLOSED ALL PANELS ASSOCIATED WITH INSPECT ION. ALL CHECKS GOOD. SUBMITTER STATES, THERE WAS A SUBSEQUENT DISCREPANCY REPORTED ON 6/29/96 ON LOG PAGE F33918 RELA TING TO AUTO PILOT OSCILLATING PLUS/MINUS 100 FEET DURING CRUISE. INSPECTION OF THE ELEVATOR SYSTEM FOUND RIGHT ACTUATO R CYLINDER ROD END NUT LOOSE WHICH WAS TIGHTENED AND INSPECTED PER THEIR MM. SYSTEM WAS CHECKED PER THE MM AND FOUND OK (M) 2 L 7 2 4F A6WE 1996082200458 19960822 00458 WP 1996 8 22 EIAA9621 1 19960709 A 2751 ST12BC FLAP TRANS DOUG DC9 DC933F 302207A WP RT TE FLAP FAILED A EIAA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 09 933F 47191 DEN - AUTO PILOT PORPOISES VIOLENTLY IN PITCH WHILE COUPLED ON ILS, BEGINNING AT 500 FEET RADAR ALTITUDE. REPLACED RIGH T FLAP POSITION TRANSMITTER AND GAUGE IAW THE DC9 MM. OPERATIONS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1996082200459 19960822 00459 WP 1996 8 22 EIAA9623 1 19960718 A 3260 CONNECTOR DOUG DC9 DC933F 302207A WP NLG RECESSED PIN A EIAA O OTHER N FALSE WARNING AP APPROACH 1 NM 09 933F 47191 SAN - NOSE GEAR WILL NOT SHOW DOWN AND LOCKED INDICATION (GREEN LIGHT) WITH VISUAL INDICATION SHOWING DOWN AND LOCKED. A T THE TOP OF DESCENT, WHEN POWER WAS IDLE, RED NOSE GEAR LIGHT WOULD NOT ILLUMINATE. RED GEAR LIGHT FOR NOSE GEAR DID C YCLE ON GEAR EXTENSION. FOUND PIN 5 OF THE NOSE GEAR LOCK SYSTEM (S1-90) RECESSED. REPAIRED PIN. NOSE GEAR INDICATION SYSTEM CHECKED NORMAL PER MAINTENANCE MANUAL. (M) 2 L 7 2 4F A6WE 1996082200460 19960822 00460 NM 1996 8 22 EIAA9624 1 19960717 A 3213 65B012134 INNER CYLINDER BOEING 747 747212B 1384886 NM LT MLG CRACKED A EIAA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 09 485EV 20712 BUR - ON POST INSPECTION, MAINTENANCE FOUND THE LEFT WING GEAR STRUT LEAKING. AIRCRAFT WAS FERRIED TO THE TEAM AER LING US FACILITY AT DUBLIN, WHERE IT WAS DISCOVERED THAT THE INNER CYLINDER WAS CRACKED. THE CRACK STARTED APPROXIMATELY 8 I NCHES ABOVE THE CHROME RUN OUT AND EXTENDED THE LENGTH OF THE INNER CYLINDER. (M) 2 L 7 4 4F A20WE 1996082200462 19960822 00462 NM 1996 8 22 EISA96100 1 19960718 A 2820 CROSSFEED BOEING 727 727221 1384071 NM NR 3 TANK INOPERATIVE A EISA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 SW 07 366PA 22538 NR 3 ENGINE FUEL CROSSFEED VALVE INTRANSIT LIGHT REMAINED ILLUMINATED AFTER CROSSFEED OPERATIONS DIVERTED TO 'ICT'. DEF ERRED PER MEL 24-2 PLACARD NR 966. (M) 2 L 7 3 4F A3WE 1996082200463 19960822 00463 WP 1996 8 22 HALA96101 1 19960725 A 5246 FUEL DOOR DOUG DC9 DC951 3022051 WP RT WING CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 679HA 47662 HNL - IN C-CHECK, FOUND MODERATE CORROSION, RT WING, ON DEFUEL VALVE ACCESS DOOR, LEVEL 2. CLEANED, TREATED AND PRIMED PER SRM 51-10-3. INSTALLED DOUBLER PER SRM 57-01 FIG 2, SHEET 2. PAINTED PER SRM 51-10-3. (M) 2 L 7 2 4F A6WE 1996082200464 19960822 00464 WP 1996 8 22 HALA96102 1 19960728 A 3230 RETRACT SPRING DOUG DC9 DC951 3022051 WP NLG BROKEN A HALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 13 673MC 47726 FLT 522 - HNL - AIR RETURN, UPON FLAP RETRACTION CLIMBING OUT OF APPROX 2000 FEET, A LOUD METALIC SOUND ORIGINATING FROM BELOW COCKPIT CREW AREA WAS HEARD AND FELT. FLIGHT ATTENDANT ALSO HEARD AND CONFIRMED. AFTER CREW DEBRIEFING MLG WAS RETRACTED AND FLAPS WERE ALSO RETRACTED. INSPECTION OF NOSE GEAR REVEALED NOSE GEAR RETRACT ASSIST DOOR SPRING BROKEN. REPLACED NOSE GEAR RETRACT ASSIST SPRING PER MM 32-21-3. SECURITY AND CONDITION CHECK OK. NO DAMAGE TO HYDRAULIC LINE S AND OTHER COMPONENTS. SECURED NOSE GEAR DOORS. (M) 2 L 7 2 4F A6WE 1996082200465 19960822 00465 NE 1996 8 22 HNAA9691446 2 19960704 A 7200 ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 FAILED A HNAA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 EA 07 914HA 53 FLT 3088 - MIA-TPA - DURING CLIMB-OUT, NR 1 ENGINE TORQUE, FUEL FLOW, AND OIL PRESSURE INDICATION WAS ZERO. SHUT DOWN T HE ENGINE IAW EMERGENCY SHUTDOWN CHECK LIST. THE AIRCRAFT TURNED BACK TO MIA AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE NR 1 ENGINE. (M) 2 H 7 2 4T 4 T RT A13NM E20NE 1996082200466 19960822 00466 NM 1996 8 22 HNAA9697944 1 19960626 A 3230 GEAR PIN DHAV DHC8 DHC8102 2809003 NM NLG NOT STOWED A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 979HA 373 FLT NR 3243 - TPA-FLL - AFTER TAKEOFF, THE NOSE GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO TPA AND LANDED WITHOUT INCIDENT. FOUND NOSE GEAR PIN NOT STOWED, RESTOWED PIN. AT RON, INSPECTED NOSE GEAR GROUND LOCK, LUBRICATED AND CHECK ED FOR PROPER OPERATION. (M) 2 H 7 2 4T RT A13NM 1996082200467 19960822 00467 NM 1996 8 22 IXKA9600056 1 19960709 A 3530 4566M37B0464 PBE ESSEX BOEING 727 727225 1384077 NM COCKPIT PIN PROTUDING A IXKA K NONE O OTHER IN INSP/MAINT 1 EA 25 8882Z V8802075 21579 INDICATOR ON COCKPIT BEYOND LIMITS. REMOVED AND REPLACED COCKPIT PBE PER MM 25-60-00. (M) 2 L 7 3 4F A3WE 1996082200468 19960822 00468 NM 1996 8 22 IXKA9600057 1 19960715 A 2782 1U11032 ACTUATOR RONSON BOEING 727 727225 1384077 NM NR 5 LE FLAP FAILED A IXKA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 25 353PA 04232BDFOMN 20622 ON DEPARTURE FROM LAS TO MDW, FLT 88 RETURNED TO LAS, AFTER NR 5 LE SLAT FAILED TO PROPERLY STOW, LE AMBER LIGHT ILLUMIN ATED. CONFIRMED NOT STOWED. REMOVED AND REPLACED NR 5 LE ACTUATOR, OPS AND LEAK CHECK OK AS PER MM 27-81. (M) 2 L 7 3 4F A3WE 1996082200469 19960822 00469 NM 1996 8 22 IXKA9600058 1 19960715 A 3350 7912 LENS BRUCE BOEING 727 727225 1384077 NM CABIN MISSING A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 354PA 20624 FOUND CLEAR LENS MISSING ON 'E' PATH LIGHTING AT 27D. INSTALLED NEW LENS AT 27D. (M) 2 L 7 3 4F A3WE 1996082200470 19960822 00470 NM 1996 8 22 IXKA9600059 1 19960709 A 3350 816901 SOCKET BRUCE BOEING 727 727225 1384077 NM CABIN WIRE BROKEN A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 354PA 20624 FOUND ROW 26 EMERGENCY TRACK LIGHT OUT. WIRE BROKEN. REMOVED AND REPLACED LIGHT SOCKET, OPS CHECK OK PER MM 33-50-121. (M) 2 L 7 3 4F A3WE 1996082200471 19960822 00471 NM 1996 8 22 IXKA9600060 1 19960716 A 3350 90031 LIGHT BOEING 727 727225 1384077 NM CABIN INOPERATIVE A IXKA K NONE O OTHER IN INSP/MAINT 1 EA 25 354PA UI024 20624 RIGHT AND LEFT OVERWING EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED LEFT AND RIGHT LIGHT ASSEMBLY. OPS CHECK OK PER MM 33-50-01. (M) 2 L 7 3 4F A3WE 1996082200472 19960822 00472 NM 1996 8 22 IXKA9600061 1 19960718 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 354PA 6909 20624 RIGHT AFT EMERGECNY OVERWING LIGHT OUT. REMOVED AND REPLACED BATTERY PACK, OPS CHECK OK PER MM 33-50-01. (M) 2 L 7 3 4F A3WE 1996082200473 19960822 00473 NM 1996 8 22 IXKA9600062 1 19960718 A 3350 900542 BATTERY CHARGER BELL BOEING 727 727225 1384077 NM CABIN INOPERATIVE A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 354PA 8572 20624 LEFT CENTER OVERWING EMERGENCY LIGHT OUT. REMOVED AND REPLACED BATTERY CHARGER, OPS CHECK OK PER MM 33-50-01. (M) 2 L 7 3 4F A3WE 1996082200474 19960822 00474 WP 1996 8 22 IXXA96104 1 19960704 A 2170 F38C37 COALESCER DOUG DC8 DC871 302199A WP RT PACK LOOSE A IXXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 11 826BX 45998 EN ROUTE FROM BNA-FLL AT FLT LEVEL 350, OIL SMOKE/MIST WAS NOTED IN THE COCKPIT. THE RIGHT PACK SYSTEM WAS SUSPECTED AN D SHUT DOWN FOR THE REMAINDER OF THE FLIGHT. MAINTENANCE FOUND AND SECURED A LOOSE CLAMP AT THE WATER SEPARATOR/COALESC ER. OPERATIONALLY CHECKED THE SYSTEM IAW THE MM. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 4 4F 4A25 1996082200475 19960822 00475 WP 1996 8 22 IXXA96106 1 19960710 A 3244 26014112 TIRE DOUG DC8 DC863F 302198F WP MLG FAILED A IXXA K NONE O OTHER LD LANDING 1 SW 11 784AL 460 46135 ON LANDING TSJU, THE NR 3 AND NR 8 TIRES BLEW, LOCAL TOWER CLOSED RUNWAY UNTIL THE A/C COULD BE REMOVED. THE NR 3 TIRE EXIBITED MULTIPLE FLAT SPOTS AND THE NR 8 TIRE HAD ONE FLAP SPOT. SUBSEQUENT DAMAGE OF THE NR 4 BRAKE LINE OCCURRED. M AINTENANCE REPLACED BLOWN TIRES, ADJACENT TIRES, NR 8 ANTI-SKID TRANSDUCER, NR 4 BRAKE LINE, AND BLED ALL BRAKES IAW THE DOUGLAS MM AND RETURNED THE AIRCRAFT TO SERVICE. (M) 2 L 7 4 4F 4A25 1996082200476 19960822 00476 WP 1996 8 22 IXXA96107 1 19960607 A 5313 LONGERON DOUG DC8 DC863 302198A WP BS 1550-1570 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 869BX 55751 46035 DURING ROUTINE B-CHECK INSPECTION, LONGERON 25 RIGHT WAS FOUND CORRODED BETWEEN FUSELAGE STATIONS 1550 AND 1570. THE DA MAGED SECTION WAS REMOVED AND REPLACED WITH A NEW SECTION. THE LONGERON WAS REPAIRED IAW DRAWING 853-39-96 WHICH WAS FA A DER APPROVED 5/13/96. (M) 2 L 7 4 4F 4A25 1996082200477 19960822 00477 WP 1996 8 22 IXXA96108 1 19960607 A 5313 5750198502 LONGERON DOUG DC8 DC863 302198A WP RT MLG WW CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 869BX 55751 46035 DURING ROUTINE B-CHECK INSPECTION, LONGERON 24 RIGHT WAS FOUND TO BE CRACKED. THE LONGERON WAS REPLACED IAW DOUGLAS DRA WING 5751027 AND THE AIRCRAFT STRUCTURAL REPAIR MANUAL. (M) 2 L 7 4 4F 4A25 1996082200478 19960822 00478 WP 1996 8 22 IXXA96109 1 19960607 A 5313 5750198501 LONGERON DOUG DC8 DC863 302198A WP LT MLG WW CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 869BX 46035 DURING ROUTINE B-CHECK INSPECTION, LONGERON 24 LEFT WAS FOUND CORRODED BETWEEN FUSELAGE STATIONS 857 AND 867. CORROSION WAS REMOVED, REPAIR DOUBLER FABRICATED AND INSTALLED IAW THE AIRCRAFT STRUCTURAL REPAIR MANUAL 53-2-2. (M) 2 L 7 4 4F 4A25 1996082200479 19960822 00479 WP 1996 8 22 IXXA96110 1 19960607 A 5313 LONGERON DOUG DC8 DC863 302198A WP BS 1550-1570 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 869BX 55751 46035 DURING ROUTINE B-CHECK INSPECTION, CORROSION WAS FOUND ON LONGERON 25 LEFT BETWEEN FUSELAGE STATIONS 1550 AND 1570. COR RODED SECTION WAS REMOVED. REPAIR OF THE AREA WAS ACCOMPLISHED BY INSTALLING A NEW SECTION IAW FAA DER APPROVED DRAWING 853-40-96. (M) 2 L 7 4 4F 4A25 1996082200480 19960822 00480 WP 1996 8 22 IXXA96111 1 19960607 A 5330 SKIN DOUG DC8 DC863 302198A WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 869BX 46035 DURING ROUTINE B-CHECK INSPECTION, CORROSION WAS LOCATED AT FUSELAGE STATION -8.0 TO PLUS 35.0 AT LONGERON 31 RIGHT. CO RROSION WAS REMOVED, EXTERNAL REPAIR DOUBLER FABRICATED AND INSTALLED IAW THE DOUGLAS STRUCTURAL REPAIR MANUAL. (M) 2 L 7 4 4F 4A25 1996082200481 19960822 00481 WP 1996 8 22 IXXA96112 1 19960607 A 5311 FRAME DOUG DC8 DC863 302198A WP BS 798 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 869BX 55751 46035 DURING ROUTINE B-CHECK INSPECTION, THE FUSELAGE FRAME AT FUSELAGE STATION 798 WAS FOUND CRACKED AND CORRODED AT BETWEEN LONGERONS 17 AND 20 LEFT. THE CORROSION WAS REMOVED AND THE CRACK STOP DRILLED. REPAIR DOUBLER AND FILLER FABRICATED A ND INSTALLED IAW FAA DER APPROVED DRAWING 853-38-96. (M) 2 L 7 4 4F 4A25 1996082200482 19960822 00482 WP 1996 8 22 IXXA96113 1 19960607 A 5730 SKIN DOUG DC8 DC863 302198A WP WS 69.5 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 869BX 55751 46035 DURING ROUTINE B-CHECK INSPECTION, THE UPPER AFT INBOARD WING SKIN WAS FOUND CRACKED AT ROW 69.5 BETWEEN STRINGER 2 AND THE REAR SPAR REPAIR OF THE AREA WAS ACCOMPLISHED BY CUTTING OUT THE CRACK, FABRICATING AND INSTALLING A FILLER, EXTERNA L DOUBLER AND TRIPLER IAW THE DOUGLAS ROD SKETCH 96-05-13-001 WHICH IS FAA DER APPROVED. (M) 2 L 7 4 4F 4A25 1996082200483 19960822 00483 WP 1996 8 22 IXXA96115 1 19960722 A 3260 H146 SWITCH DOUG DC8 DC863F 302198F WP RIGHT MLG FAILED A IXXA O OTHER N FALSE WARNING TO TAKEOFF 1 SW 11 786AL 46121 ON TAKEOFF OUT OF KRDL, GEAR NOT LATCH LIGHT CAME ON. GEAR CYCLED WITH NO CHANGE. AT TJSJ MAINTENANCE INSPECTED AIRCRA FT AND FOUND RIGHT GEAR UPLATCH TO BE BAD. SWITCH WAS REPLACED AND SYSTEM CHECKS NORMAL. (M) 2 L 7 4 4F 4A25 1996082200484 19960822 00484 WP 1996 8 22 IXXA96116 1 19960725 A 5730 SKIN DOUG DC8 DC871F 302199D WP LT WING CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 73880 45811 DURING FUEL LEAK TROUBLESHOOTING, TWO SMALL CRACKS WERE IDENTIFIED RADIATING OUT OF ONE RIVET HOLE ON LT WING LOWER EXTE RIOR PLATING, JUST OUTBOARD OF NR 1 PYLON. CRACK LOCATION BETWEEN STRINGERS 60 AND 61. TOTAL CRACK LENGTH APPROXIMATEL Y ONE INCH. ACTION CLASSIFIED AS A MAJOR REPAIR, AND REQUIRES FAA APPROVAL. REPAIR IS ACCOMPLISHED IAW AAR OKLA REPAIR SKETCH. CRACK REPAIR TO LOWER WING SKIN BETWEEN STR 60 AND 61, OUTBOARD OF NR 1 PYLON. REV IR DATED 7-23-96. WHICH W AS FAA APPROVED ON FAA FORM 8110-3. BY DER SO-443. (M) 2 L 7 4 4F RT 4A25 1996082200486 19960822 00486 NE 1996 8 22 IXXA96118 2 19960727 A 7250 9997M23G25 HPT BLADE DOUG DC8 DC871 302199A WP GE CFM56 CFM562C1 13802 NE NR 1 ENGINE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 824BX 8233 45946 693160 DURING PRECAUTIONARY BORESCOPE INSPECTION OF THE NR 1 ENGINE, MAINTENANCE FOUND ONE HIGH PRESSURE TURBINE BLADE TRAILING EDGE TIP CORNER MISSING. MISSING MATERIAL WAS LOCATED AT THE TRAILING EDGE TIP, DOWNWARD TO THE FIRST AIR SLOT IN AREA B, CFMI MM 72-00-00. APPROXIMATE MEASUREMENTS WERE .300 BY .375. FURTHER INVESTIGATION REVEALS LIBERATED MATERIAL PUN CTURED THE HPT SHROUD. NO OTHER TURBINE DAMAGE WAS FOUND. ENGINE REQUIRED REPLACEMENT. PRECAUTIONARY INSPECTION RESUL TED FROM SUSPECTED LEFT WING ENGINE STALL WHICH COULDN'T BE POSITIVELY IDENTIFIED AS BEING THE NR 1 OR NR 2 ENGINE. (M) 2 L 7 4 4F 4 F 4A25 E2GL 1996082200487 19960822 00487 WP 1996 8 22 IXXA96119 1 19960731 A 2550 CARGO CONTAINER DOUG DC8 DC871F 302199D WP CARGO COMPT FUMES A IXXA G J A O2 MASK DEPLOYED DUMP FUEL UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 11 821BX 45811 ON CLIMB-OUT FROM TOL, FUMES ENTERED THE FLIGHT DECK, THE AIRCRAFT RETURNED TO TOL. THE EMERGENCY RESPONSE TEAM LOCATED THE SOURCE OF THE FUMES. THE FUMES WERE GENERATED BY NON-HAZARDOUS MATERIAL, AUTOMOTIVE PARTS, IN THE POSITION 4, UPPE R DECK CONTAINER. THE PARTS WERE REMOVED AND THE AIRCRAFT RELOADED AND DEPARTED. THE MANUFACTURER INDICATED DURING THE MANUFACTURE PROCESS OF THE PARTS, THEY ARE CLEANED AND COATED WITH A CHEMICAL WHICH IS SPUN DRY, BAKED, AND THEN AIR DR IED FOR 24 HOURS TO DISSIPATE THE FUMES. THE ORIGINATING SHIPPING POINT HUMIDITY HAS BEEN EXTREMELY HIGH WHICH POSSIBLY HAMPERED THE AIR DRY FUME DISSIPATION. (M) 2 L 7 4 4F RT 4A25 1996082200488 19960822 00488 WP 1996 8 22 IXXA96120 1 19960626 A 2710 3654950536 CONTROL CABLE DOUG DC8 DC871 302199A WP LT AILERON BROKEN A IXXA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SW 11 824BX 2562 45946 ON TAXI OUT AND FLIGHT CONTROL CHECKS AT ATL, AILERONS FELT STIFF WITH VERY LITTLE SPOILER PRESSURE DROP. THE AIRCRAFT RETURNED TO RAMP. MAINTENANCE INSPECTED THE FLIGHT CONTROL CABLES AND FOUND THE LEFT AILERON BUS CABLE BROKEN. MAINTEN ANCE REPLACED THE BROKEN CABLE AND RIGGED THE SYSTEM IAW WITH THE DOUGLAS MAINTENANCE MANUAL 27-10-0. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 4 4F 4A25 1996082200489 19960822 00489 WP 1996 8 22 IXXA96121 1 19960627 A 2760 3644327509 LINKAGE DOUG DC8 DC863F 302198F WP LT INBD SPOILER BROKEN A IXXA O OTHER J WARNING INDICATION CR CRUISE 1 SW 11 867BX 46049 EN ROUTE BETWEEN ATL AND TOL, CREW NOTED SPOILER UNLOCK INDICATION LIGHT ILLUMINATED WITH STANDBY SPOILER PUMP OFF. FLI GHT CONTINUED WITH AN UNEVENTFUL LANDING AT TOL. MAINTENANCE FOUND AND REPLACED A BROKEN LEFT INBOARD SPOILER CRANK/LIN KAGE IAW THE DOUGLAS MM 27-60-1 AND RETURNED THE AIRCRAFT TO SERVICE. (M) 2 L 7 4 4F 4A25 1996082200490 19960822 00490 EU 1996 8 22 JBXA00015 1 19960730 A 3234 715381 SELECTOR VLV FOKKER F28 F28MK0100 4990807 EU LANDING GEAR MALFUNCTIONED A JBXA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 05 103ML 717G 11444 PHL - FLT 119 - LANDING GEAR WOULD NOT EXTEND INTO PHL. EXTENDED THE GEAR WITH THE ALTERNATE GEAR CONTROL. PILOT RESET ALTERNATE GEAR HANDLE. ISSUED SPECIAL FLIGHT PERMIT TO FERRY A/C GEAR DOWN TO RDU TO PERFORM MX. REMOVED AND REPLACED LG SELECTOR VALVE IAW 32-32-01. OPERATIONAL CHECK GOOD AT THIS TIME. MX AND RII SIGNED. (M) 2 L 7 2 4F RT 1996082200491 19960822 00491 1996 8 22 MALA965070 4 19960712 A 3442 071131900 RT UNIT DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A MALA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 833MA 343 FLT NR 3137 - EN ROUTE, THE WEATHER RADAR BECAME INOPERATIVE. THE AIRCRAFT RETURNED TO DTW. MANTENANCE REPLACED THE WE ATHER RADAR R/T. ALL CHECKS SATISFACTORY. (M) 2 H 7 2 4T RT A13NM 1996082200492 19960822 00492 1996 8 22 MALA965071 4 19960713 A 3442 071137800 RT UNIT SWRNGN SA227 SA227AC 8780603 SW COCKPIT FAILED A MALA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 442MA AC725 FLT NR 3232 - EN ROUTE, THE WEATHER RADAR BECAME INOPERATIVE. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE W EATHER RADAR R/T. ALL CHECKS SATISFACTORY. (M) 2 L 7 2 4T RT A8SW 1996082200493 19960822 00493 WP 1996 8 22 ORJA9639 1 19960708 A 3350 41B004AD073 BATTERY PACK EA1D13D3 DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 842RA 49604 EMERGENCY FLOOR TRACK LIGHTS OUT FROM BEGINNING OF COACH CLASS. REMOVED AND REPLACED BATTERY PACK. OPS NORMAL IAW MM. (M) 2 L 7 2 4F A6WE 1996082200494 19960822 00494 NM 1996 8 22 P2EA96002 1 19960528 A 2781 CIRCUIT BREAKER BOEING 737 737222 1384473 NM LE FLAP ANNUN TRIPPED A P2EA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 05 208AU 19547 FLT NR 204 - SLC - AT 5 KNOTS, TAKEOFF CONFIGURATION WARNING HORN SOUNDED. ABORTED TAKEOFF AND RETURNED TO GATE. MAIN TENANCE FOUND LEADING EDGE POSITION ANNUNCIATOR DC CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER. ACCOMPLISHED TAKEOFF WARNING SYSTEM CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1996082200495 19960822 00495 NM 1996 8 22 P2EA96003 1 19960709 A 3260 SWITCH BOEING 737 737222 1384473 NM GEAR HANDLE LACK OF LUBE A P2EA O OTHER N FALSE WARNING AP APPROACH 1 CE 05 209US 19548 FLT NR 130 - MCI - LANDING GEAR RED LIGHTS CAME ON DURING APPROACH, CYCLED GEAR AND LANDED UNEVENTFUL. MAINTENANCE FOUN D SWITCH IN GEAR HANDLE DIRTY, CLEANED AND LUBRICTED SWITCH AND HANDLE. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1996082200496 19960822 00496 NM 1996 8 22 P91A096022 1 19960625 A 2612 894120 FIRE LOOP BOEING 727 727231 1384079 NM NR 3 ENGINE SHORTED A P9IA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 03 590CA 57688 3891 20098 FOUR MINUTES AFTER TAKEOFF STX AT 2145, HAD A FIRE WARNING, NR 3 ENGINE MADE SHUTDOWN PER PROCEDURES. RETURNED TO STX. TROUBLE-SHOT SYSTEM, NR 3 FOUND FIRE DETECTION LOOP BAD. REMOVED AND REPLACED FIRE DETECTION LOOP. CHECKS GOOD MM 26-1 2-00 A AND B SYSTEM. (M) 2 L 7 3 4F A3WE 1996082200497 19960822 00497 EU 1996 8 22 PLGA9607072 1 19960707 A 2910 L38710SA SWIVEL SAAB SF340 SF340A 7850100 EU RT MLG WW BROKEN A PLGA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NE 05 344BE 340A104 ALB - FLT 4657 - AFTER TAKEOFF FROM ALB EN ROUTE TO LGA, THE CREW NOTED THE HYD LOW LEVEL WARNING LIGHT ILLUMINATED AND THE HYD QTY INDICATION DROPPING. THE CREW PERFORMED AN EMERGENCY GEAR EXTENSION AND DIVERTED BACK TO ALB. THE AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTION REVEALED THE RIGHT GEAR DOWN LOCK SWIVEL HAD BROKEN. MAINTENANCE REMOVED AND REPL ACED THE SWIVEL AND PERFORMED AN OPS CHECK OF THE GEAR WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1996082200498 19960822 00498 NE 1996 8 22 PLGA9607102 2 19960710 A 7261 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LEFT LEAKING OIL A PLGA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NE 05 747BA 17285 340A148 GEE367265 SYR - FLT 4870 - DURING CLIMB-OUT FROM SYR TO JFK, THE LEFT ENGINE OIL LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO SYR AND LANDED WITHOUT INCIDENT. THE OIL LEVEL WAS CHECKED AND FOUND 2.5 QTS DOWN. THE ENGINE OIL WAS SERVICED AND FERRIED TO PSM FOR MORE TROUBLESHOOTING. UPON INSPECTION OF THE ENGINE IT WAS NOTED THAT THE B-SUMP DRAIN WAS LEAKING. THE EN GINE WAS REMOVED AND REPLACED. A LEAK CHECK AND OPS CHECK WAS PERFORMED AND NO DEFECTS WERE NOTED. AIRCRAFT RETURNED T O SERVICE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE6 1996082200499 19960822 00499 EU 1996 8 22 REXA96021 1 19960701 A 2611 SMOKE DETECTOR SAAB SF340 SF340A 7850100 EU LAVATORY ILLUMINATED A REXA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 25 402BH 340A058 LAVATORY SMOKE ILLUMINATED ON TAKEOFF ROLL, ABORTED TAKEOFF. DEFERRED PER MEL 26-13-01. (M) 2 L 7 2 4T RT A52EU 1996082200500 19960822 00500 EU 1996 8 22 REXA96022 1 19960709 A 2550 CARGO NET SAAB SF340 340B 7860101 EU CARGO COMPT OUT OF POSITION A REXA A UNSCHED LANDING N F FALSE WARNING FLT CONT AFFECTED CR CRUISE 1 SO 25 361PX 340B249 CARGO SMOKE LIGHT ILLUMINATED IN FLIGHT, DISCHARGED BOTTLE, DECLARED EMERGENCY AND LANDED IN MGM. INSPECTED SYSTEM, FOU ND CARGO RETAINING NET HOOKED ON SMOKE DETECTOR. DEFERRED PER MEL. (M) 2 L 7 2 4T RT A52EU 1996082200501 19960822 00501 EU 1996 8 22 REXA96023 1 19960714 A 2612 FIRE DETECTOR SAAB SF340 340B 7860101 EU LT ENGINE SHORTED A REXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 360PX 1601 340B220 LEFT TAILPIPE 'HOT' LIGHT IN FLIGHT. REMOVED TAILPIPE COWLING, FOUND GROUNDED POST. RE-POSITIONED FIRE DETECTOR. GROU ND RUNS GOOD. (M) 2 L 7 2 4T RT A52EU 1996082200502 19960822 00502 CE 1996 8 22 S2YA960013 1 19960704 A 5542 130630000607 SKIN BEECH 1900 1900D 1154162 CE RUDDER CRACKED A S2YA K NONE O OTHER IN INSP/MAINT 1 GL 13 79SK 5857 5857 UE79 DURING AN INSPECTION, MAINTENANCE FOUND THE TOP SIDE OF THE RUDDER CRACKED PERPENDICULAR AT THE FORWARD RIVET OF THE TOP STATIC WICK MOUNT. THE CRACK WAS 2.25 INCHES LONG AND THE BASE SKIN IS ONLY .020 INCH THOUSANDS THICK WITH NO REPAIR A LLOWED PER BEECH. FOUND ONE OTHER AIRCRAFT AFFECTED AND REPLACED BOTH RUDDER ASSEMBLIES. APPARENTLY CAUSED BY THE LACK OF SUPPORT/STRENGTH IN THIS AREA TO HANDLE THE FLEX OF THE STATIC WICK. (M) 2 L 7 2 4T RT A24CE 1996082200503 19960822 00503 CE 1996 8 22 S2YA960014 1 19960705 A 5542 130630000607 SKIN BEECH 1900 1900D 1154162 CE RUDDER CRACKED A S2YA K NONE O OTHER IN INSP/MAINT 1 GL 13 92SK 5302 UE92 DURING AN INSPECTION, MAINTENANCE FOUND THE TOP SIDE OF THE RUDDER CRACKED PERPENDICULAR AT THE FORWARD RIVET OF THE TOP STATIC WICK MOUNT. THE CRACK WAS 2 INCHES LONG AND THE BASE SKIN IS ONLY .020 INCH THOUSANDS THICK WITH NO REPAIR ALLO WED PER BEECH. FOUND ONE OTHER AIRCRAFT AFFECTED AND REPLACED BOTH RUDDER AS SEMBLIES. APPARENTLY CAUSED BY THE LACK O F SUPPORT/STRENGTH IN THIS AREA TO HANDLE THE FLEX OF THE STATIC WICK. (M) 2 L 7 2 4T RT A24CE 1996082200504 19960822 00504 CE 1996 8 22 S2YA960015 1 19960712 A 2810 FUEL TANK BEECH 1900 1900D 1154162 CE RT WING LEAKING A S2YA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 GL 13 81SK 5777 UE81 AFTER TAKEOFF, IT WAS NOTICED THAT FLUID (FUEL) WAS LEAKING FROM THE FIRST SEAM AFT OF THE RIGHT WING BOOT OUTBOARD OF N ACELLE AND FROM ABOVE THE RIGHT FLAP IN FLT. THE CREW DECIDED TO TURN BACK TO MKE. THIS LEAK WAS DEFERRED PREVIOUSLY A S WITHIN LIMITS. PRIOR TO THIS BEECH KIT NR 129-4012-1 WAS INSTALLED (3/19/95) WHICH WAS SUPPOSED TO FIX THE FIRST LEAK . BEECH REMOVED KIT NR 129-4012-1S AND INSTALLED KIT NR 129-4013-1. SUBMITTER STATES, THIS HAS NOW BEEN FIFTH RIGHT SP AR LEAK SINCE 3/19/95. (M) 2 L 7 2 4T RT A24CE 1996082200505 19960822 00505 1996 8 22 S2YA960016 4 19960712 A 3425 J095002J598013 EHSI BEECH 1900 1900D 1154162 CE FWD AVIONICS BAY FAILED A S2YA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 13 891SK 5495 UE89 FLT NR 1203 - AFTER TAKEOFF, IT WAS NOTICED THAT THE RIGHT EHSI FAILED IN FLT AND THE CREW DECIDED TO TURN BACK TO MKE. MAINTENANCE REPAIRED WIRE NR J095002-J598013 AND OPERATIONAL CHECKED GOOD. (M) 2 L 7 2 4T RT A24CE 1996082200506 19960822 00506 CE 1996 8 22 S2YA960017 1 19960714 A 3260 444EN496 SQUAT SWITCH BEECH 1900 1900D 1154162 CE RT MLG INOP A S2YA O OTHER J WARNING INDICATION CL CLIMB 1 GL 13 841SK 5736 UE84 FLT 1163 - DAY-MKE - AFTER TAKEOFF, IT WAS FOUND THAT THE LANDING GEAR WOULD NOT RETRACT. THE CREW DECIDED TO CONTINUE ON TO MKE. MAINTENANCE FOUND THE RIGHT SQUAT SWITCH TO BE BAD AND REPLACED IT, OPERATIONAL CHECKED GOOD. (M) 2 L 7 2 4T RT A24CE 1996082200507 19960822 00507 CE 1996 8 22 S2YA960018 1 19960714 A 7931 1013890235 TRANSDUCER BEECH 1900 1900D 1154162 CE LT ENGINE INOP A S2YA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 13 118SK 5736 5736 48154151 UE108 ON TAKEOFF ROLL AT MKE, THE FLIGHT NR 1062 REPORTED LEFT ENGINE OIL PRESSURE PEGGED OUT AT 200 PSI. ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE LEFT OIL PRESSURE TRANSDUCER, OPERATIONAL AND LEAKED CHECK GOOD. (M) 2 L 7 2 4T RT A24CE 1996082200508 19960822 00508 CE 1996 8 22 S2YA960019 1 19960712 A 3260 951F04 LAMPS BEECH 1900 1900D 1154162 CE LT ANNUN PNL FAILED A S2YA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 13 87SK UE87 THE CREW NOTICED THAT THE RIGHT LANDING GEAR GREEN DOWN AND LOCKED ANNUNCIATOR WOULD NOT ILLUMINATE ON APPROACH TO MKE ( FLT NR 1197). VERIFIED THAT THE GEAR WAS DOWN AND LOCKED AND PROCEEDED TO LAND. MAINTENANCE WAS CALLED AND REPLACED BO TH LAMPS IN THE ANNUNCIATOR, OPERATIONAL CHECKED GOOD. SUBMITTER STATES, A VERY COMMON PROBLEM FOR US AND OTHER OPERATO RS. (M) 2 L 7 2 4T RT A24CE 1996082200509 19960822 00509 EU 1996 8 22 SIMA962001 1 19960718 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 223AT 3364 223 SGF - DURING MAINTENANCE CHECK, EMERGENCY FLOOR LIGHTS NR 2, NR 4 AND NR 6 WERE INOP. RAI'D BATTERY PACK DUE TO A PIN I N THE CONNECTION WAS BROKEN OFF. THE SYSTEMS OPS CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996082200510 19960822 00510 EU 1996 8 22 SIMA962041 1 19960722 A 3350 3011180 POWER SUPPLY AEROSP ATR42 ATR42300 8680920 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 249AT 644 0249 DFW - DURING PHASE 3 INSPECTION OF POWER SUPPLY 30WL, OPERATION WAS INTERMITTENT. RAI'D POWER SUPPLY UNIT. OPS CHECK G OOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996082200511 19960822 00511 EU 1996 8 22 SIMA962051 1 19960723 A 3350 30111151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 423MQ 3519 030 GRR - FORWARD EMERGENCY LIGHTS IN OP. REMOVED AND REPLACED BATTERY PACK AT 3WL (FOUND PACK TO BE LEAKING). OPERATIONAL CHECK SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996082200512 19960822 00512 EU 1996 8 22 SIMA962082 1 19960726 A 2450 E0242A115 RELAY AEROSP ATR72 ATR72212 EU AC DISTR SYS FAILED A SIMA K NONE J WARNING INDICATION CR CRUISE 1 SW 21 288AM 288 ORD - FLT 4383 - NR 2 ACW BUS OFF INTERMITTENT IN FLIGHT AND ON GROUND AFTER LANDING. NO EQUIPMENT FAILURES NOTED WITH BUS OFF INDICATION. RAI'D RELAY 6XN IN 94VU. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996082200513 19960822 00513 EU 1996 8 22 SIMA962101 1 19960728 A 3350 3011210 LIGHT AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 265AE 183 266 DFW - FLT 3665 - EMERGENCY LIGHT ON MAIN CABIN DOOR INOP. RAI'D EMERGENCY LIGHT ASSEMBLY IAW AMM. OPS CHECK GOOD. AIR CRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996082200514 19960822 00514 EU 1996 8 22 SIMA962111 1 19960729 A 2910 MS219126 TEE FITTING AEROSP ATR42 ATR42300 8680920 EU GREEN HYD SYS FAILED A SIMA K NONE K FLUID LOSS AP APPROACH 1 SW 21 12MQ 012 SGF - FLT 4076 - APPROACH TO SGF AFTER SELECTING GEAR DOWN, GREEN LOW LEVEL CAUTION ILLUMINATED. FOUND TEE TO GREEN ACC UMULATOR SHEARED AND RESULT WAS LOSS OF FLUID. RAI'D TEE FITTING AND ASSOCIATED PACKINGS. AIRCRAFT WAS RETURNED TO SER VICE. (M) 2 H 7 2 4T RT A53EU 1996082200515 19960822 00515 EU 1996 8 22 SIMA962121 1 19960730 A 3350 3011201 LIGHT AEROSP ATR72 ATR72202 8680940 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 252AM 253 IND - FLT 4090 - FOUND EMERGENCY STAIR LIGHT INOP. RAI'D LIGHT ASSEMBLY, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERV ICE. (M) 2 H 7 2 4T RT A53EU 1996082200516 19960822 00516 EU 1996 8 22 SIMA962122 1 19960730 A 3350 3011210 LIGHT AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 427MQ 091 ORD - FLT 4137 - FOUND ENTRANCE DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT ASSY. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996082200517 19960822 00517 EU 1996 8 22 SIMA962131 1 19960731 A 3350 52113091 LIGHT AEROSP ATR72 ATR72212 EU CABIN MISSING A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 410AT 410 ORD - FOUND SECOND FROM LAST EMERGENCY FLOOR LIGHT MISSING. INSTALLED NEW EMERGENCY FLOOR LIGHT ASSEMBLY. OPS CHECK GO OD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996082200518 19960822 00518 EU 1996 8 22 SIMA962141 1 19960801 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 424MQ 3632 045 DFW - DURING THE PHASE 2 CHECK, EXIT LIGHT OVER FORWARD EXIT DOORS WAS INOP. BATTERY CONTACT BROKEN ON BATTERY PACK. R AI'D BATTERY PACK, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996082200519 19960822 00519 NM 1996 8 22 SWXA960252 1 19960515 A 5347 501499 SEAT TRACK BOEING 737 7372M8 1384483 NM BS 947-967 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 141AW 21955 PAE - FLT 7812 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CORROSION ON SEAT TRACK BS 947-967, LBL 25, WL 20 8. REMOVED AND INSTALLED FABRICATED SEAT TRACK AT BS 947-967, LBL 25, WL 208 PER SRM 51-30-2, 51-10-1 AND 51-30-8. ALO DINED AND PRIMED. (M) 2 L 7 2 4F A16WE 1996082200520 19960822 00520 NM 1996 8 22 TWRA96199 1 19960722 A 3350 CL307 BULB BOEING 747 747124 1384874 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 602FF 19734 DURING DAILY CHECK, FOUND 5R MED SIDEWALL EXIT EVAC LIGHT INOP. RELAMPED, OPS CHECK NORMAL PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996082200521 19960822 00521 NM 1996 8 22 USAA960538 1 19960724 A 5315 FLOOR BEAM BOEING 737 7374B7 1384702 NM BS 344 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 19209 24556 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES FLOOR BEAM BS 344 BBL '0' TO LBL 43. INSTALLED NEW SECTION OF 'T' CAP, REPAIRED PER TR 53-10-3. CORROSION TASK NR C53-107-02, CORROSION LEVE L 1. (M) 2 L 7 2 4F RT A16WE 1996082200522 19960822 00522 NM 1996 8 22 USAA960539 1 19960724 A 5315 FLOOR BEAM BOEING 737 7374B7 1384702 NM BS 312 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 19209 24556 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND CAP HOLES FLOOR BEAM BS 312 BL 0 TO LBL 28. SPLICED 'T ' CAP AND DOUBLERS, REPAIRED PER TR 53-10-13. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996082200523 19960822 00523 NM 1996 8 22 USAA960540 1 19960724 A 5315 FLOOR BEAM BOEING 737 7374B7 1384702 NM BS 967 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 19209 24556 INT - DURING Q-4 CHECK VISUAL INSPECTION, CORROSION .25 INCH SQUARE FLOOR BEAM BS 967 LBL 18. INSTALLED DOUBLERS, REPAI RED PER SRM 53-30-51. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996082200524 19960822 00524 NM 1996 8 22 USAA960541 1 19960724 A 5315 FLOOR BEAM BOEING 737 7374B7 1384702 NM BS 987 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 19209 24556 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH TO 2 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES TOP OF FLOOR BEAM BS 987 RBL 48 TO LBL 48. CUT OFF T-CAP, FABRICATED NEW T-CAP HALVES, SPLICE AND INSTALLED. REPAIRED PER EA 41291 . CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996082200525 19960822 00525 NM 1996 8 22 USAA960542 1 19960724 A 5320 SHEAR WEB BOEING 737 7374B7 1384702 NM BS 500 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 19209 24556 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND TWO 2 INCH CRACKS SHEAR WEB BS 500 G PLUS 5 INCH AND BS 500 G PLUS 15 IN CH AT RBL 45. FABRICATED NEW SHEAR WEB AND INSTALLED, REPAIRED PER BOEING DRAWING 69-35366. (M) 2 L 7 2 4F RT A16WE 1996082200526 19960822 00526 NM 1996 8 22 USAA960543 1 19960724 A 5315 FLOOR BEAM BOEING 737 7374B7 1384702 NM BS 947 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 19209 24556 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER AREAS OF CORROSION STATION 947 FLOOR BEAM UPPER CHORD AT CLIP NUT HOLES. CUT OUT DAMAGED CAP SECTION AND SPLICED IN NEW SECTION PER EA 41312 AND SRM 53-00-51 FIG 202. REPAIRE D PER EA 41312 SRM 53-00-51 FIG 202. CORROSION TASK NR C53-107-02. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. ( M) 2 L 7 2 4F RT A16WE 1996082200527 19960822 00527 NM 1996 8 22 USAA960544 1 19960724 A 5754 SKIN BOEING 737 7374B7 1384702 NM NR 1 LE SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 19209 24556 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND THREE .5 INCH CRACKS NR 1 SLAT LOWER SKIN SLAT STATION 299.10. CUT OUT CRACKED SKIN, INSTALLED FILLER AND DOUBLER. (M) 2 L 7 2 4F RT A16WE 1996082200528 19960822 00528 WP 1996 8 22 USAAD96101 1 19960711 A 3350 A3060339101 LIGHT DOUG DC9 DC931 3022065 WP CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 938VJ 48119 GALLEY DOOR SLIDE EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY. (M) 2 L 7 2 4F A6WE 1996082200529 19960822 00529 WP 1996 8 22 USAAD96104 1 19960714 A 2613 TEMP SENSORS DOUG DC9 DC982 3022082 WP TAIL COMPT FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 817US 48097 FLT NR 1665 - PIT-FLL - 'TAIL COMPT TEMP HIGH' LIGHT ILLUMINATED DURING CLIMB. RETURNED TO FIELD. REPLACED WIRING BETW EEN TAIL COMPARTMENT TEMPERATURE SENSORS AND AFT PRESSURE BULKHEAD. (M) 2 L 7 2 4F A6WE 1996082200530 19960822 00530 NE 1996 8 22 USAAD96105 2 19960714 A 7250 T4 BLADES DOUG DC9 DC981 3022081 WP PWA JT8 JT8D217 52053 NE RT ENGINE FRACTURED A USAA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 EA 19 809US 48041 708514 SDF/PIT - FLT 2288 - ON DESCENT, HEARD THUMP ON RIGHT FUSELAGE AREA. ON FINAL, AT 1,000 FEET, RIGHT ENGINE WOULD NOT RE SPOND TO POWER INPUT. AIRCRAFT LANDED, AND CREW NOTED RIGHT ENGINE EGT WAS CLIMBING, AND SHUT DOWN THE ENGINE. REPLACE D ENGINE. FOUND ALL T4 BLADES FRACTURED NEAR ROOT. (X) 2 L 7 2 4F 4 F A6WE E9NE 1996082200531 19960822 00531 WP 1996 8 22 USAAD96110 1 19960726 A 5242 DOOR DOUG DC9 DC931 3022065 WP E/E COMPT NOT LATCHED A USAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 19 933VJ 47216 FLT NR 7003 - BNA-BOS - AFTER TAKEOFF, GOT VIBRATION FROM NOSE AREA. RETURNED TO FIELD. CLOSED E/E COMPT DOOR. (M) 2 L 7 2 4F A6WE 1996082200532 19960822 00532 NM 1996 8 22 USAASB96137 1 19960725 A 3397 WIRE BOEING 737 7372B7 1384560 NM CABIN SHORTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 266AU 22878 LGA - MAINTENANCE FOUND THE FORWARD CABIN FLOOR TRACK EMERGENCY LIGHTS INOP. ALSO, FOUND INOP WERE THE MAIN ENTRY DOOR AND SERVICE DOOR EXIT IDENTIFIERS. MAINTENANCE FOUND THE MAIN ENTRY DOOR EXIT IDENTIFIER LIGHT WIRING SHORTED OUT. REW IRED EXIT IDENTIFIER LIGHT. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1996082200533 19960822 00533 NM 1996 8 22 USAASB96138 1 19960725 A 3260 INDICATION BOEING 737 7373B7 1384580 NM LANDING GEAR MALFUNCTIONED A USAA O OTHER O OTHER AP APPROACH 1 EA 19 516AU 23702 CLT - FLT 57 - UPON LOWERING LANDING GEAR INTO CLT, CREW RECEIVED RED RIGHT MAIN GEAR LIGHT. GREEN RIGHT MAIN GEAR LIGH T WAS OFF. CREW RECYCLED GEAR AND ALL GEAR INDICATIONS WERE NORMAL. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENAN CE CHECKED GEAR WARNING AND POSITION SYSTEM PER MM 32-09-20. COMPLIED WITH GEAR LUBE. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996082200534 19960822 00534 NM 1996 8 22 usaasb96139 1 19960725 A 2170 23404061 COALESCER BAG BOEING 737 7374B7 1384702 NM AIR COND BAY FAILED A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 19 429US 24551 DEN-PIT - FLT 132 - CREW REPORTED A SMOKE TYPE SMELL IN THE COCKPIT AND FORWARD CABIN. SMELL IS STRONGEST IN THE COCKPI T. HAPPENS AT DIFFERENT FLIGHT CONDITIONS. SUSPECT LEFT PACK. MAINTENANCE REPLACED THE LEFT PACK SECONDARY (REAR) WAT ER EXTRACTOR. RAN PACKS OFF OF APU AND ENGINES. NO SMELL NOTED. OPERATES NORMAL. (M) 2 L 7 2 4F RT A16WE 1996082200535 19960822 00535 NM 1996 8 22 USAASB96140 1 19960726 A 3350 AD20131A BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 441US 24812 TPA - MAINTENANCE FOUND THE FOLLOWING EMERGENCY LIGHTS WOULD NOT ILLUMINATE, 10R, 12L AND 20L OVERHEADS, RIGHT OVERWING AND LEFT LOWER FUSELAGE LIGHTS. MAINTENANCE REPLACED THE BATTERY PACK IN OVERHEAD AT STATION 753L. OPS CHECK GOOD. (M ) 2 L 7 2 4F RT A16WE 1996082200536 19960822 00536 NM 1996 8 22 USAASB96141 1 19960728 A 2910 106056318 HYD HOSE BOEING 737 737201 1384454 NM NR 2 STRUT LOOSE A USAA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 241US 22443 PVD - FL 381 - SHORTLY AFTER TAKEOFF FROM BOS, A STRONG UNIDENTIFIABLE SMELL OCCURRED IN THE CABIN. THE SMELL TAPERED O FF DURING CLIMB-OUT, BUT CAME BACK VERY STRONG WHEN LEVELING AT FL 310. FLIGHT DIVERTED TO PVD. NO EMERGENCY WAS DECLA RED AND THE FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND HYDRAULIC LEAK AT HOSE ASSEMBLY B-NUT AT THE NR 2 STRUT/ENGINE. LEAK WAS RUNNING INTO PRECOOLER. SECURED B-NUT ON HOSE ASSEMBLY AND REPLACED BOTH WATER SEPARATOR BAGS. RAN ENGINE AND APU TO CHECK AIR CONDITIONING SYSTEM. CHECKS GOOD. NO LEAKS OR SMELL NOTED. (M) 2 L 7 2 4F A16WE 1996082200537 19960822 00537 NM 1996 8 22 USAASB96142 1 19960728 A 2150 204050101 ACM BOEING 737 737301 1384611 NM RT AIR COND BAY FAILED A USAA A B UNSCHED LANDING EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 19 334US 53465 30261 23231 PIT - FL 358 - EN ROUTE FROM DCA TO MCI AT FL 350, ALTITUDE WARNING HORN SOUNDED. NO OTHER COCKPIT INDICATIONS WERE ILL UMINATED. COCKPIT CABIN INDICATOR SHOWED CABIN AT 10,000 FEET AND RISING. EMERGENCY DESCENT WAS MADE AND THE FLIGHT DI VERTED TO PIT. DEPLOYMENT OF OXYGEN MASKS WAS NOT NECESSARY. THE FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT AIR CYCLE MACHINE. OPS CHECK AND LEAK CHECK OK. (M) 2 L 7 2 4F RT A16WE 1996082200538 19960822 00538 NM 1996 8 22 USAASB96143 1 19960729 A 3610 1074845 REGULATOR BOEING 737 7374B7 1384702 NM NR 1 ENGINE FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 782AU 25021 CLT - FLT 8053 - DUCT PRESSURE AT CRUISE POWER WAS 5 PSI LEFT SIDE, 46 PSI RIGHT SIDE. RIGHT BLEED TRIP OFF LIGHT ILLUM INATED AND CABIN STARTED CLIMBING. CREW REDUCED POWER ON NR 2 ENGINE AND RESET BLEED TRIP. CABIN STOPPED CLIMBING, HOW EVER, RIGHT BLEED TRIPPED AGAIN. CABIN STARTED CLIMBING AGAIN. FLIGHT DIVERTED TO CLT AND LANDED WITH NO FURTHER INCID ENT. MAINTENANCE REPLACED THE NR 1 ENGINE HIGH STAGE REGULATOR PER MM. RAN BOTH ENGINES. ALL PNEUMATIC INDICATIONS NO RMAL. (M) 2 L 7 2 4F RT A16WE 1996082200539 19960822 00539 NM 1996 8 22 USAASB96144 1 19960729 A 3233 654491012 ACTUATOR BOEING 737 7373B7 1384580 NM RT MLG FAILED A USAA A L UNSCHED LANDING ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 19 516AU 29564 23702 IAD - FL 2116 - ON APPROACH TO DCA AT 3,200 FEET, AN UNSAFE RIGHT GEAR INDICATION WAS NOTED. CREW RECYCLED GEAR AND DID A TOWER FLYBY. TOWER REPORTED GEAR LOOKED DOWN AND LOCKED. CREW EXECUTED MISSED APPROACH AND HELD WHILE RUNNING CHECK LIST AND TRYING MANUAL DEPLOYMENT. STILL RECEIVED UNSAFE LIGHT. CAPTAIN DECIDED TO DIVERT TO IAD. NO EMERGENCY WAS DE CLARED AND THE FLIGHT LANDED SAFELY WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT MAIN LANDING GEAR ACTUATOR . ADJUSTMENT AND TEST PER MAINTENANCE MANUAL CHECKS GOOD. (M) 2 L 7 2 4F RT A16WE 1996082200540 19960822 00540 NM 1996 8 22 USAASB96145 1 19960730 A 3350 900835A BATTERY PACK BOEING 737 737201 1384454 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 247US 22754 ROC - MAINTENANCE FOUND EMERGENCY AISLE LOW LEVEL LIGHTING INOP AT ROWS 7, 9, 11, 12, AND 13 LEFT SIDE. MAINTENANCE REP LACED BATTERY PACK AT ROW 12. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1996082200541 19960822 00541 EU 1996 8 22 VTZ96265 1 19960719 A 3260 AIR135022 UPLOCK SWITCH JETAIR JETSTM JETSTM4101 1500501 EU RT MLG FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 310UE 41028 FLT NR 6222 - JFK-IAD - DURING CLIMB-OUT, RETURNED TO JFK DUE TO RED GEAR HANDLE LIGHT REMAINED ILLUMINATED AFTER GEAR S ELECTED UP. AIRCRAFT LANDED AT JFK WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED RIGHT GEAR UPLOCK SWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996082200542 19960822 00542 EU 1996 8 22 VTZA96239 1 19960701 A 7722 8972052C EGT COMPENSATOR BAG JETSTM JETSTM3201 1500217 EU RT ENGINE OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 483UE 898 FLT NR 6173 - IAD-HVN - ABORTED TAKEOFF DUE TO THE RIGHT ENGINE BEING TORQUE AND TEMP LIMITED. AIRCRAFT RETURNED TO GAT E WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED THE EGT COMPENSATION FOR THE RIGHT ENGINE. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996082200543 19960822 00543 WP 1996 8 22 VTZA96244 2 19960706 A 7260 5725109162 CHIP DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE3311 01514 WP RT ENGINE DIRTY A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 314UE 41027 FLT NR 6502 - JFK-IAD - DURING CLIMB-OUT, MADE AN UNSCHEDULED LANDING AT JFK DUE TO RIGHT ENGINE OIL CONTAMINATION LIGHT ILLUMINATING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE CLEANED CHIP DETECTOR. ENGINE RUN AND OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 3 T RT A41NM E3WE 1996082200544 19960822 00544 EU 1996 8 22 VTZA96248 1 19960706 A 7722 TRANSDUCER BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 481UE 895 FLT NR 6446 - DURING TAKEOFF, RETURNED TO IAD DUE TO LEFT ENGINE DID NOT MAKE POWER. AIRCRAFT RETURNED TO GATE AT IAD W ITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI 09096 ON SRL COMPUTER. MAINTENANCE CLEARED DMI 09096, BY REPLACING LE FT DELTA P/P TRANSDUCER. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996082200545 19960822 00545 1996 8 22 VTZA96273 3 19960724 A 6140 865956 BETA SWITCH BAG JETSTM JETSTM3201 1500217 EU LEFT FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 487UE 906 FLT NR 6284 - IAD-HPN - ABORTED TAKEOFF DUE TO THE LEFT BETA LIGHT ILLUMINATED WHEN ADVANCING THE POWER LEVERS AND INCRE ASED THE AIRSPEED THROUGH 90 KNOTS. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLA CED LEFT BETA SWITCH, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996082200546 19960822 00546 EU 1996 8 22 VTZA96276 1 19960725 A 7712 TQ SIGNAL COND BAG JETSTM JETSTM3201 1500217 EU NR 2 ENG OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 27 478UE 892 FLT NR 6521 - IAD-BDL - ABORTED TAKEOFF DUE TO NR 2 ENGINE ONLY MAKING 90 PERCENT TORQUE (95 PERCENT TARGET). AIRCRAFT RETURNED TO GATE AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE RECALIBRATED TORQUE SIGNAL CONDITIONER, OPS CHECK OK. A IRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996082200547 19960822 00547 EU 1996 8 22 VTZA96278 1 19960719 A 5270 91SE16 SWITCH BAG JETSTM JETSTM3201 1500217 EU BAGG DOOR OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 491UE 911 FLT NR 6206 - IAD-CMH - ABORTED THE TAKEOFF DUE TO POD DOOR LIGHT ILLUMINATED ON TAKEOFF. AIRCRAFT RETURNED TO GATE WIT H NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI 18293, MEL 52-3. MAINTENANCE CLOSED DMI 18293 ON 7-22-96 BY ADJUSTING M ICROSWITCH. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996082200548 19960822 00548 EU 1996 8 22 VTZA96279 1 19960718 A 5270 91SE16 SWITCH BAG JETSTM JETSTM3201 1500217 EU BAGG DOOR OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 497UE 904 FLT NR 6401 - IAD-SWF - ABORTED TAKEOFF DUE TO POD BAGGAGE DOOR CAPTION ILLUMINATED DURING TAKEOFF. AIRCRAFT RETURNED T O GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 55120 IAW MEL 52-3-2. MAINTENANCE CLOSED DMI 55120 ON 7-22 -96 BY ADJUSTING MICROSWITCH. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996082200549 19960822 00549 EU 1996 8 22 VTZA96280 1 19960718 A 7712 8973312 TTL VLV BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 27 494UE 810 FLT NR 6177 - IAD-PIT - ABORTED TAKEOFF DUE TO LEFT ENGINE TORQUE DROPPED AND THEN SURGED. AIRCRAFT RETURNED TO GATE WI TH NO FURTHER INCIDENTS. MAINTENANCE DEFERRED TTL, OPENED DMI 42445, MEL 76-20. MAINTENANCE CLOSED DMI 42445 ON 7-25-9 6 BY REPLACING TTL VALVE. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996082200550 19960822 00550 NM 1996 8 22 W8PA960053 1 19960514 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 462 DENTED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 947WP 23376 FOUND A DENT AT BS 462, LBL 49, WL 164, BETWEEN STRINGER 22L AND 23L. REMOVED DAMAGED AREA AND INSTALLED DOUBLER IAW SR M 53-00-03. (M) 2 L 7 2 4F RT A16WE 1996082200551 19960822 00551 EU 1996 8 22 WTAA960147 2 19960701 A 7320 8974575 BYPASS VALVE BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110U 01514 WP LT ENG FUEL FAILED A WTAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 WP 17 103XV 747 RDM - LEFT ENGINE TORQUE AND EGT FLUCTUATION REPORTED AFTER TAKEOFF POWER APPLIED ON TAKEOFF ROLL. TAKEOFF ABORTED WITH OUT INCIDENT. DEFERRED TTL SYSTEM PER MEL 76-2. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERR AL BY REPLACING TTL BYPASS VLV. (M) 2 L 7 2 4T 4 T RT A21EU E4WE 1996082200552 19960822 00552 EU 1996 8 22 Y2PA96050 1 19960719 A 2822 540BHD JET PUMP AMD FALC20 FALCOND 2720304 EU LT WING CLOGGED A Y2PA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 23 811AA 187 ELP - WHEN FUEL WAS NOT ABLE TO TRANSFER PROPERLY FROM RIGHT TO LEFT WING, THE CREW RETURNED TO POINT OF DEPARTURE AT EL P. NO EMERGENCY PROCEDURES WERE REQUIRED. MAINTENANCE FOUND THAT THE LEFT WING INTERCONNECT JET PUMP WAS CLOGGED. THE OBSTRUCTION WAS REMOVED AND THE PUMP REINSTALLED. PERFORMED A LEAK AND OPERATIONS CHECK IAW FALCON MM CHAP 28-10-3. N O DEFECTS WERE NOTED. (M) 2 L 7 2 4F A7EU 1996082200553 19960822 00553 SO 1996 8 22 RAAA96E4011 1 19960820 A 3350 8621014 BATTERY PACK INTVLV 873100112 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 9744C 188C1140 LT OVERWING EXIT EGRESS INDENTIFIER LIGHT ASSEMBLY FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. 2 L 7 4 4T 4A22 1996082200554 19960822 00554 SO 1996 8 22 RAAA96E4012 1 19960820 A 3350 8621014 BATTERY PACK INTVLV 873100112 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 9744C 188C1140 RT OVERWING EXIT EGRESS IDENTIFIER LIGHT ASSEMBLY FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. 2 L 7 4 4T 4A22 1996082200555 19960822 00555 WP 1996 8 22 CALA9601190 1 19960730 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 160 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND LONGERON 4L CRACKED AT STA 160. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 53-02, FIGURE 2. 2 L 7 2 4F A6WE 1996082200556 19960822 00556 WP 1996 8 22 CALA9601191 1 19960730 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 200 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND LONGERON 4L CRACKED AT STA 200. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 53-02, FIGURE 2. 2 L 7 2 4F A6WE 1996082200557 19960822 00557 WP 1996 8 22 CALA9601192 1 19960730 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 160 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND LONGERON 3L CRACKED AT STA 160. THE CRACKED SECTION OF LONGERON WAS REMOVED AND A NEW SECTION WAS SPLI CED IN IAW SRM 53-02, FIGURE 2. 2 L 7 2 4F A6WE 1996082200558 19960822 00558 WP 1996 8 22 CALA9601193 1 19960728 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 484 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND A .5 INCH CRACK ON FLOOR SUPPORT IN FORWARD CARGO COMPARTMENT AT STA 484, LONGERON 24R. A DOUBLER WAS INSTALLED IAW ECRA 5320C01263. 2 L 7 2 4F A6WE 1996082200559 19960822 00559 WP 1996 8 22 CALA9601194 1 19960806 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 594 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 594, LONGERON 17R. THE CORROSION WAS REMOVED AND AN INTERNAL DOUBLER WAS INSTALLED IAW ECRA 5330-02427. 2 L 7 2 4F A6WE 1996082200560 19960822 00560 WP 1996 8 22 CALA9601195 1 19960801 A 5522 SKIN DOUG DC9 DC932 3022066 WP RT ELEVATOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND A 5 INCH CRACK IN RT ELEVATOR LOWER SKIN AT STA XHS 86.0. AN EXTERNAL DOUBLER WAS INSTALLED IAW ECRA 5 530-01174 AND SRM 55-03, FIGURE 13. 2 L 7 2 4F A6WE 1996082200561 19960822 00561 WP 1996 8 22 CALA9601196 1 19960727 A 5230 BEAM DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND A 1.5 INCH CRACK IN FORWARD CARGO COMPARTMENT DOOR BEAM AT UPPER FORWARD STOP. A REPAIR WAS DONE IAW S RM 51-30-2. 2 L 7 2 4F A6WE 1996082200562 19960822 00562 WP 1996 8 22 CALA9601197 1 19960727 A 5230 BEAM DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND A 1.5 INCH CRACK IN AFT CARGO COMPARTMENT DOOR BEAM AT UPPER FORWARD STOP. THE BEAM WAS REMOVED AND RE PLACED IAW SRM 52-01, FIGURE 1. 2 L 7 2 4F A6WE 1996082200563 19960822 00563 WP 1996 8 22 CALA9601198 1 19960730 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 737 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND LONGERON 5R CRACKED AT STA 737. A NEW SECTION OF LONGERON WAS SPLICED IN IAW SRM 53-02, FIGURE 2. 2 L 7 2 4F A6WE 1996082200564 19960822 00564 WP 1996 8 22 CALA9601199 1 19960727 A 5230 FITTING DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND A .375 INCH CRACK IN AFT CARGO COMPARTMENT DOOR FITTING INSIDE DOOR AT BOTTOM CENTER STOP. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1996082200565 19960822 00565 WP 1996 8 22 CALA9601200 1 19960727 A 5230 BEAM DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND A .75 INCH CRACK IN FORWARD CARGO COMPARTMENT DOOR BEAM AT LOWER FORWARD STOP. A NEW PART WAS FABRICAT ED AND INSTALLED IAW SRM 51-30-3. 2 L 7 2 4F A6WE 1996082200566 19960822 00566 WP 1996 8 22 CALA9601201 1 19960727 A 5712 RIB DOUG DC9 DC932 3022066 WP NR 1 SLAT TRACK CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND A 1 INCH CRACK IN WING LEADING EDGE RIB AT NR 1 SLAT TRACK. THE RIB WAS REPAIRED IAW ECRA 5710-01751. 2 L 7 2 4F A6WE 1996082200567 19960822 00567 WP 1996 8 22 CALA9601202 1 19960728 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 1143 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND A CRACK IN FRAME JUST FORWARD OF RUDDER TRIM MOUNT AT TAIL COMPARTMENT STA 1143. A NEW ANGLE WAS INSTA LLED ON FRAME IAW SRM 51-10-4. 2 L 7 2 4F A6WE 1996082200568 19960822 00568 NM 1996 8 22 9618132716 1 19960816 A 2613 OVERHEAT LOOP BOEING 727 7272S7 138407Z NM NR 3 STRUT OUT OF POSITION A NWAA A J UNSCHED LANDING DUMP FUEL N FALSE WARNING CL CLIMB 1 GL 01 720RC 22491 NR 3 STRUT OVERHEAT LIGHT ILLUMINATED, SHUT DOWN NR 3 ENGINE, LIGHT REMAINED ILLUMINATED. AIRCRAFT DIVERTED TO ABQ, DUM PED FUEL AND LANDED WITHOUT INCIDENT. REPOSITIONED NR STRUT OVERHEAT LOOP. INSPECTED STRUT AND RAN NR 3 ENGINE AT 1.65 EPR FOR 5 MINUTES, GROUND CHECK OK. 2 L 7 3 4F A3WE 1996082200569 19960822 00569 NM 1996 8 22 9618142276 1 19960816 A 2720 RUDDER BOEING 727 727251 138408H NM EMPENNAGE OSCILLATION A NWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 01 276US 21155 SHORTLY AFTER TAKEOFF, NOTICEABLE RUDDER OSCILLATION. RETURNED TO MEM AND LANDED WITHOUT INCIDENT. PERFORMED RUDDER AN D YAW DAMPER CHECK, SYSTEM OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996082200570 19960822 00570 NM 1996 8 22 SWAA960835 1 19960819 A 5240 LATCHES BOEING 737 7373A4 1384585 NM LAV SERVICE DOOR LOOSE A SWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 07 680SW 23505 AFTER TAKEOFF, NOTED AIRFRAME VIBRATION IN FWD SECTION OF FUSELAGE. AIRCRAFT RETURNED TO PDX AND MADE AN UNEVENTFUL LAN DING. INSPECTED AND FOUND FWD LAVATORY SERVICE DOOR LATCHES LOOSE. TEMP REPAIRED LATCHES AND DEFERRED PER MPM. REPLAC ED HINGE AND LATCH ASSEMBLIES PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996082200571 19960822 00571 NM 1996 8 22 SWAA960836 1 19960819 A 3350 CHARGERS BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 510SW 24187 DURING SCHEDULED TERMINAL CHECK, FOUND FWD ENTRY AND FWD SERVICE DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BOTH BATTERY CHARGERS ASSEMBLIES PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996082200572 19960822 00572 NM 1996 8 22 SWAA960837 1 19960819 A 2150 20405011 ACM BOEING 737 7375H4 138449D NM CABIN FAILED A SWAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 07 522SW 26564 HOT AIR AND SMOKE ENTERED CABIN AND COCKPIT AREAS DURING TAXI OUT. RETURNED TO GATE. REMOVED AND REPLACED NR 1 AIR CYC LE MACHINE DUE TO SEVERE OIL LEAK, ALONG WITH DISCHARGE SENSOR AND BAG PER BOEING M/M. ALSO, REMOVED AND REPLACED NR 2 AIR CYCLE MACHINE AND BAG AS PRECAUTIONARY PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996082200573 19960822 00573 NM 1996 8 22 SWAA960838 1 19960819 A 3350 900835A BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 73SW 22673 DURING SCHEDULED TERMINAL CHECK, FOUND EMERGENCY EXIT LIGHTS INOP BETWEEN OVERWING EMERGENCY EXITS INOP. REMOVED AND R EPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F A16WE 1996082200574 19960822 00574 NM 1996 8 22 SWAA960839 1 19960817 A 3350 20131 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 399SW 27693 DURING SCHEDULED A2 CHECK, FOUND LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996082200575 19960822 00575 NM 1996 8 22 SWAA960840 1 19960816 A 3350 BULB BOEING 737 7373H4 1384600 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 385SW 26600 DURING SCHEDULED B/C CHECK, FOUND RIGHT SIDE EMERGENCY EXIT LIGHTS INOP. RELAMPED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996082200576 19960822 00576 NM 1996 8 22 SWAA960841 1 19960816 A 3350 1000679 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 91SW 22963 DURING SCHEDULED TERMINAL CHECK, FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PE R BOEING M/M. 2 L 7 2 4F A16WE 1996082200577 19960822 00577 NM 1996 8 22 SWAA960842 1 19960816 A 3350 1000679 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 82SW 22731 DURING SCHEDULED TERMINAL CHECK, FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT REMAINING ILLUMINATED AT ALL TIMES. REMOVE D AND REPLACED LIGHT ASSEMBLY PER BOEING M/M. 2 L 7 2 4F A16WE 1996082200578 19960822 00578 NM 1996 8 22 SWAA960843 1 19960816 A 5320 CLIPS BOEING 737 7372H4 138448C NM BS 727/867 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 74SW 22674 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CORRODED AT BS 727A, S21R AND AT BS 867, S19L. REPLACED BOTH PER BOEING SRM. 2 L 7 2 4F A16WE 1996082200579 19960822 00579 NM 1996 8 22 SWAA960844 1 19960816 A 5320 STRINGER BOEING 737 7372H4 138448C NM BS 907 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 74SW 22674 DURING SCHEDULED D-CHECK, FOUND STRINGER CORRODED AT BS 907, S25L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996082200580 19960822 00580 NM 1996 8 22 SWAA960845 1 19960816 A 3350 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 52SW 21533 FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER BOEING M/M. 2 L 7 2 4F A16WE 1996082200581 19960822 00581 NM 1996 8 22 SWAA960846 1 19960818 A 3350 20121 HOUSING BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 510SW 24187 DURING SCHEDULED SERVICE CHECK, FOUND BOTH FWD ENTRY DOORS EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED LT LIGHT SO CKET AND RT AND LT BATTERY PACK HOUSINGS PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996082200582 19960822 00582 NM 1996 8 22 SWAA960847 1 19960820 A 3350 6104791 POWER SUPPLY BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 74SW 24187 DURING RON CHECK, FOUND LEFT AFT ENTRY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY POWER SUPPLY PER BOEING M/M. 2 L 7 2 4F A16WE 1996082200583 19960822 00583 NM 1996 8 22 SWAA960848 1 19960818 A 5315 FLOOR BEAM BOEING 737 7372H4 138448C NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 74SW 24187 DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORROSION AT BS 328, RBL 14, 18, 33, 37 AND 56.5. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996082200584 19960822 00584 NM 1996 8 22 SWAA960849 1 19960818 A 5315 FLOOR BEAM BOEING 737 7372H4 138448C NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 74SW 24187 DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORROSION AT BS 344, LBL 28. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996082200585 19960822 00585 NM 1996 8 22 SWAA960850 1 19960820 A 3350 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 355SW 25250 DURING SCHEDULED 1/2 D-CHECK, FOUND EMERGENCY EXIT LIGHTING INOP IN VARIOUS CABIN LOCATIONS. REPLACED BATTERY PACKS PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996082200586 19960822 00586 NM 1996 8 22 SWAA960851 1 19960820 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 970 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 316SW 23338 DURING SCHEDULED C4 CHECK, FOUND AFT FUSELAGE SKIN CRACKED AT BS 970, S21L AND AT BS 944 AT S24L. REPAIRED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1996082200587 19960822 00587 NM 1996 8 22 96FDEA01388 1 19960820 A 5280 DOOR DOUG MD11 MD11F 3023600 NM LT MLG CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 608FE 48548 SNRM 7045 AND 7046, LT MAIN LANDING GEAR DOOR CRACKED FWD AND AFT OF CENTER HINGE INTER SKIN. *S/D* STOP DRILLED CRACK PER SRM 51-00-01 AND FABRICATED DOUBLERS AND SKIN FOR REPAIR PER SRM 52-10-00. 2 L 7 3 4F RT A22WE 1996082200588 19960822 00588 NM 1996 8 22 96FDEA01387 1 19960820 A 5320 ANC7013 WEB DOUG MD11 MD11F 3023600 NM BS 2007 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 608FE 48548 HORIZONTAL WEB CRACKED 0.500 JUST AFT OF PRESSURE BULKHEAD STA 2007, APPROX RBL 20 TO 30 AND ABOVE TAG HORIZONTAL BOX SE CTION. *S/D* REMOVED NECESSARY FASTENERS. NDT VERIFIED END OF CRACK. FABRICATED AND INSTALLED REPAIR PER EA 1-5310-2 8046. 2 L 7 3 4F RT A22WE 1996082200590 19960822 00590 WP 1996 8 22 96UAL900615 1 19960812 A 2910 TUBE ASSY DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 3 PIN HOLE A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 1817U 46616 NR 3 HYDRAULIC SYSTEM SHUT-DOWN DUE TO LOSING FLUID. MADE UNSCHEDULED LANDING AT DEN. NR 3 SYSTEM HYDRAULIC LINE LEAKI NG AT FORWARD INBOARD CORNER OF RIGHT HAND WHEELWELL. SPLICED IN NEW SECTION USING RYNGLOK METHOD. 2 L 7 3 4F 4 F A22WE E23EA 1996082200591 19960822 00591 NM 1996 8 22 96UAL900616 1 19960812 A 3230 65442514 UPLOCK ACTUATOR BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE NLG INOPERATIVE A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 9013U 19051 GEAR HANDLE PUT IN THE UP POSITION GOT BOTH NOSE LANDING GEAR RED AND GREEN LIGHTS. PER CREW GEAR DID NOT RETRACT. *S/ D* FOUND NOSE LANDING GEAR UPLOCK ACTUATOR AND ADJUSTED NOSE LANDING GEAR PROXIMITY SENSOR, CHECKS OK. 2 L 7 2 4F 4 F A16WE E2EA 1996082200592 19960822 00592 NM 1996 8 22 96UAL900617 1 19960812 A 2530 OVEN SELL 8800010000 BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE GALLEY FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 605UA 8208055 21866 THE GALLEY OVEN WAS SMOKING AND SPARKING. THE OVEN WAS REMOVED FROM THE AIRCRAFT AND RETURNED TO THE SHOP. THE B-PHASE OVEN HEATING ELEMENT WAS FOUND INOPERABLE DURING OVERHAUL. 2 L 7 2 4F 4 F RT A1NM E3NE 1996082200593 19960822 00593 NM 1996 8 22 96UAL900618 1 19960812 A 3397 58781 WIRE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 943UA 26680 EMERGENCY ESCAPE PATH LIGHTING INOP ROW 12 THROUGH ROW 15. REPLACED CABLE, CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1996082200594 19960822 00594 NM 1996 8 22 96UAL900619 1 19960812 A 3350 60252 STRIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN DAMAGED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 305UA 23666 EMERGENCY ESCAPE PATH LIGHTING INOP FROM ROW 13 TO THE AFT GALLEY. REPAIRED LIGHT STRIP AND TRIMMED CARPET, CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1996082200595 19960822 00595 NE 1996 8 22 96UAL900620 2 19960812 A 7230 1663424P01 COMPRESSOR BLADE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE DAMAGED A UALA A UNSCHED LANDING E C VIBRATION/BUFFET F.O.D. TO TAKEOFF 1 WP 29 942UA 26679 856361 BIRD STRIKE NUMBER TWO ENGINE AT LIFT OFF. NOTICEABLE VIBRATION CHANGE WITH POWER CHANGE. *S/D* BIRD STRIKE CAUSED EN GINE VIBRATION, TWO BLADES WERE FOUND DAMAGED NR 17 AND NR 18. BLADES WERE REPLACED, ENGINE WAS RUN AND NO VIBRATION WA S NOTED. 2 L 7 2 4F 4 F RT A16WE E2GL 1996082200596 19960822 00596 NE 1996 8 22 96UAL900621 2 19960812 A 7311 749965 FUEL OIL COOLER BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE NR 2 ENGINE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 9010U 19048 655213 NUMBER TWO ENGINE OIL TEMPERATURE IN YELLOW BAND ON CLIMBOUT. RETURNED TO ORD. *S/D* REPLACED FUEL/OIL COOLER, ENGINE CHECKED OK ON RUN-UP. 2 L 7 2 4F 4 F A16WE E2EA 1996082200597 19960822 00597 NM 1996 8 22 96UAL900622 1 19960812 A 3350 1317 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 580UA 26698 DOOR 3 LEFT EMERGENCY LIGHT INOP. REPLACED LAMP, OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996082200598 19960822 00598 NE 1996 8 22 96UAL900623 2 19960813 A 7230 55H005 COMPRESSOR BLADE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT ENGINE FAILED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 WP 29 658UA 16200 27113 724679 DURING CLIMB-OUT, THE RIGHT ENGINE EXPERIENCED HIGH EGT AND TWO COMPRESSOR STALLS. THE CREW INITIATED AN IN-FLIGHT SHUT DOWN. AIRCRAFT RETURNED TO MIAMI WITH AN UNEVENTFUL LANDING. THE HIGH PRESSURE COMPRESSOR FIFTH STAGE BLADE FAILED. T HE ENGINE WAS REPLACED. PART TOTAL CYCLES, 2,473. 2 L 7 2 4F 4 F RT A1NM E24NE 1996082200599 19960822 00599 WP 1996 8 22 96UAL900624 1 19960813 A 3350 EMB51392 POWER SUPPLY DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1839U 46633 MID EMERGENCY LIGHT BATTERY PACK FAILED TEST. REPLACED BATTERY PACK AND CONTROLLER. 2 L 7 3 4F 4 F A22WE E23EA 1996082200600 19960822 00600 1996 8 22 96UAL900625 4 19960813 A 2565 SLIDE AIR CRUISER D29835103 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN SEAM LEAK A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7278U 21425 DURING SHOP OVERHAUL OF SLIDE REMOVED FOR TIME EXPIRATION, THE INFLATABLE PORTION DEVELOPED A SEAM LEAK. SCRAPPED UNIT. 2 L 7 3 4F 4 F A3WE E2EA 1996082200601 19960822 00601 WP 1996 8 22 96UAL900626 1 19960814 A 5330 SKIN DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE BS 1133 CORRODED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 1857U 46986 THE FUSELAGE SKIN AT BODY STATION 1133 HAD EXCESSIVE MATERIAL LOSS DUE TO CORROSION IN THE AREA OF STRINGER 46L. APPROX IMATELY 50 PERCENT OF THE ORIGINAL SKIN THICKNESS WAS REMOVED OVER A 2.5 DIAMETER AREA. THE DAMAGE WAS DETECTABLE FROM THE OUTSIDE OF THE AIRCRAFT DUE TO PILLOWING OF THE SKIN. AN INTERIM DOUBLER REPAIR WAS INSTALLED PER THE DC-10 SRM 53- 20-00, FIGURE 13 AND UAL EVA ORD-4259. PERMANENT REPAIR TO BE MADE AT NEXT C-CHECK. 2 L 7 3 4F 4 F A22WE E23EA 1996082200602 19960822 00602 WP 1996 8 22 96UAL900627 1 19960814 A 2170 COALESCER BAG DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN DIRTY A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 1813U 46612 OIL SMELL IN CABIN. NR 1 PACK AND ENGINE BLEED OFF. REPLACED COALESCER BAG AND BURNED OUT NR 1 PACK SYSTEM. UNABLE T O CONFIRM SOURCE OF SMELL. NO RECURRENCE. 2 L 7 3 4F 4 F A22WE E23EA 1996082200603 19960822 00603 WP 1996 8 22 96UAL900628 1 19960814 A 3520 80138682 OXY GENERATOR DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN FIRED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 1831U 46630 ROWS 26-28, RIGHT SIDE OF THE AIRCRAFT HAD STRONG ELECTRICAL BURNING SMELL. ALL LIGHTS WERE OFF FOR THE MOVIE. FOUND O XYGEN GENERATOR AT SEAT 29F FIRED. REPLACED GENERATOR. 2 L 7 3 4F 4 F A22WE E23EA 1996082200604 19960822 00604 WP 1996 8 22 96UAL900629 1 19960814 A 2841 FUEL QUANTITY DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE FUEL SYST DROPPED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 1855U 47837 RETURNED TO SFO DUE TO A SIGNIFICANT DROP IN FUEL QUANTITY. 2 L 7 3 4F 4 F A22WE E23EA 1996082200605 19960822 00605 NE 1996 8 22 96UAL900630 2 19960814 A 7321 7436025 CONTROL UNIT BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE ENGINE FAILED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 29 995UA 22399 649505 ENGINE WOULD NOT DEVELOP TAKEOFF THRUST, WOULD GO NO HIGHER THAN 96.5 PERCENT N-1. ABORTED TAKEOFF. *S/D* FUEL CONTRO L UNIT FAILED. REPLACED FUEL CONTROL UNIT CHECKS OK. SEVERAL ITEMS WERE FOUND UNSERVICEABLE IN THIS UNIT AND COLLECTIV ELY THEY CONTRIBUTED TO THE FAILURE. 2 L 7 2 4F 4 F A16WE E2EA 1996082200606 19960822 00606 NM 1996 8 22 96UAL900631 1 19960814 A 5230 65479531 FRAME BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 9001U 19039 AFT CARGO DOOR, LOWER AFT CORNER FRAME FOUND 16 INCH LONG CRACK IN THE RADIUS OF 7075-T6 CHANNEL SECTION. CHANNEL FORMS LOWER AFT SIDE OF DOOR FRAME. FERRIED AIRCRAFT TO IND. DOOR REMOVED AND REPAIRED PER UAL MM. 2 L 7 2 4F 4 F A16WE E2EA 1996082200607 19960822 00607 NM 1996 8 22 96UAL900475 1 19960624 A 2612 FIRE MODULE BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE NR 2 ENGINE MALFUNCTIONED A UALA F ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 WP 29 9038U 19076 CREW REPORTED NUMBER TWO ENGINE HAD FIRE WARNING ON TAXI IN. LIGHT REMAINED ON AFTER BOTH BOTTLES WERE SEQUENTIALLY DIS CHARGED. *S/D* ACCOMPLISHED VISUAL CHECK OF ENGINE, FOUND OK. CHECKED INLET AND EXHAUST, ALSO OK. REPLACED ENGINE MO DULE AND RAN ENGINE, NO FAULTS. SHOP TESTED THE MODULE AND FOUND THE UNIT OK. 2 L 7 2 4F 4 F A16WE E2EA 1996082200608 19960822 00608 NM 1996 8 22 96UAL900604 1 19960807 A 3350 LIGHTS BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN MALFUNCTIONED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7458U 21912 EMERGENCY EXIT LIGHTS IN FLOOR COME ON INTERMITTENTLY WITH SWITCH IN ARMED POSITION. CEILING EXIT LIGHTS DO NOT COME ON (UNLESS TURNED ON), BUT LOWER WALL EXIT LIGHT BENEATH FLIGHT ATTENDANT EXIT LIGHT SWITCH DOES COME ON WITH EEL. 2 L 7 3 4F 4 F A3WE E2EA 1996082200609 19960822 00609 NM 1996 8 22 96UAL900612 1 19960809 A 3350 LIGHT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE COCKPIT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7288U 21566 EMERGENCY EXIT LIGHT IN COCKPIT INOPERATIVE. 2 L 7 3 4F 4 F A3WE E2EA 1996082200610 19960822 00610 NE 1996 8 22 96UAL900632 2 19960815 A 7321 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUEL CONTROL WORN A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 520UA 24890 726502 DURING CLIMB-OUT FROM PHL, RECEIVED EICAS MESSAGE ON LEFT ENGINE PRIMARY CONTROL, ACCOMPANIED BY LENGTHY SECONDARY CONTR OL MESSAGE. FLIGHT DIVERTED TO ORD. CONNECTOR W2P7 ON FUEL CONTROL HAD LOOSE BACKSHELL. WIRES WERE TWISTED IN BUNDLE INSIDE BACKSHELL. ONE WIRE HAD INSULATION WORN THROUGH. REPAIRED INSULATION AND INSTALLED CONNECTOR. OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996082200611 19960822 00611 1996 8 22 96UAL900633 4 19960815 A 2565 D31042205 UPPER TUBE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR SLIDE POROUS A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 541UA 25253 UNIT RETURNED TO SHOP FOR SECOND TIME CONTROLLED OVERHAUL. UNIT HAS POROSITY ON THE UPPER INFLATION TUBE WHERE IT MEETS THE TOP TUBE. UNIT RETURNED TO MANUFACTURER FOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 1996082200612 19960822 00612 NM 1996 8 22 96UAL900634 1 19960814 A 3241 RESISTORS 3238878 BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ANTI-SKID SYST DAMAGED A UALA O OTHER E VIBRATION/BUFFET LD LANDING 1 WP 29 506UA 476 24627 AFTER LANDING EXPERIENCED HEAVY SHUDDER ENTERING TAXIWAY. AIRCRAFT TOWED TO GATE. *S/D* REPLACED ANTI-SKID UNIT. FAU LTY UNIT RETURNED TO SHOP WHERE 4 RESISTORS WERE FOUND DAMAGED. RESISTORS REPLACED, OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996082200613 19960822 00613 WP 1996 8 22 96UAL900635 1 19960815 A 3330 561513BIL BALLAST DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CARGO PIT BURNED A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 1814U 46613 FORWARD CARGO PIT OVERHEAD LIGHT SMOKING AND HAS A BURNED SMELL. LIGHT IS 3RD FROM AFT WALL. BURNED BALLAST REPLACED. 2 L 7 3 4F 4 F A22WE E23EA 1996082200614 19960822 00614 NM 1996 8 22 96UAL900636 1 19960816 A 2612 FIRE WARNING BOEING 285T03855 BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE ENGINE MALFUNCTIONED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 657UA D00462 27112 AIRCRAFT RETURNED TO THE FIELD AT SFO UNDER AMBER ALERT DUE TO A FIRE BELL AURAL WARNING. *S/D* THE ENGINE FIRE DETECT ION SYSTEM CAUSED THE AURAL WARNING. A BITE TEST WAS PERFORMED AND INDICATED NO FAULTS. THE M1000 BELL CHIME MODULE WA S REPLACED AS A PRECAUTION. THIS MODULE WAS DETERMINED TO BE SERVICEABLE AND WAS RETURNED TO SERVICE. NO OTHER FAULTS HAVE BEEN INDICATED SINCE THIS INCIDENT. 2 L 7 2 4F 4 F RT A1NM E24NE 1996082200615 19960822 00615 WP 1996 8 22 96UAL900637 1 19960816 A 2910 AE1010129N0226 HOSE ASSY DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 2 HYD PUMP LEAKING A UALA O OTHER K FLUID LOSS IN INSP/MAINT 1 WP 29 1849U 46939 ON FINAL WALK-AROUND FOR DEPARTURE, MECHANIC NOTICED HYDRAULIC FLUID RUNNING OFF AFT TAIL CONE. SUCTION HOSE TO NR 2 EN GINE HYDRAULIC PUMP LEAKING AT CHAFED AREA. REPLACED HOSE ASSEMBLY. 2 L 7 3 4F 4 F A22WE E23EA 1996082200616 19960822 00616 NM 1996 8 22 P5CA9600571 1 19960715 A 5753 FAIRING BOEING 747 747132 1384882 NM RT TE FLAP DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 DAMAGED NR 7 FLAP TRACK FORWARD FIXED FAIRING EXTERNAL SURFACE. REPAIRED PER BOEING SRM 52-40-15. 2 L 7 4 4F A20WE 1996082200617 19960822 00617 NM 1996 8 22 P5CA9600581 1 19960715 A 5315 FLOOR BEAM BOEING 747 747132 1384882 NM BS 2240 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION ON MAIN DECK RT OTBD FLOOR BEAM STA 2240. CORROSION REMOVED AND RE-PROTECTED PER BAC SRM 51-10-01 AND SRM 51-1-02. 2 L 7 4 4F A20WE 1996082200618 19960822 00618 WP 1996 8 22 ARWA9608005 1 19960821 A 5720 FILLET DOUG DC8 DC863 302198A WP WS 217 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 A 2 INCH CRACK IN RIGHT HAND WING INBOARD FLAP WELL LOWER EDGE FILLET XRS 217. REMOVED LOWER FILLET, FORMED FILLET PER DC-8 SRM 51-1-7, 57-2-0. INSTALLED PER DC-8 SRM 51-1-21. 2 L 7 4 4F 4A25 1996082200619 19960822 00619 WP 1996 8 22 ARWA9608006 1 19960821 A 5753 SKIN DOUG DC8 DC863 302198A WP TE FLAP DENTED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 PUTTY FILLED REPAIR DENTS RT WING INBD FLAP, 10 INCH AFT L/E XW 132.000. REPLACED PLATING SKIN IAW DC-8 SRM 57-7-1, 51- 1-4. TREATED AND INSTALLED PER DC-8 SRM 51-1-8, 51-1-21. 2 L 7 4 4F 4A25 1996082200620 19960822 00620 WP 1996 8 22 ARWA9608007 1 19960821 A 5753 FITTING DOUG DC8 DC863 302198A WP RT TE FLAP CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 RT WING FLAP NR 4 HINGE STOP BASE IS CRACKED AT STA 423. REPLACED FITTING PER DC-8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1996082200621 19960822 00621 NE 1996 8 22 CAL960618 2 19960516 A 7530 679058 STATOR VANE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 1 ENGINE FAILED A CALA A E UNSCHED LANDING ENGINE SHUTDOWN O OTHER CR CRUISE 1 SW 09 93875 49125 708479 THE NR 1 ENGINE QUIT RUNNING AT FL 280 WHILE EN ROUTE FROM EWR TO MCO. THE ENGINE FAILURE WAS ACCOMPANIED BY A MUFFLED BANG. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS DIVERTED TO JAX WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUN D METAL IN THE NR 1 ENGINE TAILPIPE. THE NR 1 ENGINE WAS REMOVED AND REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION. SHOP TEARDOWN FINDINGS REVEALED A FRACTURED C-8 S TATOR VANE. 2 L 7 2 4F 4 F A6WE E9NE 1996082200622 19960822 00622 NE 1996 8 22 9617729864 2 19960814 A 7320 FUEL CONTROL DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE NR 2 ENGINE WATER CONTAM A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 773NC 47775 696762 DURING TAKEOFF ROLL, THE NR 2 ENGINE EPR AND N1 INDICATIONS BEGAN FLUCTUATING. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE DRAINED FUEL CONTROL MOISTURE TRAP AND RAN ENGINE TO TAKEOFF POWER. ACCELERATION AND OPERATIONAL CH ECK OK. 2 L 7 2 4F 4 F A6WE E2EA 1996082200623 19960822 00623 WP 1996 8 22 9617739930 1 19960813 A 7711 611429 PT-7 LINE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7 52053 NE NR 1 ENGINE BROKEN A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 89S 47042 657547 DURING TAKEOFF, THE LEFT ENGINE EPR REACHED A MAX OF 1.85, NEEDED 1.95 FOR TAKEOFF. CREW ABORTED TAKEOFF AND RETURNED T O THE GATE. MAINTENANCE REPLACED PT-7 LINE. OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F A6WE E2EA 1996082200624 19960822 00624 EA 1996 8 22 COMA9660131 1 19960816 A 2750 TE FLAPS CNDAIR CL600 CL6002B19 EA RT WING OUT OF ADJUST A COMA K NONE F FLT CONT AFFECTED NR NOT REPORTED 1 SO 01 920CA 7022 AIRCRAFT ROLLS HARD RIGHT WHEN FLAPS SELECTED TO 45 DEGREES. ADJUSTED THE RT WING FLAPS TO M/M SPECIFICATIONS. SYSTEM CHECKS SATISFACTORY. 2 L 7 2 4F RT A21EA 1996082200625 19960822 00625 NM 1996 8 22 UPS96220833 1 19960809 A 5320 2024T3 WEB BOEING 727 727180C 138406G NM BS 293 CRACKED A IPXA O OTHER O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE: SI. WHILE WORKING CUSTOMER CARD NUMBER C53-111-01-1D (FUSELAGE 77), FOUND CRACK IN NLG WHEELWELL AT S TA 293 RBL 24 WL 179. REPAIRED CRACK IN NLG WHEELWELL STA 293 RBL 24 WL 179 IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1996082200626 19960822 00626 NM 1996 8 22 UPS96220847 1 19960806 A 5313 7075T6 STRINGER BOEING 727 727180C 138406G NM BS 360-440 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE: SI. CORROSION ON STRINGER 3 RT STA 360-440. REMOVED CORROSION REWORK DEEMED OUT OF LIMITS IAW SRM 5 3-10-1. REPAIRED STR 3 RT IAW TRAMCO E.W.O. 96-2444. 2 L 7 3 4F A3WE 1996082200627 19960822 00627 NM 1996 8 22 UPS96220848 1 19960806 A 5313 7075T6 STRINGER BOEING 727 727180C 138406G NM BS 1110-1130 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE: SI. CORROSION ON STRINGER 2 RT STA 110-1130. REPAIRED STR 2 RT IAW TRAMCO E.W.O. 96-2444. CORROSION REMOVAL REWORK WAS DEEMED OUT OF LIMITS IAW SRM 53-10-1. 2 L 7 3 4F A3WE 1996082200628 19960822 00628 NM 1996 8 22 UPS96220849 1 19960803 A 5313 BAC1493515 STRINGER BOEING 727 727180C 138406G NM BS 580-622 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 920UP 19873 INSPECTION TYPE: SI. CORROSION ON STRINGER 2 RT STA 580-622. FOUND CORROSION OUT OF LIMITS PER SRM 51-10-6 AND SRM 51 -10-1. REMOVED AND REPLACED STRINGER 2 RT STA 580-622 PER SRM'S 51-10-3, 51-30-2, 51-10-2. 2 L 7 3 4F A3WE 1996082200629 19960822 00629 NM 1996 8 22 UPS96420839 1 19960721 A 5320 PRESSURE DECK BOEING 747 747123 1384873 NM BS 1265-1300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE: C. AT PRESS MAIN DECK AT BS 1265/1300 AT RBL 75, SEVERAL SPOTS CORROSION OUT OF LIMITS. REPAIRED P RESS MAIN DECK AT BS 1265 TO BS 1300 AT RBL 75 IAW SRM 53-1 0-07 FIG 2 AND IAW UPS EFN 747-53-0780. 2 L 7 4 4F A20WE 1996082200630 19960822 00630 NM 1996 8 22 UPS96420840 1 19960725 A 5320 PRESSURE DECK BOEING 747 747123 1384873 NM STA 1265/1480 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE: C. FOUND SEVERAL SPOTS OF CORROSION ON PRESS MAIN DECK AT RBL 57 BETWEEN STA 1625/1480. CORROSIVE S POTS ARE OUT OF LIMITS. REPAIRED PRESS MAIN DECK AT RBL 57 BETWEEN BS 1265/1480 IAW SRM 53-10-07 FIG 2. 2 L 7 4 4F A20WE 1996082200631 19960822 00631 NM 1996 8 22 UPS96420841 1 19960721 A 5320 PRESSURE DECK BOEING 747 747123 1384873 NM BS 1310-1350 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE: C. PRESS MAIN DECK FOUND CRACKED IN SKIN AT RBL 33 BETWEEN BS 1310 AND BS 1350. REPAIRED PRESS MAIN DECK AT RBL 33 BS 1310/1350 IAW SRM 53-10-07 FIG 2. 2 L 7 4 4F A20WE 1996082200632 19960822 00632 NM 1996 8 22 UPS96420842 1 19960721 A 5320 PRESSURE DECK BOEING 747 747123 1384873 NM BS 1360 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE: C. FOUND AT MAIN PRESS DECK AT BS 1360 AT RBL 33 , CRACK. REPAIRED PRESS MAIN DECK AT 1360 AT RBL 3 3 IAW SRM 53-10-07 FIG 2. 2 L 7 4 4F A20WE 1996082200633 19960822 00633 NM 1996 8 22 UPS96420843 1 19960723 A 5320 PRESSURE DECK BOEING 747 747123 1384873 NM BS 1306-1380 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE: C. FOUND ON PRESS MAIN DECK AT LBL 75 BETWEEN STA 1306 AND STA 1380, SEVERAL SPOTS CORRODED OUT OF L IMITS. REPAIRED PRESS MAIN DECK AT LBL 75 BETWEEN STA 1306 AND STA 1380 IAW SRM 53-10-07 FIG 2. 2 L 7 4 4F A20WE 1996082200634 19960822 00634 NM 1996 8 22 UPS96420844 1 19960719 A 5320 PRESSURE DECK BOEING 747 747123 1384873 NM BS 1370 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE: C. CRACK FOUND ON PRESS MAIN DECK AT BS 1370 AT RBL 75 . REPAIRED PRESS MAIN DECK WEB AT RBL 75 AT BS 1370 IAW SSRM 53-10-07 FIG 2. 2 L 7 4 4F A20WE 1996082200635 19960822 00635 NM 1996 8 22 UPS96420845 1 19960721 A 5320 PRESSURE DECK BOEING 747 747123 1384873 NM BS 1270 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE: C. FOUND AT PRESS MAIN DECK WEB, CRACK AT RBL 33 AT BS 1270. REPAIRED PRESS MAIN DECK WEB AT BS 127 0 AT RBL 33 IAW SRM 53-10-07 FIG 2. 2 L 7 4 4F A20WE 1996082200636 19960822 00636 NM 1996 8 22 UPS96420846 1 19960719 A 5315 FLOOR BEAM BOEING 747 747123 1384873 NM BS 860 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE: CPCP. MAIN DECK FLOORBEAM UPPER CHORD CORRODED AT BS 860 BETWEEN RBL 65/110. CORROSION REMOVED IAW SRM 51-10-01. OUT OF LIMITS PER SRM 53-10-01. UPPER CHORD AT BS 860 RBL 65 TO RBL 110 REPAIRED IAW SRM 53-10-07. 2 L 7 4 4F A20WE 1996082200637 19960822 00637 NM 1996 8 22 UPS96420850 1 19960717 A 5247 DOOR BOEING 747 747123 1384873 NM APU CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE: C. APU BATTERY ACCESS DOOR SKIN CRACKED AND DEFORMED. REWORKED SKIN PLATE OF APU ACCESS DOOR IAW S RM 51-10-01. SKIN PLATE AND FRAMES ARE NOT IN LIMITS IAW SRM 52-00-02. REPLACED APU ACCESS DOOR ACC SRM 51-30-02. 2 L 7 4 4F A20WE 1996082200638 19960822 00638 NM 1996 8 22 UPS96420851 1 19960809 A 5320 WEB BOEING 747 747123 1384873 NM BS 460 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE: C. FOUND CORROSION ON WEB PLATE AT BS 460 BETWEEN RBL 80 AT WL 308. REMOVED CORROSION ON WEB PLATE AT BS 460 BETWEEN RBL 42/80 ACC SRM 5 1-10-01. CORROSION NOT IN LIMITS ACC SRM 53-10-01. REPLACED WEB PLATE ACC SRM 51-30-02. 2 L 7 4 4F A20WE 1996082200639 19960822 00639 WP 1996 8 22 UPS96820834 1 19960720 A 5320 0257075T6 WEB DOUG DC8 DC873F 302199F WP BS 1581 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE: CS2. FLOOR WEBBING AT FS 1581 CRACKED BOTH SIDES, LONGERONS 21L AND 21R. REPAIRED WEBBING PER RM 53- 2-0. 2 L 7 4 4F RT 4A25 1996082200640 19960822 00640 WP 1996 8 22 UPS96820835 1 19960721 A 5320 0637075T6 DOUBLERS DOUG DC8 DC873F 302199F WP BS 12 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE: CS2. LEFT AND RIGHT AFT HEAT EXCHANGERS FUSELAGE SKIN CUTOUT DOUBLERS CRACKED ON AFT LOWER CORNERS. R EPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996082200641 19960822 00641 WP 1996 8 22 UPS96820836 1 19960710 A 5320 3754930 FITTING DOUG DC8 DC873F 302199F WP BS 1202-1210 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE: CS2. 2 EA BATHTUB FITTINGS CRACKED AT LONGERONS 33R A AND B, FS 1202-1210. REPLACED FITTINGS PER SRM 53-2-0 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996082200642 19960822 00642 WP 1996 8 22 UPS96820837 1 19960625 A 5330 9754944 SKIN DOUG DC8 DC873F 302199F WP BS 1217 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE: CS2. PERMANENT REPAIR TO BE INSTALLED DUE TO CORROSION DAMAGE ON FUSELAGE SKIN STA 1217 BELOW C-BIN DOOR CUTOUT. REPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996082200643 19960822 00643 WP 1996 8 22 UPS96820838 1 19960719 A 5320 3759434 SPLICE DOUG DC8 DC873F 302199F WP BS 190 BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE: CS2. FS 190, 2 EACH, LONGERON SPLICES BROKEN AT LONGERONS 33R AND 34R. REPAIRED SPLICES PER SRM 51- 1-20D. 2 L 7 4 4F RT 4A25 1996082200644 19960822 00644 EU 1996 8 22 QXEA9600302 1 19960815 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 10966 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - CRACKED CLIP AT FRAME 10966 AND STRINGER 32. CRACK NOTED DURING C-CHECK (NR300-27). CRACK REPAIRED I/A/W SRM 53- 02-13. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996082200645 19960822 00645 EU 1996 8 22 QXEA9600303 1 19960815 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12875 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - CRACKED CLIP AT FRAME12875 AND STRINGER 30. CRACKED NOTED DURING C-CHECK (NR 300-28). CRACK REPAIRED I/A/W SRM 5 3-02-13. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996082200646 19960822 00646 EU 1996 8 22 QXEA9600304 1 19960815 A 5320 CLIPS FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - CRACKED CLIP AT FRAME 13815A AND STRINGERS 31, 47, AND 44. CRACKS NOTED DURING C-CHECK (NR 300-29,-30,-31). CRAC KS REPAIRED I/A/W SRM 53-02-13. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996082200647 19960822 00647 EU 1996 8 22 QXEA9600305 1 19960815 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 14755 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - CRACKED CLIP AT FRAME 14755 AND STRINGERS 20, 39, 40, 43, 49, AND 57. CRACKS NOTED DURING C-CHECK (NR 300-81-82-8 3-84-85-86). CRACKS REPAIRED I/A/W SRM 530213. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996082200648 19960822 00648 EU 1996 8 22 QXEA9600306 1 19960815 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - CRACKED CLIP AT FRAME 15025 AND STRINGERS 21, 24, 25, 26, 46, 48, 49, 51, 56, 58A, 16, 18, 19, AND 20. CRACKS NOT ED DURING C-CHECK (NR 300-101-102-106-107-87-88-89-90-91-94-95-96-97-98-99-100). CRACKS REPAIRED I/A/W SRM 530213. AIR CRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996082200649 19960822 00649 EU 1996 8 22 QXEA9600307 1 19960815 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 16060 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - CRACKED CLIP AT FRAME 16060 AND STRINGER 28. CRACK NOTED DURNG C-CHECK (NR 300-165). CRACK REPAIRED I/A/W SRM 53 0213. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996082200650 19960822 00650 EU 1996 8 22 QXEA9600308 1 19960815 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 16660 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - CRACKED CLIP AT FRAME 16660 AND STRINGERS 58 AND 28. CRACKS NOTED DURING C-CHECK (NR 300-110-300). CRACKS REPAIR ED I/A/W SRM 530213. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996082200651 19960822 00651 EU 1996 8 22 QXEA9600309 1 19960815 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 5305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - CRACKED CLIP AT FRAME 5305 AND STRINGERS 39, 46, 45, 44, 43, 16, 31, 35, AND 56. CRACKS NOTED DURING C-CHECK (NR 300-114-115-116-117-118-119-120-121-122). CRACKS REPAIRED I/A/W SRM 530213. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996082200652 19960822 00652 EU 1996 8 22 QXEA9600310 1 19960815 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 6305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - CRACKED CLIP AT FRAME 6305 AND STRINGER 36. CRACK NOTED DURING C-CHECK (NR 300-127). CRACK REPAIRED I/A/W SRM 53 0213. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996082200653 19960822 00653 EU 1996 8 22 QXEA9600311 1 19960815 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 7805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - CRACKED CLIP AT FRAME 7805 AND STRINGERS 45, 43, 31, AND 33. CRACKS NOTED DURING C-CHECK (NR 300-130-131-132-133) . CRACKS REPAIRED I/A/W SRM 530213. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996082200654 19960822 00654 EU 1996 8 22 QXEA9600312 1 19960815 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 8305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - CRACKED CLIP AT FRAME 8305 AND STRINGERS 46, 45,44, 39, 36, AND 30. CRACKS NOTED DURING C-CHECK (NR 300-135-136-1 37-138-139-140). CRACKS REPAIRED I/A/W SRM 530213. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996082200655 19960822 00655 EU 1996 8 22 QXEA9600313 1 19960815 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 8805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - CRACKED CLIP AT FRAME 8805 AND STRINGERS 45, 44, 43, AND 39. CRACKS NOTED DURING C-CHECK (NR 300-142-143-144-145) . CRACKS REPAIRED I/A/W SRM 530213. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996082200656 19960822 00656 EU 1996 8 22 QXEA9600314 1 19960815 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - CRACKED CLIP AT FRAME 9305A AND STRINGERS 39 AND 47. CRACKS NOTED DURING C-CHECK (NR 300-146-148). CRACKS REPAIR ED I/A/W SRM 530213. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996082200657 19960822 00657 EU 1996 8 22 QXEA9600315 1 19960815 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - CRACKED CLIP AT FRAME 9305B AND STRINGER 39. CRACK NOTED DURING C-CHECK (NR 300-149). CRACK REPAIRED I/A/W SRM 5 30213. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996082200658 19960822 00658 NM 1996 8 22 96FDEA01363 1 19960814 A 5311 65176634 FRAME BOEING 727 72722 1384002 NM BS 700 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 NR 0623 AND 012. CORROSION C53-111-01 ON FRAME STA 700 STR 27L - R WL 156. ****S/D***** COMING. 2 L 7 3 4F A3WE 1996082200659 19960822 00659 NM 1996 8 22 96FDEA01367 1 19960815 A 5320 65163388 FORMER BOEING 727 72722 1384002 NM BS 951 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 NR 0664 AND 016. WHILE WORKING NR 0647, DISCOVERED CORROSION ON RT LOWER SKIN FORMER ANGLE AT BS 951, RBL 8 WL 138. ****S/D**** COMING. 2 L 7 3 4F A3WE 1996082200660 19960822 00660 NM 1996 8 22 96UAL900473 1 19960624 A 2121 FAN BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE CABIN FAILED A UALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 9013U 19051 FLIGHT CREW REPORTED THAT EN ROUTE HAD AN ELECTRICAL SMOKE AND SMELL THROUGHOUT THE CABIN. GALLEY POWER AND GASPER FAN SHUT OFF. SUPPLEMENTAL DATA UPDATE: TROUBLESHOT SYSTEM AND FOUND BURNT BEARINGS ON THE GASPER FAN. REPLACED GASPER FAN . CHECKS O.K. 2 L 7 2 4F 4 F A16WE E2EA 1996082200661 19960822 00661 EU 1996 8 22 96UAL900594 1 19960805 A 3350 LAMPS MGG 116502 AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 421UA 500 EMERGENCY LIGHT SYSTEM FAILED TEST AT FORWARD FLIGHT ATTENDANT PANEL. *S/D* FOUND LAMPS FAILED. REPLACED AND OPERATIO NALLY CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 1996082200662 19960822 00662 EU 1996 8 22 96UAL900595 1 19960805 A 3350 D31516109 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 428UA 523 EMERGENCY LIGHT SYSTEM FAILED TEST PER NR 2 SERVICE. *S/D* CHANGED P0WER SUPPLY AND BATTERY. ALSO, REPLACED SLIDE AND OPERATIONALLY CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 1996082200663 19960822 00663 NE 1996 8 22 96UAL900596 2 19960805 A 7230 55H005 BLADE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE FAILED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK E J VIBRATION/BUFFET WARNING INDICATION TO TAKEOFF 1 WP 29 658UA 16192 27113 724678 ABORTED TAKEOFF AT LESS THAN 60 KNOTS DUE TO NR 1 ENGINE VIBRATION. THE HIGH PRESSURE COMPRESSOR EXPERIENCED A FIFTH ST AGE BLADE FAILURE. THE ENGINE WAS REPLACED. PART TOTAL CYCLES, 2,471. 2 L 7 2 4F 4 F RT A1NM E24NE 1996082200664 19960822 00664 NM 1996 8 22 96UAL900597 1 19960805 A 5330 SKIN BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE FUSELAGE BELLY CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 9027U 19065 FOUND RIVET PULLED THROUGH ON BELLY SKIN. SKIN SHOWED SLIGHT SIGNS OF PILLOWING AROUND FASTER AND SEVERAL OTHER AREAS. INTERNAL INSPECTION FOUND CORROSION. DRILLED AND REPLACED RIVET. REPAIRED CORROSION PER SHEETMETAL REPAIR MANUAL. 2 L 7 2 4F 4 F A16WE E2EA 1996082200665 19960822 00665 NM 1996 8 22 96UAL900598 1 19960806 A 2720 BACB10FS4R BEARING PARKER MKP4A BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE RUDDER CRACKED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK F FLT CONT AFFECTED TO TAKEOFF 1 WP 29 920UA 2875A 25387 ON TAKEOFF AT 60 KNOTS, AIRCRAFT JERKED TO THE RIGHT AND A KICK TO THE RIGHT IN THE RUDDER PEDALS WAS FELT. ABORTED TAK EOFF. STEERING WAS OK ON TAXI IN. *S/D* DURING SHOP OVERHAUL OF THE PCU THE PRIMARY SUMMING LEVER WAS REPLACED. AN A LTERNATE CONFIGURATION BOLT WAS USED IN PLACE OF THE BOEING SPECIFIED SUMMING LEVER BOLT. THE BOLT HEAD-TO-SHANK RADIUS HAS AN UNFAVORABLE RELATIONSHIP WITH THE BEARING INNER RACE ID CHAMFER, POSSIBLY CONTRIBUTING TO THE FAILURE OF THE BEA RINGS INNER RACE. RUDDER OPS CHECK GOOD. NOW ACTIVELY REPLACING OLD BOLTS AND INSPECTING THE SUMMING LEVER BEARING INN ER RACE TO VERIFY INTEGRITY ON ALL UNITS. 2 L 7 2 4F 4 F RT A16WE E2GL 1996082200666 19960822 00666 NM 1996 8 22 96UAL900599 1 19960806 A 4900 36144161 FAN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT FAILED A UALA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 WP 29 516UA 24860 LIGHT SMOKE IN COCKPIT WITH PACS ON AND APU RUNNING. *S/D* APU WAS REPLACED DUE TO MASSIVE COOLING FAN FAILURE. FAN R OTOR FAILED, HOUSING WAS BROKEN AND MINOR FOD TO BOTH COMPRESSORS. FAILED APU REPLACED WITH NEW UNIT, OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996082200667 19960822 00667 NM 1996 8 22 96UAL900600 1 19960807 A 2910 BAC10608119 HYD VALVE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FLAP/SLAT SYST LEAKING A UALA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 WP 29 604UA 21865 LANDED UNDER AMBER ALERT DUE TO ZERO QUANTITY INDICATION FOR CENTER HYDRAULIC SYSTEM FLUID. FLUID LOST DUE TO LEAK IN S OLENOID ON FLAP/SLAT HYD SHUTOFF VALVE. REPLACED BOTH SOLENOIDS AND GASKET PLATES ON FLAP/SLAT HYD VALVE. SERVICED CEN TER SYSTEM. OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 1996082200668 19960822 00668 NM 1996 8 22 96UAL900601 1 19960807 A 3040 HEAT UNIT BOEING BAC65528038 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 WINDOW FAILED A UALA O OTHER M J OVER TEMP WARNING INDICATION NR NOT REPORTED 1 WP 29 7462U 21916 NR 1 WINDOW OVERHEAT LIGHT CAME ON. RESET, CAME ON AGAIN. REPLACED WINDOW HEAT ACCESSORY UNIT DUE TO OUTPUT CONTROL C IRCUIT FAILURE. 2 L 7 3 4F 4 F A3WE E2EA 1996082200669 19960822 00669 NM 1996 8 22 96UAL900602 1 19960807 A 3411 652891312 PITOT TUBE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE VERT STAB BROKEN A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 7289U 21567 ELEVATOR FEEL DIFFERENTIAL PRESSURE LIGHT ON WITH A AND B HYDRAULIC SYSTEMS PRESSURIZED. FOUND TUBE ASSEMBLY FROM THE R IGHT HAND PITOT TUBE BROKEN. REPLACED DEFECTIVE PART AND TESTED SYSTEM. 2 L 7 3 4F 4 F A3WE E2EA 1996082200670 19960822 00670 WP 1996 8 22 96UAL900603 1 19960807 A 2730 ACTUATOR PARKER HANIF 21509005015 DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL LT ELEVATOR MALFUNCTIONED A UALA K NONE O OTHER NR NOT REPORTED 1 WP 29 1815U 160 46614 LT OUTBD ELEVATOR INDICATOR DOES NOT GO FULL TRAVEL AND ABNORMAL FORCE REQUIRED TO MOVE COLUMN. LT OUTBD ELEVATOR INTER MITTENTLY HANGS UP AND WILL NOT GO FULL TRAVEL. *S/D* REPLACED LEFT HAND OUTBOARD ELEVATOR ACTUATOR. 2 L 7 3 4F 4 F A22WE E23EA 1996082200671 19960822 00671 NM 1996 8 22 96UAL900605 1 19960807 A 2910 BACH5T0290FWR HYD LINE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE B HYD SYSTEM LEAKING A UALA K NONE K J FLUID LOSS WARNING INDICATION LD LANDING 1 WP 29 7258U 21405 LANDED AT ATL UNDER AMBER ALERT DUE TO B-SYSTEM HYDRAULIC FAILURE AND MAIN GEAR ANTI-SKID INOPERATIVE. NR 2 B-HYDRAULIC SYSTEM SUPPLY AND CASE DRAIN RETURN FLEX LINES HAD RUBBED TOGETHER CREATING A HOLE. REPLACED DEFECTIVE LINES. CREW RE PORTED THAT HYDRAULIC PUMPS NEVER RAN DRY. 2 L 7 3 4F 4 F A3WE E2EA 1996082200672 19960822 00672 NM 1996 8 22 96UAL900606 1 19960807 A 2121 FAN JOY MANUFACT 5007024620 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 7456U UA00063674 21910 SMOKE IN CABIN. GASPER FAN SWITCHED OFF AND SMOKE APPEARED TO DISSIPATE. *S/D* INSPECTED GASPER FAN, FOUND FAN MAKING LOUD NOISE. 2 L 7 3 4F 4 F A3WE E2EA 1996082200674 19960822 00674 1996 8 22 96UAL900608 4 19960808 A 2330 BACS14K3BACS14K SHOCK MOUNT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN FAILED A UALA O OTHER E VIBRATION/BUFFET LD LANDING 1 WP 29 584UA 10596 26706 OVERHEAD VIDEO MONITORS NR 5 AND NR 6 FELL TO FLOOR DURING LANDING. AIRCRAFT EXPERIENCED EXCESSIVE VIBRATION AFTER LAND ING AT SFO. THE VIDEO MONITOR SHOCK MOUNTS FAILED TO SUPPORT MONITORS NR 5 AND NR 6. UAL COA 50403 IMPLEMENTED BOEING SERVICE BULLETIN 757 23 0045 (INSTALL SOLID MOUNTS). LANDING CONDITIONS ARE STILL UNDER INVESTIGATION. 2 L 7 2 4F 4 F RT A2NM E17NE 1996082200675 19960822 00675 NM 1996 8 22 96UAL900609 1 19960808 A 5730 65B145967 PANEL BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE LT WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 175UA 25234 24382 DURING INSPECTION AT NRT, A 41 INCH CRACK WAS FOUND ON THE LEFT WING FIXED LEADING EDGE UPPER SKIN PANEL. THE DAMAGED S KIN PANEL IS LOCATED OUTBOARD OF WS 499.02 AND INBOARD TO THE NR 2 ENGINE. ACCOMPLISHED INTERIM SANDWICH DOUBLER REPAIR . PERMANENT REPAIR TO BE ACCOMPLISHED AT NEXT C-CHECK. PART TOTAL CYCLES, 2,663. 2 L 7 4 4F 4 F RT A20WE E24NE 1996082200676 19960822 00676 WP 1996 8 22 96UAL900610 1 19960809 A 3350 59191 CABLE PIN DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE CABIN BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1853U 47812 EEL LIGHTS INOPERATIVE IN B-ZONE LEFT SIDE STRIP. FOUND CABLE PIN BROKEN. REPLACED CABLE. 2 L 7 3 4F 4 F A22WE E23EA 1996082200677 19960822 00677 NM 1996 8 22 96UAL900611 1 19960809 A 2750 65984912 DRUM ASSY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 TE FLAP BOUND UP A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 7293U 21571 INBOARD FLAPS FAILED TO EXTEND BEYOND 2 DEGREES. EXTENDED WITH ALTERNATE SYSTEM TO 30 DEGREES. LEFT INBOARD TRAILING E DGE LAGS BEHIND OUTBOARD FLAP BY 12 INCHES. ACCOMPLISHED FLAP TORQUE LIMITER CHECK AND REPLACED NR 3 FLAP TRANSMISSION . FOUND BOUND-UP PULLEY ON RT INBD FLAP DRIVE POSITION TRANSMITTER AND REPLACED UNIT. REPLACED INBD FLAP POSITION INDI CATOR AND ADJUSTED RT INBD FLAP DRIVE POSITION TRANSMITTER. 2 L 7 3 4F 4 F A3WE E2EA 1996082200678 19960822 00678 WP 1996 8 22 96UAL900613 1 19960809 A 5330 SKIN DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL BS 1953 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 1849U 46939 DURING WALK-AROUND, FOUND FUSELAGE SKIN CORROSION/CRACK AT STATION 1953 BETWEEN LONGERONS L43 AND L45. CLEANUP OF CORRO SION/CRACK RESULTED IN A 3 INCH BY 3 INCH SECTION OF SKIN BEING REMOVED. THE CORROSION/CRACK WAS LIMITED TO THE SKIN AT ABOUT STATION 1953. NO DAMAGE TO FRAME OR LONGERONS NOTED. A CLASS 3 DOUBLER-TRIPLER REPAIR WAS INSTALLED PER DC10 SR M 53-20-00. 2 L 7 3 4F 4 F A22WE E23EA 1996082200679 19960822 00679 NM 1996 8 22 96UAL900614 1 19960809 A 2432 255823 BATTERY BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE E/ E COMPT OVERHEAT A UALA D H RETURN TO BLOCK DEACTIVATE SYST/CIRCUITS A FLAME/FIRE TX TAXI/GRND HDL 1 WP 29 992UA 22089 AIRCRAFT BATTERY WAS ON FIRE THROUGH THE TOP OF THE BATTERY. *S/D* THE BATTERY OVERHEATED DUE TO A FAILURE OF ONE OF T HE CELL SEPARATORS. THIS IS A KNOWN PROBLEM WITH MARATHON BATTERIES. THE BATTERY WAS SENT TO BOEING FOR ANALYSIS IN THE IR LABORATORY. THE BATTERY CHARGER AND THERMAL SWITCH WERE ALSO REPLACED, BUT SHOWED NO SIGN OF FAILURE IN THE SHOP. T HE BATTERY DID NOT SHOW SIGNS OF FIRE DAMAGE. 2 L 7 2 4F 4 F A16WE E2EA 1996082200680 19960822 00680 WP 1996 8 22 ABXA9600610 1 19960812 A 3350 41B004AD07G3 BATTERIES DOUG DC9 DC941 302207N WP COCKPIT DISCHARGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47494 COCKPIT EMERGENCY LIGHTS VERY DIM ON PRE-DEPARTURE CHECK. REPLACED BATTERIES FOR EMERGENCY LIGHT BATTERY PACK. 2 L 7 2 4F A6WE 1996082200681 19960822 00681 WP 1996 8 22 DHL9680601C 1 19960726 A 5311 STUB FRAME DOUG DC8 DC873F 302199F WP BS 960 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, LEFT OUTBOARD SIDE STUB FRAME FOUND CORRODED AROUND NUTS AT STA 960. REPAIRED PER SRM 53-2-0. 2 L 7 4 4F RT 4A25 1996082200682 19960822 00682 WP 1996 8 22 DHL9680602C 1 19960726 A 5311 561251618 FRAME DOUG DC8 DC873F 302199F WP BS 52 CORROSION A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FOUND EXFOLIATION CORRSOION ON FUSELAGE FRAME AT FLOOR BEAM ATTACH POINT, RIGHT SIDE OF CMPT FLOOR F.S.-52. REPAIRED FRAME IAW DOUGLAS FAX DATED 20 MAY 96 AND ROD SKETCH 96-05-001. REPAIRED FLOOR WEB PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1996082200683 19960822 00683 WP 1996 8 22 DHL9680603C 1 19960708 A 5330 57503293 SKIN DOUG DC8 DC873F 302199F WP BS 680-1030 CORROSION A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FOUND FUSELAGE UPPER EXTERIOR SKIN PANELS HAS NUMEROUS SPOTS OF CORROSION FS 680-1030 LONGERONS 1-13, LEFT A ND RIGHT SIDES. REPLACED SKIN PANELS PER SRM'S 51-1-21, 51-1-20, AND 51-1-0, AND DACO ACTION 301088. 2 L 7 4 4F RT 4A25 1996082200684 19960822 00684 WP 1996 8 22 DHL9680604C 1 19960716 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 404 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FOUND LEFT WING UPPER INTERIOR L/E HAS 4 INCH CRACK IN DOUBLER L/E, STA 404. REPAIRED DOUBLER PER DACO SKE TCH 96-05-29-002. 2 L 7 4 4F RT 4A25 1996082200685 19960822 00685 WP 1996 8 22 DHL9680605C 1 19960718 A 5320 5644011501 ANGLE DOUG DC8 DC873F 302199F WP BS 857 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, CABIN FLOOR ANGLE ON CTR FUEL TANK 28 LBL. REPLACED ANGLE AT FS 857 PER SRM 53-2-5. 2 L 7 4 4F RT 4A25 1996082200686 19960822 00686 WP 1996 8 22 DHL9680606C 1 19960718 A 5330 SKIN DOUG DC8 DC873F 302199F WP WS 96.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, LEFT UPPER PLATING STA XCW 96.5 CRACKED BEYOND LIMITS 7.5 INCHES IN LENGTH. HFEC INSPECTION PERFORMED ON CR ACK, AND ON BOLT HOLES PER S/B 57-86. REPAIRED PLATING CRACK PER SRM 57-2-1. 2 L 7 4 4F RT 4A25 1996082200687 19960822 00687 WP 1996 8 22 DHL9680607C 1 19960718 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1625 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, AFT ACCESSORY COMPT, FOUND CORROSION ON INTERIOR SKIN AT FS 1625 RBL 18. REPLACED SKIN PER SRM 53-02-01. 2 L 7 4 4F RT 4A25 1996082200688 19960822 00688 WP 1996 8 22 DHL9680608C 1 19960725 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FS 100 LEFT SIDE FRAME CORRODED BELOW CUSP ANGLE WEB ON FRAME AND FITTING. CUT CUSP ANGLE WEB AND REMOVED F ITTING, CLEANED AND TREATED CORROSION . REINSTALLED FITTING AND INSTALLED WEB SPLICE PER SRM 51-1-0 AND 51-3-0. 2 L 7 4 4F RT 4A25 1996082200689 19960822 00689 WP 1996 8 22 DHL9680609C 1 19960725 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 190 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, CABIN STA 190, RT BOTTOM FRAME ATTACHMENT CLIPS DAMAGED. REPLACED ANGLES, INSTALLED WEB SPLICE, DOOR JAMB C LOSE-OUT SPLICE, AND FRAME REPAIR PER ROD SKETCH 96-06-04-005. 2 L 7 4 4F RT 4A25 1996082200690 19960822 00690 WP 1996 8 22 DHL9680610C 1 19960726 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1624 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, COMPT AFT OF AFT BAGGAGE HAS CORROSION ON INTERIOR SKIN STA 1624 RBL 18 - LBL 18. REPLACED SKIN PER SRM 53- 02-01. 2 L 7 4 4F RT 4A25 1996082200691 19960822 00691 WP 1996 8 22 DHL9680611C 1 19960726 A 5320 PRESS PANEL DOUG DC8 DC873F 302199F WP BS 8-12 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, COCKPIT HAD HEAVY CORROSION BETWEEN FINGER DOUBLER AND PRESSURE PANEL BELOW COCKPIT FLOOR LEFT SIDE OF LBL 6 0, FS 8-12. INSTALLED FRAME REPAIR PER ROD SKETCH 96-05-16-00. 2 L 7 4 4F RT 4A25 1996082200692 19960822 00692 WP 1996 8 22 DHL9680612C 1 19960725 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, LEFT WING/LOWER SIDE SKIN DENTED AND CRACKED THROUGH. INSTALLED HOT BOND REPAIR 250 DEGREES CURE PER SRM 51 -1-9. 2 L 7 4 4F RT 4A25 1996082200693 19960822 00693 WP 1996 8 22 DHL9680613C 1 19960725 A 5330 SKIN DOUG DC8 DC873F 302199F WP FS 290 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, PREVIOUS REPAIR RT SIDE FS 290 TO COMPLY WITH SRM. UPGRADED REPAIR PER SRM 53-2-1. 2 L 7 4 4F RT 4A25 1996082200694 19960822 00694 WP 1996 8 22 DHL9680614C 1 19960725 A 7830 TR FORGING DOUG DC8 DC873F 302199F WP NR 3 ENG CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, NR 3 ENGINE OUTBOARD THRUST REVERSER UPPER HALF AFT END FORGING FOR SLIDE TUBE BRACKET CRACKED AT AFT END. REPAIRED CRACK PER HSLH REF 19-80059 AND G.E. FAX. 2 L 7 4 4F RT 4A25 1996082200695 19960822 00695 WP 1996 8 22 DHL9680615C 1 19960729 A 5542 SKIN DOUG DC8 DC873F 302199F WP RUDDER CORROSION A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FOUND RUDDER SKIN BULGED AND RIVETS POPPED RT SIDE ABOVE TRIM TAB STA ZR170. REPAIRED PER DACO ROD SKETCH 9 6-05-20-010 AND SRM 51-1-21. RE-BALANCED RUDDER. 2 L 7 4 4F RT 4A25 1996082200696 19960822 00696 WP 1996 8 22 DHL9680616C 1 19960726 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 220 BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, CABIN FRAME BROKEN AT FS 220 RIGHT BETWEEN STR 7R AND 8R. REMOVED AND REPAIRED BROKEN FRAME PER SRM 53-2-0 . 2 L 7 4 4F RT 4A25 1996082200697 19960822 00697 WP 1996 8 22 DHL9680617C 1 19960726 A 5312 BULKHEAD DOUG DC8 DC873F 302199F WP RT MLG WW CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, RIGHT W/W BULKHEAD UPPER INBD SECT OTBD OF CONTROL PULLEY HAS CORROSION. REPAIRED BULKHEAD PER EA PD 08-5 3-001 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996082200698 19960822 00698 WP 1996 8 22 DHL9680618C 1 19960726 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 80 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C- CHECK, FOUND FRAME CRACKED AT RIGHT SIDE STA 80. REPAIRED PER SRM 53-2-0. 2 L 7 4 4F RT 4A25 1996082200699 19960822 00699 WP 1996 8 22 DHL9680619C 1 19960726 A 5730 SKIN DOUG DC8 DC873F 302199F WP LEFT WING CORROSION A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, LEFT WING TOP SURFACE BETWEEN NR 1 ENGINE AND NR 2 ENGINE BULGED BY CORROSION IN SEVERAL PLACES. REMOVED CO RROSION AND REPAIRED PER SRM 57-2-1. 2 L 7 4 4F RT 4A25 1996082200700 19960822 00700 NM 1996 8 22 P5CA9600557 1 19960715 A 5210 BACB10CF14PP BEARING BOEING 747 747132 1384882 NM L5 DOOR DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 DAMAGED BEARING AT THE BODY TORQUE TUBE CAM PLATE ON L5 DOOR. REPLACED CAM PLATE BEARING AND CK'D DOOR RIG PER BAC MM 5 3-10-03 FIG 6 AND HAECO REPAIR SCHEME R-53-00-32968. 2 L 7 4 4F A20WE 1996082200701 19960822 00701 NM 1996 8 22 P5CA9600558 1 19960715 A 5313 STRINGER BOEING 747 747132 1384882 NM BS 1980 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACK AT STRINGER 3L STA 1980. REPAIRED STRINGER 3L CRACK PER BAC SRM. 2 L 7 4 4F A20WE 1996082200702 19960822 00702 NM 1996 8 22 P5CA9600559 1 19960715 A 5720 BACR15BA6AD10 FASTENER BOEING 747 747132 1384882 NM FRONT SPAR MISSING A P5CA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 23 856FT 19897 MISSING FASTENER AT FSSI 950 COMMON TO WING FRONT SPAR CHORD. RIVET REPLACED PER BAC SRM 51-30-02. 2 L 7 4 4F A20WE 1996082200703 19960822 00703 NM 1996 8 22 P5CA9600560 1 19960715 A 5320 DOOR FRAME BOEING 747 747132 1384882 NM CARGO DR CUTOUT DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 DENT IN SIDE CARGO DOOR CUTOUT FRAME INBOARD ATTACH METAL STRAP BS 1940 APPROX S11L. METAL STRAP REPLACED PER BAC SRM 5 1-10-01 PG 8. 2 L 7 4 4F A20WE 1996082200704 19960822 00704 NM 1996 8 22 P5CA9600561 1 19960715 A 5522 SKIN BOEING 747 747132 1384882 NM LT ELEV PUNCTURED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 SMALL PUNCH (HOLE) ON UPPER LEFT INBD ELEVATOR SURFACE. FIBERGLASS REPAIR PER BAC SRM 51-40-15. 2 L 7 4 4F A20WE 1996082200705 19960822 00705 NM 1996 8 22 P5CA9600562 1 19960715 A 5321 FLOOR BOEING 747 747132 1384882 NM BS 2160-2200 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION LEFT OTBD MAIN DECK FLOOR WEB UPPER SURFACE BS 2160 TO BS 2200. REMOVED CORROSION AND RE-PROTECTED PE R BAC SRM 51-01-01. 2 L 7 4 4F A20WE 1996082200706 19960822 00706 NM 1996 8 22 P5CA9600563 1 19960715 A 5315 SUPPORT BOEING 747 747132 1384882 NM BS 2200-2220 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION AT MAIN DECK LEFT OTBD LONGITUDINAL FLOOR SUPPORT STA 2200 TO STA 2220. REMOVED CORROSION AND RE-PROT ECTED PER BAC SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1996082200707 19960822 00707 NM 1996 8 22 P5CA9600564 1 19960715 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 2182 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION AT MAIN DECK TIE DOWN (SEAT) TRACK STA 2182 LBL 98. CORROSION REMOVED AND RE-PROTECTED PER BAC SRM 51 -10-01 AND SRM 51-10-02. 2 L 7 4 4F A20WE 1996082200708 19960822 00708 NM 1996 8 22 P5CA9600565 1 19960715 A 5315 FLOOR BEAM BOEING 747 747132 1384882 NM BS 2200 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION TO MAIN DECK FLOOR BEAM UPPER CHORD STA 2200 BETWEEN LBL 87 AND LBL 98. REMOVED CORROSION AND RE-PROT ECTED PER BAC SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1996082200709 19960822 00709 NM 1996 8 22 P5CA9600566 1 19960715 A 5713 STRINGER BOEING 747 747132 1384882 NM WS 670 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACK AT WING STA 670 FORWARD UPPER STRINGER CAP IN NR 2 MAIN TANK. REPAIRED IAW SB 57-2273 FIG'S 7 AND 9 AND HAECO TEC H ASSISTANCE REQUISITION 058029. 2 L 7 4 4F A20WE 1996082200710 19960822 00710 NM 1996 8 22 P5CA9600567 1 19960715 A 5753 FAIRING BOEING 747 747132 1384882 NM LT TE FLAP DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 DAMAGED LEFT WING NR 2 FLAP TRACK FORWARD FIXED FAIRING EXTERNAL SURFACE. REPAIRED PER BOEING SRM 51-40-15. 2 L 7 4 4F A20WE 1996082200711 19960822 00711 NM 1996 8 22 P5CA9600568 1 19960715 A 5320 SUPPORT BOEING 747 747132 1384882 NM BS 2350 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION ON LATERAL FLOOR SUPPORT AT MAIN DECK STA 2350 BETWEEN RBL 10 AND RBL 40. REMOVED CORROSION PER BAC S RM 51-10-01 AND RE-PROTECTED PER BAC SRM 51-10-02. 2 L 7 4 4F A20WE 1996082200712 19960822 00712 NM 1996 8 22 P5CA9600569 1 19960715 A 5753 FAIRING BOEING 747 747132 1384882 NM LT TE FLAP DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 DAMAGED NR 1 FLAP TRACK FORWARD FIXED FAIRING EXTERNAL SURFACE. REPAIRED PER BAC SRM 51-40-15. 2 L 7 4 4F A20WE 1996082200713 19960822 00713 NM 1996 8 22 P5CA9600570 1 19960715 A 5753 FAIRING BOEING 747 747132 1384882 NM RT TE FLAP DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 DAMAGED NR 8 FLAP TRACK FORWARD FIXED FAIRING EXTERIOR SURFACE. REPAIRED PER BOEING SRM 51-40-15. 2 L 7 4 4F A20WE 1996082200714 19960822 00714 NM 1996 8 22 P5CA9600572 1 19960715 A 2550 ROLLER TRAY BOEING 747 747132 1384882 NM CARGO COMPT CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACKED ANGLE AREA ON ROLLER TRAY. REPAIRED PER BOEING SRM 51-40-03. 2 L 7 4 4F A20WE 1996082200715 19960822 00715 NM 1996 8 22 P5CA9600573 1 19960715 A 5280 DOOR BOEING 747 747132 1384882 NM LT/RT MLG STRUT DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 DAMAGE EXTERNAL AREA OF BOTH WING LANDING GEAR STRUT DOORS. REPAIRED PER BOEING SRM 51-40-15. 2 L 7 4 4F A20WE 1996082200716 19960822 00716 NM 1996 8 22 P5CA9600574 1 19960715 A 5753 SKIN BOEING 747 747132 1384882 NM RT TE FORE FLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACK RIGHT WING OUTBOARD FORE FLAP LEADING EDGE SKIN. REPAIRED PER BOEING SRM 51-40-15. 2 L 7 4 4F A20WE 1996082200717 19960822 00717 NM 1996 8 22 P5CA9600575 1 19960715 A 5320 SUPPORT BOEING 747 747132 1384882 NM BS 2280-2300 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 2 CORROSION TO RT OTBD MAIN DECK FLOOR SUPPORT AT STA 2280 TO 2300. REPLACED FLOOR SUPPORT PER BAC SRM 51-10-01 P G 18. 2 L 7 4 4F A20WE 1996082200718 19960822 00718 NM 1996 8 22 P5CA9600576 1 19960715 A 5753 TE SKIN BOEING 747 747132 1384882 NM LT TE FORE FLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACK LEFT WING INBOARD FORE FLAP TRAILING EDGE AT APPROXIMATELY NR 3 FLAP TRACK POSITION. REPAIRED PER BOEING SRM 51-4 0-15. 2 L 7 4 4F A20WE 1996082200719 19960822 00719 NM 1996 8 22 P5CA9600577 1 19960715 A 5313 STRINGER BOEING 747 747132 1384882 NM BS 360-380 DEFORMED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 STRINGER 40 DEFORMED FWD CARGO COMP RT STA 360 TO STA 380. REFORMED STRINGER PER BAC SRM 51-40-01 AND HFEC CK OK. 2 L 7 4 4F A20WE 1996082200720 19960822 00720 NM 1996 8 22 P5CA9600578 1 19960715 A 5753 SKIN BOEING 747 747132 1384882 NM RT TE MID FLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 DELAMINATED RIGHT WING INBOARD MID FLAP LOWER SKIN ADJACENT TO THE INBOARD FLAP TRACK. REPAIRED PER BOEING SRM 51-40-15 . 2 L 7 4 4F A20WE 1996082200721 19960822 00721 NM 1996 8 22 P5CA9600579 1 19960715 A 5753 SKIN BOEING 747 747132 1384882 NM RT TE AFT FLAP DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 DAMAGED SKIN ON RIGHT WING INBOARD AFT FLAP LOWER SURFACE ADJACENT TO NR 6 FLAP TRACK. REPAIRED PER BOEING SRM 51-40-15 . 2 L 7 4 4F A20WE 1996082200722 19960822 00722 NM 1996 8 22 P5CA9600580 1 19960715 A 5753 SKIN BOEING 747 747132 1384882 NM RT TE AFT FLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACKED SKIN ON RIGHT WING INBOARD AFT FLAP LOWER SURFACE. REPAIRED PER BOEING SRM 51-40-06. 2 L 7 4 4F A20WE 1996082200723 19960822 00723 NM 1996 8 22 P5CA9600582 1 19960715 A 5730 PANEL BOEING 747 747132 1384882 NM LT WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACKED PANEL NR 573AB. REPAIRED PER BOEING SRM 51-40-15. 2 L 7 4 4F A20WE 1996082200724 19960822 00724 NM 1996 8 22 P5CA9600583 1 19960715 A 5320 TENSION TIE BOEING 747 747132 1384882 NM BS 900 DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 DENT ON FWD SIDE OF TENSION TIE AT MAIN DECK STA 900 RBL 60 APPROX S10L. REPAIRED TENSION TIE PER BAC SRM 51-40-03 FIG 1. 2 L 7 4 4F A20WE 1996082200725 19960822 00725 NM 1996 8 22 P5CA9600584 1 19960715 A 5320 TENSION TIE BOEING 747 747132 1384882 NM BS 800 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACK TO RT OTBD END OF TENSION TIE AT MAIN DECK STA 800 APPROX S11R. REPAIRED TENSION TIE PER HAECO DESIGN DEVIATION O RDER HX135017 AND IAI SB 747-53-2371. 2 L 7 4 4F A20WE 1996082200726 19960822 00726 NM 1996 8 22 P5CA9600585 1 19960715 A 5320 SCUFF PLATE BOEING 747 747132 1384882 NM R1 DOOR CUTOUT CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACK ON R1 DOOR SCUFF PLATE CORNER AREA. WELD REPAIR ACCOMPLISHED PER HAECO STANDARD PRACTICE 70-310-003. 2 L 7 4 4F A20WE 1996082200727 19960822 00727 NM 1996 8 22 P5CA9600586 1 19960715 A 5320 TENSION TIE BOEING 747 747132 1384882 NM BS 900 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACK AT MAIN DECK LEFT OTBD END TENSION TIE STA 900 APPROX S11L. TENSION TIE REPAIRED PER SB 747-53-2371 FIG 3 AND HAE CO DESIGN DEVIATION ORDER HX135017. 2 L 7 4 4F A20WE 1996082200728 19960822 00728 NM 1996 8 22 P5CA9600587 1 19960715 A 5320 TENSION TIE BOEING 747 747132 1384882 NM BS 780 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACK AT MAIN DECK LEFT OTBD END OF TENSION TIE AT STA 780 APPROX S11L. REPAIRED TENSION TIE PER SB 747-53-2371 AND HAE CO DESIGN DEVIATION ORDER HX135017. 2 L 7 4 4F A20WE 1996082200729 19960822 00729 NM 1996 8 22 P5CA9600588 1 19960715 A 5320 TENSION TIE BOEING 747 747132 1384882 NM BS 800 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACK AT MAIN DECK LEFT OTBD END OF TENSION TIE AT STA 800 APPROX S11L. REPAIRED TENSION TIE PER SB 747-53-2371 AND HAE CO DESIGN DEVIATION ORDER HX135017. 2 L 7 4 4F A20WE 1996082200730 19960822 00730 NM 1996 8 22 P5CA9600589 1 19960715 A 5720 STIFFENER BOEING 747 747132 1384882 NM WS 670 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACK AT OTBD FRONT SPAR VERTICAL RIB STIFFENER IN NR 3 MAIN TANK AT WS 670. TEMP REPAIR, STOP DRILLED CRACK AND INSTAL LED A REPAIR STRAP PER HAECO REPAIR SCHEME R-57-21-32967 AND BOEING FAX APPROVAL. 2 L 7 4 4F A20WE 1996082200731 19960822 00731 NM 1996 8 22 P5CA9600590 1 19960715 A 5315 FLOOR BEAM BOEING 747 747132 1384882 NM BS 2360 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION ON RT OTBD MAIN DECK FLOOR BEAM UPPER CHORD AT STA 2360. REMOVED CORROSION PER BAC SRM 51-10-01 AND RE-PROTECTED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1996082200732 19960822 00732 NM 1996 8 22 P5CA9600591 1 19960715 A 5720 BACB30MR5K20 BOLT BOEING 747 747132 1384882 NM WS 590 SHEARED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 SHEARED BOLT AT APPROX WS 590 LWR ATTACH FOR STRINGER 7 IN NR 3 MAIN TANK. REPLACED BOLT. 2 L 7 4 4F A20WE 1996082200733 19960822 00733 NM 1996 8 22 P5CA9600592 1 19960715 A 5720 BACB30MY12K11X FASTENERS BOEING 747 747132 1384882 NM WS 660 SHEARED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 TWO SHEARED RIVETS (FASTENERS) AT FRONT SPAR LOWER CHORD AT APPROX WS 660 IN NR 3 MAIN TANK. REPLACED FASTENERS PER BAC SRM 51-30-02. 2 L 7 4 4F A20WE 1996082200734 19960822 00734 NM 1996 8 22 P5CA9600593 1 19960715 A 5320 SUPPORT BOEING 747 747132 1384882 NM BS 2060-2190 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CORROSION ON RT OTBD MAIN DECK FLOOR SUPPORT BETWEEN STA 2060 AND 2190. CORROSION REPAIR PER BAC SRM 51-40-03. (REF HA ECO NR'S 5256 AND 5257). 2 L 7 4 4F A20WE 1996082200735 19960822 00735 NM 1996 8 22 P5CA9600594 1 19960715 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 2200-2220 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CORROSION AT MAIN DECK TIE DOWN (SEAT) TRACK INBD FLANGE FROM STA 2200 TO STA 2220 LBL11. CORROSION REMOVED AND RE-PROT ECTED PER BAC SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1996082200736 19960822 00736 NM 1996 8 22 P5CA9600595 1 19960715 A 5320 PLATE BOEING 747 747132 1384882 NM BS 2240 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CORROSION AT MAIN DECK TIE DOWN PLATE UPPER SURFACE AT STA 2240 LBL3. CORROSION REMOVED AS PER BAC SRM 51-10-01 AND RE- PROTECTED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1996082200737 19960822 00737 NM 1996 8 22 P5CA9600596 1 19960715 A 5320 SUPPORT BOEING 747 747132 1384882 NM BS 1720-1730 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CORROSION ON MAIN DECK RT OTBD LONG FLOOR SUPPORT UPPER SURFACE BETWEEN STA 1720 AND STA 1730. CORROSION REMOVED AND RE -PROTECTED PER BAC SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1996082200738 19960822 00738 NM 1996 8 22 P5CA9600597 1 19960715 A 5320 SUPPORT BOEING 747 747132 1384882 NM BS 400 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CORROSION AT FWD LOWER CARGO SUPPORT BEAM EDGE AT STA 400 LT/RT S44 TO 46. CORROSION REMOVED AND RE-PROTECTED PER BAC S RM 51-10-01 AND SRM 51-10-02. 2 L 7 4 4F A20WE 1996082200739 19960822 00739 NM 1996 8 22 P5CA9600598 1 19960715 A 5400 ACOUSTIC PANEL BOEING 747 747132 1384882 NM NR 3 ENG COWL DEBONDED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 DEBONDING AT NR 3 NOSE COWL 11 O'CLOCK POSITION ACOUSTIC PANEL. REPAIRED PER BAC SRM 54-30-03 FIG 29. 2 L 7 4 4F A20WE 1996082200740 19960822 00740 NM 1996 8 22 P5CA9600599 1 19960715 A 5320 BRACKET BOEING 747 747132 1384882 NM BS 960 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACK AT UPPER FRAME ATTACH ANGLE AT STA 960 S7R APPROX .6250 INCH LONG. REPLACED FRAME ATTACH BRACKET PER BAC SRM 51-1 0-10 PG 18. 2 L 7 4 4F A20WE 1996082600001 19960826 00001 WP 1996 8 26 96ZZZM1228 1 19960705 A 5753 CLEVIS DOUG DC8 DC8F54 3021926 WP LT TE FLAP CRACK A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 426FB 45667 DURING C-CHECK INSPECTION, A CRACK WAS FOUND EMANATING FROM A FASTENER HOLE IN THE LOWER TANG OF THE CLEVIS ON THE LEFT WING INBOARD FLAP. REPAIRED CLEVIS BY INSTALLING A 2 INCH BY 2 INCH DOUBLER MADE OF .125 A1S1 301 1/2 H MATERIAL IAW EO 960511. 8110 ISSUED BY DER SW-713. 2 L 7 4 4F 4A25 1996082600002 19960826 00002 WP 1996 8 26 96ZZZM1229 1 19960705 A 5753 CLEVIS DOUG DC8 DC8F54 3021926 WP RT TE FLAP CRACKED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 426FB 45667 DURING C-CHECK INSPECTION, A CRACK WAS FOUND EMANATING FROM A FASTENER HOLE IN THE LOWER TANG OF THE RIGHT WING INBOARD FLAP LOWER CLEVIS. REPAIRED CLEVIS BY INSTALLING A 2 INCH BY 2 INCH DOUBLER MADE OF .125 A1S1 301 1/2 H MATERIAL IAW EO 9606181. 8110-3 ISSUED BY DER SW-713. 2 L 7 4 4F 4A25 1996082600003 19960826 00003 EU 1996 8 26 96ZZZM1237 1 19960712 A 2131 9022157028 CONTROLLER AIRBUS 320 A320231 3930325 EU NR 2 FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 632AW 81 CMH - FLT 2688 - CMH-EWR - AIR TURNBACK, LOSS OF CABIN PRESSURE. CREW DESCENDED TO 10,000 FEET. REMOVED AND REPLACED O UTFLOW VALVE, IAW 21-31-51. REMOVED AND REPLACED CABIN PRESSURE CONTROLLERS NR 1 AND NR 2 AS PRECAUTION IAW 21-31-34. R ESTOWED CABIN MASKS. REMOVED AND REPLACED USED OXYGEN GENERATORS IAW 35-23-00. REFERENCE AWXA960337. 2 L 7 2 4F RT A28NM 1996082600004 19960826 00004 EU 1996 8 26 96ZZZM1238 1 19960712 A 2133 9023157034 OUTFLOW VLV AIRBUS 320 A320231 3930325 EU CABIN FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 632AW 3631 81 CMH - FLT 2688 - CMH-EWR - AIR TURNBACK, LOSS OF CABIN PRESSURE. CREW DESCENDED TO 10,000 FEET. REMOVED AND REPLACED O UTFLOW VALVE, IAW 21-31-51. REMOVED AND REPLACED CABIN PRESSURE CONTROLLERS NR 1 AND NR 2 AS PRECAUTION IAW 21-31-34. R ESTOWED CABIN MASKS. REMOVED AND REPLACED USED OXYGEN GENERATORS IAW 35-23-00. REFERENCE AWXA960337. 2 L 7 2 4F RT A28NM 1996082600005 19960826 00005 EU 1996 8 26 96ZZZM1240 1 19960728 A 3040 EAQTC8803405 HEAT CONTROLLER FOKKER F28 F28MK0100 4990807 EU LEFT FAILED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 889US 11358 SYR - FL 1052 - AT FL 280 NEAR ABL, CAPTAIN'S WINDSHIELD OUTER PANE SHATTERED. FLIGHT DIVERTED TO SYR AND LANDED WITH N O FURTHER INCIDENT. MAINTENANCE REPLACED THE WINDSHIELD AND THE HEAT CONTROLLER. REFERENCE USAAF96081. 2 L 7 2 4F RT 1996082600006 19960826 00006 WP 1996 8 26 ASAA9680156 1 19960724 A 5210 CNTRL ROD LOCK DOUG DC9 DC982 3022082 WP L1 DOOR LOOSE A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 934AS 49235 SEA - AFTER ARRIVAL OF FLT 371, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN AND LATCH IN OPEN POSITION. FOUND HOLD OPEN HOOK BENT AND DOOR CONTROL ROD LOCK LOOSE. REPLACED DOOR HOLD OPEN HOOK, TIGHTENED AND SAFTIED CONTROL ROD LOCK AN D DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996082600007 19960826 00007 WP 1996 8 26 ASAA9680158 1 19960725 A 5220 LANYARD DOUG DC9 DC982 3022082 WP EMERG EXIT DOOR OUT OF POSITION A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 951AS 49111 SEA - DURING MAINTENANCE CHECK, THE LEFT FORWARD OVERWING EMERGENCY EXIT DOOR WAS FOUND DIFFICULT TO OPEN. FOUND LANYAR D LODGED BETWEEN DOOR AND FRAME, REMOVED LANYARD AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996082600008 19960826 00008 EU 1996 8 26 AWXA960337 1 19960712 A 2130 CONNECTOR AIRBUS 320 A320231 3930325 EU OUTFLOW VLV LOOSE A AWXA A G UNSCHED LANDING O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 WP 28 632AW 81 CMH - FLT 2686 - CMH-EWR - AIR TURNBACK, LOSS OF CABIN PRESSURE. CREW DESCENDED TO 10,000 FEET. REMOVED AND REPLACED O UTFLOW VALVE IAW 21-31-51. REMOVED AND REPLACED CABIN PRESSURE CONTROLLERS NR 1 AND NR 2 AS PRECAUTION IAW 21-31-34. R ESTOWED CABIN MASKS. REMOVED AND REPLACED USED OXYGEN GENERATORS IAW 35-23-00. FOUND LOOSE CONNECTOR. (M) 2 L 7 2 4F RT A28NM 1996082600009 19960826 00009 EU 1996 8 26 AWXA960351 1 19960709 A 5320 BEAM AIRBUS 320 A320231 3930325 EU BS 1800 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 55 DURING ROUTINE SCHEDULED C-5 MAINTENANCE CHECK, FOUND CORROSION ON THRESHOLD SUPPORT BEAM FR 68, Y 1800, LEFT Z -540 'MA RKED'. BLENDED CORROSION 2 INCH BY 1 INCH BY .035 INCH ORIGINAL THICKNESS OF .071 FOUND OUT OF LIMITS PER MM 53-00-14. FABRICATED REPAIR AND INSTALLED PER SRM 53-00-14. (M) 2 L 7 2 4F RT A28NM 1996082600010 19960826 00010 EU 1996 8 26 AWXA960352 1 19960708 A 5320 RAIL AIRBUS 320 A320231 3930325 EU BS 254 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 55 PAE - FLT 7809 - DURING ROUTINE SCHEDULED C-5 MAINTENANCE CHECK, FOUND CORROSION ON DUMMY RAIL Y=-254, FR 20 THOUGH FR 1 6. REMOVED, FABRICATED AND INSTALLED REPAIR PER SRM 53-11-14. (M) 2 L 7 2 4F RT A28NM 1996082600011 19960826 00011 EU 1996 8 26 AWXA960353 1 19960708 A 5320 RAIL AIRBUS 320 A320231 3930325 EU BS 254 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 55 PAE - FLT 7809 - DURING ROUTINE SCHEDULED C-5 MAINTENANCE CHECK, FOUND CORROSION ON DUMMY RAIL Y=254, FR 21 THROUGH FR 1 6, Z -540. REMOVED, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-11-14. (M) 2 L 7 2 4F RT A28NM 1996082600012 19960826 00012 EU 1996 8 26 AWXA960354 1 19960711 A 5320 ASNA2222 RAIL AIRBUS 320 A320231 3930325 EU BS 1292 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 55 PAE - FLT 7809 - DURING ROUTINE SCHEDULED C-5 MAINTENANCE CHECK, FOUND CORROSION ON DUMMY RAIL AT Y 1292, FR 20 THROUGH FR 18, Z-540. REMOVED AND REPLACED DUMMY RAIL FR 16 THROUGH FR 20, Y 1292, Z -540, IAW SRM 51-72-11, SRM 53-11-14. (M) 2 L 7 2 4F RT A28NM 1996082600013 19960826 00013 EU 1996 8 26 AWXA960355 1 19960715 A 5320 RAIL AIRBUS 320 A320231 3930325 EU BS 1292 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 55 PAE - FLT 7809 - DURING ROUTINE SCHEDULED C-5 MAINTENANCE CHECK, FOUND CORROSION ON DUMMY RAIL -1292, FR 20 THROUGH FR 1 6, Z-540. REPAIRED DUMMY RAIL IAW SRM 53-11-41. (M) 2 L 7 2 4F RT A28NM 1996082600014 19960826 00014 EU 1996 8 26 AWXA960356 1 19960716 A 5347 ASNA2223E7175 SEAT TRACK AIRBUS 320 A320231 3930325 EU BS 1292 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 55 PAE - FLT 7809 - DURING ROUTINE SCHEDULED C-5 MAINTENANCE CHECK, FOUND CORROSION ON SEAT TRACK -1292, Z-540, FR 20. REM OVED AND REPLACED SEAT TRACK AT Y-1292, Z-540, FR 20 TO FR 24 PER SRM 51-72-11 AND 51-42-21. (M) 2 L 7 2 4F RT A28NM 1996082600015 19960826 00015 NM 1996 8 26 EISA96101 1 19960704 A 5230 652255750 FAIRING BOEING 727 72782 1384029 NM AFT CARGO MISSING A A EISA K NONE D INFLIGHT SEPARATION CR CRUISE 1 SW 07 357NE 19405 POST FLIGHT INSPECTION SHOWED, THE AFT CARGO MOVEABLE FAIRING WAS MISSING. REPLACED AFT CARGO DOOR MOVEABLE FAIRING AND RIGGED IAW MM 52-33-0. OPS CHECK GOOD. (M) 2 L 7 3 4F A3WE 1996082600016 19960826 00016 NM 1996 8 26 EISA96103 1 19960726 A 3231 RETRACT MECH BOEING 727 72725 1384006 NM NLG DOORS OUT OF ADJUST A EISA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SW 07 290NE 18972 NOSE GEAR DOORS VIBRATE AND FWD PANEL 'DOOR LIGHT' ON F/E PANEL NOSE GEAR DOOR LIGHTS COME ON. 305KIAS RECYCLED GEAR, S AME PROBLEM 330KIAS. RIGGED NLG DOORS PER MM 32-22-12 AND MM 32-22-1, OPS CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1996082600017 19960826 00017 NM 1996 8 26 HNAA9690945 1 19960627 A 3240 BRAKES DHAV DHC8 DHC8102 2809003 NM LANDING GEAR FAILED A HNAA K NONE O OTHER TX TAXI/GRND HDL 1 EA 07 909HA 018 FLT NR 3350 - ORF-DCA - MAIN BRAKES FAILED ON TAXI OUT FROM HANGAR. THE AIRCRAFT DEPARTED THE TAXIWAY ONTO THE GRASS. I NSPECTED THE NOSE GEAR STEERING FUSE, STEERING LINKS, AND GENERAL CONDITION OF NOSE GEAR AFTER A/C WAS TOWED BY NORMAL C ONDITIONS BACK ONTO THE TAXIWAY. PERFORMED BLEEDING OF NR 1 AND NR 2 HYDRAULIC SYSTEMS AND OPERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 1996082600018 19960826 00018 WP 1996 8 26 IXXA96105 1 19960706 A 2612 3900 FIRE DETECT AMP DOUG DC8 DC862F 3021972 WP NR 3 ENGINE MALFUNCTIONED A IXXA E F A ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 11 41CX 932 46129 EN ROUTE QPG TO OKO, THE NR 3 ENGINE FIRE WARNING LIGHTS ILLUMINATED. CREW SHUT THE ENGINE DOWN AND SEQUENCED THE FIRE BOTTLE FOR THAT ENGINE ON A PRECAUTIONARY BASIS. AIRCRAFT RETURNED QPG WITH AN UNEVENTFUL LANDING. MAINTENANCE INSPECT ED THE ENGINE FOR EVIDENCE OF A FIRE, NO EVIDENCE WAS FOUND. MAINTENANCE REPLACED THE FIRE BOTTLE, FIRE DETECTOR AMPLIF IER AND CLEANED THE FIRE DETECTOR CONNECTORS. A SUCCESSFUL ENGINE RUN WAS COMPLETED AND THE AIRCRAFT WAS RETURNED TO SE RVICE. (M) 2 L 7 4 4F 4A25 1996082600019 19960826 00019 NM 1996 8 26 MALA965072 1 19960714 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN DIRTY A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 854MA 357 DURING THE PREFLIGHT INSPECTION IN DTW, THE FLIGHT ATTENDANT WAS UNABLE TO TURN ON THE EMERGENCY LIGHTS. MAINTENANCE CL EANED A DIRTY CONNECTION AT THE EMERGENCY LIGHT CONTROL BOX. ALL CHECKS SATISFACTORY. (M) 2 H 7 2 4T RT A13NM 1996082600020 19960826 00020 NM 1996 8 26 MALA965074 1 19960714 A 2120 AIR DISTR DHAV DHC8 DHC8102 2809003 NM COCKPIT ODOR A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 15 866MA 366 FLT NR 3340 - EN ROUTE TO DTW, THE CREW NOTED AN OIL SMELL WHEN THE BLEEDS WERE TURNED ON. THE CREW WAS UNABLE TO IDENT IFY WHICH SYSTEM (LEFT OR RIGHT) WAS PRODUCING THE ODOR. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. (M) 2 H 7 2 4T RT A13NM 1996082600021 19960826 00021 NM 1996 8 26 MALA965076 1 19960718 A 7712 311197801 TQ PICKUP PROBE DHAV DHC8 DHC8102 2809003 NM LT ENG FAILED A MALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 15 865MA 364 FLT NR 3389 - ON CLIMB-OUT FROM DTW, THE LEFT ENGINE EXPERIENCED A 20 PERCENT POWER LOSS. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED A TORQUE PICKUP PROBE. ALL CHECKS SATISFACTORY. (M) 2 H 7 2 4T RT A13NM 1996082600022 19960826 00022 EU 1996 8 26 SIMA962081 1 19960726 A 2120 AIR DISTR SAAB SF340 340B 7860101 EU CABIN ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 21 359SB 340B359 DFW - FLT 3537 - APPROX 5 MINUTES PRIOR TO LANDING, FLIGHT ATTENDANT REPORTED SMELLING RUBBER/ELECTRICAL ODOR IN CABIN A REA ROW 5, FLT CREW INCREASED CABIN PRESSURIZATION AND ODOR DISAPPEARED. AIRCRAFT LANDED SAFELY AND TAXIED TO PARKING A REA. GROUND RUNS PERFORMED AND OPS CHECKED AIRCRAFT. UNABLE TO DUPLICATE ANY ODOR OR RUBBER/ELECTRICAL SMELL. AIRCRAF T WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1996082600023 19960826 00023 EU 1996 8 26 USAAF96079 2 19960717 A 7200 ENGINE FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAYMK65015 EU RIGHT FAILED A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 EA 19 880US 11331 17242 RDU - AIRCRAFT HAS SMOKY SMELL IN CABIN AT HIGH POWER SETTINGS. SMELL DISSIPATES AT LOWER POWER SETTINGS. MAINTENANCE REPLACED THE RIGHT ENGINE DUE TO AN OIL LEAK. ENGINE ASSEMBLY WAS OVERHAULED. SPECIFIC ENGINE FAILURE THAT CAUSED SMOK E IN THE CABIN WAS PROBABLY DUE TO AN OIL CATCHER PLATE NUT LOOSE ON HPC FRONT BEARING HOUSING. (M) 2 L 7 2 4F 4 F RT 1996082600024 19960826 00024 EU 1996 8 26 USAAF96080 1 19960721 A 3260 SK3852 INDICATOR MODULE FOKKER F28 F28MK0100 4990807 EU COCKPIT MALFUNCTIONED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 856US 11286 FLT NR 503 - CLT-DAY - LEFT MAIN GEAR GREEN LIGHT REMAINS ON WITH GEAR RETRACTED. RETURNED TO FIELD. MAINTENANCE REPLA CED THE LANDING GEAR INDICATOR MODULE. (M) 2 L 7 2 4F RT 1996082600025 19960826 00025 EU 1996 8 26 USAAF96081 1 19960728 A 5610 WINDSHIELD FOKKER F28 F28MK0100 4990807 EU LEFT FAILED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 889US 11358 SYR - FL 1052 - AT FL 280 NEAR ABL, CAPTAIN'S WINDSHIELD OUTER PANE SHATTERED. FLIGHT DIVERTED TO SYR AND LANDED WITH N O FURTHER INCIDENT. MAINTENANCE REPLACED THE WINDSHIELD AND THE HEAT CONTROLLER. (M) 2 L 7 2 4F RT 1996082600026 19960826 00026 EU 1996 8 26 USAAF96083 1 19960729 A 3350 6104781 BATT SUPPLY UNIT FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 854US 11282 MCI - EMERGENCY FLOOR LIGHTING SYSTEM INOPERATIVE WITH SWITCH IN ON POSITION. AIRCRAFT FERRIED TO CLT. MAINTENANCE REP LACED FOUR BATTERY SUPPLY UNITS. (M) 2 L 7 2 4F RT 1996082600027 19960826 00027 EU 1996 8 26 VTZA96240 1 19960703 A 3320 31851A CONNECTOR BAG JETSTM JETSTM3201 1500217 EU CABIN FAILED A VTZA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 27 471UE 821 FLT NR 6586 - IAD-ISP - DURING CLIMB-OUT AN EMERGENCY WAS DECLARED DUE TO REPORTED SMOKE AND ELECTRIC ODOR IN THE CABIN. AIRCRAFT RETURNED AND LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE PERFORMED INSPECTIONS AND REPLACED THE OVE RHEAD LIGHT CONNECTOR AT SEAT 2A. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996082600028 19960826 00028 EU 1996 8 26 VTZA96241 1 19960701 A 6120 91SE16 SWITCH BAG JETSTM JETSTM3201 1500217 EU CENTER CONSOLE OUT OF ADJUST A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 494UE 810 FLT NR 6228 - PHL-IAD - ABORTED THE TAKEOFF DUE TO THE RIGHT REVERSE CAP LIGHT REMAINING ILLUMINATED DURING THE TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI 42442 IAW MEL 61-2 ON THE REVERSE CA P SYSTEM. MAINTENANCE LATER CLEARED DMI NR 42442, BY ADJUSTING THE RIGHT REVERSE MICROSWITCH. AIRCRAFT WAS RELEASED AN D APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996082600029 19960826 00029 EU 1996 8 26 VTZA96242 1 19960704 A 5270 91SE16 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAG DOOR DIRTY A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 302UE 41013 FLT NR 6261 - IAD-EWR - ABORTED TAKEOFF DUE TO THE BAGGAGE DOOR WARNING LIGHT ILLUMINATING. AIRCRAFT RETURNED TO GATE W ITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 52851 IAW MEL 52-3. MAINTENANCE LATER CLEARED DMI NR 52851, BY CLE ANING AND LUBING THE DOOR WARNING MICROSWITCHES. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996082600030 19960826 00030 EU 1996 8 26 VTZA96243 1 19960706 A 5270 918E16 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGGAGE DOOR OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 314UE 41027 FLT NR 6265 - IAD-BTV - ABORTED TAKEOFF DUE TO THE BAGGAGE DOOR WARNING LIGHT ILLUMINATING. AIRCRAFT RETURNED TO GATE W ITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI03817 ON BAGGAGE DOOR LIGHT ILLUMINATING, MEL 52-30. MAINTENANCE CLOSE D DMI 03817, BY ADJUSTING MICROSWITCH. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996082600031 19960826 00031 EU 1996 8 26 VTZA96245 1 19960709 A 5270 SP4594 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU MAIN BAGG DOOR DIRTY A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 307UE 41021 FLT NR 6532 - LGA-IAD - ABORTED THE TAKEOFF DUE TO THE MAIN BAGGAGE DOOR WARNING. AIRCRAFT RETURNED TO GATE WITH NO FUR THER INCIDENTS. MAINTENANCE CLEANED AND INSPECTED BAGGAGE DOOR MICROSWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RET URN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996082600032 19960826 00032 EU 1996 8 26 VTZA96246 1 19960709 A 7797 WIRE HARNESS BAG JETSTM JETSTM3201 1500217 EU LT ENGINE CHAFED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 482UE 897 FLT NR 6284 - IAD-HPN - DURING CLIMB, RETURNED TO IAD DUE TO LEFT ENGINE EGT FLUCTUATION. AIRCRAFT LANDED AND RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPAIRED CHAFED HARNESS AND OPS CHECK OK. AIRCRAFT WAS RELEASED AND APP ROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996082600033 19960826 00033 EU 1996 8 26 VTZA96247 1 19960708 A 2611 72111211000 SMOKE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU BAGG POD DIRTY A VTZA O OTHER N FALSE WARNING LD LANDING 1 EA 27 318UE 41041 FLT NR 6501 - IAD-JFK - DURING APPROACH, MADE A SCHEDULED LANDING DUE TO POD SMOKE LIGHT. AIRCRAFT LANDED WITH NO FURTH ER INCIDENTS. MAINTENANCE CLEANED SMOKE DETECTOR AND CANNON PLUG PLUS OPENED DMI 21016, MEL 26-3. MAINTENANCE AGAIN CL EANED AND INSPECTED SMOKE DETECTOR AND CLOSED DMI. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERV ICE. (M) 2 L 7 2 4T RT A41NM 1996082600034 19960826 00034 EU 1996 8 26 VTZA96249 1 19960710 A 5270 SP4594 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGGAGE DOOR OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 314UE 41027 FLT NR 6536 - ABORTED TAKEOFF DUE TO THE BAGGAGE DOOR WARNING LIGHT ILLUMINATING. AIRCRAFT RETURNED TO GATE WITH NO FUR THER INCIDENTS. MAINTENANCE OPENED DMI 03818 ON BAGGAGE DOOR LIGHT ILLUMINATING, MEL 52-30. MAINTENANCE CLOSED DMI 038 18, ADUSTING MICROSWITCH, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996082600035 19960826 00035 EU 1996 8 26 VTZA96250 1 19960709 A 5270 SP4594 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGG DOOR LACK OF LUBE A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 308UE 41023 FLT 6510 - DURING TAKEOFF, ABORTED THE TAKEOFF DUE TO THE MAIN BAGGAGE DOOR WARNING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENT. MAINTENANCE OPENED DMI 18671, MEL 52-30. MAINTENANCE CLOSED DMI 18671, BY CLEANING AND LUBING MICROS WITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996082600036 19960826 00036 EU 1996 8 26 VTZA96252 1 19960712 A 7722 EGT COMP JETAIR JETSTM JETSTM4101 1500501 EU LT/RT ENG OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 436JX 41036 FLT NR 6158 - BTV-IAD - DURING TAKEOFF, ABORTED TAKEOFF DUE TO BOTH ENGINES WOULD NOT MAKE TARGET TORQUE. AIRCRAFT RETU RNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED EGT COMP. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN T O SERVICE. (M) 2 L 7 2 4T RT A41NM 1996082600037 19960826 00037 1996 8 26 VTZA96268 4 19960722 A 3421 CONTROL HEAD JETAIR JETSTM JETSTM4101 1500501 EU LT ADI TRIPPED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 436JX 41036 FLT NR 6186 - LYH-IAD - DURING CLIMB, AN UNSCHEDULED LANDING AT LYH DUE TO LEFT ADI/AHRS FAILED. AIRCRAFT RETURNED TO G ATE WITH NO FURTHER INCIDENTS. MAINTENANCE RERACKED LEFT ADI CONTROL HEAD, OPS CHECK GOOD. AIRCRAFT WAS RELEASED AND A PPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996082600038 19960826 00038 EU 1996 8 26 VTZA96269 1 19960723 A 2910 137311D1443 HYD LINE BAG JETSTM JETSTM3201 1500217 EU HYD SYSTEM HOLE A VTZA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 EA 27 496UE 900 FLT NR 6331 - SWF-BOS - AFTER LANDING, AIRCRAFT LOST NOSE STEERING AND NORMAL BRAKING ON BOTH LEFT AND RIGHT HYD PUMPS. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED HYD LINE FROM CHECK VALVES TO FILTERS. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996082600039 19960826 00039 EU 1996 8 26 VTZA96270 1 19960723 A 2770 GUST LOCK JETAIR JETSTM JETSTM4101 1500501 EU CONTL SURFACES LACK OF LUBE A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 327UE 41080 FLT NR 6278 - IAD-EWR - ABORTED TAKEOFF DUE TO TAKEOFF CONFIGURATION WARNING. AIRCRAFT LANDED WITH NO FURTHER INCIDENTS . MAINTENANCE INSPECTED AIRCRAFT AND LUBED GUST LOCK ASSY. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. ( M) 2 L 7 2 4T RT A41NM 1996082600040 19960826 00040 EU 1996 8 26 VTZA96271 1 19960723 A 3260 ATG135022 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU LT MLG FAILED A VTZA K NONE N FALSE WARNING CL CLIMB 1 EA 27 322UE 41058 FLT NR 6416 - PVD-IAD - AIRCRAFT HAD A RED GEAR HANDLE LIGHT REMAINING ILLUMINATING AFTER GEAR SELECTED UP. INTRANSIT A ND DOWNLOCK INDICATIONS NORMAL. AIRCRAFT CONTINUED TO IAD AND LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REP LACED BOTH LEFT UPLOCK MICROSWITCH. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996082600041 19960826 00041 EU 1996 8 26 VTZA96272 1 19960724 A 3150 TO WARNING JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT ACTIVATED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 307UE 41021 FLT NR 6598 - IAD-RDU - ABORTED THE TAKEOFF DUE TO TAKEOFF CONFIGURATION WARNING. AIRCRAFT RETURNED TO GATE WITH NO FUR THER INCIDENTS. MAINTENANCE RESET AND CYCLED GUST LOCK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996082600042 19960826 00042 EU 1996 8 26 VTZA96274 1 19960724 A 2150 1250104 FREON MOTOR JETAIR JETSTM JETSTM4101 1500501 EU AFT FUSELAGE FAILED A VTZA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 27 311UE 41029 FLT NR 6457 - EWR-IAD - DURING TAXI, AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS DUE TO SMOKE COMING FROM AIR CO NDITIONING ACCESS VENT. MAINTENANCE INSPECTED AIR CONDITIONER AND FERRIED AIRCRAFT TO LYH. MAINTENANCE REMOVED AND REP LACED FREON MOTOR, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996082600043 19960826 00043 EU 1996 8 26 VTZA96275 1 19960725 A 3010 465205 ELEV HORN JETAIR JETSTM JETSTM4101 1500501 EU ELEV DE-ICE FAILURE A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 312UE 41025 FLT NR 6578 - IAD-PWM - DURING CRUISE, MADE UNSCHEDULED LANDING AT IAD DUE TO PROP DE-ICE FAILURE, ELEVATOR HORN ICE FAI LURE, AND STALL WARNING TAPE SHOWS STALL INDICATION. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED ELEV HORN, DE-ICE FUSE AND INSPECTED STALL WARNING. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPRO VED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996082600044 19960826 00044 EU 1996 8 26 VTZA96277 1 19960725 A 3260 ATG135022 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU RT MLG FAILED A VTZA O OTHER N FALSE WARNING DE DESCENT 1 EA 27 307UE 41021 ROA - IAD - FLT 6318 - DURING DESCENT, THE AIRCRAFTS RIGHT MAIN GEAR INTRANSIT LIGHT ILLUMINATED ON DESCENT WITHOUT GEAR SELECTION. AIRCRAFT TAXIED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED MICROSWITCH. OPS CHEC K OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996082600045 19960826 00045 EU 1996 8 26 VTZA96281 1 19960716 A 2611 72111211000 SMOKE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU BAGG COMPT DIRTY A VTZA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 302UE 41013 FLT NR 6215 - CHS-IAD - DURING TAXI, RETURNED TO GATE WITH NO FURTHER INCIDENTS DUE TO VENTRAL BAGGAGE BAY SMOKE DETECTI ON CAPTION ILLUMINATED DURING TAXI. MAINTENANCE OPENED DMI NR 52859 IAW MEL 26-1. MAINTENANCE CLOSED DMI 52859 ON 7-17 -96 BY CLEANING POD SMOKE DETECTOR. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996082600046 19960826 00046 EU 1996 8 26 VTZA96282 1 19960727 A 5270 DOOR WARNING BAG JETSTM JETSTM3201 1500217 EU PAX DOOR MALFUNCTIONED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 497UE 904 FLT 6383 - CMH-IAD - DURING CLIMB, MADE A UNSCHEDULED LANDING DUE TO PASSENGER DOOR CAPTION ILLUMINATING DURING CLIMB. A IRCRAFT RETURNED TO CMH AND GATE WITH NO FURTHER INCIDENTS. MAINTENANCE INSPECTED THE DOOR AND CYCLED IT THROUGH NUMERO US TIMES, COULD NOT DUPLICATE. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996082600047 19960826 00047 EU 1996 8 26 VTZA96284 1 19960730 A 5270 DOOR WARNING JETAIR JETSTM JETSTM4101 1500501 EU BAGG COMPT MALFUNCTIONED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 312UE 41025 IAD - BOS - FLT 6506 - ABORTED TAKEOFF DUE TO MAIN BAGGAGE WARNING ON TAKEOFF DUE TO MAIN BAGGAGE WARNING ON TAKEOFF ROL L. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE INSPECTED MICROSWITCHES AND RESET DOOR WARNING, OP S CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996082600048 19960826 00048 NE 1996 8 26 VTZA96521 2 19960703 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114GR 01514 NE LEFT BIRD STRIKE A VTZA O OTHER C F.O.D. LD LANDING 1 EA 27 324UE 41017 75013 FLT NR 6540 - DURING LANDING, ENCOUNTERED A BIRD STRIKE TO THE LEFT ENGINE. AIRCRAFT LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE INSPECTED AND FERRIED AIRCRAFT TO LYH FOR A LEFT ENGINE CHANGE. MAINTENANCE CHANGED LEFT ENGINE. OPS CHEC K OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 4 T RT A41NM E18NE 1996082600049 19960826 00049 EU 1996 8 26 W8PA960066 2 19960805 A 7261 OIL LINE BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU NR 1 ENGINE LOOSE A W8PA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 03 951WP 22951 720722 NR 1 ENGINE OIL QUANTITY DECREASED FROM 4 AND THREE-QUARTERS GALLONS TO 1 AND ONE-HALF GALLONS EN ROUTE TO PDX. DIVERTE D TO BOI. FOUND LOOSE LINE BETWEEN LUBE UNIT AND REAR SCAVENGE. RETORQUED LINE. LEAK CHECKED GOOD AT ALL POWER SETTIN GS. (M) 2 L 7 2 4F 4 F RT A16WE E21EU 1996082600050 19960826 00050 EU 1996 8 26 Y2PA96052 1 19960730 A 3411 PITOT DRAIN AMD FALC20 FALCON 2720302 EU PLUGGED RIGHT A Y2PA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 819AA 26 ON CLIMB-OUT, V2 120 KTS ON LT SIDE, RT SIDE SHOWED 20 KTS LWR. AS ALT INCREASED, A/S DIFFERENTIAL INCREASED AND EPR DE CREASED SIGNIFICANTLY, FL 310 A/S ON RT SHOWED 400 KTS PLUS AND MACH O/S WARN SOUNDED. ALL OTHER GAUGES SHOWED NORM, IN CLUDING PILOTS A/S IND. ON DESCENT A/S DIFFERENTIAL DECREASED AND EPR STARTED TO SHOW NORM. A/C RETURNED. NO EMERG PR OCEDURES NECESSARY. FOUND FOREIGN OBJECT IN PITOT DRAIN BLOCK FROM RT PITOT TUBE. REMOVED ALL DEBRIS, PRESS CHK'D AND LEAK CHK'D RT PITOT/STATIC SYS IAW FALCON MM 34-10-1. OP CHK'D MACH O/S WARN SYS IAW FALCON MM 34-10-4 WITH NO DEFECTS NOTED. PERFORMED PWR ASSURANCE RUN OF BOTH ENG'S IAW FALCON 20 MX INSPECT PROCEDURES MANUAL W/NO DEFECTS NOTED. (M) 2 L 7 2 4F A7EU 1996082600051 19960826 00051 NM 1996 8 26 DL76L961883 1 19960812 A 7830 315T401472K TR UNIT BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE DAMAGED A DALA K NONE C F.O.D. IN INSP/MAINT 1 SO 27 174DN 24802 724681 ON ARRIVAL, FOUND NR 1 ENG FAN DUCT COWL ASSY DAMAGED. REPLACED NR 1 ENGINE INBD THRUST REVERSER HALF. 2 L 7 2 4F 4 F RT A1NM E24NE 1996082600052 19960826 00052 NM 1996 8 26 DL73S961918 1 19960809 A 5315 6545410223 FLOOR BEAM BOEING 737 737232 1384475 NM BS 663 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 305DL 23077 DURING INSPECTION, THE BL 0.07 FLOOR BEAM UPPER CAP OF WING CENTER SECTION IS CRACKED THROUGH AT FS 663. NO CRACKS FOUN D IN WEB. THE DAMAGE WAS REPAIRED PER B737S/B 57-1210. 2 L 7 2 4F RT A16WE 1996082700002 19960827 00002 EU 1996 8 27 SIMA962061 1 19960724 A 3397 WIRE AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 255AE 254 ORD - FLT 4212 - AIRSTAIR EMERGENCY LIGHT INOP. REPAIRED WIRING BETWEEN PIN L OF 15W AND PIN E OF PLUG 253VC. OPERATIO NAL CHECK SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996082900001 19960829 00001 EU 1996 8 29 SIMA961883 1 19960706 A 3097 WIRE HARNESS AEROSP ATR42 ATR42300 8680920 EU LT WINDSHIELD CHAFED A A SIMA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 21 423MQ 030 ORD - FLT 4211 - DURING TAKEOFF ROLL, CREW REPORTED ELECTRICAL ARCHING UNDER FLIGHT OFFICERS INSTRUMENT PANEL. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO GATE. INVESTIGATION REVEALED THE WIRE BUNDLE FOR THE LEFT WINDSHIELD HEAT CONTROLL ER HAD CHAFED ON THE CONTROLLER MOUNT BRACKET, WIRING WAS REPAIRED IAW ATR WIRING MANUAL. OPS CHECK WAS SATISFACTORY. A /C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996082900031 19960829 00031 NM 1996 8 29 CA960103003 1 19960102 A 8011 A3A4N176 CONTACTOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 ENGINE WELDED W F H ACTIVATE FIRE EXT. DEACTIVATE SYST/CIRCUITS B M SMOKE/FUMES/ODORS/SPARKS OVER TEMP TX TAXI/GRND HDL 1 CA 121151 (CAN)STARTER REMAINED ENGAGED AFTER SHUTDOWN OF #2 ENGINE, AND MARSHALLER REPORTED SMOKE. BOTH FIRE EXTINGUISHERS USED A ND ENGINE FOAMED BY FIRE DEPARTMENT. CAUSE BELIEVED TO BE STUCK START CONTACTOR. STARTER, CONTACTOR GCU AND BOTH BATTERI ES REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1996082900032 19960829 00032 EA 1996 8 29 CA960103004 1 19960102 A 7921 28E997 OIL COOLER STWARNER DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE CORE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 8572 02900520 123133 (CAN)#2 OIL COOLER LEAKING. COOLER REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1996082900083 19960829 00083 CE 1996 8 29 CA960110003 1 19960102 A 5260 604302461 STRUT BEECH 604302271 BEECH 60 B60 1153605 CE LYC DOOR STEP CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 2871 (CAN)DURING MAINTENANCE THE RETRACTABLE DOOR STEP STRUT BROKE OFF APPROXIMATELY 2 INCHES ABOVE THE LOWER AXLE CENTRE LIN E. INSPECTION REVEALED A CRACK APPROXIMATELY 5/8 INCH LONG PROPAGATING FROM THE LOWERCASTING PLUG HAD PREVIOUSLY GONE UN DETECTED. 1 L 7 2 3O A12CE 1996082900102 19960829 00102 WP 1996 8 29 CALA9601203 1 19960821 A 2740 418575 TRIM MOTOR DOUG DC10 DC1030 3023501 WP HOR STAB LEAKING A CALA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SW 09 87070 48292 THE HYDRAULIC SYSTEM NR 3 ELEVATOR OFF CAUTION LIGHT ILLUMINATED AND THE NR 3 HYDRAULIC QUANTITY BEGAN TO DECREASE WHILE EN ROUTE FROM FRA TO EWR. SHORTLY AFTERWARDS, THE NR 3 LEFT HYDRAULIC PUMP PRESSURE LOW LIGHT ILLUMINATED. ALL APPROP RIATE CHECKLISTS WERE ACCOMPLISHED AND THE AIRCRAFT WAS DIVERTED TO LGW WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE F OUND THE NR 3 HORIZONTAL STABILIZER TRIM MOTOR LEAKING. THE STABILIZER TRIM MOTOR WAS REMOVED AND REPLACED. THE NR 3 HY DRAULIC SYSTEM WAS SERVICED. LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 3 4F A22WE 1996082900103 19960829 00103 WP 1996 8 29 CALA9601204 1 19960821 A 2810 ACCESS PANEL DOUG DC9 DC981 3022081 WP LT WING LOOSE SCREWS A CALA A UNSCHED LANDING K FLUID LOSS NR NOT REPORTED 1 SW 09 16883 48073 THE AIRCRAFT WAS RETURNED TO TPA AFTER FUEL WAS REPORTED LEAKING FROM TOP OF LEFT WING. THE AIRCRAFT LANDED WITHOUT INC IDENT. MAINTENANCE FOUND EVIDENCE OF FUEL LEAKAGE FROM LT WING PANEL 1303C AND THERE WERE SEVERAL LOOSE SCREWS. THE PA NEL SCREWS WERE RETORQUED IAW MM 28-00-00, PAGE 216. THE TANK WAS FUELED TO FULL. PRESSURE AND LEAK CHECKS WERE GOOD. 2 L 7 2 4F A6WE 1996082900104 19960829 00104 WP 1996 8 29 961815960 1 19960819 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP TAILCONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 604NW 47222 DURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996082900105 19960829 00105 WP 1996 8 29 9618169604 1 19960820 A 3350 60030451 BATTERY PACK DOUG DC9 DC932 3022066 WP TAILCONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 604NW 47222 DURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE EMERGENCY EVACUATION LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND P OWER SUPPLY. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996082900106 19960829 00106 WP 1996 8 29 9618179974 1 19960821 A 3220 NLG DOUG DC9 DC931 3022065 WP NLG WW VIBRATION A NWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 01 9338 47347 EXCESSIVE VIBRATION WAS COMING FROM NOSE GEAR AREA AFTER TAKEOFF. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. M AINTENANCE INSPECTED AND FOUND BOTH NOSE GEAR DOOR UP AND LOCKED. NO DISCREPANCIES COULD BE FOUND. AIRCRAFT RETURNED T O SERVICE. 2 L 7 2 4F A6WE 1996082900107 19960829 00107 WP 1996 8 29 9618189945 1 19960821 A 5242 DOOR DOUG DC9 DC931 3022065 WP E/E COMPT NOT SEATED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 8925E 45840 AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. WIND NOISE WAS ALSO COMING FROM NOSE GEAR AREA. FLIGHT RETURNED TO DTW AN D LANDED WITHOUT INCIDENT. NOTE: FORWARD ACCESSORY COMPARTMENT DOOR LIGHT ILLUMINATED SEVERAL TIMES ON FINAL. MAINTEN ANCE FOUND E/E COMPARTMENT DOOR NOT COMPLETELY CLOSED. ALSO, FOUND CANNON PLUG DISCONNECTED AT E/E DOOR SWITCH. RESEAT ED DOOR AND RECONNECTED PLUG TO SWITCH. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996082900108 19960829 00108 WP 1996 8 29 9618199869 1 19960821 A 3397 WIRE DOUG DC9 DC951 3022051 WP CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 778NC 48100 DURING LINE CHECK, FOUND EMERGENCY LIGHTS OVER GALLEY DOOR INOPERATIVE. FOUND BAD GROUND WIRE ON LIGHT FIXTURE. REPLAC ED GROUND WIRE. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1996082900109 19960829 00109 WP 1996 8 29 9618209869 1 19960821 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 778NC 48100 DURING LINE CHECK, FOUND CEILING EMERGENCY LIGHTS IN FIRST CLASS CABIN INOPERATIVE. REPLACED POWER SUPPLY AND BATTERIES . OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996082900110 19960829 00110 1996 8 29 9618219104 4 19960820 A 3418 STALL WARNING DOUG DC9 DC915 3022036 WP RT COCKPIT ACTIVATED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 94S 47204 AFTER TAKEOFF, FIRST OFFICER'S STALL WARNING AND STICK SHAKER ACTIVATED. UNABLE TO ISOLATE WHICH SYSTEM FAILED. RETURN ED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED LEFT AND RIGHT STALL WARNING TRANSDUCERS AND SUMMING UNIT. SYSTEM TEST ED GOOD. 2 L 7 2 4F A6WE 1996082900111 19960829 00111 NM 1996 8 29 9618222714 1 19960818 A 3260 656021132 ACCESSORY BOX BOEING 727 7272S7 138407Z NM E/E BAY MALFUNCTIONED A NWAA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CL CLIMB 1 GL 01 718RC 22631 5554 22344 IMMEDIATELY UPON RAISING LANDING GEAR OUT OF PHX, THE AURAL WARNING HORN SOUNDED AND DID NOT STOP UNTIL THE CIRCUIT BREA KER WAS PULLED. THE GEAR WAS RECYCLED AND THE AURAL WARNING STOPPED WITH CIRCUIT BREAKER PUSHED BACK IN. ALL INDICATION S APPEARED NORMAL AFTER RECYCLE. INSTALLED SERVICEABLE LANDING GEAR ACCESSORY BOX. OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996082900112 19960829 00112 NM 1996 8 29 9618236301 1 19960821 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 661US 23719 DURING LINE CHECK, FOUND EMERGENCY FLOOR LIGHTS INOPERATIVE AT ROWS 51-66 LEFT AND 35-43 RIGHT. SECURED WIRING FOR EMER GENCY LIGHTS. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1996082900113 19960829 00113 NM 1996 8 29 9618246302 1 19960821 A 3250 METERING VALVE BOEING 747 747451 1384940 NM RUDDER STEERING MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 662US 23720 DURING TAKEOFF, THE STEERING TILLER WAS BINDING AND THE RUDDER STEERING HAD LIMITED CAPABILITY. ABORTED TAKEOFF AND RETU RNED TO THE GATE. REPLACED THE STEERING METERING VALVE. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1996082900114 19960829 00114 WP 1996 8 29 9618259961 1 19960820 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP COCKPIT DISCHARGED A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 924RW 47185 PILOT REPORTED COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996082900115 19960829 00115 WP 1996 8 29 9618269972 1 19960819 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9336 47338 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT OVERWING EMERGENCY EXIT LIGHTS DIM. REPAIRED GROUND WIRE TO LEFT OVERWIN G UPPER DOOR EMERGENCY LIGHTS. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996082900116 19960829 00116 WP 1996 8 29 9618279978 1 19960820 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9342 47391 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD EMERGENCY EXIT LIGHTS DIM. REPLACED BATTERIES. OPERATIONAL CHECK NOR MAL. 2 L 7 2 4F A6WE 1996082900117 19960829 00117 WP 1996 8 29 9618289978 1 19960820 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9342 47391 DURING LINE MAINTENANCE INSPECTION, FOUND SEVERAL OVERHEAD EMERGENCY LIGHTS WEAK AND FORWARD AISLE EMERGENCY LIGHTS INOP ERATIVE. REPLACED BATTERIES. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996082900118 19960829 00118 WP 1996 8 29 9618299987 1 19960819 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP TAILCONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 987US 47458 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES. OPERATION AL CHECK NORMAL. 2 L 7 2 4F A6WE 1996082900119 19960829 00119 WP 1996 8 29 9618309998 1 19960819 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8934E 47143 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD PORTABLE EMERGENCY FLASHLIGHT NOT CHARGING. REPLACED BATTERY PACK. O PERATIONAL CHECK NORMAL. PART TOTAL CYCLES, 12,994. 2 L 7 2 4F A6WE 1996082900120 19960829 00120 SO 1996 8 29 COMA9610248 1 19960820 A 3241 426871 CONTROL BOX EMB 120 EMB120RT SO ANTI SKID SYST MALFUNCTION A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 257CA 12436 120248 COMPLETE LOSS OF BRAKING DURING TAXI. REPLACED THE ANTI-SKID CONTROL BOX. 2 L 7 2 4T RT A31SO 1996082900121 19960829 00121 SO 1996 8 29 COMA9610249 1 19960820 A 2150 32144143 VALVE EMB 120 EMB120RT SO LT/ RT PACK LOW PRESSURE A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 1110J 19349 120110 BOTH LT AND RT COOLING PACKS FAIL TO COOL PROPERLY. REPLACED THE LT AND RT PRESSURE REGULATING VALVES. 2 L 7 2 4T RT A31SO 1996082900122 19960829 00122 EA 1996 8 29 COMA9660134 1 19960820 A 3250 NAS1601010 SEAL CNDAIR CL600 CL6002B19 EA NLG STEERING LEAKING A COMA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 940CA 7048 HYDRAULIC FLUID LEAKING FROM NLG. REPLACED THE O-RING SEALS ON THE NLG STEERING SERVO. 2 L 7 2 4F RT A21EA 1996082900123 19960829 00123 EA 1996 8 29 COMA9660135 1 19960820 A 3150 864806 PSEU CNDAIR CL600 CL6002B19 EA E/E COMPT MALFUNCTION A COMA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 959CA 684 7116 PROXIMITY SYSTEM FAULT MESSAGE ON EICAS. REPLACED THE PROXIMITY SENSOR ELECTRONIC UNIT. PART TOTAL CYCLES, 612. 2 L 7 2 4F RT A21EA 1996082900124 19960829 00124 NM 1996 8 29 UPS96220909 1 19960803 A 5320 CLIP BOEING 727 72730C 1384009 NM BS 312 CORRODED A IPXA O OTHER O OTHER IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE: C. CORROSION ON FRAME CLIP, NOSE W/W LOWER LOBE, STA 312 RT SIDE ON FLOOR SKIN. REMOVED, FAB'D AND I NSTALLED REPLACEMENT ANGLES PER SRM 51-10-01 AND SRM 51-30-02. 2 L 7 3 4F A3WE 1996082900125 19960829 00125 NM 1996 8 29 UPS96220910 1 19960804 A 5320 FITTING BOEING 727 72730C 1384009 NM BS 940 CRACKED A IPXA O OTHER O OTHER IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE: C. 940 FRAME FITTING RT SIDE IS CRACKED IN 3 PLACES, 1 ON FRONT AND 2 ON AFT SIDE. REPAIRED 940 FITT ING RT SIDE IAW EO'S B727-5310-3737A, B727-5310-1001A. 2 L 7 3 4F A3WE 1996082900126 19960829 00126 NM 1996 8 29 UPS96220911 1 19960716 A 5542 SKIN BOEING 727 72730C 1384009 NM RUDDER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE: C. UPPER RUDDER SKIN RT SIDE HAS CORROSION AT RUDDER FRONT SPAR. REMOVED AND REPLACED UPPER RUDDER M /M 27-20-01 AND MM 27-20-00. 2 L 7 3 4F A3WE 1996082900127 19960829 00127 NM 1996 8 29 UPS96220912 1 19960801 A 5542 SKIN BOEING 727 72730C 1384009 NM RUDDER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE: C. LOWER RUDDER SKIN AT FRONT SPAR IS CORRODED. REMOVED AND REPLACED RUDDER (LOWER) IAW M/M 27-20-11 AND MM 27-20-20. 2 L 7 3 4F A3WE 1996082900128 19960829 00128 NM 1996 8 29 UPS96420913 1 19960821 A 3350 60B5003727 CONNECTOR BOEING 747 747123 1384873 NM CABIN LOOSE A IPXA K NONE L NO TEST CR CRUISE 1 SO 01 676UP 20101 WITH THE EMERGENCY LIGHT SWITCH IN THE ARMED POSITION, THE EMERGENCY LIGHT MODULE IN THE CREW DOOR HALLWAY CEILING FLICK ERED OFF AND ON. CLEANED AND RESEATED CONNECTOR ON LIGHT ASSY, CK O.K. 2 L 7 4 4F A20WE 1996082900129 19960829 00129 NM 1996 8 29 UPS96420914 1 19960718 A 5720 SKIRT ANGLE BOEING 747 747123 1384873 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE: C. FOUND LT SKIRT ANGLE CRACKED APPROXIMATELY 6 INCHES AFT OF LAST TRAILING EDGE DOOR HINGE. ALSO, 2 INCHES FORWARD ATTACHMENT HOLES WORN OUT. REPAIRED SKATE ANGLE IAW TO KLM DFX 96-171 ISSUE NR 3 AND IAW EFN 747-54-01 31. 2 L 7 4 4F A20WE 1996082900130 19960829 00130 NM 1996 8 29 UPS96420915 1 19960731 A 5400 SKATE ANGLE BOEING 747 747123 1384873 NM NR 1 PYLON RT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE: C. SKATE ANGLE PYLON NR 1 RT HAS CRACKS AT THE TWO FIRST FASTENER HOLES. REPAIRED IAW KLM DFX 96-180 / EFN 747-54-0132. 2 L 7 4 4F A20WE 1996082900131 19960829 00131 NM 1996 8 29 UPS96420916 1 19960806 A 5330 SKIN BOEING 747 747123 1384873 NM BS 1373 BROKEN A IPXA O OTHER O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE: C. RT BLG WHEELWELL - LOWER SKIN CORNER OF PRESSURE DECK, STA 1373 OUTBOARD SIDE OF WHEELWELL IS BROK EN OFF AND THERE ARE SIGNS OF CORROSION AT THAT SKIN. REMOVED CORROSION IAW SRM 51-10-01. CORROSION OUT OF LIMITS IAW SRM 51-10- 01. REPAIRED IAW SRM 53-10-01 PER DRAWING KLM DFX96-176, EFN 747-53-0787. 2 L 7 4 4F A20WE 1996082900132 19960829 00132 NM 1996 8 29 UPS96420917 1 19960821 A 3350 CONNECTOR BOEING 747 747123 1384873 NM COCKPIT DIRTY A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE: DLY. DURING FLIGHT, THE EMERGENCY LIGHTS SWITCH IN THE ARMED POSITION, THE EMERGENCY LIGHT MODULE IN THE CREW SERVICE DOOR HALLWAY CEILING FLICKERED ON AND OFF. CLEANED AND RESEATED CONNECTOR ON LIGHT ASSY, OPS CHK NORM AL. 2 L 7 4 4F A20WE 1996082900133 19960829 00133 EU 1996 8 29 QXEA9600339 1 19960821 A 5246 DOOR PIN 2651231 FOKKER F28 F28MK4000 4990810 EU LAV SERVICE DOOR BROKEN A QXEA K NONE O OTHER CR CRUISE 1 NM 09 478US 11227 SEA - IN-FLIGHT, EXPERIENCED A LOUD PRESSURE BANG FOLLOWED BY ERRATIC PRESSURIZATION. LAV SERVICE PLUG MISSING AND SERV ICE PORT DOOR MISSING. DOOR PANEL 29AA REPLACED, SERVICE PLUG REPLACED, AND LATCH PIN REPLACED. LAV RESERVICED AND AIR CRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996082900134 19960829 00134 NM 1996 8 29 DHL96701009 1 19960821 A 2550 CONTAINER BOEING 727 72730C 1384009 NM CARGO COMPT NOT SEALED A DHLA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 01 701DH 19011 NOXIOUS ODOR DETECTED IN FORWARD CONTROL CABIN AND BECAME STRONGER AFTER TAXI IN. WHEN COCKPIT DOOR WAS OPEN, THE ODOR WAS EXTREMELY STRONG. FOUND ODOR TO BE FROM ONE CONTAINER WITH NEOPRENE SOLES FROM GDL PER A/C CREW . SEALED CONTAINER WITH PLASTIC COVERING, AIRED CARGO DECK. NO FURTHER ODOR DETECTED. 2 L 7 3 4F A3WE 1996082900135 19960829 00135 WP 1996 8 29 DHL9680201C 1 19960817 A 2730 3644178 TORQUE TUBES DOUG DC8 DC873F 302199F WP ELEVATOR CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 AT C-CHECK, DURING X-RAY INSPECTION OF THE ELEVATOR BUS TORQUE TUBES, HEAVY INTERNAL CORROSION WAS FOUND. REMOVED AND R EPLACED BOTH TORQUE TUBES PER M/M . 2 L 7 4 4F RT 4A25 1996082900136 19960829 00136 WP 1996 8 29 ARWA9608008 1 19960817 A 5753 SKIN DOUG DC8 DC863 302198A WP RT TE FLAP DAMAGED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 TEMPORARY REPAIRS (6 EA) RT WING INBD FLAP LOWER SURFACE. REMOVED TEMPORARY REPAIRS. REPAIRED FLAP SURFACE PER DC-8 SR M 57-2-1, SRM 57-2-5. FORMED PARTS PER DC-8 SRM'S 51-1-4, 57-7-1, TREATED AND INSTALLED PER DC-8 SRM'S 51-1-8, 51-1-21. 2 L 7 4 4F 4A25 1996082900137 19960829 00137 WP 1996 8 29 ARWA9608010 1 19960817 A 5730 SKIN DOUG DC8 DC863 302198A WP WS 257/303 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 LEVEL 2 CORROSION RIGHT WING LEADING EDGE LOWER LIP INBOARD AFT CORNER STA. XW 257.000 AND XFS 303.000. REPAIRED WING L EADING EDGE PER DC-8 SRM 57-2-1. FORMED DOUBLER PER DC-8 SRM 51-1-4, 57-2-2. TREATED AND INSTALLED PER DC-8 SRM 51-1-8 , 51-1-20, 51-1-11. 2 L 7 4 4F 4A25 1996082900138 19960829 00138 WP 1996 8 29 ARWA9608011 1 19960817 A 5230 FITTING DOUG DC8 DC863 302198A WP CARGO DOOR BROKEN A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 AFT LOWER CARGO COMPARTMENT NR 3 DOOR, AFT VERTICAL FITTING STRUT BROKEN. REMOVED AND REPLACED FITTING PER DC-8 SRM 51- 1-20D. 2 L 7 4 4F 4A25 1996082900139 19960829 00139 WP 1996 8 29 ARWA9608012 1 19960817 A 5330 SKIN DOUG DC8 DC863 302198A WP BS 35 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 MAIN CABIN LEVEL 2 CORROSION SKIN INNER FACE LONGERON 22R, FS 35.00. REPAIRED SKIN PER DC-8 SRM 53-2-1. FORMED DOUBLER PER DC-8 SRM'S 51-1-4, 53-3-3. TREATED AND INSTALLED IAW DC-8, 51-1-21. 2 L 7 4 4F 4A25 1996082900140 19960829 00140 WP 1996 8 29 ARWA9608013 1 19960817 A 5720 FITTING DOUG DC8 DC863 302198A WP WS 554/589 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 LT WING NR 1 ALT TANK 9 INCH CRACK SPLICE FITTING XRS 554 AND XRS 589, NR 5 STRINGER ACCESS DOOR 514H. REMOVED CRACKED SPLICE FITTING AND REPLACED PER DC-8 SRM 51-1-20D. MANUFACTURED FITTING PER DC-8 SRM'S 51-2-0, 57-403 AND DACO AUTHORIZ ATION. 2 L 7 4 4F 4A25 1996082900141 19960829 00141 WP 1996 8 29 ARWA9608014 1 19960817 A 5720 FITTING DOUG DC8 DC863 302198A WP NR 4 BOOST PUMP CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 RIGHT WING NR 4 ALT BOOSTER PUMP FITTING IS CRACKED (BOTH SIDES). REMOVED AND REPLACED FITTINGS PER DC-8 SRM 51-1-20D. DAC AUTHORIZATION. 2 L 7 4 4F 4A25 1996082900142 19960829 00142 WP 1996 8 29 ARWA9608015 1 19960817 A 5312 BULKHEAD DOUG DC8 DC863 302198A WP BS 1766 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 MAIN CARGO LEVEL 2 CORROSION BULKHEAD LOWER PART, FS 1766 LT. REPAIRED BULKHEAD PER DOUGLAS FAX DATED 24 JULY 1996, ACT ION NR 304835, SKETCH 96-07-18-004. FAA APPROVED 8110-3. 2 L 7 4 4F 4A25 1996082900143 19960829 00143 WP 1996 8 29 ARWA9608016 1 19960817 A 7830 TR UNIT DOUG DC8 DC863 302198A WP NR 2 ENGINE CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 1.50 INCH CRACK UPPER STRINGER AND T/R RT SIDE NR 2 ENGINE. REPAIRED PARTS PER ARROW DRAWING NR ARW 016675-0831. FORME D DOUBLER PER DC-8 SRM'S 51-1-7, 78-3-3. INSTALLED PER DC-8 SRM 51-1-21. 2 L 7 4 4F 4A25 1996082900144 19960829 00144 WP 1996 8 29 ARWA9608017 1 19960817 A 5230 TRACK DOUG DC8 DC863 302198A WP CARGO DOOR CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 5 INCH CRACK NR 3 LOWER CARGO DOOR TRACK AND .50 INCH CRACK IN FLANGE UPPER SECTION. REMOVED AND REPLACED DOOR TRACK PE R DC-8 SRM'S 51-1-20D, 51-3-0. 2 L 7 4 4F 4A25 1996082900145 19960829 00145 WP 1996 8 29 ARWA9608018 1 19960817 A 5320 FITTING DOUG DC8 DC863 302198A WP BS 1220 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 CRACKED FITTING IN LONGERON 29L AT STA 1220. REMOVED AND REPLACED FITTING PER DC-8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1996082900146 19960829 00146 WP 1996 8 29 ARWA9608019 1 19960817 A 5313 LONGERON DOUG DC8 DC863 302198A WP BS 1180 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 LEVEL 1 CORROSION IN FITTING, STA 1180, LONGERON 34R, TO BE RE-EVALUATED. CORROSION OUT OF LIMITS. REMOVED AND REPLACED FITTING PER DC-8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1996082900147 19960829 00147 WP 1996 8 29 ARWA9608020 1 19960817 A 5320 FITTING DOUG DC8 DC863 302198A WP BS 1200 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 CRACKED FITTING IN LONGERON 34R, STA 1200, AFT CARGO. REMOVED AND REPLACED FITTING AT INDICATED AREA PER DC-8 SRM 51-1- 20D. 2 L 7 4 4F 4A25 1996082900148 19960829 00148 WP 1996 8 29 ARWA9608021 1 19960817 A 5320 FITTING DOUG DC8 DC863 302198A WP BS 1200 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 CRACKED FITTING IN LONGERON 35R AT STA 1200, AFT CARGO. CRACKED FITTING WAS REMOVED AND REPLACED PER IAW DC-8 SRM 51-1- 20D. 2 L 7 4 4F 4A25 1996082900149 19960829 00149 WP 1996 8 29 ARWA9608022 1 19960817 A 5320 FITTING DOUG DC8 DC863 302198A WP BS 1160 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 LONGERON 28L FITTING IS CRACKED AT STA 1160, AFT CARGO. REMOVED AND REPLACED FITTING PER DC-8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1996082900150 19960829 00150 WP 1996 8 29 ARWA9608023 1 19960817 A 5320 FITTING DOUG DC8 DC863 302198A WP BS 1180 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 FITTING CRACKED FS 1180, LONGERON 27L, STA 1180, AFT CARGO. REMOVED CRACKED FITTING. FORMED NEW FITTING PER DAC AUTHORI ZATION, INSTALLED PER IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1996082900151 19960829 00151 WP 1996 8 29 ARWA9608024 1 19960817 A 5320 FITTING DOUG DC8 DC863 302198A WP BS 1200 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 CRACKED FITTING IN LONGERON 28L, STA 1200, AFT CARGO. REMOVED AND REPLACED FITTING PER DC-8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1996082900152 19960829 00152 NM 1996 8 29 VSTA9608003 1 19960821 A 3350 1102833 LIGHT BOEING 737 737204 1384458 NM CABIN INOPERATIVE A VSTA K NONE L NO TEST IN INSP/MAINT 1 WP 07 312VA 20236 EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT UNIT. OPS CHECK GOOD. 2 L 7 2 4F A16WE 1996082900230 19960829 00230 CE 1996 8 29 96ZZZX4127 1 19960730 A 2810 CAP LANYARD MTSBSI MU2 MU2B60 5780460 CE MAIN FUEL TANK DISINTEGRATED A W3NA K NONE O OTHER IN INSP/MAINT 1 GL 25 350RG 2381 773SA UPON PERFORMING A 100-HOUR INSPECTION, FOUND THE LEFT FUEL CAP LANYARD WAS MISSING. FURTHER INVESTIGATION FOUND THE LAN YARD IN SMALL PIECES IN BOTTOM OF TANK. THE LANYARD IS A SOFT PLASTIC-LIKE MATERIAL THAT HAD HARDENED AND DISINTEGRATED INTO SMALL PIECES WHICH COULD HAVE BEEN PICKED UP BY THE FUEL BOOST PUMP. 1 H 7 2 3T RT A10SW 1996082900235 19960829 00235 CE 1996 8 29 96ZZZX4132 1 19960719 A 2930 MC192322 SWITCH CESSNA 525 525 2076601 CE HYD LOW FLOW CRACKED A IMJA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 EA 25 195ME 559 0240 5250100 LOSS OF HYDRAULIC FLUID, LOW PRESSURE, AND LOW FLOW INDICATED. CAUSE OF FLUID LOSS FROM CRACKED HYDRAULIC LOW FLOW SWIT CH. CAUSE OF CRACK UNKNOWN, NO MAINTENANCE PERFORMED IN THIS AREA. LOCATION OF SWITCH (COULD HAVE BEEN USED AS HAND HO LD ENTERING FAIL CONE AREA). SUBMITTER RECOMMENDS IMPROVED SECURITY AND POSSIBLE COVER GUARD INSTALLATION. REPLACED DE FECTIVE PART. OPS AND LEAK CHECK OK. 1 L 7 2 4F RT A1WI 1996082900243 19960829 00243 WP 1996 8 29 9618099138 1 19960816 A 5230 FITTING DOUG DC9 DC915 3022036 WP CARGO DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9348 45787 DURING H-CHECK, FOUND A CRACK IN THE FORWARD CARGO DOOR LOWER FORWARD INTERCOSTAL ATTACH FITTING. REPLACED FITTING. 2 L 7 2 4F A6WE 1996082900244 19960829 00244 WP 1996 8 29 9618109931 1 19960817 A 5230 FITTING DOUG DC9 DC931 3022065 WP CARGO DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 90S 47244 DURING H-CHECK, FOUND CRACKS IN THE AFT CARGO DOOR BEAM END FITTING, SECOND FROM BOTTOM ON BOTH THE FORWARD AND AFT ENDS AND THE THIRD FROM THE TOP FORWARD END. REPLACED ALL FITTINGS PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996082900245 19960829 00245 WP 1996 8 29 9618119756 1 19960818 A 5320 FITTING DOUG DC9 DC941 302207N WP BS 1019 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 756NW 47180 DURING H-CHECK, FOUND CORROSION ON THE LONGERON 26R END FITTING AT FS 1019. REPLACED FITTING (P/N 4912798-507) PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996082900246 19960829 00246 WP 1996 8 29 9618129863 1 19960818 A 5341 FITTING DOUG DC9 DC951 3022051 WP BS 693-712 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 772NC 47774 DURING H-CHECK, FOUND CORROSION IN THE LEFT WING FRONT SPAR FITTING BETWEEN FS 693 TO 712. REPLACED FITTING PER SRM 51- 30-5, 51-30-1 AND DWG 5913055. 2 L 7 2 4F A6WE 1996082900247 19960829 00247 EU 1996 8 29 9618313222 1 19960820 A 3350 321454 POWER SUPPLY AIRBUS 320 A320211 3930320 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 322US 15017 7838 263 DURING LINE MAINTENANCE, THE CABIN INTERCOMMUNICATION DATA SYSTEM FAULTED THE LEFT AFT EMERGENCY POWER SUPPLY UNIT. R EPLACED EPSU. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996082900248 19960829 00248 WP 1996 8 29 9618159604 1 19960819 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP TAILCONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 604NW 47222 DURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996082900249 19960829 00249 NM 1996 8 29 9618322714 1 19960822 A 3260 SWITCHES BOEING 727 7272S7 138407Z NM NLG DIRTY A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 718RC 22344 ON GEAR RETRACTION, GEAR WARNING HORN SOUNDED STEADY, COULD NOT SILENCE WITH CUTOUT LEVER. CYCLED GEAR AND HORN WENT OUT . CLEANED MAIN LANDING GEAR SENSORS AND NOSE GEAR SWITCHES, PERFORMED OPERATIONAL CHECK. 2 L 7 3 4F A3WE 1996082900250 19960829 00250 NM 1996 8 29 SWAA960852 1 19960815 A 7930 OIL PRESS IND BOEING 737 7373H4 1384600 NM NR 1 ENGINE MALFUNCTIONED A SWAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 349SW 24408 DIVERTED TO PHX DUE TO NUMBER 1 ENGINE OIL PSI DROPPING TO YELLOW RANGE, APPROX 20 PSI. AIRCRAFT LANDED WITHOUT INCIDEN T. PERFORMED ENGINE RUN PER BOEING M/M, OIL PRESSURE AND QUANTITY REMAINED IN NORMAL RANGE. CHECKED METAL CHIP DETECTO RS AND FILTERS, PERFORMED ENGINE RUN A SECOND TIME, ALL NORMAL. 2 L 7 2 4F RT A16WE 1996082900251 19960829 00251 NM 1996 8 29 SWAA960853 1 19960821 A 2134 SENSOR BOEING 737 7372H4 138448C NM RT PACK INOPERATIVE A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 51SW 21448 AIRCRAFT RETURNED TO DAL DUE TO RIGHT PACK TRIPPING AND UNABLE TO CONTROL CABIN PRESSURE. REMOVED AND REPLACED 450 DEGR EE SENSOR, RT RAM AIR SENSOR AND PERFORMED TEST FLIGHT PER BOEING M/M. 2 L 7 2 4F A16WE 1996082900252 19960829 00252 NM 1996 8 29 SWAA960854 1 19960822 A 2613 OVERHEAT WARNING BOEING 737 7372H4 138448C NM NR 2 ENGINE ILLUMINATED A SWAA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SW 07 105SW 23249 NR 2 ENGINE OVERHEAT WARNING ILLUMINATED IN FLIGHT, CREW PERFORMED ENGINE SHUTDOWN CHECKLIST. AIRCRAFT LANDED AT MAF WI THOUT INCIDENT. INSPECTED AND FOUND NO EVIDENCE OF FIRE OR OVERHEAT CONDITION. DEFERRED DETECTION SYSTEM AND CONTINUED PER MEL 26-2. 2 L 7 2 4F A16WE 1996082900253 19960829 00253 NM 1996 8 29 SWAA960855 1 19960822 A 5241 SKIN BOEING 737 7372H4 138448C NM GALLEY DOOR DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 74SW 22674 DURING SCHEDULED D-CHECK, FOUND AFT GALLEY DOOR SKIN DENTED ON AFT LOWER CORNER. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996082900254 19960829 00254 NM 1996 8 29 SWAA960856 1 19960822 A 5210 SKIN BOEING 737 7372H4 138448C NM FWD ENTRY DOOR DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 74SW 22674 DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR OUTER SKIN CUTOUT BLENDED BEYOND SRM LIMITS. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996082900255 19960829 00255 NM 1996 8 29 SWAA960857 1 19960822 A 5330 SKIN BOEING 737 7372H4 138448C NM SERV DOOR CUTOUT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 74SW 22674 DURING SCHEDULED D-CHECK, FOUND RIGHT FWD SERVICE DOOR CUTOUT CRACKED IN LOWER AFT CORNER. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996082900256 19960829 00256 NM 1996 8 29 SWAA960858 1 19960821 A 5330 SKIN BOEING 737 7372T4 1384492 NM BS 747 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED SERV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, S17L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996082900257 19960829 00257 NM 1996 8 29 SWAA960859 1 19960821 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 947 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 947, S20L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996082900258 19960829 00258 NM 1996 8 29 SWAA960860 1 19960822 A 3350 900835A BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 61SW 21970 DURING SCHEDULED SERVICE CHECK, FOUND CABIN AFT CEILING EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PER BOEING M/M. 2 L 7 2 4F A16WE 1996082900259 19960829 00259 EU 1996 8 29 QXEA9600340 1 19960822 A 3350 1820 BULB FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 493US 11161 EXIT LIGHT ABOVE SEAT 8C ISN'T ILLUMINATED WHEN THE EMERGENCY LIGHTS ARE ARMED. BULB WAS REPLACED, LIGHT OPS CHECKED GO OD. 2 L 7 2 4F RT A20EU 1996082900260 19960829 00260 NM 1996 8 29 QXEA9600341 1 19960822 A 5347 85320701123 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORROSION A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 818PH 25119 58 SEAT TRACK (P/N 85320701-123) FOUND CORRODED BEYOND LIMITS. CORROSION NOTED DURING C-CHECK (NR200-80-82). TRACK REPLAC ED IAW SRM 51-40-00. 2 H 7 2 4T RT A13NM 1996082900261 19960829 00261 NM 1996 8 29 QXEA9600342 1 19960822 A 5347 85330507104 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORROSION A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 818PH 58 SEAT TRACK (P/N 85330507-104) FOUND CORRODED BEYOND LIMITS. CORROSION NOTED DURING C-CHECK (NR200-81). TRACK REPLACED I/A/W SRM 51-40-11. 2 H 7 2 4T RT A13NM 1996082900262 19960829 00262 NM 1996 8 29 QXEA9600343 1 19960822 A 5347 85330507107 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORROSION A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 818PH 58 SEAT TRACK (P/N 85330507-107) FOUND CORRODED BEYOND LIMITS. CORROSION NOTED DURING C-CHECK (NR200-83). TRACK REPLACED IAW SRM 51-40-00. 2 H 7 2 4T RT A13NM 1996082900263 19960829 00263 NM 1996 8 29 QXEA9600344 1 19960822 A 5347 85320701125 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORROSION A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 818PH 58 SEAT TRACK (P/N 85320701-125) FOUND CORRODED BEYOND LIMITS. CORROSION NOTED DURING C-CHECK (NR200-84). TRACK REPLACED IAW SRM 51-40-00. 2 H 7 2 4T RT A13NM 1996082900264 19960829 00264 NM 1996 8 29 QXEA9600345 1 19960822 A 5347 85320490135 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORROSION A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 818PH 58 SEAT TRACK (P/N 85320490-135) FOUND CORRODED BEYOND LIMITS. CORROSION NOTED DURING C-CHECK (NR200-85,133-23). TRACK RE PLACED IAW SRM 51-40-11. 2 H 7 2 4T RT A13NM 1996082900265 19960829 00265 NM 1996 8 29 QXEA9600346 1 19960822 A 5347 85330164117 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORROSION A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 818PH 58 SEAT TRACK (P/N 85330164-117) FOUND CORRODED BEYOND LIMITS. CORROSION NOTED DURING C-CHECK (NR200-86). TRACK REPLACED IAW SRM 51-40-11. 2 H 7 2 4T RT A13NM 1996082900266 19960829 00266 NM 1996 8 29 QXEA9600347 1 19960822 A 5347 85330164119 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORROSION A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 818PH 58 SEAT TRACK (P/N 85330164-119) FOUND CORRODED BEYOND LIMITS. CORROSION FOUND DURING C-CHECK (NR200-87). TRACK REPLACED IAW SRM 51-40-11. 2 H 7 2 4T RT A13NM 1996082900267 19960829 00267 NM 1996 8 29 QXEA9600348 1 19960822 A 5347 85320490133 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORROSION A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 818PH 58 SEAT TRACK (P/N 85320490-133) FOUND CORRODED BEYOND LIMITS. CORROSION NOTED DURING C-CHECK (NR200-88). TRACK REPLACED IAW SRM 51-40-00. 2 H 7 2 4T RT A13NM 1996082900268 19960829 00268 NM 1996 8 29 QXEA9600349 1 19960822 A 5347 85331040109 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORROSION A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 818PH 58 SEAT TRACK (P/N 85331040-109) FOUND CORRODED BEYOND LIMITS. CORROSION NOTED DURING C-CHECK (NR200-90). TRACK REPLACED IAW SRM 51-40-11. 2 H 7 2 4T RT A13NM 1996082900269 19960829 00269 1996 8 29 96FDEA01389 4 19960821 A 2230 TCC AIRBUS 300 A300F4605R 3930327 EU LT/RT ENGINE MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 669FE 761 AFTER TAKEOFF AT CLIMBOUT OF 9000 MSL, FUEL FLOW FLUX BOTH ENGINES, RETURN TO SALT LAKE. REMOVED AND REPLACED TRP PER M /M 22-35-12. ALSO, REMOVED AND REPLACED TCC PER M/M 22-36-34 ALL AFS/LANDS TEST GOOD. A/C REMAINS CAT II THIS ITEM CLO SES 22-30/1131 AND 73-22/1132 WRI'S OK FOR SERVICE. 2 L 7 2 4F RT A35EU 1996082900270 19960829 00270 EU 1996 8 29 96FDEA01391 1 19960826 A 2424 GCU AIRBUS 310 A310221 3930310 EU NR 1 MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 417FE 333 NR 1 GENERATOR FAULT WITH INTERMITTENT NR 1 IDG FAULT. GENERATOR DID RESET BUT STILL HAD NR 1 IDG FLASHING. *S/D* PER FORMED OPS CHECK OF AIR/COOLER, CHECKS GOOD. REMOVED AND REPLACED NR 1 GCU, OPS CK'D GOOD. 2 L 7 2 4F RT A35EU 1996082900271 19960829 00271 EU 1996 8 29 96FDEA01392 1 19960821 A 2612 SMOKE DETECTOR AIRBUS 300 A300* EU CARGO COMPT MALFUNCTIONED A FDEA B EMER. DESCENT N FALSE WARNING AP APPROACH 1 SO 25 651FE 728 MID 1 MAIN DECK CARGO SMOKE WARNING WITH NO VISUAL INDICATION OR ODORS IN FLIGHT. AN EMERGENCY WAS DECLARED ON APPROACH INTO MSP. REMOVED AND REPLACED RALTU AND REPROGRAMMED. PERFORMED DISPLAY AND INPUTS BITE TEST ON ECAM. WARNING WENT AWAY AND SYSTEM WORKED NORMALLY. 2 L 7 2 4F RT A35EU 1996082900272 19960829 00272 NM 1996 8 29 96FDEA01393 1 19960822 A 2613 OVERHEAT LOOP BOEING 727 727227 1384078 NM LWR AFT FUS OUT OF POSITION A FDEA O OTHER J WARNING INDICATION CR CRUISE 1 SO 25 481FE 21463 LOWER AFT BODY OVERHEAT LIGHT FLASHED ON AND OFF INTERMITTENTLY IN FLIGHT, BOTH PACKS ON BLEEDS 1 ENGINE 2 APU BLEED AND ENGINE 3 BLEED OPEN. LIGHT DOES NOT STAY ILLUMINATED LONG ENOUGH TO ISOLATE PROBLEM USING ABNORMAL CHECK LIST. ALSO, AFT CARGO SELECTED ON LOWER AFT BODY OVERHEAT COMPARTMENT SELECTOR SWITCH LOWER AFT BODY OVER HEAT LIGHT COMES ON INTERM ITTENTLY. FOUND LOOP TOO CLOSE TO FLIGHT RECORDER CASING AND SEVERAL INSULATING GROMMETS IMPROPERLY INSTALLED. REPOSTI ONED LOOP AND GROMMETS, CHECKED LOOP AT B-BELLY AFT BULKHEAD. RAN APU AND PACKS WITH AFT AIRSTAIR CLOSED TO CHECK FOR H EAT SENSITIVITY. 2 L 7 3 4F A3WE 1996082900273 19960829 00273 NM 1996 8 29 96FDEA01394 1 19960822 A 5320 6516317251 SHEAR TIE BOEING 727 727227 1384078 NM BS 350 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 NR 0648 AND 030, CORROSION ON CHORD BS 350 RBL 18 TO LBL 18 WL 148 UNDER NUTPLATES. 2 L 7 3 4F A3WE 1996082900274 19960829 00274 NM 1996 8 29 96FDEA1395 1 19960822 A 5313 651838739 STRINGER BOEING 727 72722 1384002 NM BS 964 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 NR0711 AND 031, WHILE WORKING ON NR0698 FOUND CORROSION ON STRINGER 30 BS 964. 2 L 7 3 4F A3WE 1996082900275 19960829 00275 NM 1996 8 29 96FDEA01396 1 19960822 A 2613 OVERHEAT LOOP BOEING 727 727227 1384078 NM LWR AFT FUS OUT OF POSITION A FDEA O OTHER N FALSE WARNING CR CRUISE 1 SO 25 481FE 21463 LWR AFT BODY OVERHEAT LIGHT BLINKED ON MOMENTARILY ONCE WHILE IN FLIGHT. REMOVED GILLINER PANELS LOWER AFT CARGO COMPAR TMENT. INSPECTED SENSOR, FOUND NUMEROUS SPOTS SENSOR RUBBING METAL BRACKETS. REPOSITIONED SAME, REMOVED KEEL BEAM PANE L, INSPECTED SENSOR AND CHECKED GOOD. LEAK CHECK SYSTEM, MANY SMALL LEAKS AFT STAIR AREA. TIGHTEN CLAMPS RAN ENGINE AN D APU NO LEAK NOTED. NO OVERHEAT NOTED, CLOSED ALL PANELS AND STILL NO OVERHEAT INDICATIONS NOTED. 2 L 7 3 4F A3WE 1996082900276 19960829 00276 WP 1996 8 29 ABXA9600613 1 19960821 A 2130 PRESSURIZATION DOUG DC9 DC941 302207N WP CABIN MALFUNCTIONED A ABXA B EMER. DESCENT O OTHER CR CRUISE 1 GL 23 970AX 47494 AIRCRAFT LOST PRESSURIZATION AT FL 350. SELECTED COLDER TEMPATURE AND MANUAL CONTROL OF PRESSURIZATION. CREW DID RAPID DEPRESSURIZATION CHECK LIST AND EMERGENCY DESCENT TO FL 200. PACKS COOLED, CLIMBED TO FL 250. TEMPATURE CONTROL SELE CTED TO MANUAL MODE AND PRESSURIZATION REMAINED IN AUTO. PERFORMED TEST OF PRESSURIZATION, TEMPATURE CONTROL AND THERMA L SHUTDOWN SYSTEMS, OPS CHECK GOOD PER DC-9 MM. 2 L 7 2 4F A6WE 1996082900277 19960829 00277 NM 1996 8 29 SCNA96226 1 19960820 A 3350 1102833 LIGHT BOEING 727 727225 1384077 NM AFT AIRSTAIR INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 283SC 22559 FOUND AFT AIRSTAIR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED AFT AIRSTAIR EMERGENCY LIGHT ASSEMBLY, OPS CHECK GOOD REFERENCE MM 33-50-01. 2 L 7 3 4F A3WE 1996082900278 19960829 00278 NM 1996 8 29 SCNA96227 1 19960820 A 3350 1102833 LIGHT BOEING 727 727225 1384077 NM AFT AIRSTAIR INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 283SC 22559 FOUND AFT AIRSTAIR OVERHEAD EMERGENCY EXIT LIGHT INOP. CHECKED AIRCRAFT WIRING. REMOVED AND REPLACED AFT AIRSTAIR EMER GENCY LIGHT ASSEMBLY, OPS CHECK GOOD IN ACCORDANCE WITH MM 33-50-01. 2 L 7 3 4F A3WE 1996082900279 19960829 00279 NM 1996 8 29 P5CA9600614 1 19960820 A 5247 DOOR BOEING 747 747123 1384873 NM APU DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 DURING APU CHANGE FOUND DENT IN APU ACCESS DOOR. REPAIRED PER BOEING SRM 51-40-02. 2 L 7 4 4F A20WE 1996082900280 19960829 00280 NM 1996 8 29 P5CA9600615 1 19960820 A 5247 FRAME BOEING 747 747123 1384873 NM APU DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 DURING APU CHANGE FOUND RIGHT APU ACCESS DOOR 2ND FRAME FROM FRONT EDGE CHORD CRACKED. REPAIRED PER BOEING SRM 51-40-03 . 2 L 7 4 4F A20WE 1996082900281 19960829 00281 NM 1996 8 29 P5CA9600616 1 19960820 A 5247 SKIN BOEING 747 747123 1384873 NM APU DOOR HOLES A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 DURING APU CHANGE FOUND 2 HOLES THROUGH SKIN ON LEFT APU ACCESS DOOR. REPAIRED PER BOEING SRM 51-40-02. 2 L 7 4 4F A20WE 1996082900282 19960829 00282 NM 1996 8 29 P5CA9600617 1 19960821 A 5711 SPAR BOEING 747 747132 1384882 NM CENTER WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION ON FRONT SPAR LOWER CHORD IN CENTER TANK DRY BAY AT LBL77. REMOVED CORROSION IAW BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01 PROTECTED PER 51-10-01. 2 L 7 4 4F A20WE 1996082900283 19960829 00283 NM 1996 8 29 P5CA9600618 1 19960819 A 5315 FLOOR BEAM BOEING 747 747132 1384882 NM BS 460 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION UPPER DECK FLOOR BEAM LOWER T-SECTION OF FALSE BEAM JUST OUTBOARD OF CIRCULAR STAIR CUTOUT STR 460 RBL 0 TO RBL 30. CORROSION REMOVED PER BOEING SRM 51-10-01 WITHIN LIMITS AND PROTECTED PER 51-10-02. 2 L 7 4 4F A20WE 1996082900284 19960829 00284 NM 1996 8 29 P5CA9600619 1 19960819 A 5315 FLOOR BEAM BOEING 747 747132 1384882 NM BS 440 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION ON UPPER DECK FLOOR BEAM LOWER-T BS 440 RBL 50. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMI TS PER 53-10-01 PROTECTED PER 51-10-02. 2 L 7 4 4F A20WE 1996082900285 19960829 00285 NM 1996 8 29 P5CA9600620 1 19960820 A 5730 SKIN BOEING 747 747132 1384882 NM CENTER WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION CENTER WING DRY BAY UPPER SKIN STRINGER 33C LBL 108 WL 190. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01 PROTECTED PER 51-10-02. 2 L 7 4 4F A20WE 1996082900286 19960829 00286 NM 1996 8 29 P5CA9600621 1 19960820 A 5730 SKIN BOEING 747 747132 1384882 NM CENTER WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION CENTER WING DRY BAY UPPER SKIN AT STRINGER 29C AT LBL 75. REMOVED CORROSION PER BOEING SRM 51-10-01 W ITHIN LIMITS PER 53-10-01 PROTECTED PER 51-10-02. 2 L 7 4 4F A20WE 1996082900287 19960829 00287 NM 1996 8 29 P5CA9600622 1 19960820 A 5730 SKIN BOEING 747 747132 1384882 NM CENTER WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION CENTER WING DRY BAY UPPER SKIN AT STRINGER 31C AT LBL 30 TO LBL 75. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01 PROTECTED PER 51-10-02. 2 L 7 4 4F A20WE 1996082900288 19960829 00288 NM 1996 8 29 P5CA9600623 1 19960820 A 5730 SKIN BOEING 747 747132 1384882 NM CENTER WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION CENTER WING DRY BAY UPPER SKIN AT STRINGER 33C RBL 108 WL 190. REMOVED CORROSION PER BOEING SRM 51-10 -01 WITHIN LIMITS PER 53-10-01 PROTECTED PER 51-10-02. 2 L 7 4 4F A20WE 1996082900289 19960829 00289 NM 1996 8 29 P5CA9600624 1 19960814 A 5330 SKIN BOEING 747 747132 1384882 NM BS 780 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION ON EXTERNAL SURFACE OF SKIN PANEL BS 780 BBL 0 AROUND RIVET HEADS. REMOVED CORROSION PER BOEING SRM 5 1-10-01 WITHIN LIMITS PER 53-10-01 PROTECTED PER 51-10-02. 2 L 7 4 4F A20WE 1996082900290 19960829 00290 NM 1996 8 29 P5CA9600625 1 19960814 A 5330 SKIN BOEING 747 747132 1384882 NM BS 760 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION ON EXTERNAL SURFACE OF SKIN PANEL BS 760 BBL 0 TO BBL 12R AROUND RIVET HEADS. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01 PROTECTED PER 51-10-02. 2 L 7 4 4F A20WE 1996082900291 19960829 00291 NM 1996 8 29 P5CA9600626 1 19960805 A 5720 BRACKET BOEING 747 747121 1384871 NM NR 2 PYLON BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FOUND BROKEN BRACKET AT BAY CUTOUT ABOVE PYLON NR 2. NEW BRACKET AND FASTENERS INSTALLED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 1996082900292 19960829 00292 NM 1996 8 29 P5CA9600627 1 19960805 A 2910 HYD FITTING BOEING 747 747121 1384871 NM NR 4 PYLON CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FOUND CORRODED HYDRAULIC FITTINGS IN WING BY NR 4 PYLON. LEVEL ONE CORROSION REMOVED AND TREATED AS PER MM 51-21-03. 2 L 7 4 4F A20WE 1996082900293 19960829 00293 NM 1996 8 29 P5CA9600628 1 19960805 A 5720 ROD BOEING 747 747121 1384871 NM NR 3 PYLON CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FOUND CORRODED ROD BEHIND HYDRAULIC TANK IN WING NEAR ATTACH TO NR 3 PYLON. LEVEL ONE CORROSION REMOVED AND TREATED AS PER MM 51-21-03. 2 L 7 4 4F A20WE 1996082900294 19960829 00294 NM 1996 8 29 P5CA9600629 1 19960805 A 2910 FITTING BOEING 747 747121 1384871 NM NR 3 PYLON CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FOUND HYDRAULIC FITTINGS CORRODED IN WING NEAR ATTACHMENT TO NR 3 PYLON. LEVEL ONE CORROSION REMOVED AND TREATED AS PER MM 51-21-01. 2 L 7 4 4F A20WE 1996082900295 19960829 00295 NM 1996 8 29 P5CA9600630 1 19960805 A 5730 ACCESS PANEL BOEING 747 747121 1384871 NM RT WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FOUND CRACKED ACCESS PANEL AND ATTACH ANGLE IN WING L/E TO INBOARD RIB IN NR 4 PYLON CAVITY. REPAIRED IAW SRM 51-40-03 AND SRM 51-40-02. 2 L 7 4 4F A20WE 1996082900296 19960829 00296 NM 1996 8 29 P5CA9600631 1 19960805 A 5720 ANGLE BOEING 747 747121 1384871 NM WS 670 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FOUND CRACK ON SUPPORT ANGLE AT WS 670 AT ATTACHMENT OF FRONT SPAR. NEW ANGLE INSTALLED PER SB 57-2159. 2 L 7 4 4F A20WE 1996082900297 19960829 00297 NM 1996 8 29 P5CA9600632 1 19960805 A 5730 PANEL BOEING 747 747121 1384871 NM WS 353 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FOUND CORROSION ON UPPER SKIN LEFT WING AT STRINGER 3, ROOT AREA CONNECTION WING TO FUSELAGE, WS 353.02. LEVEL ONE CORR OSION REMOVED AND AREA TREATED AS PER SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 57-10-01. 2 L 7 4 4F A20WE 1996082900298 19960829 00298 NM 1996 8 29 P5CA9600633 1 19960805 A 5730 SKIN BOEING 747 747121 1384871 NM WS 1270 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FOUND SWELLING ON UPPER WING SKIN STA WS 1270 IN FRONT SPAR AREA. REMOVED FASTENERS, LEVEL ONE CORROSION IAW 51-10-01 A ND FOUND WITHIN LIMITS OF SRM 57-30-01. REPAIRED PANEL IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996082900299 19960829 00299 NM 1996 8 29 P5CA9600634 1 19960805 A 5730 SKIN BOEING 747 747121 1384871 NM WS 1340-1380 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FOUND SWELLING AND PROTRUDING RIVET ON UPPER WING SKIN, STA 1340 TO 1380 IN FRONT SPAR AREA. REMOVED FASTENERS, LEVEL O NE CORROSION IAW SRM 51-10-01 AND FOUND WITHIN LIMITS OF SRM 57-30-01. REPAIRED PANEL IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996082900300 19960829 00300 NM 1996 8 29 P5CA9600635 1 19960805 A 5730 SKIN BOEING 747 747121 1384871 NM WS 1340 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FOUND SWELLING ON UPPER WING SKIN WS 1340 IN FRONT SPAR AREA. REMOVED FASTENERS, LEVEL ONE CORROSION PER 51-10-01 AND F OUND WITHIN LIMITS OF SRM 57-30-01. REPAIRED PANEL IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996082900301 19960829 00301 NM 1996 8 29 P5CA9600636 1 19960805 A 5730 SKIN BOEING 747 747121 1384871 NM WS 750 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FOUND SWELLING ON UPPER WING SKIN WS 750 IN FRONT SPAR AREA. REMOVED FASTENERS, LEVEL ONE CORROSION IAW SRM 51-10-01 AN D FOUND WITHIN LIMITS OF SRM 57-30-01. REPAIRED PANEL IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996082900302 19960829 00302 NM 1996 8 29 P5CA9600637 1 19960805 A 5730 SKIN BOEING 747 747121 1384871 NM WS 800 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FOUND SWELLING ON UPPER WING SKIN WS 800 IN FRONT SPAR AREA. REMOVED FASTENERS, LEVEL ONE CORROSION IAW SRM 51-10-01 AN D FOUND WITHIN LIMITS OF SRM 57-30-01. REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996082900303 19960829 00303 NM 1996 8 29 P5CA9600638 1 19960805 A 5730 SKIN BOEING 747 747121 1384871 NM WS 1020 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FOUND SWELLING ON UPPER WING AT WS 1020 IN FRONT SPAR AREA. REMOVED FASTENERS, LEVEL ONE CORROSION IAW SRM 51-10-01 AND FOUND WITHIN LIMITS OF SRM 57-30-01. REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1996082900304 19960829 00304 NM 1996 8 29 P5CA9600639 1 19960805 A 5730 SKIN BOEING 747 747121 1384871 NM WS 1230 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FOUND SWELLING ON UPPER WING WS 1230 IN FRONT SPAR AREA. REMOVED FASTENERS, LEVEL ONE CORROSION IAW SRM 51-10-01 AND FO UND WITHIN LIMITS OF SRM 57-30-01. REPAIRED IAW SRM 57-30-01. 2 L 7 4 4F A20WE 1996082900305 19960829 00305 NM 1996 8 29 P5CA9600640 1 19960805 A 5730 SKIN BOEING 747 747121 1384871 NM WS 580 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FOUND LEVEL ONE CORROSION ON UPPER WING SKIN STA 580 IN MID SPAR AREA. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 57-30-01. TREATED AREA IAW SRM 51-10-02. 2 L 7 4 4F A20WE 1996082900306 19960829 00306 NM 1996 8 29 P5CA9600641 1 19960805 A 5730 SKIN BOEING 747 747121 1384871 NM WS 294.62 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FOUND LEVEL ONE CORROSION ON UPPER SKIN NEAR FRONT SPAR AT ROOT AREA, WING TO FUSELAGE STA WS 294.62. CORROSION REMOVED AND TREATED AS PER SRM 51-10-01, FOUND WITHIN LIMITS OF SRM 57-30-01. 2 L 7 4 4F A20WE 1996082900307 19960829 00307 NM 1996 8 29 P5CA9600642 1 19960805 A 5720 BRACKET BOEING 747 747121 1384871 NM LT WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 LEFT WING NR 2 DIAGONAL FITTING BRACKET AT RIGHT SIDE IS CRACKED. FABRICATED NEW BRACKET AND INSTALLED AS PER SRM 51-20 -01 AND 51-30-02. 2 L 7 4 4F A20WE 1996082900308 19960829 00308 NM 1996 8 29 P5CA9600643 1 19960805 A 5720 BRACKET BOEING 747 747121 1384871 NM RT WING CHAFED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FOUND LEFTHAND FORWARD MOUNTING BRACKET CHAFED AND ONE ANCHOR NUT MISSING NEAR NR 4 PYLON. FABRICATED NEW BRACKET AND I NSTALLED BRACKET AND ANCHOR NUT IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996082900309 19960829 00309 NE 1996 8 29 P5CA9600644 2 19960821 A 7261 ENGINE BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 2 OIL LEAK A P5CA E A ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CR CRUISE 1 WP 23 854FT 69656 2270 19754 662590 AT CRUISE NR 2 ENGINE OIL QUANTITY STEADILY DECREASED FROM APPROX 5.6 GALLONS TO ZERO WITHIN 45 MINUTES FROM TAKEOFF. S HUT DOWN ENGINE AND RETURNED TO AMS. WINDMILL TIME 1 HOUR 16 PSI OIL PRESSURE. FOUND OIL LEAK TO BE INTERNAL REMOVED A ND REPLACED ENGINE PER BOEING MAINTENANCE MANUAL 71-00-02. 2 L 7 4 4F 4 F A20WE E20EA 1996082900310 19960829 00310 NM 1996 8 29 P5CA9600646 1 19960821 A 2910 B-NUT BOEING 747 747124 1384874 NM NR 4 PYLON LOOSE A P5CA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 23 855FT 19733 NR 4 HYDRAULIC SYSTEM LOSS OF FLUID. DEPRESSURIZED ENGINE DRIVEN PUMP. FOUND LOOSE B-NUT ON ENGINE DRIVEN PUMP SUPPLY LINE. LEAK CHECK OK PER MAINTENANCE MANUAL 29-00-00. 2 L 7 4 4F A20WE 1996082900311 19960829 00311 NM 1996 8 29 P5CA9600647 1 19960820 A 5730 SKIN BOEING 747 747132 1384882 NM CENTER WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION CENTER WING DRY BAY UPPER SKIN AT STRINGER S32C ON LOWER FLANGE FROM RBL 84 TO 59. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01, REPROTECTED PER 51-10-02. 2 L 7 4 4F A20WE 1996082900312 19960829 00312 NM 1996 8 29 P5CA9600648 1 19960820 A 5711 SPAR BOEING 747 747132 1384882 NM CENTER WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION FRONT SPAR UPPER CHORD IN CENTER TANK DRY BAY FROM LBL 105 TO 115. REMOVED CORROSION PER BOEING SRM 5 1-10-01 WITHIN LIMITS PER 53-10-01, REPROTECTED PER 51-10-02. 2 L 7 4 4F A20WE 1996082900313 19960829 00313 NM 1996 8 29 P5CA9600649 1 19960820 A 5713 STRINGER BOEING 747 747132 1384882 NM CENTER WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION ON CENTER WING DRY BAY UPPER SKIN STRINGER 30C AT RBL 55 TO RBL 95. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01, REPROTECTED PER 51-10-02. 2 L 7 4 4F A20WE 1996082900314 19960829 00314 NM 1996 8 29 P5CA9600650 1 19960820 A 5713 STRINGER BOEING 747 747132 1384882 NM CENTER WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION CENTER WING DRY BAY UPPER SKIN STRINGER S29C AT RBL 90. REMOVED CORROSION PER BOEING SRM 51-10-01 WIT HIN LIMITS PER 53-10-01, REPROTECTED PER 51-10-02. 2 L 7 4 4F A20WE 1996082900315 19960829 00315 WP 1996 8 29 ARWA9608025 1 19960817 A 2711 CONNECTOR DOUG DC8 DC863 302198A WP LT AILERON TAB CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 LEFT WING, LEFT AILERON CONT TAB TORQUE TUBE CONNECTOR CRACKED. REMOVED LT AILERON TAB AND SENT OUT FOR REPAIR. INSTAL LED SERVICEABLE UNIT PER DC-8 SRM 27-11-4. 2 L 7 4 4F 4A25 1996082900316 19960829 00316 EU 1996 8 29 HCMA9610 1 19960221 A 6520 7704411 SEAL MAGNETIC SNIAS 350 AS350B2 8680813 EU T/R GR BOX DEFECTIVE E HCMA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 13 972BH 908 2804 PART IS DEFECTIVE. LEAKS BADLY. 1 G 7 1 3U H9EU 1996082900317 19960829 00317 EU 1996 8 29 HCMA9612 1 19960221 A 6300 BABDRR SEAL SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE M/R DEFECTIVE E HCMA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 13 982BH 196 2876 9389 SEAL IS DEFECTIVE. SEAL IS LEAKING. 1 G 7 1 3U 3 U H9EU E19EU 1996082900318 19960829 00318 EU 1996 8 29 HCMA962 1 19960209 A 6520 350A33215300 REAR ROTOR SNIAS 350 AS350BA 8680817 EU LAMIFICATION WORN EXCESS E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 312B 813 2243 PART IS WORN EXCESSIVELY. REMOVED AND REPLACED. 1 G 7 1 3U NC H9EU 1996082900319 19960829 00319 EU 1996 8 29 HCMA963 1 19960209 A 3150 350A67614403 ALARM PANEL SNIAS 350 AS350B2 8680813 EU ROTOR BROKEN E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 992BH 178 2889 ROTOR ALARM PCB IS BROKEN. REMOVED AND REPLACED WITH NEW. 1 G 7 1 3U H9EU 1996082900320 19960829 00320 EU 1996 8 29 HCMA964 1 19960212 A 2820 355A54301926 UNION SNIAS 350 AS350B2 8680813 EU FUEL SYS BROKEN E HCMA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 13 992BH 85 2889 UNION IS BROKEN. REMOVED AND REPLACED WITH NEW. 1 G 7 1 3U H9EU 1996082900321 19960829 00321 EU 1996 8 29 HCMA965 1 19960212 A 2800 350A53101324 PLATE SNIAS 350 AS350B2 8680813 EU FUEL SYS BROKEN E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 992BH 85 2889 PART IS BROKEN. REMOVED AND REPLACED WITH NEW. 1 G 7 1 3U H9EU 1996082900322 19960829 00322 EU 1996 8 29 HCMA966 1 19960212 A 6320 1B675 CHIP DETECTOR SNIAS 350 AS350B2 8680813 EU GR BOX SHORTED E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 992BH 26 2889 CHIP DET IS SHORTED OUT. REMOVED AND REPLACED WITH NEW. 1 G 7 1 3U H9EU 1996082900323 19960829 00323 EU 1996 8 29 HCMA968 1 19960212 A 6410 355A09103600 BEARINGS SNIAS 350 AS350BA 8680817 EU T/R WORN EXCESSIVELY E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 642BH 955 2495 BEARING IS WORN EXCESSIVELY. REMOVED AND REPLACED. ORIGINAL PART CAME ON T/R BLADE ASSY S/N 6068. 1 G 7 1 3U NC H9EU 1996082900324 19960829 00324 GL 1996 8 29 HEEA967680 2 19960820 A 7260 23059588 GEAR 23053985 BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL ENG PTO GROOVED E HEEA K NONE O OTHER LD LANDING 1 SW 03 1622 CAG704111 CAE860408 ENGINE REMOVED DUE TO HARD LANDING AND SUDDEN STOPPAGE. UPON INSPECTION OF GEARBOX PARTS NOTED THE FOLLOWING: GROOVED BEYOND OVERHAUL LIMITS ON PTO GEAR FWD AND AFT SEAL JOURNALS. REPLACED DISCREPANT PART. 1 G 7 1 3U 3 U H2SW E1GL 1996082900325 19960829 00325 SW 1996 8 29 HEEA967683 1 19960820 A 5320 206033412123A HANGAR BRACKET BELL 206 206L1 1182107 SW FUSELAGE MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 2251Z 45756 BRACKET IS TOO WIDE. DOES NOT FIT INTO BELL APPROVED FIXTURE S/N 0116 AFTER MODIFICATION OF SUPPORTS AS PER PRODUCT SUP PORT CANADA. 1 G 7 1 3U H2SW 1996082900326 19960829 00326 SW 1996 8 29 HEEA967685 1 19960820 A 7722 407375001101 INDICATOR BELL 407 407 SW COCKPIT MGT READS HIGH E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 407PH 347 53003 MGT INDICATOR READS 17 DEGREES HIGH AT 750 DEGREES CELCIUS. 1 G 7 1 3U O H2SW 1996082900328 19960829 00328 SW 1996 8 29 HEEA967687 1 19960822 A 3213 412050010111A CROSSTUBE BELL 412 412 1182202 SW LANDING GEAR DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 285 CROSSTUBE SPREADS EXCESSIVELY AT GROSS WEIGHT. 1 G 7 2 4U H4SW 1996082900329 19960829 00329 SW 1996 8 29 HEEA967688 1 19960822 A 6410 222016001115 BLADE BELL 230 230 1182149 SW T/R CRACKED BEARING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 565 23009 BEARINGS, 4 EACH P/N 222-312-753-103 BEING CRACKED ON BOTH BLADES. 1 G 7 2 3U NC H9SW 1996082900330 19960829 00330 EU 1996 8 29 HEEA967689 1 19960822 A 6520 350A33215300 BEARING 350A33211905 SNIAS 350 AS350B2 8680813 EU T/R DELAMINATING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6097Z 129 2820 RUBBER SEPARATION. PART SCRAPPED LOCALLY. 1 G 7 1 3U H9EU 1996082900331 19960829 00331 EU 1996 8 29 HEEA967690 1 19960822 A 6520 350A33215300 BEARING 350A33211905 SNIAS 350 AS350B 8680801 EU T/R GR BOX SEPARATION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 2771 RUBBER SEPARATION. PART SCRAPPED LOCALLY. 1 G 7 1 3U H9EU 1996082900332 19960829 00332 SW 1996 8 29 HEEA967691 1 19960822 A 6520 212040468001 CASE ASSY 212040004009 BELL 412 412 1182202 SW BEARING LUBE PORT MISSING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893P 5934 AFS1026 33012 T/R GEARBOX REMOVED DUE TO METAL IN OIL. FOUND OUTPUT DUPLEX BEARING P/N 212-040-456-001, S/N J6885, T.T. 1669:25 SPALL ED. LUBRICATION PORT TO FEED BEARING, NOT PRESENT IN ABOVE MENTIONED CASE ASSY, CAUSING BEARING FAILURE. 1 G 7 2 4U H4SW 1996082900338 19960829 00338 EA 1996 8 29 96ZZZX4145 2 19960408 A 8530 LW14077 PISTON PIN PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA NR 3 CYLINDER BROKEN A CSJA K NONE J WARNING INDICATION IN INSP/MAINT 1 GL 25 8530 140 317952242 L206S68A ON PREFLIGHT RUN-UP, PILOT NOTICED OIL PRESSURE LOWER THAN NORMAL. MAINTENANCE FOUND METAL IN OIL SCREEN. ON TEAR-DOWN INSPECTION, FOUND NR 3 PISTON PIN BROKEN IN HALF WHICH CAUSED PISTON TO BREAK AND SUBSEQUENT DAMAGE TO CONNECTING ROD AN D CRANKCASE. 1 L 7 2 3O 3 O A20SO E14EA 1996082900376 19960829 00376 SO 1996 8 29 RAAA96E8023 1 19960821 A 5730 PANEL LKHEED 188 188C 5262604 SO WS 183 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 73120 188C2010 DURING SCHEDULED NR 1 CHECK, FOUND UPPER RT WING NR 8 PANEL CORRODED AT WS 183. REPAIRED PER LUNDBY DESIGN SERVICE DWG 188295. 2 L 7 4 4T 4A22 1996082900377 19960829 00377 SO 1996 8 29 RAAA96E8024 1 19960821 A 5711 SPAR CAP LKHEED 188 188C 5262604 SO WS 186-90 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 73120 188C2010 DURING SCHEDULED NR 1 CHECK, FOUND RT WING REAR BEAM UPPER CAP CORRODED AT WS 186 TO 190. REPAIRED PER LUNDBY DESIGN SE RVICE DWG 188295. 2 L 7 4 4T 4A22 1996082900378 19960829 00378 SO 1996 8 29 RAAA96E8025 1 19960821 A 5413 LONGERON LKHEED 188 188C 5262604 SO NR 4 NACELLE DAMAGED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 73120 188C2010 DURING SCHEDULED NR 1 CHECK, FOUND 1 INCH HOLE CHAFED IN NR 4 NACELLE INBD UPPER LONGERON AT NAC STA 103. REPAIRED PER SRM 54-2-3 FIG 1 AND 51-3-7 FIG 1 SHEET 4. 2 L 7 4 4T 4A22 1996082900379 19960829 00379 GL 1996 8 29 RAAA96E8026 2 19960821 A 7230 6873624 INLET VANE LKHEED 188 188C 5262604 SO ALLSN 501D 501D13 03004 GL NR 1 ENGINE SEPARATED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 6295 188C2010 500751 DURING SCHEDULED NR 1 CHECK, FOUND NR 1 ENGINE COMPRESSOR INLET VANE OUTER RING SEPARATED AT 9 O'CLOCK POSITION. REPLAC ED ENGINE. 2 L 7 4 4T 4 T 4A22 E282 1996082900380 19960829 00380 NE 1996 8 29 CALA9601205 2 19960822 A 7310 KB27120 O-RING BOEING 757 757224 1384958 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE PINCHED A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 14106 27296 31286 WHILE EN ROUTE, A DISCREPANCY WAS NOTED ON FMC BETWEEN CALCULATED AND TOTALIZER FUEL. THE AIRCRAFT WAS DIVERTED TO MKE TO INVESTIGATE. THE TOWER CONFIRMED FUEL LEAK FROM RT ENGINE PRIOR TO TOUCHDOWN. THE RT ENGINE WAS SHUTDOWN UPON TOUCH DOWN. MAINTENANCE FOUND O-RING ON TUBE ASSEMBLY TO RT HP FUEL PUMP PINCHED. THE O-RING WAS REPLACED. THE RT ENGINE WA S RUN AND LEAK CHECKS WERE GOOD. 2 L 7 2 4F 4 F RT A2NM E12EU 1996082900381 19960829 00381 WP 1996 8 29 CALA9601206 1 19960821 A 3246 26088921 BEARING DOUG DC9 DC982 3022082 WP RT MLG FAILED A CALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 09 14889 19301 1820 49118 THE WHEEL NOT TURNING LIGHT ILLUMINATED DURING TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AT LOW SPEED AND THE AIRCRAFT WAS RETURNED TO GATE. MAINTENANCE FOUND THE NR 3 TIRE FLAT WHEN THE NR 3 TIRE WAS REMOVED THE BEARING WAS FOUND FROZEN TO A XLE AND THE ANTI-SKID TRANSDUCER WAS SHEARED. THE NR 3 BRAKE, ANTI-SKID TRANSDUCER, AND NR 3 MAIN AXLE SLEEVE WERE REMO VED AND REPLACED. THE NR 3 AND NR 4 MAIN TIRE AND WHEEL ASSEMBLIES WERE ALSO REMOVED AND REPLACED. 2 L 7 2 4F A6WE 1996082900382 19960829 00382 WP 1996 8 29 CALA9601207 1 19960822 A 3260 833703 DNLOCK SENSOR DOUG DC9 DC982 3022082 WP NLG INOPERATIVE A CALA O OTHER N FALSE WARNING DE DESCENT 1 SW 09 17812 49250 THE NLG RED UNSAFE LIGHT ILLUMINATED DURING DESCENT. ABNORMAL PROCEDURES WERE FOLLOWED, BUT THE LIGHT REMAINED ON. THE INDICATION LIGHTS WERE NORMAL WHEN THE GEAR WAS EXTENDED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR LOCK SENSOR AT FAULT. THE SENSOR WAS REMOVED AND REPLACED. A GEAR SWING WAS PERFORMED PER MM 32-00 WITH OPE RATION AND INDICATIONS CHECKING GOOD. 2 L 7 2 4F A6WE 1996082900383 19960829 00383 WP 1996 8 29 CALA9601208 1 19960822 A 3320 P323B634 TRANSFORMER DOUG DC9 DC982 3022082 WP LT AFT LAV OVERHEATED A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 477AC 48062 A MILD ELECTRICAL ODOR WAS OBSERVED AT LEFT AFT LAV IN FLIGHT. NO OTHER ADVERSE CONDITIONS WERE NOTED, ONLY THE ODOR. T HE FLIGHT CONTINUED TO IAH WHERE IT LANDED WITHOUT FURTHER PROBLEMS REPORTED. MAINTENANCE FOUND T1-2 TRANSFORMER FOR LI GHTS AT AFT LEFT LAV AT FAULT. THE TRANSFORMER WAS REMOVED AND REPLACED, AN OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F A6WE 1996082900384 19960829 00384 WP 1996 8 29 CALA9601209 1 19960823 A 2150 20495054 ACM DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 477AC 26197 4131 48062 AN ELECTRICAL ODOR WAS OBSERVED IN FLIGHT, AIRCRAFT HAS HISTORY. THE ODOR WAS STRONGEST IN AFT LAV NEAR CEILING. THERE WAS NO SMOKE OR HEAT PRESENT AND NO ABNORMAL ELECTRICAL LOADS WERE OBSERVED. THE FLIGHT WAS COMPLETED WITHOUT INCIDENT . MAINTENANCE FOUND THE RT ACM AT FAULT. THE RT ACM WAS REMOVED AND REPLACED, LEAK AND OPERATIONAL CHECKS WERE GOOD WI TH NO ODOR IN CABIN AFTER ONE HOUR OF PACK OPERATION. 2 L 7 2 4F A6WE 1996082900385 19960829 00385 NM 1996 8 29 CALA9601210 1 19960823 A 2913 5718607 PUMP BOEING 737 7373T0 1384582 NM B-HYD SYS LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 14324 19551 6364 23375 THE B-SYSTEM HYDRAULIC QUANTITY BEGAN TO DECREASE WHILE EN ROUTE. THE AIRCRAFT LANDED AT CLE WITHOUT INCIDENT. MAINTEN ANCE FOUND THE RT B-SYSTEM ELECTRIC HYDRAULIC PUMP LEAKING AT HOUSING. THE PUMP WAS REMOVED AND REPLACED, LEAK AND OPER ATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 1996082900386 19960829 00386 1996 8 29 CALA9601211 4 19960823 A 2210 65528175 AP ACCY UNIT BOEING 737 7373T0 1384582 NM E/E COMPT INOPERATIVE A CALA O OTHER O OTHER AP APPROACH 1 SW 09 14341 23558 19512 23579 UPON SELECTING THE APP MODE AIRCRAFT LOST ALL FLIGHT DIRECTION, NR 1 AIRSPEED BUG, YAW DAMPER, BOOST PUMPS, BUT NO BUSS OFF LIGHT ILLUMINATED. THE AIRCRAFT LANDED AT CLE WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE AUTOPILOT ACC ESSORY UNIT AND THE R2-9 RELAY. A LAND VERIFY CHECK WAS COMPLIED WITH AND ALL CHECKED GOOD. 2 L 7 2 4F RT A16WE 1996082900387 19960829 00387 WP 1996 8 29 CALA9601212 1 19960821 A 5754 ARB7105502 FAIRING DOUG DC10 DC1030 3023501 WP NR 1 LE SLAT DETACHED A CALA K NONE O OTHER TO TAKEOFF 1 SW 09 68060 47850 THE NR 1 RT SLAT FILLET FAIRING DEPARTED AIRCRAFT ON DEPARTURE. NO ABNORMAL INDICATIONS WERE NOTED IN COCKPIT. MAINTEN ANCE VERIFIED THE NR 1 RT SLAT FILLET FAIRING WAS MISSING. THE FAIRING WAS RECOVERED ON THE RUNWAY IN FCO. ALSO, FOUND DAMAGE TO THE NR 1 RT SLAT. THE NR 1 RT SLAT WAS REMOVED AND REPLACED, THE MISSING SLAT FAIRING WAS REPLACED. *S/D* I NVESTIGATION REVEALED THAT A .375 FASTENER HAD FAILED SOMETIME IN THE PAST DUE TO STRESS CORROSION AND THE FILLET WAS BE ING HELD IN PLACE WITH THE 3 REMAINING FASTENERS. AN FCD WAS ISSUED TO INSPECT THE FILLET FAIRING INSTALLATION FOR INTE GRITY ON ALL AFFECTED DC-10 AIRCRAFT. 2 L 7 3 4F A22WE 1996082900388 19960829 00388 WP 1996 8 29 CALA9601213 1 19960824 A 2910 CHECK VALVE DOUG DC9 DC982 3022082 WP RT MLG WW LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 09 72825 49485 THE AIRCRAFT LOST THE RT HYDRAULIC SYSTEM QUANTITY ON APPROACH TO IAH. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENAN CE FOUND CHECK VALVE LEAKING IN RT WHEEL WELL AT LANDING GEAR CONTROL VALVE. THE LEAKING O-RING WAS REMOVED AND REPLACE D, LEAK CHECKS WERE GOOD AND THE GEAR WAS CYCLED AS A PRECAUTION IAW MM 32-30-00. 2 L 7 2 4F A6WE 1996082900389 19960829 00389 1996 8 29 CALA9601214 4 19960824 A 3418 9654020003 AOA SENSOR DOUG DC10 DC1010 3022110 WP FWD FUSELAGE FAILED A CALA A D UNSCHED LANDING RETURN TO BLOCK N FALSE WARNING CL CLIMB 1 SW 09 68043 14898 14898 46902 UPON ROTATION GOT STALL WARNING AND RED SPEED COMMAND FLAGS. LEVELED TO GET FLAPS AND SLATS UP. UPON SLAT RETRACTION G OT SLAT DISAGREE LEFT AND SLAT RESET LIGHT CAME ON, COULD NOT RESET SLATS TO BRING UP. WOULD GET PROPER SLAT INDICATION IN THE SLAT EXTEND POSITION AND THEN COULD RESET LIGHT. THE AIRCRAFT WAS RETURNED TO NRT WHERE IT LANDED WITHOUT INCID ENT. THE LEFT AOA FAILED BITE TEST. THE LEFT AOA SENSOR WAS REMOVED AND REPLACED, BITE AND OPERATIONAL CHECKS WERE GOO D. 2 L 7 3 4F A22WE 1996082900390 19960829 00390 NM 1996 8 29 CALA9601215 1 19960825 A 3397 WIRE BOEING 737 7373T0 1384582 NM CABIN SHORTED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16301 23352 INSPECTION FOUND FLOOR TRACK LIGHTING AT FIRST FOUR SEATS ON LT SIDE OF AIRCRAFT INOPERATIVE DURING A SERVICE CHECK. MA INTENANCE FOUND WIRE SHORTED TO AIRFRAME AT FORWARD COAT CLOSET. THE WIRE WAS REPAIRED AND OPERATION OF THE FLOOR TRACK LIGHTING CHECKED GOOD. 2 L 7 2 4F RT A16WE 1996082900391 19960829 00391 WP 1996 8 29 CALA9601216 1 19960823 A 4960 360948013 CENT SWITCH 3812761M DOUG DC9 DC982 3022082 WP APU INOPERATIVE A CALA O OTHER O OTHER CL CLIMB 1 SW 09 33817 18363 18184 P975 49371 THE APU HAD A HISTORY OF AUTO SHUTDOWN DURING CLIMB PORTION OF FLIGHT AROUND FL250. THE APU HAD BEEN TEMPORARILY PLACAR DED INOPERATIVE. WHILE TROUBLESHOOTING PROBLEM IN EWR, THE APU CENTRIFUGAL SWITCH WAS REMOVED AND REPLACED, LEAK AND OP ERATIONAL CHECKS WERE GOOD AND THE PLACARD WAS REMOVED. THE AIRCRAFT HAS FLOWN OVER EIGHT FLIGHTS WITHOUT A REPEAT OF A PU PROBLEMS SINCE THIS CORRECTIVE ACTION WAS IMPLEMENTED. 2 L 7 2 4F A6WE 1996082900392 19960829 00392 WP 1996 8 29 9618331225 1 19960825 A 2133 PRESS REG VALVE DOUG DC10 DC1030 3023501 WP NR 2 MALFUNCTIONED A NWAA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 GL 01 225NW 46582 DURING CLIMB, THE NR 2 MANIFOLD FAIL LIGHT ILLUMINATED AND WAS UNABLE TO CLOSE PRV PER COM. DUMPED 45,000 LBS OF FUEL A ND RETURNED TO DTW. MAINTENANCE LOCKED THE NR 2 PRV IN THE CLOSED POSITION AND PLACED ON MEL. 2 L 7 3 4F A22WE 1996082900393 19960829 00393 1996 8 29 9618349162 4 19960821 A 3421 GYRO DOUG DC9 DC914 3022034 WP LT COCKPIT INOPERATIVE A NWAA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 01 8907E 45748 DURING CRUISE, CAPTAIN'S GYRO BECAME INOPERATIVE. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED GYRO. 2 L 7 2 4F A6WE 1996082900394 19960829 00394 WP 1996 8 29 9618359950 1 19960825 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9346 47376 DURING PERIODIC CHECK, FOUND FORWARD ENTRY EMERGENCY LIGHTS WOULD NOT TEST. REPLACED BATTERIES, OPERATIONAL CHECK NORMA L. 2 L 7 2 4F A6WE 1996082900395 19960829 00395 WP 1996 8 29 9618369998 1 19960823 A 3350 60030451 BATTERY PACK DOUG DC9 DC931 3022065 WP TAILCONE MALFUNCTIONED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8934E 47143 DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND BATTERIES, OP ERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996082900396 19960829 00396 WP 1996 8 29 9618379603 1 19960823 A 3397 WIRE DOUG DC9 DC932 3022066 WP CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 603NW 47101 DURING LINE MAINTENANCE INSPECTION, FOUND OVERWING AND OVERHEAD EMERGENCY LIGHTS INOPERATIVE. SECURED GROUND WIRES AT G ROUNDING STUD 411, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996082900397 19960829 00397 WP 1996 8 29 9618389964 1 19960822 A 3350 60030451 POWER SUPPLY DOUG DC9 DC931 3022065 WP TAIL COMPT MALFUNCTIONED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 912RW 47150 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, OPERATI ONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996082900398 19960829 00398 WP 1996 8 29 9618399612 1 19960822 A 3397 WIRE HARNESS DOUG DC9 DC932 3022066 WP CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 612NW 47436 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS AT ROW 14 INOPERATIVE. SECURED LOOSE HARNESS AT ROW 14, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996082900399 19960829 00399 WP 1996 8 29 9618409940 1 19960824 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP TAIL COMPT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 3322L 47031 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY EVACUATION LIGHTS IN TAIL COMPARTMENT INOPERATIVE. REPLACED BATTERI ES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996082900400 19960829 00400 WP 1996 8 29 9618419931 1 19960825 A 3350 BATTERY PACKS DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 90S 47244 DURING PERIODIC CHECK, FOUND CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996082900401 19960829 00401 NE 1996 8 29 9618426637 2 19960824 A 7230 COMPRESSOR BOEING 747 747251B 1384892 NM PWA JT9 JT9D7R4G2 52054 NE NR 3 ENGINE STALLED A NWAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 01 637US 23548 15257 DURING INITIAL CLIMB, THE NR 3 ENGINE EXPERIENCED A COMPRESSOR STALL. THE ENGINE WAS SHUTDOWN AND RESTARTED. FLIGHT CO NTINUED AND AT TOP OF DESCENT, THE NR 3 ENGINE STALLED AGAIN. HOWEVER, ENGINE SHUTDOWN WAS NOT ACCOMPLISHED. FLIGHT CO NTINUED TO HKG WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED BORESCOPE INSPECTION OF 8TH, 9TH, 15TH STAGES OF HPT AND 13TH STAGE OF OUTER SHROUD. NO DISCREPANCIES WERE FOUND. REPLACED EVBC AND ACCOMPLISHED PRECISION TRIM OF EVBC AND FC U. 2 L 7 4 4F 4 F A20WE E3NE 1996082900402 19960829 00402 WP 1996 8 29 9618439606 1 19960809 A 5242 DOOR DOUG DC9 DC932 3022066 WP E/E COMPT NOT SECURED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 606NW 47225 DURING CLIMB, NOTED A LOUD RUMBLE FROM THE NOSE LANDING GEAR VICINITY AND INABILITY TO PRESSURIZE. RETURNED TO MSP WITH OUT FURTHER INCIDENT. FOUND THE FORWARD E/E DOOR NOT FULLY CLOSED. RESEATED THE SAME, THE DOOR WARNING SYSTEM WAS ON M EL 33-17A AT THE TIME OF THIS INCIDENT. 2 L 7 2 4F A6WE 1996082900403 19960829 00403 NM 1996 8 29 9618446308 1 19960825 A 3350 POWER SUPPLY BOEING 747 747451 1384940 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 668US 24223 DURING LINE CHECK, FOUND EMERGENCY FLOOR PATH LIGHTS INOPERATIVE FROM ROWS 21 TO 31. REPLACED POWER SUPPLY AND BATTERY PACK, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1996082900404 19960829 00404 SO 1996 8 29 COMA9610250 1 19960819 A 5320 12046963001 BUTT STRAP 1204615550 EMB 120 EMB120RT SO CABIN FLOOR CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 255CA 13219 120238 INSPECTION REVEALED CORROSION ON THE FORWARD CABIN FLOOR SUPPORT OM26A BEAM BUTT STRAP ON THE LEFT SIDE GALLEY AREA. TH E BUTT STRAP WAS REPLACED WITH A NEW PART PER EMB120 5RM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1996082900405 19960829 00405 SO 1996 8 29 COMA9610251 1 19960823 A 7920 1593731 OIL BYPASS LINE EMB 120 EMB120RT SO RT ENGINE FAILED A COMA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 1105G 120105 RT ENGINE LOST OIL PRESSURE DURING FLIGHT. ENGINE SECURED AND ACFT DIVERT TO DAY. REPLACED LEAKING OIL COOLER BYPASS L INE. 2 L 7 2 4T RT A31SO 1996082900406 19960829 00406 SO 1996 8 29 COMA9610252 1 19960821 A 3260 922AA2YAGPZ722 SENSOR EMB 120 EMB120RT SO RT MLG DEFECTIVE A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 137H 120137 THE RT MLG DOWN LOCK LIGHT REMAINED ON AFTER GEAR RETRACTION. REPLACED DEFECTIVE DOWN LOCK PROXIMITY SENSOR. 2 L 7 2 4T RT A31SO 1996082900407 19960829 00407 SO 1996 8 29 COMA9610253 1 19960821 A 3350 BULB EMB 120 EMB120RT SO CABIN FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 266CA 120258 LT AFT EMERGENCY LIGHT IS INOP. REPLACED BULB. 2 L 7 2 4T RT A31SO 1996082900408 19960829 00408 NE 1996 8 29 COMA9610254 3 19960820 A 6111 PROP BLADE EMB 120 EMB120RT SO HAMSTD 14RF 14RF9 NE RT ENGINE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 159A 14496 62 120159 900932 RT PROPELLER, NR 1 BLADE IS CRACKED NEAR THE TIP AT TWO PLACES. REMOVED AND REPLACED THE NR 1 BLADE ASSY. 2 L 7 2 4T RT A31SO 6 C P11NE 1996082900409 19960829 00409 NE 1996 8 29 COMA9610255 2 19960821 A 7310 12018198035 FUEL HOSE EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE LEAKING A COMA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 159A 120159 RT ENGINE IS LEAKING FUEL. REPLACED LEAKING PRIMARY FLOW HOSE ASSY. 2 L 7 2 4T 4 T RT A31SO E20NE 1996082900410 19960829 00410 SO 1996 8 29 COMA9610256 1 19960819 A 5413 12018760007 STRINGER EMB 120 EMB120RT SO RT NACELLE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 255CA 13219 120238 INSPECTION REVEALED A CRACK IN THE RIGHT NACELLE LT STRINGER 1. THE STRINGER WAS REPAIRED PER AERODESIGN REPORT NR 2000 -1, DATED 8-17-96. 2 L 7 2 4T RT A31SO 1996082900411 19960829 00411 SO 1996 8 29 COMA9610257 1 19960820 A 5523 12021020015 TRIM TAB EMB 120 EMB120RT SO LT ELEVATOR DAMAGED A COMA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 01 267CA 11326 120259 ELEVATOR CONTROLS ARE BINDING. FOUND LT ELEVATOR TRIM TAB RUBBING AGAINST TAIL FAIRING, TRIM TAB SHEET METAL WAS DAMAGE D. REPLACED THE ELEVATOR TRIM TAB AND CORRECTED THE ALIGNMENT OF TAIL CONE FAIRING. 2 L 7 2 4T RT A31SO 1996082900412 19960829 00412 EA 1996 8 29 COMA9660136 1 19960821 A 5230 057324 SEAL CNDAIR CL600 CL6002B19 EA CARGO DOOR LOOSE A COMA O OTHER O OTHER CR CRUISE 1 SO 01 1117H 1117 CABIN PRESSURIZATION, DUMPED AT 18,000 FEET. REPAIRED LOOSE CARGO DOOR SEAL. 2 L 7 2 4F RT A21EA 1996082900413 19960829 00413 EA 1996 8 29 COMA9660137 1 19960822 A 4990 APU CNDAIR CL600 CL6002B19 EA OVER SERVICED A COMA E H ENGINE SHUTDOWN DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 938CA 7046 LARGE AMOUNTS OF SMOKE COMING FROM APU. FOUND APU OIL SYSTEM TO BE OVER SERVICED. SERVICED APU OIL SYSTEM TO PROPER LE VEL AND ACFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1996082900414 19960829 00414 EA 1996 8 29 COMA9660138 1 19960821 A 7332 CONNECTOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RT ENGINE LOOSE A COMA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SO 01 914CA 7012 RT ENGINE LOW FUEL PRESSURE WARNING DOES NOT TEST. SECURED LOOSE WIRING CONNECTOR AT FUEL PRESSURE SWITCH. 2 L 7 2 4F 4 F RT A21EA E15NE 1996082900415 19960829 00415 NM 1996 8 29 UPS96220931 1 19960717 A 5313 STRINGER BOEING 727 72725C 138400H NM BS 1243-1342 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-C, STRINGER CRACKED STA 1243 TO 1342, 12R. REMOVED AND REPLACED STRINGER PER UPS SRM 53-10-02, 51-30-02 . 2 L 7 3 4F A3WE 1996082900416 19960829 00416 NM 1996 8 29 UPS96220932 1 19960711 A 7110 652368723 ENGINE RING BOEING 727 72725C 138400H NM BS 1352 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-C, STA 1352 ENGINE RING CORRODED. REMOVED AND REPLACED (P/N 65-23687-23) IAW SRM 51-30-02. 2 L 7 3 4F A3WE 1996082900417 19960829 00417 NM 1996 8 29 UPS96220933 1 19960712 A 5320 ANGLE BOEING 727 72725C 138400H NM BS 560 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-C, FWD LWR CARGO THRESHOLD SUPPORT ANGLE CRACKED STA 560 STR 26R TO 27R. REMOVED, FAB'D AND INSTALLED R EPAIR ANGLE PER UPS SRM 53-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 1996082900418 19960829 00418 NM 1996 8 29 UPS96220934 1 19960718 A 5320 CHORD BOEING 727 72725C 138400H NM BS 1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-C, TORQUE BOX VERTICAL FIN LT CHORD CORRODED OUT OF LIMITS STA 1342 FIN STA 0. CUT OUT DAMAGE, FAB'D AN D INSTALLED REPAIR PARTS PER DHC SK 951-984. 2 L 7 3 4F A3WE 1996082900419 19960829 00419 NM 1996 8 29 UPS96220935 1 19960720 A 5531 DOUBLER BOEING 727 72725C 138400H NM BS 1342 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-C, LT INNER SPAR SKIN, INTERNAL DOUBLER CRACKED. REMOVED, FAB'D AND INSTALLED INNER SPAR SKIN INTERNAL DOUBLER PER BOEING DWG 65-17509 AND UPS SRM 51-30-02. 2 L 7 3 4F A3WE 1996082900420 19960829 00420 NM 1996 8 29 UPS96220936 1 19960710 A 5320 CHANNEL BOEING 727 72725C 138400H NM BS 1160 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-C, FLOOR SUPPORT U-CHANNEL CORRODED AFT LWR CARGO PIT. REMOVED AND REPLACED U-CHANNEL PER UPS SRM 51-30 -2 AND 51-10-01. 2 L 7 3 4F A3WE 1996082900421 19960829 00421 NM 1996 8 29 UPS96220937 1 19960710 A 5347 SEAT TRACK BOEING 727 72725C 138400H NM BS 1160 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-C, LT SEAT TRACK AT STA 1160 LT HAS HEAVY CORROSION, AFT LWR CARGO. REMOVED AND REPLACED SEAT TRACK (P/ N 65-22797-5) PER SRM 51-30-2 AND 51-10-01. 2 L 7 3 4F A3WE 1996082900422 19960829 00422 NM 1996 8 29 UPS96220938 1 19960718 A 5531 SPAR SKIN BOEING 727 72725C 138400H NM BS 1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-C, LT INNER SPAR SKIN IS CORRODED BEYOND LIMITS STA 1342 LT. REMOVED DAMAGE, FABRICATED AND INSTALLED I NNER SPAR SKIN DOUBLERS AND REPAIR DOUBLERS PER BOEING DWG 65C-29055 AND 951-982. 2 L 7 3 4F A3WE 1996082900423 19960829 00423 NM 1996 8 29 UPS96220939 1 19960730 A 5531 RIB BOEING 727 72725C 138400H NM FS 1352 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-C, FS 1352 FIN STA 22.5 LT RIB IS CRACKED. CUTOUT DAMAGED AREA PER SRM 51-40-3, FAB'D AND INSTALLED ANG LE DOUBLER PER SRM 51-40-3 AND 51-30-2. 2 L 7 3 4F A3WE 1996082900424 19960829 00424 NM 1996 8 29 UPS96220940 1 19960708 A 5531 RIB BOEING 727 72725C 138400H NM FS 1352 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-C, FS 135 AND FIN STA 22.5 RT RIB IS CRACKED. CUT OUT DAMAGED AREA PER SRM 51-40-3, FAB'D AND INSTALLED ANGLE DOUBLER PER SRM 51-40-3 AND 51-30-2. 2 L 7 3 4F A3WE 1996082900425 19960829 00425 NM 1996 8 29 UPS96220941 1 19960706 A 5320 STIFFENER BOEING 727 72725C 138400H NM BS 940 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-C, LT KEEL BEAM VERTICAL STIFFENER EXFOLIATION CORROSION STA 940 WL 185. REMOVED DAMAGED AREA, FABRICAT ED AND INSTALLED REPAIR PARTS SRM 51-40-4 FIG 1 AND 51-30-2. 2 L 7 3 4F A3WE 1996082900426 19960829 00426 NM 1996 8 29 UPS96220942 1 19960712 A 5320 66182633 SHEAR TIE BOEING 727 72725C 138400H NM BS 590 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-C, SHEAR TIE HAS HEAVY CORROSION STA 590 BETWEEN STR 24R AND 25R. REMOVED AND REPLACED SHEAR TIE PER SR M 51-30-2 AND 51-10-01. 2 L 7 3 4F A3WE 1996082900427 19960829 00427 NM 1996 8 29 UPS96220943 1 19960729 A 5530 HORIZ CHORD BOEING 727 72725C 138400H NM BS 1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-C, VERT FIN TORQUE BOX RT HORIZ CHORD CORRODED OUT OF LIMITS STA 1342 FIN STA 0. REMOVED DAMAGED SECTIO N OF CHORD, FAB'D AND INSTALLED REPAIR PARTS PER DHC SK 951-021. 2 L 7 3 4F A3WE 1996082900428 19960829 00428 NM 1996 8 29 UPS96220944 1 19960729 A 5531 SPAR SKIN BOEING 727 72725C 138400H NM BS 1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-C, RT VERT STAB INNER SPAR SKIN CORRODED BEYOND LIMITS STA 1342. REMOVED DAMAGED SKIN, FAB'D AND INSTAL LED REPAIR PARTS PER DHC SK 951-982. 2 L 7 3 4F A3WE 1996082900429 19960829 00429 NM 1996 8 29 UPS96220945 1 19960724 A 7110 FLANGE BOEING 727 72725C 138400H NM BS 1352 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-C, FLANGE ATTACHED TO ENG RING CRACKED APPROX .25 INCH STA 1352,1 O'CLOCK POS. REMOVED RING ANGLE, RADI USED OUT DAMAGE, NDT DET NO CRACK REMAINING. REINSTALLED ANGLE, PER SRM 51-30-02 AND 51-10-01. 2 L 7 3 4F A3WE 1996082900430 19960829 00430 NM 1996 8 29 UPS96220946 1 19960711 A 5311 FRAME BOEING 727 72725C 138400H NM BS 1342 CORRODED A IPXA O OTHER O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-C, LT FRAME CHORD CORRODED STA 1342 LBL 20 WL 238. REMOVED AND REPLACED CHORD PER SRM 51-10-01 AND EO B 727-5530-4601B. 2 L 7 3 4F A3WE 1996082900431 19960829 00431 NM 1996 8 29 UPS96220947 1 19960711 A 5311 FRAME BOEING 727 72725C 138400H NM BS 1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-C, RT FRAME CHORD CORRODED STA 1342 RBL 20 WL 238. REMOVED AND REPLACED CHORD PER SRM 51-10-01 AND EO B 727-5530-4601B. 2 L 7 3 4F A3WE 1996082900432 19960829 00432 NM 1996 8 29 UPS96220948 1 19960711 A 5311 FRAME BOEING 727 72725C 138400H NM BS 1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-C, LT LWR FRAME CHORD CORRODED STA 1342 LBL 24 WL 220. REMOVED AND REPLACED CHORD PER SRM 51-10-01 EO B 727-5530-4601B. 2 L 7 3 4F A3WE 1996082900433 19960829 00433 NM 1996 8 29 UPS96220949 1 19960711 A 5320 CHANNEL BOEING 727 72725C 138400H NM BS 1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-C, CENTER CHANNEL IS CORRODED STA 1342. REMOVED AND REPLACED CENTER CHANNEL PER SRM 51-10-01 AND EO B72 7-5530-46 01B. 2 L 7 3 4F A3WE 1996082900434 19960829 00434 NM 1996 8 29 UPS96220950 1 19960711 A 5320 CHANNEL BOEING 727 72725C 138400H NM BS 1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-C, RT CHANNEL CORRODED AFT SIDE STA 1342 RBL 18 WL 247. REMOVED AND REPLACED CHANNEL PER SRM 51-10-01 A ND EO B727-5530-4601B. 2 L 7 3 4F A3WE 1996082900435 19960829 00435 NM 1996 8 29 UPS96220952 1 19960711 A 5320 CHANNEL BOEING 727 72725C 138400H NM BS 1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-C, LT CHANNEL CORRODED ON AFT SIDE STA 1342 LBL 18 WL 247. REMOVED AND REPLACED CHANNEL PER BOEING DWG 65-93155 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996082900436 19960829 00436 NM 1996 8 29 UPS96220953 1 19960711 A 5320 CHORD BOEING 727 72725C 138400H NM BS 1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-C, LT O/B CHORD CORRODED STA 1342 LBL 30 WL 250. REMOVED AND REPLACED CHORD PER SRM 51-10-1 AND EO B727 -5530-4601B. 2 L 7 3 4F A3WE 1996082900437 19960829 00437 NM 1996 8 29 UPS96220954 1 19960711 A 5320 CHORD BOEING 727 72725C 138400H NM BS 1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-C, CHORD CORRODED ON FWD SIDE STA 1342. REMOVED AND REPLACED CHORD PER BOEING DWG 65-20981, SRM 53-30-2 AND EO B727-5530-4601B. 2 L 7 3 4F A3WE 1996082900438 19960829 00438 NM 1996 8 29 UPS96220955 1 19960710 A 5320 CHANNEL BOEING 727 72725C 138400H NM BS 1046 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-C, AFT LOWER PIT STA 1046 RBL 20 FLOOR SUPPORT U-CHANNEL IS CORRODED HEAVY AT SPLICE. REMOVED CORRODED FLOOR SUPPORT AND INSTALLED REPLACEMENT FLOOR SUPPORT IN LOWER AFT PIT STA 1046 RBL 20 PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996082900439 19960829 00439 NM 1996 8 29 UPS96220956 1 19960718 A 5320 ANGLE BOEING 727 72725C 138400H NM BS 1367 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-C, FS 1367 FIN STA 22.5 LT SKIN SUPPORT ANGLE IS CRACKED. CUT OUT DAMAGED AREA, FABRICATED ANGLE AND AN GLE DOUBLER, INSTALLED PER SRM 51-40-3, 51-30-2. 2 L 7 3 4F A3WE 1996082900440 19960829 00440 NM 1996 8 29 UPS96220957 1 19960718 A 5320 ANGLE BOEING 727 72725C 138400H NM BS 1367 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-C, FS 1367 FIN STA 22.5 RT SKIN SUPPORT ANGLE IS CRACKED. CUT OUT DAMAGED AREA, FABRICATED ANGLE AND AN GLE DOUBLER, INSTALLED PER SRM 51-40-03, 51-30-2. 2 L 7 3 4F A3WE 1996082900441 19960829 00441 NM 1996 8 29 UPS96220958 1 19960711 A 5311 FRAME BOEING 727 72725C 138400H NM BS 1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-C, RT LOWER FRAME CHORD RBL 24, WL 220, STA 1342 IS CORRODED. REMOVED AND REPLACED CHORD AT STA 1342 WL 220 PER SRM 51-30-02. 2 L 7 3 4F A3WE 1996082900442 19960829 00442 NM 1996 8 29 UPS96220959 1 19960708 A 5751 SPAR CHORD BOEING 727 72725C 138400H NM RT AILERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-C, RT O/B AILERON AT CENTER I/B HINGE, LWR SPAR CHORD IS CRACKED. REMOVED, FABRICATED AND INSTALLED LWR SPAR CHORD PER BOEING DWG 65-21766, SRM 51-30-02. 2 L 7 3 4F A3WE 1996082900443 19960829 00443 NM 1996 8 29 UPS96220960 1 19960711 A 5320 CHORD BOEING 727 72725C 138400H NM BS 1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-C, RT O/B CHORD IS CORRODED STA 1342 RBL 30 WL 250. REMOVED AND EPLACED RT O/B CHORD PER EO B727-5530-4 601B AND SRM 51-10-01. 2 L 7 3 4F A3WE 1996082900444 19960829 00444 NM 1996 8 29 UPS96220961 1 19960715 A 5320 ANGLE BOEING 727 72725C 138400H NM AFT TAIL SKID CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-C, BL 0 SKIN SUPPORT ANGLE AND CLIP WAS FOUND TO HAVE HEAVY CORROSION BEYOND LIMITS. REMOVED AND FABRIC ATED REPLACEMENT ANGLE AND CLIP AND REPLACED PER SRM 51-10-01 AND 51-30-02. 2 L 7 3 4F A3WE 1996082900445 19960829 00445 NM 1996 8 29 UPS96220962 1 19960717 A 5320 CHORD BOEING 727 72725C 138400H NM BS 338 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-C, NLG W/W RT UPPER CHORD OUT OF LIMITS AFTER CORROSION REMOVAL. FLAP PEENED AREA AFTER CORROSION REMOV AL, FABRICATED AND INSTALLED REPAIR ANGLE PER DHC SK-951-598 REV B AND OHM 20-10-03 AND APPLIED TOP COAT PER SRM 51-10-2 . 2 L 7 3 4F A3WE 1996082900446 19960829 00446 NM 1996 8 29 UPS96220967 1 19960825 A 5320 SHEAR TIE BOEING 727 727247 138408F NM BS 1166 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 212UP 21392 INSPECTION TYPE-C, CORROSION (C53-113-01.02-02) ON SHEAR TIE STA 1166 BETWEEN STR 28 AND 29 LT. CORROSION REWORK OUT OF LIMITS IAW SRM 53-10-1. REMOVED AND REPLACED SHEAR TIE AT STA 1166 IAW SRM 51-30-1. 2 L 7 3 4F A3WE 1996082900447 19960829 00447 NM 1996 8 29 UPS96220968 1 19960825 A 5753 SKIN BOEING 727 727247 138408F NM TE AFT FLAP DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 212UP 21392 INSPECTION TYPE-C, LEFT WING I/B AFT FLAP HAS 2 INCH AREA OF DISBOND, LOWER SURFACE. REPAIRED PER SRM 51-40-6. 2 L 7 3 4F A3WE 1996082900448 19960829 00448 NM 1996 8 29 UPS96220969 1 19960825 A 5753 SKIN BOEING 727 727247 138408F NM TE AFT FLAP DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 212UP 21392 INSPECTION TYPE-C, LEFT WING I/B AFT FLAP HAS 2 AREAS OF DISBOND UPPER SURFACE. REPAIRED PER SRM 51-40-6. 2 L 7 3 4F A3WE 1996082900449 19960829 00449 NM 1996 8 29 UPS96220970 1 19960816 A 5320 655611915 SHEAR TIE BOEING 727 727247 138408F NM BS 950 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 212UP 21392 INSPECTION TYPE-C, CORROSION SHEAR TIE BS 950A BETWEEN STR 28 TO 29 RT. REMOVED SHEAR TIE AND REPLACED PER SRM. 2 L 7 3 4F A3WE 1996082900450 19960829 00450 NM 1996 8 29 UPS96220971 1 19960816 A 5311 FRAME BOEING 727 727247 138408F NM BS 990 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 212UP 21392 INSPECTION TYPE-C, CORROSION ON STIFFENER AND FRAME BS 990 WL 139 LBL 7 TO 13. REMOVED CORRODED AREA OF FRAME AND REPAI RED PER SRM 53-10-04. 2 L 7 3 4F A3WE 1996082900451 19960829 00451 NM 1996 8 29 UPS96220972 1 19960823 A 5312 651594010 BLKHD STIFFENER BOEING 727 727247 138408F NM BS 740 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 212UP 21392 INSPECTION TYPE-C, 740 BULKHEAD VERTICAL STIFFENER HAS CORROSION ON BOTTOM AROUND FASTENERS, RBL 25 WL 146. REMOVED COR ROSION AND FOUND OUT OF LIMITS. STIFFENER WAS REMOVED AND INSTALLED NEW STIFFENER. ALL WORK ACCOMPLISHED PER SRM 53-10 -11, 51-30-5, 51-20-2, M/M 34-35-11, 34-35-00. 2 L 7 3 4F A3WE 1996082900452 19960829 00452 NM 1996 8 29 UPS96220973 1 19960822 A 5320 SHEAR TIE BOEING 727 727247 138408F NM BS 600 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 212UP 21392 INSPECTION TYPE-C, CORROSION (C530113-01.00-01) CORROSION ON SHEAR TIE AND WEB STA 600, LBL 19 TO 22 WL 146. CORROSION REMOVAL OUT OF LIMITS ON SHEAR TIE, WEB WAS WITHIN LIMITS. FABRICATED NEW SHEAR TIE AND INSTALLED. FOUND CRACKED SKIN UNDER SHEAR TIE, REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, INSTALLED ALL WORK PER SRM 53-30-3, 51-30-2, 51-30-8. 2 L 7 3 4F A3WE 1996082900453 19960829 00453 NM 1996 8 29 UPS96220974 1 19960823 A 5320 SHEAR TIE BOEING 727 727247 138408F NM BS 1130 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 212UP 21392 INSPECTION TYPE-C, CORROSION (C53-113-01. 02-02) ON SHEAR TIE STA 1130 BETWEEN STR 28 TO 29 RT. CORROSION REMOVAL WAS O UT OF LIMITS, REMOVED DAMAGED SHEAR TIE, FABRICATED NEW SHEAR TIE AND INSTALLED. ALL WORK DONE IAW SRM 53-10-1, 53-10-4 , 51-30-2, 51-10-02. 2 L 7 3 4F A3WE 1996082900454 19960829 00454 NM 1996 8 29 UPS96220975 1 19960822 A 5754 651622369 SUPPORT BOEING 727 727247 138408F NM NR 2 LE SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 212UP 21392 INSPECTION TYPE-C, NR 2 SLAT I/B TRACK SUPPORT, O/B RIB IS CRACKED. REMOVED AND REPLACED NR 2 SLAT ASSY PER M/M 27-81-1 1. 2 L 7 3 4F A3WE 1996082900455 19960829 00455 NM 1996 8 29 UPS96220976 1 19960822 A 5320 655612611 SHEAR TIE BOEING 727 727247 138408F NM FUSELAGE CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 212UP 21392 INSPECTION TYPE-C, SHEAR TIE IS CORRODED AND FOUND OUT LIMITS. WHILE REMOVING SHEAR TIE FOUND FRAME SPLICE PLATE TO BE CRACKED. RECEIVED AND INSTALLED NEW SHEAR TIE AND FABRICATED NEW FRAME SPLICE PLATE AND INSTALLED. ALL WORK ACCOMPLISH ED PER SRM 51-10-6, 51-20-1, 51-30-2, 51-10-2, 51-20-4. 2 L 7 3 4F A3WE 1996082900456 19960829 00456 NM 1996 8 29 UPS96220977 1 19960821 A 5320 SHEAR TIE BOEING 727 727247 138408F NM BS 1070 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 212UP 21392 INSPECTION TYPE-C, CORROSION (C53-113-01.02-02) ON SHEAR TIE STA 1070 BETWEEN STR 29 TO 30 LT. CORROSION FOUND OUT OF L IMITS, DUPLICATE WRITE-UP OF NRC 584267, ALL WORK TO BE ACCOMPLISHED ON NRC 584267. 2 L 7 3 4F A3WE 1996082900457 19960829 00457 NM 1996 8 29 UPS96220978 1 19960820 A 5320 65453132 CLIP BOEING 727 727247 138408F NM BS 1040 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 212UP 21392 INSPECTION TYPE-C, CORROSION (C53-113-01.02-02) ON STRINGER CLIP STA 1040, STR 29 RT. STRINGER CLIP CORRODED OUT OF LIM ITS. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-10-1, 51-19-6 AND 53-10-1. 2 L 7 3 4F A3WE 1996082900458 19960829 00458 NM 1996 8 29 UPS96220979 1 19960821 A 5313 STRINGER BOEING 727 727247 138408F NM BS 571 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 212UP 21392 INSPECTION TYPE-C, CORROSION (C53-113-01.00-01) BROKEN STAND-OFF FOR CLAMP STA 571, LBL 8 WL 148, STR 27 LEFT. CORROSIO N OUT OF LIMITS IN A 1 BY 1 AREA, FABRICATED REPAIR PARTS AND REPAIRED PER SRM 53-10-3. 2 L 7 3 4F A3WE 1996082900459 19960829 00459 NM 1996 8 29 UPS96220980 1 19960820 A 5320 SUPPORT BOEING 727 727247 138408F NM BS 520-540 CORRODED A IPXA O OTHER O OTHER IN INSP/MAINT 1 SO 01 212UP 21392 INSPECTION TYPE-C, CORROSION (C53-113-01.00-01) AROUND BOTTOM OF NUTPLATES STA 520 TO 540. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1, FLOOR SUPPORT WILL BE REPLACED ON NRC 584590. 2 L 7 3 4F A3WE 1996082900460 19960829 00460 NM 1996 8 29 UPS96420963 1 19960726 A 5330 SKIN BOEING 747 747123 1384873 NM BS 2450-2580 SCRATCHES A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE-C, FOUND SIGNS OF TAIL STRIKE BETWEEN BS 2450 TO 2580 LOTS OF DEEP SCRATCHES AND DENTS. REPAIRED FUSELA GE IAW SRM 53-30-03. 2 L 7 4 4F A20WE 1996082900461 19960829 00461 NM 1996 8 29 UPS96420964 1 19960726 A 5711 SPAR WEB BOEING 747 747123 1384873 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE-C, RT WING FRONT SPAR WEB FOUND TWO CRACKS OUTSIDE OF SB747-57A2266. INSPECTION AREA REF NRC 710789, TH E FIFTH HOLE 2MM, SEVENTH HOLE .5MM. REPAIRED TWO CRACKS ACC KLM DFX 96-0165 ISSUE 4 APPR ACC TO FAA FORM 2110-3 AND UP S EO B747-5720-8543-A. 2 L 7 4 4F A20WE 1996082900462 19960829 00462 NM 1996 8 29 UPS96420965 1 19960723 A 5711 SPAR WEB BOEING 747 747123 1384873 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE-C, RT WING FRONT SPAR FOUND DURING NDO INSPECTION OF SB 747-57A2266 CRACK IN FRONT SPAR WEB AT STIFFENER FS 655.75 FOURTH HOLE FROM UPPER SIDE 4MM. AFTER INSP ALSO FOUND CRACKS AT FIFTH AND SEVENTH HOLE 2MM, .05MM. REPAIRE D FOURTH HOLE FROM UPPER SIDE ACC KLM DFX 96-165 ISSUE 4 APPR ACC TO FAA FORM 0110-3 AND UPS EO B747-5720-8543-A. 2 L 7 4 4F A20WE 1996082900463 19960829 00463 NM 1996 8 29 UPS96420966 1 19960719 A 5320 DOUBLER BOEING 747 747123 1384873 NM FUSELAGE INCORRECT REPAIR A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE-C, BECAUSE OF OLD NOT ACCORDING SRM REPAIR, MOD DOUBLER MUST BE REPLACED BY NEW ENLARGED DOUBLER AT MED LT LOWER AFT CORNER. REPLACED DOUBLER IAW KLM DFX 96-155 ISSUE 4. 2 L 7 4 4F A20WE 1996082900464 19960829 00464 NM 1996 8 29 UPS96520951 1 19960822 A 5751 SKIN BOEING 757 75724APF 1384969 NM RT AILERON DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 408UP 23730 INSPECTION TYPE-3C, WHILE WORKING EO B757-5760-6676B FOUND AREA OF DELAM AT INBOARD FORWARD CORNER OF RIGHT WING AILERON LOWER CONDUCTIVE FRAME. REPAIRED RT AILERON LWR SURFACE IAW SRM 51-31-01. 2 L 7 2 4F RT A2NM 1996082900465 19960829 00465 WP 1996 8 29 UPS96820259 1 19960604 A 3210 ATTACH PIN DOUG DC8 DC873F 302199F WP LT MLG SHEARED A A IPXA O OTHER O OTHER AP APPROACH 1 SO 01 806UP 46006 INSPECTION TYPE-N/A, UPON GEAR EXTENSION THERE WAS A LOUD BANG AND YAW OF THE A/C TO THE RIGHT. ONLY THE LEFT GEAR EXTEN DED AND AFTER ABOUT 10 SECONDS THE RIGHT MAIN AND NOSE GEAR EXTENDED. GEAR INDICATIONS WERE NORMAL, LATER FOUND LT MLG ATTACH PIN WAS SHEARED. REPLACED TORQUE TUBE, BUNGEE AND UPPER CYLINDER PER TASK CARD 2534 AND OHM 32-10-01 REPLACED AT TACH PIN. 2 L 7 4 4F RT 4A25 1996082900466 19960829 00466 WP 1996 8 29 UPS96820919 1 19960811 A 5753 5652288505 VANE DOUG DC8 DC871F 302199D WP NR 2 TE FLAP DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE-C, LT WING NR 2 FLAP VANE DELAMINATED. REPLACED VANE PER MM 27-51-14. 2 L 7 4 4F RT 4A25 1996082900467 19960829 00467 WP 1996 8 29 UPS96820920 1 19960811 A 5753 5701446501 VANE DOUG DC8 DC871F 302199D WP NR 2 TE FLAP DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE-C, LEFT FLAP NR 3 VANE DELAMINATED. REPLACED VANE PER MM 27-51-14. 2 L 7 4 4F RT 4A25 1996082900468 19960829 00468 WP 1996 8 29 UPS96820921 1 19960812 A 5320 3754916501 FITTING DOUG DC8 DC871F 302199D WP BS 1150 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYP-C, LONGERON 31R FS 1150 END FITTING CRACKED. REPLACED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996082900469 19960829 00469 WP 1996 8 29 UPS96820922 1 19960811 A 5310 FITTING DOUG DC8 DC871F 302199D WP BS 1150-1230 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE-C, 4 BANANA FITTINGS CRACKED AT C-BAG BIN DOOR JAMB FS 1150 TO 1230 LONGERONS 31R TO 33R. REPLACED FITT INGS PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996082900470 19960829 00470 WP 1996 8 29 UPS96820923 1 19960810 A 5320 37549301N T-FITTING DOUG DC8 DC871F 302199D WP BS 1160-1240 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE-C, 3 T-FITTINGS HEAVY CORROSION AT C-DOOR JAMB LONGERON 33R FS 1160 TO 1240, NR 2, NR 5 AND NR 3 FITTING S. REPLACED FITTINGS PER SRM 53-2-0. 2 L 7 4 4F RT 4A25 1996082900471 19960829 00471 WP 1996 8 29 UPS96820924 1 19960810 A 5347 5277266040500 TRACK DOUG DC8 DC871F 302199D WP BS 40 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE-C, HEAVY CORROSION ON TRACK NR 1 FWD END OF POSITION NR 2. REPAIRED TRACK PER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1996082900472 19960829 00472 WP 1996 8 29 UPS96820925 1 19960809 A 5347 74529523 TRACK DOUG DC8 DC871F 302199D WP BS 340 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE-C, HEAVY CORROSION ON TRACK NR 1 FWD END OF POSITION 1. REPAIRED TRACK PER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1996082900473 19960829 00473 WP 1996 8 29 UPS96820926 1 19960816 A 5720 5642940501 DOUBLER DOUG DC8 DC873F 302199F WP WS 22.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE-SPEC, LT WING UPPER ACCESS PANEL DOUBLER HAS A 1.5 INCH LONG CRACK WS XRS 22.750 STRINGER NR 6. REPAIRE D PER UPS EO. 2 L 7 4 4F RT 4A25 1996082900474 19960829 00474 WP 1996 8 29 UPS96820927 1 19960816 A 5320 46413141 FITTING DOUG DC8 DC871F 302199D WP BS 20 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE-C, FS 20 LONGERON END FITTING CRACKED, LONGERON 20R. REPLACED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996082900475 19960829 00475 WP 1996 8 29 UPS96820928 1 19960811 A 5320 DOUBLER DOUG DC8 DC871F 302199D WP BS 8-70 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE-C, FINGER DOUBLER AT FS 8 TO 70, LONGERON 31R, HAS HEAVY CORROSION. REPLACED DOUBLER PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1996082900476 19960829 00476 WP 1996 8 29 UPS96820929 1 19960812 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 528 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE-C, LT WING LEADING EDGE UPPER SURFACE STA XFS 528 HAS A 2 INCH CRACK FROM AFT EDGE OF RIVET HOLE. REPAI RED PER SRM ADDENDUM DC8-5720-7767. 2 L 7 4 4F RT 4A25 1996082900477 19960829 00477 WP 1996 8 29 UPS96820930 1 19960810 A 5320 DOUBLER DOUG DC8 DC871F 302199D WP BS 210 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE-C, LONGERON 31L FINGER DOUBLER CRACKED AT FASTENER HOLE, FS 210. REPLACED DOUBLER SECTION PER SRM 53-2- 0. 2 L 7 4 4F RT 4A25 1996082900478 19960829 00478 EU 1996 8 29 QXEA9600350 1 19960825 A 3350 1820 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 454US 11107 BOTH OVERWING EXIT LIGHTS WOULD NOT ILLUMINATE DURING NORMAL OPS. BULBS WERE REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996082900479 19960829 00479 EU 1996 8 29 QXEA9600351 1 19960825 A 3350 515800106 LIGHT FOKKER F28 F28MK1000 4990808 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 454US 11107 FORWARD EXIT LIGHT ONLY PARTIALLY ILLUMINATED. LIGHT ASSY REPLACED ABOVE FORWARD CABIN BULKHEAD, LIGHT OPS CHECKED GOOD . 2 L 7 2 4F RT A20EU 1996082900480 19960829 00480 EU 1996 8 29 QXEA9600352 1 19960825 A 3350 1820 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 802PH 11017 UPPER EVAC LIGHT AT FORWARD SERVICE/EMERGENCY DOOR IS INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996082900481 19960829 00481 EU 1996 8 29 QXEA9600353 1 19960825 A 3350 6008905 POWER SUPPLY FOKKER F28 F28MK4000 4990810 EU CARGO COMPT INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 491US 11156 UNDERWING EVAC LIGHTS ILLUMINATE WHEN AIRCRAFT POWER IS SWITCHED OFF. POWER SUPPLY IN FORWARD CARGO COMPT REPLACED AND LIGHTS OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996082900482 19960829 00482 1996 8 29 QXEA9600354 4 19960825 A 3445 TCAS FOKKER F28 F28MK1000 4990808 EU COCKPIT MALFUNCTIONED A QXEA O OTHER N FALSE WARNING CL CLIMB 1 NM 09 452US 11105 TCAS ADVISORY 'CLIMB, CLIMB, CLIMB' FOLLOWED IMMEDIATELY WITH A 'DECEND, DECEND NOW' ADVISORY. SYSTEM PLACED ON MEL 34- 16(2). 2 L 7 2 4F RT A20EU 1996082900483 19960829 00483 NM 1996 8 29 96FDEA01398 1 19960823 A 5754 6516261 BONDING JUMPER BOEING 727 72725 1384006 NM NR 2 LE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 509FE 18280 NR0349, CORROSION AT NR 2 K-FLAP I/B LOWER BONDING JUMPER ATTACH POINTS. *S/D* REMOVED AND REPLACED NR 2 K-FLAP PER FE DEX MM 27-81-1. 2 L 7 3 4F A3WE 1996082900484 19960829 00484 WP 1996 8 29 96FDEA01397 1 19960825 A 3260 LOCK SENSOR DOUG DC10 DC1030F 3023504 WP NLG MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 302FE 46801 ON T/O, NOSE GEAR WOULD NOT INDICATE UP AND LOCKED ON BOTH FRONT AND S/OS PANEL. CYCLED GEAR SEVERAL TIMES WITH NO UP A ND LOCKED INDICATION. DOWN AND LOCKED OK, COMPLIED WITH RED TABS, DUMPED LANDED. VISUALLY INSPECTED NOSE GEAR AND DOOR , NO DAMAGED NOSE LANDING GEAR AREA. JACKED NOSE GEAR, CYCLED NOSE RETRACTION CHECKS OPS NORMAL WITH BOTH PRIM AND ALT IND PER MM32-20-00, MM32-60-00. REPLACED NOSE GEAR LOCKED SENSOR LT AND RT PER MM32-60-00 AND 32-61-00 GEAR RETRACTION BOTHS PRIM AND ALT SYS NORMAL CPN 0023070. 2 L 7 3 4F RT A22WE 1996082900485 19960829 00485 NM 1996 8 29 96FDEA01401 1 19960823 A 5315 65208277 FLOOR BEAM BOEING 727 72722 1384002 NM BS 680 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 NR-0618 032, CORROSION (C53-111-01, -2) ON FLOOR BEAM STA 680 RBL 20 TO LBL 20 WL 200 FWD BAY. 2 L 7 3 4F A3WE 1996082900486 19960829 00486 NM 1996 8 29 96FDEA01402 1 19960816 A 5330 SKIN BOEING 727 727233 138408A NM BS 715 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 277 22042 CORROSION IN EXTERNAL SKIN STR 28L STA 715. REMOVED CORROSION PER SRM 53-30-3, INSTALLED DOUBLER PER SRM 53-30-3. 2 L 7 3 4F RT A3WE 1996082900487 19960829 00487 NM 1996 8 29 96FDEA01403 1 19960815 A 5330 SKIN BOEING 727 727233 138408A NM BS 715 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 277 22042 CORROSION ON SKIN I/B OF STR 28R STA 715 EXTERNAL. REMOVED CORROSION PER SRM 53-30-3 INSTALLED DOUBLER PER SRM 53-30-3. 2 L 7 3 4F RT A3WE 1996082900488 19960829 00488 NE 1996 8 29 DL757961925 2 19960819 A 7321 7791005 FUEL CONTROL 736001006 BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 ENGINE FAILED A DALA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 SO 27 648DL 716598 24372 716598 ON ENGINE START LEFT ENGINE FIRE WAS NOTED. FIRE HANDLE PULLED AND AGENT NOT DISCHARGED. REPLACED LEFT ENGINE FUEL CON TROL UNIT, LEAK CKS GOOD AND PERFORMED PFHB TEST 15. LEFT ENGINE FUEL CONTROL CKS NORMAL. ALL LT ENG PARAMETERS NORMAL . 2 L 7 2 4F 4 F RT A2NM E17NE 1996082900489 19960829 00489 NM 1996 8 29 DLM88961933 1 19960820 A 2120 AIR DISTR DOUG MD88 MD88 3023688 NM CABIN SMOKE A DALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 991DL 53343 AT FL 280 ON CLIMBOUT, CABIN SMOKE WAS OCCURING IN AFT CABIN AREA. LAV SMOKE DETECTOR WENT OFF AND VISIBLE SMOKE AND SM ELL WAS SENSED. DESCENT WAS INITATED AND SMOKE DISAPPEARED REMAINDER OF FLIGHT. A/C PACKS APPEARED NORMAL. PACK TEMP S 60F AT TIME OF INCIDENT. RT PACK TEMP WAS TURNED TO WARM UP CABIN AT TIME. CKD ENGINE AND APU FOR OIL LEAKS, NONE FO UND. ACM OIL LEVEL NORMAL. REPLACED WATER SEPARATOR BAGS, RAN PACKS WITH ENGINE AIR FOR 30 MINS, DUCT TEMP TO 140 DEG REES NO SMOKE OR SMELL. 2 L 7 2 4F RT A6WE 1996082900490 19960829 00490 NM 1996 8 29 DLM88961935 1 19960820 A 2120 DUCT 711457300 DOUG MD88 MD88 3023688 NM RT AC TRIM VLV WORN A DALA O OTHER M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 27 914DL 49545 ON CLIMBOUT AT 310 TAIL COMP OVHT LIGHT CAME ON. PLACED A/C HP BLD SWITCHES TO OFF AND LIGHT EXTINGUISHED. ON DESCENT WITH THROTTLES BACK TO IDLE CABIN CLIMBED AT 1,000 FT A MIN AND FLOW LIGHT CAME ON. FOUND RUPTURED BOOT ON DUCT JUST AB OVE RT A/C TRIM VLV. REPLACED WORN DUCT BOOTS AND CLAMPS, LK CKD SYS AT T/O PWR. 2 L 7 2 4F RT A6WE 1996082900491 19960829 00491 NE 1996 8 29 DL72S961937 2 19960821 A 7310 FUEL FILTER BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE MOIST CONTAM A DALA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SO 27 470DA 54148 20747 695292 ENGINE FLAME-OUT AT FL 370. FOUND WATER IN PUMP LINE ON FUEL CONTROL AND MOISTURE TRAP. REPLACED FUEL PUMP FILTER DUE TO CONTAMINATED WATER, OPERATIONAL CHECKS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1996082900492 19960829 00492 1996 8 29 DLM11961938 4 19960821 A 2370 VIDEO MULTIPLEX RDAA802301 DOUG MD11 MD11 3023602 NM CABIN FAILED A DALA H DEACTIVATE SYST/CIRCUITS A FLAME/FIRE CR CRUISE 1 SO 27 812DE 48601 FLAMES SHOT OUT OF VIDEO MULTIPLEX UNIT. FWD TO MCO AND PLAC 25-22-01, SYSTEM DEACTIVATED. 2 L 7 3 4F RT A22WE 1996082900493 19960829 00493 NM 1996 8 29 DL76L961939 1 19960821 A 2131 211738811 CONTROLLER BOEING 767 767332 1382001 NM COCKPIT FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 178DN 25143 AT 29,000 FT HEARD LOUD SQUEAL IN COCKPIT, ALSO CABIN DIFFERENTAL GAUGE CLOSE TO RED BAND. FLIGHT ATTENDANTS REPORTED L OUD HISS FROM 12AB AREA. NOISE QUIT WHILE DESCENDING THROUGH 18,000. SYSTEM INOP IN AUTO 2, MANUAL CONTROL WAS OK. RE TURNED TO JFK. REPLACED CONTROLLER AND SELECT PANEL, SYSTEM CHECKS NORMAL. 2 L 7 2 4F RT A1NM 1996082900494 19960829 00494 NM 1996 8 29 DL72W961942 1 19960821 A 5240 DOOR BOEING 727 7272Q8 138407W NM LT FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831L 21826 A .375 INCH VISIBLE CRACK IN UPPER HINGE CUTOUT OF LT AFT SERVICE DOOR. REPAIRED PER SRM 52-40-2 FIG 4. 2 L 7 3 4F A3WE 1996082900495 19960829 00495 NM 1996 8 29 DL72W961943 1 19960821 A 5240 DOOR BOEING 727 7272Q8 138407W NM RT FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831L 21826 RT AFT SERVICE DOOR HAS .375 INCH VISIBLE CRACK IN UPPER HINGE CUTOUT ON FWD FRAME. REPAIRED PER SRM 52-40-2 FIG 4. 2 L 7 3 4F A3WE 1996082900496 19960829 00496 NM 1996 8 29 DL72W961944 1 19960821 A 5320 WEB BOEING 727 7272Q8 138407W NM BS 1223 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831L 21826 A .25 INCH CRACK AT LIGHTENING HOLE, TORQUE BOX VERTICAL WEB STA 1223. REPAIRED PER M/M 53-11-0 PG 828. 2 L 7 3 4F A3WE 1996082900497 19960829 00497 NM 1996 8 29 DL72L961950 1 19960822 A 3350 081691 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 507DA 21309 EMER TRACK LIGHT AT ROW 25 DAMAGED AND DOES NOT ILLUMINATE. REPLACED LIGHT ASSY, OPS NORMAL. 2 L 7 3 4F A3WE 1996082900498 19960829 00498 NM 1996 8 29 DL757961953 1 19960823 A 2560 BATTERIES BOEING 757 757232 1384965 NM MEGAPHONE DISCHARGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 658DL 24420 MEGAPHONE AT 1L INOP. 2 L 7 2 4F RT A2NM 1996082900499 19960829 00499 WP 1996 8 29 DLL14961958 1 19960823 A 2432 BATTERY 158901 LKHEED 1011 1011385115 5265015 WP BATTERY COMPT FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 741DA 32151 193C1245 BATTERY CONDITION LIGHT CAME ON 3.5 HRS INTO FLT. NO AVIONIC OVERBOARD LIGHTS ON. CYCLED BATTERY CHARGER, C/B DID NOT CORRECT SITUATION. BATTERY CONDITION LIGHT WENT OUT 30 MINS AFTER IT CAME ON. BATTERY PHYSICALLY FELT WARM NOT HOT, 10 TO 15 MIN AFTER FIRST INDICATION. BATTERY CONDITION LIGHT ON A SECOND TIME 1 HR LATER. 2 L 7 3 4F A23WE 1996082900500 19960829 00500 NM 1996 8 29 DL757961967 1 19960325 A 5754 114N300280A SKIN BOEING 757 757232 1384965 NM NR 6 LE FLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 667DN 25035 L/E SKIN DAMAGED FROM 70 TO 80 INCHES FROM I/B END. REPAIRED PER SRM 57-43-01. 2 L 7 2 4F RT A2NM 1996082900501 19960829 00501 SO 1996 8 29 BIER906635 1 19960826 A 3222 AN8121 SCHRADER VALVE PIPER PA28 PA28161 7102803 SO NLG STRUT CRACKED B BIEA K NONE O OTHER IN INSP/MAINT 1 EA 21 8071S 2000 28161102 NOSE GEAR COLLAPSED, FOUND SHRADER VALVE CRACKED AT BASE OF THREADS. 1 L 7 1 3O 2A13 1996082900502 19960829 00502 WP 1996 8 29 RRXA96097 1 19960206 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 300 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 ZEE FRAME AT LONGERON 29R AND Y=300 CORRODED. REPAIRED ZEE FRAME BY DOUBLER AND FILLER REPAIR IAW REO 01815 AND TREATED AREA IAW SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996082900503 19960829 00503 WP 1996 8 29 TC8A96055 1 19960824 A 3620 FITTING DOUG DC8 DC8F55 3021928 WP PNEU MANIFOLD LOOSE A TC8A C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 23 808CK 45817 AT TAKEOFF POWER 1.87 EPR ALL ENGINE BLEEDS ON, MANIFOLD AIR PRESSURE DROPPED TO ZERO. ABORTED TAKEOFF AND RETURNED TO RAMP. FOUND LOOSE FITTING ON MANIFOLD PRESSURE INDICATOR, GROUND RAN OPS CHECK OK AS PER 36-0-0. 2 L 7 4 4F 4A25 1996082900504 19960829 00504 WP 1996 8 29 CALA9601217 1 19960823 A 2910 B-NUT DOUG DC9 DC982 3022082 WP BRAKE VALVE LOOSE A CALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 09 83873 49121 THE LT HYDRAULIC SYSTEM PRESSURE AND QUANTITY WERE LOST ON APPROACH. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A LOOSE B-NUT TO LEFT HYDRAULIC BRAKE VALVE. THE FITTING WAS TIGHTENED AND THE LEFT HYDRAULIC SYSTEM WAS SERVICE D, LEAK CHECKS WERE GOOD. 2 L 7 2 4F A6WE 1996082900505 19960829 00505 NM 1996 8 29 CALA9601218 1 19960824 A 2612 896768 FIRE DET BOEING 737 7372C0 1384488 NM APU SHORTED A CALA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SW 09 10242 20071 THE APU FIRE WARNING LIGHT AND BELL ACTIVATED ON SHORT FINAL INTO IND WITH APU START. THE APU SWITCH WAS MOVED TO OFF, BUT THE WARNING CONTINUED. THE APU FIRE BOTTLE WAS DISCHARGED, BUT THE FIRE LIGHT STAYED ON AND THE BELL WAS INTERMITTE NT. THE AIRCRAFT LANDED AT IND WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE APU MUFFLER ELEMENT WAS F OUND SHORTED. THE APU MUFFLER FIRE DETECTION ELEMENT WAS REMOVED AND REPLACED, AN OPERATIONAL CHECK WAS GOOD. IN ADDIT ION, THE APU FIRE BOTTLE WAS REMOVED AND REPLACED. 2 L 7 2 4F A16WE 1996082900506 19960829 00506 NM 1996 8 29 CALA9601219 1 19960825 A 2150 20405011 ACM BOEING 737 7373Q8 1384670 NM RT PACK LEAKING A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 09 14383 4667 4667 26312 A SOUR/MUSTY ODOR WAS OBSERVED IN THE CABIN DURING DESCENT AT 6,000 FEET. THE ODOR STOPPED AFTER LANDING. MAINTENANCE FOUND THE RT ACM LEAKING. THE RT ACM WAS REMOVED AND REPLACED IAW MM 21-51-1,. OPERATIONAL CHECKS WERE GOOD WITH NO LEA KS NOTED. 2 L 7 2 4F RT A16WE 1996082900507 19960829 00507 NM 1996 8 29 CALA9601220 1 19960826 A 2750 GIMBALS BOEING 737 7373Q8 1384670 NM TE FLAPS LACK OF LUBE A CALA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SW 09 14384 26313 WHEN FLAPS WERE SELECTED TO 30 DEGREES ON FINAL APPROACH TO SLC, THE FLAPS WOULD NOT EXTEND PAST 15 DEGREES. THE AIRCRA FT LANDED WITHOUT INCIDENT. MAINTENANCE LUBRICATED ALL FLAP JACKSCREW GIMBALS PER MM 12-22-21. THE FLAPS OPERATIONALLY CHECKED GOOD SEVERAL TIMES IAW MM 27-51-00. 2 L 7 2 4F RT A16WE 1996082900508 19960829 00508 NM 1996 8 29 CALA9601221 1 19960826 A 2910 HYD LINE BOEING 727 727232 1384082 NM B-HYD SYST CHAFED A CALA A D UNSCHED LANDING RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SW 09 45793 20647 THE AIRCRAFT LOST B-SYSTEM HYDRAULICS WHILE EN ROUTE. THE AIRCRAFT WAS RETURNED TO BDA WHERE IT LANDED WITHOUT INCIDENT . MAINTENANCE FOUND THE HYDRAULIC PRESSURE LINE FROM NR 2 B-PUMP CHAFED AT CLAMP. THE HYDRAULIC LINE WAS REPLACED. TH E HYDRAULIC SYSTEM WAS SERVICED TO FULL AND LEAK CHECKS WERE GOOD. 2 L 7 3 4F A3WE 1996082900509 19960829 00509 WP 1996 8 29 CALA9601222 1 19960730 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 427 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND BELTFRAME CRACKED IN TWO PLACES AT STA 427, LONGERON 5L. THE CRACKS WERE 3.5 LONG. THE CRACKED SECTIO N OF FRAME WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 4. 2 L 7 2 4F A6WE 1996082900510 19960829 00510 WP 1996 8 29 CALA9601223 1 19960730 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 427 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND BELTFRAME CRACKED IN TWO PLACES AT STA 427, LONGERON 5R. THE CRACKS WERE 1.5 LONG. THE CRACKED SECTIO N OF FRAME WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 4. 2 L 7 2 4F A6WE 1996082900511 19960829 00511 WP 1996 8 29 CALA9601224 1 19960730 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 446 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND BELTFRAME CRACKED IN TWO PLACES AT STA 446, LONGERON 5R. THE CRACKS WERE 2.5 LONG. THE CRACKED SECTIO N OF FRAME WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 4. 2 L 7 2 4F A6WE 1996082900512 19960829 00512 WP 1996 8 29 CALA9601225 1 19960730 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 446 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND BELTFRAME CRACKED IN TWO PLACES AT STA 446, LONGERON 5L. THE CRACKS WERE 3 LONG. THE CRACKED SECTION OF FRAME WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 4. 2 L 7 2 4F A6WE 1996082900513 19960829 00513 WP 1996 8 29 CALA9601226 1 19960729 A 5312 BULKHEAD ANGLE DOUG DC9 DC932 3022066 WP BS 598 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND A 3 INCH CRACK IN FRONT SPAR TO PRESSURE BULKHEAD ATTACH ANGLE AT STA 598, LONGERON 24R. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-0. 2 L 7 2 4F A6WE 1996082900514 19960829 00514 WP 1996 8 29 CALA9601227 1 19960729 A 5312 BULKHEAD ANGLE DOUG DC9 DC932 3022066 WP BS 598 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND A 1 INCH CRACK IN FRONT SPAR TO PRESSURE BULKHEAD ATTACH ANGLE AT STA 598, LONGERON 24L. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-0. 2 L 7 2 4F A6WE 1996082900515 19960829 00515 WP 1996 8 29 9618459878 1 19960824 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 787NC 48149 DURING LINE CHECK, FOUND CEILING EMERGENCY LIGHTS INOPERATIVE BETWEEN ROWS 20 TO 24. REPLACED BATTERIES IN POWER SUPPLY , OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996082900516 19960829 00516 WP 1996 8 29 9618469308 1 19960826 A 3350 60030451 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 311RC 48089 DURING LINE CHECK, FOUND CEILING EMERGENCY LIGHTS INOPERATIVE ROWS 10 TO 14. REPLACED EMERGENCY LIGHT POWER SUPPLY, OPE RATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996082900517 19960829 00517 WP 1996 8 29 9618479867 1 19960823 A 3350 6011779 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 776NC 47786 DURING LINE CHECK, FOUND RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY, OPERATIONAL CHE CK OK. 2 L 7 2 4F A6WE 1996082900518 19960829 00518 WP 1996 8 29 9618489903 1 19960817 A 5241 SEAL DOUG DC9 DC931 3022065 WP GALLEY SVC DR DISLODGED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 953N 47083 DURING CLIMB, THE FLIGHT CREW HEARD A LOUD SLAPPING NOISE BY THE FORWARD GALLEY SERVICE DOOR, PRESSURIZATION WAS NORMAL. RETURNED TO MSP WITHOUT FURHTER INCIDENT. FOUND THE FORWARD GALLEY SERVICE DOOR SEAL OUT OF ITS RETAINER AT THE UPPER FORWARD CORNER. DEFERRED THE REPAIR. 2 L 7 2 4F A6WE 1996082900519 19960829 00519 WP 1996 8 29 9618499903 1 19960816 A 5241 SEAL DOUG DC9 DC931 3022065 WP GALLEY SVC DR DISLODGED A NWAA A UNSCHED LANDING E VIBRATION/BUFFET TO TAKEOFF 1 GL 01 953N 47083 DURING TAKEOFF, THE FLIGHT CREW FELT VIBRATION AND HEARD A LOUD SLAPPING NOISE BY THE FORWARD GALLEY SERVICE DOOR. RETU RNED TO MSP WITHOUT FURTHER INCIDENT. FOUND THE FORWARD GALLEY SERVICE DOOR SEAL OUT OF THE RETAINER AT THE UPPER FORWA RD CORNER. REINSTALLED THE SEAL. 2 L 7 2 4F A6WE 1996082900520 19960829 00520 NM 1996 8 29 9618505509 1 19960826 A 3350 POWER SUPPLY BOEING 757 757251 1384970 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 509US 23198 DURING LINE MAINTENANCE, THE AFT SECTION OF EMERGENCY FLOOR LIGHTS WERE DIM AND PULSING. REPLACED POWER SUPPLY UNIT, OP ERATIONAL CHECK OK. 2 L 7 2 4F RT A2NM 1996082900521 19960829 00521 SO 1996 8 29 COMA9610258 1 19960823 A 2750 3472001001 CONTROL UNIT EMB 120 EMB120RT SO TE FLAPS MALFUNCTION A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 244CA 120217 FLAP CONTROL FAULT WARNING DURING TAKEOFF. REPLACED FLAP CONTROL BOX. 2 L 7 2 4T RT A31SO 1996082900522 19960829 00522 SO 1996 8 29 COMA9610259 1 19960823 A 2751 3471001001 FLAP ANNUNCIATOR EMB 120 EMB120RT SO INSTR PANEL MALFUNCTION A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 189CA 8360 432 120189 FLAP CONTROL FAULT WARNING DURING TAKEOFF. REPLACED THE FLAP ANNUNCIATOR PANEL. 2 L 7 2 4T RT A31SO 1996082900523 19960829 00523 SO 1996 8 29 COMA9610260 1 19960825 A 2460 MS2536180 CIRCUIT BREAKER EMB 120 EMB120RT SO COCKPIT DAMAGED A COMA O OTHER H ELECT. POWER LOSS-50 PC AP APPROACH 1 SO 01 152CA 120152 EMERGENCY BUS LOST POWER, CONTROL BUS INOP, RT ENGINE INSTRUMENTS INOP, COPILOTS EFIS AND COMM RADIO INOP, A LANDING GEA R INDICATION INOP. FOUND BUS BAR CONNECTION TO CIRCUIT BREAKER 0470 LOOSE WITH HEAT DAMAGE TO BREAKER. REPLACED C/B 04 70 AND ATTACHING HARDWARE. 2 L 7 2 4T RT A31SO 1996082900524 19960829 00524 EU 1996 8 29 COMA9630142 1 19960825 A 3150 004WS00 WEU SAAB SF340 SF340A 7850100 EU E/E COMPT MALFUNCTIONED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 358CA 17911 29 340A047 CONFIGURATION WARNING ACTIVATED WHEN POWER ADVANCED FOR TAKEOFF. REPLACED THE WARNING ELECTRONIC UNIT. 2 L 7 2 4T RT A52EU 1996082900525 19960829 00525 NM 1996 8 29 96FDEA01395 1 19960822 A 5313 651838739 STRINGER BOEING 727 72722 1384002 NM BS 964 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 NR0711 AND 031, WHILE WORKING ON NR0698 FOUND CORROSION ON STRINGER 30 BS 964. *S/D* REMOVED CORROSION ON SIR 30 BS 96 4, OUT OF LIMITS IAW FEDEX SRM 53-10-01. REPAIRED STRINGER IAW FEDEX SRM 53-10-03. 2 L 7 3 4F A3WE 1996082900526 19960829 00526 WP 1996 8 29 ABXA9600614 1 19960823 A 3350 60030431 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 983AX 1262 47257 EMERGENCY LIGHTS REMAIN ON WHEN AIRCRAFT POWER WAS SHUT OFF WITH EMERGENCY LIGHT SWITCH IN OFF POSITION. REPLACED EMERG ENCY LIGHT BATTERY PACK IAW DC-9 MM 33-53-0, OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996082900527 19960829 00527 WP 1996 8 29 SCNA96228 1 19960822 A 5330 SKIN DOUG DC10 DC1015 3022118 WP BS 1721- 1761 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A-CHECK INSPECTION, FIVE DIMPLES WERE NOTED IN LOCALIZED AREAS ON THE EXTERIOR OF THE FUSELAGE SKIN. THE DIMPLES ARE APPROXIMATELY 0.50 INCH IN DIAMETER AND ARE LOCATED AT STATIONS 1721, 1741, AND 1761 BETWEEN STRINGERS 45L AND 48L. INSTALLED A TIME LIMITED REPAIR. THE PERMANENT REPAIR WILL BE ACCOMPLISHED AT THE NEXT C-CHECK, PER THE DC-10 SRM, VO LUME I, 53-20-00, FIGURE 6 AND FIGURE 13 AS APPLICABLE. 2 L 7 3 4F A22WE 1996082900528 19960829 00528 WP 1996 8 29 SCNA96229 1 19960823 A 3350 EMBS1392 POWER SUPPLY DOUG DC10 DC1015 3022118 WP CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 152SY 48289 FOUND FORWARD CABIN CEILING EMERGENCY LIGHT DOES NOT COME ON WHEN SYSTEM IS ARMED AND AIRCRAFT POWER IS REMOVED. REMOV ED AND REPLACED THE FORWARD CABIN POWER SUPPLY IN ACCORDANCE WITH MM 33-51-01, SYSTEM OPS CHECKS NORMAL. 2 L 7 3 4F A22WE 1996082900529 19960829 00529 WP 1996 8 29 SCNA96230 1 19960815 A 5320 LOWER RAIL DOUG DC10 DC1010 3022110 WP BS 1709.5 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 573SC 46905 DURING INSPECTION, FOUND CENTER CARGO PIT CUT OUT LOWER RAIL UPPER SURFACE CORRODED AT BS 1709.5. BLENDED OUT CORROSION PER SABRE TECH EA DC10-53-004. 2 L 7 3 4F A22WE 1996082900530 19960829 00530 WP 1996 8 29 SCNA96231 1 19960815 A 5320 DOOR FRAME DOUG DC10 DC1010 3022110 WP BS 886 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 573SC 46905 DURING INSPECTION, FOUND FORWARD CARGO DOOR CUTOUT FRAME AT BS 885.8, FORWARD VERTICAL LEG HAS CORROSION AT APPROXIMATEL Y LONGERON 42R. REPAIRED ANGLE IN ACCORDANCE WITH SABRE TECH EA DC10-53-003. 2 L 7 3 4F A22WE 1996082900531 19960829 00531 WP 1996 8 29 SCNA96232 1 19960813 A 5320 TEE FITTING DOUG DC10 DC1010 3022110 WP CENTER CARGO CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 573SC 46905 DURING INSPECTION, FOUND CENTER CARGO PIT FORWARD LOWER CORNER TEE FITTING CORRODED. REPLACED TEE IN ACCORDANCE WITH SA BRE TECH EA DC10-53-004. 2 L 7 3 4F A22WE 1996082900532 19960829 00532 WP 1996 8 29 SCNA96233 1 19960813 A 5311 FRAME DOUG DC10 DC1010 3022110 WP CENTER CARGO CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 573SC 46905 DURING INSPECTION, FOUND CENTER CARGO COMPARTMENT LOWER FORWARD FRAME CORRODED. BLENDED OUT CORROSION IN ACCORDANCE WIT H SABRE TECH EA DC10-53-004. 2 L 7 3 4F A22WE 1996082900533 19960829 00533 WP 1996 8 29 SCNA96234 1 19960813 A 5320 FITTING DOUG DC10 DC1010 3022110 WP FWD CARGO CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 573SC 46905 DURING INSPECTION, FOUND FORWARD CARGO COMPARTMENT LOWER FORWARD CORNER FITTING CORRODED. REMOVED AND REPLACED FITTING IN ACCORDANCE WITH SABRE TECH EA DC10-53-003. 2 L 7 3 4F A22WE 1996082900534 19960829 00534 WP 1996 8 29 SCNA96235 1 19960813 A 5320 TEE FITTING DOUG DC10 DC1010 3022110 WP FWD CARGO CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 573SC 46905 DURING INSPECTION, FOUND FORWARD CARGO COMPARTMENT LOWER AFT CORNER TEE FITTING CORRODED. REMOVED AND REPLACED TEE FITT ING IN ACCORDANCE WITH SABRE TECH EA DC10-53-003. 2 L 7 3 4F A22WE 1996082900535 19960829 00535 WP 1996 8 29 SCNA96236 1 19960813 A 5320 DOOR JAMB DOUG DC10 DC1010 3022110 WP CARGO COMPT CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 573SC 46905 DURING INSPECTION, FOUND CORROSION ON FORWARD CORNER OF LOWER JAMB IN FORWARD CARGO PIT. BLENDED CORROSION IN ACCORDANCE WITH SABRE TECH EA DC10-53-003. 2 L 7 3 4F A22WE 1996082900536 19960829 00536 NM 1996 8 29 DHL96707003 1 19960822 A 2910 BACH30AT06R0250 PRESSURE LINE BOEING 727 72722 1384002 NM NLG RUPTURED A DHLA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 707DH 18321 AFTER T/O AROUND 30 MIN OUT OF IAH, AIRCRAFT SUFFERED COMPLETE FAILURE OF HYDRAULIC A-SYSTEM. TURNED BACK TO IAH. AIRC RAFT LANDED AND STOPPED AT END OF RUNWAY WAITING TO BE TOWED. RAMP FOUND NOSE GEAR HOSE BROKEN. REPLACED HOSE WITH FLE X LINE, CHECKED BOTH ENGINE HYDS FILTERS AND CASE DRAIN IN A-SYSTEM. NO CONTAMINATION FOUND. RAN ENGINE, PRESSURIZED A ND CKD SYS, OPS CKS NORMAL. 2 L 7 3 4F A3WE 1996082900537 19960829 00537 NM 1996 8 29 DHL96724005 1 19960822 A 2761 2145014 ACTUATOR BOEING 727 727228 NM NR 2 SPOILER FAILED A DHLA K NONE K FLUID LOSS LD LANDING 1 SO 01 724DH 19862 DURING APPROACH B-SYSTEM QUANTITY BEGAN TO FLUX BETWEEN .8 AND 1.3 GALLONS, ON LANDING B-PRESSURE BEGAN TO FALL. LOW PR ESSURE LIGHTS ILLUMINATED FOR AILERONS, RUDDER, ELEVATOR ON B-PUMPS. FOUND NR 1 GROUND SPOILER LEAKING. REMOVED AND RE PLACED GROUND SPOILER ACTUATOR PER MM 27-61-91. SERVICED HYD FLUID, CHECKED B-SYSTEM HYD PUMP CASE DRAIN FILTER, NO CON TAMINATION FOUND. 2 L 7 3 4F A3WE 1996082900538 19960829 00538 NM 1996 8 29 P5CA9600645 1 19960820 A 5713 STRINGER BOEING 747 747132 1384882 NM CENTER WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION CENTER WING DRY BAY UPPER SKIN STRINGER 32C AT RBL 75. REMOVED CORROSION PER BOEING SRM 51-10-01 WITH IN LIMITS PER 53-10-01 PROTECTED PER 51-10-02. 2 L 7 4 4F A20WE 1996082900539 19960829 00539 NM 1996 8 29 P5CA9600651 1 19960820 A 5713 STRINGER BOEING 747 747132 1384882 NM CENTER WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION CENTER TANK DRY-BAY UPPER SKIN STRINGER S30C AT BBL 0 TO RBL 10. REMOVED CORROSION PER BOEING SRM 51- 10-01 WITHIN LIMITS PER 53-10-01 PROTECTED PER 51-10-02. 2 L 7 4 4F A20WE 1996082900540 19960829 00540 NM 1996 8 29 P5CA9600652 1 19960826 A 5414 65B9090179 PANEL BOEING 747 747123 1384873 NM NR 3 PYLON DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 DELAMINATED NR 3 ENGINE SLOT SEAL STRUT CLOSURE PANEL, SKIN PEELED OFF. REPLACED PANEL PER BOEING MAINTENANCE MANUAL 71 -10-10. 2 L 7 4 4F A20WE 1996082900541 19960829 00541 NM 1996 8 29 P5CA9600653 1 19960819 A 5753 SKIN BOEING 747 747122 1384872 NM LT TE FORE FLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 DELAMINATE LEADING EDGE OF THE LEFT OUTBOARD TRAILING EDGE FORE FLAP BY THE OUTBOARD EDGE. REPAIRED PER BOEING SRM 51-4 0-07. 2 L 7 4 4F A20WE 1996082900542 19960829 00542 NM 1996 8 29 P5CA9600654 1 19960819 A 5753 TRACK BOEING 747 747122 1384872 NM LT TE MID FLAP WORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 WORN FORE FLAP TRACK TO LEFT OUTBOARD TRAILING EDGE MID FLAP. REPLACED TRACK PER BOEING MAINTENANCE MANUAL 27-51-04 AND 27-51-06. 2 L 7 4 4F A20WE 1996082900543 19960829 00543 NM 1996 8 29 P5CA9600655 1 19960819 A 5753 TRACK BOEING 747 747122 1384872 NM RT TE MID FLAP WORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 WORN FORE FLAP TRACK TO RIGHT OUTBOARD TRAILING EDGE MID FLAP. REPLACED TRACK PER BOEING MAINTENANCE MANUAL 27-51-04 AN D 27-51-06. 2 L 7 4 4F A20WE 1996082900544 19960829 00544 NM 1996 8 29 CALA9601228 1 19960814 A 5712 RIB BOEING 727 727232 1384082 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A 10 INCH CRACK IN OUTBOARD RIB AT NR 5 SLAT ACTUATOR ATTACH POINT. THE CRACK WAS STOP DRILLED AND A D OUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3. 2 L 7 3 4F A3WE 1996082900545 19960829 00545 NM 1996 8 29 CALA9601229 1 19960813 A 5712 RIB BOEING 727 727232 1384082 NM RT WING TIP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A 6 INCH CRACK IN FORWARD END CLOSURE RIB AND UPPER ANGLE OF RT WING TIP ASSEMBLY. THE CRACKED AREA WA S CUT OUT. REPLACEMENT PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-30-2. 2 L 7 3 4F A3WE 1996082900546 19960829 00546 NM 1996 8 29 CALA9601230 1 19960813 A 5712 RIB BOEING 727 727232 1384082 NM RT WING TIP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A 6 INCH CRACK IN FORWARD END CLOSURE RIB AND LOWER ANGLE OF RT WING TIP ASSEMBLY. THE CRACKED AREA WA S CUT OUT, REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1996082900547 19960829 00547 NM 1996 8 29 CALA9601231 1 19960813 A 5311 FRAME BOEING 727 727232 1384082 NM BS 1303 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A 1 INCH CRACK IN LEFT AND RIGHT CORNERS OF FRAME WEB ON AFT FACE OF STA 1303 FRAME, ABOVE S-DUCT. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1996082900548 19960829 00548 NM 1996 8 29 CALA9601232 1 19960813 A 5753 SKIN BOEING 727 727232 1384082 NM RT TE MID FLAP PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND RT WING INBOARD TRAILING EDGE MID FLAP PUNCTURED AT UPPER SURFACE OF TRAILING EDGE INBOARD END. THE DA MAGED AREA WAS CUT OUT AND A HOT BOND REPAIR WAS ACCOMPLISHED IAW SRM 51-40-6. 2 L 7 3 4F A3WE 1996082900549 19960829 00549 NM 1996 8 29 CALA9601233 1 19960810 A 5713 STRINGER BOEING 727 727232 1384082 NM WS 686.5 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A .5 INCH CRACK IN STRINGER INSIDE LT WING TANK AT STA 686.5. A REPAIR WAS FABRICATED AND INSTALLED IA W EA 576201050. 2 L 7 3 4F A3WE 1996082900550 19960829 00550 NM 1996 8 29 CALA9601234 1 19960810 A 5753 SKIN BOEING 727 727232 1384082 NM RT TE FLAP DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND RT WING TRAILING EDGE FLAP LOWER SKIN DELAMINATING IN TWO AREAS INBOARD OF INBOARD FAIRING. A FIBERGLA SS OVERLAY REPAIR WAS ACCOMPLISHED IAW SRM 51-40-8. 2 L 7 3 4F A3WE 1996082900551 19960829 00551 NM 1996 8 29 CALA9601235 1 19960810 A 5730 SKIN BOEING 727 727232 1384082 NM RT WING CHAFED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A HOLE CHAFED IN SKIN FORWARD OF FLUX VALVE, RT WING TIP. THE DAMAGED AREA WAS CUT OUT, A FILLER AND D OUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-20-5. 2 L 7 3 4F A3WE 1996082900552 19960829 00552 NM 1996 8 29 CALA9601236 1 19960809 A 5320 FRAME BOEING 727 727232 1384082 NM CARGO DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND AFT CARGO C-3 FORWARD DOOR FRAME CORRODED IN AREA OF STRINGER 26. THE CORROSION WAS REMOVED AND A DOUB LER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-30-2. 2 L 7 3 4F A3WE 1996082900553 19960829 00553 NM 1996 8 29 CALA9601237 1 19960808 A 5753 SKIN BOEING 727 727232 1384082 NM LT TE MID FLAP DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND THE OUTBOARD TRAILING EDGE OF LEFT OUTBOARD MID FLAP DELAMINATED. THE DELAMINATED CORE WAS CUT OUT AND A HOT BOND REPAIR WAS ACCOMPLISHED IAW SRM 51-40-6. 2 L 7 3 4F A3WE 1996082900554 19960829 00554 NM 1996 8 29 CALA9601238 1 19960808 A 5753 SKIN BOEING 727 727232 1384082 NM LT TE FORE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND LEADING EDGE OF LEFT OUTBOARD FOREFLAP SKIN CRACKED AND GALLED IN TWO PLACES AT OUTBOARD SEQUENCE CARRI AGE POSITION. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-50-4. 2 L 7 3 4F A3WE 1996082900555 19960829 00555 NM 1996 8 29 CALA9601239 1 19960808 A 5753 SKIN BOEING 727 727232 1384082 NM LT TE FORE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND OUTBOARD LEADING EDGE OF LEFT INBOARD FOREFLAP SKIN CRACKED. A DOUBLER WAS FABRICATED AND INSTALLED IA W SRM 57-50-4. 2 L 7 3 4F A3WE 1996082900556 19960829 00556 NM 1996 8 29 CALA9601240 1 19960808 A 5320 THRESHOLD BOEING 727 727232 1384082 NM BS 1178 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND CORROSION AND CRACKS ON THRESHOLD STRUCTURE BELOW CABIN FLOOR AT BS 1178, LBL 18 TO RBL 18. A NEW THRE SHOLD WAS FABRICATED AND INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996082900557 19960829 00557 NM 1996 8 29 CALA9601241 1 19960816 A 5753 SKIN BOEING 727 727232 1384082 NM LT TE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A 1.5 INCH CRACK IN LT WING INBOARD FLAP INNER SKIN AT AFT END OF OPENING FOR UPPER ACCESS PANEL NR 844 3. A NEW PART WAS FABRICATED AND INSTALLED IAW SRM 51-10-1. 2 L 7 3 4F A3WE 1996082900558 19960829 00558 NM 1996 8 29 CALA9601242 1 19960808 A 5712 RIB BOEING 727 727232 1384082 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A .25 INCH CRACK IN RIB OF NR 5 SLAT ACTUATOR ATTACH POINT INBOARD SIDE. THE CRACK WAS STOP DRILLED AN D A DOUBLER WAS INSTALLED IAW SRM 51-40-3. 2 L 7 3 4F A3WE 1996082900559 19960829 00559 NM 1996 8 29 9618512715 1 19960827 A 2750 RETRACT MECH BOEING 727 7272S7 138407Z NM RT TE AFT FLAP OUT OF ADJUST A NWAA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 GL 01 719RC 22490 DURING CRUISE, THE AIRCRAFT STARTED VIBRATING. AIRCRAFT DIVERTED TO MCO AND LANDED WITHOUT INCIDENT. ADJUSTED RIGHT IN BOARD AFT FLAP, OPERATIONAL CHECK GOOD. 2 L 7 3 4F A3WE 1996082900560 19960829 00560 WP 1996 8 29 9618529608 1 19960825 A 3260 DOOR INDICATION DOUG DC9 DC932 3022066 WP LT MLG MALFUNCTIONED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 608NW 47233 DURING APPROACH, THE LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS EXTENDED. COCKPIT OPERATING MANUAL PROCEDU RES WERE FOLLOWED AND A SUCCESSFUL LANDING WAS ACCOMPLISHED. MAINTENANCE PERSONNEL PINNED GEAR AND SECURED DOOR IN 'UP' POSITION. LANDING GEAR FUNCTIONAL TEST WAS PERFORMED ON GROUND, ALL SYSTEMS CHECKED NORMAL. DISCREPANCY COULD NOT BE DUPLICATED. LEFT MAIN GEAR DOOR WAS REPLACED DUE TO DAMAGE INCURRED ON LANDING. 2 L 7 2 4F A6WE 1996082900561 19960829 00561 WP 1996 8 29 9618539931 1 19960825 A 3230 VALVE DOUG DC9 DC931 3022065 WP LT MLG MALFUNCTIONED A NWAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 01 90S 47244 DURING APPROACH, THE LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS EXTENDED. GO-AROUND PROCEDURES WERE EXECUT ED AND GEAR WAS RECYCLED. DOOR OPEN LIGHT STAYED ON, EMERGENCY GEAR EXTENSION PROCEDURES WERE UTILIZED AND A SUCCESSFUL LANDING WAS ACCOMPLISHED ON SECOND ATTEMPT. MAINTENANCE FOUND LEFT MAIN GEAR SLOW TO RETRACT. REPLACED RESTRICTOR VAL VE, OPERATIONAL CHECK NORMAL. DOOR SKID PADS WERE REPLACED DUE TO DAMAGE INCURRED ON LANDING. 2 L 7 2 4F A6WE 1996082900562 19960829 00562 WP 1996 8 29 9618549984 1 19960823 A 3260 PROX SENSOR DOUG DC9 DC932 3022066 WP RT MLG MALFUNCTION A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 984US 47383 DURING APPROACH, THE RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS EXTENDED. RECYCLED GEAR AND NORMAL INDICATIONS WERE ACHIEVED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT MAIN GEAR DOWNLOCK PROXIM ITY SENSOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996082900563 19960829 00563 1996 8 29 9618559958 4 19960826 A 3442 20671570153 RT UNIT DOUG DC9 DC931 3022065 WP RADAR COMPT FAILED A NWAA A UNSCHED LANDING O OTHER UK UNKNOWN 1 GL 01 917RW 9326 441 47145 WEATHER RADAR SYSTEM FAILED EN ROUTE. FLIGHT DIVERTED TO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RADAR T RANSCEIVER, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996082900564 19960829 00564 WP 1996 8 29 9618569612 1 19960826 A 3260 BULB DOUG DC9 DC932 3022066 WP NLG FAILED A NWAA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 01 612NW 47436 DURING APPROACH, NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. PILOT REPLACED LIGHT BULB, CYCL ED GEAR TO 'UP' POSITION AND NOSE GEAR UNSAFE LIGHT ILLUMINATED. LOWERED GEAR AGAIN AND NORMAL INDICATIONS WERE ACHIEVE D. MAINTENANCE FOUND BULB AT NOSE GEAR UNSAFE INDICATOR BURNED OUT. REPLACED BULB, ALL INDICATIONS CHECKED NORMAL. 2 L 7 2 4F A6WE 1996082900565 19960829 00565 WP 1996 8 29 9618579953 1 19960826 A 2421 976J2526 GENERATOR DOUG DC9 DC931 3022065 WP RT ENGINE FAILED A NWAA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 GL 01 918RW 9530 756 47158 RIGHT ENGINE GENERATOR TRIPPED OFF LINE AFTER TAKEOFF. RIGHT GEN OFF LIGHT WAS ILLUMINATED. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT GENERATOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996082900566 19960829 00566 NM 1996 8 29 9618586310 1 19960827 A 3350 POWER SUPPLY BOEING 747 747451 1384940 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 670US 24225 DURING LINE CHECK, FOUND RIGHT EXTERIOR EMERGENCY LIGHTS AND FLOOR PATH EMERGENCY LIGHT AT ROWS 23, 31, 35 AND 42 INOPER ATIVE. REPLACED POWER SUPPLY AND BATTERY FOR EXTERIOR LIGHTS AND RELAMPED AND RECONNECTED LIGHT ASSEMBLIES FOR FLOOR PA TH LIGHTS, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1996082900567 19960829 00567 WP 1996 8 29 9618599601 1 19960826 A 3234 GEAR HANDLE DOUG DC9 DC932 3022066 WP COCKPIT BINDING A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 601NW 47038 LANDING GEAR HANDLE WOULD NOT RAISE AFTER TAKEOFF. ALL GEAR RED UNSAFE LIGHTS WERE ILLUMINATED. CABIN PRESSURIZED NORM ALLY, FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND DEBRIS WEDGED BETWEEN FORWARD CABLE DRUM-C AND PULLEY GUARD FS74 AND CABLE RUN 103A AND 101A. REMOVED DEBRIS AND INSPECTED CABLES AND DRUMS, ALL CHECKED NORMAL. C ONTROL LEVER OPERATED NORMALLY ON CYCLE. 2 L 7 2 4F A6WE 1996082900568 19960829 00568 EU 1996 8 29 9618603205 1 19960827 A 2810 FUEL TANK AIRBUS 320 A320211 3930320 EU LT/RT WING WATER CONTAM A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 305US 41 DURING CLIMBOUT, THE LEFT FUEL TANK NR 1 PUMP LOW PRESSURE LIGHT ILLUMINATED FOR APPROXIMATELY TWO MINUTES THEN RETURNED TO NORMAL. DUE TO NR 2 PUMP CURRENTLY ON MEL, AIRCRAFT RETURNED TO LAS AND LANDED WITHOUT INCIDENT. MAINTENANCE DRAINE D WATER FROM THE LEFT AND RIGHT FUEL TANKS, REMOVED THE NR 1 PUMP LOW PRESSURE SWITCH AND PURGED THE FUEL LINE, OPERATIO NAL CHECK OK. 2 L 7 2 4F RT A28NM 1996082900569 19960829 00569 EU 1996 8 29 QXEA9600355 1 19960826 A 3350 MGG1280 BULB GRIMES 5515800106 FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 469US 11096 CEILING EXIT SIGN AT ROW 8 PARTIALLY INOP. BULBS REPLACED AS REQUIRED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996082900570 19960829 00570 EU 1996 8 29 QXEA9600356 1 19960826 A 3397 WIRE FOKKER F28 F28MK1000 4990808 EU CABIN BROKEN A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 469US 11096 LEFT AND RIGHT UNDERWING EMERGENCY/EVAC LIGHTS INTERMITTENT. WIRE AT EVAC LIGHT REPAIRED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996082900571 19960829 00571 NM 1996 8 29 96FDEA01406 1 19960827 A 5311 6515932 FRAME BOEING 727 72725 1384006 NM BS 580 DAMAGE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 509FE 18280 NR 0357 AND 003, DAMAGE FRAME AT BS 580 RBL 18 WL 156. 2 L 7 3 4F A3WE 1996082900572 19960829 00572 NM 1996 8 29 96FDEA01407 1 19960827 A 5313 STRINGER BOEING 727 72725 1384006 NM BS 640 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 509FE 18280 NR 0451 AND 004, WHILE WORKING NR 0219 FOUND STRINGER 19 RT AT BS 640 TO BE CRACKED. 2 L 7 3 4F A3WE 1996082900573 19960829 00573 NM 1996 8 29 96FDEA01408 1 19960827 A 5320 65185385 CHORD BOEING 727 72725 1384006 NM BS 870 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 509FE 18280 NR 0544 AND 005, CORROSION BETWEEN UPPER 870 VERTICAL FLANGE OF CHORD AND 870 WEB LBL 12 TO 20. *S/D* REMOVED CORROSIO N ON VERTICAL FLANGE OF 870 CHORD FOUND TO BE WITHIN LIMITS PER FED EX SRM 57-10-1. REPAIRED 870 WEB PER FED EX SRM 57- 10-6 FIG 1. 2 L 7 3 4F A3WE 1996082900574 19960829 00574 NM 1996 8 29 96FDEA01409 1 19960827 A 5754 FLAP BOEING 727 72725 1384006 NM NR 1 LE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 509FE 45718 51518 18280 NR 0441 AND 006, CORROSION AT NR 1 K-FLAP. 2 L 7 3 4F A3WE 1996082900575 19960829 00575 WP 1996 8 29 MWEA96420 1 19960824 A 5330 SKIN DOUG DC9 DC915 3022036 WP BS 780 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 DURING C-CK, FOUND CRACK IN FUSELAGE SKIN LT SIDE STA 780 JUST BELOW PYLON. CRACK IS APPROX 1 INCH LENGTH. INSTALLED R EPAIR IAW SRM 53-04, FIG 17. 2 L 7 2 4F A6WE 1996082900576 19960829 00576 WP 1996 8 29 MWEA96421 1 19960827 A 3350 6011777 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 501ME 47132 DURING B-CK, FOUND LT ENGINE NACELLE LIGHT WOULD NOT ILLUMINATE DURING EMERGENCY LIGHT TEST. NACELLE LIGHTS WOULD NOT E XTINGUISH WHEN EMERGENCY LIGHTS TURNED OFF. REPLACED BOTH BATTERY POWER SUPPLIES, OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996082900577 19960829 00577 NM 1996 8 29 P5CA9600656 1 19960805 A 5320 SUPPORT BOEING 747 747121 1384871 NM BS 1580 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FOUND LEVEL ONE CORROSION ON FAIRING SUPPORT AT LOWER FS 1580 BETWEEN AREA RBL 100 TO LBL 100. REMOVED CORROSION IAW SR M 51-10-01. FOUND WITHIN THE LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996082900578 19960829 00578 NM 1996 8 29 P5CA9600657 1 19960805 A 5320 SUPPORT BOEING 747 747121 1384871 NM BS 1480 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FOUND LEVEL ONE CORROSION ON CENTER FAIRING SUPPORT AT LOWER FUSELAGE BETWEEN STATIONS 1480 TO 1660. REMOVED CORROSION IAW SRM 51-10-01 AND INSTALLED NEW ANCHOR NUT IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996082900579 19960829 00579 NM 1996 8 29 P5CA9600658 1 19960805 A 5320 SUPPORT BOEING 747 747121 1384871 NM BS 1580 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FOUND LEVEL ONE CORROSION ON FAIRING SUPPORT AT FUSELAGE LT SIDE STAION 1580 BETWEEN STR AREA 29 TO 40. REMOVED CORROSI ON IAW SRM 51-10-01 AND INSTALLED NEW ANCHOR NUT IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996082900580 19960829 00580 NM 1996 8 29 P5CA9600659 1 19960805 A 5320 SUPPORT BOEING 747 747121 1384871 NM BS 1540 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FOUND LEVEL ONE CORROSION ON FAIRING SUPPORT AT FUSELAGE LT SIDE STATION 1540 BETWEEN STR AREA 28 TO 37. REMOVED CORROS ION IAW SRM 51-10-01 AND INSTALLED NEW ANCHOR NUT IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996082900581 19960829 00581 NM 1996 8 29 P5CA9600660 1 19960805 A 5320 SUPPORT BOEING 747 747121 1384871 NM BS 1540 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FOUND LEVEL ONE CORROSION ON FAIRING SUPPORT AT FS RT SIDE STA 1540 BETWEEN STR AREA 33 TO 36. REMOVED CORROSION IAW SR M 51-10-01. FOUND WITHIN LIMITS OF SRM 53-10-01. 2 L 7 4 4F A20WE 1996082900582 19960829 00582 NM 1996 8 29 P5CA9600661 1 19960805 A 5320 BRACKET BOEING 747 747121 1384871 NM BS 920-960 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FOUND LEVEL ONE CORROSION ON SUPPORT BRACKET AT CENTER LOWER FUSELAGE BETWEEN STA 920 TO 960. REMOVED CORROSION AND TRE ATED AREA IAW SRM 51-10-01. REPAIRED IAW SRM 51-40-03. 2 L 7 4 4F A20WE 1996082900583 19960829 00583 NM 1996 8 29 P5CA9600662 1 19960805 A 5330 SKIN BOEING 747 747121 1384871 NM BS 1700 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FOUND LEVEL ONE CORROSION AND PROTRUDING HI-LOCK ON FUSELAGE SKIN RT SIDE AT STR 40 AREA STA 1700. REMOVED CORROSION FR OM SKIN IAW SRM 51-10-01. INSTALLED NEW HI-LOCK AND RIVET IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996082900584 19960829 00584 NM 1996 8 29 P5CA9600663 1 19960805 A 5320 BRACKET BOEING 747 747121 1384871 NM BS 1660 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FOUND LEVEL ONE CORROSION ON BRACKET AND AROUND GROUNDING BOLT AT FAIRING SUPPORT, FUSELAGE RT SIDE STA 1660, BETWEEN ST R 44 TO 45. REMOVED CORROSION IAW SRM 51-10-01, INSTALLED HI-LOCK IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996082900585 19960829 00585 NM 1996 8 29 P5CA9600664 1 19960805 A 5320 SUPPORT BOEING 747 747121 1384871 NM BS 880 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FOUND LEVEL 2 CORROSION ON FAIRING SUPPORT AT LOWER FUS STA 880 BETWEEN BL 0 TO LBL 15. REPAIRED IAW SRM 53-50-04. CP CP BASE LINE INSPECTION. 2 L 7 4 4F A20WE 1996082900586 19960829 00586 NM 1996 8 29 P5CA9600665 1 19960805 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1920 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FOUND LEVEL ONE CORROSION ON STRINGER 47 NEAR STATION 1920 RT SIDE. REMOVED CORROSION AND TREATED AREA IAW SRM 51-10-01 . 2 L 7 4 4F A20WE 1996082900587 19960829 00587 NM 1996 8 29 ASAA9640056 1 19960703 A 3397 WIRE BOEING 737 7374S3 1384711 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 786AS 24795 SEA - DURING MAINTENANCE CHECK, FOUR EMERGENCY EXIT FLOOR TRACK LIGHTS IN MID-CABIN AND THREE AFT EMERGENCY EXIT FLOOR T RACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED LOOSE WIRING AND ALL LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1996082900588 19960829 00588 NM 1996 8 29 ASAA9640057 1 19960704 A 3350 8100022601 LIGHT BOEING 737 7374S3 1384711 NM CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 786AS 24795 SEA - DURING MAINTENANCE CHECK, THE AFT THREE EMERGENCY EXIT FLOOR TRACKS LIGHTS WERE FOUND INOPERATIVE. REPLACED AFT F LOOR LIGHT ASSEMBLIES AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1996082900589 19960829 00589 NM 1996 8 29 W8PA960061 1 19960721 A 3350 323975 CONNECTOR BOEING 737 7373Q8 1384670 NM CABIN DAMAGED A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 956WP 24299 DURING A-1 CHECK, FOUND FLOOR TRACK EMERGENCY EXIT LIGHTING INOPERATIVE. REPLACED WIRE CONNECTOR. (X) 2 L 7 2 4F RT A16WE 1996082900590 19960829 00590 NM 1996 8 29 W8PA960058 1 19960717 A 3350 BULB BOEING 737 7373Q8 1384670 NM CABIN FAILED A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 956WP 24299 DURING SERVICE CHECK FOUND FLOOR TRACK EMERGENCY EXIT LIGHTING INOPERATIVE AT ROW 14. RELAMPED LIGHT ASSEMBLY AT ROW 14 . (X) 2 L 7 2 4F RT A16WE 1996082900591 19960829 00591 NM 1996 8 29 W8PA960059 1 19960717 A 3350 CONNECTOR BOEING 737 7373Q8 1384670 NM CABIN DISCONNECTED A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 956WP 24299 DURING SERVICE CHECK FOUND FLOOR TRACK EMERGENCY EXIT LIGHTING INOPERATIVE BETWEEN ROWS 19 AND 20. RECONNECTED LIGHT PL UG BETWEEN ROWS 19 AND 20. (X) 2 L 7 2 4F RT A16WE 1996082900592 19960829 00592 EA 1996 8 29 GLBA96127 2 19960628 A 7530 EVA TUBING BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA RIGHT DAMAGED A GLBA O OTHER J WARNING INDICATION CR CRUISE 1 CE 01 104GL UC104 SPI - RIGHT BLEED AIR FAIL ANNUNCIATOR ILLUMINATED IN-FLIGHT. MAINTENANCE REPLACED A SECTION OF EVA TUBING. (X) 2 L 7 2 4T 4 T RT A24CE E4EA 1996082900593 19960829 00593 WP 1996 8 29 ASAA9680144 1 19960702 A 5210 GUIDE ROD DOUG DC9 DC983 3022083 WP L2 DOOR LACK OF LUBE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 324 53471 SJC - PRIOR TO DEPARTURE OF FLIGHT 455, CREW REPORTED THE L2 DOOR WOULD NOT OPEN FROM INSIDE OR OUTSIDE. CLEANED AND LU BED L2 DOOR LOWER GUIDE ROD AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 1996082900594 19960829 00594 NM 1996 8 29 W8PA960060 1 19960721 A 3350 20121 BATTERY PACK BOEING 737 7373Y0 1384671 NM CABIN DISCHARGED A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 955WP 9988 24463 FOUND VARIOUS AISLE PATH LIGHTING ASSEMBLIES INOPERATIVE. REPLACED RIGHT AFT BATTERYY PACK ASSEMBLY. (X) 2 L 7 2 4F RT A16WE 1996082900595 19960829 00595 WP 1996 8 29 AALA961052 1 19960711 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 249AA 49269 DFW - DURING OVERNIGHT CHECK, FOUND AFT COACH SECTION EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. REPLACED AFT COACH SECTION EMERGENCY EXIT FLOOR LIGHT STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1996082900596 19960829 00596 NM 1996 8 29 96ZZZX4179 1 19960722 A 2731 69416413 BRACKET BOEING 737 7372E1 138448F NM LT ELEV TAB WORN A ZZDA O OTHER E VIBRATION/BUFFET CR CRUISE 1 SO 15 461AT 580 20976 TYS/MCO - FLT 621 - FLIGHT CREW REPORTED NR 2 ENGINE VIBRATION DURING FLIGHT. TROUBLESHOT ENGINE AND FOUND NO DISCREPAN CIES. DURING TEST FLIGHT, MAINTENANCE FOUND THAT VIBRATION ORIGINATED AT AFT FUSELAGE. INSPECTION REVEALED THAT LEFT E LEVATOR TRIM TAB HAD EXCESSIVE PLAY. THIS DISCREPANCY IS ADDRESSED IN AD 76-11-05. RECORDS RESEARCH REVEALED THAT AD H AD BEEN TERMINATED IN 1979. FOUND WORN BRACKET AND MISSING INNER HINGE BOLT AND NUT. REPLACED BRACKET AND HARDWARE. P OST-MAINTENANCE FUNCTIONAL CHECK WAS NORMAL. SUBSEQUENT TEST FLIGHT REVEALED ALL SYSTEMS NORMAL. PLACED AIRCRAFT BACK IN SERVICE. (X) 2 L 7 2 4F A16WE 1996082900597 19960829 00597 CE 1996 8 29 96ZZZX4180 1 19960720 A 3260 1143610443 SQUAT SWITCH BEECH 1900 1900C 1154161 CE RT MLG FAILED A GUUA O OTHER J WARNING INDICATION CL CLIMB 1 SO 19 190GA UB1 EYW/MIA - FLT 487 - PILOT REPORT: LANDING GEAR DOWNLOCK RELEASE DOES NOT RELEASE WITH WEIGHT OFF OF WHEELS (MUST MANUAL LY OVERRIDE SWITCH TO RAISE GEAR). REMOVED AND REPLACED RIGHT SQUAT SWITCH. (X) 2 L 7 2 4T RT A24CE 1996082900598 19960829 00598 NM 1996 8 29 USAABB96019 1 19960714 A 3350 LIGHT BOEING 757 7572B7 1384964 NM CABIN MALFUNCTIONED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 629AU 27807 PIT - EMERGENCY LIGHTS FLASH ON AND OFF. ACCOMPLISHED BITE. NO PROBLEMS FOUND. (X) 2 L 7 2 4F RT A2NM 1996082900599 19960829 00599 SO 1996 8 29 EW7A379W 1 19960808 A 5610 159SCE10011 WINDSHIELD GULSTM G1159 G1159B 3953535 SO LT COCKPIT CRACKED A EW7A A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS M OVER TEMP CR CRUISE 1 EA 11 512VB 7512 189 PILOT NOTICED INTERIM WINDOW HEATING WIRES GLOWING AND OVERHEATING. APPROXIMATELY 10 SECONDS AFTER TURNING HEAT OFF, TH E OUTER GLASS PANE CRACKED FROM SHOCK COOLING. 2 L 7 2 4F RT A12EA 1996082900600 19960829 00600 WP 1996 8 29 96ZZZX4181 2 19960715 A 7321 307080024 FUEL CONTROL AMD FALC20 FALCON20C5 2730107 EU GARRTT TFE731 TFE7315R 01518 WP RT ENGINE FAILED A WJCA A UNSCHED LANDING J R WARNING INDICATION PARTIAL RPM/PWR LOSS CL CLIMB 1 EA 11 32PB 3029 A9306C 122 P98168 AFTER TAKEOFF AND GEAR RETRACTION, RT ENGINE ROLLED BACK AND WAS UNRESPONSIVE TO THE THROTTLE, C/W ABNORMAL CHECK LIST A ND LANDED AT PSM. AIRCRAFT LANDED WITHOUT INCIDENT. CYCLES, 2,388. (X) 2 L 7 2 4F 4 F RT A7EU E6WE 1996082900601 19960829 00601 WP 1996 8 29 GAIA9623A 1 19960712 A 2422 F4510C INVERTER CVAC 440 440 2422902 WP LEFT FAILED A GAIA A G UNSCHED LANDING O2 MASK DEPLOYED B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 587CA 2021 463 YIP/OKC - FLT 587 - TWENTY NM FROM COLUMBIA, MISSOURI, THE ACFT FDR AND GPWS WARNING LIGHTS ILLUMINATED. ABOUT TEN SECO NDS LATER, THE FLIGHT CREW NOTED SMOKE IN THE COCKPIT. THE FLIGHT CREW FOLLOWED EMERGENCY PROCEDURES, NOTIFIED ATC, DE CLARED AN EMERGENCY AND MADE AN UNEVENTFUL LANDING IN COLUMBIA, MO. INSPECTION FOUND THE LT MAIN INVERTER, SN 566, PN F 45-10C, HAD HAD AN INTERNAL FAILURE, EMITTING SMOKE. REMOVED AND REPLACED INVERTER. NO OTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4R 6A6 1996082900602 19960829 00602 1996 8 29 96ZZZX4182 4 19960724 A 6113 JR28305 SPINNER GULSTM G1159 GIV 3980115 SO LP FAN HUB TIP SEPARATED A YNOA K NONE O OTHER IN INSP/MAINT 1 EA 11 917W 3 1158 POST-FLIGHT INSPECTION REVEALED RUBBER TIP OF SPINNER, PN JR28305, WAS MISSING AND DAMAGE TO THE ENGINE CASE ACOUSTICAL LINING. SUSPECT RUBBER TIP HAD SEPARATED DUE TO INSUFFICIENT BONDING TO SPINNER. RECOMMENDED BETTER ADHESIVE OR BETTER BONDING PROCESS. ACOUSTICAL LINING WAS REPAIRED AND AN OVERHAULED SPINNER WAS INSTALLED. AIRCRAFT WAS OPERATIONALLY C HECKED AND RETURNED TO SERVICE. 2 L 7 2 4F RT A12EA 1996082900603 19960829 00603 NM 1996 8 29 AWXA960295 1 19960628 A 2782 654465116 ACTUATOR BOEING 737 737275 1384485 NM NR 3 LE FLAP MALFUNCTIONED A AWXA O OTHER F FLT CONT AFFECTED CL CLIMB 1 WP 28 CGBPW 56337 1112 20958 TUS - FLT 2606 - UNCOMMMANDED ROLL EXPERIENCED ON CLIMB-OUT OF TUSCON, CAUSED BY YAW DAMPER. YAW DAMPER COUPLER FAILS S TEP 4 OF BITE, NEW COUPLER NO HELP. INSTALLED MEL 22-03. YAW DAMPER BITE CHECK GOOD AT THIS TIME PER MM 22-11-00, PAGE S 543, 544. MEL 22-03 CLEARED. FOUND NR 3 SLAT ACTUATOR TO BE INTERNALLY BYPASSING. REMOVED AND REPLACED NR 3 SLAT. F OUND NR 2 SLAT TO HAVE 6 INCHES OF DELAMINATION ON INBD SIDE UPPER T/E. REMOVED AND REPLACED NR 2 SLAT. CYCLES, 35,170 . (X) 2 L 7 2 4F A16WE 1996082900606 19960829 00606 GL 1996 8 29 96ZZZX4185 1 19960607 A 6230 2816119 SWASHPLATE YOKE ENSTRM F28 F28F 3300412 GL M/R CRACKED A PP0M K NONE O OTHER IN INSP/MAINT 1 WP 01 890JR 4393 1189488H 764 CRACKS FOUND BETWEEN CONTROL ROD AND UNIVERSAL YOKES. CRACK RUNS DOWN THE WEB BETWEEN BOTH AT 2 LOCATIONS. THIS IS SEC OND FOUND THIS MONTH. THE OTHER CRACKED SWASHPLATE IS S/N 11-897-88H WITH SIMILAR TIME IN SERVICE. CRACKED SWASHPLATE YOKE REMOVED FROM SERVICE. NEW YOKE PURCHASED AND INSTALLED. 1 G 7 1 3O H1CE 1996082900607 19960829 00607 EU 1996 8 29 96ZZZX4186 1 19960604 A 5412 2600ISW FASTENER BOLKMS 105 BO105S 5626006 EU ENGINE FIREWALL FAILED A A EOPA E A ENGINE SHUTDOWN UNSCHED LANDING C F.O.D. CR CRUISE 1 AL 01 494HL S813 DZUS FASTENER FOR ENGINE FIREWALL FAILED CAUSING FOD DAMAGE TO NR 2 ENGINE. ENGINE WAS SHUT DOWN IN-FLIGHT. AIRCRAFT L ANDED SAFELY. REPLACED NR 2 ENGINE DUE TO DAMAGE TO COMPRESSOR AND TURBINE DAMAGE. 1 G 7 2 3U H3EU 1996082900608 19960829 00608 SO 1996 8 29 WTAA960152 1 19960724 A 2121 EVAC523C2 GASPER FAN EMB 120 EMB120RT SO CABIN FAILED A WTAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 17 120AM 120012 FAT - ELECTRICAL ODOR REPORTED IN CABIN AND COCKPIT ON GROUND. MAINTENANCE INSPECTED AIRCRAFT. DETERMINED SOURCE TO BE CABIN GASPER FAN. DEFERRED PER MEL 21-24-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL WITH REPLACEMENT OF GASPER FAN. (X) 2 L 7 2 4T RT A31SO 1996082900609 19960829 00609 EU 1996 8 29 WTAA960153 1 19960724 A 3240 AC69594 MAXARET BAG JETSTM JETSTM3101 1500215 EU RT MLG FAILED A WTAA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 17 107XV 723 SFO - RIGHT BRAKE REPORTED INOPERATIVE DURING TAXI OUT. MAINTENANCE REPLACED RIGHT BRAKE MAXARET. SYSTEM OPERATIONAL C HECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A21EU 1996082900610 19960829 00610 EU 1996 8 29 WTAA960154 1 19960730 A 5730 SKIN BAG JETSTM JETSTM3201 1500217 EU LT WING BIRD STRIKE A WTAA O OTHER C F.O.D. CR CRUISE 1 WP 17 491UE 911 SFO - BIRD STRIKE ON LEADING EDGE OF LEFT WING INBOARD OF ENGINE REPORTED. MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECT ION. DAMAGE TO LEFT WING INBOARD OF ENGINE NOTED. MAINTENANCE REPAIRED DAMAGE IAW J3101 SRM. AIRCRAFT RETURNED TO SER VICE. (X) 2 L 7 2 4T RT A56EU 1996082900611 19960829 00611 SO 1996 8 29 WTAA960155 1 19960801 A 2731 922AA2YA6PZ722 PROX SENSOR EMB 120 EMB120RT SO LT WING FAILED A WTAA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 WP 17 275UE 120058 SFO - TRIM WARNING REPORTED ON TAKEOFF WITH TRIM IN THE GREEN. MAINTENANCE INSTALLED SERVICEABLE PROXIMITY SENSOR ON LE FT TRIM TAB. SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1996082900612 19960829 00612 EU 1996 8 29 WTAA960158 1 19960804 A 3234 8662B SELECTOR VALVE BAG JETSTM JETSTM3101 1500215 EU NLG FAILED A WTAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 17 418UE 780 STS - NOSE LANDING GEAR RED 'UNSAFE' LIGHT CAME ON AFTER SHUT DOWN. MAINTENANCE REPLACED LANDING GEAR HYDRAULIC SELECTO R VALVE. SYSTEM OPERATIONAL CHECK NORMAL DURING GEAR RETRACTION CHECK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A21EU 1996082900613 19960829 00613 WP 1996 8 29 96036123002 1 19960502 A 5210 57503000 DRIVE MECHANISM DOUG DC10 DC1030 3023501 WP L1 DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 230NW 46552 L1 DOOR MANUAL OPEN/CLOSE RECEPTACLE CRACKED. REMOVED AND REPLACED L1 DOOR MANUAL DRIVE MECHANISM IAW MM 52-11-05. OPS CHECKED GOOD. (MAINTENANCE ACCOMPLISHED BY LOCKHEED MARTIN AIRCRAFT CENTER, ZJ4R702M. (X) 2 L 7 3 4F A22WE 1996082900614 19960829 00614 WP 1996 8 29 96037122820 1 19960506 A 2722 11272290002 ACTUATOR DOUG DC10 DC1030 3023501 WP RUDDER FAILED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 228NW 75849 20309 46578 DURING CHECK, UPPER YAW DAMPENER FAILED SYSTEM NR 2 TEST ON FLIGHT GUIDANCE MANAGEMENT ASSESSMENT PANEL. TROUBLESHOT FO UND B-CHANNEL YAW RATE GYRO INOP. ALSO, FOUND RESISTANCE OF A AND B ON LVDT IS LOWER THAN NORMAL. REMOVED AND REPLACED RATE GYRO. REMOVED AND REPLACED UPPER FORWARD RUDDER ACTUATOR IAW MM 27-30-00. MAINTENANCE ACCOMPLISHED BY LOCKHEED M ARTIN AIRCRAFT CENTER. REFERENCE: OPERATOR CONTROL NR 96ZZZX4187, ZJ4R702M. (X) 2 L 7 3 4F A22WE 1996082900615 19960829 00615 1996 8 29 96ZZZX4187 4 19960506 A 2210 14641066 RATE GYRO DOUG DC10 DC1030 3023501 WP UPPER YAW DAMPER FAILED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 228NW 75849 20309 46578 DURING CHECK, UPPER YAW DAMPENER FAILED SYSTEM NR 2 TEST ON FLIGHT GUIDANCE MANAGEMENT ASSESSMENT PANEL. TROUBLESHOT FO UND B-CHANNEL YAW RATE GYRO INOP. ALSO, FOUND RESISTANCE OF A AND B ON LVDT IS LOWER THAN NORMAL. REMOVED AND REPLACED RATE GYRO. REMOVED AND REPLACED UPPER FORWARD RUDDER ACTUATOR IAW MM 27-30-00. MAINTENANCE ACCOMPLISHED BY LOCKHEED M ARTIN AIRCRAFT CENTER, ZJ4R702M. REFERENCE: OPERATOR CONTROL NR 96037-1228-20. 2 L 7 3 4F A22WE 1996082900616 19960829 00616 WP 1996 8 29 96ZZZX4188 1 19960625 A 5753 9957580 SKIN DOUG DC9 DC932 3022066 WP LT TE FLAP WORN A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 906VJ 68239 47379 DURING MAINTENANCE, LT INBD FLAP T/E INBD CHAFE STRIP AND SKIN NEXT TO CHAFE STRIP HAS APPROXIMATELY 12 INCH AREA CHAFED . COMPLIED WITH LMAC E.O. 3822 BY CUTTING OUT DAMAGE SECTION OF FLAP INBD WEDGE SKIN AND SPLICED IN NEW SECTION IAW LMA C E.O. 3822, AND 8110-3 DATED 14 JUN 96. REFERENCE: OPERATOR CONTROL NR 96041906VJ02. MAINTENANCE ACCOMPLISHED BY LOC KHEED MARTIN AIRCRAFT CENTER, ZJ4R702M. (X) 2 L 7 2 4F A6WE 1996082900617 19960829 00617 WP 1996 8 29 96ZZZX4189 1 19960612 A 2450 POWER RELAYS DOUG DC9 DC931 3022065 WP ELECT PANEL MISINSTALLED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 931ML 47202 DURING MAINTENANCE, L-1 ELECTRICAL PANEL (EPC PWR CTR), THE LOWER POWER RELAYS WERE FOUND TO HAVE MASKING TAPE ON CABLES NEAR TERMINAL ENDS. ALSO, FOUND TAPE ON SOME OTHER ELECTRICAL COMPONENTS IN AREA. REMOVED TAPE. NO FURTHER MAINTENAN CE REQUIRED. REFERENCE: OPERATOR CONTROL NR 96039-931ML-02. MAINTENANCE ACCOMPLISHED BY LOCKHEED MARTIN AIRCRAFT CENT ER, ZJ4R702M. 2 L 7 2 4F A6WE 1996082900618 19960829 00618 1996 8 29 96ZZZX4190 4 19960612 A 3451 5222702053 DME TRANSCEIVER DOUG DC9 DC931 3022065 WP E E COMPARTMENT INOPERATIVE A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 931ML 7874 47202 DURING MAINTENANCE, DMI CIRCUIT BREAKER CONTINUED TO TRIP. REMOVED TRANSCEIVER TO TROUBLESHOOT AND FOUND METALLIC TAPE OVER ENTIRE FACE OF CONNECTOR PINS. INSTALLED NEW TRANSCEIVER. OPS CHECKS GOOD. REFERENCE: OPERATOR CONTROL NR 96038 -931ML-01, ZJ4R702M. (X) 2 L 7 2 4F A6WE 1996082900619 19960829 00619 WP 1996 8 29 96ZZZX4191 1 19960725 A 2400 ELECT CONDUIT DOUG DC9 DC932 3022066 WP LT MLG WW CHAFED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 906VJ 68239 47379 DURING MAINTENANCE WHILE VERIFYING FLAP FOLLOW-UP CABLES FOR PROPER INSTALLATION PER FLEET CAMPAIGN 2296, FOUND LT AILER ON 'UP' CABLE NR 35 IN LT WELL CHAFING THROUGH ELECTRICAL CONDUIT APPROXIMATELY ONE INCH LONG BY .1875 INCH DEEP. REMOV ED AND REPLACED CONDUIT, REMOVED, REPAIRED AND REINSTALLED WIRING. SYSTEMS OPS CHECKED GOOD, CABLES CHANGED. REFERENCE : OPERATOR CONTROL NR 96040-906VJ-01, ZJ4R702M. (X) 2 L 7 2 4F A6WE 1996082900620 19960829 00620 WP 1996 8 29 HAL96103 1 19960729 A 3231 UPLATCH ROLLERS DOUG DC9 DC951 3022051 WP MLG DOORS WORN A HALA K NONE J WARNING INDICATION CR CRUISE 1 WP 13 601AP 47658 HNL - FLT 381 - GEAR DOOR OPEN LIGHT CAME ON IN-FLIGHT. PLACED HYDRAULIC PUMPS TO HIGH AND LIGHT WENT OUT. OCCURRED 3 TIMES. REMOVED AND REPLACED BOTH UPLATCH ROLLERS, LT AND RT GEAR DOORS. TIGHTENED HOOK GUARD, LT MLG. (X) 2 L 7 2 4F A6WE 1996082900621 19960829 00621 WP 1996 8 29 HAL96104 1 19960731 A 2780 5920257513AH DRIVE MECHANISM DOUG DC9 DC951 3022051 WP LT WING WORN A HALA K NONE F FLT CONT AFFECTED NR NOT REPORTED 1 WP 13 673MC 47726 HNL - FLT 121 - LT SLAT DISAGREEMENT LIGHT ILLUMINATED DURING SLAT EXTENSION ACCOMPANIED BY AN ADVERSE ROLL TO THE RIGHT . FOUND LT WING SLAT BELLCRANK LOWER ACTUATOR EYE BOLT MOUNT HOLE DAMAGED AND LT WING SLAT BELLCRANK HUCK BOLT SHEARED. (X) 2 L 7 2 4F A6WE 1996082900622 19960829 00622 WP 1996 8 29 HAL96106 1 19960808 A 2150 PACK DOUG DC9 DC951 3022051 WP LEFT SMOKING A HALA K NONE O OTHER TX TAXI/GRND HDL 1 WP 13 669HA 47654 HNL - FLT 102 - CABIN STARTED FILLING WITH SMOKE FROM A/C. SHUT DOWN PACK. LT PACK TEMP WAS TURNED HOT. RETURNED SW. OPS CHECK OK. (X) 2 L 7 2 4F A6WE 1996082900623 19960829 00623 WP 1996 8 29 HAL96108 1 19960808 A 3232 39567851 ACTUATOR DOUG DC9 DC951 3022051 WP NLG DOOR FAILED A HALA O OTHER E VIBRATION/BUFFET CL CLIMB 1 WP 13 699HA EFS19201 47763 HNL - FLT 504 - AFTER TAKEOFF AND GEAR UP, NOSE GEAR AREA HAD A LOUD VIBRATION. CYCLED GEAR WITH NO CHANGE. SUSPECT GE AR DOOR NOT CLOSING. REMOVED AND REPLACED RT NOSE GEAR DOOR ACTUATOR PER MM 32-22-1. OPS AND GEAR SWING OK. (X) 2 L 7 2 4F A6WE 1996082900624 19960829 00624 WP 1996 8 29 CAL960619 1 19960515 A 3230 39140165505 DNLOCK ACTUATOR DOUG DC10 DC1030 3023501 WP LT MLG FAILED A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 14074 4159 46911 MAN - FLT 9891 - THE CENTER GEAR WARNING LIGHT REMAINED ILLUMINATED FOR 2 MINUTES AFTER GEAR HANDLE HAD BEEN PLACED IN T HE 'UP' POSITION ON TAKEOFF FROM MAN. IT THEN EXTINGUISHED. GEAR WAS CYCLED AND EXTENSION OF LT MLG WAS ROUGH. CENTER GEAR DID NOT EXTEND UNTIL USE OF ALTERNATE GEAR EXTENSION. ACFT RETURNED TO MAN WHERE IT LANDED WITHOUT INCIDENT. MAI NTENANCE FND THE CLG ISOLATION SWITCH IN 'UP' POSITION. SWITCH WAS RESET. WHEN LANDING GEAR WERE SWUNG, ALL BUT LT MLG RETRACTED NORMALLY. MAINTENANCE FND LT MLG DOWNLOCK ACTUATOR BUNGEE SHEARED. ACTUATOR WAS REPLACED. DOWNLOCK TARGET AND HARNESS WERE REPLACED DUE TO DAMAGE. RESTRICTOR VALVE WAS REPLACED DUE TO BEING STUCK OPEN. GEAR OPERATION CHECKED 2 L 7 3 4F A22WE 1996082900625 19960829 00625 1996 8 29 Y2PA96061 4 19960731 A 3414 B020081129 PITOT TUBE AMD FALC20 FALCON 2720302 EU RT COCKPIT BLOCKED A Y2PA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 23 819AA 1630 26 ELP - FLT 17945 - TAKEOFF ABORTED, NO EMERGENCY PROCEDURES NECESSARY. THIS IS A REPEAT INSTANCE OF PREVIOUS DIFFICULTY REPORTED ON MISR Y2PA-96-052, DATED 7-30-96. REPLACED COPILOT'S AIRSPEED INDICATOR. CHECKED SYSTEM PER FALCON MM 34-10 -1. ALSO CHECKED MACH OVERSPEED WARNING SYSTEM IAW FALCON MM 34-10-4 WITH NO DEFECTS NOTED. ACFT ATTEMPTED DEPARTURE O N 8-1-96 AND REPORTED COPILOT'S AIRSPEED INDICATOR STUCK AT VARIOUS AIRSPEEDS. PROVIDED ERRONEOUS INDICATIONS. ACFT RE TURNED TO ELP. NO EMERGENCY PROCEDURES NECESSARY. MAINTENANCE FOUND A RESTRICTION IN THE COPILOT'S PITOT TUBE. RESTRI CTION WAS BLOWN OUT WITH NITROGEN. TESTED PITOT SYSTEM IAW FALCON MM 34-10-1 AND C/W PITOT/STATIC LEAK TEST IAW FAR 91- 2 L 7 2 4F A7EU 1996082900626 19960829 00626 EU 1996 8 29 Y2PA96063 1 19960806 A 5230 MY2029540815 DOOR HANDLE AMD FALC20 FALCOND 2720304 EU CARGO DOOR FAILED A Y2PA K NONE O OTHER IN INSP/MAINT 1 GL 23 821AA 203 BTL - FLT 18140 - INTERIOR DOOR HANDLE BROKE WHEN CREW MEMBER TRIED TO CLOSE AND LOCK THE CARGO/CREW DOOR. THERE WAS NO REPORT THAT EXCESSIVE FORCE WAS USED AT THE TIME OF CLOSING AND LATCHING THE DOOR. THE DOOR HANDLE WAS REPLACED WITH A SERVICEABLE PART. THE DOOR WAS OPERATIONALLY CHECKED FOR LOCKING AND UNLOCKING IAW AVTEC CARGO DOOR MM SECTION A, PAGE 10. THE HANDLE IS THE ORIGINAL EQUIPMENT MANUFACTURED BY DASSAULT, BUT MODIFIED TO WORK IN THIS APPLICATION BY THE STC HOLDER. THE CARGO DOOR IS INSTALLED UNDER AVTEC, INC., CARGO DOOR MODIFICATION STC SA2490S0. (X) 2 L 7 2 4F A7EU 1996082900627 19960829 00627 NM 1996 8 29 WRLA96029 1 19960806 A 2913 6506606 HYD PUMP DOUG MD11 MD11F 3023600 NM NR 3 LEFT FAILED A WRLA K NONE J K WARNING INDICATION FLUID LOSS CL CLIMB 1 EA 27 274WA 48633 ON CLIMB-OUT, CREW RECEIVED 'HYD PUMP 3 OFF' ANNUNCIATION. HYD CONTROLLER OPERATED NORMALLY, NR 3 STANDBY PUMP CAME INT O OPERATION. FLT CREW CONTINUED WITH FLT. AFTER 1HR 45 MINS AT CRUISE, FLT CREW RECEIVED 'HYD SYSTEM 3' FAILED ANNUNCI ATION. AT THAT TIME NR 3 HYD SYSTEM QUANTITY WAS NOTED ZERO. HYD CONTROLLER OPERATED NORMALLY, SHUTTING DOWN NR 3 SYS HYD PUMP. FLT CREW ELECTED TO CONTINUE TO PLANNED DESTINATION PER 'ABNORMAL PROCEDURE'. ALT LANDING GEAR EXTENSION PRO CEDURE UTILIZED. A/C LANDED W/O FURTHER INCIDENT. MX FOUND NR 3 LT PUMP FAILED. R/R LT AND RT PUMPS. SERV SYS TO FUL L. LK CHECK OK. A/C RETURNED TO SERV. HYD CONTROLLER (P/N 6506606) WILL BE REMOVED FROM A/C. FAULT MEMORY WILL BE IN 2 L 7 3 4F RT A22WE 1996082900628 19960829 00628 NM 1996 8 29 WRLA96030 1 19960806 A 2910 6506606 HYD CONTROLLER DOUG MD11 MD11F 3023600 NM FWD ACCY CMPT FAILED A WRLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 274WA 48633 DURING TAXI, FLIGHT CREW RECEIVED 'HYDRAULIC SYSTEM CONTROLLER AUTO INOP' WARNING. FLIGHT CREW RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL CONFIRMED HYDRAULIC SYSTEM CONTROLLER FAILED. REMOVED AND REPLACED HYDRAULIC SYSTEM CONTROLLER. GROUND TEST OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 3 4F RT A22WE 1996082900629 19960829 00629 NM 1996 8 29 96ZZZX4192 1 19960805 A 3211 654611316 TRUNNION PIN BOEING 737 7373B7 1384580 NM LT MLG CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 952WP Y5161 23378 LEFT MLG TRUNNION PIN IS CORRODED. REMOVED AND REPLACED TRUNNION PIN IAW MM 32-11-00. (X) 2 L 7 2 4F RT A16WE 1996082900630 19960829 00630 NM 1996 8 29 96ZZZX4193 1 19960806 A 5320 69434961 SUPPORT BOEING 737 7373B7 1384580 NM BS 847-867 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 952WP 23378 CORROSION ON FLOOR TO SIDEWALL SUPPORT, BOTH TOP AND BOTTOM AROUND NUTPLATES, BS 847-867, RBL 21, WL 162 (FOUND TO BE OU T OF LIMITS PER SRM 53-60-15). REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT PER SRM'S 53-60-15, 51-20-01, 51-40-02. ( X) 2 L 7 2 4F RT A16WE 1996082900631 19960829 00631 WP 1996 8 29 96ZZZM1247 1 19960806 A 3231 4648255 ROD ASSY DOUG DC8 DC8F54 3021926 WP NLG DOOR BROKEN A A FXLA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 426FB 45667 AFTER TAKEOFF, PARAMARIBO, EXPERIENCED LOUD NOISE AND SLIGHT VIBRATION IN NOSE AREA. DIVERTED TO POS AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED A BROKEN ROD ASSY AT THE STRUT END ON THE AFT RIGHT NOSE GEAR DOOR. REPLACED ROD ASSEMB LY, PERFORMED GEAR SWING AND RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 4 4F 4A25 1996082900632 19960829 00632 NM 1996 8 29 96ZZZM1248 1 19960724 A 2110 NH100465510 CLAMP BOEING 707 707321C 138367B NM NR 3 ENG BROKEN A MIRA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 19 722GS 19373 OXO - FLT 401 - KMIA- SHUTDOWN ENGINE NR 3 DUE TO OIL PRESSURE DROPPING TO ZERO WARNING LIGHT OIL PRESSURE INOP. REMOVE D AND REPLACED BROKEN CLAMP AT TURBO COMPRESSOR DUCT COMING FROM 16TH STAGE. REPAIRED WIRES ON NR 3 OIL PRESS TRANSMITT ER. PERFORMED GROUND OPERATION ENGINE RUN-UP ALL PARAMETERS NORMAL IAW BOEING MM 71-5-0. (M) 2 L 7 4 4F 4A26 1996082900633 19960829 00633 WP 1996 8 29 96ZZZM1249 1 19960724 A 5230 CHANNEL LKHEED 1011 10113851 5265010 WP C3 CARGO CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 313EA 193A1020 LEVEL 2 CORROSION, C3 CARGO DOOR X-BRACE BETWEEN PIVOT ARMS HAS CORROSION ON 'U' CHANNEL AT AFT INBOARD ATTACH FITTING. REMOVED AND REPLACED 'U' CHANNEL PER SRM 51-50-04. (M) 2 L 7 3 4F A23WE 1996082900634 19960829 00634 WP 1996 8 29 96ZZZM1250 1 19960721 A 3233 57740355508 RETRACT CYL DOUG DC8 DC863 302198A WP RT MLG FAILED A RIAA A J UNSCHED LANDING DUMP FUEL K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 19 4935C 45931 FLT NR 1100 - TER-CTA - DURING CLIMB, RIGHT MAIN GEAR HYDRAULIC CYLINDER SEAL BROKE DURING UPLATCH CHECK. AIRCRAFT DUMP ED FUEL, PERFORMED EMERGENCY GEAR EXTENSION, DECLARED EMERGENCY AND RETURNED TO TER. ON GROUND AT TER, MAINTENANCE FOUN D RETRACT CYLINDER SEAL FAILURE. AIRCRFT FERRIED TO MIA WITH GEARS EXTENDED ON 7/22/96. IN MIAMI, REPLACED RIGHT MLG R ETRACT CYLINDER. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 4 4F 4A25 1996082900635 19960829 00635 WP 1996 8 29 96ZZZM1251 1 19960726 A 7603 THROTTLE BOX LKHEED 1011 10113851 5265010 WP NR 3 ENGINE LACK OF LUBE A RIAA K NONE E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 19 305GB 193P1127 FLT NR 7202 - KCLE-KNKT - AFTER DEPARTURE AT ABOUT 2,000 FEET, ERRATIC/INTERMITTENT INDICATION NR 3 ENGINE ON BOTH AVM C HANNELS A AND B AT 3.5, NO ABNORMAL AIRFRAME VIBRATION, THROTTLE TO IDLE AND AVM RETURNED TO NORMAL. REAPPLICATION OF P OWER AVM REMAINED NORMAL. ON GROUND, MAINTENANCE CLEANED THROTTLE BOX AND LUBRICATED MID SPAR SUPPORTS. ENGINE CHECKED GOOD AT IDLE AND TAKEOFF POWER. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A23WE 1996082900636 19960829 00636 WP 1996 8 29 96ZZZM1252 1 19960723 A 4930 3014225 O-RING LKHEED 1011 10113851 5265010 WP NR 12/13 NOZZLE DETERIORATED A RIAA F ACTIVATE FIRE EXT. J K WARNING INDICATION FLUID LOSS TX TAXI/GRND HDL 1 SO 19 765BE 193P1105 FLT 227 - KSJC-PHNL - AFTER LANDING AND DURING TAXIING TO GATE, APU ACCOMPLISHED AUTO SHUTDOWN. FIRE BOTTLE DISCHARGED AND EMERGENCY DECLARED. AT GATE, MAINTENANCE FOUND EVIDENCE OF SMALL FIRE FROM FUEL LEAK AT APU FUEL MANIFOLD AT ABOUT 10 O'CLOCK POSITION. MAINTENANCE REPLACED O-RING AT NR 13 SECONDARY NOZZLE TRANSFER TUBE AND NR 12 NOZZLE TRANSFER TUBE . ACCOMPLISHED LEAK CHECK, EVERYTHING OK. AIRCRAFT RELEASED INTO SERVICE. (M) 2 L 7 3 4F A23WE 1996082900637 19960829 00637 NM 1996 8 29 96ZZZM1253 1 19960730 A 3350 ML7715 BULB BOEING 747 747238B 1384828 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 607PE 20011 DURING DAILY CHECK, FOUND FLOOR EVAC LIGHT AT SEAT 22H INOP. REPLACED LENS AND BULB. OPS CHECKED OK PER MM 33-51-00 PG 501. REFERENCE TWRA96254. 2 L 7 4 4F A20WE 1996082900639 19960829 00639 NM 1996 8 29 96ZZZM1255 1 19960725 A 3350 CM7715 BULB BOEING 747 747238B 1384828 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 607PE 20011 DURING DAILY CHECK, FOUND EVAC LIGHT AND LENS MISSING AT 21K, 31K, 56K, 60K. REPLACED LENS AND BULB. OPS CHECKED OK PE R MM 33-51-00. REFERENCE TWRA96222. 2 L 7 4 4F A20WE 1996082900640 19960829 00640 NM 1996 8 29 96ZZZM1256 1 19960801 A 3350 ML7715 BULB BOEING 747 747259B NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 EICEO 21730 DURING DAILY CHECK, FOUND 11H FLOOR EMERGENCY LIGHT IS INOP AND LENS IS MISSING. REPLACED LIGHT LENS AND BULB AT SEAT 1 1H. OPS CHECKED OK PER MM 33-51-00. REFERENCE TWRA96251. 2 L 7 4 4F RT A20WE 1996082900641 19960829 00641 NM 1996 8 29 96ZZZM1257 1 19960611 A 3350 20131A BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SPAA K NONE L NO TEST IN INSP/MAINT 1 WP 07 703S 22529 DURING SCHEDULED CHECK, THE AFT FLOOR TRACK EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. THE ASSOCIATED SYSTEM BATTERY PACK WAS REPLACED. SUBSEQUENT SYSTEM CHECK WAS SATISFACTORY PER BMM 33-51-11. (M) 2 L 7 2 4F A16WE 1996082900642 19960829 00642 NM 1996 8 29 96ZZZM1258 1 19960726 A 2910 6546858258 HYD LINE BOEING 737 7372T4 1384492 NM NR 2 PYLON CHAFED A SPAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 07 703S 22529 A/C RETURNED TO SLC AFTER T/O ON A REPOSITIONING FLIGHT TO BOI WHEN THE NR 1 AND NR 2 'A' SYS HYD PUMP LOW PRESS WARNING LIGHTS ILLUMINATED FOLLOWED BY THE HYDRAULIC QTY LOW LVL LIGHT. THE A/C LANDED W/O INCIDENT BUT HAD TO BE TOWED FROM T HE RUNWAY DUE TO LOSS OF STEERING CAPABILITY. TROUBLESHOOTING REVEALED THAT A HOLE HAD WORN INTO THE .5 INCH HYD PRESS LINE RUNNING FROM THE FWD END OF THE NR 2 ENG PYLON AFT AND OVER THE ENG TO THE ENG DRIVEN HYDRAULIC PUMP RESULTING IN F LUID LOSS. THE UNSERVICEABLE HYDRAULIC LINE WAS REMOVED AND REPLACED. ALL 'A' SYS PRESS AND CASE DRAIN FILTERS CHECKED FOR CONTAM. THE HYD SYS WAS RESERVICED, ALL LK AND OPS CHECK ACCOMP. A/C WAS RETURNED TO SERV. (M) 2 L 7 2 4F A16WE 1996082900643 19960829 00643 NM 1996 8 29 96ZZZM1259 1 19960711 A 3350 20131A BATTERY PACK BOEING 737 7372T4 1384492 NM AFT CABIN LOW CHARGE A SPAA K NONE L NO TEST IN INSP/MAINT 1 WP 07 703S 22529 DURING SCHEDULED CHECK, THE AFT SECTION OF EMERGENCY FLOOR TRACK LIGHTING WAS FOUND INOPERATIVE. THE ASSOCIATED SYSTEM BATTERY PACK WAS REPLACED. SUBSEQUENT SYSTEM CHECK WAS SATISFACTORY PER BMM 33-51-11. (M) 2 L 7 2 4F A16WE 1996082900644 19960829 00644 WP 1996 8 29 96ZZZM1260 1 19960724 A 2612 24408032 SENSOR LOOP DOUG DC8 DC851 3021920 WP NR 1 ENGINE CHAFED A FXLA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 19 507DC 45855 AFTER TAKEOFF IN MIAMI, RECEIVED FIRE WARNING INDICATION ON NR 1 ENGINE. SHUT DOWN ENGINE AND RETURNED TO MIAMI. LANDE D WITHOUT INCIDENT. INSPECTION REVEALED A CHAFED SENSOR LOOP ON THE AFT OUTBOARD COWLING DOOR. REPLACED SENSOR LOOP, P ERFORMED OVERWEIGHT LANDING INSPECTION. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 4 4F 4A25 1996082900645 19960829 00645 NE 1996 8 29 96ZZZM1261 2 19960421 A 7200 BEARING BOEING 727 727225 1384077 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE FAILURE A UHVA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 11 805EA 35426 22436 ON TAKEOFF, NR 1 ENGINE OIL BYPASS LIGHT CAME ON. BROUGHT THROTTLE BACK TO IDLE, ALL INDICATIONS NORMAL. AFTER CRUISE THROTTLE WAS MOVED FROM IDLE AND OIL TEMP CLIMBED WITH THROTTLE MOVEMENT. THROTTLE RETARDED AND PILOT MENTIONED HE SHUT ENGINE DOWN FOR PRECAUTION. WHEN AIRCRAFT ARRIVED, PULLED ENGINE OIL FILTERS. FOUND EXCESSIVE METAL IN SCREEN, SENT O IL OUT FOR ANALYSIS. RESULTS INDICATE BEARING FAILURE. REMOVED AND REPLACED NR 1 ENGINE. (M) 2 L 7 3 4F 4 F A3WE E2EA 1996082900646 19960829 00646 NM 1996 8 29 AALA960937 1 19960618 A 3350 A3060698101 CONNECTOR DOUG MD11 MD11 3023602 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1760A 48550 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT LEFT AISLE OF CABIN ZONE C, BETWEEN PAX SEAT ROWS 22C THROUGH 34 C INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR AT LEFT AISLE OF CABIN ZONE C BY PAX SEAT 22C. SYSTEM G ROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1996082900647 19960829 00647 WP 1996 8 29 AALA960978 1 19960627 A 3233 39281375001 ACTUATOR DOUG DC9 DC982 3022082 WP NLG LEAKING A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 283AA 49296 DFW - FLT 2012 - AFTER TAKEOFF DFW WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR DID NOT RETRACT AND NOSE GEAR UNSAFE L IGHT ILLUMINATED. EXTENDED LANDING GEAR AND ALL INDICATIONS RETURNED TO NORMAL. AIRCRAFT RETURNED TO DFW AND LANDED WI THOUT INCIDENT. REPLACED NOSE LANDING GEAR RETRACTION CYLINDER. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEF ECTS FOUND. SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996082900648 19960829 00648 NE 1996 8 29 AALA961020 2 19960706 A 7321 76960612 FUEL CONTROL DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE RT ENGINE MALFUNCTIONED A AALA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 SW 07 248AA BBCLYZD 49259 SFO - FLT 1308 - DURING CLIMB-OUT, RIGHT ENGINE SURGED TO 95 PERCENT N1 FOLLOWED BY FLAME OUT. ACCOMPLISHED ENGINE SHU TDOWN PROCEDURES AND AIRCRAFT DIVERTED TO SFO, LANDING WITHOUT INCIDENT. CHECKED RIGHT ENGINE INLET AND EXHAUST WITH NO DAMAGE OR DEFECTS FOUND. ACCOMPLISHED GROUND ENGINE RUN AND ENGINE OPERATION CHECKED NORMAL. ACCOMPLISHED BORESCOPE O F RIGHT ENGINE WITH NO DAMAGE OR DEFECTS FOUND. REPLACED RIGHT ENGINE FUEL CONTROL. ALSO, REPLACED RIGHT ENGINE FUEL P UMP AND FILTER. ACCOMPLISHED GROUND ENGINE RUN AND TRIM. SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F 4 F A6WE E9NE 1996082900649 19960829 00649 NE 1996 8 29 AALA961029 2 19960209 A 7313 500430802 FUEL NOZZLE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE RT ENGINE FAILED A A AALA A UNSCHED LANDING T ENGINE CASE PENETRATION CL CLIMB 1 SW 07 287AA 49299 709930 FLT 9147 - AFTER T/O, A BANG WAS HEARD AND RT ENG FAILED. RETURNED TO SAT AND LANDED W/O INCIDENT. FOUND EXHAUST TAILC ONE AND BEARING HOUSING MISSING, AND ENTIRE AFT TURBINE DESTROYED. REPLACED NR 2 ENG ASSY. SYS GRD CHK'D NORM OPS. AL L 3RD AND 4TH STAGE TURBINE BLADES FAILED AT THE ROOT. TURBINE CASE HAD SEVERAL HOLES FROM WHERE BLADES HAD PENETRATED. HEAVY FOD DAMAGE TO THE 2ND TURBINE AND THE MIXER DUCT. NR 6 BEARING HOUSING TORN FREE AT TIE-RODS. THE 1ST AND 2ND TURBINE VANES WERE HEAVILY DISCOLORED (OVERTEMPED) AND WARPED AT THE 3:30 POSITION. NR 3 POSITION FUEL NOZZLE HAD BAD P RIMARY TO SECONDARY FUEL LEAK PAST SEVERAL CRACKS IN CHEVRON SEAL. NO DAMAGE TO COMB, CASE, CANS OR NOZZLES. (M) 2 L 7 2 4F 4 F A6WE E9NE 1996082900650 19960829 00650 EU 1996 8 29 AALA961061 1 19960713 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77080 626 JFK - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY EXIT FLOOR PATH TRACK LIGHTS AT THE 3L DOOR INOPERATIVE. REPLACED E MERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996082900651 19960829 00651 NM 1996 8 29 AALA961062 1 19960713 A 3397 WIRE DOUG MD11 MD11 3023602 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1759 48481 DFW - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH TRACK LIGHTS FORWARD OF FLIGHT ATTENDANT SEAT INOPERATIVE. REPAIRED WIRING TO EMERGENCY EXIT FLOOR PATH SWITCH ON FLIGHT ATTENDANT PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION . (M) 2 L 7 3 4F RT A22WE 1996082900652 19960829 00652 WP 1996 8 29 AALA961063 1 19960711 A 3397 WIRE DOUG DC10 DC1030 3023501 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 144AA 47848 DFW - DURING OVERNIGHT CHECK, FOUND WIRE PULLED OFF OF PLUG FOR THE R4 DOORWAY LIGHTING FORWARD BOTTOM EMERGENCY EXIT FL OOR PATH LIGHT. REPAIRED EMERGENCY EXIT FLOOR PATH WIRES TO PLUG. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A22WE 1996082900653 19960829 00653 WP 1996 8 29 AALA961077 1 19960713 A 2150 5915112515 CLAMP DOUG DC9 DC982 3022082 WP ACM BAY DISCONNECTED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 219AA 49171 DEN - FLT 615 - WHILE EN ROUTE SLC TO ORD AT 31,000 FEET, THE FLIGHT ATTENDANTS REPORTED A BURNING SMELL IN BOTH AFT LAV ATORIES. PULLED CIRCUIT BREAKERS TO LOCATE SOURCE WITH NO AVAIL. THEN SAW SMOKE IN THE RIGHT AFT LAVATORY. AIRCRAFT D IVERTED TO DEN. AT SAME TIME THE RIGHT PACK INDICATOR PSI WAS FLUCTUATING FROM 0-3 PSI ABOUT EVERY 10 SEC. DESCENDED T O 26,000 FEET AND PACK STABILIZED. REPORTED LOUD CYCLING NOISE IN BACK THAT SEEMED TO COINCIDE WITH RIGHT PACK PSI FLUC TUATING. AIRCRAFT LANDED AT DEN WITHOUT INCIDENT. REINSTALLED RIGHT PACK AIR CYCLE MACHINE COMPRESSOR OUTLET DUCT BOOT AND CLAMP. RAN RIGHT PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996082900654 19960829 00654 EU 1996 8 29 AALA961079 1 19960717 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 70072 515 MIA - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY EXIT FLOOR PATH LIGHTING AT ROW 14-16 A AND B DAMAGED. REPAIRED EME RGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996082900655 19960829 00655 NM 1996 8 29 AALA961084 1 19960718 A 3350 EXIT SIGN BOEING 767 767223 1385123 NM R1 DOOR CABIN KNOCKED OFF A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 317AA 22319 JFK - FLT 132 - DURING AIRCRAFT GROUND PREPARATION, THE EMERGENCY DIRECTIONAL LIGHT SIGN AT THE R1 DOOR WAS FOUND ON CAB IN FLOOR AT RIGHT SIDE OF GALLEY. REPLACED EMERGENCY DIRECTIONAL LIGHT SIGN AT R1 DOOR. SYSTEM GROUND CHECKED NORMAL O PERATION. (M) 2 L 7 2 4F RT A1NM 1996082900656 19960829 00656 NM 1996 8 29 AALA961100 1 19960720 A 3350 PIN BOEING 767 767323 1385205 NM PAX SEAT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 352AA 24033 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 27B INOPERATIVE. REPLACED BROKEN PIN ON SEAT MOUNT ED EMERGENCY EXIT LIGHT AT PASSENGER SEAT 27B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1996082900657 19960829 00657 WP 1996 8 29 AALA961102 1 19960719 A 2170 21D101 COALESCER DOUG DC9 DC982 3022082 WP ACM BAYS DIRTY A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 486AA 49679 LIT - FLT 1551 - EN ROUTE EWR/DFW - DURING CRUISE AT FL 310, REPEATED INSTANCES OF SMOKE NOTED IN MAIN CABIN WHICH WOULD LAST FOR APPROXIMATELY 5 MINUTES AND THEN DISSIPATE. AIRCRAFT DIVERTED TO LIT AND LANDED WITHOUT INCIDENT. CHECKED BO TH ENGINE INLETS WITH NO DEFECTS FOUND. CHECKED ALL INDIRECT LIGHT BALLASTS WITH NO DEFECTS FOUND. CHECKED LEFT AND RI GHT PACK FANS AND RECIRCULATION FAN WITH NO DEFECTS FOUND. REPLACED LEFT AND RIGHT COALESCER BAGS AND ACCOMPLISHED BURN OUT PROCEDURE OF PNEUMATIC DUCTING. SYSTEM GROUND CHECKED NORMAL OPERATION WITH NO SMOKE OR ODOR NOTED. (M) 2 L 7 2 4F A6WE 1996082900658 19960829 00658 NM 1996 8 29 AALA961103 1 19960720 A 2750 240863 DRIVE MOTOR BOEING 727 727223 1384074 NM TE FLAP LEAKING A AALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 6835 20188 ORD - FLT 393 - EN ROUTE DTW-ORD - DURING CRUISE, SYS A HYDRAULIC QTY WENT TO LESS THAN ONE-QUARTER GALLON WITH NO LOW L EVEL INDICATION. SYSTEM A HYDRAULIC PRESSURE FLUCTUATED. ACCOMP ABNORMAL PROCEDURE FOR LOSS OF SYSTEM A HYDRAULIC FOLL OWED BY NR 2 ENG HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATING. A/C PROCEEDED TO ORD AND LANDED W/O INCIDENT. REPLACE D OUTBOARD FLAP DRIVE MOTOR FOUND LEAKING. ALSO, REPLACED BOTH ENGINE DRIVEN HYDRAULIC PUMPS AND CASE DRAIN FILTERS ON NR 2 ENGINE. ACCOMPLISHED LEAK AND GROUND CHECK WITH NO DEFECTS FOUND. ACCOMPLISHED GROUND ENGINE RUN AND CHECK OF LOW PRESSURE LIGHT OPERATION WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORM OPS. (M) 2 L 7 3 4F A3WE 1996082900659 19960829 00659 NM 1996 8 29 AALA961104 1 19960723 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 649AA 24607 SFO - DURING OVERNIGHT CHECK, EMERGENCY LIGHTS AT DOOR 2R AND SECOND RIGHT OVERWING DOOR INOPERATIVE. RESECURED LOOSE E MERGENCY LIGHT CONNECTORS AT DOOR 2R AND AT SECOND RIGHT OVERWING DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1996082900660 19960829 00660 WP 1996 8 29 AALA961105 1 19960722 A 2121 6054578 FAN DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 262AA 49290 DFW - FLT 2023 - AFTER TAKEOFF DFW DURING CLIMB-OUT, ELECTRICAL ODOR AND RUMBLING NOISE NOTED IN MAIN CABIN. ODOR DISSI PATED, BUT RUMBLING CONTINUED. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. CHECKED BOTH AIR CONDITIONING PAC KS AND FAN MOTORS WITH NO DEFECTS FOUND. CHECKED ALL OVERHEAD WHITE LIGHT BALLASTS WITH NO DEFECTS FOUND. REPLACED REC IRCULATION FAN. ACCOMPLISHED GROUND CHECK OF AIR CONDITIONING AND RECIRCULATION SYSTEM WITH NO DEFECTS OR ODORS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996082900661 19960829 00661 NM 1996 8 29 AALA961106 1 19960722 A 2822 8905K935 SWITCH BOEING 727 727223 1384074 NM F/E PANEL DEFECTIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 860AA 21087 MCI - FLT 1714 - AFTER TAKEOFF MCI DURING CLIMB-OUT, ELECTRICAL ODOR NOTED IN COCKPIT. ACCOMPLISHED ABNORMAL PROCEDURES AND ODOR DISSIPATED. AIRCRAFT RETURNED TO MCI AND LANDED WITHOUT INCIDENT. REPLACED SWITCH AND TERMINALS AT F/E PANEL FOR CENTER FUEL TANK LEFT FORWARD BOOST PUMP. ACCOMPLISHED GROUND ENGINE RUN AND OPERATED PACKS WITH NO ODOR NOTED. S YSTEM GROUND CHECKED NORMAL OPERATION WITH NO ELECTRICAL ODOR NOTED. (M) 2 L 7 3 4F A3WE 1996082900662 19960829 00662 NM 1996 8 29 AALA961109 1 19960714 A 5320 836506401 MOUNT BOEING 767 767323 1385205 NM GALLEY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 363AA 24044 AFW - FOUND G-6 GALLEY MOUNT HAS CORROSION ON VERTICAL FLANGE. FABRICATE AND INSTALL DOUBLER PER ENGINEERING MRB 767-12 72. (M) 2 L 7 2 4F RT A1NM 1996082900663 19960829 00663 WP 1996 8 29 AALA961110 1 19960722 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 1214 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 233AA 49180 TUL - FOUND BOTTOM FACE OF WEB AFT OF CARGO DOOR BETWEEN L28R AND L27R IS CORRODED AROUND NUT PLATES. INSTALLED WEB DOU BLER PER SRM 53-01 AND ESO 80559 DATED 7/22/96. (M) 2 L 7 2 4F A6WE 1996082900664 19960829 00664 NM 1996 8 29 AALA961111 1 19960725 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 680-686 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 867AA 21372 TULE - FOUND STRINGER 26 RIGHT CORRODED, STATION 680-686. CUT OUT CORROSION AND INSTALLED STRINGER REPAIR PER SRM 53-10 -3. (M) 2 L 7 3 4F A3WE 1996082900665 19960829 00665 NM 1996 8 29 AALA961113 1 19960725 A 5330 SKIN BOEING 727 727223 1384074 NM BS 706 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 867AA 53337 21372 TUL - FOUND BULGE IN FUSELAGE SKIN. REMOVED CORRODED AREA AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 5. (M) 2 L 7 3 4F A3WE 1996082900666 19960829 00666 WP 1996 8 29 AALA961114 1 19960726 A 5320 549337931200 SUPPORT DOUG DC10 DC1030 3023501 WP BS 410 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 143AA 46555 TUL - FOUND FORWARD GI GALLEY INBOARD SUPPORT HAS CORROSION AROUND AFT MOUNT ATTACH HOLE. REPLACED GALLEY INBOARD SUPPO RT TRACK FROM STATION 401 T0 422 PER SRM 53-00-01 AND 51-21-01. (M) 2 L 7 3 4F A22WE 1996082900667 19960829 00667 WP 1996 8 29 AALA961115 1 19960726 A 5320 52929169 SUPPORT DOUG DC10 DC1030 3023501 WP BS 439 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 143AA 46555 TUL - FOUND FLOOR BOARD SUPPORT BETWEEN TRACK (SEAT TRACK) 6 AND 7 HAS CORROSION DAMAGE. REPLACED FLOOR BOARD SUPPORT C HANNEL PER SRM 53-00-01, 51-81-01. (M) 2 L 7 3 4F A22WE 1996082900668 19960829 00668 WP 1996 8 29 AALA961116 1 19960726 A 5320 4929151 SUPPORT DOUG DC10 DC1030 3023501 WP BS 420 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 143AA 46555 TUL - FOUND CORROSION ON G-2 SUPPORT, RIGHT SIDE OF FLOOR TRACK NR 6. REPLACED GALLEY SUPPORT AT FORWARD G-2 GALLEY PER 53-00-01 AND 51-21-01, SUPPORT INSTALLED FROM STATION 401 TO 450. (M) 2 L 7 3 4F A22WE 1996082900669 19960829 00669 WP 1996 8 29 AALA961117 1 19960726 A 5320 5493379312000 SUPPORT DOUG DC10 DC1030 3023501 WP BS 465 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 143AA 46555 TUL - FOUND G-3 GALLEY SUPPORT HAS CORROSION DAMAGE OUTBOARD SIDE OF SEAT TRACK NR 6. REPLACED G-3 GALLEY SUPPORT FROM STATION 450 TO STATION 480 PER SRM 53-00-01 AND 51-21-01. (M) 2 L 7 3 4F A22WE 1996082900670 19960829 00670 NM 1996 8 29 AALA961118 1 19960724 A 3260 849801 PSEU CARD BOEING 767 767223 1385123 NM LT MLG DEFECTIVE A AALA O OTHER P NO WARNING INDICATION AP APPROACH 1 SW 07 307AA 22313 JFK - DURING APPROACH TO JFK WHEN LANDING GEAR EXTENDED, LEFT MAIN LANDING GEAR GREEN LIGHT FAILED TO ILLUMINATE AND WOU LD NOT TEST. CONFIRMED LEFT MAIN LANDING GEAR EXTENDED AND AIRCRAFT LANDED JFK WITHOUT INCIDENT. REPLACED PROXIMITY SW ITCH ELECTRONIC UNIT MODULE BOARDS. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CH ECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1996082900671 19960829 00671 NM 1996 8 29 AALA961119 1 19960724 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 639AA 24597 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRI P BY FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1996082900672 19960829 00672 NM 1996 8 29 AALA961120 1 19960727 A 3350 LIGHT STRIP BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 701AA 22459 RDU - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 29DEF AND 30DEF INOPERATIVE. REPLACED EMERGE NCY FLOOR LIGHT STRIP BETWEEN PAX SEAT ROWS 29DEF AND 30DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996082900673 19960829 00673 WP 1996 8 29 AALA961125 1 19960729 A 5320 ABA8312501 SUPPORT DOUG DC10 DC1030 3023501 WP BS 422 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 143AA 46555 TUL - FOUND CORROSION AT NR 2 GALLEY INBOARD AFT SUPPORT. REPLACED NR 2 GALLEY INBOARD SUPPORT WITH NEW PART, PART NR A BA 8312-501 FROM DOUGLAS AT STATION. (M) 2 L 7 3 4F A22WE 1996082900674 19960829 00674 WP 1996 8 29 AALA961126 1 19960727 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1987-2007 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 143AA 46555 TUL - FOUND FLOOR BOARD SUPPORT ABOVE LARGE DUCT AT STATION 2007 IS CORRODED SEVERAL PLACES AROUND FASTENER HOLES. FABR ICATED NEW FLOOR BOARD SUPPORT. P AND P IAW SRM 53-00-01. INSTALLED F/B SUPPORT AT AFT GALLEY FLOOR. (M) 2 L 7 3 4F A22WE 1996082900675 19960829 00675 WP 1996 8 29 AALA961128 1 19960729 A 5720 ANGLE DOUG DC10 DC1030 3023501 WP WS 240 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 143AA 46555 TUL - FOUND EXFOLIATION CORROSION ON LOWER WING SPLICE ANGLE WITH A CRACK BETWEEN 1ST AND 2ND HOLES OUTBOARD OF GEAR TRU NNION CASTING TOP OF LOWER WING. INSTALLED A NEW SPLICE ANGLE PER SRM 51-01-00-05 PG 1. (M) 2 L 7 3 4F A22WE 1996082900676 19960829 00676 WP 1996 8 29 AALA961129 1 19960725 A 5320 DOOR BEAM DOUG DC9 DC982 3022082 WP BS 674 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 278AA 49294 TUL - FOUND DOOR BEAM CORRODED UNDER PREVIOUS REPAIR NOTED IN ESO 80559 DATED 8/31/92. (M) 2 L 7 2 4F A6WE 1996082900677 19960829 00677 NM 1996 8 29 AALA961131 1 19960729 A 3350 PIN BOEING 767 767323 1385205 NM PAX SEAT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 385AM 27059 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 30B INOPERATIVE. REPLACED TWO BROKEN PINS AT PASSE NGER SEAT 30B EMERGENCY EXIT LIGHT CANNON PLUG. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1996082900678 19960829 00678 EU 1996 8 29 AALA961132 1 19960729 A 3350 A3060698101 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 14077 612 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT FORWARD PART OF FIRST CLASS CABIN RIGHT AISLE INOPERATIVE. REPL ACED BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTOR AT FORWARD PART OF FIRST CLASS CABIN RIGHT AISLE. SYSTEM GROUND CHECK ED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996082900679 19960829 00679 EU 1996 8 29 AALA961133 1 19960729 A 3350 A3060698101 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 14077 612 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROW 37HJ TO LAVATORY Z INOPERATIVE. RESECURED LOO SE EMERGENCY FLOOR LIGHT STRIP CONNECTOR BY PAX SEAT ROW 37HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996082900680 19960829 00680 WP 1996 8 29 AALA961134 1 19960730 A 3397 WIRE DOUG DC10 DC1030 3023501 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 163AA 46914 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PAX SEAT 3H INOPERATIVE. REPAIRED BROKEN EMERGENCY FLOOR LIGHT WIRE BY PAX SEAT 3H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A22WE 1996082900681 19960829 00681 WP 1996 8 29 AALA961136 1 19960729 A 5320 SHEAR TIE DOUG DC9 DC982 3022082 WP BS 1231 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 278AA 49294 TUL - FOUND SHEAR TIE EXFOLIATED, REMOVED AND REPLACED. (M) 2 L 7 2 4F A6WE 1996082900682 19960829 00682 WP 1996 8 29 AALA961138 1 19960730 A 2131 CONTROLLER DOUG DC9 DC982 3022082 WP CABIN MALFUNCTIONED A AALA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SW 07 405A 49316 CLE - FLT 1624 - EN ROUTE DFW/CLE - DURING CRUISE AT FL 370 WITH ENGINE ANTI-ICE ON, CABIN ALTITUDE BEGAN TO CLIMB AND F LOW LIGHT ILLUMINATED. ACCOMPLISHED EMERGENCY DESCENT AND AIRCRAFT PROCEEDED TO CLE, LANDING WITHOUT INCIDENT. ACCOMPL ISHED PRESSURIZATION DECAY CHECK WITH NO DEFECTS FOUND. ACCOMPLISHED BITE CHECK OF CONTROLLERS WITH NO DEFECTS FOUND. A IR CYCLE MACHINES GROUND CHECKED NORMAL OPERATION. UNABLE TO DUPLICATE PROBLEM AND SUSPECTED PROBLEM DUE TO PAC ICING A S A RESULT OF ATMOSPHERIC CONDITIONS. SUBSEQUENTLY, AS PRECAUTIONARY MEASURE, REPLACED NR 1 PRESSURIZATION CONTROLLER A T DFW/30. (M) 2 L 7 2 4F A6WE 1996082900683 19960829 00683 WP 1996 8 29 AALA961139 1 19960728 A 2130 CHECK VLV DOUG DC9 DC982 3022082 WP TAIL COMPT STUCK CLOSED A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 295AA 49307 ABQ - FLT 1191 - DFW-SFO - DURING CRUISE TAIL COMPART HIGH TEMP LIGHT ILLUMINATED. A/C DIVERTED TO ABQ AND LANDED OVERW EIGHT W/O INCIDENT. CHECKED AIR CONDITIONING DUCT AT ACM AND APU SUPPLY DUCTS WITH NO DEFECTS FOUND. ACCOMP GROUND ENG RUN AND CHECKED AUGMENTATION VLV AND ENG SUPPLY DUCTS WITH NO DEFECTS FOUND. CLEANED AND FREED UP OVERHEAT SENSOR, CHE CK VLV FOUND STUCK CLOSED. PRECAUTIONARY PLACARDED LEFT ACM. SYSTEM GROUND CHECKED NORMAL OPERATION. ACCOMPLISHED OVE RWEIGHT LANDING INSPECTION WITH NO DEFECTS FOUND. A/C REDEPARTED ABQ-SFO, SUBSEQUENTLY AT DFW, ACCOMP GROUND CHECK OF B OTH PACK AND HIGH TEMP SYSTEM W/NO DEFECTS FOUND. SYSTEMS GROUND CHECKED NORM OP AND PLACARD REMOVED. (M) 2 L 7 2 4F A6WE 1996082900684 19960829 00684 NM 1996 8 29 AALA961153 1 19960730 A 3520 OXY GENERATOR BOEING 767 767323 1385205 NM MID-LAVS NOT ARMED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 362AA 24043 SFO - DURING OVERNIGHT CHECK, WHILE GAINING ACCESS TO CEILING MOUNTED LAVATORY OXYGEN MODULES DURING FCD ACCOMPLISHMENT, OXYGEN GENERATORS AT M-1 AND M-2 MID CABIN LAVATORIES WERE FOUND WITH WARNING FLAGS AND SAFETY PINS INSTALLED. REMOVED WARNING FLAGS AND SAFETY PINS AT M-1 AND M-2 LAVATORIES. ACCOMPLISHED OXYGEN MODULE DOOR TEST WITH NO DEFECTS FOUND. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1996082900685 19960829 00685 WP 1996 8 29 AALA961156 1 19960801 A 3350 A3060698101 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN FLOOR NEEDED RESECURE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 493AA 49731 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIG HT STRIP CONNECTOR BY FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996082900686 19960829 00686 NM 1996 8 29 ASAA9610095 1 19960718 A 3350 8821004 BATTERY BOEING 737 737298C 1384490 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 16 WERE FOUND INOPERATIVE. REPLACED PALLET BATTERY AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996082900687 19960829 00687 NM 1996 8 29 ASAA9640063 1 19960726 A 3397 WIRE BOEING 737 7374S3 1384711 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 786AS 24795 SEA - DURING MAINTENANCE CHECK, SIX EMERGENCY EXIT FLOOR TRACK LIGHTS IN MID CABIN WERE FOUND INOPERATIVE. RECONNECTED LIGHTS AND SECURED TRACK, LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996082900688 19960829 00688 NM 1996 8 29 ASAA9640064 1 19960729 A 3397 WIRE BOEING 737 7374S3 1384711 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 786AS 24795 SEA - DURING MAINTENANCE CHECK, ALL FOUR RED AND ONE WHITE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT O VERWING EXITS. RECONNECTED TRACK LIGHT WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996082900689 19960829 00689 NM 1996 8 29 ASAA9640065 1 19960730 A 3397 WIRE BOEING 737 7374S3 1384711 NM CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 786AS 24795 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 9-13. REPAIRED BRO KEN WIRE AT FLOOR FEED AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996082900691 19960829 00691 NM 1996 8 29 ASAA9640067 1 19960804 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 764AS 25101 SEA - DURING MAINTENANCE CHECK, THE FORWARD TWO RED EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECT ED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996082900692 19960829 00692 WP 1996 8 29 ASAA9680155 1 19960721 A 3350 S103 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 967AS 49103 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 2 TO 7 WERE FOUND INOPERATIVE. REPLACED THE BAT TERIES AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996082900693 19960829 00693 WP 1996 8 29 ASAA9680157 1 19960725 A 3350 60030451 POWER SUPPLY DOUG DC9 DC983 3022083 WP TAILCONE DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 939AS 49657 LAX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE TAILCONE AREA WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996082900694 19960829 00694 WP 1996 8 29 ASAA9680159 1 19960730 A 3350 S103 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 954AS 49387 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 9 TO 12 WERE FOUND INOPERATIVE. REPLACED THE BA TTERIES AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996082900695 19960829 00695 WP 1996 8 29 ASAA9680160 1 19960802 A 3397 WIRE DOUG DC9 DC983 3022083 WP TAILCONE DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 947AS 53020 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY EXIT LIGHT IN THE TAILCONE AREA WAS FOUND INOPERATIVE. REPAIRED BROKEN WIRING AND LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996082900696 19960829 00696 NM 1996 8 29 AWXA960340 1 19960713 A 3620 BLEED AIR LIGHT BOEING 757 7572G7 1384963 NM NR 2 ENGINE ILLUMINATED A AWXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 28 908AW 24233 PHX - FLT 292 - AIR TURNBACK, CREW REPORTED NR 2 ENGINE BLEED OFF LIGHT ILLUMINATED AND THE PACK WAS OFF. CREW TRIED CI RCUIT BREAKER RESET TO NO AVAIL. CREW DID SEVERAL RESETS AND BLEED STILL DID NOT COME BACK ON. AIRCRAFT RETURNED TO PH X FOR REPAIR DUE TO POSSIBLE ICING CONDITIONS AT JFK. UNABLE TO DUPLICATE PROBLEM. BLEED SYSTEM CHECKED GOOD ON GROUND WITH ENGINE RUNS. (M) 2 L 7 2 4F RT A2NM 1996082900697 19960829 00697 EU 1996 8 29 AWXA960342 1 19960719 A 3350 321454 BATTERY AIRBUS 320 A320231 3930325 EU CABIN FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 633AW 527 082 PHX - FLT 2266 - DURING ROUTINE MAINTENANCE CHECK, FOUND APPROXIMATELY EVERY 3RD FLOOR PROX SEAT LIGHT INOP. ALSO, LEFT OVERWING EXIT LIGHT INOP. BITE FAULTS LEFT BATTERIES. REMOVED AND REPLACED MID BATTERY. OPS CHECK AND BITE TESTED GO OD. (M) 2 L 7 2 4F RT A28NM 1996082900698 19960829 00698 EU 1996 8 29 AWXA960349 1 19960728 A 3520 OXY MASK AIRBUS 320 A320231 3930325 EU CABIN FAILED DROP TEST A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 620AW 052 CMH - FLT 2843 - MEL 35-20-03 REQUIRED DROP TEST. DROP TEST FAILED AT 3R, 4L, 8R, 11L, 16R, 18R AND 24R. PLACED SEAT R OWS 3R, 4L, 11L, 16R, 18R, AND 24R ON MEL 35-20-03. REPLACED OXYGEN MASKS AT 3R, 4L, 11L, 16R, 18R, AND 24R PER MM 35-2 1-41. MEL CLEARED. (M) 2 L 7 2 4F RT A28NM 1996082900699 19960829 00699 NM 1996 8 29 AWXA960357 1 19960710 A 5315 FLOOR BEAM BOEING 737 737275 1384485 NM BS 987.5 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 CGBPW 20958 PAE - FLT 7820 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM AT BS 987.5, WL 208, LBL 41-45. REMOVED, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-1. (M) 2 L 7 2 4F A16WE 1996082900700 19960829 00700 NM 1996 8 29 AWXA960358 1 19960710 A 5315 BAC1505100617 FLOOR BEAM BOEING 737 737275 1384485 NM BS 947.5 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 CGBPW 20958 PAE - FLT 7820 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM UPPER CHORD UPPER SURFACE BS 947.5, WL 208, LBL 4 TO LBL 8. REMOVED DAMAGED AREA AT BS 947.5, WL 208, LBL 4 - LBL 8. FABRICATED AND INSTALLED R EPAIR PARTS FROM BS 947.5, WL 208, LBL 4-RBL 65 IAW SRM 53-00-51. (M) 2 L 7 2 4F A16WE 1996082900701 19960829 00701 NM 1996 8 29 AWXA960359 1 19960710 A 5347 SEAT TRACK BOEING 737 737275 1384485 NM BS 987 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 CGBPW 20958 PAE - FLT 7820 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND CORROSION ON SEAT TRACK OF BS 987 TO 1016, WL 208 , RBL 38. REMOVED AND FABRICATED AND INSTALLED SEAT TRACK PER SRM 53-10-1. (M) 2 L 7 2 4F A16WE 1996082900702 19960829 00702 NM 1996 8 29 AWXA960360 1 19960710 A 5320 MOP SEAL BOEING 737 737275 1384485 NM BS 967-987 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 CGBPW 20958 PAE - FLT 7820 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND CORROSION ON AFT SERVICE DOOR MOP SEAL AT PREVIOU S REWORK AREAS, BS 967 TO BS 987, WL 208, RBL 53. REMOVED AND REPLACED MOP SEAL PER SRM 53-10-1. (M) 2 L 7 2 4F A16WE 1996082900703 19960829 00703 NM 1996 8 29 AWXA960361 1 19960720 A 5313 544063 STRINGER BOEING 737 737275 1384485 NM BS 360 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 CGBPW 20958 PAE - FLT 7820 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND CRACKED LWR FLANGE OF STRINGER 27L AT BS 360. RE MOVED DAMAGED HAT CHANNEL AT BS 360, STRINGER 27L, FABRICATED NEW CHANNEL, TREATED, PRIMED AND INSTALLED PER SRM 51-10-0 3. (M) 2 L 7 2 4F A16WE 1996082900704 19960829 00704 NM 1996 8 29 AWXA960362 1 19960720 A 5753 65464287 FLAP TRACK BOEING 737 737275 1384485 NM LT TE FLAP CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 CGBPW 20958 PAE - FLT 7820 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND CORROSION EMITTING FROM AFT MOUNT OF NR 2 FLAP TR ACK. REMOVED AND REPLACED NR 2 FLAP TRACK PER CARD R3L27003. (M) 2 L 7 2 4F A16WE 1996082900705 19960829 00705 NM 1996 8 29 AWXA960363 1 19960720 A 5753 65464288 FLAP TRACK BOEING 737 737275 1384485 NM LT TE FLAP CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 CGBPW 20958 PAE - FLT 7820 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND CORROSION EMITTING FROM AFT MOUNT OF NR 1 FLAP TR ACK. REMOVED AND REPLACED NR 1 FLAP TRACK PER R3L27002. (M) 2 L 7 2 4F A16WE 1996082900706 19960829 00706 NM 1996 8 29 AWXA960364 1 19960720 A 5753 65464289 FLAP TRACK BOEING 737 737275 1384485 NM RT TE FLAP CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 CGBPW 20958 PAE - FLT 7820 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND RIGHT WING OUTBOARD FLAP, INBOARD TRACK NR 7 VERY CORRODED WHERE FLAP TRACK ATTACHES TO LOWER WING PANEL REAR SPAR. REMOVED AND REPLACED NR 7 FLAP TRACK PER CARD R3R270 04. (M) 2 L 7 2 4F A16WE 1996082900707 19960829 00707 NM 1996 8 29 AWXA960365 1 19960725 A 3520 225047 FLOW CONTL UNIT BOEING 737 737275 1384485 NM CARGO COMPT INOPERATIVE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 CGBPW 2170 20958 PAE - FLT NR 7820 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, WHILE WORKING PASSENGER OXYGEN SYSTEM CHECK, FOUND E LECTRO-PNEUMATIC CONTINUOUS FLOW CONTROL UNIT AND FUNCTIONAL TEST GOOD IAW MM 35-21-21, 35-21-0. (M) 2 L 7 2 4F A16WE 1996082900708 19960829 00708 NM 1996 8 29 AWXA960366 1 19960725 A 5320 DOOR FRAME BOEING 737 737275 1384485 NM BS 794 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 CGBPW 20958 PAE - FLT 7820 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND CRACK ON FWD SIDE OF AFT CARGO DOOR FRAME, BS 794 , STRINGER 24R. FABRICATED REPAIR PARTS AFTER CONTAINMENT OF CRACK. INSTALLED REPAIR APRTS PER SRM 53-10-4. (M) 2 L 7 2 4F A16WE 1996082900709 19960829 00709 EU 1996 8 29 AWXA96042 1 19960719 A 3350 321454 BATTERY AIRBUS 320 A320231 3930325 EU MID FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 633AW 527 082 PHX - FLT 2266 - DURING ROUTINE MAINTENANCE CHECK, FOUND APPROXIMATELY EVERY 3RD FLOOR PROXIMITY SEAT LIGHT INOP. ALSO, LEFT OVERWING EXIT LIGHT INOP. BITE FAULTS LEFT BATTERIES. REMOVED AND REPLACED MID BATTERY. OPS CHECK AND BITE TEST ED GOOD. (M) 2 L 7 2 4F RT A28NM 1996082900710 19960829 00710 NM 1996 8 29 EISA96120 1 19960809 A 2612 CLAMP BOEING 727 727251 138408H NM NR 2 ENGINE LOOSE A EISA E ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 SW 07 263US 19982 FIRE WARNING BELL SOUNDED FOLLOWED BY ENGINE NR 2 FIRE WARNING LIGHT ILLUMINATED. ACCOMPLISHED ENGINE FAILRUE FIRE DAMA GE CHECKLIST. INSPECTED NR 2 ENGINE. NO EVIDENCE OF FIRE. SECURED 13TH STAGE BLEED DUCT CLAMP AT 12 O'CLOCK POSITION. RAN ENGINE, OPS AND LEAK CHECK GOOD. FIRE WARNING TESTED AND FOUND GOOD. CLEANED ENGINE AND REPLACED FIRE BOTTLE. ( M) 2 L 7 3 4F A3WE 1996082900711 19960829 00711 NM 1996 8 29 IXKA9600064 1 19960802 A 3250 APEX PIN BOEING 727 727225 1384077 NM NLG STEERING MALFUNCTIONED A IXKA K NONE O OTHER LD LANDING 1 EA 25 356PA 20626 FLT 99 - ATLANTA-LAS VEGAS - NOSE WHEEL STEERING DISCONNECTED ON LANDING ROLL OUT. RECONNECTED TORQUE LINKS PERFORMED H IGH DRAG SIDE LOAD LANDING INSPECTION. PERFORMED EXTENSION AND RETRACTION OPERATIONAL CHECK. PERFORMED NOSE WHEEL STEE RING TEST. REMOVED AND REPLACED NOSE WHEEL TIRES AND APEX PIN. APEX PIN UNDER INVESTIGATION. (M) 2 L 7 3 4F A3WE 1996082900712 19960829 00712 NM 1996 8 29 IXKA9600065 1 19960804 A 3350 1102833 LIGHT BOEING 727 727225 1384077 NM AFT STAIR INOPERATIVE A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 361KP 2723 20627 AFT STAIR OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY. (M) 2 L 7 3 4F A3WE 1996082900713 19960829 00713 NM 1996 8 29 IXKA9600066 1 19960804 A 3350 900542 BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 361KP 4729 20627 FOUND CENTER CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK. (M) 2 L 7 3 4F A3WE 1996082900714 19960829 00714 WP 1996 8 29 IXXA96123 1 19960806 A 3230 45973405505 UPLATCH DOUG DC8 DC863F 302198F WP LT MLG FAILED A IXXA O OTHER J WARNING INDICATION CR CRUISE 1 SW 11 786AL 572 46121 EN ROUTE FROM WRI-MDT, THE GEAR UPLATCH CHECK FAILED WITH THE GEAR NOT LATCHED LIGHT ILLUMINATED. AFTER AN UNEVENTFUL L ANDING, MAINTENANCE DETERMINED THE LEFT MAIN GEAR UPLATCH TO BE WORN AND AT FAULT. THE LEFT UPLATCH ASSEMBLY WAS REMOVE D, REPLACED, AND OPERATIONALLY CHECKED IAW DOUGLAS MM 32-30-0 AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 4 4F 4A25 1996082900715 19960829 00715 EU 1996 8 29 JBXA00016 1 19960806 A 2133 1037223 OUTFLOW VLV FOKKER F28 F28MK0100 4990807 EU CABIN FAILED A JBXA G O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 SO 05 109ML 4600 63452 11485 RDU - FLT 901 - LOST CABIN PRESSURIZATION CONTROL. BOTH CABIN PRESSURE CONTROLLERS FAULTED, TRIED TO CONTROL MANUALLY W ITH NO RESPONSE. ALL OXYGEN MASKS DEPLOYED. REPLACED PRIMARY OUTFLOW VALVE IAW AMM 21-51-03. OPS CHECK OF AUTO AND MA NUAL SYSTEM GOOD. (M) 2 L 7 2 4F RT 1996082900716 19960829 00716 NM 1996 8 29 ORJA9643 1 19960708 A 3260 INTERLOCK SWITCH DOUG MD90 MD9030 3023690 NM NLG FAILED A ORJA O OTHER N FALSE WARNING AP APPROACH 1 WP 11 902RA 53490 ON FINAL APPROACH TO SAN JOSE, NO NOSE GEAR GREEN LIGHT. NLG INDICATOR INDICATED DOWN AND LOCKED. REMOVED AND REPLACED NOSE LANDING GEAR INTERLOCK SWITCH IAW MM 32-61-02. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1996082900717 19960829 00717 NM 1996 8 29 PCAA9600297 1 19960702 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN LOOSE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 976HA 15918 217 THE EMERGENCY EXIT LIGHT ABOVE THE AIRSTAIR DOOR DOES NOT ILLUMINATE. INSPECTED AND FOUND CONNECTOR DISCONNECTED. RECO NNECTED CONNECTION. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1996082900718 19960829 00718 EU 1996 8 29 RAIA960742 1 19960730 A 5320 S5367131820001 FLOOR WEB AEROSP ATR72 ATR72202 8680940 EU FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 722TE 10848 220 FOUND FLOOR WEB AT STRINGER 15R HAS CORROSION. REMOVED AND REPLACED WEB. (M) 2 H 7 2 4T RT A53EU 1996082900719 19960829 00719 EU 1996 8 29 RAIA960743 1 19960730 A 3230 7445B CONTROL VALVE BAG JETSTM JETSTM3201 1500217 EU MLG FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 427AM 1663 876 STL - FLT 7422 - WITH GEAR SELECTED UP, MAIN GEAR DID NOT RETRACT. REPLACED GEAR CONTROL VALVE. (M) 2 L 7 2 4T RT A56EU 1996082900720 19960829 00720 EU 1996 8 29 RAIA960744 1 19960730 A 5313 S53671200218 STRINGER AEROSP ATR72 ATR72202 8680940 EU FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 722TE 10848 220 FOUND STRINGER 17 HAS CORROSION BETWEEN FRAME 36 AND 40 AND 41 TO 42. REPLACED STRINGER SECTION PER SRM 53-00-00 FIG 42 8. (M) 2 H 7 2 4T RT A53EU 1996082900721 19960829 00721 EU 1996 8 29 RAIA960745 1 19960730 A 5320 S5367121729402 FLOOR WEB AEROSP ATR72 ATR72202 8680940 EU FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 722TE 220 FOUND FLOOR WEB AT PASSENGER DOOR, BETWEEN FRAME 36 AND 39, HAS CORROSION. REPLACED WEB. (M) 2 H 7 2 4T RT A53EU 1996082900722 19960829 00722 EU 1996 8 29 RAIA960746 1 19960730 A 5313 S53671407210218 STRINGER AEROSP ATR72 ATR72202 8680940 EU FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 722TE 10848 220 FOUND STRINGER 21 HAS CORROSION AT FRAME 38 AND 39. REPLACED STRINGER SECTION. (M) 2 H 7 2 4T RT A53EU 1996082900723 19960829 00723 EU 1996 8 29 RAIA960747 1 19960730 A 5315 S5367240720201 FLOOR BEAM AEROSP ATR72 ATR72202 8680940 EU FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 722TE 10848 220 FOUND FLOOR BEAM 38 HAS CORROSION. REPLACED FLOOR BEAM. (M) 2 H 7 2 4T RT A53EU 1996082900724 19960829 00724 EU 1996 8 29 RAIA960748 1 19960730 A 5320 S536724080860 FRAME AEROSP ATR72 ATR72202 8680940 EU PAX DOOR CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 722TE 10848 220 FOUND FRAME 39 HAS CORROSION AT SERVICE AND PASSENGER DOORS AT FLOOR LEVEL. REPAIRED IAW SRM 53-61-40. (M) 2 H 7 2 4T RT A53EU 1996082900725 19960829 00725 EU 1996 8 29 RAIA960749 1 19960730 A 5320 S5367131828001 FLOOR WEB AEROSP ATR72 ATR72202 8680940 EU FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 722TE 10848 220 FOUND FLOOR WEB AT SERVICE DOOR, BETWEEN FRAMES 36 AND 39, HAS CORROSION. REPAIRED IAW SRM 53-61-00. (M) 2 H 7 2 4T RT A53EU 1996082900726 19960829 00726 EU 1996 8 29 RAIA960750 1 19960730 A 5320 5367800821602 CREASE BEAM AEROSP ATR72 ATR72202 8680940 EU FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 722TE 10848 220 FOUND CREASE BEAM BETWEEN FRAMES 39 AND 41 RIGHT SIDE HAS CORROSION. REMOVED AND REPLACED CREASE BEAM. (M) 2 H 7 2 4T RT A53EU 1996082900727 19960829 00727 EU 1996 8 29 RAIA960751 1 19960730 A 5315 S5367240820201 FLOORBEAM AEROSP ATR72 ATR72202 8680940 EU FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 722TE 220 FOUND FLOOR BEAM 39 HAS CORROSION. REPAIRED IAW SRM 53-00-00 PG 498.18 FIG 429. (M) 2 H 7 2 4T RT A53EU 1996082900728 19960829 00728 EU 1996 8 29 RAIA960752 1 19960730 A 5320 S5367240700460 FRAME AEROSP ATR72 ATR72202 8680940 EU SERVICE DOOR CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 722TE 10848 220 FOUND FRAME 38 HAS CORROSION AT SERVICE DOOR. REPAIRED IAW SRM 53-67-70. (M) 2 H 7 2 4T RT A53EU 1996082900729 19960829 00729 EU 1996 8 29 RAIA960753 1 19960730 A 5315 S5367240600861 FLOOR BEAM AEROSP ATR72 ATR72202 8680940 EU FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 722TE 220 FOUND FLOOR BEAM 36 HAS CORROSION. REPAIRED IAW SRM 53-00-00 PG 498. (M) 2 H 7 2 4T RT A53EU 1996082900730 19960829 00730 EU 1996 8 29 RAIA960754 1 19960730 A 5210 S5217600103400 STRUCTURE AEROSP ATR72 ATR72202 8680940 EU PAX DOOR CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 722TE 10848 220 FOUND CORROSION IN PASSENGER DOOR STRUCTURE. REMOVED AND REPLACED DOOR. (M) 2 H 7 2 4T RT A53EU 1996082900731 19960829 00731 EU 1996 8 29 RAIA960755 1 19960730 A 5320 S53671257206 INTERCOSTAL AEROSP ATR72 ATR72202 8680940 EU FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 722TE 10848 220 FOUND INTERCOSTAL, BETWEEN FRAME 35 AND 40, HAS CORROSION. REMOVED AND REPLACED INTERCOSTAL SECTIONS. (M) 2 H 7 2 4T RT A53EU 1996082900732 19960829 00732 EU 1996 8 29 RAIA960757 1 19960730 A 5320 S5367131820001 FLOOR WEB AEROSP ATR72 ATR72202 8680940 EU FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 722TE 10848 220 FLOOR WEB AT STRINGER 15R HAS CORROSION. REMOVED AND REPLACED WEB. (M) 2 H 7 2 4T RT A53EU 1996082900733 19960829 00733 EU 1996 8 29 RAIA960801 1 19960801 A 3260 9005EN38 SWITCH BAG JETSTM JETSTM3201 1500217 EU RT MLG FAILED A RAIA A UNSCHED LANDING N FALSE WARNING LD LANDING 1 CE 03 422AM 11797 856 EVV - FLT 7427 - RIGHT MAIN GEAR INDICATING INTRANSIT WITH GEAR EXTENDED. MAINTENANCE REPLACED RIGHT MAIN UPLOCK SWITCH . (M) 2 L 7 2 4T RT A56EU 1996082900734 19960829 00734 EU 1996 8 29 RAIA960802 1 19960804 A 3260 9005EN38 SWITCH BAG JETSTM JETSTM3201 1500217 EU LT MLG FAILED A RAIA A UNSCHED LANDING N FALSE WARNING LD LANDING 1 CE 03 422AM 11801 856 CMI - FLT 7449 - UPON EXTENSION LEFT GEAR WOULD INDICATE DOWN AND LOCKED. MAINTENANCE REPLACED THE LEFT MAIN UPLOCK SWI TCH. (M) 2 L 7 2 4T RT A56EU 1996082900735 19960829 00735 EU 1996 8 29 RAIA960803 1 19960805 A 2150 ASNA214507 CLAMP AEROSP ATR72 ATR72202 8680940 EU LT PACK LOOSE A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 723TE 9187 283 STL - FLT 7164 - LEFT DUCT TEMP IS 35 TO 38 DEGREES CELSIUS WOULD NOT COOL THE CABIN OR COCKPIT. MAINTENANCE TIGHTENED THE CLAMPS AT THE COOLING TURBINE. (M) 2 H 7 2 4T RT A53EU 1996082900736 19960829 00736 NE 1996 8 29 RAIA960805 2 19960805 A 7261 30607081 FILTER JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE RT ENGINE CONTAMINATED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 567HK 198 41085 75075 STL - FLT 7514 - RIGHT ENGINE OIL CONTAMINATION LIGHT CAME ON. MAINTENANCE PERFORMED SOAP SAMPLE, PERFORMED PENALTY RUN S, AND REPLACED FILTER. OPS CHECK GOOD. (M) 2 L 7 2 4T 4 T RT A41NM E18NE 1996082900737 19960829 00737 EU 1996 8 29 RAIA960806 1 19960806 A 2910 1379305A155 FLEX LINE BAG JETSTM JETSTM3201 1500217 EU LT MLG LOOSE A RAIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CE 03 340TE 8835 939 STL - FLT 7432 - TOTAL LOSS OF HYDRAULIC PRESSURE FROM BOTH PUMPS. MAINTENANCE TIGHTENED FLEX LINE AT THE LEFT MLG RADI US ROD. (M) 2 L 7 2 4T RT A56EU 1996082900738 19960829 00738 EU 1996 8 29 RAIA960807 1 19960808 A 3260 9EN1C11HB2BB2 UPLOCK SWITCH BAG JETSTM JETSTM3201 1500217 EU LT MLG FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 432AM 11415 883 EVV - FLT 7430 - LEFT MAIN INTRANSIT LIGHT ILLUMINATED WITH GEAR UP AND LOCKED. MAINTENANCE REPLACED THE LEFT MAIN GEAR UPLOCK SWITCH. PERFORMED GEAR SWINGS, OPS CHECK GOOD. (M) 2 L 7 2 4T RT A56EU 1996082900740 19960829 00740 EU 1996 8 29 RAIA960813 1 19960812 A 7931 1241013 TRANSDUCER BAG JETSTM JETSTM3201 1500217 EU RT ENGINE STUCK A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 343TE 11713 2451 955 STL - FLT 7364 - RIGHT ENGINE OIL PRESSURE INDICATION PEGGED OUT. MAINTENANCE REPLACED THE RIGHT OIL PRESSURE TRANSDUCE R. (M) 2 L 7 2 4T RT A56EU 1996082900741 19960829 00741 EU 1996 8 29 RAIA960814 1 19960812 A 3260 9005EN38 UPLOCK SWITCH BAG JETSTM JETSTM3201 1500217 EU NLG STUCK A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 342TE 8471 954 STL - FLT 7344 - NOSE GEAR INTRANSIT LIGHT STAYED ILLUMINATED WITH THE GEAR UP AND LOCKED. MAINTENANCE REPLACED THE NOS E GEAR UPLOCK SWITCH. (M) 2 L 7 2 4T RT A56EU 1996082900742 19960829 00742 EU 1996 8 29 RAIA960815 1 19960812 A 7722 8974694 SHORT LEAD BAG JETSTM JETSTM3201 1500217 EU LT ENG EGT SHORTED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 436AM 891 STL - FLT 7344 - LEFT ENGINE EGT DROPPED TO ZERO ON TAKEOFF ROLL. MAINTENANCE REPLACED THE LEFT ENGINE EGT SHORT LEAD. PERFORMED GROUND RUNS. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A56EU 1996082900743 19960829 00743 NE 1996 8 29 SIMA962191 2 19960806 A 7321 8108001002 EEC AEROSP ATR72 ATR72212 EU PWA PW120 PW127 NE NR 2 ENGINE FAILED A SIMA A UNSCHED LANDING J X WARNING INDICATION ENGINE FLAMEOUT CL CLIMB 1 SW 21 414WF 94010009 414 127083 ORD - FLT 4381 - DURING CLIMB NR 2 ENGINE TORQUE FLUCTUATED BETWEEN 70 AND 100 PERCENT AT ONE POINT. THE TORQUE DROPPED TO ZERO THEN THE ENGINE RELIT, PROP SYNC WAS TURNED OFF WITH NO EFFECT. AIRCRAFT RETURNED TO ORD WITHOUT FURTHER INCID ENT. RAI'D NR 2 ENGINE. EEC OPS CHECK GOOD ON FCF. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1996082900744 19960829 00744 NE 1996 8 29 SIMA962192 2 19960806 A 7200 ENGINE AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE LEFT FAILED A SIMA A E UNSCHED LANDING ENGINE SHUTDOWN B X SMOKE/FUMES/ODORS/SPARKS ENGINE FLAMEOUT CL CLIMB 1 SW 21 246AE 13838 243 120148 DFW - FLT 3623 - LEFT ENGINE FAILED IN FLIGHT. PRIOR TO SHUTDOWN SMELL OF SMOKE IN CABIN COCKPIT. POSSIBLE COMPRESSOR STALL NOTICED AS AIRCRAFT CLIMBED OUT. ENGINE BEING REMOVED AND RETURNED TO PWA FOR EVALUATION. NEW ENGINE INSTALLED A S PER AMM AND WORK CARD. OPERATIONAL CHECKS GOOD. NO EVIDENCE OF SMOKE SMELL NOTED DURING OPS CHECK OF ENGINE. AIRCRA FT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1996082900745 19960829 00745 NM 1996 8 29 TAOA079608 1 19960731 A 3233 65542141 GEAR HANDLE BOEING 727 727225 1384077 NM COCKPIT DIRTY A TAOA K NONE N FALSE WARNING AP APPROACH 1 EA 15 919TS 20447 EXTENDED LANDING GEAR AND HAD INDICATION OF THREE GREEN AND THREE REDS. NO THUMPING NOISE OR LOSS OF HYDRAULIC FLUID. C YCLED GEAR AND RECEIVED INDICATION OF THREE GREEN. CLEANED SWITCHES ON LANDING GEAR HANDLE, OPERATIONAL CHECK NORMAL I AW MM CH 32-30-00. (M) 2 L 7 3 4F A3WE 1996082900746 19960829 00746 NM 1996 8 29 TSAA9653064 1 19960814 A 5330 SKIN BOEING 737 7372Q9 138448M NM BS 767 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 809AL 21720 DISCOVERED FUSELAGE SKIN CRACK AT BS 767 AND STRINGER 19L, APPROXIMATELY 1.5 INCH IN LENGTH CONFIRMED BY HFEC. REPAIRED PER SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1996082900747 19960829 00747 NM 1996 8 29 TSAA9653065 1 19960814 A 5330 SKIN BOEING 737 7372Q9 138448M NM BS 882 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 809AL 21720 DISCOVERED FUSELAGE SKIN CRACK AT BS 882 AND STRINGER 24R. APPROXIMATELY 3.5 INCHES IN LENGTH. HFEC CONFIRMED CRACK. R EPAIRED PER SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1996082900748 19960829 00748 NM 1996 8 29 TWRA96202 1 19960724 A 3350 CL307 BULB BOEING 747 747121 1384871 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 604FF 19659 DURING DAILY CHECK, FOUND EVAC OVERWING LEFT SIDE AND RIGHT SIDE. FIRST LIGHT FROM BOTTOM INOP. RELAMPED, OPS CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996082900749 19960829 00749 NM 1996 8 29 TWRA96204 1 19960721 A 3350 CONNECTOR BOEING 747 747121 1384871 NM CABIN LOOSE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 609FF 20354 DURING DAILY CHECK, FOUND L1 MED UPPER BUSTLE EVAC LIGHT INOP. FOUND CANNON PLUG OFF OF BUSTLE. RECONNECTED, OPS CHECK NORMAL PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996082900750 19960829 00750 NM 1996 8 29 TWRA96205 1 19960721 A 3350 CL307 BULB BOEING 747 747121 1384871 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 609FF 20354 DURING DAILY CHECK, FOUND SEAT 45C EVAC LIGHT INOP. REPLACED BULB, OPS CHECK NORMAL PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996082900751 19960829 00751 NM 1996 8 29 TWRA96206 1 19960719 A 3350 CL307 BULB BOEING 747 747121 1384871 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 609FF 20354 DURING DAILY CHECK, FOUND UPPER DECK CREW DOOR EXIT LIGHT OUT OF SERVICE. RELAMPED, OPS CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996082900752 19960829 00752 NM 1996 8 29 TWRA96207 1 19960719 A 3350 TERMINAL BOEING 747 747121 1384871 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 609FF 20354 DURING DAILY CHECK, FOUND LEFT SIDE STATION 1600 EXTERIOR EMERGENCY LIGHTS INOP. REPLACED TERMINAL. OPS CHECK OK PER M M 33-51-00. (M) 2 L 7 4 4F A20WE 1996082900756 19960829 00756 NM 1996 8 29 TWRA96212 1 19960721 A 3350 1317 BULB BOEING 747 747259B NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 EICEO 21730 DURING DAILY CHECK, FOUND EVAC LIGHT RIGHT SIDE OVERWING SECOND FROM BOTTOM INOP. REPLACED BULB, OPS CHECK OK PER MM 33 -51-00. (M) 2 L 7 4 4F RT A20WE 1996082900757 19960829 00757 NM 1996 8 29 TWRA96213 1 19960721 A 3350 1317 BULB BOEING 747 747259B NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 EICEO 21730 DURING DAILY CHECK, FOUND EVAC LIGHT NEXT TO UPPERDECK LAVATORY EXIT SIGN INOP. RELAMPED, OPS CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F RT A20WE 1996082900758 19960829 00758 NM 1996 8 29 TWRA96216 1 19960726 A 3350 S1356B37 BATTERY PACK BOEING 747 747136 1384883 NM CABIN DISCHARGED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 606FF 20273 DURING DAILY CHECK, FOUND CEILING EXIT SIGN AT 32 ABC AND 35 ABC FORWARD INOP. REPLACED BATTERY PACK. OPS CHECKED OK P ER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996082900759 19960829 00759 NM 1996 8 29 TWRA96222 1 19960725 A 3350 07912 LENS BOEING 747 747238B 1384828 NM CABIN MISSING A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 607PE 20011 DURING DAILY CHECK, FOUND EVAC LIGHT AND LENS MISSING AT 21K, 31K, 56K, 60K. REPLACED LENS AND BULB. OPS CHECKED OK PE R MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996082900760 19960829 00760 NM 1996 8 29 TWRA96223 1 19960724 A 3397 WIRE BOEING 747 747282B 1384860 NM CABIN BROKEN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 610FF 20501 DURING DAILY CHECK, FOUND 5L MED EMERGENCY LIGHT INOP. REPAIRED WIRING. OPS CHECKED OK PER IAW 33-51-00. (M) 2 L 7 4 4F A20WE 1996082900761 19960829 00761 NM 1996 8 29 TWRA96224 1 19960724 A 3350 58801 STRIP BOEING 747 747282B 1384860 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 610FF 20501 DURING DAILY CHECK, FOUND C-ZONE EMERGENCY LIGHT (R/S) INOP. REPLACED B-ZONE GALLEY STRIP. OPS CHECKED NORMAL PER MM 3 3-51-00. (M) 2 L 7 4 4F A20WE 1996082900762 19960829 00762 NM 1996 8 29 TWRA96225 1 19960724 A 3397 WIRE BOEING 747 747282B 1384860 NM CABIN BROKEN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 610FF 20501 DURING DAILY CHECK, FOUND R1 MED EMERGENCY LIGHT INOP. REPAIRED WIRE, OPS CHECKED GOOD PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996082900763 19960829 00763 NM 1996 8 29 TWRA96226 1 19960724 A 3350 LIGHTS BOEING 747 747282B 1384860 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 610FF 20501 DURING DAILY CHECK, FOUND EMERGENCY OVERWING LIGHTS INOP, (BOTH SIDES). REPAIRED WIRES, OPS CHECKED GOOD PER MM 33-51-0 0. (M) 2 L 7 4 4F A20WE 1996082900764 19960829 00764 NM 1996 8 29 TWRA96227 1 19960723 A 3350 ML7715 BULB BOEING 747 747130 1384880 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 603FF 19746 DURING DAILY CHECK, FOUND 30C SEAT EMERGENCY LIGHT INOP. RELAMPED, OPS CHECKED OK PER MM 33-51-00 PG 501. (M) 2 L 7 4 4F A20WE 1996082900765 19960829 00765 1996 8 29 TWRA96235 4 19960729 A 2565 7A110424 SLIDE BFGOODRICH BOEING 747 747131 1384881 NM CREW DOOR MALFUNCTIONED A TWRA K NONE O OTHER IN INSP/MAINT 1 EA 15 608FF 376 19672 UPPER DECK CREW DOOR SLIDE FAILED TO DEPLOY CORRECTLY DURING TEST. AIRCRAFT GOING THROUGH 'D' SERVICE. SLIDE WILL BE R EPLACED DURING SERVICE. (M) 2 L 7 4 4F A20WE 1996082900766 19960829 00766 NE 1996 8 29 TWRA96249 2 19960731 A 7261 OIL LINE BOEING 747 747212B 1384886 NM PWA JT9 JT9D7Q 52054 NE NR 1 ENGINE LOOSE A TWRA E A ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CR CRUISE 1 EA 15 616FF 21939 702332 DURING FLIGHT, ENGINE OIL PRESSURE LIGHT NR 1 FLICKERED, NR 1 OIL PRESSURE INDICATOR 30-40 PSI. NR 1 OIL QTY INDICATOR ZERO. SHUT DOWN ENGINE NR 1 IMMEDIATELY PER FM VOL NR 1, FLEW APPROX 1 HOUR 25 MINUTES WINDMILLING AT N1-28 PERCENT, N2 -23 PERCENT, OIL PRESSURE 2-3 PSI. (AIRCRAFT FERRYING FROM FRA TO TLV). MAINTENANCE FOUND SCAVENGE LINE SCREW BACKED O FF. SCAVENGE LINE ADAPTER COMING LOOSE ON ANGLE GEARBOX. REMOVED FITTING AND REPLACED O-RINGS. REPLACED MAIN OIL SCRE EN CHIP DETECTORS, CHECKED NORMAL. PERFORMED HIGH POWER RUN, FOUND NO OIL LEAKS. ALSO, REPLACED STARTER AND STARTER VA LVE, PER MM 80-10-00. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 4 4F 4 F A20WE E3NE 1996082900767 19960829 00767 NM 1996 8 29 TWRA96250 1 19960801 A 3350 CM7265 BULB BOEING 747 747238B 1384828 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 614FF 20534 DURING DAILY CHECK, FOUND EVAC LIGHT FLOOR AT SEAT 25H BLINKS AND REMAINS OUT SEVERAL SECONDS. RELAMPED, OPS CHECK OK P ER MM 33-51-00 PG 501. (M) 2 L 7 4 4F A20WE 1996082900768 19960829 00768 NM 1996 8 29 TWRA96251 1 19960801 A 3350 07912 LENS BOEING 747 747259B NM CABIN MISSING A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 EICEO 21730 DURING DAILY CHECK, FOUND 11H FLOOR EMERGENCY LIGHT IS INOP AND LENS IS MISSING. REPLACED LIGHT LENS AND BULB AT SEAT 1 1H. OPS CHECKED OK PER MM 33-51-00. (M) 2 L 7 4 4F RT A20WE 1996082900769 19960829 00769 NM 1996 8 29 TWRA96252 1 19960731 A 3350 LIGHT BOEING 747 747136 1384883 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 606FF 20273 DURING DAILY CHECK, FOUND UPPER DECK STAIRWAY EXIT EMERGENCY LIGHT IS INOP AND 4C THROUGH 6C. FOUND WATER AT BOTTOM OF STAIRS. DRIED WATER. OPS CHECKED UPPER DECK STAIRWAY EXIT EMERGENCY LIGHT, OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996082900770 19960829 00770 NM 1996 8 29 TWRA96253 1 19960730 A 3350 1317 BULB BOEING 747 747238B 1384828 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 614FF 20534 DURING DAILY CHECK, FOUND RT WING NR 4 OVERWING EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED NR 4 FORWARD ON RIGHT SID E OVERWING LIGHT. OPS CHECKED OK PER MM 33-51-00 PG 501. (M) 2 L 7 4 4F A20WE 1996082900771 19960829 00771 NM 1996 8 29 TWRA96254 1 19960730 A 3350 07912 LENS BOEING 747 747238B 1384828 NM CABIN MISSING A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 607PE 20011 DURING DAILY CHECK, FOUND FLOOR EVAC LIGHT AT SEAT 22H INOP. REPLACED LENS AND BULB. OPS CHECKED OK PER MM 33-51-00 PG 501. (M) 2 L 7 4 4F A20WE 1996082900772 19960829 00772 NM 1996 8 29 TWRA96255 1 19960730 A 3350 18622114 SWITCH BOEING 747 747136 1384883 NM CABIN MALFUNCTION A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 606FF 20273 DURING DAILY CHECK, FOUND EMERGENCY LIGHT TEST SWITCH NEXT TO L1 MED DOES NOT SHUT OFF. REPLACES SWITCH L1 DOOR FOR EME RGENCY LIGHTS. OPS CHECKED OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996082900774 19960829 00774 NM 1996 8 29 TWRA96257 1 19960731 A 3350 1317 BULB BOEING 747 747124 1384874 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 602FF 19734 DURING DAILY CHECK, FOUND NR 4 RIGHT MED UPPER FORWARD SILL CEILING EMERGENCY LIGHT INOP. RELAMPED, OPS CHECKED GOOD PE R MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996082900775 19960829 00775 NM 1996 8 29 TWRA96258 1 19960801 A 3397 WIRE BOEING 747 747238B 1384828 NM CABIN BROKEN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 607PE 20011 DURING DAILY CHECK, FOUND EMERGENCY EVAC LIGHT INOP AT ROW 7H. RESPLICED WIRE. OPS CHECKED NORMAL AS PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996082900776 19960829 00776 NM 1996 8 29 TWRA96259 1 19960801 A 3350 ML7715 BULB BOEING 747 747212B 1384886 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND EVAC LIGHT INOP AT 11C, 12C, 53C, 58C, 61H. RELAMPED, OPS CHECKED GOOD AS PER MM 33-51-00 PG 501. (M) 2 L 7 4 4F A20WE 1996082900777 19960829 00777 NM 1996 8 29 TWRA96260 1 19960801 A 3350 ML7715 BULB BOEING 747 747212B 1384886 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 619FF 21316 DURING DAILY CHECK, FOUND SEAT MOUNTED EMERGENCY LIGHT INOP. RELAMPED SEAT 60 HJK. OPS CHECKED NORMAL AS PER MM 33-51- 00. (M) 2 L 7 4 4F A20WE 1996082900778 19960829 00778 NM 1996 8 29 TWRA96262 1 19960804 A 3350 ML7715 BULB BOEING 747 747238B 1384828 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 614FF 20534 DURING DAILY CHECK, FOUND FLOOR EMERGENCY LIGHT INOP AT 5C, 39H, 42C. RELAMPED, OPS CHECKED OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996082900779 19960829 00779 NM 1996 8 29 TWRA96263 1 19960804 A 3350 1317 BULB BOEING 747 747282B 1384860 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 611FF 20502 DURING DAILY CHECK, FOUND RIGHT WING NR 3 OVERWING EMERGENCY LIGHT ONE BULB INOP. RELAMPED, OPS CHECKED OK PER MM 33-51 -00 PAGE 501. (M) 2 L 7 4 4F A20WE 1996082900781 19960829 00781 NM 1996 8 29 USAA960545 1 19960704 A 5330 SKIN BOEING 737 7372Q9 138448M NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 231US 43667 21976 BOS - DETECTED BY VISUAL AND EDDY CURRENT AND 4.25 INCH CRACK IN SKIN AT STATION 727B AT STRINGER 15R. INSTALLED DOUBLE R 13.375 INCH BY 8.5 INCH PER SRM REFERENCE 53-30-3 PAGE 12B. (M) 2 L 7 2 4F A16WE 1996082900782 19960829 00782 1996 8 29 USAABB96021 4 19960728 A 2565 SLIDE BOEING 767 767201 1385125 NM RT OVERWING SELF-ACTUATED A USAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 19 645US 23897 AFTER COMPLETION OF ANNUAL INFLATION/ACTUATIONS TEST, MAINTENANCE REPLACED THE RIGHT OVERWING ESCAPE SLIDE. UPONC OMPLE TION OF THE REPLACEMENT, THE SIDE SELF-ACTUATED INSIDE THE COMPARTMENT. MAINTENANCE REPLACED THE SLIDE. THE INCIDENT O CCURRED DUE TO IMPROPER INSTALLATION. (X) 2 L 7 2 4F RT A1NM 1996082900783 19960829 00783 NM 1996 8 29 USAABB96022 1 19960729 A 3350 1010741D SIGN BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 620AU 27199 PHL - EMERGENCY EXIT LOCATOR SIGN AT L2/R2 DEFECTIVE. REPLACED EXIT SIGN. (M) 2 L 7 2 4F RT A2NM 1996082900784 19960829 00784 NM 1996 8 29 USAABB96023 1 19960731 A 5400 313T21002 FAIRING BOEING 767 7672B7 1385107 NM LT PYLON DISLODGED A USAA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 EA 19 656US 26847 CLT - FLT 41 - CREW NOTED, THAT SOMEWHERE BETWEEN TAKEOFF FROM CLT AND 8000 FEET, A NR 1 ENGINE PYLON COVER DEPARTED THE AIRCRAFT. FLIGHT RETURNED TO THE FIELD AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE PANEL. SUBMITTE R STATES, MOST LIKELY CAUSE OF INCIDENT WOULD BE IMPROPER REPLACEMENT AFTER PREVIOUS MAINTENANCE. (M) 2 L 7 2 4F RT A1NM 1996082900785 19960829 00785 EU 1996 8 29 USAAF96082 1 19960801 A 4950 40742250F FLEX DUCT FOKKER F28 F28MK0100 4990807 EU APU LEAKING A USAA F ACTIVATE FIRE EXT. J WARNING INDICATION DE DESCENT 1 EA 19 887US 11349 GRR - FL 862 - UPON DESCENT INTO GRR, CREW RECEIVED APU FIRE WARNING. APU WAS AUTOMATICALLY SHUT DOWN AND THE FIRE BOTT LE DISCHARGED. FLIGHT CONTINUED TO GRR AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF A FIRE. A BLEED AIR LEAK WAS FOUND AT THE LOAD CONTROL VALVE FLEX JOINT DUCT ASSEMBLY. (M) 2 L 7 2 4F RT 1996082900786 19960829 00786 EU 1996 8 29 USAAF96084 1 19960801 A 3260 201251230 SQUAT SW FOKKER F28 F28MK0100 4990807 EU LT MLG FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 869US 11314 FLT 1025 - PIT-ABE - AFTER TAKEOFF, PILOT TRIED TO RAISE GEAR. RECEIVED GRD/FTL CONTROLS, TCAS, AND LIFT DUMPER MESSAGE S. RETURNED TO FIELD. MAINTENANCE REPLACED LEFT INBOARD GND/FLT SENSOR. CYCLED GEAR SEVERAL TIMES. ALL CHECKS NORMAL . (M) 2 L 7 2 4F RT 1996082900787 19960829 00787 EU 1996 8 29 USAAF96085 1 19960801 A 5220 D90058703 ARMREST FOKKER F28 F28MK0100 4990807 EU RT EMER DOOR BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 898US 11398 CLT - BROKEN ARMREST ON THE RIGHT OVERWING EMERGENCY EXIT. MAINTENANCE REPLACED THE ARMREST. (M) 2 L 7 2 4F RT 1996082900788 19960829 00788 1996 8 29 USAAF96086 4 19960805 A 3425 6227485421 EFIS FOKKER F28 F28MK0100 4990807 EU LEFT FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 869US 8590 11314 GSP-LGA - FLT 926 - DURING CLIMB-OUT OF GSP, NR 1 NAV DISPLAY LOCKED UP. CAPTAIN WAS UNABLE TO SWITCH TO ROSE OF SELECT HEADING. FLIGHT DIVERTED TO CLT. NO EMERGENCY DECLARED AND FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLA CED LEFT EFIS CONTROL PANEL. OPERATIONAL CHECK WAS GOOD. (M) 2 L 7 2 4F RT 1996082900789 19960829 00789 NM 1996 8 29 USAASB96147 1 19960806 A 3350 AD20131A BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 434US 24556 TPA - MAINTENANCE FOUND THE LEFT AND RIGHT AFT PASSENGER EMERGENCY EVACUATION LIGHTING INOP. MAINTENANCE REMOVED AND RE PLACED THE AFT LEFT AND RIGHT BATTERY PACKS. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996082900790 19960829 00790 NM 1996 8 29 USAASB96148 1 19960806 A 5210 90100722 SNUBBER BOEING 737 737201 1384454 NM PAX DOOR MISINSTALLED A USAA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 EA 19 235US 22275 PHL - FL 351 - DURING CLIMB-OUT, FLIGHT ATTENDANT REPORTED AN EXCESSIVE NOISE COMING FROM THE FORWARD MAIN ENTRANCE DOOR . THE CAPTAIN INDICATED THE CABIN WAS PRESSURIZING TOO SLOWLY AND DECIDED TO RETURN TO THE FIELD AT PHL. THE FLIGHT LA NDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE FORWARD MAIN ENTRANCE DOOR SNUBBER INSTALLED IN THE WRONG POSITION . REPOSITIONED DOOR SNUBBER AS PER MM. PRESSURIZATION CHECK AND OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1996082900794 19960829 00794 EU 1996 8 29 VTZA96285 1 19960805 A 2710 4006719906 SERVO JETAIR JETSTM JETSTM4101 1500501 EU AILERONS MALFUNCTION A VTZA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 EA 27 436JX 41036 FLT NR 6266 - IAD- BTV - DURING CRUISE, MADE A UNSCHEDULED LANDING DUE TO UNCOMMANDED INPUT FROM THE AILERONS. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED SERVO, OPS CHECK OK. AIRCRAFT WAS RELEASED A ND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996082900795 19960829 00795 NE 1996 8 29 VTZA96286 2 19960731 A 7260 5725109162 CHIP DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE RT ENGINE DIRTY A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 305UE 41019 P76021C FLT NR 6345 - IAD-LGA - DURING CRUISE, RETURNED TO IAD DUE TO THE RIGHT ENGINE OIL CONTAMINATION LIGHT ILLUMINATING IN F LIGHT. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE INSPECTED CHIP DETECTOR AND FOUND CHIP WITHIN LIM ITS AND C/W SOAP SAMPLE. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 4 T RT A41NM E18NE 1996082900796 19960829 00796 1996 8 29 VTZA96287 4 19960731 A 3421 4020531574 ADI BAG JETSTM JETSTM3201 1500217 EU RT COCKPIT FAILURE A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 494UE 810 FLT NR 6515 - JFK-ROC - DURING CLIMB, RETURNED TO IAD DUE TO FLIGHT OFFICERS ADI FAILED. AIRCRAFT RETURNED WITH NO FURT HER INCIDENTS. MAINTENANCE REMOVED AND REPLACED ADI. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO S ERVICE. (M) 2 L 7 2 4T RT A56EU 1996082900797 19960829 00797 1996 8 29 VTZA96288 4 19960731 A 3442 6227337001 R/T UNIT BAG JETSTM JETSTM3201 1500217 EU RADAR FAILED A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 481UE 895 FLT NR 6405 - IAD-HPN - DURING CLIMB, RETURNED TO IAD DUE TO WX RADAR FAILED IN FLIGHT. AIRCRAFT RETURNED TO GATE AT IA S WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED RADAR R/T. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPR OVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996082900798 19960829 00798 NE 1996 8 29 VTZA96290 2 19960806 A 7260 5725109162 CHIP DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE LT ENGINE DIRTY A VTZA K NONE J WARNING INDICATION CR CRUISE 1 EA 27 306UE 41020 FLT NR 6356 - BOS-IAD - LANDED AT IAD AS SCHEDULED WITH A LEFT ENGINE OIL CONTAMINATION LIGHT. AIRCRAFT WENT TO THE GAT E NO FURTHER INCIDENTS. MAINTENANCE REMOVED SMALL AMOUNT OF FUZZ ON CHIP DETECTOR. ALSO, CLEANED AND GROUND RAN AIRCRA FT, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 4 T RT A41NM E18NE 1996082900799 19960829 00799 NM 1996 8 29 W8PA960105 1 19960813 A 3350 CONNECTORS BOEING 737 7373Y0 1384671 NM CABIN LOOSE A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 955WP 24463 FOUND EMERGENCY TRACK LIGHTING BETWEEN ROWS 12 AND 16 INOP. TIGHTENED CONNECTORS. (M) 2 L 7 2 4F RT A16WE 1996083000001 19960830 00001 NM 1996 8 30 AALA961112 1 19960725 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 682 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 867AA 53337 21372 FOUND STRINGER 27 RIGHT CORRODED. REMOVED CORRODED AREA, INSTALLED SPLICE PER SRM 53-10-3 FIG 1. (M) 2 L 7 3 4F A3WE 1996090300001 19960903 00001 EU 1996 9 3 96FDEA01390 1 19960821 A 2450 TRANSFORMER AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680C2A5 NE E/E COMPT FAILED A FDEA A E UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 SO 25 660FE 759 ECAM ANNUNCIATED ENGINE ALERT AND SHOWED ZERO OIL PRESSURE ACCOMPANIED BY ZERO OIL PRESSURE ON COCKPIT GAUGE NR 2 ENGINE SHUTDOWN AS A PRECAUTION IN ACCORDANCE WITH EMERGENCY PROCEDURE. REF WRI 22-10/1361, REMOVED AND REPLACED C/B 6XN AND 26 VOLT TRANSFORMER. REMOVED AND REPLACED TRANSFORMER PER 24-51-11-4, RAN ENGINE PER JRH VOLTS AND FREQ NORMAL. 2 L 7 2 4F 4 F RT A35EU E13NE 1996090300002 19960903 00002 NM 1996 9 3 TWRA96164 1 19960715 A 3350 07912 LENS BOEING 747 747212B 1384886 NM CABIN BROKEN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 620FF 21162 DURING DAILY CHECK, FOUND BROKEN EVAC LIGHTS AT SEAT 27C.REPLACED EMERGENCY LIGHT CAP AND BULB. OPS CHECK OK PER MM 33- 51-00.(M) 2 L 7 4 4F A20WE 1996090300003 19960903 00003 NM 1996 9 3 TWRA9685 1 19960628 A 3350 3004801 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY SERVICE, FOUND L1 MED BUSTLE 'EVAC' LIGHTINOPERATIVE. REMOVED AND REPLACED BUSTLE LIGHT ASSY. OPS CHECK N ORMAL MM33-51-00. (M) 2 L 7 4 4F A20WE 1996090300004 19960903 00004 1996 9 3 TAOA079609 4 19960731 A 2565 1061474175 SLIDE BOEING 727 727225 1384077 NM L1 DOOR LOW PRESSURE A TAOA K NONE O OTHER IN INSP/MAINT 1 EA 15 919TS 20447 L-1 EMERGENCY ESCAPE SLIDE AIR PRESSURE LOW. REPLACED L-1 SLIDE. (M) 2 L 7 3 4F A3WE 1996090500001 19960905 00001 WP 1996 9 5 ARWA9608009 1 19960817 A 5720 ANGLE DOUG DC8 DC863 302198A WP WS 255 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 ONE INCH CRACK RT WING EXHAUST GATE INBOARD LOWER ANGLE XRS 255. REPAIRED EXHAUST GATE PER DC-8 SRM 57-2-1. FORMED DOU BLER AND INSTALLED PER DC-8 SRM'S 57-7-1, 51-1-4, 51-1-8 AND 51-1-21. 2 L 7 4 4F 4A25 1996090500002 19960905 00002 CE 1996 9 5 96ZZZX4198 1 19960802 A 2612 FIRE LOOP LEAR 35 35A 5170602 CE NR 2 ENGINE DIRTY CONNECTOR A AOQA F E ACTIVATE FIRE EXT. ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 EA 11 719JB 166 EN ROUTE JAN TO SGF, NR 2 ENGINE FIRE WARNING ILLUMINATED. PEFORMED ENGINE FIRE SHUT-DOWN PROCEDURES ON NR 2 ENGINE. D ISCHARGED NR 1 FIRE BOTTLE, AIRCRAFT LANDED AT SGF WITHOUT INCIDENT. INSPECTED NR 2 ENGINE FIRE LOOPS, NO DISCREPANCIES FOUND. FIRE WARNING SYSTEM OPERATING NORMAL. CLEANED NR 2 ENGINE FIRE LOOP CONNECTORS. INSTALLED REPLACEMENT NR 1 FI RE BOTTLE. AIRCRAFT RETURNED TO ISP. PERFORMED DETAILED INSPECTION OF AIRCRAFT FIRE WARNING SYSTEM. REPLACED MASTER W ARNING CONTROL BOX, P/N 2618055-23, WITH SERVICEABLE UNITS. OPERATIONAL CHECK AIRCRAFT FIRE WARNING SYSTEM SATISFACTORY FOR RETURN TO SERVICE. 2 L 7 2 4F A10CE 1996090500003 19960905 00003 NE 1996 9 5 Y2PA96053 2 19960731 A 7240 500195802 BURNER CAN DOUG DC9 DC915F 3022037 WP PWA JT8 JT8D7B 52053 NE NR 2 ENGINE CRACKED A Y2PA K NONE O OTHER IN INSP/MAINT 1 GL 23 196US 1715 47155 P657505 YIP - FLT 17790 - NR 2 ENGINE TAKES 5 SECONDS LONGER THAN NR 1 ENGINE TO SPOOL UP AND RUNS 50 DEGREES HOTTER THAN NR 1 E NGINE. ALL READINGS WITHIN LIMITS; HOWEVER, ENGINE CONDITION MONITORING SHOW ERRATIC EGT INDICATIONS. PERFORMED BORESC OPE INSPECTION OF NR 2 ENGINE. FOUND NR 6 AND NR 7 BURNER CANS SHIFTED APPROXIMATELY .0625 INCH. FOUND NR 8 BURNER CAN SHIFTED APPROXIMATELY .0625 OF AN INCH, AND DISCOVERED A 7 INCH CRACK AROUND THE CIRCUMFERENCE WELD, ADJACENT TO THE FU EL NOZZLE AREA. ENGINE REMOVED FOR REPLACEMENT OF BURNER CANS, AND DETAILED INSPECTION OF HOT SECTION. PART TOTAL CYCL ES: 1,115.(X) 2 L 7 2 4F 4 F A6WE E2EA 1996090500004 19960905 00004 WP 1996 9 5 WRLA96028 1 19960720 A 2424 976J86217 GCU DOUG DC10 DC1030 3023501 WP NR 3 INOPERATIVE A WRLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 9MMAZ 46933 DURING INITIAL TAXI OUT FROM GATE, FLIGHT CREW NOTED THAT NR 2 AND NR 3 GENERATORS WOULD NOT PARALLEL. FLIGHT CREW ELEC TED TO RETURN TO GATE. AIRCRAFT RETURNED WITHOUT INCIDENT. MAINTENANCE PERSONNEL FOUND NR 3 GENERATOR CONTROL UNIT INO PERATIVE. REPLACED NR 3 GENERATOR CONTROL UNIT GROUND RAN BOTH ENGINES AND PARALELLED GENERATORS. AIRCRAFT RETURNED TO SERVICE. PART MFG BY WESTINGHOUSE. (X) 2 L 7 3 4F A22WE 1996090500005 19960905 00005 NM 1996 9 5 96ZZZX4199 1 19960731 A 5753 SKIN BOEING 737 7373B7 1384580 NM RT TE AFT FLAP DELAMINATED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 952WP 23378 RT WING OUTBOARD AFT FLAP HAS DELAMINATED SKIN AT INBOARD CORNER. REMOVED DAMAGE. FABRICATED DOUBLERS AND INSTALLED. C HECK DONE IAW SRM 51-70-10. 2 L 7 2 4F RT A16WE 1996090500006 19960905 00006 NM 1996 9 5 96ZZZX4200 1 19960731 A 5753 SKIN BOEING 737 7373B7 1384580 NM TE FLAP DELAMINATED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 952WP 23378 RIGHT INBOARD FORWARD FLAP INNER SKIN HAS DELAMINATION AT 16 INCHES FROM INBOARD. FABRICATED FILLER AND DOUBLER AND INS TALLED. ALL WORKED IAW SRM 51-70-10. 2 L 7 2 4F RT A16WE 1996090500007 19960905 00007 NM 1996 9 5 96ZZZX4201 1 19960807 A 5320 65479573 WEB BOEING 737 7373B7 1384580 NM BS 793-847 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 952WP 23378 CORROSION ON THRESHOLD WEB PLATE BS 793 - BS 847, RBL 21, WL 160 (OUT OF LIMITS PER SRM 53-60-15). REMOVED AND REPLACED WEB IAW SRM 5140-02, SRM 51-20-01. 2 L 7 2 4F RT A16WE 1996090500008 19960905 00008 NM 1996 9 5 96ZZZX4202 1 19960806 A 5320 6547690 SUPPORT BOEING 737 7373B7 1384580 NM BS 727-767 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 952WP 23378 CORROSION ON FLOOR TO SIDEWALL SUPPORT TOP AND BOTTOM SURFACES AROUND NUTPLATES BS 727B PLUS 9, BS 767, RBL 21, WL 156 ( FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53). REMOVED DAMAGED AREA, FABRICATED, INSTALLED REPAIR SUPPORT IAW SRM'S 53-60 -53, 51-20-01, 51-40-02. 2 L 7 2 4F RT A16WE 1996090500009 19960905 00009 NM 1996 9 5 96ZZZX4203 1 19960806 A 5320 BAC1509100146 SUPPORT BOEING 737 7373B7 1384580 NM BS 772 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 952WP 23378 CORROSION AROUND NUTPLATES ON FLOOR SUPPORT BS 772, RBL 3, WL 159 (OUT OF LIMITS IAW 53-30-53). REMOVED DAMAGED AREA OF SUPPORT, FABRICATED, INSTALLED REPAIR PARTS IAW SRM 53-00-53. 2 L 7 2 4F RT A16WE 1996090500010 19960905 00010 NM 1996 9 5 96ZZZX4204 1 19960808 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 389.5 CREASED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 952WP 23378 CREASE IN SKIN BS 389.5 BETWEEN STR 15 - STR 16, LEFT HAND. REMOVED DAMAGED PORTION OF SKIN, INSPECTED CUT-OUT FOR CRAC KS. NO CRACKS NOTED. FABRICATED REPAIR PARTS, FILLER DOUBLER, AND INSTALLED REPAIR PARTS. 2 L 7 2 4F RT A16WE 1996090500011 19960905 00011 NM 1996 9 5 96ZZZX4205 1 19960807 A 5347 BAC15201397 TRACK BOEING 737 7373B7 1384580 NM BS 942-945 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 952WP 23378 AFT CARGO BAY, RIGHT FLOOR TRACK, HAS COROSION AT BS 942 AND BS 945, RBL 14 (OUT OF LIMITS PER SRM 53-60-53). REMOVED D AMAGED TRACK, FABRICATED, INSTALLED REPAIR PARTS IAW SRM 53-00-53. 2 L 7 2 4F RT A16WE 1996090500012 19960905 00012 NM 1996 9 5 96ZZZX4206 1 19960807 A 5312 654961612 BULKHEAD ANGLE BOEING 737 7373B7 1384580 NM BS 948 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 952WP 23378 CORROSION ON FLOOR TO BULKHEAD SUPPORT ANGLE, BS 948, RBL 21 - LBL 21, WL 180 (OUT OF LIMITS PER SRM 53-60-53). REMOVE D AND REPLACED SUPPORT ANGLE PER SRM 51-40-02, SRM 51-20-01. 2 L 7 2 4F RT A16WE 1996090500013 19960905 00013 NM 1996 9 5 96ZZZX4207 1 19960807 A 5320 BAC1509100146 SUPPORT BOEING 737 7373B7 1384580 NM BS 860 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 952WP 23378 CORROSION ON FLOOR SUPPORT BS 860, LBL 3, WL 164, AROUND NUTPLATES. (OUT OF LIMITS PER SRM 53-60-53.) CUT OUT DAMAGE, FABRICATED, INSTALLED REPAIR PARTS IAW SRM'S 53-00-53, 51-40-02, AND MM 25-01-12. 2 L 7 2 4F RT A16WE 1996090500014 19960905 00014 NM 1996 9 5 96ZZZX4208 1 19960807 A 5320 BAC1509100146 SUPPORT BOEING 737 7373B7 1384580 NM BS 860 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 952WP 23378 CORROSION FLOOR SUPPORT BS 860, LBL 7.5, WL 164 AROUND NUTPLATES (OUT OF LIMITS PER SRM 53-60-53). CUT OUT DAMAGE, FABR ICATED INSTALLED REPAIR PARTS IAW SRM'S 53-00-53, 51-40-02, MM 25-01-12. 2 L 7 2 4F RT A16WE 1996090500015 19960905 00015 NM 1996 9 5 96ZZZX4209 1 19960807 A 5320 BAC1509100146 SUPPORT BOEING 737 7373B7 1384580 NM BS 860 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 952WP 23378 CORROSION ON FLOOR SUPPORT AROUND NUTPLATE BS 846 AND BS 860, RBL 7.5, WL 164. (OUT OF LIMITS AT BS 860 PER SRM 53-60- 53.) REMOVED DAMAGED AREA, FABRICATED, INSTALLED REPAIR PARTS PER SRM'S 53-00-53, 51-40-02, 51-20-01. 2 L 7 2 4F RT A16WE 1996090500016 19960905 00016 NM 1996 9 5 96ZZZX4210 1 19960805 A 3210 654610914 BEAM BOEING 737 7373B7 1384580 NM LT MLG CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 952WP 4P817 23378 LEFT MLG BEAM ARM IS CORRODED. REMOVED AND REPLACED LT MLG BEAM IAW 32-11-00. 2 L 7 2 4F RT A16WE 1996090500017 19960905 00017 1996 9 5 VTZA96291 4 19960806 A 6122 31057165 PROP GOVERNOR JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 EA 27 325UE 41063 JFK/BOS - FLT 6490 - DURING TAKEOFF AT 1930 HRS ON 8-6-96, MADE AN UNSCHEDULED LANDING DUE TO LT ENGINE WOULD ONLY OBTAI N 86 PERCENT TORQUE ON TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. AIRCRAFT MADE FERRY FLIGHT T O IAD. MAINTENANCE ADJUSTED PROPELLER GOVERNOR AND PERFORMED HIGH SPEED TAXI. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1996090500018 19960905 00018 1996 9 5 VTZA96292 4 19960807 A 2350 B692254 STATION BOX BAG JETSTM JETSTM3201 1500217 EU LEFT FAILED A A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 483UE 898 IAD/HPN - FLT 6282 - DURING CLIMB AT 1315 HRS ON 8-7-96, MADE AN UNSCHEDULED LANDING DUE TO COULD NOT RECEIVE ON COMM 1 OR COMM 2 WITHOUT SELECTING EMERGENCY ON CAPTAIN'S STATION BOX. AIRCRAFT LANDED AT IAD AND RETURNED TO GATE, NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED STATION BOX, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1996090500019 19960905 00019 EU 1996 9 5 VTZA96293 1 19960808 A 5270 91SE16 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU PASSENGER DOOR OUT OF ADJUST A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 315UE 41033 IAD/CHS - FLT 6477 - DURING CRUISE AT 1705 HRS ON 8-8-96, MADE AN UNSCHEDULED LANDING DUE TO BOTH AMBER AND RED DOOR WAR NING LIGHTS ILLUMINATED IN-FLIGHT. AIRCRAFT RETURNED TO GATE, NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED PASSENGER DOO R MICROSWITCHES. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1996090500020 19960905 00020 EU 1996 9 5 VTZA96294 1 19960808 A 7714 AG34 TACH GENERATOR BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 370MT 800 IAD/ISP - FLT 6300 - DURING CRUISE AT 1830 HRS ON 8-8-96, MADE AN UNSCHEDULED LANDING DUE TO NR 2 RPM WENT TO ZERO. AIR CRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED TACHOMETER, GENERATOR, OPS CHECK OK. A IRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1996090500021 19960905 00021 1996 9 5 VTZA96295 4 19960809 A 3418 C771076 LIFT TRANSDUCER BAG JETSTM JETSTM3201 1500217 EU RIGHT FAILED A VTZA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 27 497UE 904 IAD/PHL - FLT 6237 - DURING TAKEOFF AT 1235 HRS ON 8-9-96, ABORTED TAKEOFF DUE TO RT STALL SYSTEM FAILURE. AIRCRAFT LAN DED AT IAD AND RETURNED TO GATE, NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED LIFT TRANSDUCER, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1996090500022 19960905 00022 EU 1996 9 5 VTZA96296 1 19960809 A 2421 23095002 GENERATOR JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE FAILURE A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 323UE 41059 IAD/RDU - FLT 6323 - DURING CLIMB AT 1910 HRS ON 8-9-96, MADE AN UNSCHEDULED LANDING DUE TO RT GENERATOR DROPPED OFF LIN E. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED RT GENERATOR. AIRCRAFT WAS RE LEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1996090500023 19960905 00023 EU 1996 9 5 VTZA96297 1 19960809 A 5270 91SE16 SWITCH BAG JETSTM JETSTM3201 1500217 EU DOOR OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 497UE 904 IAD/ROA - FLT 6427 - DURING TAKEOFF AT 1515 HRS ON 8-9-96, ABORTED TAKEOFF DUE TO PASSENGER DOOR WARNING. AIRCRAFT RETU RNED TO GATE, NO FURTHER INCIDENTS. MAINTENANCE INSPECTED, CLEANED AND ADJUSTED DOOR MICROSWITCH, OPS CHECK OK. AIRCRA FT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1996090500024 19960905 00024 1996 9 5 VTZA96298 4 19960810 A 3417 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU NR 1 ADC LOOSE A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 305UE 41019 LYH/IAD - FLT 6186 - DURING CLIMB AT 0935 HRS ON 8-11-96, MADE AN UNSCHEDULED LANDING DUE TO NR 1 EADI AIRSPEED INDICATO R INOP. AIRCRAFT RETURNED TO THE GATE, NO FURTHER INCIDENTS. MAINTENANCE RESECURED LOOSE CONNECTOR ON NR 1 ADC, OPS CH ECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1996090500025 19960905 00025 EU 1996 9 5 VTZA96299 1 19960812 A 5210 LATCH MECHANISM BAG JETSTM JETSTM3201 1500217 EU PASSENGER DOOR LACK OF LUBE A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 497UE 904 BDL/IAD - FLT 6183 - DURING TAKEOFF AT 1430 HRS ON 8-12-96, MADE AN UNSCHEDULED LANDING DUE TO PASSENGER DOOR CAPTION IL LUMINATED. AIRCRAFT RETURNED TO GATE, NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI 55126, MEL 52-20. MAINTENANCE CLOS ED DMI 55126 ON 8-12-96 BY CLEANING AND LUBING DOOR LATCH MECHANISM. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO S ERVICE. (X) 2 L 7 2 4T RT A56EU 1996090500026 19960905 00026 EU 1996 9 5 VTZA96301 1 19960813 A 2731 TRIM LEVER BAG JETSTM JETSTM3201 1500217 EU ELEVATOR DIRTY A VTZA K NONE F FLT CONT AFFECTED CR CRUISE 1 EA 27 491UE 911 ALB/IAD - FLT 6254 - DURING CRUISE AT 0740 HRS ON 8-13-96, ELEVATOR EXPERIENCED TRIM BINDING. AIRCRAFT LANDED AT IAD WI TH NO FURTHER INCIDENTS. MAINTENANCE FOUND FOD LIMITING TRIM LEVER MOVEMENT IN QUADRANT, MAINTENANCE REMOVED FOD, OPS C HECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1996090500027 19960905 00027 NE 1996 9 5 VTZA96302 2 19960812 A 7200 31034905 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE LEFT AUTO SHUT DOWN A A VTZA A UNSCHED LANDING J Y WARNING INDICATION ENGINE STOPPAGE CR CRUISE 1 EA 27 307UE 3712 41021 75039 CHS/IAD - FLT 6520 - DURING CRUISE AT 1900 HRS ON 8-12-96, MADE AN UNSCHEDULED LANDING AT RDU DUE TO THE LT ENGINE AUTO SHUT DOWN IN FLIGHT. AIRCRAFT LANDED AND WENT TO GATE, NO FURTHER INCIDENTS. MAINTENANCE SUMPED TANKS, C/W ENGINE RUNS , AND C/W M.A.F., COULD NOT DUPLICATE, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T 4 T RT A41NM E18NE 1996090500028 19960905 00028 EU 1996 9 5 VTZA96306 1 19960814 A 5270 91SE13 SWITCH BAG JETSTM JETSTM3201 1500217 EU PASSENGER HANDLE FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 497UE 904 IAD/CMH - FLT 6381 - DURING TAKEOFF AT 1225 HOURS ON 8-14-96, ABORTED TAKEOFF AND RETURNED TO GATE AFTER EXPERIENCING A PASSENGER DOOR WARNING INDICATION ON THE CAPTION PANEL. MAINTENANCE TROUBLESHOT THE DISCREPANCY AND FOUND THE PASSENGER DOOR HANDLE MICROSWITCH HAD FAILED. MAINTENANCE REPLACED THE MICROSWITCH AND RELEASED AIRCRAFT FOR SERVICE. (X) 2 L 7 2 4T RT A56EU 1996090500030 19960905 00030 EU 1996 9 5 USAAF96087 1 19960807 A 3350 6104781 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 895US 11380 CLT - EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED ALL EIGHT EMERGENCY LIGHT BATTERY PACKS. (X) 2 L 7 2 4F RT 1996090500031 19960905 00031 EU 1996 9 5 USAAF96088 1 19960809 A 3350 6104781 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 853US 11281 IND - MAIN ENTRY DOOR EXIT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY BATTERY PACK FOR THE LIGHT. ( X) 2 L 7 2 4F RT 1996090500032 19960905 00032 WP 1996 9 5 USAA960546 1 19960805 A 5313 27779225 LONGERON DOUG DC9 DC931 3022065 WP BS 446-465 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 963VJ 64847 47508 PIT - DURING Q4-C6 CHECK, FOUND .25 INCH CRACK IN LONGERON AT BELT FRAME 24 RIGHT BETWEEN STA 446 - STA 465. REMOVED CR ECKED SECTION, INSTALLED NEW LONGERON AND SPLICES PER TYPICAL REPAIR 53-10-07, FIGURE NR 2. (X) 2 L 7 2 4F A6WE 1996090500033 19960905 00033 NE 1996 9 5 96ZZZX4211 2 19960605 A 7260 230307203 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE CSD DRIVE LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 127HH 538 7060 LE45308E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1996090500034 19960905 00034 NE 1996 9 5 96ZZZX4212 2 19960605 A 7250 41016701 SEAL RING BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE 1ST TURB SHROUD LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 127HH 538 7060 LE45308E SEAL RING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1996090500035 19960905 00035 NE 1996 9 5 96ZZZX4213 2 19960605 A 7250 411101009 NOZZLE BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE GAS PROD CRACKED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 127HH 538 CX69 7060 LE45308E NOZZLE ASSY CRACKED BYEOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1996090500036 19960905 00036 NE 1996 9 5 96ZZZX4214 2 19960605 A 7260 430101201 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE ACC DRIVE LEAKING A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 127HH 538 7060 LE45308E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1996090500037 19960905 00037 NE 1996 9 5 96ZZZX4215 2 19960605 A 7260 430101301 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE ACCY DRIVE LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 127HH 538 7060 LE45308E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1996090500038 19960905 00038 NE 1996 9 5 96ZZZX4216 2 19960605 A 7260 430101501 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE ACC DRIVE LEAKING A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 127HH 538 7060 LE45308E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH 3 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1996090500039 19960905 00039 NE 1996 9 5 96ZZZX4217 2 19960605 A 7250 430135703 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE NR 2 BEARING LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 127HH 538 752 7060 LE45308E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1996090500040 19960905 00040 NE 1996 9 5 96ZZZX4218 2 19960414 A 7250 410106701 SEAL RING BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE 1ST TURB SHROUD WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 127HH 175 7060 LE45244E SEAL RING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1996090500041 19960905 00041 NM 1996 9 5 CALA9601243 1 19960827 A 3610 312N53061 HP2 DUCT BOEING 757 757224 1384958 NM RROYCE RB211 RB211535E4 54555 NE NR 2 ENGINE LEAKING A CALA A D UNSCHED LANDING RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SW 09 18112 27302 31378 THE RT ENGINE HAD A FIRE WARNING INDICATION AFTER TAKEOFF FROM LAX. THE AIRCRAFT WAS RETURNED TO LAX WHERE AIRCRAFT LAN DED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE HP2 DUCT WAS FOUND LEAKING. THE HP2 DUCT WAS REMOVED AND REPLACED AND LEAK CHECKS WERE GOOD. A TEST FLIGHT WAS CONDUCTED AND THE RT ENGINE PERFORMED NORMALLY. 2 L 7 2 4F 4 F RT A2NM E12EU 1996090500042 19960905 00042 NM 1996 9 5 CALA9601244 1 19960807 A 5720 TIP BOEING 727 727232 1384082 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A .50 INCH CRACK IN LOWER OUTBOARD EDGE OF LT WING TIP. THE CRACKED AREA WAS CUT OUT. A DOUBLER AND FILLER REPAIR WERE FABRICATED AND INSTALLED IAW SRM 57-20-5. 2 L 7 3 4F A3WE 1996090500043 19960905 00043 NM 1996 9 5 CALA9601245 1 19960808 A 5752 FAIRING BOEING 727 727232 1384082 NM AILERON TAB PULLED LOOSE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND FAIRING PULLED LOOSE FROM BOTTOM OF LEFT INBOARD AILERON TAB. THE FASTENERS WERE REMOVED, THE FAIRING WAS REBONDED, AND THE FASTENERS WERE REINSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996090500044 19960905 00044 NM 1996 9 5 CALA9601246 1 19960809 A 5330 SKIN BOEING 727 727232 1384082 NM BS 1243 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND LT FUSELAGE SKIN DENTED JUST BELOW NR 1 ENGINE AT STA 1243. THE DENTED AREA WAS CUT OUT. A FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3. 2 L 7 3 4F A3WE 1996090500045 19960905 00045 NM 1996 9 5 CALA9601247 1 19960807 A 5720 TIP BOEING 727 727232 1384082 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A .25 INCH CRACK IN RT WING TIP UPPER SURFACE, JUST FORWARD OF PANEL 6641. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1. 2 L 7 3 4F A3WE 1996090500046 19960905 00046 NM 1996 9 5 CALA9601248 1 19960807 A 3397 WIRE BOEING 727 727232 1384082 NM CABIN DAMAGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14788 20642 THE EMERGENCY PATH LIGHTING BETWEEN SEAT ROWS 6 ABC - 8 ABC WERE FOUND INOPERATIVE DURING AN EMERGENCY LIGHT OPERATIONA L CHECK. MAINTENANCE FOUND A FLOOR HARNESS FEEDER WIRE DAMAGED. THE WIRE WAS REPAIRED AND OPERATIONAL CHECKS WERE GOOD IAW MM 33-51-0. 2 L 7 3 4F A3WE 1996090500047 19960905 00047 WP 1996 9 5 9618619154 1 19960731 A 5713 LONGERON DOUG DC9 DC914 3022034 WP WS 91-111 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8913E 45830 DURING H-CHECK, FOUND CORROSION ON THE RIGHT WING LOWER STR 14 FROM XRS 91 - 111. REPAIRED STRINGER (P/N 591277-502) PE R EA 91-110862. 2 L 7 2 4F A6WE 1996090500048 19960905 00048 WP 1996 9 5 9618629154 1 19960801 A 5713 LONGERON DOUG DC9 DC914 3022034 WP WS 69 111 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8913E 45830 DURING H-CHECK, FOUND CORROSION ON THE RIGHT WING LOWER STRINGERS: NR 11-15 BETWEEN XRS 91-111. NR 17 BETWEEN XRS 88-1 11. NR 19 BETWEEN XRS 91-96. NR 21 BETWEEN XRS 69-111. REPAIRED STRINGERS PER EA 91-110868. 2 L 7 2 4F A6WE 1996090500049 19960905 00049 NM 1996 9 5 9618636309 1 19960807 A 5315 FLOOR BEAM BOEING 747 747451 1384940 NM BS 460-480 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 669US 24224 DURING P-CHECK, FOUND CORROSION ON THE FLOOR BEAM UPPER CHORDS BS 460 FROM RBL 39 - 61 AND BS 480 FROM RBL 64 - 75. REP AIRED CHORDS PER EA 63-106559. 2 L 7 4 4F RT A20WE 1996090500050 19960905 00050 NM 1996 9 5 9618646309 1 19960808 A 5347 SEAT TRACK BOEING 747 747451 1384940 NM BS 980-1000 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 669US 24224 DURING P-CHECK, FOUND CORROSION ON THE LBL 41 SEAT TRACK FROM BS 980 - 1000. REPAIRED TRACK (P/N 140U5617-13) PER EA 63 -101910. 2 L 7 4 4F RT A20WE 1996090500051 19960905 00051 WP 1996 9 5 9618651151 1 19960809 A 5330 DOUBLER DOUG DC10 DC1040 3023508 WP FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 151US 46760 DURING T-CHECK, FOUND CORROSION ON THE RADIO ALTIMETER MOUNTING PLATES, NR 1-2, TRANSMIT AND RECEIVE. REPAIRED PLATES ( P/N AYB7022-1, AYB7053-1, AND AYB7053-501) PER EA 11-106221. 2 L 7 3 4F A22WE 1996090500052 19960905 00052 WP 1996 9 5 9618661151 1 19960809 A 5347 SEAT TRACK DOUG DC10 DC1040 3023508 WP BS 1841 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 151US 46760 DURING T-CHECK, FOUND CORROSION ON THE RBL 75 SEAT TRACK AT FS 1841. REPAIRED TRACK (P/N S 4929147) PER EA 11-106212. 2 L 7 3 4F A22WE 1996090500053 19960905 00053 WP 1996 9 5 9618679138 1 19960814 A 5248 SUPPORT DOUG DC9 DC915 3022036 WP TAIL CONE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9348 45787 DURING H-CHECK, FOUND A CRACK IN THE AFT VENTRAL DOOR NR 2 BEAM RIGHT SUPPORT. REPAIRED SUPPORT (P/N 9915565-29) PER EA 91-110737. 2 L 7 2 4F A6WE 1996090500054 19960905 00054 NM 1996 9 5 9618682715 1 19960819 A 5754 CASTING BOEING 727 7272S7 138407Z NM NR 2 LE FLAP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 719RC 25725 22490 DURING H-CHECK, FOUND A CRACK IN THE NR 2 LEADING EDGE FLAP BULLNOSE HINGE CASTING, OUTBOARD SIDE AT THE RADIUS. REPLAC ED FLAP (P/N 65-16226-7A) PER MM 27-81-01. 2 L 7 3 4F A3WE 1996090500055 19960905 00055 WP 1996 9 5 9618699138 1 19960821 A 5320 JAMB DOUG DC9 DC915 3022036 WP SERVICE DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9348 45787 DURING H-CHECK, FOUND CRACKS IN THE FORWARD SERVICE DOOR JAMB AT BOTH UPPER CORNERS. REPAIRED JAMB (P/N 5911407-33) PE R EA 91-110734. 2 L 7 2 4F A6WE 1996090500056 19960905 00056 WP 1996 9 5 9618701162 1 19960823 A 5320 FITTING DOUG DC10 DC1040 3023508 WP BS 1521-1531 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 162US 46771 DURING T-CHECK, FOUND CORROSION ON THE LONGERON 51R END FITTING AT FS 1521 - 1531. REPLACED FITTING. 2 L 7 3 4F A22WE 1996090500057 19960905 00057 WP 1996 9 5 9618711162 1 19960824 A 5313 LONGERON DOUG DC10 DC1040 3023508 WP BS 1781 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 162US 46771 DURING T-CHECK, FOUND CORROSION ON LONGERON 52 AT FS 1781. REPAIRED LONGERON (P/N AGA7045) PER EA 11-106299. 2 L 7 3 4F A22WE 1996090500058 19960905 00058 1996 9 5 9618722710 4 19960828 A 3442 RT UNIT BOEING 727 727225 1384077 NM RADAR SYST MALFUNCTIONED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 820EA 22557 DURING CLIMB, THE RADAR SYSTEM WAS INOPERATIVE. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE RADA R ANTENNA, VERTICAL GYRO, AND RADAR TRANSCEIVER. OPERATIONAL CHECK GOOD. 2 L 7 3 4F A3WE 1996090500059 19960905 00059 NE 1996 9 5 COMA9610261 2 19960827 A 7210 PROP MTG FLANGE EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE CORRODED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 257CA 2518 120248 115517 THE RT ENGINE PROPELLER MOUNTING FLANGE HAD PITTING INSIDE THE MOUNTING BOLT HOLES. DISCREPANCY FOUND DURING SCHEDULED PROPELLER MAINTENANCE. REPLACED THE RT ENGINE. 2 L 7 2 4T 4 T RT A31SO E20NE 1996090500060 19960905 00060 SO 1996 9 5 COMA9610262 1 19960827 A 2913 63163 PUMP EMB 120 EMB120RT SO RT HYD SYST LEAKING A COMA H DEACTIVATE SYST/CIRCUITS K FLUID LOSS AP APPROACH 1 SO 01 254CA 5288 1388 120233 BLUE (RT) HYDRAULIC SYSTEM LOW FLUID LEVEL WARNING DURING APPROACH. QUANTITY GAUGE INDICATED EMPTY. REPLACED THE RT EN GINE DRIVEN HYDRAULIC PUMP DUE TO INTERNAL LEAKAGE TO CASE DRAIN. PART TOTAL CYCLES, 5,227. 2 L 7 2 4T RT A31SO 1996090500061 19960905 00061 SO 1996 9 5 COMA9610263 1 19960827 A 2750 3075001017 FLAP CONTL UNIT EMB 120 EMB120RT SO E/E COMPT MALFUNCTION A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 205CA 2079 2002 120205 FLAP DISAGREE WARNING AFTER TAKEOFF. REPLACED THE FLAP CONTROL UNIT. PART TOTAL CYCLES, 2,052. 2 L 7 2 4T RT A31SO 1996090500062 19960905 00062 EA 1996 9 5 COMA9660139 1 19960816 A 5753 PAINT CNDAIR CL600 CL6002B19 EA LT/RT TE FLAPS ROUGH A A COMA K NONE F FLT CONT AFFECTED AP APPROACH 1 SO 01 920CA 7446 7022 AIRCRAFT ROLLS HARD RIGHT WHEN FLAPS ARE SELECTED TO 45 DEGREES. AIRCRAFT REQUIRES CONSTANT 45 DEGREES OF AILERON TO CO NTROL THE ROLL. REPAIRED ROUGH PAINT ON FLAP LEADING EDGES. FLIGHT CHECK SATISFACTORY. REF: BOMBARDIER INC. SERVICE LETTER NO. RJ-SL-27-022, "AIRCRAFT NEWLY PAINTED LATERAL TRIM REQUIREMENT", DATED 8/28/96. 2 L 7 2 4F RT A21EA 1996090500063 19960905 00063 NM 1996 9 5 SWAA960861 1 19960824 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 727B CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 24SW 20925 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER 10R CRACKED AT BS 727B. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996090500064 19960905 00064 NM 1996 9 5 SWAA960862 1 19960824 A 5320 CLIP BOEING 737 7372H4 138448C NM BS 597 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 24SW 20925 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER TIE CLIP 10R CRACKED AT BS 597. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996090500065 19960905 00065 NM 1996 9 5 SWAA960863 1 19960824 A 5320 CLIPS BOEING 737 7372H4 138448C NM BS 557/559 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 24SW 20925 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER TIE CLIPS 3L CRACKED AT BS 559, S3R, S4R AND S5R CRACKED AT BS 559, AND S5L AT BS 578. REPLACED ALL PER BOEING SRM. 2 L 7 2 4F A16WE 1996090500066 19960905 00066 NM 1996 9 5 SWAA960864 1 19960824 A 5320 CLIPS BOEING 737 7372H4 138448C NM BS 272 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 24SW 20925 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER TIE CLIPS CRACKED AT 10R, BS 727, AND AT 9R, BS 727B. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996090500067 19960905 00067 NM 1996 9 5 SWAA960865 1 19960824 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 727B CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 24SW 20925 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER 9R CRACKED AT BS 727B. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996090500068 19960905 00068 NM 1996 9 5 SWAA960866 1 19960823 A 5320 BEAM BOEING 737 7372H4 138448C NM BS 707 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 51SW 21448 DURING SCHEDULED SERVICE CHECK, FOUND TRANSVERSE BEAM CRACKED FWD SIDE OF BS 707, RBL 1. REPAIRED PER SWA RA 1-257-0346 . 2 L 7 2 4F A16WE 1996090500069 19960905 00069 NM 1996 9 5 SWAA960867 1 19960823 A 5320 BEAM BOEING 737 7372H4 138448C NM BS 707 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 51SW 21448 DURING SCHEDULED SERVICE CHECK, FOUND TRANSVERSE BEAM CRACKED FWD SIDE OF BS 707, LBL 1. REPAIRED PER SWA RA 1-257-0346 . 2 L 7 2 4F A16WE 1996090500070 19960905 00070 NM 1996 9 5 SWAA960868 1 19960823 A 5312 BULKHEAD SKIN BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 74SW 22674 DURING SCHEDULED D-CHECK, FOUND BULKHEAD SKIN CRACKED AT BS 178, WL 234, RBL 11 AND 13, EMANATING FROM FASTENER HOLE. R EPAIRED PER SWA RA 1-257-0346. 2 L 7 2 4F A16WE 1996090500071 19960905 00071 NM 1996 9 5 SWAA960869 1 19960823 A 5320 SUPPORT BOEING 737 7372H4 138448C NM BS 380-500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 74SW 22674 DURING SCHEDULED D-CHECK, FOUND HORIZONTAL FLOOR SUPPORT CORRODED AT BS 380 TO 500, RBL 12, WL 150. REPAIRED PER SWA TI -A51-002. 2 L 7 2 4F A16WE 1996090500072 19960905 00072 NM 1996 9 5 SWAA960870 1 19960823 A 5320 WEB BOEING 737 7372H4 138448C NM BS 469.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 74SW 22674 DURING SCHEDULED D-CHECK, FOUND VERTICAL SUPPORT WEB CRACKED AT BS 469.5. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996090500073 19960905 00073 NM 1996 9 5 SWAA960871 1 19960823 A 5330 SKIN BOEING 737 7372H4 138448C NM FWD FUSELAGE DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 74SW 22674 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED BELOW F/O SLIDING WINDOW AND 18 INCHES AFT OF RADOME. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996090500074 19960905 00074 NM 1996 9 5 SWAA960872 1 19960823 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 946 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 74SW 22674 DURING SCHEDULED D-CHECK, FOUND CRACK IN BACKSIDE OF VALVE SUPPORT DOUBLER AT END OF NR 1 LT PANEL IN AFT CARGO COMPT, A T BS 946, LBL 20 , WL 238. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996090500075 19960905 00075 NM 1996 9 5 SWAA960873 1 19960823 A 3350 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN OVERHEAD EXIT LIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F A16WE 1996090500076 19960905 00076 NM 1996 9 5 SWAA960874 1 19960824 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE PUNCTURED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED BC4 CHECK, FOUND PUNCTURE IN FUSELAGE SKIN 10 INCHES AFT EDGE AND 28 INCHES ABOVE CARGO DOOR HANDLE. R EPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996090500077 19960905 00077 NM 1996 9 5 UPS96221007 1 19960815 A 5752 6521740501 FITTING BOEING 727 727247 138408F NM LT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 212UP 21392 INSPECTION TYPE: C. LT INBOARD TAB FITTINGS CORRODED AILERON SIDE. REMOVED AND REPLACED LT INBOARD TAB FITTINGS AILER ON SIDE PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996090500078 19960905 00078 NM 1996 9 5 UPS96221014 1 19960828 A 3260 NA INDICATION BOEING 727 72725C 138400H NM NLG MALFUNCTIONED A IPXA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 946UP 19721 DID NOT HAVE GREEN NOSE GEAR INDICATIONS (NO RED LIGHTS). RECYCLED GEAR UP/DOWN SEQUENCE AND ALL LIGHTS NORMAL. JACKE D ACFT AND CYCLED NLG 5 TIMES, COULD NOT DUPLICATE PROBLEM ON GROUND. AIRCRAFT OK TO CONTINUE SERVICE. ALL WORK DONE I AW B727 MM CHAPTERS 7 AND 32. 2 L 7 3 4F A3WE 1996090500079 19960905 00079 NM 1996 9 5 UPS96221015 1 19960716 A 5311 FRAME BOEING 727 72725C 138400H NM BS 1183 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE: RE. BS 1183 FRAME OUT OF LIMITS AFTER CORROSION REMOVAL BETWEEN STR'S 10R AND 14R. REPAIRED PER DHC SK 951-947. 2 L 7 3 4F A3WE 1996090500080 19960905 00080 NM 1996 9 5 UPS96221016 1 19960808 A 5320 CHORD BOEING 727 72725C 138400H NM BS 298 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE: C. NLG W/W RT UPPER CHORD AT BS 298 NOTED AFTER REMOVAL OF ANGLE ON NR 573976. REMOVED CORROSION PE R SRM 51-10-6, OT THICKNESS PER B727 NTM PT 1, 51-04-00 FIG 2. READINGS RANGE FROM .083-.132 INCH ON THE HORIZONTAL FLA NGE, .208-.250 INCH ON THE VERTICAL FLANGE. FLAP PEENED AREA PER 727-53-1811 AND MM 20-10-03. ALODINED AND PRIMED PER SRM 51-10-06. 2 L 7 3 4F A3WE 1996090500081 19960905 00081 NM 1996 9 5 UPS96221017 1 19960708 A 5720 STIFFENER BOEING 727 72725C 138400H NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE: C. RT WING L/E AT NR 6 SLAT INBD TRACK - INBD VERTICAL STIFFENER FOR TRACK MOUNT IS CRACKED. REMOVED FABRICATED AND INSTALLED REPLACEMENT STIFFENER PER SRM'S 51-10-1, ,51-30-2 AND SEALED PER SRM 51-20-04. 2 L 7 3 4F A3WE 1996090500082 19960905 00082 NM 1996 9 5 UPS96221018 1 19960708 A 5720 STIFFENER BOEING 727 72725C 138400H NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE: C. RT WING L/E AT NR 6 SLAT INBD TRACK - OTBD VERTICAL STIFFENER FOR TRACK MOUNT IS CRACKED. REMOVED FABRICATED AND INSTALLED REPLACEMENT STIFFENER PER SRM'S 51-10-1, 51-30-2 AND SEALED PER SRM 50-20-4. 2 L 7 3 4F A3WE 1996090500083 19960905 00083 NM 1996 9 5 UPS96620891 1 19960817 A 2560 ESCAPE ROPE BOEING 767 76734AF 1385212 NM FWD ENTRY DOOR TANGLED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 304UP 27242 FORWARD ENTRY DOOR ESCAPE ROPE TANGLED, WILL NOT DEPLOY. ROPE REINSTALLED BY BOEING DURING EO B767-3350-8522 UNDER BOEI NG 337 FORM FOR SB 767-33-0065 EMERGENCY LIGHT RELOCATION. 2 L 7 2 4F RT A1NM 1996090500084 19960905 00084 WP 1996 9 5 UPS96821001 1 19960824 A 5720 46522012U FITTING DOUG DC8 DC873F 302199F WP WS 5.812 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 RIGHT WING STA ZERO FLAP COVE FWD OF NR 1 FLAP DRIVE FWD PIVOT FITTING CRACKED ABOVE 90 DEGREE SPOILER CABLE BEND PULLEY S. REPLACED FITTING PER SRM 51-1-20D AND EO DC8-5310-8226D. 2 L 7 4 4F RT 4A25 1996090500085 19960905 00085 WP 1996 9 5 UPS96821005 1 19960809 A 5330 SKIN DOUG DC8 DC871F 302199D WP DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE: C. DOOR CUT-OUT CRACKED FWD LOWER CORNER, .50 INCH. REPAIRED PER SRM 53-2-0 PG 139. 2 L 7 4 4F RT 4A25 1996090500086 19960905 00086 WP 1996 9 5 UPS96821006 1 19960822 A 5330 SKIN DOUG DC8 DC871F 302199D WP C-4 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE: C. C-4 DOOR CUT-OUT CRACKED UPPER FWD CORNER. REPAIRED PER SRM 53-2-0 PG 149/150. 2 L 7 4 4F RT 4A25 1996090500087 19960905 00087 WP 1996 9 5 UPS96821008 1 19960806 A 5730 SKIN DOUG DC8 DC871F 302199D WP LT WING TE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE: DLY. FOUND CRACK IN WING SKIN AT LEFT DUMP SHOOT AREA. CRACKED THROUGH RIVET, EDDY CURRENT CRACK FOUN D TO BE 1.25 INCHES IN LENGTH. REPAI RED LOWER TRAILING EDGE WING COVE PANEL IAW SRM 51-1-9A. 2 L 7 4 4F RT 4A25 1996090500088 19960905 00088 WP 1996 9 5 UPS96821009 1 19960827 A 3350 5708458503 LIGHTS DOUG DC8 DC873F 302199F WP CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE: DLY. EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. OPS CHK, PART NR ON 60-1223-5, S/N 286, OFF 5708458-503, OFF A056. 2 L 7 4 4F RT 4A25 1996090500089 19960905 00089 WP 1996 9 5 UPS96821010 1 19960807 A 3230 UPLATCH MECH DOUG DC8 DC871F 302199D WP NOSE GEAR MALFUNCTIONED A IPXA O OTHER O OTHER TO TAKEOFF 1 SO 01 772UP 46072 INSPECTION TYPE: DLY. ON TAKEOFF ROLL, HEARD BUZZING NOISE LIKE A RELAY CHATTERING. ON GEAR RETRACTION COULD FEEL BUZ ZING IN THE HANDLE, BUZZING STOPPED AS GEAR STARTED UP. WHEN PLACING GEAR HANDLE INTO THE UPLATCH POSITION THE NOSE GEA R FELL OUT OF WHEEWELL AND FULLY EXTENDED. RECYCLED GEAR DOWN AND THEN UP, OPERATION WAS NORMAL. SECOND UPLATCH CHK WA S NORMAL. LIFTED NOSE OF ACFT OFF GROUND AND CYCLED NOSE GEAR. NOSE GEAR PASSED UPLATCH TEST EACH TIME. INSPECTED UPL ATCH MECHANISM, NO DEFECTS FOUND. SYSTEMS OPERATED NORMALLY IAW M/M 32-31-06, M/M 32-20-00, PG 501. 2 L 7 4 4F RT 4A25 1996090500090 19960905 00090 WP 1996 9 5 UPS96821012 1 19960820 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 1600-1640 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE: C. LONGERON NR 24L FROM STA 1600 - 1640 CORRODED. FABRICATED REPAIR FILLER AND DOUBLER IAW DC8 SRM'S 53-4-1 AND 53-2-1, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR IAW DC8 SRM 51-1-20D. PAINT TO BE ACCOMP LISHED ON UPS N/ 468048. 2 L 7 4 4F RT 4A25 1996090500091 19960905 00091 WP 1996 9 5 UPS96821013 1 19960826 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1540 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE: C. AFT ACCESS COMPT FUSELAGE FRAME AND LONGERON 33L CORRODED STA 1540. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-2-0, REMOVED GILLINER FOR ACCESS. REPAIRED FRAME SECTION IAW DC8 SRM 53-2-0 AND REO 02193 . ALODINED AND PRIMED ALL PARTS IAW 51-1-8. INSTALLED CAP AND ANGLE SPLICES IAW SRM 51-1-20D. CLOSED GILLINER PANEL I AW SRM 51-3-0. SEALED REPAIR IAW 51-1-17. 2 L 7 4 4F RT 4A25 1996090500092 19960905 00092 NM 1996 9 5 96FDEA01414 1 19960827 A 2150 ACM BOEING 727 72727 138400K NM RIGHT OIL LEAK A FDEA A B UNSCHED LANDING EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 25 145FE 19109 SMOKE IN CARGO COMPARTMENT. NOT RECOGNIZABLE ODOR. REQUIRED USE OF OXYGEN MASKS AND EMERGENCY DESCENT. FOUND OLD ACM LEAKING OIL AND BYPASSING INTERNALLY CAUSING SMOKE IN CARGO COMPARTMENT. REMOVED AND REPLACED RIGHT HAND A.C.M. PER MM 21-51 AS REQUIRED. TESTED A.C.M. RAN UNIT. OKAY FOR SERVICE. 2 L 7 3 4F A3WE 1996090500093 19960905 00093 EU 1996 9 5 96FDEA01415 1 19960828 A 2910 O-RING AIRBUS 310 A310221 3930310 EU PWA JT9 JT9D7R4D 52054 NE GREEN HYD SYST FAILED A FDEA H DEACTIVATE SYST/CIRCUITS J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SO 25 419FE 345 STA SFS - APPROX 1 HOUR INTO CRUISE, ECAM REPORTED GREEN HYD SYS RESERVOIR LOW OVERHEAD AND SYS PAGE AGREED. ACCOMPLIS HED PROCEDURE, SHUT DOWN GREEN SYSTEM. MANUALLY EXTENDED GEAR. CHECKED AND FOUND HYD GREEN SYS GREEN ELECTRO HYD SELEC TOR FITTING LEAKING. REMOVED AND REPLACED PACKING (O-RING), LEAK CHECKED OK. RESET OF SYSTEM NORMAL OPERATING CONDITIO N ON MANUAL EXTENSION PER MM 32-33-00, PG 18. 2 L 7 2 4F 4 F RT A35EU E3NE 1996090500094 19960905 00094 NM 1996 9 5 96FDEA01416 1 19960829 A 5320 66118092 CLIP BOEING 727 72725 1384006 NM BS 640 BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 509FE 18280 NR 0219 AND 010. STRINGER CLIP AT BS 640, STRINGER 19 RT IS BROKEN. REMOVED DAMAGED STR CLIP AND INSTALLED NEW STR CLI P, BS 640, STR 19 RT HAND. 2 L 7 3 4F A3WE 1996090500095 19960905 00095 NM 1996 9 5 96FDEA01417 1 19960829 A 5753 652163490 SKIN BOEING 727 72725 1384006 NM RT TE AFT FLAP DELAMINATION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 509FE 18280 NR 0520 AND 011, RT WING I/B AFT FLAP O/B AFT CORNER HAS APPROX 60 SQ INCHES OF DELAMINATION. *S/D* RT WING I/B AFT FL AP O/B AFT CORNER REPAIRED IAW FED EX SRM 51-40-6. 2 L 7 3 4F A3WE 1996090500096 19960905 00096 NM 1996 9 5 96FDEA01418 1 19960829 A 5320 65184173 WEB BOEING 727 72722 1384002 NM BS 294 - 315 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 WHILE WORKING NR O610, FOUND CORROSION ON WEB UNDER STIFFENER, STA 310, WL 184. REMOVED CORRODED WEB, FABRICATED NEW W EB AND SPLICE AT BS 294 TO BS 315, RBL 12 - LB 12, WL 184. REMOVED AND REPLACED 2 EACH CLIPS AT 294 - 301.5, RBL 12 A ND LBL 12, WL 184 DUE TO CORROSION. IAW FEDEX SRM 51-40-2 FIG 2 CLIP PART NR 65-18415- AND NR 65-18415-89. 2 L 7 3 4F A3WE 1996090500097 19960905 00097 NM 1996 9 5 96UAL900488 1 19960626 A 2612 FIRE LOOP CONN BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE APU INTERMITTENT A UALA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 WP 29 993UA 22383 APU FIRE WARNING SOUNDED. FIRE BOTTLE DISCHARGED. LANDED UNDER AMBER ALERT. REPLACED FIRE WARNING LOOP CONNECTOR. CHE CKS O.K. 2 L 7 2 4F 4 F A16WE E2EA 1996090500098 19960905 00098 NM 1996 9 5 96UAL900638 1 19960819 A 3350 LIGHT BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 4714U 19876 EMERGENCY EXIT LIGHTS FROM DOOR 2L TO SEAT 18A ARE INOPERATIVE. ADDITIONALLY, LAMP AT SEAT 20C IS INOPERATIVE. SECURED LEAD IN POWER CABLE AND ALSO SECURED LAMP AT SEAT 20C. 2 L 7 4 4F 4 F A20WE E20EA 1996090500099 19960905 00099 NM 1996 9 5 96UAL900639 1 19960819 A 5754 FLAP 65B392052 BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE NR 16 LE FLAP CORNER MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 161UA 21352 OUTBOARD CORNER OF NR 16 KRUEGER PLAP WAS FOUND MISSING. DETAILED INVESTIGATION OF THE REMAINING FLAP STRUCTURE FOUND N O DELAMINATION OR CRACKS. INSTALLED DOUBLER REPAIR. 2 L 7 4 4F 4 F A20WE E20EA 1996090500100 19960905 00100 NM 1996 9 5 96UAL900640 1 19960819 A 5730 65B145965 PANEL BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE LT WING LE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 186UA 20144 26875 LEFT WING LEADING EDGE FIBERGLASS PANEL WAS FOUND WITH A 35 INCH CRACK. CRACK HAD PROPAGATED FROM AN EXISTING 18 INCH C RACK THAT WAS PREVIOUSLY REPAIRED. PANEL IS LOCATED INBOARD OF THE NR 2 ENGINE. ACCOMPLISHED REPAIR PER GN-MM. 2 L 7 4 4F 4 F RT A20WE E24NE 1996090500101 19960905 00101 NE 1996 9 5 96UAL900641 2 19960819 A 7230 53A321 FAN BLADES BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE DAMAGED A UALA A UNSCHED LANDING C E F.O.D. VIBRATION/BUFFET TO TAKEOFF 1 WP 29 651UA 3756 25389 717695 BIRD STRIKE NR 1 ENGINE, ACCOMPANIED BY VIBRATION. AIRCRAFT RETURNED TO FIELD. EXTENSIVE FAN BLADE DAMAGE OCCURRED FRO M BIRD STRIKE. THE COMPLETE SET OF FAN BLADES WERE REPLACED. 2 L 7 2 4F 4 F RT A1NM E24NE 1996090500102 19960905 00102 NM 1996 9 5 96UAL900642 1 19960819 A 3350 LAMP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN SHORTED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 348UA 24252 EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE FROM FIRST ROW OF COACH TO THE EMERGENCY EXIT ROW. ALSO, EMERGENCY EXIT LIGH T INOPERATIVE. REPLACED SHORTED LAMP AT FIRST ROW OF COACH. CHECKS O.K. 2 L 7 2 4F 4 F RT A16WE E2GL 1996090500103 19960905 00103 EU 1996 9 5 96UAL900643 1 19960820 A 2930 SWITCH C60AA0062 AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE GREEN HYD SYST FAILED A UALA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 WP 29 413UA 470 GREEN HYDRAULIC SYSTEM RESERVOIR INDICATED LOW FOLLOWED BY ECAM ALERT, SYSTEM GREEN PRESSURE LOW. CREW FOLLOWED ECAM PR OCEDURES FOR LANDING WITH MANUAL GEAR EXTENSION ACCOMPLISHED. *S/D* FAILED LOW LEVEL SWITCH GENERATED ECAM MESSAGE. C REW PROCEDURE IS TO SHUT OFF HYDRAULIC PUMP. THIS ACTION GENERATED A LOW PRESSURE MESSAGE AND THE NEED TO GRAVITY EXTEN D GEAR. SWITCH WAS REPLACED AND OPERATIONALLY CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 1996090500104 19960905 00104 NE 1996 9 5 96UAL900644 2 19960820 A 7313 782276 FUEL NOZZLE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 NOZZLE FAILED A UALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 29 7466U 31844 6364 21920 15 MINUTES INTO THE FLIGHT, THE CREW FELT A SUDDEN VIBRATION ACCOMPANIED BY A ONE SECOND BUZZING SOUND. THE CABIN CREW REPORTED A SERIES OF 3 OR 4 THUDS THAT RESEMBLED SPEED BUMPS FOLLOWED BY A CONSTANT VIBRATION FELT IN THE FLOOR IN THE A FT GALLEY AREA. RETURNED TO ORD WITH THROTTLE IN IDLE. OIL PRESSURE NORMAL. NR 3 FUEL NOZZLE FAILED DUE TO CHEVRON SE AL LEAK. THIS CAUSED 3 (EA) T-2 NGV BURN THROUGH AND RESULTED IN SEVERE DOWN STREAM DAMAGE IN THE N1 TURBINE AND EXHAUS T CASE. PART TOTAL CYCLES, 18,652. 2 L 7 3 4F 4 F A3WE E2EA 1996090500105 19960905 00105 WP 1996 9 5 96UAL900645 1 19960820 A 3620 FAIL LIGHT DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 2 PNEU MANI ILLUMINATED A UALA D RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 29 1817U 46616 NR 2 PNEUMATIC MANIFOLD FAILURE LIGHT CAME ON WHEN ADVANCING THROTTLE FOR TAKEOFF. RETURNED TO BLOCKS. 2 L 7 3 4F 4 F A22WE E23EA 1996090500106 19960905 00106 NM 1996 9 5 96UAL900646 1 19960821 A 5754 FLAPS BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LT/RT TE FLAPS OUT OF ADJUST A UALA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 WP 29 7270U 21417 AIRFRAME VIBRATION BETWEEN 340 AND 320 KIAS. VIBRATION GOES AWAY WITH EXTENSION OF SPEED BRAKE AND BELOW 320 KIAS. AD JUSTED LT AND RT OUTBOARD AFT FLAP OUTBOARD ECCENTRICS PER THE 727 MAINTENANCE MANUAL. 2 L 7 3 4F 4 F A3WE E2EA 1996090500107 19960905 00107 NM 1996 9 5 96UAL900647 1 19960821 A 5330 SKIN BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE BS 1006 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 9022U 19060 THE FUSELAGE SKIN AND INTERNAL TEAR STRAP AT BODY STATION 1006 WERE FOUND WITH EXTENSIVE CORROSION IN THE AREA OF STRING ER 24 RIGHT. THE STRINGER WAS FOUND CRACKED DUE TO STRESS CORROSION. AN 8 INCH BY 12 INCH AREA OF SKIN AND AN 14 INCH B Y 18 INCH AREA OF INTERNAL TEAR STRAP WERE CUT OUT. THE CAUSE OF THE CORROSION WAS BLUE WATER IN THE AREA OF THE AFT LA VATORY SERVICE PANEL. A STRINGER SPLICE AND FUSELAGE REPAIR WERE ACCOMPLISHED PER THE STRUCTURAL REPAIR MANUAL. 2 L 7 2 4F 4 F A16WE E2EA 1996090500108 19960905 00108 NM 1996 9 5 96UAL900648 1 19960821 A 3350 LAMP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 306UA 23667 EMERGENCY ESCAPE PATH LIGHTING AT ROWS 12-13. REPLACED LAMP. CHECKS O.K. 2 L 7 2 4F 4 F RT A16WE E2GL 1996090500109 19960905 00109 NM 1996 9 5 96UAL900649 1 19960822 A 5245 65B1055415 DOOR BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE LT AC BAY NOT SECURED A UALA J A DUMP FUEL UNSCHED LANDING E D VIBRATION/BUFFET INFLIGHT SEPARATION CL CLIMB 1 WP 29 155UA 20104 DURING CLIMBOUT, AIRCRAFT EXPERIENCED EXTREME VIBRATION AND ASSOCIATED LOW RUMBLING NOISE IN THE AREA OF L3 AND FORWARD LOWER GALLEY NOISE. DUMPED FUEL AND RETURNED TO MIA. INVESTIGATION REVEALED THAT LEFT HAND GROUND CONNECTION AC PANEL DOOR WAS MISSING. DOOR REPLACED. CAUSE OF LOSS OF DOOR WAS DUE TO UNSECURED LOCKS ON DOOR. 2 L 7 4 4F 4 F A20WE E20EA 1996090500110 19960905 00110 NM 1996 9 5 96UAL900650 1 19960822 A 3350 LIGHT BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 158UA 21054 DOOR 4 RIGHT, EMERGENCY CEILING LIGHT IS INOPERATIVE. REPLACED LIGHT. 2 L 7 4 4F 4 F A20WE E20EA 1996090500111 19960905 00111 WP 1996 9 5 96UAL900651 1 19960822 A 5315 FLOORBEAM DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL BS 899 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 1834U 47966 CRACK IN FLOORBEAM FORWARD CARGO PIT AT STATION 899 APPROXIMATELY 2 FEET FROM LEFT WALL. *S/D* A REPAIR OF STATION 899 FLOORBEAM WAS ACCOMPLISHED. 2 L 7 3 4F 4 F A22WE E23EA 1996090500112 19960905 00112 NE 1996 9 5 96UAL900652 2 19960823 A 7230 55H705 BLADE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE COMPRESSOR FAILED A UALA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 WP 29 186UA 3628 3628 26875 724465 WHILE IN CRUISE AT FL 370 AND EPR 1.21, STALL CONDITION DEVELOPED. REDUCED THROTTLE AND CONDITION CEASED FOR SHORT TIME , HOWEVER, ENGINE THEN STALLED REPEATEDLY. ENGINE SHUT DOWN. HIGH PRESSURE COMPRESSOR STAGE 5 BLADE FAILED. REPLACED ENGINE. PART TOTAL CYCLES, 388. 2 L 7 4 4F 4 F RT A20WE E24NE 1996090500113 19960905 00113 NM 1996 9 5 96UAL900653 1 19960823 A 3350 362624 LAMP BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7274U 21421 ONE EEL STRIP SEGMENT INOPERATIVE AT APPROXIMATELY SEAT ROW 13. LAMP WAS DISCONNECTED FROM CABLE ASSEMBLY. CONNECTED C ABLE AND REPLACED LAMP ASSEMBLY. 2 L 7 3 4F 4 F A3WE E2EA 1996090500114 19960905 00114 1996 9 5 96UAL900654 4 19960823 A 2565 101630304 SLIDE BF GOODRICH BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE RT WING PUNCTURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 605UA 21866 RIGHT OFF WING EVACUATION SLIDE WAS REMOVED FOR TIME CONTROLLED OVERHAUL. UNIT HAS PUNCTURE HOLES WHICH CORRESPOND WITH THE DOOR/PACKBOARD INSTALLATION BOLTS. UNIT REPAIRED BY OUTSIDE EQUIPMENT MANUFACTURER. AIRCRAFT AND INSTALLED EVACUAT ION SLIDES WERE CHECKED TO VERIFY CORRECT BOLT LENGTH. THE 767 FLEET WILL BE SAMPLED TO CHECK FOR SIMILAR EVACUATION SL IDE DAMAGE. 2 L 7 2 4F 4 F RT A1NM E3NE 1996090500115 19960905 00115 WP 1996 9 5 MWEA96422 1 19960827 A 2560 113317 SLIDE DOUG DC9 DC932 3022066 WP GALLEY SERV DOOR FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 206ME 47791 CREW REPORTS GALLEY SERVICE DOOR EVACUATION SLIDE FELL OFF MOUNT. REINSTALLED GALLEY DOOR EVACUATION SLIDE. 2 L 7 2 4F A6WE 1996090500116 19960905 00116 NM 1996 9 5 DLM88961949 1 19960822 A 3260 49397141 SENSOR SPRING DOUG MD88 MD88 3023688 NM RT MLG UP SENSOR BROKEN A DALA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SO 27 991DL 53343 AFTER TAKEOFF WITH GEAR UP, THE RT GEAR UNSAFE LIGHT STAYED ON. GEAR DOOR CLOSED INDICATION OK AND NO ADVERSE FLT CHAR ACTERISTICS. FOUND RT MLG UPLOCK SENSOR SPRING BROKEN. REPLACED SAME, PERFORMED GEAR SWING, AND CHECK-OUT PER MM 32-60 -00. ALL INDS AND OPERATION CHECK NORMAL. 2 L 7 2 4F RT A6WE 1996090500117 19960905 00117 NM 1996 9 5 DLM88961951 1 19960822 A 3240 BRAKE 329001469 DOUG MD88 MD88 3023688 NM LT MLG OVERHEATED A DALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 27 907DL 704 49538 TEN MINUTES AFTER TAKEOFF, BRAKE OVERHEAT LIGHT ILLUMINATED. TEMP ON NR 1 BRAKE, LEFT OUTBOARD, INDICATED 500 DEGREES. LOWERING GEAR PER POM REDUCED TEMPERATURE TO 300 DEGREES LESS THAN 300 DEGREES AND OVERHEAT LIGHT WENT OUT. AFTER RAIS ING GEAR, TEMPERATURE AGAIN ROSE TO ABOVE 300 DEGREES AND LIGHT RE-ILLUMINATED. TEMPERATURE, VERY GRADUALLY, APPROXIMA TELY 1 HOUR, REDUCED TO 100 DEGREES . PRECAUTIONARY DIVERTED TO JFK FOR LONG RUNWAY. 2 L 7 2 4F RT A6WE 1996090500118 19960905 00118 NE 1996 9 5 DL73E961961 2 19960823 A 7250 TURBINE BOEING 737 737247 138448D NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE FAILED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 27 374DL 29174 23521 709144 NR 2 ENGINE HAD TURBINE FAILURE ON TAKEOFF ROLL. 2 L 7 2 4F 4 F A16WE E2EA 1996090500119 19960905 00119 NM 1996 9 5 DL767961965 1 19960825 A 2530 COFFEE MAKER 811150417 BOEING 767 767232 1385132 NM GALLEY FAULTY A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 101DA 22213 THE F/C NR 2 COFFEE MAKER STARTED SMOKING WHEN BREW BUTTON WAS PRESSED. SMOKE STOPPED AFTER CIRCUIT BREAKER PULLED. RE PLACED COFFEE MAKER. SYSTEM CHECK GOOD. 2 L 7 2 4F RT A1NM 1996090500120 19960905 00120 NM 1996 9 5 DLM11961968 1 19960825 A 3350 TRACK LIGHT DOUG MD11 MD11 3023602 NM PWA JT8 JT8D15A 52051 NE CABIN FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 801DE 0145 48472 709144 ON CHECK, FOUND TRACK LIGHTS OUT ON LT AND RT AISLES FROM ROW 37 AND 39 TO 51. FOUND PIGTAIL AT 37G BAD. REPLACED SAM E AT 37G. ALSO, REPLACED FWD LT BATTERY PACK. ALL OPS NORMAL. 2 L 7 3 4F 4 F RT A22WE E2EA 1996090500121 19960905 00121 NM 1996 9 5 DL73S961969 1 19960826 A 3350 OL3071LBPEGP BOEING 737 737232 1384475 NM CABIN BURNED OUT A DALA O OTHER L NO TEST IN INSP/MAINT 1 SO 27 329DL 23101 EMERGENCY LIGHTS AT 1L DOOR AND ROWS 17 ABC, 21 ABC, AND 25 ABC INOPERATIVE. 2 L 7 2 4F RT A16WE 1996090500122 19960905 00122 NM 1996 9 5 DL72P961980 1 19960826 A 3350 334102486 BOEING 727 727225 1384077 NM CABIN BATTERY EMPTY A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8890Z 1113 21859 FOUND LT OVERWING EMERGENCY LIGHT OUT. REPLACED BATTERY PACK. OPS CHECK OK. 2 L 7 3 4F A3WE 1996090500123 19960905 00123 NM 1996 9 5 DL72S961988 1 19960810 A 3397 WIRE BOEING 727 727232 1384082 NM CABIN CHAFED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 531DA 21814 ON SERVICE CHECK, FOUND MID-FRONT EMERGENCY TRACK LIGHTS AND ALL FOUR OVERWING EMERGENCY EXIT IDENT LIGHTS INOPERATIVE. FOUND WIRE SHORTED AT SIDEWALL WHERE TRACK LIGHT WIRES PASS THROUGH. REPAIRED SAME. LIGHTS NOW TEST OK. 2 L 7 3 4F A3WE 1996090500124 19960905 00124 NM 1996 9 5 SCNA96237 1 19960822 A 5230 SKIN BOEING 727 7272J4 1384006 NM CARGO DOOR CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 288SC 20765 FOUND A SMALL CRACK IN SKIN ON THE C3 DOOR, LOWER AFT CORNER. REPAIRED CRACK IN ACCORDANCE WITH SRM 52-20-2. 2 L 7 3 4F RT A3WE 1996090500125 19960905 00125 WP 1996 9 5 SCNA96238 1 19960826 A 2611 30231R17 BULB DOUG DC10 DC1030F 3023504 WP LWR AFT CARGO INOP A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 601GC 47921 FOUND LOWER AFT CARGO SMOKE DETECTOR NR 2 WILL NOT TEST. REPLACED BULB ON LOWER AFT CARGO SMOKE DETECTOR AND OPS CHECKE D IN ACCORDANCE WITH MM 26-00-00. 2 L 7 3 4F RT A22WE 1996090500126 19960905 00126 WP 1996 9 5 RRXA96068 1 19960828 A 2120 AIR DISTR DOUG DC8 DC863 302198A WP CABIN ODOR A RRXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 15 797AL 46163 KDEN - FLT 110 - FUMES COME FROM CABIN AIR WHEN WARM SELECTED MANUALLY, COLD SELECTION OK, (DMI NR 608227 DEFERS AUTO CO NTROL OF TEMP). RAN ENGINE OPERATED SYSTEM PER MM CHAPTER 21-00 IN WARM AND COLD POSITIONS MANUALLY. COULD NOT DUPLICA TED ANY FUMES ON GROUND. ALL DUCTS CHECKED NORMAL, NO DEFECTS NOTED AT THIS TIME. (M) 2 L 7 4 4F 4A25 1996090500134 19960905 00134 CE 1996 9 5 96ZZZX4226 1 19960715 A 7810 MUFFLER CESSNA 177 177B 2073708 CE ENGINE STACK PARTED A P GBHA K NONE O OTHER NR NOT REPORTED 1 NM 01 34348 68 17701775 EXIT STACK OF MUFFLER SEPARATED FROM THE MUFFLER. SUBMITTER STATED APPEARS WELDS MAY NOT HAVE BEEN 'NORMALIZED' CAUSING A BRITTLE AREA AROUND THE WELD. THIS WAS AN FAA-PMA PART. ENGINE SHOWED NO SIGNS OF VIBRATION. EXHAUST EXITED THE MU FFLER INTO COWLING, GASCOLATOR, AND CARBURETOR AREA. 1 H 7 1 3O A13CE 1996090500147 19960905 00147 CE 1996 9 5 96ZZZX4239 1 19960702 A 3230 GEAR CESSNA 310 310K 2074228 CE MLG MALFUNCTIONED A BSYA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 37223 310R0963 GEAR WOULD NOT EXTEND. HAND CRANKED 2-3 TURNS, THEN WAS OK. JACKED AIRCRAFT, CYCLED GEAR MANY TIMES, COULD NOT DUPLICA TE. 1 L 7 2 3O 3A10 1996090500151 19960905 00151 WP 1996 9 5 9618739609 1 19960828 A 3350 60030451 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 609NW 47234 DURING PREFLIGHT INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS AT ROWS 13 AND 14 INOPERATIVE. REPLACED BATTERY PACK AND P OWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996090500152 19960905 00152 WP 1996 9 5 9618749609 1 19960827 A 3350 6011779 BATTERY PACKS DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 609NW 47234 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT AND RIGHT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996090500153 19960905 00153 WP 1996 9 5 9618759912 1 19960829 A 3350 6011779 POWER SUPPLY DOUG DC9 DC931 3022065 WP RT NACELLE MALFUNCTIONED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 962N 47406 DURING PERIODIC CHECK, RIGHT NACELLE EMERGENCY LIGHT WOULD NOT TEST. REPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996090500154 19960905 00154 WP 1996 9 5 9618769922 1 19960829 A 3350 60030451 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 945N 47664 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OP ERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996090500155 19960905 00155 WP 1996 9 5 9618779971 1 19960829 A 3350 60030451 POWER SUPPLY DOUG DC9 DC931 3022065 WP TAILCONE MALFUNCTIONED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9335 47337 DURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE TRACK EMERGENCY LIGHTING INOPERATIVE. REPLACED POWER SUPPLY, OPERATI ONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996090500156 19960905 00156 WP 1996 9 5 9618789933 1 19960826 A 2780 PULLEY BRACKET DOUG DC9 DC931 3022065 WP LT TE FLAP FAILED A A NWAA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 01 1334U 47280 SLAT DISAGREEMENT LIGHT ILLUMINATED WITH ASYMMETRIC SLATS ON APPROACH. THERE WAS NO BLUE SLAT EXTEND LIGHT. AIRCRAFT L ANDED WITHOUT INCIDENT. MAINTENANCE FOUND LEFT INBOARD SLAT DRIVE NR 1 PULLEY, CABLE AND BRACKET PULLED FROM FORWARD SP AR. REPLACED PULLEY, BRACKET AND DAMAGED RIBS. ADJUSTED SLAT CABLES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996090500157 19960905 00157 WP 1996 9 5 9618799931 1 19960826 A 3230 RETRACT MECH DOUG DC9 DC931 3022065 WP LT/RT MLG OUT OF ADJUST A NWAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 01 90S 47244 DURING APPROACH, LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS EXTENDED. GO-AROUND PROCEDURES WERE EXECUTED A ND TOWER VISUALLY CONFIRMED THAT GEAR WAS DOWN AND THAT DOORS APPEARED CLOSED. EMERGENCY GEAR EXTENSION PROCEDURES WERE UTILIZED AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED MAIN GEAR CONTROL VALVE WITH NO HELP. ALSO, REPLA CED LEFT MAIN GEAR DOOR DUE TO DAMAGE INCURRED ON LANDING. AIRCRAFT WAS FERRIED TO ATL FOR REPAIR. MAINTENANCE ADJUSTE D LEFT AND RIGHT MAIN GEAR ACTUATING CYLINDER. CYCLED GEAR SEVERAL TIMES, ALL INDICATIONS WERE NORMAL. 2 L 7 2 4F A6WE 1996090500158 19960905 00158 WP 1996 9 5 9618809605 1 19960826 A 3260 UPLOCK SWITCH DOUG DC9 DC932 3022066 WP LT MLG MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 605NW 47233 LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. RECYCLED GEAR WITH SAME RESULTS. FLIGHT RETU RNED TO YYC AND LANDED WITHOUT INCIDENT. AIRCRAFT WAS FERRIED TO MSP. MAINTENANCE REPLACED LEFT MAIN GEAR UPLOCK SWITC H, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996090500159 19960905 00159 WP 1996 9 5 9618819613 1 19960828 A 3350 SWITCH DOUG DC9 DC932 3022066 WP CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 613NW 47438 FLIGHT ATTENDANT REPORTED EMERGENCY LIGHTS FLICKERING ON AND OFF DURING TAKEOFF AND LANDING. REPLACED EMERGENCY LIGHT S WITCH, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996090500160 19960905 00160 EU 1996 9 5 9618823249 1 19960829 A 2750 RETRACT MECH AIRBUS 320 A320212 EU TE FLAPS MALFUNCTIONED A NWAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 01 349NW 418 DURING APPROACH, RECEIVED F/CTL FLAPS LOCKED-WING TIP BRAKE ON MESSAGE WHEN MOVING THE FLAP HANDLE FROM THE NR 1 POSITIO N IN THE NR 2 POSITION. ACCOMPLISHED A MISSED APPROACH, DIVERTED TO EWR AND LANDED WITHOUT INCIDENT ON A LONGER RUNWAY. MAINTENANCE TROUBLESHOOTING REVEALED NO DISCREPANCY. 2 L 7 2 4F RT A28NM 1996090500161 19960905 00161 WP 1996 9 5 9618839978 1 19960828 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP TAIL COMPT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9342 47391 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONA L CHECK NORMAL. 2 L 7 2 4F A6WE 1996090500162 19960905 00162 WP 1996 9 5 9618849961 1 19960826 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN CHAFED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 924RW 47185 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. FOUND CHAFED WIRE S AT SEAT 3D FROM 4D FOOT REST. SECURED WIRES, REPLACED FUSE IN CHARGE UNIT AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996090500163 19960905 00163 WP 1996 9 5 9618859955 1 19960826 A 3350 6011779 BATTERY PACK DOUG DC9 DC931 3022065 WP RT NACELLE MALFUNCTIONED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 922RW 47182 DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996090500164 19960905 00164 WP 1996 9 5 9618869940 1 19960826 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 3322L 47031 DURING LINE MAINTENANCE INSPECTION, FOUND BOTH LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS DIM. REPLACED BATTERIES, O PERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996090500165 19960905 00165 WP 1996 9 5 9618879955 1 19960826 A 3350 FUSE DOUG DC9 DC931 3022065 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9922R 47182 DURING PREFLIGHT CHECK, FOUND SEVERAL INTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BLOWN FUSE FOR RIGHT AFT OVERWING EMERGENCY EXIT LIGHTS, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996090500166 19960905 00166 SO 1996 9 5 COMA9610264 1 19960829 A 5280 AN421 BOLT EMB 120 EMB120RT SO RT MLG DOOR BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 189CA 120189 RT MLG DOOR HINGE BOLT WAS BROKEN. REPLACED BROKEN BOLT. 2 L 7 2 4T RT A31SO 1996090500167 19960905 00167 SO 1996 9 5 COMA9610265 1 19960829 A 5240 12034826501 DOOR ASSY EMB 120 EMB120RT SO COCKPIT FLOOR BROKEN A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 179CA 120179 EMERGENCY LANDING GEAR EXTEND COMPARTMENT DOOR HINGE WAS BROKEN. REPAIRED BROKEN HINGE. 2 L 7 2 4T RT A31SO 1996090500168 19960905 00168 SO 1996 9 5 COMA9610266 1 19960828 A 3230 12038594001 CONTROL BOX EMB 120 EMB120RT SO LANDING GEAR MALFUNCTION A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 267CA 13755 2975 120259 WHEN LANDING GEAR SELECTED DOWN, THE INDICATION WAS BOTH DOWN LOCK GREEN AND RED UNSAFE AT THE SAME TIME. REPLACED THE LANDING GEAR CONTROL BOX. 2 L 7 2 4T RT A31SO 1996090500169 19960905 00169 SO 1996 9 5 COMA9610267 1 19960829 A 5753 12020278613 SKIN EMB 120 EMB120RT SO LT TE FLAP CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 268CA 120262 LT OUTBD FLAP WAS CRACKED AT SEVERAL PLACES ON TRAILING EDGE. REPLACED FLAP. 2 L 7 2 4T RT A31SO 1996090500170 19960905 00170 NM 1996 9 5 96FDEA01420 1 19960830 A 5330 65183874 SKIN BOEING 727 72722 1384002 NM BS 950-1080 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 REMOVE AND INSTALLED NEW BELLY SKIN FROM BS 950 TO 1080.45, STR 26 LT TO 26 RT DUE TO MULTIPLE REPAIRS REQUIRED. REMOVE D AND REPLACED BELLY SKIN FROM BS 950 TO 1080.45 STR 26 RT TO STR 26 LT IAW RED EX EA 7-5330-29745. 2 L 7 3 4F A3WE 1996090500171 19960905 00171 1996 9 5 96FDEA01421 4 19960830 A 3414 30416923 STICK SHAKER BOEING 727 72725 1384006 NM E/E COMPT FAILED TEST A FDEA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SO 25 136FE 19855 CONTINUOUS STICK SHAKER AT TAKEOFF. STANDARD POWER TAKEOFF 36C, ADVANCED THROTTLES TO MOMENTARY FIREWALL POWER. PULLED AC NR 1 STALL WARNING CIRCUIT BREAKER, SHAKER STOPPED. ATTEMPTED 1 RESET OF CIRCUIT BREAKER, STILL HAD SHAKER. PULLED CIRCUIT BREAKER AND RETURNED TO LAND. FOUND STALL COMPUTER NR 1 WOULD NOT TEST ON GROUND. REMOVED AND REPLACED NR 1 S TALL WARNING COMPUTER, GROUND CHECKS NORMAL. 2 L 7 3 4F A3WE 1996090500172 19960905 00172 NM 1996 9 5 VNAA9608005 1 19960829 A 3246 WHEELS DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NLG WORN A VNAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 442JS 3060 AT ROTATION CREW HEARD LOUD THUD, UPON GEAR RETRACTION HEARD LOUD SLAPPING SOUND. CREW DECLARED AN EMERGENCY AND DIVERT ED TO PIT. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND FOUND NO DISCREPANCIES. REPLACED NOSE WHEELS AS A PRECAUTIONARY MEASURE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996090500173 19960905 00173 NM 1996 9 5 VNAA9608006 1 19960829 A 3320 325310 BALLAST DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT CABIN DEFECTIVE A VNAA A UNSCHED LANDING B H SMOKE/FUMES/ODORS/SPARKS ELECT. POWER LOSS-50 PC CR CRUISE 1 GL 07 430JS 3044 FLIGHT ATTENDANT SMELLED ELECTRICAL ODOR IN MIDDLE OF THE CABIN. NOTIFIED CAPTAIN, DETERMINED PROBLEM TO BE LT CABIN LI GHTS. TURNED OFF THE LH LIGHTS AND THE ODOR STARTED TO DEMINISH. CREW ELECTED TO DIVERT TO PIT. AIRCRAFT LANDED WITHO UT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND FOUND NR 7 LT BALLAST UNIT DEFECTIVE. REPLACED BALLAST UNIT IN ACCORDA NCE WITH DORNIER MAINTENANCE MANUAL 33-21-21. OPERATIONAL CHECK GOOD AND AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996090500174 19960905 00174 WP 1996 9 5 ABXA9600615 1 19960828 A 3231 RETRACT MECH DOUG DC8 DC862 3021970 WP RT NLG DOOR LACK OF LUBE A ABXA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 23 803AX 45917 VIBRATION AND BUFFETING OCCURS IN FLIGHT IN GEAR UP/DOWN AND FLAPS UP/ DOWN CONFIGURATION. GREATER AT HIGHER AIRSPEEDS UP TO 210 KNOTS. FOUND RIGHT NOSE GEAR DOOR OPEN ON ARRIVAL. LUBED ALL FITTINGS, CLOSED DOOR SEVERAL TIMES AND NO DEFE CTS NOTED. 2 L 7 4 4F 4A25 1996090500175 19960905 00175 WP 1996 9 5 ABXA9600616 1 19960827 A 2120 AIR DISTR DOUG DC8 DC861 3021952 WP CABIN ODOR A ABXA G O2 MASK DEPLOYED B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 846AX 46158 NOXIOUS ODOR IN AIRCRAFT. CREW DONNED OXYGEN MASKS AS A PRECAUTION. NOTICED A METALLIC TASTE AND RESPIRATORY IRRITATIO NS. INSPECTED THE AIRCRAFT, INCLUDING BELLY AND MAIN CABIN WITH VARIOUS TEST EQUIPMENT, NO NOXIOUS SPILLS NOTED. AIRCR AFT MAINTENANCE ALSO INSPECTED THE AIRCRAFT, NO DEFECTS NOTED. 2 L 7 4 4F 4A25 1996090500176 19960905 00176 WP 1996 9 5 ABXA9600617 1 19960829 A 3350 BATTERY DOUG DC9 DC941 302207N WP CABIN CORRODED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 965AX 47498 EMERGENCY LIGHTS INOPERATIVE. CLEANED CORRODED BATTERY CONTACTS, OPS CHECKED GOOD PER DC-9 SMM 33-53-0. 2 L 7 2 4F A6WE 1996090500177 19960905 00177 NM 1996 9 5 DL76L961960 1 19960824 A 2121 FAN BOEING 767 767332 1382001 NM FWD CARGO COMPT FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 181DN 25986 AFTER TAKEOFF 1.5 HOURS INTO FLIGHT, SMELLED ELECTRICAL FUMES IN COCKPIT ACCOMPANIED BY FWD EQUIPMENT EXHAUST FAN STATUS MESSAGE ON EICAS. CALLED FLIGHT CONTROL AND MTC COORDINATOR TO DISCUSS SITUATION AND DECIDED TO PULL P-22 CB. FUMES D ISSIPATED AND FLIGHT WAS CONTINUED. UPON FURTHER INVESTIGATION FOUND THE FWD EXH EQUIP COOL FAN C/B ON P-6 PANEL POPPED . REPLACED FWD EQUIPMENT EXHAUST FAN, SYSTEM CHECKS NORMAL. 2 L 7 2 4F RT A1NM 1996090500178 19960905 00178 EU 1996 9 5 DL31J961963 1 19960824 A 3240 BRAKES AIRBUS 310 A310324 3930206 EU NR 7/8 OVER TEMP A A DALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 27 839AD 678 ON T/O PRIOR TO ROTATION, MC CAME ON WITH BRAKES HOT. T/O CONT AND GEAR LEFT EXTENDED. BRAKE UNIT 7 WENT TO 295 DEG AN D UNIT 8 TO 340 DEG CLIMBED TO 11000 AND 230 KTS, UNABLE TO COOL BRAKES AFTER APPROX 20 MINS. RETURNED TO KIN. INSP BR AKES 7 AND 8 AS PER MM 05-51-16 AND MM 32-40-00 PG 601, NO FAULTS FOUND. COOLED BRAKES WITH AIR COND AND BOTH TEMPS FEL L TO 40 DEG, BRAKE TEMP SYS FOUND SERVICEABLE. BOTH BRAKES BLED WITH SIGNIFICANT AMTS OF AIR EXPELLED. BOTH BRAKES CON SIDERED OK. 2 L 7 2 4F RT A35EU 1996090500179 19960905 00179 NM 1996 9 5 DL72S961979 1 19960827 A 3350 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 403DA 21147 ROW 35 EMERGENCY FLOOR PATH LGHT INOP. REPLACED LIGHT, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1996090500180 19960905 00180 NE 1996 9 5 DL76L961982 2 19960827 A 7230 COMPRESSOR BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE STALLED A DALA A UNSCHED LANDING E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 27 175DN 24803 723168 LEFT ENGINE COMPRESSOR STALL IMMEDIATELY AFTER T/O. MADE SUCCESSFUL LANDING WITH LEFT ENGINE AT IDLE. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 1996090500181 19960905 00181 NM 1996 9 5 DL72S961986 1 19960827 A 3350 1000677 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 406DA 21150 ON LAYOVER, FOUND LEFT FWD ENTRY DOOR EMERGENCY LIGHT NOT TESTING. REPLACED LIGHT ASSEMBLY (P/N 334701743) AND BATTERIE S. LIGHT NOW TESTS OK. 2 L 7 3 4F A3WE 1996090500182 19960905 00182 NM 1996 9 5 DL72S961996 1 19960828 A 3350 0L3071BPEGPL BULB BOEING 727 727232 1384082 NM CABIN BURNT OUT A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 537DA 22073 TWO BULBS OUT ON EMERGENCY TRACK LIGHTING. REPLACED BULBS, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1996090500183 19960905 00183 1996 9 5 DHL96804011 4 19960825 A 2210 YAW DAMPER DOUG DC8 DC873F 302199F WP RUDDER MALFUNCTIONED A DHLA A J UNSCHED LANDING DUMP FUEL O OTHER CL CLIMB 1 SO 01 804DH 46124 AFTER TAKEOFF, RUDDER BEGAN EXTREME OSCILLATION. AFTER YAW DAMPER DISENGAGED, OSCILATION STOPPED. DEFERRED PER MEL. 2 L 7 4 4F RT 4A25 1996090500184 19960905 00184 NE 1996 9 5 P5CA9600666 2 19960829 A 7200 ENGINE BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 1 OVER TEMP A P5CA C D ABORTED TAKEOFF RETURN TO BLOCK M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 WP 23 851FT 19756 662326 ON TAKEOFF ROLL, NR 1 ENGINE ROLL REACHED 942 DEGREES FOR 2 SECONDS. ABORTED TAKEOFF, RETURNED TO GATE. ENGINE CHANGE D PER BOEING MAINTENANCE MANUAL 71-00-02. 2 L 7 4 4F 4 F A20WE E20EA 1996090500185 19960905 00185 NM 1996 9 5 P5CA9600667 1 19960805 A 5210 MOUNT BOLTS BOEING 747 747121 1384871 NM L2 DOOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 LEVEL 1 CORROSION ON MOUNT BOLTS NR 2 ENTRY DOOR. REMOVED AND TREATED CORROSION PER BOEING SRM 51-21-03. 2 L 7 4 4F A20WE 1996090500186 19960905 00186 WP 1996 9 5 CKSA96082 1 19960827 A 5330 SKIN DOUG DC8 DC8F55 3021928 WP BS 600 BULGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND FS 600 L-36 BULGE IN SKIN. REPAIRED BULGE IN SKIN PER DC-8 SRM 53-2-1 FIGURE 7. TAS K NR 80841, CORROSION CARD NR 5570-0551. 2 L 7 4 4F 4A25 1996090500187 19960905 00187 WP 1996 9 5 CKSA96083 1 19960827 A 5751 SKIN DOUG DC8 DC8F55 3021928 WP AILERON DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND OUTBOARD AILERON INBOARD LOWER SKIN DAMAGED. REPAIRED LOWER SKIN IAW AIA EA DWG 2248 6161 SKETCH NR AIA/E/2249, TASK NR 80134, CORROSION CARD NR 111R-0551. 2 L 7 4 4F 4A25 1996090500188 19960905 00188 WP 1996 9 5 CKSA96084 1 19960827 A 5320 4641326N SPLICE PLATE DOUG DC8 DC8F55 3021928 WP BS 1490 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND STA 1490 S-30 LEFT IN AFT ACCESSORY COMPARTMENT SPLICE PLATE CORRODED. REMOVED AND R EPLACED SPLICE PLATE IAW SRM 51-1-21 AND 51-3-1. TASK NR 80534, CORROSION CARD NR 5600-0551. 2 L 7 4 4F 4A25 1996090500189 19960905 00189 WP 1996 9 5 CKSA96085 1 19960827 A 5320 4641326N SPLICE PLATE DOUG DC8 DC8F55 3021928 WP BS 1490 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND STA 1490 STRINGER 28R IN AFT ACCESSORY COMPARTMENT SPLICE PLATE CORRODED. REMOVED CO RRODED SPLICE PLATE AND REPLACED WITH NEW SPLICE PLATE IAW DC8 SRM 51-1-21 AND DC8 SRM 51-3-1. TASK NR 80535, CORROSION CARD NR 5600-0551. 2 L 7 4 4F 4A25 1996090500190 19960905 00190 WP 1996 9 5 CKSA96086 1 19960827 A 5730 56112703 SKIN DOUG DC8 DC8F55 3021928 WP WS 310-329 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND UPPER SKIN ON LEADING EDGE AT STA XFS 310 TO 329 WAS CRACKED AROUND SCREW HOLES. REP AIRED IAW DC8 SRM 57-2-1. TASK NR 80061, CORROSION CARD NR 116L-0550 AND 116R-0550. 2 L 7 4 4F 4A25 1996090500191 19960905 00191 WP 1996 9 5 CKSA96087 1 19960827 A 5320 4611067 FITTING DOUG DC8 DC8F55 3021928 WP BS 310 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND BATHTUB FITTING AT FS 310 STRINGER 26R CORRODED. FITTING WAS CORRODED BEYOND LIMITS. REPLACED BATHTUB FITTING IAW DC8 SRM CHAPTERS 51-1-8, 51-1-20D, 51-1-21, 51-3-0 AND 53-2-2. TASK NR 80996, CORROSION CARD NR 5670-0551. 2 L 7 4 4F 4A25 1996090500192 19960905 00192 WP 1996 9 5 CKSA96088 1 19960827 A 5311 FRAME DOUG DC8 DC8F55 3021928 WP BS 1200 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND AFT BELLY PIT CORROSION ON FS 1200 BETWEEN STRINGER 33R TO 33L. REMOVED CORROSION FR OM FRAME AND FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. REPAIRED FRAME IAW DC8 SRM 53-2-0 FIGURE 2, 51-1-21. TREATE D AND PAINTED IAW DC8 SRM 51-1-8. TASK NR 80537, CORROSION CARD NR 5590-0551. 2 L 7 4 4F 4A25 1996090500193 19960905 00193 WP 1996 9 5 CKSA96089 1 19960827 A 5330 SKIN DOUG DC8 DC8F55 3021928 WP BS 540 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND FS 540 L36 LOWER BELLY SKIN CORRODED. REMOVED CORROSION AND INSTALLED REPAIR PER SRM 53-2-1. TASK NR 80746, WORK CARD NR 0011. 2 L 7 4 4F 4A25 1996090500194 19960905 00194 WP 1996 9 5 CKSA96090 1 19960827 A 5320 1415997 FITTING DOUG DC8 DC8F55 3021928 WP BS 560 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND FS 560 L36 BULGE IN SKIN. REMOVED CORROSION, TREATED AREA AND REPLACED LONGERON END FITTING. DRAWING NR 5774353, TASK NR 80840, CORROSION CARD NR 5570-0551. 2 L 7 4 4F 4A25 1996090500195 19960905 00195 WP 1996 9 5 CKSA96091 1 19960827 A 5320 4641326N FITTING DOUG DC8 DC8F55 3021928 WP BS 1490 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND STATION 1490 STRINGER 29L IN AFT ACCESSORY COMPARTMENT SPLICE PLATE CORRODED, MARKED. CLEANED AND TREATED CORROSION IAW 51-1-8 WITHIN LIMITS 53-2-0 AND REPLACED FITTING PER SRM 51-1-20D. TASK NR 80533 CO RROSION CARD NR 5600-0551. 2 L 7 4 4F 4A25 1996090500196 19960905 00196 WP 1996 9 5 CKSA96092 1 19960827 A 5753 3646375501 LINK ASSY DOUG DC8 DC8F55 3021928 WP TE FLAPS CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND INBOARD MOST FLAP CARRIAGE LINK ASSEMBLY FWD END APPEARS CRACKED. REMOVED AND REPLAC ED INBOARD MOST FLAP CARRIAGE LINK ASSEMBLY. TASK NR 79978, CORROSION CARD NR 124L-0551. 2 L 7 4 4F 4A25 1996090500197 19960905 00197 WP 1996 9 5 CKSA96093 1 19960827 A 5313 561386135 STRINGER DOUG DC8 DC8F55 3021928 WP BS 275-295 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND STRINGER 24R CORRODED BETWEEN FS 295 AND FS 275. REMOVED AND REPLACED STRINGER IAW D C8 SRM 51-1-8, 51-1-21, 51-1-20D, 51-1-22 AND 53-2-2 FIGURE 10. TASK NR 81001 CORROSION CARD NR 5570-0551. 2 L 7 4 4F 4A25 1996090500198 19960905 00198 WP 1996 9 5 CKSA96094 1 19960827 A 5313 561386135 STRINGER DOUG DC8 DC8F55 3021928 WP BS 295-310 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND STRINGER 24R CORRODED BETWEEN FS 310 AND FS 295. REMOVED AND REPLACED STRINGER IAW D C8 SRM 51-1-8, 51-1-21, 51-1-20D, AND 51-1-22. TASK NR 80999, CORROSION CARD NR 5570-0551. 2 L 7 4 4F 4A25 1996090500199 19960905 00199 WP 1996 9 5 CKSA96095 1 19960827 A 5320 WEB DOUG DC8 DC8F55 3021928 WP PAX DOOR AREA DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND WEB ABOVE LEFT HAND AFT ENTRANCE DOOR DAMAGED. REMOVED AND REPLACED WEB IAW DC8 SRM 53-2-0, 51-1-21, AND 51-1-11. TASK NR 80958, WORK CARD NR 3043. 2 L 7 4 4F 4A25 1996090500200 19960905 00200 WP 1996 9 5 CKSA96096 1 19960827 A 5320 4611067 FITTING DOUG DC8 DC8F55 3021928 WP BS 310 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND BATHTUB FITTING AT FS 310 STRINGER 25R CORRODED. REMOVED AND REPLACED BATHTUB FITTIN G IAW DC8 SRM 51-1-8, 51-1-21, 53-2-0 AND 51-1-20D. TASK NR 80997, CORROSION CARD NR 557R-0551. 2 L 7 4 4F 4A25 1996090500201 19960905 00201 WP 1996 9 5 CKSA96097 1 19960827 A 5315 AISI177 FLOOR BEAM DOUG DC8 DC8F55 3021928 WP BS 940 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND FS 940 FLOOR BEAM CORRODED AT RBL 8. REPAIRED IAW AIA EA DRAWING NR 2259 FILE NR 225 96161 DATED 7-26-96. TASK NR 80862, CORROSION CARD NR 2000-0551. 2 L 7 4 4F 4A25 1996090500202 19960905 00202 WP 1996 9 5 CKSA96098 1 19960827 A 5330 SKIN DOUG DC8 DC8F55 3021928 WP BS 540 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND FS 540 L-36 LOWER BELLY SKIN CORRODED. REMOVED CORROSION, CLEANED AREA, TREATED INST ALLED PATCH AS PER SRM 51-1-8 SRM 53-2-1 CLASS I. TASK NR 81484, CORROSION CARD NR 5570-0551. 2 L 7 4 4F 4A25 1996090500203 19960905 00203 WP 1996 9 5 CKSA96099 1 19960827 A 5320 ANGLE DOUG DC8 DC8F55 3021928 WP BS 565 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND FS 565 DOOR JAMB FRAME ANGLE CORRODED. REPLACED ANGLE IAW SRM 53-2-0, 51-1-21, 51-3- 0. TASK NR 80686, CORROSION CARD NR 5590-0551. 2 L 7 4 4F 4A25 1996090500204 19960905 00204 WP 1996 9 5 CKSA96100 1 19960827 A 5320 INTERCOSTAL DOUG DC8 DC8F55 3021928 WP BS 1020 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND INTERCOSTAL AT FS 1020 CORRODED BELOW NUTPLATES AT STRINGER 33R. REMOVED AND REPLACE D INTERCOSTAL AT FS 1020 IAW DC8 SRM 53-2-0, AND 51-1-21. TREATED AND PRIMED IAW DC8 SRM 51-1-8. TASK NR 80645, CORROS ION CARD NR 5590-0551. 2 L 7 4 4F 4A25 1996090500205 19960905 00205 WP 1996 9 5 CKSA96101 1 19960827 A 5347 S2772660 SEAT TRACK DOUG DC8 DC8F55 3021928 WP BS 640-860 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND FS 640 TO 860 LBL 25 SEAT TRACK CORRODED. REMOVED AND REPLACED SEAT TRACK IAW DC8 SR M 53-2-3. TASK NR 80951, CORROSION CARD NR 2000-0551. 2 L 7 4 4F 4A25 1996090500206 19960905 00206 WP 1996 9 5 CKSA96102 1 19960827 A 5320 INTERCOSTAL DOUG DC8 DC8F55 3021928 WP BS 1020 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND INTERCOSTAL AT FS 1020 CORRODED AT STRINGER 33R. REMOVED AND REPLACED INTERCOSTAL AT FS 1020 IAW DC8 SRM 53-2-0 AND 51-1-21. TREATED AND PRIMED IAW DC8 SRM 51-1-8. TASK NR 80644, CORROSION CARD NR 5590- 0551. 2 L 7 4 4F 4A25 1996090500207 19960905 00207 WP 1996 9 5 CKSA96103 1 19960827 A 5313 LONGERON DOUG DC8 DC8F55 3021928 WP BS 1280 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND FS 1280 L-35 LT LONGERON HAS SURFACE CORROSION. CORROSION FOUND OUT OF LIMITS IAW DC 8 SRM 53-2-0. REPAIRED LONGERON 35 LT IAW DC8 SRM 53-2-2 AND 51-1-21. TREATED AND PRIMED IAW DC8 SRM 51-1-8. TASK NR 80549, CORROSION CARD NR 557L-0552. 2 L 7 4 4F 4A25 1996090500208 19960905 00208 WP 1996 9 5 CKSA96104 1 19960827 A 5315 AISI177 FLOOR BEAM DOUG DC8 DC8F55 3021928 WP BS 920 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND FLOOR BEAM AT FS 920 CORRODED AT RBL 33. REMOVED AND TREATED CORROSION IAW SRM 51-01 -08. REPAIRED FLOOR BEAM IAW AIA EA DRAWING NR 2256. TASK NR 80863, CORROSION CARD NR 2000-0551. 2 L 7 4 4F 4A25 1996090500209 19960905 00209 WP 1996 9 5 CKSA96105 1 19960827 A 5315 AISI177 FLOOR BEAM DOUG DC8 DC8F55 3021928 WP BS 902 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND FLOOR BEAM CORRODED AND CRACKED AT FS 902 LBL 40. REMOVED AND TREATED CORROSION IAW DC8 SRM 51-01-08. REPAIRED FLOOR BEAM IAW AIA EA DRAWING NR 2253. TASK NR 80912, CORROSION CARD NR 5700-0553. 2 L 7 4 4F 4A25 1996090500210 19960905 00210 WP 1996 9 5 CKSA96106 1 19960827 A 5320 85300919 SPLICE FITTING DOUG DC8 DC8F55 3021928 WP BS 1140-1160 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND AFT BELLY PIT SPLICE BETWEEN FS 1160 AND 1140 ON STRINGER 33R CORRODED. REMOVED SPLI CE FITTING AND FOUND CRACK IN AFT STRINGER. REPAIRED CRACKED STRINGER IAW DC8 SRM 53-2-2 AND INSTALLED NEW SPLICE FITTI NG IAW DC8 SRM 53-2-2. TREATED AND PRIMED IAW DC8 SRM 51-1-8. TASK NR 80541, CORROSION CARD NR 5590-0551. 2 L 7 4 4F 4A25 1996090500211 19960905 00211 WP 1996 9 5 CKSA96107 1 19960827 A 5320 56119433 ANGLE DOUG DC8 DC8F55 3021928 WP BS 310 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND FS 310 T-CHORD CORRODED FROM L-28LT TO 28RT. REMOVED SECTION OF FWD ANGLE FROM 28R-2 8L. INSTALLED NEW ANGLE IAW SRM 53-2-5 FIGURE 8C. TASK NR 82169, CORROSION CARD NR 5570-0551. 2 L 7 4 4F 4A25 1996090500212 19960905 00212 WP 1996 9 5 CKSA96108 1 19960827 A 5320 46146372 FITTING DOUG DC8 DC8F55 3021928 WP BS 310 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND FS 310 L-31R END FITTING CORRODED. REMOVED AND REPLACED FITTING IAW SRM 51-1-8, 51-1 -21, 51-1-20D AND 51-1-22. TASK NR 82166, CORROSION CARD NR 5570-0551. 2 L 7 4 4F 4A25 1996090500213 19960905 00213 WP 1996 9 5 CKSA96109 1 19960827 A 5320 46146372 FITTING DOUG DC8 DC8F55 3021928 WP BS 310 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND BATHTUB FITTING AT FS 310 STRINGER 31L CORRODED. REMOVED AND REPLACED FITTING PER SR M 53-2-0, 51-1-21, 51-1-20D AND 51-3-0. TASK NR 81008, CORROSION CARD NR 5570-0551. 2 L 7 4 4F 4A25 1996090500214 19960905 00214 WP 1996 9 5 CKSA96110 1 19960827 A 5347 S2772660 SEAT TRACK DOUG DC8 DC8F55 3021928 WP CABIN CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND SEAT TRACK AT RBL 50 CORRODED AT ATTACH POINTS. REMOVED AND REPLACED SEAT TRACK IAW DC8 SRM 51-1-21 AND 51-3-0. TASK NR 80938, CORROSION CARD NR 5700-0553. 2 L 7 4 4F 4A25 1996090500215 19960905 00215 WP 1996 9 5 CKSA96111 1 19960827 A 5347 S2772660 SEAT TRACK DOUG DC8 DC8F55 3021928 WP BS 1000 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND SEAT TRACK AT CENTER BL FS 1000 TO FS 850 CORRODED AT ATTACH POINTS. REMOVED AND REP LACED SEAT TRACK IAW DC8 SRM 51-1-21. TASK NR 80937, CORROSION CARD NR 5700-0553. 2 L 7 4 4F 4A25 1996090500216 19960905 00216 WP 1996 9 5 CKSA96112 1 19960827 A 5347 S2772660 SEAT TRACK DOUG DC8 DC8F55 3021928 WP BS 830-980 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND SEAT TRACK AT LBL 50 CORRODED AT ATTACH POINTS FROM FS 830 TO FS 980. REMOVED AND RE PLACED SEAT TRACK AT LBL 50. TASK NR 80939, CORROSION CARD NR 5700-0553. 2 L 7 4 4F 4A25 1996090500217 19960905 00217 WP 1996 9 5 CKSA96113 1 19960827 A 5315 56449812 FLOOR BEAM DOUG DC8 DC8F55 3021928 WP BS 295 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND CORROSION ON UPPER FLOOR BEAM FS 295 RBL 36. REPLACED UPPER FLOOR BEAM FS 295 RBL 36 IAW DC8 SRM 51-1-20 AND AIA ENGINEERING REPORT NR 96 AIA-105. TASK NR 81000, CORROSION CARD NR 5700-0553. 2 L 7 4 4F 4A25 1996090500218 19960905 00218 WP 1996 9 5 CKSA96114 1 19960827 A 5711 857001235 SPAR DOUG DC8 DC8F55 3021928 WP CENTER WING CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND CENTER WING LOWER FRONT SPAR HAS HEAVY EXFOLIATION CORROSION FROM STATION XCW 17R TO XCW 405R AT PREVIOUS REPAIR. REPAIRED SPAR IAW DC8 S/B 57-30R4 AND DRAWING SR08570012. TASK NR 80079, CORROSION CARD N R 2000-0551. 2 L 7 4 4F 4A25 1996090500219 19960905 00219 WP 1996 9 5 CKSA96115 1 19960827 A 5711 561390535 VERT STIFFENER DOUG DC8 DC8F55 3021928 WP WING FRONT SPAR CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND CENTER WING FRONT SPAR VERTICAL STIFFENER CORRODED AND CRACKED LOWER END APPROXIMATEL Y STA XCW 23R. REPAIRED IAW DC8 SRM 57-2-0 AND 51-1-8. TASK NR 80080, CORROSION CARD NR 2000-0551. 2 L 7 4 4F 4A25 1996090500220 19960905 00220 WP 1996 9 5 CKSA96116 1 19960827 A 5711 857001231 ANGLE DOUG DC8 DC8F55 3021928 WP WING FRONT SPAR CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND CENTER WING FRONT SPAR VERTICAL STIFFENER LOWER ATTACH ANGLE CRACKED APPROXIMATELY ST A XCW 35R. REPAIRED IAW DC8 DRAWING NR SR08570012. TASK NR 80081, CORROSION CARD NR 2000-0551. 2 L 7 4 4F 4A25 1996090500221 19960905 00221 WP 1996 9 5 CKSA96117 1 19960827 A 5711 AISI177 SPAR CAP DOUG DC8 DC8F55 3021928 WP CENTER WING CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND CENTER WING FRONT SPAR LOWER CAP CORRODED AND CRACKED APPROXIMATELY STATION XCW 23L T O XCW 43L. REPAIRED IAW DC8 S/B 57-30R4 DRAWING NR SR08570012. TASK NR 80082, CORROSION CARD NR 2000-0551. 2 L 7 4 4F 4A25 1996090500222 19960905 00222 WP 1996 9 5 CKSA96118 1 19960827 A 5711 561390535 VERT STIFFENER DOUG DC8 DC8F55 3021928 WP CENTER WING CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND CENTER WING FRONT SPAR VERTICAL STIFFENER CORRODED AND CRACKED APPROXIMATELY STATION XCW 29L. REPAIRED IAW DC8 SRM 57-2-0, 51-1-20 AND 51-1-8. TASK NR 80083, CORROSION CARD NR 2000-0551. 2 L 7 4 4F 4A25 1996090500223 19960905 00223 WP 1996 9 5 CKSA96119 1 19960827 A 5320 5753894 FITTING DOUG DC8 DC8F55 3021928 WP DOOR JAMB CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND CORROSION IN FWD DOOR JAM ON REAR SERVICE DOOR RIGHT HAND. CLEANED CORROSION ON FITT ING IN FWD DOOR JAM AND FOUND TO BE OUT OF LIMITS IAW DC8 SRM. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-21 AND 51- 1-20D. TREATED AND PRIMED IAW DC8 SRM 51-1-8. TASK NR 81023, WORK CARD NR 3057. 2 L 7 4 4F 4A25 1996090500224 19960905 00224 WP 1996 9 5 CKSA96120 1 19960827 A 5320 AND101332401 ANGLE DOUG DC8 DC8F55 3021928 WP BS 857 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND STA 857 FWD GEAR BOX UNDER FLOOR CENTER SECTION HAS CORROSION AT FRAMES. REPAIRED IA W AIA/E/2254 AND APPROVED FAA FORM 8110-3. TASK NR 80186 CORROSION CARD NR 2000-0557. 2 L 7 4 4F 4A25 1996090500225 19960905 00225 WP 1996 9 5 CKSA96121 1 19960827 A 5315 AISI177 FLOOR BEAM DOUG DC8 DC8F55 3021928 WP FS 740 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING C-2 CHECK, INSPECTION FOUND FS 740 FLOOR BEAM CORRODED AT RBL 27. REPAIRED IAW SKETCH AIA/E/2269 AND APPROVED FA A FORM 8110-3. TASK NR 81013, CORROSION CARD NR 5700-0553. 2 L 7 4 4F 4A25 1996090500237 19960905 00237 NM 1996 9 5 CA960111001 1 19960110 A 3230 LANDING GEAR DHAV DHC8 DHC8102 2809003 NM PWA LT MLG FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN)AFTER TAKEOFF LH FORWARD GEAR DOOR FAILED TO CLOSE. GEAR SELECTED DOWN AND LH GEAR FAILED TO EXTEND. ALTERNATE EXTE NSION CARRIED OUT. AIRCRAFT LANDED OK. GEAR TESTED ON GROUND OK. LH GEAR AND UPLOCK L UBRICATED. PROBLEM LIKELY CAUSED B Y COLD WEATHER CONDITIONS. 2 H 7 2 4T RT A13NM 1996090500238 19960905 00238 NE 1996 9 5 CA960111002 3 19960110 A 6111 SFA13M10A BLADE HAMSTD DHAV DHC8 DHC8101 2809002 NM HAMSTD 14SF 14SF7 NE NR4 BLADE FAILED NDT TEST W K NONE O OTHER IN INSP/MAINT 1 CA 7459 8771157 881010 (CAN)#4 BLADE ON #1 PROPELLER FAILED SHEAR WAVE NDT INSPECTION, AS PER SERVICE BULLETIN 14SF-61-A95. 2 H 7 2 4T RT A13NM 6 C P7NE 1996090500239 19960905 00239 NE 1996 9 5 CA960111003 3 19960110 A 6111 SFA13M1OA BLADE HAMSTD DHAV DHC8 DHC8102 2809003 NM PWA HAMSTD 14SF 14SF7 NE NR 4 BLADE FAILED NDT TEST W K NONE O OTHER IN INSP/MAINT 1 CA 11999 2396 8630987 841104 (CAN)#4 BLADE ON #2 PROPELLER FAILED SHEAR WAVE NDT TEST, AS PER SERVICE BULLETIN 14SF-61-A95. 2 H 7 2 4T RT A13NM 6 C P7NE 1996090500240 19960905 00240 NM 1996 9 5 CA960111005 1 19960110 A 7921 28E997 COOLER DHAV DHC8 DHC8102 2809003 NM NR 2 ENG OIL LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 13554 (CAN)#2 ENGINE OIL COOLER FOUND LEAKING. 2 H 7 2 4T RT A13NM 1996090500241 19960905 00241 NM 1996 9 5 CA960111006 1 19960110 A 2421 31708001A GENERATOR DHAV DHC8 DHC8102 2809003 NM NR 1 AC GEN FAILED W O OTHER H ELECT. POWER LOSS-50 PC CR CRUISE 1 CA 4441 474 (CAN)#1 AC GENERATOR FAILED IN CRUISE. SB 8-24-52 APPLIES. NO INFLIGHT SHUTDOWNS SINCE INCORPORATION OF SERVICE BULLETIN . 2 H 7 2 4T RT A13NM 1996090500242 19960905 00242 1996 9 5 CA960111012 4 19960105 A 3418 693733922 MODULE BOEING 737 737217 1384464 NM STICK SHAKER INTERMITTENT W O OTHER N FALSE WARNING CL CLIMB 1 CA (CAN)AFTER TAKEOFF AT 170 KTS AND 600 FT THE STICK SHAKER CAME ON AND STAYED ON UNTIL 230 KTS. THEN SHAKER CAME BACK ON AT 250 KTS. STALL WARNING TESTED WITH NO CHANGES. WHILE RETURNING TO YUL SHAKER STOPPED AND NEVER CAME BACK ON. MODULE R EPLACED. 2 L 7 2 4F A16WE 1996090500244 19960905 00244 GL 1996 9 5 CA960111014 2 19960108 A 7250 6870237 BLADE LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL 4TH STAGE MISSING W K NONE O OTHER IN INSP/MAINT 1 CA 4693 3591 500859 (CAN)DURING A ROUTINE A-CHECK, A CRACK WAS FOUND IN THE #3 ENGINE TAIL PIPE AND TURBINE REAR BEARING SUPPORT. FURTHER IN VESTIGATION SHOWED A PIECE MISSING FROM THE FOURTH STAGE TURBINE BLADE. DAMAGE WAS CONTAINED. TURBINE SENT FOR STRIP REP ORT. 2 H 7 4 4T 4 T A1SO E282 1996090500247 19960905 00247 WP 1996 9 5 CA960111018 1 19960102 A 6310 269A505074 BEARING HUGHES 269 269C 4470504 WP LYC IDLER PULLEY FAILED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA 637 (CAN)AIRCRAFT FLYING IN CRUISE WHEN SMELLED BURNING GREASE AND HEARD A KLUNK. UPON INSPECTION FOUND IDLER PULLEY BEARING FAILURE DUE TO GREASE LEAKING. BEARING FAILURE CAUSED EXCESSIVE HEAT DISTRIBUTION TO REINFORCED IDLER PULLEY SUPPORT BR ACKET P/N 269A5575 AND DAMAGE TO IDLER PULLEY P/N 269A5576. 1 G 7 1 3O 4H12 1996090500249 19960905 00249 EU 1996 9 5 CA960111020 1 19960104 A 5730 HLT90087 RIVET BAG BAE146 BAE146200A 1500266 EU WING TOP RH & LH SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN)RH WING TOP SKIN FRONT SPAR - RIVET HEAD MISSING, APPROXIMATELY 18 INCHES OUTBOARD OF RIB 2. LH WING TOP SKIN FRONT SPAR - RIVET HEAD MISSING APPROXIMATELY 29 INCHES OUTBOARD FROM RIB 2. 2 H 7 4 4F RT A49EU 1996090500250 19960905 00250 SW 1996 9 5 CA960111021 1 19960103 A 5311 206032308005 FRAME BELL 206 206L4 1182110 SW TOP AFT FS 217 CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1033 (CAN)CRACK FOUND ON TOP AFT RADIUS OF ANGLE P/N 206-032-308-005 ATTACHED TO STN 217.84 FRAME P/N 206-032-307-109. 1 G 7 1 3U NC H2SW 1996090500252 19960905 00252 NE 1996 9 5 CA960115002 3 19960110 A 6111 SFA13M1OA BLADE HAMSTD DHAV DHC8 DHC8102 2809003 NM HAMSTD 14SF 14SF7 NE NR 3 BLADE FAILED TEST W K NONE O OTHER IN INSP/MAINT 1 CA 10196 10196 8681207 890709 (CAN)#1 PROPELLER #3 BLADE FAILED SHEAR WAVE TEST AS PER SERVICE BULLETIN 14SF-61-A95. 2 H 7 2 4T RT A13NM 6 C P7NE 1996090500253 19960905 00253 NE 1996 9 5 CA960115003 3 19960110 A 6111 SFA13M1OA BLADE HAMSTD DHAV DHC8 DHC8102 2809003 NM HAMSTD 14SF 14SF7 NE NR 1 BLADE FAILED TEST W K NONE O OTHER IN INSP/MAINT 1 CA 11036 4342 8613187 890709 (CAN)#1 PROPELLER #1 BLADE FAILED SHEAR WAVE TEST AS PER SERVICE BULLETIN 14SF-61-A95. 2 H 7 2 4T RT A13NM 6 C P7NE 1996090500254 19960905 00254 NE 1996 9 5 CA960115004 3 19960110 A 6111 SFA13M1OA BLADE HAMSTD DHAV DHC8 DHC8102 2809003 NM PWA HAMSTD 14SF 14SF7 NE #2 PROP FAILED NDT TEST W K NONE O OTHER IN INSP/MAINT 1 CA 6758 8726857 860327 (CAN)#2 PROPELLER #1 BLADE FAILED SHEAR WAVE TEST AS PER SERVICE BULLETIN 14SF-61-A95. 2 H 7 2 4T RT A13NM 6 C P7NE 1996090500255 19960905 00255 NE 1996 9 5 CA960115005 3 19960110 A 6111 SFA13M1OA BLADE HAMSTD DHAV DHC8 DHC8102 2809003 NM PWA HAMSTD 14SF 14SF7 NE NR 1 BLADE FAILED NDT TEST W K NONE O OTHER IN INSP/MAINT 1 CA 8683 87230007 860327 (CAN)#2 PROPELLER #1 BLADE FAILED SHEAR WAVE TEST AS PER SERVICE BULLETIN 14SF-61-A95. 2 H 7 2 4T RT A13NM 6 C P7NE 1996090500256 19960905 00256 NE 1996 9 5 CA960115006 3 19960112 A 6111 SFA13M1OA BLADE HAMSTD DHAV DHC8 DHC8102 2809003 NM PWA HAMSTD 14SF 14SF7 NE NR 3 BLADE FAILED NDT TEST W K NONE O OTHER IN INSP/MAINT 1 CA 14948 6995 858745 870537 (CAN)#3 BLADE ON #1 PROPELLER FAILED SHEAR WAVE TEST AS PER SERVICE BULLETIN 14SF-61-A95. 2 H 7 2 4T RT A13NM 6 C P7NE 1996090500257 19960905 00257 NE 1996 9 5 CA960115007 3 19960112 A 6111 SFA13M1OA BLADE HAMSTD DHAV DHC8 DHC8102 2809003 NM HAMSTD 14SF 14SF7 NE NR 1 BLADE FAILED NDT TEST W K NONE O OTHER IN INSP/MAINT 1 CA 12169 2247 8625937 870537 (CAN)#1 BLADE ON #2 PROPELLER FAILED SHEAR WAVE NDT TEST AS PER SERVICE BULLETIN 14SF-61-A95. 2 H 7 2 4T RT A13NM 6 C P7NE 1996090500258 19960905 00258 NE 1996 9 5 CA960115008 3 19960112 A 6111 SFA13M1OA BLADE HAMSTD DHAV DHC8 DHC8102 2809003 NM PWA HAMSTD 14SF 14SF7 NE NR 2 BLADE FAILED NDT TEST W K NONE O OTHER IN INSP/MAINT 1 CA 14646 6651 859138 870537 (CAN)#2 BLADE ON #2 PROPELLER FAILED SHEAR WAVE NDT TEST AS PER SERVICE BULLETIN 14SF-61-A95. 2 H 7 2 4T RT A13NM 6 C P7NE 1996090500259 19960905 00259 NE 1996 9 5 CA960115009 3 19960112 A 6111 SFA13M1OA BLADE HAMSTD DHAV DHC8 DHC8102 2809003 NM PWA HAMSTD 14SF 14SF7 NE NR 3 BLADE FAILED NDT TEST W K NONE O OTHER IN INSP/MAINT 1 CA 14725 6786 859715 870537 (CAN)#3 BLADE ON #2 PROPELLER FAILED SHEAR WAVE NDT TEST AS PER SERVICE BULLETIN 14SF-61-A95. 2 H 7 2 4T RT A13NM 6 C P7NE 1996090500261 19960905 00261 EA 1996 9 5 CA960115011 1 19960108 A 2730 C6TE105913 TORQUE TUBE DHAV C6TE100115 DHAV DHC6 DHC6300 EA ELEV CONT NOT TO SPEC W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 358 (CAN)NEW PARTS FROM NEW CAL AVIATION AND DE HAVILLAND DO NOT MEET DRAWING SPECIFICATIONS. INSIDE DIMENSION OF BRACKET P/ N C6TE1020-1 SHOULD BE 1.13 TO 1.14 INCHES. NEW TORQUE TUBES HAVE BRACKETS MEASURING 1.098, 1.108, 1.118. FOUR MORE IN DE HAVILLAND STORES NOT MEETING SPECIFICATIONS. 1 H 7 2 3T A9EA 1996090500262 19960905 00262 EA 1996 9 5 CA960115012 2 19960108 A 7240 3024767 DIFFUSER PIPES PWA 3027037 DHAV DHC6 DHC6300 EA PWA PT6 PT6A27 52043 EA GAS GEN CASE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1309 PCE40595 (CAN)DURING HOT SECTION INSPECTION FIVE (5) DIFFUSER PIPES WERE FOUND WITH MULTIPLE CRACKS IN EXCESS OF MAINTENANCE MANU AL LIMITS. TWO (2) OF THE TUBES WERE BROKEN OFF, THREE (3) HAVE EXTENSIVE CRACKS. ENGINE SENT FOR REPAIR. 1 H 7 2 3T 4 T A9EA E4EA 1996090500265 19960905 00265 EU 1996 9 5 CA960115015 1 19960104 A 3232 1252511 ACTUATOR FOKKER F28 F28MK1000 4990808 EU DOOR UPLOCK CRACKED W A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 CA (CAN)AFTER TAKEOFF, ALL UTILITY HYDRAULIC SYSTEM PRESSURE WAS LOST. ONE MAIN LANDING GEAR DOOR UPLOCK CASING WAS CRACKED , FLUID LOSS. REPLACED. 2 L 7 2 4F RT A20EU 1996090500266 19960905 00266 NE 1996 9 5 CA960115016 2 19960107 A 7230 754130176008 ACTUATOR RROYCE LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE NR 3 ENG FAULTY W A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CA 4961 460 10444 (CAN)WHEN #3 THROTTLE WAS ADVANCED THE ENGINE SPOOLED DOWN AND THE ENGINE WAS SHUTDOWN. THE AIRCRAFT RETURNED TO THE RAM P AND MAINTENANCE FOUND THE MASTER AND SLAVE RAM ACTUATORS NOT WORKING PROPERLY. BOTH ACTUATORS WERE REPLACED AND THE AI RCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A23WE E12EU 1996090500267 19960905 00267 EU 1996 9 5 CA960115017 1 19960110 A 2810 FTAO17521 FUEL CELL BOLKMS 105 BO105C 5626005 EU MAIN LEAKING W K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA 788 (CAN)SMELL FUEL LEAK FROM MAIN FUEL TANK. WHILE REMOVING TANK FOUND 3 SNAPS NOT ENGAGED. 1 G 7 2 3U H3EU 1996090500277 19960905 00277 NM 1996 9 5 CA960116003 1 19960104 A 7830 65378315 VALVE BOEING 727 72725 1384006 NM THRUST CONTROL SEIZED W K NONE O OTHER LD LANDING 1 CA (CAN)AFTER TOUCHDOWN WHEN REVERSE THRUST WAS SELECTED THE #1 THROTTLE STUCK ON THE IDLE GATE AND THE REVERSER WOULD NOT ENGAGE. MAINTENANCE FOUND THE THRUST CONTROL SYSTEM DIRECTIONAL VALVE VERY STIFF. AFTER VALVE REPLACEMENT THE SYSTEM FUN CTIONED NORMALLY. 2 L 7 3 4F A3WE 1996090500278 19960905 00278 WP 1996 9 5 CA960116006 2 19960111 A 7322 8070425 FCU SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE3313UW 01514 WP R/H ENGINE ERRATIC W A O OTHER O OTHER CR CRUISE 1 CA 03453 (CAN)THIS FUEL CONTROL UNIT WAS REMOVED DUE TO MALFUNCTION CAUSED BY THE MAXIMUM POWER ADJUSTMENT SETTING BEING BOTTOMED OUT. ONE MONTH LATER THIS SAME FCU WAS SENT BACK FOR OVERHAUL DUE TO TORQUE JUMPING ERRATICALLY. 2 L 7 2 4T 4 T RT A8SW E4WE 1996090500280 19960905 00280 SO 1996 9 5 CA960116008 1 19960108 A 5511 46530003 RIB PIPER 46530003 PIPER PA31T PA31T2 7103127 SO LT STAB OUTB BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 7020 (CAN)DURING INSPECTION THE LEFT HAND STABILIZER OUTBOARD RIB WAS FOUND BROKEN. BREAK LINE INDICATES THAT THE PART HAD BE EN CRACKED FOR AN UNDETERMINED AMOUNT OF TIME PRIOR TO BREAKING, DUE TO ALUMINUM STREAKING ALONG THE BREAK LINE. SUBMITT ER SENT THE PART IN WITH THE SDR. 1 L 7 2 3T RT A8EA 1996090500281 19960905 00281 EA 1996 9 5 CA960116009 1 19960105 A 3250 711599 LINK HEROUX 7119011 DHAV DHC6 DHC6300 EA STEERING BROKEN W K NONE O OTHER TX TAXI/GRND HDL 1 CA 15202 H487 (CAN)WHILE MOVING NOSEWHEEL STEERING TILLER, A SNAPPING NOISE WAS HEARD AND NOSEWHEEL STEERING BECAME INOPERATIVE. INSPE CTION FOUND NOSE STEERING ACTUATOR LINK WAS BROKEN NEAR MOUNTING FORK. 1 H 7 2 3T A9EA 1996090500284 19960905 00284 SW 1996 9 5 CA960116101 1 19960105 A 5302 205030815003P FITTING BELL 205 205A1 1181414 SW TB STA 243.116 CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN)LOWER LEFT TAILBOOM ATTACHMENT FITTING CRACKED. STA 243.116 WL35.17. CRACK RUNNING FROM BOLT HOLE TO OUTER EDGE. 1 G 7 1 4U H1SW 1996090500287 19960905 00287 EU 1996 9 5 CA960119102 1 19960111 A 2820 HTE9001180001 SHUTOFF VALVE AIRBUS 320 A320211 3930320 EU FUEL SYS LP INOPERATIVE W A K NONE O OTHER IN INSP/MAINT 1 CA (CAN)DURING REPLACEMENT OF #2 ENGINE, IT WAS FOUND THAT THE LP VALVE WOULD NOT CLOSE AND DESPITE A NORMAL ECAM MESSAGE T HE VALVE APPEARED TO BE AT 1/4 OPEN POSITION. P/N OF ACTUATOR 1190001-1 ISSUE B. THER E IS A CAUTION IN THE AMM ON 28-24 -51 PAGE 410 TO ENSURE FLANGES OF VALVE & ACTUATOR TOUCH ACROSS THEIR FULL SURFACES. FURTHER INVESTIGATION AND FOLLOW UP IN PROGRESS. 2 L 7 2 4F RT A28NM 1996090500288 19960905 00288 EU 1996 9 5 CA960122002 1 19960116 A 2435 501113775 STARTER PLESSEY BAG BAE146 BAE146200A 1500266 EU LYC NR 3 ENGINE FAILED W H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION TX TAXI/GRND HDL 1 CA 12022 479 TE0888 (CAN)#3 ENGINE STARTER LIGHT REMAINED ON AFTER START. CIRCUIT BREAKER PULLED AND ENGINE SHUTDOWN. THE STARTER WAS REPLAC ED AND THE PROBLEM WAS RECTIFIED. 2 H 7 4 4F RT A49EU 1996090500289 19960905 00289 EA 1996 9 5 CA960122003 1 19960116 A 2150 78279012 AIR CYCLE MACH HAMSTD DHAV DHC8 DHC8311 1386006 EA REAR MAKING SMOKE W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA 1170 (CAN)WHEN #1 BLEED SUPPLY TURNED ON, CABIN FILLS WITH FINE SMOKE. REAR AIR CYCLE MACHINE REPLACED. 2 H 7 2 4T RT A13NM 1996090500290 19960905 00290 NM 1996 9 5 CA960122004 1 19960110 A 6520 BEVEL GEAR ROBSIN R22 R22BETA NM T/R GR BOX CHIPPED TOOTH W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 940 (CAN)CHIP LIGHT ON. CLEANED CHIP PLUG AND DRAINED/FLUSHED T/R GEARBOX. FOUND CHIP FROM BEVEL GEAR SET. 1 G 7 1 3O H10WE 1996090500293 19960905 00293 SO 1996 9 5 CA960122008 1 19960104 A 5720 159W100112 WING TIP GULSTM G159 G159 3952202 SO WING BENT/CRACKED W O OTHER O OTHER TX TAXI/GRND HDL 1 CA 21223 (CAN)WING TIP OF AIRCRAFT CONTACTED THE HANGAR WHILE UNDER COMMAND OF THE FLIGHT CREW. WING TIP REPLACED AND AIRCRAFT RE TURNED TO SERVICE. 2 L 7 2 4T 1A17 1996090500294 19960905 00294 EA 1996 9 5 CA960122009 2 19960113 A 7314 GR9080J4A FUEL PUMP ROMEC PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2C 41532 EA BODY LOOSE SCREWS W A K NONE K FLUID LOSS IN INSP/MAINT 1 CA 913 L125561 L125561 (CAN)DURING INSPECTION A SEVERE FUEL LEAK WAS NOTICED FROM THE ENGINE. INVESTIGATION REVEALED THE SCREWS WHICH HOLD THE FUEL PUMP BODY TOGETHER HAD BACKED OUT AND ALLOWED FUEL TO LEAK AT THE UPPER SEAMLINE . THE FUEL PUMP RETAINING SCREWS W ERE TIGHTENED AND RELOCKWIRED. THE PUMP CHECKED SERVICEABLE AND NO FURTHER ACTION WAS REQUIRED. 1 L 7 2 3O 3 O A20SO E14EA 1996090500295 19960905 00295 CE 1996 9 5 CA960122010 1 19960105 A 7603 5038901215 THROTTLE CABLE BEECH BEECH 95 95B55 1152729 CE CONT O470 IO470L 17026 SO RT HAND SEPARATED W A E UNSCHED LANDING ENGINE SHUTDOWN O OTHER CR CRUISE 1 CA CS192942R (CAN)IN CRUISE THE PILOT LOST RIGHT HAND THROTTLE CONTROL. THE ENGINE WAS SHUTDOWN AND THE AIRCRAFT MADE A PRECAUTIONARY LANDING WITHOUT INCIDENT. INVESTIGATION REVEALED THAT THE RIGHT HAND THROTTLE CABLE HAD SEPARATED INTERNALLY. SUBMITTER STATES THAT THE OAT WAS -30 DEGREES C AND THIS MAY HAVE CONTRIBUTED TO THE FAILURE. THE CABLE WAS REPLACED AND THE AIRC RAFT RETURNED TO SERVICE. 1 L 7 2 3O 3 O RT 3A16 3E1 1996090500298 19960905 00298 CE 1996 9 5 CA960122013 1 19960105 A 3260 1003810061 SWITCH BEECH 1900 1900D 1154162 CE NOSE GEAR OUT OF ADJUST W O OTHER N FALSE WARNING AP APPROACH 1 CA 2707 (CAN)ON APPROACH THE CREW SELECTED GEAR DOWN AND RECEIVED ONLY TWO DOWN AND LOCKED POSITION LIGHTS. THE GEAR WAS CYCLED AND EMERGENCY EXTENSION INITIATED. THE GEAR FINALLY FELL INTO PLACE AND A SUCCESSFUL LANDING CARRIED OUT. INVESTIGATION REVEALED THE MICROSWITCH WAS ADJUSTED TO CLOSE TO THE LIMITS. THE SWITCH WAS READJUSTED AND THE AIRCRAFT RETURNED TO SE RVICE. 2 L 7 2 4T RT A24CE 1996090500299 19960905 00299 EA 1996 9 5 CA960122014 2 19960115 A 7414 M3006 BEARING SLICK 4252R PIPER PA28 PA28140 7102802 SO LYC O320 O320E3D 41508 EA MAGNTO DRIVE WORN W D RETURN TO BLOCK E VIBRATION/BUFFET TX TAXI/GRND HDL 1 CA 1477 4040049 L4764427A (CAN)ENGINE WAS DIFFICULT TO START. ENGINE RUN REVEALED A MAG DROP OF 300 - 400 RPM. INSPECTION OF THE MAGNETO FOUND THE BEARING AT THE MAIN DRIVE END BADLY WORN. 1 L 7 1 3O 3 O 2A13 E274 1996090500301 19960905 00301 WP 1996 9 5 CA960122016 1 19960106 A 2711 1521773105 FEEDBACK LINKS LKHEED 1011 1011385114 WP WS269 AILERON MIS INSTALLED W A K NONE F FLT CONT AFFECTED TX TAXI/GRND HDL 1 CA (CAN)DURING MAINTENANCE CHECK THE LH AILERONS WERE SLOW TO RESPOND AND THE RH AILERONS WERE RESPONDING TOO RAPIDLY. BOTH FEEDBACK LINKAGES P/N 1521773-105 AND P/N 152771-10 WERE MIXED. SWITCHED AT WING STA TION 269. THIS CREATED A WRONG FEE DBACK BY AMPLIFYING THE SIGNAL. INSTALLED LINKAGES IN THEIR PROPER POSTIONS. 2 L 7 3 4F A23WE 1996090500302 19960905 00302 CE 1996 9 5 CA960122017 1 19960112 A 7931 1693800361 INDICATOR BEECH 23 C23 1151242 CE ENG OIL PRESS READING HIGH W O OTHER N FALSE WARNING TO TAKEOFF 1 CA 1467 (CAN)OIL PRESSURE GAUGE WAS FOUND TO READ 30 LBS ABOVE ACTUAL. A NEW INDICATOR WAS INSTALLED AND CHECKED OUT SERVICEABLE . 1 L 7 1 3O A1CE 1996090500304 19960905 00304 CE 1996 9 5 CA960122021 1 19960110 A 5511 SPAR CESSNA 172 172N 2072434 CE HORIZ STAB CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 7760 (CAN)DURING THE PERFORMANCE OF SEB 94-8 THE FRONT SPAR OF THE HORIZONTAL STABILIZER WAS FOUND CRACKED AT THE LIGHTENING HOLE. 1 H 7 1 3O NT 3A12 1996090500305 19960905 00305 NM 1996 9 5 CA960122022 1 19960113 A 2530 FAN BOEING 757 75723A 1384967 NM OVEN SEIZED W A H F UNSCHED LANDING DEACTIVATE SYST/CIRCUITS ACTIVATE FIRE EXT. A FLAME/FIRE CR CRUISE 1 CA (CAN)DURING FLIGHT, SMOKE CAME FROM AROUND OUTER WALL OF OVEN. CIRCUIT BREAKER PULLED, EXTINGUISHER USED, PRECAUTIONARY LANDING, OVEN FAN HAD BURNT AND SEIZED. NO OTHER DAMAGE. 2 L 7 2 4F RT A2NM 1996090500306 19960905 00306 NE 1996 9 5 CA960122024 2 19960107 A 7230 754130175004 ACTUATOR RROYCE LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE #3 ENGINE RAM FAULTY W A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CA 4961 655 10444 (CAN)WHEN #3 ENGINE THROTTLE WAS ADVANCED THE ENGINE SPOOLED DOWN AND THE ENGINE WAS SHUTDOWN. THE AIRCRAFT RETURNED TO THE RAMP AND MAINTENANCE FOUND THE MASTER AND SLAVE RAM ACTUATORS NOT WORKING PROPERLY. BOTH ACTUATORS WERE REPLACED A N D THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A23WE E12EU 1996090500307 19960905 00307 EU 1996 9 5 CA960123001 1 19960108 A 6730 704A44831107 PRIMARY SERVO SNIAS AS332 AS332C 8680808 EU HYD LINE R/H WORN W A UNSCHED LANDING K FLUID LOSS DE DESCENT 1 CA (CAN)PRESSURE LINE FROM THE R/H SERVO CHAFED ON A DZUS FASTENER CAUSING LEAK. 2 G 7 2 4U H4EU 1996090500309 19960905 00309 NE 1996 9 5 CA960123003 1 19960111 A 6730 616S61500061 SERVO ASSY SKRSKY S61 S61N 8142104 NE GE AUX SERVO HYD LEAKING W H DEACTIVATE SYST/CIRCUITS K F FLUID LOSS FLT CONT AFFECTED CR CRUISE 1 CA 11837 2495 (CAN)HYDRAULIC FLUID NOTED LEAKING FROM BELLY. AFTER OPENING CONTROL COMPARTMENT ACCESS DOOR FLUID WAS FOUND COMING FROM AUXILIARY SERVO FORE AND AFT CHANNEL POWER PISTON LOWER SEAL. AUXILIARY SERVO HYDRAU LIC RESERVOIR FOUND TO BE 1/3 L DO WN. RESERVOIR REPLENISHED AND AIRCRAFT STARTED TO RETURN TO BASE. LEAK OBSERVED TO BE INCREASING. AUXILIARY HYDRAULIC SH UT OFF, LEAK STOPPED RETURN FLIGHT COMPLETED. 2 G 7 2 4U 1H15 1996090500310 19960905 00310 EU 1996 9 5 CA960123004 1 19960113 A 8010 2520M STARTER RELAY BOLKMS 105 BO105S 5626006 EU STAR/ GENERATOR CORROSION W D RETURN TO BLOCK H J ELECT. POWER LOSS-50 PC WARNING INDICATION TX TAXI/GRND HDL 1 CA 953 (CAN)PRIOR TO FIRST FLIGHT OF THE DAY, BOTH ENGINES WERE STARTED AND #1 GENERATOR WOULD NOT COME ON LINE AND THE #2 STAR T LIGHT WAS ILLUMINATING INTERMITTENTLY AND DIMLY. #2 STARTER RELAY WAS REPLACED AND ALL PROBLEMS WERE RECTIFIED. MOIST URE AND CORROSION WERE FOUND INSIDE EVEN THOUGH THE ELECTRICAL BOX WAS DRY. 1 G 7 2 3U H3EU 1996090500311 19960905 00311 SW 1996 9 5 CA960123005 1 19960114 A 6700 VS1313842CR764 BELLOWS BELL 206 206L 1181522 SW CYCLIC ICE CONTAM W O OTHER F FLT CONT AFFECTED CR CRUISE 1 CA 5429 (CAN)WHILE AT CRUISE (4000 FEET) IN 8 DEGREES C, FOLLOWING A 10 MINUTE STOP ON A MOUNTAIN TOP IN LIGHT SNOWFALL, THE LAT ERAL CYCLIC CONTROL BECAME STIFF. AFTER LANDING AND SHUTTING DOWN, PILOT INSPECTED TH E FLIGHT CONTROLS AND FOUND BROKEN ICE IN THE RUBBER BELLOWS AROUND LATERAL CYCLIC CONTROL ROD WHERE IT COMES THROUGH THE TRANSMISSION DECK AND ALSO ICE A ROUND THE DECK AREA. PILOT REMOVED ICE AND RETURNED TO BASE. CONTROL REMAINED STIFF UNTIL LOWER ALTITUDE AND HIGHER OAT WERE REACHED. 1 G 7 1 3U H2SW 1996090500316 19960905 00316 NM 1996 9 5 CA960123010 1 19960109 A 7712 TORQUE PROBE DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE #2 ENGINE FAULTY W C D E ABORTED TAKEOFF RETURN TO BLOCK ENGINE SHUTDOWN J WARNING INDICATION TO TAKEOFF 1 CA PCE123057 (CAN)ON DEPARTURE #2 ENGINE HAD AN UNCOMMANDED AUTOFEATHER. CREW SHUTDOWN THE ENGINE AND RETURNED TO BASE. MAINTENANCE R EPLACED THE TORQUE PROBE. ENGINE RUN AND PROP CHECKS CARRIED OUT SERVICEABLE. AIRCRAF T RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 1996090500317 19960905 00317 CE 1996 9 5 CA960123011 1 19960105 A 6121 A213796 CONNECTOR WOODWARD A213796 BEECH 200 B200C 1152924 CE HARTZL HCB3T HCB3TN3 GL PROP SYNC CRIMP FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 2257139D BU14004 (CAN)DURING TROUBLESHOOTING OF THE PROPELLER SYNCHROPHASER SYSTEM, WIRES WERE FOUND PULLED OUT OF THE SYNCHROPHASER BOX CONNECTOR. WHEN THE SOCKETS WERE EXTRACTED FROM THE BOX THEY COULD BE SEEN TO BE IMPROPERLY CRIMPED. THERE WAS ALSO NO S TRAIN RELIEF BACKSHELL INSTALLED. ALL WIRES WERE PROPERLY RETERMINATED AND A BACKSHELL WAS INSTALLED, THE UNIT RETURNED TO SERVICE. SUBMITTER STATES THAT THE CAPTAINS BOOT MAY HAVE CONTRIBUTED TO THE PULLING OF THE WIRES. ALSO, THIS TYPE II SYNCHROPHASER WAS AN AFTERMARKET INSTALLATION UNDER SERVICE BULLETIN #2115. 1 L 7 2 4T A24CE 6 C P15EA 1996090500320 19960905 00320 NE 1996 9 5 96ZZZX4243 2 19960414 A 7250 414129001 ROTOR ASSY BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE POWER TURBINE BLADE SHIFT A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 127HH 175 SC14610 7060 LE45244E FAILED SB L5101-72-10-0153. EXCESSIVE IBPT BLADE SHIFT NR 9 -0.012 INCH. REPLACED WITH USED UNIT, CORRECTED PROBLEM. P ART TOTAL CYCLES: 3,425.2. 1 G 7 2 3U 3 U H13EU E5NE 1996090500321 19960905 00321 NE 1996 9 5 96ZZZX4244 2 19960414 A 7260 430101201 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE ACC DRIVE LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 127HH 175 7060 LE45244E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1996090500322 19960905 00322 NE 1996 9 5 96ZZZX4245 2 19960414 A 7260 430101301 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE ACC DRIVE LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 127HH 175 7060 LE45244E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1996090500323 19960905 00323 NE 1996 9 5 96ZZZX4246 2 19960414 A 7260 430101501 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE ACC DRIVE LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 127HH 175 7060 LE45244E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH 3 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1996090500324 19960905 00324 CE 1996 9 5 96ZZZX4247 1 19960702 A 3040 53032A VALVE CESSNA 441 441 2076020 CE WINDSHIELD HEAT STICKS A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 185GA 135 0299 4410066 WINDSHIELD HEAT VALVE SOLENOID STICKS ON. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 L 7 2 3T RT A28CE 1996090500325 19960905 00325 NM 1996 9 5 96ZZZX4248 1 19960330 A 5101 STRUCTURE BOEING 727 72723 1384004 NM AIRFRAME HAIL DAMAGE A A UHVA O OTHER C F.O.D. AP APPROACH 1 SO 11 1910 19385 AIRCRAFT DESCENDING TO MCO AT 13,000 FEET AND 250 KNOTS. ENTERED SCATTERED HAIL. NO FLAPS DOWN, NO LANDING GEAR DOWN. DAMAGE TO NR 2 ENGINE RING COWL, UPPER 180, LEADING EDGE DAMAGE AND ALL OLD REPAIRS TURN LOOSE, WINDOW SEAL TORN BACK, UPPER BEACON BROKE, RADOME DAMAGE (REPLACED). FLT NR 72 CAK TO MCO AT 3-30-96, FERRY AIRCRAFT TO MOBILE AEROSPACE FOR REPAIRS. STANDARD SRM REPAIRS WERE ACCOMPLISHED, 111 DISCREPANCIES WERE DISCOVERED TO THE SHEET METAL AND REPAIRS WERE MADE. AIRCRAFT RETURNED TO SERVICE 12 DAYS LATER, APPROXIMATELY 4-11-96. 2 L 7 3 4F A3WE 1996090500326 19960905 00326 EU 1996 9 5 SIMA962221 1 19960809 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 265AE 988 266 DFW - FLT 3690 - THREE INDIVIDUAL LIGHTS ARE OUT ON THE FORWARD STRIP OF THE CABIN FLOOR LIGHTING, AND BOTH LIGHTS UNDER THE FORWARD EMERGENCY EXITS ARE OUT. INSTALLED BATTERY PACK IN EMERGENCY LIGHTING POWER SUPPLY. OPS CHECK GOOD. AIRC RAFT WAS RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1996090500327 19960905 00327 NE 1996 9 5 96ZZZX4249 2 19960404 A 7250 414129001 ROTOR BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE TURBINE BLADE SHIFT A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 117CW 967 SC14074 7125 LE45022E ROTOR ASSY FAILED SB LT101-72-10-0153. EXCESSIVE IBPT BLADE SHIFT NR 22 -0.013 INCH. REPLACED WITH USED UNIT, CORRECTE D PROBLEM. PART TOTAL CYCLES, 2,462.7. 1 G 7 2 3U 3 U H13EU E5NE 1996090500328 19960905 00328 NE 1996 9 5 96ZZZX4250 2 19960404 A 7260 230093303 BEARING BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE ACC DRIVE PITTED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 117CW 922 7125 LE45022E BEARING HAS EXCESSIVE PITTING. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1996090500329 19960905 00329 NE 1996 9 5 96ZZZX4251 2 19960404 A 7260 230307203 SEAL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE CSD DRIVE LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 117CW 922 7125 LE45022E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1996090500331 19960905 00331 NE 1996 9 5 96ZZZX4253 2 19960404 A 7250 430144801 SEAL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE NR 3 BEARING LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 117CW 922 1190628 7125 LE45022E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1996090500332 19960905 00332 NE 1996 9 5 96ZZZX4254 2 19960404 A 7250 410106701 SEAL RING BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE 1ST TURB SHROUD WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 117CW 922 7125 LE45022E WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1996090500333 19960905 00333 NE 1996 9 5 96ZZZX4255 2 19960404 A 7260 430101201 SEAL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE ACC DRIVE LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 117CW 922 7125 LE45022E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1996090500334 19960905 00334 NE 1996 9 5 96ZZZX4256 2 19960404 A 7260 430101501 SEAL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE ACC DRIVE LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 117CW 922 7125 LE45022E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH 3 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1996090500335 19960905 00335 SW 1996 9 5 96ZZZX4257 1 19960711 A 6710 206062721105 ACTUATOR BELL 222 222 1182122 SW M/R FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 30SV 91 211 47044 STROKE ADJUSTMENT ON ACTUATOR ASSY INOPERATIVE. INTERNAL MECHANISM FELL APART. REPLACED WITH NEW UNIT, CORRECTED PROBL EM. 1 G 7 2 3U H9SW 1996090500345 19960905 00345 NE 1996 9 5 96ZZZX4267 2 19960508 A 7250 410106701 SEAL RING BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE 1ST TURB SHROUD WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 527SF 612 7111 LE45132E SEAL RING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1996090500346 19960905 00346 NE 1996 9 5 96ZZZX4268 2 19960508 A 7250 414129001 ROTOR ASSY BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE POWER TURBINE BLADE SHIFT A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 528SF 1987 612 SC17310 7104 LE45132E FAILED SB LT101-72-10-0153. EXCESSIVE IBPT BLADE SHIFT NR 18 +0.016 INCH. LEAD-THE-FLEET. REPLACED WITH USED UNIT, CO RRECTED PROBLEM. PART TOTAL CYCLES, 4,274.1. 1 G 7 2 3U 3 U H13EU E5NE 1996090500347 19960905 00347 NE 1996 9 5 96ZZZX4269 2 19960508 A 7260 430101201 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE ACC DRIVE LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 527SF 612 7111 LE45132E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1996090500348 19960905 00348 NE 1996 9 5 96ZZZX4270 2 19960508 A 7260 430101301 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE ACC DRIVE LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 527SF 612 7111 LE45132E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1996090500350 19960905 00350 NE 1996 9 5 96ZZZX4272 2 19960508 A 7260 430101501 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE ACC DRIVE LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 527SF 612 7111 LE45132E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH 3 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1996090500354 19960905 00354 NE 1996 9 5 CALA9601249 2 19960830 A 7314 SEAL DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9 52048 NE FUEL PUMP DR PAD LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 16521 47521 666143 THE NR 2 ENGINE OIL QUANTITY DROPPED FROM ABOUT 13 QUARTS TO 6.5 QUARTS AFTER 1.5 HOURS OF FLIGHT. MAINTENANCE FOUND TH E NR 2 ENGINE LEAKING OIL FROM FUEL PUMP DRIVE PAD. THE FUEL PUMP AND FUEL CONTROL ASSEMBLY WERE REMOVED AND THE GEARBO X CARBON SEAL WAS REPLACED. THE FUEL PUMP AND FUEL CONTROL ASSEMBLY WERE REINSTALLED IAW MM 73-10-1. THE ENGINE WAS RU N AND LEAK CHECKS WERE GOOD. 2 L 7 2 4F 4 F A6WE E2EA 1996090500355 19960905 00355 WP 1996 9 5 CALA9601250 1 19960831 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 937MC 49450 INSPECTION FOUND THE AFT CABIN FLOOR PATH EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE IN AFT SECTIO N OF EMERGENCY TRACK LIGHTING. THE WIRE WAS SPLICED AND OPERATION OF THE PATH LIGHTING CHECKED GOOD. 2 L 7 2 4F A6WE 1996090500356 19960905 00356 NM 1996 9 5 CALA9601251 1 19960901 A 2910 65445101306 HYD LINE BOEING 737 737130 1384435 NM LT MLG W/W CHAFED A CALA A D UNSCHED LANDING RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 09 59207 19024 THE AIRCRAFT WAS RETURNED TO EWR AFTER LOSS OF THE A-HYDRAULIC SYSTEM. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENAN CE FOUND A-SYSTEM RETURN LINE IN LT MLG WHEEL WELL CHAFED AGAINST ANOTHER HYDRAULIC LINE. BOTH HYDRAULIC LINES WERE REM OVED AND REPLACED AND LEAK CHECKS WERE GOOD. 2 L 7 2 4F A16WE 1996090500357 19960905 00357 WP 1996 9 5 CALA9601252 1 19960902 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG OVERSERVICED A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 10801 49127 THE NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE GEAR WAS RECYCLED WITH UNSUCCESSFUL RESULTS. THE AIRCRAFT WAS RETUR NED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE STRUT OVERSERVICED. THE STRUT WAS SERVICED PRO PERLY WITH NITROGEN AND A GEAR SWING WAS GOOD. A DIP WAS ISSUED REQUIRING FULL NOSE STRUT SERVICE PER MM 32-21-02, AT T HE NEXT MAINTENANCE RUN WITH CAPABILITIES. 2 L 7 2 4F A6WE 1996090500358 19960905 00358 WP 1996 9 5 CALA9601253 1 19960902 A 2842 MS29513244 O-RING DOUG DC10 DC1030 3023501 WP PROBE PLATE LEAKING A CALA A J UNSCHED LANDING DUMP FUEL K FLUID LOSS CL CLIMB 1 SW 09 68060 47850 A FUEL LEAK WAS REPORTED COMING FROM TOP OF RIGHT WING. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT L ANDED WITHOUT INCIDENT. MAINTENANCE FOUND FUEL LEAK AT RT WING FAULT ISOLATION PROBE PLATE. A NEW O-RING WAS INSTALLED AND SEALED IAW MM 28-00-00, LEAK CHECKS WERE GOOD. 2 L 7 3 4F A22WE 1996090500359 19960905 00359 WP 1996 9 5 CALA9601254 1 19960902 A 3231 ARG70961 SPRING DOUG DC10 DC1010 3022110 WP LT MLG DOOR BROKEN A CALA A D UNSCHED LANDING RETURN TO BLOCK J WARNING INDICATION CR CRUISE 1 SW 09 68042 46901 THE LT MLG RED LIGHT CAME ILLUMINATED DURING CRUISE AFTER ACCELERATING TO 300 KNOTS. THE LIGHT EXTINGUISHED BELOW 240 K NOTS WHILE ON DESCENT DURING RETURN TO GUM. MAINTENANCE FOUND THE LEFT GEAR DOOR EXTENSION SPRING ON LEVER BROKEN. THE SPRING WAS REPLACED, A TEST FLIGHT WILL BE CONDUCTED FOR OPERATIONAL CHECKS. 2 L 7 3 4F A22WE 1996090500360 19960905 00360 NM 1996 9 5 CALA9601255 1 19960902 A 3350 FUSES BOEING 727 727224 1384076 NM CABIN BLOWN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND THE EMERGENCY AISLE PATH LIGHTING INOPERATIVE IN FIRST CLASS CABIN. THE FORWARD BATTERY PACK FUSES WER E REPLACED AND OPERATION OF THE LIGHTS WAS RESTORED. 2 L 7 3 4F A3WE 1996090500361 19960905 00361 WP 1996 9 5 CALA9601256 1 19960902 A 3350 EMBS1392 BATT CHARGER DOUG DC10 DC1030 3023501 WP CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 13066 46591 THE CREW REPORTED EMERGENCY LIGHT TEST IN COCKPIT DID NOT GIVE GREEN LIGHT. MAINTENANCE FOUND MID CABIN OVERWING BATTER Y CHARGER SUPPLY AT FAULT. THE BATTERY CHARGER WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. 2 L 7 3 4F A22WE 1996090500362 19960905 00362 NM 1996 9 5 CALA9601257 1 19960902 A 2910 HYD LINE BOEING 737 7373T0 1384582 NM NR 2 ENGINE BROKEN A CALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 09 17309 23360 THE B-SYSTEM LOW PRESSURE LIGHT FOR NR 2 ENGINE HYDRAULIC PUMP ILLUMINATED FOLLOWED BY B-SYSTEM HYDRAULIC QUANTITY DROP TO 0.5 GALLONS WHILE APPROACHING CLE. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND B-SYSTEM HYDRAULIC PUMP LINE BROKEN. THE HYDRAULIC LINE WAS REMOVED AND REPLACED. IN ADDITION, THE NR 2 ENGINE DRIVEN PUMP WAS REMOVED AND REP LACED, LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 1996090500363 19960905 00363 WP 1996 9 5 9618881225 1 19960829 A 5242 SEAL DOUG DC10 DC1030 3023501 WP CENTER E/E DOOR WORN A NWAA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 01 225NW 46582 DURING CRUISE, CABIN PRESSURE FLUCTUATED AND UNABLE TO CONTROL NR 2 PNEUMATIC SYSTEM. FLIGHT RETURNED TO HNL. MAINTENA NCE REPLACED THE CENTER E/E DOOR SEAL, REINSTALLED NR 1 AND NR 2 FAN BYPASS CHECK VALVE, AND LOCKED THE NR 2 PRSOV INTO THE CLOSED POSITION. 2 L 7 3 4F A22WE 1996090500364 19960905 00364 NE 1996 9 5 9618899921 2 19960831 A 7230 COMPRESSOR DOUG DC9 DC932 3022066 WP PWA JT8 JT8D15 52051 NE LT ENGINE STALLED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK R C PARTIAL RPM/PWR LOSS F.O.D. TO TAKEOFF 1 GL 01 943N 47647 656971 WHEN APPLYING TAKEOFF POWER, THE LEFT ENGINE EXPERIENCED COMPRESSOR STALLS. CREW ABORTED TAKEOFF AND RETURNED TO THE GA TE. MAINTENANCE INSPECTED THE LEFT ENGINE INLET AND OUTLETS AND FOUND PAPER DEBRIS IN FIRST STAGE STATOR. PAPER DEBRIS WAS REMOVED AND AN ENGINE RUN-UP WAS ACCOMPLISHED. ALL PARAMETERS WERE NORMAL, NO STALLS OCCURRED. 2 L 7 2 4F 4 F A6WE E2EA 1996090500365 19960905 00365 NE 1996 9 5 9618901154 2 19960831 A 7200 ENGINE DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 1 FAILED A NWAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 01 154US 46767 86171 EN ROUTE, THE NR 1 ENGINE EXPERIENCED LOSS OF OIL QUANTITY AND PRESSURE. CREW FOLLOWED COM PROCEDURE, SHUT DOWN THE ENG INE, AND RETURNED TO SEA WITHOUT FURTHER INCIDENT. AT THE TIME OF SHUTDOWN, RESIDUAL PRESSURE WAS 28 PSI WITH 30 PERCEN T N1 AND 20 PERCENT N2 WINDMILLING RPM REMAINING. THE ENIGNE WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE WITHOUT ALL ENGINE PERFORMANCE TESTS BEING NORMAL. 2 L 7 3 4F 4 F A22WE E20EA 1996090500366 19960905 00366 NE 1996 9 5 9618916613 2 19960829 A 7230 COMPRESSOR BOEING 747 747251B 1384892 NM PWA JT9 JT9D7F 52054 NE NR 4 ENGINE STALLED A NWAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DE DESCENT 1 GL 01 613US 20358 89464 EN ROUTE, THE NR 4 ENGINE EXPERIENCED COMPRESSOR STALL AT TOP OF DESCENT. CREW FOLLOWED COM PROCEDURE AND SHUT DOWN THE ENGINE. DECLARED EMERGENCY AND CONTINUED FLIGHT TO MSP WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTION REVEALED META L IN TAILPIPE. THE AIRCRAFT IS SCHEDULED FOR NR 4 ENGINE REPLACEMENT IN MSP. 2 L 7 4 4F 4 F A20WE E20EA 1996090500367 19960905 00367 WP 1996 9 5 9618921145 1 19960901 A 7712 7551501 TT2 SENSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 1 ENGINE FAILED A NWAA E O ENGINE SHUTDOWN OTHER J R WARNING INDICATION PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 GL 01 145US 33942 8753 46754 86123 DURING TAXING OUT, THE NR 1 ENGINE EXPERIENCED COMPRESSOR STALL AND VIBRATION. AS THE NR 1 ENGINE EGT CLIMBED TO 750 DE GREES, THE CREW FOLLOWED COM PROCEDURE, SHUT DOWN THE ENGINE, AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. REPLAC ED TT2 SENSOR, LEAK AND FUNCTIONAL TEST WERE NORMAL. 2 L 7 3 4F 4 F A22WE E20EA 1996090500368 19960905 00368 NE 1996 9 5 9618932298 2 19960902 A 7532 492143 BLEED CONTL VLV BOEING 727 727251 138408H NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 01 298US 27667 1190 22152 696617 WHEN APPLYING TAKEOFF POWER, THE LEFT ENGINE EXPERIENCED COMPRESSOR STALLS. CREW ABORTED TAKEOFF AND RETURNED TO THE GA TE. MAINTENANCE REPLACED THE LEFT ENGINE PRESSURE BLEED CONTROL VALVE, LEAK AND OPERATIONAL CHECK OK. 2 L 7 3 4F 4 F A3WE E2EA 1996090500369 19960905 00369 EU 1996 9 5 9618943206 1 19960902 A 3350 321430 BATTERY AIRBUS 320 A320211 3930320 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 306US 60 DURING LINE MAINTENANCE, THE FORWARD LEFT AND LEFT OVERWING EMERGENCY LIGHTS FAILED THE EMERGENCY LIGHTS BATTERY CHECK. REPLACED BATTERY PACKS, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996090500370 19960905 00370 EU 1996 9 5 9618953208 1 19960831 A 3350 321454 LIGHTS AIRBUS 320 A320211 3930320 EU CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 308US 13022 7506 107 DURING LINE MAINTENANCE, THE EMERGENCY LIGHTS FAILED THE SELF TEST. REPLACED EPSU, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996090500371 19960905 00371 SO 1996 9 5 COMA9610268 1 19960829 A 2752 3203001005 ACTUATOR EMB 120 EMB120RT SO RT TE FLAP MALFUNCTION A COMA O OTHER J WARNING INDICATION UK UNKNOWN 1 SO 01 159A 13831 5121 120159 FLAP ASYMMETRY WARNING WHEN FLAPS SELECTED TO 25 DEGREES. REPLACED THE RT INBD FLAP ACTUATOR. 2 L 7 2 4T RT A31SO 1996090500372 19960905 00372 1996 9 5 COMA9610269 4 19960830 A 3425 6226190204 COMPUTER EMB 120 EMB120RT SO E/E COMPT MALFUNCTION A COMA O OTHER J WARNING INDICATION UK UNKNOWN 1 SO 01 264CA 10259 328 120256 HEADING FLAG ON EHSI WILL NOT RESET. REPLACED THE NR 2 AHRS COMPUTER. 2 L 7 2 4T RT A31SO 1996090500373 19960905 00373 SO 1996 9 5 COMA9610270 1 19960831 A 2752 3203001007 ACTUATOR EMB 120 EMB120RT SO LT TE FLAP MALFUNCTION A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 1117H 10362 1886 120117 FLAP CONTROL FAULT WARNING DURING FLIGHT WITH FLAPS AT ZERO. REPLACED THE LT OUTBD FLAP ACTUATOR. 2 L 7 2 4T RT A31SO 1996090500374 19960905 00374 SW 1996 9 5 COMA9620014 1 19960831 A 3260 SWITCH SWRNGN SA227 SA227AC 8780603 SW RT MLG DNLOCK MALFUNCTION A COMA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 703CA AC703 RT MLG INDICATED UNSAFE ON FIRST EXTENSION. LANDING GEAR CYCLED AND INDICATION NORMAL. REPLACED THE RT MLG DOWNLOCK SW ITCH. 2 L 7 2 4T RT A8SW 1996090500375 19960905 00375 SW 1996 9 5 COMA9620015 1 19960830 A 2711 CHAIN GUIDE SWRNGN SA227 SA227AC 8780603 SW LT AILERON TRIM LACK OF LUBE A COMA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 704C AC704 AILERON TRIM WHEEL BINDING. REPOSITIONED AND LUBED AILERON TRIM CHAIN GUIDE. 2 L 7 2 4T RT A8SW 1996090500376 19960905 00376 NM 1996 9 5 UPS96421034 1 19960831 A 3350 900835A BATTERY PACK BOEING 747 747121 1384871 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 682UP 20349 INSPECTION TYPE, UPPER DECK DOOR EMERGENCY EXIT SIGN HAS DEAD BATTERY, FAILED DURING ROUTINE CHECK. REPLACED BATTERY. 2 L 7 4 4F A20WE 1996090500377 19960905 00377 NM 1996 9 5 UPS96421035 4 19960830 A 2565 7A124836 ESCAPE SLIDE BOEING 747 747121 1384871 NM FLIGHT DECK IMPROPERLY INST A A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 691UP 19641 INSPECTION TYPE, ESCAPE SLIDE INOP. CABLES DISCONNECTED ALSO SLIDE IS NOT ON ITS MOUNT, FWD SIDE. REINSTALLED ESCAPE S LIDE PER MM 25-68-02. 2 L 7 4 4F A20WE 1996090500378 19960905 00378 NM 1996 9 5 UPS96220990 1 19960820 A 5320 69445593 STIFFENER BOEING 727 727247 138408F NM BS 969.5 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 212UP 21392 INSPECTION TYPE-C, CORROSION (C53-113-01.00-02) ON SHEAR TIE STA 969.5 WL 149 LBL 2, LBL 10 AREA MARKED. REMOVED CORROS ION AND FOUND STIFFENER OUT OF LIMITS, SHEAR TIE CORROSION WAS WITH IN LIMITS. REMOVED AND REPLACED STIFFENER. ALL WOR K IAW SRM 51-10-6, 53-10-1, 53-10-6, 53-10-2, 51-10-2, 51-30-2. 2 L 7 3 4F A3WE 1996090500379 19960905 00379 NM 1996 9 5 UPS96221026 1 19960822 A 5320 CLIPS BOEING 727 72731C 1384011 NM BS 1050 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE-C, STA 1050 STR TO FRAME CLIPS AT 6R, 7R AND 9R. REMOVED AND REPLACED CLIPS PER BOEING DWG NR 65-45313 AND SRM 51-30-2-1. 2 L 7 3 4F A3WE 1996090500380 19960905 00380 NM 1996 9 5 UPS96221027 1 19960822 A 5320 CLIPS BOEING 727 72731C 1384011 NM BS 1070 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE-C, STA 1070 STR TO FRAME CLIPS CRACKED AT STR'S 9R, 7R, 6R, 5R AND 4R. REMOVED AND REPAIRED CLIPS PER B OEING DWG NR 65-45313 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996090500381 19960905 00381 NM 1996 9 5 UPS96221028 1 19960822 A 5320 CLIPS BOEING 727 72731C 1384011 NM BS 1070 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE-C, STA 1070 STR TO FRAME CLIPS CRACKED AT STR'S 5L, 6L, 7L. REMOVED AND REPLACED CLIPS PER BOEING DWG N R 65-45313. 2 L 7 3 4F A3WE 1996090500382 19960905 00382 NM 1996 9 5 UPS96221029 1 19960823 A 5754 SKIN BOEING 727 72731C 1384011 NM NR 4 LE SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE-C, 1 INCH CRACK IN LT WING NR 4 SLAT INTERNAL NEXT TO LAST I/B RIB ON I/B SIDE AT BOTTOM IN RADIUS 6 INC HES O/B OF RIB. STOP DRILLED CRACK/ FAB AND INSTALLED REPAIR DOUBLER. 2 L 7 3 4F A3WE 1996090500383 19960905 00383 NM 1996 9 5 UPS96221030 1 19960820 A 5754 WEB BOEING 727 72731C 1384011 NM NR 1 LE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE-C, THE NR 1 SLAT ACTUATOR I/B ATTACH WEB CRACKED. REMOVED WEB DAMAGE AND FABRICATED REPLACEMENT WEB PER SB 727-57-0130, INSTALLED REPLACEMENT WEB PER SB 727-57-0130 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996090500384 19960905 00384 NM 1996 9 5 UPS96221031 1 19960821 A 5313 STRINGER BOEING 727 727247 138408F NM BS 571 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 212UP 21392 INSPECTION TYPE-C, CORROSION (C53-113-01.00-01) BROKEN STAND-OFF FOR CLAMP STA 571, LBL 8, WL 148, STR 27 LEFT. CORROSI ON OUT OF LIMITS IN A 1 INCH BY 1 INCH AREA, CUTOUT DAMAGED AREA, FABRICATED REPAIR PARTS AND REPAIRED PER SRM 53-10-3. 2 L 7 3 4F A3WE 1996090500385 19960905 00385 WP 1996 9 5 UPS96821019 1 19960826 A 5313 3202969 LONGERON DOUG DC8 DC871F 302199D WP BS 60-70 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE SPEC, LONGERON 335R CRACKED AT FS 60 TO 70. REPLACED LONGERON SECTION PER SRM 51-1-20D AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1996090500386 19960905 00386 WP 1996 9 5 UPS96821020 1 19960826 A 5313 3702969 LONGERON DOUG DC8 DC871F 302199D WP BS 70-60 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE SPEC, LONGERON 36 CRACKED AT FS 70 TO 60. REPLACED LONGERON SECTION FS 60 TO 70 PER SRM 51-1-21 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996090500387 19960905 00387 WP 1996 9 5 UPS96821021 1 19960826 A 5313 5618862 LONGERON DOUG DC8 DC871F 302199D WP BS 8-70 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE SPEC, LONGERON 32L HAS HEAVY CORROSION AT FS 8 TO 70. REPLACED LONGERON SECTION PER SRM 51-1-21 AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 1996090500388 19960905 00388 WP 1996 9 5 UPS96821022 1 19960825 A 5320 SHEAR TIE DOUG DC8 DC871F 302199D WP BS 55 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE SPEC, SHEAR TIE CRACKED ON OUTBOARD END AT LONGERON 34L FS 55. REPAIRED SHEAR TIE PER SRM 53-2-0. 2 L 7 4 4F RT 4A25 1996090500389 19960905 00389 WP 1996 9 5 UPS96821023 1 19960824 A 5313 36428382 LONGERON DOUG DC8 DC871F 302199D WP BS 8-70 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE SPEC, HEAVY CORROSION ON LONGERON 33R, FS 8 TO 70. REPLACED LONGERON SECTION PER SRM 51-3-0. 2 L 7 4 4F RT 4A25 1996090500390 19960905 00390 WP 1996 9 5 UPS96821024 1 19960826 A 5320 DOUBLER DOUG DC8 DC871F 302199D WP LT/RT NLG DOOR CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE SPEC, LT AND RT NOSE LANDING GEAR DOOR ACCESS PLATE INNER DOUBLERS HEAVILY CORRODED. REPLACED INNER DO UBLERS PER SRM 51-1-20D AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1996090500391 19960905 00391 WP 1996 9 5 UPS96821025 1 19960823 A 5330 561386261 SKIN DOUG DC8 DC871F 302199D WP BS 25 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE SPEC, INTERIM REPAIR DUE TO HEAVY CORROSION, NEED PERMANENT REPAIR AT FUSEL AGE SKIN, FS 25 LONGERON 36. REPLACED SKIN SECTION FS 70 TO 8 LONGERONS 31L AND 31R PER DRAWING NR DAC56138 62 AND UPS EO. 2 L 7 4 4F RT 4A25 1996090500392 19960905 00392 EU 1996 9 5 QXEA9600357 1 19960830 A 3350 1820 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 803PH 11031 FORWARD EMERGENCY LIGHT INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996090500393 19960905 00393 EU 1996 9 5 QXEA9600358 1 19960830 A 5210 A26179001 ROLLERS FOKKER A26000701 FOKKER F28 F28MK1000 4990808 EU PAX DOOR STICKING A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 466US 11075 MAIN CABIN DOOR WILL NOT OPEN USING THE ALTERNATE METHOD. INSIDE DOOR HANDLE WILL NOT STAY IN THE EMERGENCY POSITION. E MERGENCY PORTION OF THE MAIN CABIN DOOR ROLLERS FOUND STICKING. ROLLERS REPLACED AND RIGGED CABLE MECHANISM IAW MAINT M ANUAL, DOOR OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996090500394 19960905 00394 EU 1996 9 5 QXEA9600359 1 19960901 A 3350 1820 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 802PH 11017 EMERGENCY EXIT SIGN AT SEAT 8AB INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996090500395 19960905 00395 EU 1996 9 5 QXEA9600360 1 19960901 A 3350 6008903 BATTERY FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 469US 11096 NR 4 AND NR 5 OVERHEAD EVAC LIGHT INOP. BATTERY REPLACED AND LIGHTS OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996090500396 19960905 00396 EU 1996 9 5 QXEA9600361 1 19960901 A 3350 6008903 BATTERY FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 469US 11096 NR 1 OVERHEAD EVACUATION LIGHT INOP. BATTERY REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996090500397 19960905 00397 NM 1996 9 5 QXEA9600362 1 19960901 A 3350 321430 BATTERY DORNER DORNER DO32 DO328100 2996000 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 338PH 3029 FORWARD STARBOARD EMERGENCY LIGHT INOP IN ARM POSITION WHEN NON-ESSENTIAL TURNED OFF. BATTERY IN POWER SUPPLY 5LK REPLA CED IAW MAINT MANUAL AND LIGHT OPS CHECKED GOOD. 2 H 7 2 4T RT A45NM 1996090500398 19960905 00398 NM 1996 9 5 QXEA9600363 1 19960901 A 3350 362624 LIGHT DORNER DORNER DO32 DO328100 2996000 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 329PH 3007 RIGHT HAND FORWARD ESCAPE PATH LIGHT INOP. RECONNECTED ESCAPE PATH LIGHT STRIP AND LIGHT OPS CHECKED GOOD. 2 H 7 2 4T RT A45NM 1996090500399 19960905 00399 EU 1996 9 5 QXEA9600364 1 19960902 A 3350 1820 BULB FOKKER FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 487US 11238 RIGHT HAND AFT OVERWING EMERGENCY EXIT LIGHT INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996090500400 19960905 00400 EU 1996 9 5 QXEA9600365 1 19960902 A 3350 1820 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 803PH 11031 LEFT OVERWING EMERGENCY LIGHT INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996090500401 19960905 00401 NM 1996 9 5 QXEA9600366 1 19960903 A 5610 001A561A0000200 WINDSHIELD DORNER DO32 DO328100 2996000 NM LT COCKPIT DELAMINATION A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 335PH 3013 OUTER PANE ON THE PILOTS WINDSHIELD DELAMINATED AND CRACKED ALONG THE TOP EDGE. DELAMINATION IS 15 INCHES BY .250 INCHE S IN SIZE WITH NUMEROUS SMALL CRACKS AT THE TOP EDGE. WINDSHIELD REPLACED IAW MAINT MANUAL AND AIRCRAFT RETURNED TO SER VICE. 2 H 7 2 4T RT A45NM 1996090500402 19960905 00402 NM 1996 9 5 96FDEA01422 1 19960812 A 5313 65258111 STRINGER BOEING 727 72722 1384002 NM BS 1157 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 NR 0597 AND 036, BULGE IN SKIN AT BS 1157, STR 27 L. 2 L 7 3 4F A3WE 1996090500403 19960905 00403 NM 1996 9 5 96FDEA01423 1 19960902 A 5311 65163461 FRAME BOEING 727 72722 1384002 NM BS 1110 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 196FE 19145 NR 0255 AND 037, CRACK ON FRAME AT BS 1110, STR 27R, RBL 22 WL 153. 2 L 7 3 4F A3WE 1996090500404 19960905 00404 NM 1996 9 5 96FDEA01424 1 19960903 A 5320 65317731 CHORD BOEING 727 72725 1384006 NM BS 1176.9 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 509FE 19145 NR 0394 AND 012, CORROSION (C53-224-01, -2) ON BS 1176.9 CHORD AT RBL 1 TO 6 AND LBL 10 TO 4 OUT OF LIMITS WL 208. *S/D * CORROSION FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED DAMAGED CHORD AS PER SERVICE BULLETIN NR 727-53-0184 METHOD 3 AND DROWING 65C33557. 2 L 7 3 4F A3WE 1996090500405 19960905 00405 NM 1996 9 5 96FDEA01425 1 19960903 A 5311 6516307 FRAME BOEING 727 72725 1384006 NM BS 235 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 509FE 18280 NR 0514 AND 013, CORROSION (C53-221-01) ON FRAME BS 235 LBL 45 WL 217. 2 L 7 3 4F A3WE 1996090500406 19960905 00406 NM 1996 9 5 96FDEA01282 1 19960724 A 5730 SKIN BOEING 747 747245F 1384897 NM BS 1240 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 641FE 20827 CENTER WING TANK EXTERNAL LOWER SKIN AT BS 1240 LBL 99 FOUND CORROSION EXCEED SRM LIMIT. *S/D* REPAIR CARRIED OUT PER FED EX ENGINEERING REPAIR AUTHORIZATION-ERA NR 57-10-98. 2 L 7 4 4F A20WE 1996090500407 19960905 00407 NM 1996 9 5 96FDEA01426 1 19960822 A 5320 INTEGRAL RIB BOEING 727 727233 138408A NM BS 870 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 22346 LT 870 INTEGRAL RIB FWD CRACK FROM O/B HOLE TO EDGE. INSTALLED BATHTUB FITTING PER EA NR 7-5310-28832. 2 L 7 3 4F RT A3WE 1996090500408 19960905 00408 NM 1996 9 5 96FDEA01427 1 19960814 A 5320 SPLICE PLATE BOEING 727 72722C 138400F NM BS 870 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 CORROSION UNDER WING TO FUSE SPLICE PLATE LT SIDE AFT CORNER OF TANK BS 870 LBL 70.5. CUT OUT CORROSION, INSTALLED REPA IR PER EA 7-5710-28845. 2 L 7 3 4F A3WE 1996090500409 19960905 00409 NM 1996 9 5 96FDEA01428 1 19960815 A 5320 ANGLE BOEING 727 72722C 138400F NM BS 344 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 FLOOR BOARD SUPPORT ANGLE CORRODED AT STA 344 26 TO 45 LBL FLOOR BEAM. REMOVED CORROSION AND INSTALLED CAP STRIP REPAIR PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996090500410 19960905 00410 NM 1996 9 5 96FDEA01429 1 19960814 A 5347 SEAT TRACK BOEING 727 72722C 138400F NM BS 840 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 CORROSION ON O/B OF TRACK STA 840 RBL 48. INSTALLED DOUBLER PER EA 7531028823. 2 L 7 3 4F A3WE 1996090500411 19960905 00411 NM 1996 9 5 96FDEA01430 1 19960821 A 5730 SKIN BOEING 727 72722C 138400F NM BS 850-856 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 UPPER SURFACE CENTER WING SECTION, CENTER WING SKIN HAS HEAVY CORROSION AT LT AFT CORNER SECTION UNDER PRESS. SEAL TRAC K APPROX 6 INCH AREA, THREE PLACES FS 850 TO 856. CORROSION REMOVED, DIGITAL THICKNESS CHECKED BY NDT, ORIG 184 TAKEN D OWN TO .068. REPAIR DOUBLER INSTALLED PER ESO 11782 DATED 8/7/96 AND EA NR 7571028845 DATED 8/15/96. 2 L 7 3 4F A3WE 1996090500412 19960905 00412 NM 1996 9 5 96FDEA01431 1 19960814 A 5320 ANGLE BOEING 727 72722C 138400F NM BS 1176 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 CABIN INTERIOR, FS 1176 REINFORCEMENT CHORD ANGLE HAS HEAVY TO SEVERE CORROSION. FLOOR LEVEL BETWEEN BL 44 TO 46 LT. R EMOVED DAMAGED PORTION OF CHORD ANGLE, INSTALLED NEW SECTION AND SPLICE DOUBLER PER E/A NR 7531028817. 2 L 7 3 4F A3WE 1996090500413 19960905 00413 NM 1996 9 5 96FDEA01432 1 19960903 A 5320 TRACK BOEING 727 72722C 138400F NM BS 840 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 107FE 19202 CORROSION ON O/B OF TRACK STA 840 RBL 48. INSTALLED DOUBLER PER EA 7531-0-28823 AND 51-10-1. 2 L 7 3 4F A3WE 1996090500414 19960905 00414 WP 1996 9 5 MWEA96423 1 19960831 A 2560 113317 EVAC SLIDE DOUG DC9 DC932 3022066 WP PAX DOOR FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 207ME 47794 CREW REPORTS FWD ENTRY DOOR EVACUATION SLIDE FELL OUT WHEN OPENING DOOR. REINSTALLED EVACUATION SLIDE. 2 L 7 2 4F A6WE 1996090500415 19960905 00415 WP 1996 9 5 MWEA96424 1 19960901 A 2612 FIRE LOOP DOUG DC9 DC932 3022066 WP LT ENGINE MALFUNCTIONED A MWEA O OTHER N FALSE WARNING CL CLIMB 1 GL 31 202ME 47672 PILOT REPORTS LT ENGINE FIRE DETECTOR LOOP LIGHT ILLUMINATED WHILE CLIMBING THROUGH 23,000 FT. MASTER CAUTION AND FIRE DETECTOR LIGHTS ALSO ILLUMINATED, EXTINGUISHED AFTER 30 SEC. CLEANED LT ENG LOOP CONNECTIONS, CHECKED PYLON CONNECTIONS AND LOOPS FOR CHAFING, CHECKED BLEED AIR DUCTS. RAN ENGINE AT 1.9 EPR FOR 5 MIN, NO DEFECTS NOTED. 2 L 7 2 4F A6WE 1996090500416 19960905 00416 1996 9 5 MWEA96425 4 19960901 A 2565 113317 EVAC SLIDE DOUG DC9 DC932 3022066 WP FWD GALLEY LOW PRESS A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 DURING SERVICE CK, FOUND FWD GALLEY SERVICE DOOR EVAC SLIDE PRESSURE LOW. REPLACED GALLEY DOOR EVACUATION SLIDE. 2 L 7 2 4F A6WE 1996090500417 19960905 00417 WP 1996 9 5 SCNA96239 1 19960824 A 2611 SMOKE DETECTOR DOUG DC10 DC1030F 3023504 WP CARGO BROKEN WIRE A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 601GC 47921 FOUND BULK COMPARTMENT SMOKE DETECTOR TEST BULB WIRE BROKEN. SOLDERED BROKEN WIRE AND SMOKE DETECTOR OPS CHECKED GOOD. 2 L 7 3 4F RT A22WE 1996090500418 19960905 00418 WP 1996 9 5 SCNA96240 1 19960824 A 2612 CONNECTORS DOUG DC10 DC1030F 3023504 WP NR 2 FIRE LOOP DIRTY A SCNA K NONE N FALSE WARNING DE DESCENT 1 GL 15 603GC 47922 NR 2 FIRE LOOP-A WAS FLASHING DURING DESCENT AND APPROACH. CLEANED CONNECTOR, CHECKED LOOP-A SYSTEM FOR SHORTS. NO SH ORTS FOUND, OPS CHECKED GOOD. 2 L 7 3 4F RT A22WE 1996090500419 19960905 00419 NM 1996 9 5 P5CA9600668 1 19960901 A 3240 TORQUE LINK BOEING 747 747122 1384872 NM RT MLG BRAKE MISSING A P5CA K NONE K J D FLUID LOSS WARNING INDICATION INFLIGHT SEPARATION TO TAKEOFF 1 WP 23 853FT 19753 AFTER TAKEOFF, LOST NR 1 HYDRAULIC SYSTEM FLUID. LANDING INSPECTION REVEALED RIGHT BODY GEAR LEFT FORWARD BRAKE TORQUE LINK DISCONNECTED. ADDITIONAL DAMAGE TO BODY GEAR TILT ACTUATOR HOSE, NR 10 BRAKE HOSE BOTH FORWARD AND AFT BRAKE TORQU E LINKS. BRAKE ROD BOLT FOUND ON RUNWAY. REPLACED BRAKE TORQUE LINKS, NR 10 BRAKE AND BRAKE LINE PER M/M 32-41-00, REP LACED TILT ACTUATOR LINE PER MM 20-11-05 PAGE 815. REPLACED NR 10 TIRE PER MM 32-45-00. REPLACED NR 1 EDP, CASE DRAIN FILTER, PRESSURE FILTER AND FLUSHED LINES PER MM 29-11-05, 29-11-18, 29-11-23. 2 L 7 4 4F A20WE 1996090500420 19960905 00420 NM 1996 9 5 P5CA9600669 1 19960901 A 5280 GULL FAIRING BOEING 747 747122 1384872 NM LT MLG DOOR DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 DAMAGED GULL FAIRING LEFT WING LANDING GEAR LOWER STRUT DOOR AT AFT END. REPAIRED PER BOEING SRM 51-40-09. 2 L 7 4 4F A20WE 1996090500421 19960905 00421 NM 1996 9 5 P5CA9600670 1 19960831 A 3297 WIRE BOEING 747 747122 1384872 NM E\E COMPT CHAFED A P5CA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 851FT 19756 PRIMARY DISPLAY AND CONTROL CIRCUIT BREAKER TRIPPED. REPAIRED CHAFED WIRE AT CONNECTOR IN LANDING GEAR CARD FILE DISCON NECT PANEL, OPERATIONAL CHECKED OK PER M/M 32-61-00. 2 L 7 4 4F A20WE 1996090500422 19960905 00422 NM 1996 9 5 P5CA9600671 1 19960821 A 5711 SPAR BOEING 747 747132 1384882 NM CENTER WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION CENTER WING FRONT SPAR UPPER CHORD DRY BAY FROM RBL 90 TO RBL 115. CORROSION REMOVED PER BOEING SRM 5 1-10-01, WITHIN LIMITS PER 57-10-01, REPROTECTED PER 51-10-02. 2 L 7 4 4F A20WE 1996090500423 19960905 00423 NM 1996 9 5 P5CA9600672 1 19960822 A 5730 SKIN BOEING 747 747132 1384882 NM RT WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION AT RIGHT WING BOOST PUMP CUTOUT WBL 383. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 57-30-03, REPROTECTED PER 51-10-02. 2 L 7 4 4F A20WE 1996090500424 19960905 00424 NM 1996 9 5 P5CA9600673 1 19960823 A 5330 SKIN BOEING 747 747132 1384882 NM BS 1352 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION RIGHT BODY GEAR WHEEL WELL PRESSURE WEB SKIN BS 1352 RBL 84 ABOVE ANTI-SKID MODULE. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, REPROTECTED PER 51-10-02. 2 L 7 4 4F A20WE 1996090500425 19960905 00425 NM 1996 9 5 P5CA9600674 1 19960814 A 5312 BULKHEAD BOEING 747 747132 1384882 NM BS 1350 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION AT 1350 BULKHEAD LBL 118 WL 168 WHERE HYDRAULIC LINES PASS THROUGH BULKHEAD. CORROSION REMOVED PER BO EING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, REPROTECTED PER 51-10-02. 2 L 7 4 4F A20WE 1996090500426 19960905 00426 NM 1996 9 5 P5CA9600675 1 19960828 A 5320 PRESS DECK BOEING 747 747132 1384882 NM BS 1416 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION FASTENER HEAD BS 1416 RBL 127 ON PRESSURE DECK WEB. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, REPROTECTED PER 51-10-02. 2 L 7 4 4F A20WE 1996090500427 19960905 00427 NM 1996 9 5 P5CA9600676 1 19960831 A 3244 49X1730225CR TIRE BOEING 747 747123 1384873 NM NR 11 BLOWN A P5CA K NONE O OTHER LD LANDING 1 WP 23 858FT 20109 NR 11 TIRE BLOWN ON LANDING. PERFORMED BLOWN TIRE INSPECTION PER MAINTENANCE MANUAL 05-51-25, FOUND DAMAGE TO RT ADF SE NSE ANTENNA PANEL, 3 WIRES BROKEN ON RIGHT BODY GEAR AND NR 11 AND NR 12 BRAKE SYSTEMS FAILED LOCKED WHEEL PROTECTION ST EPS. REPLACED NR 11 AND NR 12 TIRES PER BOEING MAINTENANCE MANUAL 32-45-01, INTERIM REPAIR DOUBLER INSTALLED ON ADF SEN SE PANEL PER POLAR ENGINEERING, DEACTIVATED NR 11 AND NR 12 BRAKES PER MEL 32-5. INTERIM REPAIR ON 3 BROKEN WIRES DEFER RED, ITEM INITIATED. 2 L 7 4 4F A20WE 1996090500428 19960905 00428 WP 1996 9 5 TC8A96056 1 19960831 A 2612 FIRE SENSOR DOUG DC8 DC8F54 3021926 WP NR 2 ENGINE LOOSE A TC8A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 802CK 45679 NR 2 FIRE INDICATION AFTER TAKEOFF, C/W TCA QRH-2 CHECKLIST, RETURNED TO GRU. FOUND LT FWD COWLING SENSOR LOOP CLAMP LO OSE. TIGHTENED, CHECKED FOR PNEUMATIC LEAKS, RAN THE ENGINE AS PER MM 26-10-0, OPS NORMAL. 2 L 7 4 4F 4A25 1996090500429 19960905 00429 WP 1996 9 5 TC8A96057 1 19960901 A 7830 TR LINE DOUG DC8 DC8F54 3021926 WP NR 2 ENGINE LOOSE A TC8A A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 GL 23 802CK 45679 NR 2 ENGINE FIRE WARNING, SECURED ENGINE. FOUNDED PNEUMATIC LINES LOOSE AT AFT REVERSER AREA. TIGHTENED LINES, RAN UP TO T/O POWER 1.83 EPR, COULD NOT DUPLICATE THE ITEM MM 78-7-0 AND 71-00. 2 L 7 4 4F 4A25 1996090500430 19960905 00430 WP 1996 9 5 SRAA960813 1 19960830 A 3230 PIN DOUG DC8 DC871F 302199D WP NLG NOT REMOVED A SRAA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 GL 23 872SJ 46040 AFTER TAKEOFF, FOUND NOSE LANDING GEAR WOULD NOT RETRACT, DUMPED FUEL AND LOWERED MAIN LANDING GEAR TO ACCOMPLISH AIR TU RNBACK. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND NOSE GEAR PIN NOT REMOVED PRIOR TO DEPARTURE. REMOVED PIN AND RETURNE D AIRCRAFT TO SERVICE. 2 L 7 4 4F RT 4A25 1996090500431 19960905 00431 NM 1996 9 5 96ZZZM1262 1 19960724 A 3350 ML7715 BULB BOEING 747 747212B 1384886 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND FLOOR EVAC LIGHT AND LENS MISSING AT 53ABC. REPLACED SOCKET, BULB AND LENS. OPS CHECKED GOOD PER MM 33-51-00. REFERENCE TWRA96220. 2 L 7 4 4F A20WE 1996090500432 19960905 00432 NM 1996 9 5 96ZZZM1263 1 19960724 A 3350 07912 LENS BOEING 747 747212B 1384886 NM CABIN MISSING A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND FLOOR EVAC LIGHT AND LENS MISSING AT 53ABC. REPLACED SOCKET, BULB AND LENS. OPS CHECKED GOOD PER MM 33-51-00. REFERENCE TWRA96220. 2 L 7 4 4F A20WE 1996090500433 19960905 00433 NM 1996 9 5 96ZZZM1264 1 19960724 A 3350 07912 LENS BOEING 747 747212B 1384886 NM CABIN MISSING A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND SEAT 28C FLOOR EVAC LIGHT INOP AND ALSO LENS COVER MISSING. RELAMPED AND REPLACED LENS. OPS CHECKED OK PER MM 33-51-00. REFERENCE TWRA96218. 2 L 7 4 4F A20WE 1996090500434 19960905 00434 NM 1996 9 5 96ZZZM1265 1 19960724 A 3350 ML7715 BULB BOEING 747 747212B 1384886 NM CABIN MISSING A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND FLOOR EVAC LIGHT AND LENS MISSING AT 11ABC, 14ABC, 28ABC, 50KJH. REPLACED LENS AND BULB. OPS CHECKED OK PER MM 33-51-00. REFERENCE TWRA96221. 2 L 7 4 4F A20WE 1996090500435 19960905 00435 NM 1996 9 5 96ZZZM1266 1 19960724 A 3350 08912 LENS BOEING 747 747238B 1384828 NM CABIN MISSING A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 614FF 20534 DURING DAILY CHECK, FOUND SEAT 60C FLOOR EVAC LIGHT AND LENS COVER AREA MISSING. REPLACED BULB AND LENS. OPS CHECKED O K PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996090500436 19960905 00436 1996 9 5 96ZZZM1267 4 19960802 A 2312 6221181004 VHF COMM 2 DOUG DC9 DC915F 3022037 WP E/E COMPT FAILED A Y2PA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 23 198US 9573 47045 YIP - NR 1 COMM INOP (INTERMITTENTLY) AND NR 2 COMM INOP (INTERMITTENTLY). AIRCRAFT DIVERTED INTO YIP. NO EMERGENCY PR OCEDURES NECESSARY. MAINTENANCE WAS NOT ABLE TO DUPLICATE THE PROBLEM ON EITHER COMM. BOTH COMM'S WERE REPLACED AND BO TH SYSTEMS CHECKED GOOD IAW GMM CHAP 8, SEC 7. REFERENCE Y2PA96062. 2 L 7 2 4F A6WE 1996090500437 19960905 00437 WP 1996 9 5 96ZZZM1268 1 19960802 A 7931 42D110 OIL PRESS SW DOUG DC9 DC915F 3022037 WP RIGHT ENGINE MALFUNCTIONED A Y2PA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 196US 1487 47155 YIP - UNSCHEDULED LANDING MADE, OIL QTY WENT TO ZERO AND LOW OIL PRESSURE LIGHT FLICKERED. THE OIL PRESSURE REMAINED NO RMAL ACCORDING TO THE PRESSURE INDICATOR. REPLACED THE OIL QTY TRANSMITTER AND REPLACED THE OIL PRESSURE SWITCH. ENGIN E OPERATED AND CHECKED FOR PROPER OPERATION AND FOR LEAKS. NO DEFECTS NOTED. REFERENCE Y2PA96060. 2 L 7 2 4F A6WE 1996090500438 19960905 00438 NM 1996 9 5 96ZZZM1269 1 19960728 A 3222 MS2877520 SEAL BOEING 727 727251 138408H NM NLG LEAKING A IXKA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 25 264US 8696 19983 FLT 32 - MDW - AIR TURN BACK - UNABLE TO GET NOSE DOOR LIGHT TO GO OUT ON RETRACTION. BOTH RED LIGHT AND AMBER LIGHT ON . FOUND NOSE GEAR METERING PIN ORIFICE SEALS BAD, STRUT FLAT, TIRES HANGING UP ON DOORS. REMOVED AND REPLACED SEALS IA W 32-21-01 SWUNG NOSE GEAR IAW 32-61-0. OPS CHECK OK. REFERENCE IXKA9600063. 2 L 7 3 4F A3WE 1996090500439 19960905 00439 EU 1996 9 5 96ZZZM1270 1 19960622 A 3246 5006227 WHEEL BEARING SAAB SF340 340B 7860101 EU NLG FAILURE A A NVEA O OTHER D INFLIGHT SEPARATION TO TAKEOFF 1 SO 03 269AE 340B269 FLT 4900 - ROC - ON TAKEOFF, THE TOWER CONTACTED THE CREW STATING THAT THEY OBSERVED A TIRE FALLING FROM THE A/C. THE C AUSE HAS BEEN DETERMINED TO BE A RIGHT NOSE WHEEL, P/N 5006227, BEARING FAILURE. REMOVED NLG LOWER TORQUE LINK, AXLE AN D BOTH TIRE ASSEMBLYS. (M) 2 L 7 2 4T RT A52EU 1996090500440 19960905 00440 NM 1996 9 5 96ZZZM1271 1 19960810 A 3397 WIRE BOEING 737 7373Y0 1384671 NM CABIN LOOSE A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 955WP 24463 FOUND EMERGENCY EXIT FLOOR LIGHT COVER ROW 15 LEFT SIDE CAME UP AND WIRES CAME LOOSE. REPAIRED FLOOR TRACK LIGHTING AS REQUIRED. REFERENCE W8PA960103. 2 L 7 2 4F RT A16WE 1996090500441 19960905 00441 EA 1996 9 5 96ZZZM1272 2 19960714 A 7250 BEARING BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA LT ENGINE FAILED A GPPA E ENGINE SHUTDOWN O OTHER LD LANDING 1 CE 09 76013 UC12 AIRCRAFT WAS ON RAMP AREA, LEFT ENGINE WAS SHUT DOWN AND ALMOST STOPPED WHEN POWER SECTION SEIZED. PROPELLER WOULD NOT ROTATE. INTERNAL DAMAGE HAD OCCURED. (M) 2 L 7 2 4T 4 T RT A24CE E4EA 1996090500442 19960905 00442 GL 1996 9 5 96ZZZM1273 3 19960711 A 6111 EROSION SHIELD BEECH 1900 1900C 1154161 CE HARTZL HCB4M HCB4MP3 GL LT PROP DEBONDED A GPPA K NONE O OTHER IN INSP/MAINT 1 CE 09 32018 UC38 LEFT PROP EROSION SHIELD DELAMINATION NEAR TRAILING EDGE. DETECTED ON PRE-FLIGHT INSPECTION. MAINTENANCE DETERMINED OU T OF LIMITS DUE TO TOO WIDE AND TOO CLOSE TO TRAILING EDGE PER 1900 CAMP MAINTENANCE MANUAL. FERRIED AIRCRAFT TO CRAIG AND REMOVED AND REPLACED PROP. (M) 2 L 7 2 4T RT A24CE 6 C P56GL 1996090500443 19960905 00443 CE 1996 9 5 96ZZZM1274 1 19960709 A 5610 1143840201 WINDSHIELD BEECH 1900 1900C 1154161 CE LT COCKPIT CRACKED A GPPA K NONE O OTHER CR CRUISE 1 CE 09 39019 UC39 EN ROUTE TO JAX - CAPTAINS WINDSHIELD CRACKED (APPROX 5 PLACES NEAR UPPER EDGE), OUTER PLY ONLY. LANDED JAX. MAINTENAN CE DETERMINED UN-AIRWORTHY PER PILOT VISIBILITY AND INTERFERENCE WITH WIPER OPS. FERRIED A/C TO CRG UNPRESSURIZED AND R EMOVED AND REPLACED WINDSHIELD. (M) 2 L 7 2 4T RT A24CE 1996090500444 19960905 00444 NM 1996 9 5 96ZZZM1275 1 19960820 A 2150 870402 SENSOR BOEING 737 7373B7 1384580 NM CABIN MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 390US 23312 BWI - FLT 1245 - AFTER TAKEOFF, CREW COULD NOT GET AIRCRAFT TO PRESSURIZE. AIRCRAFT WAS HELD AT 9,000 FEET WHILE CONVER SING WITH MAINTENANCE. AFTER SEVERAL FAILED ATTEMPTS, CREW DECIDED TO RETURN TO FIELD AT BWI. NO EMERGENCY WAS DECLARE D AND THE FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT AIR CYCLE MACHINE, THE LEFT 35 DEGREE WATER SEPARATOR SENSOR AND THE LEFT AND RIGHT WATER SEPARATOR BAGS. OPS CHECK GOOD. PRESSURIZATION CHECK OF AIRCRAFT G OOD PER MAINTENANCE MANUAL. REFERENCE USAASB96163. 2 L 7 2 4F RT A16WE 1996090500445 19960905 00445 NM 1996 9 5 96ZZZM1276 1 19960820 A 2170 V1211 COALESCER BAG BOEING 737 7373B7 1384580 NM CABIN DIRTY A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 390US 23312 BWI - FLT 1245 - AFTER TAKEOFF, CREW COULD NOT GET AIRCRAFT TO PRESSURIZE. AIRCRAFT WAS HELD AT 9,000 FEET WHILE CONVER SING WITH MAINTENANCE. AFTER SEVERAL FAILED ATTEMPTS, CREW DECIDED TO RETURN TO FIELD AT BWI. NO EMERGENCY WAS DECLARE D AND THE FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT AIR CYCLE MACHINE, THE LEFT 35 DEGREE WATER SEPARATOR SENSOR AND THE LEFT AND RIGHT WATER SEPARATOR BAGS. OPS CHECK GOOD. PRESSURIZATION CHECK OF AIRCRAFT G OOD PER MAINTENANCE MANUAL. REFERENCE USAASB96163. 2 L 7 2 4F RT A16WE 1996090500446 19960905 00446 NE 1996 9 5 96ZZZM1277 2 19960814 A 7314 7086002 FUEL PUMP BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE NR 2 ENGINE FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 356US 23559 BWI - FLT 426 - ON CLIMB-OUT FROM DCA, THE NR 2 ENGINE BEGAN UNCOMMANED MOVEMENTS OF 1.5 TO 2 INCHES. WITH AUTOTHROTTLE ON, N1, N2, EGT, AND FUEL FLOW ALL FLUCTUATED. AUTOTHROTTLE DISCONNECTED AND STILL HAD FLUCTUATIONS. CAPTAIN DECIDED TO DIVERT TO BWI WHERE THE FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 ENGINE MAIN ENGINE CON TROL AND MAIN ENGINE FUEL PUMP PER MM. OPS CHECK NORMAL. RAN ENGINE THROUGH FULL POWER RANGE, NO FLUCTUATIONS NOTED. R EFERENCE USAASB96157. 2 L 7 2 4F 4 F RT A16WE E2GL 1996090500447 19960905 00447 NM 1996 9 5 96ZZZM1278 1 19960727 A 3350 07912 LENS BOEING 747 747238B 1384828 NM CABIN MISSING A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 607PE 20011 DURING DAILY CHECK, FOUND FLOOR EMERGENCY EVAC LIGHT INOP AT 3C 21H, 60H. REPLACED BULB AND LENS. OPS CHECKED NORMAL A S PER MM 33-51-00 PG 501. REFERENCE TWRA96241. 2 L 7 4 4F A20WE 1996090500448 19960905 00448 NM 1996 9 5 96ZZZM1279 1 19960729 A 3350 MIL7266100 BULB BOEING 747 747238B 1384828 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 614FF 20534 DURING DAILY CHECK, FOUND UPPER DECK AFT OF 73K, FLOOR EMERGENCY LIGHT INOP. REPLACED EMERGENCY LIGHT LENS AND BULB. O PS CHECKED OK PER MM 33-51-00 PG 501. REFERENCE TWRA96244. 2 L 7 4 4F A20WE 1996090500449 19960905 00449 NM 1996 9 5 96ZZZM1280 1 19960729 A 3350 MIL7266100 BULB BOEING 747 747238B 1384828 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 614FF 20534 DURING DAILY CHECK, FOUND FLOOR EMERGENCY LIGHT INOP AT 4H, 42C, 45C AND 50 C. REPLACED LENS AND BULB. OPS CHECKED NOR MAL AS PER MM 33-51-00 PG 501. REFERENCE TWRA96243. 2 L 7 4 4F A20WE 1996090500450 19960905 00450 NE 1996 9 5 96ZZZM1281 2 19960713 A 7250 3038613 TURBINE AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE ENGINE DAMAGED A A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 140DD 009 DURING GROUND ENGINE RUN UP, POWER TURBINE SUFFERED MASSIVE FAILURE. REPLACED ENGINE. 2 H 7 2 4T 4 T RT A53EU E20NE 1996090500451 19960905 00451 NE 1996 9 5 96ZZZM1282 2 19960714 A 7313 311610901 TRANSFER TUBE AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE NR 14 FUEL NOZZ LOOSE A TRBA E F A ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING A J FLAME/FIRE WARNING INDICATION CL CLIMB 1 SO 21 973NA 065 120641 DURING CLIMB, CREW RECEIVED FIRE INDICATION ON THE LEFT ENGINE AND FIRE BOTTLE WAS DISCHARGED. FOUND NR 14 SECONDARY FU EL NOZZLE TRANSFER TUBE LOOSE WITH FUEL LEAKAGE. ENGINE, BOTTOM COWLING ASSEMBLY AND ELECTRICAL HARNESS WERE REPLACED. SPECIFY PART CAUSING PROBLEM. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1996090500452 19960905 00452 WP 1996 9 5 96ZZZM1283 1 19960730 A 5350 UPPER PULLEY PIN DOUG DC9 DC932 3022066 WP FS 1168.895 MISSING A A ZJ4R K NONE O OTHER IN INSP/MAINT 1 SO 13 901VJ 71075 71075 47275 DURING MAINTENANCE, FOUND TAILCONE RELEASE CABLE RUN 310A FS 1168.895 OFF THE NR 2 UPPER PULLEY. ALSO, THE GUIDE PIN WA S MISSING FROM THE 2ND UPPER PULLEY FROM BOTTOM (CABLE RUN 301A). REROUTED CABLE ON PULLEY AND INSTALLED GUIDE PIN. 2 L 7 2 4F A6WE 1996090500453 19960905 00453 EU 1996 9 5 A21A9649001 2 19960731 A 7261 OIL TANK GARRTT GTPC364A FOKKER F28 F28MK4000 4990810 EU RROYCE SPEY SPEY55515P 54521 EU ENGINE LEAKING A A21A K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 17 496US P37483 11169 TEAR DOWN REPORT CONFIRMS MULTIPLE OIL LEAKS IN AREA OF OIL TANK POSSIBLY MIGRATING INTO INLET PLENNUM WHICH CAUSED SMOK E OUT THE BLEED AIR AND TAILPIPE. (M) 2 L 7 2 4F 4 F RT A20EU E2EU 1996090500454 19960905 00454 WP 1996 9 5 AALA961018 1 19960707 A 2613 805320 DETECTOR DOUG DC9 DC982 3022082 WP TAIL COMPT DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SW 07 427AA 49339 DFW - FLT 544 - DURING MAX POWER TAKEOFF WITH OAT 104 DEGREES, TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. ACCOMPLISH ED ABNORMAL PROCEDURES AND LIGHT EXTINGUISHED FOR APPROXIMATELY 1 MINUTE AND THEN ILLUMINATED AGAIN. AIRCRAFT RETURNED TO DFW AND PRIOR TO LANDING THE LIGHT EXTINGUISHED. AIRCRAFT LANDED OVERWEIGHT AT DFW WITHOUT INCIDENT. ACCOMPLISHED L EAK CHECK OF TAIL COMPARTMENT WITH NO DEFECTS FOUND. REPLACED BOTH TAIL COMPARTMENT TEMP DETECTORS. ACCOMPLISHED GROUN D ENGINE RUN TO FULL POWER WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OP. ACCOMPLISHED OVERWEIGHT LANDING INS PECTION WITH NO DEFECTS FOUND. ACCOMP FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS FOUND. SYSTEM OPS CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 1996090500455 19960905 00455 1996 9 5 AWXA960370 4 19960811 A 3442 6225132106 RT UNIT BOEING 757 757225 1384959 NM FWD FUSELAGE FAILED A AWXA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 28 914AW 16933 2874 22208 PHX - FLT 2610 - AIR TURNBACK - WEATHER WEAK MESSAGE ON SCREEN BUT WILL NOT PAINT BEYOND 30 MILES AND THEN RETURN IS NOT WHAT IS REALLY THERE. REMOVED AND REPLACED WEATHER RADAR R/T UNIT PER MM 34-41-00. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A2NM 1996090500456 19960905 00456 NM 1996 9 5 AWXA960394 1 19960815 A 3350 WIRES BOEING 737 7373G7 1384595 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 156AW 23778 PHX - FLT 2667 - DURING ROUTINE MAINTENANCE CHECK, FOUND BROKEN WIRES ON FLOOR PROX SYSTEM. REPAIRED WIRING. (M) 2 L 7 2 4F RT A16WE 1996090500457 19960905 00457 NM 1996 9 5 AWXA960395 1 19960814 A 2120 AIR DISTR BOEING 737 737112 1384412 NM CABIN ODOR A AWXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 28 708AW 19771 LAS - FLT 2574 - AIRCRAFT DIVERSION, EN ROUTE TO OAKLAND, PAX AND CREW DETECTED ODOR OF JET-A IN PASSENGER CABIN. INSPE CTION OF AIRCRAFT FOUND NO EVIDENCE OF FUEL LEAKAGE. INSPECTED BOTH ENGINES AND APU. NO LEAKS. RAN ENGINES AND APU W ITH PACKS, NO EVIDENCE OF ANY ODOR. CHECKED PACK BAY AREAS. ALL OK. INSPECTED CARGO COMPARTMENTS. ALL OK. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F A16WE 1996090500458 19960905 00458 EU 1996 9 5 C2XA96BT006 1 19960806 A 3234 F96GA0102 GEAR HANDLE AEROSP ATR42 ATR42320 8680930 EU LANDING GEAR FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 15827 175 EWR - FLT 3404 - AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO EWR UNEVENTFULLY. FOUND LANDING G EAR CONTROL HANDLE TO BE FAULTY. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE IAW ATR JIC 32-31-81-RAI-10000-006. P ERFORMED OPERATIONAL CHECK IAW ATR JIC 32-31-00-FUT-10000-003. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996090500459 19960905 00459 NE 1996 9 5 C2XA96IA184 2 19960805 A 7250 3033914 TURBINE EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE FAILED A A C2XA D RETURN TO BLOCK E VIBRATION/BUFFET TX TAXI/GRND HDL 1 SW 09 40717 13787 120133 115241 ILE - FLT 3997 - PILOT REPORTED THAT UPON TAXI, THE RIGHT ENGINE EMITTED A LOW GRADE RUMBLE/VIBRATION, AT APPROXIMATELY 60 PERCENT. THE AIRCRAFT RETURNED TO THE GATE, AND MAINTENANCE INSPECTED AND FOUND THE 2ND STAGE POWER TURBINE TO BE DA MAGED. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1996090500460 19960905 00460 NE 1996 9 5 C2XA96IA185 2 19960808 A 7250 3033914 TURBINE EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE FAILED A A C2XA K NONE E VIBRATION/BUFFET AP APPROACH 1 SW 09 40717 16277 120133 115294 IAH - FLT 3908 - PILOT REPORTED, THAT THE LEFT ENGINE EMITTED A LOW RUMBLE/VIBRATION DURING APPROACH. THE AIRCRAFT LAND ED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE LEFT ENGINE AND FOUND THE 2ND STAGE POWER TURBINE TO BE DAMAGED. MAINTE NANCE REMOVED AND REPLACED THE LEFT ENGINE AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1996090500461 19960905 00461 EU 1996 9 5 C2XA96IA186 1 19960810 A 5320 S2541003900200 SUPPORT AEROSP ATR42 ATR42320 8680930 EU LAV THRESHOLD CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14832 187 IAH - DURING C-CHECK INSPECTION, THE LAVATORY THRESHOLD SUPPORT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLA CED THE AFFECTED SUPPORT AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996090500462 19960905 00462 EU 1996 9 5 C2XA96IA187 1 19960810 A 5311 S5367240620800 FRAME AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14832 187 IAH - DURING C-CHECK INSPECTION, FRAME 36 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTI ON OF FRAME 36, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996090500463 19960905 00463 EU 1996 9 5 C2XA96IA188 1 19960810 A 5315 S5367240720202 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14832 187 IAH - DURING C-CHECK INSPECTION, FLOORBEAM 38 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED B EAM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996090500464 19960905 00464 EU 1996 9 5 C2XA96IA189 1 19960810 A 5315 S53672407202524 FLOOR BEAM AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14832 187 IAH - DURING C-CHECK INSPECTION, FLOOR BEAM 39 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996090500465 19960905 00465 WP 1996 9 5 GRAA9644 1 19960609 A 3350 079123 LENS DOUG DC9 DC915 3022036 WP AFT RAMP LOOSE A GRAA K NONE O OTHER IN INSP/MAINT 1 WP 11 1070T 45784 WHILE AT C-CHECK AT ROW, MAINTENANCE DISCOVERED THAT THE EMERGENCY LIGHTS ON THE AFT ESCAPE RAMP, HAD THE FORWARD TWO LA MP LENS NOT SECURED. MAINTENANCE RESECURED THE LENS IAW DC-9 MM 33-53-00. MAINTENANCE PERFORMED AN OPERATION INSPECTIO N OF THE EMERGENCY PATH LIGHT SYSTEM. NO DEFECTS NOTED, OPERATIONAL CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 1996090500466 19960905 00466 WP 1996 9 5 GRAA9645 1 19960702 A 3350 0816300609 TRACK LIGHT DOUG DC9 DC915 3022036 WP CABIN LOOSE A GRAA K NONE L NO TEST IN INSP/MAINT 1 WP 11 1070T 45784 LINE MAINTENANCE AT RNO, DISCOVERED EMERGENCY FLOOR TRACK AT ROW 1 LOOSE. MAINTENANCE SECURED THE EMERGENCY FLOOR TRACK . MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY FLOOR LIGHT SYSTEM. NO DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1996090500467 19960905 00467 WP 1996 9 5 GRAA9646 1 19960702 A 3350 363634 LAMP DOUG DC9 DC915 3022036 WP CABIN LOOSE A GRAA K NONE L NO TEST IN INSP/MAINT 1 WP 11 1070T 45784 LINE MAINTENANCE AT RNO, DISCOVERED THAT THE EMERGENCY FLOOR LIGHT BESIDE ROW 6, WAS INOPERATIVE. MAINTENANCE RESECURED THE LAMP. AN OPERATIONAL CHECK OF THE EMERGENCY FLOOR LIGHT SYSTEM WAS PERFORMED. NO DEFECTS WERE NOTED. OPERATIONAL LY CHECKED NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1996090500468 19960905 00468 WP 1996 9 5 GRAA9647 1 19960705 A 3350 EA1D131DE BATTERIES DOUG DC9 DC915 3022036 WP CABIN DISCHARGED A GRAA K NONE L NO TEST IN INSP/MAINT 1 WP 11 1068T 45782 LINE MAINTENANCE AT RNO, DISCOVERED THAT THE CENTER AISLE EMERGENCY FLOOR PATH LIGHT WERE INOPERATIVE AT ROWS 14-18. MA INTENANCE CHARGED THE EMERGENCY FLOOR LIGHT ON AC POWER. MAINTENANCE PERFORMED AND OPERATIONAL CHECK OF THE SYSTEM, NO DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1996090500469 19960905 00469 WP 1996 9 5 HALA96109 1 19960811 A 7830 TR UNIT DOUG DC9 DC951 3022051 WP NR 2 ENGINE INOPERATIVE A HALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 601AP 47658 HNL - FLT 108 - RIGHT ENGINE REVERSE UN-LOCK LIGHT CAME ON AFTER GEAR RETRACTION. RETURNED TO HNL FOR LANDING. LIGHT W ENT OUT AFTER LANDING. PLACARD NR 2 REVERSE INOP. LOCKED OUT REVERSER AND DMI NR 98226 ISSUED. ITEM ENTERED ON 1414. (M) 2 L 7 2 4F A6WE 1996090500470 19960905 00470 WP 1996 9 5 HALA96110 1 19960812 A 5610 5887275501 WINDSHIELD DOUG DC9 DC951 3022051 WP CTR COCKPIT CRACKED A HALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 13 699HA B03422122 47763 HNL - FLT 102 - IN FLIGHT CENTER WINDSHIELD ARCING AND CRACKING FROM HEATING ELEMENT. WINDSHIELD BURNED AND UN-SERVICEA BLE. RETURNED TO HNL. REMOVED AND REPLACED THE CENTER WINDSHIELD PER MM 56-10-1. (M) 2 L 7 2 4F A6WE 1996090500471 19960905 00471 WP 1996 9 5 HALA96111 1 19960811 A 3350 P4010049 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 699HA 6993 47763 HNL - FOUND FORWARD EMERGENCY LIGHT INOP FLOOR. REPLACED FORWARD BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1996090500472 19960905 00472 WP 1996 9 5 HALA96112 1 19960811 A 3350 BATTERY DOUG DC10 DC1010 3022110 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 153AA 46708 FLT NR 4 - HNL - FOUND EMERGENCY FLOOR PATH LIGHTING ON RIGHT SIDE OF AIRCRAFT ON. SELECTOR SWITCH IN OFF POSITION. RE POSITIONED SEAT LIGHT CONNECTOR AT ROW 1H. OPERATIONAL CHECK OK. REPLACED LOW BATTERIES. (M) 2 L 7 3 4F A22WE 1996090500473 19960905 00473 WP 1996 9 5 HALA96114 1 19960730 A 5711 SPAR DOUG DC9 DC951 3022051 WP WS 129 CORROSION A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 679HA 47662 HNL - FOUND SEVERE CORROSION ON AFT SIDE OF REAR SPAR, LOWER FLANGE AT APPROX STATION 129. REPAIRED PER DACO TELEX SVC- HNL-0092/PPS. (M) 2 L 7 2 4F A6WE 1996090500474 19960905 00474 WP 1996 9 5 HALA96115 1 19960817 A 3350 CONNECTOR DOUG DC10 DC1010 3022110 WP CABIN BROKEN A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 161AA 46942 HNL - MAINTENANCE ENTRY FOUND THE FLOOR PATH LIGHTING AT 33G TERMINAL BROKEN. REPLACED THE EMERGENCY EGRESS LIGHT RIBBO N CABLE CONNECTOR. THE OPERATIONAL CHECK WAS OK. (M) 2 L 7 3 4F A22WE 1996090500475 19960905 00475 WP 1996 9 5 HALA96116 1 19960814 A 5711 SPAR DOUG DC9 DC951 3022051 WP WS 414 CORROSION A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 679HA 47662 HNL - FOUND EXFOLIATION CORROSION ON REAR SPAR AFT LOWER TANG AT STATION 414, LEVEL 2. REPAIRED PER SRM 57-09, FIG 11 A ND DACO TELEX SVC-HNL-0088/PPS. (M) 2 L 7 2 4F A6WE 1996090500476 19960905 00476 WP 1996 9 5 HALA96119 1 19960820 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 673MC 47726 HNL - FOUND AFT CABIN EMERGENCY LIGHTING INOP. REPLACED EMERGENCY LIGHT BATTERY. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1996090500477 19960905 00477 WP 1996 9 5 HALA96120 1 19960821 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 699HA 47763 HNL - FLT 508 - FOUND EMERGENCY EGRESS FLOOR LIGHTS, AFT CABIN DIM. REPLACED AFT FLOOR BATTERY PACK. OPS CHECK OK. (M ) 2 L 7 2 4F A6WE 1996090500478 19960905 00478 WP 1996 9 5 HALA96121 1 19960820 A 3244 TIRES DOUG DC9 DC951 3022051 WP NLG SHIMMY A HALA C D ABORTED TAKEOFF RETURN TO BLOCK E VIBRATION/BUFFET TO TAKEOFF 1 WP 13 699HA 47763 FLT 512 - HNL - NOSE WHEEL SHIMMY DURING TAKEOFF ROLL, ABORTED TAKEOFF AND RETURNED TO GATE. REPLACED NLG TIRES, SPIN C HECK OK. LUBED NLG STRUT AND STEERING MECHANISM AND SECURED SPLASH GUARD MOUNTS. CONDITION AND SECURITY CHECK OK. OK FOR SERVICE. (M) 2 L 7 2 4F A6WE 1996090500479 19960905 00479 NM 1996 9 5 HNAA9693457 1 19960814 A 3350 6013211X POWER SUPPLY GRIMES DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 934HA 12317 JAX036 139 FLT 3451 - TPA-JAX - DURING PREFLIGHT CHECKS, FOUND THE CENTER AISLE AFT EMERGENCY FLOOR LIGHT INOP. REMOVED AND REPLAC ED THE BULB, NO FIX. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY 3351-PS3. (M) 2 H 7 2 4T RT A13NM 1996090500480 19960905 00480 NM 1996 9 5 IXKA9600063 1 19960728 A 3222 AN622723 SEAL BOEING 727 727251 138408H NM NLG LEAKING A IXKA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 25 264US 8696 19983 FLT 32 - MDW - AIR TURN BACK - UNABLE TO GET NOSE DOOR LIGHT TO GO OUT ON RETRACTION. BOTH RED LIGHT AND AMBER LIGHTS O N. FOUND NOSE GEAR METERING PIN ORIFICE SEALS BAD, STRUT FLAT, TIRES HANGING UP ON DOORS. REMOVED AND REPLACED SEALS I AW 32-21-01 SWUNG NOSE GEAR IAW 32-61-0. OPS CHECK OK. (M) 2 L 7 3 4F A3WE 1996090500481 19960905 00481 WP 1996 9 5 IXXA96122 1 19960705 A 2450 ELECTRICAL DOUG DC8 DC871 302199A WP COCKPIT ODOR A IXXA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 11 829BX 45994 DURING TAXI IN AT IRD, CREW NOTED A FAINT ACID LIKE SMELL AROUND CIRCUIT BREAKER PANEL. ON GROUND MAINTENANCE POWERED A LL EQUIPMENT, NO ACID LIKE SMELL NOTED. (M) 2 L 7 4 4F 4A25 1996090500482 19960905 00482 WP 1996 9 5 IXXA96124 1 19960707 A 7711 PT2 SYSTEM DOUG DC8 DC862 3021970 WP NR 1/2 CONTAMINATED A IXXA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 SW 11 31CX 5241 45911 ON TAKEOFF FROM COF, NR 3 AND NR 4 ENGINE PRESSURE RATIO INDICATION SYSTEMS READ HIGH COMPARED TO N1 AND THE NR 1 AND NR 2 ENGINES. THE FLIGHT ELECTED TO RETURN TO THE FIELD. MAINTENANCE REMOVED INSECT DEBRIS FROM BOTH ENGINE PT2 SYSTEMS, ACCOMPLISHED A HIGH POWER ENGINE RUN SUCCESSFULLY AND RELEASED THE AIRCRAFT BACK TO SERVICE. (M) 2 L 7 4 4F 4A25 1996090500483 19960905 00483 WP 1996 9 5 IXXA96125 1 19960809 A 2760 37195962 CRANK ASSEMBLY DOUG DC8 DC871 302199A WP RT SPOILER BROKEN A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 823BX 5797 46064 DURING ROUTINE PRFLIGHT INSPECTION AND INVESTIGATION OF A RELATED PROBLEM, MAINTENANCE REPLACED THE SPOILER CRANKS AND R IGGED THE SYSTEM IAW DOUGLAS MM 27-60-0. (M) 2 L 7 4 4F 4A25 1996090500484 19960905 00484 WP 1996 9 5 IXXA96126 1 19960610 A 7931 6018011 OIL PRESS LINE DOUG DC8 DC861 3021952 WP NR 2 ENGINE FAILED A IXXA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 11 861PL 45964 DURING CLIMB-OUT FROM SLC, THE NR 2 ENGINE OIL QUANTITY INDICATION STARTED DECREASNG AND THEN RAPIDLY ROSE TO FULL. CON TINUED OBSERVATION NOTED THE OIL PRESSURE STARTING TO FLUCTUATE ACCOMPANIED BY A FLICKERING OIL PRESSURE LIGHT. THE ENG INE WAS PRECAUTIONARILY SHUT DOWN. THE FLIGHT RETURNED TO SLC. GROUND INSPECTION OF THE ENGINE FOUND A RUPTURED OIL PR ESSURE LINE WHICH MAINTENANCE REPLACED. MAINTENANCE ACCOMPLISHED A LEAK CHECK DURING THE GROUND RUN AND RELEASED THE AI RCRAFT TO SERVICE. (M) 2 L 7 4 4F 4A25 1996090500485 19960905 00485 NE 1996 9 5 IXXA96127 2 19960813 A 7261 377765 SCAVENGE DOUG DC8 DC861 3021952 WP PWA JT3D JT3D3B 52039 NE NR 2 ENG OUT OF POSITION A A IXXA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 11 861PL 45964 669525 EN ROUTE FROM DAY-SLC, THE NR 2 ENGINE OIL QUANTITY DROPPED TO 4 GALLONS AND RECOVERED TO NORMAL LEVEL ACCOMPANIED BY AN OIL PRESSURE LIGHT AND OIL PRESSURE FLUCTUATION. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT DIVERTED TO STL. MAINTENAN CE FOUND THE DIFFUSER OIL SCAVENGE TUBE FOR THE NR 4, 4.5, 5 AND 6 BEARINGS DISLOCATED FROM ITS SEAL. THE ENGINE REQUIR ED REPLACEMENT PRIOR TO RETURN TO SERVICE. (M) 2 L 7 4 4F 4 F 4A25 1E8 1996090500486 19960905 00486 WP 1996 9 5 IXXA96128 1 19960814 A 3234 GEAR HANDLE DOUG DC8 DC871 302199A WP COCKPIT LACK OF LUBE A IXXA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 SW 11 829BX 76319 45994 ON APPROACH TO TOL, WHEN LOWERING LANDING GEAR, INDICATION SYSTEM DID NOT INDICATE DOWN FOR ALL THREE GEAR. THE GEAR WA S CYCLED AND THE INDICATION WAS NORMAL FOR ALL THREE GEAR. MAINTENANCE CLEANED AND LUBED THE GEAR HANDLE MECHANISM AND CLEANED THE HANDLE DETENT SWITCHES. SYSTEM WAS GROUND CHECKED SUCCESSFULLY IAW WITH THE DOUGLAS MM 32-60-0. (M) 2 L 7 4 4F 4A25 1996090500487 19960905 00487 EU 1996 9 5 RAIA960721 1 19960723 A 2612 51653151 FIRE CONTL RELAY BAG JETSTM JETSTM3201 1500217 EU NR 2 ENGINE FAILED A RAIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 339TE 8865 935 JLN - FLT 7077 - NR 2 ENGINE FIRE WARNING DURING TAXI. REPLACED FIRE CONTROL RELAY. (M) 2 L 7 2 4T RT A56EU 1996090500488 19960905 00488 EU 1996 9 5 RAIA960722 1 19960723 A 7332 1241012 TRANSMITTER BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP NR 2 ENGINE INOP A RAIA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 CE 03 436AM 11147 891 66086 STL - FLT 7320 - RIGHT ENGINE FUEL PRESSURE INDICATES 16 PSI. REPLACED FUEL PRESSURE TRANSMITTER. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996090500489 19960905 00489 EU 1996 9 5 RAIA960723 1 19960724 A 3244 TIRE AEROSP ATR72 ATR72202 8680940 EU NLG OUT OF ROUND A RAIA A UNSCHED LANDING E VIBRATION/BUFFET TO TAKEOFF 1 CE 03 721TE 217 SGF - FLT 7014 - NOSE WHEEL (AH54774) VIBRATION ON TAKEOFF. REPLACE NOSE TIRES. (M) 2 H 7 2 4T RT A53EU 1996090500490 19960905 00490 1996 9 5 RAIA960724 4 19960725 A 6122 8975481 SCREW BAG JETSTM JETSTM3201 1500217 EU LT PROP GOV OUT OF ADJUST A RAIA A UNSCHED LANDING O OTHER TO TAKEOFF 1 CE 03 423AM 10416 858 STL - FLT 7508 - LEFT ENGINE WOULD NOT PRODUCE TARGET TORQUE, RPM 103 PERCENT. ADJUSTED PROP GOVERNOR HIGH STOP (SCREW X). (M) 2 L 7 2 4T RT A56EU 1996090500491 19960905 00491 EU 1996 9 5 RAIA960725 1 19960713 A 5347 S53375001 SEAT TRACK AEROSP ATR72 ATR72202 8680940 EU CABIN CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 721TE 11026 217 FOUND LEFT AND RIGHT SEAT TRACK HAS CORROSION AT FRAME 34 AND 36 TO 39. REPLACE SEAT TRACK IN EFFECTED AREA AS PER SRM. (M) 2 H 7 2 4T RT A53EU 1996090500492 19960905 00492 EU 1996 9 5 RAIA960726 1 19960713 A 5315 S5367241000662 FLOOR BEAM AEROSP ATR72 ATR72202 8680940 EU CABIN CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 721TE 11026 217 FOUND FLOOR BEAM 41 HAS CORROSION FROM STRINGER 17 TO 21. REMOVED AND REPLACED CORRODED SECTION OF BEAM PER SRM. (M) 2 H 7 2 4T RT A53EU 1996090500493 19960905 00493 EU 1996 9 5 RAIA960727 1 19960713 A 5320 S5367241021401 ANGLE AEROSP ATR72 ATR72202 8680940 EU CABIN CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 721TE 11026 217 FOUND FRAME 41 SKIN CLIP HAS CORROSION AT FLOOR LEVEL. REMOVED AND REPLACED CORRODED SKIN CLIP PER SRM. (M) 2 H 7 2 4T RT A53EU 1996090500494 19960905 00494 EU 1996 9 5 RAIA960728 1 19960713 A 5320 S5367121828001 FLOOR WEB AEROSP ATR72 ATR72202 8680940 EU CABIN CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 721TE 11026 217 FOUND FLOOR WEB AT AFT SERVICE DOOR HAS CORROSION. REMOVED AND REPLACED WEB PER SRM. (M) 2 H 7 2 4T RT A53EU 1996090500495 19960905 00495 EU 1996 9 5 RAIA960729 1 19960713 A 5320 S5367131820001 FLOOR WEB AEROSP ATR72 ATR72202 8680940 EU CABIN CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 721TE 11026 217 FOUND FLOOR WEB RIGHT FROM FRAME 39 TO 41 HAS CORROSION. REMOVED AND REPLACED WEB PER SRM. (M) 2 H 7 2 4T RT A53EU 1996090500496 19960905 00496 EU 1996 9 5 RAIA960730 1 19960713 A 5320 S5367140400000 PANEL AEROSP ATR72 ATR72202 8680940 EU CABIN CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 721TE 217 FOUND LAVATORY SUPPORT PANEL HAS CORROSION. CLEANED AND REMOVED CORROSION AND REPAINTED PER SRM. (M) 2 H 7 2 4T RT A53EU 1996090500497 19960905 00497 EU 1996 9 5 RAIA960731 1 19960713 A 5320 S5367240920201 ANGLE AEROSP ATR72 ATR72202 8680940 EU CABIN CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 721TE 11026 217 FOUND FAIL/SAFE ANGLE AT FRAME 40 HAS CORROSION. REMOVED CORRODED SECTION AND REPLACED PER SRM. (M) 2 H 7 2 4T RT A53EU 1996090500498 19960905 00498 EU 1996 9 5 RAIA960732 1 19960713 A 5315 S5367210820201 FLOOR BEAM AEROSP ATR72 ATR72202 8680940 EU CABIN CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 721TE 11026 217 FOUND FLOOR BEAM 39 HAS CORROSION. REMOVED CORROSION AND REPAIRED FLOOR BEAM PER SRM. (M) 2 H 7 2 4T RT A53EU 1996090500499 19960905 00499 EU 1996 9 5 RAIA960733 1 19960713 A 5320 S5367800824402 BRACE AEROSP ATR72 ATR72202 8680940 EU CABIN CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 721TE 11026 217 FOUND BRACE BETWEEN BEAM 39 AND 40 HAS CORROSION. REMOVED AND REPLACED BRACE. (M) 2 H 7 2 4T RT A53EU 1996090500500 19960905 00500 EU 1996 9 5 RAIA960734 1 19960713 A 5320 S5367121720402 FLOOR WEB AEROSP ATR72 ATR72202 8680940 EU CABIN CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 721TE 217 FOUND FLOOR WEB AT PASSENGER DOOR HAS CORROSION. REMOVED AND REPLACED FLOOR WEB. (M) 2 H 7 2 4T RT A53EU 1996090500501 19960905 00501 EU 1996 9 5 RAIA960735 1 19960713 A 5315 S536720720201 FLOOR BEAM AEROSP ATR72 ATR72202 8680940 EU CABIN CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 721TE 11026 217 FOUND FLOOR BEAM 38 DOOR HAS CORROSION. REMOVED CORROSION AND REPAIRED PER SRM. (M) 2 H 7 2 4T RT A53EU 1996090500502 19960905 00502 EU 1996 9 5 RAIA960736 1 19960713 A 5311 S5367240600863 FRAME AEROSP ATR72 ATR72202 8680940 EU CABIN CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 721TE 11026 217 FOUND FRAME 36 DOOR HAS CORROSION FROM STRINGER 14 TO 15. REMOVED CORROSION AND REPAIRED PER SRM. (M) 2 H 7 2 4T RT A53EU 1996090500503 19960905 00503 EU 1996 9 5 RAIA960737 1 19960713 A 5313 S53671200218 STRINGER AEROSP ATR72 ATR72202 8680940 EU CABIN CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 721TE 11026 217 FOUND STRINGER 17R HAS CORROSION BETWEEN FRAME 24 AND 30, 33 AND 40. REMOVED CORROSION AND REPAIRED PER SRM. (M) 2 H 7 2 4T RT A53EU 1996090500504 19960905 00504 EU 1996 9 5 RAIA960738 1 19960713 A 5311 S5367240700460 FRAME AEROSP ATR72 ATR72202 8680940 EU CABIN CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 721TE 217 FOUND FRAME 37 DOOR HAS CORROSION FROM STRINGER 14 TO 15. REMOVED CORROSION AND REPAIRED PER SRM. (M) 2 H 7 2 4T RT A53EU 1996090500505 19960905 00505 EU 1996 9 5 RAIA960739 1 19960713 A 5313 S53671300218 STRINGER AEROSP ATR72 ATR72202 8680940 EU CABIN CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 721TE 11026 217 FOUND STRINGER 16R HAS CORROSION FROM FRAME 35 TO 36. REMOVED CORROSION AND REPAIRED PER SRM. (M) 2 H 7 2 4T RT A53EU 1996090500506 19960905 00506 EU 1996 9 5 RAIA960740 1 19960713 A 5313 S53671200286 STRINGER AEROSP ATR72 ATR72202 8680940 EU CABIN CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 721TE 11026 217 FOUND STRINGER 17L HAS CORROSION BETWEEN FRAME 35 AND 36. CLEANED AND FOUND WITHIN SRM LIMITS. CLEANED TREATED AND REP AINTED PER SRM. (M) 2 H 7 2 4T RT A53EU 1996090500507 19960905 00507 EU 1996 9 5 RAIA960741 1 19960713 A 5313 S53671407210212 STRINGER AEROSP ATR72 ATR72202 8680940 EU CABIN CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 721TE 11026 217 FOUND STRINGER 21R HAS CORROSION AT FRAME 39. REMOVED CORROSION AND REPAIRED PER SRM. (M) 2 H 7 2 4T RT A53EU 1996090500508 19960905 00508 EU 1996 9 5 RAIA960816 1 19960813 A 3260 9005EN38 UPLOCK SWITCH BAG JETSTM JETSTM3201 1500217 EU NOSE GEAR FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 342TE 954 PAH - FLT 7365 - NOSE INTRANSIT LIGHT ILLUMINATED AFTER TAKEOFF. MAINTENANCE REPLACED THE NOSE GEAR UPLOCK SWITCH. PER FORMED GEAR SWING, OPS CHECK GOOD. (M) 2 L 7 2 4T RT A56EU 1996090500509 19960905 00509 EU 1996 9 5 RAIA960817 1 19960814 A 2611 72111211000 SMOKE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU BAG COMPT DIRTY A RAIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 03 561HK 1299 41077 JFK - FLT 7749 - POD SMOKE CAME ON DURING FLIGHT. MAINTENANCE FOUND OLIVE OIL SPILLED IN THE BAGGAGE POD. CLEANED OLIV E OIL FROM SMOKE DETECTOR. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A41NM 1996090500510 19960905 00510 EU 1996 9 5 RAIA960818 1 19960815 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 EICBF 176 STL - FLT 7400 - EMERGENCY EXIT SIGN OVER FORWARD CABIN DOOR AND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. MAINTENANC E REPLACED THE EMERGENCY LIGHT BATTERY PACK. (M) 2 H 7 2 4T RT A53EU 1996090500511 19960905 00511 EU 1996 9 5 RAIA960819 1 19960815 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 424TE 124 STL - AFT PORTION OF THE EMERGENCY ESCAPE PATH LIGHTING INOP. MAINTENANCE REPLACED THE AFT EMERGENCY LIGHT BATTERY PACK . (M) 2 H 7 2 4T RT A53EU 1996090500512 19960905 00512 WP 1996 9 5 RAIA960820 2 19960815 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LEFT MALFUNCTIONED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 866AE 10558 866 P66074 ONT - FLT 4771 - LEFT ENGINE DID NOT ACHIEVE TARGET TORQUE. MAINTENANCE REPLACED THE LEFT ENGINE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996090500513 19960905 00513 1996 9 5 RAIA960821 3 19960816 A 6140 8659566 BETA SWITCH BAG JETSTM JETSTM3201 1500217 EU RT ENGINE STUCK A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 430AM 8218 3053 880 STL - FLT 7420 - RIGHT BETA LIGHT ILLUMINATED, AND WOULD NOT EXTINGUISH. MAINTENANCE REPLACED THE RIGHT BETA SWITCH. ( M) 2 L 7 2 4T RT A56EU 1996090500514 19960905 00514 EU 1996 9 5 RAIA960822 1 19960818 A 7332 41SG107100G14 FUEL PRESS TRANS BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RT ENGINE ERRATIC A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 338TE 932 P66169 STL - FLT 7324 - RIGHT FUEL PRESSURE INDICATION FLUCTUATED. MAINTENANCE REPLACED THE RIGHT FUEL PRESSURE TRANSDUCER. ( M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996090500515 19960905 00515 CE 1996 9 5 S2YA960020 1 19960729 A 2612 70522 FIRE LOOP BEECH 1900 1900D 1154162 CE LT ENGINE SHORTED A S2YA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 GL 13 85SK 5850 UE85 THE CREW OF FLT NR 1077.3 GRB-MKE - LANDED IN MKE AND DURING TAXI TO THE GATE THEY NOTICED THE LEFT FIRE WARNING T-HANDL E ANNUNCIATOR LIGHTS FLICKERED AND THEN STAYED 'ON'. THE CREW STOPPED THE AIRCRAFT, PROCEEDED TO BLOW THE FIRE BOTTLE A ND DEBOARDED THE AIRCRAFT VIA THE AIRSTAIR DOOR AS A PRECAUTION. MAINTENANCE REPLACED THE LEFT ENGINE AFT FIRE LOOP TO FIX THE PROBLEM. (M) 2 L 7 2 4T RT A24CE 1996090500516 19960905 00516 CE 1996 9 5 S2YA960021 1 19960730 A 5270 TERMINAL BEECH 1900 1900D 1154162 CE CARGO DOOR LOOSE A S2YA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 13 145SK UE145 AFTER THE FLIGHT CREW DEPARTED MKE ON FLT NR 1157 FOR MSN, FOUND THAT THE CARGO DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT A ND DECIDED TO RETURN TO MKE, MEL'D THE CARGO DOOR ANNUNCIATOR SYSTEM 52-2 CAT C. MAINTENANCE LATER FOUND A LOOSE TERMIN AL SCREW ON A MICROSWITCH, TIGHTENED IT AND OPERATIONAL CHECKED NUMEROUS TIMES. (M) 2 L 7 2 4T RT A24CE 1996090500517 19960905 00517 SO 1996 9 5 SRAA960801 1 19960804 A 7500 B-NUT LKHEED 382 382E 526413U SO ALLSN 501D 501D22A 03006 GL NR 2 ENG BLEED LOOSE A SRAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 923SJ 4301 AFTER TAXIING OUT FOR FLIGHT 1206 FROM HOW, NR 2 ENGINE NACELLE OVERHEAT WARNING LIGHT CAME ON. SHUT DOWN ENGINE AND RE TURNED TO BLOCK. FOUND LOOSE 'B' NUT ON NR 2 ENGINE. PERFORMED ENGINE RUN, SYSTEM OPS CHECKED GOOD PER MM CH 75. (M) 2 H 7 4 4T 4 T A1SO E282 1996090500518 19960905 00518 NM 1996 9 5 TAOA089601 1 19960806 A 3350 900835A BATTERY PCK BOEING 727 727225 1384077 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 918TS VA4695 20445 FORWARD ENTRY AISLE EMERGENCY SIGN INOP. REPLACED BATTERY PACK AND CHARGER ASSEMBLY. (M) 2 L 7 3 4F A3WE 1996090500519 19960905 00519 NM 1996 9 5 TWRA96214 1 19960726 A 3350 1317 BULB BOEING 747 747282B 1384860 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 611FF 20502 DURING DAILY CHECK, FOUND RIGHT OUTSIDE LOWER MOST EMERGENCY LIGHT INOP. RELAMPED, OPS CHECK GOOD, PER MM 33-51-00. (M ) 2 L 7 4 4F A20WE 1996090500520 19960905 00520 NM 1996 9 5 TWRA96215 1 19960727 A 3397 WIRE BOEING 747 747282B 1384860 NM GALLEY INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 611FF 20502 DURING DAILY CHECK, FOUND FLOOR EVAC EGRESS LIGHT STRIP AT 'E' GALLEY INOP. REPAIRED HARNESS, OPS CHECKED OK PER MM 33- 51-00. (M) 2 L 7 4 4F A20WE 1996090500521 19960905 00521 NM 1996 9 5 TWRA96217 1 19960727 A 3350 CONNECTOR BOEING 747 747282B 1384860 NM CABIN LOOSE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 611FF 20502 DURING DAILY CHECK, FOUND FLOOR EVAC EGRESS LIGHT STRIP INOP AT SEAT 35C. FOUND CONNECTOR LOOSE, RE-SEATED AND SECURED. OPS CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996090500522 19960905 00522 NM 1996 9 5 TWRA96218 1 19960724 A 3350 ML7715 BULB BOEING 747 747212B 1384886 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURNG DAILY CHECK, FOUND SEAT 28C FLOOR EVAC LIGHT INOP AND ALSO, LENS COVER MISSING. RELAMPED AND REPLACED LENS. OPS CHECKED OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996090500523 19960905 00523 NM 1996 9 5 TWRA96220 1 19960724 A 3350 08688 SOCKET BOEING 747 747212B 1384886 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND FLOOR EVAC LIGHT AND LENS MISSING AT 53ABC. REPLACED SOCKET, BULB AND LENS. OPS CHECKED GOOD PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996090500524 19960905 00524 NM 1996 9 5 TWRA96221 1 19960724 A 3350 07912 LENS BOEING 747 747212B 1384886 NM CABIN MISSING A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND FLOOR EVAC LIGHT AND LENS MISSING AT 11ABC, 14ABC, 28ABC, 50KJH. REPLACED LENS AND BULB. OPS CHECKED OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996090500526 19960905 00526 NM 1996 9 5 TWRA96229 1 19960724 A 3350 276001 FUSE BOEING 747 747238B 1384828 NM CEILING BLOWN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 614FF 20534 DURING DAILY CHECK, FOUND LEFT AFT LAV CEILING EVAC LIGHT INOP. REPLACED FUSE. OPS CHECKED OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996090500527 19960905 00527 NM 1996 9 5 TWRA96230 1 19960724 A 3350 S1356B37 LIGHT BOEING 747 747238B 1384828 NM CEILING INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 614FF 20534 DURING DAILY CHECK, FOUND SEAT 50KHJ AREA CEILING EVAC LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY. OPS CHECK NORMAL P ER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996090500528 19960905 00528 NM 1996 9 5 TWRA96231 1 19960724 A 3397 WIRE BOEING 747 747238B 1384828 NM CABIN BROKEN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 614FF 20534 DURING DAILY CHECK, FOUND 1L DOOR JUMPSEAT EVAC LIGHT INOP. REPAIRED BROKEN WIRE 33-51-13. OPS CHECKED OK PER MM 33-51 -00. (M) 2 L 7 4 4F A20WE 1996090500529 19960905 00529 NM 1996 9 5 TWRA96232 1 19960724 A 3350 CM7715 BULB BOEING 747 747238B 1384828 NM CABIN MISSING A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 614FF 20534 DURING DAILY CHECK, FOUND SEAT 60C FLOOR EVAC LIGHT AND LENS COVER AREA MISSING. REPLACED BULB AND LENS. OPS CHECKED O K PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996090500530 19960905 00530 NM 1996 9 5 TWRA96233 1 19960724 A 3350 ML7715 BULB BOEING 747 747238B 1384828 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 614FF 20534 DURING DAILY CHECK, FOUND SEAT 1K FLOOR EVAC LIGHT INOP. RELAMPED, OPS CHECKED OK PER MM 31-51-00. (M) 2 L 7 4 4F A20WE 1996090500531 19960905 00531 NM 1996 9 5 TWRA96236 1 19960726 A 3350 ML7715 BULB BOEING 747 747212B 1384886 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND EMERGENCY EVAC LIGHT INOP AT 11 ABC, 14 ABC, 53 ABC, 58 ABC. RELAMPED, OPS CHECKED NORMAL AS PER 33-51-00. (M) 2 L 7 4 4F A20WE 1996090500532 19960905 00532 NM 1996 9 5 TWRA96237 1 19960727 A 3350 276001 FUSE BOEING 747 747212B 1384886 NM CABIN BLOWN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND A-ZONE EXIT SIGN AT AISLE ABOVE SEAT 6KH IS INOP. REPLACED FUSE, OPS CHECKED NORMAL AS PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996090500533 19960905 00533 NM 1996 9 5 TWRA96238 1 19960729 A 3350 S1356B37 BATTERY PACK BOEING 747 747212B 1384886 NM CABIN DISCHARGED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 620FF 21162 DURING DAILY CHECK, FOUND 51H CEILING EMERGENCY LIGHT IS INOP. REPLACED EMERGENCY LIGHT BATTERY PACK. OPS CHECKED NORM AL AS PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996090500534 19960905 00534 NM 1996 9 5 TWRA96239 1 19960727 A 3350 363781 LIGHT BOEING 747 747136 1384883 NM STAIRCASE FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 606FF 20273 DURING DAILY CHECK, FOUND A-ZONE LEFT FLOOR EVAC LIGHTS DIM. FOUND LIGHT STRIP AT FAULT. REMOVED AND REPLACED LIGHT ST RIP AT STAIRCASE. SYSTEM OPS CHECKED NORMAL AS PER MM 33-51-00 PG 501. (M) 2 L 7 4 4F A20WE 1996090500535 19960905 00535 NM 1996 9 5 TWRA96240 1 19960727 A 3350 90063 BATTERY CHARGER BOEING 747 747136 1384883 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 606FF P1818 20273 DURING DAILY CHECK, FOUND 3L MED EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY CHARGER. SYSTEM OPS CHECKED NO RMAL AS PER MM 33-51-00 PG 501. (M) 2 L 7 4 4F A20WE 1996090500536 19960905 00536 NM 1996 9 5 TWRA96241 1 19960727 A 3350 ML7715 BULB BOEING 747 747238B 1384828 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 607PE 20011 DURING DAILY CHECK, FOUND FLOOR EMERGENCY EVAC LIGHT INOP AT 3C 21H, 60H. REPLACED BULB AND LENS. OPS CHECKED NORMAL A S PER MM 33-51-00 PG 501. (M) 2 L 7 4 4F A20WE 1996090500538 19960905 00538 NM 1996 9 5 TWRA96243 1 19960729 A 3350 07912 LENS BOEING 747 747238B 1384828 NM CABIN MISSING A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 614FF 20534 DURING DAILY CHECK, FOUND FLOOR EMERGENCY LIGHT INOP AT 4H, 42C, 45C AND 50 C. REPLACED LENS AND BULB. OPS CHECKED NOR MAL AS PER MM 33-51-00 PG 501. (M) 2 L 7 4 4F A20WE 1996090500539 19960905 00539 NM 1996 9 5 TWRA96244 1 19960729 A 3350 07912 LENS BOEING 747 747238B 1384828 NM CABIN MISSING A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 614FF 20534 DURING DAILY CHECK, FOUND UPPER DECK AFT OF 73K, FLOOR EMERGENCY LIGHT INOP. REPLACED EMERGENCY LIGHT LENS AND BULB. O PS CHECKED OK PER MM 33-51-00 PG 501. (M) 2 L 7 4 4F A20WE 1996090500540 19960905 00540 NM 1996 9 5 TWRA96245 1 19960727 A 3350 276001 FUSE BOEING 747 747130 1384880 NM CABIN BLOWN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 603FF 19746 DURING DAILY CHECK, FOUND NR 1 LEFT MED UPPER DOOR SILL FORWARD EVAC LIGHT INOP. REPLACED FUSE ON BATTERY PACK. PERFOR MED OPS CHECK PER MM 33-51-00 PG 501, OPS CHECKED NORMAL. (M) 2 L 7 4 4F A20WE 1996090500541 19960905 00541 NM 1996 9 5 TWRA96246 1 19960730 A 3350 MIL72661 BULB BOEING 747 747212B 1384886 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND 60H, 52H FLOOR EMERGENCY LIGHTS ARE INOP. REPLACED BULB. OPS CHECKED NORMAL PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996090500542 19960905 00542 NM 1996 9 5 TWRA96247 1 19960730 A 3350 ML7715 BULB BOEING 747 747238B 1384828 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 614FF 20534 DURING DAILY CHECK, FOUND 38H FLOOR EMERGENCY LIGHT IS INOP. RELAMPED, OPS CHECKED OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996090500543 19960905 00543 NM 1996 9 5 TWRA96248 1 19960729 A 3350 BATTERY PACK BOEING 747 747212B 1384886 NM CABIN LOOSE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 620FF 21162 DURING DAILY CHECK, FOUND LEFT OVERWING NR 3 EMERGENCY LIGHT IS INOP. RESEATED PLUG ON BATTERY PACK. EMERGENCY LIGHT O PS CHECKED GOOD PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996090500544 19960905 00544 NM 1996 9 5 TWRA96265 1 19960807 A 3350 S1356B37 LIGHT BOEING 747 747212B 1384886 NM L1 DOOR INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 620FF 481 21162 DURING DAILY CHECK, FOUND L1 DOOR OVERHEAD EMERGENCY LIGHT INOP. RELAMPED L1 OVERHEAD EMERGENCY LIGHT ASSEMBLY. OPS CH ECKED OK PER MM 33-51-00 PG 501. (M) 2 L 7 4 4F A20WE 1996090500545 19960905 00545 NM 1996 9 5 TWRA96266 1 19960809 A 3350 BATTERY PACK BOEING 747 747212B 1384886 NM CABIN LOOSE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 619FF 21316 DURING DAILY CHECK, FOUND RIGHT WING NR 3 AND NR 4 OVERWING EMERGENCY LIGHT IS INOP. RESECURED LOOSE PLUG ON BATTERY PA CK. OPS CHECKED OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996090500546 19960905 00546 NM 1996 9 5 TWRA96267 1 19960808 A 3350 S1356B37 BATTERY PACK BOEING 747 747121 1384871 NM CABIN DISCHARGED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 609FF 20354 DURING DAILY CHECK, FOUND 3R DOOR UPPER EVAC LIGHT OUT. REMOVED AND REPLACED BATTERY PACK. OPS CHECKED OK AS PER MM 33 -51-00. (M) 2 L 7 4 4F A20WE 1996090500547 19960905 00547 1996 9 5 TWRA96268 4 19960810 A 2564 D30440703 SLIDE RAFT BOEING 747 747121 1384871 NM L2 DOOR DEPLOYED A TWRA K NONE O OTHER IN INSP/MAINT 1 EA 15 604FF 0384 19659 DURING B-CHECK, FOUND L2 DOOR WAS OPENED AFTER ARMING. SLIDE PARTIALLY DEPLOYED AND DOOR ASSIST BOTTLE FULLY DISCHARGED . REMOVED AND REPLACED ESCAPE SLIDE RAFT AND ACCESS ASSIST DOOR BOTTLE ON L2 DOOR AS PER MM 25-69-00. OPERATION CHECK NORMAL. (M) 2 L 7 4 4F A20WE 1996090500548 19960905 00548 NM 1996 9 5 TWRA96269 1 19960809 A 3350 58801 LIGHT BOEING 747 747282B 1384860 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 611FF 20502 DURING DAILY CHECK, FOUND 20H THROUGH 26H FLOOR EMERGENCY LIGHTS ARE INOP. REMOVED AND REPLACED EMERGENCY LIGHT STRIP 2 0H THROUGH 26H. OPS CHECKED NORMAL AS PER 33-51-00. (M) 2 L 7 4 4F A20WE 1996090500549 19960905 00549 NM 1996 9 5 TWRA96270 1 19960809 A 3350 58801 LIGHT BOEING 747 747282B 1384860 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 611FF 20502 DURING DAILY CHECK, FOUND NEAR NR 2 MED GALLEY FLOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT. OPS CHECKED NOR MAL AS PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996090500550 19960905 00550 NM 1996 9 5 TWRA96271 1 19960809 A 3350 58801 LIGHT BOEING 747 747282B 1384860 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 611FF 20502 DURING DAILY CHECK, FOUND NEAR NR 4L MED GALLEY FLOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT STRIP. OPS CHECKED NORMAL AS PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996090500551 19960905 00551 NM 1996 9 5 TWRA96272 1 19960814 A 2611 WIRE BOEING 747 747212B 1384886 NM R4 DOOR CHAFING A TWRA K NONE O OTHER IN INSP/MAINT 1 EA 15 616FF 21939 ON PREFLIGHT CHECK, FOUND ALL RIGHT SIDE LAVATORY SMOKE DETECTORS INOP. REPAIRED CHAFED WIRE AT PIN NR 5 AT R4 DOOR, AT TENDANT CONTROL PANEL. OPS CHECKED NORMAL PER MM 26-101-3. (M) 2 L 7 4 4F A20WE 1996090500552 19960905 00552 NM 1996 9 5 TWRA96273 1 19960814 A 3350 S1356B37 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 619FF 21316 DURING DAILY CHECK, FOUND L2 MED EMERGENCY LIGHT INOP. REPLACED EMERGENCY LIGHT ASSEMBLY. OPS CHECKED OK PER MM 33-51- 00. (M) 2 L 7 4 4F A20WE 1996090500553 19960905 00553 NM 1996 9 5 TWRA96274 1 19960814 A 3350 S1356B37 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 619FF 23623 21316 DURING DAILY CHECK, FOUND L4 MED EMERGENCY LIGHT INOP. REPLACED EMERGENCY LIGHT ASSEMBLY AT L4 DOOR. OPS CHECKED NORMA L AS PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996090500554 19960905 00554 NM 1996 9 5 TWRA96275 1 19960814 A 3350 S1356B37 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 616FF 1909270 21939 DURING DAILY CHECK, FOUND 11C CEILING EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT ASSY. OPS CHECKED NOR MAL PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996090500555 19960905 00555 NM 1996 9 5 USAA960548 1 19960812 A 5347 FLOOR TRACK BOEING 737 737301 1384611 NM BS 360-520 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 585US 27699 23930 CLT - INSPECTION VISUALLY FOUND LEVEL 2 40 INCH CORROSION RANDOM TOP RAIL SURFACES, LOCATED BETWEEN BS 360 - BS 520, RBL 45, REPLACED 40 INCH SECTION FOR FLOOR TRACK AS PER BOEING SRM 53-00-52 FIG 202. (M) 2 L 7 2 4F RT A16WE 1996090500556 19960905 00556 WP 1996 9 5 USAA960549 1 19960813 A 5315 991556171 FLOOR BEAM DOUG DC9 DC931 3022065 WP BS 996 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 965VJ 67851 47374 PIT - DURING Q-4 CHECK, FOUND .5 INCH BY 10 INCH CORRODED AREA AT UPPER AND LOWER SURFACES 'T' CAP FLOOR BEAM 996 LEFT. SPLICED IN NEW 'T' ANGLE PER TYPICAL REPAIR 53-10-14. (M) 2 L 7 2 4F A6WE 1996090500557 19960905 00557 WP 1996 9 5 USAA960550 1 19960813 A 5320 593226139 CUSP DOUG DC9 DC931 3022065 WP BS 965 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 965VJ 67851 47374 PIT - DURING Q-4 CHECK, FOUND 5 INCH LONG CRACK FORWARD OF STATION 965, OUTBOARD OF LEFT OUTBOARD SEAT TRACK, CUSP MEMBR ANE. REPLACED MEMBRANE SECTION WITH 7075T6 .020 PER SRM 53-11-03 FIG 11A. (M) 2 L 7 2 4F A6WE 1996090500558 19960905 00558 WP 1996 9 5 USAA960551 1 19960813 A 5330 SKIN DOUG DC9 DC931 3022065 WP FS 266/304 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 965VJ 67851 47374 PIT - DURING Q-4 CHECK, FOUND SKIN CORROSION UNDER NR 1 ADF ANTENNA, NR 2 ADF ANTENNA AT FS 266 AND FS 304 BETWEEN LONG ERON L2 AND 1. REPAIR SECTION OF SKIN PER EA 33228. (M) 2 L 7 2 4F A6WE 1996090500559 19960905 00559 WP 1996 9 5 USAA960552 1 19960813 A 5330 SKIN DOUG DC9 DC931 3022065 WP CARGO DOOR JAMB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 965VJ 67851 47374 PIT - DURING Q-4 CHECK, FOUND .5 INCH CRACK IN SKIN AT AFT LOWER CORNER OF FORWARD CARGO DOOR JAMB. INSTALLED DOUBLERS PER SRO 9530117. (M) 2 L 7 2 4F A6WE 1996090500560 19960905 00560 WP 1996 9 5 USAA960553 1 19960815 A 5312 BULKHEAD DOUG DC9 DC931 3022065 WP BS 996 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 943VJ 72318 47058 PIT - DURING AGING AIRCRAFT VISIT, FOUND LEVEL 1 CORROSION AT AFT PRESSURE BULKHEAD 'T' CAP STATION 996 BETWEEN LONGERON S 22 AND 24 LEFT. REPAIRED PER SRM FIG 101 AND EA 33256. CUT OUT CORRODED AREAS INSTALLED FILLERS AND DOUBLERS PER SRM 53-63 FIG 1 AND EA 33256. (M) 2 L 7 2 4F A6WE 1996090500561 19960905 00561 WP 1996 9 5 USAA960554 1 19960815 A 5320 'T' CAP DOUG DC9 DC931 3022065 WP BS 996 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 943VJ 72138 47058 PIT - DURING AGING AIRCRAFT VISIT, FOUND CORROSION AND DOUBLER DRILLED HOLES AT STATION 996 'T' CAP AT LONGERON 26 LEFT. TRIM OUT, CLEANED UP HOLES AND INSTALLED DOUBLER PER EA 58531 REV 'A'. (M) 2 L 7 2 4F A6WE 1996090500562 19960905 00562 WP 1996 9 5 USAA960555 1 19960815 A 5312 BULKHEAD DOUG DC9 DC931 3022065 WP BS 996 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 943VJ 72138 47058 PIT - DURING AGING AIRCRAFT VISIT, FOUND LEVEL 1 CORROSION AT AFT PRESSURE BULKHEAD 'T' CAP STATION 996 BETWEEN LONGERON S 19 AND 20 LEFT. CUT OUT CORRODED AREAS AND INSTALLED FILLERS AND DOUBLERS PER SRM 53-03 FIG 101 AND EA 33256. (M) 2 L 7 2 4F A6WE 1996090500563 19960905 00563 WP 1996 9 5 USAA960556 1 19960815 A 5313 27779225 LONGERON DOUG DC9 DC931 3022065 WP BS 925-970 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 943VJ 72138 47058 PIT - DURING AGING AIRCRAFT VISIT, FOUND 5 FOOT SECTION OF LONGERON 27 LEFT, CORRODED FROM STATION 925 TO STATION 970. S PLICED IN NEW SECTION OF LONGERON PER REPAIR DOCUMENT 53-11-3 FIG 4, 53-02 PG 1. (M) 2 L 7 2 4F A6WE 1996090500564 19960905 00564 WP 1996 9 5 USAA960557 1 19960815 A 5313 2777948 LONGERON DOUG DC9 DC931 3022065 WP BS 925-970 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 943VJ 72138 47058 PIT - DURING AGING AIRCRAFT VISIT, FOUND 5 FOOT LONG SECTION OF LONGERON 26 LEFT CORRODED FROM STATION 925 TO STATION 97 0. SPLICED IN NEW SECTION OF LONGERON PER REPAIR DOCUMENT 53-02 PG 1 AND PG 5, FIG 4. (M) 2 L 7 2 4F A6WE 1996090500565 19960905 00565 WP 1996 9 5 USAA960558 1 19960815 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 956-996 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 943VJ 72138 47058 PIT - DURING AGING AIRCRAFT VISIT, FOUND SKIN CORROSION ON FUSELAGE STATION 956 THROUGH STATION 996 BETWEEN LONGERONS 26 L AND 29L. REPAIRED WITH FUSELAGE SKIN SPLICE PER EA 33339. (M) 2 L 7 2 4F A6WE 1996090500566 19960905 00566 NE 1996 9 5 USAAD96115 2 19960808 A 7260 717000 GEARBOX DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7B 52053 NE NR 2 ENGINE LEAKING A A USAA E A ENGINE SHUTDOWN UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CL CLIMB 1 EA 19 952VJ 37182 5007 47574 657759 FLT 1593 - PHL-CMH - ON CLIMB-OUT, GOT RIGHT OIL PRESSURE LIGHT, FOLLOWED BY RIGHT OIL QUANTITY LOSS AND DROPPING OIL TE MPERATURE. SHUT DOWN RIGHT ENGINE, RETURNED TO FIELD. REPLACED NR 2 ENGINE GEARBOX. (M) 2 L 7 2 4F 4 F A6WE E2EA 1996090500567 19960905 00567 1996 9 5 USAAD96116 4 19960818 A 3418 9650041029 STALL WARN COMP DOUG DC9 DC931 3022065 WP LEFT FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 997VJ 12495 47336 FLT 844 - PIT-DTW - AFTER ROTATION, THE STALL WARNING INDICATION WENT OFF. RETURNED TO FIELD. REPLACED LEFT STALL WARN ING COMPUTER. (M) 2 L 7 2 4F A6WE 1996090500568 19960905 00568 NM 1996 9 5 USAASB96150 1 19960810 A 3397 WIRE BOEING 737 7373B7 1384580 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 524AU 23859 LGA - PILOT REPORTED, THAT EMERGENCY EXIT LIGHTS AT ROW 3 WERE INOP. MAINTENANCE MADE REPAIR AT ROW 3 EMERGENCY PATH WI RING AND TRIM. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 1996090500569 19960905 00569 NM 1996 9 5 USAASB96151 1 19960811 A 3397 WIRE BOEING 737 7373B7 1384580 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 524AU 23859 PIT - PILOT REPORTED, THAT THE EMERGENCY FLOOR LEVEL LIGHTING IN FIRST CLASS HAS THREE ROWS INOP. MAINTENANCE REPAIRED TWO BROKEN WIRES IN THE FLOOR LEVEL LIGHTING. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996090500570 19960905 00570 NM 1996 9 5 USAASB96154 1 19960814 A 2782 65446519 ACTUATOR BOEING 737 737201 1384454 NM NR 5 LE FLAP INTERNAL LEAKAGE A USAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 EA 19 254AU 36370 22796 ROA - FLT 2520 - THE NR 5 LEADING EDGE SLAT FAILED TO RETRACT AFTER TAKEOFF. FLIGHT RETURNED TO FIELD AT ROA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE NR 5 LEADING EDGE SLAT ACTUATOR TO HAVE INTERNAL LEAKAGE. REPLACED AC TUATOR PER MM 27-81-41A. OPS CHECK NORMAL. (M) 2 L 7 2 4F A16WE 1996090500571 19960905 00571 1996 9 5 USAASB96155 4 19960814 A 2210 AUTOPILOT SYS BOEING 737 737301 1384611 NM NR 1/2 MALFUNCTIONED A A USAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 19 300AU 23228 PIT - FL 1595 - ON CLIMB-OUT, THE FLT EXPERIENCED AN UNCOMMANDED ROLL TO THE LT. FLT WAS CLEARED TO 6,000 FT AND ENCOUN TERED A BUFFET AT ABOUT 4,500 FT, WHILE CLIMBING STRAIGHT AHEAD AT 230 KTS INDICATED. A/C BEGAN ROLLING SLOWLY LT WITH A CHANNEL AUTOPILOT ENGAGED. A SHUDDER WAS FELT AS A/C CONTINUED TO ROLL TO A 30 DEGREE BANK. CREW DISENGAGED AUTOPILO T AND YAW DAMPER. FULL AILERON AND PARTIAL RUDDER INPUT WAS REQUIRED TO STRAIGHTEN AND LEVEL A/C. FLT RETURNED TO FIEL D, WITH NO FURTHER INCIDENT. MX ACCOMP T/S OF AUTOPILOT NR 1 AND NR 2 PER DIRECTION OF USAIR AVIONICS ENGINEERING. REP LACED FLT DATA RECORDER FOR READOUT WHICH INDICATED ROLL WAS CAUSED BY WAKE TURBULENCE. FDR OPS CHK GOOD. (M) 2 L 7 2 4F RT A16WE 1996090500572 19960905 00572 NM 1996 9 5 USAASB96156 1 19960810 A 3350 LIGHT BOEING 737 7372B7 1384560 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 284AU 23131 BWI - MAINTENANCE FOUND MULTIPLE INTERIOR OVERHEAD EMERGENCY EXIT LIGHTS INOP. MAINTENANCE RESEATED CANNON PLUG ON POWE R SUPPLY. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1996090500573 19960905 00573 NE 1996 9 5 USAASB96157 2 19960814 A 7321 9387M15P11 FUEL CONTROL BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE NR 2 ENGINE FAILED A A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 356US 23559 BWI - FLT 426 - ON CLIMB-OUT FROM DCA, THE NR 2 ENGINE BEGAN UNCOMMANED MOVEMENTS OF 1.5 TO 2 INCHES. WITH AUTOTHROTTLE ON, N1, N2, EGT, AND FUEL FLOW ALL FLUCTUATED. AUTOTHROTTLE DISCONNECTED AND STILL HAD FLUCTUATIONS. CAPTAIN DECIDED TO DIVERT TO BWI WHERE THE FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 ENGINE MAIN ENGINE CON TROL AND MAIN ENGINE FUEL PUMP PER MM. OPS CHECK NORMAL. RAN ENGINE THROUGH FULL POWER RANGE, NO FLUCTUATIONS NOTED. ( M) 2 L 7 2 4F 4 F RT A16WE E2GL 1996090500574 19960905 00574 NM 1996 9 5 USAASB96158 1 19960816 A 3350 3114981 SOCKET BOEING 737 7373B7 1384580 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 373US 22952 ROC - MAINTENANCE FOUND THE AFT ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOP. MAINTENANCE REPLACED THE REFLECTOR LIGHT SOCK ET ASSEMBLY AT THE AFT ENTRY DOOR, EXTERIOR FUSELAGE. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996090500575 19960905 00575 NM 1996 9 5 USAASB96159 1 19960817 A 3350 1158331 LIGHT BOEING 737 7374B7 1384702 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 438US 24560 ROC - MAINTENANCE FOUND THE MID CABIN EMERGENCY EXIT LIGHTS INOP. MAINTENANCE FOUND THE RIGHT FORWARD EMERGENCY HATCH E XIT LIGHT SOCKET AT FAULTY. REPLACED LIGHT ASSEMBLY. ALSO, REPLACED THE MID CABIN OVERHEAD BATTERY PACK, P/N AD2013-1A . OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996090500576 19960905 00576 NM 1996 9 5 USAASB96161 1 19960819 A 2750 RETRACT MECH BOEING 737 7374B7 1384702 NM TE FLAPS MALFUNCTIONED A USAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 19 433US 24555 PHL - FLT 489 - ON CLIMB-OUT FROM ISP AT 8,000 FEET, CAPTAIN ATTEMPTED TO RETRCT FLAPS. FLAPS WERE STUCK. FLIGHT DIVER TED TO PHL. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE ADJUSTED TRAILING ED GE FLAPS PER MAINTENANCE MANUAL 27-51-00. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996090500577 19960905 00577 NM 1996 9 5 USAASB96163 1 19960820 A 2150 106050616 ACM BOEING 737 7373B7 1384580 NM CABIN MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 390US 23312 BWI - FLT 1245 - AFTER TAKEOFF, CREW COULD NOT GET AIRCRAFT TO PRESSURIZE. AIRCRAFT WAS HELD AT 9,000 FEET WHILE CONVER SING WITH MAINTENANCE. AFTER SEVERAL FAILED ATTEMPTS, CREW DECIDED TO RETURN TO FIELD AT BWI. NO EMERGENCY WAS DECLARE D AND THE FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACD THE RIGHT AIR CYCLE MACHINE, THE LEFT 35 DEGREE W ATER SEPARATOR SENSOR AND THE LEFT AND RIGHT WATER SEPARATOR BAGS. OPS CHECK GOOD. PRESSURIZATION CHECK OF AIRCRAFT GO OD PER MAINTENANCE MANUAL. (M) 2 L 7 2 4F RT A16WE 1996090500578 19960905 00578 NM 1996 9 5 USAASB96164 1 19960821 A 3350 900835A BATTERY PACK BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 281AU 23114 CLT - MAINTENANCE FOUND THE CENTER AISLE OVERHEAD EMERGENCY EXIT SIGN INOP. MAINTENANCE REPLACED THE CENTER AISLE OVERH EAD EMERGENCY BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1996090500579 19960905 00579 NM 1996 9 5 W8PA960103 1 19960810 A 3350 COVER BOEING 737 7373Y0 1384671 NM CABIN LOOSE A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 955WP 24463 FOUND EMERGENCY EXIT FLOOR LIGHT COVER ROW 15 LEFT SIDE CAME UP AND WIRES CAME LOOSE. REPAIRED FLOOR TRACK LIGHTING AS REQUIRED. (M) 2 L 7 2 4F RT A16WE 1996090500580 19960905 00580 NM 1996 9 5 W8PA960106 1 19960819 A 3397 WIRE BOEING 737 7373L9 1384470 NM CABIN MISSING A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 960WP 23331 FOUND EMERGENCY EXIT LIGHTING WIRE EXPOSED AND CAP MISSING AT ROW 23. RESECURED WIRE AND CAP, FUNCTION CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996090500581 19960905 00581 NM 1996 9 5 WRLA96033 1 19960816 A 3240 2607454 TEMP SENSOR DOUG MD11 MD11F 3023600 NM NR 9 BRAKE FAILED A WRLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 274WA 48633 DURING TAXI OUT, FLIGHT CREW NOTED NR 9 BRAKE TEMPERATURE INDICATOR OVERHEAT ALERT. FLIGHT CREW ELECTED TO RETURN TO GA TE. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. REPLACED TEMP SENSOR, GROUND CHECKS OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A22WE 1996090500582 19960905 00582 EU 1996 9 5 WTAA960161 1 19960807 A 3233 6158D ACTUATOR BAG JETSTM JETSTM3101 1500215 EU NLG FAILED A WTAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 17 422UE 782 PDX - NOSE LANDING GEAR FAILED TO RETRACT ON TAKEOFF. AIRCRAFT RETURND TO STATION WITHOUT INCIDENT. AIRCRAFT WAS FERRI ED TO EUG FOR REPAIRS. MAINTENANCE REPLACED NOSE RETRACTION JACK. SYSTEM OPERATIONAL CHECK NORMAL DURING GEAR RETRCTIO N CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996090500583 19960905 00583 WP 1996 9 5 Y2PA96060 1 19960802 A 7932 8TJ92GAA2 OIL QTY TRANSM DOUG DC9 DC915F 3022037 WP RIGHT ENGINE MALFUNCTIONED A Y2PA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 196US 47155 YIP - UNSCHEDULED LANDING MADE, OIL QTY WENT TO ZERO AND LOW OIL PRESSURE LIGHT FLICKERED. THE OIL PRESSURE REMAINED NO RMAL ACCORDING TO THE PRESSURE INDICATOR. REPLACED THE OIL QTY TRANSMITTER AND REPLACED THE OIL PRESSURE SWITCH. ENGIN E OPERATED AND CHECKED FOR PROPER OPERATION AND FOR LEAKS. NO DEFECTS NOTED. (M) 2 L 7 2 4F A6WE 1996090500584 19960905 00584 1996 9 5 Y2PA96062 4 19960802 A 2312 6224088009 VHF COMM 1 DOUG DC9 DC915F 3022037 WP E/E COMPT FAILED A Y2PA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 23 198US B5447 47045 YIP - NR 1 COMM INOP (INTERMITTENTLY) AND NR 2 COMM INOP (INTERMITTENTLY). AIRCRAFT DIVERTED INTO YIP. NO EMERGENCY P ROCEDURES NECESSARY. MAINTENANCE WAS NOT ABLE TO DUPLICATE THE PROBLEM ON EITHER COMM. BOTH COMM'S WERE REPLACED AND B OTH SYSTEMS CHECKED GOOD IAW GMM CHAP 8, SEC 7. (M) 2 L 7 2 4F A6WE 1996090500585 19960905 00585 WP 1996 9 5 ZIAA96016 1 19960516 A 2612 24407332 DETECTION LOOP DOUG DC8 DC8F54 3021926 WP NR 4 ENGINE CHAFED A ZIAA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 8042U 45676 HUF - DURING CLIMB-OUT, SHUT DOWN NR 4 ENGINE DUE TO FIRE WARNING INDICATION. VISUALLY INSPECTED, FOUND UPPER DETECTION LOOP CHAFED. REPLACED DETECTION LOOP. OPERATIONAL CHECKED GOOD. NO EVIDENCE OF FIRE FOUND. (M) 2 L 7 4 4F 4A25 1996090500586 19960905 00586 SO 1996 9 5 ZIAA96017 1 19960530 A 5711 SPAR CAP LKHEED 188 188C 5262604 SO WS 70 CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 289F 69814 36920 188C1110 YIP - DURING INSPECTION, FOUND RIGHT WING FRONT SPAR LOWER 'T' RAIL CRACKED AT STATION 70. INSTALLED REPAIR AS PER ZIAA DER APPROVED DRAWING NR A91-R01. (M) 2 L 7 4 4T 4A22 1996090500587 19960905 00587 SO 1996 9 5 ZIAA96018 1 19960601 A 5730 8005182 SKIN LKHEED 188 188C 5262604 SO WS 177-179 CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 289F 69814 36920 188C1110 YIP - DURING INSPECTION, FOUND CRACK IN UPPER RIGHT WING, 2/3 PLANK JOINT AT WS NR 177-179. REMOVED CRACKED AREA AS PER L-188 BS 620. INSTALLED REPAIR AS PER ZIA DER APPROVED DRAWING NR A81-R02. (M) 2 L 7 4 4T 4A22 1996090500588 19960905 00588 WP 1996 9 5 ZIAA96019 1 19960627 A 7120 37707451 ENGINE MOUNT 5762790 DOUG DC8 DC8F54 3021926 WP NR 4 AFT BROKEN A A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 8052U 46009 LAX - DURING MAINTENANCE ON NR 4 ENGINE FOUND ENGINE AFT MOUNT, LEFT ARM, THREADED PORTION BROKEN OFF. REPLACED THE ARM WITH A SERVICEABLE PART TIME ON MOUNT SINCE LAST SHOP VISIT, 319 HOURS AND 78 CYCLES. (M) 2 L 7 4 4F 4A25 1996090500589 19960905 00589 SO 1996 9 5 ZIAA96020 1 19960510 A 5730 8376041 SKIN LKHEED 188 188C 5262604 SO WS 73.5-79.5 CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 286F 60819 25066 188C1146 YIP - DURING INSPECTION UPPER LEFT WING, PLANK NR 4 AT 3/4 PLANK SEAM CRACKED BETWEEN STATION 73.5 AND 79.5. CLEAN UP A REA OUT OF LIMITS. REPAIRED PLANK AS PER DER APPROVED ZIAA DRAWING NR A72-R04. (M) 2 L 7 4 4T 4A22 1996090500590 19960905 00590 SO 1996 9 5 ZIAA96021 1 19960510 A 5730 8376041 SKIN LKHEED 188 188C 5262604 SO WS 190-193 CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 286F 60819 25066 188C1146 YIP - DURING INSPECTION UPPER LEFT WING, PLANK NR 4 AT 3/4 PLANK SEAM CRACKED BETWEEN STATION 190 AND 193. CLEAN UP ARE A OUT OF LIMITS. REPAIRED PLANK AS PER 188 SRM AND DER APPROVED ZIAA DRAWING NR A72-R01. (M) 2 L 7 4 4T 4A22 1996090500591 19960905 00591 SO 1996 9 5 ZIAA96022 1 19960510 A 5730 8398033 SKIN LKHEED 188 188C 5262604 SO WS 244-246 CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 286F 60819 25066 188C1146 YIP - DURING INSPECTION LOWER LEFT WING, PLANK NR 3 AT 2/3 PLANK SEAM CRACKED BETWEEN STATION 244 AND 246. CLEAN UP ARE A OUT OF LIMITS. REPAIRED PLANK AS PER L-188 SRM 57-2-1 PG 33 AND 37. (M) 2 L 7 4 4T 4A22 1996090500592 19960905 00592 SO 1996 9 5 ZIAA96023 1 19960510 A 5730 8376071 SKIN LKHEED 188 188C 5262604 SO WS 121.5-124.5 CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 286F 60819 25066 188C1146 YIP - DURING INSPECTION UPPER LEFT WING, PLANK NR 7 AT 6/7 PLANK SEAM CRACKED BETWEEN STATION 121.5 AND 124.5. REPAIRED AS PER L-188 SRM 57-2-1 PG 33. (M) 2 L 7 4 4T 4A22 1996090500593 19960905 00593 SO 1996 9 5 ZIAA96024 1 19960511 A 5730 8376072 SKIN LKHEED 188 188C 5262604 SO WS 249-252 CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 286F 60819 25066 188C1146 YIP - DURING INSPECTION UPPER RT WING, PLANK NR 7 AT 6/7 PLANK SEAM CRACKED BETWEEN STATION 249 AND 252. CLEAN UP AREA OUT OF LIMITS. REPAIRED PLANK AS PER ZIAA DER APPROVED DRAWING NR A72-R02. (M) 2 L 7 4 4T 4A22 1996090500594 19960905 00594 SO 1996 9 5 ZIAA96025 1 19960511 A 5730 8376042 SKIN LKHEED 188 188C 5262604 SO WS 80 CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 286F 60819 25066 188C1146 YIP - DURING INSPECTION UPPER RT WING, PLANK NR 4 AT 4/5 PLANK SEAM CRACKED AT STATION 80 3.5 INCH FORWARD OF PLANK SEAM . REPAIRED PLANK AS PER L-188 SRM 57-2-1 PG 17. (M) 2 L 7 4 4T 4A22 1996090500595 19960905 00595 SO 1996 9 5 ZIAA96026 1 19960511 A 5730 8376061 SKIN LKHEED 188 188C 5262604 SO WS 77-80 CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 286F 60819 25066 188C1146 YIP - DURING INSPECTION UPPER LEFT WING, PLANK NR 6 AT 5/6 PLANK SEAM CRACKED BETWEEN STATION 77 AND 80. CLEAN UP AREA OUT OF LIMITS. REPAIRED PLANK AS PER ZIAA DER APPROVED DRAWING NR A72-R05. (M) 2 L 7 4 4T 4A22 1996090500596 19960905 00596 SO 1996 9 5 ZIAA96027 1 19960511 A 5730 8376012 SKIN LKHEED 188 188C 5262604 SO WS 71.5-73 CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 286F 60819 25066 188C1146 YIP - DURING INSPECTION UPPER RIGHT WING, PLANK NR 1 AT 1/2 PLANK SEAM CRACKED BETWEEN STATION 71.5 AND 73. REPAIRED AS PER L-188 LOCKHEED SB 678 DRAWING NR 842451. (M) 2 L 7 4 4T 4A22 1996090500597 19960905 00597 SO 1996 9 5 ZIAA96028 1 19960511 A 5730 8398124 SKIN LKHEED 188 188C 5262604 SO WS 76.5-79 CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 286F 60819 25066 188C1146 YIP - DURING INSPECTION, UPPER RIGHT WING, PLANK NR 2 AT 2/3 PLANK SEAM CRACKED BETWEEN STATION 76.5 AND 79. REPAIRED A S PER L-188 SRM 57-2-1 PG 33. (M) 2 L 7 4 4T 4A22 1996090500598 19960905 00598 SO 1996 9 5 ZIAA96029 1 19960511 A 5730 8398124 SKIN LKHEED 188 188C 5262604 SO WS 86-88 CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 286F 60819 25066 188C1146 YIP - DURING INSPECTION, UPPER RIGHT, PLANK NR 2 AT 2/3 PLANK SEAM CRACKED BETWEEN STATION 86 AND 88. REPAIRED AS PER L -188 SRM 57-2-1 PG 33. (M) 2 L 7 4 4T 4A22 1996090500599 19960905 00599 SO 1996 9 5 ZIAA96030 1 19960511 A 5730 8376052 SKIN LKHEED 188 188C 5262604 SO WS 75-78 CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 286F 60819 25066 188C1146 YIP - DURING INSPECTION, UPPER RIGHT WING, PLANK NR 5 AT 4/5 PLANK SEAM CRACKED BETWEEN STATION 75 AND 78. REPAIRED AS PER L-188 SRM 57-2-1 PG 33 AND LOCKHEED SB 678 DRAWING NR 842451. (M) 2 L 7 4 4T 4A22 1996090500600 19960905 00600 SO 1996 9 5 ZIAA96031 1 19960511 A 5730 8376052 SKIN LKHEED 188 188C 5262604 SO WS 90-92 CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 286F 60819 25066 188C1146 YIP - DURING INSPECTION, UPPER RIGHT WING, PLANK NR 5 AT 4/5 PLANK SEAM CRACKED BETWEEN STATION 90 AND 92. REPAIRED AS PER L-188 SRM 57-2-1 PG 33 AND LOCKHEED SB 678 DRAWING NR 842451. (M) 2 L 7 4 4T 4A22 1996090500601 19960905 00601 SO 1996 9 5 ZIAA96032 1 19960511 A 5730 8376062 SKIN LKHEED 188 188C 5262604 SO WS 74-82 CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 286F 60819 25066 188C1146 YIP - DURING INSPECTION, UPPER RIGHT WING, PLANK NR 6 AND 5/6 PLANK SEAM CRACKED BETWEEN STATION 74 AND 82. REPAIRED AS PER L-188 LOCKHEED SB 678 DRAWING NR 842451. (M) 2 L 7 4 4T 4A22 1996090500602 19960905 00602 SO 1996 9 5 ZIAA96033 1 19960511 A 5730 8376072 SKIN LKHEED 188 188C 5262604 SO WS 69-79 CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 286F 60819 25066 188C1146 YIP - DURING INSPECTION, UPPER RIGHT WING, PLANK NR 7 AT 6/7 PLANK SEAM CRACKED BETWEEN STATION 69 AND 79. REPAIRED AS PER L-188 LOCKHEED SB 678 DRAWING NR 842451. (M) 2 L 7 4 4T 4A22 1996090500603 19960905 00603 SO 1996 9 5 ZIAA96034 1 19960511 A 5730 8005184 SKIN LKHEED 188 188C 5262604 SO WS 69-83 CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 286F 60819 25066 188C1146 YIP - DURING INSPECTION, UPPER RIGHT WING, PLANK NR 8 AT 7/8 PLANK SEAM CRACKED BETWEEN STATION 69 AND 83. CLEAN UP ARE A OUT OF LIMITS. REPAIRED PLANK AS PER DER APPROVED ZIAA DRAWING NR A72-R03. (M) 2 L 7 4 4T 4A22 1996090500604 19960905 00604 SO 1996 9 5 ZIAA96035 1 19960511 A 5730 8398012 SKIN LKHEED 188 188C 5262604 SO WS 111-112.5 CORRODED A ZIAA K NONE L NO TEST IN INSP/MAINT 1 GL 23 286F 60819 25066 188C1146 YIP - DURING INSPECTION, LOWER RIGHT WING, PLANK NR 1 AT 1/2 PLANK SEAM CRACKED BETWEEN STATION 111 AND 112.5. REPAIRED AS PER L-188 SRM 57-2-1 PG 30. (M) 2 L 7 4 4T 4A22 1996090500605 19960905 00605 SO 1996 9 5 ZIAA96036 1 19960511 A 5730 8376042 SKIN LKHEED 188 188C 5262604 SO WS 328-330 CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 286F 60819 25066 188C1146 YIP - DURING INSPECTION UPPER RIGHT WING, PLANK NR 4 AT 3/4 PLANK SEAM CRACKED BETWEEN STATION 328 AND 330. REPAIRED AS PER L-188 LOCKHEED BS 620 DRAWING NR 841403. (M) 2 L 7 4 4T 4A22 1996090500606 19960905 00606 NE 1996 9 5 CALA9601258 2 19960824 A 7310 KB27120 O-RING BOEING 757 757224 1384958 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE CUT A CALA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SW 09 14106 27296 31286 THE TOWER REPORTED FUEL LEAKING FROM THE RIGHT ENGINE AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED W ITHOUT INCIDENT. MAINTENANCE FOUND THE RIGHT ENGINE HIGH PRESSURE TUBE O-RING GOING FROM HIGH PRESSURE PUMP TO FUEL FLO W GOVERNOR CUT. THE LINE WAS REMOVED AND ALL O-RINGS WERE REPLACED. THE LINE WAS REINSTALLED AND THE ENGINE WAS RUN WI TH NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A2NM E12EU 1996090500607 19960905 00607 NM 1996 9 5 CALA9601259 1 19960903 A 3260 SENSOR BOEING 737 7373T0 1384582 NM LT MLG INOPERATIVE A CALA O OTHER N FALSE WARNING TO TAKEOFF 1 SW 09 12318 23369 THE LT MLG RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER TAKEOFF. THE GEAR WAS CYCLED, BUT THE LIGHT REMAINED ILLUMINATED . WHEN GEAR WAS EXTENDED ALL THREE GREEN LIGHTS ILLUMINATED WITH NO RED LIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCI DENT. MAINTENANCE FOUND THE LEFT MLG UPLOCK SENSOR AT FAULT. THE LT UPLOCK SENSOR WAS REPLACED. IN ADDITION, THE M988 CARD WAS REPLACED AS A PRECAUTIONARY MEASURE, OPERATIONAL CHECKS WERE GOOD IAW MM 32-09-01. 2 L 7 2 4F RT A16WE 1996090500608 19960905 00608 1996 9 5 CALA9601260 4 19960903 A 2210 COMPUTER BOEING 737 7373T0 1384582 NM E/E COMPT MALFUNCTIONED A CALA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SW 09 14336 23574 THE AIRCRAFT HAD A 12 DEGREE UNCOMMANDED ROLL TO THE LEFT WITH AUTOPILOT-B ENGAGED WHILE ON APPROACH. THE FIRST OFFICER DISCONNECTED B-AUTOPILOT AND THERE WERE NO FURTHER PROBLEMS. THE FLIGHT CONTROL COMPUTER WAS REPLACED AS A PRECAUTIONA RY MEASURE. A LAND VERIFY TEST WAS PERFORMED IAW MM 22-03-00. *S/D* SHOP FINDINGS REVEALED NO TROUBLE FOUND WITH THE FLIGHT CONTROL COMPUTER. IN ADDITION, A 90 DAY REVIEW OF ATA 22 AND 27 SINCE THIS EVENT, REVEALED NO ADDITIONAL REPORTS OF AIRCRAFT UNCOMMANDED ROLL. 2 L 7 2 4F RT A16WE 1996090500609 19960905 00609 NM 1996 9 5 CALA9601261 1 19960903 A 2750 655554011 DRIVE MECHANISM BOEING 737 737130 1384435 NM LT TE FLAP WORN BEARING A A CALA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SW 09 24213 18363 19030 WHEN FLAPS WERE SELECTED TO 30 DEGREES ON APPROACH, THE AIRCRAFT ROLLED LEFT. THE FLAPS WERE SET TO 25 DEGREES AND THE ROLL STOPPED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT INBOARD AFT FLAP STICKING IN THE UP POS ITION WITH FLAPS LOWERED. THE LEFT INBOARD AFT FLAP DRIVE MECHANISM HAD A WORN CENTER BEARING. THE FLAP DRIVE MECHANIS M WAS REPLACED. THE FLAPS WERE CYCLED SEVERAL TIMES WITH NO DEFECTS. IN ADDITION, THE LEFT INBOARD TRAILING EDGE FLAP WAS ADJUSTED/TESTED IAW MM 27-51-12, PAGES 501 TO 506. 2 L 7 2 4F A16WE 1996090500610 19960905 00610 WP 1996 9 5 CALA9601262 1 19960902 A 3260 POSN SWITCH DOUG DC9 DC931 3022065 WP RT MLG DOOR OUT OF ADJUST A CALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 14564 47490 THE GEAR DOOR OPEN LIGHT REMAINED ON WITH GEAR RETRACTED AFTER TAKEOFF. CYCLING THE GEAR WAS NO HELP. WHEN THE GEAR WA S EXTENDED FOR RETURN TO IAH THE LIGHT EXTINGUISHED. THE AIRCRAFT HAD A BRIEF PROBLEM HISTORY WITH THE DOOR OPEN LIGHT AND THE LEFT GEAR DOOR SWITCH HAD BEEN REPLACED PREVIOUSLY. MAINTENANCE FOUND THE RT MLG DOOR POSITION SWITCH OUT OF RI G. AN ADJUSTMENT WAS PERFORMED IAW MM 32-60-3 AND ALL INDICATIONS WERE NORMAL. 2 L 7 2 4F A6WE 1996090500611 19960905 00611 NM 1996 9 5 9618966603 1 19960830 A 3230 69B803585 DNLOCK ACT BOEING 747 747151 1384891 NM LT WING GEAR MALFUNCTIONED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 603US 49246 2951 19780 DURING APPROACH, THE LEFT WING LANDING GEAR UNSAFE LIGHT ILLUMINATED. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND PERFORMED A TOWER FLY-BY. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE LEFT WING GEAR DOWNLOCK ACTUATOR, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996090500612 19960905 00612 NM 1996 9 5 9618976625 1 19960830 A 3234 CONTROL HANDLE BOEING 747 747251B 1384892 NM LANDING GEAR LACK OF LUBE A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 625US 21707 DURING APPROACH THE LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER LANDING GEAR EXTENSION. RECYCLED LANDING GEAR AND LIGHT EXTINGUISHED. AIRCRAFT LANDED WITHOUT INCIDENT. LUBRICATED LANDING GEAR CONTROL HANDLE, OPERATIONAL CHECK GO OD. 2 L 7 4 4F A20WE 1996090500613 19960905 00613 NM 1996 9 5 9618986739 1 19960901 A 3244 TIRES BOEING 747 747251F 1384898 NM LT MLG FAILED A NWAA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 GL 01 639US 23887 WHILE TAXIING, THE LEFT WING AND BODY LANDING GEAR BRAKES INDICATED HIGH TEMPERATURES AND THREE TIRES FAILED ON TAXI. T HREE MORE TIRES FAILED WHILE AIRCRAFT WAS PARKED AT THE GATE. INSPECTED AND OPERATIONALLY CHECKED BRAKE SYSTEM, OPERATI ONAL CHECK GOOD. REPLACED ALL EIGHT TIRES ON THE LEFT BODY AND WING LANDING GEARS. 2 L 7 4 4F A20WE 1996090500614 19960905 00614 EU 1996 9 5 9618993203 1 19960830 A 5230 DOOR HANDLE AIRBUS 320 A320211 3930320 EU CARGO COMPT LACK OF LUBE A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 303US 34 DURING TAKEOFF ROLL AT 60 KNOTS, RECEIVED AN AFT CARGO DOOR WARNING INDICATION. ABORTED THE TAKEOFF WITHOUT FURTHER INC IDENT. LUBRICATED THE DOOR HANDLE LOCK ASSEMBLY AND OPERATED THE DOOR SEVERAL TIMES PER MM 52-35-00, PG 10, CHECKED OK. 2 L 7 2 4F RT A28NM 1996090500615 19960905 00615 NM 1996 9 5 SWAA960913 1 19960828 A 5320 FRAME BOEING 737 7372H4 138448C NM CARGO DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED B-CHECK, FORWARD CARGO DOORWAY FRAME CRACKED AT LOWER STOP, UPPER INBOARD CORNER. REPAIRED PER SWA RA 1-353-1494. 2 L 7 2 4F A16WE 1996090500616 19960905 00616 NM 1996 9 5 SWAA960914 1 19960828 A 5230 SKIN BOEING 737 7372H4 138448C NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED B-CHECK, FOUND AFT CARGO DOOR HANDLE CUTOUT UPPER AFT CORNER CRACKED .25 INCH ON OUTER SKIN. REPAIRED PER SWA RA 1-A52-020. 2 L 7 2 4F A16WE 1996090500617 19960905 00617 NM 1996 9 5 SWAA960915 1 19960903 A 5315 FLOOR BOEING 737 7373H4 1384600 NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 356SW 25251 DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORRODED AT BS 344, BL ZERO, AND LBL 7. REPAIRED PER TI -A53-014 AND BOEING SRM. 2 L 7 2 4F RT A16WE 1996090500618 19960905 00618 NM 1996 9 5 SWAA960916 1 19960903 A 3350 6104781 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED TERMINAL CHECK, FOUND FORWARD CABIN EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE. REPLACED BATTERY PACK AND CHARGER PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996090500619 19960905 00619 NM 1996 9 5 SWAA960917 1 19960903 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 74SW 22674 DURING SCHEDULED D-CHECK, FOUND CRACK INDICATION IN RADIUS OF BS 178 SIDE CHORD LT SIDE FROM WL 193 TO WL 197. REPAIRED PER TRAMCO EWO 96-0410. 2 L 7 2 4F A16WE 1996090500620 19960905 00620 NM 1996 9 5 SWAA960918 1 19960828 A 5320 DOOR BEAM BOEING 737 7373H4 1384600 NM BS 807-847 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 354SW 26575 DURING SCHEDULED D-CHECK, FOUND AFT CARGO DOOR BEAM WEB CORRODED AT BS 807 TO BS 847. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996090500621 19960905 00621 NM 1996 9 5 SWAA960919 1 19960828 A 5320 STRAP BOEING 737 7373H4 1384600 NM BS 847 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 354SW 26575 DURING SCHEDULED D-CHECK, FOUND AFT CARGO DOOR BEAM STRAP CORRODED AT BS 847, RBL 20, WL 151. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996090500622 19960905 00622 1996 9 5 WWMA9600068 4 19960902 A 2320 TP4429 PRINTER SAAB SF340 340B 7860101 EU COCKPIT SHORTED A WWMA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 WP 15 320AE 7060 866 340B320 CREW REPORTED A POP NOISE FOLLOWED BY SMOKE EMITTING FROM ACARS PRINTER. MAINTENANCE DISCONNECTED THE CANNON ON BACK OF THE ACARS PRINTER AND DEFERRED THE PRINTER IAW WITH THE MEL. 2 L 7 2 4T RT A52EU 1996090500623 19960905 00623 NM 1996 9 5 VNAA9609001 1 19960903 A 2130 22260A010101 CONTROL PANEL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT DEFECTIVE A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 457PS 9535 3048 ON CLIMBOUT, PILOT WAS UNABLE TO CONTROL CABIN ALTITUDE. AFTER LEVELING OFF AT 10,000, CABIN CONTINUED TO CLIMB. RETUR NED TO FIELD AND LANDED WITHOUT INCIDENT. FOUND PRESSURIZATION CONTROL PANEL DEFECTIVE. REPLACED PANEL IN ACCORDANCE W ITH DORNIER MAINTENANCE MANUAL 21-31-01, OPERATIONAL CHECK GOOD. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996090500624 19960905 00624 NM 1996 9 5 MWEA96426 1 19960831 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 1270 GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 DURING C-CK, FOUND SKIN AT STA 1270, LONG 28L HAS 1.5 INCH GOUGE. INSTALLED REPAIR IAW SRM 53-01, FIG 2, SHEET 3. 2 L 7 2 4F RT A6WE 1996090500625 19960905 00625 WP 1996 9 5 MWEA96427 1 19960901 A 5400 ANGLE DOUG DC9 DC932 3022066 WP LT PYLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 DURING INSP, FOUND ANGLE BENEATH LT PYLON AT STA 996 CRACKED 1 INCH. INSTALLED REPAIR IAW SRM 54-04, FIG 10. 2 L 7 2 4F A6WE 1996090500626 19960905 00626 NE 1996 9 5 DLL13961973 2 19960826 A 7261 OIL PUMP 727706605 LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B02 54555 NE NR 3 ENGINE LEAKING A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 783DL LXU259 193A1009 10661 SMOKE IN CABIN, ISOLATED PACKS, FOUND PROBLM TO BE IN NR 3 ISO VLV. ALL PACK TEMPS NORMAL, CONTINUED WITH ALL PACKS AND NR 3 ISO VLV UNLATCHED. REPLACED NR 3 ENGINE OIL PUMP, OPS CHECK GOOD. 2 L 7 3 4F 4 F A23WE E12EU 1996090500627 19960905 00627 NM 1996 9 5 DL757961974 1 19960826 A 3397 WIRE BOEING 757 757232 1384965 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 645DL 24216 10661 F/C TRACK LIGHTS INOP. REPAIRED BROKEN WIRES AT FLOOR TRACK, OPN NORM. 2 L 7 2 4F RT A2NM 1996090500628 19960905 00628 NM 1996 9 5 DLM88961990 1 19960827 A 3350 6011779 PWR SUPPLY DOUG MD88 MD88 3023688 NM EXTERIOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 925DL 49712 EMER LIGHTS EXTERIOR AFT AREA INOP. REPLACED PWR SUPPLY, CHECKS GOOD. 2 L 7 2 4F RT A6WE 1996090500629 19960905 00629 NM 1996 9 5 DL757961993 1 19960828 A 2560 MV10 MEGAPHONE BOEING 757 757232 1384965 NM CABIN FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 649DL 24389 F/C MEGAPHONE SQUEALS AT ALL VOLUME SETTINGS. REPLACED MEGAPHONE AND OPS CKS GOOD. 2 L 7 2 4F RT A2NM 1996090500630 19960905 00630 NM 1996 9 5 DL767962000 1 19960828 A 3350 BPS73 POWER SUPPLY BOEING 767 767232 1385132 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 103DA 22215 FWD PART OF AFT CABIN EMERGENCY PATH LIGHTING INOP DURING L/O. REPAIRED SHORTED WIRES AT SIDEWALL 35FG AND REPLACED M90 09 BATTERY MODULE. 2 L 7 2 4F RT A1NM 1996090500631 19960905 00631 NM 1996 9 5 DL72W962008 1 19960829 A 3350 LIGHT 10011141 BOEING 727 727247 138408F NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2813W 20869 AFT AREA EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY EMERGENCY LIGHTS, CK OK. 2 L 7 3 4F A3WE 1996090500632 19960905 00632 1996 9 5 DL757962009 4 19960829 A 2330 PA SYST RDAX7308M0D8 BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 685DA 100461 27588 THE PRERECORDED PASSENGER ANNOUNCEMENT SYSTEM OVERHEATED IN FLIGHT. REMOVED THE UNIT FROM THE WAS AND DISCONNECTED THE CANNON PLUG. 2 L 7 2 4F RT A2NM 1996090500633 19960905 00633 WP 1996 9 5 DLL16962011 1 19960830 A 3350 5165741 POWER PACK LKHEED 1011 10113853 5265020 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 760DH 193Y1194 EMERGENCY EXIT LIGHTS IN MAIN COACH CABIN CAME ON FOR NO REASON. RECYCLED CB AND EMERGENCY LIGHT SWITCH TO TURN THEM OF F. FOUND LT MAIN BPS FAILED. REPLACED SAME, OPS OK. 2 L 7 3 4F A23WE 1996090500634 19960905 00634 WP 1996 9 5 DLL14962015 1 19960831 A 3300 POWER SUPPLY 5165741 LKHEED 1011 1011385115 5265015 WP L2 DOOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 737D 37451 193C1228 EMERGENCY LIGHT AT EXTERIOR OF L2 DOOR INOP. REPLACED POWER SUPPLY, CHKS GOOD. 2 L 7 3 4F A23WE 1996090500635 19960905 00635 WP 1996 9 5 DLL14962016 1 19960831 A 3350 BATTERY PACK LKHEED 1011 1011385115 5265015 WP L2 DOOR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 737D 193C1228 SECTION OF LIGHT TRACK LT SIDE FROM L2 DOOR AFT ILLUMINATES FOR ONLY A SHORT PERIOD DURING TEST. REPLACED RACK AND BATT PACK, CHKS GOOD. 2 L 7 3 4F A23WE 1996090500636 19960905 00636 NM 1996 9 5 DL72S962017 1 19960831 A 2560 MV10 MEGAPHONE BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 408DA 21152 FWD MEGAPHONE BATTERY LOW. REPLACED MEGAPHONE, TESTS GOOD. 2 L 7 3 4F A3WE 1996090500637 19960905 00637 WP 1996 9 5 DLL10962018 1 19960831 A 3350 337001090 POWER SUPPLY LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 733DS 193C1224 POWER SUPPLIES DO NOT INDICATE AMBER LIGHT CHARGING COND DURING TEST. REPLACED POWER SUPPLIES, TEST OK. LOC ADJ R1 AND L4 DOORS. 2 L 7 3 4F A23WE 1996090500638 19960905 00638 NM 1996 9 5 DLM88962022 1 19960831 A 2410 CSD 976J2526 DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE FAILED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 984DL 3752 53311 725488 AT 33,000 FT RT GEN VOLTS AND FREQS UNSTABLE AND DROPPED OFF LINE. RT CSD OIL TEMP WENT OFF SCALE ABOVE RED LINE. TRIE D TO DISCONNECT CSD, WOULD NOT DISCONNECT. REPLACED NR 2 ENG CSD AND GEN, CSD GARLOCK SEAL. FLUSHED OIL, COOLER LINES , RAN ENG, OPN NORMAL. 2 L 7 2 4F 4 F RT A6WE E9NE 1996090500639 19960905 00639 NM 1996 9 5 DL72S962025 1 19960901 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 419DA 21272 OVERWING EXIT LIGHT AT AFT CARGO DOOR INOP. REPLACED BATTERY CARTRIDGE, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1996090500640 19960905 00640 NM 1996 9 5 DL757962029 1 19960902 A 3350 BATTERY 61020 BOEING 757 757232 1384965 NM MID GALLEY DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 604DL 22811 EMERGENCY FLASH LIGHT BATTERY LOW. REPLACED BATT. 2 L 7 2 4F RT A2NM 1996090500641 19960905 00641 1996 9 5 SWIA95754 4 19960901 A 3425 AHARS COMP EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE NR 2 MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 188SW 120039 ATTITUDE AND HEADING FAILURE INFLIGHT. RIGHT SIDE COULD NOT DUPLICATE. RERACKED NR 2 AHRS COMPUTER PER EMB AHRS INITIA LIZATION AND ORIENTATION PROCEDURE. 2 L 7 2 4T 4 T RT A31SO E20NE 1996090500642 19960905 00642 1996 9 5 SWIA95755 4 19960901 A 3425 6226190204 AHRS COMP EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE NR 2 FAILED A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 188SW 120039 ADI AND HSI FAILURE INFLIGHT. REMOVED AND REPLACED NR 2 AHRS COMPUTER. COMPLIED WITH ORIENTATION PROCEDURES. SYSTEM G ROUND TESTS NORMAL. RAN AIRCRAFT FOR 30 MINUTES, SYSTEM TESTS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1996090500643 19960905 00643 WP 1996 9 5 RRXA96069 1 19960820 A 5311 2537716 FRAME DOUG DC8 DC863F 302198F WP BS 440 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 957R 46137 DURING C-CHECK, FOUND 2 HOLES DRILLED IN FRAME INBD FLANGE 3 AND 12 ABOVE FLOOR IN UPPER CARGO COMPARTMENT, Y=440, LT SI DE. FABRICATED REPAIR ANGLE IAW DER APPROVED ENGINEERING SKETCH A98-R03. DRILLED, TREATED, PRIMED AND INSTALLED IAW DC -8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1996090500644 19960905 00644 WP 1996 9 5 RRXA96070 1 19960820 A 5311 2537716 FRAME DOUG DC8 DC863F 302198F WP BS 320 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 957R 46137 DURING C-CHECK, FOUND HOLE DRILLED IN FRAME INBD FLANGE, LT SIDE OF UPPER CARGO COMPARTMENT, Y=320, 3 ABOVE FLOOR. REMO VED FASTENERS, FABRICATED REPAIR ANGLE AND HEAT TREATED IAW DER APPROVED ENGINEERING SKETCH A98-R03 AND INSTALLED IAW DC -8 SRM 51-1-21. 2 L 7 4 4F 4A25 1996090500645 19960905 00645 WP 1996 9 5 RRXA96071 1 19960820 A 5311 2537716 FRAME DOUG DC8 DC863F 302198F WP BS 280 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 957R 46137 DURING C-CHECK, FOUND 6 HOLES DRILLED IN FRAME, LT SIDE OF UPPER CARGO COMPARTMENT ABOVE CUSP, 9 AFT OF CARGO DOOR, Y=28 0. FABRICATED AND DRILLED REPAIR DOUBLER, HEAT TREATED AND AGED IAW DER APPROVED ENGINEERING SKETCH A98-R03. INSTALLED REPAIR IAW DC-8 SRM 51-1-21. 2 L 7 4 4F 4A25 1996090500646 19960905 00646 WP 1996 9 5 RRXA96072 1 19960820 A 5311 2537716 FRAME DOUG DC8 DC863F 302198F WP BS 280 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 957R 46137 DURING C-CHECK, FOUND 4 HOLES DRILLED IN FRAME, LT SIDE AT AFT LOWER CORNER OF CARGO DOOR. REMOVED FASTENERS IN REPAIR AREA, FABRICATED AND INSTALLED REPAIR IAW DER APPROVED ENGINEERING SKETCH A98-R03. 2 L 7 4 4F 4A25 1996090500647 19960905 00647 WP 1996 9 5 RRXA96073 1 19960820 A 5311 2537716 FRAME DOUG DC8 DC863F 302198F WP BS 240 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 957R 46137 DURING C-CHECK, FOUND HOLE DRILLED IN RADIUS OF FRAME AT CUSP FITTING, RH Y=240. FORMED REPAIR ANGLE FROM 7075-0 MATERI AL AND HEAT TREATED TO T-6 CONDITION IAW DER APPROVED ENGINEERING SKETCH A98-R03. DRILLED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-21. 2 L 7 4 4F 4A25 1996090500648 19960905 00648 WP 1996 9 5 RRXA96074 1 19960820 A 5311 1616373 FRAME DOUG DC8 DC863F 302198F WP BS 1100 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 957R 46137 DURING C-CHECK, FOUND CORROSION UNDER NUTPLATE ON FRAME AND FRAME SPLIT IN AFT LOWER COMPARTMENT, Y=1100 ABOVE LONGERON 34 RT. REMOVED CORROSION, CUT OUT DAMAGED AREA OF FRAME, FABRICATED FILLER DOUBLERS IAW DER APPROVED ENGINEERING SKETCH A98-R02 AND INSTALLED IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1996090500649 19960905 00649 WP 1996 9 5 RRXA96075 1 19960820 A 5730 SKIN DOUG DC8 DC863F 302198F WP WS 289 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 957R 46137 DURING C-CHECK, FOUND UPPER LEADING EDGE GOUGED AND CRACKED AT XRS 289. STOP DRILLED CRACK, FABRICATED DOUBLER FROM .06 3 7075T-6AL, IAW DER APPROVED ENGINEERING SKETCH A96-R01 AND INSTALLED IAW DC-8 SRM 51-1-20D, 21, 21D. 2 L 7 4 4F 4A25 1996090500650 19960905 00650 WP 1996 9 5 RRXA96076 1 19960820 A 5311 2537716 FRAME DOUG DC8 DC863F 302198F WP BS 1060 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 957R 46137 DURING C-CHECK, FOUND CORROSION ON FRAME Y=1060, AT LONGERON 36 UNDER NUTPLATE AND 35 LEFT, Y=1040 AT LONGERON 33 AND 34 RIGHT, UNDER NUTPLATES. REMOVED NUTPLATES, REMOVED CORROSION, TREATED AND PRIMED IAW DC-8 SRM 51-1-8, FABRICATED FILLE RS, DOUBLERS AND DRILLED IAW DER APPROVED ENGINEERING SKEYCH A98-R06 AND A98-R11. INSTALLED IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1996090500651 19960905 00651 WP 1996 9 5 RRXA96077 1 19960820 A 5730 SKIN DOUG DC8 DC863F 302198F WP WS 20 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 957R 46137 DURING C-CHECK, FOUND RT WING LEADING EDGE UPPER ATTACHMENT DAMAGED AT FASTENERS APPROX XFS 20. REMOVED FASTENERS, REMO VED CORROSION, FABRICATED REPAIR DOUBLER FROM .190 7075T-6 MATERAIL IAW DER APPROVED ENGINEERING SKETCH A98R05 AND INSTA LLED IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1996090500652 19960905 00652 WP 1996 9 5 RRXA96078 1 19960820 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 330-350 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 957R 46137 DURING C-CHECK, FOUND FUSELAGE SKIN BULGED AT Y=350, X=-19 AND Z=-59 FWD FUSELAGE. REMOVED FASTENERS ON A-PIT DOOR DOUB LER TO Y=330 AND TO LONGERON 28. CUT SKIN AT Y=389 AND PEELED UP. NO CORROSION FOUND, FABRICATED SKIN SPLICE DOUBLERS AND REPAIRED SKIN IAW DER APPROVED ENGINEERING SKETCH A98-R13 AND A98-R12. 2 L 7 4 4F 4A25 1996090500653 19960905 00653 WP 1996 9 5 RRXA96079 1 19960820 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 190-330 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 957R 46137 DURING C-CHECK, FOUND INTERNAL DOUBLER CORRODED AT Y=220 TO 265 AND LONGERONS 35L TO 35R, ALSO INNER SKIN CORRODED AND B ULGED AT Y=224 BETWEEN LONGERONS 33R TO 34R. REMOVED CORRODED SKIN AND INNER DOUBLER, FABRICATED INTERNAL DOUBLER AND E XTERNAL SKIN IAW DER APPROVED ENGINEERING SKETCHES A98-R04; A98-R08, A98-R10 FROM Y=190 TO 330 AND INSTALLED IAW DC-8 SR M 51-1-21, 51-1-20D, 51-3-0. 2 L 7 4 4F 4A25 1996090500654 19960905 00654 WP 1996 9 5 RRXA96080 1 19960820 A 5310 STRUCTURE DOUG DC8 DC863F 302198F WP BS 920 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 957R 46137 DURING C-CHECK, FOUND FLOOR TO FRAME FITTING AT Y=920 UPPER WEB, HAD CORROSION INSIDE RT WHEEL WELL. CUT UPPER WEB, REM OVED CORROSION IAW DC-8 SRM 51-1-8, REMOVED Y=920 TRAP FITTING, REPAIRED WEB AND FLOOR BEAM IAW DER APPROVED ENGINEERING SKETCH A98-R07, MODIFIED TRAP FITTING AND INSTALLED IAW SKETCH, DC-8 SRM 53-2-0. 2 L 7 4 4F 4A25 1996090500655 19960905 00655 WP 1996 9 5 RRXA96081 1 19960820 A 5313 LONGERON DOUG DC8 DC863F 302198F WP BS 42 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 957R 46137 DURING C-CHECK, FOUND CORROSION ON LONGERON 27R AT GROUND AIR CONDITION CONNECTOR PANEL DOME NUT AT Y=42. REMOVED DOME NUTS, REMOVED CORROSION AND FOUND CORROSION WAS BEYOND LIMITS. REMOVED AND REPLACED LONGERON 27R IAW DC-8 SRM 51-1-20D . INNER DOOR DOUBLER WAS CORRODED BEYOND LIMITS. REMOVED CORROSION, FABRICATED REPAIR IAW DER APPROVED ENGINEERING SKE TCH A96-R09 AND INSTALLED IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1996090500656 19960905 00656 WP 1996 9 5 RRXA96082 1 19960820 A 5512 SKIN DOUG DC8 DC863F 302198F WP LT HORIZ STAB CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 957R 46137 DURING C-CHECK, FOUND LT UPPER HORIZ STAB LEADING EDGE HAD CORROSION IN 2 PLACES AT ATTACHMENT SCREWS, APPROX. XF=143 AN D XF=153. REMOVED OLD REPAIR DOUBLER, FABRICATED NEW REPAIR DOUBLER FROM .063 7075T-6. TREATED, PRIMED AND INSTALLED I AW DER APPRVED ENGINEERING SKETCH A98-R16. 2 L 7 4 4F 4A25 1996090500657 19960905 00657 WP 1996 9 5 RRXA96083 1 19960820 A 5512 SKIN DOUG DC8 DC863F 302198F WP LT HORIZ STAB DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 957R 46137 DURING C-CHECK, FOUND TEMPORARY REPAIR ON LT HORIZ STAB LEADING EDGE, O/B SECTION. REMOVED TEMPORARY REPAIR, FABRICATED INTERNAL AND EXTERNAL DOUBLERS AND STRAPS IAW DER APPROVED ENGINEERING SKETCH A98-R14, INSTALLED IAW DC-8 SRM 51-1-20D, 51-1-21. 2 L 7 4 4F 4A25 1996090500658 19960905 00658 WP 1996 9 5 RRXA96084 1 19960820 A 5311 2537716 FRAME DOUG DC8 DC863F 302198F WP BS 1120 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 957R 46137 DURING C-CHECK, FOUND CORROSION ON FRAME UNDER NUTPLATES, AT Y=1120 AND LONGERON 36. REMOVED NUTPLATES AND CORROSION, F ABRICATED FILLER AND DOUBLERS IAW DER APPROVED ENGINEERING SKETCH A98-R15, INSTALLED IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1996090500659 19960905 00659 WP 1996 9 5 ARWA9608027 1 19960902 A 3260 H141003 SWITCH DOUG DC8 DC863 302198A WP RT MLG MALFUNCTIONED A ARWA O OTHER P NO WARNING INDICATION DE DESCENT 1 SO 19 345JW 46042 AT GEAR DOWN AT MIAMI, RT MAIN GEAR LIGHTS NOT ON. RETRACTED AND EXTENDED AGAIN. NO PUSH TO TEST, ALSO ANTI-SKID LIGHT ON AND RFI, FRO LIGHTS ON AND OFF. FLY-BY TOWER, SAID 3 GEAR DOWN ON RIGHT TURN AROUND AND FLAPS 50 DEG. THE RT GEAR LIGHT CAME ON, REPLACED CANNON PLUG RT MLG DOWN LIMIT AND SWITCH. ALSO, REPLACED LANDING GEAR WARNING LIGHT ASSEMBLY. O PS CHECKED ELECTRICAL WIRING AND FOUND NORMAL. SYSTEM OPS CHECK NORMAL ON RETRACTION TEST. 2 L 7 4 4F 4A25 1996090500660 19960905 00660 WP 1996 9 5 Y2PA960070 1 19960829 A 5330 59114123N SKIN DOUG DC9 DC915F 3022037 WP BS 237-475 CORRODED A Y2PA K NONE O OTHER IN INSP/MAINT 1 GL 23 193US 45828 DURING C AND D BRIDGING AND ALIGNMENT CHECK INSPECTION, FOUND CORROSION ON FORWARD BELLY SKIN STATION 237 TO STATION 475 . REMOVED AND REPLACED FORWARD BELLY SKIN STATION 237 TO STATION 475 IAW DC9 SRM 51-01 AND 51-30-2. HIDDEN DAMAGE REPO RT NR AIA 6015 AND NON-ROUTINE WORK CARD NR 96-0196. REPORT GENERATED BY AMERICAN INTERNATIONAL AIRWAYS, INC B4MR FOR U SA JET AIRLINES, Y2PA. 2 L 7 2 4F A6WE 1996090500661 19960905 00661 WP 1996 9 5 Y2PA960071 1 19960829 A 5313 59164411 LONGERON DOUG DC9 DC915F 3022037 WP BS 360-366 CRACKED A Y2PA K NONE O OTHER IN INSP/MAINT 1 GL 23 193US 45828 DURING C AND D BRIDGING AND ALIGNMENT CHECK INSPECTION, FOUND 6 INCH CRACK IN LONGERON 30 STATION 360 TO 366. REMOVED A ND REPLACED LONGERON 30 STATION 360 TO 366 IAW DC9 SRM 51-01 AND 51-30-5. NON-ROUTINE WORK CARD NR 96-0196 AND 96-0264. REPORT GENERATED BY AMERICAN INTERNATIONAL AIRWAYS, INC B4MR FOR USA JET AIRLINES, Y2PA. 2 L 7 2 4F A6WE 1996090500662 19960905 00662 WP 1996 9 5 Y2PA960072 1 19960829 A 5313 S27779223 LONGERON DOUG DC9 DC915F 3022037 WP BS 229-280 CORRODED A Y2PA K NONE O OTHER IN INSP/MAINT 1 GL 23 193US 45828 DURING C AND D BRIDGING AND ALIGNMENT CHECK INSPECTION, FOUND STATION 229 TO 280 LONGERON 28R CORRODED. REMOVED AND REP LACED LONGERON 28R STATION 229 TO 280 IAW DC9 SRM 51-01 AND 51-30-5. NON-ROUTINE WORK CARD NR 96-0196 AND 96-0249. REP ORT GENERATED BY AMERICAN INTERNATIONAL AIRWAYS, INC B4MR FOR USA JET AIRLINES, Y2PA. 2 L 7 2 4F A6WE 1996090500663 19960905 00663 WP 1996 9 5 Y2PA960073 1 19960829 A 5260 SKIN DOUG DC9 DC915F 3022037 WP AIRSTAIR DOOR DAMAGED A Y2PA K NONE O OTHER IN INSP/MAINT 1 GL 23 193US 45828 DURING C AND D BRIDGING AND ALIGNMENT CHECK INSPECTION, FOUND FWD AIRSTAIRS DOOR HAD DAMAGE AT INSIDE EDGE. REPAIRED FW D AIRSTAIR DOOR IAW AIA 8110-3 AND DRAWING AIA/E/2251. HIDDEN DAMAGE REPORT NR AIA 6015. NON-ROUTINE WORK CARD NR 96-0 203. REPORT GENERATED BY AMERICAN INTERNATIONAL AIRWAYS, INC B4MR FOR USA JET AIRLINES, Y2PA. 2 L 7 2 4F A6WE 1996090500671 19960905 00671 EU 1996 9 5 96ZZZX4283 1 19960812 A 2822 355A01519902 CIRCUIT BOARD AEROSP AS355 AS355F1 8680810 EU BOOST PUMP MELTED A EJYA O OTHER O OTHER NR NOT REPORTED 1 WP 07 911TX 5073 PILOT REPORTED BOOST PUMP INOPERATIVE IN-FLIGHT. FOUND PRINTED CIRCUIT BOARD AND CONNECTOR MELTED AT ONE CORNER. REPLA CED CONNECTOR AND PCB. SUBMITTER RECOMMENDS AMENDING STARTING PROCEDURE TO TURN BOOST PUMP SWITCH OF JUST PRIOR TO STAR TING ENGINES. SUSPECT HIGH CURRENT DRAW OVER THE BOARD ON START SEQUENCE WITH LOWERED VOLTAGE AVAILABLE OVERHEATS THE PCB. 1 G 7 2 3U H11EU 1996090500677 19960905 00677 CE 1996 9 5 96ZZZX4289 1 19960702 A 3297 WIRE CESSNA 310 310R 2074245 CE MLG DOWNLOCK BROKEN A BSYA K NONE P NO WARNING INDICATION NR NOT REPORTED 1 GL 07 3700G 310R0899 DSM - NO RT GEAR DOWN AND LOCK INDICATION. FOUND BROKEN GROUND WIRE. REPAIRED WIRE, OPS CHECKED GOOD. 1 L 7 2 3O 3A10 1996090500681 19960905 00681 EA 1996 9 5 96ZZZX4293 2 19960702 A 8550 DIPSTICK PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA RT ENGINE OIL NOT INSTALLED A BSYA A UNSCHED LANDING W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 42HD 318152031 L814661A GRR - RT OIL DIPSTICK LEFT OUT CAUSING OIL LEAK AND SMOKE. RETURNED TO GRR. WASHED DOWN, SERVICED OIL AND CONTINUED WI TH FLIGHT. 1 L 7 2 3O 3 O A20SO E14EA 1996090900001 19960909 00001 EU 1996 9 9 WTAA960159 1 19960804 A 3234 8662B SELECTOR VALVE BAG JETSTM JETSTM3101 1500215 EU NLG FAILED A WTAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 17 422UE 782 NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. ACFT RETURNED TO STATION WITHOUT INCIDENT. ACFT FERRIED TO EUG FOR REPAIRS. MAINTENANCE REPLACED GEAR SEL ECTOR VALVE, SYSTEM OPERATIONAL CHECK NORMAL. 2 L 7 2 4T RT A21EU 1996091100001 19960911 00001 WP 1996 9 11 AALA961057 1 19960717 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 486AA 49679 DFW - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS IN THE FORWARD CABIN BY GALLEY INOPERATIVE. RE PLACED EMERGENCY EXIT FLOOR PATH LIGHTS STRIP IN FORWARD CABIN BY GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996091200001 19960912 00001 NM 1996 9 12 TWRA96219 1 19960724 A 3350 S1356B37 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND 3L MED EVAC LIGHT INOP. REPLACED 3L MED LIGHT ASSY. OPS CHECKED NORMAL PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996091200002 19960912 00002 SW 1996 9 12 PNSA960716 1 19960716 A 2913 PV304426 PUMP SWRNGN SA227 SA227AC 8780603 SW LT HYD SYST FAILED A PNSA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 41NE AC741B LEFT HYDRAULIC FAIL LIGHT ILLUMINATED DURING CLIMB. RETURNED TO ANC. 2 L 7 2 4T RT A8SW 1996091200003 19960912 00003 WP 1996 9 12 PNSA960728 2 19960728 A 7200 ENGINE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP WING FLAMED OUT A PNSA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 AL 03 175SW AC621 ENGINE INLET BUILT UP ICE, INLET HEAT TURNED ON, ENGINE FLAMED OUT. AIR RESTART ACCOMPLISHED. LANDING UNEVENTFUL. 2 L 7 2 4T 4 T RT A8SW E4WE 1996091200004 19960912 00004 SW 1996 9 12 PNSA960801 1 19960819 A 2910 2781006019 HYD TUBE SWRNGN SA227 SA227AC 8780603 SW LT MLG WW LEAKING A PNSA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 AL 03 41NE AC741B HYDRAULIC LEAK IN LT WHEEL. REPLACED LINE. 2 L 7 2 4T RT A8SW 1996091200005 19960912 00005 SO 1996 9 12 PNSA960802 1 19960829 A 5280 4205900 DOOR PIPER PA31 PA31 7103102 SO LT MLG WORN A PNSA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 AL 03 27987 317912054 LEFT MAIN WOULD NOT INDICATE UP AND LOCKED, REPLACED GEAR DOOR. 1 L 7 2 3O A20SO 1996091200006 19960912 00006 NM 1996 9 12 CALA9601263 1 19960904 A 2720 75130 TRANSFER VALVE BOEING 737 7373T0 1384582 NM RUDDER PCU MALFUNCTIONED A CALA O OTHER F FLT CONT AFFECTED TO TAKEOFF 1 SW 09 14324 33957 29911 23375 THE FIRST OFFICER REPORTED, LEFT ROLL OF 5 TO 10 DEGREES BANK DURING TAKEOFF, 30 SECONDS LATER THE AIRCRAFT ROLLED RIGHT ABOUT 5 TO 10 DEGREES. YAW DAMPER RESPONSE WAS EXCESSIVE AND CAUSING FISH TAILING OF AIRCRAFT DURING CLIMB AND CRUISE. THE YAW DAMPER WAS TURNED OFF FOR THE DURATION OF THE FLIGHT. MAINTENANCE PLACARDED THE YAW DAMPER INOPERATIVE. THE YAW DAMPER COUPLER WAS REPLACED, BUT DID NOT HELP. THE ORIGINAL COUPLER WAS REINSTALLED. *S/D* THE RUDDER PCU TRANSFE R VALVE WAS REMOVED AND REPLACED IAW MM 22-12-21. TESTS WERE NORMAL IAW MM 22-12-00. NO ROLL PROBLEMS WERE REPORTED. 2 L 7 2 4F RT A16WE 1996091200007 19960912 00007 WP 1996 9 12 CALA9601264 1 19960904 A 2910 HYD LINE DOUG DC9 DC982 3022082 WP RT HYD SYST LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 09 57837 49582 THE AIRCRAFT LOST RT HYDRAULIC SYSTEM QUANTITY AND PRESSURE ON APPROACH TO SEA. ALTERNATE GEAR EXTENSION WAS USED AND T HE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC SYSTEM PRESSURE LINE TO VENTRAL STAIRS LEAKING AT FITTING NEAR AFT PRESSURE BULKHEAD. THE HYDRAULIC LINE WAS REPLACED AND LEAK CHECK WAS GOOD. 2 L 7 2 4F A6WE 1996091200008 19960912 00008 NM 1996 9 12 CALA9601265 1 19960902 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 1130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70755 21366 INSPECTION FOUND LOWER SURFACE OF FLOOR BEAM CORRODED AT F.S. 1130. THE AREA WAS REPAIRED IAW ECRA 5310-03318. 2 L 7 3 4F A3WE 1996091200009 19960912 00009 WP 1996 9 12 CALA9601266 1 19960820 A 5542 SKIN DOUG DC9 DC931 3022065 WP RUDDER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14564 47490 INSPECTION FOUND TWO 2 INCH CRACKS IN RUDDER SKIN, LOCATED AT TOP LEFT AND RIGHT SIDE OF RUDDER. THE CRACKS WERE STOP D RILLED AND DOUBLERS WERE INSTALLED IAW SRM 55-01. 2 L 7 2 4F A6WE 1996091200010 19960912 00010 WP 1996 9 12 CALA9601267 1 19960819 A 5350 LATCHES DOUG DC9 DC931 3022065 WP TAILCONE BINDING A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14564 47490 THE TAILCONE FAILED DROP CHECK AT 50+ POUNDS WHEN USING THE EXTERIOR RELEASE HANDLE. THE TAILCONE LATCHES WERE LUBRICAT ED AND OPERATION CHECKED GOOD. 2 L 7 2 4F A6WE 1996091200011 19960912 00011 SO 1996 9 12 COMA9610271 1 19960903 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 254CA 11349 1045 120233 EMERGENCY FLOOR LIGHTING FORWARD OF ROW 4 IS INOPERATIVE. REPLACED EMERGENCY BATTERY. PART TOTAL CYCLES, 11,712. 2 L 7 2 4T RT A31SO 1996091200012 19960912 00012 SO 1996 9 12 COMA9610272 1 19960903 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 152CA 12836 308 120152 AFT SECTION OF CABIN EMERGENCY LIGHTING IS INOPERATIVE. REPLACED EMERGENCY LIGHTING BATTERY. PART TOTAL CYCLES, 13,088 . 2 L 7 2 4T RT A31SO 1996091200013 19960912 00013 EU 1996 9 12 COMA9630143 1 19960903 A 3350 LIGHTS SAAB SF340 SF340A 7850100 EU CABIN INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 347CA 340A028 SEVERAL EMERGENCY LIGHTS AT FLOOR LEVEL ARE INOPERATIVE. CLEANED AND TIGHTENED WIRING CONNECTIONS AT FLOOR LIGHTING. 2 L 7 2 4T RT A52EU 1996091200014 19960912 00014 NM 1996 9 12 96FDEA01433 1 19960905 A 5753 652163586 WEDGE BOEING 727 72725 1384006 NM RT TE MID FLAP DELAMINATION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR 0175 AND 001, RT WING O/B MID FLAP T/E WEDGE DELAMINATED MARKED. *S/D* REMOVED AND REPLACED DAMAGED SKIN ON RT WING O/B MID FLAP T/E WEDGE IAW FDEA SRM 51-40-6. 2 L 7 3 4F A3WE 1996091200015 19960912 00015 NE 1996 9 12 96UAL900655 2 19960826 A 7261 50U63701 OIL TUBE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 1 ENGINE OBSTRUCTED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 775UA 26947 777043 AIRCRAFT RETURNED TO DEN UNDER AMBER ALERT WITH THE LEFT ENGINE SHUT DOWN DUE TO AN OIL QUANTITY AND PRESSURE IRREGULARI TY. *S/D* OIL QUANTITY WAS ZERO AND PRESSURE BELOW RED LINE AT START OF CRUISE. CAUSE WAS ATTRIBUTED TO PLASTIC SHIPP ING CAP IN MAIN OIL PRESSURE TUBE. PRATT SERVICE BULLETIN PW4G-112-79-07 HAD JUST BEEN ACCOMPLISHED. 2 L 7 2 4F 4 F RT T0001SE E46NE 1996091200016 19960912 00016 EU 1996 9 12 96UAL900656 1 19960826 A 3350 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 421UA 500 CABIN EMERGENCY LIGHTING CHECK FAILS TEST. POWER SUPPLY INOPERATIVE. REPLACED POWER SUPPLY AT DOOR 1L. 2 L 7 2 4F 4 F RT A28NM E40NE 1996091200017 19960912 00017 EU 1996 9 12 96UAL900657 1 19960826 A 2611 SMOKE DETECTOR SEXTANT MR26152 AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CARGO COMPT MALFUNCTIONED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 418UA 485 AFT CARGO SMOKE WARNING IN FLIGHT. WARNING CANCELED ON ITS OWN, RETURNED TO FIELD. *S/D* RESET CIRCUIT BREAKERS AND P ERFORMED BITE TEST OF SYSTEM, OPERATIONALLY CHECKS NORMAL. REPLACED SMOKE DETECTION CONTROL UNIT AS A PREVENTATIVE MEAS URE. 2 L 7 2 4F 4 F RT A28NM E40NE 1996091200018 19960912 00018 NE 1996 9 12 96UAL900658 2 19960827 A 7230 COMPRESSOR BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE RT ENGINE STALLED A UALA E ENGINE SHUTDOWN M OVER TEMP LD LANDING 1 WP 29 618UA 21878 709617 ON LANDING ROLL-OUT. THE RIGHT ENGINE HAD A COMPRESSOR STALL WHILE COMING OUT OF REVERSE THRUST. ENGINE EXCEEDED EXHAUS T GAS TEMPERATURE LIMIT AND WAS IMMEDIATELY SHUT DOWN. THE AIRCRAFT FLIGHT RECORDER INDICATED THAT THE ENGINE HAD BEEN IN REVERSE THRUST BELOW THE MINIMUM INDICATED AIRSPEED. THE FLIGHT MANUAL LIMITATIONS ARE BEING REVIEWED BY 767 FLIGHT OPERATIONS. 2 L 7 2 4F 4 F RT A1NM E3NE 1996091200019 19960912 00019 NM 1996 9 12 96UAL900659 1 19960828 A 2161 CONTROLLER 286T002915 BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE EQUIP COOLING MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 612UA 000041 21873 CABIN WOULD NOT PRESSURIZE. THE EQUIPMENT COOLING CONTROLLER FAILED AND THE COOLING EXHAUST DOOR WAS OPEN. REPLACED EQ UIPMENT COOLING CONTROLLER PER 767 MM 21-58-23. BITE CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 1996091200020 19960912 00020 NM 1996 9 12 96UAL900660 1 19960829 A 2820 69186127 ELBOW BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 FUEL TANK CRACKED A UALA O OTHER O OTHER CR CRUISE 1 WP 29 7283U 21561 CREW REPORTED 1,000 LBS UNWANTED FUEL TRANSFER OUT OF NR 1 TANK DURING CROSS FEEDING. *S/D* FUEL VENT TUBE ELBOW CRACK ED. REPLACED ELBOW. 2 L 7 3 4F 4 F A3WE E2EA 1996091200021 19960912 00021 NM 1996 9 12 96UAL900661 1 19960829 A 5754 65162211 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 4 TE FLAP CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7254U 21401 CRACK IN NR 4 LE SLAT HAS PROGRESSED BEYOND ORIGINAL STOP DRILL. CRACK IS AT LOWER TRAILING EDGE OUTBOARD END. *S/D* PERMANENT REPAIR INSTALLED PER STRUCTURAL REPAIR MANUAL. 2 L 7 3 4F 4 F A3WE E2EA 1996091200022 19960912 00022 NM 1996 9 12 96UAL900662 1 19960829 A 2820 69186128 ELBOW BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 FUEL TANK CRACKED A UALA O OTHER O OTHER TO TAKEOFF 1 WP 29 7453U 21907 NR 3 MAIN TANK LOST 1,000 LBS OF FUEL DURING TAKEOFF. *S/D* FUEL VENT TUBE ELBOW CRACKED. REPLACED ELBOW. 2 L 7 3 4F 4 F A3WE E2EA 1996091200024 19960912 00024 NM 1996 9 12 96UAL900664 1 19960829 A 3350 20131 BATTERY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 581UA 26701 EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE ROW 9 THROUGH ROW 15. REPLACED BATTERY PACK. CHECKS O.K. 2 L 7 2 4F 4 F RT A2NM E17NE 1996091200025 19960912 00025 NE 1996 9 12 96UAL900665 2 19960829 A 7230 COMPRESSOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 ENGINE STALLED A UALA K NONE R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 520UA 24890 726502 NUMBER ONE ENGINE HAD A COMPRESSOR STALL IN FLIGHT. ENGINE RECOVERED AND CONTINUED OPERATING. PRIOR TO STALL ENGINE WA S DECELERATING. *S/D* PERFORMED ENGINE BORESCOPE, 6TH THROUGH 9TH STAGE COMPRESSOR BLADES AND 2ND, 3RD STAGE LOW PRESS URE TURBINE, ALL CHECK OK. 2 L 7 2 4F 4 F RT A2NM E17NE 1996091200026 19960912 00026 NM 1996 9 12 96UAL900666 1 19960829 A 2720 654516013 PCU BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RUDDER INOPERATIVE A UALA H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED CR CRUISE 1 WP 29 320UA 16858 23952 HAD VERY ABRUPT YAW DAMPER INPUT TO THE LEFT AT FLIGHT LEVEL 290. DISENGAGED YAW DAMPER AND COMPLETED EMERGENCY CHECKLI ST. CONTINUED TO ORD, LANDING WAS DIFFICULT DUE TO SLUGGISH YAW ACTION BECAUSE YAW DAMPER TURNED OFF, JUST AS DESCRIBED IN THE FLIGHT MANUAL. *S/D* POWER CONTROL UNIT WAS FOUND DEFECTIVE. REPLACED POWER CONTROL UNIT, CHECKS OK. SHOP CO NFIRMED POWER CONTROL UNIT SOLENOID WAS BAD. THE SUMMING LEVER BEARING WAS FOUND CRACKED AT THE INNER RACE. 2 L 7 2 4F 4 F RT A16WE E2GL 1996091200027 19960912 00027 NM 1996 9 12 96UAL900667 1 19960829 A 2820 69186128 ELBOW BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 FUEL TANK CRACKED A UALA O OTHER O OTHER CR CRUISE 1 WP 29 7291U 21569 UNWANTED FUEL TRANSFER IN FLIGHT FROM NR 3 TANK. *S/D* FUEL VENT TUBE ELBOW CRACKED. REPLACED ELBOW. 2 L 7 3 4F 4 F A3WE E2EA 1996091200028 19960912 00028 NM 1996 9 12 96UAL900668 1 19960829 A 2820 69186127 ELBOW BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 FUEL TANK CRACKED A UALA O OTHER O OTHER TO TAKEOFF 1 WP 29 7294U 21572 UNWANTED FUEL USAGE FROM NR 1 TANK DURING TAKEOFF. DECREASE 1,000 LBS. *S/D* FUEL VENT TUBE ELBOW CRACKED. REPLACED ELBOW. 2 L 7 3 4F 4 F A3WE E2EA 1996091200029 19960912 00029 NM 1996 9 12 96UAL900669 1 19960829 A 3350 1619 LAMP BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 930UA 26655 EMERGENCY SLIDE LIGHT INOPERABLE AT DOOR TWO LEFT. REPLACED LAMP. CHECKS O.K. 2 L 7 2 4F 4 F RT A16WE E2GL 1996091200030 19960912 00030 NE 1996 9 12 96UAL900670 2 19960829 A 7200 ENGINE BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE NR 2 FAILED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 159UA 21140 685696 NR 2 ENGINE FILTER BYPASS LIGHT ON, BREATHER TEMPERATURE PEGGED AT 226 DEGREES AND ENGINE SHUT DOWN. *S/D* ENGINE REPL ACED. TEARDOWN OF ENGINE REVEALED EVIDENCE OF FIRE IN NR 3 BEARING COMPARTMENT. CAUSE OF FIRE UNKNOWN. 2 L 7 4 4F 4 F A20WE E20EA 1996091200031 19960912 00031 NM 1996 9 12 96UAL900671 1 19960829 A 5330 SKIN BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE BS 360-426 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 9063U 19944 THE FUSELAGE SKIN AT BODY STATION 360 TO 426 AND STRINGERS S-19R TO S-23R HAD CORROSION BETWEEN THE BONDED SKIN PANELS A ND TEAR STRIP. THE DAMAGE WAS DETECTABLE FROM THE OUTSIDE OF THE AIRCRAFT DUE TO PILLOWING OF THE SKIN. PERMANENT REPA IR, EXTERNAL DOUBLER, ACCOMPLISHED PER STRUCTURAL REPAIR MANUAL. 2 L 7 2 4F 4 F A16WE E2EA 1996091200032 19960912 00032 NM 1996 9 12 96UAL900672 1 19960829 A 3350 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 651UA 25389 EMERGENCY FLOOR LIGHTING AT ROWS 15AB-28AB FLASHES INTERMITTENTLY. REPLACED BATTERY PACK (ROW 26 AB) AND GROUND CHECKE D NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 1996091200033 19960912 00033 NM 1996 9 12 96UAL900673 1 19960830 A 2820 68186127 ELBOW BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 FUEL TANK CRACKED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 7457U 21911 CREW REPORTED THAT WITH FUEL LOAD OF 11.6, 45.8, 11.6, FEEDING FROM NR 2 TANK NR 1 FUEL QUANTITY DECREASED 500 TO 600 LB S. *S/D* FUEL VENT TUBE ELBOW CRACKED. REPLACED ELBOW. 2 L 7 3 4F 4 F A3WE E2EA 1996091200034 19960912 00034 NM 1996 9 12 96UAL900674 1 19960830 A 3350 60252 STRIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 338UA 24242 EMERGENCY ESCAPE PATH LIGHTING IN AFT CABIN HAS A 12 FOOT SECTION INOPERATIVE. REPLACED AFT SECTION LIGHT STRIP. CHECK S O.K. 2 L 7 2 4F 4 F RT A16WE E2GL 1996091200035 19960912 00035 NM 1996 9 12 96UAL900675 1 19960830 A 5220 GUIDE ARM 65B01836 BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE DOOR 4L OUT OF ADJUST A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 192UA 26881 AFTER TAKEOFF DOOR 4L INDICATED OPEN. RETURNED TO FIELD. *S/D* DOOR OUT OF ADJUSTMENT CAUSING A FALSE LATCH INDICATIO N. ADJUSTED DOOR GUIDE ARM. 2 L 7 4 4F 4 F RT A20WE E24NE 1996091200036 19960912 00036 NM 1996 9 12 96UAL900676 1 19960830 A 5313 BULKHEAD ANGLE BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE BS 178 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 988UA 21750 MULTI-SITE CRACKS FOUND AT BODY STATION 178 BULKHEAD CHORD ANGLE AND AT STRINGER 17R TEE COMMON TO THE BULKHEAD ANGLE. T HE CRACKS WERE APPROXIMATELY 2 INCHES AND 1 INCH RESPECTIVELY. CRACKS WERE DUE TO FATIGUE. BULKHEAD CHORD ANGLE REPAIR ED PER 737 STRUCTURAL REPAIR MANUAL, TYPICAL ANGLE REPAIR. REPAIRS TO STRINGER 17 RIGHT WERE MADE PER ENGINEERING VARIA TION AUTHORITY. TEE WAS CUT AND SPLICED WITH TWO BACK TO BACK ANGLES. AREA IS INSPECTED AT HEAVY MAINTENANCE VISITS IN TERVALS. 2 L 7 2 4F 4 F A16WE E2EA 1996091200037 19960912 00037 NM 1996 9 12 96UAL900677 1 19960830 A 5311 65465436 FRAME BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE BS 685 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 9032U 57962 19070 AT R-CHECK VISIT, AN INSPECTION OF THE BODY STATION 685 FRAME INTEGRAL RIBS, FOUND THE FORWARD RIB AT WL 202 CRACKED AN D PREVIOUSLY REPAIRED PER SERVICE BULLETIN 737-53-1055. A NEW CRACK WAS ALSO FOUND PROPAGATING OUTBOARD FROM THE OUTBOA RD STOP HOLE THAT EXTENDS INTO THE VERTICAL OUTBOARD FLANGE FOR APPROXIMATELY 1 INCH. REPLACED BODY STATION FRAME 685 P ER THE STRUCTURAL REPAIR MANUAL. 2 L 7 2 4F 4 F A16WE E2EA 1996091200038 19960912 00038 WP 1996 9 12 ABXA9600618 1 19960830 A 3350 5708458503 BATTERY PACK DOUG DC8 DC861 3021952 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 845AX 46157 EMERGENCY LIGHTING FAILED A2 CHECK INSPECTION. REPLACED EMERGENCY LIGHTING BATTERY PACK. OPS CHECKED NORMAL I/A/W DC-8 M.M. 33-50-0. 2 L 7 4 4F 4A25 1996091200039 19960912 00039 WP 1996 9 12 MWEA96428 1 19960904 A 2560 SLIDE COVER DOUG DC9 DC932 3022066 WP GALLEY DOOR LOOSE A MWEA K NONE O OTHER UK UNKNOWN 1 GL 31 602ME 48133 GALLEY DOOR SLIDE COVER CAME OFF. REINSTALLED GALLEY SLIDE COVER. 2 L 7 2 4F A6WE 1996091200040 19960912 00040 WP 1996 9 12 MWEA96429 1 19960904 A 3350 COVER DOUG DC9 DC914 3022034 WP CABIN MISSING A MWEA K NONE O OTHER UK UNKNOWN 1 GL 31 800ME 45795 SEAT 4 C, D, PLASTIC SHIELD FOR EMERGENCY FLOOR LIGHT BULB IS MISSING. REINSTALLED COVER. 2 L 7 2 4F A6WE 1996091200041 19960912 00041 1996 9 12 SCNA96241 4 19960829 A 2565 5WD230100 SLIDE ASSY DOUG DC10 DC1030F 3023504 WP L1 DOOR INOPERATIVE A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 600GC 46965 THE L1 DOOR SLIDE REMOTE PRESS-TO-TEST INDICATOR LIGHT STAYS ON. BOTTLE PRESSURE CHECKS OK. REPLACED L1 DOOR SLIDE ASS EMBLY PER MM 52. INSPECTED SLIDE INSTALLATION AND OPS CHECKED REMOTE TEST SYSTEM. 2 L 7 3 4F RT A22WE 1996091200042 19960912 00042 WP 1996 9 12 SCNA96242 1 19960831 A 2611 30231R17 SMOKE IND LIGHT DOUG DC10 DC1030F 3023504 WP COCKPIT INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 600GC 46965 LOWER AFT CARGO SMOKE DETECTOR NR 4 DOES NOT TEST ON ENGINEERS PRE-FLIGHT. RELAMPED LOWER AFT CARGO SMOKE DETECTOR NR 4 IN ACCORDANCE WITH MM 26-14-01. OPS CHECKED GOOD. 2 L 7 3 4F RT A22WE 1996091200043 19960912 00043 NM 1996 9 12 SCNA96243 1 19960901 A 3350 EMERGENCY LIGHT BOEING 727 727282 138408T NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 281SC 21949 RIGHT FORWARD OVERWING, FORWARD LOWER EMERGENCY LIGHT FOUND INOPERATIVE. REMOVED AND REPLACED BROKEN TERMINAL, OPS CHEC KED GOOD. 2 L 7 3 4F RT A3WE 1996091200044 19960912 00044 NM 1996 9 12 P5CA9600677 1 19960901 A 2550 ROLLER TRAY BOEING 747 747122 1384872 NM CARGO DECK DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 DAMAGED ROLLER TRAY BS 1820 LBL 33. REPLACED ROLLER TRAY PER BOEING SRM 51-10-01. 2 L 7 4 4F A20WE 1996091200045 19960912 00045 NM 1996 9 12 P5CA9600678 1 19960901 A 2550 ROLLER TRAY BOEING 747 747122 1384872 NM BS 1800 DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 DAMAGED ROLLER TRAY BS 1800 RBL 6. REPLACED ROLLER TRAY PER BOEING SRM 51-10-01. 2 L 7 4 4F A20WE 1996091200046 19960912 00046 NM 1996 9 12 P5CA9600679 1 19960901 A 5320 STANTION BOEING 747 747122 1384872 NM BS 460 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 STANTION CRACKED AFT END OF THE E AND E COMPARTMENT BS 460 WL 135 RBL 24. REPAIRED PER BOEING SRM 51-40-03. 2 L 7 4 4F A20WE 1996091200047 19960912 00047 WP 1996 9 12 CKSA96122 1 19960827 A 3310 BA170 BALLAST DOUG DC8 DC852 3021922 WP FLIGHT COMPT FAILED A CKSA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 810CK 45814 SMELLED ELECTRICAL BURNING ODOR LIKE FLUORESCENT LIGHT BALLAST. TURNED ALL LIGHTS OFF, TURNED ALL LIGHTS BACK ON ONE AT A TIME EXCEPT FLUORESCENT LIGHTS AND SMELL DID NOT RETURN. TRANSFERRED TO DMI NR 564 PER MEL 33-1 CAT-C PLACARDS INSTA LLED. REMOVED AND REPLACED BALLAST TRANSFORMER. OPS CHECK ALL LIGHTS GOOD, NO SMELL, DMI NR 564 CLEARED PLACARDS REMOV ED. 2 L 7 4 4F 4A25 1996091200056 19960912 00056 GL 1996 9 12 96ZZZX4324 1 19960812 A 2720 2027200100 CONTROL CABLE DIAMON DA20 DA20A1 2990000 GL PILOT LT RUDDER BROKEN A P A W9WA K NONE O OTHER IN INSP/MAINT 1 WP 07 402KT 766 10039 PILOT'S LEFT OUTBOARD RUDDER CABLE BROKE AT NICOPRESS FITTING. WITH RUDDER PEDALS ADJUSTSED FULL FORWARD POSITION, S-TU BE MAKES CONTACT WITH NICOPRESS FITTING. S-TUBE WORE THROUGH THE CABLE. AIRCRAFT WAS ON THE GROUND. 1 L 7 1 3O NT TA4CH 1996091200058 19960912 00058 WP 1996 9 12 96ZZZX4326 2 19960730 A 7320 FUEL COMPUTER LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP LT ENGINE MALFUNCTION A BSYA K NONE O OTHER NR NOT REPORTED 1 GL 07 118DA 081 P74517 LEFT ENGINE STARTED TO OVERTEMP COMING BACK TO FLIGHT IDLE. GROUND CHECKED OK. ADJUSTED FUEL COMPUTER FOR N1 OF THE DA Y, OPS CHECKED GOOD NEXT FLIGHT. 2 L 7 2 4F 4 F A10CE E6WE 1996091200067 19960912 00067 CE 1996 9 12 96ZZZX4335 1 19960814 A 3252 26430901 SHIMMY DAMPER CESSNA 208 208B 2073701 CE NLG LEAKAGE A AWHA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 WP 17 750FX 232 208B0511 PRIOR TO TAKEOFF, PILOT EXPERIENCED NOSE WHEEL SHIMMY. TAKEOFF WAS ABORTED, AIRCRAFT RETURNED TO RAMP. MAINTENANCE FOUN D FLUID LEAKAGE COMING FROM NOSE WHEEL SHIMMY DAMPER. REPLACED WITH SERVICEABLE UNIT. TAXI TEST NOTED, NO DISCREPANCIE S. AIRCRAFT RETURNED TO SERVICE. 1 H 7 1 3T A37CE 1996091200080 19960912 00080 WP 1996 9 12 9619009106 1 19960901 A 3350 BATTERY PACK DOUG DC9 DC915 3022036 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 96S 47206 DURING LINE CHECK, FOUND EMERGENCY FLOOR LIGHTS INOPERATIVE FROM ROWS 1 TO 6. REPLACED BATTERY PACK, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996091200081 19960912 00081 WP 1996 9 12 9619019163 1 19960828 A 3397 WIRE DOUG DC9 DC914 3022034 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8906E 45747 DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE FROM ROW 2 FORWARD. FOUND WIRE MISSING BETWEEN ROWS 1 AND 2. REPLACED WIRES, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996091200082 19960912 00082 EU 1996 9 12 9619153203 1 19960904 A 7830 S700Y0866 CONNECTOR AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE NR 1 ENGINE DAMAGED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 303US 34 731200 DURING TAKEOFF ROLL, NR 1 ENGINE REVERSE UNLOCK MESSAGE ILLUMINATED. TAKEOFF WAS ABORTED AT 40 KNOTS AND AIRCRAFT RETUR NED TO THE GATE. GROUND MAINTENANCE FOUND DAMAGED PINS ON CANNON PLUG 402VC. CANNON PLUG PINS WERE REPAIRED. 2 L 7 2 4F 4 F RT A28NM E29NE 1996091200083 19960912 00083 WP 1996 9 12 9619169762 1 19960904 A 3350 BATTERIES DOUG DC9 DC941 302207N WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 762NW 47395 DURING LINE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERIES IN CABIN AREA AND CLEANED BULB CONTACTS IN CATWALK AREA, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996091200084 19960912 00084 WP 1996 9 12 9619179104 1 19960905 A 3350 BATTERIES DOUG DC9 DC915 3022036 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 94S 47204 DURING LINE CHECK, FOUND EMERGENCY LIGHTS IN FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996091200085 19960912 00085 WP 1996 9 12 9619189301 1 19960904 A 2741 IND MODULE DOUG DC9 DC982 3022082 WP STABILIZER TRIM MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 301RC 48054 STABILIZER TRIM CHECKED ON TAXI BY ADVANCING LEFT THROTTLE, NO WARNING. WHEN THROTTLES ADVANCED FOR TAKEOFF, RECEIVED S TABILIZER TRIM WARNING. CLEARED RUNWAY AND RETURNED TO THE GATE. REPLACED HORIZONTAL STABILIZER POSITION INDICATION MO DULE. CHECKED AND TRIMMED PER MM 27-40-12, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996091200086 19960912 00086 WP 1996 9 12 9619199308 1 19960904 A 3244 95502677 TIRE DOUG DC9 DC982 3022082 WP NLG FAILED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 311RC 48089 ON TAKEOFF ROLL, HAD UNUSUAL VIBRATION ACCOMPANIED BY BURNING TIRE SMELL IN COCKPIT AND CABIN. RETURNED TO MSP AND LAND ED WITHOUT INCIDENT. FOUND NOSE TIRE SHREDDED ON RETURN TO GATE. CHANGED BOTH NOSE TIRES, CHECKED LEFT ENGINE INLET AN D TAILPIPE. CHECKED FLAPS BOTH SIDES AND BOTTOM OF AIRCRAFT, ALL CHECKED OK. 2 L 7 2 4F A6WE 1996091200087 19960912 00087 WP 1996 9 12 9619029154 1 19960731 A 5713 LONGERON DOUG DC9 DC914 3022034 WP WS 84-111 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8913E 45830 DURING H-CHECK, FOUND CORROSION ON THE RIGHT WING LOWER STR 15 AND 17 FROM WING STA 84 TO 111. REPAIRED STRINGERS (P/N 5911276-502, 5911278-2) PER EA 91-110863, 110864. 2 L 7 2 4F A6WE 1996091200088 19960912 00088 WP 1996 9 12 9619039931 1 19960823 A 5320 PRESSURE PANEL DOUG DC9 DC931 3022065 WP BS 83 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 90S 47244 DURING H-CHECK, FOUND A CRACK IN THE NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL AT FS 83, RIGHT SIDE. REPAI RED PANEL (P/N 9910073-3) PER EA 99-110751. 2 L 7 2 4F A6WE 1996091200089 19960912 00089 WP 1996 9 12 9619049138 1 19960824 A 5312 BULKHEAD DOUBLER DOUG DC9 DC915 3022036 WP AFT PRESS BLKHD CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9348 45787 DURING H-CHECK, FOUND CRACKS IN THE AFT PRESSURE BULKHEAD 11 AND 13 DOUBLERS IN THE AFT ENTRY DOOR JAMB UPPER RIGHT CORN ER. REPAIRED DOUBLERS (P/N 5910130) PER EA 91-110760. 2 L 7 2 4F A6WE 1996091200090 19960912 00090 WP 1996 9 12 9619059756 1 19960824 A 5320 FITTING DOUG DC9 DC941 302207N WP BS 794 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 756NW 47180 DURING H-CHECK, FOUND CORROSION ON THE LONGERON 30 END FITTING AT FS 794. REPLACED FITTING (P/N 5924878-501) PER EA 97- 110748. 2 L 7 2 4F A6WE 1996091200091 19960912 00091 WP 1996 9 12 9619069756 1 19960826 A 5720 DOUBLER DOUG DC9 DC941 302207N WP RT MLG SUPPORT CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 756NW 47180 DURING H-CHECK, FOUND CORROSION ON THE RIGHT MAIN LANDING GEAR SUPPORT UPPER DIAMOND DOUBLER. REPLACED DOUBLER (P/N 591 2438-2) PER DWG 9910010, 5910464. 2 L 7 2 4F A6WE 1996091200092 19960912 00092 WP 1996 9 12 9619079756 1 19960826 A 5743 FITTING DOUG DC9 DC941 302207N WP LT MLG CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 756NW 47180 DURING H-CHECK, FOUND A 4 INCH CRACK IN THE LEFT WING FALSE SPAR TO MAIN LANDING GEAR ATTACH FITTING. REPLACED FITTING (P/N 3912765-503) PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996091200093 19960912 00093 WP 1996 9 12 9619089756 1 19960826 A 5744 FITTING DOUG DC9 DC941 302207N WP RT WING CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 756NW 47180 DURING H-CHECK, FOUND A CRACK IN THE RIGHT WING NR 4 FLAP HINGE FITTING INBOARD INTERIOR FLAP WELL. REPLACED FITTING PE R SRM 51-30-2. 2 L 7 2 4F A6WE 1996091200094 19960912 00094 WP 1996 9 12 9619099910 1 19960826 A 5312 BULKHEAD FITTING DOUG DC9 DC931 3022065 WP AFT PRESS BLKHD CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 960N 47256 DURING M-CHECK, FOUND A ONE INCH CRACK IN THE AFT PRESSURE BULKHEAD SUPPORT FITTING AT THE UPPER LEFT VENTRAL DOOR ATTAC H POINT. REPLACED FITTING PER SRM 51-30-2. 2 L 7 2 4F A6WE 1996091200095 19960912 00095 WP 1996 9 12 9619109756 1 19960827 A 5530 FITTING DOUG DC9 DC941 302207N WP VERT STAB CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 756NW 47180 DURING H-CHECK, FOUND CORROSION ON THE VERTICAL STABILIZER FRONT SPAR GUSSET FITTING LEFT SIDE AT FS 155. REPLACED FITT ING PER SRM 51-30-2, 51-30-5. 2 L 7 2 4F A6WE 1996091200096 19960912 00096 WP 1996 9 12 9619119910 1 19960828 A 5400 SPAR DOUG DC9 DC931 3022065 WP LT PYLON CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 960N 47256 DURING M-CHECK, FOUND CORROSION ON THE LEFT PYLON FRONT LOWER SPAR CAP BEAVER TAIL. REPLACED SPAR CAP (P/N 5923937-1) P ER SRM 54-04, FIG 13 AND DWG 9958161. 2 L 7 2 4F A6WE 1996091200097 19960912 00097 WP 1996 9 12 9619121162 1 19960829 A 5315 FLOOR BEAM DOUG DC10 DC1040 3023508 WP BS 1099 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 162US 46771 DURING T-CHECK, FOUND A CRACK IN THE FS 1099 FORWARD CARGO FLOOR BEAM AT LBL 60. REPAIRED BEAM (P/N ADA 0039-5) PER EA 11-106300. 2 L 7 3 4F A22WE 1996091200098 19960912 00098 NM 1996 9 12 9619136615 1 19960829 A 5711 SPAR WEB BOEING 747 747251B 1384892 NM WS 1087 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 615US 20360 DURING P-CHECK, FOUND CRACKS AND CORROSION IN THE RIGHT WING FRONT SPAR WEB AT THE UPPER CHORD FSSI 1087. REPAIRED PER EA 66-106376. 2 L 7 4 4F A20WE 1996091200099 19960912 00099 WP 1996 9 12 9619149910 1 19960829 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 718 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 960N 47256 DURING M-CHECK, FOUND CORROSION ON THE FS 718 FRAME TO THE LOWER LEFT TRAPEZOIDAL ATTACH FITTING. REPLACED FITTING (P/N 5911366-501) PER SRM 51-10-04, 51-30-1 AND EA 99-111014. 2 L 7 2 4F A6WE 1996091200100 19960912 00100 NM 1996 9 12 UPS96221038 1 19960827 A 2782 ACTUATOR RIB BOEING 727 72731C 1384011 NM WS 286 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE-C, LT NR 2 SLAT ACTUATOR RIB MOUNT ON O/B SIDE IS CRACKED. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE PER SRM 57-50-2, 51-40-3, 51-30-1, 51-30-2, 51-10-1, 51-10-2. 2 L 7 3 4F A3WE 1996091200101 19960912 00101 NM 1996 9 12 UPS96221039 1 19960828 A 5313 STRINGER BOEING 727 72731C 1384011 NM BS 990 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE-C, AFT CARGO COMPARTMENT CORROSION ON STRINGER 28L AT STA 990. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-3, 51-30-2. 2 L 7 3 4F A3WE 1996091200102 19960912 00102 NM 1996 9 12 UPS96221040 1 19960826 A 5311 FRAME BOEING 727 72731C 1384011 NM BS 990 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE-C, AFT CARGO PIT STRINGER 28L AFT SIDE FRAME CHORD AT STA 990 HAS STRINGER ATTACH HOLE THAT IS CORRODED. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-3. 2 L 7 3 4F A3WE 1996091200103 19960912 00103 NM 1996 9 12 UPS96421041 1 19960903 A 2612 FIRE WARNING BOEING 747 747123 1384873 NM NR 3 ENGINE MALFUNCTIONED A IPXA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 673UP 20325 INSPECTION TYPE, NR 3 ENGINE FIRE LIGHT AND FIRE WARNING BELL CAME ON BRIEFLY 1 TO 2 SECONDS, 4 TIMES DURING THE 7 HOUR FLIGHT. NACELLE TEMP, EGT AND ALL OTHER PARAMETERS NORMAL. INSPECTED NR 3 ENGINE FIRE LOOPS AND PERFORMED TEST IAW MM 26-11-00, NO FAULTS DETECTED AND OPS OK. 2 L 7 4 4F A20WE 1996091200104 19960912 00104 NM 1996 9 12 UPS96521036 1 19960831 A 5321 FLOOR PANEL BOEING 757 75724APF 1384969 NM BS 200-210 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 410UP 23732 INSPECTION TYPE-3C, CORROSION ON FLOOR PANEL ON LOWER CENTER OF COCKPIT. REMOVED CORROSION AND FOUND OUT OF LIMITS, FAB ED NEW PANEL AND INSTALLED. ALL WORK PER SRM 51-40-02, 51-10-01, 53-00-51, 51-30-01 AND 53-00-50. 2 L 7 2 4F RT A2NM 1996091200105 19960912 00105 WP 1996 9 12 96FDEA01434 1 19960905 A 5101 CARGO COMPT DOUG DC10 DC1010CF 3023502 WP FUSELAGE FIRE A FDEA A UNSCHED LANDING A J FLAME/FIRE WARNING INDICATION CR CRUISE 1 SO 25 68055 47809 AIRCRAFT DIVERTED TO SWF DUE TO MAIN DECK SMOKE DETECTORS NR 7, 8 AND 9 ILLUMINATING. EMERGENCY WAS DECLARED AND AIRCRA FT LANDED. *S/D* R1 SLIDE DEPLOYED NORMALLY UNDER EMERGENCY CONDITIONS, ESCAPE ROPES USED TO EXIT COCKPIT WITH NO PRO BLEMS. A/C DESTROYED BY FIRE IN MAIN CARGO COMPARTMENT. 2 L 7 3 4F RT A22WE 1996091200106 19960912 00106 WP 1996 9 12 96FDEA01435 1 19960904 A 5400 V-PANEL DOUG DC10 DC1030F 3023504 WP NR 3 PYLON MISSING A FDEA K NONE D INFLIGHT SEPARATION UK UNKNOWN 1 SO 25 322FE 47908 UPON WALK AROUND, FOUND THE V-PANEL ON NR 3 ENGINE PYLON RIPPED AWAY. INSTALLED V-PANEL ON PYLON FARING. ALSO, REPAIRE D DAMAGED PYLON FARING HONEYCOMB PANEL OUTBOARD PER DC-10 STRUCTURE REPAIR MANUAL 51-10-00. 2 L 7 3 4F RT A22WE 1996091200107 19960912 00107 WP 1996 9 12 ABXA9600620 1 19960903 A 3350 60030431 POWER SUPPLY DOUG DC9 DC941 302207N WP CABIN INOPERATIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 967AX 3901 47509 COCKPIT EMERGENCY LIGHTS VERY DIM. REPLACED EMERGENCY LIGHT POWER SUPPLY IAW DC-9 SUPP M.M. 33-53-0. 2 L 7 2 4F A6WE 1996091200108 19960912 00108 WP 1996 9 12 ABXA9600621 1 19960903 A 7930 OIL CLOG LIGHT DOUG DC9 DC933F 302207A WP PWA JT8 JT8D9A 52048 NE RT ENGINE ILLUMINATED A ABXA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 GL 23 930AX 47363 666833 DURING FLIGHT, RIGHT OIL STRAINER CLOGGING ANNUNCIATOR CAUTION LIGHT ILLUMINATED. RIGHT THROTTLE WAS REDUCED TO IDLE, L IGHT REMAINED ILLUMINATED, PRECAUTIONARY SHUT-DOWN OF RIGHT ENGINE WAS ACCOMPLISHED. REPLACED THE RIGHT ENGINE OIL SCRE EN, MEGGED THE WIRES TO THE RIGHT ENGINE OIL FILTER DIFFERENTIAL PRESSURE SWITCH, GROUND RAN THE RIGHT ENGINE. OPS CHEC KED GOOD. 2 L 7 2 4F 4 F A6WE E2EA 1996091200109 19960912 00109 WP 1996 9 12 MWEA96430 1 19960906 A 3350 100865 BATTERY PACK DOUG DC9 DC932 3022066 WP ACCESSORY COMPT DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 206ME 47791 EMERGENCY FLOOR LIGHTING INOP IN AFT ACCESSORY COMPARTMENT. REPLACED BATTERY PACK. 2 L 7 2 4F A6WE 1996091200110 19960912 00110 WP 1996 9 12 MWEA96431 1 19960906 A 3350 100865 BATTERY PACK DOUG DC9 DC914 3022034 WP ACCESSORY COMPT DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 800ME 45842 FLOOR EMERGENCY LIGHTS INOP IN AFT COMPARTMENT ALONG CATWALK. REMOVED, CLEANED AND RECONNECTED CANNON PLUG ON BATTERY P ACK, CHARGED SYSTEM, OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996091200111 19960912 00111 SO 1996 9 12 BIER960035 1 19960906 A 8120 SEAL GARRTT LW12463 PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA TURBO CHARGER FAILED B BIEA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 EA 21 3521S RKR011 317952107 L79768A PILOT REPORTED PARTIAL POWER LOSS, LATER ATTRIBUTED TO DEAD LEFT MAG. INVESTIGATION REVEALED OIL PASSING BY TURBO CHARG ER INNER SEAL AND BEING BLOWN INTO MAG THROUGH THE PRESSURIZATION HOSE, COMTAMINATING THE LEFT MAG, BUT THE RIGHT WAS O N ITS WAY. UPON REMOVAL OF TURBO, THE TRANSITION TUBE BELOW THE TURBO WAS FOUND CRACKED AT THE SEPARATOR PLATE. 1 L 7 2 3O 3 O A20SO E14EA 1996091200112 19960912 00112 NM 1996 9 12 P5CA9600680 1 19960902 A 5320 ANGLE BOEING 747 747122 1384872 NM BS 1350 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 CRACKED ATTACH ANGLES FOR RIGHT BODY LANDING GEAR TRUCK BUMPER AT LOWER WL 140 AND UPPER WL 160 BS 1350. REPLACED LOWER ANGLE PER BOEING SRM 51-10-01 AND REPAIRED UPPER PER BOEING SRM 51-30-03. 2 L 7 4 4F A20WE 1996091200113 19960912 00113 NM 1996 9 12 P5CA9600681 1 19960902 A 5320 BRACKET BOEING 747 747122 1384872 NM BS 1350 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 CRACKED AND BENT INBOARD FLAP TORQUE TUBE WHIP GUARD BS 1350 RBL 90. REPAIRED PER BOEING SRM 51-40-03. 2 L 7 4 4F A20WE 1996091200114 19960912 00114 NM 1996 9 12 P5CA9600682 1 19960902 A 5320 BRACKET BOEING 747 747122 1384872 NM BS 1395 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 CRACKED LIGHT BRACKET IN RIGHT BODY LANDING GEAR WHEEL WELL BS 1395 RBL 90 WL 200. REPLACED LIGHT BRACKET PER BOEING S RM 51-10-01. 2 L 7 4 4F A20WE 1996091200115 19960912 00115 NM 1996 9 12 P5CA9600683 1 19960821 A 5314 KEEL BEAM BOEING 747 747132 1384882 NM BS 1005 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION BS 1005 WL 100 RIGHT KEEL BEAM BOW. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER BOEIN G SRM 53-30-10 AND TREATED PER BOEING SRM 51-10-02. 2 L 7 4 4F A20WE 1996091200116 19960912 00116 NM 1996 9 12 P5CA9600684 1 19960821 A 5314 KEEL BEAM BOEING 747 747132 1384882 NM BS 1007 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION KEEL BEAM BOX RIGHT UPPER CHORD AT BS 1007 WL 115. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN L IMITS PER BOEING SRM 53-30-10 AND TREATED PER BOEING SRM 51-10-02. 2 L 7 4 4F A20WE 1996091200117 19960912 00117 WP 1996 9 12 CKSA96123 1 19960903 A 5320 36169482 FITTING DOUG DC8 DC861 3021952 WP BS 702 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 817CK 45887 DURING B-CHECK INSPECTION, FOUND RIGHT HAND UPPER CUSP HAS CRACKED FITTING AT FS 702. REPLACED FITTING IAW DC8 SRM 53-2 -0 AND 51-1-20D. TASK NR 83371 CORROSION CARD NR 573R-0051. 2 L 7 4 4F 4A25 1996091200118 19960912 00118 WP 1996 9 12 CKSA96124 1 19960903 A 5320 36169481 FITTING DOUG DC8 DC861 3021952 WP BS 702 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 817CK 45887 DURING B-CHECK INSPECTION, FOUND CRACKED FITTING FS 702 LEFT HAND CUSP UPPER. REPLACED FITTING PER SRM 53-2-0 AND SRM 5 1-1-20D. TASK NR 83400 CORROSION CARD NR 573L-0551. 2 L 7 4 4F 4A25 1996091200119 19960912 00119 WP 1996 9 12 CKSA96125 1 19960903 A 5320 3758940501 BRACKET DOUG DC8 DC861 3021952 WP BS 390 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 817CK 45887 DURING B-CHECK INSPECTION, FOUND STATION 390 LEFT HAND LOWER CUSP FLOOR SUPPORT BRACKET CRACKED. REMOVED AND REPLACED L OWER CUSP FLOOR SUPPORT STATION 390 IAW 53-01-0. TASK NR 83416 CORROSION CARD NR 557L-0552. 2 L 7 4 4F 4A25 1996091200120 19960912 00120 WP 1996 9 12 CKSA96126 1 19960903 A 5330 SKIN DOUG DC8 DC861 3021952 WP BS 240 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 817CK 45887 DURING B-CHECK INSPECTION, FOUND STATION 240 FWD PIT STRINGER 35L AND 36L SKIN HAS CORROSION. INSTALLED CLASS II REPAIR IAW DC8 SRM 53-2-1 FIGURE 7. INSPECT REPAIR AT 4,000 CYCLES INT AND REPLACED AT 24,000 CYCLES IAW DC8 SRM 53-2-1. TAS K NR 83434 CORROSION CARD NR 5570-0551. 2 L 7 4 4F 4A25 1996091200121 19960912 00121 WP 1996 9 12 CKSA96127 1 19960903 A 5320 37589402 FITTING DOUG DC8 DC861 3021952 WP BS 410 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 817CK 45887 DURING B-CHECK INSPECTION, FOUND FWD PIT STATION 410 LEFT HAND LOWER CUSP FLOOR SUPPORT FITTING CRACKED. REMOVED AND RE PLACED FWD PIT STATION 410 LEFT HAND LOWER CUSP FLOOR SUPPORT FITTING IAW SRM 53-01-0. TASK NR 83410 CORROSION CARD NR 557L-0552. 2 L 7 4 4F 4A25 1996091200123 19960912 00123 NM 1996 9 12 HNAA9699056 1 19960813 A 3350 LIGHT DHAV DHC8 DHC8201 2809001 NM CABIN INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 990HA 428 TLH/MCO - FLT 3085 - DURING PRE-FLIGHT CHECKS, FOUND FIRST AND THIRD OVERHEAD EMERGENCY LIGHTS INOPERATIVE. SWAPPED POW ER SUPPLIES PS3 AND PS2, ALL OPERATIONS NORMAL. (X) 2 H 7 2 4T RT A13NM 1996091200124 19960912 00124 EU 1996 9 12 SIMA962142 1 19960801 A 3246 5009237 WHEEL SAAB SF340 340B 7860101 EU NR 1 MLG FAILED A A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 392AE 1087 16 MAR951372 340B392 SPS - FLT 3591 - CREW REPORTED NR 1 MAIN WHEEL ASSY WAS FLAT WITH AN APPROXIMATE 10 INCH SECTION OF INNER WHEEL HUB RIM MISSING. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED WHEEL ASSY FOR FAILURE AND ALSO REPLACED NR 2 WHEEL ASSY AND NR 1 BRAKE ASSY AS PRECAUTION. NO OTHER DAMAGE WAS FOUND. AIRCRAFT WAS RETURNED TO SERVICE. PART TOTAL CYCLES, 1,148. (X ) 2 L 7 2 4T RT A52EU 1996091200125 19960912 00125 NM 1996 9 12 WRLA96031 1 19960807 A 2822 608473 BOOST PUMP DOUG MD11 MD11 3023602 NM NR 2 TANK FAILED A WRLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 278WA 48746 DURING TAXI, FLIGHT CREW NOTED 'NR 2 TANK PUMP OFF ALERT', FLIGHT CREW ELECTED TO RETURN TO GATE. AIRCRAFT RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE PERSONNEL REMOVED AND RESEATED FSC. PERFORM RETURN TO SERVICE FUEL SYSTEM TEST. AL L TESTS PASSED. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 3 4F RT A22WE 1996091200126 19960912 00126 NM 1996 9 12 EISA96104 1 19960716 A 2731 COUNTERWEIGHT BOEING 727 7272A7 138407K NM LT ELEV TAB DELAMINATION A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 310NE 20241 RIGHT ELEVATOR TAB BOB WEIGHTS HAVE DELAMINATION. APPLIED FIBERGLASS OVERLAY PER SRM 51-40-06. (X) 2 L 7 3 4F A3WE 1996091200127 19960912 00127 NM 1996 9 12 EISA96105 1 19960716 A 2731 COUNTERWEIGHT BOEING 727 7272A7 138407K NM RT ELEV TAB DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 310NE 20241 LEFT ELEVATOR TAB BOB WEIGHTS HAVE DELAMINATION. APPLIED FIBERGLASS OVERLAY PER 51-40-06. (X) 2 L 7 3 4F A3WE 1996091200128 19960912 00128 NM 1996 9 12 EISA96107 1 19960716 A 5520 TIP FILLER BOEING 727 7272A7 138407K NM LT ELEVATOR BROKEN A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 310NE 20241 LEFT ELEVATOR OUTBOARD AFT TIP IS BREAKING. REMOVED AND REPLACED TIP FILLER PER SRM 51-30-02. TT: 66,991:57 HOURS. T C: 45,084. (X) 2 L 7 3 4F A3WE 1996091200129 19960912 00129 NM 1996 9 12 EISA96106 1 19960716 A 5520 TIP FILLER BOEING 727 7272A7 138407K NM RT ELEVATOR BROKEN A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 310NE 20241 RIGHT ELEVATOR OUTBOARD T/E TIP IS BREAKING. REMOVED AND REPLACED ITP FILLER PER SRM 51-30-2. TT: 66,991:57 HOURS. T C: 45,084. (X) 2 L 7 3 4F A3WE 1996091200130 19960912 00130 NM 1996 9 12 EISA96108 1 19960716 A 5320 WEB BOEING 727 7272A7 138407K NM BS 1310 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 310NE 20241 SIDE WEB CRACKED AT LIGHTENING HOLE JUST AFT OF RT AFT AIRSTAIR STRUT FS 1310. INSTALLED DOUBLER PER SRM 51-40-02. TT: 66,991:57 HOURS. TC: 45,084. (X) 2 L 7 3 4F A3WE 1996091200131 19960912 00131 NM 1996 9 12 EISA96109 1 19960716 A 5320 WEB BOEING 727 7272A7 138407K NM BS 1263 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 310NE 20241 AFT AIRSTAIR ACTUATOR ATTACH POINT DOUBLER, INSIDE TORQUE BOX, IS CRACKED AT UPPER WEB FS 1263. FABRICATED NEW DOUBLER AND INSTALLED WITH FILLER NAD RADIUS BLOCK PER SRM 51-40-03. TT: 66,991:57 HOURS. TC: 45,084. (X) 2 L 7 3 4F A3WE 1996091200132 19960912 00132 NM 1996 9 12 EISA96110 1 19960716 A 5753 CARRIAGE BOEING 727 7272A7 138407K NM RT TE FOREFLAP CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 310NE 20241 LEADING EDGE OF RT OTBD FOREFLAP HAS 1.375 INCH CRACK ABOVE OTBD SEQUENCE CARRIAGE. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR PER SRM 57-50-04. TT: 66,991:57 HOURS. TC: 45,084. (X) 2 L 7 3 4F A3WE 1996091200133 19960912 00133 NM 1996 9 12 EISA96111 1 19960716 A 5752 SKIN BOEING 727 7272A7 138407K NM RT AILERON TAB SEPARATING A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 310NE 20241 RIGHT OUTBOARD AILERON TAB'S PREVIOUS REPAIR DETERIORATING AND SEPARATING AT T/E. FABRICATED NEW FILLERS AND DOUBLERS. ACCOMPLISHED HOT BOND REPAIR PER SRM 51-40-06. TT: 66,991:57 HOURS. TC: 45,084. (X) 2 L 7 3 4F A3WE 1996091200134 19960912 00134 NM 1996 9 12 EISA96112 1 19960716 A 5752 SKIN BOEING 727 7272A7 138407K NM RT AILERON TAB DELAMINATION A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 310NE 20241 RIGHT OTBD AILERON TAB HAS DENT WITH DELAMINATION ON LOWER SURFACE AT 3RD HINGE FROM INBD END. FABRICATED NEW FILLER AN D DOUBLER. ACCOMPLISHED HOT BOND REPAIR PER SRM 51-40-06. TT: 66,991:57 HOURS. TC: 45,084. (X) 2 L 7 3 4F A3WE 1996091200135 19960912 00135 NM 1996 9 12 EISA96113 1 19960716 A 5755 SKIN BOEING 727 7272A7 138407K NM NR 11 SPOILER CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 310NE 20241 UPPER TRAILING EDGE SKIN CRACKED FORWARD OF BOTH CENTER HINGE CUT-OUTS, NR 1 SPOILER. FABRICATED AND INSTALLED REPAIR PER SRM 57-30-04. TT: 66,991:57 HOURS. TC: 45,084. (X) 2 L 7 3 4F A3WE 1996091200136 19960912 00136 NM 1996 9 12 EISA96114 1 19960716 A 5754 ANGLE BOEING 727 7272A7 138407K NM NR 1 SLAT CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 310NE 20241 LEFT WING, NR 1 SLAT, INBOARD TRACK ATTACH FORWARD ANGLE BRACKET CRACKED. FABRICATED AND INSTALLED REPAIR PER SRM 51-40 -03. TT: 66,991:57 HOURS. TC: 45,084. (X) 2 L 7 3 4F A3WE 1996091200137 19960912 00137 NM 1996 9 12 EISA96115 1 19960716 A 5754 ANGLE BOEING 727 7272A7 138407K NM NR 1 SLAT CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 310NE 20241 LEFT WING NR 1 SLAT OUTBOARD TRACK ATTACH FORWARD ANGLE BRACKET CRACKED. INSTALLED NEW ANGLE BRACKET PER SRM 51-10-1. T T: 66,991:57 HOURS. TC: 45,084. (X) 2 L 7 3 4F A3WE 1996091200138 19960912 00138 NM 1996 9 12 EISA96116 1 19960716 A 2782 ACTUATOR BRACKET BOEING 727 7272A7 138407K NM NR 5 SLAT CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 310NE 20241 RIGHT WING NR 5 SLAT ACTUATOR ATTACH RIB BRACKET CRACKED. FABRICATED AND INSTALLED REPAIR PER SRM 57-20-03. TT: 66,99 1:57 HOURS. TC: 45,084. (X) 2 L 7 3 4F A3WE 1996091200139 19960912 00139 NM 1996 9 12 EISA96117 1 19960716 A 5311 FRAME BOEING 727 7272A7 138407K NM BS 740 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 310NE 20241 FUSELAGE FORGING AT STA 740 RT, BETWEEN STR 18R AND STR 19R, HAS CRACK EMANATING FROM PREVIOUS STOP DRILL HOLES. INSTAL LED REPAIR PER SRM'S 51-30-2, 51-10-04, SB 53-0062 AND BOEING DRAWING 65C 15314. 2 L 7 3 4F A3WE 1996091200140 19960912 00140 NM 1996 9 12 EISA96118 1 19960716 A 5315 FLOOR BEAM BOEING 727 7272A7 138407K NM LAVATORY FLOOR CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 310NE 20241 FLOOR BEAM UNDER LAVATORY FLOOR IS CORRODED. REMOVED DAMAGED FLOOR STRINGER, FABRICATED AND INSTALLED NEW STRINGER PER SRM'S 51-40-04, 51-10-02, AND 51-20-01. TT: 66,991:57 HOURS. TC: 45,084. (X) 2 L 7 3 4F A3WE 1996091200141 19960912 00141 NM 1996 9 12 EISA96119 1 19960716 A 5320 SUPPORT WEB BOEING 727 7272A7 138407K NM AFT BIN FLOOR CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 310NE 20241 FOUR EACH FLOOR SUPPORT WEBS CRACKED AT AFT BULKHEAD LBL 40 TO RBL 35. FABRICATED AND INSTALLED NEW WEBS PER SRM 51-10- 02 AND SRM 51-40-03. TT: 66,991:57 HOURS. TC: 45,084. (X) 2 L 7 3 4F A3WE 1996091200142 19960912 00142 EU 1996 9 12 RAIA960804 1 19960805 A 7603 S2700004 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU CENTER CONSOLE DIRTY A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 573HK 76 41092 STL - FLT 7460 - CONFIGURATION WARNING CAME ON. MAINTENANCE CLEANED THE COND LEVER MICROSWITCHES. (X) 2 L 7 2 4T RT A41NM 1996091200143 19960912 00143 EU 1996 9 12 RAIA960812 1 19960811 A 5753 14157614406 FLAP JETAIR JETSTM JETSTM4101 1500501 EU RIGHT TE LIGHTNING STRIKE A RAIA K NONE C F.O.D. CR CRUISE 1 CE 03 566HK 899 41084 SBN - FLT 7489 - AIRCRAFT WAS STRUCK BY LIGHTNING DURING FLIGHT. MAINTENANCE FABRICATED AND APPLIED A PATCH TO THE RIG HT FLAP TRAILING EDGE IAW A.I.R. REPAIR DRAWING DRG141R1315 AND J41 SRM 51-20-04. AIRCRAFT TT: 899.9 HOURS. 2 L 7 2 4T RT A41NM 1996091200144 19960912 00144 NE 1996 9 12 RAIA960810 2 19960811 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE LEFT LIGHTNING STRIKE A RAIA K NONE C F.O.D. CR CRUISE 1 CE 03 566HK 899 41084 P75100 SBN - FLT 7489 - AIRCRAFT WAS STRUCK BY LIGHTNING DURING FLIGHT. MAINTENANCE REPLACED THE NR 1 ENGINE AND NR 1 PROPELLE R. (X) 2 L 7 2 4T 4 T RT A41NM E18NE 1996091200145 19960912 00145 NE 1996 9 12 RAIA960811 2 19960811 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE RIGHT LIGHTNING STRIKE A RAIA K NONE C F.O.D. CR CRUISE 1 CE 03 566HK 899 41084 P76101 SBN - FLT 7489 - AIRCRAFT WAS STRUCK BY LIGHTNING DURING FLIGHT. MAINTENANCE REPLACED THE NR 2 ENGINE AND THE NR 2 PROP ELLER. (X) 2 L 7 2 4T 4 T RT A41NM E18NE 1996091200146 19960912 00146 1996 9 12 RAIA960809 4 19960811 A 3417 7000700966 AIR DATA COMP JETAIR JETSTM JETSTM4101 1500501 EU AVIONICS BAY LOOSE A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 563HK 1153 41079 JFK - FLT 7663 - CAPTAIN'S ALTIMETER STICKING, ONLY INCREASES IN 200 FOOT INCREMENTS. MAINTENANCE RE-RACKED THE NR 1 AI R DATA COMPUTER. (X) 2 L 7 2 4T RT A41NM 1996091200147 19960912 00147 WP 1996 9 12 96ZZZX4349 1 19960724 A 3211 FITTING LKHEED 1011 10113851 5265010 WP LT MLG CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 312GB 193P1100 LEVEL 2 CORROSION, LT MAIN LANDING GEAR FITTING ON FORWARD TRUNNION, AFT LUG, FORWARD BUSHING LOOSE AND CORROSION UNDER FITTING. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 57-14-00. (X) 2 L 7 3 4F A23WE 1996091200148 19960912 00148 WP 1996 9 12 96ZZZX4350 1 19960724 A 5743 FITTING LKHEED 1011 10113851 5265010 WP LT MLG CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 312GB 193P1100 LEVEL 2 CORROSION, LEFT MAIN LANDING GEAR RIB FITTING INBOARD FACE IS RUSTED AND PITTED NEAR RETRACT ACTUATOR. REMOVED DAMAGED AREA AND REPAIRED PER SRM 57-14-00. (X) 2 L 7 3 4F A23WE 1996091200149 19960912 00149 WP 1996 9 12 96ZZZX4351 1 19960724 A 5315 FLOOR BEAM LKHEED 1011 10113851 5265010 WP BS 901 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 312GB 193P1100 LEVEL 2 CORROSION, FLOOR BEAM IS CORRODED FORWARD OF RT CART STOWAGE AREA AT FLOOR PANEL ATTACH HOLES FS 901. REMOVED D AMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-21-00. (X) 2 L 7 3 4F A23WE 1996091200150 19960912 00150 WP 1996 9 12 96ZZZX4352 1 19960724 A 5312 021201047 BULKHEAD BEAM LKHEED 1011 10113851 5265010 WP BS 1792 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 312GB 193P1100 LEVEL 2 CORROSION, FLOOR TO AFT BULKHEAD BEAM AROUND FASTENER HOLE IN C-3 BIN STA 1792, LBL 22. REPLACED BEAM PER SRM 5 1-10-05. (X) 2 L 7 3 4F A23WE 1996091200151 19960912 00151 WP 1996 9 12 96ZZZX4353 1 19960724 A 5320 021203738 SUPPORT LKHEED 1011 10113851 5265010 WP BS 1545/1565 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 312GB 193P1100 LEVEL 2 CORROSION, FLOOR SUPPORT UPPER SURFACE CORRODED AT LBL 32 BETWEEN STA 1545 AND STA 1565. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 51-10-05. (X) 2 L 7 3 4F A23WE 1996091200152 19960912 00152 WP 1996 9 12 96ZZZX4354 1 19960724 A 5320 021203236 SUPPORT LKHEED 1011 10113851 5265010 WP BS 1555 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 312GB 193P1100 LEVEL 2 CORROSION, FLOOR SUPPORT CORRODED AT STA 1555, LBL 2. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 51-10-05. (X) 2 L 7 3 4F A23WE 1996091200153 19960912 00153 WP 1996 9 12 96ZZZX4355 1 19960724 A 5320 SUPPORT LKHEED 1011 10113851 5265010 WP BS 1585-1605 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 312GB 193P1100 LEVEL 2 CORROSION, FLOOR SUPPORT CORRODED AT LBL 22 BETWEEN STA 1585 AND STA 1605. REMOVED DAMAGED SECTION OF FLOOR SUP PORT, FABRICATED AND INSTALLED REPAIR PER SRM 51-50-02. (X) 2 L 7 3 4F A23WE 1996091200155 19960912 00155 WP 1996 9 12 96ZZZX4357 1 19960724 A 5315 FLOOR BEAM LKHEED 1011 10113851 5265010 WP BS 923 CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 312GB 193P1100 LEVEL 2 CORROSION, CORROSION ON FLOOR BEAM AT FS 923, RLB 36, UNDER CART TIE DOWN. REMOVED DAMAGED SECTION OF BEAM, FAB RICATED AND INSTALLED REPAIR PER SRM 53-21-00. (X) 2 L 7 3 4F A23WE 1996091200156 19960912 00156 WP 1996 9 12 96ZZZX4358 1 19960724 A 5320 FRAME LKHEED 1011 10113851 5265010 WP CARGO DOOR CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 312GB 193P1100 LEVEL 2 CORROSION, C2 DOOR FRAME CORRODED ON LOWER FLANGE AT FS 1545, STR 26. REMOVED DAMAGED AREA, FABRICATED AND INST ALLED REPAIR PER SRM 51-50-02. (X) 2 L 7 3 4F A23WE 1996091200157 19960912 00157 WP 1996 9 12 96ZZZX4359 1 19960724 A 5320 FITTING LKHEED 1011 10113851 5265010 WP CABIN CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 312GB 193P1100 LEVEL 2 CORROSION, FLOOR SUPPORT CORRODED AT LEFT FIXED FLOOR PANEL, LBL 53, STA 1565 TO STA 1585 AND STA 1480 TO STA 15 05. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-24-00. (X) 2 L 7 3 4F A23WE 1996091200158 19960912 00158 NM 1996 9 12 AALA961015 1 19960706 A 3350 A3060698101 CONNECTOR BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 606AA 27057 JFK - DURING OVERNIGHT CHECK, FOUND EMERGENCY FLOOR LIGHTS AT MID-SECTION OF MAIN CABIN INOPERATIVE. REPLACED BROKEN EM ERGENCY FLOOR LIGHT CONNECTOR AT MID-SECTION OF MAIN CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1996091200159 19960912 00159 1996 9 12 MZZA96062 4 19960809 A 3417 07345290002 ADC BOEING 727 727264 138408M NM NR 1 MALFUNCTIONED A MZZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 623DH 20895 MNL - FLT 876 - NR 1 AND NR 2 GPS SHOW EXCESSIVE WINDS, 120 AT 215 KNOTS, TAS SHOWS 123 KNOTS AT ALL ATTITUDES. TAS INP UT FAILURE INDICATED ON NR 1 GPS. BOTH GPS UNRELIABLE. RETURNED TO MNL. REPLACED NPU NR 1 AND ADC NR 1 AND NR 2. OPS CHECK PER MM 34-12-11. OPS CHECK FOR NPU INTERFACE PER MM HT 9000 SATISFACTORY. REFERENCE: OPERATOR CONTROL NR 96ZZZ X4360. (X) 2 L 7 3 4F A3WE 1996091200160 19960912 00160 1996 9 12 96ZZZX4360 4 19960809 A 3417 07413090001 ADC BOEING 727 727264 138408M NM NR 2 MALFUNCTIONED A MZZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 623DH 20895 MNL - FLT 876 - NR 1 AND NR 2 GPS SHOW EXCESSIVE WINDS, 120 AT 215 KNOTS, TAS SHOWS 123 KNOTS AT ALL ATTITUDES. TAS INP UT FAILURE INDICATED ON NR 1 GPS. BOTH GPS UNRELIABLE. RETURNED TO MNL. REPLACED NPU NR 1 AND ADC NR 1 AND NR 2. OPS CHECK PER MM 34-12-11. OPS CHECK FOR NPU INTERFACE PER MM HT 9000 SATISFACTORY. REFERENCE: OPERATOR CONTROL NR MZZA9 6062. 2 L 7 3 4F A3WE 1996091200161 19960912 00161 NM 1996 9 12 MZZA96063 1 19960809 A 2612 1014A FIRE DETECTOR BOEING 727 727264 138408M NM APU FAILED A MZZA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 WP 13 624DH 20709 MNL - FLT 880 - AT CRUISE JUST PRIOR TO DESCENT, THE APU FIRE LIGHT AND ALARM WENT OFF. FIRE HANDLE WAS PULLED AND DISC HARGE BUTTON PUSHED. LIGHT REMAINED ILLUMINATED. REMOVED APU SHROUD AND CHECKED APU FOR EVIDENCE OF FIRE, NONE FOUND. SUSPECT FALSE WARNING. REINSTALLED PANELS AND DEACTIVATED APU PER DDP. AIRCRAFT RELEASED WITH APU INOPERATIVE PER MEL 49-01. (X) 2 L 7 3 4F A3WE 1996091200162 19960912 00162 NM 1996 9 12 MZZA96061 1 19960801 A 2612 65249203 FIRE DETECTION BOEING 727 727264 138408M NM EE COMPARTMENT FAILED A MZZA F ACTIVATE FIRE EXT. N FALSE WARNING IN INSP/MAINT 1 WP 13 624DH 20709 MNL - FLT 879 - ON GROUND IN MNL, CREW STARTED APU. AFTER APPROXIMATELY 8 MINUTES RECEIVED APU FIRE WARNING. CREW C/W EMERGENCY PROCEDURES TO PULL FIRE HANDLE AND FIRE BOTTLE. PER CREW COMMENTS, APU GENERATOR OPERATED NORMALLY - 116 VAC 403 CYC. FREQUENCY AND EGT ALSO REPORTED NORMAL. REMOVED APU SHROUD PANELS AND CHECKED FOR EVIDENCE OF FIRE. NO EVIDE NCE OF FIRE FOUND DURING INSPECTION. RE-INSTALLED AND SECURED PANELS, DEACTIVATED APU PER DDP 49-1 AND SECURED INOPERAT IVE APU PER MM 49-00, PAGE 220. AIRCRAFT RELEASED PER MEL 49-01. SUSPECT APU FIRE OVERHEAT AND DETECTOR UNIT AS THE SO URCE OF FALSE WARNING. FOUND MOISTURE AROUND UNIT AFTER VERY HEAVY RAINFALL. (X) 2 L 7 3 4F A3WE 1996091200163 19960912 00163 EU 1996 9 12 96ZZZX4361 1 19960729 A 2560 DOOR ASSIST BTL. AIRBUS 300 A300B4203 3930306 EU CABIN OUT OF ADJUST A P8NA K NONE O OTHER IN INSP/MAINT 1 SO 19 860PA 220 DURING A SPECIAL RIG CHECK, FOUND THREE DOORS THAT WERE NOT RIGGED PROPERLY AND WOULD NOT FIRE THE DOOR ASSIST BOTTLE. R E-RIGGED AND OPERATED NORMALLY, ADDED SPECIAL CHECK TO EACH C-CHECK. 2 L 7 2 4F A35EU 1996091200164 19960912 00164 NM 1996 9 12 W8PA960028 1 19960419 A 5320 SUPPORT BOEING 737 737301 1384611 NM BS 727 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 948WP 23259 DURING C-CHECK, FOUND CORROSION UNDER FLOOR SUPPORT AT BS 727D+15, LBL 3, LBL 8.10, AND LBL 12.5; WL 156. REMOVED DAMAG ED AREAS OF FLOOR SUPPORTS AND REPAIRED IAW SRM 53-00-53. (X) 2 L 7 2 4F RT A16WE 1996091200165 19960912 00165 NM 1996 9 12 W8PA960030 1 19960411 A 5330 SKIN BOEING 737 737301 1384611 NM BS 420 DENTED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 948WP 23259 FOUND SMOOTH DENT RT FUSELAGE .0937 INCH DEEP BY 3 INCH BY 2.5 INCH. REPAIRED IAW SRM 53-00-01 AND SRM 53-40-08. (X) 2 L 7 2 4F RT A16WE 1996091200166 19960912 00166 NM 1996 9 12 W8PA960029 1 19960419 A 5320 SUPPORT BOEING 737 737301 1384611 NM BS 727 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 948WP 23259 DURING C-CHECK, FOUND COROSION UNDER FLOOR SUPPORT AT BS 727D+A5, RBL 3, RBL 8.10, AND RBL 13.8; WL 156. REMOVED DAMAGE D AREAS OF FLOOR SUPPORTS AND REPAIRED IAW SRM 53-00-53. (X) 2 L 7 2 4F RT A16WE 1996091200167 19960912 00167 NM 1996 9 12 W8PA960032 1 19960416 A 5330 SKIN BOEING 737 737301 1384611 NM BS 947 DENTED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 948WP 23259 DURING C-CHECK, FOUND DENT ON FUSELAGE SKIN. DENT MEASURES 6 INCHES LONG AND 3.7 INCHES WIDE AND 0.12 INCH DEEP. REMOV ED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PATCH IAW SRM 53-00-01. (X) 2 L 7 2 4F RT A16WE 1996091200168 19960912 00168 NM 1996 9 12 W8PA960034 1 19960418 A 5315 FLOOR BEAMS BOEING 737 737301 1384611 NM BS 727 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 948WP 23259 DURING C-CHECK, FOUND CORROSION AT NUTPLATES AT NUMEROUS LOCATIONS AT FLOOR STRAP, AFT CARGO BAY; BS 727D-5; LBL 40; WL 156. REMOVED STRAP, FOUND DAMAGED FLOOR BEAMS, REMOVED DAMAGED AREAS OF FLOOR BEAMS AND REPAIRED IAW SRM 53-0-53. (X) 2 L 7 2 4F RT A16WE 1996091200169 19960912 00169 NM 1996 9 12 W8PA960033 1 19960417 A 5320 SUPPORT BOEING 737 737301 1384611 NM BS 794 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 948WP 23259 DURING C-CHECK, FOUND CORROSION ON BOTTOM SIDE OF FLOOR SUPPORT AROUND NUTPLATE AT BS 794, LBL 3, WL 158. FLOOR SUPPORT EXFOLIATED BEYOND LIMITS. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 53-00-53. (X) 2 L 7 2 4F RT A16WE 1996091200170 19960912 00170 NM 1996 9 12 W8PA960031 1 19960416 A 5320 ANGLE BOEING 737 737301 1384611 NM BS 500 CRACKED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 948WP 23259 DURING C-CHECK, FOUND CRACKED SUPPORT ANGLE UNDER FORWARD CARGO BAY FLOOR AT BS 550 AND LBL 2 AND WL 155. REMOVED AND R EPLACED DAMAGED ANGLE. (X) 2 L 7 2 4F RT A16WE 1996091200171 19960912 00171 NM 1996 9 12 W8PA960036 1 19960425 A 5753 SKIN BOEING 737 737301 1384611 NM RT TE FOREFLAP PUNCTURED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 948WP 23259 DURING C-CHECK, FOUND SMALL PUNCTURE ON UNDERSIDE OF INBOARD FOREFLAP JUST OUTBOARD OF CENTER TRACK. REPAIRED IAW SRM 5 1-70-10. (X) 2 L 7 2 4F RT A16WE 1996091200172 19960912 00172 NM 1996 9 12 W8PA960035 1 19960417 A 5320 ANGLE BOEING 737 737301 1384611 NM BS 344 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 948WP 23259 DURING C-CHECK, FOUND CRACK IN ATTACH ANGLE COMMON TO CLOSE-OUT WEB IN FORWARD ENTRY DOORWAY, AFT END OF FUSELAGE CUT-OU T. REMOVED AND REPLACED DAMAGED ANGLE IAW SRM 51-20-02. (X) 2 L 7 2 4F RT A16WE 1996091200173 19960912 00173 NM 1996 9 12 W8PA960037 1 19960425 A 5730 PANEL BOEING 737 737301 1384611 NM LEFT WING CRACKED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 948WP 23259 DURING C-CHECK, FOUND UPPER PANEL JUST INBOARD OF NR 3 TRANSMISSION CRACKED. REPAIRED IAW SRM 51-70-10. (X) 2 L 7 2 4F RT A16WE 1996091200174 19960912 00174 NM 1996 9 12 W8PA960038 1 19960417 A 5730 SKIN BOEING 737 737301 1384611 NM LEFT WING GOUGED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 948WP 23259 DURING C-CHECK, FOUND FIXED LEADING EDGE GOUGED. REPAIRED IAW SRM 51-70-11. (X) 2 L 7 2 4F RT A16WE 1996091200175 19960912 00175 NM 1996 9 12 W8PA960042 1 19960418 A 5753 SKIN BOEING 737 737301 1384611 NM LT TE FOREFLAP PUNCTURE A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 948WP 23259 DURING C-CHECK, FOUND INBOARD FOREFLAP HAS PUNCTURE ON LOWER SKIN. REPAIRED IAW SRM 57-70-10. (X) 2 L 7 2 4F RT A16WE 1996091200176 19960912 00176 NM 1996 9 12 W8PA960041 1 19960422 A 5720 ANGLE BOEING 737 737301 1384611 NM RIGHT WING CRACKED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 948WP 23259 DURING C-CHECK, FOUND SUPPORT ANGLE FOR UPPER SURFACE PANEL CRACKED (INBOARD OF INBOARD-MOST SPEED BRAKE, DIRECTLY ABOVE NR 5 FLAP TRACK). REPAIRED IAW SRM 51-30-01. (X) 2 L 7 2 4F RT A16WE 1996091200177 19960912 00177 NM 1996 9 12 W8PA960040 1 19960417 A 5413 LONGERON BOEING 737 737301 1384611 NM LEFT PYLON GOUGED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 948WP 23259 DURING C-CHECK, FOUND LEFT PYLON INBOARD UPPER LONGERON CRACKED. REPAIRED IAW SRM 51-40-02. (X) 2 L 7 2 4F RT A16WE 1996091200178 19960912 00178 NM 1996 9 12 W8PA960039 1 19960417 A 5730 PANEL BOEING 737 737301 1384611 NM LEFT WING GOUGED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 948WP 23259 DURING C-CHECK, FOUND UPPER OUTBOARD TRAILING EDGE PANEL DELAMINATED. REPAIRED IAW SRM 51-70-03. (X) 2 L 7 2 4F RT A16WE 1996091200179 19960912 00179 EU 1996 9 12 JBXA9600013 1 19960703 A 2450 740518C GPCU FOKKER F28 F28MK0100 4990807 EU E/E BAY FAILED A JBXA O OTHER J WARNING INDICATION CL CLIMB 1 SO 05 131ML 0220 11323 PBI - FLT 888 - AFTER TAKEOFF, THE FOLLOWING OCCURRED: 1. PROXIMITY SWITCH SYSTEM INOPERATIVE. 2. CAB PRESSURE CTL C HAN. 3. GROUND FLT CONTROL. 4. AFCAS MAINTENANCE REQ. 5. NR 2 YAW DAMPENER AND FLIGHT DIRECTOR INOPERATIVE. 6. T HREE-CHIME TAKEOFF CONFIGURATION WARNING, UNABLE TO CANCEL. CORRECTIVE ACTION: PERFORMED OPS CHECK ON AC CONTROL SYSTE M. NO FAULTS. REMOVED AND REPLACED NR 2 GCU IAW FMM 24-21-02, OPS NORMAL. OPS CHECK GPCU FAILED. REMOVED AND REPLACE D GPCU IAW FMM 24-41-00, OPS NORMAL ON GROUND. NO FAULTS. (X) 2 L 7 2 4F RT 1996091200180 19960912 00180 NM 1996 9 12 USAABB96020 1 19960725 A 3350 8731002511 LIGHT BOEING 757 7572B7 1384964 NM R1 DOOR INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 619AU 27198 BDL - EMERGENCY EXIT DOOR LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (X) 2 L 7 2 4F RT A2NM 1996091200181 19960912 00181 CE 1996 9 12 96ZZZX4362 1 19960716 A 5270 MS250081 SWITCH BEECH 1900 1900D 1154162 CE AFT CARGO DOOR OUT OF ADJUST A AMWA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 07 166YV 954 UE166 OMA - FLT 5721 - AIRCRAFT RETURNED TO FIELD AT OMA WHEN AFT CARGO DOOR AJAR LIGHT CAME ON AFTER TAKEOFF. MAINTENANCE CO NTROL DEFERRED IAW MEL AND WAS RETURNED TO SERVICE. MAINTENANCE ADJUSTED DOOR AJAR SWITCH SYSTEM, OPS CHECKED NORMAL. 2 L 7 2 4T RT A24CE 1996091200182 19960912 00182 NM 1996 9 12 AWXA960336 1 19960712 A 2932 ST107RM1 TRANSMITTER BOEING 737 7373Y0 1384671 NM A-SYSTEM FAILED A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 28 EICKV VP065 23747 BWI/CMH - FLT 2401 - AIR TURNBACK. A-SYSTEM HYDRAULIC PRESSURE LOSS. CONTRACT MAINTENANCE VERIFIED INDICATION ONLY, BU T HAVE HYDRAULIC TRANSFER FROM B-SYSTEM TO A-SYSTEM. WHILE TROUBLESHOOTING, NOTED HYDRAULIC FLUID FLOWING FROM RESERVOI R OVERFILL TUBE WHEN STANDBY PUMP RUNNING. A-SYSTEM UNPRESSURIZED. NOTE: B-SYSTEM RESERVOIR DOWN BELOW REFILL MARK. REMOVED AND REPLACED NR 1 ENGINE THRUST REVERSER SHUTTLE VALVE PER MM 78-34-11. LEAK CHECK GOOD. PLACED ON MEL 29-03. REMOVED AND REPLACED TRANSMITTER FOR A-HYDRAULIC SWITCH. OPS CHECK AND LEAK CHECK GOOD. MEL CLEARED. (X) 2 L 7 2 4F RT A16WE 1996091200183 19960912 00183 SO 1996 9 12 96ZZZX4363 1 19960715 A 5210 159BM1021677 FITTING GULSTM G1159 G1159 3953505 SO CABIN DOOR BROKEN A BTVA K NONE O OTHER IN INSP/MAINT 1 GL 23 802CC 7537 187 187 MAIN CABIN DOOR WOULD NOT CLOSE. CABIN DOOR ACTUATOR UPPER ATTACH POINT BRACKET BROKEN. REPAIRED STRINGER, REPLACED CH ANNEL AND FITTING, P/N'S 159B10456-23 AND 159BM10216-77. 2 L 7 2 4F RT A12EA 1996091200184 19960912 00184 NM 1996 9 12 96ZZZX4364 1 19960723 A 3397 WIRE BOEING 737 737317 138447P NM CABIN EXPOSED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 EICHH 15 23177 DEN - FLT 752 - UPON ARRIVAL, FLIGHT CREW REPORTED EMERGENCY AISLE PATH LIGHTING WIRES EXPOSED AT ROW 11. MAINTENANCE R EPAIRED WIRING AND SYSTEM CHECKED OKAY. 2 L 7 2 4F RT A16WE 1996091200185 19960912 00185 CE 1996 9 12 96ZZZX4365 1 19960704 A 3213 508100324 TORQUE LINK BEECH 90 C90 1152913 CE LT MLG FAILED A A AOBA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 EA 11 369GA 6413 LJ934 LEFT MLG UPPER TORQUE LINK FAILED AT THE PIVOT POINT WITH THE LOWER TORQUE LINK. AN EMERGENCY LANDING WAS EXECUTED. AT TOUCH-DOWN, THE LEFT LOWER STRUT, WHEEL AND TIRE ASSY DEPARTED AIRCRAFT DAMAGING THE UPPER STRUT HOUSING, INBOARD FLAP, AND THE LEFT SIDE OF THE FUSELAGE AT STA 340.0. APPEARS THE TORQUE LINK FAILURE WAS AT THE GREASE FITTING HOLE. PART TOTAL TIME: 6,413 HOURS. PART TOTAL CYCLES, 7,300. TIME SINCE LAST 7,500 CYCLE/60 MONTH INSPECTION, 2,385 HOURS. CYCL ES SINCE LAST 7,500 CYCLE/60 MONTH INSPECTION, 3,273. MONTHS SINCE LAST 7,500 CYCLE/60 MONTH INSPECTION, 50. 1 L 7 2 3T 3A20 1996091200186 19960912 00186 NM 1996 9 12 P2EA96004 1 19960706 A 5754 65671731 TRACK RIB BOEING 737 737222 1384473 NM NR 6 LE FLAP WORN A P2EA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 CE 05 603DJ 19955 DEN - FLT 48 - THE NR 6 SLAT WOULD NOT FULLY RETRACT AFTER TAKEOFF. (RETURN TO DEN, NO EMERGENCY DECLARED, LANDING UNEV ENTFUL.) REMOVED AND REPLACED INBOARD AND CENTER AUXILIARY TRACK RIBS ON NR 6 SLAT. ADJUSTED IAW MM 27-81-21. OPS CHE CK GOOD. (X) 2 L 7 2 4F A16WE 1996091200187 19960912 00187 EU 1996 9 12 96ZZZX4366 1 19960709 A 2731 SD3456028XA CONTROL CABLE STBROS SD3 SD360 8100606 EU ELEVATOR TRIM BROKEN A A TRBA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 21 384MQ SH3711 PILOT RETURNED FOR A LANDING DUE TO ELEVATOR TRIM FAILURE. ELEVATOR TRIM CABLE, P/N SD3-45-6028XA, FOUND BROKEN AND REP LACED PER MM 27-32-00. THIS CABLE IS COVERED IN EXECUTIVE MAINTENANCE PROGRAM WITH A 4,800 FH INSPECTION CONSTRAIN. EX ECUTIVE ISSUED BACK IN 1994 AN ENGINEERING ORDER TO INSPECT THIS CABLE AT 2,400 FH (EO 27-00-003). EXECUTIVE WILL REVIE W ALL DATA AVAILABLE FOR THIS CABLE TO CORRECT OR CHANGE INSPECTION INTERVAL TO THIS ITEM IF CONSIDERED NECESSARY. MANU FACTURER WILL BE CONTACTED FOR ANY AVAILABLE INFORMATION. 2 H 7 2 4T A41EU 1996091200191 19960912 00191 EU 1996 9 12 HCMA9632 1 19960806 A 6520 350A33215300 LAMIFICATION SNIAS 350 AS350BA 8680817 EU REAR ROTOR WORN EXCESS E HCMA K NONE O OTHER NR NOT REPORTED 1 WP 13 312B 290 2243 REAR ROTOR LAMIFICATION IS WORN EXCESSIVELY. REMOVED AND REPLACED. 1 G 7 1 3U NC H9EU 1996091200192 19960912 00192 EU 1996 9 12 HCMA9633 1 19960813 A 6520 350A33215300 LAMIFICATION SNIAS 350 AS350BA 8680817 EU REAR ROTOR CRACKED E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 532BH 155 2494 REAR ROTOR LAMIFICATION IS CRACKED. 1 G 7 1 3U NC H9EU 1996091200193 19960912 00193 EU 1996 9 12 HCMA9634 1 19960813 A 6520 350A33215300 LAMIFICATION SNIAS 350 AS350BA 8680817 EU REAR ROTOR CRACKED E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 532BH 195 2494 REAR ROTOR LAMIFICATION IS CRACKED. 1 G 7 1 3U NC H9EU 1996091200194 19960912 00194 EU 1996 9 12 HCMA9635 1 19960815 A 6520 350A33215300 BEARING SNIAS 350 AS350BA 8680817 EU T/R WORN EXCESS E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 642BH 646 2495 BEARING IS WORN EXCESSIVELY. 1 G 7 1 3U NC H9EU 1996091200195 19960912 00195 EU 1996 9 12 HCMA9636 1 19960815 A 6410 355A09103600 BEARINGS SNIAS 350 AS350BA 8680817 EU T/R WORN EXCESS E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 642BH 942 2495 BEARING IS WORN EXCESSIVELY. REMOVED AND REPLACED. 1 G 7 1 3U NC H9EU 1996091200196 19960912 00196 EU 1996 9 12 HCMA9637 1 19960815 A 6520 350A33215300 BEARINGS SNIAS 350 AS350BA 8680817 EU T/R WORN EXCESS E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 752BH 665 2510 BEARING IS WORN EXCESSIVELY. 1 G 7 1 3U NC H9EU 1996091200197 19960912 00197 EU 1996 9 12 HCMA9638 1 19960815 A 6520 350A33215300 BEARINGS SNIAS 350 AS350BA 8680817 EU T/R WORN EXCESS E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 862BH 226 2713 BEARING IS WORN EXCESSIVELY. 1 G 7 1 3U NC H9EU 1996091200198 19960912 00198 EU 1996 9 12 HCMA9639 1 19960815 A 6520 350A33215300 LAMIFICATION SNIAS 350 AS350B2 8680813 EU T/R CRACKED E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 972BH 374 2804 REAR ROTOR LAMIFICATION IS CRACKED. 1 G 7 1 3U H9EU 1996091200199 19960912 00199 EU 1996 9 12 HCMA9640 1 19960815 A 6520 350A33215300 LAMIFICATION SNIAS 350 AS350B2 8680813 EU T/R TORN RUBBER E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 982BH 369 2876 RUBBER IS TORN BEYOND LIMITS. 1 G 7 1 3U H9EU 1996091200200 19960912 00200 EU 1996 9 12 HCMA9641 1 19960815 A 6520 350A33215300 REAR ROTOR LAMIF SNIAS 350 AS350B2 8680813 EU T/R CRACKED E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 992BH 495 2889 LAMIFICATION IS CRACKED. 1 G 7 1 3U H9EU 1996091200201 19960912 00201 EU 1996 9 12 HCMA9642 1 19960815 A 6520 350A33215300 REAR ROTOR LAMIF SNIAS 350 AS350B2 8680813 EU T/R CRACKED E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 992BH 42 2889 LAMIFICATION IS CRACKED. 1 G 7 1 3U H9EU 1996091200202 19960912 00202 EU 1996 9 12 HCMA9643 1 19960816 A 6520 350A33215300 BEARINGS SNIAS 350 AS350BA 8680817 EU T/R WORN EXCESS E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 862BH 881 2713 BEARING IS WORN EXCESSIVELY. 1 G 7 1 3U NC H9EU 1996091200203 19960912 00203 EU 1996 9 12 HCMA9644 1 19960816 A 6520 350A33200403 SPIDER SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE T/R P/C BINDING E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 992BH 993 2889 T/R P/C SPIDER BINDING WHEN RIGHT PEDAL IS APPLIED. 1 G 7 1 3U 3 U H9EU E19EU 1996091200204 19960912 00204 EU 1996 9 12 HCMA9645 1 19960816 A 6220 704A33633109 SPHERICAL STOP SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE M/R CRACKED E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 992BH 997 2889 9402 SPHERICAL STOPS ARE CRACKING.S/N 9528,9529,&9527 1 G 7 1 3U 3 U H9EU E19EU 1996091200205 19960912 00205 EU 1996 9 12 HCMA9646 1 19960816 A 6710 SC5083 SERVO SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE M/R DEFECTIVE E HCMA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 13 992BH 997 2889 9402 SERVO IS SEEPING BEYOND LIMITS. REPLACEMENT PART IS ON ORDER 1 G 7 1 3U 3 U H9EU E19EU 1996091200206 19960912 00206 EU 1996 9 12 HCMA9647 1 19960816 A 6520 350A33215300 BEARINGS SNIAS 350 AS350B2 8680813 EU T/R CRACKED E HCMA K NONE E VIBRATION/BUFFET IN INSP/MAINT 1 WP 13 972BH 400 2804 BEARING CAUSED T/R FREQUENCY VIBRATIONS. WORN BEYOND LIMITS. 1 G 7 1 3U H9EU 1996091200207 19960912 00207 EU 1996 9 12 HCMA9648 1 19960816 A 6520 7704411 SEAL SNIAS 350 AS350B2 8680813 EU T/R DEFECTIVE E HCMA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 13 992BH 951 2889 MAGNETIC SEAL IS LEAKING. 1 G 7 1 3U H9EU 1996091200208 19960912 00208 EU 1996 9 12 HCMA9649 1 19960816 A 6410 355A09103601 BEARING SNIAS 350 AS350B2 8680813 EU T/R CRACKED E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 992BH 951 2889 BEARING WORN BEYOND LIMITS. CRACKED 1 G 7 1 3U H9EU 1996091200209 19960912 00209 EU 1996 9 12 HCMA9650 1 19960816 A 2820 571712A VALVE SNIAS 350 AS350B2 8680813 EU FUEL BY PASS DEFECTIVE E HCMA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 13 992BH 977 2889 BY-PASS VALVE HOUSING LEAKING. 1 G 7 1 3U H9EU 1996091200210 19960912 00210 1996 9 12 HCMA9651 4 19960816 A 3421 5050010902 GYRO SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE COCKPIT DG DEFECTIVE E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 193BH 41 2894 9406 INOP. SEE JUDY SMITH FOR REPLACEMENT PART DATA. 1 G 7 1 3U 3 U H9EU E19EU 1996091200211 19960912 00211 EU 1996 9 12 HCMA9652 1 19960819 A 6520 350A33215300 LAMIFICATION SNIAS 350 AS350B2 8680813 EU T/R TORN RUBBER E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 982BH 204 2876 RUBBER IS TORN BEYOND LIMITS AND THERE IS NO "J" GAP. 1 G 7 1 3U H9EU 1996091200212 19960912 00212 NE 1996 9 12 HCMA9655 2 19960819 A 7421 9550168770 IGNITOR SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE ENGINE DEFECTIVE E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 992BH 947 2889 IGNITOR INOP. 1 G 7 1 3U 3 U H9EU E19EU 1996091200213 19960912 00213 GL 1996 9 12 HEEA967693 2 19960826 A 7240 6899081 LINER BELL 206 206L3 1182108 SW ALLSN 250C 250C30 03013 GL COMBUSTION MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 108PH 51334 RECEIVING INSPECTION REVEALED: ALIGNMENT 1/2 HOLE OFF TO RIGHT ON COMB LINER PIN. LINER TRIED ON SEVERAL TURBINES AND U NABLE TO INSTALL FUEL NOZZLE WITH IGNITOR AND DUMMY PLUG IN PLACE. UNABLE TO INSTALL IGNITOR PLUG WITH FUEL NOZZLE AND DUMMY PLUG INSTALLED. REPLACED DISCREPANT PART. 1 G 7 1 3U 3 U H2SW E1GL 1996091200214 19960912 00214 SW 1996 9 12 HEEA967694 1 19960828 A 6410 222016001115 BLADE BELL 230 230 1182149 SW T/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 565 23009 BLADE IS CRACKED. BEARINGS P/N 222-312-753-103, 4 EACH BEARINGS ON BOTH BLADES ARE CRACKED. REPLACED BLADES. 1 G 7 2 3U NC H9SW 1996091200215 19960912 00215 1996 9 12 HEEA967696 4 19960829 A 3452 066106200 TRANSCEIVER KT76 AEROSP AS355 AS355F1 8680810 EU COCKPIT ATC INTERMITTENT E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5793Z 5142 INTERMITTENT TRANSMIT. VERIFIED UNIT TO HAVE LOW POWER OUT. TRIED ADJUSTING POWER TO SPECS. NO HELP. REPLACED CAVITY TUBE V101. REPAIRED. ADJUSTED FREQUENCY. COOKED UNIT UNDER HEAT LAMP, VIBRATED AND PUT IN FREEZER. FREQUENCY REMAINE D STEADY. BENCH CHECK GOOD. 1 G 7 2 3U H11EU 1996091200216 19960912 00216 1996 9 12 HEEA967697 4 19960829 A 3452 066106200 TRANSCEIVER KT76 BOLKMS 105 BO105S 5626006 EU COCKPIT ATC DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 724MB S756 REPAIR CRACKED FACEPLATE. REPLACED BROKEN FACEPLATE ASSEMBLY. ALSO REPLACED WEAK V101 CAVITY OSCILLATOR BECAUSE OF LOW POWER OUT. ADJUSTED AS NEEDED. BENCH CHECK GOOD. 1 G 7 2 3U H3EU 1996091200217 19960912 00217 1996 9 12 HEEA967698 4 19960829 A 3444 066305401 INDICATOR KI250 BOLKMS 105 BO105S 5626006 EU RADAR ALT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 133AE S800 CRACKED GLASS. REPLACED GLASS, BEZEL AND LOCK NUT. REPAIRED. PERFORMED TOTAL CALIBRATION AND ALIGNMENT. INSTALLED 28 VOLT DECAL. BENCH CHECK GOOD. 1 G 7 2 3U H3EU 1996091200218 19960912 00218 1996 9 12 HEEA967699 4 19960829 A 2312 064101701 TRANSCEIVER KAC952 BELL 212 212 1181420 SW COCKPIT VHF MALFUNCTION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5010F 30936 TRANSCEIVER WILL NOT TUNE. 1 G 7 1 4U H4SW 1996091200219 19960912 00219 1996 9 12 HEEA967700 4 19960829 A 2312 064105430 TRANSCEIVER BOLKMS 105 BO105S 5626006 EU COCKPIT VHF DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 624MB S751 STANDBY SIDE HAS BURNT SEGMENTS. 1 G 7 2 3U H3EU 1996091200221 19960912 00221 1996 9 12 HEEA967702 4 19960829 A 2312 40001452500 TRANSCEIVER RT138F BELL 206 206L1 1182107 SW COCKPIT VHF WEAK E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 50046 45173 WEAK TRANSMIT POWER OUT. 1 G 7 1 3U H2SW 1996091200222 19960912 00222 SW 1996 9 12 HEEA967703 1 19960829 A 6210 412015300109 BLADE BELL 412 412 1182202 SW M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2014K 6051 33020 BLADE IS CRACKED. (TWO CHORDWISE CRACKS ON THE OUTBOARD LEADING EDGE STRIP. THE FIRST CRACK IS AT STATION 180" WHICH I S COMPLETELY CHORDWISE. THE SECOND CRACK IS AT STATION 199.5 WHICH IS ONLY A PARTIAL CHORDWISE CRACK. 1 G 7 2 4U H4SW 1996091200223 19960912 00223 SW 1996 9 12 HEEA967704 1 19960829 A 6210 412015300109 BLADE BELL 412 412 1182202 SW M/R SEP[ARATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3911L 9817 33023 BLADE FRETTING PADS ON THE UPPER SURFACE ARE SEPARATED BEYOND LIMITS. 1 G 7 2 4U H4SW 1996091200224 19960912 00224 1996 9 12 HEEA967705 4 19960829 A 2312 064102300 TRANSCIEVER BOLKMS 105 BO105S 5626006 EU COCKPIT VHF DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 6607K S841 LOUD SQUEAL IN RADIO. 1 G 7 2 3U H3EU 1996091200226 19960912 00226 1996 9 12 HEEA967707 4 19960829 A 3442 MI5851345 INDICATOR P40 SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1545X 760050 UNIT HAS A BAD TEST PATTERN AND ALL GREEN DISPLAY. 1 G 7 2 3U H1NE 1996091200227 19960912 00227 1996 9 12 HEEA967708 4 19960829 A 2312 066106600 TRANSCEIVER BELL 212 212 1181420 SW COCKPIT INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1082G 31109 TRANSCEIVER INOPERATIVE. REPLACED BURNT F1 FUSE, SHORTED Q123 TRANSISTOR, SHORTED Q105 TRANSISTOR AND BURNT R114 RESISTO R. INSTALLED TRANSMITTER SHIELD. INSPECTED AND BENCH CHECK GOOD. 1 G 7 1 4U H4SW 1996091200228 19960912 00228 1996 9 12 HEEA967709 4 19960829 A 3442 MI585200 RADAR RT SKRSKY S76 S76A 8143006 NE COCKPIT MALFUNCTION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 22342 760096 BLOWS FUSE AND RADAR INDICATOR SCREEN FLASHES RED IN FLIGHT. 1 G 7 2 3U H1NE 1996091200229 19960912 00229 1996 9 12 HEEA967710 4 19960829 A 3457 0110005400 GPS 150 BELL 206 206L1 1182107 SW COCKPIT GPS FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5000K 45167 DATA CARD FAILURE ON DISPLAY. 1 G 7 1 3U H2SW 1996091200230 19960912 00230 SW 1996 9 12 HEEA967711 1 19960829 A 7722 206375007103 INDICATOR BELL 206 206L1 1182107 SW COCKPIT TOT STUCK E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2135V 45657 NEEDLE STUCK AT ZERO DEGREES, WON'T INDICATE. 1 G 7 1 3U H2SW 1996091200231 19960912 00231 1996 9 12 HEEA967712 4 19960829 A 2370 9806019001 CVR BELL 412 412 1182202 SW COCKPIT WONT TEST E HEEA K NONE L NO TEST NR NOT REPORTED 1 SW 03 108X 1921 33115 CVR DOES NOT TEST. TIME SINCE REPAIR 165:25. 1 G 7 2 4U H4SW 1996091200232 19960912 00232 1996 9 12 HEEA967713 4 19960829 A 3442 MI5852013 INDICATOR P4001 BEECH 200 200CBEECH 1152926 CE COCKPIT MALFUNCTION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 39PH BL3 VERTICAL ORANGE LINES IN ALL RANGE SETTINGS. 1 L 7 2 4T A24CE 1996091200233 19960912 00233 1996 9 12 HEEA967714 4 19960829 A 2370 9806019001 CVR SKRSKY S76 S76A 8143006 NE COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22342 3029 760096 CVR SYSTEM INSPECTION DUE. TAPE IS NOISY AND SPEECH HARD TO DISTINGUISH. 1 G 7 2 3U H1NE 1996091200234 19960912 00234 1996 9 12 HEEA967715 4 19960829 A 3442 MI5853001 RT UNIT SKRSKY S76 S76A 8143006 NE RADAR FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 476X 760436 RT UNIT WILL NOT POWER UP RADAR INDICATOR. 1 G 7 2 3U H1NE 1996091200235 19960912 00235 1996 9 12 HEEA967716 4 19960829 A 3452 066106200 TRANSCEIVER KT76 SNIAS 350 AS350B2 8680813 EU COCKPIT ATC DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 350BZ 2653 WEAK TRANSMIT. REPLACED CAVITY OSCILLATOR V101. REPAIRED. COOKED UNIT UNDER HEAT LAMP, VIBRATED AND PUT IN FREEZER. B ENCH CHECK GOOD. 1 G 7 1 3U H9EU 1996091200236 19960912 00236 NE 1996 9 12 HEEA967717 1 19960830 A 6210 7615009043050 TIP CAP SKRSKY S76 S76A 8143006 NE M/R SKIN BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31219 760230 FIBERGLASS SKIN BROKEN BETWEEN INNER AND OUTER DOUBLERS ON THE LOWER SIDE. THE LEADING EDGE ABRASION STRIP HAS A CRACK WITH A STOP DRILL. 1 G 7 2 3U H1NE 1996091200237 19960912 00237 NE 1996 9 12 HEEA967718 1 19960830 A 6210 7615009043050 TIP CAP SKRSKY S76 S76A 8143006 NE M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911MJ 760231 CRACK IN THE ABRASION STRIP ON THE LOWER SIDE WITH SEPARATION. 1 G 7 2 3U H1NE 1996091200238 19960912 00238 NE 1996 9 12 HEEA967719 1 19960830 A 6210 7615009100051A BLADE SKRSKY S76 S76A 8143006 NE M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911MJ 7693 760231 BLADE IS CRACKED. (BLADE HAS THE TIP RIB UNBONDED, AND A CRACK AT STATION 112" WITH SEPARATION ON EACH SIDE OF THE CRAC K ON THE LEADING EDGE. 1 G 7 2 3U H1NE 1996091200239 19960912 00239 EU 1996 9 12 HEEA967720 1 19960830 A 6410 10531980 BLADE 10531713 BOLKMS 105 BO105S 5626006 EU T/R DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81982 1587 51124 S818 RUBBER THRUST PLATE CHIPPED. 1 G 7 2 3U H3EU 1996091200240 19960912 00240 EU 1996 9 12 HEEA967721 1 19960830 A 6410 10531980 BLADE 10531713 BOLKMS 105 BO105S 5626006 EU T/R DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 54197 689 150 S805 LEADING EDGE DAMAGE. 1 G 7 2 3U H3EU 1996091200241 19960912 00241 1996 9 12 HEEA967722 4 19960830 A 2370 9806019001 CVR BELL 214 214ST 1182106 SW COCKPIT MALFUNCTION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3897N 28106 CVR GETS AUDIO ON TEST BUT NO LIGHT. 2 G 7 2 4U H10SW 1996091200242 19960912 00242 1996 9 12 HEEA967723 4 19960830 A 2370 9806019001 CVR BELL 412 412 1182202 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2298Z 33077 CVR HAS HIGH PITCH SQUEAL ON TAPE. 1 G 7 2 4U H4SW 1996091200243 19960912 00243 1996 9 12 HEEA967724 4 19960830 A 2312 064100900 TRANSCEIVER KTR905 BELL 412 412 1182202 SW COCKPIT WEAK E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3893N 33010 RECEIVE WEAK. 1 G 7 2 4U H4SW 1996091200244 19960912 00244 1996 9 12 HEEA967725 4 19960830 A 2312 40001452500 TRANSCEIVER RT138F BOLKMS 105 BO105S 5626006 EU COCKPIT DISTORTED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 818SH S753 HAS DISTORTION ON TRANSMIT TONE DEVIATION. 1 G 7 2 3U H3EU 1996091200245 19960912 00245 1996 9 12 HEEA967726 4 19960830 A 3451 066106600 TRANSCEIVER BELL 412 412 1182202 SW COCKPIT DME FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 22347 36005 NO DISPLAY ON #1 OR #2 DME. 1 G 7 2 4U H4SW 1996091200246 19960912 00246 1996 9 12 HEEA967727 4 19960830 A 2312 064105430 TRANSCEIVER BELL 206 206L1 1182107 SW COCKPIT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 513EH 45421 DISPLAY BLANKS OUT IN FLIGHT INTERMITTENTLY. CAN STILL TRANSMIT AND RECEIVE WHEN DISPLAY GOES OUT. 1 G 7 1 3U H2SW 1996091200247 19960912 00247 1996 9 12 HEEA967728 4 19960830 A 3444 066104800 ALTIMETER KRA405 BELL 412 412 1182202 SW COCKPIT RAD ALT WONT TEST E HEEA K NONE L NO TEST NR NOT REPORTED 1 SW 03 2148K 36001 WILL NOT TEST CORRECTLY. REPLACED CAL/LOOP BOARD. REPAIRED. INSTALLED MOD 10 AS PER KING SERVICE BULLETIN KRA405-10. A DJUSTED 500 FOOT TRIP. BENCH CHECK GOOD. 1 G 7 2 4U H4SW 1996091200248 19960912 00248 1996 9 12 HEEA967729 4 19960830 A 3455 066104701 RECEIVER BELL 412 412 1182202 SW COCKPIT ADF MALFUNCTION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2258F 33073 RECEIVER INOPERATIVE. WEAK RECEIVE IN ANTENNA MODE. 1 G 7 2 4U H4SW 1996091200249 19960912 00249 1996 9 12 HEEA967730 4 19960830 A 3444 066104802 ALTIMETER BELL 412 412 1182202 SW RADAR ALT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2261D 33076 RADAR ALTIMETER DOES NOT TEST OR INDICATE ALTITUDE. FOUND STRIPLINE ASSY TO BE BAD CAUSING RESISTOR R708 ON OSCILLATOR C IRCUIT REGULATOR ASSY TO BURN. ALSO FOUND WHEN UNIT IS VIBRATED, NEEDLE FLUCTUATES. FOUND CAL/LOOP BOARD TO BE BAD. 1 G 7 2 4U H4SW 1996091200250 19960912 00250 1996 9 12 HEEA967731 4 19960830 A 3454 071121627 CONTROL BELL 412 412 1182202 SW NR 2 VOR MALFUNCTION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 107X 33113 #2 VOR SWITCHES BETWEEN FREQUENCIES ON IT'S OWN. COULD NOT DUPLICATE PROBLEM, BUT FOUND PHOTOCELL (V101) NOT DIMMING. R EPLACED V101 PHOTOCELL. REPAIRED. BENCH CHECK GOOD. 1 G 7 2 4U H4SW 1996091200251 19960912 00251 1996 9 12 HEEA967732 4 19960830 A 2312 071121525 CONTROL UNIT BELL 412 412 1182202 SW COCKPIT MALFUNCTION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 108X 33115 SQUELCH IS CONSTANTLY DISABLED (BY VIBRATION OR SIGNAL RECEPTION) 1 G 7 2 4U H4SW 1996091200252 19960912 00252 1996 9 12 HEEA967733 4 19960830 A 3444 066104802 ALTIMETER BOLKMS 117 BK117B1 5626012 EU RADAR ALT ERRATIC E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 911TL 7198 NEEDLE FLUCTUATES ERRATICALLY. TEST FUNCTION SOMETIMES PEGS NEEDLE ABOVE 3000'. FOUND POWER OUT DOES NOT MEET SPECS. S TRIPLINE ASSY IS BAD. 1 G 7 2 3U H13EU 1996091200253 19960912 00253 NE 1996 9 12 HEEA967734 1 19960830 A 6210 7615009043050 TIP CAP SKRSKY S76 S76A 8143006 NE M/R DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2743E 760155 TIP CAP HAS FIBERGLASS BROKEN BETWEEN INNER DOUBLER AND OUTER DOUBLER ON THE UPPER SURFACE. 1 G 7 2 3U H1NE 1996091200254 19960912 00254 NE 1996 9 12 HEEA967735 1 19960830 A 6410 7610105101041 BLADE SKRSKY S76 S76A 8143006 NE T/R SPLIT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3122H 9903 760233 PADDLE "B" OF THIS ASSEMBLY HAS A SPLIT ON THE TIP CAP AND CHIP FILLER NEAR WEIGHT POCKET COVER. 1 G 7 2 3U H1NE 1996091200255 19960912 00255 1996 9 12 HEEA967736 4 19960830 A 3452 066106200 TRANSPONDER KT76 BOLKMS 117 BK117A3 5626015 EU COCKPIT ATC INTERMITTENT E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 8765J 7054 TOWER REPORTED TRANSPONDER TO BE WORKING INTERMITTENTLY. FOUND LOW POWER OUT. TRIED ADJUSTING. NO HELP. REPLACED CAVI TY OSCILLATOR V101. REPAIRED. ADJUSTED FREQUENCY AND PULSE WIDTH. CLEANED WAFER SWITCHES. COOKED UNIT UNDER HEAT LAM P , VIBRATED AND PUT IN FREEZER. BENCH CHECK GOOD. 1 G 7 2 3U H13EU 1996091200256 19960912 00256 1996 9 12 HEEA967737 4 19960830 A 3452 066106200 TRANSPONDER BELL 206 206L1 1182107 SW COCKPIT ATC DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1078C 45392 INTERMITTENT AND WEAK. REPLACED V101 CAVITY TUBE. REPAIRED. ALSO REPLACED DETERIORATED RESISTOR R477. BENCH CHECK GOO D. 1 G 7 1 3U H2SW 1996091200257 19960912 00257 EU 1996 9 12 96ZZZM1284 1 19960519 A 3260 1EN114N119 SWITCH STBROS SD3 SD360 8100606 EU RT MLG FAILED A TRBA O OTHER N FALSE WARNING AP APPROACH 1 SO 21 385MQ 16249 SH3707 RIGHT MAIN LANDING GEAR HAD FAULTY DOWN AND LOCK INDICATION. AFTER RECYCLING GEARS MANY TIMES, CAPTAIN DECLARES EMERGEN CY AND LANDED WITH NO INCIDENTS. ADJUSTED RIGHT DOWNLOCK MAIN GEAR MICROSWITCH AS PER MM 32-60-00. SEVERAL RETRACTION CHECKS PERFORMED AND SYSTEM WORKING SATISFACTORILY. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T A41EU 1996091200258 19960912 00258 EU 1996 9 12 96ZZZM1285 1 19960612 A 2612 51224133 FIRE LOOP STBROS SD3 SD360 8100606 EU NR 2 ENGINE DAMAGED A TRBA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SO 21 380MQ 16704 SH3702 DURING FLIGHT, RIGHT ENGINE FIRE INDICATOR ILLUMINATED. ENGINE FIRE EXTINGUISHERS WERE USED. DURING LANDING, RIGHT MAI N TIRE BURST. PERFORMED RIGHT ENGINE INSPECTION WITH NO EVIDENCE OF FIRE. RIGHT FORWARD FIRE LOOP REPLACED WITH SATISF ACTORY RESULTS AFTER OPERATIONAL CHECK. RIGHT MAIN TIRE WAS REPLACED. TIRE BURST INSPECTION PERFORMED WITH NO DEFECTS NOTED. (M) 2 H 7 2 4T A41EU 1996091200259 19960912 00259 NE 1996 9 12 96ZZZM1286 2 19960810 A 7200 ENGINE LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B NE NR 1 FAILED A RIAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 19 762BE 193P1070 10603 RIA - FLT 715 - KLAX-PHOG - THREE HOURS INTO FLIGHT NR 1 ENGINE OIL QTY DOWN TO 5 QUARTS AND OIL PRESSURE BELOW 35 PSI. ENGINE WAS SHUTDOWN AND A/C DIVERTED INTO PHNL. ON GROUND AT PHNL MX FOUND OIL IN TAILPIPE AND CHIP DETECTORS WERE FOU ND CLEAN. SUSPECT NR 6 BEARING FAILURE. ENGINE REPLACED IN PHNL. AIRCRAFT RELEASED INTO SERVICE. (M) 2 L 7 3 4F 4 F A23WE E12EU 1996091200260 19960912 00260 CE 1996 9 12 96ZZZM1287 1 19960819 A 3020 1149100681 FLEX HOSE BEECH 1900 1900C 1154161 CE RT INLET HEAT SPLIT A GUUA O OTHER J WARNING INDICATION AP APPROACH 1 SO 19 190GA UB1 FLT 433 - JAX-TPA - AT APPROXIMATELY 100 FEET ON FINAL TO TPA, THE RIGHT TEE HANDLE, RED LIGHT ILLUMINATED. DECLARED AN EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT AND NORMAL ENGINE SHUT DOWN PROCEDURES FOLLOWED. TPA MAINTENANCE DETERMIN ED THAT THE RIGHT INLET HEAT FLEX TUBE WAS BROKEN. REMOVED AND REPLACED FLEX TUBE. (M) 2 L 7 2 4T RT A24CE 1996091200261 19960912 00261 WP 1996 9 12 96ZZZM1288 1 19960818 A 2910 AE246000 HOSE DOUG DC8 DC861 3021952 WP NR 3 ENGINE RUPTURED A FXLA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 19 27UA 45942 DURING CLIMB EXPERIENCED LOSS OF HYDRAULIC QUANTITY DOWN TO HALF NORMAL RANGE. RETURNED TO MIAMI AND LANDED WITHOUT INC IDENT. INSPECTION REVEALED A RUPTURED HYDRAULIC HOSE AT NR 3 ENGINE HYDRAULIC PUMP. REPLACED HOSE AND RETURNED AIRCRAF T TO SERVICE. (M) 2 L 7 4 4F 4A25 1996091200262 19960912 00262 WP 1996 9 12 96ZZZM1289 1 19960818 A 3310 BA170 BALLAST DOUG DC8 DC8F54 3021926 WP INST LIGHTS DEFECTIVE A FXLA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 19 426FB 45667 AFTER LANDING MIAMI, INSTRUMENT WHITE LIGHT BALLAST STARTED TO SMOKE. PULLED CIRCUIT BREAKER. INSPECTION REVEALED DEFE CTIVE BALLAST. REPLACED BALLAST AND RETURNED AIRCRAFT TO SERVICE. 2 L 7 4 4F 4A25 1996091200263 19960912 00263 WP 1996 9 12 96ZZZM1290 1 19960810 A 2780 ASYMMETRY BRAKES LKHEED 1011 1011385115 5265015 WP LE FLAPS SET A A RIAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 306GB 193U1138 FLT 320 - MDE-MIA - ON CLIMB-OUT FLAP/SLAT LOCK LIGHT ILLUMINATED AND SLAT WOULD NOT RETRACT, AIRCRAFT RETURNED TO MDE. ON GROUND AT MDE MX RESET SLAT ASYMMETRY BRAKES. OPS CHECKED NORMAL UNABLE TO DUPLICATE FAULT. AIRCRAFT RELEASED INTO SERVICE. (M) 2 L 7 3 4F A23WE 1996091200264 19960912 00264 WP 1996 9 12 96ZZZM1291 1 19960817 A 5210 SEAL LKHEED 1011 10113851 5265010 WP L1 DOOR LEAKING A RIAA A J UNSCHED LANDING DUMP FUEL O OTHER CL CLIMB 1 SO 19 766BE 193P1112 FLT NR 711 - MIA-YQX - DURING CLIMB, PILOT REPORTED HIGH PITCH NOISE AT L1 DOOR. AIRCRAFT DUMPED FUEL AND RETURNED TO M IA. ON GROUND, MAINTENANCE REPAIRED SEAL AT LWR FORWARD CORNER OF L1 DOOR, PRESSURE CHECKED GOOD. AIRCRAFT RELEASED IN TO SERVICE. (M) 2 L 7 3 4F A23WE 1996091200265 19960912 00265 NM 1996 9 12 96ZZZM1292 1 19960813 A 5320 85330821109 SILL CAP DHAV DHC8 DHC8102 2809003 NM CARGO DOOR WORN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 854MA 357 DURING A C-CHECK INSPECTION IN INT, MAINTENANCE FOUND THE REAR BAGGAGE UPPER DOOR SILL WORN TO LIMITS. REPAIRS WERE COM PLETED THROUGH COMPLIANCE WITH RD 8-53-2133 AND RD 8-53-2227. REFERENCE MALA965093. 2 H 7 2 4T RT A13NM 1996091200266 19960912 00266 NM 1996 9 12 96ZZZM1293 1 19960813 A 5320 853324425503 FITTING DHAV DHC8 DHC8102 2809003 NM CARGO DOOR WORN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 854MA 357 DURING A C-CHECK INSPECTION IN INT, MAINTENANCE FOUND THE REAR BAGGAGE UPPER DOOR SILL WORN TO LIMITS. REPAIRS WRE COMP LETED THROUGH COMPLIANCE WITH RD 8-53-2133 AND RD 8-53-2227. REFERENCE MALA965093. 2 H 7 2 4T RT A13NM 1996091200267 19960912 00267 SW 1996 9 12 96ZZZM1294 1 19960816 A 5411 2735025 FORMER SWRNGN SA227 SA227AC 8780603 SW LT WING/NACELLE DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 438MA AC721B DURING SCHEDULED MAINTENANCE IN MSP, A CRACK WAS NOTED IN THE LEFT INBOARD LOWER WING TO NACELLE SKIN PATCH. MAINTENANC E REPLACED THE LEFT INBOARD UPPER WING SKIN TO NACELLE ATTACH ANGLE, P/N 27-35112, LEFT INBOARD NACELLE FORMER, P/N 27-3 5025, STRINGER LOCATED AT NS 120, P/N 27-35041-012, AND LEFT INBOARD LOWER WING SKIN TO NACELLE ATTACH ANGLE, P/N 27-351 12-039, IAW FAC SRM 51-40-01 AND 51-40-02. REFERENCE MALA965097. 2 L 7 2 4T RT A8SW 1996091200268 19960912 00268 SW 1996 9 12 96ZZZM1295 1 19960816 A 5413 2735041012 STRINGER SWRNGN SA227 SA227AC 8780603 SW LT WING/NACELLE DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 438MA AC721B DURING SCHEDULED MAINTENANCE IN MSP, A CRACK WAS NOTED IN THE LEFT INBOARD LOWER WING TO NACELLE SKIN PATCH. MAINTENANC E REPLACED THE LEFT INBOARD UPPER WING SKIN TO NACELLE ATTACH ANGLE, P/N 27-35112, LEFT INBOARD NACELLE FORMER, P/N 27-3 5025, STRINGER LOCATED AT NS 120, P/N 27-35041-012, AND LEFT INBOARD LOWER WING SKIN TO NACELLE ATTACH ANGLE, P/N 27-351 12-039, IAW FAC SRM 51-40-01 AND 51-40-02. REFERENCE MALA965097. 2 L 7 2 4T RT A8SW 1996091200269 19960912 00269 SW 1996 9 12 96ZZZM1296 1 19960816 A 5400 2735112039 ANGLE SWRNGN SA227 SA227AC 8780603 SW LT WING/NACELLE DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 438MA AC721B DURING SCHEDULED MAINTENANCE IN MSP, A CRACK WAS NOTED IN THE LEFT INBOARD LOWER WING TO NACELLE SKIN PATCH. MAINTENANC E REPLACED THE LEFT INBOARD UPPER WING SKIN TO NACELLE ATTACH ANGLE, P/N 27-35112, LEFT INBOARD NACELLE FORMER, P/N 27-3 5025, STRINGER LOCATED AT NS 120, P/N 27-35041-012, AND LEFT INBOARD LOWER WING SKIN TO NACELLE ATTACH ANGLE, P/N 27-351 12-039, IAW FAC SRM 51-40-01 AND 51-40-02. REFERENCE MALA965097. 2 L 7 2 4T RT A8SW 1996091200270 19960912 00270 EU 1996 9 12 96ZZZM1297 1 19960810 A 3350 330150 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 376AE 1122 340B376 DFW - DURING MX CHECK, EMERGENCY LIGHTS WERE FOUND TO BE INOP. RAI'D POWER SUPPLY AT LOCATIONS 20LN AND 21LN. OPS CHEC K SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. REFERENCE SIMA962231. 2 L 7 2 4T RT A52EU 1996091200271 19960912 00271 CE 1996 9 12 96ZZZM1298 1 19960714 A 5751 MS276434 BEARINGS BEECH 1900 1900D 1154162 CE AILERONS WORN A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 833CA 5391 UE24 DURING ROUTINE MAINTENANCE, BOTH AILERONS WERE DISCOVERED AS HAVING EXCESSIVE FREE PLAY. UPON INSPECTION OF COMPONENTS, ALL THREE ATTACHMENT BEARINGS AND MOUNTING HARDWARE WERE FOUND WORN AND LOOSE. BEARINGS AND HARDWARE REPLACED WITH NEW . (M) 2 L 7 2 4T RT A24CE 1996091200272 19960912 00272 CE 1996 9 12 96ZZZM1299 1 19960807 A 5751 MS276434 BEARINGS BEECH 1900 1900D 1154162 CE AILERONS WORN A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 845CA 6617 UE47 DURING ROUTINE MAINTENANCE, BOTH AILERONS WERE DISCOVERED AS HAVING EXCESSIVE FREE PLAY. UPON INSPECTION OF COMPONENTS, ALL THREE ATTACHMENT BEARINGS AND MOUNTING HARDWARE WAS FOUND WORN AND LOOSE. BEARINGS AND HARDWARE REPLACED WITH NEW. (M) 2 L 7 2 4T RT A24CE 1996091200274 19960912 00274 CE 1996 9 12 96ZZZM1301 1 19960516 A 5751 MS276434 BEARINGS BEECH 1900 1900D 1154162 CE AILERONS WORN A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 847CA 6011 UE52 DURING ROUTINE MAINTENANCE, BOTH AILERONS WERE DISCOVERED AS HAVING EXCESSIVE FREE PLAY. UPON INSPECTION OF COMPONENTS, ALL THREE ATTACHMENT BEARINGS AND MOUNTING HARDWARE WERE FOUND WORN AND LOOSE. BEARINGS AND HARDWARE REPLACED WITH NEW . (M) 2 L 7 2 4T RT A24CE 1996091200275 19960912 00275 CE 1996 9 12 96ZZZM1302 1 19960402 A 5751 MS276434 BEARINGS BEECH 1900 1900D 1154162 CE AILERONS WORN A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 840CA 6079 UE38 DURING ROUTINE MAINTENANCE, BOTH AILERONS WERE DISCOVERED AS HAVING EXCESSIVE FREE PLAY. UPON INSPECTION OF COMPONENTS, ALL THREE ATTACHMENT BEARINGS AND MOUNTING HARDWARE WAS FOUND WORN AND LOOSE. BEARINGS AND HARDWARE REPLACED WITH NEW. (M) 2 L 7 2 4T RT A24CE 1996091200276 19960912 00276 CE 1996 9 12 96ZZZM1303 1 19960228 A 5751 MS276434 BEARINGS BEECH 1900 1900D 1154162 CE AILERONS WORN A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 858CA 4876 UE72 DURING ROUTINE MAINTENANCE, BOTH AILERONS WERE DISCOVERED AS HAVING EXCESSIVE FREE PLAY. UPON INSPECTION OF COMPONENTS, ALL THREE ATTACHMENT BEARINGS AND MOUNTING HARDWARE WERE FOUND WORN AND LOOSE. BEARINGS AND HARDWARE REPLACED WITH NEW . (M) 2 L 7 2 4T RT A24CE 1996091200278 19960912 00278 1996 9 12 96ZZZM1305 4 19960707 A 3421 6226342022 ADI COLLINS SAAB SF340 340B 7860101 EU RT COCKPIT FAILED A NVEA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 03 202KD 340B202 FLT NR 5751 - MIA - PILOT REPORT, FIRST OFFICERS ADI WENT BLANK AND SMOKE WAS SMELLED IN THE COCKPIT. REMOVED AND REPLA CED FIRST OFFICERS ADI. (M) 2 L 7 2 4T RT A52EU 1996091200279 19960912 00279 NE 1996 9 12 96ZZZM1306 2 19960706 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RIGHT FAILED A NVEA E ENGINE SHUTDOWN B J K SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION FLUID LOSS AP APPROACH 1 SO 03 203NE 8842 340B203 785404 FLT 5750 - MIA - ON 15 MILE FINAL APPROACH, THE CAPTAIN NOTICED SMOKE IN THE COCKPIT. THE RIGHT ENGINE OIL PRESSURE LIG HT ILLUMINATED. THE ENGINE WAS SHUT DOWN AS A PRECAUTION. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT IN CIDENT. FOUND LARGE AMOUNTS OF OIL LEAKING INTO THE INTAKE, REMOVED AND REPLACED ENGINE. 2 L 7 2 4T 4 T RT A52EU E8NE 1996091200280 19960912 00280 NE 1996 9 12 96ZZZM1307 2 19960721 A 7320 3038044 P3 LINE AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE RT ENGINE CRACKED A A NVEA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 03 269AT 269 121129 FLT 4982 - JFK - PRIOR TO DESCENT, THE RIGHT TORQUE IND WENT TO ZERO. RIGHT ENGINE WAS SHUT DOWN AS A PRECAUTIONARY MEA SURE. AIRCRAFT LANDED IN JFK WITH NO FURTHER INCIDENT. FOUND LEFT P3 LINE CRACKED. REPLACED SAME. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1996091200281 19960912 00281 NE 1996 9 12 96ZZZM1308 2 19960805 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RIGHT MALFUNCTIONED A NVEA A E UNSCHED LANDING ENGINE SHUTDOWN O OTHER CL CLIMB 1 SO 03 218AE 340B218 FLT 5811 - MIA - PILOT REPORT, RIGHT ENGINE HAD UNCOMMANDED POWER SURGES AND OVERTEMP CONDITION. REMOVED AND REPLACED R IGHT ENGINE ASSY. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 1996091200282 19960912 00282 NM 1996 9 12 96ZZZM1309 1 19960815 A 5260 69211121 BUNGEE ASSY BOEING 727 727222 1384073 NM AFT AIRSTAIR WORN A RYNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 07 7639U 19912 AFT AIRSTAIR ANNUNCIATOR LIGHT CAME ON AFTER TAKEOFF, LIGHT WENT OFF AFTER LANDING. REMOVED AND REPLACED BUNGEE ASSEMBL Y. OPS CHECKED GOOD. (M) 2 L 7 3 4F A3WE 1996091200283 19960912 00283 WP 1996 9 12 AALA961140 1 19960729 A 2170 5953625521 DUCT DOUG DC9 DC982 3022082 WP RT ACM RUPTURED A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 295AA 49307 ABQ - FLT 203 - EN ROUTE DFW/SFO - DURING CRUISE, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. AIRCRAFT DIVERTE D TO ABQ AND LANDED WITHOUT INCIDENT. PLACARDED LEFT AIR CYCLE MACHING. ACCOMPLISHED FUNCTIONAL CHECK FLIGHT WITH NO D EFECTS FOUND. SYSTEM OPERATIONAL CHECKED NORMAL. SUBSEQUENTLY, AT DFW, REPLACED RUPTURED WATER SEPARATOR DUCT AT RIGHT AIR CYCLE MACHINE. ACCOMPLISHED LEAK AND GROUND CHECK WITH NO DEFECTS FOUND. SYSTEMS GROUND CHECKED NORMAL OPERATION AND PLACARD FOR LEFT AIR CYCLE MACHINE REMOVED. (M) 2 L 7 2 4F A6WE 1996091200285 19960912 00285 NM 1996 9 12 AALA961155 1 19960801 A 3350 CONNECTOR DOUG MD11 MD11 3023602 NM CABIN LOOSE A AALA K NONE L NO TEST CR CRUISE 1 SW 07 1759 48481 JFK - FLT 1728 - EN ROUTE SDQ/JFK DURING CRUISE, RIGHT AISLE EMERGENCY FLOOR LIGHTS IN CABIN ZONE C ILLUMINATED. NO OTH ER ABNORMAL INDICATIONS AND AIRCRAFT PROCEEDED TO JFK AND LANDED WITHOUT INCIDENT. RESECURED EMERGENCY FLOOR LIGHT CONN ECTOR AT CHARGER MODULE U-1842. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1996091200286 19960912 00286 NM 1996 9 12 AALA961157 1 19960727 A 5753 6521631323A FLAP BOEING 727 727223 1384074 NM LT TE FOREFLAP FAILED A AALA L ABORTED APPROACH D INFLIGHT SEPARATION AP APPROACH 1 SW 07 897AA 22013 MIA - FLT 2152 - DURING GO-AROUND AT MIA, PORTION OF LEFT WING OUTBOARD FORE FLAP DEPARTED THE AIRCRAFT. AIRCRAFT COMPL ETED THE GO-AROUND AND LANDED MIA WITHOUT INCIDENT. REPLACED LEFT WING OUTBOARD FORE FLAP. SYSTEM GROUND CHECKED NORMA L OPERATION. (M) 2 L 7 3 4F A3WE 1996091200287 19960912 00287 EU 1996 9 12 AALA961167 1 19960806 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN FLOOR DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 70072 515 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 23H AND 32H INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BETWEEN PAX SEAT ROWS 23H AND 32H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996091200288 19960912 00288 EU 1996 9 12 AALA961193 1 19960807 A 3397 WIRE AIRBUS 300 A300B4605R 3930308 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 11060 470 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 20AB TO 23AB INOPERATIVE. REPLACED BROKEN PO WER FEED WIRE FROM CABIN SIDEWALL CONNECTOR TO LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996091200289 19960912 00289 EU 1996 9 12 AALA961194 1 19960807 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 50051 459 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT STRIP AT LEFT AISLE BETWEEN L2 AND L3 DOORS INOPERATIVE. RESECURED LOOSE EMERGENCY FLOORLIGHT STRIP CONNECTOR BY L2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996091200290 19960912 00290 EU 1996 9 12 AALA961195 1 19960807 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN FLOOR DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 70072 515 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY R4 DOOR INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BY R4 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996091200291 19960912 00291 NM 1996 9 12 AALA961197 1 19960808 A 3260 SWITCH BOEING 727 727223 1384074 NM RT MLG OUT OF ADJUST A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 875AA 21387 MIA - FLT 1791 - AFTER TAKEOFF MIA WITH LANDING GEAR RETRACTED, RIGHT MAIN LANDING GEAR DOOR LIGHT ILLUMINATED. AIRCRAF T RETURNED TO MIA AND LANDED WITHOUT INCIDENT. ADJUSTED RIGHT MAIN LANDING GEAR DOOR SWITCH. OPERATED DOOR AND SYSTEM GROUND CHECKED NORMAL OPERATION. AIRCRAFT REDEPARTED MIA. (M) 2 L 7 3 4F A3WE 1996091200292 19960912 00292 WP 1996 9 12 AALA961198 1 19960808 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 429AA 49341 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRI P BY FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996091200293 19960912 00293 WP 1996 9 12 AALA961199 1 19960809 A 2170 21D101 COALESCER DOUG DC9 DC982 3022082 WP CABIN DIRTY A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 7538A 49992 AUS - FLT 1083 - AFTER TAKEOFF AUS DURING CLIMB-OUT, ACRID ODOR NOTED IN CABIN BUT NO VISIBLE SMOKE OR HAZE. AIRCRAFT R ETURNED TO AUS AND LANDED WITHOUT INCIDENT. ACCOMPLISHED INTERGRATED ELECTRICAL SYSTEM CHECK WITH NO DEFECTS FOUND. AC COMPLISHED PACK BURNOUT PROCEDURE AND REPLACED WATER SEPARATOR COALESCER BAGS. SYSTEM GROUND CHECKED NORMAL OPERATION W ITH NO ODORS NOTED. (M) 2 L 7 2 4F A6WE 1996091200294 19960912 00294 NM 1996 9 12 AALA961200 1 19960809 A 3350 A3060698101 CONNECTOR DOUG MD11 MD11 3023602 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1761R 48551 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 2C AND 13C INOPERATIVE. RESECURED LOOSE EMER GENCY FLOOR LIGHT STRIP CONNECTORS BETWEEN PAX SEAT ROWS 2C AND 13C. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1996091200295 19960912 00295 NM 1996 9 12 AALA961201 1 19960810 A 2130 710025 CONTL PANEL BOEING 727 727227 1384078 NM F/E PANEL DEFECTIVE A AALA B A EMER. DESCENT UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 725AA 20732 DFW - FLT 1269 - AFTER DEPARTURE DFW DURING CLIMB-OUT AT FL 210, CABIN ALTITUDE BEGAN TO CLIMB. ACCOMPLISHED EMERGENCY DESCENT AND AIRCRAFT RETURNED TO DFW, LANDING WITHOUT INCIDENT. REPLACED CABIN PRESSURIZATION CONTROL PANEL. ACCOMPLIS HED GROUND ENGINE RUN AND PRESSURIZATION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996091200296 19960912 00296 NM 1996 9 12 AALA961202 1 19960809 A 2120 AIR DISTR BOEING 757 757223 1384957 NM CABIN ODOR A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 633AA 24591 DFW - FLT 458 - AFTER TAKEOFF DFW DURING CLIMB-OUT, FLIGHT ATTENDANT REPORTED HOT SMELL AND SMOKE IN CABIN. AIRCRAFT RE TURNED TO DFW AND LANDED WITHOUT INCIDENT. CHECKED CABIN AND CARGO COMPARTMENTS, RECIRCULATION FANS AND EQUIPMENT COOLI NG FANS WITH NO ODOR OR DEFECTS NOTED. SUSPECTED CAUSE WAS NORMAL CYCLING OF PACK ANTI-ICE SYSTEM. PRECAUTIONARY ACCOM PLISHED PACK BURNOUT PROCEDURE. SYSTEMS GROUND CHECKED NORMAL OPERATION WITH NO HOT SMELL OR SMOKE NOTED. (M) 2 L 7 2 4F RT A2NM 1996091200297 19960912 00297 WP 1996 9 12 AALA961203 1 19960811 A 3233 39281375001 ACTUATOR DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 246AA 49238 SEA - FLT 1554 - AFTER TAKEOFF SEA WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR INDICATED UNSAFE. RECYCLED LANDING GE AR WITH SAME RESULTS. EXTENDED LANDING GEAR AND AIRCRAFT RETURNED TO SEA, LANDING WITHOUT INCIDENT. REPLACED NOSE LAND ING GEAR RETRACT CYLINDER. ACCOMPLISHED NOSE LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. PRECAUTIONARY REPLAC ED SCHRADER VALVE IN NOSE LANDING GEAR STRUT AND SERVICED STRUT WITH OIL AND NITROGEN. SYSTEM LEAK AND GROUND CHECKED N ORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996091200298 19960912 00298 WP 1996 9 12 AALA961209 1 19960831 A 2150 DUCT DOUG DC9 DC982 3022082 WP LT ACM BAY LOOSE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 405A 49316 IAD - FLT 1359 - AFTER TAKEOFF DCA DURING CLIMB-OUT, F/A REPORTED SMOKE IN CABIN. AIRCRAFT DIVERTED TO IAD AND LANDED W ITHOUT INCIDENT. DETERMINED OBSERVED SMOKE WAS ACTUALLY CONDENSATION FROM AIR CONDITIONING SYSTEM. RESECURED FLEX DUCT AND CLAMP AFT OF COALESCER FOR LEFT PACK. REPLACED BOTH COALESCER BAGS. ACCOMPLISHED GROUND ENGINE RUN AND OPERATED B OTH AIR CYCLE MACHINES WITH NO DEFECTS OR CONDENSATION NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996091200299 19960912 00299 EU 1996 9 12 AALA961218 1 19960814 A 3350 A3060698101 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 14053 420 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT CROSS AISLE BETWEEN L3 AND R3 DOOR AND AT RIGHT AISLE JUST FORWA RD OF R3 DOOR INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTOR AT CROSS AISLE BETWEEN L3 AND R3 DOOR AND REPLACED BROKEN POWER FEED WIRE AT RIGHT AISLE JUST FORWARD OF R3 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M ) 2 L 7 2 4F RT A35EU 1996091200300 19960912 00300 WP 1996 9 12 AALA961223 1 19960816 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN MISINSTALLED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 590AA 53253 SFO - DURING OVERNIGHT MAINTENANCE, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT 22F, LOWER, AND AFT SERVICE DOOR INOPERATIVE. REVERSED POLARITY ON CONNECTOR AT ROW 21. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 1996091200301 19960912 00301 EU 1996 9 12 AALA961224 1 19960818 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 18066 509 JFK - DURING OVERNIGHT MAINTENANCE, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS AT ROWS 8H AND 12H INOPERATIVE. SECURED CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996091200302 19960912 00302 1996 9 12 AALA961228 4 19960818 A 3460 AAP2563A DFG CONTROL PNL DOUG DC9 DC982 3022082 WP COCKPIT DEFECTIVE A A AALA K NONE O OTHER CL CLIMB 1 SW 07 474 49649 MIA - FLT 214 - WHILE CLIMBING THROUGH 29,000 FEET AT MACH .74. AIRCRAFT YAWED LEFT THEN RIGHT DUTCH ROLL. AUTO THROTT LE AND AUTO PILOT TRIPPED OFF. MANUALLY FLY REQUIRED IMMEDIATE INPUT OF 3 TO 4 DEGREE LEFT RUDDER TRIM WAS REQUIRED. A LTITUDE SET WINDOW BLANK, ACCOMPLISHED CHECKLIST, FOUND DIGITAL FLIGHT GUIDANCE C-17 CIRCUIT BREAKER POPPED. RESET CIRC UIT BREAKER, NO CHANGE. LANDED MIA WITHOUT FURTHER INCIDENT. PERFORMED FLIGHT FAULT REVIEW, TROUBLE SHOT TO DFW CONTRO L PANEL. REPLACED DFG CONTROL PANEL SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996091200303 19960912 00303 WP 1996 9 12 AALA961237 1 19960819 A 2170 21D101 COALESCER DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 234AA 49181 DFW - FLT 1945 - PRIOR TO DESCENT FOR LANDING, FLIGHT ATTENDANT NOTICED FUMES AND ODOR AS POSSIBLE FUEL OIL IN NATURE. A REA NOTED WAS AT ROW 25. FUMES NOTED IN COCKPIT PRIOR TO LANDING. LANDED DFW WITHOUT FURTHER INCIDENT. REPLACED AIR C ONDITIONING FILTERS, ACCOMPLISHED PACK BURN OUT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996091200304 19960912 00304 WP 1996 9 12 AALA961247 1 19960822 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 210AA 49161 DFW - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS UNDER EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996091200305 19960912 00305 WP 1996 9 12 AALA961248 1 19960822 A 3350 LIGHT DOUG DC10 DC1030 3023501 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 163AA 46914 DFW - DURING OVERNIGHT MAINTENANCE, FOUND LIGHT IN SEAT MOUNTED PROX LIGHTING INOPERATIVE AT 30B. REPLACED LIGHT ASSEMB LY AT SEAT 30B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A22WE 1996091200306 19960912 00306 NM 1996 9 12 ASAA9610096 1 19960806 A 5313 STRINGER BOEING 737 737290C 138448V NM BS 500 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING D-CHECK, A CRACK WAS IDENTIFIED AT THE ENDS OF STRINGER 16R, BS 500B, WHICH TERMINATES AT THE RIGHT WING LE ADING EDGE LIGHT. REPAIRED PER EA 5310-1456 AND BOEING SERVICE BULLETIN 737-53-1145. (M) 2 L 7 2 4F A16WE 1996091200307 19960912 00307 NM 1996 9 12 ASAA9610097 1 19960806 A 5315 65549053 FLOOR BEAM BOEING 737 737290C 138448V NM BS 440 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING D-CHECK, THE LOWER FORWARD FLANGE OF THE FLOOR BEAM BS 440, LBL 42.75 WAS FOUND TO BE CORRODED. REPAIRED P ER EA 5310-01460 AND BOEING TELEX ASA-SEA-96-0327RR. (M) 2 L 7 2 4F A16WE 1996091200308 19960912 00308 NM 1996 9 12 ASAA9610098 1 19960806 A 5315 65549055 FLOOR BEAM BOEING 737 737290C 138448V NM BS 480 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING D-CHECK, THE LOWER FORWARD FLANGE OF THE FLOOR BEAM BS 480, LBL 42 WAS FOUND TO BE CORRODED. REPAIRED PER EA 5310-01461 AND BOEING TELEX ASA-SEA-96-0332RR. (M) 2 L 7 2 4F A16WE 1996091200309 19960912 00309 NM 1996 9 12 ASAA9610099 1 19960806 A 5315 65549141 FLOOR BEAM BOEING 737 737290C 138448V NM BS 967 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING D-CHECK, A PREVIOUS REPAIR OF THE UPPER FORWARD FLANGE OF THE FLOOR BEAM BS 967 WAS FOUND TO BE CORRODED. R EPAIRED PER EA 5310-01457 AND BOEING TELEX ASA-SEA-94-0307RR. (M) 2 L 7 2 4F A16WE 1996091200310 19960912 00310 NM 1996 9 12 ASAA9610100 1 19960806 A 5315 65549054 FLOOR BEAM BOEING 737 737290C 138448V NM BS 460 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING D-CHECK, THE LOWER FLANGE OF THE FLOOR BEAM BS 460, LBL 42.5 WAS FOUND TO BE CORRODED. REPARIED PER EA 53 10-01459 AND BOEING TELEX ASA-SEA-96-0326RR. (M) 2 L 7 2 4F A16WE 1996091200311 19960912 00311 NM 1996 9 12 ASAA9610101 1 19960807 A 5315 65549103 FLOOR BEAM BOEING 737 737290C 138448V NM BS 887 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING D-CHECK, THE UPPER AFT FLANGE OF THE FLOOR BEAM BS 887, RBL 4 TO LBL 51 WAS FOUND TO BE CORRODED. REPAIRED PER EA 5310-01468 AND BOEING TELEX ASA-SEA-96-0348RR. (M) 2 L 7 2 4F A16WE 1996091200312 19960912 00312 NM 1996 9 12 ASAA9610102 1 19960807 A 5315 65549062 FLOOR BEAM BOEING 737 737290C 138448V NM BS 500 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING D-CHECK, THE UPPER FORWARD FLANGE OF THE FLOOR BEAM BS 500A, LBL 42 TO RBL 43 WAS FOUND TO BE CORRODED. RE PAIRED PER EA 5310-01471 AND BOEING TELEX ASA-SEA-96-0355RR. (M) 2 L 7 2 4F A16WE 1996091200313 19960912 00313 NM 1996 9 12 ASAA9610103 1 19960811 A 3350 8821004 BATTERY PACK BOEING 737 737210C 1384459 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 SEA - DURING MAINTENANCE CHECK, THE FORWARD SECTION OF EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOP. REPLACED BATT ERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1996091200314 19960912 00314 NM 1996 9 12 ASAA9610104 1 19960811 A 3350 1060091101 LIGHT BOEING 737 737210C 1384459 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 SEA - DURING MAINTENANCE CHECK, THE L-2 DOOR OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED LIGHT ASSEMB LY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1996091200315 19960912 00315 NM 1996 9 12 ASAA9610105 1 19960812 A 5315 65459051 FLOOR BEAM BOEING 737 737290C 138448V NM BS 400 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING D-CHECK, THE AFT LOWER HORIZONTAL FLANGE OF THE FLOOR BEAM AT BS400, LBL 55 TO 65 WAS FOUND TO BE CORRODED. REPAIRED PER EA 5310-01475 AND BOEING TELEX ASA-SEA-96-0374RR. (M) 2 L 7 2 4F A16WE 1996091200316 19960912 00316 NM 1996 9 12 ASAA9610107 1 19960812 A 5330 SKIN BOEING 737 737290C 138448V NM BS 360 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING D-CHECK, A 1.5 INCH CRACK WAS FOUND IN THE SKIN AT THE ELECTRONICS COMPARTMENT COOLING DUCT CUTOUT. REPAIR ED PER EA 5330-01261 AND BOEING SERVICE BULLETIN 737-53-1117 REV 1. (M) 2 L 7 2 4F A16WE 1996091200317 19960912 00317 NM 1996 9 12 ASAA9610108 1 19960812 A 5315 654680310 FLOOR BEAM BOEING 737 737290C 138448V NM BS 500 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING D-CHECK, THE LOWER FORWARD FLANGE OF THE FLOOR BEAM AT BS 500, LBL 5 TO 48 WAS FOUND TO BE CORRODED. REPAI RED PER EA 5310-01463 AND BOEING TELEX ASA-SEA-96-042RR. (M) 2 L 7 2 4F A16WE 1996091200318 19960912 00318 NM 1996 9 12 ASAA9610109 1 19960812 A 5315 6546568610 FLOOR BEAM BOEING 737 737290C 138448V NM BS 1016 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING D-CHECK, THE UPPER FORWARD FLANGE OF THE FLOOR BEAM AT BS 1016, RBL 30 TO 40 WAS FOUND TO BE CORRODED. REP AIRED PER EA 5310-01481 AND BOEING TELEX ASA-SEA-96-0378RR. (M) 2 L 7 2 4F A16WE 1996091200319 19960912 00319 NM 1996 9 12 ASAA9610110 1 19960813 A 5315 65459052 FLOOR BEAM BOEING 737 737290C 138448V NM BS 420 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING D-CHECK, THE FORWARD LOWER HORIZONTAL FLANGE OF THE FLOOR BEAM AT BS 420, LBL 5.25 TO 46 WAS FOUND TO BE CO RRODED. REPAIRED PER EA 5310-01480 AND BOEING TELEX ASA-SEA-96-0379RR. (M) 2 L 7 2 4F A16WE 1996091200320 19960912 00320 NM 1996 9 12 ASAA9610111 1 19960813 A 5315 65459052 FLOOR BEAM BOEING 737 737290C 138448V NM BS 420 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING D-CHECK, THE FORWARD UPPER HORIZONTAL FLANGE OF THE FLOOR BEAM AT BS 420, LBL 46 TO 58 WAS FOUND TO BE CORR ODED. REPAIRED PER EA 5310-01474 AND BOEING TELEX ASA-SEA-96-0372RR. (M) 2 L 7 2 4F A16WE 1996091200321 19960912 00321 NM 1996 9 12 ASAA9610112 1 19960813 A 5315 65459062 FLOOR BEAM BOEING 737 737290C 138448V NM BS 420 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING D-CHECK, THE UPPER FORWARD FLANGE OF THE FLOOR BEAM AT BS 500A, LBL 25 TO 43 WAS FOUND TO BE CORRODED. REP AIRED PER EA 5310-01472 AND BOEING TELEX ASA-SEA-96-0353RR. (M) 2 L 7 2 4F A16WE 1996091200322 19960912 00322 NM 1996 9 12 ASAA9610114 1 19960815 A 5315 65549073 FLOOR BEAM BOEING 737 737290C 138448V NM BS 767 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING D-CHECK, THE LOWER FORWARD FLANGE OF THE FLOOR BEAM AT BS 767, RBL 24 TO 30 WAS FOUND TO BE CORRODED. REPA IRED PER EA 5310-01465 AND BOEING TELEX ASA-SEA-96-0339RR. (M) 2 L 7 2 4F A16WE 1996091200323 19960912 00323 NM 1996 9 12 ASAA9610115 1 19960815 A 5315 65549102 FLOOR BEAM BOEING 737 737290C 138448V NM BS 867 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING D-CHECK, THE LOWER FORWARD FLANGE OF THE FLOOR BEAM AT BS 867, LBL 23 TO RBL 46 WAS FOUND TO BE CORRODED. R EPAIRED PER EA 5310-01477 AND BOEING TELEX ASA-SEA-96-0354RR. (M) 2 L 7 2 4F A16WE 1996091200324 19960912 00324 NM 1996 9 12 ASAA9610116 1 19960816 A 5315 65549063 FLOOR BEAM BOEING 737 737290C 138448V NM BS 500B CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING D-CHECK, THE LOWER FORWARD FLANGE OF THE FLOOR BEAM AT BS 500B, LBL 35 WAS FOUND TO BE CORRODED. REPAIRED PER EA 5310-01464 AND BOEING TELEX ASA-SEA-96-0340RR. (M) 2 L 7 2 4F A16WE 1996091200325 19960912 00325 NM 1996 9 12 ASAA9610160 1 19960812 A 5230 65549332 DOOR BEAM BOEING 737 737290C 138448V NM BS 465.5 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING D-CHECK, THE MAIN CARGO DOOR UPPER BEAM AFT END WAS FOUND TO HAVE A 1.3 INCH CRACK. REPAIRED PER EA 5230-0 1062 AND BOEING TELEX ASA-SEA-96-0302RR. (M) 2 L 7 2 4F A16WE 1996091200326 19960912 00326 NM 1996 9 12 ASAA9640068 1 19960806 A 3350 S417N50914 LIGHT BOEING 737 7374S3 1384711 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 786AS 24795 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED LIGHT ASSE MBLY AT ROW 15 AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996091200328 19960912 00328 WP 1996 9 12 ASAA9680036 1 19960125 A 3231 DOORS DOUG DC9 DC982 3022082 WP NLG UNLATCHED A ASAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 NM 01 956AS 48079 LAX - AIR TURN BACK OF FLT 505 - CREW REPORTED SEVERE VIBRATION FROM NOSE AREA, AFTER LANDING GEAR RETRACTION VIBRATION INCREASED AS AIRSPEED INCREASED. LOWERED LANDING GEAR AND RETURNED TO LAX, LANDED WITHOUT INCIDENT. FOUND NLG DOORS OP EN, CLOSED NLG DOORS AND ACCOMPLISHED RETRACTION/EXTENSION TEST AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996091200329 19960912 00329 WP 1996 9 12 ASAA9680042 1 19960130 A 2560 3753213 CONTAINER LATCH DOUG DC9 DC982 3022082 WP L1 DOOR LOOSE A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 933AS 49234 PDX - AFTER ARRIVAL OF FLT 586 - CREW REPORTED, THE L1 DOOR WAS DIFFICULT TO OPEN. FOUND EMERGENCY EVACUATION SLIDE CON TAINER LATCH LOOSE, SECURED LATCH AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996091200330 19960912 00330 WP 1996 9 12 ASAA9680161 1 19960510 A 5320 993061245 SILL DOUG DC9 DC982 3022082 WP L2 DOOR CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 954AS 49387 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON L2 DOOR WEB AT Y1144 TO Y1164, X PLUS 50, Z0. REMOVED DAMAGED AREA AND I NSTALLED NEW PIECES IAW DC-9 SRM AND ASA EA 53-20-01271. (M) 2 L 7 2 4F A6WE 1996091200331 19960912 00331 WP 1996 9 12 ASAA9680162 1 19960806 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 958AS 53024 OAK - DURING MAINTENANCE CHECK, THE RIGHT FORWARD OVERWING EMERGENCY EXIT IDENTIFIER SIGN WAS FOUND INOPERATIVE. REPLAC ED THE BATTERY PACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996091200332 19960912 00332 WP 1996 9 12 ASAA9680163 1 19960807 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 969AS 53063 SEA - PRIOR TO DEPARTURE OF FLT 203 - CREW REPORTED, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERAT IVE. RECONNECTED WIRING AT ROW 3 AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996091200337 19960912 00337 WP 1996 9 12 ASAA9680168 1 19960103 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 712-731 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 936AS 49363 PAE - DURING 30K CHECK, FOUND CORROSION ON THE FUSELAGE SKIN AND INTERNAL DOUBLER AT Y712 TO Y731, LONGERON 28L TO 28R. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM AND ASA EA 5330-01223. (M) 2 L 7 2 4F A6WE 1996091200338 19960912 00338 WP 1996 9 12 ASAA9680169 1 19960105 A 5320 THRESHOLD DOUG DC9 DC982 3022082 WP CARGO COMPT CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 936AS 49363 PAE - DURING 30K CHECK, FOUND CORROSION WAS FOUND ON THE UPPER SURFACE OF THE LOWER FLANGE ON THE AFT CARGO COMPARTMENT DOOR THRESHOLD BEAM AT Y1155, LONGERON 28R. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM AND ASA EA 5310- 01395. (M) 2 L 7 2 4F A6WE 1996091200339 19960912 00339 WP 1996 9 12 ASAA9680170 1 19960301 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 1070 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 954AS 49387 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON LONGERON 28R AT Y1070. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM AND ASA EA 5310-01418. (M) 2 L 7 2 4F A6WE 1996091200340 19960912 00340 WP 1996 9 12 ASAA9680171 1 19960810 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 937AS 49364 SEA - DURING MAINTENANCE CHECK, THE L2 DOOR EMERGENCY EXIT IDENTIFIER SIGN WAS FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996091200341 19960912 00341 WP 1996 9 12 ASAA9680173 1 19960811 A 3350 S103 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 939AS 49657 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE BAT TERIES AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996091200342 19960912 00342 WP 1996 9 12 ASAA9680174 1 19960811 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 940AS 24669 49825 SEA - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996091200343 19960912 00343 WP 1996 9 12 ASAA9680176 1 19960812 A 3350 41B004AD07G3 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 941AS 49925 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 14 TO 18 AND ROWS 29 TO 32 WERE FOUND INOPERA TIVE. REPLACED THE BATTERIES AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996091200344 19960912 00344 NM 1996 9 12 AWXA960367 1 19960722 A 5315 FLOOR BEAM BOEING 737 73733A 1384673 NM BS 947 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 PAE - FLT 7827 - DURING ROUTINE SCHEDULED C-11 MAINTENANCE CHECK, FOUND CORROSION AT BS 947, WL 208, RBL 10 TO LBL 12 ON TOP OF FLOOR BEAM. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-00-51. (M) 2 L 7 2 4F RT A16WE 1996091200345 19960912 00345 NM 1996 9 12 AWXA960368 1 19960722 A 5315 FLOOR BEAM BOEING 737 73733A 1384673 NM BS 986 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 PAE - FLT 7827 - DURING ROUTINE SCHEDULED C-11 MAINTENANCE CHECK, FOUND CORROSION AT BS 986, WL 208, BL 10-LBL 20 ON TOP OF BEAM. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-00-51. (M) 2 L 7 2 4F RT A16WE 1996091200346 19960912 00346 NM 1996 9 12 AWXA960369 1 19960723 A 5315 FLOOR BEAM BOEING 737 73733A 1384673 NM BS 796-817 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 164AW 23625 PAE - FLT 7827 - DURING ROUTINE SCHEDULED C-11 MAINTENANCE CHECK, FOUND CORROSION AT AFT. CARGO BAY CARGO FLOOR BEAM BS 796-817, RBL 13.5 AT NUTPLATE HOLES, TOP OF BOTTOM SIDE. REPLACED SECTION OF FLOOR BEAM FROM BS 780 TO 821 AT RBL 13.5 PE SRM 53-00-51. (M) 2 L 7 2 4F RT A16WE 1996091200347 19960912 00347 1996 9 12 AWXA960371 4 19960821 A 2210 285T0013105 YAW DMPR MODULE BOEING 757 757225 1384959 NM NR 1 MALFUNCTIONED A AWXA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 WP 28 914AW D00279 22208 PHX - FLT 2610 - UNCOMMANED RUDDER ON CLIMB-OUT, RUDDER KICKED TWICE, ONCE UPON TURNBACK. APPROX 1 HOUR LATER LATER, RU DDER KICKED ONCE AT 500 FEET FROM TOUCHDOWN. CHECKED YAW DAMPER PER FIM 22-21-00, PAGE 101. NO FAULTS NOTED. CHECKED THE YAW DAMPER MODULES FOR FAULT BALLS, NONE FOUND. CHECKED THE RUDDER RATIO MODULES FOR FAULTS, NONE NOTED. COMPLIED WITH RUDDER AND RUDDER TRIM SYSTEM ADJUSTMENT AND TEST PER MM 27-21-00, PAGE 501-526. OPS CHECK GOOD. COMPLIED WITH FI M TEST OF RUDDER RATIO CHANGER PER FIM MANUAL. OPS CHECK GOOD. REMOVED AND REPLACED BOTH YAW DAMPER MODULES PER BOEING ENGINEERING AS PRECAUTIONARY. (M) 2 L 7 2 4F RT A2NM 1996091200348 19960912 00348 NM 1996 9 12 AWXA960372 1 19960809 A 5210 GUIDE ARM BOEING 757 7572S7 1384962 NM ENTRY DOOR OUT OF ADJUST A AWXA K NONE J WARNING INDICATION CR CRUISE 1 WP 28 902AW 23322 PHX - FLT 9 - L-4 ENTRY DOOR LIGHT ILLUMINATED IN FLIGHT. ADJUSTED L-4 GUIDE ARM AND SERRATED PLATE PER BMM 52-11-04. P RESSURIZED A/C AND RAN ENGINES TO P/POWER. DOOR IS SECURE, NO WARNING LIGHTS. (M) 2 L 7 2 4F RT A2NM 1996091200349 19960912 00349 NM 1996 9 12 AWXA960373 1 19960811 A 5210 PROX SENSOR BOEING 757 7572S7 1384962 NM LT AFT DOOR OUT OF LIMITS A AWXA K NONE J WARNING INDICATION DE DESCENT 1 WP 28 902AW 23322 PHX - FLT FLT 9 - ON DESCENT AT 500 FEET, LEFT AFT DOOR EICAS MESSAGE. READJUSTED THE DOOR PROX SENSOR, IT WAS OUT OF L IMITS. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 1996091200350 19960912 00350 NM 1996 9 12 AWXA960374 1 19960813 A 5210 LATCH CAM BOEING 757 7572S7 1384962 NM AFT ENTRY DOOR OUT OF RANGE A AWXA K NONE J WARNING INDICATION CR CRUISE 1 WP 28 902AW 23322 LAS - FLT 6 - LEFT AFT ENTRY DOOR EICAS LIGHT ILLUMINATED MOMENTARILY. FLIGHT ATTENDANT NOTED, HANDLE CAME WAY UP AND H AD TO BE MANUALLY PUSHED DOWN TWICE. FOUND UPPER AFT LATCH CAM OUT OF ADJUSTMENT. ADJUSTED LATCH CAM PER 757 BMM 52-11 -00. OPS CHECK GOOD, DOOR NOW NORMAL. SRTC ISSUED. CHECKED THE DOOR RIG PER 52-11-00, PAGE 501 AND THE DOOR IS RIGGED PROPERLY AS FAR AS WE CAN SEE WITH NO OBVIOUS DEFECTS. THE DOOR HANDLE OVER CENTER FORCE IS APPROXIMATELY 32 POUNDS. W HEN PRESSURIZED, THE A/C OVERCENTER HANDLE FORCE WAS LIGHTER, BUT IT WAS STILL VERY FIRM IN THE OVER CENTER POSITION. (M ) 2 L 7 2 4F RT A2NM 1996091200352 19960912 00352 EU 1996 9 12 AWXA960376 1 19960811 A 7810 7401094507 EXHAUST NOZZLE AIRBUS 320 A320231 3930325 EU NR 1 ENGINE DAMAGED A A AWXA K NONE P NO WARNING INDICATION UK UNKNOWN 1 WP 28 621AW 0082 053 LAS - FLT 2993 - ON POST FLIGHT REPORT, DISCOVERED ENGINE NR 1 TAIL CONE FAIRING MISSING (UPPER PART) INSIDE WITH DAMAGE TO THE EXHAUST CONE AND HOLES INSIDE WALLS LEFT SIDE. REPLACED EXHAUST COMMON NOZZLE ASSY PER AMM 78-11-11, PAGE 401-4 15. (M) 2 L 7 2 4F RT A28NM 1996091200353 19960912 00353 SO 1996 9 12 GLBA96136 1 19960630 A 3231 GEAR DOOR EMB 120 EMB120RT SO LT MLG NOT LATCHED A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 01 279UE 120085 SAV - AIR TURN BACK AFTER HEARING UNIDENTIFIED NOISE RELATED TO GEAR RETRACTION. MX RELATCHED FWD LEFT GEAR DOOR. (M) 2 L 7 2 4T RT A31SO 1996091200354 19960912 00354 CE 1996 9 12 GLBA96137 1 19960702 A 3230 RETRACT MECH BEECH 1900 1900C 1154161 CE LANDING GEAR MALFUNCTIONED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 96UE UC96 SPI - GEAR DID NOT RETRACT AFTER DEPARTURE. MAINTENANCE CLEANED NOSE UPLOCK SYSTEM CANNON PLUG. GEAR SWING AND OPERATI ON CHECK GOOD. (M) 2 L 7 2 4T RT A24CE 1996091200355 19960912 00355 CE 1996 9 12 GLBA96138 1 19960702 A 7540 ANN LIGHT BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA LT/RT BLEED AIR ILLUMINATED A GLBA O OTHER O OTHER TO TAKEOFF 1 CE 01 170GL UE170 RDU - BOTH BLEED AIR FAIL ANNUNCIATORS ILLUMINATED IN FLIGHT. CYCLED BLEED SWITCHES TO ENVIRONMENTAL OFF AND BOTH ANNUN CIATORS REMAINED ILLUMINATED. MAINTENANCE COULD NOT DUPLICATE. (M) 2 L 7 2 4T 4 T RT A24CE E4EA 1996091200356 19960912 00356 SO 1996 9 12 GLBA96139 1 19960702 A 3230 RETRACT MECH EMB 120 EMB120RT SO LANDING GEAR MALFUNCTIONED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 267UE 120071 MQT - GEAR WOULD NOT RETRACT. MAINTENANCE INSPECTED AIR/GROUND SENSORS AND WIRING. COULD NOT DUPLICATE DISCREPANCY. ( M) 2 L 7 2 4T RT A31SO 1996091200357 19960912 00357 CE 1996 9 12 GLBA96140 1 19960702 A 5312 BULKHEAD BEECH 1900 1900C 1154161 CE AFT FUS CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 CE 01 126UE UC126 SPQ - AFT CANTED BULKHEAD CRACKED AT THE LEFT RUDDER CABLE PULLEY. REPAIRED WITH USE OF KIT P/N 129-4005-1, REF WO 7038 3. (M) 2 L 7 2 4T RT A24CE 1996091200358 19960912 00358 CE 1996 9 12 GLBA96141 1 19960704 A 7120 12991003279 ENGINE TRUSS BEECH 1900 1900C 1154161 CE LT ENGINE CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 CE 01 60UE UC60 DLH - LEFT ENGINE TRUSS CRACKED AT OUTBOARD UPPER FORWARD COWLING SUPPORT. MAINTENANCE REPAIRED CRACK WITH KIT 129-9006 -1. (M) 2 L 7 2 4T RT A24CE 1996091200359 19960912 00359 CE 1996 9 12 GLBA96144 1 19960706 A 3230 RETRACT MECH BEECH 1900 1900C 1154161 CE LANDING GEAR MALFUNCTIONED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 96UE UC96 RHI - LANDING GEAR WILL NOT COME UP. FERRIED TO SPW, MAINTENANCE COULD NOT DUPLICATE, BUT CHANGED LANDING GEAR CONTROL HANDLE PRECAUTIONARY. ALSO, REMOVED AND REPLACED HYDRAULIC POWER PACK AND 60 AMP LANDING GEAR CIRCUIT BREAKER. TEST FL IGHT SATISFACTORY. (M) 2 L 7 2 4T RT A24CE 1996091200360 19960912 00360 CE 1996 9 12 GLBA96146 1 19960708 A 3230 RETRACT MECH BEECH 1900 1900C 1154161 CE LANDING GEAR MALFUNCTIONED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 96UE UC96 SPW - PILOT TRAINING, LANDING GEAR WILL NOT RETRACT WITH GEAR SELECTOR UP. MAINTENANCE COULD NOT DUPLICATE AFTER FIFTEE N GEAR SWINGS. REMOVED AND REPLACD THE GEAR TIME DELAY PCB AND INSPECTED K5 RELAY. SERVICE VALVE SWITCH ASSEMBLY AND W IRING. TEST FLIGHT SATISFACTORY. (M) 2 L 7 2 4T RT A24CE 1996091200361 19960912 00361 CE 1996 9 12 GLBA96147 1 19960709 A 2400 ELECT WIRES BEECH 1900 1900C 1154161 CE RT COCKPIT CHAFED A GLBA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 01 150UE UC150 TUS - ELECTRICAL SMOKE CAME FROM CO-PILOTS PANEL, DURING CRUISE FLIGHT AT FL 210. MAINTENANCE FOUND TWO WIRES CHAFING T OGETHER BEHIND CO-PILOTS ALTIMETER. REPAIRED WIRES AND APPLIED SPIRAL WRAP TO AFFECTED AREA. OPERATES NORMALLY. (M) 2 L 7 2 4T RT A24CE 1996091200362 19960912 00362 CE 1996 9 12 GLBA96148 1 19960709 A 3230 RETRACT MECH BEECH 1900 1900C 1154161 CE LANDING GEAR MALFUNCTIONED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 96UE UC96 SPW - PILOT TRAINING, LANDING GEAR DOES NOT RETRACT. MAINTENANCE CYCLED GEAR FIFTEEN TIMES AND COULD NOT DUPLICATE. RE MOVED AND REPLACED THE HYDRAULIC POWER PACK PRESSURE SWITCH AND SERVICE VALVE ASSEMBLY. CYCLED GEAR SEVERAL MORE TIMES WITH NO FAILURE. (M) 2 L 7 2 4T RT A24CE 1996091200363 19960912 00363 CE 1996 9 12 GLBA96150 1 19960711 A 3230 6041H215 RELAY BEECH 1900 1900C 1154161 CE K5 RELAY INTERMITTENT A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 96UE UC96 SPW - PILOT TRAINING, GEAR WILL NOT RETRACT. MAINTENANCE COULD NOT DUPLICATE IN HANGAR ON JACKS. REMOVED AND REPLACED SERVICE VALVE. GEAR SWINGS AND OPERATIONAL CHECK WAS GOOD. TEST FLIGHT FAILED. REMOVED AND REPLACED LANDING GEAR RELA Y. GEAR OPERATIONAL NORMAL. (M) 2 L 7 2 4T RT A24CE 1996091200364 19960912 00364 CE 1996 9 12 GLBA96151 1 19960712 A 3040 1143840202 WINDSHIELD BEECH 1900 1900C 1154161 CE RT COCKPIT ARCING A GLBA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 01 122GL 10871 UC122 MBL - AT 10,000 FEET DURING MODERATE RAIN, SMOKE IN COCKPIT WITH WINDSHIELD FUEL VENTS, ALT STATIC, PITOT AND STALL HEAT ON AND THE ENGINE ANTI-ICE ON. MAINTENANCE DEFERRED WINDSHIELD HEAT IAW MEL 30-7. FOUND RIGHT WINDSHIELD GROUND BLOCK PULLED AWAY FROM WINDSHIELD SURFACE AND ARCING WHEN POWER APPLIED. (M) 2 L 7 2 4T RT A24CE 1996091200365 19960912 00365 SO 1996 9 12 GLBA96152 1 19960712 A 7712 TQ SENSOR EMB 120 EMB120ER 3260203 SO LT ENGINE LOOSE A GLBA O OTHER O OTHER CR CRUISE 1 CE 01 292UX 120292 SPI - LEFT TORQUE FLUCTUATES 30 TO 40 PERCENT. MAINTENANCE INSPECTED AND FOUND NH SENSOR LOOSE AND HMU SENSOR LOOSE. T IGHTENED AS REQUIRED. OPERATIONAL CHECK GOOD. TEST FLIGHT SATISFACTORY. (M) 2 L 7 2 4T RT A31SO 1996091200366 19960912 00366 SO 1996 9 12 GLBA96153 1 19960708 A 2751 CONNECTOR EMB 120 EMB120RT SO TE FLAPS LOOSE A GLBA O OTHER N FALSE WARNING CL CLIMB 1 CE 01 279UE 120085 RDU - CONTROL FAULT/ADVANCE STALL WARNING LIGHT AFTER TAKEOFF. MAINTENANCE SECURED CANNON PLUG ON LEFT OUTBOARD FLAP AC TUATOR. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A31SO 1996091200367 19960912 00367 CE 1996 9 12 GLBA96154 1 19960716 A 2612 24412886 FIRE LOOP BEECH 1900 1900C 1154161 CE RT ENGINE FAILED A GLBA O OTHER N FALSE WARNING CR CRUISE 1 CE 01 101UE UC101 DEN - FALSE FIRE INDICATION FOR RIGHT ENGINE. MAINTENANCE REMOVED AND REPLACED FORWARD FIRE LOOP ON RIGHT ENGINE. SYST EM OPERATES NORMALLY. (M) 2 L 7 2 4T RT A24CE 1996091200368 19960912 00368 WP 1996 9 12 HKGA0012 2 19960730 A 7261 SCAVENGE PUMP SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP RT ENGINE FAILED A A HKGA E ENGINE SHUTDOWN J K WARNING INDICATION FLUID LOSS AP APPROACH 1 SW 17 31171 AC605 P44336 AIRCRAFT WAS ON APPROACH WHEN RIGHT ENGINE OIL LIGHT CAME ON. PILOT CHECKED PRESSURE AND FOUND OIL PSI WAS LOW AND SHUT ENGINE DOWN WITH STOP AND FEATHER. LANDED WITH NO FURTHER PROBLEM. DRIVE GEAR ON THE TURBINE SCAVENGE PUMP SEARED APP ROX 3 TEETH, CAUSING TURBINE BEARING TO CAVITY AND TO FILL WITH OIL AND LEAK INTO EXHAUST. THE TEETH ON THE SHAFT DRIVI NG PUMP WAS ALSO DAMAGED AND REQUIRED REPLACEMENT. SCAVENGE PUMP AND DRIVE SHAFT WAS REPLACED. (M) 2 L 7 2 4T 4 T RT A8SW E4WE 1996091200369 19960912 00369 NM 1996 9 12 HNAA9693654 1 19960729 A 3231 RETRACT MECH DHAV DHC8 DHC8102 2809003 NM LT MLG DOOR MALFUNCTIONED A HNAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 07 936HA 145 FLT NR 3335 - DCA-PHL - AFTER GEAR RETRACTION, THE LEFT DOOR ADVISORY LIGHT ILLUMINATED. THE GEAR DOOR WAS CONFIRMED OP EN AND GEAR WAS RETRACTED IN THE WELL. THE GEAR WAS SELECTED DOWN AND BACK UP, THE LIGHT WENT OUT AND ALL WAS NORMAL. M AINTENANCE COULD NOT DUPLICATE THE PROBLEM. MAINTENANCE ADJUSTED THE ROD LENGTH OF THE FORWARD GEAR DOOR ROD AS A PRECA UTION. (M) 2 H 7 2 4T RT A13NM 1996091200370 19960912 00370 NM 1996 9 12 HNAA9694152 1 19960723 A 3260 864202 SENSOR ELDEC DHAV DHC8 DHC8102 2809003 NM NLG FAILED A HNAA K NONE N FALSE WARNING CL CLIMB 1 EA 07 941HA 19412 161 FLT NR 3481 - EYW-MIA - AFTER TAKEOFF, THE NOSE GEAR RED AND HANDLE LIGHT CYCLED ON AND OFF. THE AIRCRAFT CONTINUED ON TO MIA AND LANDED WITHOUT INCIDENT. ADJUSTED THE DRAG STRUT SENSOR AS REQUIRED AND GROUND CHECK WAS GOOD. LATER AT THE RON, THE SENSOR AT THE NOSE LANDING GEAR DRAG STRUT WS REPLACED. (M) 2 H 7 2 4T RT A13NM 1996091200371 19960912 00371 NM 1996 9 12 MALA965068 1 19960710 A 2160 CIRCUIT BREAKERS DHAV DHC8 DHC8102 2809003 NM CABIN TEMP TRIPPED A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 861MA 362 FLT NR 3418 - ON CLIMB-OUT FROM DTW, THE CREW WAS UNABLE TO CONTROL THE CABIN TEMPERATURE IN DTW. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE RESET THE CABIN TEMPERATURE CONTROL CIRCUIT BREAKERS. ALL CHECKS SATISFACTORY. (M) 2 H 7 2 4T RT A13NM 1996091200372 19960912 00372 SW 1996 9 12 MALA965069 1 19960710 A 5320 DOOR FRAME SWRNGN SA227 SA227AC 8780603 SW BS 133.87 SCUFFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 434MA AC717 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE FORWARD CABIN DOOR FUSELAGE FRAME FS 133.87, P/N 27-22126, HAD SCUFF MARKS APPROX .016 INCH DEEP AT LOWER TEFLON GUIDE PAD CONTACT AREA. FABRICATED AND INSTALLED REPAIR PLATE, 'R EPLACEABLE WEAR PLATE' ONTO FORWARD FUSELAGE FRAME FS 133.87 AT LOWER POSITION (5.375 INCH BY 3.5 INCH). PERFORMED ALL WORK IAW FAC SRM 53-90-20 PAGES 75-77 REV JAN 18, 1993. (M) 2 L 7 2 4T RT A8SW 1996091200373 19960912 00373 SW 1996 9 12 MALA965079 1 19960722 A 3260 1EN516 SWITCHES SWRNGN SA227 SA227AC 8780603 SW NLG WW LACK OF LUBE A MALA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 15 160MC AC733B FLT 3397 - ON APPROACH TO DTW, THE NOSE GEAR GREEN LIGHT FAILED TO ILLUMINATE. THE CREW CYCLED THE GEAR AND THE LIGHT I LLUMINATED AFTER 15 SECONDS. MAINTENANCE CLEANED AND LUBED THE NOSE LANDING GEAR MICROSWITCHES. THE GEAR WAS SWUNG SEV ERAL TIMES. ALL CHECKS WERE GOOD. (M) 2 L 7 2 4T RT A8SW 1996091200374 19960912 00374 NM 1996 9 12 MALA965080 1 19960724 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 846MA 344 FLT NR 3093 - DURING THE PREFLIGHT IN DTW, THE COCKPIT OVERHEAD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANC E REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY. ALL CHECKS GOOD. (M) 2 H 7 2 4T RT A13NM 1996091200375 19960912 00375 EU 1996 9 12 MALA965081 1 19960725 A 3350 6104781 BATTERY PACK SAAB SF340 SF340A 7850100 EU CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 102AE 340A102 DURING PREFLIGHT, CREW NOTED THAT THE RIGHT OVERHEAD EMERGENCY LIGHTS FAILED TO REMAIN ILLUMINATED. MAINTENANCE REPLACE D BATTERY PACK 20 LN. ALL CHECKS WERE GOOD OF THE EMERGENCY LIGHTS. (M) 2 L 7 2 4T RT A52EU 1996091200376 19960912 00376 1996 9 12 MALA965083 4 19960729 A 3442 071131900 R/T UNIT DHAV DHC8 DHC8102 2809003 NM RADAR FAILED A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 828MA 333 FLT NR 2908 - ON DEPARTURE FROM ELM, THE RADAR WAS NOT DISPLAYING WEATHER RETURNS. AIRCRAFT RETURNED TO ELM WHERE MAINT ENANCE REPLACED THE WEATHER RADAR R/T. OPS CHECK OF RADAR WAS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1996091200377 19960912 00377 EU 1996 9 12 MALA965084 1 19960729 A 3020 44730501 DE-ICE MODULE SAAB SF340 SF340A 7850100 EU RT NACELLE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 103AE 340A103 FLT NR 3453 - ON DEPARTURE FROM DTW, THE RIGHT INTAKE LIGHT WOULD ILLUMINATE 12-15 SECONDS AFTER THE RIGHT INTAKE HEAT S WITCH WAS TURNED ON. AIRCRAFT RETURNED TO DTW WHERE MAINTENANCE FOUND THE RIGHT DE-ICE MODULE TO BE AT FAULT. THE MODU LE WAS CHANGED. ALL OPS CHECKS WERE GOOD. (M) 2 L 7 2 4T RT A52EU 1996091200378 19960912 00378 NM 1996 9 12 MALA965085 1 19960729 A 3260 864202 SENSOR DHAV DHC8 DHC8102 2809003 NM NLG WORN A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 859MA 361 FLT NR 2907 - ON DEPARTURE FROM DTW, AFTER GEAR RETRACTION, THE NOSE GEAR INTRANSIT LIGHT CYCLED ON AND OFF. AIRCRAFT R ETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR DRAG STRUT WORN. DRAG STRUT AND DRAG STRUT SENSOR WERE REPLACED, P/N 8200103, 864202. GEAR SWINGS WERE COMPLETED. ALL CHECKS WERE GOOD. (M) 2 H 7 2 4T RT A13NM 1996091200379 19960912 00379 NM 1996 9 12 MALA965086 1 19960802 A 2913 570347 HYD PUMP DHAV DHC8 DHC8102 2809003 NM LT NACELLE FAILED A MALA O OTHER J WARNING INDICATION CR CRUISE 1 GL 15 828MA 333 FLT NR 3159 - EN ROUTE, THE AIRCRAFT LOST HYDRAULIC PRESSURE ON THE LEFT SIDE. THE NR 1 STANDBY PUMP WAS IN THE NORMAL POSITION. THE CREW PERFORMED QUICK REFERENCE PROCEDURES AND RETURNED TO DTW. MAINTENANCE REPLACED THE LEFT HYDRAULIC P UMP. ALL CHECKS SATISFACTORY. (M) 2 H 7 2 4T RT A13NM 1996091200380 19960912 00380 SW 1996 9 12 MALA965087 1 19960803 A 5230 HANDLE SWRNGN SA227 SA227AC 8780603 SW CARGO DOOR NOT LATCHED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 426MA AC645 FLT 3412 - AFTER TAKEOFF FROM MSP, THE CARGO DOOR ANNUNCIATOR ILLUMINATED. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE F OUND HANDLE NOT FULLY SECURED. THE LATCH WAS CYCLED SEVERAL TIMES. ALL CHECKS GOOD. (M) 2 L 7 2 4T RT A8SW 1996091200381 19960912 00381 SW 1996 9 12 MALA965088 1 19960807 A 3231 DOOR SWRNGN SA227 SA227AC 8780603 SW NLG OUT OF ADJUST A MALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 15 2692P AC658B FLT 3065 - ON CLIMB-OUT FROM CVG, THE CREW NOTED A VIBRATION FROM THE FRONT SECTION OF THE AIRCRAFT. THE AIRCRAFT RETUR NED TO CVG. MAINTENANCE ADJUSTED THE LEFT NOSE LANDING GEAR DOOR, AFTER FINDING A GAP BETWEEN THE DOOR AND AIR FRAME. ( M) 2 L 7 2 4T RT A8SW 1996091200382 19960912 00382 EU 1996 9 12 MALA965089 1 19960807 A 3350 6104789 BATTERY PACK SAAB SF340 SF340A 7850100 EU CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 119AE 340A119 FLT NR 3453 - DURING THE PREFLIGHT INSPECTION IN DTW, THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE AT SEATS 10C, D AND 9/10A, AND THE LAST AISLE POSITION AT THE REAR OF THE AIRCRAFT. MAINTENANCE REPLACED THE BATTERY PACK AT ROW 9. AL L CHECKS GOOD. (M0 2 L 7 2 4T RT A52EU 1996091200383 19960912 00383 SW 1996 9 12 MALA965090 1 19960810 A 3240 BRAKE SYSTEM SWRNGN SA227 SA227AC 8780603 SW LT MLG REQ'D SERVICE A MALA K NONE O OTHER TX TAXI/GRND HDL 1 GL 15 442MA AC725 FLT 3051 - ON TAXI INTO THE GATE IN DTW, THE LEFT BRAKE PEDAL LOSES PRESSURE WITH CONSTANT APPLICATION. MAINTENANCE BLE D THE BRAKES PER SA227 MM 32-41-00. ALL CHECKS SATISFACTORY. (M) 2 L 7 2 4T RT A8SW 1996091200384 19960912 00384 EU 1996 9 12 MALA965091 1 19960811 A 3350 6104789 BATTERY PACK SAAB SF340 SF340A 7850100 EU CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 119AE 340A119 FLT 3332 - UPON PREFLIGHT, THE LIGHTS WOULD ONLY ILLUMINATE FOR 3 SECONDS WHEN SELECTED ON. MAINTENANCE REPLACED THE EM ERGENCY LIGHT BATTERY PACKS. ALL CHECKS SATISFACTORY. (M) 2 L 7 2 4T RT A52EU 1996091200385 19960912 00385 SW 1996 9 12 MALA965092 1 19960809 A 3260 1EN516 SWITCH SWRNGN SA227 SA227AC 8780603 SW NLG DIRTY A MALA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 15 436MA AC719B FLT NR 3358 - ON APPROACH TO DTW, THE RED NOSE GEAR INTRANSIT LIGHT FAILED TO ILLUMINATE UPON GEAR EXTENSION. MAINTENAN CE CLEANED AND LUBED THE NOSE GEAR SWITCHES. ALL CHECKS GOOD. (M) 2 L 7 2 4T RT A8SW 1996091200386 19960912 00386 NM 1996 9 12 MALA965093 1 19960813 A 5320 85330821107 SILL CAP DHAV DHC8 DHC8102 2809003 NM CARGO DOOR WORN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 854MA 357 DURING A C-CHECK INSPECTION IN INT, MAINTENANCE FOUND THE REAR BAGGAGE UPPER DOOR SILL WORN TO LIMITS. REPAIRS WRE COMP LETED THROUGH COMPLIANCE WITH RD 8-53-2133 AND RD 8-53-2227. (M) 2 H 7 2 4T RT A13NM 1996091200387 19960912 00387 NM 1996 9 12 MALA965094 1 19960814 A 5210 SKIN DHAV DHC8 DHC8102 2809003 NM PAX DOOR DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 854MA 357 DURING SCHEDULED C-CHECK INSPECTION IN INT, MAINTENANCE FOUND SURFACE DENTS IN THE PASSENGER DOOR. REPAIRS WERE COMPLET ED IAW RD8-52-040 BY INSTALLATION OF 2024T-3.050 DOUBLER. (M) 2 H 7 2 4T RT A13NM 1996091200388 19960912 00388 SW 1996 9 12 MALA965095 1 19960813 A 2820 FUEL DIST SYS SWRNGN SA227 SA227AC 8780603 SW LT FUEL TANK MALFUNCTIONED A MALA O OTHER O OTHER CR CRUISE 1 GL 15 2692P AC658B FLT NR 3283 - EN ROUTE TO DTW, THE CREW WAS UNABLE TO TRANSFER FUEL INTO THE LEFT TANK. THE AIRCRAFT CONTINUED TO DTW W ITHOUT INCIDENT. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. FUEL TRANSFERRED NORMALLY, AND AN INSPECTION OF THE FUEL VENT SYSTEM WAS SATISFACTORY. (M) 2 L 7 2 4T RT A8SW 1996091200389 19960912 00389 EU 1996 9 12 MALA965096 1 19960814 A 3350 6104789 BATTERY PACK SAAB SF340 SF340A 7850100 EU CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 119AE 340A119 FLT 3461 - DURING THE PREFLIGHT INSPECTION IN DTW, THE EMERGENCY EXIT LIGHTS AT ROWS 7-9 WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACK. (M) 2 L 7 2 4T RT A52EU 1996091200390 19960912 00390 SW 1996 9 12 MALA965097 1 19960816 A 5400 2735112 ANGLE SWRNGN SA227 SA227AC 8780603 SW LT WING/NACELLE DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 438MA AC721B DURING SCHEDULED MAINTENANCE IN MSP, A CRACK WAS NOTED IN THE LEFT INBOARD LOWER WING TO NACELLE SKIN PATCH. MAINTENANC E REPLACED THE LEFT INBOARD UPPER WING SKIN TO NACELLE ATTACH ANGLE, P/N 27-35112, LEFT INBOARD NACELLE FORMER, P/N 27-3 5025, STRINGER LOCATED AT NS 120, P/N 27-35041-012, AND LEFT INBOARD LOWER WING SKIN TO NACELLE ATTACH ANGLE, P/N 27-351 12-039, IAW FAC SRM 51-40-01 AND 51-40-02. (M) 2 L 7 2 4T RT A8SW 1996091200391 19960912 00391 SW 1996 9 12 MALA965098 1 19960816 A 5320 DOOR FRAME SWRNGN SA227 SA227AC 8780603 SW PAX COMPT DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 438MA AC721B DURING SCHEDULED MAINTENANCE IN MSP, MAINTENANCE FOUND THE LOWER AFT PASSENGER DOOR FRAME CORNER ON THE FUSELAGE TO BE D ENTED. REPAIRS WERE COMPLETED BY REPLACING THE LOWER AFT FUSELAGE PASSENGER DOOR FRAME CORNER, P/N 27-24087-902, IAW SR M 51-30-02, 51-30-03, 51-40-02, AND 51-00-00. (M) 2 L 7 2 4T RT A8SW 1996091200392 19960912 00392 WP 1996 9 12 ORJA9644 1 19960803 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 842RA 49604 EMERGENCY BATTERY FLOOR LIGHT ESCAPE REQUIRES REPLACEMENT. REMOVED AND REPLACED EMERGENCY BATT FLOOR LIGHT ESCAPE PATH. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1996091200393 19960912 00393 WP 1996 9 12 ORJA9645 1 19960805 A 3350 41B994AD073 BATTERY DOUG DC9 DC983 3022083 WP EMPENNAGE DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 875RA 53182 EMPANNAGE WALKWAY OVERHEAD EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK. OPS NORMAL. (M) 2 L 7 2 4F RT A6WE 1996091200394 19960912 00394 WP 1996 9 12 ORJA9646 1 19960813 A 3350 P4010021 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 842RA 49604 FIRST CLASS FLOOR E-TRACK LIGHTS NOT ILLUMINATING. REMOVED AND REPLACED BATTERY PACK FOR FIRST CLASS E-LIGHTING FLOOR T RACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A6WE 1996091200395 19960912 00395 WP 1996 9 12 ORJA9647 2 19960809 A 7261 626447 RELIEF VALVE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D9A 52048 NE LT ENG INOPERATIVE A ORJA E D ENGINE SHUTDOWN RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 WP 11 879RA 53185 DURING TAXI, LEFT ENGINE OIL PRESSURE DROPPED BELOW 40 PSI. SHUT DOWN ENGINE, RETURNED TO GATE. REPLACED LEFT ENGINE O IL PRESSURE RELIEF VLV IAW WITH MM 79-20-03. OPS CHECK GOOD. (M) 2 L 7 2 4F 4 F RT A6WE E2EA 1996091200396 19960912 00396 EA 1996 9 12 PLGA9607262 2 19960726 A 7532 BLEED VLV BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA LT ENGINE MALFUNCTIONED A PLGA O OTHER O OTHER CR CRUISE 1 NE 05 6929M 3N146 UB27 ALB - FLT 4490 - DURING CRUISE FLT FROM BOS TO ALB, THE LEFT ENGINE EXPERIENCED A SERIES OF COMPRESSOR STALLS. THE CREW PULLED BACK POWER AND LANDED IN ALB WITHOUT INCIDENT. THE COMPRESSOR BLEED VALVE WAS REMOVED AND REPLACED AND ENGINE O PS CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A24CE E4EA 1996091200397 19960912 00397 NE 1996 9 12 PLGA9607312 2 19960731 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RIGHT FAILED A PLGA E A ENGINE SHUTDOWN UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CR CRUISE 1 NE 05 340BE 340A062 GEE367379 ALB - FLT 4693 - EN ROUTE FROM BTV TO LGA, THE RIGHT ENGINE OIL LOW PRESSURE WARNING LIGHT ILLUMINATED. THE RIGHT ENGIN E OIL PRESSURE GAUGE READ 10 PSI. THE CREW SHUT DOWN THE ENGINE AND DIVERTED INTO ALB AND LANDED WITHOUT INCIDENT. THE OIL LEVEL WHEN CHECKED WAS 4.1 QTS LOW. THE ENGINE WAS REMOVED AND REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE6 1996091200398 19960912 00398 EU 1996 9 12 SIMA962161 1 19960803 A 3350 3012001 POWER SUPPLY AEROSP ATR72 ATR72212 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 288AM 836 288 FOUND FLOOR PROXIMITY LIGHTS INOP. RAI'D POWER SUPPLY 62WL. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996091200399 19960912 00399 EU 1996 9 12 SIMA962201 1 19960807 A 3350 3011180A POWER SUPPLY AEROSP ATR42 ATR42300 8680920 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 424MQ 285 045 DFW - FOUND EMERGENCY LIGHT POWER SUPPLY AT 3WL DEFECTIVE. RAI'D POWER SUPPLY 3WL IAW ATR 42 JIC 33-51-21, WITH OPERATI ONAL CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996091200400 19960912 00400 EU 1996 9 12 SIMA962211 1 19960808 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 135MQ 3351 135 DFW - FORWARD EMERGENCY LIGHTING INOP. RAI'D BATTERY IN EMERGENCY POWER SUPPLY UNIT AT 29W1 IAW ATR 42 JIC 33-51-21 WIT H OPERATIONAL CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996091200401 19960912 00401 EU 1996 9 12 SIMA962222 1 19960809 A 3350 3011210 SOCKET AEROSP ATR42 ATR42300 8680920 EU AIRSTAIRS SHORTED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 433MQ 229 151 ORD - FLT 4073 - FOUND EMERGENCY LIGHT ON AIRSTAIRS INOP. RAI'D LIGHT ASSEMBLY. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996091200402 19960912 00402 EU 1996 9 12 SIMA962223 1 19960809 A 3397 WIRE AEROSP ATR42 ATR42300 8680920 EU AIRSTAIRS BROKEN A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 427MQ 091 ORD - FLT 4003 - FOUND EMERGENCY LIGHT AT AIRSTAIRS INOP. REPAIRED BROKEN WIRE UNDER AIRSTAIRS. OPS CHECK GOOD. AIRCR AFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996091200403 19960912 00403 EU 1996 9 12 SIMA962231 1 19960810 A 3350 330150 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 376AE 1114 340B376 DFW - DURING MX CHECK, EMERGENCY LIGHTS WERE FOUND TO BE INOP. RAI'D POWER SUPPLY AT LOCATIONS 20LN AND 21LN. OPS CHEC K SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1996091200404 19960912 00404 SO 1996 9 12 SRAA960803 1 19960801 A 3350 44910 LIGHT LKHEED 382 382G 526414U SO CREW DOOR INOPERATIVE A SRAA K NONE L NO TEST IN INSP/MAINT 1 GL 23 920SJ 4561 ON PREFLIGHT, FOUND EMERGENCY EXIT LIGHT BY CREW DOOR NOT WORKING. REPLACED EMERGENCY EXIT LIGHT, OPS CHECKED GOOD PER MM CH33. (M) 2 H 7 4 4T A1SO 1996091200405 19960912 00405 NM 1996 9 12 TWRA96276 1 19960814 A 3397 WIRE BOEING 747 747130 1384880 NM CABIN CHAFED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 603FF 19746 DURING DAILY CHECK, FOUND NR 2L MAIN ENTRY DOOR UPPER DOOR BUSTLE LIGHT INOP. FOUND CHAFED WIRE AT BUSTLE LIGHT CONNECT OR. REPAIR WIRING AND OPS CHECKED NORMAL PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996091200406 19960912 00406 NM 1996 9 12 TWRA96277 1 19960816 A 3350 S1356B37 LIGHT BOEING 747 747212B 1384886 NM L2 DOOR WEAK A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 619FF 21316 DURING DAILY CHECK, FOUND EMERGENCY OVERHEAD LIGHT JUST AFT OF L2 DOOR WEAK. REMOVED AND REPLACED LIGHT ASSY. OPS CHEC KED OK PR MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996091200407 19960912 00407 NM 1996 9 12 TWRA96278 1 19960816 A 3350 S1356B37 LIGHT BOEING 747 747212B 1384886 NM L4 DOOR INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 616FF 21939 DURING DAILY CHECK, FOUND EVAC SILL OVERHEAD LIGHT INOP BY L4 MED. REMOVED AND REPLACED LIGHT ASSY. OPS CHECKED OK PR MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996091200408 19960912 00408 NM 1996 9 12 TWRA96279 1 19960816 A 3350 S1356B37 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 616FF 21939 DURING DAILY CHECK, FOUND EVAC EMERGENCY CEILING LIGHT BY SEAT 52H INOP. REMOVED AND REPLACED LIGHT ASSY. OPS CHECKED GOOD AS PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996091200409 19960912 00409 NM 1996 9 12 TWRA96280 1 19960818 A 3350 58541 LIGHT BOEING 747 747282B 1384860 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 611FF 20502 DURING DAILY CHECK, FOUND FLOOR EVAC EGRESS LIGHT STRIP INOP BETWEEN SEATS ROW 20ABC. REPLACED BROKEN POWER STRIP. OPS CHECKED GOOD PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996091200410 19960912 00410 NM 1996 9 12 TWRA96281 1 19960817 A 3397 WIRE BOEING 747 747136 1384883 NM CABIN BROKEN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 606FF 20273 DURING DAILY CHECK, 'A' ZONE SPIRAL STAIRCASE AND FORWARD GALLEY EVAC LIGHT STRIP INOP. REPAIRED BROKEN WIRE 'A' ZONE. OPS CHECKED GOOD AS PER 33-51-00. (M) 2 L 7 4 4F A20WE 1996091200411 19960912 00411 NM 1996 9 12 TWRA96282 1 19960813 A 3350 3004083 LIGHT BOEING 747 747121 1384871 NM OVERWING INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 604FF 19659 DURING DAILY CHECK, FOUND NR 4 RIGHT OVERWING EMERGENCY LIGHT FWD LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY. OPS CHE CKED NORMAL PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996091200412 19960912 00412 NM 1996 9 12 TWRA96284 1 19960822 A 3350 S1356B37 LIGHT BOEING 747 747136 1384883 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 606FF 20273 DURING DAILY CHECK, FOUND 20H CEILING EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED LIGHT ASSY. OPS CHECKED GOOD PER M M 33-51-00. (M) 2 L 7 4 4F A20WE 1996091200413 19960912 00413 NM 1996 9 12 TWRA96285 1 19960828 A 3350 S1356B37 LIGHT BOEING 747 747259B NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 EICEO 21730 DURING DAILY CHECK, FOUND AFT CEILING EVAC LIGHT IN C-ZONE INOP. REMOVED AND REPLACED LIGHT ASSY, OPS CHECKED NORMAL PE R MM 33-51-00. (M) 2 L 7 4 4F RT A20WE 1996091200414 19960912 00414 NM 1996 9 12 TWRA96286 1 19960820 A 3350 S1356B37 LIGHT BOEING 747 747259B NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 EICEO 21730 DURING DAILY CHECK, FOUND FIRST EVAC CEILING LIGHT IN B-ZONE INOP. REMOVED AND REPLACED LIGHT ASSY. OPS CHECKED NORMAL PER MM 33-51-00. (M) 2 L 7 4 4F RT A20WE 1996091200415 19960912 00415 NM 1996 9 12 TWRA96287 1 19960821 A 3350 900835A BATTERY PACK BOEING 747 747121 1384871 NM CABIN DISCHARGED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 609FF 20354 DURING DAILY CHECK, FOUND EXIT SIGN ABOVE ROW 32 HJK INOP. REPLACED BATTERY PACK. OPS CHECKED OK PER MM 33-51-00 PAGE 501. (M) 2 L 7 4 4F A20WE 1996091200416 19960912 00416 NM 1996 9 12 TWRA96288 1 19960821 A 3350 3004083 LIGHT BOEING 747 747121 1384871 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 609FF 20354 DURING DAILY CHECK, FOUND 3L OVERWING EXIT LIGHT INOP. REMOVED AND REPLACED 3L OVERWING 'EXIT LIGHT' PER MM 33-51-00 PG 401. OPS CHECKED NORMAL. (M) 2 L 7 4 4F A20WE 1996091200417 19960912 00417 NM 1996 9 12 TWRA9669 1 19960630 A 3350 LENS BOEING 747 747212B 1384886 NM CABIN MISSING A TWRA K NONE O OTHER IN INSP/MAINT 1 EA 15 618FF 21937 FLOOR PATH LIGHT MISSING LENS AND NOT SECURED 11 ABC, 12 ABC, 15 ABC, 30 ABC, 53 ABC, 45 KJH, 35 KJH AND 31 KJH. RELAMP ED AND PLACED LENS, OPS OK. (M) 2 L 7 4 4F A20WE 1996091200418 19960912 00418 WP 1996 9 12 USAAD96112 1 19960810 A 3350 AD20131A BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 912VJ 47020 FORWARD SECTION OF EMERGENCY LIGHTS INOPERATIVE. REPLACED FORWARD BATTERY PACK. (M) 2 L 7 2 4F A6WE 1996091200419 19960912 00419 WP 1996 9 12 USAAD96113 2 19960810 A 7261 7958522501 OIL PRESS SW DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9A 52048 NE RT ENGINE LEAKING A A USAA E ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 EA 19 931VJ 47188 FLT 458 - LGA-ROC - DURING CRUISE, APPROXIMATELY 70 MILES SOUTHEAST OF ROC, THE NR 2 ENGINE OIL PRESSURE GAUGE BEGAN TO FLUCTUATE. OIL QUANTITY BEGAN TO DECREASE, AND OIL TEMPERATURE BEGAN TO RISE. THE ENGINE WAS SHUT DOWN, AND THE AIRCRA FT LANDED AT ROC. SINGLE ENGINE TIME WAS 17 MINUTES. FOUND ANTI-ICE DUCT TO COWL VALVE BROKEN AND LOW OIL PRESSURE CAU TION SWITCH LEAKING. REPLACED DUCT, SWITCH, AND SWITCH CANNON PLUG. (M) 2 L 7 2 4F 4 F A6WE E2EA 1996091200420 19960912 00420 WP 1996 9 12 USAAD96114 1 19960811 A 3610 59382501 MANIFOLD DOUG DC9 DC982 3022082 WP RT ENGINE FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 815US 48095 FLT NR 1085 - PIT-TPA - AFTER TAKEOFF, RIGHT AIR CONDITIONING SUPPLY TEMP HI LIGHT ILLUMINATED, FOLLOWED BY RIGHT ENGINE FIRE LIGHT. EXTINGUISHED WHEN THROTTLE WAS RETARDED. RETURNED TO FIELD. REPLACED RIGHT ENGINE 8TH STAGE BLEED MANIFO LD DUE TO LEAK. (M) 2 L 7 2 4F A6WE 1996091200421 19960912 00421 NM 1996 9 12 USAASB96133 1 19960717 A 2612 FIRE LOOP BOEING 737 7373B7 1384580 NM NR 1 ENGINE MALFUNCTIONED A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 506AU 23381 BWI - FLT 378 - AT CRUISE, CAPTAIN RECEIVED AN ENGINE OVERHEAT/FIRE INDICATION ON THE NR 1 ENGINE. WITH POWER REDUCED T O ENGINE IDLE, THE INDICATION REMAINED. FLIGHT DIVERTED TO BWI. NO EMERGENCY WAS DECLARED AND THE NR 1 ENGINE WAS NOT SHUT DOWN. FLIGHT LANDED WITH NO FURTHER INCIDENT. MX REPLACED THE NR 1 ENGINE FIRE DETECTOR LOOP ASSEMBLY, THE FIRE/O VERHEAT CONTROL MODULE AND THE ENGINE/APU FIRE CONTROL PANEL. SYSTEM OPERATIONAL CHECKS AND TESTS NORMAL. RAN ENGINE, 'A' LOOP CHECKS NORMAL. FIRE DET LOOP ASSY P/N 6678, FIRE/OVERHEAT CONT MODULE P/N 6594-01, ENGINE/APU FIRE CONTROL PAN EL P/N 69-37307-145. (M) 2 L 7 2 4F RT A16WE 1996091200422 19960912 00422 EU 1996 9 12 USAASB96146 2 19960801 A 7200 ENGINE BOEING 737 7372B7 1384560 NM CFMINT CFM56 CFM563B2 13802 EU RIGHT FAILED A A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 529AU 31141 24411 721341 SEA - FLT 100 - FLIGHT CREW OBSERVED THAT THE NR 2 ENGINE WAS CONSUMING MORE OIL THAN NORMAL AFTER DEPARTURE FROM SEA. C HECKING THE EN ROUTE TIME LEFT TO CLT, THEY FELT THEY WOULD NOT HAVE ENOUGH OIL TO MAKE CLT. THEY WERE NOT SURE IF IT W AS A LEAK AND/OR A HIGH OIL CONSUMPTION PROBLEM. CREW ELECTED TO RETURN TO FIELD AT SEA. THE ENGINE WAS NOT SHUTDOWN A ND THE FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 ENGINE ASSEMBLY PER JOB CARD. OPERATIONAL CHECK AND LEAK CHECK NORMAL. (M) 2 L 7 2 4F 4 F A16WE E21EU 1996091200423 19960912 00423 NM 1996 9 12 USAASB96152 1 19960813 A 2130 PRESSURIZATION BOEING 737 737401 1384701 NM CABIN MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 418US 23985 BOS - FLT 157 - DURING CLIMB-OUT FROM BOS EN ROUTE TO PIT, CAPTAIN NOTICED AIRCRAFT WAS NOT PRESSURIZING. THE CABIN PRE SSURE WAS NOT HOLDING. FLIGHT WAS AT 8,000 FEET AND CAPTAIN DECIDED TO RETURN TO FIELD AT BOS. ON DESCENT AND APPROACH , CABIN PRESSURE WAS ERRATIC. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE CHECKED ALL DUCTING AND PRESSURIZED AIRCRAFT WITH BOTH ENGINES AND APU. ALL SYSTEMS OPERATE NORMAL. (M) 2 L 7 2 4F RT A16WE 1996091200424 19960912 00424 NM 1996 9 12 USAASB96153 1 19960814 A 3230 RETRACT MECH BOEING 737 737201 1384454 NM LANDING GEAR MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 243US 22445 GOO - FLT 8028 - AFTER TAKEOFF FROM GSO, CAPTAIN WAS UNABLE TO RAISE LANDING GEAR LEVER. TWO OTHER ATTEMPTS WERE MADE B UT WERE UNSUCCESSFUL. CIRCUIT BREAKERS WERE ALL IN AND GEAR PINS WERE ONBOARD. CAPTAIN ELECTED TO RETURN TO FIELD AT G SO. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITH NO FURTHER INCIDENT. MX WAS UNABLE TO DUPLICATE AND REPLACED THE FOLLOWING COMPONENTS IN THE LANDING GEAR ACCESSORY UNIT AS PRECAUTIONARY: A2 AIR SENSE SQUAT CIRCUIT CARD, P/N 8-060 -02 AND HE K3 AIR SENSE SQUAT RELAY, P/N BACR13CG2A. PERFORMED ADJUSTMENT/TEST IS ASSOCIATION WITH MM 32-09-100. SWUNG GEAR SEVERAL TIMES. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1996091200425 19960912 00425 NM 1996 9 12 USAASB96160 1 19960817 A 3411 36024F2360104 STATIC LINE BOEING 737 7373B7 1384580 NM E/E COMPT LOOSE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 526AU 23861 IND - FL 2116 - SHORTLY AFTER TAKEOFF, CAPTAIN REPORTED THAT THE FIRST OFFCERS AIR DATA INSTRUMENTS FAILED. AIRSPEED IN DICATOR, ALTIMETER, IVSI CAPTAINS INSTRUMENTS WERE OK. THE AUTOTHROTTLES KICKED OFF, A GRADUAL DECREASE IN PITOT STATIC SYSTEM AND THE STALL WARNING SHAKER CAME ON UNTIL FLAPS WERE UP. CAPTAIN ELECTED TO RETURN TO FIELD AT IND. NO EMERGE NCY WAS DECLARED AND THE FLIGHT LANDED WITH NO FURTHER INCIDENT. UPON INSPECTION, MAINTENANCE FOUND THE NR 2 AIR DATA C OMPUTER STATIC LINE LOOSE. RECONNECTED AND PERFORMED PITOT STATIC TEST PER MM 34-11. PERFORMED CHECK OF DADC SYSTEM PE R FMC. ALL INDICATIONS WITHIN LIMITS. (M) 2 L 7 2 4F RT A16WE 1996091200426 19960912 00426 EU 1996 9 12 WTAA960148 1 19960719 A 3250 MS3476L833S CONNECTOR BAG JETSTM JETSTM3101 1500215 EU NLG STEERING DIRTY A WTAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 WP 17 420UE 788 SEA - GROUND PROXIMITY SYSTEM GEAR WARNING SOUNDED ON FINAL APPROACH. CREW ACCOMPLISHED MISSED APPROACH. FOUND LANDING GEAR CONTROL WARNING CIRCUIT BREAKER TRIPPED. RESET CIRCUIT BREAKER. ALL INDICATIONS NORMAL. ALL INDICATIONS NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED LANDING GEAR RETRACTION AND INDICATION SYSTEM. CLEANED CONTA MINANTS FROM CANNON PLUG ON STEERING ISOLATION SOLENOID VALVE. ALL GEAR INDICATIONS NORMAL ON GROUND RETRACTION TEST. A IRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996091200427 19960912 00427 SO 1996 9 12 WTAA960149 1 19960721 A 3150 MS33202 CIRCUIT BREAKER EMB 120 EMB120RT SO COCKPIT TRIPPED A WTAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 17 276UE 120067 FAT - TAKEOFF TRIM AURAL WARNING SOUNDED TO TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE FOUND AURAL WA RNING CIRCUIT BREAKER PULLED. RESET CIRCUIT BREAKER. SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4T RT A31SO 1996091200428 19960912 00428 SO 1996 9 12 WTAA960150 1 19960719 A 3260 120025226501 CONTROL BOX EMB 120 EMB120RT SO COCKPIT FAILED A WTAA O OTHER N FALSE WARNING AP APPROACH 1 WP 17 276UE 120067 SFO - NOSE LANDING GEAR GREEN 'A' INDICATION ONLY ILLUMINATED AFTER THREE RETRACTIONS ON FINAL APPROACH TO SFO. MAINTEN ANCE DEFERRED 'B' SYSTEM PER MEL 32-60-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL BY A DJUSTING NOSE LANDING GEAR DOWN LOCK PROXIMITY SENSOR AND REPLACING SELECTOR CONTROL. (M) 2 L 7 2 4T RT A31SO 1996091200429 19960912 00429 EU 1996 9 12 WTAA960151 1 19960726 A 7712 310261411 CONNECTOR BAG JETSTM JETSTM3101 1500215 EU LT ENGINE DIRTY A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 17 103XV 747 SEA - LEFT ENGINE SURGING 30 PERCENT TORQUE ON TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE ADJUSTED CO MPENSATING RESISTOR AND CLEANED TORQUE RING CANNON PLUG. NO DISCREPANCIES NOTED ON GROUND RUN. AIRCRAFT RETURNED TO SE RVICE. (M) 2 L 7 2 4T RT A21EU 1996091200430 19960912 00430 SO 1996 9 12 WTAA960156 1 19960804 A 3231 1204327 RELAY BOX EMB 120 EMB120RT SO GEAR DOORS FAILED A WTAA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 17 250YV 120250 FAT - ALL GEAR DOORS REMAIN OPEN AFTER GEAR IS DOWN AND LOCKED. MAINTENANCE REPLACED LANDING GEAR RELAY BOX. SYSTEM OP ERATIONAL CHECK NORMAL DURING GEAR RETRACTION CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996091200431 19960912 00431 SO 1996 9 12 WTAA960157 1 19960804 A 3234 12038594001 SELECTOR EMB 120 EMB120RT SO GEAR DOORS FAILED A WTAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 17 250YV 120250 FAT - ON GEAR RETRACTION AFTER DEPARTURE GEAR DOORS FAILED TO CLOSE. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MA INTENANCE REPLACED LANDING GEAR SELECTOR. SYSTEM OPERATIONAL CHECK NORMAL DURING GEAR RETRACTION CHECK. AIRCRAFT RETUR NED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996091200432 19960912 00432 WP 1996 9 12 WTAA960160 2 19960807 A 7200 ENGINE BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110U 01514 WP LEFT ERRATIC RPM A A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 17 103XV 747 SEA - LEFT ENGINE RPM REPORTED ERRATIC UPON POWER APPLICATION ON TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINT ENANCE PERFORMED FULL POWER ENGINE GROUND RUN WITH FRICTION LOCK SET ON SPEED LEVER. NO DISCREPANCIES NOTED. UNABLE TO DUPLICATE REPORTED DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A21EU E4WE 1996091200433 19960912 00433 NM 1996 9 12 CALA0961268 1 19960906 A 2121 215201 AIR DIST FAN BOEING 737 737291 138448W NM AIR COND BAY INOPERATIVE A CALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 09 15255 19183 4508 21069 THE ODOR OF SMOKE WAS OBSERVED IN THE CABIN AFTER TAKEOFF, BUT THE ODOR QUICKLY WENT AWAY. THE ODOR RETURNED AFTER LEVE LING OFF AT CRUISE. THE AIRCRAFT WAS DIVERTED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AIR DISTR IBUTION FAN CIRCUIT BREAKER POPPED. THE CIRCUIT BREAKER WOULD NOT RESET. THE AIR DISTRIBUTION FAN WAS FOUND BURNED AND INOPERATIVE. THE FAN WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. 2 L 7 2 4F A16WE 1996091200434 19960912 00434 NE 1996 9 12 CALA9601269 2 19960907 A 7230 790762 STATOR SUPP DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE 8TH STAGE BROKEN A CALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 09 18833 49493 717359 THE NR 1 ENGINE GAVE A LOUD BANG AND SPOOLED DOWN SHORTLY AFTER TAKEOFF AT 1800 FEET. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED. *S/D* SHOP FINDINGS REVEALED 8TH STAGE ST ATOR SUPPORT FAILURE. 2 L 7 2 4F 4 F A6WE E9NE 1996091200435 19960912 00435 WP 1996 9 12 CALA9601270 1 19960820 A 5210 BEAM DOUG DC9 DC931 3022065 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14564 47490 INSPECTION FOUND ONE CRACK IN EACH OF MAIN CABIN DOOR BEAMS NR 1, 5 AND 7. THE CRACKS WERE .25 TO 1 INCH IN LENGTH. TH E CRACKS WERE REPAIRED IAW SRM 52-05, FIGURE 31. 2 L 7 2 4F A6WE 1996091200436 19960912 00436 WP 1996 9 12 CALA9601271 1 19960821 A 5320 DOUBLER DOUG DC9 DC931 3022065 WP BS 408 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14564 47490 INSPECTION FOUND A .5 INCH CRACK IN DOUBLER JUST AFT OF STA 408, LONGERON 30. A NEW DOUBLER WAS INSTALLED IAW SRM 51-30 -2. 2 L 7 2 4F A6WE 1996091200437 19960912 00437 WP 1996 9 12 CALA9601272 1 19960821 A 5312 BULKHEAD FRAME DOUG DC9 DC931 3022065 WP BS 756 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14564 47490 INSPECTION FOUND A .5 INCH CRACK IN AFT PIT FORWARD BULKHEAD FRAME AT STA 756, LONGERON 26R. A DOUBLER WAS INSTALLED IA W SRM 53-01. 2 L 7 2 4F A6WE 1996091200438 19960912 00438 WP 1996 9 12 CALA9601273 1 19960822 A 5320 ANGLE DOUG DC9 DC931 3022065 WP BS 637.5 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14564 47490 INSPECTION FOUND A .5 INCH CRACK ON REPAIR ANGLE FOR FORMER IN LEFT KEEL BEAM AREA, STA 637.5. A NEW ANGLE WAS INSTALLE D IAW SRM 53-03. 2 L 7 2 4F A6WE 1996091200439 19960912 00439 WP 1996 9 12 CALA9601274 1 19960821 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 622 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14564 47490 INSPECTION FOUND A .5 INCH CRACK IN FITTING IN LEFT KEEL BEAM AREA, STA 622. A REPAIR ANGLE WAS INSTALLED IAW SRM 53-03 . 2 L 7 2 4F A6WE 1996091200440 19960912 00440 NM 1996 9 12 CALA9601275 1 19960907 A 3252 65447713 SHIMMY DAMPER BOEING 737 7373T0 1384582 NM RT MLG FAILED A CALA O OTHER O OTHER LD LANDING 1 SW 09 14307 29472 29472 23358 THE AIRCRAFT BEGAN TO BOUNCE UP AND DOWN SOON AFTER LANDING. THE BOUNCING STOPPED AFTER THE AIRCRAFT SLOWED TO 100 KNOT S, BUT THEN PULLED TO THE LEFT. THE AIRCRAFT WAS STOPPED AND TAXIED OFF THE RUNWAY. MAINTENANCE FOUND THE RT MLG SHIMM Y DAMPER HAD FAILED (BENT) AND THE RT MLG LOWER TORSION LINK WAS SHEARED. THE RT MLG CENTER AND INNER DOORS SUSTAINED D AMAGE FROM THE FAILURE. THE RT MLG SHIMMY DAMPER AND LOWER TORSION LINK WERE REMOVED AND REPLACED. THE RT MLG UPPER TO RSION LINK WAS REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. BOTH THE RT MLG CENTER AND INNER DOORS WERE REMOVED AND REPLACED. IN ADDITION, BOTH RT MLG TIRES AND BRAKES WERE REMOVED AND REPLACED. A SIDE LOAD INSPECTION WAS COMPLIED WI 2 L 7 2 4F RT A16WE 1996091200441 19960912 00441 WP 1996 9 12 6302649988 1 19960127 A 7711 EPR INDICATOR DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9A 52048 NE NR 1 ENGINE FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 8944E 47167 666927 THE NR 1 ENGINE EPR INDICATION WAS ERRATIC ON TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. M AINTENANCE REPLACED THE INDICATOR WITH A SERVICEABLE UNIT. 2 L 7 2 4F 4 F A6WE E2EA 1996091200442 19960912 00442 WP 1996 9 12 9619329609 1 19960902 A 3350 6011779 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN MALFUNCTIONED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 609NW 47234 DURING LINE MAINTENANCE INSPECTION, FOUND THE LEFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY AND POWER SUP PLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996091200443 19960912 00443 WP 1996 9 12 9619339931 1 19960830 A 2910 O-RING DOUG DC9 DC931 3022065 WP RT HYD RES BROKEN A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 90S 47244 RIGHT HYDRAULIC SYSTEM QUANTITY DECREASED TO ONE QUART EN ROUTE. WHEN RIGHT PUMPS WERE TURNED OFF, QUANTITY INCREASED T O FIFTEEN QUARTS. FLIGHT DIVERTED TO MCI AND LANDED WITHOUT INCIDENT. GEAR WAS LOWERED USING ALTERNATE EXTENSION PROCE DURES. MAINTENANCE FOUND O-RING BROKEN ON FITTING AT BOTTOM OF RIGHT HYDRAULIC RESERVOIR. REPLACED O-RING AND FILLED T O PROPER LEVELS, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996091200444 19960912 00444 NM 1996 9 12 9619342761 1 19960831 A 2752 MS9391130ZE4C DRIVE MOTOR BOEING 727 7272M7 138407S NM LT TE FLAP FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 721RW 42513 25455 21200 DURING CLIMBOUT, LOST SYSTEM A-HYDRAULICS. REPLACED LEFT FLAP DRIVE MOTOR, LEAK AND OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996091200445 19960912 00445 NM 1996 9 12 9619352717 1 19960905 A 2161 TEMP CONTROLLER BOEING 727 7272S7 138407Z NM LT PACK FAILED A NWAA B G EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 GL 01 721RX 22492 DURING CRUISE, THE LEFT PACK TRIPPED, COULD NOT RESET. CABIN WAS CLIMBING WHILE DESCENDING TO FL250 AND WOULD NOT HOLD, MADE RAPID DESCENT TO 10,000 FT, REGAINED LEFT PACK AT 10,000 FT. PASSENGER OXYGEN MASKS WERE DEPLOYED. AIRCRAFT LAND ED WITHOUT INCIDENT AT DESTINATION. PERFORMED SYSTEM CHECK OF LEFT AND RIGHT AIR CONDITIONING PACKS, LEFT AUTO TEMPERAT URE CONTROLLER WAS FOUND INOPERATIVE AND PLACED ON MEL. PERFORMED VESSEL LEAK CHECK AND FOUND WITHIN LIMITS. 2 L 7 3 4F A3WE 1996091200446 19960912 00446 NM 1996 9 12 9619366304 1 19960907 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 664US 23819 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE AT LAVATORY DR2R, DL4L2 AND AT DOOR 3R. RECONNECTED WI RES AND REPLACED LIGHT SOCKETS, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1996091200447 19960912 00447 WP 1996 9 12 9619379884 1 19960908 A 7312 320115 FUEL HEAT VALVE DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE LT ENGINE FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 677MC 47756 688231 WHILE APPLYING TAKEOFF POWER, THE LEFT ENGINE FUEL HEAT LIGHT ILLUMINATED. CREW ABORTED TAKEOFF AND THE SYSTEM WAS PLAC ED ON MEL. FLIGHT RESUMED AS SCHEDULED. MAINTENANCE REPLACED THE LEFT ENGINE FUEL HEAT VALVE. OPERATIONAL CHECKED OK. 2 L 7 2 4F 4 F A6WE E2EA 1996091200448 19960912 00448 NE 1996 9 12 9619389139 2 19960908 A 7510 CIRCUIT BREAKER DOUG DC9 DC914 3022034 WP PWA JT8 JT8D7 52053 NE LT FUEL HEAT TRIPPED A NWAA O OTHER M J OVER TEMP WARNING INDICATION CR CRUISE 1 GL 01 948L 47049 657567 DURING FLIGHT, THE LEFT ENGINE FUEL HEAT LIGHT ILLUMINATED WITH ASSOCIATED HIGH OIL TEMPERATURE. CREW DECLARED AN EMERG ENCY AND LANDED AT SCHEDULED DESTINATION WITHOUT INCIDENT. MAINTENANCE RESET LEFT ENGINE FUEL HEAT CIRCUIT BREAKER. IN SPECTED FUEL HEAT VALVE AND CONNECTOR. OPERATED SYSTEM NUMEROUS TIMES, CHECKED OK. 2 L 7 2 4F 4 F A6WE E2EA 1996091200449 19960912 00449 EU 1996 9 12 9619393237 1 19960906 A 3350 321430 BATTERY AIRBUS 320 A320212 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 337NW 358 DURING LINE MAINTENANCE, THE EMERGENCY LIGHTS TEST FAULTED THE LEFT AND RIGHT BATTERIES. REPLACED BATTERIES, OPERATIONA L CHECK OK. 2 L 7 2 4F RT A28NM 1996091200450 19960912 00450 EU 1996 9 12 9619403244 1 19960907 A 3350 321430 BATTERY AIRBUS 320 A320212 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 344NW 388 DURING LINE MAINTENANCE CHECK OF THE EMERGENCY LIGHTS SYSTEM BATTERY PACK CAPACITY CHECK, FOUR BATTERY PACKS REQUIRED RE PLACEMENT. REPLACED BATTERY PACKS, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996091200451 19960912 00451 EU 1996 9 12 9619413220 1 19960905 A 2920 680206122 RAM AIR TURBINE AIRBUS 320 A320211 3930320 EU AFT FUSELAGE DEPLOYED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 320US 13213 213 WHILE CLIMBING THROUGH 42,000 FEET, THE RAT OUT MESSAGE DISPLAYED AND THE EMERGENCY GENERATOR SHOWED POWER UP. AIRCRAFT RETURNED TO SFO AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING REVEALED NO DISCREPANCIES. 2 L 7 2 4F RT A28NM 1996091200452 19960912 00452 NM 1996 9 12 9619202715 1 19960817 A 5330 SKIN BOEING 727 7272S7 138407Z NM BS 720E CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 719RC 22490 DURING H-CHECK, FOUND A ONE INCH CRACK IN THE FUSELAGE SKIN AT BS 720E AND STR 18R. REPAIRED SKIN (P/N 65-54588-24) PER EA 27-106292. 2 L 7 3 4F A3WE 1996091200453 19960912 00453 WP 1996 9 12 9619211162 1 19960828 A 5320 WEB DOUG DC10 DC1040 3023508 WP DOOR 3L CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 162US 46771 DURING T-CHECK, FOUND THREE CRACKS IN DOOR 3L LOWER FORWARD SIDE WEB. REPAIRED WEB (P/N AEA 0115-1) PER EA 11-106311. 2 L 7 3 4F A22WE 1996091200454 19960912 00454 EU 1996 9 12 9619223203 1 19960828 A 5322 SUPPORT AIRBUS 320 A320211 3930320 EU BS 32074-32571 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 303US 34 DURING PERIODIC CHECK, FOUND CORROSION ON THE AFT GALLEY FRAMES 67 TO 68 FLOOR SUPPORT AT Y=765MM. 2 L 7 2 4F RT A28NM 1996091200455 19960912 00455 WP 1996 9 12 9619231162 1 19960829 A 5753 SUPPORT DOUG DC10 DC1040 3023508 WP LT TE FLAP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 162US 46771 DURING T-CHECK, FOUND A CRACK IN THE LEFT FLAP INBOARD FLAP SUPPORT BASE PLATE AT STA 1521. REPAIRED PLATE (P/N ANB 717 0) PER EA 11-110179. 2 L 7 3 4F A22WE 1996091200456 19960912 00456 WP 1996 9 12 9619241162 1 19960830 A 5330 SKIN DOUG DC10 DC1040 3023508 WP BS 535 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 162US 46771 DURING T-CHECK, FOUND A CRACK IN THE NR 3 AIR CONDITIONING PACK CUTOUT SKIN UPPER AFT CORNER FS 535. REPAIRED SKIN (P/N ACA 3108-501) PER EA 11-110184. 2 L 7 3 4F A22WE 1996091200457 19960912 00457 WP 1996 9 12 9619259106 1 19960830 A 5312 BULKHEAD DOUBLER DOUG DC9 DC915 3022036 WP AFT PRESS BLKHD CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 96S 47206 DURING LINE CHECK, FOUND A 0.3 INCH CRACK IN THE AFT PRESSURE BULKHEAD -9 DOUBLER IN THE AFT ENTRY DOOR JAMB. REPLACED DOUBLER SECTION PER EA DC9-53-031. 2 L 7 2 4F A6WE 1996091200458 19960912 00458 WP 1996 9 12 9619269106 1 19960901 A 5312 BULKHEAD DOUBLER DOUG DC9 DC915 3022036 WP AFT PRESS BLKHD CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 96S 47206 DURING LINE CHECK, FOUND CRACKS IN THE AFT PRESSURE BULKHEAD UPPER FORWARD DOUBLER AT THE UPPER LEFT AND RIGHT DOOR STOP S IN THE -13 DOUBLER AT THE UPPER LEFT AND RIGHT DOOR CUTOUTS AND IN THE -11 DOUBLER AT THE UPPER DOOR JAMB CORNER. REP AIRED ALL DAMAGE PER EA DC9-53-029. 2 L 7 2 4F A6WE 1996091200459 19960912 00459 WP 1996 9 12 9619279930 1 19960903 A 5753 FITTING DOUG DC9 DC931 3022065 WP NR 4 TE FLAP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 89S 47042 DURING H-CHECK, FOUND A CRACK IN THE NR 4 TRAILING EDGE FLAP INBOARD RIB TO SKIN ATTACH FITTING. REPLACED FITTING PER S RM 51-30-2. 2 L 7 2 4F A6WE 1996091200460 19960912 00460 WP 1996 9 12 9619289928 1 19960903 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 870-937 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8921E 45836 DURING M-CHECK, FOUND CORROSION ON LONGERON 23L FROM FS 870 TO 937. REPAIRED LONGERON PER EA DC9-53-033. 2 L 7 2 4F A6WE 1996091200461 19960912 00461 WP 1996 9 12 9619299180 1 19960904 A 5320 FITTING DOUG DC9 DC914 3022034 WP BS 168 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3312L 45707 DURING H-CHECK, FOUND CORROSION ON THE FS 168 FRAME T-FITTING AT THE SERVICE DOOR CUTOUT. REPLACED FITTING PER SRM 51-3 0-5. 2 L 7 2 4F A6WE 1996091200462 19960912 00462 WP 1996 9 12 9619309928 1 19960904 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 897-917 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8921E 45836 DURING M-CHECK, FOUND CORROSION ON THE INTERIOR FUSELAGE SKIN AT LONGERON 24L AT BOTH FS 897 AND FS 917. REPAIRED SKIN PER EA DC9-53-033. 2 L 7 2 4F A6WE 1996091200463 19960912 00463 WP 1996 9 12 9619319933 1 19960906 A 5312 BULKHEAD FITTING DOUG DC9 DC931 3022065 WP AFT PRESS BLKHD CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 1334U 47280 DURING H-CHECK, FOUND A CRACK IN THE FORWARD CARGO COMPARTMENT AFT BULKHEAD FITTING AT LONGERON 24L. REPLACED FITTING P ER SRM 51-30-2, 51-30-5. 2 L 7 2 4F A6WE 1996091200464 19960912 00464 1996 9 12 COMA9610273 3 19960905 A 6140 SEL0C29DH INDICATOR EMB 120 EMB120RT SO INST PANEL FAILED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 268CA 6803 120262 THE RT NP INDICATOR FAILED DURING TAKEOFF. REPLACED NP INDICATOR. 2 L 7 2 4T RT A31SO 1996091200465 19960912 00465 NE 1996 9 12 COMA9610274 2 19960904 A 7250 MS969611 BOLT EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE BROKEN A A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 196CA 2646 120196 115601 NO NP OR TORQUE INDICATION AFTER ENGINE START. PROPELLER WAS NOT ROTATING. AFTER ENGINE SHUT DOWN THE PROPELLER COULD NOT BE TURNED BY HAND. WHEN ENGINE DISASSEMBLED, A BROKEN INTERSTAGE CASE BOLT WAS FOUND TO BE JAMMING THE 1ST STAGE PO WER TURBINE DISK. BOLT AND POWER TURBINE WERE REPLACED AND ENGINE RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A31SO E20NE 1996091200466 19960912 00466 NM 1996 9 12 UPS96221044 1 19960909 A 3350 1000677 LIGHT BOEING 727 727172C 1384058 NM CABIN DEFECTIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 916UP 19808 INSPECTION TYPE N/A ON PRE-DEP CK, ENTRY DOOR EMER EXIT LIGHT INOP. REPLACED LIGHT ASSY (P/N 10-0067-7) (S/N 4255) ON, (S/N 22574) OFF, MRR FILED. 2 L 7 3 4F A3WE 1996091200467 19960912 00467 NM 1996 9 12 UPS96221046 1 19960827 A 5320 STIFFENER BOEING 727 72725C 138400H NM BS 1243 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-C, STIFFENER UNDER AIRSTAIR/CARGO DOOR MANUAL PUMP CRACKED AND HAS HOLE WORN THROUGH. FABRICATED AND IN STALLED REPAIR ANGLE PER SRM 51-40-3, 51-30-2. 2 L 7 3 4F A3WE 1996091200468 19960912 00468 NM 1996 9 12 UPS96221047 1 19960909 A 5311 FRAME BOEING 727 7272A1 138407F NM BS 1148 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-C, CORROSION ON FAIL-SAFE ANGLE ON FRAME AT BS 1148 RBL 1 AFT SIDE. REMOVED CORROSION FOUND TO BE OUT O F LIMITS PER SRM 53-10-1, CUTOUT DAMAGE AREA AND REPAIRED PER SRM 51-40-3. 2 L 7 3 4F A3WE 1996091200469 19960912 00469 NM 1996 9 12 UPS96221048 1 19960909 A 5320 655784812 FITTING BOEING 727 7272A1 138407F NM FWD CARGO PIT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-C, CORROSION ON CARGO TIE DOWN AT STA 720C RBL 23 WL 156. REMOVED CARGO TIE DOWN AND REPLACED WITH NEW PART PER SRM 51-30-2, 51-10-1, 51-20-4, 51-30-5. 2 L 7 3 4F A3WE 1996091200470 19960912 00470 NM 1996 9 12 UPS96221049 1 19960902 A 5311 FRAME BOEING 727 7272A1 138407F NM BS 1030 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-C, CORROSION AT BS 1030 ON THE AFT SIDE OF FRAME AND UNDER THE LEVELING COMPOUND RBL 5, WL 145. REMOVED LEVELING COMPOUND AND FOUND CORROSION UNDER SHEAR TIE. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED ANTENNA AND CUTOUT DAMAGE, FABED DOUBLER AND REPAIR PARTS. REINSTALLED ALL PARTS WITH FASTENERS, INSTALLED ANTENNA, SEALED, IAW SRM 51-30-2, 53-30-3, 53-30-1. 2 L 7 3 4F A3WE 1996091200471 19960912 00471 NM 1996 9 12 UPS96221050 1 19960907 A 5320 655784812 FITTING BOEING 727 7272A1 138407F NM BS 720 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-C, CORROSION ON CARGO TIE DOWN AT STA 720B RBL 23 WL 156. REPLACED CARGO TIE DOWN WITH NEW PART PER SRM 51-10-1, 51-20-4, 51-30-2, 51-30-5. 2 L 7 3 4F A3WE 1996091200472 19960912 00472 NM 1996 9 12 UPS96221051 1 19960907 A 5320 655784811 FITTING BOEING 727 7272A1 138407F NM BS 720 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-C, CORROSION ON CARGO TIE DOWN STA 720C LBL 23 WL 156. REPLACED CARGO TIE DOWN WITH NEW PART PER SRM 51 -30-2, 51-20-4. 2 L 7 3 4F A3WE 1996091200473 19960912 00473 NM 1996 9 12 UPS96221052 1 19960906 A 5320 655784817 FITTING BOEING 727 7272A1 138407F NM BS 560 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-C, CORROSION ON CARGO TIE DOWN STA 560 LBL 23 WL 156. CORROSION REWORK REVEALED TIE DOWN TO BE CRACKED. REPLACED TIE DOWN AT STA 560 LBL 23 IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996091200474 19960912 00474 NM 1996 9 12 UPS96221053 1 19960905 A 5320 655784812 FITTING BOEING 727 7272A1 138407F NM BS 500 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-C, CORROSION ON CARGO TIE DOWN AT STA 500 RBL 23 WL 156. CORROSION REWORK OUT OF LIMITS IAW SRM 53-10-1 . REPLACED TIE DOWN AT STA 500 RBL 23 IAW SRM 51-30-2, 51-30-5. 2 L 7 3 4F A3WE 1996091200475 19960912 00475 NM 1996 9 12 UPS96221054 1 19960905 A 5754 651727610 RIB BOEING 727 7272A1 138407F NM NR 5 LE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-C, NR 5 SLAT I/B RIB AT ACTUATOR MOUNT CRACKED AT SMALL TAB FLANGE. REPAIRED NR 5 SLAT I/B RIB AT ACTUA TOR MOUNT IAW SRM 57-50-3. 2 L 7 3 4F A3WE 1996091200476 19960912 00476 NM 1996 9 12 UPS96221055 1 19960905 A 3350 1000679 BATTERIES BOEING 727 72722C 138400F NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE N/A EMERGENCY LIGHT INOP. REPLACED BATTERIES. 2 L 7 3 4F A3WE 1996091200477 19960912 00477 NM 1996 9 12 UPS96221056 1 19960904 A 5320 SHEAR WEB BOEING 727 7272A1 138407F NM BS 1175 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-C, CORROSION FOUND ON SHEAR WEB AT BS 1175 LBL 32 WL 208. CORROSION REMOVAL FOUND WEB TO BE CRACKED, RE PAIRED IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1996091200478 19960912 00478 NM 1996 9 12 UPS96421042 1 19960907 A 5230 65B047316 HANDLE BOEING 747 747123 1384873 NM CARGO DOOR OUT OF POSITION A IPXA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 SO 01 672UP 20324 INSPECTION TYPE N/A, LOWER AFT CARGO DOOR WARNING LIGHT ILLUMINATED AT ROTATION. FOUND HANDLE IN THE UNLOCKED POSITION. INSPECTED AND OPERATED LOWER AFT CARGO DOOR HANDLE, NO DEFECTS NOTED. 2 L 7 4 4F A20WE 1996091200479 19960912 00479 NM 1996 9 12 UPS96421043 1 19960905 A 3350 S1356B37 LIGHT BOEING 747 747123 1384873 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST CR CRUISE 1 SO 01 676UP 20101 INSPECTION TYPE N/A, WALK WAY EXIT LIGHTS PRIOR TO CREW SERV DOOR CONTINUOUSLY FLASHED ON AND OFF. REMOVED AND REPLACED EMERGENCY UPPER DK CEILING LT ASSY, OP CK NORMAL PER MM 33-50-00 (P/N S1356B37) OFF, (S/N S1356B37) ON. 2 L 7 4 4F A20WE 1996091200480 19960912 00480 NM 1996 9 12 UPS96421045 1 19960909 A 3350 TERMINAL BOEING 747 747121 1384871 NM CREW DOOR LOOSE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE N/A, EMERGENCY EXIT DOOR SIGN INOP. TIGHTENED LOOSE TERMINAL, RESECURED EXIT SIGN OVER DOOR REF M114897 . 2 L 7 4 4F A20WE 1996091200481 19960912 00481 NM 1996 9 12 UPS96421058 1 19960904 A 3350 CONNECTOR BOEING 747 747123 1384873 NM FLIGHT CABIN LOOSE A IPXA K NONE L NO TEST CR CRUISE 1 SO 01 676UP 20101 INSPECTION TYPE N/A, EMERGENCY LIGHTS FLASH ON AND OFF CONTINUOUSLY. REMOVED EMERGENCY CEILING LIGHT, OPERATED AND CHEC KED FOR LOOSE CONNECTIONS. NONE FOUND, OPS CK NORMAL. NOTIFIED MMOC TO PUT AN ALERT ITEM ON THIS REPEAT PROBLEM. 2 L 7 4 4F A20WE 1996091200482 19960912 00482 WP 1996 9 12 UPS96821057 1 19960825 A 5347 74529523 TRACK DOUG DC8 DC873F 302199F WP BS 1342 CORROSION A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE CS2, NR 3 SEAT TRACK AT FS 1342 HAS MODERATE CORROSION. REPAIRED SEAT TRACK PER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1996091200483 19960912 00483 WP 1996 9 12 UPS96821059 1 19960828 A 5712 5770123 RIBS DOUG DC8 DC873F 302199F WP LT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE CS2, 4 RIBS CRACKED LT WING LEADING EDGE AT WS XFS780, XFS800, XFS740 AND XFS 710. REPAIRED RIBS PER MM 57-00-00 FIG 801. 2 L 7 4 4F RT 4A25 1996091200484 19960912 00484 WP 1996 9 12 UPS96821060 1 19960827 A 5712 5770123 RIBS DOUG DC8 DC873F 302199F WP LT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE CS2, 4 RIBS CRACKED AT LT WING LEADING EDGE WS XFS 623, XFS 633, XFS 648 AND XFS 653. REPAIRED RIBS PE R MM 57-00-00 FIG 801. 2 L 7 4 4F RT 4A25 1996091200485 19960912 00485 WP 1996 9 12 UPS96821061 1 19960824 A 5320 3779498 FITTING DOUG DC8 DC873F 302199F WP BS 857 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE CS2, FITTING CRACKED ON FWD SIDE OF FS 857 AT LONGERON 18R. REPLACED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996091200486 19960912 00486 WP 1996 9 12 UPS96821062 1 19960826 A 5712 5770123 RIBS DOUG DC8 DC873F 302199F WP RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE CS2, THREE RIBS CRACKED AT RT WING LEADING EDGE ST XFS 304, XFS 310 AND XFS 341. REPAIRED RIBS PER MM 5 7-00-00 FIG 801. 2 L 7 4 4F RT 4A25 1996091200487 19960912 00487 WP 1996 9 12 UPS96821063 1 19960825 A 5712 5770123 RIBS DOUG DC8 DC873F 302199F WP LT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE CS2, LT WING LEADING EDGE ASSY 1 EA RIBS CRACKED AT WS XFS 580, XFS 620, 4 EA RIBS CRACKED AT WS XFS 766 , 3 EA RIBS CRACKED AT WS XFS 800 AND 2 EA RIBS CRACKED AT WS XFS 820. REPAIRED RIBS PER MM 57-00-00 FIG 801. 2 L 7 4 4F RT 4A25 1996091200488 19960912 00488 NE 1996 9 12 WWMA9600069 2 19960906 A 7200 CT79B ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RIGHT FAILED A WWMA C D ABORTED TAKEOFF RETURN TO BLOCK Y ENGINE STOPPAGE TO TAKEOFF 1 WP 15 339SB 8609 4331 340B339 CREW REPORTED, DURING TAKEOFF ROLL AT 90 KNOTS THE RIGHT ENGINE FAILED. MAINTENANCE REPLACED THE RIGHT ENGINE. PRELIMI NARY FINDINGS INDICATE HOT SECTION MODULE FAILURE. 2 L 7 2 4T 4 T RT A52EU E8NE 1996091200489 19960912 00489 NM 1996 9 12 QXEA9600369 1 19960906 A 3350 10005511 LIGHT DHAV DHAV DHC8 DHC8102 2809003 NM COCKPIT INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 830PH 3936 314 COCKPIT PORTABLE EMERGENCY LIGHT IS INOP. LIGHT ASSY REPLACED AND LIGHT OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 1996091200490 19960912 00490 EU 1996 9 12 QXEA9600370 1 19960907 A 3350 5515800106 SIGN FOKKER FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 487US 11238 CENTER CABIN OVERHEAD EXIT SIGN INOP. SIGN REPLACED AND SIGN OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996091200491 19960912 00491 NM 1996 9 12 96FDEA01439 1 19960906 A 2121 5007024620 GASPER FAN BOEING 727 7272D4 138407U NM AIRCONDITION BAY FAILED A FDEA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SO 25 287FE 21849 GASPER FAN INOPERATIVE. CIRCUIT BREAKER POPPED OUT 3 TO 4 SECONDS AFTER TURNING GASPER FAN ON, BAD SMELL CAME OUT OF T HE GASPER SOCKETS. REMOVED AND REPLACED GASPER FAN PER B727 MAINTENANCE MANUAL 21-23-11, OPERATIONAL CHECK GOOD. 2 L 7 3 4F A3WE 1996091200492 19960912 00492 NM 1996 9 12 96FDEA01440 1 19960908 A 5311 6516309 FRAME BOEING 727 72725 1384006 NM BS 251.6 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 509FE 18280 NR 0507 AND 014, CORROSION (C53-221-01) ON FRAME AFT SIDE BS 251.6 RBL 50 WL 210 TO 225. *S/D* REPAIRED FRAME WEB AT B S 251.6 RBL 50 WL 210 TO 225 IAW FEDEX SRM 51-40-2. 2 L 7 3 4F A3WE 1996091200493 19960912 00493 NM 1996 9 12 96FDEA01441 1 19960908 A 5320 6519606 SHEAR WEB BOEING 727 72725 1384006 NM BS 1171-1175 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 509FE 19145 NR 0395 AND 015, CORROSION (C53-224-01, -2) ON SHEAR WEB AT BS 1171 TO 1175 RBL 4 RBL 15 AT NUTPLATE HOLES. *S/D* CORR OSION WAS FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED DAMAGED SHEAR WEB AS PER FED EX SRM 57-20-1. 2 L 7 3 4F A3WE 1996091200494 19960912 00494 NM 1996 9 12 96FDEA01448 1 19960909 A 5711 SPAR CHORD DOUG MD11 MD11 3023602 NM WS 782-827 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 603FE 48459 NR 6047. RIGHT WING TOP TE PANEL OUTBOARD OF NR 5 SPOILER BULGING AT AFT SPAR STA XORS 782 - 827. SUBJECT CORROSION HA S BEEN REMOVED, AREA TREATED AND PAINTED PER 51-21-01. 2 L 7 3 4F RT A22WE 1996091200495 19960912 00495 NM 1996 9 12 96FDEA01449 1 19960909 A 5230 651862222 INTERCOSTAL BOEING 727 72725 1384006 NM BS 1090 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR 0345 AND 010, AFT CARGO DOOR AFT HINGE INTERCOSTAL IS BENT AND CRACKED. *S/D* REMOVED AND REPLACED AFT CARGO DOOR A FT HINGE INTERCOSTAL. 2 L 7 3 4F A3WE 1996091200496 19960912 00496 WP 1996 9 12 ABXA9600622 1 19960905 A 2150 19838462CH CLAMP DOUG DC9 DC931 3022065 WP RT PACK LOOSE A ABXA O OTHER J WARNING INDICATION DE DESCENT 1 GL 23 942AX 47552 PRESSURIZATION FLOW LIGHT CAME ON AT FL 350 AND CABIN ALTITUDE ROSE TO 12,000 FT. CREW DONNED OXYGEN MASKS. SELECTED S TANDBY, FLOW LIGHT WENT OUT THEN CAME BACK ON. OUTFLOW VALVE FULLY CLOSED, FLOW LIGHT WENT OUT AT APPROXIMATELY 12,000 FT. SECURED LOOSE CLAMP ON THE RIGHT PACK DUCT OUTLET. 2 L 7 2 4F A6WE 1996091200497 19960912 00497 WP 1996 9 12 MWEA96432 1 19960905 A 2560 BATTERIES DOUG DC9 DC932 3022066 WP MEGAPHONE DISCHARGED A MWEA K NONE L NO TEST NR NOT REPORTED 1 GL 31 206ME 47791 CREW REPORTS CABIN MEGAPHONE INOP. MAINTENANCE REMOVED AND REPLACED BATTERIES OPS CHK GOOD. 2 L 7 2 4F A6WE 1996091200498 19960912 00498 WP 1996 9 12 MWEA96433 1 19960907 A 5210 3917853503 BEAM DOUG DC9 DC932 3022066 WP PAX DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 DURING C-CK, FOUND AFT ENTRANCE DOOR HAS CRACK AT LOWER LEFT BEAM END AND AT RADIUS OF UPPER BEAM NEAR HINGE POINT. MAI NT INSTALLED DOUBLER REPAIR ON UPPER BEAM IAW SRM 52-05 PG 201 FIG 34. REMOVED AND REPLACED LOWER BEAM IAW SRM 51-30. 2 L 7 2 4F A6WE 1996091200499 19960912 00499 WP 1996 9 12 MWEA96434 1 19960907 A 3350 60030451 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 502ME 48132 DURING C-CHECK, FOUND EMERGENCY OVERHEAD LIGHT IN AFT ACCESSORY COMPARTMENT VERY DIM. MAINTENANCE REMOVED AND REPLACED BATTERY POWER SUPPLY. OPS CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F A6WE 1996091200500 19960912 00500 NM 1996 9 12 DL757962010 1 19960829 A 2120 AIR DISTR BOEING 757 757232 1384965 NM CABIN SMOKE A DALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DE DESCENT 1 SO 27 611DL 22818 AT TOP OF DESCENT, SMOKE ALARMS IN F/C WENT OFF AND FLT ATTEN REPORTED A BURNING SMELL IN CABIN. SMELL LASTED ABOUT 15 SEC AND THEN SMOKE ALARMS STOPPED. FLT ATTEN REPORTED SEEING THIN WHITE SMOKE IN CABIN. F/A REPORT EYES AND THROAT VER Y IRRITATED. SMOKE DISSIPATED AFTER 10 MIN. OPERATED ALL GALLEY APPLIANCES, ELEC CHKED LAV TRASH O/HEAT DETECTORS AND TRASH EXTINGUISHERS, ALL OK. CHKED ALL LIGHTING BALLASTS FOR O/HEAT, RAN ENGS W/PACKS ON, NO SMOKE OR SMELL OF SMOKE. ELEC AND A/C SYS CHK NORMAL. 2 L 7 2 4F RT A2NM 1996091200501 19960912 00501 NM 1996 9 12 DL757962024 1 19960831 A 4900 GROUND STUD BOEING 757 757232 1384965 NM APU BATTERY DAMAGED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 27 680DA 19238 26956 AFT CBN FILLED WITH SMOKE UPON LANDING AFTER F/A TURNED ON OVHD LIGHTS. FOUND GROUND STUDS FOR APU START BAT TO SHOW HE AT DAMAGE. CLEANED AREA AND SECURED STUDS AND RECONNECTED WIRING. DEACT APU, ATL TO ROUTE A/C FOR EO 6-66173 APU GROUN D STUD WIRING MOD. 2 L 7 2 4F RT A2NM 1996091200502 19960912 00502 NE 1996 9 12 DL76L962040 2 19960904 A 7200 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 BIRD STRIKE A DALA A UNSCHED LANDING Y C ENGINE STOPPAGE F.O.D. CL CLIMB 1 SO 27 172DN 16047 24775 724638 NR 2 ENG SURGE SHORTLY AFTER ROTATION. ENGINE ROLLED BACK AND QUIT. FOUND BIRD REMNANTS IN ENGINE. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 1996091200503 19960912 00503 NM 1996 9 12 DL72S962041 1 19960904 A 5210 SKIN BOEING 727 727232 1384082 NM PAX DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 411DA 21223 A .375 INCH CRACK MAIN CABIN DOOR OUTER SKIN AT UPPER AFT CORNER BELOW GATE HINGE. INSTALLED DOUBLER PER M/M 52-11-01 F IG 804. 2 L 7 3 4F A3WE 1996091200504 19960912 00504 NM 1996 9 12 DL757962042 1 19960904 A 7120 MOUNT BOLTS BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 ENGINE SHEARED A DALA K NONE Z SIGNIFICANT FAILURE REPORT IN INSP/MAINT 1 SO 27 660DL 28597 24422 716392 FWD ENGINE MOUNT RT STRUT LINK FWD ATTACH FITTING HAD 4 OF 8 ATTACH BOLTS SHEARD. 2 L 7 2 4F 4 F RT A2NM E17NE 1996091200505 19960912 00505 NM 1996 9 12 DL72K962043 1 19960821 A 5311 FRAME BOEING 727 727232 1384082 NM BS 783.95 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 480DA 20860 A .5 CRACK FOUND IN THE LOWER BOLT HOLE ON THE LT EMERGENCY EXIT FRAME AT STA 783.95. THE CRACK WAS STOP DRILLED AND RE PAIRED IN ACCORDANCE WITH BAC S/B 727-53-0197, RV 2. 2 L 7 3 4F A3WE 1996091200506 19960912 00506 NM 1996 9 12 DL72S962044 1 19960828 A 5530 65174637 STRINGER BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 402DA 21146 THE VERTICAL STABILIZER STRINGER 9L WAS FOUND CRACKED AT FIN STA 157.2, DURING EXECUTION OF EO 4-59253-12AD. THIS EO CA LLS FOR A REPAIR PER B727 SRM 55-30-4, HOWEVER STR 9L CANNOT BE REPAIRED PER SRM PROCEDURE DUE TO SPACE LIMITATION ON IN BOARD FLANGE. STRINGER WILL BE REPAIRED IN ACCORDANCE WITH S/B 727-55 0075R2. 2 L 7 3 4F A3WE 1996091200507 19960912 00507 NM 1996 9 12 DL73E962045 1 19960807 A 5330 654576972 SKIN BOEING 737 737247 138448D NM BS 379 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 239WA 23187 SKIN AT THE COOLING DUCT CUTOUT BS 379 BL 2 WAS FOUND CRACKED AT THE AFT EDGE OF THE CUTOUT INTO A FASTENER HOLE. THE C RACK IS APPROXIMATELY .6 IN LENGTH AND IS TYPICAL OF CRACKS DESCRIBED IN BACO S/B 737-53-1117 R1 IN ACCORDANCE W ITH THE ABOVE S/B, THE SKIN WAS REPAIRED. 2 L 7 2 4F A16WE 1996091200508 19960912 00508 NM 1996 9 12 DL72S962047 1 19960825 A 5330 65545655 SKIN BOEING 727 727232 1384082 NM BS 505 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 477DA 20754 ER/A 222419-14 PROVIDED FOR A TEMPORARY AND PERMANENT REPAIR FOR DAMAGE TO THE UPPER SKIN PANEL OF THE LAP JOINT AT FS 5 05 AND STRINGER 26R. DURING THE PERMANENT REPAIR FOR THE ABOVE ER/A, A 0.5 CRACK WAS FOUND AT A LAP JOINT FASTENER AT FS 515. 2 L 7 3 4F A3WE 1996091200509 19960912 00509 NM 1996 9 12 DL72K962048 1 19960821 A 5312 BULKHEAD BEAM BOEING 727 727232 1384082 NM BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 480DA 20860 INSPECTING PER SI 4-58630-12, A 2 INCH CRACK WAS FOUND OUT OF A LIGHTENING HOLE IN VERTICAL BEAM AT LBL 26.83 ON AFT SID E OF BS 1183 BULKHEAD. THIS IS TYPICAL OF DAMAGE ADDRESSED BY BACO SB 727-53-0182. SI ALLOWS INSTALLATION OF REPAIR PE R EO 4-58630-3 ON ONE SIDE ONLY AT LIAISON ENGINEERING'S DISCRETION. 2 L 7 3 4F A3WE 1996091200510 19960912 00510 NM 1996 9 12 DL72E962049 1 19960823 A 5320 DOOR FRAME BOEING 727 727247 138408F NM BS 760.95 ELONGATED HOLES A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 283WA 21485 FOUR FASTENER HOLES FOUND ELONGATED ON THE STA 760.95 RT OVERWING EXIT FRAME. THESE HOLES WILL BE OVERSIZED PER B727 S/ B 53-01-97, REVISION 2. 2 L 7 3 4F A3WE 1996091200511 19960912 00511 NM 1996 9 12 DL73S962050 1 19960826 A 5311 FRAME BOEING 737 737232 1384475 NM BS 794.3 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 324DL 23096 THE C-2 DOOR CUTOUT FORWARD FRAME WAS FOUND WITH A 1 INCH CRACK AT THE NR 5 STOP FITTING. REPAIRED PER ERA 304090-14AD. 2 L 7 2 4F RT A16WE 1996091200512 19960912 00512 NM 1996 9 12 DL73S962051 1 19960830 A 5743 654948818 FITTING BOEING 737 737232 1384475 NM RT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 308DL 23080 RIGHT WING OUTBOARD AFT SUPPORT FITTING FOR THE MAIN LANDING GEAR BEAM WAS FOUD CRACKED. THE FITTING WAS INSPECTED PER BACO S/B 737-57-1216, BUT THIS DAMAGE IS NOT TYPICAL OF DAMAGE DESCRIBED IN THE SERVICE BULLETIN. THE CRACKED FITTING W ILL REMAIN IN SERVICE ON A TIME LIMITED BASIS AND WILL BE REPAIRED ACCORDING TO SERVICE BULLETIN REQUIREMENTS. 2 L 7 2 4F RT A16WE 1996091200513 19960912 00513 NM 1996 9 12 DL73E962052 1 19960830 A 5312 BULKHEAD BOEING 737 737247 138448D NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 238WA 23186 DURING ACCOMPLISHMENT OF SI 3-69482-12, TWO CRACKS FOUND ON THE FORWAD FACE OF THE FS 178 BULKHEAD WEB. THE FIRST CRACK IS LOCATED NEAR THE RBL 5.7 VERTICAL STRAP AT APPROX WL 198, THE SECOND IS LOCATED NEAR THE BL 0 VERTICAL STRAP AT AP PROXIMATELY WL 189. BOTH CUTOUTS MEASURE 1 INCH DIA. REPAIRED PER ERA 304107-14A. 2 L 7 2 4F A16WE 1996091200514 19960912 00514 NM 1996 9 12 DL72S962053 1 19960903 A 5320 DOOR FRAME BOEING 727 727232 1384082 NM BS 761 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 402DA 21146 A CRACK WAS FOUND IN THE FOURTH FASTENER HOLE LOCATED ABOVE THE CABIN FLOOR LINE ON THE LT STA 761 OVERWING EXIT FRAME. THE HOLE WAS OVERSIZED TO 0.340 AND A HIGH FREQUENCY EDDY CURRENT INSPECTION SHOWED THAT THE CRACK NO LONGER EXISTED IN THE FASTENER HOLE. REPAIRED PER ERA 304129-14AD. 2 L 7 3 4F A3WE 1996091200515 19960912 00515 NM 1996 9 12 DL73S962054 1 19960905 A 3350 BATTERY PACK BPS73 BOEING 737 737232 1384475 NM CABIN DISCHARGED A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 304DL 1113 23076 EMER EXIT LIGHTS ABOVE 1B AND 2C REMAINED ILLUM WITH SWITCH IN ARMED POSITION. REPLACED OVHD BATT PACK AND PWR SUPPLY C KS OK. 2 L 7 2 4F RT A16WE 1996091200516 19960912 00516 NM 1996 9 12 DL72S962057 1 19960905 A 3350 LIGHT 1000677 BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 490DA 15087 21020 EMERGENCY EXIT LIGHT ABOVE L-2 DOOR DID NOT COME ON DURING TEST. REPLACED LIGHT ASSY, OPS NORMAL. 2 L 7 3 4F A3WE 1996091200517 19960912 00517 NM 1996 9 12 DL72S962058 1 19960905 A 3350 BATTERIES 900835A BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 490DA 14499 21020 CENTER AISLE EMERGENCY EXIT LIGHT BETWEEN AFT LAVS DID NOT COME ON DURING TEST. REPLACED BATTERIES AND BULBS OPS NORMAL . 2 L 7 3 4F A3WE 1996091200518 19960912 00518 NM 1996 9 12 DLM88962060 1 19960906 A 3350 LIGHT 6011779 DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 904DE 722 53409 EXTERIOR EMERGENCY LIGHTS WOULD NOT TEST. REPLACED AFT RACK ASSY. 2 L 7 2 4F RT A6WE 1996091200519 19960912 00519 WP 1996 9 12 DLL10962061 1 19960903 A 5330 SKIN LKHEED 1011 10113851 5265010 WP FS 1551 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1732D 193C1213 THE BONDED FUSELAGE SKIN ASSEMBLY AROUND THE C2 CARGO DOOR WAS FOUND CORRODED NEAR STA 1551 AND STR 29. THE CORROSION W AS REMOVED WITH A CUTOUT IN THE OUTER SKIN, BONDED DOUBLER AND DOOR DOUBLER. THE CUTOUT WILL BE REPAIRED USING STANDARD SRM REPAIR TECHNIQUES. 2 L 7 3 4F A23WE 1996091200520 19960912 00520 WP 1996 9 12 DLL10962062 1 19960830 A 5712 RIB LKHEED 1011 10113851 5265010 WP WS 503 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 714DA 193C1090 A CRACK WAS FOUND ON THE LEFT HAND WING IWS 503 UPPER RIB CAP CASTELLATION. ER/A 271804-14AD WAS WRITTEN TO ACCOMPLISH RIB REPLACEMENT AT NEXT AIRCRAFT HMV. REV A OF THIS ER/A DEFERS THIS REPLACEMENT TO THE NEXT AIRCRAFT HMV. 2 L 7 3 4F A23WE 1996091200521 19960912 00521 NM 1996 9 12 DL76L962064 1 19960830 A 5414 311T3450 SKIN BOEING 767 767332 1382001 NM NR 2 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 177DN 25122 TWO CRACKS WERE REPORTED IN THE NR 2 ENGINE PYLON OUTBOARD STRUT SKIN AT THE FWD TORQUE BOX ACCESS HOLE. A .5 INCH CRAC K WAS FOUND IN THE UPPER FORWARD CORNER AT APPROX NS 158. THE SECOND CRACK IS ALSO .5 INCH LONG AND IS IN THE UPPER AFT CORNER AT NS 192. REPAIRED PER DAL ER/A 360197. 2 L 7 2 4F RT A1NM 1996091200522 19960912 00522 NM 1996 9 12 DL72S962067 1 19960906 A 3350 BATTERY PACK 900542 BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 400DA 1150 21144 LEFT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY AND PACK, LTS CKS NORMAL. 2 L 7 3 4F A3WE 1996091200523 19960912 00523 NM 1996 9 12 DL72S962068 1 19960906 A 3350 BATTERY PACK 900542 BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 400DA WA1885 21144 AFT LEFT OVERWING LIGHT INOP. REPLACED BATTERY AND RACK, LT CKS NORMAL. 2 L 7 3 4F A3WE 1996091200524 19960912 00524 NM 1996 9 12 DL72K962069 1 19960513 A 5241 65561502 DOUBLER BOEING 727 727232 1384082 NM GALLEY DOOR DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 413DA 21233 INSTALLED REPAIR DOUBLER PER SRM 52-00-3 SKIN WAS DAMAGED AT THE UPPER FWD CORNER. 2 L 7 3 4F A3WE 1996091200525 19960912 00525 NM 1996 9 12 DL76L962070 1 19960807 A 3350 333780100 POWER SUPPLY BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 182DN 25987 FOUND ON SERVICE CHECK, LEFT AFT EMERGENCY SLIDE LIGHT INOP. REPLACED PWR SUPPLY M738, EMERGENCY LIGHTS TEST OK PER MM. 2 L 7 2 4F RT A1NM 1996091200526 19960912 00526 NE 1996 9 12 DLM88962072 2 19960908 A 7200 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 FLAMED OUT A A DALA A UNSCHED LANDING X M ENGINE FLAMEOUT OVER TEMP CR CRUISE 1 SO 27 953DL 49884 726838 IN FLIGHT THE NR TWO ENGINE FLAMED OUT. THE ENGINE OVER TEMPED ON RESTART 720 C FOR 10 SEC. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A6WE E9NE 1996091200527 19960912 00527 NM 1996 9 12 DL767962074 1 19960907 A 5270 SWITCH 834802 BOEING 767 767232 1385132 NM R2 DOOR MALFUNCTIONED A DALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 27 101DA 84401 22213 ALL EXTERIOR EMERGENCY LIGHTS REPORTED ON. RETURNED TO GATE. ASSOCIATED WITH RT AFT ENT DOOR LIGHT CYCLING ON AND OFF. REPLACED PROX SWITCH AT RT AFT DOOR, SYSTEM OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 1996091200528 19960912 00528 NM 1996 9 12 SCNA96244 1 19960903 A 3350 BULB BOEING 727 727227 1384078 NM CABIN FAILED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 275AF 22092 THE AFT EXTERIOR OVERWING EMERGENCY LIGHT WAS FOUND INOP. REMOVED AND REPLACED THE AFT LAMP, AND OPS CHECKED NORMAL. 2 L 7 3 4F A3WE 1996091200541 19960912 00541 CE 1996 9 12 96ZZZX4384 1 19960813 A 5330 SKIN BEECH MU300 400BEECH CE LOWER FWD FUSE CHAFED A BQVA K NONE O OTHER IN INSP/MAINT 1 EA 01 3127R 1494 RF27 LOWER FUSELAGE SKIN WAS FOUND CHAFED FROM CONTACT WITH THE AFT NOSE LANDING GEAR DOOR. CHAFING OCCURRED WITH THE LANDIN G GEAR EXTENDED AND AIRLOADS INDUCED. FUSELAGE SKIN AREA CHAFED WAS FORWARD OF PRESSURE BULKHEAD (NON-PRESSURIZED AREA) . DOOR, P/N 45A31615-11. 2 H 7 2 4F RT A16SW 1996091200552 19960912 00552 CE 1996 9 12 96ZZZX4395 1 19960625 A 3230 98820201 ACTUATOR CESSNA 210 P210N 2073454 CE NLG DOWNLOCK PINS BROKEN A A HMGA O OTHER P NO WARNING INDICATION AP APPROACH 1 SW 15 4811K 2343 P21000330 UPON SELECTING GEAR DOWN FOR LANDING, THE PILOT COULD NOT GET A NOSE DOWN AND LOCK INDICATION. AIRCRAFT WAS LANDED AND NOSE WHEEL COLLAPSED. INVESTIGATION REVEALED THE NOSE GEAR ACTUATOR DOWNLOCK PINS WERE BROKEN WHICH ALLOWED ONE OR BOTH PINS TO VIBRATE INBOARD WHICH PREVENTED ACTUATOR SHAFT FROM RETRACTING COMPLETELY, THEREFORE, NOT ALLOWING DOWNLOCK MEC HANISM TO LATCH OVER PINS. IT APPEARS PINS HAD BEEN BROKEN FOR SOME TIME AND HAD FAILED AT THE MACHINED GROOVE WHICH WA S CUT FOR ROLL PIN PROTRUSION. CESSNA SEB 9520 DATED 12-29-95 COVERS THIS SUBJECT. SUBMITTER RECOMMENDS THE INITIAL IN SPECTION SHOULD BE REVISED TO 'BEFORE FURTHER FLIGHT'. 1 H 7 1 3O 3A21 1996091200577 19960912 00577 SO 1996 9 12 96ZZZX4420 1 19960806 A 3211 7871702 STUD PIPER PA34 PA34200T 7103406 SO MLG SIDE BRACE CRACKED A IPMA K NONE O OTHER IN INSP/MAINT 1 WP 11 2788M 1021 347870094 DURING LEVEL 1 INSPECTION PER AD 95-20-07, FOUND SIDE BRACE STUD CRACKED IN RADIUS. THIS AD DOES NOT APPLY TO THIS AIRC RAFT BY SERIAL NUMBER. RECOMMEND INSPECTION CONTINUE AS THIS PART WAS INSTALLED 5-95 AND FOUND DEFECTIVE 8-96, 1,000 HO URS TT. 1 L 7 2 3O A7SO 1996091200581 19960912 00581 WP 1996 9 12 96ZZZX4424 1 19960803 A 7810 BOLT DOUG DC3 DC3CS1C3G 3021458 WP EXH MOUNT FAILED A CSAA O OTHER A FLAME/FIRE NR NOT REPORTED 1 AL 01 19454 25309 ONE EACH EXHAUST MOUNT BOLT CAME OUT CAUSING EXHAUST TO SLIP OUT OF CLAMP LEAKING HOT EXHAUST GAS ONTO COWL FLAP HYDRAUL IC LINE. THE LINE FAILED IGNITING HYDRAULIC FLUID, THE FIRE WARNING SYSTEM OPERATED AS IT WAS SUPPOSED TO. THE COWL FL AP SELECTOR WAS SELECTED TO OFF AND THE FIRE EXTINGUISHED. MINOR COWL FLAP AND RING COWL DAMAGE OCCURRED DUE TO HEAT AL L OF WHICH HAS BEEN REPAIRED. 2 L 7 2 4R A669 1996091200628 19960912 00628 CE 1996 9 12 PNSA960901 1 19960909 A 3240 91136 BRAKE CYLINDER CESSNA 441 441 2076020 CE RT MLG BROKEN A PNSA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 AL 03 544AL 5350 4410120 LOSS OF RT BRAKE FLUID. CYLINDER BROKE AT TORQUE PLATE PIN. 1 L 7 2 3T RT A28CE 1996091200629 19960912 00629 SO 1996 9 12 RAAA96E4013 1 19960909 A 3231 8048475 YOKE ASSY LKHEED 188 188C 5262604 SO LT MLG BROKEN A RAAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 9744C 1960 188C1140 AFTER TAKEOFF, LEFT GEAR RED LIGHT FAILED TO GO OUT. VISUAL CHECK CONFIRMED GEAR WAS UP. WHEN HANDLE PUT TO NEUTRAL, L EFT GEAR EXTENDED ON ITS OWN. CONFIRMED VISUALLY AND GREEN LIGHT WAS ON. RECYCLING FAILED TO CORRECT PROBLEM. RETURNE D TO ANC. REPLACED LEFT YOKE ASSY MLG DOOR MECHANISM DUE RETRACT CYLINDER LUGS BROKEN OFF. 2 L 7 4 4T 4A22 1996091200630 19960912 00630 NM 1996 9 12 RAAA96B2034 1 19960910 A 3350 86210144 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 LEFT FORWARD OVERWING EMERGENCY EXIT EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. 2 L 7 3 4F A3WE 1996091200631 19960912 00631 NM 1996 9 12 RAAA96B2035 1 19960910 A 3350 86210144 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 RIGHT FORWARD OVERWING EMERGENCY EXIT EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. 2 L 7 3 4F A3WE 1996091200632 19960912 00632 NM 1996 9 12 RAAA96B2036 1 19960910 A 3350 86210144 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 RIGHT SERVICE DOOR EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. 2 L 7 3 4F A3WE 1996091200633 19960912 00633 NE 1996 9 12 CALA9601276 2 19960909 A 7250 775404 T4 BLADE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 2 ENGINE FAILED A CALA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SW 09 33817 49371 708485 TAKEOFF WAS ABORTED AT APPROXIMATELY 50 KNOTS AFTER THE NR 2 ENGINE LOST POWER. THE POWER LOSS WAS ACCOMPANIED BY A LOU D POP. THE AIRCRAFT WAS RETURNED TO THE GATE. MAINTENANCE FOUND THE NR 2 ENGINE TURBINE HAD FAILED. THE NR 2 ENGINE W AS REMOVED AND REPLACED. *S/D* SHOP FINDINGS REVEALED A T-4 BLADE FAILURE. 2 L 7 2 4F 4 F A6WE E9NE 1996091200634 19960912 00634 WP 1996 9 12 CALA9601277 1 19960909 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 83873 49121 INSPECTION FOUND EMERGENCY AISLE PATH LIGHTING INOPERATIVE AT ROWS 1-6. MAINTENANCE FOUND WIRING IN NEED OF REPAIR. TH E WIRING WAS REPAIRED. THE FORWARD CHARGER AND BATTERY PACK WERE ALSO REPLACED. OPERATION OF THE LIGHTS CHECKED GOOD. 2 L 7 2 4F A6WE 1996091200635 19960912 00635 WP 1996 9 12 CALA9601278 1 19960816 A 5210 INTERCOSTAL DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14840 49580 INSPECTION FOUND A 1 INCH CRACK IN MAIN CABIN DOOR INTERCOSTAL AFT OF HANDLE TORQUE SHAFT. THE INTERCOSTAL WAS REMOVED A ND REPLACED IAW SRM 51-30-3. 2 L 7 2 4F A6WE 1996091200636 19960912 00636 WP 1996 9 12 CALA9601279 1 19960819 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 946 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14840 49580 INSPECTION FOUND A .25 INCH CRACK IN KEEL STRUCTURE VERTICAL ANGLE AT STA 946, SIX INCHES LEFT OF AIRCRAFT CENTERLINE. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1996091200637 19960912 00637 WP 1996 9 12 CALA9601280 1 19960819 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP BS 946 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14840 49580 INSPECTION FOUND A .75 INCH CRACK IN KEEL STRUCTURE HORIZONTAL INTERCOSTAL AT STA 946, SIX INCHES RIGHT OF AIRCRAFT CENT ERLINE. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 1996091200638 19960912 00638 WP 1996 9 12 CALA9601281 1 19960819 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP BS 946 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14840 49580 INSPECTION FOUND A .50 INCH CRACK IN KEEL STRUCTURE VERTICAL INTERCOSTAL AT STA 946, SIX INCHES RIGHT OF AIRCRAFT CENTER LINE. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 1996091200639 19960912 00639 WP 1996 9 12 CALA9601282 1 19960819 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP BS 946 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14840 49580 INSPECTION FOUND A .25 INCH CRACK IN KEEL STRUCTURE VERTICAL INTERCOSTAL AT STA 946, SIX INCHES LEFT OF AIRCRAFT CENTERL INE. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 1996091200640 19960912 00640 WP 1996 9 12 CALA9601283 1 19960823 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 265 DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14840 49580 INSPECTION FOUND IMPACT DAMAGE TO LEFT FUSELAGE SKIN AT STA 265, LONGERON 15L. THE SKIN WAS REMOVED AND REPLACED IAW EC RA 5330-02431. 2 L 7 2 4F A6WE 1996091200641 19960912 00641 WP 1996 9 12 CALA9601284 1 19960820 A 5320 SUBFLOOR DOUG DC9 DC982 3022082 WP BS 1136-1174 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14840 49580 INSPECTION FOUND CORROSION ON SUBFLOOR AT STA 1136-1174. THE CORRODED SECTION OF SUBFLOOR WAS REMOVED AND REPLACED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1996091200642 19960912 00642 WP 1996 9 12 CALA9601285 1 19960818 A 5230 DOOR PAN DOUG DC9 DC982 3022082 WP MAIN BAG BIN CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14840 49580 INSPECTION FOUND A 1 INCH CRACK AT FORWARD LATCH AREA OF MAIN BAGGAGE BIN DOOR PAN. THE CRACK WAS STOP DRILLED AND A DO UBLER WAS INSTALLED IAW SRM 52-05. 2 L 7 2 4F A6WE 1996091200643 19960912 00643 WP 1996 9 12 CALA9601286 1 19960818 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 148-200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14840 49580 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 148-200, LEFT OF CENTERLINE. A NEW FLOOR SUPPORT WAS FABRICATED AND INST ALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1996091200644 19960912 00644 WP 1996 9 12 CALA9601287 1 19960903 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 340-400 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14840 49580 THE FUSELAGE SKIN WAS DENTED AT STA 340-400 BETWEEN LONGERON 22R AND CUSP. A REPAIR WAS INSTALLED IAW ECRA 5330-02433. 2 L 7 2 4F A6WE 1996091200645 19960912 00645 WP 1996 9 12 9619429970 1 19960909 A 7930 1163P0041 DIFFERENTAL SW DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9 52048 NE RT ENGINE FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 9334 4166 4166 47247 654032 WHILE APPLYING POWER FOR TAKEOFF, THE RIGHT ENGINE OIL STRAINER CLOGGING LIGHT ILLUMINATED. CREW ABORTED TAKEOFF AND RE TURNED TO THE GATE. MAINTENANCE REPLACED THE RIGHT ENGINE OIL FILTER AND OIL FILTER DIFFERENTIAL SWITCH. LEAK AND OPER ATIONAL CHECK OK. 2 L 7 2 4F 4 F A6WE E2EA 1996091200646 19960912 00646 WP 1996 9 12 9619439860 1 19960908 A 3350 LIGHT DOUG DC9 DC951 3022051 WP TAILCONE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 769NC 47757 DURING LINE CHECK, FOUND EMERGENCY LIGHTS ABOVE TAILCONE SLIDE INOPERATIVE. FOUND SOCKET LOOSE. RESECURED SOCKET AND I NSTALLED NEW BULBS. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996091200647 19960912 00647 WP 1996 9 12 9619449872 1 19960907 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 781NC 48121 DURING LINE CHECK, FOUND LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996091200648 19960912 00648 WP 1996 9 12 9619459105 1 19960906 A 3350 BATTERIES DOUG DC9 DC915 3022036 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 95S 47205 DURING LINE CHECK, FOUND AFT CABIN OVERHEAD EMERGENCY LIGHTS DIM. REPLACED BATTERIES. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996091200649 19960912 00649 WP 1996 9 12 9619469105 1 19960906 A 3350 POWER SUPPLY DOUG DC9 DC915 3022036 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 95S 47205 DURING LINE CHECK, FOUND THE LEFT AND RIGHT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED LEFT AND RIGHT POWER SUPP LIES. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996091200650 19960912 00650 NE 1996 9 12 COMA9610275 2 19960906 A 7200 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE RIGHT FAILED A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 258CA 5307 120247 115374 THE RIGHT ENGINE HAS HIGH NH SPEED AND LOW TORQUE. REPLACED THE RIGHT ENGINE. 2 L 7 2 4T 4 T RT A31SO E20NE 1996091200651 19960912 00651 SO 1996 9 12 COMA9610276 1 19960909 A 5246 12016900008 DOOR EMB 120 EMB120RT SO RT WING NOT CLOSED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 196CA 120196 SERVICE DOOR WARNING LIGHT ILLUMINATED DURING TAKEOFF. SECURED SINGLE POINT FUEL SERVICE DOOR. 2 L 7 2 4T RT A31SO 1996091200652 19960912 00652 NM 1996 9 12 96FDEA01455 1 19960909 A 5312 651633841 BULKHEAD WEB BOEING 727 72725 1384006 NM BS 950 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR 0506 AND 016, CRACKS IN BS 950 BULKHEAD LBL 4.5 AND RBL 4 WL 175. *S/D* REPAIRED CRACKS IN BS 950 BULKHEAD LBL 4.5 AND RBL 4, WL 175 PER FEDEX SRM 53-10-9, PERFORMED FUNCTIONAL TEST PER REDEX MM 36-00 TESTED GOOD. 2 L 7 3 4F A3WE 1996091200653 19960912 00653 NM 1996 9 12 96FDEA01447 1 19960909 A 5711 SPAR CHORD DOUG MD11 MD11 3023602 NM WS 670-830 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 603FE 48459 NR 5050 AND 505. LEFT WING REAR SPAR UPPER CHORD ANGLE AFT TANG BETWEEN STA XORS 670 TO 830 HAS NUMEROUS AREAS OF EXFOL IATION CORROSION. REMOVED CORROSION PER SRM 51-21-01. 2 L 7 3 4F RT A22WE 1996091200654 19960912 00654 WP 1996 9 12 ABXA9600619 1 19960905 A 3231 TQ TUBE BOLT DOUG DC8 DC863 302198A WP LT MLG DOOR LOOSE A ABXA O OTHER J WARNING INDICATION CR CRUISE 1 GL 23 814AX 46041 LEFT GEAR DOOR NOT LATCHED IN-FLIGHT AND RED GEAR UNSAFE LIGHT ON. RECYCLED GEAR TWICE. LIGHT FOR LEFT GEAR DOOR WENT OUT THEN BACK ON. PUT GEAR DOWN. FOUND THROUGH-BOLT AT TORQUE TUBE DRUM LOOSE. PERFORMED TEST I/A/W DC-8 M.A.B. 32-6, DATED 03-22-91. LATCH TEST WAS GOOD, RE-ASSEMBLED CABLE AND TESTED. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1996091200655 19960912 00655 NM 1996 9 12 DHL9671530D 1 19960708 A 5311 FRAME BOEING 727 727155C 138404Z NM BS 560 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, FUSELAGE FRAME AT BS 560, STR 6R TO 7 RT DENTED. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-10- 4, 12.5 INCH BY 2.5 INCH BY 1 INCH. 2 L 7 3 4F A3WE 1996091200656 19960912 00656 NM 1996 9 12 DHL9671531D 1 19960708 A 5311 FRAME BOEING 727 727155C 138404Z NM BS 540 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, FUSELAGE INTERIOR FRAME HAS DENT ON INNER FLANGE AT BS 540, STR 8 RT. CUT OUT DAMAGED AREA AND INSTALLED DO UBLER REPAIR PER SRM 53-10-4. REPAIR 10.75 INCHESBY 2 INCHES BY 1 INCH. 2 L 7 3 4F A3WE 1996091200657 19960912 00657 NM 1996 9 12 DHL9671532D 1 19960708 A 5311 FRAME BOEING 727 727155C 138404Z NM BS 540 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, FUSELAGE INTERIOR FRAME HAS TWO DENTS ON INNER FRAME AT BS 540, STR 6R AND BELOW. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR, PER SRM 53-10-4, 14.5 INCHES BY 2 INCHES BY 1 INCH. 2 L 7 3 4F A3WE 1996091200658 19960912 00658 NM 1996 9 12 DHL9671533D 1 19960708 A 5330 SKIN BOEING 727 727155C 138404Z NM BS 227-235 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, FUSLAGE SKIN CRACKED BETWEEN STA 227 AND STA 235 AT STR 17L. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER RE PAIR PER SRM 53-30-3, 8 INCHES BY 6 INCHES . 2 L 7 3 4F A3WE 1996091200659 19960912 00659 NM 1996 9 12 DHL9671534D 1 19960708 A 5330 SKIN BOEING 727 727155C 138404Z NM BS 211.8-219.8 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, FOUND SKIN CRACKED BETWEEN STA 211.8 AND STA 219.8 AT STR 15L. CUT OUT DAMAGED AREA. INSTALLED DOUBLER, P ER SRM 53-30-3, 10 INCHES BY 12 INCHES. 2 L 7 3 4F A3WE 1996091200660 19960912 00660 NM 1996 9 12 DHL9671535D 1 19960717 A 5754 RIB BOEING 727 727155C 138404Z NM NR 2 LE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, NR 2 SLAT, SECOND RIB FROM THE OUTBOARD END, FOUND CRACKED . CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REP AIR, PER SRM 57-30-3, 5 INCHES BY 3 INCHES. 2 L 7 3 4F A3WE 1996091200661 19960912 00661 NM 1996 9 12 DHL9671536D 1 19960713 A 5753 652463411 RIB BOEING 727 727155C 138404Z NM TE MID FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, LEFT OUTBOARD MID-FLAP RIB FLANGE CRACKED AT OUTBOARD FORE FLAP TRACK. REMOVED AND REPLACED RIB PER SRM 51- 10-1. 2 L 7 3 4F A3WE 1996091200662 19960912 00662 NM 1996 9 12 DHL9671537D 1 19960713 A 5753 652466617 RIB BOEING 727 727155C 138404Z NM LT TE MID FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, LEFT INBOARD MID-FLAP RIB FLANGE CRACKED AT FORE FLAP TRACK, OUTBOARD SIDE. REPLACED RIB PER SRM 51-10-1 . 2 L 7 3 4F A3WE 1996091200663 19960912 00663 NM 1996 9 12 DHL9671538D 1 19960811 A 5751 SKIN BOEING 727 727155C 138404Z NM RT AILERON DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, OUTBOARD AILERON EXTERIOR LOWER SKIN DAMAGED ON RIGHT WING. CUT OUT DAMAGED AREA, INSTALLED FLUSH REPAIR PE R SRM 57-50-5, PLUG, 2.75 INCHES BY 1.5 INCHES, FILLER, 4 INCHES BY 5 INCHES. NO RE-BALANCE REQUIRED PER SRM 51-80-4. 2 L 7 3 4F A3WE 1996091200664 19960912 00664 NM 1996 9 12 DHL9671539D 1 19960708 A 5311 FRAME BOEING 727 727155C 138404Z NM BS 580 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, FUSELAGE FRAME HAS DENTS AT STA 580 BETWEEN STR 6R AND STR 7R. INSTALLED FRAME DOUBLER REPAIR, PER SRM 53 -10-4, 13 INCHES BY 2 INCHES BY 1 INCH . 2 L 7 3 4F A3WE 1996091200665 19960912 00665 NM 1996 9 12 DHL9671540D 1 19960717 A 5522 SKIN BOEING 727 727155C 138404Z NM RT ELEVATOR DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, RIGHT ELEVATOR L/E SKIN TOP SIDE AT FORWARD SPAR HAS DENTS AT STA 147. CUT OUT DAMAGED AREA, INSTALLED REPA IR DOUBLER, PER SRM 55-20-3, 3 INCHES BY 12 INCHES. RE-BALANCED BY CALCULATION PER SRM 51-80-7. 2 L 7 3 4F A3WE 1996091200666 19960912 00666 NM 1996 9 12 DHL9671541D 1 19960730 A 5320 WINDOW FRAME BOEING 727 727155C 138404Z NM NR 7 WINDOW CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, CABIN WINDOW FRAME NR 7 HAS CORROSION AROUND FRAME LIP. INSTALLED DOUBLER REPAIR, PER SRM 56-20-3, 18 INCH ES BY 16 INCHES, INSTALL WINDOW PER M/M. 2 L 7 3 4F A3WE 1996091200667 19960912 00667 NM 1996 9 12 DHL9671542D 1 19960805 A 5320 DOOR JAMB BOEING 727 727155C 138404Z NM BS 626 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, CABIN INTERIOR MCD CUTOUT AFT JAMB WEB DAMAGED BS 626 BETWEEN STR 3L AND STR 7L. FABRICATED NEW JAMB WEB, P ER SRM 51-10-1, 33 INCHES BY 5 INCHES BY 1 INCH. 2 L 7 3 4F A3WE 1996091200668 19960912 00668 NM 1996 9 12 DHL9671543D 1 19960805 A 5320 DOOR JAMB BOEING 727 727155C 138404Z NM BS 480 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, CABIN INTERIOR MCD CUTOUT FWD JAMB WEB DAMAGED FS 480 BETWEEN STR 3L AND 7L. REMOVED WEB AND FABRICATED WEB PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996091200669 19960912 00669 NM 1996 9 12 DHL9671544D 1 19960711 A 5347 BACN15201430 SEAT TRACK BOEING 727 727155C 138404Z NM BS 761-784 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, CABIN FLOOR SEAT TRACK HAS CORROSION UPPER SURFACE BETWEEN STA 761-784 BELOW RIGHT FWD OVERWING EXIT. REMOV ED AND REPLACED SEAT TRACK PER SRM 51-30-2 . 2 L 7 3 4F A3WE 1996091200670 19960912 00670 NM 1996 9 12 DHL9671545D 1 19960711 A 5315 FLOOR BEAM BOEING 727 727155C 138404Z NM BS 825 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, FOUND FLOOR BEAM CRACKED AT WEB BS 825, RBL 47. STOP DRILLED CRACK, PERFORMED HFEC, FABRICATED AND INSTALLE D WEB REPAIR, PER SRM 51-30-2, 5 INCHES BY 4.5 INCHES. 2 L 7 3 4F A3WE 1996091200671 19960912 00671 NM 1996 9 12 DHL9671546D 1 19960714 A 5330 SKIN BOEING 727 727155C 138404Z NM BS 530 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, REPAIR AT STA 530 STR 16 AND STR 17R. REPAIRED DOUBLER, PER SRM 53-30-3, 8 INCHES BY 12 INCHES. 2 L 7 3 4F A3WE 1996091200672 19960912 00672 NM 1996 9 12 DHL9671547D 1 19960714 A 5330 SKIN BOEING 727 727155C 138404Z NM BS 500 REQ'D REPAIR A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, FOUND NON-CONFORMING PREVIOIUS REPAIR AT FS 500 BETWEEN STR 15-16R. REINSTALLED REPAIR PER SRM 53-30-3. F ILLER, 3 INCHES BY 2 INCHES, DOUBLER, 8 INCHES BY 12 INCHES. 2 L 7 3 4F A3WE 1996091200673 19960912 00673 NM 1996 9 12 DHL9671548D 1 19960713 A 5320 WEB BOEING 727 727155C 138404Z NM BS 1176.9 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, REINFORCEMENT WEB AT STA 1176.9 HAS A CRACK BETWEEN RBL 17 AND RBL 26. REMOVED AND REPLACED WEB PER SRM 51- 10-4. 2 L 7 3 4F A3WE 1996091200674 19960912 00674 NM 1996 9 12 DHL9671549D 1 19960713 A 5320 60357 SUPPORT BOEING 727 727155C 138404Z NM BS 1135 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, FOUND FLOOR BOARD SUPPORT BEAM HAS CORROSION AT STA 1135 BETWEEN LBL 50 AND LBL 60. REMOVED AND REPLACED NE W SUPPORT CHANNEL PER SRM 51-10-1 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996091200675 19960912 00675 NM 1996 9 12 DHL9671550D 1 19960711 A 5330 SKIN BOEING 727 727155C 138404Z NM BS 1108 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, AFT SKIN AT LOWER DOOR JAMB IS CRACKED IN TWO PLACES AT AFT CORNER AND 17 INCHES FORWARD OF AFT CORNER. CUT OUT CRACKED AREA AT STA 1108 AND INSTALLED REPAIR PER SRM 53-30-3, 33.75 INCHES BY 3.5 INCHES. 2 L 7 3 4F A3WE 1996091200676 19960912 00676 NM 1996 9 12 DHL9671551D 1 19960709 A 5330 SKIN BOEING 727 727155C 138404Z NM BS 259-277 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, LAP SEAM 24L HAS 4 CRACK INDICATIONS BY HFEC BETWEEN BS 259 AND BS 277. CUT OUT DAMAGED TOP SKIN AND INSTAL LED DOUBLER REPAIR PER SRM 53-30-3, 12 INCHES BY 7 INCHES . 2 L 7 3 4F A3WE 1996091200677 19960912 00677 NM 1996 9 12 DHL9671552D 1 19960709 A 5330 SKIN BOEING 727 727155C 138404Z NM BS 259-277 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, LAP SEAM 14L HAS 3 CRACK INDICATIONS, BY HFEC BETWEEN BS 259 AND BS 277. CUT OUT CRACKED AREA AND INSTALLED DOUBLER REPAIR, 22 INCHES BY 8 INCHES, AND TAPERED FILLER, 4 INCHES BY 3 INCHES PER SRM 53-30-3. 2 L 7 3 4F A3WE 1996091200678 19960912 00678 NM 1996 9 12 DHL9671553D 1 19960708 A 5320 WEB BOEING 727 727155C 138404Z NM BS 1263 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, ONE CRACK IN LOWER RIGHT TORQUE TUBE BOX VERTICAL WEB AT FS 1263 BELOW AIRSTAIRS ACTUATOR. STOP DRILLED, IN STALLED DOUBLER REPAIR PER SRM 51-40-2 AND SRM 51-30-2, 6 INCHES BY 9 INCHES. 2 L 7 3 4F A3WE 1996091200679 19960912 00679 NM 1996 9 12 DHL9671554D 1 19960708 A 5311 FRAME BOEING 727 727155C 138404Z NM BS 600 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, FOUND FUSELAGE INTERIOR FRAME CRACKED AT BS 600, INNER FLANGE ABOVE FLOOR LEVEL. CUT OUT DAMAGED AREA, INST ALLED REPAIR PER SRM 53-10-4. REPAIR, 8 INCHES BY 10.5 INCHES. 2 L 7 3 4F A3WE 1996091200680 19960912 00680 NM 1996 9 12 DHL9671555D 1 19960707 A 5320 ANGLE BOEING 727 727155C 138404Z NM LT MLG WW CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, FOUND LEFT W/W PRESSURE DECK SUPPORT ANGLE CRACKED AT OUTBOARD AFT CORNER. CUT OUT CRACKED AREA AND INSTALL ED ANGLE REPAIR PER SRM 51-40-4, 8 INCHES BY 2 INCHES. 2 L 7 3 4F A3WE 1996091200681 19960912 00681 NM 1996 9 12 DHL9671556D 1 19960712 A 3230 6596621 FITTING BOEING 727 727155C 138404Z NM RT MLG CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, FOUND RIGHT MAIN LANDING GEAR UPLOCK SUPPORT FITTING HAS DEEP CORROSION PITTING INSIDE BOLT HOLE AND HFEC SHOWS CRACK INDICATION. REPLACED SUPPORT FITTING PER S/B 53-103. 2 L 7 3 4F A3WE 1996091200682 19960912 00682 NM 1996 9 12 DHL9671557D 1 19960728 A 5343 659611710 FITTING BOEING 727 727155C 138404Z NM NLG CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, FOUND NOSE GEAR DRAG BRACE SUPPORT FITTING CORRODED ON LEFT SIDE. REMOVED AND REPLACED NOSE GEAR DRAG BRAC E SUPPORT FITTING PER S/B 53-69. 2 L 7 3 4F A3WE 1996091200683 19960912 00683 NM 1996 9 12 DHL9671558D 1 19960707 A 5230 SKIN BOEING 727 727155C 138404Z NM CARGO DOOR DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, FOUND AFT CARGO DOOR HAS DEEP GOUGES, NICKS AND DENTS. BURNISHED OUT GOUGES, NICKS AND DENTS. DEEP DENT 12 INCHES BEYOND HANDLE. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PER SRM 52-00-3. FILLER, 12 INCHES BY 18 INCHES, DOUB LER, 25 INCHES BY 34 INCHES. 2 L 7 3 4F A3WE 1996091200684 19960912 00684 NM 1996 9 12 DHL9671559D 1 19960712 A 3230 652448017 FITTING BOEING 727 727155C 138404Z NM LT MLG CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, FOUND LEFT MLG UPLOCK SUPPORT FITTING HAS DEEP CORROSION, HFEC SHOWS CRACK INDICATION. REPLACED SUPPORT FI TTING PER S/B 53-103. 2 L 7 3 4F A3WE 1996091200685 19960912 00685 NM 1996 9 12 DHL9671560D 1 19960710 A 5320 FITTING BOEING 727 727155C 138404Z NM BS 950 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, EDDY CURRENT INSPECTION SHOWS CRACK INDICATION AT ROW A, BOTTOM HOLE AT STA 950 LT, STR 9 LT. OVERSIZED HOL E, INSTALLED FASTENER PER BOEING TELEX DHL MIA 960018R AND S/B 53-0196. 2 L 7 3 4F A3WE 1996091200686 19960912 00686 NM 1996 9 12 DHL9671561D 1 19960711 A 5320 ANGLE BOEING 727 727155C 138404Z NM BS 760.95 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, VERTICAL ANGLE CORRODED AT AFT SIDE OF BS 790.95 AT LEFT SIDE OF CABIN, AT FUSELAGE FRAME TO 70.5 WING RIB UPPER CHORD ATTACH AREA. REMOVED AND REPLACED ANGLE, 3 FEET BY 3 FEET BY 2 INCHES. 2 L 7 3 4F A3WE 1996091200687 19960912 00687 NM 1996 9 12 DHL9671562D 1 19960708 A 5311 FRAME BOEING 727 727155C 138404Z NM BS 620 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, FUSELAGE INTERIOR FRAME CORRODED AT BS 620 INNER FLANGE ABOVE FLOOR LEVEL. REMOVED AND REPLACED SPLICE PLAT E PER SRM 51-40-3 . PLATE 6 INCHES BY 7 INCHES. 2 L 7 3 4F A3WE 1996091200688 19960912 00688 NM 1996 9 12 DHL9671563D 1 19960707 A 5711 SPAR BOEING 727 727155C 138404Z NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, RIGHT WING UPPER SPAR SHOWS CRACK ON VERTICAL FLANGE OUTBD SIDE OF NR 13 SPOILER ACTUATOR MOUNT CASTING. C UT OUT DAMAGED SECTION PER S/B 57-145 , 23 INCHES BY 2 INCHES. INSTALLED REPAIR PER S/B 57-145, DRAWING 65C19647 AND AV ITAS DRAWING 96PMSI127D-1. REPAIR ANGLES, 34 INCH BY 2 INCH BY 2 INCH, AND, 30 INCH BY 2 INCH BY 2 INCH. 2 L 7 3 4F A3WE 1996091200689 19960912 00689 NM 1996 9 12 DHL9671564D 1 19960710 A 5320 FITTING BOEING 727 727155C 138404Z NM BS 870 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, FS 870 FRAME HAS WEB SEPARATION OUTBOARD END OF LIGHTING HOLE BETWEEN STR 9 RT - 10 RT. ULTRA SONIC INSPECT ED CRACK SEPARATION OF LIGHTING HOLES BELOW STR 9 RT. END OF SEPARATON STOPS ABOUT .375 INCH FROM EDGE. CUT TERMINAL F ITTING PER S/B 53-194. INSTALLED REPLACEMENT FITTING SEGMENT AT STA 870 BETWEEN STR 9 AND STR 13 PER S/B 53-194. 2 L 7 3 4F A3WE 1996091200690 19960912 00690 NM 1996 9 12 DHL9671565D 1 19960707 A 5320 65C290804 BEAM BOEING 727 727155C 138404Z NM BS 1183 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, AFT BAGGAGE VERTICAL BEAM AT BS 1183 AND LBL 8 IS CRACKED AT LOWER END. STOP DRILL CRACK PER SRM. REPAIRED VERTICAL BEAM PER S/B 53-0175 . 2 L 7 3 4F A3WE 1996091200691 19960912 00691 NM 1996 9 12 DHL9671566D 1 19960730 A 5712 RIB BOEING 727 727155C 138404Z NM BL 70.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, INSPECTED WING RIB UPPER CHORD AT BL 70.5. TWO CRACKS FOUND AT FWD TWO HOLES. STOPPED DRILLED CRACKS. INS TALLED REPAIR KIT PER S/B 57-112. 2 L 7 3 4F A3WE 1996091200692 19960912 00692 NM 1996 9 12 DHL9671567D 1 19960707 A 5711 SPAR BOEING 727 727155C 138404Z NM RT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, RIGHT WING HAS CORROSION ON REAR SPAR JUST FWD OF APU EXHAUST. REMOVED DAMAGED AREA, INSTALLED REPAIR PER S RM 57-10-6, 11 INCHES BY 5 INCHES. 2 L 7 3 4F A3WE 1996091200693 19960912 00693 NM 1996 9 12 DHL9671501D 1 19960725 A 5230 SKIN BOEING 727 727155C 138404Z NM AFT CARGO DOOR CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, AFT CARGO DOOR BULGED AND CRACKED AT AFT END OF HANDLE. INSTALLED DOUBLER REPAIR AT AFT END OF HANDLE PER S RMM 51-40-2, DOUBLER 6.5 INCHES BY 4.5 INCHES, FILLER, 1.37 INCH BY 1.25 INCH. 2 L 7 3 4F A3WE 1996091200694 19960912 00694 NM 1996 9 12 DHL9671502D 1 19960719 A 5330 SKIN BOEING 727 727155C 138404Z NM BS 480 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, SHEAR TIE AT STA 480 STR 19R CRACKED AFTER REMOVING SKIN DOUBLER PER ANOTHER NON-ROUTINE. INSTALLED DOUBLER REPAIR PER SRM 51-40-2, 7 INCHES BY 2 INCHES. 2 L 7 3 4F A3WE 1996091200695 19960912 00695 NM 1996 9 12 DHL9671503D 1 19960717 A 5315 FLOOR BEAM BOEING 727 727155C 138404Z NM BS 600 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D- CHECK, FOUND FLOOR BEAM CORRODED AT FWD UPPER FLANGE LOWER SURFACE RBL 60 BS 600. CUT OUT AREA, INSTALLED REPAIR PER SRM 53-10-8, 2.5 INCHES BY 13 INCHES . 2 L 7 3 4F A3WE 1996091200696 19960912 00696 NM 1996 9 12 DHL9671504D 1 19960711 A 5320 ANGLE BOEING 727 727155C 138404Z NM BS 760.95 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, FOUND VERTICAL ANGLE CORRODED AT AFT SIDE OF BS 760.95 AT LT SIDE OF CABIN AT FUSELAGE FRAME TO 70.5 WING RI B. REPLACED ANGLE PER SRM, 3 FEET BY 3 FEET BY 2 FEET. 2 L 7 3 4F A3WE 1996091200697 19960912 00697 NM 1996 9 12 DHL9671505D 1 19960711 A 5320 WEB BOEING 727 727155C 138404Z NM AFT AIRSTAIR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, LOWER RT TORQUE BOX AFT AIRSTAIR AREA LOWER CASTING VERTICAL WEB HAS CRACK. INSTALLED DOUBLER REPAIR PER SR M 51-40-2, 5 INCHES BY 8 INCHES. 2 L 7 3 4F A3WE 1996091200698 19960912 00698 NM 1996 9 12 DHL9671506D 1 19960709 A 5330 SKIN BOEING 727 727155C 138404Z NM BS 1342 LOOSE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, STA 1342 RT SIDE, STR 8R HAS LOOSE SKIN AND RIVETS. CUT OUT DAMAGED SECTION, INSTALLED DOUBLER REPAIR PER S RM 51-40-2, 3 INCHES BY 7 INCHES. REMOVED AND REPLACED RIVETS PER SRM 51030-2. 2 L 7 3 4F A3WE 1996091200699 19960912 00699 NM 1996 9 12 DHL9671507D 1 19960708 A 5312 BULKHEAD ANGLE BOEING 727 727155C 138404Z NM BS 1183 CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D C HECK, AFT SIDE OF 1183 BULKHEAD HORIZONTAL Z ANGLE AT LBL 22 HAS BEEN CHAFFED THROUGH BY VERTIAL DOOR FRAME ANGL E INSTALLED ANGLE REPAIR PER SRM 51-40-3 10.5 X 1.5 X 1 2 L 7 3 4F A3WE 1996091200700 19960912 00700 NM 1996 9 12 DHL9671508C 1 19960708 A 5312 BULKHEAD ANGLE BOEING 727 727155C 138404Z NM BS 1183 CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, AFT SIDE OF STA 1183 BULKHEAD HORIZONTAL Z-ANGLE AT RBL 22 HAS BEEN CHAFED BY VERTICAL FRAME ANGLE. INSTAL LED ANGLE REPAIR PER SRM 51-40-3, 1.25 INCHES BY 1 INCH. 2 L 7 3 4F A3WE 1996091200701 19960912 00701 NM 1996 9 12 DHL9671509D 1 19960713 A 5347 15201432 SEAT TRACK BOEING 727 727155C 138404Z NM BS 600-650 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, SEAT TRACK CORRODED STA 600 - STA 650. REPLACED SEAT TRACK PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996091200702 19960912 00702 NM 1996 9 12 DHL9671510D 1 19960713 A 5347 1520792 SEAT TRACK BOEING 727 727155C 138404Z NM BS 640-740 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, SEAT TRACK CORRODED AT STA 640 - STA 740. REMOVED AND REPLACED SEAT TRACK PER SRM 51-10-1, 7 FEET BY 4 INCH ES . 2 L 7 3 4F A3WE 1996091200703 19960912 00703 NM 1996 9 12 DHL9671511D 1 19960718 A 5347 BAC15201430 SEAT TRACK BOEING 727 727155C 138404Z NM BS 759-848 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, CABIN SEAT TRACK 31 HAS CORROSION STA 759 - STA 848. REMOVED SEAT TRACK AND REPLACED FROM STA 740 - STA 848 PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996091200704 19960912 00704 NM 1996 9 12 DHL9671512D 1 19960713 A 5712 RIB BOEING 727 727155C 138404Z NM WS 629.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, RIGHT WING RIB HAS CRACK ON LOWER FLANGE STA 629.5. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 57-10- 5, 9 INCHES BY 1 INCH BY 1 INCH . 2 L 7 3 4F A3WE 1996091200705 19960912 00705 NM 1996 9 12 DHL9671513D 1 19960713 A 5712 RIB BOEING 727 727155C 138404Z NM WS 601.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, RIGHT WING RIB AT STA 601.5 HAS CRACK IN RADII. STOP DRILLED CRACK AND INSTALLED RIB REPAIR PER SRM 57-10-5 , 10 INCHES BY 3.5 INCHES. 2 L 7 3 4F A3WE 1996091200706 19960912 00706 NM 1996 9 12 DHL9671514D 1 19960716 A 5713 STRINGER BOEING 727 727155C 138404Z NM WS 656.5 BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, STRINGER TAB ATTACH BROKEN OFF AT WING STA 656.5 AT R 13. INSTALL REPAIR PER S/B 57A159, 12 FEET LONG. 2 L 7 3 4F A3WE 1996091200707 19960912 00707 NM 1996 9 12 DHL9671515D 1 19960716 A 5712 RIB BOEING 727 727155C 138404Z NM WS 656.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, FOUND CRACK IN LEFT WING AT STA 656.5 S-4 ATTACH RADIUS. FABRICATED AND INSTALLED PARTS PER SRM 57-10-5, 8 INCHES BY 2.5 INCHES. 2 L 7 3 4F A3WE 1996091200708 19960912 00708 NM 1996 9 12 DHL9671516D 1 19960716 A 5713 STRINGER BOEING 727 727155C 138404Z NM WS 601 BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, STRINGER TAB BROKEN AT WS 601, LEFT WING STRINGER 11. CUT OUT TAB AND INSTALLED REPAIR PER S/B 57A159, 12.5 INCHES LONG. 2 L 7 3 4F A3WE 1996091200709 19960912 00709 NM 1996 9 12 DHL9671517D 1 19960716 A 5712 RIB BOEING 727 727155C 138404Z NM WS 601 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, RIB IN LEFT WING STA 601 AT STR 2 HAS CRACK. INSTALLED DOUBLER PER SRM 57-10-5, 7 INCHES BY 4.5 INCHES . 2 L 7 3 4F A3WE 1996091200710 19960912 00710 NM 1996 9 12 DHL9671518D 1 19960713 A 5713 STRINGER BOEING 727 727155C 138404Z NM WS 629 BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, LEFT WING STA 629 TOP SKIN STRINGER HAS BROKEN ATTACH FLANGE. REPAIRED PER S/B 57A159, 12.5 INCHES LONG. 2 L 7 3 4F A3WE 1996091200711 19960912 00711 NM 1996 9 12 DHL9671519D 1 19960713 A 5712 RIB BOEING 727 727155C 138404Z NM WS 629.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, RIB W/S 629.5 LOWER FLANGE OF RIB HAS CRACK IN EXISTING DOUBLER REPAIR. REMOVED REPAIR, INSTALLED DOUBLER R EPAIR PER SRM 57-10-5, 10 INCHES BY 5 INCHES. 2 L 7 3 4F A3WE 1996091200712 19960912 00712 NM 1996 9 12 DHL9671520D 1 19960713 A 5712 RIB BOEING 727 727155C 138404Z NM WS 686.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, LEFT WING RIB STA 686.5 HAS CRACK .5 INCH. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 57-10-5, 8.5 IN CHES BY 4.5 INCHES . 2 L 7 3 4F A3WE 1996091200713 19960912 00713 NM 1996 9 12 DHL9671521D 1 19960711 A 5720 ANGLE BOEING 727 727155C 138404Z NM WS 130.7 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, LT WING LEADING EDGE CAVITY STA 130.7 LOWER SUPPORT ANGLE CRACKED AFT OF MIDDLE SUPPORT ANGLE AT ATTACH BOLT . INSTALLED SUPPORT ANGLE PER SRM 51-40-3, 9 INCHES BY 1 INCH BY 1 INCH. 2 L 7 3 4F A3WE 1996091200714 19960912 00714 NM 1996 9 12 DHL9671522D 1 19960709 A 5720 ANGLE BOEING 727 727155C 138404Z NM WS 121.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, LT WING LEADING EDGE LOWER SUPPORT ANGLE AT WS 121.5 CRACKED AT ATTACH BOLTS. STOP DRILLED AND INSTALLED AN GLE REPAIR, 4 INCHES BY 1 INCH, PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996091200715 19960912 00715 NM 1996 9 12 DHL9671523D 1 19960713 A 5712 RIB BOEING 727 727155C 138404Z NM WS 629.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, RIGHT WING STA 629.5 LOWER FLANGE OF RIB HAS CRACK. INSTALLED DOUBLER REPAIR PER SRM 57-10-5, 8 INCHES LONG . 2 L 7 3 4F A3WE 1996091200716 19960912 00716 NM 1996 9 12 DHL9671524D 1 19960711 A 5720 ANGLE BOEING 727 727155C 138404Z NM WBL 92.8 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, LT LEADING EDGE CAVITY WBL 92.8 SECOND VERTICAL SUPPORT ANGLE IS CRACKED AT BOTTOM FASTENER. STOP DRILLED C RACK, INSTALLED ANGLE REPAIR, 9 INCHES BY 1 INCH BY 1 INCH, PER SRM 51-40-3. 2 L 7 3 4F A3WE 1996091200717 19960912 00717 NM 1996 9 12 DHL9671525D 1 19960703 A 5330 SKIN BOEING 727 727155C 138404Z NM BS 600 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, FUSELAGE EXTERNAL SKIN DENTED STA 600 RIGHT STR 21 TO STR 24. CUT OUT DAMAGED AREA AND INSTALLED DOUBLERS PER SRM 53-10-3, 2 INCHES BY 4 INCHES. 2 L 7 3 4F A3WE 1996091200718 19960912 00718 NM 1996 9 12 DHL9671526D 1 19960722 A 5330 SKIN BOEING 727 727155C 138404Z NM BS 480 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, SKIN DOUBLER STA 480 STR 19R INSTALLED WITH BLIND FASTENERS. INSTALLED REPAIR DOUBLER PER SRM 53-30-3. FIL LER, 4.125 INCH BY 2 INCHES. DOUBLER, 10 INCHES BY 4 INCHES . 2 L 7 3 4F A3WE 1996091200719 19960912 00719 NM 1996 9 12 DHL9671527D 1 19960707 A 5320 BEAM BOEING 727 727155C 138404Z NM BS 1183 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, AFT BAGGAGE VERTICAL BEAM AT BS 1183 RBL 8 IS CRACKED. INSTALLED REPAIR PER S/B 53-0175. 2 L 7 3 4F A3WE 1996091200720 19960912 00720 NM 1996 9 12 DHL9671528D 1 19960713 A 5330 SKIN BOEING 727 727155C 138404Z NM BS 235.8 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, CRACK IN FUESLAGE BS 235.8, STR 15L. CUT OUT CRACKED AREA, INSTALLED DOUBLER REPAIR, PER SRM 53-30-3, 11 IN CHES BY 8 INCHES, AND FILLER, .75 INCH BY 3.375 INCHES. 2 L 7 3 4F A3WE 1996091200721 19960912 00721 NM 1996 9 12 DHL9671529D 1 19960708 A 5330 SKIN BOEING 727 727155C 138404Z NM BS 251.6 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT D-CHECK, FUSELAGE CRACKED AT BS 251.6 BETWEEN STR 15L AND STR 16L. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER, 8 INC HES BY 9 INCHES AND FILLER, 1.5 INCH BY .5 INCH, PER SRM 53-30-3. 2 L 7 3 4F A3WE 1996091200722 19960912 00722 NM 1996 9 12 DHL96726001 1 19960906 A 3260 656021132 ACCESSORY UNIT BOEING 727 727228 NM RT MLG FAILED A DHLA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 726DH 20409 AFTER TAKEOFF, RIGHT MAIN GEAR UNSAFE LIGHT REMAINED ILLUMINATED. REMOVED LANDING GEAR ACCESS UNIT IAW B727MM 32-09-121 . NO DEFECTS NOTED. 2 L 7 3 4F A3WE 1996091200723 19960912 00723 NM 1996 9 12 P5CA9600685 1 19960903 A 5320 AND101392005 STIFFENER BOEING 747 747122 1384872 NM BS 1400 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 CRACKED STIFFENER ON RIGHT BODY GEAR WHEELWELL PRESSURE DECK BS 1400 RBL 100. REMOVED STIFFENER, PERFORMED HFEC INSPECT ION OF AREA BELOW CRACK PER BOEING NDT MANUAL PART 6 51-00-00. NO DEFECTS NOTED. REPLACED STIFFENER WITH NEW PART PER BOEING SRM 51-10-01. MATERIAL IDENTIFICATION PER BOEING SRM 53-11-22, PAGE 143. 2 L 7 4 4F A20WE 1996091200724 19960912 00724 NM 1996 9 12 P5CA9600686 1 19960905 A 3350 S1356B37 LIGHT BOEING 747 747123 1384873 NM UPPER DECK INOPERATIVE A P5CA K NONE L NO TEST IN INSP/MAINT 1 WP 23 859FT 20326 UPPER DECK CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY PER BOEING MAINTENANCE MANUAL 33-51-00. 2 L 7 4 4F A20WE 1996091200725 19960912 00725 NM 1996 9 12 P5CA9600687 1 19960907 A 5753 65B1159831 SEQ CARRIAGE BOEING 747 747122 1384872 NM LT TE FLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LEFT INBOARD FLAP SEQUENCE CARRIAGE FAILED DAMAGING THE LEFT INBOARD FORE FLAP. REMOVED AND REPLACED LEFT INBOARD FORE FLAP, CARRIAGES AND TRACK OPERATIONAL CHECK GOOD PER BOEING MAINTENANCE MANUAL 27-51-02. 2 L 7 4 4F A20WE 1996091200726 19960912 00726 SO 1996 9 12 SRAA960906 1 19960907 A 7603 GIMBLE ASSY LKHEED 382 382G 526414U SO NR 4 THROTTLE JAMMED A A SRAA A UNSCHED LANDING O OTHER DE DESCENT 1 GL 23 909SJ 4763 ON DESCENT, FLT 1908 INTO AED, NR 4 THROTTLE LEVER WOULD NOT ADVANCE ABOVE 2 POUND/INCH PAST FLIGHT IDLE, OCCURED AT 7 ,000 FEET, ENGINE AT 6,900 INCH/POUNDS TORQUE, AND 720 DEGREES TIT. AIRCRAFT DIVERTED TO OTZ AND LANDED WITHOUT INCIDEN T. INSPECTED NR 4 THROTTLE CABLE SYSTEM AT NACELLE AND HORSE COLLAR AND UNDER FLIGHT DECK, FOUND A PENNY IN LOWER GIMBL E ASSY AT CENTER CONSOLE, REMOVED PENNY. SYSTEM OPS CHECKED GOOD PER M.M. CH 72. 2 H 7 4 4T A1SO 1996091200840 19960912 00840 WP 1996 9 12 CA960123014 2 19960104 A 7310 31033781 LINE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP FUEL MANIFOLD WORN W K NONE O OTHER IN INSP/MAINT 1 CA P44144C (CAN)FUEL LINE FOUND RUBBING ON AN OIL LINE ON LH ENGINE. FUEL LINE ALMOST WORN THROUGH. 2 L 7 2 4T 4 T RT A8SW E4WE 1996091200841 19960912 00841 SW 1996 9 12 CA960123015 1 19960110 A 7603 LEVER ARM SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP PROP PITCH CONT LOOSE NUT W E ENGINE SHUTDOWN O OTHER AP APPROACH 1 CA P44220C (CAN)LOST ENGINE CONTROL WITH POWER LEVER. WHEN RETARDING POWER FOR LANDING, ENGINE REMAINED AT CRUISE POWER. ENGINE SHU TDOWN AND SINGLE ENGINE LANDING MADE. FOUND ARM SEPARATED FROM PROPELLER PITCH CONTRO L. NUT AND BOLT HAD COME LOOSE. 2 L 7 2 4T 4 T RT A8SW E4WE 1996091200842 19960912 00842 SW 1996 9 12 CA960123016 1 19960108 A 3230 2781032005 LINE SWRNGN SA227 SA227AC 8780603 SW RT MAIN HYD CRACKED W K NONE K FLUID LOSS AP APPROACH 1 CA (CAN)RH MAIN LANDING GEAR SLOW TO EXTEND. CRACKED GEAR UP HYDRAULIC LINE FOUND UNDER CAPTAIN'S SEAT. 2 L 7 2 4T RT A8SW 1996091200844 19960912 00844 EA 1996 9 12 CA960123018 2 19960118 A 7210 3036674 OIL SEAL PWA 3024780 BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA GEARBOX HOUSING WORN W K NONE O OTHER IN INSP/MAINT 1 CA CPGB1659 CPPS61075 (CAN)WHILE MONITORING AIRCRAFT OIL CONSUMPTION IT WAS FOUND THAT THE COMBINING GEARBOX OIL WAS TRANSFERRING TO #2 ENGINE . THE GEARBOX WAS REMOVED AND THE PROBLEM WAS CAUSED BY THE ROTATION OF A WORN CARBONSEAL ROTATING IN THE RETAINER (P/N 3023913), WEARING THE RETAINER AND LEAVING OIL TO POSSIBLY TRANSFER TO THE POWER SECTION. 1 G 7 1 4U 4 U H4SW E22EA 1996091200845 19960912 00845 EA 1996 9 12 CA960123019 2 19960118 A 7210 3026609 CHIP DETECTOR PWA 3024780 BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA COMBINING GEARBX BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA CPGB1659 CPPS61075 (CAN)WHILE REMOVING COMBINING GEARBOX CHIP DETECTOR, ALL OIL DRAINED FROM THE GEARBOX. THIS SHOULD NOT HAVE HAPPENED AS THE CHIP DETECTOR IS A SELF SEALING TYPE. THE HOUSING WAS REMOVED FOR INSPECTION AND THE CHIP DETECTOR PLUG AND SPRING WERE MISSING. CHIP DETECTOR PLUG AND SPRING WERE FOUND IN THE GEARBOX AFTER DISASSEMBLY OF THE GEARBOX. 1 G 7 1 4U 4 U H4SW E22EA 1996091200846 19960912 00846 NE 1996 9 12 CA960123020 2 19960113 A 7230 LINER LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB21122B02 54555 NE NR 1 ENGINE DELAMINATED W C ABORTED TAKEOFF D INFLIGHT SEPARATION TO TAKEOFF 1 CA 50877 1252 10389 (CAN) ON DEPARTURE, NR 1 ENGINE SUFFERED A COMPRESSOR STALL, TAKEOFF WAS REJECTED. POST INSPECTION FOUND NR 1 ENGINE LP COMPRESSOR CASE ACOUSTIC LINER DELAMINATED AND STUCK ON BYPASS DUCT VANE. DEBRIS REMOVED ON THE GROUND. ENGINE GROUND RUN, NO VIBRATIONS, NO STALL ON ENGINE RUN. DELAMINATION PANEL INSPECTED AND FOUND WITHIN LIMITS. 2 L 7 3 4F 4 F A23WE E12EU 1996091200854 19960912 00854 EA 1996 9 12 CA960126001 1 19960124 A 2434 23088002A GENERATOR LUCAS DHAV DHC8 DHC8311 1386006 EA DC SYSTEM LIGHTNING STRIKE W A UNSCHED LANDING G H MULTIPLE FAILURE ELECT. POWER LOSS-50 PC CL CLIMB 1 CA (CAN)DOUBLE LIGHTNING STRIKE ON DEPARTURE. DOUBLE DC GENERATOR FAILURE. EMERGENCY CHECK LIST CARRIED OUT. BOTH GENERATOR S CAME BACK ON LINE. FIVE STATIC WICKS HAD TO BE REPLACED. 2 H 7 2 4T RT A13NM 1996091200855 19960912 00855 NM 1996 9 12 CA960126002 1 19960124 A 2750 734177E SPLINE SUNDSTRANDEM DHAV DHC8 DHC8102 2809003 NM LH FLAP NOT ENGAGED W A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 CA 20069 569 0141 (CAN)FLAP DRIVE CAUTION LIGHT ON AFTER TAKEOFF. AIRCRAFT RETURNED. FOUND LEFT DRIVE SPLINE NOT ENGAGING IN FLAP POWER UN IT. FPU REPLACED. 2 H 7 2 4T RT A13NM 1996091200856 19960912 00856 NM 1996 9 12 CA960126003 1 19960124 A 3232 82970018013 ACTUATOR DHAV DHC8 DHC8101 2809002 NM LH FWD GEAR DOOR LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 19059 3745 (CAN)FLUID LEAK, LH FORWARD DOOR ACTUATOR. ACTUATOR REPLACED. 2 H 7 2 4T RT A13NM 1996091200857 19960912 00857 CE 1996 9 12 CA960126004 1 19960116 A 3233 K306 MLG SOLENOID MTSBSI MU2 MU2B36 5780412 CE MAIN CONTACTS BURNT CONTACTS W L H O ABORTED APPROACH DEACTIVATE SYST/CIRCUITS OTHER J WARNING INDICATION AP APPROACH 1 CA 7920 (CAN)THE CREW SELECTED GEAR DOWN ON APPROACH AND THE GEAR DOORS OPENED BUT NOTHING FURTHER HAPPENED. THEY THEN NOTICED T HAT THE GEAR MOTOR CIRCUIT MOTOR HAD TRIPPED. THE BREAKER WAS RESET AND THE GEAR CYCL ED AGAIN WITH THE SAME RESULTS. EM ERGENCY EXTENSION WAS PERFORMED AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. INSPECTION REVEALED THE MAIN CONTACTS ON THE SOLENOID MOTOR WERE FUSED. THE SOLENOID CONTACTS WERE DRESSED OUT AND THE MOTOR RETURNED TO SERVICE. 1 H 7 2 3T RT A10SW 1996091200858 19960912 00858 NM 1996 9 12 CA960126005 1 19960114 A 3230 7326090015 ACCESSORY UNIT BOEING 737 737242C 1384478 NM NLG INTERMITTENT W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN)NOSE GEAR DID NOT RETRACT AFTER TAKEOFF. GREEN LIGHT REMAINED ON, BUT WHEN THE GEAR SELECTED OFF, THE RED LIGHT DID NOT COME ON. AIRCRAFT RETURNED. LANDING GEAR ACCESSORY UNIT REPLACED. 2 L 7 2 4F A16WE 1996091200859 19960912 00859 NM 1996 9 12 CALA9601288 1 19960824 A 5311 FRAME BOEING 727 727224 1384076 NM BS 1130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND FRAME CORRODED BETWEEN STRINGER 27L AND 28L AT STA 1130. A SHEAR TIE REPAIR WAS FABRICATED AND INSTALL ED IAW SRM 53-10-4. 2 L 7 3 4F A3WE 1996091200860 19960912 00860 NM 1996 9 12 CALA9601289 1 19960824 A 5313 STRINGER BOEING 727 727224 1384076 NM BS 1148-1166 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND STRINGER 30 CORRODED BETWEEN STA 1166 AND 1148. A STRINGER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-3-10, FIGURE 1, SHEET 1 TO 4. 2 L 7 3 4F A3WE 1996091200861 19960912 00861 NM 1996 9 12 CALA9601290 1 19960823 A 5730 SKIN BOEING 727 727224 1384076 NM LT WING LE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND THE LT WING LEADING EDGE SKIN BENT AND WITH SEVERAL 1 INCH CRACKS AT NR 3 SLAT ACTUATOR CUTOUT. REPAI R DOUBLERS AND FILLER WERE FABRICATED AND INSTALLED IAW ECRA 5720-01540. 2 L 7 3 4F A3WE 1996091200862 19960912 00862 NM 1996 9 12 CALA9601291 1 19960822 A 5753 SKIN BOEING 727 727224 1384076 NM RT TE FLAP CHAFED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND THE RT INBOARD TRAILING EDGE AFT FLAP CHAFED AT TOP SURFACE, INBOARD END. THE CHAFED AREA WAS CUT OUT AND A HOT BOND REPAIR WAS ACCOMPLISHED IAW SRM 51-40-6. 2 L 7 3 4F A3WE 1996091200863 19960912 00863 NM 1996 9 12 CALA9601292 1 19960822 A 5753 SKIN BOEING 727 727224 1384076 NM NR 4 TE FOREFLAP DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND LT INBOARD FORE FLAP LOWER SURFACE DELAMINATED BOTH SIDES OF NR 4 FLAP TRACK. A FIBERGLASS OVERLAY REP AIR WAS ACCOMPLISHED IAW SRM 51-40-6. 2 L 7 3 4F A3WE 1996091200864 19960912 00864 NM 1996 9 12 CALA9601293 1 19960822 A 5753 SKIN BOEING 727 727224 1384076 NM LT TE AFT FLAP DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND A DENT WITH DELAMINATION 33 INCHES FROM INBOARD END LOWER SURFACE OF LT OUTBOARD AFT FLAP. THE DAMAGED AREA WAS CUT OUT AND A HOT BOND REPAIR WAS ACCOMPLISHED IAW SRM 51-40-6. 2 L 7 3 4F A3WE 1996091200865 19960912 00865 NM 1996 9 12 CALA9601294 1 19960831 A 5523 SKIN BOEING 727 727224 1384076 NM RT ELEV TAB DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND RT ELEVATOR TRIM TAB TRAILING EDGE DELAMINATED. A COLD BOND REPAIR WAS ACCOMPLISHED IAW SRM 51-40-6. WEIGHT AND BALANCE CHECKED WITHIN LIMITS IAW SRM 51-80-9. 2 L 7 3 4F A3WE 1996091200866 19960912 00866 NM 1996 9 12 CALA9601295 1 19960823 A 5330 SKIN BOEING 727 727224 1384076 NM BS 720 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND RT FUSELAGE SKIN DENTED AT STA 720C. THE DENT WAS REWORKED IAW SRM 53-30-1. AN HFEC INSPECTION WAS AC COMPLISHED WITH NO CRACKS NOTED. 2 L 7 3 4F A3WE 1996091200867 19960912 00867 NM 1996 9 12 CALA9601296 1 19960823 A 3350 900835A BATTERY BOEING 727 727224 1384076 NM CABIN INOPERATIVE A A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 79748 22450 THE RT OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE DURING EMERGENCY LIGHT OPERATIONAL CHECK. THE BATTERY CARTRI DGE WAS REMOVED AND REPLACED AND OPERATION OF THE EXIT LIGHT CHECKED GOOD IAW MM 33-50-0. 2 L 7 3 4F A3WE 1996091200868 19960912 00868 NE 1996 9 12 CALA9601297 2 19960905 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 2 FAILED A A CALA F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 SW 09 14889 15547 49118 717377 THE TOWER REPORTED FIRE FROM THE NR 2 ENGINE TAILCONE AREA DURING TAXI OUT. THE CAPTAIN DISCHARGED BOTH ENGINE FIRE BOT TLES AND THE FIRE DEPARTMENT WAS SUMMONED. AN EMERGENCY EVACUATION WAS PERFORMED. THE FORWARD SERVICE DOOR AND AFT SER VICE DOOR ESCAPE SLIDES WERE DEPLOYED. THE LT FORWARD ENTRY DOOR COULD NOT BE OPENED. MAINTENANCE FOUND THAT THE NR 2 ENGINE HAD EXPERIENCED A HOT START. THE ENGINE WAS CHANGED DUE TO THE HOT START AND FIRE AGENT INGESTION. EXAMINATION OF THE LT FORWARD ENTRY DOOR FOUND THAT A PORTION OF THE EMERGENCY SLIDE ASSEMBLY WAS JAMMED ON LIP OF DOOR SILL. THE D OOR SLIDE LANYARD HAD NOT BEEN CONNECTED. ALL THREE DOOR SLIDES WERE REMOVED AND REPLACED. 2 L 7 2 4F 4 F A6WE E9NE 1996091200869 19960912 00869 NM 1996 9 12 SWAA960920 1 19960906 A 2910 HYDRAULIC LINE BOEING 737 7372H4 138448C NM LT MLG RUPTURED A SWAA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 50SW 21447 AIR TURNBACK DUE TO A-SYSTEM LOW PRESS LIGHT AND LOW QUANTITY ILLUMINATING. AIRCRAFT MADE AN UNEVENTFUL LANDING AT HOU. REPLACED LEFT MAIN GEAR RETRACT ACTUATOR PRESSURE LINE AND OP CHECKED PER BOEING M/M. 2 L 7 2 4F A16WE 1996091200870 19960912 00870 NM 1996 9 12 SWAA960921 1 19960906 A 5315 FLOOR BEAM BOEING 737 7373Q8 1384670 NM BS 987 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM AT BS 987 WL 208.1 LBL 44 DAMAGED ON FWD SIDE OF UPPER FLANGE. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996091200871 19960912 00871 NM 1996 9 12 SWAA960922 1 19960906 A 5313 STRINGER BOEING 737 7373Q8 1384670 NM BS 995 PUNCTURED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED D-CHECK, FOUND STRINGER HAD .25 PUNCTURE ON LOWER SIDE AT BS 995, S12L. REPAIRED PER TRAMCO EWO 96-048 3. 2 L 7 2 4F RT A16WE 1996091200872 19960912 00872 NM 1996 9 12 SWAA960923 1 19960906 A 5315 FLOOR BEAM BOEING 737 7373Q8 1384670 NM BS 827 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM LOWER FLANGE CRACK AT BS 827, S20L, WL 176. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996091200873 19960912 00873 NM 1996 9 12 SWAA960924 1 19960906 A 5330 SKIN BOEING 737 7373Q8 1384670 NM BS 390 OIL CANNING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN OIL CANNING AT BS 390, BETWEEN S20 AND 21R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996091200874 19960912 00874 NM 1996 9 12 SWAA960925 1 19960906 A 5330 SKIN BOEING 737 7373Q8 1384670 NM BS 183 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 183 RBL 21 WL 184. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996091200875 19960912 00875 NM 1996 9 12 SWAA960926 1 19960906 A 5330 SKIN BOEING 737 7373Q8 1384670 NM BS 372 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 372, BETWEEN S17 AND 18R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996091200876 19960912 00876 NM 1996 9 12 SWAA960927 1 19960906 A 5312 BULKHEAD BOEING 737 7373Q8 1384670 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED D-CHECK, FOUND CRACK IN AFT SIDE OF PRESSURE BULKHEAD FWD CHORD TO VERTICAL STIFFENER AT BS 178 WL 184 LBL 5.7 AND AT WL 184 LBL 5.7. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996091200877 19960912 00877 NM 1996 9 12 SWAA960928 1 19960906 A 5320 WEB BOEING 737 7373Q8 1384670 NM BS 793 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED D-CHECK, FOUND WEB CRACKED FWD OF AFT CARGO DOOR CUTOUT AT BS 793 RBL 30 WL 161. REPAIRED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1996091200878 19960912 00878 NM 1996 9 12 SWAA960929 1 19960906 A 5330 SKIN BOEING 737 7373Q8 1384670 NM BS 282/290 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 282 AND AT 290, JUST BELOW S22R. REPAIRED BOTH PER BOEING SR M. 2 L 7 2 4F RT A16WE 1996091200879 19960912 00879 NM 1996 9 12 SWAA960930 1 19960906 A 5330 SKIN BOEING 737 7373Q8 1384670 NM BS 494/916 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 494, S18R, S18R AND AT BS 916, BETWEEN SS15 AND 16L. REPAIRE D BOTH PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996091200880 19960912 00880 NM 1996 9 12 SWAA960931 1 19960906 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 74SW 22674 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 540 RBL 56 WL 165. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996091200881 19960912 00881 NM 1996 9 12 SWAA960932 1 19960906 A 5315 FLOOR BEAM BOEING 737 7373Q8 1384670 NM BS 987 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM DAMAGED AT BS 987 RBL 44 WL 208 FWD SIDE OF UPPER FLANGE. REPAIRED BOTH PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996091200882 19960912 00882 NM 1996 9 12 SWAA960933 1 19960907 A 5330 SKIN BOEING 737 7373T5 NM BS 1040 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 694SW 23061 DURING SCHEDULED C3 CHECK, FOUND DAMAGED TO FUSELAGE AT BS 1040, BETWEEN S27L AND 26L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996091200883 19960912 00883 NM 1996 9 12 SWAA960934 1 19960904 A 5320 MOPSILL BOEING 737 7373H4 1384600 NM BS 270-360 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 356SW 25251 DURING SCHEDULED D-CHECK, FOUND MOPSILL CORROSION AT BS 270 TO 360 RBL 51 TO 64 WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996091200884 19960912 00884 NM 1996 9 12 SWAA960935 1 19960906 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 601SW 27695 DURING SCHEDULED BC2 CHECK, FOUND CABIN FLOOR TRACK 4 LIGHTS INOP NEAR EMERGENCY EXIT. REPAIRED LIGHTS PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996091200885 19960912 00885 NM 1996 9 12 SWAA960936 1 19960908 A 3350 LIGHTS BOEING 737 7373A4 1384585 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED A1 CHECK, FOUND EMERGENCY LIGHTS INOP ABOVE FWD AND AFT SERVICE DOORS. CLEANED AND RESEATED CANNON PLU G PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996091200886 19960912 00886 NM 1996 9 12 SWAA960937 1 19960908 A 5314 KEEL BEAM BOEING 737 7373Q8 1384670 NM LWR FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 689SW 23387 DURING SCHEDULED BC4 CHECK, FOUND LOWER FUSELAGE KEEL BEAM FIXED PANEL CRACKED AT I/B RT ROW OF FASTENERS. REPAIRED PER SWA RA 1-A53-1273. 2 L 7 2 4F RT A16WE 1996091200887 19960912 00887 NM 1996 9 12 SWAA960938 1 19960905 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 967 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED BC1 CHECK, FOUND FUSELAGE SKIN REPAIR DOUBLER BELOW AFT ENTRY DOOR GOUGED AT BS 967. REPLACED PER SWA RA 1-353-1510. 2 L 7 2 4F RT A16WE 1996091200888 19960912 00888 NM 1996 9 12 SWAA960939 1 19960908 A 3350 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 362SW 26571 AT GATE, FOUND AFT EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996091200889 19960912 00889 NM 1996 9 12 SWAA960940 1 19960906 A 3350 20121 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 505SW 24183 AT GATE, FOUND EMERGENCY TRACK LIGHTING INOP AT ROWS 6, 7 AND 8. REPLACED EXIT LIGHT LOWER SUPPLY BASE PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996091200890 19960912 00890 EU 1996 9 12 96FDEA01456 1 19960909 A 5210 MECHANISM AIRBUS 310 A310222 3930315 EU RT CABIN DOOR NOT LOCKED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 422FE 346 DURING CLIMBOUT, RIGHT CABIN DOOR OPEN WARNING CAME ON. A/C PRESSURIZTION NORMAL. CREW BROUGHT DEADHEADS INTO COCKPIT AND MADE PRECAUTIONARY LANDING. UNABLE TO SILENCE WARNING CHIME. VISUAL INSPECTION OF DOOR LOCK INDICATOR SHOWED NOT F ULLY LOCKED DISPLAYED AT WINDOW, DISARMED DOOR AND CYCLED DOOR HANDLE AND VISUAL LOCKED INDICATOR FULLY DISPLAYED IN WIN DOW. ECAM INDICATION SHOWED NORMAL. 2 L 7 2 4F RT A35EU 1996091200891 19960912 00891 NM 1996 9 12 96FDEA01457 1 19960910 A 5330 65182176 SKIN BOEING 727 72725 1384006 NM BS 481 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 509FE 18280 NR 0545 AND 016, CORROSION EMANATING FROM BONDED DOUBLER AND SKIN AT BS 481 STR 2 LT TO STR 3 RT. *S/D* CORROSION WAS FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SKIN, DOUBLER AND STRINGER 2 RT AT BS 478 TO 494. FABRICATED AND INSTALLED REPAIR PARTS PER FED EX EA 7-5330-311-5 AND 7-5310-31114. 2 L 7 3 4F A3WE 1996091200892 19960912 00892 NM 1996 9 12 96FDEA01458 1 19960910 A 5320 65196042 WEB BOEING 727 72725 1384006 NM BS 1174 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR 0290 AND 017, CORROSION (C53-224-01, -3) EMANATING FROM UNDER NUTPLATES ON BOTTOM SIDE OF SHEAR WEB AT BS 1174 RBL 22 LBL 16 WL 208. *S/D* REPAIRED AREA AT RBL 22 STA 1174 WL 208 PER FEDEX SRM 51-40-2 FIG 1. 2 L 7 3 4F A3WE 1996091200893 19960912 00893 NM 1996 9 12 96FDEA01459 1 19960910 A 5315 652082710 FLOORBEAM BOEING 727 72725 1384006 NM BS 620 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR 0375 AND 018, CORROSION (C53-224-01, -1) AROUND FASTENER HOLES ON UNDERSIDE OF FLOORBEAM AT BS 620 LBL TO 44 WL 208. *S/D* REPAIRED FLOORBEAM AT BS 620 LBL 10 TO 44 WL 208 PER FEDEX SRM 53-10-08. 2 L 7 3 4F A3WE 1996091200894 19960912 00894 NM 1996 9 12 96FDEA01442 1 19960906 A 5315 65208279 FLOORBEAM BOEING 727 72725 1384006 NM BS 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR 0446 AND 005, CORROSION (C53-111-01, -2) ON LOWER CHORD OF FLOORBEAM AT BS 600 LBL 15 WL 200. *S/D* REMOVED AND REP LACED FLOORBEAM LOWER CHORD STA 600 LBL TO RBL 25 WL 200 PER FEDEX SRM 53-10-8 FIG 2. 2 L 7 3 4F A3WE 1996091200895 19960912 00895 NM 1996 9 12 96FDEA01443 1 19960908 A 5315 65208407 FLOOR BEAM BOEING 727 72725 1384006 NM BS 1166 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR 0248 AND 006, CORROSION (C53-111-01, -3) ON LOWER CHORD OF FLOOR BEAM AT BS 1166 WL 200 RBL 27 AT NUTPLATE. *S/D* M ECHANICALLY REMOVED CORROSION IN AN AREA OF .75 BY 4, .066 MATERIAL REMOVED FROM ORIGINAL THICKNESS OF .120, OUT OF LIMI TS PER FED EX SRM 53-10-1. CUT OUT DAMAGE AREA OF FLANGE AND REPAIRED PER FED EX SRM 53-10-8 FIG 8. 2 L 7 3 4F A3WE 1996091200896 19960912 00896 NM 1996 9 12 96FDEA01444 1 19960908 A 5315 652082725 FLOOR BEAM BOEING 727 72725 1384006 NM BS 580 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR 0378 AND 007, CORROSION (C53-224-01, -1) AROUND FASTENER HOLE ON FLOOR BEAM TOP CHORD AT BS 580 LBL 36 WL 208. 2 L 7 3 4F A3WE 1996091200897 19960912 00897 NM 1996 9 12 96FDEA01445 1 19960908 A 5315 65402691 FLOOR BEAM BOEING 727 72725 1384006 NM BS 480 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR 0370 AND 008, CORROSION (C53-224-01, -1) AND BARE METAL 480 RBL 60 LBL 44 WL 208. 2 L 7 3 4F A3WE 1996091200898 19960912 00898 NM 1996 9 12 96FDEA01446 1 19960908 A 5320 65198621 CHORD BOEING 727 72725 1384006 NM BS 350 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR 0422 AND 009, CORROSION (C53-111-01-1) ON LT MID NOSE CHORD AT BS 350 LBL 13 WL 169. *S/D* REMOVED AND REPLACED MID NOSE CHORD AT BS 350 LBL 13 WL 169 IAW DRAWING 65-18415. 2 L 7 3 4F A3WE 1996091200899 19960912 00899 NM 1996 9 12 96FDEA01436 1 19960906 A 5753 6521630173 SKIN BOEING 727 72725 1384006 NM LT TE FORE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR 0196 AND 002, LT WING I/B FORE FLAP HAS A LARGE CREASED DENT MID SPAN UPPER SURFACE WBL 203.0. *S/D* LT WING I/B FO RE FLAP REPAIRED PER FDEA SRM 51-40-6. 2 L 7 3 4F A3WE 1996091200900 19960912 00900 NM 1996 9 12 96FDEA01450 1 19960909 A 5315 652082724 FLOORBEAM BOEING 727 72725 1384006 NM BS 560 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR 0372 AND 011, CORROSION (C53-224-01, -1) AROUND FASTENER HOLES ON UNDER SIDE OF FLOORBEAM AT BS 560 RBL 56 TO LBL 56 WL 208. *S/D* REPAIRED TOP CHORD OF BS 560 FLOORBEAM LBL 65 TO RBL 56 PER FEDEX SRM 53-10-8. 2 L 7 3 4F A3WE 1996091200901 19960912 00901 NM 1996 9 12 96FDEA01451 1 19960909 A 5230 65186256 BEAM BOEING 727 72725 1384006 NM BS 1060-1108 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR 0275 AND 012, AFT CARGO DOOR BEAM NR 2 FROM TOP IS CRACKED IN RADIUS. *S/D* REMOVED AND REPLACED AFT CARGO DOOR BEA M NR 2 FROM TOP PER FEDEX SRM 51-10-1. 2 L 7 3 4F A3WE 1996091200902 19960912 00902 NM 1996 9 12 96FDEA01452 1 19960909 A 5230 651862013 BEAM BOEING 727 72725 1384006 NM BS 560-620 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR 0294 AND 013, FORWARD CARGO DOOR NR 2 FROM TOP TRANSVERSE BEAM IS CRACKED. *S/D* REMOVED AND REPLACED FWD CARGO DOO R NR 2 FROM TOP TRANSVERSE BEAM PER FEDEX SRM 51-10-1, 51-3-02. 2 L 7 3 4F A3WE 1996091200903 19960912 00903 NM 1996 9 12 96FDEA01453 1 19960909 A 5230 651862015 ANGLE BOEING 727 72725 1384006 NM BS 560-620 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR 0295 AND 014, FORWARD CARGO DOOR NR 3 L-ANGLE FROM TOP IS CRACKED. 2 L 7 3 4F A3WE 1996091200904 19960912 00904 NM 1996 9 12 96FDEA01454 1 19960909 A 5230 651862026 ANGLE BOEING 727 72725 1384006 NM BS 560-620 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR 0296 AND 015, FORWARD CARGO DOOR NR 5 L-ANGLE FROM TOP IS CRACKED. *S/D* REMOVED AND REPLACED FWD CARGO DOOR NR 5 L T, ANGLE PER FEDEX SRM 51-10-1, 53-30-2. 2 L 7 3 4F A3WE 1996091200905 19960912 00905 WP 1996 9 12 SCNA96245 1 19960903 A 2611 PU90499R3 SMOKE DETECTOR DOUG DC10 DC1015 3022118 WP AFT LAVATORY INOPERATIVE A SCNA K NONE N FALSE WARNING IN INSP/MAINT 1 GL 15 151SY 48295 AFT LAV-E SMOKE DETECTOR ON CONTINUOUSLY. REMOVED AND REPLACED SMOKE DETECTOR, OPS CHECKED NORMAL. 2 L 7 3 4F A22WE 1996091200906 19960912 00906 WP 1996 9 12 SCNA96246 1 19960906 A 2611 13131 SMOKE DETECTOR DOUG DC10 DC1010 3022110 WP CARGO COMPT INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 573SC 46905 THE SECOND LIGHT ON THE SMOKE DETECTOR PANEL WOULD NOT TEST. PLACED SMOKE DETECTOR ON MEL 26-15A. 2 L 7 3 4F A22WE 1996091200907 19960912 00907 WP 1996 9 12 SCNA96247 1 19960907 A 2611 13131 SMOKE DETECTOR DOUG DC10 DC1030F 3023504 WP CARGO COMPT INOPERATIVE A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 603GC 47922 DURING LINE CHECK, NUMBER 3 LOWER AFT CARGO SMOKE DETECTOR DID NOT TEST. RELAMPED AND TESTED NORMAL. 2 L 7 3 4F RT A22WE 1996091200908 19960912 00908 NM 1996 9 12 VSTA9609001 1 19960907 A 5754 65162251 SKIN BOEING 727 727243 138408D NM LT LE FLAP DAMAGED A VSTA K NONE O OTHER IN INSP/MAINT 1 WP 07 521DB 21266 AEROSERVICES PORTABLE ENTRY STAND LOCATED AT FWD ENTRY DOOR ROLLED INTO NR 3 LEADING EDGE FLAP DURING HELICOPTER LAUNCHE S CAUSING 4 CRACK INFLAP. REMOVED AND REPLACED NR 3 FLAP IAW MM 27-81-1. 2 L 7 3 4F RT A3WE 1996091200909 19960912 00909 WP 1996 9 12 TC8A96058 1 19960909 A 7722 152BCL4P EGT INDICATOR DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3B 52039 NE NR 3 ENGINE FAILED A TC8A K NONE O OTHER TX TAXI/GRND HDL 1 GL 23 181SK 45910 669217 NR 3 ENGINE BETWEEN 360 TO 390 DEGREES EGT DURING IDLE. REPLACED NR 3 ENGINE EGT INDICATOR, OPS CHECKED NORMAL IAW 77-2 0-1. 2 L 7 4 4F 4 F 4A25 1E8 1996091600001 19960916 00001 NE 1996 9 16 CA960111007 3 19960105 A 6111 SFA13N1OA BLADE HAMSTD DHAV DHC8 DHC8311 1386006 EA PWA HAMSTD 14SF 14SF15 NE PROP FAILED NDT TEST W K NONE O OTHER IN INSP/MAINT 1 CA 8977 1233 86806315 900519 (CAN)PROPELLER BLADE FAILED SHEAR WAVE NDT TEST, AS PER SERVICE BULLETIN 14SF-61-A95. 2 H 7 2 4T RT A13NM 6 C P7NE 1996091600002 19960916 00002 NE 1996 9 16 CA960111008 3 19960110 A 6111 SFA13N1OA PROPELLER BLADE HAMSTD DHAV DHC8 DHC8311 1386006 EA HAMSTD 14SF 14SF15 NE NR 3 BLADE FAILED NDT TEST W K NONE O OTHER IN INSP/MAINT 1 CA 8962 1218 86806215 910106 (CAN)#3 BLADE #1 PROPELLER FAILED SHEAR WAVE NDT TEST, AS PER SERVICE BULLETIN 14SF-61-A95. 2 H 7 2 4T RT A13NM 6 C P7NE 1996091600003 19960916 00003 NE 1996 9 16 CA960111009 3 19960110 A 6111 SFA13N1OA BLADE HAMSTD DHAV DHC8 DHC8311 1386006 EA PWA HAMSTD 14SF 14SF15 NE NR1 BLADE FAILED NDT TEST W K NONE O OTHER IN INSP/MAINT 1 CA 5105 86857215 910106 (CAN)#1 BLADE #2 PROPELLER FAILED SHEAR WAVE NDT TEST, AS PER SERVICE BULLETIN 14SF-61-A95. 2 H 7 2 4T RT A13NM 6 C P7NE 1996091600004 19960916 00004 NE 1996 9 16 CA960111010 3 19960110 A 6111 SFA13N1OA BLADE HAMSTD DHAV DHC8 DHC8311 1386006 EA HAMSTD 14SF 14SF15 NE NR 1 BLADE FAILED NDT TEST W K NONE O OTHER IN INSP/MAINT 1 CA 9480 3481 86903115 901009 (CAN)#1 BLADE #2 PROPELLER FAILED SHEAR WAVE NDT TEST, AS PER SERVICE BULLETIN 14SF-16-A95. 2 H 7 2 4T RT A13NM 6 C P7NE 1996091600005 19960916 00005 NE 1996 9 16 CA960111011 3 19960110 A 6111 SFA13N1OA BLADE HAMSTD DHAV DHC8 DHC8311 1386006 EA PWA HAMSTD 14SF 14SF15 NE NR 4 BLADE FAILED NDT TEST W K NONE O OTHER IN INSP/MAINT 1 CA 3948 3481 86947015 901009 (CAN)#4 BLADE #2 PROPELLER FAILED SHEAR WAVE NDT TEST, AS PER SERVICE BULLETIN 14SF-61-A95. 2 H 7 2 4T RT A13NM 6 C P7NE 1996091600006 19960916 00006 NE 1996 9 16 DLL12961981 2 19960827 A 7260 M06592AA GEARBOX LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB211524B402 54555 NE NR 1 ENGINE SEIZED A DALA E ENGINE SHUTDOWN X ENGINE FLAMEOUT CL CLIMB 1 SO 27 724DA 193C1151 14741 ENG NR 1 FLAME-OUT ON CLIMBOUT. NO INDICATION OF FIRE. COMPLIED WITH POM, NO RELIGHT ATTEMPTED. ENG INDICATED WIND MI LL ON N1, N2, N3, NO OIL PRESS INDICATED. QTY AND TEMP WAS GOOD. REPLACED 06 GEARBOX, LEAK AND OPS CHECK NORMAL. 2 L 7 3 4F 4 F A23WE E12EU 1996091900003 19960919 00003 WP 1996 9 19 HAL9695 1 19960720 A 3231 DOOR LATCH DOUG DC9 DC951 3022051 WP RT MLG BROKEN SPRING A HALA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 EICBI 48122 HNL - FLT 528 - RIGHT MAIN GEAR UNSAFE LIGHT CAME ON AND GEAR DOOR OPEN LIGHT CAME ON DURING UPLATCH CHECK. (AFTER LAND ING OGG.) FOUND DOOR LATCH SPRING BROKEN, REPLACED DOOR LATCH SPRING. (X) 2 L 7 2 4F A6WE 1996091900004 19960919 00004 1996 9 19 HEEA967695 4 19960829 A 3452 066106200 TRANSCEIVER KT76 BOLKMS 117 BK117A4 5626017 EU COCKPIT ATC INTERMITTENT E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 911RZ 7092 INTERMITTENT AS PER TOWER. REPLACED DEFECTIVE CR202 MIXER DIODE AND WEAK V101 CAVITY OSCILLATOR. ADJUSTED POWER AND FRE QUENCY TO SPECS. BENCH CHECK GOOD. 1 G 7 2 3U H13EU 1996091900086 19960919 00086 1996 9 19 CALA9601298 4 19960910 A 3444 92274473 RELAY DOUG DC9 DC932 3022066 WP LG LEVER CRACKED A A CALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SW 09 43537 47112 THE AIRCRAFT HAD A HISTORY OF THE GPWS GIVING A TOO LOW GEAR WARNING AT LOW ALTITUDES DURING LANDING, WHICH RESULTED IN TWO INSTANCES OF A GO-AROUND. THE WARNING WAS ACCOMPANIED BY DIM LOWER HALF OF GREEN DOWN AND LOCKED LIGHTS. TROUBLESH OOTING BY MAINTENANCE FOUND A LOOSE TERMINAL AT X-1 ON R2-1 LANDING GEAR LEVER RELAY AND THE RELAY WAS CRACKED. THE REL AY WAS REPLACED. THE TERMINAL ON RT MLG LOWER GREEN LIGHT WAS ALSO TIGHTENED. ALL OPERATION CHECKED NORMAL. 2 L 7 2 4F A6WE 1996091900087 19960919 00087 NM 1996 9 19 CALA9601299 1 19960823 A 5743 69149381 FLANGE BOEING 727 727224 1384076 NM LT MLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND COLLAR CRACKED THROUGH LOCKING BOLT HOLE AT PIN BETWEEN INBOARD END OF GEAR BEAM AND H-LINK IN LT WHEEL WELL AREA. THE PIN RETAINER FLANGE WAS REMOVED AND REPLACED IAW SRM 57-40-0. 2 L 7 3 4F A3WE 1996091900088 19960919 00088 WP 1996 9 19 CALA9601300 1 19960812 A 5350 CLIPS DOUG DC9 DC982 3022082 WP TAILCONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14840 49580 THE TAILCONE EXTERIOR RELEASE HANDLE PULLED TOO LIGHT OUT OF CLIPS. THE EXTERIOR HANDLE CLIPS WERE ADJUSTED PER MM 53-5 3-00. 2 L 7 2 4F A6WE 1996091900089 19960919 00089 WP 1996 9 19 CALA9601301 1 19960816 A 5350 CABLES DOUG DC9 DC982 3022082 WP TAILCONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14840 49580 THE TAILCONE WOULD NOT DROP WHEN RELEASE HANDLE WAS PULLED. THE TAILCONE CABLES WERE RIGGED IAW MM 53-53-00. 2 L 7 2 4F A6WE 1996091900090 19960919 00090 NM 1996 9 19 CALA9601302 1 19960904 A 5320 ANGLE BOEING 737 7373T0 1384582 NM BS 540 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69348 23586 INSPECTION FOUND A 1 INCH CRACK IN ANGLE AT STA 540, STRINGER 22R. THE CRACKED AREA WAS CUT OUT AND A REPAIR WAS INSTAL LED IAW SRM 51-70-11. 2 L 7 2 4F RT A16WE 1996091900091 19960919 00091 EU 1996 9 19 99619473246 1 19960910 A 3260 TARGET AIRBUS 320 A320211 3930320 EU RT MLG DOOR LOOSE A NWAA A O UNSCHED LANDING OTHER P NO WARNING INDICATION CL CLIMB 1 GL 01 346NW 400 DURING CLIMB-OUT AFTER LANDING GEAR RETRACTION, THE RIGHT MAIN LANDING GEAR DOOR DID NOT INDICATE CLOSED. CYCLED LANDIN G GEAR HANDLE WITH NO CHANGE IN INDICATION. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND TH E RIGHT MAIN LANDING GEAR DOOR UPLOCK PROXIMITY SENSOR TARGET LOOSE. THE TARGET LOCKING PLATE WAS REPLACED AND THE TARGE T TIGHTENED. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996091900092 19960919 00092 EU 1996 9 19 9619483246 1 19960909 A 3260 INDICATION AIRBUS 320 A320211 3930320 EU RT MLG DOOR MALFUNCTIONED A NWAA O OTHER N FALSE WARNING UK UNKNOWN 1 GL 01 346NW 400 RECEIVED L/G DOORS NOT CLOSED MESSAGE WITH THE RIGHT MAIN LANDING GEAR DOOR INDICATION ILLUMINATED AMBER. CYCLED LANDIN G GEAR HANDLE WITH NO CHANGE INDICATION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING REVEALED NO DIS CREPANCIES. RESEATED NR 1 AND NR 2 LANDING GEAR CONTROL INTERFACE UNITS. 2 L 7 2 4F RT A28NM 1996091900093 19960919 00093 WP 1996 9 19 9619499946 1 19960907 A 2150 AIR CYCLE MACH DOUG DC9 DC931 3022065 WP RIGHT OVERSERVICED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 8926E 45863 FLIGHT ATTENDANT REPORTED HAZE AND SMOKE IN CABIN AFTER TAKEOFF. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. M AINTENANCE FOUND RIGHT AIR CYCLE MACHINE OVERSERVICED. DRAINED OIL TO PROPER LEVEL. ALSO CHANGED COALESCER BAGS. OPER ATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996091900094 19960919 00094 WP 1996 9 19 9619509951 1 19960907 A 3260 IND SWITCH DOUG DC9 DC932 3022066 WP NLG MALFUNCTIONED A NWAA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 01 9347 45827 DURING APPROACH INTO MSP, NOSE LANDING GEAR GREEN DOWNLOCK LIGHT DID NOT ILLUMINATE AFTER GEAR WAS EXTENDED. RECYCLED G EAR AND NORMAL INDICATIONS WERE ACHIEVED. MAINTENANCE REPLACED NOSE LANDING GEAR INDICATION SWITCH AND RELAMPED INDICAT OR. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996091900095 19960919 00095 WP 1996 9 19 9619519604 1 19960909 A 3232 ACTUATOR DOUG DC9 DC932 3022066 WP RT NLG DOOR LOOSE A NWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 01 604NC 47222 VIBRATION FROM NOSE GEAR AREA OCCURRED ON GEAR RETRACTION AFTER TAKEOFF. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCI DENT. MAINTENANCE FOUND RIGHT NOSE GEAR DOOR OPEN AND ACTUATOR LOOSE. REPLACED ACTUATOR. OPERATIONAL CHECK NORMAL. A IRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996091900096 19960919 00096 WP 1996 9 19 9919529913 1 19960909 A 2133 OUT FLOW VALVE DOUG DC9 DC931 3022065 WP CABIN MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 963N 47415 AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED OUTFLOW VALVE ACTUATOR AND CABIN DIFFERENTIAL PRESSURE SENSOR. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996091900097 19960919 00097 WP 1996 9 19 9619539608 1 19960905 A 3397 WIRE DOUG DC9 DC932 3022066 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 908NW 47233 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS AT SEAT 1C INOPERATIVE. REPAIRED BROKEN WIRE . OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996091900098 19960919 00098 WP 1996 9 19 9619549613 1 19960907 A 3350 SWITCH DOUG DC9 DC932 3022066 WP COCKPIT FAILED A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 615NW 47438 FLOOR PROXIMITY EMERGENCY LIGHTS FLASHED OFF AND ON DURING LANDING. REPLACED COCKPIT OVERHEAD EMERGENCY LIGHT TOGGLE SW ITCH. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996091900099 19960919 00099 NM 1996 9 19 9619555636 1 19960907 A 2120 AIR DISTR BOEING 757 757251 1384970 NM CABIN ODOR A NWAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 01 536US 26483 AIRCRAFT RETURNED TO GATE AFTER FLIGHT ATTENDANT REPORTED HOT ELECTRICAL ODOR AND HAZY APPEARANCE IN CABIN FROM ROW 31 B ACK. MAINTENANCE CHECKED AFT GALLEY AND LAVATORIES. RAN APU AND ENGINES, NO FAULTS NOTED AND NO HAZE OR ELECTRICAL ODOR NOTED IN CABIN. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F RT A2NM 1996091900100 19960919 00100 NM 1996 9 19 9619562299 1 19960906 A 2781 INDICATION BOEING 727 727251 138408H NM LE FLAPS MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK P NO WARNING INDICATION TO TAKEOFF 1 GL 01 299US 22153 ON TAKEOFF ROLL, THE AIRCRAFT HAD NO BLUE LIGHT ON FORWARD PANEL WITH SLATS EXTENDED. TAKEOFF WAS ABORTED WITHOUT INCID ENT. AIRCRAFT RETURNED TO GATE. PLACARDED LEADING EDGE FLAP INDICATOR INOPERATIVE ON INSTRUMENT PANEL PER MEL. CYCLED FLAPS SEVERAL TIMES. ALL INDICATIONS WERE NORMAL. 2 L 7 3 4F A3WE 1996091900101 19960919 00101 EU 1996 9 19 9619663203 1 19960909 A 5270 SWITCH AIRBUS 320 A320211 3930320 EU CARGO DOOR DIRTY A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 303US 34 PHL/DTW - DURING TAKEOFF ROLL AT 50 KNOTS, RECEIVED AN AFT CARGO DOOR WARNING INDICATION. ABORTED TAKEOFF WITHOUT FURTH ER INDICATION. INSPECTED THE AFT CARGO DOOR LINKAGE. CHECKED OK. CLEANED THE DOOR WARNING PROXIMITY SWITCH. OPERATIO NAL CHECK OK. 2 L 7 2 4F RT A28NM 1996091900102 19960919 00102 EU 1996 9 19 9619673239 1 19960911 A 5270 COVER AIRBUS 320 A320212 EU LT EMER EXIT OUT OF ADJUST A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 339NW 367 MSP/MEM - DURING TAKEOFF AT 80 KNOTS, RECEIVED AN OVERWING EMERGENCY EXIT DOOR WARNING INDICATION. ABORTED TAKEOFF WITH OUT FURTHER INCIDENT. ADJUSTED THE LATCH ON THE LEFT AFT OVERWING EMERGENCY EXIT HANDLE COVER. ALSO INSPECTED THE DOOR INTERIOR AND EXTERIOR SURFACES. NO TROUBLE FOUND. 2 L 7 2 4F RT A28NM 1996091900103 19960919 00103 WP 1996 9 19 9619719957 1 19960908 A 2751 GROUND WIRE DOUG DC9 DC931 3022065 WP RT FLAP POS IND LOOSE A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 915RW 47139 STALL INDICATION FAILURE LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENA NCE FOUND BAD GROUND IN RIGHT FLAP POSITION INDICATOR WIRING. REPAIRED WIRING. ADJUSTED RIGHT TRANSMITTER. OPERATIONA L CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996091900104 19960919 00104 NM 1996 9 19 9619682275 1 19960909 A 8012 STARTER DUCT BOEING 727 727251 138408H NM NR 1 ENGINE FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 GL 01 275US 21154 ON TAKEOFF, THE NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. RE PLACED STARTER DUCT. ENGINE RUN PERFORMED. CHECKED OK. 2 L 7 3 4F A3WE 1996091900105 19960919 00105 WP 1996 9 19 9619699613 1 19960910 A 3350 SWITCH DOUG DC9 DC932 3022066 WP CABIN MALFUNCTIONED A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 613NW 47438 DURING FLIGHT, THE FLOOR PROXIMITY EMERGENCY LIGHTS IN MAIN CABIN FLICKERED ON AND OFF. REPLACED FLIGHT ATTENDANT EMERG ENCY LIGHT SWITCH. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996091900106 19960919 00106 WP 1996 9 19 9619709980 1 19960910 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9344 47440 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN POW ER SUPPLY. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996091900107 19960919 00107 WP 1996 9 19 9619571162 1 19960828 A 5320 DOOR JAMB DOUG DC10 DC1040 3023508 WP NR 3R DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 162US 46771 DURING T-CHECK, FOUND A CRACK IN THE NR 3R DOOR JAMB WEB, LOWER FORWARD CORNER. REPAIRED WEB (P/N AEA 0115-2) PER EA 11 -105144. 2 L 7 3 4F A22WE 1996091900108 19960919 00108 WP 1996 9 19 9619581162 1 19960828 A 5311 FRAME DOUG DC10 DC1040 3023508 WP BS 547 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 162US 46771 DURING T-CHECK, FOUND A .75 INCH CRACK IN THE LEFT FORWARD ACCESSORY COMPARTMENT DOOR JAMB FS 547 FRAME INBOARD CHORD. REPAIRED FRAME (P/N ACA 0051-3) PER EA 11-106313. 2 L 7 3 4F A22WE 1996091900109 19960919 00109 NM 1996 9 19 9619595515 1 19960830 A 5315 FLOOR BEAM BOEING 757 757251 1384970 NM BS 345 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 515US 23203 DURING P-CHECK, FOUND CORROSION ON THE BS 345 FLOOR BEAM UPPER CHORD AT LBL 16 AND RBL 35. REPAIRED CHORD (P/N 141N5111 ) PER EA 55-106254, -106256. 2 L 7 2 4F RT A2NM 1996091900110 19960919 00110 WP 1996 9 19 9619601162 1 19960831 A 5313 LONGERON DOUG DC10 DC1040 3023508 WP BS 1407-1548 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 162US 46771 DURING T-CHECK, FOUND CORROSION ON THE FUSELAGE OVERWING EXTERNAL LONGERONS 30L, 32L, 37L, AND 32R FROM FS 1407 - FS 154 8. REPAIRED LONGERONS PER EA 11-110189. 2 L 7 3 4F A22WE 1996091900111 19960919 00111 WP 1996 9 19 9619619933 1 19960908 A 5230 FITTING DOUG DC9 DC931 3022065 WP CARGO DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 1334U 47280 DURING H-CHECK, FOUND A CRACK IN THE AFT CARGO DOOR LOWER BEAM FORWARD END FITTING. REPLACED FITTING. 2 L 7 2 4F A6WE 1996091900112 19960919 00112 WP 1996 9 19 9619629912 1 19960908 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 579 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 962N 47406 DURING M-CHECK, FOUND A 6 INCH CRACK IN THE LONGERON 30 END FITTING AT FS 579. REPLACED FITTING (P/N 5920331-1) PER SRM 'S 51-30-2, 51-30-5. 2 L 7 2 4F A6WE 1996091900113 19960919 00113 WP 1996 9 19 9619639933 1 19960908 A 5312 BLKHD FITTING DOUG DC9 DC931 3022065 WP BS 756 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 1334U 47280 DURING H-CHECK, FOUND A CRACK IN THE LEFT KEEL TO BULKHEAD ATTACH FITTING FS 756. REPLACED FITTING (P/N 3915135-505N) P ER SRM 51-30. 2 L 7 2 4F A6WE 1996091900114 19960919 00114 WP 1996 9 19 9619649180 1 19960909 A 5320 SUPPORT CASTING DOUG DC9 DC914 3022034 WP BS 560 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3312L 45707 DURING H-CHECK, FOUND A CRACK IN THE RIGHT OUTBOARD SEAT TRACK SUPPORT CASTING AT FS 560. REPLACED CASTING PER SRM 51 -30-5. 2 L 7 2 4F A6WE 1996091900115 19960919 00115 WP 1996 9 19 9619659180 1 19960910 A 5320 FITTING DOUG DC9 DC914 3022034 WP BS 820 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3312L 45707 DURING H-CHECK, FOUND CORROSION ON THE LONGERON 24L END FITTING AT FS 820. REPLACED FITTING (P/N 3914590-501) PER SRM'S 51-30-2, 51-30-5. 2 L 7 2 4F A6WE 1996091900116 19960919 00116 SO 1996 9 19 COMA9610277 1 19960910 A 6120 M610628023 RELAY EMB 120 EMB120RT SO AUTO FEATHER FAILED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 249CA 120230 AUTOFEATHER AURAL WARNING SOUNDED DURING TAKEOFF. REPLACED RELAY K0039. 2 L 7 2 4T RT A31SO 1996091900117 19960919 00117 NM 1996 9 19 UPS96221080 1 19960909 A 5311 FRAME BOEING 727 7272A1 138407F NM BS 681 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE: C. CORROSION OF AFT SIDE LOWER FLOOR BEAM FLANGE AT STA 681 LBL 5 TO RBL 5 WL 149. REMOVED CORROSION FOUND OUT OF LIMITS PER SRM 53-10-1, CUT OUT DAMAGE AND REPAIRED PER SRM'S 53-10-4, 51-30-2, 51-10-4. 2 L 7 3 4F A3WE 1996091900118 19960919 00118 NM 1996 9 19 UPS96221081 1 19960910 A 5311 FRAME BOEING 727 7272A1 138407F NM BS 1166 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE: C. CORROSION ON SHEAR TIE AND FRAME AT STA 1166 LBL 2 WL 150. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. CUT OUT DAMAGE, FABRICATED REPAIR PARTS AND REPAIRED PER SRM 51-40-3. 2 L 7 3 4F A3WE 1996091900119 19960919 00119 NM 1996 9 19 UPS96221082 1 19960910 A 5311 FRAME BOEING 727 7272A1 138407F NM BS 321 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE: C. LEFT HAND INBOARD DOGHOUSE FRAME CRACKED AT STA 321 WL 169 LBL 25. STOP DRILLED CRACK AND REPAIRE D PER SRM 51-40-02. 2 L 7 3 4F A3WE 1996091900120 19960919 00120 NM 1996 9 19 UPS96221083 1 19960909 A 5320 69448241 FITTING BOEING 727 7272A1 138407F NM BS 588 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE: C. CORROSION ON FITTING AT STA 558 RBL 23 WL 155. REMOVED CORRODED FITTING AND INSTALLED NEW FITTING . ALL WORK DONE IAW SRM'S 53-10-1, 51-10-6, AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996091900121 19960919 00121 NM 1996 9 19 UPS96221084 1 19960909 A 5720 651620054 STIFFENER BOEING 727 7272A1 138407F NM BS 257.85 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE: C. CORROSION ON RIGHT WING STATION 257.85. FRONT SPAR STIFFENER IS CORRODED ON I/B UPPER END. REMOV ED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 57-10-1, REMOVED STIFFENER AND INSTALLED NEW STIFFENER PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996091900122 19960919 00122 NM 1996 9 19 UPS96221085 1 19960910 A 5320 651986219 CHORD BOEING 727 7272A1 138407F NM BS 296 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE: C. CORROSION ON NOSE LANDING GEAR WHEELWELL MID-CHORD AT BS 296 LBL 15 WL 169. CORROSION FOUND TO BE THROUGH 100 PERCENT OF TOTAL THICKNESS, REMOVED AND REPLACED LT MID-CHORD IAW SRM'S 51-10-1, 51-30-5, AND MM 51-30-00-5 1-20-13 AND 51-20-01. 2 L 7 3 4F A3WE 1996091900123 19960919 00123 NM 1996 9 19 UPS96221086 1 19960911 A 5751 6521773501 FITTING BOEING 727 7272A1 138407F NM LT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE: C. L/W I/B AILERON TAB HINGE FITTINGS ARE CORRODED AILERON SIDE. REMOVED AND REPLACED L/W I/B AILER ON TAB HINGE FITTINGS PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996091900124 19960919 00124 NM 1996 9 19 UPS96221087 1 19960906 A 5311 FRAME BOEING 727 7272A1 138407F NM BS 1273/1263 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE: C. CRACKED FRAME AT BS 1273 RBL 21 WL 194. REPAIRED IN ACCORDANCE WITH B727-5310-1239-E. NOTE: A DDITIONAL CRACKED FRAME AT BS 1263 RBL 21 WL 194 WAS ALSO REPAIRED ON THIS NRC. 2 L 7 3 4F A3WE 1996091900125 19960919 00125 NM 1996 9 19 UPS96221088 1 19960911 A 5711 651620050 STIFFENER BOEING 727 7272A1 138407F NM RT WING FWD SPAR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE: C. CORROSION AT RWS 245.0 FRONT SPAR STIFFENER ON UPPER O/B END. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 57-10-01, REMOVED STIFFENER AND INSTALLED NEW STIFFENER PER SRM'S 51-30-5, 51-30-2, MM 28-11-00. 2 L 7 3 4F A3WE 1996091900126 19960919 00126 NM 1996 9 19 UPS96221090 1 19960910 A 5755 651734863 RIB BOEING 727 7272A1 138407F NM NR 9 SPOILER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE: C. NR 9 SPOILER OUTBOARD CLOSURE RIB IS CORRODED. FOUND DAMAGE TO BE BEYOND ECONOMICAL REPAIR. PART WAS REPLACED IAW- MM 27-620. 2 L 7 3 4F A3WE 1996091900127 19960919 00127 NM 1996 9 19 UPS96221091 1 19960909 A 5320 655784813 FITTING BOEING 727 7272A1 138407F NM BS 540 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE: C. CORROSION ON CARGO TIE DOWN AT STATION 540 RBL 23 WL 156. REMOVED CORRODED CARGO TIE-DOWN FITTING AND INSTALLED NEW CARGO TIE-DOWN FITTING. ALL WORK DONE IAW SRM'S 53-10-1, 51-30-2. 2 L 7 3 4F A3WE 1996091900128 19960919 00128 NM 1996 9 19 UPS96221092 1 19960909 A 5320 65575539 FITTING BOEING 727 7272A1 138407F NM BS 622 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE: C. CORROSION ON CARGO TIE-DOWN SUPPORT UNDER WEB STA 622 RBL 20-22 WL 155. CORROSION REWORK OUT OF L IMITS IAW SRM 53-10-1, REPLACED TIE-DOWN FITTING AT STATION 622 RBL 21 IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996091900129 19960919 00129 NM 1996 9 19 UPS96221093 1 19960909 A 5753 SKIN BOEING 727 7272A1 138407F NM LT TE AFT FLAP DELAMINATION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE: C. AREA OF DELAMINATION ON LEFT WING I/B AFT FLAP UPPER SKIN 64 INCHES I/B OF OUTBOARD END OF FLAP AN D 14 INCHES FORWARD OF TRAILING EDGE. REPAIRED LT WING I/B AFT FLAP UPPER SKIN. ALL WORK DONE IAW SRM 51-40-6. 2 L 7 3 4F A3WE 1996091900130 19960919 00130 NM 1996 9 19 UPS96221094 1 19960909 A 5720 651620054 STIFFENER BOEING 727 7272A1 138407F NM WS 257.85 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE: C. CORROSION, RIGHT WING STATION 257.85. FRONT SPAR STIFFENER IS CORRODED ON I/B UPPER END. REMOVED CORRODED STIFFENER AND INSTALLED NEW STIFFENER. ALL WORK DONE IAW SRM 51-30-2, SRM 57-10-1, AND MM 28-11-00. 2 L 7 3 4F A3WE 1996091900131 19960919 00131 WP 1996 9 19 UPS96821089 1 19960912 A 5510 STABILIZER DOUG DC8 DC873F 302199F WP LT HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 ON PRED. CHK FOUND 2 DENTS ON LEFT STAB L/E. DENT THAT IS APPROX. 46 INCHES OUT FROM STAB L/E ROOT AND HAS 2.6258 INCH CRACK. DENT INBOARD OF PREVIOUS MENTIONED IS 6 INCHES BY 2.50 INCHES. REMOVED DAMAGED L/E SKIN PER SRM 55-2-1. FABRIC ATED DOUBLERS FROM 7075-T6 050, INSTALLED INBOARD DOUBLER DC8-5510-7652A AND SRM 55-2-1. 2 L 7 4 4F RT 4A25 1996091900132 19960919 00132 EU 1996 9 19 QXEA9600371 1 19960910 A 5320 CLIP FOKKER F28 F28MK1000 4990808 EU AFT PRESS BLKHD CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 450US 11101 PDX - LOWER FRAME CLIP CRACK NOTED DURING SIP 53-10-06/1B. CRACK NOTED DURING C-CHECK (NR 100-23). CRACK REPAIRED I/A/ W SRM 530218. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996091900133 19960919 00133 EU 1996 9 19 QXEA9600372 1 19960910 A 5312 BLKHD BEAM FOKKER F28 F28MK1000 4990808 EU FWD PRESS BLKHD CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 450US 37114 11101 PDX - CRACK NOTED IN THE FORWARD PRESSURE BULKHEAD BEAM V, CRACK RUNS BETWEEN TWO FASTENERS AT THE BULKHEAD CENTERLINE. CRACK NOTED DURING C-CHECK (NR 100-33). CRACK REPAIRED I/A/W E.A. 28-53-393. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996091900134 19960919 00134 EU 1996 9 19 QXEA9600373 1 19960910 A 5312 BLKHD BEAM FOKKER F28 F28MK1000 4990808 EU FWD PRESS BLKHD CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 450US 11101 PDX - CRACK IN FORWARD PRESSURE BULKHEAD HORIZONTAL BEAM VII UPPER FLANGE AT THE BULKHEAD CENTERLINE. CRACK NOTED DURIN G C-CHECK (NR 100-34). CRACK REPAIRED I/A/W SRM 530218. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996091900135 19960919 00135 EU 1996 9 19 QXEA9600374 1 19960910 A 5312 BLKHD BEAM FOKKER F28 F28MK1000 4990808 EU FWD PRESS BLKHD CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 450US 37114 11101 PDX - WEB PLATE ON THE AFT SIDE OF THE FORWARD PRESSURE BULKHEAD HAS 3 CRACKS ALONG BEAM 1, APPROXIMATELY ONE INCH RIGHT OF CENTER. CRACKS NOTED DURING C-CHECK (NR 100-44). CRACKS REPAIRED I/A/W SRM 530218. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996091900136 19960919 00136 EU 1996 9 19 QXEA9600375 1 19960910 A 5312 BLKHD WEB FOKKER F28 F28MK1000 4990808 EU FWD PRESS BLKHD CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 450US 37114 11101 PDX - WEB PLATE ON THE AFT SIDE OF FRONT PRESSURE BULKHEAD, LEFT OF CENTER ON BEAM 2 IS CRACKED. CRACKED NOTED DURING C -CHECK (NR 100-45). CRACK REPAIRED I/A/W SRM 530218. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996091900137 19960919 00137 EU 1996 9 19 QXEA9600376 1 19960910 A 5312 BLKHD WEB FOKKER F28 F28MK1000 4990808 EU FWD PRESS BLKHD CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 450US 37114 11101 PDX - WEB PLATE ON THE AFT SIDE OF THE FORWARD PRESSURE BULKHEAD IS CRACKED ON BEAM 2 JUST RIGHT OF CENTER. CRACK NOTED DURING C-CHECK. CRACK REPAIRED I/A/W SRM 530218. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996091900138 19960919 00138 EU 1996 9 19 QXEA9600377 1 19960910 A 5312 BLKHD BEAM FOKKER F28 F28MK1000 4990808 EU REAR PRESS BLKHD CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 450US 37114 11101 PDX - REAR PRESSURE BULKHEAD BELOW CABIN FLOOR, AFT CARGO BAY CRACKS NOTED IN TOP RADIUS OF HORIZONTAL BEAM 2. CRACKS L OCATED OUTBOARD OF VERTICAL BEAM BL 425R 6.5 INCHES TO 9 INCHES IN LENGTH. CRACKS NOTED DURING C-CHECK (NR 290-258). C RACKS REPAIRED I/A/W SRM 530218. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996091900139 19960919 00139 EU 1996 9 19 QXEA9600378 1 19960910 A 5230 SKIN A33251409 FOKKER F28 F28MK1000 4990808 EU AFT CARGO DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 450US 11101 PDX - AFT CARGO DOOR EXTERIOR SKIN HAS CORROSION ON THE INSIDE OF THE DOOR SKIN WHICH EXCEEDS F28 SRM LIMITS. 1.5 INCH BY 1.5 INCH AREA 19 INCHES FROM BOTTOM OF DOOR, 5 INCHES AFT OF FORWARD EDGE. CORRSION NOTED DURING C-CHECK (NR 290-331 ). REPAIR DOUBLER INSTALLED I/A/W E.A. 28-52-121. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996091900140 19960919 00140 EU 1996 9 19 QXEA9600379 1 19960910 A 5320 CLIP FOKKER F28 F28MK1000 4990808 EU FRAME 5305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 450US 37114 11101 PDX - FRAME CLIP CRACKED AT FRAME 5305 AND STRINGERS 1 AND 66. CRACKS NOTED DURING C-CHECK (NR 200-124-129). CRACKS RE PAIRED I/A/W SRM 530213. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996091900141 19960919 00141 EU 1996 9 19 QXEA9600380 1 19960910 A 5320 CLIP FOKKER F28 F28MK1000 4990808 EU FRAME 5805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 450US 37114 11101 PDX - FRAME CLIP CRACKED AT FRAME 5805 AND STRINGERS 3, 4, 5, AND 6. CRACKS NOTED DURING C-CHECK (NR 200-148-149-150-15 1). CRACKS REPAIRED I/A/W SRM 530213. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996091900142 19960919 00142 EU 1996 9 19 QXEA9600381 1 19960910 A 5320 CLIP FOKKER F28 F28MK1000 4990808 EU FRAME 6305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 450US 37114 11101 PDX - FRAME CLIP CRACKED AT FRAME 6305 AND STRINGERS 1 AND 2. CRACKS NOTED DURING C-CHECK (NR 200-161-162). CRACKS REP AIRED I/A/W SRM 530213. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996091900143 19960919 00143 EU 1996 9 19 QXEA9600382 1 19960910 A 5320 CLIP FOKKER F28 F28MK1000 4990808 EU FRAME 6805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 450US 37114 11101 PDX - FRAME CLIP CRACKED AT FRAME 6805 AND STRINGERS 6, 5, 3, AND 74. CRACKS NOTED DURING C-CHECK (NR 250-176-177-178-1 79). CRACKED REPAIRED I/A/W SRM 530213. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996091900144 19960919 00144 EU 1996 9 19 QXEA9600383 1 19960910 A 5320 CLIP FOKKER F28 F28MK1000 4990808 EU FRAME 7305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 450US 37114 11101 PDX - FRAME CLIP CRACKED AT FRAME 7305 AND STRINGERS 72, 74, 2, 5, AND 8. CRACKED NOTED DURING C-CHECK (NR 250-187-189- 191-193-192). CRACKED REPAIRED I/A/W SRM 530213. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996091900145 19960919 00145 EU 1996 9 19 QXEA9600384 1 19960910 A 5320 CLIP FOKKER F28 F28MK1000 4990808 EU FRAME 7805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 450US 37114 11101 PDX - FRAME CLIP CRACKED AT FRAME 7805 AND STRINGERS 7 AND 74. CRACKED NOTED DURING C-CHECK (NR 250-199-201). CRACKED REPAIRED I/A/W SRM 530213. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996091900146 19960919 00146 EU 1996 9 19 QXEA9600385 1 19960910 A 5320 CLIP FOKKER F28 F28MK1000 4990808 EU FRAME 8305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 450US 37114 11101 PDX - FRAME CLIP CRACKED AT FRAME 8305 AND STRINGERS 72, 71, 67, 66, 65, AND 62. CRACKS NOTED DURING C-CHECK (NR 250-21 0-211-212-213-214-242). CRACKS REPAIRED I/A/W SRM 530213. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996091900147 19960919 00147 EU 1996 9 19 QXEA9600386 1 19960910 A 5320 CLIP FOKKER F28 F28MK1000 4990808 EU FRAME 16060 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 450US 37114 11101 PDX - FRAME CLIP CRACKED AT FRAME 16060 AND STRINGERS 6 AND 1. CRACKS NOTED DURING C-CHECK (NR 250-286-298). CRACKS RE PAIRED I/A/W SRM 530213. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996091900148 19960919 00148 EU 1996 9 19 QXEA9600387 1 19960910 A 5320 CLIP FOKKER F28 F28MK1000 4990808 EU FRAME 14755 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 450US 37114 11101 PDX - FRAME CLIP CRACKED AT FRAME 14755 AND STRINGERS 1, 7, AND 2. CRACKS NOTED DURING C-CHECK (NR 250-301-302-354). C RACKS REPAIRED I/A/W SRM 530213. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1996091900149 19960919 00149 NM 1996 9 19 96FDEA01464 1 19960912 A 5320 6516310 ANGLE BOEING 727 72725 1384006 NM BS 259.5 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 509FE 18280 NR0623 AND 017, CORROSION (C53-100-01-4) ON ANGLE BS 259.5 RBL 14 WL 150 TO 157. *S/D* REMOVED CORROSION ON ANGLE BS 2 59.5 RBL 14 WL 150 TO 157, CLEANED AND TREATED AFFECTED AREA. ALL WORK DONE IAW FEDEX EA 7-5310-31127. 2 L 7 3 4F A3WE 1996091900150 19960919 00150 NM 1996 9 19 96FDEA01465 1 19960904 A 5320 RIVETS BOEING 727 72725C 138400H NM CTR WING BOX POPPED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 167FE 18864 CENTER WING BOX INTERIOR FUEL TANK - POPPED RIVETS (2) AT AFT SPAR UPPER CHORD (STA 865, APPROX) RBL 38. INSTALLED UPP ER CHORD REPAIR PER EA 7-5710-28852. 2 L 7 3 4F A3WE 1996091900151 19960919 00151 NM 1996 9 19 96FDEA01466 1 19960904 A 5315 FLOOR BEAM BOEING 727 72725C 138400H NM BS 344 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 167FE 18864 FLOOR BEAM STA 344 LBL 3-5 ACROSS BEAM TO RBL 19. BEAM HAS EXFOLIATION CORROSION NUMEROUS PLACES. (REF NR 0271 AND 0 272). REMOVED DAMAGED FLOOR BEAM TEE CAP FROM LBL - RBL 64 AND INSTALLED NEW TEE CAP ANGLE. REPAIR PER SRDM SR 27-53- 007 AND USING SRM 51-10-1 FOR CORRECT METAL REPLACEMENT FLOOR BEAM. 2 L 7 3 4F A3WE 1996091900152 19960919 00152 NM 1996 9 19 96UAL900678 1 19960903 A 2621 3490000433 FIRE BOTTTLE HTL/PAC SCIE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CARGO PIT MALFUNCTIONED A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 610UA 21871 CARGO COMPARTMENT FIRE BOTTLE NR 1 INDICATES DISCHARGE. *S/D* THE TEMPERATURE COMPENSATING PRESSURE SWITCH INDICATED A DISCHARGE. THE FIRE BOTTLE WAS REPLACED AND REPRESSURIZED, OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 1996091900153 19960919 00153 NM 1996 9 19 96UAL900679 1 19960903 A 3810 FILL VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE POTABLE WATER NOT CLOSED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 530UA 25043 CREW REPORTED POTABLE WATER QUANTITY DROPPED TO ZERO AFTER TAKEOFF ACCOMPANIED BY AN EXTERNAL AIR NOISE NEXT TO DOOR 2R. FLIGHT DIVERTED TO PIT. INSPECTED AIRCRAFT, FOUND ALL DOORS CLOSED. INSPECTION REVEALED WATER FILL VALVE IN OPEN POS ITION. CLOSED SAME. FLIGHT CONTINUED TO LAX. OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996091900154 19960919 00154 WP 1996 9 19 96UAL900680 1 19960904 A 3350 362624 STRIP DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE CABIN DEFECTIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1857U 46986 DEFECTIVE EEL STRIP AT LAVATORY 2 RIGHT. *S/D* REPAIRED EEL STRIP, OPERATION NORMAL. 2 L 7 3 4F 4 F A22WE E23EA 1996091900155 19960919 00155 WP 1996 9 19 96UAL900681 1 19960904 A 3350 EMSE299A BATTERY PACK DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL FLIGHT DECK DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1841U 46634 EMERGENCY LIGHT TEST FAILED IN FLIGHT DECK. MID-POWER SUPPLY FAULT. *S/D* REPLACED MID BATTERY PACK. 2 L 7 3 4F 4 F A22WE E23EA 1996091900156 19960919 00156 1996 9 19 96UAL900682 4 19960904 A 2565 SEAM AIRCRUISER 24D3005391 DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL DOOR SLIDE SEPARATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 1847U 1148 48263 DURING SHOP OVERHAUL OF SLIDE REMOVED FOR EXPIRATION OF TIME, A FLOOR SEAM UNDER THE SURVIVAL KIT SEPARATED. SCRAPPED U NIT. 2 L 7 3 4F 4 F A22WE E23EA 1996091900157 19960919 00157 1996 9 19 96UAL900683 4 19960904 A 2565 SEAM AIRCRUISER D29835103 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE DOOR SLIDE SEPARATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7254U 17537578 21401 DURING SHOP OVERHAUL OF SLIDE REMOVED FOR EXPIRATION OF TIME, A SEAM SEPARATION OCCURRED. SCRAPPED UNIT. 2 L 7 3 4F 4 F A3WE E2EA 1996091900158 19960919 00158 NE 1996 9 19 96UAL900684 2 19960905 A 7321 PMA ALIDSIGNAL 90454652 BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 4 ENGINE FAILED A UALA A UNSCHED LANDING J X WARNING INDICATION ENGINE FLAMEOUT CR CRUISE 1 WP 29 188UA 1900 26877 724658 AT CRUISE, NR 4 ENGINE LOST THRUST AND FLAMED OUT. JUST PRIOR TO FLAME-OUT, RECEIVED EEC MODE EICAS MESSAGE. PERMANENT MAGNET ALTERNATOR (PMA) FAILED IN BOTH CHANNELS. REPLACED PMA. 2 L 7 4 4F 4 F RT A20WE E24NE 1996091900159 19960919 00159 NE 1996 9 19 96UAL900685 2 19960905 A 7200 ENGINE BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE NR 3 BIRD STRIKE A UALA C D ABORTED TAKEOFF RETURN TO BLOCK C F.O.D. TO TAKEOFF 1 WP 29 165UA 21658 685611 ON TAKEOFF ROLL, HEARD LOUD BANG AND VIBRATION. ABORTED TAKEOFF AT 138 KNOTS. FOUND NR 3 ENGINE INGESTED BIRDS. 2 L 7 4 4F 4 F A20WE E20EA 1996091900161 19960919 00161 1996 9 19 96UAL900687 4 19960906 A 2565 CENTER TUBE BFGOODRICH 7A14381 BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE DOOR SLIDE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 4728U G1353 19925 DURING TIME CONTROLLED OVERHAUL WEAR WAS FOUND IN THE CENTER INFLATION TUBE AND SLIDING SURFACE. PATCHED TUBE AND SLIDI NG SURFACE PER VENDOR MANUAL 2 L 7 4 4F 4 F A20WE E20EA 1996091900162 19960919 00162 NM 1996 9 19 96UAL900688 1 19960906 A 4980 65625954 DUCT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE APU FAILED A UALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 370UA 24539 APU FIRE WARNING LIGHT AND BELL ACTUATED DURING TAXI. CAPTAIN DID NOT USE FIRE BOTTLES, WARNING INDICATORS DEACTIVATED WITH NO SECONDARIES. AIRCRAFT RETURNED TO GATE DEPLANED PASSENGERS. *S/D* THE APU TAILPIPE WAS REMOVED DUE TO GROSS D ISTORTION OF THE INNER LINER. TAILPIPE WAS INSPECTED ENGINEERING AND FOUND TO BE SEVERELY BUCKLED AND INNER LINER RIVET ING HAD FAILED. THIS CAUSED THE FLOW PATH FOR EXHAUST TO BE REDUCED BY 50 PERCENT AND DISTORTED THE MATING FLANGE. HOT GAS CAUSED THE FIRE WARNING. 2 L 7 2 4F 4 F RT A16WE E2GL 1996091900163 19960919 00163 NM 1996 9 19 96UAL900689 1 19960906 A 2781 SENSOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LE FLAPS OUT OF ADJUST A UALA L ABORTED APPROACH N FALSE WARNING LD LANDING 1 WP 29 322UA 23954 ON APPROACH, LEADING EDGE DEVICE SHOWED INTERMEDIATE POSITION. AIRCRAFT WENT AROUND, FOLLOWED CHECKLIST, LIGHT EXTINGUI SHED. DURING SECOND APPROACH SAME SLAT LIGHT AGAIN. LANDED NORMAL WITH 5 KNOTS ADDED TO APPROACH SPEED. *S/D* ADJUS TED THE NR 4 LEADING EDGE SLAT PROXIMITY SENSOR TO ALIGN WITH THE TARGET, CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1996091900164 19960919 00164 WP 1996 9 19 MWEA96435 1 19960903 A 5230 INTERCOSTAL DOUG DC9 DC914 3022034 WP AFT CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 DURING C-CHECK, FOUND AFT CARGO DOOR INTERCOSTAL UNDER LOWER STRAP STOP FITTING IS CRACKED AT LOWER END. MAINTENANCE IN STALLED REPAIR IAW SRM 52-32-0 FIG. 2. RETURNED A/C TO SERVICE. 2 L 7 2 4F A6WE 1996091900165 19960919 00165 WP 1996 9 19 MWEA96436 1 19960903 A 5230 DOOR PAN DOUG DC9 DC914 3022034 WP AFT CARGO CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 DURING C-CHECK, FOUND AFT CARGO DOOR PAN CRACKED ON AFT END IN CENTER NEAR MIDDLE STOP FITTING. MAINTENANCE INSTALLED R EPAIR SRM 52-03 FIG 8. RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996091900166 19960919 00166 WP 1996 9 19 MWEA96437 1 19960904 A 5311 FRAME DOUG DC9 DC914 3022034 WP BS 897 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 DURING C-CHECK, FOUND CRACK AT STA 897 ON FRAME AT LONGERONS 2L AND 2R. INSTALLED DOUBLER REPAIR IAW SRM 53-03, FIG. 32 . 2 L 7 2 4F A6WE 1996091900167 19960919 00167 WP 1996 9 19 MWEA96438 1 19960904 A 5230 DOUBLER DOUG DC9 DC914 3022034 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 DURING C-CHECK, FOUND FORWARD CARGO DOOR DOUBLER CRACKED AROUND THE AFT LOCKING CAM ON INSIDE STRUCTURE OF DOOR. INSTAL LED REPAIR IAW SRM 52-30-0, FIG. 1. 2 L 7 2 4F A6WE 1996091900168 19960919 00168 WP 1996 9 19 MWEA96439 1 19960905 A 5230 DOOR PAN DOUG DC9 DC914 3022034 WP CARGO COMPT CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 DURING C-CHECK, FOUND FORWARD CARGO DOOR PAN CRACKED ON AFT SIDE NEAR NR 5 BEAM ATTACH CLIP. INSTALLED REPAIR IAW SERVI CE REWORK DRAWING 5934104. 2 L 7 2 4F A6WE 1996091900169 19960919 00169 WP 1996 9 19 MWEA96440 1 19960911 A 3350 1001191 LIGHT DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 301ME 47190 DURING SERVICE CHECK, FOUND FORWARD ENTRY EMERGENCY LIGHT DOES NOT ILLUMINATE DURING TEST. REPLACED FORWARD ENTRY EMERG ENCY LIGHT ASSY. OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996091900170 19960919 00170 WP 1996 9 19 MWEA96441 1 19960912 A 5312 S2506869 BLKHD FITTING DOUG DC9 DC932 3022066 WP FWD PRESS BLKHD CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSPECTION, FOUND CABLE ATTACH FITTING EXFOLIATED IN NLG WHEELWELL ON UPPER PRESSURE BULKHEAD. FABRICATED A FITT ING AND INSTALLED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 1996091900171 19960919 00171 WP 1996 9 19 MWEA96442 1 19960912 A 5320 ANGLE DOUG DC9 DC932 3022066 WP FWD ACC COMPT BROKEN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSPECTION, RADAR RT RACK INBD AFT MOUNT BRACKET BROKEN. FABRICATED REPAIR ANGLES IAW SRM 53-01, FIG. 2, SHEET 4 , AND INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1996091900172 19960919 00172 WP 1996 9 19 MWEA96443 1 19960912 A 5313 5911401 LONGERON DOUG DC9 DC932 3022066 WP BS 180 EXFOLIATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSPECTION, LONGERON 30 WAS FOUND EXFOLIATED IN E/E COMPT AT STA 180. MAINTENANCE SPLICED IN A NEW SECTION OF LO NGERON IAW SRM 53-02, FIG. 2. 2 L 7 2 4F A6WE 1996091900173 19960919 00173 WP 1996 9 19 MWEA96444 1 19960912 A 5347 S2772660 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 180-229 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSPECTION, SEAT TRACKS NR 2 AND NR 3 WERE FOUND TO HAVE CORROSION FROM STA 180 TO STA 229. REPAIRED THE SEAT TR ACKS IAW SRM 53-05, FIG. 4D. 2 L 7 2 4F A6WE 1996091900174 19960919 00174 WP 1996 9 19 MWEA96445 1 19960912 A 5315 FLOOR BEAM DOUG DC9 DC932 3022066 WP BS 218 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSPECTION, EXFOLIATION CORROSION WAS FOUND ON A FLOOR BEAM UPPER FLANGE LOWER SURFACE INBD OF SEAT TRACK NR 1 AT STA 218. REPAIRED THE FLOOR BEAM IAW SRM 53-05, FIG. 20A. 2 L 7 2 4F A6WE 1996091900175 19960919 00175 WP 1996 9 19 MWEA96446 1 19960912 A 5755 DOUBLER DOUG DC9 DC932 3022066 WP LT OTBD SPOILER SCRATCHED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSPECTION, LT WING OTBD SPOILER PANEL WAS FOUND TO HAVE A DEEP SCRATCH ON LOWER SURFACE. COMPLETED A REPAIR IAW SRM 51-70-2, PG. 83, PARA C. 2 L 7 2 4F A6WE 1996091900176 19960919 00176 WP 1996 9 19 MWEA96447 1 19960912 A 5753 5914508 FITTING DOUG DC9 DC932 3022066 WP LT TE FLAP CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSPECTION, LT FLAP CENTER HINGE MOUNT INBD FITTING WAS FOUND CRACKED. REPLACED FITTING IAW SRM 57-09, PARA 13, AND DRWG NR 5914508. 2 L 7 2 4F A6WE 1996091900177 19960919 00177 WP 1996 9 19 MWEA96448 1 19960912 A 5711 SPAR CAP DOUG DC9 DC932 3022066 WP LT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSPECTION, LT REAR SPAR CAP LOWER HORIZONTAL LEG WAS FOUND TO HAVE SEVERE EXFOLIATION CORROSION. COMPLETED REPA IR IAW SRM 57-09, FIG. 11. 2 L 7 2 4F A6WE 1996091900178 19960919 00178 WP 1996 9 19 MWEA96449 1 19960912 A 5755 SUPPORT BEAM DOUG DC9 DC932 3022066 WP RT SPOILER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSPECTION, RT WING INBD SPOILER TORSION BAR BEARING UPPER SUPPORT BEAM IS CRACKED AT LOWER END. INSTALLED A NEW SUPPORT BEAM IAW SRM 57-01, PG 1. 2 L 7 2 4F A6WE 1996091900179 19960919 00179 WP 1996 9 19 MWEA96450 1 19960912 A 5280 DOUBLER DOUG DC9 DC932 3022066 WP RT MLG INBD DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSPECTION, THE MLG INBD DOOR OUTER SKIN WAS FOUND CRACKED AT FORWARD EDGE NEAR THE OTBD END, APPROX 1.50 INCHES. FABRICATED AND INSTALLED REPAIR IAW SRM 52-05, FIG. 4, PG 5, AND 51-30. 2 L 7 2 4F A6WE 1996091900180 19960919 00180 WP 1996 9 19 MWEA96451 1 19960912 A 5753 5914508 FITTING DOUG DC9 DC932 3022066 WP RT TE FLAP CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSPECTION, RT FLAP CENTER HINGE MOUNT INBD CASTING WAS FOUND CRACKED IN TWO PLACES ALONG THE BOTTOM FLANGE. REP LACED RT FLAP CENTER HINGE FITTING IAW SRM 57-09, PARA 13, AND DAC DRAWING 5914508. 2 L 7 2 4F A6WE 1996091900181 19960919 00181 WP 1996 9 19 MWEA96452 1 19960912 A 5521 SPAR CAP DOUG DC9 DC932 3022066 WP RT ELEVATOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSPECTION, A 1 INCH CRACK WAS FOUND IN RT ELEVATOR LOWER SPAR CAP AT STA XE25 AND A .75 INCH CRACK ON UPPER SPAR CAP AT XE25. COMPLETED REPAIR PER DAC TELEX SVC-MSP-0677/RMK DATED 11 AUG 96. 2 L 7 2 4F A6WE 1996091900182 19960919 00182 WP 1996 9 19 MWEA96453 1 19960912 A 5521 SPAR CAP DOUG DC9 DC932 3022066 WP RT ELEVATOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSPECTION, A .3750 INCH CRACK WAS FOUND IN THE ELEVATOR UPPER SPAR CAP AT STA XE68 AND A .75 INCH CRACK AT STA X E 121. REPAIRED IAW SRM 55-02, FIG. 9, CONFIGURATION -501. 2 L 7 2 4F A6WE 1996091900183 19960919 00183 WP 1996 9 19 MWEA96454 1 19960912 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 1089 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSPECTION, AN ANGLE AT STA 1089 (CANTED FRAME) WAS FOUND EXFOLIATED ON AFT SIDE AT LONGERON 12L. MANUFACTURED A ND INSTALLED A NEW ANGLE IAW DC9 SRM 53-11-4. 2 L 7 2 4F A6WE 1996091900184 19960919 00184 WP 1996 9 19 MWEA96455 1 19960912 A 5260 DOUBLER DOUG DC9 DC932 3022066 WP VENTRAL STAIR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSPECTION, A DOUBLER PLATE UNDER THE TOP STEP OF THE VENTRAL STAIR DOOR WAS FOUND EXFOLIATED. FABRICATED A NEW ANGLE AND INSTALLED IAW SRM 52-01. 2 L 7 2 4F A6WE 1996091900185 19960919 00185 WP 1996 9 19 MWEA96456 1 19960912 A 5530 CENTER HINGE DOUG DC9 DC932 3022066 WP VERT STAB CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSPECTION, VERTICAL STAB REAR SPAR CENTER HINGE FOR THE RUDDER FOUND CORRODED ON RT ATTACH LEG. REMOVED THE HIN GE AND FOUND CORRODED LEG CRACKED. REPLACED HINGE IAW DAC MM 20-16-0, PG. 209, FIG. 205. 2 L 7 2 4F A6WE 1996091900186 19960919 00186 WP 1996 9 19 MWEA96457 1 19960912 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSPECTION, THE PYLON LEADING EDGE WAS FOUND CHAFED INTO THE FUSELAGE SKIN. FABRICATED REPAIR PARTS AND INSTALLE D IAW SRM'S 51-10-3, 51-30-2, 53-04, FIG. 3A, SHEET 1, PG 6A. 2 L 7 2 4F A6WE 1996091900187 19960919 00187 WP 1996 9 19 MWEA96458 1 19960912 A 5260 SKIN DOUG DC9 DC932 3022066 WP VENTRAL STAIR TORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSPECTION, VENTRAL STAIR EXTERNAL SKIN WAS FOUND TORN AT THE TOE PLATE. COMPLETED A REPAIR IAW SRM 52--01, FIG. 2, SHEET 3. 2 L 7 2 4F A6WE 1996091900188 19960919 00188 WP 1996 9 19 MWEA96459 1 19960912 A 5320 CLIP DOUG DC9 DC932 3022066 WP BS 380 HOLE IN RADIUS A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSPECTION, AN ATTACH CLIP HAD A HOLE IN RADIUS IN FORWARD CARGO PIT FORWARD DOOR JAMB INTERCOSTAL AT STA 380. FA BRICATED A NEW CLIP AND INSTALLED IAW SRM 53-01. 2 L 7 2 4F A6WE 1996091900189 19960919 00189 WP 1996 9 19 MWEA96460 1 19960912 A 5315 FLOOR BEAM DOUG DC9 DC932 3022066 WP BS 389 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSPECTION, TWO SMALL SPOTS OF EXFOLIATION CORROSION WERE FOUND ON THE UPPER FLANGE OF CABIN FLOOR BEAM AT STA 38 9. REPAIRED FLOOR BEAM IAW SRM 53-05. 2 L 7 2 4F A6WE 1996091900190 19960919 00190 NM 1996 9 19 DLM88962073 1 19960908 A 3350 20131A BATTERY PACK DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 908DL 49539 EMERGENCY TRACK LITE SYS INOP IN FIRST CLASS AND IN 3 ROWS OF TOURIST CLASS. FOUND BATTERY PACK DEAD, REPL. BATTERY PAC K, CK'S OK. 2 L 7 2 4F RT A6WE 1996091900191 19960919 00191 NM 1996 9 19 DL72L962076 1 19960908 A 3350 BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 514DA 21430 OVERWING EXIT EMER LIGHT INOP // REPLACED BATT PACK M956 OPS CK GOOD 2 L 7 3 4F A3WE 1996091900192 19960919 00192 NM 1996 9 19 DL72S962079 1 19960908 A 3350 POWER SUPPLY BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 493DA 21062 EMERGENCY EXIT LIGHT ABOVE ROW 3 DID NOT COME ON DURING TESTREPLACED POWER SUPPLY AND BATTERY OPS NML. 2 L 7 3 4F A3WE 1996091900193 19960919 00193 NM 1996 9 19 DL72S962080 1 19960908 A 3350 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 493DA 21062 R/H EXTERIOR OVERWING EMERGENCY EXIT LIGHT FWD POS INOP. REPLACED BATTERY OPS NML. 2 L 7 3 4F A3WE 1996091900194 19960919 00194 NM 1996 9 19 DL757962085 1 19960909 A 3350 767 LAMP BOEING 757 757232 1384965 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 685DA 27588 EMERGENCY EXIT LIGHT ON EXTERIOR OF 1R DOOR INOP DURING TESTREPLACED LIGHT BULB AND OPERATIONAL CHECKED GOOD 2 L 7 2 4F RT A2NM 1996091900195 19960919 00195 NM 1996 9 19 DL72S962089 1 19960909 A 3350 LIGHT BOEING 727 727232 1384082 NM COCKPIT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 521DA 21472 FOUND C/P O/HEAD EMERGENCY LITE INOP. RPLCD BATTERIES AND TAG. 2 L 7 3 4F A3WE 1996091900196 19960919 00196 NM 1996 9 19 DL72K962092 1 19960910 A 3350 079123 BULB BOEING 727 727232 1384082 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 479DA 20756 1 RED EMERGENCY TRACK LIGHT OUT IN FWD CABIN- RELAMPED AND RPL LENS TEST OK 2 L 7 3 4F A3WE 1996091900197 19960919 00197 WP 1996 9 19 DLL10962094 1 19960910 A 3350 BATTERIES LKHEED 1011 10113851 5265010 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1734D 193C1225 EMERGENCY FLASHLIGHT AT R4 DOOR INOP REPLACED BATTERY AND BULB. CKS OK. 2 L 7 3 4F A23WE 1996091900198 19960919 00198 NM 1996 9 19 SCNA96248 1 19960907 A 2612 106087713 FIRE LOOP BOEING 727 727225 1384077 NM NR 3 ENGINE OUT OF POSITION A SCNA K NONE N FALSE WARNING IN INSP/MAINT 1 GL 15 283SC 22559 NR 3 ENGINE FIRE DETECTOR CIRCUIT GROUND LIGHT WAS ON INTERMITTENTLY FOR ABOUT AN HOUR. REPOSITIONED NR 3 ENGINE FIRE LOOP FROM AREA WHERE IT WAS RUBBING ON THE RIB OF THE LOWER COWL. OPS CHECKED NORMAL. 2 L 7 3 4F A3WE 1996091900199 19960919 00199 NM 1996 9 19 P5CA9600688 1 19960910 A 5414 SKIN BOEING 747 747132 1384882 NM NR 1 PYLON GOUGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 DEEP GOUGE IN NR 1 PYLON CAPSKIN BETWEEN NAC 193 AND 210. REPAIRED PER POLAR AIR CARGO MAINTENANCE AUTHORIZATION 5430-0 1:01. 2 L 7 4 4F A20WE 1996091900200 19960919 00200 WP 1996 9 19 RRXA96085 1 19960911 A 2612 FIRE LOOP DOUG DC8 DC863 302198A WP NR 3 ENGINE DIRTY A RRXA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 15 797AL 46163 CYQX - FLT DX3 - ON CLIMB-OUT AT INITIAL POWER REDUCTION, NR 3 FIRE WARNING ILLUMINATED, ENGINE PARAMETERS APPEARED NORM AL. SHUTDOWN ENGINE IAW DC-8 QRH. CLEANED LOWER FIRE LOOP AS PRECAUTIONARY. INSPECTED ENGINE FOR LEAKS, NO DEFECTS NO TED. PERFORMED HIGH POWER RUN PER EWW ENGINE RUN UP BOOK, NO DEFECTS NOTED. (M) 2 L 7 4 4F 4A25 1996091900201 19960919 00201 WP 1996 9 19 ARWA9609028 1 19960911 A 2612 FIRE LOOP DOUG DC8 DC863 302198A WP NR 1 ENGINE MOIST CONTAM A ARWA A E F UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING TO TAKEOFF 1 SO 19 345JW 46042 DURING TAKEOFF FROM SJU, NR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED. SHUT DOWN ENGINE, LIGHT REMAINED ON. DISCHARGED B OTH LEFT ENGINE FIRE BOTTLES. WARNING LIGHT CONTINUED TO ILLUMINATE. AIRCRAFT RETURNED TO SJU WITHOUT INCIDENT. MAINT ENANCE FOUND MOISTURE SHORTING FIRE WARNING LOOP CONNECTORS ON ENGINE. MOISTURE REMOVED AND SYSTEM OPS NORMAL. 2 L 7 4 4F 4A25 1996091900202 19960919 00202 NE 1996 9 19 ARWA9609029 2 19960910 A 7200 ENGINE DOUG DC8 DC862 3021970 WP PWA JT3D JT3D7 52039 NE NR 4 FAILED A ARWA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 19 810BN 45905 669162 NR 4 ENGINE SHUT DOWN IN FLIGHT BECAUSE OF LOW OIL PRESSURE. AIRCRAFT CONTINUED INTO ELP WITHOUT INCIDENT. MAINTENANCE FOUND OIL WAS LOST OUT OF THE ENGINE TAILPIPE. AIRCRAFT FERRIED TO MIAMI WHRE NR 4 ENGINE WAS REMOVED AND REPLACED. C AUSE OF FAILURE TO BE REVEALED AT SHOP TEARDOWN. 2 L 7 4 4F 4 F 4A25 1E8 1996091900203 19960919 00203 NM 1996 9 19 CKSA96128 1 19960902 A 5320 DOUBLER BOEING 747 747146 NM BS 1920 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 702CK 20332 RJAA - DURING C-1 CHECK INSPECTION FOUND: REPAIR DOUBLER BS 1920 BETWEEN S41L AND S44L. REPAIRED DOUBLER PER SRM 53-30 -03 FIGURE 1 EXTERNAL REPAIR WITH SOLID FASTENER. JOB CONTROL NR J052. WORK PERFORMED BY JAPAN AIRLINES (JACZ109F). 2 L 7 4 4F A20WE 1996091900204 19960919 00204 NM 1996 9 19 CKSA96129 1 19960902 A 5320 DOUBLER BOEING 747 747146 NM BS 740-760 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 702CK 20332 RJAA - DURING C-1 CHECK INSPECTION FOUND: CORROSION CENTER FUSELAGE SKIN STA 740 THROUGH STA 760 AREA BOTTOM ZONE (INSI DE). INSTALLED DOUBLER REPAIR PER SRM 53-30-3 PAGE 2A. JOB CONTROL NR J128. SOURCE CONTROL R. 7TK9061. WORK PERFORM ED BY JAPAN AIRLINES (JACZ109F). 2 L 7 4 4F A20WE 1996091900205 19960919 00205 NM 1996 9 19 CKSA96130 1 19960902 A 5330 SKIN BOEING 747 747146 NM BS 2181 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 702CK 20332 RJAA - DURING C-1 CHECK INSPECTION FOUND: BULGE STA 2181 BOTTOM FUSELAGE SKIN AREA. CORROSION BLENDED OUT PER SRM 51-1 0-01 PAR 7. ACCOMPLISHED THE SUBJECT REPAIR IN ACCORDANCE WITH CWS-MNZ/E-040 96-08-27. JOB CONTROL NR J107. WORK PER FORMED BY JAPAN AIRLINES (JACZ109F). 2 L 7 4 4F A20WE 1996091900206 19960919 00206 NM 1996 9 19 CKSA96131 1 19960902 A 5330 SKIN BOEING 747 747146 NM NR 3 PYLON CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 702CK 20332 RJAA - DURING C-1 CHECK INSPECTION FOUND: BULGE AND CRACK NR 3 NAC STRUT INBOARD SKIRT BEAM SKIN. REPLACED BEAM SKIN P ER SRM 51-10-01 PAR 9. JOB CONTROL NR J994. SOURCE CONTROL NR 7TK7273. WORK PERFORMED BY JAPAN AIRLINES (JACZ109F). 2 L 7 4 4F A20WE 1996091900207 19960919 00207 NM 1996 9 19 CKSA96132 1 19960902 A 5330 SKIN BOEING 747 747146 NM BS 1855-1863 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 702CK 20332 RJAA - DURING C-1 CHECK INSPECTION FOUND: BULGE - FUSELAGE BOTTOM SKIN AT BS 1855 THROUGH BS 1863 S49R (AFT CARGO LOWER ). PERFORMED BLEND OUT SKIN FOR CORROSION AND PERFORMED BLEND OUT STRINGER DOUBLER LOWER FACE PER SRM 53-30-1 P1 AND SR M 51-10-01 PAR 7. PERFORMED REPAIR PER TWX JAL-NRT-96-0805 RE - 1996-08-29 MNZ/E. JOB CONTROL NR J029. WORK PERFORMED BY JAPAN AIRLINES (JACZ109F). 2 L 7 4 4F A20WE 1996091900208 19960919 00208 NM 1996 9 19 CKSA96133 1 19960902 A 5330 SKIN BOEING 747 747146 NM BS 1857-1865 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 702CK 20332 RJAA - DURING C-1 CHECK INSPECTION FOUND: BULGE - FUSELAGE BOTTOM SKIN BS 1857-BS1865 S50L. PERFORMED REPAIR PER REF T WX JAL-NRT-96-0805 RE 1996-08-29 MNZ/E. JOB CONTROL NR J028. WORK PERFORMED BY JAPAN AIRLINES (JACZ109F). 2 L 7 4 4F A20WE 1996091900209 19960919 00209 NM 1996 9 19 CKSA96134 1 19960902 A 5330 SKIN BOEING 747 747146 NM BS 1840-1845 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 702CK 20332 RJAA - DURING C-1 CHECK INSPECTION FOUND: BULGE FUSELAGE BOTTOM SKIN OF BS 1840 THROUGH BS 1845 S51R (AFT CARGO AREA). PERFORMED BLEND AWAY THE DAMAGED EDGE OF STRINGER DOUBLER. PERFORMED REPAIR PER REF TWX JAL-NRT-96-0805 RE 1996-08-29 MNZ/E. JOB CONTROL NR J027. WORK PERFORMED BY JAPAN AIRLINES (JACZ109F). 2 L 7 4 4F A20WE 1996091900210 19960919 00210 WP 1996 9 19 CKSA96135 1 19960910 A 2612 51653122 FIRE WARNING LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB211524B02 54555 NE NR 2 ENGINE ACTIVATED A CKSA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 103CK 293C1212 14525 KMIA - FLT 78614 - NR 2 ENGINE A-LOOP LIGHT CAME ON WHILE SETTING CLIMB THRUST AFTER TAKEOFF. SELECTED LOOP B AND TESTE D OK. WENT BACK TO BOTH POSITIONS AND A AND B LOOPS WERE ON WITH LIGHTS AND BELL. RAN ENGINE FIRE AND SEVERE DAMAGE CH ECKLIST ALONG WITH LOSS OF BLEED AND ONE GENERATOR CHECKLIST. WHEN FIREWALL SHUT OFF HANDLE WAS PULLED, A AND B LIGHTS WENT OUT, AND RED FIRE LIGHTS WENT OUT. RETESTED FIRE WARNING, ALL OK. ELECTED NOT TO DISCHARGE BOTTLE. REMOVED AND R EPLACED NR 2 ENGINE FIRE DETECTION CONTROL UNIT IAW L1011 MM 26-11-08 AND HORIZONTAL FIREWALL FIRE DETECTION SENSOR IAW L1011 MM 26-11-03. INSPECTED ALL OTHER FIRE DETECTION SENSORS IAW L1011 MM 26-11-00. NO DEFECTS NOTED. INSPECTED ALL 2 L 7 3 4F 4 F A23WE E12EU 1996091900211 19960919 00211 SO 1996 9 19 SRAA960909 1 19960911 A 2612 GASKETS LKHEED 382 382G 526414U SO NR 2 ENGINE LEAKING A SRAA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 GL 23 918SJ 4208 DURING CRUISE INTO PHL. FLT 9010, NR 2 NACELLE OVERHEAT LIGHT CAME ON, SHUT DOWN ENGINE AND LANDED WITHOUT INCIDENT AT P HL. FOUND SCOOP ANTI-ICE LINE ON LEFT HAND SIDE OF ENGINE LEAKING, REPLACED TWO GASKETS AND PERFORMED BLEED AIR LEAK CH ECK, PER M.M. CH 75. NONE FOUND ON ENGINE RUN, AIRCRAFT RETURNED TO SERVICE. 2 H 7 4 4T A1SO 1996091900237 19960919 00237 CE 1996 9 19 96ZZZX4608 1 19960723 A 2730 2300003171 CONTROL CABLE LEAR 35 35A 5170602 CE ELEVATOR BROKEN A A EGQA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 17 78MC 490 117 PILOT FELT LOSS OF ELEVATOR AUTHORITY DURING TAKEOFF ROLL. TAKEOFF WAS ABORTED WITHOUT INCIDENT AND AIRCRAFT WAS TURNED OVER TO MAINTENANCE. THE RIGHT AFT ELEVATOR CONTROL CABLE WAS FOUND FRAYED AND BROKEN BETWEEN THE TWO UPPER PULLEY SET S. INSTALLATION OF A NEW CABLE USING SAME ROUTING REVEALED THAT CABLE COULD CHAFE ON A BOLT THAT RETAINS THE YAW DAMPEN ER SERVO. FURTHER INSPECTION SHOWED THE RUDDER CABLE (RIGHT) AND ELEVATOR CABLE CROSSED BETWEEN THE UPPER PULLEY SETS. CORRECTION OF CABLE ROUTING ELIMINATED CHAFE SITUATION. RUDDER CABLE WAS NOT CHANGED WITH ELEVATOR CABLE. THIS AREA IS DIFFICIULT TO INSPECT DUE TO BLEED AIR PLUMBING. 2 L 7 2 4F A10CE 1996091900241 19960919 00241 SW 1996 9 19 96ZZZX4612 1 19960412 A 7714 SCREW GULSTM 680 680FL 0141608 SW ENGINE TACH SHORTED A HSYA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 05 6344U 143072 BIL - FLT 5011 - PILOT REPORTED A 'FLASH' IN THE INSTRUMENT PANEL AND SMELLED WIRE INSULATION BURNED. BRASS SCREW BACKE D OUT OF THE ENGINE TACHOMETER MOUNT AND CONTACTED THE HOT PORTION OF THE INDIRECT LIGHTING BULB. SECURED SCREW IN TACH OMETER MOUNT, LIGHTING SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 1 H 7 2 3O 2A4 1996091900243 19960919 00243 NE 1996 9 19 96ZZZX4614 2 19960704 A 7310 MANIFOLD BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101650B1 41560 NE FUEL LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 AFTER LANDING AT SCENE FOR PATIENT TRANSPORT, PILOT NOTICED CLEAR FLUID RUNNING FROM AIRCRAFT. MAINTENANCE ARRIVED AND FOUND LEAK IN FUEL MANIFOLD. 1 G 7 2 3U 3 U H13EU E5NE 1996091900244 19960919 00244 NE 1996 9 19 96ZZZX4615 2 19960721 A 7200 ENGINE BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101650B1 41560 NE NR 2 CHIP LIGHT A R7MA O OTHER J WARNING INDICATION AP APPROACH 1 NM 11 NR 2 ENGINE CHIP ON SHORT FINAL, WOULD NOT PULSE OFF, LANDED AIRCRAFT. 1 G 7 2 3U 3 U H13EU E5NE 1996091900245 19960919 00245 NE 1996 9 19 96ZZZX4616 2 19960714 A 7200 ENGINE BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101650B1 41560 NE NR 1 MAKING METAL A R7MA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NM 11 NR 1 ENGINE CHIP LIGHT WOULD NOT PULSE OFF, LANDED AIRCRAFT. 1 G 7 2 3U 3 U H13EU E5NE 1996091900246 19960919 00246 NE 1996 9 19 96ZZZX4617 2 19960719 A 7200 ENGINE BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101650B1 41560 NE NR 1 CHIP LIGHT A R7MA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NM 11 NR 1 ENGINE CHIP LIGHT PULSED OFF ONCE, LIGHT ILLUMINATED AGAIN, ABORTED FLIGHT, AIRCRAFT LANDED. 1 G 7 2 3U 3 U H13EU E5NE 1996091900247 19960919 00247 NE 1996 9 19 96ZZZX4618 2 19960710 A 7200 ENGINE BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101650B1 41560 NE NR 1 MAKING METAL A R7MA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NM 11 NR 1 ENGINE CHIP LIGHT ILLUMINATED 3 TIMES, PULSED ALL 3 TIMES, RETURNED TO BASE. 1 G 7 2 3U 3 U H13EU E5NE 1996091900248 19960919 00248 EU 1996 9 19 96ZZZX4619 1 19960711 A 6520 GEAR BOX BOLKMS 117 BK117B1 5626012 EU T/R CHIP LIGHT A R7MA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NM 11 TAIL ROTOR CHIP LIGHT ILLUMINATED, ATTEMPTED TO PULSE OFF THREE TIMES, LANDED, CONTACTED MAINTENANCE. 1 G 7 2 3U H13EU 1996091900262 19960919 00262 1996 9 19 HEEA967738 4 19960903 A 3452 066106200 TRANSCEIVER KT76 BOLKMS 105 BO105S 5626006 EU COCKPIT ATC WONT TEST E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 81992 S827 NO SELF TEST. REPLACED SWITCH BOARD ASSEMBLY P/N 200-0381-01. REPAIRED. ADJUSTED PULSE WIDTH AND FREQUENCY. BENCH CHE CK GOOD. 1 G 7 2 3U H3EU 1996091900263 19960919 00263 1996 9 19 HEEA967739 4 19960903 A 2312 064102302 TRANSCEIVER KTR908 BELL 412 412 1182202 SW COCKPIT VHF DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 108X 33115 VHF BREAKS SQUELCH WITH NO SIGNAL. ADJUSTED SQUELCH. REPAIRED. REPLACED HEADER J304 AND APPLIED HUMISEAL TO HEADER FOR CORROSION CONTROL. INSTALLED MOD 2 AS PER KING SERVICE BULLETIN KTR908-2. ADJUSTED MOD., POWER OUT AND SIDETONE. BEN CH CHECK GOOD. 1 G 7 2 4U H4SW 1996091900264 19960919 00264 1996 9 19 HEEA967740 4 19960903 A 3452 066104100 TRANSPONDER BELL 412 412 1182202 SW COCKPIT INTERMITTENT E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 22608 33075 TRANSPONDER INTERMITTENTLY INOPERATIVE. 1 G 7 2 4U H4SW 1996091900265 19960919 00265 1996 9 19 HEEA967741 4 19960903 A 3450 071121004 CONTROL BOX BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 108X 33115 DOES NOT CHANNEL FREQUENCIES CORRECTLY AND KNOBS CHANGE WRONG DIGITS INTERMITTENTLY. VERIFIED, CLEANED WAFERS AND CONTAC TS. NO HELP. REPLACED SWITCH S304 AND RIVETS 2 EACH P/N 092-5009-04. ALSO REPLACED RETAINING RING P/N 090-0036-04. N O HELP. REPLACED DETENT WHEEL P/N 088-0766-01. NO HELP. 1 G 7 2 4U H4SW 1996091900266 19960919 00266 1996 9 19 HEEA967742 4 19960903 A 2312 064100900 TRANSCEIVER KTR905 BELL 412 412 1182202 SW COCKPIT INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2261D 33076 RECEIVER INOPERATIVE. SENT TO ALLIED SIGNAL AVIONICS FOR INSPECTION AND REPAIR. 1 G 7 2 4U H4SW 1996091900267 19960919 00267 EU 1996 9 19 HEEA967743 1 19960903 A 6520 350A33215300 BEARING SNIAS 350 AS350B2 8680813 EU T/R DETERIORATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100U 2863 RUBBER DETERIORATED. 1 G 7 1 3U H9EU 1996091900268 19960919 00268 EU 1996 9 19 HEEA967744 1 19960903 A 6520 350A33215300 BEARING SNIAS 350 AS350B2 8680813 EU T/R DETERIORATED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 6100U 579 2863 RUBBER DETERIORATED. 1 G 7 1 3U H9EU 1996091900269 19960919 00269 EU 1996 9 19 HEEA967745 1 19960903 A 6230 704A33651158 BEARING 355A37000001 AEROSP AS355 AS355F1 8680810 EU SWASHPLATE SEAL DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5796S 1574 M227 5164 WHEN DISASSEMBLED SWASHPLATE ASSEMBLY; FOUND WITH BOTH GREASE SEALS POPPED OUT OF THEIR SEATS OF THE SWASHPLATE BEARING. REPLACED WITH SERVICEABLE BEARING. 1 G 7 2 3U H11EU 1996091900270 19960919 00270 EU 1996 9 19 HEEA967746 1 19960903 A 7714 DL41239 INDICICATOR BOLKMS 105 BO105S 5626006 EU COCKPIT STICKS E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5421E S806 STICKS FROM 0% TO 30% INTERMITTENTLY. TIME SINCE REPAIR 17:05. 1 G 7 2 3U H3EU 1996091900271 19960919 00271 1996 9 19 HEEA967747 4 19960903 A 3452 066104100 TRANSPONDER SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 31217 760229 TRANSPONDER INOPERATIVE; ARCHING NOISE WHEN TURNED ON. 1 G 7 2 3U H1NE 1996091900272 19960919 00272 1996 9 19 HEEA967748 4 19960903 A 3453 25410038 7000 CDU BELL 412 412 1182202 SW COCKPIT LORAN FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 22608 33075 UNIT WENT OFF LINE. LOST ALL LIGHTS ON CDU AND PUSHBUTTON SWITCHES UNREADABLE. 1 G 7 2 4U H4SW 1996091900273 19960919 00273 1996 9 19 HEEA967749 4 19960903 A 3453 25410036 7000 RCU BELL 412 412 1182202 SW COCKPIT LORAN INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 22608 33075 UNIT WENT OFF LINE. LOST ALL LIGHTS ON CDU. 1 G 7 2 4U H4SW 1996091900274 19960919 00274 1996 9 19 HEEA967750 4 19960903 A 3416 8140BS20LW ENCODER SKRSKY S76 S76A 8143006 NE COCKPIT ALT INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1545K 760047 LIGHT INOPERATIVE. TIME SINCE REPAIR 71:20. 1 G 7 2 3U H1NE 1996091900275 19960919 00275 SW 1996 9 19 HEEA967751 1 19960903 A 5510 206023119151 STABILIZER ASSY BELL 206 206L1 1182107 SW BOTTOM SIDE MIS REPAIR E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2 EACH INSERTS ON R//H FORWARD BOTTOM SIDE MISLOCATED AND 4 EACH INSERTS ON L/H AFT BOTTOM SIDE MISLOCATED. TIME SINCE REPAIR 0:00. 1 G 7 1 3U H2SW 1996091900276 19960919 00276 NE 1996 9 19 HEEA967752 1 19960903 A 5321 7620402002049 PANEL SKRSKY S76 S76A 8143006 NE FLOOR DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 EDGE OF PANEL CUT FROM INSTALLATION HOLE. TIME SINCE REPAIR 0:00. 1 G 7 2 3U H1NE 1996091900277 19960919 00277 1996 9 19 HEEA967753 4 19960903 A 3444 066304401 INDICATOR BOLKMS 117 BK117B1 5626012 EU CKPIT RADIO ALT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 217UC 7152 GLASS ON FACE IS PUSHED IN. TIGHTENED AND REPOSITIONED GLASS BACK ON THE BEZEL. REPAIRED. FOUND FLAG WOULD NOT GO OUT OF VIEW. REPLACED DIODE CR212 AND FLAG ASSEMBLY. REPAIRED. BENCH CHECK GOOD. 1 G 7 2 3U H13EU 1996091900278 19960919 00278 SW 1996 9 19 HEEA967754 1 19960903 A 6520 212040468001 CASE ASY 212040004009 BELL 412 412 1182202 SW T/R GR BOX PORT MISSING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893P 5934 AFS1026 33012 T/R GEARBOX REMOVED DUE TO METAL IN OIL. FOUND OUTPUT DUPLEX BEARING P/N 212-040-456-001, S/N J6885, T.T. 1669:25 SPALLE D. LUBRICATION PORT TO FEED BEARING NOT PRESENT IN ABOVE MENTIONED CASE ASSEMBLY CAUSING BEARING FAILURE. REPAIRED GEAR BOX WITH NEW PART. 1 G 7 2 4U H4SW 1996091900279 19960919 00279 1996 9 19 HEEA967755 4 19960903 A 3451 066103708 TRANSCEIVER SKRSKY S76 S76A 8143006 NE COCKPIT DME INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 4253S 760035 DME INOPERATIVE. NO DISPLAY. 1 G 7 2 3U H1NE 1996091900280 19960919 00280 EU 1996 9 19 HEEA967756 1 19960903 A 6310 4638202007 CLUTCH 4638001004 BOLKMS 105 BO105S 5626006 EU FREEWHEEL CAGE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7170D 3101 1044 S840 INNER CAGE WORN AND ENERGIZING RIBBON WORN. REPLACED WITH SERVICEABLE CLUTCH. SEE MMIR # HEEA0007757 FOR OTHER CLUTCH R EMOVED. 1 G 7 2 3U H3EU 1996091900281 19960919 00281 EU 1996 9 19 HEEA967757 1 19960903 A 6310 4638202007 CLUTCH 4638001004 BOLKMS 105 BO105S 5626006 EU FREEWHEEL CAGE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7170D 1527 1044 S840 INNER CAGE WORN. REPLACED WITH SERVICEABLE CLUTCH. SEE MMIR # HEEA0007756 FOR OTHER CLUTCH REMOVED. 1 G 7 2 3U H3EU 1996091900282 19960919 00282 1996 9 19 HEEA967758 4 19960903 A 3444 066304401 INDICATOR BOLKMS 105 BO105S 5626006 EU COCKPIT ALT STICKS E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 818SH S753 RADAR ALTIMETER 2 YEAR INSPECTION DUE. FOUND FLAG STICKS. 1 G 7 2 3U H3EU 1996091900283 19960919 00283 1996 9 19 HEEA967759 4 19960903 A 3444 066304400 ALTIMETER SKRSKY S76 S76A 8143006 NE COCKPIT RADAR DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5435V 760158 UNRELIABLE AND DOES NOT TEST AT 50 FEET. 1 G 7 2 3U H1NE 1996091900284 19960919 00284 1996 9 19 HEEA967760 4 19960903 A 3451 066106602 TRANSCEIVER BELL 412 412 1182202 SW COCKPIT DME DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 107X 33113 RX WEAK AND TRANSMITTER INOPERATIVE. SENT TO ALLIED SIGNAL AVIONICS FOR INSPECTION AND REPAIR. 1 G 7 2 4U H4SW 1996091900285 19960919 00285 1996 9 19 HEEA967761 4 19960903 A 2310 064101600 CONTROL KCU951 BELL 412 412 1182202 SW COCKPIT HF KNOB DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 293CA HF CONTROL ON/OFF KNOB COMES OFF. SENT TO ALLIED SIGNAL AVIONICS FOR INSPECTION AND REPAIR. 1 G 7 2 4U H4SW 1996091900286 19960919 00286 1996 9 19 HEEA967762 4 19960903 A 2312 4000106010 CONTROL UNIT C10 SNIAS 350 AS350B2 8680813 EU COCKPIT INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 4000L 2873 INTERMITTENT INOP ON SELECTED CHANNELS. HAS A PROBLEM PROGRAMMING MHZ THUMBWHEEL. REPLACED THUMBWHEEL AND REPAIRED. BE NCH CHECK GOOD. 1 G 7 1 3U H9EU 1996091900287 19960919 00287 1996 9 19 HEEA967763 4 19960903 A 3453 453105004 LORAN R501 BELL 412 412 1182202 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 108X 33115 1 1/2 MILES OFF; SIGNAL WEAK AND BUTTONS ARE INTERMITTENT. 1 G 7 2 4U H4SW 1996091900288 19960919 00288 NE 1996 9 19 HEEA967764 1 19960903 A 6410 7610105101041 BLADE SKRSKY S76 S76A 8143006 NE T/R DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911MJ 8714 760231 T/R BLADE HAS VOID ON PADDLE "A" NEAR STATION 30. ALSO HAS A HOLE IN THE END CAP. 1 G 7 2 3U H1NE 1996091900290 19960919 00290 EU 1996 9 19 HEEA967766 1 19960903 A 6240 10594575 TRANSMITTER BOLKMS 105 BO105S 5626006 EU MAST TORQUE DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 50293 S677 TORQUE NEEDLE INDICATES LOW OUT OF TOLERANCE. 1 G 7 2 3U H3EU 1996091900291 19960919 00291 EU 1996 9 19 HEEA967767 1 19960903 A 6240 10594564 INDICATOR BOLKMS 105 BO105S 5626006 EU MAST MOMENT READS LOW E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 50293 S677 NEEDLE INDICATES LOW OUT OF TOLERANCE. SENT TO MASCO FOR WARRANTY REPAIR. 1 G 7 2 3U H3EU 1996091900292 19960919 00292 GL 1996 9 19 HEEA967768 2 19960903 A 7314 3881005 PUMP BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL ENG FUEL WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2125M 4149 45649 WORN INTERNAL DRIVE SPLINES. 1 G 7 1 3U 3 U H2SW E1GL 1996091900293 19960919 00293 1996 9 19 HEEA967769 4 19960903 A 3416 D120P2T ANEROID SNIAS 350 AS350B2 8680813 EU COCKPIT ENCODER DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 350BZ 2653 ENCODER OUTPUT TRANSMITS 6,200 FEET HIGH WITH NO PRESSURE APPLIED. 1 G 7 1 3U H9EU 1996091900294 19960919 00294 SW 1996 9 19 HEEA967770 1 19960903 A 7712 212070160007 INDICATOR BELL 212 212 1181420 SW NR 1 TORQUE FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1079U 31122 TORQUEMETER #1 NEEDLE HAS NO INDICATION. 1 G 7 1 4U H4SW 1996091900295 19960919 00295 NE 1996 9 19 HEEA967771 1 19960903 A 5321 7620402002049 FLOOR PANEL SKRSKY S76 S76A 8143006 NE INSERTS MIS REPAIRED E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 2743E 760155 FLOOR PANEL WAS REPAIRED AND EXISTING INSERTS IN FLOOR PANEL WERE LEFT INSIDE OLD CORE MATERIAL AND NEW SKINS WERE INST ALLED. THE OLD INSERTS INSIDE THE PANEL MAKE IT IMPOSSIBLE TO INSTALL NEW STYLE INSERTS THAT MUST GO THROUGH TOP ANDBOT TOM SKINS. TIME SINCE REPAIR 0:00. 1 G 7 2 3U H1NE 1996091900296 19960919 00296 NE 1996 9 19 HEEA967772 1 19960903 A 5321 7620402002050 FLOOR PANEL SKRSKY S76 S76A 8143006 NE INSERTS MIS REPAIRED E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 2743E 760155 FLOOR PANEL WAS REPAIRED AND EXISTING INSERTS IN FLOOR PANEL WERE LEFT INSIDE OLD CORE MATERIAL AND NEW TOP SKINS WERE INSTALLED. THE OLD INSERTS INSIDE PANEL MAKE IT IMPOSSIBLE TO INSTALL NEW STYLE INSERTS THAT MUST GO THROUGH TOP ANDBO TTOM SKINS. SENT TO DODS FOR WARRANTY REPAIR. TIME SINCE REPAIR 0:00. 1 G 7 2 3U H1NE 1996091900297 19960919 00297 NE 1996 9 19 HEEA967773 1 19960903 A 5321 7620402021041 FLOOR PANEL SKRSKY S76 S76A 8143006 NE LT OUTBOARD MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 2743E 760155 NEW FLOOR DOES NOT HAVE PROPER JOGGLE ON INBOARD AND FORWARD EDGES OF PANEL AS NEEDED TO GO BELOW (-051) LARGE FLOOR. 1 G 7 2 3U H1NE 1996091900298 19960919 00298 SW 1996 9 19 HEEA967774 1 19960903 A 2436 206075447007 VOLT REGULATOR BELL 206 206L1 1182107 SW DC SYS WRONG PARTS E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 21240 45647 REGULATOR NEEDS EVALUATION FOR CORRECT CIRCUIT BOARDS. 1 G 7 1 3U H2SW 1996091900299 19960919 00299 SW 1996 9 19 HEEA967775 1 19960903 A 2436 206075447007 VOLT REGULATOR BELL 206 206L1 1182107 SW DC SYS WRONG PARTS E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 REGULATOR NEEDS EVALUATION FOR CORRECT CIRCUIT BOARDS. 1 G 7 1 3U H2SW 1996091900300 19960919 00300 SW 1996 9 19 HEEA967776 1 19960903 A 2436 206075447007 VOLT REGULATOR BELL 206 206L1 1182107 SW DC SYS WRONG PARTS E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 REGULATOR NEEDS EVALUATION FOR CORRECT CIRCUIT BOARDS. 1 G 7 1 3U H2SW 1996091900301 19960919 00301 NE 1996 9 19 HEEA967777 2 19960904 A 7310 430137601 FUEL NOZZLE BOLKMS 117 BK117B2 5626013 EU LYC LTS101 LTS101750B1 41560 NE MANIFOLD LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 132AE 1610 7238 LE48130AER ENGINE LEAK CHECK REVEALED FUEL LEAKING FROM FUEL MANIFOLD TUBING BRAZED JOINTS. REPLACED DISCREPANT PART. 1 G 7 2 3U 3 U NC H13EU E5NE10 1996091900302 19960919 00302 1996 9 19 HEEA967778 2 19960904 A 7310 430137601 FUEL NOZZLE BOLKMS 117 BK117B2 5626013 EU MANIFOLD LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 132AE 7238 FUEL LEAKING FROM ENGINE, INSPECTION REVEALED: FUEL LEAKING FROM FUEL MANIFOLD TUBE AS MARKED (7 0'CLOCK POSITION) REPL ACED DISCREPANT PART. REQUESTING 100% WARRANTY REPAIR. PART OVERHAULED ON DELAVAN, INC. W/O # 4945. 1 G 7 2 3U NC H13EU 1996091900304 19960919 00304 GL 1996 9 19 HEEA967782 2 19960904 A 7261 6888547 INTERNAL SUMP 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL TURBINE ASSY DEFECTIVE E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 911HM CAT34091 S683 CAE834363 UPON TURBINE ASSEMBLY NOTED: INLET AIRHOLE ON INTERNAL SUMP DOES NOT LINE UP WITH AIR HOLE IN P.T. SUPPORT. NOTE: INT ERNAL SUMP TRIED ON THREE P.T. SUPPORTS. REPLACED DISCREPANT PART. 1 G 7 2 3U 3 U H3EU E4CE 1996091900305 19960919 00305 GL 1996 9 19 HEEA967783 2 19960904 A 7250 23031938 NOZZLE 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL NR 2 DEFECTIVE E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 9190Y 785 CAT25437 S669 CAE270075 ENGINE REMOVED DUE TO UNABLE TO INSTALL 6 & 7 OIL PRESSURE NOZZLE. UPON INSPECTION OF TURBINE PARTS NOTED: EXCESSIVE R UNOUT BEYOND SERVICEABLE LIMITS ON #2 NOZZLE 1ST (.006 RUNOUT) AND 2ND (.005 RUNOUT) TIP PATHS. REPLACED DISCREPANT PART . 1 G 7 2 3U 3 U H3EU E4CE 1996091900306 19960919 00306 SW 1996 9 19 HEEA967784 1 19960904 A 6220 214010248101 SEAL 214010100207 BELL 214 214ST 1182106 SW M/R LEAK E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 8045T A368 28101 I.B. SEAL LEAKING DUE TO DETERIORATION. ONE EACH O.B. SEAL SHOWING MINOR LEAK. REPLACED ALL SEALS AS A SET. PARTS SCRA PPED LOCALLY. 2 G 7 2 4U H10SW 1996091900307 19960919 00307 SW 1996 9 19 HEEA967785 1 19960904 A 6220 214010133001 SEAL 214010100207 BELL 214 214ST 1182106 SW M/R LEAK E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 8045T A368 28101 I.B. SEAL LEAKING DUE TO DETERIORATION. ONE EACH O.B. SEAL SHOWING MINOR LEAK. REPLACED ALL SEALS AS A SET. PARTS SCRA PPED LOCALLY. 2 G 7 2 4U H10SW 1996091900309 19960919 00309 SW 1996 9 19 HEEA967787 1 19960906 A 6730 222382001105 ACTUATOR ASSY BELL 230 230 1182149 SW SPLIT LINE LEAKING E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 230UN 23009 SERVO LEAKING FROM SPLIT LINE. LOWER BEARING WORN. 1 G 7 2 3U NC H9SW 1996091900310 19960919 00310 SW 1996 9 19 HEEA967788 1 19960906 A 3212 407350301101 FLOAT BAG BELL 407 407 SW LT CHAMBER LEAKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407PH 443 53003 FLOAT BAG ONE CHAMBER LEAKS. 1 G 7 1 3U O H2SW 1996091900311 19960919 00311 NM 1996 9 19 CALA9601303 1 19960911 A 3610 DUCT BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE BLOWN A CALA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 SW 09 10791 20645 657114 THE NR 2 ENGINE FAILED AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO SJU WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE F OUND THE NR 2 ENGINE 13TH STAGE DUCT BLOWN. THE NR 2 ENGINE WILL BE REMOVED AND REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 1996091900312 19960919 00312 NM 1996 9 19 CALA9601304 1 19960912 A 3260 LOGIC CARD BOEING 737 7373T0 1384582 NM RT MLG INOPERATIVE A CALA O OTHER N FALSE WARNING CL CLIMB 1 SW 09 69351 23589 THE RT MLG RED LIGHT REMAINED ON AFTER GEAR RETRACTION. WHEN THE GEAR WAS CYCLED BOTH THE MAIN GEAR RED AND GREEN LIGHT S ILLUMINATED. THE AIRCRAFT LANDED AT CLE WITHOUT INCIDENT. MAINTENANCE FOUND THE M986 LANDING GEAR LOGIC CARD AT FAUL T. THE M986 LOGIC CARD WAS REPLACED. A LANDING GEAR EXTEND AND RETRACT TEST WAS PERFORMED WITH GEAR OPERATION AND INDI CATIONS CHECKING GOOD. 2 L 7 2 4F RT A16WE 1996091900313 19960919 00313 NM 1996 9 19 CALA9601305 1 19960912 A 2910 HYD LINE BOEING 737 737130 1384435 NM NR 1 ENG PYLON RUPTURED A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SW 09 59207 19024 THE AIRCRAFT LOST A-SYSTEM HYDRAULICS AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE A-SYSTEM HYDRAULIC PRESSURE LINE FROM NR 1 ENGINE PYLON TO WING ROOT RUPTURED. THE HYDRAULIC PR ESSURE LINE WAS REPLACED, LEAK CHECK WAS GOOD. 2 L 7 2 4F A16WE 1996091900314 19960919 00314 NE 1996 9 19 CALA9601306 2 19960912 A 7314 37820112 FUEL PUMP BOEING 737 737219 1384469 NM PWA JT8 JT8D9 52048 NE NR 1 ENGINE FAILED A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 10248 25393 13453 20344 665152 THE NR 1 ENGINE SURGED AND ROLLED BACK TO APPROXIMATELY 1.6 EPR AND 85 PERCENT ON TAKEOFF AT ROTATION. THE ENGINE WOULD NOT RESPOND TO THROTTLE MOVEMENTS. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REM OVED AND REPLACED THE NR 1 ENGINE FUEL CONTROL UNIT, FUEL PUMP AND FUEL HEATER AND LEAK CHECKS WERE GOOD. AN ENGINE POW ER ASSURANCE RUN WAS PERFORMED IAW MM 71-09-226, PAGE 209 AND ENGINE OPERATION CHECKED GOOD. 2 L 7 2 4F 4 F A16WE E2EA 1996091900315 19960919 00315 NM 1996 9 19 CALA9601307 1 19960911 A 5320 FLOOR SUPPORT BOEING 727 727224 1384076 NM BS 1070 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 INSPECTION FOUND TRANSVERSE FLOOR SUPPORT CORRODED AT BS 1070, RBL 20 TO RBL 32. THE FLOOR SUPPORT WAS REMOVED AND REPL ACED IAW SRM 51-10-2. 2 L 7 3 4F A3WE 1996091900316 19960919 00316 NM 1996 9 19 CALA9601308 1 19960911 A 5320 FLOOR SUPPORT BOEING 727 727224 1384076 NM BS 1130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 INSPECTION FOUND TRANSVERSE FLOOR SUPPORT CORRODED AT BS 1130, RBL 15. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW S RM 51-00. 2 L 7 3 4F A3WE 1996091900317 19960919 00317 WP 1996 9 19 CALA9601309 1 19960901 A 5520 COVER PLATE DOUG DC9 DC932 3022066 WP RT ELEVATOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33506 47765 RT ELEVATOR TRAILING EDGE IN BETWEEN BOTH TABS, GEAR TAB INBOARD END ROD COVER UPPER PLATE WAS FOUND CRACKED. THE OLD D OUBLER WAS REMOVED AND A NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1996091900318 19960919 00318 WP 1996 9 19 CALA9601310 1 19960902 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 237 BULGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33506 47765 INSPECTION FOUND LT FUSELAGE SKIN BULGED ABOVE CUSP LINE AT STA 237, LONGERON 15 TO 18L. THE SKIN PANEL WAS REMOVED AND THE AREA WAS CLEANED, TREATED AND PRIMED. A REPLACEMENT SKIN PANEL WAS FABRICATED AND INSTALLED IAW SRM 51-10-3, 53-30 -0 AND ECRA 5330-01618. 2 L 7 2 4F A6WE 1996091900319 19960919 00319 WP 1996 9 19 CALA9601311 1 19960901 A 5543 5910257501 RUDDER TAB DOUG DC9 DC932 3022066 WP RUDDER DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33506 47765 INSPECTION FOUND RUDDER TAB DELAMINATED. THE RUDDER TAB WAS REMOVED AND REPLACED PER MM 27-20-2. 2 L 7 2 4F A6WE 1996091900320 19960919 00320 WP 1996 9 19 CALA9601312 1 19960902 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 950 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33506 47765 INSPECTION FOUND LT FUSELAGE EXTERIOR SKIN DENTED AT STA 950, STRINGERS 23 AND 24. THE DENT WAS REWORKED AND AN HFEC IN SPECTION WAS ACCOMPLISHED WITH NO CRACKS FOUND. AN INTERNAL DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-04, FIGURE 38. 2 L 7 2 4F A6WE 1996091900321 19960919 00321 NM 1996 9 19 9619726633 1 19960910 A 7797 WIRE BOEING 747 747251B 1384892 NM PWA JT9 JT9D7Q 52054 NE NR 1 ENGINE SHORTED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 633US 21991 02136 DURING TAKEOFF AND APPLICATION OF POWER, THE NR 1 EGT FLUCTUATES OFF SCALE. TAKEOFF WAS ABORTED AT 60 KTS AND AIRCRAFT RETURNED TO THE GATE. MAINTENANCE FOUND OPEN WIRE JUST AFT OF THE MAIN GEAR BOX. REPAIR WAS MADE AND ENGINE RUN-UP CHE CK WAS NORMAL. 2 L 7 4 4F 4 F A20WE E3NE 1996091900322 19960919 00322 NM 1996 9 19 9619732286 1 19960909 A 2751 1812993 FLAP INDICATOR BOEING 727 727251 138408H NM OUTBD TE FLAPS FAILED A NWAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 GL 01 286US 39532 25823 21325 DURING TAKEOFF WHILE RETRACTING FLAPS FROM 5 DEGREES TO 2 DEGREES THE OUTBOARD FLAPS REMAINED AT 5 DEGREES. ISOLATED FL APS AND RETURNED TO BOI. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED OUTBOARD FLAP INDICATOR, PERFORMED SYS TEM GROUND TEST OF FLAPS AND CHECKED OK. 2 L 7 3 4F A3WE 1996091900323 19960919 00323 WP 1996 9 19 9619749978 1 19960911 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP TAIL COMPT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9342 47391 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL SECTION EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CH ECK NORMAL. 2 L 7 2 4F A6WE 1996091900324 19960919 00324 WP 1996 9 19 9619759991 1 19960911 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8957E 47215 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD OVERWING EMERGENCY EXIT LIGHTS VERY DIM. REPLACED BATTERIES, OPERATIO NAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996091900325 19960919 00325 WP 1996 9 19 9619769613 1 19960912 A 3350 CIRCUIT BREAKER DOUG DC9 DC932 3022066 WP COCKPIT MALFUNCTIONED A NWAA K NONE L NO TEST NR NOT REPORTED 1 GL 01 613NW 47438 DURING FLIGHT, EMERGENCY LIGHTS IN MAIN CABIN REMAINED ON WHILE SWITCH WAS IN ARMED POSITION. REPLACED B1-41 CIRCUIT BR EAKER 061641, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996091900326 19960919 00326 NM 1996 9 19 SWAA960941 1 19960909 A 3350 1000679 LIGHT BOEING 737 7372H4 138448C NM COCKPIT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 29SW 21340 DURING SCHEDULED RON CHECK, FOUND COCKPIT EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT PER BOEING M/M. 2 L 7 2 4F A16WE 1996091900327 19960919 00327 NM 1996 9 19 SWAA960942 1 19960909 A 5320 BEAM BOEING 737 7372H4 138448C NM BS 707 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 51SW 21448 DURING SCHEDULED SERVICE CHECK, FOUND TRANSVERSE BEAM CRACKED FWD SIDE AT BS 707 RBL 1. REPAIRED PER SWA RA 1-257-0346. 2 L 7 2 4F A16WE 1996091900328 19960919 00328 NM 1996 9 19 SWAA960943 1 19960910 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 727 OIL CANNING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 74SW 22674 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN OIL CANNING AT BS 727A, BELOW STRINGER 20R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996091900329 19960919 00329 NM 1996 9 19 SWAA960944 1 19960910 A 5320 WEB BOEING 737 7372H4 138448C NM BS 1116-1119 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 74SW 22674 DURING SCHEDULED D-CHECK, FOUND 2 CRACKS AROUND LIGHTENING HOLE IN APU COMPARTMENT AT BS 1116 TO BS 1119, LBL 2.5, WL 25 2. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996091900330 19960919 00330 NM 1996 9 19 SWAA960945 1 19960910 A 5320 CLIP BOEING 737 7372H4 138448C NM BS 1138 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 74SW 22674 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED ON S14L AT BS 1138. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996091900331 19960919 00331 NM 1996 9 19 SWAA960946 1 19960910 A 5312 BULKHEAD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 74SW 22674 DURING SCHEDULED D-CHECK, FOUND BULKHEAD CRACKED AT BS 178, WL 234, RBL 11 AND 13 FROM FASTENER HOLE. REPAIRED PER BOEI NG SRM. 2 L 7 2 4F A16WE 1996091900332 19960919 00332 NM 1996 9 19 SWAA960947 1 19960910 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 500-520 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 74SW 22674 DURING SCHEDULED D-CHECK, FOUND TOP L-ANGLE ON WEB INTERCOSTAL CRACKED AT BS 500B TO 520, BL 0, WL 208. REPAIRED PER BO EING SRM. 2 L 7 2 4F A16WE 1996091900333 19960919 00333 NM 1996 9 19 SWAA960948 1 19960910 A 5312 BULKHEAD SKIN BOEING 737 7372H4 138448C NM BS 1016 OIL CANNING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED C1 CHECK, FOUND BULKHEAD SKIN OIL CANNING AT BS 1016 FWD OF APU GENERATOR CABLES. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996091900334 19960919 00334 NM 1996 9 19 SWAA960949 1 19960909 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED SC CHECK, FOUND SKIN CRACKED 3 AT RT AFT FUSELAGE APPROX 48 FWD OF AFT OUTFLOW VALVE AND 2 ABOVE SKIN L AP. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996091900335 19960919 00335 NM 1996 9 19 SWAA960950 1 19960909 A 3350 6104781 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED RON CHECK, FOUND FWD CABIN EMERGENCY TRACK LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996091900336 19960919 00336 NM 1996 9 19 SWAA960951 1 19960909 A 3350 6042221 CHARGER BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 354SW 25219 DURING SCHEDULED C4 CHECK, FOUND AFT CABIN EMERGENCY TRACK LIGHTS INOP. REPLACED BATTERY CHARGER PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996091900337 19960919 00337 NM 1996 9 19 SWAA960952 1 19960909 A 5312 BULKHEAD CHANNEL BOEING 737 7373H4 1384600 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 356SW 25251 DURING SCHEDULED D-CHECK, FOUND U-CHANNEL CRACKED AT BULKHEAD PANEL SUPPORT BS 727, RBL 5, WL 160. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996091900338 19960919 00338 NM 1996 9 19 SWAA960953 1 19960909 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 787 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 356SW 25251 DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AT AFT CARGO DOOR CUTOUT AT BS 787, RBL 26, WL 156. REPAIRED PER BOEING SRM . 2 L 7 2 4F RT A16WE 1996091900339 19960919 00339 NM 1996 9 19 SWAA960954 1 19960909 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE SCRAPED A SWAA K NONE O OTHER TO TAKEOFF 1 SW 07 396SW 27690 EXPERIENCED TAIL DRAG DURING TAKEOFF CAUSING SKIN DAMAGE TO BOTTOM SIDE AT BS 967, 1006, 986.5 AND 1016, PRESSURE DOME. REPAIRED PER BOEING SRM AND SWA RA 1-353-1512. 2 L 7 2 4F RT A16WE 1996091900340 19960919 00340 NM 1996 9 19 SWAA960955 1 19960909 A 5320 CLIPS BOEING 737 7373T5 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 27690 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS DAMAGED AT BS 747 S4L, BS 994 S6L, BS 663.75 S4L, BS 520 S4R, BS 578 S4L, BS 616 S4L, BS 460 S4R, BS 480 S4L, BS 500A 4R AND BS 500B S4L. REPLACED ALL PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996091900342 19960919 00342 NM 1996 9 19 SWAA960957 1 19960911 A 3230 LATCH BOEING 737 7375H4 138449D NM MLG FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 506SW 24183 AIRCRAFT RETURNED TO HOU DUE TO NOT BEING ABLE TO RAISE GEAR NORMALLY. INSPECTED, REPLACED LANDING GEAR LATCH, PRESSUR E WARNING SWITCH AND RETRACTION TESTED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996091900343 19960919 00343 NM 1996 9 19 SWAA960958 1 19960911 A 3350 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 524SW 26566 DURING SCHEDULED CHECK, FOUND EMERGENCY EXIT LIGHT AT FWD ENTRY INOP. REPLACED LIGHT ASSEMBLY PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996091900344 19960919 00344 NM 1996 9 19 SWAA960959 1 19960911 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 1031 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED BC2 CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 1031 BELOW 20R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996091900345 19960919 00345 NM 1996 9 19 SWAA960960 1 19960911 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 480 LIGHTNING STRIKE A SWAA K NONE C F.O.D. IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED BC2 CHECK, FOUND FUSELAGE SKIN DAMAGED FROM LIGHTNING STRIKE AT BS 480 BELOW S18L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996091900346 19960919 00346 NM 1996 9 19 SWAA960961 1 19960911 A 5330 SKIN BOEING 737 7373H4 1384600 NM L1 DOOR CUTOUT LIGHTNING STRIKE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED TC CHECK, FOUND FUSELAGE SKIN DAMAGED FROM LIGHTNING STRIKE AT BS LOWER CORNER L1 DOOR CUTOUT. REPAIRE D PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996091900347 19960919 00347 NM 1996 9 19 SWAA960962 1 19960911 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 360 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED TC CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 360, BETWEEN S5L AND S6L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996091900348 19960919 00348 NM 1996 9 19 SWAA960963 1 19960911 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 887/500 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED TC CHECK, FOUND FUSELAGE SKIN DENTED AT BS 887 BETWEEN S16 AND 17L, BS 500 S22 TO 23L. REPAIRED PER BO EING SRM. 2 L 7 2 4F RT A16WE 1996091900349 19960919 00349 NM 1996 9 19 UPS96421096 1 19960830 A 5320 SHEAR TIE BOEING 747 747121 1384871 NM BS 1700 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE-C, AFT CARGO COMP FOUND CRACK IN FRAME SHEAR TIE AT SKIN ATTACHMENT AT BS 1700, S 41 AND 42 RT. REMOVED DAMAGED SECTION OF SHEAR TIE AND REPAIRED SHEAR TIE ACC SRM 53-10-04 FIG 3. 2 L 7 4 4F A20WE 1996091900350 19960919 00350 NM 1996 9 19 UPS96421097 1 19960830 A 5320 SHEAR TIE BOEING 747 747121 1384871 NM BS 1680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE-C, AFT CARGO COMP FOUND CRACK IN FRAME SHEAR TIE AT SKIN ATTACHMENT BS 1680, S 41 AND 42 RT. REMOVED DA MAGED SECTION OF SHEAR TIE AND REPAIRED SHEAR TIE ACC SRM 53-10-04 FIG 3. 2 L 7 4 4F A20WE 1996091900351 19960919 00351 NM 1996 9 19 UPS96421098 1 19960828 A 5311 FRAME BOEING 747 747121 1384871 NM BS 1760 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE-C, AFT CARGO COMP FOUND INNER FLANGE OF FRAME CRACKED AT BS 1760, LBL 61, BETWEEN S41 AND 42 LT NEAR SID E GUIDE. REMOVED CRACKED SECTION OF FRAME INNER FLANGE AND REPAIRED FRAME INNER FLANGE ACC SRM 51-40-03. 2 L 7 4 4F A20WE 1996091900352 19960919 00352 NM 1996 9 19 UPS96421099 1 19960828 A 5311 FRAME BOEING 747 747121 1384871 NM BS 1800 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE-C, AFT CARGO COMP FOUND INNER FLANGE OF FRAME CRACKED AT BS 1800 BETWEEN S40 AND 39 RT. REMOVED CRACKED SECTION OF FRAME INNER FLANGE AND REPAIRED FRAME INNER FLANGE ACC SRM 51-40-03. 2 L 7 4 4F A20WE 1996091900353 19960919 00353 NM 1996 9 19 UPS96421100 1 19960828 A 5312 BULKHEAD WEB BOEING 747 747121 1384871 NM BS 2160 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE-C, BULK CARGO COMP FOUND CRACK IN BULKHEAD WEB AT BS 2160, RBL 56 WL 168. REMOVED DAMAGED SECTION OF BU LKHEAD WEB AND REPAIRED WEB ACC SRM 51-40-02 FIG 01. 2 L 7 4 4F A20WE 1996091900354 19960919 00354 NM 1996 9 19 UPS96421101 1 19960828 A 5320 SHEAR TIES BOEING 747 747121 1384871 NM BS 1600/1580 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE-C, AFT CARGO COMP FOUND FRAME SHEAR TIE AT ATTACHMENTS CRACKED AT BS 1600 AND BS 1580, BETWEEN S40 AND S 41 RT. REMOVED CRACKED FLANGES OF SHEAR TIES AND REPAIRED SHEAR TIE ACC SRM 53-10-04, FIG 3. 2 L 7 4 4F A20WE 1996091900355 19960919 00355 NM 1996 9 19 UPS96421102 1 19960829 A 5311 FRAME BOEING 747 747121 1384871 NM BS 1580 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE-C, AFT CARGO COMP FOUND CRACK IN FRAME INNER FLANGE AT BS 1580, S29 RT. REMOVED DAMAGED SECTION OF FRAM E INNER FLANGE AND REPAIRED FRAME INNER FLANGE ACC SRM 51-40-03. 2 L 7 4 4F A20WE 1996091900356 19960919 00356 NM 1996 9 19 UPS96421103 1 19960829 A 5330 SKIN BOEING 747 747121 1384871 NM BS 1670/1695 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE-C, AFT CARGO COMP FOUND HEAVY CORROSION ON INTERNAL SKIN NEAR S30 RT AT BS 1678, BS 1690 AND BS 1695. R EMOVED CORRODED SECTIONS OF SKIN PANEL BY MAKING A CUTOUT 21 BY 3.5 AND REPARED SKIN PANEL ACC SRM 53-30-03, FIG 1. 2 L 7 4 4F A20WE 1996091900357 19960919 00357 NM 1996 9 19 UPS96521095 1 19960911 A 3230 26702889 SEQUENCE VLV BOEING 757 75724APF 1384969 NM NLG DEFECTIVE A IPXA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 455UP 25476 INSPECTION TYPE N/A, ON APPROACH NOSE GEAR FAILED TO EXTEND AND GEAR DISAGREE MSG DISPLAYED, ALT GEAR EXTEND SELECTED AN D GEAR DEPLOYED. FERRIED A/C TO SDF. REMOVED AND REPLACED NOSE GEAR DOOR SEQUENCE VALVE PER MM 32-34-05. PERFORMED TE ST OF NOSE GEAR EXTENSION AND RETRACTION, SYSTEM OPS CHECKS GOOD. 2 L 7 2 4F RT A2NM 1996091900358 19960919 00358 WP 1996 9 19 UPS96821104 1 19960829 A 5320 4641324N FITTING DOUG DC8 DC873F 302199F WP FS 1690 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-CS2, FITTING CRACKED AT FS 1690 LONGERON 26L. REPLACED FITTING PER SRM 51-1-20D AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1996091900359 19960919 00359 WP 1996 9 19 UPS96821105 1 19960826 A 5400 3756842 ANGLE DOUG DC8 DC873F 302199F WP NR 4 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-CS2, NR 4 PYLON DRAG ANGLE CRACKED .25 INCH LONG PAST STOP DRILL. REPAIRED ANGLE PER TASK CARD 8040-01, STEP 4. 2 L 7 4 4F RT 4A25 1996091900360 19960919 00360 WP 1996 9 19 UPS96821106 1 19960824 A 5240 9751065 FITTING DOUG DC8 DC873F 302199F WP AFT SERV DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-CS2, AFT SERVICE DOOR FITTING CRACKED INSIDE SECOND LIGHTENING HOLE FROM TOP ON FWD SIDE. REPLACED FITT ING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996091900361 19960919 00361 WP 1996 9 19 UPS96821107 1 19960827 A 5755 56551682 PANEL DOUG DC8 DC873F 302199F WP RT NR 4 SPOILER DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-CS2, RIGHT HAND WING NR 4 SPOILER PANEL DELAMINATED. REPLACED SPOILER PANEL PER MM 27-61-01. 2 L 7 4 4F RT 4A25 1996091900362 19960919 00362 WP 1996 9 19 UPS96821108 1 19960824 A 5320 SHEAR TIE DOUG DC8 DC873F 302199F WP FS 1100 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-CS2, SHEAR TIE CRACKED AT HOLE, FS 1100 LONGERON 11L. REPLACED SHEAR TIE SECTION PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996091900363 19960919 00363 WP 1996 9 19 UPS96821109 1 19960822 A 5752 5717798501 TAB DOUG DC8 DC873F 302199F WP LT AILERON DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-CS2, LT AILERON GEAR TAB DELAMINATED. REPLACED TAB ASSY PER MM 27-13-01. 2 L 7 4 4F RT 4A25 1996091900364 19960919 00364 WP 1996 9 19 UPS96821111 1 19960830 A 5320 5773275231 SUPPORT DOUG DC8 DC873F 302199F WP FS 717 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-CS2 FLOOR BEAM SUPPORT CRACKED AT FS 717 UNDER SEAT TRACK NR 5. REPLACED SUPPORT ASSY PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996091900365 19960919 00365 WP 1996 9 19 UPS96821112 1 19960830 A 5315 FLOOR BEAM DOUG DC8 DC873F 302199F WP FS 8 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-CS2, WEBBING ON TOP OF FLOOR BEAM IS CRACKED FS 8, RBL 1. REPAIRED WEB PER SRM DC8-5350-7876. 2 L 7 4 4F RT 4A25 1996091900366 19960919 00366 WP 1996 9 19 UPS96821113 1 19960826 A 5730 57583825 SKIN DOUG DC8 DC873F 302199F WP WS 69.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-CS2, LT WING UPPER SKIN HAS A 3.25 INCH LONG CRACK AT STA 69.5 REAR SPAR. REPAIRED SKIN PER SRM 57-2-1, FIG 20. 2 L 7 4 4F RT 4A25 1996091900367 19960919 00367 EU 1996 9 19 WWMA9600070 1 19960911 A 3240 AT645205 CONTROL CABLE SAAB SF340 340B 7860101 EU PARKING BRAKE DEFECTIVE A WWMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 15 338SB 340B338 CREW REPORTS THAT THE PARKING BRAKE FRICTION LOCK SLIPS, RELEASING THE PARKING BRAKE UNEXPECTEDLY. MAINTENANCE REPLACED THE INNER PARKING BRAKE TELEFLEX CABLE AND RELEASED THE AIRCRAFT TO SERVICE WITH NO FURTHER PROBLEMS. 2 L 7 2 4T RT A52EU 1996091900368 19960919 00368 NM 1996 9 19 96FDEA01467 1 19960909 A 5330 SKIN BOEING 727 72722 1384002 NM BS 1163 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 167FE 18864 FUSE SKIN BULGING AROUND FASTENERS STA 1163 STR 27 AND 26L. CUT OUT SKIN, REMOVED CORROSION, INSTALLED DOUBLER PER SRM 53-30-3. 2 L 7 3 4F A3WE 1996091900369 19960919 00369 NM 1996 9 19 96FDEA01468 1 19960904 A 5330 SKIN BOEING 727 72725C 138400H NM BS 595 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 167FE 18864 BULGE IN SKIN STR 27L AT STA 595L. REMOVED SECTION OF SKIN, REMOVED DEBRIS BETWEEN BELT FRAME AND SKIN, NO CORROSION NO TED. FAB DOUBLER, TREATED, PAINTED AND INSTALLED REPAIR PARTS PER SRM 53-30-3 PG 74 TO 75. 2 L 7 3 4F A3WE 1996091900370 19960919 00370 NM 1996 9 19 96FDEA01469 1 19960904 A 5330 SKIN BOEING 727 72722 1384002 NM BS 1080 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 167FE 18864 FUSELAGE EXT, SKIN BULGE AT STR 29L AFT OF STA 1080 FRAME. REMOVED CORROSION, INSTALLED FILLER AND DOUBLER PER SRM 53-3 0-3, SEALED EDGES OF DOUBLER PER SRM 51-20-04. 2 L 7 3 4F A3WE 1996091900371 19960919 00371 NM 1996 9 19 96FDEA01470 1 19960912 A 5315 65208276 FLOOR BEAM BOEING 727 72725 1384006 NM BS 660 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR0365 AND 022, CORROSION (C53-224-02, -1) AROUND FASTENER HOLES ON FLOOR BEAM TOP CHORD AT BS 660 RBL 11 AND 35 WL 208. 2 L 7 3 4F A3WE 1996091900372 19960919 00372 NM 1996 9 19 96FDEA01471 1 19960912 A 5315 BAC1518338 FLOOR BEAM BOEING 727 72725 1384006 NM BS 380 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR0369 AND 023, CORROSION (C53-224-01) AROUND FASTENER HOLE ON UNDERSIDE OF FLOOR BEAM TOP CHORD BS 380 LBL 25 WL 208, O UT OF LIMITS. *S/D* REMOVED DAMAGED AREA AROUND FASTENER HOLE ON UNDERSIDE OF FLOOR BEAM TOP CHORD AT BS 380 LBL 25 WL 208. REPAIRED PER FED EX SRM 53-10-8. 2 L 7 3 4F A3WE 1996091900373 19960919 00373 NM 1996 9 19 96FDEA01472 1 19960912 A 5320 6522217954 DOORWAY FRAME BOEING 727 72725 1384006 NM BS 215 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR0558 AND 024, CORROSION (C53-111-01-1) ON DOOR CUTOUT SIDE FRAME AT BS 215 RBL 16 WL 167. *S/D* REMOVED DAMAGED SIDE FRAME WEB AND INSTALLED NEW SIDE FRAME WEB IAW FED EX SRM 51-10-1. 2 L 7 3 4F A3WE 1996091900374 19960919 00374 NM 1996 9 19 96FDEA01437 1 19960906 A 5315 65308331 FLOOR BEAM BOEING 727 72725 1384006 NM BS 1030 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR 0292 AND 003, CORROSION (C53-224-01, -3) AROUND NUTPLATE HOLES ON BS 1030 UPPER CHORD RBL 21 TO LBL 21 WL 208. *S/D* REPAIRED OUT OF LIMITS UPPER CHORD IAW FEDEX SRM 53-10-8. 2 L 7 3 4F A3WE 1996091900375 19960919 00375 NM 1996 9 19 96FDEA01460 1 19960909 A 2421 750860 IDG DOUG MD11 MD11F 3023600 NM NR 3 ENGINE FAILED A FDEA A B J UNSCHED LANDING EMER. DESCENT DUMP FUEL H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 25 612FE 48605 THIS A/C HAD THE NR 2 IDG DEFERRED. IN FLIGHT THE NR 3 IDG WENT INOP, THE CREW DID AN AIR TURNBACK INTO NADI. PER THE MEL YOU CANNOT DEFER TWO IDG AT THE SAME TIME. REMOVED AND REPLACED THE NR 3 IDG. 2 L 7 3 4F RT A22WE 1996091900376 19960919 00376 NM 1996 9 19 96FDEA01473 1 19960912 A 2612 894120 ELEMENT BOEING 727 72725F NM NR 1 ENGINE FALSE WARNING A FDEA E ENGINE SHUTDOWN N FALSE WARNING AP APPROACH 1 SO 25 204FE 22926 NR 1 MASTER FIRE WARNING ILLUMINATED FOLLOWED BY NR 1 ENGINE FIRE INDICATIONS. EMERGENCY ACTIONS ACCOMPLISHED, LIGHTS W ENT OUT, FIRE TEST NORMAL. AFTER LANDING FIRE LIGHT NR 1 REILLUMINATED. CREW AGGRESSED AIRCRAFT, EXITED AIRCRAFT VIA E SCAPE SLIDE. TROUBLESHOT AND FOUND FIRE DETECTION ELEMENT BAD. REMOVED AND REPLACED FIRE DETECTION ELEMENT PER MM 26-1 1-12. TESTED FIRE DETECTION SYSTEM, SYSTEM GROUND TESTED GOOD PER M/M 26-11-01. 2 L 7 3 4F RT A3WE 1996091900377 19960919 00377 NM 1996 9 19 96FDEA01474 1 19960913 A 2782 CONNECTOR BOEING 727 72725 1384006 NM NR 7 SLAT ACT DIRTY A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 134FE 19852 ON FLAP RETRACTION FROM 2 DEGREES TO 0 DEGREES THE AMBER LEADING EDGE FLAP LIGHT REMAINED ON. SECOND OFFICER'S AUXILIAR Y PANEL POSITION INDICATOR SHOWED THAT THE NR 7 LEADING EDGE DEVICE WAS INTRANSIT. COMPLETED CHECKLIST FOR LEADING EDGE DEVICE FAILURE ON FLAP RETRACTION. LEADING EDGE DEVICES NORMAL AT FLAP 5 DEGREES PER CHECKLIST LANDED WITH 30 DEGREES FLAP NORMAL LEADING EDGE DEVICES. CLEANED NR 7 SLAT ACTUATOR CANNON PLUG, OPERATIONAL CHECKED SEVERAL TIMES ON GROUND A ND OPERATIONAL CHECK GOOD. 2 L 7 3 4F A3WE 1996091900378 19960919 00378 NM 1996 9 19 96FDEA01475 1 19960913 A 5320 651841411 WEB BOEING 727 72725 1384006 NM BS 234-245 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 509FE 18280 NR 0626 AND 018, WHILE ACCESSING FOR NR0623, FOUND WEB DAMAGED BS 234 TO 245 RBL 24 WL 156. 2 L 7 3 4F A3WE 1996091900379 19960919 00379 WP 1996 9 19 ABXA9600623 1 19960911 A 3260 DOOR OPEN LIGHT DOUG DC9 DC931 3022065 WP LANDING GEAR ILLUMINATED A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 944AX 47550 GEAR UPLATCH CHECK WAS GOOD. ABOVE APPROXIMATELY 11,000 FT, THE GEAR DOOR OPEN LIGHT ILLUMINATED. RECYCLED THE LANDING GEAR, THE LIGHT REMAINED ILLUMINATED. ON DESCENT, BELOW 11,000 FT, THE GEAR DOOR OPEN LIGHT EXTINGUISHED. CHECKED MAI N LANDING GEAR DOOR RIGGING AND CLEARANCES, NO DISCREPANCIES NOTED PER DC-9 SUPP MM 32-60-3. 2 L 7 2 4F A6WE 1996091900380 19960919 00380 WP 1996 9 19 ABXA9600624 1 19960910 A 2510 SEAT MECH DOUG DC8 DC863 302198A WP RT COCKPIT LACK OF LUBE A ABXA K NONE O OTHER CR CRUISE 1 GL 23 818AX 46075 FORE AND AFT LATCH ON FIRST OFFICER'S SEAT WILL NOT ENGAGE, SLIPS. CLEANED AND LUBRICATED FORE AND AFT HANDLE, CABLE AN D TRACK SYSTEM, OPS CHECKED GOOD IAW DC8 MM 25-10-0. 2 L 7 4 4F 4A25 1996091900381 19960919 00381 WP 1996 9 19 ABXA9600625 1 19960910 A 3350 5D00015 CIRCUIT BREAKER DOUG DC8 DC861 3021952 WP COCKPIT MALFUNCTIONED A ABXA O OTHER L NO TEST CR CRUISE 1 GL 23 852AX 46016 EMERGENCY EXIT LIGHT ILLUMINATED AND WOULD NOT TURN OFF UNTIL RESETTING THE EMERGENCY EXIT LIGHT CONTROL CIRCUIT BREAKER . FOUND EMERGENCY EXIT LIGHT CONTROL CIRCUIT BREAKER D-1 WEAK AND INTERMITTENT. REPLACED CIRCUIT BREAKER, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1996091900382 19960919 00382 WP 1996 9 19 ABXA9600626 1 19960911 A 5610 WINDOW LOCK DOUG DC8 DC861 3021952 WP LT COCKPIT LACK OF LUBE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 CAPTAIN'S CLEAR VIEW WINDOW WILL NOT OPEN. FREED STUCK UPPER LOCK ON CAPTAIN'S CLEAR VIEW WINDOW, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1996091900383 19960919 00383 WP 1996 9 19 MWEA96461 1 19960912 A 5320 5911412 DOUBLERS DOUG DC9 DC932 3022066 WP FWD BAG PIT NOT INSTALLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, STRUCTURAL HARD POINTS TO BE INSTALLED IN FWD BAG PIT PER DAC DRAWING NR 5911412 AT BELLY STATIONS 396, 339 , 453 AND 510. INSTALLED ALL FOUR ANTENNA ATTACH DOUBLERS IAW DAC DWG 5911412. 2 L 7 2 4F A6WE 1996091900384 19960919 00384 WP 1996 9 19 MWEA96462 1 19960912 A 5280 491450 HINGE DOUG DC9 DC932 3022066 WP LT MLG DOOR WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, LT MAIN GEAR DOOR ATTACH HINGE WAS FOUND TO HAVE EXCESSIVE PLAY AND CRACKED LOBE. REPLACED HINGE IAW SRM 5 2-05, FIG 15. 2 L 7 2 4F A6WE 1996091900385 19960919 00385 WP 1996 9 19 MWEA96463 1 19960912 A 5320 FORMER DOUG DC9 DC932 3022066 WP BS 660 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, TWO FORMERS FOUND CRACKED IN WING CENTER SECTION AREA LT AND RT OUTBD END AT STA 660. FABRICATED TWO NEW P ARTS, HEAT TREATED AND INSTALLED IAW 53-03 PG 31, FIG 12. 2 L 7 2 4F A6WE 1996091900386 19960919 00386 WP 1996 9 19 MWEA96464 1 19960912 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 389-408 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, FLOOR BEAMS AT STA 389 AND 408 LOWER FLANGE WERE DAMAGED FROM FWD CARGO DOOR HITTING THEM. FABRICATED PART S FOR REPAIRS AND INSTALLED IAW SRM 53-05 FIG 86, SHEET 2. 2 L 7 2 4F A6WE 1996091900387 19960919 00387 WP 1996 9 19 MWEA96465 1 19960912 A 5320 PANEL DOUG DC9 DC932 3022066 WP LT MLG WW CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, LT WHEEL WELL SLANT PRESSURE PANEL WAS FOUND TO HAVE MODERATE CORROSION AROUND A BOTTOM ROW FASTENER AND WI RE BUNDLE ATTACH CLIP. FABRICATED A NEW PANEL AND CLIP, INSTALLED IAW SRM 53-11-3, FIG 12. 2 L 7 2 4F A6WE 1996091900388 19960919 00388 WP 1996 9 19 MWEA96466 1 19960912 A 5320 CLIP DOUG DC9 DC932 3022066 WP BS 965 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, EXFOLIATION CORROSION FOUND ON INTERCOSTAL ATTACH CLIP AFT CARGO COMPT STA 965, LONG 29R. INSTALLED A FABR ICATED ATTACH CLIP IAW SRM 51-30-5. 2 L 7 2 4F A6WE 1996091900389 19960919 00389 WP 1996 9 19 MWEA96467 1 19960912 A 5311 FRAME DOUG DC9 DC932 3022066 WP AFT FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, LIGHT CORROSION WAS FOUND ON FRAME AFT SIDE AFT CARGO COMPT FROM LONG 24R TO 29R. FABRICATED AND INSTALLED A REPAIR IAW SRM 53-03, PAGE 4A FIG 2A. 2 L 7 2 4F A6WE 1996091900390 19960919 00390 WP 1996 9 19 MWEA96468 1 19960912 A 5313 5911423 LONGERON DOUG DC9 DC932 3022066 WP BS 965-996/970 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, LONGERON 20 AND 21R WERE FOUND CORRODED AT STA 965 TO 996 AND 970. REPLACED LONGERONS IAW SRM 53-11-3. 2 L 7 2 4F A6WE 1996091900391 19960919 00391 WP 1996 9 19 MWEA96469 1 19960912 A 5320 4914957 CLIPS DOUG DC9 DC932 3022066 WP BS 992 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, LONG 20 AND 21L HAD CORROSION AT STA 992 AND AT SHOVEL CLIPS. REPLACED CLIPS AND LONGERON IAW SRM 53-11-3. 2 L 7 2 4F A6WE 1996091900392 19960919 00392 WP 1996 9 19 MWEA96470 1 19960912 A 3800 LAV SERVICE PNL DOUG DC9 DC932 3022066 WP AFT FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, THE LAV SERVICE PANEL PAN WAS FOUND CRACKED AT THE RT DRAIN HANDLE BOSS. REPAIRED CRACK IAW SRM 53-01 FIG 2, SHEET 3. 2 L 7 2 4F A6WE 1996091900393 19960919 00393 WP 1996 9 19 MWEA96471 1 19960912 A 5310 DOOR PAN DOUG DC9 DC932 3022066 WP AFT CABIN DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, AFT CABIN DOOR PAN ON LT SIDE WAS FOUND CRACKED AT BEAM NR 2. ALSO, SUPPORT ANGLE WAS CRACKED. REPAIRED T HE PAN IAW DAC TELEX MSP-SVC-643/DAI DATED 2 AUG 96. ANGLE INSTALLED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 1996091900394 19960919 00394 WP 1996 9 19 MWEA96472 1 19960912 A 5320 5917463 JAMB DOUG DC9 DC932 3022066 WP VENT DOOR JAMB CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, VENTRAL DOOR JAMB PAN WAS CRACKED IN UPPER LT CORNER AND LWR FWD EDGE WAS EXFOLIATED. REPLACED DOOR PAN IA W SRM 51-30-2. 2 L 7 2 4F A6WE 1996091900395 19960919 00395 WP 1996 9 19 MWEA96473 1 19960912 A 5320 5917579 DOOR FRAME DOUG DC9 DC932 3022066 WP VENT DOOR JAMB CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, VENTRAL DOOR JAMB FRAME IS CRACKED AT UPPER RT STRIKER PLATE FOR DOOR STOP. REPLACED DOOR JAMB FRAME IAW S RM 51-30-2. 2 L 7 2 4F A6WE 1996091900396 19960919 00396 WP 1996 9 19 MWEA96474 1 19960912 A 5320 5910130 DOUBLER DOUG DC9 DC932 3022066 WP VENT DOOR JAMB CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, LT AND RT UPPER VENTRAL DOOR JAMB DOUBLERS WERE FOUND CRACKED. REPLACED DOUBLERS IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1996091900397 19960919 00397 WP 1996 9 19 MWEA96475 1 19960912 A 5313 SR09530128 LONGERON DOUG DC9 DC932 3022066 WP BS 699 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, LONG 5L AND 6L WERE FOUND CRACKED AT FRAME ATTACH POINTS AT STA 699. REPLACED SECTION OF LONGERONS IAW DAC DWG SR09530128. 2 L 7 2 4F A6WE 1996091900398 19960919 00398 WP 1996 9 19 MWEA96476 1 19960912 A 5313 SR09530128 LONGERON DOUG DC9 DC932 3022066 WP BS 756 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, LONGERON 4L AND 3R WERE FOUND CRACKED AT FRAME ATTACH POINTS AT STA 756. SPLICED IN NEW SECTIONS OF LONGER ON IAW DAC DWG SR09530128. 2 L 7 2 4F A6WE 1996091900399 19960919 00399 WP 1996 9 19 MWEA96477 1 19960912 A 5320 WINDOW FRAME DOUG DC9 DC932 3022066 WP BS 600 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, A CABIN WINDOW FRAME FWD LOWER LEG WAS FOUND CRACKED APPROX .1875 INCH FROM EDGE AT STA 600, LONG 15R. REP AIRED CRACK IAW SRM 53-01 FIG 2, SHEET 4. 2 L 7 2 4F A6WE 1996091900400 19960919 00400 WP 1996 9 19 MWEA96478 1 19960912 A 5315 FLOOR BEAM DOUG DC9 DC932 3022066 WP BS 313.12 CORROSION A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, FLOOR BEAM UPPER LEG AT STA 313, 12 INCHES INBD OF LONG 18L HAD A 1 INCH AREA OF EXFOLIATION CORROSION. FA BRICATED AND INSTALLED A REPAIR IAW SRM 53-05, FIG 20A. 2 L 7 2 4F A6WE 1996091900401 19960919 00401 WP 1996 9 19 MWEA96479 1 19960912 A 5320 5911415 FITTING DOUG DC9 DC932 3022066 WP BS 640-658 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, FOUND PREVIOUS DAMAGE TO LONG 2R, 3R HAT CHANNEL LIP BETWEEN STA 640 AND 658 FITTINGS FOR ANTI-COLLISION LI GHT MOD. REPAIRED DAMAGED AREAS IAW SRM 53-01, FIG 2 SHEET 4. 2 L 7 2 4F A6WE 1996091900402 19960919 00402 WP 1996 9 19 MWEA96480 1 19960912 A 5400 ANGLE DOUG DC9 DC932 3022066 WP RT PYLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, RT PYLON TO FUSELAGE ATTACH ANGLE WAS FOUND CRACKED IN 2 PLACES FWD EDGE OF LEADING EDGE. INSTALLED A REPA IR IAW SRM 54-04, FIG 10. 2 L 7 2 4F A6WE 1996091900403 19960919 00403 WP 1996 9 19 MWEA96481 1 19960912 A 5400 ANGLE DOUG DC9 DC932 3022066 WP LT PYLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, LT PYLON TO FUS UPPER ATTACH ANGLE WAS FOUND CRACKED AT STA 935, 965 AND 1019. COMPLETED REPAIRS IAW SRM 5 4-04, FIG 10. 2 L 7 2 4F A6WE 1996091900404 19960919 00404 WP 1996 9 19 MWEA96482 1 19960912 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 1076 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, AFT ACCESSORY FRAME WAS FOUND CRACKED AT STA 1076 AT LONG 2L AND 2R. REPAIRED FRAMES IAW SRM 53-03, FIG 32 . 2 L 7 2 4F A6WE 1996091900405 19960919 00405 WP 1996 9 19 MWEA96483 1 19960912 A 5320 5910130 DOUBLER DOUG DC9 DC932 3022066 WP VENT DOOR JAMB CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, A 1.5 INCH CRACK WAS FOUND IN VENTRAL DOOR JAMB ANGLE DOUBLER BOTTOM RT END. REPAIRED ANGLE DOUBLER IAW SR M 51-30. 2 L 7 2 4F A6WE 1996091900406 19960919 00406 WP 1996 9 19 MWEA96484 1 19960912 A 5320 5910130 DOUBLER DOUG DC9 DC932 3022066 WP VENTRAL STAIR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, A 1 INCH CRACK WAS FOUND IN LT LOWER VENTRAL DOOR JAMB CORNER ON AFT SIDE. FABRICATED AND INSTALLED A REPA IR IAW SB 53-137R4. 2 L 7 2 4F A6WE 1996091900407 19960919 00407 WP 1996 9 19 MWEA96485 1 19960912 A 5260 STEPS DOUG DC9 DC932 3022066 WP AFT AIRSTAIRS CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, THE AFT AIRSTAIR THREE STEPS FROM BOTTOM HAS CRACKED RT SIDE. COMPLETED A REPAIR IAW SRM 52-01, SHEET 4. 2 L 7 2 4F A6WE 1996091900408 19960919 00408 WP 1996 9 19 MWEA96486 1 19960912 A 5711 SPAR CAP DOUG DC9 DC932 3022066 WP WS 295.324 CORROSION A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, RT WING LOWER FWD FLANGE OF SPAR CAP WAS FOUND WITH SEVERE EXFOLIATION CORROSION FROM STA XRS 295 TO 324. C OMPLETED REPAIR IAW DAC TELEX SVC-MSP-0630/RMK DATED 31 JULY 96. 2 L 7 2 4F A6WE 1996091900409 19960919 00409 WP 1996 9 19 MWEA96487 1 19960912 A 5711 SPAR DOUG DC9 DC932 3022066 WP WS 167/200-210 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, FOUND RT WING HAD EXFOLIATION CORROSION IN TWO PLACES ON FRONT SPAR FWD LOWER TANG AT STA XRS-167 AND XRS-2 00-210. COMPLETED REPAIRS IAW DAC TELEX DATED 6 AUG 96. 2 L 7 2 4F A6WE 1996091900410 19960919 00410 WP 1996 9 19 MWEA96488 1 19960912 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 980 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, A FRAME WAS FOUND CRACKED WHERE IT ATTACHES TO THE LONGERON AT FRAME STA 980, LONG 17R. REPAIRED THE FRAME IAW SRM 53-03, FIG 32. 2 L 7 2 4F A6WE 1996091900411 19960919 00411 WP 1996 9 19 MWEA96489 1 19960912 A 5312 BULKHEAD WEB DOUG DC9 DC932 3022066 WP BS 965 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, RT LAV FWD BULKHEAD WAS FOUND CRACKED IN NUMEROUS PLACES AT THE LOWER EDGE FWD SIDE STA 965. REPAIRED THE BULKHEAD PER SRM 53-03 FIG 21. 2 L 7 2 4F A6WE 1996091900412 19960919 00412 WP 1996 9 19 MWEA96490 1 19960912 A 5320 2777976 ANGLE DOUG DC9 DC932 3022066 WP BS 975 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, RT LAV CUSP ANGLE WAS FOUND SEVERELY EXFOLIATED AT STA 975. REPLACED CORRODED SECTION OF CUSP ANGLE PER SR M 53-05, FIG 25. 2 L 7 2 4F A6WE 1996091900413 19960919 00413 WP 1996 9 19 MWEA96491 1 19960912 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 992 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, FUSELAGE SKIN WAS FOUND CRACKED IN LT LAV AT STA 992. REPAIRED THE SKIN IAW SRM 53-04, FIG 46. 2 L 7 2 4F A6WE 1996091900414 19960919 00414 WP 1996 9 19 MWEA96492 1 19960912 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS990 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, LT CUSP ANGLE IN LT LAV AREA WAS FOUND MODERATELY EXFOLIATED AT STA 990. COMPLETED A REPAIR TO CUSP ANGLE IAW SRM 53-05, FIG 25. 2 L 7 2 4F A6WE 1996091900415 19960919 00415 WP 1996 9 19 MWEA96493 1 19960912 A 5313 2777922 LONGERON DOUG DC9 DC932 3022066 WP BS 965 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, LONG 17R WAS FOUND CRACKED AT STA 965. COMPLETED A REPAIR IAW SRM 53-02, FIG 2. 2 L 7 2 4F A6WE 1996091900416 19960919 00416 WP 1996 9 19 MWEA96494 1 19960912 A 5311 FRAME DOUG DC9 DC932 3022066 WP FWD CARGO COMPT CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, MODERATE CORROSION FOUND ON THE AFT SIDE OF FRAME 389 IN FWD CARGO COMPT AT LONGERON 30. REPAIRED FRAME IA W SRM 51-10-2A. 2 L 7 2 4F A6WE 1996091900417 19960919 00417 WP 1996 9 19 MWEA96495 1 19960912 A 5320 JAMB DOUG DC9 DC932 3022066 WP BS 380 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, AN INTERCOSTAL WAS FOUND CRACKED IN FWD CARGO DOOR FWD JAMB AT STA 380, CRACKED PAST A STOP DRILL. COMPLET ED REPAIR IAW SRM 53-01. 2 L 7 2 4F A6WE 1996091900418 19960919 00418 WP 1996 9 19 MWEA96496 1 19960912 A 5414 SKIN DOUG DC9 DC932 3022066 WP LT PYLON CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, FOUND A SMALL AREA OF SURFACE CORROSION ON BOTTOM SKIN OF LT PYLON. FOUND CORROSION OUT OF LIMITS AND FABR ICATED A REPAIR IAW SRM 54-01, FIG 2 AND INSTALLED IAW SRM 51-30. 2 L 7 2 4F A6WE 1996091900419 19960919 00419 WP 1996 9 19 MWEA96497 1 19960912 A 5532 SKIN DOUG DC9 DC932 3022066 WP VERT STAB CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, LT AND RT SIDES OF THE VERTICAL STAB CANOE AFT END EXTERNAL SKINS WERE HEAVILY CHAFED FROM THE FAIRINGS. R EPLACED SKINS IAW SRM 55-31-0. 2 L 7 2 4F A6WE 1996091900420 19960919 00420 WP 1996 9 19 MWEA96498 1 19960912 A 5320 BRACKET DOUG DC9 DC932 3022066 WP AFT ACCESSORY CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, STRUCTURE UNDER THE RT CATWALK RETRACT CABLE ARM SUPPORT BRACKET WAS FOUND CRACKED. REPAIRED STRUCTURE IAW SRM 53-01 FIG 2, SHEET 4. 2 L 7 2 4F A6WE 1996091900421 19960919 00421 WP 1996 9 19 MWEA96499 1 19960912 A 5320 2777922 STIFFENER DOUG DC9 DC932 3022066 WP BS 1132 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, A STIFFENER WAS FOUND EXFOLIATED IN AFT ACCESS COMPARTMENT ON CANTED FRAME WEB AT STA 1132 AND LONG 12L. I NSTALLED NEW STIFFENER IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1996091900422 19960919 00422 WP 1996 9 19 MWEA96500 1 19960912 A 5320 ANGLE DOUG DC9 DC932 3022066 WP AFT ACC COMPT CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, STIFFENERS IN AFT ACCESS COMPT OF FRAME 1132 WEB RT SIDE AT LONG 12 AND 13 RT WERE FOUND SEVERELY CORRODED. CLEANED UP THE CORROSION AND INSTALLED A NEW L-ANGLE IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1996091900423 19960919 00423 WP 1996 9 19 MWEA96501 1 19960912 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 1121 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 57730 DURING INSP, A CANTED FRAME FWD ATTACH ANGLE WAS FOUND CRACKED AT STA 1121 BETWEEN LONG 17 AND 18R APPROX 6 INCHES. FAB RICATED AND INSTALLED A REPAIR IAW SRM 53-01, FIG 2 SHEET 4. 2 L 7 2 4F A6WE 1996091900424 19960919 00424 WP 1996 9 19 MWEA96502 1 19960912 A 5531 SPAR CAP DOUG DC9 DC932 3022066 WP RT ELEVATOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, A 1.25 INCH CRACK FOUND IN RT ELEVATOR UPPER SPAR CAP AT STA XE151. COMPLETED A REPAIR IAW SRM 55-02 FIG 9 , CONFIGURATION -503. 2 L 7 2 4F A6WE 1996091900425 19960919 00425 WP 1996 9 19 MWEA96503 1 19960912 A 5711 SPAR DOUG DC9 DC932 3022066 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, RT WING REAR SPAR LOWER TEE CAP HORIZONTAL LEG BLEND OUT REPAIR AT STA XRS 179 REQUIRED EVALUATION. FABRIC ATED AND INSTALLED A REPAIR IAW SRM 57-09, FIG 11. 2 L 7 2 4F A6WE 1996091900426 19960919 00426 WP 1996 9 19 MWEA96504 1 19960912 A 5720 ACCESS PANEL DOUG DC9 DC932 3022066 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, RT WING LARGE LEADING EDGE LOWER ACCESS PANEL WAS FOUND TO HAVE CORROSION AT STA XRS 140. FABRICATED A REP AIR AND INSTALLED IAW SRM 57-01. 2 L 7 2 4F A6WE 1996091900427 19960919 00427 WP 1996 9 19 MWEA96505 1 19960912 A 5712 RIB DOUG DC9 DC932 3022066 WP WS 164 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, LT WING RIB STA 164 BOTTOM INBD FLANGE AT STRINGER 16 WAS FOUND CORRODED. COMPLETED REPAIR IAW DAC TELEX S VC-MSP-0667/DLP DATED 9 AUG 96. 2 L 7 2 4F A6WE 1996091900428 19960919 00428 WP 1996 9 19 MWEA96506 1 19960912 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP BS 180 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, A CRACKED INTERCOSTAL WAS FOUND AT STA 180, 18 INCHES LEFT OF CENTER UNDER THE SUBFLOOR. REPAIRED THE INTE RCOSTAL IAW SRM 53-01, FIG 2. 2 L 7 2 4F A6WE 1996091900429 19960919 00429 WP 1996 9 19 MWEA96507 1 19960912 A 5313 2777922 LONGERON DOUG DC9 DC932 3022066 WP BS 699 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, LONG 4L WAS FOUND CRACKED AT FRAME ATTACH POINT AT STA 699. REPAIRED LONGERON 4L IAW DWG SR09530128. 2 L 7 2 4F A6WE 1996091900430 19960919 00430 WP 1996 9 19 MWEA96508 1 19960912 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 313 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, FWD CARGO PIT STA 313 FRAME WAS FOUND CORRODED ON FRONT SIDE FROM LONG 29L TO 29R. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-03, FIG 2A. 2 L 7 2 4F A6WE 1996091900431 19960919 00431 WP 1996 9 19 MWEA96509 1 19960912 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 256 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, FWD CARGO PIT STA 256 FRAME WAS FOUND CORRODED FROM LONG 29L TO 29R. FABRICATED PARTS AND INSTALLED IAW SR M 53-03, FIG 2A. 2 L 7 2 4F A6WE 1996091900432 19960919 00432 WP 1996 9 19 MWEA96510 1 19960912 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 237 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, FWD CARGO PIT STA 237 FRAME WAS FOUND CORRODED BETWEEN LONG 29L AND 29R. FABRICATED PARTS AND INSTALLED IA W SRM 53-03, FIG 2A. 2 L 7 2 4F A6WE 1996091900433 19960919 00433 WP 1996 9 19 MWEA96511 1 19960912 A 5532 SKIN DOUG DC9 DC932 3022066 WP VERT STAB CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, BOTH LT AND RT SIDES OF VERT STAB CANOE FWD END EXTERNAL SKINS WERE HEAVILY CHAFED FROM THE FAIRINGS. REPL ACED THE SKINS IAW SRM 55-31-0. 2 L 7 2 4F A6WE 1996091900434 19960919 00434 WP 1996 9 19 MWEA96512 1 19960912 A 5730 SKIN DOUG DC9 DC932 3022066 WP RT WING CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, RT WING L/E WAS FOUND CHAFED BY SCREWS JUST OUTBD OF VORTILON. COMPLETED REPAIR IAW SRM 57-06A, FIG 4. 2 L 7 2 4F A6WE 1996091900435 19960919 00435 WP 1996 9 19 MWEA96513 1 19960912 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP COCKPIT WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, IT WAS FOUND THAT THE F/O'S LOWER AFT SEAT TRACKS INBD AND OUTBD HAD WORN ADJUSTMENT HOLES FOR THE SEAT LOC KING PIN. REPAIRED THE TRACKS IAW SRM 53-05, FIG 28. 2 L 7 2 4F A6WE 1996091900436 19960919 00436 WP 1996 9 19 MWEA96514 1 19960912 A 5730 SKIN DOUG DC9 DC932 3022066 WP RT WING CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, RT WING LEADING EDGE WAS FOUND TO HAVE A CHAFED AREA ON BOTH SIDES OF THE NR 1 SLAT DRIVE TRACK. MAINT COM PLIED WITH REPAIR IAW SRM 57-06A, FIG 4. 2 L 7 2 4F A6WE 1996091900437 19960919 00437 WP 1996 9 19 MWEA96515 1 19960912 A 5315 FLOOR BEAM DOUG DC9 DC932 3022066 WP BS 389 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 DURING INSP, CORROSION FOUND ON FLOOR BEAM TOP FLANGE STA 389 AROUND TWO HOLES 12 INCHES INBD LT SIDE. REPAIRED FLOOR B EAM IAW SRM 53-05. 2 L 7 2 4F A6WE 1996091900438 19960919 00438 WP 1996 9 19 MWEA96516 1 19960912 A 3350 6011779 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 209ME 47132 DURING SERVICE CK, FOUND RT NACELLE LIGHT INOP. REPLACED BATTERY POWER SUPPLY, OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996091900439 19960919 00439 WP 1996 9 19 MWEA96517 1 19960910 A 2760 SWITCH DOUG DC9 DC932 3022066 WP LT PANEL OUT OF ADJUST A MWEA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 31 401ME 57133 PILOT REPORTS SPOILER DEPLOYED LIGHT ON ANNUNCIATOR PANEL ILLUMINATED DURING TAKEOFF ROLL. RETURNED TO GATE. ADJUSTED LT OUTBD SPOILER PANEL SWITCH IAW ME EO 1-27-014R2, OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996091900440 19960919 00440 WP 1996 9 19 MWEA96518 1 19960911 A 5270 STRIKER PLATE DOUG DC9 DC932 3022066 WP CARGO DOOR OUT OF ADJUST A MWEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 31 502ME 48132 PILOT REPORTS AFT CARGO DOOR LIGHT ON ANNUNCIATOR PANEL ILLUMINATED DURING TAKEOFF. ABORTED TAKEOFF, RETURNED TO GATE. MTCE CHECKED DOOR SECURITY AND DEFERRED SYSTEM FOR FLT TO MKE. IN MKE RESHIMMED LIGHT STRIKER PLATE, OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996091900441 19960919 00441 1996 9 19 MWEA96519 4 19960912 A 2565 113317 SLIDE DOUG DC9 DC914 3022034 WP PAX DOOR LOW PRESSURE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 DURING SERVICE CHECK, FOUND FWD ENTRY EVAC SLIDE PRESSURE LOW. REPLACED FWD ENTRANCE DOOR EVAC SLIDE. 2 L 7 2 4F A6WE 1996091900442 19960919 00442 NM 1996 9 19 SCNA96249 1 19960908 A 3350 328 BULB BOEING 727 727227 1384078 NM CABIN FAILED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 275AF 22092 LEFT AFT OVERWING EXIT LOWER SIGN HAS A BULB INOP. RELAMPED EMERGENCY EXIT LIGHTING AND OPS CHECKED GOOD IN ACCORDANCE WITH MM 33-50-01. 2 L 7 3 4F A3WE 1996091900443 19960919 00443 NM 1996 9 19 DHL96720003 1 19960911 A 5270 1322RQ18A2 SWITCH BOEING 727 727228 NM CARGO DOOR MALFUNCTIONED A DHLA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 720DH 19544 CARGO DOOR UNLOCKED LIGHT ILLUMINATED DURING CLIMBOUT THROUGH14,000 FEET. REPLACED SWITCHES 15, 16, 17, ADJUSTED TO SPE CIFICATIONS OPERATIONS CHECK GOOD. 2 L 7 3 4F A3WE 1996091900444 19960919 00444 NM 1996 9 19 P5CA9600689 1 19960912 A 5320 69B109444 SHEAR TIE BOEING 747 747132 1384882 NM BS 1000 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 CRACKED SHEAR TIE ON TIE DOWN TRACK BS 1000 WL 195 LBL 57. REPLACED PART PER BOEING SRM 51-10-03 PART MANUFACTURED PER DRAWING 64-53-1096. 2 L 7 4 4F A20WE 1996091900445 19960919 00445 NM 1996 9 19 P5CA9600690 1 19960912 A 5320 69B109444 SHEAR TIE BOEING 747 747132 1384882 NM BS 1000 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 CRACKED SHEAR TIE ON TIE DOWN TRACK BS 1000 WL 195 RBL 57. REPLACED PART PER BOEING SRM 51-10-03 PART MANUFACTURED PER DRAWING 64-53-1096. 2 L 7 4 4F A20WE 1996091900446 19960919 00446 NM 1996 9 19 P5CA9600692 1 19960910 A 5522 SKIN BOEING 747 747124 1384874 NM ELEVATOR DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 DELAMINATED SKIN ON LEFT INBOARD ELEVATOR TRAILING EDGE INBOARD MID. REPAIRED WITH FIBERGLASS OVERLAY PER BAC SRM 51-41 -00. 2 L 7 4 4F A20WE 1996091900447 19960919 00447 NM 1996 9 19 P5CA9600693 1 19960909 A 2150 65B409338 DUCT BOEING 747 747124 1384874 NM NR 1 ACM CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 DUCT CRACKED AT NR 1 AIR CYCLE MACHINE. REMOVED AND REPLACED DUCT PER BAC MM 21-50-03. 2 L 7 4 4F A20WE 1996091900448 19960919 00448 NM 1996 9 19 P5CA9600694 1 19960912 A 5730 PANEL BOEING 747 747122 1384872 NM RT WING LE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 DELAMINATED UNDERWING PANEL AT RIGHT INBOARD LEADING EDGE. REPAIRED DAMAGED AREA PER BAC SRM 51-40-09. 2 L 7 4 4F A20WE 1996091900449 19960919 00449 NM 1996 9 19 P5CA9600695 1 19960911 A 7110 BRACKET BOEING 747 747124 1384874 NM NR 4 ENGINE COWL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 CRACKED BRACKET AT NR 4 ENGINE NOSE COWL. FABRICATED AND INSTALLED NEW BRACKET PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1996091900450 19960919 00450 NM 1996 9 19 P5CA9600696 1 19960909 A 5320 65B2347139 BRACKET BOEING 747 747124 1384874 NM MAIN CARGO DECK BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 BROKEN SUPPORT BRACKET AT RIGHT SIDE MAIN DECK CARGO SAFETY NET. REPLACED BRACKET, FABRICATED PER BAC SRM 51-10-01 AND 51-30-02. 2 L 7 4 4F A20WE 1996091900451 19960919 00451 NM 1996 9 19 P5CA9600697 1 19960912 A 5320 69B109444 SHEAR TIE BOEING 747 747132 1384882 NM BS 1000 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 CRACKED SHEAR TIE ON TIE DOWN TRACK BS 1000 WL 195 RBL 75. REPLACED PART PER BOEING SRM 51-10-03 PART MANUFACTURED PER DRAWING 64-53-1096. 2 L 7 4 4F A20WE 1996091900452 19960919 00452 NM 1996 9 19 P5CA9600698 1 19960910 A 2750 BUSHING BOEING 747 747124 1384874 NM LT TE FLAP MIGRATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 MIGRATED BUSHING ON FORE FLAP SUPPORT FITTING OF LEFT INBOARD FLAP OUTBOARD TRACK. REPLACED BUSHING FASTENERS. 2 L 7 4 4F A20WE 1996091900453 19960919 00453 NM 1996 9 19 P5CA9600699 1 19960911 A 5711 SPAR WEB BOEING 747 747132 1384882 NM FSS 668 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 CRACKED LEFT WING FRONT SPAR WEB FS 668 TO 697. REPAIRED IN ACCORDANCE WITH BOEING DRAWING 112U8040. 2 L 7 4 4F A20WE 1996091900454 19960919 00454 NM 1996 9 19 P5CA9600700 1 19960911 A 5711 SPAR WEB BOEING 747 747132 1384882 NM FSS 680 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 CRACKED RIGHT WING FRONT SPAR WEB FS 668 TO 697. REPAIRED IN ACCORDANCE WITH BOEING DRAWING 112U8040. 2 L 7 4 4F A20WE 1996091900455 19960919 00455 NM 1996 9 19 P5CA9600701 1 19960911 A 5230 65B0185563 SEAL DEPRESSOR BOEING 747 747124 1384874 NM AFT CARGO DOOR TORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 TORN AND BENT SEAL DEPRESSOR AFT CARGO DOOR. REMOVED AND REPLACED SEAL DEPRESSOR PER BOEING SRM 51-10-01. 2 L 7 4 4F A20WE 1996091900456 19960919 00456 NM 1996 9 19 P5CA9600702 1 19960911 A 5230 65B0185563 SEAL DEPRESSOR BOEING 747 747124 1384874 NM CARGO DOOR TORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 TORN SEAL DEPRESSOR FORWARD CARGO DOOR AFT EDGE. REPLACED PER BOEING SRM 51-40-01. 2 L 7 4 4F A20WE 1996091900457 19960919 00457 NM 1996 9 19 P5CA9600703 1 19960911 A 5330 SKIN BOEING 747 747124 1384874 NM BS 2484 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 BULGE IN FUSELAGE SKIN AT BS 2484 S46L. REMOVED FASTENERS AT THE AREA OF THE BULGE, INSPECTED FOR CORROSION AND NO CORR OSION FOUND. REINSTALLED FASTENERS PER BOEING SRM 51-30-02. 2 L 7 4 4F A20WE 1996091900458 19960919 00458 NM 1996 9 19 P5CA9600704 1 19960910 A 5280 SKIN BOEING 747 747124 1384874 NM LT MLG STRUT DR PUNCTURED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 PUNCTURED SKIN ON LEFT BODY GEAR STRUT DOOR TRAILING EDGE. ROUTED DAMAGED AREA PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1996091900459 19960919 00459 NM 1996 9 19 P5CA9600705 1 19960909 A 3211 RIVET BOEING 747 747124 1384874 NM RT MLG SHEARED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 SHEARED RIVETS ON AFT OUTBOARD CORNER OF RIGHT BODY GEAR. REPLACED DAMAGED RIVETS PER BAC SRM 51-30-02. 2 L 7 4 4F A20WE 1996091900460 19960919 00460 NM 1996 9 19 P5CA9600706 1 19960909 A 2170 DRAIN LINE BOEING 747 747124 1384874 NM NR 3 SEPARATOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 CRACKED DRAIN LINE AT NR 3 PACK WATER SEPARATOR. REPLACED DAMAGED LINE WITH NEW LINE AND INSTALLED PER BAC MM 21-51-00. 2 L 7 4 4F A20WE 1996091900461 19960919 00461 NM 1996 9 19 P5CA9600707 1 19960910 A 2750 BUSHING BOEING 747 747124 1384874 NM TE FLAP FITTING MIGRATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 BUSHING MIGRATED AT RIGHT INBOARD FOREFLAP TRACK ATTACH FITTING. FOUND FASTENERS AT FAULT AND REPLACED BUSHING FASTENER S PER BAC MM 27-51-02. 2 L 7 4 4F A20WE 1996091900462 19960919 00462 NM 1996 9 19 P5CA9600708 1 19960909 A 5520 FAIRING BOEING 747 747124 1384874 NM LT HORIZ STAB PULLED RIVETS A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 RIVET HEADS SUNK INTO UPPER FIXED FAIRING MID SECTION ON LEFT HORIZONAL STABLIZER. MADE FIBERGLASS REPAIR PER BAC SRM 5 1-40-09. 2 L 7 4 4F A20WE 1996091900463 19960919 00463 NM 1996 9 19 P5CA9600709 1 19960910 A 5280 DOOR BOEING 747 747124 1384874 NM RT MLG CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LIGHT SURFACE CORROSION ON WHEEL WELL DOOR OF RIGHT BODY GEAR. REMOVED CORROSION PER BAC SRM 51-10-52. 2 L 7 4 4F A20WE 1996091900464 19960919 00464 NM 1996 9 19 P5CA9600710 1 19960910 A 5512 SKIN BOEING 747 747124 1384874 NM HORIZ STAB BUCKLED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 BUCKLED SKIN ON LEFT HORIZONAL STABLIZER UPPER TRAILING EDGE. REPAIRED SKIN PER BAC SRM 51-40-09. 2 L 7 4 4F A20WE 1996091900465 19960919 00465 NM 1996 9 19 P5CA9600711 1 19960910 A 5247 SKIN BOEING 747 747124 1384874 NM APU DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 SKIN CRACKED ON LEADING EDGE OF APU BATTERY ACCESS DOOR. FABRICATED REPAIR PER BAC SRM 51-40-02 AND INSTALLED PER BAC S RM 51-30-02. 2 L 7 4 4F A20WE 1996091900466 19960919 00466 NM 1996 9 19 P5CA9600712 1 19960909 A 5350 RADOME BOEING 747 747124 1384874 NM FWD FUSELAGE DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 THREE HOLES IN A/C RADOME. MADE FIBERGLASS REPAIR PER BAC SRM 53-30-03, 53-50-03 AND 51-24-11. 2 L 7 4 4F A20WE 1996091900467 19960919 00467 NM 1996 9 19 P5CA9600713 1 19960911 A 5730 PANEL BOEING 747 747124 1384874 NM LT WING LE DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 THREE DAMAGED LEADING EDGE FIBERGLASS PANELS ON LEFT WING. REPAIRED PANELS PER BAC SRM 51-40-15 AND 51-40-11. 2 L 7 4 4F A20WE 1996091900468 19960919 00468 NM 1996 9 19 P5CA9600714 1 19960910 A 7110 COWLING BOEING 747 747124 1384874 NM NR 2 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 CRACKED UPPER FORWARD CORNER ON NR 2 ENGINE INBOARD COWL. FABRICATED REPAIR AND INSTALLED PER BAC SRM 51-10-02 AND 51-3 0-02. 2 L 7 4 4F A20WE 1996091900469 19960919 00469 EU 1996 9 19 96ZZZX4633 1 19960709 A 2560 7012978000 ASSIST BOTTLE AIRBUS 300 A300B4203 3930306 EU L2 DOOR MISFIRED A P8NA K NONE O OTHER IN INSP/MAINT 1 SO 19 861PA 216 DURING THE MINI-EVACUATION, THE L2 DOOR DID NOT OPEN PROPERLY. THIS CAUSED THE SLIDE/RAFT TO NOT DEPLOY PROPERLY. IT W AS FOUND THAT THE DOOR ASSIST BOTTLE DID NOT PROPERLY OPERATE. THE FIRING PIN WAS NOT STRIKING THE DISC HARD ENOUGH TO DISLODGE PROPERLY. RE-RIGGED FIRING MECHANISM, OPERATIONAL CHECK OK. 2 L 7 2 4F A35EU 1996091900470 19960919 00470 1996 9 19 96ZZZX4634 4 19960729 A 2565 D294498118 SLIDE AIRBUS 300 A300B4203 3930306 EU R3 DOOR FAILED A P8NA K NONE O OTHER IN INSP/MAINT 1 SO 19 861PA 3493 216 THE PLASTIC TUBE THAT CONNECTS THE SLIDE BUSTLE ASSIST BOTTLE TO THE AIR BAG FAILED DUE TO 'AGE' HARDENING. 2 L 7 2 4F A35EU 1996091900471 19960919 00471 1996 9 19 96ZZZX4635 4 19960731 A 2565 D29498117 SLIDE AIRBUS 300 A300B4203 3930306 EU L3 EMERG DOOR FAILED A P8NA K NONE O OTHER IN INSP/MAINT 1 SO 19 861PA 3438 216 THE SLIDE WAS NOT USABLE BECAUSE SB 001-25-13 WAS NOT IMPLEMENTED AND RESULTED IN A JAMMED AUTOMATIC INFLATION CABLE. T EAR-DOWN REPORT FROM AIR CRUISERS CONCLUDED THE FAILURE WAS CAUSED BY FAILURE OF THE SLIDER BLOCK MECHANISM. SB 001-25- 13 REPLACES THE SLIDER BLOCK TO PREVENT THIS FAILURE FROM HAPPENING. 2 L 7 2 4F A35EU 1996091900472 19960919 00472 1996 9 19 96ZZZX4636 4 19960702 A 2565 D30477110 SLIDE AIRBUS 300 A300B4203 3930306 EU R4 DOOR FAILED A P8NA K NONE O OTHER IN INSP/MAINT 1 SO 19 861PA 216 SLIDE RAFT FAILED TO DEPLOY DURING AN FAA MINI/EVACUATION TEST ON JULY 2, 1996. SLIDE/RAFT WAS SENT TO REPAIR FACILITY FOR RECEIVING INSPECTION AND TEAR DOWN. FINDINGS: CONTAINER RELEASE CABLE PATCH, P/N C30524-103, WAS SEPARATED FROM IT S CEMENTED POSTION ON THE GIRT. THE CABLE ASSEMBLIES WERE STILL CONNECTED TO THE VALISE RELEASE BAR AND EJECTOR BAG INF LATOR CABLE. THE EJECTOR BAG INFLATOR CABLE WAS KINKED AND FRAYED AT THE POSITION WHERE IT ROUTES THROUGH THE PACKBOARD . 2 L 7 2 4F A35EU 1996091900473 19960919 00473 1996 9 19 96ZZZX4637 4 19960702 A 2565 D29498116 SLIDE AIRBUS 300 A300B4203 3930306 EU R3 DOOR MALFUNCTIONED A P8NA K NONE O OTHER IN INSP/MAINT 1 SO 19 861PA 216 DURING MINI-EVACUATION TEST, AIRCRUISER SLIDE/RAFT LOCATED AT THE R3 DOOR DID NOT PERFORM ITS REQUIRED OPERATIONAL FUNCT ION. UPON ACTIVATION, THE ASSEMBLY WENT THROUGH ITS NORMAL ACTIVATION PROCESS TILL REACHING THE HALF-TIME FRANGIBLE RES TRAINT. AT THIS POINT, THE UNIT WAS STALLED AND DID NOT COMPLETE FULL-UP ACTIVATION. TEAR DOWN INSPECTION REVEALED NO DISCREPANCIES THAT WOULD RESULT IN THE FAILURE OF THE DEPLOYMENT. UNIT WAS OVERHAULED AND RETURNED TO SERVICE. 2 L 7 2 4F A35EU 1996091900474 19960919 00474 NE 1996 9 19 96ZZZX4638 2 19960808 A 7421 CH34595 IGNITER SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 781LF 160 1178 415 IGNITER INTERMITTENT, FOUND SEPARATED INTERNALLY. LESS THAN 160 HOURS ON IGNITER. 1 G 7 1 3U 3 U H9EU E19EU 1996091900476 19960919 00476 NE 1996 9 19 96ZZZX4640 2 19960804 A 7421 CH34595 IGNITER SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1A 60030 NE ENGINE DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 792LF 150 1035 768 ELECTRODE SLIDE OUT OF INSULATION OVER .25 INCH. CONCERN FOR INTERNAL FOD POTENTIAL. 1 G 7 1 3U 3 U H9EU E19EU 1996091900477 19960919 00477 EU 1996 9 19 96ZZZX4641 1 19960810 A 6310 330A54070628 DISC 355A35203400 AEROSP AS355 AS355F 8680806 EU NR 2 ENG GRBOX CRACKED A NYBA K NONE O OTHER IN INSP/MAINT 1 EA 11 5776D 5030 DURING DAILY INSPECTION AFTER LAST FLIGHT OF THE DAY, THE MECHANIC NOTED THAT ONE DISC WAS FOUND CRACKED, ON THE NR 2 EN GINE MAIN GEARBOX DRIVESHAFT COUPLING. SUSPECT FATIGUE. REPLACED AFFECTED DISC IAW AS355F MAINTENANCE WORK CARDS. 1 G 7 2 3U H11EU 1996091900512 19960919 00512 NE 1996 9 19 96ZZZX4676 2 19960601 A 7260 230307203 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE CSD DRIVE LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 528SF 363 7104 LE45343E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1996091900513 19960919 00513 NE 1996 9 19 96ZZZX4677 2 19960601 A 7250 410106701 SEAL RING BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE 1ST TURB SHROUD WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 528SF 363 7104 LE45343E FIRST TURBINE SHROUD SEAL RING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH, NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1996091900514 19960919 00514 NE 1996 9 19 96ZZZX4678 2 19960601 A 7260 430101201 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE ACCY DRIVE LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 528SF 363 7104 LE45343E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1996091900515 19960919 00515 NE 1996 9 19 96ZZZX4679 2 19960601 A 7260 430101301 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE ACCY DRIVE LEAK A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 528SF 363 7104 LE45343E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1996091900516 19960919 00516 NE 1996 9 19 96ZZZX4680 2 19960601 A 7260 430101501 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE ACCY DRIVE LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 528SF 363 7104 LE45343E ACCESSORY DRIVE SEALS LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW 3 EACH UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1996091900517 19960919 00517 NE 1996 9 19 96ZZZX4681 2 19960601 A 7250 430144801 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE NR 3 BEARING LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 528SF 363 1737 7104 LE45343E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1996091900518 19960919 00518 1996 9 19 96ZZZX4682 4 19960817 A 3160 900A3720002105 DISPLAY SYSTEM DOUG MD900 MD900 3027375 NM FUEL QUANTITY ERROR A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 347 008251005 90000012 DISPLAY SYSTEM FUEL QUANTITY INDICATOR FLUCTUATES 200 POUNDS. REPLACED WITH USED UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1996091900522 19960919 00522 SW 1996 9 19 96ZZZX4686 1 19960718 A 2430 SM20PCD200P21 RELAY BELL 206 206L1 1182107 SW BATTERY RELAY A G8SA K NONE O OTHER IN INSP/MAINT 1 SO 03 2618 MFD9517 45503 BATTERY POWER STAYS ON AFTER SWITCH IS TURNED OFF. 1 G 7 1 3U H2SW 1996091900524 19960919 00524 NE 1996 9 19 CA960126006 1 19960117 A 6310 7636109103104 FLANGE SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL NR 1 ENG OUTPUT CRACKED W K NONE E VIBRATION/BUFFET LD LANDING 1 CA CAE890255S (CAN)DURING FLIGHT PILOTS REPORTED A HIGH FREQUENCY VIBRATION IN THE FOOT PEDALS AND PARKING BRAKE 'T' HANDLE. A LOUD GR OWL NOISE WAS ALSO HEARD FROM THE #1 ENGINE. UPON SHUT DOWN AND FURTHER INVESTIGATION , IT WAS FOUND THAT THE #1 ENGINE OUTPUT FLANGE SHAFT HAD SHEARED AT THE POINT WHERE THE ATTACHMENT NUT AND COTTER PIN ARE LOCATED. THE OUTPUT FLANGE WAS REPLACED. 1 G 7 2 3U 3 U H1NE E1GL 1996091900534 19960919 00534 1996 9 19 CA960126016 4 19960124 A 3422 5050002904 GYRO SNIAS 350 AS350B 8680801 EU COCKPIT DG MALFUNCTION W K NONE O OTHER IN INSP/MAINT 1 CA 120 (CAN)GYRO WILL NOT HOLD A HEADING, TIME THIS INSTALLATION 119.5 HOURS. 1 G 7 1 3U H9EU 1996091900535 19960919 00535 SW 1996 9 19 CA960126017 1 19960119 A 5302 206031329001 FITTING BELL 206 206B 1181511 SW UPPER LT TB CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 16753 (CAN)UPPER LEFT HAND TAILBOOM ATTACH FITTING (INTERCOSTAL) FOUND CRACKED. 1 G 7 1 3U H2SW 1996091900536 19960919 00536 GL 1996 9 19 CA960126018 2 19960108 A 7250 68726656244 RETAINING RING ALLSN 250C20 BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE MIS INSTALLED W K NONE O OTHER IN INSP/MAINT 1 CA 670 CAT31575P CAE820289 (CAN)RETAINING RING FOUND NOT TO BE FULLY INSTALLED DURING A TURBINE REMOVAL. IT WAS APPROXIMATELY 3/4 OF THE WAY OUT. A SSEMBLY RE-SHIMMED AND NEW RETAINING RING INSTALLED. AIRCRAFT RETURNED TO SERVICE. 1 G 7 1 3U 3 U H2SW E4CE 1996091900537 19960919 00537 WP 1996 9 19 CA960126019 1 19960116 A 6210 369A10045 BLADE PINS HUGHES 369 369D 4470706 WP M/R WORN W K NONE O OTHER IN INSP/MAINT 1 CA 6462 (CAN)FOUND PINS DID NOT PROTRUDE THROUGH BLADES AND LEAD-LAG LINKS PROPERLY, MEASURED AS PER HMI AND FOUND WORN BEYOND L IMITS. 10 PINS AFFECTED. 1 G 7 1 3U H3WE 1996091900538 19960919 00538 WP 1996 9 19 CA960126020 1 19960103 A 6320 369D25100505 TRANSMISSION HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL M/R CONTAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA 4435 988 CAE832104 (CAN)METAL CONTAMINATION ON BOTH CHIP DETECTORS. 1 G 7 1 3U 3 U H3WE E4CE 1996091900539 19960919 00539 WP 1996 9 19 CA960126021 1 19960103 A 7712 369H45267 INDICATOR HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL ENG TORQUE STICKING W K NONE O OTHER IN INSP/MAINT 1 CA 409 CAE832104 (CAN)INDICATOR SLUGGISH RESPONSE AND NEEDLE STICKS. 1 G 7 1 3U 3 U H3WE E4CE 1996091900541 19960919 00541 EU 1996 9 19 CA960126023 1 19960109 A 2913 704A34310006 PUMP SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1B 6OO30 NE HYD WORN W K NONE O OTHER IN INSP/MAINT 1 CA 290 (CAN)PUMP SPLINES WORN BEYOND LIMITS. 1 G 7 1 3U 3 U H9EU E19EU 1996091900542 19960919 00542 SW 1996 9 19 CA960126024 2 19960114 A 7320 SYLC95481 LINEAR ACTUATOR BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE SEIZED W K NONE O OTHER IN INSP/MAINT 1 CA 802694 (CAN)ACTUATOR UNIT SEIZED WILL NOT RETRACT OR EXTEND. 1 G 7 1 3U 3 U H2SW E4CE 1996091900544 19960919 00544 SW 1996 9 19 CA960126027 1 19960119 A 2910 2981006143 LINE SWRNGN SA226 SA226TC 8780404 SW LH WING ROOT HOLED W O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 CA 15288 (CAN)CREW REPORTED LOSS OF HYDRAULIC FLUID. LEAK FOUND FROM LINE IN L/H WING ROOT LEADING EDGE. THIS LINE IS A 3/8 SUPPL Y LINE AND HAD CRACKED AT 90 DEGREE BEND. ALSO LINE WAS BADLY WORN AT LINE BLOCK CLAMP. 2 L 7 2 4T RT A8SW 1996091900545 19960919 00545 CE 1996 9 19 CA960126028 1 19960117 A 2820 1009200357 FUEL TUBE BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA FERREL CRACKED W A K NONE O OTHER IN INSP/MAINT 1 CA 14720 PCE50201 (CAN)DURING INSPECTION THE FERREL WAS FOUND CRACKED ON THE FUEL TUBE. SUBMITTER STATES THAT THE COMPANY INITIATED A FLEE T WIDE INSPECTIION AND FOUND SEVERAL OTHER CRACKS IN THE SAME LOCATION ON DIFFERENT A IRCRAFT. 1 L 7 2 3T 4 T A14CE E4EA 1996091900546 19960919 00546 NE 1996 9 19 CA960126029 2 19960115 A 7260 GEARBOX BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE NR1 ENGINE CRACKED W O OTHER O OTHER IN INSP/MAINT 1 CA 30751 (CAN)DURING "A" CHECK #1 ENGINE GEARBOX WAS FOUND CRACKED ABOVE THE FUEL FLOW GOVERNOR. ENGINE REPLACED. 2 L 7 2 4F 4 F RT A2NM E12EU 1996091900547 19960919 00547 SW 1996 9 19 CA960126030 1 19960108 A 2916 2781032367 LINE SWRNGN SA227 SA227AC 8780603 SW HYD.RESERVOIR WORN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN)DURING PRE-FLIGHT MAINTENANCE FOUND A WORN HYDRAULIC LINE, WHICH GOES FROM SIGHT GAUGE TO HYDRAULIC RESERVOIR. LINE WAS TOUCHING EDGE OF HOLE IN WHICH IT PASSES AT KEILSON WEB. LINE REPLACED. 2 L 7 2 4T RT A8SW 1996091900548 19960919 00548 EA 1996 9 19 CA960126031 1 19960118 A 2750 72740226001 BEARING DHAV DHAV DHC7 DHC7102 2802708 EA FLAPS SEIZED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN)WHEN FLAPS SELECTED DOWN DURING MAINTENANCE, A LOUD SQUEAL WAS HEARD. INSPECTION FOUND THAT THE LEFT HAND, INBOARD BEARING HANGER ASSEMBLY HAD SEIZED. THE SHAFT THAT RUNS ON THE BEARING WAS SPINNING I N THE SLEEVE. THIRTY PERCENT OF TH E SHAFT HAD BEEN WORN AWAY AS A RESULT. 2 H 7 4 4T A20EA 1996091900550 19960919 00550 WP 1996 9 19 CA960126033 2 19960109 A 7260 30728851 BEARING LEAR 35 35A 5170602 CE GARRTT TFE731 TFE7312 01518 WP ACCESSORY GEARBX FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 8878 8878 P74369 (CAN)SUBMITTER NOTICED HIGH METAL CONTENT IN S.O.A.P. SAMPLE. FOUND REAR ACCESSORY GENERATOR DRIVE BEARING WITH RACE DES TROYED, AND BALL BEARINGS FLATTENED. 2 L 7 2 4F 4 F A10CE E6WE 1996091900554 19960919 00554 EA 1996 9 19 CA960126038 2 19960115 A 8530 VALVE LYC CESSNA 150 152 2071835 CE LYC O235 O235L2C 41505 EA NR3 CYL EXH STICKING W O OTHER K FLUID LOSS IN INSP/MAINT 1 CA 289 L2000215 (CAN)ENGINE HAD OIL LEAK #3 CYLINDER, AFTER REMOVING THE CYLINDER IT WAS FOUND THAT THE EXHAUST VALVE WAS STICKING AND T HE PUSH ROD WAS BENT. 1 H 7 1 3O 3 O NT 3A19 E223 1996091900555 19960919 00555 SO 1996 9 19 CA960126039 1 19960118 A 2731 20802003 JACK SCREW PIPER 20802003 PIPER PA23 PA23250 7102308 SO ELEV TAB FROZEN IN DRUM W K NONE O OTHER IN INSP/MAINT 1 CA (CAN)PILOT TRIMMED THE AIRCRAFT FULL NOSE UP AND THE JACK SCREW FROZE IN THE DRUM BARREL. SCREW IN BARREL REMOVED AND CL EANED AND LUBRICATED AND RETURNED TO SERVICE. 1 L 7 2 3O 1A10 1996091900557 19960919 00557 EA 1996 9 19 CA960126042 1 19960126 A 5311 C2FS1503A FRAME DHAV DHAV DHC2 DHC2MK1 2800102 EA FORWARD WALL WORN W K NONE O OTHER IN INSP/MAINT 1 CA 20835 (CAN)INSPECTION IN ACCORDANCE WITH SB 2/49 FOUND TWO AREAS AT AFT FACE OF FORWARD WALL NOT MEETING ORIGINAL THICKNESS. 1 H 7 1 3R A806 1996091900558 19960919 00558 SO 1996 9 19 CA960126043 1 19960128 A 3260 SWITCH PIPER PA31 PA31 7103102 SO LYC MLG DIRTY W K NONE N FALSE WARNING IN INSP/MAINT 1 CA (CAN)WRONG INDICATION OF UNDERCARRIAGE. AFTER CLEANING THE SWITHC AND CHECKING, RETURNED TO NROMAL. 1 L 7 2 3O A20SO 1996091900559 19960919 00559 EA 1996 9 19 CA960126044 2 19960111 A 7250 3024767 DIFFUSER PIPE DHAV DHC6 DHC6300 EA PWA PT6 PT6A27 52043 EA DUCT ASSY EXIT CRACKED W A O OTHER O OTHER IN INSP/MAINT 1 CA 2352 PCE40606 (CAN)DURING BOROSCOPE INSPECTION OF THE COMPRESSOR TURBINE VANE RING FOUND WHAT APPEARED TO BE A CRACK OF THE RING. UPON REMOVAL OF THE TURBINE WHEEL THE RING WAS FOUND SERVICEABLE, BUT FURTHER INSPECTION FOUND A DIFFUSER PIPE WELD AT THE DUCT TO BE CRACKED. THE CRACK EXTENDED 90 PERCENT OF THE WELD. THE DIFFUSER PIPE REMAINS TIGHT IN THE DUCT ASSEMBLY DIFF USER EXIT. 1 H 7 2 3T 4 T A9EA E4EA 1996091900560 19960919 00560 SW 1996 9 19 CA960126045 1 19960119 A 6420 204011769001 BEARING BELL 206 206L 1181522 SW T/R TRUNNION BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN)WHILE INSPECTING PITCH CHANGE ASSEMBLY P/N 206-011-720-015, THE BEARING WAS FOUND BROKEN IN THE TRUNNION. 1 G 7 1 3U H2SW 1996091900561 19960919 00561 NE 1996 9 19 CA960129001 3 19960126 A 6111 SFA13G1OA BLADE HAMSTD DHAV DHC8 DHC8102 2809003 NM HAMSTD 14SF 14SF7 NE NR1 BLADE FAILED NDT TEST W K NONE O OTHER IN INSP/MAINT 1 CA 14620 8315 891003 (CAN)#1 BLADE #1 PROPELLER FAILED SHEAR WAVE NDT TEST AS PER SERVICE BULLETIN 14SF-61-A95. 2 H 7 2 4T RT A13NM 6 C P7NE 1996091900562 19960919 00562 NE 1996 9 19 CA960129002 3 19960126 A 6111 SFA13M1OA BLADE HAMSTD DHAV DHC8 DHC8102 2809003 NM HAMSTD 14SF 14SF7 NE NR 2 BLADE FAILED NDT TEST W K NONE O OTHER IN INSP/MAINT 1 CA 9460 848295 891003 (CAN)#2 BLADE #1 PROPELLER FAILED SHEAR WAVE NDT TEST AS PER SERVICE BULLETIN 14SF-61-A95. 2 H 7 2 4T RT A13NM 6 C P7NE 1996091900563 19960919 00563 NE 1996 9 19 CA960129003 3 19960126 A 6111 SFA13N1OA BLADE HAMSTD DHAV DHC8 DHC8301 NM HAMSTD 14SF 14SF15 NE PROP FAILED NDT TEST W K NONE O OTHER IN INSP/MAINT 1 CA 8927 86806115 901121 (CAN)PROPELLER BLADE FAILED SHEAR WAVE NDT TEST AS PER SERVICE BULLETIN 14SF-61-A95. 2 H 7 2 4T RT A13NM 6 C P7NE 1996091900567 19960919 00567 SW 1996 9 19 CA960129010 1 19960118 A 2910 2781006455 TUBE SWRNGN SA226 SA226TC 8780404 SW HYD SYS FRACTURED W O OTHER K FLUID LOSS NR NOT REPORTED 1 CA (CAN)#4 ALUMINUM TUBE FOUND FRACTURED AT THE FLARE. ALL HYDRAULIC FLUID DUMPED AS A RESULT. CREW NOTED 0 PSI AND CARRIED OUT EMERGENCY GEAR EXTENSION. FLAPLESS LANDING MADE. 2 L 7 2 4T RT A8SW 1996091900568 19960919 00568 WP 1996 9 19 CA960129011 1 19960118 A 6710 369A7301501 BELLCRANK ASSY HUGHES 369 369D 4470706 WP COLLECTIVE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 4832 (CAN)ON A ROUTINE SCHEDULED INSPECTION, A CRACK WAS FOUND IN ONE LUG OF THE BELLCRANK ASSY, (P/N 369A7301-501). AFTER RE MOVAL OF THE BELLCRANK, PART OF THE LUG REMAINED ON THE BOLTS WHICH CONNECT THE CONTROL ROD (P/N 369A7011) TO THE IDLER ASSEMBLY (P/N 369N2666-505). A LOSS OF THE CONNECTION BETWEEN THE BELLCRANK AND THE CONTROL ROD WOULD LEAD TO A COMPLETE LOSS OF COLLECTIVE CONTROL. 1 G 7 1 3U H3WE 1996091900569 19960919 00569 SW 1996 9 19 CA960129012 1 19960121 A 2910 2781006259 HYDRAULIC LINE SWRNGN SA226 SA226TC 8780404 SW POWER PACK WORN THRU W K NONE K FLUID LOSS TX TAXI/GRND HDL 1 CA 24410 (CAN)AFTER SHUTDOWN, HYDRAULIC LEAK NOTED FROM LH WHEEL WELL. INSPECTION FOUND ALUMINUM PRESSURE LINE HAD WORN THROUGH A T CLAMP BLOCK ADJACENT TO POWER PACK. LINE REPLACED WITH STAINLESS. NEW P/N IS 27-810 06-419 AS PER IPC. 2 L 7 2 4T RT A8SW 1996091900571 19960919 00571 EA 1996 9 19 CA960129014 1 19960115 A 5220 CMQ1546 VALVE DHAV 85220283001 DHAV DHC8 DHC8311 1386006 EA RH EMERG.EXIT CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 10333 S2WAE040 (CAN)RH EMERGENCY EXIT FOUND STUCK AND COULD NOT BE OPENED. EXIT HANDLE WOULD ONLY MOVE 1/3 OF REQUIRED DISTANCE AND AIR VALVE WAS NOT ALLOWING DOOR SEAL TO DEFLATE. WITH PRESSURE STILL INDOOR SEAL, DOOR W OULD NOT OPEN. VALVE REPLACED. FUR THER INVESTIGATION FOUND AIR VALVE CORRODED AT LEVER PIVOT ARM. 2 H 7 2 4T RT A13NM 1996091900596 19960919 00596 EU 1996 9 19 96ZZZX4708 1 19960820 A 2822 RR1Z500E PUMP ISRAEL 1124 1124 4500102 EU FUEL BOOST SEAL LEAKS A F4GA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 23 26TJ 290 204 THREE PUMPS HAVE FAILED IN 90 DAYS. THESE PUMPS ARE A HIGH CHANGE RATE ITEM. LEAKAGE IS THE HIGHEST COMPLAINT. SUBMIT TER STATED IT APPEARS THAT CARBON SEAL FAILURE MIGHT BE THE LEADING PROBLEM. 2 M 7 2 4F A2SW 1996091900600 19960919 00600 EU 1996 9 19 96ZZZX4713 1 19960816 A 2731 SD3456030XA CONTROL CABLE STBROS SD3 SD360 8100606 EU ELEVATOR TRIM BROKEN A PIVA O OTHER F FLT CONT AFFECTED CR CRUISE 1 WP 13 711HJ SH3697 DURING LEVEL OFF PHASE OF FLIGHT, THE ELEVATOR TRIM CONTROL WHEEL BECAME VERY LOOSE, TRIM INOPERABLE. AFTER NORMAL LAND ING AT FINAL DESTINATION, MAINTENANCE FOUND THE ELEVATOR TRIM CABLE HAD BROKEN. ELEVATOR TRIM CABLE WAS REMOVED AND REP LACED, RIGGED, AND OPS CHECKED. ACFT RETURNED TO SERVICE. 2 H 7 2 4T A41EU 1996091900618 19960919 00618 SO 1996 9 19 96ZZZX4731 1 19960718 A 2430 587837 SWITCH 99377013 PIPER PA34 PA34200T 7103406 SO BATTERY MASTER FAILED A BVYA O OTHER H ELECT. POWER LOSS-50 PC CR CRUISE 1 CE 07 5463F 3183 347770022 AIRCRAFT LOST ALL ELECTRICAL POWER IN-FLIGHT. MASTER SWITCH WAS FOUND PARTIALLY DEFECTIVE. THE BATTERY CONTACTS SIDE O F SWITCH WORKED NORMALLY WHILE THE LT AND RT ALTERNATOR CONTACTS SIDE OF MASTER SWITCH FAILED CAUSING LOSS OF POWER TO A LTERNATOR SWITCHES. AIRCRAFT BATTERY POWER WAS DRAINED CAUSING ELECTRICAL FAILURE. DETERMINED CAUSE TO BE HIGH TIMED M ASTER SWITCH AND WORN OUT CONTACTS ON ALTERNATOR SIDE OF SWITCH. SUBMITTER RECOMMENDS REPLACING HIGH TIMED MASTER SWITC HES. 1 L 7 2 3O A7SO 1996091900623 19960919 00623 SO 1996 9 19 RAAA96E8027 1 19960912 A 3350 8621014 BATTERY PACK LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 AFT RT PAX CABIN EMERGENCY EXIT EGRESS IDENTIFIER LIGHT ASSEMBLY FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE LOW CHA RGE. 2 L 7 4 4T 4A22 1996091900624 19960919 00624 SO 1996 9 19 RAAA96E8028 1 19960912 A 3350 1000553 LIGHT LKHEED 188 188C 5262604 SO CABIN INOPERATIVE A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 LT FWD OVERWING EXIT EMERGENCY LIGHT FAILED SERVICE CHECK. CHANGED LIGHT ASSEMBLY. 2 L 7 4 4T 4A22 1996091900625 19960919 00625 SO 1996 9 19 RAAA96E8029 1 19960912 A 3350 1000553 LIGHT LKHEED 188 188C 5262604 SO CABIN INOPERATIVE A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 RT AFT OVERWING EXIT EMERGENCY LIGHT FAILED SERVICE CHECK. CHANGED LIGHT ASSEMBLY. 2 L 7 4 4T 4A22 1996091900626 19960919 00626 SO 1996 9 19 RAAA96E9012 1 19960913 A 3350 1000553 LIGHT LKHEED 188 188C 5262604 SO CABIN INOPERATIVE A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 FWD RT EMERGENCY EXIT OVERHEAD PULL DOWN EMERGENCY LIGHT WILL NOT DISARM, FAILED SERVICE CHECK. REPAIRED MISWIRED DISAR M WIRE AT FS 269 AND REPLACED LIGHT ASSY. 2 L 7 4 4T 4A22 1996091900627 19960919 00627 SO 1996 9 19 RAAA96E9013 1 19960913 A 3350 100553 LIGHT LKHEED 188 188C 5262604 SO CABIN INOPERATIVE A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 FWD LT PAX DOOR PULL DOWN EMERGENCY LIGHT FAILED SERVICE CHECK. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4T 4A22 1996091900628 19960919 00628 SO 1996 9 19 RAAA96E9014 1 19960913 A 3350 1000553 LIGHT LKHEED 188 188C 5262604 SO CABIN INOPERATIVE A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 AISLE PULL DOWN EMERGENCY LIGHT AT FWD ENTRY DOOR FAILED SERVICE CHECK. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4T 4A22 1996091900629 19960919 00629 NM 1996 9 19 CALA9601313 1 19960913 A 3610 652673831 DUCT BOEING 727 727224 1384076 NM PWA JT8 JT8D9 52048 NE NR 3 ENGINE BLOWN A CALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 93738 20666 674384 THE NR 3 ENGINE FIRE WARNING LIGHT ILLUMINATED AFTER TAKEOFF. THE EMERGENCY CHECKLIST WAS COMPLIED WITH AND THE WARNING LIGHT WENT OUT. THE AIRCRAFT WAS RETURNED TO PHX WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 3 ENGINE 13TH STAGE BLEED AIR DUCT TO EJECTOR VALVE BLOWN. THE DUCT WAS REPLACED, THE ENGINE WAS RUN AND ALL CHECKS WERE GOOD. 2 L 7 3 4F 4 F A3WE E2EA 1996091900630 19960919 00630 NE 1996 9 19 CALA9601314 2 19960913 A 7261 SEAL BOEING 737 737130 1384435 NM PWA JT8 JT8D7 52053 NE NR 2 ENGINE LEAKING A CALA A E UNSCHED LANDING ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 15207 19024 655871 THE NR 2 ENGINE OIL QUANTITY DROPPED TO .5 GALLON WHILE EN ROUTE. THE NR 2 ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS DI VERTED TO BWI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE OIL LEAKING FROM HYDRAULIC PUMP CAVIT Y DRAIN. THE CARBON SEAL IN GEARBOX BEHIND HYDRAULIC PUMP WAS REMOVED AND REPLACED. THE ENGINE WAS RUN AT HIGH POWER A ND NO LEAKS WERE FOUND. 2 L 7 2 4F 4 F A16WE E2EA 1996091900631 19960919 00631 NE 1996 9 19 9619776623 2 19960915 A 7530 EVBC BOEING 747 747251B 1384892 NM PWA JT9 JT9D7Q 52054 NE NR 1 ENGINE MALFUNCTIONED A NWAA O OTHER R PARTIAL RPM/PWR LOSS DE DESCENT 1 GL 01 623US 21705 02038 EN ROUTE, THE NR 1 ENGINE EXPERIENCED TOP OF DESCENT COMPRESSOR STALL AND FLAME-OUT. CREW FOLLOWED COM PROCEDURE, RESTA RTED ENGINE AT FL290, AND CONTINUED FLIGHT TO KIX WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED EVBC AND TRIMMED ENGIN E. 2 L 7 4 4F 4 F A20WE E3NE 1996091900632 19960919 00632 WP 1996 9 19 9619781153 1 19960912 A 2612 FIRE WIRE DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20J 52054 NE NR 3 ENGINE CHAFED A NWAA O OTHER J WARNING INDICATION DE DESCENT 1 GL 01 153US 46762 86161 DURING INITIAL CLIMB, THE NR 3 ENGINE B-LOOP LIGHT ILLUMINATED. CREW FOLLOWED COM PROCEDURE AND CONTINUED FLIGHT AS SCH EDULED. ON FINAL APPROACH, THE NR 3 ENGINE FIRE WARNING INDICATION ILLUMINATED AGAIN. CREW SHUT THE ENGINE DOWN AND MA DE A TWO ENGINE LANDING WITHOUT FURTHER INCIDENT. FOUND B-LOOP ON LOWER CORE COWL CHAFED. REPLACED LOOP AND TEST WAS N ORMAL. 2 L 7 3 4F 4 F A22WE E20EA 1996091900633 19960919 00633 NM 1996 9 19 9619796303 1 19960914 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 663US 23818 DURING LINE CHECK, FOUND FOUR FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROW 27B THROUGH DR 3L. RECONNECTED WIRING AN D INSTALLED LIGHT ASSEMBLY, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1996091900634 19960919 00634 NM 1996 9 19 9619806615 1 19960916 A 7930 CONNECTOR BOEING 747 747251B 1384892 NM PWA JT9 JT9D7Q 52054 NE NR 1 ENGINE DEFECTIVE A NWAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 01 615US 02360 02168 EN ROUTE, THE NR 1 ENIGNE OIL BYPASS FILTER LIGHT ILLUMINATED AT FL370. CREW FOLLOWED COM PROCEDURE, SHUT DOWN THE ENGI NE AND FLIGHT CONTINUED TO NRT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE ENGINE OIL FILTER AND A DEFECTIVE ELE CTRICAL CONNECTOR D0013J AT HORIZONTAL ENGINE FIRE WALL. CHECK WAS NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4 F A20WE E3NE 1996091900635 19960919 00635 WP 1996 9 19 9619819945 1 19960915 A 5270 DOOR TRACK DOUG DC9 DC931 3022065 WP E/E DOOR DIRTY A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 8925E 45840 AFTER TAKEOFF RECEIVED AN E/E DOOR WARNING INDICATION, LIGHT EXTINGUISHED AFT PRESSURIZATION. RETURNED TO SDF WITHOUT F URTHER INCIDENT. RECYCLED THE DOOR, CLEANED DEBRIS FROM THE DOOR TRACK AND RESET THE PLUG ON THE SWITCH, CHECKED OK. 2 L 7 2 4F A6WE 1996091900636 19960919 00636 EA 1996 9 19 COMA9660141 1 19960911 A 2997 WIRE CNDAIR CL600 CL6002B19 1900309 EA AFT EQUIP BAY BROKEN A COMA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 927CA 6993 7031 NR 1 HYDRAULIC SYSTEM INDICATES ZERO PRESSURE. REPLACED BROKEN WIRE AT HYDRAULIC PRESSURE TRANSDUCER. 2 L 7 2 4F RT A21EA 1996091900637 19960919 00637 EA 1996 9 19 COMA9660140 1 19960911 A 2750 860D10014 FECU CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 917CA 3958 2443 7017 FLAPS STUCK AT 20 DEGREES. REPLACED THE FLAP ELECTRONIC CONTROL UNIT. 2 L 7 2 4F RT A21EA 1996091900638 19960919 00638 NM 1996 9 19 UPS96221114 1 19960907 A 5313 STRINGER BOEING 727 72725C 138400H NM BS 1050 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE-SP, BS 1050 STR 16 HAS 2 CRACKS AND STR 17, 1 CRACK THROUGH FUSELAGE SKIN. REMOVED AND REPLACED DISCREP ANT SKIN AND DOUBLER. FABRICATED REPLACEMENT PARTS PER UPS SRM 53-30-3 FIG 12 53-30-2, 51-40-05 SKIN REPLACEMENT FROM S TA 1020 TO 1080 FROM STR 14R TO 20R. 2 L 7 3 4F A3WE 1996091900639 19960919 00639 NM 1996 9 19 UPS96221115 1 19960908 A 5412 INTERCOSTAL BOEING 727 72725C 138400H NM NR2 ENG FIREWALL CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE-SP, CRACK ACROSS 2 RIVET HOLES ON FLANGE OF HORIZONTAL INTERCOSTAL ON NR 2 ENG FIREWALL 4TH FWD FROM REA R ENG MT. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 54-10-3 FIG 2 AND 54-10-3 FIG 1. 2 L 7 3 4F A3WE 1996091900640 19960919 00640 NM 1996 9 19 UPS96221116 1 19960914 A 5311 FRAME BOEING 727 72725C 138400H NM BS 1070 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE-SP, FRAME CRACKED AT BS 1070 ABOVE AFT CARGO DOOR AT FWD HINGE ATTACH POINT. STOP DRILLED CRACK, REPAIR ED PER SRM 53-10-4 FIG 6. 2 L 7 3 4F A3WE 1996091900641 19960919 00641 NM 1996 9 19 96FDEA01477 1 19960913 A 5711 65185381 SPAR CHORD BOEING 727 72725 1384006 NM BS 870 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR 0661 AND 025, CORROSION AT BS 870 RBL 40 TO RBL 55, WL 190 UPPER CHORD. CORROSION IS OUT OF LIMITS AS PER FEDEX SRM. *S/D* REMOVED CORROSION ON UPPER STA 870 SPAR CHORD, FOUND SPAR CHORD IS OUT OF LIMITS PER FEDEX SRM 57-12-20. REMOV ED AND REPLACED UPPER CHORD PER FEDEX EA NR 7-5710-31178. 2 L 7 3 4F A3WE 1996091900642 19960919 00642 NM 1996 9 19 96FDEA01478 1 19960913 A 5315 BAC150529222 FLOORBEAM BOEING 727 72725 1384006 NM BS 328 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR 0656 AND 026, WHILE WORKING NR 0571, UPON REMOVAL OF HAT CHANNEL FOUND CORROSION ON FLOORBEAM UPPER CHORD AT BS 328 R BL 12 TO 15 WL 208. *S/D* UPPER CHORD OF FLOORBEAM WAS FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. REPAIRED FLOO RBEAM PER FEDEX SRM 53-10-8 FIG 9. 2 L 7 3 4F A3WE 1996091900643 19960919 00643 NM 1996 9 19 96FDEA01479 1 19960913 A 5320 65317731 CHORD BOEING 727 72725 1384006 NM BS 1176 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR 0288 AND 027, CORROSION (C53-224-01, -3) ON FWD FLANGE OF BS 1176 CHORD RBL 15 TO LBL 15 WL 208. *S/D* REPAIRED BS 1176.9 CHORD PER SB 727-53-0184 PART II OPTIONS. 2 L 7 3 4F A3WE 1996091900644 19960919 00644 NM 1996 9 19 96FDEA01480 1 19960913 A 5730 ARB126823 PANEL DOUG MD11 MD11 3023602 NM LT WING MISSING A FDEA K NONE O OTHER CR CRUISE 1 SO 25 586FE 48487 REF N0965, LT WING LWR SURFACE SLAT DRIVE ACCESS PNL MISSING AFTER TEST FLIGHT (P/N ARB1268-23) RIPPED OFF. REMOVED REM AINING PIECES, INSPECTED FOR DAMAGE, INSTALLED NEW ARB1268-23 PANEL AND HINGE ASSY, VERIFY LATCH TOLERANCES AND DOCUMENT ED ON NRB 6719 TABULATION SHEET. ALSO, VERIFIED AND DOCUMENTED RT WING. 2 L 7 3 4F RT A22WE 1996091900645 19960919 00645 NM 1996 9 19 96FDEA01481 1 19960916 A 5320 HFAB53FR011 DOORWAY FRAME BOEING 727 72725 1384006 NM BS 1057 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 509FE 18280 NR 0065 AND 019, FOUND AFT CARGO DOOR FWD CUTOUT FRAME CRACKED AT BS 1057 WL 162 RBL 40. *S/D* REMOVED AND REPLACED FR AME AT BS 1057 WL 162, RBL 40 PER FED EX DWG 6520728 AND FED EX EA 7-5310-2979D. 2 L 7 3 4F A3WE 1996091900646 19960919 00646 NM 1996 9 19 96FDEA01482 1 19960916 A 5330 65183864 SKIN BOEING 727 72725 1384006 NM BS 1060 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR 0300 AND 028, BS 1060 STR 24R WL 155 THERE IS A CRACK IN SKIN. *S/D* REMOVED DAMAGED SKIN AT BS 1060 STR 24R WL 155 AND REPAIRED PER FEDEX SRM 53-30-3 FIG 3A. 2 L 7 3 4F A3WE 1996091900647 19960919 00647 NM 1996 9 19 96FDEA01483 1 19960916 A 5330 651842013 SKIN BOEING 727 72725 1384006 NM BS 328 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR 0271 AND 029, BS 328 PLUS 7 WL 142 LBL 20 SKIN IS BULGING. *S/D* REMOVED DAMAGED SKIN AND INSTALLED EXTERNAL DOUBLE R AT BS 330 TO 356 WL 148 T0 152 LBL 20 IAW FEDEX SRM 53-30-3 FIG 3. 2 L 7 3 4F A3WE 1996091900648 19960919 00648 NM 1996 9 19 96FDEA01484 1 19960916 A 5320 651841 STIFFENER BOEING 727 72725 1384006 NM BS 314 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR 0425 AND 030, CORROSION (C53-111-01-1) ON HORIZONTAL STIFFENER AT BS 314 BL 0 TO LBL 12 WL 183. 2 L 7 3 4F A3WE 1996091900649 19960919 00649 WP 1996 9 19 96520 1 19960912 A 2560 113313 SLIDE DOUG DC9 DC932 3022066 WP FWD ENTRY FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 207ME 47794 CREW REPORTS FWD ENTRY DOOR EVACUATION SLIDE FELL OFF. MAINTENANCE REINSTALLED FWD ENTRY DOOR EVACUATION SLIDE. 2 L 7 2 4F A6WE 1996091900650 19960919 00650 WP 1996 9 19 96521 1 19960914 A 3350 P2070001201 LIGHT DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 602ME 48133 DURING SERVICE CHECK, FOUND AFT CABIN EMERGENCY FLASH LIGHT LED NOT FLASHING. MAINTENANCE REMOVED AND REPLACED AFT CABI N EMERGENCY FLASHLIGHT. 2 L 7 2 4F A6WE 1996091900651 19960919 00651 1996 9 19 96522 4 19960915 A 2565 SLIDE DOUG DC9 DC932 3022066 WP TAILCONE LOW PRESSURE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 DURING SERVICE CHECK, FOUND TAIL EVACUATION SLIDE PRESSURE LOW. MAINTENANCE REMOVED AND REPLACED TAIL EVACUATION SLIDE. 2 L 7 2 4F A6WE 1996091900652 19960919 00652 WP 1996 9 19 96523 1 19960916 A 2560 5917689103 SLIDE COVER DOUG DC9 DC932 3022066 WP GALLEY DOOR LOOSE A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 502ME 48132 CREW REPORTS GALLEY SERVICE DOOR EVACUATION SLIDE COVER WILL NOT STAY SECURE. MAINTENANCE SECURED GALLEY DOOR EVACUATIO N SLIDE COVER. 2 L 7 2 4F A6WE 1996091900653 19960919 00653 WP 1996 9 19 RRXA96086 1 19960912 A 2612 FIRE LOOP DOUG DC8 DC862 3021970 WP NR 2 ENGINE BROKEN WIRE A RRXA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 15 993CF 46028 KDAY - FLT 228 - IN FLIGHT, NR 2 ENGINE FIRE WARNING (BOTTLES WERE NOT DISCHARGED). SHUTDOWN ENGINE IN FLIGHT. INSPECT ED ALL FIRE LOOPS. FOUND BROKEN WIRE AT SPLICE ON FORWARD UPPER FIRE LOOP. REPAIRED SPLICE, HOT AIR LEAK CHECKED NR 2 ENGINE. NO LEAKS OR DEFECTS NOTED. PERFORMED MAINTENANCE POWER RUN NR 2 ENGINE. NR 2 ENGINE FIRE WARNING OPS CHECKS G OOD. (M) 2 L 7 4 4F 4A25 1996091900654 19960919 00654 NE 1996 9 19 CKSA96136 2 19960911 A 7530 555446 PS4 LINE DOUG DC8 DC8F55 3021928 WP PWA JT3D JT3D3B 52039 NE NR 1 ENGINE LOOSE A CKSA K NONE J WARNING INDICATION CR CRUISE 1 GL 23 6161C 45856 645442 NR 1 ENGINE FIRE CAME ON INTERMITTENTLY DURING FLIGHT WITH BLEED AIR ON FIRE WARNING TEST OK. TIGHTENED LOOSE LINE TO P RBC ON NR 1 ENGINE. RAN ENGINE AT VARIOUS POWER SETTING WITH BLEED ON, NO LEAKS NOTED. NO FIRE WARNING, OPS CHECK NORM AL. 2 L 7 4 4F 4 F 4A25 1E8 1996091900655 19960919 00655 WP 1996 9 19 CALA9601315 1 19960915 A 3260 802530 PROX CONTROL DOUG DC10 DC1010 3022110 WP NLG INOPERATIVE A CALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 09 68042 16954 8576 46901 THE NOSE GEAR RED LIGHT REMAINED ILLUMINATED AFTER GEAR EXTENSION ON APPROACH. ALTERNATE GEAR EXTENSION WAS USED AND GE AR WAS DOWN AND LOCKED. THE AIRCRAFT LANDED AT KIX WITHOUT INCIDENT. MAINTENANCE RESEATED THE PROXIMITY CONTROL UNIT, GEAR INDICATIONS CHECKED GOOD. 2 L 7 3 4F A22WE 1996091900656 19960919 00656 NM 1996 9 19 CALA9601316 1 19960915 A 3246 260151111 WHEEL HALF BOEING 737 737219 1384469 NM RT MLG DETACHED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10248 20344 WHILE REPLACING THE NR 4 MLG TIRE/WHEEL ASSEMBLY DUE TO TIRE WEAR, THE INNER WHEEL ASSEMBLY HUB WAS FOUND DETACHED FROM WHEEL HALF. THE NR 4 TIRE/WHEEL ASSEMBLY WAS REMOVED AND REPLACED. IN ADDITION, THE NR 3 MLG TIRE/WHEEL ASSEMBLY WAS R EMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. 2 L 7 2 4F A16WE 1996091900657 19960919 00657 WP 1996 9 19 9619821152 1 19960911 A 5330 SKIN DOUG DC10 DC1040 3023508 WP BS 1851 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 152US 46761 DURING T-CHECK, FOUND CORROSION AND A SHEARED BOLT IN THE 4L DOOR CUTOUT SPLICE FS 1851 AT LONGERON 15L. REPLACED BOLT PER SRM 51-31-01. 2 L 7 3 4F A22WE 1996091900658 19960919 00658 WP 1996 9 19 9619839609 1 19960913 A 5312 BULKHEAD WEB DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 609NW 47234 DURING LINE CHECK, FOUND A .375 INCH CRACK IN THE AFT PRESSURE BULKHEAD -13 SKIN AT THE UPPER LEFT DOOR STOP FITTING, LB L 6. ALSO, FOUND A CRACK IN THE UPPER RIGHT DOOR JAMB FITTING BEHIND THE STOP. REPLACED FITTING PER SRM 51-30-2 AND RE PAIRED THE SKIN CRACK PER EM 5312-01130 AND DWG J060088. 2 L 7 2 4F A6WE 1996091900659 19960919 00659 WP 1996 9 19 9619841152 1 19960915 A 5320 FITTING DOUG DC10 DC1040 3023508 WP BS 1521 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 152US 46761 DURING T-CHECK, FOUND CORROSION ON THE LONGERON 52 END FITTING AT FS 1521. REPLACED FITTING PER SRM 53-00-01. 2 L 7 3 4F A22WE 1996091900660 19960919 00660 WP 1996 9 19 9619859614 1 19960915 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 756 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 614NW 47128 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION AND A CRACK IN THE FLOOR SUPPORT FITTING AT FS 756 AND LON GERON 28R. REPLACED FITTING PER SRM 51-30-02. 2 L 7 2 4F A6WE 1996091900661 19960919 00661 WP 1996 9 19 9619869613 1 19960914 A 3350 CONNECTOR DOUG DC9 DC932 3022066 WP CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 615NW 47438 DURING FLIGHT, THE EMERGENCY EVACUATION LIGHTS ON SEATS KEEP FLASHING ON AND OFF. FOUND QUICK DISCONNECT CONNECTOR AT F S 250 LOOSE. RECONNECTED, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996091900662 19960919 00662 WP 1996 9 19 9619879931 1 19960915 A 2751 SRDL12C FLAP POS IND DOUG DC9 DC931 3022065 WP COCKPIT FAILED A NWAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 01 90S 35103 24854 47244 AFTER TAKEOFF AND UPON FLAP RETRACTION, THE LEFT FLAP INDICATED FULL RETRACTION WITH RIGHT FLAP INDICATING 15 DEGREES. F LIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED FLAP POSITION INDICATOR AND RESET CIRCUIT BREAK ER, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996091900663 19960919 00663 NM 1996 9 19 9619882715 1 19960913 A 3244 TIRES BOEING 727 7272S7 138407Z NM NR 1/2 FAILED A NWAA K NONE O OTHER LD LANDING 1 GL 01 719RC 22490 LEFT MAIN OUTBOARD TIRE APPEARS TO HAVE BLOWN OUT ON LANDING IN DTW. REPLACED BOTH NR 1 AND NR 2 TIRE ASSEMBLIES. 2 L 7 3 4F A3WE 1996091900664 19960919 00664 NM 1996 9 19 9619892709 1 19960913 A 2782 1U11032 ACTUATOR BOEING 727 727225 1384077 NM NR 3 LE SLAT FAILED A NWAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 01 818EA 10964 10948 22555 DURING TAKEOFF ON FLAP RETRACTION, THE NR 3 LEADING EDGE SLAT INDICATED DOWN. AIRCRAFT RETURNED TO MKE AND LANDED WITHO UT INCIDENT. REPLACED NR 3 LEADING EDGE FLAT ACTUATOR AND SLAT EXTEND SWITCH, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996091900665 19960919 00665 WP 1996 9 19 9619909607 1 19960915 A 5610 5912290506 WINDSHIELD DOUG DC9 DC932 3022066 WP RT COCKPIT SHATTERED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 607NW 2347 2347 47232 DURING CLIMB THROUGH FL240, THE FIRST OFFICER'S WINDSHIELD SHATTERED. RETURNED TO DTW WITHOUT FURTHER INCIDENT. REPLAC ED WINDSHIELD AND HEAT CONTROL UNIT (P/N 961-5059-002), (S/N 2253A) CHECKED OK. 2 L 7 2 4F A6WE 1996091900666 19960919 00666 WP 1996 9 19 9619919967 1 19960915 A 5270 SWITCH DOUG DC9 DC931 3022065 WP E/E DOOR STUCK A NWAA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 GL 01 9331 47263 DURING CLIMB, COULD NOT PRESSURIZE THE AIRCRAFT AND NOTED EXCESSIVE NOISE FROM THE AREA FORWARD OF THE INSTRUMENT PANEL. THE AUTO PRESSURIZATION AND DOOR WARNING SYSTEMS APPEARED TO BE OPERATING NORMALLY. RETURNED TO PHX WITHOUT FURTHER I NCIDENT. FOUND THE E/E COMPARTMENT DOOR OPEN AND THE SWITCH STUCK RESULTING IN A FALSE DOOR WARNING INDICATION. REPLAC ED THE DOOR WARNING SWITCH, CHECKED OK. 2 L 7 2 4F A6WE 1996091900667 19960919 00667 WP 1996 9 19 9619929862 1 19960910 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 771NC 47769 DURING LINE CHECK, FOUND THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHEC K OK. 2 L 7 2 4F A6WE 1996091900668 19960919 00668 NE 1996 9 19 9619931145 2 19960914 A 7320 7551501 SENSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 1 ENGINE FAILED A NWAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS LD LANDING 1 GL 01 145US 33942 8753 46754 86123 DURING LANDING ROLLOUT, THE NR 1 AND NR 3 ENGINES EXPERIENCED REVERSE STALL SIMULTANEOUSLY. BOTH ENGINES WERE SHUT DOWN DUE TO INCREASING EGT AND AIRCRAFT TAXIED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED BORESCOPE INSPECTION OF THE NR 3 ENGINE AND NO DISCREPANCIES WERE FOUND. VISUAL INSPECTION OF THE NR 1 ENGINE WAS NORMAL AND BORESCOPE WILL BE ACCOMPLISHED WITHIN FIVE CYCLES. REPLACED TT2 SENSOR ON THE NR 1 ENIGNE, LEAK CHECK WAS NORMAL. 2 L 7 3 4F 4 F A22WE E20EA 1996091900669 19960919 00669 1996 9 19 9619943220 4 19960914 A 2210 K217A8M8 FLT CONTL UNIT AIRBUS 320 A320211 3930320 EU E/E COMPT MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 01 320US 7229 213 IMMEDIATELY AFTER LEVEL OFF AT CRUISE FL350, LOST NR 1 AUTO-PILOT. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND RES ET NR 1 FLIGHT MANAGEMENT AND GUIDANCE COMPUTER WITH NO HELP. LATER, LOST THE FLIGHT CONTROL UNIT. AIRCRAFT DIVERTED T O MIA AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FLIGHT CONTROL UNIT, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996091900670 19960919 00670 NE 1996 9 19 9619959873 2 19960916 A 7530 492143 PRBC DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE LT ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 01 782NC 31482 48107 688793 WHEN APPLYING TAKEOFF POWER, THE LEFT ENGINE EXPERIENCED COMPRESSOR STALLS. CREW ABORTED TAKEOFF AND RETURNED TO THE GA TE. MAINTENANCE REPLACED THE LEFT ENGINE PRBC, RAN ENGINE TO TAKEOFF POWER, LEAK AND OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F A6WE E2EA 1996091900671 19960919 00671 WP 1996 9 19 9619969610 1 19960916 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 610NW 47432 DURING LINE MAINTENANCE INSPECTION, EXTERIOR EMERGENCY LIGHTS ILLUMINATED WITH SWITCH IN ARMED POSITION. TIGHTENED TERM INAL 7 ON BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996091900672 19960919 00672 WP 1996 9 19 9619979950 1 19960913 A 3350 60303451 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9346 47376 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS AT ROWS 12 THROUGH 14 INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996091900673 19960919 00673 WP 1996 9 19 9619989921 1 19960915 A 3350 60030451 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 943N 47647 DURING LINE MAINTENANCE INSPECTION, FOUND OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONA L CHECK NORMAL. 2 L 7 2 4F A6WE 1996091900674 19960919 00674 WP 1996 9 19 9619999903 1 19960915 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 953N 47083 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS IN FORWARD CABIN AND AT ROWS 13 THROUGH 14 INOPERATI VE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996091900675 19960919 00675 WP 1996 9 19 9620009957 1 19960915 A 3397 WIRE DOUG DC9 DC931 3022065 WP TAIL COMPT CORRODED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 915RW 47139 DURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPAIRED CORRODED SPLICE IN TAIL AREA, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996091900676 19960919 00676 WP 1996 9 19 9620019972 1 19960913 A 3350 LIGHT DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9336 47338 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS AT ROWS 8 THROUGH 15 INOPERATIVE. REPLACED POWER SU PPLIES AND BATTERY PACKS, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996091900677 19960919 00677 WP 1996 9 19 9620029996 1 19960913 A 3350 LIGHT DOUG DC9 DC931 3022065 WP LT NACELLE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8932E 47141 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. PROBLEM COULD NOT BE DUPLICATED. 2 L 7 2 4F A6WE 1996091900678 19960919 00678 WP 1996 9 19 9620039966 1 19960916 A 3350 6011779 BATTERY PACK DOUG DC9 DC931 3022065 WP LT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9330 47138 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996091900679 19960919 00679 NM 1996 9 19 SWAA960964 1 19960912 A 3350 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 360SW 26571 FOUND AFT EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996091900680 19960919 00680 NM 1996 9 19 SWAA960965 1 19960915 A 3350 900542 PWR SUPPLY BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 24SW 20925 DURING SCHEDULED SERVICE CHECK, FOUND FWD CABIN CEILING LIGHT INOP. REPLACED POWER SUPPLY PER BOEING M/M. 2 L 7 2 4F A16WE 1996091900681 19960919 00681 NM 1996 9 19 SWAA960966 1 19960913 A 3350 HOUSING BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 96SW 23055 DURING SCHEDULED SERVICE CHECK, FOUND AFT DOORS OVERHEAD EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK HOUSING PER BOEING M/M. 2 L 7 2 4F A16WE 1996091900682 19960919 00682 NM 1996 9 19 SWAA960967 1 19960913 A 3350 BATTERY BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED A2 CHECK, FOUND EMERGENCY BATTERY PACKS FOR OVERWING LIGHTS WILL NOT HOLD CHARGE. REPLACED BATTERY PAC KS PER BOEING M/M. 2 L 7 2 4F A16WE 1996091900683 19960919 00683 NM 1996 9 19 SWAA960968 1 19960913 A 3350 6104781 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 328SW 23342 DURING SCHEDULED TERMINAL CHECK, FOUND FWD CABIN EMERGENCY LIGHTS ERRATIC. REPLACED BATTERY PACK AND CHARGER PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996091900684 19960919 00684 NM 1996 9 19 SWAA960969 1 19960913 A 3350 LIGHTS BOEING 737 7373H4 1384600 NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 635SW 27708 DURING SCHEDULED RON CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOP AT MID CABIN INOP. REINSTALLED WIRING AND OP CHECKE D PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996091900685 19960919 00685 NM 1996 9 19 SWAA960970 1 19960915 A 5330 SKIN BOEING 737 7375H4 138449D NM BS 440 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 527SW 26569 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN DENTED AT BS 440, STRINGER 18R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996091900686 19960919 00686 NM 1996 9 19 SWAA960971 1 19960914 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 341/347 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED BC3 CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 341 AND 347, S17L. REPAIRED BOTH PER SWA RA 1-353-1515. 2 L 7 2 4F RT A16WE 1996091900687 19960919 00687 NM 1996 9 19 SWAA960972 1 19960914 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 500 OIL CANNING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED BC3 CHECK, FOUND FUSELAGE SKIN OIL CANNING AT BS 500 , S17L AND BS 500A, AT S22L. REPAIRED BOTH PER SW A RA 1-353-1515. 2 L 7 2 4F RT A16WE 1996091900688 19960919 00688 NM 1996 9 19 SWAA960973 1 19960913 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 847 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 356SW 25251 DURING SCHEDULED D-CHECK, FOUND AFT CARGO DOOR CUTOUT WEB DENTED AT BS 847 RBL 26 WL 156. REPLACED WITH NEW SECTION PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996091900689 19960919 00689 NM 1996 9 19 SWAA960974 1 19960913 A 5330 SKIN BOEING 737 7375H4 138449D NM PAX DOOR CUTOUT GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 525SW 26567 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED 15.5 BELOW AFT ENTRY DOOR. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996091900690 19960919 00690 NM 1996 9 19 SWAA960975 1 19960913 A 3350 BASE BOEING 737 7373H4 1384600 NM COCKPIT MALFUNCTIONED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 601SW 27695 AT GATE, FOUND EMERGENCY EXIT LIGHTS WOULD NOT TEST. REPLACED ARMED LIGHT BASE AND OP CHECKED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996091900691 19960919 00691 NM 1996 9 19 SWAA960976 1 19960907 A 3230 CIRCUIT BREAKER BOEING 737 7373H4 1384600 NM LANDING GEAR TRIPPED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 621SW 28037 AFTER TAKEOFF, CREW WAS UNABLE TO RAISE LANDING GEAR HANDLE. RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING. RESET LAN DING GEAR LATCH C/B AND RETRACTION TESTED GEAR PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996091900692 19960919 00692 NE 1996 9 19 WWMA9600071 2 19960915 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RIGHT FAILED A WWMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 WP 15 358RZ 5860 340B358 CREW REPORTED A LOUD NOISE AND AUTOCOURSEN ON TAKEOFF ROLL FROM THE RIGHT ENGIN E. MAINTENANCE REPLACED THE RIGHT ENGIN E. PRELIMINARY FINDINGS ON A BORESCOPE INSPECTION REVEALED EXTENSIVE DAMAGE TO BOTH THE HOT AND POWER SECTIONS OF THE E NGINE. THE ENGINE HAS BEEN SENT TO GENERAL ELECTRIC FOR FURTHER EVALUATION AND CAUSE OF DAMAGE. 2 L 7 2 4T 4 T RT A52EU E8NE 1996091900693 19960919 00693 WP 1996 9 19 96FDEA01489 1 19960916 A 5530 HI-LOCK COLLARS DOUG DC10 DC1030F 3023504 WP VERT STAB MISSING A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 322FE 47908 SNRM NR 0352, VERTICAL STABILIZER ALL COLLARS MISSING FROM HI-LOCKS BETWEEN AFT H-11 BOLTS THAT ATTACH UPPER VERICAL STA BILIZER TO LOWER VERTICAL STABILER. REF LAX C-CH-02, SNRM NR 0352. 2 L 7 3 4F RT A22WE 1996091900694 19960919 00694 WP 1996 9 19 96FDEA01476 1 19960913 A 3260 PROX CONTROL DOUG DC10 DC1030F 3023504 WP RT MLG MALFUNCTIONED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 303FE 46802 ON TAKEOFF, AFTER GEAR UP RIGHT MAIN GEAR RED LIGHT ILLUMINATED ON BOTH FRONT AND S/O PANEL RECYCLED GEAR AND LIGHT WENT OUT ON APPROACH TO ATL BEFORE GEAR DOWN RIGHT MAIN GEAR LIGHT AGAIN ILLUMNA, ON FRONT PANEL ONLY S/O PANEL NO LIGHT F ACT 11SEP96 22:30 ATL U REPLACED PROXIMITY SWITCH CONTROL UNIT MM 32-61-01. 2 L 7 3 4F RT A22WE 1996091900695 19960919 00695 WP 1996 9 19 SCNA96250 1 19960912 A 3350 A3060719103 TRACK DOUG DC10 DC1010 3022110 WP CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 573SC 46905 EMERGENCY FLOOR TRACK LIGHTING IN FORWARD CABIN, RIGHT SIDE FROM SEAT 5 TO SEAT 11, LIGHT INOP. FOUND DAMAGED RIBBON WI RE. REPAIRED WIRES, OPS CHECKED NORMALLY IN ACCORDANCE WITH MM 33-50-00. 2 L 7 3 4F A22WE 1996091900696 19960919 00696 NM 1996 9 19 SCNA96251 1 19960912 A 3350 900835A BATTERY PACK BOEING 727 7272A1 138407F NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 286SC 21601 FOUND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOP ON LINE CHECK. REMOVED AND REPLACED RIGHT OVERWING BATTERY PACK. EMERG ENCY LIGHTS OPS CHECK GOOD. 2 L 7 3 4F A3WE 1996091900697 19960919 00697 NM 1996 9 19 SCNA96252 1 19960912 A 3350 LAMP BOEING 727 7272A1 138407F NM CABIN FAILED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 286SC 21601 FOUND RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT INOP ON LINE CHECK. REMOVED AND REPLACED RIGHT OVERWING EMERGENCY LIG HT LAMP. EMERGENCY LIGHTS OPS CHECK GOOD. 2 L 7 3 4F A3WE 1996091900698 19960919 00698 NE 1996 9 19 96ZZZM1310 2 19960726 A 7321 FUEL CONTL BEECH 1900 1900C 1154161 CE PWA PT6 PT6A67D NE LT ENGINE MALFUNCTIONED A GLBA O OTHER J WARNING INDICATION CL CLIMB 1 CE 01 170GL UE170 CHS - AFTER DEPARTURE ON CLIMB-OUT, LEFT ENGINE STUCK AT 3600 TORQUE. N1 STAYED AT 95 PERCENT. MAINTENANCE REMOVED AND REPLACED HIGH PRESSURE FUEL PUMP AND FCU. OPERATIONAL CHECKED GOOD. REFERENCE GLBA96166. 2 L 7 2 4T 4 T RT A24CE E26NE 1996091900699 19960919 00699 CE 1996 9 19 96ZZZM1311 1 19960804 A 7120 12991003279 TRUSS BEECH 1900 1900D 1154162 CE ENGINE FAILED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 01 31YV 8433 UE31 DURING COMPLIANCE INSPECTION OF AD 95-02-18 AREA A, RIGHT ENGINE INBOARD UPPER TRUSS WAS FOUND SHEARED AT THE RIVET USED TO SEAL LINSEED OIL. TRUSS WAS REPLACED ENGINE INSPECTED. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A24CE 1996091900700 19960919 00700 NM 1996 9 19 96ZZZM1312 1 19960807 A 2530 DCH1072088 GALLEY CART BOEING 727 727230 1384080 NM AFT GALLEY NOT LATCHED A A IXKA O OTHER O OTHER LD LANDING 1 EA 25 357KP 20675 FLT NR 7 ATLANTA TO NEWARK - RUNAWAY SERVICE CART FROM AFT GALLEY BROKE THROUGH COCKPIT DOOR ON LANDING ROLLOUT. INSPEC TED AFT GALLEY, LATCHES AND GALLEY CART. FOUND ALL OK FOR SERVICE. REMOVED AND REPLACED COCKPIT DOOR. GALLEY CART REM OVED PRECAUTIONARY. (M) 2 L 7 3 4F A3WE 1996091900701 19960919 00701 1996 9 19 96ZZZM1313 4 19960821 A 3422 2594484 FLUX DETECTOR BAG JETSTM JETSTM3201 1500217 EU LT WING DAMAGED A VTZA K NONE O OTHER TX TAXI/GRND HDL 1 EA 27 493UE 805 FLT 6331 - IAD-BOS - DURING BOARDING, SHUTTLE BUS HIT RIGHT WING. NO FURTHER INCIDENTS OCCURRED. MX INSPECTED WING AND FOUND DAMAGE TO RIGHT AILERON AND WING TIP. MX REMOVED AND REPLACED LT AILERON ASSEMBLY, LT WING TIP, AND LT FLUX DETE CTOR AND BRACKETS. PERFORMED COMPASS SWING AND MAF. MAF PROVED GOOD, FERRIED AIRCRAFT TO IAD FOR FINAL VERIFICATION OF COMPASS SYSTEM. REFERENCE VTZA96318. 2 L 7 2 4T RT A56EU 1996091900703 19960919 00703 WP 1996 9 19 96ZZZM1315 2 19960821 A 7310 39423041 FUEL S/O VALVE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33110U 01514 WP RT ENGINE MALFUNCTIONED A VTZA F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 27 491UE 911 FLT NR 6550 - CHO-IAD - DURING TAXI, CREW BLEW BOTH FIRE BOTTLES ON RIGHT SIDE DUE TO RESIDUAL SMOKE DUE TO IMPROPER SHU T DOWN. BOTH BOOST PUMPS WERE LEFT ON AND PILOTS DID NOT MOTOR ENGINE THROUGH. AIRCRAFT WAS AT GATE, AND NO FURTHER IN CIDENTS. MAINTENANCE REMOVED AND REPLACED FIRE BOTTLES AND FUEL SHUT OFF VALVE, OPS CHECK OK. AIRCRAFT WAS RELEASED AN D APPROVED FOR RETURN TO SERVICE. REFERENCE VTZA96317. 2 L 7 2 4T 4 T RT A56EU E4WE 1996091900704 19960919 00704 NE 1996 9 19 96ZZZM1316 2 19960822 A 7532 A39710K PT2 PROBE BOEING 747 747136 1384883 NM PWA JT9 JT9D7A 52054 NE NR 3 ENG MALFUNCTIONED A A TWRA E ENGINE SHUTDOWN M R OVER TEMP PARTIAL RPM/PWR LOSS DE DESCENT 1 EA 15 606FF 20273 ON DESCENT FROM FL 390 THROTTLES RT BACK TO STOP, ENG AUDIBLE STALL ON NR 3 ENG. ENG SHUTDOWN, EGT 810 DEGREES CELSIUS. RELITE ATTEMPT AT FL 200 N2 40 PERCENT MAX EGT APPROACHED 650 DEGREE CELSIUS ENG SHUTDOWN SECOND RELITE ATTEMPT AT FL 110 WAS A NORM START ENG RAN NORM REMAINDER OF FLT PERFORMED PT2 LEAK CHK. FOUND PT2 PROBE CRACKED. REPLACED PT2 PROBE PER MM 77-11-06. LK CHECKED GOOD PER WIC 77-202-0. R/R PRBC AND FUEL AIR CONVERTER AS PER WIC 75-364 AND WIC 75-365. OPS AND LK CHECKED NORM, PERFORMED WIND MILL INSPECT, REPLACED OIL FILTER AND INSPECT CHIP DETECTORS. NO CHIPS FOUND, PERFORMED BOROSCOPE INSPECT OF COMPRESSOR AND TURBINE NO DEFECTS FOUND PER MM 72-00-00, RETURNED TO SERV, REF TWRA96289. 2 L 7 4 4F 4 F A20WE E20EA 1996091900705 19960919 00705 NE 1996 9 19 96ZZZM1317 2 19960822 A 7530 705942 CONVERTER BOEING 747 747136 1384883 NM PWA JT9 JT9D7A 52054 NE NR 3 ENG MALFUNCTIONED A A TWRA E ENGINE SHUTDOWN M R OVER TEMP PARTIAL RPM/PWR LOSS DE DESCENT 1 EA 15 606FF 20273 ON DESCENT FROM FL 390 THROTTLES RT BACK TO STOP, ENG AUDIBLE STALL ON NR 3 ENG. ENG SHUTDOWN, EGT 810 DEGREES CELSIUS. RELITE ATTEMPT AT FL 200 N2 40 PERCENT MAX EGT APPROACHED 650 DEGREE CELSIUS ENG SHUTDOWN SECOND RELITE ATTEMPT AT FL 110 WAS A NORM START ENG RAN NORM REMAINDER OF FLT PERFORMED PT2 LEAK CHK. FOUND PT2 PROBE CRACKED. REPLACED PT2 PROBE PER MM 77-11-06. LK CHECKED GOOD PER WIC 77-202-0. R/R PRBC AND FUEL AIR CONVERTER AS PER WIC 75-364 AND WIC 75-365. OPS AND LK CHECKED NORM, PERFORMED WIND MILL INSPECT, REPLACED OIL FILTER AND INSPECT CHIP DETECTORS. NO CHIPS FOUND, PERFORMED BOROSCOPE INSPECT OF COMPRESSOR AND TURBINE NO DEFECTS FOUND PER MM 72-00-00, RETURNED TO SERV, REF TWRA96289. 2 L 7 4 4F 4 F A20WE E20EA 1996091900706 19960919 00706 EU 1996 9 19 96ZZZM1318 1 19960821 A 7722 21180422 SRL COMPUTERS BAG JETSTM JETSTM3101 1500215 EU RT ENGINE FAILED A CX7A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 03 462CE 3867 684 FLT NR 404 - MDW - AT 300 FEET AGL, THE RIGHT ENGINE FAILED. AIRCRAFT RETURNED TO MDW UNEVENTFUL. MECHANIC INSPECTED A ND FOUND SRL COMPUTER INOPERATIVE. REPLACED SRL COMPUTER AND GROUND RUN WAS SATISFACTORY IAW MM. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996091900707 19960919 00707 NM 1996 9 19 96ZZZM1319 1 19960815 A 3350 6013211 BATTERY PACK BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHT RECEIVER WAS FOUND TO BE INOPERATIVE AT ROW 16. RE PLACED RECEIVER AND BATTERY PACK AND LIGHTS OPERATED NORMALLY. REFERENCE ASAA9610113. 2 L 7 2 4F A16WE 1996091900708 19960919 00708 EU 1996 9 19 96ZZZM1320 1 19960827 A 3260 CONNECTOR SAAB SF340 340B 7860101 EU LT MLG LOOSE A NVEA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 03 191AE 340B191 FLT 4905 - ROC - LEFT MAIN GEAR INDICATION, NO GREEN DOWN AND LOCKED. TRANSIT LIGHTS DID ILLUMINATE. FOLLOWED QRH PROC EDURES. VISUALLY SAW GEAR DOWN. COMPLETED A TOWER FLY BY FOR VERIFICATION. DECLARED EMERGENCY, LANDED WITHOUT FURTHER INCIDENT. INSPECTED WIRING AND SWITCHES, FOUND CANNON PLUG CAME OFF SWITCH ASSEMBLY. RECONNECTED AND ALL INDICATIONS NORMAL. (M) 2 L 7 2 4T RT A52EU 1996091900709 19960919 00709 EU 1996 9 19 96ZZZM1321 1 19960825 A 3350 LIGHT STBROS SD3 SD360 8100606 EU CABIN MALFUNCTIONED A GUUA K NONE L NO TEST IN INSP/MAINT 1 SO 19 830BE SH3756 FLT 388 - FPO-MIA - EMERGENCY PASSENGER COMPARTMENT LIGHTING ILLUMINATED INFLIGHT. OPERATED SYSTEM, FOUND TO FUNCTION P ROPERLY, COULD NOT DUPLICATE. (M) 2 H 7 2 4T A41EU 1996091900710 19960919 00710 EU 1996 9 19 96ZZZM1322 1 19960827 A 3350 6F40 DIODE STBROS SD3 SD360 8100606 EU COCKPIT FAILED A GUUA K NONE L NO TEST IN INSP/MAINT 1 SO 19 830BE SH3756 FLT 485 - TPA-MIA - EMERGENCY PASSENGER LIGHTING TRIPS ON (ARMED POSITION) WHEN TRANSFERRING POWER FROM EXTERNAL TO INTE RNAL. REMOVED AND REPLACED LIGHT DIODE. (M) 2 H 7 2 4T A41EU 1996091900711 19960919 00711 NM 1996 9 19 AALA961007 1 19960625 A 5315 141N5112 FLOOR BEAM BOEING 757 757223 1384957 NM BS 365 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 652AA 24610 AFW - FOUND FLOOR BEAM CORROSION BLENDED BEYOND SRM LIMITS. REPAIR PER MRB 757-868. (M) 2 L 7 2 4F RT A2NM 1996091900712 19960919 00712 NM 1996 9 19 AALA961008 1 19960625 A 5315 141N5113 FLOOR BEAM BOEING 757 757223 1384957 NM BS 377 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 652AA 24610 AFW - FOUND FLOOR BEAM AT STATION 377 CORROSION BEYOND SRM LIMITS. REPAIR PER MRB 757-867. (M) 2 L 7 2 4F RT A2NM 1996091900713 19960919 00713 NM 1996 9 19 AALA961009 1 19960625 A 5311 143N1013 FRAME BOEING 757 757223 1384957 NM BS 524 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 652AA 24610 AFW - FOUND FUSELAGE FRAME CRACKED AT 524R. REPAIRED PER MRB 757-872. (M) 2 L 7 2 4F RT A2NM 1996091900714 19960919 00714 NM 1996 9 19 AALA961010 1 19960625 A 5320 DOOR SILL BOEING 757 757223 1384957 NM CARGO COMPT CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 652AA 24610 AFW - FOUND CORRODED LOWER SILL BEYOND SRM LIMITS. REPAIRED PER MRB 757-865. (M) 2 L 7 2 4F RT A2NM 1996091900715 19960919 00715 NM 1996 9 19 AALA961011 1 19960625 A 5321 146N5300 DECK PLATE BOEING 757 757223 1384957 NM BS 1681 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 652AA 24610 AFW - FOUND DECK PLATE CORROSION BEYOND SRM LIMITS. REPAIR PER MRB 757-871. (M) 2 L 7 2 4F RT A2NM 1996091900716 19960919 00716 NM 1996 9 19 AALA961012 1 19960625 A 5210 141N8315 STUB FRAME BOEING 757 757223 1384957 NM PAX DOOR GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 652AA 24610 AFW - FOUND NR 1 ENTRY DOOR HAS GOUGE BLENDED BEYOND SRM LIMITS. REPAIR PER MRB 757-875. (M) 2 L 7 2 4F RT A2NM 1996091900717 19960919 00717 NM 1996 9 19 AALA961127 1 19960725 A 5330 146N3780 SKIN BOEING 757 757223 1384957 NM BS 1701 SCRATCHED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 624AA 24582 AFW - FOUND SKIN SCRATCH APPROX 6 INCHES LONG AND .004 INCH DEEP. SCRATCH IS THROUGH 4 FASTENER HEADS STATION 1701, STR 29L. FASTENERS HAVE BEEN REPLACED. REPLACED AFFECTED FASTENERS CHECK BLENDED AREA USING DYE CHECK AND EDDY CURRENT TO ENSURE NO CRACKS EXIST, APPLY CLEAR ALODINE. (M) 2 L 7 2 4F RT A2NM 1996091900718 19960919 00718 NM 1996 9 19 AALA961151 1 19960731 A 5531 173N1207 RIB BOEING 757 757223 1384957 NM VERT STAB DRILL MARKS A AALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 662AA 25296 AFW - FOUND VERTICAL STABILIZER RIB AT STATION 206 HAS DRILL MARKS. (M) 2 L 7 2 4F RT A2NM 1996091900719 19960919 00719 NM 1996 9 19 AALA961152 1 19960731 A 5330 146N34000 SKIN BOEING 757 757223 1384957 NM BS 1580 SCRATCHED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 662AA 25296 AFW - FOUND SCRATCH IN SKIN AFT FUSELAGE APPROX STATION 1580, STRINGER 27R. (M) 2 L 7 2 4F RT A2NM 1996091900720 19960919 00720 NM 1996 9 19 AALA961161 1 19960806 A 5315 FLOOR BEAM BOEING 727 727223 1384074 NM BS 1130 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - FOUND TOP OF FLOOR BEAM CORRODED, RBL 20 INCHES TO WS 70. INSTALLED REPAIR STRAPS PER 53-10-7-1 PG 1 3727 AARD/MS /MG. (M) 2 L 7 3 4F A3WE 1996091900721 19960919 00721 WP 1996 9 19 AALA961162 1 19960802 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1967-2007 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 143AA 46555 TUL - FOUND OUTBOARD G-7 GALLEY SUPPORT HAS CORROSION DAMAGE FROM STATION 1967-2007. INSTALL S/S STRAP DOUBLER PER ESO 7349, DATED 8-1-96. (M) 2 L 7 3 4F A22WE 1996091900722 19960919 00722 WP 1996 9 19 AALA961163 1 19960802 A 5320 52924410 ANGLE DOUG DC10 DC1030 3023501 WP BS 2007 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 143AA 46555 TUL - FOUND CORROSION ON 'T' ANGLE BETWEEN OUTBOARD G-7 GALLEY SUPPORT AND NR 8 SEAT TRACK. INSTALL REPAIR ANGLE ON LOW ER SIDE OF 'T' ANGLE AND STRAP ON TOP PER ESO 7349 DTD 8-1-96. (M) 2 L 7 3 4F A22WE 1996091900723 19960919 00723 WP 1996 9 19 AALA961164 1 19960802 A 5347 NFA622213 SEAT TRACK DOUG DC10 DC1030 3023501 WP BS 1960 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 143AA 46555 TUL - FOUND CORROSION ON SEAT TRACK NR 8. REMOVED DAMAGED SECTION OF TRACK AND SPLICE IN NEW SECTION PER ESO 7399 AND D ATED 8-1-96. (M) 2 L 7 3 4F A22WE 1996091900724 19960919 00724 NM 1996 9 19 AALA961171 1 19960729 A 5730 111T3013 SKIN BOEING 767 767223 1385123 NM WING BOX CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 325AA 22326 AFW - FOUND WING BOX UPPER SKIN CORRODED. REMOVED FASTENERS AND REMOVED CORROSION AND BLENDED. SHOT PEENED AND SPOT FA CED FASTENER HOLES ALODINED AND PRIMED. APPROVED BY ENGINEERING PER MRB 767-1275. (M) 2 L 7 2 4F RT A1NM 1996091900725 19960919 00725 NM 1996 9 19 AALA961174 1 19960805 A 5711 SPAR BOEING 727 727223 1384074 NM WS 720-738 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 709AA 22466 TUL - FOUND CORROSION ON FORWARD WING SPAR AND LOWER CHORD ANGLE. CORROSION REMOVED INSTALLED DOUBLERS PER SRM 57-10-6 PG 2A-2C, 6, 7, AND 9. (M) 2 L 7 3 4F A3WE 1996091900726 19960919 00726 NM 1996 9 19 AALA961175 1 19960805 A 2782 4031396 ACT BRACKET BOEING 727 727223 1384074 NM NR 5 LE FLAP CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 709AA 22466 TUL - FOUND CORROSION VERTICAL BRACKET 11B NR 5 LSAT ACTUATOR BY NR 3 FUEL VALVE. REMOVED AND REPLACED BRACKET WITH NEW SERVICABLE BRACKET. (M) 2 L 7 3 4F A3WE 1996091900727 19960919 00727 NM 1996 9 19 AALA961176 1 19960805 A 5512 SKIN BOEING 727 727223 1384074 NM CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 709AA 22466 TUL - FOUND LEFT HORIZONTAL STABILIZER TRAILING EDGE SKIN CORRODED, AT UPPER SKIN ABOVE OUTBOARD ELEVATOR FITTING. REMO VED CORROSION, TREATED AND INSTALLED EXTERNAL DOUBLER PER ESO1 697 DATED 6-21-96. (M) 2 L 7 3 4F A3WE 1996091900728 19960919 00728 NM 1996 9 19 AALA961177 1 19960805 A 5330 SKIN BOEING 727 727223 1384074 NM BS 720 WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 709AA 22466 TUL - FOUND LEFT LEADING EDGE WING RUBBING FUSELAGE 2 SPOTS STATIONS 720D AND 720E, STRINGER 18L AND STRINGER 19. CUT O UT WORN SPOTS (2) ON FUSELAGE. INSTALLED FILLERS AND OUTSIDE DOUBLER OVER Z AREAS. DOUBLERS ARE ONE CONTINUED PIECE CO NSTRUCTION. 2 L 7 3 4F A3WE 1996091900729 19960919 00729 NM 1996 9 19 AALA961178 1 19960805 A 5530 STRINGER BOEING 727 727223 1384074 NM VERT FIN CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 709AA 22466 TUL - FOUND VERT FIN INTERIOR, STRINGER 9L, CRACKED AT BOLT ATTACH POINT TO RIB NR 2. REPAIRED WITH DOUBLER PER ESO 116 97, DATED 7-1-96. (M) 2 L 7 3 4F A3WE 1996091900730 19960919 00730 NM 1996 9 19 AALA961179 1 19960805 A 5320 TQ BOX WEB BOEING 727 727223 1384074 NM BS 1273 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 709AA 22466 TUL - FOUND 2 INCH CRACK IN RIGHT TORQUE BOX WEB BELOW AIR STAIR ACTUATOR. INSTALLED WEB REPAIR ON TORQUE BOX PER SB 72 7-53-0129 DATED 11-7-91 FIG 1-4. (M) 2 L 7 3 4F A3WE 1996091900731 19960919 00731 NM 1996 9 19 AALA961180 1 19960805 A 3220 651841316 DRAG BRACE BOEING 727 727223 1384074 NM BS 294.5 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 709AA 22466 TUL - FOUND DRAG BRACE BUSHING BORES CORRODED BEYOND ALLOWABLE LIMITS 2.730. REMOVED AND REPLACED DRAG BRACE PER DWG N R 6518413 AND SRM 53-43-1 PG 1. (M) 2 L 7 3 4F A3WE 1996091900732 19960919 00732 NM 1996 9 19 AALA961181 1 19960805 A 5320 6558518 SPLICE BOEING 727 727223 1384074 NM BS 870 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 709AA 22466 TUL - FOUND CORROSION ON THE STRINGER 18 SPLICES PLATE RIGHT. REMOVED AND TREATED CORROSION, BLENDOUT BEYOND MM AND SRM LIMITS. REPAIRED PER BOEING MESSAGE AND ESO 11697 DTD 7-25-96. (M) 2 L 7 3 4F A3WE 1996091900733 19960919 00733 NM 1996 9 19 AALA961182 1 19960805 A 5310 STRUCTURE BOEING 727 727223 1384074 NM BS 783-804 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 709AA 22466 TUL - FOUND CORROSION LOWER FUSELAGE RIGHT INSIDE A/C BAY STATION 783.95 TO 804.5, 2 SMALL AREAS. REMOVED CORROSION BEY OND SRM LIMITS 57-30-1 BY ESO 11697, DATED 7/5/96. (M) 2 L 7 3 4F A3WE 1996091900734 19960919 00734 NM 1996 9 19 AALA961183 1 19960805 A 5321 FLOOR PNL BOEING 727 727223 1384074 NM BS 1158-1179 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 709AA 22466 TUL - FOUND LEFT AFT LAVATORY FLOOR CORRODED THREE PLACES AND AROUND THE PUMP SHUTE TO THE ANGLE AT THE DITCHING PANELS. MADE STAINLESS STEEL WEB REPAIR, CAD-PLATED AND PRIMED AND INSTALLED WITH 870 SEALER REF SRM 51-40-2. (M) 2 L 7 3 4F A3WE 1996091900735 19960919 00735 NM 1996 9 19 AALA961184 1 19960805 A 5330 SKIN BOEING 727 727223 1384074 NM BS 700-720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 709AA 22466 TULE - FOUND CORROSION ON BELLY SKIN BETWEEN STRINGERS 28L-28R AND STATIONS 700-720 PLUS 10. REPLACED BELLY SKIN FROM S TATION 680-720A AND STRINGER 28L - 28R PER SRM 53-30-3 PG 60. (M) 2 L 7 3 4F A3WE 1996091900736 19960919 00736 NM 1996 9 19 AALA961185 1 19960805 A 5320 DOOR FRAME BOEING 727 727223 1384074 NM BS 372 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 709AA 22466 TUL - FOUND GALLEY DOOR SUPPORT FRAME HAS CORROSION AT STA 372, STRINGER 17R TO 6 INCHES ABOVE 17R. FABRICATED AND INST ALLED FORMED ANGLE REPAIR PER SRM 51-40-3 PG 3. (M) 2 L 7 3 4F A3WE 1996091900737 19960919 00737 NM 1996 9 19 AALA961186 1 19960805 A 5330 SKIN BOEING 727 727223 1384074 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 709AA 22466 TUL - FOUND CORROSION ON SKIN AFT OF BUTTE AIR DOOR. REMOVED CORROSION. INSTALLED DOUBLER PER ESO 11697, DATED 6-28-96 AND SRM 53-30-3 FIG 2/3. (M) 2 L 7 3 4F A3WE 1996091900738 19960919 00738 NM 1996 9 19 AALA961187 1 19960805 A 5320 DOOR FRAME BOEING 727 727223 1384074 NM BS 377 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 709AA 22466 TUL - FOUND FORWARD GALLEY FORWARD DOOR FRAME HAS CORROSION AT STRINGER 17R TO 'I' ABOVE 17R, STATION 376-377. CUT OUT CORROSION AREA, MADE AND INSTALLED FILLER TO FORMED ANGLE PER SRM 51-40-3 PG 3. (M) 2 L 7 3 4F A3WE 1996091900739 19960919 00739 NM 1996 9 19 AALA961188 1 19960805 A 5315 FLOOR BEAM BOEING 727 727223 1384074 NM BS 380 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 709AA 22466 TUL - FOUND FLOOR BEAM CORRODED FROM INBOARD SEAT TRACK TO OUTBOARD CREASE ANGLE RIGHT STATION 380. CUT OUT CORRODED FL OOR BEAM UPPER FLANGE AND REPAIRED PER SRM 53-10-8 PG 9B. (M) 2 L 7 3 4F A3WE 1996091900740 19960919 00740 NM 1996 9 19 AALA961211 1 19960809 A 5210 146N62016 DOOR PAN BOEING 757 757223 1384957 NM R4 DOOR GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 655AA 24613 AFW - FOUND DOOR HANDLE PAN GOUGED BEYOND SRM LIMITS. REPAIR PER MRB 757 909. (M) 2 L 7 2 4F RT A2NM 1996091900741 19960919 00741 NM 1996 9 19 AALA961212 1 19960809 A 5315 146N5089 FLOOR BEAM BOEING 757 757223 1384957 NM BS 1640 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 655AA 24613 AFW - AFTER CORROSION REMOVAL, REMAINING THICKNESS IS BEYOND SRM LIMITS. REPAIR PER MRB 757-907. (M) 2 L 7 2 4F RT A2NM 1996091900742 19960919 00742 NM 1996 9 19 AALA961213 1 19960809 A 5310 141N5161 FLOOR STRUCTURE BOEING 757 757223 1384957 NM BS 370 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 655AA 24613 AFW - AFTER REMOVING CORROSION, REMAINING THICKNESS BEYOND SRM LIMITS. REPAIR PER MRB 757-903. (M) 2 L 7 2 4F RT A2NM 1996091900743 19960919 00743 NM 1996 9 19 AALA961214 1 19960809 A 5321 146N5300 DECK PLATE BOEING 757 757223 1384957 NM BS 1701 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 655AA 24613 AFW - AFTER CORROSION REMOVAL, REMAINING THICKNESS BEYOND SRM LIMITS. REPAIR PER MRB 757-902. (M) 2 L 7 2 4F RT A2NM 1996091900744 19960919 00744 NM 1996 9 19 AALA961215 1 19960809 A 5315 141N5112 FLOOR BEAM BOEING 757 757223 1384957 NM BS 365 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 655AA 24613 AFW - FOUND AFTER CORROSION REMOVAL, BEAM THICKNESS LESS THAN SRM LIMITS. REPAIR PER MRB 757-901. (M) 2 L 7 2 4F RT A2NM 1996091900745 19960919 00745 NM 1996 9 19 AALA961216 1 19960809 A 3230 160N02D3 BUSHING BOEING 757 757223 1384957 NM RT MLG WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 655AA 24613 AFW - INSPECT RIGHT MLG BUSHING FOR MIGRATION. INSPECTION PER MRB 757-900. (M) 2 L 7 2 4F RT A2NM 1996091900746 19960919 00746 WP 1996 9 19 AALA961229 1 19960816 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 401-422 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 137AA 47847 TUL - FOUND GALLEY NR 2 STRUCTURE SUPPORT HAS CORROSION AROUND MOUNTING HOLE AND AT END ATTACHMENT. REMOVED AND REPLACE D SUPPORT STRUCTURE WITH NEWLY FABRICATED PART PER SRM 53-00-01 TREATED AND PAINTED AREA PER SRM 51-21-01. (M) 2 L 7 3 4F A22WE 1996091900747 19960919 00747 NM 1996 9 19 AALA96173 1 19960826 A 5315 111T5008 FLOOR BEAM BOEING 767 767223 1385123 NM CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 325AA 22326 AFW - FOUND FLOOR BEAM HAS CORROSION BEYOND SRM LIMITS. ACCEPTABLE WITH NOTED CONDITION PER ENGINEERING MRB 767-1274. ( M) 2 L 7 2 4F RT A1NM 1996091900748 19960919 00748 NM 1996 9 19 ASAA9610113 1 19960815 A 3350 883200312 RECEIVER BOEING 737 737290C 138448V NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHT RECEIVER WAS FOUND TO BE INOPERATIVE AT ROW 16. RE PLACED RECEIVER AND BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1996091900749 19960919 00749 NM 1996 9 19 ASAA9610118 1 19960828 A 5210 507945178 HINGE PLATE BOEING 737 737210C 1384459 NM L-1 DOOR LACK OF LUBE A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 744AS 21822 SEA - FLT 64 - CREW REPORTED, L-1 DOOR HARD TO CLOSE. CLEANED AND LUBED HINGE PLATE BEARING SURFACE. INSPECTED DOOR, N O DEFECTS FOUND. DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1996091900750 19960919 00750 NM 1996 9 19 ASAA9610119 1 19960830 A 5315 65549064 FLOOR BEAM BOEING 737 737290C 138448V NM BS 520 CORROSION A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING D-CHECK, THE FLOOR BEAM FORWARD FLANGE AT BS 520, LBL 35 TO LBL 43 WAS FOUND TO BE CORRODED. REPAIRED PER EA 5310-01487 AND BOEING TELEX ASA-SEA-96-0392RR. (M) 2 L 7 2 4F A16WE 1996091900751 19960919 00751 NM 1996 9 19 ASAA9610120 1 19960830 A 5315 65549064 FLOOR BEAM BOEING 737 737290C 138448V NM BS 520 CORROSION A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING D-CHECK, THE FLOOR BEAM FORWARD LOWER FLANGE AT BS 520, LBL 40 TO LBL 45 WAS FOUND TO BE CORRODED. REPAIRE D PER EA 5310-01487 AND BOEING TELEX ASA-SEA-96-0392RR. (M) 2 L 7 2 4F A16WE 1996091900752 19960919 00752 NM 1996 9 19 ASAA9610123 1 19960830 A 5314 6545435501 KEEL BEAM BOEING 737 737290C 138448V NM BS 540 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING D-CHECK, A CRACK WAS IDENTIFIED ON THE HORIZONTAL FLANGE OF THE KEEL BEAM CHORD AT BS 540, RBL 6.30. REPAI RED PER EA 5310-01479 AND BOEING TELEX ASA-SEA-96-0404RR. (M) 2 L 7 2 4F A16WE 1996091900753 19960919 00753 NM 1996 9 19 ASAA9610124 1 19960830 A 5315 65549083 FLOOR BEAM BOEING 737 737290C 138448V NM BS 787 CORROSION A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING D-CHECK, THE FLOOR BEAM LOWER FORWARD FLANGE AT BS 787, LBL 25 AND RBL 3 WERE FOUND TO BE CORRODED. REPAIR ED PER EA 5310-01484 AND BOEING TELEX ASA-SEA-96-0390RR. (M) 2 L 7 2 4F A16WE 1996091900754 19960919 00754 NM 1996 9 19 ASAA9640070 1 19960817 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 771AS 25104 SEA - FLT 441 - PRIOR TO DEPARTURE, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 19 WERE FOUND TO BE INOPERATIVE. RECON NECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996091900756 19960919 00756 NM 1996 9 19 ASAA9640072 1 19960825 A 5210 BACB10AF6F3H CAM BEARING BOEING 737 7374Q8 NM R1 DOOR FROZEN A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 783AS 25114 PHX - FLT 97 - DURING CREW PREFLIGHT, THE R-1 DOOR WAS HARD TO OPEN PAST 50 PERCENT. FERRIED AIRCRAFT TO SEA. FOUND FO RWARD CAM ROLLER FROZEN, REPLACED FORWARD CAM ROLLER. DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996091900757 19960919 00757 WP 1996 9 19 ASAA9680175 1 19960812 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 941AS 49925 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996091900758 19960919 00758 WP 1996 9 19 ASAA9680177 1 19960813 A 3397 WIRE DOUG DC9 DC982 3022082 WP CATWALK BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 955AS 48080 SEA - DURING MAINTENANCE CHECK, THE FORWARD OVERHEAD EMERGENCY LIGHT IN CATWALK WAS FOUND INOPERATIVE. REPAIRED BROKEN WIRE AT GROUND TERMINAL AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996091900759 19960919 00759 WP 1996 9 19 ASAA9680178 1 19960821 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 969AS 53063 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS AT ROW 6 WERE FOUND INOPERATIVE. FOUND WIRING DISCONNE CTED, RECONNECTED WIRING AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996091900760 19960919 00760 SO 1996 9 19 ASOA96032 1 19960807 A 2710 AILERON CONTL EMB 120 EMB120RT SO LT/RT WINGS ROLL RIGHT A A YSOA O OTHER F FLT CONT AFFECTED CL CLIMB 1 EA 03 275AS 120234 FLT NR 7259 - OUTBOUND ATL-BQK, CAPTAIN EXPERIENCED A STRONG RIGHT ROLL TENDENCY IN THE AILERONS WITH AUTOPILOT OFF. CR EW ELECTED TO RETURN TO ATL AND REQUESTED EQUIPMENT TO MEET THE AIRCRAFT. LANDING WAS MADE SAFELY IN ATL WITHOUT FURTHE R INCIDENT. EXTENSIVE TROUBLESHOOTING AND OPERATIONAL CHECKS WERE GOOD, THE PROBLEM COULD NOT BE DUPLICATED. A TEST FL IGHT WAS REQUESTED TO CHECK THE AILERON AND AUTOPILOT SYSTEMS AND WAS COMPLETED SATISFACTORILY. (M) 2 L 7 2 4T RT A31SO 1996091900761 19960919 00761 NM 1996 9 19 AWXA960377 1 19960727 A 5315 FLOOR BEAM BOEING 737 737277 1384570 NM BS 294 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 PAE - FLT 7848 - DURING ROUTINE SCHEDULED C-16 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM AT STATION 294, LBL 15 T O RBL 45, WL 208. REPLACED UPPER T-CHORD WITH FABRICATED PART BS 294, LBL 60 TO RBL 60, WL 208. (M) 2 L 7 2 4F RT A16WE 1996091900762 19960919 00762 NM 1996 9 19 AWXA960378 1 19960729 A 5330 SKIN BOEING 737 737277 1384570 NM BS 727 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 PAE - FLT 7848 - DURING ROUTINE SCHEDULED C-16 MAINTENANCE CHECK, FOUND 2 HOLES THROUGH SKIN AT BS 727B, STRINGER 16L (C RACK IN SKIN). REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-30-3. (M) 2 L 7 2 4F RT A16WE 1996091900763 19960919 00763 NM 1996 9 19 AWXA960379 1 19960729 A 5320 SILL BOEING 737 737277 1384570 NM BS 344 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 PAE - FLT 7848 - DURING ROUTINE SCHEDULED C-16 MAINTENANCE CHECK, FOUND CORROSION ON FWD MOPSILL AT BS 344, LBL 65, WL 2 08. REPLACED FWD MOPSILL AT BS 294 TO 360, LBL 65, WL 208. (M) 2 L 7 2 4F RT A16WE 1996091900764 19960919 00764 NM 1996 9 19 AWXA960380 1 19960731 A 5320 SILL BOEING 737 737277 1384570 NM BS 270-360 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 PAE - FLT 7848 - DURING ROUTINE SCHEDULED C-16 MAINTENANCE CHECK, FOUND RIGHT FWD THRESHOLD CORRODED BS 270-360, WL 208, RBL 60. REMOVED AND REPLACED MOPSILL PER SRM 51-30-2, SRM 51-10-1. (M) 2 L 7 2 4F RT A16WE 1996091900765 19960919 00765 NM 1996 9 19 AWXA960381 1 19960729 A 5347 SEAT TRACK BOEING 737 737277 1384570 NM BS 328-344 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 PAE - FLT 7848 - DURING ROUTINE SCHEDULED C-16 MAINTENANCE CHECK, FOUND CORROSION ON SEAT TRACK AT STATION 328-344, RBL 45, WL 208. REMOVED, FABRICATED AND INSTALLED PER SRM 51-10-1, 51-21-41. (M) 2 L 7 2 4F RT A16WE 1996091900767 19960919 00767 NM 1996 9 19 AWXA960388 1 19960802 A 5511 6547987504 RIB BOEING 737 737277 1384570 NM HORIZ STAB CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 PAE - FLT 7803 - DURING ROUTINE SCHEDULED C-8 MAINTENANCE CHECK, FOUND CRACK AT L/E ON RIGHT H-STAB RIBS NR 1, 2, 6 AND 7 FROM INBOARD SIDE. REMOVED NR 1 RIB, REPLACED CHORD AND REINSTALLED RIB PER SRM 51-30-2. REMOVED NR 2 RIB, FABRICATE D DOUBLER AND INSTALLED DOUBLER AND REINSTALLED RIB PER SRM 51-30-2. REMOVED RIB NR 6, FABRICATED DOUBLER AND INSTALLED AND REINSTALLED RIB PER SRM 51-30-2. REMOVED RIB NR 7 AND REPLACED WITH NEW ONE PER SRM 51-30-2. (M) 2 L 7 2 4F RT A16WE 1996091900768 19960919 00768 NM 1996 9 19 AWXA960389 1 19960802 A 5511 6547987504 RIB BOEING 737 737277 1384570 NM HORIZ STAB CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 PAE - FLT 7803 - DURING ROUTINE SCHEDULED C-8 MAINTENANCE CHECK, FOUND RIGHT H-STAB L/E RIB NR 4 FROM INBOARD SIDE CRACK ED. REMOVED AND REPLACED RIB ON RIGHT H-STAB L/E PER SRM 51-30-2. (M) 2 L 7 2 4F RT A16WE 1996091900769 19960919 00769 NM 1996 9 19 AWXA960390 1 19960803 A 5511 654789504 RIB BOEING 737 737277 1384570 NM HORIZ STAB CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 PAE - FLT 7803 - DURING ROUTINE SCHEDULED C-8 MAINTENANCE CHECK, FOUND RIGHT H-STAB L/E RIB NR 10 FROM INBOARD SIDE CRAC KED. REPLACED RIB NR 10 PER SRM 51-30-2. (M) 2 L 7 2 4F RT A16WE 1996091900770 19960919 00770 NM 1996 9 19 AWXA960391 1 19960803 A 5511 65479886 RIB BOEING 737 737277 1384570 NM HORIZ STAB CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 PAE - FLT 7803 - DURING ROUTINE SCHEDULED C-8 MAINTENANCE CHECK, FOUND RIGHT H-STAB L/E RIB NR 8 FROM INBOARD SIDE CRACK ED REPLACED RIB NR 8 PER SRM 51-30-2. (M) 2 L 7 2 4F RT A16WE 1996091900771 19960919 00771 NM 1996 9 19 AWXA960392 1 19960803 A 5511 6547536506 RIB BOEING 737 737277 1384570 NM HORIZ STAB CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 PAE - FLT 7803 - DURING ROUTINE SCHEDULED C-8 MAINTENANCE CHECK, FOUND RIGHT H-STAB L/E RIB NR 9 FROM INBOARD END CRACKE D. REPLACED RIGHT H-STAB RIB NR 9 PER SRM 51-30-2. (M) 2 L 7 2 4F RT A16WE 1996091900772 19960919 00772 NM 1996 9 19 BJNA96801 1 19960809 A 3397 WIRE BOEING 737 7372H4 138448C NM CABIN BROKEN A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 456TM 20336 AFT RIGHT DOOR LOWER EMERGENCY EXIT LIGHT INOP. SPLICED BROKEN WIRE TO LIGHT PER STANDARD PRACTICE MANUAL 20-30-22. (M ) 2 L 7 2 4F A16WE 1996091900773 19960919 00773 SW 1996 9 19 BSAA042696 1 19960426 A 7603 PWR LEVER ARM SWRNGN SA226 SA226TC 8780404 SW RIGHT BROKE A BSAA K NONE O OTHER IN INSP/MAINT 1 NM 05 116BS TC311 FLT 1133 - RIGHT POWER LEVER ARM BROKE AT BOLT CUTOUT FOR LOCKOUT LEVER BOLT. FATIGUE BREAK. REMOVED AND REPLACED RIGH T POWER LEVER ARM, AIRCRAFT FERRIED BACK TO BIL FOR RII INSPECTION, ACCOMPLISHED INSPECTION AND RETURNED TO SERVICE. (M ) 2 L 7 2 4T RT A8SW 1996091900774 19960919 00774 CE 1996 9 19 COEA9685002 1 19960823 A 7931 OIL PRESS IND CESSNA 208 208B 2073701 CE ENGINE FLUCTUATION A COEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 13 850FE 208B0164 DEPARTING PHX ON CLIMB-OUT, PILOT NOTICED THE OIL PRESSURE FLUCTUATING FROM A LOW OF 80 PSI TO A HIGH OF 10 PSI (RED LIN E). PILOT LEVELED OFF AND ELECTED TO RETURN TO PHX. MAINTENANCE IS CURRENTLY TROUBLESHOOTING THE PROBLEM. MAINTENANCE COULD NOT DUPLICATE THE PROBLEM DURING GROUND RUN. THE OIL FILTER WAS INSPECTED BUT NO CONTAMINATION WAS FOUND. THE O IL FILTER WAS REPLACED AS A PRECAUTION AND A SECOND ENGINE GROUND RUN WAS PERFORMED. OIL PRESSURE WAS NORMAL. OPERATIO NAL CHECK FLIGHT WAS PERFORMED AND NO ABNORMALITIES WERE FOUND. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 1 H 7 1 3T A37CE 1996091900775 19960919 00775 NM 1996 9 19 EIAA9622 1 19960711 A 7920 672395 OIL TUBE BOEING 747 747212B 1384886 NM NR 3 ENGINE LEAKING A EIAA E ENGINE SHUTDOWN J K WARNING INDICATION FLUID LOSS DE DESCENT 1 NM 09 485EV 20712 FJK - TWENTY MIN PRIOR TO TOP OF DESCENT, NR 3 ENGINE OIL PRESSURE DROPPED TO 35 PSI FLUCTUATING. OIL PRESSURE LIGHT FL ASHED ON AND OFF. PRECAUTIONARY ENGINE SHUTDOWN WAS ACCOMPLISHED WHEN PRESSURE DROPPED TO 34 PSI. WINDMILLING TIME WAS 40 MINS. WINDMILLING PRESSURE WAS 25 PSI. FOUND INLET OIL LINE TO THE FUEL COOLED OIL COOLER LEAKING. SAME REPLACED. PERFORMED ENGINE WINDMILLING INSPECTION AND FOUND OK. REPLACED MAIN OIL FILTER AND CHECKED CHIP DETECTOR, FOUND OK. ( M) 2 L 7 4 4F A20WE 1996091900776 19960919 00776 NE 1996 9 19 EIAA9625 2 19960727 A 7261 678960 OIL TUBE BOEING 747 747132 1384882 NM PWA JT9 JT9D7J 52054 NE NR 2 ENGINE LEAKING A EIAA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 NM 09 479EV 19898 662377 JFK - ENGINE NR 2 SHUT DOWN DUE TO LOW OIL QTY AND PRESSURE. WINDMILLING PRESSURE 18 PSI. FOUND NR 1 AND NR 2 BEARING TUBE LEAKING. REPLACED SAME. PERFORMED ENGINE WINDMILLING INSPECTION. LEAK CHECK AND OPERATIONS CHECK NORMAL ON ENGIN E RUN. (M) 2 L 7 4 4F 4 F A20WE E20EA 1996091900777 19960919 00777 NE 1996 9 19 EIAA9627 2 19960807 A 7320 THROTTLE LINKAGE DOUG DC9 DC933F 302207A WP PWA JT8 JT8D9A 52048 NE LT ENG FCU LOOSE A EIAA O OTHER O OTHER DE DESCENT 1 NM 09 945F 47279 678072 DEN - LEFT ENGINE THROTTLE WOULD NOT RESPOND TO POWER REDUCTION ON DESCENT, PERFORMED ENGINE SECURING CHECKLIST. FOUND LEFT ENGINE FCU THROTTLE LINKAGE ATTACH BOLT BACKED OUT. INSPECTED BOLT, NUT AND LINKAGE ATTACH POINT. NO DEFECTS NOTE D. REATTACHED LINKAGE AND CHECKED CLEARANCE THROUGH FULL THROTTLE MOVEMENT. PERFORMED ENGINE TRIM. OPS CHECK GOOD. R II ACCOMPLISHED. (M) 2 L 7 2 4F 4 F A6WE E2EA 1996091900778 19960919 00778 NM 1996 9 19 EIAA9628 1 19960811 A 7930 BYPASS LIGHT BOEING 747 747273C 1384896 NM NR 2 ENGINE MALFUNCTIONED A EIAA A J E UNSCHED LANDING DUMP FUEL ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 NM 09 470EV 20653 LAX - ON CLIMB-OUT, NR 2 ENGINE OIL BYPASS LIGHT CAME ON AND STAYED ON EVEN AT IDLE THRUST. ENGINE SHUTDOWN, DUMPED FUE L, AND RETURNED TO LAX. OIL PRESSURE NORMAL. NR 2 ENGINE OIL FILTER INSPECTED AND FOUND TO BE CLEAN AS PER DDPG 79-3. OIL FILTER REPLACED AS A PRECAUTION. INOPERATIVE ENGINE OIL PRESSURE BYPASS WARNING LIGHT TRANSFERRED TO CAT C DMI PER MEL 79-3. OIL FILTER TO BE CHECKED EVERY 30 HOURS. (M) 2 L 7 4 4F A20WE 1996091900779 19960919 00779 NE 1996 9 19 EIAA9629 2 19960824 A 7530 7479555 ENG VANE CNTL BOEING 747 747212B 1384886 NM PWA JT9 JT9D7J 52054 NE NR 3 ENG MALFUNCTIONED A A EIAA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 NM 09 485EV 8561 20712 662268 JFK - NR 3 ENGINE TOP OF DESCENT, AS POWER LEVERS WERE CLOSED SLOWLY, AUDIBLE COMPRESSOR STALL, EGT CLIMBED TO 917 DEGRE ES BEFORE SHUT DOWN. HUNG ON RESTART. MADE SECOND START ATTEMPT, HUNG START AGAIN. MADE THREE ENGINE LANDING. AFTER SHUT DOWN FOUND THE NR 3 ENGINE EVC WAS FULL OPEN. REPLACED NR 3 EVC AS PER MM 75-31-01. RUN-UP AND OPS, LEAK CHECK OK . WINDMILL CHECK ACCOMPLISHED WITH REPLACEMENT OF MAIN OIL SCREEN AND CHIP DETECTORS SUBSEQUENT TO INSPECTION. (M) 2 L 7 4 4F 4 F A20WE E20EA 1996091900780 19960919 00780 NM 1996 9 19 EISA96148 1 19960916 A 7933 CONNECTOR BOEING 727 72782 1384029 NM FE PANEL BROKEN WIRE A EISA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 357NE 19405 NR 2 ENGINE GENERATOR CSD 'IN' TEMP PEGGED HIGH. TROUBLESHOT AND FOUND BROKEN WIRE AT PIN 2 OF CONNECTOR D4392 BEHIND F /E PANEL. REPAIRED WIRE AND OPS CHECKED GOOD AND ENGINE RUN. (M) 2 L 7 3 4F A3WE 1996091900781 19960919 00781 CE 1996 9 19 GLBA96155 1 19960716 A 3246 BEARING BEECH 1900 1900C 1154161 CE NR 2 MLG CEASED A GLBA K NONE O OTHER IN INSP/MAINT 1 CE 01 87GL UC87 FAR - NR 2 MAIN LANDING GEAR TIRE MISSING ON POST FLIGHT INSPECTION. MAINTENANCE REMOVED AND INSTALLED AXLE AND STRUT A SSEMBLY. NR 2 BRAKE, NR 1 AND NR 2 WHEEL AND TIRE ASSEMBLIES. OK FOR SERVICE. (M) 2 L 7 2 4T RT A24CE 1996091900782 19960919 00782 CE 1996 9 19 GLBA96156 1 19960720 A 3234 1013841377 GEAR HANDLE BEECH 1900 1900C 1154161 CE LANDING GEAR MALFUNCTIONED A GLBA O OTHER O OTHER TO TAKEOFF 1 CE 01 105GL UC105 SPI - GEAR INTRANSIT LIGHT ILLUMINATES WHEN FLAPS LOWERED. MAINTENANCE REPLACED NOSE UPLOCK SWITCH, DIODE, AND GEAR HAN DLE. CYCLED GEAR. OPERATES NORMALLY. (M) 2 L 7 2 4T RT A24CE 1996091900783 19960919 00783 1996 9 19 GLBA96157 3 19960721 A 6140 CONNECTOR EMB 120 EMB120ER 3260203 SO RT BETA LIGHT DIRTY A GLBA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 01 297UX 120297 ORD - RIGHT BETA LIGHT FLICKERS ON AND OFF WHEN POWER LEVER IS IN BETA. MAINTENANCE CLEANED RIGHT PCU LOW PITCH SWITCH CANNON PLUG. OPERATES NORMALLY. (M) 2 L 7 2 4T RT A31SO 1996091900784 19960919 00784 SO 1996 9 19 GLBA96158 1 19960722 A 3230 CONNECTOR EMB 120 EMB120RT SO RT MLG DIRTY A GLBA O OTHER J WARNING INDICATION CL CLIMB 1 CE 01 267UE 120071 CIU - GEAR WON'T RETRACT AFTER TAKEOFF. MAINTENANCE CLEANED RIGHT SHOCK ABSORBER CANNON PLUG. GEAR OPERATES NORMALLY. (M) 2 L 7 2 4T RT A31SO 1996091900785 19960919 00785 CE 1996 9 19 GLBA96159 1 19960722 A 5350 FILLET BEECH 1900 1900C 1154161 CE RT WING/FUS PUNCTURED A GLBA K NONE O OTHER IN INSP/MAINT 1 CE 01 141UE UC141 DVL - REPAIRED HOLE ON FUSELAGE ON RIGHT WING FILLET IAW SRM 51-70-00. (M) 2 L 7 2 4T RT A24CE 1996091900786 19960919 00786 SO 1996 9 19 GLBA96160 1 19960720 A 7712 TQ SIG COND EMB 120 EMB120ER 3260203 SO LT ENGINE DIRTY A GLBA O OTHER O OTHER TO TAKEOFF 1 CE 01 299UX 120299 OSH - LEFT ENGINE TORQUE GAUGE FLUCTUATED ABOUT 7 PERCENT THEN DROPPED TO LESS THAN 20 PERCENT TORQUE. CAUSED AUTOFEATH ER ON LEFT ENGINE. MAINTENANCE INSPECTED AND CLEANED CANNON PLUG ON TORQUE SIGNAL CONDITIONING UNIT AND PCU, NG. OPERA TIONAL CHECK OK, HIGH SPEED TAXI CHECK OK. (M) 2 L 7 2 4T RT A31SO 1996091900787 19960919 00787 CE 1996 9 19 GLBA96161 1 19960720 A 7331 FUEL FLOW TRANS BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA RT ENGINE BROKEN WIRE A GLBA O OTHER N FALSE WARNING TO TAKEOFF 1 CE 01 60UE UC60 ESC - RIGHT FUEL FLOW INDICATION DROPS TO APPROXIMATELY 350 PPH AFTER 5 SECONDS INTO TAKEOFF ROLL. MAINTENANCE DEFERRED FUEL FLOW AND LATER REPAIRED BROKEN WIRE AT FUEL FLOW TRANSMITTER. (M) 2 L 7 2 4T 4 T RT A24CE E4EA 1996091900788 19960919 00788 SO 1996 9 19 GLBA96162 1 19960721 A 2750 TRACKS EMB 120 EMB120RT SO TE FLAPS DIRTY A GLBA O OTHER J WARNING INDICATION TO TAKEOFF 1 CE 01 128AM 120109 RDU - FLAP DISAGREEMENT AFTER TAKEOFF ROLL. MAINTENANCE CLEANED FLAP TRACKS AS REQUIRED AND PERFORMED BITE TEST IAW EM B120 MM. SYSTEM OPERATES GOOD. (M) 2 L 7 2 4T RT A31SO 1996091900789 19960919 00789 CE 1996 9 19 GLBA96163 1 19960722 A 7800 BOLT BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA LT ENG EXHAUST LOOSE A GLBA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 CE 01 166GL UC166 RDU - ON TAXI OUT RECEIVED LEFT ENGINE FIRE WARNING. SHUTDOWN ENGINE PER CHECKLIST. MAINTENANCE TIGHTENED BOLT ON EXHA UST STACK FLANGE. RUN UP CHECK GOOD. (M) 2 L 7 2 4T 4 T RT A24CE E4EA 1996091900790 19960919 00790 CE 1996 9 19 GLBA96164 1 19960722 A 3213 AXLE BEECH 1900 1900D 1154162 CE RT MLG DAMAGED A GLBA K NONE O OTHER IN INSP/MAINT 1 CE 01 101UX UE101 ISN - LOST NR 4 WHEEL ASSEMBLY. MAINTENANCE REMOVED AND REPLACED RIGHT MAIN LANDING GEAR ASSEMBLY AFTER FINDING DAMAGED AXLE. INSPECTED FOR FURTHER DAMAGE AND LANDING GEAR OPERATIONAL CHECKS GOOD. (M) 2 L 7 2 4T RT A24CE 1996091900791 19960919 00791 SO 1996 9 19 GLBA96165 1 19960725 A 2750 3472001001 FLAP CONTL UNIT EMB 120 EMB120ER 3260203 SO TE FLAPS MALFUNCTIONED A A GLBA O OTHER J WARNING INDICATION TO TAKEOFF 1 CE 01 297UX 120297 ORD - FLAP CONTROL FAULT, ALL POSITIONS. MAINTENANCE REMOVED AND REPLACED FLAP CONTROL UNTI. TESTED GOOD. (M) 2 L 7 2 4T RT A31SO 1996091900792 19960919 00792 NE 1996 9 19 GLBA96166 2 19960726 A 7314 FUEL PUMP BEECH 1900 1900C 1154161 CE PWA PT6 PT6A67D NE LT ENGINE MALFUNCTIONED A GLBA O OTHER J WARNING INDICATION CL CLIMB 1 CE 01 170GL UE170 CHS - AFTER DEPARTURE ON CLIMB-OUT LEFT ENGINE STUCK AT 3600 TORQUE. N1 STAYED AT 95 PERCENT. MAINTENANCE REMOVED AND REPLACED HIGH PRESSURE FUEL PUMP AND FCU. OPERATIONAL CHECKED GOOD. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 1996091900793 19960919 00793 CE 1996 9 19 GLBA96167 1 19960727 A 3297 WIRE BEECH 1900 1900C 1154161 CE RT MLG BROKEN A GLBA O OTHER J WARNING INDICATION CL CLIMB 1 CE 01 123UE UC123 MIE - GEAR WOULD NOT RETRACT. MAINTENANCE REPAIRED BROKEN WIRE IN SPLICE AREA OF RIGHT SQUAT SWITCH. LANDING GEAR SWUN G 10 TIMES. NO FAULTS NOTED. (M) 2 L 7 2 4T RT A24CE 1996091900794 19960919 00794 NE 1996 9 19 GLBA96168 2 19960728 A 7532 311701101A BLEED VLV BEECH 1900 1900C 1154161 CE PWA PT6 PT6A67D NE RT ENGINE STICKING A GLBA O OTHER O OTHER TO TAKEOFF 1 CE 01 170GL UE170 AVL - RIGHT ENGINE DOES NOT MAKE TORQUE, ONLY UP TO 2900 FEET LBS TORQUE. MAINTENANCE REMOVED, CLEANED AND REPLACED BLE ED VALVE. OPERATES NORMALLY. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 1996091900795 19960919 00795 SO 1996 9 19 GLBA96169 1 19960729 A 3150 CIRCUIT BREAKER EMB 120 EMB120RT SO AURAL WARNING TRIPPED A GLBA O OTHER O OTHER TO TAKEOFF 1 CE 01 451UE 120108 DLH - TAKEOFF AURAL WARNING SOUNDED ON TAKEOFF ROLL, TESTED NORMAL ON PREFLIGHT. AURAL WARNING CIRCUIT BREAKER POPPED. MAINTENANCE RERACKED AURAL WARNING UNIT. RESET CIRCUIT BREAKER. OPERATIONAL CHECKS GOOD ON GROUND. (M) 2 L 7 2 4T RT A31SO 1996091900796 19960919 00796 CE 1996 9 19 GLBA96170 1 19960731 A 7120 12991003279 TRUSS BEECH 1900 1900C 1154161 CE RT ENGINE CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 CE 01 122GL UC122 SPI - RIGHT TRUSS CRACKED AT AREA 'A'. REMOVED AND REPLACED RIGHT TRUSS. (M) 2 L 7 2 4T RT A24CE 1996091900797 19960919 00797 CE 1996 9 19 GLBA96171 1 19960805 A 6120 WIRE BEECH 1900 1900C 1154161 CE RT ENGINE BROKEN A GLBA O OTHER J WARNING INDICATION LD LANDING 1 CE 01 84GL UC84 ORD - ON TOUCHDOWN, RIGHT PROP DOES NOT GO INTO GROUND IDLE FROM FLIGHT IDLE. MAINTENANCE REPAIRED BROKEN WIRE ON RIGHT ENGINE LOW PITCH SOLENOID. (M) 2 L 7 2 4T RT A24CE 1996091900798 19960919 00798 CE 1996 9 19 GLBA96172 1 19960806 A 3230 101388083 SERVICE VALVE BEECH 1900 1900C 1154161 CE LANDING GEAR FAILED A GLBA O OTHER J WARNING INDICATION AP APPROACH 1 CE 01 159GL UC159 TUS - GEAR WOULD NOT EXTEND. MAINTENANCE REMOVED AND REPLACED SERVICE VALVE. OPERATES NORMALLY. (M) 2 L 7 2 4T RT A24CE 1996091900799 19960919 00799 CE 1996 9 19 GLBA96173 1 19960809 A 2121 1143800281 BLOWER BEECH 1900 1900C 1154161 CE CABIN FAILED A GLBA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 01 89UE 2896 420 UC89 ORD - AFTER TAKEOFF, THE CREW SMELLED SMOKE AND DID AN AIR TURN BACK. MAINTENANCE REMOVED AND REPLACED THE FORWARD VENT BLOWER. OPS NORMAL. (M) 2 L 7 2 4T RT A24CE 1996091900800 19960919 00800 CE 1996 9 19 GLBA96174 1 19960812 A 3230 CIRCUIT BREAKER BEECH 1900 1900C 1154161 CE LANDING GEAR TRIPPED A GLBA O OTHER J WARNING INDICATION AP APPROACH 1 CE 01 98GL UC98 SPW - GEAR WILL NOT COME DOWN. MAINTENANCE RESET 60 AMP CIRCUIT BREAKER IN LEFT NACELLE. CYCLED GEAR SEVERAL TIMES WIT H NO DISCREPANCY. (M) 2 L 7 2 4T RT A24CE 1996091900801 19960919 00801 CE 1996 9 19 GLBA96175 1 19960812 A 7120 TRUSS BEECH 1900 1900C 1154161 CE LT ENGINE CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 CE 01 101UE UC101 SPW - MAINTENANCE FOUND LEFT TRUSS CRACKED AT AREA 'A' OF INBOARD SIDE. REMOVED AND REPLACED TRUSS. (M) 2 L 7 2 4T RT A24CE 1996091900802 19960919 00802 NE 1996 9 19 GLBA96176 2 19960804 A 7322 311875702 FUEL CONTROL BEECH 1900 1900C 1154161 CE PWA PT6 PT6A67D NE RT ENGINE FAILED A GLBA K NONE L NO TEST TO TAKEOFF 1 CE 01 170GL 11434931 UE170 RDU - RIGHT TORQUE FLUCTUATIONS OF 600 TO 700 LBS. HIGH ITT WHEN TORQUE IS ABOVE 2000 FT/LBS. MAINTENANCE REMOVED AND REPLACED FCU. OPERATIONAL CHECKS NORMAL. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 1996091900803 19960919 00803 EA 1996 9 19 HNAA9690555 2 19960806 A 7321 32447531917 FUEL CONTL UNIT DHAV DHC7 DHC7102 2802708 EA PWA PT6 PT6A50 52043 EA NR 4 ENG FAILED A HNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 07 905HA 15631 A54234 070 FLT NR 3258 - DCA-BWI - THE NR 4 ENGINE TORQUE ROLLED BACK INFLIGHT AND NG DROPPED TO APPROXIMATELY 40 PERCENT. THE ENG INE WAS SHUTDOWN INFLIGHT IAW STANDARD PROCEDURES. THE AIRCRAFT TURNED BACK AND LANDED IN DCA WITHOUT INCIDENT. REMOVE D AND REPLACED THE NR 4 ENGINE FUEL CONTROL UNIT. (M) 2 H 7 4 4T 4 T A20EA E4EA 1996091900804 19960919 00804 NM 1996 9 19 HNAA9690758 1 19960817 A 3350 6013211X POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 907HA 13170 10131 011 FLT NR 77 - ORF-PHF - DURING PREFLIGHT CHECKS, THE FIRST TWO ESCAPE PATH RED LIGHTS WERE FOUND INOP. REMOVED AND REPLAC ED THE POWER SUPPLY AT 3352-PS2. (M) 2 H 7 2 4T RT A13NM 1996091900805 19960919 00805 NM 1996 9 19 HNAA9690765 1 19960828 A 5260 85210263101 GAS STRUT DHAV DHC8 DHC8102 2809003 NM AIRSTAIR DOOR FAILED A HNAA K NONE O OTHER TX TAXI/GRND HDL 1 EA 07 907HA 30227 011 FLT NR 3172 - PHF-PIT - UPON LANDING IN PIT, THE FLIGHT ATTENDANT WAS UNABLE TO OPEN THE AIRSTAIR DOOR WITHOUT ASSISTANC E. FERRIED THE AIRCRAFT TO ORF FOR REPAIRS. REMOVED AND REPLACED THE FORWARD GAS STRUT. (M) 2 H 7 2 4T RT A13NM 1996091900806 19960919 00806 NM 1996 9 19 HNAA9692461 1 19960822 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN LOOSE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 924HA 105 FLT NR 3184 - SBY-PHL - DURING PREFLGIHT CHECKS, FOUND THE RIGHT FORWARD EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED POWER SUPPLY 3351-PS2, NO FIX. MAINTENANCE FOUND WIRES NOT SEATED IN MATRIX BLOCK. RESEATED WIRES, OPS CHECK GOOD. ( M) 2 H 7 2 4T RT A13NM 1996091900807 19960919 00807 NM 1996 9 19 HNAA9698164 1 19960825 A 7603 V319 SWITCHES DHAV DHC8 DHC8102 2809003 NM PWR LEVER FAILED A HNAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 07 981HA 6260 378 FLT 3040 - DCA-HPN - THE AUTOFEATHER SYSTEM WOULD NOT ARM ON TAKEOFF. THE AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. REMOVED AND REPLACED POWER LEVER MICROSWITCHES 6121-S12 AND S13. (M) 2 H 7 2 4T RT A13NM 1996091900808 19960919 00808 NM 1996 9 19 IXKA9600071 1 19960821 A 8012 WIRE BOEING 727 727225 1384077 NM NR 2 START VLV CHAFED A IXKA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 EA 25 354PA 20624 FLT NR 84 - ATL-TPA - NR 2 START VALVE OPEN LIGHT CAME ON IN FLIGHT. NR 2 ENGINE WAS SHUT DOWN AS PER KIWI PROCEDURES. CONDITIONS WERE DESCENDING 29,000 FEET TO 17,000 FEET WINDMILL TIME 43 MINUTES WINDMILLING. FOUND WIRING IN START VALV E CHAFING ON ENGINE CASE. REPAIRED WIRING AS REQUIRED. LIGHT OPERATING NORMAL DURING ENGINE AS PER MM 80-11-01. (M) 2 L 7 3 4F A3WE 1996091900809 19960919 00809 NM 1996 9 19 IXKA9600072 1 19960824 A 3350 LIGHT BOEING 727 727225 1384077 NM CABIN INOP A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 356PA 20626 FOUND EMERGENCY PATH LIGHT OUT AT ROW 4 AND 25. REPAIRED WIRING AT ROW 4 AND RELAMPED, P/N CM1307BPEGP1, AT ROW 25. (M ) 2 L 7 3 4F A3WE 1996091900810 19960919 00810 WP 1996 9 19 IXXA96130 1 19960823 A 5101 STRUCTURE DOUG DC8 DC863F 302198F WP AIRFRAME VIBRATION A IXXA K NONE E VIBRATION/BUFFET AP APPROACH 1 SW 11 867BX 46049 DURING APPROACH TO CLT, AIRCRAFT EXPERIENCED A SIGNIFICANT VIBRATION WITH FLAP 23 SELECTED. MAINTENANCE INSPECTED THE A IRCRAFT FLIGHT CONTROL SYSTEMS, LANDING GEAR SYSTEMS, WINGS, AND FUSELAGE WITH NO CAUSE FOUND. A SUBSEQUENT TEST FLIGHT WAS ACCOMPLOSHED WITH NO FINDINGS OR PROBLEMS REPORTED. THE AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 4 4F 4A25 1996091900811 19960919 00811 WP 1996 9 19 IXXA96131 1 19960824 A 5280 STRIKER DOUG DC8 DC861 3021952 WP RT MLG DOOR MISSING A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 861PL 50489 45964 ON DEPARTURE FROM DAY AND LANDING GEAR RETRACTION, 'DOORS NOT LATCHED' AND 'RIGHT DOOR UNSAFE' LIGHTS REMAINED ILLUMINAT ED. THE GEAR WAS CYCLED WITH THE LIGHT REMAINING ON. UPLATCH CHECK WAS ACCOMPLISHED SUCCESSFULLY. NO VIBRATION OR NOI SE WAS NOTED. FLIGHT CONTINUED TO SLC WHERE AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE FOUND AND REPLACED A M ISSING SWITCH STRIKER AT RIGHT MAIN LANDING GEAR DOOR. THE INDICATION SYSTEM PASSED THE OPERATIONAL CHECK AND THE AIRCR AFT WAS RETURNED TO SERVICE. (M) 2 L 7 4 4F 4A25 1996091900812 19960919 00812 NE 1996 9 19 M3HA96022A 2 19960816 A 7313 AS320920 FUEL NOZZLE AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE RT ENGINE FAILED A A M3HA C E F ABORTED TAKEOFF ENGINE SHUTDOWN ACTIVATE FIRE EXT. J WARNING INDICATION TO TAKEOFF 1 WP 13 4209G 129 120856 HNL - FLT 744 - DURING NORM T/O ROLL, NR 2 ENG TORQUE INDICATED LOSS OF TQ. F/O'S CALLED FOR ABORT AND CAPTAIN INITIATE D ABORT PROCEDURES. ATC WAS INFORMED OF ABORT AND NO ASSIST WAS REQUESTED. AS A/C CLEARED TAXIWAY, NR 2 ENG SHOWED A F IRE WARN WITH ASSOCIATED AURAL ALERTS. A/C WAS STOPPED AND ENG FIRE ON THE GROUND PROCEDURES INITIATED. 30 SECONDS AFT ER NR 2 ENG HAD BEEN SHUT DOWN AND THE FIRST FIRE AGENT DISCHARGED, A SECOND AGENT WAS DISCHARGED DUE TO CONTINUING FIRE WARN INDICATIONS. AFTER SECOND AGENT WAS FIRED, ENG FIRE INDICATIONS EXTINGUISHED. REPLACED FUEL NOZZLE PACKINGS, REP LACED DAMAGED WIRING, AND PERFORMED TASKS IAW JIC 70-00-00 SDI 10000-1,54-11-61 DVI 10000-1, 54-21-61DVI 10000-1.(M) 2 H 7 2 4T 4 T RT A53EU E20NE 1996091900813 19960919 00813 NM 1996 9 19 MZZA96057 1 19960709 A 5330 SKIN BOEING 727 727224 1384076 NM BS 1030-1070 CORROSION A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69742 22251 GUM - DURING B-CHECK, FOUND PREVIOUS SKIN REPAIR, LOWER BELLY, STATION 1030 TO STATION 1070, HAS IG CORROSION. REMOVED PREVIOUS SKIN REPAIR, REMOVED CORROSION PER SRM 51-10-6, ALODINED AND PRIMED PER SRM 51-10-2. FABRICATED REPAIR DOUBLER FROM 2024 T3 SHEET STOCK, .071 THICKNESS AND INSTALLED PER SRM 51-30-3, FTG 3 SEALED AND APPLIED TOP COAT PER MM 51-20- 0. (M) 2 L 7 3 4F A3WE 1996091900814 19960919 00814 NM 1996 9 19 MZZA96058 1 19960710 A 7931 652186713 OIL PRESS LINE BOEING 727 727224 1384076 NM NR 2 ENGINE CRACKED A A MZZA E J ENGINE SHUTDOWN DUMP FUEL K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 13 79745 22448 FLT NR 915 - GUM - ENGINE NR 2 LOST OIL QTY AND PRESS SHORTLY AFTER LEVEL OFF FL 31, SHUT DOWN ENGINE NR 2 PER EMERGENCY PROCEDURE, 8,000 LBS DUMPED. ENGINE WINDMILLING 40 MINUTES. N1 16 PERCENT, N2 22 PERCENT OIL PRESS O, OIL QUANTITY 0. DURING ENG INSPECTION, FOUND OIL PRESSURE LINE FLARE TIP CRACKED. REMOVED AND REPLACED LINE GOING TO OIL PRESSURE TRA NSMITTER. C/W JT8D MM 7200 PG 518D PARA J RUN ENG, ALL SYSTEM OPS CHECK GOOD. (M) 2 L 7 3 4F A3WE 1996091900815 19960919 00815 NM 1996 9 19 MZZA96059 1 19960711 A 5610 WINDSHIELD BOEING 727 727232 1384082 NM RT COCKPIT AIR LEAK A MZZA A J UNSCHED LANDING DUMP FUEL O OTHER CL CLIMB 1 WP 13 15781 20636 FLT NR 958 - GUM - AIR TURN BACK, NOTED AIR LEAK ON T/O (RT SIDE F/O'S WINDOW AREA) AS DIFFERENTIAL INCREASED NOISE TURN ED TO SQUEL AND INCREASED AT 5 PSI. NOISE WAS DEAFENING AND CREW/RADIO COMMUNICATIONS BECAME IMPOSSIBLE, DUMPED 9000 LB S OF FUEL OFFSHORE AND RETURNED TO GUAM, LANDING WEIGHT 134,000 LBS. FOUND FLIGHT OFFICERS WINDSHIELD (R1) PEELING ON O UTSIDE. REMOVED ALL OUTER SEALANT, RETORQUED, RESEALED PER MM 56-11-11. (M) 2 L 7 3 4F A3WE 1996091900817 19960919 00817 NE 1996 9 19 MZZA96064 2 19960811 A 7250 TURBINE BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE FAILED A A MZZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 15781 20636 FLT NR 915 - GUM - ON TAKEOFF HEARD LOUD EXPLOSION, THEN CAW NR 1 ENGINE FAIL LIGHT CAME ON. EPR WENT TO ZERO, HOWEVER, EGT, N1 AND N2 APPEARED NORMAL. LOUD RUMBLE HEARD FROM NR 1 ENGINE WHEN AT IDLE. FOUND TURBINE SECTION FAILED. REMOV ED AND REPLACED NR 1 ENGINE PER WORKCARD 07-7100-1-8001. (M) 2 L 7 3 4F 4 F A3WE E2EA 1996091900818 19960919 00818 NM 1996 9 19 MZZA96065 1 19960818 A 3230 1899219 PROX SENSOR BOEING 727 727264 138408M NM LT MLG FAILED A MZZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 623DH 20895 FLT 876 - MNL - AFTER TAKEOFF, UNABLE TO RAISE THE LANDING GEAR, RETURNED TO MNL. ON TROUBLE SHOOTING CONFIRMED HANDLE WILL NOT GO PAST OFF DURING NORMAL OPERATION. FOUND AIR SENSING SENSOR M831 AT FAULT. REPLACED SAME, OPERATION AND TES T NORMAL. (M) 2 L 7 3 4F A3WE 1996091900819 19960919 00819 NM 1996 9 19 MZZA96066 1 19960818 A 2450 CONNECTOR BOEING 727 727224 1384076 NM E/E COMPT FAILED A MZZA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 13 69742 22251 GUM - FLT 958 - SITTING AT GATE WITH APU RUNING, APU ELECTRICAL POWER KICKED OFF WITH A PHASE UNBALANCED LIGHT ON, ON EL ECTRICAL FAULT PANEL. SHORTLY THEREAFTER, ELECTRICAL SMOKE IN COCKPIT. FOUND T3 TERMINAL ON 'A' PHASE FEEDER CABLE BUR NED AT APU GENERATOR CIRCUIT BREAKER T3 TERMINAL. REPLACED APU GENERATOR CIRCUIT BREAKER AND REPLACED 'A' PHASE TRANSFO RMER. REQUIRES TERMINAL END TO CONNECT 'A' PHASE FEEDER CABLE TO TERMINAL T3. UNABLE TO LOCATE. PLACARDED APU GENERAT OR PER MEL 24-01-2. (M) 2 L 7 3 4F A3WE 1996091900820 19960919 00820 NM 1996 9 19 MZZA96069 1 19960829 A 2782 269002918 ACTUATOR BOEING 727 727224 1384076 NM NR 3 LE FLAP CRACKED A MZZA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 13 69742 22251 FLT NR 916 - SPN - MAINTENANCE FOUND NR 3 LEADING EDGE SLAT LEAKING HYDRAULIC FLUID ON GROUND. MAINTENANCE REMOVED AND REPLACED NR 3 SLAT ACTUATOR DUE TO CRACK IN THE ACTUATOR HOUSING SYSTEM LEAK CHECK AND OPERATION CHECK GOOD, MM REFEREN CE 27-81-22. (M) 2 L 7 3 4F A3WE 1996091900821 19960919 00821 NE 1996 9 19 NSVA96001 2 19960809 A 7230 INLET GUIDE VANE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE MISRIGGED A NSVA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 EA 27 224TH 9771 340B224 785308 RIGHT ENGINE EXPERIENCED A COMPRESSOR STALL SHORTLY AFTER TAKEOFF. ITT REACHED 1023 DEGREES FOR 4 SECONDS. ENGINE WAS SHUT DOWN AND THE AIRCRAFT RETURNED TO GATE. THE CAUSE OF THE REPORTED IN FLIGHT SHUTDOWN WAS SEVERE MISRIGGING OF THE INLET GUIDE VANES. THIS MISRIGGING CAUSED A SEVERE COMPRESSOR STALL AND RESULTANT ENGINE SHUTDOWN AND OVERTEMPERATURE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 1996091900822 19960919 00822 EU 1996 9 19 PLGA9608211 1 19960821 A 2430 WIRE SAAB SF340 SF340A 7850100 EU LT GENERATOR BROKEN A PLGA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 NE 05 744BA 340A105 BOS - FLT 4575 - EN ROUTE TO ACK FROM BOS, THE LEFT DC GENERATOR DROPPED OFF LINE AND WOULD NOT RESET. THE AIRCRAFT RET URNED TO BOS, LANDING WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT AND FOUND A WIRE BROKEN AT THE TERMI NAL BLOCK OF THE GENERATOR. THE WIRE WAS REPAIRED, ALL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1996091900823 19960919 00823 NE 1996 9 19 PLGA9608252 2 19960825 A 7260 CHIP LIGHT SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT ENGINE ILLUMINATED A PLGA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NE 05 365BE 340B299 GEE785317 BOS - FLT 4304 - DURING FLT FROM BOS TO YOW, THE LEFT ENGINE CHIP DETECTOR LIGHT ILLUMINATED. THE AIRCRFT DIVERTED BACK TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED CHIP DETECTOR AND FOUND ONE CHIP. CHIP WAS WITHIN LIMITS PE R GE MM. INSPECTIONS AND RUNS WERE PERFORMED PER GE MM AND NO FURTHER DEFECTS NOTED. AIRCRAFT RELEASED TO SERVICE. (M ) 2 L 7 2 4T 4 T RT A52EU E8NE 1996091900824 19960919 00824 EU 1996 9 19 REXA96028 1 19960502 A 3260 GE327 BULB BAG JETSTM JETSTM3101 1500215 EU NLG FAILED A REXA O OTHER P NO WARNING INDICATION LD LANDING 1 SO 25 319PX 691 NO NOSE GEAR DOWN AND LOCKED INDICATION WITH INTERMITTENT UNLOCKED INDICATION. INSPECTION FOUND NLG GREEN INDICATOR LAM PS BURNED OUT. CONFIRMED POWER AT INDICATOR WITH VOLTMETER. GOOD FOR SERVICE. (M) 2 L 7 2 4T RT A21EU 1996091900825 19960919 00825 EU 1996 9 19 REXA96029 1 19960616 A 2621 FIRE BOTTLE SAAB SF340 340B 7860101 EU CARGO BAY DEPLETED A REXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 370PX 340B300 CARGO SMOKE INDICATION AIRBORNE, NO INDICATION OF COMBUSTION WHEN INSPECTED ON GROUND. CARGO FIRE BOTTLE DEPLETED, DEFE RRED DM14773. CLEANED CANNON PLUG AND INSPECTED, OPS CHECK GOOD A/P 260113924. CLEARED DEFER 14773 BY REMOVING AND REP LACING CARGO FIRE BOTTLE AND SQUIB. OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1996091900826 19960919 00826 EU 1996 9 19 REXA96030 1 19960709 A 2550 CARGO NET SAAB SF340 340B 7860101 EU BAGG COMPT OUT OF POSITION A REXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 361PX A2764 340B249 CARGO SMOKE ILLUMINATED IN FLIGHT, DISCHARGED BOTTLE, DECLEARED EMERGENCY, LANDED IN MGM. INSPECTED SYSTEM, FOUND CARGO NET HOOKED ON SMOKE DETECTOR, P/N 72111121100. (M) 2 L 7 2 4T RT A52EU 1996091900827 19960919 00827 EU 1996 9 19 REXA96031 1 19960707 A 2611 72111211000 SMOKE DETECTORS SAAB SF340 340B 7860101 EU CARGO HOLD DIRTY A REXA F ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 SO 25 361PX 340B249 CARGO SMOKE CAME ON IN FLIGHT FIRE BOTTLE, NO FIRE. REPLACED CARGO HALON FIRE BOTTLE. OK FOR SERVICE. REMOVED AND REP LACED FORWARD AND AFT SMOKE DETECTORS (S/N AFT A2764, FWD A3202), TEST NORMAL. (M) 2 L 7 2 4T RT A52EU 1996091900828 19960919 00828 CE 1996 9 19 S2YA960024 1 19960823 A 3244 196K089 TIRE BEECH 1900 1900D 1154162 CE NLG FLAT SPOTTED A S2YA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 13 831SK 27 UE83 AFTER THE FLIGHT CREW DEPARTED MKE ON FLT NR 1053, THE CREW NOTED SEVERE VIBRATION FROM THE NOSE, RETURNED TO MKE. MAIN TENANCE CHANGED THE NOSE WHEEL ASSY, AND IT WAS DETERMINED THAT A TIRE FLAT SPOT OUT OF BALANCE CONDITION CAUSED THE VIB RATION. (M) 2 L 7 2 4T RT A24CE 1996091900829 19960919 00829 NE 1996 9 19 SABA9600021 2 19960830 A 7200 ENGINE STBROS SD3 SD360 8100606 EU PWA PT6 PT6A67R 52043 NE RIGHT FAILED A SABA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 33 360CC SH3731 106034 CLT - FLT 5097 - RIGHT ENGINE LOST OIL PRESSURE IN CRUISE, PERFORMED PRECAUTIONARY SHUTDOWN. RETURNED TO CLT AND MADE L ANDING. INSPECTED ENGINE, FOUND METAL IN OIL FILTER AND PROP HARD TO TURN. REMOVED AND REPLACED ENGINE. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 H 7 2 4T 4 T A41EU E26NE 1996091900830 19960919 00830 EU 1996 9 19 SIMA962481 1 19960904 A 3234 F96GA0102 GEAR SELECTOR AEROSP ATR72 ATR72212 EU COCKPIT FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 260AE 263 HOU - FLT 3548 - UPON DEPARTURE, THE AIRCRAFT GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO HOUSTON SAFELY, MEL 32-3 ISS UED. AIRCRAFT WAS FLOWN TO DFW, REPLACED LANDING GEAR SELECTOR HANDLE THERE. PERFORMED OPERATIONAL CHECK IAW AMM 32-30 . AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996091900831 19960919 00831 NE 1996 9 19 SRAA960802 2 19960810 A 7260 INSERT BOEING 747 747212B 1384886 NM PWA JT9 JT9D7J 52054 NE NR 1 GEAR BOX LOOSE A SRAA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 23 745SJ 20888 DURING FLT SJ103 - NR 1 ENGINE LOST OIL QTY AND OIL PRESSURE DROPPED TO 15 PSI WITH BREATHER TEMP INCREASING, SHUT DOWN NR 1 ENGINE AND ACCOMPLISHED AIR TURN BACK TO MIA. AIRCRAFT LANDED WITHOUT INCIDENT. SERVICED ENGINE AND FOUND OIL LEA K AT ANGLE BEAR BOX SCAVENGE TUBE FLANGE FITTING. REMOVED FLANGE FITTING AND FOUND HELI-COIL LOOSE. PERFORMED REPAIR B Y INSTALLING 'TWINSERT' PER PWA IEN 777210 AND PWA MM 72-61-01 FIG 901. PERFORMED ENGINE RUNUP. NO LEAKS NOTED, SYSTEM OPS CHECKED GOOD PER MM CH 71. (M) 2 L 7 4 4F 4 F A20WE E20EA 1996091900832 19960919 00832 NM 1996 9 19 TAOA089606 1 19960822 A 3397 WIRE BOEING 727 727225 1384077 NM CABIN BROKEN A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 922TS 20415 EMERGENCY PATH LIGHTING TRACK DISPLACED AND WIRE BROKEN AT 2 DEF. RED INDICATOR LIGHTS INOP AT L1 AND R1 DOOR. REPAIRE D BROKEN WIRE AT 2 DEF, OPERATIONAL CHECK OF LIGHTS NORMAL. REPLACED TRACK SECTION. (M) 2 L 7 3 4F A3WE 1996091900833 19960919 00833 NM 1996 9 19 TAOA089607 1 19960823 A 2752 MS93911307E4C FLAP MOTOR VICKER BOEING 727 727254 138408L NM TE FLAP LEAKING A TAOA O OTHER J K WARNING INDICATION FLUID LOSS TO TAKEOFF 1 EA 15 912TS MX348025C 20438 SYSTEM 'A' HYDRAULIC FAILURE (LOW QUANTITY) SHORTLY AFTER TAKEOFF. FOUND OUTBOARD FLAP MOTOR LEAKING, REPLACED MOTOR AN D CHECKED OK PER MM CHAPTER 27-51-62. (M) 2 L 7 3 4F A3WE 1996091900834 19960919 00834 NM 1996 9 19 TAOA089608 1 19960823 A 3350 S106 BATTERY BOEING 727 727254 138408L NM AFT AIRSTAIR DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 913TS 20250 AFT AIRSTAIR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES. (M) 2 L 7 3 4F A3WE 1996091900835 19960919 00835 1996 9 19 TAOA089610 4 19960827 A 2565 22D227127 SLIDE AIRCRUISERS BOEING 727 727227 1384078 NM CABIN DEPLOYED A TAOA O OTHER O OTHER IN INSP/MAINT 1 EA 15 925TS 138A 21244 FLT ATTENDANT TRAINING, DEPLOYED SLIDE FROM FORWARD RIGHT GALLEY SERVICE DOOR. SLIDE INFLATION AND EMERGENCY LIGHTS CHE CKED NORMAL. (M) 2 L 7 3 4F A3WE 1996091900837 19960919 00837 NM 1996 9 19 TAOA089612 1 19960828 A 3230 106122629 UPLOCK SENSOR BOEING 727 727227 1384078 NM RT MLG INOPERATIVE A TAOA O OTHER J WARNING INDICATION AP APPROACH 1 EA 15 925TS 21244 RIGHT MAIN GEAR UNSAFE LIGHT CAME ON DURING GEAR EXTENSION, LIGHT WENT OUT UNDER 160 KTS. VISUAL INDICATION CONFIRMED G EAR DOWN AND LOCKED. REPLACED RIGHT UPLOCK SENSOR PER 32-61-01, OPERATIONAL CHECKED NORMAL PER MM CHAPTER 32-61-81. (M ) 2 L 7 3 4F A3WE 1996091900838 19960919 00838 NE 1996 9 19 TWRA96283 2 19960821 A 7320 PT2 SENSE LINE BOEING 747 747136 1384883 NM PWA JT9 JT9D7A 52054 NE NR 3 ENGINE LOOSE A A TWRA E ENGINE SHUTDOWN M R OVER TEMP PARTIAL RPM/PWR LOSS DE DESCENT 1 EA 15 606FF 20273 ENGINE NR 3 WAS SHUT DOWN IN FLIGHT AT FLIGHT LEVEL 360. DESCENDED MACH .85, SAT 45 DEGREE CELSIUS. TAT 15 DEGREES CEL SIUS DUE TO RAPID RISE IN EGT WITH THRUST LEVER MOVEMENT (AFT) MAX EGT WAS 840 DEGREES CELSIUS IN FLIGHT START WAS SUCCE SSFUL. MAINTENANCE FOUND PT2 SENSE LINE AT UNION LOOSE ON RACEWAY TO PRBC. RESECURED LINE. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 4 4F 4 F A20WE E20EA 1996091900840 19960919 00840 NM 1996 9 19 TWRA96291 1 19960822 A 3350 900835A BATTERY BOEING 747 747259B NM CABIN DISCHARGED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 EICEO 21730 DURING DAILY CHECK, FOUND OVERHEAD EXIT SIGN INOP AT 20C, 32C, 32H, 45H AND 50H. REMOVED AND REPLACED EVAC LIGHT BATTER Y. OPS CHECKED OK PER MM 33-51-00 PG 501. (M) 2 L 7 4 4F RT A20WE 1996091900841 19960919 00841 NM 1996 9 19 TWRA96292 1 19960822 A 3350 S1356B37 LIGHT BOEING 747 747259B NM CREW DOOR INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 EICEO 21730 DURING DAILY CHECK, FOUND CREW DOOR AREA CEILING EMERGENCY LIGHT IS INOP. REPLACED CEILING EMERGENCY LIGHT. OPS CHECKE D NORMAL AS PER MM 33-51-00. (M) 2 L 7 4 4F RT A20WE 1996091900842 19960919 00842 NM 1996 9 19 TWRA96293 1 19960822 A 3397 WIRE BOEING 747 747212B 1384886 NM FLOOR BROKEN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND, BETWEEN 31H AND NR 3 R MED, FLIGHT ATTENDANT SEAT FLOOR EMERGENCY LIGHTS ARE INOP. REWIRED 3 1H, FLIGHT ATTENDANT SEAT LIGHT. OPS CHECKED OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996091900843 19960919 00843 NM 1996 9 19 TWRA96294 1 19960822 A 3350 S1356B37 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 620FF 11632 21162 DURING DAILY CHECK, FOUND EMERGENCY LIGHTS, L1 DOOR OVERHEAD DID NOT ILLUMINATE ON TEST. REPLACED LIGHT ASSEMBLY. OPS CHECKED OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996091900844 19960919 00844 NM 1996 9 19 TWRA96295 1 19960821 A 3350 S1356B37 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 616FF 21939 DURING DAILY CHECK, FOUND C-ZONE LEFT AFT CEILING LIGHT IS INOP. REPLACED LIGHT ASSEMBLY. OPS CHECKED NORMAL PER MM 33 -51-00 PG 501. (M) 2 L 7 4 4F A20WE 1996091900845 19960919 00845 NM 1996 9 19 TWRA96296 1 19960822 A 3350 S1356A36 LIGHT BOEING 747 747121 1384871 NM CREW DOOR INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 609FF 20354 DURING DAILY CHECK, FOUND CREW DOOR OVERHEAD EXIT SIGN INOP. REPLACED EMERGENCY LIGHT CREW DOOR EXIT SIGN. OPS CHECKED OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996091900847 19960919 00847 NM 1996 9 19 TWRA96298 1 19960826 A 3350 S1356B37 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 616FF 15169 21939 DURING DAILY CHECK, FOUND L3 MED EVAC LIGHT AT UPPER BUSTLE INOP. REPLACED AISLE LIGHT ASSEMBLY OVERHEAD DOOR, BUSTLE L IGHT. OPS CHECKED NORMAL AS PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996091900848 19960919 00848 NM 1996 9 19 TWRA96299 1 19960823 A 3350 3004181A LIGHT BOEING 747 747130 1384880 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 603FF 19746 DURING DAILY CHECK, FOUND L1 DOOR UPPER BUSTLE EVAC LIGHT INOP. REPLACED BUSTLE LIGHT. OPS CHECKED NORMAL PER MM 33-51 -00. (M) 2 L 7 4 4F A20WE 1996091900849 19960919 00849 NM 1996 9 19 TWRA96301 1 19960829 A 2913 7583599 SEAL BOEING 747 747130 1384880 NM HYD PUMP DRIVE WORN A TWRA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 15 603FF 662867 19746 DURING FLIGHT, NR 3 ENGINE OIL QUANTITY DROPPED TO 75 GALLONS, OIL PRESSURE 32-45-PSI, OIL TEMPERATURE ROSE TO 109 DEGRE ES CELSIUS. ENGINE WAS SHUT DOWN. PERFORMED WINDMILL INSPECTION PER MM 72-00-00 PAGE 682. DURING GROUND IDLE FOUND HY DRAULIC PUMP DRIVE SEAL LEAKING. REMOVED AND INSTALLED HYDRAULIC PUMP DRIVE SEAL PER MM 72-61-09 PAGE 401. NO CONTAMIN ATION OF MAIN OIL FILTER AND CHIP DETECTORS FOUND. MAIN OIL FILTER, CHIP DETECTORS AND ENGINE HYDRAULIC PUMP DRIVE SEAL LEAK CHECKED GOOD DURING ENGINE RUN UP PER MM 71-00-00 PAGE 518. AIRCRAFT RETURN TO SERVICE. (M) 2 L 7 4 4F A20WE 1996091900850 19960919 00850 NM 1996 9 19 TWRA96302 1 19960827 A 3350 S1356B37 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 619FF 19425 21316 DURING DAILY CHECK, FOUND CEILING MOUNTED EMERGENCY EXIT LIGHT ABOVE AISLE AT 21C INOP. REMOVED AND REPLACED CEILING LI GHT ABOVE 21C PER MM 33-51-00 PAGE 501. OPS CHECKED OK. (M) 2 L 7 4 4F A20WE 1996091900851 19960919 00851 NM 1996 9 19 USAA960559 1 19960822 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 532 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 236US 41396 22352 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND TWO .25 INCH CRACKS AT FASTENER HOLES STATION 532, STRINGER 15R. REMOVE D DAMAGED SECTION OF STRINGER AND PERFORMED STRINGER SPLICE REPAIR. REPAIRED PER SRM 53-10-3. (M) 2 L 7 2 4F A16WE 1996091900852 19960919 00852 NM 1996 9 19 USAA960560 1 19960822 A 5320 BEAM BOEING 737 737201 1384454 NM BS 420-500 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 236US 41396 22352 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY 1 INCH CORRODED AREAS BS 420 TO BS 500, STRINGER 26R B EAM. FABRICATED AND REPLACED WITH NEW BEAM. SPLICED AT 420 AND 500. REPAIRED PER SRM 53-00-53 AND SRM 53-10-5. CORRO SION TAKS NR 53-208-01, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996091900853 19960919 00853 NM 1996 9 19 USAA960561 1 19960822 A 5320 ANGLE BOEING 737 737201 1384454 NM BS 277-340 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 236US 41396 22352 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 40 INCH STATION 277 TO 340 'Z' ANGLE RIGHT SIDE. IN STALLED DOUBLER, REPAIRED PER SRM 51-40-3. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996091900854 19960919 00854 NM 1996 9 19 USAA960562 1 19960822 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 532 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 236US 41396 22352 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND TWO .25 INCH CRACKS IN FASTENER HOLES FOR STRINGER 15R TO STATION 532. C UT OUT DAMAGED AREA AND FABRICATED AND REPLACED DAMAGED SECTION WITH STRINGER. REPAIRED SPLICE REPAIR PER SRM 53-10-3 F IG 1. (M) 2 L 7 2 4F A16WE 1996091900855 19960919 00855 NM 1996 9 19 USAA960563 1 19960822 A 5315 FLOOR BEAM BOEING 737 737201 1384454 NM BS 947.5 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 236US 41396 22352 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION .5 INCH BY 6 INCH AT STATION 947.5 FLOOR BEAM. REPAIRED T-CAP , DOUBLERS AND REPAIR ANGLES. REPAIRED PER TR 53-10-05C. SUBMITTER STATES, CORROSION ATTRIBUTED TO CHEMICAL SPILL. CO RROSION TASK NR C53-107-02, CORROSION LEVEL 1. (M) 2 L 7 2 4F A16WE 1996091900856 19960919 00856 NM 1996 9 19 USAA960564 1 19960822 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 967 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 236US 41396 22352 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 7 INCH CORRODED AREA STRINGER 27L, STATION 967. CUT OUT DAMAG E AND INSTALLED STRINGER SPLICE REPAIR. REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M ) 2 L 7 2 4F A16WE 1996091900857 19960919 00857 NM 1996 9 19 USAA960565 1 19960822 A 5315 FLOOR BEAM BOEING 737 737201 1384454 NM BS 663 BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 236US 22352 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND UPPER 'T' OF FLOOR BEAM BROKEN INTO STATION 663 BL0. INSTALLED DOUBLER ON T-CAP AND WEB. REPAIRED PER BOEING DRAWING 65C34537. (M) 2 L 7 2 4F A16WE 1996091900858 19960919 00858 NM 1996 9 19 USAA960566 1 19960821 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 987 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 281AU 35254 23114 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 5 INCH, 2 INCH BY 6 INCH AND SMALLER SPOTS OF CORROSION BS 987 LBL 16 TO RBL 45 TOP FLOOR BEAM T-CAP. REMOVED T-CAP, FABRICATED AND INSTALLED NEW T-CAP, REPAIRED PER TR 53-10-5C. C ORROSION TASK NR C53-107-02, CORROSION LEVEL 1. (M) 2 L 7 2 4F A16WE 1996091900859 19960919 00859 NM 1996 9 19 USAA960567 1 19960822 A 5315 FLOOR BEAM BOEING 737 737201 1384454 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 236US 41396 22352 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND ONE .25 INCH CRACK BS 520 AT RBL 25 CABIN FLOOR BEAM. INSTALLED NEW CHA NNELS AND DOUBLERS PER EA 41421. (M) 2 L 7 2 4F A16WE 1996091900860 19960919 00860 NM 1996 9 19 USAA960568 1 19960822 A 5315 FLOOR BEAM BOEING 737 737201 1384454 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 236US 41396 22352 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND ONE .25 INCH CRACK BS 520 AT RBL 45 INCH FLOOR BEAM. INSTALLED NEW CHAN NEL AND DOUBLERS, REPAIRED PER EA 41421. (M) 2 L 7 2 4F A16WE 1996091900861 19960919 00861 NM 1996 9 19 USAA960569 1 19960821 A 5320 T-CAP BOEING 737 7372B7 1384560 NM BS 360 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 281AU 35254 23114 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH SURFACE CORROSION AT BS 360 RBL 12 T-CAP. CUT OUT DAMAGE, FABRIC ATED FILLER, REPAIR ANGLES AND INSTALLED PER SRM 53-10-9, 51-10-1. (M) 2 L 7 2 4F A16WE 1996091900862 19960919 00862 NM 1996 9 19 USAA960570 1 19960821 A 5314 KEEL BEAM BOEING 737 7372B7 1384560 NM BS 710-727 FRETTING A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 281AU 35254 23114 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND FRETTING AT BOLT HOLES RIGHT HAND BOTTOM FLANGE OF KEEL BEAM STATION 710 -727. SPOT FACED HOLES, FABRICATED FILLERS, STRAP DOUBLER AND INSTALLED PER EA 41405. (M) 2 L 7 2 4F A16WE 1996091900863 19960919 00863 NM 1996 9 19 USAA960571 1 19960821 A 5314 KEEL BEAM BOEING 737 7372B7 1384560 NM BS 727-710 CHAFFING A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 281AU 35254 23114 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CHAFFING AT 5 FASTENER HOLES 17 INCH LEFT STATION 727 TO STATION 710 KEE L BEAM LOWER CHORD ANGLE. SPOT FACED HOLES, FABRICATED FILLERS, STRAP DOUBLER AND INSTALLED PER EA 41405. (M) 2 L 7 2 4F A16WE 1996091900864 19960919 00864 NM 1996 9 19 USAA960572 1 19960821 A 5320 ANGLE BOEING 737 7372B7 1384560 NM BS 270 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 281AU 35254 23114 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 4 INCH SPOT OF CORROSION ON Z-ANGLE BS 270 LBL 10 TO LBL 5. I NSTALLED ANGLE REPAIR/SPLICE, REPAIRED PER TR 53-20-04. CORROSION TASK NR C53-107-02, CORROSION LEVEL 1. (M) 2 L 7 2 4F A16WE 1996091900865 19960919 00865 NM 1996 9 19 USAA960573 1 19960821 A 5320 T-CAP BOEING 737 7372B7 1384560 NM BS 328 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 281AU 35254 23114 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND SURFACE CORROSION BS 328 FROM RBL 12 TO RBL 49 T-CAP. REMOVED CORRODED T-CAP, FABRICATED AND INSTALLED NEW ONE. REPAIRED PER TR 53-10-13. CORROSION TASK NR C53-107-02, CORROSION LEVEL 1. ( M) 2 L 7 2 4F A16WE 1996091900866 19960919 00866 NM 1996 9 19 USAA960577 1 19960822 A 5330 SKIN BOEING 737 7374B7 1384702 NM BS 344 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 19509 24554 CLT - INSPECTION VISUALLY FOUND 24 INCH SECTION OF SKIN CORROSION, LOCATED AT STATION 344 BBL 0 - LBL 24, AT FASTENER HO LES. INSTALLED REPAIR ANGLES AS PER TYPICAL REPAIR MANUAL 53-10-03. (M) 2 L 7 2 4F RT A16WE 1996091900867 19960919 00867 NM 1996 9 19 USAA960578 1 19960822 A 5315 FLOOR BEAM BOEING 737 7374B7 1384702 NM BS 312 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 29711 24554 CLT - INSPECTION VISUALLY FOUND 1 INCH BY 1 INCH CORROSION AREA, LOCATED AT STATION 312 FLOOR BEAM AT BL 0 RBL 24. FABR ICATED AND INSTALLED T-CAP AS PER SRM AND TYPICAL REPAIR MANUAL 53-10-03. (M) 2 L 7 2 4F RT A16WE 1996091900868 19960919 00868 NM 1996 9 19 USAA960579 1 19960823 A 5330 SKIN BOEING 737 737201 1384454 NM BS 937 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 262AU 35245 22868 ROA - DURING 'CX-1' CHECK VISUAL INSPECTION, FOUND 2.5 INCH BY 1.75 INCH DENT STRINGER 22L BS 937 FUSELAGE SKIN. REMOVE D DAMAGE AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 6. (M) 2 L 7 2 4F A16WE 1996091900869 19960919 00869 NM 1996 9 19 USAA960595 1 19960823 A 5315 FLOOR BEAM BOEING 737 7374B7 1384702 NM BS 344 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 436US 19302 24558 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION .25 INCH SPOTS FLOOR BEAM T-CAP BS 344, BL 0 - RBL 8. SPLICED T-CAP INSTALLED FILLER AND DOUBLERS, REPAIRED PER TR 53-10-03. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996091900870 19960919 00870 NM 1996 9 19 USAA960596 1 19960823 A 5315 FLOOR BEAM BOEING 737 7374B7 1384702 NM BS 312 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 436US 19302 24558 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER SPOTS OF CORROSION TOP OF FLOOR BEAM BS 312 LBL 14 BBL 0 RBL 8. CUT OFF UPPER CHORD RBL 19 TO LBL 33 AND INSTALLED NEW T-CAP. REPAIRED PER TR 53-10-03. CORROSION TASK NR C53 -107-02, CORROSION LEVEL 1. (M) 2 L 7 2 4F RT A16WE 1996091900871 19960919 00871 NM 1996 9 19 USAA960597 1 19960823 A 5315 FLOOR BEAM BOEING 737 7374B7 1384702 NM BS 328 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 436US 19302 24558 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION .5 INCH DIAMETER SPOTS FLOOR BEAM 'T' CAP BS 328 RBL 13, 14, 2 1, 23, 28, 35, 42, 49. INSTALLED T-CAP CAP SPLICE AND DOUBLERS, REPAIRED PER TR 53-10-03. CORROSION TASK NR C53-107-02 , CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996091900872 19960919 00872 NM 1996 9 19 USAA960603 1 19960829 A 5320 CHORD BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 266AU 37906 22878 CLT - INSPECTION FOUND, BY ULTRASONIC, CRACKS .5 INCH LONG FROM FASTENER HOLE TO EDGE OF CHORD AT STATION 727 STRINGER 1 8A OUTER CHORD LEFT SIDE. REPLACED CHORD PER EO NR 5394GD68, EA NR 58752 AND EA NR 58778. (M) 2 L 7 2 4F A16WE 1996091900873 19960919 00873 NM 1996 9 19 USAABB96024 1 19960821 A 2910 AS11608K0195 HYD LINE BOEING 757 757225 1384959 NM LT MLG WW LEAKING A USAA A UNSCHED LANDING B J K SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION FLUID LOSS CL CLIMB 1 EA 19 604AU 22199 PIT - FL 88 - AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. LEFT SIDE HYDRAULIC QUANTITY AND PRESSURE WENT TO ZERO. S YSTEM PRESSURE LIGHT ILLUMINATED AND CREW RECEIVED EICAS MESSAGE 'L HYD SYS PRESS'. TOWER ADVISED THAT SMOKE WAS COMING FROM THE LEFT SIDE OF THE AIRCRAFT. FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR DOWNLOCK LINE. (M) 2 L 7 2 4F RT A2NM 1996091900874 19960919 00874 WP 1996 9 19 USAAD96117 1 19960817 A 3350 41B030CF00101 BATTERY PACK DOUG DC9 DC931 3022065 WP CARGO COMPT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 951VJ 47576 LEFT NACELLE EMERGENCY LIGHT DOES NOT ILLUMINATE. REPLACED BATTERY PACK IN CARGO COMPARTMENT CEILING. (M) 2 L 7 2 4F A6WE 1996091900875 19960919 00875 WP 1996 9 19 USAAD96119 1 19960813 A 3350 41B030CF00101 BATTERY PACK DOUG DC9 DC931 3022065 WP AFT CARGO DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 984VJ 47207 LEFT AND RIGHT NACELLE EMERGENCY LIGHTS INOPERATIVE. REPLACED BOTH BATTERY PACKS. (M) 2 L 7 2 4F A6WE 1996091900876 19960919 00876 EU 1996 9 19 USAAF96089 1 19960813 A 3230 200497005 DOWNLOCK ACT FOKKER F28 F28MK4000 4990810 EU LT MLG FAILED A USAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 19 476US 11224 CLT-GSO - FLT 690 - BEFORE LANDING AT GSO, LEFT MAIN GEAR WAS DOWN BUT SHOWED A RED UNSAFE INDICATION. CREW DID A GO AR OUND PROCEDURE. CAPTAIN REQUESTED CFR. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT MLG DOWNLOCK ACT UATOR. GEAR SWING WAS PERFORMED AFTER INSTALL. ALL OPERATIONS CHECKED GOOD. (M) 2 L 7 2 4F RT A20EU 1996091900877 19960919 00877 EU 1996 9 19 USAAF96090 1 19960814 A 5270 SWITCH FOKKER F28 F28MK4000 4990810 EU CARGO DOOR BROKEN A USAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 19 481US 11230 CLT-CAE - FLT 751 - DURING TAKEOFF ROLL, CARGO DOOR WARNING LIGHT ILLUMINATED. CAPTAIN REJECTED TAKEOFF. SPEED AT TIME OF REJECTION WAS 90 KTS. AIRCRAFT RETURNED TO GATE. MAINTENANCE FOUND CENTER CARGO DOOR WARNING SWITCH OUT OF ADJUSTE MENT. THEY ADJUSTED THE SWITCH. OPERATION CHECK NORMAL. (M) 2 L 7 2 4F RT A20EU 1996091900878 19960919 00878 EU 1996 9 19 USAAF96091 1 19960814 A 2750 BEARING FOKKER F28 F28MK0100 4990807 EU RT TE FLAP LOOSE A USAA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 EA 19 884US 11338 CLT-ILM - FLT 909 - ON APPROACH TO ILM, FLAP DISAGREE ALERTED. CREW TRIED TO RAISE FLAPS BUT THEY WERE STUCK AT 3 DEGRE ES. FLIGHT RETURNED TO CLT WITH FLAPS AT 3 DEGREES. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TIGHTENED LOO SE VERTICAL ROLLER BEARING AT FLAP ZONE 633KL RIGHT WING INNER FAIRING DOOR. CYCLED FLAPS SEVERAL TIMES. OPERATIONAL C HECKS GOOD. (M) 2 L 7 2 4F RT 1996091900879 19960919 00879 EU 1996 9 19 USAAF96092 2 19960815 A 7200 ENGINE FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAYMK65015 EU NR 2 FAILED A USAA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 EA 19 852US 11280 017261 ERI-PIT - FLT 1533 - AS AIRCRAFT WAS STARTING DESCENT AT FL 160 INTO PIT, THE CAPTAIN REPORTED LOW OIL PRESSURE ON NR 2 ENGINE. CAPTAIN SHUT DOWN ENGINE AND DECLARED EMERGENCY. AIRCRAFT WAS CLEARED TO PIT AND LANDED AT PIT WITHOUT INCIDEN T. MAINTENANCE REPLACED RIGHT ENGINE ASSEMBLY. (M) 2 L 7 2 4F 4 F RT 1996091900880 19960919 00880 EU 1996 9 19 USAAF96093 1 19960820 A 3350 1315 LAMP FOKKER F28 F28MK4000 4990810 EU CABIN BLOWN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 476US 11224 CLT - LEFT OVERWING EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED THE LEFT OVERWING EXIT LIGHT. (M) 2 L 7 2 4F RT A20EU 1996091900881 19960919 00881 EU 1996 9 19 USAAF96096 1 19960901 A 5414 BLOWOUT PNL FOKKER F28 F28MK4000 4990810 EU RT STUBWING OPEN A USAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 19 490US 11152 CLT-HSV - FLT 546 - ON CLIMB-OUT REACHING 16,000 FEET, CREW FELT AIRFRAME VIBRATION. NO EMERGENCY DECLARED. RETURNED T O CLT. NO FURTHER INCIDENT DURING THE FLIGHT. MAINTENANCE FOUND RIGHT STUBWING BLOWOUT PANEL OPEN. REPAIRED BLOWOUT PANEL HINGE AND SECURED THE PANEL. (M) 2 L 7 2 4F RT A20EU 1996091900882 19960919 00882 NM 1996 9 19 USAASB96162 1 19960819 A 2612 6678 FIRE DETECTOR BOEING 737 737301 1384611 NM NR 1 ENGINE FAILED A USAA A E UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 EA 19 335US 23232 CLT - FLT 1594 - CREW RECEIVED NR 1 ENGINE OVERHEAT LIGHT DURING FLIGHT. THE NR 1 ENGINE WAS SHUT DOWN AND THE FLIGHT R ETURNED TO FIELD AT CLT. EMERGENCY WAS DECLARED AND THE FLIGHT LANDED SAFELY WITH NO FURTHER INCIDENT. TOTAL SINGLE EN GINE TIME WAS 20 MINUTES. MAINTENANCE FOUND THE NR 1 ENGINE CORE LOOP FAILED. REPLACED SAME PER THE MM. OPS CHECK GOO D. (M) 2 L 7 2 4F RT A16WE 1996091900883 19960919 00883 NM 1996 9 19 USAASB96171 1 19960830 A 3320 61362 LIGHT BALLAST BOEING 737 737201 1384454 NM FORWARD GALLEY BURNED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 19 236US 22352 IAH - FL 1183 - ON DESCENT INTO IAH, CREW DETECTED SMELL OF SMOKE IN THE COCKPIT. WHILE LOOKING FOR THE SOURCE, THE SMO KE ALARM IN THE FORWARD LAV WENT OFF. SHORTLY AFTER, SMOKE WAS SPOTTED ABOVE THE LEFT FORWARD JUMP SEAT. CREW WENT ON OXYGEN AND STARTED ELECTRICAL SMOKE/FIRE CHECKLIST. THE FLIGHT LANDED SAFELY AT IAH WITH NO FURTHER INCIDENT. MAINTENA NCE FOUND THE LIGHT BALLAST FOR THE FORWARD GALLEY BURNED UP. REPLACED SAME. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1996091900884 19960919 00884 EU 1996 9 19 VTZA96300 1 19960812 A 7722 CONNECTOR BAG JETSTM JETSTM3201 1500217 EU RT EGT DIRTY A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 27 483UE 898 FLT NR 6328 - PIT-IAD - ABORTED TAKEOFF DUE TO RIGHT EGT AND TORQUE DROPPED DURING TAKEOFF. AIRCRAFT LANDED AT PIT AND RETURNED TO GATE NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI 56658, MEL 76-10, ON SRL, OPS CHECK OK. AIRCRAFT WAS REL EASED AND APPROVED FOR RETURN TO SERVICE. MAINTENANCE CLOSED DMI 56658 ON 8-15-96 BY CLEANING ZONE 2 CANNON PLUG. (M) 2 L 7 2 4T RT A56EU 1996091900885 19960919 00885 EU 1996 9 19 VTZA96303 1 19960813 A 2611 SMOKE WARNING JETAIR JETSTM JETSTM4101 1500501 EU LAVATORY ACTIVATED A VTZA K NONE N FALSE WARNING DE DESCENT 1 EA 27 315UE 41033 FLT NR 6355 - IAD-TYS - THE LAV SMOKE WARNING CAME ON DURING DESCENT. AIRCRAFT WENT TO GATE, NO FURTHER INCIDENTS. MAI NTENANCE OPENED DMI 8077, MEL 26-10, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. MAINTENAN CE CLOSED DMI 8077 BY INSPECTION AND TESTING SMOKE DETECTOR, COULD NOT DUPLICATE AND NO DEFECTS NOTED. (M) 2 L 7 2 4T RT A41NM 1996091900886 19960919 00886 EU 1996 9 19 VTZA96304 1 19960814 A 5246 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU REFUEL DOOR OUT OF ADJUST A VTZA C ABORTED TAKEOFF J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 322UE 41058 FLT 6207 - IAD-MHT - DURING TAXI OUT, RETURNED TO GATE AFTER EXPERIENCING A REFUEL DOOR WARNING LIGHT. AIRCRAFT RETURNE D TO THE GATE NO FURTHER INCIDENTS. MAINTENANCE TROUBLE SHOT THE PROBLEM AND DEFERRED THE REFUEL DOOR UNDER MEL 28-6. A IRCRAFT WAS THEN RELEASED FOR SERVICE. MEL 28-6 REQUIRES THAT THE REFUEL DOOR IS TO BE VERIFIED CLOSED BEFORE EACH FLIG HT. CURRENTLY AWAITING PARTS FOR REPLACEMENT AND CLOSE-OUT. MAINTENANCE CLOSED DMI 17636 ON 8-15-96 BY ADJUSTING LATCH MICROSWITCH. AIRCRAFT RELEASED AND APPROVED FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1996091900887 19960919 00887 EU 1996 9 19 VTZA96305 1 19960813 A 2751 TY176004A POS TRANSDUCER JETAIR JETSTM JETSTM4101 1500501 EU LT TE FLAP FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 302UE 41013 FLT 6429 - IAD-JFK - DURING TAKEOFF, RETURNED TO THE GATE AFTER EXPERIENCING A FLAP FAULT CAPTION ILLUMINATION ON THE CA PTION PANEL. AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE TROUBLESHOT THE DISCREPANCY AND FOUND THAT THE LEFT FLAP POSITION TRANSDUCER HAD FAILED. MAINTENANCE REPLACED THE LEFT FLAP POSITION TRANSDUCER AND RELEASED THE AIRCRAFT FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1996091900888 19960919 00888 EU 1996 9 19 VTZA96307 1 19960815 A 5210 DOOR MECH BAG JETSTM JETSTM3201 1500217 EU PAX DOOR NOT LATCHED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 476UE 884 FLT 6152 - BGM-IAD - ABORTED TAKEOFF DUE TO PAX DOOR OPENED DURING TAKEOFF ROLL AT 90 KTS. AIRCRAFT RETURNED TO GATE, N O FURTHER INCIDENTS. MAINTENANCE COMPLETED REPAIRS ON 8-17-96 BY REMOVING AND REPLACING PAX DOOR HINGE AND PLATES PLUS HARDWARE, RIGGED DOOR IAW MM AND C/W PRESSURIZATION CHECK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. ( M) 2 L 7 2 4T RT A56EU 1996091900889 19960919 00889 EU 1996 9 19 VTZA96308 1 19960816 A 5270 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGG DOOR DIRTY A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 303UE 41015 FLT NR 6416 - PVD-IAD - AIRCRAFT ABORTED TAKEOFF DUE TO BAGGAGE DOOR WARNING LIGHT ILLUMINATED. MAINTENANCE OPENED DMI0 3925, MEL 52,30. MAINTENANCE CLOSED DMI 03925 ON 8-18-96 BY CLEANING CONTACTS ON DOOR MICROSWITCH, OPS CHECK OK. AIRCR AFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996091900890 19960919 00890 1996 9 19 VTZA96309 4 19960816 A 3442 7008470822 RT UNIT JETAIR JETSTM JETSTM4101 1500501 EU RADAR FAILED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 326UE 41064 FLT NR 6418 - IAD-BOS - DURING CRUISE, MADE AN UNSCHEDULED LANDING DUE TO RADAR INOP, WEATHER WOULD NOT PERMIT AIRCRAFT TO CONTINUE TO BOS. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED RADAR RIGHT. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996091900891 19960919 00891 EU 1996 9 19 VTZA96310 1 19960816 A 5230 DOOR JETAIR JETSTM JETSTM4101 1500501 EU BAGG COMPT NOT CLOSED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 307UE 41021 FLT NR 6563 - IAD-RDU - ABORTED TAKEOFF DUE TO THE BAGGAGE WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO THE GATE NO FURTHER INCIDENTS. MAINTENANCE FOUND BAGGAGE DOOR NOT CLOSED PROPERLY, RESET DOOR HANDLE, OPS CHECK OK. AIRCRAFT WAS R ELEASED AND APPROVED FOR RETURN TO SRVICE. (M) 2 L 7 2 4T RT A41NM 1996091900892 19960919 00892 EU 1996 9 19 VTZA96311 1 19960816 A 7930 696230 TRIPLE GAUGE IND BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A VTZA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 27 370MT 800 FLT NR 6435 - IAD-RDU - DURING TAXI, RETURNED TO GATE DUE TO RIGHT OIL TEMP GAUGE INOP. MAINTENANCE REMOVED AND REPLACE D OIL TEMP GAUGE, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996091900893 19960919 00893 1996 9 19 VTZA96312 3 19960816 A 6140 31056899 BETA SWITCH JETAIR JETSTM JETSTM4101 1500501 EU LT PROP FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 27 314UE 41027 FLT NR 6490 - JFK-BOS - ABORTED TAKEOFF DUE TO LEFT RED BETA LIGHT ILLUMINATED DURING TAKEOFF. AIRCRAFT RETURNED TO GAT E NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED BETA SWITCH. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVE D FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996091900894 19960919 00894 1996 9 19 VTZA96313 4 19960818 A 3418 C850067 SIGNAL PROCESSOR BAG JETSTM JETSTM3201 1500217 EU LEFT FAILED A VTZA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 27 476UE 884 FLT NR 6300 - IAD-ISP - DURING TAXI, RETURNED TO GATE DUE TO LEFT STALL WARNING LIGHT WILL NOT EXTINGUISH. MAINTENANCE REMOVED AND REPLACED SIGNAL PROCESSOR, OPS CHECK OK. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996091900895 19960919 00895 WP 1996 9 19 VTZA96314 2 19960819 A 7320 FCU ROD END JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE3311 01514 WP LT ENGINE LOOSE A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 27 314UE 41027 FLT 6233 - IAD-PWN - ABORTED TAKEOFF DUE TO LEFT ENGINE LOW TORQUE. AIRCRAFT RETURNED TO GATE NO FURTHER INCIDENTS. MA INTENANCE SECURED LOOSE ROD END ON FCU. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 3 T RT A41NM E3WE 1996091900896 19960919 00896 1996 9 19 VTZA96315 3 19960819 A 6140 8956596 BETA SWITCH BAG JETSTM JETSTM3201 1500217 EU RT PROP FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 485UE 901 FLT 6351 - IAD-SWF - DURING CLIMB, MADE UNSCHEDULED LANDING DUE TO RIGHT BETA LIGHT ILLUMINATED DURING TAKEOFF. AIRCRAF T LANDED AT IAD AND RETURNED TO GATE, NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED BETA SWITCH, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996091900897 19960919 00897 EU 1996 9 19 VTZA96316 1 19960819 A 3260 ATC135022 UPLOCK SWITCH JETAIR JETSTM JETSTM4101 1500501 EU RT MLG FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 327UE 41080 FLT 6158 - BTU-IAD - DURING CLIMB, MADE AN UNSCHEDULED LANDING DUE TO RED GEAR HANDLE ILLUMINATED AFTER GEAR WAS RETRACT ED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED RIGHT UPLOCK SWITCH. OPS CH ECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996091900898 19960919 00898 EU 1996 9 19 VTZA96317 1 19960821 A 2621 301000273 FIRE BOTTLE BAG JETSTM JETSTM3201 1500217 EU RT ENGINE BLOWN A VTZA F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 27 491UE 911 FLT NR 6550 - CHO-IAD - DURING TAXI, CREW BLEW BOTH FIRE BOTTLES ON RIGHT SIDE DUE TO RESIDUAL SMOKE DUE TO IMPROPER SHU T DOWN. BOTH BOOST PUMPS WERE LEFT ON AND PILOTS DID NOT MOTOR ENGINE THROUGH. AIRCRAFT WAS AT GATE, AND NO FURTHER IN CIDENTS. MAINTENANCE REMOVED AND REPLACED FIRE BOTTLES AND FUEL SHUT OFF VALVE, OPS CHECK OK. AIRCRAFT WAS RELEASED AN D APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996091900900 19960919 00900 1996 9 19 VTZA96319 4 19960820 A 3422 258719343 DIRECTIONAL GYRO BAG JETSTM JETSTM3201 1500217 EU NR 1 INTERMITTENT A VTZA K NONE O OTHER CR CRUISE 1 EA 27 494UE 810 FLT NR 6319 - IAD-CLE - LANDED AIRCRAFT AS SCHEDULED AT CLE DUE TO NR 1 DIRECTION GYRO INTERMITTENTLY FAILED IN FLIGHT. AIRCRAFT WENT TO GATE, NO FURTHER INCIDENTS. AIRCRAFT WAS FERRIED TO IAD. MAINTENANCE REMOVED AND REPLACED DIRECTIONA L GYRO, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996091900901 19960919 00901 EU 1996 9 19 VTZA96320 1 19960819 A 7722 6100116 EGT INDICATOR BAG JETSTM JETSTM3201 1500217 EU NR 1 STICKS A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 27 490UE 909 FLT NR 6427 - IAD-ROA - ABORTED TAKEOFF DUE TO NR 1 EGT INDICATION STICKS. AIRCRAFT RETURNED TO GATE NO FURTHER INCIDEN TS. MAINTENANCE REMOVED AND REPLACED EGT INDICATOR. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SE RVICE. (M) 2 L 7 2 4T RT A56EU 1996091900902 19960919 00902 EU 1996 9 19 VTZA96323 1 19960825 A 3230 14110001403 LOCK DOWN PIN JETAIR JETSTM JETSTM4101 1500501 EU NLG NOT REMOVED A A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 302UE 41013 FLT 6203 IAD - MHT - RETURNED TO IAD DURING CLIMB AFTER EXPERIENCING AN UNRESPONSIVE NOSE GEAR RETRCTION SCENARIO. AIRC RAFT DECLARED AN EMERGENCY AND RETURNED TO IAD AND THE GATE. MAINTENANCE FOUND THAT THE RAMP PERSONNEL HAD NOT COMPLIED WITH THE PROCEDURES FOR REMOVING THE GEAR LOCK DOWN PINS PRIOR TO SENDING THE AIRCRAFT OUT. MAINTENANCE REMOVED THE PI N AND RELEASED THE AIRCRAFT FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1996091900903 19960919 00903 EU 1996 9 19 VTZA96324 1 19960824 A 2611 7211121100 SMOKE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU BAGG COMPT INOPERATIVE A VTZA B EMER. DESCENT N FALSE WARNING CR CRUISE 1 EA 27 315UE 41033 FLT 6267 - IAD-BTV - DURING TAKEOFF AND CRUISE, EXPERIENCED A VENTRAL BAGGAGE SMOKE CAPTION LIGHT. THE AIRCRAFT DECLARE D AN EMERGENCY AND RETURNED TO IAD. UPON ARRIVAL AT IAD, THE MAINTENANCE DEPARTMENT EVALUATED THE PROBLEM AND FOUND THE BAGGAGE BAY SMOKE DETECTOR INOPERATIVE. MAINTENANCE REPLACED THE SMOKE DETECTOR AND RELEASED THE AIRCRAFT FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1996091900904 19960919 00904 EU 1996 9 19 VTZA96325 1 19960825 A 2611 7211121100 SMOKE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU BAGG COMPT INOPERATIVE A VTZA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 27 301UE 41012 FLT 6429 - IAD-JFK - DURING TAKEOFF, EXPERIENCED A MOMENTARY BAGGAGE POD SMOKE CAPTION LIGHT AND ABORTED THE TAKEOFF AND RETURNED TO THE GATE. UPON ARRIVAL AT THE GATE, THE MAINTENANCE DEPARTMENT EVALUATED THE PROBLEM AND FOUND THE BAGGAGE POD SMOKE DETECTOR INOPERATIVE. MAINTENANCE REPLACED THE SMOKE DETECTOR AND RELEASED THE AIRCRAFT FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1996091900905 19960919 00905 EU 1996 9 19 VTZA96326 1 19960825 A 2611 7211121100 SMOKE DETECTOR BAG JETSTM JETSTM3201 1500217 EU BAGGAGE POD INOPERATIVE A VTZA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 495UE 818 FLT 6283 - IAD-HPN - ABORTED TAKEOFF DUE TO A MOMENTARY BAGGAGE SMOKE LIGHT INDICATION. THE AIRCRAFT RETURNED TO THE GA TE WHERE MAINTENANCE REMOVED AND REPLACED THE BAGGAGE POD SMOKE DETECTOR IAW THE AIRCRAFT MM. THE AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996091900906 19960919 00906 EU 1996 9 19 VTZA96327 1 19960823 A 2432 BTCA520 BATTERY BAG JETSTM JETSTM3201 1500217 EU NR 2 BATTERY OVERHEATED A VTZA B EMER. DESCENT M OVER TEMP CR CRUISE 1 EA 27 472UE 823 FLT 6283 - IAD-HPN - DURING CRUISE, RETURNED DUE TO NR 2 BATTERY OVERTEMP INDICATION. AIRCRAFT RETURNED TO IAD. MAINTE NANCE REMOVED AND REPLACED THE NR 2 BATTERY IAW THE AIRCRAFT MM. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVI CE. (M) 2 L 7 2 4T RT A56EU 1996091900907 19960919 00907 1996 9 19 VTZA96328 4 19960826 A 3414 39948B2236 AIRSPEED IND BAG JETSTM JETSTM3201 1500217 EU LT COCKPIT FAILED A VTZA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 27 477UE 890 FLT NR 6342 - IAD-ELM - DURING TAKEOFF, AIRCRAFT EXPERIENCED AN AIRSPEED INDICATOR (ASI) FAILURE ON THE PILOTS SIDE. AI RCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE WHERE MAINTENANCE REPLACED THE CAPTAINS ASI. SYSTEM WAS THEN OPERATIONA LLY CHECKED, WITH NO FURTHER PROBLEMS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996091900908 19960919 00908 EU 1996 9 19 VTZA96329 1 19960826 A 2421 51539002B GCU BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A VTZA D RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 EA 27 497UE 904 FLT 6570 - IAD-MDT - AIRCRAFT EXPERIENCED A RIGHT GENERATOR THAT WOULD NOT RESET. AIRCRAFT RETURNED TO THE GATE AND MAI NTENANCE REPLACED THE RIGHT GCU. SYSTEM WAS THEN OPERATIONALLY CHECK WITH NO FURTHER PROBLEMS. AIRCRAFT WAS RELEASED A ND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996091900909 19960919 00909 EU 1996 9 19 VTZA96330 1 19960827 A 5210 1371376C403 SHOOT BOLTS BAG JETSTM JETSTM3201 1500217 EU PAX DOOR DIRTY A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 494UE 810 FLT NR 6262 - IAD-GSO - DURING CLIMB, EXPERIENCED A PASSENGER DOOR WARNING INDICATION. THE AIRCRAFT RETURNED TO IAD DUE TO REQUIREMENTS AS OUTLINED IN THE AIRCRAFT QRH. MAINTENANCE CLEANED AND LUBRICATED THE PASSENGER DOOR SHOOT BOLTS AND PERFORMED AN OPERATIONAL CHECK OF THE DOOR TO ENSURE COMPLIANCE WITH PROPER ADJUSTMENTS. AIRCRAFT WAS THEN RELEASED AN D APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996091900910 19960919 00910 EU 1996 9 19 VTZA96331 1 19960828 A 2750 5148YMK83NP FLAP SELECTOR BAG JETSTM JETSTM3201 1500217 EU COCKPIT OPEN CIRCUIT A A VTZA L ABORTED APPROACH F FLT CONT AFFECTED DE DESCENT 1 EA 27 484UE 899 FLT NR 6311 - EWR-IAD - DURING DESCENT, EXPERIENCED A FLAP PROBLEM. PROBLEM INVOLVED FLAPS NOT GOING TO 10 DEGREES. FL APS WOULD ONLY GO TO EITHER O TO 35 DEGREES. THE AIRCRAFT LANDED AT IAD WHERE MAINTENANCE TROUBLESHOT AND REPLACED THE FLAP SELECTOR HANDLE. MAINTENANCE THEN PERFORMED AN OPERATIONAL CHECK OF THE FLAP SYSTEM TO ENSURE COMPLIANCE WITH ALL PROPER PARAMETERS. AIRCRAFT WAS THEN RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996091900911 19960919 00911 EU 1996 9 19 VTZA96333 1 19960828 A 3260 GEAR LIGHTS JETAIR JETSTM JETSTM4101 1500501 EU LT MLG MALFUNCTIONED A VTZA K NONE N FALSE WARNING CL CLIMB 1 EA 27 314UE 41027 FLT NR 6553 - PWM-BOS - DURING CLIMB, EXPERIENCED A LEFT MAIN GEAR INTRANSIT LIGHT AND GEAR HANDLE LIGHT ILLUMINATION AF TER THE GEAR WAS SELECTED TO THE UP POSITION. FLIGHT CREW SELECTED GEAR DOWN AND OBSERVED THREE GREEN DOWN AND LOCKED I NDICATIONS. AIRCRAFT LANDED AT BOS. AIRCRAFT WAS THEN FERRIED TO IAD WHERE THE MAINTENANCE DEPARTMENT PERFORMED AN INS PECTION AND OPERATIONAL CHECK OF THE LANDING GEAR SYSTEM. THE SYSTEM PERFORMED IAW THE MM GUIDELINES WITH NO DISCREPANC Y FOUND. MAINTENANCE THEN RELEASED THE AIRCRAFT FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1996091900912 19960919 00912 EU 1996 9 19 VTZA96334 1 19960829 A 3233 AIR864960 ACTUATOR JETAIR JETSTM JETSTM4101 1500501 EU LT MLG FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 314UE 41027 FLT 6193 - IAD-JFK - DURING CLIMB, EXPERIENCED A LEFT MAIN GEAR INTRANSIT LIGHT AND GEAR HANDLE LIGHT ILLUMINATION, AFTE R THE GEAR WAS SELECTED TO THE UP POSITION. FLIGHT CREW SELECTED GEAR DOWN AND OBSERVED THREE GREEN DOWN AND LOCKED IND ICATIONS. AIRCRAFT RETURNED TO IAD. THE MAINTENANCE DEPARTMENT PERFORMED AN INSPECTION AND OPERATIONAL CHECK OF THE LA NDING GEAR SYSTEM AND REPLACED THE LEFT GEAR ACTUATOR. THE SYSTEM PERFORMED IAW THE MM GUIDELINES WITH NO FURTHER DISCR EPANCY NOTED. MAINTENANCE THEN RELEASED THE AIRCRAFT FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1996091900913 19960919 00913 EU 1996 9 19 VTZA96335 1 19960829 A 2120 DUCT BAG JETSTM JETSTM3201 1500217 EU RT ACM LOOSE A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 487UE 906 FLT NR 6424 - IAD-BUF - DURING CLIMB, AN UNSCHEDULED LANDING DUE TO RIGHT FLOW INOP. AIRCRAFT LANDED AT IAD AND RETURNE D TO GATE NO FURTHER INCIDENTS. MAINTENANCE RESECURED LOOSE DUCT ON RIGHT ACM, PRESSURE AND OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996091900914 19960919 00914 EU 1996 9 19 VTZA96336 1 19960829 A 2750 S2700004 CONTROL RELAY BAG JETSTM JETSTM3201 1500217 EU TE FLAPS FAILED A A VTZA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 EA 27 484UE 899 FLT NR 6319 - IAD-CLE - DURING APPROACH, EXPERIENCED A FLAP PROBLEM. WHEN FLAPS SELECTED TO 10 PERCENT THE FLAP WENT TO 35 PERCENT UNCOMMANDED. THE AIRCRAFT LANDED AT IAD WHERE MAINTENANCE TROUBLESHOT AND REPLACED FLAP CONTROL RELAY. MAI NTENANCE THEN PERFORMED AN OPERATIONAL CHECK OF THE FLAP SYSTEM TO ENSURE COMPLIANCE WITH ALL PROPER PARAMETERS. AIRCRA FT WAS THEN RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996091900915 19960919 00915 1996 9 19 VTZA96337 4 19960901 A 3416 4016341905 ALTIMETER JETAIR JETSTM JETSTM4101 1500501 EU LT COCKPIT FAILED A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 326UE 41064 FLT NR 6217 - IAD-PVD - DURING CLIMB, AN UNSCHEDULED LANDING DUE TO CAPTAINS ALTIMETER INOP. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED ALTIMETER. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROV ED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996091900916 19960919 00916 EU 1996 9 19 VTZA96338 1 19960902 A 7722 EGT IND BAG JETSTM JETSTM3201 1500217 EU LT ENGINE HIGH A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 491UE 911 FLT NR 6321 - IAD-AVP - ABORTED TAKEOFF DUE TO HIGH EGT AND RPM OF 107 PERCENT AT TAKEOFF. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE PERFORMED EXTENSIVE GROUND RUNS INCLUDING OVERSPEED GOVERNOR, PLUS PERFORMED LEFT ENG INE SOAP SAMPLE, COULD NOT DUPLICATE, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996091900917 19960919 00917 EU 1996 9 19 VTZA96339 1 19960830 A 2432 BTCA520 BATTERY BAG JETSTM JETSTM3201 1500217 EU NR 1 OVERTEMP A VTZA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP TO TAKEOFF 1 EA 27 480UE 894 FLT NR 6388 - HPN-IAD - DURING TAKEOFF, MADE A UNSCHEDULED LANDING DUE TO NR 1 BATTERY HOT LIGHT ILLUMINATED. AIRCRAFT LANDED AT HPN AND RETURNED TO GATE NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED BATTERY, OPS CHECK OK. AIRCR AFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996091900918 19960919 00918 EU 1996 9 19 VTZA96340 1 19960830 A 2432 BTCA520 BATTERY BAG JETSTM JETSTM3201 1500217 EU NR 2 OVERHEATED A VTZA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CR CRUISE 1 EA 27 472UE 823 FLT 6156 - AIB-IAD - DURING CRUISE, DEVIATED TO MDT DUE TO NR 2 BATTERY OVERTEMP INDICATION. MAINTENANCE REMOVED AND RE PLACED THE NR 2 BATTERY IAW THE AIRCRAFT MM. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996091900919 19960919 00919 EU 1996 9 19 VTZA96341 1 19960831 A 2133 OUTFLOW VLV BAG JETSTM JETSTM3201 1500217 EU CABIN WIRED OPEN A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 480UE 894 FLT NR 6296 - IAD-RON - DURING CLIMB, AN UNSCHEDULED LANDING DUE TO MANUAL PRESSURE WOULD NOT WORK. AIRCRAFT LANDED AT IAD AND RETURNED TO GATE NO FURTHER INCIDENTS. MAINTENANCE FOUND OUTFLOW VALVE SECURED OPEN. MAINTENANCE REMOVED SECUR ING DEVICE, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996091900920 19960919 00920 1996 9 19 VTZA96342 4 19960901 A 3417 7000700966 DADC JETAIR JETSTM JETSTM4101 1500501 EU LT COCKPIT FAILED A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 326UE 41064 FLT NR 6217 - IAD-PVD - UNSCHEDULED LANDING DUE TO CAPTAINS ALT LAGS BEHIND FLIGHT OFFICERS. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED DADC. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FO R RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996091900951 19960919 00951 NM 1996 9 19 CALA9601317 1 19960915 A 5330 SKIN BOEING 737 7372C0 1384488 NM BS 472.4 CRACKED A CALA K NONE O OTHER TX TAXI/GRND HDL 1 SW 09 14241 20070 THE AIRCRAFT SKIN WAS CRACKED AT C1 DOOR DURING CARGO LOADING. THE CRACK WAS LOCATED AT STA 472.4 BETWEEN STRINGER 20R AND 21R AND MEASURED 1.5 INCH LONG. A REPAIR WAS INSTALLED IAW ECRA 5330-02437. 2 L 7 2 4F A16WE 1996091900952 19960919 00952 WP 1996 9 19 CALA9601318 1 19960917 A 5350 ANB710059 FAIRING DOUG DC10 DC1030 3023501 WP LT WING/FUS DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14075 46922 THE LT WING INBOARD SLAT TO FUSELAGE FAIRING WAS FOUND DAMAGED ON ARRIVAL. ICE DAMAGE WAS SUSPECT DUE TO THE NR 2 WATER SYSTEM WAS FOUND LEAKING FROM OVERFLOW AT SERVICING PANEL. THE NR 2 WATER SYSTEM WAS EMPTY ON ARRIVAL. THE NR 2 WATER SYSTEM WAS PLACARDED INOPERATIVE. THE FAIRING WAS REPAIRED IAW ECRA 5350-01284. A DIP WAS ISSUED TO REINSPECT THE REP AIR EVERY FLIGHT UNTIL A PERMANENT REPAIR IS ACCOMPLISHED WITHIN 15 DAYS. 2 L 7 3 4F A22WE 1996091900953 19960919 00953 NM 1996 9 19 9620045639 1 19960916 A 3260 UPLOCK SENSOR BOEING 757 757251 1384970 NM LT MLG FAILED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 539US 26486 DURING TAKEOFF CLIMB HAD GEAR WARNING INDICATION. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. PERFORMED SYST EM CHECK OF MAIN LEFT LANDING GEAR UPLOCK. REPLACED BOTH LEFT MAIN GEAR UPLOCK SENSORS. CHECKED AIR GAP AND PERFORMED GEAR SWING, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A2NM 1996091900954 19960919 00954 WP 1996 9 19 9620059609 1 19960917 A 3350 6011779 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 609NW 47234 DURING PERIODIC CHECK, FOUND LEFT AND RIGHT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL C HECK NORMAL. 2 L 7 2 4F A6WE 1996091900955 19960919 00955 EU 1996 9 19 9620063228 1 19960917 A 3260 INTERFACE UNIT AIRBUS 320 A320211 3930320 EU LANDING GEAR MALFUNCTIONED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 326NW 298 DURING APPROACH, RECEIVED L/G NOT DOWN LOCKED MESSAGE AFTER LANDING GEAR EXTENSION. CYCLED THE LANDING GEAR HANDLE AND ALL INDICATIONS NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR CONTROL INTERFACE UNIT AND NOSE LANDING GEAR DOOR SENSOR 376A, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A28NM 1996091900956 19960919 00956 NM 1996 9 19 UPS96221122 1 19960917 A 3350 LIGHTS BOEING 727 72727C 138400J NM CREW ENTRANCE INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 909UP 19115 INSPECTION TYPE N/A, EMERGENCY EXIT LIGHT OVER CREW ENTRANCE INOP. CLEANED CONNECTORS FOR BATTERIES, CKS OK. 2 L 7 3 4F A3WE 1996091900957 19960919 00957 NE 1996 9 19 UPS96421064 2 19960910 A 7200 ENGINE BOEING 747 747121 1384871 NM PWA JT9 JT9D7A 52054 NE NR 4 FAILED A A IPXA E ENGINE SHUTDOWN M P OVER TEMP NO WARNING INDICATION CL CLIMB 1 SO 01 691UP 19641 INSPECTION TYPE N/A, NR FOUR ENG FAILED AFTER LIFTOFF, NO FIRE LIGHT. FIRE SHOT OUT OF INTAKE WITH MODERATE THUMP, COMP STALL. MAX T/O EGT 907 DEGREES, ENGINE SHUTDOWN CHECKLIST COMPLETED. REMOVED AND REPLACED NR 4 ENGINE PER TASK CARD A ND MAINT MANUAL. ALL LEAK CKS AND OPS CKS GOOD POWER ASSURANCE RUN GOOD. (P/N JT9D-7AH) (S/N 663023) ON, (P/N JT9D-7AH) (S/N 662203) OFF. 2 L 7 4 4F 4 F A20WE E20EA 1996091900958 19960919 00958 NM 1996 9 19 UPS96421118 1 19960829 A 5210 DOOR BOEING 747 747121 1384871 NM PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE C/D, DOOR STRUCTURE LWR HINGE ARM CUTOUT FOUND SMALL CRACK. REPAIRED SMALL CRACK AT MED 1 LT HINGE ARM CUTOUT IAW SRM 51-40-03. 2 L 7 4 4F A20WE 1996091900959 19960919 00959 NM 1996 9 19 UPS96521120 1 19960917 A 3350 20131A BATTERY PACK BOEING 757 75724APF 1384969 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 402UP 23724 INSPECTION TYPE N/A, EMER LIGHTS WEAK. REPLACED BATTERY PACK PER MM 33-51-07. 2 L 7 2 4F RT A2NM 1996091900960 19960919 00960 WP 1996 9 19 UPS96821119 1 19960916 A 5730 SKIN DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 WING SKIN CRACKED ON LOWER SURFACE INBOARD OF NR 4 PYLON JUST OUTBOARD OF NR 4 ALT AFT SUMP. CRACKED VERIFIED BY EDDY C URRENT INSPECTION. TRANSFERRED TO DMI D 115401. TRANSFERRED TO N/R 449303. 2 L 7 4 4F RT 4A25 1996091900961 19960919 00961 WP 1996 9 19 UPS96821121 1 19960914 A 3350 LIGHTS DOUG DC8 DC871F 302199D WP CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE N/A, EMERGENCY EXIT LIGHTS WOULD NOT DISARM. RELAMPED, CHECKED GOOD. 2 L 7 4 4F RT 4A25 1996091900962 19960919 00962 WP 1996 9 19 96FDEA01490 1 19960914 A 5720 ARB0029506N TENSION STRAP DOUG DC10 DC1030F 3023504 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 322FE 47908 SMRM NR 00506, RT WING, O/B FLAP I/B HINGE O/B SIDE TENSION STRAP IS CRACKED AT THE LOWER BOLT HOLE LOWER FLANGE. *S/D* REMOVED AND REPLACED TENSION STRAP BRACKET AS PER SRM 51-00-01 VOL NR I. 2 L 7 3 4F RT A22WE 1996091900963 19960919 00963 NM 1996 9 19 96FDEA01491 1 19960829 A 5320 66118092 CLIP BOEING 727 72725 1384006 NM BS 640 BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 509FE 18280 NR 0219 AND 010, STRINGER CLIP AT BS 640 STRINGER 19 RT IS BROKEN. REMOVED DAMAGED STR CLIP AND INSTALLED NEW STR CLIP BS 640 STR 19 RT. 2 L 7 3 4F A3WE 1996091900964 19960919 00964 NM 1996 9 19 96FDEA01492 1 19960917 A 5720 65185401 CHORD BOEING 727 72725 1384006 NM BS 740 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR 0674 AND 035, CORROSION (C53-224-05) ON BS 740 LOWER CHORD FOR CENTER WING SECTION FROM LBL 7 TO LBL 27. *S/D* REMO VED DAMAGED LOWER CHORD AT BS 740 AND INSTALLED NEW CHORD PER FEDEX EA NR 7-5710-31187. 2 L 7 3 4F A3WE 1996091900965 19960919 00965 WP 1996 9 19 ABXA9600628 1 19960916 A 3350 014597101 BATTERIES DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST TO TAKEOFF 1 GL 23 953AX 47608 EMERGENCY EVACUATION LIGHTS FLASH ON AND OFF DURING TAKEOFF AND TURBULENCE. REPLACED EMERGENCY LIGHT BATTERIES IAW DC-9 MM. 2 L 7 2 4F A6WE 1996091900966 19960919 00966 WP 1996 9 19 ABXA9600627 1 19960913 A 3350 5708458503 BATTERY PACK DOUG DC8 DC861 3021952 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 846AX 46158 EMERGENCY BATTERY PACK HAS LOW VOLTAGE. REPLACED BATTERY PACK, OPS CHECKED GOOD IAW DC-8 CARD DC8-1, ITEM 8. 2 L 7 4 4F 4A25 1996091900967 19960919 00967 WP 1996 9 19 96524 1 19960917 A 2560 113313 SLIDE DOUG DC9 DC932 3022066 WP FWD ENTRY DOOR FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 209ME 47730 CREW REPORTS FWD ENTRY DOOR EVAC, SLIDE FELL OFF DOOR AND GIRT BAR WAS DIFFICULT TO REMOVE. REINSTALLED FWD ENTRY EVACU ATION SLIDE AND TRIMMED CARPET GIRT BAR LATCH. 2 L 7 2 4F A6WE 1996091900968 19960919 00968 NM 1996 9 19 P5CA9600715 1 19960910 A 7830 FAIRING PLATE BOEING 747 747124 1384874 NM NR 2 ENGINE TORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 BLOCKER DOOR FAIRING PLATE TEARING UPWARD THROUGH SCREWS OF NR 2 ENGINE FAN REVERSE SLEEVE IN AFT AREA AT 6:30 POSITION. REMOVED AND REPLACED FAIRING PLATE PER BAC SRM 51-10-01 AND 51-30-02. 2 L 7 4 4F A20WE 1996091900969 19960919 00969 NM 1996 9 19 P5CA9600716 1 19960909 A 5350 FAIRING BOEING 747 747124 1384874 NM BS 920 BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 BROKEN DRAIN HOLE FAIRING AT BODY FAIRING STATION 920. REPAIRED BODY FAIRING DRAIN HOLE FAIRING PER BAC 53-30-03. 2 L 7 4 4F A20WE 1996091900970 19960919 00970 NM 1996 9 19 P5CA9600717 1 19960910 A 5400 ANGLE BOEING 747 747124 1384874 NM NR 3 ENGINE TORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 NR 3 ENGINE INBOARD COWL INNER ANGLE TORN AT LATCH. REPAIRED COWL PER BAC SRM 51-10-02 AND 51-10-01. 2 L 7 4 4F A20WE 1996091900971 19960919 00971 NM 1996 9 19 P5CA9600718 1 19960910 A 5532 SKIN BOEING 747 747124 1384874 NM RT VERT STAB DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 ROUGH REPAIL LIFTED OUT, DELAMINATED ON RIGHT VERTICAL STABLIZER LOWER SKIN. REPAIRED AREA PER BAC SRM 51-40-06. 2 L 7 4 4F A20WE 1996091900972 19960919 00972 NM 1996 9 19 P5CA9600719 1 19960910 A 5280 DOOR BOEING 747 747124 1384874 NM LT MLG CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 CRACKED WEB ON AFT END OF LEFT WING GEAR STRUT DOOR. REPAIRED PER BAC SRM 51-10-1 AND 51-30-02. 2 L 7 4 4F A20WE 1996091900973 19960919 00973 NM 1996 9 19 P5CA9600720 1 19960913 A 5542 SKIN BOEING 747 747124 1384874 NM RUDDER DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 HOLE FOUND ON PRE-DELIVERY CK ON LEFT OUTER LOWER MID SKIN OF UPPER RUDDER. REPAIRED PER BAC SRM 51-40-15 AND 51-40-11. 2 L 7 4 4F A20WE 1996091900974 19960919 00974 NM 1996 9 19 P5CA9600721 1 19960821 A 5711 SPAR BOEING 747 747132 1384882 NM WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 CORROSION ON LOWER CHORD OF FRONT SPAR IN CENTER TANK DRY BAY RBL 77. CORROSION REMOVED PER BAC SRM 51-10-01 AND AREA R EPROTECTED PER BAC SRM 51-10-02. 2 L 7 4 4F A20WE 1996091900975 19960919 00975 NM 1996 9 19 VSTA9609003 1 19960905 A 2612 894481 CONNECTOR BOEING 737 737247 138448D NM APU FIRE LOOP DIRTY A VSTA K NONE N FALSE WARNING CR CRUISE 1 WP 07 303VA 20125 APU FIRE WARNING LIGHT FLICKERS INTERMITTENTLY IN FLIGHT. ENCOUNTERED TURBULENCE AND IT STOPPED. CLEANED AND RECONNECT ED APU FIRE LOOP CANNON PLUG, OPS CHECK GOOD. 2 L 7 2 4F A16WE 1996091900976 19960919 00976 EU 1996 9 19 MALA965077 1 19960720 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 SF340A 7850100 EU CABIN DEFECTIVE A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 98XJ 340A098 DTW - FLT 3029 - ON CLIMB-OUT FROM DTW, THE LAVATORY SMOKE INDICATOR IN THE COCKPIT ILLUMINATED INTERMITTENTLY, THEN CAM E ON STEADILY. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE LAVATORY SMOKE DETECTOR. ALL CHECKS GOOD. (X) 2 L 7 2 4T RT A52EU 1996091900977 19960919 00977 NM 1996 9 19 96ZZZX4766 1 19960321 A 7722 SEL0C19E EGT INDICATOR BOEING 737 7372P6 NM NR 1 FAILED A A6XA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 13 EICKL 78ABC 21356 AIRCRAFT ON TAKEOFF ROLL AT APPROXIMATELY 80 KTS WHEN NR 1 EGT CLIMBED TO RED BAND, CREW REJECTED TAKEOFF AND RETURNED T O GATE. FOUNT NR 1 EGT INDICATOR BAD AND REPLACED. NR 1 EGT INDICATOR WAS SENT OFF FOR REPAIR AND RETURNED FOR INSTALL ATION. 2 L 7 2 4F RT A16WE 1996091900978 19960919 00978 WP 1996 9 19 96ZZZX4767 1 19960815 A 2424 51511003 GEN CNTRL UNIT LKHEED 1011 10113853 5265020 WP NR 1 POSITION DEFECTIVE A RIAA A J UNSCHED LANDING DUMP FUEL J H WARNING INDICATION ELECT. POWER LOSS-50 PC CL CLIMB 1 SO 19 501GB 193J1183 FRA/ANC - FLT 101 - DURING CLIMB, CREW WAS UNABLE TO CLOSE GENERATOR NR 3 FIELD BREAKER, GENERATOR BREAKER NR 3 AC BUS T IE BREAKER AFTER OPENING OF BREAKERS IN-FLIGHT, ACFT DUMPED FUEL AND AIR-RETURNED TO FRA. ON GROUND IN FRA, MAINTENANC E REPLACED GENERATOR CONTROL UNIT IAW MM 24-20-00, PAGE 401. OPS CHECKED NORMAL. ACFT RELEASED INTO SERVICE. 2 L 7 3 4F A23WE 1996091900981 19960919 00981 SW 1996 9 19 96ZZZX4770 1 19960727 A 6520 GEARBOX BELL 222 222U 1182140 SW TAIL ROTOR MAKING METAL A QMLA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 03 611SJ 47564 TAIL ROTOR GEARBOX CHIP LIGHT CAME ON IN-FLIGHT ACCOMPANIED WITH A HIGH PITCH INTERMITTENT SQUEAL. TOOK THREE ATTEMPTS WITH FUZZ BURNER SYSTEM TO EXTINGUISH THE LIGHT. FAILURE OF ONE OF THE INTERNAL BEARINGS OF THE 90 DEGREE GEARBOX. FOU ND CHIP PLUG FULL OF METAL FLAKES. INSTALLED SERVICEABLE T/R GEARBOX, PN 222-042-001-007, S/N AMS-50036, AND T/R HUB AN D BLADES, P/N 222-012-701-107, S/N A235. BLADE, P/N 222-016-001-111, S/N A390 AND A387, T/R DRIVE SHAFT HANGER BEARING ASSY 222-044-003-101, S/N A20-00608. 1 G 7 2 3U H9SW 1996091900982 19960919 00982 SW 1996 9 19 96ZZZX4771 1 19960721 A 7931 INDICATION BELL 222 222 1182122 SW NR 1 ENG OIL MALFUNCTION A QMLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 222LL 47060 NINE MINUTES INTO THE FLIGHT, NR 1 ENGINE OIL PRESSURE READ ZERO (PRESSURE WAS NORMAL PRIOR TO TAKEOFF). NO CAPTION LIG HTS ILLUMINATED AND TEMPERATURE WAS WIT HIN NORMAL OPERATING RANGE. RETURNED TO SUPERIOR AND LANDED. DURING COOL DOWN, OIL PRESSURE SLOWLY RETURNED TO NORMAL RANGE. PROBLEM NEVER RECURRED. SUSPECT LOOSE WIRE POSSIBLY AS A RESULT OF MECH ANIC WIPING DOWN ENGINE DECK EARLIER IN THE DAY. 1 G 7 2 3U H9SW 1996091900983 19960919 00983 SW 1996 9 19 BSAA072696 1 19960726 A 3234 SELECT SWITCH SWRNGN SA226 SA226TC 8780404 SW LANDING GEAR FAILED A BSAA O OTHER O OTHER CL CLIMB 1 NM 05 101GS 36 TC267 LANDING GEAR WAS SELECTED UP AND A SURGING WAS FELT ALONG WITH A LONGER THAN USUAL GEAR INTRANSIT LIGHT. FOUND GEAR UP SELECT SWITCH HAD FAILED. REPLACED GEAR UP SELECT SWITCH, GEAR RETRACTION CHECKED NORMAL. (X) 2 L 7 2 4T RT A8SW 1996091900984 19960919 00984 EU 1996 9 19 SIMA962281 1 19960815 A 3246 5009237 WHEEL 5010488 SAAB SF340 340B 7860101 EU NR 2 MLG FAILED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 380AE DEC930950 340B380 DFW - FLT 3564 - CREW REPORTED NR 2 MAIN TIRE FAILURE. MAINTENANCE FOUND APPROXIMATELY 10 INCH SECTION OF INNER WHEEL H UB RIB MISSING. REPLACED NR 2 WHEEL ASSY AND NR 2 BRAKE ASSY DUE TO MINOR DAMAGE AND NR 1 ASSY AS A PRECAUTION. AIRCRA FT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1996091900985 19960919 00985 EU 1996 9 19 SIMA962241 1 19960811 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU FORWARD CARGO FAILED A SIMA O OTHER N FALSE WARNING CR CRUISE 1 SW 21 391AE A368 340B391 DFW - FLT 3564 - CARGO SMOKE WARNING CAME ON INTERMITTENTLY IN-FLIGHT AND WOULD EXTINGUISH WITHIN 3 SECONDS. REPLACED A FT AND FORWARD CARGO SMOKE DETECTORS, OPS CHECK SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. REFERENCE: OPERATOR C ONTROL NR 96ZZZX4772. (X) 2 L 7 2 4T RT A52EU 1996091900986 19960919 00986 EU 1996 9 19 96ZZZX4772 1 19960811 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU AFT CARGO FAILED A SIMA O OTHER N FALSE WARNING CR CRUISE 1 SW 21 391AE A5077 340B391 DFW - FLT 3564 - CARGO SMOKE WARNING CAME ON INTERMITTENTLY IN-FLIGHT AND WOULD EXTINGUISH WITHIN 3 SECONDS. REPLACED A FT AND FORWARD CARGO SMOKE DETECTORS, OPS CHECK SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. REFERENCE OPERATOR CON TROL NR SIMA962241. 2 L 7 2 4T RT A52EU 1996091900987 19960919 00987 CE 1996 9 19 96ZZZX4773 1 19960607 A 5712 ATTACH RIB BEECH 1900 1900D 1154162 CE RT WING FAILED A MASA K NONE F FLT CONT AFFECTED LD LANDING 1 SW 01 99YV UE99 ON FINAL APPROACH INTO CLB, FLAPS 35 DEGREES WERE SELECTED. FLAPS SPLIT TO ASYMMETRICAL CONDITION AND AILERONS BECAME J AMMED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. UPON INVESTIGATION, RT OUTBOARD FLAP INBOARD UPPER ATTACH BOLT WAS FO UND PULLED THROUGH ATTACH RIB. FLAP WAS REPLACED, AIRCRAFT INSPECTED, AND POSITIONED TO MAINTENANCE FOR FURTHER INSPECT ION. AILERON WAS REPAIRED AND AIRCRAFT RELEASED. 2 L 7 2 4T RT A24CE 1996091900988 19960919 00988 CE 1996 9 19 96ZZZX4774 1 19960608 A 3233 1430846 ACTUATOR 11238002223 BEECH 1900 1900D 1154162 CE NLG FAILED A MASA O OTHER J WARNING INDICATION AP APPROACH 1 SW 01 3YV 443 UE3 AIRCRAFT WAS ON FINAL APPROACH TO PHX WHEN UPON LANDING GEAR EXTENSION, THE PILOTS DELCARED AN EMERGENCY AND MANUALLY EX TENDED GEAR AND LANDED WITH NO FURTHER INCIDENT. AIRCRAFT WAS T/S, AND FERRIED TO IFP WITH GEAR DOWN AND LOCKED. 2 L 7 2 4T RT A24CE 1996091900989 19960919 00989 CE 1996 9 19 96ZZZX4775 1 19960625 A 2730 3094301 SWITCH BEECH 1900 1900D 1154162 CE LT CNTRL WHEEL MALFUNCTIONED A MASA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SW 01 161YV UE161 PILOT ENCOUNTERED UNSCHEDULED NOSE DOWN ATTITUDE IN-FLIGHT. PILOT NOTICED ELEVATOR TRIM WHEEL MOVING WITH NO INPUT GIVE N TO SYSTEM. CREW THEN OPENED ELECTRIC ELEVATOR TRIM CB, CONTINUED FLIGHT WITH NO FURTHER DISCREPANCIES NOTED. MAINTEN ANCE TROUBLESHOT SYSTEM, CONFIRMED THE PILOT'S CONTROL YOKE TRIM SWITCH STICKING. REMOVED AND REPLACED SWITCH, RETURNED TO SERVICE. NOTE: SWITCH IN QUESTION IS A 'SPLIT' SWITCH WHICH IS ACTIVATED WHEN BOTH PARTS ARE MOVED TO PROVIDE THE GROUND AND POWER FOR ACTIVATION. 2 L 7 2 4T RT A24CE 1996091900990 19960919 00990 NM 1996 9 19 96ZZZX4776 1 19960713 A 2910 82960010191 HYD TUBE DHAV DHC8 DHC8202 2809007 NM NR 2 HYD SYST FAILED A MASA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 01 437YV 358 437 DEN/JAC - FLT 7532 - EN ROUTE APPROXIMATELY 40 MILES OUT OF DEN, EXPERIENCED NR 1 HYD SYSTEM PRESSURE AND QUANTITY LOSS. THE CREW THEN DELCARED AN EMERGENCY AND RETURNED TO DEN WITHOUT INCIDENT. MAINTENANCE INSPECTED ACFT AND FOUND A HYD LINE, P/N 82960010191, AT THE NR 2 SPU WHICH HAD CRACKED AT THE FLARE. THE LINE WAS REPLACED BY A TEMPORARY FLEXIBLE LI NE, P/N DSC-252B40124, PER AMM TO BE REPLACED WITHIN 200 FLIGHT CYCLES. THE NR 2 HYD SYSTEM WAS THEN SERVICED AND LEAK CHECKED WITH NO DISCREPANCIES AND THE ACFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1996091900991 19960919 00991 CE 1996 9 19 96ZZZX4777 1 19960726 A 2121 1143800281 VENT BLOWER ELECTROMECH EM630 BEECH 1900 1900D 1154162 CE CABIN FAILED A MASA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 01 165YV 1608 765 UE165 CREW REPORTED A LIGHT HAZE IN CABIN AND FLT DK. RETURNED TO FIELD WITH NO FURTHER DIFFICULTIES. THE LIGHT HAZE DISSAPA TED WHEN CREW DUMPED CABIN. UPON INITIAL INSPECTION, NO INDICATION OF SMOKE OR FLAMES OF ANY KIND WERE FOUND. ALL CIRC UIT BREAKERS WERE SET, ACFT GROUND RUN WITH ALL SYSTEMS CHECKED WITH NO CONDITION REPEATED. ACFT WAS FLOWN TO MAINTENAN CE BASE WITH NO CONDITION REPEATED. UPON FURTHER INSPECTION, AFT VENT BLOWER WAS FOUND INOPERATIVE. REMOVED AND REPLAC ED AFT VENT BLOWER, FOUND RESISTOR ASSY BURNT. RETURNED ACFT TO SERVICE. 2 L 7 2 4T RT A24CE 1996091900992 19960919 00992 NM 1996 9 19 IXKA9600070 1 19960816 A 2131 106120917 CONTROLLER HAMSTD 106120917 BOEING 727 727224 1384076 NM CABIN FAILED A IXKA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 25 32719 80091718 20388 TPA/ATL - FLT 12 - ON CLIMB-OUT, NR 2 A/C PACK TRIPPED. RESET, TRIPPED AGAIN. UNABLE TO MAINTAIN PRESSURIZATION ON LEF T A/C PACK. FOLLOWED ABNORMAL PROCEDURES AND RETURNED TO TPA. REMOVED AND REPLACED FAILED AUTO CONTROLLER AND OPS CHEC K OK PER MM 21-31-0. (X) 2 L 7 3 4F A3WE 1996091900993 19960919 00993 NM 1996 9 19 IXKA9600069 1 19960816 A 8012 CONNECTOR PIN BOEING 727 727225 1384077 NM NR 2 START VALVE BENT A IXKA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 EA 25 354PA 20624 MCO/ATL - FLT 8 - IN-FLIGHT, ENGINE START VALVE NR 2 ILLUMINATED IN-FLIGHT. SHUT DOWN NR 2 ENGINE. LIGHT EXTINGUISHED. FOUND PIN AT NR 2 START VALVE CONNECTOR BENT. STRAIGHTENED PIN, SECURED CONNECTOR, RUN UP AND OPS CHECK OK PER MM 80- 11-11. (X) 2 L 7 3 4F A3WE 1996091900994 19960919 00994 NM 1996 9 19 IXKA9600068 1 19960815 A 2782 1U109592 ACTUATOR SWITCH RONSON BOEING 727 727225 1384077 NM NR 8 L/E FLAP STUCK A IXKA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 25 8882Z 04319 21579 EWR/BDA - FLT 2 - AFTER TAKEOFF DURING FLAP RETRACTION, THE L/E FLAPS LIGHT ON FORWARD PANEL REMAINED ON (AMBER). AS FL AP RETRACTED TO ZERO DEGREES ON SECOND OFFICER'S SLAT POSITION INDICATOR, NR 8 WAS ILLUMINATED AMBER. A/C RETURNED TO E WR. REMOVED AND REPLACED NR 8 L/E SLAT ACTUATOR. OPS CHECK OK PER MM 27-81-32. (X) 2 L 7 3 4F A3WE 1996091900995 19960919 00995 NM 1996 9 19 HNAA9698950 1 19960713 A 2611 7504341 WARN ANNUN PNL DHAV DHC8 DHC8201 2809001 NM COCKPIT FAILED A HNAA K NONE N FALSE WARNING AP APPROACH 1 EA 07 989HA 940 0543 427 TPA/FLL - FLT 3243 - DURING APPROACH INTO FLL, THE SMOKE WARNING LIGHT ILLUMINATED FOR APPROXIMATELY 10 SECONDS. REMOVE D AND REPLACED THE WARNING ANNUNCIATOR PANEL AND BOTH SMOKE DETECTORS. REFERENCE: OPERATOR CONTROL NRS 96ZZZX4778 AND 96ZZZX4779. (X) 2 H 7 2 4T RT A13NM 1996091900996 19960919 00996 NM 1996 9 19 96ZZZX4778 1 19960713 A 2611 302313 SMOKE DETECTOR DHAV DHC8 DHC8201 2809001 NM BAG BAY FAILED A HNAA K NONE N FALSE WARNING AP APPROACH 1 EA 07 989HA 940 0226 427 TPA/FLL - FLT 3243 - DURING APPROACH INTO FLL, THE SMOKE WARNING LIGHT ILLUMINATED FOR APPROXIMATELY 10 SECONDS. REMOVE D AND REPLACED THE WARNING ANNUNCIATOR PANEL AND BOTH SMOKE DETECTORS. REFERENCE: OPERATOR CONTROL NRS HNAA9698950 AN D 96ZZX4779. 2 H 7 2 4T RT A13NM 1996091900997 19960919 00997 NM 1996 9 19 96ZZZX4779 1 19960713 A 2611 302313 SMOKE DETECTOR DHAV DHC8 DHC8201 2809001 NM BAG BAY FAILED A HNAA K NONE N FALSE WARNING AP APPROACH 1 EA 07 989HA 940 0167 427 TPA/FLL - FLT 3243 - DURING APPROACH INTO FLL, THE SMOKE WARNING LIGHT ILLUMINATED FOR APPROXIMATELY 10 SECONDS. REMOVE D AND REPLACED THE WARNING ANNUNCIATOR PANEL AND BOTH SMOKE DETECTORS. REFERENCE: OPERATOR CONTROL NRS HNAA9698950 AND NR 96ZZZX4778. 2 H 7 2 4T RT A13NM 1996091900998 19960919 00998 NM 1996 9 19 HNAA9698949 1 19960712 A 2611 8006221 CONTROL BOX GRIMES DHAV DHC8 DHC8201 2809001 NM E/E BAY FAILED A HNAA K NONE J WARNING INDICATION CR CRUISE 1 EA 07 989HA 936 0259 427 TPA/FLL - FLT 3421 - DURING FLIGHT, THE SMOKE WARNING LIGHT CAME ON. THE LIGHT REMAINED ILLUMINATED FOR 10 MINUTES THEN WENT OUT. LIGHT ILLUMINATED AGAIN SHORTLY BEFORE LANDING. REMOVED AND REPLACED THE WARNING LIGHTS CONTROL BOX. (X) 2 H 7 2 4T RT A13NM 1996091900999 19960919 00999 SO 1996 9 19 96ZZZX4782 1 19960806 A 3800 SE251521021 LAV SERVICE PNL GULSTM G1159 G1159 3953505 SO BS 512-556 MISSING A IMKA O OTHER D INFLIGHT SEPARATION NR NOT REPORTED 1 EA 25 11NZ 846 214 ON 8-6-96 AT APPROXIMATELY 18:36 EST AFTER ARRIVAL AT ANDALUSIA, ALABAMA (K79J), OBSERVED THE AFT LAVATORY SERVICE PANEL WAS MISSING. 2 L 7 2 4F RT A12EA 1996092000001 19960920 00001 WP 1996 9 20 AALA961206 1 19960812 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP NR 2 GALLEY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 137AA 47847 TUL - FOUND CORROSION IN GALLEY SUPPORT BEYOND LIMITS. REPLACED NR 2 GALLEY CENTER SUPPORT WITH NEW PART. (M) 2 L 7 3 4F A22WE 1996092600013 19960926 00013 SW 1996 9 26 ERAA96192 1 19960220 A 6230 412010182101 BEARING BELL 412 412 1182202 SW M/R GR BOX DEFECTIVE A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 167EH 702 33089 BEARING HAS EXCESSIVE RADIAL & AXIAL PLAY. 1 G 7 2 4U H4SW 1996092600014 19960926 00014 GL 1996 9 26 ERAA96193 2 19960221 A 7250 A23038218 NOZZLE 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL 1ST STAGE CRACKED A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 125EH 784 CAT25407 S562 #1 NOZZLE HAS CRACKED VANE TRAILING EDGES. 1 G 7 2 3U 3 U H3EU E4CE 1996092600015 19960926 00015 GL 1996 9 26 ERAA96194 2 19960221 A 7250 A6898764 SEAL 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL NR 5 DAMAGED A ERAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 125EH 691 CAT25407 S562 BELLOWS SEAL HAS CHIPS ON SEAL FACE. 1 G 7 2 3U 3 U H3EU E4CE 1996092600016 19960926 00016 GL 1996 9 26 ERAA96195 2 19960221 A 7250 A6890040 HEAT SHIELD 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL NR 1 CRACKED A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 125EH CAT25407 S562 OUTER BAND OF #1 HEAT SHIELD IS CRACKED. 1 G 7 2 3U 3 U H3EU E4CE 1996092600017 19960926 00017 GL 1996 9 26 ERAA96196 2 19960221 A 7250 6879867 NOZZLE 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL 3RD STAGE CRACKED A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 149EH 425 CAT25376 S705 NOZZLE WAS OVERHAULED ON AVIALL W/O C67134 . NOZZLE HAS CRACKS IN SADDLE AREAS. 1 G 7 2 3U 3 U H3EU E4CE 1996092600018 19960926 00018 GL 1996 9 26 ERAA96197 2 19960222 A 7250 23038218 NOZZLE 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL 1ST STAGE CRACKED A ERAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 149EH 427 CAT25376 S705 NOZZLE WAS OVERHAULED ON DALLAS AIRMOTIVE W/O F1329, HAS 426.7 TSO AND VANES ARE CRACKED & BURNED. 1 G 7 2 3U 3 U H3EU E4CE 1996092600019 19960926 00019 GL 1996 9 26 ERAA96198 2 19960223 A 7250 A68777361 LABYRINTH SEAL 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL TURBINE MIS MFG A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 125EH 784 CAT25407 S562 BEARING BORE OVER MAX DIMENSION. 1 G 7 2 3U 3 U H3EU E4CE 1996092600020 19960926 00020 GL 1996 9 26 ERAA96199 2 19960223 A 7250 A23038218 NOZZLE VANE 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL 1ST STAGE CRACKED A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 126EH 522 CAT25375 S567 NR 1 NOZZLE VANES CRACKED. 1 G 7 2 3U 3 U H3EU E4CE 1996092600021 19960926 00021 GL 1996 9 26 ERAA96200 2 19960226 A 7250 A6890040 HEAT SHIELD 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL NR 1 CRACKED BAND A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 126EH 522 CAT25375 S567 #1 HEAT SHIELD HAS 522.4 HRS ON IT AND HAS A CRACKED OUTER BAND. 1 G 7 2 3U 3 U H3EU E4CE 1996092600022 19960926 00022 SW 1996 9 26 ERAA96201 1 19960226 A 6320 212070116009 INDICATOR BELL 412 412 1182202 SW XMSN OIL DEFECTIVE A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 177EH 33037 NO TEXT 1 G 7 2 4U H4SW 1996092600023 19960926 00023 EU 1996 9 26 ERAA96202 1 19960226 A 6520 4619310070 BEARING 4619002003 BOLKMS 105 BO105S 5626006 EU T/R GR BOX MAKING METAL A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 133EH 17 17 1285 S598 GEARBOX MAKING METAL, OUTER RACE HAS PITS, ROLLERS ARE ROUGH. 1 G 7 2 3U H3EU 1996092600024 19960926 00024 EU 1996 9 26 ERAA96203 1 19960226 A 6520 4619310069 ROLLER BEARING 4619002003 BOLKMS 105 BO105S 5626006 EU T/R GR BOX MAKING METAL A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 133EH 1296 S598 NEW BEARING THAT HAS PITTING ON OUTER RACE, GEARBOX MAKING METAL. 1 G 7 2 3U H3EU 1996092600025 19960926 00025 EU 1996 9 26 ERAA96204 1 19960226 A 6520 4619310072 ROLLER BEARING 4619002003 BOLKMS 105 BO105S 5626006 EU T/R GR BOX MAKING METAL A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 133EH 17 1285 S598 GEARBOX MAKING METAL. INNER RACE HAS DAMAGE THAT CAN BE FELT WITH A PROBE. 1 G 7 2 3U H3EU 1996092600026 19960926 00026 EU 1996 9 26 ERAA96237 1 19960513 A 6310 4638302002 GEAR TOOTH BOLKMS 105 BO105S 5626006 EU ENG/XMSN DRIVE CHIPPED A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 NEW PINIONS RECEIVED WITH TOOTH CHIPPED AND BEARING RACE HAS SCRATCHES THAT CAN BE FELT WITH PROBES. SN 3100 & 3153 1 G 7 2 3U H3EU 1996092600027 19960926 00027 EU 1996 9 26 ERAA96238 1 19960513 A 6720 10545361 CONTROL ROD BOLKMS 105 BO105S 5626006 EU T/R CORRODED A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 TUBE HAS METAL BLISTER ON INSIDE. POSSIBLE CORROSION . 1 G 7 2 3U H3EU 1996092600028 19960926 00028 SW 1996 9 26 ERAA96239 1 19960516 A 6230 212061107011 TUBE BELL 412 412 1182202 SW M/R MIS MFG A ERAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 NEW TUBE . FITTING AND ROD END HAVE INCORRECT FIT. WALL THICKNESS TOO GREAT. 1 G 7 2 4U H4SW 1996092600029 19960926 00029 SW 1996 9 26 ERAA96240 1 19960516 A 6230 412310400107 BEARING BELL 412 412 1182202 SW M/R EXCESS PLAY A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 412EH 531 33001 BEARINGS HAVE EXCESS RADIAL AND AXIAL PLAY. 1 G 7 2 4U H4SW 1996092600030 19960926 00030 GL 1996 9 26 ERAA96242 2 19960517 A 7250 6886407 WHEEL BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL 1ST STAGE BLADE STRETCH A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 135EH 252 S675 WHEEL HAS 252.0 HRS ON IT AND HAS BLADE TIP STRETCH TO 6.197". 1 G 7 2 3U 3 U H3EU E4CE 1996092600031 19960926 00031 GL 1996 9 26 ERAA96244 2 19960610 A 7250 6879879 EXHAUST COLLECTO 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL 4TH NOZZLE MIS REPAIR A ERAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 124EH CAT38452F S559 EXHAUST COLLECTOR SENT FOR OVERHAUL 3-18-96 AND RETURNED WITH 4TH NOZZLE TIGHT FIT INTO COLLECTOR. 1 G 7 2 3U 3 U H3EU E4CE 1996092600032 19960926 00032 GL 1996 9 26 ERAA96245 2 19960611 A 7261 23035102 HOUSING BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL OIL FILTER DEFECTIVE A ERAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 426EH S552 HOUSING WAS O/H AND RECEIVED BACK AT ERA 6-6-96. OIL FILTER HOUSING STAYS IN OIL BY-PASS MODE. 1 G 7 2 3U 3 U H3EU E4CE 1996092600033 19960926 00033 GL 1996 9 26 ERAA96246 2 19960614 A 7250 6888547 SUMP COVER 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL PT SUMP DEFECTIVE A ERAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 124EH CAT36823 S559 PART SENT FOR OVERHAUL AND RETURNED TO ERA 9-18-95. LARGE U-RING SEALING SURFACE NOT TRUE. U-RING WILL NOT CRUSH EVENL Y AND LEAKS. 1 G 7 2 3U 3 U H3EU E4CE 1996092600034 19960926 00034 GL 1996 9 26 ERAA96247 2 19960614 A 7323 2524667 GOVERNOR BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENGINE MALFUNCTION A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 133EH 1921 S598 GOVERNOR CAUSES TORQUE SPLIT 12% ON TAKEOFF AND CRUISE. GOVERNOR WAS OVERHAULED 9-18-96. 1 G 7 2 3U 3 U H3EU E4CE 1996092600035 19960926 00035 SW 1996 9 26 ERAA96248 1 19960618 A 6220 412018056105 LOWER CONE SEAT 412010100139 BELL 412 412 1182202 SW M/R MIS MFG A ERAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 416EH AAD00095M 33011 NEW LOWER CONE SEAT THAT HAS TWO BOLT HOLES THAT ARE NOT THREADED. 1 G 7 2 4U H4SW 1996092600036 19960926 00036 SW 1996 9 26 ERAA96249 1 19960618 A 6230 412310400107 BEARING 412010406115 BELL 412 412 1182202 SW M/R MAST WORN A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 412EH 759 A944 33001 BEARINGS ARE WORN BEYOND LIMITS. 1 G 7 2 4U H4SW 1996092600037 19960926 00037 EU 1996 9 26 ERAA96250 1 19960618 A 6320 4619210902 BEVEL GEAR SET 4619002003 BOLKMS 105 BO105S 5626006 EU GR BOX MAKING METAL A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 427EH 1420 S554 GEARBOX MAKING METAL, GEAR SET HAS HARD WEAR LINE AND NICADING COMING OFF, ALL BEARINGS HAVE BEEN CHANGED TWICE. 1 G 7 2 3U H3EU 1996092600038 19960926 00038 EU 1996 9 26 ERAA96251 1 19960619 A 7120 10560363 STRUT BOLKMS 105 BO105S 5626006 EU ENGINE DAMAGED A ERAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 424EH S548 THIS PART REMOVED FROM SUPPLY FOR A/C N424 BUT COULD NOT BE INSTALLED BECAUSE LOWER STRUT HAS DAMAGE TO LOWER BOLT HOLE S. 1 G 7 2 3U H3EU 1996092600039 19960926 00039 SW 1996 9 26 ERAA96254 1 19960620 A 6220 412010100139 M/R HEAD BELL 412 412 1182202 SW LOWER CONE DEFECTIVE A ERAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 416EH 10302 33011 LOWER CONE SEAT WAS INSTALLED IN AC 416EH AND HAD TO BE REMOVED BECAUSE IT WAS NOT PROPERLY TAPPED & THREADED FOR LOWER CONE HOLES. RETURNED LOWER CONE SEAT PART REF ERA MMIR# ERAA000248. 1 G 7 2 4U H4SW 1996092600040 19960926 00040 GL 1996 9 26 ERAA96256 2 19960621 A 7250 A6875351 U RING GASKET 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENGINE SPLIT A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 297EH 781 CAT40073 S835 U RING GASKET SPLIT. 1 G 7 2 3U 3 U H3EU E4CE 1996092600041 19960926 00041 GL 1996 9 26 ERAA96257 2 19960621 A 7250 A23037413 OUTER SHAFT 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENGINE WORN CURVIC A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 297EH 781 CAT40072 S835 OUTER SHAFT HAS WORN CURVIC. 1 G 7 2 3U 3 U H3EU E4CE 1996092600042 19960926 00042 GL 1996 9 26 ERAA96258 2 19960621 A 7250 A23037413 OUTER SHAFT 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL CURVIC MATERIAL FLAKE A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 296EH 1078 CAT37013 S849 MATERIAL AROUND CURVIC IS FLAKING OFF. 1 G 7 2 3U 3 U H3EU E4CE 1996092600043 19960926 00043 GL 1996 9 26 ERAA96259 2 19960624 A 7250 A6898784 SPLINE ADAPTER 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENGINE COAT FLAKE A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 297EH 781 CAT40072 S835 COATING OF SPLINED ADAPTER IS FLAKING OFF. 1 G 7 2 3U 3 U H3EU E4CE 1996092600044 19960926 00044 GL 1996 9 26 ERAA96260 2 19960624 A 7250 A23038218 NOZZLE 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL 1ST STAGE CRACKED A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 297EH 781 CAT40072 S835 #1 NOZZLE CRACKED. 1 G 7 2 3U 3 U H3EU E4CE 1996092600045 19960926 00045 GL 1996 9 26 ERAA96261 2 19960624 A 7250 A6898784 SPLINE ADAPTER 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENGINE PLATING FLAKE A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 296EH 1078 CAT37013 S849 PLATING FLAKING OFF OF SPLINED ADAPTER. 1 G 7 2 3U 3 U H3EU E4CE 1996092600046 19960926 00046 GL 1996 9 26 ERAA96263 2 19960624 A 7250 A23031938 NOZZLE 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL NR 2 PLUGGED A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 297EH 781 CAT40072 S835 FOUR AIR HOLES ON #2 NOZZLE PLUGGED. 1 G 7 2 3U 3 U H3EU E4CE 1996092600047 19960926 00047 GL 1996 9 26 ERAA96264 2 19960624 A 7323 2524667 GOVERNOR BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENGINE MALFUNCTION A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 134EH S635 GOVERNOR WAS OVERHAULED 7/95 AND HAS 590.1 HRS TSO. GOVERNOR IS SLOW TO REACT. 1 G 7 2 3U 3 U H3EU E4CE 1996092600048 19960926 00048 SO 1996 9 26 RAAA96E8030 1 19960916 A 3350 86210066 BATTERY PACK INTVLV 873100112 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 EGRESS FLOOR PROXIMITY LIGHT PAX ROW 9 FAILED SERVICE CHECK. REPLACED BATTERY PACK DUE TO LOW CHARGE. 2 L 7 4 4T 4A22 1996092600049 19960926 00049 WP 1996 9 26 CALA9601319 1 19960918 A 2910 97608 HYD LINE DOUG DC10 DC1030 3023501 WP NR 1 ENGINE LEAKING A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 12061 47851 THE AIRCRAFT LOST THE NR 1 HYDRAULIC SYSTEM WHILE IN FLIGHT. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT I NCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE LT HYDRAULIC PUMP SUPPLY LINE LEAKING. THE HYDRAULIC SUPPLY LINE WAS REMOVE D AND REPLACED. THE HYDRAULIC SYSTEM WAS SERVICED, THE ENGINE WAS RUN AND NO LEAKS WERE DETECTED. 2 L 7 3 4F A22WE 1996092600050 19960926 00050 WP 1996 9 26 9620149759 1 19960912 A 3150 T/O WARNING DOUG DC9 DC941 302207N WP COCKPIT ACTIVATED A NWAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 01 759NW 47287 RECEIVED TAKEOFF WARNING WHEN POWER ADVANCED FOR TAKEOFF. REPLACED INTERRUPTER, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996092600051 19960926 00051 WP 1996 9 26 9620159880 1 19960913 A 3150 WARNING HORN DOUG DC9 DC951 3022051 WP COCKPIT MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 675MC 47651 UPON ADVANCING THROTTLES FOR TAKEOFF, RECEIVED TAKEOFF WARNING HORN AT ABOUT 20 KTS. RETURNED TO THE GATE. REPLACED TA KEOFF WARNING HORN, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996092600052 19960926 00052 WP 1996 9 26 9620169853 1 19960916 A 3260 PROX SWITCH DOUG DC9 DC951 3022051 WP NLG FAILED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 762NC 47710 AFTER TAKEOFF, NOSE GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. RECYCLED GEAR, LIGHT REMAINED ON, INDICATION N ORMAL WITH GEAR DOWN. FLIGHT CONTINUED TO ORD AND LANDED WITHOUT INCIDENT. FOUND NOSE GEAR DOWNLOCK PROXIMITY SWITCH W ITH DELAMINATED FACE. REPLACED SWITCH PROXIMITY SENSOR, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996092600053 19960926 00053 WP 1996 9 26 9620179970 1 19960918 A 3350 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9334 47247 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY FLASHLIGHT ABOVE FORWARD FLIGHT ATTENDANT INOPERATIVE. REPLACED BAT TERY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996092600054 19960926 00054 SO 1996 9 26 COMA9610278 1 19960916 A 7722 3035061 THERMOCPL RING EMB 120 EMB120RT SO RT ENGINE BROKEN A COMA K NONE O OTHER CR CRUISE 1 SO 01 243CA 120212 DURING CRUISE FLIGHT, THE LEFT ENGINE T6 INDICATED 675 DEGREES AND THE RIGHT ENGINE T6 INDICATED 548 DEGREES. REPLACED BROKEN T6 THERMOCOUPLE RING ON RT ENGINE. 2 L 7 2 4T RT A31SO 1996092600055 19960926 00055 SO 1996 9 26 COMA9610279 1 19960914 A 3260 INDICATION EMB 120 EMB120RT SO LANG ING GEAR MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 244CA 120217 WHEN LANDING GEAR SELECTED TO RETRACT, BOTH THE GREEN DOWN AND RED INTRANSIT LIGHTS WERE ON. COULD NOT DUPLICATE DISCRE PANCY. OPERATIONAL AND FUNCTIONAL CHECKS OF LANDING GEAR RETRACTION SYSTEM WERE NORMAL. 2 L 7 2 4T RT A31SO 1996092600056 19960926 00056 WP 1996 9 26 COMA9620016 2 19960917 A 7313 3103235 FUEL NOZZLES SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP LT ENGINE MALFUNCTIONED A COMA K NONE O OTHER TO TAKEOFF 1 SO 01 702M 400 AC702 44588 LEFT ENGINE DOES NOT ACHIEVE REQUIRED TORQUE FOR TAKEOFF. REPLACED THE ENGINE FUEL NOZZLES. 2 L 7 2 4T 4 T RT A8SW E4WE 1996092600057 19960926 00057 EU 1996 9 26 COMA9630144 1 19960917 A 2730 DL3827M157 ACTUATOR SAAB SF340 SF340A 7850100 EU RT ELEVATOR MALFUNCTIONED A COMA K NONE F FLT CONT AFFECTED UK UNKNOWN 1 SO 01 358CA 12763 277 340A047 THE STANDBY PITCH TRIM OPERATES WHEN ONLY HALF OF THE TRIM SWITCH IS ACTIVATED. REPLACED THE PITCH TRIM ACTUATOR. 2 L 7 2 4T RT A52EU 1996092600058 19960926 00058 EU 1996 9 26 COMA9630145 1 19960912 A 2751 522858 FLAP INDICATOR SAAB SF340 SF340A 7850100 EU TE FLAPS MALFUNCTIONED A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 359CA 17679 793 340A053 WHEN FLAPS SELECTED TO 20 DEGREES, THEY INDICATE 18 DEGREES. REPLACED THE FLAP INDICATOR. 2 L 7 2 4T RT A52EU 1996092600059 19960926 00059 NE 1996 9 26 COMA9660142 2 19960914 A 7530 WIRE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE ISOLATION VLV CHAFED A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 966CA 60 7132 THE 14TH STAGE BLEED AIR ISOLATION VALVE WILL NOT CLOSE. REPAIRED CHAFED WIRE AT WIRING CONNECTOR. 2 L 7 2 4F 4 F RT A21EA E15NE 1996092600060 19960926 00060 EA 1996 9 26 COMA9660143 1 19960916 A 3010 434419882 HEAT SENSOR CNDAIR CL600 CL6002B19 EA RT WING MALFUNCTION A COMA K NONE O OTHER CR CRUISE 1 SO 01 959CA 855 7116 DURING FLIGHT IN ICING CONDITIONS, WING OVERHEAT MESSAGE ON EICAS. REPLACED DEFECTIVE WING HEAT SENSOR. 2 L 7 2 4F RT A21EA 1996092600061 19960926 00061 1996 9 26 COMA9660144 4 19960917 A 3417 8220372115 ADC CNDAIR CL600 CL6002B19 EA NR 1 FAILED A COMA K NONE J WARNING INDICATION UK UNKNOWN 1 SO 01 929CA 4651 2123 7035 PILOTS ALTIMETER AND VERTICAL SPEED INDICATORS FAILED. REPLACED THE NR 1 AIR DATA COMPUTER. 2 L 7 2 4F RT A21EA 1996092600062 19960926 00062 1996 9 26 COMA9660145 4 19960918 A 2210 6229968001 YAW DAMPER CNDAIR CL600 CL6002B19 EA NR 1 FAILED A COMA K NONE F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 01 912CA 4918 568 7011 THE NR 1 YAW DAMPER FAILED. REPLACED THE NR 1 YAW DAMPER. 2 L 7 2 4F RT A21EA 1996092600063 19960926 00063 EA 1996 9 26 COMA9660146 1 19960917 A 3210 NAS620870D BOLT CNDAIR CL600 CL6002B19 EA LT MLG BROKEN A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 933CA 6063 7040 AFTER TAKEOFF, LANDING GEAR RETRACT LEVER COULD NOT BE SELECTED UP. OVERRIDE WAS USED, NLG RETRACTED BUT MLG REMAINED D OWN. THE LT MLG TRAILING ARM HINGE PIN BOLT WAS BROKEN ALLOWING THE HINGE PIN TO ROTATE AND GIVE FALSE SIGNAL TO WOW SW ITCHES. REPLACED BOLT. 2 L 7 2 4F RT A21EA 1996092600064 19960926 00064 NM 1996 9 26 SWAA960977 1 19960916 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 326SW 23690 DURING SCHEDULED A-CHECK, FOUND STRINGER 18A AT BS 727 CRACKED ON LEFT AND RIGHT SIDES. REPAIRED PER SWA ACO 6580-53. 2 L 7 2 4F RT A16WE 1996092600065 19960926 00065 NM 1996 9 26 SWAA960978 1 19960917 A 5320 CEILING BOEING 737 7372H4 138448C NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 24SW 20925 DURING SCHEDULED C1 CHECK, FOUND A 4.5 CRACK IN NOSE WHEEL WELL CEILING RIGHT SIDE JUST AFT OF MANUAL GEAR EXTENSION RET URN SPRING BRACKET. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996092600066 19960926 00066 NM 1996 9 26 SWAA960979 1 19960917 A 5330 SKIN BOEING 737 7372H4 138448C NM PAX DOOR CUTOUT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 24SW 20925 DURING SCHEDULED C1 CHECK, FOUND A 1 INCH CRACK IN FUSELAGE SKIN AT FWD ENTRY DOOR CUTOUT UPPER FWD CORNER. REPAIRED PE R SWA ACO 6317-53. 2 L 7 2 4F A16WE 1996092600067 19960926 00067 NM 1996 9 26 SWAA960980 1 19960917 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 312 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 24SW 20925 DURING SCHEDULED C1 CHECK, FOUND FLOORBEAM T-CAP AT BS 312 CRACKED ABOVE FWD UPPER AIRSTAIR DOOR STOP AT LWR RADIUS. RE PAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996092600068 19960926 00068 NM 1996 9 26 SWAA960981 1 19960918 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 767 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 62SW 22060 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED 3 INCHES AT BS 767, S17R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996092600069 19960926 00069 NM 1996 9 26 SWAA960982 1 19960918 A 3350 900835A BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 67SW 22356 DURING SCHEDULED TERMINAL CHECK, FOUND FWD AND AFT EMERGENCY EXIT LIGHTS INOP. REPLACED FWD AND AFT BATTERY PACKS PER B OEING M/M. 2 L 7 2 4F A16WE 1996092600070 19960926 00070 NM 1996 9 26 SWAA960983 1 19960918 A 3350 10147440001 LIGHT BOEING 737 7372H4 138448C NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 89SW 22904 DURING SCHEDULED RON CHECK, FOUND EMERGENCY EXIT LIGHT OVER FWD SERVICE DOOR UNSECURED. REPLACED LIGHT ASSEMBLY PER BOE ING M/M. 2 L 7 2 4F A16WE 1996092600071 19960926 00071 NM 1996 9 26 SWAA960984 1 19960918 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 90SW 22905 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 344, LBL 18 AND 14. REPLACED T-CAPS PER BOEING SRM. 2 L 7 2 4F A16WE 1996092600072 19960926 00072 NM 1996 9 26 SWAA960985 1 19960918 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 294 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 90SW 22905 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 294, BS 0, RBL 26.5 AND RBL 8. REPLACED T-CAPS PER BOEING SRM. 2 L 7 2 4F A16WE 1996092600073 19960926 00073 NM 1996 9 26 SWAA960986 1 19960918 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 90SW 22905 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 344, LBL 29, 33, 35, 49 AND 43. REPLACED T-CAPS PER BOEIN G SRM. 2 L 7 2 4F A16WE 1996092600074 19960926 00074 NM 1996 9 26 SWAA960987 1 19960918 A 5312 BULKHEAD SKIN BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED D-CHECK, FOUND FUSELAGE BULKHEAD SKIN CRACK INDICATION AT BS 178, WL 195. REPLACED DAMAGED SECTION OF SIDE CHORD AND SPLICED IN NEW PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996092600075 19960926 00075 NM 1996 9 26 SWAA960988 1 19960918 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 388 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 388, S21L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996092600076 19960926 00076 NM 1996 9 26 SWAA960989 1 19960918 A 5230 SKIN BOEING 737 7373H4 1384600 NM AFT CARGO DOOR DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 392SW 27379 DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR SKIN CREASED AND OIL CANNING. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996092600077 19960926 00077 NM 1996 9 26 SWAA960990 1 19960918 A 5320 WEB BOEING 737 7373Q8 1384670 NM BS 793 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED D-CHECK, FOUND WEB CRACKED FORWARD OF AFT CARGO DOOR CUTOUT AT BS 793, RBL 30, WL 161. REPAIRED PER B OEING SRM. 2 L 7 2 4F RT A16WE 1996092600078 19960926 00078 NM 1996 9 26 SWAA960991 1 19960918 A 5330 SKIN BOEING 737 7373Q8 1384670 NM BS 494 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 494, S18R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996092600079 19960926 00079 NM 1996 9 26 SWAA960992 1 19960918 A 3350 LIGHT BOEING 737 7375H4 138449D NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 511SW 24188 DURING SCHEDULED C2 CHECK, FOUND CABIN UPPER EMERGENCY FLASHLIGHT NOT TESTING. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996092600080 19960926 00080 NM 1996 9 26 UPS96421123 1 19960902 A 5320 STIFFENER BOEING 747 747121 1384871 NM BS 1860 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE-C, AFT CARGO COMP FOUND FRAME STIFFENER BENT AND CRACKED AT BS 1860, S41 LT. REPLACED FRAME STIFFENER A CC SRM 51-30-02. 2 L 7 4 4F A20WE 1996092600081 19960926 00081 NM 1996 9 26 UPS96421124 1 19960828 A 5320 INTERCOSTAL BOEING 747 747121 1384871 NM BS2000/2020 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE-C, BULK CARGO COMP FOUND THRESHOLD SUPPORT INTERCOSTAL CRACKED AT BS 2000 AND 2020 RBL 53. REPLACED THR ESHOLD SUPPORT INTERCOSTAL ACC SRM 51-30-02. 2 L 7 4 4F A20WE 1996092600082 19960926 00082 NM 1996 9 26 UPS96421125 1 19960829 A 5311 FRAME BOEING 747 747121 1384871 NM BS 1520 S29 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE-C, AFT CARGO COMP FOUND CRACK IN FRAME INNER FLANGE AT BS 1520 S29 RT. REMOVED DAMAGED SECTION OF FRAME INNER FLANGE AND REPAIRED FRAME INNER FLANGE ACC SRM 51-40-03 FIG 1. 2 L 7 4 4F A20WE 1996092600083 19960926 00083 NM 1996 9 26 UPS96421126 1 19960830 A 5313 STRINGR BOEING 747 747121 1384871 NM BS 1650 S32 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE-C, AFT CARGO COMP FOUND CRACK IN STRINGER FLANGE AT S32 LT BS 1650. REMOVED DAMAGED SECTION OF STRINGER FLANGE AND REPAIRED STRINGER FLANGE ACC TO SRM 53-10-03 FIG 2. 2 L 7 4 4F A20WE 1996092600084 19960926 00084 NM 1996 9 26 UPS96421127 1 19960829 A 5320 SHEAR TIE BOEING 747 747121 1384871 NM BS 1520 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE-C, AFT CARGO COMP FOUND CRACK IN FRAME SHEAR TIE AT STRINGER CUTOUT CORNER BS 1520, S27 RT. STOP DRILLE D CRACK AND REPAIRED FRAME SHEAR TIE AT STRINGER CUTOUT CORNER ACC SRM 53-10-04 FIG 39. 2 L 7 4 4F A20WE 1996092600085 19960926 00085 WP 1996 9 26 UPS96821128 1 19960828 A 5313 56493268 LONGERON DOUG DC8 DC873F 302199F WP BS 1740 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE CS2, LONGERON 5R CRACKED AT THE VERTICAL STAB FS 1740. REPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996092600086 19960926 00086 WP 1996 9 26 UPS96821129 1 19960827 A 5511 565208612 SPAR WEB DOUG DC8 DC873F 302199F WP RT HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE CS2, RT HORIZONTAL STAB CLOSING REAR SPAR WEB HAS CRACKED HOLE AT STA XE 142. REPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996092600087 19960926 00087 1996 9 26 96UAL900690 4 19960909 A 2310 HF TR UNIT COLLINS 6225272 BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE E/E COMPT DAMAGED A UALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 WP 29 549UA 25397 TUNING RIGHT HIGH FREQ SYSTEM CAUSES ERRATIC AUTOPILOT AND FALSE RIGHT AFT EMERGENCY DOOR OPEN EICAS MESSAGE. REPLACED RIGHT HIGH FREQ TRANSCEIVER, OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996092600088 19960926 00088 NE 1996 9 26 96UAL900691 2 19960910 A 7260 697063 BEARING BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE RT GEARBOX FAILED A UALA A E UNSCHED LANDING ENGINE SHUTDOWN Y ENGINE STOPPAGE CR CRUISE 1 WP 29 614UA 11501 21875 707515 DIVERTED TO DTW UNDER AMBER ALERT WITH RIGHT ENGINE SHUT-DOWN DUE TO LOW OIL PRESSURE AND QUANTITY. THE NR 3 AND NR 4 S CAVENGE PUMP DRIVE IDLER GEAR BEARING FAILED. THE MAIN GEARBOX ASSEMBLY WAS REPLACED AND DISASSEMBLED FOR OVERHAUL. THI S BEARING WILL BECOME A ONE TIME USE ITEM. 2 L 7 2 4F 4 F RT A1NM E3NE 1996092600089 19960926 00089 1996 9 26 96UAL900692 4 19960914 A 2297 W32300622 WIRE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE VERT STAB OPEN A UALA K NONE F FLT CONT AFFECTED CL CLIMB 1 WP 29 7461U 21915 ON CLIMB-OUT 12-15 DEGREES NOSE UP AND 220 KNOTS, GOT A HARD KICK TO THE RIGHT (ABOUT SIX DEGREE HEADING CHANGE). RUDDE R POSITION INDICATORS SPLIT, CREW REPORTED LOWER RUDDER TO THE RIGHT. AIRCRAFT HAD PREVIOUS REPORTS OF YAW DAMPER PROBL EMS. FOUND W323-006-22 OPEN AT SM 1. REPAIRED OPEN WIRE AND ACCOMPLISHED YAW DAMPER COUPLER TEST. 2 L 7 3 4F 4 F A3WE E2EA 1996092600090 19960926 00090 NM 1996 9 26 96UAL900693 1 19960910 A 3230 273N10051 LOCK ACTUATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NLG MALFUNCTIONED A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 504UA 24625 NOSE LANDING GEAR DID NOT EXTEND. RECYCLED GEAR, WOULD NOT EXTEND. A SHORT TIME LATER GEAR EXTENDED. ACCOMPLISHED BOE ING SERVICE BULLETIN 757-32-0113 TO CORRECT PROBLEM. OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996092600091 19960926 00091 1996 9 26 96UAL900695 4 19960913 A 2210 4030952902 COUPLER BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE RUDDER MALFUNCTIONED A UALA A UNSCHED LANDING F FLT CONT AFFECTED TO TAKEOFF 1 WP 29 9063U 19944 CREW REPORTS UNCOMMANDED YAW DAMPER KICK ON TAKEOFF AT V-1. *S/D* AIRCRAFT SYSTEMS WERE TESTED AND FUEL LOAD CHECKED. COULD NOT FIND ANYTHING THAT FAILED. YAW DAMPER COUPLER WAS REPLACED PRECAUTIONARY. SHOP COULD NOT FIND ANYTHING WRON G. 2 L 7 2 4F 4 F A16WE E2EA 1996092600092 19960926 00092 NM 1996 9 26 96UAL900696 1 19960913 A 2613 355644310 OVERHEAT SENSOR BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE WING INOPERATIVE A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 913UA 25291 RIGHT WING OVERHEAT LIGHT CAME ON AFTER TAKEOFF. ACCOMPLISHED PROCEDURE AND LIGHT WENT OUT AFTER TWO MINUTES. APPEARS TO COINCIDE WITH HIGH POWER SETTINGS. REPLACED RIGHT WING LEADING EDGE CAVITY OVERHEAT DETECTOR SENSOR. CHECKS O.K. 2 L 7 2 4F 4 F RT A16WE E2GL 1996092600093 19960926 00093 NM 1996 9 26 96UAL900697 1 19960913 A 2752 2061141 INDICATOR BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE COCKPIT INOPERATIVE A UALA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 990UA 21980 FLAPS WOULD NOT EXTEND DURING APPROACH,TRIED MULTIPLE TIMES AND THEY FINALLY EXTENDED AFTER THE SIXTH TRY. AFTER LANDIN G FLAPS WOULD NOT RETRACT. *S/D* REPLACED TRAILING EDGE FLAP POSITION INDICATOR, CHECKED OK. 2 L 7 2 4F 4 F A16WE E2EA 1996092600094 19960926 00094 NM 1996 9 26 96UAL900699 1 19960914 A 3350 BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7457U 21911 AIRSTAIR EMERGENCY EXIT LIGHT INOPERATIVE BATTERIES EXPIRED. REPLACED BATTERIES. 2 L 7 3 4F 4 F A3WE E2EA 1996092600095 19960926 00095 NE 1996 9 26 96UAL900700 2 19960914 A 7310 FUEL SO VALVE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE MALFUNCTIONED A UALA O OTHER X ENGINE FLAMEOUT NR NOT REPORTED 1 WP 29 7256U 21403 700247 DURING START, NR 1 ENGINE STABILIZED MOMENTARILY, THEN SHUT DOWN/FLAMED OUT. FUEL FLOW RANGED BETWEEN 800 AND 1,200 THE N WENT TO ZERO. *S/D* REPLACED FUEL SHUT OFF VALVE, RAN ENGINE AT POWER AND CHECKED GOOD IN ALL PARAMETERS. 2 L 7 3 4F 4 F A3WE E2EA 1996092600096 19960926 00096 NM 1996 9 26 96UAL900701 1 19960914 A 2612 91180 SOCKET BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7256U 21403 NR 1 ENGINE FIRE LOOP WILL NOT TEST. REPAIRED SHORT IN LIGHT SOCKET. REPLACED OPERATING POWER UNIT AS PRECAUTIONARY ME ASURE. 2 L 7 3 4F 4 F A3WE E2EA 1996092600097 19960926 00097 NM 1996 9 26 96UAL900702 1 19960914 A 2820 69186127 VENT TUBE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 FUEL TANK CRACKED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 7443U 21897 AFTER CLIMBING TO FL 310, NR 1 FUEL TANK QUANTITY WENT DOWN 600 POUNDS, WHEN ALL ENGINES SUPPLIED FROM NR 2 TANK WITH AL L CROSS-FEEDS OPEN. NR 1 FUEL TANK VENT TUBE ELBOW CRACKED AT THE WELD AREA. REPAIRED AND REINSTALLED VENT TUBE ELBOW . 2 L 7 3 4F 4 F A3WE E2EA 1996092600098 19960926 00098 GL 1996 9 26 96UAL900703 2 19960914 A 7250 9198M38GO7 TURBINE BLADE DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 2 ENGINE BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 1838U 46632 NR 2 ENGINE SECOND STAGE HIGH PRESSURE TURBINE BLADE DAMAGED BEYOND LIMITS. *S/D* ONE HPT 2ND STAGE BLADE WAS SEPARATE D ALONG A LINE PARALLEL TO THE BLADE CHORD AND APPROXIMATELY 1.5 INCHES OUTBOARD OF THE BLADE PLATFORM. PRIME CAUSE OF FAILURE WAS INTERNAL OXIDATION RESULTING IN FATIGUE FAILURE. 2 L 7 3 4F 4 F A22WE E23EA 1996092600099 19960926 00099 NM 1996 9 26 96UAL900704 1 19960914 A 2730 COMPUTER 4016027215 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE ELEVATOR FEEL FAILED A UALA O OTHER F FLT CONT AFFECTED TO TAKEOFF 1 WP 29 7252U 21399 ON ROTATION, HEAVY CONTROL FORCES FOR TAKEOFF (ADDITIONAL 3-4 UNITS OF TRIM). FORCES ESPECIALLY HEAVY WITH FLAP EXTENSI ON. REPLACED ELEVATOR FEEL COMPUTER. SUBSEQUENT OPERATION NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1996092600100 19960926 00100 NM 1996 9 26 96UAL900705 1 19960914 A 2913 OVER HEAT LIGHT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE B-HYD SYST ILLUMINATED A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 7459U 21913 B HYDRAULIC SYSTEM OVERHEAT LIGHT ON DURING CLIMB. OVERHEAT LIGHT OFF WITH NO. 2 ELECTRIC PUMP OFF. 2 L 7 3 4F 4 F A3WE E2EA 1996092600101 19960926 00101 NM 1996 9 26 96UAL900706 1 19960914 A 2820 69186127 VENT TUBE ELBOW BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 FUEL TANK BROKEN A UALA O OTHER K FLUID LOSS CR CRUISE 1 WP 29 7456U 21910 NR 1 FUEL TANK 300 POUNDS BELOW RIGHT WING WHILE FEEDING ALL ENGINES FROM NR 2 FUEL TANK. REPLACED BROKEN NR 1 FUEL TAN K VENT TUBE ELBOW. 2 L 7 3 4F 4 F A3WE E2EA 1996092600102 19960926 00102 1996 9 26 96UAL900707 4 19960914 A 2211 4030951901 ROLL COMPUTER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE AUTO PILOT FAILED A UALA O OTHER F FLT CONT AFFECTED CR CRUISE 1 WP 29 7454U 21908 UPON ENGAGEMENT OF THE AILERON CHANNEL OF THE AUTOPILOT IN MODE (A), HARD UNCOMMANDED ROLL TO RIGHT OCCURS. MODE (B) SA ME BUT AT REDUCED RATE AND CORRECTS ITSELF. REPLACED ROLL COMPUTER AND NR 1 DIRECTIONAL GYRO AND TESTED SYSTEM. 2 L 7 3 4F 4 F A3WE E2EA 1996092600103 19960926 00103 NM 1996 9 26 96UAL900708 1 19960914 A 2730 PITCH TRIM BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE ELEVATOR MALFUNCTIONED A UALA K NONE F FLT CONT AFFECTED NR NOT REPORTED 1 WP 29 7253U 21400 AT SLOW SPEED, PITCH TRIM TRIMS NOSE DOWN WHEN NOSE UP ACTUATED. AT HIGH SPEED, TRIM CONTINUES TO TRIM NOSE DOWN WHEN S WITCH RELEASED. 2 L 7 3 4F 4 F A3WE E2EA 1996092600104 19960926 00104 1996 9 26 96UAL900709 4 19960914 A 2565 SLIDE AIR CRUISERS D29835103 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE INFLATE TUBE SEPARATED A UALA K NONE L NO TEST UK UNKNOWN 1 WP 29 7280U 179241078 21558 DURING TIME CONTROLLED OVERHAUL, SLIDE FAILED DUE TO SEAM SEPARATION OF THE INFLATION TUBE. *S/D* UNIT SCRAPPED. 2 L 7 3 4F 4 F A3WE E2EA 1996092600105 19960926 00105 WP 1996 9 26 MWEA96525 1 19960918 A 2420 CONTL PANEL DOUG DC9 DC914 3022034 WP E/E COMPT INOPERATIVE A MWEA O OTHER H ELECT. POWER LOSS-50 PC CL CLIMB 1 GL 31 700ME 45696 PILOT REPORTS LH GENERATOR OFF LIGHT ILLUMINATED ON CLIMB. STARTED APU PER QRH PROCEDURES, AC CROSSTIE LOCKOUT & ACBUSS OFF LIGHTS ILLUMINATE. PLACED BUSS SWITCH BACK TO OFF POSITION. ALL BUSSES POWERED AGAIN. -- REPLACED AC CROSSTIE R ELAY AND AC GENERATOR CONTROL PANEL FOR APU. OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996092600106 19960926 00106 WP 1996 9 26 DLL10962093 1 19960910 A 3350 LIGHT LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1734D 193C1225 3R EXTERIOR EMER EXIT LGT INOP. RELAMPED. CKS OK 2 L 7 3 4F A23WE 1996092600107 19960926 00107 WP 1996 9 26 DLL12962098 1 19960911 A 2612 FIRE CONTL UNIT LKHEED 1011 1011385115 5265015 WP NR 2 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 724DA 39135 14608 193C1151 14608 #2 ENGINE FIRE INDICATION IN FLIGHT ENGINE AND SEVERE DAMAGE SHUTDOWN PERFORMED _REPAIRED CHAFED WIRE ON A LOOP NE AR CONN. P700. REPLACED NO.2 ENG FIRE DETECT CONTROL UNIT FOR B LOOP. ALL CKS OK ON ENG RUN. 2 L 7 3 4F A23WE 1996092600108 19960926 00108 NM 1996 9 26 DL72S962101 1 19960911 A 3350 BATTERY PACK 900835A BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 406DA VA6168 21150 RT AFT SLIDE EMERG LITE INOP C/A RPLD BATT PACK AT RACK M957 OPS CHKS GOOD 2 L 7 3 4F A3WE 1996092600109 19960926 00109 NM 1996 9 26 DL72W962103 1 19960912 A 2121 GASPER FAN 215201 BOEING 727 727247 138408F NM CABIN FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 2812W AA77783 20868 STRONG BURNING SMELL IN COCKPIT REPLACED GASPER FAN. OPERATIONAL CHECKS GOOD. 2 L 7 3 4F A3WE 1996092600110 19960926 00110 NE 1996 9 26 DL757962104 2 19960912 A 7200 ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 FAILED A DALA E ENGINE SHUTDOWN Y ENGINE STOPPAGE CL CLIMB 1 SO 27 657DL 31657 24419 716391 JUST BEFORE A/C REACHED CRUIS NO. 2 ENG LOST OIL PRESS. THE ENG PLACED AT IDLE . THE ENG SHUT ITSELF OFF BEFORE THE P ILOT COULD TURN OFF THE FUEL CONTROL. FOUND METAL IN OIL SCREEN. FOUND THE ENG LOCKED UP. 2 L 7 2 4F 4 F RT A2NM E17NE 1996092600111 19960926 00111 NM 1996 9 26 DL72K962105 1 19960912 A 3350 BATTERY PACK 6104789 BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 472DA 20749 LT AND RT FWD EMERGENCY SLIDE ILLUM LIGHTS INOP. REPLACED BATT PACK-CKS NML. 2 L 7 3 4F A3WE 1996092600112 19960926 00112 NM 1996 9 26 DL757962106 1 19960912 A 5330 SKIN BOEING 757 757232 1384965 NM RT WING CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 626DL 22916 DURING INSPECTION, THE FUSELAGE SKIN WAS FOUND CORRODED AT THE RH FWD OVERWING EXIT DOOR, ON THE INNER SIDE, IN THE 'CUB STRAP' FROM APPROX. THE CENTER OF THE HATCH OPENING AND FWD. THE CORROSION WAS BLENDED IN ACCORDANCE WITH BACO TELEX D AL-ATL-96-1418RR DATED 11 SEP 96. 2 L 7 2 4F RT A2NM 1996092600113 19960926 00113 NM 1996 9 26 DL72W962109 1 19960914 A 3350 S106 BATTERY BOEING 727 727247 138408F NM AFT AIRSTAIR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2810W 20648 FOUND AFT AIRSTAIR_EMERGENCY EXIT LIGHTS AND LIGHT BELOW FLIGHT ATTENDANT PANEL INOP. REPLACED BATTERIES, RELAMPED, R EPLACED EMERG. LIGHT ASSY AND RESECURED WIRES TO THE LIGHT ASSY BELOW FLT ATT PNL. 2 L 7 3 4F A3WE 1996092600114 19960926 00114 WP 1996 9 26 DLL10962110 1 19960915 A 3350 BATTERY PACK 5165741 LKHEED 1011 10113851 5265010 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 729DA 62829 193C1180 MID GALLEY EMERGENCY LITE INOP. REPLACED BATTERY PACK OPERATES NORMAL. 2 L 7 3 4F A23WE 1996092600115 19960926 00115 1996 9 26 DL767962113 4 19960915 A 3442 TR UNIT 20412170416 BOEING 767 767232 1385132 NM RADAR COMPT FAILED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 109DL 2759 22221 RADAR FAILED IN FLIGHT. R/T FAULT DISPLAYED. REPLACED TRANSCVR. OPS. CHECK NORMAL. 2 L 7 2 4F RT A1NM 1996092600116 19960926 00116 NM 1996 9 26 DL73S962117 1 19960906 A 5312 BULKHEAD WEB BOEING 737 737232 1384475 NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 308DL 23080 DURING INSPECTION, 2 CRACKS WERE DISCOVERED IN THE FWD. FACEOF THE STA. 178 BULKHEAD WEB. FIRST CRACK CUTOUT MEASURES 1 1/8 X 1 AND IS LOCATED AT RBL 5.7 VERTICAL STRAP AT_WL 198. THE SECOND CRACK CUTOUT MEASURES 1.5 X 1 LOCATED_AT THE LB L 5.7 VERTICAL STRAP ALSO AT WL 198. IN ACCORDANCE WITH 8110-3 FORM SIGNED BY DER SO-867 DATED SEPT. 6, 1996, THE CR ACKS WERE TRIMMED OUT AND A DOUBLER WAS INSTALLED. 2 L 7 2 4F RT A16WE 1996092600117 19960926 00117 NM 1996 9 26 DL72S962119 1 19960912 A 5320 65184201046 POST BOEING 727 727232 1384082 NM COCKPIT WINDOW CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 402DA 21146 FOUND CRACK AT THE INBOARD LOWER CORNER OF THE L4 COCKPIT WINDOW. REPAIRED IN ACCORDANCE WITH DER FORM 8110-3, DER DES IGNATIONSO-831, DATED 9/12/96. 2 L 7 3 4F A3WE 1996092600118 19960926 00118 NM 1996 9 26 DL76S962120 1 19960916 A 2910 HYD LINE AE70577778 BOEING 767 767332 1382001 NM NR 1 ENGINE CHAFED A DALA K NONE K FLUID LOSS AP APPROACH 1 SO 27 119DL 23278 L HYD QTY EICAS MSG. LT ENG HYD QTY 0.46 RF. LT ENG PRIMARY AND DEMAND PUMPS OFF. REPLACED HYDRAULIC LINE AT #1 ENGINE H YDRAULIC PUMP. SYSTEM CHECKS NORMAL. 2 L 7 2 4F RT A1NM 1996092600119 19960926 00119 WP 1996 9 26 RRXA96087 1 19960919 A 5330 SKIN DOUG DC8 DC873 302199C WP BS 25-33 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 105WP 46095 KMCN - DURING MAINTENANCE VISIT, FOUND CORROSION CRACK IN FUSELAGE SKIN AT Y=23 TO Y=55 BETWEEN LONGERONS 33R AND 34R. R EMOVED DAMAGED AREA. FABRICATED FILLERS, DOUBLERS, AND INSTALLED REPAIR IAW DER APPROVED COTNEY ENGINEERING SKETCH B31- R01. ACFT TT: 61,420 HOURS. ACFT TOTAL CYCLES, 19,753. (X) 2 L 7 4 4F RT 4A25 1996092600132 19960926 00132 CE 1996 9 26 96ZZZX4795 1 19960820 A 2910 3A0900009 LINE WIPLINEINC CESSNA 206 TU206G 2073357 CE LT FLOAT FAILED A FVAA K NONE O OTHER IN INSP/MAINT 1 NE 03 9624R U20606907 HYDRAULIC HARDLINE FAILED ON LT FLOAT ROUTED BETWEEN NR 3 BULKHEAD AND NOSE GEAR RETRACTOR. UPON INVESTIGATION, VISUAL INSPECTION OF FAILED HYDRAULIC LINE INDICATED SIGNS OF TOOL MARKS FROM MFG PROCESS ABOUT THE FLARED PORTION OF THE LINE THAT HAD APPARENTLY MIGRATED AND LED TO FAILURE. EXISTING LINES SHOULD BE EVALUATED AND NEW LINES INSPECTED FOR SIMILAR DEFECTS PRIOR TO INSTALLATION. 1 H 7 1 3O A4CE 1996092600170 19960926 00170 WP 1996 9 26 9620189856 1 19960917 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 765NC 47718 DURING LINE CHECK, FOUND BOTH CATWALK EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996092600171 19960926 00171 WP 1996 9 26 9620199878 1 19960918 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 787NC 48149 DURING LINE CHECK, FOUND CEILING EMERGENCY LIGHTS OUT AT ROW 20 TO 24. REPLACED POWER SUPPLY AND BATTERIES, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996092600172 19960926 00172 WP 1996 9 26 9620209976 1 19960919 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9340 47389 DURING LINE MAINTENANCE INSPECTION, FOUND AFT STAIRWELL EMERGENCY LIGHTS DIM. SECURED LOOSE GROUND WIRE, OPERATIONAL CH ECK NORMAL. 2 L 7 2 4F A6WE 1996092600173 19960926 00173 WP 1996 9 26 9620219976 1 19960919 A 3350 60030451 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9340 47389 DURING LINE MAINTENANCE INSPECTION, FOUND UPPER CABIN AFT OF OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTE RY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996092600174 19960926 00174 WP 1996 9 26 9620229976 1 19960919 A 3350 60030451 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9340 47389 DURING LINE MAINTENANCE INSPECTION, FOUND AFT INTERIOR OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS, O PERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996092600175 19960926 00175 NE 1996 9 26 9620239989 2 19960920 A 7260 7578679 OIL FILTER DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7B 52053 NE RT ENGINE CONTAMINATED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 8945E 47181 655196 DURING TAKEOFF ROLL, THE RIGHT ENGINE OIL STRAINER CLOG LIGHT ILLUMINATED. CREW ABORTED TAKEOFF AND RETURNED TO THE GAT E. MAINTENANCE REPLACED THE RIGHT ENGINE MAIN OIL STRAINER, LEAK AND OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F A6WE E2EA 1996092600176 19960926 00176 EU 1996 9 26 9620243242 1 19960919 A 3350 321454 POWER SUPPLY AIRBUS 320 A320212 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 342NW 381 DURING LINE MAINTENANCE, THE EMERGENCY LIGHTS SYSTEM CHECK FAULTS THE LEFT FORWARD POWER SUPPLY. REPLACED POWER SUPPLY, OPERAITONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996092600177 19960926 00177 WP 1996 9 26 9620259856 1 19960919 A 2913 PUMP DOUG DC9 DC931 3022065 WP RT HYD SYST FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 01 765NC 47718 DURING CRUISE, THE RIGHT HYDRAULIC SYSTEM QUANTITY AND PRESSURE WENT TO ZERO. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT EDP AND FILTERS. REPLACED RIGHT AUXILIARY PUMP AND FILTERS AND PRESSURE LINE FROM AUXIL IARY PUMP. SERVICED SYSTEM, LEAK AND OPERATIONAL CHECK. 2 L 7 2 4F A6WE 1996092600178 19960926 00178 NM 1996 9 26 96FDEA01493 1 19960919 A 5230 CABLE BOEING 727 72722 1384002 NM AFT CARGO DOOR DISLODGED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 194FE 19143 AFT CARGO DOOR WARNING LIGHT ON SECOND OFFICER'S PANEL ILLUMINATED DURING CLIMBOUT PASSING 2,600 FEET. RETURN TO FIELD TO TROUBLESHOOT. FOUND CABLE STUCK IN DOOR JAMB. OPENED AND CLOSED DOOR, ALL LIGHTS WENT OUT. 2 L 7 3 4F A3WE 1996092600179 19960926 00179 NM 1996 9 26 96FDEA01494 1 19960907 A 5315 FLOOR BEAM BOEING 727 72722C 138400F NM BS 640 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 113FE 19894 STA 640 BL 0 LBL 60 FLOOR BEAM IS CORRODED ON UPPER FLANGE TOP AND BOTTOM SIDES. FLOOR BEAM HAS BEEN REPAIRED PER SRM 5 3-10-8 FIG 15. 2 L 7 3 4F A3WE 1996092600180 19960926 00180 NM 1996 9 26 96FDEA01495 1 19960827 A 5315 FLOOR BEAM BOEING 727 72722C 138400F NM BS 680 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 113FE 19894 STA 680 BL 0 LBL 60 FLOOR BEAM IS HEAVY CORRODED BL 0 TO LBL 50 MEDIUM CORROSION 50 TO 60 LBL. REMOVED CORROSION PER 51-10-6 INSTALLED REPAIR PER SRM 53-10-8 FIG 8. 2 L 7 3 4F A3WE 1996092600181 19960926 00181 NM 1996 9 26 96FDEA01496 1 19960827 A 5315 FLOOR BEAM BOEING 727 72722C 138400F NM BS 680 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 113FE 19894 STA 680 LBL 48 FLOOR BEAM IS CRACKED AROUND CORRODED FASTENER HOLE. REMOVED CORROSION PER 51-10-6, INSTALLED REPAIR PER SRM 53-10-8. 2 L 7 3 4F A3WE 1996092600182 19960926 00182 NM 1996 9 26 96FDEA01497 1 19960827 A 5315 BAC150529222 FLOOR BEAM BOEING 727 72722C 138400F NM BS 344 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 113FE 19894 FLOOR BEAM AT STA 344 TOP SURFACE CORRODED FROM LBL 55 RBL 15. REMOVED DAMAGED SECTION OF UPPER CHORD, INSTALLED REPAIR CHORD AND ANGLES PER FEDEX SRD NR SR 27-53-007. 2 L 7 3 4F A3WE 1996092600183 19960926 00183 NM 1996 9 26 96FDEA01498 1 19960828 A 5315 BAC1518332 FLOOR BEAM BOEING 727 72722C 138400F NM BS 440 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 113FE 19894 CABIN FLOOR BEAM CORRODED AROUND HOLE LWR SURFACE OF UPPER FLANGE STA 440 RBL 35 MKD. CUT OUT DAMAGED SECTION OF FLOOR BEAM UPPER CHORD, FWD ANGLE, INSTALLED FLOOR BEAM REPAIR ANGLES PER SRM 53-10-8 FIG 8. 2 L 7 3 4F A3WE 1996092600184 19960926 00184 NM 1996 9 26 96FDEA01499 1 19960904 A 5315 FLOOR BEAM BOEING 727 72722C 138400F NM BS 640 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 113FE 19894 UPPER LOBE STA 640 FLOOR BEAM CORRODED ON BOTTOM OF UPPER CHORD, FWD AND AFT FLANGES BETWEEN RBL 45 TO 65. REMOVED COR ROSION PER SRM 51-10-6 FOR A SMOOTH BLEND OUT. INSTALLED 2 REINFORCEMENT REPAIR STRAPS TO LWR SIDE OF FLOOR BEAM STA 64 0 UPPER CHORD PER FEDEX EA 7-5310-28850 REV A DATED 9-3-96. 2 L 7 3 4F A3WE 1996092600185 19960926 00185 NM 1996 9 26 96FDEA1500 1 19960828 A 5315 FLOOR BEAM BOEING 727 72722C 138400F NM BS 680 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 113FE 19894 UPPER LOBE STA 680 FLOOR BEAM WAS CORRODED. CORROSION WAS REMOVED ON NR0484 LBL 50, MATERIAL REMOVED EXCEEDED SRM 53-1 0-1 LIMIT MEASURES .121. ACCOMPLISHED REPAIR AS PER SRM 53-10-8 FIG 8. 2 L 7 3 4F A3WE 1996092600186 19960926 00186 NM 1996 9 26 96FDEA01502 1 19960908 A 5315 FLOOR BEAM BOEING 727 72722C 138400F NM BS 480 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 113FE 19894 UPPER LOBE CORROSION AT FS 480 LBL 10 TOP FLOOR BEAM. REMOVED CORROSION PER SRM 51-10-6 OUT OF LIMITS PER SRM 53-10-1. INSTALLED FLOOR BEAM REPAIR STA 480 LBL 4 TO 22 PER SRM 53-10-8. 2 L 7 3 4F A3WE 1996092600187 19960926 00187 NM 1996 9 26 96FDEA01503 1 19960828 A 5315 FLOOR BEAM BOEING 727 72722C 138400F NM BS 680 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 113FE 19894 UPPER LOBE STA 680 FLOOR BEAM WAS CORRODED. CORROSION WAS REMOVED ON NR0484 LBL 5, MATERIAL REMOVAL EXCEEDED SRM 53-10- 1 LIMITS MIN .140 MINIMUM PER SRM IS .150. FABRICATED AND INSTALLED DOUBLERS PER SRM 53-10-8 PG 33, REF S/O'S W45M AND W45U FOR DOUBLERS. ALL PARTS WERE TREATED AND PRIMED. 2 L 7 3 4F A3WE 1996092600188 19960926 00188 NM 1996 9 26 96FDEA01504 1 19960906 A 5315 FLOOR BEAM BOEING 727 72722C 138400F NM BS 480 CORROSION A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 113FE 19894 HEAVY CORROSION ON MAIN CARGO FLOOR BEAM STA 480. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER SRM 53-10-08. 2 L 7 3 4F A3WE 1996092600189 19960926 00189 NM 1996 9 26 96FDEA01505 1 19960911 A 5347 SEAT TRACK BOEING 727 72722C 138400F NM BS 540-560 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 113FE 19894 UPPER LOBE CORROSION AT LBL 35 FROM FS 540 TO 560. REMOVED CORROSION FOUND OUT OF LIMITS. REMOVED AND REPLACED SEAT TR ACK PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996092600190 19960926 00190 NM 1996 9 26 96FDEA01506 1 19960910 A 5315 FLOOR BEAM BOEING 727 72722C 138400F NM BS 681 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 113FE 19894 UPPER LOBE, CORROSION ON FLOOR BEAM STA 681 UPPER CHORD, LBL 45 ON BOTTOM OF AFT FLANGE AT FLOOR BOARD ATTACH HOLE. RE MOVED CORROSION, INSTALLED REPAIR STRAP PER B727 AARD 53-10-07-2 FIG 1. 2 L 7 3 4F A3WE 1996092600191 19960926 00191 NM 1996 9 26 96FDEA01507 1 19960911 A 5320 654939815 FITTING BOEING 727 72722C 138400F NM BS 365 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 113FE 19894 UPPER LOBE MAIN CARGO FLOOR LT BARRIER NET FITTING 9G CORRODED AND CRACKED IN NUMEROUS PLACES STA 365 LBL 60. REMOVED D AMAGED FITTING, FABRICATED NEW FITTING PER EA 7-5320-28860. INSTALLED NEW FITTING PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996092600192 19960926 00192 NM 1996 9 26 96FDEA01508 1 19960918 A 5311 BELLFRAME BOEING 727 72722C 138400F NM BS 520 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 113FE 19894 MAIN CABIN STA 520 AT STR 6R BELLFRAME DENTED, NR0760 MAIN CABIN STA 520 4 INCHES BELOW STR 6R TO BELL FRAME DENTED NR02 61. MAIN CABIN STA 520 BETWEEN STR 7 TO 8R BELLFRAME CRACKED AND DENTED NR0262. REPAIRED PER EA 7-5310-28854 NR 0260, 0261 AND 0262. 2 L 7 3 4F A3WE 1996092600193 19960926 00193 NM 1996 9 26 96FDEA01509 1 19960917 A 5311 BELLFRAME BOEING 727 72722C 138400F NM BS 580 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 113FE 19894 MAIN CABIN STA 580 BELLFRAME DENTED AND DISTORTED AT FLOOR LEVEL RIGHT SIDE ABOVE STR 17R. CUT OUT DAMAGE AND REPAIRED PER SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 1996092600194 19960926 00194 NM 1996 9 26 96FDEA01510 1 19960829 A 5714 WEB BOEING 727 72722C 138400F NM BS 870 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 113FE 19894 CENTER WING BOX 3RD BAY WEB AT STA 870 RBL 25.08 TO 45.61 POPPED FASTENER. REMOVED CORRODED AREA AND INSTALLED DOUBLER PER EA 7-5771-28858. 2 L 7 3 4F A3WE 1996092600195 19960926 00195 NM 1996 9 26 96FDEA01511 1 19960920 A 5754 65217445 BONDING JUMPER BOEING 727 72725 1384006 NM NR 1 LE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 511FE 18283 NR 0214 AND 002. NR 1 K-FLAP TO BULLNOSE INBOARD BONDING JUMPER UPPER AND LOWER ATTACH POINTS ARE CORRODED. REMOVED CO RRODED AREAS, BLENDED, AND TREATED UPPER ATTACH POINT. REMOVED DAMAGED AREA ON NR 1 K-FLAP TO BULLNOSE INBOARD BONDING JUMPER AND REPAIRED IAW FEDEX SRM 57-50-3. 2 L 7 3 4F A3WE 1996092600196 19960926 00196 WP 1996 9 26 SCNA96253 1 19960915 A 2611 3023117 SMOKE DETECTOR DOUG DC10 DC1030F 3023504 WP FWD CARGO MALFUNCTIONED A SCNA K NONE N FALSE WARNING UK UNKNOWN 1 GL 15 602GC 47923 OBSERVED A MOMENTARY LOWER CARGO FIRE INDICATION. CHECKED FORWARD CARGO SMOKE DETECTOR IN ACCORDANCE WITH TAFI 26-14-00 , CLEANED PLUG AND TESTED SEVERAL TIMES ON GROUND. 2 L 7 3 4F RT A22WE 1996092600197 19960926 00197 NM 1996 9 26 DHL96721002 1 19960918 A 3150 3186301001057 LIGHT SOCKET BOEING 727 727228 NM FWD PANEL SHORTED A DHLA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 721DH 19545 AFTER LIFT OFF, MAIN WHEELS ALL TEST LIGHTS FRONT PANEL ILLUMINATED. ENGINE OPERATION AND GENERATORS NORMAL. RETURN TO DEN. T/S FOUND A .25 INCH NUT JAMMED ONTO WIRES FOR L/E GREEN LIGHTS ON FWD PANEL. REMOVED NUT, ALL WARNING LIGHTS TE STED GOOD PER M/M 33-150. 2 L 7 3 4F A3WE 1996092600198 19960926 00198 SO 1996 9 26 SWIA95761 1 19960913 A 3260 PROX SENSOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT MLG DIRTY A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 235SW 120310 RT MAIN GEAR INTRANSIT LIGHTS STAYED ON AFTER GEAR RETRACTION. CYCLED GEAR AND LIGHTS REMAINED ON. CLEANED RIGHT GEAR UPLOCK PROX SENSOR, CYCLED GEAR 10 TIMES AND OPS CKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1996092600199 19960926 00199 SO 1996 9 26 SWIA95762 1 19960914 A 3260 GEAR LIGHT EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE NLG MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 193SW 120088 AFTER TAKEOFF WITH GEAR HANDLE IN UP POSITION, SYSTEM -A+ GEAR POSITION INDICATION LIGHT FOR NOSE GEAR STAYED ILLUMINATE D. SYSTEM -B+ LIGHT SHOWED NORMAL OPERATION. DID NOT CONCUR WITH -A+ SYSTEM. LOW RUMBLE HEARD FROM ENGINE DURING RETR ACT PERIOD. INSPECTED NOSE LANDING GEAR IAW WITH MM 32. PERFORMED SEVEN GEAR SWINGS. NO DEFECT NOTED, ALL CHECKS GOOD . 2 L 7 2 4T 4 T RT A31SO E20NE 1996092600200 19960926 00200 NE 1996 9 26 SWIA95763 2 19960916 A 7314 3035526 FUEL PUMP EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT ENGINE MALFUNCTIONED A SWIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 NM 07 190SW 120050 LEFT ENGINE FAILED ON TAKEOFF ROLL. REJECTED TAKEOFF, RETURNED TO GATE. REMOVED AND REPLACED LEFT ENGINE FUEL PUMP WIT H SERVICEABLE UNIT. WORK PERFORMED IAW MM 77-01-40, OPS CKS GOOD, NO LEAKS. 2 L 7 2 4T 4 T RT A31SO E20NE 1996092600201 19960926 00201 SW 1996 9 26 SWIA95756 1 19960901 A 2612 FIRE LIGHT SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP LT ENGINE SHORTED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 27297 AC735 ON CLIMBOUT, LEFT ENGINE FIRE LIGHT ILLUMINATED. FOLLOWED CHECKLIST, RETURNED TO LAX. FOUND FIRE PROBE TERMINAL ON LEF T ENGINE SHORTED AGAINST FUEL LINE. REPOSITIONED FUEL LINE AND PROBE AND INSULATED BOTH, OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A8SW E4WE 1996092600202 19960926 00202 NE 1996 9 26 SWIA95757 2 19960904 A 7314 3035526 FUEL PUMP EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT ENGINE FAILED A SWIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 NM 07 189SW 120048 ADVANCED POWER LEVERS FOR TAKEOFF FOLLOWED BY FUEL AND OIL AURAL WARNINGS. ABORTED TAKEOFF ON RIGHT ENGINE. REMOVED AN D REPLACED RIGHT ENGINE FUEL PUMP ASSY WITH SERVICEABLE UNIT. ENGINE GROUND RUNS CHECKED GOOD, NO LEAKS. WORK PERFORME D IAW MM 72-01-40. 2 L 7 2 4T 4 T RT A31SO E20NE 1996092600203 19960926 00203 SO 1996 9 26 SWIA95758 1 19960904 A 3230 12038594001 CONTROL BOX EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LANDING GEAR MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 213SW 120277 LANDING GEAR WOULD NOT RETRACT. REPLACED LANDING GEAR CONTROL BOX, OPS CKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1996092600204 19960926 00204 SO 1996 9 26 SWIA95759 1 19960905 A 5210 DOOR STOP EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE PAX DOOR FAILED A SWIA A UNSCHED LANDING D INFLIGHT SEPARATION CR CRUISE 1 NM 07 190SW 120050 AT 25,000 FEET, HEARD A BIG BANG. FLIGHT ATTENDANT REPORTED THAT ONE OF THE LATCHES ON THE FORWARD DOOR BROKE OFF. LAN DED AT SBA. REPLACED UPPER FORWARD ENTRY DOOR BACKSTOP AND ADJUSTED BOTH UPPER DOOR BACKSTOPS PER MM 52-11-00, CHECKS G OOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1996092600205 19960926 00205 EA 1996 9 26 SWIA95760 1 19960911 A 3610 SENSOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE BLEED AIR CHAFED A SWIA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 NM 07 405SW 7029 RIGHT 14TH DUCT RED EICAS MESSAGE DURING CLIMB. MESSAGE OUT WITHIN 2 MINUTES OF POWER REDUCTION TO IDLE. MESSAGE RETUR NED AT CLIMB POWER EVEN WITH 14TH STAGE VALUE CLOSED. AFTER POWER REDUCTION TO IDLE AGAIN, LIGHT OUT. WARNING RETURNED AND STAYED ON AFTER LANDING AND ENGINE WAS SHUTDOWN. FOUND CHAFED 14TH STAGE BLEED AIR SENSOR ELEMENT. REMOVED AND RE PLACED ELEMENT IAW MM 36-21-00, DUCT OPS TEST GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 1996092600206 19960926 00206 WP 1996 9 26 ARWA9609030 1 19960920 A 2460 92074521 RELAY DOUG DC8 DC862 3021970 WP COCKPIT MALFUNCTIONED A ARWA A UNSCHED LANDING G H MULTIPLE FAILURE ELECT. POWER LOSS-50 PC CL CLIMB 1 SO 19 802BN 45909 WHILE ON CLIMBOUT, LOST NR 1 DC BUS, CAPTAIN'S INSTRUMENTS LIGHTS OUT, 1 AND 2 ENGINE OIL TEMP, OIL QTY, CSD NR 1 FUEL F EED PUMP NR 1 ALT FUEL PUMP, HYD QTY. RETURNED TO MIAMI WITHOUT INCIDENT. WHEN PUT GEAR DOWN, ALL ABOVE RETURNED TO NO RMAL. REMOVED AND REPLACED NR 1 LOAD MONITOR RELAY IAW 24-20-8, SYSTEMS OPS NORMAL NR 1 BUS. 2 L 7 4 4F 4A25 1996092600207 19960926 00207 WP 1996 9 26 CKSA96137 1 19960918 A 2612 D5020 FIRE LOOP DOUG DC8 DC861 3021952 WP PWA JT3D JT3D3B 52039 NE NR 2 ENGINE DIRTY A CKSA K NONE N FALSE WARNING AP APPROACH 1 GL 23 817CK 45887 645251 FIRE WARNING ON NR 2 ENGINE CAME ON AT 500 FT ON THIS APPROACH AND AGAIN ON TAXI IN AND WILL NOT TEST. CLEANED CONNECTO RS ON LOOP, REPOSITIONED LOOP ALONG FRAME IN SEVERAL AREAS. RAN ENGINE FOR POSSIBLE PNEUMATIC LEAK, NO LEAK NOTED. FIR E WARNING OPS CHECKS GOOD AS PER MM 26-00. 2 L 7 4 4F 4 F 4A25 1E8 1996092600208 19960926 00208 WP 1996 9 26 CKSA96138 1 19960919 A 2612 CA06LE16S8R CONNECTOR DOUG DC8 DC861 3021952 WP PWA JT3D JT3D3B 52039 NE NR 2 ENGINE LOOSE A CKSA K NONE J WARNING INDICATION DE DESCENT 1 GL 23 817CK 45887 645251 NR 2 ENGINE FIRE WARNING CAME ON FOR 1 TO 2 SECONDS ON DESCENT AND WENT OFF WITH NO ACTION TAKEN. REPAIRED WIRE CONNECT OR AT UPPER AFT FIRE LOOP SYSTEM, OPS CHECKS NORMAL IAW DC8 MM CHAPTER 26-10-0. 2 L 7 4 4F 4 F 4A25 1E8 1996092600209 19960926 00209 SO 1996 9 26 SRAA960910 1 19960917 A 3230 1ENG16B SWITCH LKHEED 382 382G 526414U SO RT MLG DEFECTIVE A SRAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 921SJ 4586 AFTER TAKEOFF, FOUND RIGHT MAIN LANDING GEAR WOULD NOT RETRACT. ACCOMPLISHED AIR TURNBACK, AIRCRAFT LANDED WITHOUT INC IDENT. PERFORMED MLG RETRACTION TEST, FOUND UPLOCK SWITCH DEFECTIVE. REPLACED SWITCH AND CYCLED GEARS, SYSTEM OPS CHEC KED GOOD. 2 H 7 4 4T A1SO 1996092600210 19960926 00210 WP 1996 9 26 SRAA960911 1 19960920 A 2822 BOOST PUMP DOUG DC8 DC873F 302199F WP NR 2 ENGINE FAILED A SRAA E ENGINE SHUTDOWN X ENGINE FLAMEOUT DE DESCENT 1 GL 23 875SJ 46063 ON DESCENT, NR 2 ENGINE FLAMED-OUT WITH FUEL PRESSURE AND QUANTITY NORMAL. ENGINE RESTARTED NORMALLY EXCEPT BOOST FEED PUMP PRESSURE LIGHT FLICKERED ON SHORTLY AFTER INFLIGHT START. LANDED LAX WITHOUT INCIDENT. ITEM IS UNDER INVESTIGATI ON. 2 L 7 4 4F RT 4A25 1996092600218 19960926 00218 EU 1996 9 26 96ZZZX4840 1 19960718 A 2822 355A61519902 CIRCUIT BOARD AEROSP AS355 AS355F1 8680810 EU BOOST PUMP FAILED A EJYA O OTHER O OTHER CR CRUISE 1 WP 07 911TX 5073 FORWARD TANK BOOST PUMP QUIT DURING FLIGHT. REPLACED ALPHA 15 CIRCUIT BOARD. OPS CHECK GOOD. 1 G 7 2 3U H11EU 1996092600242 19960926 00242 NE 1996 9 26 96ZZZX4864 3 19960414 A 6111 R8106403 BLADE SHEATH HAMSTD SFA13M1OA AEROSP ATR72 ATR72212 EU HAMSTD 14SF 14SF5 NE LT PROPELLER MISSING A A TRBA O OTHER E VIBRATION/BUFFET CR CRUISE 1 SO 21 429AT 4102 FR533 429 DURING CRUISE, CREW REPORTED SEVERE VIBRATION FROM THE LEFT PROPELLER ALONG WITH TORQUE FLUCTUATIONS. DURING INSPECTION OF LEFT PROPELLER, FOUND ONE BLADE WITH ITS LEADING EDGE NICKEL SHEATH MISSING. BLADE WAS REMOVED AND REPLACED WITH SA TISFACTORY RESULTS AFTER RUN-UP. 2 H 7 2 4T RT A53EU 6 C P7NE 1996092600243 19960926 00243 SW 1996 9 26 BSAA050496 1 19960506 A 5230 SEAL SWRNGN SA226 SA226TC 8780404 SW CARGO DOOR FAILED A BSAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 05 116BS TC311 LOST CABIN PRESSURE. CARGO DOOR SEAL HAD A LEAK AND WENT SOFT ALLOWING LOSS OF CABIN PRESSURE. REPLACED CARGO DOOR SEA L. OPS CHECKED OKAY. HOURS SINCE LAST C-INSPECTION/CHECK: 45.3. (X) 2 L 7 2 4T RT A8SW 1996092600244 19960926 00244 EU 1996 9 26 USAAF96094 1 19960822 A 3297 WIRE HARNESS FOKKER F28 F28MK4000 4990810 EU LT MLG OUT OF POSITION A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 475AU 11222 CLT/DAY - FLT 0382 - AFTER TAKEOFF, GEAR WOULD NOT LOCK-UP IN PLACE. LEFT MAIN RED L IGHT REMAINED ON. UTILITY PUMPS O FF AND AMBER LIGHT COMES ON. PILOT COMPLETED ABNORMAL PROCEDURES CHECK AND RETURNED TO CLT. NO FURTHER INCIDENTS. MAI NTENANCE FOUND MLG UPPER HARNESS HANGING UP ON AFT DOOR UPLOCK HOOK. REPOSITIONED HARNESS AND SWUNG GEAR. ALL OPERATIO NS CHECKED GOOD. (X) 2 L 7 2 4F RT A20EU 1996092600245 19960926 00245 EU 1996 9 26 USAAF96095 1 19960829 A 3244 5004069 TIRE FOKKER F28 F28MK4000 4990810 EU NR 4 MAIN GEAR BLOWN A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 475AU 11222 CLT/ROA - FLT 0654 - ON ROTATION, CREW HEARD MUFFLED NOISE AND HAD VIBRATION IN NOSE GEAR. EMERGENCY WAS DECLARED AND A IRCRAFT RETURNED TO FIELD. NO FURTHER INCIDENTS. INSPECTION SHOWED NR 4 MAIN TIRE WAS BLOWN. ALSO FOUND RT MLG UPPER BRAKE TUBING AND RT MLG UPPER ELECTRICAL HARNESS WERE DAMAGED. MAINTENANCE REPLACED HARNESS, BRAKE TUBING, AND BOTH RT MLG WHEEL ASSEMBLIES. (X) 2 L 7 2 4F RT A20EU 1996092600246 19960926 00246 NM 1996 9 26 P9IA96025 1 19960809 A 2613 356802255 SENSING ELEMENT BOEING 727 727231 1384079 NM CARGO COMPT LOOSE A P9IA O OTHER N FALSE WARNING DE DESCENT 1 SO 03 12305 64591 19562 DURING DESCENT, LOWER AFT BODY OVERHEAT LIGHT WAS INTERMITTENTLY FLICKERING ON AND OFF. SECURED LOOP IN SEVERAL SPOTS A LONG LT SIDE WALL AFT CARGO IAW MM 26-14-1. GROUND CHECKS NORMAL PER MM 26-14-0. (X) 2 L 7 3 4F A3WE 1996092600247 19960926 00247 NM 1996 9 26 P9IA96026 1 19960812 A 3350 CHARGER PACK GRIMES P72914 BOEING 727 727231 1384079 NM CABIN DIRTY A P9IA K NONE L NO TEST IN INSP/MAINT 1 SO 03 12305 64597 19562 RIGHT OVERWING EMERGENCY LIGHT CENTER POSITION INOPERATIVE. CLEANED TERMINALS ON CHARGER PACK, CHECKS GOOD PER MM 33-50 -0. (X) 2 L 7 3 4F A3WE 1996092600248 19960926 00248 NM 1996 9 26 P9IA96027 1 19960812 A 3350 P4010021 BATTERY P4010021 BOEING 727 727231 1384079 NM CABIN DISCHARGED A P9IA K NONE L NO TEST IN INSP/MAINT 1 SO 03 12305 64597 19562 AFT F/A PANEL ONE EMERGENCY FLASHLIGHT INOPERATIVE. GUARD BROKEN. REPLACED BATTERY IN EMERGENCY FLASHLIGHT AND BREAK-A WAY SEAL IAW MM 25-60-02. (X) 2 L 7 3 4F A3WE 1996092600249 19960926 00249 NM 1996 9 26 P9IA096021 1 19960613 A 3350 BATTERY PACK GRIMES BOEING 727 727231 1384079 NM CABIN DIRTY A P9IA K NONE L NO TEST IN INSP/MAINT 1 SO 03 12305 64167 19562 AFT AIR STAIR O/H EMERGENCY LIGHT DOES NOT ILLUMINATE. CLEANED CONTACTS AT BATTERY PACK. OPS CHECKS GOOD IAW MM 33-50- 0. (X) 2 L 7 3 4F A3WE 1996092600250 19960926 00250 NM 1996 9 26 96ZZZX4865 1 19960627 A 2750 65218901 CONTROL VALVE BOEING 727 7272J7 138400E NM TE FLAPS CRACKED A ULHF A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SO 23 553NA 20707 FLIGHT RETURN. LOST A-SYSTEM HYDRAULICS IN-FLIGHT DUE TO LOSS OF FLUID. FOUND OUTBOARD FLAP CONTROL VALVE LEAKING (DUE TO CRACK IN CASE). THE OUTBOARD FLAP CONTROL VALVE WAS REPLACED TO CORRECT THE PROBLEM. 2 L 7 3 4F A3WE 1996092600251 19960926 00251 NM 1996 9 26 96ZZZX4866 1 19960701 A 2910 BACH30A506W0341 HOSE BOEING 727 7272J7 138400E NM NR 1 ENGINE RUPTURED A ULHF A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SO 23 552NA 20706 FLIGHT RETURN. LOST A-SYSTEM HYDRAULICS IN-FLIGHT DUE TO LOSS OF FLUID. FOUND NR 1 ENGINE HYDRAULIC CASE DRAIN LINE RU PTURED. THE PUMP AND CASE DRAIN LINE WERE BOTH REPLACED TO CORRECT PROBLEM. 2 L 7 3 4F A3WE 1996092600255 19960926 00255 EU 1996 9 26 96ZZZX4870 1 19960803 A 6220 704A33640040 FREQ ADAPTER SNIAS 350 AS350B 8680801 EU MAIN ROTOR DEFECTIVE A EJYA K NONE E VIBRATION/BUFFET IN INSP/MAINT 1 WP 07 911MV 10 2262 INSTALLED NEW FREQUENCY ADAPTERS BECAUSE OF LIFE LIMIT ON OLD ADAPTERS. TRACK AND BALANCE ACCOMPLISHED. SEVEN FLIGHT H OURS LATER, PILOTS COMPLAINED OF VIBRATION. COULD NOT COMPLETE TRACK AND BALANCE ATTEMPT TO MINIMUM IPS. REPLACED FREQ UENCY ADAPTER. TRACK AND BALANCE ACCOMPLISHED. NO FURTHER PROBLEMS NOTED. 1 G 7 1 3U H9EU 1996092600272 19960926 00272 NM 1996 9 26 CALA9601320 1 19960921 A 2910 65446541001 HYD LINE BOEING 737 737217 1384464 NM NR 2 SLAT ACT CRACKED A CALA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 SW 09 12230 19884 THE AIRCRAFT LOST A-SYSTEM HYDRAULIC PRESSURE AND QUANTITY UPON LANDING. THE AIRCRAFT STOPPED SAFELY AND WAS TOWED TO T HE GATE. MAINTENANCE FOUND HYDRAULIC LINE JUST OUTBOARD OF NR 2 SLAT ACTUATOR CRACKED. A FLEX LINE WAS INSTALLED AND A DIP WAS ISSUED TO REPLACE THE FLEX LINE WITHIN 1,200 HOURS OR 500 FLIGHTS. THE HYDRAULIC SYSTEM WAS SERVICED TO FULL A ND LEAK CHECKS WERE GOOD. 2 L 7 2 4F A16WE 1996092600273 19960926 00273 NM 1996 9 26 CALA9601321 1 19960922 A 2121 6454051 FAN BOEING 737 7373T0 1384582 NM LT PACK INOPERATIVE A CALA H DEACTIVATE SYST/CIRCUITS B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 09 19357 20659 23841 THE FLIGHT ATTENDANT REPORTED ODOR AND SMOKE IN CABIN DURING CRUISE. THE LT PACK WAS SECURED, THEN THE FORWARD LAV SMOK E DETECTOR ACTIVATED. THE RECIRCULATION FAN WAS TURNED OFF AND THE LEFT PACK WAS RESTORED TO OPERATION. THE FLIGHT CON TINUED WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND THE RECIRCULATION FAN AT FAULT. THE FAN WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. 2 L 7 2 4F RT A16WE 1996092600274 19960926 00274 NM 1996 9 26 CALA9601322 1 19960922 A 2720 8816001001 SOLENOID VALVE 65C370524 BOEING 737 7372C0 1384488 NM RUDDER PCU MALFUNCTIONED A CALA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SW 09 14245 R0629 20074 THE AIRCRAFT BECAME HARD TO CONTROL ABOUT THE VERTICAL AXIS WHILE ON FINAL APPROACH. THE AIRCRAFT WANTED TO DUTCH ROLL AND YAW EXCESSIVELY AND DIDN'T RESPOND EFFECTIVELY TO PILOT CONTROLLED INPUTS ON RUDDER. THE AIRCRAFT HANDLED THE SAME WITH AND WITHOUT YAW DAMPER. THE STANDBY RUDDER PCU CHECKED NORMAL PER MM 22-11-0, PAGE 112A. THE RUDDER PCU WAS REMOV ED, REPLACED, AND ADJUSTED/TESTED IAW MM 27-21-91. THE YAW DAMP COUPLER WAS REMOVED AND REPLACED AND AN OPERATIONAL/SEL F TEST WAS PERFORMED WITH NORMAL OPERATION IAW MM 22-11-41. *S/D* THE RUDDER PCU REVEALED THE SOLENOID VALVE WAS AT FA ULT. VENDOR TEARDOWN WAS UNABLE TO CONFIRM FAILURE OF THE YAW DAMP COUPLER. 2 L 7 2 4F A16WE 1996092600275 19960926 00275 NM 1996 9 26 CALA9601323 1 19960920 A 3350 1000677 LIGHT BOEING 737 737247 138448D NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14246 20129 THE LT OVERWING EMERGENCY EXIT SIGN DID NOT TEST. THE EMERGENCY EXIT LIGHT WAS REMOVED AND REPLACED. 2 L 7 2 4F A16WE 1996092600276 19960926 00276 NM 1996 9 26 CALA9601324 1 19960920 A 3350 6104789 BATTERY PACK BOEING 737 737247 138448D NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14246 20129 THE RT EXTERIOR OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED. 2 L 7 2 4F A16WE 1996092600277 19960926 00277 WP 1996 9 26 9620079930 1 19960906 A 5320 WEB DOUG DC9 DC931 3022065 WP BS 83 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 89S 47042 DURING H-CHECK, FOUND A 3.6 INCH CRACK IN THE NOSE LANDING GEAR HORIZONTAL PRESSURE WEB RIGHT FRAME FITTING FS 83. REPA IRED WEB (P/N 9910073-313) PER EA 99-110787. 2 L 7 2 4F A6WE 1996092600278 19960926 00278 WP 1996 9 26 9620089930 1 19960906 A 5320 WEB DOUG DC9 DC931 3022065 WP BS 108 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 89S 47042 DURING H-CHECK, FOUND CRACKS IN THE NOSE LANDING GEAR HORIZONTAL PRESSURE WEB FS 108 AT LBL/RBL 25 AND 37 AT THE VERTICA L STIFFENER UPPER FITTING. REPAIRED WEB (P/N 9910073-313, 9911583) PER EA 99-110786. 2 L 7 2 4F A6WE 1996092600279 19960926 00279 WP 1996 9 26 9620099930 1 19960907 A 5312 BLKHD SPLICE DOUG DC9 DC931 3022065 WP BS 756 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 89S 47042 DURING H-CHECK, FOUND CORROSION ON THE FS 756 BULKHEAD T-SPLICE BETWEEN LONGERON 29R TO 30. REPAIRED SPLICE (P/N 995821 2-3) PER EA 99-110785. 2 L 7 2 4F A6WE 1996092600280 19960926 00280 WP 1996 9 26 9620109912 1 19960911 A 5240 DOUBLER DOUG DC9 DC931 3022065 WP LAV SERVICE DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 962N 47406 DURING M-CHECK, FOUND A CRACK IN THE EXTERIOR FUSELAGE LAVATORY SERVICE DOOR DOUBLERS, LOWER FORWARD CORNER. REPAIRED D OUBLERS (P/N 5911423-43, -99) PER EA 99-111219. 2 L 7 2 4F A6WE 1996092600281 19960926 00281 WP 1996 9 26 9620119912 1 19960911 A 5320 WEB DOUG DC9 DC931 3022065 WP BS 108 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 962N 47406 DURING M-CHECK, FOUND A CRACK IN THE NOSE LANDING GEAR HORIZONTAL PRESSURE PANEL WEB AT FS 108, LBL 35. REPAIRED THE WE B (P/N 9910073-313) PER EA 99-11216. 2 L 7 2 4F A6WE 1996092600282 19960926 00282 WP 1996 9 26 9620129960 1 19960917 A 5720 FITTING DOUG DC9 DC931 3022065 WP BS 610 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 920RW 47163 DURING M-CHECK, FOUND CORROSION ON THE CENTER WING TANK FORWARD RIGHT ATTACH FITTING FS 610. REPLACED FITTING PER SRM 5 1-30-5, 51-30-1. 2 L 7 2 4F A6WE 1996092600283 19960926 00283 WP 1996 9 26 9620139180 1 19960918 A 5312 BLKHD FITTING DOUG DC9 DC914 3022034 WP AFT PRESS BLKHD CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3312L 45707 DURING H-CHECK, FOUND CORROSION ON THE AFT PRESSURE BULKHEAD SHOVEL FITTING AT LONERON 20R. REPLACED FITTING (P/N 49125 15-1N) PER SRM 51-30-2, 51-30-5. 2 L 7 2 4F A6WE 1996092600284 19960926 00284 EU 1996 9 26 COMA9630146 1 19960920 A 6120 CONNECTOR SAAB SF340 SF340A 7850100 EU AUTO COARSEN DIRTY A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 359CA 340A053 AUTO COARSEN FAULT WARNING DURING TAKEOFF. CLEANED WIRING CONNECTORS AT AUTO COARSEN P3 SENSORS, SYSTEM TEST NORMAL. 2 L 7 2 4T RT A52EU 1996092600285 19960926 00285 EA 1996 9 26 COMA9660147 1 19960920 A 2613 356002255 ELEMENT CNDAIR CL600 CL6002B19 EA FUSELAGE MALFUNCTIONED A COMA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 931CA 7037 ANTI-ICE DUCT MESSAGE ON EICAS DURING TAXI. REPLACED LEFT FUSELAGE DUCT LEAK SENSOR LOOP. 2 L 7 2 4F RT A21EA 1996092600286 19960926 00286 EA 1996 9 26 COMA9660148 1 19960922 A 3260 864806 PSEU CNDAIR CL600 CL6002B19 EA E/E COMPT MALFUNCTION A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 943CA 5452 3157 7062 MULTIPLE CAUTION CHIMES AND PROX WARNING LANDING GEAR CAUTION. REPLACED THE PROXIMITY SENSOR ELECTRONIC UNIT. 2 L 7 2 4F RT A21EA 1996092600287 19960926 00287 NM 1996 9 26 UPS96221131 1 19960918 A 5754 RIB BOEING 727 727247 138408F NM NR 5 LE SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 207UP 21699 INSPECTION TYPE-C, WHILE WORKING WINGS 162 FOUND CRACKED RIB ON NR 5 SLAT O/B OF ROD END DUE TO OTHER DAMAGE TO NR 5 SLAT. THE SLAT IS BEING REPLACED ON NRC 607692 AND INSTALLED ON NRC 607694. 2 L 7 3 4F A3WE 1996092600288 19960926 00288 NM 1996 9 26 UPS96221133 1 19960919 A 5240 6556992554 FRAME BOEING 727 727247 138408F NM AFT SERVICE DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 207UP 21699 INSPECTION TYPE-C, RIGHT HAND AFT SERVICE DOOR FORWARD FRAME LOWER HINGE CUTOUT UPPER I/B CORNER IS CRACKED .35 LONG. R EMOVED AND REPLACED AFT SERVICE DOOR FORWARD FRAME IAW SRM 51-10-1, 51-10-2, MM 51-20-151, 52-14-00. 2 L 7 3 4F A3WE 1996092600289 19960926 00289 NM 1996 9 26 UPS96221134 1 19960919 A 5320 SHEAR TIE BOEING 727 727247 138408F NM BS 950 CORRODED A IPXA O OTHER O OTHER IN INSP/MAINT 1 SO 01 207UP 21699 INSPECTION TYPE-C, CORROSION ON SHEAR TIE AT BS 950E PLUS 3 WL 149 RBL 9. MECHANICALLY REMOVED CORROSION FROM SHEAR TIE AT BS 950E PLUS 3 WL 149 RBL 9. REWORKED DEEMED OUT OF LIMITS IAW SRM 53-10-1, REPAIRED SHEAR TIE/FRAME IAW SRM 53-10- 4. 2 L 7 3 4F A3WE 1996092600290 19960926 00290 NM 1996 9 26 UPS96221135 1 19960918 A 5754 65162252 BULLNOSE BOEING 727 727247 138408F NM NR 4 LE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 207UP 21699 INSPECTION TYPE-C, CORROSION ON NR 4 K-FLAP BULLNOSE OUTBOARD BONDING JUMPER ATTACH POINT. MECHANICALLY REMOVED CORROSI ON ON NR 4 K-FLAP BULLNOSE OUTBOARD BONDING JUMPER ATTACH POINT. REWORKED DEEMED OUT OF LIMITS IAW SRM ADDENDUM B727-57 40-3980A. REPAIRED AREA IAW TRAMCO EWO 96-2517 N/A. 2 L 7 3 4F A3WE 1996092600291 19960926 00291 1996 9 26 UPS96221138 4 19960919 A 3416 CIRCUIT BREAKER BOEING 727 72725C 138400H NM COCKPIT TRIPPED A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 931UP 19858 INSPECTION TYPE-N/A, AFTER TAKEOFF ENTIRE CREW NOTED A STRONG ODOR IN COCKPIT RESEMBLING ELECTRICAL SMOKE. FOUND STBY ALT/AS CB POPPED, ODOR STOPPED. DID NOT ATTEMPT TO RESET CB. PERFORMED OPS CHK ON STBY ALT/AS IND PER MM 34-12-06 P G 501, SYS OPS CHK GOOD COULD NOT DUPLICATE. 2 L 7 3 4F A3WE 1996092600292 19960926 00292 NM 1996 9 26 UPS96221144 1 19960908 A 5320 CLIP BOEING 727 72731C 1384011 NM BS 1070 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE-C, BS 1070 STR 6R STRINGER TO FRAME CLIP CRACKED. REMOVED, FABRICATED AND INSTALLED NEW CLIP IAW DWG 65 -45313 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996092600293 19960926 00293 NM 1996 9 26 UPS96221145 1 19960908 A 5320 CLIP BOEING 727 72731C 1384011 NM BS 1070 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE-C, BS 1070 AT STR 6L AND 5L STRINGER TO FRAME CLIPS CRACKED. REMOVED, FABRICATED AND INSTALLED NEW CLIP S IAW BAC DWG 65-45313 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996092600294 19960926 00294 NM 1996 9 26 UPS96221146 1 19960906 A 5320 CHANNEL BOEING 727 72731C 1384011 NM BS 303-348 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE-C, U-CHANNEL DIRECTLY BELOW THE LAV DOOR IS CORRODED. REMOVED DAMAGED U-CHANNEL IAW SRM 51-10-01. FABR ICATED U-CHANNEL IAW SRM 53-10-01 AND INSTALLED IAW SRM 51-10-01. 2 L 7 3 4F A3WE 1996092600295 19960926 00295 NM 1996 9 26 UPS96221147 1 19960905 A 5280 SEAL RETAINER BOEING 727 72731C 1384011 NM NLG DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE-C, LT AFT NLG DOOR SEAL RETAINER CORRODED. REPLACED LT AFT NLG DOOR SEAL RETAINER PER SRM 51-30-02. 2 L 7 3 4F A3WE 1996092600296 19960926 00296 NM 1996 9 26 UPS96221148 1 19960905 A 5280 SEAL RETAINER BOEING 727 72731C 1384011 NM NLG DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE-C, RT AFT NLG DOOR SEAL RETAINER CORRODED. REPLACED RT AFT NLG DOOR SEAL RETAINER PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996092600297 19960926 00297 NM 1996 9 26 UPS96221149 1 19960907 A 5311 FRAME BOEING 727 72731C 1384011 NM BS 990 BULGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE-C, LT FUSELAGE IS BULGED AT FRAME BS 990 BETWEEN S17 AND S18L. REMOVED DAMAGED AREA, TREATED AND PRIMED , INSTALLED REPAIR AND REINSTALLED FAIRING ATTCH FITTING. 2 L 7 3 4F A3WE 1996092600298 19960926 00298 NM 1996 9 26 UPS96221150 1 19960905 A 5320 WEB BOEING 727 72731C 1384011 NM BS 1270 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE-C, AFT TORQUE BOX UPPER WEB AT BS 1270 IS CRACKED AT FASTENER IN THE INBD CHORD. REMOVED DAMAGED AREA, INSTALLED FILLER AND DOUBLER. 2 L 7 3 4F A3WE 1996092600299 19960926 00299 NM 1996 9 26 UPS96221151 1 19960907 A 5720 VERT STIFFENER BOEING 727 72731C 1384011 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE-C, LT WINGS L/E NR 2 SLAT I/B TRACK O/B MOUNT VERTICAL STIFFENER ANGLE IS CRACKED AT THE BOTTOM. REMOVE D, FABRICATED AND INSTALLED STIFFENER ANGLE PER DWG 65-16200 SHT 1 AND 8 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996092600300 19960926 00300 NM 1996 9 26 UPS96221152 1 19960907 A 5720 VERT STIFFENER BOEING 727 72731C 1384011 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE-C, LT WING NR 3 SLAT O/B TRACK, O/B MOUNT VERTICAL STIFFENER ANGLE IS CRACKED AT BOTTOM. REMOVED DAMAGE D STIFFENER, FAB AND INSTALLED REPLACEMENT STIFFENER SEALED DOME FASTENERS. 2 L 7 3 4F A3WE 1996092600301 19960926 00301 NM 1996 9 26 UPS96221153 1 19960907 A 5720 VERT STIFFENER BOEING 727 72731C 1384011 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE-C, LT WING L/E, NR 3 SLAT I/B TRACK, O/B MOUNT VERTICAL STIFFENER ANGLE IS CRACKED AT BOTTOM. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW 65-16200 AND SRM 51-30-02. 2 L 7 3 4F A3WE 1996092600302 19960926 00302 NM 1996 9 26 UPS96221154 1 19960908 A 5751 SPAR CHORD BOEING 727 72731C 1384011 NM RT AILERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE-C, RT O/B AILERON UPPER SPAR CHORD IS CRACKED, JUST O/B OF THE CENTER I/B HINGE. FABBED AND INSTALLED R EPLACEMENT PART IAW SRM 57-30-02 AND 51-30-2. 2 L 7 3 4F A3WE 1996092600303 19960926 00303 NM 1996 9 26 UPS96221155 1 19960908 A 5712 RIBS BOEING 727 72731C 1384011 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE-C, RT WING NR 5 SLAT, OUTBD AND INBD ACTUATOR ATTACH RIBS ARE CRACKED. REMOVED RIBS AND FABRICATED REPL ACEMENT RIBS IAW DWG 65-17276 AND INSTALLED IAW SRM 51-30-02. 2 L 7 3 4F A3WE 1996092600304 19960926 00304 NM 1996 9 26 UPS96221156 1 19960908 A 5720 STIFFENER BOEING 727 72731C 1384011 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 925UP 19230 INSPECTION TYPE-C, RT WING NR 5 SLAT AT ACTUATOR ROD MOUNT STIFFENER IS CRACKED IN RADIUS. REPAIRED IAW SRM 51-40-03 AN D SRM 51-30-02. 2 L 7 3 4F A3WE 1996092600305 19960926 00305 NM 1996 9 26 UPS96421132 1 19960919 A 3310 65B47529 LIGHTS BOEING 747 747123F NM COCKPIT INOPERATIVE A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SO 01 677UP 20391 INSPECTION TYPE-N/A, SMOKE IN COCKPIT COMING FROM MAST DIM AND TEST CONTROL BOX SELF TERMINATED AFTER 2 TO 3 MIN SUSPECT ASSOCIATION W NO SMOKE FATEN SEAR- BELT LIGHTS INOP IN DIM AND ALT ALERT LIGHT INDIM INOP. REF M115479 AN LOGPAGE 78741 90. FOUND A6 MD AND T CARD BURNT. REMOVED AND REPLACED LIGHTS BRIGHT DIM AND TEST GOOD (P/N 65B47529-3) (S/N 2095) ON, (P/N 65B47529) OFF. 2 L 7 4 4F A20WE 1996092600306 19960926 00306 NM 1996 9 26 UPS96421137 1 19960903 A 5315 FLOORBEAM BOEING 747 747121 1384871 NM BS 1580 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE-C, MAIN DECK FLOOR STRUCTURE FLOOR BEAM UPPER CHORD CORRODED AT BS 1580 BTWEEN LBL 60/108. CORROSION OU T OF LIMITS IAW SRM 53-10-01. REPLACED FLOOR BEAM IAW SRM 53-10-07. 2 L 7 4 4F A20WE 1996092600307 19960926 00307 NM 1996 9 26 UPS96421143 1 19960920 A 2611 SMOKE DETECTOR BOEING 747 747123 1384873 NM AFT CARGO COMPT FAILED A IPXA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 672UP 20324 LOWER CARGO LT BLINKED ON BRIEFLY ACCOMPANIED BY A BELL. ALL OTHER INDICATIONS WERE NORMAL. REMOVED AND REPLACED 6 AFT SMOKE DETECTORS, OPS CHECK GOOD. 2 L 7 4 4F A20WE 1996092600308 19960926 00308 NM 1996 9 26 UPS96521130 1 19960918 A 5753 SKIN BOEING 757 75724APF 1384969 NM TE FLAP DELAMINATION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 428UP 25459 INSPECTION TYPE-3C, RIGHT WING O/B MAIN FLAP HAS AREAS OF DELAMINATION ON I/B END UPPER SURFACE. REPAIRED RT WING O/B M AIN FLAP UPPER SURFACE. ALL WORK DONE IAW SRM 57-53-01 AND SRM 51-70-07. 2 L 7 2 4F RT A2NM 1996092600309 19960926 00309 NM 1996 9 26 UPS96521136 1 19960919 A 5753 FAIRING BOEING 757 75724APF 1384969 NM LT WING TE FLAP DAMAGED A IPXA K NONE O OTHER AP APPROACH 1 SO 01 427UP 25458 INSPECTION TYPE-N/A, DECLARED EMERGENCY DUE TO SUSPECTED LIGHTENING STRIKE AND INDICATED DECREASING OIL QUANTITY IN RT E NG OIL INDICATION RETURNED TO NORMAL LEFT WING O/B FLAP I/B FAIRING DAMAGED. REF D 115519 LEFT WING AFT FLAP I/B FAIRIN G DAMAGED ON O/B SIDE. 2 L 7 2 4F RT A2NM 1996092600310 19960926 00310 WP 1996 9 26 UPS96821139 1 19960830 A 5730 PANEL DOUG DC8 DC873F 302199F WP CENTER WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE-C, 506A RT WING CRACKED PNL LAND NR 4 MAIN. REMOVED CRACKED AREA OF PNL AND FABRICATED INTERNAL AND EXT ERNAL DOUBLERS, FILLERS IAW SRM 57-2-1, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED ALL REPAIR PARTS IAW DC8 SRM 5 1-1-20D AND 51-1-20A. 2 L 7 4 4F RT 4A25 1996092600311 19960926 00311 WP 1996 9 26 UPS96821140 1 19960901 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1766-1790 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE-C, AFT FUSELAGE SKIN LT SIDE STA 1766 TO 1790 L10L AT LAP SEAM HAS CORROSION. REMOVED CORROSION IAW DC8 SRM 51-1-8, MATERIAL LOSS EXCEED 20 PERCENT. REMOVED DAMAGE IAW DC8 SRM 53-2-1, MATERIAL ID FOR REPAIRS ARE IAW DC8 53 -5-3 FIG 1 AND 53-21-1. FABD DOUBLERS AND FILLERS IAW SRM 51-1-8, INSTALLED REPAIRS WET WITH SEALER IAW 51-1-16, 51-1-1 7, 51-1-20D AND 51-1-20B. 2 L 7 4 4F RT 4A25 1996092600312 19960926 00312 WP 1996 9 26 UPS96821141 1 19960910 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE-C, RT LEADING EDGE ATTACHMENT HOLE HAVE CRACKS IN NR 1, 2, 4, 7, 8, 10 AND 11. REPAIRED PER DRAWING NR J060232. 2 L 7 4 4F RT 4A25 1996092600313 19960926 00313 WP 1996 9 26 UPS96821142 1 19960910 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE-C, LT LEADING EDGE ATTACHMENT HOLE HAVE CRACKS IN NR 7, 8, 9, 10 AND 11. REPAIRED PER DRAWING NR J06023 2. 2 L 7 4 4F RT 4A25 1996092600314 19960926 00314 EU 1996 9 26 WWMA9600074 1 19960920 A 3230 D49412001 CONTROL PANEL SAAB SF340 340B 7860101 EU LANDING GEAR DEFECTIVE A WWMA O OTHER O OTHER LD LANDING 1 WP 15 256AE 340B256 THE LANDING GEAR CIRCUIT BREAKER POPPED ON GEAR EXTENSION, RESET CIRCUIT BREAKER AND IT POPPED AGAIN. RESET CIRCUIT BRE AKER A SECOND TIME AND THE GEAR EXTENDED AND LOCKED. THE BREAKER POPPED AGAIN 30 TO 40 SECONDS AFTER THE GEAR WAS DOWN AND LOCKED. ALSO, THE CREW HAD TO PULL THE FLIGHT IDLE OVERRIDE STOP TO GET THE POWER LEVERS INTO REVERSE. MAINTENANCE REPLACED THE LANDING GEAR CONTROL PANEL AND PERFORMED GEAR SWINGS. AIRCRAFT WAS RELEASED TO SERVICE WITH NO FURTHER PR OBLEMS. 2 L 7 2 4T RT A52EU 1996092600315 19960926 00315 EU 1996 9 26 WWMA9600073 1 19960920 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT DEFECTIVE A WWMA O OTHER N FALSE WARNING CR CRUISE 1 WP 15 284AE 340B284 CARGO SMOKE LIGHT CAME ON IN FLIGHT FOR APPROXIMATELY 2 SECONDS AND WENT OUT. ON THE GROUND THE LIGHT AGAIN CAME ON FOR 2 SECONDS AND WENT OUT. MAINTENANCE REPLACED BOTH CARGO SMOKE DETECTORS AND RELEASED THE AIRCRAFT FOR SERVICE. 2 L 7 2 4T RT A52EU 1996092600316 19960926 00316 EU 1996 9 26 WWMA9600072 1 19960920 A 3520 K386384 OXY MASK BAG JETSTM JETSTM3201 1500217 EU CABIN DEPLOYED A WWMA G O2 MASK DEPLOYED O OTHER UK UNKNOWN 1 WP 15 953LM 953 SEAT 5 B/C PASSENGER OXYGEN MASK DEPLOYED BY ITSELF. MAINTENANCE REINSTALLED THE OXYGEN MASK AND RETURNED THE AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A56EU 1996092600317 19960926 00317 WP 1996 9 26 ABXA9600630 1 19960919 A 3350 60030431 BATTERY PACK DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST CR CRUISE 1 GL 23 958AX 47760 EMERGENCY LIGHTS CYCLED ON AND OFF INTERMITTENTLY DURING FLIGHT, WHILE THE EMERGENCY LIGHT SWITCH WAS IN THE ARMED POSIT ION. REPLACED THE EMERGENCY LIGHT BATTERY PACK IAW DC-9 MM. 2 L 7 2 4F A6WE 1996092600318 19960926 00318 WP 1996 9 26 ABXA9600629 1 19960920 A 3350 5708458503 BATTERY RACK DOUG DC8 DC863F 302198F WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 826AX 46061 EMERGENCY LIGHTS WEAK. REPLACED EMERGENCY LIGHT BATTERY RACK IAW DC-8 MM 33-50-1, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1996092600319 19960926 00319 NM 1996 9 26 DLM11962114 1 19960916 A 3350 61020 BATTERIES DOUG MD11 MD11 3023602 NM CABIN DISCHARGED A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 810DE 48565 THE 4R FLASHLIGHT DOES NOT BLINK. REPLACED BATTERY, OPS NORMAL. 2 L 7 3 4F RT A22WE 1996092600320 19960926 00320 WP 1996 9 26 DLL10962122 1 19960906 A 5753 SKIN 1529504104 LKHEED 1011 10113851 5265010 WP NR 2 TE FLP VANE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 714DA 193C1090 NR 2 FLAP VANE INBOARD TRACK HAS A CRACK APPROX 20 INCHES LONG. REPLACED TRACK. 2 L 7 3 4F A23WE 1996092600321 19960926 00321 WP 1996 9 26 DLL10962125 1 19960917 A 3350 5165741 PWR SUPPLY LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 725DA 193C1162 R3 DOOR EMERGENCY SIGNS AND TRACK LIGHTS INOP. REPLACED PWR SUPPLY AT R3 DOOR, EMER LIGHTS TEST OK. 2 L 7 3 4F A23WE 1996092600322 19960926 00322 NM 1996 9 26 DL73E962132 1 19960913 A 5312 65163007 BULKHEAD WEB BOEING 737 737247 138448D NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 382DL 23609 DURING ACCOMPLISHMENT OF SI 3-69482-12, TWO CRACKS WERE DISCOVERED ON THE FORWARD FACE OF THE FS 178 BULKHEAD WEB. THE FIRST CRACK IS LOCATED NEAR THE RBL 5.7 VERTICAL STRAP AT APPROXIMATELY WL 202. THE SECOND IS LOCATED NEAR THE LBL 5.7 VERTICAL STRAP AT APPROXIMATELY WL 202. DAMAGE REMOVAL RESULTED IN A 1.0 DIAMETER CUTOUT AT BOTH THE RBL 5.7 AND LBL 5. 7 LOCATIONS. REPAIRED PER ERA 304175-14. 2 L 7 2 4F A16WE 1996092600323 19960926 00323 NM 1996 9 26 DL72S962137 1 19960919 A 3350 POWER SUPPLY RPS1 BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 541DA 1291 22387 AFT CABIN EMERGENCY TRACK LIGHTS INOP. REPLACED POWER SUPPLY M9027 AND INSTALLED NEW BATTERIES, OPS CK NORMAL. 2 L 7 3 4F A3WE 1996092600324 19960926 00324 NM 1996 9 26 DL72S962139 1 19960919 A 2150 2040751 ACM BOEING 727 727232 1384082 NM RT PACK CONTAMINATED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 416DA 21258 SMOKE IN CABIN DURING CRUISE FLT. INSPECTED CABIN NR 1 AND 2 ENGINES AND LEFT AND RIGHT PACKS. FOUND WATER IN RIGHT AC M OIL. REPLACED RIGHT ACM AND COALESCER, OPS CK NORMAL. 2 L 7 3 4F A3WE 1996092600325 19960926 00325 NM 1996 9 26 DL72S962140 1 19960919 A 2782 BRACKET BOEING 727 727232 1384082 NM NR 2 LE FLP ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 517DA 21433 FOUND DURING A-1 LETTER CHECK, NR 2 L/E FLAP ACTUATOR MOUNT BRACKET CRACKED AT LWR I/B RADIUS. REPAIRED PER M/M 57-20-2 1 PAR 12. 2 L 7 3 4F A3WE 1996092600326 19960926 00326 NM 1996 9 26 DL72S962141 1 19960919 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 940 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 517DA 21433 FOUND DURING A-1 LETTER CHECK, .75 INCH CRACK STR 18A LEFT 8 INCHES AFT BS 940 FRAME ATTACH. REPAIRED PER M/M 53-12-0. 2 L 7 3 4F A3WE 1996092600327 19960926 00327 NM 1996 9 26 DL72L962142 1 19960919 A 5532 SKIN BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 507DA 21309 A .25 INCH CRACK AT FASTENER HOLE LT SIDE OF VERT STAB AT BASE AT STR 10L. INSTALLED DOUBLER PER MM 55-30-0 PG 801. 2 L 7 3 4F A3WE 1996092600328 19960926 00328 NM 1996 9 26 DL72L962143 1 19960919 A 5320 WEB BOEING 727 727232 1384082 NM BS 1213 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 507DA 21309 VERTICAL WEB OF TORQUE BOX CRACKED AT STA 1213 RT SIDE. INSTALLED DOUBLER PER MM 53-11-0 PG 832. 2 L 7 3 4F A3WE 1996092600329 19960926 00329 NM 1996 9 26 DL72L962144 1 19960919 A 5320 WEB BOEING 727 727232 1384082 NM BS 1270 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 507DA 21309 LOWER TORQUE BOX LIGHTENING HOLE CRACKED .25 INCH AT STA 1270 LT SIDE. ROUTED OUT DAMAGE PER MM 53-11-0 PG 828. 2 L 7 3 4F A3WE 1996092600330 19960926 00330 NM 1996 9 26 DL72L962145 1 19960919 A 5320 ANGLE BOEING 727 727232 1384082 NM AC BAY CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 507DA 21309 FOUND ON D2 LETTER CK, CORROSION AT FWD HINGE ATTACH POINT OF PANEL 3448R. REPAIRED PER MM 53-30-1. 2 L 7 3 4F A3WE 1996092600331 19960926 00331 NM 1996 9 26 DL72S962149 1 19960920 A 5320 WEB BOEING 727 727232 1384082 NM BS 1273 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 467DA 20744 FOUND DURING E-1 LETTER CHECK, .1875 INCH CRACK LWR TORQUE BOX VERTICAL WEB BS 1273 LEFT SIDE AT LIGHTENING HOLE. REPAI RED PER M/M 53-11-0. 2 L 7 3 4F A3WE 1996092600332 19960926 00332 NM 1996 9 26 DL757962150 1 19960920 A 3350 BATTERY PACK BPS73 BOEING 757 757232 1384965 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 673DL 24480 25978 F/C EMERGENCY LIGHTS WON'T TEST AT AISLE AND LT OVHD SIDES. REMOVED AND REPLACED BATT PACK M730. REMOVED AND REPLACED PWR SUPPLY AND BATT PACK M371, OPN TEST NORMAL. 2 L 7 2 4F RT A2NM 1996092600333 19960926 00333 NM 1996 9 26 DL72S962153 1 19960921 A 3260 LOCK SWITCH H1010153 BOEING 727 727232 1384082 NM NLG FAILED A DALA K NONE N FALSE WARNING TO TAKEOFF 1 SO 27 478DA 9121 20755 NOSE GEAR RED INTRANSIT LIGHT DID NOT ILLUMINATE WHEN GEAR RAISED. LIGHT TESTS GOOD, WORKED WELL WHEN GEAR LOWERED/CA. REPLACED NOSE GEAR LOCK SW, PERFORMED NLG RETRACTION ALL INDICATIONS NORMAL. 2 L 7 3 4F A3WE 1996092600334 19960926 00334 WP 1996 9 26 DLL10962154 1 19960920 A 3350 5165741 BATTERY PACK LKHEED 1011 10113851 5265010 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 712DA 193C1088 ON LAYOVER CK, FOUND EMERGENCY LIGHTING SYSTEM BATTERY PACK CHARGING LIGHTS FLASHING AT R2 AND L2 DOOR PACKS. REPLACED BOTH BATTERY PACKS, CKS OK PER M/M. 2 L 7 3 4F A23WE 1996092600335 19960926 00335 NM 1996 9 26 DL73S962156 1 19960921 A 3350 BPS73 BATTERY PACK BOEING 737 737232 1384475 NM CABIN DISCHARGED A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 315DL 23087 EMERGENCY TRACK LIGHTING WILL NOT TURN OFF. REPLACED BATTERY PACK M9012, OP CK OK. 2 L 7 2 4F RT A16WE 1996092600341 19960926 00341 WP 1996 9 26 CKSA96139 1 19960918 A 5313 STRINGER LKHEED 1011 1011385115 5265015 WP BS 549-569 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 DURING A-3 CHECK, INSPECTION FOUND LONGERON 31 CORRODED AT STA 549 TO 569. REMOVED CORROSION AND INSTALLED FORMED AND E XTRUDED STRINGERS REPAIR 53-13-00 FIGURE 803. TASK CARD NR 82673. 2 L 7 3 4F A23WE 1996092600342 19960926 00342 WP 1996 9 26 CKSA96140 1 19960918 A 5313 STRINGER LKHEED 1011 1011385115 5265015 WP BS 569 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 DURING A-3 CHECK, INSPECTION FOUND LONGERON 32 CORRODED AT STA 569. REMOVED CORROSION AND INSTALLED FORMED AND EXTRUDED STRINGERS REPAIR 53-13-00 FIGURE 803. TASK CARD NR 82674. 2 L 7 3 4F A23WE 1996092600343 19960926 00343 WP 1996 9 26 CKSA96141 1 19960918 A 5313 STRINGER LKHEED 1011 1011385115 5265015 WP BS 589 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 DURING A-3 CHECK INSPECTION, FOUND LONGERON 32 CORRODED AT STA 589. REMOVED CORROSION AND INSTALLED FORMED AND EXTRUDED STRINGERS REPAIR 53-13-00 FIGURE 803. TASK CARD NR 82675. 2 L 7 3 4F A23WE 1996092600344 19960926 00344 WP 1996 9 26 CKSA96142 1 19960918 A 5313 STRINGER LKHEED 1011 1011385115 5265015 WP BS 599-649 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 DURING A-3 CHECK INSPECTION, FOUND LONGERON 32 CORRODED AT STA 599 TO 649. REMOVED CORROSION AND INSTALLED FORMED AND E XTRUDED STRINGERS REPAIR 53-13-00 FIGURE 803. TASK CARD NR 82676. 2 L 7 3 4F A23WE 1996092600345 19960926 00345 WP 1996 9 26 CKSA96143 1 19960918 A 5320 SHEAR TIE LKHEED 1011 1011385115 5265015 WP BS 669 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 DURING A-3 CHECK INSPECTION, FOUND SHEAR TIE CRACKED BETWEEN STRINGER 30 AND STRINGER 31 AT STA 669. REMOVED DAMAGE AND INSTALLED DOUBLER REPAIR IAW L-1011 SRM 51-50-04 FIGURE 2. TASK CARD NR 82677. 2 L 7 3 4F A23WE 1996092600346 19960926 00346 WP 1996 9 26 CKSA96144 1 19960918 A 5320 SHEAR TIE LKHEED 1011 1011385115 5265015 WP BS 669 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 DURING A-3 CHECK INSPECTION, FOUND SHEAR TIE CRACKED BETWEEN STRINGER 34 AND STRINGER 35 AT STA 669. REMOVED DAMAGE AND INSTALLED DOUBLER REPAIR IAW L-1011 SRM 51-50-04 FIGURE 2. TASK CARD NR 82679. 2 L 7 3 4F A23WE 1996092600347 19960926 00347 WP 1996 9 26 CKSA96145 1 19960918 A 5330 1507014127 SKIN LKHEED 1011 1011385115 5265015 WP BS 739 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 DURING A-3 CHECK INSPECTION, FOUND EVIDENCE OF SKIN BULGE AND CRACKED DUE TO CORROSION FS 739 L-36. REMOVED DAMAGED SEC TION OF FUSELAGE SKIN. INSTALLED FLUSH SKIN, REPAIR IAW L-1011 SRM 53-31-00 FIGURE 802. TASK CARD NR 82672. 2 L 7 3 4F A23WE 1996092600348 19960926 00348 WP 1996 9 26 CKSA96146 1 19960918 A 5320 SHEAR TIE LKHEED 1011 1011385115 5265015 WP BS 703 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 DURING A-3 CHECK INSPECTION, FOUND SHEAR TIE CRACKED BETWEEN LONGERON 33 AND LONGERON 34 STA 703. REPAIRED SHEAR TIE IA W L-1011 SRM 53-12-00 FIGURE 806. TASK NR 82690. 2 L 7 3 4F A23WE 1996092600349 19960926 00349 WP 1996 9 26 CKSA96147 1 19960918 A 5320 SHEAR TIE LKHEED 1011 1011385115 5265015 WP BS 769 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 DURING A-3 CHECK INSPECTION, FOUND SHEAR TIE CRACKED BETWEEN LONGERON 34 AND LONGERON 32 AT STA 769. REPAIRED SHEAR TIE IAW L-1011 SRM 53-12-00 FIGURE 806. TASK CARD NR 82689. 2 L 7 3 4F A23WE 1996092600350 19960926 00350 WP 1996 9 26 CKSA96148 1 19960918 A 5313 LS13417 STRINGER LKHEED 1011 1011385115 5265015 WP BS 649-697 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 DURING A-3 CHECK INSPECTION, FOUND LONGERON 31 CORRODED AT STA 649 TO 697. REMOVED CORRODED SECTION OF STRINGER AND SPL ICED IN STRINGER INSERT IAW L1011 SRM 53-13-00 FIGURE 804. TASK CARD NR 82685. 2 L 7 3 4F A23WE 1996092600351 19960926 00351 WP 1996 9 26 CKSA96149 1 19960918 A 5313 LS13417 LONGERON LKHEED 1011 1011385115 5265015 WP BS 709-729 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 DURING A-3 CHECK INSPECTION, FOUND LONGERON 31 CORRODED AT STA 709 TO 729. REMOVED CORROSION AND REPAIRED LONGERON 31 S TA 709 TO 729 IAW L1011 SRM 53-13-00 FIGURE 803. TASK CARD NR 82684. 2 L 7 3 4F A23WE 1996092600352 19960926 00352 WP 1996 9 26 CKSA96150 1 19960918 A 5320 SHEAR TIE LKHEED 1011 1011385115 5265015 WP BS 829 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 DURING A-3 CHECK INSPECTION, FOUND CRACKED SHEAR TIE STA 829 BETWEEN LONGERON 32 AND LONGERON 33. REPAIRED SHEAR TIE IA W L1011 SRM 53-12-00 FIGURE 805. TASK CARD NR 82708. 2 L 7 3 4F A23WE 1996092600353 19960926 00353 WP 1996 9 26 CKSA96151 1 19960918 A 5320 SHEAR TIE LKHEED 1011 1011385115 5265015 WP BS 865 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 DURING A-3 CHECK INSPECTION, FOUND CORRODED SHEAR TIE STA 865 BETWEEN LONGERON 31 AND LONGERON 32. REPAIRED SHEAR TIE I AW L1011 SRM 53-12-00 FIGURE 805. TASK CARD NR 82709. 2 L 7 3 4F A23WE 1996092600354 19960926 00354 WP 1996 9 26 CKSA96152 1 19960918 A 5314 1503680201 KEEL BEAM LKHEED 1011 1011385115 5265015 WP BS 983 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 DURING A-3 CHECK INSPECTION, FOUND CORROSION DAMAGE LOWER FLANGE KEELSON BEAM LBL 25 FS 983. REMOVED CORROSION DAMAGE L OWER FLANGE KEELSON BEAM LBL 25 FS 983 IAW AIA/E/2331 DRAWING DATED 9-9-96 AND 8110-3 DATED 9-16-96. TASK CARD NR 82707 . 2 L 7 3 4F A23WE 1996092600355 19960926 00355 WP 1996 9 26 CKSA96153 1 19960918 A 5347 TMS604818 SEAT TRACK LKHEED 1011 1011385115 5265015 WP BS 980-1000 DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 DURING A-3 CHECK INSPECTION, FOUND DAMAGED SECTION OF SEAT TRACK FS 980 TO FS 1000 LBL 74.5. REMOVED DAMAGED SECTION OF SEAT TRACK FS 980 TO FS 1000 LBL 74.5. REPAIRED DAMAGE IAW AIA/E/2338 DRAWING DATED 9-17-96 AND FORM 8110-3 DATED 9-17 -96. TASK CARD NR 82731. 2 L 7 3 4F A23WE 1996092600356 19960926 00356 WP 1996 9 26 CKSA96154 1 19960918 A 5330 SKIN LKHEED 1011 1011385115 5265015 WP BS 535-903 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 DURING A-3 CHECK INSPECTION, FOUND DUE TO CORROSION REPLACE BELLY SKIN FROM FS 535 TO FS 903. REPLACED LOWER FUSELAGE S KIN FROM STATION 539 TO STATION 931 STRINGER 31 TO STRINGER 35. REPAIR ORDER NR 106-034. 2 L 7 3 4F A23WE 1996092600357 19960926 00357 WP 1996 9 26 CKSA96155 1 19960914 A 5330 SKIN DOUG DC8 DC8F55 3021928 WP BS 400-420 DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 ON CREW PREFLIGHT, CARGO LOADING DAMAGE WAS NOTED ON RIGHT HAND SIDE OF FUSELAGE, JUST AFT OF A PIT DOOR, AT APPROXIMATE LONGERON 28, FUSELAGE STA 412. SKIN PUNCTURED AND LONGERON 28 DENTED AND CRACKED. REMOVED DAMAGED AREA AS REQUIRED. C OMPLIED WITH FLUSH REPAIR AND LONGERON 28 REPAIR BETWEEN RIGHT HAND FUSELAGE STA 400 TO 420 IAW AIA ENGINEERING SKETCH N R AIA/E/2333, FAA DER APPROVED 9-15-96. NO FURTHER ACTION REQUIRED. 2 L 7 4 4F 4A25 1996092600358 19960926 00358 SO 1996 9 26 SRAA960912 1 19960920 A 5753 SKIN LKHEED 382 382B 5264104 SO RT TE FLAP CRACKED A SRAA K NONE O OTHER IN INSP/MAINT 1 GL 23 916SJ 4134 ON PREFLIGHT INSPECTION, FOUND RT TRAILING EDGE SKIN BETWEEN FLAP STATION 28 AND 100 FORWARD PANEL SPLIT. REPAIRED SKIN DAMAGE AREA PER LOCKHEED SRM 51-140-12. 2 H 7 4 4T A1SO 1996092600359 19960926 00359 NM 1996 9 26 96ZZZX4887 1 19960507 A 5753 SKIN BOEING 747 747273C 1384896 NM NR 5 FORE FLAP DAMAGED A L EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 RIGHT INBOARD MID-FLAP OUTBOARD LEADING EDGE DAMAGED ADJACENT TO INBOARD FORE FLAP, OUTBOARD TRACK. ALSO, L/E RIB DAMAG ED AND CRACKED. NR 5 FORE FLAP SEQUENCE CARRIAGE ATTACH LUGS FOUND TO BE SHEARED AND FORE FLAP DETACHED FROM CARRIAGE A SSY. APPEARS TO HAVE BEEN DAMAGED FOR SOME CONSIDERABLE TIME. INBOARD FORE FLAP REMOVED. NR 5 FORE FLAP SEQUENCE CARR IAGE REMOVED AND QUARANTINED. INBD MID FLAP OTBD L/E AND DAMAGED RIB REMOVED TO FACILITATE REPAIRS. ALL ATTACH LOCATIO NS VISUALLY CHECKED FOR CRACKS AND NDT INSPECTIONS REQUESTED. SUBMITTER STATED A POSSIBLE CAUSE OF DAMAGE, FORE FLAP AT TACH LUGS CORRODED LEADING TO EVENTUAL FAILURE. SUBMITTED BY CRS: B7AY. 2 L 7 4 4F A20WE 1996092600360 19960926 00360 NM 1996 9 26 96ZZZX4888 1 19960507 A 5753 RIB BOEING 747 747273C 1384896 NM NR 5 FORE FLAP CRACKED A L EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 RIGHT INBOARD MID-FLAP OUTBOARD LEADING EDGE DAMAGED ADJACENT TO INBOARD FORE FLAP, OUTBOARD TRACK. ALSO, L/E RIB DAMAG ED AND CRACKED. NR 5 FORE FLAP SEQUENCE CARRIAGE ATTACH LUGS FOUND TO BE SHEARED AND FORE FLAP DETACHED FROM CARRIAGE A SSY. APPEARS TO HAVE BEEN DAMAGED FOR SOME CONSIDERABLE TIME. INBOARD FORE FLAP REMOVED. NR 5 FORE FLAP SEQUENCE CARR IAGE REMOVED AND QUARANTINED. INBD MID FLAP OTBD L/E AND DAMAGED RIB REMOVED TO FACILITATE REPAIRS. ALL ATTACH LOCATIO NS VISUALLY CHECKED FOR CRACKS AND NDT INSPECTIONS REQUESTED. SUBMITTER STATED A POSSIBLE CAUSE OF DAMAGE, FORE FLAP AT TACH LUGS CORRODED LEADING TO EVENTUAL FAILURE. SUBMITTED BY CRS: B7AY. 2 L 7 4 4F A20WE 1996092600361 19960926 00361 NM 1996 9 26 96ZZZX4889 1 19960507 A 5753 ATTACH LUGS BOEING 747 747273C 1384896 NM NR 5 FORE FLAP SHEARED A L EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 RIGHT INBOARD MID-FLAP OUTBOARD LEADING EDGE DAMAGED ADJACENT TO INBOARD FORE FLAP, OUTBOARD TRACK. ALSO, L/E RIB DAMAG ED AND CRACKED. NR 5 FORE FLAP SEQUENCE CARRIAGE ATTACH LUGS FOUND TO BE SHEARED AND FORE FLAP DETACHED FROM CARRIAGE A SSY. APPEARS TO HAVE BEEN DAMAGED FOR SOME CONSIDERABLE TIME. INBOARD FORE FLAP REMOVED. NR 5 FORE FLAP SEQUENCE CARR IAGE REMOVED AND QUARANTINED. INBD MID FLAP OTBD L/E AND DAMAGED RIB REMOVED TO FACILITATE REPAIRS. ALL ATTACH LOCATIO NS VISUALLY CHECKED FOR CRACKS AND NDT INSPECTIONS REQUESTED. SUBMITTER STATED A POSSIBLE CAUSE OF DAMAGE, FORE FLAP AT TACH LUGS CORRODED LEADING TO EVENTUAL FAILURE. SUBMITTED BY CRS: B7AY. 2 L 7 4 4F A20WE 1996092600362 19960926 00362 WP 1996 9 26 AALA961191 1 19960807 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1380 WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 478AA 49653 TUL - 1380 FRAME WEB HAS WORN AREA BELOW TEMPERATURE CONTROL VALVE, LT SIDE. INSTALLED DOUBLER PER SRM 53-01, FIGURE 2, SHEET 3, PAGE 8. TST: 23,096.48 HOURS. CYCLES: 13,154. (X) 2 L 7 2 4F A6WE 1996092600363 19960926 00363 WP 1996 9 26 AALA961192 1 19960807 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1380 WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 478AA 49653 TUL - 1380 FRAME, LT SIDE, WORN BELOW TEMPERATURE CONTROL VALVE. INSTALLED DOUBLER PER ESO 80559. TST: 23,096.48 HOUR S. CYCLES: 13,154. (X) 2 L 7 2 4F A6WE 1996092600364 19960926 00364 WP 1996 9 26 AALA961166 1 19960805 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 547 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 478AA 49653 TUL - CORROSION AND GOUGE ON NR 1 SEAT TRACK. ACCOMPLISHED SEAT TRACK PLUG REPAIR. TST: 23,096.48 HOURS. CYCLES: 13 ,154. (X) 2 L 7 2 4F A6WE 1996092600365 19960926 00365 NM 1996 9 26 AALA961069 1 19960712 A 5210 141N8315 STUB FRAME BOEING 757 757223 1384957 NM PASSENGER DOOR GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 653A 24611 AFW - STUB FRAME INSTALLATION, LT FORWARD NR 1 DOOR, HAD GOUGE BLENDED BEYOND 10 PERCENT OF THICKNESS PER MRB 883. TST: 15,185 HOURS. CYCLES: 5,323. (X) 2 L 7 2 4F RT A2NM 1996092600366 19960926 00366 NM 1996 9 26 AALA961070 1 19960722 A 5320 146N8522 SILL BOEING 757 757223 1384957 NM CARGO DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 653A 24611 AFW - INNER CHORD HAS CORROSION REMOVED, MATERIAL REMAINING IS BEYOND SRM LIMITS PER MRB 757-887. TST: 15,185 HOURS. CYCLES: 5,323. (X) 2 L 7 2 4F RT A2NM 1996092600367 19960926 00367 NM 1996 9 26 AALA961071 1 19960712 A 5321 146N5300 DECK PLATE BOEING 757 757223 1384957 NM BS 1720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 653A 24611 AFW - DECK PLATE HAS CORROSION BLENDED BEYOND SRM LIMITS IN VARIOUS LOCATIONS PER MRB 757-880. TST: 15,185 HOURS. CY CLES: 5,323. (X) 2 L 7 2 4F RT A2NM 1996092600368 19960926 00368 NM 1996 9 26 AALA961148 1 19960728 A 5320 141N5162 SUPPORT BOEING 757 757223 1384957 NM CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 654A 24612 AFW - GALLEY SUPPORTS WITH CORROSION REMOVED, MATERIAL REMAINING IS BEYOND SRM LIMITS. REPAIR PER MRB 757-892. TST: 1 5,172 HOURS. CYCLES: 5,361. (X) 2 L 7 2 4F RT A2NM 1996092600369 19960926 00369 NM 1996 9 26 AALA961147 1 19960728 A 5751 113N1511 RIB BOEING 757 757223 1384957 NM AILERON CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 654A 24612 AFW - AILERON SUPPORT RIB WITH CORROSION REMOVED. MATERIAL REMAINING IS BEYOND SRM LIMITS. REPAIR PER MRB 757-894. T ST: 15,172 HOURS. CYCLES: 5,361. (X) 2 L 7 2 4F RT A2NM 1996092600370 19960926 00370 NM 1996 9 26 AALA961149 1 19960728 A 5230 146N660397 DOOR BOEING 757 757223 1384957 NM CARGO COMPT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 654A 24612 AFW - DOOR EDGE DAMAGE AFT EDGE AT BOTTOM OF DOOR. REPAIR PER MRB 96C039. TST: 15,172 HOURS. CYCLES: 5,361. (X) 2 L 7 2 4F RT A2NM 1996092600371 19960926 00371 NM 1996 9 26 AALA961150 1 19960728 A 5321 146N5300 DECK PLATE BOEING 757 757223 1384957 NM BS 1680 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 654A 24612 AFW - DECK PLATE WITH CORROSION REMOVED. REMAINING MATERIAL IS BEYOND SRM LIMITS. REPAIR PER MRB 757-889. TST: 15,1 72 HOURS. CYCLES: 5,361. (X) 2 L 7 2 4F RT A2NM 1996092600372 19960926 00372 NM 1996 9 26 AALA961146 1 19960728 A 5315 146N5136 FLOOR BEAM BOEING 757 757223 1384957 NM BS 1640 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 654A 24612 AFW - FLOOR BEAM WITH CORROSION REMOVED. MATERIAL REMAINING IS BEYOND SRM LIMITS. REPAIR PER MRB 757-890. TST: 15,1 72 HOURS. CYCLES: 5,361. (X) 2 L 7 2 4F RT A2NM 1996092600373 19960926 00373 NM 1996 9 26 MZZA96068 1 19960822 A 2612 1061096125 FIRE LOOP BOEING 727 7272F9 138407D NM NR 2 ENGINE CHAFING A MZZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 13 83428 21426 TPE - FLT 5922 - DURING TAKEOFF ROLL, NR 1 ENGINE FIRE BELL ACTIVATED INTERMITTENTLY AT 80 KNOTS. ABORTED TAKEOFF BELOW 100 KNOTS. FOUND COWLING CHAFING AGAINST B-LOOP, GROUNDING LOOP AND CAUSING ALARM. REMOVED AND REPLACED DETECTION LOO P. OPS CHECK GOOD PER MM 26-11-01. (X) 2 L 7 3 4F RT A3WE 1996092600374 19960926 00374 NM 1996 9 26 MZZA96067 1 19960821 A 2750 18157013 FLAP TRANSMITTER BOEING 727 7272F9 138407D NM RT TE FLAP FAILED A MZZA A J UNSCHED LANDING DUMP FUEL J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 WP 13 83428 3316 21426 TPE - FLT 922 - OUTBOARD FLAPS FAILED TO RETRACT BEYOND 15 DEGREES AFTER TAKEOFF. FOUND OUTBOARD RT FLAP POSITION TRANS MITTER AT FAULT. REMOVED AND REPLACED RT OUTBOARD POSITION TRANSMITTER PER MM 27-52-01, ADJUSTED PER MM 27-52-11. OPER ATED FLAPS TO 40 DEGREES AND TO STOWED POSITION NUMEROUS TIMES. SYSTEM OPS CHECK GOOD. (X) 2 L 7 3 4F RT A3WE 1996092600375 19960926 00375 NM 1996 9 26 MZZA96056 1 19960628 A 3260 656021123 ACCESSORY UNIT BOEING 727 727212 138407G NM LANDING GEAR MALFUNCTIONED A MZZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 13 86430 R00655 21947 GUM - FLT 937 - ON TAKEOFF CLIMB FROM GUM, UNABLE TO MOVE GEAR HANDLE TO THE UP POSITION. FLIGHT CREW VISUALLY INSPECTE D GEAR AND CHECKED OKAY. SECOND ATTEMPT AT GEAR RETRACTION WAS OKAY. FLIGHT CREW DECIDED TO RETURN BACK TO GUM. MAINT ENANCE INSPECTED THE LANDING GEARS AND WAS UNABLE TO FIND ANY DISCREPANCY. MAINTENANCE ALSO CHECKED THE GEAR LATCH SOLE NOID BEHIND THE GEAR HANDLE AND THE SQUAT SWITCHES ON THE LANDING GEAR ASSEMBLIES AND ALL CHECKED OKAY. THE LANDING GEA R ACCESSORY WAS PRECAUTIONARY REPLACED. MAINTENANCE PERFORMED GEAR RETRACTION CHECK AND SYSTEM CHECKED NORMAL. AIRCRAF T RETURNED BACK TO SERVICE. (X) 2 L 7 3 4F A3WE 1996092600376 19960926 00376 EU 1996 9 26 Y2PA96065 1 19960820 A 2711 13150 TRIM CONTROL BOX AMD FALC20 FALCON20C5 2730107 EU E/E COMPT FAILED A A Y2PA O OTHER O OTHER DE DESCENT 1 GL 23 826AA 359A 67 MCI - FLT 18713 - AILERON TRIM RAN AWAY FULL LEFT AND CIRCUIT BREAKER TRIPPED. RESET CIRCUIT BREAKER EMERGENCY/ABNORMAL CHECK LIST FOLLOWED BY CREW. APPROACH AND LANDING WERE NORMAL, AIRCRAFT WAS CONTROLLABLE. CORRECTIVE ACTION: THE TRI M SYSTEM WAS ACTUATED NUMEROUS TIMES WITHOUT REPEAT OF THE FAILURE IN THE TRIM SYSTEM. REMOVED AND REPLACED TRIM CONTRO L BOX, AS A PRECAUTION, AND PERFORMED COMPLETE OPS CHECK IAW FALCON MM 27-10-00. OPS CHECK NORMAL. NO DEFECTS NOTED. A IRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A7EU 1996092600377 19960926 00377 EU 1996 9 26 Y2PA96066 1 19960821 A 2721 RUDDER TRIM AMD FALC20 FALCON20C5 2730107 EU EMPENNAGE MALFUNCTIONED A A Y2PA O OTHER O OTHER DE DESCENT 1 GL 23 826AA 67 YIP - FLT 18779 - DURING DESCENT INTO YIP, THE RUDDER TRIM RAN AWAY FULL RIGHT AND CIRCUIT BREAKER TRIPPED. THE AIRCRAF T CONTINUED ON TO LANDING AT ITS INTENDED DESINATION AT YIP. CORRECTIVE ACTION: COULD NOT DUPLICATE. OPS CHECKED RUDD ER TRIM SYSTEM BY OPERATION OF RUDDER TRIM SWITCH THROUGH ITS ENTIRE TRAVEL RANGE. OPS CHECKED NORMAL. NO DEFECTS NOTE D. THE AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A7EU 1996092600378 19960926 00378 EU 1996 9 26 Y2PA96068 1 19960827 A 2915 2504926V RETURN VLV AMD FALC20 FALCOND 2720304 EU HYDRAULIC SYSTEM FAILED A A Y2PA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 822AA 1868 195 YIP - FLT 19041 - JEWEL LIGHT CAME ON WHILE CLIMBING THROUGH 1,000 FEET. AI RCRAFT RETURNED TO POINT OF DEPARTURE AT YI P AND MADE AN UNSCHEDULED LANDING. NO EMERGENCY PROCEDURES WERE NECESSARY. CORRECTIVE ACTION: THE HYDRAULIC RESERVOIR PRESSURIZATION SYSTEM NON-RETURN VALVE WAS FOUND STUCK IN THE CLOSED POSITION. THE VALVE WAS REPLACED WITH A SERVICEABL E PART. PERFORMED A GROUND RUN OF ENGINE TO PRESSURIZE THE SYSTEM AND NO DEFECTS WERE NOTED. (X) 2 L 7 2 4F A7EU 1996092600379 19960926 00379 WP 1996 9 26 Y2PA96067 1 19960827 A 7711 14697 EPR LINE DOUG DC9 DC915F 3022037 WP LT ENGINE PUNCTURED A Y2PA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 199US 47153 ELP - FLT 18920 - LEFT ENGINE 'EPR' LOWER THAN RIGHT ENGINE IN CRUISE. CORRECTIVE ACTION: FOUND SMALL HOLE IN LEFT ENGI NE PT7 EPR LINE. REPLACED PT7 LINE. (X) 2 L 7 2 4F A6WE 1996092600380 19960926 00380 EU 1996 9 26 96ZZZX4890 1 19960829 A 3310 3224599630 SOCKET STBROS SD3 SD360 8100606 EU COCKPIT SHORTED A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 19 263GA SH3754 MCO/MIA - FLT 395 - PILOT REPORT: SMOKE COMING OUT OF PANEL 11P. CORRECTIVE: TROUBLESHOT, DETERMINED TO BE SHORTED EI SOCKET. REMOVED AND REPLACED SOCKET ASSEMBLY. OPS CHECK GOOD. 2 H 7 2 4T A41EU 1996092600381 19960926 00381 EU 1996 9 26 96ZZZX4891 1 19960827 A 3350 CONNECTOR STBROS SD3 SD360 8100606 EU CABIN LOOSE A GUUA K NONE L NO TEST IN INSP/MAINT 1 SO 19 263GA SH3754 FPO/MIA - FLT 5201 - PILOT REPORT: EMERGENCY FLOOR LIGHTING STRIPS BURNED OUT. CORRECTIVE: RESEATED CONNECTORS. 2 H 7 2 4T A41EU 1996092600382 19960926 00382 EU 1996 9 26 96ZZZX4892 1 19960825 A 3350 LIGHT STBROS SD3 SD360 8100606 EU CABIN FAILED A GUUA K NONE L NO TEST IN INSP/MAINT 1 SO 19 263GA SH3754 MCO/MIA - FLT 395 - PILOT REPORT: EMERGENCY FLOOR LIGHTING, 4 STRIPS BURNED OUT. CORRECTIVE: OPERATED SYSTEM, FOUND T O FUNCTION PROPERLY. COULD NOT DUPLICATE. 2 H 7 2 4T A41EU 1996092600383 19960926 00383 NM 1996 9 26 96ZZZX4893 1 19960806 A 2750 69335132 COUPLING BOEING 707 707321C 138367B NM LT TE FLAP LOOSE A A MIRA H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED AP APPROACH 1 SO 19 517MA 20017 OXO - FLT 404 - MDSD. DURING APPROACH, SPLIT FLAP ON LEFT SIDE. FOUND COUPLING LOOSE AT OUTBOARD JACKSCREW OF INBOARD FLAP. FOUND INBOARD FLAP, P/N 65-18441-51, S/N BN336, DAMAGED. REPLACED FLAP WITH OVERHAULED FLAP. REPAIRED LEFT HAND FILLET FLAP. REPAIRED LEFT HAND INBOARD AILERON. 2 L 7 4 4F 4A26 1996092600384 19960926 00384 CE 1996 9 26 NSVA96002 1 19960825 A 7931 MS3116E84S CONNECTOR AMP BEECH 1900 1900C 1154161 CE LT ENGINE BROKEN WIRE A NSVA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 15031 UC103 LEFT ENGINE OIL PRESSURE DROPPED TO ZERO PSI SHORTLY AFTER TAKEOFF. LOW OIL PRESSURE ANNUNCIATOR REMAINED EXTINGUISHED. AIRCRAFT LANDED AND RETURNED TO GATE. INSPECTION REVEALED A BROKEN WIRE AT THE TRANSMITTER CANNON PLUG. AIRCRAFT WAS FERRIED TO HYANNIS MAINTENANCE BASE AND REPLACEMENT OF CANNON PLUG WAS ACCOMPLISHED. 2 L 7 2 4T RT A24CE 1996092600385 19960926 00385 EU 1996 9 26 SIMA962411 1 19960828 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO BAY FAILED A SIMA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 21 382AE A4972 340B382 DFW - FLT 3878 - EN ROUTE FROM BTR TO DFW, THE CARGO SMOKE LIGHT ILLUMINATED. THE CREW DISCHARGED NR 1 FIRE EXTINGUISHE R PER THE CHECK LIST. SMOKE LIGHT WENT OUT AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND NO EVIDENCE OF SMOKE OR FIRE. REPLACED FORWARD AND AFT CARGO SMOKE DETECTORS. DISCHARGED BOTTLE WAS ALSO REPLAC ED. REFERENCE: OPERATOR CONTROL NR 96ZZZX4894. (X) 2 L 7 2 4T RT A52EU 1996092600386 19960926 00386 EU 1996 9 26 96ZZZX4894 1 19960828 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO BAY FAILED A SIMA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 21 382AE A4971 340B382 DFW - FLT 3878 - EN ROUTE FROM BTR TO DFW, THE CARGO SMOKE LIGHT ILLUMINATED. THE CREW DISCHARGED NR 1 FIRE EXTINGUISHE R PER THE CHECK LIST. SMOKE LIGHT WENT OUT AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND NO EVIDENCE OF SMOKE OR FIRE. REPLACED FORWARD AND AFT CARGO SMOKE DETECTORS. DISCHARGED BOTTLE WAS ALSO REPLAC ED. REFERENCE: OPERATOR CONTROL NR SIMA962411. 2 L 7 2 4T RT A52EU 1996092600387 19960926 00387 NE 1996 9 26 96ZZZX4895 2 19960808 A 8530 327628 CYLINDER CVAC 240 240* 2422601 WP PWA R2800 CB16 52026 NE LT ENGINE CRACKED A TFAA A E UNSCHED LANDING ENGINE SHUTDOWN E VIBRATION/BUFFET CL CLIMB 1 SO 15 22913 2053 316 P33526 LEFT ENGINE BEGAN CONTINUOUSLY BACKFIRING AFTER LEAVING 2,000 FEET. ALL PRESSURES WERE NORMAL, TORQUE METER FLUCTUATION S BETWEEN BACKFIRES. ENGINE WAS SHUT DOWN AND SECURED, RETURNED TO AIRPORT. NR 1 CYLINDER WAS FOUND CRACKED AT EXHAUST PORT. CYLINDER REPLACED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4R 4 R A793 E264 1996092600388 19960926 00388 CE 1996 9 26 COEA9696001 1 19960816 A 2750 RETRACT MECH CESSNA 208 208B 2073701 CE TE FLAPS OUT OF ADJUST A COEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 13 960FE 208B0075 AFTER DEPARTURE FROM GEG, THE PILOT EXPERIENCED A NUMBER OF ELECTRICAL PROBLEMS. THE TRIM WARNING LIGHT AND HORN CAME O N. THE TRIM TEST BUTTON, ELECTRICAL TRIM CIRCUIT BREAKER, AND AUTOPILOT CIRCUIT BREAKER HAD NO EFFECT. THE FLAP MOTOR C IRCUIT BREAKER TRIPPED AND ODOR OF SMOKE. NO VISUAL EVIDENCE OF SMOKE. PILOT ELECTED TO TURN BACK TO GEG. NO INCIDENT UPON LANDING. NO EVIDENCE OF FIRE FOUND. FLAP SYSTEM CURRENTLY UNDER REPAIR. CORRECTIVE ACTION: FOUND FLAP SYSTEM O UT OF RIG. SET UP/DOWN AND TRAVEL LIMIT SWITCHES. SYSTEM OPS CHECKED AND TRAVEL CHECKED GOOD. NO FAULTS OCCURRED OR C AUSED BY FLAP SYSTEM. (X) 1 H 7 1 3T A37CE 1996092600390 19960926 00390 EU 1996 9 26 96ZZZM1324 1 19960719 A 2752 791A000002 ACTUATOR AIRBUS 320 A320231 3930325 EU RT TE FLAP MALFUNCTIONED A AWXA O OTHER E VIBRATION/BUFFET AP APPROACH 1 WP 28 628AW J172 67 PHX - FLT 2247 - WHEN FLAPS FULL ARE SELECTED ON APPROACH, A HEAVY VIBRATION IS FELT THROUGHOUT THE AIRFRAME. PERFORMED VISUAL INSPECTION PER 27-54-00. NO DEFECTS NOTED AT THIS TIME AND RAN FLAP. NO VIBRATION NOTED AND VISUAL INSPECTION WHILE FLAP MOVED, NO DEFECT. OK FOR SERVICE. AIRCRAFT VIBRATION FELT WHEN FLAPS SELECTED FULL IN AIRSPEED RANGE 140-17 0 KIAS. REMOVED AND REPLACED NR 1 RIGHT FLAP ACTUATOR IAW 27-54-49, PG 401-421. OPS CHECK GOOD. AIRCRAFT SHAKES NOTIC EABLE AT FLAPS FULL POSITION (TEST FLT). REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATOR ASSEMBLY PER AMM 27-54-49, PGS 401-408. OPS CHECK GOOD. TEST FLT COMPLETED. NO ABNORMAL VIBRATION NOTED BY MAINTENANCE. REFERENCE AWXA960406. 2 L 7 2 4F RT A28NM 1996092600391 19960926 00391 1996 9 26 96ZZZM1325 4 19960821 A 2210 285T0013106 YAW DMPR MODULE BOEING 757 757225 1384959 NM NR 1 MALFUNCTIONED A A AWXA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 WP 28 914AW D00024 22208 PHX - FLT 2610 - UNCOMMANED RUDDER ON CLIMB-OUT, RUDDER KICKED TWICE, ONCE UPON TURNBACK. APPROX 1 HOUR LATER LATER, RU DDER KICKED ONCE AT 500 FEET FROM TOUCHDOWN. CHECKED YAW DAMPER PER FIM 22-21-00, PAGE 101. NO FAULTS NOTED. CHECKED THE YAW DAMPER MODULES FOR FAULT BALLS, NONE FOUND. CHECKED THE RUDDER RATIO MODULES FOR FAULTS, NONE NOTED. COMPLIED WITH RUDDER AND RUDDER TRIM SYSTEM ADJUSTMENT AND TEST PER MM 27-21-00, PAGE 501-526. OPS CHECK GOOD. COMPLIED WITH FI M TEST OF RUDDER RATIO CHANGER PER FIM MANUAL. OPS CHECK GOOD. REMOVED AND REPLACED BOTH YAW DAMPER MODULES PER BOEING ENGINEERING AS PRECAUTIONARY. REFERENCE AWXA960371. 2 L 7 2 4F RT A2NM 1996092600392 19960926 00392 NM 1996 9 26 96ZZZM1326 1 19960822 A 5242 65216357 DOOR BOEING 727 72721 1384003 NM E/E BAY UNSECURED A RYNA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 07 357QS 19259 UNABLE TO PRESSURIZE AIRCRAFT. AIRCRAFT MADE AN ATB INTO DAYTON. RESEATED E/E COMPARTMENT DOOR. 2 L 7 3 4F A3WE 1996092600393 19960926 00393 WP 1996 9 26 96ZZZM1327 1 19960822 A 2760 CONTROL BOX DOUG DC9 DC951 3022051 WP THROTTLE QUAD OVERHEAT A HALA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 WP 13 601AP 5513 5513 1605 47658 HNL - FLT 519 - STRONG ELECTRICAL BURNING SMELL IN COCKPIT. SEEMS TO BE CENTERED AT THROTTLE QUADRANT. REPLACED AUTO S POILER ACTUATOR, CONTROL BOX AND INTERLOCK BOX. THE OPERATIONAL CHECK WAS GOOD. REFERENCE HALA96122. 2 L 7 2 4F A6WE 1996092600394 19960926 00394 WP 1996 9 26 96ZZZM1328 1 19960822 A 2760 INTERLOCK BOX DOUG DC9 DC951 3022051 WP THROTTLE QUAD OVERHEAT A HALA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 WP 13 601AP 487 47658 HNL - FLT 519 - STRONG ELECTRICAL BURNING SMELL IN COCKPIT. SEEMS TO BE CENTERED AT THROTTLE QUADRANT. REPLACED AUTO S POILER ACTUATOR, CONTROL BOX AND INTERLOCK BOX. THE OPERATIONAL CHECK WAS GOOD. REFERENCE HALA96122. 2 L 7 2 4F A6WE 1996092600395 19960926 00395 NE 1996 9 26 96ZZZM1329 2 19960901 A 7250 GAS GENERATOR BEECH 1900 1900C 1154161 CE PWA PT6 PT6A67D NE RT ENG FAILED A A MASA C E ABORTED TAKEOFF ENGINE SHUTDOWN A FLAME/FIRE TO TAKEOFF 1 SW 01 76YV 7762 UC76 114018 DURING TAKEOFF ROLL AT PHX, CREW AND PASSENGERS NOTICED SPARKS AND FLAMES COMING FROM RIGHT ENGINE. CREW ABORTED TAKEOF F AND RETURNED TO GATE. MAINTENANCE FOUND COMPRESSOR FODDED. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 1996092600396 19960926 00396 NE 1996 9 26 96ZZZM1330 2 19960901 A 7230 COMPRESSOR BEECH 1900 1900C 1154161 CE PWA PT6 PT6A67D NE RT ENGINE FOD A MASA C E ABORTED TAKEOFF ENGINE SHUTDOWN A FLAME/FIRE TO TAKEOFF 1 SW 01 76YV UC76 114182 DURING TAKEOFF ROLL AT PHX, CREW AND PASSENGERS NOTICED SPARKS AND FLAME COMING FROM RIGHT ENGINE. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE FOUND COMPRESSOR FODDED. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 1996092600397 19960926 00397 NE 1996 9 26 96ZZZM1331 2 19960829 A 7250 GAS GENERATOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ENG FAILED A MASA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 01 35YV 8343 UE35 114125 DURING APPROACH TO DIA, LEFT ENGINE SURGED AND LOW OIL PRESSURE ANNUNCIATOR ILLUMINATED. CREW NOTICED SMOKE COMING FROM LEFT EXHAUST STACKS. SECURED LEFT ENGINE AND LANDED WITHOUT INCIDENT. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 1996092600398 19960926 00398 NE 1996 9 26 96ZZZM1332 2 19960829 A 7250 TURBINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ENGINE FAILED A MASA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 01 35YV 9267 1156 UE35 114031 DURING APPROACH TO DIA, LEFT ENGINE SURGED AND LOW OIL PRESSURE ANNUNCIATOR ILLUMINATED. CREW NOTICED SMOKE COMING FROM LEFT EXHAUST STACKS. SECURED LEFT ENGINE AND LANDED WITHOUT INCIDENT. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 1996092600399 19960926 00399 NM 1996 9 26 96ZZZM1333 1 19960901 A 3244 TIRE DORNER DO32 DO328100 2996000 NM RT MLG FAILED A EQGA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SW 19 350AD 52100256 3050 A RETREADED TIRE WAS INSTALLED IN THE NR 4 MAIN POSITION. THE AIRCRAFT DEPARTED HOT AND ARRIVED IN DFW. ON THE NEXT TA KEOFF DEPARTING DFW, THE TREAD DEPARTED THE NR 4 MAN TIRE DESTROYING THE RIGHT MAIN LANDING GEAR DOOR AND TORE THE BRAKE LINES OFF BOTH RIGHT BRAKES. THE PILOT ABORTED THE TAKEOFF AND TAXIED BACK IN WITHOUT FURTHER INCIDENT. THE TIRE WAS CHANGED AT DFW, THEN THE AIRCRAFT WAS FERRIED TO HOT FOR THE REMAINDER OF THE REPAIRS. (M) 2 H 7 2 4T RT A45NM 1996092600400 19960926 00400 WP 1996 9 26 96ZZZM1334 1 19960725 A 5330 SKIN DOUG DC9 DC931 3022065 WP AFT FUSELAGE CORRODED A A4JA K NONE O OTHER IN INSP/MAINT 1 SO 15 8924E 45839 FOUND CORROSION ON FUSELAGE SKIN LAP JOINTS AT LEFT TAIL AROUND TAIL CONE RELEASE PANEL. REMOVED LOWER TAIL SECTION SKI NS, FORMERS AND FRAMES AT AREAS OF CORROSION. CORROSION WAS FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR PARTS IAW AERO EO 96-335 AND RES-1-00984, SRM CHAPTERS 53-11-4, 53-31-0, 53-04-0, 51-30-2 AND 51-10-1. (M) 2 L 7 2 4F A6WE 1996092600401 19960926 00401 WP 1996 9 26 96ZZZM1335 1 19960808 A 5313 LONGERON DOUG DC9 DC915 3022036 WP BS 566 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 969Z 47001 STL - DURING OP-15, FOUND .5 INCH CRACK IN RIGHT FLANGE, LONGERON 1, STATION 566. INSTALLED LONGERON REPAIR SPLICE PER SRM 53-02, FIGURE 4. (M) 2 L 7 2 4F A6WE 1996092600402 19960926 00402 WP 1996 9 26 96ZZZM1336 1 19960809 A 2612 WKA36614 FIRE LOOP LKHEED 1011 10113851 5265010 WP NR 2 ENGINE DEFECTIVE A TWAA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 CE 05 31019 193B1066 STL - DURING CRUISE SHUT DOWN NR 2 ENGINE, S/N 4497, DUE TO OVERHEAT WARNING ON A AND B SYSTEMS. FOUND A AND B LOOP ASS EMBLY, MFG P/N WKA36614, DEFECTIVE. REPLACED LOOP ASSEMBLY. ENGINE OPERATION AND OVERHEAT INDICATION THEN CHECKED NORM AL. (M) 2 L 7 3 4F A23WE 1996092600403 19960926 00403 WP 1996 9 26 96ZZZM1337 1 19960808 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP BS 1250-1271 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 954U 49426 MCI - DURING OP-16, FOUND CORROSION ON INTERCOSTAL TOP SURFACE, FS 1250 TO FS 1271, STRINGER 25L. REMOVED CORROSION PER SRM 51-10-03 AND REPLACED INTERCOSTAL PER SRM 51-01, PAGE 1, ITEM C. (M) 2 L 7 2 4F A6WE 1996092600404 19960926 00404 NM 1996 9 26 96ZZZM1338 1 19960809 A 2933 INDICATOR BOEING 727 727231 1384079 NM 'A' HYD SYS MALFUNCTIONED A TWAA O OTHER N FALSE WARNING CR CRUISE 1 CE 05 64346 21633 ATL - FLT 518 - DURING CRUISE, CREW NOTED AN 'A' SYSTEM HYDRAULIC QUANTITY INDICATION DROP. PRESSURIZED 'A' SYSTEM HYDR AULICS AND OPERATED ALL FLIGHT CONTROLS, LEADING AND TRAILING EDGE DEVICES AND GEAR HANDLE. CHECKED GEAR WELL AREAS AND AFT AIRSTAIR AREA, NO LEAKS DETECTED. SYSTEM OPERATIONAL CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1996092600405 19960926 00405 WP 1996 9 26 96ZZZM1339 1 19960809 A 3230 ANTI RETRACT MEC DOUG DC9 DC931 3022065 WP LANDING GEAR OUT OF ADJUST A TWAA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 988Z 47134 STL - AFTER TAKEOFF WHEN LANDING GEAR WAS SELECTED TO RETRACT, LANDING GEAR DID NOT RETRACT. FOUND ANTI-RETRACT LATCH O UT OF ADJUSTMENT. RIGGED ANTI-RETRACT MECHANISM. LANDING GEAR OPERATIONS THEN CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 1996092600406 19960926 00406 NM 1996 9 26 96ZZZM1340 1 19960809 A 3260 H1010261 DNLOCK SENSOR BOEING 727 727231 1384079 NM LT MLG FAILED A TWAA O OTHER N FALSE WARNING AP APPROACH 1 CE 05 54330 20308 SLC - FLT 475 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED . CYCLED LANDING GEAR AND USED ALTERNATE EXTENSION. FOUND LEFT MAIN LANDING GEAR DOWNLOCK SENSOR, MFG P/N H10-1026-1, FAULTY. REPLACED DOWNLOCK SENSOR AND LANDING GEAR INDICATION CHECKED NORMAL. (M) 2 L 7 3 4F A3WE 1996092600407 19960926 00407 WP 1996 9 26 96ZZZM1341 1 19960810 A 3320 BALLAST LKHEED 1011 1011385115 5265015 WP GALLEY SMOKING A TWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 31029 193B1109 STL - FLT 450 - DURING CRUISE FORWARD GALLEY LIGHT FIXTURE EMMITTED SMOKE. TURNED OFF LIGHT. FOUND WORK LIGHT BALLAST, MFG P/N 11-2493-1, FAULTY. REPLACED WORK LIGHT BALLAST AND LIGHT OPERATION CHECKED NORMAL. (M) 2 L 7 3 4F A23WE 1996092600408 19960926 00408 WP 1996 9 26 96ZZZM1342 1 19960808 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 954U 49426 MCI - DURING OP-16, FOUND CORROSION AT LBL 44 CHAIR TRACK FLANGE, FS 1212, 1250, 1257, 1296. REPLACED PART PER SRM 51-1 0-01 AND TWA STANDARD PRACTICES. (M) 2 L 7 2 4F A6WE 1996092600409 19960926 00409 WP 1996 9 26 96ZZZM1343 1 19960808 A 5313 STRINGER DOUG DC9 DC982 3022082 WP BS 207 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 950U 49230 MCI - DURING OP-15, FOUND CORROSION ON FORMER, ABOVE STRINGER 30, BS 207, AFT OF DOOR. REMOVED CORROSION PER SRM 51-10- 3 AND REINSTALLED FASTENERS PER SRM 51-30-0. (M) 2 L 7 2 4F A6WE 1996092600410 19960926 00410 WP 1996 9 26 96ZZZM1344 1 19960808 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1174 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 954U 49426 MCI - DURING OP-16, FOUND CORROSION ON AFT SIDE OF FS 1174 FRAME WEB BETWEEN STRINGERS 29L AND 30L. REMOVED CORROSION P ER SRM 51-10-03 AND REPAIRED FRAME PER SRM 53-01, PAGE 3. (M) 2 L 7 2 4F A6WE 1996092600411 19960926 00411 WP 1996 9 26 96ZZZM1345 1 19960808 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 1300-1322 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 954U 49426 MCI - DURING OP-16, FOUND CORROSION ON LONGERON 25R INBOARD FLANGE AT FASTENER HOLES, STATION 1309. REPLACED TRACK STAT ION 1300 TO 1322 PER SRM 51-01, PAGE 1, ITEM C AND INSTALLED SPLICE PER SRM 53-03, FIGURE 5. (M) 2 L 7 2 4F A6WE 1996092600412 19960926 00412 WP 1996 9 26 96ZZZM1346 1 19960808 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1211-1320 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 954U 49426 MCI - DURING OP-16, FOUND CORROSION AT FLOOR TRACK, STATION 1211 TO 1320, RIGHT SIDE. REPLACED FLOOR TRACK PER SRM 51-0 1, PAGE 1 AND TWA STANDARD PRACTICES. (M) 2 L 7 2 4F A6WE 1996092600413 19960926 00413 WP 1996 9 26 96ZZZM1347 1 19960808 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 200 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 954U 49426 MCI - DURING OP-16, FOUND CORROSION ON FLOOR SUPPORT AND STRUCTURE, FS 200, RBL 6 TO RBL 42. REPAIRED BY INSTALLING NEW FLOOR SUPPORT ANGLE PER SRM 57-01. 2 L 7 2 4F A6WE 1996092600414 19960926 00414 WP 1996 9 26 96ZZZM1348 1 19960808 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1309 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 954U 49426 MCI - DURING OP-16, FOUND CORROSION ON LOWER SIDE OF FRAME, STATION 1309, LONGERON 25R TO 26R. REPAIRED PER SRM 53-03, FIGURE 2A AND TWA STANDARD PRACTICES. (M) 2 L 7 2 4F A6WE 1996092600415 19960926 00415 WP 1996 9 26 96ZZZM1349 1 19960808 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 1309 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 954U 49426 MCI - DURING OP-16, FOUND CORROSION ON LONGERON 5-30 TOP LEFT FLANGE, AFT OF FORMER BS 1309. REPAIRED PER SRM 51-01. ( M) 2 L 7 2 4F A6WE 1996092600416 19960926 00416 WP 1996 9 26 96ZZZM1350 1 19960808 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1311-1320 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 954U 49426 MCI - DURING OP-16, FOUND CORROSION AT RIGHT FLOOR TRACK, STATION 1311 TO STATION 1320. REMOVED AND REPLACED FLOOR TRAC K PER SRM 51-01 AND TWA STANDARD PRACTICES. (M) 2 L 7 2 4F A6WE 1996092600417 19960926 00417 WP 1996 9 26 96ZZZM1351 1 19960726 A 3350 58222 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 405EA 47688 STL - DURING OVERNIGHT MAINTENANCE, FOUND AISLE EGRESS LIGHTS INOPERATIVE AT SEAT ROW 5 THROUGH 11. FOUND POWER SUPPLY, MFG P/N 5822-2, WEAK. REPLACED POWER SUPPLY AND SYSTEM OPERATION CHECKED NORMAL. 2 L 7 2 4F A6WE 1996092600418 19960926 00418 NM 1996 9 26 96ZZZM1352 1 19960728 A 3210 657276177 LANDING GEAR BOEING 727 727231 1384079 NM LT MLG FRACTURED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54341 21628 JFK - DURING PREFLIGHT, FOUND LEFT MAIN LANDING GEAR, MFG P/N 65-72761-77, FRACTURED AT AFT TRUNNION BEARING. REPLACED LEFT MAIN LANDING GEAR ASSEMBLY. LANDING GEAR OPERATION THEN CHECKED NORMAL. (M) 2 L 7 3 4F A3WE 1996092600419 19960926 00419 WP 1996 9 26 96ZZZM1353 1 19960805 A 3350 58222 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 983Z 47411 STL - DURING CRUISE, EMERGENCY EGRESS LIGHTS ILLUMINATED INTERMITTENTLY. REMOVED AND REPLACED POWER SUPPLY, MFG P/N 582 2-2. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996092600420 19960926 00420 WP 1996 9 26 96ZZZM1354 1 19960805 A 2160 8564111 GASKET DOUG DC9 DC983 3022083 WP TAIL COMPT FAILED A TWAA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 9302B 49528 STL - DURING CLIMB-OUT, TAIL COMPARTMENT OVERHEAT LIGHT ILLUMINATED. REMOVED AND REPLACED THERMOSTAT GASKET, MFG P/N 85 6411-1. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1996092600421 19960926 00421 NM 1996 9 26 96ZZZM1355 1 19960801 A 2611 30231R4B SMOKE DETECTOR BOEING 747 747131 1384881 NM CARGO COMPT DEFECTIVE A TWAA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 CE 05 93109 19675 CDG - DURING CRUISE, FORWARD CARGO COMPT SMOKE DETECTOR WARNING LIGHT ILLUMINATED. DISCHARGED EXTINGUISHING AGENT. FOU ND DEFECTIVE SMOKE DETECTOR, MFG P/N 30231R4B. REPLACED EXTINGUISHING AGENT BOTTLE, REPLACED SMOKE DETECTOR AND FORWARD CARGO COMPARTMENT SMOKE DETECTION SYSTEM OPERATION CHECKED NORMAL. (M) 2 L 7 4 4F A20WE 1996092600422 19960926 00422 NM 1996 9 26 96ZZZM1356 1 19960812 A 2121 732591E FAN BOEING 767 767231 1385131 NM FLT DECK FAILED A TWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 05 610TW 22573 BOS - DURING CLIMB, FORWARD EXHAUST COOLING FAN, MFG P/N 732591E, OVERHEATED AND EMITTED SMOKE ELECTRICAL ODOR TO FLIGHT DECK. TURNED OFF COOLING FAN. FOUND COOLING FAN SHAFT BEARINGS WORN. REPLACED FORWARD EXHAUST COOLING FAN AND OPERAT ION CHECKED NORMAL. (M) 2 L 7 2 4F RT A1NM 1996092600423 19960926 00423 WP 1996 9 26 96ZZZM1357 1 19960806 A 3310 FLOOD LIGHT LKHEED 1011 10113851 5265010 WP FLIGHT DECK SMOKING A TWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 11004 193B1016 STL - DURING CRUISE CAPTAIN'S SIDE FLOOD LIGHT RHEOSTAT TRANSFORMER EMITTED SMOKE. CIRCUIT BREAKER WAS PULLED. REMOVED AND REPLACED CAPTAIN'S FLOOD LIGHT RHEOSTAT TRANSFORMER, MFG P/N 26446. OPERATIONAL CHECK NORMAL. (M) 2 L 7 3 4F A23WE 1996092600424 19960926 00424 NM 1996 9 26 96ZZZM1358 1 19960805 A 2140 CLAMP BOEING 727 727231 1384079 NM HEAT EXCHANGER LOOSE A TWAA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 54325 20232 JFK - DURING CLIMB-OUT, NR 2 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. SECURED AND TIGHTENED HEAT EXCHANGER CLAMP. OPER ATIONAL CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1996092600425 19960926 00425 WP 1996 9 26 96ZZZM1359 1 19960723 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 935 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 STL - DURING OP-15, FOUND SKIN CORROSION AFT OF CARGO DOOR BETWEEN LONGERON 26R AND 27R, STATION 935. REPAIRED PER ARA 10375. (M) 2 L 7 2 4F A6WE 1996092600426 19960926 00426 WP 1996 9 26 96ZZZM1360 1 19960726 A 5320 DOUBLER DOUG DC9 DC931 3022065 WP BS 1076 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 STL - DURING OP-15, FOUND .5 INCH CRACK INSIDE REPAIR DOUBLER INSIDE LONGERON 2L, STATION 1076. REPAIRED PER SRM 52-02, PAGE 8. 2 L 7 2 4F A6WE 1996092600427 19960926 00427 WP 1996 9 26 96ZZZM1361 1 19960726 A 5320 DOUBLER DOUG DC9 DC931 3022065 WP BS 1076 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 STL - DURING OP-15, FOUND .5 INCH CRACK INSIDE REPAIR DOUBLER INSIDE LONGERON 2R, STATION 1076. REPAIRED PER SRM 53-02, PGES 8-10, SECTION 2. (M) 2 L 7 2 4F A6WE 1996092600428 19960926 00428 WP 1996 9 26 96ZZZM1362 1 19960805 A 5320 BELT RING DOUG DC9 DC951 3022051 WP BS 794 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 415EA 47749 STL - DURING SPECIAL CHECK, FOUND .25 INCH CRACK AT LONGERON 3R BELT RING, STATION 794. REPAIRED PER SRM 53-02, PAGE 2A , FIGURE 2. 2 L 7 2 4F A6WE 1996092600429 19960926 00429 WP 1996 9 26 96ZZZM1363 1 19960808 A 3350 BATTERY PACK DOUG DC9 DC915 3022036 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 970Z 45772 STL - DURING CRUISE, EMERGENCY EGRESS LIGHTS ILLUMINATED. REMOVED, RECHARGED AND INSTALLED BATTERY PACK. OPERATIONAL CH ECK NORMAL. 2 L 7 2 4F A6WE 1996092600430 19960926 00430 NM 1996 9 26 96ZZZM1364 1 19960808 A 2530 41200011 WARMING PAD BOEING 727 727231 1384079 NM GALLEY SMOKING A TWAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 54348 21967 STL - DURING CRUISE, D-GALLEY COFFEEMAKER WARMING PAD EMITTED SMOKE. REMOVED AND REPLACED COFFEEMAKER, MFG P/N 412-0001 -1. OPERATIONAL CHECK NORMAL. 2 L 7 3 4F A3WE 1996092600431 19960926 00431 WP 1996 9 26 96ZZZM1365 1 19960808 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 1211 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 950U 49230 MCI - DURING OP-15, FOUND FLOOR SUPPORT CORROSION, LONGERON 28R, STATION 1211. REPLACED SUPPORT PER SRM 51-30-0. 2 L 7 2 4F A6WE 1996092600432 19960926 00432 WP 1996 9 26 96ZZZM1366 1 19960813 A 2530 5316E OVEN DOUG DC9 DC982 3022082 WP GALLEY SMOKING A TWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 953U 49267 JFK - DURING CRUISE, GALLEY OVEN EMITTED SMOKE. SHUT DOWN OVEN. FOUND DEFECTIVE FAN MOTOR. REPLACED OVEN, MFG P/N 531 6E. OVEN OPERATION THEN CHECKED NORMAL. 2 L 7 2 4F A6WE 1996092600433 19960926 00433 WP 1996 9 26 96ZZZM1367 1 19960807 A 3350 0105606003 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9401W 53137 STL - DURING PREFLIGHT, EGRESS LIGHT STRIPS BETWEEN ROWS 12 THROUGH 16 WERE INOPERATIVE. REMOVED AND REPLACED WORN LIGH T STRIP, MFG P/N 0105606-003. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1996092600434 19960926 00434 WP 1996 9 26 96ZZZM1368 1 19960802 A 2150 CLAMP DOUG DC9 DC951 3022051 WP RT PACK BROKEN A TWAA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 412EA 47733 STL - TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF. REMOVED AND REPLACED BROKEN CLAMP AT R IGHT PACK HOT AIR DUCT AND RETORQUED LOOSE CLAMP AT LEFT PACK PRIMARY HEAT EXCHANGER. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996092600435 19960926 00435 NM 1996 9 26 96ZZZM1369 1 19960815 A 5260 69211121 BUNGEE ASSEMBLY BOEING 727 727222 1384073 NM AIRSTAIR WORN A RYNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 07 7643U 20037 AFT AIRSTAIR ANNUNCIATOR LIGHT CAME ON AFTER TAKEOFF, LIGHT WENT OFF AFTER LANDING. REMOVED AND REPLACED BUNGEE ASSEMBL Y. OPS CHECKED GOOD. 2 L 7 3 4F A3WE 1996092600436 19960926 00436 EU 1996 9 26 96ZZZM1370 1 19960812 A 2611 004WS00 WEU SAAB SF340 340B 7860101 EU AVIONICS RACK FAILED A NVEA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SO 03 280AE 340B280 FLT 4935 - JFK - CREW REPORTS, AFT CARGO SMOKE CWP CAPTION ILLUMINATED, THEN WENT OUT AND CAME BACK ON. CREW FIRE ONE E XTINGUISHER AND RTG. DECLARED EMERGENCY, CFR FOUND NO SMOKE OR FIRE INDICATIONS. LANDED WITHOUT FURTHER INCIDENT. REM OVED AND REPLACED WARNING ELECTRONIC UNIT. INSPECTED THE SMOKE DETECTOR AND WIRING. (M) 2 L 7 2 4T RT A52EU 1996092600437 19960926 00437 EU 1996 9 26 96ZZZM1371 1 19960812 A 2611 06232855001 SMOKE DETECTOR FENWAL 72111211000 SAAB SF340 340B 7860101 EU CARGO COMPT FAILED A NVEA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SO 03 280AE A4773 340B280 FLT NR 4931 - CMH - CREW REPORTS, AFT CARGO SMOKE CWP CAPTION ILLUMINATED. CREW SHOT AFT FIRE EXTINGUISHING SYSTEM. DE CLARED EMERGENCY, CFR ARRIVED AND FOUND NO SMOKE OR FIRE INDICATIONS. LANDED WITHOUT FURTHER INCIDENT. REMOVED AND REP LACED AFT SMOKE DETECTOR AND FIREBOTTLE. (M) 2 L 7 2 4T RT A52EU 1996092600438 19960926 00438 EU 1996 9 26 96ZZZM1372 1 19960908 A 3350 321454 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 636AW 107 098 PHX - FLT 2274 - DURING ROUTINE MAINTENANCE CHECK, EMERGENCY EXIT LIGHT TEST FAILED. REMOVED AND REPLACED EMERGENCY LIG HT BATTERY FORWARD LEFT OVERWING. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT FWD LEFT OVERWING. SYSTEM CHARGED, OPERATIONS CHECK GOOD. REFERENCE AWXA960479. 2 L 7 2 4F RT A28NM 1996092600439 19960926 00439 NM 1996 9 26 96ZZZM1373 1 19960814 A 3350 20121 CHARGER BOEING 757 757225 1384959 NM CABIN INOP A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 914AW 2221 22208 PHX - FLT 2020 - DURING ROUTINE MAINTENANCE CHECK, FOUND AFT CABIN SECTION OF EMERGENCY LIGHTS INOP AND BATTERY PACK AT L-2 DOOR NOT CHARGING. REMOVED AND REPLACED BATTERY PACK IN AFT SECTION. OPS GOOD. REMOVED AND REPLACED CHARGER AT L- 2 DOOR. OPS GOOD. REFERENCE AWXA960429. 2 L 7 2 4F RT A2NM 1996092600440 19960926 00440 EU 1996 9 26 A21A32002 1 19960830 A 3260 602EN166 SWITCH FOKKER F28 F28MK4000 4990810 EU NLG MALFUNCTIONED A A21A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 17 499US 11182 AIR TURN BACK, NOSE GEAR GREEN DOWN LIGHT WOULD NOT GO OUT. JACKED AIRCRAFT AND CLEANED DOWNLOCK SWITCH, GEAR SWING OPS CHECKED OK. ON ARRIVAL AT PSP PM, SAME DAY SWITCH STUCK AGAIN. CAPTAIN REQUESTED TOWER CHECK AND OK. MANUAL INDICATI ON OK. AIRCRAFT FERRIED TO FAT. SWITCH REPLACED AND GEAR SWING CHECK OK. (M) 2 L 7 2 4F RT A20EU 1996092600441 19960926 00441 NM 1996 9 26 AALA961005 1 19960703 A 3210 DEFLECTOR BOEING 727 727223 1384074 NM LT MLG OUT OF ADJUST A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 874AA 21386 FLT 443 - EN ROUTE MIA/CLE - DURING CRUISE, ODOR OF BURNING RUBBER IN CABIN, IN THE AREA OF MAIN W/W'S, W/NO OTHER ABNOR M IND'S. A/C DIVERTED TO CLT AND LANDED OVERWEIGHT W/O INCIDENT. ACCOMP EXT CHECK W/NO DEFECTS FOUND. CHECKED CABIN I NTERIOR W/NO DEFECTS FOUND. CHECKED E/E COMPT AND OPERATED APU W/NO DEFECTS FOUND. ACCOMP GRD ENG RUN AND OPERATED ENG BLEEDS, ACCOMP PRESS CHK AND OPERATED PACKS TO FULL HOT AND FULL COLD W/NO DEFECTS FOUND. ACCOMP OVERWEIGHT LANDING CH K W/NO DEFECTS FOUND. A/C PROCEEDED CLT/CLE WITH NO ODOR NOTED. SUBSEQUENTLY AT CLE, ADJUSTED LT MLG SLUSH DEFELECTOR TO CORRECT INTERFERENCE BETWEEN LT MAIN NR 2 TIRE AND LT MLG SLUSH DEFLECTOR. SYS GRD CHK'D NORM OPS. (M) 2 L 7 3 4F A3WE 1996092600442 19960926 00442 EU 1996 9 26 AALA961196 1 19960808 A 3231 715391 VALVE FOKKER F28 F28MK0100 4990807 EU NLG DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 1435D 11425 DFW - FLT 2051 - AFTER TAKEOFF DFW, WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR DID NOT RETRACT. AIRCRAFT RETURNED T O DFW AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR DOOR SELECTOR VALVE. ACCOMPLISHED NOSE GEAR RETRACTION C HECK WITH NO DEFECTS FOUND. SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1996092600443 19960926 00443 NM 1996 9 26 AALA961207 1 19960813 A 3350 0201922001 HOUSING BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 372AA 25199 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 4B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT HOUSING AT PAX SEAT 4B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1996092600444 19960926 00444 NM 1996 9 26 AALA961217 1 19960814 A 3350 0201922001 HOUSING BOEING 767 767223 1385123 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 312AA 22315 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 3H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT HOUSING AT PAX SEAT 3H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1996092600445 19960926 00445 NM 1996 9 26 AALA961221 1 19960816 A 3350 CONNECTORS BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 642AA 24600 BOS - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTING FROM LAST ROW FIRST CLASS CABIN TO OVERWING E XIT, L2 DOOR EMERGENCY EXIT SIGN, R2 DOOR EMERGENCY EXIT SIGN INOPERATIVE. RESEATED CONNECTIONS AT MID GALLEY FLOOR AND RIGHT FORWARD OVERWING DOOR, CLEANED CONNECTORS AT DOOR SIGNS. SYSTEMS GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1996092600446 19960926 00446 NM 1996 9 26 AALA961222 1 19960816 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 868AA 21373 ATL - DURING OVERNIGHT MAINTENANCE, FOUND THE FORWARD LEFT EXTERIOR EMERGENCY SLIDE LIGHT INOPERATIVE. REPLACED THE M98 2 MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996092600447 19960926 00447 NM 1996 9 26 AALA961225 1 19960818 A 3350 A3060698101 CONNECTOR BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 662AA 25296 SFO - DURING OVERNIGHT, MAINTENANCE FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS IN THE FORWARD CABIN INTERMITTENT. REPLA CED CONNECTOR AT RIGHT SIDE FIRST CLASS SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1996092600448 19960926 00448 NM 1996 9 26 AALA961226 1 19960818 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 633AA 24591 DFW - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS DISLODGED. REPLACED EMERGENCY E XIT FLOOR PATH LIGHT STRIP AND BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1996092600449 19960926 00449 NM 1996 9 26 AALA961227 1 19960818 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 708AA 22465 MIA - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY EXIT FLOOR PATH LIGHTING IN FIRST CLASS INOPERATIVE. REPAIRED WIRES TO THE EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996092600450 19960926 00450 NM 1996 9 26 AALA961234 1 19960819 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 352AA 24033 SFO - EMERGENCY EXIT LIGHT AT SEAT 27B INOPERATIVE. RECONNECTED LOOSE CONNECTOR AND SECURED AT SEAT 27B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1996092600451 19960926 00451 NM 1996 9 26 AALA961236 1 19960819 A 3232 26702888 ACTUATOR BOEING 757 757223 1384957 NM LT MLG DOOR DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 606AA 27057 DFW - UPON GEAR RETRACTION, THE AMBER GEAR LIGHT REMAINED ON AND RECIEVED AND EICAS GEAR DISAGREE MESSAGE. RETURNED TO NORMAL AT 235 KNOTS DURING DESCENT. RETURNED AND LANDED DFW WITHOUT INCIDENT BUT OVERWEIGHT. REPLACED LEFT MAIN GEAR D OOR ACTUATOR. ACCOMPLISHED LANDING GEAR RETRACTION. ACCOMPLISHED OVERWEIGHT INSPECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1996092600452 19960926 00452 NM 1996 9 26 AALA961240 1 19960820 A 3397 WIRE BOEING 767 767323 1385205 NM RT FWD DOOR LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 374AA 25201 SFO - DURING OVERNIGHT MAINTENANCE, FOUND THE RIGHT FORWARD ENTRY DOOR OUTSIDE EMERGENCY EXIT LIGHT INOPERATIVE. TIGHTE NED LOOSE GROUND WIRE ON RIGHT FORWARD ENTRY DOOR OUTSIDE EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1996092600453 19960926 00453 NM 1996 9 26 AALA961243 1 19960821 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 660AM 25294 DFW - DURING OVERNIGHT CHECK, FOUND THE RIGHT AFT OVER WATER EMERGENCY EXIT IDENTIFIER INOPERATIVE. REPLACED LIGHT ASSE MBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1996092600454 19960926 00454 NM 1996 9 26 AALA961244 1 19960820 A 3350 1000679 LIGHT BOEING 727 727227 1384078 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 727AA 20734 DFW - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT LIGHT ABOVE THE R1 DOOR INOPERATIVE. REPLACED THE EMERGENCY EXIT LIGHT ABOVE R1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996092600455 19960926 00455 NM 1996 9 26 AALA961245 1 19960822 A 3350 CONNECTOR BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 6819 19494 DFW - DURING OVERNIGHT MAINTENANCE, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS AT ROWS 27 AND 28 INOPERATIVE. REPAIRED CONNECTOR AT ROW 27. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996092600456 19960926 00456 NM 1996 9 26 AALA961254 1 19960826 A 5321 FLOOR PAN BOEING 727 727223 1384074 NM BS 1175 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - FOUND CORROSION ON LAV FLOOR PAN, AT STATION 1175 RBL 34-36. REMOVED CORRODED SECTION OF FLOOR PAN AND INSTALLED REPAIR DOUBLER PER SRM 51-40-2 FIG 1 PAGE 6. (M) 2 L 7 3 4F A3WE 1996092600457 19960926 00457 NM 1996 9 26 AALA961255 1 19960826 A 2810 TANK LANDING BOEING 727 727223 1384074 NM STUB TANK CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - FOUND CORROSION ON LEFT STUB TANK PLATE 7340 LANDING. REMOVED CORROSION AND REPAIRED PER EOS 11697 DATE 8-21-96. (M) 2 L 7 3 4F A3WE 1996092600458 19960926 00458 NM 1996 9 26 AALA961256 1 19960826 A 5321 FLOOR PAN BOEING 727 727223 1384074 NM BS 1175 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - FOUND RIGHT AFT LAVATORY (FLOOR PANEL) CORRODED AT SEVERAL AREAS, (FWD TO AFT) AREA MARKED. INSTALLED TYPICAL WEB REPAIR SRM 51-40-2 PG 1-6. (M) 2 L 7 3 4F A3WE 1996092600459 19960926 00459 NM 1996 9 26 AALA961257 1 19960827 A 5321 FLOOR PAN BOEING 727 727223 1384074 NM BS 1170 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - FOUND AREA OF RIGHT AFT LAV FLOOR PAN WEB HAS HEAVY CORROSION IN AREA OF HOLE FOR DUMP SHUTE FLANGE. REMOVED CORR ODED AREA. INSTALLED REPAIR PER SRM 51-40-2, PG 1-6. (M) 2 L 7 3 4F A3WE 1996092600460 19960926 00460 NM 1996 9 26 AALA961258 1 19960826 A 5321 FLOOR PAN BOEING 727 727223 1384074 NM BS 1133 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - FOUND CORROSION ON FLOOR PAN RIGHT AFT LAV. CUT OUT CORRODED AREA AND INSTALLED DOUBLER PER SRM 51-40-2 PG 1-6. ( M) 2 L 7 3 4F A3WE 1996092600461 19960926 00461 WP 1996 9 26 AALA961263 1 19960825 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 224AA 49174 SEA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRI P BY FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996092600462 19960926 00462 NM 1996 9 26 AALA961265 1 19960827 A 5315 FLOOR BEAM BOEING 727 727227 1384078 NM BS 1166 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 716AA 20608 TUL - FOUND CORROSION ON FLOOR BEAM UPPER FLANGE STATION 1166, LBL 39. CUT OUT CORRODED AREA AND REPAIRED PER SRM 53-10 -8 PG 9C-9E. (M) 2 L 7 3 4F A3WE 1996092600463 19960926 00463 NM 1996 9 26 AALA961266 1 19960827 A 5730 SKIN BOEING 727 727227 1384078 NM WING CTR SECT CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 716AA 20608 TUL - FOUND CORROSION ON SKIN INBOARD OF LT PRIMARY HEAT EXCHANGER. REPAIRED PER ESO 11697, DATED 8-9-96. (M) 2 L 7 3 4F A3WE 1996092600464 19960926 00464 NM 1996 9 26 AALA961268 1 19960827 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 480 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 716AA 20608 TUL - FOUND CORROSION ON SKIN AND STRINGER. REMOVED FASTENERS, CLEANED SKIN. INSTALLED STRINGER REPAIR PER SRM 53-10-5 FIG 1. (M) 2 L 7 3 4F A3WE 1996092600465 19960926 00465 NM 1996 9 26 AALA961269 1 19960827 A 5330 SKIN BOEING 727 727227 1384078 NM BS 670-680 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 716AA 20608 TUL - FOUND SKIN BULGED AND CRACKED STATION 670-680 AT STRINGER 26R AT SKIN LAP. CUT OUT CORROSION AND INSTALLED DOUBLE R PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 1996092600466 19960926 00466 NM 1996 9 26 AALA961283 1 19960829 A 5330 SKIN BOEING 727 727223 1384074 NM BS 468 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 850AA 20991 TUL - FOUND SKIN DENTED STATION 468 BELOW, STRINGER 24L. CUT OUT DAMAGED AREA, FABRICATED DOUBLER AND FILLER. REPAIRED DENTED AREA, STATION 468 BELOW, STRINGER 24L PER SRM. (M) 2 L 7 3 4F A3WE 1996092600467 19960926 00467 NM 1996 9 26 AALA961284 1 19960829 A 5320 DOOR FRAME BOEING 727 727223 1384074 NM CARGO DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 850AA 20991 TUL - FORWARD CARGO DOOR CUTOUT LOWER FRAME WEB HAS CORROSION IN SKIN, STATION 588, 605 AND 577. INSTALLED NEW MANUFACT URED WEB PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1996092600468 19960926 00468 NM 1996 9 26 AALA961285 1 19960829 A 5311 FRAME BOEING 727 727223 1384074 NM BS 303.9 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 850AA 20991 TUL - FOUND HEAVY CORROSION ON FRAME STATION NR 303.9 WL 153.5, WHERE SKATE ANGLE WAS REMOVED. REMOVED CORROSION, FABRI CATED REPAIR PARTS TREATED AND PRIMED PER 51-10-6. INSTALLED FASTENERS PER 51-30. (M) 2 L 7 3 4F A3WE 1996092600469 19960926 00469 NM 1996 9 26 AALA961287 1 19960829 A 5741 BOTTLE PIN BOEING 727 727223 1384074 NM LT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 850AA 20991 TUL - FOUND LEFT WING STATION 870 BOTTLE PIN HAS CORROSION ON PIN. INSTALLED NEW BOTTLE PIN PER 57-41-1. (M) 2 L 7 3 4F A3WE 1996092600470 19960926 00470 NM 1996 9 26 AALA961288 1 19960829 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 487 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 850AA 20991 TUL - FOUND STRINGER 28L HAS CORROSION, STATION 487. REPAIRED PER SRM 53-10-3 FIG 1. (M) 2 L 7 3 4F A3WE 1996092600471 19960926 00471 NM 1996 9 26 AALA961289 1 19960829 A 5330 SKIN BOEING 727 727223 1384074 NM BS 500-524 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 850AA 20991 TUL - FOUND SKIN HAS LIGHT CORROSION. INSTALLED EXTERNAL DOUBLER IAW SRM 53-30-3 FIG 1 SHEET 4. (M) 2 L 7 3 4F A3WE 1996092600472 19960926 00472 NM 1996 9 26 AALA961291 1 19960829 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 300 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 850AA 20991 TUL - FOUND CORROSION AND BULGED SEALANT IN LEFT NLG TRUNNION TORQUE BOX WELL BILDGE AREA, STATION 300. CORROSION ON SK ATE ANGLE IN NLG LEFT TORQUE BOX. REMOVED AND REPLACED LEFT SKATE ANGLE WITH NEW PART PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1996092600473 19960926 00473 NM 1996 9 26 AALA961292 1 19960829 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 560-564 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 850AA 20991 TUL - FOUND CORRODED STRINGER 27R STATION 560-564. CUT OUT CORRODED SECTION OF STRINGER AND INSTALLED STRINGER REPAIR P ER SRM 53-10-3 FIG 1. (M) 2 L 7 3 4F A3WE 1996092600474 19960926 00474 NM 1996 9 26 AALA961293 1 19960829 A 5330 SKIN BOEING 727 727223 1384074 NM BS 440 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 850AA 20991 TUL - FOUND SMALL GOUGE IN SKIN AT STATION 440, STRINGER 19R. ROUTED OUT DAMAGED AREA AND REPAIRED PER SRM 53-30-3 FIG 14. (M) 2 L 7 3 4F A3WE 1996092600475 19960926 00475 NM 1996 9 26 ASAA9610117 1 19960827 A 3350 6013211 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING MAINTENANCE CHECK, THE L2 AND R2 DOOR EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996092600476 19960926 00476 NM 1996 9 26 ASAA961267 1 19960827 A 5730 SKIN BOEING 727 727227 1384078 NM WING CTR SECT CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 716AA 20608 TUL - FOUND CORROSION ON SKIN INBOARD OF RT PRIMARY HEAT EXCHANGER. REPAIRED PER ESO 11697 DATED 8-9-96. (M) 2 L 7 3 4F A3WE 1996092600477 19960926 00477 WP 1996 9 26 ASAA9680181 1 19960827 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 950AS 53023 SEA - DURING MAINTENANCE CHECK, THE AFT FIVE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED LIGH TS AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996092600478 19960926 00478 NM 1996 9 26 AWXA96034 1 19960803 A 5347 BAC1520792 SEAT TRACK BOEING 737 737277 1384570 NM BS 337 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 PAE - DURING ROUTINE SCHEDULED C-8 MAINTENANCE CHECK, FOUND CORROSION IN SEAT TRACK WELL BS 337, RBL 45, WL 208. REMOVE D AND REPLACED SEAT TRACK FROM BS 328 TO 380, RBL 45, WL208. (M) 2 L 7 2 4F RT A16WE 1996092600479 19960926 00479 NM 1996 9 26 AWXA960382 1 19960807 A 5320 DOOR FRAME BOEING 737 737277 1384570 NM CARGO DOOR CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 PAE - FLT 7803 - DURING ROUTINE SCHEDULED C-8 MAINTENANCE CHECK, FOUND CRACK IN FRAME AT NR 5 STOP PAD AFT CARGO DOOR FW D FRAME. REPAIRED IAW 737 SRM 51-30-02 AND 51-40-3. (M) 2 L 7 2 4F RT A16WE 1996092600480 19960926 00480 NM 1996 9 26 AWXA960385 1 19960804 A 5315 FLOOR BEAM BOEING 737 737277 1384570 NM BS 344 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 PAE - FLT 7803 - DURING ROUTINE SCHEDULED C-8 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM BS 344, LBL 15 - 30, WL 2 08. REMOVED, FABRAICATED, INSTALLED REPAIR PARTS PER SRM 53-10-9. (M) 2 L 7 2 4F RT A16WE 1996092600481 19960926 00481 NM 1996 9 26 AWXA960386 1 19960806 A 5313 STRINGER BOEING 737 737277 1384570 NM BS 945 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 PAE - FLT 7803 - DURING ROUTINE SCHEDULED C-8 MAINTENANCE CHECK, FOUND EVIDENCE OF CORROSION, FUSELAGE SKIN BULGING AT B S 945, STR 26L. REPAIRED CORRODED STRINGER PER SRM 53-30-3, FIG 6 AND SRM 53-10-3, FIG 1. (M) 2 L 7 2 4F RT A16WE 1996092600482 19960926 00482 NM 1996 9 26 AWXA960387 1 19960803 A 5347 SEAT TRACK BOEING 737 737277 1384570 NM BS 347 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 DURING ROUTINE SCHEDULED C-8 MAINTENANCE CHECK, FOUND CORROSION ON SEAT TRACK FLANGE BS 347, LB 25, WL 208. REMOVED, FA BRICATED AND INSTALLED REPAIR PARTS PER SRM 51-30-2. (M) 2 L 7 2 4F RT A16WE 1996092600483 19960926 00483 NM 1996 9 26 AWXA960393 1 19960814 A 3350 20131A BATTERY PACK BOEING 757 757225 1384959 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 914AW 22208 PHX - FLT 2020 - DURING ROUTINE MAINTENANCE CHECK, FOUND ENTRY AFT CABIN EMERGENCY LIGHTS INOP. SHOT IN WIRING KEPT FUS ES IN THE CHARGER OPENING UP. DEACTIVATED SEAT ROWS AND RECONNECTED EACH SEAT INDIVIDUALLY UNTIL ROW WAS IDENTIFIED. R EPAIRED WIRING CHAFED ON SEAT FRAME. OPS CHECK OK. REMOVED AND REPLACED BATTERY PACK IN AFT SECTION. OPS OK. (M) 2 L 7 2 4F RT A2NM 1996092600484 19960926 00484 EU 1996 9 26 AWXA960396 1 19960823 A 2450 ASD000103060000 BUS BAR AIRBUS 320 A320231 3930325 EU E/E COMPT DAMAGED A AWXA K NONE J WARNING INDICATION UK UNKNOWN 1 WP 28 625AW 064 CMH - FLT 2258 - AIRCRAFT ARRIVED IN CMH WITH NUMEROUS ECAM MESSAGES AND INOP SYSTEMS. AVIONICS COOLING FAN POPPING C/B . DURING TROUBLESHOOTING, FOUND WIRES BURNED AT BUS BAR 2XP-AC BUS 2 (1000XN2). REF WDM 24-51-10. REPAIRED WIRES AND INSTALLED NEW BUS TIE. SYSTEM OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A28NM 1996092600485 19960926 00485 1996 9 26 AWXA960397 4 19960819 A 2210 4030952906 YAW DMP COUPLER BOEING 737 7372E3 NM RUDDER MALFUNCTIONED A A AWXA O OTHER F FLT CONT AFFECTED TO TAKEOFF 1 WP 28 138AW 86112498 22792 PHX - FLT 2450 - DURING TAKEOFF ROLL, EXPERIENCED TWO SEVERE SIDE JOLTS ABOUT 4-5 SECONDS APART. PER QUALITY CONTROL AL ERT BULLETIN NR 95-15 PERFORMED RUDDER PCU LEAK CHECK IAW A8M27001, NO DEFECTS NOTED. PER MX CONTROL CHANGED YAW DAMPNE R COUPLER IAW 22-11-141. (M) 2 L 7 2 4F RT A16WE 1996092600486 19960926 00486 NM 1996 9 26 AWXA960398 1 19960817 A 2720 BACB10EU06 RT CAM ROLLER BOEING 757 757225 1384959 NM RUDDER FAILED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 914AW 22208 PHX - FLT 2294 - AIRCRAFT ARRIVED WITH FLIGHT CREW COMPLAINING OF STIFF RUDDER PEDALS. WE CONFIRMED A TIGHT RATCHETY FE EL WHEN OPERATING PEDALS, ESPECIALLY WHEN LEFT PEDAL WAS PUSHED. RUDDER TRIM STICKS AND IS NOT RESPONSIVE TO PILOT INPU TS. FOUND THE SEAL BLOWN OUT OF ONE SIDE OF THE RUDDER CENTERING CAM BEARING AND REPLACED IT. RAN THE RUDDER AND THE T RIM THROUGH SEVERAL CYCLES WITH NO NOTICEABLE BINDING IN THE SYSTEM WITH OR WITHOUT HYDRAULIC PRESSURE ON. REMOVED AND REPLACED RUDDER TRIM CAM ROLLER. OPERATED RUDDER TRIM ACTUATOR THROUGH SEVERAL CYCLES, OPERATIONS CHECK NORMAL. (M) 2 L 7 2 4F RT A2NM 1996092600487 19960926 00487 NM 1996 9 26 AWXA960399 1 19960820 A 2722 1U1150 STANDBY ACT BOEING 737 737275 1384485 NM RUDDER INOPERATIVE A AWXA K NONE E VIBRATION/BUFFET IN INSP/MAINT 1 WP 28 CGBPW 990 20958 PHX - FLT 98 - FLT CREW REPORTED, A RUDDER FLUTTER WHEN CHECKING THE STANDBY RUDDER. PERFORMED RIGHT CHECKS ON NORMAL R UDDER SYSTEM, ALL CHECKS NORMAL. STANDBY SYSTEM CHECKS OK. FOUND STANDBY ACTUATOR DEAD BAND CHECK OUT OF LIMITS. COUL D NOT RIG ACTUATOR. REMOVED AND REPLACED RUDDER STANDBY ACTUATOR PER R6B27001 RIGGED AND OPS CHECK PER BMM 27-21-141. ( M) 2 L 7 2 4F A16WE 1996092600488 19960926 00488 NM 1996 9 26 AWXA960400 1 19960820 A 3230 106122615 SENSOR BOEING 737 73733A 1384673 NM LANDING GEAR INOPERATIVE A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 167AW 23628 LAS - FLT 916 - AIR TURN BACK, LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. FOUND AIR SAFETY GAP NOT PER BMM. REPLACE D SENSOR S106 AND ADJUSTED AND TESTED PER MM, OPS GOOD. (M) 2 L 7 2 4F RT A16WE 1996092600489 19960926 00489 NM 1996 9 26 AWXA960401 1 19960820 A 5610 WINDSHIELD BOEING 737 7373G7 1384595 NM COCKPIT BIRD STRIKE A AWXA A UNSCHED LANDING C F.O.D. CL CLIMB 1 WP 28 307AW 24634 LAS - FLT 2084 - AIR TURN BACK, BIRD STRIKE AROUND COCKPIT WINDSHIELD AREA ON CLIMB-OUT. EMERGENCY DECLARED. PERFORMED BIRD STRIKE INSPECTION PER CARD AWM 392. NO DAMAGE NOTED. (M) 2 L 7 2 4F RT A16WE 1996092600490 19960926 00490 NM 1996 9 26 AWXA960402 1 19960806 A 3397 WIRE BOEING 737 737301 1384611 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 326AW 23258 PHX - FLT 98 - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PROX EMERGENCY EXIT LIGHTS INOP AT SEATS 3, 6, 14 AND 17. R ESPLICED POWER WIRES AT SEAT ROWS 3, 6, 14 AND 17. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996092600491 19960926 00491 NM 1996 9 26 AWXA960403 1 19960812 A 3397 WIRE BOEING 737 737301 1384611 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 326AW 23258 PHX - FLT 2226 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT ROW 7 INOP. INSTALLED NEW BUTT SPLICE. OPS GO OD. (M) 2 L 7 2 4F RT A16WE 1996092600492 19960926 00492 EU 1996 9 26 AWXA960406 1 19960719 A 2752 791A000001 ACTUATOR AIRBUS 320 A320231 3930325 EU RT TE FLAP MALFUNCTIONED A AWXA O OTHER E VIBRATION/BUFFET AP APPROACH 1 WP 28 628AW J173 67 PHX - FLT 2247 - WHEN FLAPS FULL ARE SELECTED ON APPROACH, A HEAVY VIBRATION IS FELT THROUGHOUT THE AIRFRAME. PERFORMED VISUAL INSPECTION PER 27-54-00. NO DEFECTS NOTED AT THIS TIME AND RAN FLAP. NO VIBRATION NOTED AND VISUAL INSPECTION WHILE FLAP MOVED, NO DEFECT. OK FOR SERVICE. AIRCRAFT VIBRATION FELT WHEN FLAPS SELECTED FULL IN AIRSPEED RANGE 140-17 0 KIAS. REMOVED AND REPLACED NR 1 RIGHT FLAP ACTUATOR IAW 27-54-49, PG 401-421. OPS CHECK GOOD. AIRCRAFT SHAKES NOTIC EABLE AT FLAPS FULL POSITION (TEST FLT). REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATOR ASSEMBLY PER AMM 27-54-49, PGS 401-408. OPS CHECK GOOD. TEST FLT COMPLETED. NO ABNORMAL VIBRATION NOTED BY MAINTENANCE. (M) 2 L 7 2 4F RT A28NM 1996092600493 19960926 00493 NM 1996 9 26 AWXA960409 1 19960811 A 5315 FLOOR BEAM BOEING 737 7373G7 1384595 NM BS 344 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 DURING ROUTINE SCHEDULED C-8 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM AT BS 344, LBL 15, LBL 42, LBL 48, WL 208. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1996092600494 19960926 00494 NM 1996 9 26 AWXA960410 1 19960811 A 5315 FLOOR BEAM BOEING 737 7373G7 1384595 NM BS 294 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 PAE - FLT 7821 - DURING ROUTINE SCHEDULED C-8 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM AT BS 294 RBL 15, RBL 45, NL 208. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1996092600495 19960926 00495 NM 1996 9 26 AWXA960411 1 19960811 A 5315 FLOOR BEAM BOEING 737 7373G7 1384595 NM BS 312 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 PAE - FLT 7821 - DURING ROUTINE SCHEDULED C-8 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM AT BS 312, LBL 12, BL 0, RBL 7, WL 208. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1996092600496 19960926 00496 NM 1996 9 26 AWXA960412 1 19960815 A 5320 SILL BOEING 737 7373G7 1384595 NM BS 284-332 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 160AW 23782 PAE - FLT 7821 - DURING ROUTINE SCHEDULED C-8 MAINTENANCE CHECK, FOUND CORROSION ON FWD MOPSIL BS 284 TO BS 332, WL 208, RBL 55. REMOVED AND REPLACED MOPSIL PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1996092600497 19960926 00497 EU 1996 9 26 AWXA960413 1 19960803 A 3350 321430 BATTERY PACK AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 641AW 3326 453 PHX - FLT 2294 - DURING ROUTINE MAINTENANCE CHECK, FOUND L-1 DOOR BATTERY PACK FOR EXIT LIGHTS NOT HOLDING CHARGE. REMO VED AND REPLACED PER AMM 33-51-38. OPS CHECK GOOD AT THIS TIME. (M) 2 L 7 2 4F RT A28NM 1996092600498 19960926 00498 NM 1996 9 26 AWXA960414 1 19960804 A 3350 CONNECTOR BOEING 737 737277 1384570 NM CABIN LOOSE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 181AW 22648 PHX - FLT 7803 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS OVER EXIT WINDOWS INOP. REINSTALLED CANN ON PLUG ABOVE CEILING PANEL PAX ROW 9. FUNCTIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996092600499 19960926 00499 NM 1996 9 26 AWXA960415 1 19960804 A 3350 20131A BATTERY PACK BOEING 757 7572S7 1384962 NM CABIN INOP A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 906AW 54541 23568 DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS AT DOOR L-4 OVERHEAD INOP. REMOVED AND REPLACED EMERGENCY LIGH T BATTERY PACK FOR DOOR L-4. OPS NORMAL. (M0 2 L 7 2 4F RT A2NM 1996092600500 19960926 00500 NM 1996 9 26 AWXA960416 1 19960806 A 3397 WIRE BOEING 737 737301 1384611 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 326AW 23258 PHX - FLT 98 - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PROX EMERGENCY EXIT LIGHTS INOP AT SEATS 3,6, 14 AND 17. R ESPLICED POWER WIRES AT SEATS ROWS 3, 6, 14 AND 17. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996092600501 19960926 00501 NM 1996 9 26 AWXA960419 1 19960806 A 3397 WIRE BOEING 757 7572S7 1384962 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 906AW 23568 PHX - FLT 2211 - REFERENCE MEL 33-51-03, EMERGENCY LIGHT ROW 20 INOP. REPAIRED BROKEN WIRE UNDER SEAT. OPS CHECKED NOR MAL. MEL REMOVED. (M) 2 L 7 2 4F RT A2NM 1996092600502 19960926 00502 NM 1996 9 26 AWXA960420 1 19960806 A 3397 WIRE BOEING 737 7373B7 1384580 NM CABIN TORN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 328AW 23377 PHX - FLT 2035 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY FLOOR LIGHTING WIRE TORN FROM FLOOR. REPAIRED EMERGE NCY FLOOR LIGHTING WIRES AND TRACK SYSTEM. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996092600504 19960926 00504 NE 1996 9 26 AWXA960423 2 19960825 A 7261 4A7117B OIL SCAV PUMP AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE NR 2 ENGINE FAILED A A AWXA E ENGINE SHUTDOWN A FLAME/FIRE TX TAXI/GRND HDL 1 WP 28 625AW 14924 250 F11477 064 RNO - FLT 2012 - ON ARRIVAL IN RNO AND SHUTDOWN, GROUND CREW REPORTED A TAIL PIPE FIRE IN THE NR 2 ENGINE. AFTER SUBSEQ UENT DRY MOTORINGS, GROUND FIRE EXTINGU ISHER WAS USED, THE FIRE WAS PUT OUT. FOUND OIL PUDDLED IN ENGINE CORE TAIL PI PE. REMOVED AND REPLACED NR 2 ENGINE OIL SCAVENGER PUMP PER AWA TASK CARD R5M79301. PERFORMED ENGINE RUN LEAK/CHECK, O PS CHECK NORMAL AT THIS TIME. (M) 2 L 7 2 4F 4 F RT A28NM E311NE 1996092600505 19960926 00505 NM 1996 9 26 AWXA960424 1 19960807 A 3350 1102833 BATTERY PACK BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 178AW 5786 22645 PHX - FLT 2674 - DURING ROUTINE MAINTENANCE CHECK, FOUND R-1 EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK. O PS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996092600506 19960926 00506 NM 1996 9 26 AWXA960425 1 19960810 A 3350 831862 BATTERY PACK BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 189AW 0270 22656 PHX - FLT 7820 - DURING ROUTINE MAINTENANCE CHECK, FOUND R-1 AND R-2 EXTERIOR EMERGENCY LIGHTS INOP. RIGHT OVERWING EME RGENCY LIGHTS INOP. REMOVED AND REPLACED FORWARD EMERGENCY BATTERY PACK PER MM 33-51-71. OPS CHECK GOOD. ADJUSTED RIG HT EMERGENCY EXIT HATCH LIGHT SWITCH PER MM 33-51-121. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996092600507 19960926 00507 NM 1996 9 26 AWXA960426 1 19960811 A 3397 WIRE BOEING 737 7373B7 1384580 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 328AW 23377 PHX - FLT 2278 - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PROX LIGHTING INOP AT ROWS 13 AND 14. REPAIRED WIRING AS REQUIRED. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996092600508 19960926 00508 NM 1996 9 26 AWXA960427 1 19960811 A 3350 900835A POWER UNIT BOEING 737 7372A6 138448B NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 145AW 20194 PHX - FLT 2312 - DURING ROUTINE MAINTENANCE CHECK, FOUND R-2 DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED POWER UNIT . OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1996092600509 19960926 00509 NM 1996 9 26 AWXA960428 1 19960813 A 3397 WIRE BOEING 737 7372U9 1384498 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 149AW 22575 PHX - FLT 2287 - REFERENCE MEL 33-19, EMERGENCY LIGHT AT 3 C INOP. REPAIRED WIRING AS REQUIRED. OPS CHECK GOOD IAW MM 33-00. MEL PLACARD REMOVED. (M) 2 L 7 2 4F RT A16WE 1996092600510 19960926 00510 NM 1996 9 26 AWXA960429 1 19960814 A 3350 69B475142 BATTERY PACK BOEING 757 757225 1384959 NM CABIN INOP A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 914AW 5309 22208 PHX - FLT 2020 - DURING ROUTINE MAINTENANCE CHECK, FOUND AFT CABIN SECTION OF EMERGENCY LGIHTS INOP AND BATTERY PACK AT L-2 DOOR NOT CHARGING. REMOVED AND REPLACED BATTERY PACK IN AFT SECTION. OPS GOOD. REMOVED AND REPLACED CHARGER AT L- 2 DOOR. OPS GOOD. (M) 2 L 7 2 4F RT A2NM 1996092600511 19960926 00511 NM 1996 9 26 AWXA960430 1 19960814 A 3397 WIRE BOEING 737 7372A6 138448B NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 145AW 20194 PHX - FLT 2312 - DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 1 EMERGENCY LIGHT INOP. REPAIRED WIRING AT ROW 1. SYSTEM OPS NORMAL. (M) 2 L 7 2 4F A16WE 1996092600512 19960926 00512 EU 1996 9 26 AWXA960431 1 19960815 A 3350 321430 BATTERY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 634AW 3010 091 PHX - FLT 2249 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS INTERMITTENTLY INOP THROUGHOUT CABIN. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AT CABIN LEFT. OPS GOOD. (M) 2 L 7 2 4F RT A28NM 1996092600513 19960926 00513 NM 1996 9 26 AWXA960439 1 19960821 A 3397 WIRE BOEING 737 7373G7 1384595 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 156AW 23778 PHX - FLT 2202 - REFERENCE MEL 33-15, SEAT ROW 6 A, B, C EMERGENCY LIGHTS INOP. REPAIRED BROKEN WIRE AT ROW 6 A, B, C. EMERGENCY LIGHT FUNCTION CHECK, MEL REMOVED. (M) 2 L 7 2 4F RT A16WE 1996092600514 19960926 00514 EU 1996 9 26 AWXA960440 1 19960821 A 3350 321430 BATTERY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 300ML 10477 317 PHX - FLT 7913 - DURING ROUTINE MAINTENANCE CHECK, FOUND VARIOUS EMERGENCY LIGHTS INOP. REPLACED BAD EMERGENCY LIGHT BA TTERY. OPS CHECK GOOD, IAW MM 33-51-00. (M) 2 L 7 2 4F RT A28NM 1996092600515 19960926 00515 NM 1996 9 26 AWXA960441 1 19960822 A 3397 WIRE BOEING 757 7572S7 1384962 NM CABIN LOOSE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 903AW 23323 LAS - FLT 739 - DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT EMERGENCY LIGHT WIRING HANGING LOOSE AT SEATS 7-8, 13-14 AN D 18. SECURED WIRING. (M) 2 L 7 2 4F RT A2NM 1996092600516 19960926 00516 NM 1996 9 26 AWXA960442 1 19960823 A 3350 CONNECTOR BOEING 737 737277 1384570 NM CABIN LOOSE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 185AW 22652 PHX - FLT 2590 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT SEAT ROW 12 A, B, C. RECONNECTED SEPARATED CONNECTOR. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996092600517 19960926 00517 NM 1996 9 26 AWXA960444 1 19960823 A 3350 1000679 LIGHT BOEING 737 737277 1384570 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 181AW 14152 22648 LAS - FLT 2157 - DURING ROUTINE MAINTENANCE CHECK, FOUND L-2 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED EMERGENCY EXIT LI GHT ASSEMBLY AS REQUIRED. OPS NORMAL AT THIS TIME. (M) 2 L 7 2 4F RT A16WE 1996092600518 19960926 00518 NM 1996 9 26 AWXA960445 1 19960823 A 3350 LIGHT BOEING 737 7373G7 1384595 NM CABIN MISSING A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 150AW 23218 PHX - FLT 2205 - DURING ROUTINE MAINTENANCE CHECK, FOUND OVERHEAD BIN EMERGENCY EXIT LIGHT MISSING FROM HOLE ROW 21 LEFT . SECURED LIGHT ASSEMBLY IN BULLNOSE, OPS GOOD. (M) 2 L 7 2 4F RT A16WE 1996092600519 19960926 00519 NM 1996 9 26 AWXA960446 1 19960828 A 2910 BACH8A06NN0263T HYDRAULIC LINE BOEING 737 737277 1384570 NM 'A' HYD SYSTEM SPLIT A AWXA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CL CLIMB 1 WP 28 185AW 22652 CMH - FLT 2938 - AIR TURN BACK, DUE TO LOSS OF 'A' SYSTEM HYDRAULICS. EMERGENCY DECLARED. FOUND HYDRAULIC LINE IN NOSE GEAR WHEEL WELL RUPTURED. LINE FROM NLG RETRACT AND EXTEND ACTUATOR. REMOVED AND REPLACED HYDRAULIC LINE AND SERVICED TO FULL. (M) 2 L 7 2 4F RT A16WE 1996092600520 19960926 00520 EU 1996 9 26 AWXA960447 1 19960705 A 3350 321454 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN INOP A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 632AW 378 81 PHX - FLT 2266 - DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 22 EMERGENCY LIGHT LENS MISSING AND OVERWING EMERGENCY EXIT LIGHT ON AIRCRAFT RIGHT INOP. INSTALLED LENS COVER. REMOVED AND REPLACED POWER SUPPLY PER CH 33. BITE TEST GOOD. (M ) 2 L 7 2 4F RT A28NM 1996092600521 19960926 00521 EU 1996 9 26 AWXA960448 1 19960704 A 3350 321454 POWER SUPPLY AIRBUS 320 A320232 3930326 EU CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 639AW 471 PHX - FLT 2640 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS INOP AT SEATS 3, 7, 15, 22 AND 26. AFTER TROU BLESHOOTING, REMOVED AND REPLACED POWER SUPPLY AT 12 WL AND 12 WL AS PRECAUTION. (M) 2 L 7 2 4F RT A28NM 1996092600522 19960926 00522 EU 1996 9 26 AWXA960449 1 19960721 A 3350 321430 BATTERY AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 641AW 4410 453 PHX - FLT 2082 - DURING ROUTINE MAINTENANCE CHECK, FOUND OVERWING INTERIOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY AT RIGHT MID. OPERATIONS CHECK GOOD. (M) 2 L 7 2 4F RT A28NM 1996092600523 19960926 00523 EU 1996 9 26 AWXA960450 1 19960723 A 3350 321430 BATTERY PACK AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 641AW 453 LAS - FLT 146 - DURING ROUTINE MAINTENANCE CHECK, FOUND LEFT OVERHEAD AND LEFT OVERWING EMERGENCY EXIT LIGHTS INOP. REM OVED AND REPLACED LEFT OVERWING BATTERY PACK IAW AWM MM 33-51-00. OPERATIONS CHECK GOOD. (M) 2 L 7 2 4F RT A28NM 1996092600524 19960926 00524 EU 1996 9 26 AWXA960451 1 19960827 A 3350 321430 BATTERY PACK AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 626AW 9076 65 PHX - FLT 1236 - DURING ROUTINE MAINTENANCE CHECK, FOUND THAT EMERGENCY LIGHT BATTERY TEST FAILS. REMOVED AND REPLACED BATTERY PACK. OPERATIONS CHECK GOOD. (M) 2 L 7 2 4F RT A28NM 1996092600525 19960926 00525 EU 1996 9 26 AWXA960452 1 19960827 A 3397 WIRE AIRBUS 320 A320231 3930325 EU CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 625AW 064 PHX - FLT 2541 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT AT SEAT 22L INOP. REPAIRED WIRING AS REQUIRED. OPERATIONS CHECK GOOD. (M) 2 L 7 2 4F RT A28NM 1996092600526 19960926 00526 EU 1996 9 26 AWXA960453 1 19960827 A 3350 321430 BATTERY PACK AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 626AW 9076 65 PHX - FLT 1236 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT BATTERY FAILS TEST. REMOVED AND REPLACED FORWA RD BATTERY PACK. OPERATIONS CHECK GOOD. (M) 2 L 7 2 4F RT A28NM 1996092600527 19960926 00527 NM 1996 9 26 AWXA960454 1 19960820 A 5240 6545849139 TORQUE TUBE BOEING 737 73733A 1384673 NM SERV DOOR CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 165AW 23626 PAE - FLT 7846 - DURING ROUTINE SCHEDULED C-11 MAINTENANCE CHECK, FOUND RUST EMITTING FROM FUSELAGE TORQUE TUBE LOWER BE ARING AT R-2 DOOR. REMOVED AND REPLACED TORQUE TUBE, IAW MM 52-41-41 AND OHM 20-50-03. (M) 2 L 7 2 4F RT A16WE 1996092600528 19960926 00528 NM 1996 9 26 AWXA960455 1 19960820 A 5315 FLOOR BEAM BOEING 737 73733A 1384673 NM BS 294.5 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 165AW 23626 PAE - FLT 7846 - DURING ROUTINE SCHEDULED C-11 MAINTENANCE CHECK, FOUND FLOOR BEAM UPPER CHORD CORRODED BS 294.5 RBL 31 TO 52, WL 208. REPAIRED IAW, SRM 53-10-08, SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1996092600529 19960926 00529 NM 1996 9 26 AWXA960456 1 19960821 A 5320 654587545 SILL BOEING 737 73733A 1384673 NM BS 270-328 CORROSION A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 165AW 23626 DURING ROUTINE SCHEDULED C-11 MAINTENANCE CHECK, FOUND CORROSION ON FWD GALLEY DOOR MOPSILL BS 270-328, RBL 50-52, WL 20 8. REMOVED AND REPLACED MOPSILL PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 1996092600530 19960926 00530 NM 1996 9 26 AWXA960457 1 19960819 A 5315 FLOOR BEAM BOEING 737 73733A 1384673 NM BS 967 CORROSION A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 165AW 23626 PAE - FLT 7846 - DURING ROUTINE SCHEDULED C-11 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM STATION 967, RBL 23-26, WL 208. REPAIRED FLOOR BEAM IAW, SRM 53-00-51. (M) 2 L 7 2 4F RT A16WE 1996092600531 19960926 00531 NM 1996 9 26 AWXA960458 1 19960823 A 5315 FLOOR BEAM BOEING 737 73733A 1384673 NM BS 986.5 CORROSION A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 165AW 23626 PAE - FLT 7846 - DURING ROUTINE SCHEDULED C-11 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM STATION 986.5, LBL 20, W L 208. REPAIRED FLOOR BEAM PER ER 3-53-16-34. TCO-PAN-96-1169RR, 8110-3. (M) 2 L 7 2 4F RT A16WE 1996092600532 19960926 00532 NM 1996 9 26 AWXA960459 1 19960818 A 5320 TEAR STRAP BOEING 757 7572G7 1384963 NM YS 1280 NO EDGE DISTANCE A AWXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 28 908AW 24233 PAE - FLT 7829 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, AT BS 1280, STRINGER 6R, FOUND REPAIR FASTENER BREAKING THROUGH EDGE OF TEAR STRAP, NO ED. REMOVED EXT DOUBLER, CUT OUT INTERNAL TEAR STRAP, FABRICATED REPAIR PARTS AND INSTA LLED IAW ER 5-53-34-02, TCO-PAN 96-1173RR. (M) 2 L 7 2 4F RT A2NM 1996092600533 19960926 00533 NM 1996 9 26 AWXA960460 1 19960816 A 5315 FLOOR BEAM BOEING 757 7572G7 1384963 NM BS 1681 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 908AW 24233 PAE - FLT 7829 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK WHILE WORKING INT 57, CUSTOMER ID NR 00312737, FOUND BS 1681 FLOOR BEAM TO BE CORRODED LBL 33-48 AROUND NUT PLATES ON UPPER CHORD. CUT OUT DAMAGE AT BS 1681, LBL 43-RBL 48. C LEANED CORROSION AT BS 1681, LBL 33 - LBL 40. FABRICATED PARTS AND INSTALLED FASTENERS PER ER TCO-PAN 1159RR AND SRM 53 -60-51. (M) 2 L 7 2 4F RT A2NM 1996092600534 19960926 00534 NM 1996 9 26 AWXA960461 1 19960818 A 5320 TEAR STRAP BOEING 757 7572G7 1384963 NM BS 1220 NO EDGE DISTANCE A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 908AW 24233 PAE - FLT 7829 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK WHILE ACCESSING AREA AT BS 1220, STRINGER 5R, FOUND REPA IR FASTENERS BREAKING THROUGH EDGE OF TEAR STRAP, NO ED. REMOVED EXTERNAL DOUBLER. REMOVED DAMAGED SECTION OF TEAR STR AP. FABRICATED AND INSTALLED REPAIR PARTS PER ER 5-53-34-02 AND PER TCO-PAN-96-1173RR. (M) 2 L 7 2 4F RT A2NM 1996092600535 19960926 00535 NM 1996 9 26 AWXA960462 1 19960816 A 5315 FLOOR BEAM BOEING 757 7572G7 1384963 NM BS 1640 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 908AW 24233 PAE - FLT 7829 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CORROSION AT BS 1640 UPPER CHORD OF FLOOR BEAM LB L 65 - RBL 65. REMOVED CORRODED PART AT BS 1640, LBL 65 - RBL 65, WL 208 AND INSTALLED FABRICATED PART PER SRM 51-30-01 , SRM 53-00-51. (M) 2 L 7 2 4F RT A2NM 1996092600536 19960926 00536 NM 1996 9 26 AWXA960463 1 19960816 A 5320 WEB BOEING 757 7572G7 1384963 NM BS 1681 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 908AW 24233 PAE - FLT 7829 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CORROSION ON PRESSURE WEB BS 1681, BL 0 - LBL 50. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR PARTS IAW, SRM 53-60-51, 53-00-51. (M) 2 L 7 2 4F RT A2NM 1996092600537 19960926 00537 EU 1996 9 26 AWXA960465 1 19960829 A 3350 321430 BATTERY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 300ML 317 PHX - FLT 2249 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INTERMITTENT INOP THROUGH CABIN. DTP PAN EL FAILS LEFT BATTERY. REMOVED AND REPLACED LEFT EMERGENCY LIGHT BATTERY. OPS AND TEST GOOD. (M) 2 L 7 2 4F RT A28NM 1996092600538 19960926 00538 NM 1996 9 26 AWXA960466 1 19960830 A 3350 1060091101 LIGHT BOEING 737 737277 1384570 NM CABIN INOP A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 188AW 22655 LAS - FLT 2125 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT SEAT 5C. REPLACED LIGHT ASSEMBLY. FUNCTION CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996092600539 19960926 00539 NM 1996 9 26 AWXA960467 1 19960829 A 3350 831136 LIGHT BOEING 737 73733A 1384673 NM CABIN INOP A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 173AW 23632 PHX - FLT 2834 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT AT ROW 6 A/C LEFT IN OVERHEAD INOP. PLACED ON MEL 33-15. REASSEMBLED AND SECURED LIGHT ASSEMBLY. OPERATIONS CHECK GOOD. MEL CLEARED. (M) 2 L 7 2 4F RT A16WE 1996092600540 19960926 00540 NM 1996 9 26 AWXA960468 1 19960901 A 3350 900542 BATTERY PACK BOEING 737 737112 1384412 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 708AW 19771 PHX - FLT 2944 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT INOP ON LEFT SIDE AT SEATS ROW 1-5. RESEA TED BATTERY PACK. OPS GOOD. (M) 2 L 7 2 4F A16WE 1996092600541 19960926 00541 EU 1996 9 26 AWXA960469 1 19960903 A 3350 321430 BATTERY PACK AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 636AW 098 LAS - FLT 2687 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT AFT CENTER AISLE, R-1 AND R-2 DOO RS. REMOVED AND REPLACED BATTERY PACK OVER R-1 DOOR. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A28NM 1996092600543 19960926 00543 NM 1996 9 26 AWXA960471 1 19960830 A 3350 1000679 LIGHT BOEING 737 737277 1384570 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 187AW 19818 22654 PHX - FLT 2636 - DURING ROUTINE MAINTENANCE CHECK, FOUND L-2 DOOR EMERGENCY EXIT SIGN ABOVE DOOR INOP. REMOVED AND REPL ACED EMERGENCY LIGHT ASSEMBLY. SYSTEM OPS NORMAL. (M) 2 L 7 2 4F RT A16WE 1996092600544 19960926 00544 NM 1996 9 26 AWXA960472 1 19960824 A 5320 SUPPORT BOEING 757 7572G7 1384963 NM RADAR BAY CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 910AW 24523 PAE - FLT 7849 - DURING ROUTINE SCHEDULED C-6 MAINTENANCE CHECK, FOUND FORWARD RADAR BAY LEFT VERTICAL SUPPORT FOR BATTE RY TRAY 13 CRACKED IN RADIUS. REPAIRED PER SRM 53-10-2, SRM 51-40-2. (M) 2 L 7 2 4F RT A2NM 1996092600545 19960926 00545 NM 1996 9 26 AWXA960473 1 19960824 A 5311 FRAME BOEING 757 7572G7 1384963 NM BS 1540 DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 910AW 24523 PAE - FLT 7849 - DURING ROUTINE SCHEDULED C-6 MAINTENANCE CHECK, FOUND STATION 1540, LBL 30, WL 153 FRAME DENTED. REPAI RED PER SRM 51-70-11, 51-40, 51-20-01. (M) 2 L 7 2 4F RT A2NM 1996092600546 19960926 00546 EU 1996 9 26 AWXA960474 1 19960725 A 3397 WIRE AIRBUS 320 A320231 3930325 EU CABIN CUT A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 628AW 67 LAS - FLT 2085 - DURING ROUTINE MAINTENANCE CHECK, FOUND L-1 DOOR BULKHEAD EMERGENCY EXIT LIGHT INOP. FOUND BULKHEAD/SI DEWALL WIRES CUT. SPLICED TOGETHER. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A28NM 1996092600547 19960926 00547 EU 1996 9 26 AWXA960475 1 19960725 A 3350 321430 BATTERY PACK AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 624AW 10482 55 LAS - FLT 2609 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOP OVERWING. REPLACED BATTERY PACK OVE RWING LEFT SIDE IAW, AMM 33-51-38, TEST OK. (M) 2 L 7 2 4F RT A28NM 1996092600548 19960926 00548 NM 1996 9 26 AWXA960476 1 19960804 A 3397 WIRE BOEING 757 7572S7 1384962 NM CABIN DISCONNECTED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 906AW 23568 PHX - FLT 700 - DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 25 EMERGENCY LIGHT INOP. RECONNECTED TERMINAL. (M) 2 L 7 2 4F RT A2NM 1996092600549 19960926 00549 NM 1996 9 26 AWXA960478 1 19960907 A 3397 WIRE BOEING 737 737277 1384570 NM CABIN DISCONNECTED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 183AW 22650 PHX - FLT 2062 - DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT MOUNTED EMERGENCY LIGHTS ON DIM, ROW 1-5, AT ALL TIMES. R ECONNECTED WIRE. REPAIRED SHORT IN WIRING. OPERATIONS CHECK OK. (M) 2 L 7 2 4F RT A16WE 1996092600550 19960926 00550 EU 1996 9 26 AWXA960479 1 19960908 A 3350 321430 BATTERY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 636AW 098 PHX - FLT 2274 - DURING ROUTINE MAINTENANCE CHECK, EMERGENCY EXIT LIGHT TEST FAILED. REMOVED AND REPLACED EMERGENCY LIG HT BATTERY FORWARD LEFT OVERWING. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT FWD LEFT OVERWING. SYSTEM CHARGED, OPERATIONS CHECK GOOD. (M) 2 L 7 2 4F RT A28NM 1996092600551 19960926 00551 SO 1996 9 26 C2XA96IA190 1 19960822 A 5320 12064442001 T-PROFILE EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15732 120195 IAH - DURING C-CHECK INSPECTION, THE T-PROFILE AT FRAME 42 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED T HE T-PROFILE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996092600552 19960926 00552 SO 1996 9 26 C2XA96IA191 1 19960822 A 5315 12006158001 FLOOR BEAM EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15732 120195 IAH - DURING C-CHECK INSPECTION, THE CENTER FLOOR BEAM FROM FRAMES 38 TO 44 WAS FOUND TO BE CORRODED. MAINTENANCE REMOV ED AND REPLACED THE AFFECTED FLOOR BEAM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996092600553 19960926 00553 SO 1996 9 26 C2XA96IA192 1 19960822 A 5315 12006158003 FLOOR BEAM EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15732 120195 IAH - DURING C-CHECK INSPECTION, THE RIGHT FLOOR BEAM FROM FRAME 38 TO 44 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR BEAM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996092600554 19960926 00554 SO 1996 9 26 C2XA96IA193 1 19960822 A 5320 12004449001 T-PROFILE EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15732 120195 IAH - DURING C-CHECK INSPECTION, THE T-PROFILE AT FRAME 40, RIGHT CENTER, WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE RIGHT CENTER T-PROFILE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996092600555 19960926 00555 SO 1996 9 26 C2XA96IA194 1 19960822 A 5320 12005779001 T-PROFILE EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15732 120195 IAH - DURING C-CHECK INSPECTION, THE RIGHT T-PROFILE AT FRAME 40 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPL ACED THE PROFILE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996092600556 19960926 00556 SO 1996 9 26 C2XA96IA195 1 19960822 A 5320 12004149002 T-PROFILE EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15732 120195 IAH - DURING C-CHECK INSPECTION, THE T-PROFILE ON FRAMES 36 AND 38 LEFT WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE T-PROFILES AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996092600557 19960926 00557 SO 1996 9 26 C2XA96IA196 1 19960822 A 5320 12004449001 T-PROFILE EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15732 120195 IAH - DURING C-CHECK INSPECTION, THE T-PROFILES AT FRAMES 36 RIGHT, 38 RIGHT AND CENTER WERE FOUND TO BE CORRODED. MAIN TENANCE REMOVED AND REPLACED THE T-PROFILES, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996092600558 19960926 00558 SO 1996 9 26 C2XA96IA197 1 19960822 A 5320 12004471002 CREASE BEAM EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15732 120195 IAH - DURING C-CHECK INSPECTION, THE RIGHT CREASE BEAM FROM FRAME 34 TO FRAME 38 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE CREASE BEAM AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996092600559 19960926 00559 SO 1996 9 26 C2XA96IA198 1 19960822 A 5320 12006158002 CREASE BEAM EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15732 120195 IAH - DURING C-CHECK INSPECTION, THE RIGHT HAND CREASE BEAM FROM FRAME 38 TO FRAME 44 WAS FOUND TO BE CORRODED. MAINTEN ANCE REMOVED AND REPLACED THE CREASE BEAM AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996092600560 19960926 00560 SO 1996 9 26 C2XA96IA199 1 19960822 A 5320 12046163001 BUTTSTRAP EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15732 120195 IAH - DURING C-CHECK INSPECTION, THE LEFT CENTER AND RIGHT FLOOR BUTTSTRAPS FROM FRAME 34 TO FRAME 38 WERE FOUND TO BE C ORRODED. MAINTENANCE REMOVED THE DAMAGED SECTIONS AND SPLICED IN SERVICEABLE SECTIONS OF BUTTSTRAPS AND THE AIRCRAFT WA S APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996092600561 19960926 00561 SO 1996 9 26 C2XA96IA200 1 19960822 A 5320 12020235001A BRACKET EMB 120 EMB120RT SO CABIN BROKEN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15732 120195 IAH - DURING C-CHECK INSPECTION, THE CARGO DOOR TORSION ROD FORWARD BRACKET WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE BRACKET AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996092600562 19960926 00562 SO 1996 9 26 C2XA96IA201 1 19960822 A 5347 12016000003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15732 120195 IAH - DURING C-CHECK INSPECTION, THE RIGHT FORWARD FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND R EPLACED THE SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996092600563 19960926 00563 SO 1996 9 26 C2XA96IA202 1 19960822 A 5347 12015997003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15732 120195 IAH - DURING C-CHECK INSPECTION, THE RIGHT FORWARD SIDEWALL SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AN D REPLACED THE SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996092600564 19960926 00564 SO 1996 9 26 C2XA96IA203 1 19960822 A 5347 12026865009 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15732 120195 IAH - DURING C-CHECK INSPECTION, THE LEFT AFT FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLAC ED THE SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996092600565 19960926 00565 SO 1996 9 26 C2XA96IA204 1 19960822 A 5347 12015994003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15732 120195 IAH - DURING C-CHECK INSPECTION, THE LEFT FORWARD SIDEWALL SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996092600566 19960926 00566 SO 1996 9 26 C2XA96IA205 1 19960822 A 5347 12015995003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15732 120195 IAH - DURING C-CHECK INSPECTION, THE LEFT LOWER SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED T HE SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996092600567 19960926 00567 SO 1996 9 26 C2XA96IA206 1 19960822 A 5347 12026864007 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15732 120195 IAH - DURING C-CHECK INSPECTION, THE RIGHT AFT FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLA CED THE SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996092600568 19960926 00568 SO 1996 9 26 C2XA96IA207 1 19960822 A 5320 12008000002 ANGLE EMB 120 EMB120RT SO CABIN CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15732 120195 IAH - DURING C-CHECK INSPECTION, THE LEFT AND RIGHT WEB ATTACH ANGLES ON THE FLOOR SUPPORTS AT FRAME 13 WERE FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE ATTACH ANGLES, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996092600569 19960926 00569 SO 1996 9 26 C2XA96IA208 1 19960822 A 2622 A8251007 FIRE BOTTLE EMB 120 EMB120RT SO LAVATORY UNDER WEIGHT A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15732 120195 IAH - DURING C-CHECK INSPECTION, THE TOILET TRASH COMPARTMENT FIRE BOTTLE WAS FOUND TO BE UNDER WEIGHT. MAINTENANCE REM OVED AND REPLACED THE FIRE BOTTLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996092600570 19960926 00570 SO 1996 9 26 C2XA96IA209 1 19960822 A 5330 12017417021 SKIN EMB 120 EMB120RT SO LOWER FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15732 120195 IAH - DURING C-CHECK INSPECTION, THE BELLY SKIN BETWEEN FRAMES 39 AND 41 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE BELLY SKIN FROM FRAME 38 TO FRAME 42, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996092600571 19960926 00571 SO 1996 9 26 C2XA96IA210 1 19960822 A 5313 12017417007 STRINGER EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15732 120195 IAH - DURING C-CHECK INSPECTION, STRINGER 20 ON THE RIGHT FUSELAGE WAS FOUND TO BE CORRODED FROM FRAME 38.5 TO FRAME 40. MAINTENANCE REMOVED THE DAMAGED SECTION OF STRINGER AND PERFORMED A SPLICE REPAIR PER EMB SRM 53-00-01, AND THE AIRCRA FT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996092600572 19960926 00572 SO 1996 9 26 C2XA96IA211 1 19960822 A 5313 12017417009 STRINGER EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15732 120195 IAH - DURING C-CHECK INSPECTION, STRINGER 19 ON THE RIGHT FUSELAGE WAS FOUND TO BE CORRODED BETWEEN FRAME 38.5 AND FRAME 40. MAINTENANCE REMOVED THE DAMAGED SECTION OF STRINGER AND PERFORMED A SPLICE REPAIR PER EMB SRM 53-00-01, AND THE AI RCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996092600573 19960926 00573 SO 1996 9 26 C2XA96IA212 1 19960822 A 5313 12017417011 STRINGER EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15732 120195 IAH - DURING C-CHECK INSPECTION, STRINGER 18 ON THE RIGHT FUSELAGE WAS FOUND TO BE CORRODED BETWEEN FRAME 38.5 AND FRAME 40. MAINTENANCE REMOVED THE DAMAGED SECTION OF STRINGER AND PERFORMED A SPLICE REPAIR PER EMB SRM 53-00-01, AND THE AI RCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996092600574 19960926 00574 NM 1996 9 26 EIAA9626 1 19960729 A 7931 OIL PRESS TRANS BOEING 747 747132 1384882 NM PWA JT9 JT9D7J 52054 NE NR 2 ENG BROKEN A EIAA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 09 479EV 19898 662377 HNL - AT FLT LEVEL 310, NR 2 OIL QTY WENT FROM 7/8 TO 1/8, OIL PRESSURE BEGAN TO FLUCTUATE PLUS OR MINUS 3 PSI AND OIL P RESS LIGHT FLICKERED. OIL PRESSURE WENT TO 35 PSI. ACCOMPLISHED ABNORMAL PROCEDURE AND SHUT ENGINE DOWN AT 940Z. OIL PRESSURE DURING WINDMILLING, 10 PSI. WIND MILLING TIME WAS 2 HOURS AND 30 MINUTES. FOUND DIFF OIL PRESS TRANSMITTER SH EARED FROM IT'S MOUNTS CAUSING OIL LINE, P/N 65B9011564, TO RUPTURE. RESECURED TRANSMITTER TO MOUNT AND INSTALLED FUEL LINE PER ECRA NR 662377-79-007-1. LEAK AND FUNCTIONAL CHECK OF DIFF PRESS TRANSMITTER CHECKED NORMAL. (M) 2 L 7 4 4F 4 F A20WE E20EA 1996092600575 19960926 00575 NE 1996 9 26 EISA96102 2 19960721 A 7261 FILTER BOEING 727 727221 1384071 NM PWA JT8 JT8D17R 52049 NE NR 2 ENGINE CLOGGED A EISA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SW 07 363PA 22535 ENGINE NR 2 OIL PRESSURE FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT. REDUCED POWER LIGHT REMAINED ILLUMINATED WITH POWER AT IDLE. ENGINE SHUT DOWN AND RETURNED TO EWR. REPLACED NR 2 MAIN OIL SCREEN, RUN-UP AND LEAK CHECK OK. OIL PRESSURE LIGHT OPS CHECK NORMAL. (M) 2 L 7 3 4F 4 F A3WE E2EA 1996092600576 19960926 00576 WP 1996 9 26 HALA960824 1 19960824 A 3350 P4010049 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 709HA 47764 HNL - FLT 504 - FOUND EMERGENCY FLOOR LIGHT IN AFT SECTION INOP. REPLACED EMERGENCY BATTERY. OPS CHECK OK. (M) 2 L 7 2 4F A6WE 1996092600577 19960926 00577 WP 1996 9 26 HALA96122 1 19960822 A 2760 ACTUATOR DOUG DC9 DC951 3022051 WP THROTTLE QUAD OVERHEAT A HALA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 WP 13 601AP 6131 1226 47658 HNL - FLT 519 - STRONG ELECTRICAL BURNING SMELL IN COCKPIT, SEEMS TO BE CENTERED AT THROTTLE QUADRANT. REPLACED AUTO SP OILER ACTUATOR, CONTROL BOX AND INTERLOCK BOX. THE OPERATIONAL CHECK WAS GOOD. (M) 2 L 7 2 4F A6WE 1996092600578 19960926 00578 WP 1996 9 26 HALA96125 1 19960824 A 3260 STRIKER PLATE DOUG DC9 DC951 3022051 WP LT MLG WORN A HALA K NONE N FALSE WARNING CL CLIMB 1 WP 13 672MC 47661 HNL - FLT 376 - AFTER TAKEOFF, LEFT GEAR UNSAFE LIGHT CAME ON. FOUND STRIKER PLATE WORN. REPLACED STRIKER PLATE. PERF ORMED ALTERNATE UPLATCH CHECK ON DOOR PER MM 32-31-4. OPS CHECKED OK. (M) 2 L 7 2 4F A6WE 1996092600579 19960926 00579 WP 1996 9 26 HALA96127 1 19960826 A 3260 GEAR INDICATION DOUG DC10 DC1010 3022110 WP LANDING GEAR MALFUNCTIONED A HALA O OTHER N FALSE WARNING AP APPROACH 1 WP 13 148AA 46703 FLT NR 11 - HNL - WITH GEAR HANDLE DOWN ON APPROACH, ALL THREE GEAR LIGHTS WERE RED. RECYCLED GEAR, SAME THING HAPPENED . THIRD TIME, GEAR LIGHTS WERE ALL GREEN. HYDRAULIC PRESSURE WAS 3000 PSI EACH TIME. INSPECTED ALL THREE LANDING GEAR PROX SENSORS FOR CONDITION AND SECURITY. CONTACTED TULSA FOR TROUBLESHOOTING. NO HISTORY PAST 60 DAYS. REPLACED PROX CONTROL BOX FOR PRECAUTIONARY. BITE CHECK OK. (M) 2 L 7 3 4F A22WE 1996092600580 19960926 00580 WP 1996 9 26 HALA96128 1 19960828 A 2780 CONTROL CABLE DOUG DC9 DC951 3022051 WP NR 1 LE SLAT BROKEN A A HALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 699HA 47763 HNL - FLT 538 - AFTER LANDING IN KOA, RIGHT SLAT BROKEN BETWEEN 1ST AND 2ND SECTIONS, JUST OUTBOARD OF THE VORTILON. FO UND NR 1 SLAT EXTEND CABLE BROKEN. DAMAGE TO NR 2 SLAT INBOARD EDGE AND DAMAGE TO SLAT LEADING EDGE COVER NR 1. FERRIE D TO HNL. REPLACED SLAT CABLE, NR 1 SLAT PANEL AND NR 2 SLAT. ADJUSTED AND OPS CHECK OK PR MM 27-80-1, -2. (M) 2 L 7 2 4F RT A6WE 1996092600581 19960926 00581 NM 1996 9 26 HNAA9690667 1 19960830 A 3230 RETRACT MECH DHAV DHC8 DHC8102 2809003 NM NLG MALFUNCTIONED A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 906HA 009 FLT 3089 - JAX-TPA - AFTER GEAR RETRACTION ON DEPARTURE, THE MAIN GEAR RETRACTED BUT THE GEAR DOORS REMAINED OPEN. THE LT AND RT GEAR DOOR AMBER LIGHTS ILLUMINATED. THE NOSE GEAR ALSO SHOWED UNSAFE AND A GRINDING NOISE WAS HEARD FROM THE NOSE AREA. THE AIRCRAFT TURNED BACK TO JAX AND LANDED WITHOUT INCIDENT. INSPECTED THE NOSE GEAR AREA AND FOUND HALF OF TOWING LUG MISSING. SUBMITTER STATES, SUSPECT THAT THE WOW SENSOR COVER JAMMED THE NOSE GEAR FROM FULLY COMING UP. RE MOVED THE SENSOR COVER AND PLACED ON 70 HR DMT. THE NOSE LANDING GEAR WOW SENSOR COVER AND THE TOWING SPOOLS WERE REINS TALLED AT RON. (M) 2 H 7 2 4T RT A13NM 1996092600582 19960926 00582 NE 1996 9 26 M3HA96023 2 19960725 A 7320 FLIGHT IDLE GATE AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE LT ENGINE LACK OF LUBE A M3HA O OTHER G MULTIPLE FAILURE LD LANDING 1 WP 13 4204G 061 LIH - FLT 733 - LOSS OF AIRCRAFT BRAKING AND NLG STEERING ON LANDING WITH NORMAL SYSTEM INDICATIONS IN COCKPIT. IDLE GA TE WOULD NOT RELEASE MANUALLY FOLLOWING FAILURE TO RELEASE NORMALLY ON LANDING. FOUND FLT IDLE GATE STUCK IN FLT MODE. LUBED GATE LINKAGE AND SOLENOID ACTUATOR. PERFORMED PSEU BITE TEST. TEST OK. AIRCAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1996092600583 19960926 00583 EU 1996 9 26 REXA96024 1 19960805 A 2612 FIRE LIGHT SAAB SF340 340B 7860101 EU CARGO COMPT ILLUMINATED A REXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 363PX 340B260 CARGO SMOKE LIGHT CAME ON IN FLIGHT. CARGO FIRE EXTINGUISHER DISCHARGE. INSTALLED BOTTLE, P/N 365000071. OPERATIONAL CHECKED GOOD IAW AMM. PERFORMED OPERATIONAL CHECKED OF CARGO SMOKE DETECTOR. OPERATIONAL CHECKED GOOD. CLEANED AND RE SEATED CANNON PLUG ON FWD CARGO SMOKE DETECTOR. REMOVED AND REPLACED CARGO SMOKE DETECTOR TIMER RELAY. (M) 2 L 7 2 4T RT A52EU 1996092600584 19960926 00584 1996 9 26 REXA96025 4 19960411 A 3454 6226137001 NAV RECEIVER SAAB SF340 SF340A 7850100 EU AVIONICS BAY SHORTED A REXA A UNSCHED LANDING J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 25 329PX 2501 340A076 AVIONICS SMOKE LIGHT CAME ON AND A SMELL OF SMOKE EMANATED FROM AVIONICS BAY CREW DECLARED AND EMERGENCY AND AIR RETURNE D TO ATW. REMOVED AND REPLACED NR 2 VIR 32, OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1996092600585 19960926 00585 NE 1996 9 26 REXA96026 2 19960808 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE RIGHT VIBRATION A REXA E ENGINE SHUTDOWN E VIBRATION/BUFFET CR CRUISE 1 SO 25 321PX 26276 340A031 RIGHT ENGINE HAS AN UNUSUAL VIBRATION. WHEN PROPS ARE INCREASED TO MAX, EMERGENCY CHECKLIST, SHUTDOWN ENGINE. INSPECTE D PGB MOUNTS, ENGINE, AND PROPS AND PERFORMED GROUND RUNS TO 100 PERCENT. NO DISCREPANCY FOUND. ALSO, SECURED O-RING O N RIGHT SPINNER. AIRCRAFT OK FOR CONTINUED SERVICE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 1996092600586 19960926 00586 NE 1996 9 26 REXA96027 2 19960808 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LEFT FAILED A REXA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 25 361PX 340B249 785279 LEFT ENGINE MADE A LOUD POP AT APPROX 50 PERCENT AND ITT ROSE TO 970. REMOVED AND REPLACED ENGINE. REPLACED LEFT ENGIN E, PERFORMED GROUND POWER RUNS AND LEAK CHECK IAW AMM 72-00-00. 2 L 7 2 4T 4 T RT A52EU E8NE 1996092600587 19960926 00587 EU 1996 9 26 SIMA962351 1 19960822 A 2910 MS219126 HYD FITTING AEROSP ATR42 ATR42300 8680920 EU GREEN ACCUM CRACKED A SIMA O OTHER J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SW 21 12MQ 012 ORD - FLT 4020 - CREW REPORTED, GREEN SYSTEM LOW LEVEL LIGHT CAME ON IN FLIGHT. MAINTENANCE FOUND A CRACKED HYDRAULIC F ITTING AT THE GREEN SYSTEM ACCUMULATOR AND REPLACED THE FITTING. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996092600589 19960926 00589 EU 1996 9 26 SIMA962361 1 19960823 A 3350 3012001 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST CR CRUISE 1 SW 21 425MJ 846 425 ORD - FLT 4131 - DURING FLIGHT, FORWARD ROW OR EMERGENCY LIGHTS CAME ON. CHANGED BATTERY PACK FOR EMERGENCY LIGHTS AT 4 3WL. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996092600590 19960926 00590 NM 1996 9 26 TSAA9653071 1 19960909 A 5320 FRAME BOEING 737 7372M6C 1384708 NM SERVICE DOOR CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 21809 DURING SCHEDULED INSPECTION OF FUSELAGE, FORWARD SERVICE DOORWAY AFT FRAME, DISCOVERED INTERCOSTAL S8A CRACKED. REPAIRE D PER ECO 1475R4 PART 3 AND PER DRAWING 65C33436. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1996092600591 19960926 00591 NM 1996 9 26 USAASB96149 1 19960809 A 2130 PRESSURIZATION BOEING 737 7372B7 1384560 NM CABIN MALFUNCTIONED A USAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 EA 19 284AU 23131 PIT - FLT 1217 - DUE TO HEAVY LOAD, TAKEOFF WAS ACCOMPLISHED WITH APU BLEED USED FOR PRESSURIZATION. IN CLIMB, CREW SWI TCHED RIGHT PACK ON AND HEARD A BANGING NOISE FOLLOWED BY A LOUD HISS. PRESSURIZATION WENT TO AUTO FAIL AND THE CABIN B EGAN TO CLIMB WITH THE PLANE. FLIGHT ATTENDANT NOTIFIED CREW THAT CABIN WAS FILLING WITH SMOKE. CREW TURNED OFF ALL BL EEDS AND PACKS, DECLARED AN EMERGENCY AND RETURNED TO FIELD AT PIT WHERE THE FLIGHT LANDED SAFELY WITH NO FURTHER INCIDE NT. MAINTENANCE RAN BOTH ENGINES AND APU ONE AT A TIME TO PRESSURIZE CABIN. NO SMOKE NOTED IN CABIN OR COCKPIT. PRESS URIZATION CONTROL CHECKED OK PER MM 21-30-0. (M) 2 L 7 2 4F A16WE 1996092600592 19960926 00592 WP 1996 9 26 VTZA96283 2 19960726 A 7321 31059005 FUEL CONTL UNIT JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE3311 01514 WP NR 2 ENG FAILED A VTZA D E RETURN TO BLOCK ENGINE SHUTDOWN X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 EA 27 301UE 41012 FLT 6216 - PVD-IAD - DURING TAX, RETURNED TO GATE DUE TO NR 2 ENGINE FLAMED OUT WHEN CONDITION LEVER MOVED TO FLT. AIRC RAFT WAS ABOUT TO START TAKEOFF ROLL. MAINTENANCE REMOVED AND REPLACED FUEL CONTROL UNIT, OPS CHECK OK. AIRCRAFT WAS R ELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 3 T RT A41NM E3WE 1996092600593 19960926 00593 WP 1996 9 26 VTZA96289 2 19960802 A 7320 FUEL CONTROL JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE3311 01514 WP RT ENG OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 27 316UE 41055 FLT NR 6508 - ROA-IAD - DURING TAKEOFF, ABORTED TAKEOFF DUE TO RIGHT ENGINE WOULD ONLY MAKE 78 PERCENT TORQUE ON TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED MAX FLOW STOP AND RANGE COMPENSATION. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 3 T RT A41NM E3WE 1996092600594 19960926 00594 NM 1996 9 26 W8PA960107 1 19960731 A 5754 SKIN BOEING 737 7373B7 1384580 NM NR 5 LE FLAP DELAMINATED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 952WP 23378 NR 5 SLAT UPPER SKIN AT OUTBOARD END HAS DELAMINATED SKIN. REMOVED DAMAGE ON UPPER SKIN TIE OUTBOARD. RECOVERED AND FA BRICATED DOUBLERS. INSTALLED DOUBLERS AND ADHESIVE CORE. BAGGED FOR A 250 DEGREE COOK. REMOVED BAG CLEANED AND SANDED AREA IAW SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 1996092600595 19960926 00595 NM 1996 9 26 W8PA960108 1 19960731 A 5753 SKIN BOEING 737 7373B7 1384580 NM RT TE AFT FLAP DELAMINATED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 952WP 23378 OUTBOARD AFT FLAP HAS DELAMINATED SKIN AT INBOARD CORNER. REMOVED DAMAGE. FABRICATED DOUBLERS AND INSTALLED WORK DONE IAW SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 1996092600596 19960926 00596 NM 1996 9 26 W8PA960109 1 19960731 A 5753 SKIN BOEING 737 7373B7 1384580 NM RT TE FLAP DELAMINATED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 952WP 23378 RT WING INBOARD FORWARD FLAP INNER SKIN HAS DELAMINATED SKIN, 16 INCHES FROM INBOARD EDGE. FABRICATED FILLER AND DOUBLE R AND INSTALLED ALL WORKED IAW SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 1996092600597 19960926 00597 NM 1996 9 26 W8PA960110 1 19960808 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 389.5 CREASED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 952WP 23378 FOUND CREASE IN SKIN BS 389.5 BETWEEN STRINGER 15-16 LEFT. REMOVED DAMAGED PORTION OF SKIN INSPECTED CUTOUT FOR CREASE. NO CRACKS NOTED. FABRICATED REPAIR PARTS FILLER DOUBLERS AND INSTALLED REPAIR PARTS. (M) 2 L 7 2 4F RT A16WE 1996092600598 19960926 00598 NM 1996 9 26 W8PA960111 1 19960807 A 5347 BAC15201397 FLOOR TRACK BOEING 737 7373B7 1384580 NM BS 942, 945 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 952WP 23378 AFT CARGO BAY RIGHT FLOOR TRACK HAS CORROSION AT BS 942 AND BS 945, RBL 14 (OUT OF LIMITS PER SRM 53-60-53). REMOVED DA MAGED TRACK, FABRICATED, INSTALLED REPAIR PARTS IAW SRM 53-00-53. (M) 2 L 7 2 4F RT A16WE 1996092600599 19960926 00599 NM 1996 9 26 W8PA960112 1 19960807 A 5320 BAC1509100146 SUPPORT BOEING 737 7373B7 1384580 NM BS 860 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 952WP 23378 FOUND CORROSION ON FLOOR SUPPORT AROUND NUT PLATE, BS 846 AND BS 860 RBL 7.5, WL 164 (OUT OF LIMITS AT BS 860 PER SRM 53 -60-53). REMOVED DAMAGED AREA, FABRICATED, INSTALLED REPAIR PARTS PER SRM 53-00-53, 51-40-021, 51-20-01. (M) 2 L 7 2 4F RT A16WE 1996092600600 19960926 00600 NM 1996 9 26 W8PA960113 1 19960807 A 5320 654961612 ANGLE BOEING 737 7373B7 1384580 NM BS 948 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 952WP 23378 CORROSION ON FLOOR TO BULKHEAD SUPPORT ANGLE, BS 948 RBL 21-LBL 21 WL 180 (OUT OF LIMITS PER SRM 53-60-53). REMOVED AND REPLACED SUPPORT ANGLE PER SRM 51-40-02, 51-20-01. (M) 2 L 7 2 4F RT A16WE 1996092600601 19960926 00601 NM 1996 9 26 W8PA960114 1 19960807 A 5320 BAC150910048 SUPPORT BOEING 737 7373B7 1384580 NM BS 860 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 952WP 23378 FOUND CORROSION ON FLOOR SUPPORT BS 860 LBL 7.5, WL 164 AROUND NUTPLATES (OUT OF LIMITS PER SRM 53-60-53). CUT OUT DAMA GE, FABRICATED, INSTALLED REPAIR PARTS IAW SRM 53-00-53, 51-40-02, MM 25-01-12. (M) 2 L 7 2 4F RT A16WE 1996092600602 19960926 00602 NM 1996 9 26 W8PA960115 1 19960807 A 5320 65479573 THRESHOLD BOEING 737 7373B7 1384580 NM BS 793-847 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 952WP 23378 FOUND CORROSION ON THRESHOLD WEB PLATE BS 793-847, RBL 21, WL 160. OUT OF LIMITS PER SRM 53-60-15. REMOVED AND REPLACE D WEB IAW SRM 51-40-02, 51-20-01. (M) 2 L 7 2 4F RT A16WE 1996092600603 19960926 00603 NM 1996 9 26 W8PA960116 1 19960806 A 5320 BAC1509100146 SUPPORT BOEING 737 7373B7 1384580 NM BS 722 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 952WP 23378 FOUND CORROSION AROUND NUTPLATED ON FLOOR SUPPORT BS 772, RBL 3 WL 159 (OUT OF LIMITS IAW 53-30-53). REMOVED DAMAGED AR EA OF SUPPORT, FABRICATED INSTALLED REPAIR PARTS IAW SRM 53-00-53. (M) 2 L 7 2 4F RT A16WE 1996092600604 19960926 00604 NM 1996 9 26 W8PA960117 1 19960807 A 5320 BAC1509100148 SUPPORT BOEING 737 7373B7 1384580 NM BS 860 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 952WP 23378 FOUND CORROSION ON FLOOR SUPPORT BS 860 LBL 3 WL 164 AROUND NUTPLATES. OUT OF LIMITS PER SRM 53-60-53. CUT OUT DAMAGE, FABRICATED, INSTALLED REPAIR PARTS IAW SRM 53-00-53, 51-40-02, MM 25-01-12. (M) 2 L 7 2 4F RT A16WE 1996092600605 19960926 00605 NM 1996 9 26 W8PA960118 1 19960806 A 5320 6547690 SUPPORT BOEING 737 7373B7 1384580 NM BS 727-767 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 952WP 23378 FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT TOP AND BOTTOM SURFACES AROUND NUTPLATES BS 727B PLUS 9 - 767 RBL 21 WL 156 . FOUND TO BE OUT OF LIMITS IN IAW SRM 53-60-53. REMOVED DAMAGED AREA, FABRICATED, INSTALLED REPAIR SUPPORT IAW SRM 53 -60-53, 51-20-01, 51-40-02. (M) 2 L 7 2 4F RT A16WE 1996092600606 19960926 00606 NM 1996 9 26 W8PA960119 1 19960806 A 5320 69434961 SUPPORT BOEING 737 7373B7 1384580 NM BS 847-867 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 952WP 23378 FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT, BOTH TOP AND BOTTOM AROUND NUTPLATES BS 847-867 RBL 21 WL 162. FOUND TO B E OUT OF LIMITS PER SRM 53-60-15. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT PER SRM 53-60-15, 51-20-01, 51-40-02. (M) 2 L 7 2 4F RT A16WE 1996092600607 19960926 00607 NM 1996 9 26 W8PA960120 1 19960805 A 3210 654610914 BEAM ARM BOEING 737 7373B7 1384580 NM LT MLG CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 952WP 4P817 23378 LEFT MLG BEAM ARM IS CORRODED. REMOVED AND REPLACED LEFT MLG BEAM IAW 32-11-00. (M) 2 L 7 2 4F RT A16WE 1996092600608 19960926 00608 NM 1996 9 26 W8PA960121 1 19960805 A 3211 654611316 TRUNNION PIN BOEING 737 7373B7 1384580 NM LT MLG CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 952WP YS161 23378 FOUND LEFT MLG TRUNNION PIN IS CORRODED. REMOVED AND REPLACED TRUNNION PIN IAW HN 32-11-00. (M) 2 L 7 2 4F RT A16WE 1996092600609 19960926 00609 NM 1996 9 26 W8PA960122 1 19960820 A 3350 BULB BOEING 737 7373B7 1384580 NM CABIN LOOSE A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 952WP 23378 FOUND EMERGENCY EXIT TRACK LIGHTING BULB DISLODGED. RESECURED EXIT LIGHTING TRACK. (M) 2 L 7 2 4F RT A16WE 1996092600610 19960926 00610 NM 1996 9 26 W8PA960123 1 19960820 A 3397 WIRE BOEING 737 7373L9 1384470 NM CABIN LOOSE A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 960WP 23331 FOUND EMERGENCY EXIT LIGHTING WIRE LOOSE AND EXPOSED, ROW 23. RESECURED WIRES. (M) 2 L 7 2 4F RT A16WE 1996092600611 19960926 00611 NM 1996 9 26 W8PA960124 1 19960828 A 3350 BPS73 BATTERY BOEING 737 7373L9 1384470 NM CABIN DISCHARGED A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 961WP 5815 23332 WHEN EMERGENCY LIGHTS ACTIVATED, POWER DROPS, L1 DOOR AND FLOOR LIGHTS ROW 1-5 WORKS. REPLACED BATTERY/CHARGER ASSEMBLY . (M) 2 L 7 2 4F RT A16WE 1996092600612 19960926 00612 NM 1996 9 26 W8PA960125 1 19960904 A 3350 LIGHT BOEING 737 7373Y0 1384671 NM CABIN BROKEN A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 955WP 24463 EMERGENCY EXIT TRACK LIGHT BROKEN, LEFT SIDE ROW 9 AND EMERGENCY EXIT LIGHTS INOP, ROW 7 TO ROW 15. RESECURED LIGHT TRA CK COVER. FOUND SEVERAL WIRES PULLED AT LIGHT CONNECTIONS THROUGHOUT AIRCRAFT. RECONNECTED LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A16WE 1996092600613 19960926 00613 NM 1996 9 26 W8PA960129 1 19960831 A 3350 CONNECTORS BOEING 737 7373Q8 1384670 NM CABIN LOOSE A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 956WP 24299 EMERGENCY EXIT FLOOR LIGHTING INOP BETWEEN ROWS 15 AND 18. RESEATED WIRE CONNECTIONS. (M) 2 L 7 2 4F RT A16WE 1996092600614 19960926 00614 NM 1996 9 26 W8PA960130 1 19960904 A 3350 LIGHT BOEING 737 7373Y0 1384671 NM CABIN BROKEN A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 955WP 24463 EMERGENCY EXIT TRACK LIGHT BROKEN, LEFT SIDE ROW 9. RESECURED LIGHT TRACK COVER. (M) 2 L 7 2 4F RT A16WE 1996092600615 19960926 00615 NM 1996 9 26 W8PA960131 1 19960904 A 3397 WIRE BOEING 737 7373Y0 1384671 NM CABIN LOOSE A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 955WP 24463 EMERGENCY EXIT LIGHTS INOP ROW 7 TO 15. FOUND SEVERAL WIRES PULLED AT LIGHT CONNECTIONS THROUGH OUT AIRCRAFT. RECONNEC TED LIGHT ASSEMBLY, OPS CHECK OK. (M) 2 L 7 2 4F RT A16WE 1996092600616 19960926 00616 EU 1996 9 26 Y2PA96051 1 19960724 A 3260 A5238022 SQUAT SWITCH AMD FALC20 FALCOND 2720304 EU NLG FAILED A Y2PA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 817AA 233 GRR - AFTER TAKEOFF, THE GEAR HANDLE WOULD NOT MOVE TO RETRACT POSITION. AIRCRAFT MADE AN UNSCHEDULED LANDING. NO EMER GENCY PROCEDURES NECESSARY. FOUND NOSE LANDING GEAR SQUAT SWITCH OUT OF ADJUSTMENT. ADJUSTED NOSE GEAR SQUAT SWITCH IA W FALCON MM 32-60-10. PERFORMED LANDING GEAR RETRACTION TEST IAW FALCON MM 32-30-00. NO DEFECTS NOTED. (M) 2 L 7 2 4F A7EU 1996092600617 19960926 00617 NM 1996 9 26 RAAA96B2037 1 19960923 A 3350 900833A BATTERY PACK GRIMES 1000679LB BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 LT MID EXTERNAL EMERGENCY LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE LOW CHARGE. 2 L 7 3 4F A3WE 1996092600618 19960926 00618 NM 1996 9 26 RAAA96B2038 1 19960923 A 3350 900833A BATTERY PACK GRIMES 1000679LB BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 RT OVERWING WINDOW EMERGENCY EXIT LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE LOW CHARGE. 2 L 7 3 4F A3WE 1996092600619 19960926 00619 NM 1996 9 26 RAAA96B2039 1 19960923 A 3350 S106 BATTERY GRIMES 1000679 BOEING 727 72722C 138400F NM VENTRAL STAIR DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 VENTRAL STAIR OVERHEAD EMERGENCY EXIT LIGHT FAILED SERVICE CHECK. CHANGED 2 BATTERIES DUE LOW CHARGE. 2 L 7 3 4F A3WE 1996092600620 19960926 00620 SO 1996 9 26 RAAA96E8031 1 19960923 A 3350 100053 LIGHT LKHEED 188 188C 5262604 SO CABIN FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 RT AFT EMERGENCY EXIT PULLDOWN LIGHT FAILED SERVICE CHECK. CHANGED LIGHT ASSY. 2 L 7 4 4T 4A22 1996092600621 19960926 00621 SO 1996 9 26 RAAA96E8032 1 19960923 A 3350 S106 BATTERY PACK GRIMES 1102832 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT FAILED SERVICE CHECK. CHANGED BATTERY DUE LOW CHARGE. 2 L 7 4 4T 4A22 1996092600622 19960926 00622 NM 1996 9 26 CALA9601325 1 19960923 A 2121 215201 AIR DIST FAN BOEING 737 737130 1384435 NM AIR DIST BAY INOPERATIVE A CALA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 09 77215 18630 1502 19032 A STRONG ELECTRICAL ODOR WAS SMELLED IN THE COCKPIT AFTER TAKEOFF. THE FLIGHT ATTENDANT'S REPORTED SMOKE IN THE AFT/MID CABIN. THE AIR DISTRIBUTION FAN WAS TURNED OFF AND THE SMOKE APPEARED TO DISSIPATE. THE AIRCRAFT WAS DIVERTED TO IAD WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AIR DISTRIBUTION FAN AT FAULT. THE FAN CIRCUIT BREAKERS WERE C OLLARED AND THE CONTROL SWITCH WAS PLACARDED INOPERATIVE. 2 L 7 2 4F A16WE 1996092600623 19960926 00623 NM 1996 9 26 CALA9601326 1 19960923 A 3610 652244143 DUCT BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE RUPTURED A A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 27783 20638 685586 THE BLOW OUT PANEL ON NR 3 ENGINE UPPER OUTBOARD COWLING WAS FOUND MISSING WHEN AIRCRAFT ARRIVED. THE COWLS WERE OPENED AND THE DUCTING WAS INSPECTED. THE 13TH STAGE DUCT WAS FOUND RUPTURED. THE DUCT WAS REMOVED AND REPLACED AND A NEW BL OW OUT PANEL WAS INSTALLED. THE COWL SKIN ADJACENT TO THE SEVENTH RIB WAS FOUND HEAT DAMAGED. THE RIB WAS STRAIGHTENED AND DAMAGED RIVETS WERE REPLACED, NO CRACKS WERE FOUND. ECRA 7110-01170 WAS ISSUED FOR PERMANENT REPAIR. A DIP WAS I SSUED TO REINSPECT THE AREA EVERY 7 DAYS AND TO PERFORM A PERMANENT REPAIR WITHIN 30 DAYS. THE ENGINE WAS RUN AND DUCTS WERE LEAK CHECKED WITH NO LEAKS NOTED. 2 L 7 3 4F 4 F A3WE E2EA 1996092600624 19960926 00624 EU 1996 9 26 9620263239 1 19960810 A 5270 WARNING SYST AIRBUS 320 A320212 EU CARGO DOOR MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 339NW 367 AFTER APPLYING TAKEOFF POWER, THE AFT CARGO DOOR WARNING LIGHT ILLUMINATED. ABORTED TAKEOFF. FOUND THE DOOR LOCKED AND SECURE, DOOR OPERATION CHECKED OK. 2 L 7 2 4F RT A28NM 1996092600625 19960926 00625 WP 1996 9 26 9620279936 1 19960921 A 3350 60030451 POWER SUPPLY DOUG DC9 DC931 3022065 WP TAIL COMPT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 1799U 47370 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY B5-28, O PERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996092600626 19960926 00626 WP 1996 9 26 9620289955 1 19960920 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 922RW 47182 EMERGENCY LIGHTS IN GALLEY AND FIRST CLASS ILLUMINATED WITH NO SWITCHES ACTIVATED. REPLACED BATTERIES, OPERATIONAL CHEC K NORMAL. 2 L 7 2 4F A6WE 1996092600627 19960926 00627 WP 1996 9 26 9620299977 1 19960921 A 3350 60030451 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9341 47390 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONA L CHECK NORMAL. 2 L 7 2 4F A6WE 1996092600628 19960926 00628 NM 1996 9 26 9620306636 1 19960921 A 3350 POWER SUPPLY BOEING 747 747251B 1384892 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 636US 23547 DURING LINE CHECK, FOUND UPPER DECK FLOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996092600629 19960926 00629 1996 9 26 9620311226 4 19960921 A 2330 1022040101 DECODER DOUG DC10 DC1030 3023501 WP CABIN FAILED A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 01 226NW 26020 784 46583 DURING PREFLIGHT, THE DEMULTIPLEXER UNDER SEAT 25F BEGAN PRODUCTING ELECTRICAL SMOKE. REPLACED AFT INBOARD SECTION TIME R DECODER, SEAT HARNESS FROM 27 TO 26FG, 26 TO 25FG AND 25 TO 24FG. ALSO, REPLACED SEAT. 2 L 7 3 4F A22WE 1996092600630 19960926 00630 WP 1996 9 26 9620329923 1 19960922 A 3350 60030451 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 927RC 47469 DURING PERIODIC CHECK, TWO OVERHEAD EMERGENCY LIGHTS IN MID CABIN REMAINED ON WITH POWER TURNED OFF. REPLACED BATTERY P ACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996092600631 19960926 00631 WP 1996 9 26 9620339940 1 19960920 A 3350 POWER SUPPLY DOUG DC9 DC932 3022066 WP TAIL COMPT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 3322L 47031 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT CATWALK AND CONE RELEASE HANDLE EMERGENCY LIGHTS INOPERATIVE. REPLACED FLOOD LIGHT/POWER SUPPLY ASSEMBLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996092600632 19960926 00632 NE 1996 9 26 9620341143 2 19960922 A 7530 7426005 EVC DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 2 ENGINE MALFUNCTIONED A NWAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DE DESCENT 1 GL 01 133JC 51986 46752 86135 EN ROUTE, THE NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL DURING DESCENT. THE ENGINE WAS SHUT DOWN AND RESTARTED. CREW FOLLOWED COM PROCEDURES AND CONTINUED FLIGHT TO MSP WITHOUT FURTHER INCIDENT. ENGINE BORESCOPE WAS ACCOMPLISHED AND NO DISCREPANCIES WERE FOUND. REPLACED THE EVC AND PRECISION TRIMMED. 2 L 7 3 4F 4 F A22WE E20EA 1996092600633 19960926 00633 WP 1996 9 26 9620359752 1 19960921 A 3350 BATTERY PACK DOUG DC9 DC941 302207N WP TAILCONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 752NW 47116 DURING LINE CHECK, FOUND TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996092600634 19960926 00634 EU 1996 9 26 WWMA9600075 1 19960920 A 7603 7276100885 CONTROL CABLE SAAB SF340 340B 7860101 EU RT COND LEVER FAILED A WWMA F ACTIVATE FIRE EXT. K FLUID LOSS TX TAXI/GRND HDL 1 WP 15 313AE 340B313 UPON ARRIVAL AT THE GATE THE RIGHT CONDITION LEVER SEVERED. THE CREW WAS UNABLE TO SHUTDOWN THE RIGHT ENGINE WITH THE C ONDITION LEVER. FUEL WAS OBSERVED COMING OUT OF THE RIGHT NACELLE. THE RIGHT FIRE HANDLE WAS PULLED AND THE ENGINE SH UTDOWN IN 20 TO 30 SECONDS, THE PROPELLER DID NOT FEATHER. PASSENGERS WERE EVACUATED THROUGH THE FORWARD AIRSTAIR. MAI NTENANCE FOUND THE RIGHT FORWARD CONDITION LEVER CABLE SEVERED AND THE NR 3 PULLEY IN THE FORWARD BRACKET ASSEMBLY BROKE N. THE CABLE AND PULLEY WERE REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. PULLEY PART NUMBER IS MS202154. 2 L 7 2 4T RT A52EU 1996092600635 19960926 00635 EU 1996 9 26 WWMA9600076 1 19960923 A 2611 MS35362XX RELAY SAAB SF340 340B 7860101 EU E/E COMPT DEFECTIVE A WWMA F ACTIVATE FIRE EXT. N FALSE WARNING NR NOT REPORTED 1 WP 15 284AE 340B284 CARGO SMOKE LIGHT ILLUMINATED REPEATEDLY IN FLIGHT. BLEW BOTH CARGO FIRE EXTINGUISHERS, NO EVIDENCE OF SMOKE NOTED. UP ON LANDING BLEW BOTH ENGINE FIRE BOTTLES PER QRH. MAINTENANCE REPLACED RELAY 17WK, ALL FIRE BOTTLES AND WEU. 2 L 7 2 4T RT A52EU 1996092600636 19960926 00636 NM 1996 9 26 96FDEA01519 1 19960921 A 5210 65267491 DOOR FRAME BOEING 727 72725 1384006 NM PAX DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 511FE 18283 NR0055, 004, AFT ENTRY DOOR LT SIDE FRAME IS CRACKED AT 41 INCHES FROM BOTTOM OF DOOR. 2 L 7 3 4F A3WE 1996092600637 19960926 00637 NM 1996 9 26 96FDEA01520 1 19960921 A 5320 65267491 FRAME BOEING 727 72725 1384006 NM PAX DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 511 18283 NR0055 (004) AFT ENTRY DOOR LT SIDE FRAME IS CRACKED AT 41 INCHES FROM BOTTOM OF DOOR. *S/D* REMOVED DAMAGE AFT ENTRY DOOR LT SIDE FRAME 41 FROM BOTTOM OF DOOR. FABRICATED AND INSTALLED REPAIR PER FEDEX SRM 52-10-1 AND 51-40-03. 2 L 7 3 4F A3WE 1996092600638 19960926 00638 WP 1996 9 26 96FDEA01521 1 19960922 A 5710 FRAME DOUG DC10 DC1030 3023501 WP R/H SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 318 46837 NR6024, RT WING NR 1 SLAT O/B RIB FRAME BORESCOPE INSP HAS A CRACK INDICATION APPRX .3125 INCH PASSING THROUGH NUTPLATE AS VIEWED THROUGH LWR ACCESS HOLE. *S/D* INSTALLED NEW RIB FLANGE PER SRM 51-00-01. 2 L 7 3 4F A22WE 1996092600639 19960926 00639 WP 1996 9 26 96FDEA01522 1 19960922 A 5754 RIB DOUG DC10 DC1030 3023501 WP NR 1 LE SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 318FE 46837 NR5032, LT WING NR 1 SLAT O/B RIB FRAME HAS A2 INCH CRACK INDICATION AS VIEWED THROUGH LWR BORESCOPE ACCESS HOLE. * REMO VED AND REPLACED RIB PER SRM 53-00-01. 2 L 7 3 4F A22WE 1996092600640 19960926 00640 NM 1996 9 26 96FDEA01518 1 19960921 A 3260 65402691H1010154 SWITCH BOEING 727 72725 1384006 NM NLG INOPERATIVE A FDEA O OTHER N FALSE WARNING AP APPROACH 1 SO 25 155FE 18288 WHEN PUTTING GEAR DOWN, NOSE GEAR DOOR LIGHT INOPERATIVE. REMOVED AND REPLACED NOSE LANDING GEAR LOCK SWITCH IN ACCORDA NCE WITH MAINTENANCE MANUAL 32-61-21 PAGE 404, TESTED GOOD PER 32-61-21 PAGE 502. 2 L 7 3 4F A3WE 1996092600641 19960926 00641 NM 1996 9 26 96FDEA01517 1 19960920 A 3260 H1010154 SWITCH BOEING 727 72725 1384006 NM NLG INOPERATIVE A FDEA O OTHER N FALSE WARNING AP APPROACH 1 SO 25 155FE 18288 DURING APPROACH, GREEN NOSE GEAR LIGHT EXTINGUISHED AFTER THREE GREEN GEAR INDICATIONS WERE OBTAINED, NO RED UNSAFE LIGH TS CAME ON. GEAR WAS RECYCLED, SAFE INDICATOR WAS OBTAINED AND VISUALLY CHECKED. REMOVED AND REPLACED NG DOWN AND LOCK POSITION SWITCH, CHECKS GOOD. 2 L 7 3 4F A3WE 1996092600642 19960926 00642 1996 9 26 96FDEA01523 4 19960922 A 3418 AOA SENSOR DOUG DC10 DC1030 3023501 WP RIGHT FAILED A FDEA K NONE L NO TEST DE DESCENT 1 SO 25 68058 46705 AT 8,000 FT SLAT EXTENDED SPOILER DEPLOYED 200 STOWED AT 210 BUG WAS 197 AUTO SLAT EXTENSION + STICK SHAKER. SLAT DISA GREE LIGHT CYCLED TO T/O AND SLAT DISAGREE 3X. 35 LANDING WITH SLATS WAS ACCOMPLISHED SLAT SPEED 230. INSTALLED LT SYS OPS NORMAL AND RT AOA SENSOR HTR CUR TEST FAILED - INOP. *S/D* CORRECTED WIRING ON RT AOA SENSOR PER WIRING DIAGRAM A ND REPLACED SENSOR, O/C NORMAL. 2 L 7 3 4F A22WE 1996092600643 19960926 00643 NM 1996 9 26 96FDEA01501 1 19960906 A 5330 SKIN BOEING 727 72722C 138400F NM BS 680-700 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 113FE 19894 CORROSION ON FUSE SKIN BETWEEN STR 4 TO 6L AT STA 680 TO 700. CUT OUT DAMAGED SECTION OF FUSE SKIN, INSTALLED REPAIR DO UBLER PER SRM 53-30-3. 2 L 7 3 4F A3WE 1996092600644 19960926 00644 NM 1996 9 26 96FDEA01512 1 19960920 A 5320 6516346 DOORWAY FRAME BOEING 727 72725 1384006 NM BS 1110 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 511FE 18283 NR0324 AND 003, CORROSION (C53-111-01, -3) IN THE AFT CARGO BAY ON THE FWD SIDE OF THE AFT CARGO DOOR FRAME BS 1110 STR 19R. *S/D* REMOVED DAMAGED AREA ON FRAME AT BS 1110 STR 19R. INSTALLED REPAIR DOUBLER AND FILLER, FABRICATED AND INST ALLED 2 REPAIR SPLICES PER FEDEX SRM 51-40-3. 2 L 7 3 4F A3WE 1996092600645 19960926 00645 NM 1996 9 26 96FDEA01513 1 19960918 A 5315 6520827 FLOORBEAM BOEING 727 72725 1384006 NM BS 520 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 511FE 18283 NR0250 AND 001, CORROSION (C53-111-01-2) ON FLOORBEAM LOWER FLANGE AROUND NUTPLATE HOLE AT BS 520 WL 200 RBL 4. *S/D* C ORROSION FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLES AND REPAIR FILLER PER FEDEX SRM 53-10-8 ON FLOORBEAM LOWER FLANGE AT BS 520 WL 200 RBL 4. 2 L 7 3 4F A3WE 1996092600646 19960926 00646 NM 1996 9 26 96FDEA01515 1 19960919 A 5320 65192921 WEB BOEING 727 72725 1384006 NM BS 870 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR0686 AND 036, UPON REMOVAL OF WEB FOR ACCESS OF 870 UPPER CHORD. FOUND 870 WEB TO BE CORRODED BS 870 RBL TO LBL 50 W L 161. *S/D* REMOVED AND REPLACED 870 WEB STA 870 LBL TO RBL 70 WL 161 TO 187 PER FEDEX SRM 51-30-2. 2 L 7 3 4F A3WE 1996092600647 19960926 00647 WP 1996 9 26 96FDEA01516 1 19960920 A 5730 SKIN DOUG DC10 DC1030F 3023504 WP WS 118 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 318FE 46837 SNRM 6022, RT WING AT STA XCW118 TOP SURFACE OF WING HAS HEAVY CORROSION JUST FWD OF R3 DOOR. *S/D* BURNISHED CORROSIO N CK BY NDT AND FOUND TO BE WITHIN LIMITS PER SRM 57-10-00 FIG 61. TREATED, PRIMED. 2 L 7 3 4F RT A22WE 1996092600648 19960926 00648 NM 1996 9 26 96FDEA01524 1 19960923 A 5320 651758830 BEAM BOEING 727 72725 1384006 NM BS 266 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR0697 AND 037, WHILE WORKING NR0642 FOUND CORROSION UNDER INTERCOSTAL ON TOP FLANGE OF TRACK BEAM STA 266 WL 208 LBL 10 TO 8. *S/D* REMOVED AND REPLACED WL 208 PER FEDEX SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996092600649 19960926 00649 NM 1996 9 26 96FDEA01525 1 19960924 A 5313 65956002753 STRINGER BOEING 727 72725 1384006 NM BS 1163 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR0673 AND 038, WHILE WORKING ON NR0039 FOUND CORROSION ON STRINGER 20L AT BS 1163. 2 L 7 3 4F A3WE 1996092600650 19960926 00650 WP 1996 9 26 SCNA96259 1 19960917 A 3350 EMBS1392 POWER SUPPLY DOUG DC10 DC1010 3022110 WP CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 573SC 46905 OVERWING EMERGENCY LIGHT FAILED TEST. REMOVED AND REPLACED OVERWING EMERGENCY POWER SUPPLY IN ACCORDANCE WITH MM 33-51- 01 AND OPS CHECKED GOOD. 2 L 7 3 4F A22WE 1996092600651 19960926 00651 NM 1996 9 26 SCNA96260 1 19960920 A 3350 1315 BULB BOEING 727 727282 138408T NM CABIN FAILED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 281SC 21949 CENTER AISLE OVERHEAD EXIT SIGN HAS TWO BULBS INOP. RELAMPED AND OPS CHECKED GOOD. 2 L 7 3 4F RT A3WE 1996092600652 19960926 00652 NM 1996 9 26 SCNA96261 1 19960920 A 3350 1315 BULB BOEING 727 727282 138408T NM CABIN FAILED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 281SC 21949 EXIT SIGN OVER AFT LEFT ENTRY DOOR WAS FOUND WITH TWO BULBS INOP. RELAMPED SIGN AND OPS CHECKED GOOD. 2 L 7 3 4F RT A3WE 1996092600653 19960926 00653 NM 1996 9 26 SCNA96262 1 19960920 A 3350 328 BULB BOEING 727 727282 138408T NM CABIN FAILED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 281SC 21949 LEFT FORWARD OVERWING EXIT SIGN HAS BULBS BURNT OUT. RELAMPED SIGN AND OPS CHECKED NORMAL. 2 L 7 3 4F RT A3WE 1996092600654 19960926 00654 WP 1996 9 26 SCNA96263 1 19960921 A 2612 3512440633 FIRE LOOP DOUG DC10 DC1010 3022110 WP NR 2 ENGINE MALFUNCTIONED A SCNA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 15 572SC 46977 ENGINE NUMBER 2, LOOP-A LIGHT ILLUMINATED. PLACED ENGINE NUMBER 2 LOOP-A LIGHT ON MEL 26-1A. 2 L 7 3 4F A22WE 1996092600655 19960926 00655 CE 1996 9 26 GLBA96177 1 19960730 A 3297 WIRE BEECH 1900 1900C 1154161 CE LANDING GEAR BROKEN A GLBA O OTHER J WARNING INDICATION AP APPROACH 1 CE 01 159GL UC159 PGA - GEAR SELECTED DOWN WITH NO INDICATION OF MOTOR RUNNING OR GEAR EXTENDING. PUMPED GEAR DOWN MANUALLY. MAINTENANCE REPAIRED SMASHED WIRE. (X) 2 L 7 2 4T RT A24CE 1996092600656 19960926 00656 SO 1996 9 26 GLBA96180 1 19960821 A 2170 44E202A WATER SEPARATOR EMB 120 EMB120RT SO LEFT LEAKING A GLBA E ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 CE 01 267UE RF2605 120071 SPW - LEFT ENGINE DUCK LEAK. CREW PERFORMED IN-FLIGHT ENGINE SHUT DOWN PER CHECK LIST. MAINTENANCE REMOVED AND REPLACE D WATER SEPARATOR. (X) 2 L 7 2 4T RT A31SO 1996092600657 19960926 00657 SO 1996 9 26 GLBA96181 1 19960820 A 2750 RETRACT MECH EMB 120 EMB120RT SO TE FLAPS DIRTY A GLBA O OTHER J WARNING INDICATION CL CLIMB 1 CE 01 128AM 120109 RDU - FLAP DISAGREEMENT AFTER TAKEOFF. MAINTENANCE CLEANED FLAP TRACKS AND COULD NOT DUPLICATE DISAGREEMENT. (X) 2 L 7 2 4T RT A31SO 1996092600658 19960926 00658 CE 1996 9 26 GLBA96182 1 19960825 A 2612 24412886 FIRE LOOP BEECH 1900 1900C 1154161 CE RIGHT MALFUNCTIONED A GLBA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 CE 01 105GL 8940 UC105 CIU - RIGHT FIRE INDICATION ON GROUND. MAINTENANCE REMOVED AND REPLACED FORWARD AND AFT FIRE LOOPS. REFERENCE: OPERAT OR CONTROL NR 96ZZZX4896. (X) 2 L 7 2 4T RT A24CE 1996092600659 19960926 00659 CE 1996 9 26 96ZZZX4896 1 19960825 A 2612 24409015 FIRE LOOP BEECH 1900 1900C 1154161 CE RIGHT MALFUNCTIONED A GLBA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 CE 01 105GL 8734 UC105 CIU - RIGHT FIRE INDICATION ON GROUND. MAINTENANCE REMOVED AND REPLACED FORWARD AND AFT FIRE LOOPS. REFERENCE: OPERAT OR CONTROL NR GLBA96182. 2 L 7 2 4T RT A24CE 1996092600660 19960926 00660 CE 1996 9 26 GLBA96183 1 19960830 A 3230 571302 DC MOTOR BEECH 1900 1900C 1154161 CE LANDING GEAR MALFUNCTIONED A GLBA O OTHER J WARNING INDICATION CL CLIMB 1 CE 01 123UE 896A UC123 HON - LANDING GEAR WILL NOT RETRACT. MAINTENANCE REMOVED AND REPLACED DC MOTOR AND HYDRAULIC POWER PACK. REFERENCE: O PERATOR CONTROL NR 96ZZZX4897. (X) 2 L 7 2 4T RT A24CE 1996092600661 19960926 00661 CE 1996 9 26 96ZZZX4897 1 19960830 A 3230 1143880009 HYD POWER PACK BEECH 1900 1900C 1154161 CE LANDING GEAR MALFUNCTIONED A GLBA O OTHER J WARNING INDICATION CL CLIMB 1 CE 01 123UE MX502984 UC123 HON - LANDING GEAR WILL NOT RETRACT. MAINTENANCE REMOVED AND REPLACED DC MOTOR AND HYDRAULIC POWER PACK. REFERENCE: O PERATOR CONTROL NR GLBA96183. 2 L 7 2 4T RT A24CE 1996092600662 19960926 00662 NM 1996 9 26 96ZZZX4898 1 19960830 A 3310 24454 SWITCH BOEING 747 747284B 1384862 NM COCKPIT FAILED A TWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 305TW 20742 JFK - FLT 885 - DURING CRUISE, LIGHT SWITCH MFG PN 2445-4, ARCED AND EMITTED SMOKE AT THE R4 PANEL. TURNED OFF LIGHT SW ITCH. REPLACED LIGHT SWITCH AND LIGHTS; OPERATION CHECKED NORMAL. CHECK C-3 - 2-15-96 - MCI. 2 L 7 4 4F RT A20WE 1996092600663 19960926 00663 WP 1996 9 26 96ZZZX4899 1 19960820 A 5313 LONGERON DOUG DC9 DC915 3022036 WP BS 313 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 969Z 47001 STL - DURING OP-15, FOUND .50 INCH CRACK IN LONGERON 28L, STA 313. REPAIRED PER SRM 53-02, FIGURE 2. AIRCRAFT TOTAL TI ME: 63,463 HOURS; 76,506 CYCLES. 2 L 7 2 4F A6WE 1996092600664 19960926 00664 NM 1996 9 26 96ZZZX4900 1 19960911 A 3350 10604503 RELAY BOEING 727 727231 1384079 NM CABIN FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 64320 20053 STL - FLT 539 - DURING CRUISE, EGRESS AND EXIT LIGHTS WOULD INTERMITTENTLY ILLUMINATE. FOUND LIGHT BATTERY CHARGING REL AY R70 OPERATING INTERMITTENTLY, MFGT PN 10-604500-3. REPLACED R70 CHARGING RELAY AND LIGHTING SYSTEM OPERATION CHECKED NORMAL. CHECK C-4 - 10-29-05 - MCI. 2 L 7 3 4F A3WE 1996092600665 19960926 00665 WP 1996 9 26 96ZZZX4901 1 19960820 A 5313 LONGERON DOUG DC9 DC915 3022036 WP BS 313 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 969Z 47001 STL - DURING OP-15, FOUND A .25 INCH CRACK IN LONGERON 27L AND .50 INCH CRACK IN OUTBOARD HAT SECTION, STA 313. REPAIRE D PER SRM 53-02, FIGURE 2. AIRCRAFT TOTAL TIME: 64,463 HOURS; 76,506 CYCLES. 2 L 7 2 4F A6WE 1996092600666 19960926 00666 NE 1996 9 26 96ZZZX4902 2 19960825 A 7310 210715 FUEL FILTER BOEING 747 747131 1384881 NM PWA JT9 JT9D7A 52054 NE NR 1 ENGINE CONTAMINATED A TWAA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 CE 05 93108 19674 JFK - FLT 843 - DURING CRUISE, NR 1 ENGINE, S/N 4124, FLAMED OUT. IN-FLIGHT START WAS SUCCESSFUL. FOUND WATER IN FUEL FILTER. REPLACED FUEL FILTER, MFG P/N 210715, AND CHECKED FUEL TANKS FOR WATER. ENGINE OPERATION AND LEAK CHECK NORMAL . CHECK C-3 - 1-15-96 - MCI. 2 L 7 4 4F 4 F A20WE E20EA 1996092600667 19960926 00667 NM 1996 9 26 96ZZZX4903 1 19960825 A 2150 2040751 ACM BOEING 727 727231 1384079 NM LEFT MALFUNCTIONED A TWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 94314 20047 STL - FLT 632 - DURING CRUISE, A FAINT SMOKE ODOR WAS NOTICED IN CABIN. CLOSED NR 2 BLEED VALVE. FOUND LEFT AIR CYCLE MACHINE MALFUNCTIONING. REPLACED LEFT AIR CYCLE MACHINE, MFG P/N 204075-1. AIR CONDITIONING SYSTEM OPERATION THEN CHEC KED NORMAL. CHECK C-3 - 9-12-95 - MCI. 2 L 7 3 4F A3WE 1996092600668 19960926 00668 NM 1996 9 26 96ZZZX4904 1 19960903 A 2530 WIRE BOEING 747 747131 1384881 NM GALLEY BURNED A TWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 53116 20321 JFK - FLT 925 - DURING CRUISE, ELECTRICAL ARCING AND SMOKE WAS EMITTED FROM WORK LIGHT WIRING AT B-GALLEY COFFEEMAKER. S HUT OFF GALLEY ELECTRICAL POWER. FOUND CHARRED ELECTRICAL WIRING INSULATION. REPAIRED W0RK LIGHT AND GALLEY POWER OPER ATION CHECKED NORMAL. CHECK C-1 - 10-2-95 - JFK. 2 L 7 4 4F A20WE 1996092600669 19960926 00669 WP 1996 9 26 96ZZZX4905 1 19960903 A 2530 OVEN DOUG DC9 DC982 3022082 WP GALLEY SMOKING A TWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 957U 49702 STL - FLT 224 - DURING CRUISE, GALLEY OVEN EMITTED SMOKE. SHUT OFF OVEN. FOUND SPILLED FOOD IN OVEN. CLEANED OVEN AND OVEN OPERATION CHECKED NORMAL. CHECK C-1D - 5-16-96 - JFK. 2 L 7 2 4F A6WE 1996092600670 19960926 00670 NE 1996 9 26 96ZZZX4906 2 19960706 A 7230 789788 STATOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 2 ENGINE FAILED A TWAA E ENGINE SHUTDOWN J WARNING INDICATION IN INSP/MAINT 1 CE 05 911TW 49182 OMA - FLT 114 - INVESTIGATION OF NR 2 ENGINE, S/N 3225, SHUTDOWN REVEALED AN 8TH STAGE COMPRESSOR STATOR, MFG P/N 789788 , FRACTURED LIBERATING METAL PARTICLES INTO GAS PATH CAUSING MASSIVE HIGH PRESSURE COMPRESSOR AND TURBINE DAMAGE. ENGIN E WAS REPAIRED AND RETURNED TO SERVICE. 2 L 7 2 4F 4 F A6WE E9NE 1996092600671 19960926 00671 WP 1996 9 26 96ZZZX4907 1 19960831 A 3222 STRUT DOUG DC9 DC931 3022065 WP NLG REQUIRED SERVICE A TWAA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 993Z 47082 CVG - FLT 421 - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, NLG WOULD NOT RETRACT. LUBRICATED NOSE GEAR, SERVICED ST RUT WITH HYDRUALIC FLUID AND NITROGEN. OPERATED LANDING GEAR SEVERAL TIMES AND OPERATION AND INDICATION CHECKED NORMAL. CHECK C - 8-11-96 - STL. 2 L 7 2 4F A6WE 1996092600672 19960926 00672 NM 1996 9 26 96ZZZX4908 1 19960902 A 3350 58801 LIGHT BOEING 747 747131 1384881 NM CABIN BROKEN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 93107 19673 STL - FLT 721 - DURING CRUISE, EGRESS LIGHTS WOULD NOT TEST. FOUND LI GHT STRIP, MFG P/N 5880-1, BROKEN. REPLACED LIGH T STRIP AND EGRESS LIGHT OPERATION CHECK NORMAL. CHECK C - 6-5-96 - MCI. 2 L 7 4 4F A20WE 1996092600673 19960926 00673 NE 1996 9 26 96ZZZX4909 1 19960831 A 2841 GUAGE BOEING 747 747131 1384881 NM PWA JT9 JT9D7A 52054 NE NR 3 STICKING A A TWAA E ENGINE SHUTDOWN X ENGINE FLAMEOUT CR CRUISE 1 CE 05 93109 19675 FCO - FLT 840 - DURING CRUISE, NR 3 ENGINE, S/N 4198, FLAMED OUT. ACCOMPLISHED ENGINE SHUT-DOWN PROCEDURES. FOUND NR 3 FUEL QUANTITY GAUGE STICKING AND TANK EMPTY. CHECKED ENGINE OIL FILTERS AND CHIP DETECTORS. CHANGED FUEL FILTER. SER VICED NR 3 FUEL TANK AND ENGINE OPERATION CHECKED NORMAL. CHECK C-3 - 1-16-96 - JFK. 2 L 7 4 4F 4 F A20WE E20EA 1996092600674 19960926 00674 WP 1996 9 26 96ZZZX4910 1 19960820 A 5313 LONGERON DOUG DC9 DC915 3022036 WP BS 313 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 969Z 47001 STL - DURING OP-15, FOUND A .25 INCH CRACK IN LONGERON 26L, STA 313. REPAIRED PER SRM 53-02, FIGURE 4. AIRCRAFT TOTAL TIME: 63,463 HOURS; 76,506 CYCLES. 2 L 7 2 4F A6WE 1996092600675 19960926 00675 WP 1996 9 26 96ZZZX4911 1 19960820 A 5313 LONGERON DOUG DC9 DC915 3022036 WP BS 768 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 969Z 47001 STL - DURING O-15, FOUND A .25 INCH CRACK IN LONGERON 13R, STA 768. REPAIRED PER SRM 53-02, FIGURE 2. AIRCRAFT TOTAL T IME: 63,463 HOURS; 76,506 CYCLES. 2 L 7 2 4F A6WE 1996092600676 19960926 00676 WP 1996 9 26 96ZZZX4912 1 19960905 A 2530 50198A COFFEEMAKER DOUG DC9 DC932 3022066 WP GALLEY MALFUNCTIONED A TWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 05 925L 47357 STL - FLT 247 - AFTER TAKEOFF, GALLEY COFFEEMAKER EMITTED SMOKE AND NOXIOUS FUMES. TURNED OFF GALLEY. FOUND COFFEEMAKE R SOLENOID MALFUNCTIONING. REPLACED COFFEEMAKER, MFG P/N 50198A. GALLEY AND COFFEEMAKER OPERATION CHECK NORMAL. CHECK C - 8-21-96 - STL. 2 L 7 2 4F A6WE 1996092600677 19960926 00677 NM 1996 9 26 96ZZZX4913 1 19960909 A 2530 888011 SERVING CART BOEING 747 747131 1384881 NM GALLEY SMOKING A TWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 53110 19676 STL - FLT 2 - DURING CRUISE, FOOD SERVING CARTS EMITTED SMOKE. TURNED OFF SERVING CARTS. FOUND SPILLED FOOD IN CARTS. REPLACED SERVING CARTS, MFG P/N 88801-1, AND OPERATION CHECKED NORMAL. CHECK C-2 - 6-15-96 - JFK. 2 L 7 4 4F A20WE 1996092600678 19960926 00678 WP 1996 9 26 96ZZZX4914 1 19960906 A 3350 58222 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN WEAK A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 925L 47357 STL - FLT 200 - DURING CRUISE, EGRESS LIGHTS FROM SEAT ROW 20 TO AFT STAIR DOOR ILLUMINATED AND WOULD NOT EXTINGUISH. F OUND POWER SUPPLY WEAK, MFG P/N 5822-2. REPLACED POWER SUPPLY AND EGRESS LIGHT OPERATION CHECKED NORMAL. CHECK C-12 - 1-11-95 - STL. 2 L 7 2 4F A6WE 1996092600679 19960926 00679 WP 1996 9 26 96ZZZX4915 1 19960908 A 3350 41B030CF00101 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 418EA 47676 STL - FLT 517 - DURING GROUND OPERATION CHECK, OVERWING EXIT LIGHTS REMAINED ILLUMINATED. FOUND BATTERY PACK WEAK, MFG P/N 41B030CF00101, AND POWER SUPPLY MALFUNCTIONING, MFG P/N 60-1177-5. REPLACED BATTERY PACK AND POWER SUPPLY AND OVERW ING EXIT LIGHT OPERATION CHECKED NORMAL. CHECK C-12 - 10-22-95 - STL. REFERENCE: OPERATOR CONTROL NR: 96ZZZX4916. 2 L 7 2 4F A6WE 1996092600680 19960926 00680 WP 1996 9 26 96ZZZX4916 1 19960908 A 3350 6011775 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 418EA 47676 STL - FLT 517 - DURING GROUND OPERATION CHECK, OVERWING EXIT LIGHTS REMAINED ILLUMINATED. FOUND BATTERY PACK WEAK, MFG P/N 41B030CF00101, AND POWER SUPPLY MALFUNCTIONING, MFG P/N 60-1177-5. REPLACED BATTERY PACK AND POWER SUPPLY AND OVERW ING EXIT LIGHT OPERATION CHECKED NORMAL. CHECK C-12 - 10-22-95 - STL. REFERENCE: OPERATOR CONTROL NR: 96ZZZX4915. 2 L 7 2 4F A6WE 1996092600682 19960926 00682 EU 1996 9 26 C2XA96BT008 1 19960907 A 7931 S7931000600100 OIL PRESS LINE AEROSP ATR42 ATR42320 8680930 EU NR 1 ENGINE LOOSE UNION A C2XA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 34820 159 ROC/EWR - FLT 3625 - AFTER TAKEOFF IN CRUISE, CREW NOTED NR 1 ENGINE OIL PRESSURE LOW AND LOOSING PRESSURE. SHUT DOWN E NGINE AND RETURNED TO ROC UNEVENTFULLY. UPON INSPECTION OF THE ENGINE IN ROC, FOUND B-NUT LOOSE. RESECURED B-NUT AND S ERVICED ENGINE WITH OIL, LEAK AND OPERATIONALLY CHECKED SATISFACTORY. ACFT TT: 14,935.5 HOURS. ACFT CYCLES: 19,104. 2 H 7 2 4T RT A53EU 1996092600683 19960926 00683 NE 1996 9 26 C2XA96CL028 2 19960903 A 7200 310440001 ENGINE AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE NR 2 FAILED A A C2XA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 09 15827 12179 514 175 120871 CLE - FLT 3075 - CREW REPORTED THE NR 2 ENGINE INTERNAL TURBINE TEMPERATURE EXCEEDED LIMITS AFTER TAKEOFF, AIRCRAFT RETU RNED TO FIELD. MAINTENANCE INSPECTED THE ENGINE AND FOUND A BLEED AIR LINE CLAMP TO HAVE BROKEN CAUSING THE LINE TO LOO SEN AND THE ENGINE ITT TO RISE BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE IAW CONTINENTAL EXPRESS TASK CARD NR 72-00-00, ALL OPERATONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T 4 T RT A53EU E20NE 1996092600684 19960926 00684 SO 1996 9 26 C2XA96CL029 1 19960904 A 7312 MS9967116 O-RINGS EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE CUT A C2XA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 58733 120197 115267 BUF - FLT 3000 - CREW REPORTED THAT DURING CRUISE, THE RIGHT HAND ENGINE LOST OIL PRESSURE, AIRCRAFT DIVERTED TO BUF. M AINTENANCE INSPECTED O-RINGS IAW EMB-120 MM 73-12-00. OPERATIONAL AND LEAK CHECKS WERE GOOD IAW EMB-120 MM 71-00-00. A IRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T 4 T RT A31SO E20NE 1996092600685 19960926 00685 EU 1996 9 26 C2XA96IA224 1 19960907 A 5313 S5367130023000 STRINGER AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14825 170 IAH - DURING C-CHECK INSPECTION, STR 13 RT UNDER FRAME 40, WAS FOUND CORRODED. MAINTENANCE REMOVED THE DAMAGED SECTION OF STRINGER AND PERFORMED A SPLICE REPAIR PER ATR SRM 53-00-00, AND THE AIRCRAFT WAS APPROVED FOR RETURNED TO SERVICE. A IRCRAFT TT: 14,093.6 HOURS. TC: 17,152. (X) 2 H 7 2 4T RT A53EU 1996092600686 19960926 00686 EU 1996 9 26 C2XA96IA225 1 19960907 A 5313 S5367140024100 STRINGER AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14825 170 IAH - DURING C-CHECK INSPECTION, STR 20 RT BETWEEN FRAMES 32 AND 33 WAS FOUND CORRODED. MAINTENANCE REMOVED THE DAMAGED SECTION OF STRINGER AND PERFORMED A SPLICE REPAIR PER ATR SRM 53-00-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SER VICE. ACFT TT: 14,093.6 HOURS. TC: 17,152. (X) 2 H 7 2 4T RT A53EU 1996092600687 19960926 00687 EU 1996 9 26 C2XA96IA226 1 19960907 A 5753 S5751002220100 RIB AEROSP ATR42 ATR42320 8680930 EU LT TE FLAP WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14825 170 IAH - DURING C-CHECK INSPECTION, THE AFT ATTACH POINT ON THE LEFT INBOARD FLAP CENTER HINGE ARM WAS FOUND TO HAVE PLAY. MAINTENANCE REPAIRED THE FLAP PER EC5750-01091, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 14,093. 6 HOURS. TC: 17,152. (X) 2 H 7 2 4T RT A53EU 1996092600688 19960926 00688 SO 1996 9 26 C2XA96IA227 1 19960912 A 5553 12015374001 ANGLE EMB 120 EMB120RT SO VERTICAL STAB CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17728 120182 IAH INSPECTION: 1C, 2C, 4C. TOTAL TIME: 12,085.2 HOURS. TOTAL CYCLES: 17,466. DURING A ROUTINE INSPECTION, THE VE RTICAL STABILIZER TO FUSELAGE, LEFT ATTACHMENT ANGLE WAS FOUND CRACKED AT 2 FASTENER HOLES. MAINTENANCE REMOVED AND REP LACED PART, AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1996092600689 19960926 00689 SO 1996 9 26 C2XA96IA229 1 19960912 A 5400 12030995001 ANGLE EMB 120 EMB120RT SO LT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17728 120182 IAH - INSPECTION: 1C, 2C, 4C. TOTAL TIME: 12,085.2 HOURS. TOTAL CYCLES: 17,466. DURING A ROUTINE INSPECTION, THE L T NACELLE WAS FOUND TO HAVE A CRACKED SUPPORT ANGLE AT FRAME NR 2. MAINTENANCE REMOVED ANE REPLACED SUPPORT ANGLE AT N ACELLE FRAME NR 2. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1996092600690 19960926 00690 SO 1996 9 26 C2XA96IA230 1 19960912 A 5347 12015995003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17728 120182 IAH - INSPECTION: 1C, 2C, 4C. TOTAL TIME: 12,085.2 HOURS. TOTAL CYCLES: 17,466. DURING A ROUTINE INSPECTION, THE C ABIN FLOOR LEVEL LT SEAT TRACK WAS FOUND CORRODED BEYOND MANUFACTURER'S LIMITS. THE CABIN LT FORWARD FLOOR LEVEL SEAT T RACK WAS REMOVED AND REPLACED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1996092600691 19960926 00691 SO 1996 9 26 C2XA96IA231 1 19960912 A 5347 12026864007 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17728 120182 IAH - INSPECTION: 1C, 2C, 4C. TOTAL TIME: 12,085.2 HOURS. TOTAL CYCLES: 17,466. DURING A ROUTINE INSPECTION, THE C ABIN FLOOR LEVEL LT AFT SEAT TRACK WAS FOUND TO BE CORRODED BEYOND MANUFACTURER'S LIMITS. MAINTENANCE REMOVED AND REPLA CED LT AFT FLOOR SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1996092600692 19960926 00692 SO 1996 9 26 C2XA96IA232 1 19960912 A 5347 12016000003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17728 120182 IAH - INSPECTION: 1C, 2C, 4C. TOTAL TIME: 12,085.2 HOURS. TOTAL CYCLES: 17,466. DURING A ROUTINE INSPECTION, THE R T FLOOR LEVEL FORWARD SEAT TRACK WAS FOUND CORRODED BEYOND MANUFACTURER'S LIMITS. MAINTENANCE REMOVED AND REPLACED THE RT FORWARD FLOOR SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1996092600693 19960926 00693 SO 1996 9 26 C2XA96IA233 1 19960912 A 5347 12015997003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17728 120182 IAH - INSPECTION: 1C, 2C, 4C. TOTAL TIME: 12,085.2 HOURS. TOTAL CYCLES: 17,466. DURING A ROUTINE INSPECTION, THE C ABIN RT FORWARD SIDEWALL SEAT TRACK WAS FOUND CORRODED BEYOND THE MANUFACTURER'S LIMITS. MAINTENANCE REMOVED AND REPLAC ED THE RT FORWARD SIDEWALL SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1996092600694 19960926 00694 NE 1996 9 26 96ZZZX4917 2 19960720 A 7230 804061 BEARING DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE NR 2 ENGINE FAILED A A TWAA K NONE E VIBRATION/BUFFET IN INSP/MAINT 1 CE 05 9409F 53121 STL - FLT 315 - INVESTIGATION OF NR 2 ENGINE, S/N 1213, SHUT DOWN DUE TO VIBRATION REVEALED THE NR 3 BEARING, MFG P/N 80 4061, RIVETS FRACTURED LIBERATING METAL PARTICLES INTO OIL SYSTEM. THE NR 3 BEARING WAS REPLACED AND ENGINE REPAIRED AN D RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A6WE E9NE 1996092600695 19960926 00695 NE 1996 9 26 96ZZZX4918 2 19960611 A 7230 BEARING BOEING 727 727231 1384079 NM PWA JT8 JT8D9A 52048 NE NR 3 ENGINE FAILED A A TWAA E ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 CE 05 54352 21984 JFK - FLT 766 - INVESTIGATION OF NR 3 ENGINE, S/N 1545, SHUT DOWN DUE TO OIL FILTER BYPASS LIGHT ILLUMINATION REVEALED T HE NR 3 BEARING, MFG P/N 57796, RIVETS FRACTURED LIBERATING METAL PARTICLES INTO OIL SYSTEM. THE NR 3 BEARING WAS REPLA CED AND ENGINE REPAIRED AND RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 1996092600696 19960926 00696 SO 1996 9 26 WTAA960165 1 19960818 A 7712 30005000041 TQ SIGNAL COND EMB 120 EMB120RT SO RT ENGINE FAILED A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 17 251YV 120251 SBP - NO TORQUE INDICATION ON RIGHT INDICATORS ON TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. AIRCRAFT FERRIED TO FAT FOR MAINTENANCE. MAINTENANCE REPLACED RIGHT ENGINE TORQUE SIGNAL CONDITIONER. ENGINE GROUND RUN NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1996092600697 19960926 00697 EU 1996 9 26 WTAA960166 1 19960818 A 3220 LANDING GEAR BAG JETSTM JETSTM3101 1500215 EU NLG BIRD STRIKE A WTAA O OTHER C F.O.D. TO TAKEOFF 1 WP 17 431UE 813 SFO - ON TAKEOFF AT BFL, CREW DETECTED POSSIBLE BIRD STRIKE AT NOSE LANDING GEAR ON ROTATION. AIRCRAFT CONTINUED TO STA TION AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED NOSE LANDING GEAR AND NOSE AREA. NO EVIDENCE OF BIRD STRIKE, N O DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A21EU 1996092600698 19960926 00698 EU 1996 9 26 WTAA960167 1 19960819 A 3233 6158E ACTUATOR BAG JETSTM JETSTM3101 1500215 EU NLG BYPASSING FLUID A WTAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 17 423UE 799 FAT - NOSE LANDING GEAR FAILED TO RETRACT ON TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE REMOV ED AND REPLACED NOSE LANDING GEAR ACTUATOR. GEAR RETRACTION SYSTEM OPERATIONAL AND LEAK CHECK NORMAL. AIRCRAFT RETURNE D TO SERVICE. (X) 2 L 7 2 4T RT A21EU 1996092600699 19960926 00699 NE 1996 9 26 WTAA960168 2 19960826 A 7200 ENGINE EMB 120 EMB120RT SO PWA 118 PW118A NE RIGHT BIRD STRIKE A WTAA O OTHER C F.O.D. CL CLIMB 1 WP 17 120AM 120012 SFO - BIRD STRIKE REPORTED ABOVE RIGHT ENGINE INTAKE ON DEPARTURE FROM SFO. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENA NCE ACCOMPLISHED BIRD STRIKE INSPECTION. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T 4 T RT A31SO E20NE 1996092600700 19960926 00700 SO 1996 9 26 RAAA96E4014 1 19960924 A 3234 MS2876240160 HOSE ASSY LKHEED 188 188C 5262604 SO BS 90 MISROUTED A RAAA A UNSCHED LANDING O OTHER CL CLIMB 1 AL 03 9744C 188C1140 AFTER TAKEOFF, LANDING GEAR CONTROL HANDLE WOULD NOT GO PAST NEUTRAL TO THE UP POSITION. AIRCRAFT RETURNED TO ANC AND L ANDED WITHOUT INCIDENT. FOUND WINDSHIELD WIPER HYDRAULIC PRESSURE HOSE ASSY INTERFERING WITH MAIN LANDING GEAR CONTROL LEVER ARM ASSY. REPOSITONED HOSE ASSY AND LANDING GEAR CONTROL LEVER FUNCTIONAL CHECKED NORMAL. 2 L 7 4 4T 4A22 1996092600701 19960926 00701 NM 1996 9 26 CALA9601327 1 19960923 A 3251 651781411 ACTUATOR BOEING 727 727232 1384082 NM NLG STEERING DAMAGED A CALA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 09 14788 31434 13252 20642 THE NOSE GEAR LOCKED UP IN 90 DEGREE POSITION AFTER TAKING RUNWAY AND CREW WAS UNABLE TO STEER AIRCRAFT. THE AIRCRAFT W AS TOWED BACK TO THE GATE. MAINTENANCE FOUND THE NOSE GEAR LT STEERING ACTUATOR ROD END STRIPPED. THE NOSE GEAR LT STE ERING ACTUATOR WAS REMOVED AND REPLACED. THE RT STEERING ACTUATOR AND METERING VALVE WERE REPLACED AS A PRECAUTIONARY M EASURE. AN OPERATIONAL CHECK AND TEST OF THE STEERING SYSTEM WAS PERFORMED IAW MM 32-51-21 AND THE SYSTEM CHECKED GOOD WITH NO LEAKS NOTED. 2 L 7 3 4F A3WE 1996092600702 19960926 00702 NM 1996 9 26 CALA9601328 1 19960924 A 2913 6507506 HYD PUMP BOEING 727 727232 1384082 NM NR 1 ENGINE LEAKING A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 09 59792 17209 1360 20646 THE A-SYSTEM HYDRAULIC QUANTITY DROPPED TO APPROXIMATELY 2 .75 AND BOTH A-PUMP LOW PRESSURE LIGHTS ILLUMINATED AFTER TAK EOFF, WHEN THE GEAR LEVER WAS RAISED TO THE UP POSITION. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCID ENT. MAINTENANCE FOUND THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP AND LEFT GEAR DOOR ACTUATOR LINE LEAKING. THE NR 1 HYDRAU LIC PUMP AND THE GEAR DOOR ACTUATOR LINE WERE REMOVED AND REPLACED. THE NR 2 ENGINE HYDRAULIC PUMP WAS FOUND LEAKING HY DRAULIC FLUID OUT DRAIN LINE DURING ENGINE RUN. THE NR 2 HYDRAULIC PUMP WAS REMOVED AND REPLACED. THE HYDRAULIC SYSTEMS WERE SERVICED TO FULL AND LEAK CHECKS WERE GOOD. 2 L 7 3 4F A3WE 1996092600703 19960926 00703 NM 1996 9 26 CALA9601329 1 19960923 A 2560 69B148551 SPRING BOEING 747 747230B 1384889 NM DOOR 2L BENT A CALA K NONE O OTHER TX TAXI/GRND HDL 1 SW 09 78019 20527 DOOR 2L WOULD NOT DISARM, THE LEVER WOULD NOT MOVE TO DISARM. MAINTENANCE FOUND LEAF SPRING ON GIRT BAR BENT. THE LEAF SPRING CLIP WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 4 4F A20WE 1996092600705 19960926 00705 NM 1996 9 26 9620366635 1 19960921 A 3610 7880461 CONTROLLER BOEING 747 747227B 1384888 NM PWA JT9 JT9D7Q 52054 NE NR 2 ENGINE MALFUNCTIONED A A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 635US 32858 1279 21682 02179 DURING TAKEOFF ROLLOUT, THE NR 2 ENGINE WOULD NOT REACH TAKEOFF EPR. CREW FOLLOWED COM PROCEDURE, ABORTED TAKEOFF AND R ETURNED TO THE GATE. MAINTENANCE FOUND HIGH STAGE CONTROLLER COVER BLOWN OFF. REPLACED THE CONTROLLER AND PNEUMATIC PR ESSURE RELIEF VALVE. ALL CHECKS WERE NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4 F A20WE E3NE 1996092600706 19960926 00706 WP 1996 9 26 9620379878 1 19960922 A 3350 LIGHT DOUG DC9 DC951 3022051 WP TAILCONE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 787NC 48149 DURING LINE CHECK, FOUND TAILCONE EMERGENCY LIGHTS AND EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, BULBS AND POWER SUPPLY, OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996092600707 19960926 00707 WP 1996 9 26 9620389908 1 19960923 A 3350 6011779 BATTERY PACK DOUG DC9 DC931 3022065 WP RT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 958N 47254 DURING PERIODIC CHECK, THE RIGHT NACELLE EMERGENCY LIGHTS FAILED TEN MINUTE TEST. REPLACED BATTERY PACK, OPERATIONAL CH ECK NORMAL. 2 L 7 2 4F A6WE 1996092600708 19960926 00708 NE 1996 9 26 9620399923 2 19960922 A 7260 618700 GEARBOX DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9 52048 NE RT ENGINE CRACKED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 927RC 46936 7059 47469 666717 DURING CRUISE FLIGHT, THE RIGHT ENGINE OIL QUANTITY BEGAN DECREASING AND OIL PRESSURE WAS FLUCTUATING. CREW PERFORMED P RECAUTIONARY SHUTDOWN OF THE RIGHT ENGINE AND DIVERTED TO ABQ WHERE THEY LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT ENGINE GEARBOX, LEAK AND OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F A6WE E2EA 1996092600709 19960926 00709 EU 1996 9 26 9620503226 1 19960923 A 2761 31077050 ACTUATOR AIRBUS 320 A320211 3930320 EU NR 2 SPOILER LEAKING A NWAA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 326US 282 DURING CLIMBOUT, THE YELLOW HYDRAULIC SYSTEM FLUID DECREASED TO ZERO ACCOMPANIED BY A RIGHT WING NR 2 SPOILER ECAM INDIC ATION. THE SPOILER WAS DEPLOYED AT APPROXIMATELY 45 DEGREES. AIRCRAFT CONTINUED TO ORIGINAL DESTINATION AND LANDED WIT HOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT WING NR 2 SPOILER ACTUATOR, LEAK AND OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996092600710 19960926 00710 EU 1996 9 26 QXEA9600388 1 19960910 A 3350 1820 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 452US 11105 EVAC LIGHT AT LEFT WING EMERGENCY EXIT INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996092600711 19960926 00711 EU 1996 9 26 QXEA9600389 1 19960910 A 3350 1820 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 462AU 11054 EMERGENCY LIGHT IN CABIN OVERHEAD INOP. BULBS WERE REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996092600712 19960926 00712 EU 1996 9 26 QXEA9600390 1 19960910 A 3350 MGG1280 BULB GRIMES 5515800106 FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 802PH 11017 MID CABIN AFT FACING EMERGENCY EXIT SIGN ALL 28V BULBS ARE INOP. BULBS WERE REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996092600713 19960926 00713 EU 1996 9 26 QXEA9600391 1 19960910 A 3350 1820 BULB FOKKER FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 487US 11238 EMERGENCY LIGHT AT OVERWING EXIT 9A IS INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996092600714 19960926 00714 EU 1996 9 26 QXEA9600392 1 19960911 A 3350 1820 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 462AU 11054 EMERGENCY LIGHT IN CABIN OVERHEAD IS INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996092600715 19960926 00715 SW 1996 9 26 QXEA9600393 1 19960914 A 3230 246006 VALVE AIRIGHT 2781009015 SWRNGN SA227 SA227AC 8780603 SW LANDING GEAR MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 26861 833 AC649 SELECTED GEAR UP, NO GEAR RETRACTION. SELECTED GEAR DOWN THEN UP AGAIN, GEAR CAME UP BUT WOULDN'T STAY UP. GEAR WOULD PARTIALLY COME DOWN THEN BACK UP AGAIN, GEAR CYCLED ABOUT 3 TIMES THEN FINALLY STAYED UP. AIRCRAFT LANDED IN GEG WITHOU T FURTHER PROBLEM, FERRIED TO PDX FOR REPAIR. GEAR CONTROL VALVE REPLACED AND GEAR OPS CHECKED GOOD ON GEAR SWING. 2 L 7 2 4T RT A8SW 1996092600716 19960926 00716 EU 1996 9 26 QXEA9600394 1 19960915 A 2424 914F5696 GCU FOKKER F28 F28MK1000 4990808 EU NR 3 FAILED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 802PH 6154 11017 GENERATOR NUMBER 3 ON LINE TAXIING TO THE GATE, NUMBER ONE ENGINE WAS SHUTDOWN, BOTH AC BUSSES DROPPED OFF LINE AND ELEC TRICAL SMOKE IN THE COCKPIT. CREW WAS UNABLE TO RESET THE NUMBER 3 GENERATOR. NUMBER 3 GCU REPLACED AND SYSTEM OPS CHE CKED GOOD. 2 L 7 2 4F RT A20EU 1996092600717 19960926 00717 EU 1996 9 26 QXEA9600395 1 19960915 A 3350 MS24266R12B12SN CONNECTOR FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN LOOSE PIN A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 802PH 11017 FRONT ONE HALF OF THE FLOOR PROXIMITY LIGHTS ARE INOP. LOOSE PIN CONNECTION FOUND AND REPAIRED, LIGHTS OPS CHECKED GOOD . 2 L 7 2 4F RT A20EU 1996092600718 19960926 00718 NM 1996 9 26 QXEA9600396 1 19960915 A 2761 NAS16124 O-RING DHAV DHC8 DHC8102 2809003 NM SPOILER ACT FTG SPLIT A QXEA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 09 816PH 54 NUMBER 2 HYDRAULIC SYSTEM CAUTION LIGHT ILLUMINATED, LOST ALL HYD FLUID IN THE NUMBER 2 SYSTEM. ALTERNATE GEAR EXTENSIO N PERFORMED FOR LANDING AND AIRCRAFT LANDED WITHOUT FURTHER PROBLEM. REPLACED SPLIT O-RING AT GROUND SPOILER FITTING, R ETURN FITTING. SERVICED NUMBER 2 HYDRAULIC SYSTEM AND SYSTEM OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 1996092600719 19960926 00719 NM 1996 9 26 QXEA9600397 1 19960916 A 3350 6038443 BATTERY PACK DHAV DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 826PH 214 AFT CABIN CEILING EMERGENCY LIGHTING IS INOP. BATTERY PACK 3351-PS5 REPLACED AND LIGHT OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 1996092600720 19960926 00720 NM 1996 9 26 QXEA9600398 1 19960916 A 2150 EN249501AU CIRCUIT BREAKER DORNER DO32 DO328100 2996000 NM COCKPIT TRIPPED A QXEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 09 332PH 3010 FLIGHT ATTENDENT REPORTED SMOKE IN CABIN ON CLIMBOUT. LEFT AIR PACK SWITCHED OFF AND AIRCRAFT RETURNED TO FIELD. AIRCR AFT LANDED WITHOUT FUTHTER PROBLEM. LEFT HX FAN CIRCUIT BREAKER TRIPPED CAUSING PACK TO OVERHEAT. ALSO, TAXI LIGHT BRE AKER TRIPPED. CIRCUIT BREAKERS RESET AND LEFT AIR PACK OPS CHECKED GOOD. 2 H 7 2 4T RT A45NM 1996092600721 19960926 00721 EU 1996 9 26 QXEA9600399 1 19960916 A 3350 1820 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 452US 11105 RIGHT HAND OVERWING EMERGENCY EXIT LIGHTS ARE INOP. BULBS WERE REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996092600722 19960926 00722 EU 1996 9 26 QXEA9600400 1 19960916 A 3350 1820 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 454US 11107 RIGHT HAND OVERWING EXIT EMERGENCY LIGHT INOP AT ROW 8. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996092600723 19960926 00723 EU 1996 9 26 QXEA9600401 1 19960917 A 3350 5515800106 LIGHT FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 462AU 11054 EMERGENCY EXIT SIGN ABOVE COCKPIT DOOR INOP. LIGHT ASSY REPLACED AND SIGN OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996092600724 19960926 00724 EU 1996 9 26 QXEA9600402 1 19960917 A 3350 1820 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU GALLEY FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 462AU 11054 LOWER EMERGENCY EXIT LIGHT AT GALLEY SERVICE/EMERGENCY DOOR IS INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996092600725 19960926 00725 EU 1996 9 26 QXEA9600403 1 19960917 A 3350 1820 BULB FOKKER FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 487US 11238 EMERGENCY LIGHT OUT AT WINDOW EXIT 9E. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996092600726 19960926 00726 NM 1996 9 26 QXEA9600404 1 19960918 A 3350 1005511 LIGHT DHAV DHAV DHC8 DHC8102 2809003 NM COCKPIT INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 830PH 101 314 COCKPIT OVERHEAD EMERGENCY LIGHT INOP. LIGHT ASSY REPLACED AND LIGHT OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 1996092600727 19960926 00727 NM 1996 9 26 QXEA9600405 1 19960921 A 3350 501122803 POWER SUPPLY DORNER DORNER DO32 DO328100 2996000 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 338PH 3029 VARIOUS EMERGENCY LIGHTS ARE INOP. POWER SUPPLY REPLACED AND LIGHTS OPS CHECKED GOOD. 2 H 7 2 4T RT A45NM 1996092600728 19960926 00728 EU 1996 9 26 QXEA9600406 1 19960923 A 3350 1820 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 457US 11036 EMERGENCY LIGHT THIRD FROM THE FRONT IN THE CABIN IS INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996092600729 19960926 00729 EU 1996 9 26 QXEA9600407 1 19960923 A 3350 1820 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 803PH 11031 SEVERAL OVERHEAD EMERGENCY LIGHTS ARE INOP. BULBS WERE REPLACED AND LIGHTS OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996092600730 19960926 00730 EU 1996 9 26 QXEA9600408 1 19960924 A 3350 608903 BATTERY PACK FOKKER FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 493US 11161 EVAC LIGHT AT ROW 2 AND 4 ARE INOP. NR 4 BATTERY PACK REPLACED AND LIGHTS OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996092600731 19960926 00731 EU 1996 9 26 QXEA9600409 1 19960924 A 3350 1820 BULB FOKKER FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 487US 11238 OVERHEAD EMERGENCY LIGHT INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996092600732 19960926 00732 EU 1996 9 26 QXEA9600410 1 19960924 A 3350 MGG1280 BULB GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 478US 11227 EXIT SIGN ABOVE CABIN ENTRY WAY HAS THREE 28V BULBS INOP. BULBS WERE REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996092600733 19960926 00733 WP 1996 9 26 MWEA96526 1 19960923 A 2170 21D101 COALESCER BAG DOUG DC9 DC932 3022066 WP RT PACK DISLOGED A MWEA B G EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 GL 31 401ME 47133 PILOT REPORTS DURING CRUISE AT 25,000 FT THE CABIN ALTITUDE BEGAN INCREASING THROUGH 8,000 FT. AS IT APPROACHED 9,000 F T PERFORMED EMERGENCY DESCENT AFTER QRH PROCEDURES FAILED TO MAINTAIN CABIN ALTITUDE. ALL MASKS DROPPED AT 10,000 FT CA BIN ALTITUDE. FOUND RT WATER SEPARATOR SOCK HAD FALLEN OFF CAUSING IT TO COLLECT MOISTURE AND ICING, BLOCKED THE RT PAC K COMPLETELY OF AIR. REPLACED BOTH WATER SEPARATOR SOCKS AND THE WATER SEPERATOR TEMP CONTROL AS PRECAUTIONARY. OPS, L EAK CHECK GOOD. 2 L 7 2 4F A6WE 1996092600735 19960926 00735 WP 1996 9 26 DHL96807001 1 19960919 A 3230 AN325 BOLT DOUG DC8 DC873F 302199F WP RT MLG LACK OF LUBE A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 807DH 45990 AFTER TAKEOFF, GEAR NOT LATCHED LIGHT ILLUMINATED DURING UPLATCH CHECK. ABNORMAL PROCEDURES COMPLIED, FOUND RIGHT HAND GEAR UPLATCH UPPER AND LOWER LINK BOLTS STIFF. CLEANED, LUBED AND RETORQED, OPS CHECK OK MM 32-60. 2 L 7 4 4F RT 4A25 1996092600736 19960926 00736 NM 1996 9 26 P5CA9600722 1 19960922 A 3230 65B015397 ACTUATOR BOEING 747 747123 1384873 NM RT MLG TILT LEAKING A P5CA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 23 859FT 20326 NR 4 HYDRAULIC SYSTEM FLUID LOSS, EXTENDED WING GEAR AND WING FLAPS BY ALTERNATE METHOD. FOUND RIGHT WING LANDING GEAR POSITIONING ACTUATOR LEAKING AND NR 4 ENGINE HYDRAULIC PUMP LEAKING. REPLACED ACTUATOR AND BLED PER BOEING MAINTENANCE MANUAL 32-11-20. REPLACED NR 4 ENGINE DRIVEN PUMP PER BOEING MAINTENANCE MANUAL 29-11-05. 2 L 7 4 4F A20WE 1996092600737 19960926 00737 NM 1996 9 26 P5CA9600723 1 19960923 A 5330 SKIN BOEING 747 747123 1384873 NM FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 TWO CRACKS AT FORWARD LAVATORY SERVICE PANEL AT CUTOUT FOR PANEL 194R. REPAIRED PER BOEING SRM 51-30-03. 2 L 7 4 4F A20WE 1996092600738 19960926 00738 NM 1996 9 26 P5CA9600724 1 19960923 A 5247 RIBS BOEING 747 747123 1384873 NM APU DOOR DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 DAMAGED RIBS ON THE APU DOOR. REPAIRED PER BOEING SRM 51-10-01. 2 L 7 4 4F A20WE 1996092600739 19960926 00739 NM 1996 9 26 P5CA9600725 1 19960923 A 5330 PANEL BOEING 747 747123 1384873 NM FUSELAGE DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 DAMAGED ACCESS PANEL NR 191CL. REPAIRED PER BOEING SRM 51-40-09. 2 L 7 4 4F A20WE 1996092600740 19960926 00740 NM 1996 9 26 P5CA9600726 1 19960921 A 5730 PANEL BOEING 747 747123 1384873 NM WS 499 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 CRACKED FLYING PANEL TOP LEFT WING NEAR OLD REPAIR WS 499. REPAIRED PER BOEING SRM 51-40-09. 2 L 7 4 4F A20WE 1996092600741 19960926 00741 NE 1996 9 26 VSTA9609004 2 19960923 A 7310 8TJ88CAP4 POWER SUPPLY BOEING 737 737284 138448R NM PWA JT8 JT8D9A 52048 NE E/E COMPT INOPERATIVE A VSTA K NONE O OTHER IN INSP/MAINT 1 WP 07 310VA 31501 NO FUEL FLOW AND NR 2 ENGINES BAD POWER SUPPLY. REMOVED AND REPLACED POWER SUPPLY, OPS CHECKED GOOD. 2 L 7 2 4F 4 F A16WE E2EA 1996092700001 19960927 00001 SW 1996 9 27 GXPA96003 1 19960826 A 3260 SWITCH SWRNGN SA226 SA226TC 8780404 SW LT MLG DOWNLOCK WIRE BROKEN A GXPA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 23 167GA TC219 LEFT GEAR WOULD NOT INDICATE DOWN AND LOCKED. CYCLED, STILL NOT INDICATING DOWN AND LOCKED. VERIFIED DOWN BY CONTROL T OWER AND LANDED WITHOUT INCIDENT. REPAIRED BROKEN WIRE AT DOWNLOCK SWITCH. (X) 2 L 7 2 4T RT A8SW 1996092700002 19960927 00002 EU 1996 9 27 AWXA960528 1 19960825 A 3350 LIGHTS AIRBUS 320 A320231 3930325 EU CABIN MALFUNCTIONED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 622AW 054 PHX - FLT 583 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS IN CABIN ON WITH AC ELECT NORMAL AND SWITC H IN ARMED POSITION. CYCLED EMERGENCY LIGHT SWITCH TO ON THE BACK TO OFF. LIGHT OPERATIONS CHECK GOOD. NO FAULTS NOTE D. (M) 2 L 7 2 4F RT A28NM 1996092700003 19960927 00003 1996 9 27 COMA9610280 4 19960916 A 3414 39948E2903 AIRSPEED IND EMB 120 EMB120RT SO LT INST PANEL DEFECTIVE A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 261CA 12573 1992 120254 PILOTS AIRSPEED INDICATION IS 15 KNOTS HIGHER THAN COPILOTS. REPLACED AIRSPEED INDICATOR. 2 L 7 2 4T RT A31SO 1996092700004 19960927 00004 SO 1996 9 27 COMA9610281 1 19960918 A 7603 0881824 SOLENOID EMB 120 EMB120RT SO LT ENGINE MALFUNCTION A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 241CA 120211 FLIGHT IDLE STOP SOLENOID CHECK DOES NOT FUNCTION. REPLACED SOLENOID. 2 L 7 2 4T RT A31SO 1996092700005 19960927 00005 SO 1996 9 27 COMA9610282 1 19960920 A 7931 1153P001301 SWITCH EMB 120 EMB120RT SO RT ENGINE DEFECTIVE A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 105G 11583 195 120105 RT ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED. PRESSURE GAUGE INDICATION WAS NORMAL. REPLACED THE ENGINE OIL PRESSU RE SWITCH. 2 L 7 2 4T RT A31SO 1996092700006 19960927 00006 SO 1996 9 27 COMA9610283 1 19960919 A 3250 POTENTIOMETER EMB 120 EMB120RT SO NLG STEERING OUT OF ADJUST A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 254CA 120233 DURING TAXI AIRCRAFT PULLS HARD TO THE RIGHT. ADJUSTED NWS FEEDBACK POTENTIOMETER. TAXI CHECK SATISFACTORY. 2 L 7 2 4T RT A31SO 1996092700007 19960927 00007 SO 1996 9 27 COMA9610284 1 19960920 A 7712 300005000052 TQ SIG COND EMB 120 EMB120RT SO LT ENGINE MALFUNCTION A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 267CA 1619 609 120259 AUTO FEATHER WARNING DURING TAKEOFF. REPLACED THE LT ENGINE TORQUE SIGNAL CONDITIONER. 2 L 7 2 4T RT A31SO 1996092700008 19960927 00008 NE 1996 9 27 COMA9610285 2 19960922 A 7310 311610901 TUBE EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE LEAKING A COMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 248CA 120228 RT ENGINE LEAKING FUEL AND SMOKING AFTER SHUT DOWN. REPLACED LEAKING FUEL NOZZLE TRANSFER TUBE. 2 L 7 2 4T 4 T RT A31SO E20NE 1996092700009 19960927 00009 NE 1996 9 27 DHL96726002 2 19960921 A 7260 313594 VENT LINE BOEING 727 727228 NM PWA JT8 JT8D7A 52053 NE NR 2 ENGINE GB PLUGGED A DHLA E ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 SO 01 726DH 20409 649254 LOST OIL QUANTITY AND OIL PRESSURE ON NR 2 ENGINE, COMPLETED ENGINE SHUTDOWN. FOUND FITTING OIL DIFF SWITCH VENT LINE P ULLED OUT OF GEARBOX. REWORKED PER PW 72-61-01 REPAIR 38, REATTACHED LINE AND OPS CHECK OK. 2 L 7 3 4F 4 F A3WE E2EA 1996093000001 19960930 00001 NM 1996 9 30 96UAL900694 1 19960914 A 2782 ACTUATOR DECOTO 269002910 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 2 LE FLAP FAILED A UALA K NONE J WARNING INDICATION AP APPROACH 1 WP 29 7257U 21404 WHEN EXTENDING FLAPS TO 15, NR 2 SLAT DID NOT EXTEND. REPLACED NR 2 SLAT ACTUATOR. OPERATIONAL CHECK WAS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1996093000002 19960930 00002 NM 1996 9 30 TWRA96261 1 19960805 A 5210 65B100034 ROLLER CRANK BOEING 747 747121 1384871 NM L3 DOOR BROKEN A TWRA K NONE J WARNING INDICATION IN INSP/MAINT 1 EA 15 609FF 20354 ON POST FLIGHT INSPECTION, FOUND L3 DOOR LIGHT ON IN COCKPIT WITH DOOR CLOSED. REMOVED UPPER GATE AND UPPER GATE CONTRO L ROD. REMOVED TORQUE TUBE, LOWER GATE CONTROL ROD. REMOVED AND REPLACED LATCH ROLLER CRANKS PER MM 52-11-19. OPS CHE CKED NORMAL. RIGGING CHECKS ACCOMPLISHED ON FORWARD AND AFT UPPER ROLLERS AFTER REPLACEMENT. UPPER GATE RIGGING ADJUST MENTS OK. (M) 2 L 7 4 4F A20WE 1996100200002 19961002 00002 NM 1996 10 2 AALA961253 1 19960822 A 5330 141N3331 SKIN BOEING 757 757223 1384957 NM L1 DOOR CUTOUT GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 654A 24612 AFW - FOUND FUSELAGE SKIN AT L-1 DOOR CUTOUT HAD GOUGE BLENDED BEYOND SRM LIMITS, PER MRB 757-933. (M) 2 L 7 2 4F RT A2NM 1996100300001 19961003 00001 WP 1996 10 3 9620409933 1 19960911 A 5320 WEB DOUG DC9 DC931 3022065 WP BS 83 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 1334U 47280 DURING H-CHECK, FOUND A 6 INCH CRACK IN THE HORIZONTAL PRESSURE PANEL AT FS 83 AT THE LEFT VERTICAL FRAME ATTACH POINT. REPAIRED THE PANEL (P/N 9910073-3) PER EA 99-111213. 2 L 7 2 4F A6WE 1996100300002 19961003 00002 WP 1996 10 3 9620419912 1 19960911 A 5320 WEB DOUG DC9 DC931 3022065 WP BS 83 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 962N 47406 DURING M-CHECK, FOUND CRACKS IN THE HORIZONTAL PRESSURE PANEL AT FS 83 AT BOTH THE LEFT AND RIGHT FRAME FITTINGS. REPAI RED PANEL (P/N 9910073-3) PER EA 99-111214, 99-111215. 2 L 7 2 4F A6WE 1996100300003 19961003 00003 NM 1996 10 3 9620425534 1 19960916 A 5315 FLOORBEAM BOEING 757 757251 1384970 NM BS 1640 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 534US 24265 DURING PERIODIC CHECK, FOUND CORROSION ON THE BS 1640 FLOORBEAM UPPER CHORD FROM LBL 6 TO RBL 60. REPAIRED CHORD (P/N 1 46N5089) PER EA 55-106273. 2 L 7 2 4F RT A2NM 1996100300004 19961003 00004 WP 1996 10 3 9620439180 1 19960919 A 5320 FITTING DOUG DC9 DC914 3022034 WP BS 795 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3312L 45707 DURING H-CHECK, FOUND CORROSION ON THE LONGERON 28L END FITTING AT FS 795. REPLACED FITTING PER SRM 51-10-03. 2 L 7 2 4F A6WE 1996100300005 19961003 00005 WP 1996 10 3 9620449614 1 19960919 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 351 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 314NW 47128 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FORWARD CARGO FLOOR SUPPORT ATTACH FITTING AT FS 35 1, RBL 16. REPLACED FITTING PER SRM 51-30-2. 2 L 7 2 4F A6WE 1996100300006 19961003 00006 WP 1996 10 3 9620459178 1 19960919 A 5230 FITTING DOUG DC9 DC914 3022034 WP CARGO DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3310L 45705 DURING H-CHECK, FOUND A CRACK IN THE FORWARD CARGO DOOR SECOND FROM BOTTOM BEAM FORWARD END FITTING. REPLACED FITTING PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996100300007 19961003 00007 WP 1996 10 3 9620461152 1 19960921 A 5320 FITTING DOUG DC10 DC1040 3023508 WP BS 1509-1521 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 152US 46761 DURING T-CHECK, FOUND CORROSION ON THE LONGERON 48R ATTACH FITTING AT FS 1509 TO 1521. REPLACED FITTING (P/N AYB 7061-1 ). 2 L 7 3 4F A22WE 1996100300008 19961003 00008 WP 1996 10 3 9620479910 1 19960921 A 5320 FITTINGS DOUG DC9 DC931 3022065 WP BS 742-755 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 960N 47256 DURING H-CHECK, FOUND CORROSION ON THE LEFT AND RIGHT LONGERON 30 KEEL BEAM FITTINGS FROM FS 742 TO 755. REPLACED FITTI NGS PER SRM 51-01 PG 1. 2 L 7 2 4F A6WE 1996100300009 19961003 00009 WP 1996 10 3 9620489872 1 19960922 A 5320 FITTINGS DOUG DC9 DC951 3022051 WP PAX DOOR JAMB CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 781NC 48121 DURING H-CHECK, FOUND CRACKS IN THE AFT ENTRY DOOR JAMB FITTINGS AT BOTH THE LOWER AND MIDDLE DOOR STOPS. REPLACED FITT INGS PER SRM 51-30-2. 2 L 7 2 4F A6WE 1996100300010 19961003 00010 WP 1996 10 3 9620499304 1 19960922 A 5320 FITTING DOUG DC9 DC982 3022082 WP BS 1211 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 931MC 48057 DURING H-CHECK, FOUND CORROSION IN THE AFT CARGO DOOR CUTOUT OF THE AFT LOWER CORNER FS 1211 FRAME FITTING. REPLACED FI TTING (P/N 5936469-1) PER SRM 51-01, PAR C. 2 L 7 2 4F A6WE 1996100300011 19961003 00011 EA 1996 10 3 COMA9660149 1 19960924 A 3232 AIR917103 ACTUATOR CNDAIR CL600 CL6002B19 EA NLG DOOR MALFUNCTIONED A COMA K NONE O OTHER AP APPROACH 1 SO 01 917CA 8279 7017 NOSE LANDING GEAR VERY SLOW TO EXTEND, GEAR DISAGREE WARNING SOUNDED WHEN LANDING GEAR LOWERED. COULD NOT DUPLICATE. R EPLACED THE NOSE LANDING GEAR DOORS ACTUATOR FOR TROUBLESHOOTING. 2 L 7 2 4F RT A21EA 1996100300012 19961003 00012 EA 1996 10 3 COMA9660150 1 19960923 A 2450 V201D090BC RELAY CNDAIR CL600 CL6002B19 EA E/E COMPT MALFUNCTION A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 915CA 7013 AC ESSENTIAL BUS CAUTION INDICATOR ON. REPLACED RELAY KIXD SYSTEM, OPERATIONAL CHECK SATISFACTORY. 2 L 7 2 4F RT A21EA 1996100300013 19961003 00013 EA 1996 10 3 COMA9660151 1 19960924 A 5330 SKIN CNDAIR CL600 CL6002B19 EA FWD FUSELAGE BIRD STRIKE A COMA K NONE C F.O.D. CR CRUISE 1 SO 01 945CA 7069 BIRD STRIKE JUST FORWARD OF COPILOTS WINDSHIELD. C/W BIRD STRIKE INSPECTION, NO DAMAGE FOUND AND AIRCRAFT RETURNED TO S ERVICE. 2 L 7 2 4F RT A21EA 1996100300014 19961003 00014 NM 1996 10 3 UPS96221164 1 19960917 A 5320 SHEAR TIE BOEING 727 727247 138408F NM BS 720 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 207UP 21699 INSPECTION TYPE-C, CORROSION ON AFT SIDE OF SHEAR TIE AT BS 720C WL 149 RBL 10. MECHANICALLY REMOVED CORROSION IAW SRM 51-10-6, REWORK DEEMED OUT OF LIMITS IAW SRM 53-10-1. REPLACED SHEAR TIE IAW SRM 51-20-1, 51-30-2 AND MM 51-20-151. 2 L 7 3 4F A3WE 1996100300015 19961003 00015 NM 1996 10 3 UPS96221165 1 19960917 A 5311 FRAME BOEING 727 727247 138408F NM BS 970 CORRODED A IPXA O OTHER O OTHER IN INSP/MAINT 1 SO 01 207UP 21699 INSPECTION TYPE-C, CORROSION ON SHEAR TIE AT BS 970 FRAME RBL 8 WL 149. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-1, CUT OUT DAMAGE AND REPLACED PER SRM 53-10-4. 2 L 7 3 4F A3WE 1996100300016 19961003 00016 NM 1996 10 3 UPS96421157 1 19960829 A 5411 FRAME BOEING 747 747121 1384871 NM LT NACELLE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE-C, FRAME CRACKED AT NAC STA 163 LT. REPLACED FRAME 163 LT ACC SRM 51-30-02. 2 L 7 4 4F A20WE 1996100300017 19961003 00017 NM 1996 10 3 UPS96421158 1 19960829 A 5411 FRAME BOEING 747 747121 1384871 NM LT NACELLE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE-C, CRACK IN FRAME NAC STA 285, 7 INCHES ABOVE FIREWALL. REPLACED FRAME NAC STA 285 LT ACC SRM 51-30-02. 2 L 7 4 4F A20WE 1996100300018 19961003 00018 NM 1996 10 3 UPS96421159 1 19960829 A 5414 SKIN BOEING 747 747121 1384871 NM LT NACELLE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE-C, CRACK IN SKIN .75 INCH AT ACCESS PANEL CUTOUT NAC STA 207 LT. REPAIRED SKIN AT ACCESS PANEL CUTOUT N AC STA 207 LT, ACC SRM 54-30-03, FIG 17B. 2 L 7 4 4F A20WE 1996100300019 19961003 00019 NM 1996 10 3 UPS96421160 1 19960829 A 5320 SHEAR TIE BOEING 747 747121 1384871 NM BS 1560 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE-C, AFT CARGO COMPT FOUND CORROSION AND CRACKS IN FRAME SHEAR TIE AT SKIN ATTACHMENT BS 1560 BETWEEN S42/ 41 LT. REMOVED DAMAGED SHEAR TIE AND REPAIRED FRAME SHEAR TIE ACC SRM 53-20-04 FIG 3. 2 L 7 4 4F A20WE 1996100300020 19961003 00020 NM 1996 10 3 UPS96421161 1 19960829 A 5320 SHEAR TIE BOEING 747 747121 1384871 NM BS 1580 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE-C, AFT CARGO COMPT FOUND CRACK IN FRAME SHEAR TIE AT SKIN ATTACHMENT BS 1580 BETWEEN S34/33 RT. REMOVED CRACKED SHEAR TIE AND REPAIRED FRAME SHEAR TIE ACC SRM 53-10-04 FIG 3. 2 L 7 4 4F A20WE 1996100300021 19961003 00021 NM 1996 10 3 UPS96421162 1 19960904 A 5320 STIFFENER BOEING 747 747121 1384871 NM BS 2220 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE-C, AREA AFT OF BULK CARGO COMP FOUND CORROSION AND CRACK IN TOPSIDE OF FRAME STIFFENER AT BS 2220 S-40 L T. REPLACED FRAME STIFFENER ACC SRM 51-30-02. REMOVED REMAINING CORRROSION ON FRAME ACC SRM 51-10-01, WITHIN LIMITS OF SRM 53-10-10. 2 L 7 4 4F A20WE 1996100300022 19961003 00022 NM 1996 10 3 UPS96421163 1 19960902 A 5311 FRAME BOEING 747 747121 1384871 NM BS 1860 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE-C, AFT CARGO COMP FOUND CRACK IN FRAME INNER FLANGE UNDER REINFORCEMENT STRAP AT BS 1860, S41. REMOVED DAMAGED SECTION OF FRAME INNER FLANGE AND REPAIRED FRAME INNER FLANGE ACC SRM 51-40-03. 2 L 7 4 4F A20WE 1996100300023 19961003 00023 NM 1996 10 3 UPS96421176 1 19960910 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1980 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE-C, BULK CARGO COMPT FOUND STRINGER DENTED, CRACKED AND NOT PROPERLY REPAIRED, DUE TO OLD SKIN DAMAGE AT BS 1980, S39 LT. ALSO, FOUND SHEAR TIES BENT AT SAME LOCATION. REMOVED EXISTING REPAIR DOUBLER FROM SKIN. ENLARGED EX ISTING SKIN CUTOUT TO REMOVE ALL DAMAGED SKIN AND REPAIRED SKIN ACC TO SRM 53-30-03 FIG 1. REMOVED DAMAGED STRINGER AND REPAIRED STRINGER ACC SRM 53-10-03 FIG 1, REMOVED DAMAGED SHEAR TIES AND REPAIRED ACC TO SRM 53-10-04 FIG 3. 2 L 7 4 4F A20WE 1996100300024 19961003 00024 NM 1996 10 3 UPS96421177 1 19960830 A 5400 SPAR WEB BOEING 747 747121 1384871 NM NR 2 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE-C, AT THE FWD LOWER SPAR WEB PYLON NR 2 HEAT SHIELD BAFFLE CRACKED AT SEVERAL PLACES. REPLACED HEAT SHI ELD BAFFLE AT THE FWD LWR SPAR WEB ACC SRM 51-30-02. 2 L 7 4 4F A20WE 1996100300025 19961003 00025 NM 1996 10 3 UPS96421178 1 19960830 A 5400 HEAT SHLD BAFFLE BOEING 747 747121 1384871 NM NR 3 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE-C, AT THE FWD LOWER SPAR WEB PYLON NR 3 HEAT SHIELD BAFFLE CRACKED AT SEVERAL PLACES. REPLACED HEAT SHI ELD BAFFLE AT THE FWD LOWER SPAR WEB ACC SRM 51-30-02. 2 L 7 4 4F A20WE 1996100300026 19961003 00026 NM 1996 10 3 UPS96421179 1 19960830 A 5400 HEAT SHLD BAFFLE BOEING 747 747121 1384871 NM NR 1 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE C, AT THE FWD LOWER SPAR WEB PYLON NR 1 HEAT SHIELD BAFFLE CRACKED AT SEVERAL PLACES. REPLACED HEAT SHI ELD BAFFLE AT THE FWD LOWER SPAR WEB ACC SRM 51-30 -02. 2 L 7 4 4F A20WE 1996100300027 19961003 00027 NM 1996 10 3 UPS96421180 1 19960830 A 5400 HEAT SHLD BAFFLE BOEING 747 747121 1384871 NM NR 4 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE-C, AT THE FWD LOWER SPAR WEB PYLON NR 4 HEAT SHEILD BAFFLE CRACKED AT SEVERAL PLACES. REPLACED HEAT SHI ELD BAFFLE AT THE FWD LOWER SPAR WEB ACC SRM 51-3 0-02. 2 L 7 4 4F A20WE 1996100300028 19961003 00028 NM 1996 10 3 UPS96421181 1 19960829 A 5311 FRAME BOEING 747 747121 1384871 NM BS 1680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE-C, AFT CARGO COMP FOUND CRACK IN FRAME INNER FLANGE AT BS 1680, S35 TO 34 RT. REMOVED CRACKED SECTION F ROM FRAME INNERFLANGE AND REPAIRED FRAME INNER FLANGE ACC SRM 51-40-03. 2 L 7 4 4F A20WE 1996100300029 19961003 00029 NM 1996 10 3 UPS96421184 1 19960806 A 5320 WEB BOEING 747 747121 1384871 NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE-C, NLG WHEEL WELL TOP PANEL WEB UNDERNEATH LT SPINBRAKE INTERCOSTAL IS CRACKED. REPAIRED WEB ACC SRM 53 -30-03 FIG 1. 2 L 7 4 4F A20WE 1996100300030 19961003 00030 NM 1996 10 3 UPS96421185 1 19960925 A 5320 WEB BOEING 747 747121 1384871 NM LT MLG WW CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE-C, LT BLG WHEEL WELL CORNER OF PRESSURE DECK WEB STA 1372, LBL 127 IS CORRODED. PRESSURE DECK WEB REPAI RED ACC SRM 53-10-07. 2 L 7 4 4F A20WE 1996100300031 19961003 00031 NM 1996 10 3 UPS96421188 1 19960925 A 5320 STIFFENER BOEING 747 747121 1384871 NM LT MLG WW CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE-C, LT WLG WHEEL WELL STA 1241 FOUND CORROSION ON THE 2ND STIFFENER I/B OF THE BULKHEAD FITTING LBL 80. C ORROSION REMOVED IAW SRM 51-10-01, STIFFENER OUT OF LIMIT IAW 53-10-01, REPLACED STIFFENER ACC SRM 51-30-02. 2 L 7 4 4F A20WE 1996100300032 19961003 00032 NM 1996 10 3 UPS96421189 1 19960916 A 3232 ACTUATOR FITTING BOEING 747 747121 1384871 NM RT MLG WW CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE-C, RT WING DOOR ACTUATOR BEARING HAS TOO MUCH PLAY. REMOVED BEARING, FOUND CORROSION IN THE FITTING. R EMOVED FITTING FOUND CORROSION AFT SIDE FITTING AND ON THE KEEL BEAM. REMOVED MLG DOORS ACC 32-12-01, REPLACED DOOR ACT UATOR FITTING IAW 53-43-02, REPAIRED KEEL BEAM WEB ACC SRM 53-10-09 FIG 4, INSTALLED MLG DOORS ACC MM 32-12-01. 2 L 7 4 4F A20WE 1996100300033 19961003 00033 WP 1996 10 3 UPS96821166 1 19960825 A 5753 377590712 TRACK DOUG DC8 DC873F 302199F WP LT TE FLAP CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-CS2, LT WING FLAP STA 410 TRACKS PITTED. REPLACED TRACKS PER MM 27-51-03. 2 L 7 4 4F RT 4A25 1996100300034 19961003 00034 WP 1996 10 3 UPS96821167 1 19960826 A 5753 377590512 TRACK DOUG DC8 DC873F 302199F WP LT TE FLAP CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-CS2, LT WING STA 219 FLAP TRACKS PITTED. REPLACED TRACKS PER MM 27-51-03. 2 L 7 4 4F RT 4A25 1996100300035 19961003 00035 WP 1996 10 3 UPS96821168 1 19960826 A 5753 377590412 TRACK DOUG DC8 DC873F 302199F WP LT TE FLAP CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-CS2, LT WING STA 98 FLAP TRACKS PITTED. REPLACED TRACKS PER MM 27-51-03. 2 L 7 4 4F RT 4A25 1996100300036 19961003 00036 WP 1996 10 3 UPS96821169 1 19960826 A 5753 377590312 TRACK DOUG DC8 DC873F 302199F WP LT TE FLAP CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-CS2, LT WING STA 3 FLAP TRACKS PITTED. REPLACED TRACKS PER MM 27-51-03. 2 L 7 4 4F RT 4A25 1996100300037 19961003 00037 WP 1996 10 3 UPS96821170 1 19960824 A 5753 377590512 TRACK DOUG DC8 DC873F 302199F WP RT TE FLAP CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-CS2, MODERATE CORROSION DAMAGE ON RT WING STA 219 FLAP TRACKS. REPLACED TRACKS PER MM 27-51-03. 2 L 7 4 4F RT 4A25 1996100300038 19961003 00038 WP 1996 10 3 UPS96821171 1 19960828 A 5320 37549301N FITTING DOUG DC8 DC873F 302199F WP BS 1210 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-CS2, MODERATE CORROSION DAMAGE ON C-DOOR LOWER JAMB T-BOLT BACK UP FITTING FS 1210. REPLACED FITTING PE R SRM 53-2-0, FIG 2D. 2 L 7 4 4F RT 4A25 1996100300039 19961003 00039 WP 1996 10 3 UPS96821172 1 19960828 A 5320 4641324N FITTING DOUG DC8 DC873F 302199F WP BS 1692 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-CS2, HEAVY CORROSION AND CRACKED FITTING AT FS 1692 LONGERON 28R. REPLACED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996100300040 19961003 00040 WP 1996 10 3 UPS96821173 1 19960828 A 5313 564932856 LONGERON DOUG DC8 DC873F 302199F WP BS 1706 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-CS2, HEAVY CORROSION ON LONGERON 26R, FS 1706. REPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996100300041 19961003 00041 WP 1996 10 3 UPS96821174 1 19960828 A 5313 564932859 LONGERON DOUG DC8 DC873F 302199F WP BS 1765 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-CS2, HEAVY CORROSION ON LONGERON 28L FS 1765 OUTBOARD LEG. REPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996100300042 19961003 00042 WP 1996 10 3 UPS96821175 1 19960826 A 5320 3751192503 FITTING DOUG DC8 DC873F 302199F WP BS 1640 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-CS2, CRACKED FLOORBEAM ATTACH FITTING FS 1640 LONGERON 21R. REPLACED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996100300043 19961003 00043 1996 10 3 UPS96821183 2 19960925 A 7200 ENGINE DOUG DC8 DC873F 302199F WP NR 1 FAILED A IPXA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 812UP 46112 INSPECTION TYPE-N/A, LOSS OF OIL QTY FOLLOWED BY LOSS OF OIL PRESSURE AFTER APPROX 2 HRS ON NR 1 ENGINE. INFLIGHT SHUTD OWN ACCOMPLISHED BEFORE PRESSURE GOT BELOW 10 PSI. REPLACED ENGINE. 2 L 7 4 4F RT 4A25 1996100300044 19961003 00044 WP 1996 10 3 UPS96821186 1 19960828 A 5320 5612298343 WEB DOUG DC8 DC873F 302199F WP BS 8-20 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-CS2, HEAVY CORROSION ON COCKPIT SUBFLOOR WEB UPPER HORIZONTAL SURFACE FS 20 TO 8 LONGERON 22L. REPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996100300045 19961003 00045 WP 1996 10 3 UPS96821187 1 19960828 A 5320 DC853B003501 DOUBLER DOUG DC8 DC873F 302199F WP BS 1470 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-CS2, HEAVY CORROSION DAMAGE AT 2 SEAT TRACK SPLICE DOUBLERS FS 1470 LBL 33 AND FS 1500 TO 1520, BL 0. R EPLACED DOUBLERS PER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1996100300046 19961003 00046 1996 10 3 WWMA9600080 4 19960925 A 2310 CONTROL HEAD BAG JETSTM JETSTM3201 1500217 EU NR 2 COMM RADIO FAILED A WWMA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 15 951AE 951 NR 2 COMM RADIO, DISPLAY WAS FADING AND SMELL OF SMOKING WIRES. SMELL WENT AWAY WHEN NR 2 COMM TURNED OFF. REPLACED NR 2 COMM CONTROL HEAD, OPS CHECK GOOD. 2 L 7 2 4T RT A56EU 1996100300047 19961003 00047 EU 1996 10 3 WWMA9600079 1 19960925 A 2530 HOT JUG SAAB SF340 340B 7860101 EU GALLEY FAILED A WWMA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 15 319AE 340B319 FLIGHT ATTENDANT SMELLED AN ELECTRICAL BURNING ODOR COMING FROM THE GALLEY COMPARTMENT. ALSO, THE HOT JUG AREA IS UNUSA LLY WARM. REMOVED AND DEFERRED HOT JUGS, SAFETY CLIPPED THE CIRCUIT BREAKER TO PREVENT USE OF GALLEY CIRCUITS. 2 L 7 2 4T RT A52EU 1996100300048 19961003 00048 EU 1996 10 3 WWMA9600078 1 19960925 A 2611 72111211002 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT DEFECTIVE A WWMA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 WP 15 284AE 340B284 DURING PREFLIGHT, CARGO LIGHT CAME ON APPROXIMATELY 10 TIMES. REMOVED AND REPLACED AFT CARGO SMOKE DETECTOR IAW AMM 26- 10, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1996100300049 19961003 00049 EU 1996 10 3 WWMA9600077 1 19960924 A 2611 72111211002 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT DEFECTIVE A WWMA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 WP 15 284AE 340B284 CARGO SMOKE LIGHT ILLUMINATED BEFORE START. REMOVED AND REPLACED FORWARD DETECTOR, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1996100300050 19961003 00050 NM 1996 10 3 96FDEA01526 1 19960924 A 5320 FITTING BOEING 727 72722C 138400F NM BS 950 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 106FE 19201 NR0853, STR 8L END FITTING CRACKED AT STA 950 FRAME ATTACH LEGS. *S/D* NDT CHECKED AND CRACK FOUND. 2 L 7 3 4F A3WE 1996100300051 19961003 00051 NM 1996 10 3 96FDEA01527 1 19960924 A 5320 FITTING BOEING 727 72722C 138400F NM BS 950 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 106FE 19201 NR0582, STR 7L END FITTING CRACKED AT STA 950 FRAME ATTACH LEGS. *S/D* NDT CHECKED, NO CRACK FOUND. 2 L 7 3 4F A3WE 1996100300052 19961003 00052 NM 1996 10 3 96FDEA01528 1 19960924 A 5320 FITTING BOEING 727 72722C 138400F NM BS 950 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 106FE 19201 NR0581 STR 6L END FITTING CRACKED AT STA 950 FRAME ATTACH LEGS. *S/D* REPLACED END FITTING PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996100300053 19961003 00053 NM 1996 10 3 96FDEA01529 1 19960924 A 5320 FITTING BOEING 727 72722C 138400F NM BS 950 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 106FE 19201 NR0580, STR 5L END FITTING CRACKED AT STA 950 FRAME ATTACH LEGS. *S/D* CHECKED BY NDT, NO CRACK FOUND. 2 L 7 3 4F A3WE 1996100300054 19961003 00054 NM 1996 10 3 96FDEA01530 1 19960924 A 5320 FITTING BOEING 727 72722C 138400F NM BS 950 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 106FE 19201 NR0579, STR 4L END FITTING CRACKED AT STA 950 FRAME ATTACH LEGS. *S/D* NDT CHECKED, NO CRACK FOUND. 2 L 7 3 4F A3WE 1996100300055 19961003 00055 NM 1996 10 3 96FDEA01531 1 19960924 A 5320 FITTING BOEING 727 72722C 138400F NM BS 950 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 106FE 19201 NR0578, STR 3L END FITTING CRACKED AT STA 950 FRAME ATTACH LEGS. *S/D* REPLACED END FITTING PER 51-10-1. 2 L 7 3 4F A3WE 1996100300056 19961003 00056 NM 1996 10 3 96FDEA01532 1 19960924 A 5320 FITTING BOEING 727 72722C 138400F NM BS 950 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 106FE 19201 NR0577, STR 2L END FITTING CRACKED AT STA 950 FRAME ATTACH LEGS. *S/D* REPLACED END FITTING PER 51-10-1. 2 L 7 3 4F A3WE 1996100300057 19961003 00057 1996 10 3 96FDEA01533 2 19960920 A 7530 CF680C2D1F STATOR CASE DOUG MD11 MD11F 3023600 NM NR 1 ENGINE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 612FE 48605 INSP OF THE FIRST STAGE BOOSTER VANES, EA 1-7220-31513, EA COMPLETED ON NR 1 ENG, FOUND 22 MISSING FASTENERS AND SEVERA L CRACKS IN STATOR CASE. REMOVED AND REPLACED NR 1 ENG PER WORK CARD 29T0301, 54T0201, 71T0101, 71T0701 AND FEC -M-323 8, OPS CK AND LEAK CK GOOD. 2 L 7 3 4F RT A22WE 1996100300058 19961003 00058 NM 1996 10 3 96FDEA01534 1 19960925 A 2782 651729410 ACT MOUNT BOEING 727 72725 1384006 NM NR 3 LE SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 511FE 18283 NR 0219 AND 006. NR 3 SLAT ACTUATOR ROD END MOUNT I/B AND O/B RIBS ARE CRACKED. ***S/D***** REMOVED AND REPLACED NR 3 SLAT ACTUATOR ROD AND MOUNT I/B AND O/B RIBS ON SLAT. 2 L 7 3 4F A3WE 1996100300059 19961003 00059 NM 1996 10 3 96FDEA01535 1 19960925 A 5753 66218309 SKIN BOEING 727 72725 1384006 NM RT TE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 511FE 18283 NR0576 AND 007, RT WING I/B FORE FLAP IS DELAMINATED AT I/B END UPPER SURFACE. *S/D* REPAIRED DAMAGED AREA TO RT WING I/B FORE FLAP PER SRM 51-40-6. 2 L 7 3 4F A3WE 1996100300060 19961003 00060 NM 1996 10 3 96FDEA01487 1 19960916 A 5315 65208241 FLOORBEAM BOEING 727 72725 1384006 NM BS 1166 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR 0623 AND 033, WHILE WORKING NR 0248 FOUND A CORRODED NUTPLATE HOLE AT BS 1166 LBL 12 WL 200 AFT LOWER FLANGE. *S/D* REPAIRED BS 1166 FLOORBEAM LOWER CHORD IAW EA 7-5310-31129. 2 L 7 3 4F A3WE 1996100300061 19961003 00061 NE 1996 10 3 VNAA9609004 2 19960923 A 7261 OIL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE LOW QTY A VNAA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 07 429JS 3043 EN ROUTE AT 22,000, OIL PRESSURE ON LT ENGINE DROPPED INTO PRECAUTIONARY RANGE. IN ACCORDANCE WITH THE QUICK REFERENCE HANDBOOK, FEATHERED ENGINE. DIVERTED INTO TYS AND LANDED WITHOUT INCIDENT. FOUND OIL LEVEL LOW FOR LT ENGINE. SERVICE D OIL AND AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996100300062 19961003 00062 NM 1996 10 3 96FDEA01536 1 19960925 A 5330 BAC50009 SKIN BOEING 727 72725 1384006 NM BS 1163-1183 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR0039 AND 039, BULGE IN SKIN ABOVE AFT LT SERVICE DOOR STA 1170 TO 118 STR 18L. *S/D* REPLACED SECTION OF SKIN AND R EPAIRED REF FEDEX EA 7-5330-31176. 2 L 7 3 4F A3WE 1996100300063 19961003 00063 NM 1996 10 3 96FDEA01537 1 19960926 A 5320 65198612 CHORD BOEING 727 72725 1384006 NM BS 293 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR0702 AND 040, WHILE WORKING NR0689 FOUND RT LOWER NOSE CHORD CRACKED AT BS 293 RBL 15 WL 140. *S/D* REMOVED CRACKED RT LOWER NOSE CHORD. NEW RT LOWER NOSE CHORD TO BE REINSTALLED ON NR0689 IAW BAC DRW NR 65C15724. 2 L 7 3 4F A3WE 1996100300064 19961003 00064 NM 1996 10 3 96FDEA01538 1 19960926 A 5320 651986511 CHORD BOEING 727 72725 1384006 NM BS 320 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR0705 AND 041, WHILE WORKING NR0689 FOUND LOWER LT NOSE CHORD AT 320 LBL 19 TO BE CORRODED OUT OF LIMITS. *S/D* REMOV ED CORRODED LOWER LT LOWER NOSE CHORD, NEW LOWER LT NOSE CHORD TO BE REINSTALLED ON NR0689 PER BAC DRW NR 65C15724. 2 L 7 3 4F A3WE 1996100300065 19961003 00065 WP 1996 10 3 MWEA96527 1 19960925 A 3350 1001191 FLASHLIGHT DOUG DC9 DC932 3022066 WP CABIN BROKEN CLIP A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 206ME 47791 CREW REPORTS, FWD ENTRANCE DOOR EMERGENCY FLASHLIGHT INOP DUE TO BROKEN LOWER CLIP. REPLACED FWD ENTRANCE EMERGENCY FLA SHLIGHT, OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996100300066 19961003 00066 NM 1996 10 3 DL76S962146 1 19960920 A 3350 0L3071BPEGPL BULB BOEING 767 767332 1382001 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 122DL 23436 ON FAA INSP FOUND EMERGENCY FLOOR TRACK WHITE LIGHT OUT, SEAT 45FG. 2 L 7 2 4F RT A1NM 1996100300067 19961003 00067 NM 1996 10 3 DL767962148 1 19960920 A 2121 FAN 732591D BOEING 767 767232 1385132 NM E/E COMPT SHORTED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 102DA 22214 STRONG ELECTRICAL ODOR IN AIRCRAFT ON TAXI-OUT. FWD EXHAUST EQUIPMENT COOLING FAN POPPED C/B. FWD TO MCO AND PLAC PER MEL 21-58-04A, NEEDS FAN DAL 211002542. 2 L 7 2 4F RT A1NM 1996100300068 19961003 00068 WP 1996 10 3 DLL15962155 1 19960922 A 3350 LIGHT 081691 LKHEED 1011 10113853 5265020 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 755DL 193Y1184 EMERGENCY LIGHT INOP AT SEAT 32C. REPLACED LIGHT SOCKET, BULB AND LENS. 2 L 7 3 4F A23WE 1996100300069 19961003 00069 NM 1996 10 3 DL76S962159 1 19960921 A 2560 101651303 SLIDE BOEING 767 767332 1382001 NM L-2 DOOR MALFUNCTIONED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 127DL 24077 L2 SERV DOOR ESCAPE SLIDE PACK FELL OUT OF DOOR UPON OPENING OF DOOR SLIDE. DID NOT FALL ENOUGH TO DEPLOY, DOOR WAS NOT FULLY OPENED. REPLACED L2 DOOR SLIDE ASSY, ARM/DIARM CKS NML. DOOR NOT FULLY DISARMED BY FLT ATTEND. 2 L 7 2 4F RT A1NM 1996100300070 19961003 00070 WP 1996 10 3 DLL10962163 1 19960922 A 2560 MEGAPHONE MV10 LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 725DA 193C1162 F/C MEGAPHONE IS INOP. REPLACED MEGAPHONE. 2 L 7 3 4F A23WE 1996100300071 19961003 00071 NM 1996 10 3 DL76S962165 1 19960922 A 3320 LIGHT BOEING 767 767332 1382001 NM GALLEY DIRTY A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 131DN 24852 INFLIGHT F/A REPORTED ELECT ODOR IN THE MID AND AFT GALLEY AREAS. TURNED OFF COFFEE MAKERS, GALLEY OVENS AND WORK LIGHT S ODOR WENT AWAY. FOUND GALLEY LIGHT FIXTURE WITH COOKED COFFEE RESIDUE. 2 L 7 2 4F RT A1NM 1996100300072 19961003 00072 NM 1996 10 3 DL757962166 1 19960922 A 2121 FAN BOEING 757 757232 1384965 NM CABIN FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 681DA 26957 ELECT SMELL AT MID GALLEY AREA AND SEAT ROW 20 TO 26. FOUND COOLING FAN BEARING FAILED. 2 L 7 2 4F RT A2NM 1996100300073 19961003 00073 NM 1996 10 3 DLM88962167 1 19960923 A 5210 HOLD OPEN HOOK DOUG MD88 MD88 3023688 NM PAX DOOR BENT A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 970DL 43173 FWD ENTRY DOOR HOLD OPEN HOOK BENT, WON,T HOOK DOOR. REPLACED HOOK, CKS GOOD. 2 L 7 2 4F RT A6WE 1996100300074 19961003 00074 NM 1996 10 3 DLM88962168 1 19960923 A 5210 HOLD OPEN HOOK DOUG MD88 MD88 3023688 NM PAX DOOR BENT A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 970DL 43173 ON A/C INSPECTION, FOUND THE L1 DOOR HOLD OPEN HOOK BENT. REPLACED DOOR HOLD OPEN HOOK. 2 L 7 2 4F RT A6WE 1996100300075 19961003 00075 NM 1996 10 3 DL73S962169 1 19960923 A 3350 BPS73 LIGHT BOEING 737 737232 1384475 NM CABIN INOPERATIVE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 315DL 23087 AFTER ELECT TRANSFER, EMERGENCY EXIT LIGHTS ILLUMINATED IN TOURIST CLASS, FIRST CLASS TRACK LIGHTS WERE OFF AND OVERHEAD BIN LIGHTS AND EXIT LIGHTS WERE ON. ALL WITH SWITCH IN 'ARM'. REPLACED F/C AND Y/C TRACK LIGHT POWER SUPPLYS AND BATT ERY PACKS. 2 L 7 2 4F RT A16WE 1996100300076 19961003 00076 NM 1996 10 3 DLM88962170 1 19960923 A 3350 20131A BATTERY PACK DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 953DL 49884 EMERGENCY EXIT LIGHTS FWD OF CABIN DIVIDER INOP. REPLACED FWD BATTERY PACK IN F/C OVERHEAD EMERGENCY EXIT LIGHTING SYST EM, OPS CHECKS GOOD AND TESTS GOOD. 2 L 7 2 4F RT A6WE 1996100300077 19961003 00077 NM 1996 10 3 DL72S962171 1 19960913 A 5414 SKIN BOEING 727 727232 1384082 NM BS 1099 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 403DA 21147 TWO CRACKS IN LT SIDE OF DOG HOUSE NR 2 ENG S-DUCT, 1 FT ABOVE FUSELAGE SKIN STA 1099. DYE CHECKED FOR CRACKS PER PS 90 0-6-3, 2 CRACKS FOUND. REPAIRED ONE CRACK PER MM 54-30-0 PG 802. REMOVED DAMAGED SECTION OF FWD LOWER AREA AND DRILLED REPAIR DOUBLER PER MM 53-30-0 FIG 802. INSTALLED REPAIR PER MM 54-30-0 PG 802. 2 L 7 3 4F A3WE 1996100300078 19961003 00078 1996 10 3 DL76L962172 4 19960923 A 2210 YAW DAMPER 15366005 BOEING 767 767332 1382001 NM E/E COMPT FAILED A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 172DN 1922 24775 LT HYD QUANTITY DECREASED TO .039, EDP DEPRESSURIZED AND ACMP OFF AND QUANTITY CONTINUED TO DECREASE. FOUND YAW DAMP MO DULE LEAKING. REPLACED RT YAW DAMP MODULE. 2 L 7 2 4F RT A1NM 1996100300079 19961003 00079 NM 1996 10 3 DL72S962173 1 19960923 A 5210 FRAME BOEING 727 727232 1384082 NM R2 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 421DA 21274 A .5 INCH CRACK R2 DOOR FWD FRAME AT UPPER HINGE CUTOUT LOWER CORNER. REPLACED DOOR PER M/M. 2 L 7 3 4F A3WE 1996100300080 19961003 00080 NM 1996 10 3 DL72K962175 1 19960918 A 5530 STRINGER BOEING 727 727232 1384082 NM VERTICAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 471DA 20748 CRACK IN VERTICAL STAB STRINGER AT RIB CHORD ATTACH POINT RT SIDE STR 8 FIN STA 157.2, REF EO 4-59253-12. INSTALLED DOU BLER PER M/M 55-30-0. 2 L 7 3 4F A3WE 1996100300081 19961003 00081 NM 1996 10 3 DL72S962176 1 19960924 A 5330 SKIN BOEING 727 727232 1384082 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 526DA 21586 FOUND DURING E-2 LETTER CHECK, CORROSION UNDER AFT HINGE OF FUSELAGE ACCESS PANEL 3448R, CORROSION ON I/B AND O/B SIDES OF ATTACH ANGLE. REPAIRED PER B727 MM 53-30-1 PG 807 TO 808. 2 L 7 3 4F A3WE 1996100300083 19961003 00083 NM 1996 10 3 SCNA96265 1 19960924 A 3350 582214 POWER SUPPLY BOEING 727 727282 138408T NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 281SC 21949 EMERGENCY FLOOR TRACK LIGHTING WAS FOUND INOP AT ROWS 9 THROUGH 16. REMOVED AND REPLACED BATTERY (P/N 5776-1) AND POWER SUPPLY (P/N 5822-14) AND REPLACED EMERGENCY LIGHT TRACK LEAD ASSEMBLY, OPS CHECKED NORMAL. 2 L 7 3 4F RT A3WE 1996100300084 19961003 00084 NM 1996 10 3 VSTA9609005 1 19960908 A 3350 1000677 LIGHT GRIMES 1000677 BOEING 737 737247 138448D NM CABIN INOPERATIVE A VSTA K NONE L NO TEST UK UNKNOWN 1 WP 07 304VA 2400 19617 LT OVERWING EXIT LIGHT FLICKERS ON/OFF IN FLIGHT. DEFECTIVE EXIT LIGHT ASSY. REMOVED AND REPLACED LIGHT ASSY EMER EXIT . 2 L 7 2 4F A16WE 1996100300085 19961003 00085 SO 1996 10 3 SRAA960809 1 19960820 A 2913 66039 PUMP LKHEED 382 382G 526414U SO NR 1 HYD SYST FAILED A SRAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 23 909SJ 4863 152436B 4763 DURING FLIGHT, NR 1 HYDRAULIC PUMP PRESSURE WENT TO O PSI WHEN RAISING MLG. ACCOMPLISHED AIR TURNBACK, AIRCRAFT LANDED WITHOUT INCIDENT. FOUND NR 1 HYD PUMP FAILED. REPLACED PUMP AND FILTER, INSPECTED UTILITY SYSTEM MAIN AND DRAIN FILTER S, NO CONTAMINATION NOTED. SYSTEM OPS CHECKED AND LEAK CHECKED PER MM CH 29-11-00. 2 H 7 4 4T A1SO 1996100300086 19961003 00086 SO 1996 10 3 SRAA960810 1 19960823 A 2140 GASKETS LKHEED 382 382G 526414U SO HEAT DIVIDER VLV LEAKING A SRAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 905SJ 4472 DURING FLIGHT, CARGO COMPARTMENT OVERHEAT LIGHT CAME ON GOING THROUGH 11,000 FT. TURNED SYSTEM OFF AFTER ONE MINUTE AND LIGHT WAS STILL ON, ISOLATED SYSTEM, LIGHT WENT OUT. ACCOMPLISHED AIR TURNBACK, AIRCRAFT LANDED WITHOUT INCIDENT AT 14 6,900 LBS. FOUND UPPER GASKET ON FLOOR HEAT DIVIDER VALVE AND BOTTOM GASKET OF FLOW CONTROL VALVE LEAKING. REPLACED GA SKETS AND TEMP CONTROL VALVE BLEED AIR OPS CHECKED GOOD PER MM 30 AND 21. PERFORMED HEAVY WEIGHT LANDING INSPECTION IAW J/C 5101-10, FOUND FUEL SEEP AT LEFT BOTTOM WING, RESEALED NR 2 TANK ACCESS PANEL IN DRY BAY PER MM CH 28. 2 H 7 4 4T A1SO 1996100300087 19961003 00087 SO 1996 10 3 SRAA960811 1 19960823 A 2131 1025381 CONTROLLER LKHEED 382 382G 526414U SO COCKPIT DEFECTIVE A SRAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 23 918SJ 4208 DURING FLIGHT, AIRCRAFT WOULD NOT PRESSURIZE OVER 4 AT 14,000 FT IN AUTO OR MANUAL. ACCOMPLISHED AIR TURNBACK TO LCK AN D LANDED WITHOUT INCIDENT. FOUND PRESSURE CONTROLLER DEFECTIVE. REPLACED CONTROLLER, SYSTEM OPS CHECKED GOOD PER MM CH 21. 2 H 7 4 4T A1SO 1996100300088 19961003 00088 SO 1996 10 3 SRAA960812 1 19960827 A 3350 P2 BULB LKHEED 382 382G 526414U SO CARGO COMPT FAILED A SRAA K NONE L NO TEST IN INSP/MAINT 1 GL 23 920SJ 4561 ON PREFLIGHT, FOUND CARGO EMERGENCY EXIT LIGHT WEAK, FOUND P2 LIGHT BULB DEFECTIVE. REPLACED BULB, OPS CHECKED GOOD PER MM CH 33. 2 H 7 4 4T A1SO 1996100300089 19961003 00089 SO 1996 10 3 SRAA960901 1 19960905 A 2910 SR980060296 HYD HOSE LKHEED 382 382G 526414U SO NLG LEAKING A SRAA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 23 921SJ 4586 ON APPROACH, LOST UTILITY HYDRAULIC PRESSURE WHILE LOWERING GEARS, NOSE LANDING GEAR DID NOT FULLY EXTEND. USED ALTERNA TE GEAR EXTENSION WITH AUX HYDRAULIC PRESSURE, ALL GEARS CAME DOWN AND LOCKED. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND NOSE GEAR EXTENSION HYDRAULIC HOSE DAMAGED AND LEAKING. REPLACED HOSE AND PERFORMED OPS CHECK AND LEAK CHECK PER MM CH 29-00-3E. 2 H 7 4 4T A1SO 1996100300090 19961003 00090 NM 1996 10 3 SRAA960902 1 19960905 A 2613 TEMP IND BOEING 747 747246F NM NR 1 NACELLE MALFUNCTIONED A SRAA K NONE N FALSE WARNING CL CLIMB 1 GL 23 741SJ 22063 ON CLIMBOUT, NR 1 NACELLE TEMPERATURE CLIMBED TO 4 UNITS ON BOTH A AND B LOOPS THEN DROPPED BACK TO NORMAL AT CRUISE ALT ITUDE. INSPECTED ENGINE COWLING, PYLON AND ENGINE DUCTING, NO DISCREPANCY NOTED. PERFORMED ENGINE RUN TO TAKEOFF POWER , FOUND NACELLE TEMP NORMAL. 2 L 7 4 4F A20WE 1996100300091 19961003 00091 WP 1996 10 3 SRAA960903 1 19960908 A 2612 FIRE LOOP DOUG DC8 DC873F 302199F WP NR 1 ENGINE SHORTED A SRAA A J UNSCHED LANDING DUMP FUEL N FALSE WARNING CR CRUISE 1 GL 23 875SJ 46063 DURING FLIGHT SJ203 FROM MIA TO BOG NO. 1 ENGINE FIRE WARNING SHORT CIRCUIT LIGHT CAME ON, DUMPED FUEL AND ACCOMPLISHED AIR TURN BACK TO MIA , LANDED WITHOUT INCIDENT. REPAIRED SHORTED FIRE LOOP WIRING JUMPER AT LOWER ELEMENT, SYSTEM OPS C HECKED GOOD PER M.M. CH 26-10-00. 2 L 7 4 4F RT 4A25 1996100300092 19961003 00092 GL 1996 10 3 SRAA960904 2 19960907 A 7200 ENGINE LKHEED 382 382E 526413U SO ALLSN 501D 501D22A 03006 GL NR 3 ENGINE MALFUNCTIONED A SRAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 23 923SJ 4301 ON TAKEOFF ROLL, NR 3 ENGINE WAS FOUND SLOW TO RESPOND TO THROTTLE MOVEMENT, AT APPROXIMATELY 40 KTS TAKEOFF WAS REJECTE D, NO EXCESSIVE BRAKING FORCE USED. PERFORMED ENGINE RUNUP AND FOUND NR 3 ENGINE OPERATED NORMALLY. 2 H 7 4 4T 4 T A1SO E282 1996100300093 19961003 00093 SO 1996 10 3 SRAA960905 1 19960903 A 2613 OVERHEAT WARNING LKHEED 382 382E 526413U SO NR 2 ENGINE ACTIVATED A SRAA O OTHER N FALSE WARNING IN INSP/MAINT 1 GL 23 923SJ 4301 WHILE PULLING OFF OF RUNWAY, NR 2 ENGINE NACELLE OVERHEAT WARNING LIGHT CAME ON. SHUTDOWN NR 2 ENGINE WHILE TAXING. 2 H 7 4 4T A1SO 1996100300094 19961003 00094 SO 1996 10 3 SRAA960907 1 19960911 A 3610 DUCT SEAL LKHEED 382 382G 526414U SO NR 2 ENGINE FAILED A SRAA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 23 918SJ 4208 DURING FLIGHT, NR 2 NACELLE OVERHEAT LIGHT CAME ON APPROXIMATELY FIVE MINUTES AFTER LEVELED OFF. SHUTDOWN ENGINE AND AC COMPLISHED AIR TURNBACK TO CHS, AIRCRAFT LANDED WITHOUT INCIDENT. FOUND F-DUCT SEAL DETERIORATED. RESEALED F-DUCT PER MM CH 72 AND ACCOMPLISHED ENGINE RUN, SYSTEM OPS CHECKED GOOD, NO LEAK NOTED. 2 H 7 4 4T A1SO 1996100300095 19961003 00095 SO 1996 10 3 SRAA960913 1 19960924 A 3213 STRUT SHOE LKHEED 382 382G 526414U SO RT MLG DEFECTIVE A SRAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 921SJ 4586 AFTER TAKEOFF, RIGHT MAIN LANDING GEAR UNSAFE LIGHT CAME ON, CYCLED GEAR AND VERIFIED IN DOWN AND LOCKED POSITION. AIRC RAFT LANDED WITHOUT INCIDENT. INSPECTED RIGHT MAIN LANDING GEAR, FOUND RT AFT STRUT SHOE FACINGS DEFECTIVE AND RT FORWA RD STRUT BALL SCREW HAD METAL CHIPS ON BALL NUT. REPLACED AFT MLG SHOES AND FORWARD BALL SCREW ON RHS, PERFORMED GEAR R ETRACTION SYSTEM, OPS CHECKED GOOD. 2 H 7 4 4T A1SO 1996100300096 19961003 00096 SO 1996 10 3 C2XA96IA228 1 19960912 A 5400 12030995001 ANGLE EMB 120 EMB120RT SO RT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17728 120182 IAH - INSPECTION 1C, 2C, 4C. TOTAL TIME: 12,085.2 HOURS. TOTAL CYCLES: 17,466. DURING A ROUTINE INSPECTION, THE RT NACELLE WAS FOUND TO HAVE A CRACKED SUPPORT ANGLE AT FRAME NR 2. MAINTENANCE REMOVED AND REPLACED SUPPORT ANGLE AT NACE LLE FRAME NR 2. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1996100300097 19961003 00097 WP 1996 10 3 WTAA960169 2 19960825 A 7321 8070432 FUEL CNTRL UNIT BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE331* 01514 WP RT ENGINE MALFUNCTIONED A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 17 422UE 782 SEA - RIGHT ENGINE FAILED TO DEVELOP REQUIRED TAKEOFF POWER. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE ACCOMPLISHE D ENGINE GROUND RUN. FOUND ENGINE PRODUCING ADEQUATE POWER FOR REDUCED POWER TAKEOFF. AIRCRAFT FERRIED TO EUG FOR REPA IRS USING REDUCED POWER TAKEOFF PROCEDURES. MAINTENANCE REPLACED RT ENGINE FUEL CONTROL UNIT. NO DISCREPANCIES NOTED O N GROUND RUN. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T 3 T RT A21EU E2WE 1996100300098 19961003 00098 EU 1996 10 3 WTAA960170 1 19960826 A 2912 QA03043 FILTER BAG JETSTM JETSTM3101 1500215 EU HYD SYSTEM FAILED A WTAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 WP 17 425UE 798 PDX - DURING AIRCRAFT TAXI, NOSE LANDING GEAR RED UNSAFE INDICATION ILLUMINATED. AIRCRAFT FERRIED TO EUG FOR REPAIRS. M AINTENANCE INSPECTED SYSTEM. REPLACED HYDRAULIC RETURN FILTER. GEAR POSITION INDICATION NORMAL FOLLOWING GEAR RETRACTI ON CHECK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A21EU 1996100300099 19961003 00099 WP 1996 10 3 WTAA960171 2 19960827 A 7321 8070429 FUEL CNTRL UNIT BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE331* 01514 WP RT ENGINE OUT OF ADJUST A WTAA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 17 422UE 782 SEA - RIGHT ENGINE FAILED TO DEVELOP REQUIRED TAKEOFF POWER. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE ADJUSTED EN GINE RIGGING. CHECKS GOOD ON ENGINE GROUND RUN. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T 3 T RT A21EU E2WE 1996100300100 19961003 00100 EU 1996 10 3 PLGA9608301 1 19960830 A 2611 7211121100 DETECTOR SAAB SF340 340B 7860101 EU CARGO BAY FAULTY A PLGA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NE 05 362BE 135 A3714 340B291 BDL - FLT 4688 - EN ROUTE TO JFK FROM BOS, THE CARGO SMOKE WARNING LIGHT ILLUMINATED. THE CARGO COMPARTMENT FIRE EXTING UISHER WAS DISCHARGED AND THE AIRCRAFT DIVERTED TO BDL, LANDING WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIR CRAFT AND FOUND NO EVIDENCE OF SMOKE OR FIRE. THE AIRCRAFT WAS THEN FERRIED TO PSM. PSM MAINTENANCE REMOVED AND REPLAC ED THE CARGO FIRE BOTTLE AND THE SMOKE DETECTOR RETURNING THE AIRCRAFT TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1996100300101 19961003 00101 EU 1996 10 3 PLGA9609081 1 19960908 A 3234 D49410001 HANDLE SAAB SF340 SF340A 7850100 EU MLG MALFUNCTIONED A PLGA O OTHER P NO WARNING INDICATION AP APPROACH 1 NE 05 341BE 6064 340A063 BOS - FLT 4916 - ON APPROACH, THE NOSE GEAR DOWN AND LOCK LIGHT FAILED TO ILLUMINATE UNTIL THE THIRD ATTEMPT. ON THE TH IRD ATTEMPT, THE GEAR LIGHT ILLUMINATED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. BOS MAINTENANCE DEFERRED THE GEAR IAW MEL 32-33-1. THE AIRCRAFT RETURNED TO MAINTENANCE WHERE GEAR SWINGS CHECKED GOOD. AS A PRECAUTION, MAINTENANCE REPLAC ED THE GEAR HANDLE AND RETURNED THE AIRCRAFT TO SERVICE. PART TOTAL CYCLES, 6,646. (X) 2 L 7 2 4T RT A52EU 1996100300102 19961003 00102 NM 1996 10 3 W6PA960134 1 19960905 A 3350 LIGHT BOEING 737 7373B7 1384580 NM CABIN INOPERATIVE A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 509AU 23384 22C FLOOR TRACK LIGHTING INOPERATIVE. ONE LIGHT. CORRECTIVE ACTION: REPLACED TRACK LIGHTING SOCKET AT ROW 22. (X) 2 L 7 2 4F RT A16WE 1996100300103 19961003 00103 NM 1996 10 3 W8PA960136 1 19960913 A 2612 FIRE LOOP BOEING 737 7373L9 1384470 NM RIGHT ENGINE MALFUNCTIONED A W8PA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 03 960WP 23331 NR 2 ENGINE FIRE LOOP CAME ON IN-FLIGHT. AIRCRAFT RETURNED TO COS. CORRECTIVE ACTION: PLACED NR 2 ENGINE B-LOOP ON ME L. A-LOOP OKAY. (X) 2 L 7 2 4F RT A16WE 1996100300104 19961003 00104 NM 1996 10 3 W8PA960139 1 19960924 A 3350 LENSE BOEING 737 7373L9 1384470 NM CABIN LOOSE A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 960WP 23331 EMERGENCY EXIT LIGHT LENSE ABOVE COCKPIT DOOR COMING OFF. RESECURED EMERGENCY EXIT LIGHT LENSE ABOVE COCKPIT DOOR. 2 L 7 2 4F RT A16WE 1996100300105 19961003 00105 NM 1996 10 3 W8PA960140 1 19960923 A 2131 7638102 CONTROLLER BOEING 737 7373L9 1384470 NM EE BAY FAILED A W8PA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 NM 03 960WP DA3385 23331 LOST CABIN PRESSURIZATION WITH AUTO FAIL LIGHT ILLUMINATION AND ALTITUDE WARNING HORN. BOTH STANDBY AND MANUAL OKAY. P ERFORMED EMERGENCY DESCENT. REMOVED AND REPLACED PRESSURE CONTROLLER. (X) 2 L 7 2 4F RT A16WE 1996100300106 19961003 00106 NM 1996 10 3 AWXA960408 1 19960726 A 3350 CONNECTOR BOEING 737 737277 1384570 NM CABIN MISSING A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 181AW 22648 PAE - FLT 7848 - DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 6 LT PROX WIRING CONNECTOR MISSING. REPLACED PER STANDARD WIRE MANUAL. (X) 2 L 7 2 4F RT A16WE 1996100300107 19961003 00107 NM 1996 10 3 AWXA960417 1 19960722 A 3397 WIRE BOEING 737 7373G7 1384595 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 155AW 23777 PHX - FLT 0102 - DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT 14C EXIT LIGHT INOPERATIVE. REPARIED BROKEN WIRE. OPERAT IONS CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1996100300108 19961003 00108 NM 1996 10 3 AWXA960418 1 19960712 A 3350 849029 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 907AW 22691 PHX - FLT 2611 - DURING ROUTINE MAINTENANCE CHECK, FOUND R-4 DOOR OVERHEAD EMERGENCY LIGHT INOPERATIVE. CHARGED BATTERY . OPERATES GOOD. (X) 2 L 7 2 4F RT A2NM 1996100300109 19961003 00109 NM 1996 10 3 AWXA960421 1 19960712 A 3350 831862 BATTERY PACK BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 185AW 00048 22652 PHX - FLT 2456 - DURING ORUTINE MAINTENANCE CHECK, FOUND OUTSIDE EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACE D EMERGENCY EXIT BATTERY PACK IN FORWARD BAG PIT, LT WALL. OPERATONS CHECK GOOD. 2 L 7 2 4F RT A16WE 1996100300110 19961003 00110 EU 1996 10 3 AWXA960432 1 19960719 A 3350 321430 BATTERY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 633AW 3181 082 PHX - FLT 2266 DURING ROUTINE MAINTENANCE CHECK, FOUND APPROXIMATELY EVERY 3RD FLOOR PROX SEAT LIGHT INOPERATIVE. ALSO , LT OVERWING EXIT LIGHT INOPERATIVE. BITE FAULTS LT BATTERIES. REMOVED AND REPLACED LT MID-BATTERY. OPERATIONS CHECK AND BITE TESTED GOOD. (X) 2 L 7 2 4F RT A28NM 1996100300111 19961003 00111 NM 1996 10 3 AWXA960433 1 19960701 A 3350 900835A BATTERY BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST CR CRUISE 1 WP 28 189AW 27775 22656 CMH - FLT 2939 - EMERGENCY ROW EXIT LIGHTS FIRST 5 ROWS CAME ON AFTER TAKEOFF. POSITION EMERGENCY EXIT LIGHT SWITCH OFF LIGHTS REMAIN ON. FOUND A BROKEN WIRE. REPAIRED SAME. REMOVED AND REPLACED BATTERY. OPERATIONS CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1996100300112 19961003 00112 NM 1996 10 3 AWXA960434 1 19960728 A 3397 WIRE BOEING 737 7373G7 1384595 NM CABIN DISCONNECTED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 155AW 23777 PHX - FLT 0589 - DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT 1 A, B, EMERGENCY LIGHTS INOPERATIVE. RECONNECTED SPLICE. OPERATIONS OK. (X) 2 L 7 2 4F RT A16WE 1996100300113 19961003 00113 NM 1996 10 3 AWXA960438 1 19960731 A 3350 CONNECTOR BOEING 757 7572G7 1384963 NM CABIN DISCONNECTED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 910AW 24523 PHX - FLT 2616 - DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT MOUNTED EMERGENCY EXIT LIGHTING AT ROW 15 INOPERATIVE. RE CONNECTED SEAT HARNESS AT ROW 15. OPERATIONS CHECK GOOD. (X) 2 L 7 2 4F RT A2NM 1996100300114 19961003 00114 EU 1996 10 3 AWXA960443 1 19960706 A 3350 321454 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 633AW 723 082 PHX - FLT 1236 - DURING ROUTINE MAINTENANCE CHECK, FOUND LT MID-CABIN EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND RE PLACED LT MID-CABIN EMERGENCY LIGHT POWER SUPPLY UNITS. OPERATIONS CHECK GOOD. (X) 2 L 7 2 4F RT A28NM 1996100300115 19961003 00115 1996 10 3 AWXA960464 4 19960831 A 2565 D30665103 SLIDE AIRBUS 320 A320231 3930325 EU R-2 DOOR MALFUNCTIONED A AWXA K NONE O OTHER TX TAXI/GRND HDL 1 WP 28 624AW 14789 4984 A5052 55 LAX/PHX - FLT 2274 - R-2 DOOR SLIDE INADVERTENTLY DEPLOYED, BUT DID NOT INFLATE IN LAX. INSTALLED R-2 DOOR SLIDE PER C ARD R1C25304. PART TOTAL CYCLES, 7,527. (X) 2 L 7 2 4F RT A28NM 1996100300116 19961003 00116 EU 1996 10 3 AWXA960480 1 19960723 A 3350 CONNECTOR AIRBUS 320 A320231 3930325 EU CABIN DISCONNECTED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 634AW 091 PHX - FLT 2249 - DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 26 EMERGENCY LIGHT INOPERATIVE. REPINNED SIDE WALL CONNECT OR. OPS CHECK GOOD. (X) 2 L 7 2 4F RT A28NM 1996100300117 19961003 00117 EU 1996 10 3 AWXA960481 1 19960706 A 3350 321430 BATTERY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 632AW 3899 81 PHX - FLT 2640 - DURING ROUTINE MAINTENANCE CHECK, FOUND RT OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY. REMOVED AND REPLACED POWER SUPPLY. BITE TEST GOOD. REFERENCE: OPERATOR CONTROL NR 96ZZZX49 19. (X) 2 L 7 2 4F RT A28NM 1996100300118 19961003 00118 EU 1996 10 3 96ZZZX4919 1 19960706 A 3350 321454 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 632AW 378 81 PHX - FLT 2640 - DURING ROUTINE MAINTENANCE CHECK, FOUND RT OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY. REMOVED AND REPLACED POWER SUPPLY. BITE TEST GOOD. REFERENCE: OPERATOR CONTROL NR AWXA9604 81. 2 L 7 2 4F RT A28NM 1996100300119 19961003 00119 NM 1996 10 3 AWXA960482 1 19960707 A 3350 20131A BATTERY PACK BOEING 757 75723A 1384967 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 916AW 16429 24291 PHX - FLT 2020 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS IN OVERHEAD BIN, LT, ROWS 16 AND 22, INOP ERATIVE. LT EXIT SIGN NEAR MID-AFT LAVATORY INOPERATIVE. REPLACED BATTERY PACK AT ROW 25 RT. LIGHTS OPERATE OK. (X) 2 L 7 2 4F RT A2NM 1996100300120 19961003 00120 EU 1996 10 3 AWXA960483 1 19960721 A 3350 321430 BATTERY AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 641AW 4410 453 PHX - FLT 2082 - DURING ROUTINE MAINTENANCE CHECK, FOUND OVERWING INTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND RE PLACED BATTERY AT RIGHT MID. OPERATIONS CHECK GOOD. (X) 2 L 7 2 4F RT A28NM 1996100300121 19961003 00121 NM 1996 10 3 AWXA960484 1 19960727 A 3350 CONNECTION BOEING 737 737277 1384570 NM CABIN LOOSE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 179AW 22646 PHX - FLT 2267 - DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT 18 A, B, C, WITH EMERGENCY LIGHTS INOPERATIVE. FOUND CONN ECTION SEPARATED AND RECONNECTED. LIGHTS OPS CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1996100300122 19961003 00122 NM 1996 10 3 AWXA960485 1 19960720 A 3350 CONNECTOR BOEING 737 7373G7 1384595 NM CABIN DISCONNECTED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 157AW 23779 PHX - FLT 2170 - DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT MOUNTED EMERGENCY EXIT LIGHTS OUT AT ROWS 19 - 23. RESET BATTERY PACK CONNECTOR AND SYSTEM OPERATES NORMALLY. (X) 2 L 7 2 4F RT A16WE 1996100300123 19961003 00123 EU 1996 10 3 AWXA960486 1 19960723 A 3350 321430 BATTERY AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 641AW 1892 453 LAS - FLT 0146 - DURING ROUTINE MAINTENANCE CHECK, FOUND LT OVERWING EMERGENCY EXIT BATTERY PACK INOPERATIVE. REMOVED A ND REPLACED LT OVERWING BATTERY PACK. OPS CHECK GOOD. (X) 2 L 7 2 4F RT A28NM 1996100300124 19961003 00124 NM 1996 10 3 AWXA960487 1 19960724 A 3350 831136 LIGHT BOEING 737 73733A 1384673 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 173AW 23632 PHX - FLT 7925 - DURING ROUTINE MAINTENANCE CHECK, FOUND ONE EMERGENCY EXIT LIGHT INOPERATIVE, ROW 11 LEFT SEAT MOUNTED. REPLACED LIGHT ASSEMBLY. OPERATIONS CHECK OK. (X) 2 L 7 2 4F RT A16WE 1996100300125 19961003 00125 EU 1996 10 3 AWXA960488 1 19960725 A 3350 321430 BATTERY PACK AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 624AW 10482 55 LAS - FLT 2609 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE, OVERWING. REPLACED BATTERY PACK OVERWING, LEFT SIDE. TEST OK. (X) 2 L 7 2 4F RT A28NM 1996100300126 19961003 00126 NM 1996 10 3 AWXA960489 1 19960725 A 3350 864705 POWER UNIT BOEING 737 737112 1384412 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 708AW 19771 LAS - FLT 2944 - DURING ROUTINE MAINTENANCE CHECK, FOUND DOOR MOUNTED EMERGENCY LIGHT AT 2-R DIM. REMOVED AND REPLACED POWER UNIT. OPERATIONS CHECK GOOD. (X) 2 L 7 2 4F A16WE 1996100300127 19961003 00127 EU 1996 10 3 AXWA960490 1 19960715 A 3397 WIRE AIRBUS 320 A320231 3930325 EU CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 621AW 053 LAS - FLT 2687 - DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 26 SEAT MOUNT EMERGENCY LIGHT INOPERATIVE, BOTH BULBS. REP AIRED WIRING FOR EMERGENCY LIGHT AT ROW 26. LIGHTS OPERATIONS CHECKS GOOD. (X) 2 L 7 2 4F RT A28NM 1996100300128 19961003 00128 NM 1996 10 3 AWXA960491 1 19960716 A 3350 PIN BOEING 737 73733A 1384673 NM CABIN UNSEATED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 169AW 23630 PHX - FLT 2475 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT 3-L INOPERATIVE. RESEATED PIN IN CONNECTOR UND ER SEAT 3A. OPERATONS CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1996100300129 19961003 00129 EU 1996 10 3 AWXA960492 1 19960730 A 3350 CONNECTOR AIRBUS 320 A320231 3930325 EU CABIN DISCONNECTED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 635AW 092 LAS - FLT 2990 - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PROX LIGHTING INOPERATIVE AT 9R. RECONNECTED CANNON PLUG AT SIDE WALL. (X) 2 L 7 2 4F RT A28NM 1996100300130 19961003 00130 NM 1996 10 3 AWXA960493 1 19960707 A 3350 FUSE BOEING 757 7572S7 1384962 NM CABIN BLOWN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 901AW 23321 PHX - FLT 0001 - DURING ROUTINE MAINTENANCE CHECK, FOUND AFT ROW EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE IN AFT BAT TERY PACK ASSEMBLY. OPERATIONS CHECK GOOD AT THIS TIME. (X) 2 L 7 2 4F RT A2NM 1996100300131 19961003 00131 NM 1996 10 3 AWXA960494 1 19960701 A 3350 831862 BATTERY BOEING 737 7372A6 138448B NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 145AW 20194 PHX - FLT 2573 - DURING ROUTINE MAINTENANCE CHECK, FOUND L-2 DOOR EMERGENCY EXIT LIGHT DIM. REMOVED AND REPLACED BATTER Y ASSEMBLY. OPERATIONS CHECK GOOD. (X) 2 L 7 2 4F A16WE 1996100300132 19961003 00132 NM 1996 10 3 AWXA960495 1 19960721 A 3397 WIRE BOEING 737 737277 1384570 NM CABIN DISCONNECTED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 181AW 22648 PHX - FLT 2081 - DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT 3C FLOOR PROX LIGHT OUT. RESECURED WIRE CONNECTOR. OPERA TIONS CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1996100300133 19961003 00133 EU 1996 10 3 AWXA960496 1 19960722 A 3350 321452 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 624AW 55 DTW - FLT 0058 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTING ROW 9 AND ROW 11 A/C LEFT, INOPERATIVE. SWAPPED EMERGENCY LIGHT OVER-WING EXIT DOOR POWER SUPPLIES PER 33-51-38. REMOVED POWER FROM A/C. POWER UP A/C EMERGE NCY LIGHT SYSTEM, OPERATIONS CHECK GOOD. LEFT S/N - 433. RIGHT S/N - 1551. (X) 2 L 7 2 4F RT A28NM 1996100300134 19961003 00134 NM 1996 10 3 AWXA960497 1 19960727 A 3397 WIRE BOEING 737 7373Y0 1384671 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 323AW 23684 PHX - FLT 2517 - DURING ROUTINE MAINTENANCE CHECK, FOUND NUMEROUS WIRES EXPOSED AT ROW 22, A, B, C. SOME BROKEN. REPAI RED EMERGENCY EXIT FLOOR TRACK WIRING. SYSTEM CHECKS GOOD. (X) 2 L 7 2 4F RT A16WE 1996100300135 19961003 00135 NM 1996 10 3 AWXA960499 1 19960716 A 3350 831862 BATTERY PACK BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 188AW 0124 22655 PHX - FLT 2636 - DURING ROUTINE MAINTENANCE CHECK, FOUND L2 AND R2 EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED EMER GENCY LIGHTS BATTERY PACK. SYSTEM OPERATIONS CHECK NORMAL. (X) 2 L 7 2 4F RT A16WE 1996100300136 19961003 00136 NM 1996 10 3 AWXA960500 1 19960716 A 3350 849029 BATTERY BOEING 737 7373G7 1384595 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 157AW 23779 PHX - FLT 0092 - DURING ROUTINE MAINTENANCE CHECK, FOUND RT OVERWING EMERGENCY LIGHT INOPERATIVE. RECHARGED BATTERY. O PERATIONS CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1996100300137 19961003 00137 NM 1996 10 3 AWXA960501 1 19960722 A 3350 831136 LIGHT BOEING 737 73733A 1384673 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 167AW 23628 PHX - FLT 2220 - DURING ROUTINE MAINTENANCE CHECK, FOUND R1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. INSTALLED NEW SO CKET. (X) 2 L 7 2 4F RT A16WE 1996100300138 19961003 00138 NM 1996 10 3 AWXA960502 1 19960725 A 3350 831862 BATTERY PACK BOEING 737 737277 1384570 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 188AW 244 22655 PHX - FLT 2257 - DURING ROUTINE MAINTENANCE CHECK, FOUND L2 AND R2 EMERGENCY LIGHTS (EXTERIOR) INOPERATIVE. REMOVED AND REPLACED BATTERY PACK PER MM 33-51-71. OPERATIONS CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1996100300139 19961003 00139 NM 1996 10 3 AWXA960503 1 19960727 A 3350 831136 REFLECTOR BOEING 737 7373G7 1384595 NM CABIN DAMAGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 303AW 24010 PHX - FLT 2498 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT AFT OF L-2 DOOR DOES NOT LIGHT UP. REMOVE D AND REPLACED REFLECTOR. OPERATIONS CHECK NORMAL. (X) 2 L 7 2 4F RT A16WE 1996100300140 19961003 00140 NM 1996 10 3 AWXA960504 1 19960910 A 3350 110049 BATTERY CHARGER BOEING 737 73733A 1384673 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 165AW 9943 23626 PHX - FLT 0543 - DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT ROWS 1-5, CHAIR LIGHTS INOPERATIVE. ALSO, FOUND AFT BATTE RY CHARGER EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY CHARGER ASSEMBLY. REMOVED AND REPLACED AFT BATTE RY CHARGER ASSEMBLY. REFERENCE: OPERATOR CONTROL NR: 96ZZZX4920. (X) 2 L 7 2 4F RT A16WE 1996100300141 19961003 00141 NM 1996 10 3 96ZZZX4920 1 19960910 A 3350 110049 BATTERY CHARGER BOEING 737 73733A 1384673 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 165AW 9951 23626 PHX - FLT 0543 - DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT ROWS 1-5, CHAIR LIGHTS INOPERATIVE. ALSO, FOUND AFT BATTE RY CHARGER EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY CHARGER ASSEMBLY. REMOVED AND REPLACED AFT BATTE RY CHARGER ASSEMBLY. REFERENCE: OPERATOR CONTROL NR: AWXA960504. 2 L 7 2 4F RT A16WE 1996100300142 19961003 00142 NM 1996 10 3 AWXA960505 1 19960909 A 5753 654648181 CARRIAGE ASSY BOEING 737 737277 1384570 NM TE FLAPS BROKEN A AWXA O OTHER F FLT CONT AFFECTED DE DESCENT 1 WP 28 186AW 294 22653 PHX - FLT 2452 - CREW REPORTED AIRCRAFT ROLLS LEFT. CHECKED FLAPS/SPOILERS PER MM 27-09-400, PG 106. PERFORMED HILT TES T PER TASK CARD F8M29003. NO DEFECTS FOUND. INSPECTED SPOILERS AND SPOILER ACTUATOR. NO SPOILER ANOMALIES NOTED DURIN G ENTIRE FLIGHT. DURING INSPECTION, INBD SIDE OF OTBD FLAP ASSY JUMPED FWD APPROX 1 INCH OR MORE AS IF BINDING. FOUND MAJOR SLOP IN ENTIRE OTBD LT SIDE OTBD FLAP ASSY AT INBD END. FOUND LT OTBD FLAP INBD SIDE FLAP CARRIAGE SPINDLE BROKEN UNDER CRES SLEEVE. REMOVED AND REPLACED SPINDLE ASSY. REMOVED AND REPLACED FLAP FOR COMPANY CONVENIENCE. (X) 2 L 7 2 4F RT A16WE 1996100300143 19961003 00143 NM 1996 10 3 AWXA960506 1 19960701 A 3350 964080 BATTERY BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 187AW 23559 22654 PHX - FLT 0099 - DURING ROUTINE MAINTENANCE CHECK, FOUND L-2 AND R-2 EXTERNAL EMERGENCY EXIT LIGHTS WILL NOT ILLUMINATE. REMOVED AND REPLACED BATTERY. OPERATIONS CHECK GOOD PER CARD A/C 33009. (X) 2 L 7 2 4F RT A16WE 1996100300144 19961003 00144 NM 1996 10 3 AWXA960507 1 19960705 A 3350 900542 BATTERY PACK BOEING 737 737277 1384570 NM CABIN UNSEATED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 187AW 22654 PHX - FLT 2245 - DURING ROUTINE MAINTENANCE CHECK, FOUND BOTH EMERGENCY LIGHTS OVER THE OVERWING EXIT DOORS (LT AND RT D OORS) INOPERATIVE. RESEATED BATTERY PACK. OPERATIONS CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1996100300145 19961003 00145 NM 1996 10 3 AWXA950509 1 19960911 A 3397 WIRE BOEING 757 7572S7 1384962 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 906AW 23568 PHX - FLT 2616 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS AFT OF LAVATORIES INOPERATIVE. REPAIRED BROKEN WIRES AS REQUIRED. OPERATES NORMALLY. (X) 2 L 7 2 4F RT A2NM 1996100300146 19961003 00146 NM 1996 10 3 AWXA960510 1 19960704 A 3350 900542 BATTERY PACK BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 185AW 21498 22652 PHX - FLT 2081 - DURING ROUTINE MAINTENANCE CHECK, FOUND LT AND RT OVERWING EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED OVERWING EXIT SIGN BATTERY PACK. OPERATIONS CHECK OK. (X) 2 L 7 2 4F RT A16WE 1996100300147 19961003 00147 NM 1996 10 3 ASAA9640075 1 19960910 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 762AS 25099 SEA - FLT 110 - DURING CREW PRE-FLIGHT, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE NEAR THE AFT GALLEY AREA. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1996100300148 19961003 00148 NM 1996 10 3 ASAA9640076 1 19960910 A 3350 1060091101 LIGHT BOEING 737 7374Q8 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 765AS 25102 SEA - DURING MAINTENANCE CHECK, THE R-2 ESCAPE SLIDE EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPAIRED CONTACT AND L IGHT OPERATED NORMALLY. 2 L 7 2 4F RT A16WE 1996100300149 19961003 00149 WP 1996 10 3 ASAA9680182 1 19960828 A 3350 2550325 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 933AS 49234 SEA - DURING MAINTENANCE CHECK, THE L-1 DOOR PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED BATTERIES IN LIGH T ASSY AND LIGHT OPERATED NORMALLY. (X) 2 L 7 2 4F A6WE 1996100300150 19961003 00150 WP 1996 10 3 ASAA9680183 1 19960830 A 3350 S103 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 953AS 49386 SEA - DURING MAINTENANCE CHECK, THE INTERIOR EMERGENCY EXIT LIGHT BATTERY PACK AT ROW 21 WAS FOUND DISCHARGED. REPLACED BATTERIES AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F A6WE 1996100300151 19961003 00151 EU 1996 10 3 VTZA96344 1 19960904 A 3234 877701 GEAR HANDLE JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT FAILED A VTZA K NONE J WARNING INDICATION CL CLIMB 1 EA 27 316UE 41055 BOS/EWR - FLT 7567 - DURING CLIMB AT 1800 HRS ON 9-4-96, CONTINUED TO EWR WITH ONE DISCREPANCY WHICH WAS GEAR WOULD NOT RETRACT, RED GEAR HANDLE ILLUMINATED WITH ALL GEAR DOWN AND LOCKED INDICATIONS. AIRCRAFT WAS FLOWN WITH GEAR DOWN TO EW R AND THEN FERRY FLIGHT TO IAD. MAINTENANCE REMOVED AND REPLACED GEAR HANDLE, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1996100300152 19961003 00152 EU 1996 10 3 VTZA96345 1 19960904 A 7712 31024762 TQ SIGNAL COND BAG JETSTM JETSTM3201 1500217 EU NR 2 ENGINE OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 27 483UE 898 IAD/HVN - FLT 6173 - DURING TAKEOFF AT 1840 HOURS ON 9-4-96, ABORTED TAKEOFF DUE TO NR 2 ENGINE TORQUE ROLLED BACK ON TA KEOFF. AIRCRAFT LANDED AND RETURNED TO GATE AT IAD WITH NO FURTHER INCIDENT. MAINTENANCE ADJUSTED NR 2 TORQUE SIGNAL C ONDITIONER, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1996100300153 19961003 00153 1996 10 3 VTZA96346 4 19960904 A 3425 7003360948 AHRS COMP JETAIR JETSTM JETSTM4101 1500501 EU NR 2 FAILED A VTZA K NONE J WARNING INDICATION CR CRUISE 1 EA 27 320UE 41043 IAD/BOS - FLT 6506 - DURING CRUISE AT 1100 HRS ON 9-4-96, LANDED AT BOS WITH ONE DISCREPANCY WHICH WAS THE NR 2 AHRS FAI LED IN-FLIGHT. MAINTENANCE REMOVED AND REPLACED NR 2 AHRS UNIT. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVI CE. (X) 2 L 7 2 4T RT A41NM 1996100300154 19961003 00154 EU 1996 10 3 VTZA96347 1 19960904 A 5610 14146002403 WINDSHIELD JETAIR JETSTM JETSTM4101 1500501 EU LT COCKPIT CRACKED A VTZA O OTHER O OTHER CR CRUISE 1 EA 27 301UE 41012 IAD/ORF - DURING CRUISE AT 2245 HRS ON 9-4-96, LANDED AT ORF WITH ONE DISCREPANCY WHICH WAS CAPTAIN'S WINDSCREEN CRACKED ON OUTER PANEL. MAINTENANCE REMOVED AND REPLACED WINDSCREEN, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RET URN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1996100300155 19961003 00155 EU 1996 10 3 VTZA96348 1 19960906 A 2611 72111211002 SMOKE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU BAGG COMPT MALFUNCTIONED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 324UE 41017 IAD/TYS - FLT 6353 - DURING CLIMB AT 0815 HRS ON 9-6-96, MADE AN UNSCHEDULED LANDING AND RETURNED TO GATE DUE TO POD SMO KE CAPTION ILLUMINATED ON CLIMB-OUT. MAINTENANCE REMOVED AND RPELACED SMOKE DETECTOR. AIRCRAFT WAS RELEASED AND APPROV ED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1996100300156 19961003 00156 EU 1996 10 3 VTZA96349 1 19960906 A 5270 SWITCH BAG JETSTM JETSTM3201 1500217 EU PASSENGER DOOR LACK OF LUBE A VTZA K NONE N FALSE WARNING AP APPROACH 1 EA 27 492UE 790 ALB/IAD - FLT 6254 - DURING APPROACH AT 0900 HOURS ON 9-6-96, ENCOUNTERED PASSENGER DOOR WARNING CAPTION ILLUMINATION. A IRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE LUBED AND CLEANED DOOR MICROSWITCH, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1996100300157 19961003 00157 EU 1996 10 3 VTZA96351 1 19960903 A 2613 OVERHEAT LIGHT JETAIR JETSTM JETSTM4101 1500501 EU NR 2 PACK ILLUMINATED A VTZA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 327UE 41080 FLT NR 6484 - JFK-BOS - RETURNED TO GATE, DUE TO NR 2 PACK OVERTEMP LIGHT ILLUMINATED WHILE ON GROUND IN AUTO OR MANUAL. MAINTENANCE OPENED DMI 64100, MEL 21-18. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996100300158 19961003 00158 EU 1996 10 3 VTZA96356 1 19960906 A 7712 TTL SYSTEM BAG JETSTM JETSTM3201 1500217 EU COCKPIT MALFUNCTIONED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 27 488UE 907 IAD/PHL - DURING TAKEOFF AT 1340 HOURS ON 9-6-96, ABORTED TAKEOFF DUE TO TTL ROLLED BACK TO 80 PERCENT. AIRCRAFT RETURN ED TO GATE WITH NO FURTHER INCIDENT. MAINTENANCE OPENED DMI 06518, MEL 76-2. MAINTENANCE CLOSED DMI 06518 ON 9-7-96 BY PERFORMING OPS CHECK OF TTL SYSTEM, COULD NOT DUPLICATE. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X ) 2 L 7 2 4T RT A56EU 1996100300159 19961003 00159 EU 1996 10 3 VTZA96361 1 19960907 A 3240 141R0439 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU EMERGENCY BRAKE OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 325UE 41063 IAD/EWR - FLT 6276 - DURING TAKEOFF AT 1945 HRS ON 9-7-96, ABORTED TAKEOFF DUE TO TAKEOFF CONFIGURATION WARNING. AIRCRA FT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED EMERGENCY BRAKE MICROSWITCH, OPS CHECK OK. AIRCRAF T WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1996100300160 19961003 00160 NE 1996 10 3 VTZA96362 2 19960906 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE LEFT FLAME OUT A VTZA E ENGINE SHUTDOWN X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 EA 27 317UE 41031 75095 LGA/IAD - FLT 6532 - DURING TAXI AT 1215 HRS ON 9-6-96, RETURNED TO GATE DUE TO LT ENGINE FLAMED OUT AFTER LANDING GOING TO GATE. MAINTENANCE GROUND RAN AIRCRAFT AND NOTED NO DEFECTS AND COULD NOT DUPLICATE, OPS CHECK OK. AIRCRAFT WAS REL EASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T 4 T RT A41NM E18NE 1996100300161 19961003 00161 EU 1996 10 3 VTZA96363 1 19960908 A 5270 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU PASSENGER DOOR OUT OF ADJUST A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 316UE 41055 ORF/IAD - FLT 6517 - DURING TAKEOFF AT 0650 HRS ON 9-8-96, MADE AN UNSCHEDULED LANDING DUE TO PASSENGER DOOR WARNING LIG HT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI 17409 MEL 52-2. MAINTENAN CE CLOSED DMI 17409 ON 9-11-96 BY ADJUSTING FORWARD MICROSWITCH, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR R ETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1996100300162 19961003 00162 WP 1996 10 3 VTZA96364 2 19960906 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UAR 01514 WP RIGHT FLAMED OUT A VTZA A UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 EA 27 471UE 821 IAD/ISP - FLT 6168 - DURING CRUISE AT 1415 HOURS ON 9-6-96, MADE AN UNSCHEDULED LANDING DUE TO RT ENGINE FLAME OUT IN-FL IGHT. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENT. (X) 2 L 7 2 4T 4 T RT A56EU E4WE 1996100300163 19961003 00163 EU 1996 10 3 VTZA96365 1 19960908 A 3260 93M1C11HB2BB2 SWITCH BAG JETSTM JETSTM3201 1500217 EU MLG DIRTY A VTZA O OTHER N FALSE WARNING DE DESCENT 1 EA 27 492UE 790 ELM/IAD - FLT 6275 - DURING DESCENT AT 2015 HOURS ON 9-8-96, ENCOUNTERED GEAR WARNING HORN DURING DESCENT WITH GEAR DOWN AND FLAPS AT 20 PERCENT. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE CLEANED AND INSPECTED UPLOCK MIC ROSWITCH, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1996100300164 19961003 00164 EU 1996 10 3 VTZA96366 1 19960909 A 7160 147102331 INTAKE DUCT JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE MISSING A VTZA K NONE D INFLIGHT SEPARATION CR CRUISE 1 EA 27 302UE 41013 IAD/BOS - FLT 6418 - DURING CRUISE AT 1345 HRS ON 9-9-96, LANDED AT BOS WITH ONE DISCREPANCY WHICH WAS LT ENGINE OUTBOAR D NACA DUCT MISSING IN-FLIGHT. MAINTENANCE REPLACED DUCT, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1996100300165 19961003 00165 NM 1996 10 3 96ZZZX4921 1 19960724 A 5753 65267665 CARRIAGE BOEING 727 727222 1384073 NM TE FORE FLAP BROKEN A RYNA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CE 07 7643U 20037 GSP - DURING CLIMB-OUT, THE INBOARD FLAPS WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO GSP AND LANDED WITHOUT INCIDENT. FOUND RIGHT INBOARD FLAP ASSEMBLY OUTBOARD FORE FLAP SEQUENCING CARRIAGE DAMAGED WITH TOGGLE ASSEMBLY MISSING. REPLACE D CARRIAGE ASSEMBLY PER MM 27-52-52. OPS CHECKS GOOD. (X) 2 L 7 3 4F A3WE 1996100300166 19961003 00166 NM 1996 10 3 USAASB96195 1 19960916 A 5270 694280939 SENSOR BOEING 737 7374B7 1384702 NM CARGO DOOR OUT OF ADJUST A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 448US 24892 RDU - FLT 1605 - CAPTAIN NOTICED THE FORWARD CARGO DOOR WARNING LIGHT ILLUMINATED DURING TAKEOFF ROLL. CABIN PRESSURE A PPEARED NORMAL AFTER TAKEOFF ROLL. CAPTAIN ELECTED TO RETURN TO FIELD AT RDU. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE ADJUSTED AND CLEANED THE FORWARD CARGO DOOR SENSOR. OPS CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1996100300167 19961003 00167 EU 1996 10 3 USAA960580 1 19960601 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 4610-5100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 487US 20640 11238 YYC - DURING FC-06 CHECK, FOUND LIGHT SURFACE CORROSION AT BL 600 RT, STA 4610 - STA 5100, SEAT TRACK. REPLACED SEAT TR ACK PER SRM 51-10-00, REPAIRED BY PART REPLACEMENT. (X) 2 L 7 2 4F RT A20EU 1996100300168 19961003 00168 EU 1996 10 3 USAA960581 1 19960602 A 5347 A31921004 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 15400-16495 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 487US 20640 11238 YYC - DURING FC-06 CHECK, FOUND LIGHT SURFACE ATTACK CORROSION AT BL 600 RT STA 15400 - STA 16495 SEAT TRACK. SPLICED S EAT TRACK AT STA 15400 AND STA 16495 (FACTORY SPLICE) PER SRM 53-02-15 CHAIR RAIL REPAIR. (X) 2 L 7 2 4F RT A20EU 1996100300169 19961003 00169 EU 1996 10 3 USAA960582 1 19960602 A 5347 A31911004 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 8955 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 487US 20640 11238 YYC - DURING FC-06 CHECK, FOUND CORROSION, LIGHT SURFACE ATTACK, AT BL 600 RT STA 8955 SEAT TRACK. INSTALLED REPAIR ANG LE PER TOKKER TS96.61491 AND SRM 53-02-15 CHAIR RAIL REPAIR. (X) 2 L 7 2 4F RT A20EU 1996100300170 19961003 00170 EU 1996 10 3 USAA960583 1 19960602 A 5347 A31911003 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 5100-8305 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 487US 20640 11238 YYC - DURING FC-06 CHECK, FOUND GOUGES AND LIGHT SURFACE ATTACK CORROSION AT SEAT TRACK, BL 600 LT, STA 5100 - STA 8305. SEAT TRACK SPLICED AT STA 5100 (FACTORY SPLICE) AND STA 8305. REPAIRED PER SRM 53-02-15, CHAIR RAIL REPAIR. (X) 2 L 7 2 4F RT A20EU 1996100300171 19961003 00171 EU 1996 10 3 USAA960584 1 19960602 A 5347 A31911003 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 10753-11630 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 487US 20640 11238 YYC - DURING FC-06 CHECK, FOUND GOUGES AND LIGHT SURFACE ATTACK CORROSION AT BL 600 LT, STA 10753 - STA 11630 AT SEAT TR ACK. SEAT TRACK SPLICED AT STA 10753 (FACTORY SPLICE) AND STA 11630. REPAIRED PER SRM 53-02-15, CHAIR RAIL REPAIR. (X ) 2 L 7 2 4F RT A20EU 1996100300172 19961003 00172 EU 1996 10 3 USAA960585 1 19960602 A 5347 A31921004 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 12900-13600 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 487US 20640 11238 YYC - DURING FC-06 CHECK, FOUND GOUGES AND LIGHT SURFACE ATTACK CORROSION AT SEAT TRACK BL 1127 LT, STA 12900 - STA 1361 0. SEAT RAIL SPLICED AT 12900 AND 13610, BL 1172 LT PER SRM 53-02-15 CHAIR RAIL REPAIR. (X) 2 L 7 2 4F RT A20EU 1996100300173 19961003 00173 EU 1996 10 3 USAA960586 1 19960510 A 5210 A26052083 CORNER FOKKER F28 F28MK4000 4990810 EU PASSENGER DOOR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 487US 20640 11238 YYC - DURING FC-06 CHECK, FOUND 120 MM BY 80 MM CORRODED AREA MCD FORWARD LOWER CORNER (WITH DOOR CLOSED). REPLACED FOR WARD LOWER CORNER MCD PER SRM 51-31-01 AND SRM 51-31-05. REPLACED WITH IDENTICAL PART NUMBER. (X) 2 L 7 2 4F RT A20EU 1996100300174 19961003 00174 EU 1996 10 3 USAA960587 1 19960512 A 5315 FLOOR BEAM FOKKER F28 F28MK4000 4990810 EU BS 3840 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 487US 20640 11238 YYC - DURING FC-06 CHECK, FOUND 1 INCH BY 2 INCH CORRODED AREA TOP OF FLOOR BEAM AT STA 3840, BL 600R. REMOVED, FABRICA TED NEW SEAT RAIL SECTION AND INSTALLED PER SRM 53-11-05, PAGE 14, FIGURE 4, ITEM 80. (X) 2 L 7 2 4F RT A20EU 1996100300175 19961003 00175 EU 1996 10 3 USAA960588 1 19960513 A 5321 FLOOR PANEL FOKKER F28 F28MK4000 4990810 EU GALLEY CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 487US 20640 11238 YYC - DURING FC-06 CHECK, FOUND SEVERAL SMALL AREAS OF CORROSION ON GALLEY FLOOR PANEL 24AB. CORROSION CLEANED AND TREA TED. FLOOR BOARD REPAINTED PER SRM 51-10-04. (X) 2 L 7 2 4F RT A20EU 1996100300176 19961003 00176 EU 1996 10 3 USAA960589 1 19960512 A 5347 SEAT TRACKS FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 487US 20640 11238 YYC - DURING FC-06 CHECK, FOUND MINOR CORROSION, FRETTING AND GOUGES ON ALL FOUR SEAT TRACKS. BLENDED OUT CORROSION, TR EATED, AND REPAINTED SEAT TRACKS PER SRM 53-01-01. (X) 2 L 7 2 4F RT A20EU 1996100300177 19961003 00177 EU 1996 10 3 USAA960590 1 19960512 A 5315 FLOOR BEAM FOKKER F28 F28MK4000 4990810 EU BS 4900 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 487US 20640 11238 YYC - DURING FC-06 CHECK, FOUND 30 MM BY 20 MM CORRODED AREA AT FLOOR BEAM AT STA 4900 BL ZERO. CONNECTION AND COUPLI NG ANGLES REPAIRED PER SRM IPC-53-15-05, ITEM 90, FIGURE 23, AND FOKKER REPAIR REF NRT J96-61467. (X) 2 L 7 2 4F RT A20EU 1996100300178 19961003 00178 EU 1996 10 3 USAA960591 1 19960601 A 5347 128743003 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 5100-9305 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 487US 20640 11238 YYC - DURING FC-06 CHECK, FOUND MULTIPLE GOUGES AND LIGHT SURFACE CORROSION AT BL 1127 LT, STA 5100 - STA 9305. SEAT TR ACK SPLICED AT STA 9305 PER SRM 53-02-15 CHAIR RAIL REPAIR. (X) 2 L 7 2 4F RT A20EU 1996100300179 19961003 00179 EU 1996 10 3 USAA960592 1 19960510 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 487US 20640 11238 YYC - DURING FC-06 CHECK, FOUND 8 MM LONG CRACK AT SERVICE EMERGENCY DOOR UPPER FORWARD CORNER SKIN. INSTALLED DOUBLERS PER SRM 53-02-16, PAGE 7. (X) 2 L 7 2 4F RT A20EU 1996100300180 19961003 00180 EU 1996 10 3 USAA960593 1 19960602 A 5347 A28747001 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 5100-6250 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 487US 20640 11238 YYC - DURING FC-06 CHECK, FOUND MULTIPLE CORRODED AREAS AT SEAT TRACK BL 1127 RT, STA 5100 - STA 6250. SEAT TRACK SPLIC ED AT STA 6250 PER SRM 53-02-15, CHAIR RAIL REPAIR. (X) 2 L 7 2 4F RT A20EU 1996100300181 19961003 00181 EU 1996 10 3 USAA960594 1 19960602 A 5347 A34070003 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 16495-17845 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 487US 20640 11238 YYC - DURING FC-06 CHECK, FOUND LIGHT SURFACE ATTACK CORROSION AT SEAT TRACK, BL 600 RT, STA 16495 - STA 17845. INSTALL ED NEW SEAT RAIL PER SRM 51-10-00 REPAIR BY PART REPLACEMENT. (X) 2 L 7 2 4F RT A20EU 1996100300182 19961003 00182 EU 1996 10 3 USAA960610 1 19960917 A 5522 SKIN FOKKER F28 F28MK0100 4990807 EU RT ELEVATOR DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 859US 15668 11293 PIT - DURING Q-1 CHECK, FOUND 3 INCH BY 3 INCH DENT/DELAMINATION AT RT ELEVATOR JUST INBOARD OF RIB 1265. REPAIRED AND REPLACED DAMAGED SKIN AND HONEYCOMB CORE AND INSTALLED A DOUBLER PER SRM 51-70-03. (X) 2 L 7 2 4F RT 1996100300183 19961003 00183 EU 1996 10 3 USAA960611 1 19960917 A 5522 SKIN FOKKER F28 F28MK0100 4990807 EU LT ELEVATOR DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 859US 15668 11293 PIT - DURING Q-1 CHECK, FOUND 4 INCH BY 4 INCH DENT/DELAMINATION LT ELEVATOR BETWEEN RIB 215 AND RIB 1265. REPLACED AND REPAIRED DAMAGED SKIN AND HONEYCOMB CORE AND INSTALLED A DOUBLER PER SRM 51-70-03. (X) 2 L 7 2 4F RT 1996100300184 19961003 00184 EU 1996 10 3 USAA960612 1 19960917 A 5311 FRAME FOKKER F28 F28MK0100 4990807 EU BS 11-BS 64 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 859US 15668 11293 PIT - DURING Q-1 CHECK, FOUND 3 INCH CRACKS (2 EACH) AND .075 INCH CRACKS (2 EACH) AT FUSELAGE CENTER WING FRONT SPAR FR AME AND ANGLES AT STA 11 (LHS) AND STA 64 (RHS). ROUTED OUT CRACK AREAS IN FRAME AND INSTALLED NEW ANGLES PER EA NR 334 30 AND EA NR 32077. (X) 2 L 7 2 4F RT 1996100300185 19961003 00185 NM 1996 10 3 CALA9601330 1 19960926 A 3260 106122628 LOCK SENSOR BOEING 737 7373T0 1384582 NM NLG INOPERATIVE A CALA O OTHER N FALSE WARNING CR CRUISE 1 SW 09 14307 23358 THE AIRCRAFT HAD A HISTORY OF THE NLG RED UNSAFE LIGHT COMING ON IN FLIGHT. THE M983 LOGIC CARD HAD BEEN REPLACED PREVI OUSLY, BUT THE PROBLEM WAS REPEATED. MAINTENANCE REMOVED AND REPLACED THE R374 LATCHING RELAY AND THE NOSE GEAR LOCK SE NSOR. SYSTEM FUNCTIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 1996100300186 19961003 00186 WP 1996 10 3 CALA9601331 1 19960926 A 2170 1808492 COALESCER BAG DOUG DC9 DC982 3022082 WP LT/RT PACKS DIRTY A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 09 69803 49229 A STRONG ODOR WAS OBSERVED TEMPORARILY IN THE CABIN DURING TAKEOFF AND CLIMB. THE ODOR DISAPPEARED AFTER SEVERAL MINUTE S. THE FLIGHT WAS CONTINUED WITHOUT FURTHER PROBLEM. MAINTENANCE REMOVED AND REPLACED BOTH WATER SEPARATOR BAGS. THE ENGINES WERE RUN WITH ALL BLEED SOURCES USED AND NO ODOR WAS DETECTED. 2 L 7 2 4F A6WE 1996100300187 19961003 00187 WP 1996 10 3 CALA9601332 1 19960926 A 2150 20495053 AIR CYC MACH DOUG DC9 DC982 3022082 WP RT PACK INOPERATIVE A CALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 09 15820 19735 5908 49480 SMOKE ENTERED THE CABIN DURING TAXI OUT. THE AIRCRAFT WAS RETURNED TO THE GATE. THE AIR COND TURBINE NOZZLE C/B POPPED WHEN COLDER POSITION SELECTED. MAINTENANCE FOUND WIRING CHAFING/SHORTING TO RT TURBINE NOZZLE SHUTOFF VALVE. THE WIRI NG WAS SPLICED AND THE WIRE BUNDLE WAS REPOSITIONED. THE AIR CONDITIONING SYSTEM OPERATED NORMALLY. SMOKE APPEARED IN THE CABIN AGAIN DURING TAXI IN AT EWR. THE RIGHT PACK WAS TURNED OFF AND THE SMOKE CLEARED. MAINTENANCE FOUND THE RT AIR CYCLE MACHINE AT FAULT. THE RT ACM WAS REMOVED AND REPLACED, OPERATIONAL CHECKS WERE GOOD WITH NO SMOKE DETECTED. 2 L 7 2 4F A6WE 1996100300188 19961003 00188 WP 1996 10 3 CALA9601333 1 19960910 A 5350 LATCHES DOUG DC9 DC982 3022082 WP TAILCONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16893 49392 THE TAILCONE RELEASE AT EXTERIOR HANDLE AND AFT ENTRY DOOR WAS LOW. THE TAILCONE LATCHES WERE ADJUSTED IAW MM 53-53-00. 2 L 7 2 4F A6WE 1996100300189 19961003 00189 WP 1996 10 3 CALA9601334 1 19960910 A 5350 CLIPS DOUG DC9 DC982 3022082 WP TAILCONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16893 49392 THE TAILCONE INTERIOR RELEASE HANDLE PULL FROM CLIPS WAS LOW. THE CLIPS WERE ADJUSTED IAW MM 53-53-00. 2 L 7 2 4F A6WE 1996100300190 19961003 00190 WP 1996 10 3 CALA9601335 1 19960924 A 5320 59174633 PAN DOUG DC9 DC932 3022066 WP DOOR JAMB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12539 45792 INSPECTION FOUND A 3 AND 2.5 INCH CRACK IN RT FORWARD SIDE UPPER CORNER OF DOOR JAMB PAN. A REPAIR WAS INSTALLED IAW DA C DRAWING J060088. 2 L 7 2 4F A6WE 1996100300191 19961003 00191 WP 1996 10 3 CALA9601336 1 19960922 A 5312 BULKHEAD DOUG DC9 DC932 3022066 WP AFT PRESS DOME CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12539 45792 INSPECTION FOUND AFT PRESSURE BULKHEAD DOME CRACKED IN UPPER LEFT AND RIGHT CORNERS OF VENTRAL DOOR CUTOUT. DOUBLERS WE RE INSTALLED IAW DAC DRAWING J060088, SHEETS 2 OF 2, STEPS 1 TO 11. 2 L 7 2 4F A6WE 1996100300192 19961003 00192 NE 1996 10 3 9620516717 2 19960925 A 7230 COMP BLADES BOEING 747 747251F 1384898 NM PWA JT9 JT9D7F 52054 NE NR 3 ENGINE DAMAGED A NWAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 GL 01 617US 21121 89465 DURING CRUISE, THE NR 3 ENGINE EXPERIENCED MULTIPLE COMPRESSOR STALLS AND SUBSEQUENT ENGINE FAILURE. CREW FOLLOWED COM PROCEDURE, SHUT DOWN THE ENGINE AND DIVERTED TO MSP WITHOUT FURTHER INCIDENT. BORESCOPE INSPECTION OF THE ENGINE REVEAL ED DAMAGE TO THE 6TH, 7TH AND 8TH STAGE BLADES. THE ENGINE WAS REPLACED AND RUN-UP TEST WAS NORMAL. 2 L 7 4 4F 4 F A20WE E20EA 1996100300193 19961003 00193 NE 1996 10 3 9620532713 2 19960924 A 7250 TURBINE BOEING 727 7272S7 138407Z NM PWA JT8 JT8D17 52049 NE NR 2 ENGINE FAILURE A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN O OTHER CL CLIMB 1 GL 01 716RC 39307 2524 22021 707902 AFTER TAKEOFF AT 1,500 FEET AGL, THE NR 2 ENGINE BEGAN VIBRATING, EGT REDLINED AND EPR N1 INDICATIONS WERE DECREASING. C REW PERFORMED A PRECAUTIONARY SHUTDOWN OF NR 2 ENGINE AND RETURNED TO DEN WHERE THEY LANDED WITHOUT INCIDENT. MAINTENAN CE REPLACED THE NR 2 ENGINE. 2 L 7 3 4F 4 F A3WE E2EA 1996100300194 19961003 00194 NM 1996 10 3 9620545501 1 19960926 A 5270 SWITCH BOEING 757 757251 1384970 NM DOOR 4L OUT OF ADJUST A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 501US 23190 ABORTED TAKEOFF AT 120 KNOTS DUE TO A LEFT AFT ENTRY DOOR WARNING INDICATION. FOUND THE DOOR CLOSED AND LOCKED. ADJUST ED THE SWITCH PER MM 52-71-00, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A2NM 1996100300195 19961003 00195 1996 10 3 9620559605 4 19960925 A 3442 RADAR SYSTEM DOUG DC9 DC932 3022066 WP COCKPIT MALFUNCTIONED A NWAA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 GL 01 605NW 47233 WEATHER RADAR SYSTEM FAILED AFTER TAKEOFF. THE FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACE D RADAR TRANSCEIVER AND INDICATOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996100300196 19961003 00196 WP 1996 10 3 9620569930 1 19960925 A 3010 12294411 ANTI-ICE VALVE DOUG DC9 DC931 3022065 WP LT MLG WW MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 89S 73653 5239 47042 AIRFOIL ICE PROTECTION PRESSURE ABNORMAL LIGHT ILLUMINATED WITH TAIL ANTI-ICE SELECTED AFTER TAKEOFF. FLIGHT RETURNED T O MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED WING ANTI-ICE VALVE, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996100300197 19961003 00197 WP 1996 10 3 9620579963 1 19960925 A 3350 60030451 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 913RW 47171 DURING LINE MAINTENANCE INSPECTION, FOUND AFT EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHE CK NORMAL. 2 L 7 2 4F A6WE 1996100300198 19961003 00198 WP 1996 10 3 9620589946 1 19960925 A 3350 LIGHTS DOUG DC9 DC931 3022065 WP TAILCONE LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8926E 45863 DURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE EMERGENCY LIGHT AND POWER SUPPLY LOOSE FROM BRACKET. REPLACED POWER SUPPLY AND BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996100300199 19961003 00199 WP 1996 10 3 9620599980 1 19960926 A 3350 60030451 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9344 47440 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD GALLEY, FORWARD ENTRY AND COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLA CED POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996100300200 19961003 00200 1996 10 3 9620609605 4 19960926 A 2565 113317 SLIDE DOUG DC9 DC932 3022066 WP CABIN DOOR LOW PRESSURE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 605NW 1268 1255 47223 DURING PERIODIC CHECK, FOUND MAIN CABIN DOOR EVACUATION SLIDE LOW ON PRESSURE. REPLACED SLIDE. 2 L 7 2 4F A6WE 1996100300201 19961003 00201 NM 1996 10 3 SWAA960993 1 19960922 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 988 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 329SW 23693 DURING SCHEDULED C4 CHECK, FOUND SHARP DENT ON FUSELAGE SKIN BS 988 AT STRINGER 16L. REPAIRED PER SWA RA 1-353-1519. 2 L 7 2 4F RT A16WE 1996100300202 19961003 00202 NM 1996 10 3 SWAA960994 1 19960919 A 3350 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 62SW 22060 DURING SCHEDULED RON CHECK, FOUND FORWARD CABIN EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F A16WE 1996100300203 19961003 00203 NM 1996 10 3 SWAA960995 1 19960919 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 90SW 22905 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOBEAM CORROSION AROUND CLIP NUT HOLES AT BS 344 LBL 7, 10, 12 AND BL 0, ON FWD A ND AFT FLANGES. REPLACED T-CAP PER BOEING SRM. 2 L 7 2 4F A16WE 1996100300204 19961003 00204 NM 1996 10 3 SWAA960996 1 19960919 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED D-CHECK, FOUND A 2 INCH CRACK ON BS 178 BULKHEAD AT WL 189, LBL 7.5. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996100300205 19961003 00205 1996 10 3 SWAA960997 4 19960919 A 3416 ALTIMETER BOEING 737 7373A4 1384585 NM RT COCKPIT INOPERATIVE A SWAA D RETURN TO BLOCK O OTHER CL CLIMB 1 SW 07 679SW 23291 AIR RETURN DUE TO F/O ALTIMETER STICKING AT 800 FT. AIRCRAFT MADE AN UNEVENTFUL LANDING AT MDW. REPLACED INDICATOR PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996100300206 19961003 00206 NM 1996 10 3 SWAA960998 1 19960919 A 3350 LIGHTS BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 636SW 27709 AT GATE, FOUND NUMEROUS EMERGENCY TRACK LIGHTS INOP. RELAMPED AND REPAIRED NUMEROUS WIRES THAT WERE PULLED LOOSE PER BO EING M/M. 2 L 7 2 4F RT A16WE 1996100300207 19961003 00207 NM 1996 10 3 SWAA960999 1 19960921 A 5330 SKIN BOEING 737 7373H4 1384600 NM L1 DOOR CUTOUT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY LOWER HINGE CUTOUT CRACKED ON LOWER CORNER. REPAIRED PER SWA RA 1-352-255. 2 L 7 2 4F RT A16WE 1996100300208 19961003 00208 NM 1996 10 3 SWAA961000 1 19960920 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN DAMAGED AFT OF AFT CARGO DOOR. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996100300209 19961003 00209 NM 1996 10 3 SWAA961001 1 19960920 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 847 TORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN TEAR AT BS 847, BETWEEN STRINGERS 24 AND 25R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996100300210 19961003 00210 NM 1996 10 3 SWAA961002 1 19960920 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 915 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 394SW 27380 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE GOUGED AND DENTED AT BS 915 AT STRINGER S21L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996100300211 19961003 00211 NM 1996 10 3 SWAA961003 1 19960920 A 5330 SKIN BOEING 737 7373Q8 1384670 NM BS 372 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE DENTED AT BS 372, BETWEEN S17 ABD 18R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996100300212 19961003 00212 NM 1996 10 3 SWAA961004 1 19960920 A 3350 LIGHTS BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 515SW 25154 DURING SCHEDULED C4 CHECK, FOUND FLOOR EMERGENCY LIGHTS IN CENTER CABIN INOP. RECONNECTED AND REINSTALLED LIGHTS PER BO EING M/M. 2 L 7 2 4F RT A16WE 1996100300213 19961003 00213 EU 1996 10 3 QXEA9600412 1 19960926 A 3350 1820 BULB FOKKER FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 493US 11161 THREE EMERGENCY LIGHT IN THE CABIN OVERHEAD ARE INOP. BULBS WERE REPLACED AND LIGHTS OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996100300214 19961003 00214 NM 1996 10 3 96FDEA01539 1 19960926 A 5270 CIRCUIT BREAKER BOEING 727 727225 1384077 NM MAIN TRIPPED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 462FE 22550 DURING CLIMBOUT PASSING FLT LVL 260 MCD WARNING LIGHT CAME ON AND CABIN PRESSURIZATION STARTED CLIMBING AT APPROX 500 TO 800 FRM LEVELED OFF, THEN STARTED DESCENDING WHILE ACCOMP RED-TAB PROCEDURES. ACCOMP MANUAL DEPRESSURIZATION WITH MANU AL DC OUTFLOW VALVE. LANDED AT PIA UNEVENTFUAL. AFTER S/D FOUND CARGO DOOR WARNING C/B POPPED. NOTE: HEAVY RAIN ENCOU NTERED ON GRD PRIOR TO THIS FLT. RESET CARGO DOOR WARNING C/B, CYCLED CARGO DOOR SEVERAL TIMES AND CK'D GOOD. PRESSURI ZED A/C TO 2.2 PSI, PRESSURE HELD GOOD. LEAK CK'D, MCD CK'D GOOD. VISUALLY CK'D MCD LOCK, OK FOR SERVICE. 2 L 7 3 4F A3WE 1996100300215 19961003 00215 NE 1996 10 3 96FDEA01540 2 19960927 A 7200 ENGINE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE NR 2 ENGINE FAILED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 608FE 48548 ENGINE FAILED INSPECTION PER EA 7-7220-31529 INSP OF FIRST STAGE BOOSTER VANES. 2 L 7 3 4F 4 F RT A22WE E31N3 1996100300216 19961003 00216 NE 1996 10 3 96FDEA01541 2 19960927 A 7200 ENGINE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE NR 2 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 611FE 48604 ENGINE FAILED INSPECTION PER EA 1-7220-31511 INSP OF FIRST STAGE BOOSTER VANES. 2 L 7 3 4F 4 F RT A22WE E31N3 1996100300217 19961003 00217 NM 1996 10 3 96FDEA01542 1 19960926 A 5311 FRAME BOEING 727 72722C 138400F NM BS 580 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 106FE 19201 FRAME DENTED STA 580 STR 6R. INSTALLED FRAME REPAIR STA 580 STR 6R PER SRM 53-10-6. 2 L 7 3 4F A3WE 1996100300218 19961003 00218 NM 1996 10 3 96FDEA01543 1 19960926 A 5311 FRAME BOEING 727 72722C 138400F NM BS 540 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 106FE 19201 FRAME DENTED STA 540 STR 6R. INSTALLED FRAME REPAIR STA 540 STR 6R PER SRM 53-10-6. 2 L 7 3 4F A3WE 1996100300219 19961003 00219 NM 1996 10 3 96FDEA01545 1 19960926 A 5311 FRAME BOEING 727 72722C 138400F NM STA 580 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 106FE 19201 FRAME DENTED STA 580 STR 6R. INSTALLED FRAME REPAIR STA 580 STR 6R PER SRM 53-10-6. 2 L 7 3 4F A3WE 1996100300220 19961003 00220 NM 1996 10 3 96FDEA01546 1 19960925 A 5320 BEAM BOEING 727 72722C 138400F NM BS 600 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 106FE 19201 NR1051 AND 0104, LOWER LOBE FWD CARGO CORROSION STA 600 FROM LBL 25 TO RBL 25 BOTTOM SIDE OF MAIN DECK BEAM. *S/D* REM OVED CORROSION, TREATED, PRIMED AND INSTALLED DOUBLER REPAIR PER FEDEX EA NR 7-5310-28904 DATED 01 OCT 96. 2 L 7 3 4F A3WE 1996100300221 19961003 00221 NM 1996 10 3 96FDEA01547 1 19960923 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 1148 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 106FE 19201 NRO312, HEAVY CORROSION STA 1148 STR 19L. *S/D* REMOVED CORROSION AND INSTALLED REPAIR PER 53-30-3. 2 L 7 3 4F A3WE 1996100300222 19961003 00222 NM 1996 10 3 96FDEA01548 1 19960925 A 5320 BEAM BOEING 727 72722C 138400F NM BS 540 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 106FE 19201 NR1052, 0104, LOWER LOBE CORROSION STA 540 BETWEEN C/L AND LB 25 BOTTOM SIDE OF MAIN DECK BEAM. *S/D* REMOVED CORROSIO N WITH LIMITS, PRIMED AND TREATED. 2 L 7 3 4F A3WE 1996100300223 19961003 00223 NE 1996 10 3 96UAL900710 2 19960916 A 7261 BREATHER TUBE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 ENGINE BROKEN A UALA A E UNSCHED LANDING ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 581UA 26701 727112PW DURING CRUISE, NR 2 ENGINE OIL QUANTITY INDICATED ZERO. FLIGHT CREW SHUTDOWN ENGINE AND DIVERTED TO COS. *S/D* OIL LO SS DUE TO BROKEN BREATHER TUBE. 2 L 7 2 4F 4 F RT A2NM E17NE 1996100300224 19961003 00224 NM 1996 10 3 96UAL900711 1 19960917 A 3350 BATTERY PACK BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 159UA 21140 FORWARD RIGHT HAND OVERWING EMERGENCY LIGHT ASSEMBLIES INOP. BATTERY PACK DEAD, REPLACED BATTERY PACK. 2 L 7 4 4F 4 F A20WE E20EA 1996100300225 19961003 00225 NM 1996 10 3 96UAL900712 1 19960917 A 3350 LIGHT BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 159UA 21140 EMERGENCY LIGHT ABOVE MAIN ENTRY DOOR 2 LEFT IS INOP. LIGHT BURNED OUT, REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F A20WE E20EA 1996100300226 19961003 00226 EU 1996 10 3 96UAL900713 1 19960918 A 3350 BATTERY PACK DIEHL 321430 AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 403UA 442 EMERGENCY LIGHT TEST GAVE A FAILED INDICATION DURING TESTING. *S/D* REPLACED FORWARD EMERGENCY BATTERY PACK AT FORWARD OVERHEAD DOOR 1 LEFT. 2 L 7 2 4F 4 F RT A28NM E40NE 1996100300227 19961003 00227 EU 1996 10 3 96UAL900714 1 19960918 A 3350 BATTERY PACK RADIANT ILLU 20131A AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 410UA 463 SEAT EEL LIGHTS ARE INOPERATIVE AT SEAT ROWS 13 THROUGH 15 AND 19 THROUGH 21. *S/D* REPLACED RIGHT HAND AFT ESCAPE PAT H BATTERY PACK. 2 L 7 2 4F 4 F RT A28NM E40NE 1996100300228 19961003 00228 NM 1996 10 3 96UAL900715 1 19960918 A 3350 60252 LIGHT BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 906UA 25006 FORWARD GALLEY EMERGENCY ESCAPE PATH LIGHTING INOP. REPLACED FORWARD GALLEY EMERGENCY LIGHT STRIP, CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1996100300229 19961003 00229 EU 1996 10 3 96UAL900716 1 19960918 A 2560 ASSIST BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2R DOOR DISCHARGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 411UA 464 WHILE PERFORMING OPERATIONAL CHECK OF NR 2 AFT RIGHT DOOR AFTER SLIDE REPLACEMENT, THE DOOR ASSIST BOTTLE DISCHARGED AND DOOR WAS UNABLE TO OPEN. 2 L 7 2 4F 4 F RT A28NM E40NE 1996100300230 19961003 00230 1996 10 3 96UAL900717 4 19960919 A 2565 INFLATE TUBE AIR CRUISERS D29835103 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE SLIDE SEPARATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7281U 17517478 21559 DURING TIME CONTROLLED OVERHAUL, SLIDE FAILURE DUE TO SEAM SEPARATION OF THE INFLATION TUBE. UNIT SCRAPPED. 2 L 7 3 4F 4 F A3WE E2EA 1996100300231 19961003 00231 1996 10 3 96UAL900718 4 19960919 A 2565 INFLATE TUBE AIRCRUISERS D29835103 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE SLIDE SEPARATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7274U 179251078 21421 DURING CONTROLLED OVERHAUL, SLIDE FAILED DUE TO SEAM SEPARATION OF THE INFLATION TUBE. SLIDE SCRAPPED. 2 L 7 3 4F 4 F A3WE E2EA 1996100300232 19961003 00232 1996 10 3 96UAL900720 4 19960921 A 3422 25883024 DIRECT GYRO 4O30951901 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 FAILED A UALA K NONE F FLT CONT AFFECTED CR CRUISE 1 WP 29 7454U 21908 UPON ENGAGEMENT OF THE AILERON CHANNEL OF THE AUTOPILOT, MODE A, HARD UNCOMMANDED ROLL TO THE RIGHT OCCURS. SAME CONDI TION OCCURS IN MODE B BUT AT A REDUCED RATE AND CORRECTS ITSELF. REPLACED ROLL COMPUTER AND NR 1 DIRECTIONAL GYRO DUE TO FAILURE. 2 L 7 3 4F 4 F A3WE E2EA 1996100300233 19961003 00233 NM 1996 10 3 96UAL900721 1 19960921 A 2780 RETRACT MECH BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 LE FLAP MALFUNCTIONED A UALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 WP 29 7269U 21416 NR 1 LEADING EDGE FLAP WOULD NOT RETRACT FULLY AT FLAPS 2. AMBER LIGHT ON FRONT PANEL AND SECOND OFFICER PANEL WERE ILL UMINATED. 2 L 7 3 4F 4 F A3WE E2EA 1996100300234 19961003 00234 NM 1996 10 3 96UAL900722 1 19960921 A 2781 WARNING LIGHT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 2 LE FLAP ILLUMINATED A UALA O OTHER N FALSE WARNING DE DESCENT 1 WP 29 7466U 21920 CREW REPORTS, NR 2 LEADING EDGE FLAP AMBER LIGHT ON BOTH PANELS FORWARD AND SECOND OFFICER WHILE PASSING THROUGH 28,000 FEET. NO VIBRATION. 2 L 7 3 4F 4 F A3WE E2EA 1996100300235 19961003 00235 NM 1996 10 3 96UAL900723 1 19960921 A 3397 58631 WIRE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DEFECTIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7264U 21411 FLOOR LEVEL EMERGENCY EXIT SIGN AT DOOR 1 LEFT INOPERATIVE. POWER CABLE FAILED, REPLACED CABLE. 2 L 7 3 4F 4 F A3WE E2EA 1996100300236 19961003 00236 NE 1996 10 3 96UAL900724 2 19960921 A 7261 O-RING BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE CUT A UALA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 7452U 21906 700226 NR 2 ENGINE SHUT DOWN AT FLIGHT LEVEL 310 DUE TO LOSS OF OIL QUANTITY AND PRESSURE. RETURNED TO FIELD. *S/D* FOUND CU T O-RING ON MAIN OIL FILTER COVER. REPLACED O-RING, MOTORED ENGINE AND FOUND NO LEAKS. 2 L 7 3 4F 4 F A3WE E2EA 1996100300238 19961003 00238 NM 1996 10 3 96UAL900726 1 19960921 A 2780 RETRACT MECH BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 4 LE FLAP MALFUNCTIONED A UALA K NONE J WARNING INDICATION NR NOT REPORTED 1 WP 29 7260U 21407 LEADING EDGE SLAT NR 4 PARTIALLY EXTENDED. VERIFIED BY VISUAL CHECK. ON GROUND FLAPS MOVED TO TAKEOFF SETTING DURING S EVERAL OPERATIONS. 2 L 7 3 4F 4 F A3WE E2EA 1996100300239 19961003 00239 NM 1996 10 3 96UAL900727 1 19960921 A 2730 CONTROL SURFACES BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE ELEVATOR OUT OF TRIM A UALA K NONE F FLT CONT AFFECTED TO TAKEOFF 1 WP 29 7252U 21399 CONTROL FORCES HEAVY OUT OF TRIM ON ROTATION WITH FLAPS 15 DEGREES. NORMAL ON APPROACH. 2 L 7 3 4F 4 F A3WE E2EA 1996100300240 19961003 00240 NM 1996 10 3 96UAL900728 1 19960921 A 3246 WHEEL BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NLG SHIMMY A UALA K NONE E VIBRATION/BUFFET TO TAKEOFF 1 WP 29 7297U 21892 SEVERE NOSE WHEEL SHIMMY ON TAKEOFF. 2 L 7 3 4F 4 F A3WE E2EA 1996100300241 19961003 00241 NE 1996 10 3 96UAL900729 2 19960921 A 7311 FUEL OIL COOLER PRATT & WHIT 534096 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE LEAKING A UALA O OTHER K FLUID LOSS IN INSP/MAINT 1 WP 29 7459U 21913 UPON ARRIVAL, FOUND FUEL RUNNING OUT OF BOTTOM OF COWLING ON NR 1 ENGINE. MOTORED ENGINE AND FOUND FUEL/OIL COOLER LEAK ING FUEL OUT FORWARD VENT HOLE. *S/D* A SEAL FAILED WITHIN THE FUEL/OIL COOLER, CAUSING THE FUEL TO LEAK OUT OF THE F UEL/OIL COOLER FORWARD VENT HOLE. THE FUEL/OIL COOLER WAS REPLACED, OPERATIONS CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1996100300242 19961003 00242 NM 1996 10 3 96UAL900730 1 19960921 A 2750 RETRACT MECH BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE TE FLAPS MALFUNCTIONED A UALA K NONE F FLT CONT AFFECTED TX TAXI/GRND HDL 1 WP 29 7263U 21410 ON TAXI IN, INBOARD TRAILING EDGE FLAPS DO NOT OPERATE HYDRAULICALLY, STUCK AT 25 DEGREES. FLAPS RETRACTED FROM 30 TO 2 5 ON LANDING ROLLOUT. 2 L 7 3 4F 4 F A3WE E2EA 1996100300243 19961003 00243 GL 1996 10 3 96UAL900731 2 19960921 A 7261 9013M796019005 GAMMAH FITTING DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL ENGINE OIL SYST LOOSE A UALA O OTHER K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 WP 29 1825U 46624 UPON ARRIVAL FOUND ENGINE OIL QUANTITY AT ZERO. ADDED 19 QUARTS, RAN ENGINE AND FOUND LEAK AT AFT OIL SCAVENGE STRUT IN SIDE AND OUTSIDE TAILPIPE. ALSO, FOUND OIL POOLING AT TURBINE EXIT GUIDE VANES. *S/D* D-SUMP GAMMAH FITTING LOOSE/WOR N, SLEEVE ID WORN. BOTH LINES REPLACED ALONG WITH THE VENT TUBING IN THE MID SHAFT AREA FRONT TO BACK. THE LPT ROTOR/S TATOR/TRF WAS REPLACED DUE TO OIL WET AND TO REMEASURE AIR/OIL SEALS. THE ENGINE RUN WAS GOOD. THIS IS UNIQUE AND CON SIDERED TO BE A ONE TIME OCCURANCE (P/N 9013M79601, 9005M71601, 9013MSCP10). 2 L 7 3 4F 4 F A22WE E23EA 1996100300244 19961003 00244 NM 1996 10 3 96UAL900732 1 19960921 A 5330 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUSELAGE LIGHTNING STRIKE A UALA A UNSCHED LANDING C F.O.D. CL CLIMB 1 WP 29 7298U 21893 AIRCRAFT SUSTAINED LIGHTNING STRIKE NEAR RADOME. AIRCRAFT RETURNED TO FIELD. NUMEROUS STRIKES FOUND ALONG LEFT SIDE OF FUSELAGE FROM RADOME TO JUST FORWARD OF WING LEADING EDGE. *S/D* REPLACED RADOME, REPLACED DAMAGED RIVETS AND REPAIRE D FUSELAGE SKIN PER SRM 53-30-03. 2 L 7 3 4F 4 F A3WE E2EA 1996100300245 19961003 00245 NM 1996 10 3 96UAL900733 1 19960921 A 3260 WARNING LIGHT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE RT MLG DOOR MALFUNCTIONED A UALA O OTHER N FALSE WARNING CL CLIMB 1 WP 29 7467U 21921 RIGHT GEAR RED LIGHT IS ON, GEAR DOOR LIGHT IS OUT, NO VIBRATION REPORTED. 2 L 7 3 4F 4 F A3WE E2EA 1996100300246 19961003 00246 NM 1996 10 3 96UAL900734 1 19960921 A 3350 S106 BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7252U 21399 EMERGENCY EXIT SIGN AT ROW 3 OUT. BATTERY FOUND TO BE INOPERATIVE. REPLACED BATTERY AND LIGHT CHECKS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1996100300247 19961003 00247 WP 1996 10 3 96UAL900735 1 19960921 A 2612 FIRE LOOP DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 3 ENGINE NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1858U 46987 NR 3 ENGINE A FIRE DETECTION LOOP NO TEST. 2 L 7 3 4F 4 F A22WE E23EA 1996100300248 19961003 00248 WP 1996 10 3 96UAL900736 1 19960921 A 2612 B-FIRE LOOP DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 3 ENGINE NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1858U 46987 NR 3 ENGINE B-LOOP NO TEST. 2 L 7 3 4F 4 F A22WE E23EA 1996100300249 19961003 00249 NM 1996 10 3 96UAL900737 1 19960921 A 3350 6104781 BATTERY PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7459U 21913 DOOR 1 RIGHT AND DOOR 1 LEFT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. FUSELAGE SLIDE LIGHTS INOPERATIVE. REPLACED BATTER Y PACK AND THE LIGHT OPERATION IS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1996100300252 19961003 00252 WP 1996 10 3 96DHL802005 1 19960924 A 2710 57147155512 AILERON CTL VLV 55972735502 DOUG DC8 DC873F 302199F WP RT BYPASSING A DHLA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 802DH AC2710101119 46076 AFTER TAKEOFF, AIRCRAFT ROLLED TO THE RIGHT IN LEVEL FLIGHT AND FELT AS IF IT WAS OPERATING IN MANUAL REVERSION MODE. T HERE WERE NO OTHER INDICATIONS OF THE A/C OPERATING IN MANUAL REVERSION. REMOVED AND REPLACED AILERON CONTROL VALVE CYL INDER AND AILERON TAB LOCKOUT CYLINDER, PULLEYS, TRIPLE PULLEY ASSY AND AILERON BUS CABLE. 2 L 7 4 4F RT 4A25 1996100300253 19961003 00253 NM 1996 10 3 P5CA9600727 1 19960924 A 5245 HINGE BOEING 747 747122 1384872 NM ACM DOOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 LEVEL 1 CORROSION ON NR 3 AIR CYCLING MACHINE ACCESS DOOR. REPLACED HINGE PER BOEING MAINTENANCE MANUAL 52-48-01. 2 L 7 4 4F A20WE 1996100300254 19961003 00254 NM 1996 10 3 P5CA9600728 1 19960925 A 7110 NOSE COWL BOEING 747 747122 1384872 NM NR 4 ENGINE DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 DENT AT 6 O'CLOCK POSITION NR 4 ENGINE NOSE COWL. REPAIRED PER BOEING SRM 54-30-03. 2 L 7 4 4F A20WE 1996100300255 19961003 00255 WP 1996 10 3 ARWA9609031 1 19960925 A 3350 207004001 BATTERY PACK DOUG DC8 DC862 3021970 WP CABIN DISCHARGED A ARWA K NONE L NO TEST LD LANDING 1 SO 19 791AL 46150 EMERGENCY EXIT LIGHT DOES NOT DISARM. DOME LIGHT STAYS ON. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CHEC KED OK IAW MM 3-50-00. 2 L 7 4 4F 4A25 1996100300256 19961003 00256 WP 1996 10 3 ARWA9609032 1 19960927 A 2612 390D FIRE WARN AMP DOUG DC8 DC863 302198A WP NR 1 ENGINE MALFUNCTIONED A ARWA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 SO 19 345JW 46042 AFTER TAKEOFF, FIRE WARNING NR 1 ENGINE. ENGINE SHUTDOWN WITH ENGINE FIRE CHECKLIST. DISCHARGED BOTH LEFT WING FIRE BO TTLES. AIRCRAFT RETURNED TO SJU AND MADE OVERWEIGHT LANDING, BLOWING NR 1, 2 AND 8 TIRES. FALSE FIRE WARNING, NO VISUA L INDICATION OF FIRE. TROUBLESHOOTING NOTED FAULTY FIRE WARNING AMP. REMOVED AND REPLACED AMP SYSTEM, OPS CHECKED NORM AL. PERFORMED OVERWEIGHT/HARD LANDING INSPECTION, NO STRUCTURAL DAMAGE NOTED. REMOVED AND REPLACED NR 1, 2, 7 AND 8 TI RES, CLEANED ENGINE, REMOVED AND REPLACED NR 1 AND 2 FIRE BOTTLE. 2 L 7 4 4F 4A25 1996100300257 19961003 00257 WP 1996 10 3 TC8A96059 1 19960924 A 5313 37542251 LONGERON DOUG DC8 DC862F 3021972 WP BS 600-620 CRACKED A TC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 183SK 45904 DURING BASE MODIFICATION, FOUND LONGERON SPLICE CRACKED AT LONGERON 31 LEFT HAND BETWEEN STA 600 TO 620 CRACKED .25 INCH . REMOVED AND REPLACED LONGERON SPLICE IAW DC8 SRM 51-1-20D AND 51-1-8. TASK CARD NR 81712. REPORT GENERATED BY AMERI CAN INTERNATIONAL AIRWAYS, INC B4MR FOR TRANS CONTINENTIAL AIRLINES TC8A. 2 L 7 4 4F 4A25 1996100300258 19961003 00258 WP 1996 10 3 TC8A96060 1 19960924 A 5312 57726383 BULKHEAD WEB DOUG DC8 DC862F 3021972 WP AFT PRESS BLKHD DAMAGED A TC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 183SK 45904 COMPLIED WITH AD 90-16-05 AFT PRESSURE BULKHEAD WEB MODIFICATION. REPAIRED AFT PRESSURE BULKHEAD WEB IAW SB 53-53 REF D AC FAX FILE NR GLP1813/96-07-23-010. TASK CARD NR 79494. REPORT GENERATED BY AMERICAN INTERNATIONAL AIRWAYS, INC B4MR FOR TRANS CONTINENTIAL AIRLINES TC8A. 2 L 7 4 4F 4A25 1996100300259 19961003 00259 NE 1996 10 3 VSTA9609006 2 19960922 A 7230 750801 BLADE BOEING 737 737204 1384458 NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE DAMAGED A VSTA K NONE O OTHER UK UNKNOWN 1 WP 07 312VA 20236 NR 1 ENGINE FAN C1 BLADE DAMAGED. REPLACED 3 C1 FAN BLADES. 2 L 7 2 4F 4 F A16WE E2EA 1996100300260 19961003 00260 WP 1996 10 3 TC8A96061 1 19960926 A 2923 165W010103 PUMP DOUG DC8 DC851 3021920 WP SPOILER SYST MALFUNCTIONED A TC8A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 805CK 45649 DURING FLIGHT CONTROL CHECK, NOTED SPOILER PRESSURE ONLY 1,OOO PSI. REMOVED AND REPLACED SPOILER PUMP, OPS CHECKED NORM AL NUMEROUS TIMES IAW 27-34-6. 2 L 7 4 4F 4A25 1996100300261 19961003 00261 NE 1996 10 3 CALA9601337 2 19960927 A 7261 3051157040 SEAL BOEING 737 737524 1384721 NM GE CFM56 CFM563B1 13802 NE CSD DR PAD LEAKING A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 16607 27320 857822 THE NR 1 ENGINE OIL DECREASED TO ZERO QUANTITY AND OIL PRESSURE FLUCTUATED WHILE EN ROUTE FROM EWR TO DFW. THE AIRCRAFT WAS DIVERTED TO ATL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND OIL LEAKAGE AT THE CSD DRIVE PAD MAGNETIC SEAL . THE SEAL WAS REMOVED AND REPLACED IAW MM 72-60-00. LEAK AND OPERATIONAL CHECKS WERE GOOD DURING ENGINE RUN. 2 L 7 2 4F 4 F RT A16WE E2GL 1996100300262 19961003 00262 NM 1996 10 3 CALA9601338 1 19960927 A 3260 655825029 CIRCUIT CARD BOEING 737 7373T0 1384582 NM LOGIC SHELF MALFUNCTIONED A CALA O OTHER N FALSE WARNING CR CRUISE 1 SW 09 14307 23358 THE NOSE GEAR RED UNSAFE LIGHT ILLUMINATED AT ALTITUDE AND REMAINED ON. WHEN THE GEAR HANDLE WAS LOWERED, THE RED LIGHT STAYED ON AND THE GREEN LIGHT DID NOT COME ON. A MANUAL GEAR EXTENSION WAS PERFORMED AND A VISUAL CHECK THROUGH THE VI EW PORT SHOWED STRIPES ALIGNED. THE NOSE GEAR RED LIGHT WENT OUT AND THE GREEN LIGHT CAME ON AFTER TOUCHDOWN AND WEIGHT ON THE NOSE GEAR. MAINTENANCE WAS UNABLE TO DUPLICATE THE PROBLEM ON THE GROUND. THE M983 AND M1214 CIRCUIT CARDS WER E REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. BITE TEST AND GROUND CHECKS WERE GOOD IAW MM 32-09-20. 2 L 7 2 4F RT A16WE 1996100300263 19961003 00263 WP 1996 10 3 CALA9601339 1 19960928 A 2424 947F9452 GCU DOUG DC9 DC982 3022082 WP APU INOPERATIVE A CALA O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 SW 09 809NY 30880 1378 49263 WHILE OPERATING THE APU DURING CRUISE FLIGHT WITH THE LEFT GENERATOR PLACARDED INOPERATIVE, THE APU GENERATOR TRIPPED OF F. THE FAILURE WAS ACCOMPANIED BY AN AC CROSSTIE LOCKOUT LIGHT. THE APU GENERATOR WAS RESET AND POWER WAS RESTORED. MA INTENANCE REMOVED AND REPLACED THE APU GENERATOR CONTROL UNIT PER MM 24-20-07 AND OPERATION CHECKED GOOD. PART TOTAL CY CLES, 14,523. 2 L 7 2 4F A6WE 1996100300264 19961003 00264 WP 1996 10 3 CALA9601340 1 19960929 A 4930 360800010 FUEL CONTROL DOUG DC9 DC982 3022082 WP APU LEAKING A CALA O OTHER B K SMOKE/FUMES/ODORS/SPARKS FLUID LOSS DE DESCENT 1 SW 09 16887 603 603 49116 A STRONG FUEL SMELL WAS NOTICED IN THE COCKPIT AND CABIN WHILE DESCENDING INTO CLE. THE AIRCRAFT LANDED WITHOUT INCIDEN T. MAINTENANCE FOUND FUEL LEAKING FROM APU FUEL CONTROL DRAIN. THE APU FUEL CONTROL UNIT WAS REMOVED AND REPLACED PER MM 49-01-1. THE APU WAS RUN AND OPERATION CHECKED GOOD. PART TOTAL CYCLES, 273. 2 L 7 2 4F A6WE 1996100300265 19961003 00265 1996 10 3 CALA9601341 4 19960927 A 3417 HG480B20 AIR DATA COMP BOEING 737 7372C0 1384488 NM E/E COMPT CONTAMINATED A CALA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SW 09 73243 12401 20072 THE ACFT EXPERIENCED INTERMITTENT ROLL OF NO MORE THAN 10 DEGREES UNCOMMANDED WITH BOTH AUTOPILOT A ANDB SELECTED WHILE EN ROUTE. PITCH MODE FUNCTIONED NORMALLY. MAINTENANCE PERFORMED A GROUND TEST OF BOTH AUTOPILOT SYSTEMS. THE A-SYSTEM WAS TOTALLY INOPERATIVE IN ROLL. INSPECTION FOUND LOOSE PINS ON SOME PITCH AND ROLL COMPUTER CONNECTORS. THE ROLL COM PUTER WAS REMOVED AND REPLACED DUE TO FAILURE OF SELF TEST. THE AIRCRAFT HAS CONTINUED TO HAVE ROLL RELATED PROBLEMS ON SUBSEQUENT FLIGHTS. *S/D* IN A SUBSEQUENT PROBLEM THE AIR DATA COMPUTER WAS REPLACED. SHOP FINDINGS REVEALED LIQUID CONTAMINATION IN THE ADC. AN INSPECTION OF THE E AND E COMPARTMENT DRIP PAN AND SHROUDS INSTALLATION, REVEALED THAT THE 2 L 7 2 4F A16WE 1996100300266 19961003 00266 1996 10 3 9620529153 4 19960926 A 3442 20671570153 TR UNIT DOUG DC9 DC914 3022034 WP FWD FUSELAGE MALFUNCTIONED A NWAA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 01 8912E 45829 EN ROUTE TO MEM, RADAR WOULD NOT PAINT KNOWN WEATHER. FLIGHT DIVERTED TO LIT AND LANDED WITHOUT INCIDENT. REPLACED RAD AR TRANSCEIVER. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996100300267 19961003 00267 NE 1996 10 3 9620725515 2 19960925 A 7200 ENGINE PRATT PW2037 BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE NR 2 FAILED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN X ENGINE FLAMEOUT CL CLIMB 1 GL 01 515US 716346 23203 716346 DURING CRUISE FLIGHT, CREW DESCENDED TO AVOID TURBULENCE. DURING CLIMBOUT BACK TO ORIGINAL FLIGHT ALTITUDE, NR 2 ENGIN E EXPERIENCED AN UNCOMMANDED SHUTDOWN. AIRCRAFT DIVERTED TO YEG AND PERFORMED AN UNEVENTFUL SINGLE ENGINE LANDING. GRO UND MAINTENANCE REMOVED AND REPLACED ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 1996100300268 19961003 00268 NE 1996 10 3 9620739935 2 19960927 A 7230 COMPRESSOR DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7 52053 NE RT ENGINE BIRD STRIKE A NWAA A E F UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. C F.O.D. CL CLIMB 1 GL 01 1332U 47404 649626 AT ROTATION, THE RIGHT ENGINE INGESTED A BIRD CAUSING SEVERE VIBRATION. CREW SHUT DOWN THE RIGHT ENGINE AND PERFORMED A N AIR TURNBACK LANDING AT MDW. AFTER LANDING, FIRE PERSONNEL REPORTED FUEL LEAKING FROM THE RIGHT ENGINE. AS A PRECAUT ION, CREW PULLED RIGHT ENGINE FIRE HANDLE AND FIRED ONE BOTTLE. FUEL LEAK CEASED AND AIRCRAFT RETURNED TO THE GATE WITH OUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE. 2 L 7 2 4F 4 F A6WE E2EA 1996100300269 19961003 00269 WP 1996 10 3 9620749753 1 19960925 A 3260 DOOR LIGHT DOUG DC9 DC941 302207N WP LANDING GEAR MALFUNCTIONED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 753NW 47117 AFTER TAKEOFF, GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED. FOLLOWED COM PROCEDURES, LIGHT REMAINED ON. RECYCLED GEAR AN D LIGHT EXTINGUISHED. FLIGHT CONTINUED TO MCI AND LANDED WITHOUT INCIDENT. MAINTENANCE CYCLED GEAR DOORS SEVERAL TIMES AND CHECKED GOOD. CHECKED SWITCH ADJUSTMENT PER MM. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996100300270 19961003 00270 SO 1996 10 3 COMA9610288 1 19960926 A 5270 SWITCH EMB 120 EMB120RT SO CARGO DOOR OUT OF ADJUST A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 247CA 120225 CARGO DOOR WARNING SOUNDED DURING TAKEOFF. ADJUSTED CARGO DOOR MICROSWITCH. AIRCRAFT CONTINUED SERVICE. 2 L 7 2 4T RT A31SO 1996100300271 19961003 00271 SO 1996 10 3 COMA9610289 1 19960926 A 6120 7944441 SEALS EMB 120 EMB120RT SO LT PROP WORN A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 130G 120130 LEFT PROPELLER IS SLOW TO FEATHER OR UNFEATHER. REPLACED PROPELLER TRANSFER TUBE SEALS. 2 L 7 2 4T RT A31SO 1996100300272 19961003 00272 EU 1996 10 3 COMA9630147 1 19960926 A 2435 23080031 STARTER GEN SAAB SF340 SF340A 7850100 EU LT ENGINE INOPERATIVE A COMA D RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 SO 01 347CA 18713 284 340A028 LEFT ENGINE STARTER IS INOPERABLE. REPLACED LEFT STARTER/GENERATOR. PART TOTAL CYCLES, 19,217. 2 L 7 2 4T RT A52EU 1996100300273 19961003 00273 EA 1996 10 3 COMA9660152 1 19960926 A 2750 857SD10015 SHAFT CNDAIR CL600 CL6002B19 EA LT TE FLAP BROKEN A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 946CA 7072 FLAPS FAIL MESSAGE ON EICAS. FLAPS WILL NOT OPERATE. REPLACED DEFECTIVE FLEX DRIVE CABLE ON LEFT INBOARD FLAP. 2 L 7 2 4F RT A21EA 1996100300274 19961003 00274 EA 1996 10 3 COMA9660153 1 19960925 A 2760 4916405 SECU CNDAIR CL600 CL6002B19 EA E/E COMPT MALFUNCTION A COMA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 01 915CA 7013 LEFT SPOILERON IS DEPLOYED AND WILL NOT STOW. REPLACED THE NR 1 SPOILER ELECTRONIC CONTROL UNIT. 2 L 7 2 4F RT A21EA 1996100300275 19961003 00275 NM 1996 10 3 96FDEA01550 1 19960926 A 2910 HYD LINE BOEING 727 72722 1384002 NM NR 12 SPOILER CRACKED A FDEA O OTHER F K J FLT CONT AFFECTED FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 107FE 19202 IN-FLIGHT AT FL 280, NR 1 ENGINE HYDRAULIC PUMP LIGHT STARTED BLINKING WITH FLUCTUATION IN PRESSURE. TWO SECONDS LATER, NR 2 ENGINE HYD PRESS LIGHT BLINKED, THEN BOTH LIGHTS CAME ON STEADY WITH RAPID LOSS OF ALL A-SYSTEM HYD FLUID. PUMPS WERE OPERATED WITHOUT FLUID FOR ABOUT THIRTY MINUTES. QUANTITY WENT TO ZERO ALMOST IMMEDIATELY WITH ILLUMINATION OF PUM P LIGHTS. FOUND HYD RETURN LINE BY NR 12 SPOILER CRACKED. REMOVED AND REPLACED LINE. CHANGED BOTH A-SYSTEM PRESSURE F ILTERS AND RETURN FILTER. SERVICED SYSTEM. REMOVED AND REPLACED NR 2 HYD PUMP AND CASE DRAIN FILTERS. LEAK CK GOOD. 2 L 7 3 4F A3WE 1996100300276 19961003 00276 NM 1996 10 3 96FDEA01551 1 19960928 A 5753 66216309 SKIN BOEING 727 72725 1384006 NM RT TE FOREFLAP DELAMINATION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 511FE 18283 NR0579 AND 008, WHILE WORKING NR0576 FOUND THREE AREAS OF DELAMINATION ON LOWER SURFACE. *S/D* REPAIRED DAMAGED SKIN T O RIGHT I/B FORE FLAP LOWER SURFACE PER FEDEX SRM 51-40-6. 2 L 7 3 4F A3WE 1996100300277 19961003 00277 NM 1996 10 3 96FDEA01552 1 19960928 A 5315 BAC1518391 FLOORBEAM BOEING 727 72725 1384006 NM BS 620 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 511FE 18283 NR0434 AND 009, CORROSION (C53-224-01, -1, -100) AT STA 620 RBL 3 WL 208 ON FRAME FILLER. *S/D* REPAIRED FLOORBEAM AT BS 620 WL 208 RBL 35 TO LBL 24 IAW FEDEX SRM 53-10-8 FIG 3. 2 L 7 3 4F A3WE 1996100300278 19961003 00278 NM 1996 10 3 SCNA96266 1 19960926 A 2611 PU90421S SMOKE DETECTOR BOEING 727 7272J4 1384006 NM FORWARD LAV INTERMITTENT A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 288SC 20765 FORWARD LAVATORY SMOKE DETECTOR TEST BUTTON WAS FOUND INTERMITTENT. REMOVED AND REPLACED SMOKE DETECTOR AND OPS CHECKED GOOD. 2 L 7 3 4F RT A3WE 1996100300279 19961003 00279 WP 1996 10 3 ARWA9609033 1 19960928 A 2110 S43C51 CLAMP DOUG DC8 DC863F 302198F WP TURBO COMPRESSOR LOOSE A ARWA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 19 441J 45988 DURING FLIGHT FROM SJU, COULD ONLY PRESSURIZE AIRCRAFT AT TO 5.0PSI DIFFERENTIAL, WITH ALL T.C.'S RUNNING AND OUTFLOW CL OSED. CABIN CONTINUED TO CLIMB TO F.L.16.0 AFTER LEVEL OFF AT F.L. 29.0. AIRCRAFT DIVERTED TO MIA WITHOUT INCIDENT. F OUND CONNECTOR CLAMP AT NR 1 AND NR 2 T/C DELIVERY DUCT TO MIXING VALVE DISCONNECTED. RECONNECTED CONNECTORS, PRESSURIZ ED AIRCRAFT, OPS CHECKED NORMAL, 8PSI DIFFERENTIAL. 2 L 7 4 4F 4A25 1996100300280 19961003 00280 WP 1996 10 3 ARWA9609034 1 19960928 A 2910 AE7007651 HOSE DOUG DC8 DC863 302198A WP NR 2 ENGINE LOOSE A ARWA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 19 345JW 46042 ON APPROACH TO MIA, LOST MAIN HYDRAULIC (GENERAL SYSTEM), SLOW LEAK. EXECUTED ABNORMAL HYDRAULIC CHECK LIST AND DECLARE D EMERGENCY TO ATC. AIRCRAFT LANDED IN MIAMI WITHOUT INCIDENT. TROUBLESHOOTING REVEALED LEAKING PRESSURE LINE ON NR 2 E NGINE. RE-SECURED LINE. LEAK CHECK GOOD ON RUN-UP. 2 L 7 4 4F 4A25 1996100300281 19961003 00281 NM 1996 10 3 VNAA9609006 1 19960926 A 2731 8409 ACTUATOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT/RT ELEV TRIM MOISTURE CONTAM A VNAA O OTHER J F WARNING INDICATION FLT CONT AFFECTED CR CRUISE 1 GL 07 426JS 33581 3038 ELEVATOR TRIM FAILED WHILE AT FL290. EMERGENCY DECLARED TO ALLOW DESCENT AT UNUSUAL AIRSPEED. PROBLEM CLEARED AT 8,000 FT, AIRCRAFT LANDED WITHOUT INCIDENT. FOUND MOISTURE IN ELEVATOR TRIM ACTUATORS. REPLACED ACTUATORS IN ACCORDANCE WIT H DORNIER MAINTENANCE MANUAL 27-32-00, OPERATIONAL CHECK GOOD. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996100300282 19961003 00282 SO 1996 10 3 SRAA960917 1 19960927 A 6120 582855 VALVE HOUSING LKHEED 382 382B 5264104 SO NR 1 PROP FAILED A SRAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 GL 23 907SJ 5800 4248 DURING FLIGHT SJ9404 FROM CHS TO HOW, NR 1 ENGINE RPM FLUXED AND DECAYING STEADILY WITH ENGINE TORQUE, TIT, AND FUEL FLO W INDICATIONS FOLLOWING. SHUT DOWN NR 1 ENGINE AND LANDED WITHOUT INCIDENT AT HOW. INSPECTED NR 1 ENGINE INTAKE AND EX HAUST, NO DEFECTS FOUND, VISUALLY AND OHM METER USED TO CHECK MAG PLUGS, ALL CHECKED GOOD. SUSPECT VALVE HOUSING FAULT Y, REPLACED VALVE HOUSING, PERFORMED ENGINE RUN SYSTEM OPS CHECKED GOOD. 2 H 7 4 4T A1SO 1996100300283 19961003 00283 NM 1996 10 3 SWAA961005 1 19960926 A 2450 RELAY BOEING 737 7372T4 1384492 NM NR 1 TRANS BUS FAILED A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 722WN 22698 AIRCRAFT RETURNED TO IND AND LANDED WITHOUT INCIDENT DUE TO A REPORTED ELECTRICAL SMELL. REPLACED NR 1 TRANSFER BUS REL AY PER BOEING M/M. 2 L 7 2 4F A16WE 1996100300284 19961003 00284 NM 1996 10 3 SWAA961006 1 19960927 A 2120 AIR DISTR BOEING 737 7372T4 1384492 NM COCKPIT ODOR A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 722WN 22698 AIRCRAFT DIVERTED TO SDF DUE TO AN ELECTRICAL SMELL OF FUMES IN COCKPIT. CHECKED GASPER AIR FAN AND EQUIPMENT COOLING F ANS, J-10 AND J-5 SHIELDS, P6 AND P18 PANELS, COALESER BAGS, E/E COMPARTMENT, RAN ENGINES WITH AC BUSSES AND SYSTEMS POW ERED UP PER BOEING M/M. NO DEFECTS NOTED. 2 L 7 2 4F A16WE 1996100300285 19961003 00285 NM 1996 10 3 SWAA961007 1 19960926 A 3350 20121 BATTERY BOEING 737 7375H4 138449D NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 510SW 24187 DURING SCHEDULED BC4 CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHTING INOPERATIVE AT AFT SERVICE DOOR. REPLACED BATTERY AN D CHARGER HOUSING PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996100300286 19961003 00286 NM 1996 10 3 SWAA961008 1 19960926 A 5330 SKIN BOEING 737 7375H4 138449D NM BS 969 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 510SW 24187 DURING SCHEDULED BC4 CHECK, FOUND FUSLAGE SKIN GOUGED AT BS 969, S17L. REPAIRED PER SWA RA 1-553-1523. 2 L 7 2 4F RT A16WE 1996100300287 19961003 00287 NM 1996 10 3 SWAA961009 1 19960925 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 1006 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 51SW 21448 DURING SCHEDULED C4 CHECK, FOUND S27L CORRODED AT BS 1006. REPAIRED PER BOEING M/M. 2 L 7 2 4F A16WE 1996100300288 19961003 00288 NM 1996 10 3 SWAA961010 1 19960925 A 3350 6104791 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 92SW 22964 DURING SCHEDULED TERMINAL CHECK, FOUND OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK PER BOEING M/M . 2 L 7 2 4F A16WE 1996100300289 19961003 00289 NM 1996 10 3 SWAA961011 1 19960925 A 5313 STRINGER BOEING 737 7372T4 1384492 NM BS 747 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED TERMINAL CHECK, FOUND S16R CRACKED AT BS 747. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996100300290 19961003 00290 NM 1996 10 3 SWAA961012 1 19960925 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 200 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 200, RBL 9, WL 168. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996100300291 19961003 00291 NM 1996 10 3 SWAA961013 1 19960926 A 2120 AIR DISTR BOEING 737 7373H4 1384600 NM CABIN ODOR A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 318SW 23340 IN-FLIGHT, EXPERIENCED A STRONG SMELL OF HYDRAULIC FLUID IN CABIN AND COCKPIT DURING TAKEOFF AND AGAIN WHEN LOWERING FLA PS COMING INTO LAX. INSPECTED A/C BAYS, PERFORMED ENGINE RUN WITH BLEEDS ON PER BOEING M/M, NO DEFECTS NOTED. 2 L 7 2 4F RT A16WE 1996100300292 19961003 00292 NM 1996 10 3 SWAA961014 1 19960926 A 3350 6104791 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 57SW 21722 DURING SCHEDULED TERMINAL CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK PER BOEI NG M/M. 2 L 7 2 4F A16WE 1996100300293 19961003 00293 1996 10 3 SWAA961015 4 19960926 A 2565 22D22900131 SLIDE BOEING 737 7372H4 138448C NM FWD SERV DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 67SW 22356 DURING SCHEDULED SERVICE CHECK, FOUND FORWARD SERVICE DOOR EVACUATION SLIDE PRESSURE LOW. REPLACED SLIDE PER BOEING M/M . 2 L 7 2 4F A16WE 1996100300294 19961003 00294 NM 1996 10 3 SWAA961016 1 19960922 A 5320 SKIN BOEING 737 7372H4 138448C NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 26SW 21117 DURING SCHEDULED C1 CHECK, FOUND NOSE W/W CEILING SKIN CRACKED AFT OF MANUAL EXTENSION RETURN SPRING BRACKET. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996100300295 19961003 00295 NM 1996 10 3 SWAA961017 1 19960923 A 5330 SKIN BOEING 737 7372K6 NM BS 747-767 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED TERMINAL CHECK, FOUND 3 FUSELAGE SKIN CRACKS BETWEEN BS 747 AND BS 767. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996100300296 19961003 00296 NM 1996 10 3 SWAA961018 1 19960923 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 328SW 23689 DURING SCHEDULED A1 CHECK, FOUND CRACK FORWARD OF SHEAR WEB BEAM STRINGER 18A. REPAIRED PER ACO 6580-56 AND RA 1-353-15 18. 2 L 7 2 4F RT A16WE 1996100300297 19961003 00297 NM 1996 10 3 SWAA961019 1 19960927 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED D-CHECK, FOUND CRACK INDICATION AT BS 178, WL 195, RBL 30. REPAIRED PER TRAMCO EWO 96-0461. 2 L 7 2 4F RT A16WE 1996100300298 19961003 00298 NM 1996 10 3 SWAA961020 1 19960927 A 5315 FLOOR BEAM BOEING 737 7372H4 138448C NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 90SW 22905 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 344, LBL 49, 43, 35, 33, 29, 28 AROUND NUTPLATE HOLE. REP LACED T-CAP PER BOEING SRM, 2 L 7 2 4F A16WE 1996100300299 19961003 00299 NM 1996 10 3 SWAA961021 1 19960927 A 5315 FLOOR BEAM BOEING 737 7372H4 138448C NM BS 294 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 90SW 22905 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 294. REPLACED T-CAP PER BOEING SRM, 2 L 7 2 4F A16WE 1996100300300 19961003 00300 NM 1996 10 3 SWAA961022 1 19960927 A 5315 FLOOR BEAM BOEING 737 7372H4 138448C NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 90SW 22905 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 344. REPLACED T-CAP PER BOEING SRM, 2 L 7 2 4F A16WE 1996100300301 19961003 00301 NM 1996 10 3 SWAA961023 1 19960927 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 1088 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 90SW 22905 DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER 17L CRACKED AT BS 1088. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996100300302 19961003 00302 NM 1996 10 3 SWAA961024 1 19960927 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 251 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 56SW 21721 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN DAMAGED AT BS 251, AT S24R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996100300303 19961003 00303 NM 1996 10 3 SWAA961025 1 19960927 A 5320 GUIDE PLATE BOEING 737 7372H4 138448C NM AFT ENTRY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 24SW 20925 DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR FRAME UPPER HINGE GUIDE PLATE CRACKED BETWEEN FASTENERS TO EDGE. REPLAC ED WEB PER BOEING SRM. 2 L 7 2 4F A16WE 1996100300304 19961003 00304 NM 1996 10 3 SWAA961026 1 19960928 A 3350 1000679 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 51SW 21448 DURING SCHEDULED SERVICE CHECK, FOUND RT AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED LIGHT ASSE MBLY PER BOEING M/M. 2 L 7 2 4F A16WE 1996100300305 19961003 00305 NM 1996 10 3 SCNA96267 1 19960925 A 3350 S106 BATTERY BOEING 727 7272A1 138407F NM AIRSTAIR DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 286SC 21601 FOUND AFT AIRSTAIR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERIES AND OPS CHECKED GOOD. 2 L 7 3 4F A3WE 1996100300306 19961003 00306 WP 1996 10 3 DU4R9600040 1 19960930 A 5320 S2912293S ANGLE DOUG DC9 DC932 3022066 WP BS 996 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 949VV 47484 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND BS 996.0 BETWEEN LONGERON 28L - 27L IN AFT CARGO PIT FL OOR SUPPORT IS CORRODED. 2 L 7 2 4F A6WE 1996100300307 19961003 00307 WP 1996 10 3 DU4R9600001 1 19960930 A 5313 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 949VV 47484 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND PREVIOUS CORROSION GRIND-OUT ON T-CHORD OUT OF LIMITS D UE TO CORROSION. 2 L 7 2 4F A6WE 1996100300308 19961003 00308 WP 1996 10 3 DU4R9600002 1 19960930 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 740 CRACKED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 949VV 47484 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND 2.50 INCH CRACK IN MAIN LANDING GEAR AREA LOWER KEEL SK IN AT STA 740 RBL-15. 2 L 7 2 4F A6WE 1996100300309 19961003 00309 WP 1996 10 3 DU4R9600003 1 19960930 A 5320 59124372 DOUBLER DOUG DC9 DC932 3022066 WP RT MLG CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 949VV 47484 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND RT LOWER MAIN LANDING GEAR SUPPORT DOUBLER BLEND-OUT BE YOND LIMITS. 2 L 7 2 4F A6WE 1996100300310 19961003 00310 WP 1996 10 3 DU4R9600004 1 19960930 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 917-935 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 949VV 47484 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND CORROSION ON INTERCOSTAL AT L-29R FS 917 - 935 INSIDE W EB AND OUTSIDE. 2 L 7 2 4F A6WE 1996100300311 19961003 00311 WP 1996 10 3 DU4R9600005 1 19960930 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 813 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 949VV 47484 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND CORROSION ON AFT SIDE OF FS 813 FRAME BETWEEN L-29L - 2 9R. 2 L 7 2 4F A6WE 1996100300312 19961003 00312 WP 1996 10 3 DU4R9600006 1 19960930 A 5414 SKIN DOUG DC9 DC932 3022066 WP LT PYLON DENTED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 949VV 47484 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND HI-REACH DAMAGE ABOVE AND AFT OF LEFT ENGINE PYLON. 2 L 7 2 4F A6WE 1996100300313 19961003 00313 WP 1996 10 3 DU4R9600007 1 19960930 A 5720 59124381 DOUBLER DOUG DC9 DC932 3022066 WP LT WING CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 949VV 47484 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND THE LT WING UPPER BEAVER TAIL DOUBLER PANEL HAS CORROSI ON THROUGHOUT PANEL. STRIPPING REQUIRED FOR FURTHER INSPECTION. 2 L 7 2 4F A6WE 1996100300314 19961003 00314 WP 1996 10 3 DU4R9600008 1 19960930 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 195-205 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 949VV 47484 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND CORROSION ON L-30 IN FORWARD E/E BAY BETWEEN STA 195 - 205. 2 L 7 2 4F A6WE 1996100300315 19961003 00315 WP 1996 10 3 DU4R9600009 1 19960930 A 5320 DOOR FRAME DOUG DC9 DC932 3022066 WP R 1 DOOR DENTED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 949VV 47484 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND GOUGES AND DENTS AT R-1 AFT DOOR FRAME. 2 L 7 2 4F A6WE 1996100300316 19961003 00316 WP 1996 10 3 DU4R9600010 1 19960930 A 5320 3915135 FITTING DOUG DC9 DC932 3022066 WP BS 750 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 949VV 47484 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND CORROSION AT S-28L END FITTING AT FS 750. 2 L 7 2 4F A6WE 1996100300317 19961003 00317 WP 1996 10 3 DU4R9600011 1 19960930 A 5313 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 949VV 47484 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND CORROSION AT L-29L, L-30L, AND 29R. 2 L 7 2 4F A6WE 1996100300318 19961003 00318 WP 1996 10 3 DU4R9600012 1 19960930 A 5320 59124382 DOUBLER DOUG DC9 DC932 3022066 WP RT MLG CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 949VV 47484 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND RT UPPER MLG SUPPORT DOUBLER HAS CORROSION BLEND-OUT BE YOND LIMITS. 2 L 7 2 4F A6WE 1996100300319 19961003 00319 WP 1996 10 3 DU4R9600013 1 19960930 A 5320 3915135506N FITTING DOUG DC9 DC932 3022066 WP BS 750 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 949VV 47484 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND CORROSION AT STRINGER 28R END FITTING AT BS 750 IN RT W /W. 2 L 7 2 4F A6WE 1996100300320 19961003 00320 WP 1996 10 3 DU4R9600014 1 19960930 A 5400 DOUBLER DOUG DC9 DC932 3022066 WP NR 1 ENG PYLON CRACKED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 949VV 47484 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND FINGERS DOUBLERS HAD NUMEROUS CRACKS AND CORROSION ON L T NR 1 ENGINE PYLON BOTTOM PANEL. 2 L 7 2 4F A6WE 1996100300321 19961003 00321 WP 1996 10 3 DU4R9600015 1 19960930 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 218 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 949VV 47484 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND CORROSION ON FORWARD CARGO INSIDE LONGERON CHANNEL 25L AT STA. 218. 2 L 7 2 4F A6WE 1996100300322 19961003 00322 WP 1996 10 3 DU4R9600016 1 19960930 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 225 DENTED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 949VV 47484 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND FORWARD CARGO LONGERON 27R DENTED IN UPPER FLANGE OF LO NGERON AT STA 225. 2 L 7 2 4F A6WE 1996100300323 19961003 00323 WP 1996 10 3 DU4R9600017 1 19960930 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 750 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 949VV 47484 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND CORROSION BEYOND LIMITS AT L-28L END FITTING AT BS 750 . FITTING ON L-28L CORRODED. 2 L 7 2 4F A6WE 1996100300324 19961003 00324 WP 1996 10 3 DU4R9600018 1 19960930 A 5720 FITTING DOUG DC9 DC932 3022066 WP LT FWD SPAR CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 949VV 47484 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND THE LT FORWARD SPAR TO TRAP FITTING SUPPORT (SKI FITTI NG) HAS CORROSION AROUND FASTENERS. 2 L 7 2 4F A6WE 1996100300325 19961003 00325 WP 1996 10 3 DU4R9600019 1 19960930 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 996 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 920VV 47262 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND AFT CARGO PIT, BS 996.0 APPROXIMATELY 10 INCHES BELOW F LOOR LEVEL ON AFT SIDE OF WEB TEE EXTRUSION, HORIZONTAL SUPPORT IS CRACKED. 2 L 7 2 4F A6WE 1996100300326 19961003 00326 WP 1996 10 3 DU4R9600020 1 19960930 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 920VV 47262 DURING REPETITIVE INSPECTION AT AERO CORP IN LAKE CITY, FL, OF AD 90-18-03, SB 5798 R8, FOUND THE RADIUS BETWEEN STR 13 AND 14R HAS CORROSION AND A CRACK INDICATION NOTED AT BOTTOM OF RADIUS. ALSO, CORROSION AND CRACKS NOTED BETWEEN STR 1 6 AND 17R. 2 L 7 2 4F A6WE 1996100300327 19961003 00327 WP 1996 10 3 DU4R9600021 1 19960930 A 5313 62756001 LONGERON DOUG DC9 DC932 3022066 WP BS 889-965 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 920VV 47262 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND AFT CARGO PIT BS 889.0 TO 965.0 LONGERON 30 IS CORRODED . 2 L 7 2 4F A6WE 1996100300328 19961003 00328 WP 1996 10 3 DU4R9600022 1 19960930 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 870 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 920VV 47262 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND AFT CARGO PIT BS 870.0 LONGERON 29R TO 29L FRAME IS COR RODED. 2 L 7 2 4F A6WE 1996100300329 19961003 00329 WP 1996 10 3 DU4R9600023 1 19960930 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 870 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 920VV 47262 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND AFT CARGO PIT BS 870.0 LONGERON 30 FRAME IS CORRODED. 2 L 7 2 4F A6WE 1996100300330 19961003 00330 WP 1996 10 3 DU4R9600024 1 19960930 A 5320 STIFFENER DOUG DC9 DC932 3022066 WP BS 996 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 920VV 47262 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND AFT CARGO PIT BS 996.0 LBL 28.0 VERTICAL STIFFENER (HAT SECTION) CORRODED. 2 L 7 2 4F A6WE 1996100300331 19961003 00331 WP 1996 10 3 DU4R9600025 1 19960930 A 5320 J0602289 DOOR JAMB DOUG DC9 DC932 3022066 WP CARGO COMPT CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 920VV 47262 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND AFT CARGO PIT DOOR JAMB AREA HAS SEVERAL AREAS OF CORRO SION. 2 L 7 2 4F A6WE 1996100300332 19961003 00332 WP 1996 10 3 DU4R9600026 1 19960930 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 803-860 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 920VV 47262 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND AFT CARGO PIT AREA BS 803.0 TO 860.0 LONGERON 30 SKIN U NDER LONGERON 30 IS CORRODED. 2 L 7 2 4F A6WE 1996100300333 19961003 00333 WP 1996 10 3 DU4R9600027 1 19960930 A 5320 5920303501N FITTING DOUG DC9 DC932 3022066 WP BS 794 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 920VV 47262 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND BS 794.0 LONGERON 30 END FITTING CORRODED AT AT END UND ER SPLICE. 2 L 7 2 4F A6WE 1996100300334 19961003 00334 WP 1996 10 3 DU4R9600028 1 19960930 A 5320 1287425 ANGLE DOUG DC9 DC932 3022066 WP BS 996 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 920VV 47262 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND BS 996.0 LBL 39.0 AFT CARGO PIT VERTICAL STIFFENER CORR ODED AT BOTTOM. 2 L 7 2 4F A6WE 1996100300335 19961003 00335 WP 1996 10 3 DU4R9600029 1 19960930 A 5320 49149571 FITTING DOUG DC9 DC932 3022066 WP BS 945-996 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 920VV 47262 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND AFT CARGO PIT BS 945.0 TO 996.0 LONGERON 20R. LONGERON IS CORRODED; ALSO, END FITTING IS CORRODED. 2 L 7 2 4F A6WE 1996100300336 19961003 00336 WP 1996 10 3 DU4R9600030 1 19960930 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 996 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 920VV 47262 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND AFT CARGO PIT BS 996.0 ABOVE LONGERON 23R VERTICAL STIF FENER IS CORRODED. 2 L 7 2 4F A6WE 1996100300337 19961003 00337 WP 1996 10 3 DU4R9600031 1 19960930 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 965 CRACKED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 920VV 47262 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND AFT CARGO PIT BS 965.0 FLOOR BEAM IS CRACKED. 2 L 7 2 4F A6WE 1996100300338 19961003 00338 WP 1996 10 3 DU4R9600032 1 19960930 A 5312 2926943505 BULKHEAD DOUG DC9 DC932 3022066 WP BS 996 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 920VV 47262 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND AFT CARGO PIT BS 996.0 LONGERONS 26L - 24R AFT PRESSURE BULKHEAD HAS SEVERAL AREAS OF CORROSION AT BOTTOM END. 2 L 7 2 4F A6WE 1996100300339 19961003 00339 WP 1996 10 3 DU4R9600033 1 19960930 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 945 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 920VV 47262 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND BS 945.0 LONGERON 28R AFT CARGO PIT FRAME IS CORRODED. 2 L 7 2 4F A6WE 1996100300340 19961003 00340 WP 1996 10 3 DU4R9600034 1 19960930 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 980 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 920VV 47262 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND AFT CARGO PIT BS 980.0 LONGERONS 22L - 20R FRAME IS COR RODED. 2 L 7 2 4F A6WE 1996100300341 19961003 00341 WP 1996 10 3 DU4R9600035 1 19960930 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP BS 965 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 920VV 47262 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND AFT CARGO PIT BS 965.0 RBL 40 ABOVE LONGEORN 23R FORMED DOUBLER ATTACHING VERTICAL STRUT TO FRAME AT BS 965 IS CORRODED. 2 L 7 2 4F A6WE 1996100300342 19961003 00342 WP 1996 10 3 DU4R9600036 1 19960930 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP BS 945 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 920VV 47262 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND AFT CARGO PIT BS 945.0 LONGERON 29R AREA HAS EXISTING R EPAIR CORRODED. 2 L 7 2 4F A6WE 1996100300343 19961003 00343 WP 1996 10 3 DU4R9600037 1 19960930 A 5313 39146541 LONGERON DOUG DC9 DC932 3022066 WP BS 945-996 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 920VV 47262 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND AFT CARGO PIT BS 945.0 TO 996.0 LONGERON 22R CORRODED. 2 L 7 2 4F A6WE 1996100300344 19961003 00344 WP 1996 10 3 DU4R9600038 1 19960930 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 945-996 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 920VV 47262 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND BS 945.10 TO 996.0 LONGERON 21R IN AFT CARGO PIT IS COR RODED. 2 L 7 2 4F A6WE 1996100300345 19961003 00345 WP 1996 10 3 DU4R9600039 1 19960930 A 5320 3914590 END CAPS DOUG DC9 DC932 3022066 WP AFT CARGO PIT CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 920VV 47262 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND AFT CARGO PIT BS 996.0 LONGERONS 29R, 30, 29L, 28L, 27L , 26L, 25L AND 24L LONGERON END CAPS CORRODED. 2 L 7 2 4F A6WE 1996100300346 19961003 00346 WP 1996 10 3 DU4R9600041 1 19960930 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 996 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 920VV 47262 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND BS 996.0 AT CARGO PIT FRAME HAS 8 EACH VERTICAL STIFFEN ERS ON AFT SIDE OF WEB CORRODED. 2 L 7 2 4F A6WE 1996100300347 19961003 00347 WP 1996 10 3 DU4R9600042 1 19960930 A 5315 1666744 FLOOR BEAM DOUG DC9 DC932 3022066 WP BS 980 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 920VV 47262 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND BS 980.0 RBL 28 WL 208.0 AT CARGO PIT FLOOR BEAM SUPPOR T CORRODED. 2 L 7 2 4F A6WE 1996100300348 19961003 00348 WP 1996 10 3 DU4R9600043 1 19960930 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 945 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 920VV 47262 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND BS 945.0 TO 996.0 LONGERON 23R FLOOR SUPPORT CORRODED. 2 L 7 2 4F A6WE 1996100300349 19961003 00349 WP 1996 10 3 DU4R9600044 1 19960930 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP BS 965 NON APPROVED A VJ6A K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 11 920VV 47262 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND BS 965.0 BETWEEN LONGERONS 30 - 20L AREA HAS A NON-APPR OVED REPAIR. 2 L 7 2 4F A6WE 1996100300350 19961003 00350 WP 1996 10 3 DU4R9600045 1 19960930 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 965-980 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 920VV 47262 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND BS 965.0 TO 980 APPROX AFT CARGO PIT LONGERON 28R CORRO DED. 2 L 7 2 4F A6WE 1996100300351 19961003 00351 WP 1996 10 3 DU4R9600046 1 19960930 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 200-237 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 920VV 47262 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND BS 200.0 TO 237.0 LBL 20.0 FLOOR BEAM SUPPORT CORRODED BEYOND LIMITS. 2 L 7 2 4F A6WE 1996100300352 19961003 00352 WP 1996 10 3 DU4R9600047 1 19960930 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 996 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 920VV 47262 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND BS 996.0 LONGERONS 21L - 21R AFT CARGO PIT AREA FRAME A ND AFT WALL CORRODED ALONG FLOOR PANEL SUPPORTS AND RT AFT WALL. 2 L 7 2 4F A6WE 1996100300353 19961003 00353 WP 1996 10 3 DU4R9600048 1 19960930 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 917 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 920VV 47262 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND AFT CARGO PIT BS 917.0 BETWEEN LONGEONS 29R AND 29L FRA ME IS CORRODED FORWARD AFT, UPPER AND LOWER SURFACES. 2 L 7 2 4F A6WE 1996100300354 19961003 00354 WP 1996 10 3 DU4R9600049 1 19960930 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 397 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 920VV 47262 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND CABIN SEAT TRACK INBOARD LT SIDE BS 397.0 CORRODED BEYO ND LIMITS. 2 L 7 2 4F A6WE 1996100300355 19961003 00355 WP 1996 10 3 DU4R9600050 1 19960930 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 996 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 920VV 47262 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND BS 996.0 RBL-28 VERTICAL SUPPORT ON AFT SIDE OF WEB COR RODED BOTTOM END. 2 L 7 2 4F A6WE 1996100300356 19961003 00356 SW 1996 10 3 MALA965122 1 19960913 A 2752 ACTUATOR MOUNT SWRNGN SA227 SA227AC 8780603 SW RT TE FLAP ELONGATED HOLES A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428MA AC646 MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND RIGHT FLAP ACTUATOR LINK UPPER SUPPORTING MOUNT HOLES ELONGATED. REPAIRED FLAP ACTUATOR UPPER SUPPORTING MOUNT HOLES BY REAMING HOLES AND INSTALLING INTERFERENCE FIT BUSHINGS IAW AERO TECH DESIGNS EA 01-96081. (X) 2 L 7 2 4T RT A8SW 1996100300357 19961003 00357 1996 10 3 MALA965129 4 19960912 A 3442 071131900 RT UNIT DHAV DHC8 DHC8102 2809003 NM RADOME FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 826MA 330 FLT 3178 - IN CRUISE FLIGHT, THE WEATHER RADAR WOULD INTERMITTENTLY SPIKE AND PAINT THE GROUND ON THE LEFT SIDE OF THE D ISPLAY. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE WEATHER RADAR R/T. ALL CHECKS SATISFACTORY. (X) 2 H 7 2 4T RT A13NM 1996100300358 19961003 00358 SW 1996 10 3 MALA965128 1 19960913 A 5412 FIREWALL SWRNGN SA227 SA227AC 8780603 SW RT NACELLE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428MA AC646 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND 0.500 INCH TRANSVERSE CRACK IN RT FIREWALL. APPROXIMATE LOCATIO N IS BL 6.00 AND WL 91.00. STOP DRILLED CRACK, FABRICATED AND INSTALLED A 0.020 INCH STAINLESS REPAIR DOUBLER (3.50 INC H BY 1.20 INCH) IAW FAIRCHILD SRM 54-90-10, PAGES 43-45, REV. AUG 16, 1993. (X) 2 L 7 2 4T RT A8SW 1996100300359 19961003 00359 SW 1996 10 3 MALA965127 1 19960913 A 5230 27240082003 CORNER SWRNGN SA227 SA227AC 8780603 SW CARGO DOOR CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428MA AC646 MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND LOWER AFT CORNER OF CARGO DOOR FRAME DAMAGED. REMOVED LOWER AFT CARGO DOOR CORNER, PN 27-240082-003, AND INSTALLED NEW CORNER IAW FAIRCHILD SRM 51-00-00, PAGE 4 AND SEALED IAW FAIRCHIL D SRM 51-30-03. (X) 2 L 7 2 4T RT A8SW 1996100300360 19961003 00360 SW 1996 10 3 MALA965125 1 19960913 A 2720 2742051037 TORQUE TUBE SWRNGN SA227 SA227AC 8780603 SW RUDDER CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428MA AC646 MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND RUDDER TORQUE TUBE CHAFED AT PRESSURE SEAL MOUNT AREA. REMOVED R UDDER TORQUE TUBE, PN 27-42051-037, AND INSTALLED NEW TORQUE TUBE IAW FAIRCHILD MM 27-20-20, PAGES 201-202. (X) 2 L 7 2 4T RT A8SW 1996100300361 19961003 00361 SW 1996 10 3 MALA965124 1 19960913 A 5712 2731523 RIB SWRNGN SA227 SA227AC 8780603 SW WS 27.03 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428MA AC646 MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND AT WS 27.03 RT AFT WING RIB TRAILING EDGE (PN 27-31523), A 0.375 INCH CRACK. COMPLETED REPAIR PER FAC SRM 57-90-10, PAGES 3-6, REV. NOVEMBER 1, 1994, BY FABRICATING AND INSTALLING A 0. 050 INCH BY 4.00 INCH BY 2.50 INCH REPAIR DOUBLER TO AFFECTED AREA. (X) 2 L 7 2 4T RT A8SW 1996100300362 19961003 00362 SW 1996 10 3 MALA965123 1 19960913 A 5330 SKIN SWRNGN SA227 SA227AC 8780603 SW BS 241 CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428MA AC646 MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND CHAFE DAMAGE AT FS 241.00 AND ON BOTH SIDES OF BL 0.00. CHAFE DA MAGE IS APPROXIMATELY 0.025 INCH DEEP. (SUSTAINED DAMAGE ON RT SIDE WAS TO A FASTENER, AND ON LT SIDE, DAMAGE WAS TO FU SELAGE SKIN). REMOVED AND REPLACED AFFECTED FASTENER ON RT SIDE OF BL 0.00. FABRICATED AND INSTALLED AN EXTERNAL REPAI R DOUBLER (0.040 INCH BY 2.50 INCH BY 2.50 INCH) IAW AEROTECH DESIGNS EA01-96086, DATED 9-6-96. (X) 2 L 7 2 4T RT A8SW 1996100300363 19961003 00363 SW 1996 10 3 MALA965121 1 19960913 A 5400 ANGLE SWRNGN SA227 SA227AC 8780603 SW WING/NACELLE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428MA AC646 MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND REPAIR ANGLE ON LEFT NACELLE INBOARD LOWER 'WING TO NACELLE' ATTA CH ANGLE CRACKED. REMOVED PREVIOUS REPAIR ANGLE, FABRICATED AND INSTALLED NEW REPAIR ANGLE IAW ARP 54-20-9101, REV. B. (X) 2 L 7 2 4T RT A8SW 1996100300364 19961003 00364 SW 1996 10 3 MALA965120 1 19960913 A 5320 INTERCOSTAL SWRNGN SA227 SA227AC 8780603 SW FUSELAGE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428MA AC646 MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND LOWER LT BELT FRAME INTERCOSTAL CRACKED IN TWO LOCATIONS AT CORNE R RELIEF RADIUS CUT-OUTS. ONE CRACK IS 0.250 INCH AND THE OTHER IS 0.400 INCH. FABRICATED AND INSTALLED REPAIR DOUBLER IAW AEROTECH DESIGNS EA01-96087, DATED 9-10-96. (X) 2 L 7 2 4T RT A8SW 1996100300365 19961003 00365 SW 1996 10 3 MALA965119 1 19960913 A 5210 SKIN SWRNGN SA227 SA227AC 8780603 SW PASSENGER DOOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428MA AC646 MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE UPPER PASSENGER DOOR HINGE TO SKIN FASTENERS (ON PASSENGER DO OR) 'WORKING' AND CHAFING SKIN. REMOVED AFFECTED SKIN, FABRICATED AND INSTALLED A 10.50 INCH REPAIR SKIN SPLICE ONTO UP PER PASSENGER DOOR HINGE AREA IAW FAIRCHILD SRM 52-90-10, PAGE 12, REV. APRIL 15, 1992. (X) 2 L 7 2 4T RT A8SW 1996100300366 19961003 00366 NM 1996 10 3 MALA965134 1 19960913 A 3350 6038443 LIGHTS DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 852MA 349 FLT 3059 - DURING THE PRE-FLIGHT INSPECTION IN DTW, THE FORWARD MOST CLUSTER OF FLOOR TRACK LIGHTS WERE FOUND INOPERATIV E. MAINTENANCE REPLACED BATTERY POWER SUPPLY. ALL CHECKS SATISFACORY. (X) 2 H 7 2 4T RT A13NM 1996100300367 19961003 00367 NM 1996 10 3 MALA965132 1 19960914 A 5347 85330217001 FLOOR TRACK DHAV DHC8 DHC8102 2809003 NM CARGO COMPT CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 861MA 362 MSP - DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE AFT CARGO FLOOR TRACK RAIL TO HAVE CORROSION. REPAIRS WERE COMPLETED BY REPLACING THE RAIL ASSEMBLY, PN 85330217-001. (X) 2 H 7 2 4T RT A13NM 1996100300368 19961003 00368 NM 1996 10 3 MALA965130 1 19960912 A 5347 85320490125 SEAT TRACKS DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 861MA 362 INT - DURING A SCHEDULED INSPECTION, THE LEFT AND RIGHT CABIN INBOARD SEAT RAILS WERE FOUND PITTED BETWEEN FS 210 AND FS 220. REPAIRS WERE COMPLETED BY REPLACING THE DEFECTIVE SECTIONS. REFERENCE: OPERATOR CONTROL NR 96ZZZX4922. (X) 2 H 7 2 4T RT A13NM 1996100300369 19961003 00369 NM 1996 10 3 96ZZZX4922 1 19960912 A 5347 85320490127 SEAT TRACKS DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 861MA 362 INT - DURING A SCHEDULED INSPECTION, THE LEFT AND RIGHT CABIN INBOARD SEAT RAILS WERE FOUND PITTED BETWEEN FS 210 AND FS 220. REPAIRS WERE COMPLETED BY REPLACING THE DEFECTIVE SECTIONS. REFERENCE: OPERATOR CONTROL NR MALA965130. 2 H 7 2 4T RT A13NM 1996100300370 19961003 00370 SW 1996 10 3 MALA965126 1 19960913 A 5330 SKIN SWRNGN SA227 SA227AC 8780603 SW BS 159.24 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428MA AC646 MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND FUSELAGE SKIN AT FS 159.24 AND WL 75.13 CRACKED TRANSVERSELY. CR ACK LENGTH APPROXIMATELY 0.450 INCH. FABRICATED AND INSTALLED A 0.032 INCH BY 4.00 INCH BY 4.00 INCH SURFACE REPAIR DOU BLER TO AFFECTED AREA IAW FAIRCHILD SRM 51-90-04, PAGES 7-8, REV. 6-1-93. (X) 2 L 7 2 4T RT A8SW 1996100300371 19961003 00371 NM 1996 10 3 MALA965131 1 19960913 A 3260 ADVISORY LIGHT DHAV DHC8 DHC8102 2809003 NM LT MLG MALFUNCTIONED A MALA O OTHER N FALSE WARNING CR CRUISE 1 GL 15 826MA 330 FLT 3072 - IN CRUISE FLIGHT WITH GEAR UP, THE LEFT LANDING GEAR ADVISORY LIGHT (AMBER) WOULD FLICKER ON AND OFF. THE LI GHT WOULD EXTINGUISH WITH THE GEAR LOWERED WHILE ON APPROACH TO DTW. MAINTENANCE PERFORMED TROUBLESHOOTING, BUT WERE UN ABLE TO DUPLICATE THE DISCREPANCY. (X) 2 H 7 2 4T RT A13NM 1996100300372 19961003 00372 NM 1996 10 3 MALA965133 1 19960914 A 3260 82400033057 PROX SENSOR DHAV DHC8 DHC8102 2809003 NM LT MLG OUT OF ADJUST A MALA O OTHER N FALSE WARNING CR CRUISE 1 GL 15 826MA 330 FLT 2926 - IN CRUISE FLIGHT, THE LEFT LANDING GEAR DOOR ADVISORY LIGHT INTERMITTENTLY ILLUMINATES. MAINTENANCE ADJUSTED THE AFT GEAR DOOR PROXIMITY SENSOR. ALL CHECKS SATISFATORY. (X) 2 H 7 2 4T RT A13NM 1996100300373 19961003 00373 EU 1996 10 3 SIMA962621 1 19960918 A 3397 33512216 WIRE AEROSP ATR72 ATR72212 8680945 EU CABIN BROKEN A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 270AT 270 ICT - PERIODIC SERVICE INSPECTION REVEALED EMERGENCY LIGHT ON PASSENGER DOOR INOPERATIVE. FOUND BROKEN WIRE, NR 3351221 6. REPAIRED WIRE, OPS CHECK SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1996100300374 19961003 00374 WP 1996 10 3 HAL96134 1 19960916 A 4990 APU DOUG DC10 DC1010 3022110 WP APU COMPT OIL LEAK A HALA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 13 151AA 46706 HNL - FLT 022 - SMELLS LIKE APU OIL IS IN AIR PACKS. STRONGEST SMELL IN COCKPIT AND GALLEY WITH NR 1 PACK ON. WITH NR 1 PACK OFF, SMELL IS STILL EVIDENT IN COCKPIT AND CABIN WITH NR 2, NR 3, PACKS ON. AFTER ENGINE RUN DETERMINED SOURCE I S COMING FROM APU, ACCOMPLISHED AIR CONDITIONING DUCT PURGING PER MM 36-10-00. GROUND OPERATION CHECKED GOOD. (X) 2 L 7 3 4F A22WE 1996100300375 19961003 00375 NM 1996 10 3 96ZZZX4923 1 19960904 A 5610 1A561D006002 WINDSHIELD SIERRACIN DORNER DO32 DO328100 2996000 NM RT COCKPIT CRACKED A EQGA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 19 350AD 1913 372 3050 AIRCRAFT WAS EN ROUTE TO CUU WHEN THE FIRST OFFICER NOTICED A 6 INCH CRACK IN THE FORWARD, UPPER PORTION OF THE SIDE WIN DSHIELD. THE CREW RETURNED TO DFW WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS FERRIED TO HOT WHERE THE WINDSHIELD WAS R EPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A45NM 1996100300377 19961003 00377 WP 1996 10 3 CALA9601343 1 19960909 A 5311 995823879 BELT FRAME DOUG DC9 DC982 3022082 WP STA 1322 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35888 49117 INSPECTION FOUND BELT FRAME CORRODED ON RT SIDE AT STA 1322. A BELT FRAME WAS INSTALLED IAW SRM 53-03. 2 L 7 2 4F A6WE 1996100300378 19961003 00378 WP 1996 10 3 CALA9601344 1 19960907 A 5311 SR0953008683 FRAME DOUG DC9 DC982 3022082 WP STA 1446 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35888 49117 INSPECTION FOUND CANTED FRAME STA 1446 CRACKED OUT WHERE LONGERONS 4R AND 5R ATTACH. THE UPPER CANTED CAP FRAME WAS REP LACED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1996100300379 19961003 00379 WP 1996 10 3 CALA9601345 1 19960907 A 5311 SR0953008683 FRAME DOUG DC9 DC982 3022082 WP STA 1446 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35888 49117 INSPECTION FOUND CANTED FRAME STA 1446 CRACKED OUT WHERE LONGERONS 3L, 4L AND 5L ATTACH. THE UPPER CANTED CAP FRAME WAS REPLACED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1996100300380 19961003 00380 WP 1996 10 3 CALA9601346 1 19960926 A 5330 SKIN DOUG DC9 DC932 3022066 WP STA 756 CRACK/CORR A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 27522 47524 INSPECTION FOUND A 1 INCH CRACK AND CORROSION IN AIRCRAFT BELLY SKIN APPROXIMATELY 17 FORWARD OF LOWER BEACON AND 7 RIGH T OF CENTER STA 756 LONGERON 29R. THE AREA WAS REPAIRED IAW ECRA 5330-02442 AND SRM 53-04, FIGURE 12B SHEET 1 AND 10. 2 L 7 2 4F A6WE 1996100300381 19961003 00381 NM 1996 10 3 CALA9601347 1 19960918 A 5313 STRINGER BOEING 737 737214 138446R NM STA 295 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14239 19920 INSPECTION FOUND A .75 INCH CRACK IN STRINGER 12L AT STA 295. THE STRINGER WAS REPAIRED IAW SRM 53-10-2. 2 L 7 2 4F A16WE 1996100300382 19961003 00382 NM 1996 10 3 CALA9601348 1 19960918 A 5313 STRINGER BOEING 737 737214 138446R NM CTR WING BOX CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14239 19920 INSPECTION FOUND A .75 INCH CRACK AT RT OUTBOARD END OF CENTER WING BOX UPPER STRINGER NR 3. THE CRACKED SECTION OF STR INGER WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-10-4, FIGURE 4 FIGURE 8 AND SRM 57-10-2. 2 L 7 2 4F A16WE 1996100300383 19961003 00383 NM 1996 10 3 CALA9601349 1 19960918 A 5313 STRINGER BOEING 737 737214 138446R NM F.S. 837 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14239 19920 INSPECTION FOUND A 1.125 INCH CRACK IN STRINGER 17R BELOW CABIN FLOOR AT FS 837. REPAIR DOUBLERS WERE FABRICATED AND IN STALLED IAW SRM 51-40-4, 51-10-2 AND 51-30-2. 2 L 7 2 4F A16WE 1996100300384 19961003 00384 NM 1996 10 3 CALA9601350 1 19960918 A 5320 BEAM BOEING 737 737214 138446R NM STA 685 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14239 19920 INSPECTION FOUND A 3 INCH CRACK IN RADIUS OF TRANSVERSE BEAM AT STA 685. THE CRACK WAS STOP DRILLED, REPAIR ANGLES AND RADIUS FILLERS WERE FABRICATED AND INSTALLED IAW SRM 51-10-1 AND BAC DRAWING NR 65C17103. 2 L 7 2 4F A16WE 1996100300385 19961003 00385 NM 1996 10 3 CALA9601351 1 19960918 A 5312 BULKHEAD BOEING 737 737214 138446R NM STA 178 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14239 19920 INSPECTION FOUND A 3.25 CRACK IN R/H SIDE OF PRESSURE BULKHEAD AT STA 178. THE BULKHEAD WAS REPAIRED IAW SRM 53-10-11 AN D 53-10-2. 2 L 7 2 4F A16WE 1996100300386 19961003 00386 NM 1996 10 3 CALA9601352 1 19960918 A 5315 FLOORBEAM BOEING 737 737214 138446R NM STA 360 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14239 19920 INSPECTION FOUND FLOORBEAM CORRODED BETWEEN SEAT TRACK ROW D AND CUSP LINE AT STA 360. A NEW FLOORBEAM WAS FABRICATED A ND INSTALLED IAW SRM 53-10-9, 51-10-2 AND 51-30-3. 2 L 7 2 4F A16WE 1996100300387 19961003 00387 NM 1996 10 3 CALA9601353 1 19960918 A 5330 SKIN BOEING 737 737214 138446R NM B.S. 890 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14239 19920 INSPECTION FOUND A 3 BY 5 INCH AREA OF FUSELAGE SKIN DENTED AT BS 890, LT SIDE, TOP OF WINDOW BELT. THE DENTED AREA WAS CUT OUT, DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-2, 51-10-2 AND SRM 51-30-2. 2 L 7 2 4F A16WE 1996100300388 19961003 00388 NM 1996 10 3 CALA9601354 1 19960918 A 5713 STRINGER BOEING 737 737214 138446R NM W.S. 6R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14239 19920 INSPECTION FOUND A 1.25 INCH CRACK IN WING SUPPORT STRINGER AT RIGHT WBL 70.85, WS 6. THE CRACKED SECTION OF STRINGER W AS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-10-4, FIGURE 8 AND SRM 57-10-2. 2 L 7 2 4F A16WE 1996100300389 19961003 00389 NM 1996 10 3 CALA9601355 1 19960918 A 5330 SKIN BOEING 737 737214 138446R NM AFT LAV CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14239 19920 INSPECTION FOUND SKIN BULGED/CORRODED WITH POPPED FASTENERS AT FORWARD INBOARD CORNER OF AFT LAV DUMP CHUTE DOOR CUTOUT. THE CORRODED AREA OF SKIN WAS REMOVED IAW SRM 53-30-3. SKIN FILLER, DOUBLER AND SHIMS WERE FABRICATED IAW SRM 53-30-2 . STRINGER 26R WAS REMOVED AND A NEW STRINGER WAS DRILLED IAW SRM 51-30-2. THE REPAIR WAS INSTALLED IAW SRM 51-30. 2 L 7 2 4F A16WE 1996100300390 19961003 00390 NM 1996 10 3 CALA9601356 1 19960918 A 5315 FLOORBEAM BOEING 737 737214 138446R NM STA 986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14239 19920 INSPECTION FOUND FLOORBEAM AND SUPPORT CORRODED AT AFT CABIN L-2 DOOR THRESHOLD, STA 986. A REPAIR WAS FABRICATED AND I NSTALLED IAW SRM 53-10-9, 51-10-2 AND 51-30-2. 2 L 7 2 4F A16WE 1996100300391 19961003 00391 NM 1996 10 3 CALA9601357 1 19960918 A 5320 STIFFENER BOEING 737 737214 138446R NM F.S. 295 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14239 19920 INSPECTION FOUND A .5 INCH CRACK IN STIFFENER BETWEEN STRINGER 10L AND 11L AT FS 295. THE CRACKED SECTION OF STIFFENER WAS REMOVED AND A NEW SECTION WAS FABRICATED AND INSTALLED IAW SRM 53-10-3 AND 51-10-2. 2 L 7 2 4F A16WE 1996100300392 19961003 00392 NM 1996 10 3 CALA9601358 1 19960918 A 5320 ANGLE BOEING 737 737214 138446R NM STA 540 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14239 19920 INSPECTION FOUND A .5 INCH CRACK THROUGH RADIUS OF RT WING ROOT FORWARD FILLET PANEL SUPPORT ANGLE. THE CRACK WAS LOCAT ED AT STA 540, 10 INCHES BELOW LOWER CAP OF FORWARD SPAR ADJACENT TO FORWARD END OF HINGED RAM AIR DUCT ACCESS PANEL. T HE ANGLE WAS REPAIRED IAW ECRA 5350-01227. 2 L 7 2 4F A16WE 1996100300393 19961003 00393 NM 1996 10 3 CALA9601359 1 19960918 A 5320 CHORD ANGLE BOEING 737 737214 138446R NM STA 673 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14239 19920 INSPECTION FOUND A 3.25 INCH CRACK IN MAIN CABIN FLOORBEAM LOWER CHORD ANGLE AT STA 673, BL 0. THE AREA WAS REPAIRED IA W BOEING DRAWING 65-45410, CAL ENGINEERING ORDER 031-5710-01322, SRM 51-40-4 AND 51-30-2. 2 L 7 2 4F A16WE 1996100300394 19961003 00394 NM 1996 10 3 CALA9601360 1 19960918 A 5315 FLOORBEAM BOEING 737 737214 138446R NM STA 684 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14239 19920 INSPECTION FOUND A 2 INCH CRACK IN FLOORBEAM AT STA 684, RBL 24.8. THE FLOORBEAM WAS REPAIRED IAW EA 5710-01638 AND SRM 51-40-4. 2 L 7 2 4F A16WE 1996100300395 19961003 00395 NM 1996 10 3 CALA9601361 1 19960918 A 5311 FRAME BOEING 737 737214 138446R NM STA 947 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14239 19920 INSPECTION FOUND A 2.5 INCH CRACK IN FRAME AT STA 947, STRINGER 18R. THE FRAME WAS REPAIRED IAWS SRM 53-10-2, 53-10-4, 51-10-7, 51-10-2 AND 51-30-2. 2 L 7 2 4F A16WE 1996100300396 19961003 00396 NM 1996 10 3 CALA9601362 1 19960918 A 5314 FLANGE BOEING 737 737214 138446R NM BS 663-727 GALLED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14239 19920 INSPECTION FOUND RT KEEL BEAM FAYING FLANGE FROM BS 663 TO BS 727 GALLED ON LOWER SURFACE AND WORN AROUND FASTENER HOLES ON UPPER SURFACE. A REPAIR STRAP WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2 AND ECRA 5310-03324. 2 L 7 2 4F A16WE 1996100300397 19961003 00397 EU 1996 10 3 09620753249 1 19960927 A 3260 848401 SENSOR AIRBUS 320 A320211 3930320 EU LANDING GEAR MALFUNCTION A NWAA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 GL 01 349NW 417 AFTER TAKEOFF, LANDING GEAR DOOR OPEN WAS INDICATED. CREW RETURNED AIRCRAFT TO DEPARTURE AIRPORT. GROUND MAINTENANCE R EPLACED GEAR DOOR PROXIMITY SWITCH. 2 L 7 2 4F RT A28NM 1996100300398 19961003 00398 WP 1996 10 3 9620769753 1 19960929 A 3350 LIGHT DOUG DC9 DC941 302207N WP INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 753NW 47117 DURING LINE CHECK, FOUND EMERGENCY LIGHT AT FORWARD LEFT OVERWING EXIT INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHE CK GOOD. 2 L 7 2 4F A6WE 1996100300399 19961003 00399 WP 1996 10 3 9620779605 1 19960927 A 3260 DOWNLOCK SWITCH DOUG DC9 DC932 3022066 WP MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 605NW 47223 DURING CLIMBOUT ON GEAR RETRACTION, GOT LEFT GEAR UNSAFE LIGHT. RECYCLED GEAR AND RETURNED TO SLC. AIRCRAFT LANDED WIT HOUT INCIDENT. REPLACED LEFT DOWNLOCK SWITCH, CHECKED WIRING AND UPLOCK SWITCH, RAN GEAR SEVERAL TIMES AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996100300400 19961003 00400 NM 1996 10 3 9620786302 1 19960929 A 3350 LIGHTS BOEING 747 747451 1384940 NM INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 662US 23720 DURING LINE CHECK, FOUND EMERGENCY FLOOR PATH LIGTHS INOPERATIVE FROM ROWS 36R TO 43R. REPAIRED PLUG, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1996100300401 19961003 00401 NM 1996 10 3 9620796634 1 19960928 A 3350 LIGHT BOEING 747 747227B 1384888 NM INOP A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 634US 22234 DURING LINE CHECK, FOUND 'E' ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS, OPERATIONA L CHECK GOOD. 2 L 7 4 4F A20WE 1996100300402 19961003 00402 NM 1996 10 3 9620802769 1 19960929 A 2530 OVEN BOEING 727 7272M7 138407S NM SMOKING A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 729RW 21742 DURING CLIMB, FLIGHT ATTENDANT REPORTED SMOKE COMING FROM AFT GALLEY OVENS. AIRCRAFT RETURNED TO MCO AND LANDED WITHOUT INCIDENT. REPLACED AFT GALLEY FORWARD OVENS. FAN AND HEATER ELEMENT GUARDS MISSING, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996100300403 19961003 00403 NM 1996 10 3 96FDEA01553 1 19960930 A 5754 65162261 BONDING JUMPER BOEING 727 72725 1384006 NM NR 2 LE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 511FE 18283 NR0589 AND 010, WHILE WORKING NR0218 FOUND NR 2 K-FLAP I/B BULLNOSE BONDING JUMPER UPPER ATTACH POINT CORRODED. *S/D* R EPAIRED PER FEDEX SRM 57-50-3. 2 L 7 3 4F A3WE 1996100300404 19961003 00404 NM 1996 10 3 96FDEA01554 1 19960930 A 3230 NOSE GEAR BOEING 727 72722 1384002 NM NLG MALFUNCTION A FDEA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 101FE 19197 WHEN LANDING GEARS WERE EXTENDED ON APPROACH, THE MAINS EXTENDED GREEN, BUT THE NOSE GEAR LIGHT REMAINED AMBER. NO NOSE GEAR DOOR LIGHT ON SECOND OFFICER'S PANEL. CYCLED GEAR AND ALL GEAR EXTENDED NORMALLY. PERFORMED NOSE GEAR EXTENSION AND RETRACTION TEST PER MM 32-33-0 P 501 AND 502. CYCLED 10 TO 12 TIMES WITH NO INDICATIOIN PROBLEMS. 2 L 7 3 4F A3WE 1996100300405 19961003 00405 NM 1996 10 3 DL76S962128 1 19960918 A 2530 OVEN 828450407 BOEING 767 767332 1382001 NM FWD GALLEY SMOKING A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 138DL 25409 BOTTOM OVEN IN F/C GALLEY PRODUCING SMOKE. PULLED AND COLLARED OVEN CIRCUIT BREAKER. FORWARD ITEM TO MCO. REPLACED OV EN. 2 L 7 2 4F RT A1NM 1996100300406 19961003 00406 NM 1996 10 3 DL757962177 1 19960925 A 3350 LENS AND LIGHT BOEING 757 757232 1384965 NM CABIN MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 606DL 22813 LIGHT AND LENS MISSING ON EMERGENCY LIGHT TRACK AT ROWS 25 AND 39. 2 L 7 2 4F RT A2NM 1996100300407 19961003 00407 WP 1996 10 3 DLL10962178 1 19960925 A 2752 VANE ACTUATOR 1577937101 LKHEED 1011 10113851 5265010 WP RT I/B O/B TRACK FAILED A DALA O OTHER F FLT CONT AFFECTED LD LANDING 1 SO 27 722DA 193C1147 UPON ARRIVAL, MTC NOTICED RT I/B FLAP O/B FAIRING DAMAGE. RT I/B FLAP O/B ROD VANE ACTUATOR ASSY, WAS PROTRUDING THROUG H THE FLAP FAIRING. NEW ROD ACTUATOR AND ATTACHING PARTS WERE OBTAINED FROM TWA, EXCEPT FOR LOCKING BOLT, (P/N 0112281 42), REF IPC 27-51-33 FIG 1 PAGE 8 ITEM 290. SAFETY BOLT TO BE SHIPPED AOG ATL/LAX ON FIRST FLIGHT, 09/26/96. FLAP FAI RING REMOVED AND SENT TO ATL FRONT DESK, FAIRING DEFERRED PER CDL 57-54-00 DISPATCH APPROVAL OBTAINED. 2 L 7 3 4F A23WE 1996100300408 19961003 00408 NM 1996 10 3 DL72W962180 1 19960923 A 5241 65569923 FRAME BOEING 727 7272Q8 138407W NM L/H AFT SERVICE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831L 21826 FWD FRAME CRACKED AT UPPER HINGE. REPAIRED PER SRM 52-40-2 PG 15. 2 L 7 3 4F A3WE 1996100300409 19961003 00409 NM 1996 10 3 DL757962184 1 19960926 A 2530 COFFEE MAKER 811150417 BOEING 757 757232 1384965 NM AFT NBR 1 FAILED A DALA H DEACTIVATE SYST/CIRCUITS O OTHER CR CRUISE 1 SO 27 619DL 0915 22909 AFT GALLEY NR 1 COPILOTS SIDE COFFEE MAKER MAKES POPPING SOUND WITH SPARKS FLYING WHEN TURNED ON. CIRCUIT BREAKER DID N OT POP. REPLACED COFFEE MAKER. 2 L 7 2 4F RT A2NM 1996100300410 19961003 00410 NM 1996 10 3 DL76S962187 1 19960927 A 2910 130606100720J HOSE BOEING 767 767332 1382001 NM LT GEAR TRK ACT LEAKING A DALA A UNSCHED LANDING K FLUID LOSS TO TAKEOFF 1 SO 27 122DL 23436 AFTER T/O UPON GEAR RETRACTION, GOT GEAR DOOR MSG AND GEAR DISAGREE MSG ON EICAS. LT MAIN GEAR GREEN LIGHT REMAINED ILL UMINATED. FOUND UP PRESSURE LINE TO LT GEAR TRUCK POSITIONER ACTUATOR LEAKING. REPLACED SAME. 2 L 7 2 4F RT A1NM 1996100300411 19961003 00411 NM 1996 10 3 DL72K962196 1 19960920 A 5320 ANGLE BOEING 727 727232 1384082 NM R2 DOOR CUTOUT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 471DA 20748 FOUND DURING MV1 CHECK, .5 INCH CRACK AT R2 DOOR FWD FRAME UPPER HINGE CUTOUT LWR CORNER. REPAIRED PER SRM 52-40-2. 2 L 7 3 4F A3WE 1996100300412 19961003 00412 NM 1996 10 3 DL73E962197 1 19960927 A 3350 CHARGER 110049 BOEING 737 737247 138448D NM AFT CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 382DL 1985 23609 DURING L/O CHECK, FOUND EMERGENCY TRACK LIGHTING SECTION INOP FROM ROWS 10 TO 16. REPLACED AFT EMERGENCY LIGHT BATTERY CHARGER POWER SUPPLY, OPERATION CHECKS GOOD. 2 L 7 2 4F A16WE 1996100300434 19961003 00434 CE 1996 10 3 96ZZZX4945 1 19960901 A 5522 ELEVATOR BEECH 18 C45H 1151018 CE ELEVATOR LT FABRIC FAILED A A STZA A UNSCHED LANDING F D FLT CONT AFFECTED INFLIGHT SEPARATION NR NOT REPORTED 1 AL 03 400WA AF764 ELEVATOR FABRIC FAILED IN-FLIGHT CAUSING SEVERE CONTROL SURFACE FLUTTER. DAMAGE TO ELEVATOR ATTACH POINT HINGE. LEFT E LEVATOR TRIM ACTUATOR DEPARTED THE AIRCRAFT. FABRIC WAS VERY OLD AND HAD NUMEROUS REPAIRS. REMOVED ELEVATOR AND REPLAC ED WITH METALLIZED ELEVATOR PER HAMILTON AVIATION CO. STC NR SA2815 WE. TAT: 15,998.5 HOURS. 1 L 7 2 3R A765 1996100300448 19961003 00448 NM 1996 10 3 96ZZZM1374 1 19960822 A 2820 MS29513028 O-RING BOEING 737 7373B7 1384580 NM CTR FUEL TANK LEAKING A USAA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 505AU 23380 CLT - FLT 278 - CREW REPORTED A STRONG FUEL ODOR IN FORWARD CABIN WITH RECIRCULATION FAN ON, REGARDLESS OF PACK POSITION . WITH FAN OFF, ODOR DISSIPATED. MAINTENANCE FOUND CENTER TANK AFT FITTING (FROM AUX TANK) LEAKING. REPLACED O-RINGS AT CENTER TANK AFT FITTING. LEAK CHECK GOOD. REFERENCE USAASB96168. 2 L 7 2 4F RT A16WE 1996100300449 19961003 00449 NM 1996 10 3 96ZZZM1375 1 19960822 A 2820 MS29513222 O-RING BOEING 737 7373B7 1384580 NM CTR FUEL TANK LEAKING A USAA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 505AU 23380 CLT - FLT 278 - CREW REPORTED A STRONG FUEL ODOR IN FORWARD CABIN WITH RECIRCULATION FAN ON, REGARDLESS OF PACK POSITION . WITH FAN OFF, ODOR DISSIPATED. MAINTENANCE FOUND CENTER TANK AFT FITTING (FROM AUX TANK) LEAKING. REPLACED O-RINGS AT CENTER TANK AFT FITTING. LEAK CHECK GOOD. REFERENCE USAASB96168. 2 L 7 2 4F RT A16WE 1996100300450 19961003 00450 NM 1996 10 3 96ZZZM1376 1 19960822 A 2820 MS29513227 O-RING BOEING 737 7373B7 1384580 NM CTR FUEL TANK LEAKING A USAA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 505AU 23380 CLT - FLT 278 - CREW REPORTED A STRONG FUEL ODOR IN FORWARD CABIN WITH RECIRCULATION FAN ON, REGARDLESS OF PACK POSITION . WITH FAN OFF, ODOR DISSIPATED. MAINTENANCE FOUND CENTER TANK AFT FITTING (FROM AUX TANK) LEAKING. REPLACED O-RINGS AT CENTER TANK AFT FITTING. LEAK CHECK GOOD. REFERENCE USAASB96168. 2 L 7 2 4F RT A16WE 1996100300451 19961003 00451 NM 1996 10 3 96ZZZM1377 1 19960825 A 7933 1122514 OIL TEMP BULB BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU NR 1 ENGINE MALFUNCTIONED A USAA A UNSCHED LANDING M OVER TEMP CR CRUISE 1 EA 19 376US 22955 IND - FL 247 - FLIGHT DIVERTED TO IND DUE TO HIGH OIL TEMPERATURE READING ON THE NR 1 ENGINE. THE OIL TEMP WENT TO 140 DEGREES CELCIUS, THEN INTO RED BAND AND BACK TO YELLOW. WHEN THROTTLE WAS RETARDED, TEMP WAS IN THE HIGH GREEN BAND. N O EMERG WAS DECLARED AND THE FLT LANDED WITH NO FURTHER INCIDENT. THE NR 1 ENGINE WAS NOT SHUT DOWN. MAINTENANCE REPLA CED THE NR 1 ENGINE OIL/FUEL HEAT EXCHANGER AND THE OIL TEMP BULB PER THE MM. DRAINED AND REFILLED OIL TANK. RAN ENGIN E. OP CHECK AND LEAK CHECK GOOD. REFERENCE USAASB96170. 2 L 7 2 4F 4 F RT A16WE E21EU 1996100300452 19961003 00452 NM 1996 10 3 96ZZZM1378 1 19960904 A 3350 900835A BATTERY PACK BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 270AU 22882 PIT - FL 560 - ON PREFLIGHT COCKPIT CHECK, CREW REPORTED LOW LEVEL TRACK LIGHTING AND EMERGENCY LIGHTS INOP THROUGHOUT C ABIN. MAINTENANCE REPLACED THREE BATTERY PACKS IN THE FORWARD AND AFT SECTIONS OF THE CABIN. OPS CHECK GOOD. REFERENC E USAASB96177. 2 L 7 2 4F A16WE 1996100300453 19961003 00453 WP 1996 10 3 96ZZZM1379 1 19960806 A 3350 6100928 LENS DOUG DC9 DC987 3022087 WP CABIN MISSING A GRAA K NONE L NO TEST IN INSP/MAINT 1 WP 11 1074T 49727 ENV MAINTENANCE FOUND THE EMERGENCY LIGHT INOP AND LENS MISSING FROM ROW 19. THEY RELAMPED AND REPLACED THE LENS. SYST EM OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. REFERENCE GRAA9658. 2 L 7 2 4F RT A6WE 1996100300454 19961003 00454 SW 1996 10 3 96ZZZM1380 1 19960904 A 5230 1127511 SPRING SWRNGN SA227 SA227AC 8780603 SW CARGO DOOR WORN A MALA K NONE O OTHER TX TAXI/GRND HDL 1 GL 15 425MA AC640 FLT 3095 - ON TAXI, CREW REPORTED THE CARGO DOOR WARNING LIGHT ILLUMINATED. MAINTENANCE FOUND THE CARGO DOOR EXTERNAL H ANDLE WORN AND THE HANDLE RETURN SPRING WEAK. MAINTENANCE REPLACED THE EXTERNAL HANDLE AND RETURN SPRING. OPS CHECK OF THE HANDLE AND CARGO DOOR WARNING SYSTEM CHECKED GOOD. REFERENCE MALA965109. 2 L 7 2 4T RT A8SW 1996100300455 19961003 00455 CE 1996 10 3 96ZZZM1381 1 19960819 A 7810 1149100683 FLEX TUBE BEECH 1900 1900C 1154161 CE RT ENG SPLIT A GUUA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 19 190GA UB1 FLT 453 - JAX-TPA - RIGHT ENGINE FIRE WARNING ILLUMINATED IN FLIGHT. REMOVED AND REPLACED EXHAUST FLEX. 2 L 7 2 4T RT A24CE 1996100300456 19961003 00456 NE 1996 10 3 96ZZZM1382 2 19960725 A 7200 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RIGHT FAILED A MASA E ENGINE SHUTDOWN Y ENGINE STOPPAGE AP APPROACH 1 SW 01 51YV UE51 114074 ON SHORT FINAL, THE RIGHT ENGINE LOST OIL PRESSURE AND THE ENGINE QUIT RUNNING. AIRCRAFT LANDED WITHOUT INCIDENT. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 1996100300457 19961003 00457 NM 1996 10 3 96ZZZM1383 1 19960905 A 3246 9560571B WHEEL ASSY BOEING 707 707321C 138367B NM RT MLG DAMAGED A MIRA O OTHER E VIBRATION/BUFFET LD LANDING 1 SO 19 517MA 20017 MSLP-MGGT - STRONG VIBRATION RIGHT SIDE UPON LANDING AT MGGT. FOUND NR 3 AND NR 4 FRONT TIRES DESTROYED, WHEELS HAD DAM AGE TO THE RIMS. FOUND ONE FUSELAGE PLUG BLOWN ON ONE OF THE WHEELS. SPECULATE THAT THE OTHER TIRE WAS DESTROYED BY TH E SHREDDING OF THE TIRE THAT WAS WITHOUT AIR. CHANGED THE NR 3 AND NR 1 REAR WHEELS AND TIRES AS PRECAUTIONARY MEASURES . CHECKED ANTI-SKID AND FOUND OPERATIONAL. ACCOMPLISHED SIDE LOAD LANDING INSPECTION PER MILLION AIR WORK 707/2131 AND FOUND OK. WHEELS IN WERE OVERHAULED IN JUNE AND JULY OF 1996 RESPECTIVELY. 2 L 7 4 4F 4A26 1996100300458 19961003 00458 NM 1996 10 3 96ZZZM1384 1 19960811 A 3350 0105606002 LIGHT BOEING 757 75723A 1384967 NM 3L DOOR INOP A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 757NA 24567 E-PATH LIGHT AT 31-33 ABC INOP. REPAIRED WIRES, CHECKED OK. EXTERIOR EMERGENCY LIGHT AT 3L DOOR INOP. RELAMPED, CHECK ED OK. E-PATH LIGHT AT 5ABC INOP. RELAMPED, CHECKED OK. (M) 2 L 7 2 4F RT A2NM 1996100300459 19961003 00459 WP 1996 10 3 96ZZZM1385 1 19960811 A 3350 1315 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOP A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 183NA 49808 E-PATH LIGHT AT 21FED AND 5ABC INOP. REPLACED LAMPS, CHECKED OK. EMERGENCY LIGHT AT 33FED INOP. REPLACED BULBS, CHECK ED OK. (M) 2 L 7 2 4F RT A6WE 1996100300461 19961003 00461 NM 1996 10 3 96ZZZM1387 1 19960904 A 3610 69218903 DUCT BOEING 727 72721C 138400M NM NR 2 ENG CRACKED A PCSA F E A ACTIVATE FIRE EXT. ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 17 1186Z 19134 DURING CLIMB-OUT FROM TOLEDO, NR 2 ENGINE FIRE WARNING SOUNDED. CREW FIRED ONE EXTINGUISHER AND SHUT DOWN THE ENGINE. A IRCRAFT LANDED UNEVENTFULLY AT TOL. MAINTENANCE DISCOVERED 13TH STAGE BLEED SADDLE DUCT CAP (RT) FAILED AT WELD ALLOWIN G HOT BLEED AIR INTO THE COWLING NACELLE. REPLACED CAP AND FIRE BOTTLE, LEAK CHECKED DUCT, AND RETURNED TO SERVICE. (M ) 2 L 7 3 4F A3WE 1996100300462 19961003 00462 EA 1996 10 3 96ZZZM1388 2 19960825 A 7200 ENGINE DHAV DHC7 DHC7102 2802708 EA PWA PT6 PT6A50 52043 EA NR 1 FAILED A CICA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SO 17 703MG 20338 103 PCE86501 FLT 4924 - PID-MIA - DIVERTED TO NAS, LOST NR 1 ENGINE ERRATIC TORQUE INDICATION, THEN HIGH T5 AND LOW OIL PRESSURE. SH UT DOWN BEFORE TOTAL FAILURE. NR 1 CHIP DETECTOR ILLUMINATED. NR 1 ENGINE WAS INSPECTED AND FOUND TO HAVE METAL IN OIL AND ON OIL FILTER. THE AIRCRAFT WAS INSPECTED AND FOUND SAFE FOR 3 ENGINE FERRY TO FLL MAINTENANCE BASE. THE ENGINE W AS REMOVED AND REPLACED WITH SERVICEABLE ENGINE. OIL SAMPLE WAS TAKEN AND SENT FOR EVALUATION. ENGINE SENT TO OVERHAUL FACILITY FOR REPAIR. (M) 2 H 7 4 4T 4 T A20EA E4EA 1996100300463 19961003 00463 NM 1996 10 3 96ZZZM1389 1 19960619 A 3220 65737625 GEAR ASSY BOEING 737 7372L9 1384497 NM NLG CORRODED A ZZDA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 15 737Q W519B 21279 PRIOR TO BOARDING PASSENGERS FOR FLT 561, MECHANICS OBSERVED HYDRAULIC FLUID LEAKING FROM BOTTOM GLAND NUT ON NOSE LANDI NG GEAR. UPON TEAR DOWN INSPECTION REVEALED THAT THE OUTER CYCLINDER GLAND NUT THREADS WERE SEVERELY PITTED DUE TO CORR OSION, SEAL NOT IN PROPER GROOVE, GLAND NUT THREADS SEVERELY PITTED DUE TO CORROSION AND UPPER CENTERING CAM INNER AND O UTER SURFACE PLATING PITTED. THE NOSE GEAR ASSEMBLY WAS REPLACED WITH AN OVERHAULED UNIT, FUNCTIONAL CHECK WAS NORMAL. THE LEAKING NOSE GEAR ASSY HAD BEEN INSTALLED 3 DAYS PRIOR AS AN OVERHAULED UNIT AND ACCUMULATED 29.5 FLT HOURS AND 15 CYCLES BEFORE REMOVAL. 2 L 7 2 4F RT A16WE 1996100300464 19961003 00464 NM 1996 10 3 96ZZZM1390 1 19960822 A 3610 1074922 BLEED AIR REG BOEING 737 7374B7 1384702 NM LT ENGINE MALFUNCTIONED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 782AU 25021 PHL - FL 1268 - CAPTAIN REPORTED, THAT THE LEFT ENGINE BLEED AIR VALVE WOULD NOT OPEN AT TAKEOFF POWER. RECYCLED SWITCH AND CIRCUIT BREAKER WITH NO HELP. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE RE MOVED AND REPLACED THE FOLLOWING LISTED ITEMS PER THE MM. LEAK CHECK AND OPS CHECK GOOD. REFERENCE USAASB96166. 2 L 7 2 4F RT A16WE 1996100300465 19961003 00465 NM 1996 10 3 96ZZZM1391 1 19960822 A 3620 1296662 CONTL VLV SENSOR BOEING 737 7374B7 1384702 NM LT ENGINE MALFUNCTIONED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 782AU 25021 PHL - FL 1268 - CAPTAIN REPORTED, THAT THE LEFT ENGINE BLEED AIR VALVE WOULD NOT OPEN AT TAKEOFF POWER. RECYCLED SWITCH AND CIRCUIT BREAKER WITH NO HELP. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE RE MOVED AND REPLACED THE FOLLOWING LISTED ITEMS PER THE MM. LEAK CHECK AND OPS CHECK GOOD. REFERENCE USAASB96166. 2 L 7 2 4F RT A16WE 1996100300466 19961003 00466 NM 1996 10 3 96ZZZM1392 1 19960822 A 3610 MFGSPEC0032140 CONTL PANEL BOEING 737 7374B7 1384702 NM LT ENGINE MALFUNCTIONED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 782AU 25021 PHL - FL 1268 - CAPTAIN REPORTED, THAT THE LEFT ENGINE BLEED AIR VALVE WOULD NOT OPEN AT TAKEOFF POWER. RECYCLED SWITCH AND CIRCUIT BREAKER WITH NO HELP. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE RE MOVED AND REPLACED THE FOLLOWING LISTED ITEMS PER THE MM. LEAK CHECK AND OPS CHECK GOOD. REFERENCE USAASB96166. 2 L 7 2 4F RT A16WE 1996100300467 19961003 00467 NM 1996 10 3 96ZZZM1393 1 19960822 A 3620 129642 OVERTEMP SENSOR BOEING 737 7374B7 1384702 NM LT ENGINE MALFUNCTIONED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 782AU 25021 PHL - FL 1268 - CAPTAIN REPORTED, THAT THE LEFT ENGINE BLEED AIR VALVE WOULD NOT OPEN AT TAKEOFF POWER. RECYCLED SWITCH AND CIRCUIT BREAKER WITH NO HELP. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE RE MOVED AND REPLACED THE FOLLOWING LISTED ITEMS PER THE MM. LEAK CHECK AND OPS CHECK GOOD. REFERENCE USAASB96166. 2 L 7 2 4F RT A16WE 1996100300468 19961003 00468 NM 1996 10 3 96ZZZM1394 1 19960904 A 5230 65622191 CASTING BOEING 737 7372X6C 1384552 NM BS 480 CRACKED A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 746AS 23123 YAK - FLT 66 - THE MAIN CARGO DOOR ACTUATOR CASTING BROKE WHILE DOOR WAS BEING OPENED. MAINTENANCE MANUALLY CLOSED MAIN CARGO DOOR AND RELEASED AIRCRAFT FOR MAINTENANCE FERRY FLIGHT TO SEA FOR REPAIR. THE AIRCRAFT WAS INDUCTED INTO C-CHEC K UPON ITS ARRIVAL INTO SEA AND THE MAIN CARGO DOOR ACTUATOR CASTING IS CURRENTLY IN WORK. REFERENCE ASAA9610128. 2 L 7 2 4F RT A16WE 1996100300469 19961003 00469 NM 1996 10 3 ASAA9610121 1 19960830 A 5315 65549064 FLOOR BEAM BOEING 737 737290C 138448V NM BS 520 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING D-CHECK, BS 520 RBL 24.75 FLOOR BEAM UPPER CHORD WAS FOUND CRACKED IN RADIUS. REPAIRED PER EA 5310-01485 A ND BOEING TELEX ASA-SEA-96-0392RR. (M) 2 L 7 2 4F A16WE 1996100300470 19961003 00470 NM 1996 10 3 ASAA9610122 1 19960830 A 5315 65549064 FLOOR BEAM BOEING 737 737290C 138448V NM BS 520 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING D-CHECK, BS 520 LBL 24.75 FLOOR BEAM UPPER CHORD WAS FOUND CRACKED IN RADIUS. REPAIRED PER EA 5310-01485 A ND BOEING TELEX ASA-SEA-96-0392RR. (M) 2 L 7 2 4F A16WE 1996100300471 19961003 00471 NM 1996 10 3 ASAA9610125 1 19960830 A 5315 65671408 FLOOR BEAM BOEING 737 737290C 138448V NM BS 549-727 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING D-CHECK, CORROSION WAS FOUND ON THE LEFT FLANGE OF THE LONGITUDINAL FLOOR BEAM AT RBL 45, BETWEEN BS 549 AN D 727A. REPAIRED PER EA 5310-01489 AND BOEING TELEX ASA-SEA-96-0400RR. (M) 2 L 7 2 4F A16WE 1996100300472 19961003 00472 NM 1996 10 3 ASAA9610126 1 19960831 A 3350 RPS1B BATTERY PACK BOEING 737 737290C 138448V NM CARGO COMPT DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING MAINTENANCE, THE FWD PALLET EMERGENCY TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1996100300473 19961003 00473 NM 1996 10 3 ASAA9610127 1 19960909 A 3350 8821004 BATTERY BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROW 2. REPLACED B ATTERY AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1996100300474 19961003 00474 NM 1996 10 3 ASAA9610128 1 19960904 A 5230 6562216501 CASTING BOEING 737 7372X6C 1384552 NM BS 480 BROKEN A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 746AS 23123 YAK - FLT 66 - THE MAIN CARGO DOOR ACTUATOR CASTING BROKE WHILE DOOR WAS BEING OPENED. MAINTENANCE MANUALLY CLOSED MAIN CARGO DOOR AND RELEASED AIRCRAFT FOR MAINTENANCE FERRY FLIGHT TO SEA FOR REPAIR. THE AIRCRAFT WAS INDUCTED INTO C-CHEC K UPON ITS ARRIVAL INTO SEA AND THE MAIN CARGO DOOR ACTUATOR CASTING IS CURRENTLY IN WORK. (M) 2 L 7 2 4F RT A16WE 1996100300475 19961003 00475 NM 1996 10 3 ASAA9640073 1 19960831 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 772AS 25105 SEA - FLT 102 - DURING PRE-FLT, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AND WIRES EXPOSED AT THE AFT EMERGENCY EXIT DOORS. RECONNECTED AND STOWED WIRING, AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996100300476 19961003 00476 NM 1996 10 3 ASAA9640074 1 19960908 A 3397 WIRE BOEING 737 7374S3 1384711 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 786AS 24795 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 13 AND 14 WERE FOUND TO BE INOPERATIVE. S ECURED LOOSE WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996100300477 19961003 00477 WP 1996 10 3 ASAA9680172 1 19960810 A 5240 HINGE MECHANISM DOUG DC9 DC983 3022083 WP SERV DOOR OUT OF ADJUST A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 960AS 53074 PDX - AFTER CATERING AIRCRAFT, THE R1 DOOR WAS REPORTED DIFFICULT TO CLOSE. FOUND DOOR HINGE LOCKOUT BAYONET PIVOT SHIM TOO TIGHT. RESHIMMED BAYONET PIVOT AND LUBED MECHANISM AND DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996100300478 19961003 00478 WP 1996 10 3 ASAA9680180 1 19960825 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 962AS 53076 PDX - FORWARD PORTABLE EMERGENCY EXIT LIGHT NEON LAMP INOPERATIVE. REPLACED LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996100300479 19961003 00479 WP 1996 10 3 ASAA9680184 1 19960901 A 3350 0105610001 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 937AS 49364 PDX - DURING MAINTENANCE CHECK, THE L2 DOOR EMERGENCY EXIT IDENTIFIER SIGN WAS FOUND INOPERATIVE. REPLACED THE LIGHT BA SE ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996100300480 19961003 00480 WP 1996 10 3 ASAA9680185 1 19960902 A 5210 TURNBUCKLE DOUG DC9 DC982 3022082 WP PAX DOOR OUT OF ADJUST A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 931AS 49232 PDX - AFTER ARRIVAL OF FLT 485, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN FROM INSIDE. ADJUSTED TURNBUCKLE FOR UP PER DOOR RELIEF GATE AND DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996100300481 19961003 00481 WP 1996 10 3 ASAA9680186 1 19960902 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 954AS 49387 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996100300482 19961003 00482 WP 1996 10 3 ASAA9680187 1 19960903 A 5210 HANDLE DOUG DC9 DC982 3022082 WP PAX DOOR OUT OF ADJUST A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 933AS 49234 PDX - AFTER ARRIVAL OF FLT 485, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN, HANDLE STOPPED AND HAD TO BE CYCLED TO OPEN DOOR. CLEANED AND LUBED L1 DOOR MECHANISM AND DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996100300483 19961003 00483 WP 1996 10 3 ASAA9680188 1 19960904 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 944AS 53019 PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 22 TO 33 WERE FOUND DIM. REPLACED THE BATTER Y PACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996100300484 19961003 00484 WP 1996 10 3 ASAA9680189 1 19960905 A 2560 ESCAP ROPE CLIP DOUG DC9 DC982 3022082 WP RT EMER EXIT LODGED IN DOOR A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 957AS 49126 PDX - DURING MAINTENANCE CHECK, THE FORWARD RIGHT OVERWING EMERGENCY EXIT DOOR WAS FOUND DIFFICULT TO OPEN. FOUND ESCAP E ROPE CLIP LODGED BETWEEN DOOR AND FRAME. STOWED ESCAPE ROPE CLIP IN PROPER POSITION AND DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996100300485 19961003 00485 WP 1996 10 3 ASAA9680190 1 19960906 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 969AS 53063 SFO - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996100300486 19961003 00486 WP 1996 10 3 ASAA9680191 1 19960907 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 937AS 49364 ANC - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHT IN THE AFT CABIN WAS FOUND INOPERATIVE. REPLACED THE BATTE RY PACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996100300487 19961003 00487 WP 1996 10 3 ASAA9680192 1 19960907 A 3350 S103 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 941AS 49925 SEA - DURING MAINTENANCE CHECK, THE FORWARD LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. REPLA CED THE BATTERIES AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996100300488 19961003 00488 WP 1996 10 3 ASAA9680193 1 19960907 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 950AS 53023 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. REPAIRED TRAC K WIRING AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996100300489 19961003 00489 1996 10 3 ASAA9680194 4 19960907 A 2565 D37013115 SLIDE BOTTLE DOUG DC9 DC983 3022083 WP R1 DOOR LOW PRESSURE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 962AS 53076 LAX - DURING MAINTENANCE CHECK, THE R1 DOOR EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. REPLACE D THE EMERGENCY EVACUATION SLIDE. (M) 2 L 7 2 4F RT A6WE 1996100300490 19961003 00490 WP 1996 10 3 ASAA9680195 1 19960907 A 2560 MOUNT DOUG DC9 DC983 3022083 WP L2 DOOR LOOSE A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 962AS 53076 SEA - PRIOR TO DEPARTURE OF FLT 358, CREW REPORTED THE L2 DOOR EMERGENCY EVACUATION SLIDE GIRT BAR WOULD NOT ARM. FOUND THE AFT GIRT BAR FLOOR MOUNT LOOSE, SECURED MOUNT AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996100300491 19961003 00491 WP 1996 10 3 ASAA9680196 1 19960908 A 3350 S103 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 936AS 49363 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE BAT TERIES AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996100300492 19961003 00492 WP 1996 10 3 ASAA9680197 1 19960814 A 3350 20131A BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 939AS 49657 PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 1 TO 6 WERE FOUND DIM. REPLACED THE BATTERIE S AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996100300493 19961003 00493 WP 1996 10 3 ASAA9680198 1 19960911 A 3350 S103 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 955AS 48080 SEA - DURING MAINTENANCE CHECK, THE AFT LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996100300494 19961003 00494 SO 1996 10 3 ASOA96033 1 19960829 A 5230 12023348005 SEAL EMB 120 EMB120RT SO CARGO DOOR TORN A ASOA B EMER. DESCENT O OTHER CR CRUISE 1 SO 11 127AM 120103 FLT 7268 - ROA-ATL - DURING CRUISE FLIGHT AT 20,000 FEET, CABIN PRESSURIZATION STARTED TO CLIMB. CREW ELECTED TO MAKE A N EMERGENCY DESCENT TO 10,000 FEET AND CONTINUE TO ATL, WHERE LANDING WAS MADE SAFELY AND WITHOUT INCIDENT. REMOVED AND REPLACED CARGO DOOR SEAL. OPERATIONAL AND LEAK CHECKS WERE GOOD AND AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M) 2 L 7 2 4T RT A31SO 1996100300495 19961003 00495 SO 1996 10 3 ASOA96034 1 19960829 A 3260 922FS2A6NZ735A PROX SENSOR EMB 120 EMB120RT SO LT MLG DEFECTIVE A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 211AS 120007 FLT 7228 - AFTER TAKEOFF MEI-ATL - CYCLED THE GEAR UP AND THE GEAR DID NOT RETRACT. CREW DECLARED A PRECAUTIONARY EMERG ENCY AND RETURNED TO MEI, WHERE LANDING WAS MADE SAFELY AND WITHOUT INCIDENT. REMOVED AND REPLACED LEFT 'A' UPLOCK PROX IMITY SENSOR. PERFORMED GEAR SWING AND DETERMINED PROPER OPERATION. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996100300496 19961003 00496 EU 1996 10 3 ASOA96035 1 19960902 A 5280 S5287900100066 DOOR AEROSP ATR72 ATR72212 EU NLG DAMAGED A ASOA O OTHER O OTHER CL CLIMB 1 SO 11 630AS 336 FLT 7138 - DURING TAKEOFF VPS-ATL, THERE WAS A LOUD NOISE HEARD CONCURRENT WITH A ONE-TIMER SHUDDER. CAPTAIN LEFT THE G EAR DOWN AND FLEW BY THE TOWER, WHICH REPORTED NO APPARENT DAMAGE. CREW ELECTED TO CONTINUE TO ATL AND DECLARED AND PRE CAUTIONARY EMERGENCY. LANDING WAS MADE SAFELY AND WITHOUT INCIDENT. INSPECTED ALL LANDING GEAR AND GEAR DOORS. NOTED DAMAGE TO THE LEFT NOSE GEAR DOOR. DOOR WAS REMOVED, SENT TO MCN FOR REPAIR AND REINSTALLED AFTER REPAIR. A TEST FLIGH T WAS PERFORMED (INCLUDED THREE GEAR CYCLES) AND AIRCRAFT WAS FOUND TO BE SATISFACTORY FOR CONTINUED SERVICE. (M) 2 H 7 2 4T RT A53EU 1996100300497 19961003 00497 SO 1996 10 3 ASOA96036 1 19960905 A 2121 EVAC2322C2 COOLING FAN EMB 120 EMB120RT SO AC BAY INOPERATIVE A ASOA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 11 233AS 120031 DURING TAXI-OUT ATL-AVL, EXPERIENCED RIGHT PACK FAILURE CAUSING SMOKE IN THE CABIN. AIRCRAFT RETURNED TO THE GATE AND D EBOARDED WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED THE RIGHT GROUND COOLING FAN. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996100300498 19961003 00498 SO 1996 10 3 ASOA96037 1 19960908 A 4950 BLEED SYSTEM EMB 120 EMB120RT SO APU SMOKING A ASOA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 11 214AS 120009 SHORTLY AFTER TAKEOFF GPT-ATL, CREW SELECTED BLEED TO AUTO AND SHUT DOWN THE APU, THEN NOTICED A BUNRING SMELL IN THE CO CKPIT. THE CREW SHUT OFF PACKS, BLEEDS, RECIRCULATION AND GASPER FANS. THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO GPT WHERE LANDING WAS MADE SAFELY WITHOUT FURTHER INCIDENT. PERFORMED OPERATIONAL CHECK OF THE APU BLEED AND LEFT AN D RIGHT PACKS WITH NO SMOKE NOTED. PROBLEM COULD NOT BE DUPLICATED. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. (M) 2 L 7 2 4T RT A31SO 1996100300499 19961003 00499 SW 1996 10 3 BDHA00016 1 19960805 A 2435 230790001 START/GEN SWRNGN SA226 SA226TC 8780404 SW LT ENG FAILED A BDHA O OTHER H ELECT. POWER LOSS-50 PC IN INSP/MAINT 1 GL 15 328BA 1316 TC253 FSD - FLT 434 - THE LEFT GENERATOR FELL OFF LINE AND WOULD NOT RESET. INSPECTION OF THE SYSTEM FOUND THE GENERATOR WAS THE PROBLEM. THIS GENERATOR WAS RETURNED TO SERVICE AFTER A BENCH CHECK AND OPERATED ONE HOUR BEFORE FAILING. (M) 2 L 7 2 4T RT A8SW 1996100300500 19961003 00500 SW 1996 10 3 BDHA00017 1 19960806 A 2435 230790001 START/GEN SWRNGN SA226 SA226TC 8780404 SW LT ENG FAILED A BDHA O OTHER H ELECT. POWER LOSS-50 PC IN INSP/MAINT 1 GL 15 328BA 2737 TC253 MOT - FLT 421 - THE LEFT GENERATOR FELL OFF LINE AND WOULD NOT RESET. AFTER LANDING, THE CREW WAS INSTRUCTED TO PERFORM A STARTER TEST. THE ENGINE WOULD NOT ROTATE WITH THE STARTER. THE PROPELLER SPUN FREE BY HAND. THE START/GEN WAS REP LACED AND OPERATION CHECK PERFORMED. THE AIRCRAFT WAS RELEASED. (M) 2 L 7 2 4T RT A8SW 1996100300501 19961003 00501 SW 1996 10 3 BDHA9600018 1 19960829 A 7722 8974696 EGT LEAD SWRNGN SA226 SA226TC 8780404 SW RT ENG OPEN A BDHA K NONE O OTHER IN INSP/MAINT 1 GL 15 328BA TC253 MSP - FLT 434 - THE CREW REPORTED, THE RIGHT EGT INDICATOR WAS ERRATIC ON ENGINE START. INSPECTION OF THE SYSTEM FOUND THE EGT LEAD, AT THE RAKE WAS DETERIORATING. THE LEAD WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A8SW 1996100300502 19961003 00502 SW 1996 10 3 BDHA960015 1 19960517 A 3260 27425 CONTROL BOX SWRNGN SA226 SA226TC 8780404 SW COCKPIT MALFUNCTIONED A BDHA O OTHER N FALSE WARNING LD LANDING 1 GL 15 229AM TC305 FAR - FLT 421 - AFTER A NOSE GEAR UP LANDING, IT WAS DISCOVERED THAT THE FLAP/GEAR WARNING HORN WAS MALFUNCTIONING. WIT H THE GEAR SELECTOR DOWN (GEAR IN AN UNSAFE CONDITION), FLAPS DOWN, AND THE POWER LEVERS AT THE FLIGHT IDLE GATE, THE HO RN SOUNDED. WHEN THE POWER LEVERS WERE ADVANCED FORWARD OF THE FLIGHT IDLE GATES, THE HORN STOPPED. IN NORMAL OPERATIO N, WITH THE FLAPS DOWN PAST 20 DEGREES, THE WARNING HORN MUST SOUND WHENEVER THE LANDING GEAR IS IN AN UNSAFE CONDITION, NO MATTER WHAT THE POSITION OF THE POWER LEVERS. 2 L 7 2 4T RT A8SW 1996100300503 19961003 00503 NE 1996 10 3 BJNA96802 2 19960820 A 7230 C1/C2 DISK BOEING 737 737214 138446R NM PWA JT8 JT8D15A 52051 NE ENGINE LOOSE A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 457TM 20156 ON WALK AROUND INSPECTION, FOUND C1/C2 SPACER RETAINING NUT AND KEY WASHER INSIDE HUB ASSY. REMOVED ENGINE. (M) 2 L 7 2 4F 4 F A16WE E2EA 1996100300504 19961003 00504 EU 1996 10 3 C2XA96CL022 1 19960829 A 2460 29951000011 BATTERY SHUNT AEROSP ATR42 ATR42320 8680930 EU COCKPIT SHORTED A C2XA H E DEACTIVATE SYST/CIRCUITS ENGINE SHUTDOWN H N ELECT. POWER LOSS-50 PC FALSE WARNING TX TAXI/GRND HDL 1 SW 09 14830 184 CLT - FLT 3030 - CREW REPORTED THAT ON TAXI, THE NR 1 ENGINE WOULD NOT START, AFTER THREE ATTEMPTS ALL THE LIGHTS FLICKE RED ON AND OFF AND THEY RECEIVED A FIRE LIGHT ON THE NR 2 ENGINE, WHICH WAS SUBSEQUENTLY SHUT DOWN. THE LIGHTS AND RELA YS CONTINUED TO FLICKER ON BATTERY POWER ONLY, THE CREW THEN SHUT OFF ALL POWER TO AIRCRAFT. THE NR 2 ENGINE GENERATOR NEVER FELL OFF LINE. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE MAIN BATTERY POWER SHUNT IAW ATR 4 2MM 24-00-00 RAI-10040-003, OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RELEASED FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 1996100300505 19961003 00505 SO 1996 10 3 C2XA96CL024 1 19960830 A 3250 12037995001 STEERING HANDLE EMB 120 EMB120RT SO NLG STEERING WORN A C2XA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 09 16729 120118 120185 CLE - FLT 3216 - CREW REPORTED, THAT THE NOSE WHEEL STEERING DISCONNECTS WHEN MAKING FULL LEFT TURNS WITH THE TILLER AND RUDDER PEDALS. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED THE STEERING HANDLE IAW EMB-120 MM 32-50-01, OP ERATIONAL CHECKS WERE GOOD IAW EMB-120 MM 32-50-00. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996100300506 19961003 00506 SO 1996 10 3 C2XA96CL025 1 19960902 A 3250 MS250851 SWITCH EMB 120 EMB120RT SO NLG STEERING OUT OF ADJUST A C2XA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 09 16729 120185 CLE - FLT 3070 - CREW REPORTED, THAT THE NOSE WHEEL STEERING DISCONNECTS WHEN MAKING FULL LEFT TURNS USING THE TILLER. M AINTENANCE INSPECTED AIRCRAFT AND ADJUSTED THE NOSE WHEEL STEERING TILLER MICROSWITCH IAW EMB-120 MM 32-50-00. OPS CHEC KS WERE GOOD, AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996100300507 19961003 00507 EU 1996 10 3 C2XA96IA213 1 19960827 A 2510 134022105 LOCKING MECH AEROSP ATR42 ATR42320 8680930 EU CREW SEAT CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 26826 172 IAH - DURING C-CHECK INSPECTION, THE FLIGHT ATTENDANTS SEAT ATTACH POINTS WERE FOUND TO BE CORRODED. MAINTENANCE REMOVE D AND REPLACED THE AFFECTED ATTACH FITTINGS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996100300508 19961003 00508 EU 1996 10 3 C2XA96IA214 1 19960827 A 5311 S5397091627600 FRAME AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 26826 172 IAH - DURING C-CHECK INSPECTION, THE FAIRING FRAME UNDER PANEL 291AL WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND R EPLACED THE AFFECTED FRAME, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996100300509 19961003 00509 EU 1996 10 3 C2XA96IA215 1 19960827 A 5347 S5367800120200 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 26826 172 IAH - DURING C-CHECK INSPECTION, THE RIGHT INBOARD SEAT TRACK FROM FRAME 31 TO 32 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996100300510 19961003 00510 EU 1996 10 3 C2XA96IA216 1 19960827 A 5347 S5367800120100 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 26826 172 IAH - DURING C-CHECK INSPECTION, THE RIGHT OUTBOARD SEAT TRACK FROM FRAME 31 TO 32 WAS FOUND TO BE CORRODED. MAINTENANC E REMOVED AND REPLACED THE AFFECTED SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996100300511 19961003 00511 EU 1996 10 3 C2XA96IA217 1 19960827 A 5315 S5367240620800 FLOOR BEAM AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 26826 172 IAH - DURING C-CHECK INSPECTION, THE FLOOR BEAM AT FRAME 36 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR BEAM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996100300512 19961003 00512 EU 1996 10 3 C2XA96IA218 1 19960827 A 5315 S5367240720200 FLOOR BEAM AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 26826 172 IAH - DURING C-CHECK INSPECTION, THE FLOOR BEAM AT FRAME 38 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOOR BEAM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996100300513 19961003 00513 EU 1996 10 3 C2XA96IA219 1 19960827 A 5320 S5367131830400 THRESHOLD AEROSP ATR42 ATR42320 8680930 EU SERV DOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 26826 172 IAH - DURING C-CHECK INSPECTION, THE THRESHOLD WEB AT FRAME 36 TO 39 AT THE SERVICE DOOR CUTOUT WAS FOUND TO BE CORRODED . MAINTENANCE REMOVED AND REPLACED THE AFFECTED WEB AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996100300514 19961003 00514 EU 1996 10 3 C2XA96IA220 1 19960827 A 5315 S5367240820200 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 26826 172 IAH - DURING C-CHECK INSPECTION, THE FLOOR BEAM AT FRAME 39 WAS FOUND BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOOR BEAM AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996100300515 19961003 00515 EU 1996 10 3 C2XA96IA221 1 19960827 A 5311 S5367131120000 FRAME AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 26826 172 IAH - DURING C-CHECK INSPECTION, FRAME 37 WAS FOUND TO BE CORRODED. MAINTENANCE REPAIRED THE FRAME BY REMOVING THE CORR ODED PORTION AND INSERTING A REPAIR DOUBLER. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996100300516 19961003 00516 EU 1996 10 3 C2XA96IA222 1 19960827 A 5753 S5751008002800 SKIN AEROSP ATR42 ATR42320 8680930 EU LT TE FLAP DELAMINATED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 26826 172 IAH - DURING C-CHECK INSPECTION, THE LEFT OUTBOARD FLAP WAS FOUND THROUGH ULTRASONIC TESTING TO BE DELAMINATED ON THE UP PER SKIN AT RIB 14. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLAP AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV ICE. (M) 2 H 7 2 4T RT A53EU 1996100300517 19961003 00517 NM 1996 10 3 EISA96121 1 19960812 A 5311 FRAME BOEING 727 727223 1384074 NM BS 440 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 FRAME CRACKED AT FS 440, STRINGER 16 LT. FABRICATED DOUBLER PER SRM 51-40-03 AND INSTALLED PER SRM 51-40-03. (M) 2 L 7 3 4F A3WE 1996100300518 19961003 00518 NM 1996 10 3 EISA96122 1 19960812 A 5311 FRAME BOEING 727 727223 1384074 NM BS 480 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 JUST ABOVE CABIN FLOOR, AT FS 480 RIGHT, FRAME CRACKED. INSTALLED REPAIR PER SRM 51-40-03. (M) 2 L 7 3 4F A3WE 1996100300519 19961003 00519 NM 1996 10 3 EISA96123 1 19960812 A 5311 FRAME BOEING 727 727223 1384074 NM BS 460 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 JUST ABOVE CABIN FLOOR AT FS 460 RIGHT, FRAME CRACKED. FABRICATED AND INSTALLED DOUBLER PER SRM 51-40-03. (M) 2 L 7 3 4F A3WE 1996100300520 19961003 00520 NM 1996 10 3 EISA96124 1 19960812 A 5311 FRAME BOEING 727 727223 1384074 NM BS 440 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 JUST ABOVE CABIN FLOOR AT FS 440 RIGHT, FRAME CRACKED. STOP DRILLED CRACKS AND INSTALLED REPAIR DOUBLER PER SRM 51-40-0 3. (M) 2 L 7 3 4F A3WE 1996100300521 19961003 00521 NM 1996 10 3 EISA96125 1 19960812 A 5311 FRAME BOEING 727 727223 1384074 NM BS 740 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 JUST ABOVE CABIN FLOOR AT FS 740 LEFT, FRAME CRACKED. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER PER SRM 51-4 0-03. (M) 2 L 7 3 4F A3WE 1996100300522 19961003 00522 NM 1996 10 3 EISA96126 1 19960812 A 5311 FRAME BOEING 727 727223 1384074 NM BS 720 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 JUST ABOVE CABIN FLOOR AT FS 720 LEFT, FRAME CRACKED. CUT OUT DAMAGE AREA, FABRICATED AND INSTALLED DOUBLER PER SRM 51- 40-03. (M) 2 L 7 3 4F A3WE 1996100300523 19961003 00523 NM 1996 10 3 EISA96127 1 19960812 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM CARGO COMPT CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 FORWARD CARGO COMPARTMENT, LEFT STRINGER 27, SHEAR TIE CRACKED. INSTALLED NEW SHEAR TIE PER SRM 53-01. (M) 2 L 7 3 4F A3WE 1996100300524 19961003 00524 NM 1996 10 3 EISA96128 1 19960812 A 5712 RIB BOEING 727 727223 1384074 NM WS 340 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 RIGHT WING LEADING EDGE WING AT APPROX WS 340, PREVIOUS REPAIR DOUBLER CRACKED. FABRICATED NEW WEB ANGLE AND INSTALLED PER SRM 51-10-02. (M) 2 L 7 3 4F A3WE 1996100300525 19961003 00525 NM 1996 10 3 EISA96129 1 19960812 A 5754 RIB BOEING 727 727223 1384074 NM NR 5 LE FLAP CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 RIGHT WING NR 5 SLAT, TWO CRACKED RIBS AT ACTUATOR ATTACH BOLT. FABRICATED DOUBLER PER SRM 51-40-00 AND INSTALLED PER S RM 53-40-0. (M) 2 L 7 3 4F A3WE 1996100300526 19961003 00526 NM 1996 10 3 EISA96130 1 19960812 A 5754 BRACKET BOEING 727 727223 1384074 NM NR 5 LE FLAP CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 RIGHT WING NR 5 SLAT INBOARD TRACK, INBOARD SIDE, BRACKET CRACKED. FABRICATED AND INSTALLED NEW BRACKET PER SRM 51-10-0 1. (M) 2 L 7 3 4F A3WE 1996100300527 19961003 00527 NM 1996 10 3 EISA96131 1 19960812 A 5280 DOOR BOEING 727 727223 1384074 NM NLG CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 NOSE GEAR, RIGHT FORWARD DOOR ACCESS HOLE CUTOUT HAS CRACK. INSTALLED NEW WEB PER SRM 51-10-02. (M) 2 L 7 3 4F A3WE 1996100300528 19961003 00528 NM 1996 10 3 EISA96132 1 19960812 A 5753 SKIN BOEING 727 727223 1384074 NM LT TE FOREFLAP DEBONDED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 LEFT WING, INBOARD FOREFLAP UPPER SKIN HAS APPROX 8 INCHES BY 9 INCHES DEBONDED AREA, AFT OF NR 6 SPOILER. REPLACED FOR EFLAP WITH SERVICEABLE UNIT. (M) 2 L 7 3 4F A3WE 1996100300529 19961003 00529 NM 1996 10 3 EISA96133 1 19960812 A 5755 SKIN BOEING 727 727223 1384074 NM NR 5 SPOILER CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 LEFT WING, NR 5 SPOILER HAS TWO CRACKS IN UPPER SKIN AT CENTER HINGE. REPLACED SPOILER WITH OVERHAULED UNIT. (M) 2 L 7 3 4F A3WE 1996100300530 19961003 00530 NM 1996 10 3 EISA96134 1 19960812 A 5730 SKIN BOEING 727 727223 1384074 NM LT WING TE SKIN CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 LEFT WING, UPPER TE SKIN HAS THREE CRACKS, FORWARD OF NR 4 SPOILER. REPLACED SKIN PANEL PER SRM 51-10-01. (M) 2 L 7 3 4F A3WE 1996100300531 19961003 00531 NM 1996 10 3 EISA96135 1 19960812 A 5730 SKIN BOEING 727 727223 1384074 NM LT WING TE SKIN CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 LEFT WING, UPPER TE SKIN HAS TWO CRACKS, FORWARD OF NR 3 SPOILER. INSTALLED NEW SKIN PANEL PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1996100300532 19961003 00532 NM 1996 10 3 EISA96136 1 19960812 A 5320 TIE CLIP BOEING 727 727223 1384074 NM BS 540 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 FS 540 HAS STRINGER CLIP DAMAGED AT STRINGER 8 RIGHT. FABRICATED AND INSTALLED NEW TIE CLIP PER SRM 51-30-02. (M) 2 L 7 3 4F A3WE 1996100300533 19961003 00533 NM 1996 10 3 EISA96137 1 19960812 A 5311 FRAME BOEING 727 727223 1384074 NM BS 680 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 JUST ABOVE CABIN FLOOR, FS 680 LEFT, FRAME CRACKED. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR PER SRM 51-40-3 . (M) 2 L 7 3 4F A3WE 1996100300534 19961003 00534 NM 1996 10 3 EISA96138 1 19960812 A 5311 FRAME BOEING 727 727223 1384074 NM BS 700 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 JUST ABOVE CABIN FLOOR AT FS 700 LEFT, FRAME CRACKED. CUT OUT DAMAGED AREA. FABRICATED DOUBLER AND FILLER PER SRM 51-2 0-00. INSTALLED REPAIR PER SRM 51-40-03. (M) 2 L 7 3 4F A3WE 1996100300535 19961003 00535 NM 1996 10 3 EISA96139 1 19960812 A 5520 COVER BOEING 727 727223 1384074 NM RT ELEV CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 RIGHT ELEVATOR TAB, BOB WEIGHT COVERS CRACKED. RIGHT ELEVATOR TAB REPLACED. (M) 2 L 7 3 4F A3WE 1996100300536 19961003 00536 NM 1996 10 3 EISA96140 1 19960812 A 5523 SKIN BOEING 727 727223 1384074 NM RT ELEV TAB DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 RIGHT ELEVATOR TAB, INBOARD TRAILING EDGE DELAMINATED. RIGHT ELEVATOR TAB REPLACED. (M) 2 L 7 3 4F A3WE 1996100300537 19961003 00537 NM 1996 10 3 EISA96141 1 19960812 A 5754 SHIELD BOEING 727 727223 1384074 NM NR 3 LE FLAP CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 LEFT WING, NR 3 LEADING EDGE FLAP ANTI-ICE SHIELD CRACKED IN SEVERAL PLACES AROUND RIVETS. REPLACED BAFFLES PER SRM 51- 30-02. (M) 2 L 7 3 4F A3WE 1996100300538 19961003 00538 NM 1996 10 3 EISA96142 1 19960812 A 5520 COVER BOEING 727 727223 1384074 NM LT ELEV CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 312NE 20193 LEFT ELEVATOR TAB BOB WEIGHT COVERS CRACKED. REPLACED LEFT ELEVATOR. (M) 2 L 7 3 4F A3WE 1996100300539 19961003 00539 NM 1996 10 3 EISA96143 1 19960817 A 2150 3216741 PACK VLV BOEING 727 72782 1384029 NM RT A/C BAY INOPERATIVE A EISA H DEACTIVATE SYST/CIRCUITS O OTHER CL CLIMB 1 SW 07 357NE 743054 19405 AFTER TAKEOFF EXCESSIVE RATE OF CLIMB, RIGHT PACK TEMP AT 30 DEGREES, THE RIGHT MIX VALVE STUCK IN FULL COLD. REPLACED RIGHT PACK VALVE, SYSTEM OPS CHECK GOOD. (M) 2 L 7 3 4F A3WE 1996100300540 19961003 00540 NM 1996 10 3 EISA96144 1 19960820 A 2780 H1010262 SWITCH BOEING 727 727223 1384074 NM NR 6 LE FLAP INOP A EISA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 07 312NE 20193 NR 6 LEADING EDGE FLAP WOULD NOT RETRACT IN FLIGHT. REMOVED AND REPLACED NR 6 L/E FLAP SWITCH, OPS CHECK GOOD. (M) 2 L 7 3 4F A3WE 1996100300541 19961003 00541 WP 1996 10 3 GRAA9654 1 19960804 A 3350 LENS DOUG DC9 DC915 3022036 WP CABIN MISSING A GRAA K NONE O OTHER IN INSP/MAINT 1 WP 11 1070T 45784 DURING L/S RNO MAINTENANCE DISCOVERED, THE EMERGENCY FLOOR LIGHT AT SEAT 10C, MISSING LENS. THEY REPLACED LENS, OPS CHE CK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1996100300542 19961003 00542 WP 1996 10 3 GRAA9656 1 19960808 A 3350 LENS DOUG DC9 DC915 3022036 WP CABIN LOOSE A GRAA K NONE O OTHER IN INSP/MAINT 1 WP 11 1070T 45784 DURING L/S RNO MAINTENANCE DISCOVERED THE EMERGENCY FLOOR TRACK WHITE LIGHT LENS IN ROW 10 UNSECURED. SECURED THE LENS, OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1996100300543 19961003 00543 WP 1996 10 3 GRAA9657 1 19960802 A 3350 6100925 LIGHT DOUG DC9 DC915 3022036 WP CABIN INOPERATIVE A GRAA K NONE L NO TEST IN INSP/MAINT 1 WP 11 1068T 45782 DURING L/S RNO MAINTENANCE DISCOVERED EMERGENCY LIGHT AT ROW 13 INOP. RELAMPED AND SECURED WIRING UNDER SEAT SYSTEM OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1996100300544 19961003 00544 WP 1996 10 3 GRAA9658 1 19960831 A 2130 PRESS CONTL SYST DOUG DC9 DC915 3022036 WP CABIN MALFUNCTIONED A GRAA G O2 MASK DEPLOYED J WARNING INDICATION AP APPROACH 1 WP 11 1064T 45778 THE AUTO PRESSURE CONTROL SYS FAIL ON APPROACH. THE CABIN OXYGEN MASKS DROPPED. THE A/C CONTINUED WITHOUT FURTHER INCI DENT. MAINTENANCE CONTROL ISSUED A MX FERRY PERMIT TO RNO WITH THE MASKS DOWN AND AIRCRAFT TO FLY UNPRESSURIZED. AIRCR AFT ARRIVED INTO RNO WITHOUT FURTHER INCIDENT. MX REINSTALLED OXYGEN MASKS. MX REPAIRED THE RIGHT AIR CONDITIONING SYS TEM AND PERFORMED AN OPERATIONAL CHECK OF THE SYSTEM, NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1996100300545 19961003 00545 WP 1996 10 3 GRAA9659 1 19960830 A 3350 LIGHT DOUG DC9 DC915 3022036 WP CABIN INOPERATIVE A GRAA K NONE L NO TEST IN INSP/MAINT 1 WP 11 1068T 45782 DURING L/S MAINTENANCE, CREW IN RNO DISCOVERED THE EMERGENCY LIGHTS MAIN CABIN DOOR NOT ARMED. CREW RELAMPED, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1996100300546 19961003 00546 WP 1996 10 3 GRAA9660 1 19960820 A 3397 WIRE DOUG DC9 DC987 3022087 WP CABIN BROKEN A GRAA K NONE L NO TEST IN INSP/MAINT 1 WP 11 1074T 49727 LINE MAINTENANCE AT ENV, DISCOVERED THAT EMERGENCY FLOOR LIGHT AT ROW 18 WAS INOPERATIVE. MAINTENANCE SOLDERED BROKEN W IRE, OPERATIONAL CHECK WAS PERFORMED. NO DEFECTS NOTED. OPERATIONAL CHECKED NORMAL. THE AIRCRAFT WAS RETURNED TO SERV ICE. (M) 2 L 7 2 4F RT A6WE 1996100300547 19961003 00547 WP 1996 10 3 GRAA9661 1 19960814 A 3350 0816901 LAMP DOUG DC9 DC987 3022087 WP CABIN INOPERATIVE A GRAA K NONE L NO TEST IN INSP/MAINT 1 WP 11 1074T 49727 ENV MAINTENANCE FOUND THE EMERGENCY LIGHT INOP AND LENS MISSING FROM ROW 19. THEY RELAMPED AND REPLACED THE LENS. SYST EM OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A6WE 1996100300548 19961003 00548 WP 1996 10 3 GRAA9662 1 19960815 A 3350 08169304 LENS DOUG DC9 DC987 3022087 WP CABIN MISSING A GRAA K NONE L NO TEST IN INSP/MAINT 1 WP 11 1074T 49727 LINE MAINTENANCE AT ENV, DISCOVERED RED EMERGENCY FLOOR TRACK LIGHT AT ROW 19R WAS MISSING. MAINTENANCE REPLACED THE SO CKET PIGTAIL, LAMP, AND LENS. MAINTENANCE PERFORMED OPERATIONAL CHECK. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE . (M) 2 L 7 2 4F RT A6WE 1996100300549 19961003 00549 WP 1996 10 3 GRAA9663 1 19960822 A 3350 LIGHT DOUG DC9 DC987 3022087 WP CABIN INOPERATIVE A GRAA K NONE L NO TEST IN INSP/MAINT 1 WP 11 1075T 49724 LINE MAINTENANCE AT IFP, DISCOVERED THAT THE EMERGENCY FLOOR LIGHT WAS INOPERATIVE. MAINTENANCE RELAMPED OPERATIONAL CH ECKED NORMAL. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A6WE 1996100300550 19961003 00550 WP 1996 10 3 GRAA9664 1 19960829 A 3350 LIGHT DOUG DC9 DC915 3022036 WP CABIN INOPERATIVE A GRAA K NONE L NO TEST IN INSP/MAINT 1 WP 11 1070T 45784 DURING L/S MAINTENANCE, CREW IN RNO DISCOVERED THE EMERGENCY FLOOR LIGHT INOP AT SEAT 10C. CREW RELAMPED, P/N 363634. O PS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1996100300551 19961003 00551 NM 1996 10 3 IXKA9600074 1 19960902 A 2131 1310461 CONTROLLER BOEING 727 727251 138408H NM CABIN FAILED A IXKA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 25 267US 35365 20289 FLT 73 - ATL-MCO - PRESSURIZATION WAS ERRATIC, SWITCHED TO MANUAL, UNABLE TO CONTROL. RETURNED TO ATL. REMOVED AND REP LACED AND REPLACED MANUAL CONTROLLER, PERFORMED ADJUSTMENT TEST AND OPS CHECK NORMAL PER MM 21-30-00. (M) 2 L 7 3 4F A3WE 1996100300552 19961003 00552 NM 1996 10 3 IXKA9600075 1 19960902 A 3350 10126215 LIGHT GRIMES BOEING 727 727225 1384077 NM CABIN BROKEN A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8882Z 21579 EMERGENCY LIGHT AT L1 DOOR BROKEN. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY AND OPS CHECKED OK AS PER MM 33-50-01. (M) 2 L 7 3 4F A3WE 1996100300553 19961003 00553 NM 1996 10 3 IXKA9600077 1 19960905 A 2131 1310461 CONTROLLER BOEING 727 727251 138408H NM CABIN INOPERATIVE A IXKA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 25 259US 19978 FLT 9 - EWR-MCO - AT CRUISE, EXPERIENCED RAPID DECOMPRESSION AT 31,000 FEET, DECLARED EMERGENCY AND FOLLOWED RAPID DECOM PRESSION AND EMERGENCY DESCENT PROCEDURES. MADE NORMAL APPROACH AND LANDING AT MCO. VISUALLY INSPECTED EXTERIOR DOOR S EALS AND OUTFLOW VALVES. REPLACED MANUAL PRESSURE CONTROLLER AND OPS CHECK OK AS PER 21-30-00, PAGE 501. (M) 2 L 7 3 4F A3WE 1996100300554 19961003 00554 NM 1996 10 3 IXKA9600078 1 19960903 A 3397 WIRE BOEING 727 727230 1384080 NM CABIN BROKEN A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 357KP 20675 ON INTERIOR CHECK, FOUND MOST FORWARD SECTION OF 'E' PATH LIGHTS OUT. REPAIRED BROKEN WIRES FOR 'E' PATH LIGHTS. OPS C HECK OK AS PER MM 33-50-01. (M) 2 L 7 3 4F A3WE 1996100300555 19961003 00555 NM 1996 10 3 IXKA960076 1 19960824 A 3397 WIRE BOEING 727 727225 1384077 NM CABIN BROKEN A IXKA K NONE L NO TEST IN INSP/MAINT 1 EA 25 356PA 20626 'E' PATH LIGHTS OUT AT ROW NR 4 AND NR 25. REPAIRED WIRE AT ROW 4 AND RELAMPED LIGHT AT ROW 25. OPS CHECK OK AS PER 33 -50-01. (M) 2 L 7 3 4F A3WE 1996100300556 19961003 00556 WP 1996 10 3 IXXA96132 1 19960722 A 5311 FRAME DOUG DC8 DC871 302199A WP BS 1300 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 823BX 74464 46064 DURING ROUTINE C-CHECK INSPECTION, THE FUSELAGE FRAME AT STATION 1300 WAS FOUND TO BE CRACKED. THE CRACK WAS LOCATED BE TWEEN LONGERONS 35 LEFT AND 35 RIGHT. THE CRACK WAS REPAIRED IAW THE DOUGLAS STRUCTURAL REPAIR MANUAL 53-2-0, FIGURE 1B , SHEET 3. (M) 2 L 7 4 4F 4A25 1996100300557 19961003 00557 WP 1996 10 3 IXXA96133 1 19960722 A 7830 3055191020 TR COWL DOUG DC8 DC871 302199A WP NR 3 ENGINE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 823BX 29067 5806 46064 DURING ROUTINE C-CHECK INSPECTION, THE NR 3 THRUST REVERSER OUTBOARD COWLING WAS FOUND CRACKED AT THE FOUR O'CLOCK POSIT ION. REPAIR WAS ACCOMPLISHED IAW CFMI SHOP MANUAL 78-32-11, REPAIR 30. (M) 2 L 7 4 4F 4A25 1996100300558 19961003 00558 WP 1996 10 3 IXXA96134 1 19960722 A 3230 575500921 FITTING DOUG DC8 DC871 302199A WP LT MLG CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 823BX 74464 5806 46064 DURING ROUTINE C-CHECK INSPECTION, THE LEFT MAIN LANDING GEAR TORQUE TUBE SUPPORT FITTING WAS FOUND CRACKED. THE CRACK WAS STOP DRILLED AND REPAIRED IAW DOUGLAS SERVICE BULLETIN 53-61 R3 CONDITION 2 REQUIREMENTS. (M) 2 L 7 4 4F 4A25 1996100300559 19961003 00559 WP 1996 10 3 IXXA96135 1 19960806 A 5711 5597830 SPAR DOUG DC8 DC862 3021970 WP RT WING RT CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 61CX 58805 3096 46142 WHILE ACCOMPLISHING THE REPLACEMENT OF THE RIGHT MAIN LANDING GEAR FITTING, THE RIGHT LOWER REAR SPAR WAS FOUND TO BE CR ACKED BETWEEN WING STATION S XRS 13 AND XRS 20. THE REPAIR OF THE SPAR WAS ACCOMPLISHED IAW DOUGLAS DRAWINGS 5613917, 5 613918, 5613919, 5613920, 5613921 AND THE SRM. (M) 2 L 7 4 4F 4A25 1996100300560 19961003 00560 WP 1996 10 3 IXXA96136 1 19960806 A 5751 SKIN DOUG DC8 DC862 3021970 WP LT AILERON CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 61CX 46142 DURING ROUTINE C-CHECK INSPECTION, THE LEFT OUTBOARD AILERON LOWER PLATING SURFACE WAS FOUND TO BE CORRODED BETWEEN STAT IONS XW500 AND 577. THE PLATING WAS REPLACED IAW THE STRUCTURAL REPAIR MANUAL 51-1-21 AND FAA DER APPROVED SKETCH A89-R 05. (M) 2 L 7 4 4F 4A25 1996100300561 19961003 00561 WP 1996 10 3 IXXA96137 1 19960806 A 5330 SKIN DOUG DC8 DC862 3021970 WP BS 1495 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 61CX 46142 DURING ROUTINE C-CHECK INSPECTION, THE EXTERNAL PLATING WAS FOUND TO BE CORRODED AT FUSELAGE STATION 1495 AND LONGERON 3 2 RIGHT. REPAIR OF THE PLATING WAS ACCOMPLISHED BY CUTTING OUT THE DAMAGED AREA, FABRICATING AND INSTALLING REPAIR FILL ERS AND DOUBLERS IAW THE STRUCTURAL REPAIR MANUAL AND FAA DER APPROVED DRAWING A89-R06. (M) 2 L 7 4 4F 4A25 1996100300562 19961003 00562 WP 1996 10 3 IXXA96138 1 19960723 A 2710 BUS LINKS DOUG DC8 DC862 3021970 WP RT AILERON CRACKED A IXXA K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 SW 11 61CX 46142 DURING ROUTINE C-CHECK INSPECTION, THE RIGHT INBOARD AILERON, INBOARD BUS LINKS WERE FOUND TO BE CRACKED. THE BUS LINKS WERE REPLACED IAW THE DOUGLAS SRM AND MM. (M) 2 L 7 4 4F 4A25 1996100300563 19961003 00563 WP 1996 10 3 IXXA96139 1 19960722 A 5313 56153281 LONGERON DOUG DC8 DC862 3021970 WP LT MLG WW CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 61CX 58805 46142 DURING ROUTINE C-CHECK INSPECTION, THE LEFT LONGERON 24 WAS FOUND CRACKED IN THE WING ATTACH BOTTLE BOLT AREA. THE LONG ERON WAS REPLACED IAW THE DOUGLAS REPLACEMENT GUIDE AND THE SRM. (M) 2 L 7 4 4F 4A25 1996100300564 19961003 00564 WP 1996 10 3 IXXA96140 1 19960722 A 5312 97516493 BULKHEAD DOUG DC8 DC862 3021970 WP BS 680 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 61CX 58805 3096 46142 DURING ROUTINE C-CHECK INSPECTION, THE PRESSURE BULKHEAD (CABLE FEED THROUGH) AT FUSELAGE STATION 680 WAS FOUND TO BE CR ACKED AT LONGERON 27 LEFT. THE BULKHEAD WAS REPLACED IAW THE AIRCRAFT SRM. (M) 2 L 7 4 4F 4A25 1996100300565 19961003 00565 WP 1996 10 3 IXXA96141 1 19960722 A 5720 57500922 FITTING DOUG DC8 DC862 3021970 WP RT MLG WW CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 61CX 58805 3096 46142 DURING ROUTINE C-CHECK INSPECTION, THE RIGHT MAIN LANDING GEAR TORQUE TUBE SUPPORT FITTING WAS FOUND TO BE CRACKED. THE FITTING WAS REPLACED IAW THE STRUCTURAL REPAIR MANUAL. (M) 2 L 7 4 4F 4A25 1996100300566 19961003 00566 WP 1996 10 3 IXXA96142 1 19960722 A 5743 56114252 FITTING DOUG DC8 DC862 3021970 WP RT MLG WW CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 61CX 58805 3096 46142 DURING ROUTINE C-CHECK INSPECTION, THE RIGHT MAIN LANDING GEAR FITTING WAS FOUND CRACKED. THE FITTING WAS REPLACED IAW THE DOUGLAS SRM AND FITTING REPLACEMENT GUIDE. (M) 2 L 7 4 4F 4A25 1996100300567 19961003 00567 WP 1996 10 3 IXXA96143 1 19960722 A 5730 PLATING DOUG DC8 DC862 3021970 WP RT WING CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 61CX 58805 3096 46142 DURING ROUTINE C-CHECK INSPECTION, THE RIGHT WING LEADING EDGE PLATING WAS FOUND CRACKED AT THE INBOARD STUB WING, INBOA RD END. THE CRACK WAS REPAIRED IAW THE DOUGLAS SRM 57-2-1. (M) 2 L 7 4 4F 4A25 1996100300568 19961003 00568 WP 1996 10 3 IXXA96144 1 19960723 A 5751 PLATING DOUG DC8 DC862 3021970 WP RT AILERON CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 61CX 46142 DURING ROUTINE C-CHECK INSPECTION, THE RIGHT OUTBOARD AILERON LOWER PLATING ON THE INBOARD SIDE WAS FOUND TO BE CORRODED . REPAIR TO THE AREA WAS ACCOMPLISHED IAW THE STRUCTURAL REPAIR MANUAL 57-10-0. (M) 2 L 7 4 4F 4A25 1996100300569 19961003 00569 WP 1996 10 3 IXXA96145 1 19960723 A 5330 SKIN DOUG DC8 DC862 3021970 WP CARGO DR OPENING CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 61CX 58805 3096 46142 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND IN THE EXTERNAL FUSELAGE PLATING AT THE FORWARD UPPER CORNER OF THE FORWARD LOWER CARGO DOOR OPENING. THE CRACK WAS REMOVED BY CUTOUT, AND FABRICATION AND INSTALLATION OF A FILLER AND RE PAIR DOUBLERS IAW THE STRUCTURAL REPAIR MANUAL 53-2-0, FIGURE 20. (M) 2 L 7 4 4F 4A25 1996100300570 19961003 00570 WP 1996 10 3 IXXA96146 1 19960722 A 5330 PLATING DOUG DC8 DC862 3021970 WP FS 225 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 61CX 58805 46142 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND IN THE EXTERNAL PLATING A FUSELAGE STATION 225 BETWEEN LONGERONS 29 AND 30 LEFT. THE CRACK WAS REPAIRED IAW THE STRUCTURAL REPAIR MANUAL. (M) 2 L 7 4 4F 4A25 1996100300571 19961003 00571 WP 1996 10 3 IXXA96147 1 19960827 A 5730 SKIN DOUG DC8 DC862 3021970 WP LT WING CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 735PL 57549 46153 DURING ROUTINE C-CHECK INSPECTION, A 6 INCH CRACK WAS FOUND AT THE LEFT WING SLOT PLATING AT STATION 341.5. THE PLATING WAS REPAIRED IAW FAA DER APPROVED DRAWING B12-R01. (M) 2 L 7 4 4F 4A25 1996100300572 19961003 00572 WP 1996 10 3 IXXA96148 1 19960827 A 5730 SKIN DOUG DC8 DC862 3021970 WP LT WING CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 735PL 57549 46153 DURING ROUTINE C-CHECK INSPECTION, THE LEFT WING CENER LEADING EDGE SLOT PLATING WAS FOUND CORRODED. REPAIR OF THE PLAT ING WAS ACCOMPLISHED IAW FAA DER APPROVED DRAWING B12-R02. (M) 2 L 7 4 4F 4A25 1996100300573 19961003 00573 WP 1996 10 3 IXXA96149 1 19960820 A 5743 56114252 FITTING DOUG DC8 DC862 3021970 WP RT MLG WW CRACKED A IXXA K NONE Z SIGNIFICANT FAILURE REPORT IN INSP/MAINT 1 SW 11 735PL 57549 8531 46153 DURING ROUTINE C-CHECK INSPECTION, THE RIGHT MAIN LANDING GEAR ATTACH FITTING WAS FOUND TO HAVE CRACKED. THE 1 INCH CRA CK IS TYPICAL AND ILLUSTRATED IN VIEW FF OF S/B 57-94. THE MAIN LANDING GEAR FITTING WAS REPLACED IAW THE SRM AND DOUGL AS FITTING CHANGE GUIDE. (M) 2 L 7 4 4F 4A25 1996100300574 19961003 00574 WP 1996 10 3 IXXA96150 1 19960820 A 5312 97516493 BULKHEAD DOUG DC8 DC862 3021970 WP BS 680 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 735PL 57549 46153 DURING ROUTINE C-CHECK INSPECTION, AN 8 INCH CRACK WAS FOUND IN THE PRESSURE BULKHEAD (CABLE FEED THROUGH) AT FUSELAGE S TATION 680 LEFT. THE PRESSURE BULKHEAD WAS REPLACED. (M) 2 L 7 4 4F 4A25 1996100300575 19961003 00575 WP 1996 10 3 IXXA96151 1 19960827 A 5751 SKIN DOUG DC8 DC862 3021970 WP RT AILERON CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 735PL 46153 DURING ROUTINE C-CHECK INSPECTION, THE RIGHT INBOARD AILERON LOWER PLATING WAS FOUND TO BE CORRODED. REPAIR TO THE PLAT ING WAS ACCOMPLISHED IAW FAA DER APPROVED REPAIR B12-R09. (M) 2 L 7 4 4F 4A25 1996100300576 19961003 00576 WP 1996 10 3 IXXA96152 1 19960827 A 5730 SKIN DOUG DC8 DC862 3021970 WP LT WING CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 735PL 57549 46153 DURING ROUTINE C-CHECK INSPECTION, THE LEFT WING, LEADING EDGE, INNER SLOT CUTOUT WAS FOUND TO BE CORRODED. REPAIR WAS ACCOMPLISHED IAW FAA DER APPROVED DRAWING B12-R03. (M) 2 L 7 4 4F 4A25 1996100300577 19961003 00577 WP 1996 10 3 IXXA96153 1 19960827 A 5730 SKIN DOUG DC8 DC862 3021970 WP LT WNG CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 735PL 57549 46153 DURING ROUTINE C-CHECK INSPECTION, A 1 INCH CRACK WAS FOUND IN THE LEFT WING LEADING EDGE, THE CRACK WAS LOCATED 6 INCHE S FORWARD OF THE FORWARD SPAR AT WING STATION XFS 422. THE DAMAGE WAS REPAIRED IAW FAA DER APPROVED DRAWING B12-R05. ( M) 2 L 7 4 4F 4A25 1996100300578 19961003 00578 WP 1996 10 3 IXXA96154 1 19960827 A 5320 CUSP DOUG DC8 DC862 3021970 WP BS 225-254 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 735PL 57549 46153 DURING ROUTINE C-CHECK INSPECTION, THE RIGHT CUSP EXTRUSTION WAS FOUND CORRODED BETWEEN FUSELAGE STATIONS 225 AND 245. T HE CUSP WAS REPAIRED IAW FAA DER APPROVED DRAWING B12-R10. (M) 2 L 7 4 4F 4A25 1996100300579 19961003 00579 WP 1996 10 3 IXXA96156 1 19960906 A 2550 CONTAINER DOUG DC8 DC871F 302199D WP CARGO COMPT DAMAGED A IXXA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SW 11 821BX 45811 ON TAKEOFF ROLL, DEPARTING LRD, POSITION 6 CONTAINER SHIFTED AFT, DUE TO ITS BASE BEING DISTORTED, JUMPING OVER THE FULL Y ERECTED LOCKS TO POSITION 8. CREW ACCOMPLISHED REJECTED TAKEOFF PROCEDURE AND RETURNED TO THE BLOCKS. THE CONTAINER WAS DOWNLOADED AND REPLACED. MAINTENANCE PERFORMED A REJECTED TAKEOFF INSPECTION AND THE AIRCRAFT WAS RETURNED TO SERVI CE. (M) 2 L 7 4 4F RT 4A25 1996100300580 19961003 00580 WP 1996 10 3 IXXA96157 1 19960909 A 2121 X702256D FAN DOUG DC8 DC862 3021970 WP AIR COND BAY FAILED A IXXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 11 728PL 45918 AFTER TAKEOFF, AN ACRID ELECTRICAL SMELL ACCOMPANIED WITH SMOKE WAS DETECTED BY THE FLIGHT CREW. THE RECIRCULATION FANS WERE TURNED OFF AND THE SMOKE AND SMELL DISIPATED. MAINTENANCE INSPECTED BOTH FANS AND FOUND THE RIGHT FAN APPEARED TO BE OVERHEATED AND AT FAULT. THE FAN WAS DEFERRED AND THE AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 4 4F 4A25 1996100300581 19961003 00581 EU 1996 10 3 JBXA9600017 1 19960901 A 3231 SOLENOID FOKKER F28 F28MK0100 4990807 EU GEAR HANDLE OUT OF ADJUST A JBXA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 05 131ML 11323 RDU - FLT 301 - GEAR WOULD NOT RETRACT NORMALLY, ON USING OVERRIDED FUNCTION, MOVEMENT OF HANDLE SEEMED ROUGH. SUBMITTE R STATES, REPEAT GRIPE FROM YESTERDAY. REMOVED AND INSPECTED AND ADJUSTED LANDING GEAR SELECTOR SOLENOID IAW AMM 32-31- 02 OPS CHECK OK (M) 2 L 7 2 4F RT 1996100300582 19961003 00582 SW 1996 10 3 MALA965082 1 19960726 A 3260 1EN516 SWITCH SWRNGN SA227 SA227AC 8780603 SW NLG DIRTY A MALA O OTHER J WARNING INDICATION CL CLIMB 1 GL 15 436MA AC719B FLT NR 3329 - ON DEPARTURE FROM TOL, THE NOSE GEAR INTRANSIT LIGHT DID NOT ILLUMINATE UPON RETRACTION. AIRCRAFT CONTINU ED TO DTW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE UPLOCK SWITCH TO BE STICKING. SWITCH WAS CLEANED AND LUBED AND GEAR SWINGS WERE COMPLETED. ALL CHECKS WERE GOOD. (M) 2 L 7 2 4T RT A8SW 1996100300583 19961003 00583 SW 1996 10 3 MALA965099 1 19960816 A 5320 2724087901 CORNER SWRNGN SA227 SA227AC 8780603 SW PAX DOOR FRAME DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 438MA AC721B DURING SCHEDULED MAINTENANCE IN MSP, FOUND THE LOWER FORWARD PASSENGER DOOR FRAME CORNER TO BE DENTED. MAINTENANCE REPL ACED THE LOWER FORWARD FUSELAGE PASSENGER DOOR FRAME CORNER, P/N 27-24087-901, IAW WITH SRM 51-30-02, 51-30-03, 51-40-02 , AND 51-00-00 PAGE 4. (M) 2 L 7 2 4T RT A8SW 1996100300584 19961003 00584 NM 1996 10 3 MALA965100 1 19960820 A 2421 31708001A GENERATOR DHAV DHC8 DHC8102 2809003 NM LT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 848MA 346 FLT 3390 - EN ROUTE FROM DTW, THE LEFT STALL WARNING, TRU AND NR 1 AC GENERATOR CAUTION LIGHTS ILLUMINATED. THE AIRCRAF T RETURNED TO DTW. MAINTENANCE REPLACED THE LEFT AC GENERATOR. ALL CHECKS SATISFACTORY. (M) 2 H 7 2 4T RT A13NM 1996100300585 19961003 00585 NM 1996 10 3 MALA965101 1 19960822 A 3350 1005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 861MA 362 FLT 3107 - DURING THE POST FLIGHT, THE COCKPIT OVERHEAD EMERGENCY LAMP ASSEMBLY WAS INOPERATIVE. MAINTENANCE REPLACED T HE ASSEMBLY. (M) 2 H 7 2 4T RT A13NM 1996100300586 19961003 00586 NM 1996 10 3 MALA965102 1 19960825 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 833MA 343 FLT 3378 - DURING THE PREFLIGHT IN DTW, THE COCKPIT OVERHEAD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE R EPLACED THE EMERGENCY EXIT LAMP ASSEMBLY. ALL CHECKS SATISFACTORY. (M) 2 H 7 2 4T RT A13NM 1996100300587 19961003 00587 NM 1996 10 3 MALA965104 1 19960827 A 5210 SKIN DHAV DHC8 DHC8102 2809003 NM PAX DOOR DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 859MA 361 DURING A C-CHECK INSPECTION IN INT, THE PASSENGER DOOR OUTER SKIN HAD DENTS THAT WERE OUT OF LIMITS. REPAIRS WERE COMPL ETED IAW DEHAVILLAND RD8-52-040, INSTALLATION OF REPAIR DOUBLER AND REMOVAL OF DENTED SKIN. (M) 2 H 7 2 4T RT A13NM 1996100300588 19961003 00588 SW 1996 10 3 MALA965107 1 19960901 A 2150 20475546 COOLING TURBINE SWRNGN SA227 SA227AC 8780603 SW CABIN FAILED A MALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 15 422MA AC635 FLT 3092 - ON CLIMB-OUT FROM DTW, CREW REPORTED SMOKE IN THE CABIN. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE VERIFIED RIGHT COOLING TURBINE TO BE AT FAULT. RIGHT AIR CONDITIONING SYSTEM WAS DEFERRED, AND AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A8SW 1996100300589 19961003 00589 SW 1996 10 3 MALA965109 1 19960904 A 5230 1127491 HANDLE SWRNGN SA227 SA227AC 8780603 SW CARGO DOOR WORN A MALA K NONE O OTHER TX TAXI/GRND HDL 1 GL 15 425MA AC640 FLT 3095 - ON TAXI, CREW REPORTED THE CARGO DOOR WARNING LIGHT ILLUMINATED. MAINTENANCE FOUND THE CARGO DOOR EXTERNAL H ANDLE WORN AND THE HANDLE RETURN SPRING WEAK. MAINTENANCE REPLACED THE EXTERNAL HANDLE AND RETURN SPRING. OPS CHECK OF THE HANDLE AND CARGO DOOR WARNING SYSTEM CHECKED GOOD. (M) 2 L 7 2 4T RT A8SW 1996100300590 19961003 00590 SW 1996 10 3 MALA965110 1 19960831 A 5712 2731523 RIB SWRNGN SA227 SA227AC 8780603 SW WS 27.03 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 421MA AC634 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND AT WS 27.03 RIGHT AFT WING RIB TRAILING EDGE (P/N 27-31523), A . 25 INCH CRACK. COMPLETED REPAIR PER FAC SRM 57-90-10 PAGES 3-6, REV NOV 1/94 BY INSTALLING A 4 INCH BY 2.5 INCH REPAIR DOUBLER TO AFFECTED AREA. (M) 2 L 7 2 4T RT A8SW 1996100300591 19961003 00591 SW 1996 10 3 MALA965111 1 19960831 A 5720 ANGLE SWRNGN SA227 SA227AC 8780603 SW RT WING/NACELLE CRACKED A MALA O OTHER O OTHER IN INSP/MAINT 1 GL 15 421MA AC634 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE RIGHT OUTBOARD UPPER WING TO NACELLE ATTACH ANGLE CRACKED IN TWO LOCATIONS. FABRICATED NEW ANGLE USING LIKE MATERIAL AND THICKNESS. INSTALLED ANGLE IAW FAIRCHILD SRM 51-00-00 PAG E 4 'PART FOR PART REPLACEMENT', 51-30-02, 51-40-01, AND 51-40-02 REV JUN 1/93. (M) 2 L 7 2 4T RT A8SW 1996100300592 19961003 00592 WP 1996 10 3 ORJA9648 1 19960805 A 3350 41B994AD073 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 875RA 53182 EMPENNAGE WALKWAY OVERHEAD EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK. OPS NORMAL. (M) 2 L 7 2 4F RT A6WE 1996100300593 19961003 00593 WP 1996 10 3 ORJA9649 1 19960809 A 7920 626447 PRESS RELIEF VLV DOUG DC9 DC983 3022083 WP LT ENG FAILED A ORJA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 11 879RA 53185 DURING TAXI, LEFT ENGINE OIL PRESSURE DROPPED BELOW 40 PSI. SHUT DOWN ENGINE, RETURNED TO GATE. REPLACED LEFT ENGINE O IL PRESSURE RELIEF VALVE IAW MAINTENANCE MANUAL 79-20-03. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1996100300594 19961003 00594 WP 1996 10 3 ORJA9650 1 19960831 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN BROKEN A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 842RA 49604 UPON ARRIVAL INTO SJC, WHEN ELECTRICAL POWER DISCONNECTED, THE FIRST CLASS SECTION OF FLOOR LEVEL EMERGENCY LIGHTS WOULD NOT ILLUMINATE. LATER TESTS PROVED SAME RESULTS. REPAIRED FLOOR TRACK ELECTRICAL CONNECTION FOR FIRST CLASS EMERGENCY LIGHTS. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1996100300595 19961003 00595 EU 1996 10 3 REXA96032 1 19960721 A 2611 SMOKE DETECTOR FENWAL 72111211000 SAAB SF340 340B 7860101 EU CARGO COMPT DIRTY A REXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 363PX A2102 340B260 CARGO SMOKE WARNING. CREW DECLARED EMERGENCY AND BLEW BOTTLE. DEFERRED CARGO FIRE EXTINGUISHER SYSTEM. REPLACED CARGO FIRE BOTTLE AND SQUIB. DEFER CLEARED. REPLACED AFT AND FWD CARGO SMOKE DETECTOR, CHECKS GOOD. (M) 2 L 7 2 4T RT A52EU 1996100300596 19961003 00596 EU 1996 10 3 REXA96033 1 19960730 A 2611 SMOKE DETECTOR FENWAL 72111211000 SAAB SF340 340B 7860101 EU CARGO COMPT DIRTY A REXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 363PX 340B260 CARGO SMOKE LIGHT ILLUMINATED IN FLIGHT. CARGO FIRE EXTINGUISHER BOTTLE WAS FIRED. REMOVED AND REPLACED CARGO SMOKE DE TECTOR ON LAV WALL (FWD), OPS CHECK GOOD. OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1996100300597 19961003 00597 EU 1996 10 3 SIMA962511 1 19960907 A 3260 D49412001 CONTROL PANEL SAAB SF340 340B 7860101 EU LANDING GEAR FAILED A SIMA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SW 21 374AE 1884 5730394 340B374 DFW - FLT 3582 - GEAR INTRANSIT LIGHT CAME ON DURING TAXI. RAI'D LANDING GEAR CONTROL PANEL. OPS CHECKED GOOD. AIRCRA FT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1996100300598 19961003 00598 NM 1996 10 3 TAOA089604 1 19960814 A 5754 SKIN BOEING 727 727254 138408L NM NR 4 LE SLAT CRACKED A TAOA K NONE O OTHER IN INSP/MAINT 1 EA 15 912TS 20438 FOUND NR 4 LEADING EDGE SLAT, P/N 651622171, HAS 2.5 INCH TO 3 INCH CRACK ON LOWER TRAILING EDGE AT OUTBOARD EDGE OF SKI N. (M) 2 L 7 3 4F A3WE 1996100300600 19961003 00600 NM 1996 10 3 TAOA099602 1 19960905 A 3350 0L3071BPEGPL LAMP GRIMES BOEING 727 727254 138408L NM CABIN MISSING A TAOA K NONE O OTHER IN INSP/MAINT 1 EA 15 912TS 20438 EMERGENCY PATH LIGHTING, AT ROW 18, MISSING BULB AND LENS. REPLACED BULB AND LENS. (M) 2 L 7 3 4F A3WE 1996100300601 19961003 00601 NM 1996 10 3 TAOA099603 1 19960908 A 7930 42D107A2 BYPASS SWITCH BOEING 727 727254 138408L NM NR 3 ENGINE INOPERATIVE A TAOA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 EA 15 916TS 3155 20437 NR 3 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED FIVE MINUTES AFTER TAKEOFF, OIL PRESSURE AND QUANTITY WERE NORMAL. ENGI NE WAS SHUT DOWN AND WINDMILLED AT GREATER THAN 10 PSI OIL PRESSURE FOR 10 MINUTES. REPLACED NR 3 OIL FILTER BYPASS LIG HT SWITCH AND MAIN OIL FILTER, CHECKS OK IAW MM CHAP 79-33-02. (M) 2 L 7 3 4F A3WE 1996100300602 19961003 00602 NM 1996 10 3 TSAA9650070 1 19960906 A 5320 CLIP BOEING 737 737297 1384480 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 726AL 22426 DURING HEAVY MAINTENACNE VISIT, FOUND STRINGER TO FRAME TIE CLIP CRACKED AT BS 685-S1L, BS 727A-S1R, BS 727A-S3L, BS 727 B-S34, AND BS 727B-S4R. REPLACED TIE CLIPS PER ECO 1897R2. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1996100300603 19961003 00603 NM 1996 10 3 TSAA9653069 1 19960906 A 5320 CLIP BOEING 737 737297 1384480 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 726AL 22426 DURING HEAVY MAINTENANCE VISIT, FOUND STRINGER TO FRAME TIE CLIP CRACKED AT BS 727B-S5R, BS 787-S3R, BS 767-S3R, BS 597- S1R, AND SHEARED RIVET HEAD AT BS 727B-S3L. REPLACED TIE CLIPS PER ECO1897R2. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1996100300604 19961003 00604 NM 1996 10 3 TSAA9655066 1 19960906 A 5510 BEAM BOEING 737 737297 1384480 NM HORIZ STAB CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 726AL 22426 DURING HEAVY MAINTENANCE VISIT, EXFOLIATION NOTED ON RIGHT HORIZONTAL STABILIZER T/E SUPPORT BEAM (TOP) BETWEEN BS 66.54 -94.07. REPAIRED PER ECO2306 PART 1 WITH DEVIATION D. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1996100300605 19961003 00605 NM 1996 10 3 TSAA9657067 1 19960906 A 5711 SPAR BOEING 737 737297 1384480 NM WSS 148 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 726AL 22426 DURING HEAVY MAINTENANCE VISIT, FOUND CORROSION BULGE ALONG FRONT SPAR LOWER CHORD, SS 148 LEFT WING. REPAIRED PER ECO 2135R1. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1996100300606 19961003 00606 NM 1996 10 3 TSAA9657068 1 19960906 A 5711 SPAR BOEING 737 737297 1384480 NM WSS 133/145 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 726AL 22426 DURING HEAVY MAINTENANCE VISIT, RIGHT WING CORROSION NOTED ON BOTTOM SIDE OF LOWER CHORD OF FRONT SPAR, SS133 AND 145. R EPAIRED PER ECO2135R1. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1996100300607 19961003 00607 NM 1996 10 3 TWRA96300 1 19960826 A 3397 WIRE BOEING 747 747136 1384883 NM CABIN BROKEN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 606FF 20273 DURING DAILY CHECK, FOUND 'B' ZONE RIGHT SIDE EVAC LIGHTS INOP. REPLACED AND SECURED BROKEN WIRE AT 'B' ZONE RIGHT SIDE PER MM 33-51-00. OPS CHECKED NORMAL. (M) 2 L 7 4 4F A20WE 1996100300610 19961003 00610 NM 1996 10 3 TWRA96305 1 19960901 A 3397 WIRE BOEING 747 747212B 1384886 NM CABIN DISCONNECTED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND B-ZONE EVAC FLOOR STRIP BOTH SIDES AND R2 AND L2 EXIT SIGN IS INOP. FOUND WIRES DISCONNECTED AT FWD PART OF AISLE. RECONNECTED, OPS CHECKED GOOD PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996100300611 19961003 00611 NM 1996 10 3 TWRA96307 1 19960903 A 3397 WIRE BOEING 747 747136 1384883 NM CABIN BROKEN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 606FF 20273 DURING DAILY CHECK, FOUND 'E' PATH AND EXIT SIGN AT STAIRCASE INOP. REPAIRED BROKEN WIRE. OPS CHECKED GOOD PER MM 33-5 1-00. (M) 2 L 7 4 4F A20WE 1996100300612 19961003 00612 NM 1996 10 3 TWRA96308 1 19960901 A 3397 WIRE BOEING 747 747124 1384874 NM CABIN BROKEN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 602FF 19734 DURING DAILY CHECK, FOUND SEAT 35C EVAC LIGHT INOP. REPAIRED BROKEN WIRE AT SEAT HARNESS. OPS CHECKED NORMAL PER MM 33 -51-00. (M) 2 L 7 4 4F A20WE 1996100300613 19961003 00613 NM 1996 10 3 TWRA96309 1 19960904 A 3350 S1356B37 LIGHT BOEING 747 747238B 1384828 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 607PE 2428 20011 DURING DAILY CHECK, FOUND EMERGENCY LIGHT INOP AT L4 DOOR. REMOVED AND REPLACED LIGHT ASSY. OPS CHECKED NORMAL PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996100300614 19961003 00614 NE 1996 10 3 UIEA9610 2 19960830 A 7320 747306 PS4 TUBE BOEING 747 747245F 1384897 NM PWA JT9 JT9D70A 52054 NE NR 3 ENG BROKEN A UIEA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 EA 15 638FE 21841 689150 EN ROUTE GRV-MEX - FLIGHT NR VG986 - NR 3 ENGINE FLAMEOUT FL 310. AIRCRAFT DIVERTED TO MAO DUMPED 40K FUEL. INSPECTION REVEALED A BROKEN PS4 TUBE TO THE FUEL CONTROL UNIT. FUEL FILTER SOME FOREIGN DEBRIS. REPLACE TUBE FILTER, OPS OK. ( M) 2 L 7 4 4F 4 F A20WE E3NE 1996100300615 19961003 00615 NM 1996 10 3 USAA960574 1 19960821 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 312 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 281AU 23114 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 INCH CORROSION ON T-CAP ON FLOOR BEAM STATION 312, AT BL 0. CUT OFF T -CAP, FABRICATED AND INSTALLED NEW PIECE FROM LBL 18 TO RBL 39, REPAIRED PER TR 53-107-02, CORROSION LEVEL 1. (M) 2 L 7 2 4F A16WE 1996100300616 19961003 00616 NM 1996 10 3 USAA960575 1 19960821 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 947 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 281AU 35254 23114 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER SPOTS CORROSION AT SCREW HOLES BS 947 LBL 15, 17, 18, 21 , 30, 36 AND 49 TOP OF FLOOR BEAM T-CAP. INSTALLED T-CAP REPAIR LESS THAN 1 LB WEIGHT CHANGE, REPAIRED PER TP 53-10-05C . CORROSION TASK NR C53-107-02, CORROSION LEVEL 1. (M) 2 L 7 2 4F A16WE 1996100300617 19961003 00617 NM 1996 10 3 USAA960576 1 19960822 A 5315 FLOOR BEAM BOEING 737 7374B7 1384702 NM BS 328 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 19509 24554 CLT - INSPECTION VISUALLY FOUND 1 INCH BY 1 INCH CORRODED AREA, LOCATED AT STATION 328 FLOOR BEAM AND RBL 15 - RBL 36. I NSTALLED TOE CAP EXTRUSION. REPAIRED ANGLES/STRAPS AS PER TYPICAL REPAIR MANUAL 53-10-03. (M) 2 L 7 2 4F RT A16WE 1996100300618 19961003 00618 EU 1996 10 3 USAA960598 1 19960621 A 5532 SKIN FOKKER F28 F28MK4000 4990810 EU VERT STAB CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 487US 20640 11238 YYC - DURING FC-06 CHECK, FOUND CHAF IN SKIN LEFT SIDE 4.5 INCH BY 2 INCH AND RIGHT SIDE 2.75 INCH BY 1.25 INCH FORWARD OF INTERIM SPAR 2 OF RIB 5, LEFT AND RIGHT SIDE OF VERT STAB TORSION BOX. AREAS BLENDED, FILLED, AND REPAIR PATCHES INS TALLED PER FOKKER FAX TS96.61659. (M) 2 L 7 2 4F RT A20EU 1996100300619 19961003 00619 EU 1996 10 3 USAA960599 1 19960621 A 5414 SKIN FOKKER F28 F28MK4000 4990810 EU FS 2103-2738 BUCKLED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 487US 20640 11238 YYC - DURING FC-06 CHECK, FOUND AFT SKIN BUCKLED TOP RIGHT NACELLE BETWEEN FRAME 2103-2738. INSTALLED DOUBLER PER FOKKE R TS96.62079. (M) 2 L 7 2 4F RT A20EU 1996100300620 19961003 00620 EU 1996 10 3 USAA960600 1 19960621 A 5320 DOUBLER FOKKER F28 F28MK4000 4990810 EU HYD SERV PNL CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 487US 20640 11238 YYC - DURING FC-06 CHECK, FOUND DOUBLER HAS SMALL CRACKS ON EDGE OF HYD SERVICE PANEL CUT OUT. INSTALLED DOUBLER PER FO KKER TS 96.61580/JE. (M) 2 L 7 2 4F RT A20EU 1996100300621 19961003 00621 WP 1996 10 3 USAA960604 1 19960913 A 5320 99100789 CUSP DOUG DC9 DC931 3022065 WP BS 598-617 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 963VJ 64847 47508 PIT - DURING Q4/C6 CHECK, FOUND CRACKED MEMBRANE AT STATION 598 TO STATION 617 RIGHT SIDE. REMOVED CRACKED MEMBRANE AND MFG NEW SECTION OF MEMBRANE 2024 T-3 .032 PER SRM 53-05 FIG 96, 97. (M) 2 L 7 2 4F A6WE 1996100300622 19961003 00622 WP 1996 10 3 USAA960605 1 19960913 A 5320 99100789 CUSP DOUG DC9 DC931 3022065 WP BS 180-204 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 963VJ 64847 47508 PIT - DURING Q4/C6 CHECK, FOUND CORROSION 3 INCH BY 3 INCH AREA CORRODED CUSP MEMBRANE AT STATION 204 LT TO STATION 180. INSTALLED NEW CUSP SECTION AND ADDED DOUBLERS 7075 PLUS 6 071 AND 7075 PLUS 6 .080 PER EA NR 33169/SRM 53-05 FIG 55. ( M) 2 L 7 2 4F A6WE 1996100300623 19961003 00623 WP 1996 10 3 USAA960606 1 19960916 A 5530 9911885511 FRAME DOUG DC9 DC931 3022065 WP VERT STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 974VJ 74679 47130 PIT - DURING Q-3/C2 CHECK, FOUND .5 INCH CRACK IN LOWER FIXED LEADING EDGE FRAME 5 OF VERTICAL STABILIZER. REPLACED DEF ECTIVE PART WITH IDENTICAL PART NR 991188511. (M) 2 L 7 2 4F A6WE 1996100300624 19961003 00624 WP 1996 10 3 USAA960607 1 19960916 A 5530 991188411 FRAME DOUG DC9 DC931 3022065 WP VERT STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 974VJ 74679 47130 PIT - DURING Q-3/C2 CHECK FOUND .5 INCH CRACK AT LOWER FIXED LEADING EDGE FRAME 4 OF VERTICAL STABILIZER. REPLACED DEFE CTIVE PART WITH IDENTICAL PART NR 991188411. (M) 2 L 7 2 4F A6WE 1996100300625 19961003 00625 NM 1996 10 3 USAA960609 1 19960913 A 5241 SKIN BOEING 737 737201 1384454 NM FWD GALLEY DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 226US 45760 21815 ROA - DURING 'CX-3' CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND .125 INCH CRACK FORWARD GALLEY DOOR CUT OUT AFT LOWER CO RNER FUSELAGE SKIN. REMOVED CRACK AND INSTALLED DOUBLER. REPAIRED PER TYPICAL REPAIR 53-10-19 REV A. (M) 2 L 7 2 4F A16WE 1996100300626 19961003 00626 NM 1996 10 3 USAABB96025 1 19960823 A 2897 W33063502Y20 WIRE BOEING 757 7572B7 1384964 NM LT SPAR VLV SHORTED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 633AU 27811 PIT - FL 114 - AFTER TAKEOFF FROM PIT, CREW RECEIVED EICAS MESSAGE 'L FUEL SPAR VAL'. FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE WIRE TO THE SPAR VALVE AT THE CONNECTOR SHORTING TO THE SHIELDING. TH E WIRE WAS REPAIRED. (M) 2 L 7 2 4F RT A2NM 1996100300627 19961003 00627 NM 1996 10 3 USAABB96026 1 19960824 A 3350 8731002511 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 619AU 27198 PHL - LEFT AFT EMERGENCY IDENTIFIER INOPERATIVE. REPLACED IDENTIFIER. (M) 2 L 7 2 4F RT A2NM 1996100300628 19961003 00628 NM 1996 10 3 USAABB96027 1 19960827 A 2612 FIRE WARNING BOEING 767 767201 1385125 NM LT ENG ACTIVATED A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 649US 23901 PIT - FL 3 - AT CRUISE ALTITUDE, CREW RECEIVED EICAS MESSAGE, 'L ENG FIRE LP2'. THE LEFT FIRE LOOP NR 1 WAS ALREADY ON MEL. FLIGHT DIVERTED TO PIT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE PERFORMED THE FIM PROCEDURE 926-11-00, FI G 104) AND COULD NOT DUPLICATE THE PROBLEM. AFOLTS CARDS WERE SWAPPED (LEFT TO RIGHT) PER THE FIM. (M) 2 L 7 2 4F RT A1NM 1996100300629 19961003 00629 NM 1996 10 3 USAABB96028 1 19960909 A 3260 834802 LOCKED SENSOR BOEING 757 757225 1384959 NM NLG FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 605AU 22201 CLT - FLT 8081 - AFTER TAKEOFF AND GEAR RETRACTION, CREW RECEIVED THE EICAS MESSAGES 'LDG GEAR MONITOR' AND GEAR DISAGRE E'. FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 SYSTEM NOSE GEAR LOCKED SENSOR AND ADJUSTED THE NR 1 SYSTEM SENSOR. GEAR WAS SWUNG WITH NO FURTHER PROBLEMS. (M) 2 L 7 2 4F RT A2NM 1996100300630 19961003 00630 NM 1996 10 3 USAABB96031 1 19960916 A 5210 411N221351 DOOR SEAL BOEING 757 757225 1384959 NM RT FWD DOOR LOOSE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 609AU 22205 PHL - FLT 79 - AFTER TAKEOFF, RIGHT FORWARD DOOR ANNUNCIATOR LIGHT ILLUMINATED. AIRCRAFT WOULD NOT HOLD PRESSURIZATION. FLIGHT RETURNED TO PHL AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE DOOR SEAL LOOSE AND IN THE DOOR TRA CK. SEAL WAS REINSTALLED. (M) 2 L 7 2 4F RT A2NM 1996100300631 19961003 00631 NM 1996 10 3 USAABB96032 1 19960917 A 3350 8731002511 LIGHT BOEING 757 7572B7 1384964 NM R1 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 633AU 27811 SFO - EMERGENCY EXIT IDENTIFIER INOPERATIVE. REPLACED EMERGENCY IDENTIFIER. (M) 2 L 7 2 4F RT A2NM 1996100300632 19961003 00632 NE 1996 10 3 USAAD96118 2 19960822 A 7200 ENGINE DOUG DC9 DC981 3022081 WP PWA JT8 JT8D217 52053 NE LEFT FAILED A USAA E ENGINE SHUTDOWN E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS DE DESCENT 1 EA 19 805US 48053 708514 FLT 790 - CLT-IND - DURING DESCENT, HEARD A LOUD THUMP, FELT VIBRATION, AND LOST POWER IN LEFT ENGINE. SHUT DOWN LEFT E NGINE. SHUT DOWN ENGINE. SET = 10 MINUTES. REPLACED ENGINE. (M) 2 L 7 2 4F 4 F A6WE E9NE 1996100300633 19961003 00633 WP 1996 10 3 USAAD96120 1 19960825 A 3350 60030451LB BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 991VJ 47310 CEILING EMERGENCY LIGHTS BETWEEN ROWS 5-9 INOPERATIVE. REPLACED BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1996100300634 19961003 00634 WP 1996 10 3 USAAD96121 1 19960828 A 3350 60030451LB BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 923VJ 48143 EMERGENCY LIGHT AT MAIN ENTRANCE DOOR INOPERATIVE. REPLACED BATTERY PACK. (M) 2 L 7 2 4F A6WE 1996100300635 19961003 00635 WP 1996 10 3 USAAD96122 1 19960828 A 2410 696233B CSD DOUG DC9 DC931 3022065 WP NR 1 FAILED A USAA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 EA 19 978VJ 70202 262 47371 FLT 1611 - PH-YUL - AFTER TAKEOFF, WITH APU GENERATOR ON MEL, THE NR 1 GENERATOR FAILED. RETURNED TO FIELD. REPLACED N R 1 CSD. (M) 2 L 7 2 4F A6WE 1996100300636 19961003 00636 NE 1996 10 3 USAAD96124 2 19960902 A 7230 COMP BLADES DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE LT ENGINE FOD DAMAGE A USAA A UNSCHED LANDING R C PARTIAL RPM/PWR LOSS F.O.D. CL CLIMB 1 EA 19 817US 48097 708120 FLT 1224 - ATL-PIT - LEFT ENGINE COMPRESSOR STALLS ON CLIMB-OUT FROM ATL. RETURNED TO FIELD. NO ENGINE SHUTDOWN. FOUN D FOD DAMAGE TO 7TH STAGE COMPRESSOR BLADES. REPLACED ENGINE. (M) 2 L 7 2 4F 4 F A6WE E9NE 1996100300637 19961003 00637 WP 1996 10 3 USAAD96125 1 19960907 A 5210 CFH58S BUSHING DOUG DC9 DC982 3022082 WP 2L DOOR FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 823US 49142 FLT 2382 - MCO-DCA - AIRCRAFT WOULD NOT PRESSURIZE ON TAKEOFF, 2L DOOR APPEARED NOT TO SEAL PROPERLY. REPLACED 2L DOOR MECHANISM BUSHING AND SPRING FROM BAYONET. (M) 2 L 7 2 4F A6WE 1996100300638 19961003 00638 WP 1996 10 3 USAAD96129 1 19960916 A 7931 1163P0041 SWITCH DOUG DC9 DC931 3022065 WP NR 2 ENGINE LEAKING A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 987VJ 72768 35910 47210 FLT 2371 - CLT-BHM - NR 2 ENGINE OIL QUANTITY STARTED DROPPING IN FLIGHT. RETURNED TO CLT. NO ENGINE SHUTDOWN. FOUND NR 2 OIL PRESSURE SWITCH LEAKING. REPLACED SWITCH. (M) 2 L 7 2 4F A6WE 1996100300639 19961003 00639 WP 1996 10 3 USAADB96123 1 19960901 A 2133 54447211 OUTFLOW VLV ACT DOUG DC9 DC931 3022065 WP CABIN FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 971VJ 20440 47051 FLT 1422 - ROC-CLT - CABIN WOULD NOT PRESSURIZE AFTER TAKEOFF. RETURNED TO FIELD. REPLACED OUTFLOW VALVE ACTUATOR. (M ) 2 L 7 2 4F A6WE 1996100300640 19961003 00640 EU 1996 10 3 USAAF96097 1 19960908 A 2150 9785606 BYPASS VLV FOKKER F28 F28MK0100 4990807 EU LEFT TURBINE FAILED A USAA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 EA 19 882US 11334 RDU-PIT - FLT 1423 - ON CLIMB GOING THROUGH FL 100, PACK CABIN SUPPLY TEMP WENT TO 100F EVEN WITH TEMP SELECT FULL COLD. ONE PACK WAS ON MEL AS WELL AS APU BLEED AIR. AIRCRAFT DIVERTED TO GSO. NO FURTHER INCIDENTS. MAINTENANCE REPLACED LEFT BYPASS VALVE. (M) 2 L 7 2 4F RT 1996100300641 19961003 00641 EU 1996 10 3 USAAF96098 1 19960907 A 3350 0158500501 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 488US 11240 CLT - EMERGENCY EXIT LIGHT IS BROKEN ON ROW 8 BY SEAT A. MAINTENANCE REPLACED LEFT EMERGENCY DOOR VERTICAL EXIT SIGN. ( M) 2 L 7 2 4F RT A20EU 1996100300642 19961003 00642 EU 1996 10 3 USAAF96099 1 19960912 A 3350 MGG104406 LAMP FOKKER F28 F28MK0100 4990807 EU CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 885US 11345 PIT - EMERG EXIT LIGHT BY SEAT 12AC BURNED OUT. MAINTENANCE RELAMPED THE LIGHT. (M) 2 L 7 2 4F RT 1996100300643 19961003 00643 EU 1996 10 3 USAAF96100 1 19960913 A 3350 MGG104406 LAMP FOKKER F28 F28MK0100 4990807 EU CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 883US 11337 CLT - EMERGENCY EXIT LIGHT, ROW 11F, INOP. MAINTENANCE RELAMPED LIGHT. (M) 2 L 7 2 4F RT 1996100300644 19961003 00644 NM 1996 10 3 USAASB96165 1 19960821 A 2170 V1211 COALESCER BAGS BOEING 737 7373B7 1384580 NM AIR COND BAY DIRTY A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 505AU 23380 TPA - FL 1291 - APPROXIMATELY 30 MINUTES PRIOR TO LANDING, AN UNUSUAL ODOR WAS DETECTED IN THE MID CABIN. ALL COCKPIT I NDICATIONS WERE NORMAL. THE DOOR DISSIPATED DURING DESCENT AND THE FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE INSPECTED AND CHECKED THE INSIDE OF THE CABIN WITH THE PACKS ON. NO ODOR WAS DETECTED. REMOVED AND REPLACED LEFT AND RIGHT WATER SEPARATOR COALESCER BAGS. (M) 2 L 7 2 4F RT A16WE 1996100300645 19961003 00645 NM 1996 10 3 USAASB96166 1 19960822 A 3610 32895624 TEMP CONTL BOEING 737 7374B7 1384702 NM LT ENGINE MALFUNCTIONED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 782AU 25021 PHL - FL 1268 - CAPTAIN REPORTED, THAT THE LEFT ENGINE BLEED AIR VALVE WOULD NOT OPEN AT TAKEOFF POWER. RECYCLED SWITCH AND CIRCUIT BREAKER WITH NO HELP. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE RE MOVED AND REPLACED THE FOLLOWING LISTED ITEMS PER THE MM. LEAK CHECK AND OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996100300646 19961003 00646 NM 1996 10 3 USAASB96167 1 19960823 A 5210 DOOR TAPE BOEING 737 737201 1384454 NM PASSENGER DOOR DETACHED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 225US 21667 CLT - FL 1024 - CREW AND PASSENGERS HEARD A LOUD THUMPING NOISE COMING FROM THE TOP OF THE AIRCRAFT DURING CLIMB. AT AP PROX 5,000 FEET, CREW DECIDED TO RETURN TO FIELD AT CLT. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE DISCOVERE D DUCT TAPE AT UPPER RIGHT CORNER OF LEFT FORWARD ENTRY DOOR. REMOVED SAME. SUBMITTER STATES, SUSPECT TAPE CAME FROM J ETWAY CURTAIN, C-14. (M) 2 L 7 2 4F A16WE 1996100300647 19961003 00647 NM 1996 10 3 USAASB96168 1 19960822 A 2820 MS2951224 O-RING BOEING 737 7373B7 1384580 NM CTR FUEL TANK LEAKING A USAA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 505AU 23380 CLT - FLT 278 - CREW REPORTED A STRONG FUEL ODOR IN FORWARD CABIN WITH RECIRCULATION FAN ON, REGARDLESS OF PACK POSITION . WITH FAN OFF, ODOR DISSIPATED. MAINTENANCE FOUND CENTER TANK AFT FITTING (FROM AUX TANK) LEAKING. REPLACED O-RINGS AT CENTER TANK AFT FITTING. LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996100300648 19961003 00648 NM 1996 10 3 USAASB96169 4 19960824 A 3442 6225132108 TR UNIT BOEING 737 7372B7 1384560 NM FWD FUSELAGE FAILED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 284AU 10379 10379 23131 PIT - FL 2165 - AIRCRAFT WAS AT CRUISE ALTITUDE APPROXIMATELY 20 MINUTES OUT OF BWI WHEN RADAR BECAME INTERMITTENT. CAP TAIN CYCLED BREAKERS AND WEATHER RADAR WENT COMPLETELY OUT BUT STILL HAD TCAS. CAPTAIN RADIOED INTO OPERATIONS CONTROL AND AFTER FAILED ATTEMPTS TO RESET RADAR SCREEN, CAPTAIN WAS ADVISED TO DIVERT TO PIT WHERE THE FLIGHT LANDED WITH NO FU RTHER INCIDENT. MAINTENANCE REPLACED THE WEATHER RADAR TRANSCEIVER. SYSTEM OPS CHECK NORMAL. R/T COOLING FAN OPS CHEC K GOOD. (M) 2 L 7 2 4F A16WE 1996100300649 19961003 00649 EU 1996 10 3 USAASB96170 2 19960825 A 7311 6920230011 HEAT EXCHANGER BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU NR 1 ENGINE MALFUNCTIONED A USAA A UNSCHED LANDING M OVER TEMP CR CRUISE 1 EA 19 376US 22955 IND - FL 247 - FLIGHT DIVERTED TO IND DUE TO HIGH OIL TEMPERATURE READING ON THE NR 1 ENGINE. THE OIL TEMP WENT TO 140 DEGREES CELCIUS, THEN INTO RED BAND AND BACK TO YELLOW. WHEN THROTTLE WAS RETARDED, TEMP WAS IN THE HIGH GREEN BAND. NO EMERG WAS DECLARED AND THE FLT LANDED WITH NO FURTHER INCIDENT. THE NR 1 ENGINE WAS NOT SHUT DOWN. MAINTENANCE REPLAC ED THE NR 1 ENGINE OIL/FUEL HEAT EXCHANGER AND THE OIL TEMP BULB PER THE MM. DRAINED AND REFILLED OIL TANK. RAN ENGINE . OP CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F 4 F RT A16WE E21EU 1996100300650 19961003 00650 NM 1996 10 3 USAASB96172 1 19960831 A 3350 1000679 LIGHT BOEING 737 7372B7 1384560 NM SERVICE DOOR FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 281AU 23114 PIT - FL 902 - CREW REPORTED, THE EMERGENCY EXIT LIGHT ABOVE THE FORWARD SERVICE DOOR IS INOP. MAINTENANCE REPLACED THE LIGHT ASSEMBLY ABOVE THE FORWARD SERVICE DOOR. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1996100300651 19961003 00651 NM 1996 10 3 USAASB96173 1 19960831 A 3350 20121 POWER SUPPLY BOEING 737 737301 1384611 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 584US 23743 ALB - MAINTENANCE FOUND THE LOW LEVEL EMERGENCY LIGHTS AT ROWS 5 THROUGH 8 INOP AND THE LEFT OVERWING EVACUATION LIGHT I NOP. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AT ROW 9 CEILING, CENTER RIGHT HAND SIDE. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996100300652 19961003 00652 NM 1996 10 3 USAASB96174 1 19960901 A 3350 20121 POWER SUPPLY BOEING 737 737301 1384611 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 575US 23740 PHL - MAINTENANCE FOUND THE EXTERIOR EMERGENCY ESCAPE SLIDE LIGHT INOP AT THE AFT RIGHT SERVICE DOOR. MAINTENANCE REMOV ED AND REPLACED THE POWER SUPPLY IN THE AFT OVERHEAD CABIN. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996100300653 19961003 00653 NM 1996 10 3 USAASB96175 1 19960831 A 3350 900835A BATTERY PACK BOEING 737 737201 1384454 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 236US 22352 CLT - MAINTENANCE FOUND BOTH OVERWING EMERGENCY EXIT LIGHTS FLASHING. MAINTENANCE REMOVED AND REPLACD THE BATTERY PACK FOR THE OVERWING EMERGENCY EXIT LIGHTS. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1996100300654 19961003 00654 1996 10 3 USAASB96176 4 19960902 A 3425 7725005009 ATTITUDE DIR IND BOEING 737 7373B7 1384580 NM COCKPIT P1 PNL FAILED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 514AU 30498 23700 MCI - FLT 139 - AT CRUISE, CAPTAINS ATTITUDE IN PITCH BEGAN JUMPING 2 TO 3 DEGREES. SELECTED ATTITUDE TRANSFER SWITCH T O 'BOTH ON 2' WITH NO HELP. FLIGHT DIVERTED TO MCI WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE CAPTAINS ATTITU DE DIRECTOR INDICATOR. PERFORMED OPS CHECK OF ADI PER MM. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996100300655 19961003 00655 NM 1996 10 3 USAASB96177 1 19960904 A 3350 AD20131A BATTERY PACK BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 270AU 22882 PIT - FL 560 - ON PREFLIGHT COCKPIT CHECK, CREW REPORTED LOW LEVEL TRACK LIGHTING AND EMERGENCY LIGHTS INOP THROUGHOUT C ABIN. MAINTENANCE REPLACED THREE BATTERY PACKS IN THE FORWARD AND AFT SECTIONS OF THE CABIN. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1996100300656 19961003 00656 NM 1996 10 3 USAASB96178 1 19960904 A 3230 CIRCUIT BREAKER BOEING 737 7374B7 1384702 NM LANDING GEAR TRIPPED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 434US 24556 MCI - FLT 797 - AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT AND THE GEAR INDICATION LIGHTS WENT OUT. WHILE TROUBL ESHOOTING AND PREPARING TO RETURN TO FIELD AT MCI, CREW FOUND THE AIR/GROUND SENSOR CIRCUIT BREAKER POPPED. CREW RESET THE BREAKER AND MADE A NORMAL LANDING AT MCI. NO EMERGENCY WAS DECLARED. MAINTENANCE PERFORMED OPERATIONAL CHECK OF LA NDING GEAR SYSTEM. OPS CHECK GOOD. COULD NOT DUPLICATE AIR/GROUND SENSOR CIRCUIT BREAKER TO POP. (M) 2 L 7 2 4F RT A16WE 1996100300657 19961003 00657 NM 1996 10 3 USAASB96179 1 19960905 A 3350 SOCKET BOEING 737 7373B7 1384580 NM CABIN SHORTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 387US 22959 TPA - MAINTENANCE FOUND EMERGENCY LIGHTS INOP ON RIGHT EXTERIOR OF FUSELAGE AND IN THE INTERIOR CENTER CABIN. MAINTENAN CE FOUND SHORTED LIGHT SOCKET ON RIGHT SIDE OF FUSELAGE AND BY AFT GALLEY. REPLACED SAME AND RELAMPED LIGHTS. OPS CHEC K GOOD. (M) 2 L 7 2 4F RT A16WE 1996100300658 19961003 00658 NM 1996 10 3 USAASB96180 1 19960905 A 3350 M3902932248 SOCKET BOEING 737 737201 1384454 NM CABIN LOOSE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 229US 21818 CLT - FL 1188 - CREW REPORTED EMERGENCY EXIT SIGN IN CENTER OF CABIN, ROW 9 OVERHEAD, IS LOOSE/INOP. MAINTENANCE REPAIR ED WIRING AT EMERGENCY EXIT SIGN SOCKET AND RESECURED LIGHT ASSEMBLY. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1996100300659 19961003 00659 NM 1996 10 3 USAASB96181 1 19960906 A 2120 AIR DISTR BOEING 737 737201 1384454 NM CABIN ODOR A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 226US 21815 PIT - FL 553 - FLIGHT ATTENDANTS ADVISED COCKPIT CREW THAT THEY SMELLED SMOKE OR FUMES IN THE REAR OF THE AIRCRAFT. THE Y DID NOT DETECT ANY SIGHT OF SMOKE. CAPTAIN COULD NOT ISOLATE PROBLEM AND ELECTED TO DECLARE AN EMERGENCY AS A PRECAUT IONARY MEASURE AND DIVERT TO PIT. FLIGHT LANDED AT PIT WITH NO FURTHER INCIDENT. CREW ADVISED DISPATCH THAT SMELL WENT AWAY AFTER STARTING APPROACH TO PIT. MAINTENANCE CHECKED CONDITION AND OPERATION OF BOTH PACKS WITH APU AND ENGINES RU NNING. COULD NOT DUPLICATE SMELL. (M) 2 L 7 2 4F A16WE 1996100300660 19961003 00660 NM 1996 10 3 USAASB96182 1 19960906 A 2150 655281046 ACCESSORY UNIT BOEING 737 7374B7 1384702 NM RT PACK FAILED A USAA A B UNSCHED LANDING EMER. DESCENT J WARNING INDICATION CL CLIMB 1 EA 19 781AU 13012 25020 PIT - FL 1211 - AFTER TAKEOFF, FLIGHT EXPERIENCED PRESSURIZATION PROBLEM AT 12,000 FEET. CREW DESCENDED TO 10,000 FEET. RIGHT PACK WAS INOP AND ON MEL AND LEFT PACK WOULD NOT PRESSURIZE A/C. FLIGHT RETURNED TO FIELD IN PIT AND LANDED WIT H NO FURTHER INCIDENT. NO EMERGENCY WAS DELCARED. MAINTENANCE TROUBLESHOT RIGHT PACK AND FOUND AN OPEN WIRE BETWEEN TH E P-5 OVERHEAD PANEL AND THE RIGHT AIR CONDITIONING ACCESSORY UNIT. REPAIRED WIRING. THE LEFT PACK WAS TROUBLESHOT TO A FAILED LEFT AIR CONDITIONING ACCESSORY UNIT. REPLACED SAME. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996100300661 19961003 00661 NM 1996 10 3 USAASB96183 1 19960907 A 3350 20121 POWER SUPPLY BOEING 737 7373B7 1384580 NM CABIN INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 504AU 23379 CLT - FL 1209 - PILOT REPORTED, THAT THE LAST EMERGENCY LIGHT ON THE RIGHT SIDE OF CABIN REMAINS ILLUMINATED. MAINTENAN CE REPLACED THE POWER SUPPLY AT THE AFT CABIN CEILING, RIGHT SIDE. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996100300662 19961003 00662 NM 1996 10 3 USAASB96184 1 19960908 A 2150 20405010 ACM BOEING 737 7373B7 1384580 NM LEFT FAILED A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 19 390US 32758 23312 ROC - FL 1836 - ON FINAL APPROACH, A STRONG BURNING SMELL WAS DETECTED IN THE CABIN. SMELL WAS NOTICEABLY STRONGER AT R OW 4. FLIGHT LANDED SAFELY. ON TAXI IN, AN INTERMITTENT RUBBING/GRINDING NOISE COULD BE HEARD THROUGHOUT CABIN. MAINT ENANCE FOUND THE LEFT AIR CYCLE MACHINE SEIZED. REPLACED SAME. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996100300663 19961003 00663 NM 1996 10 3 USAASB96185 1 19960909 A 3350 AD20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 520AU 23706 DFW - FL 1587 - PILOT REPORTED, THAT THE COCKPIT EMERGENCY LIGHTS ARE INOP. MAINTENANCE REPLACED THE EMERGENCY LIGHT BA TTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996100300664 19961003 00664 NE 1996 10 3 USAASB96186 2 19960911 A 7230 ENGINE BOEING 737 737201 1384454 NM PWA JT8 JT8D15 52051 NE LEFT FAILED A USAA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 EA 19 257AU 61718 22799 657495 PIT - FLT 111 - AT 30,500 FEET, THE NR 1 ENGINE EXPERIENCED A FIRST AND SECOND COMPRESSOR STALL. CREW STARTED DESCENT A ND GOT A THIRD STALL. CREW PULLED THROTTLE BACK AND COMPRESSOR STALLS CEASED. CREW CONTINUED DESCENT AND DIVERTED TO P IT WHERE THE FLIGHT LANDED SAFELY WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 ENGINE ASSEMBLY PER JOB CARD. OPERATIONAL CHECK AND LEAK CHECK NORMAL. (M) 2 L 7 2 4F 4 F A16WE E2EA 1996100300665 19961003 00665 EU 1996 10 3 USAASB96188 2 19960911 A 7230 COMP BLADES BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU NR 2 ENG BIRDSTRIKE A USAA A UNSCHED LANDING C E F.O.D. VIBRATION/BUFFET CL CLIMB 1 EA 19 375US 22954 SAT - FL 1594 - DURING TAKEOFF RUN AT 120 KNOTS, THE NR 2 ENGINE STRUCK AND INJESTED A LARGE BIRD. VIBRATION ROSE TO 4. 5 ON THE NR 2 ENGINE. FLIGHT RETURNED TO FIELD AT SAT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE INSPECTED INLET AND FOUND BLADE NR 34 DAMAGED. REPLACED SAME, ALONG WITH OPPOSING BLADE NR 15 PER JOB CARD. RAN ENGINE, ALL PARAMETER S NORMAL. (M) 2 L 7 2 4F 4 F RT A16WE E21EU 1996100300666 19961003 00666 NM 1996 10 3 USAASB96189 1 19960802 A 3350 AD20131A BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 777AU 24979 ORD - MAINTENANCE FOUND FORWARD OVERWING EMERGENCY LIGHTS AND MISCELLANEOUS CABIN EMERGENCY LIGHTS INOP DURING SYSTEM TE ST ON OVERNIGHT CHECK. MAINTENANCE REPLACED THE BATTERY PACK AT STATION 727G RIGHT SIDE. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996100300667 19961003 00667 NE 1996 10 3 USAASB96194 2 19960914 A 7200 ENGINE BOEING 737 737201 1384454 NM PWA JT8 JT8D9A 52048 NE NR 2 BIRD STRIKE A USAA A UNSCHED LANDING C F.O.D. TO TAKEOFF 1 EA 19 241US 22443 BOS - FL 1153 - DURING TAKEOFF ROLL, THE AIRCRAFT INJESTED A LARGE SEAGULL INTO THE NR 2 ENGINE. CREW AND DISPATCH ELEC TED TO DIVERT TO BOS AS A PRECAUTIONARY MEASURE. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITH NO FURTHER INCIDE NT. MAINTENANCE PERFORMED BIRD STRIKE INSPECTION PER MM 05-51-201 AND FOUND THE NR 2 ENGINE CSD OIL COOLER TO BE UNSERV ICEABLE. REPLACED SAME. LEAK CHECK GOOD. TAKEOFF POWER RUN OPS CHECK NORMAL. (M) 2 L 7 2 4F 4 F A16WE E2EA 1996100300668 19961003 00668 NM 1996 10 3 W8PA960132 1 19960909 A 3240 65445816 VALVE BOEING 737 7373B7 1384580 NM BRAKE SYSTEM LEAKING A W8PA C D ABORTED TAKEOFF RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 NM 03 951WP 1106 22951 ON TAKEOFF, 'A' SYSTEM PRESSURE DROPPED TO 1000 PSI. DURING GEAR RETRACTION, PRESSURE RETURNED TO NORMAL. RETURNED TO GATE. FOUND BRAKE ISOLATION VALVE LEAKING. REMOVED AND REPLACED VALVE. SERVICED HYDRAULICS TO FULL. (M) 2 L 7 2 4F RT A16WE 1996100300680 19961003 00680 CE 1996 10 3 96ZZZX4970 1 19960911 A 3222 084120015 PIN BEARING 1243610214 CESSNA 206 P206 2073304 CE NLG STRUT SEIZED A D3IA K NONE O OTHER LD LANDING 1 WP 19 2600X 3261 P2060100 ON LANDING/RUNOUT, NOSE FORK/WHEEL POSSIBLY STUCK IN A LOCKED POSITION CAUSING ACFT TO ROLL OFF OF RUNWAY. NO MAJOR DAM AGE, NO INJURIES. SUBMITTER RECOMMENDS ADDING A ZERK FITTING TO ENABLE MECHANIC TO LUBE NOSE GEAR BEARINGS. 1 H 7 1 3O A4CE 1996100300704 19961003 00704 SW 1996 10 3 HEEA967790 1 19960909 A 6720 206001713001 SUPPORT ASSY BELL 206 206L1 1182107 SW T/R CONTROL CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3904L 45597 PART IS CORRODED. (CORROSION AROUND BASE OF PEDAL SUPPORT) REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 1996100300705 19961003 00705 SW 1996 10 3 HEEA967791 1 19960909 A 6720 206001703006 PEDAL ASSY BELL 206 206L1 1182107 SW T/R CONTROL WORN EXCESS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2133X 45634 PART IS WORN EXCESSIVELY. (BEARING WORN BEYOND LIMITS) REPLACED WITH SERVICEABLE PEDAL ASSEMBLY. 1 G 7 1 3U H2SW 1996100300706 19961003 00706 1996 10 3 HEEA967792 4 19960909 A 2312 069102525 TRANSCEIVER KX165 BELL 206 206L1 1182107 SW COCKPIT VHF DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 10761 45381 VHF FREQUENCY SELECT KNOB. INTERMITTENT WON'T CHANGE FREQUENCY. 1 G 7 1 3U H2SW 1996100300707 19961003 00707 1996 10 3 HEEA967793 4 19960909 A 3454 066107800 RECEIVER BELL 412 412 1182202 SW NR 1 VOR INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 108X 33115 #1 VOR DOES NOT RECEIVE USABLE SIGNAL INOPERATIVE. 1 G 7 2 4U H4SW 1996100300708 19961003 00708 SW 1996 10 3 HEEA967795 1 19960909 A 3212 206050248115 FLOAT BAG BELL 206 206L1 1182107 SW SEAM DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3892R 45594 FLOAT BAG HAS UNBONDED SEAM. DATE OF MANUFACTURE 10-93. 1 G 7 1 3U H2SW 1996100300709 19961003 00709 1996 10 3 HEEA967796 4 19960909 A 3457 0110005400 GPS 150 BELL 206 206B3 1181506 SW COCKPIT GPS INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 104PH 3622 INOPERATIVE AND KNOB ALSO MISSING. TIME SINCE REPAIR 0:00. 1 G 7 1 3U H2SW 1996100300710 19961003 00710 SW 1996 10 3 HEEA967797 1 19960909 A 5312 206032400027 BULKHEAD ASSY 206033004177 BELL 206 206L4 1182110 SW TAILBOOM CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7077B 4514 52037 52037 FORWARD BULKHEAD ASSY CRACKED AT 3 EACH ATTACHMENT SHIM LOCATIONS. FOUND CRACKS DURING COMPLIANCE OF T.B. 206L-94-169. ALSO FOUND SEVERAL LOOSE RIVETS ATTACHING TAIL ROTOR GEARBOX SUPPORT FITTING TO AFT END OF TAILBOOM ASSY AND SEVERAL LO OSE(WORKING) RIVETS ON ATTACH FITTINGS AND INTERCOSTALS AT FORWARD END OF TAILBOOM ASSEMBLY. REPLACED FWD BULKHEAD ASSY. REWORKED ALL INTERCOSTAL ASSEMBLIES PER BHT-206-SRM-1 SECTION 6-3-1. REMOVED, CLEANED AND REINSTALLED GEARBOX SUPPORT AS PER BHT-206-SRM-1 SECTION 6-3-7. 1 G 7 1 3U NC H2SW 1996100300711 19961003 00711 SW 1996 10 3 HEEA967798 1 19960909 A 5302 206033004143 INTERCOSTAL BELL 206 206L3 1182108 SW TAILBOOM ASSY LOOSE RIVETS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 32041 3111 51539 WORKING RIVETS IN 4 EACH INTERCOSTALS WHERE ATTACHED TO FITTINGS. REMOVED INTERCOSTALS. REMOVED RIVETS, APPLIED 890 PRO -SEAL, INSTALLED MS20470E-5 RIVETS AND REPLACED INTERCOSTALS AS PER BHT-206-SRM-1. 1 G 7 1 3U H2SW 1996100300712 19961003 00712 SW 1996 10 3 HEEA967799 1 19960909 A 5320 206033110241S STIFFENER BELL 206 206L3 1182108 SW FUSELAGE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6251X 51552 STIFFENER IS CRACKED. (CRACK IS AT UPPER RIVET HOLE) REPLACED WITH SERVICEABLE STIFFENER. 1 G 7 1 3U H2SW 1996100300713 19961003 00713 SW 1996 10 3 HEEA967800 1 19960909 A 5320 206033110239 STIFFENER BELL 206 206L4 1182110 SW FUSELAGE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7077F 52038 STIFFENER IS CRACKED. (CRACKED AT TOP IN BENT ARM 4 7/8 FROM TOP EDGE. REPLACED WITH SERVICEABLE STIFFENER. 1 G 7 1 3U NC H2SW 1996100300714 19961003 00714 SW 1996 10 3 HEEA967801 1 19960909 A 5302 206032308003S FRAME BELL 206 206L3 1182108 SW TAILBOOM CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 32041 51539 FRAME IS CRACKED. (TAILBOOM FRAME CRACKED AT UPPER R/H CORNER WEAR RADIUS) REMOVED AND REPLACED FRAME. 1 G 7 1 3U H2SW 1996100300715 19961003 00715 SW 1996 10 3 HEEA967802 1 19960909 A 6210 412015300109 BLADE BELL 412 412 1182202 SW M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22347 8100 36005 BLADE IS CRACKED. (BLADE HAS A CRACK IN THE OUTBOARD LEADING EDGE ABRASION STRIP AT STATION 185" COMPLETE CHORDWISE. 1 G 7 2 4U H4SW 1996100300716 19961003 00716 SW 1996 10 3 HEEA967803 1 19960909 A 7714 412075010109 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3893P 33012 #2 NEEDLE WILL NOT GO TO ZERO AND #1 NEEDLE INDICATES LOW.TIME SINCE REPAIR 108:20. 1 G 7 2 4U H4SW 1996100300717 19961003 00717 NM 1996 10 3 CALA9601363 1 19960918 A 5314 KEEL BEAM BOEING 737 737214 138446R NM BS 663-727 GALLED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14239 19920 INSPECTION FOUND LT KEEL BEAM FAYING FLANGE FROM BS 663 TO 727 GALLED ON LOWER SURFACE AND WORN AROUND FASTENER HOLES ON UPPER SURFACE. EXISTING HOLES WERE OVERSIZED AND 3 EACH PRESS FIT BUSHINGS WERE INSTALLED. A REPAIR STRAP WAS FABRICA TED AND INSTALLED. ALL WORK WAS PERFORMED IAW SRM 51-10-2, 51-30-2, ECRA 5310-03324, AND REO 02234. 2 L 7 2 4F A16WE 1996100300718 19961003 00718 NM 1996 10 3 CALA9601364 1 19960918 A 5330 SKIN BOEING 737 737214 138446R NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14239 19920 INSPECTION FOUND THREE .125 INCH CRACKS IN SECTION 41R, RT FORWARD FUSELAGE EXTERNAL SKIN PANEL. THE CRACKED AREA WAS C UT OUT, FILLERS AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-10-2 AND EA 5310-01188. 2 L 7 2 4F A16WE 1996100300719 19961003 00719 NM 1996 10 3 CALA9601365 1 19960918 A 5330 SKIN BOEING 737 737214 138446R NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14239 19920 INSPECTION FOUND FOUR .125 INCH CRACKS IN SECTION 41, LT FORWARD FUSELAGE EXTERNAL SKIN PANEL. THE CRACKED AREA WAS CUT OUT, FILLERS AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-10-2 AND EA 5310-01188. 2 L 7 2 4F A16WE 1996100300720 19961003 00720 NM 1996 10 3 CALA9601366 1 19960918 A 5315 FLOORBEAM BOEING 737 737214 138446R NM BS 684 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14239 19920 INSPECTION FOUND A 1.5 INCH CRACK IN FLOORBEAM AT STA 684, LBL 24.8. THE FLOORBEAM WAS REPAIRED IAW EA 5710-01638 AND S RM 51-40-4. 2 L 7 2 4F A16WE 1996100300721 19961003 00721 NM 1996 10 3 CALA9601367 1 19960918 A 5551 FITTING BOEING 737 737214 138446R NM RT HORIZ STAB GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14239 19920 INSPECTION FOUND THE RT HORIZONTAL STABILIZER UPPER AFT SPAR INBOARD ATTACH FITTING GOUGED. THE ATTACH FITTING WAS REPA IRED IAW ECRA 5510-01338. 2 L 7 2 4F A16WE 1996100300722 19961003 00722 NM 1996 10 3 CALA9601368 1 19960918 A 5315 FLOORBEAM BOEING 737 737214 138446R NM BS 724 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14239 19920 INSPECTION FOUND A 1 INCH CRACK IN MAIN CABIN FLOORBEAM AT STA 724, BL 0. THE WEB AND STIFFENER WERE REMOVED IAW SRM 51 -30-2. A WEB AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-20-4, 57-30-2, ECRA 5710-01755 AND REO 02209 . 2 L 7 2 4F A16WE 1996100300723 19961003 00723 WP 1996 10 3 9620611152 1 19960912 A 5320 DOOR JAMB DOUG DC10 DC1040 3023508 WP BS 1250 1256 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 152US 46761 DURING T-CHECK, FOUND TWO CRACKS IN THE NR 3R DOOR JAMB FORWARD WEB FS 1250 TO 1256 AT THE FLOOR LEVEL. REPAIRED WEB (P /N AEA 0155-2) PER EA 11-110246. 2 L 7 3 4F A22WE 1996100300724 19961003 00724 WP 1996 10 3 9620621152 1 19960917 A 5347 SEAT TRACK DOUG DC10 DC1040 3023508 WP BS 1841 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 152US 46761 DURING T-CHECK, FOUND CORROSION ON THE RBL 65 SEAT TRACK AT FS 1841. REPAIRED TRACK (P/N NFA 6222-39) PER EA 11-110225. 2 L 7 3 4F A22WE 1996100300725 19961003 00725 EU 1996 10 3 9620633213 1 19960919 A 5320 SUPPORT AIRBUS 320 A320211 3930320 EU BS 32074 32571 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 313US 153 DURING IL CHECK, FOUND CORROSION ON THE AFT GALLEY FLOOR SUPPORT BETWEEN FRAMES 67 AND 68 AT THE LEFT AFT ENTRY DOOR SIL L. REPAIRED SUPPORT PER EA 32-106351. 2 L 7 2 4F RT A28NM 1996100300726 19961003 00726 WP 1996 10 3 9620641152 1 19960920 A 5313 LONGERON DOUG DC10 DC1040 3023508 WP BS 1432-1501 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 152US 46761 DURING T-CHECK, FOUND CORROSION ON THE OVERWING EXTERNAL LONGERONS 29R AND 30R FROM FS 1432 TO 1501. REPAIRED LONGERONS PER EA 11-110221. 2 L 7 3 4F A22WE 1996100300727 19961003 00727 WP 1996 10 3 9620659180 1 19960923 A 5320 FITTING DOUG DC9 DC914 3022034 WP BS 786 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3312L 45707 DURING H-CHECK, FOUND CORROSION ON THE LAVATORY FITTINGS AT FS 786 AND FS 801 AT THE RIGHT CUSP. REPLACED FITTINGS PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996100300728 19961003 00728 WP 1996 10 3 9620669618 1 19960923 A 5753 SKIN DOUG DC9 DC932 3022066 WP RT TE FLAP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 618NW 47433 DURING M-CHECK, FOUND CORROSION IN THE RIGHT FLAP EXTERNAL SKIN AND DOUBLER AT THE VANE SPRING BAY. ALSO, FOUND A CRACK ED T-FITTING. REPLACED SKIN/DOUBLER PER SRM 51-30-2 AND THE FITTING PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996100300729 19961003 00729 WP 1996 10 3 9620671152 1 19960924 A 5320 FITTING DOUG DC10 DC1040 3023508 WP BS 1509-1521 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 152US 46761 DURING T-CHECK, FOUND CORROSION ON LONGERON 52 AT THE CENTER WHEEL WELL AFT SHELF FS 1509 TO 1521. REPLACED FITTING (P/ N AYB 7063-501) PER SRM 51-00-00. 2 L 7 3 4F A22WE 1996100300730 19961003 00730 WP 1996 10 3 9620689614 1 19960925 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 907-996 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 614NW 47128 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON LONGERON 29L FROM FS 907 TO 996 AND ON THE END FITTING AT FS 996. REPLACED THE LONGERON PER SRM 51-30-01 AND THE FITTING PER SRM 51-30-05. 2 L 7 2 4F A6WE 1996100300731 19961003 00731 WP 1996 10 3 9620699910 1 19960925 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 622 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 960N 47256 DURING H-CHECK, FOUND CORROSION ON THE LONGERON 30 RIGHT KEEL TO FS 622 FRAME ATTACH FITTING. REPLACED FITTING (P/N 991 0164-85) PER SRM 51-01. 2 L 7 2 4F A6WE 1996100300732 19961003 00732 WP 1996 10 3 9620709974 1 19960925 A 5320 FITTING DOUG DC9 DC931 3022065 WP PAX DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9338 47347 DURING M-CHECK, FOUND CRACKS IN THE AFT ENTRY DOOR FITTINGS. REPLACED FITTINGS (P/N 3917624-521 AND 4917851-501) PER SR M 51-30. 2 L 7 2 4F A6WE 1996100300733 19961003 00733 WP 1996 10 3 9620719872 1 19960926 A 5320 FITTING DOUG DC9 DC951 3022051 WP BS 693 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 781NC 48121 DURING H-CHECK, FOUND A TWO INCH CRACK IN THE CENTER TANK UPPER RIGHT SUPPORT FITTING AT FS 693. REPLACED FITTING PER S RM 51-30-5 AND 51-30-1. 2 L 7 2 4F A6WE 1996100300734 19961003 00734 NE 1996 10 3 9620819155 2 19960929 A 7200 ENGINE DOUG DC9 DC914 3022034 WP PWA JT8 JT8D9 52048 NE RIGHT BIRD STRIKE A NWAA A UNSCHED LANDING C F.O.D. CL CLIMB 1 GL 01 8914E 45831 666304 DURING CLIMB AT 1,000 FEET, THE AIRCRAFT ENCOUNTERED A FLOCK OF GEESE AT WHICH TIME THE RIGHT ENGINE INGESTED ONE BIRD. RIGHT ENGINE EPR DROPPED FROM 2 TO 1.8. CREW REDUCED ENGINE POWER AND PERFORMED AN AIR TURNBACK TO YQR WHERE THEY LAND ED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE. 2 L 7 2 4F 4 F A6WE E2EA 1996100300735 19961003 00735 WP 1996 10 3 9620829952 1 19960928 A 3350 CONNECTOR DOUG DC9 DC932 3022066 WP CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 916RW 47144 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. RESEATED PLUGS ON GALLEY LIGHT ASSEMBLY POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996100300736 19961003 00736 WP 1996 10 3 9620839956 1 19960930 A 3350 60030451 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 923RW 47183 DURING FLIGHT, THE RIGHT OVERWING EXIT EMERGENCY LIGHTS AT SEATS ILLUMINATED. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996100300737 19961003 00737 WP 1996 10 3 9620849986 1 19960930 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 986US 47480 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERA TIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996100300738 19961003 00738 WP 1996 10 3 9620859604 1 19960927 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 604NW 47222 DURING LINE MAINTENANCE INSPECTION, FOUND CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN PACK, OPER ATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996100300739 19961003 00739 WP 1996 10 3 9620869605 1 19960926 A 3260 CONNECTORS DOUG DC9 DC932 3022066 WP LT MLG DIRTY A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 605NW 47223 LEFT MAIN GEAR UNSAFE LIGHT ILLUMINATED AFTER TAKEOFF. RECYCLED GEAR WITH SAME RESULTS. FLIGHT RETURNED TO SLC AND LAN DED WITHOUT INCIDENT. MAINTENANCE CLEANED AND RESEATED ELECTRICAL CONNECTORS TO SWITCHES. OPERATIONAL CHECK NORMAL ON GEAR SWING. 2 L 7 2 4F A6WE 1996100300740 19961003 00740 WP 1996 10 3 9620879967 1 19960930 A 2740 SWITCHES DOUG DC9 DC931 3022065 WP RT PRIMARY TRIM MALFUNCTIONED A NWAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 01 9331 47263 PRIMARY LONGITUDINAL TRIM FAILED AFTER TAKEOFF. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLAC ED FIRST OFFICER'S PRIMARY TRIM SWITCHES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996100300741 19961003 00741 WP 1996 10 3 9620889971 1 19961001 A 3350 NW9A33903681 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9335 47337 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATI ONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996100300742 19961003 00742 WP 1996 10 3 9620899956 1 19961001 A 3350 CONNECTOR DOUG DC9 DC931 3022065 WP CABIN LOOSE A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 923RW 47183 EMERGENCY EVACUATION LIGHTS AT ROWS 8, 9 AND 10 FLICKERED DURING FLIGHT. FOUND CONNECTOR UNDER SEAT 8D NOT MAKING GOOD CONTACT. RESEATED CONNECTOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996100300743 19961003 00743 WP 1996 10 3 9620909907 1 19960930 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 957N 47253 DURING LINE MAINTENANCE INSPECTION, FOUND MID CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIO NAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996100300744 19961003 00744 WP 1996 10 3 9620919907 1 19960930 A 3350 6011779 BATTERY PACKS DOUG DC9 DC931 3022065 WP RT/LT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 957N 47253 DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT AND LEFT NACELLE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996100300745 19961003 00745 WP 1996 10 3 9620929919 1 19960927 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 941N 47450 DURING LINE MAINTENANCE INSPECTION, FOUND BOTH AFT OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPER ATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996100300746 19961003 00746 WP 1996 10 3 9620939944 1 19960927 A 3350 6011779 BATTERY PACK DOUG DC9 DC931 3022065 WP RT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 1309T 47316 DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996100300747 19961003 00747 WP 1996 10 3 9620949951 1 19960929 A 3350 LIGHTS DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9347 45827 DURING LINE MAINTENANCE INSPECTION, FOUND ALL OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BOTH BATTERY PACKS A ND POWER SUPPLIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996100300748 19961003 00748 SO 1996 10 3 COMA9610290 1 19960930 A 3232 WTC22461 ACTUATOR EMB 120 EMB120RT SO RT MLG DOOR LEAKING A COMA K NONE K FLUID LOSS TX TAXI/GRND HDL 1 SO 01 162CA 19415 19415 120150 RT OUTBD MAIN GEAR DOOR ACTUATOR LEAKING. REPLACED GEAR DOOR ACTUATOR. 2 L 7 2 4T RT A31SO 1996100300749 19961003 00749 SO 1996 10 3 COMA9610291 1 19960930 A 3260 P0318 CONNECTOR EMB 120 EMB120RT SO RT NACELLE DIRTY A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 189CA 120189 GEAR HANDLE WOULD NOT MOVE AFTER TAKEOFF. CLEANED PROX SENSOR CONNECTORS IN RIGHT NACELLE. 2 L 7 2 4T RT A31SO 1996100300750 19961003 00750 SO 1996 10 3 COMA9610292 1 19960930 A 6120 MS33201 CIRCUIT BREAKER EMB 120 EMB120RT SO COCKPIT FAILED A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 1110J 120110 NR 2 FLIGHT IDLE STOP CB POPPED. REPLACED NR 2 FLIGHT IDLE STOP CIRCUIT BREAKER. 2 L 7 2 4T RT A31SO 1996100300751 19961003 00751 SO 1996 10 3 COMA9610293 1 19960927 A 5753 12020278614 SKIN EMB 120 EMB120RT SO RT TE FLAP DELAMINATED A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 264CA 120256 RT OUTBOARD FLAP OUTBOARD TRAILING EDGE DELAMINATED. REPAIRED IN ACCORDANCE WITH EMB120 51-70-01 WET LAY UP. 2 L 7 2 4T RT A31SO 1996100300752 19961003 00752 EU 1996 10 3 COMA9630148 1 19960930 A 3230 7232206029 SPRING SAAB SF340 SF340A 7850100 EU NLG BROKEN A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 340SF 014 NOSE GEAR ASSIST SPRING BROKEN. REPLACED NOSE UPLOCK HOOK RETRACT SPRING. 2 L 7 2 4T RT A52EU 1996100300753 19961003 00753 EU 1996 10 3 COMA9630149 1 19960930 A 3233 AIR864141 ACTUATOR SAAB SF340 SF340A 7850100 EU NLG LEAKING A COMA K NONE K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 357CA 25384 AC044 HYDRAULIC FLUID LEAKING FROM NOSE GEAR. REPLACED NOSE GEAR RETRACT ACTUATOR. 2 L 7 2 4T RT A52EU 1996100300754 19961003 00754 1996 10 3 COMA9630150 4 19960928 A 3421 6226342022 DPU SAAB SF340 SF340A 7850100 EU NR 1 FAILED A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 357CA 6999 044 CAPTAINS EADI WENT BLACK. REPLACED NR 1 DPU. 2 L 7 2 4T RT A52EU 1996100300755 19961003 00755 EA 1996 10 3 COMA9660154 1 19961001 A 3150 70621 MCU CNDAIR CL600 CL6002B19 EA VERT STAB FAILED A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 920CA 1460 7022 STAB CHANNEL 1 MESSAGE APPEARED TWICE. REPLACED MCU. 2 L 7 2 4F RT A21EA 1996100300756 19961003 00756 EA 1996 10 3 COMA9660155 1 19960930 A 3260 601R861361 PROX SENSOR CNDAIR CL600 CL6002B19 EA NLG DOOR OUT OF ADJUST A COMA K NONE N FALSE WARNING AP APPROACH 1 SO 01 915CA 7013 'NOSE DOOR OPEN' WARNING IN FLIGHT AFTER GEAR EXTENSION. ADJUSTED NOSE GEAR DOOR PROX SENSORS. 2 L 7 2 4F RT A21EA 1996100300757 19961003 00757 EA 1996 10 3 COMA9660156 1 19960928 A 3150 864806 PROX SENSOR CNDAIR CL600 CL6002B19 EA SPOILER SYST FAILED A COMA K NONE O OTHER LD LANDING 1 SO 01 915CA 7723 7723 7013 GLD DID NOT DEPLOY ON TOUCHDOWN. REPLACED PSEU. 2 L 7 2 4F RT A21EA 1996100300758 19961003 00758 1996 10 3 COMA9660157 4 19960928 A 3418 501125904 ACTUATOR CNDAIR CL600 CL6002B19 EA STICK PUSHER FAILED A COMA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 929CA 6786 7035 STALL FAIL ABNORMAL CAPTION DISPLAYED. REPLACED STICK PUSHER ACTUATOR. 2 L 7 2 4F RT A21EA 1996100300759 19961003 00759 NE 1996 10 3 COMA9660158 2 19960927 A 7200 ENGINE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RIGHT BIRD STRIKE A COMA A UNSCHED LANDING C F.O.D. CL CLIMB 1 SO 01 947CA 2831 7077 807310 BIRD STRIKE ON TAKEOFF, AT LEAST 8 TO 12 BIRDS. REPLACED RT ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 1996100300760 19961003 00760 EA 1996 10 3 COMA9660159 1 19960927 A 5753 601R145001 FLAP CNDAIR CL600 CL6002B19 EA LEFT PAINT LOOSE A COMA K NONE F FLT CONT AFFECTED AP APPROACH 1 SO 01 917CA 7017 WITH FLAPS 45 DEGREES AIRCRAFT ROLLS HARD TO LEFT. REMOVED RAISED PAINT FROM LT OUTBOARD FLAP. 2 L 7 2 4F RT A21EA 1996100300761 19961003 00761 EA 1996 10 3 COMA9660160 1 19960926 A 2760 270003 PCU CNDAIR CL600 CL6002B19 EA LT SPOILER INOPERATIVE A COMA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 01 915CA 604 7013 LEFT SPOILERON STATUS MESSAGE ON EICAS. REPLACED LT OUTBD FLIGHT SPOILER PCU. 2 L 7 2 4F RT A21EA 1996100300762 19961003 00762 NM 1996 10 3 96FDEA01555 1 19961001 A 3110 5910104 POWER RELAY DOUG MD11 MD11F 3023600 NM RT COCKPIT FAILED A FDEA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 618FE 48754 SFS - APPROXIMATELY 25 MINUTES INTO FLIGHT, THE FIRST OFFICER LOST ALL DISPLAYED INSTRUMENTATION. AIR TURNBACK TO SFS, CURRENTLY BEING T/S. REMOVED AND REPLACED THE NR 3 AUXILIARY POWER RELAY. RAN ENGINE, POWER TRANSFER OK. 2 L 7 3 4F RT A22WE 1996100300763 19961003 00763 NM 1996 10 3 96FDEA01556 1 19960927 A 5311 651630918 FRAME BOEING 727 72725 1384006 NM BS 251.6 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 511FE 18283 NR0541 AND 011, FOUND CORROSION (C53-221-01) ON FRAME WEB AND TWO STIFFENERS AFT SIDE OF BS 251.6 RBL 51 WL 215 TO 221. *S/D* REMOVED CORRODED WEB AND STIFFENERS AT BS 251.6 RBL 51 WL 215 TO 221. FABRICATED AND INSTALLED WEB AND STIFFEN ERS IAW FEDEX SRM 51-40-2. 2 L 7 3 4F A3WE 1996100300764 19961003 00764 NM 1996 10 3 96FDEA01557 1 19960930 A 5315 65208279 FLOORBEAM BOEING 727 72725 1384006 NM BS 1050 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 511FE 18283 NR0440 AND 012, CORROSION (C53-111-01,-3) IN AFT CARGO BAY AT BS1050 LBL TO RBL 20 WL 199 ON FLOOR BEAM AT NUTPLATE HOLE S. *S/D* REMOVED CORRODED SECTION OF BS 1050 FLOORBEAM FROM LBL TO RBL 25 LOWER FLANGE. REPAIRED LOWER FLANGE PER FED EX SRM 53-10-8 FIG 3, EA NR 7-5310-31192. 2 L 7 3 4F A3WE 1996100300765 19961003 00765 NM 1996 10 3 96FDEA01463 1 19960910 A 5320 6925827 INTERCOSTAL BOEING 727 72725 1384006 NM BS 266 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR 0624 AND 021, CORROSION (C53-221-01) ON TOP OF INTERCOSTAL STA 266 WL 208 LBL 6. *S/D* REMOVED AND REPLACED TOP CHO RD OF INTERCOSTAL AT BS 259 TO 277 LBL 6 WL 208 PER FEDEX SRM 51-10-1, 51-30-2. 2 L 7 3 4F A3WE 1996100300766 19961003 00766 NM 1996 10 3 SCNA96268 1 19960929 A 3350 S106 BATTERY BOEING 727 727227 1384078 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 275AF 22092 FOUND AFT AIRSTAIR EMERGENCY LIGHT INOP. REPLACED BATTERIES AND OPS CHECKED GOOD. 2 L 7 3 4F A3WE 1996100300767 19961003 00767 NM 1996 10 3 P5CA9600729 1 19961001 A 2780 698816985 SHAFT BOEING 747 747123 1384873 NM NR 2 LE FLAP WORN A P5CA K NONE O OTHER LD LANDING 1 WP 23 858FT 20109 ON ARRIVAL, FOUND NR 2 LEADING EDGE GROUP TORQUE TUBE SPLINES COMPLETELY WORN OUT, WOULD NOT DRIVE NR 2 LEADING EDGE GRO UP. REPLACED SHAFT PER BOEING MAINTENANCE MANUAL 27-81-05. 2 L 7 4 4F A20WE 1996100300768 19961003 00768 NM 1996 10 3 P5CA9600730 1 19960922 A 5330 SKIN BOEING 747 747122 1384872 NM AFT FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 CRACK ON SMALL FAIRING AND FAIRING IS LOOSE AFT FUSELAGE ON LEFT UNDER APU EXHAUST DUCT. REPAIRED PER BAC SRM 51-10-01 AND 51-40-02. 2 L 7 4 4F A20WE 1996100300769 19961003 00769 NM 1996 10 3 P5CA9600731 1 19960922 A 3340 HOUSING BOEING 747 747122 1384872 NM NOSE TAXI LIGHT TORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 TORN LEFT CORNER OF NOSE TAXI LIGHT HOUSING. REPAIRED PER BAC SRM 51-40-09. 2 L 7 4 4F A20WE 1996100300770 19961003 00770 NM 1996 10 3 P5CA9600732 1 19960923 A 7110 COWL PIN/SUPPORT BOEING 747 747122 1384872 NM ENGINE DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 DAMAGED ALIGNMENT PIN AND SUPPORT ON NR 2 ENGINE CORE COWL. REPAIRED PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1996100300771 19961003 00771 NM 1996 10 3 P5CA9600733 1 19960927 A 5414 SKIN BOEING 747 747123 1384873 NM NR 4 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 CRACK AT LOWER FORWARD ACCESS HOLE NR 4 PYLON, NR 483CL. REPAIRED PER BOEING SRM 54-30-03, TIME LIMITED REPAIR. 2 L 7 4 4F A20WE 1996100300772 19961003 00772 NM 1996 10 3 P5CA9600734 1 19960928 A 5210 SKIN BOEING 747 747122 1384872 NM NR 1 PAX DOOR SEPARATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 SKIN SEPARATION ON NR 1 MAIN ENTRY DOOR AT FORWARD UPPER CORNER. REPAIRED PER BOEING SRM 51-30-00. 2 L 7 4 4F A20WE 1996100300773 19961003 00773 NM 1996 10 3 P5CA9600735 1 19960922 A 7110 COWL BOEING 747 747122 1384872 NM NR 3 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 CRACK AT 5TH LATCH ON NR 3 ENGINE POWER COWL. REPAIRED PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1996100300774 19961003 00774 NM 1996 10 3 P5CA9600736 1 19960923 A 2550 65B634521 LOCK ARM BOEING 747 747122 1384872 NM MAIN DECK CARGO BENT A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 BENT FORWARD LOCK ARM ON MAIN DECK SIDE RAIL AT STA 1780. REPLACED SIDE RAIL LOCK ARM PER BAC MM 25-58-00. 2 L 7 4 4F A20WE 1996100300775 19961003 00775 NM 1996 10 3 P5CA9600737 1 19960924 A 5400 RIB BOEING 747 747122 1384872 NM NR 1 PYLON CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LEVEL 1 CORROSION NR 1 PYLON FIRE BOTTLE SUPPORT RIB. REMOVED CORROSION PER BOEING SRM 51-10-01 TREATED PER BOEING SRM 51-10-02. 2 L 7 4 4F A20WE 1996100300776 19961003 00776 NM 1996 10 3 P5CA9600738 1 19960922 A 7830 SKIN BOEING 747 747122 1384872 NM ENG TR SLEEVE DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 DAMAGED TRAILING EDGE SKIN ON NR 3 ENGINE T-FAN THRUST REVERSER SLEEVE. REPAIRED WITH HOT BONDED DOUBLER PER BAC SRM 51 -40-06. 2 L 7 4 4F A20WE 1996100300777 19961003 00777 NM 1996 10 3 P5CA9600739 1 19960924 A 7830 SLEEVE BOEING 747 747122 1384872 NM ENG TR SLEEVE DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 DENT NR 1 ENGINE FAN REVERSER SLEEVE AT 3 O'CLOCK POSITION. REPAIRED PER BOEING SRM 54-34-03 PAGE 85. 2 L 7 4 4F A20WE 1996100300778 19961003 00778 NM 1996 10 3 P5CA9600740 1 19960924 A 7830 EXHAUST PLUG BOEING 747 747122 1384872 NM NR 1 ENGINE DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 DENTED END CAP ON NR 1 ENGINE EXHAUST PLUG. REMOVED AND REPLACED PER BOEING MAINTENANCE MANUAL 78-32-08. 2 L 7 4 4F A20WE 1996100300779 19961003 00779 NM 1996 10 3 P5CA9600741 1 19960925 A 5210 HINGE COVER BOEING 747 747122 1384872 NM L1 DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 CRACKED HINGE COVER LEFT NR 1 ENTRY DOOR LOWER OUTER. REPAIRED PER BOEING SRM 51-10-01 FIG II PAGE 19 TO 21. 2 L 7 4 4F A20WE 1996100300780 19961003 00780 NM 1996 10 3 P5CA9600742 1 19960926 A 5210 HINGE COVER BOEING 747 747122 1384872 NM L1 DOOR DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 DENT ON NR 1 LEFT ENTRY DOOR FORWARD CENTER HINGE COVER. MANUFACTURED AND REPLACED HINGE COVER PER BOEING SRM 51-10-06. 2 L 7 4 4F A20WE 1996100300781 19961003 00781 NM 1996 10 3 P5CA9600743 1 19960927 A 5320 INTERCOSTAL BOEING 747 747122 1384872 NM BS 2742 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 CRACKED INTERCOSTAL BS 2742 LBL 12. FABRICATED AND REPLACED INTERCOSTAL PER BOEING SRM 51-30-02. 2 L 7 4 4F A20WE 1996100300782 19961003 00782 WP 1996 10 3 ARWA9610035 1 19960905 A 5280 DOOR DOUG DC8 DC863F 302198F WP RT MLG CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK INSPECTION, FOUND 2 INCH CRACK ON RT MLG I/B DOOR SURFACE. REPAIRD AREA IAW DC-8 SRM 52-2-0 FIG 2 SH 3. FORMED AND TREATED DOUBLER IAW DC-8 SRM 52-6-1 PG 2; 51-1-5. INSTALLED AT RT MLG I/B DOOR IAW DC-8 SRM 51-1-17, 51-1-2 1, CF W/O 017404 N/R 0227. 2 L 7 4 4F 4A25 1996100300783 19961003 00783 WP 1996 10 3 ARWA9610036 1 19960905 A 5311 FRAME DOUG DC8 DC863F 302198F WP RT MLG WW BROKEN A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK INSPECTION, FOUND BROKEN FRAME AT RT MLG WHEEL WELL INNER SECTION. REPAIRED SECTION AT RT MAIN GEAR IAW DC8 SRM 53-2-1, FIG 1B SH 3. TREATED AND INSTALLED ANGLE DOUBLER IAW DC8 SRM 51-1-8, 51-1-21, CF W/O 017402 N/R 0229. 2 L 7 4 4F 4A25 1996100300784 19961003 00784 WP 1996 10 3 ARWA9610037 1 19960910 A 5320 COVER DOUG DC8 DC863F 302198F WP BS 1160 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION IN AFT LOWER CARGO COMPARTMENT, INTERCOASTAL COVER AT L252 STA 1160. CORRODED PLATE SECTION WAS REMOVED, REPAIRED AREA IAW DC8 SRM 53-2-0, FIG 1D SH 3. FORMED AND TREATED DOUBLERS IAW DC8 SRM 53-4-1, FIG 51 SH 10, 41-1-8. INSTALLED IAW DC8 SRM 51-1-17, 51-1-21, 51-1-20D, CF W/O 017420 N/R 0573. 2 L 7 4 4F 4A25 1996100300785 19961003 00785 WP 1996 10 3 ARWA9610038 1 19960911 A 5230 SKIN DOUG DC8 DC863F 302198F WP CARGO DOOR CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK INSPECTION, FOUND 1 IN. CRACK IN #3 PIT DOOR INNER SKIN R/H CNTR SECTION. CRACKED AREA WAS REMOVED I.A.W. DC8 SRM 52-2-0, FIG. 4. FORMED AND TREATED DOUBLERS I.A.W. DC8 SRM 52-4-1, FIG. 2, 51-1-8. INSTALLED AT #3 PIT DOOR I.A .W. DC8 SRM 51-1-17, 51-1-21. CF W/O 017402 N/R 0740. 2 L 7 4 4F 4A25 1996100300786 19961003 00786 WP 1996 10 3 ARWA9610039 1 19960911 A 5230 SKIN DOUG DC8 DC863F 302198F WP CARGO DOOR CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C CHECK INSPECTION, FOUND 1 IN. CRACK IN #3 PIT DOOR INNER SKIN L/H CNTR SECTION. REPAIRED CARGO DOOR PLATING I.A .W. DC8 SRM 52-2-0, FIG. 4. FORMED AND TREATED REPAIR PARTS I.A.W. DC8 SRM 51-1-4, 51-1-8. INSTALLED AT #3 PIT DOOR I.A. W. DC8 SRM 51-1-17, 51-1-21. CF W/O 017402 N/R 0739. 2 L 7 4 4F 4A25 1996100300787 19961003 00787 WP 1996 10 3 ARWA9610040 1 19960907 A 5230 SKIN DOUG DC8 DC863F 302198F WP CARGO DOOR BROKEN A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C CHECK INSPECTION, FOUND BROKEN OUTER SKIN LOWER SIDE AT #1 PIT DOOR. REPAIRED #1 PIT DOOR SKIN I.A.W. DC8 SRM 5 2-2-0, FIG. 2 SH. 3. INSTALLED DOUBLER I.A.W. DC8 SRM 52-4-1, 51-1-17, 51-1-21. TREATED AREA I.A.W. DC8 SRM 51-1-8. CF W /O 017402 N/R 0460. 2 L 7 4 4F 4A25 1996100300788 19961003 00788 WP 1996 10 3 ARWA9610041 1 19960906 A 5220 DOOR DOUG DC8 DC863F 302198F WP EMER EXIT CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C CHECK INSPECTION, FOUND 2 IN. CRACKS IN OVERWING EMERGENCY EXIT DOOR LOWER AND UPPER CORNERS, R/H FORWARD SIDE AT MAIN CARGO COMPARTMENT. REPAIRED I.A.W. DC8 SRM 52-2-0, FIG. 2, SH. 3. FORMED DOUBLER I.A.W. DC8 DRM 52-7-1, FIG. 2. TREATED AND INSTALLED I.A.W. DC8 SRM 51-1-8, 51-1-17, 51-1-21. CF W/O 017402 N/R 0320. 2 L 7 4 4F 4A25 1996100300789 19961003 00789 WP 1996 10 3 ARWA9610042 1 19960909 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 290 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C CHECK INSPECTION, FOUND CRACK IN INNER SKIN AFT OF FORWARD CARGO STA. 290 L36. REPAIRED I.A.W. DC8 SRM 53-2-0, FIG. 1D, SH. 3. DAMAGED SKIN WAS REMOVED. FORMED SKIN SECTION AND DOUBLER I.A.W. DC8 SRM 53-4-1, 51-1-4. TREATED AND INS TALLED REPAIR PARTS I.A.W. DC8 SRM 51-1-8, 51-1-17, 51-1-21. CF W/O 017402 N/R 0482. 2 L 7 4 4F 4A25 1996100300790 19961003 00790 WP 1996 10 3 ARWA9610043 1 19960912 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 798 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C CHECK INSPECTION, FOUND 2 IN. AND 1 IN. CRACK IN LOWER FUSELAGE SKIN STA. 798 AT R/H SIDE OF FRAME, ALSO, CNTR SIDE. REPAIRED WEB I.A.W. DC8 SRM 53-2-0, FIG. 9B, SH. 3. FORMED AND TREATED DOUBLER I.A.W. DC8 SRM 53-8-3, FIG. 1, 51-1 -8. INSTALLED DOUBLER I.A.W. DC8 SRM 51-1-17, 51-1-21. CF W/O 017402 N/R 0802. 2 L 7 4 4F 4A25 1996100300791 19961003 00791 WP 1996 10 3 ARWA9610044 1 19960912 A 5280 CHANNEL DOUG DC8 DC863F 302198F WP RT MLG DOOR CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C CHECK INSPECTION, FOUND 4 IN. CRACK IN R/H MLG I/B DOOR EDGE, AFT LOWER SIDE. REPAIRED CHANNEL I.A.W. DC8 SRM 5 2-2-0, FIG. 2, SH. 3. FORMED AND TREATED DOUBLER I.A.W. DC8 SRM 51-1-4, 52-0-1, 51-1-8. INSTALLED DOUBLER AT MLG DOOR I. A.W. DC8 SRM 51-1-17, 51-1-21. CF W/O 017402 N/R 0791. 2 L 7 4 4F 4A25 1996100300792 19961003 00792 WP 1996 10 3 ARWA9610045 1 19960912 A 5230 SKIN DOUG DC8 DC863F 302198F WP CARGO DOOR CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C CHECK INSPECTION, FOUND 1 IN. CRACK IN #3 PIT DOOR INNER SKIN L/H UPPER SIDE. REPIARED AREA I.A.W. DC8 SRM 52-2 -0, FIG. 4, SH. 3. FORMED AND TREATED RE PAIR PARTS I.A.W. DC8 SRM 51-1-4, 52-4-1 AND 51-1-8. INSTALLED REPAIR PARTS I.A .W. DC8 SRM 51-1-17, 51-1-21. CF W/O 017402 N/R 0738. 2 L 7 4 4F 4A25 1996100300793 19961003 00793 NM 1996 10 3 CKSA96156 1 19961001 A 5330 SKIN BOEING 727 727223 1384074 NM R 1 DOOR CUTOUT CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6812 19487 KOSC - DURING B CHECK INSPECTION FOUND: R-1 DOOR FORWARD LOWER CORNER OF FUSELAGE SKIN CRACKED (1-1/4 INCH IN LENGTH). S TOP DRILLED CRACK AND REPAIRED IAW BOEING MESSAGE #M7272-96-4633 (NOTE: BOTH CRACK IN SKIN AND BEAR STRAP TERMINATED AT THE SAME LOCATION). TASK CARD NO. 86522 CORROSION CARD NO. C53-100-01 2 L 7 3 4F A3WE 1996100300795 19961003 00795 NM 1996 10 3 CA960129021 1 19960117 A 2751 251N511714 SWITCH BOEING 757 757236 NM FLAP LOSS FAILED W C D ABORTED TAKEOFF RETURN TO BLOCK F FLT CONT AFFECTED TO TAKEOFF 1 CA (CAN)DURING TAKEOFF ROLL THE LEADING EDGE SLAT ASYMMETRY MESSAGE OCCURRS AND THE AIRCRAFT ABORTED THE TAKEOFF. AFTER VER IFICATION THE FLAP SLAT ELECTRONIC UNIT WAS REPLACED. SAME MESSAGE OCCURRED ON NEXT F LIGHT. L/H FLAP LOSS SWITCH REPLAC ED. 2 L 7 2 4F RT A2NM 1996100300796 19961003 00796 SW 1996 10 3 CA960129022 1 19960111 A 6220 529052 SEAL BELL 206 206L4 1182110 SW ALLSN 250C 250C30P 03013 GL M/R HEAD UNSEATS W K NONE O OTHER IN INSP/MAINT 1 CA 1033 CAE895748 (CAN)WHILE GREASING HEAD THE SEAL BECOME DISLODGED AND MOVE INBOARD, AND HAVE TO BE RESEATED. 1 G 7 1 3U 3 U NC H2SW E1GL 1996100300797 19961003 00797 SW 1996 10 3 CA960129023 1 19960111 A 6520 206340103101 SEAL BELL 206 206L4 1182110 SW T/R GR BOX INPUT LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 1033 (CAN)SEAL LEAKING. REQUIRES OIL TO BE ADDED TO GEARBOX DAILY. 1 G 7 1 3U NC H2SW 1996100300798 19961003 00798 SW 1996 10 3 CA960129024 1 19960111 A 6520 406340105101 SEAL BELL 206 206L4 1182110 SW T/R GR BOX OUT LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 1033 (CAN)SEAL LEAKING. OIL HAS TO BE ADDED DAILY. 1 G 7 1 3U NC H2SW 1996100300799 19961003 00799 SW 1996 10 3 CA960129025 1 19960111 A 6320 50501008380401 SEAL BELL 206 206L4 1182110 SW OIL PUMP LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 1033 (CAN)SEAL LEAKING. OIL HAS TO BE ADDED AT THE RATE OF 1 QUART PER 30 HOURS OF OPERATION. 1 G 7 1 3U NC H2SW 1996100300800 19961003 00800 SW 1996 10 3 CA960129026 1 19960111 A 6520 260017023 SEAL BELL 206 206L4 1182110 SW ALLSN T/R GR BOX INB LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 1033 (CAN)SEAL LEAKING TO THE POINT WHERE OIL HAS TO BE ADDED DAILY. 1 G 7 1 3U NC H2SW 1996100300801 19961003 00801 CE 1996 10 3 CA960129027 1 19960114 A 7120 26430092C SHIMMY DAMPNER CESSNA 265102215 CESSNA 208 208B 2073701 CE PWA PT6 PT6A114 52043 NE ENGINE MOUNT LEAKING W C D ABORTED TAKEOFF RETURN TO BLOCK E VIBRATION/BUFFET TO TAKEOFF 1 CA PCE17008 (CAN)AIRCRAFT WAS ROLLING FOR TAKEOFF WHEN PILOT OBSERVED A SEVERE NOSE SHIMMY. AIRCRAFT RETURNED TO HANGER. THE NOSE SH IMMY DAMPNER WAS SUSPECTED TO BE AT FAULT AND WAS FOUND TO BE LEAKING. COMPANY POLICYALSO INSPECTS THE ENGINE MOUNT RING AND IN THIS CASE IT WAS FOUND CRACKED. ENGINE MOUNT RING AND SHIMMY DAMPNER WERE REPLACED. 1 H 7 1 3T 3 T A37CE E4EA 1996100300802 19961003 00802 CE 1996 10 3 CA960129028 1 19960111 A 2750 26111441 SUPPORT 26111441 CESSNA 208 208B 2073701 CE PWA PT6 PT6A114 52043 NE FLAP MOTOR SUPP. CRACKED W O OTHER J WARNING INDICATION LD LANDING 1 CA 5885 5885 PCE19182 (CAN)FLAP CIRCUIT BREAKER POPPED OUT WHEN FULL FLAP IS SELECTED MAINTENANCE FOUND THE SUPPORT FOR THE FLAP MOTOR/TRANSMI SSION SUPPORT CRACKED THE SUPPORT WAS REPLACED 1 H 7 1 3T 3 T A37CE E4EA 1996100300804 19961003 00804 EA 1996 10 3 CA960131002 2 19960102 A 8520 LW17031 CRANKSHAFT LYC CESSNA 172 172P 2072436 CE LYC O320 O320D2J 41508 EA NR1 BRG BORE ECCENTRIC W K NONE O OTHER IN INSP/MAINT 1 CA 3437 1381 L1198739A (CAN)THE CRANKSHAFT WAS INSPECTED IN ACCORDANCE WITH LYCOMING SB 505A AND FOUND PITTED. WHEN REPAIRS OF THE AFFECTED ARE A WERE ATTEMPTED THE CENTRE BORE OF THE CRANKSHAFT WAS FOUND TO BE ECCENTRIC, WITH TH E #1 BEARING CIRCUMFERENCE OFFSET BY .085". THE CRANKSHAFT WAS NOT REPAIRABLE AND IS CONSIDERED SCRAP. THIS CRANKSHAFT HAS NOT BEEN MODIFIED OR ALTERED SI NCE NEW, SO IT MUST BE CONSIDERED THAT IT WAS MANUFACTURED WITH THE INNER CRANKSHAFT BORE ECCENTRIC. 1 H 7 1 3O 3 O NT 3A12 E274 1996100300805 19961003 00805 SW 1996 10 3 CA960131003 1 19960122 A 2742 G0162 SHAFT SIMMONDS DL5040M5 SWRNGN SA226 SA226TC 8780404 SW PITCH TRIM LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA 3042 G0162 (CAN)ACTUATOR HAD REFURBISHED NUTS AND SHAFTS INSTALLED AT OVERHAUL. DURING ROUTINE INSPECTION AT 2800 HOURS IN SERVICE SOME FREE PLAY WAS NOTED. HOWEVER, AT REMOVAL FREE PLAY WAS 0.009 BOTH LH AND RH. ALS O THE ROD END ASSEMBLY HAD FREE PL AY DUE TO THE LOCK NUT BEING LOOSE AND ROD END ATTACH FITTING WAS LOOSE DUE TO A LOOSE LOCKING DEVISE. SUBMITTER NOTES T HAT THE LOOSE INNER SHAFT CAUSES CONCERN AS IT APPEARS THAT THE INNER SHAFT COULD CONCEIVABLY UNSCREW AND JAM OR DISCONN ECT. THE AD DOES NOT ADDRESS A LOOSE INNER SHAFT. 2 L 7 2 4T RT A8SW 1996100300806 19961003 00806 WP 1996 10 3 CA960131004 2 19960118 A 7322 89356117 FUEL CONTRL UNIT WOODWARD SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP NR1 ENGINE FAULTY W K NONE O OTHER IN INSP/MAINT 1 CA 1958 P54219 (CAN)ON START #1 ENGINE FUEL FLOW INDICATED 250 LBS WITH START TEMPERATURE RISING TO MAXIMUM LIMITS. THE START WAS ABORT ED. AFTER ALLOWING FOR A COOLING DOWN PERIOD A FURTHER TWO STARTS WERE UNSUCESSFUL. T HE FUEL CONTROL UNIT AND THE HP FU EL PUMP WERE REPLACED AND CHECKED SERVICEABLE AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A8SW E4WE 1996100300807 19961003 00807 EU 1996 10 3 RAIA960910 1 19960909 A 5240 14153133217 LAV SERVICE DOOR JETAIR JETSTM JETSTM4101 1500501 EU AFT LEFT FUS MISSING A RAIA K NONE D INFLIGHT SEPARATION IN INSP/MAINT 1 CE 03 557HK 41074 JFK - FLT 7771 - ON POST FLIGHT WALK AROUND, FOUND LAVATORY SERVICE DOOR MISSING FROM AIRCRAFT. NO DAMAGE NOTED OTHER T HAN DOOR MISSING. MAINTENANCE PLACED LAV SERVICE DOOR ON CDL 52-40. (M) 2 L 7 2 4T RT A41NM 1996100300808 19961003 00808 EU 1996 10 3 RAIA960909 1 19960905 A 3350 ML44 BULB AEROSP ATR72 ATR72202 8680940 EU CABIN FAILED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 721TE 217 STL - FLT 7546 - EMERGENCY LIGHT IN CABIN DOOR INOP. MAINTENANCE REPLACED THE BULB IN THE CABIN DOOR EXIT LIGHT. (M) 2 H 7 2 4T RT A53EU 1996100300809 19961003 00809 EU 1996 10 3 RAIA960908 1 19960905 A 3350 0L3071BPE BULB AEROSP ATR72 ATR72202 8680940 EU CABIN FAILED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 722TE 220 STL - FLT 7115 - ESCAPE PATH LIGHTS IN THE FORWARD SECTION INOP. MAINTENANCE REPLACED 2 BULBS IN THE FORWARD PART OF TH E ESCAPE PATH LIGHTING. (M) 2 H 7 2 4T RT A53EU 1996100300810 19961003 00810 EU 1996 10 3 RAIA960907 1 19960907 A 3350 ML44 BULB AEROSP ATR42 ATR42300 8680920 EU AIRSTAIR FAILED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 426TE 228 STL - FLT 7541 - EMERGENCY EXIT LIGHT IN AIRSTAIR IS INOPERATIVE. MAINTENANCE REPLACED THE BULB IN THE AIRSTAIR EXIT LI GHT. (M) 2 H 7 2 4T RT A53EU 1996100300811 19961003 00811 EU 1996 10 3 RAIA960906 1 19960905 A 2435 23079009 STARTER/GEN BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 CE 03 871JX 8668 871 LAX - FLT 4761 - LEFT GENERATOR LIGHT CAME ON DURING FLIGHT. MAINTENANCE REPLACED THE LEFT STARTER/GENERATOR. (M) 2 L 7 2 4T RT A56EU 1996100700001 19961007 00001 1996 10 7 COMA9610286 2 19960923 A 7313 311610901 TRANSFER TUBE EMB 120 EMB120RT SO RT ENGINE NOT SEATED A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 248CA 120228 RT ENGINE LEAKING FUEL AND SMOKING AFTER SHUT DOWN. SECURED LOOSE FUEL TRANSFER TUBES ON THE NR 14 FUEL NOZZLE. 2 L 7 2 4T RT A31SO 1996100700002 19961007 00002 SO 1996 10 7 COMA9610287 1 19960925 A 3231 12032943001 SEQUENCE VALVE EMB 120 EMB120RT SO LT MLG DOOR MALFUNCTION A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 266CA 11813 120258 LANDING GEAR WILL NOT RETRACT. REPLACED LT MLG DOOR SEQUENCE VALVES. 2 L 7 2 4T RT A31SO 1996100900001 19961009 00001 NM 1996 10 9 DL76L962164 1 19960921 A 4990 380029816 APU BOEING 767 767332 1382001 NM AFT FUSELAGE LOST OIL A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 179DN 17424 25144 APU SHUTDOWN AND WOULD NOT RESTART, SINGLE GEN OPERATION OIL QTY CHECKED FOUND LOW. SERVICED AND LEAK CHECKED FOR 15 MI NS, NO LEAKS FOUND. RECHECKED TANK, NO OIL ADDED. PERFORMED PROCEDURE SECOND TIME, NO ABNORMALTIES. 2 L 7 2 4F RT A1NM 1996100900002 19961009 00002 WP 1996 10 9 TC8A96059R1 1 19960924 A 5313 37542251 LONGERON DOUG DC8 DC862F 3021972 WP BS 600-620 CRACKED A TC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 183SK 45904 KOSC - DURING BASE MODIFICATION FOUND: LONGERON SPLICE CRACKED AT LONGERON 31 LEFT HAND BETWEEN STA 600-620 (CRACK .25 INCH). REMOVED AND REPLACED LONGERON SPLICE IAW DC8 SRM 51-1-20D AND 51-1-8. TASK CARD NR 81712. REPORT GENERATED BY AMERICAN INTERNATIONAL AIRWAYS, INC. (B4MR) FOR TRANS CONTINENTIAL AIRLINES (TC8A). 2 L 7 4 4F 4A25 1996100900003 19961009 00003 WP 1996 10 9 TC8A96060R1 1 19960924 A 5312 57726383 BULKHEAD WEB DOUG DC8 DC862F 3021972 WP AFT PRESS BLKHD DAMAGED A TC8A K NONE O OTHER IN INSP/MAINT 1 GL 23 183SK 45904 KOSC - COMPLIED WITH AD 90-16-05 AFT PRESSURE BULKHEAD WEB MODIFICATION. REPAIRED AFT PRESSURE BULKHEAD WEB IAW SB 53-5 3. REF DAC FAX FILE NR GLP1813/96-07-23-010. TASK CARD NR 79494. REPORT GENERATED BY AMERICAN INTERNATIONAL AIRWAYS, INC. (B4MR) FOR TRANS CONTINENTIAL AIRLINES (TC8A). 2 L 7 4 4F 4A25 1996100900005 19961009 00005 1996 10 9 96UAL900719 4 19960921 A 2210 54093022 SERVO STOP 2586232 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE AILERON SYST FAILED A UALA K NONE F FLT CONT AFFECTED CR CRUISE 1 WP 29 7945U 21899 AUTOPILOT CAUSES SHARP UNCOMMANDED TURNS. REPLACED AILERON SERVO AND STOP MECHANISM. 2 L 7 3 4F 4 F A3WE E2EA 1996100900006 19961009 00006 CE 1996 10 9 PNSA0902 1 19960909 A 3243 MASTER CYL PARKERHANFIN 26820011 CESSNA 208 208 2073702 CE RT BRAKES LEAKING A PNSA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 AL 03 9602F 20800103 RT BRAKE FAILED DURING ENGINE START. RESEALED MASTER CYL. 1 H 7 1 3T NT A37CE 1996101000001 19961010 00001 WP 1996 10 10 9620959905 1 19961002 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 955N 47160 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS AFT OF OVERWING EXITS INOPERATIVE. REPLACED BATTERIES. OPER ATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996101000002 19961010 00002 NM 1996 10 10 9620965519 1 19961001 A 2424 GEN CONTL UNIT BOEING 757 757251 1384970 NM LT ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 519US 23207 DURING APPLICATION OF TAKEOFF THRUST, THE LEFT IDG DRIVE LIGHT CAME ON. AIRCRAFT ABORTED TAKEOFF WITHOUT INCIDENT. REP LACED GENERATOR CONTROL UNIT AND SERVICED LEFT IDG. PERFORMED IDG CHECK OUT. SYSTEM CHECKED OK. 2 L 7 2 4F RT A2NM 1996101000003 19961010 00003 NE 1996 10 10 9620989873 2 19960930 A 7250 TURBINE DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE LT ENGINE FAILED A A NWAA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 GL 01 782NC 45273 8478 48107 688793 DURING CLIMB AT FL270 A NOISE WAS HEARD, THE LEFT ENGINE EPR DROPPED TO 1.2. CREW DIVERTED TO ALB AND LANDED WITHOUT IN CIDENT. MAINTENANCE REPLACED THE LEFT ENGINE. 2 L 7 2 4F 4 F A6WE E2EA 1996101000004 19961010 00004 NM 1996 10 10 9620976730 1 19960903 A 2780 126344171 PDU BOEING 747 7472J9F 1384806 NM NR 4 LE FLAP FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 630US 53031 219 21668 DURING CLIMB, THE LEFT NR 4 LEADING EDGE FLAP INDICATED INTRANSIT WHEN THE FLAPS WERE RETRACTED. AIRCRAFT RETURNED TO A NC AND LANDED WITHOUT INCIDENT. REPLACED THE NR 4 LEADING EDGE POWER DRIVE UNIT. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1996101000005 19961010 00005 NM 1996 10 10 UPS96221218 1 19961003 A 3234 LNDING GEAR HNDL BOEING 727 72727C 138400J NM COCKPIT LACK OF LUBE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 939UP 19532 LANDING GEAR HANDLE IS VERY HARD TO MOVE OUT AND IN DETENT, ALSO, UP AND DOWN. WHEN PLACING HANDLE FROM UP TO OFF, HAND LE DID NOT STOP AND LOWERED GEAR. LUBRICATED GEAR HANDLE AND OVERRIDE TRIGGER. PINNED LANDING GEAR AND ACTUATED HANDLE . GEAR HANDLE OPS CHECKED NORMAL. 2 L 7 3 4F A3WE 1996101000006 19961010 00006 NM 1996 10 10 UPS96421205 1 19960829 A 5320 FITTING BOEING 747 747121 1384871 NM BS 488/500 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE: C. FOUND CRACKS IN FITTING DUE TO INCORRECT RIVETING PRACTICE AT BS 488 - BS 500 STR 16 LT. REPLACED FITTING AT BS 488 - BS 500 STR 16 IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996101000007 19961010 00007 NM 1996 10 10 UPS96421206 1 19960917 A 5330 SKIN BOEING 747 747121 1384871 NM BS 340-360 MISDRILLED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE: C. EXISTING HOLE PITCH ON STR 6 BETWEEN STA 340 AND STA 360 LT HAS A SHORT FASTENER SPACING BETWEEN 9 FASTENERS. INSTALLED BACR15BB6D8 ON STR 6 BETWEEN STA 340 AND STA 360 LT ACC BOEING FAX DFX95-167. 2 L 7 4 4F A20WE 1996101000008 19961010 00008 NM 1996 10 10 UPS96421207 1 19960903 A 5320 UPPERCHORD BOEING 747 747121 1384871 NM BS 2140 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE: C. UPPER CHORD CORRODED AT BS 2140 BETWEEN LBL 57 TO LBL 100. REMOVED CORROSION AT UPPER CHORD AT BS 2140 BETWEEN LBL 57 TO LBL 10 0 ACC SRM 51-10-01. CORROSION NOT IN LIMITS ACC SRM 53-10-01, REPLACED UPPER CHORD FROM LBL 48 TO LBL 108 ACC SRM 53-10-07 FIG 12. 2 L 7 4 4F A20WE 1996101000009 19961010 00009 NM 1996 10 10 UPS96421208 1 19960919 A 5320 SPLICE BOEING 747 747121 1384871 NM BS 520 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE: C. STRINGER SPLICE 16 FRAME STA 520 LT DAMAGED. REPLACED STRINGER SPLICE 16 AT STA 520 LT IAW SRM 51 -30-02. 2 L 7 4 4F A20WE 1996101000010 19961010 00010 NM 1996 10 10 UPS96421209 1 19960917 A 5311 FRAME BOEING 747 747121 1384871 NM BS 360 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE: C. CRACKS ON FRAME 360 RT AT STRINGER 15 CUT-OUT AND ON CABLE PULLEY CUT-OUT. REPAIRED FRAME AT STA 360 RT IAW SRM 53-10-04. 2 L 7 4 4F A20WE 1996101000011 19961010 00011 NM 1996 10 10 UPS96421210 1 19960911 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 180-200 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE: C. STRINGER 5 CRACKED BETWEEN STA 180 AND STA 200 RT. REPLACED STRINGER 5 BETWEEN STA 180 AND STA 20 0 RT IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996101000012 19961010 00012 NM 1996 10 10 UPS96421211 1 19960916 A 5320 INTERCOSTAL BOEING 747 747121 1384871 NM BS 400-420 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE: C. INTERCOSTAL BETWEEN STA 400/420 RT AT STR 3A CRACKED. INTERCOSTAL BETWEEN STA 400/420 RT AT STR 3 A REPAIRED IAW SRM 51-40-03. 2 L 7 4 4F A20WE 1996101000013 19961010 00013 NM 1996 10 10 UPS96421212 1 19960917 A 5311 FRAME BOEING 747 747121 1384871 NM BS 360 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE: C. FRAME 360 LT CRACKED ON CABLE CUT-OUT BETWEEN STR 15 AND STR 16. FRAME 360 LT ON CABLE CUT-OUT BE TWEEN STR 15 AND STR 16 REPAIRED IAW SRM 53-10-04 FIG 18. 2 L 7 4 4F A20WE 1996101000014 19961010 00014 NM 1996 10 10 UPS96421213 1 19960915 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 434 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE: C. CRACK ON STRINGER 23 STA 434 RT. CRACK REPAIRED ON STR 23 STA 434 RT IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996101000015 19961010 00015 NM 1996 10 10 UPS96421214 1 19960910 A 5320 WEB BOEING 747 747121 1384871 NM BS 440-460 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE: C. WEB BETWEEN STA 460 AND STA 440 LT AT STRINGER 14 CRACKED. REPLACED WEB BETWEEN STA 460 AND STA 440 LT IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996101000016 19961010 00016 NM 1996 10 10 UPS96421215 1 19960919 A 5320 SPLICE BOEING 747 747121 1384871 NM BS 520 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE: C. STRINGER SPLICE DAMAGE AT STR 23 AND STR 24 STA 520 LT. REPLACED STRINGER SPLICE STR 23 AND STR 2 4 STA 520 LT IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996101000017 19961010 00017 NM 1996 10 10 UPS96421219 1 19960913 A 5320 FITTING BOEING 747 747121 1384871 NM BS 1416.06 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE: C. CORROSION AT FITTING AT BS 1416.06 BETWEEN RBL 11.33 TO LBL 11.33. FITTING OUT OF LIMITS AT BS 14 16.06 BETWEEN RBL 11.33 TO LBL 11.33 ACC SRM 53-10-01. REPLACED FITTING IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996101000018 19961010 00018 NM 1996 10 10 UPS96421220 1 19960913 A 5311 FRAME BOEING 747 747121 1384871 NM BS 1780 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE: C. FOUND FRAME DAMAGE AT BS 1780 STR 13 RT. REPAIRED FRAME AT BS 1780 BETWEEN STR 11 AND STR 15 RT IAW SRM 51-40-03 FIG 2. 2 L 7 4 4F A20WE 1996101000019 19961010 00019 NM 1996 10 10 UPS96421221 1 19960829 A 5320 SHEAR TIES BOEING 747 747121 1384871 NM BS 1660 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE: C. AFT CARGO COMPARTMENT, FOUND CRACK IN FRAME SHEAR TIES AT SKIN ATTACHMENTS BS 1660 RT, BETWEEN S 41/40 AND S 39/38 (3 EA). REMOVED CRACKED SHEAR TIES AND REPAIRED SHEAR TIES ACC SRM 53-10-04 FIG 3. 2 L 7 4 4F A20WE 1996101000020 19961010 00020 NM 1996 10 10 UPS96421222 1 19960830 A 5320 PRESSURE PAN BOEING 747 747121 1384871 NM BS 2360 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE: C. BS 2360 PRESS PAN ASSY APU DUCT MOUNT FLANGE AND UPPER SIDE, MAJOR DAMAGE. REPLACED PRESS PAN AT BS 2360 IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996101000021 19961010 00021 NM 1996 10 10 UPS96421223 1 19960910 A 5320 WEB BOEING 747 747121 1384871 NM BS 1380 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE: C. FOUND FOUR CRACKS IN WEB ASSY AT BS 1380 LBL 98 TO 117. REPLACED WEB ASSY IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996101000022 19961010 00022 NM 1996 10 10 UPS96421225 1 19961002 A 5730 SKIN BOEING 747 747121 1384871 NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE: C. RT LOWER WING SKIN, REPAIRED CORROSION INSIDE LEADING EDGE CAVITY FORWARD OF LOWER FRONT SPAR AT I LES 944.1015. REPAIRED LOWER SKIN ACC KLM DFX96-192. APPROVED PER UPS EFN 747-57-0339. 2 L 7 4 4F A20WE 1996101000023 19961010 00023 NM 1996 10 10 UPS96421226 1 19960903 A 5311 FRAME BOEING 747 747121 1384871 NM BS 2120 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE: C. BULK CARGO COMPARTMENT, FOUND CRACK IN FRAME WEB AT STRINGER CUTOUT CORNER AT BS 2120, S29L. REPA IRED FRAME WEB AT STRINGER CUTOUT CORNER ACC TO SRM 53-10-04, FIG 39. 2 L 7 4 4F A20WE 1996101000024 19961010 00024 NM 1996 10 10 UPS96421227 1 19961001 A 5320 SPLICE ANGLE BOEING 747 747121 1384871 NM BS 1960 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE: C. BULK CARGO COMPARTMENT, FOUND DURING REPAIR OF FRAME, CRACK BS 1360 NRC 7126 21, A CRACK IN SPLICE ANGLE AT BS 1960 FRAME/SPLICE S34L. REPLACED FRAME/SPLICE ANGLE ACC TO SRM 51-30-02. 2 L 7 4 4F A20WE 1996101000025 19961010 00025 NE 1996 10 10 UPS96521199 2 19960930 A 7261 ENGINE BOEING 757 75724APF 1384969 NM PWA 2037 PW2040 NE NR 2 HIGH OIL CONSMPT A A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 428UP 25459 P726657 ACID SMELL IN COCKPIT IN-FLIGHT. SAME INTENSITY NOTICED WITH EITHER ACM OPERATING. ENG ANTI-ICE WAS USED FOR SHORT DUR ATION. DID NOT NOTICE SMELL ON GROUND WITH ACM'S RUNNING WITH BLEED SOURCE. BURNS EYES AND THROATS. NR 2 ENG REQUIRES CHANGING DUE TO HIGH OIL CONSUMPTION. CHANGED NR 2 ENG IN REF TO TC 5001 PW THROUGH STEP 74-E. P/N OFF PW 2040. S/N OFF P726657. P/N ON PW2040. S/N ON 717929. 2 L 7 2 4F 4 F RT A2NM E17NE 1996101000026 19961010 00026 WP 1996 10 10 UPS96821198 1 19960930 A 3230 35973395505 BUNGEE ACTUATOR DOUG DC8 DC873F 302199F WP LT MLG FAILED A IPXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 868UP 45968 INSPECTION TYPE N/A, ATB DUE TO LANDING GEAR DR/LANDING GEAR UP NOT LATCHED LT ON. DISCOVERED DWN LCK CYL ACT ROD END E YELET FAILURE. THIS ALSO LED TO GOUGES IN THE ATTACHMENT FITTING OF THE UPPER DWN LCK LINKS FWD AND AFT. FOUND LT OVER CENTER BUNGEE ACTUATOR ROD END FAILED. REMOVED AND REPLACED ACTUATOR AND BOTH UPPER OVERCENTER LINKS ON LT GEAR PER MM 32-32-03 PG 201 TO 207 AND PERFORMED GEAR RETRACT OPERATION, ALL FUNCT NORMAL. (P/N 5714918-2) (S/N 71 RH) OFF, (P/N 5 714918-1) ON. 2 L 7 4 4F RT 4A25 1996101000027 19961010 00027 WP 1996 10 10 UPS96821200 1 19960930 A 3230 HOOK ASSY DOUG DC8 DC873F 302199F WP MLG FAILED A IPXA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 812UP 46112 AFTER TAKEOFF, GEAR WOULD NOT RETRACT. RAN CHECKLIST. SAW SOMETHING WHITE FLAPPING ON RIGHT SIDE OF STRUT. AIR TURN B ACK TO DEN. FOUND HOOK ASSY SEPARATED FROM ANTI-RETRACTION ACTUATOR DUE TO CORROSION OF HOOK ASSY. REPLACED HOOK ASSY. GROUND SHIFT CHK NORMAL. 2 L 7 4 4F RT 4A25 1996101000028 19961010 00028 WP 1996 10 10 UPS96821201 1 19960827 A 5312 56150402 BULKHEAD FRAME DOUG DC8 DC873F 302199F WP BS 980 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE: CS2. HEAVY CORROSION ON BULKHEAD FRAME FS 980 LONGERON 25R, AND A 3 INCH LONG CRACK BETWEEN LONGERONS 23R-24R. REPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996101000029 19961010 00029 WP 1996 10 10 UPS96821202 1 19960827 A 5511 565208611 SPAR DOUG DC8 DC873F 302199F WP LT HOR STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE: CS2. LEFT HORIZONTAL STABILIZER REAR SPAR WEB CRACKED AROUND FASTENER HOLD STA XE119.52. REPAIRED P ER UPS EO. 2 L 7 4 4F RT 4A25 1996101000030 19961010 00030 WP 1996 10 10 UPS96821203 1 19960917 A 5730 5769859505 SKIN DOUG DC8 DC873F 302199F WP LT WING LE CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE: CS2. LEFT WING LEADING EDGE ASSY OVER NR 2 PYLON HAS 69 COUNTER SINK ATTACH FASTENER HOLES CORRODED. REPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996101000031 19961010 00031 WP 1996 10 10 UPS96821217 1 19961002 A 3350 6012235 LIGHTS DOUG DC8 DC871F 302199D WP CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 718UP 46018 EMERGENCY LIGHTS INOPERATIVE. ARM SYST KILL POWER NO LIGHTS. PULL CONTROL CIRCUIT BREAKER. SYST. LIGHTS COME ON. REMO VED AND REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT IAW M/M 33-50-01. EMERGENCY LIGHTS OPERATION TEST IAW M/M 33 -50-01. P/N ON 5708458-503. S/N ON FTL064. P/N OFF 60-1223-5. S/N OFF 335. 2 L 7 4 4F RT 4A25 1996101000032 19961010 00032 NM 1996 10 10 96FDEA01558 1 19960923 A 5315 FLOOR BEAM BOEING 727 727233 138408A NM BS 344 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 280FE 22347 FORWARD CABIN FLOOR BEAM STA 344 HAS CORROSION BOTH TOP AND BOTTOM OF TOP FLANGE AT NUTPLATE HOLES LBL 30 - RBL 15 ( MARKED TOP AND BOTTOM). REMOVED CORROSION PER MM 51-10-6. OUT OF LIMITS AT LBL 4, 12, AND 22 PER 53-10-8 FIG 9. INST ALLED SPLICE ANGLES PER FEDEX DRAWING NR SR27-53-007. 2 L 7 3 4F RT A3WE 1996101000033 19961010 00033 NE 1996 10 10 96FDEA01560 2 19961003 A 7200 ENGINE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE NR 2 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 612FE 48605 702922 ENGINE FAILED INSP PER EA 1-7220-31514, INSP OF FIRST STAGE BOOSTER VANES. FOUND NUMEROUS LOOSE AND MISSING FASTENERS BOOSTER CASE CRACKED IN SEVERAL PLACES. REMOVED AND REPLACED NR 2 ENGINE. RII COMPLETED, ENG RUN, LEAK AND OPS CHECK G OOD. 2 L 7 3 4F 4 F RT A22WE E31N3 1996101000034 19961010 00034 NM 1996 10 10 96UAL900698 1 19960914 A 2752 2061121 DRIVE MOTOR VICKERS 240863 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE TE FLAPS LEAKING A UALA O OTHER K FLUID LOSS AP APPROACH 1 WP 29 7287U 21565 OUTBOARD FLAPS DID NOT EXTEND TO FLAP 30 POSITION WHEN SELECTED. STOPPED IN THE BLACK JUST PAST FLAPS 25 POSITION. FLA PS EXTENDED WITH ALTERNATE FLAP MOTOR. REPLACED OUTBOARD TRAILING EDGE FLAP MOTOR DUE TO LEAKING AT DRIVE SEAL. ALSO REPLACED OUTBOARD TRAILING EDGE INDICATOR. SYSTEM CHECKED NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1996101000035 19961010 00035 NM 1996 10 10 96UAL900739 1 19960923 A 3020 ANTI ICE DUCT BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE NR 1 ENGINE CRACKED A UALA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 WP 29 9030U 19068 DURING CLIMB OUT NR 1 ENGINE OVERHEAT DETECTION WARNING ACTIVATED. ENGINE RETARDED TO IDLE POSITION, WARNING ABATED. A IRCRAFT RETURNED TO FIELD. NR ONE ENGINE COWL ANTI-ICE DUCT CRACKED AT 12 O'CLOCK POSITION. REMOVED AND REPLACED. PAR T TOTAL CYCLES, 9,056. 2 L 7 2 4F 4 F A16WE E2EA 1996101000036 19961010 00036 NM 1996 10 10 96UAL900740 1 19960923 A 3230 LOCK PIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LANDING GEAR NOT REMOVED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 505UA 24626 ON CLIMB-OUT, LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO FIELD. REMOVED NOSE LANDING GEAR DOWNLOCK PIN. OPER ATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996101000037 19961010 00037 NE 1996 10 10 96UAL900741 2 19960923 A 7200 ENGINE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE PYLON BIRD STRIKE A UALA A UNSCHED LANDING C F.O.D. TO TAKEOFF 1 WP 29 924UA 13804 26645 DURING TAKEOFF FROM DEN, NR 2 ENGINE EXPERIENCED A BIRD STRIKE. AIRCRAFT RETURNED TO FIELD. ENGINE WAS REPLACED DUE TO A FAN INLET CASE ABRAIDABLE WAS MISSING. 2 L 7 2 4F 4 F RT A16WE E2GL 1996101000038 19961010 00038 NM 1996 10 10 96UAL900742 1 19960924 A 4950 BLEED SYST BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE APU INOPERATIVE A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 7453U 21907 APU BLEED SYSTEM INOPERATIVE. WHEN APU BLEED SWITCH IS PLACED IN THE OFF POSITION, EGT RISES RAPIDLY AND PACKS TRIP. 2 L 7 3 4F 4 F A3WE E2EA 1996101000039 19961010 00039 NM 1996 10 10 96UAL900743 1 19960924 A 2822 M259883245 O-RING GEC S34W1013 BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE BOOST PUMP FAILED A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 773UA 26929 FUEL LEAKING FROM THE RIGHT AFT MAIN BOOST PUMP ON REAR SPAR. *S/D* LEAK RESULTED FROM DAMAGED O-RING. REMOVED PUMP P ER MM 28-22-05, REPLACED O-RING AND REINSTALLED PUMP, CHECKED OK AFTER INSTALLATION. 2 L 7 2 4F 4 F RT T0001SE E46NE 1996101000040 19961010 00040 NM 1996 10 10 96UAL900744 1 19960924 A 2130 69B4128414 DUCT BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE CABIN RUPTURED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 160UA 19524 19524 21237 UNABLE TO MAINTAIN CABIN PRESSURE. PNEUMATIC CROSS-OVER DUCT RUPTURED IN-FLIGHT. DUCT FAILED NEAR A WELD. CAUSE UNKNO WN. DUCTS REPLACED. PART TOTAL CYCLES, 2,804. 2 L 7 4 4F 4 F A20WE E20EA 1996101000041 19961010 00041 NE 1996 10 10 96UAL900747 2 19960925 A 7200 ENGINE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 1 FAILED A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 775UA 26947 NR 1 ENGINE LEAKING FLUID WITH APPEARANCE OF BURNED SKYDROL. LOCATION IS REVERSER COWL, LOWER AFT SECTION. 2 L 7 2 4F 4 F RT T0001SE E46NE 1996101000042 19961010 00042 NE 1996 10 10 96UAL900748 2 19960926 A 7250 629704 TURBINE BLADE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE FAILED A UALA O OTHER E J VIBRATION/BUFFET WARNING INDICATION DE DESCENT 1 WP 29 7270U 3587 21417 700136 NR 2 ENGINE VIBRATION NOTICED WHEN REDUCING POWER FOR DESCENT, LOUDER AT LOWER N1'S. ALL ENGINE INSTRUMENTS NORMAL. *S /D* ONE T-4 BLADE FAILED AT THE AIRFOIL MID-SPAN. EXAMINATION SHOWS FAILURE MODE TO BE THAT OF STRESS RUPTURE DUE TO B LADE CREEP WHICH RESULTED FROM OVER TEMPERATURE. THE BLADES ON EITHER SIDE OF FAILED BLADE HAD MISSING SHROUDS BUT DID NOT INDICATE OVER TEMPERATURE. REPLACED N1 TURBINE ASSEMBLY. 2 L 7 3 4F 4 F A3WE E2EA 1996101000043 19961010 00043 NM 1996 10 10 96UAL900749 1 19960926 A 2740 TRIM BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE STAB TRIM MALFUNCTIONED A UALA O OTHER F FLT CONT AFFECTED CR CRUISE 1 WP 29 7457U 21911 STABILIZER TRIM ERRATIC. WHEN THE CREW RELEASES THE TRIM SWITCHES THE WHEEL CONTINUES TO MOVE FORWARD AND SOMETIMES IT WILL GO IN THE OTHER DIRECTION. (TRIM OR CRUISE.) 2 L 7 3 4F 4 F A3WE E2EA 1996101000044 19961010 00044 NM 1996 10 10 96UAL900750 1 19960926 A 2780 RETRACT MECH BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 6 LE FLAP MALFUNCTIONED A UALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 WP 29 7457U 21911 AFTER TAKEOFF, NR 6 LEADING EDGE FLAP WOULD NOT RETRACT. AMBER COCKPIT INDICATION AND VISUAL INSPECTION IN-FLIGHT VERIF IED FLAP EXTENDED. RETURNED TO ORD. 2 L 7 3 4F 4 F A3WE E2EA 1996101000045 19961010 00045 NM 1996 10 10 96UAL900751 1 19960926 A 2120 AIR DISTR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 7299U 21894 AIR CONDITIONING SYSTEM ODOR IN ALL CABINS DURING CLIMB WITH BOTH PACKS ON. 2 L 7 3 4F 4 F A3WE E2EA 1996101000046 19961010 00046 NM 1996 10 10 96UAL900752 1 19960926 A 2750 RETRACT MECH BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE TE FLAPS OUT OF ADJUST A UALA O OTHER J F WARNING INDICATION FLT CONT AFFECTED NR NOT REPORTED 1 WP 29 7281U 21559 ON APPROACH TO ORD, OUTBOARD FLAPS STOP AT 15 DEGREES. INBOARDS WENT TO 25 DEGREES. OUTBOARDS SHOW SOME ASYMMETRY IN N EEDLES AT 15 DEGREES. 2 L 7 3 4F 4 F A3WE E2EA 1996101000047 19961010 00047 NM 1996 10 10 96UAL900753 1 19960926 A 5330 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7442U 21896 LOWER FUSELAGE OUTBOARD AND JUST AFT OF VHF ANTENNA HAS EVIDENCE OF CORROSION AND CRACK IN SKIN. 2 L 7 3 4F 4 F A3WE E2EA 1996101000048 19961010 00048 NM 1996 10 10 96UAL900754 1 19960926 A 2820 69186127 VENT TUBE ELBOW BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 FUEL TANK CRACKED A UALA O OTHER O OTHER CR CRUISE 1 WP 29 7254U 21401 X-FEEDING TO ALL 3 ENGINES FROM NR 2 FUEL TANK, WITHIN 1 HOUR AND 25 MINUTES INTO FLIGHT HAD UNWANTED FUEL TRANSFER OF 8 00 POUNDS FROM NR 1 TANK. *S/D* REPLACED NR 1 FUEL TANK VENT TUBE ELBOW. 2 L 7 3 4F 4 F A3WE E2EA 1996101000049 19961010 00049 NE 1996 10 10 96UAL900755 2 19960926 A 7200 ENGINE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 2 VIBRATION A UALA O OTHER E VIBRATION/BUFFET CL CLIMB 1 WP 29 7256U 21403 NR 2 ENGINE VIBRATING ABOVE 3000 POUNDS FUEL FLOW 1.75 EPR 82 PERCENT N1. A METAL RAPPING IS FELT IN THE THROTTLE AT H IGHER POWER SETTINGS. 2 L 7 3 4F 4 F A3WE E2EA 1996101000050 19961010 00050 NM 1996 10 10 96UAL900756 1 19960927 A 3350 BATTERY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 586UA 26710 EMERGENCY LIGHTS ROW 16L, 18L INOP. EMERGENCY EGRESS LIGHTING ROWS 16-23 INOP. BATTERY PACK FAILED. REPLACED BATTERY PACK. OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996101000051 19961010 00051 1996 10 10 96UAL900757 4 19960927 A 2565 SEAM AIR CRUISER D29835103 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE SLIDE SEPARATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7265U 17564578 21412 DURING TIME CONTROLLED OVERHAUL SLIDE, ENCOUNTERED SEAM SEPARATION. SCRAPPED UNIT. 2 L 7 3 4F 4 F A3WE E2EA 1996101000052 19961010 00052 NE 1996 10 10 96UAL900758 2 19960927 A 7200 ENGINE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 2 LOW POWER A UALA O OTHER R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 29 771UA 26932 ON TAKEOFF AT GRU (SAO PAULO), NR 2 ENGINE DID NOT DEVELOP FULL TAKEOFF, E.P.R. N1 WAS IN TOLERANCE. TAKEOFF WAS MADE W ITH AIR CONDITIONING PACKS OFF. PRELIMINARY INFORMATION INDICATES E.P.R. TARGET FOR NR 2 ENGINE DIFFERENT FROM NR 1 ENG INE TARGET. 2 L 7 2 4F 4 F RT T0001SE E46NE 1996101000053 19961010 00053 GL 1996 10 10 96UAL900759 2 19960927 A 7240 9135M62P01 BORESCOPE PLUG DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 2 ENGINE MISSING A UALA K NONE A FLAME/FIRE IN INSP/MAINT 1 WP 29 1846U 48262 NR 2 ENGINE RIGHT SIDE REVERSER CORE INNER FIRE BLANKET MISSING AND INNER SKIN TORN AWAY WITH A 9 INCH SECTION MISSING. DAMAGED AREA APPROXIMATELY 23 INCHES BY 10 INCHES. A COMBUSTOR BORESCOPE PLUG IN THE GENERAL AREA OF THE DAMAGED RIGHT REVERSER HALF WAS MISSING. UNDER INVESTIGATION. REPLACED RIGHT REVERSER HALF. 2 L 7 3 4F 4 F A22WE E23EA 1996101000054 19961010 00054 NM 1996 10 10 96UAL900760 1 19960927 A 2820 FUEL TRANSFER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 TANK MALFUNCTIONED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 7294U 21572 UNWANTED FUEL TRANSFER FROM NR 1 TO NR 2 TANK. NR 3 TANK WAS 700 POUNDS HIGHER THAN NR 1. 2 L 7 3 4F 4 F A3WE E2EA 1996101000055 19961010 00055 NM 1996 10 10 96UAL900761 1 19960927 A 3350 LIGHT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7253U 21400 OVERHEAD EMERGENCY LIGHT ABOVE SEAT ROW 21 INOPERATIVE. 2 L 7 3 4F 4 F A3WE E2EA 1996101000056 19961010 00056 NM 1996 10 10 P5CA9600744 1 19960926 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 1648 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION AT STRINGER 48R STA 1648. REMOVED CORROSION PER BAC SRM 51-22-00, WITHIN LIMITS PER BAC SRM 51-12-00, REPROTECTED AREA PER BAC SRM 51-21-00. 2 L 7 4 4F A20WE 1996101000057 19961010 00057 NM 1996 10 10 P5CA9600745 1 19960924 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 1416 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION AT STRINGER 41 STA 1416 RBL 160. REMOVED CORROSION PER BAC SRM 51-10-03, WITHIN LIMITS PER BAC SRM 53 -40-01, REPROTECTED AREA PER BAC SRM 51-21-00. 2 L 7 4 4F A20WE 1996101000058 19961010 00058 NM 1996 10 10 P5CA9600746 1 19961003 A 3350 S1356B37 LIGHT BOEING 747 747132 1384882 NM CABIN INOPERATIVE A P5CA K NONE L NO TEST IN INSP/MAINT 1 WP 23 856FT 19897 INOPERATIVE EMERGENCY LIGHT ON UPPER DECK CEILING. REPLACED EMERGENCY LIGHT ASSEMBLY PER BAC MM 33-51-06. 2 L 7 4 4F A20WE 1996101000059 19961010 00059 NM 1996 10 10 P5CA9600747 1 19960926 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 1678 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION STRINGER S48R BS 1678. CORROSION REMOVED PER BOEING SRM 51-22-00. FOUND WITHIN LIMITS PER 51-12-00 RE PROTECTED PER 51-21-00. 2 L 7 4 4F A20WE 1996101000060 19961010 00060 WP 1996 10 10 CKSA96157 1 19960919 A 5330 SKIN DOUG DC8 DC851 3021920 WP BS 400-420 DENTED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 804CK 45689 KORD - ONE INCH DIAMETER HOLE IN AIRCRAFT SKIN, 18 INCHES AFT OF RIGHT FORWARD STATIC PORT. DISCOVERED ON POST-FLIGHT I NSPECTION. REPAIRED IAW SKETCH NR AIA/E/2339. DATED 09-19-96. 2 L 7 4 4F 4A25 1996101000061 19961010 00061 GL 1996 10 10 ERAA96266 2 19960627 A 7250 6853279 WHEEL 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL CURVIC WORN A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 296EH 1078 CAT37013 S849 WHEEL HAS WORN CURVIC DUE TO OUTER SHAFT THAT WAS PURCHASED FROM SUPERIOR , THAT HAS MATERIAL AROUND CURVIC FLAKING OFF. WORN WHEEL IS DUE TO OUTER SHAFT PROBLEM. THE #4 WHEEL IS AN ALLISON PART. SEE ERAA MMIR REPORT #ERAA000258. 1 G 7 2 3U 3 U H3EU E4CE 1996101000063 19961010 00063 GL 1996 10 10 ERAA96268 2 19960627 A 7310 23055466 GEARBOX COVER BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL RED GR BOX LEAKING A ERAA K NONE K FLUID LOSS IN INSP/MAINT 1 AL 03 130EH S558 GEARBOX OVERHAULED ON CADORATH WORK ORDER L707 AND REC'D BACK AT ERA 6-11-96. TORQUE METER BUSHING LEAKING. 1 G 7 2 3U 3 U H3EU E4CE 1996101000064 19961010 00064 GL 1996 10 10 ERAA96269 2 19960628 A 7250 A23038218 NOZZLE 6898735 BOLKMS 105 BO105A EU ALLSN 250C 250C20 03013 GL 1ST STAGE DEFECTIVE A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 296EH 1078 CAT37013 S849 OUTER BAND AND VANE CRACKS. 1 G 7 2 3U 3 U H3EU E4CE 1996101000065 19961010 00065 GL 1996 10 10 ERAA96270 2 19960628 A 7250 A23031938 NOZZLE 6898735 BOLKMS 105 BO105A EU ALLSN 250C 250C20 03013 GL NR 2 DEFECTIVE A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 296EH 1078 CAT37013 S849 CRACKS IN DIAPHRAGM AND WARPED VANES. 1 G 7 2 3U 3 U H3EU E4CE 1996101000066 19961010 00066 GL 1996 10 10 ERAA96271 2 19960628 A 7250 A6875351 U RING GASKET 6898735 BOLKMS 105 BO105A EU ALLSN 250C 250C20 03013 GL TURBINE SPLIT A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 296EH 1078 CAT37013 S849 U RING SPLIT. RETURNING TO SUPERIOR. 1 G 7 2 3U 3 U H3EU E4CE 1996101000067 19961010 00067 EU 1996 10 10 ERAA96272 1 19960628 A 6520 4619310069 ROLLER BEARING 4619002003 BOLKMS 105 BO105S 5626006 EU T/R GR BOX FAILED A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 427EH 15 1295 S554 OUTER RACE BREAKING DOWN. 1 G 7 2 3U H3EU 1996101000068 19961010 00068 EU 1996 10 10 ERAA96273 1 19960628 A 6520 4619310070 ROLLER BEARING 4619002003 BOLKMS 105 BO105S 5626006 EU T/R GR BOX FAILED A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 427EH 15 1295 S554 OUTER RACE BREAKING DOWN. 1 G 7 2 3U H3EU 1996101000069 19961010 00069 GL 1996 10 10 ERAA96276 2 19960710 A 7250 23038218 NOZZLE 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL 1ST STAGE CRACKED A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 125EH CAT25326 S562 #1 NOZZLE WAS RET'D FROM OVERHAUL , 10-4-95. T.S.O. IS 174.2 HRS AND NOZZLE HAS CRACKED OUTER BAND AND VANES. 1 G 7 2 3U 3 U H3EU E4CE 1996101000070 19961010 00070 GL 1996 10 10 ERAA96277 2 19960711 A 7250 6878498 NOZZLE 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL 2ND STAGE CRACKED A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 125EH CAT25326 S562 #2 NOZZLE HAS CRACKS IN OUTER BAND AND VANES. 1 G 7 2 3U 3 U H3EU E4CE 1996101000071 19961010 00071 GL 1996 10 10 ERAA96278 2 19960715 A 7250 6870813 VANE ASSY BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL TURBINE FAILED A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 124EH S559 VANE ASSY SENT FOR OVERHAUL ON STANDARD AERO WORK ORDER L127225 2-9-96. VANE ASSY HAS -0- TSO AND STUB BROKE OFF DU RING INSTALLATION. 1 G 7 2 3U 3 U H3EU E4CE 1996101000072 19961010 00072 GL 1996 10 10 ERAA96279 2 19960715 A 7323 2524667 GOVERNOR BOLKMS 105 BO105A EU ALLSN 250C 250C20 03013 GL NR 1 ENG FAULTY A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 423EH 10283 S543 #ONE ENGINE WOULD DROP OFF LINE ABOVE IDLE SETTING CAUSING MORE THAN 12% TORQUE SPLIT. GOVERNOR WAS SET AS FAST AS POSS IBLE. GOVERNOR HAS 895.8 HRS SINCE O/H 2/28/95. 1 G 7 2 3U 3 U H3EU E4CE 1996101000073 19961010 00073 GL 1996 10 10 ERAA96280 2 19960715 A 7323 2524667 GOVERNOR BOLKMS 105 BO105A EU ALLSN 250C 250C20 03013 GL ENGINE DEFECTIVE A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 293EH 11232 S844 TORQUE SPLITS UP TO 30%. GOVERNOR WAS O/H 9/21/95. 1 G 7 2 3U 3 U H3EU E4CE 1996101000074 19961010 00074 GL 1996 10 10 ERAA96281 2 19960716 A 7260 6896437 GEAR BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL OIL PUMP PITTED A ERAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 124EH S559 FUEL CONTROL/OIL PUMP GEAR WAS O/H AND RETURNED TO ERA 7/10/96 RECEIVED BACK WITH PITS IN GEAR TEETH. 1 G 7 2 3U 3 U H3EU E4CE 1996101000075 19961010 00075 GL 1996 10 10 ERAA96282 2 19960716 A 7323 2524667 GOVERNOR BOLKMS 105 BO105A EU ALLSN 250C 250C20 03013 GL ENGINE FAULTY A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 296EH 9769 S849 GOVERNOR WAS OVERHAULED. PART HAS 587.3 HRS TSO AND IS VERY SLOW, WILL NOT KEEP UP WITH OTHER GOVERNOR. TORQUE SPLITS WITH HIGH TORQUE. 1 G 7 2 3U 3 U H3EU E4CE 1996101000076 19961010 00076 GL 1996 10 10 ERAA96283 2 19960716 A 7321 2524644 FUEL CONTROL BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENGINE DEFECTIVE A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 127EH 11348 11348 S571 FUEL CONTROL WILL NOT METER FUEL. OVERHAULED 11-95; HAS 486.8 HRS TSO. 1 G 7 2 3U 3 U H3EU E4CE 1996101000077 19961010 00077 GL 1996 10 10 ERAA96284 2 19960719 A 7230 6851574 SCROLL BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENGINE DAMAGED A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 124EH S559 SCROLL OVERHAULED 6-13-96 AND HAS THREAD DAMAGE TO STUD AS MARKED. 1 G 7 2 3U 3 U H3EU E4CE 1996101000078 19961010 00078 GL 1996 10 10 ERAA96286 2 19960730 A 7250 6898731 PT SUPPORT BOLKMS 105 BO105A EU ALLSN 250C 250C20 03013 GL SUMP COVER DEFECTIVE A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 135EH S675 PT SUPPORT OVERHAULED 7-3-96. REAR SUMP COVER NOT SECURE TO SUPPORT. EVALUATE CRACKS ADJACENT TO 6 O'CLOCK STRUT. 1 G 7 2 3U 3 U H3EU E4CE 1996101000079 19961010 00079 1996 10 10 ERAA96290 2 19960816 A 7230 6851574 SCROLL BOLKMS 105 BO105S 5626006 EU ENGINE DEFECTIVE A ERAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 126EH S567 SCROLL OVERHAULED AND REC'D BACK AT ERA 8-13-96 WITH ROUGH WELD ON OUTER RIM ADJACENT TO STUDS. 1 G 7 2 3U H3EU 1996101000080 19961010 00080 GL 1996 10 10 ERAA96292 2 19960816 A 7250 23031938 NOZZLE BOLKMS 105 BO105A EU ALLSN 250C 250C20 03013 GL 2ND STAGE DEFECTIVE A ERAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 135EH S675 #2 NOZZLE WAS OVERHAULED. ERA REC'D BACK AT ERA 7-18-96. SEAL BORE TOO LARGE. PROTRUSIONS ON THE INNER BAND, NEE DS TO BE REMOVED. 1 G 7 2 3U 3 U H3EU E4CE 1996101000081 19961010 00081 GL 1996 10 10 ERAA96293 2 19960819 A 7210 23008021 HOUSING BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL GR BOX DEFECTIVE A ERAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 427EH S554 HOUSING OVERHAULED 8/2 96. TSO -0- UNABLE TO INSTALL CHECK VALVE INTO HOUSING BORE. 1 G 7 2 3U 3 U H3EU E4CE 1996101000082 19961010 00082 GL 1996 10 10 ERAA96294 2 19960819 A 7261 23035102 HOUSING BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL OIL FILTER DEFECTIVE A ERAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 427EH S554 RETURNED FROM OVERHAUL 5-6-96 UNABLE TO PASS FLOW TEST AT 180 PPH, PSIG=118. ALLISON OVERHAUL MANUAL PAR 7-54 C. (8) P ART HAS -0- TSO . 1 G 7 2 3U 3 U H3EU E4CE 1996101000083 19961010 00083 EU 1996 10 10 ERAA96295 1 19960820 A 6230 4638305001 BEARING 4638001001 BOLKMS 105 BO105S 5626006 EU MAST FAILED A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 149EH 488 923 S705 OUTER RACE BREAKING DOWN. 1 G 7 2 3U H3EU 1996101000084 19961010 00084 EU 1996 10 10 ERAA96296 1 19960820 A 6320 4638305028 BEARING 4638001001 BOLKMS 105 BO105S 5626006 EU M/R GR BOX FAILED A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 149EH 488 923 S705 OUTER RACE BREAKING DOWN. 1 G 7 2 3U H3EU 1996101000085 19961010 00085 GL 1996 10 10 ERAA96297 2 19960820 A 7210 23055464 GEARBOX COVER BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENGINE DEFECTIVE A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 427EH S554 NON SELF LOCKING INSERT NEEDS TO BE INSTALLED AT ACCESSORY LOCATION AS PER CEB-A-1226. 1 G 7 2 3U 3 U H3EU E4CE 1996101000086 19961010 00086 EU 1996 10 10 ERAA96299 1 19960820 A 6210 10515110 BLADE BOLKMS 105 BO105A EU M/R DEFECTIVE A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 298EH 768 S845 BLADES REM'D FROM A/C WITH 767.8 HRS TSN, DUE TO GROUND SHUFFLE. RETURNING REQUESTING ROOT END EXAMINATION AND REPAI R. SERIAL NUMBERS OF BLADES ARE: 72, 95, 98, 100 . 1 G 7 2 3U H3EU 1996101000087 19961010 00087 GL 1996 10 10 ERAA96300 2 19960823 A 7250 6851531 NOZZLE BOLKMS 105 BO105A EU ALLSN 250C 250C20 03013 GL 4TH STAGE DEFECTIVE A ERAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 299EH S807 OVERHAULED AND REC'D BACK AT ERA 8-5-96. SEAL AND TIP PATHS WON'T RUN OUT WITHIN LIMITS. 1 G 7 2 3U 3 U H3EU E4CE 1996101000088 19961010 00088 GL 1996 10 10 ERAA96301 2 19960905 A 7250 A6840406 TIE BOLT NUT BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENGINE DEFECTIVE A ERAA K NONE K FLUID LOSS IN INSP/MAINT 1 AL 03 125EH 174 S562 OIL LEAKING PAST TIE BOLT NUT. SENDING TO EXTEX FOR EVALUATION TO DETERMINE CAUSE. OTHER PARTS AFFECTED ARE TIE BOLT P/N A23008020, S/N H144, #2 WHEEL P/N 6898782, S/N HX115226, #1 WHEEL P/N 6886407, S/N X134859, SPLINED ADA PTER, P/N6898784, S/N 102474. ALL LISTED PARTS ARE BEING SENT IN FOR EVALUATION ON ERA P.O.G 120690. 1 G 7 2 3U 3 U H3EU E4CE 1996101000089 19961010 00089 EU 1996 10 10 ERAA96303 1 19960905 A 2435 230322111 ARMATURE BOLKMS 105 BO105S 5626006 EU START GEN DEFECTIVE A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 149EH S705 GENERATOR ARMATURE REPAIRED AND REC'D BACK AT ERA 8-23-96. INSTALLED IN GENERATOR AND WILL NOT PASS START TEST. COULD N OT INSTALL IN AIRCRAFT. 1 G 7 2 3U H3EU 1996101000090 19961010 00090 SW 1996 10 10 ERAA96304 1 19960905 A 2435 230461030 ARMATURE BELL 412 412 1182202 SW START/GEN FAILED TIR INSP A ERAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 414EH 33007 UNIT REPAIRED AND HAS NOT BEEN INST'D ON A/C SINCE RETURNING FROM REPAIR. FAILED T.I.R. INSPECTION AND DRAGS ON STATOR . 1 G 7 2 4U H4SW 1996101000091 19961010 00091 SW 1996 10 10 ERAA96305 1 19960905 A 2436 51509002R D.C. CONTROLLER BELL 412 412 1182202 SW NR 1 GEN FAILED A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 422EH 33068 #1 GENERATOR INOP WITH THIS REGULATOR INSTALLED. CHANGED REGULATOR AND GENERATOR WORKED FINE. UNIT WAS PURCHASED AS E XCHANGE AND ONLY HAD 4 HRS ON IT. 1 G 7 2 4U H4SW 1996101000092 19961010 00092 GL 1996 10 10 ERAA96306 2 19960905 A 7210 6875035 BEARING BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENG GR BOX FAILED A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 426EH S552 WAS INSPECTED BY BEARINGS INSP., INC ON W/O 17456-409 SEPT. 12, 1995 AND HAS BEEN DETERMINED TO BE BAD AND INOPERABLE. 1 G 7 2 3U 3 U H3EU E4CE 1996101000093 19961010 00093 GL 1996 10 10 ERAA96307 2 19960906 A 7250 6890040 NOZZLE BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL 1ST STAGE DEFECTIVE A ERAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 NOZZLE WAS OVERHAULED AND RET'D TO ERA 7-22-96. NOZZLE IS NOT FUNCTIONAL. COMBUSTION LINER WILL NOT INSERT TO SHIEL D. 1 G 7 2 3U 3 U H3EU E4CE 1996101000108 19961010 00108 CE 1996 10 10 96ZZZX5009 1 19960917 A 2820 52001066 FUEL LINE CESSNA 402 402B 207590P CE FIREWALL AFT CHAFE/LEAK A OEZA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 19 773EA 10152 402B0544 DURING PRE-FLIGHT, PILOT NOTICED FUEL COMING FROM BEHIND ENGINE. MAINTENANCE FOUND FUEL LINE CHAFED THROUGH BY A NUTPLA TE. THIS LINE WAS APPARENTLY ORIGINAL EQUIPMENT AND SHOWED SEVERAL WEAR SPOTS. 1 L 7 2 3O A7CE 1996101000120 19961010 00120 NE 1996 10 10 96ZZZX5021 2 19960904 A 7414 SB9RN4 MAGNETO DHAV DHC3 DHC3 2800202 EA PWA R1340 R134059 52016 NE ENGINE CONDENSER FAILED A ENFA A UNSCHED LANDING E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 491K 3225 810029 434 ENGINE DEVELOPED ROUGHNESS, DETERMINED TO BE MAGNETO FAILURE. PILOT LANDED AND TAXIED ON BEACH WHERE IT WAS DETERMINED THE EXHAUST ROCKER CHAMBER NR 1 CYLINDER HAD CRACKED, PRESUMABLY FROM ENGINE ROUGHNESS. BOTH COMPONENTS WERE REPLACED. 1 H 7 1 3R 3 R A815 5E2 1996101000121 19961010 00121 NE 1996 10 10 96ZZZX5022 2 19960827 A 8530 244757 CYLINDER DHAV DHC3 DHC3 2800202 EA PWA R1340 R134059 52016 NE NR 1 FAILED A ENFA A UNSCHED LANDING R E PARTIAL RPM/PWR LOSS VIBRATION/BUFFET CR CRUISE 1 AL 03 491K 3225 434 ON COMPANY FLIGHT 8-27-96, AIRCRAFT WAS LANDED WHILE EN ROUTE BECAUSE OF LT MAGNETO FAILURE. IT WAS THEN DETERMINED NR 1 CYLINDER EXHAUST ROCKER CHAMBER WAS CRACKED. CYLINDER REPLACED AND AIRCRAFT CONTINUED FLIGHT. 1 H 7 1 3R 3 R A815 5E2 1996101000128 19961010 00128 NM 1996 10 10 CALA9601369 1 19961002 A 2910 AS116080264 HYD LINE BOEING 737 7373T0 1384582 NM B-HYD SYST RUPTURED A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 09 12327 23457 AIRCRAFT LOST B-SYSTEM HYDRAULIC FLUID SHORTLY AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND HYDRAULIC FLEX LINE AT B-SYSTEM ELECTRIC PUMP RUPTURED. THE FLEX LINE WAS REMOVED AND REPL ACED. THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP WAS REMOVED AND REPLACED DUE TO THE LOW PRESSURE LIGHT REMAINING ON. THE H YDRAULIC SYSTEM WAS SERVICED, LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 1996101000129 19961010 00129 NM 1996 10 10 CALA9601370 1 19960827 A 5330 SKIN BOEING 757 757224 1384958 NM FUSELAGE LIGHTNING STRIKE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14115 27557 INSPECTION FOUND DENTS AND LIGHTNING STRIKE IN FUSELAGE SKIN APPROXIMATELY FOUR FEET FORWARD OF WING SCAN LIGHT ON LT SI DE 610 WL LONGERON 16L. THE AREA WAS CLEANED AND THE DENTS WERE FOUND WITHIN LIMITS PER SRM 53-00-01, DETAIL III. THE LIGHTNING STRIKE HOLE WAS REPAIRED PER ECRA 5330-0235 AND SRM 53-00-01, PAGE 220, ITEM 3. A DIP WAS ISSUED TO INSPECT B LIND RIVET REPAIR AT 2500 FLIGHT CYCLE INTERVALS AND TO REPLACE WITH SOLID RIVET WITHIN 12,000 FLIGHT HOURS. A PERMANEN T REPAIR WAS INSTALLED SEP 28, 1996 IAW SRM 53-00-01, FIGURE 203, PAGES 206 TO 208 AND THE DIP WAS CLOSED. 2 L 7 2 4F RT A2NM 1996101000130 19961010 00130 NM 1996 10 10 CALA9601371 1 19960923 A 5330 SKIN BOEING 737 737130 1384435 NM BS 727 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14211 19028 INSPECTION FOUND A 1 INCH CRACK IN FUSELAGE SKIN BETWEEN STRINGER 19L AND 20L AT STA 727. A MOD AND REPAIR WAS ACCOMPLI SHED IAW BOEING DRAWING 65C28086 AND EA 5330-01198, OP 1 AND OP 2. 2 L 7 2 4F A16WE 1996101000131 19961010 00131 NM 1996 10 10 CALA9601372 1 19960927 A 5320 ANGLE BOEING 737 737130 1384435 NM BS 360 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14211 19028 INSPECTION FOUND A 1 INCH CRACK IN ATTACH ANGLE AT STRINGER 22L STA 360. THE CRACKED SECTION WAS REMOVED, REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-2, 51-10-2, AND 51-30-2. 2 L 7 2 4F A16WE 1996101000132 19961010 00132 NM 1996 10 10 CALA9601373 1 19960927 A 5320 ANGLE BOEING 737 737130 1384435 NM BS360 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14211 19028 INSPECTION FOUND A 1.5 INCH CRACK IN ATTACH ANGLE AT STA 360, STRINGER 21R. THE ATTACH ANGLE WAS REMOVED IAW SRM 51-30- 2, REPAIR ANGLES AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, AND 51-30-2. 2 L 7 2 4F A16WE 1996101000133 19961010 00133 NM 1996 10 10 CALA9601374 1 19960927 A 5330 SKIN BOEING 737 737130 1384435 NM BS 765 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14211 19028 INSPECTION FOUND A 4 INCH CRACK IN FUSELAGE SKIN AT FS 765, STRINGER 19R. THE CRACKED AREA OF SKIN WAS REMOVED, REPAIR DOUBLER AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, 51-10-2, AND 51-30-2. 2 L 7 2 4F A16WE 1996101000134 19961010 00134 NM 1996 10 10 CALA9601375 1 19960918 A 5320 ANGLE BOEING 737 737130 1384435 NM E/E DOOR CUTOUT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14211 19028 INSPECTION FOUND EXFOLIATION CORROSION AND SHEARED FASTENERS AT LT AFT CORNER OF E AND E DOOR CUTOUT SUPPORT STRUCTURE. THE T-ANGLE WAS REMOVED AND REPLACED IAW EC 5310-01233. 2 L 7 2 4F A16WE 1996101000135 19961010 00135 NM 1996 10 10 CALA9601376 1 19960928 A 5311 FRAME BOEING 737 737130 1384435 NM BS 380 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14211 19028 INSPECTION FOUND A 2 INCH CRACK IN FRAME AT STA 380, STRINGER 21R. THE CRACK WAS STOP DRILLED IAW SRM 53-10-4. A DOUBL ER, FILLER AND CLIP WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, AND 51-30-2. 2 L 7 2 4F A16WE 1996101000136 19961010 00136 NM 1996 10 10 CALA9601377 1 19960925 A 5320 ANGLE BOEING 737 737130 1384435 NM BS 540 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14211 19028 INSPECTION FOUND A .75 INCH CRACK FROM LAST FASTENER HOLE OF RT UPPER RAM AIR ATTACH ANGLE AT STA 540, STRINGER 14R. TH E CRACKED SECTION OF ANGLE WAS CUT OUT, A NEW SECTION AND SPLICE ANGLE WERE FABRICATED AND INSTALLED IAW SRM 53-50-1, 51 -40-3 AND 51-10-2. 2 L 7 2 4F A16WE 1996101000137 19961010 00137 1996 10 10 9620999857 4 19961002 A 2350 MICROPHONE JACK DOUG DC9 DC951 3022051 WP LT COCKPIT FAILED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 766NC 47739 AFTER TAKEOFF, CATPAIN'S VHF TRANSMITTER BECAME INOPERATIVE. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. FOUND CAPTAIN'S MICROPHONE JACK INTERMITTENT. REPLACED MICROPHONE JACK, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996101000138 19961010 00138 NE 1996 10 10 9621009979 2 19961002 A 7261 515107 OIL PUMP DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9 52048 NE RT ENGINE MALFUNCTIONED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 9343 47439 657259 DURING CLIMB, THE RIGHT ENGINE OIL PRESSURE STARTED FLUCTUATING AND OIL QUANTITY BEGAN DROPPING. CREW THROTTLED BACK RI GHT ENGINE TO IDLE AND RETURNED TO MSP WHERE THEY LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FUEL OIL CO OLER, MAIN OIL PUMP AND CASE FILTER ON THE RIGHT ENGINE. THE OIL TANK WAS SERVICED AND ENGINE LEAK AND OPERATIONAL CHEC K WAS OK. 2 L 7 2 4F 4 F A6WE E2EA 1996101000139 19961010 00139 NE 1996 10 10 9621019983 2 19961003 A 7321 7915PMPASSY FUEL CONTROL DOUG DC9 DC932 3022066 WP PWA JT8 JT8D15 52051 NE LT ENGINE FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 983US 16365 16365 47282 656984 DURING CLIMB, THE LEFT ENGINE EPR AND FUEL FLOW INDICATIONS BEGAN FLUCTUATING. CREW RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE FUEL CONTROL AND TRIMMED ENGINE, LEAK AND OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F A6WE E2EA 1996101000140 19961010 00140 WP 1996 10 10 9612029978 1 19961003 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9342 47391 DURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE AND FORWARD CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BA TTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996101000141 19961010 00141 WP 1996 10 10 9621039956 1 19961003 A 3350 6014113 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST DE DESCENT 1 GL 01 923RW 47183 EMERGENCY PATH LIGHTS AT ROWS 8, 9 AND 10 TURN ON AND OFF AS AIRCRAFT DESCENDS BELOW 10,000 FEET. REPLACED BATTERY PACK POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996101000142 19961010 00142 NE 1996 10 10 9621043217 2 19961001 A 7200 ENGINE AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE NR 2 VIBRATION A A NWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 01 317US 197 731642 DURING CLIMB AFTER TAKEOFF, AIRCRAFT DEVELOPED A VIBRATION. CAPTAIN REPORTED THAT NR 2 ENGINE PYLON WAS SHAKING EXCESSI VELY. AIRCRAFT RETURNED TO DEPARTURE AIRPORT. 2 L 7 2 4F 4 F RT A28NM E29NE 1996101000143 19961010 00143 GL 1996 10 10 9621051223 2 19961003 A 7230 COMPRESSOR DOUG DC10 DC1030 3023501 WP GE CF6 CF650C 30018 GL NR 3 ENGINE STALLED A NWAA A E J UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL R PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 01 223NW 46580 455144 AFTER TAKEOFF AT 1,000 FEET, THE NR 3 ENGINE EXPERIENCED TWO COMPRESSOR STALLS. FLIGHT CREW SHUTDOWN NR 3 ENGINE, DUMPE D FUEL AND PERFORMED AN UNEVENTFUL LANDING AT DEPARTURE AIRPORT. MAINTENANCE REPLACING THE NR 3 ENGINE. 2 L 7 3 4F 4 F A22WE A23EA 1996101000144 19961010 00144 EU 1996 10 10 WWMA9600081 1 19961003 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU AVIONICS MALFUNCTIONED A WWMA O OTHER N FALSE WARNING CR CRUISE 1 WP 15 256AE 340B256 THE RED AVIONICS SMOKE LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE REPLACED THE AVIONICS SMOKE DETECTOR AND RELEASED THE A IRCRAFT FOR SERVICE. 2 L 7 2 4T RT A52EU 1996101000145 19961010 00145 NM 1996 10 10 96FDEA01561 1 19960920 A 5315 6520827 FLOORBEAM BOEING 727 72725 1384006 NM BS 1110 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 511FE 18283 NR0439 AND 013, CORROSION (C53-111-01, -3) IN THE AFT CARGO BAY AT BS 1110 LBL 16 TO 30 WL 199 ON FLOORBEAM AT NUTPLATE HOLES. *S/D* CORROSION FOUND TO BE OUT OF LIMITS. REMOVED CORRODED SECTION AND REPAIRED LOWER FLANGE IAW FEDEX EA 7-5 310-31192. 2 L 7 3 4F A3WE 1996101000146 19961010 00146 NM 1996 10 10 96FDEA01562 1 19960920 A 5315 6580653 FLOORBEAM BOEING 727 72725 1384006 NM BS 1130 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 511FE 18283 NR0435 AND 014, CORROSION (C53-224-01, -3, C53-224-04) STR 9L STA 1130 RBL 25 TO 45 WL 208 UPPER FLANGE. *S/D* FOUND C ORROSION TO BE OUT OF LIMITS. REPAIRED FLOORBEAM UPPER FLANGE BS 1130, RBL 25 TO 45 WL 208 IAW FEDEX EA 7-5310-31186. 2 L 7 3 4F A3WE 1996101000147 19961010 00147 NM 1996 10 10 DL757962205 1 19960930 A 2560 MEGAPHONE MV10 BOEING 757 757232 1384965 NM CABIN DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 671DN 25332 F/A REPORTS, AFT MEGAPHONE BROKEN. REPLACED MEGAPHONE. 2 L 7 2 4F RT A2NM 1996101000148 19961010 00148 NM 1996 10 10 DL757962212 1 19961001 A 3510 OXYGEN HOSE MC1025104 BOEING 757 757232 1384965 NM RT COCKPIT LEAKING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 673DL 307 25978 307 FIRST OFFICER OXYGEN MASK HEADSET HOSE LEAKED AND DID NOT INFLATE. 2 L 7 2 4F RT A2NM 1996101000149 19961010 00149 NM 1996 10 10 DL72S962213 1 19961002 A 3350 08163000602 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 476DA 20753 ESCAPE PATH LIGHTING LENS CRACKED AND LIGHT INOP. REPLACED LENS AND LIGHT, OPS CHECK NORMAL. 2 L 7 3 4F A3WE 1996101000150 19961010 00150 NM 1996 10 10 DLM88962216 1 19961002 A 2910 HYD LINE DOUG MD88 MD88 3023688 NM RT WW LEAKING A DALA A B UNSCHED LANDING EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 906DL 49537 307 AFTER T/O, STRONG FUME/SMELL THROUGHOUT CABIN AND COCKPIT. DECLARED EMERGENCY LANDING AND DURING TAXI COCKPIT'S SMOKE A LARM SOUNDED. FOUND TRANS PUMP SUPPLY LINE LEAKING IN RT W/W, REPLACED LINE. 2 L 7 2 4F RT A6WE 1996101000151 19961010 00151 NM 1996 10 10 DLM88962217 1 19961002 A 2910 PLUG AP7002D08W DOUG MD88 MD88 3023688 NM RT WHEEL WELL LEAKING A DALA O OTHER K FLUID LOSS AP APPROACH 1 SO 27 977DL 53258 307 ON APPROACH, THE RT HYD SYSTEM QTY WENT TO ZERO. ALTERNATE GEAR EXTENSION WAS USED FOR LANDING. A/C WAS TOWED OFF RUNW AY. CONTRACT MTC FOUND THE A-PLUG IPC REF 29-10-00 FIG 01S ITEM 325 HAD BACK OFF. TIGHTENED PLUG AND SAFTIED, SER VICED RESERVIOR AND LEAK CHECKED THE PLUG. NO DAMAGE TO WHEEL WELL DOORS CAUSED BY LANDING. 2 L 7 2 4F RT A6WE 1996101000152 19961010 00152 NM 1996 10 10 DL73S962218 1 19960924 A 5310 STRUCTURE BOEING 737 737232 1384475 NM BS 31 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 311DL 23083 307 FS 31F CORRODED FROM LBL 10 TO RT SIDE OF FUSELAGE. REMOVED CORROSION PER SRM 51-10-6, CORROSION OUT OF LIMITS PER 53-1 0. REMOVED T-CAP AND FAB REPLACEMENT PER SRM 53-21-0, COMPLETED INSTALLATION OF REPAIR PER MM 53-21-0 FIG 803. 2 L 7 2 4F RT A16WE 1996101000153 19961010 00153 NM 1996 10 10 DL73S962219 1 19960924 A 5310 STRUCTURE BOEING 737 737232 1384475 NM BS 312 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 311DL 23083 307 AT MV-2, FOUND FS 312 CORRODED FROM LBL 10 TO RT SIDE OF FUSELAGE. REMOVED CORROSION PER SRM 51-10-6, CORROSION OUT OF LIMITS PER 53-10. REMOVED T-CAP AND FAB REPLACEMENT PER SRM 53-21-0 PG 803. COMPLETED INSTALLATION OF REPAIR PER MM 53 -21-0 PG 803. 2 L 7 2 4F RT A16WE 1996101000154 19961010 00154 NM 1996 10 10 SCNA96269 1 19960929 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 283SC 22559 FOUND OVERHEAD EMERGENCY LIGHT BLINKING BETWEEN R2 AND L2 DOOR. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, CHEC KS NORMAL. 2 L 7 3 4F A3WE 1996101000155 19961010 00155 NM 1996 10 10 SCNA96270 1 19961002 A 3350 10605529 BATTERY PACK BOEING 727 7272A1 138407F NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 287SC 21345 FOUND AFT CABIN EMERGENCY FLOOR TRACK LIGHTING TO BE DIM. REMOVED AND REPLACED THE AFT EMERGENCY TRACK BATTERY PACK. 2 L 7 3 4F A3WE 1996101000156 19961010 00156 WP 1996 10 10 SCNA96271 1 19960928 A 3213 ARG7002 STRUT DOUG DC10 DC1015 3022118 WP RT MLG SCRATCHED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY MAINTENANCE, FOUND SCRATCHES IN THE CHROME ON THE OUTER CYLINDER OF THE RIGHT MAIN LANDING GEAR. REMOVED A ND REPLACED THE RIGHT MAIN LANDING GEAR OUTER CYLINDER IN ACCORDANCE WITH CHAPTER 32 OF THE MAINTENANCE MANUAL. 2 L 7 3 4F A22WE 1996101000157 19961010 00157 WP 1996 10 10 SCNA96272 1 19960928 A 3213 NRG6020 STRUT DOUG DC10 DC1015 3022118 WP LT MLG SCRATCHED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY MAINTENANCE, FOUND SCRATCHES ON THE INNER AND OUTER CYLINDERS OF THE LEFT MAIN LANDING GEAR. ALSO, FOUND DAMAGED UPPER AND LOWER BEARINGS. REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR SHOCK STRUT ASSEMBLY IN ACCORDANCE WI TH CHAPTER 32 OF THE MAINTENANCE MANUAL. 2 L 7 3 4F A22WE 1996101000158 19961010 00158 WP 1996 10 10 SCNA96273 1 19960927 A 5320 ANGLE DOUG DC10 DC1015 3022118 WP BS 1801 BROKEN A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY MAINTENANCE, FOUND BROKEN PANEL SUPPORT ANGLE AT BS 1801 RBL 32. FABRICATED AND INSTALLED NEW SUPPORT ANGL E IN ACCORDANCE WITH SRM 53-00-01 AND SRM 51-31-01. 2 L 7 3 4F A22WE 1996101000159 19961010 00159 WP 1996 10 10 SCNA96274 1 19960927 A 5320 ANGLE DOUG DC10 DC1015 3022118 WP BS 1701 BROKEN A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY MAINTENANCE, FOUND NON STANDARD INSTALLATION OF SUPPORT ANGLE AT BS 1701 RBL 5. FABRICATED AND INSTALLED NEW SUPPORT ANGLE IN ACCORDANCE WITH SRM 53-00-01 AND SRM 51-31-01. 2 L 7 3 4F A22WE 1996101000160 19961010 00160 WP 1996 10 10 SCNA96275 1 19960917 A 5320 FRAME DOUG DC10 DC1015 3022118 WP AFT CARGO DOOR CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY MAINTENANCE, FOUND CORROSION AROUND INSERTS ON THE AFT SIDE OF THE DOOR FRAME IN THE AFT CARGO COMPARTMENT. REMOVED CORROSION, FABRICATED AND INSTALLED A REPAIR IN ACCORDANCE WITH SRM 53-50-00. 2 L 7 3 4F A22WE 1996101000161 19961010 00161 WP 1996 10 10 SCNA96276 1 19960921 A 5315 FLOORBEAM DOUG DC10 DC1015 3022118 WP BS 735 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY MAINTENANCE, FOUND FLOORBEAM CRACKED AT BS 735 IN THE LOWER GALLEY AREA. CUT OUT MATERIAL, FABRICATED AND INSTALLED A REPAIR IN ACCORDANCE WITH SRM 53-00-01 AND 53-13-01. 2 L 7 3 4F A22WE 1996101000162 19961010 00162 WP 1996 10 10 SCNA96277 1 19960919 A 5330 SKIN DOUG DC10 DC1015 3022118 WP BS 1741 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY MAINTENANCE, FOUND FUSELAGE SKIN CORRODED AT BS 1741, LONGERON 44. REMOVED CORROSION, TRIMMED OUT SKIN, FA BRICATED AND INSTALLED A REPAIR IN ACCORDANCE WITH SRM 51-21-01 AND EO 53-5283-1. 2 L 7 3 4F A22WE 1996101000163 19961010 00163 WP 1996 10 10 SCNA96278 1 19960919 A 5330 SKIN DOUG DC10 DC1015 3022118 WP BS 1721 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY MAINTENANCE, FOUND FUSELAGE SKIN CORRODED AT BS 1721, LONGERON 42. REMOVED CORROSION, TRIMMED OUT SKIN, FA BRICATED AND INSTALLED A REPAIR IN ACCORDANCE WITH SRM 51-21-01 AND EO 53-5283-1. 2 L 7 3 4F A22WE 1996101000164 19961010 00164 WP 1996 10 10 SCNA96279 1 19960919 A 5330 SKIN DOUG DC10 DC1015 3022118 WP BS 1761 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY MAINTENANCE, FOUND FUSELAGE SKIN CORRODED AT BS 1761, LONGERON 44. REMOVED CORROSION, TRIMMED OUT SKIN, FA BRICATED AND INSTALLED A REPAIR IN ACCORDANCE WITH SRM 51-21-01 AND EO 53-5283-1. 2 L 7 3 4F A22WE 1996101000165 19961010 00165 WP 1996 10 10 SCNA96280 1 19960920 A 5311 FRAME DOUG DC10 DC1015 3022118 WP BS 1841 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY MAINTENANCE, FOUND NON-STANDARD REPAIR INSIDE AFT CARGO BAY AT BS 1841, L 45R. REMOVED EXISTING REPAIR AND CLEANED UP DAMAGE, FABRICATED AND INSTALLED A FILLER AND DOUBLER IN ACCORDANCE WITH SRM 53-16-01 AND 53-00-01. 2 L 7 3 4F A22WE 1996101000166 19961010 00166 WP 1996 10 10 SCNA96281 1 19960920 A 5311 FRAME DOUG DC10 DC1015 3022118 WP BS 1841 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY MAINTENANCE, FOUND NON-STANDARD REPAIR INSIDE AFT CARGO BAY AT BS 1841, L 50L. REMOVED EXISTING REPAIR AND CLEANED UP DAMAGE, FABRICATED AND INSTALLED A FILLER AND DOUBLER IN ACCORDANCE WITH SRM 51-20-00 AND 53-00-01. 2 L 7 3 4F A22WE 1996101000167 19961010 00167 WP 1996 10 10 SCNA96282 1 19960920 A 5312 BULKHEAD DOUG DC10 DC1015 3022118 WP BS 1841 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY MAINTENANCE, FOUND NON-STANDARD REPAIR INSIDE AFT CARGO BAY AT BS 1841, L 48R. REMOVED EXISTING REPAIR AND CLEANED UP DAMAGE, FABRICATED AND INSTALLED A FILLER AND DOUBLER IN ACCORDANCE WITH SRM 53-00-01. 2 L 7 3 4F A22WE 1996101000168 19961010 00168 NM 1996 10 10 SCNA96283 1 19960815 A 5315 FLOORBEAM BOEING 727 727251 138408H NM BS 110-1130 DAMAGED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 280US 21159 CUT HOLE IN FUESLAGE BETWEEN BETWEEN BS 1110 AND BS 1130 AND BETWEEN S-17L AND S-19L TO INSTALL LOWER FLANGE OF FLOORBEA M. FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH ENGINEERING AUTHORIZATION EA 53-690. 2 L 7 3 4F A3WE 1996101000169 19961010 00169 NM 1996 10 10 SCNA96284 1 19960918 A 3350 GE81 LIGHT BOEING 727 727251 138408H NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 280US 21159 FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LEFT OVERWING EMERGENCY EXIT LIGHT IN ACCORDANCE WI TH MM 33-50-11, OPS CHECKED GOOD. 2 L 7 3 4F A3WE 1996101000170 19961010 00170 NM 1996 10 10 P5CA9600748 1 19961003 A 3340 FAIRING BOEING 747 747122 1384872 NM RUNWAY LIGHT DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 DAMAGED LOWER AFT CORNER OF NOSE RUNWAY TURNOFF FAIRING. APPLIED FIBERGLASS OVERLAY PER BAC SRM 51-40-09. 2 L 7 4 4F A20WE 1996101000171 19961010 00171 NM 1996 10 10 P5CA9600749 1 19961003 A 3610 PRECOOLER BOEING 747 747122 1384872 NM NR 3 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 CRACKED PRECOOLER NR 3 ENGINE NEAR HI-STAGE VALVE CONNECTION. WELD REPAIRED PER BAC 59-75. 2 L 7 4 4F A20WE 1996101000172 19961010 00172 NM 1996 10 10 P5CA9600750 1 19961003 A 5400 SILL BOEING 747 747122 1384872 NM NR 4 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 CRACKED SILL ON NR 4 PYLON LEFT SAILBOAT DOOR. FABRICATED AND INSTALLED SILL PER BOEING SRM 51-30-02 AND 51-10-01. 2 L 7 4 4F A20WE 1996101000173 19961010 00173 NM 1996 10 10 P5CA9600751 1 19961003 A 5711 SPAR BOEING 747 747122 1384872 NM RT WING CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 LEVEL 1 CORROSION ON RIGHT WING FRONT SPAR LOWER CHORD AT NR 19 LEADING EDGE FLAP PANEL WELL. REMOVED LEVEL 1 CORROSION AND TREATED AREA PER BAC SRM 57-30-01. 2 L 7 4 4F A20WE 1996101000174 19961010 00174 NM 1996 10 10 P5CA9600752 1 19961003 A 5720 SUPPORT ROD BOEING 747 747122 1384872 NM LT WING BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 BROKEN ANGLED SUPPORT ROD LEFT WING NR 7 LEADING EDGE FLAP WELL. FABRICATED AND INSTALLED NEW SUPPORT ROD PER BOEING SR M 51-10-01 AND 51-30-02. 2 L 7 4 4F A20WE 1996101000175 19961010 00175 NM 1996 10 10 P5CA9600753 1 19961003 A 5280 SKIN BOEING 747 747122 1384872 NM RT MLG DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 CRACKED INNER SKIN ON RIGHT BODY OUTBOARD DOOR. STOP DRILLED, FABRICATED AND INSTALLED DOUBLER PER BAC SRM 51-40-02. 2 L 7 4 4F A20WE 1996101000176 19961010 00176 NM 1996 10 10 P5CA9600754 1 19961003 A 7110 COWL BOEING 747 747122 1384872 NM NR 2 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 CRACKED NR 2 ENGINE CORE COWL STRUCTURE AT AFT BOTTOM ALIGNMENT PIN WITH PUSHED IN PIN. FABRICATED AND INSTALLED NEW CO WL RIB AND ATTACH CLIPS PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1996101000177 19961010 00177 WP 1996 10 10 CKSA96158 1 19960929 A 2120 AIR DISTR DOUG DC8 DC855 3021927 WP CABIN ODOR A CKSA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 801CK 45816 NASI SYSTEM PLACES NAUSEATING ODOR INTO AIRCRAFT, OILY SMELL AND TASTE. TROUBLESHOT SYSTEM, PERFORMED OPS CHECK OF NASI FLOW CONTROL SYSTEM AND NO DISCREPANCIES NOTED. OPS GOOD IAW NASI OPERATIONS MANUAL 21-7-0 PAGE 1. 2 L 7 4 4F 4A25 1996101000178 19961010 00178 WP 1996 10 10 CKSA96159 1 19961001 A 5320 DOUBLER DOUG DC8 DC862 3021970 WP BS 390 DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 801MG 45986 PERFORM DOUBLER REWORK IAW EA 96-268A STATIC PORT STATION 390 LBL 25 TO LBC 281 DRAWING NR AIA/E/2250 REVISION ORIGINAL DATED 07/17/96. PERFORMED DOUBLER REWORK IAW EA 96-268A DRAWING NR AIA/E/2250 REVISION ORIGINAL DATED 07/17/96 STATIC P ORT STATION 390 LBL 25 TO LBC 281. 2 L 7 4 4F 4A25 1996101000179 19961010 00179 SO 1996 10 10 SRAA961002 1 19961002 A 5320 FITTINGS LKHEED 382 382G 526414U SO BS 780/830 CRACKED A SRAA K NONE O OTHER IN INSP/MAINT 1 GL 23 918SJ 4208 ON PRE-FLIGHT INSPECTION AT HOW, FOUND AIRCRAFT FUSELAGE FITTINGS AT STA 780 AND 830 CRACKED. ADDITIONAL INSPECTION FOU ND TOTAL OF THREE CARGO COMPARTMENT SUPPORT STRUTS ATTACH UPPER FITTINGS CRACKED AT FS 869 RT, FS 803 LT, AND FS 825 LT. REPLACED THREE SUPPORT STRUT UPPER FITTINGS IAW SRM 51-60 AND 51-70. 2 H 7 4 4T A1SO 1996101000205 19961010 00205 NM 1996 10 10 DHL9670801C 1 19960905 A 5320 DOOR FRAME BOEING 727 72725 1384006 NM BS 635 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, GALLEY DOOR CUTOUT AT FS 635 DAMAGED AND CRACKED JUST ABOVE FLOOR LEVEL. INSTALLED FRAME REPAIR PER SRM 53- 10-4. REPAIR SIZE 8 INCHES BY 6 INCHES BY 2 INCHES. 2 L 7 3 4F A3WE 1996101000206 19961010 00206 NM 1996 10 10 DHL9670802C 1 19960904 A 5347 SEAT TRACK BOEING 727 72725 1384006 NM BS 615 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, FWD BAGGAGE COMPT HAS SEAT TRACK CORROSION AT STA 615. REPLACED FWD BAGGAGE SEAT TRACK FROM STA 580 TO 700, PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996101000207 19961010 00207 NM 1996 10 10 DHL9670803C 1 19960906 A 5712 RIB BOEING 727 72725 1384006 NM WS 546.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, RIGHT WING RIB CRACKED AT WS 546.5 STR 7 AND STR 8. STOP DRILLED CRACKS, INSTALLED RIB REPAIR PER S/B 57-0 127, 3.125 INCHES BY 17 INCHES. 2 L 7 3 4F A3WE 1996101000208 19961010 00208 NM 1996 10 10 DHL9670804C 1 19960905 A 5311 FRAME BOEING 727 72725 1384006 NM BS 620 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, CABIN FRAME AT STA 620 CRACKED AND DAMAGED AT PREVIOUS REPAIR RT SIDE FWD OF MID GALLEY DOOR JUST ABOVE FLOO R LEVEL. CUT OUT DAMAGED AREA OF FRAME, INSTALLED REPAIR DOUBLER STA 620 PER SRM 53-10-4, 13 INCHES BY 8 INCHES. 2 L 7 3 4F A3WE 1996101000209 19961010 00209 NM 1996 10 10 DHL9670805C 1 19960904 A 5712 RIB BOEING 727 72725 1384006 NM WS 601.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, WING RIB CRACKED AT LOWER FLANGE AT STA 601.5, STR 7. STOP DRILLED CRACK, INSTALLED DOUBLER REPAIR AT LOWER FLANGE PER SRM 57-10-5, 15 INCHES BY 5 INCHES. 2 L 7 3 4F A3WE 1996101000210 19961010 00210 NM 1996 10 10 DHL9670806C 1 19960902 A 5320 SUPPORT BEAM BOEING 727 72725 1384006 NM NLG CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, LEFT CORNER OF NLG SUPPORT BEAM IS CRACKED OUTSIDE OF REPAIR AND PAST STOP DRILL. ACCOMPLISHED REPAIR PER S /B 53-108 AND DRAWING 65C15312. REPAIR 9 INCHES BY 10 INCHES. 2 L 7 3 4F A3WE 1996101000211 19961010 00211 NM 1996 10 10 DHL9670807C 1 19960901 A 5330 SKIN BOEING 727 72725 1384006 NM BS 228 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, FUSELAGE SKIN DENTED AT STA 228 AT STR 26 RT. CUT OUT DAMAGED AREA, INSTALLED PER SRM 53-30-3. FILLER 3 IN CHES BY 2 INCHES, 10 INCHES BY 10 INCHES AND DOUBLER 10 INCHES BY 10 INCHES . 2 L 7 3 4F A3WE 1996101000212 19961010 00212 NM 1996 10 10 DHL9670808C 1 19960904 A 5712 RIB BOEING 727 72725 1384006 NM WS 686.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, INSPECTION REVEALED CRACKS AT RIB UPPER FLANGE AT STR 13 AND 14 AND LOWER FLANGE AT STR 8 WS 686.5. INSTALL ED REPAIRS PER S/B 57-0127, UPPER REPAIR 15 INCHES BY 3.5 INCHES, LOWER DOUBLER 8 INCHES BY 3.5 INCHES. 2 L 7 3 4F A3WE 1996101000213 19961010 00213 NM 1996 10 10 DHL9670809C 1 19960906 A 5712 6597104104 RIB BOEING 727 72725 1384006 NM WS 656.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, INSPECTION REVEALED WING RIB AT WS 656.5 HAS CRACK AT LOWER STR 6, 8 AND TOP STR 9 AND 13. REMOVED AND REPL ACED RIB PER S/B 57-127. 2 L 7 3 4F A3WE 1996101000214 19961010 00214 NM 1996 10 10 DHL9670810C 1 19960906 A 5712 6597104124 RIB BOEING 727 72725 1384006 NM BS 601.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, WING RIB AT STA 601.5 HAS CRACKS AT LOWER STR 6, 8 AND TOP STRINGER 11. REMOVED AND REPLACED WING RIB AT S TA 601.5 PER S/B 57-127. 2 L 7 3 4F A3WE 1996101000215 19961010 00215 NM 1996 10 10 DHL9670811C 1 19960829 A 5330 SKIN BOEING 727 72725 1384006 NM BS 1130 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, FUSELAGE SKIN DENTED AT BS 1130 BETWEEN S-8 AND S-17 LT. CUT OUT DAMAGED AREA, INSTALLED DOUBLER PER SRM 53 -30-3, 9 INCHES BY 12 INCHES. 2 L 7 3 4F A3WE 1996101000216 19961010 00216 NM 1996 10 10 DHL9670812C 1 19960903 A 5312 651630627 BULKHEAD CHANNEL BOEING 727 72725 1384006 NM BS 227 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, FWD NOSE COMPT STA 227 BULKHEAD VERTICAL CHANNEL HAS CORROSION STARTING FROM BILGE CENTER LINE. REMOVED AND REPLACED VERTICAL CHANNEL PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996101000217 19961010 00217 NM 1996 10 10 DHL9670813C 1 19960907 A 5311 FRAME BOEING 727 72725 1384006 NM BS 227 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, FOUND FWD NOSE COMPT STA 227, BULKHEAD HAS CORROSION AFT OF NOSE DOOR ON BILGE CENTER LINE FRAME. REMOVED C ORROSION, OUT OF LIMITS. FABRICATED REPAIR ANGLE AND INSTALLED PER SRM 51-40-3, 3 INCHES BY 12 INCHES. 2 L 7 3 4F A3WE 1996101000218 19961010 00218 NM 1996 10 10 DHL9670814C 1 19960908 A 5313 BAC149813 STRINGER BOEING 727 72725 1384006 NM AFT AIRSTAIR CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, AFT AIR STAIR LOWER AFT END SKID PAD SUPPORT CASTING HEAVILY CORRODED. REMOVED CASTING, CUT OUT DAMAGED STR INGER, INSTALLED STRINGER REPAIR PER SRM 53-10-3, 10 INCHES LONG. INSTALLED NEW AFT AIRSTAIR SKID PAD SUPPORT CASTING P ER SRM 51-10-1. 2 L 7 3 4F A3WE 1996101000219 19961010 00219 NM 1996 10 10 DHL9670815C 1 19960906 A 5712 RIB BOEING 727 72725 1384006 NM WS 738.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, CRACKS FOUND AT WING STA 738.5 RIB AT LWR STR 6 AND UPPER STR 14. STOPPED DRILLED CRACKS, INSTALLED REPAIR AT STR 14 PER SRM 57-10-5, 10 INCHES LONG. INSTALLED REPAIR AT STR 6 PER SRM 57-10-5, 10 INCHES LONG. 2 L 7 3 4F A3WE 1996101000220 19961010 00220 NM 1996 10 10 DHL9670816C 1 19960909 A 5320 WEB BOEING 727 72725 1384006 NM NLG WW CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, LEFT HAND WALL OF NOSE WHEEL WELL HAS CRACK FROM RIG HOLE TO DOOR BELL CRANK. INSTALLED DOUBLER REPAIR PER SRM 53-10-9, 8 INCHES BY 6 INCHES. 2 L 7 3 4F A3WE 1996101000221 19961010 00221 NM 1996 10 10 DHL9670817C 1 19960907 A 5712 6597104121 RIB BOEING 727 72725 1384006 NM WS 629 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, FOUND WING RIB ON LEFT WING STA 629.0 HAS CRACKS AT STRINGERS 8 AND 10. THREE AT TOP AND TWO AT BOTTOM. RE PLACED RIB PER S/B 57-0127. 2 L 7 3 4F A3WE 1996101000222 19961010 00222 NM 1996 10 10 DHL9670818C 1 19960902 A 2782 ANGLE BOEING 727 72725 1384006 NM NR 7 SLAT ACT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, NR 7 SLAT ACTUATOR, INBD TRUNNION VERT ANGLE AT FWD SPAR, STAINLESS DOUBLER HAS CRACK BEYOND STOP DRILL. FA BRICATED ANGLE 1 INCH BY 35 INCHES PER S/B 57-0130, FABRICATED DOUBLER PER S/B, 8 INCHES BY 3.5 INCHES AND INSTALLED PER SRM 51-30-2 AND S/B 57-130. 2 L 7 3 4F A3WE 1996101000223 19961010 00223 NM 1996 10 10 DHL9670819C 1 19960904 A 5712 6597104122 RIB BOEING 727 72725 1384006 NM WS 629 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, INSPECTION OF RIGHT WING SHOWS CRACKS AT STR 11 AND 15 UPPER AND 8 AND 9 LOWER, STA 629.0. REMOVED AND REPL ACED RIB PER S/B 57-127. 2 L 7 3 4F A3WE 1996101000224 19961010 00224 NM 1996 10 10 DHL9670820C 1 19960906 A 5315 FLOORBEAM BOEING 727 72725 1384006 NM BS 600 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, FWD CARGO COMPT STA 600 CABIN FLOORBEAM HEAVILY CORRODED LBL 12 TO 16. INSTALLED REPAIR PER SRM 53-10-8, 2 ANGLES 40 INCHES, STRAP 2 INCHES BY 36 INCHES AND T-ANGLE 29 INCHES. 2 L 7 3 4F A3WE 1996101000225 19961010 00225 NM 1996 10 10 DHL9670821C 1 19960902 A 5320 WEB BOEING 727 72725 1384006 NM NLG WW CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, NOSE WHEEL WELL HAS EXFOLIATION CORROSION AT BS 298 BL 0 TO RBL 6, HORIZONTAL WEB OF DOG HOUSE. CUT OUT DAM AGED AREA, INSTALLED DOUBLER PER SRM 53-10-9, 11 INCHES BY 15 INCHES. 2 L 7 3 4F A3WE 1996101000226 19961010 00226 NM 1996 10 10 DHL9670822C 1 19960905 A 5320 651833245 FITTING BOEING 727 72725 1384006 NM BS 950 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, BS 950 FITTING ON LEFT SIDE HAS A 11 INCH CRACK AROUND BOSS FOR UPPER SEGMENT AFT BEARING. REMOVED AND REPL ACED FITTING PER S/B 53-196 AND S/B 53-126. 2 L 7 3 4F A3WE 1996101000227 19961010 00227 NM 1996 10 10 DHL9670823C 1 19960904 A 5712 6597104153 RIB BOEING 727 72725 1384006 NM WS 738.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, RIB CRACKED AT WS 738.5, 2 CRACKS IN LOWER FLANGE AT STR 6 AND BETWEEN STR 6 AND 8 AND UPPER RIB AT STR 12. REMOVED AND REPLACED RIB PER 57-127. 2 L 7 3 4F A3WE 1996101000228 19961010 00228 NM 1996 10 10 DHL9670824C 1 19960906 A 5330 SKIN BOEING 727 72725 1384006 NM BS 360 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, MATERIAL LOSS NOTED AT BS 360 BETWEEN STR R 19 AND STR R 23 FWD SIDE OF BS 360. REMOVED DAMAGED SECTION S TA 338 TO 360, STR 19 TO STR 24, 22 INCHES BY 42 INCHES. ACCOMPLISHED SKIN SPLICE IAW AVITAS EO 96 PMSI 129RO-2. 2 L 7 3 4F A3WE 1996101000229 19961010 00229 NM 1996 10 10 DHL9670825C 1 19960831 A 5751 SKIN BOEING 727 72725 1384006 NM LT AILERON DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, EFFECT PERMANANT REPAIR ON LT OUTBOARD AILERON TRAILING EDGE. INSTALLED BONDING REPAIR PER SRM 51-40-6 AND REPLACED SKIN LOWER SURFACE, SIZE 43.5 INCHES BY 7 INCHES. CHECK BALANCE PER SRM 51-80-4. 2 L 7 3 4F A3WE 1996101000230 19961010 00230 NM 1996 10 10 DHL9670826C 1 19960831 A 5712 RIB BOEING 727 72725 1384006 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, LEFT WING RIB UPPER CHORD AT BL 70.5, SHOWED CRACK INDICATIONS IN VERTICAL FLANGE DURING HFEC INSPECTON. TR IMMED AREAS PER BOEING INSTRUCTIONS. HFEC TRIMMED EDGES AND FASTENER HOLES COMMON TO REPAIR AREA. INSTALLED REPAIR PER S/B 57-112 AND BOEING TELEX DHLMIA 96-0022RR. 2 L 7 3 4F A3WE 1996101000231 19961010 00231 NM 1996 10 10 DHL9670827C 1 19960901 A 2782 MOUNT BOEING 727 72725 1384006 NM NR 2 LE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, NR 2 LEADING EDGE FLAP ACTUATOR MOUNT CRACKED ON INBD SIDE TOP AND BOTTOM. REMOVED AND REPLACED ACTUATOR MO UNT PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996101000232 19961010 00232 NM 1996 10 10 DHL9670828C 1 19960909 A 5712 RIB BOEING 727 72725 1384006 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, RIGHT WING RIB UPPER CHORD AT BL 70.5 HAS CRACK WITH PREVIOUS STOP DRILL. HFEC, HFEC FASTENER HOLES COMMON TO REPAIR AREA. INSTALLED REPAIR PER S/B 57-0112. 2 L 7 3 4F A3WE 1996101000233 19961010 00233 NM 1996 10 10 DHL9670829C 1 19960905 A 5330 SKIN BOEING 727 72725 1384006 NM BS 211.9 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, FUSELAGE EXTERIOR SKIN CRACKED AROUND FASTENER AT BS 211.9 RIGHT SIDE APPROX WL 210. CUT OUT DAMAGED AREA, FABRICATED DOUBLER REPAIR PER SRM 53-30-3 18 INCHES BY 15 INCHES. 2 L 7 3 4F A3WE 1996101000234 19961010 00234 NM 1996 10 10 DHL9670830C 1 19960905 A 5311 FRAME BOEING 727 72725 1384006 NM BS 848 DRILLED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, FOUND MISDRILLED HOLES INTO RADIUS ON FRAME I/B FLANGE AT BS 848 RIGHT SIDE 4 INCHES ABOVE FLOOR LINE. INSTA LLED REPAIR KIT 65C36282-2 PER S/B 53-197. 2 L 7 3 4F A3WE 1996101000235 19961010 00235 NM 1996 10 10 DHL9670831C 1 19960905 A 5311 FRAME BOEING 727 72725 1384006 NM BS 760.5 MISDRILLED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, MISDRILLED HOLES INTO RADIUS OF LEFT FRAME I/B FLANGE AT BS 760.5 ABOVE FLOOR LINE. INSTALLED REPAIR PER S/B 53-197 2 L 7 3 4F A3WE 1996101000236 19961010 00236 NM 1996 10 10 DHL9670832C 1 19960906 A 5311 FRAME BOEING 727 72725 1384006 NM BS 760 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, LEFT SIDE FRAME WEB CRACKED AT STA 760 FLOOR LEVEL. HFEC, INSTALLED REPAIR PER S/B 53-0197 . 2 L 7 3 4F A3WE 1996101000237 19961010 00237 NM 1996 10 10 DHL9670833C 1 19960906 A 5280 65216362 FLYING DOOR BOEING 727 72725 1384006 NM RT MLG CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, FOUND RIGHT MLG FLYING DOOR AFT FITTING CRACKED. REMOVED AND REPLACED FLYING DOOR PER M/M 32-12-1. 2 L 7 3 4F A3WE 1996101000238 19961010 00238 NM 1996 10 10 DHL9670834C 1 19960831 A 3221 65881895 TRUNNION BOEING 727 72725 1384006 NM LT NLG CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, INSTALLED PERMANENT REPAIR OF NOSE GEAR LT TRUNNION AFT SIDE. REMOVED AND REPLACED TRUNNION PER S/B 53-119 . 2 L 7 3 4F A3WE 1996101000239 19961010 00239 NM 1996 10 10 DHL9672201C 1 19960911 A 5320 GUSSET BOEING 727 727228 NM BS 825 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, GUSSET CRACKED ON FWD SIDE OF FRAME BS 825 JUST ABOVE CENTER WING TANK, RIGHT SIDE. FABRICATED AND INSTALL ED NEW GUSSET PER SRM 51-10-1 AND 51-30-2, 4.5 INCHES BY 3 INCHES. 2 L 7 3 4F A3WE 1996101000240 19961010 00240 NM 1996 10 10 DHL9672202C 1 19960914 A 5712 RIB BOEING 727 727228 NM WS 629 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, LOWER ANGLE CRACKED ON RT WING RIB AT STA 629 AT STR 6. STOP DRILLED CRACK AND INSTALLED RIB REPAIR PER SRM 57-10-5, 9 INCHES BY 4 INCHES. 2 L 7 3 4F A3WE 1996101000241 19961010 00241 NM 1996 10 10 DHL9672203C 1 19960914 A 5712 RIB BOEING 727 727228 NM WS 601.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, LEFT WING RIB AT STA 601.5 HAS CRACK IN LOWER CHORD AT STR 6. STOP DRILLED CRACK AND INSTALLED RIB REPAIR P ER SRM 57-10-5, 9 INCHES BY 4 INCHES. 2 L 7 3 4F A3WE 1996101000242 19961010 00242 NM 1996 10 10 DHL9672204C 1 19960912 A 5315 FLOORBEAM BOEING 727 727228 NM BS 950 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, FLOORBEAM HAS CORROSION TOP CHORD AT BS 950 LBL 24 TO RBL 24. PERFORMED ANGLE AND STRAP REPAIR PER SRM 51-4 0-4, ANGLE 12 INCHES BY 3 INCHES, STRAP 12 INCHES BY 1.5 INCHES. 2 L 7 3 4F A3WE 1996101000243 19961010 00243 NM 1996 10 10 DHL9672205C 1 19960912 A 5347 BAC1520792 SEAT TRACK BOEING 727 727228 NM BS 870-950 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, FOUND SEAT TRACKS CORRODED LBL 24 FROM BS 870 TO BS 950. REMOVED, REPAIRED AND REPLACED SEAT TRACK PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996101000244 19961010 00244 NM 1996 10 10 DHL9672206C 1 19960913 A 5330 SKIN BOEING 727 727228 NM BS 950 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, FOUND EXFOLIATION CORROSIION AT STR 20L LAP SEAM, BETWEEN BS 950E AND BS 950F. CUT OUT DAMAGED AREA 4 INCHE S BY 2 INCHES 5 INCHES. INSTALLED DOUBLER 11 INCHES BY 7 INCHES AND FILLER 4 INCHES BY 3 INCHES PER SRM 53-30-3. 2 L 7 3 4F A3WE 1996101000245 19961010 00245 NM 1996 10 10 DHL9672207C 1 19960910 A 5320 TIE CLIP BOEING 727 727228 NM BS 970 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, TIE CLIP AT STA 970 TO STR 3L CRACKED. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996101000246 19961010 00246 NM 1996 10 10 DHL9672208C 1 19960910 A 5320 TIE CLIP BOEING 727 727228 NM BS 970-950 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, STR 7R 7 TIE CLIPS, AT STA 970 THROUGH 950A ARE CRACKED. REMOVED AND REPLACED TIE CLIPS PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996101000247 19961010 00247 NE 1996 10 10 CALA9601378 2 19961004 A 7260 GEARBOX BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE LEAKING A CALA A J UNSCHED LANDING DUMP FUEL J K WARNING INDICATION FLUID LOSS TO TAKEOFF 1 SW 09 10791 71924 2786 20645 700615 THE NR 3 ENGINE LOST OIL QUANTITY AFTER TAKEOFF. THE LOSS OF OIL WAS ACCOMPANIED BY LOSS OF OIL PRESSURE AND ILLUMINATI ON OF FORWARD PANEL LIGHT. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO SJU WHERE IT LANDED WITHOUT INCIDENT. MAIN TENANCE FOUND THE NR 3 ENGINE GEARBOX LEAKING. THE NR 3 ENGINE GEARBOX WAS REMOVED AND REPLACED, LEAK AND OPERATIONAL C HECKS WERE GOOD. 2 L 7 3 4F 4 F A3WE E2EA 1996101000248 19961010 00248 NM 1996 10 10 CALA9601379 1 19961004 A 3260 655825029 CIRCUIT CARD BOEING 737 7373T0 1384582 NM NLG FAILED A CALA O OTHER N FALSE WARNING CL CLIMB 1 SW 09 12313 23364 THE RED NOSE GEAR UNSAFE LIGHT WOULD NOT EXTINGUISH AFTER GEAR RETRACTION. THE GEAR WAS CYCLED, BUT THE LIGHT REMAINED ON. A LOOK THROUGH THE VIEWPORT EVIDENCED THAT GEAR AND DOORS WERE RETRACTED. THE FLIGHT WAS CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. THE M983 AND M1215 CIRCUIT CARDS WERE REMOVED AND REPLACED. THE NOSE GEAR WAS SWUNG AND OPER ATION AND INDICATIONS CHECKED GOOD. 2 L 7 2 4F RT A16WE 1996101000249 19961010 00249 NM 1996 10 10 CALA9601380 1 19961004 A 2750 65C275082 TRANSMISSION BOEING 737 7373T0 1384582 NM NR 8 TE FLAP FAILED A A CALA O OTHER J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 SW 09 14335 31730 9236 23573 THE FLAPS WOULD NOT EXTEND USING NORMAL SYSTEMS ON APPROACH. WHEN THE ALTERNATE FLAP SYSTEM WAS USED, THE LEADING EDGE DEVICES EXTENDED, BUT THE FLAPS SHOWED .5 DEGREE AND THEN FROZE. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOU ND THE NR 8 FLAP TRANSMISSION AT FAULT. THE FLAP TRANSMISSION WAS REMOVED AND REPLACED, OPERATIONAL CHECK OF FLAPS WAS GOOD. 2 L 7 2 4F RT A16WE 1996101000250 19961010 00250 NM 1996 10 10 CALA9601381 1 19961004 A 3242 214572 BRAKE BOEING 757 757224 1384958 NM RT MLG LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 09 13113 6460 6460 27555 THE EICAS MESSAGE LEFT HYDRAULIC QUANTITY STATUS PAGE SHOWED .46RF DURING GEAR EXTENSION FOR LANDING. THE RIGHT HYDRAUL IC QUANTITY LOW CAME ON SHOWING .73RF DURING TAXI IN. MAINTENANCE FOUND THE NR 8 BRAKE LEAKING. THE NR 8 BRAKE WAS REM OVED AND REPLACED. THE LEFT AND RIGHT HYDRAULIC SYSTEMS WERE SERVICED TO FULL, LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A2NM 1996101000251 19961010 00251 NM 1996 10 10 CALA9601382 1 19961005 A 2910 65446541001 HYD LINE BOEING 737 737217 1384464 NM NR 2 LE SLAT ACT CRACKED A CALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 09 12230 19884 THE A-HYDRAULIC SYSTEM QUANTITY WAS LOST WHILE ON APPROACH. THE A-SYSTEM HYDRAULIC QUANTITY LOSS CHECKLIST WAS COMPLIED WITH AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 SLAT ACTUATOR HYDRAULIC PRESSURE LINE CRACK ED AT B-BUT. THE LINE WAS REMOVED AND REPLACED. THE A-HYDRAULIC SYSTEM WAS SERVICED TO FULL. IN ADDITION, THE NR 1 EN GINE DRIVEN HYDRAULIC PUMP WAS REMOVED AND REPLACED FOR NO OUTPUT. THE ENGINES WERE RUN AND LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F A16WE 1996101000252 19961010 00252 WP 1996 10 10 9621029978 1 19961003 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9342 47391 DURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE AND FORWARD CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BA TTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996101000253 19961010 00253 WP 1996 10 10 9621069908 1 19961004 A 3231 CYLINDER DOUG DC9 DC931 3022065 WP RT NLG DOOR OUT OF ADJUST A NWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 01 958N 47254 VIBRATION WAS COMING FROM NOSE GEAR AREA AFTER TAKEOFF. RECYCLED GEAR WITH SAME RESULTS. FLIGHT RETURNED TO MEM AND LA NDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE RIGHT NOSE GEAR DOOR LOCK CYLINDER, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996101000254 19961010 00254 NM 1996 10 10 9621075517 1 19961003 A 5610 WINDOW SEAL BOEING 757 757251 1384970 NM LT COCKPIT DISLODGED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 517US 23205 DURING CLIMB AT 10,000 FEET, THE CAPTAIN'S SLIDING WINDOW DEVELOPED A LOUD SQUEAL WHICH PROGRESSIVELY WORSENED UNTIL COM MUNICATION BECAME DIFFICULT AT 28,000 FEET. RETURNED TO MSP WITHOUT FURTHER INCIDENT. FOUND THE SLIDING WINDOW PANE TO FRAME SEAL DISLODGED IN THE WINDOW ASSEMBLY. REPLACED SAME, PRESSURIZATION CHECK OK. 2 L 7 2 4F RT A2NM 1996101000255 19961010 00255 NM 1996 10 10 9621085504 1 19961004 A 4990 GTCP331200ER OIL PRESS VALVE BOEING 757 757251 1384970 NM APU MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 01 504US 24474 9094 23193 DURING CRUISE FLIGHT, APU OIL LOW LIGHT ANNUNCIATED. FLIGHT CREW SHUT DOWN APU AND DIVERTED TO LAS DUE TO NR 2 ENGINE I DG ON MEL. MAINTENANCE REPLACED APU OIL PRESSURE REGULATING VALVE, SERVICED APU WITH OIL, GROUND RAN APU FOR 3.5 HOURS AND NO OIL LOSS NOTED. REPLACED NR 2 ENGINE IDG. 2 L 7 2 4F RT A2NM 1996101000256 19961010 00256 NE 1996 10 10 9621093206 2 19961003 A 7200 ENGINE AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE NR 1 FAILED A A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 306US 13972 13972 60 731580 DURING TAKEOFF ROLL, THE NR 1 ENGINE EXPERIENCED A CONTAINED FAILURE. TAKEOFF WAS ABORTED AT 75 KNOTS. MAINTENANCE FOU ND METAL IN TAILPIPE. REMOVED AND REPLACED THE NR 1 ENGINE. 2 L 7 2 4F 4 F RT A28NM E29NE 1996101000257 19961010 00257 WP 1996 10 10 9621109969 1 19961005 A 3350 LIGHTS DOUG DC9 DC931 3022065 WP AFT TAILCONE FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9333 47246 DURING LINE MAINTENANCE INSPECTION, FOUND AFT TAILCONE EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE CHARGED BATTERIES AND CLEANED LAMP SOCKETS, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996101000258 19961010 00258 WP 1996 10 10 9621119944 1 19961005 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 1309T 47316 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS INOPERATIVE. FOUND WIRE PIN LOOSE AT CANNON PLUG 40 11. SECURED WIRE, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996101000259 19961010 00259 WP 1996 10 10 9621129943 1 19961005 A 3350 60030451 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 1308T 47315 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT AFT OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, O PERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996101000260 19961010 00260 EA 1996 10 10 COMA9660161 1 19961003 A 5210 051940 SEAL CNDAIR CL600 CL6002B19 EA PAX DOOR DIRTY A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 931CA 7037 ON CLIMBOUT, FLIGHT ATTENDANT NOTICED GREEN MARKS NOT LINING UP ON THE DOOR. AIRCRAFT RETURNED TO CVG WHERE MAINT FOUND ALL MARKS ALIGNING. CLEANED PAX DOOR SEAL AS A PRECAUTIONARY MEASURE. 2 L 7 2 4F RT A21EA 1996101000261 19961010 00261 EA 1996 10 10 COMA9660162 1 19961003 A 2913 PV304448 PUMP CNDAIR CL600 CL6002B19 EA NR 2 HYD SYSTEM LEAKING A COMA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 SO 01 912CA 8263 7011 NR 2 HYDRAULIC QUANTITY FLUCTUATING BETWEEN O AND 10 PERCENT ON TAXI OUT. REPLENISHED SYSTEM, FERRIED A/C TO CVG WHERE THE RIGHT ENGINE DRIVEN HYDRAULIC PUMP WAS REPLACED. 2 L 7 2 4F RT A21EA 1996101000262 19961010 00262 EA 1996 10 10 COMA9660163 1 19961003 A 2760 270003 PCU CNDAIR CL600 CL6002B19 EA LT SPOILERON MALFUNCTIONED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 915CA 731 7013 LT SPOILERON HAS A FAULT, WILL NOT RESET. FERRIED A/C TO CVG AND REPLACED THE LT OUTBOARD SPOILERON PCU. 2 L 7 2 4F RT A21EA 1996101000263 19961010 00263 EA 1996 10 10 COMA9660164 1 19961003 A 2913 PUMP CNDAIR CL600 CL6002B19 EA LEFT LEAKING A COMA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 941CA 5314 7050 NR 1 HYD RESERVOIR AT 40 DEGREES. FOUND NR 1 ENGINE DRIVEN PUMP LEAKING. REPLACED HYDRAULIC PUMP. 2 L 7 2 4F RT A21EA 1996101000264 19961010 00264 NM 1996 10 10 UPS96221247 1 19961003 A 5753 6521630188 SKIN BOEING 727 727247 138408F NM RT TE FOREFLAP DISBOND A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 211UP 21700 INSPECTION TYPE-C, RIGHT WING I/B FOREFLAP 10 INCHES FROM I/B END UPPER SURFACE HAS AREA OF DISBOND. REPAIRED DISBONDS, 10 INCHES FROM I/B END AND AT 39 INCHES FROM I/B END IAW SRM 51-40-6. 2 L 7 3 4F A3WE 1996101000265 19961010 00265 NM 1996 10 10 UPS96221267 1 19961005 A 5711 SPAR BOEING 727 72722C 138400F NM WS 290 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-D, CRACK IN REAR SPAR UPPER CHORD AT WS 290 RT. REPAIRED PER BOEING INSTRUCTIONS SRS EO 96-33-01. 2 L 7 3 4F A3WE 1996101000266 19961010 00266 NM 1996 10 10 UPS96221268 1 19961005 A 5210 FRAME BOEING 727 72722C 138400F NM FWD ENTRY DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-D, CRACK IN FWD ENTRY DOOR FWD FRAME. REPAIRED PER BOEING INSTRUCTIONS SRS EO 96-33-05. 2 L 7 3 4F A3WE 1996101000267 19961010 00267 NM 1996 10 10 UPS96221269 1 19961005 A 5753 FITTING BOEING 727 72722C 138400F NM LT TE MID FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-D, FLANGE OF FLAP CARRIAGE FITTING ON LT O/B MID FLAP AT STATION 442 CO RRODED AND CRACKED. REPAIRED PE R BOEING INSTRUCTIONS SRS EO 96-33-03. 2 L 7 3 4F A3WE 1996101000268 19961010 00268 NM 1996 10 10 UPS96221270 1 19961005 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 860 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-D, STRINGER 18A, BS 860 CORRODED. REPAIRED PER SRS EO 96-33-02. 2 L 7 3 4F A3WE 1996101000269 19961010 00269 NM 1996 10 10 UPS96221271 1 19961005 A 5347 SEAT TRACK BOEING 727 72722C 138400F NM BS 950 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-D, SEAT TRACK CRACKED AT BS 950, LBL 63. REPAIRED PER SRM 53-10-1. 2 L 7 3 4F A3WE 1996101000270 19961010 00270 NM 1996 10 10 UPS96221272 1 19961005 A 5347 SEAT TRACK BOEING 727 72722C 138400F NM BS 620 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-D, SEAT TRACK FLANGE AT BS 620, LBL 62.5 CORRODED. REPAIRED PER SRM 53-10-5. 2 L 7 3 4F A3WE 1996101000271 19961010 00271 NM 1996 10 10 UPS96221273 1 19961005 A 5320 WINDOW FRAME BOEING 727 72722C 138400F NM BS 227.8-235.8 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-D, SURFACE CORROSION ON UNDERSIDE OF RT SLIDING WINDOW FRAME AT STA 227 .78 TO 235.8. REPLACED WEB. 2 L 7 3 4F A3WE 1996101000272 19961010 00272 NM 1996 10 10 UPS96221274 1 19961005 A 5320 SILL BOEING 727 72722C 138400F NM BS 310-350 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-D, DOOR SILL TOP HAT SECTION CORRODED AT BS 310 TO 350, RBL 14. REPLACED DOOR SILL EXTRUSION. 2 L 7 3 4F A3WE 1996101000273 19961010 00273 NM 1996 10 10 UPS96221275 1 19961005 A 5320 STIFFENER BOEING 727 72722C 138400F NM BS 243.7 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-D, CORROSION ON STIFFENER ANGLE ON FRAME AT STA 243.7, STRINGER 14R. STIFFENER REPLACED PER SRM 51-30-2 . 2 L 7 3 4F A3WE 1996101000274 19961010 00274 NM 1996 10 10 UPS96221276 1 19961005 A 5311 FRAME BOEING 727 72722C 138400F NM BS 880 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-D, CREASE BEAM CRACKED AT BS 880, STRINGER 15L. REPLACED FRAME CHORD AT BS 880 PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996101000275 19961010 00275 NM 1996 10 10 UPS96221277 1 19961005 A 5315 FLOORBEAM BOEING 727 72722C 138400F NM BS 560 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-D, CORROSION UNDER ANCHOR NUT ON FLOORBEAM AT BS 560, LBL 55. FLOORBEAM REPAIRED SRS EO 96-33-015. 2 L 7 3 4F A3WE 1996101000276 19961010 00276 NM 1996 10 10 UPS96421228 1 19960902 A 5311 FRAME BOEING 747 747121 1384871 NM BS 1360 S37 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE-C, BULK CARGO COMP FOUND CRACKS IN FRAME INNER FLANGE, WEB AND REINFORCEMENT ANGLE AT BS 1960, S37 LT. R EPAIRED FRAME INNER FLANGE, WEB AND REINFORCEMENT ANGLE. REPAIR APPROVED PER EFN 747-53-0790. 2 L 7 4 4F A20WE 1996101000277 19961010 00277 NM 1996 10 10 UPS96521233 1 19961003 A 5522 SKIN BOEING 757 75724APF 1384969 NM RT ELEVATOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 430UP 25461 INSPECTION TYPE-3C, FIBER IS DAMAGED ON THE RT ELEVATOR LOWER TRAILING EDGE 68 INCHES OUTBOARD FROM INBOARD END. REPAIR ED PER SRM 55-20-01, 51-70-04, 51-20-05 AND SRM 51-40-02. 2 L 7 2 4F RT A2NM 1996101000278 19961010 00278 WP 1996 10 10 UPS96821229 1 19960908 A 5320 47731561N FITTING DOUG DC8 DC873F 302199F WP FS 1690 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, LONGERON 24R END FITTING CRACKED AT FS 1690 FWD SIDE. REPLACED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996101000279 19961010 00279 WP 1996 10 10 UPS96821230 1 19960908 A 5320 4641324N FITTING DOUG DC8 DC873F 302199F WP FS 1680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, LONGERON 24 END FITTING CRACKED AT FS 1680 AFT SIDE. REPLACED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996101000280 19961010 00280 WP 1996 10 10 UPS96821231 1 19960918 A 5712 5770123 RIB DOUG DC8 DC873F 302199F WP RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, RT WING LEADING EDGE WING 3 RIBS CRACKED AT STA XFS212, XFS242 AND XFS285. REPAIRED RIBS PER MM 57 -00-00 FIG 801. 2 L 7 4 4F RT 4A25 1996101000281 19961010 00281 WP 1996 10 10 UPS96821232 1 19960903 A 5313 5750198 LONGERON DOUG DC8 DC873F 302199F WP FS 857 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, LONGERON 24R AT FS 857, CRACKED AT BOTTLE BOLT HOLE. REPLACED LONGERON PER DRAWING NR 5750198 DAC. 2 L 7 4 4F RT 4A25 1996101000282 19961010 00282 WP 1996 10 10 UPS96821234 1 19960903 A 5712 5770123 RIB DOUG DC8 DC873F 302199F WP RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, RT WING LEADING EDGE 4 RIBS CRACKED AT STA XFS820, XFS800, XFS695 AND XFS680. REPAIRED RIBS PER MM 57-00-00, FIG 801. 2 L 7 4 4F RT 4A25 1996101000283 19961010 00283 WP 1996 10 10 UPS96821235 1 19960903 A 5755 5655168 SKIN DOUG DC8 DC873F 302199F WP NR 4 SPOILER DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, RT WING NR 4 SPOILER DELAMINATED. REPLACED SPOILER PER MM 27-61-01. 2 L 7 4 4F RT 4A25 1996101000284 19961010 00284 WP 1996 10 10 UPS96821236 1 19960831 A 5755 5655168 SKIN DOUG DC8 DC873F 302199F WP NR 4 SPOILER DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, LT WING NR 4 SPOILER DELAMINATED. REPLACED SPOILER ASSY PER MM 27-61-01. 2 L 7 4 4F RT 4A25 1996101000285 19961010 00285 WP 1996 10 10 UPS96821237 1 19960909 A 7110 D51B11401 DEFELCTOR DOUG DC8 DC873F 302199F WP NR 3 NR 3 ENG CRACK A IPXA O OTHER O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, NR 3 ENGINE NOSE COWL ANTI-ICE D-DUCT INNER WING DEFLECTOR CRACKED AND PIECES MISSING. REPAIRED PE R SRM ADDENDUM/EO. 2 L 7 4 4F RT 4A25 1996101000286 19961010 00286 WP 1996 10 10 UPS96821238 1 19961003 A 3231 51036 LINK ASSY LOCK DOUG DC8 DC873F 302199F WP NLG DOOR FAILED A IPXA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 836UP 45936 INSPECTION TYPE-C, GEAR NOT LATCHED LIGHT ILLUMINATED, CONFIRMED OPEN BY LOUD AIR NOISE. COMPLETED QRH DID NOT FIX PROB LEM. FOUND L-FWD NOSE GEAR DOOR HANGING OPEN DUE TO DEFECTIVE LOCK ON LINK ASSY. REMOVED AND REPLACED LINK PER MM 32-2 2-02. PERFORMED GEAR SWING ALL OPS CHECK NORMAL. (P/N 5-1036) (S/N 312) ON, (P/N 5-1036) (S/N 462) OFF. 2 L 7 4 4F RT 4A25 1996101000287 19961010 00287 WP 1996 10 10 UPS96821239 1 19960903 A 5320 WEB DOUG DC8 DC873F 302199F WP BS 340 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, WEB CRACKED FS 340 RBL 48 ABOVE A BIN DOOR JAMB. REPAIRED WEB PER UPS EO. 2 L 7 4 4F RT 4A25 1996101000288 19961010 00288 WP 1996 10 10 UPS96821240 1 19960910 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 200 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, BELTFRAME FS 200 VERTICAL SUPPORT FRAME WEB AT LONGERON 27R IS CRACKED. REPLACED WEB SECTION PER S RM 53-2-0 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996101000289 19961010 00289 WP 1996 10 10 UPS96821241 1 19960823 A 5330 SKIN DOUG DC8 DC873F 302199F WP NLG CUTOUT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, .5 INCH LONG CRACK AT NOSE GEAR WHEEL WELL CUTOUT. REPAIRED PER UPS EO AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1996101000290 19961010 00290 WP 1996 10 10 UPS96821242 1 19960909 A 5320 5753113502N FITTING DOUG DC8 DC873F 302199F WP BS 920 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, FS 920 LONGERON 24R FITTING IS CRACKED. REPLACED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996101000291 19961010 00291 WP 1996 10 10 UPS96821243 1 19960909 A 5320 36471171N FITTING DOUG DC8 DC873F 302199F WP FS 960 L24L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, FS 960 LONGERON 24L FITTING IS CRACKED. REPLACED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996101000292 19961010 00292 WP 1996 10 10 UPS96821244 1 19960909 A 5320 36410041N FITTING DOUG DC8 DC873F 302199F WP BS 880 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, B/T FITTING CRACKED AT FS 880 LONGERONS 23L TO 24L. REPLACED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996101000293 19961010 00293 WP 1996 10 10 UPS96821245 1 19961004 A 3350 5708458503 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHTING DID NOT TEST. REPLACED EMERGENCY EXIT LIGHTING BATTERY PACK. 2 L 7 4 4F RT 4A25 1996101000294 19961010 00294 EU 1996 10 10 WWMA9600082 1 19961005 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT DEFECTIVE A WWMA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 WP 15 356SB 340B356 CARGO SMOKE LIGHT ON CWP ILLUMINATED MOMENTARILY WHILE ON GROUND. REMOVED AND REPLACED BOTH SMOKE DETECTORS PER SAAB MM 26-10, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1996101000295 19961010 00295 NM 1996 10 10 96FDEA01563 1 19961004 A 5315 BAC1518388 FLOOR BEAM BOEING 727 72725 1384006 NM BS 1110 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 511FE 18283 NR0594 AND 015, CORROSION (C53-224-01, -3) AT BS 1110 RBL 43 WL 207 EMITTING FROM UNDER SIDE OF TOP FLANGE OF FLOOR BEAM AT FASTENER HOLE. *S/D* REPAIRED CORROSION DAMAGE ON FLOOR BEAM AT BS 1110 RBL 43 WL 207 PER FEDEX SRM 53-10-8 FIG 8. 2 L 7 3 4F A3WE 1996101000296 19961010 00296 EU 1996 10 10 96FDEA01564 1 19961005 A 2131 CONTROLLER AIRBUS 310 A310200 3930310 EU NR 1 FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 413FE 345 AT 10,000 FT ON DEPARTURE, CABIN ALTITUDE WARNING APPEARED ON ECAM, NO DOOR OR WINDOWS INDICATED OPEN. CABIN PRESSURE W AS VERIFIED ABOVE 10,000 FT, MANUAL PRESSURIZATION CONTROLLER WOULD NOT CONTROL CABIN ALTITUDE. T/S PER TSM 21-30-00 FO UND NR 1 PRESSURE CONTROLLER BAD. REPLACED THE SAME AND TESTED OK. BOTH CABIN PRESS TESTED SYS 1 AND 2 TESTED OK. 2 L 7 2 4F RT A35EU 1996101000297 19961010 00297 WP 1996 10 10 96FDEA01565 1 19961005 A 3234 CONTROL HANDLE DOUG DC10 DC1030F 3023504 WP LANDING GEAR LACK OF LUBE A FDEA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 307FE 48291 WHEN GEAR SELECTED DOWN BOTH PILOTS AND S/O PANEL IND FOUND RED LIGHTS. RAN RED TAB PROCEDURE, PER CHECKLIST WHEN ALTER NATE GEAR HANDLE RAISED, GOT FOUR GEAR DOWN GREEN LIGHTS BOTH PANELS. LANDED DOV WITHOUT INCIDENT. MX FOUND LANDING GE AR LEVER NOT RETRACTING CORRECTLY CAUSING SWITCH S1-431 ERRATIC OPERATION. MX CLEANED AND LUBED GEAR SELECTOR CONTROL H ANDLE, OPS CHECKED OK. 2 L 7 3 4F RT A22WE 1996101000298 19961010 00298 NE 1996 10 10 ABXA9600632 2 19961002 A 7200 ENGINE DOUG DC8 DC861 3021952 WP PWA JT3D JT3D3B 52039 NE NR 2 FAILED A ABXA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 23 845AX 46157 645339 NR 2 OIL PRESSURE LIGHT ILLUMINATED, OIL PRESSURE FLUCTUATED BELOW 35 PSI TO 20 PSI. SECURED ENGINE AT 1243 Z, RPM NEVE R FELL BELOW 24 PERCENT N-2 UNTIL TOUCHDOWN. HIGHEST WAS 35 PERCNET N-2, APPROXIMATELY 5 PSI OIL PRESSURE. REPLACED NR 2 ENGINE IAW ABX ENGINE CHANGE CARD J-7001. MAINTENANCE PROCEDURES COMPLIED WITH. 2 L 7 4 4F 4 F 4A25 1E8 1996101000299 19961010 00299 WP 1996 10 10 ABXA9600633 1 19961001 A 3350 5708458503 BATTERY PACK DOUG DC8 DC863 302198A WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 821AX 46116 ON SERVICE CHECK, FOUND COCKPIT EMERGENCY LIGHTING DIM. REPLACED EMERGENCY BATTERY PACK IAW DC-8 MM 33-50-1, OPS CHECKE D GOOD. 2 L 7 4 4F 4A25 1996101000300 19961010 00300 WP 1996 10 10 ABXA9600634 1 19961003 A 3260 CONNECTOR PIN DOUG DC9 DC932 3022066 WP RT MLG LOOSE A ABXA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 23 900AX 47380 UPON LOWERING LANDING GEAR, NO RIGHT MAIN GEAR INDICATION NOR RIGHT GEAR UNSAFE LIGHT. RECYCLED, CHANGED BULBS TO NO EF FECT. ALTERNATE MAIN GEAR INDICATION NORMAL. LANDED WITHOUT INCIDENT. VERIFIED PIN 5 ON CANNON PLUG PL-129 NOT SECUR ED. RESEATED PIN, SECURED AND LOCKED, SYSTEM OPS CHECKED GOOD IAW DC9 MM 32-60-00. 2 L 7 2 4F A6WE 1996101000301 19961010 00301 WP 1996 10 10 ABXA9600635 1 19961004 A 7931 K0098C RELIEF VALVE DOUG DC8 DC861F 3021953 WP PWA JT3D JT3D3B 52039 NE NR 3 ENGINE STICKING A ABXA E ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 GL 23 849AX 45891 669610 DURING DESCENT, NR 3 OIL PRESSURE DROPPED TO 25 PSI WITH NR 3 OIL PRESSURE LIGHT ILLUMINATED. ENGINE SECURED, OIL QUANT ITY 9 GALLONS, OIL TEMPERATURE 75 DEGREES CELSIUS AT SHUTDOWN. WIND MILLED APPROXIMATELY 12 MINUTES, OIL PRESSURE DID N OT GO BELOW 24 PSI. RAN NR 3 ENGINE AT IDLE, COULD NOT DUPLICATE. SUSPECTED ENGINE OIL PRESSURE RELIEF VALVE. UPON IN SPECTION OF OIL PRESSURE RELIEF VALVE, FOUND VALVE STICKING IN VALVE HOUSING. REPLACED NR 3 OIL PRESSURE RELIEF VALVE I AW PRATT AND WHITNEY MM 72-0. RAN ENGINE AND ADJUSTED OIL PRESSURE RELIEF VALVE IAW DC-8 MM 79-20-5, OPS CHECKED GOOD. RESERVICED OIL TANK. 2 L 7 4 4F 4 F 4A25 1E8 1996101000302 19961010 00302 WP 1996 10 10 ABXA9600636 1 19961004 A 3260 H146 SWITCH DOUG DC8 DC862 3021970 WP RT MLG DEFECTIVE A ABXA O OTHER P NO WARNING INDICATION DE DESCENT 1 GL 23 808AX 45954 RIGHT MAIN LANDING GEAR GREEN DOWN AND LOCKED LIGHT DID NOT ILLUMINATE AFTER GEAR HANDLE SELECTED DOWN. RECYCLED GEAR, NO HELP. RED LIGHT OUT, NO HORN AT 35 DEGREE FLAPS. GREEN LIGHT ILLUMINATED JUST PRIOR TO LANDING. REPLACED RIGHT MLG DOWN LOCK SWITCH IAW DC-8 MM 32-60-00, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1996101000303 19961010 00303 NM 1996 10 10 DL76L962207 1 19960930 A 2530 COFFEE MAKER BOEING 767 767332 1382001 NM AFT GALLEY SHORTED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 176DN 25061 AT FL 330, 2.5 HRS INTO FLIGHT RIGHT AC BUS AND RIGHT BUS TIE ILLUMINATED, ALONG WITH NUMEROUS ASSOCIATED EICAS MESSAGES . AFTER RESETTING RIGHT GENERATOR, THE RIGHT AC BUS WAS RESTORED BUT THE ISLN LIGHT REMAINED ON. SHORTLY AFTER THAT TH E FLIGHT ATTENDANTS REPORTED SPARKS COMING FROM AFT GALLERY CONTROL PANEL ON RIGHT SIDE. FLIGHT ATTENDANTS REMOVED POWE R FROM GALLEY AND FLIGHT CREW REMOVED POWER FROM UTILITY BUSSES. REPLACED COFFEE MAKER. 2 L 7 2 4F RT A1NM 1996101000304 19961010 00304 NM 1996 10 10 DL757962220 1 19961003 A 7500 BLEED AIR BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 ENGINE SMOKE A DALA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 658DL 31180 24420 716385 AT APPROX 110 KTS ON T/O, SMOKE VISIBLE IN COCKPIT AND CABIN NORMAL. ABORTED, PERFORMED DUCT BURNOUT WITH NR 1 ENG AND BOTH PACTS RUNNING WARM AND NO MORE SMELL OR VISIBLE SMOKE. 2 L 7 2 4F 4 F RT A2NM E17NE 1996101000305 19961010 00305 WP 1996 10 10 DLL10962221 1 19961003 A 2150 ACM LKHEED 1011 10113851 5265010 WP PWA 2037 PW2037 NE FUSELAGE SEIZED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 730DA 193C1199 716385 DURING TAXI OUT, THERE WAS A LOUD BANG FROM UNDER AREA NEAR 2R DOOR. SHORTLY AFTER AFT PART OF CABIN BEGAN TO FILL WITH SMOKE. ALL PACKS AND ENG BLEEDS SHUT OFF AND SMOKE STOPPED. FOUND ACM SEIZED, REPLACED ACM. 2 L 7 3 4F 4 F A23WE E17NE 1996101000306 19961010 00306 NM 1996 10 10 DL72S962223 1 19961004 A 3350 LIGHTS BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 478DA 20755 AFT SECTION OF EMERGENCY FLOOR TRACK LIGHTS INOP. REPLACED SPLICE IN AFT SECTION, OPERATION NOW NORMAL. 2 L 7 3 4F A3WE 1996101000307 19961010 00307 NM 1996 10 10 DL767962229 1 19961005 A 3350 LENS 07912 BOEING 767 767232 1385132 NM CABIN MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 107DL 22219 FROM CDL RED TRACK LIGHT EXIT LENS MISSING FROM RT OVERWING EXIT. REPLACED LENS AND BULB, OPN NORMAL. 2 L 7 2 4F RT A1NM 1996101000308 19961010 00308 NM 1996 10 10 P5CA9600755 1 19960923 A 5753 SKIN BOEING 747 747122 1384872 NM RT TE MIDFLAP CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 FOUND LEVEL ONE SURFACE CORROSION ON UPPER SKIN OF INBOARD MIDFLAP AT JOINT TO TRAILING EDGE FALSE WORK, RWBL 333 TO 352 . CORROSION REMOVED IAW SRM 51-10-01 AND FOUND WITHIN LIMITS IAW SRM 57-50-01. REPROTECTED AFTER INSPECTION CLEARANCE IAW SRM 51-10-02. 2 L 7 4 4F A20WE 1996101000309 19961010 00309 NM 1996 10 10 P5CA9600756 1 19960923 A 5753 SKIN BOEING 747 747122 1384872 NM RT TE MIDFLAP CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 FOUND LEVEL ONE SURFACE CORROSION ON INBOARD MIDFLAP ON CENTER PANEL AT JOINT TO AFT PANEL ON LOWER SURFACE RWBL 225. C ORROSION REMOVED IAW SRM 51-10-01 AND FOUND WITHIN LIMITS IAW SRM 51-40-00. REPORTECTED AFTER INSPECTION CLEARANCE IAW SRM 51-10-02. 2 L 7 4 4F A20WE 1996101000310 19961010 00310 NM 1996 10 10 P5CA9600757 1 19961001 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 516-618 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 FOUND LEVEL ONE CORROSION ON FORWARD CARGO HOLD S47L, BS 516 TO 518. REMOVED CORROSION IAW SRM 51-10-01, FOUND WITHIN L IMITS IAW SRM 51-10-01. REPROTECTED AFTER INSPECTION CLEARANCE IAW SRM 51-10-02. RIVETS REMOVED FOR ACCESS AND REINSTA LLED IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996101000311 19961010 00311 NM 1996 10 10 P5CA9600758 1 19960823 A 5711 SPAR CHORD BOEING 747 747132 1384882 NM CENTER TANK CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 FOUND FRONT SPAR LOWER CHORD CORRODED IN CENTER TANK DRY BAY AT RBL 120. CORROSION REMOVED IAW SRM 51-10-01 AND FOUND W ITHIN LIMITS IAW SRM 57-10-01. REPROTECTED AFTER INSPECTION CLEARANCE IAW SRM 51-10-02. 2 L 7 4 4F A20WE 1996101000312 19961010 00312 NM 1996 10 10 P5CA9600759 1 19960821 A 5711 SPAR CHORD BOEING 747 747132 1384882 NM CENTER TANK CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 FRONT SPAR LOWER CHORD FOUND CORRODED IN CENTER TANK DRY BAY RBL 77. LEVEL ONE CORROSION REMOVED AND FOUND WITHIN LIMIT S IAW SRM 57-10-01. TREATED AND PRIMED IAW SRM 57-20-01. 2 L 7 4 4F A20WE 1996101000313 19961010 00313 NM 1996 10 10 P5CA9600760 1 19960823 A 5730 PANEL BOEING 747 747132 1384882 NM RT WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 BOOST PUMP CUTOUT AT PANEL LOCATION 645CB HAS LEVEL ONE SURFACE CORROSION. CORROSION REMOVED IAW SRM 51-10-07, FOUND WI THIN LIMITS IAW SRM 57-30-03. REPROTECTED AFTER INSPECTION CLEARANCE IAW SRM 51-10-02. 2 L 7 4 4F A20WE 1996101000362 19961010 00362 NE 1996 10 10 96ZZZX5054 2 19960820 A 7314 9234A9 PUMP LEAR 25 25 5170506 CE GE CJ610 CJ6106 30006 NE LT ENGINE FAILED A BSYA C D ABORTED TAKEOFF RETURN TO BLOCK X ENGINE FLAMEOUT TO TAKEOFF 1 GL 07 121EL 666BE3484 010 251382 LEFT ENGINE FLAMED OUT ON TAKEOFF ROLL. INSTALLED OVERHAULED FUEL PUMP AND FUEL CONTROL. OPS CHECKED GOOD. 2 L 7 2 4J 4 J A10CE 1E16 1996101000393 19961010 00393 EU 1996 10 10 96ZZZX5085 1 19960830 A 6320 3203004 MAIN GEARBOX SNIAS 350 AS350BA 8680817 EU XMSN DECK DEFECTIVE A P ECAA K NONE O OTHER IN INSP/MAINT 1 EA 11 350SL 2782 TROUBLESHOOTING VIBRATION PROBLEM DISCOVERED TRANSMISSION INPUT PINION SHAFT WAS LOOSE. REMOVED SHORT SHAFT AND RELATED ACCESSORIES AND FOUND INPUT PINION SHAFT HAD LOSS OF PRE-LOAD TORQUE. INPUT PINION SHAFT NUT PN DH5439-111-42 STILL AP PEARED TIGHT, BUT ROTOR BRAKE DISC HAD AXIAL PLAY OF .055 INCH. REMOVED BEVEL REDUCTION GEARBOX PN 350A32-0300-04 AND REPLACED WITH SERVICABLE UNIT. 1 G 7 1 3U NC H9EU 1996101000394 19961010 00394 GL 1996 10 10 96ZZZX5086 1 19960821 A 6220 LWB22658 BOLT ENSTRM F28 280FX 3300506 GL M/R DAMPER FAILED A S DIBA K NONE O OTHER NR NOT REPORTED 1 SO 15 THE BOLTS THAT FAILED ATTACH INBOARD END OF MAIN ROTOR DAMPER. NEITHER DAMPER CAME LOOSE SINCE THE DESIGN OF THE ROTOR HEAD PREVENTS BOLT FROM COMING OUT ALL THE WAY. REMOVED ALL SAP BOLTS FROM SERVICE AND CHECKED TORQUE ON ALL M/R DAMPER BOLTS. 1 G 7 1 3O H1CE 1996101000406 19961010 00406 EU 1996 10 10 CA960122023 1 19960108 A 5610 14156002409 WINDSCREEN BAG JETSTM JETSTM4112 EU PILOTS CRACKED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA 1972 (CAN)CAPTAIN'S FRONT WINDSCREEN CRACKED DURING CLIMBOUT. AIRCRAFT RETURNED TO RAMP. 1 L 7 2 4T RT A196 1996101000407 19961010 00407 1996 10 10 CA960129015 4 19960110 A 3425 6225224003 COMPUTER AMD FALC20 FALCON20C5 2730107 EU FWD RADIO RACK SMELLS W O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA (CAN)UPON SHUT DOWN, A STRONG SMELL OF BURNT ELECTRICAL WIRE WAS REPORTED NEAR NOSE OF AIRCRAFT IN AND OUTSIDE. #2 FLIGH T GUIDANCE COMPUTER WAS IDENTIFITED AS UNIT CAUSING SMELL. UNIT REMOVED. SYSTEMS CHEC KED AND FOUND SERVICEABLE. CO-PILO T'S FLIGHT DIRECTOR SYSTEM DEFERRED IN ACCORDANCE WITH MEL PAGE 34-5 ITEM 6. 2 L 7 2 4F RT A7EU 1996101000408 19961010 00408 EU 1996 10 10 CA960129016 1 19960110 A 2131 133077 CONTROLLER AMD FALC20 FALCON20C5 2730107 EU CABIN PRESS FAULTY W A UNSCHED LANDING O OTHER CL CLIMB 1 CA (CAN)AFTER TAKEOFF, AIRCRAFT WOULD NOT PRESSURIZE IN EITHER MANUAL OR AUTO MODE. PROBLEM WAS INTERMITTENT. PRESSURE CONT ROLLER REPLACED AND SYSTEM CHECKED SERVICEABLE. 2 L 7 2 4F RT A7EU 1996101000409 19961010 00409 EU 1996 10 10 CA960129020 1 19960120 A 3230 C24589000 UPLOCK BOX AEROSP ATR42 ATR42300 8680920 EU LEFT MLG FROZEN W O OTHER J WARNING INDICATION CL CLIMB 1 CA 11767 11767 N392 (CAN)ON GEAR UP SELECTION, LEFT MAIN GEAR UPLOCK LIGHT STAYED ON GEAR SELECTED DOWN AND LEFT DOWN INSPECTION FOUND LEF T MAIN GEAR UPLOCK BOX WAS FROZEN 2 H 7 2 4T RT A53EU 1996101000410 19961010 00410 SW 1996 10 10 CA960131005 1 19960125 A 5610 2719442004A WINDSHIELD SWRNGN SA227 SA227AC 8780603 SW ARSRCH RIGHT HAND SHATTERED W A D I UNSCHED LANDING RETURN TO BLOCK CABIN DEPRESSURIZATION O OTHER CL CLIMB 1 CA 5963 (CAN)RIGHT HAND WINDSHIELD SHATTERED IN FLIGHT, BUT STAYED INTACT. AD 93-19-06 IS RELEVANT. 2 L 7 2 4T RT A8SW 1996101000411 19961010 00411 CE 1996 10 10 CA960131006 1 19960118 A 2820 MS244845 REFUEL ADAPTER ADI208 CESSNA 208 208 2073702 CE SURFACE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 252 252 93104 (CAN)REFUELING ASSEMBLY DRIPS FUEL CONTINUOUSLY PAST THE SEALING SURFACE OF THE BASE PLATE SUBMITTER STATES THAT IT APP EARS THE 'O' RING IS NOT DURABLE ENOUGH FOR THIS APPLICATION 1 H 7 1 3T NT A37CE 1996101000412 19961010 00412 1996 10 10 CA960131007 4 19960115 A 6122 311849602 GOVERNOR BEECH 1900 1900D 1154162 CE HARTZL HCE4A HCE4A3A NE NR 2 ENGINE FAULTY W C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CA 1617 (CAN)ON TAKEOFF ROLL THE #2 PROPELLER WENT INTO UNCOMMANDED AUTOFEATHER AT 90 KIAS.TAKEOFF WAS ABORTED AND AIRCRAFT RETU RNED TO BLOCKS. GROUND INSPECTION REVEALED A FAULTY PROPELLER GOVERNOR WHICH WAS RE PLACED. CHECKED SERVICEABLE, AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A24CE 5 C P10NE 1996101000413 19961010 00413 CE 1996 10 10 CA960131008 1 19960115 A 6120 50329017 ARM ASSEMBLY BEECH 90 B90 1152912 CE PWA PT6 PT6A20 52043 EA HARTZL HCB3T HCB3TN3 GL #1 ENGINE MISSING PARTS W K NONE L NO TEST TX TAXI/GRND HDL 1 CA PCE21010 BU462 (CAN)AFTER START THE LEFT HAND SECONDARY LOW PITCH ANNUNCIATOR WAS NOT ILLUMINATING AS REQUIRED. MAINTENANCE INVESTIGATI ON REVEALED THE CARBON BRUSH BLOCK OF THE PROPELLER PITCH REVERSING ARM ASSEMBLY WAS MISSING & THE ATTACHING LEVER ARM WAS BENT. THERE WAS ALSO CIRCULAR MARKS ON THE SPINNER BULKHEAD WHERE THE LEVER ARM WAS CONTACTING IT. THERE WERE ALSO S EVERAL BULKHEAD RIVETS DAMAGED. CAUSE OF THE DAMAGE IS BELIEVED TO BE A RESULT OF THE ARM ASSEMBLY CONTACTING THE PROXIT Y SENSOR (P/N 189915). THE AIRCRAFT HAD FLOWN 20 HOURS & HAD MADE 30 LANDINGS SINCE THE #1 PROPELLER WAS REINSTALLED AF TER HEAVY ENGINE MAINTENANCE. 1 L 7 2 3T 3 T 3A20 E4EA 6 C P15EA 1996101000414 19961010 00414 NM 1996 10 10 CA960131011 1 19960121 A 2760 G61111 RELAY BOEING 727 727264 138408M NM PWA JT8 JT8D17 52049 NE BRAKE CONTROL INTERMITTENT W D RETURN TO BLOCK J L WARNING INDICATION NO TEST TX TAXI/GRND HDL 1 CA 687323 (CAN)DURING TAXI FOR TAKEOFF THE SPEED BRAKE CONTROL TEST WOULD NOT SOUND DURING TAKEOFF WARNING TEST WITH SPOILERS SELE CTED & SAFETY RELAY BY-PASS SWITCH SELECTED. SPEED BRAKE CONTROL RELAY AT FAULT. REPL ACED. 2 L 7 3 4F 4 F A3WE E2EA 1996101000421 19961010 00421 EA 1996 10 10 CA960202006 2 19960122 A 7322 3024973 DRIVE DHAV DHC6 DHC6300 EA PWA PT6 PT6A27 52043 EA FUEL CONTRL UNIT STRIPPED W E ENGINE SHUTDOWN O OTHER CR CRUISE 1 CA PCE41189 (CAN)THIS ENGINE HAD A PREVIOUS PROBLEM WHERE THE FUEL CONTROL UNIT SEIZED AND STRIPPED THE FCU DRIVE. THE ENGINE WAS SH IPPED FOR REPAIR, BUT IT APPEARS THE DAMAGED PART (DRIVE) WAS MISSED AND WAS REINSTAL LED ON THE ENGINE. IT WORKED FOR A PPROXIMATELY 60 HOURS BEFORE SECOND FAILURE. THE PART WAS REPLACED AND THE ENGINE RAN SERVICEABLE. 1 H 7 2 3T 4 T A9EA E4EA 1996101000426 19961010 00426 EA 1996 10 10 CA960202011 2 19960115 A 8520 72877R TAPPET BODY PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA CAMSHAFT SURFACE WEAR W K NONE O OTHER IN INSP/MAINT 1 CA 1417 L430261AA (CAN)REGROUND TAPPET BODIES WERE REUSED AT OVERHAUL AND SUFFERED PREMATURE WEAR AND WORE DOWN SEVERAL CAM LOBES. ENGINE PERFORMANCE WAS DETERIORATING, ALTHOUGH NO METAL PARTICLES WERE FOUND IN THE ENGINE. 1 L 7 2 3O 3 O A20SO E14EA 1996101000428 19961010 00428 CE 1996 10 10 CA960202013 1 19960129 A 3246 35601821 AFT STRUT FITTNG C3500 CESSNA 206 U206C 2073332 CE BOLT HOLE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA C3542930 (CAN)INSPECTION OF THE FLOATS REVEALED A CRACK RADIATING FROM THE BOLT HOLE OF THE AFT LEFT HAND FITTING WE FOUND THAT T HE AN7 BOLT WAS SEIZED IN THE FITTING BY CORROSION TO SUCH AN EXTENT THAT IT SHEARED WHILE ATTEMPTING TO REMOVE IT. THE CORROSION BETWEEN THE STEEL BOLT AND THE ALUMINUM FITTING CAUSED CRACKS TO FORM AROUND THE BOLT HOLES. REMOVAL OF THE OTHER FITTINGS REVEALED DAMAGE TO THE RIGHT HAND FITTING ALSO. SUBMITTER STATES THAT AN ANNUAL INSPECTION AND CORROSION PREVENTION PLAN WAS DISCUSSED WITH THE OWNER OF THE AIRCRAFT. 1 H 7 1 3O A4CE 1996101000429 19961010 00429 EA 1996 10 10 CA960202014 2 19960129 A 7322 3035279 P3 LINE DHAV DHC7 DHC7102 2802708 EA PWA PT6 PT6A50 52043 EA FLANGE FITTING CRACKED W E ENGINE SHUTDOWN X ENGINE FLAMEOUT DE DESCENT 1 CA PCE86031 (CAN)#1 ENGINE ROLLED BACK TO MIN FLOW ON INBOUND. POST FLIGHT INVESTIGATION FOUND THE LINE FROM THE COMPRESSOR TO THE P 3 FILTER CRACKED AT THE FLANGE FITTING. THE LINE WAS REPLACED AND THE AIRCRAFT RETURN ED TO SERVICE. 2 H 7 4 4T 4 T A20EA E4EA 1996101000430 19961010 00430 CE 1996 10 10 CA960202015 1 19960126 A 2434 EOFF10300BA TIE BOLT FORD EOFF10300BA CESSNA 210 210R 2073458 CE CONT O520 IO520L 17032 SO CASE HALF BROKEN W H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 CA 241 A54557 270293R (CAN)PILOT REPORTED AN INCREASING WHINING OVER THE HEADSET FOLLOWED BY THE #2 ALTERNATOR LIGHT ILLUMINATING. #2 ALTERNAT OR SHUT DOWN AND THE AIRCRAFT FINISHED FLIGHT. MAINTENANCE FOUND THE LOWER ALTERNATOR TIE BOLT BROKEN AND WAS FOUND IN T HE LOWER COWL AREA. THE ALTERNATOR CASE HALVES SHOWED SIGN FRETTING WEAR. THE UNIT WAS NOT DISASSEMBLED TO ASSESS FURTHE R DAMAGE, ALTHOUGH THE ROTOR TURNED FREELY. SUBMITTER REPORTS THAT THIS IS THE SECOND INSTANCE OF TIE BOLT FAILURE EXPER IENCED. 1 H 7 1 3O 3 O RT 3A21 E5CE 1996101000431 19961010 00431 CE 1996 10 10 CA960202016 1 19960126 A 8010 6041H190 RELAY CONTACTS CUTLERHAM 6041H190 BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA START CONTACTO BRUNED W K NONE O OTHER IN INSP/MAINT 1 CA 5132 PCE81939 (CAN)DURING ROUTINE INSPECTION OF THE START CONTACTOR, A HIGHER THAN NORMAL RESISTANCE WAS MEASURED BETWEEN A1 AND A2 TE RMINALS. THE CONTACTS WERE SUSPECTED BURNED. 1 L 7 2 4T 4 T A24CE E4EA 1996101000432 19961010 00432 CE 1996 10 10 CA960202017 1 19960126 A 3060 3E19643 DEICE TIMER BFGOODRICH BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA HARTZL HCD4N3 HCD4N3A GL PROP FAULTY W K NONE O OTHER DE DESCENT 1 CA 3441 3441 U1399 PCE81939 FY998 (CAN)PILOT REPORTED THAT BOTH PROPELLER DEICERS, LEFT AND RIGHT, DID NOT SEEM TO PREVENT ICE BUILT UP AS THEY SHOULD. DU RING BENCH TEST OF TIMER IT WAS NOTED THAT POWER WAS AVAILABLE AT BOTH OUTPUT PINS SI MULTANEOUSLY, CONTRARY TO THE MAIN TENANCE MANUAL. 1 L 7 2 4T 4 T A24CE E4EA 5 C STC 1996101000434 19961010 00434 WP 1996 10 10 CA960202020 1 19960129 A 2910 AE1007828M0400 HOSE LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE C SYS HYD RUPTURED W J DUMP FUEL K FLUID LOSS CR CRUISE 1 CA 10248 (CAN)'C' SYSTEM LOST DURING FLIGHT. 'C' SYSTEM PUMP PRESSURE HOSE CAME APART AT ELBOW AT THE PRESSURE MODULE. REPLACED. 2 L 7 3 4F 4 F A23WE E12EU 1996101000436 19961010 00436 CE 1996 10 10 CA960202022 1 19960125 A 3230 ADIISVA BLEED VALVE BEECH 100 A100 1152915 CE NOSE GEAR BAY LEAKING W K NONE O OTHER IN INSP/MAINT 1 CA 480 (CAN)WHILE TESTING THE LANDING GEAR EMERGENCY SYSTEM, IT WAS NOTICED THAT THE BLEED VALVE WAS LEAKING AIR AND WOULD NOT CLOSE COMPLETELY. THE VALVE WAS DISMANTLED AND FOUND TO BE FULL OF WATER AND GRIME. T HE VALVE WAS CLEANED AND RETURNED TO SERVICE. SUBMITTER STATES THAT THE LOCATION OF THE VALVE IN THE NOSE WHEEL WELL IS A CONTRIBUTING FACTOR IN THE BUILD UP OF DIRT AND WATER. 1 L 7 2 3T A14CE 1996101000437 19961010 00437 EA 1996 10 10 CA960202023 1 19960121 A 2435 23048004 STARTER LEARSIEGLER DHAV DHC6 DHC6300 EA PWA PT6 PT6A27 52043 EA ENGINE FAILED W O OTHER O OTHER TX TAXI/GRND HDL 1 CA 1024 PCE40719 (CAN)AIRCRAFT ENGINE SHUTDOWN FOR DEPLANE, AND WOULD NOT RESTART. STARTER GENERATOR REPLACED. 1 H 7 2 3T 4 T A9EA E4EA 1996101000440 19961010 00440 NM 1996 10 10 CA960205001 1 19960201 A 3213 102007 DRAG STRUT DHAV DHAV DHC8 DHC8102 2809003 NM PWA MLG CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 19035 DCL2787 (CAN)MAIN LANDING GEAR DRAG STRUT LOWER BORE CAVITY BETWEEN BUSHINGS AT SHOCK STRUT ATTACHMENT SHOWING SIGNS OF HEAVY CO RROSION. 2 H 7 2 4T RT A13NM 1996101000441 19961010 00441 EA 1996 10 10 CA960205002 1 19960201 A 2910 B-NUT DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE #2 HYD. SYSTEM LEAKING W A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 CA 123129 (CAN)AIRCRAFT RETURNED TO AIRPORT BECAUSE OF BAD HYDRAULIC LEAK. B NUT ON LINE TO GEAR DOOR FOUND LOOSE. 2 H 7 2 4T 4 T RT A13NM E20NE 1996101000442 19961010 00442 EA 1996 10 10 CA960205003 2 19960129 A 8540 71664 GEAR ASSY IDLER PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2C 41532 EA FUEL PUMP MISSING TEETH W O OTHER Y E ENGINE STOPPAGE VIBRATION/BUFFET CR CRUISE 1 CA 43620 L720161A (CAN)IN CRUISE THERE WAS A SLIGHT ROUGHNESS FROM #1 ENGINE,FOLLOWED SHORTLY BY ENGINE STOPPAGE & PROP FEATHERING.THE CRE W SECURED THE ENGINE & THE FLIGHT WAS COMPLETED WITH AN UNEVENTFUL SINGLE ENGINE LAND ING.UPON ENGINE DISASSEMBLY,THE FU EL PUMP IDLER GEAR WAS FOUND TO HAVE TEETH MISSING & HAD JAMMED AGAINST THE FUEL PUMP GEARSHAFT DUE TO TOOTH MISALIGNMEN T BREAKING THE FUEL PUMP DRIVE ADAPTER ASSEMBLY (P/N LW-103240).THIS ADAPTER CRACKED THROUGH THE OIL PRESSURE GALLEY & A LLOWED OIL TO DISHCARGE OVERBOARD VIA THE FUEL SEAL DRAIN.THE OIL LOSS APPEARED TO HAVE TAKEN ONLY A FEW MINUTES,BUT RES ULTED IN PROGRESSIVE CONNECTING ROD BEARING FAILURE FROM #6 TOWARDS #2 & ENGINE SEIZURE.THE ENGINE WAS REPLACED. 1 L 7 2 3O 3 O A20SO E14EA 1996101000444 19961010 00444 NM 1996 10 10 CA960205008 1 19960116 A 3244 314353 TIRE DHAV DHC8 DHC8102 2809003 NM #4 MAIN RUPTURED W C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CA (CAN)ON TAKEOFF #4 MAIN WHEEL TIRE RUPTURED. REPORTED TO PILOTS BY PASSENGERS. INSPECTION COULD NOT DETERMINE CAUSE. 2 H 7 2 4T RT A13NM 1996101000445 19961010 00445 NE 1996 10 10 CA960205010 2 19960129 A 7200 ENGINE BELL 205 205A1 1181414 SW LYC T53 T5313B 41549 NE NR 2 FAULTY W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA LE07592 (CAN)N2 FAILURE. #N2 INDICATION. CHIP DETECTOR LIGHT CAME ON. METAL FOUND IN AIRFRAME OIL FILTER. NO METAL IN ENGINE FIL TER. 1 G 7 1 4U 4 U H1SW E17EA 1996101000446 19961010 00446 CE 1996 10 10 96ZZZX5089 1 19960816 A 2820 R221485 HOSE CESSNA 208 208B 2073701 CE FUEL DIST DEFECTIVE A AWHA K NONE O OTHER IN INSP/MAINT 1 WP 17 707FX 760 208B0427 INSPECTION PER CESSNA CAB 96-15. LEFT WING, AFT FUEL HOSE RESTRICTED. ALL OTHER HOSES OK. 1 H 7 1 3T A37CE 1996101000447 19961010 00447 CE 1996 10 10 96ZZZX5090 1 19960816 A 2820 R221485 HOSE CESSNA 208 208B 2073701 CE FUEL DIST DEFECTIVE A AWHA K NONE O OTHER IN INSP/MAINT 1 WP 17 713FX 651 208B0438 INSPECTION PER CESSNA CAB 96-15. LEFT WING, AFT FUEL HOSE RESTRICTED. ALL OTHER HOSES OK. 1 H 7 1 3T A37CE 1996101000448 19961010 00448 CE 1996 10 10 96ZZZX5091 1 19960816 A 2820 R221485 HOSE CESSNA 208 208B 2073701 CE FUEL DIST DEFECTIVE A AWHA K NONE O OTHER IN INSP/MAINT 1 WP 17 722FX 495 208B0454 INSPECTION PER CESSNA CAB 96-15. LEFT WING, AFT FUEL HOSE RESTRICTED. ALL OTHER HOSES OK. 1 H 7 1 3T A37CE 1996101000449 19961010 00449 CE 1996 10 10 96ZZZX5092 1 19960816 A 2820 R221485 HOSE CESSNA 208 208B 2073701 CE FUEL DIST DEFECTIVE A AWHA K NONE O OTHER IN INSP/MAINT 1 WP 17 726FX 494 208B0465 INSPECTION PER CESSNA CAB 96-15. LEFT WING, AFT FUEL HOSE RESTRICTED. ALL OTHER HOSES OK. 1 H 7 1 3T A37CE 1996101000450 19961010 00450 CE 1996 10 10 96ZZZX5093 1 19960816 A 2820 R221485 HOSE CESSNA 208 208B 2073701 CE FUEL DIST DEFECTIVE A AWHA K NONE O OTHER IN INSP/MAINT 1 WP 17 744FX 296 208B0492 INSPECTION PER CESSNA CAB 96-15. LEFT WING, AFT FUEL HOSE RESTRICTED. ALL OTHER HOSES OK. 1 H 7 1 3T A37CE 1996101000451 19961010 00451 CE 1996 10 10 96ZZZX5094 1 19960816 A 2820 R221485 HOSE CESSNA 208 208B 2073701 CE FUEL DIST DEFECTIVE A AWHA K NONE O OTHER IN INSP/MAINT 1 WP 17 748FX 271 208B0503 INSPECTION PER CESSNA CAB 96-15. LEFT WING, AFT FUEL HOSE RESTRICTED. ALL OTHER HOSES OK. 1 H 7 1 3T A37CE 1996101000452 19961010 00452 CE 1996 10 10 96ZZZX5095 1 19960816 A 2820 R221485 HOSE CESSNA 208 208B 2073701 CE FUEL DIST DEFECTIVE A AWHA K NONE O OTHER IN INSP/MAINT 1 WP 17 750FX 197 208B0511 INSPECTION PER CESSNA CAB 96-15. LEFT WING, AFT FUEL HOSE RESTRICTED. ALL OTHER HOSES OK. 1 H 7 1 3T A37CE 1996101000453 19961010 00453 CE 1996 10 10 96ZZZX5096 1 19960816 A 2820 R221485 HOSE CESSNA 208 208B 2073701 CE FUEL DIST DEFECTIVE A AWHA K NONE O OTHER IN INSP/MAINT 1 WP 17 754FX 149 208B0526 INSPECTION PER CESSNA CAB 96-15. LEFT WING, AFT FUEL HOSE RESTRICTED. ALL OTHER HOSES OK. 1 H 7 1 3T A37CE 1996101000454 19961010 00454 CE 1996 10 10 96ZZZX5097 1 19960822 A 2820 R221485 HOSE CESSNA 208 208B 2073701 CE FUEL DIST DEFECTIVE A AWHA K NONE O OTHER IN INSP/MAINT 1 WP 17 758FX 75 208B0539 INSPECTION PER CESSNA CAB 96-15. LEFT WING, AFT FUEL HOSE RESTRICTED. ALL OTHER HOSES OK. 1 H 7 1 3T A37CE 1996101000455 19961010 00455 CE 1996 10 10 96ZZZX5098 1 19960816 A 2820 R221485 HOSE CESSNA 208 208B 2073701 CE FUEL DIST DEFECTIVE A AWHA K NONE O OTHER IN INSP/MAINT 1 WP 17 759FX 54 208B0542 INSPECTION PER CESSNA CAB 96-15. LEFT WING, AFT FUEL HOSE RESTRICTED. ALL OTHER HOSES OK. 1 H 7 1 3T A37CE 1996101000478 19961010 00478 CE 1996 10 10 96ZZZX5121 1 19960912 A 3230 08411065 BELLCRANK CESSNA 310 310Q 2074242 CE RETRACT IDLER LT BROKEN A S GTUA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 19 7935Q 6423 310Q0667 LEFT MLG INBD DOOR CAME OPEN AFTER TAKEOFF, REPORTED BY CONTROL TOWER. LANDING MADE WITHOUT INCIDENT. FND GEAR RETRACT IDLER BELLCRANK BROKEN 2 INCHES FROM END OF ARM THAT RUNS GEAR DOOR EXTEND/RETRACT LINKAGE. BELLCRANK SHOWS EVIDENCE O F HAVING BEEN CRACKED ONE-THIRD OF ITS THICKNESS FOR SOME TIME, MONTHS PERHAPS. THE RT BELLCRANK ON ACFT CRACKED AND LA TER BROKE IN SIMILAR FASHION ABOUT 1 YEAR PRIOR. SUSPECT PRIOR IMPROPER RIGGING AND TOO MUCH GEAR DOOR TENSION WHEN GEA R DOWN. SUGGEST CLOSE INSPECTION AS THIS BELLCRANK IS IN SUCH A LOCATION THAT IT IS DIFFICULT TO INSPECT THOROUGHLY. S UGGEST CLOSE ADHERANCE TO CESSNA RIGGING PROCEDURES. CRACK BEGAN AT TOP. 1 L 7 2 3O 3A10 1996101000481 19961010 00481 WP 1996 10 10 CALA9601383 1 19961005 A 4930 360800010 FCU 3812761 DOUG DC9 DC982 3022082 WP APU INOPERATIVE A CALA O OTHER O OTHER DE DESCENT 1 SW 09 18833 6515 3508 P571 49493 THE APU WOULD NOT START WHILE ON DESCENT. MAINTENANCE FOUND THE APU FUEL CONTROL UNIT AT FAULT. THE APU FCU WAS REMOVE D AND REPLACED. LEAK AND OPERATIONAL CHECKS WERE PERFORMED WITH NO FAULTS NOTED. THE APU OPERATED NORMALLY. 2 L 7 2 4F A6WE 1996101000482 19961010 00482 WP 1996 10 10 CALA9601384 1 19961005 A 4900 38003681 APU DOUG DC9 DC982 3022082 WP AFT FUSELAGE MALFUNCTIONED A CALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 09 72830 31603 3693 49490 WHILE OPERATING THE APU EN ROUTE WITH THE NR 2 GENERATOR PLACARDED INOPERATIVE, THE APU FAILED. THE AIRCRAFT WAS DIVERT ED TO MSY WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE OPERATED THE APU UNDER FULL LOAD WHILE ON THE GROUND AT MSY AND APU OPERATION WAS NORMAL. NO FAULTS WERE FOUND. 2 L 7 2 4F A6WE 1996101000483 19961010 00483 NM 1996 10 10 CALA9601385 1 19961006 A 2782 65446516 ACTUATOR BOEING 737 737130 1384435 NM NR 2 LE SLAT INOPERATIVE A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 14206 12686 3859 19023 THE NR 2 LEADING EDGE SLAT DID NOT RETRACT AFTER TAKEOFF. THE LEADING EDGE TRANSIT LIGHT WAS ON AFTER FLAP RETRACTION A ND A VISUAL CHECK CONFIRMED THE NR 2 SLAT WAS STILL EXTENDED. A RECYCLE WAS PERFORMED, BUT THE SLAT REMAINED EXTENDED. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 LEADING EDGE SLAT ACTUAT OR AT FAULT. THE SLAT ACTUATOR WAS REMOVED AND REPLACED IAW MM 27-81-41, LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F A16WE 1996101000484 19961010 00484 NM 1996 10 10 CALA9601386 1 19961005 A 5720 65C2630079 CLEARANCE DOOR BOEING 737 7373T0 1384582 NM LT TE MIDFLAP OUT OF POSITION A A CALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 09 12318 23369 THE FLAPS WOULD NOT EXTEND BEYOND 8 DEGREES DURING FLAP EXTENSION FOR LANDING. THE FLAPS WOULD NOT MOVE USING ALTERNATE FLAP SYSTEM. THE LEADING EDGE DEVICES WENT TO FULL EXTENSION. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUN D THE LT INBOARD FLAP JAMMED ON MIDFLAP TORQUE SHAFT CLEARANCE DOOR. THE CLEARANCE DOOR WAS REMOVED AND PLACED ON CONFI GURATION DEVIATION LIST(CDL) 57-19. 2 L 7 2 4F RT A16WE 1996101000485 19961010 00485 NM 1996 10 10 CALA9601387 1 19960904 A 5330 SKIN BOEING 727 727224 1384076 NM BS 1000 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 69736 INSPECTION FOUND LT FUSELAGE SKIN DENTED AT STA 1000, BETWEEN STRINGER 17 AND 18. THE DENTED AREA WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. 2 L 7 3 4F A3WE 1996101000486 19961010 00486 NM 1996 10 10 CALA9601388 1 19960904 A 5240 SKIN BOEING 727 727224 1384076 NM RT SERVICE DR BENT A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 69736 INSPECTION FOUND RT SERVICE DOOR SKIN BENT AT BOTH HINGES. THE SKIN AT UPPER HINGE CUTOUT WAS STRAIGHTENED AND NO CRACK S WERE FOUND. THE LOWER HINGE CUTOUT WAS CRACKED AND THE CRACK WAS ROUTED OUT. A FILLER AND DOUBLER REPAIR WAS FABRICA TED AND INSTALLED IAW SRM 52-00-3, FIGURE 3. 2 L 7 3 4F A3WE 1996101000487 19961010 00487 NM 1996 10 10 CALA9601389 1 19960920 A 5330 SKIN BOEING 727 727224 1384076 NM BS 430 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 69736 INSPECTION LT FUSELAGE SKIN BULGED AT STA 430. THE BULGED AREA WAS CUT OUT, A REPAIR PLATE WAS FABRICATED AND INSTALLED IAW SRM 53-30-2. 2 L 7 3 4F A3WE 1996101000488 19961010 00488 NM 1996 10 10 CALA9601390 1 19960904 A 5512 SKIN BOEING 727 727224 1384076 NM RT HORIZ STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 69736 INSPECTION FOUND INBOARD LEADING EDGE OF RT HORIZONTAL STABILIZER DENTED. A HFEC INSPECTION FOUND A .5 INCH CRACK. THE CRACKED AND DENTED AREA WAS CUT OUT, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 55-10-3. 2 L 7 3 4F A3WE 1996101000489 19961010 00489 NM 1996 10 10 CALA9601391 1 19960904 A 5522 SKIN BOEING 727 727224 1384076 NM RT ELEVATOR SEPARATING A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 69736 INSPECTION FOUND RT ELEVATOR SEPARATING JUST OUTBOARD OF TAB TRAILING EDGE. THE AREA WAS SMOOTHED AND A BONDING REPAIR WAS INSTALLED IAW SRM 51-20-3. 2 L 7 3 4F A3WE 1996101000490 19961010 00490 NM 1996 10 10 CALA9601392 1 19960904 A 5522 SKIN BOEING 727 727224 1384076 NM RT ELEVATOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 69736 INSPECTION FOUND CONNECTING CRACKS COVERING AN AREA OF APPROXIMATELY 4 BY 8 IN LOWER INBOARD SKIN OF RT ELEVATOR. THE S KIN PANEL WAS REMOVED, A REPAIR DOUBLER WAS INSTALLED IAW SRM 55-20-3, FIGURE 5 AND THE PANEL WAS REINSTALLED. 2 L 7 3 4F A3WE 1996101000491 19961010 00491 NM 1996 10 10 CALA9601393 1 19960904 A 5330 SKIN BOEING 727 727224 1384076 NM BS 1313 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 69736 INSPECTION FOUND RT FUSELAGE SKIN DENTED JUST ABOVE ANTI- HIJACK VANE AT STA 1313. THE DENTED AREA WAS CUT OUT AND A RE PAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. 2 L 7 3 4F A3WE 1996101000492 19961010 00492 NM 1996 10 10 CALA9601394 1 19960906 A 5280 FLYING DOOR BOEING 727 727224 1384076 NM RT MLG CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 69736 INSPECTION FOUND RT MLG FLYING DOOR CRACKED AT AFT SECTION LOWER CORNER NEXT TO SEAL RETAINER. THE CRACK WAS STOP DRILL ED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-4. 2 L 7 3 4F A3WE 1996101000493 19961010 00493 NM 1996 10 10 CALA9601395 1 19960906 A 5230 STOP PLATE BOEING 727 727224 1384076 NM CARGO DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 69736 INSPECTION FOUND RIVET PULLING THROUGH AND SLIGHT BULGING UNDER STOP PLATE INSIDE C-2 DOOR AT FORWARD PRESSURE RELIEF DO OR. THE STOP PLATE WAS REMOVED AND REPLACED IAW SRM 51-40-1. 2 L 7 3 4F A3WE 1996101000494 19961010 00494 NM 1996 10 10 CALA9601396 1 19960907 A 5230 STOP PLATE BOEING 727 727224 1384076 NM CARGO DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 69736 INSPECTION FOUND RIVETS PULLING THROUGH AND BULGING UNDER STOP PLATE INSIDE C-2 DOOR AT AFT PRESSURE RELIEF DOOR. THE S TOP PLATE WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-10-1 AND 51-10-6. 2 L 7 3 4F A3WE 1996101000495 19961010 00495 NM 1996 10 10 CALA9601397 1 19960908 A 5320 BRACKET BOEING 727 727224 1384076 NM BS 940 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 69736 INSPECTION FOUND A CRACK ON ANGLE BRACKET IN LT MLG WHEEL WELL AT STA 940, STRINGER 18A. THE BRACKET WAS REMOVED AND RE PLACED IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996101000496 19961010 00496 NM 1996 10 10 CALA9601398 1 19960908 A 5320 BRACKET BOEING 727 727224 1384076 NM BS 940 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 69736 INSPECTION FOUND BRACKET CRACKED IN RT MLG WHEEL WELL AT STA 940, STRINGER 18A. THE BRACKET WAS REMOVED AND REPLACED IA W SRM 51-10-2, 51-40-5 AND 51-10-6. 2 L 7 3 4F A3WE 1996101000497 19961010 00497 NM 1996 10 10 CALA9601399 1 19960909 A 5320 SUPPORT BOEING 727 727224 1384076 NM BS 720 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 69736 INSPECTION FOUND FLOORBOARD SUPPORT CORRODED IF FORWARD CARGO COMPARTMENT AT STA 720D, STRINGER 26L. THE CORRODED AREA WAS CUT OUT, A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1996101000498 19961010 00498 NM 1996 10 10 CALA9601400 1 19960909 A 5320 ANGLE BOEING 727 727224 1384076 NM BS 580 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 69736 INSPECTION FOUND A CRACK PROTRUDING PAST STOP DRILL IN ANGLE BELOW FLOOR SUPPORT AT STA 580 ABOVE STRINGER 28L. THE CRA CK WAS STOP DRILLED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3. 2 L 7 3 4F A3WE 1996101000499 19961010 00499 NM 1996 10 10 CALA9601401 1 19960909 A 5320 SUPPORT BOEING 727 727224 1384076 NM BS 580-600 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 69736 INSPECTION FOUND CENTER SUPPORT FOR FLOORBOARD IN FORWARD CARGO COMPARTMENT CRACKED AT STA 580 TO 600. ALSO, THE WEB BE LOW WAS CRACKED. THE CRACKS WERE STOP DRILLED, REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-40-3. 2 L 7 3 4F A3WE 1996101000500 19961010 00500 NM 1996 10 10 CALA9601402 1 19960908 A 5313 STRINGER BOEING 727 727224 1384076 NM BS 480-500 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 69736 INSPECTION FOUND STRINGER 28L CORRODED IN FORWARD CARGO COMPARTMENT BETWEEN BS 480 AND 500. THE CORRODED AREA WAS CUT O UT, A STRINGER AND SPLICE WERE FABRICATED AND INSTALLED IAW 51-20-2. 2 L 7 3 4F A3WE 1996101000501 19961010 00501 SO 1996 10 10 COMA9610294 1 19961004 A 3260 1204327501 RELAY BOX EMB 120 EMB120RT SO E/E COMPT MALFUNCTION A COMA K NONE N FALSE WARNING CL CLIMB 1 SO 01 266CA 14551 120258 LANDING GEAR RETRACTED NORMALLY AND INDICATED UP, BUT THE LANDING GEAR AURAL WARNING SOUNDED CONTINUOUSLY. REPLACED THE LANDING GEAR RELAY BOX. 2 L 7 2 4T RT A31SO 1996101000502 19961010 00502 SO 1996 10 10 COMA9610295 1 19961007 A 6120 7902015 ACTUATOR EMB 120 EMB120RT SO RT PROPELLER LEAKING A COMA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 161CA 16556 8820 120143 RT ENGINE NACELLE, WING AND PROPELLER ARE COVERED WITH OIL. REPLACED THE PROPELLER ACTUATOR ASSY. 2 L 7 2 4T RT A31SO 1996101000503 19961010 00503 SO 1996 10 10 COMA9610296 1 19961007 A 3250 MS250851 SWITCH EMB 120 EMB120RT SO LT CONTROL YOKE FAILED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 263CA 120255 PILOTS PEDAL STEER DISCONNECT SWITCH IS INOP. REPLACED SWITCH. 2 L 7 2 4T RT A31SO 1996101000504 19961010 00504 SO 1996 10 10 COMA9610297 1 19961005 A 2820 2810050101 VALVE EMB 120 EMB120RT SO RT WING DEFECTIVE A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 248CA 12207 9246 120228 AFTER TAKEOFF, THERE WAS A 1,500 LB FUEL IMBALANCE. AIRCRAFT RETURNED TO FIELD. REPLACED DEFECTIVE RIGHT WING FUEL PIL OT VALVE. 2 L 7 2 4T RT A31SO 1996101000505 19961010 00505 NM 1996 10 10 SWAA961027 1 19960930 A 2781 SWITCH BOEING 737 7372H4 138448C NM NR 6 LE SLAT FAILED A SWAA D RETURN TO BLOCK N FALSE WARNING CL CLIMB 1 SW 07 64SW 22062 RETURNED DUE TO NR 6 L/E SLAT TRANSIT LIGHT INDICATION AND REQUIRED 1.5 TO 2.5 OF RT RUDDER TRIM TO FLY LEVEL. REPLACED NR 6 SLAT ROD END SWITCH AND CHECKED RIGGING PER BOEING M/M. 2 L 7 2 4F A16WE 1996101000506 19961010 00506 NM 1996 10 10 SWAA961028 1 19960930 A 3350 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 505SW 24182 AT GATE FOUND AN EMERGENCY EXIT LIGHT INOP. RELAMPED AND RESECURED LIGHT ASSEMBLY PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996101000507 19961010 00507 NM 1996 10 10 SWAA961029 1 19960930 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 636SW 27709 AT GATE FOUND EMERGENCY TRACK LIGHTING INOP AT ROWS 13 AND 21. RELAMPED RED LIGHT AND OPS CHECKED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996101000508 19961010 00508 NM 1996 10 10 SWAA961030 1 19960930 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 621SW 28037 AT GATE FOUND EMERGENCY TRACK LIGHTING INOP AT ROW 23. REINSTALLED WIRING AND ADJUSTED TRACKS. 2 L 7 2 4F RT A16WE 1996101000509 19961010 00509 NM 1996 10 10 SWAA961031 1 19960930 A 5210 SEAL BOEING 737 7372H4 138448C NM L1 DOOR OUT OF POSITION A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 61SW 21970 RETURNED DUE TO FWD ENTRY DOOR SQUEALING VERY LOUD ON CLIMBOUT. REPOSITIONED FWD ENTRY DOOR SEAL AND PRESSURE TESTED PE R BOEING M/M. 2 L 7 2 4F A16WE 1996101000510 19961010 00510 NM 1996 10 10 SWAA961032 1 19960930 A 3350 6104791 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED SERVICE CHECK, FOUND L1 AND R1 DOOR EXTERIOR EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK HOUSING PER BOEING M/M. 2 L 7 2 4F A16WE 1996101000511 19961010 00511 NM 1996 10 10 SWAA961033 1 19960930 A 5311 65C35243 FRAME BOEING 737 7372K6 NM BS 774.3 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED TERMINAL CHECK, FOUND AFT CARGO DOOR FWD FRAME CRACKED AT FLOOR PROXIMITY SENSOR LIGHTENING HOLE. REPA IRED PER SWA ACO 484-53 R3. 2 L 7 2 4F RT A16WE 1996101000512 19961010 00512 NM 1996 10 10 SWAA961034 1 19960930 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 394 5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 394.5, LBL 10 TO 12, WL 208 AND RBL 37 TO 50. REPAIRED PER BO EING SRM. 2 L 7 2 4F RT A16WE 1996101000513 19961010 00513 NM 1996 10 10 SWAA961035 1 19960930 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER FLANGE CORROSION AT BS 986.5 RBL 37 LBL 5 WL 208. REPAIRED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1996101000514 19961010 00514 NM 1996 10 10 SWAA961036 1 19960930 A 5315 FLOORBEAM WEB BOEING 737 7373H4 1384600 NM BS 1019/1030 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED D-CHECK, FOUND WEB CORRODED AT BS 1019 RBL 5 AND AT BS 1030 RBL 10 WL 208. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996101000515 19961010 00515 NM 1996 10 10 SWAA961037 1 19960930 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 1004 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT AND STRAP CORRODED AT BS 1012 TO 1016 AND BS 1004. REPLACED PER BOEING SR M. 2 L 7 2 4F RT A16WE 1996101000516 19961010 00516 NM 1996 10 10 SWAA961038 1 19960930 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 327 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOORWAY OUTER SKIN CRACKED AT BS 327 RBL 65 WL 210. REPAIRED PER BOEING SRM . 2 L 7 2 4F RT A16WE 1996101000517 19961010 00517 NM 1996 10 10 SWAA961039 1 19960930 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 1139-1143 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED D-CHECK, FOUND LOWER STRINGER 5 CHORD CRACKED AT BS 1139 TO 1143. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996101000518 19961010 00518 NM 1996 10 10 SWAA961040 1 19960930 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED D-CHECK, FOUND PRESSURE BULKHEAD BS 178 CRACKED AT RBL 4.7 WL 201 TO 201.5 AT RBL 6.7, WL 212 TO 212.5 , AT LBL 4.7, WL 198 TO 199, LBL 6.7, WL 201.5 TO 202 AND AT LBL 4.7 WL 200 TO 201. REPAIRED PER BOEING SRM AND TRAMCO EWO 96-0468. 2 L 7 2 4F RT A16WE 1996101000519 19961010 00519 NM 1996 10 10 SWAA961041 1 19960930 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACK AT BS 727 WL 190 RBL 60 COMMON TO S18A SHEAR WEB. REPAIRED PER SWA ACO 6580-53. 2 L 7 2 4F RT A16WE 1996101000520 19961010 00520 NM 1996 10 10 SWAA961042 1 19960930 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 225 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 225 LBL 31 WL 212. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996101000521 19961010 00521 NM 1996 10 10 SWAA961043 1 19960930 A 5320 CLIP BOEING 737 7373H4 1384600 NM BS 1138 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 1138. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996101000522 19961010 00522 NM 1996 10 10 UPS96221287 1 19961005 A 3350 1000679 LIGHT BOEING 727 727185C 138406N NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE-N/A, EMERGENCY LIGHTS INOP IN COCKPIT. REPLACED LIGHT ASSY PER 33-50-00, OPS CK NORMAL. 2 L 7 3 4F A3WE 1996101000523 19961010 00523 NM 1996 10 10 UPS96221288 1 19961005 A 5230 FRAME BOEING 727 72722C 138400F NM AFT CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-D, CRACK ON AFT CARGO DOOR MAIN FRAME RADIUS BELOW UPPER FWD DOOR STOP. REPLACED PER BOEING DRAWING 65- 18625. 2 L 7 3 4F A3WE 1996101000524 19961010 00524 NM 1996 10 10 UPS96221289 1 19961005 A 5230 ANGLE BOEING 727 72722C 138400F NM AFT CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-D, THREE WEBS AND AN ATTACH ANGLE WERE FOUND CRACKED ON THE INTERNAL OF THE AFT CARGO DOOR. REPLACED W EBS AND ANGLE. 2 L 7 3 4F A3WE 1996101000525 19961010 00525 NM 1996 10 10 UPS96221290 1 19961005 A 5753 RIB BOEING 727 72722C 138400F NM LT TE MIDFLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-D, LT WING O/B MID FLAP INTERSPAR RIB CRACKED AT STATION 319. REPLACED RIB. 2 L 7 3 4F A3WE 1996101000526 19961010 00526 NM 1996 10 10 UPS96221291 1 19961005 A 5753 RIB BOEING 727 72722C 138400F NM LT TE MIDFLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-D, LT WING O/B MID FLAP INTERSPAR RIB CRACKED AT STA 321. REPLACED RIB. 2 L 7 3 4F A3WE 1996101000527 19961010 00527 NM 1996 10 10 UPS96221292 1 19961005 A 5753 RIB BOEING 727 72722C 138400F NM LT TE MIDFLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-D, LT O/B MID FLAP O/B INTERSPAR RIB CRACKED. REPLACED RIB. 2 L 7 3 4F A3WE 1996101000528 19961010 00528 NM 1996 10 10 UPS96221293 1 19961005 A 5753 RIB BOEING 727 72722C 138400F NM LT TE MIDFLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-D, LT O/B MID FLAP INTERSPAR RIB CRACKED AT STA 388. REPLACED RIB. 2 L 7 3 4F A3WE 1996101000529 19961010 00529 NM 1996 10 10 UPS96221294 1 19961005 A 5744 HINGE FITTING BOEING 727 72722C 138400F NM LT AILERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-D, LT AILERON HINGE FITTING ON WING T/E IS CRACKED. REPLACED FITTING PER DRAWING 65-19276. 2 L 7 3 4F A3WE 1996101000530 19961010 00530 NM 1996 10 10 UPS96221295 1 19961005 A 5311 FRAME BOEING 727 72722C 138400F NM BS 870 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-D, CORROSION ON BS 870 FRAME, FWD LOWER TANG AT SEAL OF STR 18A. REMOVED CORROSION AND REPAIRED. 2 L 7 3 4F A3WE 1996101000531 19961010 00531 NM 1996 10 10 UPS96221296 1 19961005 A 5320 ANGLE BOEING 727 72722C 138400F NM BS 720-740 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-D, CRACK IN INTERCOSTAL AND ATTACH ANGLE BETWEEN FLOORBEAMS 720 AND 740. REPLACED ANGLE AND REPAIRED WE B PER SRM 51-10-1, 53-10-2. 2 L 7 3 4F A3WE 1996101000532 19961010 00532 NM 1996 10 10 UPS96221297 1 19961005 A 5315 FLOORBEAM BOEING 727 72722C 138400F NM BS 560 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-D, CORROSION UNDER ANCHOR NUT ON FLOORBEAM AT BS 560, LBL 35. REPAIRED FLOORBEAM. 2 L 7 3 4F A3WE 1996101000533 19961010 00533 NM 1996 10 10 UPS96421279 1 19961007 A 2612 FIRE LOOP BOEING 747 747123 1384873 NM APU SHORTED A IPXA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 676UP 20101 INSPECTION TYPE-N/A, ON SHORT FINAL APU A FAULT LIGHT CAME ON AND STAYED ON UNTIL SHUTDOWN, CHECKLIST INTERMITTENT FIRE BELL. FOUND APU A-LOOP SHORTED, REPOSITIONED. 2 L 7 4 4F A20WE 1996101000534 19961010 00534 NM 1996 10 10 UPS96521278 1 19961007 A 3350 20131A POWER SUPPLY BOEING 757 75724APF 1384969 NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 411UP 23851 INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED POWER SUPPLY AS PER MM 33-51-07, OPS CK'D GOOD. 2 L 7 2 4F RT A2NM 1996101000535 19961010 00535 EU 1996 10 10 WWMA9600083 1 19961007 A 3240 BRAKE SYST SAAB SF340 340B 7860101 EU LANDING GEAR REQD SERVICE A WWMA O OTHER O OTHER NR NOT REPORTED 1 WP 15 280AE 340B280 PILOT REPORTED, THE AIRCRAFT BRAKES WERE NOT HOLDING. MAINTENANCE BLED THE BRAKES IAW SAAB AMM 32-40, OPERATIONAL CHECK S WERE GOOD. 2 L 7 2 4T RT A52EU 1996101000536 19961010 00536 NM 1996 10 10 96FDEA01566 1 19961007 A 5315 6580653 FLOOR BEAM BOEING 727 72725 1384006 NM BS 1130 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 511FE 18283 NR0438 AND 016, CORROSION (C53-111-01, -3) IN THE AFT CARGO BAY AT BS 1130 LBL 11 TO 13 WL 199 ON FLOORBEAM AT NUTPLATE HOLES. *S/D* CORROSION FOUND TO BE OUT OF LIMITS. REMOVED DAMGE, FABRICATED REPAIR FILLERS AND ANGLES, INSTALLED IAW FEDEX EA 7-5310-31190. 2 L 7 3 4F A3WE 1996101000537 19961010 00537 NM 1996 10 10 96FDEA01438 1 19960906 A 5315 150529222 FLOORBEAM BOEING 727 72725 1384006 NM BS 344 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR 0285 AND 004, CORROSION (C53-224-02) ON 344 FLOORBEAM RBL 18 TO LBL 65 WL 208, OUT OF LIMITS. *S/D* REMOVED CORROSI ON ON BS 344 FLOORBEAM RBL 18 TO LBL 65 WL 208. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOORBEAM UPPER CHORD RBL 70 TO LBL 70 IAW FEDEX STANDARD REPAIR DRAWING SR 27-53-007. 2 L 7 3 4F A3WE 1996101000538 19961010 00538 NE 1996 10 10 ABXA9600637 2 19960930 A 7200 ENGINE DOUG DC9 DC933F 302207A WP PWA JT8 JT8D11 52044 NE LEFT BIRD STRIKE A ABXA A UNSCHED LANDING C F.O.D. CL CLIMB 1 GL 23 935AX 47413 BIRD STRIKE LEFT ENGINE. REMOVED THE DAMAGED AREA TO THE LEFT ENGINE NR 1 BLADE, BORESCOPED THE LEFT ENGINE AND GROUND RAN TO TAKEOFF EPR, OPS CHECKED GOOD. 2 L 7 2 4F 4 F A6WE E2EA 1996101000539 19961010 00539 WP 1996 10 10 ABXA9600638 1 19961007 A 3350 60030431 POWER SUPPLY DOUG DC9 DC941 302207N WP CABIN DEFECTIVE A ABXA K NONE L NO TEST CR CRUISE 1 GL 23 971AX 3546 47497 CREW REPORTED, THE EMERGENCY LIGHTS COME ON WHEN FLYING THROUGH TURBULENCE. REPLACED EMERGENCY LIGHT POWER SUPPLY. 2 L 7 2 4F A6WE 1996101000540 19961010 00540 NM 1996 10 10 SCNA96285 1 19961003 A 3350 9008354 BATTERY PACK BOEING 727 7272J4 1384006 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 285SC 21676 FOUND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED RIGHT OVERWING EMERGENCY EXIT LIGHT BATTERY PACK, OPS CHECKED GOOD. 2 L 7 3 4F RT A3WE 1996101000541 19961010 00541 NM 1996 10 10 P5CA9600761 1 19961008 A 2510 SEAT MECHANISM BOEING 747 747122 1384872 NM COCKPIT WORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 F/E SEAT TRACK HAS WORN HOLES, HORIZONTAL LATCH WILL NOT LATCH SECURELY. REPLACED SEAT ASSY PER MM 25-11-02. 2 L 7 4 4F A20WE 1996101000542 19961010 00542 NM 1996 10 10 P5CA9600762 1 19961007 A 5414 SKIN BOEING 747 747122 1384872 NM NR 2 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 NR 2 PYLON LOWER FWD PYLON ACCESS PANEL 463CL CUTOUT HAS .5 INCH CRACK AT THE AFT UPPER END. STOP DRILLED CRACK AND INS TALLED DOUBLER IAW SRM 54-30-05. 2 L 7 4 4F A20WE 1996101000543 19961010 00543 WP 1996 10 10 ARWA9610046 1 19961008 A 2420 515008000 GENERATOR DOUG DC8 DC863F 302198F WP NR 2 MISWIRED A ARWA D RETURN TO BLOCK B H J SMOKE/FUMES/ODORS/SPARKS ELECT. POWER LOSS-50 PC WARNING INDICATION TX TAXI/GRND HDL 1 SO 19 441J 45988 ON TAXI OUT NR 2 GENERATOR FIELD RELAY TRIPPED. STRONG BURNING SMELL IN COCKPIT BEHIND ELECTRICAL CONTROL PANEL BULKHEA D. DISCONNECTED NR 2 GENERATOR CSD AND RETURNED TO BLOCK. NO FIRE NOTED. TROUBLESHOOTING REVEALED A WIRING PROBLEM AT NR 2 GENERATOR, CAUSING THE GENERATOR CONTROL UNIT IN THE COCKPIT TO OVERHEAT AND FAIL. WIRING AT THE GENERATOR WAS RE PAIRED, GCU CHANGED AND SYSTEM OPERATED NORMAL. THE GCU CAUSED THE SMOKE. 2 L 7 4 4F 4A25 1996101000544 19961010 00544 CE 1996 10 10 96ZZZM1396 1 19960808 A 7603 POWER LEVER BEECH 1900 1900C 1154161 CE COCKPIT OUT OF ADJUST A GUUA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 19 199GA UB13 FLT 408 - TPA-MIA - GEAR WARNING HORN WILL NOT SILENCE WITH BUTTON WHEN POWER IS REDUCED BELOW 84-89 PERCENT N1 (GEAR UP ). ADJUSTED POWER LEVER SWITCHES IAW MM 32-60-00. (M) 2 L 7 2 4T RT A24CE 1996101000545 19961010 00545 CE 1996 10 10 96ZZZM1397 1 19960908 A 7120 12991003279 TRUSS BEECH 1900 1900D 1154162 CE RT ENG CRACKED A A MASA K NONE O OTHER IN INSP/MAINT 1 SW 01 65YV 7521 UE65 DURING SCHEDULED DETAIL INSPECTION, FOUND SEVERAL OF THE EIGHT ISOLATOR PADS FAILED ON RIGHT ENGINE. SUBSEQUENT INVESTI GATION REVEALED TRUSS CRACKED AT LINSEED RIVET JUST AFT OF TOP INBOARD AREA A AND WELD JOINT CRACK AT TOP INBOARD AREA A (TYPICAL). REMOVED AND REPLACED TRUSS WITH SAME TYPE. (M) 2 L 7 2 4T RT A24CE 1996101000546 19961010 00546 EA 1996 10 10 96ZZZM1398 1 19960906 A 3232 75313134001 BRACKET DHAV DHC7 DHC7102 2802708 EA NLG DOOR BROKEN A CICA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 17 25AG 25 FLT 4911 - FLL-PID - RETURNED TO FLL, PILOT REPORTS NOSE GEAR ONLY RETRACTS HALFWAY SELECTING GEAR UP (MAIN RETRACTED OK ). INSPECTION REVEALED NOSE GEAR DOOR ACTUATOR ATTACH BRACKET TORN OFF AND NOSE GEAR DOORS JAMMED UP. FREED THE DOORS AND INSPECTED AREA FOR FURTHER DAMAGES. SKIN TORN AT STATION 217 BULKHEAD. REPAIRED TORN 217 BULKHEAD SKIN IAW AVITAS DWG NR 96 PARA .051D-1 'A' AND REPLACED DOOR ACTUATOR ATTACH BRACKET (P/N 75313134-001). 2 H 7 4 4T A20EA 1996101000547 19961010 00547 EA 1996 10 10 96ZZZM1399 2 19960911 A 7261 MS9388009 O-RING DHAV DHC7 DHC7102 2802708 EA PWA PT6 PT6A50 52043 EA NR 3 ENGINE NICKED A CICA E ENGINE SHUTDOWN J K WARNING INDICATION FLUID LOSS AP APPROACH 1 SO 17 703MG 103 86499 FLT 4905 - MIA-PID - PILOT SHUTDOWN NR 3 ENGINE ON APPROACH TO PID DUE TO LOW OIL PRESSUE (BELOW RED LINE, WARNING LIGHT CAME ON). TROUBLESHOOTING INDICATED O-RING IN OIL FILLER NECK TO BE UNSERVICEABLE. REPLACED O-RING AND OPERATIONAL CH ECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 4 4T 4 T A20EA E4EA 1996101000548 19961010 00548 NE 1996 10 10 96ZZZM1400 1 19960917 A 7160 AIR SCOOP CVAC 240 24013 2422626 WP PWA R2800 R2800* 52026 NE NR 1 ENG FOD A A TFAA C D ABORTED TAKEOFF RETURN TO BLOCK C J F.O.D. WARNING INDICATION TO TAKEOFF 1 SO 15 91237 140 P27657 ON TAKEOFF ROLL, LEFT ENGINE ONLY DEVELOPED 46 INCH MAP AND 2600 RPM. THE TAKEOF WAS ABORTED AND RETURNED TO RAMP. REM OVED FOD FROM UPPER AIR INTAKE SCOOP. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4R 4 R A793 5E8 1996101000549 19961010 00549 NE 1996 10 10 96ZZZM1401 2 19960917 A 7322 39145217 CARBURETOR CVAC 240 240* 2422601 WP PWA R2800 R2800* 52026 NE NR 2 ENGINE DEFECTIVE A TFAA A E UNSCHED LANDING ENGINE SHUTDOWN X ENGINE FLAMEOUT CL CLIMB 1 SO 15 22913 316 P30853 ON CLIMB-OUT, HAD COMPLETE POWER LOSS ON NR 2 ENGINE. ENGINE WAS FEATHERED AND AIRCRAFT RETURNED TO AIRPORT. CARBURETO R WAS FOUND TO BE DEFECTIVE AND REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4R 4 R A793 5E8 1996101000550 19961010 00550 WP 1996 10 10 96ZZZM1402 1 19960918 A 2611 302842 SMOKE DETECTOR DOUG DC8 DC851 3021920 WP CARGO COMPT DEFECTIVE A FXLA O OTHER J WARNING INDICATION CR CRUISE 1 SO 19 508DC 45935 DURING CRUISE CARGO SMOKE WARNING LIGHT CAME ON. EXECUTED SMOKE/FIRE CHECK LIST AND VISUAL INSPECTION REVEALED NO EVIDE NCE OF SMOKE. ON DESCENT WARNING LIGHT WENT OUT. INSPECTION REVEALED NR 3 SMOKE DETECTOR DEFECTIVE. REPLACED SMOKE DE TECTOR. SYSTEM CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 4 4F 4A25 1996101000551 19961010 00551 NM 1996 10 10 96ZZZM1403 1 19960923 A 3020 29S5D5240212 DE-ICE BOOT DORNER DO32 DO328100 2996000 NM LT ENG DEBONDING A EQGA K NONE O OTHER IN INSP/MAINT 1 SW 19 350AD 2046 M212710 3050 DURING ROUTINE INSPECTION OF THE LEFT ENGINE INTAKE, THE FORWARD LIP DE-ICE BOOT WAS FOUND TO BE DEBONDING. REPLACED TH E LEFT ENGINE INTAKE AND RETURNED AIRCRAFT TO AIRWORTHY CONDITION. (M) 2 H 7 2 4T RT A45NM 1996101000553 19961010 00553 SO 1996 10 10 ASOA96038 1 19960911 A 2910 12045381007 HYD LINE EMB 120 EMB120RT SO LT MLG CHAFED A ASOA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 11 221AS 120020 EN ROUTE BQK-ATL, CAPTAIN DISCOVERED A SLOW LEAK IN THE GREEN HYDRAULIC SYSTEM. CREW DECLARED AND EMERGENCY AND PREPARE D TO LAND IN ATL WITH LOSS OF THE SYSTEM, HOWEVER, WAS ABLE TO MOVE HYDRAULIC FLUID FROM RIGHT TO LEFT AND EXTEND GEARS AND FLAPS FOR NORMAL APPROACH. LANDING WAS MADE SAFELY AND WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED THE LEFT MAI N LANDING GEAR HYDRAULIC PRESSURE LINE. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. (M) 2 L 7 2 4T RT A31SO 1996101000555 19961010 00555 NE 1996 10 10 EISA96145 2 19960820 A 7200 ENGINE BOEING 727 727223 1384074 NM PWA JT8 JT8D7B 52053 NE NR 1 CASE CRACK A EISA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SW 07 6839 54285 20192 649517 NR 1 ENGINE WOULD NOT MAKE TAKEOFF POWER. BOROSCOPED ENGINE FOUND INTERMEDIATE CASE AT 8TH STAGE BLEED BOSS CRACKED. R EMOVED AND REPLACED ENGINE. (M) 2 L 7 3 4F 4 F A3WE E2EA 1996101000556 19961010 00556 NE 1996 10 10 EISA96147 2 19960907 A 7200 ENGINE BOEING 727 72731 1384010 NM PWA JT8 JT8D9 52048 NE NR 1 FAILED A EISA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 240NE 18906 P665247B NR 1 ENGINE ICING LIGHT BLINKED ON AND OFF 2-3 TIMES. NR 1 ENGINE BEGAN TO FLUCTUATE AND FAILED SHORTLY THEREAFTER. IN FLIGHT, RESTART WAS SUCCESSFULL. NO RECURRING PROBLEM. (M) 2 L 7 3 4F 4 F A3WE E2EA 1996101000557 19961010 00557 NM 1996 10 10 GAIA9624 1 19960828 A 3350 1000679 LIGHT BOEING 727 727251 138408H NM L1 DOOR INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 278US 21157 UPON ARRIVAL OF FLT 726 - AT BRO, CREW NOTED ON LOG PAGE 575-03 DISCREPANCY. EMERGENCY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY. (M) 2 L 7 3 4F A3WE 1996101000558 19961010 00558 CE 1996 10 10 GLBA96178 1 19960809 A 3251 993880043 ACTUATOR BEECH 1900 1900C 1154161 CE NLG STEERING BINDING A GLBA O OTHER F FLT CONT AFFECTED LD LANDING 1 CE 01 101UE 6509 93033 UC101 ORD - ON TOUCHDOWN THE RUDDER PEDALS JAMMED. AIRCRAFT PULLED HARD RIGHT AND FELT A SNAP BEFORE NORMAL STEERING WAS AVAI LABLE. MAINTENANCE REMOVED AND REPLACED NOSE STEERING ACTUATOR. (M) 2 L 7 2 4T RT A24CE 1996101000559 19961010 00559 CE 1996 10 10 GLBA96179 1 19960812 A 3230 CIRCUIT BREAKER BEECH 1900 1900C 1154161 CE LANDING GEAR TRIPPED A GLBA O OTHER J WARNING INDICATION AP APPROACH 1 CE 01 98GL UC98 SPW - GEAR WILL NOT COME DOWN. MAINTENANCE RESET 60 AMPS CIRCUIT BREAKER IN LEFT NACELLE AND COULD NOT DUPLICATE THE PR OBLEM. (M) 2 L 7 2 4T RT A24CE 1996101000560 19961010 00560 WP 1996 10 10 GTIA96NK001 1 19960101 A 5210 PAX DOOR DOUG DC9 DC932 3022066 WP CABIN WOULD NOT CLOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 941ML 47131 MAIN CABIN DOOR WOULD NOT CLOSE. CLOSED FORWARD AIR STAIR DOOR IAW DC-9MM 52-11-0. (M) 2 L 7 2 4F A6WE 1996101000561 19961010 00561 WP 1996 10 10 GTIA96NK002 1 19960101 A 3230 RETRACT MECH DOUG DC9 DC932 3022066 WP NLG MALFUNCTIONED A GTIA O OTHER J WARNING INDICATION AP APPROACH 1 GL 23 942ML 47478 NOSE GEAR WOULD NOT EXTEND FOR LANDING. RECYCLED, LOWERED NOSE GEAR WITH MANUAL EXTENSION NORMAL, OPERATION FROM THE EX T HANDLE WAS SECURED AND DOOR LIGHT WENT OUT. PERFORMED GEAR SWING ON NOSE IAW 32-30. NO DEFECTS NOTED. UNABLE TO DUP LICATE. (M) 2 L 7 2 4F A6WE 1996101000562 19961010 00562 WP 1996 10 10 GTIA96NK003 1 19960103 A 3230 39147385001 BUNGEE CYLINDER DOUG DC9 DC932 3022066 WP NLG FAILED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 942ML 47478 ON GEAR EXTENSION, NOSE GEAR WOULD NOT EXTEND, F-COM PROCEDURE FOLLOWED. REPLACED NOSE LANDING GEAR BUNGEE CYLINDER IAW DC-9MM 32-32-7. ACCOMPLISHED THREE GEAR SWINGS, GEAR OPERATED OK. NO LEAKS. (M) 2 L 7 2 4F A6WE 1996101000563 19961010 00563 WP 1996 10 10 GTIA96NK004 1 19960101 A 2150 DUCT DOUG DC9 DC931 3022065 WP RT PACK FAILED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 934ML 47526 CABIN DEPRESSURIZED, COULD NOT CONTROL IN MANUAL, CABIN OXYGEN MASKS DEPLOYED. FOD BLOWN DUCT BY RIGHT WATER SEPARATOR. REINSTALLED DUCT AND REPLACED PASSENGER OXYGEN MASKS. OPS CHECK OF OXYGEN MASKS CHECKED GOOD. (M) 2 L 7 2 4F A6WE 1996101000564 19961010 00564 WP 1996 10 10 GTIA96NK005 1 19960205 A 7711 LG80A2 EPR TRANSMITTER DOUG DC9 DC931 3022065 WP NR 2 ENGINE MALFUNCTIONED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 RIGHT EPR GAUGE WOULD NOT POWER WHEN SPOOLING THE ENGINES UPON TAKING THE RUNWAY FOR TAKEOFF. REMOVED AND REPLACED RIGH T EPR TRANSMITTER. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1996101000600 19961010 00600 WP 1996 10 10 GTIA96NK042 1 19960112 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 627 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 DURING C-CHECK, FOUND STATION 627 LONGERON 14RH HAS CORROSION FROM SKIN TO SPLICE AREA. REMOVED CORROSION AND TREATED M ETAL IAW SRM 51-10-3. (M) 2 L 7 2 4F A6WE 1996101000601 19961010 00601 WP 1996 10 10 GTIA96NK043 1 19960112 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 639 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 DURING C-CHECK, FOUND STATION 639, LONGERON 14R HAS SURFACE CORROSION FROM CLIP TO INTERCOSTAL AREA. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. (M) 2 L 7 2 4F A6WE 1996101000602 19961010 00602 WP 1996 10 10 GTIA96NK044 1 19960112 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 639 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 DURING C-CHECK, FOUND STATION 639, 14R LONGERON, WINDOW LOWER FRAME 'L' SHAPE ANGLE HAS SURFACE CORROSION. REMOVED CORR OSION AND TREATED METAL IAW SRM 51-10-3. (M) 2 L 7 2 4F A6WE 1996101000603 19961010 00603 WP 1996 10 10 GTIA96NK045 1 19960112 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 617 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 DURING C-CHECK, FOUND STATION 617 LONGERON 14 LEFT HAS SURFACE CORROSION FROM SKIN TO SPLICE AREA. REMOVED CORROSION AN D TREATED METAL IAW SRM 51-10-3. (M) 2 L 7 2 4F A6WE 1996101000604 19961010 00604 WP 1996 10 10 GTIA96NK046 1 19960112 A 5522 SKIN DOUG DC9 DC932 3022066 WP RT ELEVATOR CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 DURING C-CHECK, FOUND RIGHT ELEVATOR ABOVE OUTBOARD TRIM TAB ON ELEVATOR TRAILING EDGE SKIN BOTTOM CORRODED AND SEPARATE D. TRIMMED AWAY EXCESS LAMINATED SHIM STOCK, REMOVED CORROSION AND TREATED IAW SRM 51-10-03. (M) 2 L 7 2 4F A6WE 1996101000605 19961010 00605 WP 1996 10 10 GTIA96NK047 1 19960115 A 5230 DOOR DOUG DC9 DC932 3022066 WP CARGO COMPT CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 DURING C-CHECK, FOUND FOWARD CARGO COMPARTMENT DOOR STRUCTURE HAS SURFACE CORROSION AROUND SEVERAL RIV-NUTS. REMOVED CO RROSION AND TREATED METAL IAW SRM 51-10-3. (M) 2 L 7 2 4F A6WE 1996101000606 19961010 00606 WP 1996 10 10 GTIA96NK048 1 19960112 A 5313 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 DURING C-CHECK, FOUND CORROSION AT THE FOLLOWING STATIONS; STA 889 AND LONGERON 24LT TO 30LT, STATION 945 LONGERON 26LT TO 30LT, STATION 1030 LONGERON 26LT TO 27LT, STA 1129 LONGERON 29RT TO 30RT, STATION 1098 AND 113 FLOOR SUPPORT. REMOVE D CORROSION AND TREATED METAL IAW SRM 51-10-3. MATERIAL FOUND TO BE IN LIMITS. (M) 2 L 7 2 4F A6WE 1996101000607 19961010 00607 WP 1996 10 10 GTIA96NK049 1 19960206 A 7711 JG298H1 EPR INDICATOR DOUG DC9 DC931 3022065 WP NR 2 ENGINE INOPERATIVE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 NR 2 EPR INOP. CLEARED MOISTURE FROM PT2 AND PT7 LINES AND FOUND NR 2 EPR GAUGE INOP. REMOVED AND REPLACED EPR GAUGE. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1996101000675 19961010 00675 WP 1996 10 10 GTIA96NK143 1 19960112 A 5321 FLOOR DOUG DC9 DC932 3022066 WP GALLEY CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 DURING C-CHECK, FOUND CORROSION THROUGHOUT THE GALLEY BOTTOM PANEL AND THE MAIN CABIN FLOOR. REMOVED CORROSION IAW SRM 51-10-3. FABRICATED DOUBLER AND INSTALLED, TREATED IAW SRM 51-01 AND SRM 51-10-3. (M) 2 L 7 2 4F A6WE 1996101000676 19961010 00676 WP 1996 10 10 GTIA96NK144 1 19960112 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 160 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 DURING C-CHECK, FOUND SURFACE CORROSION ON CREW COMPARTMENT FLOOR PANEL AT STATION 160 LBL 12-RBL 12. REPAIRED FLOOR DO UBLER IAW SRM 53-05, FIG 2. REMOVED CORROSION AND TREATED METAL IAW SRM 53-10-3, AREA WITHIN LIMITS. (M) 2 L 7 2 4F A6WE 1996101000677 19961010 00677 WP 1996 10 10 GTIA96NK145 1 19960112 A 5320 CHANNEL DOUG DC9 DC932 3022066 WP BS 160-196 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 DURING C-CHECK, FOUND FLOOR SUPPORT 'U' CHANNEL MAIN CABIN FLOOR AT STATION 160-196 LBL 46 HAS CORROSION. REPAIRED 'U' CHANNEL IAW SRM 51-01 FIG 2, TREATED METAL IAW SRM 53-01-3. (M) 2 L 7 2 4F A6WE 1996101000678 19961010 00678 WP 1996 10 10 GTIA96NK146 1 19960112 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 200-237 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 DURING C-CHECK, FOUND CORROSION AT STA 200-237, LBL 46 - RBL 56, ON SEAT TRACKS AND FLOOR SUPPORT STRUCTURE. REMOVED CO RROSION AND TREATED METAL IAW SRM 53-01-3, AREAS WITHIN LIMITS. (M) 2 L 7 2 4F A6WE 1996101000679 19961010 00679 WP 1996 10 10 GTIA96NK147 1 19960112 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 120-218 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 DURING C-CHECK, FOUND CABIN FLOOR FROM STATION 120-218 LBL 5 TO RBL 5 CORROSION. REMOVED CORROSION AND TREATED METAL IA W SRM 51-10-3. (M) 2 L 7 2 4F A6WE 1996101000680 19961010 00680 WP 1996 10 10 GTIA96NK148 1 19960113 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 200-237 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 DURING C-CHECK, FOUND SURFACE CORROSION BETWEEN STATION 200-237, SEAT TRACK AND FLOOR SUPPORT STRUCTURE. REMOVED CORROS ION AND TREATED METAL IAW SRM 53-01-3, AREA FOUND TO BE WITHIN LIMITS IAW SRM 53-05 PG 8P. (M) 2 L 7 2 4F A6WE 1996101000681 19961010 00681 WP 1996 10 10 GTIA96NK149 1 19960113 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 160-200 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12536 47113 DURING C-CHECK, FOUND MAIN CABIN FLOOR HAS SURFACE CORROSION BETWEEN STATION 160 AND 200 LBL 12 - LBL 46. FABRICATED AN D REPLACED FLOOR BOARDS AND TREATED METAL IAW SRM 51-10-4, 51-70-0, 51-10-3. (M) 2 L 7 2 4F A6WE 1996101000682 19961010 00682 WP 1996 10 10 GTIA96NK150 1 19960330 A 2130 12911021 THERMOSTAT DOUG DC9 DC931 3022065 WP LEFT MALFUNCTIONED A GTIA A G UNSCHED LANDING O2 MASK DEPLOYED J WARNING INDICATION DE DESCENT 1 GL 23 932ML 47547 CABIN PRESSURIZATION FAILURE DESENDING THROUGH 27000 FEET. DECLARED EMERGENCY, MASKS DROPPED. DIVERTED TO TPA. REPLAC ED LEFT AUG VALVE THERMOSTAT. GROUND RUN PERFORMED. SYTSEM CHECKS SATISFACTORY. (M) 2 L 7 2 4F A6WE 1996101000683 19961010 00683 WP 1996 10 10 GTIA96NK151 1 19960330 A 2130 12911211 ANTICIPATOR DOUG DC9 DC931 3022065 WP LEFT MALFUNCTIONED A GTIA A G UNSCHED LANDING O2 MASK DEPLOYED J WARNING INDICATION DE DESCENT 1 GL 23 932ML 47547 CABIN PRESSURIZATION FAILURE. DESCENDING THROUGH 27,000 FEET. DECLARED EMERGENCY, MASKS DROPPED. DIVERTED TO TPA. RE PLACED LEFT AUG VALVE ANTICIPATOR. GROUND RUN PERFORMED, SYSTEM CHECKS SATISFACTORY. (M) 2 L 7 2 4F A6WE 1996101000684 19961010 00684 WP 1996 10 10 GTIA96NK152 1 19960330 A 2131 10256862 CONTROLLER DOUG DC9 DC931 3022065 WP CABIN FAILED A GTIA A G UNSCHED LANDING O2 MASK DEPLOYED J WARNING INDICATION DE DESCENT 1 GL 23 932ML 47547 CABIN PRESSURIZATION FAILURE DESCENDING THROUGH 27,000 FEET. DECLARED EMERGENCY, MASKS DROPPED. DIVERTED TO TPA. REPL ACED CABIN PRESSURE CONTROLLER. GROUND RUN PERFORMED, SYSTEM CHECKS SATISFACTORY. (M) 2 L 7 2 4F A6WE 1996101000685 19961010 00685 WP 1996 10 10 GTIA96NK153 1 19960403 A 3297 WIRE DOUG DC9 DC931 3022065 WP LT MLG BROKEN A GTIA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 23 969ML 47268 LEFT GEAR GREEN LIGHT CAME ON AND OFF IN FLIGHT. UPON GEAR EXTENSION THE GEAR UNSAFE LIGHT CAME ON. GEAR VISUALLY CHEC KED DOWN AND LOCKED. REPAIRED BAD GROUND CONNECTION AT STUD NR 551, REPAIRED BAD CONNECTION TO TERM NR 5 (53-65). REPA IRED BROKEN WIRE AT P1-130 PIN NR 5. PERFORMED GEAR SWING SYSTEMS CHECKS GOOD. (M) 2 L 7 2 4F A6WE 1996101000686 19961010 00686 WP 1996 10 10 GTIA96NK154 1 19960330 A 2731 95906 ACTUATOR DOUG DC9 DC931 3022065 WP ELEVATOR FAILED A GTIA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 GL 23 969ML 47268 ON CLIMB-OUT, AT 8,000 FEET, PRIMARY LONGITUDINAL TRIM FAILED, NEITHER YOKE SWITCHES NOR THE SUITCASE SWITCHES WORKED. U SED AUTOPILOT WITH ALTERNATE TRIM TO RETURN TO TPA. REMOVED PRIMARY LONGITUDINAL TRIM MOTOR. OPS CHECKED GOOD. (M) 2 L 7 2 4F A6WE 1996101000687 19961010 00687 WP 1996 10 10 GTIA96NK155 1 19960427 A 2613 6712152180 THERMO SWITCH DOUG DC9 DC931 3022065 WP TAIL COMPT MALFUNCTIONED A GTIA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 969ML 47268 TAIL COMPARTMENT TEMP HI-LIGHT ILLUMINATED AFTER TAKEOFF PRIOR TO 1000 FEET AGL. WARNING EXTINGUISHED WITH BOTH HP BLEE D SWITCHES OFF. REPLACED TAIL COMPARTMENT TEMP SENSORS. OPS CHECKED GOOD. (M) 2 L 7 2 4F A6WE 1996101000688 19961010 00688 WP 1996 10 10 GTIA96NK156 1 19960429 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DIRTY A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 947ML 47514 BOTH COCKPIT EMERGENCY LIGHTS WILL NOT ILLUMINATE WHEN EMERGENCY LIGHTS ARE SELECTED 'ON' FOR TESTING CABIN AND COCKPIT LIGHTS. CLEANED TERMINALS AT BATTERY PACK, OP CHECKED LIGHTS OK. (M) 2 L 7 2 4F A6WE 1996101000689 19961010 00689 WP 1996 10 10 GTIA96NK157 1 19960429 A 3350 BULBS DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 12536 47113 FIRST TEN FEET OF FLOOR TRACK LIGHTING INOP. REMOVED AND REPLACED BULBS AS REQUIRED. OP CHECKS GOOD. (M) 2 L 7 2 4F A6WE 1996101000690 19961010 00690 WP 1996 10 10 GTIA96NK158 1 19960501 A 3260 H1410051 SWITCH DOUG DC9 DC932 3022066 WP NLG INOPERATIVE A GTIA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 23 12536 47113 NOSE GEAR DOWN 'GREEN' LIGHT FAILED TO ILLUNMINATE DURING GEAR EXTENSION. GEAR VERIFIED DOWN VISUALLY. LIGHT CAME ON D URING SECOND APPROACH. CONTACTS ON NLG UPLIMIT SWITCH INOP. REMOVED NLG UPLIMIT MICROSWITCH. OPS CHECK GOOD IAW MM 32 . (M) 2 L 7 2 4F A6WE 1996101000691 19961010 00691 WP 1996 10 10 GTIA96NK159 1 19960503 A 2612 WIRE DOUG DC9 DC932 3022066 WP RT ENGINE CHAFED A GTIA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 12536 47113 AT CRUISE, MCO-PHL, FIRE DETECTOR LOOP ANNUNCIATOR LIGHT AND RIGHT ENGINE 'B' LOOP LIGHT STARTED FLICKERING, COMPLIED WI TH FCOM PROCEDURES. FOUND WIRES W255A16 AND W286A16N RUBBING TOGETHER. NO DAMAGE FOUND TO EXPOSED WIRES, REPAIRED WIRI NG IAW MM CHP 20. FIRE DETECTOR OP CHECKS GOOD. (M) 2 L 7 2 4F A6WE 1996101000692 19961010 00692 WP 1996 10 10 GTIA96NK160 1 19960417 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP BS 160-200 EXFOLIATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12505 45788 DURING C-CHECK, FOUND FORWARD ENTRY DOOR WAY FLOOR SUPPORT MEMBER AT FS 160-200 EXFOLIATED. FABRICATED, TREATED AND INS TALLED NEW FLOOR SUPPORT IAW SRM 51-10-1, 51-30-0, 51-10-3. (M) 2 L 7 2 4F A6WE 1996101000693 19961010 00693 WP 1996 10 10 GTIA96NK161 1 19960417 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP BS 160-200 CORROSION A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12505 45788 DURING C-CHECK, FOUND UNDER FLOOR MEMBRANE CORRODED ALONG FLOOR SUPPORT MEMBER BETWEEN FS 160-200, 36 INCHES LEFT OF CEN TER. FABRICATED, TREATED AND INSTALLED NEW MEMBRANE IAW SRM 53-01, 51-10-03, AND 51-30-0. (M) 2 L 7 2 4F A6WE 1996101000694 19961010 00694 WP 1996 10 10 GTIA96NK162 1 19960417 A 5320 FLOOR SUPPORT DOUG DC9 DC932 3022066 WP BS 160-200 CORROSION A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12505 45788 DURING C-CHECK, FOUND FLOOR SUPPORT MEMBER IS GALLEY SERVICE DOOR ENTRYWAY, 36 INCHES RIGHT OF CENTER CORRODED ALONG TOP OF FLANGE. FABRICATED, TREATED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-10-1, 51-30-0 AND 51-10-3. (M) 2 L 7 2 4F A6WE 1996101000695 19961010 00695 WP 1996 10 10 GTIA96NK163 1 19960417 A 5320 MEMBRANE DOUG DC9 DC932 3022066 WP BS 180 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12505 45788 DURING C-CHECK, FOUND LEVEL 2 CORROSION IN GALLEY DOOR ENTRY WAY AT FS 180 AND APPROX 40 INCHES RIGHT OF CENTERLINE. AL SO, MEMBRANE HAS CORROSION UNDER THE SEAM AREA. REMOVED CORROSION AND REPLACED MEMBRANE, TREATED AREA IAW 53-10, 51-10- 3 AND 51-30-0. (M) 2 L 7 2 4F A6WE 1996101000696 19961010 00696 WP 1996 10 10 GTIA96NK164 1 19960417 A 5712 RIB CAP DOUG DC9 DC932 3022066 WP BS 930 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12505 45788 DURING C-CHECK, FOUND CORRODED RIB CAP IN AFT CARGO COMPARTMENT STATION 930 LEFT. FABRICATED, TREATED AND INSTALLED NEW RIB CAP IAW SRM 51-10-3, 51-10-1 AND 51-10-4. (M) 2 L 7 2 4F A6WE 1996101000697 19961010 00697 WP 1996 10 10 GTIA96NK165 1 19960417 A 5320 STRAP DOUG DC9 DC932 3022066 WP BS 327 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12505 45788 DURING C-CHECK, FOUND FORWARD CARGO BAY STATION 327 TO 370, RIGHT SIDE RBL 17 FLOOR BOARD SUPPORT STRAP CORRODED. FABRI CATED SUPPORT STRAP AND TREATED CORROSION IAW SRM 53-03, 51-10-3. (M) 2 L 7 2 4F A6WE 1996101000698 19961010 00698 WP 1996 10 10 GTIA96NK167 1 19960519 A 2520 SEAT BELT DOUG DC9 DC932 3022066 WP CABIN CUT A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12505 45788 FORWARD LIGHT ATTENDANT JUMPSEAT OUTBOARD SEAT BELT INBOARD HARNESS STRAP CUT AND FRAYED. REPLACED SEAT BELT HARNESS ST RAP. (M) 2 L 7 2 4F A6WE 1996101000699 19961010 00699 WP 1996 10 10 GTIA96NK168 1 19960519 A 2612 FIRE LIGHT DOUG DC9 DC932 3022066 WP LT ENGINE ILLUMINATED A GTIA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 23 947ML 47514 LEFT ENGINE LOOP B-LOOP FAIL LIGHT ON. SYSTEM TESTS NORMAL. INSPECTED LOOPS FOUND NOTHING ABNORMAL AT THIS TIME. LOOP FAIL LIGHT NOT ILLUMINATED. (M) 2 L 7 2 4F A6WE 1996101000700 19961010 00700 WP 1996 10 10 GTIA96NK169 1 19960519 A 2612 59100241 FIRE LOOP DOUG DC9 DC932 3022066 WP LT ENG FAILED A GTIA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 23 947ML 47514 'L' FIRE LOOP B ILLUMINATED IN FLIGHT. REMOVED AND REPLACED LEFT ENGINE FIRE LOOP. OP CHECKS GOOD. (M) 2 L 7 2 4F A6WE 1996101000701 19961010 00701 1996 10 10 GTIA96NK170 4 19960518 A 3418 9650041027 STALL WARN COMP DOUG DC9 DC931 3022065 WP NR 1 MALFUNCTIONED A GTIA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 932ML 47547 STALL WARNING STICK SHAKER ACTIVATED 240 KTS CLEAN, PULLED P35 PER FCOM. SWAPPED NR 1 AND NR 2 STALL WARN COMP. FOUND BOTH INDICATOR PINS POPPED ON NR 1 STALL WARNING COMPUTER. RESET AND SELF TESTED SYSTEM. SYSTEM OPS CHECKS GOOD. (M) 2 L 7 2 4F A6WE 1996101000702 19961010 00702 WP 1996 10 10 GTIA96NK172 1 19960626 A 2781 H20624 SWITCH DOUG DC9 DC931 3022065 WP LE FLAPS MALFUNCTIONED A GTIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 23 969ML 47268 TAKEOFF WARNING HORN ACTIVATED ON TAKEOFF ROLL. RETURNED TO GATE. REMOVED AND REPLACED LE FLAP TAKEOFF WARNING SWITCH IAW DC-9MM CHAP 27. OPS CHECKS GOOD. (M0 2 L 7 2 4F A6WE 1996101000703 19961010 00703 WP 1996 10 10 GTIA96NK173 1 19960624 A 4980 5915793107 EXHAUST DUCT DOUG DC9 DC931 3022065 WP APU CRACKED A GTIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 23 969ML 47268 TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATES WITHIN 3-5 MINUTES AFTER PUTTING APU AIR ON. LIGHT GOES OUT 30-60 SEC AFTE R TURNING APU AIR OFF. CLEANED TAIL TEMP SENSOR, NO HELP. DEFERRED APU PER MEL 49-1 CAT C. LOG PAGE 5218 - REMOVED AN D REPLACED APU EXHAUST DUCT. (M) 2 L 7 2 4F A6WE 1996101000704 19961010 00704 WP 1996 10 10 GTIA96NK174 1 19960706 A 3244 A9560892 TIRE DOUG DC9 DC931 3022065 WP LT MLG FAILED A GTIA K J NONE DUMP FUEL D INFLIGHT SEPARATION TO TAKEOFF 1 GL 23 969ML 47268 NR 2 MAIN TIRE RECAP CAME OFF ON TAKEOFF. ON LANDING DTW REQUEST EMERGENCY EQUIPMENT STANDBY. ON GEAR EXTENSION LEFT G EAR LIGHT DID NOT ILLUMINATE. TOWER REPORTED GEAR LOOKED NORMAL. CARRIED OUT GEAR UNSAFE PROCEDURES. LANDING NORMAL. AIRCRAFT TOWED TO GATE DUE TO HYD FLUID LOSS. FOUND DAMAGE TO ANTI-SKID HYD LINES. FLAP TRAILING EDGE AND NR 1 ENGINE FOD'ED. REPLACED DAMAGED HYD LINES. REPAIRED TRAILING EDGE FLAP, REPLACED NR 1 ENGINE, AND REPLACED BOTH LEFT MAIN TI RES/WHEELS. (M) 2 L 7 2 4F A6WE 1996101000705 19961010 00705 WP 1996 10 10 GTIA96NK176 1 19960709 A 3350 LIGHT DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 969ML 47268 ON DAILY, FOUND REAR EMERGENCY TRACK LIGHTS WOULD NOT ILLUMINATE. FOUND SEVERAL LIGHT ASSEMBLYS BAD. REMOVED AND REPLA CED LIGHT ASSEMBLYS. (M) 2 L 7 2 4F A6WE 1996101000706 19961010 00706 WP 1996 10 10 GTIA96NK177 1 19960712 A 2150 CLAMP DOUG DC9 DC931 3022065 WP ACM LOOSE A GTIA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 969ML 47268 TAIL COMPARTMENT TEMP 'HIGH' LIGHT ON DURING CLIMB-OUT FROM RSW. LIGHT WENT OUT WHEN POWER REDUCED TO 1.6 EPR FOR TAKEO FF PROFILE AND REMAINED OUT. FOUND DUCT LEAK ON ACM. REPOSITIONED CLAMP AND SECURED. RAN PACK LEFT SIDE, NO LEAKS NOT ED. (M) 2 L 7 2 4F A6WE 1996101000707 19961010 00707 WP 1996 10 10 GTIA96NK178 1 19960715 A 2530 WATER LINE DOUG DC9 DC932 3022066 WP COFFEE MAKER LOOSE A GTIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 23 942ML 47478 COFFEE MAKER SMOKING AND SPARKS COMING OUT FROM BACK. FOUND DE-ACTIVATED WATER LINE SPARKING AGAINST TERMINAL END. RE- POSITIONED AND SECURED LINE. (M) 2 L 7 2 4F A6WE 1996101000708 19961010 00708 WP 1996 10 10 GTIA96NK179 1 19960718 A 3610 5910245625 DUCT DOUG DC9 DC931 3022065 WP LEFT 8TH STAGE CRACKED A GTIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 969ML 47268 AIRTURN BACK - TAIL COMPARTMENT TEMP 'HIGH' LIGHT ILLUMINATED ON TAKEOFF AND CRUISE. FOUND 8TH STAGE DUCT FROM FIRE WAL L ON INSIDE OF THE TAIL COMPARTMENT CRACKED. REPLACED DUCT. (M) 2 L 7 2 4F A6WE 1996101000709 19961010 00709 WP 1996 10 10 GTIA96NK180 1 19960719 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN CHAFED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 934ML 47526 EMERGENCY EXIT LIGHT AT REAR EDGE OF GALLEY SERVICE DOOR CONTINUOUSLY FLICKER IN FLIGHT. FOUND WIRE CHAFED ON LIGHT ASS EMBLY. REPAIRED AS NECESSARY. (M) 2 L 7 2 4F A6WE 1996101000710 19961010 00710 WP 1996 10 10 GTIA96NK181 1 19960720 A 3610 CLAMP DOUG DC9 DC931 3022065 WP TAIL COMP LOOSE A GTIA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 969ML 47268 TAIL COMPARTMENT TEMP 'HIGH' LIGHT CAME ON AFTER TAKEOFF FROM MYR. ILLUMINATED FOR ABOUT 1.5 MINUTE, FOLLOWED F COM PRO CEDURES, WENT OUT, CONTINUED NORMALLY TO DTW. SECURED CLAMP AT LEFT ACM COMPRESSOR DISCHARGE DUCT. OPS CHECKED OK. CO ULD NOT DUPLICATE. (M) 2 L 7 2 4F A6WE 1996101000711 19961010 00711 WP 1996 10 10 GTIA96NK183 1 19960730 A 3397 WIRE DOUG DC9 DC932 3022066 WP CABIN MISINSTALLED A GTIA K NONE L W NO TEST INADEQUATE Q C IN INSP/MAINT 1 GL 23 12536 47113 LAST SIX FEET OF FLOOR TRACK LIGHTS IN CABIN, AND FLOOR TRACK LIGHTS IN TAIL CONE, NOT ILLUMINATING WHEN POT IN TEST MOD E. SWITCHED CROSSED WIRES ON B5-27 AS REQUIRED. OPS CHECKS GOOD IAW DC-9 MM CHAPTER 33. (M) 2 L 7 2 4F A6WE 1996101000712 19961010 00712 WP 1996 10 10 GTIA96NK186 1 19960801 A 3350 20131A BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 12536 47113 FORWARD CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY ASSEMBLY. OPS NORMAL IAW DC-9 MM CHAP 33. (M) 2 L 7 2 4F A6WE 1996101000713 19961010 00713 WP 1996 10 10 GTIA96NK190 1 19960816 A 2760 RETRACT MECH DOUG DC9 DC932 3022066 WP SPOILERS MALFUNCTIONED A GTIA O OTHER J WARNING INDICATION LD LANDING 1 GL 23 12536 47113 SPOILERS FAILED TO DEPLOY ON TOUCHDOWN SMELL OF SMOKE OR BURNING INSULATION COMING FROM PEDISTAL. OPERATED SYSTEM FOUND AUTO SPOILER NOT RESETTING. FOUND NO DEFECTS ON ODOR. PLACED ON DMI PER MEL 27-19-1 CAT C. (M) 2 L 7 2 4F A6WE 1996101000714 19961010 00714 WP 1996 10 10 GTIA96NK191 1 19960818 A 3297 WIRE DOUG DC9 DC932 3022066 WP RT MLG DETERIORATED A GTIA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 23 941ML 47131 RIGHT LANDING GEAR UNSAFE LIGHT FLICKERS INTERMITTENTLY DURING TRANSIT OF LANDING GEAR BOTH IN RETRACTION AND EXTENSION. REPAIRED WIRING AT AND REPLACE CANNON PLUG ON RIGHT LANDING GEAR UPLIMIT SWITCH. (M) 2 L 7 2 4F A6WE 1996101000715 19961010 00715 WP 1996 10 10 GTIA96NK192 1 19960821 A 2530 COFFEE MAKER DOUG DC9 DC932 3022066 WP FWD GALLEY FAILED A GTIA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 23 947ML 47514 AFTER BLOCKING INTO ACY, FLIGHT ATTENDANT REPORTED A BURN SMELL COMING FROM THE AREA OF THE COFFEE MAKER. FOUND COFFEE POT WARMER BUTTON STUCK ON 'IN' POSITION. CLEANED AND FREED BUTTON, NO OTHER SMELL IN AREA. (M) 2 L 7 2 4F A6WE 1996101000716 19961010 00716 WP 1996 10 10 GTIA96NK194 1 19960904 A 3350 60030431 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 947ML 47514 ON PREFLIGHT, SOME OF THE OVERHEAD EMERGENCY LIGHTS WERE INOP. AS PER WIRING DIAGRAM 33-51-01, ALL EMERGENCY LIGHTING I S OPERATIVE. REPLACED AFT BATTERY PACK. (M) 2 L 7 2 4F A6WE 1996101000717 19961010 00717 WP 1996 10 10 GTIA96NK195 1 19960904 A 3350 60030431 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOP A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 947ML 47514 ON DAILY, FOUND BATTERY PACK INOP (REF PREVIOUS LOG PAGE DISCREPANCY M629). REMOVED AND REPLACED BATTERY CHARGER IAW DC -9 MM CHAP 33. OP CHECKED GOOD. (M) 2 L 7 2 4F A6WE 1996101000718 19961010 00718 WP 1996 10 10 GTIA96NK196 1 19960905 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN LOW VOLTAGE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 928ML 47326 ON DAILY INSPECTION, FOUND LEFT OVERWING EXIT LIGHTING INOP. RECHARGED EMERGENCY LIGHTING POWER SUPPLY BATTERIES. SYST EM OPERATIONAL CHECKS GOOD. (M) 2 L 7 2 4F A6WE 1996101000719 19961010 00719 WP 1996 10 10 GTIA96NK198 1 19960907 A 2612 CONNECTOR DOUG DC9 DC932 3022066 WP B FIRE LOOP INOP A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 941ML 47131 NR 1 ENGINE FIRE DETECTOR B-LOOP INOP, FOUND ON DAILY. FOUND BAD CONNECTOR FORWARD PYLON B-LOOP. CONNECTOR ON ORDER DE FERRED B-LOOP SYSTEM. NR 1 ENGINE PER MEL 26-1 DMI NR 002701. (M) 2 L 7 2 4F A6WE 1996101000720 19961010 00720 WP 1996 10 10 GTIA96NK199 1 19960912 A 2130 PRESSURE SYSTEM DOUG DC9 DC932 3022066 WP CABIN FAILED A GTIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 12505 45788 AIRCRAFT LOG PAGE NR 028813, ITEM NR P744 - PRESSURIZATION FAILED ON TAKEOFF OUT OF ACY. RETURNED ON TAKEOFF, OUT OF AC Y. RETURNED FOR MAINTENANCE INSPECTION. DEFERRED PRESSURIZATION IAW MEL 21-24, DMI NR 2595. (M) 2 L 7 2 4F A6WE 1996101000721 19961010 00721 WP 1996 10 10 GTIA96NK200 1 19960913 A 5312 DOOR FRAME DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 947ML 47514 DURING X-RAY INSPECTION OF THE AFT PRESS BULKHEAD VENTRAL STAIR DOOR FRAME, A 1.375 IN CRACK WAS DISCOVERED AT THE UPPER LEFT CORNER. EVAULATED CRACK AS DESCRIBED PER SB53-137R4 PG 19 GROUP 22 COND 4. THE AIRCRAFT IS OK FOR CONTINUED SERVI CE PER SB53-137R4 PAGE NR 48. VISUAL AND X-RAY INSPECTION OF THE UPPER CORNERS IS COMPLIED AT INTERVALS NOT TO EXCEED 5 00 LANDINGS PER PARAGRAPH 2A OF SB 53-137R4. THIS ITEM TRANSFERRED TO CARRY OVER ITEM NR 5A-53-005, PER REPAIR. (M) 2 L 7 2 4F A6WE 1996101000722 19961010 00722 WP 1996 10 10 GTIA96NK201 1 19960913 A 3510 11417530260 OXY HOSE DOUG DC9 DC932 3022066 WP COCKPIT FAILED A GTIA O OTHER O OTHER CL CLIMB 1 GL 23 941ML 47131 DURING CLIMB-OUT OF 18,000 FEET, CREW OXYGEN BOTTLE INDICATED JUST BELOW 1500 PSI. RETURNED TO DTW. SHUT OFF BOTTLE AT 1300 PSI. WITH BOTTLE OFF, OXYGEN STILL DECREASED TO 1200 PSI. REMOVED AND REPLACED CREW OXYGEN BOTTLE. FOUND CRACKE D OXYGEN FITTING ON OXYGEN REGULATOR HOSE. REMOVED AND REPLACED OXYGEN HOSE ASSY. NO LEAKS OK FOR FLT. (M) 2 L 7 2 4F A6WE 1996101000723 19961010 00723 WP 1996 10 10 GTIA96NK202 1 19960914 A 5230 SKIN DOUG DC9 DC932 3022066 WP BAGG DOOR DENTED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 947ML 47514 RIGHT FUSELAGE, FORWARD OF FORWARD BAGGAGE DOOR, HAS NUMEROUS MINOR DENTS. DAMAGE INSPECTION DETERMINED, UNABLE TO REPA IR AT THIS TIME. DOUGLAS INFORMED OF DAMAGE AND APPROVED RESPONSE IAW ACTION NR 310001. REPAIRS TO BE COMPLIED WITH AT NEXT C-CHECK INSPECTION. ENTERED INTO CARRY OVER. (M) 2 L 7 2 4F A6WE 1996101000724 19961010 00724 WP 1996 10 10 GTIA96NK203 1 19960130 A 2910 FILTERS DOUG DC9 DC932 3022066 WP HYD SYS DIRTY A GTIA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 23 942ML 47478 ON APPROACH, NOSE GEAR DID NOT SHOW DOWN. EXTENDED NOSE GEAR WITH MANUAL EXTENSION LEVER, LANDING UNEVENTFUL. REMOVED AND REPLACED HYD SYSTEM FILTERS, FLUSHED SYSTEM, DID GEAR SWING (SEVERAL TIMES). NO DEFECTS NOTED. (M) 2 L 7 2 4F A6WE 1996101000725 19961010 00725 WP 1996 10 10 GTIA96NK204 1 19960824 A 2530 50405100 COFFEE MAKER DOUG DC9 DC932 3022066 WP FWD GALLEY FAILED A GTIA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 23 947ML 47514 TRANSFERRED FROM CABIN DISCREPANCIES LOG ITEM 1 'COFFEE POT SMELLS LIKE ITS BURNING AND WARMER BUTTON IS STUCK IN THE ON POSTION.' DEFERRED COFFEE MAKER IAW MEL 25-12 DMI 5006 CATD PLACARDED. LOG PAGE 028771. REMOVED AND REPLACED COFFEE MAKER CLEARED 5006 PLACARD REMOVED. (M) 2 L 7 2 4F A6WE 1996101000727 19961010 00727 WP 1996 10 10 HALA96130 1 19960912 A 2150 204950 PACK DOUG DC9 DC951 3022051 WP LEFT MALFUNCTIONED A A HALA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 13 EICBI 631437 48122 FLT 539 - OGG - FLIGHT ATTENDANT REPORTED STRONG BURNING SMELL THROUGHOUT CABIN, SMELLED ELECTRICAL. ODOR STARTED JUST AFTER TAXI FROM RAMP. INSPECTED TAIL COMPARTMENT, E/E COMPT AND BOTH ENGINES. OPERATED BOTH PACKS AND NOTICED LEFT PAC K DUCT TEMP VERY HIGH AT 120 DEGREES, AND HOT AIR COMING THROUGH RIGHT PACK. OPS CHECK OK WHEN ISOLATED FROM LEFT PACK. ITEM CONTINUED PER MEL AND LEFT PACK SCHEDULED FOR CHANGE. (M) 2 L 7 2 4F A6WE 1996101000728 19961010 00728 NM 1996 10 10 MZZA96070 1 19960905 A 2910 BACH8ANN0310T HYD LINE BOEING 727 727232 1384082 NM ON DOOR ACT RUPTURED A MZZA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 13 15781 20636 FLT 864 - GUM - LOST ALL 'A' SYSTEM HYDRAULIC FLUID DURING GEAR AND FLAP RETRACTION AFTER TAKEOFF. FOUND RIGHT GEAR DOO R ACTUATOR PRESSURE LINE BLOWN. REPLACED LINE AND PERFORMED LEAK CHECK. REPLACED 'A' SYSTEM HYDRAULIC PUMP ON NR 1/2 E NGINES. CHECKED BOTH CASE DRAIN FILTERS. RAN ENGINES AND PERFORMED LEAK CHECK. (M) 2 L 7 3 4F A3WE 1996101000729 19961010 00729 NM 1996 10 10 PCAA9600298 1 19960808 A 3350 82410162005 CONTROL BOX DHAV DHC8 DHC8102 2809003 NM E/E COMPT FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 811AW 201 EMERGENCY LIGHTS INTERMITTENTLY ILLUMINATE IN FLIGHT. TROUBLESHOT AND FOUND EMERGENCY LIGHTS CONTROL BOX AT FAULT. REM OVED AND REPLACED CONTROL BOX. SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1996101000730 19961010 00730 NM 1996 10 10 PCAA9600299 1 19960819 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN LOOSE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 820EX 19178 019 FOUND FLOOR EMERGENCY LIGHTS INOP ON LEFT SIDE, AFT OF ROW 6. REATTACHED WIRE CONNECTOR AT ROW 9, OPS CHECK GOOD. AIRC RAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1996101000731 19961010 00731 NM 1996 10 10 PCAA9600301 1 19960824 A 3260 841005 PROX CONTL BOX DHAV DHC8 DHC8102 2809003 NM E/E COMPT FAILED A PCAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 13 831EX 11308 246 160 ELECTRICAL SMELL WAS NOTICED 10 MINUTES INTO FLIGHT, RETURNED TO FIELD. TROUBLESHOT AND FOUND PROXIMITY SENSOR ELECTRON IC UNIT AT FAULT. REMOVED AND REPLACED PSEU IAW DHC MM. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1996101000732 19961010 00732 NM 1996 10 10 PCAA9600302 1 19960825 A 3320 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 13 808EX 12355 299 DURING DESCENT INTO BWI, AT LOW POWER SETTINGS, NOTICED A HOT BURNING ODOR IN COCKPIT AND CABIN. TROUBLESHOT AND FOUND ODOR EMITTING FROM LIGHT FIXTURE ABOVE SEAT 4AC. DISABLED FIXTURE AND ISSUED MEL. APU BLEED ALSO RENDERED INOPERATIVE PER MEL, DUE TO ODOR COMING FROM IT. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1996101000733 19961010 00733 NM 1996 10 10 PCAA9600303 1 19960825 A 3320 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 13 808EX 12355 299 DURING DESCENT INTO ALB, A BURNING PLASTIC SMELL WAS NOTICED IN CABIN. FOUND OVER HEAD LAMP ARCING AT RECEPTICAL 4AC. R EMOVED AND REPLACED BULB, OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1996101000734 19961010 00734 EU 1996 10 10 RAIA960823 1 19960816 A 3397 3351157 WIRE AEROSP ATR72 ATR72202 8680940 EU CABIN BROKEN A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 721TE 217 MLI - FLT 7163 - EMERGENCY ESCAPE PATH LIGHTING IS INOP AT ROW 2AB. MAINTENANCE REPAIRED BROKEN WIRE AT BULB AT SEAT 2A . (M) 2 H 7 2 4T RT A53EU 1996101000735 19961010 00735 EU 1996 10 10 RAIA960824 1 19960820 A 7712 KPT06F84S CONNECTOR BAG JETSTM JETSTM3201 1500217 EU LT ENGINE DIRTY A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 433AM 11250 885 FWA - FLT 7509 - LEFT ENGINE DID NOT MAKE TORQUE. PERFORMED GROUND RUNS, MADE TORQUE WITH THE TTL TURNED OFF. MAINTENA NCE CLEANED OIL FROM THE BYPASS VALVE CANNON PLUG. (M) 2 L 7 2 4T RT A56EU 1996101000736 19961010 00736 EU 1996 10 10 RAIA960825 1 19960826 A 3030 49380 PITOT HEAT AEROSP ATR42 ATR42300 8680920 EU NR 1 FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 424TE 3700 124 STL - FLT 7408 - CAPTAINS PITOT HEAT FAULTED. UNABLE TO DEFER DUE TO THUNDERSTORMS. MAINTENANCE REPLACED THE NR 1 PITO T TUBE. (M) 2 H 7 2 4T RT A53EU 1996101000737 19961010 00737 EU 1996 10 10 RAIA960826 1 19960827 A 7931 696219 OIL PRESS TEMP BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 860AE 4701 860 FAT - FLT 4752 - LEFT OIL TEMP STARTED INCREASING, AND OIL PRESSURE STARTED TO DROP. MAINTENANCE REPLACED THE LEFT OIL TEMP/PRESSURE INDICATOR. (M) 2 L 7 2 4T RT A56EU 1996101000738 19961010 00738 EU 1996 10 10 RAIA960828 1 19960828 A 7712 KPT06F84S CONNECTOR BAG JETSTM JETSTM3201 1500217 EU LT ENGINE OIL SOAKED A RAIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 433AM 11288 885 ALO - FLT 7415 - LEFT ENGINE WAS SMOKING FROM TAILPIPE DURING TTL TEST. MAINTENANCE CLEANED OIL FROM THE LEFT BYPASS VA LVE CANNON PLUG. PERFORMED GROUND RUNS, OPS CHECK GOOD. (M) 2 L 7 2 4T RT A56EU 1996101000739 19961010 00739 EU 1996 10 10 RAIA960901 1 19960903 A 3241 140071 TRANSDUCER AEROSP ATR42 ATR42300 8680920 EU LT MLG INTERMITTENT A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 EICBK 14161 199 STL - FLT 7174 - LEFT BRAKE SLIPS DURING TAXI. MAINTENANCE REPLACED THE LEFT INBOARD ANTI-SKID TRANSDUCER. (M) 2 H 7 2 4T RT A53EU 1996101000740 19961010 00740 EU 1996 10 10 RAIA960911 1 19960915 A 5610 1379146C406 WINDSCREEN BAG JETSTM JETSTM3201 1500217 EU RT COCKPIT CRACKED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 428AM 8638 877 STL - FLT 7466 - DURING CRUISE, THE FLIGHT OFFICERS FORWARD WINDSCREEN CRACKED. MAINTENANCE REPLACED THE FLIGHT OFFICER S WINDSCREEN. (M) 2 L 7 2 4T RT A56EU 1996101000741 19961010 00741 EU 1996 10 10 SIMA962541 1 19960910 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 223AT 3725 223 ORD - FLT 4205 - FORWARD CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND INSTALLED SERVICEABLE BATTERY PACK AT 10WLA. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996101000742 19961010 00742 EU 1996 10 10 SIMA962551 1 19960911 A 2161 6248201 CONTROLLER AEROSP ATR72 ATR72212 EU COCKPIT FAILED A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 431AT 04C855 431 CMI - FLT 4374 - ON GROUND IN CMI, FLIGHT CREW REPORTED SMOKE IN COCKPIT, AND ALSO NOTED BOTH AUTO TEMP CONTROLLERS WERE INOP. MAINTENANCE REPLACED COCKPIT TEMP CONTROLLER. GROUND RUN A/C, CABIN TEMP CONTROLLER OPERATES NORMAL IN MANUAL, COCKPIT CONTROLLER CHECKED GOOD BOTH AUTO AND MANUAL AND NOTED NO EVIDENCE OF SMOKE. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996101000743 19961010 00743 EU 1996 10 10 SIMA962571 1 19960913 A 3350 LH6151 SOCKET AEROSP ATR72 ATR72212 EU CABIN LOOSE WIRES A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 274AT 274 DFW - EMERGENCY LIGHT NEAR SEAT 7AB NOT WORKING. FOUND WIRE SEPARATED FROM SOCKET. RESOLDERED CONNECTIONS ON SOCKET. O PS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996101000744 19961010 00744 NM 1996 10 10 TAOA099604 1 19960910 A 5311 65C3628040 FRAME BOEING 727 727254 138408L NM BS 783.95 CRACKED A TAOA K NONE O OTHER IN INSP/MAINT 1 EA 15 915TS 20252 ASSIGNED CHECK FOR CRACKS AT BS 783.95 NEAR STRINGER 17, PER SERVICE BULLETIN 727-53-0197 REV 2. INSPECTION REVEALS CRA CK IN RIGHT FRAME AT 783.95 NEAR STRINGER 17 OUTBOARD OF WEB MOD. REPAIR ACCOMPLISHED PER SB 727-53-0197 AND EO 2753A05 4. (M) 2 L 7 3 4F A3WE 1996101000745 19961010 00745 NE 1996 10 10 TAOA099606 2 19960910 A 7230 COMPRESSOR BOEING 727 727227 1384078 NM PWA JT8 JT8D7B 52053 NE LT ENGINE STALLED A TAOA O OTHER R PARTIAL RPM/PWR LOSS CL CLIMB 1 EA 15 925TS 21244 655315 DURING TAKEOFF, COMPRESSOR STALL REPORTED TO BE LEFT SIDE AT 800 FEET ALTITUDE. RAN ALL THREE ENGINES, CHECKED THE POWE R, BLEED SCHEDULING AND ACCELERATION. ALL CHECKED OK WITH NO STALLS. ACCOMPLISHED COMPRESSOR WASH NR 1 ENGINE, RAN ENG INE, ALL NORMAL IAW MM CHAPTER 71-00 PAGE 210A-212A. (M) 2 L 7 3 4F 4 F A3WE E2EA 1996101000746 19961010 00746 NM 1996 10 10 TWRA96310 1 19960902 A 3397 WIRE BOEING 747 747238B 1384828 NM CABIN BROKEN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 607PE 20011 DURING DAILY CHECK, FOUND D-ZONE EVAC FLOOR LIGHT AT SEAT 43C INOP. FOUND BROKEN WIRE, RESPLICED WIRE. OPS CHECKED GOO D PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996101000747 19961010 00747 NM 1996 10 10 TWRA96311 1 19960907 A 3397 WIRE BOEING 747 747212B 1384886 NM CABIN SHORTED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND EVAC LIGHTS HAVE A SHORTED CIRCUIT ALONG SIDE SEAT 50H. REPAIRED WIRING. OPS CHECKED GOOD PE R 33-51-00. (M) 2 L 7 4 4F A20WE 1996101000748 19961010 00748 NM 1996 10 10 TWRA96312 1 19960908 A 3350 6012111RF BATTERY PACK BOEING 747 747136 1384883 NM CABIN DISCHARGED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 606FF 855 20273 DURING DAILY CHECK, FOUND OVERWING EVAC LIGHTS (2 EACH) INOP LEFT WING. REMOVED AND REPLACED BATTERY PACK. OPS CHECKED NORMAL PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996101000749 19961010 00749 EU 1996 10 10 VTZA96321 1 19960823 A 2150 MOTOR JETAIR JETSTM JETSTM4101 1500501 EU AIR CONDITIONING FAILED A VTZA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 27 313UE 41026 FLT NR 6235 - JFK-IAD - DURING TAXI RETURNED TO GATE, DUE TO FREON COMPRESSOR MOTOR BURNED UP CAUSING SMOKE OUT OF EXHAU ST DUCT. NO SMOKE REPORTED IN CABIN. MAINTENANCE OPENED DMI 07407, MEL 21-10 AND DEACTIVATED SYSTEM. MAINTENANCE CLOSE D DMI 07407 ON 8-25-96 BY REMOVING AND REPLACING FREON MOTOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996101000750 19961010 00750 EU 1996 10 10 VTZA96322 1 19960822 A 5270 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGGAGE DOOR DIRTY A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 303UE 41015 FLT 6416 - PVD-IAD - ABORTED TAKEOFF DUE TO BAGGAGE DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO F URTHER INCIDENTS. MAINTENANCE OPENED DMI 03932 MEL 52-3. MAINTENANCE CLOSED DMI 03932 ON 08-24-96 BY CLEANING AND LUBI NG MICROSWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1996101000751 19961010 00751 EU 1996 10 10 VTZA96350 1 19960903 A 7930 CONNECTOR BAG JETSTM JETSTM3201 1500217 EU OIL COOLER LOOSE A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 483UE 898 FLT 6373 - SYN-IAD - DURING CLIMB, MADE AN UNSCHEDULED LANDING BACK TO SYN, DUE TO OIL COOLER CAPTION ILLUMINATED. MAIN TENANCE RESECURED CANNON PLUG ON OIL COOLER, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. ( M) 2 L 7 2 4T RT A56EU 1996101000752 19961010 00752 EU 1996 10 10 VTZA96352 1 19960907 A 7712 8953804 TTL VALVE BAG JETSTM JETSTM3201 1500217 EU LT ENGINE DIRTY A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 27 481UE 895 FLT 6182 - IAD-SCY - ABORTED TAKEOFF, DUE TO LEFT ENGINE TTL LIGHT ILLUMINATED. MAINTENANCE CLEANED WATER AND OIL FROM CANNON PLUG, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996101000753 19961010 00753 EU 1996 10 10 VTZA96353 1 19960906 A 7712 8953804 TTL VALVE BAG JETSTM JETSTM3101 1500215 EU LT ENGINE DIRTY A VTZA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 27 473UE 828 FLT 6435 - IAD-RDU - ABORTED TAKEOFF DUE TO BOTH RIGHT AND LEFT ENGINE NOT MAKING REQUIRED TAKEOFF TORQUE. MAINTENANCE CLEANED WATER AND OIL FROM TTL CANNON PLUG, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M ) 2 L 7 2 4T RT A21EU 1996101000754 19961010 00754 EU 1996 10 10 VTZA96354 1 19960906 A 5270 91SE13 SWITCH BAG JETSTM JETSTM3201 1500217 EU PAX DOOR OUT OF ADJUST A VTZA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 27 470UE 814 FLT 6218 - IAD-ELM - ABORTED TAKEOFF, DUE TO PAX DOOR WARNING LIGHT ILLUMINATED ON TAKEOFF ROLL. AIRCRAFT RETURNED TO G ATE WITH NO FURTHER INCIDENT. MAINTENANCE ADJUSTED DOOR HANDLE MICROSWITCH, OPS CHECK OK. AIRCRAFT WAS RELEASED AND AP PROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996101000755 19961010 00755 EU 1996 10 10 VTZA96355 1 19960906 A 2611 72111211000 SMOKE DETECTOR BAG JETSTM JETSTM3201 1500217 EU BAGGAGE MALFUNCTIONED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 487UE 906 FLT 6473 - JFK-IAD - DURING CLIMB, MADE A UNSCHEDULED LANDING AT JFK, DUE TO BAGGAGE SMOKE DETECTOR LIGHT ILLUMINATED. A IRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED SMOKE DETECTOR, OPS CHECK OK. AIRC RAFT WAS RLEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996101000756 19961010 00756 1996 10 10 VTZA96357 4 19960906 A 3416 066306202 ALTIMETER BAG JETSTM JETSTM3201 1500217 EU LT COCKPIT FAILED A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 482UE 897 FLT 6370 - IAD-HPN - DURING CLIMB, MADE A UNSCHEDULED LANDING, DUE TO NR 1 ALTIMETER FAILED 400 FEET OFF GROUND. AIRCRA FT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED ALTIMETER. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996101000757 19961010 00757 EU 1996 10 10 VTZA96358 1 19960906 A 7712 31024762 TQ SIGNAL COND BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 27 494UE 810 FLT NR 6339 - IAD-EWR - ABORTED TAKEOFF, DUE TO LEFT ENGINE WOULD NOT MAKE TAKEOFF TORQUE, ALSO OIL TEMP AND PRESSURE FL UCTUATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED TORQUE SIGNAL CONDITIO NER, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996101000758 19961010 00758 EU 1996 10 10 VTZA96360 1 19960907 A 3240 141R0439 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU EMER BRAKE OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 27 327UE 41080 FLT NR 6537 - IAD-RIC - ABORTED TAKEOFF DUE TO TAKEOFF CONFIGURATION WARNING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED EMERGENCY BRAKE MICROSWITCH. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RE TURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996101000759 19961010 00759 EU 1996 10 10 VTZA96368 4 19960908 A 6122 PROP GOV JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 301UE 41012 FLT 6920 - BOS-IAD - ABORTED TAKEOFF, DUE TO LEFT ENGINE RPM 102 PERCENT, TORQUE SLOW TO COME UP. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED ENG MAX PROP SPEED, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPRO VED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996101000760 19961010 00760 EU 1996 10 10 VTZA96370 1 19960910 A 7603 14176003 ENG CONTL JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT FOD A VTZA K NONE X ENGINE FLAMEOUT AP APPROACH 1 EA 27 301UE 41012 FLT 6199 - BDL-IAD - DURING APPROACH, LANDED WITH ONE DISCREPANCY DUE TO RIGHT ENGINE FLAME OUT. AIRCRAFT WENT TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE FOUND FOD ON CAM FOR FUEL SHUTOFF MICROSWITCH. OPS CHECK OK. QA HAS OPENED A F CD TO INSPECT BOTH FLEETS FOR FOD IN CONDITION LEVERS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996101000761 19961010 00761 1996 10 10 VTZA96371 4 19960910 A 3425 7003360948 AHRS COMP JETAIR JETSTM JETSTM4101 1500501 EU NR 2 FAILED A VTZA O OTHER J WARNING INDICATION CR CRUISE 1 EA 27 320UE 41043 FLT 6447 - DAY-IAD - DURING CRUISE, LANDED AT IAD WITH ONE DISCREPANCY WHICH WAS THE NR 2 AHRS FAILED IN FLIGHT. MAINTE NANCE REMOVED AND REPLACED NR 2 AHRS UNIT. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996101000762 19961010 00762 EU 1996 10 10 VTZA96372 1 19960911 A 2435 23079009 STARTER/GEN BAG JETSTM JETSTM3201 1500217 EU RT ENGINE MALFUNCTIONED A VTZA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 EA 27 477UE 890 FLT 6555 - EWR-IAD - DURING CLIMB, MADE AN UNSCHEDULED LANDING, DUE TO RIGHT GENERATOR FAILED AFTER TAKEOFF. AIRCRAFT R ETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE INSPECTED WIRES AND CONNECTIONS, STARTER/GENERATOR REMAINED ON L INE WITH A LOAD AND NO AMP SPLIT. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996101000763 19961010 00763 EU 1996 10 10 VTZA96373 1 19960912 A 3150 TO WARNING JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT ACTIVATED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 325UE 41063 FLT 6543 - EWR-IAD - ABORTED TAKEOFF DUE TO TAKEOFF CONFIGURATION WARNING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PR OBLEMS. MAINTENANCE INSPECTED SYSTEM, NO DEFECTS NOTED. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996101000764 19961010 00764 EU 1996 10 10 VTZA96374 1 19960914 A 5270 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGGAGE DOOR OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 307UE 41021 FLT 6157 - BOS-IAD - ABORTED TAKEOFF DUE TO BAGGAGE DOOR LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER P ROBLEMS. MAINTENANCE OPENED DMI 41017, MEL 52-3. MAINTENANCE CLOSED DMI 41017 BY ADJUSTING MICROSWITCH. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996101000765 19961010 00765 EU 1996 10 10 VTZA96375 2 19960913 A 7320 31058691 PROBE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE RIGHT.IEC FAILED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 302UE 41013 FLT 6267 - IAD - BTV - DURING CRUISE AN UNSCHEDULED LANDING DUE TO RIGHT IEC FAULT. AIRCRAFT RETURNED TO GATE WITH NO F URTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED AIR RETURN DELTA P/P, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROV ED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 4 T RT A41NM E18NE 1996101000766 19961010 00766 EU 1996 10 10 VTZA96376 1 19960914 A 3210 AIR830900 LANDING GEAR JETAIR JETSTM JETSTM4101 1500501 EU RT MLG FAILED A VTZA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 27 327UE 41080 FLT 6525 - JFK-ROC - ABORTED TAKEOFF DUE TO ANTI-SKID LIGHT AND RIGHT TIRE OFF RIM. AIRCRAFT RETURNED TO GATE WITH NO F URTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED RIGHT MAIN LANDING GEAR, OPS CHECK OK. AIRCRAFT WAS RELEASED AND AP PROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996101000767 19961010 00767 SW 1996 10 10 HEEA967789 1 19960909 A 6710 206001058001 TUBE ASSY BELL 206 206L1 1182107 SW M/R CONTROL CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3904L 45597 PART IS CORRODED. (CORROSION OCCURING UNDER NYLATRON SLEEVES ON ENDS WHERE BONDING STARTS. REPLACED WITH SERVICEABLE TU BE. 1 G 7 1 3U H2SW 1996101000768 19961010 00768 1996 10 10 HEEA967804 4 19960909 A 3452 066106200 TRANSPONDER KT76 BOLKMS 105 BO105S 5626006 EU COCKPIT ATC MALFUNCTION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 135AE S838 TRANSPONDER WORKS INTERMITTENTLY. FOUND MAXIMUM POWER OUT TO BE APPROXIMATELY 20 WATTS. REPLACED CAVITY TUBE V101. REP AIRED. ADJUSTED FREQUENCY. COOKED UNIT UNDER HEAT LAMP, VIBRATED AND PUT IN FREEZER. BENCH CHECK GOOD. 1 G 7 2 3U H3EU 1996101000769 19961010 00769 EU 1996 10 10 HEEA967805 1 19960909 A 7810 1176513502 EJECTOR DUCT BOLKMS 117 BK117A3 5626015 EU BUMPER PADS DAMAGED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 911NC 7026 DAMAGE DONE TO EJECTORS. FROM BUMPER PADS THAT ARE MOUNTED TO ENG. COWLING AND AIRFRAME. BUMPER PADS ARE RUBBING HARD ON EXHAUST STACK (EJECTOR) CAUSING WORN AREAS IN FOUR SPOTS. REMOVED DAMAGED AREAS, MANUFACTURER DOUBLERS USING TITANIUM MIL-T9046 TYPE 1 COMP B AMS4901 USING MAINT MANUAL MBB-BK-117 AND AC 43.13-1A. 1 G 7 2 3U H13EU 1996101000770 19961010 00770 EU 1996 10 10 HEEA967806 1 19960909 A 6240 10594575 TRANSMITTER BOLKMS 105 BO105S 5626006 EU MAST MOMENT WONT CALIB E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 721MB S752 INDICATOR WILL NOT CALIBRATE. TIME SINCE REPAIR 163:30. 1 G 7 2 3U H3EU 1996101000771 19961010 00771 EU 1996 10 10 HEEA967807 1 19960909 A 6240 10594565 INDICATOR BOLKMS 105 BO105S 5626006 EU MAST MOMENT WONT CALIB E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 721MB S752 TRANSMITTER CAUSES INDICATOR NOT TO CALIBRATE. TIME SINCE REPAIR 163:30. 1 G 7 2 3U H3EU 1996101000772 19961010 00772 NE 1996 10 10 HEEA967808 1 19960909 A 6210 7615009100051A BLADE SKRSKY S76 S76A 8143006 NE M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545K 8458 760047 BLADE IS CRACKED. (BLADE HAS CRACKS IN THE TITANIUM LEADING EDGE AS STATION 167". ALONG WITH SEPARATION AND SECTION LI FTING FROM THE BLADE SURFACE. 1 G 7 2 3U H1NE 1996101000773 19961010 00773 NE 1996 10 10 HEEA967809 1 19960910 A 6210 7615009043050 TIP CAP SKRSKY S76 S76A 8143006 NE M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545K 760047 TIP CAP IS CRACKED. (TIP CAP HAS THE ABRASION STRIP CRACKED AND SEPARATED. 1 G 7 2 3U H1NE 1996101000774 19961010 00774 1996 10 10 HEEA967810 4 19960910 A 3444 066304400 INDICATOR SKRSKY S76 S76A 8143006 NE RADAR ALT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1546K 760082 UNABLE TO ROTATE DECISION HEIGHT NEEDLE FULL SWING AND LOOSE GLASS. FOUND GLASS PUSHED IN AND CLAMP WHICH HOLDS GLASS DO WN TO BE BROKEN. REPLACED CLAMP. REPAIRED. FOUND FLAG TO GET STUCK WHEN PRESSING SELF-TEST. RE-POSITIONED RETAINER O N FLAG ASSY. FOUND SHIELD TO BE STOPPING FLAG FROM MOVING. 1 G 7 2 3U H1NE 1996101000775 19961010 00775 1996 10 10 HEEA967811 4 19960910 A 3444 066104800 ALTIMETER KRA405 SKRSKY S76 S76A 8143006 NE COCKPIT RAD ALT INTERMITTENT E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 707AE 760276 INDICATION INTERMITTENT. REPLACED RESISTOR R518,R519,R534 AND R260 TO INCORPORATE MOD 10 AS PER KING SERVICE BULLETIN KR A405-10. BENCH CHECK GOOD. 1 G 7 2 3U H1NE 1996101000776 19961010 00776 1996 10 10 HEEA967812 4 19960910 A 2312 064101500 TRANSCEIVER KTR953 BELL 214 214ST 1182106 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 8045T 28101 REMOVED SERVICEABLE. PERFORMED INSPECTION, CLEANED CORROSION FROM UNIT. FOUND RECEIVER SENSITIVITY WEAK IN AM MODE. SE NT TO ALLIED SIGNAL AVIONICS FOR INSPECTION AND REPAIR. 2 G 7 2 4U H10SW 1996101000778 19961010 00778 GL 1996 10 10 HEEA967814 2 19960910 A 7532 23005366 BLEED VALVE BELL 407 407 SW ALLSN 250C 250C* GL ENGINE DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 407PH 347 53003 CAE847006 LOW POWER CHECKS AND ENGINE TORQUE FLUCTUATIONS. REPLACED WITH SERVICEABLE BLEED VALVE. 1 G 7 1 3U 3 U O H2SW E4CE 1996101000780 19961010 00780 EU 1996 10 10 HEEA967816 1 19960910 A 3340 356H2802 POWER SUPPLY SNIAS 350 AS350B2 8680813 EU STROBE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 2771 LIGHT WOULD NOT FLASH. REPLACED WITH SERVICEABLE POWER SUPPLY. 1 G 7 1 3U H9EU 1996101000781 19961010 00781 1996 10 10 HEEA967817 4 19960910 A 3422 206075606103 GYRO SNIAS 350 AS350B2 8680813 EU COCKPIT DG DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 6100R 2862 GYRO PRECESSES 6 DEGREES ON EAST HEADING IN 10 MINUTES. 1 G 7 1 3U H9EU 1996101000782 19961010 00782 EU 1996 10 10 HEEA967818 1 19960910 A 3340 356H2802 POWER SUPPLY SNIAS 350 AS350B2 8680813 EU STROBE DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 2771 BULB INOPERATIVE. REPLACED WITH SERVICEABLE BULB. 1 G 7 1 3U H9EU 1996101000783 19961010 00783 EU 1996 10 10 HEEA967819 1 19960910 A 2841 VT4261 INDICATOR BOLKMS 105 BO105S 5626006 EU FUEL SYS FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 81832 S828 INDICATOR NEEDLE ON SUPPLY SIDE WILL NOT GO TO ZERO. 1 G 7 2 3U H3EU 1996101000784 19961010 00784 GL 1996 10 10 HEEA967820 2 19960912 A 7230 23007208 DIFFUSER VANE 23033191 BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL ENGINE WELD BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1073W CAC70394 45386 CAE860771 UPON INSTALLATION OF VANE NOTED: TWO STUD WELDS BROKEN AS MARKED DURING TORQUE. REPLACED DISCREPANT PART. 1 G 7 1 3U 3 U H2SW E1GL 1996101000785 19961010 00785 EU 1996 10 10 HEEA967821 1 19960912 A 2435 150SG122Q STARTER SNIAS 350 AS350B2 8680813 EU ENG START/GEN FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 6100U 2863 WHEN UNIT IS HOT WILL NOT CRANK. WHEN UNIT DOES NOT CRANK, IT MAKES ARCHING NOISES. 1 G 7 1 3U H9EU 1996101000786 19961010 00786 EU 1996 10 10 HEEA967822 1 19960912 A 7712 30571365 INDICATOR SNIAS 350 AS350B2 8680813 EU ENG TORQUE FLUCTUATION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 4000L 326 2873 TORQUE FLUCTUATION, INTERMITTENT HIGH SIDE. 1 G 7 1 3U H9EU 1996101000787 19961010 00787 EU 1996 10 10 HEEA967823 1 19960912 A 6220 ELT302301 FREQ ADAOTER SNIAS 350 AS350B2 8680813 EU M/R CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6097Z 1911 2820 FREQ ADAPTER IS CORRODED. (SEPARATION AND CORROSION) SERIAL NUMBERS REMOVED 7590, 7591 AND 7593. 1 G 7 1 3U H9EU 1996101000788 19961010 00788 EU 1996 10 10 HEEA967824 1 19960912 A 6220 117775P STARFLEX SNIAS 350 AS350B2 8680813 EU M/R CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6097Z 1911 2820 BALL JOINT SEAL CAME OUT. SCRAPPED LOCALLY. 1 G 7 1 3U H9EU 1996101000789 19961010 00789 EU 1996 10 10 HEEA967825 1 19960912 A 6220 350A31190703 STARFLEX SNIAS 350 AS350B2 8680813 EU M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100R 1435 2862 STARFLEX IS CRACKED. 1 G 7 1 3U H9EU 1996101000790 19961010 00790 EU 1996 10 10 HEEA967826 1 19960912 A 3340 356H2802 POWER SUPPLY SNIAS 350 AS350B2 8680813 EU STROBE FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 60951 2771 STROBE DOES NOT FLASH. 1 G 7 1 3U H9EU 1996101000791 19961010 00791 EU 1996 10 10 HEEA967829 1 19960912 A 6330 704A33633109 BEARING SNIAS 350 AS350B2 8680813 EU M/R XMSN WORN EXCESSIVELY E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6097Z 1911 2820 BEARING IS WORN EXCESSIVELY. SERIAL NUMBERS REMOVED 7824, 7825 AND 7826. 1 G 7 1 3U H9EU 1996101000792 19961010 00792 EU 1996 10 10 HEEA967830 1 19960912 A 7722 56375600010 INDICATOR SNIAS 350 AS350B2 8680813 EU COCKPIT T4 STICKS E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 4000L 359 2873 STICKS INTERMITTENTLY ON ZERO. 1 G 7 1 3U H9EU 1996101000793 19961010 00793 1996 10 10 HEEA967831 4 19960912 A 3120 B1894522282A CLOCK SNIAS 350 AS350B2 8680813 EU COCKPIT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 350BZ 1844 2653 CLOCK WOUND UP AND WON'T RUN. 1 G 7 1 3U H9EU 1996101000794 19961010 00794 EU 1996 10 10 HEEA967832 1 19960912 A 2510 AFG0348056 INERTIA SPRING SNIAS 350 AS350B2 8680813 EU HARNESS BROKEN E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 6100U 1366 2863 HARNESS SPRING IS BROKEN. 1 G 7 1 3U H9EU 1996101000795 19961010 00795 EU 1996 10 10 HEEA967833 1 19960912 A 2822 P94B12209 PUMP SNIAS 350 AS350B2 8680813 EU FUEL BOOST INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 60951 1918 2771 PUMP INOPERATIVE. 1 G 7 1 3U H9EU 1996101000796 19961010 00796 EU 1996 10 10 HEEA967834 1 19960912 A 7910 703A53000010 OIL TANK SNIAS 350 AS350B2 8680813 EU SIGHT GLASS CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 3400 2771 OIL TANK IS CRACKED. (SIGHT GLASS CRACKED) 1 G 7 1 3U H9EU 1996101000797 19961010 00797 NE 1996 10 10 HEEA967981 2 19960930 A 7310 430123604 MANIFOLD BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE ENG FUEL CRACKED E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 911NC 1094 7026 LE45074AE ENGINE LEAK CHECK REVEALED: FUEL LEAKING FROM FUEL MANIFOLD TUBING. REPLACED DISCREPANT PART. 1 G 7 2 3U 3 U H13EU E5NE 1996101000798 19961010 00798 GL 1996 10 10 HEEA967982 2 19960930 A 7250 23053335 NOZZLE 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL NR 2 VANE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5031U 1151 CAT31642F S678 CAE820845F TURBINE REMOVED DUE TO CYCLES. UPON INSPECTION OF TURBINE PARTS NOTED: CRACKED BEYOND SERVICEABLE LIMITS ON #2 NOZZLE VANES AND DIAPRAGM. 1 G 7 2 3U 3 U H3EU E4CE 1996101000799 19961010 00799 SW 1996 10 10 HEEA967991 1 19961001 A 7931 407375004101 INDICATOR BELL 407 407 SW ENG OIL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 141MA 28 53016 ENGINE OIL PRESSURE FAILED. RECEIVED AIRCRAFT WITH WRITE UP THAT INDICATOR FAILED. 1 G 7 1 3U O H2SW 1996101000800 19961010 00800 SW 1996 10 10 HEEA967992 1 19961001 A 6320 407375005101 INDICATOR BELL 407 407 SW XMSN OIL TEMP MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407PH 521 53003 TRANSMISSION OIL TEMPERATURE WILL FALL OFF LINE INTERMITTENTLY. MECHANICS GO TO AIRCRAFT AND WILL CHECK AND FIND TEMPER ATURE IS INDICATING NORMALLY. 1 G 7 1 3U O H2SW 1996101000801 19961010 00801 SW 1996 10 10 HEEA967994 1 19961001 A 6500 204040623003 BEARING BELL 212 212 1181420 SW T/R DRIVE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5010F 58 30936 DUST SHIELD SPINNING. 1 G 7 1 4U H4SW 1996101000802 19961010 00802 SW 1996 10 10 HEEA967995 1 19961001 A 6500 204040623003 BEARING BELL 212 212 1181420 SW T/R DRIVE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5010F 58 30936 DUST SHIELD SPINNING. REPLACEMENT PART PURCHASED AS PER ASB212-95-95 REV. B. 1 G 7 1 4U H4SW 1996101000803 19961010 00803 SW 1996 10 10 HEEA967996 1 19961001 A 6500 204040623003 BEARING BELL 212 212 1181420 SW T/R DRIVE FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5010F 58 30936 DUST SHIELD SPINNING. REPLACEMENT PART PURCHASED AS PER ASB212-95-95 REV. B. 1 G 7 1 4U H4SW 1996101000804 19961010 00804 1996 10 10 HEEA967997 4 19961002 A 3451 6221233001 DME40 SKRSKY S76 S76A 8143006 NE COCKPIT INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 792CH 760193 DME INOPERATIVE. 1 G 7 2 3U H1NE 1996101000805 19961010 00805 SW 1996 10 10 HEEA967998 1 19961002 A 2422 412075101101 INVERTER BELL 412 412 1182202 SW AC SYS MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22608 33075 FUEL QUANTITY FLUCTUATES. TIME SINCE REPAIR 214:55. 1 G 7 2 4U H4SW 1996101000806 19961010 00806 EU 1996 10 10 HEEA967999 1 19961002 A 7714 614764021 INDICATOR SNIAS 350 AS350B2 8680813 EU COCKPIT TACH READS LOW E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 350BZ 1626 2653 INDICATOR INTERMITTENTLY READS LOW. 1 G 7 1 3U H9EU 1996101000807 19961010 00807 NM 1996 10 10 CALA9601403 1 19960908 A 5320 SUPPORT BOEING 727 727224 1384076 NM BS 480 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 20665 INSPECTION FOUND FORWARD CARGO COMPARTMENT FLOORBOARD SUPPORT CRACKED AT STA 480. THE CRACKED AREA WAS CUT OUT, A FILLE R AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3. 2 L 7 3 4F A3WE 1996101000808 19961010 00808 NM 1996 10 10 CALA9601404 1 19960908 A 5320 ANGLE BOEING 727 727224 1384076 NM BS 480 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 20665 INSPECTION FOUND LOWER ANGLE OF FORWARD CARGO FORWARD BULKHEAD PANEL CRACKED AT STA 480 ABOVE STRINGER 27. THE ANGLE WA S REMOVED AND THE CRACK WAS STOP DRILLED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND THE ANGLE WAS REINST ALLED. 2 L 7 3 4F A3WE 1996101000809 19961010 00809 NM 1996 10 10 CALA9601405 1 19960909 A 5313 STRINGER BOEING 727 727224 1384076 NM BS 580 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 20665 INSPECTION FOUND STRINGER 26L IN FORWARD CARGO COMPARTMENT CORRODED AT STA 580. THE CORROSION WAS REMOVED AND THE STRIN GER WAS REPAIRED IAW SRM 53-10-3. 2 L 7 3 4F A3WE 1996101000810 19961010 00810 NM 1996 10 10 CALA9601406 1 19960909 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM BS 1110 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 20665 INSPECTION FOUND AFT CARGO COMPARTMENT FLOORBEAM CORRODED AT STA 1110, RBL 16 TO RBL 52. THE CORROSION WAS REMOVED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8. 2 L 7 3 4F A3WE 1996101000811 19961010 00811 NM 1996 10 10 CALA9601407 1 19960909 A 5320 SUPPORT BOEING 727 727224 1384076 NM BS 480-720D CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 20665 INSPECTION FOUND FLOORBOARD SUPPORT CORRODED ON UPPER AND LOWER SURFACES IN FORWARD CARGO COMPARTMENT ABOVE STRINGER 26R FROM STA 480-720D. THE FLOOR SUPPORT WAS REMOVED AND THE CORROSION WAS CLEANED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-6, 51-10-1, 51-30-2 AND 51-10-2. 2 L 7 3 4F A3WE 1996101000812 19961010 00812 NM 1996 10 10 CALA9601408 1 19960909 A 5320 SUPPORT BOEING 727 727224 1384076 NM BS 480-720 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 20665 INSPECTION FOUND FLOORBOARD SUPPORT CORRODED ON UPPER AND LOWER SURFACES IN FORWARD CARGO COMPARTMENT ABOVE STRINGER 26L FROM STA 480 TO 720D. THE CORROSION WAS REMOVED, REPLACEMENT SECTIONS WERE FABRICATED AND INSTALLED IAW SRM 51-40-5, 5 1-10-0, 51-10-2 AND 51-10-6. 2 L 7 3 4F A3WE 1996101000813 19961010 00813 NM 1996 10 10 CALA9601409 1 19960909 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM BS 1068 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 20665 INSPECTION FOUND CORROSION ON CABIN FLOORBEAM AT STA 1068, RBL 48. THE FLOORBEAM WAS REMOVED AND A NEW PART WAS FABRICA TED AND INSTALLED IAW SRM 51-30-1. 2 L 7 3 4F A3WE 1996101000814 19961010 00814 NM 1996 10 10 CALA9601410 1 19960918 A 5330 SKIN BOEING 727 727224 1384076 NM BS 480-500 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 20665 INSPECTION FOUND CORROSION ON SKIN UNDER STRINGER 28L BETWEEN STA 480 AND 500. THE CORRODED AREA WAS CUT OUT, REPAIR DO UBLER AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 51-10-2, 53-30-2 AND 53-30-3. 2 L 7 3 4F A3WE 1996101000815 19961010 00815 NM 1996 10 10 CALA9601411 1 19960918 A 5320 ANGLE BOEING 727 727224 1384076 NM BS 620-630 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 20665 INSPECTION FOUND CORROSION ON BOTTOM SIDE OF SPLICE ANGLE ABOVE STRINGER 27R AT STA 620 TO 630. THE OLD SPLICE WAS REMO VED AND A NEW SPLICE WAS FABRICATED AND INSTALLED IAW SRM 51-40-4 AND 51-10-2. 2 L 7 3 4F A3WE 1996101000816 19961010 00816 NM 1996 10 10 CALA9601412 1 19960910 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM BS 344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 20665 INSPECTION FOUND FORWARD FLANGE OF FLOORBEAM AT STA 344 AND LBL 21 CORRODED. THE FLANGE WAS REMOVED AND A NEW FLANGE WA S FABRICATED AND INSTALLED IAW SRM 53-10-8. 2 L 7 3 4F A3WE 1996101000817 19961010 00817 NM 1996 10 10 CALA9601413 1 19960910 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM BS 344 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 20665 INSPECTION FOUND A 1 INCH CRACK THROUGH NUTPLATE HOLE ON TOP AFT FLANGE OF STA 344 FLOORBEAM AT LBL 26. THE UPPER FLANG E WAS CUT OFF AND A REPLACEMENT FLANGE WAS INSTALLED IAW SRM 53-10-8. 2 L 7 3 4F A3WE 1996101000818 19961010 00818 NM 1996 10 10 CALA9601414 1 19960910 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM BS 344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 20665 INSPECTION FOUND CORROSION AT NUTPLATE HOLES OF FLOORBEAM FLANGE AT STA 344, LBL 40. THE FLANGE WAS CUT OFF AND REPLACE D IAW SRM 53-10-8. 2 L 7 3 4F A3WE 1996101000819 19961010 00819 NM 1996 10 10 CALA9601415 1 19960911 A 5320 SUB FLOOR BOEING 727 727224 1384076 NM BS 1134-1140 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 20665 INSPECTION FOUND RT AFT LAV SUBFLOOR CORRODED AT STA 1134 TO 1140, RBL 19. THE CORROSION WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1996101000820 19961010 00820 NM 1996 10 10 CALA9601416 1 19960911 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM BS 1070 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 20665 INSPECTION FOUND FLOORBEAM CORRODED AT STA 1070, RBL 48 TO 57. THE CORROSION WAS REMOVED AND A REPAIR WAS FABRICATED AN D INSTALLED IAW SRM 53-10-8. 2 L 7 3 4F A3WE 1996101000821 19961010 00821 NM 1996 10 10 CALA9601417 1 19960911 A 5320 ANGLE BOEING 727 727224 1384076 NM BS 760.95 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 20665 INSPECTION FOUND A 2.25 INCH CRACK ON INBOARD FLANGE, JUST BELOW CABIN FLOORBOARD ATTACH ANGLE, OF LEFT FRAME AT BS 760. 95. THE AREA WAS REPAIRED IAW BOEING DRAWING NR 65C36279-1. 2 L 7 3 4F A3WE 1996101000822 19961010 00822 NM 1996 10 10 CALA9601418 1 19960907 A 5720 ANGLE BOEING 727 727224 1384076 NM WS 338 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 20665 INSPECTION FOUND A 1.5 INCH CRACK IN UPPER ANGLE JUST FORWARD OF FRONT SPAR AT LT WING LEADING EDGE RIB, STA 338. THE A NGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3. 2 L 7 3 4F A3WE 1996101000823 19961010 00823 NM 1996 10 10 CALA9601419 1 19960909 A 5720 WEB BOEING 727 727224 1384076 NM LT WING TIP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 20665 INSPECTION FOUND LATERAL WEB CRACKED AT UPPER AND LOWER RADIUS INSIDE LEFT WING TIP, FORWARD OF FLUX VALVE COMPARTMENT. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-40-5. 2 L 7 3 4F A3WE 1996101000824 19961010 00824 NM 1996 10 10 CALA9601420 1 19960911 A 5713 STRINGER BOEING 727 727224 1384076 NM BS 686.50 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 20665 INSPECTION FOUND LT WING FUEL TANK STRINGER CRACKED AT STA 686.50. THE CRACK WAS STOP DRILLED, A REPAIR WAS FABRICATED AND INSTALLED IAW EA 5762-01050. 2 L 7 3 4F A3WE 1996101000825 19961010 00825 NM 1996 10 10 CALA9601421 1 19960919 A 5754 RIB BOEING 727 727224 1384076 NM NR 3 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 20665 INSPECTION FOUND NR 3 LEADING EDGE SLAT INBOARD END CLOSURE RIB CRACKED. THE RIB WAS REMOVED AND REPLACED IAW SRM 51-30 -2. 2 L 7 3 4F A3WE 1996101000826 19961010 00826 NM 1996 10 10 CALA9601422 1 19960911 A 5320 656097122 SUPPORT BOEING 727 727224 1384076 NM BS 1130-1142 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 20665 FLOOR SUPPORT AND INTERCOSTAL CORRODED AT STATION 1130 TO 1142 RBL 12 TO 16. REMOVED AND REPLACED FLOOR SUPPORT AND INT ERCOSTAL IAW SRM 51-10-1 AND 51-10-2. 2 L 7 3 4F A3WE 1996101000827 19961010 00827 NM 1996 10 10 9621132287 1 19961007 A 2421 GENERATOR BOEING 727 727251 138408H NM NR 1 MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J H WARNING INDICATION ELECT. POWER LOSS-50 PC TO TAKEOFF 1 GL 01 287US 21375 WITH TAKEOFF POWER BEING APPLIED, THE NR 1 GENERATOR DROPPED OFF LINE. TAKEOFF WAS ABORTED WITHOUT INCIDENT AND AIRCRAF T RETURNED TO GATE. CSD OIL LEVEL WAS CHECKED AND FOUND TO BE OK. CSD WAS DEACTIVATED AND THE NR 1 GENERATOR WAS PLACE D ON MEL. 2 L 7 3 4F A3WE 1996101000828 19961010 00828 NM 1996 10 10 96FDEA01567 1 19961008 A 5720 64833350 STIFFENER BOEING 727 72725 1384006 NM BS 740 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 511FE 18283 NR0510 AND 017, TOP OF THE VERTICAL STIFFENER IS CRACKED IN THE WING CENTER SECTION AT BS 740 RBL 45. *S/D* REMOVED AN D REPLACED VERTICAL STIFFENER IN THE WING CENTER SECTION AT BS 740 RBL 45 IAW FEDEX SRM 51-30-2. 2 L 7 3 4F A3WE 1996101000829 19961010 00829 WP 1996 10 10 96FDEA01568 1 19961008 A 5720 ARB00291 STRAP DOUG DC10 DC1030 3023501 WP LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 301FE 46800 SNRM 00181, LEFT O/B T/E FLAP I/B HINGE O/B SIDE AT REAR SPAR TENSION STRAP IS CRACKED AT BOTTOM FLANGE. *S/D* COMPLIE D WITH EA 8-5710-31702, INSTALLED NEW PART PER SRM 53-00-01. 2 L 7 3 4F A22WE 1996101000830 19961010 00830 WP 1996 10 10 96FDEA01569 1 19961008 A 5720 ARB00292 STRAP DOUG DC10 DC1030 3023501 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 301FE 46800 SNRM 00182, RIGHT O/B FLAP I/B HINGE O/B SIDE AT REAR TENSION STRAP IS CRACKED AT BOTTOM FLANGE. *S/D* COMPLIED WITH E A 8-5710-31702, INSTALLED NEW PART PER SRM 53-00-01. 2 L 7 3 4F A22WE 1996101000831 19961010 00831 NM 1996 10 10 96FDEA01570 1 19961008 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 1110 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 281FE 19201 MAIN CARGO CORROSION ON FLOORBEAM AT STA 1110 FROM 10 TO 24 LBL. REMOVED CORROSION PER SRM 51-10-6. ALL WITHIN TOLERA NCE PER SRM 53-10-1 EXCEPT FOR AREA AT LBL 20 CENTER OF F/B WHICH IS OUT OF TOLERANCE. FABRICATED DOUBLER PER AARD 53-1 0-07-2 PER AARD 53-10-07-02. 2 L 7 3 4F RT A3WE 1996101000832 19961010 00832 WP 1996 10 10 ABXA9600639 1 19961006 A 3260 189915 PROX SWITCH DOUG DC8 DC863F 302198F WP LT MLG DEFECTIVE A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 814AX 46041 AFTER GEAR RETRACTION, GREEN GEAR LIGHTS OUT. THE RED LANDING GEAR UNSAFE LIGHT WAS ILLUMINATED ALONG WITH THE LEFT DOO R NOT LATCHED ON FLIGHT ENGINEER'S PANEL. COMPLIED WITH ALL ABNORMAL PROCEDURES AND LIGHTS REMAINED ILLUMINATED. REPLA CED LEFT LANDING GEAR DOOR PROXIMITY SWITCH IAW DC-8 SUPPLEMENTAL MM 32-60-00. VISUAL INSPECTION WAS GOOD. 2 L 7 4 4F 4A25 1996101000833 19961010 00833 WP 1996 10 10 ABXA9600640 1 19961008 A 3260 INTERLOCK CABLE DOUG DC8 DC863 302198A WP RT MLG DOOR OUT OF ADJUST A ABXA O OTHER N FALSE WARNING AP APPROACH 1 GL 23 818AX 46075 RIGHT MAIN LANDING GEAR DOOR WOULD NOT SHOW LATCHED ON ARRIVAL AFTER RECYCLING GEAR UP TWICE. ADJUSTED RIGHT UPLATCH PO SITION INTERLOCK CABLE IAW MAB DC-8-32-6, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1996101000834 19961010 00834 WP 1996 10 10 ABXA9600641 1 19961006 A 3233 5759101 ATTACH BOSS DOUG DC8 DC863 302198A WP LT MLG ACTUATOR CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 DURING LINE MAINTENANCE, LEFT MAIN LANDING GEAR ATTACH PIN FOUND TO BE LOOSE. FOUND LEFT MAIN LANDING GEAR ACTUATOR ATT ACH BOSS CORRODED. REPAIRED IAW REA D832-16660-MR. 2 L 7 4 4F 4A25 1996101000835 19961010 00835 WP 1996 10 10 ABXA9600642 1 19961007 A 2510 SEAT DOUG DC8 DC863 302198A WP LT COCKPIT MALFUNCTIONED A ABXA O OTHER O OTHER CL CLIMB 1 GL 23 820AX 46155 LEFT SIDE OF CAPTAIN'S SEAT DROPPED DOWN RIGHT AFTER ROTATION AND HAD TO BE LIFTED BACK UP TO GET IT TO LOCK IN POSITION . CAPTAIN'S SEAT OPS CHECKED GOOD IAW DC-8 MM. 2 L 7 4 4F 4A25 1996101000836 19961010 00836 WP 1996 10 10 ABXA9600643 1 19961007 A 7931 318100 TRANSMITTER DOUG DC8 DC861F 3021953 WP PWA JT3D JT3D3B 52039 NE NR 3 ENGINE DEFECTIVE A ABXA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 23 849AX 828 45891 669610 NR 3 OIL PRESSURE FLUCTUATES BETWEEN 46 AND 51 PSI WITH CRUISE POWER SET. FLUCTUATION STOPS AS THROTTLE IS RETARDED TO IDLE IN DESCENT BUT FLUCTUATION BEGINS AS POWER IS APPLIED. AT INTERMEDIATE LEVEL OFF OIL TEMP WAS 45 DEGREES CELSIUS, OIL QUANTITY 8.9 GALLLONS. WINDMILLING OIL PRESSURE 16 PSI ENGINE SHUTDOWN IN FLIGHT. REPLACED NR 3 OIL PRESSURE TRANS MITTER, INSPECTED OIL SCREEN AND OIL SCREEN WAS CLEAN. PERFORMED GROUND RUN, AT ALL POWER SETTINGS SYSTEM CHECKED GOOD WITH NO FLUCTUATION. ALL IAW DC-8 MM AND PRATT AND WHITNEY JT3D MM 72-0. 2 L 7 4 4F 4 F 4A25 1E8 1996101000837 19961010 00837 NM 1996 10 10 SCNA96286 1 19961004 A 3397 6579599 WIRE BOEING 727 727259 138408J NM CABIN BROKEN A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 FOUND AISLE EMERGENCY LIGHT UNSECURED AND WIRES SEVERED BETWEEN AFT SERVICE DOORS. REPAIRED EMERGENCY EXIT WIRES, RESEC URED FIXTURE AND OPS CHECKED GOOD. 2 L 7 3 4F A3WE 1996101000838 19961010 00838 NM 1996 10 10 SCNA96287 1 19961005 A 3350 900J42 POWER SUPPLY BOEING 727 727259 138408J NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 FOUND R2 DOOR OVERHEAD EMERGENCY EXIT SIGN DIM. REMOVED AND REPLACED BATTERY PACK AND POWER SUPPLY IN ACCORDANCE WITH M M 33-50-91, SYSTEM OPS CHECKED GOOD. 2 L 7 3 4F A3WE 1996101000839 19961010 00839 WP 1996 10 10 RRXA96089 1 19961008 A 2612 FIRE LOOP DOUG DC8 DC871F 302199D WP NR 4 ENGINE MALFUNCTIONED A RRXA A E F UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 WP 15 8177U 45983 ON CLIMB AT 10,000 FT, NR 4 ENGINE FIRE WARNING WENT OFF. PERFORMED ENGINE FIRE AND DAMAGE CHECKLIST PER EWA QRH. DISC HARGED BOTH FIRE BOTTLES, RETURNED TO TJSJ, LANDED AT 273,000 LBS. MAINTENANCE CLEANED AND REPOSITIONED ALL FIRE LOOP C ONNECTIONS, TESTED SYSTEM IAW 26-10-0, OPS CHECKED OK. 2 L 7 4 4F RT 4A25 1996101000840 19961010 00840 NM 1996 10 10 CKSA96160 1 19961007 A 5530 6AL4V STIFFENER BOEING 727 727223 1384074 NM VERT STAB CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6808 19483 DURING B-CHECK INSPECTION, FOUND INTERNAL VERTICAL STABILIZER STA 1342, VERTICAL STIFFENER CRACKED LEFT HAND SIDE. REMO VED AND REPLACED VERTICAL STIFFENER STA 1342 IAW B727 SRM 51-10-1 AND ENGINEERING REPORT NR 96 AIA-132. TASK CARD NR 86 459 CORRSION CARD NR C55-395-11 PART 1 OF 1. 2 L 7 3 4F A3WE 1996101000841 19961010 00841 NM 1996 10 10 CKSA96161 1 19961007 A 5530 6AL4V BRACKET BOEING 727 727223 1384074 NM VERT STAB CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6808 19483 DURING B-CHECK INSPECTION, FOUND INTERNAL VERTICAL STABILIZER STA 1342 FIN REAR SPAR CHORD BRACKET CRACKED IN RADIUS APP ROXIMATELY 6 INCHES LONG LEFT HAND SIDE. REMOVED AND REPLACED PART IAW 727 SRM 51-10-1 AND ENGINEERING REPORT NR 96 AIA -132. TASK CARD NR 86458 CORROSION CARD NR C55-395-11 PART 1 OF 1. 2 L 7 3 4F A3WE 1996101000842 19961010 00842 WP 1996 10 10 TC8A96062 1 19961004 A 7711 EPR GUAGE DOUG DC8 DC8F55 3021928 WP NR 2 ENGINE MALFUNCTIONED A TC8A C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 23 808CK 45817 NR 2 ENGINE NOT PRODUCING T/O POWER, ABORTED AT 88 KNOTS. SWAPPED NR 1 AND NR 2 EPR GAUGES IAW DC-8 MM CHAPTER 77-1-0, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1996101000866 19961010 00866 CE 1996 10 10 96ZZZX5146 1 19960925 A 2613 OVERHEAT SYSTEM LEAR 60 60LEAR 5170707 CE TAIL CONE BLEED MALFUNCTION A OICA K NONE O OTHER IN INSP/MAINT 1 SW 09 399SC 1213 60040 DURING TROUBLESHOOTING FOR EXCESSIVE INSULATION MATERIAL LOOSE IN THE TAIL CONE, THE TAIL CONE BLEED AIR OVERHEAT WARNIN G WAS FOUND INOPERATIVE. THE SYSTEM TESTED NORMAL IN THE COCKPIT, BUT WOULD NOT TRIGGER WHEN HEATED IAW THE MM. INSTAL LED GROUND STRAPS PER RECOMMENDED SB 60-26-2. SYSTEM OPERATED NORMALLY. SUBMITTER STATES THIS BULLETIN NEEDS TO BE MAND ATORY, OR AN AD. 2 L 7 2 4F RT A10CE 1996101000875 19961010 00875 SW 1996 10 10 96ZZZX5155 1 19960923 A 2910 222080575101 TUBE ASSY BELL 222 222B 1182124 SW NR 2 HYD SYSTEM CRACKED A A RW8A O OTHER K FLUID LOSS CR CRUISE 1 EA 21 492CK 47145 DURING FLIGHT, TUBE ASSY CRACKED CAUSING LOSS OF NR 2 HYDRAULIC SYSTEM PRESSURE. ALSO, FOUND BROKEN WAS BRACE P/N 222-0 80-134-102 THAT SUPPORTS FILTER MANIFOLD TO WHICH TUBE ASSEMBY IS CONNECTED. 1 G 7 2 3U H9SW 1996101000876 19961010 00876 SW 1996 10 10 96ZZZX5156 1 19960923 A 2910 222080134102 BRACE BELL 222 222B 1182124 SW HYD SYS FILTER BROKEN A A RW8A K NONE O OTHER IN INSP/MAINT 1 EA 21 492CK 19 47145 BRACE, P/N 222-080-134-102, WAS FOUND BROKEN TO NR 2 SYSTEM HYDRAULIC FILTER MANIFOLD. SUBMITTER STATED BRACE MANUFACTU RING PROCEDURE NEEDS TO BE CHANGED. BRACES ALWAYS BREAK AT BEND LINE. 1 G 7 2 3U H9SW 1996101000877 19961010 00877 EU 1996 10 10 96ZZZX5157 1 19960828 A 5302 1053040212 FITTING BOLKMS 105 BO105C 5626005 EU TAIL BOOM CRACKED A EHAA K NONE O OTHER IN INSP/MAINT 1 AL 03 911MH 7106 S148 THIS FITTING IS THE FORWARD, UPPER ATTACHMENT FITTING FOR THE T/R GEARBOX. THE CRACK RAN DOWN THE LEFT SIDE BETWEEN TWO RIVET HOLES INTO THE AFT RADIUS AND UP THE BACK SIDE OF THE FITTING. SUSPECT HAPPENED FROM NOT BEING DEBURRED OR T/R V IBRATIONS. 1 G 7 2 3U H3EU 1996101000882 19961010 00882 WP 1996 10 10 CA960205013 1 19960112 A 2434 51911003 CONTROLLER LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB21122B02 54555 NE NR 3 GENERATOR FAILED W A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS G MULTIPLE FAILURE CR CRUISE 1 CA 10285 (CAN)DURING CRUISE #1 & #3 GENERATORS DROPPED OFF LINE. #2 GENERATOR INDICATED LOW FREQUENCY. #1 LOAD FREQUENCY CONTROLL ER AND GENERATOR CONTROL UNIT REPLACED. #3 GENERATOR CONTROL UNIT REPLACED. 2 L 7 3 4F 4 F A23WE E12EU 1996101000884 19961010 00884 NE 1996 10 10 CA960206102 2 19960105 A 8530 27056 PISTON DHAV DHC2 DHC2MK1 2800102 EA PWA R985 R985AN14B 52008 NE #8 CYLINDER CRACKED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA 1118 P159408 (CAN)PILOT REPORTED SMOKE IN COCKPIT AND A BIT OF OIL ON THE WINDSHIELD. AIRCRAFT RETURNED TO POINT OF DEPARTURE. POST F LIGHT INSPECTION FOUND #8 CYLINDER PISTON CRACKED AND PISTON RING BROKEN. THE PISTON WAS CRACKED FROM THE PISTON PIN HO LE TO OVER THE TOP OF THE PISTON WITH A SMALL PIECE OF THE PISTON MISSING. NEW PISTON AND RINGS INSTALLED. OIL SCREENS A ND SUMP CHECKED SERVICEABLE AND AIRCRAFT RETURNED TO SERVICE. 1 H 7 1 3R 3 R A806 5E1 1996101000885 19961010 00885 WP 1996 10 10 CA960208101 1 19960126 A 4900 38102621 APU DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE APU ENG SMOKING W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA 70174 7680 517410 (CAN)PRIOR TO DEPARTURE, APU AUTO SHUT DOWN, EMITTING CLOUDS OF SMOKE. APU WAS MEL'D AND AIRCRAFT DEPARTED. ON CLIMB, CA BIN AIR CONDITIONING SYSTEM DISCHARGED OIL VAPOURS. AIRCRAFT RETURNED TO BLOCKS AND C OMPLETED AN OVERWEIGHT LANDING. OV ERWEIGHT LANDING CHECK CARRIED OUT AND APU REPLACED. COLOESCER BAGS REPLACED AND AIR CONDITIONING PURGED. 2 L 7 3 4F 4 F A22WE E23EA 1996101000887 19961010 00887 EU 1996 10 10 CA960212001 1 19960208 A 3320 S2806102 LAMP HOLDER BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE SEAT 17AB BURNT W O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 CA LF05494A (CAN)ELECTRICAL BURNING SMELL NOTED IN CABIN DURING LAST 10 MINUTES OF DESCENT. LAMP SOCKET AT SEAT 17AB FOUND BURNED. 2 H 7 4 4F 4 F RT A49EU E6NE 1996101000888 19961010 00888 EU 1996 10 10 CA960212004 1 19960202 A 2822 PUMP AIRBUS 320 A320211 3930320 EU FUEL BOOST LOW PRESS WARN W A A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN)DURING CRUISE THE LEFT FUEL TANK BOOST PUMPS LOW PRESSURE WARNING ANNUNCIATED (BOTH PUMPS). OPENED FUEL CROSSFEED, UNABLE TO MAINTAIN FUEL BALANCE IN THIS CONFIGURATION WITH #1 AND #2 FUEL PUMPS (TANK1) STILL SELECTED ON. DIVERTED AIRC RAFT TO YXE. MAINTENANCE ACTION INVOLVED HANGARING AIRCRAFT, DRAINED FUEL SUMPS, FOUND ICE CRYSTALS IN THE FUEL. AIRCRAF T REFUELED AND RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 1996101000889 19961010 00889 EU 1996 10 10 CA960212005 1 19960125 A 3230 114079015 SELECTOR VALVE AIRBUS 320 A320211 3930320 EU MLG INOPERATIVE W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN)ON CLIMB LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO BASE. MAINTENANCE CHECK REVEALED MAIN LANDING DOORS W ERE NOT FULLY CLOSED. MAINTENANCE ACTION INVOLVED CHANGING MLG SELECTOR VALVE AS PER AMM 32-31-0. BOTH LGCIU TESTED AND GEAR SWING WAS NORMAL. 2 L 7 2 4F RT A28NM 1996101000892 19961010 00892 EU 1996 10 10 CA960212009 1 19960205 A 2842 647510033 TRANSMITTER SNIAS 350 AS350D 8680803 EU LYC FUEL QTY FLUCTUATING W K NONE O OTHER IN INSP/MAINT 1 CA (CAN)INCORRECT FUEL GAUGE READINGS AND GAUGE WOULD STICK IN ONE POSITION. 1 G 7 1 3U H9EU 1996101000893 19961010 00893 CE 1996 10 10 CA960212013 1 19960205 A 7160 9591911719 VANE BEECH 959191171 BEECH 95 E95 1153410 CE LYC O360 IO360B1B 41514 EA LT ENG ALT AIR FROZEN W A UNSCHED LANDING R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CA L496351A (CAN)DURING TAKEOFF ROLL A LEFT YAW WAS NOTICED AND ONCE AIRBORNE THE FUEL FLOW AND MANIFOLD PRESSURE ON THE LEFT ENGINE WAS NOTED TO BE LOW. THE ALTERNATE AIR CONTROL WAS NOTED IN THE HEAT POSITION. WHEN THE ALTERNATE AIR WAS RETURNED TO THE FILTER POSITION FULL POWER RETURNED. INSPECTION FOUND THE AIR BOX WAS ICED UP IN THE CLOSED POSITIION. THE VANE WAS THAWED AND THE AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 3O 3 O 3A16 1E10 1996101000894 19961010 00894 CE 1996 10 10 CA960212015 1 19960209 A 7160 9591911719 VANE BEECH 9591911719 BEECH 95 E95 1153410 CE LYC O360 IO360B1B 41514 EA LT ENG ALT AIR STUCK W K NONE R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CA L496351A (CAN)ON TAKEOFF THE LEFT HAND ENGINE WOULD NOT DEVELOP FULL POWER. INSPECTION REVEALED THE ALTERNATE AIR DOOR CABLE TO B E OUT OF RIG, CAUSING THE AFT VANE TO JAM IF THE CONTROL CABLE WAS PUSHED TOO FAR TOWARDS THE FILTER POSITION. THE ALTER NATE AIR CONTROL WAS RERIGGED, TESTED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1 L 7 2 3O 3 O 3A16 1E10 1996101000901 19961010 00901 WP 1996 10 10 CA960212023 1 19960202 A 3210 528072 TORSION ARM MENASCO 528400 CVAC 440 440 2422902 WP ALLSN 501D 501D13 03004 GL LT MLG BROKEN W A B I EMER. DESCENT CABIN DEPRESSURIZATION J WARNING INDICATION CR CRUISE 1 CA 15322 SM101 501619 (CAN)DURING FLIGHT AT 16,000 FT. A LOUD THUMP WAS FELT & HEARD. ALL ENGINE PARAMETERS WERE NORMAL BUT CABIN ALTITUDE BEG AN TO CLIMB. AIRCRAFT DESCENDED TO 10,000 FT. CREW SELECTED LANDING GEAR DOWN BUT LEF T MAIN LANDING GEAR WOULD NOT EXTE ND. AFTER SEVERAL ATTEMPTS LANDING GEAR EXTENDED & INDICATED DOWN & LOCKED. AIRCRAFT LANDED SAFELY. MAINTENANCE INVESTIG ATION REVEALED LEFT MAIN LANDING GEAR TORSION ARM WAS BROKEN AT THE APEX BOLT HOLE BOSS.THE WHEELS HAD ROTATED 180 DEGRE ES & TRACKED THIS WAY ON LANDING ROLL. THIS CONDITION PREVIOUSLY PREVENTED THE GEAR FROM EXTENDING DUE TO BEING JAMMED I N THE WHEEL WELL. THE COMPLETE GEAR WAS REPLACED. 2 L 7 2 4R 4 T 6A6 E282 1996101000903 19961010 00903 CE 1996 10 10 CA960212025 1 19960202 A 2820 FUEL LINES CESSNA 150 150L 2071826 CE CONT O200 O200A 17020 SO ENG FUEL ICE BLOCKAGE W A UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 CA 2052139A (CAN) IN CRUISE, THE ENGINE SUDDENLY STOPPED. THE AIRCRAFT LANDED ON THE HIGHWAY WITHOUT ANY PROBLEM. AFTER INSPECTION F OR CAUSE, THE FUEL LINES WERE FOUND CONTAMINATED WITH ICE, BLOCKING THE LINE IN QUESTION. ANTI FREEZE WAS PUT INTO THE F UEL AND AFTER FIFTEEN MINUTES, THE FLIGHT CONTINUED. THE FUEL WAS SUBSEQUENTLY DRAINED. 1 H 7 1 3O 3 O 3A19 E252 1996101000904 19961010 00904 EU 1996 10 10 CA960212026 1 19960127 A 2997 AH58351 WIRE ABEX 4019501 AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE HYDRAULIC BAY CHAFED W H O DEACTIVATE SYST/CIRCUITS OTHER J WARNING INDICATION CR CRUISE 1 CA AH58351 120619 (CAN)IN CRUISE, CREW NOTED BLUE HYDRAULIC PUMP LOW PRESSURE WARNING. PUMP SWITCHED OFF AND CROSSFEED VALVE TURNED ON. IN SPECTION FOUND ONE OF THE 3 PHASE CURRENT FEEDING WIRES DAMAGED INSIDE HYDRAULIC BAY. 2 H 7 2 4T 4 T RT A53EU E20NE 1996101000907 19961010 00907 NM 1996 10 10 CA960212033 1 19960131 A 3222 88303 PISTON CAP ROTOL 8800121 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NLG BROKEN W K O NONE OTHER O OTHER IN INSP/MAINT 1 CA DCL10787 PCE120861 (CAN)ON 'L' CHECK, FLANGE PORTION OF PISTON WITH WRENCHING INSERTED WAS FOUND BROKEN OFF AND BEING RETAINED ONLY BY LOWE R LINK ASSEMBLY. PART SENT TO DOWTY MESSIER FOR EVALUATION. AWAITING INFO. 2 H 7 2 4T 4 T RT A13NM E20NE 1996101000908 19961010 00908 EU 1996 10 10 CA960212034 1 19960112 A 6710 V51313842CR764 BELLOWS BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL LT CYCLIC FROZEN W O OTHER F FLT CONT AFFECTED CR CRUISE 1 CA 4833 CAE834772 (CAN)LEFT CYCLIC INPUT RESTRICTED DUE TO BUILD UP OF ICE ON FORWARD BELLOWS ON THE HYDRAULIC PACK INPUT ROD. 1 G 7 2 3U 3 U H3EU E4CE 1996101000909 19961010 00909 EU 1996 10 10 CA960212035 1 19960129 A 3246 NAS13035 BOLT DUNLOP AHA1837 BAG JETSTM JETSTM4112 EU MCAULY INBOARD TIRE SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA 769 041 (CAN)RIGHT MAIN INBOARD TIRE FOUND FLAT. 5 BOLTS FOUND SHEARED IN THREADED SECTION. 1 L 7 2 4T RT A196 1996101000910 19961010 00910 EU 1996 10 10 CA960212101 1 19960121 A 6220 350A31190703 STARFLEX SNIAS 350 AS350B1 8680811 EU YELLOW ARM CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 948 (CAN)YELLOW ARM OF STARFLEX FOUND CRACKED. CRACK STARTED 223 MM FROM SLEEVE END AND RUNS 6 MM TOWARD SLEEVE THEN CURVED BACK AND RAN ANOTHER 9 MM. CRACK DEPTH 4 MM. 1 G 7 1 3U H9EU 1996101000911 19961010 00911 NE 1996 10 10 CA960212102 2 19960117 A 7200 ENGINE SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1D NE FUEL CONT SYS FLAMED OUT W B EMER. DESCENT X ENGINE FLAMEOUT HO HOVERING 1 CA 7008 (CAN)ENGINE FLAMED OUT ON APPROACH AT 8,000 FEET ALTITUDE. OAT 20 DEGREES. ENGINE WAS RUNNING NORMAL PRIOR TO LANDING. P ILOT PULLED ON COLLECTIVE TO CHECK HIS DESCENT WHEN THE LIGHTS AND HORN CAME ON AND E NGINE FLAMED OUT. FUEL INSPECTED F OR ICE AND WATER, BUT NONE FOUND. ENGINE INTAKE INSPECTED FOR ICE, SNOW, OR FOD, BUT NONE FOUND. ENGINE WAS GROUND RUN F OR 20 MINUTES BUT THERE WAS NO HESITATION. HELICOPTER FLOWN BACK TO BASE AND FUEL CONTROL REMOVED FOR TESTING. 1 G 7 1 3U 3 U H9EU E19EU 1996101000912 19961010 00912 NM 1996 10 10 CA960212103 1 19960207 A 3230 651781910 ACTUATOR BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE NLG DOWNLOCK BROKEN W A UNSCHED LANDING O OTHER CL CLIMB 1 CA 47273 5557 702737 (CAN)NOSE GEAR FAILED TO RETRACT AFTER TAKEOFF. NOSE GEAR DOWN LOCK ACTUATOR REPLACED. ONE INCH OF BEARING RETAINING CAS TING BROKEN OFF. 2 L 7 2 4F 4 F A16WE E2EA 1996101000913 19961010 00913 NM 1996 10 10 CA960214006 1 19960207 A 5610 WINDOW BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE CAPT SIDE DELAMINATED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA 702669 (CAN)AFTER TAKEOFF THE CAPTAINS SIDE WINDOW APPEARED CRACKED IN THE UPPER RH CORNER AS IF ARCING. AIRCRAFT RETURNED. CAP TAINS SLIDING WINDOW REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1996101000914 19961010 00914 NM 1996 10 10 CA960214007 1 19960211 A 2731 65794256 BUSHING BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE ELEV RT TAB WORN W K NONE E VIBRATION/BUFFET CL CLIMB 1 CA 29301 8802 708805 (CAN)DURING CLIMB, ONCE FLAPS RETRACTED AND ESTABLISHED IN CLIMB, STRONG VIBRATION AND RUMBLE FELT THROUGHOUT AIRCRAFT. STRONG IN AFT GALLEY THAN FORWARD. FELT THROUGH MAIN FLOOR AND SEATS IN COCKPIT AND R UMBLE NOISE QUITE PRONOUNCED. VIBR ATION AND NOISE SUDDENLY REDUCED CLIMBING THROUGH 24,000 -25,000 FT. ALSO FELT VIBRATION IN CONTROL YOKE AND THRUST/STAR T LEVERS. ON DESCENT VIBRATION DISAPPEARED. BOEING SL 737-SL-02-02, ELEVATOR RH TAB HAD EXCESSIVE PLAY DUE TO WORN BUSHI NG. MECHANISM REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1996101000916 19961010 00916 SW 1996 10 10 CA960214010 1 19960209 A 5620 2722180803 WINDOW SWRNGN SA226 SA226TC 8780404 SW #9 PAX CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 15632 0213 (CAN)EARLY INSPECTION PER AD 93-19-06 AND SB 226-56-002 & 003 CARRIED OUT. WINDOW AT PAX SEAT #9 SHOWED CRACK INDICATION WINDOW HAD BEEN REPLACED ABOUT ONE YEAR PREVIOUS,ABOUT 1200 HOURS AND 1600 CYCLES EXAMINATION OF CRACK AND ASSOCIATED HOLE SHOWED THAT HOLE WAS MISDRILLED BY ABOUT .040. THUS PUTTING STRESS LOAD ON HOLE AND CAUSING CRACK. INSTALLATION ON PROCEDURES REVISED TO PRECLUDE THIS HAPPENING AGAIN. 2 L 7 2 4T RT A8SW 1996101000917 19961010 00917 SW 1996 10 10 CA960214011 1 19960204 A 2612 FIRE WARN SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP RH ENGINE ILLUMINATED W C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CA 22315 P54259 (CAN)ON TAKEOFF ROLL, AND SHORTLY AFTER SELECTING 'SPEED LEVERS HIGH', RIGHT ENGINE FIRE WARNING CAME ON. POWER REDUCED AND RH 'STOP AND FEATHER' PULLED. NO SMOKE OR FIRE NOTED FROM ENGINE. INVESTIGATION FOUND RH FIRE WARNING STILL ON AND E NGINE COLD. LIGHT OUT WHEN LOWER COWL REMOVED. ALL FIRE DETECTORS CHECKED FOR POSITION AND CLEARANCE. NO OBVIOUS DISCREP ANCY. 2 L 7 2 4T 4 T RT A8SW E4WE 1996101000920 19961010 00920 EU 1996 10 10 CA960214014 1 19960203 A 5711 FITTING ADAPTOR ZLIN 242 Z242L 9970204 EU SPAR LEAKING W K NONE J WARNING INDICATION IN INSP/MAINT 1 CA 178 (CAN)DURING PREFLIGHT THE PILOT NOTICED THAT THE SPAR PRESSURE WAS LOW. THE SPAR ADAPTOR FITTING WAS FOUND WITH A SLOW LEAK. THE AIRCRAFT MANUFACTURER RECOMMENDED REMOVING THE FITTING AND RESEALING WITH LOCTITE VERSES THE FACTORY SEALANT. THIS WAS ACCOMPLISHED AND THE SPAR WAS RECHARGED WITH NITROGEN AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1 L 7 1 3O 0 A76EU 1996101000922 19961010 00922 SO 1996 10 10 CA960214016 1 19960120 A 7921 455192 OIL COOLER 455192 PIPER PA44 PA44180 7104402 SO LYC O360 O360A1H 41514 EA RT ENG LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 24 E95206018 L3466736A (CAN)ON WALKAROUND THE PILOT NOTICED OIL COMING FROM THE RIGHT HAND ENGINE. INVESTIGATION FOUND OIL COOLER SHOWED SIGNS OF LEAKAGE. COOLER REMOVED AND PRESSURE TESTED AND FOUND TO HAVE PIN HOLES. COOLER RE PLACED WITH A NEW UNIT. 1 L 7 2 3O 3 O A19S0 E286 1996101000923 19961010 00923 NM 1996 10 10 CA960214017 1 19960123 A 3260 43467410332206 SWITCH BOEING 757 75728A 1384976 NM RROYCE LT MLG INTERMITTENT W L ABORTED APPROACH O OTHER AP APPROACH 1 CA (CAN)WHEN GEAR SELECTED DOWN THE LH GEAR INDICATION WOULD NOT ILLUMINATE. SLIGHT TAP ON SWITCH GOT INDICATION WORKING. L H GEAR SWITCH ASSEMBLY REPLACED. 2 L 7 2 4F RT A2NM 1996101000925 19961010 00925 EA 1996 10 10 CA960214019 1 19960205 A 7830 335C FLEXSHAFT LOCK AIRESRCH 1267586 CNDAIR CL600 CL6002A12 1900304 EA GE CF34 CF341A NE T/R PWR DRV UNIT NOT ENGAGING W K NONE O OTHER IN INSP/MAINT 1 CA 3031 335C 350143 (CAN)FLEXSHAFT LOCK NOT ENGAGING CAM. FOUND UNSECURED AND FAILED ON SHAFT. 2 L 7 2 4F 4 F RT A21EA E15NE 1996101000927 19961010 00927 EU 1996 10 10 CA960215101 1 19960129 A 2820 835303495 FUEL SCREEN AIRBUS 320 A320211 3930320 EU NR 1 ENG ICED W A E ENGINE SHUTDOWN J X WARNING INDICATION ENGINE FLAMEOUT TX TAXI/GRND HDL 1 CA (CAN)DURING TAXIING IN TO RAMP,LEFT TANK PUMPS 1 & 2 FAULT ON ECAM & OVERHEAD.CHECK LIST COMPLETED AS PER ECAM.APPROXIMA TELY 2 MINUTES LATER #1 ENGINE FLAMED OUT & WAS SHUTDOWN,ACCORDING TO ECAM.FUEL IN LE FT TANK 3020,FUEL IN RIGHT TANK 31 80. CHECK POST FLIGHT REPORTS.NO FAULTS RECORDED ON THE #11 ENGINE CHANNEL "A" & "B" FADAC TEST REPORT.MINIMUM IDLE & 50 PERCENT POWER ASSURANCE TESTS COMPLETED PER RUN-UP MANUAL.ALL ENGINES WITHIN LIMITS. #1 ENGINE FUEL FILTER INSPECTED WI TH NO FAULTS FOUND.FUEL TANKS FOUND CONTAMINATED WITH WATER DURING SUMPING.ANTI-ICE ADDITIVE ETHOL CARBITOL ADDED DURING REFUELING.AIRBUS IS AWARE OF A PROBLEM WITH THE BOOSTER PUMP SUCTION SCREENS ICING DURING COLD WEATHER OPERATIONS, MOD 2 L 7 2 4F RT A28NM 1996101000928 19961010 00928 NM 1996 10 10 CA960220101 1 19960210 A 8012 1638616927 SWITCH BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE NR 2 ENG START FAILED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 687714 (CAN)#2 ENGINE SHUTDOWN IN FLIGHT DUE TO ENGINE START VALVE LIGHT. AIRCRAFT DIVERTED. REPLACED VALVE AND SWITCH. 2 L 7 2 4F 4 F A16WE E2EA 1996101000930 19961010 00930 SW 1996 10 10 CA960221202 1 19960204 A 6220 212311007101 BEARING BELL 212 212 1181420 SW M/R GRIP CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA 317 (CAN)THE MAIN ROTOR HEAD WAS BEING REPAIRED FOR GREASE LEAKAGE PAST THE SEAL SLEEVE 'O' RING. PRIOR TO REINSTALLATION OF THE MAIN ROTOR GRIP, IT WAS NOTICED THAT FIVE OF THE INBOARD BEARING CAGE BARS HAD CHAFED THROUGH. ALL ROLLERS REMAINED IN PLACE. 1 G 7 1 4U H4SW 1996101700001 19961017 00001 WP 1996 10 17 GTIA96NK166 1 19960417 A 5321 FLOOR BOARD DOUG DC9 DC932 3022066 WP COCKPIT CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 12505 45788 DURING C-CHECK, FOUND CENTER COCKPIT FLOOR BOARD CORRODED. FABRICATED, TREATED AND INSTALLED REPLACEMENT FLOOR BOARD IA W 51-10-2, 51-10-3, 51-30-0 AND 51-20-0. (M) 2 L 7 2 4F A6WE 1996101700002 19961017 00002 NE 1996 10 17 CALA9601423 2 19961007 A 7597 6130036 WIRE BOEING 737 737130 1384435 NM PWA JT8 JT8D7A 52053 NE ENG ANTI ICE BURNED A CALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 33202 19019 SMOKE DEVELOPED FROM BEHIND COCKPIT OVERHEAD PANEL AFTER TURNING ON ENGINE ANTI-ICE WHILE CRUISING AT FL 240 EN ROUTE FR OM EWR TO CAE. THE SMOKE CEASED WHEN ANTI-ICE WAS TURNED OFF. THE FLIGHT WAS CONTINUED TO CAE WHERE IT LANDED WITHOUT FU RTHER PROBLEMS. MAINTENANCE FOUND BURNT WIRING TO ANTI-ICE MODULE AND AFT OF ANTI-ICE MODULE IN THE COCKPIT OVERHEAD PA NEL. THE BURNT WIRING WAS REPLACED. IN ADDITION, THE C146 CIRCUIT BREAKER AND ANTI-ICE VALVE WERE REPLACED. OPERATIONA L CHECKS OF THE SYSTEM WERE GOOD WITH NO OTHER DEFECTS FOUND. 2 L 7 2 4F 4 F A16WE E2EA 1996101700003 19961017 00003 WP 1996 10 17 CALA9601424 1 19961008 A 3233 39208025507 ACTUATOR DOUG DC9 DC932 3022066 WP RT MLG INOPERATIVE A CALA K NONE J WARNING INDICATION TO TAKEOFF 1 SW 09 17535 18794 0357 47111 WHEN GEAR WAS RETRACTED ON TAKEOFF, THE GEAR DOOR OPEN AND RIGHT MAIN GEAR UNSAFE LIGHTS REMAINED ILLUMINATED. APPROXIM ATELY 15 SECONDS LATER THE SPEED BRAKE SPOILER HANDLE SOUNDED AS THOUGH IT CYCLED TO AIR MODE AND BOTH GEAR UNSAFE LIGHT S EXTINGUISHED. THE FLIGHT WAS CONTINUED WITHOUT FURTHER PROBLEMS. MAINTENANCE FOUND THE RT MLG RETRACT ACTUATOR AT FAUL T. THE ACTUATOR WAS REPLACED PER MM 32-32-2. A GEAR SWING WAS PERFORMED AND GEAR OPERATION CHECKED GOOD. PART TOTAL C YCLES, 14,545. 2 L 7 2 4F A6WE 1996101700004 19961017 00004 WP 1996 10 17 CALA9601425 1 19961009 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 937MC 49450 INSPECTION FOUND EMERGENCY FLOOR TRACK LIGHTING FROM ROWS 25 TO 32 LOOSE AND INOPERATIVE. MAINTENANCE FOUND A BROKEN WI RE IN AFT SECTION. THE WIRE WAS REPLACED AND OPERATION OF THE TRACK LIGHTING WAS RESTORED. 2 L 7 2 4F A6WE 1996101700005 19961017 00005 WP 1996 10 17 CALA9601426 1 19961009 A 3397 WIRE DOUG DC9 DC932 3022066 WP CABIN DAMAGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 33506 47765 INSPECTION FOUND EMERGENCY TRACK LIGHTING IN FIRST CLASS SECTION OF CABIN COMING UP AND INOPERATIVE. MAINTENANCE FOUND DAMAGED TRACK LIGHT WIRING. THE WIRING WAS REPAIRED AND THE TRACK WAS REINSTALLED. 2 L 7 2 4F A6WE 1996101700006 19961017 00006 NM 1996 10 17 CALA9601427 1 19960911 A 5320 SUPPORT BOEING 727 727224 1384076 NM BS 1140 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 20665 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1140, LBL 12. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2 . 2 L 7 3 4F A3WE 1996101700007 19961017 00007 NM 1996 10 17 CALA9601428 1 19960911 A 5320 656097124 ANGLE BOEING 727 727224 1384076 NM BS 1067 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 20665 INSPECTION FOUND FLOOR SUPPORT CORRODED BETWEEN RBL 24 AND RBL 48 AT STA 1067. THE FLOOR SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM'S 51-10-1, 51-10-2, AND 51-30-2. 2 L 7 3 4F A3WE 1996101700008 19961017 00008 NM 1996 10 17 CALA9601429 1 19960911 A 5320 656097124 ANGLE BOEING 727 727224 1384076 NM BS 1034 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 20665 INSPECTION FOUND FLOOR SUPPORT ANGLE CORRODED AT LBL 35, STA 1034. THE FLOOR SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM'S 51-10-1, 51-30-2, 51-10-2, AND 51-40-5. 2 L 7 3 4F A3WE 1996101700009 19961017 00009 NM 1996 10 17 CALA9601430 1 19960912 A 5320 ANGLE BOEING 727 727224 1384076 NM BS 720 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 20665 INSPECTION FOUND A HOLE BROKEN THROUGH CAP ANGLE OF CABIN FLOOR INTERCOSTAL BETWEEN STA 720 AND 720A, BL ZERO. THE CAP WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1. 2 L 7 3 4F A3WE 1996101700010 19961017 00010 NM 1996 10 17 CALA9601431 1 19960905 A 5753 SKIN BOEING 727 727224 1384076 NM RT TE FLAP DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 20665 INSPECTION FOUND TWO DENTS ON LOWER SURFACE OF RT OUTBOARD FLAP AFT SEGMENT. THE DENTED AREAS WERE CUT OUT. FILLERS AN D CORE WERE FABRICATED AND A HOT BOND REPAIR WAS ACCOMPLISHED IAW SRM 51-40-6. 2 L 7 3 4F A3WE 1996101700011 19961017 00011 NM 1996 10 17 CALA9601432 1 19960905 A 5712 RIB BOEING 727 727224 1384076 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 20665 INSPECTION FOUND A .50 INCH CRACK IN BOTTOM OF RIB INSIDE OF RIGHT NAV LIGHT COMPARTMENT (RT WING TIP). THE RIB WAS REM OVED . A NEW RIB WAS FABRICATED AND INSTALLED IAW SRM'S 51-10-1 AND 51-40-2. A DOUBLER WAS ALSO INSTALLED TO REPAIR CRA CKED WEB IN SAME AREA. 2 L 7 3 4F A3WE 1996101700012 19961017 00012 NM 1996 10 17 CALA9601433 1 19960904 A 5754 BRACKET BOEING 727 727224 1384076 NM NR 6 LE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 20665 INSPECTION FOUND LOWER OUTBOARD RADIUS OF NR 6 KRUGER FLAP ACTUATOR MOUNT BRACKET CRACKED. 2 L 7 3 4F A3WE 1996101700013 19961017 00013 NM 1996 10 17 CALA9601434 1 19960909 A 5720 ANGLE BOEING 727 727224 1384076 NM BS 332 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 20665 INSPECTION FOUND A .50 INCH CRACK BETWEEN BOLTS OF UPPER RIB CAP ANGLE AT RT WING LEADING EDGE, STA 332. A REPLACEMENT ANGLE WAS FABRICATED AND INSTALLED IAW SRM'S 51-40-3, 51-8-0, AND 51-30-2. 2 L 7 3 4F A3WE 1996101700014 19961017 00014 NM 1996 10 17 CALA9601435 1 19960909 A 5754 65172862 RIB BOEING 727 727224 1384076 NM NR 5 LE SLAT GROOVED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 20665 INSPECTION FOUND OUTBOARD RIB OF NR 5 SLAT DEEPLY GROOVED. THE RIB WAS REMOVED AND REPLACED IAW SRM 51-10-1. 2 L 7 3 4F A3WE 1996101700015 19961017 00015 NM 1996 10 17 CALA9601436 1 19960910 A 5753 69207722 FITTING BOEING 727 727224 1384076 NM RT TE MID FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 20665 INSPECTION FOUND A .75 INCH CRACK IN CHORD FITTING AT AFT UPPER INBOARD CORNER OF RT WING INBOARD MID FLAP REAR SPAR, WB L 124.2. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996101700016 19961017 00016 NM 1996 10 17 CALA9601437 1 19960910 A 5753 RIB BOEING 727 727224 1384076 NM RT TE MID FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 20665 INSPECTION FOUND A .75 INCH CRACK IN LOWER AFT END OF INBOARD RIB OF RT OUTBOARD MID FLAP. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM'S 51-10-0, 51-10-2, AND 51-40-3. 2 L 7 3 4F A3WE 1996101700017 19961017 00017 NM 1996 10 17 CALA9601438 1 19960912 A 5754 RIB BOEING 727 727224 1384076 NM NR 5 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 20665 INSPECTION FOUND LOWER FORWARD END OF NINE RIBS CRACKED AT INTERIOR OF NR 5 SLAT. THE CRACKS RANGED IN LENGTH FROM .1250 INCH TO 1 INCH. THE CRACKS WERE STOP DRILLED. REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 57-50-3. 2 L 7 3 4F A3WE 1996101700018 19961017 00018 NM 1996 10 17 CALA9601439 1 19960911 A 5315 FLOOR BEAM BOEING 727 727224 1384076 NM BS 1130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 20665 INSPECTION FOUND EXFOLIATION CORROSION ON FLOORBEAM AT STA 1130, LBL 18. THE CORROSION WAS REMOVED IAW SRM 51-10-6. RE PAIR STRAPS WERE INSTALLED IAW SRM'S 51-10-2, 51-30, 51-40-5, AND 53-30-4. 2 L 7 3 4F A3WE 1996101700019 19961017 00019 NM 1996 10 17 CALA9601440 1 19960909 A 5315 FLOOR BEAM BOEING 727 727224 1384076 NM BS 1130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 20665 INSPECTION FOUND THE AFT CARGO HORIZONTAL FLOORBEAM CORRODED AT STA 1130, RBL 30 TO RBL 53. 2 L 7 3 4F A3WE 1996101700020 19961017 00020 NM 1996 10 17 CALA9601441 1 19960909 A 5315 FLOOR BEAM BOEING 727 727224 1384076 NM BS 1130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 20665 INSPECTION FOUND HORIZONTAL LEG OF AFT CARGO FLOORBEAM CORRODED AT STA 1130, RBL ZERO TO RBL 56. THE CORROSION WAS REMO VED IAW SRM 51-10-6. THE FLOORBEAM WAS REPAIRED IAW ECRA 5330-03333. 2 L 7 3 4F A3WE 1996101700021 19961017 00021 NM 1996 10 17 CALA9601442 1 19960913 A 5315 FLOOR BEAM BOEING 727 727224 1384076 NM BS 1070 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69736 20665 INSPECTION FOUND LOWER HORIZONTAL LEG AT CABIN FLOORBEAM CORRODED FROM BL ZERO TO RBL 56, STA 1070 (AFT CARGO). A STRAP AND ANGLE REPAIR WERE FABRICATED AND INSTALLED IAW SRM 53-10-8. 2 L 7 3 4F A3WE 1996101700022 19961017 00022 WP 1996 10 17 CALA9601443 1 19961013 A 2150 20495054 ACM DOUG DC9 DC982 3022082 WP LEFT SMOKES A CALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 16893 5963 49392 IMMEDIATELY AFTER TAKEOFF, CABIN FILLED WITH AIR CONDITIONING SMOKE. PERFORMED UNEVENTFUL AIR RETURN. REMOVED AND REPL ACED LEFT AIR CYCLE MACHINE AND COALESCER BAGS PER MM 21-51-01. 2 L 7 2 4F A6WE 1996101700023 19961017 00023 WP 1996 10 17 9621149180 1 19960914 A 5320 WEB DOUG DC9 DC914 3022034 WP BS 110 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3312L 45707 DURING H-CHECK, FOUND CRACKS IN THE NOSE LANDING GEAR HORIZONTAL PRESSURE PANEL AT FS 83, LEFT SIDE AND AT FS 110, RBL 3 5. REPAIRED PANEL (P/N 9910073-313) PER EA 91-110780, DASH 110779. 2 L 7 2 4F A6WE 1996101700024 19961017 00024 WP 1996 10 17 9621159178 1 19960917 A 5230 WEB DOUG DC9 DC914 3022034 WP CARGO DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3310L 45705 DURING H-CHECK, FOUND CRACKS IN THE AFT CARGO DOOR HORIZONTAL BEAM WEB. REPAIRED WEB (P/N 9957665-17) PER EA 91-111246. 2 L 7 2 4F A6WE 1996101700025 19961017 00025 WP 1996 10 17 9621161152 1 19960917 A 5313 LONGERON DOUG DC10 DC1040 3023508 WP BS 1964-1970 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 152US 46761 DURING T-CHECK, FOUND CORROSION ON LONGERON 48R FROM FS 1964 - 1970. REPAIRED LONGERON (P/N AGA 7047-501) PER EA 11-110 251. 2 L 7 3 4F A22WE 1996101700026 19961017 00026 WP 1996 10 17 9621171152 1 19960918 A 5313 LONGERON DOUG DC10 DC1040 3023508 WP BS 1754-1812 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 152US 46761 DURING T-CHECK, FOUND CORROSION ON LONGERON 46R FROM FS 1754 - 1812. REPAIRED LONGERON (P/N AFA 7098-1) PER EA 11-11022 0. 2 L 7 3 4F A22WE 1996101700027 19961017 00027 WP 1996 10 17 9621189304 1 19960919 A 5240 SKIN DOUG DC9 DC982 3022082 WP SERVICE DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 931MC 48057 DURING H-CHECK, FOUND A CRACK IN THE LEFT AFT SERVICE DOOR SKIN AT THE HOLD OPEN HOOK. REPAIRED SKIN (P/N 5937601-3) PE R EA 93-110332. 2 L 7 2 4F A6WE 1996101700028 19961017 00028 WP 1996 10 17 9621191152 1 19960919 A 5315 FLOOR BEAM DOUG DC10 DC1040 3023508 WP BS 1099 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 152US 46761 DURING T-CHECK, FOUND A CRACK IN THE FORWARD CARGO FLOOR BEAM AT FS 1099, LBL 58. REPAIRED BEAM (P/N ADA 0039-5) PER EA 11-110248. 2 L 7 3 4F A22WE 1996101700029 19961017 00029 WP 1996 10 17 9621209910 1 19960920 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 606 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 960N 47256 DURING H-CHECK, FOUND THE LONGERON 30 KEEL FITTINGS DAMAGED AT FS 606; A CRACK IN THE LEFT FITTING AND CORROSION ON THE RIGHT FITTING. REPLACED BOTH FITTINGS. 2 L 7 2 4F A6WE 1996101700030 19961017 00030 WP 1996 10 17 9621219910 1 19960920 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 1019 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 960N 47256 DURING H-CHECK, FOUND A .75 INCH CRACK IN THE FS 1019 FRAME FORMER AT LONGERON 14R. REPAIRED FORMER (P/N 9958239-12) PE R EA 99-110350. 2 L 7 2 4F A6WE 1996101700031 19961017 00031 WP 1996 10 17 9621229910 1 19960924 A 5312 BULKHEAD WEB DOUG DC9 DC931 3022065 WP BS 218 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 960N 47256 DURING H-CHECK, FOUND A CRACK IN THE FS 218 BULKHEAD WEB AT RBL 44. REPAIRED WEB (P/N 9911520-173) PER EA 99-106321. 2 L 7 2 4F A6WE 1996101700032 19961017 00032 WP 1996 10 17 9621239872 1 19960925 A 5320 SUPPORT DOUG DC9 DC951 3022051 WP BS 229-265 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 781NC 48121 DURING H-CHECK, FOUND CORROSION ON THE CENTERLINE FLOOR SUPPORT FROM FS 229 - 265. REPAIRED SUPPORT (P/N 5910760-11) PER EA 98-111257. 2 L 7 2 4F A6WE 1996101700033 19961017 00033 WP 1996 10 17 9621249910 1 19960925 A 5720 DOUBLER DOUG DC9 DC931 3022065 WP WS 530 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 960N 47256 DURING H-CHECK, FOUND A CRACK IN THE RIGHT WING FRONT SPAR DOUBLER AT XOS 530. REPAIRED DOUBLER (P/N 9919343-2) PER EA 99-110333. 2 L 7 2 4F A6WE 1996101700034 19961017 00034 WP 1996 10 17 9621259910 1 19960925 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 1133 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 960N 47256 DURING H-CHECK, FOUND A CRACK IN THE AFT FUSELAGE SKIN AT FS 1133, LEFT SIDE BENEATH THE RAIN GUTTER. REPAIRED SKIN PE R EA 99-105056. 2 L 7 2 4F A6WE 1996101700035 19961017 00035 WP 1996 10 17 9621269180 1 19960926 A 5320 DOUBLER DOUG DC9 DC914 3022034 WP BS 786-805 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3312L 45707 DURING H-CHECK, FOUND CORROSION ON THE WATER SERVICE PANEL DOUBLER LOCATED BETWEEN FS 786 - 805 FROM LONGERON 20R - 22R. REPAIRED THE DOUBLER PER EA 91-111223. 2 L 7 2 4F A6WE 1996101700036 19961017 00036 WP 1996 10 17 9621279974 1 19960927 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 579 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9338 47347 DURING M-CHECK, FOUND A CRACK IN THE FS 579 LOWER RIGHT FRAME FITTING, PSE 53.09.016. REPLACED FITTING PER SRM 51-10-4. 2 L 7 2 4F A6WE 1996101700037 19961017 00037 WP 1996 10 17 9621289872 1 19960927 A 5720 FITTING DOUG DC9 DC951 3022051 WP BS 693 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 781NC 48121 DURING H-CHECK, FOUND A 4 INCH CRACK IN THE CENTER WING FRONT SPAR UPPER LEFT SUPPORT FITTING AT FS 693. REPLACED FITTI NG (P/N 5913055-507). 2 L 7 2 4F A6WE 1996101700038 19961017 00038 WP 1996 10 17 9621299872 1 19960927 A 5311 FRAME DOUG DC9 DC951 3022051 WP BS 1303 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 781NC 48121 DURING H-CHECK, FOUND A CRACK ON THE FS 1303 CANTED FRAME ON THE UPPER FLANGE. REPAIRED FRAME (P/N 9911877-7) PER EA 98 -111263. 2 L 7 2 4F A6WE 1996101700039 19961017 00039 WP 1996 10 17 9621309910 1 19960929 A 5312 BULKHEAD FITTING DOUG DC9 DC931 3022065 WP BS 737-755 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 960N 47256 DURING H-CHECK, FOUND CORROSION ON THE RIGHT KEEL TO BULKHEAD FITTING FS 737 - 755 AT RBL 7. REPLACED FITTING (P/N 3915 135-506) PER SRM 51-01, PAR. 1C. 2 L 7 2 4F A6WE 1996101700040 19961017 00040 WP 1996 10 17 9621319178 1 19960930 A 5320 WEB DOUG DC9 DC914 3022034 WP BS 83 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3310L 45705 DURING H-CHECK, FOUND CRACKS IN THE NOSE LANDING GEAR HORIZONTAL PRESSURE WEB AT FS 83, RIGHT SIDE, AND AT FS 108, LBL 2 5, 37, AND RBL 25. REPAIRED WEB (P/N 9910073-313) PER EA 91-111232 AND DASH 111230. 2 L 7 2 4F A6WE 1996101700041 19961017 00041 WP 1996 10 17 9621329614 1 19961001 A 5320 FITTING DOUG DC9 DC932 3022066 WP DOOR FRAME CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 614NW 47128 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE AFT ENTRY DOOR, AFT LEFT FRAME FITTING. REPLACED FIT TING PER SRM 51-30-2. 2 L 7 2 4F A6WE 1996101700042 19961017 00042 WP 1996 10 17 9621339178 1 19961001 A 5320 FITTING DOUG DC9 DC914 3022034 WP BS 470 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3310L 45705 DURING H-CHECK, FOUND A CRACK IN THE LONGERON 27R END FITTING AT FS 470. REPLACED FITTING PER SRM 51-30-2, 51-30-5. 2 L 7 2 4F A6WE 1996101700043 19961017 00043 WP 1996 10 17 9621349304 1 19961001 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 229-399 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 931MC 48057 DURING H-CHECK, FOUND CORROSION ON THE LONGERON 26L FROM FS 229 - 399. REPAIRED LONGERON (P/N 5936434-29) PER EA 93-110 340. 2 L 7 2 4F A6WE 1996101700044 19961017 00044 WP 1996 10 17 9621359304 1 19961001 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 480 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 931MC 48057 DURING H-CHECK, FOUND CORROSION ON LONGERON 29L AT FS 480. REPAIRED LONGERON (P/N 3936478-503) PER EA 93-110321. 2 L 7 2 4F A6WE 1996101700045 19961017 00045 WP 1996 10 17 9621369304 1 19961001 A 5320 CUSP DOUG DC9 DC982 3022082 WP BS 200 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 931MC 48057 DURING H-CHECK, FOUND CORROSION ON THE LEFT CUSP AT FS 200. REPAIRED CUSP (P/N 9923666-3) PER EA 93-109586. 2 L 7 2 4F A6WE 1996101700046 19961017 00046 WP 1996 10 17 9621379872 1 19961001 A 5311 FRAME DOUG DC9 DC951 3022051 WP BS 579/598 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 781NC 48121 DURING H-CHECK, FOUND CORROSION ON THE FS 579 AND FS 598 FRAMES BETWEEN LONGERONS 29L - 30. REPAIRED FRAMES (P/N 591144 7-1 AND 5911448-525) PER EA 98-111271, 98-11276. 2 L 7 2 4F A6WE 1996101700047 19961017 00047 WP 1996 10 17 9621389304 1 19961002 A 5320 DOUBLER DOUG DC9 DC982 3022082 WP BS 1079-1089 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 931MC 48057 DURING H-CHECK, FOUND CRACKS IN THE FS 1079 -1089 WINDOW RINGPAN LEFT SIDE. REPAIRED RINGPAN (P/N 5912285) PER EA 93-11 0339. 2 L 7 2 4F A6WE 1996101700048 19961017 00048 WP 1996 10 17 9621399304 1 19961002 A 5313 LONGERON DOUG DC9 DC982 3022082 WP S 1287-1309 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 931MC 48057 DURING H-CHECK, FOUND CORROSION ON LONGERON 22L AT FS 1287 AND 1309. REPAIRED LONGERON (P/N S-1242886) PER EA 93-110348 . 2 L 7 2 4F A6WE 1996101700049 19961017 00049 WP 1996 10 17 9621409178 1 19961003 A 5711 SPAR CAP DOUG DC9 DC914 3022034 WP CTR WING CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 310L 45705 DURING H-CHECK, FOUND A 4 INCH CRACK IN THE CENTER WING REAR SPAR UPPER CAP AT THE VERTICAL KEEL PANEL. REPAIRED CAP (P /N 9911752-1) PER EA 91-111701. 2 L 7 2 4F A6WE 1996101700050 19961017 00050 WP 1996 10 17 9621419851 1 19961008 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 760NC 47708 DURING LINE CHECK, FOUND RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996101700051 19961017 00051 WP 1996 10 17 9621429178 1 19961004 A 3350 BATTERY PACK DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 3310L 45705 DURING LINE CHECK, RIGHT NACELLE EMERGENCY LIGHT FAILED 10 MINUTE CHECK. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996101700052 19961017 00052 WP 1996 10 17 9621439978 1 19961007 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9342 47391 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. OPERAT IONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996101700053 19961017 00053 WP 1996 10 17 9621449992 1 19961007 A 3350 60030451 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8960E 45869 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN AISLE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPE RATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996101700054 19961017 00054 WP 1996 10 17 9621459990 1 19961006 A 2460 TERMINAL BLOCK DOUG DC9 DC931 3022065 WP CABIN SHORTED A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 GL 01 8950E 47186 DURING LANDING, FLIGHT ATTENDANT OBSERVED SPARKS COMING FROM OVEN TIMER AREA. COCKPIT CREW SMELLED AN ELECTRICAL BURNIN G SMELL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND TERMINAL STUD SHORTED AT S3-25 TERMINAL BLOCK IN OVERHEAD COMPANIONWAY. REPLACED TERMINAL BLOCK AND INSTALLED NEW TERMINAL STRIP. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996101700055 19961017 00055 WP 1996 10 17 9621469911 1 19961008 A 2133 OUTFLOW VALVE DOUG DC9 DC931 3022065 WP BLOCKED BY FOD A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 961N 47405 AUTO PRESSURIZATION SYSTEM FAILED AFTER TAKEOFF. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND INSULATION LODGED IN OUTFLOW VALVE WHICH WAS RESTRICTING MOVEMENT. REMOVED INSULATION AND REPLACED OUTFLOW VALVE ACTUA TOR. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996101700056 19961017 00056 WP 1996 10 17 9621479910 1 19961007 A 3231 CONTROL CABLE DOUG DC9 DC931 3022065 WP NLG DOOR MECH FRAYED A NWAA O OTHER E VIBRATION/BUFFET CL CLIMB 1 GL 01 960N 47256 VIBRATION AND NOISE COMING FROM NOSE GEAR AREA AFTER TAKEOFF FROM MSN. RECYCLED GEAR THREE TIMES BEFORE NORMAL INDICATI ONS WERE ACHIEVED. FLIGHT CONTINUED TO DESTINATION (MSP) AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BOTH NOSE GEAR DOORS BINDING AND RIGHT UPPER DOOR STOP CABLE FRAYED. RIGGED BOTH NOSE GEAR DOORS AND REPLACED RIGHT UPPER DOOR STOP C ABLE. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996101700057 19961017 00057 1996 10 17 9621489910 4 19961007 A 3442 RADAR DOUG DC9 DC931 3022065 WP COCKPIT MALFUNCTIONED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 960N 47256 WEATHER RADAR SYSTEM FAILED AFTER TAKEOFF. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RA DAR ANTENNA AND NR 2 VERTICAL GYRO. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996101700058 19961017 00058 WP 1996 10 17 9621499945 1 19961007 A 2420 976J2544 GEN CONTL PNL DOUG DC9 DC931 3022065 WP RT COCKPIT FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 8925E WP2179A80 45840 RIGHT GENERATOR DROPPED OFF LINE ACCOMPANIED BY AC CROSSTIE LOCKOUT AFTER TAKEOFF. FLIGHT RETURNED TO DTW AND LANDED WI THOUT INCIDENT. MAINTENANCE REPLACED RIGHT GENERATOR CONTROL PANEL. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SE RVICE. 2 L 7 2 4F A6WE 1996101700059 19961017 00059 NM 1996 10 17 9621506310 1 19961009 A 3510 OXY LINE BOEING 747 747451 1384940 NM UPPER DECK DISCONNECTED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 670US 24225 DURING P-CHECK, FOUND THAT THE OXYGEN COMPARTMENT AT THE UPPER DECK FLIGHT ATTENDANT SEAT FAILED TO OPEN AND THAT NO OXY GEN FLOWED INTO THE MASKS WHEN THE PINS WERE PULLED. RECONNECTED THE OXYGEN LINE. FUNCTIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996101700060 19961017 00060 NE 1996 10 17 9621511161 2 19961008 A 7230 COMPRESSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20J 52054 NE NR 3 ENGINE STALLED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 01 161US 46770 86138 DURING APPLICATION OF POWER FOR TAKEOFF, THE NR 3 ENGINE EXPERIENCED COMPRESSOR STALL. CREW ABORTED THE TAKEOFF AS EGT CLIMBED TO 990 DEGREES WITHIN ONE SECOND. AIRCRAFT RETURNED TO THE GATE AND VISUAL INSPECTION REVEALED NO DISCREPANCIES . BORESCOPE INSPECTION WILL BE DONE WITHIN FIVE CYCLES. AIRCRAFT RETURNED TO SERVICE WITHOUT FURTHER INCIDENT. 2 L 7 3 4F 4 F A22WE E20EA 1996101700061 19961017 00061 NE 1996 10 17 9621525529 2 19961008 A 7261 50007436C OIL PUMP BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE NR 1 ENGINE MALFUNCTIONED A A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN J K WARNING INDICATION FLUID LOSS CR CRUISE 1 GL 01 529US 12689 2247 00588 23844 716428 DURING CRUISE FLIGHT, NR 1 ENGINE OIL PRESSURE LIGHT BEGAN TO FLICKER AND OIL QUANTITY INDICATED ZERO. THE NR 1 ENGINE WAS SHUT DOWN. FLIGHT DIVERTED TO DTW AND PERFORMED AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED CHIP DETECTORS, NO ME TAL FOUND. NR 1 ENGINE MAIN OIL PUMP WAS REMOVED AND REPLACED. ENGINE WAS GROUND RUN AND LEAK CHECKED. NO LEAKS NOTED . AIRCRAFT RETURNED TO SERVICE. PART TOTAL CYCLES, 5,208. 2 L 7 2 4F 4 F RT A2NM E17NE 1996101700062 19961017 00062 SO 1996 10 17 COMA9610298 1 19961008 A 3350 10130115 SIGN EMB 120 EMB120RT SO CABIN MISSING A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 205CA 120205 EMERGENCY EXIT SIGN AT ROW 5 IS MISSING. REPLACED EMERGENCY EXIT SIGN. 2 L 7 2 4T RT A31SO 1996101700063 19961017 00063 EU 1996 10 17 COMA9630151 1 19961009 A 5321 FLOORBOARD SAAB SF340 SF340A 7850100 EU COCKPIT CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 320CA 340A064 C1 INSPECTION TASK 117/118-01I. CORROSION UNDER FLOORBOARDS ON RT SIDE OF COCKPIT THRESHOLD UNDER GALLEY AREA. REMOVED CORROSION, CLEANED, PRIMED, AND RESTORED CORROSION PREVENTATIVE COMPOUND. 2 L 7 2 4T RT A52EU 1996101700064 19961017 00064 EU 1996 10 17 COMA9630152 1 19961009 A 5741 7257403001 FITTING SAAB SF340 SF340A 7850100 EU WING CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 320CA 24460 340A064 7-YEAR THRESHOLD, 4-YEAR INTERVAL CHECK. TASK 191-01I, UPPER ATTACH FITTING FOR LEFT WING AFT SPAR TO FUSELAGE FITTING HAS A DEEP GOUGE. C/W NDT INSPECION, BLENDED OUT DAMAGE IAW SRM. AIRCRAFT TOTAL CYCLES, 27,592. 2 L 7 2 4T RT A52EU 1996101700065 19961017 00065 EA 1996 10 17 COMA9660165 1 19961009 A 2750 601R931057 BPSU CNDAIR CL600 CL6002B19 EA LT TE FLAPS MALFUNCTION A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 951CA 4119 254 230 7091 FLAPS FAILED AT FULL DOWN. REPLACED THE LT FLAP BRAKE AND POSITION SENSOR UNIT. PART TOTAL CYCLES, 3,657. 2 L 7 2 4F RT A21EA 1996101700066 19961017 00066 EA 1996 10 17 COMA9660166 1 19961004 A 2760 270003 PCU CNDAIR CL600 CL6002B19 EA LT SPOILERON MALFUNCTION A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 915CA 8275 0076 7013 TAKEOFF ABORTED AT 100 KTS DUE TO CONFIG SPOILERS WARNING. REPLACED LT INBD SPOILER ON POWER CONTROL UNIT. SYSTEM TEST NORMAL. PART TOTAL CYCLES, 7,574. 2 L 7 2 4F RT A21EA 1996101700067 19961017 00067 EA 1996 10 17 COMA9660167 1 19961008 A 2150 321387611 SHUT OFF VALVE CNDAIR CL600 CL6002B19 EA RT PACK JAMMED A COMA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SO 01 940CA 5252 7048 SMOKE IN CABIN AFTER ENGINE START. A.P.U. TEMP REACHED 747 DEGREE DURING ENGINE START. REMOVED DEBRIS THAT WAS JAMMING THE RT AIR CONDITIONING PACK SHUT OFF VALVE. SYSTEM OPERATION NORMAL. PART TOTAL CYCLES, 4,653. 2 L 7 2 4F RT A21EA 1996101700068 19961017 00068 SO 1996 10 17 COMA9610301 1 19961009 A 5320 12008896001 T SECTION EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 152CA 18161 120150 FOUND FUSELAGE FLOOR SUPPORT STRUCTURE T-SECTION CORRODED IN FWD CABIN AREA. REMOVED CORRODED T-SECTION AND INSTALLED N EW PART PER REPORT NR 2057-1, REV. IR, DATED 10-6-96. AIRCRAFT TOTAL CYCLES, 19,871. 2 L 7 2 4T RT A31SO 1996101700069 19961017 00069 SO 1996 10 17 COMA9610300 1 19961009 A 5320 12026671001 BUTT STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 152CA 18161 120150 FOUND FUSELAGE FLOOR SUPPORT STRUCTURE FORWARD LT BUTT STRAP CORRODED. REMOVED CORRODED BUTT STRAP AND INSTALLED NEW PA RT PER EMB120 SRM STANDARD PRACTICES, CH 51-40-02. AIRCRAFT TOTAL CYCLES, 19,871. 2 L 7 2 4T RT A31SO 1996101700070 19961017 00070 SO 1996 10 17 COMA9610299 1 19961009 A 5320 12007089003 BUTT STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 162CA 18161 120150 FOUND FUSELAGE FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP CORRODED. REMOVED CORRODED BUTT STRAP AND INSTALLED NEW PART P ER REPORT NR 1671-1, REV. IR, DATED 10-22-95. AIRCRAFT TOTAL CYCLES, 19,871. 2 L 7 2 4T RT A31SO 1996101700071 19961017 00071 NM 1996 10 17 SWAA961044 1 19961008 A 5330 SKIN BOEING 737 7373H4 1384600 NM ENTRY DR CUTOUT GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED BC4 CHECK, FOUND A FUSELAGE SKIN GOUGED 12 INCHES AND 16 INCHES BELOW AFT ENTRY DOOR. REPAIRED PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1996101700072 19961017 00072 NM 1996 10 17 SWAA961045 1 19961003 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED D-CHECK, FOUND A CRACK INDICATION AT BULKHEAD BS 178, WL 195, LBL 30, SECTION OF SIDE CHORD. REPAIRED PER TRAMCO EWO 96-0461. 2 L 7 2 4F RT A16WE 1996101700073 19961017 00073 NM 1996 10 17 SWAA961046 1 19961003 A 5320 CLIP BOEING 737 7373H4 1384600 NM BS 500/663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 500A, S16R AT BS 663, S10R, AND AT BS 663, S10L. REPLACED ALL PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996101700074 19961017 00074 NM 1996 10 17 SWAA961047 1 19961003 A 5240 DOOR FRAME BOEING 737 7373H4 1384600 NM BS 294.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED D-CHECK, FOUND SERVICE DOOR FWD DOOR FRAME CRACKED AT LOWER SECTION, BS 294.5, WL 208. REPAIRED PER BO EING SRM. 2 L 7 2 4F RT A16WE 1996101700075 19961017 00075 NM 1996 10 17 SWAA961048 1 19961003 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED D-CHECK, FOUND WEB TO FRAME ATTACH ANGLES CRACKED AT BS 360, S10 AND 11L. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996101700076 19961017 00076 NM 1996 10 17 SWAA961049 1 19961003 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 359.5 HOLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED D-CHECK, FOUND A SMALL HOLE IN FUSELAGE SKIN AT BS 359.5, WL 268, LBL 5.7. INSTALLED REPAIR DOUBLER PE R BOEING SRM. 2 L 7 2 4F RT A16WE 1996101700077 19961017 00077 NM 1996 10 17 SWAA961050 1 19961003 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 372.5 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 372.5, WL 210, LBL 70. INSTALLED REPAIR DOUBLER PER BOEING S RM. 2 L 7 2 4F RT A16WE 1996101700078 19961017 00078 NM 1996 10 17 SWAA961051 1 19961003 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 827 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, S9L, AT ANGLE FASTENER HOLE. INSTALLED REPAIR PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1996101700079 19961017 00079 NM 1996 10 17 SWAA961052 1 19961004 A 5320 CLIP BOEING 737 7372H4 138448C NM BS 807 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 90SW 22905 DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER TIE CLIP CRACKED AT S15L, BS 807. REPLACED PER BOEING SR. 2 L 7 2 4F A16WE 1996101700080 19961017 00080 NM 1996 10 17 SWAA961053 1 19961004 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 251 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 90SW 22905 DURING SCHEDULED 1/2 D-CHECK, FOUND FUSELAGE SKIN DAMAGED AT BS 251, S6R. REPAIRED PER BOEING SR. 2 L 7 2 4F A16WE 1996101700081 19961017 00081 NM 1996 10 17 SWAA961054 1 19961004 A 5312 BULKHEAD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKS AROUND FASTENERS, AT WL 234, LBL 10, 11.5, AND 13. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996101700083 19961017 00083 NM 1996 10 17 SWAA961056 1 19961004 A 5312 BULKHEAD ANGLE BOEING 737 7372H4 138448C NM BS 520 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 DURING SCHEDULED D-CHECK, FOUND BULKHEAD SUPPORT ANGLE CORRODED AT BS 520, RBL 26, S26R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996101700084 19961017 00084 NM 1996 10 17 SWAA961057 1 19961004 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 818 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 818, S15 AND 16R. INSTALLED REPAIR DOUBLER PER BOEING SRM. 2 L 7 2 4F A16WE 1996101700085 19961017 00085 NM 1996 10 17 SWAA961058 1 19961004 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 967 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 967, S20L. INSTALLED REPAIR PER BOEING SRM. 2 L 7 2 4F A16WE 1996101700086 19961017 00086 NM 1996 10 17 SWAA961059 1 19961004 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 367 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AFT OF FWD ENTRY DOOR AT BS 367, ABOVE S17L. REPAIRED PER BOEING S RM. 2 L 7 2 4F A16WE 1996101700087 19961017 00087 NM 1996 10 17 SWAA961060 1 19961004 A 5320 DOUBLER BOEING 737 7372H4 138448C NM DOOR CUTOUT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 DURING SCHEDULED D-CHECK, FOUND SERVICE DOOR LOWER AFT CORNER STOP FITTING DOUBLER, FRAME TO SKIN CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996101700088 19961017 00088 NM 1996 10 17 SWAA961061 1 19961003 A 3350 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 93SW 22965 DURING SCHEDULED A2 CHECK, FOUND FWD LT AND RT EXTERNAL EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK PER BO EING M/M. 2 L 7 2 4F A16WE 1996101700089 19961017 00089 NM 1996 10 17 SWAA961062 1 19961003 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 374 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 62SW 22060 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED OUT OF SRM LIMITS AT BS 374, BETWEEN S3 AND 4L. REPAIRED PER BOEIN G SRM. 2 L 7 2 4F A16WE 1996101700090 19961017 00090 NM 1996 10 17 SWAA961063 1 19961003 A 2120 AIR DISTR BOEING 737 7373H4 1384600 NM CABIN ODOR A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 303SW 22943 NOTED ELECTRICAL ODOR IN MID CABIN AREA. INSPECTED ELECTRICAL WIRING AND NOTED NO DEFECTS PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996101700091 19961017 00091 NM 1996 10 17 SWAA961064 1 19961003 A 3350 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 507SW 24184 DURING SCHEDULED SC-CHECK, FOUND CABIN FLOOR TRACK LIGHTING INOPERATIVE AT ROWS 7 AND 8. SECURED WIRING PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996101700092 19961017 00092 NM 1996 10 17 SWAA961065 1 19961002 A 3397 WIRE BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 636WN 27709 DURING SCHEDULED SC-CHECK, FOUND EMERGENCY TRACK LIGHT INOPERATIVE AT ROW 18. RECONNECTED WIRE PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996101700093 19961017 00093 NM 1996 10 17 SWAA961066 1 19961003 A 3350 LIGHT BOEING 737 7372H4 138448C NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 91SW 22963 DURING SCHEDULED SC-CHECK, FOUND RIGHT EMERGENCY EXIT ESCAPE HATCH EMERGENCY LIGHT ASSEMBLY BROKEN. REPLACED LIGHT ASSE MBLY PER BOEING M/M. 2 L 7 2 4F A16WE 1996101700094 19961017 00094 NM 1996 10 17 SWAA961067 1 19961003 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 259.5 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED SC-CHECK, FOUND SKIN DAMAGED AT BS 259.5 UNDER GUSSET FITTING IN UPPER NOSE GEAR AREA. INSTALLED WEB R EPAIR PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996101700095 19961017 00095 NM 1996 10 17 SWAA961068 1 19961003 A 3350 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 64SW 22062 DURING SCHEDULED TERMINAL CHECK, FOUND EMERGENCY TRACK LIGHTING INOPERATIVE AT MID CABIN AREA. RELAMPED PER BOEING M/M. 2 L 7 2 4F A16WE 1996101700096 19961017 00096 NM 1996 10 17 SWAA961069 1 19961003 A 5210 SKIN BOEING 737 7372H4 138448C NM FWD ENTRY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 52SW 21533 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR UPPER HINGE CUTOUT CRACKED IN RADIUS OF OUTER SKIN. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996101700097 19961017 00097 NM 1996 10 17 SWAA961070 1 19961008 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 312 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 312, LBL 45, WL 283. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996101700098 19961017 00098 NM 1996 10 17 SWAA961071 1 19961008 A 5315 FLOOR BEAM BOEING 737 7372H4 138448C NM CABIN CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 312, 328, 270, AND 294. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996101700099 19961017 00099 NM 1996 10 17 SWAA961072 1 19961008 A 5320 CHORD BOEING 737 7372H4 138448C NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 24SW 20925 DURING SCHEDULED TERMINAL CHECK, FOUND BS 727 OUTBOARD CHORD CRACKED AT S18A, LEFT SIDE. FORWARD HOLE. REPAIRED PER BO EING SRM. 2 L 7 2 4F A16WE 1996101700100 19961017 00100 NM 1996 10 17 UPS96221246 1 19961006 A 3350 1000679 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 937UP 2036 19302 FORWARD ENTRY EMERGENCY EXIT LIGHT INOPERATIVE DURING WEEKEND CHECK, LIGHT ASSY JARRED LOOSE DURING LAST LEG. REMOVED B ATTERY PACK AND CHARGED BATTERY OVER THE WEEKEND, OPS CK'ED NORMAL. 2 L 7 3 4F A3WE 1996101700101 19961017 00101 NM 1996 10 17 UPS96221248 1 19961003 A 5753 6521630188 SKIN BOEING 727 727247 138408F NM RT TE FOREFLAP DISBOND A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 211UP BN68 21700 INSPECTION TYPE: C. RIGHT WING INBOARD FOREFLAP 65 FROM INBOARD END UPPER SURFACE HAS SMALL DISBOND. REPAIRED DISBOND ON RT WING INBOARD FOREFLAP IAW SRM 51-40-6. 2 L 7 3 4F A3WE 1996101700102 19961017 00102 NM 1996 10 17 UPS96221249 1 19960927 A 5753 69185582 RIB BOEING 727 727247 138408F NM RT TE FOREFLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 211UP 21700 INSPECTION TYPE: C. RT WING INBOARD MIDFLAP HAS CRACKED NOSE RIB IN L/E AT CENTER FOREFLAP TRACK INBOARD OF TRACK. R EMOVED DAMAGED RIB, INSTALLED NEW RIB, ALL WORK DONE PER SRM'S 51-30-2 AND 51-30-5. 2 L 7 3 4F A3WE 1996101700103 19961017 00103 NM 1996 10 17 UPS96221250 1 19960930 A 5720 SHEAR TIE BOEING 727 727247 138408F NM BS 500 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 211UP 21700 INSPECTION TYPE: C. CORROSION ON SHEAR TIE STA 500 RBL 17-22 WL 150. MECH REMOVED CORROSION FROM SHEAR TIE AT STA 500 RBL 17-22 WL 150. REWORKED DEEMED OUT OF LIMITS IAW SRM 53-10-1. REPAIRED SHEAR TIE IAW SRM 53-10-4. 2 L 7 3 4F A3WE 1996101700104 19961017 00104 NM 1996 10 17 UPS96221251 1 19960930 A 5320 SHEAR TIE BOEING 727 727247 138408F NM BS 950 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 211UP 21700 INSPECTION TYPE: C. CORROSION ON FRAME AROUND FASTENERS AT BS 950F RBL 3 WL 151. REMOVED CORROSION FROM FRAME AT STA 950F RBL 3 WL 151. REWORKED FRAME FOUND TO BE WITHIN LIMITS IAW SRM 53-10-1, HOWEVER, CORROSION WAS FOUND ON SHEAR TIE OUT OF LIMITS IAW SRM 53-10-1. REPAIRED SHEAR TIE IAW SRM 53-10-4. 2 L 7 3 4F A3WE 1996101700105 19961017 00105 NM 1996 10 17 UPS96221252 1 19960930 A 5320 SPLICE BOEING 727 727247 138408F NM BS 675-685 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 211UP 21700 INSPECTION TYPE: C. CORROSION ON STR 28R SPLICE STA 675-685 WL 149. REMOVED, FABRICATED FROM STOCK, AND REPLACED STRI NGER SPLICE IAW SRM'S 51-10-6, 51-10-1, 51-30-2, AND 51-10-5. 2 L 7 3 4F A3WE 1996101700106 19961017 00106 NM 1996 10 17 UPS96221253 1 19960930 A 5320 SPLICE BOEING 727 727247 138408F NM BS 675-685 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 211UP 21700 INSPECTION TYPE: C. CORROSION ON STR 27R SPLICE STA 675-685 AREA MARKED. REMOVED, FABRICATED FROM STOCK, AND REPLACED STRINGER SPLICE IAW SRM'S 51-10-1, 51-10-6, AND 51-10-5 AND 51-30-2. 2 L 7 3 4F A3WE 1996101700107 19961017 00107 NM 1996 10 17 UPS96221254 1 19960930 A 5320 ANGLE BOEING 727 727247 138408F NM BS 610-613 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 211UP 21700 INSPECTION TYPE: C. CORROSION ON SUPPORT ANGLE STA 610-613 RBL 13 WL 158. REMOVED, FABRICATED AND REPLACED ANGLE IAW SRM'S 51-30-2, 53-10-2 AND MM 57-20-31. 2 L 7 3 4F A3WE 1996101700108 19961017 00108 NM 1996 10 17 UPS96221255 1 19961003 A 5320 HAT SECTION BOEING 727 727247 138408F NM BS 304 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 211UP 21700 INSPECTION TYPE: C. CORROSION AT BS 304 RBL 12 WL 207.5 AT HAT SECTION. REMOVED, FABRICATED FROM EXTRUSION STOCK, AND REPLACED FLOOR STRUCTURE HAT SECTION IAW SRM'S 51-30-2, 51-20-4, 51-10-6, 51-10-2. 2 L 7 3 4F A3WE 1996101700109 19961017 00109 NM 1996 10 17 UPS96221256 1 19961002 A 5320 CHANNEL BOEING 727 727247 138408F NM BS 302 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 211UP 21700 INSPECTION TYPE: C. CORROSION AT BS 302 LBL 12-RBL 12 WL 207.5 AT NUTPLATES IN U-CHANNEL. REMOVED, FABRICATED, AND R EPLACED FLOOR STRUCTURE U-CHANNEL IAW SRM'S 51030-3, 51-30-8, 51-20-4, AND 51-10-6, 51-10-2. 2 L 7 3 4F A3WE 1996101700110 19961017 00110 NM 1996 10 17 UPS96221257 1 19961002 A 5320 WEB BOEING 727 727247 138408F NM BS 575-580 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 211UP 21700 INSPECTION TYPE: C. CORROSION ON WEB STA 575-580 RBL 22 WL 152. MECH REMOVED CORROSION, REWORK DEEMED OUT OF LIMITS I AW SRM'S 53-20-1 51-30-2, 51-10-2 AND MM 51-20-151. 2 L 7 3 4F A3WE 1996101700111 19961017 00111 NM 1996 10 17 UPS96221258 1 19961001 A 5311 FRAME BOEING 727 727247 138408F NM BS 720 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 211UP 21700 INSPECTION TYPE: C. CORROSION ON LOWER FLANGE OF FRAME STA 720A WL 149 RBL 7-10. CUT OUT DAMAGED SECTION AND ACCOMPLI SHED REPAIR IAW SRM 53-10-4. 2 L 7 3 4F A3WE 1996101700112 19961017 00112 NM 1996 10 17 UPS96221298 1 19961007 A 5753 652466628 RIB BOEING 727 727247 138408F NM RT TE FORE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 211UP 21700 INSPECTION TYPE: C. RIGHT WING INBOARD MIDFLAP HAS CRACKED RIB AT CENTER FOREFLAP TRACK OUTBOARD RIB. REMOVED AND RE PLACED CRACKED RIB IAW SRM 51-30-2, OHM 57-52-01 MM 27-51-00. 2 L 7 3 4F A3WE 1996101700113 19961017 00113 NM 1996 10 17 UPS96221299 1 19961007 A 5753 SKIN BOEING 727 727247 138408F NM RT TE FORE FLAP DELAMINATION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 211UP 21700 INSPECTION TYPE: C. RIGHT WING INBOARD FOREFLAP HAS AREA OF DELAMINATION ON LOWER SURFACE INBOARD TRAILING EDGE. REPA IRED PER SRM 51-40-06. 2 L 7 3 4F A3WE 1996101700114 19961017 00114 NM 1996 10 17 UPS96221300 1 19961007 A 5320 SHEAR TIE BOEING 727 727247 138408F NM BS 1130 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 211UP 21700 INSPECTION TYPE: C. CORROSION ON SHEAR TIE AT BS 1130 RBL 10 WL 149. REMOVED CORROSION FROM SHEAR TIE AT STA 1130 RBL 10 WL 149. REWORK DEEMED OUT OF LIMITS IAW 53-10-1. REPAIRED SHEAR TIE IAW SRM 53-10-4. 2 L 7 3 4F A3WE 1996101700115 19961017 00115 NM 1996 10 17 UPS96521303 1 19961009 A 3230 273N10037 SEQUENCE VALUE BOEING 757 75724APF 1384969 NM NLG FAILED A IPXA O OTHER P NO WARNING INDICATION AP APPROACH 1 SO 01 447UP 27736 INSPECTION TYPE N/A, NOSE GEAR GREEN DOWN LIGHT FAILED TO ILLUMINATE WITH GEAR HANDLE DOWN. EICAS MESSAGE GEAR DISAGREE AND GEAR DOORS DISPLAYED. DOORS AND GEAR AMBER LIGHTS ILLUMINATED. INDICATIONS WERE NORMAL AFTER ALTERNATE GEAR EXTEN SION. TROUBLESHOT PER FAULT ISOLATION MANUAL 32-20-00 FIG 104, FOUND SEQUENCE VALVE AT FAULT. REMOVED AND REPLACED SAM E PER MM 32-34-05, COMPLIED WITH NOSE GEAR ADJUSTMENT TEST PER 32-34-00 AND 07-11-02. NO DEFECTS NOTED, (P/N 2670288-7) ON, (P/N 2670288-9) OFF, (S/N 2204) ON, (S/N 0260) OFF. 2 L 7 2 4F RT A2NM 1996101700116 19961017 00116 WP 1996 10 17 UPS96821259 1 19960909 A 5320 36410042N FITTING DOUG DC8 DC873F 302199F WP BS 879 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. FS 879 LONGERON 24R B/T FITTING IS CRACKED. REPLACED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996101700117 19961017 00117 WP 1996 10 17 UPS96821260 1 19960925 A 5320 WEB DOUG DC8 DC873F 302199F WP BS 980 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. RT WHEELWELL FS 980 CENTER FRAME INNER WEB CRACKED AT SPLICE. REPAIRED WEB PER SRM 53-2-0. 2 L 7 4 4F RT 4A25 1996101700118 19961017 00118 WP 1996 10 17 UPS96821261 1 19960909 A 5320 4750426501 FITTING DOUG DC8 DC873F 302199F WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. CRACKED FITTING FS 680 LONGERON 36. REPLACED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996101700119 19961017 00119 WP 1996 10 17 UPS96821262 1 19960903 A 5320 46495771 FITTING DOUG DC8 DC873F 302199F WP WS 410 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. LT WS XRS410 CANOE FITTING OUTBOARD SIDE BRACE FITTING CRACKED INSIDE CHANNEL. REPLACED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996101700120 19961017 00120 WP 1996 10 17 UPS96821264 1 19960903 A 5712 5770123 RIB DOUG DC8 DC873F 302199F WP LT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. LT WING LEADING EDGE 9 EA RIBS CRACKED AT WS XFS730, XFS750, XFS755 , XFS760, XFS765, XFS775, XF S780, XFS785 AND XFS800. REPAIRED RIBS PER MM 57-00-00 FIG 801. 2 L 7 4 4F RT 4A25 1996101700121 19961017 00121 WP 1996 10 17 UPS96821265 1 19960903 A 5712 5770123 RIB DOUG DC8 DC873F 302199F WP RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. RT WING LEADING EDGE UPPER RIB CRACK AT STA XFS560. REPAIRED RIB PER MM 57-00-00 FIG 801. 2 L 7 4 4F RT 4A25 1996101700122 19961017 00122 WP 1996 10 17 UPS96821266 1 19960909 A 5320 36169482 FITTING DOUG DC8 DC873F 302199F WP BS 700 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. FS 700 FLOOR BEAM TO LONGERON 23R FITTING IS CRACKED. REPLACED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996101700123 19961017 00123 WP 1996 10 17 UPS96821280 1 19960831 A 5752 5717798501 TRIM TAB DOUG DC8 DC873F 302199F WP LT AILERON DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. LT AILERON TRIM TAB DELAMINATED. REPLACED TAB PER MM 27-13-01. 2 L 7 4 4F RT 4A25 1996101700124 19961017 00124 WP 1996 10 17 UPS96821281 1 19960904 A 5755 3655456 FITTING DOUG DC8 DC873F 302199F WP NR 4 SPOILER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. 2 EA LT WING NR 4 SPOILER INBOARD AND OUTBOARD ATTACH FITTINGS CRACKED. REPLACED FITTINGS PER M M 27-61-01. 2 L 7 4 4F RT 4A25 1996101700125 19961017 00125 WP 1996 10 17 UPS96821282 1 19960903 A 5210 SKIN DOUG DC8 DC873F 302199F WP MAIN ENTRY DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. FORWARD ENTRY DOOR OUTER SKIN LOWER FWD CORNER CRACKED. REPAIRED SKIN PER SRM 52-2-0. 2 L 7 4 4F RT 4A25 1996101700126 19961017 00126 WP 1996 10 17 UPS96821283 1 19960831 A 5210 975106530 FITTING DOUG DC8 DC873F 302199F WP AFT ENTRY DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. LT AFT ENTRY DOOR FITTING CRACKED INSIDE 2ND LIGHTNING HOLE FROM TOP FWD SIDE. REPLACED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996101700127 19961017 00127 WP 1996 10 17 UPS96821284 1 19960903 A 5712 5770123 RIB DOUG DC8 DC873F 302199F WP LT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. LT WING LEADING EDGE ASSY 7 EA RIBS CRACKED AT WS XFS985 LOWER, XFS 600 UPPER, XFS605 UPPER, XFS 610 UPPER, XFS615 UPPER, XFS625 UPPER AN D XFS645 UPPER RIBS. REPAIRED RIBS PER MM 57-00-00 FIG 801. 2 L 7 4 4F RT 4A25 1996101700128 19961017 00128 WP 1996 10 17 UPS96821285 1 19960903 A 5712 5770123 RIB DOUG DC8 DC873F 302199F WP LT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. LT WING LEADING EDGE ASSY 7 EA RIBS CRACKED AT WS XFS550 UPPER, XFS 565 LOWER, XFS565 UPPER, XFS 570 UPPER, XFS575 UPPER, XFS580 UPPER AN D XFS585 UPPER RIBS. REPAIRED PER MM 57-00-00 FIG 801 2 L 7 4 4F RT 4A25 1996101700129 19961017 00129 WP 1996 10 17 UPS96821304 1 19960911 A 5400 580273865 DOUBLER DOUG DC8 DC873F 302199F WP NR 2 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. NR 2 PYLON LOWER DOUBLER JUST ABOVE T-DOUBLER CRACKED ON FWD SIDE. REPAIRED PER UPS EO'S DC8-57- 0717/-0726. 2 L 7 4 4F RT 4A25 1996101700130 19961017 00130 WP 1996 10 17 UPS96821305 1 19960903 A 5313 5750198501 LONGERON DOUG DC8 DC873F 302199F WP BS 857 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. LONGERON 24L CRACKED (3 EA) AT BOTTLE BOLT HOLE FS 857. REPLACED LONGERON SECTION PER DAC DRAWI NGS NR 5779948 AND 5779938. 2 L 7 4 4F RT 4A25 1996101700131 19961017 00131 WP 1996 10 17 UPS96821306 1 19960911 A 5720 5769600 DOUBLER DOUG DC8 DC873F 302199F WP LT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. LT WING LEADING EDGE SKIN DOUBLER CRACKED AT DRAIN HOLE STA XFS597 **(MRR FILED OPEN)** REPAI RED PER UPS EO. 2 L 7 4 4F RT 4A25 1996101700132 19961017 00132 WP 1996 10 17 UPS96821307 1 19960909 A 5320 5750127 TRAP FITTING DOUG DC8 DC873F 302199F WP LT MLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. LT TRAPEZOID FITTING CRACKED IN VERTICAL WEB. REPLACED FITTING PER DAC DRAWING NR 5750127. 2 L 7 4 4F RT 4A25 1996101700133 19961017 00133 WP 1996 10 17 UPS96821308 1 19960913 A 5720 56422052 FITTING DOUG DC8 DC873F 302199F WP RSS 97 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. FLAP SUPPORT FITTING CRACKED AND CORRODED ON RT WING REAR SPAR STA 97. REPAIRED PER UPS EO DC8- 57-0720. 2 L 7 4 4F RT 4A25 1996101700134 19961017 00134 WP 1996 10 17 UPS96821309 1 19960913 A 5720 74748374 FITTING DOUG DC8 DC873F 302199F WP RRS 98 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. FLAP ACTUATOR ATTACH FITTING CRACKED AND CORRODED ON RT WING REAR SPAR STA 98. REPLACED FITTING PER MM 20-16-00. 2 L 7 4 4F RT 4A25 1996101700135 19961017 00135 NM 1996 10 17 96FDEA01571 1 19961008 A 5330 651842012 SKIN BOEING 727 72725 1384006 NM BS 254 CREASED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 511FE 18283 NR0145 AND 018, CREASE ON SKIN AT BS 254 STR 20 TO 21R. *S/D* REMOVED DAMAGE FROM SKIN AT BS 254 BETWEEN STR 20 TO 21R , FABRICATED AND INSTALLED REPAIR PER FEDEX SRM 53-30-03. 2 L 7 3 4F A3WE 1996101700136 19961017 00136 NM 1996 10 17 MWEA96530 1 19961009 A 3350 BATTERIES DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 601ME 49762 CREW REPORTS DURING RECEIVING CHECK, THE TWO FORWARD OVERWING EMERGENCY LIGHTS ARE INOPERATIVE. MAINT. REPLACED BATTERI ES IN POWER SUPPLY. OPS CHECK GOOD. 2 L 7 2 4F RT A6WE 1996101700137 19961017 00137 WP 1996 10 17 MWEA96531 1 19961010 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 602ME 48133 DURING A CHECK, FOUND FWD CABIN EMERGENCY CEILING LIGHTS WOULD NOT EXTINGUISH. MAINT. REPLACED D-CELL BATTERIES IN POWE R SUPPLY. OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996101700138 19961017 00138 NM 1996 10 17 P5CA9600763 1 19961009 A 5400 ANGLE BOEING 747 747122 1384872 NM NR 2 ENGINE CHAFED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 NR 2 ENGINE FWD NOSE FAIRING AFT LT/RT ANGLES AND BRACKETS WITH DEEP CHAFE MARKS. BURNISHED ANGLES AND BRACKET IAW SRM 53-10-01. REPLACED ANGLE ON FWD NOSE FAIRING IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996101700139 19961017 00139 NM 1996 10 17 P5CA9600764 1 19961009 A 7830 TR SKIN BOEING 747 747122 1384872 NM NR 1 ENGINE SEPARATING A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 NR 1 ENGINE INBOARD SIDE OF T/R COWL AT 4 O'CLOCK POSITION SKIN SEPARATING. REBONDED SKINS IAW SRM'S 51-21-04 AND 51-70 -00. 2 L 7 4 4F A20WE 1996101700140 19961017 00140 NM 1996 10 17 P5CA9600765 1 19961008 A 7110 COWL SKIN BOEING 747 747122 1384872 NM NR 2 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 NR 2 ENGINE O/B CORE COWL BREATHER EXHAUST OUTER SKIN CRACKED ALONG WELD JOINT AREA. SKIN REWELDED AT JOINT IAW SRM 51- 10-40. 2 L 7 4 4F A20WE 1996101700141 19961017 00141 NM 1996 10 17 P5CA9600766 1 19961009 A 7110 COWL SKIN BOEING 747 747122 1384872 NM NR 3 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 NR 3 ENGINE RT FAN COWL HANGER FAIRING FWD HINGE CUTOUT SKIN CRACKED AT 1 O'CLOCK POSITION. BLENDED OUT MINOR CRACK AND SMOOTHED OUT AREA IAW SRM 51-10-01. 2 L 7 4 4F A20WE 1996101700142 19961017 00142 NM 1996 10 17 P5CA9600767 1 19961009 A 7110 COWL SKIN BOEING 747 747122 1384872 NM NR 3 ENGINE GOUGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 NR 3 ENGINE O/B CORE COWL INNER SKIN AND ANGLES CAVE-IN, GOUGED, AND WORN OUT 7 EA LOCATIONS. BLENDED OUT GOUGE IAW SR M 51-10-01. 2 L 7 4 4F A20WE 1996101700143 19961017 00143 NM 1996 10 17 P5CA9600768 1 19961009 A 5414 SKIN BOEING 747 747122 1384872 NM RT INBD SAILBOAT DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 RIGHT HAND INBOARD SAILBOAT INNER SKIN HAS A HOLE. CLEANED, APPLIED FILLER, HOT BONDED DOUBLER IN PLACE IAW SRM 51-40-0 6. 2 L 7 4 4F A20WE 1996101700144 19961017 00144 NM 1996 10 17 P5CA9600769 1 19961009 A 5414 SKIN BOEING 747 747122 1384872 NM NR 3 SAILBOAT DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 NR 3 ENGINE I/B O/B SAILBOAT FAIRING INNER SKIN HAS A HOLE. REPAIRED WITH METAL TO METAL BOND IAW SRM 51-40-06. 2 L 7 4 4F A20WE 1996101700145 19961017 00145 NM 1996 10 17 P5CA9600770 1 19961008 A 5720 BRACKET BOEING 747 747124 1384874 NM LT FUEL PANEL BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEFT WING FUEL PANEL HOLD OPEN BRACKET BROKEN. REPAIRED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996101700146 19961017 00146 NM 1996 10 17 P5CA9600771 1 19961005 A 7110 ANGLE BOEING 747 747122 1384872 NM NR 4 ENGINE COWL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 NR 4 ENGINE INBOARD CORE COWL LOWER HOT SECTION ANGLE IS CRACKED IN TWO PLACES. FABRICATED NEW ANGLE AND INSTALLED IAW SRM 51-10-01. 2 L 7 4 4F A20WE 1996101700147 19961017 00147 NM 1996 10 17 P5CA9600772 1 19961005 A 7110 SKIN BOEING 747 747122 1384872 NM NR 2 ENGINE COWL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 NR 2 ENGINE OUTBOARD CORE COWL SECOND FROM FWD LATCH CUTOUT IS CRACKED. FABRICATED NEW LONGERON AND INSTALLED IAW SRM 5 1-40-03. 2 L 7 4 4F A20WE 1996101700148 19961017 00148 NE 1996 10 17 P5CA9600773 2 19961005 A 7250 R RAIL BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 1 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 67915 3149 19753 662231 NR 1 ENGINE 'R' RAIL IS CRACKED AT THE 7 O'CLOCK POSITION. WELDED, STRESS RELIEVED, AND PEENED IAW MM 72-53-01. PART T OTAL CYCLES, 15,294. 2 L 7 4 4F 4 F A20WE E20EA 1996101700149 19961017 00149 NM 1996 10 17 P5CA9600774 1 19961005 A 5400 FAIRING BOEING 747 747122 1384872 NM NR 3 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 NR 3 PYLON FORWARD FAIRING AFT OUTBOARD EDGE CRACKED AND RIVETS SHEARED. FABRICATED AND INSTALLED REPAIR DOUBLER AND FI LLER IAW SRM 51-40-03. 2 L 7 4 4F A20WE 1996101700150 19961017 00150 NM 1996 10 17 P5CA9600775 1 19961005 A 5400 DOUBLER BOEING 747 747122 1384872 NM NR 2 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 NR 2 PYLON OUTBOARD MID SPAR PIN FITTING LUG DOUBLER IS CRACKED. FABRICATED AND INSTALLED NEW DOUBLER IAW SRM 51-30-04. 2 L 7 4 4F A20WE 1996101700151 19961017 00151 WP 1996 10 17 SRAA961004 1 19961006 A 5720 57541084 WING TIP DOUG DC8 DC873F 302199F WP RT WING DAMAGED A SRAA K NONE O OTHER TX TAXI/GRND HDL 1 GL 23 873SJ 46091 WHILE ON GROUND AT SIN, AIRCRAFT'S RIGHT WING TIP GOT STRUCK BY GROUND EQUIPMENT. REMOVED AND REPLACED RIGHT WING TIP P ER DOUGLAS M.M. CH 57-24. 2 L 7 4 4F RT 4A25 1996101700249 19961017 00249 SW 1996 10 17 96ZZZX5165 1 19960822 A 2150 ES570084 SWITCH BELL 206 206L4 1182110 SW AIR COND SYS FAILED A NYBA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 11 123NH 52076 PILOT REPORTED SEEING SMOKE APPEAR FROM THE AIR CONDITIONER VENTS AND BY GROUND PERSONNEL SEEING SMOKE APPEAR FROM TAILB OOM AND AIR CONDITIONER DUCT AREAS. INSPECTION OF THE AIR CONDITIONER SYSTEM REVEALED THE HIGH PRESSURE SWITCH FAILED C AUSING THE RECEIVER/DRYER RELIEF PLUG TO BLOW. FREON FROM THE RECEIVER/DRYER WAS DRAWN INTO THE CONDENSER BLOWER MOTOR CAUSING FREON TO ENTER AIRCRAFT THROUGH THE VENTS. FREON VAPOR WAS MISTAKEN AS SMOKE. REPLACED HIGH PRESSURE SWITCH AL ONG WITH RECEIVER DRYER IAW KEITH PRODUCTS MM. 1 G 7 1 3U NC H2SW 1996101700250 19961017 00250 EU 1996 10 17 VTZA96343 1 19960827 A 2752 AIR864600 ACTUATOR BAG JETSTM JETSTM3201 1500217 EU TE FLAPS FAILED A A VTZA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 27 492UE 790 ALB/IAD - FLT 6255 - DURING APPROACH FLIGHT AT 1120 HOURS ON 8-27-96, ABORTED APPROACH DUE TO SELECTING FLAPS TO 20 DEG REES, FLAPS SLOWLY CONTINUED TO 35 DEGREES. MAINTENANCE TROUBLESHOT AND INSPECTED FLAPS. REMOVED AND REPLACED THE ACTU ATOR, LOCK VALVE, EMERGENCY RELIEF VALVE, SELECTOR VALVE, WARNING HORN, AND UNLOCK LIGHT. ALL SYSTEMS FUNCTIONED PROPER LY IAW MM. MAINTENANCE THEN RELEASED THE AIRCRAFT FOR SERVICE. REF: OPERATOR CONTROL NRS 96ZZZX5166, 96ZZZX5167, 96ZZ ZX5168, 96ZZZX5169, AND 96ZZZX5170. (X) 2 L 7 2 4T RT A56EU 1996101700251 19961017 00251 EU 1996 10 17 96ZZZX5166 1 19960827 A 2750 6981A LOCK VALVE BAG JETSTM JETSTM3201 1500217 EU TE FLAPS MALFUNCTIONED A VTZA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 27 492UE 790 ALB/IAD - FLT 6255 - DURING APPROACH FLIGHT AT 1120 HOURS ON 8-27-96, ABORTED APPROACH DUE TO SELECTING FLAPS TO 20 DEG REES, FLAPS SLOWLY CONTINUED TO 35 DEGREES. MAINTENANCE TROUBLESHOT AND INSPECTED FLAPS. REMOVED AND REPLACED THE ACTU ATOR, LOCK VALVE, EMERGENCY RELIEF VALVE, SELECTOR VALVE, WARNING HORN, AND UNLOCK LIGHT. ALL SYSTEMS FUNCTIONED PROPER LY IAW MM. MAINTENANCE THEN RELEASED THE AIRCRAFT FOR SERVICE. REF: OPERATOR CONTROL NRS VTZA96343, 96ZZZX5167, 96ZZZ X5168, 96ZZZX5169, AND 96ZZZX5170. 2 L 7 2 4T RT A56EU 1996101700252 19961017 00252 EU 1996 10 17 96ZZZX5167 1 19960827 A 2750 8661D EMER RELIEF VLV BAG JETSTM JETSTM3201 1500217 EU TE FLAPS MALFUNCTIONED A VTZA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 27 492UE 790 ALB/IAD - FLT 6255 - DURING APPROACH FLIGHT AT 1120 HOURS ON 8-27-96, ABORTED APPROACH DUE TO SELECTING FLAPS TO 20 DEG REES, FLAPS SLOWLY CONTINUED TO 35 DEGREES. MAINTENANCE TROUBLESHOT AND INSPECTED FLAPS. REMOVED AND REPLACED THE ACTU ATOR, LOCK VALVE, EMERGENCY RELIEF VALVE, SELECTOR VALVE, WARNING HORN, AND UNLOCK LIGHT. ALL SYSTEMS FUNCTIONED PROPER LY IAW MM. MAINTENANCE THEN RELEASED THE AIRCRAFT FOR SERVICE. REF: OPERATOR CONTROL NRS VTZA96343, 96ZZZX5166, 96ZZZ X5168, 96ZZZX5169, AND 96ZZZX5170. 2 L 7 2 4T RT A56EU 1996101700253 19961017 00253 EU 1996 10 17 96ZZZX5168 1 19960827 A 2750 7445B SELECTOR VALVE BAG JETSTM JETSTM3201 1500217 EU TE FLAPS MALFUNCTIONED A VTZA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 27 492UE 790 ALB/IAD - FLT 6255 - DURING APPROACH FLIGHT AT 1120 HOURS ON 8-27-96, ABORTED APPROACH DUE TO SELECTING FLAPS TO 20 DEG REES, FLAPS SLOWLY CONTINUED TO 35 DEGREES. MAINTENANCE TROUBLESHOT AND INSPECTED FLAPS. REMOVED AND REPLACED THE ACTU ATOR, LOCK VALVE, EMERGENCY RELIEF VALVE, SELECTOR VALVE, WARNING HORN, AND UNLOCK LIGHT. ALL SYSTEMS FUNCTIONED PROPER LY IAW MM. MAINTENANCE THEN RELEASED THE AIRCRAFT FOR SERVICE. REF: OPERATOR CONTROL NRS VTZA96343, 96ZZZX5166, 96ZZZ X5167, 96ZZZX5169, AND 96ZZZX5170. 2 L 7 2 4T RT A56EU 1996101700255 19961017 00255 EU 1996 10 17 96ZZZX5170 1 19960827 A 3260 UNLOCK LIGHT BAG JETSTM JETSTM3201 1500217 EU NLG MALFUNCTIONED A VTZA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 EA 27 492UE 790 ALB/IAD - FLT 6255 - DURING APPROACH FLIGHT AT 1120 HOURS ON 8-27-96, ABORTED APPROACH DUE TO NOSE GEAR RED UNLOCKED L IGHT WOULD NOT ILLUMINATE. MAINTENANCE TROUBLESHOT AND INSPECTED LANDING GEAR WITH NO FAULTS FOUND. REMOVED AND REPLAC ED THE ACTUATOR, LOCK VALVE, RELIEF VALVE, SELECTOR VALVE, WARNING HORN, AND UNLOCK LIGHT. ALL SYSTEMS FUNCTIONED PROPE RLY IAW MM. MAINTENANCE THEN RELEASED THE AIRCRAFT FOR SERVICE. REF: OPERATOR CONTROL NRS VTZA96343, 96ZZZX5166, 96ZZ ZX5167, 96ZZZX5168, AND 96ZZZX5169. 2 L 7 2 4T RT A56EU 1996101700256 19961017 00256 CE 1996 10 17 96ZZZX5171 1 19960507 A 3230 BREAKER BEECH 99 C99 1154006 CE MLG CONTROL TRIPPED A HSYA O OTHER J WARNING INDICATION CL CLIMB 1 NM 05 167EE U167 CPR - LANDING GEAR WOULD NOT RETRACT COMPLETELY WHEN IT WAS RETRACTED THE SECOND TIME DURING CLIMB-OUT. PILOT FOUND LAN DING GEAR CONTROL CIRCUIT BREAKER WAS TRIPPED DUE TO BEING TRIPPED BY LANDING GEAR MOTOR TIME DELAY RELAY. VERIFIED COR RECT OPERATION OF GEAR BY PERFORMING GEAR SWING ON JACKS. AIRCRAFT WAS TEST FLOWN, THE GEAR OPERATED CORRECTLY. 1 L 7 2 3T A14CE 1996101700257 19961017 00257 CE 1996 10 17 96ZZZX5172 1 19960910 A 3260 993640201 SWITCH BEECH 99 C99 1154006 CE RT MLG OUT OF RIG A HSYA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 05 167EE U167 DEN - FLT 8511 - AFTER TAKEOFF, GEAR HANDLE WOULD NOT MOVE TO THE 'UP' POSITION. PILOT OVERRODE THE RELASE SWITCH AND M OVED HANDLE TO 'UP' POSITION, BUT GEAR REMAINED DOWN. HANDLE WAS SELECTED DOWN. AIRCRAFT RETURNED TO BASE. RIGHT MLG SAFETY SWITCH (WEIGHT-ON-WHEELS) OUT OF RIG. 1 L 7 2 3T A14CE 1996101700258 19961017 00258 NM 1996 10 17 USAASB96192 1 19960913 A 5244 DOOR BOEING 737 737301 1384611 NM EXTERNAL POWER NOT CLOSED A USAA A UNSCHED LANDING E W VIBRATION/BUFFET INADEQUATE Q C CR CRUISE 1 EA 19 592US 23937 CLT - FLT 1635 - AIRCRAFT DEVELOPED AN AIRFRAME VIBRATION AT LEVEL OFF AT FL 260. AFTER CHECKING THAT ALL AIRCRAFT SYST EMS WERE NORMAL, THE CAPTAIN DECIDED TO DIVERT TO CLT. THE CAPTAIN BELIEVED THERE WAS AN ACCESS DOOR OPEN. THE FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND AND CONFIRMED THE EXTERNAL POWER ACCESS DOOR WAS OPEN CAUSING VIBRAT IONS. DOOR WAS CHECKED FOR DEFECTS AND FOUND OK. SECURED DOOR. NO OTHER DEFECTS FOUND. (X) 2 L 7 2 4F RT A16WE 1996101700259 19961017 00259 NM 1996 10 17 AWXA960477 1 19960708 A 3397 WIRE BOEING 737 73733A 1384673 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 509DC 23636 PHX - FLT 0543 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT INOPERATIVE AT ROW 16. REPAIRED BROKEN WIRE. O SP CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1996101700263 19961017 00263 GL 1996 10 17 96ZZZX5175 1 19960911 A 6710 KUP14D5524 RELAY ENSTRM F28 F28F 3300412 GL CYCLIC TRIM STUCK CONTACTS C L A PP0M A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 WP 01 890JR 1394 764 POINTS IN RELAY FUSE TOGETHER CAUSING RUNAWAY TRIM ACTION RESULTING IN UNCONTROLLED ATTITUDES OF ACFT. REQUIRES TWO PIL OTS ON CYCLIC TO OVERRIDE AND LAND ACFT. RELAY MFG (SIEMENS) HAS INDICATED THIS MAY NOT BE THE CORRECT RELAY FOR THIS A PPLICATION. INSTALLED NEW RELAYS PER MM, SDB, AND AD. NOTE: A SINGLE PILOT MAY NOT BE ABLE TO RECOVER AND LAND SAFELY . THIS PROBLEM HAS BEEN OCCURRING SINCE 2-92. 1 G 7 1 3O H1CE 1996101700265 19961017 00265 WP 1996 10 17 HAL96124 1 19960825 A 2750 3922841543 BUSS CABLE DOUG DC9 DC951 3022051 WP TE FLAPS BROKEN A HALA D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 EICBI 48122 OGG - FLT 525 - (BLOCK TURN BACK) ON 15 DEGREE FLAP SELECT, FLAP INDICATOR INDICATED SPLIT FLAP POSITION 12 DEGREES RIG HT, 15 DEGREES LEFT. FOUND FLAP BUSS CABLE BROKEN. REPLACED LEFT FLAP BUSS CABLE PER MM 27-50-0. (CABLE RUN 33A). RIG AND OPS CHECK OK. (X) 2 L 7 2 4F A6WE 1996101700266 19961017 00266 CE 1996 10 17 96ZZZX5177 1 19960806 A 3240 BRAKE CESSNA 402 402CESSNA 207590K CE RT MLG FAILED A A AJZA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 19 4055Q 4020155 WHILE TAXIING, PILOT ATTEMPTED TO USE THE BRAKES AND REPORTED THE LEFT BRAKE LOCKED UP AND THE RIGHT BRAKE FAILED CAUSIN G THE AIRCRAFT TO VEER LEFT OFF THE TAXIWAY INTO A DITCH WITH SUFFICIENT FORCE TO COLLAPSE THE NOSE GEAR BY BREAKING THE RETRACT LINKAGE AND TEARING THE RT DRAG FROM ITS MOUNTING IN THE WHEELWELL. AFTER REMOVING THE AIRCRAFT FROM THE DITCH , MAINTENANCE CHECKED THE BRAKES FOR PROPER OPERATION, NO DEFECT WAS FOUND. INSPECTED THE BRAKE SYSTEM, NO DEFECTS WERE FOUND. NOTE: SINCE THE OCCURRENCE OF THIS INCIDENT, THERE HAVE BEEN PREVIOUS REPORTS OF THIS PHENOMENON. 1 L 7 2 3O A7CE 1996101700267 19961017 00267 WP 1996 10 17 HAL96123 1 19960823 A 3350 LIGHT DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 699HA 47763 HNL - EMERGENCY FLOOR LIGHTS INOPERATIVE FROM OVERWING EXIT UNTIL AFT OF CABIN. REPLACED BATTERY PACKS AND CONDITION SA ME. REPLACED AFT FLOOR LIGHTING STRIP AND OPERATION CHECK WAS GOOD. 2 L 7 2 4F A6WE 1996101700268 19961017 00268 CE 1996 10 17 C2XA96CL031 1 19960909 A 2121 1143800281 BLOWER BEECH 1900 1900D 1154162 CE COCKPIT FAILED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 87551 1006 850 UE206 FLT 3013 - CREW REPORTED A STRONG SMELL OF SMOKE IN THE COCKPIT AND CABIN, GREY SMOKE WAS ALSO VISIBLY OBSERVED. MAINTE NANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED THE FORWARD VENT BLOWER IAW B1900D MM 21-10-01. OPERATIONAL CHECKS WE RE GOOD, AIRCRAFT RETURNED TO SERVICE. ACFT TT: 1,005.9 HOURS. ACFT TC: 1,196. 2 L 7 2 4T RT A24CE 1996101700269 19961017 00269 EU 1996 10 17 C2XA96BT009 1 19960910 A 2150 22051201 ACM AEROSP ATR72 ATR72212 EU LEFT FAILED A C2XA A UNSCHED LANDING M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 12903 459 BDL/EWR-BGR - FLT 3396 - EN ROUTE EWR TO BGR, CREW REPORTED 'SULFA ODOR IN CABIN AND COCKPIT WITH PACKS ON'. AIRCRAFT D IVERTED INTO BDL UNEVENTFULLY. AIRCRAFT WAS INSPECTED AND FERRIED BACK TO EWR WITH BOTH PACKS OFF AND UNPRESSURIZED. DU RING FURTHER CHECKS IN EWR DETERMINED LT ACM TO BE INOPERATIVE. AIRCRAFT RELEASED IAW MEL 21-50-01 PLACARD NR 895339, A ND RETURNED TO SERVICE. AIRCRAFT RON BDL ON 9-12-96 WHERE THE LT COOLING TURBINE (ACM) WAS REMOVED AND REPLACED, OPERAT IONALLY CHECKED GOOD. THE MEL ITEM WAS REMOVED AND AIRCRAFT RETURNED TO SERVICE. ACFT HOURS: 1,775.7. ACFT CYCLES, 1 ,730. (X) 2 H 7 2 4T RT A53EU 1996101700270 19961017 00270 EU 1996 10 17 AWXA960437 1 19960729 A 3350 321430 BATTERY PACK AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 640AW 3372 448 PHX - FLT 2249 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT INTERMITTENTLY INOPERATIVE THROUGHOUT CABIN. M ID-RIGHT BATTERY DEAD. REMOVED AND REPLACED BATTERY PACK. OPERATIONS CHECK GOOD. (X) 2 L 7 2 4F RT A28NM 1996101700271 19961017 00271 EU 1996 10 17 AWXA960435 1 19960729 A 3350 321430 BATTERY PACK AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 640AW 5962 448 PHX - FLT 2249 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT FORWARD INOPERATIVE. FORWARD BATTERY DEAD. RE MOVED AND REPLACED BATTERY PACK. OPERATES GOOD. (X) 2 L 7 2 4F RT A28NM 1996101700276 19961017 00276 WP 1996 10 17 CALA9601444 1 19961013 A 3244 500K424 TIRE DOUG DC10 DC1010 3022110 WP NR 4 FAILED A CALA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SW 09 68044 46903 NUMBER FOUR MAIN LANDING GEAR TIRE BLEW ON TAKEOFF. REMOVED AND REPLACED NUMBER FOUR MAIN LANDING GEAR TIRE PER MM 32-4 5-01. 2 L 7 3 4F A22WE 1996101700277 19961017 00277 NM 1996 10 17 CALA9601445 1 19961012 A 2910 BACH8A04NN0260 LINE BOEING 737 737130 1384435 NM NR 1 ENGINE LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 09 59207 19024 LOSS OF A-SYSTEM HYD ON SHORT FINAL. A-SYSTEM PUMPS TURNED OFF. FOUND BLOWN PRESSURE LINE AT FORWARD WHEEL WELL WALL. REMOVED AND REPLACED LINE AND NR 1 ENGINE HYD PUMP PER MM 29-11-32 AND REPLACED SYSTEM CASE DRAIN FILTERS PER MM 29-11- 41. 2 L 7 2 4F A16WE 1996101700278 19961017 00278 NM 1996 10 17 CALA9601446 1 19961013 A 2912 CLAMP BOEING 727 727243 138408D NM A-SYS FILTER BROKEN A CALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 09 579PE 21662 ON APPROACH, GEAR EXTENDED NORMAL THEN FLAPS SELECTED TO 30, A-SYTEM QUANTITY REDUCED TO 0. SYSTEM PUMPS WERE TURNED OF F. FOUND A-SYSTEM RETURN FILTER MOUNT CLAMP BROKEN. REPLACED RETURN FILTER ASSEMBLY PER MM 29-11-102 AND REPLACED ENGI NE A-PUMP, EDP CASE DRAIN FILTER, PRESSURE FILTER AND FLUSHED A-SYSTEM PER MM 29-11-33, MM 29-11-41, MM 29-11-41 AND 29 -11-0. 2 L 7 3 4F RT A3WE 1996101700279 19961017 00279 NM 1996 10 17 CALA9601447 1 19961012 A 2910 LINE BOEING 737 737130 1384435 NM NR 2 ENGINE LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 09 77215 19032 LOSS OF A-SYSTEM HYDRAULICS. FOUND PRESSURE LINE FROM NR 2 ENGINE LEAKING. REPLACED LINE AND BOTH ENGINE DRIVEN AND EL ECTRIC HYDRAULIC PUMPS AND REPLACED ALL FILTERS PER MM 29-11-32 AND 29-12-21. 2 L 7 2 4F A16WE 1996101700280 19961017 00280 NE 1996 10 17 CALA9601448 2 19961012 A 7230 798207 C7 BLADE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE NR 1 ENGINE BROKEN A CALA A E UNSCHED LANDING ENGINE SHUTDOWN Y ENGINE STOPPAGE CR CRUISE 1 SW 09 16895 49394 716792 NUMBER 1 ENGINE COMPRESSOR STALLED TWICE THEN FAILED. SHUT DOWN PROCEDURE ACCOMPLISHED. PRELIM INSP FOUND METAL IN THE TAILPIPE. REPLACED NUMBER 1 ENGINE PER MM 71-00-00. *S/D* SHOP FINDINGS REVEALED A BROKEN C-7 BLADE AS THE PRIMARY C AUSE OF ENGINE FAILURE. 2 L 7 2 4F 4 F A6WE E9NE 1996101700281 19961017 00281 NM 1996 10 17 CALA9601449 1 19960917 A 5730 PANEL BOEING 727 727232 1384082 NM RT WING TE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 RIGHT WING TRAILING EDGE PANEL ATTACHED TO INBOARD END OF GEAR BEAM HAS AREA WORN THROUGH AND CRACKED INBOARD OF NR 8 SP OILER AREA. REMOVED PANEL, ACCOMPLISHED HOT BOND REPAIR AND REINSTALLED PER SRM 51-40-6. 2 L 7 3 4F A3WE 1996101700282 19961017 00282 NM 1996 10 17 CALA9601450 1 19960918 A 5720 BRACKET BOEING 727 727232 1384082 NM RT WING LE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 RIGHT WING BRACKET HAS CORROSION INSIDE FIXED L/E AT OUTBOARD SIDE OF NR 5 L/E FLAP OUTBOARD HINGE. REMOVED FABRICATED AND INSTALLED REPLACEMENT BRACKET PER SRM 51-10-1 AND 51-10-2. 2 L 7 3 4F A3WE 1996101700283 19961017 00283 NM 1996 10 17 CALA9601451 1 19960918 A 5315 FLOOR BEAM BOEING 727 727232 1384082 NM BS 1130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 AFT CARGO COMPARTMENT STATION 1130 BLU TO RBL 60 FLOORBEAM LOWER CAP HAS HEAVY CORROSION. REMOVED LOWER CAP, FABRICATED REPAIR TREATED, PRIMED, THEN INSTALLED IAW DWG 25770-5065 AND EC/RA 5310-03334. 2 L 7 3 4F A3WE 1996101700284 19961017 00284 NM 1996 10 17 CALA9601452 1 19960918 A 5330 SKIN BOEING 727 727232 1384082 NM BS 1352 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 RIGHT HAND FUSELAGE SKIN DENTED AT APPROX STATION 1352. CUT OUT DENTED AREA, FABRICATED AND INSTALLED DOUBLER PER SRM 5 4-30-3 FIG 7. 2 L 7 3 4F A3WE 1996101700285 19961017 00285 NM 1996 10 17 CALA9601453 1 19960918 A 5330 SKIN BOEING 727 727232 1384082 NM FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 RIGHT HAND FUSELAGE SKIN JUST BELOW FORWARD SERVICE DOOR AREA HAS DENT. REWORKED DENT TO BRING WITHIN LIMITS. ACCOMPLI SHED HFEC, NO CRACKS NOTED PER SRM 53-10-1 AND 51-40-1. 2 L 7 3 4F A3WE 1996101700286 19961017 00286 NM 1996 10 17 CALA9601454 1 19960918 A 5754 SKIN BOEING 727 727232 1384082 NM NR 2 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 LEFT NR 2 SLAT HAS 1.5 INCH CRACK AT OUTBOARD ACCESS FOR ACTUATOR ATTACMENT. FABRICATED AND INSTALLED DOUBLER PER SRM 5 7-50-3. 2 L 7 3 4F A3WE 1996101700287 19961017 00287 NM 1996 10 17 CALA9601455 1 19960917 A 5753 SKIN BOEING 727 727232 1384082 NM LT TE FORE FLAP GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 LEFT INBOARD FORE FLAP LEADING EDGE GOUGED INBOARD AND OUTBOARD OF NR 4 CARRIAGE. REMOVED DOUBLER, FABRICATED AND INSTA LLED REPLACEMENT DOUBLER PER SRM 57-40-04. 2 L 7 3 4F A3WE 1996101700288 19961017 00288 NM 1996 10 17 CALA9601456 1 19961006 A 5330 SKIN BOEING 727 727232 1384082 NM BS 470-478 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 EXTERNAL SKIN HAS CORROSION AT BOTTOM OF FUSELAGE STATION 470 TO STATION 478. REMOVED SKIN PANEL, CLEANED UP AREA, INST ALLED NEW SKIN PANEL PER EA 5330-01320. 2 L 7 3 4F A3WE 1996101700289 19961017 00289 NM 1996 10 17 CALA9601457 1 19961005 A 5330 SKIN BOEING 727 727232 1384082 NM BS 612 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 ONE INCH CORROSION/CRACK ON FUSELAGE SKIN AT STATION 612 STRINGER 26L. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED R EPAIR PER SRM 53-30-2 FIG 5. 2 L 7 3 4F A3WE 1996101700290 19961017 00290 WP 1996 10 17 9621539756 1 19960824 A 5711 SPAR DOUG DC9 DC941 302207N WP RRS 164 RT CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 756NW 47180 DURING H-CHECK, FOUND A CRACK IN THE RIGHT WING REAR SPAR LOWER CAP AT XRS 164. REPAIRED CAP (P/N 5911301) PER EA 97-1 10758. 2 L 7 2 4F A6WE 1996101700291 19961017 00291 WP 1996 10 17 9621549105 1 19960913 A 5312 BULKHEAD DOUBLER DOUG DC9 DC915 3022036 WP AFT PRESS BLKHD CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 95S 47205 DURING H-CHECK, FOUND CRACKS IN THE AFT PRESSURE BULKHEAD -13 DOUBLER UPPER DOOR JAMB. REPAIRED DOUBLER (P/N 5910130-13 ) PER EA 91-111229. 2 L 7 2 4F A6WE 1996101700292 19961017 00292 WP 1996 10 17 9621559103 1 19960919 A 5312 BULKHEAD WEB DOUG DC9 DC915 3022036 WP BS 817 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 93S 47078 DURING H-CHECK, FOUND A 5.75 INCH CRACK IN THE FS 817 AFT PRESSURE BULKHEAD AT Z=63.5 AT THE LEFT DOOR JAMB. REPAIRED W EB (P/N 5910130-3) PER EA 91-111251. 2 L 7 2 4F A6WE 1996101700293 19961017 00293 NM 1996 10 17 9621576613 1 19960924 A 5315 FLOOR BEAM BOEING 747 747251B 1384892 NM BS 520 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 613US 20358 DURING P-CHECK, FOUND CORROSION ON THE BS 520 UPPER DECK FLOOR BEAM UPPER CHORD FROM LBL 40 TO 50. REPAIRED CHORD (P/N 65B10936-12) PER EA 66-106402. 2 L 7 4 4F A20WE 1996101700294 19961017 00294 NM 1996 10 17 9621585517 1 19960926 A 5315 FLOOR BEAM BOEING 757 757251 1384970 NM BS 365 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 517US 23205 DURING P-CHECK, FOUND CORROSION IN THE BS 365 FLOOR BEAM UPPER CHORD FROM RBL 45 TO 56. REPAIRED CHORD (P/N 141N5112) P ER EA 55-110352. 2 L 7 2 4F RT A2NM 1996101700295 19961017 00295 WP 1996 10 17 9621599908 1 19960927 A 5320 FITTING DOUG DC9 DC931 3022065 WP LONGERON CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 958N 47254 DURING H-CHECK, FOUND A CRACK IN THE LONGERON 28L FORWARD KEEL, FORWARD END FITTING. REPLACED FITTING PER SRM 53-01. 2 L 7 2 4F A6WE 1996101700296 19961017 00296 WP 1996 10 17 9621609908 1 19960927 A 5320 FITTING DOUG DC9 DC931 3022065 WP LONGERON CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 958N 47254 DURING H-CHECK, FOUND A CRACK IN THE LONGERON 29L END FITTING AFT OF THE FORWARD CARGO COMPARTMENT T-CAP. REPLACED FITT ING PER SRM 51-30-2. 2 L 7 2 4F A6WE 1996101700297 19961017 00297 WP 1996 10 17 9621619956 1 19960927 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 237 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 923RW 47183 DURING M-CHECK, FOUND CORROSION IN THE SKIN SPLICE DOUBLER FITTING AT FS 237, LONGERON 18R. REPLACED FITTING PER SRM 51 -30-5, 51-30-3. 2 L 7 2 4F A6WE 1996101700298 19961017 00298 WP 1996 10 17 9621629908 1 19960928 A 5320 WEB DOUG DC9 DC931 3022065 WP BS 83 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 958N 47254 DURING H-CHECK, FOUND CRACKS IN THE NOSE LANDING GEAR HORIZONTAL PRESSURE PANEL AT FS 83, RIGHT SIDE. REPAIRED PANEL (P /N 9910073-313) PER EA 99-111278. 2 L 7 2 4F A6WE 1996101700299 19961017 00299 NM 1996 10 17 9621636613 1 19961001 A 5412 BULKHEAD WEB BOEING 747 747251B 1384892 NM NR 1 PYLON CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 613US 20358 DURING P-CHECK, FOUND A 1.5 INCH CRACK IN THE NR 1 PYLON LOWER BULKHEAD WEB AT NACELLE STA 210. REPAIRED WEB PER EA 66- 106410. 2 L 7 4 4F A20WE 1996101700300 19961017 00300 WP 1996 10 17 9621649851 1 19961001 A 5330 SKIN DOUG DC9 DC951 3022051 WP BS 200 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 760NC 47708 DURING LINE CHECK, FOUND A CRACK IN THE FORWARD ENTRANCE DOOR JAMB UPPER AFT SKIN FS 200 AT LONGERON 9L. REPAIRED SKIN (P/N 5911406-501) PER EA 98-109587. 2 L 7 2 4F A6WE 1996101700301 19961017 00301 NM 1996 10 17 9621656613 1 19961002 A 5412 BULKHEAD FITTING BOEING 747 747251B 1384892 NM NR 3 PYLON CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 613US 20358 DURING P-CHECK, FOUND A CRACK IN THE NR 3 PYLON AFT ENGINE MOUNT BULKHEAD TO FRONT SPAR ATTACH FITTING AT NACELLE STA 22 1. REPLACED FITTING (P/N 65B91314-3). 2 L 7 4 4F A20WE 1996101700302 19961017 00302 EU 1996 10 17 9621663214 1 19961002 A 5320 SUPPORT AIRBUS 320 A320211 3930320 EU BS 32571 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 314US 160 DURING IL CHECK, FOUND CORROSION IN THE FS 68 FLOOR BEAM SUPPORT AT THE LEFT DOOR SILL. REPAIRED SUPPORT (P/N D53480043 ) PER EA 32-109588. 2 L 7 2 4F RT A28NM 1996101700303 19961017 00303 WP 1996 10 17 9621679852 1 19961005 A 5320 FITTING DOUG DC9 DC951 3022051 WP BS 1167 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 761NC 47709 DURING H-CHECK, FOUND CRACKS IN BOTH THE LEFT AND RIGHT SIDE FS 1167 FLOOR BEAM TO FRAME FITTINGS. REPLACED FITTINGS PE R SRM 51-30-5. 2 L 7 2 4F A6WE 1996101700304 19961017 00304 WP 1996 10 17 9621689852 1 19961006 A 5320 FITTING DOUG DC9 DC951 3022051 WP BS 1060-1068 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 761NC 47709 DURING H-CHECK, FOUND A CRACK IN THE RIGHT LONGERON 30 FLOOR SUPPORT FITTING BETWEEN FS 1060 TO 1068. REPLACED FITTING PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996101700305 19961017 00305 1996 10 17 9621699914 4 19961009 A 2565 113317 BATTERIES DOUG DC9 DC931 3022065 WP DOOR SLIDE DISCHARGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 964N 47416 DURING PERIODIC CHECK, FOUND MAIN CABIN DOOR AND GALLEY DOOR EVACUATION SLIDES WITH LOW BATTERIES. REPLACED SLIDE. 2 L 7 2 4F A6WE 1996101700306 19961017 00306 WP 1996 10 17 9621709902 1 19961009 A 3350 GROUND WIRE DOUG DC9 DC931 3022065 WP CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 952N 47073 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT INTERIOR OVERWING EMERGENCY EXIT LIGHTS WEAK. REPAIRED FAULTY GROUND FOR LEFT OVERWING EXIT SIGNS, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996101700307 19961017 00307 WP 1996 10 17 9621719938 1 19961009 A 3350 BATTERY DOUG DC9 DC931 3022065 WP TAIL COMPT DIRTY A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 1798U 47369 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY EVACUATION LIGHTS INOPERATIVE. CLEANED BATTERY, OP ERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996101700308 19961017 00308 WP 1996 10 17 9621729928 1 19961008 A 3260 UPLOCK SWITCH DOUG DC9 DC931 3022065 WP RT MLG MALFUNCTIONED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 8921E 45836 DURING CLIMBOUT, THE RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. RECYCLED GEAR WITH SAME RESULTS. FLIGHT CONTINUED TO DESTINATION AT REDUCED SPEED AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT MAIN GEAR UPLOCK SWITCH, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996101700309 19961017 00309 WP 1996 10 17 9621741146 1 19961008 A 7830 REV UNLOCK LIGHT DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20J 52054 NE NR 3 ENGINE ILLUMINATED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 146US 46755 86177 DURING TAKEOFF ROLLOUT, THE NR 3 ENGINE REVERSER UNLOCK LIGHT ILLUMINATED. CREW ABORTED TAKEOFF AND RETURNED TO GATE. M AINTENANCE INSPECTED THE REVERSER AND DEFERRED REPAIR PER MEL 78-1A. 2 L 7 3 4F 4 F A22WE E20EA 1996101700310 19961017 00310 WP 1996 10 17 9621759604 1 19961010 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 604NW 47222 DURING PERIODIC CHECK, FOUND EMERGENCY LIGHTS AT ROWS 6 THROUGH 10 INOPERATIVE. REPLACED BATTERIES IN BATTERY PACKS, OP ERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996101700311 19961017 00311 WP 1996 10 17 9621769180 1 19961010 A 3230 GRD SHIFT CABLES DOUG DC9 DC914 3022034 WP LANDING GEAR OUT OF ADJUST A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 3312L 45707 AFTER LIFTOFF, UNABLE TO RAISE THE LANDING GEAR HANDLE. NOSE WHEEL WAS STEERABLE AND GROUND SHIFT WAS IN GROUND MODE. F LIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. ADJUSTED NOSE GEAR GROUND SHIFT CABLES, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996101700312 19961017 00312 WP 1996 10 17 9621731146 1 19961010 A 7830 TR LIGHT DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20J 52054 NE NR 3 ENGINE ILLUMINATED A NWAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 01 146US 46755 86177 DURING TAKEOFF ROLLOUT, THE NR 3 THRUST REVERSER LIGHT ILLUMINATED AT 60 KNOTS. CREW ABORTED TAKEOFF AND WHILE TAXING, REALIZED THAT THE REVERSER WAS ON MEL FROM A PREVOUS INCIDENT. FLIGHT DEPARTED AND TO BOS WITHOUT FURTHER INCIDENT. 2 L 7 3 4F 4 F A22WE E20EA 1996101700313 19961017 00313 NE 1996 10 17 9621779883 2 19961011 A 7320 PT2 LINE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D17 52049 NE RT ENGINE LEAKING A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 983US 47282 688772 DURING CLIMB, THE RIGHT ENGINE EPR WAS INDICATING A HIGH READING. CREW PERFORMED AN AIR TURNBACK WHERE THEY LANDED AT M SP WITHOUT FURTHER INCIDENT. MAINTENANCE REPAIRED A LEAK ON THE PT2 LINE, LEAK AND OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F A6WE E2EA 1996101700315 19961017 00315 WP 1996 10 17 9621799926 1 19961011 A 3350 60030451 POWER SUPPLY DOUG DC9 DC932 3022066 WP TAILCONE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 926NW 47425 DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS IN TAILCONE INOPERATIVE. REPLACED POWER SUPPLY AND B ATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996101700316 19961017 00316 WP 1996 10 17 9621809989 1 19961012 A 2150 20495053 ACM DOUG DC9 DC931 3022065 WP LEFT MALFUNCTIONED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 8945E 2767 2757 47181 FLIGHT ATTENDANT REPORTED BURNING SMELL IN CABIN AFTER TAKEOFF. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MA INTENANCE INSPECTED AND FOUND FUMES COMING FROM LEFT AIR CYCLE MACHINE. REPLACED AIR CYCLE MACHINE, LEAK AND OPERATIONA L CHECK NORMAL. 2 L 7 2 4F A6WE 1996101700317 19961017 00317 WP 1996 10 17 9621819607 1 19961013 A 3397 WIRE DOUG DC9 DC932 3022066 WP AFT CEILING LOOSE A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 607NW 47232 FLIGHT ATTENDANT REPORTED ELECTRICAL SMELL IN AFT CABIN DURING TAKEOFF. FLIGHT RETURNED TO YWG AND LANDED WITHOUT INCID ENT. MAINTENANCE INSPECTED CEILING AREA BETWEEN AFT LAVATORIES AND FOUND WIRE CONDUITS LOOSE. RECLAMPED CONDUITS, OPER ATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996101700318 19961017 00318 SO 1996 10 17 COMA9610302 1 19961011 A 2751 INDICATION EMB 120 EMB120RT SO LT TE FLAP MALFUNCTIONED A COMA O OTHER N FALSE WARNING LD LANDING 1 SO 01 179CA 120179 AFTER TOUCHDOWN, FLAP ASYMMETRY WARING. FLAP WERE SET AT 45 DEGREES, LEFT INBD FLAP INDICATED 25 DEGREES. COULD NOT DU PLICATE DISCREPANCY, OPERATIONAL CHECK OF FLAP SYSTEM NORMAL. 2 L 7 2 4T RT A31SO 1996101700319 19961017 00319 SO 1996 10 17 COMA9610303 1 19961012 A 2752 3203001005 ACTUATOR EMB 120 EMB120RT SO RT TE FLAP MALFUNCTIONED A COMA O OTHER J WARNING INDICATION LD LANDING 1 SO 01 179CA 12433 4054 120179 AFTER LANDING, WHEN FLAPS SELECTED UP, THE LT INBD FLAP INDICATED 15 DEGREES AND THE RT INBD FLAP INDICATED 45 DEGREES. COULD NOT DUPLICATE DISCREPANCY. REPLACED THE RT INBD FLAP ACTUATOR FOR TROUBLESHOOTING. 2 L 7 2 4T RT A31SO 1996101700320 19961017 00320 SO 1996 10 17 COMA9610304 1 19961012 A 3231 12012347001 LATCH EMB 120 EMB120RT SO LT MLG DOOR BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 161CA 120143 LT MLG FORWARD DOOR LATCH IS BROKEN, DOOR HANGS OPEN. REPLACED THE DOOR LATCH ASSY. 2 L 7 2 4T RT A31SO 1996101700321 19961017 00321 SO 1996 10 17 COMA9610305 1 19961009 A 3250 922FS2A6NZ735 STEERING EMB 120 EMB120RT SO NLG FAILED A A COMA O OTHER O OTHER LD LANDING 1 SO 01 254CA 120233 NOSE WHEEL STEERING FAILED. AIRCRAFT DEPARTED RUNWAY. COULD NOT DUPLICATE DISCREPANCY. WEIGHT ON WHEELS PROXIMITY SEN SORS WERE REPLACED FOR TROUBLESHOOTING. AIRCRAFT FLIGHT CHECK SATISFACTORY. 2 L 7 2 4T RT A31SO 1996101700322 19961017 00322 NM 1996 10 17 SWAA961073 1 19961009 A 2841 INDICATOR BOEING 737 7373G7 1384595 NM NR 2 FUEL TANK INACCURATE A SWAA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 670SW 23784 DIVERTED TO ABQ DUE TO TOTAL FUEL QUANTITY FLUCTUATING, +/- 2,000 LBS. INSPECTED FOR LEAKS AND CHECKED FUEL QUANITITY, DEFERRED NR 2 FUEL TANK INDICATION AND CONTINUED PER MEL 28-6. 2 L 7 2 4F RT A16WE 1996101700323 19961017 00323 NM 1996 10 17 SWAA961074 1 19961009 A 2782 65446519 ACTUATOR BOEING 737 7372H4 138448C NM NR 5 LE SLAT FAILED A SWAA D RETURN TO BLOCK F FLT CONT AFFECTED CL CLIMB 1 SW 07 80SW 22675 RETURNED TO PHX DUE TO NR 5 L/E SLAT NOT FULLY RETRACTING. INSPECTED, REPLACED NR 5 SLAT ACTUATOR AND OP CHECKED PER B OEING M/M. 2 L 7 2 4F A16WE 1996101700324 19961017 00324 NM 1996 10 17 SWAA961075 1 19961008 A 2121 20405011 ACM BOEING 737 7375H4 138449D NM RIGHT FAILED A SWAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 502SW 24179 AFTER PUSHBACK FROM GATE, EXPERIENCED SMOKE IN CABIN. RETURNED TO GATE. INSPECTED, REPLACED RIGHT AIR CYCLE MACHINE AN D AIR CONDITION RELAY MODULE PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996101700325 19961017 00325 EU 1996 10 17 QXEA9600413 1 19960928 A 3350 XB864042 BULB FOKKER FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 478US 11227 EMERGENCY LIGHT AT SEAT 9A IS INOP. BULBS WERE REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996101700326 19961017 00326 NM 1996 10 17 QXEA9600414 1 19960929 A 3350 6104781 POWER SUPPLY DHAV DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 814PH 43 EMERGENCY LIGHTS WILL NOT TURN OFF. CYCLED CIRCUIT BREAKER WITHOUT HELP. REPLACED POWER SUPPLIES 1 THROUGH 6 AND LIGH TS OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 1996101700327 19961017 00327 NM 1996 10 17 QXEA9600415 1 19960929 A 3350 1005511 LIGHT DHAV DHAV DHC8 DHC8102 2809003 NM COCKPIT MALFUNCTIONED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 814PH 43 DURING OPS CHECK OF EMERGENCY LIGHTS, LIGHTS WOULD STAGGER OFF AND THEIR OWN WITHIN A COUPLE ON MINUTES. AIRCRAFT FERRI ED TO PDX FOR REPAIR. PORTABLE EMERGENCY LIGHT AND RECEPTICAL WERE REPLACED AND LIGHTS OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 1996101700328 19961017 00328 EU 1996 10 17 QXEA9600416 1 19960930 A 3350 1820 BULB FOKKER FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 491US 11156 EMERGENCY EXIT LIGHT AT 8E IS INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996101700329 19961017 00329 NM 1996 10 17 QXEA9600417 1 19960930 A 3350 1005511 LIGHT DHAV DHAV DHC8 DHC8102 2809003 NM COCKPIT INOPERATIVE A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 826PH 214 COCKPIT PORTABLE EMERGENCY LIGHT INOP. LIGHT REPLACED AND LIGHT OPS CHECKED GOOD, LIGHT WAS DISCHARGED DUE TO IMPROPER INSTALLATION. 2 H 7 2 4T RT A13NM 1996101700330 19961017 00330 EU 1996 10 17 QXEA9600418 1 19961002 A 3350 1820 BULB FOKKER FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 493US 11161 LOWER EXIT LIGHT BY RIGHT HAND FORWARD EXIT IS INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996101700331 19961017 00331 EU 1996 10 17 QXEA9600419 1 19961004 A 3350 5515800106 SIGN FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN DIM A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 466US 11075 CABIN FORWARD BULKHEAD EXIT SIGN DIM. SIGN REPLACED AND LIGHTS OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996101700332 19961017 00332 NM 1996 10 17 QXEA9600420 1 19961006 A 3350 82410162007 CONTROL BOX DHAV DHAV DHC8 DHC8102 2809003 NM CABIN MALFUNCTIONED A QXEA K NONE L NO TEST LD LANDING 1 NM 09 812PH 26 EMERGENCY LIGHTS FLASHED DURING LANDING. CONTROL BOX REPLACED AND LIGHTS OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 1996101700333 19961017 00333 NM 1996 10 17 QXEA9600421 1 19961008 A 5610 001A561A0000200 WINDSHIELD DORNER DO32 DO328100 2996000 NM LT COCKPIT CRACKED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 09 336PH 4789 3014 DURING DESCENT CAPTAINS WINDSHIELD STARTED TO BURN AND CRACK. AIRCRAFT LANDED IN ACV WITHOUT FURTHER PROBLEM. WINDSHIE LD REPLACED AND WINDSHIELD HEAT OPS CHECKED GOOD. 2 H 7 2 4T RT A45NM 1996101700334 19961017 00334 EU 1996 10 17 QXEA9600422 1 19961008 A 3350 1820 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 466US 11075 MAIN CABIN DOOR EMERGENCY LIGHT IS INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996101700335 19961017 00335 EU 1996 10 17 QXEA9600423 1 19961008 A 3350 MGG1280 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 452US 11105 FORWARD CENTER AISLE EXIT ANNUNCIATOR IS INOP AT ROW 8 (28V). BULBS WERE REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996101700336 19961017 00336 NM 1996 10 17 QXEA9600424 1 19961010 A 3350 321430 BATTERY DORNER DORNER DO32 DO328100 2996000 NM CABIN DISCHARGED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 336PH 3014 MID SECTION OF FLOOR PROXIMITY LIGHTING IS DIM, SECTION FADES OUT IN 10 SECONDS. BATTERY PACKS 2, 3 AND 4 REPLACED AND LIGHT OPS CHECKED GOOD. 2 H 7 2 4T RT A45NM 1996101700337 19961017 00337 EU 1996 10 17 QXEA9600425 1 19961010 A 3350 1820 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 454US 11107 THE 8A OVERWING EMERGENCY LIGHT IS INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996101700338 19961017 00338 NM 1996 10 17 QXEA9600426 1 19961010 A 3350 1005511 LIGHT DHAV DHAV DHC8 DHC8102 2809003 NM COCKPIT INOPERATIVE A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 830PH 314 COCKPIT PORTABLE EMERGENCY LIGHT IS INOP. LIGHT ASSY REPLACED AND LIGHT OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 1996101700339 19961017 00339 NM 1996 10 17 96FDEA01572 1 19961011 A 3610 32902741 FAN AIR VALVE DOUG MD11 MD11F 3023600 NM NR 2 ENGINE MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 603FE 48459 NR 2 ENG BLEED AIR HIGH TEMP, POWER REDUCED, ALERT WENT OUT. REMOVED AND REPLACED NR 2 ENG FAN AIR VALVE SYS OPS CHECK GOOD WITH ENG RUN. 2 L 7 3 4F RT A22WE 1996101700340 19961017 00340 WP 1996 10 17 96FDEA01573 1 19961010 A 5320 SIDEWALL DOUG DC10 DC1030 3023501 WP BS 1259 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 301FE 46800 MAIN DECK TOP OF CENTER FUEL TANK RT RBL SIDEWALL STA 1259, TWO PLACES EXFOLIATED. *S/D* REMOVED 6 FASTENERS, BURNISHE D CORROSION IN REF TO SRM 57-10-00, C/W MATERIAL REMOVED MAPPING REQUIRED BY ENGINEERING, REPAIRED PER EA 8-5710-31711, LEAK CK OK 10/17/96. 2 L 7 3 4F A22WE 1996101700341 19961017 00341 WP 1996 10 17 96FDEA01574 1 19961011 A 3233 ACTUATOR DOUG DC10 DC1030F 3023504 WP NLG MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 302FE 46801 ON TAKEOFF, THE NOSE LIGHT ON BOTH PANELS REMAINS RED. HYD SYS 3 WAS NORMAL, RAN THE RED TAB PROCEDURES AND LANDING GEA R SHOWED 4 GEAR LIGHT WITH GEAR HANDLE DOWN. TRIED TO RAISE THE GEAR AGAIN WITH NO SUCCESS, RED LIGHT STILL ON WITH HAN DLE UP. LOWERED GEAR AND LANDED. REPLACED NOSE GEAR RETRACT CYLINDER AND PROXIMITY CONTROL BOX FOR PRECAUTIONALLY. 2 L 7 3 4F RT A22WE 1996101700342 19961017 00342 WP 1996 10 17 96FDEA01575 1 19961013 A 5610 NBA60452 WINDOW DOUG DC10 DC1010CF 3023502 WP R1 WINDOW SHATTERED A FDEA H DEACTIVATE SYST/CIRCUITS O OTHER CR CRUISE 1 SO 25 68049 47803 AT 1100Z F/O'S WINDSCREEN OUTER PANEL SHATTERED, FL350, TAT - 48, COMPLIED WITH RED TABS. REMOVED AND REPLACED WINDOW A ND WINDOW HEAT CONTROLLER PRECAUTIONARY PER MAINTENANCE MANUAL. 2 L 7 3 4F RT A22WE 1996101700343 19961017 00343 1996 10 17 96UAL900762 4 19960930 A 2210 2588880901 YAW COUPLER BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE RUDDER INTERMITTENT A UALA O OTHER F FLT CONT AFFECTED CR CRUISE 1 WP 29 9007U 621 19045 YAW DAMPER ABRUPTLY MOVES RUDDER OCCASIONALLY FOR NO APPARENT REASON. *S/D* YAW COUPLER WAS INTERMITTENT. REPLACED YA W DAMPER COUPLER, CHECKED OK. 2 L 7 2 4F 4 F A16WE E2EA 1996101700344 19961017 00344 NM 1996 10 17 96UAL900763 1 19960930 A 3350 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 352UA 24320 ONE SECTION OF EMERGENCY EGRESS LIGHTING INOP ROW 12. INSTALLED NEW LIGHT SECTION, OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 1996101700345 19961017 00345 1996 10 17 96UAL900764 4 19960930 A 2565 61199107 REGULATOR CARLTON B181161 BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXCAPE SLIDE FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 526UA 24994 SLIDE REMOVED FOR TIME CONTROLLED OVERHAUL. DURING FLAT FIRE, BOTTLE VALVE FAILED TO FULLY OPEN DUE TO DAMAGED ROTATION SHAFT AND PIN. OVERHAULED VALVE, REPLACED SHAFT AND CONTACTED MANUFACTURER. 2 L 7 2 4F 4 F RT A2NM E17NE 1996101700346 19961017 00346 NM 1996 10 17 96UAL900765 1 19960930 A 3397 WIRE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7461U 21915 MAIN CABIN CEILING LIGHT OVERWING EXIT INOPERATIVE. *S/D* THE WIRES WERE BROKEN. THE WIRES WERE REPAIRED AT THE CONNE CTOR-TO-CEILING MOUNTED LIGHT ASSEMBLY AT THE OVERWING EXIT, OPERATIONS CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1996101700347 19961017 00347 NM 1996 10 17 96UAL900766 1 19960930 A 2810 FUEL CAP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT WING FAILED A UALA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 WP 29 566UA 26670 DURING FLIGHT, LEFT OVERWING FUEL CAP DEVELOPED A LEAK. AIRCRAFT DIVERTED TO DEN. REPLACED FUEL CAP, OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996101700348 19961017 00348 NM 1996 10 17 96UAL900767 1 19960930 A 3260 BR20AXH5V3 RELAY BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE E/E COMPT MISINSTALLED A UALA O OTHER P NO WARNING INDICATION LD LANDING 1 WP 29 324UA 23956 CREW REPORTED NO GEAR WARNING LIGHT ILLUMINATED AND NOSE GEAR HAD A UNSAFE LIGHT. AIRCRAFT LANDED UNDER AMBER ALERT. * S/D* FOUND RELAY R374 LOCATED IN E-11 RACK INSTALLED BACKWARDS. REINSTALLED RELAY CORRECTLY AND REPLACED M983 CARD, CH ECKS OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1996101700349 19961017 00349 1996 10 17 96UAL900768 4 19960930 A 2565 EXCAPE SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DEPLOYED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 539UA 25223 PER CREW, DOOR 4R SLIDE DEPLOYED. AIRCRAFT FERRIED TO LAX. REPLACED SLIDE AND DOOR EMERGENCY BOTTLE, OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996101700350 19961017 00350 NM 1996 10 17 96UAL900769 1 19961002 A 5320 146N539110 SIDE PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1420 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 528UA 25018 DISCOVERED CORRODED AFT CARGO FLOOR SIDE PANEL MEMBER, JUST INBOARD FO CARGO DOOR SILL, SRM 53-60-53 PG 8 NR 4. REMOVED CORROSION AND REPAIRED PER SRM GUIDELINES, OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996101700352 19961017 00352 NM 1996 10 17 96UAL900771 1 19961004 A 2422 90670903790012 INVERTER BOEING 285W00122 BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CACP FAILED A UALA F H ACTIVATE FIRE EXT. DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 776UA D00028 26937 SMOKE REPORTED COMING FROM BEHIND THE CABIN AREA CONTROL PANEL AT DOOR 2 LEFT. DISCHARGED TWO HALON FIRE BOTTLES, SMOKE STOPPED. CIRCUIT BREAKERS PULLED AT P210 PANEL. *S/D* OPEN CIRCUIT CONDITION FOR BOTH FLUORESCENT BACKLIGHTS CAUSED TRANSFORMER (906-70903-7) AND POWER FET'S (900-12472-012) TO OVERHEAT AND FAIL EMITTING SMOKE. NO EVIDENCE OF FLAME. B OEING TO RELEASE ADVISORY TO REPLACE CACP/CSCP TOUCHSCREEN IF DISPLAY BECOMES DIM, ONE FLUORESCENT BACKLIGHT OPEN. 2 L 7 2 4F 4 F RT T0001SE E46NE 1996101700353 19961017 00353 WP 1996 10 17 96UAL900772 1 19961004 A 4950 FAN 381027NP22 DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL APU DAMAGED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 1825U 46624 ODOR IN CABIN. INBOUND CREW REPORTED OIL SMELL COMING FROM NR 1 OR NR 3 ENGINE. ISOLATED TO NR 3 BLEED. NO APU EXTERN AL LEAKS FOUND. REMOVED APU GENERATOR COOLING AIR DUCTS AND FOUND TO BE SOAKED WITH OIL. REPLACED APU COOLING FAN DUE TO LEAKING SEAL. 2 L 7 3 4F 4 F A22WE E23EA 1996101700354 19961017 00354 NM 1996 10 17 96UAL900779 1 19961007 A 3397 58781 WIRE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 304UA 23665 EMERGENCY ESCAPE PATH LIGHTING INOP BETWEEN ROWS 11 AND 13. *S/D* FOUND DAMAGED CABLE CONNECTION. REPAIRED CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1996101700355 19961017 00355 WP 1996 10 17 MWEA96532 1 19961011 A 5313 2777976 LONGERON DOUG DC9 DC914 3022034 WP BS 801-817 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CK, FOUND LONGERON 18 HAS CORROSION BEYOND LIMITS AT STA 801 TO 817 UNDER RT LAV. INSTALLED NEW LONGERON SECTI ON IAW SRM 53-05, FIG 25. 2 L 7 2 4F A6WE 1996101700356 19961017 00356 WP 1996 10 17 MWEA96533 1 19961011 A 5320 ANGLE DOUG DC9 DC914 3022034 WP BS 69.5-76.5 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CK, FOUND TEMPORARY REPAIR INSTALLED ON FUSELAGE BETWEEN STA 69.5 AND 76.5 IN WINDSHIELD WIPER MOTOR CAVITY. I NSTALLED REPAIR IAW SRM 53-04, FIG 38, SHEET 21. 2 L 7 2 4F A6WE 1996101700357 19961017 00357 WP 1996 10 17 MWEA96534 1 19960111 A 5330 SKIN DOUG DC9 DC914 3022034 WP BS 133 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CK, FOUND DENT IN FUSELAGE SKIN AT STA 133 LONGERON 19L. INSTALLED DOUBLER REPAIR IAW SRM 53-04, PG 218 G,S,T, W. 2 L 7 2 4F A6WE 1996101700358 19961017 00358 WP 1996 10 17 MWEA96535 1 19961011 A 5330 SKIN DOUG DC9 DC914 3022034 WP BS 101 BULGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CK, FOUND SKIN BULGED OUT AT STA 101, LONGERON 25R. INSTALLED DOUBLER REPAIR IAW SRM 53-04, FIG 38, VIEW P. 2 L 7 2 4F A6WE 1996101700359 19961017 00359 WP 1996 10 17 MWEA96536 1 19961011 A 5330 SKIN DOUG DC9 DC914 3022034 WP BS 170-196 LIGHTNING STRIKE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CK, FOUND LIGHTNING STRIKES BETWEEN STA 170 TO 196, LONGERON 9R ABOVE FWD GALLEY SERVICE DOOR. INSTALLED REPAI R IAW SRM 53-04, FIG 37. 2 L 7 2 4F A6WE 1996101700360 19961017 00360 WP 1996 10 17 MWEA96537 1 19961011 A 5330 SKIN DOUG DC9 DC914 3022034 WP BS 88-101 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CK, FOUND DENT IN SKIN BETWEEN STA 88 AND 101, LONGERON 24L AND 25L. INSTALLED DOUBLER REPAIR IAW SRM 53-04, F IG 38, SHEET 20. 2 L 7 2 4F A6WE 1996101700361 19961017 00361 WP 1996 10 17 MWEA96538 1 19961011 A 5330 SKIN DOUG DC9 DC914 3022034 WP BS 190 LIGHTNING STRIKE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CK, FOUND LIGHTNING STRIKE AT STA 190 LONGERON 4L. INSTALLED DOUBLER REPAIR IAW SRM 53-04, FIG 38, VIEW H. 2 L 7 2 4F A6WE 1996101700362 19961017 00362 WP 1996 10 17 MWEA96539 1 19961011 A 5531 RIB DOUG DC9 DC914 3022034 WP VERT STAB CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CK, FOUND VERTICAL STABILIZER LEADING EDGE UPPER RIB CRACKED NEAR MOUNTING FLANGE AND RIB CRACKED AT LT SIDE OF VOR ANTENNA BOX. INSTALLED ANGLE REPAIR IAW SRM 55-02, FIG 19. 2 L 7 2 4F A6WE 1996101700363 19961017 00363 WP 1996 10 17 MWEA96540 1 19961011 A 5720 591001471 FRAME DOUG DC9 DC914 3022034 WP LT WING TIP DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CK, FOUND LT WING TIP FRAME DENTED LOWER EDGE OF NAV LIGHT CAVITY. REPLACED WING TIP FRAME. 2 L 7 2 4F A6WE 1996101700364 19961017 00364 WP 1996 10 17 MWEA96541 1 19961011 A 5512 SKIN DOUG DC9 DC914 3022034 WP LT HORIZ STAB GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CK, FOUND 2 GOUGES IN LT HORIZONTAL STAB SKIN, LOWER, AT STA XHS32 AND 45. INSTALLED DOUBLER REPAIR IAW SRM 55 -03, FIG 19. 2 L 7 2 4F A6WE 1996101700365 19961017 00365 WP 1996 10 17 MWEA96542 1 19961011 A 5511 RIB DOUG DC9 DC914 3022034 WP RT HORIZ STAB CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CK, FOUND RT HORIZONTAL STAB OUTBD LEADING EDGE SECTION INBD RIB CRACKED. INSTALLED DOUBLER REPAIR IAW SRM 55- 02, FIG 14. 2 L 7 2 4F A6WE 1996101700366 19961017 00366 WP 1996 10 17 MWEA96543 1 19961011 A 5510 STRINGER DOUG DC9 DC914 3022034 WP RT HORIZ STAB CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CK, FOUND RT HORIZONTAL STAB UPPER STRINGER NR 3 CRACKED AT STA XHS50. INSTALLED REPAIR IAW SRM 55-02, FIG 16, SHEET 7. 2 L 7 2 4F A6WE 1996101700367 19961017 00367 WP 1996 10 17 MWEA96544 1 19961011 A 5330 SKIN DOUG DC9 DC914 3022034 WP BS 389/412/415 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CK, FOUND THREE DENTS IN FUSELAGE SKIN AT STA'S 389, LONG 20R, STA 412, LONG 19R AND STA 415, LONG 25R. INSTAL LED REPAIRS IAW SRM 53-04, FIG 38, VIEWS 3 AND F. 2 L 7 2 4F A6WE 1996101700368 19961017 00368 WP 1996 10 17 MWEA96545 1 19961011 A 5753 SKIN DOUG DC9 DC914 3022034 WP RT TE FLAP DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CK, FOUND RT FLAP SKIN DENTED AT STA XRS 75. REPLACED SKIN SECTION IAW SRM 57-50-3, FIG 6. 2 L 7 2 4F A6WE 1996101700369 19961017 00369 WP 1996 10 17 MWEA96546 1 19961011 A 5521 SPAR DOUG DC9 DC914 3022034 WP RT ELEVATOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CK, FOUND RT ELEVATOR FWD SPAR LOWER FLANGE CRACKED STA XE145. INSTALLED REPAIR IAW SRM 55-02, FIG 9. 2 L 7 2 4F A6WE 1996101700370 19961017 00370 WP 1996 10 17 MWEA96547 1 19961011 A 5511 RIB DOUG DC9 DC914 3022034 WP LT HORIZ STAB CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CK, FOUND LT HORIZ STAB LEADING EDGE, 6TH RIB FROM OUTBD END IS CRACKED AT UPPER END. INSTALLED DOUBLER REPAIR IAW SRM 55-02, FIG 18. 2 L 7 2 4F A6WE 1996101700371 19961017 00371 WP 1996 10 17 MWEA96548 1 19961011 A 5522 SKIN DOUG DC9 DC914 3022034 WP RT ELEVATOR DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CK, FOUND RT ELEVATOR UPPER SKIN DENTED BEYOND LIMITS AT STA XE83, 3 INCHES FROM TRAILING EDGE. 2 L 7 2 4F A6WE 1996101700372 19961017 00372 WP 1996 10 17 MWEA96549 1 19961011 A 5330 SKIN DOUG DC9 DC914 3022034 WP BS 697-702 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CK, FOUND AREA OF CORROSION ON FUSELAGE SKIN BEYOND LIMITS AT STA 697 TO 702 BETWEEN LONGERON 25R AND 26R. INS TALLED REPAIR IAW SRM 53-04, FIG 53. 2 L 7 2 4F A6WE 1996101700373 19961017 00373 WP 1996 10 17 MWEA96550 1 19961011 A 5730 PANEL DOUG DC9 DC914 3022034 WP RT WING LE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CK, FOUND RT WING L/E PANEL NR 2 TOP SKIN DENTED BEYOND LIMITS. INSTALLED REPAIR IAW SRM 57-03, FIG 4B. 2 L 7 2 4F A6WE 1996101700374 19961017 00374 WP 1996 10 17 MWEA96551 1 19961011 A 5712 RIB DOUG DC9 DC914 3022034 WP RT WING LE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CK, FOUND RT WING L/E SECTION NR 4 HAS THREE CRACKED RIBS. INSTALLED ANGLE REPAIRS IAW SRM 57-01, FIG 2. 2 L 7 2 4F A6WE 1996101700375 19961017 00375 WP 1996 10 17 MWEA96552 1 19961011 A 5320 991184093 CLIP DOUG DC9 DC914 3022034 WP BS 916 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CK, FOUND CRACK IN FRAME TO SKIN ATTACH CLIP AT STA 916 BETWEEN LONGERON 3L AND 4L AFT ACCESSORY COMPT. REPLAC ED ATTACH CLIP IAW SRM 51-30-01. 2 L 7 2 4F A6WE 1996101700376 19961017 00376 WP 1996 10 17 MWEA96553 1 19961011 A 5330 SKIN DOUG DC9 DC914 3022034 WP BS 699-718 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CK, FOUND FUSELAGE SKIN DENTED BETWEEN STA 699 TO 718 ABOVE LONGERON 17L. INSTALLED REPAIR IAW SRM 53-04, FIG 38, SHEET 17. 2 L 7 2 4F A6WE 1996101700377 19961017 00377 WP 1996 10 17 MWEA96554 1 19961011 A 5312 39151291 BULKHEAD FITTING DOUG DC9 DC914 3022034 WP AFT PRESS BLKHD CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CK, FOUND END FITTING AT PRESSURE BULKHEAD T-CAP HAS HEAVY CORROSION LONG 26L. REPLACED END FITTING IAW SRM 51 -10-4 AND 51-30. 2 L 7 2 4F A6WE 1996101700378 19961017 00378 WP 1996 10 17 MWEA96555 1 19961011 A 5320 39151291 FITTING DOUG DC9 DC914 3022034 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CK, FOUND IN FWD KEEL AREA LONGERON 27L, 28L, 29L, END FITTINGS HAVE HEAVY CORROSION. REPLACED L27L, 28L, 29L END FITTINGS IAW SRM 51-10-4 AND 51-30. 2 L 7 2 4F A6WE 1996101700379 19961017 00379 WP 1996 10 17 MWEA96556 1 19961011 A 5320 WEB DOUG DC9 DC914 3022034 WP BS 508-523 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CK, FOUND WEB IN KEEL AREA BETWEEN STA 508 TO 523 BULGED AND CRACKED, LONG 30. FABRICATED AND INSTALLED WEB SE CTION IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1996101700380 19961017 00380 WP 1996 10 17 MWEA96557 1 19961011 A 5730 SKIN DOUG DC9 DC914 3022034 WP LT WING LE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CK, FOUND LT WING LEADING EDGE SECTION NR 2 HAS .5 INCH CRACK IN AIR EXIT DUCT ON INNER SKIN. INSTALLED REPAIR IAW SRM 57-06, FIG 1. 2 L 7 2 4F A6WE 1996101700381 19961017 00381 WP 1996 10 17 MWEA96558 1 19961011 A 5712 RIB DOUG DC9 DC914 3022034 WP LT WING LE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CK, FOUND LEADING EDGE SECTION ON LT WING HAS TWO CRACKED RIBS, 6TH FROM INBD END AND MOST OUTBOARD. BOTH CRAC KED AT UPPER ENDS. INSTALLED DOUBLE ANGLE REPAIR IAW SRM 57-01 FIG 2, SHEET 3. 2 L 7 2 4F A6WE 1996101700382 19961017 00382 WP 1996 10 17 MWEA96559 1 19961011 A 5313 2777922 LONGERON DOUG DC9 DC914 3022034 WP BS 880 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80MKE 45795 DURING D-CK, FOUND LONGERON 11R CRACKED AT STA 880. INSTALLED NEW SECTION OF LONGERON 11R IAW SRM 53-02, FIG 2. 2 L 7 2 4F A6WE 1996101700383 19961017 00383 WP 1996 10 17 MWEA96560 1 19961011 A 5313 2777922 LONGERON DOUG DC9 DC914 3022034 WP BS 916 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CK, FOUND LONGERON 8R LOWER FLANGE DAMAGED AT STA 916 AFT ACCESSORY. SPLICED IN SECTION OF LONGERON 8R IAW SRM 53-02 FIG 2A. 2 L 7 2 4F A6WE 1996101700384 19961017 00384 WP 1996 10 17 MWEA96561 1 19961011 A 5311 FRAME DOUG DC9 DC914 3022034 WP BS 904 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CK, FOUND FRAME CRACKED AT STA 904, LONGERON 25L. INSTALLED FRAME REPAIR IAW SRM 53-01 FIG 2. 2 L 7 2 4F A6WE 1996101700385 19961017 00385 WP 1996 10 17 MWEA96562 1 19961011 A 5320 9911840 CLIP DOUG DC9 DC914 3022034 WP BS 916 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CK, FOUND FRAME TO SKIN ATTACH CLIP CRACKED AT STA 916 BETWEEN LONGERON 16R AND 17R. REPLACED SHEAR CLIP IAW S RM 51-30-01, FIG 1. 2 L 7 2 4F A6WE 1996101700386 19961017 00386 WP 1996 10 17 MWEA96563 1 19961011 A 5311 FRAME DOUG DC9 DC914 3022034 WP BS 925 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CK, FOUND FRAME CRACKED AT CANTED STA 925, LONGERON 13R. INSTALLED FRAME REPAIR IAW SRM 53-01 FIG 2. 2 L 7 2 4F A6WE 1996101700387 19961017 00387 WP 1996 10 17 MWEA96564 1 19961011 A 5720 TRAP PANEL DOUG DC9 DC914 3022034 WP RT MLG WW CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CK, FOUND RT TRAPEZOIDAL PANEL FWD FLANGE HAS A CRACK THAT EXTENDS AFT THROUGH THE FOURTH FASTENER APPROX .125 INCH. INSTALLED DOUBLER REPAIR IAW SRM 57-09, FIG 6 AND DAC TELEX SVC-MSP-0789. 2 L 7 2 4F A6WE 1996101700388 19961017 00388 WP 1996 10 17 MWEA96565 1 19961011 A 5312 BLKHD STIFFENER DOUG DC9 DC914 3022034 WP AFT PRESS BULKHD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CK, FOUND CRACK IN STIFFENER, AFT SIDE OF AFT PRESSURE BULKHEAD AT FOUR O'CLOCK POSITION JUST OUTBD OF DOOR JAM B APPROX .25 INCH IN LENGTH. INSTALLED DOUBLE ANGLE REPAIR IAW SRM 53-01, SHEET 4. 2 L 7 2 4F A6WE 1996101700389 19961017 00389 WP 1996 10 17 MWEA96566 1 19961011 A 5312 4594694 BLKHD STIFFENER DOUG DC9 DC914 3022034 WP AFT PRESS BLKHD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CK, FOUND CRACKED STIFFENER ON AFT SIDE OF AFT PRESSURE BULKHEAD JUST BELOW DOOR JAMB. INSTALLED STIFFENER IAW SRM 53-01. 2 L 7 2 4F A6WE 1996101700390 19961017 00390 WP 1996 10 17 MWEA96568 1 19961011 A 5522 2024T3 SKIN DOUG DC9 DC914 3022034 WP LT ELEVATOR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CK, FOUND LT ELEVATOR SKIN HAS SURFACE CORROSION AT OUTBD END. INSTALLED DOUBLER REPAIR IAW SRM 55-03 FIG 15. 2 L 7 2 4F A6WE 1996101700391 19961017 00391 WP 1996 10 17 MWEA96569 1 19961011 A 5242 59127561 DOOR PAN DOUG DC9 DC914 3022034 WP E/E DOOR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND E AND E DOOR JAMB PAN HAS CORROSION IN SEVERAL AREAS. MAINTENANCE REPLACED DOOR JAMB PAN IAW SRM 51-10-3 AND 51-30. 2 L 7 2 4F A6WE 1996101700392 19961017 00392 WP 1996 10 17 DLL14962233 1 19961006 A 3350 LIGHT 672320101 LKHEED 1011 1011385115 5265015 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 741DA 60832 193C1245 ON LAYOVER, FOUND EMERGENCY LIGHT POWER SUPPLY AT 3R INOP. 2 L 7 3 4F A23WE 1996101700393 19961017 00393 NM 1996 10 17 DL72K962236 1 19961001 A 5320 FITTING BOEING 727 727232 1384082 NM BS 740 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 417DA 21259 CORROSION AT STA 740 BETWEEN STR 28R AND 29R AT SKIN SUPPORT FITTING. REPLACED FITTING PER MM 53-11-0 PG 858. 2 L 7 3 4F A3WE 1996101700394 19961017 00394 NM 1996 10 17 DL72W962239 1 19961007 A 5522 657278420 SKIN BOEING 727 7272Q8 138407W NM RT ELEVATOR GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831L 21826 TWO HOLES PUNCTURED IN STIFFENER ON UPPER SKIN. REPAIRED STIFFENER PER SRM 55-20-3 FIG 3. 2 L 7 3 4F A3WE 1996101700395 19961017 00395 NM 1996 10 17 DL72W962240 1 19961007 A 5522 657278420 SKIN BOEING 727 7272Q8 138407W NM RT ELEVATOR GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831L 21826 UPPER L/E SKIN GOUGED. REPAIRED SKIN PER SRM 55-20-3 FIG 1. 2 L 7 3 4F A3WE 1996101700396 19961017 00396 NM 1996 10 17 DL76L962241 1 19961007 A 2530 OVEN 828450407 BOEING 767 767332 1382001 NM AFT GALLEY OVERHEATING A DALA H DEACTIVATE SYST/CIRCUITS A FLAME/FIRE CR CRUISE 1 SO 27 179DN 0097 25144 OVEN AT AFT GALLEY DEFECTIVE, NR 7 OVEN CAUSING SIDEWALL TO GET HOT AND CURLING VINYL WALLPAPER. C/B PULLED AND OVEN SE CURED. REPLACED OVEN, CHECKS OK. 2 L 7 2 4F RT A1NM 1996101700397 19961017 00397 NM 1996 10 17 DL76S962242 1 19961007 A 2530 OVEN 828450407 BOEING 767 767332 1382001 NM FWD GALLEY SPARKING A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 132DN 24981 NR 1 UPPER OVEN MADE A LOUD POP AND SPARKS FLEW WHEN TURNED ON. REPLACED OVEN. 2 L 7 2 4F RT A1NM 1996101700398 19961017 00398 NM 1996 10 17 DL72W962243 1 19961007 A 3350 900835A BATTERY PACK BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2817W 20873 FWD OVERWING EXIT LIGHT ON RIGHT SIDE OF FUSELAGE INOP. REPLACED BATTERY PACK, OVERWING EXIT LIGHT CHECKED GOOD. 2 L 7 3 4F A3WE 1996101700399 19961017 00399 NM 1996 10 17 DL72S962248 1 19961007 A 5320 ANGLE BOEING 727 727232 1384082 NM RT KEEL BEAM CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 539DA 22385 FOUND A 1.5 INCH CRACK IN RT KEEL BEAM SUPPORT ANGLE. MADE TIME LIMITED REPAIR PER SRM 53-10-9. 2 L 7 3 4F A3WE 1996101700400 19961017 00400 NM 1996 10 17 DL72S962249 1 19961007 A 5330 SKIN BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 539DA 22385 A .375 INCH CRACK IN FUSELAGE SKIN JUST AFT OF R-3 WINDOW. INSTALLED DOUBLER PER SRM 53-03-3 FIG 8, IV. 2 L 7 3 4F A3WE 1996101700401 19961017 00401 NM 1996 10 17 DLM11962253 1 19961008 A 2100 INLET DUCT 9276021 DOUG MD11 MD11 3023602 NM HEAT EXCHANGER CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 801DE 48472 FOUND NR 1, NR 2, NR 3 HEAT EXCHANGER TURBINE INLET DUCTS CORRODED AT THE INLET FLANGE. SUSPECT SEAL LEAKAGE IPC LOC 21 -53-01-01 NR 325. 2 L 7 3 4F RT A22WE 1996101700402 19961017 00402 WP 1996 10 17 DLL10962257 1 19960916 A 5743 1527275140 RIB FITTING LKHEED 1011 10113851 5265010 WP RT WING CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 714DA 193C1090 THE RT MLG ATTACH RIB FITTING HAD CORROSION REMOVED FROM THE LUG FACES AND BORE OF THE FWD AND AFT LUGS OF THE OF THE FO RWARD TRUNNION LUG SET AND THE FWD AND AFT LUGS OF THE AFT TRUNNION LUG SET. THE DAMAGED AREAS WERE REWORKED. 2 L 7 3 4F A23WE 1996101700403 19961017 00403 WP 1996 10 17 DLL13962258 1 19960929 A 5711 1528363250 SPAR WEB LKHEED 1011 10113851 5265010 WP WS 310-330 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 786DL 193A1123 THE RT WING REAR SPAR WEB AT THE UPPER CAP ATTACH AT IWS 310-330 AND UPPER WING SKIN HAS A CRACK. THE DAMAGE WAS REINFO RCED WITH A REPAIR PLATE. 2 L 7 3 4F A23WE 1996101700404 19961017 00404 WP 1996 10 17 DLL10962259 1 19960910 A 5712 1647070 RIB LKHEED 1011 10113851 5265010 WP LT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 714DA 193C1090 LT WING PYLON SUPPORT UPPER RIB CAP AT IWS 529-555 HAS A CRACKED CASTELLATION. THE DAMAGE WAS CUT OUT AND REPLACED. 2 L 7 3 4F A23WE 1996101700405 19961017 00405 WP 1996 10 17 DLL10962260 1 19960924 A 5753 1529504104 TORQUE BOX LKHEED 1011 10113851 5265010 WP RT FLAP VANE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 714DA 193C1090 THE RT WING FLAP VANE I/B TRACK NR 2 TORQUE BOX WAS FOUND CRACKED. THE TORQUE BOX WAS REPLACED. 2 L 7 3 4F A23WE 1996101700406 19961017 00406 WP 1996 10 17 DLL10962261 1 19960916 A 5330 1504624 SKIN LKHEED 1011 10113851 5265010 WP FS 1685 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 714DA 193C1090 SKIN CORROSION WAS FOUND BETWEEN FS 1675 TO 1695 AND FROM JUST BELOW STR 38 TO SLIGHTLY ABOVE STR 39. THE CORROSION WAS TRIMMED OUT AND REINFORCED WITH A DOUBLER. 2 L 7 3 4F A23WE 1996101700407 19961017 00407 WP 1996 10 17 DLL10962263 1 19960904 A 5712 1647070 RIB LKHEED 1011 10113851 5265010 WP WS 503 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 714DA 193C1090 BOTH SIDES IWS 503 RIB UPPER CAP WAS FOUND WITH SEVERAL ATTACH TAB CRACKS IN THE TYPICAL LOCATIONS AFT OF STR 24, AS WEL L AS FWD OF STR 24. THESE FWD CRACKS NECESSITATED THE COMPLETE REPLACEMENT OF THE UPPER CAPS. 2 L 7 3 4F A23WE 1996101700408 19961017 00408 WP 1996 10 17 DLL10962264 1 19960911 A 5320 1505672103 SILL LKHEED 1011 10113851 5265010 WP BS 892 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 714DA 193C1090 THE L2 DOOR LOWER SILL AND THE UNDERLYING AREA OF THE O/B LONGERON BELOW WAS FOUND WITH CORROSION. THE CORROSION WAS BL ENDED OUT AND THE AREA WAS REINFORCED. 2 L 7 3 4F A23WE 1996101700409 19961017 00409 WP 1996 10 17 DLL10962265 1 19960905 A 5330 1503490 SKIN LKHEED 1011 10113851 5265010 WP BS 479 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 714DA 193C1090 THE FUSELAGE SKIN AT FS 469 TO 489 AT STR 39 TO 42 SURROUNDING THE PNEUMATIC BLEED AIR EXHAUST WAS FOUND WITH CORROSION. THE CORROSION WAS TRIMMED OUT AND REINFORCED WITH A DOUBLER. 2 L 7 3 4F A23WE 1996101700410 19961017 00410 WP 1996 10 17 DLL10962266 1 19960830 A 5320 LS13112 DECK LKHEED 1011 10113851 5265010 WP FS 378 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 714DA 193C1090 THE FUSELAGE HORIZ PRESSURE DECK PANEL WAS FOUND WITH A CRACK AT RBL 102 AND FS 378. THE CRACK WAS TRIMMED OUT AND REIN FORCED WITH DOUBLERS AND TRIPLERS. 2 L 7 3 4F A23WE 1996101700411 19961017 00411 WP 1996 10 17 DLL16962267 1 19961003 A 5730 1528363 SKIN LKHEED 1011 10113853 5265020 WP WS 324/329 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 762DA 193Y1210 A CRACK WAS FOUND IN THE UPPER WING SKIN AT THE REAR SPAR UPPER CAP ATTACH LOCATION IN THE FWD ROW AT APPROX IWS 324 AN D IN THE AFT ROW AT IWS 329. THE CRACKS WERE REMOVED BY OVERSIZING NEARBY HOLES. 2 L 7 3 4F A23WE 1996101700412 19961017 00412 WP 1996 10 17 DLL10962268 1 19960916 A 5320 154239511 DECK LKHEED 1011 10113851 5265010 WP BS 339 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 714DA 193C1090 THE NLG PRESSURE DECK PANEL BETWEEEN FS 328 TO 349 ON THE UPPER SURFACE OF THE PANEL ON BOTH SIDES OF LBL 22 WAS FOUND T O BE CORRODED. THE CORROSION WAS CUT OUT AND REINFORCED WITH A DOUBLER. 2 L 7 3 4F A23WE 1996101700413 19961017 00413 NM 1996 10 17 DL76S962269 1 19960426 A 5330 143T3520 SKIN BOEING 767 767332 1382001 NM FS 445/490 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 126DL 24076 THE FUSELAGE SKIN AT FS 445 AND FS 490 BETWEEN STR 33R AND34R ON THE RT SIDE WERE FOUND WITH PREVIOUS DAMAGE. ALSO A CR ACK WAS FOUND AT FS 500 STR 38. THE CRACK WAS CUT OUT, REINFORCED AND THE PREVIOUS DAMAGE HAD UPDATED REPAIRS. 2 L 7 2 4F RT A1NM 1996101700414 19961017 00414 NM 1996 10 17 DL73S962270 1 19961003 A 5743 ATTACH FITTING BOEING 737 737232 1384475 NM RT MLG BEAM CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 332DL 23104 RIGHT WING OB AFT SUPPORT FITTING FOR THE MAIN LANDING GEAR BEAM WAS FOUND CRACKED. CRACKING TYPICAL TO THAT DESCRIBED IN BOEING SERVICE BULLETIN 737-57-1216. A/C 332 IDENTIFIED AS A GROUP 5 BY THE SERVICE BULLETIN. THE CRACKED FITTING W ILL REMAIN IN SERVICE ON A TIME LIMITED BASIS AND WILL BE REPAIRED ACCORDING TO SERVICE BULLETIN REQUIREMENTS. 2 L 7 2 4F RT A16WE 1996101700415 19961017 00415 NM 1996 10 17 DL73S962271 1 19960927 A 5312 65163007 BULKHEAD BOEING 737 737232 1384475 NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 334DL 23105 MULTIPLE CRACKS DISCOVERED ON THE FORWARD FACE OF THE FS 178 BULKHEAD WEB WHILE ACCOMPLISHING SI 3-69482-14. DAMAGE REM OVAL RESULTED IN ONE CUTOUT AT LBL 5.7, RANGING FROM WL 197 TO WL 203, AND A SECOND CUTOUT AT RBL 5.7, RANGING_FROM WL 1 97 TO WL 203. LBL 5.7 CUTOUT MEASURES 4.125 VERTICALLY BY 1.0 IB TO OB. THE RBL 5.7 CUTOUT MEASURES 4.75 VERTICALLY BY 1.125 IB TO OB. THE WEB IS MANUFACTURED FROM 0.32 2023-T3CLAD ALUMINUM. 2 L 7 2 4F RT A16WE 1996101700416 19961017 00416 NM 1996 10 17 DL73S962272 1 19961003 A 5312 651630084 BULKHEAD WEB BOEING 737 737232 1384475 NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 311DL 23083 DURING ACCOMPLISHMENT OF SI 3-69482-12, 3 CRACKS DISCOVERED ON THE FWD FACE OF THE FS 178 BULKHEAD WEB. THREE INDEPENDE NT CUTOUTS WERE REQUIRED TO REMOVE THE CRACKS. FIRST CUTOUT, LOCATED I/B OF THE RBL 5.7 VERTICAL STRAP AT WL 201, MEAS URES 1.6 VERTICALLY BY 1.O IB TO OB. THE 2ND CUTOUT IS LOCATED JUST BELOW 1ST CUTOUT AT WL 198 AND MEASURES 1.7 VERTICA LLY BY 1.O IB TO OB. THE 3RD CUTOUT, LOCATED ON THE O/B SIDE OF THE LBL 5.7 VERTICAL STRAP AT WL 198, IS A 1.O DIAMET ER CIRCLE. THE BULKHEAD WEB IS MANUFACTURED FROM 0.032 THICK 2024-T3 CLAD ALUMINUM. 2 L 7 2 4F RT A16WE 1996101700417 19961017 00417 NM 1996 10 17 DL73S962273 1 19961003 A 5330 6545778569 SKIN BOEING 737 737232 1384475 NM C-2 DOOR OPENING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 311DL 23083 AFT EDGE STA 840 OF C-2 DOOR OPENING HAS 3 SMALL CRACKS THAT ARE STOP DRILLED BETWEEN STRINGERS 21R AND 22R. THE CRACKS EXTEND THROUGH THE BONDED SKIN 0.036 + 0.036 CLAD 2024-T3 AND BEAR STRAP 0.125 2024-T3. 2 L 7 2 4F RT A16WE 1996101700418 19961017 00418 NM 1996 10 17 DL73S962274 1 19960930 A 5320 65C31716 DOORWAY FRAME BOEING 737 737232 1384475 NM BS 847 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 311DL 23083 AFT FRAME ON THE C-1 DOORWAY WAS FOUND TO BE CRACKED APPROX 6 BELOW THE LOWER STOP FITTING. THE CRACK IS LOCATED WHERE FRAME WAS GOUGED. A 1.10 DIAMETER HOLE WAS REQUIRED TO CLEAN UP THE DAMAGE TO THE WEB. MATERIAL IS 0.071 7075-T6. THE CRACK WILL BE REPAIRED PER THE INSTRUCTIONS OF AD 93-14-10 AND SB 737-53-1096, REV 5 (DAL SI 3-55297-12AD). 2 L 7 2 4F RT A16WE 1996101700419 19961017 00419 NM 1996 10 17 DL72L962262 1 19961009 A 3350 LIGHT 1000677 BOEING 727 727232 1384082 NM COCKPIT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 508DA 9288 21310 COCKPIT EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY, CK OK. 2 L 7 3 4F A3WE 1996101700420 19961017 00420 NM 1996 10 17 DL72S962276 1 19961009 A 5610 WINDOW BOEING 727 727232 1384082 NM R-1 SMOKING A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 485DA 20865 WHITE SMOKE EMITTED FROM UPPER RIGHT CORNER OF R-1 WINDOW WHILE CLIMBING THROUGH 27,000 FT. NO OVERHEAT LIGHT, WINDOW W AS HOTTER TO TOUCH THAN R-2, L-1, L-2. SECURED R-1 HEAT, FOUND OUTBD WINDOW HEAT CONTACT TOUCHING WINDOW FRAME. RETERM INATED WIRE AND DRESSED AREA, OPERATION NORMAL. 2 L 7 3 4F A3WE 1996101700421 19961017 00421 NM 1996 10 17 DL72L962280 1 19961009 A 3320 61482 BALLAST BOEING 727 727232 1384082 NM CABIN SHORTED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 502DA 21304 SMOKE AND FUMES COMING FROM FWD LAV. SECURED WATER HEATER AND FLUSH MOTOR, SMOKE AND FUMES IMMEDIATELY DISSIPATED. AIR CRAFT WAS ON APPROACH INTO PHX. MAINTENANCE ACTION TROUBLESHOOTING FOUND FWD ENTRY LIGHT BRIGHT C/B POPPED AND WOULD NO T RESET. FOUND BAD ENTRY LIGHT BALLAST. REPLACED BALLAST, OPERATIONAL CHECKS OK. 2 L 7 3 4F A3WE 1996101700422 19961017 00422 NM 1996 10 17 DLM88962282 1 19961010 A 3350 41B004AD073 BATTERY DOUG MD88 MD88 3023688 NM COCKPIT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 996DL 53363 OVERHEAD COCKPIT EMERGENCY LIGHT INOP. C/A REPLACED B5-23 POWER SUPPLY BATTERIES, OP CK OK. 2 L 7 2 4F RT A6WE 1996101700423 19961017 00423 NM 1996 10 17 DLM11962283 1 19961010 A 3510 OXY REGULATOR 223900015 DOUG MD11 MD11 3023602 NM E/E COMPARTMENT LEAKING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 802DE 005 48473 CREW O2 LOW, FOUND REGULATOR LEAKING AT BOTTLE CONNECTION. REPLACED REGULATOR, SERVICED O2 BOTTLE AND LEAK CK OK. 2 L 7 3 4F RT A22WE 1996101700424 19961017 00424 NE 1996 10 17 DL757962289 2 19961010 A 7200 ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 FAILED A DALA F ACTIVATE FIRE EXT. A FLAME/FIRE AP APPROACH 1 SO 27 612DL 17277 22819 716571 RIGHT ENGINE EGT WENT INTO THE RED AT ABOUT 500 FT AGL ON APPROACH, FOLLOWED BY A RED INDICATION ON RIGHT ENGINE OIL PRE SSURE. FLIGHT ATTENDANT REPORTED FIRE FROM RIGHT ENGINE. PERFORMED ENGINE FIRE CHECKLIST INCLUDING USING BOTH FIRE BO TTLES. 2 L 7 2 4F 4 F RT A2NM E17NE 1996101700425 19961017 00425 NM 1996 10 17 DL72E962291 1 19961011 A 3350 BATTERY S106 BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 830WA 9709 21482 LEFT SIDE EMERGENCY LIGHT OUTSIDE AND BEHIND LEFT WING WOULD NOT ILLUMINATE STEADY. REPLACED BATTERY. 2 L 7 3 4F A3WE 1996101700426 19961017 00426 NM 1996 10 17 DL72K962292 1 19961001 A 5400 S-DUCT WEB BOEING 727 727232 1384082 NM NR 2 ENGINE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 417DA 21259 DURING ACCOMPLISHMENT OF EO 4-59253-12 OPN 0120, FOUND .5 INCH VISIBLE CRACK IN LOWER LT CORNER OF VERTICAL WEB CROSSING NR 2 ENG INLET S-DUCT AT STA 1303. STOP DRILLED CRACK PER SRM 53-10-4 PG 65, INSTALLED DOUBLER PER SRM 53-10-4. 2 L 7 3 4F A3WE 1996101700427 19961017 00427 NM 1996 10 17 DL76S962294 1 19961010 A 7120 MOUNT BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 2 ENGINE LOOSE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 137DL 17603 25306 580384 DURING LETTER CHECK NR 34 WRITTEN, GAP BETWEEN FWD ENG MOUNT AND AND PYLON. REMOVED ENG PER 1T147, INSPECTED ON NR 34 A ND NO DAMAGE FOUND TO MOUNTS. REPLACED ALL MOUNT NUTS, REINSTALLED SAME ENG. 2 L 7 2 4F 4 F RT A1NM E13NE 1996101700428 19961017 00428 NM 1996 10 17 DL72K962296 1 19961011 A 3350 RPS1B PWR SUPPLY BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 491DA 21060 AFT 3 SECTIONS OF E PATH LIGHTS REMAIN ILLUM IN ARM POS. REPLACED FWD E PATH SLED, OPS NORMAL. 2 L 7 3 4F A3WE 1996101700429 19961017 00429 WP 1996 10 17 DLL14962298 1 19961011 A 3350 LIGHT LKHEED 1011 1011385115 5265015 WP GE CF680 CF680A2 NE CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1738D 193C1234 580384 ONE BULB INOP EMERGENCY PATH LIGHT NEAR 1C. REPAIRED LIGHT FIXTURE AND REPLACED WORN TRACK IN FWD FIRST CLASS, EMERGENC Y LIGHT OPS CHECKS GOOD. 2 L 7 3 4F 4 F A23WE E13NE 1996101700430 19961017 00430 NM 1996 10 17 DL72W962299 1 19961011 A 3350 BATTERY PACK 900835A BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 292WA 8458 22110 OVERWING EXIT SIGNS INOP ON RIGHT SIDE. REPLACED BATTERY PACK AT M1086, OPS CHECKS OK. 2 L 7 3 4F A3WE 1996101700431 19961017 00431 NM 1996 10 17 DL72W962300 1 19961011 A 3350 LIGHT 1000677 BOEING 727 727247 138408F NM FWD GALLEY INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 292WA 2511 22110 FWD GALLEY DOOR REMOVABLE EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY AND BATTERIES, OPS CHECKS OK. 2 L 7 3 4F A3WE 1996101700432 19961017 00432 NM 1996 10 17 DL757962305 1 19961012 A 3397 WIRE BOEING 757 757232 1384965 NM L-2 DOOR SHORTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 623DL 22913 EMERGENCY FLOOR TRACK LIGHTS INOP IN F/C. REPAIRED SHORTED WIRE AT L-2 DOOR. 2 L 7 2 4F RT A2NM 1996101700433 19961017 00433 NM 1996 10 17 DL757962306 1 19961011 A 3350 LIGHT BOEING 757 757232 1384965 NM CABIN MISSING A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 633DL 23614 EMERGENCY TRACK LIGHT MISSING AT SEAT 3B. REPLACED LIGHT AND LENS. 2 L 7 2 4F RT A2NM 1996101700434 19961017 00434 WP 1996 10 17 DLL13962307 1 19961012 A 3350 LIGHT 07912 LKHEED 1011 10113851 5265010 WP CABIN MISSING A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 787DL 193A1126 EMERGENCY TRACK LIGHT AT SEAT 3D IS MISSING A LIGHT AND A WIRE IS STICKING OUT. REPLACED LIGHT LENS, CHECKS NORMAL. 2 L 7 3 4F A23WE 1996101700435 19961017 00435 NE 1996 10 17 DL76L962308 2 19961012 A 7200 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 FAILED A DALA E A ENGINE SHUTDOWN UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 SO 27 183DN 14917 2962 27110 724146 LEFT ENGINE STALLED AT CRUISE, ENGINE WAS SHUTDOWN. A/C MADE AN UNSCHEDULED LANDING IN YYR. NR 1 ENGINE CHANGE. 2 L 7 2 4F 4 F RT A1NM E24NE 1996101700438 19961017 00438 NM 1996 10 17 SCNA96288 1 19961006 A 3350 900835A BATTERY PACK BOEING 727 7272J4 1384006 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 284SC 21438 OVERHEAD EMERGENCY EXIT SIGN ABOVE R2 DOOR FLASHES ON AND OFF. REMOVED AND REPLACED BATTERY PACK IN ACCORDANCE WITH MM 33-50-31, SYSTEM OPS CHECKS GOOD. 2 L 7 3 4F RT A3WE 1996101700439 19961017 00439 NM 1996 10 17 SCNA96289 1 19961007 A 3350 1315 BULB BOEING 727 727225 1384077 NM CABIN FAILED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 282SC 22558 LEFT AFT OVERWING EXIT SIGN HAS A BULB INOP. RELAMPED LEFT AFT OVERWING EXIT SIGN AND OPS CHECKS GOOD. 2 L 7 3 4F A3WE 1996101700440 19961017 00440 SO 1996 10 17 SRAA961005 1 19961010 A 3230 1650E615 RETRACT MECH LKHEED 382 382G 526414U SO LT MLG OUT OF ADJUST A SRAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 23 912SJ 2536 161 4388 DURING FINAL APPROACH, LEFT MAIN LANDING GEAR FAILED TO LOCK IN DOWN POSITION USING NORMAL PROCEDURE. MANUALLY EXTENDED LEFT MLG TO DOWN AND LOCK BY AOM PROCEDURE. AIRCRAFT LANDED WITHOUT INCIDENT. PLACED AIRCRAFT ON JACKS AND PERFORMED GEAR RETRACTION CHECK. FOUND LEFT MAIN GEAR DIFFICULT TO RETRACT MANUALLY. REMOVED AND REPLACED LEFT FORWARD BALLSCREW ASSY AND ADJUSTED SHOES, SYSTEM OPS CHECKED GOOD. 2 H 7 4 4T A1SO 1996101700441 19961017 00441 NM 1996 10 17 SRAA961006 1 19961013 A 5210 65B0431116 SKIN BOEING 747 747212B 1384886 NM R4 DOOR DAMAGED A SRAA K NONE D INFLIGHT SEPARATION UK UNKNOWN 1 GL 23 745SJ 20888 POST FLIGHT INSPECTION, FOUND LOWER RIGHT CORNER OF R4 DOOR SKIN MISSING APPROX 1 SQ FT. ACCOMPLISHED UNPRESSURIZED MAI NTENANCE FERRY TO LUX FOR REPAIR. REMOVE R4 DOOR, INSPECTED DOOR FRAME AND NO DEFECTS NOTED. REPLACED R4 WITH SERVICEA BLE UNIT, RIGGED AND OPS CHECKED PER MM CH 52-11-01. 2 L 7 4 4F A20WE 1996101700442 19961017 00442 EU 1996 10 17 HEEA968000 1 19961002 A 6330 579063 LAMINATE SNIAS 350 AS350B2 8680813 EU BEARING TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100R 1026 2862 BEARING LAMINATE TORN. 1 G 7 1 3U H9EU 1996101700443 19961017 00443 EU 1996 10 17 HEEA968001 1 19961002 A 2121 420800001 BLOWER SNIAS 350 AS350B2 8680813 EU COOLING FAN INOP E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 350BZ 305 2653 BLOWER INOPERATIVE. 1 G 7 1 3U H9EU 1996101700444 19961017 00444 EU 1996 10 17 HEEA968002 1 19961002 A 6520 350A27191004 ROD,ACTUATING SNIAS 350 AS350B2 8680813 EU T/R GR BOX WORN EXCESS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 2990 2771 ACTUATING ROD IS WORN EXCESSIVELY. 1 G 7 1 3U H9EU 1996101700445 19961017 00445 NE 1996 10 17 HEEA968003 2 19961003 A 7510 5044T08P05 VALVE BELL 214 214ST 1182106 SW GE CT7TS CT72A 30030 NE ANTI ICE OUT OF LIMIT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 PISTON MOVEMENT EXCEEDS LIMITS PER SBCT7-TS)75-2. 2 G 7 2 4U 4 U H10SW E8NE 1996101700446 19961017 00446 EU 1996 10 17 HEEA968004 1 19961003 A 2612 9560129970 FIRE DETECTOR SNIAS 350 AS350B2 8680813 EU ENGINE MALFUNCTION E HEEA K NONE N FALSE WARNING IN INSP/MAINT 1 SW 03 6100R 1318 2862 ENGINE FIRE LIGHT STAYS ON. 1 G 7 1 3U H9EU 1996101700447 19961017 00447 1996 10 17 HEEA968005 4 19961003 A 3454 066107810 RECEIVER KNR634A SKRSKY S76 S76A 8143006 NE COCKPIT NAV FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 476X 493 760436 WILL NOT POINT TO STATION OR HOLD STATION. 1 G 7 2 3U H1NE 1996101700449 19961017 00449 SW 1996 10 17 HEEA968007 1 19961003 A 6300 214040091105 HOUSING BELL 214 214ST 1182106 SW M/R DRV CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 745H 1724 28200 HOUSING IS CORRODED. (CORROSION ON FLANGES) (ARAMCO AIRCRAFT) 2 G 7 2 4U H10SW 1996101700450 19961017 00450 SW 1996 10 17 HEEA968008 1 19961003 A 2810 206064633105 FUEL CELL BELL 206 206L1 1182107 SW FUEL SYS LEAKS E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 FUEL CELL FAILED ACCEPTANCE CHECK. LEAKS. TIME SINCE REPAIR 0:00. 1 G 7 1 3U H2SW 1996101700451 19961017 00451 EU 1996 10 17 HEEA968009 1 19961003 A 6520 350A33020005 GEAR BOX SNIAS 350 AS350B2 8680813 EU T/R LEAKS E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 6100U 1104 2863 LEAKS OIL FROM FRONT SEAL AND OUTPUT SHAFT, SEAL IS TORN. 1 G 7 1 3U H9EU 1996101700452 19961017 00452 1996 10 17 HEEA968010 4 19961003 A 2340 900C3010064105 ICS SWITCH DOUG MD900 MD900 3027375 NM CYCLIC STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 9214U 70 90000014 CYCLIC GRIP ICS SWITCH STICKS-HOT MIC CONDITION. 1 G 7 2 3U NC H19NM 1996101700453 19961017 00453 EU 1996 10 17 HEEA968011 1 19961003 A 2121 420800001 BLOWER SNIAS 350 AS350B2 8680813 EU COOLER FAN INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 41 BLOWER INOPERATIVE. 1 G 7 1 3U H9EU 1996101700454 19961017 00454 EU 1996 10 17 HEEA968012 1 19961003 A 7712 9580113720X TRANSMITTER SNIAS 350 AS350B2 8680813 EU ENG TORQUE DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4000L 321 2873 GAUGE FLUCTUATES AND PEGS OUT. 1 G 7 1 3U H9EU 1996101700455 19961017 00455 1996 10 17 HEEA968013 4 19961003 A 3454 066107810 RECEIVER KNR634A SKRSKY S76 S76A 8143006 NE COCKPIT NAV DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 476X 760436 WITH STATION OFF, HSI GLIDE SLOPE OFF. FLAG COMES OUT. GLIDE SLOPE INDICATOR PARKS AT TOP OF HSI. 1 G 7 2 3U H1NE 1996101700456 19961017 00456 1996 10 17 HEEA968014 4 19961003 A 3421 40205773 GYRO BOLKMS 117 BK117A4 5626017 EU COCKPIT DG DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911RZ 1952 7092 COCKPIT DIR GYRO WILL NOT ALIGN OR SLAVE. 1 G 7 2 3U H13EU 1996101700457 19961017 00457 1996 10 17 HEEA968015 4 19961003 A 2210 7690001803101 CONTROL PANEL SKRSKY S76 S76A 8143006 NE COCKPIT AFCS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911MJ 760231 ROLL CHANNEL NOT SHOWING RESPONSE OR INDICATOR PANEL. 1 G 7 2 3U H1NE 1996101700458 19961017 00458 1996 10 17 HEEA968016 4 19961003 A 3420 7690001808102 RATE GYRO SKRSKY S76 S76A 8143006 NE AUTO FLT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 RATE GYRO CAUSES ACTUATOR TO CHATTER. 1 G 7 2 3U H1NE 1996101700459 19961017 00459 SW 1996 10 17 HEEA968017 1 19961003 A 7712 412075008111 INDICATOR BELL 412 412 1182202 SW NR 2 TORQUE DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 107X 33113 TORQUE METER #2 WILL NOT GO BELOW 35%. 1 G 7 2 4U H4SW 1996101700460 19961017 00460 SW 1996 10 17 HEEA968018 1 19961003 A 7712 412075008111 INDICATOR BELL 412 412 1182202 SW TORQUE DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893S 33022 INDICATOR IS CAUSING NUMBER 1 TORQUE CIRCUIT BREAKER TO POP. 1 G 7 2 4U H4SW 1996101700461 19961017 00461 NE 1996 10 17 HEEA968019 1 19961003 A 2421 7655009005110 GENERATOR SKRSKY S76 S76A 8143006 NE AC SYS FAILED E HEEA K NONE J WARNING INDICATION NR NOT REPORTED 1 SW 03 2743E 760155 A/C BEARING LIGHT CAME ON IN FLIGHT. 1 G 7 2 3U H1NE 1996101700462 19961017 00462 EU 1996 10 17 HEEA968020 1 19961003 A 7714 KDWO21A RPM WARN BOX BOLKMS 105 BO105S 5626006 EU ENG MALFUNCTION E HEEA K NONE J WARNING INDICATION NR NOT REPORTED 1 SW 03 5421E S806 WARNING LIGHT ILLUMINATES AT 100% N2 AND 100% NR WITH N1'S MATCHED. DOES NOT ILLUMINATE WITH 12% N1 SPLIT. 1 G 7 2 3U H3EU 1996101700463 19961017 00463 SW 1996 10 17 HEEA968021 1 19961003 A 7933 209070262101 INDICATOR BELL 412 412 1182202 SW ENG OIL TEMP FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 7128R 36007 NO TEMP INDICATION. 1 G 7 2 4U H4SW 1996101700464 19961017 00464 1996 10 17 HEEA968022 4 19961003 A 2210 214074300107 AFCS BELL 214 214ST 1182106 SW COCKPIT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 8045T 28101 ALTITUDE HOLD LIGHT INOPERATIVE. 2 G 7 2 4U H10SW 1996101700465 19961017 00465 SW 1996 10 17 HEEA968023 1 19961003 A 2844 124044 INDICATION BELL 412 412 1182202 SW FUEL PRESS FLUCTUATION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2261D 33076 PRESSURE FLUCTUATION. 1 G 7 2 4U H4SW 1996101700466 19961017 00466 NE 1996 10 17 HEEA968024 2 19961003 A 7250 3017600 ENGINE BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE POWER SECT RUMBLE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893S 13757 33022 WHEN ENGINE IS HOT, THERE IS A RUBBING SOUND IN ENGINE. RUMBLE SOUND WITH HIGH FREQUENCY WHEN RUNNING. 1 G 7 2 4U 4 U H4SW E22EA 1996101700467 19961017 00467 NE 1996 10 17 HEEA968025 2 19961003 A 7230 3017600 ENGINE BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE POWER SECT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3911L 12772 33023 COMPRESSOR FAILURE CAUSING MAJOR ENGINE DAMAGE. 1 G 7 2 4U 4 U H4SW E22EA 1996101700468 19961017 00468 SW 1996 10 17 HEEA968026 1 19961003 A 6220 412010190103 SPINDLE BELL 412 412 1182202 SW M/R UNBONDED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893P 2977 33012 BEARING UNBONDED. 1 G 7 2 4U H4SW 1996101700469 19961017 00469 SW 1996 10 17 HEEA968027 1 19961003 A 7714 8DJ131LAV1 INDICATOR BELL 212 212 1181420 SW TRIPLE TACH INTERMITTENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1079U 31122 #1 NEEDLE HAS INTERMITTENT OPERATION. 1 G 7 1 4U H4SW 1996101700471 19961017 00471 NM 1996 10 17 HEEA968029 1 19961003 A 3212 62915102 FLOAT BOTTLE DOUG MD900 MD900 3027375 NM FLOAT LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 9214U 90000014 FLOAT BOTTLE LEAKING. 1 G 7 2 3U NC H19NM 1996101700472 19961017 00472 SW 1996 10 17 HEEA968030 1 19961003 A 7714 206070266009 INDICATOR BELL 206 206L1 1182107 SW COCKPIT STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 406EH 45183 NEEDLE STICKS ON LOW END. 1 G 7 1 3U H2SW 1996101700473 19961017 00473 SW 1996 10 17 HEEA968031 1 19961003 A 2840 206075186005 INDICATOR BELL 206 206L1 1182107 SW FUEL SIDE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1072T 45385 NEEDLE ON FUEL SIDE HAS NO INDICATION. 1 G 7 1 3U H2SW 1996101700474 19961017 00474 1996 10 17 HEEA968032 4 19961003 A 3416 59341 ALTIMETER BELL 206 206L3 1182108 SW COCKPIT CASE LEAK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 206LS 51070 EXCESSIVE CASE LEAK. ALSO AT 10,000 FEET NEEDLE INDICATES 50,000 FEET. 1 G 7 1 3U H2SW 1996101700476 19961017 00476 SW 1996 10 17 HEEA968035 1 19961003 A 2621 A352T EXTINGUISHER BELL 412 412 1182202 SW FIRE SYS DISCHARGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D 105 33076 DISCHARGED. SENT TO HRD AERO SYSTEMS FOR OVERHAUL. 1 G 7 2 4U H4SW 1996101700477 19961017 00477 NE 1996 10 17 HEEA968036 1 19961003 A 3230 7625100702043 LINK ASSY SKRSKY S76 S76A 8143006 NE MLG BENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 117WB 760092 LINK IS BENT. 1 G 7 2 3U H1NE 1996101700478 19961017 00478 EU 1996 10 17 HEEA968037 1 19961003 A 7921 1176801101 OIL COOLER BOLKMS 117 BK117A4 5626017 EU ENG OIL CONTAMINATION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911RZ 7092 OIL COOLER METAL CONTAMINATION. 1 G 7 2 3U H13EU 1996101700479 19961017 00479 1996 10 17 HEEA968039 4 19961003 A 3452 066106200 TRANSCEIVER KT76 BOLKMS 117 BK117B1 5626012 EU COCKPIT ATC DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 217UC 7152 ATC NOT PICKING UP SIGNAL. FOUND SWITCH ASSY WORKING INTERMITTENTLY. CLEANED SWITCHES , NO HELP. REPLACED SWITCH ASSY P/N 200-00381-0001. REPAIRED. BENCH CHECK GOOD. 1 G 7 2 3U H13EU 1996101700480 19961017 00480 1996 10 17 HEEA968040 4 19961003 A 3452 066106200 TRANSCEIVER KT76 SNIAS 350 AS350B2 8680813 EU COCKPIT ATC FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4031L 2907 SIGNAL IS INTERMITTENT. INSTALLED Q415 HEATSINK. REPLACED HEAT SHRINK ON 9V LINE FOR LOCAL OSCILLATOR. PLACED IN FREEZ ER, UNIT STILL INTERMITTENT. FOUND IC I405 BAD. REPLACED IC I405. REPAIRED. BENCH CHECK GOOD. 1 G 7 1 3U H9EU 1996101700482 19961017 00482 1996 10 17 HEEA968042 4 19961003 A 3452 066106200 TRANSCEIVER KT76 BELL 206 206L1 1182107 SW COCKPIT ATC DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 50182 45242 KNOB BROKEN. REPLACED FACEPLATE ASSEMBLY. ALSO REPLACED WEAK V301 PHOTODETECTOR AND REPLACED BROKEN PLASTIC LOCKING MEC HANISM. BENCH CHECK GOOD. 1 G 7 1 3U H2SW 1996101700483 19961017 00483 1996 10 17 HEEA968043 4 19961003 A 3452 066106200 TRANSCEIVER KT76 BELL 206 206L1 1182107 SW COCKPIT ATC INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2770Y 45291 INOPERATIVE. REPLACED V101CAVITY OSC. REPAIRED. ADJUSTED PULSE WIDTH AND FREQUENCY, ALSO ADJUSTED SLS. BENCH CHECK GO OD. 1 G 7 1 3U H2SW 1996101700484 19961017 00484 NE 1996 10 17 HEEA968044 1 19961003 A 6210 7615009100048 BLADE SKRSKY S76 S76A 8143006 NE M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31217 11736 760229 DUE AN ULTRASOUND INSPECTION FOR TIME EXTENSION. BLADE ALSO HAS A COMPLETE CHORDWISE CRACK AT STATION 47". SENT TO COMP OSITE TECHNIC FOR INSPECTION AND REPAIR. 1 G 7 2 3U H1NE 1996101700485 19961017 00485 1996 10 17 HEEA968047 4 19961003 A 2370 9806019001 CVR SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5435V 760158 USING COCKPIT TEST SWITCH, THERE IS NO SECOND SET OF TONES, NO FLASHING LIGHT AND CVR DOES NOT ILLUMINATE. SHUT DOWN LI GHT EVEN AFTER 15 MINUTES WITH NO ENGINE OIL PRESSURE TO SWITCHES. SENT TO ALLIED SIGNAL REDMOND SUPT. FOR RETURN...THEI R PROPERTY BEING RETURNED. 1 G 7 2 3U H1NE 1996101700486 19961017 00486 SW 1996 10 17 HEEA968048 1 19961003 A 7722 206375007103 INDICATOR BELL 206 206L3 1182108 SW COCKPIT TOT READS HIGH E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3107N 51512 READS HIGH THROUGHOUT SCALE & NEEDLE INTERMITTENTLY STICKS AT 100 DEGREES. 1 G 7 1 3U H2SW 1996101700487 19961017 00487 1996 10 17 HEEA968049 4 19961003 A 2370 9806019001 CVR SKRSKY S76 S76A 8143006 NE COCKPIT WONT TEST E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 22342 760096 CVR WILL NOT TEST. 1 G 7 2 3U H1NE 1996101700488 19961017 00488 1996 10 17 HEEA968050 4 19961003 A 2370 9806019001 CVR BELL 214 214ST 1182106 SW COCKPIT WONT TEST E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5748M 28102 WILL NOT TEST. SENT TO ALLIED SIGNAL AEROSPACE RED. FOR INSPECTION AND REPAIR. 2 G 7 2 4U H10SW 1996101700489 19961017 00489 EU 1996 10 17 HEEA968051 1 19961003 A 6210 10515141 BLADE BOLKMS 105 BO105S 5626006 EU M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7170D 3072 S840 BLADE IS CRACKED. (NOSE AND NECK SHELLS CRACKED) 1 G 7 2 3U H3EU 1996101700490 19961017 00490 SW 1996 10 17 HEEA968052 1 19961003 A 6410 212010750105 BLADE BELL 412 412 1182202 SW T/R DENTED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 692 BLADE IS DENTED. (FOUND .040 DENT ON LEADING EDGE. 1 G 7 2 4U H4SW 1996101700491 19961017 00491 SW 1996 10 17 HEEA968053 1 19961003 A 7722 206375007103 INDICATOR BELL 206 206L4 1182110 SW COCKPIT TOT STUCK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7077B 2175 52037 NEEDLE STUCK ON ZERO AND WOULD NOT INDICATE. TIME SINCE REPAIR 138:20. 1 G 7 1 3U NC H2SW 1996101700492 19961017 00492 EU 1996 10 17 AWXA960405 1 19960728 A 3350 321430 BATTERY AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 640AW 3881 448 PYX - FLT 2249 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT INTERMITTENT, INOPERATIVE THROUGHOUT CABIN. FO RWARD AND MID-RIGHT BATTERIES DEAD. REMOVED AND REPLACED BATTERY PACKS. OPS CHECK GOOD. REF: OPERATOR CONTROL NR 96Z ZZX5182. (X) 2 L 7 2 4F RT A28NM 1996101700493 19961017 00493 EU 1996 10 17 96ZZZX5182 1 19960728 A 3350 321430 BATTERY AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 640AW 4410 448 PYX - FLT 2249 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT INTERMITTENT, INOPERATIVE THROUGHOUT CABIN. FO RWARD AND MID-RIGHT BATTERIES DEAD. REMOVED AND REPLACED BATTERY PACKS. OPS CHECK GOOD. REF: OPERATOR CONTROL NR AWX A960405. 2 L 7 2 4F RT A28NM 1996101700494 19961017 00494 NM 1996 10 17 AWXA960498 1 19960714 A 3350 831862 BATTERY PACK BOEING 737 737275 1384485 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 CGPW 0181 20958 PHX - FLT 2455 - DURING ROUTINE MAINTENANCE CHECK, FOUND FORWARD FUSELAGE EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. OPERATIONS CHECK OK. (X) 2 L 7 2 4F A16WE 1996101700495 19961017 00495 NM 1996 10 17 W8PA960126 1 19960825 A 5313 BAC1498159 STRINGER BOEING 737 737301 1384611 NM BS 1010 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 950WP 23229 CORROSION IN STR 26R, BS 1010, WL 186 IN AFT EQUIPMENT. FABRICATED AND INSTALLED STRINGER. (X) 2 L 7 2 4F RT A16WE 1996101700496 19961017 00496 NM 1996 10 17 W8PA960127 1 19960826 A 5313 STRINGER BOEING 737 737301 1384611 NM BS 994-1016 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 950WP 23229 CORROSION ON STR 27L, BS 1010, WL 186. REMOVED AND REPLACED STRINGER FROM BS 995 TO BS 1016 PER SRM 53-00-03. (X) 2 L 7 2 4F RT A16WE 1996101700497 19961017 00497 NM 1996 10 17 W8PA960128 1 19960828 A 5311 FRAME BOEING 737 737301 1384611 NM BS 1006 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 950WP 23229 CORROSION ON FRAME BS 1006, BL ZERO, WL 188, IN AFT EQUIPMENT BAY. CUT OUT DAMAGE, REPAIRED FRAME PER SRM 53-00-07. RE PAIRED AREA IAW SRM 53-00-07. (X) 2 L 7 2 4F RT A16WE 1996101700498 19961017 00498 NM 1996 10 17 96ZZZX5183 1 19960812 A 2530 5852 OVEN BOEING 747 747143 1384901 NM GALLEY SMOKING A TWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 128TW 19729 JFK - FLT 925 - DURING CRUISE, AUXILIARY BAR OVEN EMITTED SMOKE AND BURNING ODOR. TURNED OFF OVEN. FOUND OVEN, MFG PN 5852, DEFECTIVE. REPLACED AUXILIARY BAR OVEN. OPERATION THEN CHECKED NORMAL. CHECK C-2 - 7-12-96 - JFK. 2 L 7 4 4F A20WE 1996101700499 19961017 00499 WP 1996 10 17 AALA961241 1 19960820 A 3240 26088921 BRAKE ASSY DOUG DC9 DC982 3022082 WP NR 2 TIRE DEFECTIVE A AALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 07 584AA 53247 LAX - FLT 0084 - DURING TAXIING, BRAKES WERE BINDING, DURING TAXI BACK TO GATE NR 2, TIRE FUSE PLUGS BLEW OUT. DEPLANED PASSENGERS AND TOWED AIRCRAFT TO HANGAR. REPLACED BRAKE ASSEMBLY AND WHEEL ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPE RATION. (X) 2 L 7 2 4F A6WE 1996101700500 19961017 00500 NM 1996 10 17 AALA961238 1 19960820 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 668AA 25333 DFW - DURING OVERNIGHT CHECK, FOUND THE FORWARD COACH SECTION EMERGENCY EXIT FLOOR PATH EXIT PLACARD LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1996101700501 19961017 00501 NM 1996 10 17 AALA961158 1 19960804 A 3320 05939109 BALLAST BRUCE BOEING 757 757223 1384957 NM CABIN OVERHEAD OVERHEATED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 699AN 27051 MSY - FLT 1894 - EN ROUTE DFW/SJU DURING CRUISE, SMOKE NOTED IN CABIN BY L1 DOOR. AIRCRAFT DIVERTED TO MSY AND LANDED O VERWEIGHT WITHOUT INCIDENT. REMOVED FORWARD ENTRYWAY CEILING PANELS AND CHECKED LIGHT BALLASTS. PLACARDED TWO FLUORESCE NT LIGHTS IN FORWARD ENTRY OVERHEAD DUE TO TWO BALLASTS (M10381 AND M10382) FOUND HOT, BUT NOT SMOKING. ACCOMPLISHED OV ERWEIGHT LANDING INSPECTION WITH NO DEFECTS FOUND. SUBSEQUENTLY AT DFW/06, FORWARD ENTRY OVERHEAD BALLASTS REPLACED. S YSTEM GROUND CHECKED, NORMAL OPERATION WITH NO SMOKE OR ODOR NOTED. REMOVED PLACARD FOR FORWARD ENTRY OVERHEAD LIGHTS. (X) 2 L 7 2 4F RT A2NM 1996101700502 19961017 00502 SO 1996 10 17 96ZZZX5185 1 19960627 A 3250 AN3H7A BOLT 4531400 PIPER PA31 PA31350 7103110 SO NLG SHEARED A A JIBA K NONE O OTHER LD LANDING 1 NE 03 400RA 317450167 PILOT EXTENDED LANDING GEAR. UPON CHECKING NOSE GEAR IN MIRROR LOCATED ON LEFT ENGINE COWLING, OBSERVED NOSE WHEEL TIRE WAS NOT CENTERED. IT APPEARED TO BE TURNED APPROXIMATELY 20 DEGREES. AIRCRAFT LANDED WITHOUT INCIDENT. UPON INSPECTI ON, FOUND TWO OF THE THREE AN3H-7A BOLTS, WHICH ATTACH STEERING ARM ASSY PIPER PN 44386-00, TO THE NOSE GEAR STRUT HAD B EEN SHEARED ALLOWING NOSE WHEEL TO TURN FREELY TO ITS TURN LIMITS, UNABLE TO BE CONTROLLED BY NORMAL MEANS. 1 L 7 2 3O A20SO 1996101700503 19961017 00503 NM 1996 10 17 W8PA960135 1 19960823 A 5753 SKIN BOEING 737 737301 1384611 NM RT FORE FLAP DENTED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 950WP 23229 RIGHT WING OUTBOARD FORE FLAP HAS A CREASED DELAMINATED DENT; MIDSPAR, UPPER SURFACE. REMOVED DAMAGED AREA, FABRICATED CORE REPLACEMENT, APPLIED, CURED, AND TREATED PER SRM 51-70-10, SRM 51-40-00. (X) 2 L 7 2 4F RT A16WE 1996101700504 19961017 00504 1996 10 17 C2XA96CL030 4 19960908 A 3418 1143800515 COMPUTER BEECH 1900 1900D 1154162 CE AVIONICS BAY FAULTED A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 81535 282 UE147 RIC - FLT 3053 - CREW REPORTED THE STALL WARNING SOUNDED AFTER ROTATION WITH THE LANDING GEAR DOWN AND FLAPS AT 17 DEGRE ES, WARNING CONTINUED TO SOUND AFTER LANDING GEAR AND FLAPS WERE RETRACTED. AIRCRAFT RETURNED TO FIELD. MAINTENANCE IN SPECTED AIRCRAFT AND REMOVED AND REPLACED THE STALL WARNING COMPUTER, CALIBRATION, AND OPERATIONAL CHECKS WERE GOOD. AL L WORK ACCOMPLISHED IAW B1900D MM 27-31-00, AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1996101700514 19961017 00514 WP 1996 10 17 96ZZZX5195 1 19960808 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9407R 49400 STL - DURING SPECIAL CHECK, FOUND A FOUR INCH HOLE, RIGHT SIDE OF FUSELAGE, BELOW AND AFT OF R1 DOOR. REPAIRED PER SRM 53-02, FIGURE 2, AND SRM 53-04, FIGURE 12. AIRCRAFT TOTAL TIME: 23,197 HOURS; 12,153 CYCLES. 2 L 7 2 4F RT A6WE 1996101700515 19961017 00515 WP 1996 10 17 96ZZZX5196 1 19960603 A 5720 9911603 TEE CAP DOUG DC9 DC932 3022066 WP WS 58 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 920VV 47262 DURING ACCOMPLISHMENT OF AD 90-18-03, REF DC-9 SB 57-98, REV 8, FOLLOWING DISCREPANCIES: RT WING LOWER TEE CAP AT STA X CW 58.00 BETWEEN STR'S 11-17, EXFOLIATION CORROSION EXISTS. REMOVED CORROSION BTWN STR'S 11-12, .100 INCH MATL LOSS; ST R'S 12-13, .067 INCH MATL LOSS; STR'S 13-14, .099 INCH MATL LOSS; STR'S 15-16, .060 INCH MATL LOSS; STR'S 16-17, .160 IN CH MATL LOSS. INSP LT WING LOWER TEE CAP AT XCW 58.00 BTWN STR'S 11-17. EXFOLIATION CORROSION ALSO EXISTS. REMD CORRO SION BTWN STR'S 11-12, .050 INCH MATL LOSS; STR'S 13-14, .050 MATL LOSS; STR'S 15-16, .012 MATL LOSS. CORROSION NOTED I N BARREL NUT HOLES AT STR'S 11-17, LT AND STR'S 18-23, LT. ACFT TT: 69,772.10 HRS. ACFT CYCLES, 82,067. 2 L 7 2 4F A6WE 1996101700516 19961017 00516 WP 1996 10 17 96ZZZX5197 1 19960603 A 5720 5910006 TEE CAP DOUG DC9 DC932 3022066 WP WS 58 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 920VV 47262 DURING ACCOMPLISHMENT OF AD 90-18-03, REF DC-9, SB 57-98, REV 8, FOLLOWING DISCREPANCIES: RT WING LOWER TEE CAP AT STA XCW 58.00 BTWN STR'S 11-17 EXFOLIATON CORROSION EXISTS. REMD CORROSION BTWN STR'S 11-12, .100 INCH MATERIAL LOSS; STR'S 12-13, .067 MATL LOSS; STR'S 13-14, .099 INCH MATL LOSS; STR'S 15-16, .060 INCH MATL LOSS; STR'S 16-17, .160 INCH MATL LOSS. INSP LT WING LOWER TEE CAP AT XCW 58.00 BTWN STR'S 11-17. EXFOLIATION CORROSION ALSO EXISTS. REMD CORROSION BTW N STR'S 11-12, .050 INCH MATL LOSS; STR'S 13-14, .050 INCH MATL LOSS; STR'S 15-16, .012 INCH MATL LOSS. CORROSION ALSO NOTED IN BARREL NUT HOLES AT STR'S 11-17, LT AND STR'S 18-23, LT. ACFT TT: 69,772.10 HRS. ACFT CYCLES, 82,067. 2 L 7 2 4F A6WE 1996101700517 19961017 00517 1996 10 17 C2XA96IA223 3 19960828 A 6112 4E30171 DEICE BOOT BEECH 1900 1900D 1154162 CE NR 1 PROP DEBONDED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 82539 UE168 TYL - FLT 9447 - PILOT REPORTED DURING A POST-FLIGHT WALKAROUND INSPECTION, FOUND LT PROPELLER HAD ONE DEICE BOOT DEBOND ED FROM BLADE. THE DEICE BOOT REMOVED AND ACFT FERRIED TO IAH WHERE MAINTENANCE INSTALLED A DEICE BOOT ON PROPELLER. A CFT WAS THEN APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1996101700518 19961017 00518 CE 1996 10 17 96ZZZX5198 1 19960903 A 2750 BZ7RW82255518T LIMIT SWITCH BEECH 1900 1900D 1154162 CE RT TE FLAP OUT OF ADJUST A C2XA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 09 87550 UE205 AZO - FLT 3018 - CREW REPORTED AFTER TAKEOFF, FLAPS WOULD NOT RETRACT. ACFT RETURNED TO AZO, FLAPS RETRACTED TO ZERO AF TER LANDING. MAINTENANCE INSPECTED ACFT AND RELEASED IT IAW MEL 27-2 CONTROL NR 895224. AFTER ACFT RETURNED TO A MAINT ENANCE BASE (CLE) THE RT FLAP SPLIT LIMIT SWITCH WAS ADJUSTED IAW B1900D, MM 27-50-05. OPERATIONAL CHECKS WERE GOOD IAW B1900D, MM 27-50-00, ACFT WAS REMOVED FROM MEL AND RELEASED FOR SERVICE. (X) 2 L 7 2 4T RT A24CE 1996101700519 19961017 00519 EA 1996 10 17 96ZZZX5199 2 19960720 A 7250 GAS GENERATOR BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA RT ENGINE FAILED A MASA E A ENGINE SHUTDOWN UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 SW 01 156YV 11652 5049 UC156 32460 ON CLIMB-OUT, RT ENGINE TORQUE SPIKED UP AND DROPPED TO ZERO. RT PROP AUTOFEATHERED AND ENGINE FROZE. ACFT RETURNED TO FARMINGTON AND LANDED WITHOUT INCIDENT. PART TOTAL CYCLES, 17,661. 2 L 7 2 4T 4 T RT A24CE E4EA 1996101700520 19961017 00520 EA 1996 10 17 96ZZZX5200 2 19960720 A 7250 POWER SECTION BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA RT ENGINE FAILED A MASA E A ENGINE SHUTDOWN UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 SW 01 156YV 10207 2268 UC156 32551 ON CLIMB-OUT, RT ENGINE TORQUE SPIKED UP AND THEN DROPPED TO ZERO. THE RT PROP AUTOFEATHERED AND ENGINE FROZE. ACFT RE TURNED TO FARMINGTON AND LANDED WITHOUT INCIDENT. PART TOTAL CYCLES, 15,450. 2 L 7 2 4T 4 T RT A24CE E4EA 1996101700521 19961017 00521 NM 1996 10 17 96ZZZX5201 1 19960830 A 3411 10607023 PITOT TUBE BOEING 727 7272J7 138400E NM LEFT BLOCKED A C8GA C D ABORTED TAKEOFF RETURN TO BLOCK C F.O.D. TO TAKEOFF 1 SO 15 128NA 20879 MIAMI - ON TAKEOFF ROLL, THERE WAS NO AIRSPEED INDICATION ON THE CAPTAIN'S AIRSPEED INDICATOR. DISCONNECTED PITOT PRESS URE LINE, APPLIED NITROGEN PRESSURE AND FOUND INSECTS (BEES) CLOGGING CAPTAIN'S PITOT TUBE. CLEARED AL INSECTS FROM CAP TAIN'S PITOT LINES, RECONNECTED LINE, OPERATION AND LEAKED CHECKED PITOT SYSTEM IAW B727 MM, REF 34-11-0. ACFT RELEASED FOR FLIGHT. 2 L 7 3 4F A3WE 1996101700522 19961017 00522 EU 1996 10 17 MALA965103 1 19960825 A 2421 31342001 GENERATOR SAAB SF340 SF340A 7850100 EU RT ENGINE FAILED A MALA K NONE J WARNING INDICATION CR CRUISE 1 GL 15 99XJ 340A099 DTW - FLT 3415 - EN ROUTE TO DFW, RT AC GENERATOR FAIL LIGHT ILLUMINATED. CREW ATTEMPTED TO RESET GENERATOR, BUT IT REM AINED INOPERATIVE. THE ACFT LANDED IN DTW WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED AC GENERATOR. ALL CHECKS GOO D. (X) 2 L 7 2 4T RT A52EU 1996101700523 19961017 00523 SW 1996 10 17 96ZZZX5202 1 19960518 A 2910 6790246215 HOSE GULSTM 680 680FL 0141608 SW HYD PRESSURE SEPARATED A HSYA O OTHER J K WARNING INDICATION FLUID LOSS CR CRUISE 1 NM 05 6344U 143072 BIL - FLT 5011 - HYDRAULIC SYSTEM FAILURE DURING CRUISE FLIGHT FROM WOLF POINT TO BILLINGS. HYDRAULIC PUMP PRESSURE HOS E SEPARATED AT HOSE AND FITTING ON LEFT ENGINE. REMOVED AND REPLACED HOSE. ENGINE RUN AND LEAK CHECK COMPLETED WITH NO FURTHER DEFECTS NOTED. (X) 1 H 7 2 3O 2A4 1996101700524 19961017 00524 CE 1996 10 17 96ZZZX5203 1 19960601 A 3260 MS250413 LIGHT BEECH 200 200BEECH 1152920 CE NLG DOWNLOCK LOOSE A HSYA O OTHER P NO WARNING INDICATION AP APPROACH 1 NM 05 4298S BB198 BIL - WHEN LANDING GEAR WAS EXTENDED FOR LANDING IN BILLINGS, THE NOSE GEAR DOWN AND LOCK LIGHT DID NOT COME ON. THE RE D GEAR UNSAFE LIGHT IN THE LANDING GEAR HANDLE DID GO OUT. THE GEAR WAS CYCLED, EXTENDED MANUALLY. THE NOSE GEAR COULD BE SEEN IN THE EXTENDED POSITION FROM THE CHROME EXHAUST STACK. NOSE GEAR DOWNAND LOCKED LIGHT WAS NOT SCREWED IN ALL THE WAY. PUSH-TO-TEST WORKED, BUT NOT THE NORMAL FUNCTION. TIGHTENED BULB HOLDER AND SWUNG GEAR FOR OPS CHECK. SYSTEM OPERATED CORRECTLY. 1 L 7 2 4T A24CE 1996101700525 19961017 00525 CE 1996 10 17 96ZZZX5204 1 19960703 A 3244 185884 TIRE BEECH 99 99A 1154003 CE LT MLG RECAP FAILED A HSYA O OTHER J WARNING INDICATION AP APPROACH 1 NM 05 199CA 55 4256176 U96 DEN - FLT 1825 - NO GEAR DOWN AND LOCKED INDICATION ON LT MLG ON DESCENT INTO DEN. PILOT PERFORMED TOWER FLYBY AND COMP LETED EMERGENCY GEAR EXTENSION PROCEDURES. ACFT LANDED WITHOUT FURTHER INCIDENT. ENGINES WERE SHUT DOWN AND PROPS WERE FEATHERED UPON LANDING AS PRECAUTIONARY MEASURE. NR 1 TIRE (LT OTBD) RECAP TREAD CAME OFF DURING TAKEOFF. THIS SEPARA TED THE CANNON PLUG ON THE LOWER MLG DRAG LEG FOR THE DOWNLOCK SWITCH. TIRE MISSING TREAD. STILL HOLDING AIR, WAS DEFL ATED BEFORE REMOVAL. REMOVED AND REPLACED NR 1 WHEEL ASSY, REPAIRED BROKEN CANNON PLUG AND INSPECTED AREA FOR FURTHER D AMAGE. NONE WAS NOTED. GEAR SWING PERFORMED WITH NO FURTHER DEFECTS NOTED. 1 L 7 2 3T A14CE 1996101700526 19961017 00526 1996 10 17 ASOA96039 4 19960918 A 3197 W110157924 WIRE EMB 120 EMB120RT 3260202 SO CABIN BROKEN A ASOA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 11 236AS 120049 TXK/DFW - FLT 7998 - EN ROUTE, LEFT ENGINE DUCT LEAK LIGHT ILLUMINATED. THE CREW SHUT DOWN LEFT ENGINE AS PRECAUTIONARY MEASURE AND DECLARED AN EMERGENCY. LANDING WAS MADE SAFELY AND WITHOUT INCIDENT IN DFW. REPAIRED BROKEN WIRES UNDER F LOOR AT ROW 5. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT RELEASED FOR FURTHER SERVICE. (X) 2 L 7 2 4T RT A31SO 1996101700527 19961017 00527 NM 1996 10 17 CALA9601458 1 19960922 A 5210 WEB BOEING 727 727232 1384082 NM FWD ENT DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 AT FORWARD ENTRY DOOR AFT END OF UPPER FRAME WEB HAS 4 INCH CRACK RUNNING FROM UPPER STOP FITTING. CUT OUT CRACKED AREA , FABRICATED AND INSTALLED REPAIR PER S/B 727-52-115. 2 L 7 3 4F A3WE 1996101700528 19961017 00528 NM 1996 10 17 CALA9601459 1 19961005 A 5210 FITTING BOEING 727 727232 1384082 NM L1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 L 1 DOOR TOP AFT DOOR STOP FITTING CRACKED. REMOVED AND REPLACED STOP FITTING PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996101700529 19961017 00529 NM 1996 10 17 CALA9601460 1 19960922 A 5751 WEB BOEING 727 727232 1384082 NM LT AILERON GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 LEFT HAND OUTBOARD AILERON INBOARD HINGE AT WING TRAILING EDGE HAS WEB BADLY GOUGED AT OUTBOARD SIDE OF HINGE FITTING. G OUGE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 57-10-4. 2 L 7 3 4F A3WE 1996101700530 19961017 00530 NM 1996 10 17 CALA9601461 1 19960922 A 5751 WEB BOEING 727 727232 1384082 NM LT AILERON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 LEFT HAND OUTBOARD AILERON NR 3 AILERON HINGE FITTING AT WING TRAILING EDGE HAS OUTBOARD WEB CRACKED. FABRICATED AND IN STALLED DOUBLER PER SRM 51-40-2. 2 L 7 3 4F A3WE 1996101700531 19961017 00531 NM 1996 10 17 CALA9601462 1 19960917 A 5755 651734866 PANEL BOEING 727 727232 1384082 NM RT SPOILER DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 SPOILER PANEL FOUND DELAMINATED. REPAIRED PANEL PER SRM 51-40-6. 2 L 7 3 4F A3WE 1996101700532 19961017 00532 NM 1996 10 17 CALA9601463 1 19960917 A 5752 652172633 TAB BOEING 727 727232 1384082 NM LT AILERON DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 LEFT OUTBOARD AILERON TAB UPPER SURFACE HAS A SMALL AREA OF DELAMINATION AND SEVERAL DENTS. PERFORMED HOT BOND REPAIR P ER SRM 51-40-6. 2 L 7 3 4F A3WE 1996101700533 19961017 00533 NM 1996 10 17 CALA9601464 1 19960917 A 5755 651734866 PANEL BOEING 727 727232 1384082 NM NR 6 SPOILER DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 NUMBER 6 SPOILER UPPER SURFACE DELAMINATED. REPAIRED SPOILER PANEL PER SRM 51-40-6. 2 L 7 3 4F A3WE 1996101700534 19961017 00534 WP 1996 10 17 CALA9601465 1 19961003 A 5330 5074802609 SKIN DOUG DC9 DC981 3022081 WP BS 256-275 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14871 48022 LEFT SIDE SKIN DENTED 256 TO 275 LONG 16 TO 18 DENTED SEVERAL TIMES. FABRICATED AND INSTALLED NEW SKIN DOUBLER PER EC/R A 5330-02445. 2 L 7 2 4F A6WE 1996101700535 19961017 00535 WP 1996 10 17 CALA9601466 1 19960927 A 5320 49128232 INTERCOSTAL DOUG DC9 DC981 3022081 WP SERV DR CUTOUT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14871 48022 LOWER AFT CORNER OF FORWARD SERVICE DOOR FRAME INTERCOSTAL HAS CORROSION. INSTALLED NEW FITTING PER SRM 51-30-05. 2 L 7 2 4F A6WE 1996101700536 19961017 00536 WP 1996 10 17 CALA9601467 1 19960926 A 5320 59101419 DOOR PAN DOUG DC9 DC981 3022081 WP CARGO DR CUTOUT TORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14871 48022 AFT CARGO DOOR AFT SIDE CUTOUT AROUND LOCKING CAM BENT, TORN AND SEPARATED. INSTALLED DOUBLER PER SRM 52-05 FIG 26A. 2 L 7 2 4F A6WE 1996101700537 19961017 00537 WP 1996 10 17 CALA9601468 1 19961013 A 3397 L3003A20 WIRE DOUG DC9 DC981 3022081 WP BS 1083-1205 BURNED A A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16883 48073 TWENTY-FOUR LIGHTING WIRES FOUND WITH BURNT SHIELDING ON RIGHT SIDE OF AIRCRAFT BETWEEN STATION 1083 AND 1205. REMOVED AND REPLACED BURNT WIRE BUNDLE AND REPLACED WIRES FROM CONNECTOR TO CONNECTOR WITH NO SPLICES PER MM 3300. REFERENCE MC DONNELL DOUGLAS AD 96-11-13. 2 L 7 2 4F A6WE 1996101700538 19961017 00538 1996 10 17 CALA9601469 4 19961015 A 2565 113317 SLIDE DOUG DC9 DC982 3022082 WP R1 DOOR TORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35888 7572 49117 SLIDE ON FORWARD GALLEY TORN AT GIRT BAR. REMOVED AND REPLACED SLIDE PER MAINTENANCE MANUAL. 2 L 7 2 4F A6WE 1996101700539 19961017 00539 WP 1996 10 17 9621909178 1 19960921 A 5330 SKIN DOUG DC9 DC914 3022034 WP BS 167 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3310L 45705 DURING H-CHECK, FOUND A .5 INCH CRACK IN THE FUSELAGE SKIN AT FS 167 LONGERON 4L. REPAIRED SKIN (P/N 5911406-5) PER EA 91-111714. 2 L 7 2 4F A6WE 1996101700540 19961017 00540 WP 1996 10 17 9621919908 1 19960928 A 5741 FITTING DOUG DC9 DC931 3022065 WP BS 609 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 958N 47254 DURING H-CHECK, FOUND A CRACK IN THE WING TO FUSELAGE ATTACH FITTING, FS 609 BETWEEN LONGERONS 22R TO 23R. REPAIRED FIT TING (P/N 5910006-44) PER EA 99-111296. 2 L 7 2 4F A6WE 1996101700541 19961017 00541 NM 1996 10 17 9621926310 1 19961002 A 5320 INTERCOSTAL BOEING 747 747451 1384940 NM BS 1627-1670 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 670US 24225 DURING PERIODIC CHECK, FOUND CORROSION ON THE LBL 42 INTERCOSTAL FLANGE BETWEEN BS 1627 TO 1670. REPAIRED INTERCOSTAL P ER EA 63-110092. 2 L 7 4 4F RT A20WE 1996101700542 19961017 00542 NM 1996 10 17 9621936310 1 19961002 A 5320 INTERCOSTAL BOEING 747 747451 1384940 NM BS 820-921 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 670US 24225 DURING P-CHECK, FOUND CORROSION IN THE LBL 42 INTERCOSTAL BETWEEN BS 820 TO 921. REPAIRED INTERCOSTAL PER EA 63-106408. 2 L 7 4 4F RT A20WE 1996101700543 19961017 00543 NM 1996 10 17 9621946310 1 19961003 A 5315 FLOOR BEAM BOEING 747 747451 1384940 NM BS 520 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 670US 24225 DURING P-CHECK, FOUND CORROSION ON THE BS 520 MAIN DECK FLOOR BEAM UPPER CHORD FROM RBL 46 TO 64. REPAIRED CHORD PER EA 63-110096. 2 L 7 4 4F RT A20WE 1996101700544 19961017 00544 NM 1996 10 17 9621956310 1 19961003 A 5315 FLOOR BEAM BOEING 747 747451 1384940 NM BS 480 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 670US 24225 DURING P-CHECK, FOUND CORROSION ON THE BS 480 MAIN DECK FLOOR BEAM UPPER CHORD AT RBL 64. REPAIRED CHORD PER EA 63-1064 24. 2 L 7 4 4F RT A20WE 1996101700545 19961017 00545 NM 1996 10 17 9621966310 1 19961003 A 5320 INTERCOSTAL BOEING 747 747451 1384940 NM BS 817-863 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 670US 24225 DURING P-CHECK, FOUND CORROSION ON THE RBL 42 INTERCOSTAL BETWEEN FS 817 TO 863. REPAIRED INTERCOSTAL PER EA 63-110093. 2 L 7 4 4F RT A20WE 1996101700546 19961017 00546 NM 1996 10 17 9621972706 1 19961004 A 5240 FRAME BOEING 727 727225 1384077 NM SERVICE DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 815EA 22552 DURING L-CHECK, FOUND A CRACK IN THE LEFT AFT SERVICE DOOR UPPER FORWARD HINGE CUTOUT. REPAIRED FRAME (P/N 65-56992-3) PER EA 27-110323. 2 L 7 3 4F A3WE 1996101700547 19961017 00547 WP 1996 10 17 9621989614 1 19961011 A 5210 FITTING DOUG DC9 DC932 3022066 WP SERVICE DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 614NW 47128 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE AFT ENTRY DOOR FRAME FITTING, LEFT AFT SIDE. REPLACE D FITTING PER SRM 51-10-3. 2 L 7 2 4F A6WE 1996101700548 19961017 00548 WP 1996 10 17 9621999960 1 19961013 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 604 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 920RW 47163 DURING H-CHECK, FOUND CORROSION IN THE LONGERON 30 LEFT KEEL END FITTING AT FS 604. REPLACED FITTING PER SRM 51-10-3. 2 L 7 2 4F A6WE 1996101700549 19961017 00549 WP 1996 10 17 9622009960 1 19961013 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 691 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 920RW 47163 DURING H-CHECK, FOUND CORROSION IN THE RIGHT KEEL 'T' FITTING AT FS 691. REPLACED 'T' FITTING PER SRM 51-10-3. 2 L 7 2 4F A6WE 1996101700550 19961017 00550 WP 1996 10 17 9622019960 1 19961013 A 5320 FITTING DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 920RW 47163 DURING H-CHECK, FOUND CORROSION IN THE LONGERON 29.5R END FITTING. REPLACED FITTING PER SRM 51-10-3. 2 L 7 2 4F A6WE 1996101700551 19961017 00551 WP 1996 10 17 9622029618 1 19961014 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 990-996 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 618NW 47433 DURING M-CHECK, FOUND CORROSION ON THE LONGERON 23L AND LONGERON 30 TIE FITTINGS AT FS 990 TO 996. REPLACED TIE FITTING S PER SRM 51-10-03. 2 L 7 2 4F A6WE 1996101700552 19961017 00552 WP 1996 10 17 9622039960 1 19961014 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 756 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 920RW 47163 DURING H-CHECK, FOUND CORROSION ON THE FS 756 KEEL FITTING AT LONGERON 30, LEFT SIDE. REPLACED FITTING PER SRM 51-30-5 . 2 L 7 2 4F A6WE 1996101700553 19961017 00553 NM 1996 10 17 9621826307 1 19961012 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 667US 24222 DURING LINE CHECK, FOUND FIRST CLASS LEFT EMERGENCY FLOOR LIGHTS INOPERATIVE. RECONNECTED WIRES, OPERATIONAL CHECK OK. 2 L 7 4 4F RT A20WE 1996101700554 19961017 00554 NM 1996 10 17 9621836637 1 19961012 A 3610 60B901241 COUPLING BOEING 747 747251B 1384892 NM NR 1 ENGINE CRACKED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 GL 01 637US 23548 DURING TAKEOFF AND CLIMB, THE NR 1 ENGINE EPR AND N1 DROPPED AND THE FIRE LIGHT ILLUMINATED. SHUT DOWN NR 1 ENGINE AND RETURNED TO DTW. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. REPLACED THE 15TH STAGE COUPLING, HIGH STAGE VALVE, TWO DUC TS FORWARD OF HIGH PRESSURE VALVE, AND CLAMPS CONNECTING HIGH STAGE VALVE. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996101700555 19961017 00555 NM 1996 10 17 9621846608 1 19961012 A 3610 PNEUMATIC SYST BOEING 747 747151 1384891 NM RT WING MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 608US 19785 DURING CLIMB, THE RIGHT WING OVERHEAT LIGHT ILLUMINATED. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND LIGHT REMAINE D ILLUMINATED. AIRCRAFT RETURNED TO NRT AND LANDED WITHOUT INCIDENT. REPLACED NR 4 PYLON VALVE, NACELLE ANTI-ICE VALVE CLAMP, LEADING EDGE FLAP DRIVE UNIT AIR INLET DUCT SEAL AND ISOLATION VALVE, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996101700556 19961017 00556 NM 1996 10 17 9621856608 1 19961012 A 2613 OVERHEAT SWITCH BOEING 747 747151 1384891 NM NR 4 ENGINE MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 608US 19785 DURING CLIMB, THE RIGHT WING OVERHEAT LIGHT ILLUMINATED. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND LIGHT REMAINE D ILLUMINATED. AIRCRAFT RETURNED TO NRT AND LANDED WITHOUT INCIDENT. REPLACED THE NR 3 ENGINE PYLON AFT OVERHEAT SWITC H TERMINAL AND REPAIRED TWO WIRES ON OVERHEAT LIGHT INDICATOR IN NR 4 ENGINE STRUT, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996101700557 19961017 00557 WP 1996 10 17 9621869305 1 19961013 A 3620 GASKET DOUG DC9 DC982 3022082 WP RT TEMP SENSOR FAILED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 307RC 48086 DURING CLIMB, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. FOLLOWED COM PROCEDURES AND LIGHT WENT OUT. RETURNE D TO ONT AND LANDED WITHOUT INCIDENT. REPLACED GASKET IN RIGHT SIDE PNEUMATIC SUPPLY TEMPERATURE SENSOR. RAN BOTH ENGI NES TO TAKEOFF POWER, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996101700558 19961017 00558 NE 1996 10 17 9621876310 2 19961013 A 7200 ENGINE BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE NR 4 FAILED A A NWAA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 GL 01 670US 24225 717668 ENROUTE, THE NBR 4 ENGINE EXPERIENCED OIL LOSS AND FLUCTUATING OIL PRESSURE. THE ENGINE WAS SHUT DOWN AND THE FLIGHT CO NTINUED TO DTW WITHOUT FURTHER INCIDENT. VISUAL INSPECTION REVEALED OIL IN NR 4 ENGINE TAILPIPE. THE ENGINE WAS REPLAC ED AND CHECK WAS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 1996101700559 19961017 00559 1996 10 17 9621889960 4 19961014 A 2565 113317 SLIDE BATTERY DOUG DC9 DC931 3022065 WP MAIN CABIN DOOR DISCHARGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 920RW 25953 4412 47163 DURING PERIODIC CHECK, FORWARD ENTRANCE DOOR EVACUATION SLIDE FAILED BATTERY TEST. REPLACED SLIDE. 2 L 7 2 4F A6WE 1996101700560 19961017 00560 WP 1996 10 17 9621899925 1 19961014 A 3350 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 925US 47472 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS AT MAIN CABIN DOOR AND FLOOR PROXIMITY LIGHTS AT RIGHT GALLEY ACROSS FROM LAVATORY INOPERATIVE. REPLACED POWER SUPPLY AND BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996101700561 19961017 00561 EU 1996 10 17 9622043218 1 19961014 A 3150 SKIN VALVE IND AIRBUS 320 A320211 3930320 EU COCKPIT MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 318US 206 DURING TAKEOFF ROLL, RECEIVED VENT SKIN VALVE FAULT. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GATE. MAINTENANC E TROUBLESHOOTING REVEALED NO DISCREPANCIES. 2 L 7 2 4F RT A28NM 1996101700562 19961017 00562 EU 1996 10 17 9622053218 1 19961014 A 2120 B7292325V04 COMPUTER AIRBUS 320 A320211 3930320 EU AVIONICS BAY MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 318US 16831 12141 206 AFTER RECEIVING VENT SKIN VALVE FAULT DURING A PREVIOUS TAKEOFF ATTEMPT, RECEIVED THE SAME MESSAGE. TAKEOFF WAS AGAIN A BORTED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE PLACED THE EXTRACT VALVE ON MEL. THE AVIONICS EQUIPMENT VENTIL ATION COMPUTER WAS LATER REPLACED, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996101700563 19961017 00563 EA 1996 10 17 COMA9660168 1 19961012 A 3350 CONNECTION CNDAIR CL600 CL6002B19 EA CABIN LOOSE A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 949CA 7080 THE FORWARD FLOOR PATH EMERGENCY LIGHTING IS INOP. REPAIRED LOOSE WIRING CONNECTION, FLOOR PATH LIGHTING OPERATES NORMA L. 2 L 7 2 4F RT A21EA 1996101700564 19961017 00564 NM 1996 10 17 96FDEA01577 1 19961014 A 5400 6558885 S-DUCT SKIN BOEING 727 72725 1384006 NM BS 1201 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 511FE 18283 NR0496 AND 019, CORROSION (C54-451-02) ON INTERIOR SKIN OF S-DUCT AT BS 1201 AT CENTER LINE, MIDDLE OF S-DUCT. *S/D* R EMOVED DAMAGED SKIN OF INTERIOR OF S-DUCT AT BS 1201. INSTALLED REPAIR DOUBLER IAW FEDEX 727 SRM 54-10-03. 2 L 7 3 4F A3WE 1996101700565 19961017 00565 NM 1996 10 17 96FDEA01576 1 19961015 A 2121 215201 GASPER FAN BOEING 727 7272S2F 1384O81 NM COCKPIT FAILED A FDEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 25 216FE 22937 CREW HAD AIR RETURN DUE SMOKE IN COCKPIT, ODOR POSSIBLY OIL/HYD CMA SMOKE AND FUMES. T/S A/C SYSTEM FOUND CONDENSOR/WA TER SEPARATOR BAGS BLACK COLOR WITH BAD SMELL. GASPER FAN HAD OIL ON BLADES WITH BAD SMELL. REMOVED AND REPLACED CONDE NSOR/WATER SEPARATOR BAGS PER MM 21-23-51. REMOVED AND REPLACED GASPER FAN PER MM 21-23-11, OPS CHK NORMAL. RAN APU OP ERATED LT AND RT PACKS, OPENED ALL GASPER AIR VENTS IN COCKPIT, NO SMOKE OR FUMES. RAN ENGINES OPERATED LT AND RT PACKS , ALL GASPER AIR VENTS OPEN IN COCKPIT NO SMOKE OR FUMES. 2 L 7 3 4F A3WE 1996101700566 19961017 00566 NM 1996 10 17 96FDEA01399 1 19960823 A 5315 6520827 FLOOR BEAM BOEING 727 72725 1384006 NM BS 560 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 509FE 18280 NR0456, CORROSION (C53-224-01) ON FLOOR BEAM STR 560 RBL 21 WL 208 GLAND NUTPLATE HOLE. *S/D* REMOVED CORROSION ON UPP ER CORD, FABRICATED REPAIR ANGLES AND FILLER. INSTALLED REPAIR PER FEDEX SRM-53-10-8 FIG 8 AND 53-10-1 FIG 4. 2 L 7 3 4F A3WE 1996101700567 19961017 00567 NM 1996 10 17 96FDEA01462 1 19960910 A 5320 651862226 BEAR STRAP BOEING 727 72725 1384006 NM BS 1105 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR 0499 AND 020, CORROSION (C53-111-01, -3) ON BEAR STRAP AT BS 1105 RBL 28 WL 151. *S/D* REPAIRED BEAR STRAP PER FEDE X EA 7-5310-31169. 2 L 7 3 4F A3WE 1996101700568 19961017 00568 NE 1996 10 17 ABXA9600647 2 19961011 A 7261 769792 OIL PUMP DOUG DC8 DC861 3021952 WP PWA JT3D JT3D3B 52039 NE NR 3 ENGINE FAILED A ABXA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 GL 23 849AX 45891 669610 NR 3 ENGINE OIL PRESSURE CLIMBED TO 62 PSI, OIL TEMP WAS 100 DEGREES CELSIUS. OIL PRESSURE THEN BEGAN TO FLUCTUATE BETW EEN 55 TO 62 PSI. ENGINE SECURED AT 0430 Z, ENGINE WINDMILLED FOR 17 MINUTES. MINIMUM OIL PRESSURE DURING WINDMILLING WAS15 PSI. REPLACED NR 3 ENGINE OIL PUMP, OIL FILTER AND OIL FILTER HOUSING. 2 L 7 4 4F 4 F 4A25 1E8 1996101700569 19961017 00569 WP 1996 10 17 MWEA96570 1 19961011 A 5313 2777948 LONGERON DOUG DC9 DC914 3022034 WP E/E COMPT CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND CORROSION ON LONGERON 27R AT STA 132 TO 140, 142 TO 144, 148 TO 154 BEYOND LIMITS. INSTALLED SECT ION OF LONGERON IAW 53-02, FIG 4. 2 L 7 2 4F A6WE 1996101700570 19961017 00570 WP 1996 10 17 MWEA96571 1 19961011 A 5320 INTERCOSTAL DOUG DC9 DC914 3022034 WP BS 360-371 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND FLOOR BEAM INTERCOSTAL CRACKED AT STA 360 AND 371 AND A/C CENTER LINE. INSTALLED DOUBLER REPAIR I AW SRM 53-01. 2 L 7 2 4F A6WE 1996101700571 19961017 00571 WP 1996 10 17 MWEA96572 1 19961011 A 5313 5915441501 LONGERON DOUG DC9 DC914 3022034 WP BS 474/303 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND LONGERON 29L CRACKED AT STA 474 AND 303. INSTALLED NEW LONGERON SECTION IAW SRM 51-30-5. 2 L 7 2 4F A6WE 1996101700572 19961017 00572 WP 1996 10 17 MWEA96573 1 19961011 A 5313 59164412 LONGERON DOUG DC9 DC914 3022034 WP BS 229-365/435 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND LONGERON 30 CRACKED AT STA 229, 365 AND 435. INSTALLED LONGERON SECTION STA 229 TO 465 IAW SRM 51 -30-5. 2 L 7 2 4F A6WE 1996101700573 19961017 00573 WP 1996 10 17 MWEA96574 1 19961011 A 5320 3913209501 FITTING DOUG DC9 DC914 3022034 WP BS 470 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND LONGERON 26L END FITTING CRACKED AT STA 470. REPLACED END FITTING IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1996101700574 19961017 00574 WP 1996 10 17 MWEA96575 1 19961011 A 5313 591141833 LONGERON DOUG DC9 DC914 3022034 WP BS 500 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND LONGERON 29L AT STA 500 CORRODED BEYOND LIMITS. REPLACED LONGERON IAW SRM 51-30. 2 L 7 2 4F A6WE 1996101700575 19961017 00575 WP 1996 10 17 MWEA96576 1 19961011 A 5320 ANGLE DOUG DC9 DC914 3022034 WP BS 817 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND FLOOR BEAM UPPER CAP ANGLE CORRODED BEYOND LIMITS. INSTALLED NEW CAP ANGLE IAW SRM 53-01. 2 L 7 2 4F A6WE 1996101700576 19961017 00576 WP 1996 10 17 MWEA96577 1 19961011 A 5753 99576003 FITTING DOUG DC9 DC914 3022034 WP LT TE FLAP CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND LT FLAP OUTBD HINGE FITTING MOUNT INBD AND OUTBD RIBS CRACKED. REPLACED CRACKED FITTINGS IAW SRM 57-30-2 AND SRM 51-30. 2 L 7 2 4F A6WE 1996101700577 19961017 00577 WP 1996 10 17 MWEA96578 1 19961011 A 5720 49114612 FITTING DOUG DC9 DC914 3022034 WP WS 164 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND RT WING UPPER OUTBD SKIN FITTINGS AT STA XRS 164 NEAR REAR SPAR ARE CRACKED. MAINTENANCE FABRICAT ED AND INSTALLED NEW FITTINGS IAW DAC DRAWING 4913298, 4911461, AND SRM 57-01. 2 L 7 2 4F A6WE 1996101700578 19961017 00578 WP 1996 10 17 MWEA96579 1 19961011 A 5330 SKIN DOUG DC9 DC914 3022034 WP BS 817 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND AFT CARGO COMPT SIDE SKIN CRACKED AT STA 817 RT SIDE LONGERON 22R, 8 INCHES IN LENGTH. INSTALLED REPAIR IAW DAC TELEX SVC-ORD-0232/RAK. 2 L 7 2 4F A6WE 1996101700579 19961017 00579 WP 1996 10 17 MWEA96580 1 19961011 A 5312 BULKHEAD DOUG DC9 DC914 3022034 WP AFT PRESS BLKHD SCRATCH A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND SMALL SCRATCH ON FWD SIDE OF AFT PRESSURE BULKHEAD FIVE INCHES ABOVE FLOOR LEVEL BLENDED BEYOND LI MITS. INSTALLED REPAIR IAW DAC TELEX SVC-ORD-0246/DMF. 2 L 7 2 4F A6WE 1996101700580 19961017 00580 WP 1996 10 17 MWEA96581 1 19961011 A 5312 BULKHEAD DOUBLER DOUG DC9 DC914 3022034 WP AFT PRESS BLKHD MISSING A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND PART OF FINGER DOUBLER MISSING ON FWD SIDE OF AFT PRESSURE BULKHEAD AT 10 O'CLOCK POSITION NEAR DO OR JAMB. FABRICATED AND INSTALLED FINGER DOUBLER IAW SRM 53-01. 2 L 7 2 4F A6WE 1996101700581 19961017 00581 WP 1996 10 17 MWEA96582 1 19961011 A 5315 FLOOR BEAM DOUG DC9 DC914 3022034 WP BS 801 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND FLOOR BEAM AT STA 801 HAS SEVERAL AREAS OF EXFOLIATION CORROSION AROUND NUTPLATES ON UPPER ANGLE O F FLOOR BEAM. FABRICATED AND INSTALLED REPAIR IAW SRM 53-05, FIG 20M. 2 L 7 2 4F A6WE 1996101700582 19961017 00582 WP 1996 10 17 MWEA96583 1 19961011 A 5210 STRAP DOUG DC9 DC914 3022034 WP PAX DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND CRACK IN STRAP ALONG FWD EDGE OF MAIN CABIN ENTRY DOOR OUTER PAN BELOW NR 2 STOP FITTING. FABRICA TED AND INSTALLED REPAIR IAW SRM 52-01 FIG 2. 2 L 7 2 4F A6WE 1996101700583 19961017 00583 WP 1996 10 17 MWEA96584 1 19961011 A 5330 SKIN DOUG DC9 DC914 3022034 WP BS 930 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND SKIN CRACK AT STA 930 AND LONGERON 3L, .625 INCH IN LENGTH. INSTALLED DOUBLER REPAIR IAW SRM 53-0 4 FIG 38. 2 L 7 2 4F A6WE 1996101700584 19961017 00584 WP 1996 10 17 MWEA96585 1 19961011 A 5531 RIB DOUG DC9 DC914 3022034 WP VERT STAB CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND VERTICAL STAB LEADING EDGE STA ZV147 UPPER RIB CRACKED AT AFT END. FABRICATED AND INSTALLED ANGLE REPAIR IAW SRM 55-01 FIG 2, SHEET 3. 2 L 7 2 4F A6WE 1996101700585 19961017 00585 WP 1996 10 17 MWEA96586 1 19961011 A 5320 PANEL DOUG DC9 DC914 3022034 WP BS 83 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND PRESSURE PANEL SKIN IN NOSE WHEEL WELL CRACKED STA 83 AND LT CUSP LINE 5 INCHES IN LENGTH, RT CUSP LINE 2 PLACES STA 83. INSTALLED DOUBLER REPAIR IAW DAC SB53-187. 2 L 7 2 4F A6WE 1996101700586 19961017 00586 WP 1996 10 17 MWEA96587 1 19961011 A 5753 SKIN DOUG DC9 DC914 3022034 WP LT TE FLAP WRINKLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CK, FOUND LT FLAP TRAILING EDGE NR 3 COUNTERSUNK HOLE ON UPPER SURFACE DAMAGED AND SKIN WRINKLED. INSTALLED DO UBLER REPAIR IAW SRM 57-01 FIG 2. 2 L 7 2 4F A6WE 1996101700587 19961017 00587 WP 1996 10 17 MWEA96588 1 19961011 A 5753 39129701 BRACKET DOUG DC9 DC914 3022034 WP LT TE FLAP CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND LT FLAP TRAILING EDGE NR 3 OUTBD END RIB FWD UPPER BRACKET CRACKED. REPLACED BRACKET IAW SRM 51-3 0-2. 2 L 7 2 4F A6WE 1996101700588 19961017 00588 WP 1996 10 17 MWEA96589 1 19961011 A 5330 SKIN DOUG DC9 DC914 3022034 WP BS 305-313 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND CORROSION ON SKIN IN FWD CARGO COMPT STA 305 TO 313, LONGERON 24R TO 26R. INSTALLED LONGERON SPLI CE REPAIRS AND DOUBLER REPAIRS IAW SRM 53-04. 2 L 7 2 4F A6WE 1996101700589 19961017 00589 WP 1996 10 17 MWEA96590 1 19961011 A 5330 SKIN DOUG DC9 DC914 3022034 WP BS 660-649 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND AFT CARGO COMPT BELLY SKIN CORRODED TO EXCESS STA 660 AND 649, LONGERON 28L AND 27L. INSTALLED DO UBLER REPAIR IAW SRM 53-04 FIG 38. 2 L 7 2 4F A6WE 1996101700590 19961017 00590 WP 1996 10 17 MWEA96591 1 19961011 A 5347 SEAT TRACK DOUG DC9 DC914 3022034 WP BS 294 CORROSION A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND CABIN SEAT TRACK NR 3 HAS CORROSION AT STA 294 BEYOND LIMITS AND CABIN SEAT TRACK NR 1 HAS CORROSI ON AT STA 408 BEYOND LIMITS. INSTALLED REPAIR ON BOTH SEAT TRACKS IAW SRM 53-04 FIG 4. 2 L 7 2 4F A6WE 1996101700591 19961017 00591 WP 1996 10 17 MWEA96592 1 19961011 A 5313 LONGERON DOUG DC9 DC914 3022034 WP BS 176-186 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND PREVIOUS REPAIR AT STA 544 TO 558, LONGERON 176 TO 186 THAT NEEDS REWORK. INSTALLED DOUBLER REPAI R IAW SRM 53-04 FIG 22. 2 L 7 2 4F A6WE 1996101700592 19961017 00592 WP 1996 10 17 MWEA96593 1 19961011 A 5320 053720005 DOUBLER DOUG DC9 DC914 3022034 WP BS 110-125 MISSING A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND SKIN REPAIR AT STA 110 TO 125 AND LONGERON 25R TO 26R NEED TITANIUM FINGER DOUBLER. INSTALLED REP AIR IAW SRM 53-04 FIG 26, SHEET 1. 2 L 7 2 4F A6WE 1996101700593 19961017 00593 WP 1996 10 17 MWEA96594 1 19961011 A 5320 INTERCOSTAL DOUG DC9 DC914 3022034 WP BS 624 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND INTERCOSTAL UNDER NR 2 SEAT TRACK IS CRACKED FWD OF STA 642. INSTALLED DOUBLER REPAIR IAW SRM 53- 01 FIG 2. 2 L 7 2 4F A6WE 1996101700594 19961017 00594 WP 1996 10 17 MWEA96595 1 19961011 A 5313 S1242886 LONGERON DOUG DC9 DC914 3022034 WP BS 754 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND LONGERON 30 CRACKED AT STA 754 AFT CARGO COMPT. MAINTENANCE SPLICED IN NEW SECTION OF LONGERON IA W SRM 53-10-3. 2 L 7 2 4F A6WE 1996101700595 19961017 00595 WP 1996 10 17 MWEA96596 1 19961011 A 5313 27779223 LONGERON DOUG DC9 DC914 3022034 WP BS 218 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND LONGERON 23R IS CRACKED AT STA 218. INSTALLED LONGERON IAW SRM 53-02 FIG 2. 2 L 7 2 4F A6WE 1996101700596 19961017 00596 WP 1996 10 17 MWEA96597 1 19961011 A 5330 SKIN DOUG DC9 DC914 3022034 WP BS 218 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND SKIN BULGED AT STA 218, LONGERON 23R, NO CORROSION FOUND. INSTALLED DOUBLER REPAIR IAW SRM 53-04 FIG 38. 2 L 7 2 4F A6WE 1996101700597 19961017 00597 WP 1996 10 17 MWEA96598 1 19961011 A 5320 ANGLE DOUG DC9 DC914 3022034 WP BS 237 ENLARGED HOLE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND ENLARGED FASTENER HOLE ON FRAME TO SKIN ATTACH ANGLE AT STA 237, LONGERON 8R. INSTALLED FABRICATE D ANGLE IAW SRM 53-03 FIG 32. 2 L 7 2 4F A6WE 1996101700598 19961017 00598 WP 1996 10 17 MWEA96599 1 19961011 A 5753 SKIN DOUG DC9 DC914 3022034 WP LT TE FLAP CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND LEFT FLAP UPPER EXTERIOR SKIN CHAFED 12 INCHES STA XFLS 273 TO 285. MAINTENANCE INSTALLED DOUBLER REPAIR IAW SRM 57-01. 2 L 7 2 4F A6WE 1996101700599 19961017 00599 WP 1996 10 17 MWEA96600 1 19961011 A 5330 59147073N SKIN DOUG DC9 DC914 3022034 WP BS 690-817 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND AFT CARGO COMPT SKIN FROM STA 690 TO 817 LONG 26L TO 26R HAS SEVERAL AREAS OF CORROSION. MAINTENA NCE REMOVED AND REPLACED SKIN STA 690 TO 817 L26L TO 26R IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1996101700600 19961017 00600 WP 1996 10 17 MWEA96601 1 19961011 A 5730 PANEL DOUG DC9 DC914 3022034 WP LT WING TE GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND LEFT WING TRAILING EDGE PANEL HAS 2 GOUGES ON THE SURFACE FWD OF THE GROUND SPOILER PANEL. MTC BL ENDED GOUGES FOUND OUT OF LIMITS. INSTALLED DOUBLER REPAIR IAW SRM 57-01 FIG 2. 2 L 7 2 4F A6WE 1996101700601 19961017 00601 WP 1996 10 17 MWEA96602 1 19961011 A 5330 59114015 SKIN DOUG DC9 DC914 3022034 WP BS 110-229 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND E AND E COMP BELLY SKIN HAS CORROSION IN SEVERAL AREAS BETWEEN STA 110 TO 229 LONG 26 TO 26R. REM OVED AND REPLACED BELLY SKIN STA 110 TO 229 IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1996101700602 19961017 00602 WP 1996 10 17 MWEA96603 1 19961011 A 5313 LONGERON DOUG DC9 DC914 3022034 WP BS 897 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND REPAIR OF LONGERON 2L AND 2R AT STA 897 NEED EVALUATION FOR REWORK. MAINTENANCE REMOVED REPAIR ON LONGERONS 2L AND 2R AT STA 897 AND INSTALLED SPLICE REPAIR IAW SRM 53-02 FIG 2. 2 L 7 2 4F A6WE 1996101700603 19961017 00603 WP 1996 10 17 MWEA96604 1 19961011 A 5315 FLOOR BEAM DOUG DC9 DC914 3022034 WP BS 801 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND FLOOR BEAM AT STA 801 HAS SEVERAL AREAS OF EXFOLIATION CORROSION ON UPPER FLANGE UNDER RT LAV. MA INTENANCE INSTALLED DOUBLER REPAIR IAW SRM 53-05 FIG 20A. 2 L 7 2 4F A6WE 1996101700604 19961017 00604 WP 1996 10 17 MWEA96605 1 19961011 A 5753 RIB DOUG DC9 DC914 3022034 WP LT TE FLAP CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND LEFT FLAP TRAILING EDGE NR 5, SECOND FROM INBD RIB IS CRACKED UPPER END. MAINTENANCE INSTALLED DO UBLER REPAIR IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1996101700605 19961017 00605 WP 1996 10 17 MWEA96606 1 19961011 A 5242 59103435 DOUBLER DOUG DC9 DC914 3022034 WP E/E COMPT DOOR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND AFTER REMOVAL OF E AND E COMP SKIN DOOR DOUBLER CORRODED BEYOND LIMITS. MAINTENANCE INSTALLED NEW DOUBLER IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1996101700606 19961017 00606 WP 1996 10 17 MWEA96607 1 19961011 A 5230 59101577 DOOR DOUG DC9 DC914 3022034 WP AFT CARGO COMPT CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 AFT CARGO DOOR HAS SEVERAL CRACKS AT STOP SUPPORT ON AFT END BEAM NR 4, INNER PAN AT FWD END AND UPPER STOP SUPPORT, UPP ER AND LOWER CENTER STOP AREA OUTER PAN CRACKED, CORROSION ON LWR CTR INTERCOSTAL ATTACH CLIP. MTC INSTALLED DOUBLER RE PAIRS IAW SRM 52-01, FIG 2 AND 51-10-4, SR05934104. 2 L 7 2 4F A6WE 1996101700607 19961017 00607 WP 1996 10 17 MWEA96608 1 19961011 A 5230 DOUBLER DOUG DC9 DC914 3022034 WP FWD CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND REPAIR DOUBLER CRACKED ON OUTER PAN NEAR FWD LOWER STOP. MAINTENANCE INSTALLED DOUBLER REPAIR IAW SRO 5934104. 2 L 7 2 4F A6WE 1996101700608 19961017 00608 WP 1996 10 17 MWEA96609 1 19961011 A 5312 5910367 BULKHEAD DOOR DOUG DC9 DC914 3022034 WP AFT PRESS BLKHD DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND AFT PRESSURE BULKHEAD PLUG DOOR HAS DENT IN LOWER PAN NEAR BAYONET. MAINTENANCE INSTALLED REPAIR IAW SRM 52-01 FIG 2. 2 L 7 2 4F A6WE 1996101700609 19961017 00609 WP 1996 10 17 MWEA96610 1 19961011 A 5730 SKIN DOUG DC9 DC914 3022034 WP LT WING LE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND LEFT WING INBD LEADING EDGE SECTION NR 1 HAS A SHARP DENT ON EXTERIOR SKIN LOWER SURFACE STA 192. MAINTENANCE INSTALLED DOUBLER REPAIR IAW SRM 57-06 FIG 1. 2 L 7 2 4F A6WE 1996101700610 19961017 00610 WP 1996 10 17 MWEA96611 1 19961011 A 5330 SKIN DOUG DC9 DC914 3022034 WP BS 239 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND DENT ON FUSELAGE SKIN STA 239 AND L176. MAINTENANCE INSTALLED DOUBLER REPAIR IAW SRM 53-01 FIG 38 . 2 L 7 2 4F A6WE 1996101700611 19961017 00611 WP 1996 10 17 MWEA96612 1 19961011 A 5730 SKIN DOUG DC9 DC914 3022034 WP LT WING TE BULGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CHECK, FOUND LEFT WING TRAILING EDGE PANEL OUTBD OF AILERON HAS BULGED SKIN AND DAMAGED RIB. MAINTENANCE FABRI CATED AND INSTALLED NEW SKIN IAW SRM 51-30-2 AND REPAIRED RIB IAW SRM 57-01 FIG 2 SHT 4. 2 L 7 2 4F A6WE 1996101700612 19961017 00612 WP 1996 10 17 MWEA96613 1 19961013 A 3397 L795U18 WIRE DOUG DC9 DC932 3022066 WP CABIN DETACHED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 209 47730 DURING SERVICE CHECK, FOUND EMERGENCY LIGHTS OVER TAIL EVACUATION SLIDE WOULD NOT ILLUMINATE. MAINTENANCE FOUND WIRE SE PARATED FROM TERMINAL RESECURED WIRE IAW DC9MM 33-51-01, OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996101700613 19961017 00613 NM 1996 10 17 MWEA96614 1 19961013 A 5330 SKIN DOUG MD88 MD88 3023688 NM FWD FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601 49768 DURING C-CHECK, FOUND CRACK IN SKIN AT NOSE LANDING GEAR DOOR CUTOUT OF AFT HINGE .75 INCH IN LENGTH. MAINTENANCE INST ALLED REPAIR IAW SRM 53-05 FIG 62. 2 L 7 2 4F RT A6WE 1996101700614 19961017 00614 SO 1996 10 17 SWIA95765 1 19960926 A 3230 CONTROL BOX EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LANDING GEAR FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 214SW 120280 LANDING GEAR WOULD NOT RETRACT. REPLACED LANDING GEAR CONTROL BOX, DID SEVERAL GEAR SWINGS AND OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1996101700615 19961017 00615 SW 1996 10 17 SWIA95766 1 19960926 A 3297 WIRE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP LT MLG UPLOCK SW FAILED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 2702Z AC669 LANDING GEAR WILL NOT RESPOND PROPERLY TO GEAR CONTROL INPUTS, WILL NOT FULLY RETRACT WITH SELECTOR UP. INTERMITTENTLY EXTENDED WITH GEAR CONTROL IN UP POSITION. LANDING GEAR CONTROL CIRCUIT BREAKER POPPED WHEN NOSE WHEEL STEERING SWITCH ARMED AND TESTED. REPAIRED WIRING TO LEFT GEAR UP POSITION SWITCH, CYCLED GEAR 20 TIMES AND OPS CKS GOOD. 2 L 7 2 4T 4 T RT A8SW E4WE 1996101700616 19961017 00616 SO 1996 10 17 SWIA95767 1 19960930 A 7920 1593731 HOSE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT OIL COOLER CHAFED A SWIA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 07 207SW 120266 AT CRUISE ALTITUDE, RIGHT OIL PRESSURE DROPPED TO 40 PSI. PERFORMED PRECAUTIONARY ENGINE SHUT DOWN ON RIGHT ENGINE. RE MOVED AND REPLACED UPPER HOSE ASSY ON RIGHT OIL COOLER. OPS CHECK AND LEAK CHECKS GOOD AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 1996101700617 19961017 00617 NM 1996 10 17 EISA96193 1 19960928 A 3230 UPLOCK FITTING BOEING 727 727223 1384074 NM LT MLG CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK , FOUND THE LEFT MLG UPLOCK SUPPORT FITTING CRACKED. REPLACED FITTING PER SB 727-53-103. ( M) 2 L 7 3 4F A3WE 1996101700618 19961017 00618 NM 1996 10 17 EISA96192 1 19960928 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 620 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND STRINGER 27R CORRODED STATION 620. REPAIRED STRINGER PER SRM 53-10-5. (M) 2 L 7 3 4F A3WE 1996101700619 19961017 00619 NM 1996 10 17 EISA96191 1 19960928 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 620 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND A CABIN SEAT TRACK CORRODED STATION 620 LBL 40. REPLACED SEAT TRACK PER SRM 53-10-5. (M) 2 L 7 3 4F A3WE 1996101700620 19961017 00620 NM 1996 10 17 EISA96190 1 19960928 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 690 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND CABIN SEAT TRACK CORRODED STATION 690 BL 40R. REPLACED SEAT TRACK PER SRM 53-10-5. 2 L 7 3 4F A3WE 1996101700621 19961017 00621 NM 1996 10 17 EISA96189 1 19960928 A 5712 RIB BOEING 727 727223 1384074 NM WS 629 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND RIGHT WING RIB CRACKED AT STATION 629. REPAIRED RIB PER SB 727-57-127. (M) 2 L 7 3 4F A3WE 1996101700622 19961017 00622 NM 1996 10 17 EISA96187 1 19960928 A 5311 FRAME BOEING 727 727223 1384074 NM BS 480 DAMAGED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND BELT FRAME STATION 480 STRINGER 14R TO STRINGER 16R DAMAGED. REPAIRED PER SRM 53-10-4 . (M) 2 L 7 3 4F A3WE 1996101700623 19961017 00623 NM 1996 10 17 EISA96188 1 19960928 A 5712 RIB BOEING 727 727223 1384074 NM WS 601.5 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND LEFT WING RIB CRACKED AT STATION 601.5. REPAIRED RIB PER SB 57-127. (M) 2 L 7 3 4F A3WE 1996101700624 19961017 00624 NM 1996 10 17 EISA96185 1 19960928 A 5311 FRAME BOEING 727 727223 1384074 NM BS 460 TORN A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND 1 INCH TEAR IN BELT FRAME STATION 460 STRINGER 16R. REPAIRED PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1996101700625 19961017 00625 NM 1996 10 17 EISA96184 1 19960928 A 5311 FRAME BOEING 727 727223 1384074 NM BS 420 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND BELT FRAME STATION 420 STRINGER 20R TO STRINGER 21R CRACKED PAST PREVIOUS STOP DRILLS. REPAIRED PER SRM 51-40-6. (M) 2 L 7 3 4F A3WE 1996101700626 19961017 00626 NM 1996 10 17 EISA96183 1 19960928 A 5320 T-CAP BOEING 727 727223 1384074 NM BS 1060-1075 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND T-CAP CORRODED STATION 1060-1075 BL 10L. REPAIRED PER SRM 53-10-8. (M) 2 L 7 3 4F A3WE 1996101700627 19961017 00627 NM 1996 10 17 EISA96182 1 19960928 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 540-640 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND CABIN SEAT TRACK CORRODED STATION 540-640 BL 40R. REPLACED TRACK PER SRM 53-10-5. (M ) 2 L 7 3 4F A3WE 1996101700628 19961017 00628 NM 1996 10 17 EISA96181 1 19960928 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 540-620 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND CABIN SEAT TRACK CORRODED STATION 540-620 LBL 40. REPLACED TRACK PER SRM 53-10-5. (M ) 2 L 7 3 4F A3WE 1996101700629 19961017 00629 NM 1996 10 17 EISA96180 1 19960928 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 700 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND CABIN SEAT TRACK CORRODED STATION 700 BL 20R. REPLACED TRACK PER SRM 53-10-5. (M) 2 L 7 3 4F A3WE 1996101700630 19961017 00630 NM 1996 10 17 EISA96179 1 19960928 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 1030 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND SEAT TRACK CORRODED STATION 1030 BL 12L. REPLACED TRACK PER SRM 53-10-5. (M) 2 L 7 3 4F A3WE 1996101700631 19961017 00631 NM 1996 10 17 EISA96178 1 19960928 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 690-700 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND CABIN SEAT TRACK CORRODED STATION 690-700 RBL 2A. REPLACED TRACK PER SRM 53-10-5. (M ) 2 L 7 3 4F A3WE 1996101700632 19961017 00632 NM 1996 10 17 EISA96177 1 19960928 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1110 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND FRAME CRACKED STATION 1110, STRINGER 19R. REPAIRED FRAME PER SRM 51-40-5. (M) 2 L 7 3 4F A3WE 1996101700633 19961017 00633 NM 1996 10 17 EISA96176 1 19960928 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 480-540 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND CABIN SEAT TRACK CORRODED STATION 480-540 RBL 40. REPLACED SEAT TRACK PER SRM 53-10-5 . (M) 2 L 7 3 4F A3WE 1996101700634 19961017 00634 NM 1996 10 17 EISA96175 1 19960928 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 540-660 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND SEAT TRACK CORRODED STATION 540-660 RBL 40. REPLACED SEAT TRACK PER SRM 53-10-5. (M) 2 L 7 3 4F A3WE 1996101700635 19961017 00635 NM 1996 10 17 EISA96174 1 19960928 A 5320 CLIP BOEING 727 727223 1384074 NM BS 950 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED STATION 950A STRINGER 7R. REPLACED CLIP PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1996101700636 19961017 00636 NM 1996 10 17 EISA96173 1 19960928 A 5320 CLIP BOEING 727 727223 1384074 NM BS 950 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED STATION 950A STRINGER 7R. REPLACED CLIP PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1996101700637 19961017 00637 NM 1996 10 17 EISA96172 1 19960928 A 5320 CLIP BOEING 727 727223 1384074 NM BS 950 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED STATION 950A STRINGER 9R. REPLACED CLIP PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1996101700638 19961017 00638 NM 1996 10 17 EISA96171 1 19960928 A 5320 CLIP BOEING 727 727223 1384074 NM BS 950 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED STATION 950B STRINGER 9R. REPLACED CLIP PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1996101700639 19961017 00639 NM 1996 10 17 EISA96170 1 19960928 A 5320 CLIP BOEING 727 727223 1384074 NM BS 950 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED STATION 950B STRINGER 7R. REPLACED CLIP PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1996101700640 19961017 00640 NM 1996 10 17 EISA96168 1 19960928 A 5320 CLIP BOEING 727 727223 1384074 NM BS 950 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED STATION 950B STRINGER 5R. REPLACED CLIP PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1996101700641 19961017 00641 NM 1996 10 17 EISA96169 1 19960928 A 5320 CLIP BOEING 727 727223 1384074 NM BS 950 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED STATION 950B STRINGER 6R. REPLACED CLIP PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1996101700642 19961017 00642 NM 1996 10 17 EISA96167 1 19960928 A 5320 CLIP BOEING 727 727223 1384074 NM BS 950C CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED STATION 950C STRINGER 9C. REPLACED CLIP PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1996101700643 19961017 00643 NM 1996 10 17 EISA96166 1 19960928 A 5320 CLIP BOEING 727 727223 1384074 NM BS 950 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED STATION 950C STRINGER 8L. REPLACED CLIP PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1996101700644 19961017 00644 NM 1996 10 17 EISA96165 1 19960928 A 5320 CLIP BOEING 727 727223 1384074 NM BS 950 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED STATION 950C STRINGER 7L. REPLACED CLIP PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1996101700645 19961017 00645 NM 1996 10 17 EISA96164 1 19960928 A 5320 CLIP BOEING 727 727223 1384074 NM BS 720 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED STATION 720C STRINGER 7R AND STRINGER 8R. REPLACED CLIP PER SR M 51-10-1. (M) 2 L 7 3 4F A3WE 1996101700646 19961017 00646 NM 1996 10 17 EISA96163 1 19960928 A 5320 CLIP BOEING 727 727223 1384074 NM BS 720 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED STATION 720C STRINGER 9R. REPLACED CLIP PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1996101700647 19961017 00647 NM 1996 10 17 EISA96162 1 19960928 A 5320 CLIPS BOEING 727 727223 1384074 NM BS 720 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED STATION 720D, STRINGERS 5R AND 7R. REPLACED CLIP PER SRM 51-10 -1. (M) 2 L 7 3 4F A3WE 1996101700648 19961017 00648 NM 1996 10 17 EISA96161 1 19960928 A 5320 CLIP BOEING 727 727223 1384074 NM BS 825 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED STATION 825 STRINGER 5R. REPLACED CLIP PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1996101700649 19961017 00649 NM 1996 10 17 EISA96160 1 19960928 A 5311 FRAME BOEING 727 727223 1384074 NM BS 890 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND FRAME CRACKED STATION 890, STRINGER 14L. REPAIRED FRAME PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1996101700650 19961017 00650 NM 1996 10 17 EISA96159 1 19960928 A 5320 CLIP BOEING 727 727223 1384074 NM BS 950 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED STATION 950B STRINGERS 6L, 7L, 8L. REPLACED CLIP PER SRM 51-10 -1. (M) 2 L 7 3 4F A3WE 1996101700651 19961017 00651 NM 1996 10 17 EISA96158 1 19960928 A 5320 CLIP BOEING 727 727223 1384074 NM BS 720 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED STATION 720 STRINGER 5L. REPLACED CLIP PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1996101700652 19961017 00652 NM 1996 10 17 EISA96157 1 19960928 A 5320 CLIP BOEING 727 727223 1384074 NM BS 720 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED STATION 720A STRINGER 6R. REPLACED CLIP PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1996101700653 19961017 00653 NM 1996 10 17 EISA96156 1 19960928 A 5320 CLIP BOEING 727 727223 1384074 NM BS 720 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED STATION 720A, STRINGERS 7R, 8R, 9R. REPLACED CLIP PER SRM 51-1 0-1. (M) 2 L 7 3 4F A3WE 1996101700654 19961017 00654 NM 1996 10 17 EISA96155 1 19960928 A 5320 CLIP BOEING 727 727223 1384074 NM BS 720 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED STATION 720C STRINGER 7L. REPLACED CLIP PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1996101700655 19961017 00655 NM 1996 10 17 EISA96154 1 19960928 A 5320 CLIP BOEING 727 727223 1384074 NM BS 720 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED STATION 720C STRINGER 9R AND STRINGER 6R. REPLACED CLIPS PER S RM 51-10-1. (M) 2 L 7 3 4F A3WE 1996101700656 19961017 00656 NM 1996 10 17 EISA96153 1 19960928 A 5320 CLIP BOEING 727 727223 1384074 NM BS 950 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED STATION 950C STRINGER 5L. REPLACED CLIP PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1996101700657 19961017 00657 NM 1996 10 17 EISA96152 1 19960928 A 5320 CLIP BOEING 727 727223 1384074 NM BS 950 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED STATION 950C STRINGER 6R. REPLACED CLIP PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1996101700658 19961017 00658 NM 1996 10 17 EISA96151 1 19960928 A 5320 CLIP BOEING 727 727223 1384074 NM BS 950 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED STATION 950D STRINGER 5L. REPLACED CLIP PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1996101700659 19961017 00659 NM 1996 10 17 EISA96150 1 19960928 A 5320 CLIP BOEING 727 727223 1384074 NM BS 990 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED STATION 990 STRINGER 4L. REPLACED CLIP PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1996101700660 19961017 00660 NM 1996 10 17 EISA96149 1 19960928 A 5320 CLIP BOEING 727 727223 1384074 NM BS 700 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED STATION 700 STRINGER 7R-8R. REPLACED CLIP PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1996101700661 19961017 00661 NM 1996 10 17 USAA960658 1 19960927 A 5315 FLOOR BEAM BOEING 737 737201 1384454 NM BS 707-712 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 224US 47115 21666 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND FOUR .75 INCH CRACKS, LBL 25 INCHES LONG FLOOR BEAM WEB STATION 707 TO 7 12, WL 203.5. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2. (M) 2 L 7 2 4F A16WE 1996101700662 19961017 00662 NM 1996 10 17 USAA960638 1 19960927 A 5315 BAC1518338 FLOOR BEAM BOEING 737 737301 1384611 NM BS 344 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 353US 26941 23556 CLT - INSPECTION VISUALLY FOUND A 1 INCH BY .5 INCH LEVEL 2 CORRODED AREA, LOCATED AT FLOOR BEAM STATION NR 344 LBL 22. INSTALLED REPAIR ANGLES PER USAIR TYPICAL REPAIR 53-10-01A. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996101700663 19961017 00663 NM 1996 10 17 USAA960634 1 19960927 A 5315 BAC1518338 FLOOR BEAM BOEING 737 737301 1384611 NM BS 312 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 353US 26941 23556 CLT - INSPECTION VISUALLY FOUND A .5 INCH BY 4 INCH LEVEL 2 CORRODED AREA, LOCATED AT FLOOR BEAM STATION NR 312, LBL 26. INSTALLED REPAIR ANGLES AS PER USAIR TYPICAL REPAIR 53-10-03. CORROSION TASK NR C53-107-02, CORRROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996101700664 19961017 00664 NM 1996 10 17 USAA960657 1 19960927 A 5315 FLOOR BEAM BOEING 737 737201 1384454 NM BS 707-712 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 224US 47115 21666 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND FOUR .5 INCH CRACKS BL 0 INCH LONG FLOOR BEAM WEB STATION 707 TO STATION 712, WL 203.5. INSTALLED REPAIR WEB, REPAIRED PER SRM 51-40-2. (M) 2 L 7 2 4F A16WE 1996101700665 19961017 00665 NM 1996 10 17 USAA960656 1 19960927 A 5240 SKIN BOEING 737 737201 1384454 NM FWD SERV DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 224US 47115 21666 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .375 INCH CRACK EXTERNAL SKIN DOUBLER FORWARD SERVICE DOOR LOWER HINGE. INSTALLED NEW DOUBLER, REPAIRED PER TR 52-10-01A. (M) 2 L 7 2 4F A16WE 1996101700666 19961017 00666 NM 1996 10 17 USAA960655 1 19960927 A 5240 SKIN BOEING 737 737201 1384454 NM FWD SERV DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 224US 47115 21666 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK CORNER OF HINGE CUT OUT FORWARD SERVICE DOOR SKIN. INST ALLED DOUBLER, REPAIRED PER TR 52-40-03A. (M) 2 L 7 2 4F A16WE 1996101700667 19961017 00667 NM 1996 10 17 USAA960654 1 19960927 A 5320 STUB BEAM BOEING 737 737201 1384454 NM BS 597 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 224US 47115 21666 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK STATION 597 STUB BEAM WEB RBL 60 TO RBL 62, WL 207.5. INS TALLED DOUBLER, REPAIRED PER SRM 51-40-2. (M) 2 L 7 2 4F A16WE 1996101700668 19961017 00668 NM 1996 10 17 USAA960653 1 19960927 A 5312 BULKHEAD BOEING 737 737201 1384454 NM BS 663 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 224US 47115 21666 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK STATION 663 BULKHEAD UPPER CHORD ANGLE AT LBL 25, WL 202. INSTALLED DOUBLER, REPAIRED PER DRAWING 65C37732. (M) 2 L 7 2 4F A16WE 1996101700669 19961017 00669 NM 1996 10 17 USAA960652 1 19960927 A 5312 BULKHEAD BOEING 737 737201 1384454 NM BS 663 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 224US 47115 21666 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK STATION 663 BULKHEAD UPPER CHORD ANGLE AT LBL 25, WL 202. INSTALLED DOUBLERS, REPAIRED PER DRAWING 65C37732. (M) 2 L 7 2 4F A16WE 1996101700670 19961017 00670 NM 1996 10 17 USAA960651 1 19960927 A 5311 FRAME BOEING 737 737201 1384454 NM BS 328 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 224US 47115 21666 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK IN CIRCUFERENTIAL FRAME STATION 328 3 INCHES BELOW STRINGER STRINGER 20R. FABRICATED 707576 .040 MATERIAL, INSTALLED WEB REPAIR, REPAIRED PER SRM 51-40-2 FIG 1. (M) 2 L 7 2 4F A16WE 1996101700671 19961017 00671 NM 1996 10 17 USAA960650 1 19960927 A 5315 FLOOR BEAM BOEING 737 737201 1384454 NM BS 707-712 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 224US 47115 21666 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACKS IN FOUR PLACES, RBL 25 INCHES LONG, FLOOR BEAM WEB STATIO N 707 TO 712, WL 203.5. INSTALLED WEB REPAIR, REPAIRED PER SRM 51-40-2. (M) 2 L 7 2 4F A16WE 1996101700672 19961017 00672 NM 1996 10 17 USAA960649 1 19960927 A 5320 SUPPORT CHANNEL BOEING 737 737201 1384454 NM RBL 45 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 224US 47115 21666 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRCK RBL 45 SEAT TRACK SUPPORT CHANNEL ABOVE UPPER INBOARD BOLT. INSTALLED DOUBLERS, REPAIRED PER EA 41455 AND SB 737-53-1120. (M) 2 L 7 2 4F A16WE 1996101700673 19961017 00673 NM 1996 10 17 USAA960648 1 19960927 A 5320 WEB BOEING 737 737201 1384454 NM BS 639 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 224US 47115 21666 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND TWO CRACKS 1 INCH BY 3 INCH CREASE BEAM WEB 2 INCHES AFT OF STATION 639 PLUS 1 INCH FORWARD OF STATION 663 FRAME LBL 67, WL 208. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2. (M) 2 L 7 2 4F A16WE 1996101700674 19961017 00674 NM 1996 10 17 USAA960647 1 19960927 A 5320 SUPPORT CHANNEL BOEING 737 737201 1384454 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 224US 47115 21666 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK LBL BS 520, WL 207.5 SUPPORT CHANNEL. FABRICATED DOUBLER CHANNEL RADIUS FILLERS, INSTALLED CHANNEL AND FILLERS. REPAIRED PER EA 41455 SB 337-53-1120. (M) 2 L 7 2 4F A16WE 1996101700675 19961017 00675 NM 1996 10 17 USAA960646 1 19960927 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 525 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 224US 47115 21666 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACKS EMITTING FROM FASTENER HOLES (2) STRINGER 15L BS 525. C HANNEL REPAIR INSTALLED ON STRINGER, REPAIRED PER SRM 53-10-3. (M) 2 L 7 2 4F A16WE 1996101700676 19961017 00676 NM 1996 10 17 AALA961246 1 19960822 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 6819 19494 DFW - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY EXIT FLOOR PATH LIGHT AT ROWS 3 INOPERATIVE. REPAIRED LIGHT STRIP A T ROW 3. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996101700677 19961017 00677 NM 1996 10 17 AALA961381 1 19960922 A 3350 A3060698101 CONNECTOR BOEING 727 727223 1384074 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 865AA 21370 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FORWARD PART OF MAIN CABIN INOPERATIVE. REPLACED BROKEN EMERGEN CY FLOOR LIGHT STRIP CONNECTORS AT FORWARD PART AND MID PART OF MAIN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M ) 2 L 7 3 4F A3WE 1996101700678 19961017 00678 NM 1996 10 17 AALA961352 1 19960913 A 3350 A3060698101 CONNECTOR BOEING 727 727223 1384074 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 701AA 22459 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIG HT STRIP CONNECTOR BY FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996101700679 19961017 00679 WP 1996 10 17 AALA961351 1 19960913 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 571AA 49353 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FORWARD HALF OF MAIN CABIN INOPERATIVE. REPLACED EMERGENCY FLOO R LIGHTS STRIPS AT PAX SEAT ROWS 6E, 10D, 14D, AND 18D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 1996101700680 19961017 00680 WP 1996 10 17 AALA961377 1 19960920 A 3260 PROX SENSOR DOUG DC9 DC982 3022082 WP NLG DIRTY A AALA O OTHER N FALSE WARNING CL CLIMB 1 SW 07 276AA 49273 MEX - FLT 1321 - AFTER TAKEOFF DFW WHEN LANDING GEAR RETRACTED, RED NOSE LANDING GEAR LIGHT REMAINED ILLUMINATED WITH NO OTHER ABNORMAL INDICATIONS. AIRCRAFT PROCEEDED TO MEX AND LANDED WITHOUT INCIDENT. CLEANED GREASE FROM NOSE LANDING G EAR TARGET AND PROXIMITY SENSOR. CHECKED UP, DOWN AND LOCK SENSOR FOR PROPER GAP WITH NO DEFECTS FOUND. ACCOMPLISHED B ITE CHECK OF NOSE GEAR SENSORS AND WIRING WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. UNABLE TO DUP LICATE PROBLEM AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996101700681 19961017 00681 WP 1996 10 17 AALA961378 1 19960921 A 3260 POSITION SENSOR DOUG DC9 DC982 3022082 WP NLG MALFUNCTIONED A AALA O OTHER N FALSE WARNING CL CLIMB 1 SW 07 276AA 49273 DFW - FLT 1793 - AFTER TAKEOFF MEX WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR RED LIGHT REMAINED ILLUMINATED WITH NO OTHER ABNORMAL INDICATIONS. RECYCLED LANDING GEAR AND ALL INDICATIONS RETURNED TO NORMAL. AIRCRAFT PROCEEDED TO DFW A ND LANDED WITHOUT INCIDENT. ACCOMPLISHED NOSE LANDING GEAR RETRACTION CHECK MULTIPLE CYCLED WITH NO DEFECTS FOUND. PRE CAUTIONARY REPLACED LANDING GEAR INTERLOCK RELAY AND NOSE LANDING GEAR POSITION SENSOR. SYSTEM GROUND CHECKED NORMAL OP ERATION AND AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1996101700682 19961017 00682 WP 1996 10 17 AALA961374 1 19960917 A 2913 314195 PUMP VICKERS DOUG DC9 DC982 3022082 WP RT ENG FAILED A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 224AA 49174 ATL - FLT 455 - AFTER TAKEOFF ATL DURING CLIMB-OUT WHEN SWITCHING ENGINE HYDRAULIC PUMPS TO LOW, RIGHT PUMP FAILED WITH COMPLETE LOSS OF HYDRAULIC FLUID. ACCOMPLISHED ABNORMAL PROCEDURES, MANUALLY EXTENDED LANDING GEAR AND AIRCRAFT RETURNE D TO ATL, LANDING WITHOUT INCIDENT. REPLACED RIGHT ENG HYD PUMP AND SYS FILTERS. SERVICED RIGHT HYD SYSTEM. ACCOMP GR OUND ENG RUN AND SYS LEAK AND GROUND CHECKED NORMAL. A/C MX FERRY ATL/TUL. REPLACED RIGHT MAIN LANDING GEAR DOOR DUE T O DAMAGE SUSTAINED DURING LANDING AT ATL. ACCOMPLISHED DOOR RIG AND LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996101700683 19961017 00683 WP 1996 10 17 AALA961411 1 19960923 A 3260 833703 LOCK SENSOR ELDEC DOUG DC9 DC983 3022083 WP NLG DEFECTIVE A AALA O OTHER N FALSE WARNING CL CLIMB 1 SW 07 562AA 49344 DFW - FLT 1212 - AFTER TAKEOFF MEX WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR RED LIGHT REMAINED ILLUMINATED WITH NO OTHER ABNORMAL INDICATIONS. ACCOMPLISHED ABNORMAL PROCEDURE AND LIGHT EXTINGUISHED. AIRCRAFT PROCEEDED TO DFW AND LAN DED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR LOCK SENSOR. ACCOMPLISHED NOSE LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 1996101700684 19961017 00684 EU 1996 10 17 AALA961350 1 19960915 A 2170 20D102 COALESCER AIRBUS 300 A300B4605R 3930308 EU ACM BAY DIRTY A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 70072 515 SDQ - FLT 1728 - AFTER TAKEOFF SDQ DURING CLIMB-OUT, ELECTRICAL TYPE ODOR NOTED IN CABIN WITH NO VISIBLE SMOKE. AIRCRAF T RETURNED SDQ AND LANDED WITHOUT INCIDENT. CHECKED CABIN AREA WITH NO DEFECTS FOUND. ACCOMPLISHED PACK BURNOUT PROCED URE AND PRECAUTIONARY REPLACED COALESCER BAGS. SYSTEM GROUND CHECKED NORMAL OPERATION AND UNABLE TO DUPLICATE ODOR. AI RCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A35EU 1996101700685 19961017 00685 EU 1996 10 17 AALA961233 1 19960819 A 5270 DOOR WARNING AIRBUS 300 A300B4605R 3930308 EU L3 EMER EXIT DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 8067A 510 JFK - DURING OVERNIGHT MAINTENANCE, FOUND THE L3 EMERGENCY EXIT DOOR WARNING HORN WOULD NOT SOUND. REPLACED L3 EMERGENC Y EXIT DOOR WARNING HORN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996101700686 19961017 00686 EU 1996 10 17 AALA961095 1 19960721 A 3230 D226550002 DAMPER MESSIER AIRBUS 300 A300B4605R 3930308 EU LT MLG DAMAGED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 90070 513 SJU - FLT 1600 - AFTER TAKEOFF SJU WHEN LANDING GEAR RETRACTED, LEFT MAIN LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETU RNED TO SJU AND LANDED WITHOUT INCIDENT. REPLACED LEFT MAIN LANDING GEAR LEVELING CYLINDER (PITCH DAMPER) FOUND DAMAGED . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996101700687 19961017 00687 EU 1996 10 17 AALA961323 1 19960905 A 2150 20497524 ACM GARRTT AIRBUS 300 A300B4605R 3930308 EU NR 2 ACM BAY DEFECTIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 14053 116259 420 MIA - FLT 1901 - AFTER TAKEOFF MIA DURING CLIMB-OUT, AIR CYCLE MACHINE NR 2 FAILED AND PRODUCED SMOKE IN CABIN. AIRCRAF T RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED NR 2 AIR CYCLE MACHINE, RIGHT PACK TURBINE BYPASS VALVE, SENSE LINE AND REPLACED COALESCER BAG. ACCOMPLISHED PACK BURNOUT PROCEDURE. SYSTEM GROUND CHECKED NORMAL OPERATION WITH NO S MOKE OR ODOR NOTED. (M) 2 L 7 2 4F RT A35EU 1996101700688 19961017 00688 1996 10 17 ASAA9640086 4 19960925 A 2565 61621469 SLIDE BOEING 737 7374Q8 NM LT AFT DOOR MISINSTALLED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 1637 25096 OAK - DURING C-CHECK, DURING THE REINSTALLATION OF THE LEFT AFT DOOR EMERGENCY EXIT SLIDE, THE SLIDE WAS FOUND TO HAVE H AD A RED SECURING STRAP WRAPPED AROUND THE SLIDE. REMOVED STRAP AND COMPLETED SLIDE INSTALLATION. (M) 2 L 7 2 4F RT A16WE 1996101700689 19961017 00689 WP 1996 10 17 ASAA9680214 1 19961002 A 3350 6011779 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 931AS 24119 49232 SEA - DURNG MAINTENANCE CHECK,THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996101700690 19961017 00690 WP 1996 10 17 ASAA9680213 1 19961001 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 53016 BUR - PRIOR TO DEPARTURE OF FLT 535 - CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATI VE. RECONNECTED ELECTRICAL CONNECTOR AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996101700691 19961017 00691 WP 1996 10 17 ASAA9680211 1 19960928 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 969AS 53063 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 14 TO 16 WERE FOUND INOPERATIVE. RECONNECTED WIRE AT ROW 17 AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996101700692 19961017 00692 WP 1996 10 17 ASAA9680210 1 19960928 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 947AS 53020 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 29 TO 31 WERE FOUND INOPERATIVE. REPAIRED BR OKEN WIRE AT ROW 31 AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996101700693 19961017 00693 NM 1996 10 17 ASAA9640087 1 19961001 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 773AS 25106 ANC - FLIGHT 66 - PRIOR TO DEPARTURE, THE CREW REPORTED THAT THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE INOPERATIVE AT T HE AFT OVERWING EXIT AREA. RECONNECTED LOOSE WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996101700694 19961017 00694 NM 1996 10 17 ASAA9640085 1 19960926 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 780AS 25112 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 14 THROUGH 17 . RECONNECTED WIRES AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996101700695 19961017 00695 NM 1996 10 17 ASAA9640084 1 19960926 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 771AS 25104 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 15 THROUGH 18 . RECONNECTED WIRES AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996101700696 19961017 00696 NM 1996 10 17 ASAA9610130 1 19960927 A 3397 WIRE BOEING 737 737290C 138448V NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 16 AND 17. RECONNE CTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1996101700697 19961017 00697 NM 1996 10 17 ASAA9610129 1 19960919 A 5314 6547693502 KEEL BEAM BOEING 737 737298C 1384490 NM BS 727 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 ANC - DURING NON ROUTINE MAINTENANCE, FOUND THE RIGHT KEEL BEAM CHORD CORRODED AND CRACKED AT BS 727 PLUS 10, RBL 6.3. I NSPECTED AND RELEASED AIRCRAFT FOR FERRY FLIGHT TO SEA FOR REPAIR. SUBSEQUENTLY REPAIRED AREA PER EA 5310-01492, BOEING TELEX ASA-SEA-96-0466RR, AND ASA-SEA-96-0472RR. (M) 2 L 7 2 4F RT A16WE 1996101700698 19961017 00698 WP 1996 10 17 ASAA9680209 1 19960922 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 953AS 5037 49386 PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996101700699 19961017 00699 WP 1996 10 17 ASAA9680207 1 19960921 A 3350 6030431 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 962AS 53076 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE TAILCONE AREA WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996101700700 19961017 00700 WP 1996 10 17 ASAA9680206 1 19960921 A 3350 014597101 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 939AS 49657 SEA - DURING MAINTNENANCE CHECK, THE 0VERHEAD EMERGENCY LIGHTS IN THE TAILCONE AREA WERE FOUND INOPERATIVE. REPLACED TH E BATTERIES AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996101700701 19961017 00701 WP 1996 10 17 ASAA9680205 1 19960921 A 3350 014597101 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 939AS 49657 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROW 29 AFT WERE FOUND INOPERATIVE. REPLACED THE B ATTERIES AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996101700702 19961017 00702 WP 1996 10 17 ASAA9680203 1 19960919 A 3350 41B004AD07G3 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 954AS 49387 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 9 TO 11 WERE FOUND INOPERATIVE. REPLACED THE BA TTERIES AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996101700703 19961017 00703 WP 1996 10 17 ASAA9680202 1 19960918 A 3350 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 953AS 49386 ONT - DURING MAINTENANCE CHECK, THE OVERWING EMERGENCY LIGHTS ILLUMINATED WHEN THE AIRCRAFT BATTERY SWITCH WAS TURNED OF F. RECHARGED THE BATTERIES AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996101700704 19961017 00704 NM 1996 10 17 ASAA9640083 1 19960819 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 771AS 25104 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 15, 16, AND 1 7. REPAIRED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996101700705 19961017 00705 NM 1996 10 17 AWXA960542 1 19960929 A 2751 1817385 FLAP POS XMITTER BOEING 737 737277 1384570 NM LT TE FLAP OUT OF RIG A A AWXA O OTHER N FALSE WARNING DE DESCENT 1 WP 28 185AW 43928 22652 PHX - FLT 2647 - SELECTING FLAPS 15 FROM 5, A NOTICEABLE SPLIT OCCURRED CAUSING A SLIGHT ROLL. SPLIT DID NOT EXCEED LIM ITS OF WHITE BAND, IMPROVED WHEN SELECTING FLAPS 30. OCCURRED AGAIN WHEN SELECTING FLAPS UP. FOUND LEFT FLAP POSITION TRANSMITTER OUT OF RIG. REMOVED AND REPLACED TRANSMITTER, IAW R3M17012, OPERATIONS CHECK GOOD. CYCLED FLAPS AND PERFOR MED VISUAL INSPECTION. NO DEFECTS NOTED. (M) 2 L 7 2 4F RT A16WE 1996101700706 19961017 00706 NM 1996 10 17 AWXA960543 1 19960930 A 3350 1060091101 LIGHT BOEING 737 7372A6 138448B NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 145AW 20194 PHX - FLT 2312 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT ON SEAT 17C INOP. REPLACED LIGHT ASSEMBLY . OPERATIONS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1996101700707 19961017 00707 NM 1996 10 17 AWXA960539 1 19960929 A 3350 831862 BATTERY BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 186AW 22653 PHX - FLT 7706 - DURING ROUTINE MAINTENANCE CHECK, FOUND THE EMERGENCY LIGHTS WERE LEFT ON. ALL LIGHTS WERE INOP. FERR IED BACK TO PHX. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F RT A16WE 1996101700708 19961017 00708 NM 1996 10 17 AWXA960532 1 19960928 A 3350 LIGHT BOEING 737 737277 1384570 NM CABIN MISSING A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 178AW 22645 PHX - FLT 2287 - DURING ROUTINE MAINTENANCE CHECK, FOUND SELF ILLUMINATING EXIT SIGN MISSING FROM AFT SIDE OF CLASS DIVI DER. INSTALLED SELF ILLUMINATING LIGHT. (M) 2 L 7 2 4F RT A16WE 1996101700709 19961017 00709 NM 1996 10 17 AWXA960531 1 19960927 A 3350 LAMP BOEING 737 737277 1384570 NM CABIN LOOSE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 184AW 22651 PHX - FLT 7887 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT SEAT 5 C INOP. FOUND LAMP OUT OF SOCKET. REIN STALLED, LAMP OPERATES GOOD. (M) 2 L 7 2 4F RT A16WE 1996101700710 19961017 00710 NM 1996 10 17 AWXA960530 1 19960927 A 3350 LIGHT BOEING 737 737277 1384570 NM CABIN MISSING A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 188AW 22655 DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 5 EMERGENCY FLOOR PROX SEAT MOUNTED LIGHT MISSING. REPLACED MISSING LIGHT. OPS GOOD. (M) 2 L 7 2 4F RT A16WE 1996101700712 19961017 00712 NM 1996 10 17 AWXA960547 1 19960915 A 5230 FRAME BOEING 757 7572S7 1384962 NM CARGO DOOR GOUGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 904AW 23566 PAE - FLT 7803 - DURING ROUTINE SCHEDULED C-4 MAINTENANCE CHECK, FOUND AFT CARGO DOOR GOUGED. REMOVED AND REPLACED LOWE R DOOR FRAME PER SRM 51-40-02. (M) 2 L 7 2 4F RT A2NM 1996101700713 19961017 00713 NM 1996 10 17 AWXA960544 1 19960912 A 5320 SILL BOEING 757 7572S7 1384962 NM BS 318 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 904AW 23566 DURING ROUTINE SCHEDULED C-4 MAINTENANCE CHECK, FOUND CORROSION ON R1 MOPSILL BS 318 TO 324, RBL 65. REMOVED AND REPLAC ED MOPSILL, IAW, SRM 51-40-02, 51-30-01, 53-10-15. (M) 2 L 7 2 4F RT A2NM 1996101700714 19961017 00714 NM 1996 10 17 AWXA960545 1 19960912 A 5320 SHEAR TIE BOEING 757 7572S7 1384962 NM BS 1300 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 904AW 23566 DURING ROUTINE SCHEDULED C-4 MAINTENANCE CHECK, FOUND CORROSION ON SHEAR TIE BETWEEN STRINGER 18R AND 19R, BS 1300. FAB RICATED AND INSTALLED NEW SHEAR TIE, IAW, SRM 51-40-02. (M) 2 L 7 2 4F RT A2NM 1996101700715 19961017 00715 NM 1996 10 17 AWXA960541 1 19960930 A 2530 OVEN BOEING 757 7572S7 1384962 NM GALLEY DIRTY A AWXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 28 905AW 23567 PHX - FLT 25 - INBOARD OVEN IN FORWARD GALLEY PRODUCED SMOKE WHEN TURNED ON TO HEAT MEALS. CLEANED FOIL FROM OVEN. OPE RATES GOOD. (M) 2 L 7 2 4F RT A2NM 1996101700716 19961017 00716 NM 1996 10 17 AWXA960538 1 19960914 A 5315 FLOOR BEAM BOEING 757 7572S7 1384962 NM BS 377.7 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 904AW 23566 PAE - FLT 7803 - DURING ROUTINE SCHEDULED C-4 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM STATION 377.7, LBL 6-65. REMOVED DAMAGE AND REPAIRED FLOOR BEAM BY SPLICING IN A NEW TOP CHORD, IAW 53-00-51. (M) 2 L 7 2 4F RT A2NM 1996101700717 19961017 00717 NM 1996 10 17 AWXA960537 1 19960916 A 5315 FLOOR BEAM BOEING 757 7572S7 1384962 NM BS 365.5 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 904AW 23566 PAE - FLT 7803 - DURING ROUTINE SCHEDULED C-4 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM BS 365.25, RBL 30 RBL 65. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED NEW UPPER CHORD, IAW 53-00-51. (M) 2 L 7 2 4F RT A2NM 1996101700718 19961017 00718 EU 1996 10 17 AWXA960519 1 19960919 A 3397 WIRE AIRBUS 320 A320231 3930325 EU CABIN BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 303ML 304 LAS - FLT 365 - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PROX LIGHTING INOP AT ROW 11R. WIRES PULLED FROM LIGHT. R EPAIRED WIRING. (M) 2 L 7 2 4F RT A28NM 1996101700719 19961017 00719 NM 1996 10 17 AWXA960514 1 19960918 A 3397 WIRE BOEING 737 737277 1384570 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 182AW 22649 PHX - FLT 2517 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT AT ROW 11 HAS BROKEN WIRES AND IS INOP. REPAIR ED WIRING. OPERATED OK. (M) 2 L 7 2 4F RT A16WE 1996101700720 19961017 00720 NM 1996 10 17 AWXA960513 1 19960918 A 3350 900542 POWER SUPPLY BOEING 737 7372M8 1384483 NM CABIN INOP A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 141AW 5245 21955 PHX - FLT 2622 - DURING ROUTINE MAINTENANCE CHECK, FOUND RIGHT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED MID RIGHT EMERGENCY LIGHT POWER SUPPLY. OPERATES NORMALLY. (M) 2 L 7 2 4F A16WE 1996101700721 19961017 00721 NM 1996 10 17 AWXA960533 1 19960927 A 3350 900835A BATTERY PACK BOEING 737 7372M8 1384483 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 141AW 23334 21955 PHX - FLT 2622 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY FLOOR LIGHT SIGNS AT R1, L1 AND RIGHT OVERWING INOP. REMOVED AND REPLACED BATTERY PACK M1050. OPS CHECKED GOOD. (M) 2 L 7 2 4F A16WE 1996101700722 19961017 00722 NM 1996 10 17 AWXA960521 1 19960921 A 3350 CONNECTOR BOEING 737 7372M8 1384483 NM CABIN SHORTED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 141AW 21955 PHX - FLT 2267 - DURING ROUTINE MAINTENANCE CHECK, FOUND RIGHT EMERGENCY EXIT AFT VERTICAL EXIT LIGHT INOP. FOUND POWER CONNECTOR SHORTING ON A/C FRAME. REPLACED HEATSHRINK WRAP AND SECURED. (M) 2 L 7 2 4F A16WE 1996101700723 19961017 00723 NM 1996 10 17 AWXA960522 1 19960921 A 3350 849029 BATTERY BOEING 737 7373G7 1384595 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 157AW 4451 23779 PHX - FLT 1258 - DURING ROUTINE MAINTENANCE CHECK, FOUND INTERIOR EMERGENCY LIGHTS INOP NEAR LEFT EMERGENCY EXIT. REPLA CED BATTERY ASSEMBLY FOR THAT AREA. LIGHTS OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996101700724 19961017 00724 NM 1996 10 17 AWXA960523 1 19960921 A 3397 WIRE BOEING 737 7373G7 1384595 NM CABIN DISCONNECTED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 155AW 23777 PHX - FLT 2539 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT BOTTLE CAP MISSING FROM ROW 3 (C). CONNECTED W IRING FOR EMERGENCY LIGHT AT SEAT 3C, F/C GOOD. (M) 2 L 7 2 4F RT A16WE 1996101700725 19961017 00725 NM 1996 10 17 AWXA960524 1 19960922 A 3397 WIRE BOEING 737 7373G7 1384595 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 157AW 23779 PHX - FLT 220 - DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 5 EMERGENCY EXIT LIGHT INOP. SPLICED BROKEN EMERGENCY EXIT LIGHT WIRING AT ROW 5. OPERATIONS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 1996101700726 19961017 00726 EU 1996 10 17 AWXA960511 1 19960913 A 3350 321454 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 624AW 434 55 PHX - FLT 2051 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS INOP AT SEATS 13, 17, 19 AND 24. BULLNOSE LIG HTS INOP AT ROW 19 AND 2. ALL SIGNS INOP IN AFT GALLEY. SYSTEM TEST FAILS LEFT AFT UNIT. REMOVED AND REPLACED EMERGEN CY POWER SUPPLY UNIT. (M) 2 L 7 2 4F RT A28NM 1996101700727 19961017 00727 EU 1996 10 17 AWXA960512 1 19960916 A 3350 321430 BATTERY PACK AIRBUS 320 A320231 3930325 EU CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 643AW 9493 315 PHX - FLT 2540 - DURING ROUTINE MAINTENANCE CHECK, FOUND MISCELLANEOUS EMERGENCY EXIT LIGHTS INOP AT MID-CABIN, OVERWING AND AISLE LIGHTS. REMOVED AND REPLACED BATTERY PACK ON AIRCRAFT RIGHT, MID-CABIN, PER MM 33-51-48, PG 410. (M) 2 L 7 2 4F RT A28NM 1996101700728 19961017 00728 NM 1996 10 17 AWXA960526 1 19960923 A 3350 CONNECTOR BOEING 757 7572G7 1384963 NM CABIN LOOSE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 909AW 24522 PHX - FLT 2016 - DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 5 EMERGENCY EXIT LIGHTS ON SEAT INOP PLACED ON MEL 33-51-03 . REF MEL 33-51-01 RE-SEATED CONNECTOR PIN ON HARNESS AT ROW 5 EMERGENCY LIGHTS CHECK OK MEL REMOVED. (M) 2 L 7 2 4F RT A2NM 1996101700729 19961017 00729 NM 1996 10 17 EISA96186 1 19960928 A 5311 FRAME BOEING 727 727223 1384074 NM BS 440 PUNCTURED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING A SCHEDULED D-CHECK, FOUND A HOLE IN THE RADIUS AND 1 INCH GOUGE IN FRAME STATION 440 STRINGER 16R. REPAIRED PER SRM 51-40-4. (M) 2 L 7 3 4F A3WE 1996101700730 19961017 00730 NM 1996 10 17 USAA960645 1 19960927 A 5320 STUB BEAM BOEING 737 737201 1384454 NM BS 578 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 224US 47115 21666 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK STATION 578 STUB BEAM WEB LBL 61.5 TO LBL 62.5, WL 207.5. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2. (M) 2 L 7 2 4F A16WE 1996101700731 19961017 00731 NM 1996 10 17 USAA960644 1 19960927 A 5311 FRAME BOEING 737 737201 1384454 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 224US 47115 21666 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 4 INCH LONG CRACK STATION 747 STRINGER 19 L CIRCUMFERENTIAL FRAME. INST ALLED DOUBLERS, REPAIRED PER SRM 53-10-4. (M) 2 L 7 2 4F A16WE 1996101700732 19961017 00732 NM 1996 10 17 USAA960643 1 19960927 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 363-500 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 224US 47115 21666 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION ON STRINGER 1 INCH BY 3 INCH SECTION AROUND RIVETS, BS 363 TO BS 500 PLUS 13 INCHES. REPLACED STRINGER SECTION, REPAIRED PER SRM 53-10-3 FIG 3 SHEET 2 TABLE 1. CORROSION TASK NR C5 3-107-01, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996101700733 19961017 00733 NM 1996 10 17 USAA960642 1 19960927 A 5315 FLOOR BEAM BOEING 737 737201 1384454 NM BS 675 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 224US 47115 21666 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1.25 INCH CRACK BS 675 WL 202.5 LONGITUDINAL FLOOR BEAM LOWER CHORD. IN STALLED REINFORCING ANGLE/SPLICE, REPAIRED PER EA 41578. (M) 2 L 7 2 4F A16WE 1996101700734 19961017 00734 NM 1996 10 17 USAA960641 1 19960927 A 5315 FLOOR BEAM BOEING 737 737201 1384454 NM BS 695 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 224US 47115 21666 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK RBL 45 LONG FLOOR BEAM LOWER CHORD STATION 695 WL 202.5. INSTALLED REPAIR ANGLE, REPAIRED PER EA 41557. (M) 2 L 7 2 4F A16WE 1996101700735 19961017 00735 NM 1996 10 17 USAASB96202 1 19960928 A 3610 1074922 BLEED AIR REG BOEING 737 7374B7 1384702 NM NR 1 ENG FAILED A A USAA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 EA 19 431US 17734 24553 PHX - FL 152 - AIRCRAFT WAS CLIMBING THROUGH 8,000 FEET WHEN THE FLIGHT EXPERIENCED NR 1 ENGINE BLEED VALVE FAILURE. CR EW RECEIVED NO INDICATIONS BY WAY OF WARNING LIGHTS. CAPTAIN WENT THROUGH CHECKS AND PROCEDURES WITH NO HELP TO CORRECT THE PROBLEM. CAPTIAN THEN MADE DECISION TO RETURN TO FIELD AT PHX. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WI TH NO FURTHER INCIDENT. MX TESTED SYSTEM PER MM WITH PNEUMATIC TEST SET AND FOUND THE NR 1 ENGINE BLEED AIR REGULATOR H AD FAILED. REPLACED SAME. RAN SYS AT VARIOUS POWER SETTINGS. PNEUMATIC SYS CHECKED GOOD. 2 L 7 2 4F RT A16WE 1996101700736 19961017 00736 NM 1996 10 17 USAA960635 1 19960927 A 5315 6546811 FLOOR BEAM BOEING 737 7374B7 1384702 NM BS 986.5 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 19672 24557 CLT - INSPECTION VISUALLY FOUND .5 INCH BY .5 INCH LEVEL 2 CORRODED AREA AT CLIP NUT HOLES LOCATED AT FLOOR BEAM STATION NR 986.5, LBBL 45 - RBBL 45. INSTALLED REPLACEMENT T-CAP AND SPLICE ANGLES PER USAIR EA NR 58809. CORROSION TASK NR C 53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996101700737 19961017 00737 NM 1996 10 17 USAASB96203 1 19960930 A 2613 65528083A OVERHEAT MODULE BOEING 737 737301 1384611 NM F/E COMPARTMENT FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 576US 12018 23741 PIT - FL 133 - LEFT WING BODY OVERHEAT LIGHT ILLUMINATED ON TAKEOFF AND REMAINED ON IN CLIMB. CAPTAIN TURNED OFF LEFT B LEED SWITCH BUT LIGHT REMAINED ON. AT 10,000 FEET, CAPTAIN ELECTED TO RETURN TO FIELD AT PIT. ON DESCENT, LIGHT WENT O UT BUT ON FINAL APPROACH WHEN POWER WAS APPLIED, LIGHT ILLUMINATED AGAIN. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MX C HECKED SYSTEM FOR BLEED LEAKS AND CONDITION OF LOOPS. TROUBLESHOT SYSTEM PER MM 26-18-00 TO A FAULTY M237 OVERHEAD MODU LE. REPLACED SAME. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 1996101700738 19961017 00738 NM 1996 10 17 USAA960632 1 19960926 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 437US 19323 24559 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO .375 INCH CRACKS STATION 178 PRESSURE BULKHEAD RBL 4.75 INCH, ONE AT 6 INCHES BELOW FLOOR LEVEL AND ONE AT 8.5 INCHES BELOW FLOOR LEVEL. INSTALLED FILLER AND DOUBLER. REPAIRED PER TR 53- 10-07. (M) 2 L 7 2 4F RT A16WE 1996101700739 19961017 00739 NM 1996 10 17 USAA960659 1 19960927 A 5320 BEAM BOEING 737 737201 1384454 NM BS 706 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 37764 22757 ROA - DURING BX CHECK VISUAL CONFIRMED WITH HFEC INSPECTION, FOUND .5 INCH CRACK BS 706 STRINGER 18A SHEAR BEAM WEB, LEF T. INSTALLED DOUBLER REPAIR, REPAIRED PER EO 5393G256 PART 3 SECTION IV PRIOR TO REV FLIGHT. (M) 2 L 7 2 4F A16WE 1996101700740 19961017 00740 NM 1996 10 17 USAASB96200 1 19960917 A 3350 900835A BATTERY PACK BOEING 737 737201 1384454 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 232US 22018 PHL - MAINTENANCE FOUND THE OVERHEAD EMERGENCY EXIT IDENTIFIER LIGHT INOP AT ROW 2. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1996101700741 19961017 00741 EU 1996 10 17 RAIA960934 1 19960926 A 5280 SP4954 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU CARGO DOOR OUT OF ADJUST A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 561HK 1541 41077 DCA - FLT 7738 - MAIN BAGGAGE DOOR WARNING ILLUMINATED. MAINTENANCE ADJUSTED THE FORWARD MICRO-SWITCH. (M) 2 L 7 2 4T RT A41NM 1996101700742 19961017 00742 1996 10 17 RAIA960933 4 19960926 A 3421 7001182902 ADI INDICATOR BAG JETSTM JETSTM3201 1500217 EU LT INSTR PNL FAILED A RAIA A UNSCHED LANDING I FLT. ATTITUDE INST. CL CLIMB 1 CE 03 426AM 8702 874 STL - FLT 7029 - CAPTAINS ADI FELL OFF LINE. MAINTENANCE REPLACED THE ADI INDICATOR. (M) 2 L 7 2 4T RT A56EU 1996101700743 19961017 00743 EU 1996 10 17 RAIA960932 1 19960925 A 2435 8260121 STARTER/GEN AEROSP ATR42 ATR42300 8680920 EU LT ENGINE FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 421TE 9050 102 STL - FLT 7400 - LEFT DC GENERATOR FAULTED, AND WOULD NOT RESET. MAINTENANCE REPLACED THE LEFT STARTER/GENERATOR. (M) 2 H 7 2 4T RT A53EU 1996101700744 19961017 00744 WP 1996 10 17 RAIA960928 2 19960921 A 7320 31081961 P3 GASKETS BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT ENGINE LEAKS A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 866AE 300 866 P66036 FAT - FLT 4782 - LEFT ENGINE UNABLE TO PRODUCE TARGET TORQUE. MAINTENANCE REPLACED THE LEFT ENGINE P3 GASKETS. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996101700745 19961017 00745 EU 1996 10 17 RAIA960927 1 19960921 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 EICBK 5519 199 STL - FLT 7142 - THE MIDDLE CABIN EMERGENCY EXIT LIGHTS ARE INOP. MAINTENANCE REPLACED THE NR 3 EMERGENCY BATTERY PACK. (M) 2 H 7 2 4T RT A53EU 1996101700746 19961017 00746 EU 1996 10 17 RAIA960930 1 19960922 A 2910 1379305A77 HOSE BAG JETSTM JETSTM3201 1500217 EU NR 1 PUMP LEAKING A RAIA O OTHER K FLUID LOSS DE DESCENT 1 CE 03 864AE 11430 864 LAX - FLT 4757 - LOST LEFT HYDRAULIC PRESSURE AND RIGHT PRESSURE FLUCTUATING. REPLACE LEFT HYDRAULIC HOSE. (M) 2 L 7 2 4T RT A56EU 1996101700747 19961017 00747 EU 1996 10 17 RAIA960929 1 19960919 A 2120 F1897P05 DUCT BAG JETSTM JETSTM3201 1500217 EU NR 2 ACM LEAKING A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 342TE 8680 954 STL - FLT 7061 - AIRCRAFT WOULD NOT PRESSURIZE, RIGHT FLOW WEAK. REPAIRED ACM DUCT. (M) 2 L 7 2 4T RT A56EU 1996101700748 19961017 00748 EU 1996 10 17 RAIA960926 1 19960921 A 3350 3011079 LIGHT AEROSP ATR42 ATR42300 8680920 EU PAX DOOR INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 425TE 125 STL - FLT 7943 - EMERGENCY EXIT LIGHT IN PASSENGER DOOR IS INOP. MAINTENANCE CLEANED CORROSION FROM THE EMERGENCY EXIT LIGHT SOCKET. (M) 2 H 7 2 4T RT A53EU 1996101700749 19961017 00749 EU 1996 10 17 RAIA960925 1 19960921 A 3350 3012001 BATTERY PACK AEROSP ATR72 ATR72202 8680940 EU CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 723TE 2256 283 STL - FLT 7121 - AFT HALF OF THE EMERGENCY PATH LIGHTING IS INOP. MAINTENANCE REPLACED THE AFT EMERGENCY BATTERY PACK. (M) 2 H 7 2 4T RT A53EU 1996101700750 19961017 00750 EU 1996 10 17 RAIA960924 1 19960922 A 7722 CA3108R12S3SF80 T2 CONNECTOR BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RT ENGINE SHORTED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 424AM 12033 865 STL - FLT 7029 - RIGHT ENGINE EGT FLUCTUATES. MAINTENANCE REPLACED THE RIGHT T2 CANNON PLUG. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996101700751 19961017 00751 EU 1996 10 17 RAIA960923 1 19960919 A 3241 AH084357 SHUTTLE VLV BAG JETSTM JETSTM3201 1500217 EU RT MLG LEAKS A RAIA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 CE 03 423AM 12083 858 STL - FLT 7109 - RIGHT MAIN WHEEL HAS BRAKE FLUID LEAKING FROM OUTER HUB. HARD TO MAKE RIGHT TURNS WITH BRAKE PEDALS DE PRESSED. MAINTENANCE REPLACED THE RIGHT ANTI-SKID SHUTTLE VALVE. (M) 2 L 7 2 4T RT A56EU 1996101700752 19961017 00752 EU 1996 10 17 RAIA960922 1 19960920 A 2435 23095002 STARTER/GEN JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE FAILED A RAIA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 CE 03 564HK 1093 41081 STL - FLT 7478 - DURING START OF LEFT ENGINE, THE STARTER CAUGHT ON FIRE. MAINTENANCE INSPECTED THE LEFT ENGINE AND REP LACED THE LEFT STARTER/GENERATOR. NO OTHER DEFECTS NOTED. (M) 2 L 7 2 4T RT A41NM 1996101700753 19961017 00753 EU 1996 10 17 RAIA960921 1 19960918 A 3241 AC63740 MAXARETT BAG JETSTM JETSTM3201 1500217 EU RT MAIN BYPASSING A RAIA K NONE O OTHER TX TAXI/GRND HDL 1 CE 03 423AM 8937 858 STL - FLT 7327 - LEFT BRAKE IS ENGAGING FASTER THAN RIGHT BRAKE. MAINTENANCE REPLACED THE RIGHT ANTI-SKID MAXARETT. (M ) 2 L 7 2 4T RT A56EU 1996101700754 19961017 00754 EU 1996 10 17 RAIA960920 1 19960919 A 2435 23095002 STARTER/GEN JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE LOOSE LUG A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 559HK 41075 ORF - FLT 7758 - RIGHT GENERATOR FELL OFF LINE. MAINTENANCE TIGHTENED TERMINAL LUG 'E' ON THE RIGHT STARTER GENERATOR. (M) 2 L 7 2 4T RT A41NM 1996101700755 19961017 00755 EU 1996 10 17 RAIA960919 1 19960919 A 7797 KR40AL WIRE BAG JETSTM JETSTM3201 1500217 EU LT ENGINE LOOSE A RAIA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 CE 03 973JX 973 SMF - FLT 4755 - SHUTDOWN LEFT ENGINE DUE TO EGT SPIKES TO 700 DEGREES CELSIUS WITH ASSOCIATED TORQUE REDUCTIONS. MAINT ENANCE REPAIRED WIRE KR40AL TO LEFT ENGINE EGT RAKE. PERFORMED ENGINE RUNS, OPS CHECK GOOD. (M) 2 L 7 2 4T RT A56EU 1996101700756 19961017 00756 EU 1996 10 17 RAIA960918 1 19960919 A 3350 8GS00599705 BULB JETAIR JETSTM JETSTM4101 1500501 EU CABIN FAILED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 566HK 41084 STL - FLT 7442 - THE AFT EMERGENCY EXIT LIGHT IS INOP. MAINTENANCE REPLACED THE AFT EMERGENCY EXIT LIGHT BULB. (M) 2 L 7 2 4T RT A41NM 1996101700757 19961017 00757 EU 1996 10 17 RAIA960917 1 19960919 A 2612 51224127 FIRE LOOP BAG JETSTM JETSTM3201 1500217 EU RT ENGINE MALFUNCTIONED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 339TE 11344 935 PAH - FLT 7361 - RIGHT ENGINE FIRE DETECT LIGHT ILLUMINATED AT 80 PERCENT TQ. WHEN THE POWER WAS DROPPED BELOW 80 PERCE NT TORQUE THE LIGHT EXTINGUISHED. MAINTENANCE REPLACED THE RIGHT ENGINE FIRE LOOP. (M) 2 L 7 2 4T RT A56EU 1996101700758 19961017 00758 EU 1996 10 17 RAIA960916 1 19960918 A 2611 FR3222 SMOKE DETECTOR AEROSP ATR72 ATR72202 8680940 EU CARGO COMPT FAILED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 723TE 11037 283 STL - FLT 7164 - AFT SMOKE DETECTOR WILL NOT TEST. MAINTENANCE REPLACED THE AFT SMOKE DETECTOR. (M) 2 H 7 2 4T RT A53EU 1996101700759 19961017 00759 EU 1996 10 17 RAIA960915 1 19960918 A 3350 311701 BATTERY PACK BAG JETSTM JETSTM3201 1500217 EU CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 430AM 5278 880 STL - FLT 7412 - EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE FORWARD AND AFT EMERGENCY BATTERY PACKS. (M) 2 L 7 2 4T RT A56EU 1996101700760 19961017 00760 EU 1996 10 17 RAIA960914 1 19960917 A 7722 EGT CONNECTOR BAG JETSTM JETSTM3201 1500217 EU RT ENGINE DIRTY A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 424AM 865 BMI - FLT 7327 - RIGHT EGT FLUCTUATES WITH SRL ON, SRL OFF EGT STABILIZES. MAINTENANCE CLEANED T2 CANNON PLUG AND PERFO RMED TROUBLE SHOOTING, COULD NOT DUPLICATE. (M) 2 L 7 2 4T RT A56EU 1996101700761 19961017 00761 WP 1996 10 17 RAIA960913 2 19960917 A 7320 31081961 P3 GASKETS BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RT ENGINE LEAKING A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 429AM 300 879 P66128 STL - FLT 7342 - RIGHT BETA LIGHT ILLUMINATED AND WOULD NOT EXTINGUISH. MAINTENANCE REPLACED THE RIGHT ENGINE P3 GASKET S. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996101700762 19961017 00762 EU 1996 10 17 RAIA960912 1 19960911 A 2611 72111211000 SMOKE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU POD DIRTY A RAIA O OTHER N FALSE WARNING DE DESCENT 1 CE 03 550HK 3691 41039 ORF - FLT 7755 - POD SMOKE LIGHT CAME ON DURING DESCENT, AFTER TOUCHDOWN LIGHT WENT OUT. MAINTENANCE CLEANED CONNECTOR ON SMOKE DETECTOR. (M) 2 L 7 2 4T RT A41NM 1996101700763 19961017 00763 SW 1996 10 17 BSAA083196 1 19960830 A 2430 GROUND WIRE SWRNGN SA226 SA226TC 8780404 SW LEFT LOOSE A BSAA O OTHER J WARNING INDICATION CL CLIMB 1 NM 05 101GS TC267 BATTERIES TRIPPED OFF LINE AND WERE HARD TO RESET. AIRCRAFT FERRIED BACK TO BIL TO INVESTIGATE PROBLEM. CREW REPORTED NO PROBLEMS ON RETURN FLIGHT. FOUND LEFT GROUND IN THE WHEELWELL FOR THE LEFT BATTERY AND GENERATOR HAD INDICATIONS OF A POOR GROUND CONNECTION WHEN DISASSEMBLED. NO OTHER VISUAL INDICATIONS WERE NOTED. GROUND RUN AND FLIGHT OPERATIONAL CHECK OK AFTER CLEANING GROUND CONNECTION. (M) 2 L 7 2 4T RT A8SW 1996101700764 19961017 00764 WP 1996 10 17 BSAA082396 2 19960823 A 7250 8650821 NUT SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110 01514 WP TURBINE BROKEN A BSAA K NONE O OTHER IN INSP/MAINT 1 NM 05 115BS TC324 GDV - ENGINE HARD TO PULL THROUGHT AND NOISEY. FOUND AFT TURBINE NUT (P/N 865082-1) BROKEN ALLOWING TURBINE RUB. PERFO RMED COMPLETE ENGINE TEARDOWN AND INSPECTION FOR DAMAGE. PARTS WILL BE REPLACED AS REQUIRED AND MAINTENANCE CHECKS COMP LETED. (M) 2 L 7 2 4T 4 T RT A8SW E4WE 1996101700765 19961017 00765 SW 1996 10 17 BSAA082296 1 19960822 A 2430 50284001 FAULT PANEL SWRNGN SA226 SA226TC 8780404 SW COCKPIT FAILED A BSAA O OTHER S AFFECT SYSTEMS CL CLIMB 1 NM 05 101GS TC267 SDY - BATTERY FAULT CAME ON AND WOULD NOT RESET IN THE AIR. RESET ON THE GROUND. STATIC FEEDER FAULT PANEL. REPLACED FAULT PROTECTINO PANEL, GROUND OPS OK. (M) 2 L 7 2 4T RT A8SW 1996101700766 19961017 00766 SW 1996 10 17 BSAA081996 1 19960816 A 7712 TQ INDICATOR SWRNGN SA226 SA226TC 8780404 SW RIGHT FAILED A BSAA O OTHER O OTHER CL CLIMB 1 NM 05 115BS TC324 BIL-OLF - RIGHT TORQUE INDICATION BECAME ERRATIC. TORQUE INDICATOR FAILING. REPLACED RIGHT TORQUE INDICATOR, SETUP, AN D OPERATIONAL CHECKED OK. RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A8SW 1996101700767 19961017 00767 1996 10 17 BSAA092096 4 19960923 A 6122 89361513 PROP GOVERNOR SWRNGN SA226 SA226TC 8780404 SW RT ENGINE FAILED A BSAA K NONE O OTHER IN INSP/MAINT 1 NM 05 101GS TC267 BIL - RIGHT ENGINE LOW TORQUE. PROP GOVERNOR STICKING ALLOWING ENGINE RPM TO GO TOO HIGH. INSTALLED SERVICEABLE PROP G OVERNOR, GROUND RUN CHECKED OK. PERFORMED FLIGHT TEST AND NTS SHUTDOWN. RELEASED TO SERVICE. (M) 2 L 7 2 4T RT A8SW 1996101700768 19961017 00768 NM 1996 10 17 HNAA9692468 1 19960929 A 3234 574205 SELECTOR VALVE DHAV DHC8 DHC8102 2809003 NM LANDING GEAR FAILED A HNAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 07 924HA 12621 12621 85 105 FLT 3444 - TLH - TPA - ON APPROACH INTO TPA, THE LANDING GEAR WAS SELECTED DOWN, NO RESPONSE. THREE RED LIGHTS AND HAND LE LIGHT ILLUMINATED. THE CREW CYCLED THE GEAR HANDLE AND THE GEAR CAME DOWN. AIRCRAFT LANDED IN TPA WITHOUT INCIDENT. REMOVED AND REPLACED THE LANDING GEAR SELECTOR VALVE. (M) 2 H 7 2 4T RT A13NM 1996101700769 19961017 00769 WP 1996 10 17 HALA96139 1 19960923 A 2612 FIRE LOOP DOUG DC10 DC1010 3022110 WP NR 1 ENGINE MALFUNCTIONED A HALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 13 161AA 46942 HNL - FLT 921 - NR 1 ENGINE FIRE HANDLE DOES NOT TEST. (LIGHT DOES NOT ILLUMINATE). FOUND NR 1 ENGINE 'B' LOOP INOP. R EPLACED NR 1 ENGINE FIREWARNING B-LOOP PER THE MM. THE OPERATIONAL CHECK WAS GOOD. (M) 2 L 7 3 4F A22WE 1996101700770 19961017 00770 NM 1996 10 17 MALA965148 1 19960924 A 3260 DNLOCK SENSOR DHAV DHC8 DHC8102 2809003 NM LT MLG BROKEN WIRE A MALA O OTHER N FALSE WARNING AP APPROACH 1 GL 15 861MA 362 FLT 3461 - ON APPROACH TO DTW, THE LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR EXTENSION. THE CREW PERFORMED AN ALTERNATE EXTENSION. THE UNSAFE LIGHT REMAINED ON BUT THE GEAR WAS VERIFIED TO BE SAFE THROUGH IN INFRARED SYSTEM. MAINTENANCE REPAIRED A BROKEN WIRE ON THE DOWN LOCK SENSOR. ALL CHECKS SATISFACTORY. (M) 2 H 7 2 4T RT A13NM 1996101700771 19961017 00771 NM 1996 10 17 MALA965147 1 19960920 A 3231 DOOR MECHANISM DHAV DHC8 DHC8102 2809003 NM LT/RT MLG WORN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 848MA 346 DURING A SCHEDULED INSPECTION IN DTW, THE LEFT AND RIGHT MAIN LANDING GEAR DOOR SPRINGS AND BUSHINGS WERE WORN. THE RIG HT AND LEFT MAIN LANDING GEAR DOOR SPRINGS AND BUSHINGS WERE REPLACED. (M) 2 H 7 2 4T RT A13NM 1996101700772 19961017 00772 SW 1996 10 17 MALA965146 1 19960923 A 3260 1EN516 POSITION SWITCH SWRNGN SA227 SA227AC 8780603 SW RT MLG FAILED A MALA O OTHER N FALSE WARNING AP APPROACH 1 GL 15 436MA AC719B FLT 3049 - ON APPROACH TO MSP, THE RIGHT GEAR INTRANSIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE RIG HT MLG DOWN POSITION SWITCH. ALL CHECKS SATISFACTORY. (M) 2 L 7 2 4T RT A8SW 1996101700773 19961017 00773 SW 1996 10 17 MALA965145 1 19960924 A 5512 SKIN SWRNGN SA227 SA227AC 8780603 SW RT HORIZ STAB CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 863MA AC650B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND ON RIGHT HORIZONTAL STABILIZER LOWER SKIN JUST OUTBOARD OF BL 72 .43 AT LOCATION OF PREVIOUS REPAIR, A 3.5 INCH HORIZONTAL CRACK. REMOVED PREVIOUS REPAIR AND EXAMINED PREVIOUS DAMAGE A ND FOUND A 1.5 INCH CRACK, TOTAL CRACK LENGTH IS 5 INCHES. FABRICATED AND INSTALLED A SURFACE REPAIR DOUBLER, 8.5 INCH BY 7 INCH, ONTO LOWER SKIN IAW FAC SRM 55-90-10 PGS 21-23, REV NOV 5/93. (M) 2 L 7 2 4T RT A8SW 1996101700774 19961017 00774 NM 1996 10 17 MALA965143 1 19960921 A 3350 6104789 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 827MA 331 FLT 3140 - DURING THE PREFLIGHT INSPECTION IN DTW, THE CREW FOUND THE TWO MOST AFT AND ONE MOST FORWARD FLOOR TRACK LIGH TS TO BE INOPERATIVE. MAINTENANCE REPLACED THE RIGHT FORWARD AND LEFT AFT BATTERY PACKS. ALL CHECKS SATISFACTORY. (M) 2 H 7 2 4T RT A13NM 1996101700775 19961017 00775 NM 1996 10 17 MZZA96073 1 19960903 A 3350 EXIT SIGN BOEING 727 727212 138407G NM CABIN BROKEN A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 86430 21947 TNN - DURING 1/2 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, BROKEN COVER WAS FOUND ON FORWARD GALLEY 'EXIT' SIGN COVER. THE DAMAGED 'EXIT' SIGN ASSEMBLY WAS REMOVED AND REPLACED WITH BR9279-103 ASSEMBLY PER B727 MM 33-50-11 AND OPERATIONA L CHECK FOUND SATISFACTORY. REF HANGAR NON ROUTINE REPAIR ITEM CARD NR 803479 9SEQ NR 02199). (M) 2 L 7 3 4F A3WE 1996101700776 19961017 00776 NM 1996 10 17 MZZA96074 1 19960909 A 3350 EXIT SIGN BOEING 727 727212 138407G NM CABIN BROKEN A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 86430 21947 TNN - DURING 1/2 D-CHECK INSPECT ON A/C AT AIR ASIA, BROKEN COVER WAS FOUND ON PASSENGER CABIN AT THE FOLLOWING POSITION 'EXIT' SIGN COVER; R2 CABIN DOOR, R1 CABIN DOOR, RT FORWARD EMERGENCY EXIT DOOR. THE DAMAGED 'EXIT' SIGN ASSEMBLIES WE RE REMOVED AND REPLACED WITH BR9279-106 ASSEMBLIES PER B727 MM 33-50-11 AND OPERATIONAL CHECK FOUND SATISFACTORY. REF H ANGAR NON ROUTINE REPAIR ITEM CARD NR 803487, 803485 AND 803480 (SEQ NR 02217, 02215 AND 0220). (M) 2 L 7 3 4F A3WE 1996101700777 19961017 00777 NM 1996 10 17 TSAA9655077 1 19960927 A 5511 SPAR BOEING 737 7372S2C 138448G NM RT HORIZ STAB RT CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 806AL 21927 DURING C-CHECK VISIT, FOUND CORROSIN RIGHT HORIZONTAL REAR SPAR UPPER CHORD FORWARD FLANGE. REPAIRED PER ECO 2746. AIR CRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1996101700778 19961017 00778 WP 1996 10 17 USAAD96131 1 19960924 A 3350 P4010020 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 984VJ 47207 GALLEY DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK. (M) 2 L 7 2 4F A6WE 1996101700779 19961017 00779 NM 1996 10 17 USAASB96199 1 19960921 A 3350 AD20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 520AU 23706 ROC - MAINTENANCE FOUND THE AFT CABIN EMERGENCY LIGHTS INOP. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK. OP S CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996101700780 19961017 00780 WP 1996 10 17 USAA960628 1 19960923 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 354 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 931VJ 74051 47188 PIT - DURING C-2 CHECK, FOUND .5 INCH CRACK IN FUSELAGE SKIN AT STATION 354 LONGERON 6L. CUT OUT CRACKED AREA, INSTALLE D A FILLER AND AN EXTERNAL DOUBLER WITH BLIND FASTENERS PER SRM 53-04 FIG 12B SHEET 16 (CLASS III REPAIR). (M) 2 L 7 2 4F A6WE 1996101700781 19961017 00781 WP 1996 10 17 USAA960627 1 19960923 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 658 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 931VJ 74051 47188 PIT - DURING C-2 CHECK, FOUND .4375 INCH CRACK IN FUSELAGE SKIN AT STATION 658 BETWEEN R1 AND R2. DETECTED BY EDDY CURR ENT. CUT OUT CRACKED AREA. INSTALLED A FILLER AND AN EXTERNAL DOUBLER WITH BLIND FASTENER PER SRM 53-04 FIG 12B SHEET 16 (CLASS II REPAIR). (M) 2 L 7 2 4F A6WE 1996101700782 19961017 00782 WP 1996 10 17 USAA960626 1 19960927 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 1474 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 830US 27804 49443 PIT - DURING Q-2 CHECK, FOUND RIGHT AFT RIGHT VERT STAB ATTACH ANGLE CRACKED AT STATION 1474. INSTALLED DOUBLER PER SRM 53-05 FIG 23A. (M) 2 L 7 2 4F A6WE 1996101700783 19961017 00783 NE 1996 10 17 HEEA968054 1 19961003 A 6210 7615009100051A BLADE SKRSKY S76 S76A 8143006 NE M/R DEFECTIVE E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 11694 BLADE HAS THE TIP RIB OUT OF LINE. TIP CAP DOES NOT FIT. 1 G 7 2 3U H1NE 1996101700784 19961017 00784 NE 1996 10 17 HEEA968055 1 19961003 A 6410 7610105101041 BLADE SKRSKY S76 S76A 8143006 NE T/R CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22342 9674 760096 BLADE IS CORRODED. (PRIMARY POLYURETHANE RUBBERS ERRODED AND THE BOX BEAM HAS AN EXCESSIVE AMOUNT OF CORROSION.) 1 G 7 2 3U H1NE 1996101700785 19961017 00785 EU 1996 10 17 HEEA968056 1 19961003 A 2435 150SG122Q STARTER SNIAS 350 AS350B2 8680813 EU START/GEN FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 956 2771 STARTER ARCS BADLY AND TURNS SLOW. 1 G 7 1 3U H9EU 1996101700786 19961017 00786 EU 1996 10 17 HEEA968057 1 19961003 A 6210 10515141 BLADE BOLKMS 105 BO105S 5626006 EU M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5031U 10638 S678 BLADE IS CRACKED. (BLADE HAS NOSE AND NECK SHELLS CRACKED AND SEPARATED. THE INBOARD LEADING EDGE STRIP IS SEPARATED O N THE INBOARD END BEYOND LIMITS. THE NO. 2 CENTER STRIP HAS SMALL AREAS OF SEPARATION. 1 G 7 2 3U H3EU 1996101700787 19961017 00787 SW 1996 10 17 HEEA968058 1 19961003 A 7722 206375007103 INDICATOR BELL 206 206L3 1182108 SW COCKPIT TOT STICKS E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 31077 51520 NEEDLE INTERMITTENTLY STICKS AT ZERO. SENT TO MASCO FOR INSPECTION AND REPAIR. 1 G 7 1 3U H2SW 1996101700788 19961017 00788 NE 1996 10 17 HEEA968059 1 19961003 A 6410 7610105101041 BLADE SKRSKY S76 S76A 8143006 NE T/R SEPARATION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22342 9979 760096 BLADE HAS SEPARATION ON PADDLE "A" ON THE OUTBOARD SIDE IN THE AIRFOIL REGION. THE ABRASION STRIP IS ALSO CRACKED WITH SMALL AMOUNT OF SEPARATION. SENT TO COMPOSITE TECHNICS FOR INSPECTION AND REPAIR. 1 G 7 2 3U H1NE 1996101700789 19961017 00789 1996 10 17 HEEA968060 4 19961003 A 2370 9806019001 CVR BELL 412 412 1182202 SW COCKPIT INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 108X 33115 CVR INOPERATIVE. 1 G 7 2 4U H4SW 1996101700790 19961017 00790 EU 1996 10 17 HEEA968061 1 19961003 A 6310 4638202007 CLUTCH 4638001004 BOLKMS 105 BO105S 5626006 EU FREEWHEEL BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7136H 4144 1070 S833 CLUTCH INNER CAGE BROKEN. REPLACED WITH SERVICEABLE CLUTCH 1 G 7 2 3U H3EU 1996101700791 19961017 00791 SW 1996 10 17 HEEA968062 1 19961003 A 6320 206040030003 BEARING 206040004111 BELL 206 206L1 1182107 SW M/R XMSN SPALLED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5737T BMC00300 45454 TRANSMISSION WAS REMOVED FOR METAL IN OIL AND FOUND TRIPLEX BEARING BALLS SPALLING. REPLACED WITH SERVICEABLE TRIPLEX BE ARING. 1 G 7 1 3U H2SW 1996101700792 19961017 00792 SW 1996 10 17 HEEA968063 1 19961003 A 6320 206040561103 SUN GEAR 206040004107 BELL 206 206L3 1182108 SW M/R XMSN CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 979BH 4496 B51694 51403 CORROSION IN SPLINES OF GEAR. REPLACED WITH SERVICEABLE SUN GEAR. 1 G 7 1 3U H2SW 1996101700793 19961017 00793 SW 1996 10 17 HEEA968064 1 19961003 A 6320 206040531105 CASE ASSY 206040004107 BELL 206 206L3 1182108 SW M/R XMSN CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 979BH 4496 B51694 51403 TWO EACH CRACKS INDICATED IN ONE EACH ARM OF WEB. REPLACED WITH SERVICEABLE CENTER CASE. 1 G 7 1 3U H2SW 1996101700794 19961017 00794 SW 1996 10 17 HEEA968065 1 19961003 A 6320 206040531105 CASE ASSY 206040004111 BELL 206 206L1 1182107 SW M/R XMSN CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1078G BMC45063 45398 CORROSION IN ORING GROOVE. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 1996101700795 19961017 00795 SW 1996 10 17 HEEA968066 1 19961003 A 6320 206040031003 BEARING 206040004111 BELL 206 206L1 1182107 SW M/R XMSN PITTED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1078G BMC45063 45398 PITTING ON ROLLERS. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 1996101700796 19961017 00796 SW 1996 10 17 HEEA968067 1 19961003 A 6320 206040037001 BEARING 206040004111 BELL 206 206L1 1182107 SW M/R XMSN PITTED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1078G BMC45063 45398 PITTING ON ROLLERS. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 1996101700797 19961017 00797 SW 1996 10 17 HEEA968068 1 19961003 A 6320 400040082101 GEARSHAFT 206040004111 BELL 206 206L1 1182107 SW M/R GR BOX CORRODED NUT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1078G BMC45063 45398 CORROSION IN THREADS. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 1996101700798 19961017 00798 SW 1996 10 17 HEEA968069 1 19961003 A 6520 212040004009 GEAR BOX 212040004009 BELL 412 412 1182202 SW 90 DEG GR BOX CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2298Z AHT07516 33077 GR BOX IS CORRODED. (CLEVIS ON CASE HAS CORROSION COMPLETELY AROUND BOLT HOLE. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 1996101700799 19961017 00799 SW 1996 10 17 HEEA968070 1 19961003 A 6520 212040462001 SHAFT 212040004009 BELL 412 412 1182202 SW T/R GR BOX CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2298Z AHT07516 33077 SHAFT IS CORRODED. (CORROSION IN BASE OF SPLINES AND BEHIND LAST SET OF SPLINES) REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 1996101700800 19961017 00800 SW 1996 10 17 HEEA968071 1 19961003 A 6520 212040462001 SHAFT 212040004009 BELL 212 212 1181420 SW T/R GR BOX CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1079U AHT50612 31122 SHAFT IS CORRODED.( FOUND EXCESSIVE CORROSION IN SPLINES "N" (REF. BHT 412 CR&0 SEC. 65-00-00 PAGE 133 FIG. 65-40) BEYO ND LIMITS. REPLACED WTH SERVICEABLE SHAFT. 1 G 7 1 4U H4SW 1996101700801 19961017 00801 SW 1996 10 17 HEEA968072 1 19961003 A 6520 212040452001 SLEEVE ASSY 212040004009 BELL 412 412 1182202 SW T/R GR BOX CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 21498 AHT08273 36003 SLEEVE ASSY IS CORRODED. (FOUND EXCESSIVE CORROSION SLEEVE IN AREA "A") REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 1996101700802 19961017 00802 SW 1996 10 17 HEEA968073 1 19961003 A 6520 212040468001 CASE ASSY 212040004009 BELL 412 412 1182202 SW T/R GR BOX CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 21498 AHT08273 36003 CORROSION ON LUG OF IDLER CLEVIS ALL AROUND BOLT HOLE ON O.D. OF CLEVIS. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 1996101700803 19961017 00803 1996 10 17 HEEA968074 4 19961003 A 3457 0110005400 GPS 150 BELL 407 407 SW COCKPIT INOPERATIVE E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 407PH 53003 GPS INOPERATIVE ON INSTALLATION. 1 G 7 1 3U O H2SW 1996101700804 19961017 00804 1996 10 17 HEEA968075 4 19961003 A 3457 0110005400 GPS 150 BELL 206 206L1 1182107 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5000K 45167 GPS NOT ACCEPTING DATA CARD. TIME SINCE REPAIR 0:00. 1 G 7 1 3U H2SW 1996101700805 19961017 00805 1996 10 17 HEEA968076 4 19961003 A 2210 2593996444 TARSYN GYRO BELL 412 412 1182202 SW COPILOT PRECESSES E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3893P 33012 COPILOTS GYRO COMPASS PRECESSES. TIME SINCE REPAIR 839:15. 1 G 7 2 4U H4SW 1996101700806 19961017 00806 1996 10 17 HEEA968077 4 19961003 A 2312 40001452502 TRANSCEIVER RT138F BOLKMS 117 BK117A3 5626015 EU COCKPIT VHF DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 401PH 7050 WILL NOT TRANSMIT. FOUND UNIT TO HAVE INTERMITTENT TRANSMIT POWER AND WEAK RECEIVER SENSITIVITY. ADJUSTED PRESELECTOR T UNING VOLTAGE AND ALIGNED RECEIVER, REPAIRED RECEIVER SENSE PROBLEM. UNIT HAS INTERMITTENT TRANSMIT PROBLEM FROM 138-14 0MHZ, REPLACED VCO MODULE ,REPAIRED. BENCH CHECK GOOD. 1 G 7 2 3U H13EU 1996101700807 19961017 00807 SW 1996 10 17 HEEA968078 1 19961003 A 7714 212070108007 INDICATOR BELL 212 212 1181420 SW TRIPLE TACH FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 27805 31106 #2 NEEDLE HAS NO INDICATION. 1 G 7 1 4U H4SW 1996101700808 19961017 00808 1996 10 17 HEEA968079 4 19961003 A 2312 064100900 TRANSCEIVER KTR905 BELL 212 212 1181420 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3131S 30953 VERY INTERMITTENT TRANSMIT AFTER WARM UP. 1 G 7 1 4U H4SW 1996101700809 19961017 00809 1996 10 17 HEEA968080 4 19961003 A 2312 064100900 TRANSCEIVER KTR905 BELL 212 212 1181420 SW COCKPIT VHF FAULTY E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5010F 30936 AFTER UNIT HEATS UP, MODULATION BEGINS TO BREAK UP. 1 G 7 1 4U H4SW 1996101700810 19961017 00810 1996 10 17 HEEA968081 4 19961003 A 2312 064102300 TRANSCIEVER BELL 214 214ST 1182106 SW COCKPIT VHF DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 UNREADABLE, POWER OUT LOW ON LOW END RANGE. SENT TO ALLIED SIGNAL AVIONICS FOR INSPECTION AND REPAIR. 2 G 7 2 4U H10SW 1996101700811 19961017 00811 SW 1996 10 17 HEEA968082 1 19961003 A 5320 212030009115A DECK ASSY BELL 212 212 1181420 SW ENGINE TOO WIDE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 30888 TRANSITION AREA TOO WIDE. HITS CAP ANGLES ON LH AND RH SIDE. 1 G 7 1 4U H4SW 1996101700812 19961017 00812 1996 10 17 HEEA968083 4 19961003 A 3453 4530103 LORAN ARNAV21 BELL 206 206L3 1182108 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3207Q 51540 SOME BUTTONS HAVE INTERMITTENT BACKLIGHTING. 1 G 7 1 3U H2SW 1996101700813 19961017 00813 1996 10 17 HEEA968084 4 19961003 A 3453 4530093 RECEIVER ARNAV20 BELL 206 206L3 1182108 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4282Z 51499 DISPLAY AND BEARING INOPERATIVE, BUTTONS INTERMITTENT AND STICKY. 1 G 7 1 3U H2SW 1996101700815 19961017 00815 1996 10 17 HEEA968086 4 19961003 A 3442 MI5851345 INDICATOR P40 SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31219 760230 BLANK SCREEN. 1 G 7 2 3U H1NE 1996101700816 19961017 00816 1996 10 17 HEEA968087 4 19961003 A 3442 MI58513454 INDICATOR P40 BELL 212 212 1181420 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5010F 30936 INDICATOR CAUSES R/T NOT TO TRANSMIT. 1 G 7 1 4U H4SW 1996101700817 19961017 00817 1996 10 17 HEEA968088 4 19961003 A 3442 MI5852013 INDICATOR P4001 BELL 412 412 1182202 SW FRONT PANEL DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893N 33010 FOUND CYCLIC BUTTON ON FRONT PANEL NOT LIGHTING. 1 G 7 2 4U H4SW 1996101700818 19961017 00818 1996 10 17 HEEA968089 4 19961003 A 3442 MI5852013 INDICATOR P4001 SKRSKY S76 S76A 8143006 NE COCKPIT MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 792CH 760193 STANDBY REMAINS ON AT ALL TIMES WHEN OTHER FUNCTIONS ARE SELECTED AND DISPLAY DISTORTED. 1 G 7 2 3U H1NE 1996101700819 19961017 00819 1996 10 17 HEEA968090 4 19961003 A 3444 066304401 INDICATOR SKRSKY S76 S76A 8143006 NE RADAR ALTIMETER ERRORS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546K 760082 VARIES 500 FEET. 1 G 7 2 3U H1NE 1996101700820 19961017 00820 1996 10 17 HEEA968091 4 19961003 A 3453 25410036 7000 RCU BELL 412 412 1182202 SW COCKPIT LORAN FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893P 33012 WON'T RECEIVE STATIONS. 1 G 7 2 4U H4SW 1996101700821 19961017 00821 1996 10 17 HEEA968092 4 19961003 A 3416 D120P2T ANEROID SNIAS 350 AS350B2 8680813 EU ALTIMETER DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4031L 2907 BARO ANEROID UNIT HAS AN OUTPUT OF 13,400 FEET WITH NO PRESSURE APPLIED. 1 G 7 1 3U H9EU 1996101700822 19961017 00822 1996 10 17 HEEA968093 4 19961003 A 2312 064105430 TRANSCEIVER BOLKMS 117 BK117A3 5626015 EU COCKPIT VHF DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8765J 7054 SQUELCH STAYS ON. 1 G 7 2 3U H13EU 1996101700823 19961017 00823 SW 1996 10 17 HEEA968094 1 19961003 A 5520 206023119151 STABILIZER ASSY BELL 206 206L1 1182107 SW LT ELEV MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 5745N 45489 INSTALLED STABILIZER AND TRIED TO INSTALL ELEVATOR ASSEMBLY. THE LEFT ELEV PIVOT PIN HAD BEEN INSTALLED 5/16" INBOARD T OO FAR. UNABLE TO INSTALL ELEVATOR. 1 G 7 1 3U H2SW 1996101700824 19961017 00824 EU 1996 10 17 HEEA968095 1 19961003 A 5610 04011650990 WINDOW SNIAS 350 AS350B2 8680813 EU SLIDER CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 2771 WINDOW IS CRACKED. (SLIDING WINDOW TRACK BROKEN AND CRACKED) 1 G 7 1 3U H9EU 1996101700825 19961017 00825 1996 10 17 HEEA968096 4 19961003 A 3450 071121004 CONTROL BOX BELL 412 412 1182202 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 FREQUENCY CHANGE BUTTOM STICKS. REPLACED S301 TRANSFER SWITCH P/N 031-0399-01. REPAIRED. BENCH CHECK GOOD. 1 G 7 2 4U H4SW 1996101700826 19961017 00826 1996 10 17 HEEA968097 4 19961003 A 3455 066107700 RECEIVER BELL 412 412 1182202 SW COCKPIT ADF MALFUNCTION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 7128R 36007 CUTS IN AND OUT FREQUENCY AND CHANGES FREQUENTLY TO 808. WHEN UNIT IS VIBRATED, AUDIO CUTS OUT. FOUND VCO COVER BENT IN AND TAPPING ON COVER CUTS AUDIO OUT. REMOVED COVER AND STRAIGHTENED OUT. REPAIRED. VIBRATED AND COULD NOT GET AUDIO OUT AGAIN. FOUND BFO AUDIO TO BE GARBLED. REPLACED INTEGRATEDCIRCUIT I309 AND CAPACITOR C332. REPAIRED. BENCH CHECK GOOD. 1 G 7 2 4U H4SW 1996101700827 19961017 00827 1996 10 17 HEEA968098 4 19961003 A 3454 071121612 CONTROL UNIT SKRSKY S76 S76A 8143006 NE COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 15460 760223 ON/OFF SWITCH VERY LOOSE - INDICATOR GLASS IS LOOSE. PERFORMED PRELIMINARY INSPECTION. TIGHTENED SET SCREWS ON ON/OFF K NOB. REPAIRED. REPLACED FADED AND CRACKED LENS. REPLACED BAD DISPLAY DS101. REPLACED HEADER P201 AND APPLIED HUMISEA L FOR CORROSION CONTROL. CHECKED 28V LIGHTS. BENCH CHECKGOOD. 1 G 7 2 3U H1NE 1996101700828 19961017 00828 EU 1996 10 17 HEEA968099 1 19961003 A 3040 350A89103701 ARM SNIAS 350 AS350B2 8680813 EU WINDSHIELD WIPER MOUNT BROKE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 2771 WIPER ARM MOUNT HOLD BROKE. REPLACED WITH SERVICEABLE WIPER ARM ASSEMBLY. 1 G 7 1 3U H9EU 1996101700829 19961017 00829 SW 1996 10 17 HEEA968100 1 19961003 A 7931 APTE138100G TRANSMITTER BELL 412 412 1182202 SW OIL PRESSURE FAULTY E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893N 33010 REPORTED C/BOX PRESSURE RUNS AT MINIMUM GREEN (MFG DATE 6-96) 1 G 7 2 4U H4SW 1996101700830 19961017 00830 SW 1996 10 17 HEEA968101 1 19961003 A 2437 209070263003 INDICATOR BELL 412 412 1182202 SW DUAL VOLTS STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D 33076 NEEDLE ON DC SIDE INTERMITTENTLY STICKS. TIME SINCE REPAIR 186:45. 1 G 7 2 4U H4SW 1996101700832 19961017 00832 EU 1996 10 17 HEEA968103 1 19961003 A 6220 350A31003306 VIBRATION ABSORB SNIAS 350 AS350B2 8680813 EU M/R BOLT BROKE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6097Z 2195 2820 MOUNTING BOLT BROKE OFF AND THE NUTPLATE BROKE OFF AND BOTH PIECES ARE INSIDE TUBE. 1 G 7 1 3U H9EU 1996101700833 19961017 00833 1996 10 17 HEEA968104 4 19961004 A 3442 7009330901 RADAR RT BELL 230 230 1182149 SW COCKPIT INTERMITTENT E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 230UN 23009 INTERMITTENT OPERATION. TIME SINCE REPAIR 212:15. 1 G 7 2 3U NC H9SW 1996101700834 19961017 00834 1996 10 17 HEEA968105 4 19961004 A 3453 27010045 ANTENNA BELL 412 412 1182202 SW LORAN DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D 33076 LORAN ANTENNA CAUSING SYSTEM TO BE INTERMITTENT. 1 G 7 2 4U H4SW 1996101700835 19961017 00835 EU 1996 10 17 HEEA968106 1 19961004 A 6240 10594565 INDICATOR BOLKMS 105 BO105S 5626006 EU MAST MOMENT WONT TEST E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5031U S678 INDICATOR WILL NOT TEST PROPERLY. 1 G 7 2 3U H3EU 1996101700836 19961017 00836 EU 1996 10 17 HEEA968107 1 19961004 A 6240 10594575 TRANSMITTER BOLKMS 105 BO105S 5626006 EU MAST MOMENT WONT TEST E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5031U S678 INDICATOR WILL NOT TEST PROPERLY. 1 G 7 2 3U H3EU 1996101700837 19961017 00837 EU 1996 10 17 HEEA968108 1 19961004 A 2844 DK042 TRANSMITTER BOLKMS 105 BO105S 5626006 EU FUEL PRESS READS HIGH E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81992 S827 FUEL PRESSURE READING HIGH. 1 G 7 2 3U H3EU 1996101700838 19961017 00838 EU 1996 10 17 HEEA968109 1 19961004 A 2844 DK042 TRANSMITTER BOLKMS 105 BO105S 5626006 EU FUEL PRESS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7161J S834 FUEL PRESSURE DOES NOT INDICATE. 1 G 7 2 3U H3EU 1996101700839 19961017 00839 SW 1996 10 17 HEEA968110 1 19961004 A 7722 206075187001 INDICATOR BELL 206 206L1 1182107 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 513EH 45421 BEZEL LOOSE ON UNIT. 1 G 7 1 3U H2SW 1996101700840 19961017 00840 NE 1996 10 17 HEEA968111 1 19961004 A 5280 7620902019105 FITTING SKRSKY S76 S76A 8143006 NE MLG DOOR CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31219 760230 FITTING CRACKED APPROXIMATELY 1/4". REPLACED WITH SERVICEABLE FITTING. 1 G 7 2 3U H1NE 1996101700841 19961017 00841 EU 1996 10 17 HEEA968112 1 19961004 A 6410 355A09103601 BEARING SNIAS 350 AS350B2 8680813 EU T/R HALF SHELL SPLIT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100R 1026 2862 LAMINATES SPLITTING. REPLACED WITH SERVICEABLE BEARING KIT. 1 G 7 1 3U H9EU 1996101700842 19961017 00842 EU 1996 10 17 HEEA968113 1 19961004 A 6310 350A35106920 PIN SNIAS 350 AS350B2 8680813 EU GIMBAL JOINT CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 2771 ENGINE TO TRANSMISSION GIMBAL RING PIN CORRODED. REPLACED WITH SERVICEABLE PIN. 1 G 7 1 3U H9EU 1996101700843 19961017 00843 EU 1996 10 17 HEEA968114 1 19961004 A 5510 350A13111620 BOLT SNIAS 350 AS350B2 8680813 EU HORIZ STAB WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 2771 BOLTS FOR HORIZONTAL STABILIZER WORN. REPLACED WITH SERVICEABLE HORIZONTAL STABILIZER. 1 G 7 1 3U H9EU 1996101700844 19961017 00844 SW 1996 10 17 HEEA968115 1 19961004 A 5530 206030114165 SUPPORT ASSY 206020113223 BELL 407 407 SW ANTI COLL LIGHT CHAFE WIRES E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407PH 279 53003 ON JULY 5, 1996 AT AIRCRAFT TOTAL TIME 214:10 3 WIRE CABLES WERE INSTALLED IN VERTICAL FIN AS THE OTHERS WERE SEVERELY C HAFED. THE NEW CABLE WAS REPAIRED 2 OR 3 TIMES. THEN ON JULY 22, 1996, THE CABLE WAS REPLACED AGAIN BECAUSE IT IS CHAF ING SEVERELY WHERE THE WIRE GOES THROUGH SUPPORT P/N 206-030-114-165 AND WIRE MAKES A 90 DEGREE TURN TO GO FORWARD. SOME SORT OF CHAFE PROTECTION NEEDS TO BE INSTALLED FOR THE ANTI-COLLISION WIRE TO FREELY TRAVEL THROUGH SUPPORT P/N 206-030 -114-165. IT NEEDS TO BE SOFT ENOUGH TO GIVE THE WIRE PROTECTION AND BIG ENOUGH TO ALLOW A NEW WIRE TO BE STRUNG WITHOU TDISASSEMBLY. 1 G 7 1 3U O H2SW 1996101700845 19961017 00845 1996 10 17 HEEA968117 4 19961004 A 3420 5040017901 INDICATOR SNIAS 350 AS350B2 8680813 EU COCKPIT ATTITUDE DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4000L 410 2873 INDICATOR WON'T PULL FLAG. 1 G 7 1 3U H9EU 1996101700846 19961017 00846 1996 10 17 HEEA968118 4 19961004 A 2312 4000106010 CONTROL UNIT C10 BOLKMS 105 BO105S 5626006 EU COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7161J S834 SECOND THUMBWHEEL AND SECOND DISPLAY LIGHTS INCORRECT. 1 G 7 2 3U H3EU 1996101700847 19961017 00847 1996 10 17 HEEA968119 4 19961004 A 3444 066305401 INDICATOR KI250 BELL 206 206L3 1182108 SW COCKPIT STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8594X 51531 NEEDLE STICKS AT 500 FEET. 1 G 7 1 3U H2SW 1996101700848 19961017 00848 NE 1996 10 17 HEEA968122 1 19961004 A 6730 7665009805109 SERVO SKRSKY S76 S76A 8143006 NE M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546K 10384 760082 WORN BEARINGS. SENT TO HASE FOR MODIFICATION FOR CSN76-173 AND HR TEXTRON S.B. 0006760-06. 1 G 7 2 3U H1NE 1996101700849 19961017 00849 NE 1996 10 17 HEEA968123 1 19961004 A 6730 7665009805109 SERVO SKRSKY S76 S76A 8143006 NE M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545X 10955 760050 INPUT LEVER BEARINGS WORN. SENT TO HASE FOR MODIFICATION FOR CSN76-173 AND HR TEXTRON S.B. 0006760-06. 1 G 7 2 3U H1NE 1996101700850 19961017 00850 NE 1996 10 17 HEEA968124 1 19961004 A 6730 7665009805109 SERVO SKRSKY S76 S76A 8143006 NE M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3122G 9066 760232 UPPER BEARING WORN. SENT TO HASE FOR MODIFICATION FOR CSN76-173 AND HR TEXTRON S.B. 0006760-06. 1 G 7 2 3U H1NE 1996101700851 19961017 00851 NE 1996 10 17 HEEA968125 1 19961004 A 6730 7665009805109 SERVO SKRSKY S76 S76A 8143006 NE M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3122H 9816 760233 UPPER BEARING WORN. SENT TO HASE FOR MODIFICATION FOR CSN76-173 AND HR TEXTRON S.B. 0006760-06. 1 G 7 2 3U H1NE 1996101700852 19961017 00852 NE 1996 10 17 HEEA968126 1 19961004 A 6730 7665009805109 SERVO SKRSKY S76 S76A 8143006 NE M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22342 12608 760096 UPPER BEARING HAS EXCESSIVE WEAR. SENT TO HASE FOR MODIFICATION FOR CSN76-173 AND HR TEXTRON S.B. 0006760-06. 1 G 7 2 3U H1NE 1996101700853 19961017 00853 1996 10 17 HEEA968127 4 19961004 A 3413 55034670102 INDICATOR SKRSKY S76 S76A 8143006 NE COCKPIT V SPEED DEFECTIVE E HEEA O OTHER O OTHER CL CLIMB 1 SW 03 5128 760181 READS 3000 FOOT CLIMB IN A DECENT. 1 G 7 2 3U H1NE 1996101700854 19961017 00854 NE 1996 10 17 HEEA968128 1 19961004 A 6210 7615009043050 TIP CAP SKRSKY S76 S76A 8143006 NE M/R BLADE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545X 760050 TIP CAP HAS THE ABRASION STRIP CRACKED WITH MULTIPLE BRANCHES AND SEPARATION. ALSO HAS SOME FIBERGLASS EROSION. 1 G 7 2 3U H1NE 1996101700855 19961017 00855 NM 1996 10 17 HEEA968129 1 19961004 A 7170 LINE DOUG MD900 MD900 3027375 NM FUEL DRAIN LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 9214U 90 90000014 FUEL LEAKING FROM DRAIN LINE INTO BAGGAGE COMPT OH AND QUILTED BLANKET AND RUNNING ON THE LH E.E.C. RUBBER HOSE DETERIO RATED AND BROKE AT STAINLESS STEEL TUBE ASSY P/N 90002660875-103. INSPECTION OF RH SIDE REVEALED THE SAME DETERIORATION OF THERUBBER HOSE WITH AN IMMINENT FAILURE. NOTE: P/N OF AFFECTED HOSE NOT LISTED IN PARTS BOOK- REF. 71-70-00. 1 G 7 2 3U NC H19NM 1996101700856 19961017 00856 SW 1996 10 17 HEEA968130 1 19961004 A 3270 222035233103S SKID ASSY BELL 230 230 1182149 SW TAIL HOLE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 3198 23009 SKID MOUNT HOLE WORN. 1 G 7 2 3U NC H9SW 1996101700857 19961017 00857 SW 1996 10 17 HEEA968131 1 19961004 A 6220 206011125105 PIN STRAP BELL 206 206B3 1181506 SW M/R CORRODED E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 PART IS CORRODED. (PINS RECEIVED FROM STOCK WITH CORROSION ON PARTS) 1 G 7 1 3U H2SW 1996101700884 19961017 00884 CE 1996 10 17 96ZZZX5231 1 19960809 A 3230 HOOK CESSNA 402 402C 207590R CE LT MLG UPLOCK FAILED A OEZA K NONE O OTHER NR NOT REPORTED 1 WP 19 763EA 402C0497 UPLOCK HOOK FAILED. UNABLE TO DETERMINE THE OLD PART NUMBER IN CESSNA PARTS BOOK. INSTALLED NEW STEEL HOOK, P/N 514131 2-2. SUBMITTER STATED THIS HOOK (STEEL) IS THE WAY TO GO. THE STOCK PART DELIVERED (THIN ALUMINUM) AND THE ONE SUPPLIE D BY SERVICE KITS (THICK ALUMINUM), FAIL ALOT. 1 L 7 2 3O A7CE 1996101700886 19961017 00886 EU 1996 10 17 USAA960602 1 19960604 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU BS 3820 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 487US 20640 11238 YYC - DURING FC-06 CHECK, FOUND 3MM TYPE 1 CRACK AT STA 3820, STR 72, ON SKIN. REMOVED FINGER STRIP AND REPAIRED PER SR M 53-02-18. (X) 2 L 7 2 4F RT A20EU 1996101700893 19961017 00893 CE 1996 10 17 96ZZZX5239 1 19960930 A 8120 4066109028 TURBOCHARGER CESSNA 402 402C 207590R CE CONT O520 TSIO520UB 17040 SO SHAFT SEAL FAILED A OEZA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 19 2714B ZG009434 402C0210 811020R DURING PRE-OILING OF NEWLY INSTALLED TCM REBUILT ENGINE, OIL LEAKED OUT OF EXHAUST TAILPIPE. FOUND OIL POURING FROM TUR BINE SHAFT LIKE SEAL WAS NOT INSTALLED. 1 L 7 2 3O 3 O A7CE E8CE 1996101700899 19961017 00899 SO 1996 10 17 RAAA96E4015 1 19961015 A 3350 8621006 BATTERY PACK INTVLV 873100212 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 9744C 188C1140 EGRESS FLOOR PROXIMITY LIGHTS AT ROW 19 AND 22 FAILED SERVICE CHECK. CHANGED 2 BATTERY PACKS DUE TO LOW CHARGE. 2 L 7 4 4T 4A22 1996101700900 19961017 00900 WP 1996 10 17 CALA9601470 1 19961010 A 5730 SKIN DOUG DC10 DC1030 3023501 WP WS 602 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 87070 48292 RIGHT HAND WING LEADING EDGE LOWER SKIN AT STATION XOS602 HAS A ONE INCH CRACK. INSTALLED DOUBLER PER EC/RA 5730-01421 REV A. 2 L 7 3 4F A22WE 1996101700901 19961017 00901 WP 1996 10 17 CALA9601471 1 19961015 A 4950 3812761 APU DOUG DC9 DC982 3022082 WP CABIN SMOKING A CALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 16893 3279 49392 APU FILLS CABIN WITH SMOKE WITH AIR ON. PLACARD APU INOPERATIVE, REPLACE COALESCER BAGS, CLEAN APU COMPARTMENT AND PERF ORMED BURN OUT OF DUCTING. 2 L 7 2 4F A6WE 1996101700902 19961017 00902 NM 1996 10 17 CALA9601472 1 19960911 A 5754 SKIN BOEING 737 7373T0 1384582 NM NR 5 LE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76355 23593 NUMBER 5 SLAT HAS CRACK COMING FROM FASTENERS. FABRICATED DOUBLERS AND REPAIRED PER EC/RA 5750-01159. 2 L 7 2 4F RT A16WE 1996101700903 19961017 00903 NE 1996 10 17 9622065517 2 19961005 A 7200 ENGINE BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE NR 2 FAILED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 01 517US 23205 716449 DURING CRUISE FLIGHT, NR 2 ENGINE OIL FILTER EICAS MESSAGE ANNUNCIATED. COM PROCEDURES WERE FOLLOWED, SHUT DOWN NR 2 EN GINE, FLIGHT DIVERTED TO MSP AND PERFORMED AN UNEVENTFUL LANDING. MAINTENANCE FOUND METAL ON MAG PLUG. REPLACED THE NR 2 ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 1996101700904 19961017 00904 NM 1996 10 17 9622076636 1 19961015 A 3297 W724G032718 WIRE BOEING 747 747251B 1384892 NM LT MLG SHORTED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 636US 23547 DURING TAKEOFF, THE LANDING GEAR RED UNSAFE LIGHT ILLUMINATED AND THE LANDING GEAR ALTERNATE DISCONNECT/CONNECT CIRCUIT BREAKER POPPED. AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACED SHORTED WIRE ON LEFT WING LANDING GEAR, OP ERAITONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996101700905 19961017 00905 WP 1996 10 17 9622089930 1 19961014 A 3260 DOWNLOCK SWITCH DOUG DC9 DC931 3022065 WP NLG MALFUNCTIONED A NWAA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 01 89S 47042 ON APPROACH, THE NOSE GEAR GREEN DOWNLOCK LIGHT DID NOT ILLUMINATE AFTER GEAR WAS EXTENDED. RECYCLED GEAR AND NORMAL IN DICATIONS WERE ACHIEVED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY ON GROUND. REP LACED NOSE GEAR DOWNLOCK SWITCH AS A PRECAUTION, OPERATIONAL CHECK NORMAL ON GEAR SWING. 2 L 7 2 4F A6WE 1996101700906 19961017 00906 WP 1996 10 17 9622099981 1 19961015 A 3350 6011779 POWER SUPPLY DOUG DC9 DC931 3022065 WP LT NACELLE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 994Z 47097 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996101700907 19961017 00907 NM 1996 10 17 96FDEA01578 1 19961015 A 2170 COALESCER BAGS BOEING 727 7272S2F 1384O81 NM CABIN DIRTY A FDEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 25 209FE 22931 AFTER LIFT OFF STRONG ACRID SMELL IN COCKPIT ALONG WITH BURNING EYES (LEFT PACK #1 BLD) SWITCHED PACK/BLD SOURCE (RIGHT PACK #3 BLD) NO CHANGE IN SMELL. INTENSITY SEEMED TO CHANGE WITH PWR SETTINGS. INSPECTED INLETS & EXHAUST OF ALL ENG INES FOR FLUID NONE FOUND RAN ALL 3 ENGINES AT POWER FOR 20 MIN. WITH PACKS ON NO ARID SMELL OR BURNING EYES WHEEL WELL WERE CLEANED DURING WEEKEND LAYOVER SERVICE CK. SUSPECT VAPORS FROM SOLVENT ENTERED APU R&R LEFT AND RIGHT WATER SEPARA TOR SOCKS OK FOR SERVICE. 2 L 7 3 4F A3WE 1996101700908 19961017 00908 NE 1996 10 17 96FDEA01579 2 19961015 A 7530 VALVE BOEING 727 7272S2F 1384O81 NM PWA JT8 JT8D217C 52053 NE NR 3 ENGINE MALFUNCTIONED A FDEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 25 209FE 22921 AGAIN ON DEPARTURE STRONG ACRID SMELL, RETURNED LEFT PACK AND NR 1 BLEED SELECTED. RETURNED TO AIRPORT. REMOVED AND RE PLACED 3 HYD BLEED RESERVOIR CHECK VALVES. GROUND RAN NR 1 ENG WITH LT AND RT PACKS ON NR 1 BLEED AT H. POWER AND MAX HEAT, NO SMELL NOTED. SAME ON NR 3 ENG BLEED, NO SMELL NOTED. OPERATED LT PACK NR 1 ENG AND RT PACK ON NR 3 ENG BLEED, NO SMELL NOTED. ALL BLEEDS ON AND LT AND RT PACKS OPERATING, NO SMELL NOTED ON GROUND. 2 L 7 3 4F 4 F A3WE E9NE 1996101700909 19961017 00909 NM 1996 10 17 96FDEA01580 1 19961015 A 3260 UPLOCK SENSOR BOEING 727 727233 138408A NM RT MLG MALFUNCTIONED A FDEA O OTHER N FALSE WARNING LD LANDING 1 SO 25 263FE 21625 DURING LANDING GEAR EXTENSION, RIGHT HAND MAIN LANDING GEAR RED LIGHT ON CENTER PANEL FLICKERED ON AND OFF WHEN GREEN LI GHT WAS ILLUMINATED. THIS CONDITION CONTINUED THROUGH RECYCLING. ACCOMPLISHED RED TABS FOR MAIN LANDING GEAR FAILURE T O EXTEND. LANDING UNEVENTFUL, CONDITION RECURRED ON TAXI INTO BLOCKS. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT AND ANNUNCIATOR MODULE NO HELP. FURTHER TROUBLESHOOTING INDICATES UPLOCK SENSOR INOPERATIVE. REMOVED AND REPLACED RT MAIN LANDING GEAR UPLOCK SENSOR PER MAINTENCE MANUAL 32-61-81. GROUND OPERATIONAL CHECKS SERVICEABLE. 2 L 7 3 4F RT A3WE 1996101700910 19961017 00910 WP 1996 10 17 MWEA96615 1 19961015 A 4950 38025611 APU BLEED AIR DOUG DC9 DC914 3022034 WP CABIN SMOKING A MWEA O OTHER J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 31 700ME 704 45696 PILOT REPORTS ON GROUND WITH RT PACK ON AND APU AIR ON BOTH LT AND RT SIDE CABIN HAD SMALL AMOUNT OF SMOKE AND BOTH LAV SMOKE DETECTORS SOUNDED INTERMITTENTLY. REPLACED APU, OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996101700911 19961017 00911 NM 1996 10 17 P5CA9600776 1 19961013 A 7110 NOSE COWL LINER BOEING 747 747132 1384882 NM NR 1 ENGINE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 DELAMINATED AND DAMAGED NR 1 ENGINE NOSE COWL ACCOUSTICAL INNER LINER DUE TO BIRD STRIKE. REMOVED AND REPLACED NOSE COW L PER BAC MM 71-11-01. 2 L 7 4 4F A20WE 1996101700912 19961017 00912 NE 1996 10 17 P5CA9600777 2 19961013 A 7230 RUB STRIP BOEING 747 747132 1384882 NM PWA JT9 JT9D7A 52054 NE NR1 ENG FAN CASE MISSING A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 MISSING NR 1 ENGINE FAN CASE RUB STRIP SECTIONS DUE TO BIRD STRIKE. REPAIRED PER BAC MM 72-31-04. 2 L 7 4 4F 4 F A20WE E20EA 1996101700913 19961017 00913 NE 1996 10 17 P5CA9600778 2 19961013 A 7230 FAN EXH STATORS BOEING 747 747132 1384882 NM PWA JT9 JT9D7A 52054 NE NR 1 ENGINE DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 DAMAGED NR 1 ENGINE FAN EXHAUST STATORS DUE TO BIRD STRIKE. REPAIRED PER BAC MM 72-31-05. 2 L 7 4 4F 4 F A20WE E20EA 1996101700914 19961017 00914 NE 1996 10 17 P5CA9600779 2 19961013 A 7230 771731 FAN BLADES BOEING 747 747132 1384882 NM PWA JT9 JT9D7A 52054 NE NR 1 ENGINE DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 DAMAGED NR 1 ENGINE FAN BLADES DUE TO BIRD STRIKE. REPLACED OUT OF LIMIT BLADES AND BLENDED OTHER DAMAGED FAN BLADES PE R BAC MM 72-31-02. 2 L 7 4 4F 4 F A20WE E20EA 1996101700915 19961017 00915 NM 1996 10 17 P5CA9600780 1 19961001 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 810 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 2 CORROSION AT S46R BS 810 FORWARD CARGO COMPARTMENT. REPAIRED STRINGER PER BOEING SRM 53-10-03. 2 L 7 4 4F A20WE 1996101700916 19961017 00916 NM 1996 10 17 P5CA9600781 1 19961001 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 775/785 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 2 CORROSION S44L AT BS 775 AND 785. REPAIRED PER BOEING SRM 53-10-03. 2 L 7 4 4F A20WE 1996101700917 19961017 00917 NM 1996 10 17 P5CA9600782 1 19961010 A 5512 SKIN BOEING 747 747122 1384872 NM RT HORIZ STAB CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION TOP OF RIGHT HORIZONTAL STABILIZER STA 335 RBL 260, STA 340 RBL 270, STA 310 RBL 260 TO 270, STA 260 T O 310 RBL 255.2, STA 310 RBL 260 TO 300, STA 0 TO 260 RBL 255, STA 0 TO 26 RBL 231, STA 0 TO 26 RBL 170. CORROSION REMO VED AND REPROTECTED PER BOEING SRM 55-10-01 AND 55-10-02. 2 L 7 4 4F A20WE 1996101700918 19961017 00918 NM 1996 10 17 P5CA9600783 1 19961015 A 3246 260356110 WHEEL BOEING 747 747123 1384873 NM LT MLG CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 89 20109 CRACKED INNER HUB BETWEEN LIGHTENING HOLES WITH BEARING RACE SEPARATED FROM REST OF ASSEMBLY,(WHEEL HALVES DID NOT SEPAR ATE. REPLACED WHEEL AND TIRE ASSEMBLY PER BAC MM 32-45-01. 2 L 7 4 4F A20WE 1996101700919 19961017 00919 NM 1996 10 17 P5CA9600784 1 19961014 A 7810 EXHAUST STRUT BOEING 747 747123 1384873 NM NR 1 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 CRACK OF MORE THEN 50 PERCENT OF CHORD WIDTH TO NR 1 ENGINE 7 O'CLOCK EXHAUST STRUT. NO CORRECTIVE ACTION, TO BE INSPEC TED EVERY 100 HOURS PER BAC MM 72-53-02. 2 L 7 4 4F A20WE 1996101700920 19961017 00920 NM 1996 10 17 P5CA9600785 1 19961007 A 5755 PANEL BOEING 747 747122 1384872 NM NR 7 SPOILER DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 DELAMINATED NR 7 SPOILER PANEL ON RIGHT WING. REPLACED NR 7 SPOILER PANEL PER BAC MM 27-62-01. 2 L 7 4 4F A20WE 1996101700921 19961017 00921 NM 1996 10 17 P5CA9600786 1 19961007 A 7110 ANGLE BOEING 747 747122 1384872 NM NR 2 ENG COWL GOUGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 GOUGED INNER FORWARD STRUCTURAL ANGLE ON NR 2 ENGINE OUTBOARD CORE COWL. REPLACED ANGLE PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1996101700922 19961017 00922 NM 1996 10 17 P5CA9600787 1 19961007 A 7110 RIVET BOEING 747 747122 1384872 NM ENGINE FAIRING PULLED THROUGH A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 SUNK RIVETS ON NR 2 SLOT SEAL FAIRING. REPLACED RIVETS PER BAC SRM 51-30-02. 2 L 7 4 4F A20WE 1996101700923 19961017 00923 NM 1996 10 17 P5CA9600788 1 19961007 A 7110 RIVETS BOEING 747 747122 1384872 NM ENGINE FAIRING MISSING A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 SEVERAL LOOSE OR MISSING RIVETS ON NR 2 SLOT SEAL FAIRING. REPLACED RIVETS PER BAC SRM 51-30-02. 2 L 7 4 4F A20WE 1996101700924 19961017 00924 NM 1996 10 17 P5CA9600789 1 19961007 A 5414 SKIN BOEING 747 747122 1384872 NM NR 3 PYLON DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 DAMAGED SKIN ON PYLON LEADING EDGE FROM 11 O'CLOCK TO 7 O'CLOCK. TRIMMED DAMAGED AREA PER BAC SRM 54-30-01. 2 L 7 4 4F A20WE 1996101700925 19961017 00925 NM 1996 10 17 P5CA9600790 1 19961007 A 5754 SKIN BOEING 747 747122 1384872 NM LT LE FLAP CHAFED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 HOLE CHAFED IN OUTBOARD END LEADING EDGE OF LEFT OUTBOARD LEADING EDGE FLAP. CLEANED, POTTED AND APPLIED A FIBERGLASS O VERLAY REPAIR PER BAC SRM 51-40-09. 2 L 7 4 4F A20WE 1996101700926 19961017 00926 NM 1996 10 17 P5CA9600791 1 19961007 A 7110 COWL SKIN BOEING 747 747122 1384872 NM NR 3 ENGINE LIFTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LIFTED OUTER SKIN ON NR 3 ENGINE OUTBOARD CORE COWL MID SECTION. REPLACED SKIN PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1996101700927 19961017 00927 NM 1996 10 17 P5CA9600792 1 19961007 A 7110 ANGLE BOEING 747 747122 1384872 NM NR 2 ENG COWL GOUGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 DEEP GOUGE ON NR 2 ENGINE OUTBOARD CORE COWL HAT SECTION STRUCTURAL ANGLE. FABRICATED NEW ANGLE AND INSTALLED PER BAC S RM 51-10-01. 2 L 7 4 4F A20WE 1996101700928 19961017 00928 NM 1996 10 17 P5CA9600793 1 19961007 A 7110 ANGLE BOEING 747 747122 1384872 NM NR 3 ENG COWL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 CRACKS, HOLES AND CAVED IN SECTIONS AT 3 PLACES ON LOWER STRUCTURAL HAT ANGLE OF NR 3 ENGINE INBOARD CORE COWL. FABRICA TED AND INSTALLED NEW HAT ANGLE ON NR 3 ENGINE CORE COWL PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1996101700929 19961017 00929 NM 1996 10 17 P5CA9600794 1 19961007 A 7110 SKIN BOEING 747 747122 1384872 NM NR 3 ENGINE COWL DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 DAMAGED AND WORN OUTER SKIN AT NR 3 ENGINE INBOARD CORE COWL BLOW OUT PANEL AND CUTOUT RADIUS. REPAIRED DAMAGED AREA PE R BAC SRM 51-40-02. 2 L 7 4 4F A20WE 1996101700930 19961017 00930 NM 1996 10 17 P5CA9600795 1 19961007 A 7110 SKIN BOEING 747 747122 1384872 NM NR 2 ENGINE COWL DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 DAMAGED AND WORN SKIN ON BLOW OUT DOOR AND CUTOUT OF NR 2 ENGINE INBOARD CORE COWL. BLENDED DAMAGED AREAS PER BAC SRM 5 1-10-01. 2 L 7 4 4F A20WE 1996101700931 19961017 00931 NM 1996 10 17 P5CA9600796 1 19961007 A 7110 RIVETS BOEING 747 747122 1384872 NM NR 2 ENGINE COWL LOOSE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 SKIN LIFTING AT PRECOOLER EXHAUST CUTOUT ON NR 2 INBOARD CORE COWL DUE TO LOOSE RIVETS. REPAIRED BY RECOUNTOURING SKIN AND REPLACING LOOSE RIVETS PER BAC SRM 51-30-02. 2 L 7 4 4F A20WE 1996101700932 19961017 00932 NM 1996 10 17 P5CA9600797 1 19961007 A 7110 ANGLE BOEING 747 747122 1384872 NM NR 2 ENGINE COWL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 CRACKED, WORN AND CAVED IN STRUCTURAL ANGLE ON NR 2 ENGINE INBOARD CORE COWL. FABRICATED AND REPLACED STRUCTURAL ANGLE PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1996101700933 19961017 00933 NM 1996 10 17 P5CA9600798 1 19961007 A 5210 SKIN BOEING 747 747122 1384872 NM 3R DOOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL 1 CORROSION TO RIVET HEADS ON NR 3R DOOR OUTER SKIN. REMOVED AND REPLACED CORRODED RIVETS PER BAC SRM 51-30-02. 2 L 7 4 4F A20WE 1996101700934 19961017 00934 NM 1996 10 17 P5CA9600799 1 19961007 A 7110 RIVETS BOEING 747 747122 1384872 NM NR 2 ENGINE MISSING A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 MANY MISSING AND PULLING THROUGH RIVETS ON NR 2 ENGINE EXHAUST SLEEVE. REPLACED RIVETS PER BAC SRM 51-30-02. 2 L 7 4 4F A20WE 1996101700935 19961017 00935 NM 1996 10 17 P5CA9600800 1 19961007 A 5400 DOUBLER BOEING 747 747122 1384872 NM NR 2 PYLON DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 DAMAGED AND WORN SKIN DOUBLER ON NR 2 PYLON AFT OF ENGINE MOUNT AREA. FABRICATED AND INSTALLED NEW FILLER AND DOUBLER P ER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1996101700936 19961017 00936 NM 1996 10 17 P5CA9600801 1 19961007 A 7110 RIVETS BOEING 747 747122 1384872 NM NR 3 ENG FAIRING MISSING A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 MISSING AND PULLED THROUGH RIVETS AT ABOUT 30 PLACES ON LEFT AND RIGHT SKIRT FAIRING ON NR 3 ENGINE. REPLACED RIVETS ON LEFT AND RIGHT SKIRT FAIRINGS PER BAC SRM 51-30-02. 2 L 7 4 4F A20WE 1996101700937 19961017 00937 NM 1996 10 17 P5CA9600802 1 19961007 A 7110 COWL BOEING 747 747122 1384872 NM NR 2 ENGINE FAN DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 SEVERAL DENTS ON NR 2 ENGINE OUTBOARD FAN COWL. REPAIRED WITH HOT BOND FILLER AND DOUBLER PER BAC SRM 51-40-06 AND PAIN TED PER BAC SRM 51-24-11. 2 L 7 4 4F A20WE 1996101700938 19961017 00938 WP 1996 10 17 RRXA96117 1 19961002 A 5350 56583512 FILLET PANEL DOUG DC8 DC863 302198A WP BS 718 DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 796AL 46054 DURING PREFLIGHT FOUND 17 BY 24 HOLE ON RING WING FILLET PANEL (P/N 5658351-2), PANEL NUMBER 261H, AT Y=718. REPAIRED R ING WING FILLET PANEL BY FABRICATING EXTERNAL DOUBLER AND INSTALLED IAW PER DRAWING B36-RO1, TEMPORARY REPAIR. PANEL NU MBER 261H WAS REMOVED AND REPLACED AT DAYTON OHIO ON 96/10/03, IAW DC-8 MAINTENANCE MANUAL. 2 L 7 4 4F 4A25 1996101700939 19961017 00939 SO 1996 10 17 SRAA961007 1 19961013 A 5320 FITTING LKHEED 382 382G 526414U SO BS 557 CRACKED A SRAA K NONE O OTHER IN INSP/MAINT 1 GL 23 921SJ 4586 POST FLIGHT INSPECTION, FOUND BOW BEAM FITTING ON LEFT HAND SIDE FS 557 CRACKED. ACCOMPLISHED BOW BEAM FITTING REPAIR P ER LOCKHEED SRM 53-40-12. 2 H 7 4 4T A1SO 1996101700940 19961017 00940 SO 1996 10 17 SRAA961008 1 19961014 A 7810 23052623 TAILCONE LKHEED 382 382B 5264104 SO NR 1 ENGINE DAMAGED A A SRAA K NONE D INFLIGHT SEPARATION LD LANDING 1 GL 23 907SJ 4248 DURING LANDING NR 1 ENGINE TAILCONE DEPARTED FROM AIRCRAFT. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED NR 2 ENGINE REA R SCAVENGE PUMP CONE PER MM CH 72. 2 H 7 4 4T A1SO 1996101800001 19961018 00001 WP 1996 10 18 CALA960147S 1 19961005 A 5330 SKIN DOUG DC9 DC982 3022082 WP CARGO DR CUTOUT TORN A CALA K NONE O OTHER TX TAXI/GRND HDL 1 SW 09 98876 49444 INSPECTION FOUND ALL SKIN LAYERS TORN 1.5 INCH DEEP AT MID CARGO DOOR FRAME LOWER AFT CORNER. A DOUBLER AND TRIPLER WE RE INSTALLED IAW ECRA 5330-02447. 2 L 7 2 4F A6WE 1996101800002 19961018 00002 WP 1996 10 18 MWEA96567 1 19961011 A 5330 59114121 SKIN DOUG DC9 DC914 3022034 WP BS 229-484 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 DURING D-CK, FOUND FWD CARGO BELLY SKIN STA 229 THROUGH 484 LONG 26L, 26R HAS EXISTING SCAB PATCH REPAIRS AT FIVE ANTENN A LOCATIONS. REPLACED BELLY SKIN STA 229 THROUGH 484, LONG 226L, 26R IAW SRM 53-01. 2 L 7 2 4F A6WE 1996101800003 19961018 00003 WP 1996 10 18 GRAA9670 1 19960703 A 3350 0816300609 LIGHT DOUG DC9 DC987 3022087 WP CABIN LOOSE A GRAA K NONE L NO TEST IN INSP/MAINT 1 WP 11 750RA 49777 LINE MAINTENANCE AT IFP, DISCOVERED THAT EMERGENCY FLOOR PATH LIGHT STRIP CAME LOOSE IN PASSENGER CABIN. MAINTENANCE SE CURED THE EMERGENCY FLOOR TRACK LIGHT STRIP. MAINTENANCE PERFORMED OPERATIONAL CHECK OF THE SYSTEM. NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A6WE 1996101800004 19961018 00004 WP 1996 10 18 GRAA9671 1 19960801 A 3350 100865 BATTERY PACK DOUG DC9 DC987 3022087 WP CABIN DISCHARGED A GRAA K NONE L NO TEST IN INSP/MAINT 1 WP 11 1074T 49727 MAINTENANCE FOUND EMERGENCY FLOOR LIGHTING INOP FROM ROW 22 AFT WHILE PERFORMING A T/O. REMOVED AND REPLACED THE BATTER Y PACK. SYSTEM OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A6WE 1996101800005 19961018 00005 SW 1996 10 18 MALA965166 1 19960920 A 3260 1EN516 POSITION SWITCH SWRNGN SA227 SA227AC 8780603 SW LT MLG FAILED A MALA O OTHER N FALSE WARNING CL CLIMB 1 GL 15 439MA AC722 FLT 3201 - AFTER TAKEOFF FROM YQT, THE LEFT GEAR INTRANSIT LIGHT FAILED TO ILLUMINATE DURIG GEAR RETRACTION. THE AIRCRA FT CONTINUED TO MSP WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT GEAR UP POSITION SWITCH. ALL CHECKS SATISF ACTORY. (M) 2 L 7 2 4T RT A8SW 1996102200001 19961022 00001 WP 1996 10 22 UPS96821263 1 19960830 A 5755 56551672 SKIN DOUG DC8 DC873F 302199F WP NR 3 SPOILER DELAMINATION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. NR 3 SPOILER PANEL DELAMINATED ON RT WING. REPLACED SPOILER PER MM 27-61-01. 2 L 7 4 4F RT 4A25 1996102300001 19961023 00001 NM 1996 10 23 UPS96621224 1 19961002 A 7931 41809104 OIL PRESS TRANS BOEING 767 76734AF 1385212 NM GE CF6 CF680C2B7 NE LT ENGINE INOPERATIVE A IPXA E D ENGINE SHUTDOWN RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 303UP 27241 704300 BLOCK TURN BACK, LEFT OIL PRESSURE EICAS IN AMBER. DECREASE TO RED RANGE. READ 8 PSI, SHUT ENGINE DOWN AND RETURNED TO RAMP. OIL PRESSURE LIGHT NOT ILLUM. REMOVED AND REPLACED LEFT ENGINE OIL PRESSURE TRANSMITTER, LEAK AND OPS CK'D OK. P/N OFF 418-09104. S/N OFF 9501031. P/N ON 418-09104. S/N ON 9537088. 2 L 7 2 4F 4 F RT A1NM E13NE 1996102300002 19961023 00002 NM 1996 10 23 96UAL900745 1 19960924 A 3350 BATTERY BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 991UA 21981 EMERGENCY EGRESS LIGHTING INOP ROW 1AB. REPLACED EEL BATTERY. OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F A16WE E2EA 1996102300003 19961023 00003 NM 1996 10 23 96UAL900746 1 19960924 A 3350 CONNECTOR BOEING 737 737522 138449F NM CABIN DISCONNECTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 929UA 26652 15 FEET OF EMERGENCY EGRESS LIGHTING INOPERATIVE. RECONNECTED EMERGENCY EGRESS LIGHTING STRIP. OPERATION CHECKS NORMA L. 2 L 7 2 4F RT A16WE 1996102300005 19961023 00005 WP 1996 10 23 RRXA96088 1 19961003 A 3230 RETRACT MECH DOUG DC8 DC8F54 3021926 WP LANDING GEAR MALFUNCTIONED A RRXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 15 991CF 45801 LANDING GEAR WOULD NOT RETRACT AFTER TAKE0FF. AIRCRAFT MADE SUDDEN HARD PULL TO LEFT JUST BEFORE ROTATION. INSPECTED L ANDING GEAR, NO DEFECTS NOTED. OPS CHECKED LANDING GEAR LEVER GOOD IAW MM CH 32-6-1, OPS CHECK GOOD ON GEAR SWING. 2 L 7 4 4F 4A25 1996102300016 19961023 00016 NM 1996 10 23 96ZZZX5184 1 19960823 A 2120 AIR DISTR BOEING 767 767330 NM CABIN ODOR A TWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 691LF 25137 LAX - FLT 15 - DURING CRUISE, AN ODOR OF OVERHEATED RUBBER WAS OBSERVED AT SEAT ROWS 32 TO 38, RIGHT SIDE. INSPECTED AR EA OF SEAT ROWS 32 TO 38 AND CARGO BIN AREA. NO OVERHEAT INDICATIONS OR DEFECTS FOUND. UNABLE TO DUPLICATE AND NO ODOR S WERE OBSERVED. CHECK C-5B - 7-24-96 - LAX. 2 L 7 2 4F RT A1NM 1996102400004 19961024 00004 CE 1996 10 24 96ZZZX5247 1 19960111 A 3710 442CW PUMP AIRBORNE CESSNA 414 414A 2075907 CE LT VACUUM PUMP SHAFT SHEARED A CWNA K NONE O OTHER IN INSP/MAINT 1 WP 09 414RW 30 5K550 414A0295 FOLLOWING PUMP REMOVAL FOR FAILURE, FOUND DRIVE SHAFT SHEARED. THIS IS A VACUUM TYPE SYSTEM. 1 L 7 2 3O A7CE 1996102400007 19961024 00007 CE 1996 10 24 96ZZZX5250 1 19960707 A 3710 442CW PUMP AIRBORNE CESSNA 414 414A 2075907 CE RT VACUUM PUMP SHAFT SHEARED A CWNA K NONE O OTHER IN INSP/MAINT 1 WP 09 414RW 109 12AD1583 414A0295 FOLLOWING PUMP REMOVAL FOR FAILURE, FOUND DRIVE SHAFT SHEARED. THIS IS A VACUUM TYPE SYSTEM. 1 L 7 2 3O A7CE 1996102400008 19961024 00008 CE 1996 10 24 96ZZZX5251 1 19960723 A 3710 442CW PUMP AIRBORNE CESSNA 414 414A 2075907 CE RT VACUUM PUMP SHAFT SHEARED A CWNA K NONE O OTHER IN INSP/MAINT 1 WP 09 414RW 2 064699 414A0295 FOLLOWING PUMP REMOVAL FOR FAILURE, FOUND DRIVE SHAFT SHEARED. THIS IS A VACUUM TYPE SYSTEM. 1 L 7 2 3O A7CE 1996102400009 19961024 00009 CE 1996 10 24 96ZZZX5252 1 19960731 A 3710 442CW PUMP AIRBORNE CESSNA 414 414A 2075907 CE RT VACUUM PUMP SHAFT SHEARED A CWNA K NONE O OTHER IN INSP/MAINT 1 WP 09 414RW 2 064899 414A0295 FOLLOWING PUMP REMOVAL FOR FAILURE, FOUND DRIVE SHAFT SHEARED. THIS IS A VACUUM TYPE SYSTEM. 1 L 7 2 3O A7CE 1996102400018 19961024 00018 CE 1996 10 24 96ZZZX5261 1 19960909 A 3241 40955 TRANSDUCER CESSNA 500 550 2076604 CE ANTI-SKID INOPERATIVE A FRKA K NONE O OTHER IN INSP/MAINT 1 NE 01 245CC 3305 2568 5500212 DURING MAINTENANCE INSPECTION, NOTED THAT ANTI-SKID SYSTEM WAS INOPERATIVE. TROUBLESHOOTING OF SYSTSEM SHOWED LEFT WHEE L SPEED TRANSDUCER INOPERATIVE. TRANSDUCER REPLACED WITH OVERHAULED UNIT AND SYSTEM WORKED WITHIN LIMITS. 1 L 7 2 4F A22CE 1996102400033 19961024 00033 NE 1996 10 24 PLG92796JG1 2 19960927 A 7510 ANTI-ICE SYSTEM SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE RT ENGINE MALFUNCTIONED A PLGA O OTHER J WARNING INDICATION DE DESCENT 1 NE 05 745BA 340A111 FLT 4889 - BOS-ROC - DURING FLIGHT, IN HEAVY CLOUDS AND ICING CONDITION, THE RIGHT AIR VALVE LIGHT CAME ON WHEN DESCENDI NG TO A LOWER ALTITUDE. THE RIGHT ENGINE EXPERIENCED TWO POWER INTERRUPTIONS JUST AFTER LEAVING ICING. THE CREW ATTEMP TED TO ADD POWER AND THE RIGHT ENGINE SHUT ITSELF DOWN. THE IGNITION LIGHT CAME ON AND NO OVERTEMP DURING SHUTDOWN. T HE AIRCRAFT WAS REPOSITIONED TO PSM. MAINTENANCE REPLACED AISBV, GARRETT VALVES AND IGNITOR PLUGS. AIRCRAFT OPERATED S ATISFACTORY. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 1996102400035 19961024 00035 SW 1996 10 24 HEEA968132 1 19961004 A 6220 206011149105 YOKE BELL 206 206L1 1182107 SW M/R CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 YOKE IS CORRODED. (CORROSION ON BEARING JOURNALS) 1 G 7 1 3U H2SW 1996102400036 19961024 00036 SW 1996 10 24 HEEA968133 1 19961004 A 5302 206033412123A HANGER BRACKET 206033004011 BELL 206 206L1 1182107 SW TAILBOOM MIS MFG E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 AOKP00677 HANGER BRACKET FOUND TO BE MIS-MANUFACTURED. 1 G 7 1 3U H2SW 1996102400037 19961024 00037 SW 1996 10 24 HEEA968134 1 19961004 A 6220 412010427101 BEARING 412010405109 BELL 412 412 1182202 SW M/R LOOSE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 108X 43 A1591 33115 BEARING UNSTAKED. PART SCRAPPED LOCALLY. 1 G 7 2 4U H4SW 1996102400038 19961024 00038 SW 1996 10 24 HEEA968135 1 19961004 A 6220 412010427101 BEARING 412010405109 BELL 412 412 1182202 SW M/R LOOSE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 108X 43 A1587 33115 BEARING UNSTAKED. PART SCRAPPED LOCALLY. 1 G 7 2 4U H4SW 1996102400039 19961024 00039 GL 1996 10 24 HEEA968136 2 19961004 A 7240 23056108 COMB LINER 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL MID SKIRT NOT WELDED E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 5421E CAT38001F S806 CAE833901 RECEIVING INSPECTION REVEALED: MID SKIRT NOT WELDED TO LOWER SKIRT ON COMBUSTION LINER AS MARKED. REPLACED DISCREPANT P ART. 1 G 7 2 3U 3 U H3EU E4CE 1996102400040 19961024 00040 SW 1996 10 24 HEEA968137 1 19961004 A 6510 206040338009 HANGER ASSY BELL 206 206B3 1181506 SW T/R DRIVE OUT OF LIMIT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2268G 3603 REMOVED PER ASB 206-95-86 REV. A. (SPRING I.D. OUT OF LIMITS) 1 G 7 1 3U H2SW 1996102400041 19961024 00041 SW 1996 10 24 HEEA968138 1 19961004 A 6510 206040338009 HANGER ASSY BELL 206 206B3 1181506 SW T/R DRIVE OUT OF LIMITS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2275Y 3626 REMOVED PER ASB 206-95-86 REV. A. (SPRING I.D. OUT OF LIMITS) 1 G 7 1 3U H2SW 1996102400042 19961024 00042 SW 1996 10 24 HEEA968139 1 19961004 A 6510 206040355001 HANGER ASSY BELL 206 206B3 1181506 SW T/R DRIVE OUT OF LIMITS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2275Y 3626 REMOVED PER ASB 206-95-86 REV. A. (SPRING I.D. OUT OF LIMITS) 1 G 7 1 3U H2SW 1996102400043 19961024 00043 SW 1996 10 24 HEEA968140 1 19961004 A 6510 206040355001 HANGER ASSY BELL 206 206B3 1181506 SW T/R DRIVE OUT OF LIMITS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 103PH 3000 REMOVED PER ASB 206-95-86 REV. A. (SPRING I.D. OUT OF LIMITS) 1 G 7 1 3U H2SW 1996102400044 19961024 00044 SW 1996 10 24 HEEA968141 1 19961004 A 6510 206040355003 HANGER ASSY BELL 206 206L3 1182108 SW T/R DRIVE OUT OF LIMITS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8591X 51495 REMOVED PER ASB 206L-95-101 REV. A. (SPRING I.D. OUT OF LIMITS) 1 G 7 1 3U H2SW 1996102400045 19961024 00045 SW 1996 10 24 HEEA968142 1 19961004 A 6510 206040355003 HANGER ASSY BELL 206 206L1 1182107 SW T/R DRIVE OUT OF LIMITS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2772A 45311 REMOVED PER ASB 206L-95-101 REV. A. (SPRING I.D. OUT OF LIMITS) 1 G 7 1 3U H2SW 1996102400046 19961024 00046 SW 1996 10 24 HEEA968143 1 19961004 A 6510 206040346021 HANGER ASSY BELL 206 206L1 1182107 SW T/R DRIVE OUT OF LIMITS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2253E 45758 REMOVED PER ASB 206L-95-101 REV. A. (SPRING I.D. OUT OF LIMITS) 1 G 7 1 3U H2SW 1996102400047 19961024 00047 SW 1996 10 24 HEEA968144 1 19961004 A 6510 206040344009 HANGER ASSY BELL 206 206L1 1182107 SW T/R DRIVE OUT OF LIMITS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5737T 45454 REMOVED PER ASB 206L-95-101 REV. A. (SPRING I.D. OUT OF LIMITS) 1 G 7 1 3U H2SW 1996102400048 19961024 00048 SW 1996 10 24 HEEA968145 1 19961004 A 6510 206040344009 HANGER ASSY BELL 206 206L1 1182107 SW T/R DRIVE OUT OF LIMITS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2761X 45283 REMOVED PER ASB 206L-95-101 REV. A. (SPRING I.D. OUT OF LIMITS) 1 G 7 1 3U H2SW 1996102400049 19961024 00049 SW 1996 10 24 HEEA968146 1 19961004 A 6510 206040344009 HANGER ASSY BELL 206 206L1 1182107 SW T/R DRIVE OUT OF LIMITS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2135V 45657 REMOVED PER ASB 206L-95-101 REV. A. (SPRING I.D. OUT OF LIMITS) 1 G 7 1 3U H2SW 1996102400050 19961024 00050 SW 1996 10 24 HEEA968147 1 19961004 A 6510 206040344009 HANGER ASSY BELL 206 206L1 1182107 SW T/R DRIVE OUT OF LIMITS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 50046 45173 REMOVED PER ASB 206L-95-101 REV. A. (SPRING I.D. OUT OF LIMITS) HELD AT PHI FOR CSR SIGNATURE. PHI REQUESTS FOR WARRANT Y CREDIT AGAINST REPLACEMENT PART PURCHASED AS OUTLINED IN ASB. 1 G 7 1 3U H2SW 1996102400051 19961024 00051 SW 1996 10 24 HEEA968148 1 19961004 A 6510 206040344009 HANGER ASSY BELL 206 206L1 1182107 SW T/R DRIVE OUT OF LIMITS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5014V 45217 REMOVED PER ASB 206L-95-101 REV. A. (SPRING I.D. OUT OF LIMITS) 1 G 7 1 3U H2SW 1996102400052 19961024 00052 SW 1996 10 24 HEEA968149 1 19961004 A 6510 206040344009 HANGER ASSY BELL 206 206L1 1182107 SW T/R DRIVE OUT OF LIMITS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5748Q 45499 REMOVED PER ASB 206L-95-101 REV. A. (SPRING I.D. OUT OF LIMITS) 1 G 7 1 3U H2SW 1996102400053 19961024 00053 SW 1996 10 24 HEEA968150 1 19961004 A 6510 206040344009 HANGER ASSY BELL 206 206L1 1182107 SW T/R DRIVE OUT OF LIMITS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5745N 45489 REMOVED PER ASB 206L-95-101 REV. A. (SPRING I.D. OUT OF LIMITS) 1 G 7 1 3U H2SW 1996102400054 19961024 00054 SW 1996 10 24 HEEA968152 1 19961007 A 6220 214010248101 SEAL 214010100207 BELL 214 214ST 1182106 SW M/R UNBONDED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 1624 A529 28106 RUBBER UNBONDED FROM METAL RING. RUBBER BOOT APPEARS TO BE DRY ROTTED. 2 G 7 2 4U H10SW 1996102400055 19961024 00055 SW 1996 10 24 HEEA968153 1 19961007 A 5320 206033412123A HANGER BRACKET BELL 206 206L1 1182107 SW FUSELAGE MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 HANGER BRACKET MISMANUFACTURED. 1 G 7 1 3U H2SW 1996102400056 19961024 00056 SW 1996 10 24 HEEA968156 1 19961009 A 2420 1820300150 SHUNT BELL 230 230 1182149 SW AC SYS DEFECTIVE E HEEA K NONE H ELECT. POWER LOSS-50 PC IN INSP/MAINT 1 SW 03 230UN 3035 23009 CAUSING OPPOSITE GENERATOR TO DROP OFF LINE. 1 G 7 2 3U NC H9SW 1996102400057 19961024 00057 SW 1996 10 24 HEEA968157 1 19961009 A 6400 222012715101 LEVER ASSY BELL 230 230 1182149 SW T/R BEARING WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 1107 23009 PIVOT BEARING WORN. 1 G 7 2 3U NC H9SW 1996102400058 19961024 00058 SW 1996 10 24 HEEA968158 1 19961009 A 6330 222331618105 ISOLATION MOUNT BELL 230 230 1182149 SW M/R XMSN ERRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 434 23009 TEFLON ERRODED AND BEARING GALLED. 1 G 7 2 3U NC H9SW 1996102400059 19961024 00059 SW 1996 10 24 HEEA968159 1 19961009 A 3340 900601 LIGHT BELL 230 230 1182149 SW SEARCH LIGHT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 1410 23009 LIGHT WILL NOT COME ON. 1 G 7 2 3U NC H9SW 1996102400060 19961024 00060 SW 1996 10 24 HEEA968160 1 19961009 A 6400 222012711107 LINK ASSY BELL 230 230 1182149 SW T/R COUNTERWT HOUSING LOOSE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 1621 23009 BEARING HOUSING LOOSE IN LINK. (T/R COUNTERWEIGHT) 1 G 7 2 3U NC H9SW 1996102400061 19961024 00061 SW 1996 10 24 HEEA968161 1 19961009 A 6220 222310117105 SPRING BELL 230 230 1182149 SW M/R FLAPPING SEPARATION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 3022 23009 SEPARATION OF FLAPPING SPRINGS. SERIAL NUMBERS REMOVED LK0208M AND LK0181M. 1 G 7 2 3U NC H9SW 1996102400062 19961024 00062 SW 1996 10 24 HEEA968162 1 19961009 A 5210 1008402 LATCH ASSY BELL 230 230 1182149 SW RT DOOR BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 172 23009 PILOT'S DOOR LATCH BROKEN. 1 G 7 2 3U NC H9SW 1996102400063 19961024 00063 SW 1996 10 24 HEEA968163 1 19961009 A 5210 1008402 LATCH ASSY BELL 230 230 1182149 SW RT DOOR CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 666 23009 PITLOT DOOR LATCH MECHANISM CRACKED. 1 G 7 2 3U NC H9SW 1996102400064 19961024 00064 SW 1996 10 24 HEEA968164 1 19961009 A 7810 230063301101 EXHAUST DUCT BELL 230 230 1182149 SW NR 1 ENG CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 1115 23009 EXHAUST DUCT CRACKED ON #1 ENGINE. 1 G 7 2 3U NC H9SW 1996102400065 19961024 00065 NE 1996 10 24 HEEA968167 2 19961009 A 7200 0292005220 ENGINE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE OIL SYS MAKING METAL E HEEA K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 03 6097Z 2429 2820 LOW OIL PRESSURE, STARTING TO MAKE METAL ON UPPER ELECTRIC PLUG. 1 G 7 1 3U 3 U H9EU E19EU 1996102400067 19961024 00067 1996 10 24 HEEA968170 4 19961010 A 3444 7001840913 TRANSCEIVER BELL 212 212 1181420 SW COCKPIT WILL NOT TEST E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5736J 31140 TRANSCEIVER WILL NOT TEST. TIME SINCE REPAIR 75:50. 1 G 7 1 4U H4SW 1996102400068 19961024 00068 EU 1996 10 24 HEEA968171 1 19961010 A 6210 10515141 BLADE BOLKMS 105 BO105S 5626006 EU M/R SEPARATION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5029H 5931 S670 SEPARATION ON LEADING EDGE ABRASION STRIP ON THE NO. ONE OUTBOARD END AND THE NO.ONE CENTER INBOARD END LOWER SIDE. 1 G 7 2 3U H3EU 1996102400069 19961024 00069 1996 10 24 HEEA968172 4 19961010 A 3453 25410038 7000 CDU SKRSKY S76 S76A 8143006 NE COCKPIT LORAN DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545K 760047 SEVERAL LED SEGMENTS ARE INOPERATIVE. 1 G 7 2 3U H1NE 1996102400070 19961024 00070 1996 10 24 HEEA968173 4 19961010 A 3451 066106602 TRANSCEIVER SKRSKY S76 S76A 8143006 NE COCKPIT DME DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31219 760230 UNIT DRAWS TOO MUCH CURRENT AND NEED TO UPDATE MODS. 1 G 7 2 3U H1NE 1996102400071 19961024 00071 EU 1996 10 24 HEEA968174 1 19961010 A 6310 4638202007 CLUTCH 4638001004 BOLKMS 105 BO105S 5626006 EU FREEWHEEL BROKEN RIBBON E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6607K 1347 1311 S841 S/N 3692 BROKEN ENERGIZING RIBBON. S/N 3780 WORN INNER CAGE. REPLACED WITH SERVICEABLE CLUTCHES. 1 G 7 2 3U H3EU 1996102400072 19961024 00072 1996 10 24 HEEA968175 4 19961010 A 3452 066106200 TRANSCEIVER KT76 SNIAS 350 AS350B2 8680813 EU COCKPIT ATC INTERMITTENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4034Q 2918 INTERMITTENT SIGNAL. 1 G 7 1 3U H9EU 1996102400073 19961024 00073 1996 10 24 HEEA968176 4 19961010 A 2312 063100700 TRANSCEIVER KTR993 AEROSP SA316 SA315B 8680615 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3207T 2441 DOES NOT TRANSMIT OR RECEIVE. 1 G 7 1 4U H1IN 1996102400074 19961024 00074 1996 10 24 HEEA968177 4 19961010 A 2312 064101501 TRANSCEIVER KTR953 BELL 212 212 1181420 SW COCKPIT MALFUNCTION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5010F 30936 FREQUENCY DOES NOT SHOW TILL 20 OR 30 MINUTES. 1 G 7 1 4U H4SW 1996102400076 19961024 00076 1996 10 24 HEEA968179 4 19961010 A 2312 071104302 CONTROL KFS570B BELL 212 212 1181420 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1082G 31109 DOESN'T COME ONE. CLEANED ON/OFF SWITCH AND RESOLDERED COLD SOLDER JOINT ON SWITCH. REPAIRED. ALSO FOUND "IDENT" AND " TEST" SWITCHES INTERMITTENT. REPLACED "IDENT" (S106) P/N 031-0061-00 AND "TEST" (S108) P/N031-0061-00. REPAIRED. ALSO REPLACED MISSING BOTTOM COVER P/N 047-01366-0001. REPAIRED. BENCH CHECK GOOD. 1 G 7 1 4U H4SW 1996102400077 19961024 00077 1996 10 24 HEEA968180 4 19961010 A 3455 071121009 CONTROL BELL 412 412 1182202 SW COCKPIT ADF INTERMITTENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 INTERMITTENT AND HALF OF DISPLAY NOT USUABLE. PERFORMED PRELIMINARY INSPECTION, FOUND PHOTOCELL (V301) DIMMING. REPLACE D PHOTOCELL (V301), ALSO FOUND LIGHTING INOPERATIVE. REPLACED 28V BULB. REPAIRED. BENCH CHECK GOOD. 1 G 7 2 4U H4SW 1996102400078 19961024 00078 1996 10 24 HEEA968181 4 19961010 A 3422 200DCL GYRO BELL 407 407 SW COCKPIT DG PRECESSING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407PH 53003 REPORTED UNIT PRECESSING EXCESSIVELY. 1 G 7 1 3U O H2SW 1996102400079 19961024 00079 1996 10 24 HEEA968182 4 19961010 A 3444 066304401 INDICATOR BOLKMS 117 BK117A3 5626015 EU INST LIGHTS LIGHTS INOP E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 401PH 7050 INSTRUMENT LIGHTS ON 1/2 WORK. FOUND 4 BURNT LAMPS. PERFORMED PRELIMINARY INSPECTION. REPLACED 4 EACH LAMPS. PERFORME D COMPLETE CALIBRATION AND ALIGNMENT. BENCH CHECK GOOD. 1 G 7 2 3U H13EU 1996102400080 19961024 00080 1996 10 24 HEEA968183 4 19961010 A 2312 4000106010 CONTROL UNIT C10 BOLKMS 105 BO105S 5626006 EU COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 205UC S668 THIRD THUMBWHEEL WHEN ADJUSTED HAS NO LED READOUT. CLEANED THUMBWHEEL. NO HELP. REPLACED THUMBWHEEL S1. REPAIRED. IN STALLED 5 EACH MISSING SCREWS FOR FACEPLATE. BENCH CHECK GOOD. 1 G 7 2 3U H3EU 1996102400081 19961024 00081 1996 10 24 HEEA968184 4 19961010 A 2312 071121612 CONTROL UNIT BOLKMS 117 BK117A3 5626015 EU COCKPIT MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911NC 7026 ADJUSTMENT KNOBS FOR FREQUENCY CHANGE DON'T WORK PROPERLY. PERFORMED PRELIMINARY INSPECTION. CLEANED WAFERS, FOUND PHOT OCELL (V101) NOT DIMMING. REPLACED V101 PHOTOCELL. REPAIRED. RAISED HEADER (P101) AND APPLIED HUMISEAL. ALSO REPLACE D 28V BULB (DS301). REPAIRED. BENCH CHECK GOOD. 1 G 7 2 3U H13EU 1996102400082 19961024 00082 1996 10 24 HEEA968185 4 19961010 A 3455 066107700 RECEIVER BELL 412 412 1182202 SW COCKPIT ADF INTERMITTENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K 36001 INTERMITTENT AUDIO SIGNAL. PERFORMED PRELIMINARY INSPECTION AND FOUND CORROSION AND BURN SPOT ON MAIN BOARD. CLEANED CO RROSION AND SCRAPED CARBON OUT AND CLEANED MAIN BOARD. REPLACED CORRODED INTEGRATED CIRCUITS I323 AND I324, ALSO CORROD ED CAPACITOR C380. REPAIRED OPENFAIL FROM CAPACITOR C364 TO RESISTOR R397 DUE TO BURN SPOT. FOUND UNIT DOES NOT POINT CORRECTLY IN "ANT" MODE. FOUND OUTPUT OF INTEGRATED CIRCUIT I319 TO BE SHORTED TO GROUND. REPLACED INTEGRATED CIRCUIT I319. NO HELP. CONTINUEDTROUBLESHOOTING AND FOUND SILVER MIGRATION FROM NUT WHICH HOLDS POWER SUPPLY TO BE SHORTING ON TO OUTPUT LINE OF INTEGRATED CIRCUIT I319. REMOVED SILVER MIGRATION AND REPAIRED. BENCH CHECK GOOD. 1 G 7 2 4U H4SW 1996102400083 19961024 00083 1996 10 24 HEEA968186 4 19961010 A 3451 066106900 INDICATOR KDI572 BOLKMS 117 BK117A4 5626017 EU COCKPIT INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911RZ 7092 REMOVED FOR TROUBLESHOOTING, DID NOT CURE PROBLEM. FOUND DISPLAY DIGITS INOPERATIVE. REPLACED BAD DS901 DISPLAY. CLEAN ED DISPLAY CONTACTS, APPLIED HUMISEAL TO PREVIOUSLY DONE HEADER MOD. UNIT BENCH CHECK GOOD. 1 G 7 2 3U H13EU 1996102400084 19961024 00084 1996 10 24 HEEA968187 4 19961010 A 2211 7000298901 COMPUTER BELL 412 412 1182202 SW COCKPIT AFCS ERRATIC E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22347 36005 AFCS COMPUTER LIGHTS ERRATIC. 1 G 7 2 4U H4SW 1996102400121 19961024 00121 WP 1996 10 24 CALA9601473 1 19961016 A 5755 SUPPORT LEG DOUG DC9 DC982 3022082 WP SPOILER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 809NY 49263 FOUND OUTBOARD SUPPORT BRACKET OF LEFT HAND GROUND SPOILER UPPER AFT LEG WITH ONE INCH CRACK IN SUPPORT LEG. REPLACED C ROSS BRACE PER EC/RA 5710-01756. 2 L 7 2 4F A6WE 1996102400122 19961024 00122 WP 1996 10 24 CALA9601476 1 19961003 A 5311 995823823 FRAME DOUG DC9 DC982 3022082 WP BS 1418 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14816 49370 BELT FRAME CRACKED AT STATION 1418 LONG 2 LT AND RT 1. REPAIRED BELT FRAME PER SRM 53-03-32. 2 L 7 2 4F A6WE 1996102400123 19961024 00123 NM 1996 10 24 CALA9601477 1 19961011 A 5330 SKIN BOEING 737 7373T0 1384582 NM BS 272 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17321 23372 LOWER FUSELAGE SKIN UNDER NUMBER 3 VHF ANTENNA CRACKED JUST AFT OF STATION 727D. INSTALLED FILLER AND DOUBLER PER SRM 5 3-00-01. 2 L 7 2 4F RT A16WE 1996102400124 19961024 00124 NM 1996 10 24 CALA9601478 1 19961013 A 5330 SKIN BOEING 737 7373T0 1384582 NM AFT FUSE FRETTING A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17321 23372 AFT FUSELAGE AT DORSAL FIN ASSEMBLY FORWARD RIGHT AND LEFT SKIN FRETTING WHERE SEAL RIDES. FABRICATED AND INSTALLED DOU BLER PER SRM 53-00-01 FIG 201 SHEETS 1 TO 3. 2 L 7 2 4F RT A16WE 1996102400125 19961024 00125 WP 1996 10 24 CALA9601479 1 19961017 A 2560 1131DGACR SLIDE DOUG DC9 DC982 3022082 WP L1 DOOR FELL OFF A CALA K NONE O OTHER TX TAXI/GRND HDL 1 SW 09 35836 169 49441 FORWARD ENTRY DOOR SLIDE FELL OFF DOOR. REINSTALLED SLIDE PACK PER MAINTENANCE MANUAL. 2 L 7 2 4F A6WE 1996102400126 19961024 00126 WP 1996 10 24 CALA9601480 1 19961017 A 3234 HANDLE DOUG DC10 DC1010 3022110 WP LANDING GEAR LACK OF LUBE A CALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SW 09 68046 47800 ON GEAR EXTENSION CREW REPORTED THREE GEAR UNSAFE LIGHTS. USED EMERGENCY EXTENSION HANDLE TO GET THREE GREEN LIGHTS. A FTER NORMAL LANDING, UNABLE TO RESTOW ALTERNATE GEAR HANDLE. RESECURED ALTERNATE GEAR HANDLE. CLEANED AND LUBRICATED L ANDING GEAR HANDLE AND CYCLED SEVERAL TIMES, NO DEFECTS WERE NOTED. 2 L 7 3 4F A22WE 1996102400127 19961024 00127 NM 1996 10 24 CALA9601481 1 19961003 A 5330 SKIN BOEING 737 737222 1384473 NM BS 727 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10236 19937 FUSELAGE SKIN CRACKED IN 2 PLACES ON LEFT SIDE BETWEEN STA 727A AND 727B AT STRINGER 18 APPROX 3 EACH. CUT OUT DAMAGED AREA, FABRICATED FILLER AND EXTERNAL DOUBLER AND INSTALLED PER SRM 53-30-3, 53-30-2, AND 51-10-2. 2 L 7 2 4F A16WE 1996102400128 19961024 00128 NM 1996 10 24 CALA9601482 1 19961003 A 5312 BULKHEAD BOEING 737 737222 1384473 NM BS 178 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10236 19937 FORWARD FACE OF FORWARD PRESSURE BULKHEAD STATION 178 CRACKED ON RIGHT SIDE ABOVE WL STA 208, APPROX 8. CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND FILLERS, INSTALLED PER SRM 53-10-11, 53-30-2, AND 51-10-2. 2 L 7 2 4F A16WE 1996102400129 19961024 00129 NM 1996 10 24 CALA9601483 1 19961003 A 5312 BLKHD WEB BOEING 737 737222 1384473 NM BS 178 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10236 19937 FORWARD FACE OF FORWARD PRESSURE BULKHEAD STATION 178 CRACKED ON LEFT SIDE ABOVE WL 208 APPROX 8. CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND FILLER, INSTALLED PER SRM 53-10-11, 51-30-2, AND 51-10-2. 2 L 7 2 4F A16WE 1996102400130 19961024 00130 NM 1996 10 24 CALA9601484 1 19961003 A 5330 SKIN BOEING 737 737222 1384473 NM BS 390 OIL CAN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10236 19937 FUSELAGE SKIN OIL CAN AT BS 390L AND STR 17L. TRIMMED OUT DAMAGED AREA PER SRM 53-30-3, FABRICATED DOUBLER PER SRM 53-3 0-3 AND 51-10-2, INSTALLED DOUBLER PER SRM 53-30-3 AND 51-30-2. 2 L 7 2 4F A16WE 1996102400131 19961024 00131 NM 1996 10 24 CALA9601485 1 19961003 A 5330 SKIN BOEING 737 737222 1384473 NM BS 235.8-251.8 BULGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10236 19937 EXTERIOR SKIN ON LEFT SIDE NOSE WHEEL WELL EDGE HAS BULGES AND RIVETS PULLING THROUGH FROM STATION 235.8 TO 251.8. CUT OUT DAMAGED AREA, FABRICATED FILLER AND DOUBLER, INSTALLED PER SRM 53-30-3, 51-30-2, AND 51-10-2. 2 L 7 2 4F A16WE 1996102400132 19961024 00132 NM 1996 10 24 CALA9601486 1 19961012 A 3350 BATTERY PACK BOEING 737 737222 1384473 NM L2 DOOR DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 10236 19937 L2 DOOR MOUNTED ESCAPE SLIDE LIGHT INOP. REPLACED BATTERY PACK PER MM 33-51-63. 2 L 7 2 4F A16WE 1996102400133 19961024 00133 NM 1996 10 24 CALA9601487 1 19961012 A 5330 SKIN BOEING 737 737222 1384473 NM BS 877-857 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10236 19937 AFT FUSELAGE STATION 877 TO 857 AT STATION 24R LAP JOINT SWOLLEN BETWEEN FASTENER HEADS. REMOVED FASTENERS AT LAP JOINT AND CORROSION PER SRM 51-10-2 AND 51-10-6 AND INSTALLED FASTENERS PER SRM 51-30-2. 2 L 7 2 4F A16WE 1996102400134 19961024 00134 NM 1996 10 24 CALA9601488 1 19961012 A 5313 STRINGER BOEING 737 737222 1384473 NM RT AC BAY CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10236 19937 RIGHT A/C BAY OUTBOARD SIDE APPROX 1.5 LONG CRACK EXTENDING UNDER STIFFENER AT FUSELAGE STATION. REMOVED STIFFENER, STO P DRILLED CRACK, AND INSTALLED PER SRM 51-10-1 AND 51-30-2. 2 L 7 2 4F A16WE 1996102400135 19961024 00135 NM 1996 10 24 9622186739 1 19961004 A 3234 HANDLE BOEING 747 747251F 1384898 NM LANDING GEAR LACK OF LUBE A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 639US 23887 DURING APPROACH, THE LANDING GEAR HANDLE WAS DIFFICULT TO MOVE AND THE LANDING GEAR UNSAFE LIGHT ILLUMINATED AFTER LANDI NG GEAR EXTENSION. RECYCLED LANDING GEAR AND LIGHT EXTINGUISHED. LUBRICATED LANDING GEAR HANDLE ASSEMBLY, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996102400136 19961024 00136 WP 1996 10 24 9622109956 1 19961014 A 5711 SPAR WEB DOUG DC9 DC931 3022065 WP WS 58 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 923RW 47183 DURING SCHEDULED MAINTENANCE, FOUND A 1.7 INCH CRACK IN THE RIGHT WING REAR SPAR WEB UNDER THE REAR SPAR PANEL ATTACH FI TTING WS 58. REPAIRED PER EM 57-10-00028. 2 L 7 2 4F A6WE 1996102400137 19961024 00137 WP 1996 10 24 9622119960 1 19961015 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 598 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 920RW 47163 DURING H-CHECK, FOUND CORROSION ON THE INTERCOSTAL END FITTING AT THE FS 598 FRAME BETWEEN LONGERON 27L AND 28L. REPLAC ED FITTING (P/N 9915553-5N) PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996102400138 19961024 00138 WP 1996 10 24 9622129963 1 19961015 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 756 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 913RW 47171 DURING M-CHECK, FOUND A 5 INCH LONG CRACK IN THE FS 756 RIGHT SIDE FRAME, LOWER INBOARD FLANGE. REPAIRED FRAME (PSE 53. 09.014) PER SRM 51-10-3. 2 L 7 2 4F A6WE 1996102400139 19961024 00139 WP 1996 10 24 9622139852 1 19961015 A 5320 FITTING DOUG DC9 DC951 3022051 WP BS 693 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 761NC 47709 DURING H-CHECK, FOUND A CRACK IN THE LONGERON 29L END FITTING AT FS 693. REPLACED FITTING PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996102400140 19961024 00140 WP 1996 10 24 9622149960 1 19961015 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 756 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 920RW 47163 DURING H-CHECK, FOUND CORROSION IN THE LONGERON 30 END FITTING AT FS 756. REPLACED FITTING (P/N 5920303-501) PER SRM 51 -30-2. 2 L 7 2 4F A6WE 1996102400141 19961024 00141 WP 1996 10 24 9622159960 1 19961015 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 585 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 920RW 47163 DURING H-CHECK AT FS 585, FOUND A 6 INCH CRACK IN THE LONGERON 27L END FITTING AND A 4 INCH CRACK IN THE LONGERON 28R EN D FITTING. REPLACED BOTH END FITTINGS PER SRM 51-30-2, 51-30-5. 2 L 7 2 4F A6WE 1996102400142 19961024 00142 WP 1996 10 24 9622169618 1 19961016 A 5530 FITTING DOUG DC9 DC932 3022066 WP VERT STAB CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 618NW 47433 DURING M-CHECK, FOUND CORROSION ON THE VERTICAL STABILIZER LEFT RUB STRIP ATTACH FITTING AND A CRACK IN THE RIGHT RUB ST RIP ATTACH FITTING. REPLACED BOTH FITTINGS PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996102400143 19961024 00143 WP 1996 10 24 9622179963 1 19961016 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 1005 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 913RW 47171 DURING M-CHECK, FOUND A CRACK IN THE LOWER DOOR STOP STIFFENER FITTING AT FS 1005, LONGERON 15R. REPLACED FITTING PER S RM 51-10-1. 2 L 7 2 4F A6WE 1996102400144 19961024 00144 SO 1996 10 24 COMA9610306 1 19961015 A 2750 12042642507 FLAP SELECTOR EMB 120 EMB120RT SO INST PANEL MALFUNCTION A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 152CA 13357 139 120152 FLAP CONTROL FAULT WARNING. REPLACED THE FLAP SELECTOR UNIT. 2 L 7 2 4T RT A31SO 1996102400145 19961024 00145 SO 1996 10 24 COMA9610307 1 19961015 A 5754 12040327602 FLAP EMB 120 EMB120RT SO RT TE FLAP CHAFING A COMA O OTHER J WARNING INDICATION UK UNKNOWN 1 SO 01 1105G 120105 NACELLE FLAP DISAGREEMENT WARNING WHEN FLAPS LOWERED. FOUND RT NACELLE FLAP CHAFING AT THE OUTBD HINGE. REPLACED FLAP. 2 L 7 2 4T RT A31SO 1996102400146 19961024 00146 EA 1996 10 24 COMA9660169 1 19961015 A 2910 AE1000884G0122 HYDRAULIC LINE CNDAIR CL600 CL6002B19 EA NOSE LEAKING A COMA K NONE K FLUID LOSS UK UNKNOWN 1 SO 01 914CA 7012 HYDRAULIC FLUID LEAKING FROM FWD FUSELAGE AREA. REPLACED LEAKING AIR DRIVEN GENERATOR RETRACT ACTUATOR LINE. 2 L 7 2 4F RT A21EA 1996102400147 19961024 00147 EA 1996 10 24 COMA9660170 1 19961016 A 2760 270003 PCU CNDAIR CL600 CL6002B19 EA LT SPOILERON MALFUNCTION A COMA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 01 937CA 7044 SPOILERONS FAULT MESSAGE ON EICAS. REPLACED LEFT OUTBD SPOILERON POWER CONTROL UNIT. 2 L 7 2 4F RT A21EA 1996102400148 19961024 00148 EA 1996 10 24 COMA9660171 1 19961015 A 2760 4916405 SECU CNDAIR CL600 CL6002B19 EA E/E BAY MALFUNCTION A COMA O OTHER F FLT CONT AFFECTED LD LANDING 1 SO 01 924CA 1365 1365 7026 GROUND LIFT DUMP UNSAFE MESSAGE ON EICAS AFTER LANDING. REPLACED THE SPOILER ELECTRONIC CONTROL UNIT. 2 L 7 2 4F RT A21EA 1996102400149 19961024 00149 NM 1996 10 24 SWAA961076 1 19961011 A 3350 6104789 BATTERY BOEING 737 7373A4 1384585 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED TERMINAL CHECK, FOUND AFT SECTION OF ESCAPE PATH LIGHTING VERY DIM. REPLACED BATTERY PACK AND CHARGER PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996102400150 19961024 00150 NM 1996 10 24 SWAA961077 1 19961010 A 3350 BATTERY BOEING 737 7372H4 138448C NM FWD GALLEY DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 52SW 21533 DURING SCHEDULED SERVICE CHECK, FOUND FWD GALLEY EMERGENCY FLASHLIGHTS NOT CHARGING. REPLACED BATTERIES PER BOEING M/M. 2 L 7 2 4F A16WE 1996102400151 19961024 00151 NM 1996 10 24 SWAA961078 1 19961010 A 5330 SKIN BOEING 737 7372H4 138448C NM PAX DR CUTOUT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 29SW 21340 DURING SCHEDULED B-CHECK, FOUND FWD FORWARD ENTRY DOOR CUTOUT UPPER RADIUS ON FUSELAGE SKIN CRACKED. REPAIRED PER SWA A CO 6317-53 AND RA 1-253-1521. 2 L 7 2 4F A16WE 1996102400152 19961024 00152 NM 1996 10 24 SWAA961079 1 19961010 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 315 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 29SW 21340 DURING SCHEDULED B-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 315 BETWEEN S7 AND 8L. REPAIRED PER SWA RA 1-253-1531 AND A CO 6317-53. 2 L 7 2 4F A16WE 1996102400153 19961024 00153 NM 1996 10 24 SWAA961080 1 19961010 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 294.5 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 29SW 21340 DURING SCHEDULED B-CHECK, FOUND FUSELAGE SKIN GOUGED BEYOND SRM LIMITS AT BS 294.5 AND S8L. REPAIRED PER SWA RA 1-253-1 521. 2 L 7 2 4F A16WE 1996102400154 19961024 00154 NM 1996 10 24 SWAA961081 1 19961009 A 2120 AIR DISTR BOEING 737 7372H4 138448C NM AFT GALLEY SMOKE A SWAA K NONE O OTHER NR NOT REPORTED 1 SW 07 60SW 21812 SMOKEY ODOR NOTED IN AFT GALLEY AREA, BUT NO VISIBLE SMOKE. INSPECTED AFT GALLEY COFFEEMAKERS AND C/B PANEL, NO DISCREP ANCIES NOTED. 2 L 7 2 4F A16WE 1996102400155 19961024 00155 NM 1996 10 24 SWAA961082 1 19961012 A 2530 COFFEEMAKER BOEING 737 7372H4 138448C NM FWD GALLEY INOPERATIVE A SWAA K NONE O OTHER DE DESCENT 1 SW 07 93SW 22965 DURING DESCENT, NOTED A PLASTIC TYPE BURNING SMELL IN FWD GALLEY AREA. INSPECTED GALLEY COFFEEMAKERS, PULLED AND COLLAR ED C/B'S TO FWD GALLEY COFFEEMAKERS, NO OTHER DISCREPANCIES NOTED. 2 L 7 2 4F A16WE 1996102400156 19961024 00156 NM 1996 10 24 SWAA961083 1 19961012 A 2121 FANS BOEING 737 7373H4 1384600 NM CABIN SMOKING A SWAA K NONE O OTHER CR CRUISE 1 SW 07 616SW 27699 EN ROUTE, NOTED AN ELECTRICAL SMELL AND HAZE IN CABIN. TURNED OFF GASPER AND RECIRCULATING FANS, SMELL AND HAZE DISAPPE ARED. INSPECTED AND RAN RECIRCULATING AND GASPER FANS ON GROUND, NO SMELL OR SMOKE NOTED. 2 L 7 2 4F RT A16WE 1996102400157 19961024 00157 NM 1996 10 24 SWAA961084 1 19961009 A 3230 65C310991 LOCK ACTUATOR BOEING 737 7373H4 1384600 NM NLG MALFUNCTIONED A SWAA K NONE J WARNING INDICATION DE DESCENT 1 SW 07 304SW 22944 ON GEAR EXTENSION, NOSE GEAR DID NOT EXTEND. RECYCLED GEAR LEVER AND ALL THREE GEARS EXTENDED NORMALLY. MADE AN UNEVEN TFUL LANDING AT OMA. INSPECTED, FERRIED AIRCRAFT TO MDW WHERE MAINT REPLACED NOSE GEAR LOCK ACTUATOR AND PERFORMED GEAR LUBE PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996102400158 19961024 00158 NM 1996 10 24 SWAA961085 1 19961010 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 727B CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 92SW 22964 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACK AT BS 727B, S18L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996102400159 19961024 00159 NM 1996 10 24 SWAA961087 1 19961012 A 5230 SKIN BOEING 737 7373H4 1384600 NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED BC3 CHECK, FOUND AFT CARGO DOOR SKIN CRACKED AT LOWER AFT CORNER. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996102400160 19961024 00160 NM 1996 10 24 SWAA961088 1 19961012 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 380 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED BC3 CHECK, FOUND A 1 INCH CRACK IN FUSELAGE SKIN AT E AND E COOLIING DUCT AT BS 380. REPAIRED PER BOEI NG SRM. 2 L 7 2 4F RT A16WE 1996102400161 19961024 00161 NM 1996 10 24 SWAA961089 1 19961009 A 5330 SKIN BOEING 737 7372H4 138448C NM FWD ENTRY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 89SW 22904 DURING SCHEDULED B2 CHECK, FOUND FUSELAGE SKIN CRACKED AT UPPER HINGE CUTOUT OF FWD ENTRY DOOR. REPAIRED PER BOEING SR M. 2 L 7 2 4F A16WE 1996102400162 19961024 00162 NM 1996 10 24 SWAA961090 1 19961012 A 5320 FRAME BOEING 737 7372H4 138448C NM DOOR CUTOUT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 61SW 21970 DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR CUTOUT FRAME CRACKED AT AFT UPPER STOP FITTING. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996102400163 19961024 00163 NM 1996 10 24 SWAA961091 1 19961012 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 61SW 21970 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 957, LBL 61, WL 182, AT BS 390 TO 410, RBL 33, WL 156, AND A T BS 251, RBL 27, WL 168. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996102400164 19961024 00164 NM 1996 10 24 SWAA961092 1 19961012 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 1001 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 61SW 21970 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 1001, LBL 15, WL 170. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996102400165 19961024 00165 NM 1996 10 24 SWAA961093 1 19961012 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 440-500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 61SW 21970 DURING SCHEDULED D-CHECK, FOUND FWD CARGO BAY FLOOR BEAM CRACKED AT BS 440 AND 500, ABOVE S27R. REPAIRED PER BOEING SRM . 2 L 7 2 4F A16WE 1996102400166 19961024 00166 NM 1996 10 24 SWAA961094 1 19961012 A 5315 BULKHEAD ANGLE BOEING 737 7372H4 138448C NM BS 520 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 61SW 21970 DURING SCHEDULED D-CHECK, FOUND LOWER BULKHEAD ANGLE CORRODED AT BS 520, AT S26 LT AND RT. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996102400167 19961024 00167 NM 1996 10 24 SWAA961095 1 19961012 A 5320 STIFFENER BOEING 737 7372H4 138448C NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 61SW 21970 DURING SCHEDULED D-CHECK, FOUND STIFFENER CRACKED AT BS 540 PRESSURE BULKHEAD AT BS 540, LBL 25, WL 194. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996102400168 19961024 00168 NM 1996 10 24 SWAA961096 1 19961012 A 5311 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 61SW 21970 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 400 S22 TO 23L, BS 420 S24 TO 25L, BS 500 S24 TO 25L, BS 5 00A S23 TO 24L, BS 500B 23 TO 24L, BS 500A S23 TO 25R, BS 500 S23 TO 24R, BS 1104 S19L, AND AT BS 460 24L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996102400169 19961024 00169 NM 1996 10 24 SWAA961097 1 19961012 A 5312 BULKHEAD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 61SW 21970 DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACK AT WL 191 AND 201, LBL 5. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996102400170 19961024 00170 NM 1996 10 24 SWAA961098 1 19961012 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 312 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 61SW 21970 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME DAMAGED AT BS 312, 18 INCHES BELOW FWD AIRSTAIR DOOR OPENING. REPAIRED P ER BOEING SRM. 2 L 7 2 4F A16WE 1996102400171 19961024 00171 NM 1996 10 24 SWAA961099 1 19961012 A 5320 SUPPORT BOEING 737 7372H4 138448C NM BS 313-329 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 61SW 21970 DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CRACKED AT BS 313 TO 329, LBL 46, WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996102400172 19961024 00172 NM 1996 10 24 SWAA961100 1 19961012 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 947 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 61SW 21970 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CRACKED AT BS 947, LBL 53, WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996102400173 19961024 00173 NM 1996 10 24 SWAA961101 1 19961012 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 987/1006 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 61SW 21970 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 987, LBL 53, WL 208 AND AT BS 1006, WL 208, LBL 30. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996102400174 19961024 00174 NM 1996 10 24 SWAA961102 1 19961012 A 5320 CLIP BOEING 737 7372H4 138448C NM BS 887 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 61SW 21970 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, S14R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996102400175 19961024 00175 1996 10 24 SWAA961103 4 19961014 A 2565 D31591462 SLIDE BOEING 737 7373H4 1384600 NM FWD SERV DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 358SW 26595 DURING SCHEDULED A1 CHECK, FOUND FWD SERVICE DOOR ESCAPE SLIDE PRESSURE LOW. REPLACED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996102400176 19961024 00176 NM 1996 10 24 SWAA961104 1 19961012 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 507 HOLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 61SW 21970 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN HOLE AT BS 507, BETWEEN S2 AND 3L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996102400177 19961024 00177 NM 1996 10 24 SWAA961105 1 19961012 A 5320 WEB BOEING 737 7372H4 138448C NM BS 357 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 61SW 21970 DURING SCHEDULED D-CHECK, FOUND WEB CRACK AT S16L, BS 357, WL 217. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996102400178 19961024 00178 NM 1996 10 24 SWAA961086 1 19961012 A 5320 CLIPS BOEING 737 7372H4 138448C NM BS 360/400/559 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 61SW 21970 DURING SCHEDULED D-CHECK, FOUND STRINGER T-CLIPS CRACKED AT BS 400 S4R, BS 360 S5R AND AT BS 559 S17L. REPAIRED PER BOE ING SRM. 2 L 7 2 4F A16WE 1996102400179 19961024 00179 NM 1996 10 24 UPS96221316 1 19960926 A 2782 651626937 ACT BRACKET BOEING 727 72751C 1384015 NM NR 5 LE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE-C, RT WING L/E NR 5 K-FLAP ACTUATOR I/B SUPPORT BRACKET IS CRACKED UNDER MOUNT LUG. FABRICATED AND INS TALLED NEW BRACKET PER SRM 51-10-1, BOEING DRAWING 65-16269, SRM 51-30-2. 2 L 7 3 4F A3WE 1996102400180 19961024 00180 NM 1996 10 24 UPS96221317 1 19960925 A 5754 RIB BOEING 727 72751C 1384015 NM NR 4 LE SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE-C, NR 4 SLAT INBOARD TRACK, O/B ATTACH RIB IS CRACKED. REPAIRED RIB PER SRM 51-40-3. 2 L 7 3 4F A3WE 1996102400181 19961024 00181 NM 1996 10 24 UPS96221318 1 19960922 A 2782 651627537 ACT BRACKET BOEING 727 72751C 1384015 NM NR 6 LE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE-C, RT WING NR 6 K-FLAP ACTUATOR O/B SUPPORT BRACKET IS CRACKED AT LOWER MOUNT LUG. FABRICATED REPLACEME NT BRACKET AND INSTALLED PER SRM 51-10-1, 51-30- 1, BOEING DRAWING 65-16275. 2 L 7 3 4F A3WE 1996102400182 19961024 00182 NM 1996 10 24 UPS96221319 1 19960922 A 2782 651627536 ACT BRACKET BOEING 727 72751C 1384015 NM NR 6 LE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE-C RT WING NR 6 K-FLAP ACTUATOR I/B SUPPORT BRACKET IS CRACKED AT LOWER MOUNT LUG. FABRICATED AND INSTAL LED NEW BRACKET PER SRM 51-10-1, 51-30-1, BOEING DRAWING 65-16275. 2 L 7 3 4F A3WE 1996102400183 19961024 00183 NM 1996 10 24 UPS96221320 1 19960925 A 5754 RIB BOEING 727 72751C 1384015 NM NR 7 LE SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE-C, NR 7 SLAT RIB AT THE I/B SIDE OF ACTUATOR IS CRACKED. REMOVED FASTENERS, STOP DRILLED CRACK, FABRICA TED AND INSTALLED REPAIR ANGLE PER SRM 57-50-2. 2 L 7 3 4F A3WE 1996102400184 19961024 00184 NM 1996 10 24 UPS96221321 1 19960923 A 2782 ATTACH RIB BOEING 727 72751C 1384015 NM NR 7 LE SLAT ACT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE-C, RT WING NR 7 SLAT ACTUATOR ROD END ATTACH O/B RIB IS CRACKED. REMOVED FASTENERS, STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE PER SRM 57-50-2, 51-40-3. 2 L 7 3 4F A3WE 1996102400185 19961024 00185 NM 1996 10 24 UPS96221322 1 19960921 A 5347 65234104 SEAT TRACK BOEING 727 72751C 1384015 NM LOWER CARGO CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE-C, RT SEAT TRACK HAS LIGHT SURFACE CORROSION FULL LENGTH OF FWD LOWER CARGO. REPLACED SEAT TRACK PER SR M 51-30-2. 2 L 7 3 4F A3WE 1996102400186 19961024 00186 NM 1996 10 24 UPS96221323 1 19960922 A 5320 6522419 BRACKET BOEING 727 72751C 1384015 NM BS 870 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE-C, ATTACH CLIP CRACKED IN RADIUS AT LT W/W FWD UPPER STR 18A TO 870 FITTING. FABRICATED AND INSTALLED C LIP PER BOEING DRAWING 65-22419 AND SRM 51 -30-2. 2 L 7 3 4F A3WE 1996102400187 19961024 00187 NM 1996 10 24 UPS96221324 1 19960925 A 5320 WEB BOEING 727 72751C 1384015 NM BS 1218 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE-C, RT AFT LOWER TORQUE BOX I/B WEB AT STA 1218 IS CRACKED. FABRICATED AND INSTALLED DOUBLER PER SRM 51- 40-42. 2 L 7 3 4F A3WE 1996102400188 19961024 00188 NM 1996 10 24 UPS96221330 1 19961015 A 3610 BLEED AIR SO VLV BOEING 727 72730C 1384009 NM NR 2 ENGINE INOPERATIVE A IPXA K NONE O OTHER NR NOT REPORTED 1 SO 01 919UP 19012 INSPECTION TYPE-N/A, SMELL/ODOR OF BURNT OIL/RUBBER WHEN USING NR 1 BLEED AIR FOR LEFT PACK SMELL GOES AWAY WHEN AIR SOU RCE SWITCHED TO ENG NR 2. NR 1 ENG BLEED AIR S/O VALVE INOP, PER MEL 36-6-1-2 M-116899. 2 L 7 3 4F A3WE 1996102400189 19961024 00189 NM 1996 10 24 UPS96221339 1 19961016 A 2910 651782114 HYD MODULE BOEING 727 72722C 138400F NM A-HYD SYST FAILED A IPXA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 928UP 19091 INSPECTION TYPE N/A, INFLIGHT HAD HYD A-SYS OVERHEAT. FOLLOWED CHECKLIST, TURNED PUMPS OFF AFTER OVERHEAT EXT, TURNED P UMPS BACK ON AND GOT 200 LBS PRESS PER PUMP. A TOTAL OF 500 PSI WAS ATTAINED WITH BOTH PUMPS, QTY WAS GOOD. PROCEEDED WITH LOSS OF HYD SYS-A CHECKLIST. WHILE MANUAL EXTENDING FLAPS THE OUTBOARDS WOULD NOT EXTEND, GOT ALL LEADING EDGE DEV ICES. REMOVED AND REPLACED HYDRAULIC SYS-A MODULAR IAW MM 29-11-00, LEAKED CHECKED GOOD. (P/N 65-17821-14) (S/N 2381A) ON, (P/N MR29108-60) OFF. 2 L 7 3 4F A3WE 1996102400190 19961024 00190 NM 1996 10 24 UPS96421325 1 19961010 A 5312 BULKHEAD WEB BOEING 747 747121 1384871 NM BS 1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE-C, CRACK IN BULKHEAD WEB AT BS 1480. INSTALLED REPAIR DOUBLER IAW UPS EO B747-5310-3100C. 2 L 7 4 4F A20WE 1996102400191 19961024 00191 NM 1996 10 24 UPS96421326 1 19961010 A 5343 TRUSS FITTING BOEING 747 747121 1384871 NM BS 1810 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE-C, FORWARD TRUSS FITTING POS 9 CRACKED AT FWD LOWER FLANGE. REPLACED LATCH AND TRUSS FITTINGS IAW UPS E O B747-5340-0191. 2 L 7 4 4F A20WE 1996102400192 19961024 00192 NM 1996 10 24 UPS96421327 1 19961010 A 5730 SKIN BOEING 747 747121 1384871 NM WS 1437-1462 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE-C, CORROSION ON LT LOWER WING SKIN AT OLES 1437 TO 1462. REPAIRED PER UPS EFN 747-57-0338, BOEING DRAWI NG 65B22997-11. 2 L 7 4 4F A20WE 1996102400193 19961024 00193 NM 1996 10 24 UPS96421328 1 19961010 A 5730 SKIN BOEING 747 747121 1384871 NM WS 1386 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE-C, CORROSION ON LT WING LOWER SKIN AT OLES 1386. REPAIRED PER UPS EFN 747-57-0338, BOEING DRAWING 65B22 997-11. 2 L 7 4 4F A20WE 1996102400194 19961024 00194 NM 1996 10 24 UPS96421329 1 19961010 A 5320 PRESSURE PAN BOEING 747 747121 1384871 NM BS 2360 DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C PRESSURE PAN UPPER SIDE DAMAGED AT APU CUT OUT REINFORCEMENT BS 2360. REPLACED PRESSURE PAN IAW SRM 5 1-30-02, 51-40-00. 2 L 7 4 4F A20WE 1996102400195 19961024 00195 NM 1996 10 24 UPS96421331 1 19961010 A 5320 PRESSURE PAN BOEING 747 747121 1384871 NM BS 2360 DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE-C, PRESSURE PAN DELAMINATED AT BS 2360, RT HYDRAULIC LINE, APU CUT OUT REINFORCEMENT. REPLACED PRESSURE PAN IAW SRM 51-30-2. 2 L 7 4 4F A20WE 1996102400196 19961024 00196 NM 1996 10 24 UPS96421332 1 19961010 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1700 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE-C, CORROSION ON LOWER SIDE OF STRINGER 60R AT BS 1700. REPLACED STRINGER PER SRM 53-10-03, 53-10-1. 2 L 7 4 4F A20WE 1996102400197 19961024 00197 NM 1996 10 24 UPS96421338 1 19961016 A 2460 C338 CIRCUIT BREAKER BOEING 747 747123 1384873 NM P-14 CTR MAIN MELTED A IPXA K NONE A FLAME/FIRE UK UNKNOWN 1 SO 01 676UP 20101 INSPECTION TYPE N/A, FOUND ACCESS LEFT UPPER DECK C/B C338 BURNED. REPLACED C338 BREAKER, UPPER DECK LIGHTS TEST GOOD. DEFERRED P-14 C/B PANEL NEEDS HOLE REPAIRED, DEFERRAL NR D117075. 2 L 7 4 4F A20WE 1996102400198 19961024 00198 NM 1996 10 24 UPS96421341 1 19961015 A 8012 214N411B PRESSURE SWITCH BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE NR 4 ENGINE DEFECTIVE A IPXA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 01 671UP 20323 INSPECTION TYPE-N/A, PERFORMED PRECAUTIONARY SHUTDOWN OF NR 4 ENGINE DUE TO START VALVE LIGHT ILLUMINATION. REPLACED NR 4 START VALVE PRESSURE SWITCH. 2 L 7 4 4F 4 F A20WE E20EA 1996102400199 19961024 00199 1996 10 24 UPS96521346 2 19961016 A 7200 ENGINE BOEING 757 75724APF 1384969 NM LEFT HI OIL CONSUMPT A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 458UP 25479 INSPECTION TYPE-N/A, LT ENGINE WHEN LT PACK SELECTED ON, OIL FUMES CAME THROUGH PACK, VERY STRONG FUMES, OIL ON TAXI AND T/O HIGH OIL CONSUMPTION. REMOVED AND REPLACED LT ENGINE. 2 L 7 2 4F RT A2NM 1996102400200 19961024 00200 WP 1996 10 24 UPS96821334 1 19960923 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 463 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE-C/CK, CRACKED RIGHT WING LOWER SKIN AT STRINGER 64 AND XRS463, I/B OF NR 4 PYLON. REPAIRED CRACKED WING SKIN IAW TIMCO REO 02292 AND DOUGLAS DWG SRO85 70013. 2 L 7 4 4F RT 4A25 1996102400201 19961024 00201 WP 1996 10 24 UPS96821335 1 19961004 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1270 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE-C/CK, LONGERON END FITTING STA 1270 L35 LT IS CRACKED. REMOVED FITTING, DRILLED NEW FITTING IAW DC8 SRM 5-1-24, INSTALLED FITTING WITH HI-LOKS IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996102400202 19961024 00202 WP 1996 10 24 UPS96821336 1 19960928 A 5720 WEB DOUG DC8 DC873F 302199F WP WS 23 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE-C/CK, RIGHT CENTER WING STA XCW23 WEB HAS CRACKED LOWER ATTACH ANGLE AT ST RINGER 58. REMOVED CRACKED A TTACH ANGLE, LOCATED, DRILLED AND REAMED NEW ATTACHED ANGLE IAW DC8 SRM 51-1-24, ALODINED AND PRIMED NEW ATTACH ANGLE IA W DC8 SRM 51-1-8, INSTALLED NEW ATTACH ANGLE IAW DC8 SRM 51-1-20A. 2 L 7 4 4F RT 4A25 1996102400203 19961024 00203 WP 1996 10 24 UPS96821337 1 19960924 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1220 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE-C/CK, FRAME AT STA 1220 CORRODED BETWEEN L32R AND L33R. REMOVED CORRODED Z- FITTING, DRILLED AND INSTAL LED NEW Z-FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996102400204 19961024 00204 WP 1996 10 24 UPS96821340 1 19961016 A 3260 PROX SWITH DOUG DC8 DC873F 302199F WP RT MLG FAILED A IPXA O OTHER P NO WARNING INDICATION AP APPROACH 1 SO 01 812UP 46112 INSPECTION TYPE N/A, WHEN GEAR EXTENDED, LEFT AND NOSE GREEN, NO GREEN ON RT SIDE, BOTH GEAR AND DOOR RED LIGHTS ON. AL T DOOR LIGHTS ON WITH GEAR RETRACTED AND DOOR RED LIGHTS ON. ALT DOOR LIGHTS ON, FLY-BY INDICATED GEAR DOWN, DOORS CLOS ED. DECLARED EMERGENCY PULLED GPWS C/B, L/G C/B. GEAR PINS INSTALLED, A/C TAXIED TO GATE. REMOVED AND REPLACED PROXIM ITY BOX (P/N 287) OFF, (P/N 751) ON. SELF TEST ON BOX OK, RUN OPS CHK OF DOOR AND GEAR WARNING LIGHTS PER MM 32-60-00, SYS OPERATES PER CHK 007. 2 L 7 4 4F RT 4A25 1996102400205 19961024 00205 GL 1996 10 24 UPS96821342 2 19961016 A 7200 ENGINE DOUG DC8 DC871F 302199D WP GE CFM CFM562 GL NR 1 FLAMED OUT A IPXA O OTHER X ENGINE FLAMEOUT DE DESCENT 1 SO 01 709UP 45914 INSPECTION TYPE N/A, AT TOP OF DESCENT WITH BALANCED FUEL AT 390 NR 1 ENGINE FLAMED OUT. INITIATED FLAME-OUT CHKLIST. R ESTART NORMAL WITH NO EXCESSIVE OR ERRATIC ENGINE INDICATIONS. ALL BOOST AND FEED PUMPS WERE ON AND WORKING. PERFORMED HIGH POWER ENGINE WITH SNAP DECELL TO GROUND IDLE AND FLIGHT IDLE. DID DECELL AND POWER RUN WITH OUT BOOST AND FEED PU MPS. TESTED BOOST AND NASH PUMP IAW 73-10-01. ALL PUMPS CHECKED GOOD, COULD NOT GET FLAME-OUT. 2 L 7 4 4F 4 F RT 4A25 E2GL 1996102400206 19961024 00206 WP 1996 10 24 UPS96821343 1 19960906 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 1520-1540 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, MODERATE CORROSION OUT OF LIMITS AT LONGERON 26L BETWEEN FS 1520 TO 1540. REPAIRED LONGERON PER SR M 53-2-2, FIG 10. 2 L 7 4 4F RT 4A25 1996102400207 19961024 00207 WP 1996 10 24 UPS96821344 1 19961008 A 5314 KEEL BEAM DOUG DC8 DC871F 302199D WP BS 890 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE-C, CRACK AND HEAVY CORROSION INSIDE KEEL BEAM PANEL APPROX FS 890 RT SIDE WHEEL WELL. REPAIRED PANEL SE CTION PER SRM 53-2-0. 2 L 7 4 4F RT 4A25 1996102400208 19961024 00208 WP 1996 10 24 UPS96821345 1 19961008 A 5330 SKIN DOUG DC8 DC871F 302199D WP LT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE-C, ADJACENT SKIN OUTBOARD OF LT WING INBOARD SLOT IS CRACKED. REPLACED SKIN PANEL SECTION PER SRM 51-1- 4 AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 1996102400209 19961024 00209 WP 1996 10 24 UPS96821347 1 19960930 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 1350 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE-C/CK, LONGERON L35L AT STA 1350 CRACKED. REMOVED CRACKED FITTING, DRILLED NEW FITTING IAW DC8 SRM 51-1- 24, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, LONGERON WITH HI-LOKS IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996102400210 19961024 00210 WP 1996 10 24 UPS96821348 1 19960927 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 139 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE-C/CK, LEFT WING UPPER IB RIB CRACKED AT XRS 139 BARREL NUT END IN NR 2 MAIN TANK. REMOVED UPPER CAP, SP LICED RIB CAP AND REINSTALLED FWD SECTION OF RIB CAP IAW TIMCO REO 02311. 2 L 7 4 4F RT 4A25 1996102400211 19961024 00211 NM 1996 10 24 96FDEA01581 1 19961017 A 3230 RETRACT MECH BOEING 727 727247 138408F NM NLG LACK OF LUBE A FDEA O OTHER P NO WARNING INDICATION AP APPROACH 1 SO 25 234FE 21328 ON GEAR EXTENSION NOSE GEAR REMAINED UNSAFE, GEAR WAS RECYCLED AND NO DOOR LIGHT FOR NOSE GEAR WAS NOTICED ON RETRACTION . GEAR WAS EXTENDED AGAIN WITH SAFE INDICATION ALL GEARS. GREASED, JACKED AND VISUALLY INSPECTED. OPERATED NOSE LANDI NG GEAR PER MAINTENANCE MANUAL 32-33-0, GEAR OPERATIONAL CHECKS NORMAL. 2 L 7 3 4F A3WE 1996102400212 19961024 00212 NM 1996 10 24 96FDEA01582 1 19961014 A 5315 65208271 FLOORBEAM BOEING 727 72725 1384006 NM BS 1110 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 511FE 18203 NR 0609 AND 021, CORROSION (C53-224-01, -3) ON STA 1110 RBL 23 WL 208 UNDER TOP FLANGE OF FLOORBEAM. *S/D* FOUND CORRO SION TO BE OUT OF LIMITS. CUT OUT DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR IAW FEDEX EA 7-5310-31193. 2 L 7 3 4F A3WE 1996102400213 19961024 00213 NM 1996 10 24 96FDEA01583 1 19961015 A 5315 65208271 FLOORBEAM BOEING 727 72725 1384006 NM BS 1148 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 511FE 18203 NR 0437 AND 022, CORROSION (C53-111-01, -3) IN THE AFT CARGO BAY AT BS 1148 LBL 11 TO 23 WL 199 ON FLOORBEAM AT NUTPLATE HOLES. *S/D* CORROSION FOUND TO BE OUT OF LIMITS. REPAIRED FLOORBEAM AT BS 1148 LBL 11 TO 23 WL 199 IAW FEDEX EA 7-5 310-31191. 2 L 7 3 4F A3WE 1996102400214 19961024 00214 NM 1996 10 24 96FDEA01584 1 19960925 A 5751 65217661 SKIN BOEING 727 72725 1384006 NM LT OUTBD AILERON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 511FE 18283 NR 0580 AND 020, CRACK IN L/W O/B AILERON I/B AFT TRAILING EDGE CHORD. *S/D* STOP DRILLED CRACK, FABRICATED AND INST ALLED REPAIR DOUBLER PER FEDEX SRM 51-40-3. 2 L 7 3 4F A3WE 1996102400215 19961024 00215 NM 1996 10 24 96FDEA01585 1 19961018 A 2170 COALESCER BAG BOEING 727 7272S2F 1384O81 NM LT PACK DIRTY A FDEA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 25 209FE 22931 AFTER TAKEOFF, AGAIN STRONG SMELL FROM NR 1 ENGINE BLEED ON LEFT PACK. CHANGED TO NR 3 BLEED AND RIGHT PACK, SMELL WENT AWAY. AT 18,000 FT USING NR 2 BLEED AND LEFT PACK, SMELL CAME BACK BUT NOT AS STRONG. SELECTED WARMER TEMPERATURE LEF T PACK, SLOWLY SMELL DISSIPATED. REMOVED AND REPLACED LEFT PACK WATER SEPARATOR BAG, CHECKED AIR CYCLE MACHINE FOR FREE DOM OF MOVEMENT AND CHIP DETECTOR PLUG FOR METAL, NONE. NO EVIDENCE OF OIL FROM NR 1 BLEED, PACK OPERATED NORMAL DURING GROUND OPERATION USING APU. 2 L 7 3 4F A3WE 1996102400216 19961024 00216 NM 1996 10 24 96FDEA01586 1 19961018 A 2120 AIR DISTR BOEING 727 727227 1384078 NM CARGO COMPT ODOR A FDEA A G UNSCHED LANDING O2 MASK DEPLOYED B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SO 25 492FE 21530 FAINT SMELL IN CABIN BECAME A VERY HEAVY PAINT SMELL, SO MUCH SO THAT NORMAL BREATHING IN CARGO AREA WAS DIFFICULT. PAI NT SMELL WAS VERY NOTICEABLE IN COCKPIT. DONNED OXYGEN AND DIVERTED TO TYS. SOURCE OF HEAVY SMELL SEEMED TO BE EMANATI NG FROM NORMAL CARGO CANS. GROUND CREW COMMENTED ON STRENGTH OF ODORS WHEN FIRST ENTERING THE AIRCRAFT. THE FUMES DID NOT COME FROM THE DANGEROUS GOODS. WET INK ON PAMPHLETS IN 3R AND 4 CAUSED THE ODOR. THESE WERE DOWN LOADED AND SHIPPE D VIA GROUND TO DESTINATION. 2 L 7 3 4F A3WE 1996102400217 19961024 00217 NM 1996 10 24 96FDEA01587 1 19960920 A 5315 6520834 FLOORBEAM BOEING 727 72725 1384006 NM BS 1050 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 511FE 18283 CORROSION (C53-111-01, -3) IN AFT CARGO BAY AT BS 1050 LBL 20 TO RBL 20 WL 199 ON FLOORBEAM AT NUTPLATES HOLES. REMOVED CORRODED SECTION OF BS 1050 FLOORBEAM FROM LBL 25 TO RBL 25 WL 199 LOWER FLANGE. REPAIRED LOWER FLANGE PER FEDEX SRM 5 3-10-8 FIG 3 EA NR 7-5310-31192. 2 L 7 3 4F A3WE 1996102400218 19961024 00218 WP 1996 10 24 ABXA9600644 1 19960826 A 5720 7760086520 FITTING DOUG DC8 DC862 3021970 WP WS 340 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 805AX 45906 DURING 'C' CHECK, FOUND RIGHT WING SUPPORT FITTING CRACKED AT XW 340. REPAIRED RIGHT WING SUPPORT FITTING IAW REA NR D8 27-16054. 2 L 7 4 4F 4A25 1996102400219 19961024 00219 WP 1996 10 24 ABXA9600645 1 19960826 A 5744 1514376501 FITTING DOUG DC8 DC862 3021970 WP WS 340 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 805AX 45906 DURING 'C' CHECK, FOUND LEFT WING FLAP SUPPORT FITTING CRACKED AT XW 340. REMOVED CRACKED FLAP SUPPORT FITTING AND INST ALLED SERVICEABLE FLAP SUPPORT FITTING. 2 L 7 4 4F 4A25 1996102400220 19961024 00220 WP 1996 10 24 ABXA9600646 1 19960820 A 5730 SKIN DOUG DC8 DC861 3021952 WP WS 69.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 851AX 45940 DURING 'C' CHECK, FOUND UPPER I/B AFT SKIN PANEL ALONG DIHEDRAL BREAK CRACKED ON RW S-800. VERIFIED THROUGH NDT AT XCW 69.5. REPAIRED CRACK IAW REA NR D857-15733MR. 2 L 7 4 4F 4A25 1996102400221 19961024 00221 WP 1996 10 24 ABXA9600648 1 19961017 A 3350 5708458503 BATTERY RACK DOUG DC8 DC863F 302198F WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 815AX 46097 EMERGENCY EXIT LIGHTING FAILS TEST ON A-1 CHECK. REPLACED EMERGENCY LIGHTING BATTERY RACK ASSEMBLY, OPS CHECKED GOOD IA W DC-8 MM 33-50-0. 2 L 7 4 4F 4A25 1996102400222 19961024 00222 WP 1996 10 24 SCNA96292 1 19961006 A 5522 SKIN DOUG DC10 DC1015 3022118 WP RT ELEVATOR DAMAGED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY MAINTENANCE, FOUND LIP BENT AND TORN ON CUT OUT, SECOND HINGE FROM OUTBOARD END ON RIGHT HAND ELEVATOR. RE MOVED DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER IN ACCORDANCE WITH SRM 55-21-01 AND SRM 55-00-01. 2 L 7 3 4F A22WE 1996102400223 19961024 00223 WP 1996 10 24 SCNA96293 1 19961006 A 5522 SKIN DOUG DC10 DC1015 3022118 WP LT ELEVATOR DAMAGED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY MAINTENANCE, FOUND LIP TORN ON CUT OUT, SECOND HINGE FROM OUTBOARD END ON LEFT HAND ELEVATOR. REMOVED DAMA GED AREA, FABRICATED AND INSTALLED DOUBLER IN ACCORDANCE WITH SRM 55-21-01 AND SRM 55-00-01. 2 L 7 3 4F A22WE 1996102400224 19961024 00224 WP 1996 10 24 SCNA96294 1 19960927 A 5512 SKIN DOUG DC10 DC1015 3022118 WP RT HORIZ STAB DENTED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY MAINTENANCE, FOUND A DENT APPROXIMATELY 12 INCHES FROM THE INBOARD END OF THE RIGHT HAND HORIZONTAL STABILI ZER. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IN ACCORDANCE WITH SRM 55-10-00 AND 53- 30-10. 2 L 7 3 4F A22WE 1996102400225 19961024 00225 WP 1996 10 24 SCNA96295 1 19961003 A 5400 ANGLE DOUG DC10 DC1015 3022118 WP NR 1 PYLON CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY MAINTENANCE, FOUND A CRACKED L-ANGLE IN THE NUMBER 1 PYLON AT APPROXIMATE STATION 272 OUTBOARD END, IN BACK AND ABOVE PRECOOLER. REMOVED EXISTING ANGLE, FABRICATED AND INSTALLED A NEW ANGLE IN ACCORDANCE WITH SRM 54-71-02, SRM 51-33-00 AND SRM 51-35-01. 2 L 7 3 4F A22WE 1996102400226 19961024 00226 WP 1996 10 24 SCNA96296 1 19960919 A 5330 SKIN DOUG DC10 DC1015 3022118 WP BS 715 GOUGED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY MAINTENANCE, FOUND 3 GOUGES IN THE LEFT SIDE OF THE FUSELAGE AT BS 715, JUST ABOVE THE FLOOR LINE. BLENDED OUT GOUGES IN ACCORDANCE WITH SRM 52-00-01. FABRICATED AND INSTALLED A DOUBLER IN ACCORDANCE WITH SRM 53-20-00. 2 L 7 3 4F A22WE 1996102400227 19961024 00227 WP 1996 10 24 SCNA96297 1 19960919 A 5330 SKIN DOUG DC10 DC1015 3022118 WP BS 550 GOUGED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY MAINTENANCE, FOUND A DENT ON THE LEFT SIDE OF THE FUSELAGE AT BS 560 JUST BELOW THE FLOOR LINE. BLENDED OU T DENT, FABRICATED AND INSTALLED A DOUBLER IN ACCORDANCE WITH SRM 53-20-00 FIGURE 13. 2 L 7 3 4F A22WE 1996102400228 19961024 00228 WP 1996 10 24 SCNA96298 1 19960919 A 5312 BULKHEAD DOUG DC10 DC1015 3022118 WP BS 1841 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY MAINTENANCE, FOUND A CRACK EXTENDING BEYOND THE STOP DRILL LOCATION IN AN EXISTING REPAIR ON THE BS 1841 BU LKHEAD. REMOVED EXISTING REPAIR AND DAMAGED MATERIAL, FABRICATED AND INSTALLED A FILLER AND DOUBLER IN ACCORDANCE WITH SRM 53-00-11 FIGURE 4 AND SRM 51-30-00. 2 L 7 3 4F A22WE 1996102400229 19961024 00229 WP 1996 10 24 SCNA96299 1 19960919 A 5330 SKIN DOUG DC10 DC1015 3022118 WP BS 865 DENTED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY MAINTENANCE, FOUND A SMOOTH DENT AT BS 765, BELOW LONGERON L-27. FABRICATED AND INSTALLED A DOUBLER IN ACC ORDANCE WITH SRM 53-20-00 FIGURE 13. 2 L 7 3 4F A22WE 1996102400230 19961024 00230 WP 1996 10 24 SCNA96300 1 19960920 A 5315 FLOORBEAM DOUG DC10 DC1015 3022118 WP LWR GALLEY CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY MAINTENANCE, FOUND CORROSION ON THE FLOORBEAM BELOW THE THRESHOLD ON THE FORWARD SIDE OF THE SERVICE ELEVA TOR IN THE LOWER GALLEY. REMOVED CORRODED SECTION OF FLOORBEAM, FABRICATED AND INSTALLED A NEW SECTION OF FLOORBEAM IN ACCORDANCE WITH SRM 53-30-00. 2 L 7 3 4F A22WE 1996102400231 19961024 00231 WP 1996 10 24 SCNA96301 1 19960921 A 5315 FLOORBEAM DOUG DC10 DC1015 3022118 WP BS 823 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY MAINTENANCE, FOUND CORROSION ON THE FLOORBEAM AT BS 823 IN THE FORWARD GALLEY. REMOVED CORROSION, FABRICAT ED AND INSTALLED A FILLER AND DOUBLER IN ACCORDANCE WITH SRM 53-00-01. 2 L 7 3 4F A22WE 1996102400232 19961024 00232 WP 1996 10 24 SCNA96302 1 19960921 A 5315 FLOORBEAM DOUG DC10 DC1015 3022118 WP BS 685 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY MAINTENANCE, FOUND CORROSION ON THE FLOORBEAM AT BS 685 IN THE LOWER GALLEY. REMOVED CORRODED MATERIAL, FA BRICATED AND INSTALLED A FILLER AND DOUBLER IN ACCORDANCE WITH SRM 53-00-01. 2 L 7 3 4F A22WE 1996102400233 19961024 00233 WP 1996 10 24 SCNA96303 1 19960922 A 5315 FLOORBEAM DOUG DC10 DC1015 3022118 WP BS 750 - 830 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY MAINTENANCE, FOUND CORROSION ON THE FLOORBEAM AT BS 775 TO 830, RIGHT HAND SIDE OF THE LOWER GALLEY. REMOV ED CORRODED MATERIAL, FABRICATED AND INSTALLED A FILLER AND DOUBLER IN ACCORDANCE WITH SRM 53-00-01 AND ENGINEERING AUTH ORIZATION EA DC10-53-13. 2 L 7 3 4F A22WE 1996102400234 19961024 00234 WP 1996 10 24 SCNA96304 1 19960922 A 5315 FLOORBEAM DOUG DC10 DC1015 3022118 WP BS 735 - 737 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY MAINTENANCE, FOUND CORROSION ON THE FLOORBEAM AT BS 735 TO BS 737 RIGHT HAND SIDE OF THE LOWER GALLEY. RE MOVED CORRODED MATERIAL, FABRICATED AND INSTALLED A FILLER AND DOUBLER IN ACCORDANCE WITH SRM 53-00-01 AND ENGINEERING AUTHORIZATION EA DC10-53-13. 2 L 7 3 4F A22WE 1996102400235 19961024 00235 WP 1996 10 24 SCNA96305 1 19960921 A 5315 FLOORBEAM DOUG DC10 DC1015 3022118 WP BS 750 RT CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY MAINTENANCE, FOUND CORROSION ON THE FLOORBEAM AT BS 750 RIGHT HAND SIDE OF THE LOWER GALLEY. REMOVED CORRO DED MATERIAL, FABRICATED AND INSTALLED A FILLER AND DOUBLER IN ACCORDANCE WITH SRM 53-00-01 AND ENGINEERING AUTHORIZATIO N EA DC10-53-13. 2 L 7 3 4F A22WE 1996102400236 19961024 00236 WP 1996 10 24 SCNA96306 1 19960924 A 5315 FLOORBEAM DOUG DC10 DC1015 3022118 WP BS 1887 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY MAINTENANCE, FOUND CORROSION ON THE FLOORBEAM AT BS 1887, LBL 30 AND RBL 24. REMOVED CORRODED SECTIONS, FA BRICATED AND INSTALLED FILLERS AND DOUBLERS IN ACCORDANCE WITH SRM 51-21-00, SRM 53-00-01 AND ENGINEERING AUTHORIZATION EA DC10-53-014. 2 L 7 3 4F A22WE 1996102400237 19961024 00237 WP 1996 10 24 SCNA96307 1 19960919 A 5322 CEILING SUPPORT DOUG DC10 DC1015 3022118 WP BS 919 RBL 67 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY MAINTENANCE, FOUND CEILING SUPPORT CRACKED IN THE FORWARD CARGO COMPARTMENT AT BS 919, RBL 67. REMOVED CRA CKED CEILING SUPPORT, FABRICATED AND INSTALLED A NEW CEILING SUPORT IN ACCORDANCE WITH SRM 51-00-01 AND SRM 53-00-01. 2 L 7 3 4F A22WE 1996102400238 19961024 00238 WP 1996 10 24 SCNA96308 1 19960920 A 5320 INTERCOSTAL DOUG DC10 DC1015 3022118 WP BS 1841 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY MAINTENANCE, FOUND CORROSION AROUND NUTPLATE UNDER SEAT TRACK AT BS 1841, RBL 27. REMOVED INTERCOSTAL, FAB RICATED AND INSTALLED A NEW INTERCOSTAL IN ACCORDANCE WITH SRM 53-30-01. 2 L 7 3 4F A22WE 1996102400239 19961024 00239 WP 1996 10 24 SCNA96309 1 19960926 A 5311 FRAME DOUG DC10 DC1015 3022118 WP BS 1501 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY MAINTENANCE, FOUND A CRACK IN THE LONGERON HOLE FOR LONGERON 48L AT BS 1501. REMOVED DAMAGED SECTION, FABR ICATED AND INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH SRM 53-30-00 AND ENGINEERING AUTHORIZATION EZ DC10-53-012. 2 L 7 3 4F A22WE 1996102400240 19961024 00240 WP 1996 10 24 SCNA96310 1 19960917 A 5755 SKIN DOUG DC10 DC1015 3022118 WP NR 4 SPOILER CHAFFED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY MAINTENANCE, FOUND CHAFING SPOTS ON THE LOWER SURFACE OF THE LEFT HAND NUMBER 4 SPOILER. FABRICATED AND IN STALLED A REPAIR ON THE LOWER SURFACE OF THE NUMBER 4 SPOILER PER SRM 51-70-00 AND ENGINEERING AUTHORIZATION EA DC10-57- 010. 2 L 7 3 4F A22WE 1996102400241 19961024 00241 WP 1996 10 24 SCNA96311 1 19960918 A 5755 SKIN DOUG DC10 DC1015 3022118 WP NR 3 SPOILER CHAFFED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY MAINTENANCE, FOUND CHAFING SPOTS ON THE LOWER SURFACE OF THE LEFT HAND NUMBER 3 SPOILER. FABRICATED AND IN STALLED A REPAIR ON THE LOWER SURFACE OF THE NUMBER 3 SPOILER PER SRM 51-70-00 AND ENGINEERING AUTHORIZATION EA DC10-57 -010. 2 L 7 3 4F A22WE 1996102400242 19961024 00242 WP 1996 10 24 SCNA96312 1 19960917 A 5753 SKIN DOUG DC10 DC1015 3022118 WP RT TE FOREFLAP DENTED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY MAINTENANCE, FOUND A DENT IN THE INBOARD FOREFLAP ABOVE AND BEHIND THE MAIN GEAR ON THE RIGHT SIDE. FABRIC ATED AND INSTALLED A PERMANENT REPAIR IN ACCORDANCE WITH SRM 51-71-00, VOLUME II PAGE 68 AND FIGURE 33. 2 L 7 3 4F A22WE 1996102400243 19961024 00243 NM 1996 10 24 DHL96712004 1 19961015 A 3411 851CM PITOT TUBE BOEING 727 72729 1384007 NM RT FUSELAGE PLUGGED A DHLA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 712DH 19401 FIRST OFFICERS AIRSPEED INDICATOR FAILED, TAPPED GAUGE AND HAD NO EFFECT. BLEW FIRST OFFICERS PITOT TUBE OUT WITH HIGH PSI AIR AND TEST FIRST OFFICERS AIRSPEED INDICATOR WITH PITOT STATIC TEST BOX PER MM 34-11-0. 2 L 7 3 4F A3WE 1996102400244 19961024 00244 1996 10 24 DHL96721007 4 19961013 A 3455 612034717 ANTENNA CABLE BOEING 727 727228 NM NR 1 ADF OPEN A DHLA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 721DH 19545 NR 1 ADF WEAK AND WANDERS. REPLACED NR 1 ADF LOOP ANTENNA CABLE ASSY AND NR 1 ADF SENSE ANTENNA CABLE PIGTAIL BETWEEN N R 1 ADF RECEIVER AND STANCHION, OPS CHECK NORMAL REF MM 34-37-0. 2 L 7 3 4F A3WE 1996102400245 19961024 00245 EA 1996 10 24 BIER960036 2 19961018 A 8530 CYLINDER PIPER PA28 PA28161 7102803 SO LYC O320 O320D3G 41508 EA NR 4 CRACKED B BIEA K NONE O OTHER IN INSP/MAINT 1 EA 21 8071S 1264 28161102 L1337039A DURING INSPECTION OF NR 4 CYL COMBUSTION DOME FOR UNRELATED PROBLEM FOUND SEVERAL STRESS RELATED CRACKS IN DOME IN AREA BETWEEN EXH VALVE AND BOTTOM SPARK PLUG. THE CRACKS WERE SPREAD OUT AND NOT CONTAINED IN ONE PARTICULAR AREA. ONE CRAC K HAD OPENED TO APPROXIMATLY 1 MM. SUBMITTER STATES THIS PROBLEM WAS NOT VISIBLE WITHOUT REMOVING THE CYLINDER AND LEFT UNATTENDED COULD HAVE LEAD TO ENGINE FAILURE. 1 L 7 1 3O 3 O 2A13 E274 1996102400246 19961024 00246 NM 1996 10 24 P5CA9600803 1 19961014 A 7110 RIVETS BOEING 747 747123 1384873 NM NR 4 ENG FAIRING MISSING A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 SEVERAL MISSING RIVETS ON NR 4 ENGINE LEFT AND RIGHT SKIRT FAIRINGS. REPLACED RIVETS PER BAC SRM 51-30-02. 2 L 7 4 4F A20WE 1996102400247 19961024 00247 NM 1996 10 24 P5CA9600804 1 19961014 A 7810 EXHAUST SLEEVE BOEING 747 747123 1384873 NM NR 4 ENGINE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 DELAMINATED AND CURLED LEADING EDGE SKIN ON NR 4 ENGINE EXHAUST SLEEVE. REPAIRED PER BAC SRM 51-40-02. 2 L 7 4 4F A20WE 1996102400248 19961024 00248 NM 1996 10 24 P5CA9600805 1 19961014 A 7830 SLEEVE SKIN BOEING 747 747123 1384873 NM NR1 ENG TR DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 DELAMINATED PREVIOUS REPAIR ON NR 1 ENGINE FAN THRUST REVERSE SLEEVE. REPAIRED PER BAC SRM 51-40-06. 2 L 7 4 4F A20WE 1996102400249 19961024 00249 NM 1996 10 24 P5CA9600806 1 19961014 A 7830 SKIN BOEING 747 747123 1384873 NM NR 2 PYLON TORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 SKIN TORN ON NR 2 PYLON ABOVE STINGER FAIRING. REPAIRED PER BAC SRM 51-40-01. 2 L 7 4 4F A20WE 1996102400250 19961024 00250 NM 1996 10 24 P5CA9600807 1 19961017 A 5312 BULKHEAD WEB BOEING 747 747122 1384872 NM LT MLG WW CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 CRACK AT APU DUCT CUTOUT AT LEFT WHEEL WELL BULKHEAD. REPAIRED WITH KIT 015M0425-1 PER BAC SERVICE BULLETIN 747-53-2309 . 2 L 7 4 4F A20WE 1996102400251 19961024 00251 NM 1996 10 24 P5CA9600808 1 19961001 A 5320 SHEAR TIE BOEING 747 747122 1384872 NM BS 760 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 2 CORROSION FORWARD CARGO HOLD SHEAR TIE AT BS 760 BETWEEN S46L AND S47L. MANUFACTURED REPLACEMENT PART PER BOEIN G SRM 51-20-01 AND INSTALLED PER 53-10-04. 2 L 7 4 4F A20WE 1996102400252 19961024 00252 NM 1996 10 24 P5CA9600809 1 19960916 A 5315 FLOORBEAM BOEING 747 747122 1384872 NM BS 700 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION ON FORWARD CARGO HOLD LATERAL FLOORBEAM UPPER CHORD UPPER SURFACE AT BS 780 RBL 15 TO RBL 23. CORROSI ON REMOVED PER BOEING SRM 51-10-01 WITHIN LIMITS PROTECTED PER 51-10-02. 2 L 7 4 4F A20WE 1996102400253 19961024 00253 WP 1996 10 24 RRXA96091 1 19960912 A 3233 ACTUATOR O-RING DOUG DC8 DC871F 302199D WP LT MLG FAILED A RRXA O OTHER K FLUID LOSS CR CRUISE 1 WP 15 8079U 45947 LOST HYDRAULIC FLUID DOWN TO STANDPIPE LEVEL IN CRUISE FLIGHT. ACCOMPLISHED HYDRAULIC FLUID OR PRESSURE LOSS CHECKLIST PER EWA QRH. MAINTENANCE REMOVED AND REPLACED O-RING ON LT RETRACT ACTUATOR, OPS CHECKS OK. 2 L 7 4 4F RT 4A25 1996102400254 19961024 00254 WP 1996 10 24 RRXA96118 1 19961011 A 5312 5772638103 BULKHEAD DOUG DC8 DC862F 3021972 WP BS 1606 HOLE A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 WHILE PREFORMING CONSTANT SECTION INSPECTION FOUND A 3 INCH HOLE IN AFT PRESSURE BULKHEAD WEB AT Y=1606 RT. REPAIRED BY DOUBLER REPAIR IAW DALFORT AVIATION EXPEDITE ENGINEERING AUTHORIZATION XEA: X8-53-866. 2 L 7 4 4F 4A25 1996102400255 19961024 00255 WP 1996 10 24 RRXA96119 1 19960830 A 2780 O-RING DOUG DC8 DC862 3021970 WP SLOT CONTL VLV FAILED A RRXA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 15 995CF 46024 ON CLIMBOUT, LOST HYDRAULIC SYSTEM PRESSURE, STOPPED QUANTITY LOSS AT 6 GALLONS INDICATED. LOSS OF HYDRAULIC SYSTEM AND PRESSURE EMERGENCY CHECKLIST FOLLOWED. MAINTENANCE REPLACED THE O-RING IN THE SLOT CONTROL VALVE MOUNT, SERVICED THE H YDRAULIC SYSTEM. HYDRAULIC POWERED FLT CONTROLS OPERATED NORMALLY ON GROUND CHECK, NO LEAKS NOTED. 2 L 7 4 4F 4A25 1996102400261 19961024 00261 WP 1996 10 24 RRXA96092 1 19960112 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 790-795 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8079U 45947 WHEEL WELL AT Y= 790 TO Y= 795, X=-3, SKIN HAS SKIN CORROSION DAMAGE PASS LIMITATIONS IAW SRM 53-2-0. REPAIRED INNER SK IN DAMAGE BY FABRICATING NEW SKIN PART IAW DAC DRWG 5642970, SRM 53-2-0, 51-3-2, 51-1-22 AND TREATED AREA IAW DC-8 SRM 5 1-1-8. 2 L 7 4 4F RT 4A25 1996102400262 19961024 00262 WP 1996 10 24 RRXA96093 1 19960112 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 790-795 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8079U 45947 WHEEL WELL AT Y= 790 TO Y= 795, X=33, SKIN HAS CORROSION DAMAGE PASS LIMITATIONS IAW SRM 53-2-0. REPAIRED INNER SKIN DA MAGE BY FABRICATING NEW SKIN PART IAW DAC-DRWG 5642970, SRM 53-2-0, 51-3-2, 51-1-22 AND TREATED AREA DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996102400263 19961024 00263 WP 1996 10 24 RRXA96094 1 19960206 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS270/285 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 LONGERON 28R BETWEEN Y=270 AND Y=285 CRACKED AND CORRODED. REPAIRED LONGERON 28R BY REPAIR STRAPS IAW REO 01816 AND TRE ATED AREA IAW SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996102400264 19961024 00264 WP 1996 10 24 RRXA96095 1 19960206 A 5320 DOUBLER DOUG DC8 DC871F 302199D WP BS 450-510 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 FINGER DOUBLER ATTACH TO LONGERON 31R AND OUTER SKIN BETWEEN Y= 450 AND Y= 510, CORROSION DAMAGE BEYOND LIMITATIONS IAW SRM 53-2-0. REPAIRED FINGER DOUBLER AND SKIN BY DOUBLER REPAIR IAW DWG 5779934, REPLACED LONGERON 31R AND TREATED IAW S RM 51-1-8. 2 L 7 4 4F RT 4A25 1996102400265 19961024 00265 WP 1996 10 24 RRXA96096 1 19960206 A 5320 WEB DOUG DC8 DC871F 302199D WP BS 520 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 TORQUE BOX WEB AT LONGERON 31R AND Y= 520, CORROSION DAMAGE BEYOND LIMITATIONS IAW SRM 53-2-0. REPAIRED WEB BY DOUBLER REPAIR IAW DWG 5753892 AND TREATED AREA IAW SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996102400266 19961024 00266 WP 1996 10 24 RRXA96098 1 19960206 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 1320-1350 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8087U 45977 LONGERON 31L BETWEEN Y=1320 AND Y=1250, CORROSION DAMAGE BEYOND LIMITATIONS IAW SRM 51-2-0. REPAIRED LONGERON 31L BY DO UBLER AND FILLER REPAIR IAW REO 01809 AND TREATED AREA IAW SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996102400267 19961024 00267 WP 1996 10 24 RRXA96099 1 19960302 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 980-990 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8084U 45974 DURING A MAINTENANCE VISIT, FOUND LONGERON 36 BETWEEN Y=980 TO Y=990 CORRODED. CORROSION DAMAGE PAST LIMITATIONS. REPA IRED LONGERON 36 BY REMOVING DAMAGE AND FABRICATING REPAIR STRAP AND SHIMS AND INSTALLED, IAW REO 01847 AND TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996102400268 19961024 00268 WP 1996 10 24 RRXA96100 1 19960302 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 990-1010 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8084U 45974 DURING A MAINTENANCE VISIT, FOUND LONGERON 31R BETWEEN Y=990 TO Y=1010 CORRODED. CORROSION DAMAGE PAST LIMITATIONS AFT ER BLEND-OUT. REPAIRED LONGERON 31R BY FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED IAW REO 01847 AND TREATED ARE A IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996102400269 19961024 00269 WP 1996 10 24 RRXA96101 1 19960302 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 1220-1240 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8084U 45974 DURING A MAINTENANCE VISIT, FOUND LONGERON 27R BETWEEN Y=1220 TO Y=1240 CORRODED. CORROSION DAMAGE PAST LIMITATIONS. R EPAIRED LONGERON 27R BY FABRICATING REPAIR STRAP AND INSTALLED IAW REO 01841 AND TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996102400270 19961024 00270 WP 1996 10 24 RRXA96102 1 19960516 A 5312 BULKHEAD CAP DOUG DC8 DC871F 302199D WP BS 70 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8076U 45941 LOWER BULKHEAD CAP AT Y=70, BETWEEN LONGERONS 31R AND 33R CORRODED AND CRACKED. LOWER BULKHEAD REPAIRED BY DOUBLER REPA IR SECURED WITH HL329-6 HI-LOCKS IAW REO 01903, SRM 51-1-20D, AND TREATED IAW SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996102400271 19961024 00271 WP 1996 10 24 RRXA96103 1 19960516 A 5312 BULKHEAD CAP DOUG DC8 DC871F 302199D WP BS 8 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8076U 45941 LOWER BULKHEAD CAP AT Y=8, BETWEEN LONGERONS 32R AND 33R CORRODED AND CRACKED. LOWER BULKHEAD CAP REPAIRED BY DOUBLER R EPAIR IAW REO 01903, SRM 51-1-20D AND TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996102400272 19961024 00272 WP 1996 10 24 RRXA96104 1 19960503 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 10501060 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 INTERNAL SKIN AT Y=1050 AND Y=1060 BETWEEN LONGERONS 35R AND35L CORROSION PAST LIMITATIONS. REPAIRED INTERNAL SKIN BY D OUBLER AND FILLER REPAIR IAW REO-01934 AND TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996102400273 19961024 00273 WP 1996 10 24 RRXA96105 1 19960503 A 5312 BULKHEAD DOUG DC8 DC871F 302199D WP BS 70 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 BULKHEAD CAP AT Y=70 BETWEEN LONGERONS 28L TO 28R CORROSION DAMAGE. BULKHEAD CAP REPAIRED BY DOUBLER AND FILLER REPAIR IAW REO-01930 AND TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996102400274 19961024 00274 WP 1996 10 24 RRXA96106 1 19960503 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 980-1020 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 SKIN AT Y=980 AND Y=1020 BETWEEN LONGERONS 36 TO 35L CORROSION DAMAGE PAST LIMITATIONS. SKIN REPAIRED BY DOUBLER AND FI LLER REPAIR IAW REO-01946 AND TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996102400275 19961024 00275 WP 1996 10 24 RRXA96107 1 19960503 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 70-80 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 LONGERON 31L BETWEEN Y=70 AND Y=80 CORROSION DAMAGE PAST LIMITATIONS. REPAIRED LONGERON 31L BY REMOVING 10 INCHES OF DA MAGE AREA AND INSTALLED SPLICE, DOUBLER AND FILLER REPAIR IAW REO-01929 AND TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996102400276 19961024 00276 WP 1996 10 24 RRXA96108 1 19960503 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 319 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 FRAME AT Y=319 AND LONGERON 29R CORROSION DAMAGE PAST LIMITATIONS. REPAIRED FRAME BY INSTALLING A STRAP REPAIR IAW REO- 01935, SRM 53-4-1 AND TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996102400277 19961024 00277 WP 1996 10 24 RRXA96109 1 19960503 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 500 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 LONGERON 29L AT Y=500, CORRSION DAMAGE PAST LIMITATIONS AFTER BLEND-OUT. REPAIRED LONGERON 29L BY DOUBLER REPAIR IAW RE O-01927, SRM 53-4-1 AND TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996102400278 19961024 00278 WP 1996 10 24 RRXA96110 1 19960503 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 600 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 FRAME AT Y=600 AND LONGERON 31L CORROSION DAMAGE PAST LIMITATIOINS AFTER BLEND-OUT. FRAME REPAIRED BY SPLICE REPAIR IA W REO-01932 AND TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996102400279 19961024 00279 WP 1996 10 24 RRXA96111 1 19960503 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 980 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 FRAME AT Y=980 BETWEEN LONGERONS 33L AND 33R CORROSION BLENDED OUT PAST LIMITATIONS. FRAME REPAIRED BY USING 2 ANGLES U SED AS DOUBLER SUPPORTS AND ONE ANGLE DOUBLER FOR STIFFENER IAW RFTTS ENGINEERING DISPOSITION 24-28787, SRM 53-2-0 AND T REATED AREA IAW SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996102400280 19961024 00280 WP 1996 10 24 RRXA96112 1 19960503 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 1080 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 INTERNAL SKIN AT Y=1080 AND LONGERON 36 CORRODED PAST LIMITATIONS. REPAIRED SKIN BY BLEND-OUT IAW REO-01933 AND TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996102400281 19961024 00281 WP 1996 10 24 RRXA96113 1 19960503 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 1120 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 INTERNAL SKIN AT Y=1120 AND LONGERON 36 CORRODED PAST LIMITATIONS. REPAIRED INTERNAL SKIN BY BLEND-OUT IAW REO-01938 AN D TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996102400282 19961024 00282 WP 1996 10 24 RRXA96114 1 19960503 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 1040-1445 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 LONGERON 34R BETWEEN Y=1040 AND Y=1445 CORROSION DAMAGE PAST LIMITATIONS. REPAIRED LONGERON 34R BY STRAP REPAIR IAW REO -01937 AND TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996102400283 19961024 00283 WP 1996 10 24 RRXA96115 1 19960503 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS1440 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 FRAME AT Y=1440 AND LONGERON 33R CORROSION DAMAGE PAST LIMITATIONS AFTER BLEND-OUT. REPAIRED FRAME BY INSTALLING A SPLI CE REPAIR IAW REO-01936 AND TREATED AREA DC-8 IAW SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996102400284 19961024 00284 WP 1996 10 24 RRXA96116 1 19960916 A 5320 154029 FITTING DOUG DC8 DC871F 302199D WP BS 20 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING MAINTENANCE VISIT, FOUND LONGERON END-FITTING AT LONGERON 34R AND Y=20 CORROSION DAMAGE PAST LIMITATIONS. REPAIR ED LONGERON END-FITTING BY FABRICATING NEW AND INSTALL IAW DAC DAW 4711722 AND TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996102400285 19961024 00285 NE 1996 10 24 TC8A96063 2 19961017 A 7532 563883 BLEED VALVE DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3B 52039 NE NR 3 ENGINE MALFUNCTIONED A TC8A E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 GL 23 181SK 45910 669217 IN CLIMBOUT, NR 3 ENGINE FIRE WARNING CAME ON. REMOVED AND REPLACED BLEED VALVE AND BLEED DUCT. CHECKED SYSTEM AS PER MM, OPS NORMAL. 2 L 7 4 4F 4 F 4A25 1E8 1996102400286 19961024 00286 NE 1996 10 24 TC8A96064 2 19961016 A 7532 560339 BLEED VALVE DOUG DC8 DC8F54 3021926 WP PWA JT3D JT3D3B 52039 NE NR 3 ENGINE MALFUNCTIONED A A TC8A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 802CK 18514 18514 45679 643688 NUMBER 3 ENGINE VERY SLOW TO ACCELERATE. REMOVED AND REPLACED NUMBER 3 ENGINE INTERSTAGE BLEED VALVE, ENGINE RUN-UP IAW MM CHAPTER 72-00, ALL PARAMETERS WERE NORMAL. 2 L 7 4 4F 4 F 4A25 1E8 1996102400287 19961024 00287 WP 1996 10 24 TC8A96065 1 19961017 A 2612 FIRE WIRE DOUG DC8 DC8F54 3021926 WP NR 1 ENGINE BROKEN A TC8A K NONE N FALSE WARNING UK UNKNOWN 1 GL 23 802CK 45679 NUMBER 1 ENGINE FIRE WARNING OPERATING IN AN INTERMITTENT MANNER. REPAIRED BROKEN WIRE AT FIRE WALL DOOR LOOP PLUG, SYS TEM OPS CHECKS NORMAL AS PER MM 26-10-1. 2 L 7 4 4F 4A25 1996102400288 19961024 00288 WP 1996 10 24 TC8A96066 1 19961017 A 2611 BULB DOUG DC8 DC8F54 3021926 WP NR 2 SMOKE DET MALFUNCTIONED A TC8A O OTHER N FALSE WARNING CR CRUISE 1 GL 23 802CK 45679 CARGO SMOKE LIGHT CAME ON DURING FLIGHT WITHOUT ANY VISIBLE SMOKE IN THE CARGO COMPARTMENT. RELAMPED NR 2 SMOKE DETECTO R, SYSTEM OPS CHECKS NORMAL AS PER MM 26-10-5. 2 L 7 4 4F 4A25 1996102400289 19961024 00289 WP 1996 10 24 SRAA961009 1 19961008 A 2750 LOCK OUT CYL DOUG DC8 DC873F 302199F WP TE FLAPS REQD SERVICE A SRAA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 23 875SJ 46063 FLAP INDICATION SPLIT BY ONE NEEDLE WIDTH AT 23 DEGREES AND FULL FLAP, CAUSING THE AIRCRAFT TO ROLL RIGHT. AIRCRAFT LAN DED WITHOUT INCIDENT. SERVICED AND BLED FLAP LOCK OUT CYLINDER, OPS CHECKED SYSTEM PER MM CH 27-51-10. 2 L 7 4 4F RT 4A25 1996102400290 19961024 00290 WP 1996 10 24 SRAA961011 1 19961016 A 2750 FLAP MECHANISM DOUG DC8 DC873F 302199F WP RT TE FLAP OUT OF ADJUST A SRAA K NONE F FLT CONT AFFECTED AP APPROACH 1 GL 23 875SJ 46063 EXPERIENCED SPLIT FLAP AT 23 DEGREES AND AIRCRAFT ROLLED TO THE RIGHT, ACCOMPLISHED AIR TURNBACK TO MIA. AIRCRAFT LANDE D WITHOUT INCIDENT. PERFORMED FLAP BUS TENSION CHECK, FOUND OUT OF LIMITS. INSPECTED FLAP WELL AND FOUND FLAPERETE ON RHS LOOSE, SECURED FLAPERETE AND RE-RIGGED FLAP CONTROL SYSTEM. BUS TENSION CHECKED GOOD PER MM CH 27-50-0. 2 L 7 4 4F RT 4A25 1996102400291 19961024 00291 SW 1996 10 24 HEEA968188 1 19961010 A 5610 M206R31113 CHIN BUBLE BELL 206 206L1 1182107 SW LT FWD DEFECTIVE E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 WINDOW IS NOT ACCEPTABLE FOR USE AT PHI. HAS ABRASIONS ON EDGE. 1 G 7 1 3U H2SW 1996102400292 19961024 00292 NE 1996 10 24 HEEA968189 1 19961010 A 6210 7615009100051A BLADE SKRSKY S76 S76A 8143006 NE M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 15460 7237 760223 BLADE IS CRACKED. (REMOVED TO COMPLY WITH 500 HOUR INSPECTION - FOUND SEVERAL CRACKS ON THE TITANIUM STRIP WITH SEPARAT ION. THE CRACK AT STATION 123" HAS MULTIPLE BRANCHES. 1 G 7 2 3U H1NE 1996102400294 19961024 00294 EU 1996 10 24 HEEA968191 1 19961010 A 6410 10531757 BLADE BOLKMS 105 BO105S 5626006 EU T/R WRONG PART E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 461 BLADES ARE DIFFERENT. P/N DOES NOT COMPLY WITH BO105S139. REMOVED FROM N8199J AT AIRCRAFT TOTAL TIME 619.4. 1 G 7 2 3U H3EU 1996102400295 19961024 00295 SW 1996 10 24 HEEA968192 1 19961010 A 6520 206040440001 PINION BELL 206 206BELL 1181502 SW T/R GR BOX DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6262 REMOVED FROM T/R GEARBOX S/N AFS2844 DUE TO IRREGULAR TRACK PATTERN. 1 G 7 1 3U H2SW 1996102400296 19961024 00296 SW 1996 10 24 HEEA968193 1 19961010 A 6520 206040439001 SHAFT BELL 206 206BELL 1181502 SW T/R GR BOX DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6262 SHAFT REMOVED FROM T/R GEARBOX S/N AFS2844 DUE TO IRREGULAR TRACK PATTERN. 1 G 7 1 3U H2SW 1996102400297 19961024 00297 NM 1996 10 24 HEEA968194 1 19961010 A 6210 369D21100516 BLADE DOUG MD900 MD900 3027375 NM M/R BLISTERED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 780 ON POST FLIGHT WALK AROUND, NOTICED A BLISTER IN THE BOTTOM SIDE OF THE M/R BLADE ABRASION STRIP. 1 G 7 2 3U NC H19NM 1996102400299 19961024 00299 1996 10 24 HEEA968196 4 19961010 A 3422 066306001 INDICATOR KNI582 BELL 212 212 1181420 SW COCKPIT ERROR E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3208H 31304 NAV INDICATOR POINTS 60 DEGREES OFF. 1 G 7 1 4U H4SW 1996102400300 19961024 00300 1996 10 24 HEEA968197 4 19961010 A 3442 MI5851345 INDICATOR P40 SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 31217 760229 NO PICTURE. 1 G 7 2 3U H1NE 1996102400301 19961024 00301 SW 1996 10 24 HEEA968199 1 19961010 A 6300 214040991105 HOUSING SET BELL 214 214ST 1182106 SW M/R DRIVE FLANGE DEFECT E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 DEFECTS ON REPAIR PERFORMED ON FLANGES. 2 G 7 2 4U H10SW 1996102400302 19961024 00302 NM 1996 10 24 HEEA968200 1 19961010 A 7160 900P3620001105 SEPARATOR DOUG MD900 MD900 3027375 NM INTAKE PART SEP SEPARATION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 9214U 134 134 90000014 WHEN PARTICLE SEPARATOR PANELS WERE REMOVED FOR ENGINE CHANGE, FOUND LOWER SECTION SEPARATED FROM PANEL. 1 G 7 2 3U NC H19NM 1996102400303 19961024 00303 NM 1996 10 24 HEEA968201 1 19961010 A 7120 900P3620001106 SEPARATOR DOUG MD900 MD900 3027375 NM INTAKE PART SEP SEPARATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 9214U 134 134 90000014 WHEN PARTICLE SEPARATOR PANELS WERE REMOVED FOR ENGINE CHANGE, FOUND LOWER SECTION SEPARATED FROM PANEL. 1 G 7 2 3U NC H19NM 1996102400304 19961024 00304 EU 1996 10 24 HEEA968202 1 19961010 A 2121 420800001 BLOWER SNIAS 350 AS350B2 8680813 EU COOLING FAN FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6095S 60 2777 BLOWER WILL NOT RUN. 1 G 7 1 3U H9EU 1996102400305 19961024 00305 NM 1996 10 24 HEEA968203 1 19961010 A 6700 900C3010004105 TRIM ACTUATOR DOUG MD900 MD900 3027375 NM FLT CONTROL INTERMITTENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 9214U 90000014 INTERMITTENT OPERATION WITH 33 OHM RESISTOR AND 280HM RESISTOR. 1 G 7 2 3U NC H19NM 1996102400307 19961024 00307 1996 10 24 HEEA968205 4 19961010 A 3442 7007700705 INDICATOR P700 BELL 230 230 1182149 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 23009 DOES NOT PICK UP GOOD SIGNAL BEYOND 15-20 MILE RANGE, VERY WEAK. TIME SINCE REPAIR 2310:55. 1 G 7 2 3U NC H9SW 1996102400308 19961024 00308 EU 1996 10 24 HEEA968206 1 19961010 A 7712 53516 TRANSMITTER SNIAS 350 AS350B2 8680813 EU ENG TORQUE READS HIGH E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 2771 TORQUE READS 4% HIGH. 1 G 7 1 3U H9EU 1996102400310 19961024 00310 EU 1996 10 24 HEEA968208 1 19961010 A 6520 3160S66100005 GEARBOX AEROSP SA316 SA316B 8680207 EU T/R LEAKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 LEAKS AT INPUT SEAL, OUTPUT AND PITCH CHANGE SHAFT WEAR ON PITCH CHANGE SHAFT AND SPLINES. REMOVED FROM AIRCRAFT N37074 . SENT TO NAMPA VALLEY HELICOPTERS FOR EXCHANGE. 1 G 7 1 4U H1IN 1996102400311 19961024 00311 1996 10 24 HEEA968209 4 19961010 A 3418 10138000517 LIFT COMPUTER BEECH 200 200BEECH 1152920 CE STALL SYS DEFECTIVE E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 WARRANTY SEAL BROKEN UPON RECEIPT. REFERENCE: BEECH 200 MM 27-31-00 PG. 201 STEP F: VOLTAGE TEST FAILURE (10.54VAC), STEP G: 24.5 VDC OK, STEP H: VOLTAGE TEST FAILURE (1.04V), HORN FAILS TO ACTIVATE WITH ANY FORCE. ALL A/C WIRING, GRO UNDS ANDTEST EQUIPMENT OK. 1 L 7 2 4T A24CE 1996102400312 19961024 00312 SW 1996 10 24 HEEA968210 1 19961010 A 7712 206075739103 TORQUEMETER BELL 206 206L3 1182108 SW ENGINE DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 206FS 51506 ENGINE TORQUE GAUGE FLUCTUATES. 1 G 7 1 3U H2SW 1996102400313 19961024 00313 SW 1996 10 24 HEEA968211 1 19961010 A 6322 214076333107 MOTOR BELL 214 214ST 1182106 SW BLOWER SEAL LEAK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 BLOWER MOTOR SHAFT SEAL LEAKING. 2 G 7 2 4U H10SW 1996102400314 19961024 00314 1996 10 24 HEEA968212 4 19961010 A 3421 7660002113103 GYRO SKRSKY S76 S76A 8143006 NE COCKPIT VG PRECESSES E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546K 760082 GYRO SLOW TO BECOME OPERATIONAL, PRECESSES. 1 G 7 2 3U H1NE 1996102400315 19961024 00315 SW 1996 10 24 HEEA968213 1 19961010 A 5510 206023119151 STABILIZER ASSY BELL 206 206L1 1182107 SW AUX FIN ANGLE MIS MFG E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 LH SIDE OF STABILIZER AT CENTER, MEASURES 1.778, ANGLES ON AUX FIN MEASURE 1.704 WHICH MAKES STABILIZER .074 TOO THICK. RH SIDE OF STABILIZER AT CENTER MEASURES 1.799 ANGLES ON AUX FIN MEASURES 1.708 WHICH MAKES STAB. .091 TOO THICK. 1 G 7 1 3U H2SW 1996102400316 19961024 00316 EU 1996 10 24 HEEA968214 1 19961010 A 2422 2A10001G INVERTER BOLKMS 117 BK117A4 5626017 EU AC SYS DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911RZ 7092 NOISE IN #2 VHF RADIO FREQUENCY RANGE 118-136. NEEDS MOD "A". UNIT LOCATED IN VERY HOT AREA. 1 G 7 2 3U H13EU 1996102400317 19961024 00317 1996 10 24 HEEA968215 4 19961010 A 2210 214074303115 AMPLIFIER ASSY BELL 214 214ST 1182106 SW COCKPIT ALT HOLD MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 ALT HOLD WILL NOT ENGAGE. 2 G 7 2 4U H10SW 1996102400318 19961024 00318 SW 1996 10 24 HEEA968216 1 19961011 A 6330 230030535103 BEARING BELL 230 230 1182149 SW RT XMSN MT WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 1670 23009 PART IS WORN EXCESSIVELY. (BEARING WORN ON RIGHT TRANSMISSION ISOLATION MOUNT) 1 G 7 2 3U NC H9SW 1996102400319 19961024 00319 SW 1996 10 24 HEEA968217 1 19961011 A 6330 222331618105 ISOLATION MOUNT BELL 230 230 1182149 SW XMSN BEARING WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 175 23009 ISOLATION MOUNT WORN BEARING. 1 G 7 2 3U NC H9SW 1996102400320 19961024 00320 SW 1996 10 24 HEEA968218 1 19961011 A 6330 230030535103 BEARING BELL 230 230 1182149 SW M/R XMSN MT WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 1587 23009 WORN BEARING. 1 G 7 2 3U NC H9SW 1996102400321 19961024 00321 SW 1996 10 24 HEEA968219 1 19961011 A 6220 407010111101 CONE SET BELL 407 407 SW M/R DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407PH 588 53003 COULD NOT TRACK AND BALANCE MAIN ROTOR SYSTEM. 1 G 7 1 3U O H2SW 1996102400322 19961024 00322 NE 1996 10 24 HEEA968221 2 19961011 A 7310 430137601 FUEL NOZZLE BOLKMS 117 BK117B2 5626013 EU LYC LTS101 LTS101750B1 41560 NE ENGINE LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 134AE 1940 7237 LE45758AEF AIRCRAFT ENGINE LEAK CHECK REVEALED: FUEL LEAKING FROM FUEL MANIFOLD TUBING. INSTALLED A SERVICEABLE MANIFOLD. 1 G 7 2 3U 3 U NC H13EU E5NE10 1996102400323 19961024 00323 GL 1996 10 24 HEEA968222 2 19961011 A 7230 6851430 REAR DIFFUSER 6890550 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL BEARING BORE MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 4573B CAC24057 S673 CAE895939 RECEIVING INSPECTION REVEALED: BEARING BORE UNDERSIZED MEASURED 2.165 (SPECS 2.1654 - 2.1659) ON REAR DIFFUSER. 1 G 7 2 3U 3 U H3EU E4CE 1996102400324 19961024 00324 SW 1996 10 24 HEEA968223 1 19961011 A 6300 406012129101 LINK ASSEMBLY BELL 407 407 SW M/R DRIVE WORN BEARING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407PH 598 53003 WORN BEARING ON FIXED ROD END SIDE. 1 G 7 1 3U O H2SW 1996102400325 19961024 00325 SW 1996 10 24 HEEA968224 1 19961011 A 2840 222366621103 FUEL FILTER BELL 407 407 SW TEST FUNCTION DEFECTIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 407PH 380 53003 TEST BUTTON WILL NOT MAKE LIGHT COME ON. 1 G 7 1 3U O H2SW 1996102400326 19961024 00326 SW 1996 10 24 HEEA968225 1 19961011 A 5302 222035352105 FITTING ASSY BELL 230 230 1182149 SW T/R HOLE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 2425 23009 WORN BOLT HOLE. 1 G 7 2 3U NC H9SW 1996102400327 19961024 00327 GL 1996 10 24 HEEA968226 2 19961011 A 7260 23055466 GEARBOX COVER 6894171 BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL ENGINE DEFECTIVE E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 2268X CAG33413 3607 CAE821999F ENGINE REMOVED DUE TO AFT T/M LEAK. UPON INSPECTION OF GEARBOX PARTS NOTED: T/M BORE TO BUSHING HAS A LINE TO LINE FIT ON COVER ASSY. INSTALLED A NEW COVER ASSY. 1 G 7 1 3U 3 U H2SW E4CE 1996102400328 19961024 00328 GL 1996 10 24 HEEA968227 2 19961011 A 7250 23055430 NOZZLE 230033185 BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL ENGINE EXCESS RUNOUT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2772A CAT70274 45311 CAE860387 DISASSEMBLED TURBINE DUE TO N1 TIP DRAG ON TEST CELL. UPON INSPECTION OF TURBINE PARTS NOTED: EXCESSIVE RUNOUT .007 BE YOND SERVICEABLE LIMITS ON #2 NOZZLE #1 AND #2 TIP PATHS. INSTALLED A DALLAS AIRMOTIVE OVERHAULED #2 NOZZLE. 1 G 7 1 3U 3 U H2SW E1GL 1996102400330 19961024 00330 SW 1996 10 24 HEEA968229 1 19961011 A 2435 214060056103 STARTER BELL 214 214ST 1182106 SW START/GEN FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 STARTER WILL NOT ENGAGE, BURNT ARMATURE. 2 G 7 2 4U H10SW 1996102400331 19961024 00331 SW 1996 10 24 HEEA968230 1 19961011 A 7712 206075739103 TORQUEMETER BELL 206 206L3 1182108 SW ENG TORQUE READS LOW E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3107N 51512 TORQUMETER LOW, OUT OF TOLERANCE AT 100% AND ABOVE. 1 G 7 1 3U H2SW 1996102400332 19961024 00332 1996 10 24 HEEA968231 4 19961011 A 2210 214074303115 AMPLIFIER ASSY BELL 214 214ST 1182106 SW COCKPIT ALT HOLD FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 ALT HOLD INOPERATIVE. 2 G 7 2 4U H10SW 1996102400333 19961024 00333 1996 10 24 HEEA968232 4 19961011 A 2210 574074264001 ALT CONTROLLER BELL 214 214ST 1182106 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 ALT HOLD UNRELIABLE. 2 G 7 2 4U H10SW 1996102400334 19961024 00334 EU 1996 10 24 HEEA968233 1 19961011 A 7933 53062550011 INDICATOR AEROSP AS355 AS355F1 8680810 EU OIL TEMP READS LOW E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5774M 5009 OIL TEMP STAYS IN YELLOW, VERY LOW. 1 G 7 2 3U H11EU 1996102400335 19961024 00335 SW 1996 10 24 HEEA968234 1 19961011 A 7931 APTE138100G TRANSMITTER BELL 412 412 1182202 SW OIL PRESS DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893N 33010 TRANSMITTER CAUSED LOW OIL PRESSURE READINGS. 1 G 7 2 4U H4SW 1996102400336 19961024 00336 1996 10 24 HEEA968235 4 19961011 A 2210 214074303115 AMPLIFIER ASSY BELL 214 214ST 1182106 SW COCKPIT ALT HOLD DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 ALT HOLD LIGHT TOO DIM ENGAGE LIGHT. 2 G 7 2 4U H10SW 1996102400337 19961024 00337 SW 1996 10 24 HEEA968236 1 19961011 A 7712 206075739103 TORQUEMETER BELL 206 206L3 1182108 SW COCKPIT STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31077 51520 TORQUEMETER STICKS AT 75-80%. 1 G 7 1 3U H2SW 1996102400338 19961024 00338 SW 1996 10 24 HEEA968238 1 19961011 A 2435 214060056103 STARTER BELL 214 214ST 1182106 SW ENGINE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 75 28106 WILL NOT DISENGAGE AT PRESENT RPM AND OCCASIONALLY WILL DISENGAGE EARLY. 2 G 7 2 4U H10SW 1996102400339 19961024 00339 SW 1996 10 24 HEEA968239 1 19961011 A 2435 214060056103 STARTER BELL 214 214ST 1182106 SW ENGINE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 818 28106 STARTER HAS BURNT CURRENT LIMITING RESISTOR, CLUTCH END PLAY IS OVERPOINT .010 AND TERMINAL BLOCK AND COVER IS CRACKED. 2 G 7 2 4U H10SW 1996102400340 19961024 00340 EU 1996 10 24 HEEA968240 1 19961011 A 6400 741C000005 ACTUATOR BOLKMS 117 BK117B1 5626012 EU T/R LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 911TL 7198 T/R ACTUATOR LEAKING EVERYWHERE. 1 G 7 2 3U H13EU 1996102400341 19961024 00341 1996 10 24 HEEA968241 4 19961011 A 3421 4021541671 GYRO BOLKMS 117 BK117B1 5626012 EU COCKPIT HORIZ DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911TL 7198 FLAG PULLS BUT VERY SLOW TO ERECT 45 DEGREE/15 MINUTES. 1 G 7 2 3U H13EU 1996102400342 19961024 00342 1996 10 24 HEEA968242 4 19961011 A 2562 ELT910 ELT NARCO BOLKMS 105 BO105S 5626006 EU COCKPIT MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7136J S830 ELT GOES OFF INADVERTENTLY. 1 G 7 2 3U H3EU 1996102400343 19961024 00343 1996 10 24 HEEA968243 4 19961011 A 2562 ACRRLB21 EPIRB BOLKMS 105 BO105S 5626006 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3071K S859 EPIRB (RESCUE BEACON) INOPERATIVE. NO LIGHT OR SIGNAL. SENT TO ACR ELECTRONICS, INC. FOR REPAIR. 1 G 7 2 3U H3EU 1996102400344 19961024 00344 SW 1996 10 24 HEEA968244 1 19961011 A 5260 FYLM735023 MOTOR ASSY BELL 412 412 1182202 SW STEP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 108X 33115 ARMATURE HAS DEAD SPOT. 1 G 7 2 4U H4SW 1996102400345 19961024 00345 1996 10 24 HEEA968245 4 19961011 A 2210 7690001802106 ACTUATOR SKRSKY S76 S76A 8143006 NE AFCS DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546K 4568 760082 ACTUATOR INTERMITTENTLY MOVES FROM RIGHT TO LEFT. TIME SINCE REPAIR 905:40. 1 G 7 2 3U H1NE 1996102400346 19961024 00346 1996 10 24 HEEA968246 4 19961011 A 3422 2891ESR GYRO AEROSP AS355 AS355F1 8680810 EU COCKPIT DG DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5793Z 5142 UNIT PRECESSING AND SLAVE METER WILL NOT SWING. 1 G 7 2 3U H11EU 1996102400347 19961024 00347 1996 10 24 HEEA968247 4 19961011 A 3422 2891ESR GYRO BELL 206 206L1 1182107 SW COCKPIT DG DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3905B 45598 UNIT PRECESSING AND SLAVE SYSTEM INOPERATIVE. 1 G 7 1 3U H2SW 1996102400348 19961024 00348 1996 10 24 HEEA968248 4 19961011 A 3422 2891ESR GYRO BELL 206 206L1 1182107 SW COCKPIT DG DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5737T 45454 UNIT PRECESSING AND SLAVE SYSTEM INOPERATIVE. 1 G 7 1 3U H2SW 1996102400349 19961024 00349 SW 1996 10 24 HEEA968249 1 19961011 A 6730 206076062003 CYLINDER BELL 206 206L3 1182108 SW M/R LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 3108E 51498 LEAKING AT PILOT VALVE. 1 G 7 1 3U H2SW 1996102400350 19961024 00350 NE 1996 10 24 HEEA968250 1 19961011 A 6322 7630807902106 BLOWER SKRSKY S76 S76A 8143006 NE OIL COOLER IMPELLER LOOSE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3122H 760233 BLOWER IMPELLER LOOSE ON SHAFT. 1 G 7 2 3U H1NE 1996102400351 19961024 00351 NE 1996 10 24 HEEA968251 1 19961011 A 6220 7610608000047 DAMPER SKRSKY S76 S76A 8143006 NE M/R DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3122H 760233 DAMPER INNER BUSHING CAVITY OVERSIZED. 1 G 7 2 3U H1NE 1996102400352 19961024 00352 NE 1996 10 24 HEEA968252 1 19961011 A 6220 7610608000049 DAMPER SKRSKY S76 S76A 8143006 NE M/R DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22342 760096 DAMPER INNER BUSHING CAVITY OVERSIZED. 1 G 7 2 3U H1NE 1996102400353 19961024 00353 SW 1996 10 24 HEEA968253 1 19961011 A 3212 206377010 BOTTLE ASSY BELL 206 206L1 1182107 SW FLOAT FAILED TEST E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 UNIT CONDEMNED. THE BOTTLE FAILED HYROSTATIC TEST BECAUSE IT WOULD NOT HOLD PRESSURE. IT ALSO HAD A POPPING NOISE WHEN THE PRESSURE WAS RELEASED. 1 G 7 1 3U H2SW 1996102400354 19961024 00354 SW 1996 10 24 HEEA968254 1 19961011 A 3212 206377010 BOTTLE ASSY BELL 206 206L1 1182107 SW FLOAT FAILED TEST E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 UNIT CONDEMNED. THE BOTTLE FAILED HYROSTATIC TEST BECAUSE IT WOULD NOT HOLD PRESSURE. IT ALSO HAD A POPPING NOISE WHEN THE PRESSURE WAS RELEASED. 1 G 7 1 3U H2SW 1996102400355 19961024 00355 SW 1996 10 24 HEEA968255 1 19961011 A 3212 206377010 BOTTLE ASSY BELL 206 206L1 1182107 SW FLOAT FAILED TEST E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 UNIT CONDEMNED. THE BOTTLE FAILED HYROSTATIC TEST BECAUSE IT WOULD NOT HOLD PRESSURE. IT ALSO HAD A POPPING NOISE WHEN THE PRESSURE WAS RELEASED. 1 G 7 1 3U H2SW 1996102400356 19961024 00356 SW 1996 10 24 HEEA968256 1 19961011 A 3212 206377010 BOTTLE ASSY BELL 206 206L1 1182107 SW FLOAT FAILED TEST E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 UNIT CONDEMNED. THE BOTTLE FAILED HYROSTATIC TEST BECAUSE IT WOULD NOT HOLD PRESSURE. IT ALSO HAD A POPPING NOISE WHEN THE PRESSURE WAS RELEASED. SENT TO AERONAUTICAL ACCESSORY, INC. FOR CREDIT. 1 G 7 1 3U H2SW 1996102400357 19961024 00357 SW 1996 10 24 HEEA968257 1 19961011 A 6730 C4264214 SERVO VALVE 206076062003 BELL 206 206BELL 1181502 SW M/R DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 RH4275A UPON TESTING SERVO WITH A REPAIRED S/S ASSEMBLY, FOUND INTERNAL LEAK IN NEUTRAL POSITION ABOVE 100CC PER MIN. UPON DISA SSEMBLING A SCRATCH MARK WAS FOUND IN CENTER LOBE OF P/N C42642-40. 1 G 7 1 3U H2SW 1996102400358 19961024 00358 SW 1996 10 24 HEEA968258 1 19961011 A 5610 407030607115S WINDOW BELL 407 407 SW COCKPIT BROKEN E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 417PH 48 53038 WINDOW BROKEN. 1 G 7 1 3U O H2SW 1996102400360 19961024 00360 SW 1996 10 24 HEEA968260 1 19961011 A 2913 214076334105 PUMP BELL 214 214ST 1182106 SW HYD METAL CONTAM E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 HYD PUMP METAL CONTAMINATION. 2 G 7 2 4U H10SW 1996102400361 19961024 00361 EU 1996 10 24 HQEA962 1 19960911 A 2810 109061102112 TANK ASSY 109061102112 AGUSTA A109 A109C 0260118 EU UPPER NIPPLE BROKEN E HQEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NE 05 100S 1328 62066 7644 TANK ASSY IS BROKEN. FOUND UPPER NIPPLE WHERE AUX FUEL TRANSFER TUBE ATTACHES TORN OFF. THE AUX FUEL WAS NOT TRANSFERI NG INTO THE FORWARD PART OF THE TANK. WHEN REMOVING THE TANK FOR REPAIR, A 7/8" WRENCH WAS FOUND UNDER THE TANK. THIS TANK WAS ORIGINAL EQUIPMENT INSTALLED AT THE FACTORY. SENT TANK TO AUTHORIZED REPAIR STATION FOR REPAIR. 1 G 7 2 3U H7EU 1996102400362 19961024 00362 EU 1996 10 24 HQEA963 1 19960912 A 5551 109095119103 SUPPORT BRACKETS 109095119103 AGUSTA A109 A109C 0260118 EU HORIZ STAB CRACKED E HQEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NE 05 652DH 587 7652 BRACKET IS CRACKED. THE -103 IS .050" STAINLESS STEEL. THIS REPLACED THE EARLIER ALUMINUM BRACKET. THE REPLACEMENT PA RT -111 IS .062" STAINLESS STEEL. THE CRACKED PART HAD TOOLING MARKS AT THE CORNERS WHERE THE CRACKS PROPAGATED. INSTAL LED NEW -111 BRACKET. 1 G 7 2 3U H7EU 1996102400365 19961024 00365 CE 1996 10 24 C2XA96CL021 1 19960827 A 3260 1003810061 SWITCH BEECH 1900 1900D 1154162 CE NLG DIRTY A C2XA O OTHER P NO WARNING INDICATION AP APPROACH 1 SW 09 49543 UE181 CLE - FLT 3242 - CREW REPORTED AFTER LANDING GEAR EXTENSION, NOSE GEAR LIGHT DID NOT ILLUMINATE. THE CREW RECEIVED NO W ARNING HORN WITH THE POWER REDUCED OR WITH FLAPS SET AT 35 DEGREES, THE LIGHT TESTED PROPERLY WITH THE PRESS-TO-TEST SWI TCH. THE LIGHT DID ILLUMINATE AFTER CYCLING THE LANDING GEAR 3 TIMES. MAINTENANCE INSPECTED AIRCRAFT AND CLEANED NOSE GEAR DOWNLOCK SWITCH, OPERATIONAL CHECKS WERE GOOD IAW B1900D MM 32-30-00. THE ACFT RELEASED FOR SERVICE. (X) 2 L 7 2 4T RT A24CE 1996102400366 19961024 00366 CE 1996 10 24 C2XA96CL020 1 19960826 A 3230 1143640681 PC BOARD BEECH 1900 1900D 1154162 CE LANDING GEAR FAULTED A C2XA O OTHER J WARNING INDICATION LD LANDING 1 SW 09 49543 UE181 CLE - FLT 3102 - CREW REPORTED LANDING GEAR HANDLE WOULD NOT GO INTO RETRACT POSITION WITHOUT USING DOWNLOCK RELEASE BUT TON. MAINTENANCE INSPECTED AND RELEASED ACFT IAW B1900D MEL NR 32-8, CONTROL NR 89516. ON 8-28-96, MAINTENANCE REMOVED AND REPLACED THE PRINTED CIRCUIT BOARD IAW B1900D MM 32-31-01. OPERATIONAL CHECKS WERE GOOD IAW B1900D MM 32-30-00. T HE AIRCRAFT WAS REMOVED FROM MEL AND RELEASED FOR SERVICE. (X) 2 L 7 2 4T RT A24CE 1996102400367 19961024 00367 CE 1996 10 24 C2XA96CL019 1 19960823 A 3260 1293640693 INDICATOR BEECH 1900 1900D 1154162 CE NLG FAULTED A C2XA O OTHER P NO WARNING INDICATION AP APPROACH 1 SW 09 49543 UE181 CLE - FLT 3278 - CREW REPORTED WHEN LANDING GEAR WAS EXTENDED, NOSE GEAR LIGHT DID NOT ILLUMINATE. THE CREW CYCLED THE LANDING GEAR TWICE AND THE NOSE GEAR LIGHT ILLUMINATED, ALL OTHER INDICATIONS WERE NORMAL. MAINTENANCE INSPECTED THE AI RCRAFT AND REMOVED AND REPLACED THE LANDING GEAR INDICATOR IAW B1900D MM 32-10-00. OPERATIONAL CHECKS WERE GOOD IAW B19 00D MM 32-60-00. AIRCRAFT RELEASED FOR SERVICE. (X) 2 L 7 2 4T RT A24CE 1996102400368 19961024 00368 CE 1996 10 24 C2XA96CL023 1 19960930 A 3260 1003810061 SWITCH 114820021601 BEECH 1900 1900D 1154162 CE NLG DIRTY A C2XA K NONE O OTHER AP APPROACH 1 SW 09 49543 548A95 UE181 CLE - FLT 3107 - CREW REPORTED GREEN LIGHT FOR THE NOSE LANDING GEAR CAME ON ABOUT ONE MINUTE AFTER GEAR EXTENSION, NO O THER WARNING INDICATIONS. MAINTENANCE INSPECTED AIRCRAFT AND CLEANED NOSE GEAR MICROSWITCHES. OPERATIONAL CHECKS WERE GOOD IAW B100D MM 32-30-00. AIRCRAFT WAS RELEASED FOR SERVICE. (X) 2 L 7 2 4T RT A24CE 1996102400369 19961024 00369 CE 1996 10 24 C2XA96CL027 1 19960904 A 3233 11238002223 ACTUATOR BEECH 1900 1900D 1154162 CE NLG FAILED A C2XA O OTHER P NO WARNING INDICATION AP APPROACH 1 SW 09 49543 1883 471 UE181 CLE - FLT 3097 - CREW REPORTED THE NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. THE GREEN LIG HT DID ILLUMINATE AFTER THE LANDING GEAR WAS CYCLED SEVERAL TIMES. MAINTNANCE INSPECTED ACFT AND REMOVED AND REPLACED N OSE GEAR ACTUATOR IAW B1900D MM 32-30-14. THE NLG WAS RIGGED AND ADJUSTED IAW B1900D, MM 32-30-13, 32-60-01, AND 32-60- 01. OPERATIONAL CHECKS WERE GOOD, AIRCRAFT RELEASED FOR SERVICE. (X) 2 L 7 2 4T RT A24CE 1996102400370 19961024 00370 NM 1996 10 24 96ZZZX5314 1 19960830 A 2597 C0294660 WIRE BOEING 747 747128 1384894 NM CABIN SEAT SHORTED A TWAA F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 CE 05 129TW 21141 LGW - FLT 720 - DURING LANDING, SPARKS EMITTED FROM UNDER SEAT 31-7. USED HALON EXTINGUISHER. FOUND SEAT ELECRONIC UNI T CABLE SHORTED UNDER CHAIR LEG, MFG P/N C02946-60. REPLACED SEAT ELECTRONIC UNIT CABLE AND ALL SEAT CONTROLS OPERATION CHECKED NORMAL. CHECK C-2 - 6-22-96 - MZJ. (X) 2 L 7 4 4F A20WE 1996102400371 19961024 00371 NM 1996 10 24 96ZZZX5315 1 19960827 A 2530 OVEN BOEING 747 747128 1384894 NM GALLEY SMOKING A TWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 129TW 21141 JFK - FLT 903 - DURING CRUISE FIRST CLASS GALLEY OVEN 1-6 EMITTED SMOKE. TURNED OFF OVEN. FOUND FOOD SPILLAGE IN OVEN. CLEANED OVEN, OVEN OPERATION THEN CHECKED NORMAL. CHECK C-2 - 6-22-96 - MZJ. 2 L 7 4 4F A20WE 1996102400374 19961024 00374 WP 1996 10 24 GTIA96NK189 1 19960816 A 5350 RELEASE MECH DOUG DC9 DC921 302205A WP TAIL CONE OUT OF ADJUST A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 125NK 47302 LOG PAGE 027001. TAIL CONE FAILED TO RELEASE DURING TAIL CONE RELEASE SYSTEM CHECK. ADJUSTED TAIL CONE RELEASE SYSTEM MECHANISM IAW DC-9 MM 53-50-0. OPS CHECKS GOOD. (X) 2 L 7 2 4F A6WE 1996102400375 19961024 00375 EU 1996 10 24 HQEA000002 1 19960911 A 2810 109061102112 TANK ASSY AGUSTA A109 A109C 0260118 EU AUX FUEL DEFECTIVE A HQEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NE 05 100S 1328 62066 7644 PART IS BROKEN. FOUND UPPER NIPPLE WHERE AUXILIARY FUEL TRANSFER TUBE ATTACHES TORN OFF. THE AUXILIARY FUEL WAS NOT TR ANSFERRING INTO THE FORWARD PART OF THE TANK. WHEN REMOVING THE TANK FOR REPAIR, A .8750 INCH WRENCH WAS FOUND UNDER TH E TANK. THIS TANK WAS ORIGINAL EQUIPMENT INSTALLED AT THE FACTORY. SENT TANK TO AUTHORIZED REPAIR STATION FOR REPAIR. 1 G 7 2 3U H7EU 1996102400376 19961024 00376 WP 1996 10 24 GTIA96NK205 1 19960923 A 3397 WIRE DOUG DC9 DC941 302207N WP CABIN BROKEN A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 130NK 47604 LOG PAGE 028953. EMERGENCY FLOOR TRACK LIGHTING BY F/A FORWARD JUMP SEAT PARTIALLY NOT ILLUMINATED. REPAIRED BROKEN WI RE TO FLOOR TRACK LIGHTING. OPS CHECK GOOD. (X) 2 L 7 2 4F A6WE 1996102400377 19961024 00377 NE 1996 10 24 GTIA96NK175 2 19960709 A 7320 FUEL CONTROL DOUG DC9 DC941 302207N WP PWA JT8 JT8D9A 52048 NE NR 1 ENGINE OUT OF TRIM A GTIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 23 130NK 47604 665657 LOG PAGE 07467. ABORTED TAKEOFF. NR 1 ENGINE WOULD NOT PRODUCE TAKEOFF POWER MAX EPR 1.93 MAX N1 94.1 PERCENT, N2 100. 1 PERCENT. CHECKED PT2 LINES FOR LEAKS, BLEW OUT (CLEANED). PERFORMED ENGINE TRIM RUN PER MM 71-00. ALL INDCATIONS CH ECK NORMAL. LOCAL TEMPERATURE DROPPED 12 DEGREES. (X) 2 L 7 2 4F 4 F A6WE E2EA 1996102400378 19961024 00378 WP 1996 10 24 GTIA96NK182 1 19960726 A 3350 BATTERY PACK DOUG DC9 DC941 302207N WP CABIN DIRTY A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 130NK 47604 LOG PAGE 05466. COCKPIT EMERGENCY LIGHTS WILL NOT TEST WITH EMERGENCY LIGHT SWITCH. CLENAED CONNECTORS ON BATTERY PACK . SYSTEM OPS CHS GOOD. (X) 2 L 7 2 4F A6WE 1996102400379 19961024 00379 WP 1996 10 24 GTIA96NK112 1 19960626 A 3350 BATTERY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 130NK 47604 MIDDLE SECTION OF EMERGENCY LIGHT TRACK DOES NOT ILLUMINATE. REMOVED AND REPLACED NICAD BATTERIES IAW DC-9-MM 33-50. ( X) 2 L 7 2 4F A6WE 1996102400380 19961024 00380 WP 1996 10 24 GTIA96NK188 1 19960804 A 2611 FTA716 SMOKE DETECTOR DOUG DC9 DC941 302207N WP RT AFT LAV INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 130NK 47604 LOG PAGE 27064. RIGHT LAVATORY SMOKE DETECTOR WILL NOT TEST. REMOVED AND REPLACED RIGHT LAVATORY SMOKE DETECTOR IAW DC -9 MM CHAPTER 26. OPS CHECK GOOD. (X) 2 L 7 2 4F A6WE 1996102400381 19961024 00381 WP 1996 10 24 GTIA96NK187 1 19960802 A 3350 60030431 BATTERY SUPPLY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 131NK 47605 LOG PAGE 05501. AFT OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED AFT OVERWING EMERGENCY LIGHT BATTERY S UPPLY. OPS CHK GOOD IAW DC-9 MM, CHAPTER 3350-0. (X) 2 L 7 2 4F A6WE 1996102400382 19961024 00382 WP 1996 10 24 GTIA96NK193 1 19960826 A 3260 PROX SWITCH DOUG DC9 DC941 302207N WP LANDING GEAR MALFUNCTIONED A GTIA O OTHER N FALSE WARNING AP APPROACH 1 GL 23 131NK 47605 LOG PAGE 028993. CREW NOTED THEN CORRECTED LANDING GEAR DOWN AND LOCK LIGHT DISCREPANCY BY RESETTING POPPED 'PROX SWITC H CONTROL', CB (Z-21). CREW FOLLOWED F-COM PROCEDURES (VISUAL CHECKS, ETC.) TO CONFIRM DOWN AND LOCKED POSITION OF ALL LANDING GEAR. INSPECTED LANDING GEAR PROXIMITY SWITCHES, TARGETS, ASSOCIATED WIRING IN GEAR WELLS AND CONNECTORS. FOUN D ALL TO BE IN SERVICEABLE CONDITION. (X) 2 L 7 2 4F A6WE 1996102400383 19961024 00383 WP 1996 10 24 GTIA96NK185 1 19960801 A 3350 60030431 BATTERY SUPPLY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 131NK 47605 LOG PAGE 05500. AFT OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY SUPPLY - AFT OVERWING EMERGENC Y LIGHT. OPS CHKS GOOD IAW DC-9 MM, CHAPTER 33. (X) 2 L 7 2 4F A6WE 1996102400384 19961024 00384 EU 1996 10 24 96ZZZX5317 1 19960914 A 2760 RETRACT SYSTEM AMD FALC20 FALCON 2720302 EU AIRBRAKES MALFUNCTIONED A DKAA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 23 212R 212 UNCOMMANDED EXTENSION OF AIRBRAKES DURING FLIGHT. BLED AIRBRAKE SYSTEM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F A7EU 1996102400385 19961024 00385 1996 10 24 RAIA960902 4 19960903 A 3425 7003360948 AHRS COMPUTER JETAIR JETSTM JETSTM4101 1500501 EU E/E COMPT INOPERATIVE A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 571HK 542 41090 STL - FLT 7514 - NR 1 AHRS FELL OFF-LINE IN FLIGHT. MAINTENANCE RE-RACKED THE NR 1 AHRS COMPUTER. (X) 2 L 7 2 4T RT A41NM 1996102400386 19961024 00386 NE 1996 10 24 SIMA962521 2 19960908 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RIGHT FAILED A A SIMA F E ACTIVATE FIRE EXT. ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 381AE 1423 340B381 GEE785619 FLIGHT CREW REPORTED ENGINE PRODUCED EXCESSIVE SMOKE FROM TAIL PIPE DURING START-UP, SHUTDOWN OF ENGINE. RESTARTED PER MOC REQUEST AND OIL PRESSURE FLUCTUATED, SHUT DOWN AFTER 20 SECONDS AND NOTICED OIL DRIPPING OUT OF TAIL PIPE. MTX VISU ALLY CHECKED ENGINE PRIOR TO RESTARTING ENGINE TO PERFORM GROUND OPERATIONAL CHECK. ALL PARAMETERS APPEARED NORMAL UNTI L APPROXIMATELY 90/90 PERCENT NG. ENGINE BANGED, CHIP DETECTOR LIGHT CAME ON, SHUT DOWN ENGINE AND DISCHARGED ENGINE FI RE BOTTLE AS A PRECAUTION. REPLACED FIRE BOTTLE AND RT ENGINE ASSY PER APPLICABLE MANUALS. PERFORMED GROUND RUNS. AIR CRAFT RETURNED TO SERVICE. NOTE: FAILED ENGINE WILL BE SENT TO GE FOR TEAR-DOWN EVALUATION. PART TOTAL CYCLES. (X) 2 L 7 2 4T 4 T RT A52EU E8NE 1996102400388 19961024 00388 NE 1996 10 24 CA960222004 1 19960210 A 6321 2446271 BRAKE LINING SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL LH ROTOR BRAKE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 297 CAE890255S (CAN)DURING A POST FLIGHT INSPECTION, IT WAS NOTICED THAT THE L/H ROTOR BRAKE ASSEMBLY, FORWARD PAD, LOWER END LINING WA S BROKEN AWAY. THE AMOUNT OF LINING MISSING WAS APPROXIMATELY 25-30 PERCENT. 1 G 7 2 3U 3 U H1NE E1GL 1996102400389 19961024 00389 NM 1996 10 24 CA960222010 1 19960209 A 3230 763041 NOSE GEAR OZONE 45050001 PIPER PA60 PA60600 7106001 NM HYDRAULICS MALFUNCTION W A O UNSCHED LANDING OTHER O OTHER CL CLIMB 1 CA 3161 (CAN)AIRCRAFT DEPARTED FOR A LOCAL TEST FLIGHT. IT WAS FOUND THAT THE NOSE LANDING GEAR WOULD NOT FULLY RETRACT. THE GEA R WAS CYCLED AND EVENTUALLY MADE ITS WAY DOWN AND LOCKED. THE AIRCRAFT LANDED SAFELY.MAINTENANCE INSPECTED AND FOUND THA T DUE TO A LONG PERIOD OF INACTIVITY THEY BELIEVE THAT THERE WAS AIR IN THE HYDRAULIC SYSTEM. 1 M 7 2 3O RT A17WE 1996102400390 19961024 00390 1996 10 24 CA960222011 4 19960209 A 3424 100000901 TURN AND SLIP KING H14B6274 BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA YAW RATE INTERMIT SHORT W H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED CR CRUISE 1 CA 677 PCE50205 (CAN)AUTOPILOT DOES NOT MAINTAIN BANK ANGLES IN RIGHT TURN ONLY, ROLLS 45 DEGREES, PITCHES DOWN. SYSTEM TROUBLESHOT AND EVENTUALLY T AND S INDICATORS REPLACED AND AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 3T 4 T A14CE E4EA 1996102400391 19961024 00391 CE 1996 10 24 CA960222012 1 19960205 A 5751 501300021 AILERON BEECH 501300021 BEECH 90 65A90 1152908 CE LT AIL SPAR CRACKED W A K NONE O OTHER IN INSP/MAINT 1 CA J128 (CAN)DURING A 600 HOUR INSPECITON THE LEFT HAND AILERON WAS FOUND TO HAVE A 2 INCH CRACK IN THE MAIN SPAR AT THE INBOARD HINGE MOUNT AREA. A SECOND AILERON WAS PURCHASED ONLY TO FIND THAT A 1.5 INCH CRACK EXISTED IN IT. THE RIGHT HAND AILE RON WAS FOUND TO HAVE A CRACK JUST 164 HOURS PRIOR TO THIS OCCURRENCE. SUBMITTER RECOMMENDS INSPECTING THESE AREAS AS PE R MAINTENANCE MANUAL. 1 L 7 2 3T 3A20 1996102400392 19961024 00392 1996 10 24 CA960222013 4 19960208 A 3421 5040032906 GYRO AIM 5052C BEECH 200 200BEECH 1152920 CE COCKPIT ATTITUDE UNRELIABLE W O OTHER I FLT. ATTITUDE INST. CR CRUISE 1 CA 501 (CAN)PILOTS REPORT HAVING TO AUTO ERECT CAPTS GYRO EVERY TEN MINUTES. SUBMITTER STATES THAT THIS SDR IS IN RESPONSE TO S EVERAL FAILURES OF THIS GYRO USED IN THEIR FLEET. MODELS 510-8A, 510-8F, 505-2C, 251- ECFR AND 251-ECFRB. 1 L 7 2 4T A24CE 1996102400393 19961024 00393 CE 1996 10 24 CA960222014 1 19960212 A 2720 3540036610 SUPPORT ASSY LH BEECH BEECH 95 95B55 1152729 CE LEFT PEDAL ROD CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 10271 (CAN)THE SUPPORT ASSEMBLY WAS FOUND CRACKED THROUGH 80 PERCENT OF THE STRUCTURE. THE SUPPORT ASSEMBLY WAS FOUND TO BE DI STORTED TO THE POINT WHERE THE RUDDER CONTROL WOULD BE INTERFERED WITH AND GROUND NOS E WHEEL STEERING WOULD BE DIFFICUL T. THE SUBMITTER SUSPECTS THAT THE DAMAGE WAS CAUSED BY TOWING THE AIRCRAFT WITH THE FLIGHT CONTROLS LOCKED OR PERHAPS A SUDDEN STRONG WIND GUST FROM THE REAR OF THE AIRCRAFT WITHOUT THE GUST LOCKS IN PLACE. 1 L 7 2 3O RT 3A16 1996102400394 19961024 00394 SW 1996 10 24 CA960222015 1 19960214 A 3232 2755001299 TANGS SWRNGN SWRNGN SA226 SA226TC 8780404 SW MLG DOOR ACTUATR MISFIT W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA (CAN)WHILE ATTEMPTING TO INSTALL KIT ON LH LANDING GEAR DOOR ACTUATOR, PARTS DID NOT FIT AS PER THE SB. THIS MISFIT REST RICTED THE WIDTH OF THE OPENING TO APPROXIMATELY HALF OF REQUIRED 0.78 INCH; THUS NOT ALLOWING GEAR DOOR ROLLER BEARING ENTRANCE AND COULD LEAD TO FAILURE OF GEAR TO RETRACT. COMPANY CONTACTED (FAIRCHILD). 2 L 7 2 4T RT A8SW 1996102400395 19961024 00395 EU 1996 10 24 CA960222016 1 19960213 A 2720 T67B45219 CABLE SLNSBY T67F22007 SLNSBY T67 T67M260 8323006 EU RUD AFT PULLEY FRAYED W K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 CA 417 (CAN)THE NEW CABLES WERE INSPECTED UNDER THE INSPECATION SCHEDULE OF 500 HOURS OR 12 MONTHS WHICHEVER COMES FIRST AS DIR ECTED IN SERVICE BULLETIN 78. THE TWO AIRCRAFT INSPECTED HAD ONE FRAYED CABLE EACH. R EFERENCE ADDITIONAL SDR 96022039. CANADA REVIEWING POSSIBLE AIRWORTHINESS DIRECTIVE ACTION ON THIS PARTICULAR INCIDENT. 1 L 7 1 3O NT A73EU 1996102400401 19961024 00401 NM 1996 10 24 CA960222022 1 19960214 A 3230 DSC252B40124 HOSE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NLG DOWN LEAKING W K NONE K FLUID LOSS TX TAXI/GRND HDL 1 CA LH120817 (CAN)HYDRAULIC LEAK FOUND DURING WALK AROUND. FLUID LEAKING FROM NOSE GEAR WHEEL WELL. HOSE IS FOR GEAR DOWN PRESSURE FO R LANDING GEAR. 2 H 7 2 4T 4 T RT A13NM E20NE 1996102400402 19961024 00402 NM 1996 10 24 CA960222023 1 19960209 A 5210 85210096103 FITTING DHAV 85210240005 DHAV DHC8 DHC8102 2809003 NM MAIN DOOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 15950 (CAN)UPPER FITTING ON FORWARD UPPER STRUT FOR MAIN ENTRANCE DOOR CRACKED AND BROKEN OFF JUST ABOVE UPPER SWAGE SLEEVE. N O CORROSION FOUND. 2 H 7 2 4T RT A13NM 1996102400415 19961024 00415 EU 1996 10 24 CA960222039 1 19960213 A 2720 T67B45219 CONTROL CABLE SLNSBY T67F33007 SLNSBY T67 T67M260 8323006 EU RUD AFT PULLEY FRAYED W K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 CA 354 (CAN)THE NEW CABLES WERE INSPECTED UNDER THE INSPECTION SCHEDULE OF 500 HOURS OR 12 MONTHS WHICHEVER COMES FIRST AS DIRE CTED IN SERVICE BULLETIN 78. THE TWO AIRCRAFT INSPECTED HAD ONE FRAYED CABLE EACH. RE FERENCE ADDITIOINAL SDR 960222016. CANADA REVIEWING POSSIBLE AIRWORTHINESS DIRECTIVE ACTION ON THIS PARTICULAR INCIDENT. 1 L 7 1 3O NT A73EU 1996102400416 19961024 00416 CE 1996 10 24 CA960223001 1 19960210 A 5753 351153963 CLIP BEECH 100 100BEECH 1152916 CE INB FLAP TRACK CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 18120 (CAN)IT WAS NOTICED THAT THE INBOARD FLAP TRACK WAS NOT SYMMETRICAL WITH THE OTHER FLAP. INSPECTION REVEALED DAMAGED CL IPS WHICH ANCHOR THE FLAP TRACK TO THE WING. AFTER REPLACING THE CLIPS THE OTHER WINGWAS INSPECTED AND A SIMILAR, BUT SM ALLER CRACK WAS FOUND. SUBMITTER NOTES THAT BOTH SETS OF CLIPS WERE REPLACED. 1 L 7 2 3T A14CE 1996102400417 19961024 00417 WP 1996 10 24 CA960223002 1 19960219 A 5511 5361887 SPAR DOUG DC6 DC6B 3021712 WP HORIZ STAB CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 27052 (CAN)DURING ANNUAL INSPECTION OF HORIZONTAL STABILIZER AND COMPLIANCE WITH AD 83-20-04, A CRACK WAS DETECTED ON THE CENT RE SECTION SPAR LOWER STARBOARD SIDE. CRACK LOCATION IS IN THE BORE HOLE FOR THE ATTA CH BOLT AT THE BOTTOM OF THE BORE. THE CRACK LENGTH IS APPROXIMATELY ONE INCH. REPAIR OF DEFECT AS PER SRM TO BE CARRIED OUT PRIOR TO AIRCRAFT BEING RETUR NED TO SERVICE. 2 L 7 4 4R 6A4 1996102400420 19961024 00420 CE 1996 10 24 CA960223005 1 19960215 A 5510 12326231 REINFORCEMENT CESSNA 206 U206F 2073333 CE LT HORIZ STAB CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN)LEFT HAND HORIZONTAL STABILIZER REINFORCEMENT PART #12326231 FOUND CRACKED. 1 H 7 1 3O A4CE 1996102400421 19961024 00421 CE 1996 10 24 CA960223006 1 19960205 A 2434 C6FF10335D DRIVE ASSEMBLY FORD DOFF10300E CESSNA 337 337G 2075730 CE CONT O360 IO360G 17025 SO DRIVE END POLES ADRIFT W K NONE O OTHER IN INSP/MAINT 1 CA 99 PA5347 352164 734041 (CAN)CUSTOMER BROUGHT IN THE ALTERNATOR FOR TEST AND REPAIR. DISASSEMBLY FOUND THE ROTOR ASSEMBLY LOOSE FROM THE SHAFT A ND ABLE TO ROTATE ON THE SHAFT ABOUT 10 DEGREES. 1 H 7 2 3O 3 O A6CE E1CE 1996102400422 19961024 00422 CE 1996 10 24 CA960223008 1 19960210 A 3246 16298 WHEEL HALF PARKERHANFIN 40172 BEECH 200 200BEECH 1152920 CE WEB JUNCTION CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1111 (CAN)INSPECTION OF THE WHEEL HALVES FOUND CRACKS IN THE WEB JUNCTION AREAS. LIQUID PENETRANT INSPECTION PERFORMED AS REQ UIRED BY CLEVELAND MAINTENANCE MANUAL. THIS INSPECTION IS REQUIRED AT EACH TIRE CHANG E. TO DATE WE HAVE SCRAPPED SEVEN WHEEL ASSEMBLIES DO TO SIMILAR FAULTS. WHEEL ASSEMBLY 40-172 IS NOW SUPERSEDED BY WHEEL ASSEMBLY 40-289. SUBMITTER STATE S NO PROBLEMS WITH THE LATER WHEEL ASSEMBLY. 1 L 7 2 4T A24CE 1996102400423 19961024 00423 CE 1996 10 24 CA960223010 1 19960223 A 5521 115610010175 RIB BEECH 115600010277 BEECH 100 100BEECH 1152916 CE ELEV LE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 11819 B75 (CAN)WHILE PERFORMING SB 2145 ELEVATOR TORQUE TUBE INSPECTION, THE AME REMOVED THE TORQUE TUBE AND LOOKED INSIDE THE ELE VATOR AND FOUND A 1.5 INCH LONG CRACK BETWEEN THE FLANGE AND THE WEB OF THE INBOARD L EADING EDGE RIB WHICH ALSO SUPPORT S THE ELEVATOR COUNTERWEIGHT. THE RIB WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 3T A14CE 1996102400424 19961024 00424 NM 1996 10 24 CA960223011 1 19960217 A 2910 DSC252D40130180 LINE DHAV DHC8 DHC8102 2809003 NM #1 MAIN MANIFOLD CRACKED W O OTHER K FLUID LOSS AP APPROACH 1 CA 16505 (CAN)HYDRAULIC LINE FROM #1 MAIN PRESSURE MANIFOLD TO ANTI SKID VALVE CRACKED AT FLARE RESULTING IN LOSS OF #1 HYDRAULIC FLUID AND SUBSEQUENT LOSS OF ALL #1 HYDRAULIC SERVICES. AIRCRAFT LANDED OK. 2 H 7 2 4T RT A13NM 1996102400426 19961024 00426 NM 1996 10 24 CA960227004 1 19960222 A 7921 28E997 OIL COOLER STWARNER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 ENGINE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 31 06900503 120657 (CAN)HEAVY OIL LEAK #2 ENGINE, OIL COOLER LEAKING, REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1996102400427 19961024 00427 SO 1996 10 24 CA960227008 1 19960219 A 5280 46652 DOOR HINGE PIPER PA31 PA31350 7103110 SO MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 12580 (CAN)CRACK WAS FOUND IN THE INNER RADIUS OF THE MAIN LANDING GEAR DOOR HINGE. THIS PART IS COVERED BY SB 682 AND AD 80-2 6-05. SUBMITTER STATES THAT THIS IS THE FIRST TIME THIS HAS BEEN FOUND IN 7000 HOURS OF OPERATIONS. 1 L 7 2 3O A20SO 1996102400428 19961024 00428 GL 1996 10 24 CA960227012 1 19960207 A 3213 28171211 CLAMP ENSTRM F28 F28F 3300412 GL LYC FWD CROSSTUBE CRACKED W O OTHER O OTHER IN INSP/MAINT 1 CA 2402 (CAN)CRACKED CLAMP ON FORWARD CROSSTUBE. AIRCRAFT USED AS A TRAINER. 1 G 7 1 3O H1CE 1996102400429 19961024 00429 GL 1996 10 24 CA960227015 1 19960220 A 3240 A600 RESERVOIR DIAMON DA20A1 DA20A1 05626UX GL LT BRAKE PIN HOLE LEAK W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 835 (CAN)HYDRAULIC FLUID FOUND ON THE PILOTS FLOOR DURING 200 HOUR CHECK. FOUND LEFT HAND BRAKE RESERVOIR LOW. REMOVAL OF TH E RESERVOIR FOUND A PIN HOLE IN THE WELD OF THE LOWER FITTING USED FOR THE ATTACHMENTOF THE MASTER CYLINDER. 1 L 7 1 3O NT TA4CH 1996102400430 19961024 00430 NM 1996 10 24 CA960227016 1 19960222 A 5270 82420018001 SENSOR DHAV DHC8 DHC8102 2809003 NM BAGGAGE DOOR FROZEN W C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CA (CAN)DURING TAKEOFF ROLL, BAGGAGE DOOR WARNING LIGHT CAME ON. TAKEOFF ABORTED. AFT SENSOR FOUND FROZEN. 2 H 7 2 4T RT A13NM 1996102400431 19961024 00431 1996 10 24 CA960227017 4 19960212 A 3414 85C0109 INDICATOR DHAV DHC8 DHC8102 2809003 NM #2 AIR SPEED FROZEN W C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CA 18020 239664 (CAN)#2 AIRSPEED INDICATOR FROZEN. TAKEOFF ABORTED. AIRSPEED INDICATOR REPLACED AND SYSTEM PURGED. 2 H 7 2 4T RT A13NM 1996102400432 19961024 00432 SO 1996 10 24 CA960227019 1 19960123 A 2140 CD2045 COMBUSTION TUBE JANITROL B4050 PIPER PA31 PA31350 7103110 SO HEATER PUNCTURED PLATE W A H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA 733 1761688 (CAN)PILOT REPORTED NOISE AND THEN FUMES AND FUEL SMELL IN COCKPIT. INVESTIGATION FOUND THE JANITROL HEATER HAD A SMALL PUNCTURE IN THE LOWER END PLATE. THE EDGES WERE FOUND BURNT. SUBMITTER RECOMMENDS A GOOD VISUAL INSPECTION ANNUALLY. 1 L 7 2 3O A20SO 1996102400433 19961024 00433 NM 1996 10 24 CA960227021 1 19960220 A 5310 TAIL SECTION BOEING 757 757236 NM FUSELAGE DAMAGED W K NONE O OTHER LD LANDING 1 CA (CAN)TAIL SECTION STRUCK RUNWAY DUE TO OVER ROTATION ON LANDING. REPAIRED IN ACCORDANCE WITH SRM. 2 L 7 2 4F RT A2NM 1996102400434 19961024 00434 NM 1996 10 24 CA960227022 1 19960219 A 7500 69179641 BALL JOINT BOEING 727 727212 138407G NM PWA JT8 JT8D17 52049 NE 13TH STG DUCT DISCONNECTED W C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CA 688149 (CAN)#3 ENGINE FIRE WARNING DURING TAKEOFF ROLL. REJECTED. 13TH STAGE CROSS-OVER DUCT BALL JOINT ON TOP OF ENGINE DISCON NECTED, SAFETY WIRE MISSING. CONNECTED AND SAFETY WIRED. 2 L 7 3 4F 4 F A3WE E2EA 1996102400435 19961024 00435 SW 1996 10 24 CA960227023 1 19960219 A 5330 SKIN SWRNGN SWRNGN SA226 SA226TC 8780404 SW FS332.271-347.2 CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA 17141 (CAN)CHAFING CAUSED BY LOOSE PANEL ON UNDERSIDE OF FUSELAGE. RIBS ON PANEL RUBBING AGAINST FUSELAGE SKIN. 2 L 7 2 4T RT A8SW 1996102400436 19961024 00436 NM 1996 10 24 CA960229001 1 19960228 A 7921 28E997 OIL COOLER STWARNER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE #2 ENGINE LEAKING W K NONE O OTHER IN INSP/MAINT 1 CA 31 01901003 120657 (CAN)HEAVY OIL LEAK #2 ENGINE. OIL COOLER LEAKING. 2 H 7 2 4T 4 T RT A13NM E20NE 1996102400437 19961024 00437 WP 1996 10 24 CALA9601489 1 19961019 A 2170 20D103 WAT SEP BAGS DOUG DC10 DC1030 3023501 WP AC PACK DIRTY A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 09 14062 47863 THE FLIGHT ATTENDANTS REPORTED AN ODOR OF ELECTRICAL SMOKE WHILE ON APPROACH. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDE NT. MAINTENANCE INSPECTED THE AIRCRAFT FOR AN ELECTRICAL FAILURE AND FOUND NO FAULTS. ALL THREE WATER SEPARATOR BAGS W ERE FOUND EXTREMELY SOILED. THE WATER SEPARATOR BAGS WERE REMOVED AND REPLACED. THE PACKS WERE RUN WITH AND WITHOUT EN GINES OPERATING AT HIGH AND LOW POWER AND NO ODOR WAS PRODUCED. IN ADDITION, LIGHTS AND AUDIO/VIDEO EQUIPMENT WERE ALL CHECKED WITH NO TROUBLE FOUND. 2 L 7 3 4F A22WE 1996102400438 19961024 00438 WP 1996 10 24 CALA9601490 1 19961019 A 3260 12888005 BULBS DOUG DC9 DC932 3022066 WP LANDING GEAR FAILED A CALA O OTHER P NO WARNING INDICATION AP APPROACH 1 SW 09 19504 47638 THE RT MLG DID NOT INDICATE DOWN AND LOCKED WITH GEAR HANDLE DOWN NOR WITH ALTERNATE EXTENSION WHILE ON APPROACH. THE G EAR WAS CONFIRMED DOWN AND LOCKED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BOTH LANDING GEAR ANNUNCI ATOR LAMPS BURNED OUT. THE LANDING GEAR ANNUNCIATOR LAMPS WERE REPLACED AND ALL INDICATIONS WERE NORMAL. 2 L 7 2 4F A6WE 1996102400439 19961024 00439 WP 1996 10 24 CALA9601491 1 19961020 A 2161 60714622 CONTROLLER DOUG DC9 DC932 3022066 WP LT PACK INOPERATIVE A CALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 19504 19174 13304 47638 SHORTLY AFTER TAKEOFF, THE LT PACK VALVE WENT TO FULL HOT IN AUTO, THE CONTROL WAS SWITCHED TO MANUAL AND MODULATED TO C OLD. THE PACK VALVE DID NOT RESPOND AND THE CABIN AND COCKPIT BEGAN TO FILL WITH SMOKE. THE PACK AUTO SHUTDOWN, BUT TH E SMOKE CONTINUED. THE AIRCRAFT WAS RETURNED TO MDW WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT PACK TE MP CONTROLLER AT FAULT. THE TEMP CONTROLLER WAS REMOVED AND REPLACED, OPERATIONAL CHECKS WERE GOOD WITH NO SMOKE NOTED. 2 L 7 2 4F A6WE 1996102400440 19961024 00440 WP 1996 10 24 9622199872 1 19960319 A 5330 SKIN DOUG DC9 DC951 3022051 WP BS 200 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 781NC 48121 DURING LINE CHECK, FOUND A .25 INCH CRACK IN THE FORWARD ENTRY DOOR JAMB UPPER AFT SKIN FS 200 AT LONGERON 9L. REPAIRED SKIN (P/N 5911406-5) PER EA 98-104202. 2 L 7 2 4F A6WE 1996102400441 19961024 00441 NM 1996 10 24 9622205526 1 19961009 A 5320 SILL BOEING 757 757251 1384970 NM CARGO DOOR CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 526US 23620 DURING P-CHECK, FOUND CORROSION ON THE AFT CARGO DOOR LOWER SILL INNER CHORD. REPAIRED CHORD (P/N 146N8522-51) PER EA 5 5-110371. 2 L 7 2 4F RT A2NM 1996102400442 19961024 00442 WP 1996 10 24 9622219852 1 19961011 A 5320 ANGLE DOUG DC9 DC951 3022051 WP BS 1267 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 761NC 47709 DURING H-CHECK, FOUND A 1.5 INCH CRACK IN THE LEFT FUSELAGE TO VERTICAL STABILIZER ATTACH ANGLE AT FS 1267. REPAIRED AN GLE (P/N 5912141-59) PER EA 99-111716. 2 L 7 2 4F A6WE 1996102400443 19961024 00443 WP 1996 10 24 9622229852 1 19961011 A 5315 FLOORBEAM DOUG DC9 DC951 3022051 WP BS 1136 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 761NC 47709 DURING H-CHECK, FOUND CORROSION IN THE FS 1136 FLOORBEAM CAP AT THE AIRCRAFT CENTER LINE. REPAIRED FLOORBEAM CAP (P/N 9 912243-55) PER EA 98-111715. 2 L 7 2 4F A6WE 1996102400444 19961024 00444 NM 1996 10 24 9622235526 1 19961011 A 5315 FLOORBEAM BOEING 757 757251 1384970 NM BS 1661 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 526US 23620 DURING P-CHECK, FOUND CORROSION ON THE BS 1661 FLOORBEAM UPPER CHORD ALONG THE ENTIRE LENGTH. REPAIRED CHORD PER EA 55- 110373. 2 L 7 2 4F RT A2NM 1996102400445 19961024 00445 WP 1996 10 24 9622249963 1 19961017 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 200 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 913RW 47171 DURING M-CHECK, FOUND CORROSION ON THE FS 200 FRAME TO FLOOR FITTING AT LONGERON 18R. REPLACED FITTING (P/N 4912823-2) PER SRM 51-30-1, 51-30-5. 2 L 7 2 4F A6WE 1996102400446 19961024 00446 WP 1996 10 24 9622259951 1 19961017 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 690 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9347 45827 DURING H-CHECK, FOUND CORROSION ON THE LEFT WHEEL WELL ATTACH FITTING FS 690 AT THE KEEL SKIN. REPLACED FITTING PER SRM 53-01 FIG 1. 2 L 7 2 4F A6WE 1996102400447 19961024 00447 NE 1996 10 24 9622266612 2 19961017 A 7200 ENGINE BOEING 747 747251B 1384892 NM PWA JT9 JT9D7F 52054 NE NR 3 FLAMED OUT A NWAA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 GL 01 612US 20357 89471 DURING CRUISE, THE NR 3 ENGINE EXPERIENCED FLAME-OUT. FLAME-OUT OCCURRED WHILE FUEL MANAGEMENT PROCEDURES WERE BEING AC COMPLISHED. NO OVERTEMP OCCURRED AND RELIGHT WAS SUCCESSFUL ON SECOND ATTEMPT AT FL250. ENGINE OPERATION WAS NORMAL FO R THE REMAINDER OF THE FLIGHT. MAINTENANCE ACCOMPLISHED VISUAL INSPECTION, OPERATIONAL CHECK OF CONDITION MOTOR AND FUE L TANK SUMPS. ALL CHECKS WERE NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4 F A20WE E20EA 1996102400448 19961024 00448 WP 1996 10 24 9622279868 1 19961015 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 777NC 47787 DURING LINE CHECK, FOUND REAR EXIT CABIN WINDOW SEAL LIGHTS INOPERATIVE ON EVACUATION LIGHT CHECK. REPLACED BATTERIES A T B5-25, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996102400449 19961024 00449 WP 1996 10 24 9622289867 1 19961017 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 776NC 47786 DURING LINE CHECK, FOUND EMERGENCY EXIT LIGHTS IN VENTRAL STAIR INOPERATIVE. REPLACED BATTERIES IN B5-28, OPERAITONAL C HECK OK. 2 L 7 2 4F A6WE 1996102400450 19961024 00450 NE 1996 10 24 9622292298 2 19961020 A 7230 COMPRESSOR BOEING 727 727251 138408H NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE STALLED A NWAA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 01 298US 22152 700564 UPON APPLYING TAKEOFF POWER, NR 2 ENGINE STALLED. CREW ABORTED TAKEOFF. CROSSWINDS WERE PRESENT WHILE TAKEOFF WAS ATTE MPTED. ENGINE WAS INSPECTED AND STALL COULD NOT BE DUPLICATED. 2 L 7 3 4F 4 F A3WE E2EA 1996102400451 19961024 00451 EU 1996 10 24 9622303235 1 19961019 A 2121 EVT3454G FAN AIRBUS 320 A320212 EU AVIONICS BAY SEIZED A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 01 335NW 13611 5744 340 DURING APPROACH AT 7,000 FEET, CREW NOTED A BURNING SMELL IN COCKPIT FOLLOWED FIVE MINUTES LATER BY A VENT EXTRACT FAULT . FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND T HE AVIONICS COOLING EXTRACT FAN SEIZED. REPLACED SAME, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996102400452 19961024 00452 SO 1996 10 24 COMA9610308 1 19961018 A 3697 WIRE EMB 120 EMB120RT 3260202 SO LT BLEED AIR CHAFED A COMA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 200CD 120200 LT BLEED AIR DUCT LEAK WARNING CAME ON DURING CLIMB. REPAIRED CHAFED WIRING AT DUCT LEAK SENSOR. 2 L 7 2 4T RT A31SO 1996102400453 19961024 00453 SO 1996 10 24 COMA9610309 1 19961017 A 2750 3075001017 FLAP CONTL UNIT EMB 120 EMB120RT SO E/E BAY MALFUNCTION A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 152CA 7652 42 120152 FLAP CONTROL FAULT WARNING, INBD FLAPS ARE FAILED. REPLACED THE FLAP CONTROL UNIT. 2 L 7 2 4T RT A31SO 1996102400454 19961024 00454 EA 1996 10 24 COMA9660172 1 19961017 A 3241 428853 CONTROL BOX CNDAIR CL600 CL6002B19 EA E/E BAY MALFUNCTION A COMA K NONE O OTHER LD LANDING 1 SO 01 924CA 7026 GROUND LIFT DUMP UNSAFE MESSAGE ON EICAS. REPLACED THE ANTI-SKID CONTROL BOX. 2 L 7 2 4F RT A21EA 1996102400455 19961024 00455 EA 1996 10 24 COMA9660173 1 19961017 A 2760 270003 PCU CNDAIR CL600 CL6002B19 EA LT SPOILERON MALFUNCTION A COMA K NONE J WARNING INDICATION UK UNKNOWN 1 SO 01 937CA 5584 7044 SPOILERONS FAULT MESSAGE ON EICAS. REPLACED THE LT SPOILERON POWER CONTROL UNIT. 2 L 7 2 4F RT A21EA 1996102400456 19961024 00456 NM 1996 10 24 UPS96221381 1 19961016 A 5330 SKIN BOEING 727 72727C 138400J NM BS 1323/1343 CORRODED A IPXA O OTHER O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE-C/R, FUSELAGE SKIN CORRODED AT STA 1323 AND 1343 AT STRS 5L TO 8L. CUT OUT DAMAGED SKIN SRM 53-30-03 FI G 12 TREATED AND PRIMED AREA. FABRICATED SKIN FILLER AND REPAIR PARTS AND INSTALLED REPAIR IAW SRM 53-30-3 FIG 12. 2 L 7 3 4F A3WE 1996102400457 19961024 00457 NM 1996 10 24 UPS96221382 1 19961016 A 5542 SKIN BOEING 727 72727C 138400J NM RUDDER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 911UP 19119 INSPECTION TYPE-C/R, LWR RUDDER RT SIDE STA 110.0 HAS SMALL AREA OF CORROSION. CUT OUT DAMAGE AND REPAIRED AREA IAW SRM 55-20-03. 2 L 7 3 4F A3WE 1996102400458 19961024 00458 NM 1996 10 24 UPS96221386 1 19960921 A 5313 STRINGER BOEING 727 72725C 138400H NM BS 1243-1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE-C, STRINGR 12R CORRODED BS 1243 TO 1342. REMOVED, FABRICATED AND REPLACED STRINGER BS 1243 TO 1342 IAW SRM 53-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 1996102400459 19961024 00459 NM 1996 10 24 UPS96221387 1 19960921 A 5313 STRINGER BOEING 727 72725C 138400H NM BS 1243-1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE-C, STR 13L CORRODED BS 1243 TO 1342. REMOVED CORRODED STR FABRICATED AND INSTALLED STR 13L PER SRM 53-1 0-2, BS 1243 TO 1342. 2 L 7 3 4F A3WE 1996102400460 19961024 00460 NM 1996 10 24 UPS96221388 1 19960921 A 5313 STRINGER BOEING 727 72725C 138400H NM BS 1243-1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE-C, STRINGER 12L CORRODED BS 1342 TO 1243. REMOVED, FABRICATED AND REPLACED STR 12 BS 1243 TO 1342 PER S RM 53-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 1996102400461 19961024 00461 NM 1996 10 24 UPS96221389 1 19960921 A 5313 STRINGER BOEING 727 72725C 138400H NM BS 1243-1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE-C, STRINGER 13R CORRODED BS 1243 TO 1342. REMOVED, FABRICATED AND INSTALLED STR 13R BS 1243 TO 1342 PER SRM 53-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 1996102400462 19961024 00462 NM 1996 10 24 UPS96221390 1 19960918 A 5330 SKIN BOEING 727 72725C 138400H NM BS 1243-1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE-C, FUSELAGE SKIN IS CORRODED STA 1243 TO 1342 STR 10L TO 14L. REMOVED, FABRICATED AND REPLACED SKIN PER SRM 53-30-2 AND 51-30-2. 2 L 7 3 4F A3WE 1996102400463 19961024 00463 NM 1996 10 24 UPS96221391 1 19960918 A 5311 FRAME BOEING 727 72725C 138400H NM BS 1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE-C, BS 1342 LT FRAME CHORD, LBL 20 IS SEVERELY RUSTED. REMOVED AND REPLACED LT FRAME CHORD IAW SRM 51-30 -2 AND EO B727-5530-4601. 2 L 7 3 4F A3WE 1996102400464 19961024 00464 NM 1996 10 24 UPS96221392 1 19960918 A 5311 FRAME BOEING 727 72725C 138400H NM BS 1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE-C, BS 1342 RT FRAME CHORD RBL 20 IS SEVERELY RUSTED. REMOVED AND REPLACED CHORD IAW SRM 51-30-2 AND EO B727-5530-4601. 2 L 7 3 4F A3WE 1996102400465 19961024 00465 NM 1996 10 24 UPS96221393 1 19960920 A 5530 CHORD BOEING 727 72725C 138400H NM BS 1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE-C, VERT FIN TORQUE BOX LT HORIZ CHORD FS 1342 FIN STA 0 IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED AREA AND REPLACED CHORD AT STA 1342 FIN STA 0 PER DHC SK 950-435. 2 L 7 3 4F A3WE 1996102400466 19961024 00466 NM 1996 10 24 UPS96521383 1 19961018 A 2121 COOLING FAN BOEING 757 75724APF 1384969 NM NR 1 FLIGHT DECK DEFECTIVE A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 424UP 25369 INSPECTION TYPE-N/A, STRONG ELECTRICAL BURNING SMELL FROM UNDER FORWARD PANEL BOTH SIDES AFTER 1HR 30M FLT TIME. UNABLE TO DETERMINE CAUSE. FOUND NR 1 FD EQUIP COOLING SUPPLY FAN BAD. DEFERRED PER MEL 21-58-04. 2 L 7 2 4F RT A2NM 1996102400467 19961024 00467 WP 1996 10 24 UPS96821349 1 19960905 A 5313 4613574 LONGERON DOUG DC8 DC873F 302199F WP BS 200-220 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, HEAVY CORROSION AT LONGERON 8R, FS 200 TO 220. REPLACED LONGERON SPLICE PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996102400468 19961024 00468 WP 1996 10 24 UPS96821350 1 19960904 A 5313 4619165 LONGERON DOUG DC8 DC873F 302199F WP BS 1500-1520 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, MODERATE CORROSION DAMAGE AT LONGERON 1, FS 1500 TO 1520. SPLICED LONGERON SECTION PER SRM 51-1-21 . 2 L 7 4 4F RT 4A25 1996102400469 19961024 00469 WP 1996 10 24 UPS96821351 1 19960911 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1338 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, HEAVY CORROSION ON WEB FRAME FS 1338, LONGERON 11L. REPAIRED WEB PER SRM 53-2-0. 2 L 7 4 4F RT 4A25 1996102400470 19961024 00470 WP 1996 10 24 UPS96821352 1 19960904 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1360 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, BELT FRAME AT FS 1360 FWD SIDE HAS HEAVY CORROSION AT LONGERON 5L. REPAIRED FRAME PER SRM 53-2-0. 2 L 7 4 4F RT 4A25 1996102400471 19961024 00471 WP 1996 10 24 UPS96821353 1 19960904 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1640 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, HEAVY CORROSION ON BELT FRAME FS 1640 LONGERON 2R TO 10R. REPLACED FRAME SECTION PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996102400472 19961024 00472 WP 1996 10 24 UPS96821354 1 19960904 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1520 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, HEAVY CORROSION ON BELT FRAME FS 1520 LONGERON 1L. REPAIRED FRAME PER SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1996102400473 19961024 00473 WP 1996 10 24 UPS96821355 1 19960905 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 120-140 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, HEAVY CORROSION ON FRAME BOX BETWEEN LONGERONS 8R TO 9R, FS 120 TO 140. SPLICED FRAME BOX PER SRM 51-1-20D AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1996102400474 19961024 00474 WP 1996 10 24 UPS96821356 1 19960904 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1380 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, HEAVY CORROSION ON BELT FRAME AFT SIDE FS 1380 LONGERON 7L. REPAIRED FRAME PER SRM 53-2-0 FIG 2 SH EET 4. 2 L 7 4 4F RT 4A25 1996102400475 19961024 00475 WP 1996 10 24 UPS96821357 1 19960905 A 5313 4619670 LONGERON DOUG DC8 DC873F 302199F WP BS 1260-1280 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, HEAVY CORROSION ON LONGERONS 7R AND 8R AT FS 1260 TO 1280. INSTALLED LONGERON SPLICES PER SRM 51-1 -21 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996102400476 19961024 00476 WP 1996 10 24 UPS96821358 1 19960915 A 5320 9611067 FITTING DOUG DC8 DC873F 302199F WP BS 70 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, HEAVY CORROSION AT FITTINGS FWD SIDE OF FS 70 LONGERONS 3L AND 1. REPLACED FITTINGS PER SRM 51-1-2 0D. 2 L 7 4 4F RT 4A25 1996102400477 19961024 00477 WP 1996 10 24 UPS96821359 1 19960915 A 5320 4611067 FITTING DOUG DC8 DC873F 302199F WP BS 70 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, HEAVY CORROSION ON LONGERONS FITTING FS 70 FWD SIDE LONGERON 6R. REPLACED FITTING PER SRM 51-1-20D . 2 L 7 4 4F RT 4A25 1996102400478 19961024 00478 WP 1996 10 24 UPS96821360 1 19960915 A 5320 4611067 FITTING DOUG DC8 DC873F 302199F WP BS 70 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, HEAVY CORROSION ON LONGERON 4R END FITTING FWD SIDE OF FS 70. REPLACED FITTING PER SRM 51-1-20D AN D SRM 51-3-0. 2 L 7 4 4F RT 4A25 1996102400479 19961024 00479 WP 1996 10 24 UPS96821361 1 19960915 A 5320 4611067N FITTING DOUG DC8 DC873F 302199F WP BS 70 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, HEAVY CORROSION ON LONGERON 8L END FITTING FWD SIDE OF FS 70. REPLACED FITTING PER SRM 51-1-20 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1996102400480 19961024 00480 WP 1996 10 24 UPS96821362 1 19960916 A 5320 5750868 FITTING DOUG DC8 DC873F 302199F WP BS 1781 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS, VERTICAL ATTACH FITTING FOR THE TAIL SKID CARTRIDGE HAS A 6 INCH LONG CRACK ON BOTTOM FACE. REPLACE D FITTING PER SRM 51-3-0 AND SRM 51-1-23. 2 L 7 4 4F RT 4A25 1996102400481 19961024 00481 WP 1996 10 24 UPS96821363 1 19960905 A 5330 564932975 SKIN DOUG DC8 DC873F 302199F WP BS 1690-1910 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, LOWER BELLY SKIN FS 1690 TO 1910 HEAVY CORROSION. REPLACED SKIN SECTION PER SRM 51-1-21 AND SRM 51 -1-20D. 2 L 7 4 4F RT 4A25 1996102400482 19961024 00482 WP 1996 10 24 UPS96821364 1 19960916 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP BS 1690-1710 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, HEAVY CORROSION AT LONGERON 28L DOUBLER FS 1690 TO 1710. REPLACED DOUBLER PER SRM 51-1-20D AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1996102400483 19961024 00483 WP 1996 10 24 UPS96821365 1 19960916 A 5313 564932946 LONGERON DOUG DC8 DC873F 302199F WP BS 1740-1766 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, FS 1740 TO 1766 HEAVY CORROSION AT LONGERON 34R. REPLACED LONGERON SECTION PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996102400484 19961024 00484 WP 1996 10 24 UPS96821366 1 19960916 A 5315 988942 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1730 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, FS 1730, FLOORBEAM HAS MODERATE CORROSION DAMAGE FROM BL 0 TO LBL 60. REPLACED FLOORBEAM SECTION P ER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996102400485 19961024 00485 WP 1996 10 24 UPS96821367 1 19960923 A 5311 577384631 FRAME DOUG DC8 DC873F 302199F WP BS 1730 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, HEAVY CORROSION AT BELT FRAME FS 1730 LONGERON 22L TO 22R. REPLACED FRAME SECTION PER SRM 51-1-20D . 2 L 7 4 4F RT 4A25 1996102400486 19961024 00486 WP 1996 10 24 UPS96821368 1 19960916 A 5320 564932949 DOUBLER DOUG DC8 DC873F 302199F WP BS 1766-1810 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, HEAVY CORROSION AT BELLY DOUBLER FS 1766 TO 1810. REPLACED DOUBLER PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996102400487 19961024 00487 WP 1996 10 24 UPS96821369 1 19961017 A 3260 801801 PROX SENSOR DOUG DC8 DC873F 302199F WP RT MLG FAILED A IPXA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 812UP 46112 INSPECTION, INTRANSIT LIGHT SHOWING. REPLACED FAILED RT MLG PROX SENSOR. 2 L 7 4 4F RT 4A25 1996102400488 19961024 00488 WP 1996 10 24 UPS96821370 1 19961017 A 2424 51508000 GCU DOUG DC8 DC873F 302199F WP AC GEN SYST MALFUNCTIONED A IPXA O OTHER O OTHER DE DESCENT 1 SO 01 806UP 46006 INSPECTION TYPE N/A, GEN UNPARALLEL LIGHT ILLUMINATED ON DECENT. AC LOAD AND FREQ WENT TO ZERO, STARTED GETTING AN ELEC T BURNING SMELL, SO WE DISCONNECTED GENERATOR. REMOVED AND REPLACED VR AND GCU, RAN ENG AND OPS CHK GOOD. THIS CLEARS M-117170, (P/N 51508-000) (S/N 665ABC) ON, (P/N 51508-0000) (S/N 217ACB) OFF. 2 L 7 4 4F RT 4A25 1996102400489 19961024 00489 WP 1996 10 24 UPS96821371 1 19960908 A 5320 4611067N FITTING DOUG DC8 DC873F 302199F WP BS 70 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, MODERATE CORROSION DAMAGE ON END FITTING FS 70 LONGERON 33R. REPLACED FITTING PER SRM 51-1-20D AND SRM 51-1-2. 2 L 7 4 4F RT 4A25 1996102400490 19961024 00490 WP 1996 10 24 UPS96821372 1 19960917 A 5315 5616795503 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 12 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, FS 12 LBL 40 TO 60 FLOORBEAM LOWER FLANGE HAS EXFOLIATED CORROSION. REPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996102400491 19961024 00491 WP 1996 10 24 UPS96821373 1 19960910 A 5315 3774609503 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 55 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, MAIN CABIN FLOORBEAM FS 55 HEAVY CORROSION ON RBL 28 TO RBL 45. REPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996102400492 19961024 00492 WP 1996 10 24 UPS96821374 1 19960916 A 5330 5613861361 SKIN DOUG DC8 DC873F 302199F WP BS 25-70 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, FUSELAGE SKIN HEAVY CORROSION FS 70 TO 25 LONGERONS 21L TO 31L. REPAIRED SKIN PER DAL DRAWING NR 5 613861 AND UPS EO. 2 L 7 4 4F RT 4A25 1996102400493 19961024 00493 WP 1996 10 24 UPS96821375 1 19960904 A 5320 5612298 DOUBLER DOUG DC8 DC873F 302199F WP BS 52-67 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, HEAVY CORROSION ON FUSELAGE FWD NOSE SECTION PANEL DOUBLER FS 52 TO 67 LONGERON 22R. REPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996102400494 19961024 00494 WP 1996 10 24 UPS96821376 1 19960904 A 5320 5612298 DOUBLER DOUG DC8 DC873F 302199F WP BS 32-12 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, HEAVY CORROSION ON FWD NOSE SECTION RT SIDE DOUBLER FS 32 TO FS 12 RBL 25 TO RBL 45. REPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996102400495 19961024 00495 WP 1996 10 24 UPS96821377 1 19960918 A 5315 57735231 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 680 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, HEAVY EXFOLIATED CORROSION AT CABIN FLOORBEAM FS 680 UPPER FLANGE RBL 60. REPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996102400496 19961024 00496 WP 1996 10 24 UPS96821378 1 19960907 A 5313 97585011 LONGERON DOUG DC8 DC873F 302199F WP BS 1140 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, FS 1140 AT LONGERON 29L HAS HEAVY CORROSION. REPAIRED LONGERON PER UPS EO. 2 L 7 4 4F RT 4A25 1996102400497 19961024 00497 WP 1996 10 24 UPS96821379 1 19961001 A 5320 56119433 ANGLE DOUG DC8 DC873F 302199F WP BS 70 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, HEAVY CORROSION AT FS 70 CAP ANGLE FWD SIDE BETWEEN LONGERONS 31L TO 31R. REPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996102400498 19961024 00498 WP 1996 10 24 UPS96821380 1 19960907 A 5320 559799214 FITTING DOUG DC8 DC873F 302199F WP BS 130 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-CS2, HEAVY CORROSION ON COCKPIT SUBFLOOR AND VERTICAL RETAINER FITTING FS 130 RBL 40. REPLACED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996102400499 19961024 00499 1996 10 24 UPS96821384 4 19961020 A 2565 51561004DG DOOR SLIDE DOUG DC8 DC873F 302199F WP ENTRY DOOR LOW PRESS A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE-N/A, MAIN ENTRY DOOR ESCAPE SLIDE PRESSURE LOW SEE REQ A446735. REMOVED AND REPLACED MAIN ENTRY DOOR ES CAPE SLIDE ON 5156100-4DG. 2 L 7 4 4F RT 4A25 1996102400500 19961024 00500 WP 1996 10 24 UPS96821385 1 19961019 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE-N/A, EMERGENCY LIGHTS WEAK. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. 2 L 7 4 4F RT 4A25 1996102400501 19961024 00501 EU 1996 10 24 WWMA9600085 1 19961020 A 2612 FIRE SENSOR SAAB SF340 340B 7860101 EU CARGO COMPT MALFUNCTIONED A WWMA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 WP 15 245AE 340B245 CARGO SMOKE CWP LIGHT CAME ON IN FLIGHT. FOLLOWED QRH AND FIRED NR 1 BOTTLE. EMERGENCY WAS DECLARED. REPLACED NR 1 FI RE BOTTLE AND FORWARD AND AFT SENSORS. 2 L 7 2 4T RT A52EU 1996102400502 19961024 00502 EU 1996 10 24 WWMA9600084 1 19961019 A 2611 SMOKE SENSOR SAAB SF340 340B 7860101 EU CARGO COMPT MALFUNCTIONED A WWMA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 WP 15 245AE 340B245 CARGO SMOKE CWP LIGHT CAME ON IN FLIGHT. FIRED NR 1 BOTTLE. NO FIRE OR SMOKE, EMERGENCY WAS DECLARED. INSPECTED CARGO COMPARTMENT FOR SIGNS OF FIRE, FOUND NONE. DEFERRED TO DFW, REPLACED NR 1 FIRE BOTTLE AND FORWARD SENSOR. 2 L 7 2 4T RT A52EU 1996102400503 19961024 00503 NM 1996 10 24 96FDEA01588 1 19960916 A 5320 65504531 SHELF BOEING 727 72725 1384006 NM BS 336 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR 0689 - 042, WHILE WORKING NR0669 FOUND NOSE GEAR DRAG BRACE SUPPORT BEAM TO BE CRACKED BS 336 WL 153 LBL 13 TO LBL 20 . *S/D* REMOVED DRAG BRACE SHELF, INSTALLED NEW DRAG BRACE SHELF AND REINSTALLED ALL ITEMS REMOVED FOR ACCESS IAW FE DEX EA 7-5310-31130, AT BS 336 TO 360 WL 153 LBL 15 TO RBL 15. 2 L 7 3 4F A3WE 1996102400504 19961024 00504 NM 1996 10 24 96FDEA01589 1 19960926 A 5311 FRAME BOEING 727 72722C 138400F NM BS 540 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 106FE 19201 FRAME DENTED STA 540 STR 6R. INSTALLED FRAME REPAIR STA 540 STR 6R PER SRM 53-10-6. 2 L 7 3 4F A3WE 1996102400505 19961024 00505 NM 1996 10 24 96FDEA01590 1 19960926 A 5311 FRAME BOEING 727 72722C 138400F NM BS 580 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 106FE 19201 FRAME DENTED STA 580 STR 6R. INSTALLED FRAME REPAIR STA 580 STR 6R PER SRM 53-10-6. 2 L 7 3 4F A3WE 1996102400506 19961024 00506 NM 1996 10 24 96FDEA01591 1 19961001 A 5320 WEB BOEING 727 72722C 138400F NM BS 870 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 106FE 19201 CENTER TANK, 2 BAD RIVETS ON BACK WEB RBL 40 TO 60 STA 870. REMOVED WEB TO GAIN ACCESS, REMOVED CORROSION, INSTALLED RE PAIR PER SRM 51-40-2 AND EA 7-5710-28898 DATED OCT 1, L996. 2 L 7 3 4F A3WE 1996102400507 19961024 00507 NM 1996 10 24 96FDEA01592 1 19961002 A 5320 FITTING BOEING 727 72722C 138400F NM CARGO COMPT CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 106FE 19201 MAIN CARGO COMPT 3RD FITTING BOX HAS HEAVY EXFOLIATION CORROSION, 3RD FITTING I/B FROM RT SIDE OF AIRCRAFT, FOR CARGO BA RRIER NET 9G FITTING. FABRICATED NEW 9G FITTING BOX ON SHOP W/O AND YUB 2 ATTACHED. REMOVED AND REPLACED 9G FITTING BO X PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996102400508 19961024 00508 NM 1996 10 24 96FDEA01593 1 19961002 A 5320 DOUBLER BOEING 727 72722C 138400F NM BS 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 106FE 19201 FINGER DOUBLER IS CRACKED AT DOOR REINFORCEMENT, STATION 600 BELOW STRINGER 2 RT. REMOVED CRACKED BENT SECTION, FABRICA TED REPLACEMENT DOUBLER, ALODINED, PRIMED AND INSTALLED WET WITH SEALER. INSTALLED REPAIR IAW SRM 51-40-2. REPLACEMEN T DOUBLER 3 BY 6 MATERIAL 2024-T3 X .063 THICK. 2 L 7 3 4F A3WE 1996102400509 19961024 00509 NM 1996 10 24 96FDEA01594 1 19961010 A 5315 FLOORBEAM BOEING 727 72722C 138400F NM BS 344 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 106FE 19201 EXFOLIATION CORROSION ON FLOORBEAM AT FS 344 FROM RBL 14 TO LBL 35. CUT AND SPLICED IN NEW SECTION OF UPPER FLOORBEAM C AP AT FS 344 FROM 14 RBL TO 70 LBL IAW SRM 53-10-8 FIG 9. 2 L 7 3 4F A3WE 1996102400510 19961024 00510 NM 1996 10 24 96FDEA01595 1 19961019 A 5315 652083289 FLOOR BEAM BOEING 727 727233 138408A NM BS 1010 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 NR0180 - 001, CORROSION (C53-113-01, -2) ON LOWER CHORD OF FLOORBEAM AT BS 1010 LBL 1 TO LBL 43 WL 200 AT NUTPLATE HOLES . *S/D* B/S 1010 LBL 1 TO LBL 43 WL 200 REPAIRED LOWER CHORD OF FLOORBEAM PER FEDEX SRM 53-10-8 FIG 8. 2 L 7 3 4F RT A3WE 1996102400511 19961024 00511 NM 1996 10 24 96FDEA01596 1 19961020 A 5754 65162252 BONDING JUMPER BOEING 727 727233 138408A NM NR 4 LE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 NR0318 - 002, CORROSION (C 57-562-01-02) NR 4 K-FLAP O/B RIB AT PREVIOUS BONDING JUMPER ATTACH POINT. *S/D* FOUND TO B E OUT OF LIMITS. REPAIRED NR 4 K-FLAP O/B RIB AT BONDING JUMPER ATTACH POINT IAW FEDEX SRM 57-50-3. 2 L 7 3 4F RT A3WE 1996102400512 19961024 00512 NM 1996 10 24 96FDEA01597 1 19961020 A 5711 65C21532 SPAR CHORD BOEING 727 72722 1384002 NM BS 740 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 150FE 19141 NR0172 - 001, CORROSION (C53-132-02-01) ON LOWER 740 CHORD AT LBL 4. *S/D* REMOVED CORRODED BS 740 FRONT SPAR LOWER CH ORD AND INSTALLED NEW BS 740 FRONT SPAR LOWER CHORD PER FEDEX EA NR 7-5710-31160. 2 L 7 3 4F A3WE 1996102400513 19961024 00513 WP 1996 10 24 96FDEA01598 1 19961020 A 2780 ARH0052516 DRIVE MECH DOUG DC10 DC1030 3023501 WP LE FLAPS CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 329FE 47820 SNRM N00046. DURING REPETITIVE INSP OF RT O/B SLAT DRIVE MECHANISM REF: E.O. 8-2780-7-2319 C1 PT 1, FOUND BRACKET ASSY FWD ATTACH FLANGE HAS MULTIPLE CRACKS. REMOVED AND REPLACED SLAT DRIVE MECHANISM PER MM 27-83-02. RIGGED FOLLOW-UP CA BLES PER MM 27-80-00. 2 L 7 3 4F A22WE 1996102400514 19961024 00514 NM 1996 10 24 96FDEA01485 1 19960916 A 5320 65185401 CHORD BOEING 727 72725 1384006 NM BS 740 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR 0431 AND 031, CORROSION (C53-224-05) BS 740 LBL 12 ON LOWER CHORD OF CENTER FUEL CELL. *S/D* REMOVED DAMAGED LOWER CHORD AT BS 740 AND INSTALLED NEW CHORD PER FEDEX EA NR 7-5710-31187, REF NR 0674. 2 L 7 3 4F A3WE 1996102400515 19961024 00515 NM 1996 10 24 96FDEA01486 1 19960916 A 5320 651594017 CHORD BOEING 727 72725 1384006 NM BS 740 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR 0542 AND 032, CORROSION (C53-224-05) BS 740 RBL 68 ON UPPER CHORD OF CENTER FUEL CELL. *S/D* REMOVED DAMAGED UPPER CHORD AT BS 740 AND INSTALLED NEW CHORD IAW FEDEX EA 7-5710-31199. 2 L 7 3 4F A3WE 1996102400516 19961024 00516 NM 1996 10 24 96FDEA01488 1 19960916 A 5711 65185371 SPAR CHORD BOEING 727 72725 1384006 NM BS 870 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 510FE 18282 NR 0685 AND 034, UPON REMOVAL OF REAR SPAR WEB FOUND CORROSION ON LOWER 870 SPAR CHORD BS 870 LBL 50 TO RBL 50 WL 161. * S/D* REMOVED CORROSION ON BS 870 SPAR CHORD, FOUND CHORD IS OUT OF LIMITS PER FEDEX SRM 57-12-20. REMOVED AND REPLACED LOWER CHORD PER FEDEX EA 7-5710-31178. 2 L 7 3 4F A3WE 1996102400517 19961024 00517 NM 1996 10 24 P5CA9600810 1 19961017 A 3350 S1356B37 LIGHT BOEING 747 747122 1384872 NM CABIN INOPERATIVE A P5CA K NONE L NO TEST IN INSP/MAINT 1 WP 23 850FT 19755 INOPERATIVE EMERGENCY LIGHT ASSEMBLY ON UPPER DECK. REPLACED EMERGENCY LIGHT AND BATTERY PACK ASSEMBLY PER BAC MM 33-51 -00. 2 L 7 4 4F A20WE 1996102400518 19961024 00518 NM 1996 10 24 P5CA9600811 1 19961018 A 2131 7102976 CONTROLLER BOEING 747 747122 1384872 NM COCKPIT FAILED A P5CA A J UNSCHED LANDING DUMP FUEL O OTHER CL CLIMB 1 WP 23 852FT 19757 AT 13 FT THE AUTO FAIL LIGHT CAME ON, WENT MANUAL BACK TO AUTO FAIL LIGHT OFF AND BACK ON. CABIN WENT TO 8.6 FEET DIFFE RENTIAL PRESSURE 9.4 BOTH OUT FLOW VALVES CLOSED, CABIN STILL CLIMBING AT FL 20.0. REPLACED AUTO PRESSURE CONTROLLER, O PERATIONAL CHECK OF PER BOEING MAINTENANCE MANUAL 21-31-02. 2 L 7 4 4F A20WE 1996102400519 19961024 00519 NM 1996 10 24 P5CA9600812 1 19961014 A 5400 FAIRING BOEING 747 747123 1384873 NM LT WING/PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 CRACKED WING TO PYLON FAIRING ON LEFT WING NR 1 PYLON INBOARD OF NR 5 LEADING EDGE FLAP. REPAIRED PER BOEING SRM 51-40- 09. 2 L 7 4 4F A20WE 1996102400520 19961024 00520 NM 1996 10 24 P5CA9600813 1 19961016 A 5330 SKIN BOEING 747 747124 1384874 NM CARGO DR CUTOUT CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 CRACK BY FORWARD CARGO DOOR CUTOUT LOWER FORWARD CORNER. BLENDED OUT IN OUTER SKIN AS PER BOEING SRM 51-30-01 FIG 1 AND CLEANED AND PAIRNET PER BOEING SRM 51-21-04 EDDY CURRENT OUTER SKIN PER NDT MANUAL PART 6 53-10-25. ACCOMPLISHED PER P OLAR AIR CARG0 MA 5330-11-01. 2 L 7 4 4F A20WE 1996102400521 19961024 00521 NM 1996 10 24 P5CA9600814 1 19961018 A 5230 65B047306 STOP BOEING 747 747123 1384873 NM CARGO DOOR BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 BROKEN LOWER AFT STOP ON FORWARD LOWER LOBE CARGO DOOR. REPLACED STOP PER BAC MM 52-34-00. 2 L 7 4 4F A20WE 1996102400522 19961024 00522 NM 1996 10 24 P5CA9600815 1 19961017 A 5320 65B028292 RIB BOEING 747 747122 1384872 NM APU COMPT CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 CRACKED RIB IN APU COMPARTMENT IN STRUCTURE FOR HOLDING AFT APU REMOVAL FISH POLE AND CRACKED BOLT HOLE. PARTS TO BE RE PLACED WITHIN 50 CYCLE OPERATION WITH APU REMOVED APPROVED BY BOEING. REPLACED SUPPORT RIB ASSEMBLY PER BOEING SRM 51-1 0-01. 2 L 7 4 4F A20WE 1996102400523 19961024 00523 NM 1996 10 24 P5CA9600816 1 19961016 A 5330 SKIN BOEING 747 747124 1384874 NM BS 540 DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 DENT IN SKIN AT STATION 540 BETWEEN LAP SEAM S39R AND STRINGER S38R. EDDY CURRENT CHECK CONFIRMED NO CRACK. REPAIRED P ER BAC SRM 51-40-01. 2 L 7 4 4F A20WE 1996102400524 19961024 00524 NM 1996 10 24 P5CA9600817 1 19961016 A 5230 SKIN BOEING 747 747124 1384874 NM CARGO DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 SEVEN INCH CRACK AT LOWER FORWARD SKIN ON THE REAR LOWER LOBE CARGO DOOR. REPAIRED PER BAC SRM 52-00-03 FIG 4. 2 L 7 4 4F A20WE 1996102400525 19961024 00525 NM 1996 10 24 P5CA9600818 1 19961018 A 2912 60B002012 FILTER MODULE BOEING 747 747122 1384872 NM NR 3 HYD SYST CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 CRACKED NR 3 HYDRAULIC SYSTEM FILTER MODULE. REPLACED MODULE PER BOEING MAINTENANCE MANUAL 29-11-23. 2 L 7 4 4F A20WE 1996102400526 19961024 00526 NM 1996 10 24 P5CA9600819 1 19961018 A 2550 ROLLER TRACK BOEING 747 747123 1384873 NM BS 1800 DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 DAMAGED ROLLER TRACK AFT CARGO COMPARTMENT BS 1800 RBL 36. REMOVED FABRICATED REPLACEMENT TRACK AND INSTALLED PER BOEIN G SRM 51-10-01. 2 L 7 4 4F A20WE 1996102400527 19961024 00527 NM 1996 10 24 P5CA9600820 1 19961018 A 5330 SKIN BOEING 747 747123 1384873 NM FUSELAGE BENT A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 BENT EXTERNAL SKIN AT NR 1 MAIN ENTRY DOOR HINGE CUT OUT. REPAIRED PER BOEING SRM 52-00-02. 2 L 7 4 4F A20WE 1996102400528 19961024 00528 NM 1996 10 24 P5CA9600821 1 19961018 A 2550 ROLLER AND TRAY BOEING 747 747123 1384873 NM FWD CARGO BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 BROKEN ROLLER AND TRAY FWD CARGO COMPARTMENT BS 660 RBL 25. REPLACED ROLLER AND TRAY PER BOEING SRM 51-10-01. 2 L 7 4 4F A20WE 1996102400529 19961024 00529 NM 1996 10 24 P5CA9600822 1 19961018 A 7110 NOSE COWL BOEING 747 747123 1384873 NM NR 2 ENGINE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 DELAMINATED OUTER SKIN ON NR 2 ENGINE NOSE COWL AT 5 AND 7 O'CLOCK POSITIONS. REPAIRED PER BOEING SRM 51-40-06. 2 L 7 4 4F A20WE 1996102400530 19961024 00530 NM 1996 10 24 P5CA9600823 1 19961018 A 7110 FAN REV SLEEVE BOEING 747 747123 1384873 NM NR 4 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 CRACKED REPAIR PATCH ON NR 4 ENGINE FAN REVERSER SLEEVE AT 8 AND 9 O'CLOCK. REPAIRED PER BOEING SRM 51-40-06. 2 L 7 4 4F A20WE 1996102400531 19961024 00531 NM 1996 10 24 P5CA9600824 1 19961018 A 5314 KEEL BEAM BOEING 747 747123 1384873 NM BS 1350 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 CRACKED LEFT BODY GEAR INBOARD DOOR AT KEEL BEAM PANEL BS 1350 LBL 09 WL 90. REPAIRED PER BOEING SRM 51-40-09. 2 L 7 4 4F A20WE 1996102400532 19961024 00532 NE 1996 10 24 P5CA9600825 2 19961018 A 7250 TURBINE CASE BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE NR 1 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 662599 CRACKS IN R AND S RAILS AT 2 O'CLOCK POSITION. WELD REPAIRED AND STRESS RELIEVED PER PRATT AND WHITTNEY MAINTENANCE MAN UAL 73-53-01, FLAP PEENED PER BOEING OVERHAUL MANUAL 20-10-03. 2 L 7 4 4F 4 F A20WE E20EA 1996102400533 19961024 00533 NM 1996 10 24 P5CA9600826 1 19961018 A 7110 FAN COWL BOEING 747 747123 1384873 NM NR 3 ENGINE DISBONDING A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 DISBONDING REPAIR ON NR 3 ENGINE LEFT FAN COWL AT 10 O'CLOCK POSITION. REPAIRED PER BOEING SRM 51-40-06. 2 L 7 4 4F A20WE 1996102400534 19961024 00534 NM 1996 10 24 P5CA9600827 1 19961014 A 2450 CONNECTOR BOEING 747 747123 1384873 NM NR 4 PYLON BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 BROKEN CANNON PLUG (D0048P) BACK SHELL NR 4 PYLON. REPAIRED PER BOEING STANDARD PRACTICE 20-31-00. 2 L 7 4 4F A20WE 1996102400535 19961024 00535 NM 1996 10 24 P5CA9600828 1 19961019 A 2780 TORQUE TUBE BOEING 747 747122 1384872 NM RT LT FLAPS SHEARED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 SHEARED TORQUE TUBE OUTBOARD OF THE RIGHT WING SET 4 LEADING EDGE POWER DRIVE UNIT. REPAIRED PER BOEING SRM 51-30-02, I NSTALLED PER MAINTENANCE MANUAL 27-81-05, RIG AND FUNCTIONAL CHECKED PER 27-81-00. 2 L 7 4 4F A20WE 1996102400536 19961024 00536 WP 1996 10 24 RRXA96124 1 19961018 A 2420 GENERATION SYST DOUG DC8 DC862F 3021972 WP NR 2 MALFUNCTIONED A RRXA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 WP 15 996CF 46162 DURING CRUISE, NR 2 GENERATOR LOCKED OUT. BUS RESET, VOLTS AND FREQS NORMAL, GEN RELAY OPEN, LT EMERGENCY BUS POWER FAI LURE LIGHT ILLUM AND LOST ASSOCIATED BUS. 996CF DIVERTED TO KORD. *S/D* MAINTENANCE TRANSFERED THE NR 2 GEN TO THE DM I LIST. NR 2 BUS OPERATED NORMALLY THROUGH THE AC TIE SYSTEM. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE NR 2 G ENERATOR SYSTEM AND FOUND NO DEFECTS. THE DMI WAS CLEARED ON 10/18/96. THIS CLOSES SDR RRXA96124. 2 L 7 4 4F 4A25 1996102400537 19961024 00537 WP 1996 10 24 RRXA96123 1 19961021 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 36-70 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A RECENT MAINTENANCE VISIT, FOUND WIDESPREAD CORROSION DAMAGE TO LONGERONS 25R AND 26R AT Y=36 TO Y=70 PAST LIMI TATIONS. REMOVED, FABRICATED AND INSTALLED NEW LONGERONS 26R IAW DGW 569028 AND LONGERON 27R IAW DWG 3648667. INSTALLE D ALL SHEAR TIES, CLIPS TO LONGERONS 25R, 26R AND 27R IAW DWG 5649028. REMOVED ALL CORROSION, ALODINED AND PRIMED IAW S RM 51-1-8. 2 L 7 4 4F RT 4A25 1996102400538 19961024 00538 WP 1996 10 24 RRXA96122 1 19961021 A 5320 ANGLE DOUG DC8 DC871F 302199D WP BS 856-902 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A RECENT MAINTENANCE VISIT, FOUND ANGLE ON FORWARD SKIN IN RIGHT WHEEL WELL AT Y=856 TO Y=902 CORRODED PAST LIMIT ATIONS. FABRICATED NEW ANGLE IAW DRW 5616306, INSTALLED ANGLE IAW DC-8 SRM 51-1-21 AND TREATED AREA IAW SR 51-1-8. 2 L 7 4 4F RT 4A25 1996102400539 19961024 00539 WP 1996 10 24 RRXA96121 1 19961021 A 5320 DOUBLER DOUG DC8 DC871F 302199D WP BS 520 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8085U 45975 DURING A RECENT MAINTENANCE VISIT FOUND SKIN DOUBLER AT Y=520 AND LONGERON 31R CORRODED BEYOND LIMITATIONS. REPAIRED SK IN DOUBLER BY FABRICATING NEW SKIN DOUBLER, SUBSTITUTION OF ORIGINAL MATERIAL 0.040 TITANIUM FOR STAINLESS STEEL PER DWG 5616520. INSTALLED SKIN DOUBLER IAW DC-8 SRM 51-1-21 AND 51-1-20D AND TREATED AREA IAW SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996102400540 19961024 00540 NM 1996 10 24 CALA9601492 1 19961019 A 2612 FIRE WARNING BOEING 727 727224 1384076 NM APU ACTIVATED A CALA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 09 79748 22450 THE APU FIRE WARNING LIGHT ILLUMINATED WHILE EN ROUTE. THE APU FIRE BOTTLE WAS DISCHARGED AND THE LIGHT EXTINGUISHED, B UT CAME BACK ON. THE AIRCRAFT WAS DIVERTED TO PIT. THE LIGHT EXTINGUISHED AGAIN AFTER 10 MINUTES AND THE AIRCRAFT LAND ED AT PIT WITHOUT FURTHER PROBLEM. MAINTENANCE INSPECTED THE WHEEL WELL AREA, APU AND APU EXHAUST AND FOUND NO EVIDENCE OF FIRE OR OVERHEAT CONDITIONS. THE APU FIRE BOTTLE WAS REMOVED AND REPLACED. THE APU WAS RUN AND A FIRE TEST WAS PER FORMED WITH NO FIRE WARNING INDICATIONS NOTED. MAINTENANCE WAS UNABLE TO DUPLICATE THE PROBLEM. 2 L 7 3 4F A3WE 1996102400541 19961024 00541 WP 1996 10 24 CALA9601493 1 19961021 A 3260 833604 PROX SWITCH DOUG DC9 DC981 3022081 WP NLG DIRTY A CALA O OTHER N FALSE WARNING CL CLIMB 1 SW 09 16884 48074 THE RED NOSE GEAR UNSAFE LIGHT ILLUMINATED INTERMITTENTLY AFTER GEAR WAS RETRACTED. THE GEAR WAS CYCLED, BUT THE LIGHT CONTINUED TO ILLUMINATE INTERMITTENTLY. THE LIGHT EXTINGUISHED AT A SPEED OF 240 KNOTS AND REMAINED OUT. THE FLIGHT WA S CONTINUED TO EWR WHERE IT LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND MOISTURE AND DEBRIS ON THE NLG PROXIMITY SWITCH AND THE SWITCH WAS CLEANED. THE GEAR WAS CYCLED SEVERAL TIMES WITH OPERATION AND INDICATIONS CHECKING GOOD. THE AIRCRAFT HAS FLOWN FOUR FLIGHTS WITHOUT A REPEAT OF NLG INDICATION PROBLEMS SINCE THIS CORRECTIVE ACTION WAS IMPLEMENTE D. 2 L 7 2 4F A6WE 1996102400542 19961024 00542 WP 1996 10 24 9622319997 1 19961020 A 3610 5958765503 MANIFOLD DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7 52053 NE RT ENGINE CRACKED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 8933E 47142 649604 DURING CLIMBOUT, THE RIGHT ENGINE FIRE LOOP WARNING LIGHT ILLUMINATED. CREW RETARDED THE RIGHT ENGINE THROTTLE SETTING AND THE LIGHT EXTINGUISHED. AIRCRAFT RETURNED TO IND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE 13T H STAGE MANIFOLD ON THE RIGHT ENGINE, LEAK AND OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F A6WE E2EA 1996102400543 19961024 00543 NM 1996 10 24 9622322706 1 19961013 A 5751 BUSHING BOEING 727 727225 1384077 NM LT AILERON WORN A NWAA A UNSCHED LANDING E F VIBRATION/BUFFET FLT CONT AFFECTED CL CLIMB 1 GL 01 815EA 22552 DURING CLIMBOUT WHILE ACCELERATING TO 300 KTS IN CLEAN CONFIGURATION, THE AIRCRAFT BEGAN A MEDIUM FREQUENCY VIBRATION. V ISUAL CHECK OF WINGS SHOWED LEFT INBOARD AILERON VIBRATING UP AND DOWN PLUS OR MINUS 2 INCHES AT THE TRAILING EDGE, RIGH T AILERON PLUS OR MINUS 1 INCH. SLOWED AIRCRAFT TO 250 KTS AND VIBRATION STOPPED. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED WORN BUSHING IN THE LEFT INBOARD AILERON QUADRANT, RIG CHECK OK. 2 L 7 3 4F A3WE 1996102400544 19961024 00544 WP 1996 10 24 9622339755 1 19961020 A 2613 TEMP SENSOR DOUG DC9 DC941 302207N WP TAIL COMPT MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 755NW 47179 TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED DURING TAKEOFF. FOLLOWED COM AND LIGHT WENT OUT. FLIGHT RETURNED T O HOU AND LANDED WITHOUT INCIDENT. REPLACED TAIL COMPARTMENT SENSOR AND RIGHT COALESCER BAG. RAN AIRCRAFT TO FULL POWE R, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996102400545 19961024 00545 WP 1996 10 24 9622349101 1 19961018 A 2750 FLAP SW ARM DOUG DC9 DC915 3022036 WP FLAP HANDLE BINDING A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 91S 47063 AFTER TAKEOFF, THE FLAP HANDLE WAS VERY DIFFICULT TO MOVE TO RETRACT POSITION. FLIGHT RETURNED TO MSP AND LANDED WITHOU T INCIDENT. FOUND FLAP SWITCH ARM BINDING ON SECTOR COTTER PINS. REPLACED PINS AND SHIMMED SWITCH, OPERATIONAL CHECK O K. 2 L 7 2 4F A6WE 1996102400546 19961024 00546 WP 1996 10 24 9622359972 1 19961020 A 3010 12294411 ANTI-ICE VALVE DOUG DC9 DC931 3022065 WP LT WING FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 9336 49808 10 47338 AIRFOIL ICE PROTECTION PRESSURE ABNORMAL LIGHT ILLUMINATED AFTER TAKEOFF. WING ANTI-ICE BLUE LIGHT WAS NOT ON. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE CONFIRMED POWER TO WING VALVE AT PIN-B IN LEFT WHEEL WELL. RE PLACED LEFT WING ICE PROTECTION SHUTOFF VALVE, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996102400547 19961024 00547 WP 1996 10 24 9622369609 1 19961020 A 2130 94840213 AMPLIFIER DOUG DC9 DC932 3022066 WP E/E COMPARTMENT MALFUNCTIONED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 609NW 36691 2764 47234 AUTO PRESSURIZATION SYSTEM FAILED AFTER TAKEOFF. OUTFLOW VALVE WENT FROM FULL OPEN TO FULL CLOSED. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED CABIN PRESSURE AMPLIFIER, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996102400548 19961024 00548 WP 1996 10 24 9622379868 1 19961017 A 2741 DT2RA7 SWITCH DOUG DC9 DC951 3022051 WP STABILIZER MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 777NC 47787 TAKEOFF WARNING HORN SOUNDED ON TAKEOFF ROLL. ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE FOUND STABILIZER POSIT ION SWITCH S1-141 INOPERATIVE. REPLACED SWITCH, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996102400549 19961024 00549 WP 1996 10 24 9622389903 1 19961016 A 3610 CLAMPS DOUG DC9 DC931 3022065 WP TAIL COMPT LOOSE A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 953N 47083 TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LOOSE CLAMPS ON CROSSFEED VALVE AND RIGHT AUGMENTATION VALVE. TIGHTENED CLAMPS, LEAK AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996102400550 19961024 00550 WP 1996 10 24 9622399881 1 19961017 A 2781 SWITCH DOUG DC9 DC951 3022051 WP RT LE FLAPS MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 676MC 47652 TAKEOFF WARNING HORN SOUNDED AS TAKEOFF POWER WAS APPLIED. ABORTED TAKEOFF AT 5 KTS AND RETURNED TO THE GATE. MAINTENA NCE REPLACED THE RIGHT SLAT SWITCH, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996102400551 19961024 00551 WP 1996 10 24 9622409991 1 19961016 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP TAILCONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8957E 47215 DURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996102400552 19961024 00552 1996 10 24 9622419304 4 19961020 A 2565 100503101 SLIDE DOUG DC9 DC982 3022082 WP AFT TAILCONE DEPLOYED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 931MC 25660 2423 480574 AFT TAILCONE EVACUATION SLIDE INADVERTANTLY DEPLOYED. REPLACED SLIDE. 2 L 7 2 4F A6WE 1996102400553 19961024 00553 WP 1996 10 24 9622429958 1 19961020 A 3350 6014113 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 917RW 47145 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS, OPERATI ONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996102400554 19961024 00554 WP 1996 10 24 9622439964 1 19961019 A 3350 6011779 POWER SUPPLY DOUG DC9 DC931 3022065 WP RT NACELLE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 912RW 47150 DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT ENGINE NACELLE EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, OPE RATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996102400555 19961024 00555 WP 1996 10 24 9622449150 1 19961020 A 3350 60030451 BATTERY PACK DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8908E 45749 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, O PERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996102400556 19961024 00556 WP 1996 10 24 9622459307 1 19961019 A 3350 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 309RC 48088 DURING PERIODIC CHECK, FOUND OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 25 THROUGH 28 INOPERATIVE. REPLACED BATTERIES, OPER ATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996102400557 19961024 00557 WP 1996 10 24 9622469856 1 19961019 A 3350 LIGHTS DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 765NC 47718 DURING LINE MAINTENANCE INSPECTION, FOUND AFT OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. CYCLED SWITCH SEVERAL TIMES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996102400558 19961024 00558 WP 1996 10 24 9622479867 1 19961019 A 3350 6014113 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 776NC 47786 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS BETWEEN ROWS 9 THROUGH 15 VERY DIM. REPLACED POWER SUPPLY AND BATTERY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996102400559 19961024 00559 WP 1996 10 24 9622489883 1 19961019 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 671MC 47660 DURING LINE MAINTENANCE INSPECTION, FOUND ROWS 12 THROUGH 15 OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996102400560 19961024 00560 WP 1996 10 24 9622499961 1 19961017 A 3350 FUSE DOUG DC9 DC931 3022065 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 924RW 47185 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996102400561 19961024 00561 WP 1996 10 24 9622509946 1 19961016 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8926E 45863 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS AT ROW 13 INOPERATIVE. MAINTENANCE FOUND BRO KEN WIRE ON CONNECTOR UNDER SEAT. REPAIRED BROKEN WIRE, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996102400562 19961024 00562 EU 1996 10 24 COMA9630153 1 19961020 A 2460 A2042C PDU SAAB SF340 SF340A 7850100 EU LEFT FAILED A COMA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 SO 01 361CA 23692 200 340A056 LEFT MAIN ELECTRICAL BUS DROPPED OFF LINE. REPLACED THE LT POWER DISTRIBUTION UNIT. 2 L 7 2 4T RT A52EU 1996102400563 19961024 00563 EA 1996 10 24 COMA9660174 1 19961018 A 3411 PITOT SYST CNDAIR CL600 CL6002B19 EA COCKPIT WATER CONTAM A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 963CA 7127 TAKE OFF ABORTED DUE TO 50 KTS DIFFERENCE BETWEEN PILOT AND COPILOTS AIRSPEED INDICATORS. REMOVED WATER FROM PITOT SYST EM, SYSTEM TEST SATISFACTORY. 2 L 7 2 4F RT A21EA 1996102400564 19961024 00564 EA 1996 10 24 COMA9660175 1 19961020 A 2750 860D10018AB FECU CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION LD LANDING 1 SO 01 914CA 2797 1093 7012 FLAPS FAIL MESSAGE ON EICAS, FLAPS STUCK AT 45 DEGREES. COULD NOT DUPLICATE PROBLEM. REPLACED THE FLAP ELECTRONIC CONT ROL UNIT FOR TROUBLESHOOTING. 2 L 7 2 4F RT A21EA 1996102400565 19961024 00565 EA 1996 10 24 COMA9660176 1 19961019 A 2910 AE2460010HO264 HYD LINE CNDAIR CL600 CL6002B19 EA LT PYLON FAILED A COMA K NONE K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 956CA 7105 NR 1 HYDRAULIC SYSTEM INDICATES ZERO PRESSURE AND ZERO QUANTITY. REPLACED FAILED HYDRAULIC LINE IN LT ENGINE PYLON. 2 L 7 2 4F RT A21EA 1996102400566 19961024 00566 EA 1996 10 24 COMA9660177 1 19961018 A 2760 270003 PCU CNDAIR CL600 CL6002B19 EA LT SPOILER MALFUNCTION A COMA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 01 937CA 7044 FLIGHT SPOILERS FAULT MESSAGE ON EICAS. REPLACED THE LT OUTBD FLIGHT SPOILER POWER CONTROL UNIT. 2 L 7 2 4F RT A21EA 1996102400567 19961024 00567 NM 1996 10 24 SWAA961106 1 19961017 A 3350 LIGHT BOEING 737 7373G7 1384595 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED 3C1 CHECK, FOUND EMERGENCY LIGHTING AT FWD F/A STATION BROKEN. REPLACED LIGHT ASSEMBLY PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996102400568 19961024 00568 NM 1996 10 24 SWAA961107 1 19961017 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 60SW 21812 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 862, RBL 16, WL 160, AT BS 502, RBL 52, WL 169, AT BS 819, R BL 11, WL 155 AND AT BS 421, RBL 47, WL 165. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996102400569 19961024 00569 NM 1996 10 24 SWAA961108 1 19961017 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 60SW 21812 DURING SCHEDULED D-CHECK, FOUND CORROSION BULGING BETWEEN DOUBLERS AND SKIN AT BS 727, WL 148, LBL 4. REPAIRED PER BOEI NG SRM. 2 L 7 2 4F A16WE 1996102400570 19961024 00570 NM 1996 10 24 SWAA961109 1 19961017 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 60SW 21812 DURING SCHEDULED D-CHECK, FOUND DOUBLER CRACKED AT BS 1088 TO 1138 S5L. ALSO, AT BS 1088 TO 1156, S12L. REPAIRED PER B OEING SRM. 2 L 7 2 4F A16WE 1996102400571 19961024 00571 NM 1996 10 24 SWAA961110 1 19961017 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 520 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 60SW 21812 DURING SCHEDULED D-CHECK, FOUND CRACK INDICATIONS AT SKIN LAP JOINT BS 520, S10L. INSTALLED REPAIR DOUBLER PER BOEING S RM. 2 L 7 2 4F A16WE 1996102400572 19961024 00572 NM 1996 10 24 SWAA961111 1 19961017 A 5320 CLIP BOEING 737 7372H4 138448C NM BS 1138 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 60SW 21812 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 1138, S16L. INSTALLED REPAIR DOUBLER PER BOEING SRM. 2 L 7 2 4F A16WE 1996102400573 19961024 00573 NM 1996 10 24 SWAA961112 1 19961017 A 5210 DOOR BOEING 737 7372H4 138448C NM AFT ENTRY DAMAGE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 60SW 21812 DURING SCHEDULED D-CHECK, FOUND AFT ENTRY DOOR DAMAGE AROUND LOWER HINGE FITTING ARM. INSTALLED REPAIR DOUBLER PER BOEI NG SRM. 2 L 7 2 4F A16WE 1996102400574 19961024 00574 NM 1996 10 24 SWAA961113 1 19961017 A 2121 215201 FAN BOEING 737 7373H4 1384600 NM COCKPIT FAILED A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 626SW 27702 ON DEPARTURE, CREW NOTED STRONG ELECTRICAL ODOR. GASPER FAN C/B TRIPPED, SMELL DISAPPEARED. CONTINUED PER CREW DEFERRA L MEL 21-25. REMOVED AND REPLACED DEFECTIVE GASPER FAN PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996102400575 19961024 00575 NM 1996 10 24 SWAA961114 1 19961011 A 2751 1817387 TRANSMITTER BOEING 737 7373A4 1384585 NM RT TE FLAPS FAILED A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 673AA 23251 ON CLIMBOUT, FLAPS WOULD NOT RETRACT PAST 2 UNITS, SPILT INDICATION. AIRCRAFT DIVERTED TO OAK AND MADE AN UNEVENTFUL LA NDING. REMOVED AND REPLACED RT FLAP POSITION TRANSMITTER AND OP CHECKED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996102400576 19961024 00576 NM 1996 10 24 SWAA961115 1 19961016 A 3350 1000679 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 87SW 22903 DURING SCHEDULED SERVICE CHECK, FOUND RT AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBL Y AND OP CHECKED PER BOEING M/M. 2 L 7 2 4F A16WE 1996102400577 19961024 00577 NM 1996 10 24 SWAA961116 1 19961016 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 639 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 82SW 22731 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, LEFT SIDE. REPLACED FRAME PER BOEING SRM. 2 L 7 2 4F A16WE 1996102400578 19961024 00578 NM 1996 10 24 SWAA961117 1 19961016 A 3350 900835A BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 61SW 21970 DURING SCHEDULED D-CHECK, FOUND FWD CENTER AISLE EMERGENCY LIGHT BATTERY PACK NOT CHARGING. REMOVED AND REPLACED BATTER Y PACK PER BOEING M/M. 2 L 7 2 4F A16WE 1996102400579 19961024 00579 NM 1996 10 24 SWAA961118 1 19961016 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 61SW 21970 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 1016, WL 208, RBL 3 TO 8. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996102400580 19961024 00580 NM 1996 10 24 SWAA961119 1 19961016 A 3350 2330127 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 56SW 21721 DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR EMERGENCY LIGHT NOT TESTING. REMOVED AND REPLACED LIGHT ASSEMBLY AND OP CHECKED PER BOEING M/M. 2 L 7 2 4F A16WE 1996102400581 19961024 00581 1996 10 24 SWAA961120 4 19961015 A 2565 D31354418 SLIDE BOEING 737 7373H4 1384600 NM AFT ENTRY DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 354SW 25219 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR SLIDE PRESSURE BELOW MINIMUM. REMOVED AND REPLACED SLIDE ASSEMBLY PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996102400582 19961024 00582 NM 1996 10 24 SWAA961121 1 19961015 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 294 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 61SW 21970 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 294, WL 1208, RBL 14, 26, 27 AND 32. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996102400583 19961024 00583 NM 1996 10 24 SWAA961122 1 19961015 A 3397 WIRE BOEING 737 7373H4 1384600 NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 621SW 28037 DURING RON CHECK, FOUND 2 WHITE FLOOR TRACK LIGHTS INOP AND WIRING EXPOSED. REMOVED AND REPLACED WIRING PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996102400584 19961024 00584 NM 1996 10 24 SWAA961123 1 19961011 A 3397 WIRE BOEING 737 7373H4 1384600 NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 636SW 27709 AT GATE FOUND EMERGENCY TRACK LIGHTING INOP AT FORWARD CABIN AREA. REPAIRED WIRING PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996102400585 19961024 00585 NM 1996 10 24 SWAA961124 1 19961016 A 5311 BELT FRAME BOEING 737 7372H4 138448C NM BS 294 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED SERVICE CHECK, FOUND BS 294 BELT FRAME I/B CHORD CRACKED AT S13R. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996102400586 19961024 00586 NM 1996 10 24 SWAA961125 1 19961016 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 278/291 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED SERVICE CHECK, FOUND EXTERIOR FUSELAGE SKIN ATTACH ANGLE CRACKED AT BS 278 AND 291. REPLACED PER BOEIN G SRM. 2 L 7 2 4F A16WE 1996102400587 19961024 00587 NM 1996 10 24 SWAA961126 1 19961016 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 272-291 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED SERVICE CHECK, FOUND EXTERIOR FUSELAGE SKIN CRACKED AT FWD SERVICE DOOR LOWER HINGE CUT OUT BS 291 TO 2 72.5. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996102400588 19961024 00588 NM 1996 10 24 SWAA961127 1 19961016 A 5320 SHEAR TIE BOEING 737 7372H4 138448C NM BS 271 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED SERVICE CHECK, FOUND BELT FRAME SHEAR TIE CRACKED AT BS 271, BETWEEN S12 AND 13. REPAIRED PER SWA RA 1 -353-1535. 2 L 7 2 4F A16WE 1996102400589 19961024 00589 NM 1996 10 24 SWAA961128 1 19961016 A 5320 STRAP BOEING 737 7372H4 138448C NM BS 294 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED SERVICE CHECK, FOUND TEAR STRAP CRACKED THROUGH O/B CHORD OF FRAME AT S16R. REPAIRED PER SWA RA 1-353- 1536. 2 L 7 2 4F A16WE 1996102400590 19961024 00590 NM 1996 10 24 SWAA961129 1 19961016 A 5240 DOUBLER BOEING 737 7372H4 138448C NM FWD SERV DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED SERVICE CHECK, FOUND A 2 INCH LONG CRACK AT BS 294 BETWEEN S9 AND 10 ON DOUBLER, FWD SERV DOOR. REPAIR ED PER SWA RA 1-253-1537. 2 L 7 2 4F A16WE 1996102400591 19961024 00591 NM 1996 10 24 96UAL900780 1 19961007 A 3350 767 BULB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 588UA 26717 EMERGENCY LIGHT AT DOOR 2R INOP. REPLACED BULB, OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996102400592 19961024 00592 NM 1996 10 24 96UAL900782 1 19961008 A 3350 LIGHT BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 161UA 21352 DOOR 1R EMERGENCY BUSTLE LIGHT INOP. REPLACED LIGHT ASSY. 2 L 7 4 4F 4 F A20WE E20EA 1996102400593 19961024 00593 NM 1996 10 24 96UAL900783 1 19961008 A 5730 65B149624 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE WS 821-908 CRACKED A A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 176UA 24383 RIGHT WING FIXED LEADING EDGE UPPER SKIN PANEL AT APPROXIMATELY WBL STA 821 TO STA 908 BETWEEN THE NR 3 AND NR 4 ENGINES WAS FOUND CRACKED. THE CRACK MEASURED 44 INCHES LONG IN THE CHORD WISE DIRECTION. CRACK WAS IN OUTER LAYER OF COMPOSI TE PANEL ONLY. INTERIM REPAIR ACCOMPLISHED, PERMANENT REPAIR TO BE ACCOMPLISHE D PRIOR TO PLANE TOTAL TIME 25845. 2 L 7 4 4F 4 F RT A20WE E24NE 1996102400594 19961024 00594 NM 1996 10 24 96UAL900784 1 19961008 A 3350 BULB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 536UA 25156 DOOR 4R EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY EXIT LIGHT, OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996102400595 19961024 00595 NE 1996 10 24 96UAL900785 2 19961008 A 7261 ENGINE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LEFT OIL LOSS A UALA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 781UA 26945 LEFT ENGINE OIL QUANTITY TO ZERO, OIL PRESSURE TO ZERO AND ENGINE SHUTDOWN. RETURN TO FIELD. 2 L 7 2 4F 4 F RT T0001SE E46NE 1996102400596 19961024 00596 NE 1996 10 24 96UAL900787 2 19961008 A 7260 50G631 BEARING BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 2 ENGINE GB FAILED A UALA A UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 WP 29 178UA 24385 724694 NR 2 ENGINE FLAME-OUT. *S/D* ANGLE GEARBOX AB-1 BEARING FAILED. ENGINE REPLACED. 2 L 7 4 4F 4 F RT A20WE E24NE 1996102400597 19961024 00597 NM 1996 10 24 96UAL900788 1 19961008 A 2820 69186127 ELBOW BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 FUEL TANK CRACKED A A UALA K NONE O OTHER CR CRUISE 1 WP 29 7287U 21565 CREW REPORTED, NR 1 FUEL TANK WENT 500 POUNDS LOWER THAN NR 3 TANK. BALANCED FUEL, BUT IMBALANCE OCCURRED AGAIN. *S/D* THE NR 1 FUEL TANK VENT ELBOW CRACKED. REPLACED THE VENT ELBOW. SEVERAL OCCURENCES OF THIS DISCREPANCY HAVE BEEN REP ORTED. FAILURE HAS BEEN ATTRIBUTED TO RESTRICTED VENT LINE MOVEMENT FROM LINE SUPPORT CLAMPS INSTALLED DURING MAINTENAN CE. A SPECIAL PROJECT TO CHECK ALL AFFECTED AIRCRAFT IS BEING ACCOMPLISHED. 2 L 7 3 4F 4 F A3WE E2EA 1996102400598 19961024 00598 NE 1996 10 24 96UAL900789 2 19961008 A 7261 O-RING BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE CUT A UALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 7453U 21907 696564 NR 2 ENGINE SHUT DOWN IN FLIGHT DUE TO EXCESSIVE OIL CONSUMPTION, 1 GALLON PER HOUR. *S/D* FOUND MAIN OIL SCREEN O-RIN G CUT. REPLACED O-RING AND RAN ENGINE FOR 5 MINUTES, NO LEAKS NOTED. 2 L 7 3 4F 4 F A3WE E2EA 1996102400599 19961024 00599 WP 1996 10 24 96UAL900790 1 19961008 A 2170 21D10011 COALESCER BAGS DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN DIRTY A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 WP 29 1828U 46627 OUT OF OIL SMELL IN CABIN DURING TAKEOFF AND CLIMB. *S/D* COULD NOT DUPLICATE ON GROUND. REPLACED COALESCER BAGS, NO REOCCURANCE. 2 L 7 3 4F 4 F A22WE E23EA 1996102400600 19961024 00600 WP 1996 10 24 96UAL900791 1 19961008 A 3350 POWER SUPPLY DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1817U 46616 MID AND AFT EMERGENCY ESCAPE LIGHT FAILED TO TEST. REPLACED FAILED POWER SUPPLY. 2 L 7 3 4F 4 F A22WE E23EA 1996102400601 19961024 00601 NM 1996 10 24 96UAL900792 1 19961008 A 3350 LIGHT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7289U 21567 AFT AIRSTAIR EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSEMBLY, OPERATIONAL CHECKS OK. 2 L 7 3 4F 4 F A3WE E2EA 1996102400602 19961024 00602 NM 1996 10 24 96UAL900793 1 19961008 A 4970 R631 RELAY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE APU FAILED A UALA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 WP 29 7271U 21418 FLIGHT CREW REPORTS WHEN APU SHUT DOWN, LIGHT REMAINS ON. APU PLACED ON INOPERATIVE STATUS. REPLACED APU LIGHT RELAY. SYSTEM TESTED OKAY. 2 L 7 3 4F 4 F A3WE E2EA 1996102400603 19961024 00603 NM 1996 10 24 96UAL900794 1 19961009 A 4920 6936161 SEAL BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE APU COMRESSOR WORN A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 7464U 21918 CREW REPORTED SMOKE AND ODOR IN CABIN. ISOLATED TO RIGHT AIR CONDITIONING PACK. *S/D* FOUND CARBON SEALS WORN. REPLA CED CARBON SEALS AND CLEANED COKE FROM APU. 2 L 7 3 4F 4 F A3WE E2EA 1996102400604 19961024 00604 NM 1996 10 24 96UAL900797 1 19961010 A 2913 PUMP BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE FAILED A UALA E ENGINE SHUTDOWN E VIBRATION/BUFFET CR CRUISE 1 WP 29 7945U 21899 696553 NR 1 ENGINE HIGH VIBRATION. ENGINE SHUT DOWN, LOUD NOISE FROM ENGINE DURING SHUTDOWN. COULD NOT DUPLICATE NOISE. TWO DAYS LATER IN DEN MECHANICS REPORTED NR 1 ENGINE NOISY WITH HYDRAULIC PUMP ON AND STOPS WITH PUMP OFF. REPLACED PUMP AN D RUN-UP WAS GOOD. 2 L 7 3 4F 4 F A3WE E2EA 1996102400605 19961024 00605 NM 1996 10 24 96UAL900798 1 19961010 A 7711 EPR INDICATION BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE ENGINE LOW A UALA O OTHER R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 29 7260U 21407 700137 UNABLE TO REACH TAKE OFF EPR, MAX WAS 2.1, DESIRED WAS 2.8, THROTTLES FULL ADVANCE. DID NOT EXCEED EGT LIMITS. *S/D* R AN ALL ENGINES AND ALL PARAMETERS WERE NORMAL. NO SUBSEQUENT COMMENTS. 2 L 7 3 4F 4 F A3WE E2EA 1996102400606 19961024 00606 WP 1996 10 24 96UAL900799 1 19961010 A 3350 BATTERY PACK DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1843U 46636 MID CABIN EMERGENCY LIGHT BATTERY FAILED TEST. REPLACED BATTERY PACK AND CHARGER, TESTS OK. 2 L 7 3 4F 4 F A22WE E23EA 1996102400607 19961024 00607 NM 1996 10 24 96UAL900800 1 19961011 A 2913 65066 PUMP BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE NR 4 HYD SYST LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 165UA 21658 LOST NR 4 HYDRAULIC SYSTEM FLUID. *S/D* FOUND HYDRAULIC FLUID LEAKED FROM ENGINE DRIVEN PUMP. REPLACED ENGINE DRIVEN PUMP, CASE DRAIN FILTER AND PRESSURE FILTER. 2 L 7 4 4F 4 F A20WE E20EA 1996102400608 19961024 00608 NM 1996 10 24 96UAL900801 1 19961011 A 7932 OIL QTY IND BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE MALFUNCTIONED A UALA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 WP 29 7264U 21411 NR 2 ENGINE OIL QUANTITY WENT TO ZERO, TEMPERATURE 130 AND CLIMBING, PRESSURE DOWN TO 41 PSI, ENGINE SHUT DOWN. *S/D* I NSPECTED INLET AND EXHAUST, CHECKED OIL QUANTITY AND MAIN OIL SCREEN. RAN ENGINE TO 1.65 EPR, NO DEFECTS FOUND. 2 L 7 3 4F 4 F A3WE E2EA 1996102400609 19961024 00609 NE 1996 10 24 96UAL900802 2 19961011 A 7530 56H156 STATOR VANE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 1 ENGINE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 768UA 5600 26919 FOUND NR 1 ENGINE 6TH STAGE HIGH PRESSURE COMPRESSOR VARIABLE STATOR VANE BEYOND CRACK LIMITS. ALSO, SUSPECT A CRACK AT THE TENTH VANE BELOW AP3 PORT. *S/D* REMOVED ENGINE AND REPLACED ALL HPC 6TH STAGE STATOR VANES. PROBLEM PREVIOUSLY DOCUMENTED. NEW VANE DESIGN IN PROCESS. 2 L 7 2 4F 4 F RT T0001SE E46NE 1996102400610 19961024 00610 NM 1996 10 24 96UAL900803 1 19961011 A 2131 CONTROLLER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN PRESS MALFUNCTIONED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 611UA 21872 THE CABIN PRESSURIZATION CONTROLLER FAILED. AIRCRAFT DESCENDED EARLY TO FL 240. WHEN TROUBLESHOOTING TO DETERMINE THE CAUSE OF THE CABIN PRESSURIZATION CONTROLLER FAILURE, BOTH AUTO PRESSURE CONTROLLERS WERE BITE TESTED AND THE OUTFLOW V ALVE WAS OPERATED. OPERATIONS CHECK NORMAL. NO FAULTS FOUND. THERE HAVE BEEN NO FURTHER DISCREPANCIES INDICATED. 2 L 7 2 4F 4 F RT A1NM E3NE 1996102400611 19961024 00611 NM 1996 10 24 SCNA96313 1 19961015 A 2611 PU90421S SMOKE DETECTOR BOEING 727 727259 138408J NM FWD LAV INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 FORWARD LAV SMOKE DETECTOR DID NOT TEST. REMOVED AND REPLACED SMOKE DETECTOR AND OPS CHECKED NORMAL. 2 L 7 3 4F A3WE 1996102400612 19961024 00612 WP 1996 10 24 SCNA96314 1 19961017 A 3040 9615046004 TEMP CONTROLLER DOUG DC10 DC1030F 3023504 WP RT WINDSHIELD FAILED A SCNA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 601GC 47921 RIGHT WINDSHIELD ANTI-ICE POPPED CIRCUIT BREAKER. THE SMELL OF SMOKE OCCURRED BREIFLY AND THEN DISSIPATED. SECURED WIN DOW ANTI-ICE. REMOVED AND REPLACED WINDSHIELD TEMPERATURE CONTROLLER. 2 L 7 3 4F RT A22WE 1996102400613 19961024 00613 WP 1996 10 24 SCNA96315 1 19961018 A 5270 H2024B SWITCH DOUG DC10 DC1010 3022110 WP NLG AVIONIC DOOR FAILED A SCNA A J UNSCHED LANDING DUMP FUEL P NO WARNING INDICATION CL CLIMB 1 GL 15 572SC 46977 UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF. ADJUSTED FUEL LEVEL TO MAXIMUM LANDING WEIGHT AND RETURNED TO LAS. FOUND NOSE WHEEL WELL AVIONICS DOOR OPEN AND DOOR WARNING SWITCH INOP. REMOVED AND REPLACED DOOR WARNING SWITCH. 2 L 7 3 4F A22WE 1996102400614 19961024 00614 NM 1996 10 24 SCNA96316 1 19961020 A 3350 900542 POWER SUPPLY BOEING 727 7272A1 138407F NM L2 DOOR INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 286SC 21601 FOUND L2 OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED THE POWER SUPPLY (P/N 9005-42), (S/N 19440) AND THE B ATTERY PACK (P/N 9008-3-5A), (S/N 10000), OPS CHECKED NORMAL. 2 L 7 3 4F A3WE 1996102400615 19961024 00615 WP 1996 10 24 RRXA96125 1 19961017 A 3260 GEAR HANDLE DOUG DC8 DC871F 302199D WP COCKPIT LACK OF LUBE A RRXA O OTHER P NO WARNING INDICATION AP APPROACH 1 WP 15 8177U 45983 NO GEAR DOWN GREEN OR RED WARNING LIGHTS. COMPLIED WITH QRH, GEAR CONFIRMED DOWN AND LOCKED. MAINTENANCE CLEANED AND L UBED THE LINKAGES ON THE LANDING GEAR HANDLE. LANDING GEAR POSITION INDICATION AND WARNING OPS CHK GOOD. 2 L 7 4 4F RT 4A25 1996102400616 19961024 00616 WP 1996 10 24 CKSA96162 1 19961018 A 2612 27775641 INSULATOR DOUG DC8 DC861F 3021953 WP PWA JT3D JT3D3B 52039 NE NR 3 FIRE LOOP OUT OF POSITION A CKSA K NONE N FALSE WARNING CR CRUISE 1 GL 23 813CK 45893 643333 IN FLIGHT, NR 3 FIRE WARNING WENT OFF. COMPLETED ALL APPROPRIATE CHECKLISTS, VISUALLY INSPECTED NR 3 ENGINE AND NO DEFE CTS NOTED. FOUND INSULATOR NR 3 ENGINE FIRE LOOP OUT OF PLACE. REINSTALLED INSULATOR PER DACO DC-8 MM 26-10-1. NR 3 E NGINE FIRE WARNING TESTS GOOD PER DACO DC-8 MM 26-10-0. 2 L 7 4 4F 4 F 4A25 1E8 1996102400617 19961024 00617 WP 1996 10 24 CKSA96163 1 19961021 A 2612 FIRE AMPLIFIER DOUG DC8 DC861 3021952 WP PWA JT3D JT3D3B 52039 NE NR 2 ENGINE MALFUNCTIONED A CKSA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. J WARNING INDICATION CR CRUISE 1 GL 23 817CK 45887 645251 NR 2 ENGINE SHUTDOWN AT 2345Z DUE TO FIRE WARNING. FIRE WARNING CAME ON THEN OFF, MONITORED ENGINE NORMAL. THEN GANG T ESTED FIRE LOOP, TEST FAILED. AT THAT TIME FIRE HANDLE LIGHT CAME ON, SO NR 1 AND NR 2 FIRE BOTTLE DISCHARGED. LIGHT R EMAINED ON AND NO TEST ON NR 2 FIRE LOOP. OIL PRESSURE ON WINDMILL 6 PSI. REMOVED AND INSTALLED NR 2 ENGINE FIRE BOTTL E IAW MM 26-3-0. REPLACED NR 1 FIRE BOTTLE, NR 2 FIRE CONTROL AMPLIFIER. PERFORMED ENGINE RUN-UP AT TAKEOFF POWER, OPS CHECK NORMAL. NO FIRE WARNING, GROUND CHECK OF FIRE WARNING SYSTEM NORMAL. FIRE BOTTLE (P/N 893244) (S/N 25957DG), FI RE BOTTLE (P/N 893244) (SN 25934DC), FIRE AMPLIFIER (P/N 377-115-22) (S/N EP4). 2 L 7 4 4F 4 F 4A25 1E8 1996102400618 19961024 00618 1996 10 24 HEEA968261 4 19961014 A 3421 5040017901 INDICATOR BOLKMS 105 BO105S 5626006 EU COCKPIT ATTITUDE INCORRECT TILT E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 INCORRECT TILT RECEIVED. S/N 1236 &4566 1 G 7 2 3U H3EU 1996102400619 19961024 00619 1996 10 24 HEEA968262 4 19961014 A 3421 5040017901 INDICATOR BOLKMS 105 BO105S 5626006 EU COCKPIT ATTITUDE INCORRECT TILT E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 INCORRECT TILT RECEIVED. 1 G 7 2 3U H3EU 1996102400620 19961024 00620 1996 10 24 HEEA968263 4 19961014 A 3413 RC30VIL INDICATOR BELL 412 412 1182202 SW RATE OF CLIMB ERROR E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 108X 33115 NEEDLE IS OFF 200 FEET. 1 G 7 2 4U H4SW 1996102400621 19961024 00621 SW 1996 10 24 HEEA968264 1 19961014 A 3040 204070907001 CONVERTER BELL 412 412 1182202 SW WIPER DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 22347 36005 WILL NOT STOW AND EXCESSIVE PLAY IN SHAFT. 1 G 7 2 4U H4SW 1996102400622 19961024 00622 NE 1996 10 24 HEEA968265 1 19961014 A 5321 7620402021041 FLOOR SKRSKY S76 S76A 8143006 NE LT OUTBRD MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 FLOOR DOES NOT HAVE PROPER JOGGLE ON INBOARD AND FORWARD EDGE OF PANEL AS NEEDED TO GO BELOW (-051) LARGE FLOOR. 1 G 7 2 3U H1NE 1996102400623 19961024 00623 EU 1996 10 24 HEEA968266 1 19961014 A 6240 10594575 TRANSMITTER BOLKMS 105 BO105S 5626006 EU MAST MOMENT FLUCTUATION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81832 S828 AFTER UNIT WARMS UP NEEDLE FLUCTUATES BETWEEN GREEN AND YELLOW ARCS. 1 G 7 2 3U H3EU 1996102400624 19961024 00624 EU 1996 10 24 HEEA968267 1 19961014 A 6240 10594564 INDICATOR BOLKMS 105 BO105S 5626006 EU MAST MOMENT FLUCTUATES E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81832 S828 AFTER UNIT WARMS UP NEEDLE FLUCTUATES BETWEEN GREEN AND YELLOW ARCS. SENT TO MASCO FOR INSPECTION AND REPAIR. 1 G 7 2 3U H3EU 1996102400625 19961024 00625 1996 10 24 HEEA968268 4 19961014 A 3416 5035P2P25 ALTIMETER BOLKMS 105 BO105S 5626006 EU COCKPIT ENCODER ERROR E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7170D S840 NEEDLE OFF 1500 FEET.TIME SINCE REPAIR 325:30. 1 G 7 2 3U H3EU 1996102400626 19961024 00626 1996 10 24 HEEA968269 4 19961014 A 3416 5035P2P42 ALTIMETER BELL 214 214ST 1182106 SW COCKPIT WATER CONTAM E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5748M 28102 WATER CONTAMINATION INSIDE INSTRUMENT. 2 G 7 2 4U H10SW 1996102400627 19961024 00627 SW 1996 10 24 HEEA968270 1 19961014 A 7712 206075739103 TORQUEMETER BELL 206 206L3 1182108 SW COCKPIT OUT OF SPECS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 INDICATES READING 2% HIGHER THAN MANUFACTURER'S SPECS. TIME SINCE REPAIR 0:00. 1 G 7 1 3U H2SW 1996102400628 19961024 00628 SW 1996 10 24 HEEA968271 1 19961014 A 2824 L88010491 VALVE BELL 212 212 1181420 SW FUEL SYS INTERMITTENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5010F 30936 INOPERATIVE, CYCLES INTERMITTENT. 1 G 7 1 4U H4SW 1996102400629 19961024 00629 EU 1996 10 24 HEEA968272 1 19961014 A 2844 BSE20660G1 TRANSMITTER BOLKMS 105 BO105S 5626006 EU FUEL PRESS DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911HM S683 NO VALID OUTPUT, #1 READS 0 PRESSURE. 1 G 7 2 3U H3EU 1996102400630 19961024 00630 1996 10 24 HEEA968273 4 19961014 A 2210 7660002113103 GYRO SKRSKY S76 S76A 8143006 NE COCKPIT VG DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1547D 760077 VG KICKS IN ROLL. 1 G 7 2 3U H1NE 1996102400631 19961024 00631 1996 10 24 HEEA968274 4 19961014 A 2210 7660002113103 GYRO SKRSKY S76 S76A 8143006 NE COCKPIT VG NR 2 DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 911MJ 760231 #2 ROLL KICKS. 1 G 7 2 3U H1NE 1996102400632 19961024 00632 NE 1996 10 24 HEEA968275 1 19961014 A 6720 7640003191051 CABLE ASSEMBLY SKRSKY S76 S76A 8143006 NE T/R CONTROL MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 1545X 760050 CABLE 1/2 INCH TOO SHORT WHEN MEASURED AGAINST OLD T/R CABLE. WHEN INSTALLED IN AIRCRAFT EXPOSED THREAD ON TURNBUCKLE O UT OF LIMITS WITH CORRECT CABLE TENSION. 1 G 7 2 3U H1NE 1996102400633 19961024 00633 EU 1996 10 24 HEEA968277 1 19961014 A 2422 2A10001G INVERTER BOLKMS 117 BK117A4 5626017 EU AC SYS DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911RZ 7092 INVERTER CAUSES STATIC ON THE #2 VHF AND VOR. 1 G 7 2 3U H13EU 1996102400634 19961024 00634 SW 1996 10 24 HEEA968278 1 19961014 A 2432 32007001 BATTERY MARATHON BELL 206 206L1 1182107 SW DC SYS FAILED E HEEA K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 03 5017G 45228 BATTERY HOT LIGHT. INSPECTED BY ACCESSORY SHOP AND FOUND BATTERY WILL NOT PASS CAPACITY AND WILL NOT EXCEPT A CHARGE. 1 G 7 1 3U H2SW 1996102400635 19961024 00635 SW 1996 10 24 HEEA968279 1 19961014 A 2432 32007001 BATTERY MARATHON BELL 206 206L3 1182108 SW DC SYS WEAK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6603X 51412 BATTRERY WEAK. INSPECTED BY THE ACCESSORY SHOP AND FOUND BATTERY WILL NOT PASS CAPACITY TEST. 1 G 7 1 3U H2SW 1996102400636 19961024 00636 SW 1996 10 24 HEEA968280 1 19961014 A 3212 206050248117 FLOAT BAG VALVE BELL 206 206L3 1182108 SW EMERG FLOAT UNBONDED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8590X 51494 FLOAT BAG ASSY DEFECTIVE DUE TO UNBONDED VALVE. 1 G 7 1 3U H2SW 1996102400637 19961024 00637 SW 1996 10 24 HEEA968281 1 19961014 A 7810 212061202009 DUCT ASSY BELL 212 212 1181420 SW LT EXH CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3208H 31304 DUCT ASSY CRACKED. 1 G 7 1 4U H4SW 1996102400638 19961024 00638 EU 1996 10 24 HEEA968282 1 19961014 A 2841 VT4261 GAUGE BOLKMS 105 BO105S 5626006 EU FUEL LEVEL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81832 S828 GAUGE NEEDLE ON SUPPLY SIDE WILL NOT GO TO ZERO. 1 G 7 2 3U H3EU 1996102400639 19961024 00639 EU 1996 10 24 HEEA968284 1 19961014 A 7722 10590947 INDICATOR BOLKMS 105 BO105S 5626006 EU COCKPIT TOT READS LOW E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911FL S717 INDICATOR READS LOW AND WILL NOT CALIBRATE. 1 G 7 2 3U H3EU 1996102400640 19961024 00640 SW 1996 10 24 HEEA968285 1 19961014 A 7931 APTE138100G TRANSMITTER BELL 412 412 1182202 SW OIL PRESSURE DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7128R 46 36007 PRESSURE READS HIGH. 1 G 7 2 4U H4SW 1996102400641 19961024 00641 SW 1996 10 24 HEEA968286 1 19961014 A 2822 2C273 CARTRIDGE BELL 412 412 1182202 SW FUEL XSFER PUMP DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3893N 33010 FUEL TRANSFER PUMP WILL NOT TRANSFER FUEL TO MAIN TANK IN FLIGHT. YOU CAN HEAR PUMP RUN, BUT IT DOESN'T TRANSFER. 1 G 7 2 4U H4SW 1996102400642 19961024 00642 SW 1996 10 24 HEEA968287 1 19961014 A 6730 206076031023 SERVO BELL 206 206B 1181511 SW M/R DEFECTIVE E HEEA K NONE F FLT CONT AFFECTED NR NOT REPORTED 1 SW 03 2272J 3620 SERVO DEFECTIVE. PILOT INPUT VERY HIGH. 1 G 7 1 3U H2SW 1996102400643 19961024 00643 EU 1996 10 24 HEEA968288 1 19961014 A 2842 VT044 TRANSMITTER BOLKMS 105 BO105S 5626006 EU FUEL QTY FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 9190Y S669 STICKS AT BOTTOM OF PROBE AND FLANGE WARPED. SENT TO FIVE STAR TECHNOLOGIES, INC. FOR INSPECTION AND REPAIR. 1 G 7 2 3U H3EU 1996102400644 19961024 00644 SW 1996 10 24 HEEA968289 1 19961014 A 6220 204010937009 DAMPER ASSY BELL 212 212 1181420 SW M/R LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 27805 31106 DAMPER LEAKING FLUID AND CAN'T SEE PIN. 1 G 7 1 4U H4SW 1996102400645 19961024 00645 1996 10 24 HEEA968290 4 19961014 A 2210 2593996333 TARSYN BELL 212 212 1181420 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 27805 31106 DG PRECESSES EXCESSIVELY. 1 G 7 1 4U H4SW 1996102400646 19961024 00646 1996 10 24 HEEA968291 4 19961014 A 3444 7001840913 TRANSCEIVER SKRSKY S76 S76A 8143006 NE COCKPIT FAIL TEST E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 4253S 760035 UNIT FAILED ALTITUDE OUTPUT TEST 5.5 ON SST. 1 G 7 2 3U H1NE 1996102400647 19961024 00647 SW 1996 10 24 HEEA968292 1 19961014 A 6330 206033506101 RESTRAINT BELL 206 206L3 1182108 SW XMSN BEARING UNSTAKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6251X 51552 RESTRAINT BEARING UNSTAKED. 1 G 7 1 3U H2SW 1996102400648 19961024 00648 SW 1996 10 24 HEEA968293 1 19961014 A 6330 206033506101 RESTRAINT BELL 206 206L3 1182108 SW XMSN BEARING WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 21497 51518 BEARING WORN. SENT TO LORD MANUFACTURING FOR EXCHANGE. 1 G 7 1 3U H2SW 1996102400649 19961024 00649 SW 1996 10 24 HEEA968294 1 19961014 A 6330 206033506101 RESTRAINT BELL 206 206L3 1182108 SW XMSN BEARING WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31077 51520 RESTRAINT BEARING WORN. 1 G 7 1 3U H2SW 1996102400650 19961024 00650 EU 1996 10 24 HEEA968295 1 19961014 A 2436 51530001EI REGULATOR BOLKMS 117 BK117B1 5626012 EU NR 2 GENERATOR DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 217UC 7152 #2 GENERATOR WILL NOT COME ON LINE. 1 G 7 2 3U H13EU 1996102400651 19961024 00651 1996 10 24 HEEA968296 4 19961014 A 3421 206075607103 GYRO BELL 206 206L3 1182108 SW COCKPIT ATTITUDE DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 GYRO SLOW IN PTICH. 1 G 7 1 3U H2SW 1996102400652 19961024 00652 EU 1996 10 24 HEEA968297 1 19961014 A 7714 1179405603 INDICATOR BOLKMS 117 BK117A3 5626015 EU ENG N1 READS HIGH E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911NC 7026 INDICATES HIGH OUT OF TOLERANCE AT 100%. STICKS ON START. 1 G 7 2 3U H13EU 1996102400653 19961024 00653 SW 1996 10 24 HEEA968298 1 19961014 A 7722 206375007103 INDICATOR BELL 206 206L3 1182108 SW COCKPIT TOT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 206FS 51506 NO TOT INDICATIONS. 1 G 7 1 3U H2SW 1996102400654 19961024 00654 1996 10 24 HEEA968299 4 19961014 A 3416 212070238003 ALTIMETER BELL 412 412 1182202 SW COCKPIT FRICTION ERROR E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z 36019 EXCESSIVE FRICTION ERROR. 1 G 7 2 4U H4SW 1996102400655 19961024 00655 1996 10 24 HEEA968300 4 19961014 A 3421 1113034 INDICATOR SKRSKY S76 S76A 8143006 NE COCKPIT ATTITUDE DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22342 760096 VERTICAL BAR DOES NOT CENTER. 1 G 7 2 3U H1NE 1996102400656 19961024 00656 EU 1996 10 24 HEEA968301 1 19961014 A 6340 KDWO21A RPM WARN BOX BOLKMS 105 BO105S 5626006 EU M/R FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 135AE S838 WARNING HORN AND LIGHT WOULD COME ON IN LEVEL FLIGHT. 1 G 7 2 3U H3EU 1996102400657 19961024 00657 SW 1996 10 24 HEEA968302 1 19961014 A 7810 212061201011 EJECTOR ASSY BELL 212 212 1181420 SW LT EXH CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3208H 31304 EXCESSIVE CRACKING. SENT TO ALPINE AEROTECH LTD. FOR INSPECTION AND REPAIR. 1 G 7 1 4U H4SW 1996102400658 19961024 00658 1996 10 24 HEEA968303 4 19961014 A 3421 1113034 INDICATOR BELL 212 212 1181420 SW COCKPIT FLAG STICKS E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3208H 31304 INDICATOR GS FLAG STICKING. 1 G 7 1 4U H4SW 1996102400659 19961024 00659 1996 10 24 HEEA968304 4 19961014 A 3421 1113034 INDICATOR BELL 212 212 1181420 SW COCKPIT SPHERE STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3208H 31304 INDICATOR SPHERE STICKS IN PITCH. 1 G 7 1 4U H4SW 1996102400660 19961024 00660 1996 10 24 HEEA968305 4 19961014 A 3421 1113025 INDICATOR BELL 212 212 1181420 SW COCKPIT HSI FLAG STICKS E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3208H 31304 HSI OFF FLAG STICKS. 1 G 7 1 4U H4SW 1996102400661 19961024 00661 1996 10 24 HEEA968309 4 19961014 A 3416 A30 ENCODER ACK BELL 206 206L1 1182107 SW ALTIMETER DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 21240 45647 ENCODER CAN'T CALIBRATE AND UPGRADE TO MOD 3 STATUS. 1 G 7 1 3U H2SW 1996102400662 19961024 00662 1996 10 24 HEEA968310 4 19961014 A 3413 1003840541 INDICATOR BEECH 200 200CBEECH 1152926 CE COCKPIT VSI STICKS E HEEA K NONE O OTHER CL CLIMB 1 SW 03 39PH BL3 VSI STICKS IN CLIMB AND DESCENT. 1 L 7 2 4T A24CE 1996102400663 19961024 00663 NE 1996 10 24 HEEA968311 1 19961014 A 7931 7645001078101 INDICATOR SKRSKY S76 S76A 8143006 NE ENG OIL STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 PRESSURE INDICATOR STICKS 1 G 7 2 3U H1NE 1996102400664 19961024 00664 SW 1996 10 24 HEEA968312 1 19961014 A 7810 212061201012 EJECTOR ASSY BELL 212 212 1181420 SW RT EXH CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3131S 30953 EJECTOR CRACKED ON INSIDE SKIN BEYOND REPAIR. 1 G 7 1 4U H4SW 1996102400665 19961024 00665 CE 1996 10 24 HEEA968313 1 19961014 A 7722 9038402611 INDICATOR BEECH 200 200CBEECH 1152926 CE COCKPIT TOT STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 500PH BL29 INDICATOR STICKS AT 600 DEGREES. 1 L 7 2 4T A24CE 1996102400666 19961024 00666 CE 1996 10 24 HEEA968314 1 19961014 A 7700 9038402611 INDICATOR BEECH 200 200CBEECH 1152926 CE COCKPIT READS HIGH E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 500PH BL29 INDICATOR READS HIGH; CANNOT ADJUST. 1 L 7 2 4T A24CE 1996102400667 19961024 00667 SW 1996 10 24 HEEA968315 1 19961014 A 2840 206063656001 TRANSMITTER BELL 206 206L1 1182107 SW FUEL SYS FLUCTUATES E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5019G 45247 FLUCTUATES THROUGHOUT RANGE. 1 G 7 1 3U H2SW 1996102400668 19961024 00668 EU 1996 10 24 HEEA968316 1 19961014 A 2844 BSE20660G1 TRANSMITTER BOLKMS 105 BO105S 5626006 EU FUEL PRESS FLUCTUATES E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 54191 S804 FLUCTUATING OUTPUT WHEN UNIT IS VIBRATED. 1 G 7 2 3U H3EU 1996102400669 19961024 00669 EU 1996 10 24 HEEA968317 1 19961014 A 7921 3701020000 COOLER BOLKMS 105 BO105S 5626006 EU OIL SYS CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7170D S840 OIL COOLER CRACKED IN NUMEROUS LOCATIONS. SENT TO DRAKE AIR FOR INSPECTION AND REPAIR. 1 G 7 2 3U H3EU 1996102400670 19961024 00670 EU 1996 10 24 HEEA968318 1 19961014 A 7921 37010200004 OIL COOLER BOLKMS 105 BO105S 5626006 EU OIL SYS CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7170D S840 COOLER CRACKED AT TOP. ELONGATED MOUNTING HOLES AND CORROSION. 1 G 7 2 3U H3EU 1996102400671 19961024 00671 EU 1996 10 24 HEEA968319 1 19961014 A 7923 209072433101 VALVE BOLKMS 105 BO105S 5626006 EU OIL SYS STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911HM S683 VALVE STICKING AND CORRODED SOLENOID. 1 G 7 2 3U H3EU 1996102400672 19961024 00672 EU 1996 10 24 HEEA968320 1 19961014 A 2842 VT044 TRANSMITTER BOLKMS 105 BO105S 5626006 EU FUEL QTY FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 86CH S557 TRANSMITTER UNRELIABLE. 1 G 7 2 3U H3EU 1996102400673 19961024 00673 SW 1996 10 24 HEEA968321 1 19961014 A 5520 206023119159 ELEVATOR ASY BELL 206 206L1 1182107 SW RT ELEV CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5745N 45489 ELEV ASSY CORRODED BEYOND LIMITS. 1 G 7 1 3U H2SW 1996102400674 19961024 00674 SW 1996 10 24 HEEA968322 1 19961014 A 5521 206023119159 ELEVATOR ASY BELL 206 206L1 1182107 SW RT ELEV SEPARATED SPAR E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5019F 45244 SEPARATED BEYOND LIMITS. REPLACE SPAR. 1 G 7 1 3U H2SW 1996102400675 19961024 00675 SW 1996 10 24 HEEA968323 1 19961014 A 5520 206023119157 ELEVATOR ASY BELL 206 206L1 1182107 SW LT ELEV CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5745N 45489 ELEV ASSY CORRODED BEYOND LIMITS. 1 G 7 1 3U H2SW 1996102400676 19961024 00676 SW 1996 10 24 HEEA968324 1 19961014 A 5521 206023119157 SPAR BELL 206 206L1 1182107 SW LT ELEV CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5019F 45244 ELEV ASSY CORRODED BEYOND LIMITS. PITTED THROUGH. REPLACE SPAR. 1 G 7 1 3U H2SW 1996102400677 19961024 00677 SW 1996 10 24 HEEA968325 1 19961014 A 5520 206023119157 ELEVATOR ASY BELL 206 206L1 1182107 SW LT ELEV CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2133X 45634 ELEV CRACKED AT PIVOT HOLES. 1 G 7 1 3U H2SW 1996102400678 19961024 00678 SW 1996 10 24 HEEA968326 1 19961014 A 5521 206023119159 SPAR BELL 206 206L1 1182107 SW RT ELEV CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2133X 45634 ELEV SPAR CORRODED. 1 G 7 1 3U H2SW 1996102400679 19961024 00679 EU 1996 10 24 HEEA968327 1 19961014 A 7722 TM42739 INDICATOR BOLKMS 105 BO105S 5626006 EU EXH TEMP READS HIGH E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 9190Y S669 READS HIGH AND EXCESSIVE FRICTION ERROR. 1 G 7 2 3U H3EU 1996102400680 19961024 00680 SW 1996 10 24 HEEA968328 1 19961014 A 2844 124044 INDICATOR BELL 412 412 1182202 SW FUEL PRESS READS HIGH E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2258F 33073 READS HIGH ON LOW END AND LOW ON HIGH END OF SCALE. 1 G 7 2 4U H4SW 1996102400681 19961024 00681 SW 1996 10 24 HEEA968329 1 19961014 A 6240 206076373001 TACH GENERATOR BELL 206 206L3 1182108 SW RPM WARN DEFECTIVE E HEEA K NONE J WARNING INDICATION NR NOT REPORTED 1 SW 03 6603X 51412 RPM WARNING HORN COMES ON ALL THE TIME. 1 G 7 1 3U H2SW 1996102400682 19961024 00682 SW 1996 10 24 HEEA968330 1 19961014 A 6240 206076373001 TACH GENERATOR BELL 206 206L1 1182107 SW OIL PUMP SHAFT STUCK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3905B 45598 SHAFT STUCK ON OIL PUMP. SHAFT SPLINES BAD. 1 G 7 1 3U H2SW 1996102400683 19961024 00683 1996 10 24 HEEA968331 4 19961014 A 3414 212070122011 INDICATOR BELL 212 212 1181420 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3208H 31304 RED LINE AT 130 KNOTS. 1 G 7 1 4U H4SW 1996102400684 19961024 00684 1996 10 24 HEEA968332 4 19961014 A 3421 102005901 INDICATOR BELL 206 206L3 1182108 SW COCKPIT SLOW ERECT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8589X 51487 ATTITUDE SLOW ERECTION. SLOW ON ROLL ERECTION RATES. 1 G 7 1 3U H2SW 1996102400685 19961024 00685 1996 10 24 HEEA968333 4 19961014 A 3421 7660002113103 GYRO SKRSKY S76 S76A 8143006 NE PILOT ATTITUDE PRECESSING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5435V 760158 PILOT'S ATTITUDE INDICATOR PRESSING. 1 G 7 2 3U H1NE 1996102400686 19961024 00686 1996 10 24 HEEA968334 4 19961014 A 2211 4025008918 COMPUTER BELL 412 412 1182202 SW AFCS DEFECTIVE E HEEA K NONE F FLT CONT AFFECTED NR NOT REPORTED 1 SW 03 108X 33115 IN ATT MODE NO. 1 ROLL CHANNEL INTERMITTENTLY SATURATES FULL LEFT CAUSING NO. 2 ROLL TO CORRECT RIGHT. 1 G 7 2 4U H4SW 1996102400687 19961024 00687 SW 1996 10 24 HEEA968335 1 19961014 A 3040 204070907001 CONVERTER BELL 412 412 1182202 SW WIPER FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D 33076 MOTOR SPINS BUT DOES NOT DRIVE CONNECTOR. 1 G 7 2 4U H4SW 1996102400688 19961024 00688 1996 10 24 HEEA968337 4 19961014 A 3416 5934D1 ALTIMETER BELL 206 206L3 1182108 SW COCKPIT LEAKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8591X 51495 ALTIMETER LEAKS AT BAROMETRIC KNOB. 1 G 7 1 3U H2SW 1996102400689 19961024 00689 EU 1996 10 24 HEEA968338 1 19961014 A 7722 TM42739 INDICATOR BOLKMS 105 BO105S 5626006 EU EXH TEMP STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 50293 S677 INDICATOR NEEDLE INDICATES HIGH IN UPPER RANGE AND INTERMITTENTLY STICKS. 1 G 7 2 3U H3EU 1996102400690 19961024 00690 EU 1996 10 24 HEEA968339 1 19961014 A 7722 TM42739 INDICATOR BOLKMS 105 BO105S 5626006 EU EXH TEMP READS HIGH E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7170D S840 LOW END READS HIGH AND HIGH END READS LOW. 1 G 7 2 3U H3EU 1996102400691 19961024 00691 EU 1996 10 24 HEEA968340 1 19961014 A 7722 TM42739 INDICATOR BOLKMS 105 BO105S 5626006 EU EXH TEMP FRICTION ERROR E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911FL S717 NEEDLE HAS EXCESSIVE FRICTION ERROR. SENT TO MASCO FOR INSPECTION AND REPAIR. 1 G 7 2 3U H3EU 1996102400692 19961024 00692 1996 10 24 HEEA968341 4 19961014 A 3416 A30 ENCODER ACK BELL 206 206B3 1181506 SW ALTIMETER DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2268A 3602 ENCODER UNIT REPORTS 25,000 WITH NO PRESSURE APPLIED AND WILL NOT CALIBRATE. 1 G 7 1 3U H2SW 1996102400693 19961024 00693 1996 10 24 HEEA968342 4 19961014 A 3416 A30 ENCODER ACK BELL 206 206L1 1182107 SW ALTIMETER DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2764F 45279 ENCODER UNIT HAS AN INCONSISTANT OUTPUT. 1 G 7 1 3U H2SW 1996102400694 19961024 00694 1996 10 24 HEEA968343 4 19961014 A 3416 A30 ENCODER ACK BELL 206 206L1 1182107 SW ALTIMETER FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2770Y 45291 ENCODER NO OUTPUT. 1 G 7 1 3U H2SW 1996102400695 19961024 00695 EU 1996 10 24 HEEA968344 1 19961014 A 7722 TM42739 INDICATOR BOLKMS 105 BO105S 5626006 EU EXH TEMP DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7170D S840 INDICATOR NOT LINEAR ERRATIC AND EXCESSIVE FRICTION ERROR. 1 G 7 2 3U H3EU 1996102400696 19961024 00696 1996 10 24 HEEA968345 4 19961014 A 3424 214075244001 RATE GYRO BELL 412 412 1182202 SW C0CKPIT DEFECTIVE E HEEA K NONE I FLT. ATTITUDE INST. NR NOT REPORTED 1 SW 03 7128R 36007 RATE GYRO INDICATING 15 DEGREES LEFT TURN IN STRAIGHT LEVEL FLIGHT. 1 G 7 2 4U H4SW 1996102400697 19961024 00697 1996 10 24 HEEA968346 4 19961014 A 3421 1113034 INDICATOR BELL 412 412 1182202 SW COCKPIT BALL STICKS E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 33008 36004 INDICATOR BALL STICKS IN PITCH AND ROLL. 1 G 7 2 4U H4SW 1996102400698 19961024 00698 1996 10 24 HEEA968347 4 19961014 A 3421 1113034 INDICATOR BELL 214 214ST 1182106 SW COCKPIT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 8045T 28101 INDICATOR INTERMITTENTLY RATCHETS RIGHT 360 DEGREES IN ROLL AXIS AFTER ABOUT AN HOUR OF OPERATION. 2 G 7 2 4U H10SW 1996102400699 19961024 00699 EU 1996 10 24 HEEA968348 1 19961014 A 2841 90321003 INDICATOR BOLKMS 105 BO105S 5626006 EU FUEL QTY ERROR E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 721MB S752 INDICATOR MAIN SIDE HAS EXCESSIVE FRICTION ERROR. SUPPLY SIDE IS HIGH OUT OF TOLERANCE. 1 G 7 2 3U H3EU 1996102400700 19961024 00700 SW 1996 10 24 HEEA968349 1 19961014 A 2844 BSE20630G TRANSDUCER BELL 206 206L3 1182108 SW FUEL PRESSURE OUT OF TOL E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6251X 51552 TRANSDUCER UNIT TRANSMITS LOW OUT OF TOLERANCE. 1 G 7 1 3U H2SW 1996102400701 19961024 00701 1996 10 24 HEEA968350 4 19961014 A 2340 AMS44 AUDIO CONTROL BELL 206 206L3 1182108 SW COCKPIT MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 92MT 51175 ICS HOT WHEN VOX CONTROL IN PTT POSITION. 1 G 7 1 3U H2SW 1996102400702 19961024 00702 EU 1996 10 24 HEEA968351 1 19961014 A 6240 117945641 INDICATOR BOLKMS 117 BK117B1 5626012 EU MAST MOMENT ERRATIC E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 217UC 7152 INDICATOR NEEDLE HAS AN ERRATIC INDICATION. 1 G 7 2 3U H13EU 1996102400703 19961024 00703 EU 1996 10 24 HEEA968352 1 19961014 A 6240 10594575 TRANSMITTER BOLKMS 117 BK117B1 5626012 EU MAST MOMENT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 217UC 7152 MAST MOMENT NEEDLE HAS AN ERRATIC INDICATION. 1 G 7 2 3U H13EU 1996102400704 19961024 00704 EU 1996 10 24 HEEA968353 1 19961014 A 6240 10594575 TRANSMITTER BOLKMS 105 BO105S 5626006 EU MAST MOMENT DEFECTIVE E HEEA K NONE N FALSE WARNING NR NOT REPORTED 1 SW 03 54197 S805 MAST MOMENT RED LIGHT INTERMITTENTLY COMES ON IN GREEN AREA. 1 G 7 2 3U H3EU 1996102400705 19961024 00705 EU 1996 10 24 HEEA968354 1 19961014 A 6240 10594564 INDICATOR BOLKMS 105 BO105S 5626006 EU MAST MOMENT FAILED E HEEA K NONE N FALSE WARNING NR NOT REPORTED 1 SW 03 54197 S805 MAST MOMENT LIGHT COMES ON AT ANY TIME WITHOUT THE NEEDLE LEAVING THE GREEN ARC. 1 G 7 2 3U H3EU 1996102400706 19961024 00706 SW 1996 10 24 HEEA968355 1 19961014 A 7714 206070266009 INDICATOR BELL 206 206B 1181511 SW COCKPIT DEFECTIVE E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 2753F 2729 INDICATOR FACE IS ROTATED 45 DEGREES FROM VERTICAL. 1 G 7 1 3U H2SW 1996102400707 19961024 00707 SW 1996 10 24 HEEA968356 1 19961014 A 7714 206070265101 INDICATOR BELL 206 206L1 1182107 SW DUAL TACH NEEDLE STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 50182 45242 TURBINE NEEDLE STICKS AT 33%. 1 G 7 1 3U H2SW 1996102400708 19961024 00708 SW 1996 10 24 HEEA968357 1 19961014 A 6240 206075681105 INDICATOR BELL 206 206L3 1182108 SW DUAL TACH FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 205FC 51130 ROTOR NEEDLE HAS NO INDICATION. 1 G 7 1 3U H2SW 1996102400709 19961024 00709 EU 1996 10 24 HEEA968358 1 19961014 A 7334 BSE206150G3 TRANSDUCER BOLKMS 105 BO105S 5626006 EU FUEL PRESS DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911PF S718 AT 30 PSI VOLTAGE DROPS TO ZERO INTERMITTENTLY. 1 G 7 2 3U H3EU 1996102400710 19961024 00710 EU 1996 10 24 HEEA968359 1 19961014 A 7930 6607190A SWITCH BOLKMS 105 BO105S 5626006 EU OIL PRESS DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6607K S841 PRESS LIGHT DOES NOT COME ON. 1 G 7 2 3U H3EU 1996102400711 19961024 00711 1996 10 24 HEEA968360 4 19961014 A 2210 574074101015 MODULE ASSY BELL 212 212 1181420 SW AUTO PILOT AFCS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3208H 31304 NO PITCH COMMANDS FROM AUTOPILOT THUMBWHEEL STEP #22 OF AFCS CHECK. 1 G 7 1 4U H4SW 1996102400712 19961024 00712 SW 1996 10 24 HEEA968361 1 19961014 A 6730 212076004005 SERVO ACTUATOR BELL 212 212 1181420 SW M/R LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 3208H 31304 SERVO STARTED LEAKING AT THE FIRST PRESSURE TEST AFTER INSTALLATION. 1 G 7 1 4U H4SW 1996102400713 19961024 00713 1996 10 24 HEEA968362 4 19961015 A 3422 200DC GYRO COMPASS BOLKMS 105 BO105S 5626006 EU COCKPIT PRECESSES E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 724MB S756 GYRO COMPASS EXCESSIVE PRECESSION. 1 G 7 2 3U H3EU 1996102400714 19961024 00714 CE 1996 10 24 HEEA968363 1 19961015 A 6120 213446 ROD END ASSY WOODWARD BEECH 200 200CBEECH 1152926 CE GOV BINDING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 30PH BB635 ROD END IS BINDING. 1 L 7 2 4T A24CE 1996102400715 19961024 00715 1996 10 24 HEEA968364 4 19961015 A 3460 5205160 INDICATOR BELL 212 212 1181420 SW COCKPIT CSI FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3208H 31304 METER MOVEMENT BAD. SENT TO LITTON SYSTEMS FOR INSPECTION AND REPAIR. 1 G 7 1 4U H4SW 1996102400716 19961024 00716 1996 10 24 HEEA968365 4 19961015 A 3454 066306000 INDICATOR KNI582 SNIAS 350 AS350B2 8680813 EU COCKPIT RMI LIGHTS INOP E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4036H 2919 RMI INTERNAL LIGHTS INOPERATIVE. 1 G 7 1 3U H9EU 1996102400717 19961024 00717 1996 10 24 HEEA968366 4 19961015 A 2312 064102300 TRANSCIEVER BELL 412 412 1182202 SW COCKPIT VHF FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22347 36005 TRANSCEIVER UNUSABLE AFTER 3 MILES - SQUELCH IS INTERMITTENT. UNIT WAS SENT TO ALLIED SIGNAL ON 7-23-96 FOR UNIT BECOMI NG DISTORTED AND BAD RECEIVER SQUELCH AFTER WARM UP. UNIT REPAIRED BY ALLIED SIGNAL ON 8-16-96 AND IS BACK IN SHOP 9-6- 96 FOR SQUELCH PROBLEMS. 1 G 7 2 4U H4SW 1996102400718 19961024 00718 EU 1996 10 24 HEEA968367 1 19961015 A 6520 350A33020005 GEAR BOX ASSY AEROSP AS355 AS355F1 8680810 EU T/R GR BOX DAMAGED E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 T/R GR BOX RECEIVED DAMAGED. UPON INSTALLING GEARBOX, NOTICED INPUT FLANGE WAS NOT LINING UP AS IT SHOULD. ON CLOSER I NSPECTION FOUND ONE OF 3 EARS OF FLANGE BENT BACK APPROXIMATELY 3/32". INSPECTED SHIPPING BOX AND FOUND INADEQUATE CLEA RANCE OR PACKING BETWEEN INPUT FLANGE AND BOX. ALSO FOUND DAMAGE TO BOX IN AREA WHERE FLANGE WAS LOCATED, INDICATING IT HAS BEEN IMPACTED. 1 G 7 2 3U H11EU 1996102400719 19961024 00719 EU 1996 10 24 HEEA968368 1 19961015 A 6320 0750111091 INPUT SEAL 4638001010 BOLKMS 105 BO105S 5626006 EU M/R GR BOX LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 133AE 304 1173 S800 SEAL LEAKING. REPLACED SEAL WITH NEW PART. 1 G 7 2 3U H3EU 1996102400720 19961024 00720 1996 10 24 HEEA968369 4 19961015 A 3455 066107700 RECEIVER BELL 412 412 1182202 SW COCKPIT ADF INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 107X 33113 RECEIVER INTERMITTENLY INOPERATIVE. PERFORMED PRELIMINARY INSPECTION. REPLACED I.C.'S I323, I324, CAPACITOR C380, DIODE CR315 AND RESISTOR R424. REPLACED CORRODED FRONT CONNECTOR J8061 AND BROKEN SPACER PLATE. BENCH CHECK GOOD. 1 G 7 2 4U H4SW 1996102400721 19961024 00721 1996 10 24 HEEA968370 4 19961015 A 2370 9806019001 CVR BELL 214 214ST 1182106 SW COCKPIT WONT TEST E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 3897N 28106 CVR DOES NOT TEST. 2 G 7 2 4U H10SW 1996102400722 19961024 00722 1996 10 24 HEEA968371 4 19961015 A 3444 066304400 ALTIMETER SKRSKY S76 S76A 8143006 NE RADAR ALT NEEDLE STICKS E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 31219 760230 RADAR ALTIMETER NEEDLE STICKS AROUND 45 FEET. DH LIGHT INOPERATIVE. NEEDLE FLUCTUATES INTERMITTENTLY. 1 G 7 2 3U H1NE 1996102400723 19961024 00723 1996 10 24 HEEA968372 4 19961015 A 3452 066106200 TRANSPONDER KT76 BELL 206 206L1 1182107 SW COCKPIT ATC FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2764F 45279 TRANSPONDER WILL NOT REPORT. CHECKED VOLTAGE, SWAPPED HALVES OF UNIT WITH A GOOD UNIT. VERIFIED PROBLEM ON LOCAL OSCILL ATOR HALF OF UNIT. REPLACED V101 AND DID NOT HELP. SWAPPED MIXER DIODE. ALSO NO HELP. 1 G 7 1 3U H2SW 1996102400724 19961024 00724 1996 10 24 HEEA968373 4 19961015 A 3454 066107800 RECEIVER BELL 212 212 1181420 SW COCKPIT NAV DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3208H 31304 NAV RECEIVER CAUSES RMI TO BE 30 DEGREE ERROR. 1 G 7 1 4U H4SW 1996102400725 19961024 00725 1996 10 24 HEEA968374 4 19961015 A 3453 25410036 7000 RCU BELL 412 412 1182202 SW COCKPIT LORAN FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 2261D 33076 LORAN WILL NOT MAINTAIN STATIONS. 1 G 7 2 4U H4SW 1996102400726 19961024 00726 SW 1996 10 24 HEEA968375 1 19961015 A 6220 412010182101 BEARING BELL 412 412 1182202 SW M/R EXCESS WEAR E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 23023 124 33080 EXCESSIVE WEAR ON OUTBOARD BEARING FACE. INSTALLED SERVICEABLE BEARING. CHECK FOR PROPER FIT AND CORRECT TORQUE. 1 G 7 2 4U H4SW 1996102400727 19961024 00727 1996 10 24 HEEA968376 4 19961015 A 2370 9806019001 CVR BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893P 33012 CVR NO TEST LIGHT WHEN SWITCH TO PILOT OR COPILOT TEST POSITION, GARBLED NOISE AND SQUEAL OVERHEAD SET IN TEST POSITION, AND NO LIGHT AFTER 10 MINUTES WITHOUT AIRCRAFT RUNNING. 1 G 7 2 4U H4SW 1996102400728 19961024 00728 1996 10 24 HEEA968377 4 19961015 A 3460 5205160006 INDICATOR BELL 212 212 1181420 SW COCKPIT CSI METER INOP E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5736J 31140 GLIDE SCOPE METER INOPERATIVE. 1 G 7 1 4U H4SW 1996102400729 19961024 00729 GL 1996 10 24 HEEA968378 2 19961017 A 7250 68777361 LAB SEAL 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL POWER SECT EXCESS RUNOUT E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 7136J CAT22850 S830 CAE836416 RECEIVING INSPECTION REVEALED: EXCESSIVE RUNOUT ON LAB SEAL BORE. TIR .006 INSTALLED AND NOT INSTALLED IN SUPPORT. INS TALLED A NEW LAB SEAL. 1 G 7 2 3U 3 U H3EU E4CE 1996102400730 19961024 00730 GL 1996 10 24 HEEA968383 2 19961018 A 7260 6896437 GEARSHAFT 6894171 BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL ENGINE SPALLED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2268X 98 CAG33143 3607 CAE821999F ENGINE REMOVED DUE TO AFT T/M LEAK. UPON INSPECTION OF GEARBOX PARTS NOTED: SPALLING ON F/C AND O/P GEAR GEARTEETH. IN STALLED A SERVICEABLE F/C & O/P GEAR. 1 G 7 1 3U 3 U H2SW E4CE 1996102400731 19961024 00731 GL 1996 10 24 HEEA968384 2 19961018 A 7260 6876925 TUBE ASSY. 6894171 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENGINE GR BOX OUT OF LIMIT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4294R 2941 CAG23108 S860 CAE836414 ENGINE REMOVED DUE TO PTO GEARSHAFT SHEARED FROM ENGINE TO TRANSMISSION. UPON INSPECTION OF GEARBOX PARTS NOTED: TUBE ASSEMBLY FAILED DIMENSIONAL CHECK PER CEB1307. INSTALLED A NEW TUBE ASSEMBLY. 1 G 7 2 3U 3 U H3EU E4CE 1996102400732 19961024 00732 1996 10 24 HEEA968385 4 19961018 A 2211 4033089901 COMPUTER FZ702 BELL 412 412 1182202 SW AUTO FLT INOP E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 FZ702 COMPUTER INOPERATIVE - ALL MODES. 1 G 7 2 4U H4SW 1996102400733 19961024 00733 GL 1996 10 24 HEEA968386 2 19961018 A 7250 6895010 GP SUPPORT 6898735 BELL 206 206B3 1181506 SW ALLSN 250C 250C20B 03013 GL NR 8 BEARING DEFECTIVE E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 104PH CAT25180 3622 CAE270042 RECEIVING INSPECTION REVEALED: .0015 OVERSIZED ON GP SUPPORT #8 BEARING BORE I.D. B/P SPECS. (1.7050 - 1.7060) REQUESTI NG 100% WARRANTY REPAIR PER DAVID MENARD AND ROB HALDEMAN. THIS UNIT OVERHAULED ON DALLAS AIRMOTIVE W/O LF0828. 1 G 7 1 3U 3 U H2SW E4CE 1996102400734 19961024 00734 GL 1996 10 24 HEEA968387 2 19961018 A 7230 23057142 CASE HALVES 6890550 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL COMPRESSOR CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 724MB CAC40525 S756 CAE835286 ENGINE REMOVED DUE TO METAL IN OIL. UPON INSPECTION OF COMPRESSOR PARTS NOTED: PLASTIC CRACKED AND LIFTING ON CASE ASS EMBLY. INSTALLED A DALLAS AIRMOTIVE OVERHAULED CASE ASSEMBLY. 1 G 7 2 3U 3 U H3EU E4CE 1996102400735 19961024 00735 SW 1996 10 24 HEEA968388 1 19961018 A 6720 212011708105 PITCH HORN BELL 412 412 1182202 SW CHORD WEIGHT DEFECTIVE E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 3911L 76 33023 HOLE FOR SAFETY OF CHORDWISE WEIGHTS LOCATED IN WRONG PLACE. UNABLE TO SAFETY WITH REQUIRED WASHERS. ALSO REPLACED PIT CH LINKS. SEE MMIR# HEEA0008389 AND HEEA0008390 FOR INFORMATION. S/N A9 A11 1 G 7 2 4U H4SW 1996102400736 19961024 00736 SW 1996 10 24 HEEA968389 1 19961018 A 6720 212AD2130101 PITCH LINK BELL 412 412 1182202 SW CHORD WEIGHT DEFECTIVE E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 3911L 76 33023 HOLE FOR SAFETY OF CHORDWISE WEIGHTS LOCATED IN WRONG PLACE. UNABLE TO SAFETY WITH REQUIRED WASHERS. ALSO REPLACED PIT CH HORNS. SEE MMIR# HEEA0008388 AND HEEA0008390 FOR INFORMATION. 1 G 7 2 4U H4SW 1996102400737 19961024 00737 SW 1996 10 24 HEEA968390 1 19961018 A 6720 212AD2132101 PITCH LINK BELL 412 412 1182202 SW CHORD WEIGHT DEFECTIVE E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 3911L 76 33023 HOLE FOR SAFETY OF CHORDWISE WEIGHTS LOCATED IN WRONG PLACE. UNABLE TO SAFETY WITH REQUIRED WASHERS. ALSO REPLACED PIT CH HORNS. SEE MMIR# HEEA0008388 AND HEEA0008389 FOR INFORMATION. 1 G 7 2 4U H4SW 1996102400738 19961024 00738 EU 1996 10 24 HEEA968391 1 19961018 A 6520 350A33020005 TAIL GEAR BOX SNIAS 350 AS350B2 8680813 EU OUTPUT SHAFT PLATING FLAKE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4000L 484 2873 CHROME PLATING COMING OFF OUTPUT SHAFT. 1 G 7 1 3U H9EU 1996102400739 19961024 00739 EU 1996 10 24 HEEA968392 1 19961018 A 6520 350A33215300 BEARING 350A33211905 SNIAS 350 AS350B2 8680813 EU T/R GR BOX SEPARATION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100R 426 2862 BEARING SEPARATION. 1 G 7 1 3U H9EU 1996102400740 19961024 00740 EU 1996 10 24 HEEA968393 1 19961018 A 6720 350A33214501 ROD SNIAS 350 AS350B2 8680813 EU T/R PITCH LINK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 3737 2771 BOTH T/R P/C LINKS WORN. 1 G 7 1 3U H9EU 1996102400753 19961024 00753 CE 1996 10 24 96ZZZX5330 1 19961004 A 3243 06111800 CYLINDER CESSNA 208 208B 2073701 CE LT BRAKE CRACKED A AWHA K NONE O OTHER IN INSP/MAINT 1 WP 17 781FE 1647 400 208B0278 PILOT REPORTED BRAKE MALFUNCTION ON LANDING. MAINTENANCE INSPECTED AND FOUND LT BRAKE CYLINDER, LOWER PORTION CRACKED. APPEARED TO BE IMPACT DAMAGE DUE TO TRACES OF YELLOW PAINT AND SCRATCHES OF CYLINDER HOUSING. ADDITIONAL DAMAGE INCLUD ED THE LOWER ANCHOR BOLT BENT AND THE LOWER LUG ON THE TORQUE PLATE CRACKED. INSPECTED RIGHT BRAKE ASSY AND FOUND SPONG Y BRAKING ACTION. REPAIRS WERE MADE TO THE LEFT BRAKE ASSY AND BOTH BRAKES PURGED OF TRAPPED AIR, OPERATIONAL CHECK OF BRAKES WAS NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. 1 H 7 1 3T A37CE 1996102400759 19961024 00759 NE 1996 10 24 96ZZZX5335 2 19960930 A 7261 310238201 FILLER CAP CESSNA 208 208B 2073701 CE PWA PT6 PT6A114 52043 NE ENGINE OIL OIL LOSS A A AWHA A UNSCHED LANDING K FLUID LOSS NR NOT REPORTED 1 WP 17 759FX 208B0542 PC0430 CAP ASSY NUT WAS ADJ TO EASE LOCKING COMPLAINT. P & W MM DOES NOT ADDRESS ADJ. A REPLACEMENT CAP ASSY PN 3102382-01 WA S INSTALLED. IT, TOO, WAS ADJ FOR STIFF LOCKING MECHANISM. IN ADDITON, THE LENGTH OF THE DIPSTICK DEFEATED THE CHECK B ALL INSTALLED VIA P & W SB 1451. THE RESULT WAS AN UNSCHED STOP AND LOSS OF 4 QTS OF ENG OIL. SUBMITTER STATED P & W S HOULD LOOK AT RE-ENGINEERING ADJ PROTION OF OIL CAP ASSY. MANUAL SHOULD ADDRESS IN THE FORM OF A 'WARNING', THE CONSEQU ENCES OF ADJUSTMENT TO THE OIL CAP ASSY. IPC SHOULD REMOVE THE INTERCHANGABILITY OF PN 3102382-01 AND 3115095-01. INVE NTORY OF 3102382-01 SHOULD BE PURGED OR MODIFIED PER P & W SB 1451. 1 H 7 1 3T 3 T A37CE E4EA 1996102400766 19961024 00766 SO 1996 10 24 96ZZZX5342 1 19960903 A 7810 EXHAUST STACK STOLAM RC3 RC3 3080202 SO RT STARBOARD ELBOW FAILED A P A EKQA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 AL 05 6256K 550 463 AFTER TAKEOFF AT 200 FEET AGL, THE ENGINE QUIT. INVESTIGATION REVEALED THE RT EXHAUST STACK ELBOW HAD PULLED LOOSE FROM STACK ASSY INSIDE ENGINE COWL. INTENSE HEAT FROM EXHAUST BURNED THROUGH ALUMINUM STRUCTURE AFT OF ENGINE AND MELTED MA GNETO WIRES AND OTHERS TOGETHER CAUSING MAGS TO SHORT OUT. RECOMMEND ALL ALUMINUM PIECES ACTING AS FIREWALL BE CHANGED TO STAINLESS STEEL. 1 H 7 1 3O A769 1996102400799 19961024 00799 EU 1996 10 24 RAIA960905 1 19960907 A 2435 23095002 STARTER/GEN JETAIR JETSTM JETSTM4101 1500501 EU RT ENG FAILED A RAIA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 CE 03 554HK 41067 JFK - FLT 7680 - NOTICED A VIBRATION THROUGH THE FLOOR AND YOKES. MAINTENANCE PERFORMED A PROP BALANCE AND REPLACED THE NR 2 STARTER/GENERATOR. (M) 2 L 7 2 4T RT A41NM 1996102400800 19961024 00800 WP 1996 10 24 RAIA960904 2 19960907 A 7530 8961151 SEALS BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 03 433AM 200 885 P66163 STL - FLT 7075 - NR 1 ENGINE WOULD NOT PRODUCE TARGET TORQUE. MAINTENANCE REPLACED THE NR 1 ENGINE P3 BLEED SEALS. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996102400801 19961024 00801 EU 1996 10 24 RAIA960827 1 19960827 A 3234 1005383Y00 SELECTOR VLV AEROSP ATR42 ATR42300 8680920 EU LANDING GEAR FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 422TE 18238 106 STL - FLT 7516 - WHEN GEAR SELECTED UP, THE GEAR REMAINED DOWN, AND THE INTRANSIT AND DOWN AND LOCKED LIGHTS WERE ILLUMI NATED. MAINTENANCE REPLACED THE LANDING GEAR SELECTOR VALVE. (M) 2 H 7 2 4T RT A53EU 1996102400802 19961024 00802 EU 1996 10 24 RAIA960903 1 19960904 A 3350 OL3071BPE BULB AEROSP ATR72 ATR72202 8680940 EU CABIN FAILED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 721TE 217 STL - FLT 7408 - FORWARD SECTION OF EMERGENCY ESCAPE PATH LIGHTING HAS A BULB INOPERATIVE. MAINTENANCE REPLACED THE FOR WARD BULB OF THE ESCAPE PATH LIGHTING. (M) 2 H 7 2 4T RT A53EU 1996102400803 19961024 00803 WP 1996 10 24 VTZA96359 2 19960906 A 7321 31059003 FUEL CONTROL JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33110U 01514 WP NR 2 ENG FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK X ENGINE FLAMEOUT TO TAKEOFF 1 EA 27 301UE 41012 FLT NR 6402 - BOS-IAD - ABORTED TAKEOFF DUE TO NR 2 ENGINE SHUTDOWN ON TAKEOFF. AIRCRAFT RETURNED TO GATE WITH NO FURTH ER INCIDENTS. MAINTENANCE REMOVED AND REPLACED FUEL CONTROL UNIT. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FO R RETURN TO SERVICE. (M) 2 L 7 2 4T 4 T RT A41NM E4WE 1996102400804 19961024 00804 WP 1996 10 24 GTIA96NK184 1 19960730 A 3297 WIRE DOUG DC9 DC932 3022066 WP LT MLG WW BROKEN A GTIA O OTHER P NO WARNING INDICATION CL CLIMB 1 GL 23 941ML 47131 LEFT MAIN INTRANSIT RED LIGHT DID NOT ILLUMINATE DURING GEAR RETRACTION. FOUND BROKEN WIRES IN LEFT MAIN WHEEL WELL, RE PAIRED SAME. (M) 2 L 7 2 4F A6WE 1996102400805 19961024 00805 1996 10 24 96ZZZM1415 4 19960822 A 2562 4530130D BATTERY BEECH 1900 1900C 1154161 CE ELT DISCHARGED A JIKA K NONE L NO TEST IN INSP/MAINT 1 WP 01 31704 UB12 ELT BATTERY, WITH 2 MOS REMAINING UNTIL CALENDAR EXPIRATION, BEGAN LEAKING, CAUSING PLASTIC CASE TO CRACK AND DISINTEGRA TE. ACID LEAKED INTO TRANSMITTER RENDERING IT INOPERATIVE. LEAKING ACID ALSO CAUSED THE PLASTIC TRAY (ORIGINALLY SUPPL IED WITH THE ELT AS PART OF THE INSTALLATION KIT) TO CRACK AND DISINTEGRATE AS WELL, REDUCING OR ELIMINATING THE 9G REST RAINT CAPABILITY. ACID ALSO SPILLED ON AIRFRAME MEMBERS. FOUND DURING A SCHEDULED INSPECT. SUBMITTER STATES, THIS IS THE 2ND UNIT TO HAVE BEEN FOUND FAILED IN THIS MANNER. S/N 55215 WAS ALSO FOUND TO HAVE CRACKED CASE AND TRAY DUE TO LE AKING ACID. 2 L 7 2 4T RT A24CE 1996102400806 19961024 00806 1996 10 24 96ZZZM1416 4 19960902 A 2562 4530130D CASE PIPER PA31 PA31 7103102 SO ELT CRACKED A JIKA K NONE O OTHER IN INSP/MAINT 1 WP 01 6733L 31636 ELT BATTERY WAS FOUND TO HAVE 2 SMALL CRACKS IN PLASITC CASE, AND TRACES OF ACID. UPON OPENING OF THE BATTERY, FOUND TH AT ONE OF THE PANASONIC MADE 'D' CELLS WAS LEAKING FROM THE BASE (NEGATIVE END). LEAK WAS FOUND BEFORE DAMAGE WAS CAUSE D TO TRANSMITTER OR ELT TRAY. SUBMITTER STATES, THIS IS THE THIRD FINDING OF DAMAGE CAUSED BY LEAKING ACID FROM AN ELT 110-4 BATTERY, THIS BATTERY WAS HALF WAY THROUGH ITS TWO YEAR LIFE. 1 L 7 2 3O A20SO 1996102400807 19961024 00807 NE 1996 10 24 M3HA96024 2 19960906 A 7261 ENGINE AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE LEFT LOW OIL A M3HA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 WP 13 4206G 081 120352 HNL - FLT 428 - DURING CLIMB-OUT, RECEIVED MASTER CAUTION WARNING ON THE NR 1 ENG OIL ON THE CREW ALERT COMP. THE CAUTI ON WOULD COME ON THEN CLEAR ITSELF. ON THE PRESS GAUGE 1 OIL WAS REPORTED DOWN INTO THE CAUTIONARY RANGE. CREW SHUTDOW N THE NR 1 ENG AND RETURNED HNL. CHECKED OIL LVL NR 1 ENG, FOUND 2 QTS LOW, SERV ENG OIL PER PWA MM 72-00-01 FIG 7, PUL LED FILTERS AND CHIP DET'S INSPECTED AND FOUND NO FOREIGN MAT. RETURNED FILTERS AND CHIP DETECTORS, RAN ENG FOR 10 MIN AT 80 PERCENT TQ. FOUND NO MATERIAL. ENG OIL CONSUMPTION HIGH PER A/C LOGS. CHECKED 6/7 BEARING VENT TUBE, FOUND TO B E COKED UP. CLEANED TUBE AND RETURNED ENG TO SERV WITH CARRYOVER WATCH TO CHECK FILTERS IN 70 PLUS OR MINUS 5 FLT HRS. 2 H 7 2 4T 4 T RT A53EU E20NE 1996102400808 19961024 00808 NM 1996 10 24 IXKA9600073 1 19960830 A 2780 CONTROL VLV BOEING 727 727251 138408H NM LE FLAPS OUT OF ADJUST A IXKA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 EA 25 264US 19983 FLT 25 - EWR-ATL - AFTER TAKEOFF, NR 2, 3, 6 AND 7 LE DEVICES WOULD NOT RETRACT WHEN FLAP SELECTED UP. RETURNED AND LAN DED AT EWR. RERIGGED LEADING EDGE SLAT CONTROL VALVE PER MM 27-81-81, OPS CHECK OK. (M) 2 L 7 3 4F A3WE 1996102400809 19961024 00809 SW 1996 10 24 MALA965116 1 19960906 A 5270 WARNING LIGHT SWRNGN SA227 SA227AC 8780603 SW CABIN DOOR ILLUMINATED A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 421MA AC634 FLT 3451 - IN CRUISE FLIGHT TO AZO, THE CABIN DOOR LIGHT ILLUMINATED IN FLIGHT. THE AIRCRAFT DIVERTED TO AZO. MAINTENA NCE INSPECTED THE CABIN DOOR SWITCHES AND BAYONETS. NO DISCREPANCIES NOTED. MAINTENANCE WAS UNABLE TO DUPLICATE THE DI SCREPANCY. ALL CHECKS SATISFACTORY. (M) 2 L 7 2 4T RT A8SW 1996102400810 19961024 00810 SW 1996 10 24 MALA965114 1 19960831 A 5720 ANGLE SWRNGN SA227 SA227AC 8780603 SW RT WING/NACELLE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 421MA AC634 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE RIGHT INBOARD LOWER WING TO NACELLE ATTACH ANGLE CRACKED. C OMPLETED REPAIR TO ATTACH ANGLE BY FABRICATING AND INSTALLING REPAIR ANGLE IAW FAIRCHILD ARP 54-20-9101 REV B. (M) 2 L 7 2 4T RT A8SW 1996102400811 19961024 00811 SW 1996 10 24 MALA965113 1 19960831 A 5320 2722085 DOOR FRAME SWRNGN SA227 SA227AC 8780603 SW BS 491 DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 421MA AC634 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERFORMED A REPAIR TO THE CARGO DOOR FRAME, P/N 27-22085, AT FS 491.00 BY REMOVING DAMAGED GAS STRUT MOUNT HOLE (1.625 BY 1.825). FABRICATED, PREPPED AND INSTALLED A REPAIR ANGLE, REPAIR PL ATE, AND FILLER IAW FAIRCHILD ARP 53-20-9503 DATED MARCH 1. (M) 2 L 7 2 4T RT A8SW 1996102400812 19961024 00812 NM 1996 10 24 MALA965108 1 19960804 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN LOOSE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 848MA 346 FLT 2926 - ON POST FLGHT, CREW REPORTED SIDEWALL EMERGENCY LIGHT AT SEAT 1E WAS INTERMITTENT. MAINTENANCE RESECURED CAN NON PLUG BACK SHELL ON LIGHT. OPS CHECK OF LIGHT WAS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1996102400813 19961024 00813 EU 1996 10 24 USAAF96101 1 19960921 A 2822 229432 FUEL PUMP FOKKER F28 F28MK0100 4990807 EU NR 1/NR 2 FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 864US 11306 PIT-DTW - FLT 1140Z - ON CLIMB-OUT, RECEIVED FAULT LIGHTS FOR NR 1 AND NR 2 RIGHT FUEL PUMPS. AIRCRAFT RETURNED TO PIT. NO FURTHER INCIDENTS DURING FLIGHT. MAINTENANCE REPLACED R1 AND R2 FUEL BOOST PUMPS. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT 1996102400814 19961024 00814 WP 1996 10 24 USAA960623 1 19960920 A 5311 991224617 FRAME DOUG DC9 DC931 3022065 WP BS 1038 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 974VJ 74679 47130 PIT - DURING Q3-C2 CHECK, FOUND 3 INCH CRACK IN FRAME WEB STATION 1038 LONGERON 5L AND 9L. SPLICED IN SECTION OF WEB PE R EA NR 33533. (M) 2 L 7 2 4F A6WE 1996102400815 19961024 00815 WP 1996 10 24 USAA960624 1 19960920 A 5720 DOUBLER DOUG DC9 DC931 3022065 WP LWR WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 974VJ 74698 47130 PIT - DURING Q-3/C-2 CHECK, FOUND .5 INCH CRACK LOWER WING SKIN PLATE DOUBLER AT LOWER WING ACCESS PLATE 1456A DOUBLER. INSTALLED DOUBLERS PER SRM 57-03 FIG 29A AND EA 33614. (M) 2 L 7 2 4F A6WE 1996102400816 19961024 00816 WP 1996 10 24 USAAD96130 1 19960918 A 3231 RETRACT MECH DOUG DC9 DC981 3022081 WP NLG DOORS MALFUNCTIONED A USAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 19 801US 48037 FLT 368 - RSW-CLT - ON TAKEOFF, CREW HEARD SOUND FROM NOSE AREA, RETURNED TO FIELD. FOUND NOSEGEAR DOORS OPEN. CLOSED DOORS, INSPECTED NOSE AREA AND GLIDESLOPE ANTENNA. NO DEFECTS NOTED, RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 2 4F A6WE 1996102400817 19961024 00817 NM 1996 10 24 USAASB96196 1 19960918 A 3260 806002 PROX SWITCH CARD BOEING 737 7373B7 1384580 NM NLG FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 533AU 24515 PHL - AIRCRAFT WAS POSITION FERRYING TO CLT AND DURING CLIMB CREW RECEIVED RIGHT MAIN GEAR RED UNSAFE LIGHT. CREW WAS A DVISED TO RETURN TO FIELD AT PHL. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE INSPECTED GEAR, SENSORS AND WIRI NG. JACKED AIRCRAFT, SWUNG GEAR AND FOUND M982 LOGIC CARD HARD FAULTED. REPLACED SAME AND PERFORMED SYSTEM TEST. SWUN G GEAR SEVERAL TIMES. ALL TESTED GOOD. (M) 2 L 7 2 4F RT A16WE 1996102400818 19961024 00818 NM 1996 10 24 USAA960625 1 19960920 A 5330 SKIN BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 264AU 34505 22961 ROA - DURING CX-1 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND .0625 INCH CRACK FORWARD GALLEY DOOR CUT OUT AFT LOWER CORNER FUSELAGE SKIN. STOP DRILLED CRACK AND INSTALLED DOUBLER. REPAIRED PER TYPICAL REPAIR 53-10-19 REV A. (M) 2 L 7 2 4F A16WE 1996102400819 19961024 00819 NM 1996 10 24 96ZZZM1417 1 19960619 A 3222 65737625 STRUT BOEING 737 7372L9 1384497 NM NLG CORRODED A ZZDA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 15 737Q W519B 21279 FLT 561 - MECHANICS OBSERVED HYDRAULIC FLUID LEAKING FROM BOTTOM GLAND NUT ON NOSE LANDING GEAR. UPON TEAR DOWN (FOR A SEAL KIT REPLACEMENT) INSPECTION REVEALED THAT THE OUTER CYLINDER GLAND NUT THREADS WERE PITTED DUE TO CORROSION, UPPER CENTERING CAM INNER AND OUTER SURFACE PLATING PITTED DUE TO CORROSION. THE NOSE GEAR ASSEMBLY WAS REPLACED AND FUNCTION AL CHECK WAS NORMAL. THE LEAKING NOSE GEAR ASSEMBLY HAD BEEN INSTALLED 3 DAYS PRIOR AS AN OVERHAULED UNIT. THE DEFECTI VE NOSE GEAR ASSEMBLY HAD ACCUMULATED 29.5 FLT HOURS AND 15 CYCLES BEFORE REMOVAL. (M) 2 L 7 2 4F RT A16WE 1996102400820 19961024 00820 NM 1996 10 24 96ZZZM1418 1 19960712 A 3246 26015711 WHEEL ASSY BENDIX BOEING 737 737297 1384480 NM RT MLG FAILED A ZZDA O OTHER O OTHER LD LANDING 1 SO 15 462AT B2928 22631 AFTER LANDING, DURING TAXI TO GATE, THE NR 4 MLG WHEEL ASSY FAILED CAUSING THE NR 4 HUB CAP TO IMPACT THE NR 2 ENG INBOA RD COWLING DAMAGING THE FORWARD AND AFT SECTIONS. UPON OPENING UP NR 2 ENGINE COWL INVESTIGATION REVEALED AFT FIREWALL AND TAILPIPE DAMAGE. INVESTIGATION OF THE WHEEL ASSEMBLY REVEALED THAT THE OUTBOARD FLANGE HAD FAILED AND SEPARATED FRO M THE ASSEMBLY. WHEEL ASSEMBLY IS IMPOUNDED AND WILL BE RETURNED TO MCO. WHEEL ASSEMBLY WAS OVERHAULED BY AVIALL IN HO LLYWOOD, FL. WHEEL ASSY HAD ACCUMULATE 210 CYCLES. A/C IS CURRENTLY UNDERGOING REPAIR IN DAYTON. 2 L 7 2 4F A16WE 1996102400821 19961024 00821 NM 1996 10 24 W8PA960144 1 19960930 A 3350 LIGHT BOEING 737 7373Q8 1384670 NM ROW 1-14-19-21 LOOSE A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 956WP 24299 EMERGENCY FLOOR LIGHTING INOP ROW 1, ROW 14 AND ROWS 19-21. FOUND LOOSE CONNECTION AT ROW 1, 14, AND 19-21. RECONNECTE D. (M) 2 L 7 2 4F RT A16WE 1996102400822 19961024 00822 NM 1996 10 24 W8PA960145 1 19960930 A 3350 LIGHT BOEING 737 7373K9 138447L NM CABIN INOPERATIVE A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 945WP 24212 LEFT EMERGENCY EXIT COVE LIGHT INOP. RELAMPED. (M) 2 L 7 2 4F RT A16WE 1996102400823 19961024 00823 NM 1996 10 24 W8PA960141 1 19960926 A 3350 BULB BOEING 737 7373S3 1384711 NM AFT BODY FAILED A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 375TA 23787 LEFT AFT BODY FAIRING EMERGENCY LIGHT INOP. REPLACED BULB. (M) 2 L 7 2 4F RT A16WE 1996102400824 19961024 00824 NM 1996 10 24 W8PA960143 1 19960930 A 3350 LENS BOEING 737 7373Q8 1384670 NM CABIN MISSING A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 956WP 24299 EMERGENCY FLOOR TRACK LIGHTING MISSING LIGHT LENS AT SEAT ROW 18. INSTALLED NEW LIGHT LENS. (M) 2 L 7 2 4F RT A16WE 1996102400825 19961024 00825 SO 1996 10 24 WTAA960163 1 19960812 A 3150 80055711 COMPUTER EMB 120 EMB120RT SO AURAL WARNING LOOSE CONNECT A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 17 454UE 120155 FAT - AURAL TRIM WARNING SOUNDED ON TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE RERACKED AURAL WARNING COMPUTER. SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996102400826 19961024 00826 SO 1996 10 24 WTAA960162 1 19960811 A 5242 12034957001 DOOR LATCH EMB 120 EMB120RT SO AVIONICS BAY OBSTRUCTED A WTAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 17 284YV 120284 FAT - SERVICE DOOR LIGHT CAME ON DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE REMOVED RUBBER TRI M PIECE FROM AVIONICS BAY DOOR LATCH. SYSTEM OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996102400827 19961024 00827 WP 1996 10 24 96ZZZM1419 1 19960918 A 3246 311422 WHEEL BFGOODRICH DOUG DC6 DC6A 3021706 WP NR 1 MLG CRACKED A TALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 19 874TA 1583 44641 NR 1 MAIN WHEEL ASSEMBLY SPLIT AND OUTER PORTION OF WHEEL AND TIRE LEFT AIRCRAFT DURING TAXI. SUBMITTER STATES, POSSIBL E CAUSE, UNDETECTED CRACK OR METAL FATIGUE. 2 L 7 4 4R 6A3 1996102400828 19961024 00828 NM 1996 10 24 TSAA9628076 1 19960921 A 2823 61185 FUEL SHUTOFF VLV BOEING 737 7372T4 1384492 NM NR 1 ENGINE INOP A A TSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 807AL 23443 FLT 302 - HNL-OGG - AFTER TAKEOFF, THE NR 1 FUEL VALVE CLOSED LIGHT ILLUMINATED BRIGHT. ALL ENGINE INDICATIONS REMAINED NORMAL. RETURNED TO HNL. REMOVED AND REPLACED NR 1 ENGINE FUEL SHUTOFF VALVE IAW MM 28-22-11. OPS CHECK GOOD. AIRCR AFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1996102400829 19961024 00829 1996 10 24 TSAA96075 4 19960921 A 3425 5224703002 STEERING COMP BOEING 737 7372Q9 138448M NM E/E BAY FAILED A TSAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 13 804AL 21719 FLT 257 - HNL-LIH - FLIGHT OFFICERS VERTICAL GYRO COMPUTER FLAG CAME ON IN FLIGHT. FLIGHT DIRECTOR 2 AC CIRCUIT BREAKER OPEN. NOT RESET. FLIGHT ATTENDANT REPORTED STRONG ELECTRICAL SMOKE/SMELL IN CABIN. REPLACED STEERING COMPUTER. AIRC RAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1996102400830 19961024 00830 NM 1996 10 24 TSAA9657074 1 19960923 A 5730 SKIN BOEING 737 737297 1384480 NM WS 150 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 726AL 22426 DURING C-CHECK VISIT, FOUND SKIN BULGE LOWER SKIN AT WS 150 L/G OF WING .125 INCH HIGH, 4.5 INCHES LONG. REPAIRED PER E CO 2744. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1996102400831 19961024 00831 NE 1996 10 24 TWRA96290 2 19960822 A 7230 COMPRESSOR BOEING 747 747136 1384883 NM PWA JT9 JT9D7J 52054 NE NR 3 ENGINE STALLED A TWRA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 EA 15 606FF 43023 685708 20273 WHILE DESCENDING OUT OF FL 320, NR 3 ENGINE COMPRESSOR STALLED WITH AUDIBLE SOUND AND RAPIDLY RISING EGT (MAX 750 DEGREE S CELSIUS). NR 3 ENGINE WAS SHUT DOWN. ENGINE WAS RELITE AT FL 220. AFTER N2 STABILIZED AT 50 PERCENT. EGT BEGAN TO RISE CONTINOUSLY TO 650 DEGREES CELSIUS WITH MULTIPLE AUDIBLE SOUNDS. ENGINE WAS SHUT DOWN. AT NO TIME WERE ANY PARAME TERS EXCEED LIMITS. ENGINE NR 3 WAS REPLACED AT JFK. NO FURTHER ENGINE PROBLEMS OCCURRED. (M) 2 L 7 4 4F 4 F A20WE E20EA 1996102400832 19961024 00832 EU 1996 10 24 SIMA962671 1 19960923 A 2120 AIR DISTR SAAB SF340 340B 7860101 EU CABIN ODOR A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 21 391AE 340B391 DFW - FLT 3552 - CREW REPORTED OIL/SMOKE FUMES IN COCKPIT DURING APPROACH TO DFW. MAINTENANCE CHECKED ACM AND ENGIEN FO R OIL LEAKS, NONE WERE FOUND. FCF WAS PERFORMED AT VARIOUS ALTITUDES AND POWER SETTINGS AND THE PROBLEM COULD NOT BE DU PLICATED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1996102400833 19961024 00833 WP 1996 10 24 IXXA96159 1 19960924 A 3230 UPLATCH ASSY DOUG DC8 DC871 302199A WP NLG LACK OF LUBE A IXXA O OTHER J WARNING INDICATION CR CRUISE 1 SW 11 829BX 45994 EN ROUTE FROM ORD-TOL, THE AIRCRAFT FAILED A GEAR UPLATCH CHECK, ACCOMPANIED BY A LANDING GEAR UNSAFE LIGHT. NOISE HEAR D AT NOSE GEAR. TOL MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NOSE GEAR UPLATCH DIRTY AND DRY. MAINTENANCE CLEA NED AND LUBRICATED LATCH MECHANISM. PERFORMED A NOSE GEAR SWING PER DACO MM 32-30-0 AND 32-31-6 WITH NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 4 4F 4A25 1996102400834 19961024 00834 NE 1996 10 24 IXXA96155 2 19960903 A 7200 ENGINE DOUG DC8 DC871 302199A WP GE CFM56 CFM562C1 13802 NE NR 4 FAILED A A IXXA E ENGINE SHUTDOWN E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SW 11 822BX 27730 45813 692266 EN ROUTE KPOB TO KICT, A PRECAUTIONARY SHUTDOWN OF THE NR 4 ENGINE WAS ACCOMPLISHED DUE TO HEAVY VIBRATION, LOSS OF OIL PRESSURE AND FLUCTUATING FUEL FLOW. THE ENGINE WAS REMOVED AND REPLACED, AND AIRCRAFT WAS RETURNED TO SERIVICED. (M) 2 L 7 4 4F 4 F 4A25 E2GL 1996102400835 19961024 00835 NE 1996 10 24 IXXA96158 2 19960924 A 7200 ENGINE DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7A 52039 NE NR 1 FLAMED OUT A IXXA E ENGINE SHUTDOWN X ENGINE FLAMEOUT CL CLIMB 1 SW 11 784AL 46135 669753 ON CLIMB-OUT FROM BNA TO TOL, THE NR 1 ENGINE FLAMED OUT. THE IGNITORS WERE SELECTED FOR 'BOTH' AND A SUCCESSFUL RESTAR T WAS ACCOMPLISHED. THE AIRCRAFT CONTINUED TO TOL WITH NO ABNORMAL PROBLEMS. INSPECTION OF THE ENGINE AND FUEL SYSTEM REVEALED NO ABNORMALITY. A PERFORMANCE RUN WAS ACCOMPLISHED IAW ATI JRH, AND ENGINE OPERATION WAS NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 4 4F 4 F 4A25 1E8 1996102400836 19961024 00836 NM 1996 10 24 IXKA9600081 1 19960922 A 2751 18129932 INDICATOR BOEING 727 727251 138408H NM TE FLAP POSITION INOPERATIVE A IXKA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 25 264US 361 19983 FLT 78 - MDW-ATL - AFTER TAKEOFF UPON FLAP RETRACTION, INBOARD FLAPS WOULD NOT INDICATE LESS THAN 5 DEGREES. AIR TURN B ACK TO MDW. REMOVED AND REPLACED FLAP POSITION INBOARD INDICATOR. OPS CHECK OK AS PER 27-52-00. (M) 2 L 7 3 4F A3WE 1996102400837 19961024 00837 NM 1996 10 24 IXKA9600080 1 19960921 A 2750 CONNECTOR BOEING 727 727251 138408H NM RT TE FLAP DAMAGED A IXKA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 25 264US 181 19983 ATL - FLT 84 - AFTER TAKEOFF, ATL-TPA, RETURNED TO ATL WHEN INBOARD TRAILING EDGE FLAPS DID NOT RETRACT. STOPPED AT 5 D EGREES. ALL LE DEVICES RETRACTED. CHECKED AND FOUND RIGHT INBOARD FLAP TRANSMITTER, P/N 9660022001, ELECTRICAL CONNECT OR DAMAGED. REPLACED TRANSMITTER AND ELECTRICAL CONNECTOR, LUBED GEAR BOXES AND JACKSCREWS AND OPS CHECK OK AS PER MM 2 7-52-02. (M) 2 L 7 3 4F A3WE 1996102400838 19961024 00838 NM 1996 10 24 IXKA9600079 1 19960906 A 2150 65266871 RAM AIR DOOR BOEING 727 727225 1384077 NM LEFT MISSING A IXKA K NONE O OTHER IN INSP/MAINT 1 EA 25 361KP 20627 UPON GATE ARRIVAL AND WALKAROUND INSPECTION, FOUND LEFT PACK RAM AIR DOOR MISSING. INSPECTED SURROUNDING AREA, NO DAMAG E FOUND ON AIRFRAME, INSPECTED FORWARD CARGO PRESSURE AREA. PERFORMED PERSSURIZATION CHECK OK. LEFT RAM AIR DOOR ACTUA TOR INOP. REMOVED AND REPLACED LEFT RAM AIR DOOR ACTUATOR PER MM 21-56-11, PAGE 401-406, 406-408. REPLACED MISSING LEF T RAM AIR DOR PER 21-26-10. OPS CHECK OK. (M) 2 L 7 3 4F A3WE 1996102400839 19961024 00839 WP 1996 10 24 HALA96137 1 19960921 A 3350 60030431 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 679HA 47662 HNL - FLT 103 - EMERGENCY LIGHTS IN THE COCKPIT, DIM TO NONE. REMOVED AND REPLACED THE BATTERIES AND THE OPERATIONAL CH ECK WAS GOOD. (M) 2 L 7 2 4F A6WE 1996102400840 19961024 00840 WP 1996 10 24 GTIA96NK206 1 19960924 A 2150 PACK DOUG DC9 DC931 3022065 WP CABIN SMOKING A GTIA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 GL 23 928ML 47326 AFTER LANDING AND BLOCK IN RSW. APPEARS TO HAVE A TRACE OF SMOKE IN CABIN AREA WITH PACK OPERATING. INSPECTED AND OPER ATED BOTH LEFT AND RIGHT PACKS USING RIGHT PACK IN NORMAL. ALL OPERATIONS AND INDICATIONS ARE NORMAL, IAW CHAP 21. NO SMOKE IN CABIN NOTED. (M) 2 L 7 2 4F A6WE 1996102400841 19961024 00841 EU 1996 10 24 COEA9672002 1 19960919 A 5532 2001058901 SKIN FOKKER F27 F27MK500 4990629 EU VERT STAB LE DENTED A COEA K NONE C F.O.D. IN INSP/MAINT 1 NM 13 720FE 729 10464 UPON ARRIVAL INTO SBA FROM ONT, MECHANIC OBSERVED BLOOD ON THE VERTICAL STABILIZER LEADING EDGE WHILE PERFORMING THE WAL K AROUND. MAINTENANCE DISCOVERED A DENT FROM AN APPARENT BIRD STRIKE. THE STRUCTURAL DAMAGE EXCEEDS SRM PARAMETERS. P ARTS ARE CURRENTLY EN ROUTE. REMOVED AND INSTALLED SERVICEABLE LEADING EDGE. (M) 2 H 7 2 4T A817 1996102400842 19961024 00842 NM 1996 10 24 96ZZZM1420 1 19960815 A 3350 0816323610 TRACK BRUCE BR2013737GF BOEING 737 7372P6 NM CABIN BROKEN A A6XA K NONE O OTHER IN INSP/MAINT 1 SO 13 EICKL 21356 DURING AN INSPECTION, IT WAS DISCOVERD THAT THE EMERGENCY FLOOR TRACK LIGHTING WAS BROKEN BY PASSENGERS WALKING AND KICK ING THE TRACK AT ROW 22. BAD SECTION REPLACED AND SECURED. FLOOR LIGHTS OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A16WE 1996102400843 19961024 00843 NM 1996 10 24 96ZZZM1421 1 19960820 A 2121 215201 GASPER FAN BOEING 737 737242 1384477 NM COCKPIT FAILED A A6XA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 13 159PL 1762 21186 AIRCRAFT ON APPROCH TO CHS AND A STRONG ODOR FILLED THE COCKPIT AND CABIN. SHORTLY AFTER DETECTING ODOR, THE GASPER FAN CIRCUIT BREAKER POPPED. UPON INSPECTION FOUND FAN HAD FAILED. (M) 2 L 7 2 4F A16WE 1996102400844 19961024 00844 EU 1996 10 24 VTZA96383 1 19960919 A 3230 ATG1350202 WOW SWITCH JETAIR JETSTM JETSTM4101 1500501 EU LT MLG OUT OF ADJUST A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 309UE 41022 FLT 6323 - IAD-RDU - RETURNED TO IAD AFTER THE FLIGHT CREW EXPERIENCED THE THAT THE LANDING GEAR WOULD NOT RETRACT WHEN THE GEAR HANDLE WAS SELECTED TO THE UP POSITION. THE AIRCRAFT RETURNED TO IAD WHERE THE MAINTENANCE PERSONNEL TROUBLESH OT THE DISCREPANCY AND FOUND THAT THE WEIGHT ON ON WHEEL SWITCH (LT POSITION) WAS OUT OF ADJUSTMENT. THE WOW SWITCH WA S PROPERLY ADJUSTED AND THE SYSTEM WAS FUNCTIONALLY CHECKED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1996102400845 19961024 00845 EU 1996 10 24 VTZA96382 1 19960917 A 3260 ATG135022 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU RT MLG OUT OF ADJUST A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 327UE 41080 FLT NR 6203 - IAD-MHT - DURING CLIMB, RETURNED TO IAD AFTER THE FLIGHT CREW EXPERIENCED THE RIGHT GEAR INTRANSIT LIGHT R EMAINING ILLUMINATED AND THE RED GEAR HANDLE REMAINING ILLUMINATED AFTER THE GEAR WAS SELECTED UP. THE AIRCRAFT RETURNE D TO IAD WHERE THE MAINTENANCE PERSONNEL TROUBLESHOT THE DISCREPANCY AND FOUND THAT THE RIGHT GEAR MICROSWITCH WAS OUT O F ADJUSTMENT. THE MICROSWITCH WAS PROPERLY ADJUSTED AND THE SYSTEM WAS FUNCTIONALLY CHECKED. THE AIRCRAFT WAS THEN REL EASED FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1996102400846 19961024 00846 EU 1996 10 24 VTZA96381 1 19960917 A 3240 91SE16 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU PARKING BRAKE OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 311UE 41029 FLT NR 6525 - JFK-ROC - DURING TAKEOFF, THE CREW ABORTED THEIR TAKEOFF DUE TO A CONFIGURATION WARNING INDICATION. THE A IRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE CONTROL WAS NOTIFIED. ACA MAINTENANCE PERSONNEL WERE AT JFK COMPLETING A MAINTENANCE ACTION ON ANOTHER AIRCRAFT. THE MAINTENANCE PERSONNEL TROUBLESHOT THE DISCREPANCY AND FOUND THAT THE PARKI NG BRAKE MICROSWITCH WAS OUT OF ADJUSTMENT. THE MICROSWITCH WAS ADJUSTED AND THE SYSTEM WAS FUNCTIONALLY CHECKED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1996102400847 19961024 00847 EU 1996 10 24 VTZA96380 1 19960917 A 2751 TY176004A TRANSDUCER JETAIR JETSTM JETSTM4101 1500501 EU LT TE FLAP FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 305UE 41019 FLT 6393 - PIT-IAD - DURING TAKEOFF, THE CREW EXPERIENCED A TAKEOFF CONFIGURATION WARNING INDICATION. THE AIRCRAFT ABOR TED ITS TAKEOFF AT PIT. MAINTENANCE CONTROL WAS NOTIFIED AND THE AIRCRAFT WAS FERRIED TO IAD FOR MAINTENANCE. UPON ARR IVING AT IAD THE MAINTENANCE PERSONNEL TROUBLESHOT THE DISCREPANCY AND FOUND THAT THE LEFT FLAP POSITION TRANSDUCER HAD FAILED INTERNALLY. THE FLAP POSITION TRANSDUCER WAS REPLACED AND THE SYSTEM WAS FUNCTIONALLY. THE FLAP POSITION TRANSD UCER WAS REPLACED AND THE SYSTEM WAS FUNCTIONALLY CHECK. AIRCRAFT WAS THEN RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1996102400848 19961024 00848 EU 1996 10 24 VTZA96479UE 1 19960919 A 3260 622800200 UPLOCK SWITCH BAG JETSTM JETSTM3201 1500217 EU LT MLG FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 474UE 849 FLT NR 6442 - IAD-HVN - DURING CRUISE, EXPERIENCED A LEFT GEAR INTRANSIT LIGHT AFTER SELECTING THE GEAR UP FUNCTION. AI RCRAFT RETURNED TO IAD WHERE THE MAINTENANCE PERSONNEL TROUBLESHOT THE DISCREPANCY AND FOUND THAT THE LEFT GEAR UPLOCK M ICROSWITCH HAD FAILED. THE MICROSWITCH WAS REPLACED AND THE SYSTEM WAS FUNCTIONALLY CHECKED. THE AIRCRAFT WAS THEN REL EASED FOR SERVICE. (M) 2 L 7 2 4T RT A56EU 1996102400849 19961024 00849 EU 1996 10 24 VTZA96378 1 19960918 A 5270 91SE13 SWITCH BAG JETSTM JETSTM3201 1500217 EU MAIN PAX DOOR DIRTY A VTZA K NONE N FALSE WARNING LD LANDING 1 EA 27 492UE 790 FLT NR 6268 - BUF-IAD - AFTER LANDING AND DURING ROLL OUT, EXPERIENCED A PASSENGER DOOR WARNING CAPTION ILLUMINATION. T HE AIRCRAFT TAXIED TO THE RAMP WHERE THE MAINTENANCE PERSONNEL TROUBLESHOT THE PROBLEM AND FOUND THAT THE DOOR WARNING M ICROSWITCHES WERE DIRTY. THE SWITCHES WERE CLEANED, LUBRICATED AND CHECKED FOR PROPER ADJUSTMENT. THE AIRCRAFT WAS THE N RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A56EU 1996102400850 19961024 00850 CE 1996 10 24 PLGA9609071 1 19960907 A 2913 1143880007 POWER PACK BEECH 1900 1900C 1154161 CE HYD SYSTEM FAILED A PLGA O OTHER J WARNING INDICATION AP APPROACH 1 NE 05 3069K 3736 MX409998 UB71 BOS - FLT 4523 - ON APPROACH, THE GEAR DOWN AND LOCK LIGHT FAILED TO ILLUMINATE, THE LANDING GEAR RELAY CIRCUIT BREAKER WAS FOUND POPPED AND WOULD NOT RESET. THE GEAR WAS EXTENDED MANUALLY AND THE AIRCRAFT LANDED WITHOUT INCIDENT. BOS MAI NTENANCE PINNED THE GEAR DOWN AND FERRIED THE AIRCRAFT TO ALB. ALB MAINTENANCE REMOVED AND REPLACED THE HYDRAULIC POWER PACK AND RETURNED THE AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1996102400851 19961024 00851 EU 1996 10 24 SIMA962701 1 19960926 A 3350 3011180 POWER PACK AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 12MQ 130 012 WHEN AIRCRAFT POWER IS SELECTED OFF AND EMERGENCY LIGHTS SELECTED TO FLOOR LIGHTS, 31WL WOULD NOT ILLUMINATE. RAI'D EME RGENCY POWER SUPPLY 29WL PER JIC33-51-21. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996102400853 19961024 00853 NE 1996 10 24 ASOA96040 2 19960924 A 7260 311169301 SPUR GEAR EMB 120 EMB120RT SO PWA 118 PW118A NE RT ENGINE WORN A ASOA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 11 217AS 120011 FLT NR 7768 - EN ROUTE LFT-DFW, CREW EXPERIENCED A COMPLETE LOSS OF POWER OF THE RT ENGINE ACCOMPANIED BY AN AURAL WARNI NG OF 'OIL' AND 'ENGINE CONTROL'. OIL PRESSURE INDICATED NEAR ZERO, CREW PROCEEDED WITH THE ENGINE FAILURE CHECKLIST AN D SHUT DOWN THE RIGHT ENGINE AND DIVERTED INTO AEX WHERE LANDING WAS MADE SAFELY AND WITHOUT FURTHER INCIDENT. FOUND ME TAL CONTAMINATION AS A RESULT OF FUEL PUMP SPUR GEAR TEETH WORN. REMOVED AND REPLACED THE RIGHT ENGINE. OPERATIONAL AN D LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1996102400854 19961024 00854 NE 1996 10 24 USAASB96197 2 19960919 A 7510 320115 FUEL HEAT VLV BOEING 737 7372B7 1384560 NM PWA JT8 JT8D15A 52051 NE NR 1 ENG STUCK OPEN A A USAA A E UNSCHED LANDING ENGINE SHUTDOWN M OVER TEMP CL CLIMB 1 EA 19 267AU 45050 22879 CMH - FL 1183 - DURING CLIMB AT FL 280, CAPTAIN SHUT DOWN THE NR 1 ENGINE DUE TO HIGH OIL TEMPERATURE. THE OIL TEMPERAT URE WAS IN THE YELLOW BAND FOR APPROX 15 MINS PRIOR TO SHUTDOWN. CREW DECLARED AN EMERGENCY AND DIVERTED TO CMH WHERE T HE FLIGHT LANDED WITH NO FURTHER INCIDENT. TOTAL SINGLE ENG TIME WS 20 MINS. MX FOUND THE NR 1 ENG FUEL HEAT VLV STUCK IN THE OPEN POSITION. REPLACED SAME. INSPECTED AND REPLACED THE MAIN ENGINE OIL FILTER AND INSPECTED CHIP DETECTORS. ALL CHECKS OK PER MM. RAN ENGINE AT POWER AND AT IDLE PER MM. OIL TEMP OK. LEAK CHECK OK. NO DISCREPANCIES FOUND. ( M) 2 L 7 2 4F 4 F A16WE E2EA 1996102400855 19961024 00855 EU 1996 10 24 VTZA96396 1 19960923 A 3260 622800200 SWITCH BAG JETSTM JETSTM3201 1500217 EU NOSE OUT OF ADJUST A VTZA O OTHER N FALSE WARNING AP APPROACH 1 EA 27 471UE 821 FLT 6394 - HVN-IAD - DURING APPROACH, DECLARED AND EMERGENCY DUE TO NOSE GEAR UNSAFE LIGHT ON APPROACH AFTER GEAR EXTENS ION. AIRCRAFT LANDED AND RETURNED TO GATE WITH NO FURTHER INCIDENT. MAINTENANCE ADJUSTED NOSE DOWNLOCK MICROSWITCH. A IRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996102400856 19961024 00856 WP 1996 10 24 VTZA96394 2 19960924 A 7260 OIL CONTAM LIGHT JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE3311 01514 WP RT ENGINE ILLUMINATED A VTZA O OTHER O OTHER CR CRUISE 1 EA 27 306UE 41020 FLT 6353 - IAD-TYS - DURING CRUISE FLIGHT, CONTINUED FLIGHT WITH ONE DISCREPANCY WHICH WAS RIGHT ENGINE OIL CONTAMINATIO N LIGHT ILLUMINATED IN FLIGHT, ENGINE PARAMETERS NORMAL. AIRCRAFT LANDED AND WENT TO GATE WITH NO FURTHER PROBLEMS. MA INTENANCE INSPECTED AND FOUND VERY SLIGHT METAL FUZZ ON CHIP DETECTOR, METAL FUZZ WITHIN LIMITS. MAINTENANCE CLEANED CH IP DETECTOR AND RAN AIRCRAFT. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 3 T RT A41NM E3WE 1996102400857 19961024 00857 WP 1996 10 24 VTZA96391 2 19960924 A 7260 OIL CONTAM LIGHT JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE3311 01514 WP LT ENGINE ILLUMINATED A VTZA O OTHER J WARNING INDICATION CR CRUISE 1 EA 27 326UE 41064 FLT - 6517 - IAD-BOS - DURING CRUISE, CONTINUED FLIGHT WITH ONE DISCREPANCY WHICH WAS LEFT ENGINE OIL CONTAMINATION LIGH T ILLUMINATING INFLIGHT. ENGINE PARAMETERS NORMAL. AIRCRAFT LANDED AND WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTEN ANCE INSPECTED SYSTEM, FOUND SMALL SLIVER WITHIN LIMITS, PLUS CLEANED CHIP DETECTOR AND RAN AIRCRAFT, OPS CHECK OK. AIR CRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 3 T RT A41NM E3WE 1996102400858 19961024 00858 WP 1996 10 24 VTZA96390 2 19960922 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE3311 01514 WP RIGHT MALFUNCTIONED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 EA 27 327UE 41080 FLT 6160 - IAD-TYS - ABORTED TAKEOFF DUE TO RIGHT ENGINE SLOW TO MADE TORQUE. THE AIRCRAFT RETURNED TO GATE WITH NO FUR THER PROBLEMS. MAINTENANCE RAN AIRCRAFT AND WAS WITHIN MANUAL LIMITS. THE AIRCRAFT WAS RELEASED AND APPROVED FOR SERVI CE. (M) 2 L 7 2 4T 3 T RT A41NM E3WE 1996102400859 19961024 00859 EU 1996 10 24 VTZA96389 1 19960921 A 2770 GUST LOCK JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT DEFECTIVE A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 312UE 41025 FLT 6198 - IAD-BDL - ABORTED TAKEOFF DUE TO A CONFIGURATION WARNING INDICATION. THE AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. CREW RESET GUST LOCK HANDLE. THE AIRCRAFT WAS RELEASED AND APPROVED FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1996102400860 19961024 00860 EU 1996 10 24 VTZA96393 1 19960924 A 3233 6158E RETRACTION JACK BAG JETSTM JETSTM3201 1500217 EU NLG FAILED A VTZA O OTHER J WARNING INDICATION CL CLIMB 1 EA 27 476UE 884 FLT 6152 - BGM-IAD - DURING CLIMB, CONTINUED FLIGHT TO IAD WITH ONE DISCREPANCY DUE TO NOSE GEAR INTRANSIT LIGHT WOULD N OT EXTINGUISH. AIRCRAFT LANDED AND WENT TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED RETRACTION JACK. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996102400861 19961024 00861 WP 1996 10 24 VTZA96392 2 19960924 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE3311 01514 WP RIGHT LOW POWER A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 EA 27 327UE 41080 FLT NR 6150 - IAD-EWR - ABORTED TAKEOFF DUE TO RIGHT ENGINE SLOW TO MAKE TORQUE. THE AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE RAN AIRCRAFT, ADJUSTED MAX PROP SPEED, OPS CHECK OK. THE AIRCRAFT WAS RELEASED AND APPRO VED FOR SERVICE. (M) 2 L 7 2 4T 3 T RT A41NM E3WE 1996102400862 19961024 00862 EU 1996 10 24 VTZA96386 1 19960920 A 3222 14132029 NOSE STRUT JETAIR JETSTM JETSTM4101 1500501 EU NLG UNDER INFLATED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 306UE 41020 FLT NR 6305 - IAD-JFK - ABORTED TAKEOFF DUE TO NUMEROUS WARNING ON GROUND INCLUDING LEFT STICK SHAKER ASSOCIATED WITH NO SE SQUAT SWITCH. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE SERVICED STRUT WITH NITROGEN TO CORRE CT INFLATION. AIRCRAFT WAS RELEASED AND APPROVED FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1996102400863 19961024 00863 EU 1996 10 24 VTZA96385 1 19960919 A 2731 189982001 SCREW JACK JETAIR JETSTM JETSTM4101 1500501 EU ELEV TRIM LACK OF LUBE A VTZA K NONE F FLT CONT AFFECTED CR CRUISE 1 EA 27 302UE 41013 FLT 6222 - JFK-IAD - DURING CRUISE, A SCHEDULED LANDING WITH ONE DISCREPANCY TO ELEVATOR TRIM IS STICKY IN FLIGHT. AIRC RAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND LUBRICATED ELEVATOR TRIM, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996102400864 19961024 00864 EU 1996 10 24 REXA96046 1 19960918 A 8200 WATER METH SYST BAG JETSTM JETSTM3101 1500215 EU RT ENGINE MALFUNCTIONED A REXA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 300PX 652 WATER METHANOL SYSTEM CAUSES TORQUE SURGE. DEFERRED PER MEL 82-00-00. DM16329. PERFORMED OPERATIONAL CHECK OF WATER M ETHANOL SYSTEM, NO DEFECTS NOTED. OK FOR SERVICE. (M) 2 L 7 2 4T RT A21EU 1996102400865 19961024 00865 NM 1996 10 24 TWRA96314 1 19960913 A 3397 591215 WIRE BOEING 747 747282B 1384860 NM CABIN BROKEN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 610FF 20501 DURING DAILY CHECK, FOUND UPPER DECK FLOOR STRIP EVAC LIGHT IS INOP. REPLACED WIRE FROM POWER SOURCE TO EVAC STRIP. OP S CHECKED NORMAL PER MM 33-59-00. (M) 2 L 7 4 4F A20WE 1996102400866 19961024 00866 NM 1996 10 24 TWRA96313 1 19960912 A 3397 WIRE BOEING 747 747238B 1384828 NM CABIN BROKEN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 614FF 20534 DURING DAILY CHECK, FOUND RIGHT WING THIRD OVERWING EVAC LIGHT IS INOP. FOUND BROKEN WIRE. REPAIRED WIRE, OPS CHECKED GOOD PER MM 33-51-00 PAGE 501. (M) 2 L 7 4 4F A20WE 1996102400867 19961024 00867 NM 1996 10 24 TAOA099608 1 19960916 A 3350 079123 LIGHT BOEING 727 727254 138408L NM CABIN MISSING A TAOA K NONE O OTHER IN INSP/MAINT 1 EA 15 915TS 20252 EMERGENCY AISLE PATH LIGHT BROKEN IN REAR OF AIRCRAFT. REPLACED AFT SECTION OF EMERGENCY PATH LIGHT TRACK. (M) 2 L 7 3 4F A3WE 1996102400868 19961024 00868 NM 1996 10 24 TAOA099605 1 19960909 A 2823 MS29513223 O-RING BOEING 727 727225 1384077 NM NR 3 FUEL SO VLV LEAKING A TAOA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 EA 15 918TS 20445 ODOR OF FUEL IN THE CABIN ON THE GROUND WITH THE APU RUNNING AND PACKS ON. REPLACED O-RINGS ON NR 3 ENGINE FUEL SHUTOFF VALVE. RAN NR 3 ENGINE OPERATES NORMAL AND NO LEAKS FOND, PER MM CHAPTER 28-22-1. (M) 2 L 7 3 4F A3WE 1996102400869 19961024 00869 EU 1996 10 24 SIMA962662 1 19960922 A 3350 SWITCH GUARD SAAB SF340 340B 7860101 EU COCKPIT OUT OF ADJUST A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 359SB 340B359 SJT - FLT 3915 - AFTER LANDING AND SHUTDOWN CREW REPORTED THAT EMERGENCY LIGHTS STAY ON IRRELEVANT TO SWITCH POSITION IN COCKPIT. MAINTENANCE FOUND SWITCH GUARD AT FLIGHT ATTENDANT POSITION TO BE DEPRESSING EMERGENCY LIGHT BUTTON KEEPING L IGHTS ON. REMOVED AND REINSTALLED GUARD. OPS CHECK SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1996102400870 19961024 00870 EU 1996 10 24 REXA96045 1 19960916 A 2611 SMOKE DETECTOR FENWAL 72000211000 SAAB SF340 SF340A 7850100 EU CARGO COMPT MALFUNCTIONED A REXA F ACTIVATE FIRE EXT. J WARNING INDICATION CL CLIMB 1 SO 25 401BH A907 340A057 CARGO SMOKE LIGHT CAME ON IN FLIGHT. REMOVED AND REPLACED CARGO SMOKE DETECTOR IAW AMM. WIRES CHECKED GOOD WITH MEGOME TER. SYSTEM GROUND CHECKED GOOD. (M) 2 L 7 2 4T RT A52EU 1996102400871 19961024 00871 EU 1996 10 24 REXA96044 1 19960916 A 2611 SMOKE DETECTOR FENWAL 72111211000 SAAB SF340 SF340A 7850100 EU AVIONICS BAY DIRTY A REXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 341PX 340A142 AVIONICS SMOKE ON CWP. CLENAED AVIONICS SMOKE DETECTOR AND CANNON PLUG. OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1996102400872 19961024 00872 EU 1996 10 24 REXA96043 1 19960916 A 2910 L38710SA SWIVEL SAAB SF340 SF340A 7850100 EU RT MLG BROKEN A REXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 320PX 340A027 HYDRAULIC CAPTION IN FLIGHT. HYDRAULIC MAIN PRESSURE LOW. PUMPED GEAR AND FLAPS DOWN. REMOVED AND REPLACED RIGHT HYDR AULIC SWIVEL AT UPLOCK RELEASE ACTUATOR. SERVICED SYSTEM, BLED SWIVEL. PERFORMED GEAR SWINGS, SWINGS CHECK GOOD. NO L EAKS NOTED. OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1996102400873 19961024 00873 WP 1996 10 24 REXA96042 2 19960908 A 7210 31032331 PROP GEAR CASE BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110U 01514 WP LT ENGINE SHEARED TOOTH A REXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 319PX 691 LEFT ENGINE FAILED IN FLIGHT. REMOVED AND REPLACED ENGINE. (M) 2 L 7 2 4T 4 T RT A21EU E4WE 1996102400874 19961024 00874 EU 1996 10 24 REXA96041 1 19960908 A 2611 SMOKE DETECTOR FENWAL 72111211000 SAAB SF340 SF340A 7850100 EU LAVATORY MALFUNCTIONED A REXA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 25 404BH A1554 340A061 ABORTED TAKEOFF FOR LAVATORY SMOKE LIGHT. REMOVED AND REPLACED SMOKE DETECTOR ASSEMBLY. (M) 2 L 7 2 4T RT A52EU 1996102400875 19961024 00875 EU 1996 10 24 REXA96040 1 19960817 A 2110 MS3106510SL CONNECTOR BAG JETSTM JETSTM3101 1500215 EU 4 PSI SWITCH BROKEN A REXA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 25 304PX 663 DUCT FAIL AIR OFF CIRCUIT BREAKER POPS. REMOVED AND REPLACED PSI SWITCH CANNON PLUG. SYSTEM TEST GOOD IAW AMM. OK FOR SERVICE CLEARED DEFER. (M) 2 L 7 2 4T RT A21EU 1996102400876 19961024 00876 EU 1996 10 24 REXA96039 1 19960813 A 7712 TQ SIG COND BAG JETSTM JETSTM3101 1500215 EU NR 1 ENGINE DRIFTING A REXA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 25 319PX 691 LEFT TORQUE GAUGE READS NO LOWER THAN 22 PERCENT TORQUE AT GROUND IDLE, NO THRUST 20 PERCENT AT SHUTDOWN. SWAPPED TO BR IDGE NR 1 ON RIGHT SIGNAL CONDITIONER AND CALIBRATED IAW JS MM 72-00. GOOD FOR SERVICE. (M) 2 L 7 2 4T RT A21EU 1996102400877 19961024 00877 NE 1996 10 24 REXA96038 2 19960812 A 7230 6053TO7G05 LINKAGE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE COMPRESSOR LACK OF LUBE A REXA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 25 341PX 340A142 GEE367213 RIGHT ENGINE EXCEEDED 930 F ON TAKEOFF ROLL. ABORTED TAKEOFF. LUBED INLET GUIDE VANE LINKAGE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE6 1996102400878 19961024 00878 NE 1996 10 24 REXA96035 2 19960623 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LEFT FAILED A REXA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 25 325PX 340A051 ABORTED TO WITH LOUD LEFT ENGINE BANG ALONG WITH TORQUE ROLL BACK AND ITT RISE (APPROX 950). REPLACED LEFT ENGIEN IAW S F AMM 71-00-00, OPS CHECK GOOD. (M) 2 L 7 2 4T 4 T RT A52EU E8NE6 1996102400879 19961024 00879 EU 1996 10 24 REXA96047 1 19960922 A 3000 FACIA PANEL BAG JETSTM JETSTM3101 1500215 EU LT COCKPIT SHORTED A REXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 25 307PX 673 AFTER TAKEOFF A THIN STREAM OF SMOKE CAME FROM ICE PROTECTION SWITCH. REMOVED AND REPLACED LEFT FACIA PANEL. INSPECTED ICE PROTECTION SWITCH. FOUND TO BE IN GOOD ORDER. AIRCRAFT GOOD FOR CONTINUED SERVICE. (M) 2 L 7 2 4T RT A21EU 1996102400880 19961024 00880 WP 1996 10 24 ORJA9654 1 19960922 A 3350 60030451 BATTERY PACK GRIMES DOUG DC9 DC987 3022087 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 752RA 49780 ROWS 12-15 SEAT MOUNTED EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1996102400881 19961024 00881 WP 1996 10 24 ORJA9655 1 19960922 A 3350 FUSE DOUG DC9 DC987 3022087 WP CABIN BLEW A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 752RA 49780 EMERGENCY LIGHTS ROWS 16-18 OUT. INSTALLED NEW FUSE IN EMERGENCY POWER PACK, ROW 20 DEF. OPERATIONAL CHECK NORMAL. (M ) 2 L 7 2 4F RT A6WE 1996102400882 19961024 00882 WP 1996 10 24 ORJA9657 1 19960920 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN CUT A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 823RA 49889 FORWARD FIRST CLASS EMERGENCY LIGHTS INOP. RETERMINATED BROKEN WIRE BEHIND FORWARD COAT CLOSET. OPS CHECK NORMAL. (M) 2 L 7 2 4F A6WE 1996102400883 19961024 00883 WP 1996 10 24 ORJA9658 1 19960921 A 3260 PROX SENSOR DOUG DC9 DC982 3022082 WP NLG OUT OF ADJUST A ORJA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 11 842RA 49604 NOSE GEAR RED UNSAFE LIGHT STAYED ON AFTER GEAR HANDLE UP. RECYCLED GEAR PER AOM, LIGHT WENT OUT. CAME BACK ON WITH PU MPS LOW AND OFF. TURNED ENGINE PUMPS TO HIGH. LIGHT EXTINGUISHED. ADJUSTED NOSE GEAR UP/DOWN AND LOCKED PROXIMITY SEN SOR IAW MM 32-60-05. TESTED LANDING GEAR POSITION AND WARNING INDICATING SYSTEM IAW 32-60-00. ALL INDICATIONS NORMAL. (M) 2 L 7 2 4F A6WE 1996102400884 19961024 00884 NE 1996 10 24 ORJA9656 2 19960922 A 7261 7578578 OIL FILTER DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE RT ENGINE CLOGGED A ORJA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 11 754RA 49641 RETURNED TO GATE FOR LEFT OIL STRAINER CLOGGING LIGHT. REMOVED AND REPLACED RIGHT (NR2) ENGINE OIL AND OIL FILTER. LEA KS AND OPS CHECK NORMAL AT THIS TIME. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 1996102400885 19961024 00885 WP 1996 10 24 ORJA9652 1 19960917 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN CUT A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 840RA 49424 ROWS 6 THROUGH 14 AND 25 FLOOR EMERGENCY LIGHTS OUT. FOUND CUT WIRES, RECONNECTED. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1996102400886 19961024 00886 WP 1996 10 24 ORJA9653 1 19960919 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 840RA 49424 FLOOR TRACK EMERGENCY LIGHTS AT ROW 7-14 INOP. REPAIRED BROKEN WIRE RIBBON SHREDDED BY SEAT INSTALLATION. OPS NORMAL. (M) 2 L 7 2 4F A6WE 1996102400887 19961024 00887 WP 1996 10 24 ORJA9651 1 19960915 A 4920 3812761 APU DOUG DC9 DC983 3022083 WP APU COMPT FAILED A ORJA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 11 878RA 16611 P773 53184 WHILE OPERATING ON THE GROUND, APU MADE A LOUD BANG AND SHUT DOWN. APU TROUBLESHOT TO UNCONTAINED TURBINE FAILURE. REP LACED AUXILIARY POWER UNIT. (M) 2 L 7 2 4F RT A6WE 1996102400888 19961024 00888 SW 1996 10 24 MALA965135 1 19960917 A 5320 2722085 DOOR FRAME SWRNGN SA227 SA227AC 8780603 SW BS 438 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 423MA AC636 DURING BLOCK INSPECTION IN MSP, MAINTENANCE COMPLETED REPAIR TO FUSELAGE FORWARD CARGO DOOR FRAME P/N 27-22085 AT FS 438 DUE TO .250 INCH CRACK NOTED IN AREA OF THE DOOR GAS STRUT SUPPORT LOWER MOUNT HOLE. REMOVED CRACKED AREA AND INSTALLE D REPAIR DOUBLERS IAW FAC ARP 53-20-9503. (M) 2 L 7 2 4T RT A8SW 1996102400889 19961024 00889 NM 1996 10 24 MALA965136 1 19960916 A 3260 3261J23 CONNECTOR DHAV DHC8 DHC8102 2809003 NM LT MLG DOOR FAILED A MALA O OTHER N FALSE WARNING CR CRUISE 1 GL 15 826MA 330 FLT 3195 - EN ROUTE TO DTW, THE LEFT ADVISORY LANDING GEAR DOOR LIGHT INTERMITTENTLY ILLUMINATES DURING FLIGHT. MAINTEN ANCE REPLACED A CANNON PLUG CONNECTOR AT 3261-J23. ALL CHECKS SATISFACTORY. (M) 2 H 7 2 4T RT A13NM 1996102400890 19961024 00890 SW 1996 10 24 MALA965137 1 19960918 A 3260 2782186057 POSITION IND SWRNGN SA227 SA227AC 8780603 SW RT MLG FAILED A MALA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 15 424MA AC639 FLT 2903 - ON APPROACH TO DTW, THE RIGHT GEAR DOWN LIGHT FAILED TO ILLUMINATE UPON GEAR EXTENSION. THE INDICATOR LIGHT WOULD ILLUMINATE INTERMITTENTLY WHEN WIGGLED. THE CREW PERFORMED AND EMERGENCY EXTENSION AND LANDED AT DTW WITHOUT INCI DENT. MAINTENANCE REPLACED THE LANDING GEAR POSITION INDICATOR. ALL CHECKS SATISFACTORY. (M) 2 L 7 2 4T RT A8SW 1996102400891 19961024 00891 SW 1996 10 24 MALA965138 1 19960918 A 7714 2719157003 RPM INDICATOR SWRNGN SA227 SA227AC 8780603 SW RT ENGINE FAILED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 442MA AC725 FLT 3395 - AFTER TAKEOFF FROM DTW, THE RIGHT ENGINE RPM DROPPED TO 97 PERCENT. THE AIRCRAFT RETURNED TO DTW. MAINTENAN CE REPLACED THE RIGHT RPM INDICATOR. ALL CHECKS SATISFACTORY. (M) 2 L 7 2 4T RT A8SW 1996102400892 19961024 00892 SW 1996 10 24 MALA965139 1 19960919 A 3260 1EN516 SWITCH SWRNGN SA227 SA227AC 8780603 SW RT MLG FAILED A MALA O OTHER N FALSE WARNING AP APPROACH 1 GL 15 2692P AC658B FLT 3009 - ON APPROACH TO MSP, THE RIGHT GEAR INTRANSIT LIGHT FAILED TO ILLUMINATE UPON GEAR EXTENSION. MAINTENANCE REP LACED THE RIGHT INBOARD GEAR DOWN POSITION SWITCH. ALL CHECKS SATISFACTORY. (M) 2 L 7 2 4T RT A8SW 1996102400893 19961024 00893 SW 1996 10 24 MALA965140 1 19960918 A 5330 SKIN SWRNGN SA227 SA227AC 8780603 SW BS 241 CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 423MA AC636 DURING SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND CHAFE DAMAGE AT FS 241 AND ON BOTH SIDES OF BL 0. CHAFE DAMAGE IS APPROX .025 DEEP AND .125 INCH IN DIAMETER. FABRICATED AND INSTALLED AN EXTERNAL REPAIR DOUBLER (.050 INCH AND 4 INCH BY 5 INCH) IAW FAC SRM 51-90-04 PG 7-8 REV JUN 1/93. (M) 2 L 7 2 4T RT A8SW 1996102400894 19961024 00894 SW 1996 10 24 MALA965141 1 19960918 A 5330 SKIN SWRNGN SA227 SA227AC 8780603 SW BS 491 OVERSIZED HOLES A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 423MA AC636 DURING A SCHEDULED INSPECTION IN MSP, AFTER REMOVAL OF AFT LOWER CARGO DOOR FRAME FILLET, P/N 27-24082-9003 AT FS 491, M AINTENANCE FOUND THE FUSELAGE SKIN RIVET HOLES TO BE OVERSIZED (CARGO DOOR SURROUND SKIN). REMOVED AND REPLACED THE AFT LOWER SKIN SECTION (7 INCH BY 7 INCH) AND INSTALLED A REPAIR DOUBLER OVER SKIN SPLICE (2.5 INCH BY 3.5 INCH). ALL WORK COMPLETED IAW FAC SRM 51-90-04 PGS 7-8 REV JUN 1/93 AND AEROTECH DESIGNS EA01-96090 REV A, DATED SEPT 18/96. (M) 2 L 7 2 4T RT A8SW 1996102400895 19961024 00895 SW 1996 10 24 MALA965142 1 19960918 A 5230 SKIN SWRNGN SA227 SA227AC 8780603 SW CARGO DOOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 423MA AC636 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE AFT UPPER CARGO DOOR SKIN JUST FORWARD OF FS 491 CHAFED APPR OX .50 INCH. CHAFED DAMAGE CAUSED FROM CARGO DOOR HINGE PIN END, HINGE PIN LENGTH DETERMINED TO BE TOO LONG. CARGO SKI N AREA REPAIR IAW FAC ARP 52-30-9130 DATED JUNE 20, 1991. (M) 2 L 7 2 4T RT A8SW 1996102400896 19961024 00896 WP 1996 10 24 ASAA9680200 1 19960912 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 974AS 53450 PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996102400897 19961024 00897 WP 1996 10 24 ASAA9680199 1 19960909 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 967AS 49103 SEA - DURNG MAINTENANCE CHECK, THE EMERGENCY LIGHTS IN THE FORWARD GALLEY, AT THE L1 DOOR AND IN THE COCKPIT ILLUMINATED WHEN THE AIRCRAFT BATTERY SWITCH WAS TURNED OFF. REPLACED THE BATTERY PACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996102400898 19961024 00898 WP 1996 10 24 ASAA9680179 1 19960822 A 3350 S103 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 967AS 49103 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996102400899 19961024 00899 NM 1996 10 24 ASAA9640082 1 19960917 A 3397 WIRE BOEING 737 7374S3 1384711 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 786AS 24795 SEA - DURING MAINTENANCE CEHCK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT THE FORWARD OVERWING ARE A. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996102400900 19961024 00900 NM 1996 10 24 ASAA9640081 1 19960916 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 779AS 25111 SEA - DURING MAINTENANCE CHECK, BOTH THE FORWARD AND AFT EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED BOTH FORWARD AND AFT WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996102400901 19961024 00901 NM 1996 10 24 ASAA9640080 1 19960915 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 763AS 25100 ANC - DURING MAINTENANCE CHECK, THE AFT RED EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996102400902 19961024 00902 NM 1996 10 24 ASAA9640079 1 19960915 A 3397 WIRE BOEING 737 7374S3 1384711 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 786AS 24795 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROW 14. RECONNECT ED LOOSE WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996102400903 19961024 00903 NM 1996 10 24 ASAA9640078 1 19960913 A 3397 WIRE BOEING 737 7374S3 1384711 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 786AS 24795 SEA - FLT 467 - PRIOR TO FLIGHT, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROW 15. RECONNEC TED/REPAIRED WIRING AT LIGHT ASSEMBLY AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996102400904 19961024 00904 NM 1996 10 24 ASAA9640077 1 19960912 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 771AS 25104 SEA - FLT 158 - DURING CREW PREFLIGHT, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 15 THR OUGH 19. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996102400905 19961024 00905 EU 1996 10 24 AWXA960527 1 19960926 A 3234 210TSO7Y01 CONTROL LEVER AIRBUS 320 A320231 3930325 EU LANDING GEAR INOPERATIVE A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 633AW 2629 658 082 PHX - FLT 2082 - AIR TURN BACK, LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. FOUND NO POWER TO RELAY 48GA. FOUND LAND ING CONTROL LEVER FAULTY. REMOVED AND REPLACED LANDING GEAR CONTROL LEVER PER AMM 32-31-11, PG 401-406. (M) 2 L 7 2 4F RT A28NM 1996102400906 19961024 00906 NM 1996 10 24 AWXA960518 1 19960902 A 5315 AND101362404 FLOOR BEAM BOEING 737 7373S3 1384711 NM BS 328 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 PAE - FLT 7818 - DURING ROUTINE SCHEDULED C-10 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM BS 328 - LBL 28. REPAIR ED FLOOR BEAM AT BS 328, LBL 28 TO 65 PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1996102400907 19961024 00907 NM 1996 10 24 AWXA960517 1 19960910 A 5754 SKIN BOEING 737 7373S3 1384711 NM NR 1 LE FLAP CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 DURING ROUTINE SCHEDULED C-10 MAINTENANCE CHECK, FOUND SEVERAL SMALL CRACKS IN OUTER SKIN COMING FROM RIVETS AT CENTER I NBOARD STOP MOUNT ON NR 1 SLAT. REPAIRED PER DWG 65C30133PT2. (M) 2 L 7 2 4F RT A16WE 1996102400908 19961024 00908 NM 1996 10 24 AWXA960516 1 19960903 A 5315 FLOOR BEAM BOEING 737 7373S3 1384711 NM BS 344 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 DURING ROUTINE SCHEDULED C-10 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM BS 344, LBL 28 TO LBL 56 IN NUMEROUS PLAC ES. REMOVED UPPER CHORD, FABRICATED AND INSTALLED REPLACEMENT AT BS 344, IAW SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1996102400909 19961024 00909 NM 1996 10 24 AWXA960515 1 19960903 A 5320 MOPSILL BOEING 737 7373S3 1384711 NM BS 304-328 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 313AW 23712 PAE - FLT 7818 - DURING ROUTINE SCHEDULED C-10 MAINTENANCE CHECK, FOUND CORROSION ON FORWARD ENTRY DOOR MOPSILL, STATION 304-328, LBL 42. REMOVED AND REPLACED FORWARD MOPSILL, STATION 304-328, LBL 42 PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1996102400910 19961024 00910 NM 1996 10 24 WRLA96034 1 19960829 A 2432 021932 BATTERY CHARGER DOUG MD11 MD11 3023602 NM FWD ACCY COMPT DISCHARGED A WRLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 273WA 48519 DURING TAXING OUT, FLIGHT CREW RECEIVED BATTERY CHARGER FAILURE 'ALERT'. AIR CRAFT RETURNED TO GATE WITHOUT FURTHER INC IDENT. REMOVED AND REPLACED AIRCRA FT BATTERIES. OPS CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A22WE 1996102400911 19961024 00911 NM 1996 10 24 WRLA96035 1 19960904 A 3234 ABH7357513 SELECTOR DOUG MD11 MD11 3023602 NM LANDING GEAR BINDING A WRLA O OTHER J WARNING INDICATION DE DESCENT 1 EA 27 280WA 48458 WHEN ON FINAL APPROACH AT EDDB, FLIGHT CREW SELECTED GEAR DOWN. ALL GEAR INDICATION UNSAFE. FLIGHT CREW UTILIZED ABNOR MAL PROCEDURES EXTENDING LANDING GEAR, UTILIZING ALTERNATE GEAR HANDLE. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MX P ERSONNEL AT EDDB, WERE UNABLE TO INDENTIFY ANY MALFUNCTION. ALL LANDING GEAR ASSEMBLY WERE PINNED IN DOWN POSITION, AIR CRAFT WAS FERRIED TO EHAM FOR FURTHER TROUBLESHOOTING. AT EHAM, MAINTENANCE PERSONNEL JACKED AIRCRAFT, PERFORMED GEAR S WING, IDENTIFIED THAT LANDING GEAR CONTROL HANDLE WAS NOT GOING FORWARD INTO DETENT WHEN DOWN POSITION WAS SELECTED. GE AR HANDLE CLEANED PER MM 32-31-00, PAGE 703, PERFORMED GEAR SWING, ALL NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A22WE 1996102400912 19961024 00912 WP 1996 10 24 WRLA96039 1 19960925 A 7722 8DJ185WAA1 EGT INDICATOR DOUG DC10 DC1030 3023501 WP NR 3 ENGINE FAILED A WRLA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 9MMAW 46959 DURING TAXI OUT FROM GATE, FLIGHT CREW NOTED FAILURE OF NR 3 ENGINE EGT INDICATION. FLIGHT CREW ELECTED TO RETURN TO GA TE FOR MAINTENANCE ACTION. AIRCRAFT RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED FAULTY INDICATOR . GROUND RUN PERFORMED WITH NO FAULTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A22WE 1996102400914 19961024 00914 WP 1996 10 24 USAAD96136 1 19960929 A 3350 AD20131A BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 918VJ 48138 FLOOR PATH EMERGENCY LIGHTS DIM AT SECTIONS 2, 3, 4, AND 5. REPLACED BATTERY PACK AT AFT FLOOR PATH POWER SUPPLY. (M) 2 L 7 2 4F A6WE 1996102400915 19961024 00915 NE 1996 10 24 USAABB96038 2 19961002 A 7321 ESC10304C4 FUEL CONTROL BOEING 757 757225 1384959 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 603AU 4301 22198 30543 SFO - FL 74 - ON CLIMB FROM SFO, LEFT ENGINE WOULD NOT DEVELOP CLIMB POWER WITHOUT EXCEEDING EGT LIMITS. FUEL FLOW WAS MUCH HIGHER ON THE LEFT ENGINE. FLIGHT RETURNED TO SFO AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE L EFT ENGINE EEC LIMITER. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 1996102400916 19961024 00916 NM 1996 10 24 USAABB96034 1 19960926 A 3610 16J081 DUCT BOEING 757 757225 1384959 NM RT ENGINE LEAKING A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 608AU 22204 SFO - FLT 56 - CLIMBING THROUGH 10,000 FEET, CREW RECEIVED RIGHT ENGINE OVERHEAT LIGHT. CREW REDUCED POWER ON THE ENGIN E AND LIGHT EXTINGUISHED. FLIGHT RETURNED TO SFO AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE SIXTH S TAGE HIGH PRESSURE DUCT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 1996102400917 19961024 00917 NM 1996 10 24 USAABB96033 1 19960925 A 3610 B-NUT BOEING 757 757225 1384959 NM RT HPSOV LOOSE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 608AU 22204 SFO - FLT 60 - CLIMB THROUGH 10,000 FEET, CREW RECEIVED RIGHT ENGINE OVERHEAT LIGHT. CREW REDUCED POWER ON THE ENGINE A ND LIGHT EXTINGUISHED. FLIGHT RETURNED TO SFO AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE UPPER RIGHT ' B' NUT ON THE HPSOV LOOSE AND TIGHTENED IT. THE ENGINE WAS RUN AT TAKEOFF POWER FOR FIVE MINUTES WITH NO RECURRANCE OF THE PROBLEM. (M) 2 L 7 2 4F RT A2NM 1996102400918 19961024 00918 NM 1996 10 24 USAABB96036 1 19961002 A 3350 LIGHTS BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 618AU 22210 BDL - EXTERIOR EMERGENCY LIGHTS WOULD NOT TEST FROM THE NOSE LANDING GEAR TEST SWITCH. MAINTENANCE REPAIRED WIRING AT S WITCH S10035. (M) 2 L 7 2 4F RT A2NM 1996102400919 19961024 00919 NM 1996 10 24 USAASB96204 1 19961003 A 5610 5717623116 SLIDING WINDOW BOEING 737 737201 1384454 NM RT COCKPIT CRACKED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 247US 25854 22754 PIT - FLT 1111 - WHILE EN ROUTE TO IND, THE FLIGHT OFFICERS SLIDING WINDOW DEVELOPED A CRACK. AFTER CHECKING WITH MAINT ENANCE, IT WAS DECIDED TO DIVERT TO PIT DUE TO POSSIBLE ICING CONDITIONS. NO EMERGENCY WAS DECLARED AND THE FLIGHT LAND ED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FLIGHT OFFICERS SLIDING WINDOW AND THE WINDOW HEAT CONTROL UNIT ( P/N 231-2). OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1996102400920 19961024 00920 EU 1996 10 24 Y2PA96079 1 19961002 A 3260 A2238012 SWITCH AMD FALC20 FALCON 2720302 EU RT MLG FAILED A Y2PA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 23 819AA 372 26 DSM - RIGHT MAIN GEAR GREEN LIGHT DID NOT COME ON DURING NORMAL EXTENSION. AIRCRAFT FLIGHT MANUAL EMERGENCY EXTENSION P ROCEDURE USED TO EXTEND GEAR AT WHICH TIME GREEN LIGHT ILLUMINATED. AIRCRAFT LANDED WITHOUT INCIDENT AT INTENDED DESTIN ATION AT DSM. NO OTHER EMERGENCY PROCEDURES REQUIRED. TROUBLESHOOTING DETERMINED THAT THE RIGHT GEAR DOOR ACTUATOR POS ITION SWITCH WAS FAULTY AND PREVENTED THE RIGHT MAIN GEAR FROM SEQUENCING AND EXTENDING NORMALLY. THE GEAR DOOR ACTUATO R SWITCH WAS REPLACED AND THE LANDING GEAR CYCLED WITH NO DEFECTS NOTED. (M) 2 L 7 2 4F A7EU 1996102400921 19961024 00921 EU 1996 10 24 SIMA962771 1 19961003 A 3350 SWITCH AEROSP ATR42 ATR42300 8680920 EU CABIN LOOSE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 135MQ 135 ORD - FLT 4181 - RIGHT FORWARD EMERGENCY EXIT BOTTOM LIGHT INOP. RESECURED EMERGENCY LIGHT SWITCH. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996102400922 19961024 00922 EU 1996 10 24 SIMA962781 1 19961004 A 3350 3011180 POWER SUPPLY AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 430MQ 1366 0136 LAN - FORWARD AND FLOOR EMERGENCY LIGHTS INOP. RAI'D POWER SUPPLY 3WL (2 UNITS) AND 29WL (2 UNITS). AIRCRAFT WAS RETUR NED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996102400923 19961024 00923 EU 1996 10 24 96ZZZM1423 1 19961004 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 430MQ 644 0136 LAN - FORWARD AND FLOOR EMERGENCY LIGHTS INOP. RAI'D POWER SUPPLY 3WL (2 UNITS) AND 29WL (2 UNITS). AIRCRAFT WAS RETUR NED TO SERVICE. REFERENCE SIMA962781. 2 H 7 2 4T RT A53EU 1996102400924 19961024 00924 EU 1996 10 24 96ZZZM1424 1 19961004 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 430MQ 10281 0136 LAN - FORWARD AND FLOOR EMERGENCY LIGHTS INOP. RAI'D POWER SUPPLY 3WL (2 UNITS) AND 29WL (2 UNITS). AIRCRAFT WAS RETUR NED TO SERVICE. REFERENCE SIMA962781. 2 H 7 2 4T RT A53EU 1996102400925 19961024 00925 CE 1996 10 24 PLG92696JB1 1 19960926 A 7722 1143800045 ITT INDICATOR BEECH 1900 1900C 1154161 CE RIGHT FAILED A PLGA A UNSCHED LANDING O OTHER CR CRUISE 1 NE 05 819BE UB62 FLT 4356 - ALB-BOS - DURING FLIGHT, THE RIGHT HAND ITT INDICATOR FAILED. AIRCRAFT DIVERTED BACK TO ALB AND LANDED WITHO UT INCIDENT. MAINTENANCE REPLACED THE RIGHT ITT INDICATOR AND RECALIBRATED THE SYSTEM. ALL CHECKS WERE GOOD AND THE AI RCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1996102400926 19961024 00926 NM 1996 10 24 MZZA96078 1 19960927 A 5330 SKIN BOEING 727 727227 1384078 NM BS 1151.5 GOUGED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 89427 21365 DURING B-CHECK, LEFT AFT FUSELAGE SKIN HAS 2 DEEP GOUGES LOCATED AT BS 1151.5 AND RIGHT BELOW STRINGER 21L. CUT OUT DAM AGED AREA, FABRICATED FILLER FROM .080, 2024T3 ALUMINUM SHEET AND REPAIR DOUBLER FROM .090 2024T3. INSTALLED REPAIR WIT H SOLID FASTENERS PER SRM 53-30-3. APPLIED FINISH COAT PER MM 51-20-00. (M) 2 L 7 3 4F A3WE 1996102400927 19961024 00927 WP 1996 10 24 GTIA96NK210 1 19960930 A 5220 DOOR LOCK DOUG DC9 DC932 3022066 WP RT EMER EXIT OUT OF ADJUST A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 941ML 47131 REF - CABIN LOG ENTRY NR 1 FROM C/N 8113 EMERGENCY EXIT HATCH ROW 15. AIRCRAFT RIGHT COMES LOOSE ON LANDING. INSPECTED AND ADJUSTED DOOR LOCK BAR IAW DC-9 MM 52-20-0. (M) 2 L 7 2 4F A6WE 1996102400928 19961024 00928 WP 1996 10 24 GTIA96NK209 1 19960927 A 3350 1001191 LIGHT DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 934ML 47526 L1 DOOR EMERGENCY LIGHT ASSEMBLY INTERMITTENT. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY. OPS CHECKS GOOD PER 33-5 0-1. (M) 2 L 7 2 4F A6WE 1996102400929 19961024 00929 WP 1996 10 24 GTIA96NK207 1 19960924 A 2540 WALL COVERING DOUG DC9 DC932 3022066 WP LT LAV WALL CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 947ML 47514 DURING X-RAY INSPECTION OF AFT PRESSURE BULKHEAD VENTRAL STAIR DOOR FRAME A1.375 INCH CRACK WAS NOTED AT UPPER LEFT CORN ER APPROX 6 INCH OUTBOARD OF CENTER RADIUS AT 11 O'CLOCK POSITION. DETAILED LOW FREQUENCY EDDY CURRENT AND A DETAILED V ISUAL INSPECTION OF AREA REVEALED THAT CRACK WAS IN THE LAV WALL COVERING (PLASTIC). THIS WAS CONFIRMED BY PLACING THE X-RAY FILM AND THE WALL COVERING TOGETHER. THE CRACK IN THE COVERING WAS EXACTLY THE SAME AS ON THE FILM. (M) 2 L 7 2 4F A6WE 1996102400930 19961024 00930 WP 1996 10 24 GAIA9627 1 19961004 A 3240 8794650 BRAKE LINE CVAC 340 34031 2422704 WP RT MLG RUPTURED A A GAIA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 SW 07 3412 32 FLT 475 - CVG-CLE - DURIGN TAXI AFTER NORMAL LANDING AT CLE A LOSS OF BRAKING ACTION WAS NOTICED. EMERGENCY AIR BRAKES WERE APPLIED AND THE AIRCRAFT WAS STOPPED ON THE RUNWAY. THE AIRCRAFT WAS TOWED OFF THE RUNWAY. INVESTIGATION REVEALED THAT THE RIGHT INBOARD FLEXIBLE BRAKE LINE HAD RUPTURED BETWEEN THE MLG AND THE BRAKE HOUSING. THE LINE WAS REPLACED T HE BRAKES WERE BLED AND THE AIRCRAFT WAS SERVICED IAW THE CV MM. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4R 6A6 1996102400931 19961024 00931 NM 1996 10 24 F3LA96027 1 19960930 A 3230 2732512 CONTROL CABLE BOEING 737 737301 1384611 NM RT MLG OUT OF ADJ A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 PAE - LANDING GEAR WILL NOT RETRACT AFTER TAKEOFF. AFTER EXECUTING CHECK LIST, LANDING GEAR WAS SUCCESSFULLY RAISED AND THEN LOWERED. FOUND TELEFLEX CABLE ON RIGHT MAIN LANDING GEAR FOR GROUND SPOILER INTERLOCK VALVE OUT OF ADJUSTMENT. R E-RIGGED TELEFLEX CABLE AND FUNCTIONAL TEST GOOD PER MM 27-62-00. (M) 2 L 7 2 4F RT A16WE 1996102400932 19961024 00932 NM 1996 10 24 EISA96194 1 19961011 A 2121 215201 GASPER FAN BOEING 727 72725 1384006 NM BS 400 INOPERATIVE A EISA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 290NE 18195 18972 WHEN GASPER FAN WAS TURNED ON, A SMOKEY SMELL ENTERED THE COCKPIT. PLACARDED GASPER FAN PER MEL 21-24. REMOVED AND REP LACED GASPER FAN, OPS TEST OK. (M) 2 L 7 3 4F A3WE 1996102400933 19961024 00933 WP 1996 10 24 ASAA9680212 1 19960721 A 2150 20495054 COOLING TURBINE DOUG DC9 DC983 3022083 WP AFT FUSELAGE LEAKING OIL A ASAA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 01 942AS 21211 53052 SEA - DURING DESCENT OUT OF 13,000 FEET ON FLIGHT 393, CREW REPORTED SMELLING AN OILY ODOR AND FUMES IRRITATING TO THE E YES IN THE COCKPIT, APPEARED TO BE COMING FROM THE LEFT AIR CONDITIONING PACK. FOUND THE LEFT COOLING TURBINE LEAKING O IL. REPLACED THE LEFT COOLING TURBINE, BOTH WATER SEPARATOR COALESCERS AND THE RECIRCULATION FAN FILTER. OPERATED BOTH AIR CONDITIONING PACKS WITH ENGINES AND APU FOR PNEUMATIC SUPPLY, NO ODOR OR FUMES NOTED. (M) 2 L 7 2 4F RT A6WE 1996102400934 19961024 00934 WP 1996 10 24 ASAA9680204 1 19960920 A 2560 LANYARD DOUG DC9 DC982 3022082 WP TAILCONE DISCONNECTED A A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 940AS 49825 PDX - DURING MAINTENANCE CHECK, THE TAILCONE EMERGENCY EVACUATION SLIDE DEPLOY LANYARD WAS FOUND DISCONNECTED. RECONNEC TED THE DEPLOY LANYARD AND INSPECTED THE DEPLOY MECHANISM FOR PROPER INSTALLATION AND SECURITY. (M) 2 L 7 2 4F A6WE 1996102400935 19961024 00935 1996 10 24 ASAA9680208 4 19960922 A 2565 C37030105 EVAC SLIDE DOUG DC9 DC982 3022082 WP R1 DOOR BROKEN A A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 938AS 49365 SEA - PRIOR TO DEPARTURE OF FLIGHT 598 - CREW REPORTED THE R1 DOOR EMERGENCY EVACUATION SLIDE DEPLOY LANYARD WAS BROKEN AND DETACHED. REPLACED THE EMERGENCY EVACUATION SLIDE. (M) 2 L 7 2 4F A6WE 1996102400936 19961024 00936 WP 1996 10 24 ASAA9680201 1 19960918 A 5240 49376681 SPRING DOUG DC9 DC982 3022082 WP L2 DOOR BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 933AS 49234 ANC - DURING MAINTENANCE CHECK, THE L2 DOOR HOLD OPEN LATCH SPRING WAS FOUND BROKEN. REPLACED THE SPRING AND OPERATED N ORMALLY. (M) 2 L 7 2 4F A6WE 1996102400937 19961024 00937 NM 1996 10 24 USAABB96035 1 19960930 A 3350 LIGHT BOEING 767 767201 1385125 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 648US 23900 SFO - AFT RIGHT SERVICE DOOR EMERGENCY EXIT LIGHT INOPERTIVE. MAINTENANCE REPAIRED THE LIGHT SOCKET GROUND. (M) 2 L 7 2 4F RT A1NM 1996102400938 19961024 00938 WP 1996 10 24 USAAD96132 1 19960924 A 3244 3910063507 TIRE DOUG DC9 DC931 3022065 WP LT MLG FAILED A USAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 19 931VJ 47188 FLT 1544 - ABE-PIT - ON DEPARTURE, CREW BELIEVED A NOSE TIRE HAD BLOWN. DIVERTED TO PHL WITH GEAR DOWN. NO GREEN DOWN ADN LOCKED LIGHT WAS OBSERVED ON LEFT MAIN GEAR. FOUND LEFT MAIN INBOARD TIRE RECAP FAILED. ALSO, FOUND LEFT MAIN GEAR DOWNLOCK SWITCH HARNESS PARTIALLY MISSING. THIS WAS FOUND ON THE RUNWAY IN ABE. REPLACED BOTH LEFT MAIN WHEEL ASSEMBL IES AND LEFT MAIN GEAR DOWNLOCK SWITCH AND HARNESS. (M) 2 L 7 2 4F A6WE 1996102400940 19961024 00940 WP 1996 10 24 USAAD96134 1 19960923 A 3350 60030451LB BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 824US 49143 AFT SERVICE DOOR CEILING EMERGENCY LIGHTS DID NOT TEST. REPLACED POWER SUPPLY B5-58. (M) 2 L 7 2 4F A6WE 1996102400941 19961024 00941 WP 1996 10 24 USAA960636 1 19960927 A 5347 1802421 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 373 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 830US 28154 49443 PIT - DURING Q-2 CHECK, FOUND CORRODED AREA .75 INCH BY 4 INCH AT STATION 373 SEAT TRACK RIGHT OUTBOARD. SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG 4F. CORROSION TASK NR C58-53302, CORROSION LEVEL 1. (M) 2 L 7 2 4F A6WE 1996102400942 19961024 00942 WP 1996 10 24 USAA960637 1 19960927 A 5311 1097553 BELT FRAME DOUG DC9 DC982 3022082 WP BS 1322 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 830US 28154 49443 PIT - DURING Q2 CHECK, FOUND SEVERAL CORRODED AREAS .5 INCH BY 1 INCH AROUND FASTENERS AT STATION 1322 BELTFRAME L28L TO L28R. INSTALLED BELTFRAME SPLICE PER SRM 53-03 FIG 2A. CORROSION TASK NR C57-55300, CORROSION LEVEL 1. (M) 2 L 7 2 4F A6WE 1996102400943 19961024 00943 NM 1996 10 24 USAA960639 1 19961001 A 5315 6546811 FLOOR BEAM BOEING 737 7374B7 1384702 NM BS 986.5 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT - INSPECTION VISUALLY FOUND LEVEL 2 CORROSION AT CLIP NUT HOLES, LOCATED AT FLOOR BEAM FULL SPAN, BS 986.5. REPLACE D UPPER FLANGE AS PER USAIR EA NR 58809. CORROSION TASK NR C-53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996102400944 19961024 00944 WP 1996 10 24 USAAD96135 1 19961002 A 2424 947F9453 GEN CONTRL UNIT DOUG DC9 DC981 3022081 WP LEFT FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 826US 48026 FLIGHT 320 - CLT-SAV - AFTER TAKEOFF, LEFT GENERATOR FAILED, APU WAS ALREADY ON MEL. RETURNED TO CLT. REPLACED LEFT GC U. (M) 2 L 7 2 4F A6WE 1996102400945 19961024 00945 WP 1996 10 24 USAAA960640 1 19960927 A 5347 CC1802421 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1125-1168 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 830US 28154 49443 PIT - DURING Q-2 CHECK, FOUND SEAT TRACK CORRODD AT LEFT INBOARD SEAT TRACK STATION 1125 TO 1168. SPLICED IN NEW SECTIO N OF SEAT TRACK PER SRM 53-05 FIG 4F. CORROSION TASK NR C58-53302, CORROSION LEVEL 1. (M) 2 L 7 2 4F A6WE 1996102400946 19961024 00946 WP 1996 10 24 USAA960662 1 19960927 A 5347 CC1802421 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 339-360 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 830US 28154 49443 PIT - DURING Q-2 CHECK, FOUND LEVEL ONE SUSPECT, LEVEL TWO CORROSION AT RIGHT INBOARD SEAT TRACK AT STATION 339 TO STATI ON 360. SPLICED IN NEW SECTION OF SEAT TRCK PER SRM 53-05 FIG 4F. CORROSION TASK NR C58-53302, CORROSION LEVEL 1. (M) 2 L 7 2 4F A6WE 1996102400947 19961024 00947 WP 1996 10 24 USAA960661 1 19960927 A 5347 CC1802421 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 321-398 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 830US 28154 49443 PIT - DURING Q-2 CHECK, FOUND SEAT TRACK CORROSION AT RIGHT INBOARD STATION 321 TO STATION 398. SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG 4. CORROSION TASK NR C58-53302, CORROSION LEVEL 1. (M) 2 L 7 2 4F A6WE 1996102400948 19961024 00948 NM 1996 10 24 USAASB96201 1 19960926 A 2932 94P11 PRESS SWITCH BOEING 737 7372Q9 138448M NM 'A' HYD SYSTEM LEAKING A USAA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CL CLIMB 1 EA 19 230AU 21975 CLT - FL 338 - SHORTLY AFTER TAKEOFF, THE 'A' SYSTEM HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED. HYDRAULIC QUANTITY INDIC ATED ZERO. CREW RETURNED TO FIELD AT CLT. FLAPS WERE EXTENDED TO 15 DEGREES WITH ALTERNATE SYSTEM AND THE LANDING GEAR WAS LOWERED MANUALLY. THE FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE LEFT THRUST REVERSER HYDRAULI C PRESSURE SWITCH LEAKING AT THE B-NUT. REPLACED SWITCH. RESERVICED SYSTEM. OPS CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F A16WE 1996102400949 19961024 00949 NM 1996 10 24 USAA960633 1 19960927 A 5320 T-CAP BOEING 737 7374B7 1384702 NM BS 312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 437US 19323 24559 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 10 INCH CORRODED AREA T-CAP BS 312 LBL 33 TO RBL 25. REMOVED AND REPLACED T-CAP, COMPLETED REPAIR. REPAIRED PER TR 53-10-03, SRM 53-10-3. CORROSION TASK NR C53-107-02, CORROSION L EVEL 1. (M) 2 L 7 2 4F RT A16WE 1996102400950 19961024 00950 NM 1996 10 24 USAA960629 1 19960926 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 437US 19323 24559 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1.25 INCH CRACK LBL 4.5 INCH STATION 178 PRESSURE BULKHEAD 6 INCHES BELO W FLOOR LEVEL. INSTALL FILLER AND DOUBLER, REPAIRED PER TR 53-10-07. (M) 2 L 7 2 4F RT A16WE 1996102400951 19961024 00951 NM 1996 10 24 USAA960631 1 19960926 A 5311 FRAME BOEING 737 7374B7 1384702 NM BS 344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 437US 19323 24559 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH FRAME T-CAP CORRODED AT AREAS BY 10, FS 344 FROM RBL 10 THROUGH LBL 15. SPLICED IN NEW T-CAP. REPAIRED PER TR 53-10-01 A. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. ( M) 2 L 7 2 4F RT A16WE 1996102400952 19961024 00952 NM 1996 10 24 USAA960630 1 19960926 A 5330 SKIN BOEING 737 7374B7 1384702 NM BS 480-500 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 437US 19323 24559 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND APPROX 9 INCH BY 8 INCH BY .25 INCH DENT FUSELAGE SKIN NEAR STRINGER 27 R BETWEEN STATION 480 AND 500 PLUS 10. CUT OUT DAMAGED SKIN AND INSTALLED 37 INCHES BY 19 INCHES DOUBLER REPAIR ADDED W EIGHT OF REPAIR IS 5.85 LBS. REPAIRED PER SRM 53-00-01. (M) 2 L 7 2 4F RT A16WE 1996102400953 19961024 00953 NM 1996 10 24 USAA960608 1 19960913 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 235US 41898 22275 CLT - INSPECTION VISUALLY FOUND 1 INCH AND 1.4 INCH SKIN CRACKS LOCATED AT STATION 727A, 2 INCH AND PLUS 7 INCH IN THE FUSELAGE SKIN, RIGHT BL 70 BETWEEN STRINGER 17 AND 18. INSTALLED DOUBLER AS PER BOEING SRM 53-10-1 AND 53-30-3. (M) 2 L 7 2 4F A16WE 1996102400954 19961024 00954 SO 1996 10 24 C2XA96IA243 1 19961002 A 5320 12019264001 BEAM EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12705 120089 IAH - DURING C-CHECK INSPECTION, THE CENTER OMEGA-BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REPAIRED THE AFFECTED PORT ION OF THE BEAM AT FRAMES 37 TO 39, BY USING A BEAM SPLICE AND DOUBLERS. WORK WAS ACCOMPLISHED IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATIONS EC5340-01020, AND EC5340-01043. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO S ERVICE. (M) 2 L 7 2 4T RT A31SO 1996102400955 19961024 00955 SO 1996 10 24 C2XA96IA242 1 19961002 A 5320 12004449001 T-PROFILE EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12705 120089 IAH - DURING C-CHECK INSPECTION, THE T-PROFILE AT FRAME 38 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED T HE AFFECTED T-PROFILE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996102400956 19961024 00956 SO 1996 10 24 C2XA96IA241 1 19961002 A 5320 12006158003 BUTTSTRAP EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12705 120089 IAH - DURING C-CHECK INSPECTION, THE CENTER BUTTSTRAP AT FRAMES 39 TO 44 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996102400957 19961024 00957 SO 1996 10 24 C2XA96IA240 1 19961002 A 5320 12027929001 BUTTSTRAP EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12705 120089 IAH - DURING C-CHECK INSPECTION, THE RIGHT CENTER BUTTSTRAP AT FRAMES 34 TO 38 WAS FOUND TO BE CORRODED. MAINTENANCE RE MOVED AND REPLACED THE AFFECTED BUTTSTRAP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996102400958 19961024 00958 EU 1996 10 24 C2XA96IA238 1 19960928 A 3230 D229240003 PROXIMITY SWITCH AEROSP ATR42 ATR42320 8680930 EU LT MLG FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 27806 075 IAH - FLT 3969 - PILOT REPORTED THAT AFTER TAKEOFF THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN GEAR FORWARD PROXIMITY SWITCH, AND THE AIRCRAF T WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996102400959 19961024 00959 EU 1996 10 24 C2XA96IA237 1 19960928 A 3230 D229240003 PROXIMITY SWITCH AEROSP ATR42 ATR42320 8680930 EU LT MLG FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 27806 075 IAH - FLT 3969 - PILOT REPORTED THAT AFTER TAEKOFF, THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH AN D LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN GEAR AFT PROXIMITY SWITCH, AND THE AIRCRAFT W AS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996102400960 19961024 00960 SO 1996 10 24 C2XA96IA239 1 19960928 A 3246 3006041 WHEEL EMB 120 EMB120RT SO LT MLG FAILED A C2XA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SW 09 15713 120114 IAH - FLT 3797 - PILOT REPORTED THAT DURING TAKEOFF, THE NR 1 MAIN GEAR TIRE BLEW OUT. THE AIRCRAFT RETURNED TO THE FIE LD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 MAIN TIRE, AND BRAKE ASSEMBLY WHICH WAS DAMAGED FROM THE TIRE. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996102400961 19961024 00961 NM 1996 10 24 USAASB96198 1 19960920 A 3260 GEAR LIGHT BOEING 737 737201 1384454 NM NLG NO TEST A USAA A UNSCHED LANDING L NO TEST CL CLIMB 1 EA 19 245US 22751 CLT - FLT 2002 - AT FL270 CLIMBING OUT FROM IAD, A LOUD BANG WAS HEARD UNDER THE LT SIDE OF FWD ENTRY DOOR. ENG PARAMET ERS AND HYD NORMAL. NOSE WHEEL GREEN LIGHT WOULD NOT TEST. CHECKED LIGHT BULBS, C/B AND SOCKETS. CAPTAIN MADE PRECAUT IONARY DIVERSION TO CLT. CHECKED GEAR SIGHT VIEWER BEFORE FINAL APPROACH. NO EMERGENCY WAS DECLARED AND THE FLIGHT LAN DED WITHOUT INCIDENT. ALL GEAR INDICATIONS NORMAL ON LANDING, THREE GREEN AND NO RED. MX INSPECTED LEFT SIDE OF FUSELA GE FOR POSSIBLE BIRD STRIKE DAMAGE. NONE FOUND. PRESSURIZED A/C TO 3 PSI. NO BANGS HEARD. SWUNG GEAR. ALL GEAR INDI CATIONS NORMAL. LIGHT PRESS TO TEST CHECK GOOD. (M) 2 L 7 2 4F A16WE 1996102400962 19961024 00962 EU 1996 10 24 C2XA96BT010 1 19960914 A 2424 243211 GEN CONTL UNIT AEROSP ATR42 ATR42320 8680930 EU NR 2 FAILED A A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 14822 163 BTV-EWR -FLT 3381 - DIVERTED INTO ALB CREW REPORTED ACW GEN 2 FAULTED IN FLIGHT AND SMOKE IN COCKPIT. CHANGED ACW GCU A ND DC BPCU OPS CHECKED GOOD. PROBLEM REOCCURRED GOING INTO EWR/PHL. A/C WAS RELEASED IAW ATR MEL 24-22-4 PLACARD NR 89 6301. 9/16/96, MEL 24-22-4 PLACARD NR 891301 WAS CLEARED IN EWR BY REPLACING NR 2 GCU AND A/C BPCU OPERATIONALLY CHECKE D GOOD. EN ROUTE TO SYR FLT 3652 NR 2 ACW GEN FAILED IN FLT. A/C WAS MX FERRIED TO BTV. FOUND SEVERAL BURNED AND BROK EN WIRES ON BACKSIDE OF CANNON PLUG 411VC2, REPAIRED WIRING, CHANGED ACW GCU OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 1996102400963 19961024 00963 NE 1996 10 24 C2XA96CL033 2 19960916 A 7261 TM118 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE LEFT OIL LEAK A C2XA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 09 15730 120187 115386 CLE - DURING A ROUTINE LINE CHECK INSPECTION, MAINTENANCE FOUND THE LEFT ENGINE TO HAVE ENGINE OIL LEAKING OUT OF THE IN LET DUE TO INTERNAL LEAK. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE IAW CONTINENTAL EXPRESS MX DIRECTIVES NR 7, NR 8, AND NR 9. ALL OPS AND LEAKS WERE GOOD, AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1996102400964 19961024 00964 NE 1996 10 24 C2XA96CL032 2 19960917 A 7200 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE LEFT FAILED A C2XA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 SW 09 27707 120095 CLE - FLT 3074 - CREW REPORTED THAT ON SHORT FINAL THEY HAD A BURNING SMELL IN COCKPIT WITH NO SMOKE WARNINGS OR LIGHTS. MX INSPECTED AIRCRAFT AND FOUND THE LEFT ENGINE TO HAVE AN INTERNAL OIL LEAK. THE LEFT ENGINE WAS REMOVED AND REPLACE D IAW CONTINENTAL EXPRESS MX DIRECTIVES NR 7, NR 8, AND NR 9, ALL OPERATIONAL AND LEAK CHECKS WERE GOOD IAW EMB120 MM 61 -00-00, AND 71-00-00. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1996102400965 19961024 00965 SO 1996 10 24 C2XA96IA253 1 19961002 A 5400 12030995001 ANGLE EMB 120 EMB120RT SO LT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12705 120089 IAH - DURING C-CHECK INSPECTION, THE LEFT NACELLE FRAME 2 ATTACH ANGLE WAS FOUND TO BE CRACKED. MX REMOVED AND REPLACED THE ANGLE AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996102400966 19961024 00966 SO 1996 10 24 C2XA96IA252 1 19961002 A 5400 12030995002 ANGLE EMB 120 EMB120RT SO RT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12705 120089 IAH - DURING C-CHECK INSPECTION, THE RIGHT NACELLE FRAME 2 ATTACH ANGLE WAS FOUND TO BE CRACKED. MX REMOVED AND REPLACE D THE FRAME AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996102400967 19961024 00967 SO 1996 10 24 C2XA96IA251 1 19961002 A 5347 12015996601 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12705 120089 IAH - DURING C-CHECK INSPECTION, THE RIGHT AFT SIDEWALL SEAT TRACK WAS FOUND TO BE CORRODED. MX REMOVED AND REPLACED TH E AFFECTED SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996102400968 19961024 00968 SO 1996 10 24 C2XA96IA250 1 19961002 A 5347 12016000003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12705 120089 IAH - DURING C-CHECK INSPECTION, THE RIGHT FORWARD FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND R EPLACED THE AFFECTED SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996102400969 19961024 00969 SO 1996 10 24 C2XA96IA249 1 19961002 A 5347 12026865609 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12705 120089 IAH - DURING C-CHECK INSPECTION, THE RIGHT AFT FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLA CED THE AFFECTED PORTION OF SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996102400970 19961024 00970 SO 1996 10 24 C2XA96IA248 1 19961002 A 5347 12015995603 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12705 120089 IAH - DURING C-CHECK INSPECTION, THE LEFT FORWARD FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND RE PLACED THE AFFECTED PORTION OF SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996102400971 19961024 00971 SO 1996 10 24 C2XA96IA247 1 19961002 A 5347 12026864007 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12705 120089 IAH - DURING C-CHECK INSPECTION, THE LEFT AFT FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLAC ED THE AFFECTED PORTION OF SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996102400972 19961024 00972 SO 1996 10 24 C2XA96IA246 1 19961002 A 5347 12026863007 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12705 120089 IAH - DURING C-CHECK INSPECTION, THE LEFT AFT SIDEWALL SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REP LACED THE AFFECTED PORTION OF SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996102400973 19961024 00973 SO 1996 10 24 C2XA96IA245 1 19961002 A 5347 12015996005 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12705 120089 IAH - DURING C-CHECK INSPECTION, THE RIGHT AFT SIDEWALL SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND RE PLACED THE AFFECTED PORTION OF SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1996102400974 19961024 00974 SO 1996 10 24 C2XA96IA244 1 19961002 A 5347 12015994003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12705 120089 IAH - DURING C-CHECK INSPECTION, THE LEFT FORWARD SIDEWALL SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996102400992 19961024 00992 NM 1996 10 24 CALA9601494 1 19961002 A 5720 ANGLE BOEING 727 727243 138408D NM FS 333 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 579PE 21662 INSPECTION FOUND A 1.5 INCH CRACK AT AFT END OF UPPER RIB CAP INSIDE OF RT WING LEADING EDGE, FS 333. THE CRACKED ANGLE WAS REMOVED AND A REPLACEMENT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-20-2. 2 L 7 3 4F RT A3WE 1996102400993 19961024 00993 NM 1996 10 24 CALA9601495 1 19961003 A 5320 STIFFENER BOEING 727 727243 138408D NM BS 328 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 579PE 21662 INSPECTION 'A', 2 INCH CRACK IN FLOORBEAM LOWER CHORD STIFFENER AT STA 328, RBL 48. THE CRACKED AREA WAS CUT OUT, A REP AIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. 2 L 7 3 4F RT A3WE 1996102400994 19961024 00994 NM 1996 10 24 CALA9601496 1 19961003 A 5320 STIFFENER BOEING 727 727243 138408D NM BS 328 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 579PE 21662 INSPECTION FOUND A 1.5 INCH CRACK IN FLOORBEAM LOWER CHORD STIFFENER AT STA 328, LBL 24. THE STIFFENER WAS REMOVED, A N EW STIFFENER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1. 2 L 7 3 4F RT A3WE 1996102400995 19961024 00995 NM 1996 10 24 CALA9601497 1 19961003 A 5320 STIFFENER BOEING 727 727243 138408D NM BS 344 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 579PE 21662 INSPECTION FOUND A 1.5 INCH CRACK IN FLOORBEAM LOWER CHORD STIFFENER AT STA 344, BL 0. A DOUBLER WAS FABRICATED AND INS TALLED IAW SRM 51-40-3. 2 L 7 3 4F RT A3WE 1996102400996 19961024 00996 NM 1996 10 24 CALA9601498 1 19961003 A 5320 SPLICE BOEING 727 727243 138408D NM CARGO DR CUTOUT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 579PE 21662 INSPECTION FOUND STRINGER 27R SPLICES AT AFT CARGO DOOR CUTOUT LOWER CENTER SECTION CORRODED. A REPAIR WAS INSTALLED IA W ECRA 5310-02509. 2 L 7 3 4F RT A3WE 1996102400997 19961024 00997 NM 1996 10 24 CALA9601499 1 19961002 A 5720 ANGLE BOEING 727 727243 138408D NM WS 333 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 579PE 21662 INSPECTION FOUND A 1 INCH CRACK IN ANGLE OF LT WING LEADING EDGE CAVITY AT STA 333. THE ANGLE WAS REMOVED, A REPLACEMEN T ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-20-2. 2 L 7 3 4F RT A3WE 1996102400998 19961024 00998 NM 1996 10 24 CALA9601500 1 19961003 A 5210 DOOR FRAME BOEING 727 727243 138408D NM AFT ENTRY DR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 579PE 21662 INSPECTION FOUND A HOLE AND CRACKS IN AFT ENTRY DOOR FRAME ON LT SIDE, 31 INCHES UP FROM FLOOR. THE DAMAGED AREA WAS CU T OUT, AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-40-3. 2 L 7 3 4F RT A3WE 1996102400999 19961024 00999 NE 1996 10 24 96UAL900823 2 19961018 A 7230 50D364 FAN EXIT CASE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT ENGINE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 648UA 24556 25285 THE RIGHT ENGINE CASE AND VANE ASSEMBLY FAN EXIT HAS A CRACK AT THE 5 O'CLOCK POSITION LOOKING FORWARD. THE CRACK EXTEN DS OUTWARD ON THE CASE STIFFENER FLANGE. THE CRACK IS LOCATED ON THE B1 FLANGE. THE CRACK RUNS FROM THE OUTER DIAMETER OF THE FLANGE INTO AN UNUSED BOLT HOLE. A FAN EXIT CASE CRACK IS COMMONLY FOUND DURING ENGINE SHOP VISITS. THE CONDITIO N WILL BE MONITORED DURING SUBSEQUENT A-CHECKS. PART TOTAL CYCLES, 1,970. 2 L 7 2 4F 4 F RT A1NM E24NE 1996102600001 19961026 00001 NE 1996 10 26 RRXA96067 2 19960823 A 7200 ENGINE DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE NR 1 FLAMED OUT A RRXA E ENGINE SHUTDOWN X ENGINE FLAMEOUT CR CRUISE 1 WP 15 500MH 45812 FLT 174 - EBBR - IN CRUISE, AT FL 330, NR 1 ENGINE FLAMED OUT. PERFORMED INFLGIHT ENGINE START ACCORDING TO QRH. ALL P ARAMETERS NORMAL THEREAFTER. INSPECTED PER CFM MM 71-00-00 FAULT 51 PROCEDURES. NO DEFECTS NOTED. (M) 2 L 7 4 4F 4 F RT 4A25 E2GL 1996102600002 19961026 00002 NM 1996 10 26 DHL9674103A 1 19960614 A 7331 8TJ80GAA PWR SUPPLY BOEING 727 7272Q9 138448M NM PWA JT8 JT8D17R 52049 NE NR 2 ENGINE FAILED A T DHLA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 SO 01 741DH 21931 DURING CLIMB, NR 1, 2 AND 3 FUEL FLOW ERRATIC. FOUND NR 2 FUEL FLOW TRANSMITTER CAUSING FAULTS IN NR 1 AND NR 3 FUEL FL OW INDICATIONS. REMOVED AND REPLACED FUEL FLOW POWER SUPPLY PER M/M 73-31-12. REPLACED NR 2 ENGINE FUEL FLOW TRANSMITT ER PER M/M 73-30-0, OPS CHECK GOOD. 2 L 7 3 4F 4 F RT A3WE E2EA 1996103000001 19961030 00001 1996 10 30 DHL96721006 4 19961012 A 3455 ADF BOEING 727 727228 NM NR 1 BROKEN WIRE A DHLA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 721DH 19545 NR 1 ADF INOP. FOUND BROKEN SHIELD ON PIGTAIL CONNECTOR FOR SENSE ANTENNA AT RECEIVER. REPAIRED AS REQUIRED, OPS CHECK GOOD IAW MM 34-37-0. 2 L 7 3 4F A3WE 1996103000003 19961030 00003 EU 1996 10 30 HEEA968283 1 19961014 A 2841 23065560010 INDICATOR AEROSP AS355 AS355F1 8680810 EU FUEL GAGE ERRATIC E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5793Z 5142 GAGE ERRATIC WITH 20% MORE FUEL. 1 G 7 2 3U H11EU 1996103000004 19961030 00004 SW 1996 10 30 MALA965112 1 19960831 A 5311 FRAME SWRNGN SA227 SA227AC 8780603 SW BS 147 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 421MA AC634 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND RELIEF RADIUS CRACKED AT LOWER RIGHT SIDE OF BELT FRAME AT FS 14 7. COMPLETED REPAIR TO BELT FRAME 147 RIGHT SIDE BY STOP DRILLING CRACK, FABRICATING AND INSTALLING REPAIR DOUBLER IAW FAC SRM 53-90-20 PAGES 83-85. (M) 2 L 7 2 4T RT A8SW 1996103000005 19961030 00005 1996 10 30 CALA9601474 4 19961016 A 2565 D29985107 SLIDE DOUG DC9 DC983 3022083 WP AFT SERV DOOR FAILED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14879 2780 49526 AFT SERVICE DOOR SLIDE FAILED EMERGENCY SLIDE LIGHT FUNCTIONAL CHECK. REPLACED EMERGENCY SLIDE PER MAINTENANCE MANUAL. 2 L 7 2 4F RT A6WE 1996103000006 19961030 00006 NM 1996 10 30 UPS96221333 1 19961006 A 5330 SKIN BOEING 727 727185C 138406N NM BS 1123-1143 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 940UP 19826 INSPECTION TYPE-SV, STR 4R BETWEEN BS 1123 AND BS 1143, SKIN LAP HAD CORROSION BULGING EXCESSIVE SEALANT. REPAIRED IAW SRM 53-30-01. 2 L 7 3 4F A3WE 1996103000008 19961030 00008 NM 1996 10 30 96UAL900786 1 19961008 A 3350 LIGHT BOEING 747 747222B 1384904 NM PWA JT9 JT9D7R4G2 52054 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 151UA 23736 DOOR 1L SLIDE EMERGENCY LIGHT INOP. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E3NE 1996103000009 19961030 00009 NM 1996 10 30 96UAL900796 1 19961010 A 3397 WIRE BOEING 747 747222B 1384904 NM PWA JT9 JT9D7R4G2 52054 NE CABIN BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 151UA 23736 DOOR 1L BUSTLE EMERGENCY LIGHT COMES ON INTERMITTENTLY. REPAIRED WIRE NEAR TERMINAL BLOCK AT DOOR 1L FORWARD UPPER SILL AREA. 2 L 7 4 4F 4 F RT A20WE E3NE 1996110100001 19961101 00001 NM 1996 11 1 EISA96146 1 19960904 A 3411 PITOT TUBE BOEING 727 72781 1384025 NM RIGHT PLUGGED A EISA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 110NE 18952 DURING TAKEOFF ROLL, AIRSPEED INDICATOR DROVE TO ZERO, INFLIGHT FLIGHT OFFICERS MACH INDICATOR AND IVSI ALSO WERE READIN G ZERO. REMOVED OBSTRUCTION FROM FLIGHT OFFICERS PITOT TUBE, OPS CHECK GOOD. (M) 2 L 7 3 4F A3WE 1996110100002 19961101 00002 CE 1996 11 1 CA960229007 1 19960226 A 2430 S136050 CIRCUIT BREAKER BEECH 95 95B55 1152729 CE CONT LT ALTERNATOR FAILED W O OTHER B H SMOKE/FUMES/ODORS/SPARKS ELECT. POWER LOSS-50 PC CR CRUISE 1 CA 14593 (CAN)DURING CRUISE THE PILOT NOTICED THAT BOTH ALTERNATOR OUTPUTS WERE ZERO AND THE BATTERY VOLTAGE WAS DOWN TO 19 VOLTS . THE LEFT HAND, 50 AMP BRKER WAS POPPED. BOTH ALTERNATORS WERE SHUTOFF, THE LEFT HAND BUS CIRCUIT BREAKER WAS RESET AND THE ALTERNATORS TURNED BACK ON. THE RIGHT HAND SHOWED NO LOAD AND THE LEFT HAND INDICATED 100 PERCENT AND BEGAN TO SMOK E. BOTH ALTERNATORS WERE SHUT OFF. INSPECTION REVEALED THAT THE RIGHT HAND ALTERNATOR HAD FAILED AND THEN THE LEFT HAND CIRCUIT BREAKER WAS NOT CAPABLE OF HANDLING THE FULL LOAD. ALL OFFENDING ITEMS REPLACED AND THE AIRCRAFT RETURNED TO SER VICE. 1 L 7 2 3O RT 3A16 1996110100004 19961101 00004 NM 1996 11 1 CA960304001 1 19960301 A 3230 54C546347 VALVE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 NACELLE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 9919 4450 00963 120056 (CAN)HEAVY HYDRAULIC LEAK FROM #2 NACELLE. GEAR SOLENOID SEQUENCE VALVE FOUND CRACKED. SB 8-32-124 IS RELEVANT. 2 H 7 2 4T 4 T RT A13NM E20NE 1996110100005 19961101 00005 SO 1996 11 1 CA960304010 1 19960201 A 5210 4662403 BRACKET SUPPORT PIPER PIPER PA42 PA42 7104202 SO PWA DOOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) INDICATION WAS A 1/2 INCH CRACK IN THE EDGE OF THE DOOR SKIN WHICH HAD PREVIOUSLY BEEN STOP DRILLED. INSPECTION FO UND PART TO HAVE A 3 INCH CRACK ACROSS FOUR RIVET HOLES. A CRACK WAS ALSO FOUND AT TWO OF THE FOUR RIVET HOLES WHICH PIC K UP THE HINGE IN THE BULKHEAD P/N 46550-04. 1 L 7 2 4T A23SO 1996110100007 19961101 00007 EA 1996 11 1 CA960304013 1 19960209 A 5210 85210096103 FITTING DHAV 85210240005 DHAV DHC8 DHC8311 1386006 EA MAIN DOOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 10785 (CAN)UPPER FITTING ON AFT UPPER STRUT FOR MAIN ENTRANCE DOOR CRACKED AND BROKE OFF JUST ABOVE UPPER SWAGE SLEEVE. NO COR ROSION FOUND IN AREA. 2 H 7 2 4T RT A13NM 1996110100008 19961101 00008 EA 1996 11 1 CA960304014 1 19960214 A 2910 82970010131 TUBE ASSEMBLY DHAV DHC8 DHC8311 1386006 EA LT DRAIN CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA 10815 (CAN)DURING 200 HOUR GEAR INSPECTION, LH CASE DRAIN RETURN TUBE ASSEMBLY FOUND CHAFED BEYOND LIMITS. STANDBY POWER UNIT PRESSURE LINE CAUSING CHAFING. 2 H 7 2 4T RT A13NM 1996110100009 19961101 00009 NM 1996 11 1 CA960304015 1 19960221 A 2910 82970010217 TUBE DHAV DHC8 DHC8102 2809003 NM NR 2 HYD SYS CRACKED W H DEACTIVATE SYST/CIRCUITS K FLUID LOSS LD LANDING 1 CA 16571 LH120337 (CAN)HYDRAULIC LINE CRACKED. ALL HYDRAULIC FLUID LOST FROM #2 SYSTEM. 2 H 7 2 4T RT A13NM 1996110100010 19961101 00010 NM 1996 11 1 CA960306001 1 19960212 A 3234 574205 SELECTOR VALVE DHAV DHC8 DHC8301 NM LANDING GEAR FAILED W L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 CA 435 (CAN)ON APPROACH THREE RED WARNING LIGHTS ON WITH NO GEAR MOVEMENT WHEN GEAR SELECTED DOWN. CREW DID GO AROUND. ALTERNAT E GEAR EXTENSION, OK. ALSO NOSE WHEEL STEERING FAILED DURING TAXI. LANDING GEAR SELECTOR VALVE REPLACED. 2 H 7 2 4T RT A13NM 1996110100011 19961101 00011 SO 1996 11 1 CA960306005 1 19960129 A 3230 HYD HOSE PIPER PA31T PA31T2 7103127 SO NLG DOWN LINE LEAKING W O OTHER K FLUID LOSS AP APPROACH 1 CA (CAN) PILOT SELECTED GEAR DOWN AND RECEIVED INDICATION FROM MAIN GEAR ONLY, NO NOSE GEAR LIGHT. GEAR WAS RECYCLED AND I NDICATION WAS RECEIVED. INVESTIGATION FOUND THE NOSE GEAR DOWN HYDRAULIC LINE LOOSE AND LEAKING HYDRAULIC FLUID. SUSPE CT A VIBRATION PROBLEM THAT HAD OCCURRED EARLIER TO BE THE SOURCE OF THE LINE BECOMING LOOSE. 1 L 7 2 3T RT A8EA 1996110100012 19961101 00012 EU 1996 11 1 CA960306013 1 19960216 A 5320 350A21106605 MOUNT AEROSP AS355 AS355F1 8680810 EU ALLSN 250C 250C20F 03013 GL FORWARD L/H CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 4468 CAE840298 (CAN)LEFT HAND FORWARD MOUNT ASSEMBLY FOUND CRACKED. 1 G 7 2 3U 3 U H11EU E4CE 1996110100014 19961101 00014 WP 1996 11 1 CA960306015 1 19960224 A 3234 AN32101 SWITCH CVAC 440 440 2422902 WP GEAR LEVER INTERMITTENT W L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 CA (CAN)ON APPROACH DID NOT GET THREE GREEN ON LANDING GEAR EXTENSION. TOWER CONFIRMED LANDING GEAR EXTENDED ON TOWER FLY B Y. LANDING GEAR LEVER WIGGLED AND SAFE GEAR INDICATION OBTAINED. AIRCRAFT LANDED SAFE LY. MAINTENANCE INVESTIGATION REVE ALED LANDING GEAR LEVER SWITCH WAS INTERMITTENT. DEFECTIVE SWITCH REPLACED. 2 L 7 2 4R 6A6 1996110100016 19961101 00016 SO 1996 11 1 CA960306018 1 19960224 A 5210 4358606 BRACKET PIPER 53335 PIPER PA31 PA31350 7103110 SO FS 215 DOOR SUP BROKEN SCREWS W K NONE O OTHER IN INSP/MAINT 1 CA 7662 317852024 (CAN)UPPER SCREWS FOUND BROKEN. INVESTIGATION REVEALED THE LIP OF THE TRIM WAS INSTALLED BETWEEN THE BRACKET AND THE REI NFORCING PLATE CAUSING STRESS AND EVENTUAL BREAKING OF THE SCREWS. 1 L 7 2 3O A20SO 1996110100017 19961101 00017 NM 1996 11 1 CA960306019 1 19960214 A 3230 DSC252B40124 HOSE DHAV DHC8 DHC8102 2809003 NM NLG UP LINE LEAKING W K NONE K FLUID LOSS NR NOT REPORTED 1 CA (CAN)NOSE LANDING GEAR WOULD NOT RETRACT AND #2 HYDRAULIC SYSTEM READ EMPTY. NOSE GEAR DOWNLOCK ACTUATOR 'UP' LINE FOUND LEAKING. 2 H 7 2 4T RT A13NM 1996110100018 19961101 00018 NM 1996 11 1 CA960306021 1 19960227 A 2450 MCR6WIK CAPACITOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE RH TX 26VAC BURNT W K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 CA 18719 120013 (CAN)ON APPROACH, ELECTRICAL SMELL NOTED IN COCKPIT. RIGHT 26VAC CAUTION LIGHT ON. CB G10 BEHIND CAPTAIN POPPED. FIRST O FFICER LOST AC FLIGHT INSTRUMENTS. IN-LINE CAPACITOR FOR STEP DOWN TRANSFORMER 115/26VAC RIGHT HAND, FOUND BURNT. 2 H 7 2 4T 4 T RT A13NM E20NE 1996110100019 19961101 00019 NE 1996 11 1 CA960311001 1 19960303 A 6320 NAS62827 BOLT SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL L/H FWD ATTACH CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1800 CAE890255S (CAN)UPON REMOVING L/H MGB COWLING FOR ROUTINE MAINTENANCE, THE FORWARD MGB ATTACHMENT BOLT WAS NOTICED TO BE RAISED UP FROM FEET. UPON REMOVAL OF THE BOLT IT WAS FOUND CRACKED IN HALF. THE REMAINING HALF OF THE BOLT WAS REMOVED WITH A BOL T EXTRACTOR AND A THOROUGH INSPECTION WAS CARRIED OUT ON THE MGB AND AIRFRAME STRUCTURE. 1 G 7 2 3U 3 U H1NE E1GL 1996110100020 19961101 00020 NM 1996 11 1 CA960311006 1 19960227 A 3310 0360 PC BOARD GRIMES 7002537 DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE ADVISORY LIGHTS BURNT W D RETURN TO BLOCK B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 CA 0360 PCE123030 (CAN)ADVISORY LIGHT CONTROL BOX SHORTED OUT CAUSING A STRONG ELECTRICAL BURNING SMELL IN COCKPIT CAUTION LIGHTS SWITCHE D FROM DIM TO BRIGHT ON THEIR OWN JUST PRIOR CREW COULD NOT SWITCH LIGHTS BACK TO DI M. ADVISORY LIGHT BOX PC BOARD 'B' FOUND BURNT. 2 H 7 2 4T 4 T RT A13NM E20NE 1996110100025 19961101 00025 CE 1996 11 1 CA960311012 1 19960229 A 2437 S13201 AMMETER CESSNA S13201 CESSNA 150 150L 2071826 CE CONT O200 O200A 17020 SO MCAULY 1A101 1A101HCM GL INST PANEL BURNED OUT W F ACTIVATE FIRE EXT. A B FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA 4481 619465A G7878 (CAN)DURING TROUBLESHOOTING OF THE INSTRUMENT LIGHT SWITCH, WITH THE MASTER SWITCH ON SMOKE WAS NOTED IN THE CABIN. THE MASTER WAS SHUT OFF. FLAME WAS NOTED UNDER THE RIGHT SIDE OF THE INSTRUMENT PANEL ANDTHE FIRE EXTINGUISHER WAS DISCHARGE D INTO THE FIRE. INVESTIGATION FOUND THE POSITIVE TERMINAL SIDE OF THE PLASTIC CASE AND THE PLASTIC HOLD DOWN FIXTURE WE RE FOUND BADLY BURNED. LITTLE DAMAGE WAS FOUND DONE TO THE WIRING EXCEPT FOR THE TERMINAL ATTACHMENT LUG. 1 H 7 1 3O 3 O 3A19 E252 5 N P918 1996110100026 19961101 00026 SO 1996 11 1 CA960311013 1 19960123 A 3230 40277 RETRACT LINK PIPER 40277 PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2B 41532 EA L/H GEAR BROKEN W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 8754 L58061 (CAN)AFTER TAKEOFF THE PILOT SELECTED GEAR UP AND THE LEFT HAND GREEN LIGHT WOULD NOT EXTINGUISH. A SAFE LANDING WAS MAD E AND INVESTIGATION FOUND THE LEFT HAND RETRACT LINK WAS BROKEN. SUBMITTER STATES THA T AD 88-05-05 WAS COMPLIED WITH 66 .04 HOURS PRIOR TO THE INCIDENT. FURTHER INVESTIGATION FOUND THE DOWNLOCK RIVETS SHEARED. THIS CONDITION WOULD NOT ALLOW THE UNLOCKING OF THE DOWNLOCK MECHANISM AND THE PRESSURE FROM THE GEAR RETRACT ACTUATOR CAUSED THE RETRACT LINK TO BREA K. 1 L 7 2 3O 3 O A20SO E14EA 1996110100027 19961101 00027 CE 1996 11 1 CA960311014 1 19960304 A 5751 SKIN BEECH BEECH 100 B100 1152919 CE PWA PT6 PT6A28 EA AILERON CORROSION W K NONE O OTHER IN INSP/MAINT 1 CA PCE50113 (CAN)AILERON DEVELOPED A CRACK. DURING THE REPAIR, NEW SKINS WERE ORDERED AFTER FINDING HEAVY CORROSION AFTER REMOVING T HE SKIN. SUBMITTER STATES THAT THIS COULD NOT BE SEEN FROM THE OUTSIDE. 1 L 7 2 4T 4 T A14CE E4EA 1996110100028 19961101 00028 EU 1996 11 1 CA960311016 1 19960305 A 2420 GENERATOR AIRBUS 320 A320212 EU AC SYS MALFUNCTIONED W O H OTHER DEACTIVATE SYST/CIRCUITS H O ELECT. POWER LOSS-50 PC OTHER LD LANDING 1 CA (CAN)ON COMPLETION OF LANDING ROLL AIRCRAFT LOST ELECTRICAL POWER FROM BOTH AC GENERATOS AND WENT TO BATTERY POWER. ONCE AIRCRAFT CLEARED RUNWAY GENERATOR SYSTEM RESTORED AUTOMATICALLY. FURTHER INVESTIGATI ON REVEALED THAT BOTH GENERATORS D ROPPED OFF LINE FOR A BRIEF PERIOD. CFDS INTERROGATION DID NOT REVEAL ANY FAULTS. IT WAS REPORTED THAT THRUST REVERSERS WERE LEFT DEPLOYED AT IDLE FOR AN EXTENDED PERIOD DUE TO SNOW ON RUNWAY. SUSPECTED CAUSE OF FAILURE ATTRIBUTED TO SNOW I NGESTION RESULTING IN ENGINE ROLL BACK SUFFICIENT TO CAUSE GENERATORS TO TRIP OFF. 2 L 7 2 4F RT A28NM 1996110100029 19961101 00029 NM 1996 11 1 CA960311018 1 19960306 A 5610 NP15790210 SIDE WINDOW PPG DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE COCKPIT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 4615 92199H4511 LH120389 (CAN)DURING COCKPIT SIDE WINDOW INSPECTION TOP FORWARD SCREW HOLE FOUND CRACKED. THE WINDOW DID NOT HAVE THE REINFORCEME NT MOD. 2 H 7 2 4T 4 T RT A13NM E20NE 1996110100030 19961101 00030 EA 1996 11 1 CA960311019 1 19960303 A 2750 745581A CASING SUNDSTRANDEM DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE RT OUTB FLAP DRV WORN W K NONE O OTHER IN INSP/MAINT 1 CA 10580 1623 LH123018 (CAN)RIGHT HAND OUTBOARD SECONDARY FLAP DRIVE, OUTER CASING END FERRULES FOUND WORN BEYOND LIMITS. 2 H 7 2 4T 4 T RT A13NM E20NE 1996110100031 19961101 00031 SO 1996 11 1 CA960311020 1 19960222 A 2437 AMMETER PIPER PA30 PA30 7103002 SO LYC O320 IO320B1A 41508 EA INSTRUMENT PANEL FAILED W A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 CA L428855A (CAN)BATTERY FAILURE AS IN SDR 960311021 WAS NOT INDICATED BY THE AMMETER. 1 L 7 2 3O 3 O A1EA 1E12 1996110100032 19961101 00032 SO 1996 11 1 CA960311021 1 19960221 A 2432 R35 BATTERY AVIALL R35 PIPER PA30 PA30 7103002 SO LYC O320 IO320B1A 41508 EA INTERNAL FAILED W A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 CA L428855A (CAN)REPORTED SLOW DISCHARGE OF BATTERY WITH THE EVENTUAL LOSS OF ALL RADIOS AND SLOW GEAR EXTENSION. RADIO LOSS WAS THE FIRST SIGN. 1 L 7 2 3O 3 O A1EA 1E12 1996110100034 19961101 00034 NM 1996 11 1 CA960311027 1 19960120 A 2910 HYDRAULIC DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 HYD AIR IN SYSTEM W K NONE J WARNING INDICATION AP APPROACH 1 CA 120543 (CAN)LOSS OF #2 HYDRAULIC PRESSURE. ALTERNATE EXTENSION CARRIED OUT. AIR IN SYSTEM LIKELY DUE TO EXTREME COLD. EVERYTHIN G ELSE FOUND OK. SYSTEM TO BE BLEED AT EACH "L" CHECK. 2 H 7 2 4T 4 T RT A13NM E20NE 1996110100035 19961101 00035 EU 1996 11 1 CA960311028 1 19960302 A 5610 TGA300146 WINDSHIELD AIRBUS 310 A310324 3930206 EU PWA 4152 PW4152 NE RH COCKPIT CRACKED W O OTHER J WARNING INDICATION CR CRUISE 1 CA 717738 (CAN)AT 39,000 FT. PILOT REPORTED RH WINDOW FAULT AND MADE ONE RESET. APPROXIMATELY 10 SECONDS LATER, WINDOW FAULT MESSA GE APPEARED AND RH WINDSHIELD OUTER PANE CRACKED. QRH PROCEDURE FOR CRACKED PANE CARRIED OUT. MAINTENANCE ACTION INVOLVE D REPLACEMENT OF WINDSHIELD AND THE CAUSE OF THE PROBLEM WAS A FAULT WINDOW HEAT CONTROLLER. 2 L 7 2 4F RT A35EU E24NE 1996110100037 19961101 00037 SO 1996 11 1 CA960311032 1 19960304 A 3230 CENTERING SYSTEM EMB 110 EMB110P1 3260122 SO PWA PT6 PT6A34 52043 EA NOSE GEAR OUT OF ADJUST W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA PCE56941 (CAN)AFTER TAKEOFF PILOT COULD NOT SELECT GEAR UP. NOSE CENTERING SYSTEM ADJUSTMENT REQUIRED. 1 L 7 2 4T 4 T A21SO E4EA 1996110100038 19961101 00038 EU 1996 11 1 CA960311033 2 19960303 A 7320 CASC211 FUEL FLOW REG FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU #1 ENGINE FAULTY W A D E UNSCHED LANDING RETURN TO BLOCK ENGINE SHUTDOWN J M WARNING INDICATION OVER TEMP CL CLIMB 1 CA 9007 (CAN)DURING CLIMB, #1 ENGINE EXCEEDED MAXIMUM TGT FOR THIS STAGE OF FLIGHT. THE ENGINE WAS SHUT DOWN, AND AIRCRAFT RETUR NED TO BLOCKS. THE FUEL FLOW REGULATOR WAS REPLACED, GROUND RUN WAS CARRIED OUT AND F OUND SERVICEABLE. 2 L 7 2 4F 4 F RT A20EU E2EU 1996110100040 19961101 00040 CE 1996 11 1 CA960311037 1 19960227 A 3260 444EN496 SQUAT SWITCH BEECH BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA MLG OUT OF ADJUST W A UNSCHED LANDING L NO TEST CL CLIMB 1 CA PCE81053 (CAN) AFTER TAKEOFF THE PILOT SELECTED GEAR UP WITH NO RESPONSE. GEAR SELECTED DOWN AND AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. INVESTIGATION FOUND THE MICRO SQUAT SWITCH TO BE OUT OF ADJUSTMENT. SWITCH ADJUSTED AND THE AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 4T 4 T A24CE E4EA 1996110100042 19961101 00042 EA 1996 11 1 CA960311101 2 19960301 A 8530 7380685 PUSH ROD LYC LW16703 CESSNA 150 152 2071835 CE LYC O235 O235L2C 41505 EA #4 EXHAUST MUSHROOMED W K NONE O OTHER IN INSP/MAINT 1 CA 849 849 L2044115 KD023 (CAN)WHILE CARRYING OUT TEXTRON LYCOMING SERVICE INSTRUCTION #1068A, #4 EXHAUST PUSH ROD MUSHROOMED ON OUTER END, ALL OT HER PUSH RODS OK. AD 95-03-10 NOT APPLICABLE BY ENGINE SERIAL NUMBER AND PUSH ROD PART NUMBER. 1 H 7 1 3O 3 O NT 3A19 E223 1996110100043 19961101 00043 NM 1996 11 1 CA960311102 1 19960216 A 2140 VALVE BOEING 767 767375 NM CARGO OVHEAT FAILED W A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 CA (CAN)AFTER TAKEOFF AFT CARGO OVERHEAT EICAS FOLLOWED AND RETURNED TO BLOCKS. REPLACED AFT CARGO HEAT VALVE WHICH WAS IN POOR CONDITION - TRYING TO DRIVE BEYOND ITS LIMITS. 2 L 7 2 4F RT A1NM 1996110100044 19961101 00044 WP 1996 11 1 CA960311103 1 19960215 A 2910 61912 HYDRAULIC FUSE DOUG DC10 DC1030 3023501 WP GE NR 3 HYD SYS CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN)DURING "C" CHECK AND HYDRAULIC FUNCTION CHECK, THE VALVE SPLIT OPEN ALONG THE VALVE BODY BETWEEN THE FUSE PLUG AND HYDRAULIC FILTER IN ADAPTER ALLOWING LOSS OF #3 HYDRAULIC SYSTEM. VALVE REPLACED. 2 L 7 3 4F A22WE 1996110100045 19961101 00045 NM 1996 11 1 CA960312001 1 19960308 A 7312 10781D HEATER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE OIL TO FUEL OVERTEMP W O OTHER M OVER TEMP CR CRUISE 1 CA 9072 690 2078 120657 (CAN)#2 FUEL TEMP RED LINE. OIL TO FUEL HEAT EXCHANGER REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1996110100046 19961101 00046 NM 1996 11 1 CA960312003 1 19960308 A 8010 AA4N103 CONTACTOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE #2 ENG STARTER WELDED SHUT W H DEACTIVATE SYST/CIRCUITS O OTHER IN INSP/MAINT 1 CA 120165 (CAN)#2 ENGINE MOTORS WHEN BATTERIES OR GROUND POWER TURNED ON. STARTER CONTACTOR WELDED SHUT. 2 H 7 2 4T 4 T RT A13NM E20NE 1996110100047 19961101 00047 EA 1996 11 1 CA960312005 1 19960308 A 7312 10839E HEATER DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE OIL TO FUEL OVERTEMP W O OTHER M OVER TEMP CR CRUISE 1 CA 729 WA5882 123151 (CAN)#2 FUEL TEMP INDICATING RED LINE IN CRUISE. OIL TO FUEL HEAT EXCHANGER REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1996110100048 19961101 00048 SW 1996 11 1 CA960312007 1 19960130 A 6520 206040400005 GEARBOX BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL T/R GR BOX TEETH WEAR W K NONE J O WARNING INDICATION OTHER IN INSP/MAINT 1 CA 13427 4554 CAE821010 (CAN)CHIP LIGHT ON. PLUG INSPECTED AND FOUND GRAY PASTE. 23.2 HOURS LATER DURING 600 HOUR INSPECTION PROBLEM FOUND WITH GEAR TEETH. 1 G 7 1 3U 3 U H2SW E4CE 1996110100049 19961101 00049 SW 1996 11 1 CA960312010 1 19960202 A 6310 206040236013 HOUSING BELL 206 206L 1181522 SW ALLSN 250C 250C20B 03013 GL ENG/ XMSN DRV LOOSE STUD W K NONE O OTHER IN INSP/MAINT 1 CA 7956 692 830805 (CAN)FORWARD HOUSING ASSEMBLY P/N 206-040-236-013 HAS A STUD P/N AN125982 PULLING OUT. 1 G 7 1 3U 3 U H2SW E4CE 1996110100050 19961101 00050 SW 1996 11 1 CA960312011 1 19960205 A 6710 206001344001 CYCLIC STICK BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL M/R CONTROL WORN W K NONE O OTHER IN INSP/MAINT 1 CA CAE820289 (CAN)AN INSPECTION OF THE LOWER END OF THE CYCLIC STICK REVEALED MECHANICAL DAMAGE GREATER THAN ALLOWABLE LIMIT. 1 G 7 1 3U 3 U H2SW E4CE 1996110100052 19961101 00052 WP 1996 11 1 CA960312014 1 19960123 A 7714 65011040 TACHOMETER HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL COCKPIT STICKING W K NONE O OTHER IN INSP/MAINT 1 CA 20 CAE832104 (CAN)GAUGE STICKS AT LOW TEMPERATURE (-25 TO -40 DEGREES). GAUGE WORKS NORMALLY IF HEAT APPLIED TO GAUGE. 1 G 7 1 3U 3 U H3WE E4CE 1996110100053 19961101 00053 EU 1996 11 1 CA960312016 1 19960127 A 2842 647510032 TRANSMTITTER SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE FUEL QTY FAILED W K NONE N FALSE WARNING CR CRUISE 1 CA 75 834 (CAN)LOW FUEL LIGHT ON ALL TIME, REGARDLESS OF FUEL QUANTITY. TRANSMITTER OVERHAULED 75 HOURS PREVIOUSLY. 1 G 7 1 3U 3 U H9EU E19EU 1996110100054 19961101 00054 SW 1996 11 1 CA960312017 1 19960122 A 7722 206070267007 GAUGE BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL COCKPIT TOT READS HIGH W K NONE O OTHER IN INSP/MAINT 1 CA 46 CAE802241BA (CAN)GAUGE READS 30 DEGREES HIGH. 1 G 7 1 3U 3 U H2SW E4CE 1996110100055 19961101 00055 SW 1996 11 1 CA960312018 1 19960214 A 6310 206040230025 FREEWHEEL ASSY BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL FORWARD SEAL LEAKING SEAL W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 11094 2027 CAE822258 (CAN)FORWARD SEAL LEAKING EXCESSIVELY. TIME SINCE REPAIR THIS INSTALLATION 496.8 HOURS. 1 G 7 1 3U 3 U H2SW E4CE 1996110100056 19961101 00056 SW 1996 11 1 CA960312020 1 19960106 A 6230 206010450113 SWASHPLATE ASSY BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL SLEEVE BEARINGS WEARING W K NONE O OTHER IN INSP/MAINT 1 CA 3262 CAE822258 (CAN)UPON 300 HOUR INSPECTION PARTICLES OF TEFLON AND BRASS WERE FOUND COMING FROM PIVOT SLEEVE AND SWASHPLATE SUPPORT. SWASHPLATE ASSY WAS REMOVED FOR INSPECTION AND FOUND BRASS SHIMS UNDER SLIDER BEARING S WERE WORKING OUT AND BREAKING AP ART CAUSING SLIDER WEAR. BRASS SHIM IS NOT APPROVED FOR USE IN THIS AREA, NOR IS IT REQUIRED. THE SHIM WORKING OUT CAUSE SERIOUS PREMATURE WEAR OF THE SWASHPLATE SUPPORT AND CAN CAUSE SERIOUS BINDING OF THE COLLECTIVE IN FLIGHT. THIS UNAPPR OVED PROCEDURE WAS VERBALLY DISCUSSED A FEW YEARS AGO WITH THE OVERHAUL FACILITY. 1 G 7 1 3U 3 U H2SW E4CE 1996110100057 19961101 00057 GL 1996 11 1 CA960312023 2 19960209 A 7412 6895573 EXCITER HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL ENG IGNITION INTERMITTENT W K NONE O OTHER IN INSP/MAINT 1 CA CAE832056 (CAN)INTERMITTENT OPERATION, SUSPECT LOOSE INTERNAL COMPONENT AS EXCITER WORKS FOR 3-5 SECONDS IF TAPPED. 1 G 7 1 3U 3 U H3WE E4CE 1996110100058 19961101 00058 WP 1996 11 1 CA960312024 1 19960223 A 6210 369D21100516 BLADE HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL M/R DEBONDING W K NONE O OTHER IN INSP/MAINT 1 CA 1920 CAE830896 (CAN)LEADING EDGE ABRASION STRIP DEBONDING. BLADE P/N 369D21100-516A. TIME THIS INSTALLATION 589.8 HOURS. 1 G 7 1 3U 3 U H3WE E4CE 1996110100060 19961101 00060 WP 1996 11 1 CA960312026 1 19960223 A 6210 369D21100517 BLADE HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL M/R DEBONDED W K NONE O OTHER IN INSP/MAINT 1 CA 590 CAE830896 (CAN)LEADING EDGE ABRASION STRIP DEBONDED. 1 G 7 1 3U 3 U H3WE E4CE 1996110100061 19961101 00061 WP 1996 11 1 CA960312027 1 19960223 A 6210 369D21100513 BLADE HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL M/R DEBONDING W K NONE O OTHER IN INSP/MAINT 1 CA 2564 CAE830896 (CAN)LEADING EDGE STRIP DEBONDED. 1 G 7 1 3U 3 U H3WE E4CE 1996110100062 19961101 00062 1996 11 1 CA960312031 4 19960219 A 2312 069102100 TRANSCEIVER HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL COCKPIT VHF STATIC W K NONE O OTHER IN INSP/MAINT 1 CA 24 CAE832104 (CAN)B SIDE OF RADIO DID NOT WORK FROM INITIAL INSTALLATION, UNIT HAD VERY BAD STATIC ALSO. 23.6 HOURS SINCE OVERHAUL. 1 G 7 1 3U 3 U H3WE E4CE 1996110100064 19961101 00064 NE 1996 11 1 CA960313001 1 19960223 A 2913 WAP2002 HYDRAULIC PUMP SKRSKY S61 S61N 8142104 NE GE CT58 CT581401 30011 NE MAIN GEARBOX BEARING FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 15 295123 (CAN)IN FLIGHT, THE CYCLIC CONTROL STARTED GETTING STIFF, ACCOMPANIED BY A GROWLING NOISE FROM MAIN GEARBOX AREA. AFTER HYDRAULIC PUMP WAS REMOVED IT WAS FOUND THAT A BEARING HAD FAILED. NOTE THIS PUMP HASHAD A PREVIOUS HISTORY OF PREMATURE FAILURE. 2 G 7 2 4U 4 U 1H15 1E3 1996110100065 19961101 00065 EA 1996 11 1 CA960313002 2 19960102 A 7260 3011218 CARBON SEAL PIPER PA31T PA31T 7103124 SO PWA PT6 PT6A28 EA BREATHER LEAKING W K NONE O OTHER IN INSP/MAINT 1 CA 88 PCE41649 (CAN) APPROXIMATELY 60 HOURS OUT OF OVERHAUL THE ENGINE OIL CONSUMPTION WAS FOUND TO BE EXCESSIVE. INVESTIGATION FOUND T HE OIL WAS BEING VENTED OVERBOARD AND WAS TROUBLESHOT TO THE ACCESSORY GEARBOX BREATHER IMPELLER CARBON SEAL. AFTER REPL ACEMENT THE OIL CONSUMPTION RETURNED TO NORMAL. 1 L 7 2 3T 4 T A8EA E4EA 1996110100066 19961101 00066 EA 1996 11 1 CA960313003 1 19960303 A 2750 745581A CASING SUNDSTRANDEM DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE LT INB FLAP DRV WORN FERRULE W K NONE O OTHER IN INSP/MAINT 1 CA 10580 1629 LH123018 (CAN)LEFT HAND INBOARD SECONDARY FLAP DRIVE OUTER CASING END FERRULES FOUND WORN BEYOND LIMITS. 2 H 7 2 4T 4 T RT A13NM E20NE 1996110100067 19961101 00067 EA 1996 11 1 CA960313004 1 19960303 A 2750 745581A CASING SUNDSTRANDEM DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE RT INB FLAP DRV WORN FERRULE W K NONE O OTHER IN INSP/MAINT 1 CA 10580 1628 LH123018 (CAN)RIGHT HAND INBOARD SECONDARY FLAP DRIVE OUTER CASING END FERRULES FOUND WORN BEYOND LIMITS. 2 H 7 2 4T 4 T RT A13NM E20NE 1996110100068 19961101 00068 EA 1996 11 1 CA960313005 1 19960303 A 2750 745581A CASING SUNDSTRANDEM DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE LT OUTB FLAP DR WORN FERRULE W K NONE O OTHER IN INSP/MAINT 1 CA 10580 1616 LH123018 (CAN)LEFT HAND OUTBOARD SECONDARY FLAP DRIVE OUTER CASING END FERRULES FOUND WORN BEYOND LIMITS. 2 H 7 2 4T 4 T RT A13NM E20NE 1996110100070 19961101 00070 NM 1996 11 1 CA960313008 1 19960302 A 5330 SKIN BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE FS 533 DAMAGED W K NONE O OTHER TX TAXI/GRND HDL 1 CA 30734 (CAN)DURING GROUND HANDLING AIRCRAFT WAS STRUCK BY SERVICE TRUCK AT FS 533 STRINGER 24 R. PRESSURE SKIN DAMAGED AND REPA IRED AS PER SRM AND RELEASED. 2 L 7 2 4F 4 F RT A2NM E12EU 1996110100071 19961101 00071 SO 1996 11 1 RAAA96E8033 1 19961023 A 3350 86210144 BATTERY PACK INTVLV 873100112 LKHEED 188 188C 5262604 SO CABIN LOW CHARGE A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 AFT CABIN SERVICE DOOR EGRESS IDENTIFIER LIGHT DOES NOT TEST. REPLACED BATTERY PACK. 2 L 7 4 4T 4A22 1996110100072 19961101 00072 WP 1996 11 1 CALA9601504 1 19961023 A 2823 AV16A1323B1 FUEL SO VLV DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 2 ENGINE OUT OF RIG A CALA A D J UNSCHED LANDING RETURN TO BLOCK DUMP FUEL R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SW 09 14075 46922 455894 THE NR 2 ENG SPOOLED DOWN TO IDLE RPM SHORTLY AFTER TAKEOFF. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED. MAINTENANC E FOUND THE NR 2 ENG FUEL PUMP HAD FAILED. THE NR 2 ENG FUEL PUMP WAS REMOVED AND REPLACED. IN ADDITION, THE FUEL/OIL HEAT EXCHANGER AND ENG FUEL CONTROL WERE REPLACED AS A PRECAUTIONARY MEASURE. FUEL LEAK CHECKS WERE ALSO GOOD. *S/D* T HE FUEL PUMP AND FUEL CONTROL UNIT WERE BOTH TESTED IAW THE CF6 COMPONENT MM AND NO TROUBLE WAS FOUND. THIS AIRCRAFT HAD AN ABORTED TAKEOFF THE FOLLOWING DAY (10/24) FOR THE SAME PROBLEM. ENGINEERING REPORTED THAT THE NR 2 ENGINE FIRE SHUT OFF VALVE WAS RERIGGED AT THAT TIME, AND IT CORRECTED THE PROBLEM. 2 L 7 3 4F 4 F A22WE E23EA 1996110100073 19961101 00073 NM 1996 11 1 CALA9601505 1 19961003 A 5320 RIB BOEING 727 727243 138408D NM BS 1130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 579PE 21662 INSPECTION FOUND RIB CORRODED AT STA 1130, STRINGER 29R. THE CORRODED SECTION OF RIB WAS REMOVED. NEW SPLICE REPAIR PA RTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-4. 2 L 7 3 4F RT A3WE 1996110100074 19961101 00074 NM 1996 11 1 CALA9601506 1 19961011 A 5330 SKIN BOEING 727 727243 138408D NM BS 1150 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 579PE 21662 INSPECTION FOUND SKIN CORRODED AT DRAIN LINE IN AFT CARGO COMPARTMENT, STA 1150, STRINGER 30. THE AREA WAS REPAIRED IAW SRM 51-10-1. 2 L 7 3 4F RT A3WE 1996110100075 19961101 00075 NM 1996 11 1 CALA9601507 1 19961002 A 5754 SKIN BOEING 727 727243 138408D NM NR 5 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 579PE 21662 INSPECTION FOUND A .50 INCH CRACK IN LOWER SKIN OF NR 5 SLAT. THE CRACK WAS LOCATED AT CORNER OF SKIN BELOW INBOARD TRA CK. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-50-3. 2 L 7 3 4F RT A3WE 1996110100076 19961101 00076 NM 1996 11 1 CALA9601508 1 19960911 A 5754 SKIN BOEING 737 7373T0 1384582 NM NR 5 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76355 23593 INSPECTION FOUND 1 INCH CRACKS COMING FROM FASTENER HOLES IN NR 5 SLAT LOWER SKIN. REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW ECRA 5750-01159. 2 L 7 2 4F RT A16WE 1996110100077 19961101 00077 NM 1996 11 1 UPS96221394 1 19961008 A 5320 655343319 DOOR STOP BOEING 727 72722C 138400F NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE: C. LOWER AFT CARGO DOOR CUT OUT. DOOR STOP CRACKED AT AFT FRAME MID STOP. STOP REPLACED IAW SRM 51- 30-2. 2 L 7 3 4F A3WE 1996110100078 19961101 00078 NM 1996 11 1 UPS96221413 1 19961020 A 5313 STRINGER BOEING 727 72725C 138400H NM BS 87 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE: C. VERT STAB STRINGER 11 CRACKED BETWEEN TORQUE BOX LOWER CHORD AND FIN STA 87. REPAIR VERT STAB STR INGER IAW SRM 55-30-4 FIG 1. 2 L 7 3 4F A3WE 1996110100079 19961101 00079 NM 1996 11 1 UPS96221414 1 19960920 A 5330 SKIN BOEING 727 72725C 138400H NM BS 1330 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE: C. FUSELAGE SKIN CORRODED B/S 1330 BETWEEN STRINGER 7R AND 10R. CUTOUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIRED IAW SRM 53-30-3 FIG 12 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996110100080 19961101 00080 NM 1996 11 1 UPS96221415 1 19960926 A 5320 STRAP BOEING 727 72725C 138400H NM BS 1342 OUT OF LIMITS A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE: C. B/S 1342 LT OTBD UPPER T-CHORD STRAP OUT OF LIMITS. CUT OUT DAMAGED STRAP AT STA 1342. FABRICATE D STRAP DOUBLER AND INSTALLED PER SRM 51-40-4 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996110100081 19961101 00081 NM 1996 11 1 UPS96221416 1 19960918 A 5311 FRAME BOEING 727 72725C 138400H NM BS 1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE: C. B/S 1342 LT LOWER FRAME CHORD LBL 24 IS SEVERELY RUSTED. REMOVED AND REPLACED CHORD IAW SRM 51-30 -2. 2 L 7 3 4F A3WE 1996110100082 19961101 00082 NM 1996 11 1 UPS96221417 1 19960918 A 5311 FRAME BOEING 727 72725C 138400H NM BS 1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE: C. B/S 1342 RT LOWER FRAME CHORD SEVERELY CORRODED. REMOVED AND REPLACED FRAME CHORD IAW SRM 51-30-0 2. 2 L 7 3 4F A3WE 1996110100083 19961101 00083 NM 1996 11 1 UPS96221418 1 19960918 A 5320 CHANNEL BOEING 727 72725C 138400H NM BS 1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE: C. B/S 1342 LT CHANNEL LBL 18 WL 247 SEVERELY CORRODED. REMOVED AND REPLACED LT CHANNEL IAW SRM 51- 30-2. 2 L 7 3 4F A3WE 1996110100084 19961101 00084 NM 1996 11 1 UPS96221419 1 19960918 A 5320 CHANNEL BOEING 727 72725C 138400H NM BS 1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE: C. B/S 1342 RT CHANNEL RBL 18 WL 247 SEVERELY CORRODED. REMOVED AND REPAIRED RT CHANNEL IAW SRM 51- 30-2. 2 L 7 3 4F A3WE 1996110100085 19961101 00085 NM 1996 11 1 UPS96221420 1 19960918 A 5320 CHORD BOEING 727 72725C 138400H NM BS1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE: C. B/S 1342 LT OTBD CHORD LBL 30 WL 250 SEVERELY CORRODED. REMOVED AND REPLACED CHORD IAW SRM 51-30 -2. 2 L 7 3 4F A3WE 1996110100086 19961101 00086 NM 1996 11 1 UPS96221421 1 19960918 A 5320 CHORD BOEING 727 72725C 138400H NM BS 1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE: C. B/S 1342 RT OTBD CHORD RBL 30 WL 250 SEVERELY CORRODED. REMOVED AND REPLACED CHORD PER SRM 51-30- 2. 2 L 7 3 4F A3WE 1996110100087 19961101 00087 NM 1996 11 1 UPS96221423 1 19960918 A 5320 CHANNEL BOEING 727 72725C 138400H NM BS 1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE: C. B/S 1342 CENTER CHANNEL SEVERELY CORRODED. REMOVED AND REPLACED CENTER CHANNEL IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996110100088 19961101 00088 NM 1996 11 1 UPS96221424 1 19960919 A 5531 RIB BOEING 727 72725C 138400H NM VERT STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE: C. B/S 1367, FIN STA 22.5 RT RIB IS CRACKED. CUT OUT DAMAGED AREA, FABRICATED AN INSTALLED REPAIR PAR TS IAW SRM 51-40-3 AND 51-30-2. 2 L 7 3 4F A3WE 1996110100089 19961101 00089 NM 1996 11 1 UPS96221425 1 19960921 A 5320 SHEAR TIE BOEING 727 72725C 138400H NM BS 1283 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE: C. SHEAR TIE CORRODED AT B/S 1283 BETWEEN STRINGER 13L AND 14L. SHEAR TIE, FABRICATED SHEAR TIE PER BAC DWG 65-17500 AND INSTALLED SHEAR TIE PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996110100090 19961101 00090 NM 1996 11 1 UPS96221426 1 19960921 A 5320 SHEAR TIE BOEING 727 72725C 138400H NM BS 1303 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE: C. SHEAR TIE CORRODED AT BS B/S 1303 BETWEEN STR 12L AND 13L. REMOVED SHEAR TIE, FAB'D SHEAR TIE PER BAC DWG 6517500 AND INSTALLED PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996110100091 19961101 00091 NM 1996 11 1 UPS96221427 1 19960921 A 5320 SHEAR TIE BOEING 727 72725C 138400H NM BS 1303 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE: C. SHEAR TIE CORRODED AT BS 1303 BETWEEN STRINGERS 13L AND 14L. REMOVED SHEAR TIE AND FAB'D SHEAR TI E PER BAC DWG 65-17500 AND INSTALLED SHEAR TIE PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996110100092 19961101 00092 NM 1996 11 1 UPS96221428 1 19960921 A 5320 SHEAR TIE BOEING 727 72725C 138400H NM BS 1283 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE: C. SHEAR TIE CORRODED AT B/S 1283 BETWEEN STR'S 13R AND 14R. REMOVED SHEAR TIE AT B/S 1283, FAB'D SHE AR TIE PER DWG 65-17500 AND INSTALLED SHEAR TIE PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996110100093 19961101 00093 NM 1996 11 1 UPS96221429 1 19960921 A 5320 SHEAR TIE BOEING 727 72725C 138400H NM BS 1303 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE: C. SHEAR TIE CORRODED B/S 1303 BETWEEN STR'S 13R - 14R. REMOVED SHEAR TIE AT B/S 1303, FAB'D SHEAR TI E PER BAC DWG 65-17500 AND INSTALLED PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996110100094 19961101 00094 NM 1996 11 1 UPS96221430 1 19960921 A 5320 SHEAR TIE BOEING 727 72725C 138400H NM BS 1303 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE: C. SHEAR TIE CORRODED AT B/S 1303 BETWEEN STR'S 12R AND 13R. REMOVED SHEAR TIE, FAB'D SHEAR TIE PER B AC DWG 65-17500 AND INSTALLED PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996110100095 19961101 00095 NM 1996 11 1 UPS96221431 1 19960926 A 5320 T CHORD BOEING 727 72725C 138400H NM BS 1342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE: C. B/S 1342 LBL 15, RBL15 WL 280 UPPER T-CHORD CORRODED BEYOND LIMITS. REMOVED AND REPLACED T-CHORD IAW SRM 51-30-2 AND BAC DWG 65-17508. 2 L 7 3 4F A3WE 1996110100096 19961101 00096 NM 1996 11 1 UPS96221432 1 19961008 A 5320 ANGLE BOEING 727 72725C 138400H NM BS 1342 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE: C. B/S 1342 RT SKIN ATTACH ANGLE CRACKED. REMOVED, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51- 30-2 AND 51-40-3. 2 L 7 3 4F A3WE 1996110100097 19961101 00097 NM 1996 11 1 UPS96221437 1 19961016 A 5711 SPAR BOEING 727 72722C 138400F NM WS 349 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE: C. WHILE CARRYING OUT REPAIR TO LEADING EDGE AT WS 349 ON RT WING, CORROSION FOUND ON UPPER SURFACE O F FRONT SPAR UPPER CHORD. REPAIR CARRIED OUT PER BOEING INSTRUCTIONS. SEE SRS EO 96-35-005 REFERENCE UPS REPAIR AUTHO RIZATION ENGINEERING FILE NUMBER 727-57-17 43. 2 L 7 3 4F A3WE 1996110100098 19961101 00098 NM 1996 11 1 UPS96221438 1 19961004 A 7830 TR DOOR BOEING 727 72722C 138400F NM NR 3 ENGINE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE: C. NR 3 ENGINE TR LOWER DOOR CRACK 2.5 INCHES LONG LOCATED FWD RT SIDE IN A FORE/AFT DIRECTION. REPA IRED PER DEE HOWARD SRM SUPPLEMENT 78-30-01. 2 L 7 3 4F A3WE 1996110100099 19961101 00099 NM 1996 11 1 UPS96221439 1 19961010 A 5320 65931151 FITTING BOEING 727 72722C 138400F NM BS 500 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE: C. MAIN CARGO DOOR LATCH SUPPORT FITTING BS 500 LT FOUND CRACKED. REPLACED PER UPS EO B727-5310-0437 . 2 L 7 3 4F A3WE 1996110100100 19961101 00100 NM 1996 11 1 UPS96221440 1 19961007 A 5330 SKIN BOEING 727 72722C 138400F NM BS 440 OIL CANNING A IPXA K NONE C F.O.D. IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE: C. FUSELAGE AT BS 440 BETWEEN S21-S22L SKIN IS PANTING ( OIL CANNING). REPAIRED PER SRM 53-30-3 FIG 1. 2 L 7 3 4F A3WE 1996110100101 19961101 00101 NM 1996 11 1 UPS96221441 1 19961008 A 5320 655343319 STOP FITTING BOEING 727 72722C 138400F NM AFT CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE: C. LOWER AFT CARGO DOOR STOP CUT OUT. DOOR STOP CRACKED AT AFT FRAME MID STOP. REPLACED PER SRM 51- 30-2. 2 L 7 3 4F A3WE 1996110100102 19961101 00102 NM 1996 11 1 UPS96221443 1 19961022 A 5320 69341814 STRAP BOEING 727 72725C 138400H NM 2-24 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: SI. CORROSION ON OUTBOARD SEAT TRACK SPLICE STRAP STA 380 RBL 56 WL 207. REMOVED CORROSION, REWORK D EEMED OUT OF LIMITS IAW SRM 53-10-1. REPLACED SPLICE STRAP AT STA 380 RBL 56 IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996110100103 19961101 00103 NM 1996 11 1 UPS96221447 1 19961021 A 5530 69201622 FITTING BOEING 727 72725C 138400H NM VERT STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: SI. POSSIBLE CRACK IN ATTACH FITTING COMMON TO STR 11 UNDER PANEL 9780 RT VERT STAB (MARKED). REMOVE D AND REPLACED ATTACH FITTING AT RT VERT STAB STR 11 PER 51-30-2 OF THE SRM. 2 L 7 3 4F A3WE 1996110100104 19961101 00104 NM 1996 11 1 UPS96221448 1 19961020 A 5313 BAC1493522 STRINGER BOEING 727 72725C 138400H NM BS 863 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: SI. STR 5R CRACKED ON LOWER FLANGE LIP STA 863. REPAIRED PER SRM'S 53-10-3, 51-10-2, 51-30-2, 53-10-3 , 51-30-15. 2 L 7 3 4F A3WE 1996110100105 19961101 00105 NM 1996 11 1 UPS96221449 1 19961018 A 5754 RIB BOEING 727 72725C 138400H NM NR 1 LE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: SI. NR 1 SLAT FIRST RIB INBOARD OF TAIL DUCT CRACKED AT T/E CHORD ATTACH POINT. REPAIRED NR 1 SLAT F IRST RIB INBOARD OF TAIL DUCT PER SRM 57-30-3. 2 L 7 3 4F A3WE 1996110100106 19961101 00106 NM 1996 11 1 UPS96221450 1 19961016 A 5754 RIB BOEING 727 72725C 138400H NM NR 1 LE SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: SI. NR 1 SLAT, NR 2 RIB FROM INBOARD OF TAIL DUCT CRACKED AT T/E CHORD ATTACH POINT. REPAIRED NR 1 S LAT NR 2 RIB FROM INBOARD OF TAIL DUCT PER SRM 57-50-3. 2 L 7 3 4F A3WE 1996110100107 19961101 00107 NM 1996 11 1 UPS96221451 1 19961015 A 5754 692848211 RIB BOEING 727 72725C 138400H NM NR 3 LE SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: SI. NR 3 SLAT OUTBOARD END RIB IS CRACKED IN RADIUS. REMOVED AND REPLACED NR 3 SLAT O/B END RIB IAW SRM 51-30-2, 51-10-1. 2 L 7 3 4F A3WE 1996110100108 19961101 00108 NM 1996 11 1 UPS96221452 1 19961011 A 5330 SKIN BOEING 727 72722C 138400F NM CARGO DR CUTOUT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE: C. CRACK IN SKIN AT FWD CARGO DOOR (LWR) CUT OUT AFT LWR CORNER. REPAIR CARRIED OUT PER BOEING INSTR UCTIONS (SEE SRS EO 96-35-006) UPS EO B727-5330-8728-A. 2 L 7 3 4F A3WE 1996110100109 19961101 00109 NM 1996 11 1 UPS96221453 1 19961015 A 5754 65162276 JUMPER BOEING 727 72725C 138400H NM NR 6 LE SLAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: SI. NR 6 K-FLAP BULLNOSE BONDING JUMPER O/B UPPER ATTACH BOLT HAS PITTING AROUND BOLT HEAD. BLEND C ORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 57-50-0. K-FLAP ASSY WAS REPLACED ON NRC 597765. 2 L 7 3 4F A3WE 1996110100110 19961101 00110 NM 1996 11 1 UPS96221454 1 19961014 A 5754 TPN74 RIB BOEING 727 72725C 138400H NM NR 3 LE SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: SI. NR 3 SLAT 3RD RIB O/B OF ROD END ATTACH RIBS IS CRACKED IN RADIUS AT EXTRUDED CHORD ATTACH POINT. REMOVED AND REPLACED DOUBLER IAW SRM 57-50-3, 57-50-30. 2 L 7 3 4F A3WE 1996110100111 19961101 00111 NM 1996 11 1 UPS96221455 1 19961011 A 5754 651727115 RIB BOEING 727 72725C 138400H NM NR 4 LE SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: SI NR 4 SLAT INBD TRACK INBD RIB HAS TEMPORARY STOP DRILLED CRACK IN FLANGE. REMOVED AND REPLACED SRM 51-30-2, 51-30-5, OHM 57-51-61. 2 L 7 3 4F A3WE 1996110100112 19961101 00112 NM 1996 11 1 UPS96221456 1 19961022 A 5313 BAC1498142050 STRINGER BOEING 727 72725C 138400H NM BS 1110-1130 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: SI. CORROSION ON BACKSIDE OF STRINGER 12 TOP FLANGE STA 1110-1130 LT WL 246. REMOVED CORROSION, REWO RK DEEMED OUT OF LIMITS IAW SRM 53-10-1. REPAIRED STR 12L IAW SRM 53-10-3. 2 L 7 3 4F A3WE 1996110100113 19961101 00113 NM 1996 11 1 UPS96221457 1 19961022 A 5320 66151251 STIFFENER BOEING 727 72725C 138400H NM BS 745 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: SI. CORROSION AT BS 745 RBL 11 WL 168 AROUND FASTENER IN UPPER DELTA BEAM BOX. FOUND STIFFENER TO B E OUT OF LIMITS PER SRM 51-10-1, REMOVED AND REPLACED STIFFENER PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996110100114 19961101 00114 NM 1996 11 1 UPS96221458 1 19961021 A 5313 BAC1498110 STRINGER BOEING 727 72725C 138400H NM BS 990-1148 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: SI. CORROSION ON STR 3 LT STA 990-1148. FOUND CORROSION OUT OF LIMITS AT STR 3 LT BS 1037 AND 104. R EPAIRED PER SRM 51-10-1, 51-40-02, 51-30-2, 51-10-2, MM 51-20-151. 2 L 7 3 4F A3WE 1996110100115 19961101 00115 NM 1996 11 1 UPS96221459 1 19961023 A 3350 BATTERIES BOEING 727 7272A1 138407F NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE: FOUND BOTH EMERGENCY EXIT LIGHTS INOP. REPLACED NI-CAD BATTERIES. OPS CHECK GOOD. 2 L 7 3 4F A3WE 1996110100116 19961101 00116 NM 1996 11 1 UPS96221463 1 19961024 A 3350 LIGHTS BOEING 727 727247 138408F NM CABIN DIM A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 208UP 21701 EMERGENCY EXIT LIGHT ABOVE FWD ENTRY DOOR PARTIALLY LIT. REMOVED AND REINSTALLED EXIT LIGHT ASSY. OPS CHK GOOD. 2 L 7 3 4F A3WE 1996110100117 19961101 00117 WP 1996 11 1 UPS96821395 1 19960907 A 5522 5654970 SKIN DOUG DC8 DC873F 302199F WP RT ELEVATOR CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. MODERATE CORROSION ON RT ELEVATOR BOTTOM SKIN JUST FORWARD OF THE OUTBOARD END OF GEAR TAB. REP LACED MIDDLE LOWER SKIN PANEL PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1996110100118 19961101 00118 WP 1996 11 1 UPS96821396 1 19960911 A 5522 5654970 SKIN DOUG DC8 DC873F 302199F WP RT ELEVATOR CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. RT ELEVATOR UPPER MIDDLE SKIN HAS MODERATE CORROSION DAMAGE. REPLACED MIDDLE UPPER SKIN PER SR M 51-1-21. 2 L 7 4 4F RT 4A25 1996110100119 19961101 00119 WP 1996 11 1 UPS96821397 1 19960910 A 5347 DC853B203501 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 640-1280 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2 EXFOLIATED CORROSION ON CABIN SEAT TRACK, AT SEVERAL PLACES FS 640 THROUGH FS 1280 TRACK NR 9. R EPLACED TRACK SECTION PER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1996110100120 19961101 00120 WP 1996 11 1 UPS96821398 1 19960906 A 5320 3649114 FITTING DOUG DC8 DC873F 302199F WP BS 920 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. FS 920 LONGERON 23L RIGHT HAND ATTACH FITTING HAS MODERATE CORROSION. REPLACED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996110100121 19961101 00121 WP 1996 11 1 UPS96821399 1 19960907 A 5320 56434832N FITTING DOUG DC8 DC873F 302199F WP BS 878 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. HEAVY CORROSION AT FS 878 LONGERON 23R ATTACH FITTING. REPLACED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996110100122 19961101 00122 WP 1996 11 1 UPS96821400 1 19960907 A 5320 0717075T6 SHEAR TIE DOUG DC8 DC873F 302199F WP BS 702 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. FS 702 RBL 8 SHEAR TIE CRACKED AND HEAVILY CORRODED IN KEEL AREA. REPAIRED SHEAR TIE PER SRM 53 -2-0, FIG 2 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996110100123 19961101 00123 WP 1996 11 1 UPS96821401 1 19960917 A 5321 0322024T3 FLOOR PANS DOUG DC8 DC873F 302199F WP BS 55 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. FS 55 RBL 30 AND RBL 20. RECESSED FLOOR PANS HAVE EXFOLIATED. CORROSION REPLACED FLOOR PANS PE R SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996110100124 19961101 00124 WP 1996 11 1 UPS96821402 1 19960917 A 5320 0327075T6 INTERCOSTAL DOUG DC8 DC873F 302199F WP BS 50-40 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. INTERCOSTAL BEAM HAS EXFOLIATED CORROSION FS 40 TO 50 RBL 30 AT CABIN FLOOR BEAM. REPLACED INTE RCOSTAL SECTION PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996110100125 19961101 00125 WP 1996 11 1 UPS96821403 1 19960905 A 5320 4597643 FITTING DOUG DC8 DC873F 302199F WP BS 320 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. MODERATE CORROSION AT LONGERON 21L TO BELT FRAME FITTING FS 320. REPLACED FITTING PER SRM 51-1- 20D. 2 L 7 4 4F RT 4A25 1996110100126 19961101 00126 WP 1996 11 1 UPS96821404 1 19960908 A 5320 0907075T6 FITTING DOUG DC8 DC873F 302199F WP BS 980 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. RT WHEELWELL AFT CANTED BULKHEAD FITTING FS 980 RBL 38. HEAVY CORROSION. REPLACED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996110100127 19961101 00127 WP 1996 11 1 UPS96821405 1 19960906 A 5311 3773159 FRAME DOUG DC8 DC873F 302199F WP BS 1040 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. SPLICE FITTING HEAVY CORROSION ON BELT FRAME FS 1040, LONGERON 27R. REPLACED FITTING PER SRM 51 -1-20D. 2 L 7 4 4F RT 4A25 1996110100128 19961101 00128 WP 1996 11 1 UPS96821406 1 19960922 A 5320 0637075T6 ANGLE DOUG DC8 DC873F 302199F WP BS1540 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. FS 1540 LONGERON 30L VERTICAL SUPPORT ATTACH ANGLE HAS EXFOLIATED CORROSION. REPLACED ANGLE PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1996110100129 19961101 00129 WP 1996 11 1 UPS96821407 1 19960905 A 5313 DC8530093 LONGERON DOUG DC8 DC873F 302199F WP BS 430 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. FS 430 LONGERON 30R HEAVY CORROSION. REPAIRED LONGERON PER SRM 53-2-3 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996110100130 19961101 00130 WP 1996 11 1 UPS96821408 1 19960906 A 5320 3755822511 FITTING DOUG DC8 DC873F 302199F WP BS300 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. MODERATE CORROSION ON FITTING FS 300, BETWEEN LONGERONS 35R-36. REPLACED FITTING PER SRM 51-1-2 0D. 2 L 7 4 4F RT 4A25 1996110100131 19961101 00131 WP 1996 11 1 UPS96821409 1 19960906 A 5320 3755822 FITTING DOUG DC8 DC873F 302199F WP BS 280 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. MODERATE CORROSION ON B/T FITTING FS 280 BETWEEN LONGERONS 31L-32L. REPLACED FITTING PER SRM 53 -2-0 FIG 2D. 2 L 7 4 4F RT 4A25 1996110100132 19961101 00132 WP 1996 11 1 UPS96821410 1 19960906 A 5320 3755822505 FITTING DOUG DC8 DC873F 302199F WP BS 300 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. MODERATE CORROSION AT B/T FITTING FS 300, LONGERON 27L. REPLACED FITTING PER SRM 53-2-0. 2 L 7 4 4F RT 4A25 1996110100133 19961101 00133 WP 1996 11 1 UPS96821411 1 19960906 A 5313 3275597319600 LONGERON DOUG DC8 DC873F 302199F WP BS 300-280 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. HEAVY CORROSION ON LONGERON 32L FS 280-300. REPAIRED LONGERON PER SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 1996110100134 19961101 00134 WP 1996 11 1 UPS96821412 1 19960914 A 5320 9754002 ANGLE DOUG DC8 DC873F 302199F WP BS 280 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. HEAVY CORROSION ON SUPPORT ANGLE FS 280 AFT SIDE LONGERON 27L. REPLACED ANGLE PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996110100135 19961101 00135 WP 1996 11 1 UPS96821442 1 19960907 A 5320 5773846 SHEAR TIE DOUG DC8 DC873F 302199F WP BS 1720 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. FS 1720 AT LONGERON 26R HEAVY CORROSION ON SHEAR TIE. REPLACED SHEAR TIE SECTION PER SRM 51-1-2 0D. 2 L 7 4 4F RT 4A25 1996110100136 19961101 00136 WP 1996 11 1 UPS96821444 1 19960829 A 2560 375321341 LANYARD DOUG DC8 DC873F 302199F WP MAIN ENTRY DOOR FRAYED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. EVACUATION SLIDE LANYARD ASSY CABLE FRAYED. REPLACED LANYARD PER MM 25-60-01. 2 L 7 4 4F RT 4A25 1996110100137 19961101 00137 WP 1996 11 1 UPS96821445 1 19960910 A 5320 57501992 FITTING DOUG DC8 DC873F 302199F WP BS 937 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. HEAVY CORROSION AT FS 937 LONGERON FITTING AT LONGERON 24R. REPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996110100138 19961101 00138 WP 1996 11 1 UPS96821446 1 19960829 A 5330 577992549 SKIN DOUG DC8 DC873F 302199F WP BS 120-140 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. HEAVY CORROSION AT FUSELAGE SKIN PANEL FS 120-140 BETWEEN LONGERONS 3 5L-35R. REPAIRED PER UPS EO. 2 L 7 4 4F RT 4A25 1996110100139 19961101 00139 WP 1996 11 1 UPS96821460 1 19961011 A 5744 37511941 FITTING DOUG DC8 DC871F 302199D WP WS S98 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE: C. LT WING STA XRS98 FLAP CARRIAGE FITTING CRACKED. REPLACED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996110100140 19961101 00140 WP 1996 11 1 UPS96821461 1 19961011 A 5311 5764343 FRAME DOUG DC8 DC871F 302199D WP BS 1020 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE: C. HEAVY CORROSION ON BELT FRAME FS 1020 LONGERONS 35R-36. REPLACED BELT FRAME SECTION PER SRM 51-1- 21. 2 L 7 4 4F RT 4A25 1996110100141 19961101 00141 WP 1996 11 1 UPS96821462 1 19961007 A 5744 5751182505 FITTING DOUG DC8 DC871F 302199D WP WS 98 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE: C. LT WING FLAP STA XRS98 INBOARD CARRIAGE FITTING HAS 12 INCH LONG CRACK. REPLACED FITTING PER SRM 51-3-0 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1996110100142 19961101 00142 WP 1996 11 1 UPS96821465 1 19961007 A 5320 5750776 FITTING DOUG DC8 DC871F 302199D WP BS 879 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE: C. RT TRAPEZOID FITTING CRACKED AT HOLD-ON FWD SIDE JUST BELOW LONGERON 24R. REPAIRED FITTING PER DA C DRAWING NR 5750776. 2 L 7 4 4F RT 4A25 1996110100143 19961101 00143 WP 1996 11 1 UPS96821466 1 19961023 A 2120 DUCTS DOUG DC8 DC873F 302199F WP COCKPIT DIRTY A IPXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 813UP 46059 INSPECTION TYPE: CS2. (AIR TURN BACK) STRONG SMELL AND SKYDROL FUMES INSIDE COCKPIT DURING TEST FLIGHT. FOUND SKYDROL RESIDUES ON AIR CYCLE MACHINE DUCTS, WATER SEPARATOR SOCK DUE TO LEAK DURING MAINTENANCE CHECK. CLEANED DUCTS AND REPL ACED SOCKS PER MM 21-55-01. 2 L 7 4 4F RT 4A25 1996110100144 19961101 00144 NM 1996 11 1 96FDEA01603 1 19961022 A 8012 SUPPLY DUCT BOEING 727 72724C 1384005 NM NR 3 ENGINE BLOWN A A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 114FE 19527 FIRE LIGHT AND BELL NR 3 ENGINE AFTER TAKEOFF AT 600 FEET ABOVE GROUND LEVEL. AFTER THROTTLE BROUGHT TO IDLE FIRE LIGH T WENT OUT. BOTH FIRE LOOPS TEST GOOD. LANDED WITHOUT FURTHER INCIDENT. FOUND START VALVE SUPPLY DUCT BLOWN. REPLACE D DUCT NR 3 ENGINE. LEAK CHECK GOOD. OK FOR SERVICE. 2 L 7 3 4F A3WE 1996110100145 19961101 00145 NM 1996 11 1 96FDEA01604 1 19961021 A 3610 SUPPLY DUCT BOEING 727 7272S2F 1384O81 NM NR 1 ENGINE BURNT SMELL A FDEA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 25 216FE 22937 BURNT OIL SMELL FROM AIR CONDITIONING WHEN NR 1 BLEED USED FOR PACK AIR SOURCE ON DESCENT. REPEAT GRIPE. RAN NR 1 AND NR 3 ENGINES TOGETHER AND SEPARATELY AS AIR SOURCE . RAN LEFT AND RIGHT PACKS TOGETHER AND SEPARATELY WITH BOTH PACKS ON. USING NR 1 BLEED, ABLE TO GET A HOT PACK SMELL (VERY SLIGHT) , BUT WERE UNABLE TO DUPLICATE DISCREPANCY. FOUND OIL IN NR 1 ENGINE 6TH STAGE SUPPLY DUCT AT PYLON. ENGINE REMOVED PER WORK CARD 70T005. REMOVED AND REPLACED ENGINE NR 1 PER WORK CARD 70T0005 AND 70T0301. RAN ENGINE. OPERATIONAL AND LEAK CHECK GOOD. OK FOR SERVICE. 2 L 7 3 4F A3WE 1996110100146 19961101 00146 NM 1996 11 1 96FDEA01605 1 19961024 A 3260 INDICATION BOEING 727 72725C 138400H NM NLG MALFUNCTIONED A FDEA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 25 134FE 19852 ON INITIAL LANDING GEAR EXTENSION, NOSE GEAR DID NOT INDICATE DOWN AND LOCKED. RAN CHECK LIST AFTER GO AROUND ON SECON D EXTENSION INDICATED DOWN AND LOCKED. NOSE GEAR DOOR LIGHT WAS ILLUMINATED FOR AN EXCESSIVELY LONG TIME DURING EXTENSI ON. INSPECTED NOSE GEAR EXTEND SWITCHES. FOUND NO PROBLEMS, EXTENDED AND RETRACTED NOSE GEAR SEVERAL TIMES. FOUND NOS E GEAR OVER CENTER KNUCKLE DRY. LUBRICATED NOSE GEAR AND PERFORMED EXTENSION AND RETRACTION TEST PER MAINTENANCE MANUAL 32-30-0. WITHIN LIMITS, OK FOR SERVICE. 2 L 7 3 4F A3WE 1996110100147 19961101 00147 WP 1996 11 1 SCNA96317 1 19961020 A 2611 13131 LAMP DOUG DC10 DC1015 3022118 WP CARGO SMOKE DET FAILED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 152SY 48289 NR 1 SMOKE DETECTOR IN THE FORWARD CARGO COMPARTMENT DID NOT TEST. REMOVED AND REPLACED BULB AND OPS TESTED NORMAL. 2 L 7 3 4F A22WE 1996110100148 19961101 00148 1996 11 1 BIER960037 4 19961024 A 2562 E01 ELT ACK E01 PIPER PA28 PA28161 7102803 SO ELT FAILED TEST B BIEA K NONE L NO TEST IN INSP/MAINT 1 EA 21 3033D 015371 287916157 AT UNRELATED INSPECTION, TECH INSPECTED ELT IAW FAR 91.207 BY ACTIVATION OF ELT WITHIN 6 INCHES OF AM RADIO, THE RECOMME NDED PROCEDURE. THE RESULTS WERE SATISFACTORY. AN ADDITIONAL CHECK USING CALIBRATED AVIONICS TEST EQUIPMENT REVEALED A DISTORTED UNACCEPTABLE LOW OUTPUT. THE UNIT WAS RETURNED TO THE MFG FOR REPAIR/OVERHAUL.. SUBMITTER STATES THAT AS EVID ENCED BY THIS INSPECTION, THE FAA RECOMMENDED PROCEDURE FOR TESTING ELT OUTPUT MAY LEAD ONE TO A FALSE CONCLUSION AS TO THE AIRWORTHINESS OF THESE UNITS AND RECOMMENDS A CHANGE IN RECOMMENDED TEST PROCEDURES IF AN IMPROVEMENT IN RELIABILITY IS THE GOAL WITH THESE UNITS. 1 L 7 1 3O 2A13 1996110100149 19961101 00149 NM 1996 11 1 P5CA9600829 1 19961015 A 5320 654463334 ANGLE BOEING 747 747122 1384872 NM BS 1380 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 CRACKED SHEAR ANGLE AT STATION 1380 / RBL 100. REPAIRED PER BAC SERVICE BULLETIN 747 SB 2213. 2 L 7 4 4F A20WE 1996110100150 19961101 00150 NM 1996 11 1 P5CA9600830 1 19961023 A 5245 COVER, HINGE BOEING 747 747122 1384872 NM PACK DOOR DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 DAMAGED HINGE COVERS AT 3 POSITIONS ON AIR CONDITIONING PACK DOORS. REPAIRED PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1996110100151 19961101 00151 NM 1996 11 1 P5CA9600831 1 19961023 A 5400 FAIRING BOEING 747 747122 1384872 NM NR 3 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 CRACKED TIP ON NR 3 PYLON AFT FAIRING ABOVE STRINGER. REPAIRED PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1996110100152 19961101 00152 NM 1996 11 1 P5CA9600832 1 19961023 A 5400 DOUBLER BOEING 747 747122 1384872 NM NR 3 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 CRACKED DOUBLER ON NR 3 PYLON SLOT SEAL FAIRING. REPAIRED PER BAC SRM 54-30-03 FIG 6. 2 L 7 4 4F A20WE 1996110100153 19961101 00153 NM 1996 11 1 P5CA9600833 1 19961023 A 2612 BRACKET BOEING 747 747122 1384872 NM APU FIRE LOOP BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 TWO BROKEN ATTACH BRACKETS FOR APU FIRE LOOP ON APU DOOR. REPAIRED PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1996110100154 19961101 00154 NM 1996 11 1 CKSA96164 1 19961018 A 5320 INTERCOSTAL BOEING 747 747132 1384882 NM BS 2733 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 KOSC - DURING C-2 CHECK INSPECTION FOUND: APU COMPARTMENT STA 2733 RIGHT SIDE INTERCOSTAL CRACKED 3RD FROM BOTTOM OF FR AME. MANUFACTURED NEW INTERCOSTAL IAW B747 SRM 53-11-24. CLEANED AND TREATED AREA IAW B747 SRM 51-10-02 AND MM 51-21-0 2. INSTALLED NEW INTERCOSTAL IAW B747 SRM 51-30-02. C-CHECK WORK CARD NR 7TK0317. TASK CARD NR 85643. 2 L 7 4 4F A20WE 1996110100155 19961101 00155 NM 1996 11 1 CKSA96165 1 19961018 A 5320 65B0014895 FRAME BOEING 747 747132 1384882 NM APU COMPT CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 KOSC - DURING C-2 CHECK INSPECTION FOUND: APU COMPARTMENT RIGHT DOOR FORWARD LOWER FRAME CRACKED. CLEANED UP OF DAMAGE D AREA IAW B747 SRM 52-00-2. C-CHECK CARD NR 7TK0317. TASK CARD NR 85650. 2 L 7 4 4F A20WE 1996110100156 19961101 00156 NM 1996 11 1 CKSA96166 1 19961018 A 5320 2024T3040 DOUBLER BOEING 747 747132 1384882 NM BS 550 DISBONDED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 KOSC - DURING C-2 CHECK INSPECTION FOUND: A PIT STA 550R BETWEEN STR 35 AND 36 INNER DOUBLER DISBONDED. REPAIRED INNER DOUBLER IAW B747 SRM 53-30-2 FIGURE 3 AND ENGINEERING RESPONSE B4 05018. CORROSION CARD NR C53-110-01. TASK CARD NR 8 5605. 2 L 7 4 4F A20WE 1996110100157 19961101 00157 NM 1996 11 1 CKSA96167 1 19961018 A 5311 FRAME BOEING 747 747132 1384882 NM BS 880 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 KOSC - DURING C-2 CHECK INSPECTION FOUND: A PIT STA 880R CRACK IN FRAME ABOVE STA 37R. REPAIRED PER ENGINEERING RESPON SE B405021 AND AIA/E/2345. CORROSION CARD NR C53-110-01. TASK CARD NR 75767. 2 L 7 4 4F A20WE 1996110100158 19961101 00158 NM 1996 11 1 CKSA96168 1 19961018 A 5315 FLOOR BEAM BOEING 747 747132 1384882 NM BS 1780 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 KOSC - DURING C-2 CHECK INSPECTION FOUND: MAIN CARGO COMPARTMENT STA 1780 BL-ZERO UPPER CHORD OF FLOOR BEAM HAS EXFOLIA TION. REPAIRED IAW B747 SRM 51-40-4 AND 51-50-2. CORROSION CARD NR C53-210-01, PART 4 OF 8. TASK CARD NR 76169. 2 L 7 4 4F A20WE 1996110100159 19961101 00159 NM 1996 11 1 CKSA96169 1 19961018 A 5720 112U50257 FITTING BOEING 747 747132 1384882 NM WS 669.5 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 KOSC - DURING C-2 CHECK INSPECTION FOUND: CRACK IN RIB SUPPORT FITTING 65B01020-1137 WING STATION 669.5. REPLACED RIB SUPPORT FITTING IAW BOEING 747 SRM 51-10-1 AND 53-30-2. C-CHECK CARD NR 7GK0542. TASK CARD NR 85710. 2 L 7 4 4F A20WE 1996110100160 19961101 00160 NM 1996 11 1 CKSA96170 1 19961018 A 5720 112U505257 SHEAR TIE BOEING 747 747132 1384882 NM WS 670 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 KOSC - DURING C-2 CHECK INSPECTION FOUND: NR 2 MAIN TANK INTERIOR SHEAR TIE CRACKED WS 670 (FORWARD PYLON INBOARD STRUT SUPPORT APPROXIMATELY 11 INCHES AFT OF FORWARD SPAR) 1.50 INCH CRACK. REPAIRED SHEAR TIE IAW SB 747-57-2273 REV 2 FIGUR E 10 AND 11. AD 94-15-18 SID NR W-22C TASK CARD NR 85657. 2 L 7 4 4F A20WE 1996110100161 19961101 00161 NM 1996 11 1 CKSA96171 1 19961018 A 5347 BAC15201566 SEAT TRACK BOEING 747 747132 1384882 NM BS 1880 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 KOSC - DURING C-2 CHECK INSPECTION FOUND: CABIN: SEAT TRACK AT FS 1880 RBL 34 CORRODED. REMOVED CORROSION IAW B747 SRM 51-10-01, FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED TRACK IAW 51-10-01 AND 51-30-2. CORROSION TASK CARD NR C53- 210-01 PART 4 OF 8 TASK CARD NR 76192. 2 L 7 4 4F A20WE 1996110100162 19961101 00162 NM 1996 11 1 CKSA96172 1 19961018 A 5347 BAC15201566 SEAT TRACK BOEING 747 747132 1384882 NM BS 1860 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 KOSC - DURING C-2 CHECK INSPECTION FOUND: SEAT TRACK AT STA 1860 RBL 34 CORRODED. REMOVED AND REPLACED SEAT TRACK STA 1860 AS REQUIRED PER SRM'S 51-10-01 AND 51-30-2 AND 51-10-2. AD NR 94-15-18 SID NR W-44A TASK CARD NR 76194. 2 L 7 4 4F A20WE 1996110100163 19961101 00163 NM 1996 11 1 CKSA96173 1 19961018 A 5347 BAC15201566 SEAT TRACK BOEING 747 747132 1384882 NM BS 1905 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 KOSC - DURING C-2 CHECK INSPECTION FOUND: STA 1905 MAIN CABIN RBL 34 SEAT TRACK CORRODED. REMOVED AND REPLACED SEAT TR ACK STA 1905 PER SRM'S 51-10-01 AND 51-30-2, 51-10-2. C-CHECK CARD NR 7GK0232 TASK CARD NR 86824. 2 L 7 4 4F A20WE 1996110100164 19961101 00164 NM 1996 11 1 CKSA96174 1 19961018 A 5311 65B381764 FRAME BOEING 747 747132 1384882 NM BS 1700 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 KOSC - DURING C-2 CHECK INSPECTION FOUND: FS 1700 RBL 65 FLOOR FRAME CORRODED. REPAIRED PER AMERICAN INTERNATIONAL AIR WAYS ENGINEERING SKETCH AIA/E/2372. PART FABRICATION DOCUMENTED ON 4 EA M-59 FORMS. CORROSION TASK CARD NR C53-210-01 PART 4 OF 8. TASK CARD NR 76195. 2 L 7 4 4F A20WE 1996110100165 19961101 00165 NM 1996 11 1 CKSA96175 1 19961018 A 5330 SKIN BOEING 747 747132 1384882 NM BS 2220 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 KOSC - DURING C-2 CHECK INSPECTION FOUND: STATION 2220 STR 35R SKIN HAS CORROSION AT SHEAR TIE AND TEAR STRAP. REMOVE D CORROSION. CORROSION OUT OF LIMITS IAW SRM 53-30-01. REPAIRED DAMAGE IAW SRM 53-30-03 FIGURE 1. CORROSION TASK CARD NR C53-110-01 TASK CARD NR 76179. 2 L 7 4 4F A20WE 1996110100166 19961101 00166 NM 1996 11 1 CKSA96176 1 19961018 A 5347 BAC15201834 SEAT TRACK BOEING 747 747132 1384882 NM BS 1242 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 KOSC - DURING C-2 CHECK INSPECTION FOUND: CABIN: STATION 1242 MAIN CABIN RBL 82 SEAT TRACK FLANGE CORRODED. REMOVED C ORRODED SEAT TRACK AND REPAIRED IAW AIA/EA B405042 AND SKETCH AIA/E2359. INSTALLED FASTENERS IAW B747 SRM 51-30-02 ALOD INED AND PRIMED IAW B747 SRM 51-10-2. C-CHECK CARD NR 7GK0232 TASK CARD NR 86635. 2 L 7 4 4F A20WE 1996110100167 19961101 00167 NM 1996 11 1 CKSA96177 1 19961018 A 5711 SPAR CAP BOEING 747 747132 1384882 NM WS 1300 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 KOSC - DURING C-2 CHECK INSPECTION FOUND: RIGHT WING LEADING EDGE LOWER SPAR CAP CORRODED AT WS 1300. REMOVED CORRODED SPAR CAP AND REPAIRED IAW B747 SRM 57-30-03. CORROSION CARD NR C57-510-01. TASK CARD NR 85485. 2 L 7 4 4F A20WE 1996110100168 19961101 00168 NM 1996 11 1 CKSA96178 1 19961018 A 5347 BAC15201547 SEAT TRACK BOEING 747 747132 1384882 NM BS 1230 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 KOSC - DURING C-2 CHECK INSPECTION FOUND: STA 1230 RIGHT OUTBOARD SEAT TRACK HAS CORROSION ON INBOARD SIDE. REMOVED DA MAGED SEAT TRACK STA 1230 RIGHT OUTBOARD. REPAIRED IAW EER B4-05046 DATED 10-15-96 AND AIA SKETCH NR AIA/E/2359 DATED 10/4/96 8110-3 AIA ENGINEERING REPORT 96 AIA-151 DATED 10/15/96 EER B4-05035 DATED 10/4/96. C-CHECK CARD NR 7GK0232 TAS K CARD NR 87071. 2 L 7 4 4F A20WE 1996110100169 19961101 00169 NM 1996 11 1 CKSA96179 1 19961018 A 5315 BAC15201566 FLOOR BEAM BOEING 747 747132 1384882 NM BS 1820 CORRODED/SPLIT A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 KOSC - DURING C-2 CHECK INSPECTION FOUND: STA 1820 LBL 67 FLOOR BEAM UPPER CORD SPLIT AND CORRODED. REPAIRED FLOOR BEA M STA 1820 LBL 67 IAW REPORT NR 96AIA-152 AND 8110-3 DATED 10/15/96. CORROSION TASK CARD NR C53-110-01 TASK CARD NR 870 61. 2 L 7 4 4F A20WE 1996110100170 19961101 00170 NM 1996 11 1 CKSA96180 1 19961018 A 5330 SKIN BOEING 747 747132 1384882 NM BS 2055 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 KOSC - DURING C-2 CHECK INSPECTION FOUND: STA 2055 BETWEEN 37R AND 38R SKIN HAS CORROSION. CUT OUT DAMAGED AREA, FABRI CATED REPAIR IAW SRM 53-30-03 FIGURE 1. CORROSION TASK CARD NR C53-110-01. TASK CARD NR 86602. 2 L 7 4 4F A20WE 1996110100171 19961101 00171 NM 1996 11 1 CKSA96181 1 19961018 A 5230 FRAME BOEING 747 747132 1384882 NM CARGO DOOR CORROSION A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 KOSC - DURING C-2 CHECK INSPECTION FOUND: AFT PIT CARGO DOOR AFT FRAME BEHIND LOCK SWITCH SKIN HAS CORROSION. REPAIRED IAW SKETCH AIA/EI2357. CORROSION TASK CARD NR C53-110-01. TASK CARD NR 76020. 2 L 7 4 4F A20WE 1996110100172 19961101 00172 NM 1996 11 1 CKSA96182 1 19961018 A 5320 ANGLE BOEING 747 747132 1384882 NM BS 680 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 KOSC - DURING C-2 CHECK INSPECTION FOUND: A PIT STA 680L ABOVE STRINGER 38 INNER CORD REINFORCEMENT ANGLE CRACKED. RE MOVED CRACKED ANGLE. VERIFIED AND FABRICATE NEW ANGLE IAW SRM'S 53-10-21, 51-30-02, 51-10-02, AND MM 51-21-02. AD NR 9 3-08-12 CORROSION TASK CARD NR C53-110-01 TASK CARD NR 86592. 2 L 7 4 4F A20WE 1996110100173 19961101 00173 NM 1996 11 1 CKSA96184 1 19961018 A 5320 ANGLE BOEING 747 747132 1384882 NM BS 560 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 KOSC - DURING C-2 CHECK INSPECTION FOUND: A PIT STA 560 LEFT INNER CORD LOWER SUPPORT ANGLE CRACKED IN RADIUS ABOVE STR 39. REMOVED CRACKED ANGLE AND FABRICATED NEW ANGLE PER SRM 51-10-21. INSTALLED NEW ANGLE PER SRM'S 51-10-02, 51-21-02 AND MM AND SRM 51-30-02. REF M-40 86588 AD NR 86-18-01 AND CORROSION TASK CARD NR C53-110-01 TASK CARD NR 86587. 2 L 7 4 4F A20WE 1996110100174 19961101 00174 NM 1996 11 1 CKSA96185 1 19961018 A 5313 STRINGER BOEING 747 747132 1384882 NM BS 743 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 KOSC - DURING C-2 CHECK INSPECTION FOUND: A PIT STA 743R CRACK IN STRINGER 44 AT RIVET. REPAIRED IAW SRM 53-10-3. CO RROSION TASK CARD NR C53-110-01, TASK CARD NR 75771. 2 L 7 4 4F A20WE 1996110100175 19961101 00175 NM 1996 11 1 CKSA96186 1 19961018 A 5320 65B07627503 ANGLE BOEING 747 747132 1384882 NM BS 330 CORROSION A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 KOSC - DURING C-2 CHECK INSPECTION FOUND: FLOOR BEAM ANGLE AT FS 330 UPPER CABIN HAS CORROSION FROM LBL 6 TO FUSELAGE S KIN. REPAIRED IAW ENGINEERING DOC B405022. C-CHECK TASK CARD NR 7GK0224,TASK CARD NR 76102. 2 L 7 4 4F A20WE 1996110100176 19961101 00176 NM 1996 11 1 CKSA96187 1 19961018 A 5347 BAC15201834 SEAT TRACK BOEING 747 747132 1384882 NM BS 1210-1265 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 KOSC - DURING C-2 CHECK INSPECTION FOUND: SEAT TRACK REPAIR BETWEEN STA 1210 AND 1265 LBL 75 CORRODED. REMOVED AND REP LACED IAW SRM 51-30-02 AND AIA/E/2359. C-CHECK CARD NR 7GK0232 TASK CARD NR 87072. 2 L 7 4 4F A20WE 1996110100240 19961101 00240 NM 1996 11 1 CALA9601509 1 19961023 A 3350 S1356A36 LIGHT BOEING 747 747230B 1384889 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 78019 20527 INSPECTION FOUND LEFT EMERGENCY CEILING LIGHT B-ZONE, FOURTH LIGHT BACK INOPERATIVE. THE EMERGENCY CEILING LIGHT WAS RE MOVED AND REPLACED. 2 L 7 4 4F A20WE 1996110100241 19961101 00241 NM 1996 11 1 CALA9601510 1 19961024 A 2913 5718610 HYD PUMP BOEING 737 737524 1384721 NM B-HYD SYS LEAKING A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 33637 1902 1902 27540 AIRCRAFT LOST B-SYSTEM HYDRAULICS WHILE EN ROUTE. THE AIRCRAFT WAS DIVERTED TO EWR WHERE IT LANDED WITHOUT INCIDENT. M AINTENANCE FOUND THE HYDRAULIC LEAK ON THE RT ELECTRIC B-PUMP PRESSURE ACCESS PLUG. THE O-RING ON THE PLUG WAS FOUND BR OKEN. THE O-RING WAS REMOVED AND REPLACED. THE B-SYSTEM HYDRAULIC RESERVOIR WAS SERVICED TO FULL PER MM 12-12-00. LEA K AND OPERATIONAL CHECKS DURING RUN OF B-SYSTEM HYDRAULIC PUMPS WERE GOOD. 2 L 7 2 4F RT A16WE 1996110100242 19961101 00242 WP 1996 11 1 CALA9601511 1 19961025 A 3260 DC00F14S7S CONNECTOR DOUG DC10 DC1030 3023501 WP RT MLG PULLED WIRE A CALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SW 09 12061 47851 THE RT MLG RED UNSAFE LIGHT ILLUMINATED DURING APPROACH FOR LANDING AT LGW. THE APPROACH WAS ABORTED AND ALTERNATE GEAR EXTENSION WAS USED. GEAR DOWN INDICATIONS WERE NORMAL AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT MLG PROXIMITY DOWNLOCK SENSOR WIRING PULLED FROM R5-261 CONNECTOR. THE CONNECTOR WAS REPLACED AND CONDUIT WAS REROU TED, GROUND OPERATIONAL CHECKS WERE GOOD. 2 L 7 3 4F A22WE 1996110100243 19961101 00243 NM 1996 11 1 CALA9601512 1 19961024 A 3350 FUSE BOEING 737 7373T0 1384582 NM BATTERY PACK BLOWN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 34315 23366 INSPECTION FOUND CENTER SECTION OF EMERGENCY SEAT TRACK LIGHTS INOPERATIVE DURING A PREFLIGHT CHECK. MAINTENANCE FOUND LOWER FUSE BLOWN ON THE AFT EMERGENCY BATTERY PACK. THE FUSE WAS REPLACED AND OPERATION OF THE SEAT TRACK LIGHTS WAS RE STORED. 2 L 7 2 4F RT A16WE 1996110100244 19961101 00244 EA 1996 11 1 COMA9660178 1 19961023 A 2910 NAS16124 O-RING CNDAIR CL600 CL6002B19 EA NLG CUT A COMA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 967CA 257 7134 HYDRAULIC LEAK AT NOSE LANDING GEAR AREA. REPLACED CUT O-RING AT THE NWS PRESSURE SWITCH. 2 L 7 2 4F RT A21EA 1996110100245 19961101 00245 EA 1996 11 1 COMA9660179 1 19961023 A 2701 NAS142314 NUT CNDAIR CL600 CL6002B19 EA CONTROL COLUMN LOOSE A A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 941CA 5266 7050 COPILOTS CONTROL YOKE IS CATCHING AT EXTREME ENDS OF TRAVEL. RETORQUED THE CONTROL YOKE RETAINING NUT. FLIGHT CONTROL SYSTEM FUNCTION CHECK NORMAL. 2 L 7 2 4F RT A21EA 1996110100246 19961101 00246 EA 1996 11 1 COMA9660180 1 19961022 A 3030 2SC1175A CURRENT SENSOR CNDAIR CL600 CL6002B19 EA PITOT HEAT FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 164D 120164 PITOT STATIC HEAT INOP. REPLACED THE CURRENT SENSOR. 2 L 7 2 4F RT A21EA 1996110100247 19961101 00247 NM 1996 11 1 SWAA961171 1 19961022 A 2730 65C2546512 ELEV FEEL UNIT BOEING 737 7373T5 NM TAIL MALFUNCTIONED A A SWAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 07 692SW 23062 AIRCRAFT WAS DIFFICULT TO ROTATE ON TAKEOFF. NOSE WOULD NOT COME UP WITH NORMAL BACK PRESSURE. NOSE FINALLY ROSE AFTER SEVERAL INCHES OF ADDITIONAL YOKE DISPLACEMENT. RESISTANCE WAS NOT EXCESSIVE, BUT DISPLACEMENT WAS. RETURNED TO PHX A ND MADE AN UNEVENTFUL LANDING. REPLACED ELEVATOR FEEL AND CENTERING UNIT PER BOEING M/M. UNIT WAS FOUND TO HAVE A BENT INPUT ARM. 2 L 7 2 4F RT A16WE 1996110100248 19961101 00248 NM 1996 11 1 96FDEA01606 1 19961023 A 5320 651627910 BEAM BOEING 727 727233 138408A NM BS 807 - 812 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 NR 0713 004. CORROSION (C53-224-01 (2)) ON LONGITUDINAL BEAM AT BS 807 - BS 812 LBL 45 WL 208. REMOVED AND REPLACED L ONGITUDINAL BEAM AT BS 740-848, LBL 45 WL 208. 2 L 7 3 4F RT A3WE 1996110100249 19961101 00249 NM 1996 11 1 96FDEA01607 1 19961023 A 5311 BAC1514329 FRAME BOEING 727 727233 138408A NM BS 203.8 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 NR 0100, CORROSION NOSE E-BAY FRAME BS 203.8 LBL 15 WL 170 UPPER AND LOWER SURFACE OF UPPER CHORD. *S/D* REPAIRED NOSE E-BAY FRAME BS 203.8 LBL 15 WL 170 UPPER AND LOWER SURFACE OF UPPER CHORD PER FEDEX SRM 51-40-4. 2 L 7 3 4F RT A3WE 1996110100250 19961101 00250 NM 1996 11 1 96FDEA01608 1 19961007 A 5330 SKIN BOEING 727 727223 1384074 NM BS 715 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 281FE 22348 LOWER FUSELAGE OUTER SKIN HAS CORROSION BLOW OUT AT FUSELAGE STATION 715 RT AT STRINGER 28 RT, BETWEEN STRINGER AND INTE RCOSTAL INSIDE FUSELAGE. CORROSION REMOVED BY CUTTING OUT DAMAGED AREA PER SRM 51-10-6, REPAIRED DOUBLER INSTALLED PER SRM 53-30-3 FIG 3 PAGE 12 TO 14 A. 2 L 7 3 4F A3WE 1996110100251 19961101 00251 NM 1996 11 1 96FDEA01609 1 19961011 A 5347 4029040 TIE DOWN TRACK BOEING 727 727223 1384074 NM BS 690-740 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 281FE 22348 NR 0869, CORROSION ON TOP SIDE OF INBD LEG OF CABIN TIE DOWN TRACK STA 690 TO 692 LBL 23. NR 0870, CORROSION TOP SIDE I NBD TIE DOWN TRACK STA 720A TO 720B LBL 23. NR 0874, CORROSION TOP SIDE OF OUTBD LEG OF TIE DOWN TRACK STA 720B TO 740 AREA LBL 25. REMOVED DAMAGED BELOW LIMITS ON SEAT TRACK. INSTALLED NEW SEAT FLOOR TRACK STA 690 TO 740 LBL 24 PER SRM 53-10-5. 2 L 7 3 4F A3WE 1996110100252 19961101 00252 NM 1996 11 1 96FDEA01610 1 19961012 A 5311 FRAME BOEING 727 727233 138408A NM BS 804.5 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 281FE 22348 MAIN CARGO STA 804.5 STR 14R BELL FRAME HAS CRACK. INSTALLED DOUBLER PER SRM 51-40-3. 2 L 7 3 4F RT A3WE 1996110100253 19961101 00253 NM 1996 11 1 96FDEA01611 1 19961012 A 5311 FRAME BOEING 727 727223 1384074 NM BS 804.5 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 281FE 22348 UPPER LOBE CARGO COMPARTMENT, FRAME 804.5 4H HAS CRACK AT ATTACHMENT. BELT FRAME TO STRINGER AT STRINGER 144H CRACK AT FASTENER. STOP DRILLED CRACK PER SRM 51-10-01 PG 6B. INSTALLED DOUBLER PER SRM 51-40-3 PG 1 FIG 1. 2 L 7 3 4F A3WE 1996110100254 19961101 00254 WP 1996 11 1 DLL10962310 1 19961014 A 3350 P4010021 BATTERY LKHEED 1011 10113851 5265010 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 735D 193C1226 FLASHLIGHT AT 4R INOP. REPLACED BATTERY, BULB AND PLACARD. 2 L 7 3 4F A23WE 1996110100255 19961101 00255 NM 1996 11 1 DLM11962311 1 19961008 A 2450 CABLES DOUG MD11 MD11 3023602 NM NR 2 GENERATOR CHAFED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 801DE 48472 NR 2 ENGINE GENERATOR FEEDER CABLES CHAFED ABOVE RIGHT HAND OVER WING EXIT. REPAIRED PER ERA 358406 14. 2 L 7 3 4F RT A22WE 1996110100256 19961101 00256 NM 1996 11 1 DLM88962312 1 19961014 A 4990 38005041 APU DOUG MD88 MD88 3023688 NM APU COMP FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 982DL 53273 AFTER T/O CREW REPORTED, SMOKE IN CABIN WITH A VERY BAD ODOR. FLT RETURNED TO COS. FOUND OIL LEAKING FROM APU CHIP DET ECTOR. OIL BEING INJECTED INTO THE INTAKE. REPLACED CHIP DETECTOR. 2 L 7 2 4F RT A6WE 1996110100257 19961101 00257 1996 11 1 DLM88962313 2 19961014 A 7200 ENGINE DOUG MD88 MD88 3023688 NM PWA NR 1 BIRD STRIKE A DALA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 902DE 17180 53379 725582 AFTER TAKEOFF GOT STRONG SMOKE ODOR THROUGHOUT CABIN FRONT TO AFT. ACFT INJUSTED BIRD IN NR 1 ENGINE AFTER TAKEOFF. EV IDENCE SHOWS IT WENT THROUGH COMPRESSOR. BORO, OK. 2 L 7 2 4F RT A6WE 1996110100258 19961101 00258 NM 1996 11 1 DL757962316 1 19961015 A 2530 COFFEE MAKER BOEING 757 757232 1384965 NM AFT GALLEY ODOR A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 661DN 24972 AFT GALLEY COFFEEMAKER CAPT SIDE CREATES A BURNT/TOXIC ODOR IN FLIGHT. REPLACED DISPENSER, LEAK CK GOOD AND OP CK NORM AL. 2 L 7 2 4F RT A2NM 1996110100259 19961101 00259 NM 1996 11 1 DLM11962317 1 19961015 A 3350 LIGHT DOUG MD11 MD11 3023602 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 811DE 48566 FIRST CLASS EMERGENCY LIGHTS INOP. REPLACED FLOOR TRACK LIGHT SOCKET AT SEAT 1E. CLEANED AND RESEATED CONNECTORS ON FI RST CLASS CONTROLLER AND POWER SUPPLY U1756, OPS CHECKS OK. 2 L 7 3 4F RT A22WE 1996110100260 19961101 00260 NM 1996 11 1 DL72S962318 1 19961015 A 3350 LIGHT BOEING 727 727232 1384082 NM COCKPIT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 400DA 21144 EMERGENCY EXIT LIGHT IN COCKPIT FOUND INOP (P/N 334701743) (S/N 3874). REPLACED ASSEMBLY WITH (S/N 5829), OPERATION CKS GOOD. 2 L 7 3 4F A3WE 1996110100261 19961101 00261 NM 1996 11 1 DL757962319 1 19961015 A 2560 MEGAPHONE BOEING 757 757232 1384965 NM CABIN WEAK A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 667DN 25035 MEGAPHONE WEAK. REPLACED MEGAPHONE. 2 L 7 2 4F RT A2NM 1996110100262 19961101 00262 NM 1996 11 1 DL72P962323 1 19961009 A 5530 STRINGER BOEING 727 727225 1384077 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8891Z 21860 FOUND DURING HMV, STRINGER 6L FIN ST IS CRACKED. INSTALLED NEW ANGLE PER M/M 55-30-0. 2 L 7 3 4F A3WE 1996110100263 19961101 00263 NM 1996 11 1 DL72P962324 1 19961009 A 5530 STRINGER BOEING 727 727225 1384077 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8891Z 21860 FOUND DURING HMV, STRINGER 10L FIN ST 133.80 IS CRACKED. INSTALLED REPAIR ANGLE PER M/M 53-30-0 FIG 803. 2 L 7 3 4F A3WE 1996110100264 19961101 00264 NM 1996 11 1 DL72P962325 1 19961009 A 5530 STRINGER BOEING 727 727225 1384077 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8891Z 21860 FOUND DURING HMV, STRINGER 6L FIN STA 157.2 IS CRACKED. INSTALLED NEW ANGLE PER M/M 55-30-0. 2 L 7 3 4F A3WE 1996110100265 19961101 00265 NM 1996 11 1 DL72P962326 1 19961009 A 5343 BEARNG BOEING 727 727225 1384077 NM NLG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8891Z 21860 FOUND DURING HMV, PITTING ON I/B FACE AND LOWER SURFACE OF CAP OF NLG PIVOT BEARING. REMOVED CORROSION PER SRM 53-40-1. 2 L 7 3 4F A3WE 1996110100266 19961101 00266 NM 1996 11 1 DL72P962327 1 19961009 A 5343 BEARNG BOEING 727 727225 1384077 NM NLG CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8891Z 21860 FOUND DURING HMV, PITTING ON I/B FACE OF NLG PIVOT BEARING CAP. REPAIRED AND REMOVED CORRISION PER SRM 53-40-1. 2 L 7 3 4F A3WE 1996110100267 19961101 00267 NM 1996 11 1 DL72P962328 1 19961009 A 5343 BEARNG BOEING 727 727225 1384077 NM NLG CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8891Z 21860 FOUND DURING HMV, PITTING ON FWD AND AFT FACE AND TOP SURFACE OF NLG PIVOT BEARING CAP. REPAIRED AND REMOVED CORROSION PER SRM 53-40-1. 2 L 7 3 4F A3WE 1996110100268 19961101 00268 NM 1996 11 1 DL72P962329 1 19961009 A 5343 BEARNG BOEING 727 727225 1384077 NM NLG CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8891Z 21860 FOUND DURING HMV, PITTING ON FWD AND AFT FACE OF NLG PIVOT BEARING CAP. REPAIRED AND REMOVED CORROSION PER SRM 53-40-1. 2 L 7 3 4F A3WE 1996110100269 19961101 00269 WP 1996 11 1 DLL14962331 1 19961016 A 3350 BATTERY PACK RPS1 LKHEED 1011 1011385115 5265015 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 740DA 80 193C1244 E-PATH LIGHTS ON, IN BOTH AISLES IN SECTIONS. REPLACED BATTERY PACK AND RACK AT 2L DOOR FOR E-PATH, OPN NORMAL. 2 L 7 3 4F A23WE 1996110100270 19961101 00270 NM 1996 11 1 DL72W962332 1 19961016 A 5720 STIFFENER BOEING 727 727247 138408F NM RT WING LE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2816W 20872 A 1 INCH CRACK IN WING L/E VERTICAL STIFFENER AT NR 5 SLAT I/B TRACK O/B POSITION. REPLACED STIFFENER PER M/M. 2 L 7 3 4F A3WE 1996110100271 19961101 00271 NM 1996 11 1 DL72W962333 1 19961016 A 5240 FRAME BOEING 727 727247 138408F NM RT SERVICE DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2816W 20872 RT AFT SERVICE DOOR FWD FRAME CRACKED .5 INCH AT LWR I/B CORNER OF UPPER HINGE CUTOUT. REPAIRED PER SRM 52-40-2 FIG 4. 2 L 7 3 4F A3WE 1996110100272 19961101 00272 NM 1996 11 1 DL76L962334 1 19961016 A 3150 EEC SW PANEL 233T324210 BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE FAULTY A DALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 27 175DN 24803 724416 AFTER T/O, RT ENG EEC ALTN LIGHT CAME ON, EPR NORMAL NO EICAS MSG. REPLACED EEC SWITCH LIGHT PANEL, OPS CHECK OK. 2 L 7 2 4F 4 F RT A1NM E24NE 1996110100273 19961101 00273 NM 1996 11 1 DL757962335 1 19961010 A 5720 TE WEDGE BOEING 757 757232 1384965 NM WING DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 649DL 24389 T/E WEDGE DELAMINATED ALONG FORWARD SPAR. REPLACED WEDGE PER SRM 57-43-02 FIG 202. 2 L 7 2 4F RT A2NM 1996110100274 19961101 00274 NM 1996 11 1 DL72W962336 1 19961016 A 5240 FRAME BOEING 727 727247 138408F NM RT SERVICE DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2816W 20872 RT AFT SERVICE DOOR FWD FRAME CRACKED .5 INCH AT LOWER I/B CORNER OF UPPER HINGE CUTOUT. REPAIRED PER SRM 52-40-2 FIG 4 . 2 L 7 3 4F A3WE 1996110100275 19961101 00275 NM 1996 11 1 DL72L962338 1 19961017 A 5240 FRAME BOEING 727 727232 1384082 NM LT AFT DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 506DA 21308 FOUND ON D-2 LETTER CK, .375 INCH VISIBLE CRACK LT AFT SERVICE DOOR PAN AT UPPER HINGE CUTOUT. REPAIRED PER SRM 52-40-2 . 2 L 7 3 4F A3WE 1996110100276 19961101 00276 WP 1996 11 1 DLL16962339 1 19961017 A 3350 POWER SUPPLY 516574 LKHEED 1011 10113853 5265020 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 761DA 60834 193Y1208 DURING LAYOVER INSPECTION OF EMERGENCY TRACK LIGHTING SYSTEM, TRACK LIGHTS WENT OUT AFTER 2 MINUTES. NOTICED POWER SUPP LY\CHARGING ERRATICALLY FOR A MINUTE AND THEN STOPPED ALL TOGETHER. REPLACED POWER SUPPLY ASSY AND OPERATION CHECKS NOR MAL. 2 L 7 3 4F A23WE 1996110100277 19961101 00277 WP 1996 11 1 DLL16962340 1 19961017 A 3350 POWER SUPPLY 516574 LKHEED 1011 10113853 5265020 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 761DA 65562 193Y1208 ON L/O, FOUND F/C EMERGENCY TRACK LIGHTING INOP. REPLACED POWER SUPPLY RT HAND SIDE, OPS CHK NORMAL. 2 L 7 3 4F A23WE 1996110100278 19961101 00278 WP 1996 11 1 DLL16962341 1 19961017 A 3350 POWER SUPPLY 516574 LKHEED 1011 10113853 5265020 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 761DA 38036 193Y1208 ON L/O, FOUND EXTERIOR EMERGENCY LIGHTS FWD PART OF A/C EXTINGUISHED AFTER 2 MINUTES OF TEST. REPLACED POWER SUPPLY, OP S CHK OK. 2 L 7 3 4F A23WE 1996110100279 19961101 00279 NM 1996 11 1 DL76S962342 1 19961018 A 2121 732591D COOLING FAN BOEING 767 767332 1382001 NM COCKPIT FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 116DL 23275 ELECTRICAL WIRING SMELL NOTICED IN COCKPIT AT 1,000 FT AGL ON APPROACH. SMELL INCREASED THROUGH LANDING. REPLACED EXHA UST RACK COOLING FAN FOR POPPING C/B, EQUIP COOLING NOW CHKS OK. 2 L 7 2 4F RT A1NM 1996110100280 19961101 00280 NE 1996 11 1 DLM11962343 2 19961017 A 7530 04P238 SOLENOID DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE NR 1 ENGINE MALFUNCTIONED A DALA K NONE E VIBRATION/BUFFET TO TAKEOFF 1 SO 27 803DE 48474 723951 AFTER T/O, PILOT NOTICED SLIGHTLY MORE THAN NORMAL AIRFRAME VIBRATION AND NOISE. DURING CLIMB F/A AT DOOR 3L COMPLAINED OF VIBS IN FLOOR. FOUND NR 1 ENGINE LEFT HALF THRUST REVERSER DAMAGED DUE TO UNSCHEDULED OPENING OF 2.9 STABILITY BLEE D VALVE. REPLACED 2.9 BLEED VALVE SOLENOID. 2 L 7 3 4F 4 F RT A22WE E24NE 1996110100281 19961101 00281 NM 1996 11 1 DL73K962355 1 19961018 A 3350 BPS73 CHARGER BOEING 737 737232 1384475 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 319DL 23091 FOUND ON L/O CHECK, EMERGENCY FLOOR TRACK LIGHTING HAS A SECTION INOP. REPLACED CHARGER ASSY, OPS CHECK NORMAL. 2 L 7 2 4F RT A16WE 1996110100282 19961101 00282 NM 1996 11 1 DL76S962358 1 19961019 A 3610 212T312713 DUCT BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 1 ENGINE CRACKED A DALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 SO 27 118DL 23277 580156 LT BLEED DUCT LIGHT ON AT FL 390. FOUND BLEED DUCT CRACKED IN WING JUST INBOARD OF LT ENGINE PYLON. REPLACED DUCT. 2 L 7 2 4F 4 F RT A1NM E13NE 1996110100283 19961101 00283 NM 1996 11 1 DLM88962361 1 19961020 A 2910 7936913576 HYDRAULIC LINE DOUG MD88 MD88 3023688 NM FUSELAGE LEAKING A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 945DL 49818 SMOKE IN CABIN DURING T/O, SMOKE DETECTORS WENT OFF AND SMOKE DISAPPEARED DURING T/O THRUST. REPLACED HYD LINE IN 48 SE CTION DROPPING FLUID INTO APU INLET. 2 L 7 2 4F RT A6WE 1996110100284 19961101 00284 NM 1996 11 1 DL73K962366 1 19961020 A 3350 LIGHT BOEING 737 737232 1384475 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 320DL 23092 FOUND ON SERVICE CHECK, TRACK LIGHT AT 2C INOP. INSTALLED NEW LIGHT ASSY WITH NEW SPLICES, OPN NORMAL. 2 L 7 2 4F RT A16WE 1996110100285 19961101 00285 NM 1996 11 1 DLM88962368 1 19961021 A 4900 38005041 APU DOUG MD88 MD88 3023688 NM AFT FUSELAGE DIRTY A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 970DL 43173 SMOKE REPORTED IN AFT CABIN IMMEDIATELY AFTER T/O. AFT LAV\SMOKE DETECTOR WENT OFF, UNUSUAL SMELL IN COCKPIT. FOUND OI L LEAKING FROM APU, FWD APU TO MCO AND PLAC. CLEANED OILY AREA AROUND APU INLET, REPLACED WATER SEPARATOR BAGS AND SYST EM CHECKS NORMAL. 2 L 7 2 4F RT A6WE 1996110100286 19961101 00286 NM 1996 11 1 DL72S962369 1 19961021 A 3350 900542 PWR SUPPLY BOEING 727 727232 1384082 NM CARGO DOOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 489DA 21019 ON L/O, FOUND EMER LGT ON AFT CARGO DOOR INOP. REPLACED PWR SUPPLY AND CONDUIT. 2 L 7 3 4F A3WE 1996110100287 19961101 00287 NM 1996 11 1 DL757962378 1 19961022 A 3350 LIGHT GE167271 BOEING 757 757232 1384965 NM CABIN DAMAGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 608DA 22815 L2 EXIT DOOR SIGN DAMAGED. REPLACED LIGHT ASSEMBLY, OPS CKS NORMAL. 2 L 7 2 4F RT A2NM 1996110100288 19961101 00288 NE 1996 11 1 DLL10962379 2 19961023 A 7260 GEAR BOX M06157 LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B NE NR 2 ENGINE FAILED A A DALA E ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 SO 27 716DA 193C1095 14703 ENGINE NR 2 SHUT DOWN IN FLT DUE TO INSTANT LOSS OF OIL QUANTITY. SERVICED ENG WITH OIL, OIL LEAKING FROM STARTER PAD C LAMP. REMOVED ACCESSORY DRIVE CHIP DETECTOR HOUSING. PIECES OF METAL VISABLE IN HOUSING. ACCESSORY DRIVE GEAR BOX REP LACEMENT IN PROGRESS. 2 L 7 3 4F 4 F A23WE E12EU 1996110100289 19961101 00289 NM 1996 11 1 DL72S962380 1 19961023 A 5751 652176633 AILERON BOEING 727 727232 1384082 NM LT WING GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 526DA 21586 SPAR GOUGED AT I/B SIDE OF T/E WEDGE. SPLICED IN SPAR SECTION PER SRM 51-40-3. 2 L 7 3 4F A3WE 1996110100290 19961101 00290 NM 1996 11 1 DL72S962383 1 19961023 A 5320 FRAME BOEING 727 727232 1384082 NM R-2 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 420DA 21273 FOUND ON C2 LETTER CK, R2 DOOR HAS A .375 INCH CRACK AT THE UPPER HINGE CUT OUT LOWER AFT RADIUS ON FWD DOOR FRAME. REP AIRED PER SRM 52-40-2. 2 L 7 3 4F A3WE 1996110100291 19961101 00291 NM 1996 11 1 DL72S962384 1 19961023 A 5400 SKIN BOEING 727 727232 1384082 NM S-DUCT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 420DA 21273 FOUND ON C2 LETTER CK, 2.75 INCH CRACK IN THE OUTER SKIN OF THE NR 2 ENGINE INLET 3 O'CLOCK POSITION 16 INCHES AFT OF TH E INLET LIP. REPAIRED PER MM 54-30-0. 2 L 7 3 4F A3WE 1996110100292 19961101 00292 NM 1996 11 1 DL73E962387 1 19961012 A 5712 RIB BOEING 737 737247 138448D NM BS 851 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 376DL 23603 THE WING RIB UPPER CHORD AT RBL 70.5 AND BS 851 HAS TWO CRACKS IN THE VERTICAL FLANGE. ONE CRACK EXTENDS FROM THE AFT E ND OF THE PART IN THE BOTTOM FASTENER ROW. THE SECOND CRACK EXTENDS FROM THE MIDDLE OF THE AFT EDGE OF THE VERTICAL FLA NGE TO THE END FASTENER IN THE UPPER ROW. IN ADDITION, CORROSION WAS FOUND AT THE UPPER FLANGE OF THE RIB CHORD AT BS 8 46. THE CORROSION IS .050 DEEP AND IS APPROXIMATELY 1 INCH OUTBOARD OF THE VERTICAL FLANGE OF THE RIB CHORD. THE BLEND ED AREA MEASURES APPROX 3 FWD/AFT AND 1.5 INBD/OUTBD. REPAIRED PER DALA ER/A 304296-14, REV A. 2 L 7 2 4F A16WE 1996110100293 19961101 00293 NM 1996 11 1 DHL9672214C 1 19960920 A 5315 FLOOR BEAM BOEING 727 727228 NM BS 480 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, CORROSION ON CABIN FLOOR SUPPORT BEAM STA 480 RBL 0 TO RBL 16. CUT OUT DAMAGED AREA, INSTALLED FLOOR BEAM R EPAIR PER SRM 53-10-8, T-ANGLE 34 INCHES LONG. 2 L 7 3 4F A3WE 1996110100294 19961101 00294 NM 1996 11 1 DHL9672215C 1 19960914 A 5347 BAC1520792 SEAT TRACK BOEING 727 727228 NM BS 480 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, FOUND CORROSION ON CABIN SEAT TRACK FLANGE RBL 25 STA 480 TO 520. REMOVED AND REINSTALLED NEW SEAT TRACK PE R SRM 51-10-1 FROM STA 480 TO 520. 2 L 7 3 4F A3WE 1996110100295 19961101 00295 NM 1996 11 1 DHL9672216C 1 19960914 A 5320 440014 SUPPORT BOEING 727 727228 NM BS 400 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, FLOOR SUPPORT FLANGE AT LBL 20 IS CRACKED JUST FWD OF BS 400. INSTALLED NEW FLOOR SUPPORT PER SRM 51-10-1 2 0. 2 L 7 3 4F A3WE 1996110100296 19961101 00296 NM 1996 11 1 DHL9672217C 1 19960913 A 5320 WINDOW POST BOEING 727 727228 NM COCKPIT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, X-RAY INSPECTION REVEALED CRACK ON LT SIDE WINDOW POST F TO N. INSTALLED DOUBLER REPAIR PER S/B 53-0086 RE V 11. 2 L 7 3 4F A3WE 1996110100297 19961101 00297 NM 1996 11 1 DHL9672218C 1 19960925 A 5315 FLOOR BEAM BOEING 727 727228 NM BS 400 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, FOUND HEAVY CORROSION ON TOP FLOOR BEAM CHORD AT STA 400 RBL 4 AND LBL 4. INSTALLED FLOOR BEAM REPAIR AT UP PER CHORD, PER SRM 53-10-8 FROM RBL 4 TO LBL 4. 2 L 7 3 4F A3WE 1996110100298 19961101 00298 NM 1996 11 1 DHL9672219C 1 19960920 A 5315 FLOOR BEAM BOEING 727 727228 NM BS 1030 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, CABIN FLOOR BEAM HAS CORROSION AT BOTTOM OF UPPER FLANGE BS 1030 RBL 22. CUT OUT DAMAGED SECTION, INSTALLED FLOOR BEAM REPAIR FROM RBL 9 TO RBL 34 PER SRM 53-10-8. 2 L 7 3 4F A3WE 1996110100299 19961101 00299 NM 1996 11 1 DHL9672220C 1 19960917 A 5315 FLOOR BEAM BOEING 727 727228 NM BS 380 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, FOUND CABIN FLOOR BEAM CORRODED AT BS 380 RBL 23. CUT OUT DAMAGED AREA, APPROX 19, INSTALLED REPAIR 24 BY 2 .5 PER SRM 53-10-8. 2 L 7 3 4F A3WE 1996110100300 19961101 00300 NM 1996 11 1 DHL9672221C 1 19960907 A 5315 FLOOR BEAM BOEING 727 727228 NM BS 1070 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, CABIN FLOOR BEAM CORRODED AT BS 1070 RBL 55. REMOVED DAMAGED AREA, INSTALLED FLOOR BEAM REPAIR AT RBL 55, 3 4 LONG PER SRM 53-10-8. 2 L 7 3 4F A3WE 1996110100301 19961101 00301 NM 1996 11 1 DHL9672222C 1 19960913 A 5347 SEAT TRACK BOEING 727 727228 NM BS 995 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, SEAT TRACK FLANGE LBL 24 STA 995 HAS CORROSION. CUT OUT SEAT TRACK LBL 24 FROM BS 970 TO BS 1010. INSTALL ED SEAT TRACK PER SRM 53-10-1. 2 L 7 3 4F A3WE 1996110100302 19961101 00302 NM 1996 11 1 DHL9672223C 1 19960913 A 5321 FLOOR BOEING 727 727228 NM BS 1176 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, FOUND HEAVY CORROSION ON CABIN FLOOR AT BS 1176 LBL 66. REMOVED CORROSION, INSTALLED NEW CHORD ANGLE LBL 66 TO RBL 66, INSTALLED NEW CHORD ANGLE PER SRM 51-30-2. INSTALLED AFT DOOR THRESHOLD PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996110100303 19961101 00303 NM 1996 11 1 DHL9672224C 1 19960911 A 5320 INTERCOSTAL BOEING 727 727228 NM BS 1030 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, INTERCOSTAL CRACKED AT STA 1030 BELOW STR 10R. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-10-1, 10 BY 5. 2 L 7 3 4F A3WE 1996110100304 19961101 00304 NM 1996 11 1 DHL9672225C 1 19960908 A 5330 SKIN BOEING 727 727228 NM BS 1183 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, FOUND SKIN BULGING AT STA 1183 BETWEEN STR 19L AND 26L. CUT OUT SKIN BETWEEN STR 25 AND 26, NO EVIDENCE OF CORROSION AT OTHER AREAS. INSTALLED EXTERNAL DOUBLER PER SRM 51-10-2. 8.5 BY 12.5. 2 L 7 3 4F A3WE 1996110100305 19961101 00305 NM 1996 11 1 DHL9672226C 1 19960910 A 5320 69144723 TIE CASTING BOEING 727 727228 NM BS 950 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, STR 8 TIE CASTING THROUGH STA 950 FORGING HAS CRACK AT AFT LOWER CLIP TO SKIN. REMOVED AND INSTALLED NEW TI E CASTING AT STR 8 LT PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996110100306 19961101 00306 NM 1996 11 1 DHL9672227C 1 19960919 A 5712 RIB BOEING 727 727228 NM WS 686.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, RT WING RIB STA 686.5 HAS LOWER CHORD CRACKED AT STR 8. STOP DRILLED, HFEC AND INSTALLED REPAIR PER SRM 57- 10-5, 9 BY 4. 2 L 7 3 4F A3WE 1996110100307 19961101 00307 NM 1996 11 1 DHL9672228C 1 19960919 A 5712 RIB BOEING 727 727228 NM WS 656.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, RIGHT WING RIB HAS PREVIOUS REPAIR DOUBLER CRACKED AT LOWER CHORD STA 656.5 AT STR 6. REMOVED REPAIR, REAM ED STOP HOLE, CONDUCTED HFEC, INSTALLED REPAIR PER SRM 57-10-5. 2 L 7 3 4F A3WE 1996110100308 19961101 00308 NM 1996 11 1 DHL9672229C 1 19960918 A 5712 RIB BOEING 727 727228 NM WS 629 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, RIGHT WING RIB STA 629 CRACKED AT LOWER CHORD IN AREA OF STR 8 ATTACH BOLT. STOP DRILLED, HFEC AND INSTALLE D DOUBLER PER SRM 57-10-5, 10.5 BY 3.5. 2 L 7 3 4F A3WE 1996110100309 19961101 00309 NM 1996 11 1 DHL9672230C 1 19960917 A 5712 RIB BOEING 727 727228 NM WS 656.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, WING RIB STA 656.5 CRACKED AT PREVIOUS REPAIR DOUBLER AT STR 6 LOWER CHORD. REMOVED EXISTING REPAIR, INSTAL LED WING REPAIR PER SRM 57-10-5, 9 BY 2.25. 2 L 7 3 4F A3WE 1996110100310 19961101 00310 NM 1996 11 1 DHL9672231C 1 19960911 A 5730 SKIN BOEING 727 727228 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, RIGHT WING NR 13 SPOILER HINGE CUTOUT SKIN CRACKED AND SEPARATED. INSTALLED DOUBLER REPAIR PER SRM 57-30-04 , 5 BY 3. 2 L 7 3 4F A3WE 1996110100311 19961101 00311 NM 1996 11 1 DHL9672232C 1 19960911 A 5730 SKIN BOEING 727 727228 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, RIGHT WING NR 12 SPOILER, O/B HINGE CUTOUT SKIN CRACKED. INSTALLED DOUBLER PER SRM 57-30-04, 4 BY 6. 2 L 7 3 4F A3WE 1996110100312 19961101 00312 NM 1996 11 1 DHL9672233C 1 19960909 A 5754 SKIN BOEING 727 727228 NM NR 5 LE FLAP DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, SKIN CONTOUR IRREGULAR ON UPPER SURFACE OF NR 5 SLAT IN AREA OF I/B TRACK ATTACH POINT. CUT OUT DAMAGED POR TION OF SLAT, INSTALLED DOUBLER REPAIR PER SRM 57-50-3, 14 BY 6. 2 L 7 3 4F A3WE 1996110100313 19961101 00313 NM 1996 11 1 DHL9672234C 1 19960921 A 5712 RIB BOEING 727 727228 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, LEFT WING RIB AT STA 629.0 HAS A CRACK IN PREVIOUS REPAIR DOUBLER ON LOWER CHORD IN AREA OF STR 6. REMOVED CRACKED REPAIR AT LEFT WING, STOP DRILLED END OF CRACK, INSTALLED REPAIR AT WING RIB PER SRM 57-10-5, 9 BY 4. 2 L 7 3 4F A3WE 1996110100314 19961101 00314 NM 1996 11 1 DHL9672235C 1 19960919 A 5712 RIB BOEING 727 727228 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, LEFT WING RIB AT STA 656.5 CRACKED AT LOWER CHORD AT STR 8 ATTACH BOLT AREA. STOP DRILLED END OF CRACK, INS TALLED WING RIB REPAIR PER SRM 57-10-5, 9 BY 4. 2 L 7 3 4F A3WE 1996110100315 19961101 00315 NM 1996 11 1 DHL9672236C 1 19960917 A 5712 RIB BOEING 727 727228 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, WING RIB STA 686.5 HAS PREV REPAIR CRACKED AT LOWER CHORD STR 6. REMOVED PREVIOUS REPAIR, INSTALLED NEW REP AIR PER SRM 57-10-5, CHANNEL 8.5 BY 2.5. 2 L 7 3 4F A3WE 1996110100316 19961101 00316 NM 1996 11 1 DHL9672237C 1 19960909 A 5754 SLAT BOEING 727 727228 NM NR 4 LE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, NR 4 SLAT OUTBOARD CLOSURE RIB IS CRACKED. REMOVED AND REPLACED RIB PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996110100317 19961101 00317 NM 1996 11 1 DHL9672238C 1 19960919 A 5754 692848111 RIB BOEING 727 727228 NM NR 3 LE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, NR 3 SLAT INBOARD CLOSURE RIB IS CRACKED IN 2 PLACES. REPLACED RIB PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996110100318 19961101 00318 NM 1996 11 1 DHL9672239C 1 19960909 A 5754 SKIN BOEING 727 727228 NM NR 2 LE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, NR 2 SLAT INNER SKIN IS CRACKED ABOVE INBOARD TRACK. ROUTED OUT CRACK, INSTALLED DOUBLER REPAIR PER SRM 57- 50-3, 4 BY 5. 2 L 7 3 4F A3WE 1996110100319 19961101 00319 NM 1996 11 1 DHL9672240C 1 19960908 A 2761 STIFFENER BOEING 727 727228 NM NR 2 SPOILER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, NR 2 SPOILER ACTUATOR MOUNT, INBOARD VERTICAL STIFFENER IS CRACKED AT LOWER END. REMOVED AND REPLACED VERTI CAL STIFFENER PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996110100320 19961101 00320 NM 1996 11 1 DHL9672241C 1 19960914 A 5320 BAC1518359 FLOOR SUPPORT BOEING 727 727228 NM BS 344-380 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, FLOOR SUPPORT FLANGE AT LBL 20 HAS CORROSION FROM BS 344 TO BS 380. REMOVED AND REPLACED FLOOR SUPPORT FROM BS 344 TO BS 360 AND FROM BS 360 TO BS 380. 2 L 7 3 4F A3WE 1996110100321 19961101 00321 NM 1996 11 1 DHL9672242C 1 19960831 A 5712 RIB BOEING 727 727228 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, CRACKED RIB UPPER CHORD AT BL 70.5. STOP DRILLED CRACKS, HFEC AND INSTALLED REPAIR KIT PER S/B 57-0112. 2 L 7 3 4F A3WE 1996110100322 19961101 00322 NM 1996 11 1 DHL9672243C 1 19960913 A 5347 BAC1520792 SEAT TRACK BOEING 727 727228 NM BS 1130-1070 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, SEAT TRACK FLANGE RBL 53 STA 1130 TO 1070 HAS CORROSION. REPLACED SEAT TRACK PER SRM 51-10-1, 60 LONG. 2 L 7 3 4F A3WE 1996110100323 19961101 00323 NM 1996 11 1 DHL9672244C 1 19960913 A 5347 SEAT TRACK BOEING 727 727228 NM BS 1090-1070 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, SEAT TRACK FLANGE LB 45 STA 1090 TO 1070 CORRODED. REMOVED AND REPLACED SEAT TRACK FROM STA 1060 TO 1130 PE R SRM 53-10-5. 2 L 7 3 4F A3WE 1996110100324 19961101 00324 NM 1996 11 1 DHL9672245C 1 19960912 A 5313 STRINGER BOEING 727 727228 NM BS 294.5-303 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, FOUND CORROSION ON STR 21R BETWEEN BS 294.5 AND BS 303. CUT OUT DAMAGED AREA, INSTALLED STRINGER SPLICE PER SRM 53-10-3. 2 L 7 3 4F A3WE 1996110100325 19961101 00325 NM 1996 11 1 DHL9672246C 1 19960912 A 5313 STRINGER BOEING 727 727228 NM BS 1130 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, AFT CARGO BLOW OUT STRINGER CORRODED, STR 28L AT STA 1130. CUT OUT DAMAGED STRINGER AND UNDERLYING SKIN, I NSTALLED STRINGER REPAIR PER SRM 53-10-3, FILLER 10.5, INSTALLED SKIN REPAIR PER SRM 53-30-3, 34 BY 10. 2 L 7 3 4F A3WE 1996110100326 19961101 00326 NM 1996 11 1 DHL9672247C 1 19960911 A 5313 STRINGER BOEING 727 727228 NM BS 1125 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, STRINGER CORRODED AT STA 1125, STR 30. INSTALLED STRINGER REPAIR AT STA 1125 PER SRM 53-10-3, 14 LONG. 2 L 7 3 4F A3WE 1996110100327 19961101 00327 NM 1996 11 1 DHL9672248C 1 19960912 A 5744 65327343 SUPPORT FTG BOEING 727 727228 NM NR 1 TE FLAP CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, NR 1 FLAP TRACK FWD ATTACH FITTING ON WING HAS HEAVY CORROSION AT OUTBD LOWER SIDE. REMOVED AND REPLACED SU PPORT FITTING PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996110100328 19961101 00328 NM 1996 11 1 DHL9672249C 1 19960912 A 5744 653273333 FITTING BOEING 727 727228 NM NR 2 LE FLAP CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, NR 2 FLAP TRACK FWD SUPPORT FITTING INNER RADIUS CORRODED. REMOVED AND REPLACED SUPPORT FITTING PER SRM 51 -10-1. 2 L 7 3 4F A3WE 1996110100329 19961101 00329 NM 1996 11 1 DHL9672250C 1 19960912 A 5347 BAC1520792 SEAT TRACK BOEING 727 727228 NM BS 870-950 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, SEAT TRACK HAS CORROSION AT RBL 24 FROM BS 870 TO BS 950. REMOVED AND REPLACED SEAT TRACK PER SRM 53-10-3. 2 L 7 3 4F A3WE 1996110100330 19961101 00330 NM 1996 11 1 DHL9672251C 1 19960910 A 5330 SKIN BOEING 727 727228 NM NLG WW CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, FOUND AT FUSELAGE INTERIOR NOSE W/W BOX CORROSION AND BARE METAL AT TOP LEFT SIDE AT STA 329. REMOVED STIFF ENERS, CUT OUT TOP SKIN, INSTALLED NEW SKIN AND DOUBLER PER SRM 51-10-2 . INSTALLED STIFFENERS, SKIN 14 BY 25, DOUBLER 1 6 BY 25. 2 L 7 3 4F A3WE 1996110100331 19961101 00331 NM 1996 11 1 DHL9672252C 1 19960910 A 5330 SKIN BOEING 727 727228 NM BS 308. CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, FUSELAGE INTERIOR NOSE W/W BOX CORROSION AT STA 308. REMOVED STIFFENERS AND CUT OUT SKIN, INSTALLED NEW SKI N PER SRM 51-40-2, REINSTALLED STIFFENERS. 2 L 7 3 4F A3WE 1996110100332 19961101 00332 NM 1996 11 1 DHL9672253C 1 19960908 A 2782 MOUNT BOEING 727 727228 NM NR 7 LE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, NR 7 SLAT ACTUATOR O/B MOUNT REPAIR PLATE CRACKED. REMOVED AND REPLACED SUPPORT ANGLE PER S/B 57-130 AND RE PLACED ATTACH DOUBLER PER S/B 57-0130. 2 L 7 3 4F A3WE 1996110100333 19961101 00333 NM 1996 11 1 DHL9672254C 1 19960910 A 5753 651926919 SPACER BOEING 727 727228 NM NR 5 TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, NR 5 FLAP TRACK SPACER BLOCK CRACKED AT AFT END OF TRACK. REMOVED AND REPLACED SPACER BLOCK PER OHM 57-40-1 . 2 L 7 3 4F A3WE 1996110100334 19961101 00334 NM 1996 11 1 DHL9672255C 1 19961002 A 5754 SKIN BOEING 727 727228 NM NR 5 LE FLAP CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, NR 5 SLAT UPPER AND LOWER SKIN HAS CORROSION. CUT OUT DAMAGED AREA, INSTALLED EXTERNAL DOUBLER REPAIR PER 5 7-30-3. 2 L 7 3 4F A3WE 1996110100335 19961101 00335 NM 1996 11 1 DHL9672256C 1 19960930 A 5347 BAC1520792 SEAT TRACK BOEING 727 727228 NM BS 1032 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, SEAT TRACK FLANGE CORRODED AT STA 1032 AND RBL 1. REMOVED AND REPLACED SEAT TRACK FROM STA 1010 TO 1050 PER SRM 53-10-5. 2 L 7 3 4F A3WE 1996110100336 19961101 00336 NM 1996 11 1 DHL9672257C 1 19960909 A 5754 MOUNT BOEING 727 727228 NM NR 2 LE SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, NR 2 SLAT INBOARD MOUNT IS CRACKED AT TOP BOLT. REMOVED AND REPLACED DOUBLER PER S/B 57-130. 2 L 7 3 4F A3WE 1996110100337 19961101 00337 NM 1996 11 1 DHL9672258C 1 19960910 A 5753 ANGLE BOEING 727 727228 NM LT TE MID FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, INBOARD MID FLAP TRAILING EDGE ANGLE IS CRACKED AT CUT OUT FOR INBOARD ACTUATING ROD. REMOVED SKIN PANEL, S TOP DRILLED CRACK, INSTALLED ANGLE REPAIR PER SRM 51-40-4, 12 BY 2. 2 L 7 3 4F A3WE 1996110100338 19961101 00338 NM 1996 11 1 DHL9672259C 1 19960908 A 5330 SKIN BOEING 727 727228 NM BS 950 CORROSION A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, SKIN BULGING AND RIVETS POPPED AT STA 950E BETWEEN STR 26R AND 27R. REMOVED CORRODED SHIM AND L-FILLER AND CUT OUT OUTER SKIN. INSTALLED NEW FILLER, 20 BY 18, NEW SHIM 4.5 BY 6 PER SRM 51-10-1 AND 51-30-2. INSTALLED OUTER SKI N SPLICE AT SKIN CUTOUT AT FS 950E. DOUBLER INSTALLED PER AVITAS EO 96 PMSI 130D-1. 2 L 7 3 4F A3WE 1996110100339 19961101 00339 NM 1996 11 1 DHL9672260C 1 19960912 A 5320 651573252 FITTING BOEING 727 727228 NM BS 940 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, FOUND FRAME FITTING BS 940 RT SIDE CRACKED AT FLOOR LEVEL BEAM ATTACHMENT FLANGE AFT END I/B. ACCOMPLISHED EDDY CURRENT INSP, REPLACED RIGHT SIDE FITTING PER S/B 53-0118 AND DRAWING 65 15732 AND 65C13539. 2 L 7 3 4F A3WE 1996110100340 19961101 00340 NM 1996 11 1 DHL9672261C 1 19960912 A 5320 SUPPORT BOEING 727 727228 NM BS 1140 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, CABIN FLOOR SUPPORT CORRODED AT BS 1140 RBL 16 AND BELOW SHEAR WEB AT RBL 23. INSTALLED REPAIR PER SRM 51-4 0-3 AND PER SRM 51-30-2, 10 BY 25. 2 L 7 3 4F A3WE 1996110100341 19961101 00341 NM 1996 11 1 DHL9672262C 1 19960913 A 5347 BAC1520192 SEAT TRACK BOEING 727 727228 NM BS 1070-1030 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, SEAT TRACK FLANGE RBL 46 BETWEEN STA 1070 AND 1030 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK FROM STA 1010 TO 1130 PER SRM 53-10-5. 2 L 7 3 4F A3WE 1996110100342 19961101 00342 NM 1996 11 1 DHL9672263C 1 19960913 A 5347 BAC1520792 SEAT TRACK BOEING 727 727228 NM BS 950-1010 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, SEAT TRACK FLANGE RBL 24 BETWEEN STA 1010 TO 950B HAS CORROSION. REMOVED AND REPLACED SEAT TRACK FROM STA 9 55 TO 1020 PER SRM 51-10-1. SEAT TRACK WAS REPLACED BETWEEN STA 950 FRAME PLUS 5 TO STA 1020 AT RBL 24. 2 L 7 3 4F A3WE 1996110100343 19961101 00343 NM 1996 11 1 DHL9672264C 1 19960919 A 5320 FRAME BOEING 727 727228 NM NR 2 CARGO DOOR CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, FOUND CORROSION AFT CARGO NR 2 DOOR FWD CUTOUT FRAME AT BOTTOM ATTACH TO LOWER FRAME. CUT OUT CORRODED AREA OF FRAME FLANGE, INSTALLED REPAIR PER SRM 51-40-4, 22 BY 3. 2 L 7 3 4F A3WE 1996110100344 19961101 00344 NM 1996 11 1 DHL9672265C 1 19960923 A 5320 65224978 FITTING BOEING 727 727228 NM BS 930 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, WHILE REPLACING 940 FITTING, RT BS 930 FRAME WITH 2 CRACKS BELOW FLOOR LEVEL. REPLACED FRAME FITTING PER S/ B 53-130. 2 L 7 3 4F A3WE 1996110100345 19961101 00345 NM 1996 11 1 DHL9672266C 1 19960930 A 5313 STRINGER BOEING 727 727228 NM BS 970-990 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, AFT CARGO COMPT STR 28 LT CORRODED BETWEEN STA 970 AND 990. INSTALLED STRINGER REPAIR PER SRM 53-10-3, 20 L ONG. 2 L 7 3 4F A3WE 1996110100346 19961101 00346 NM 1996 11 1 DHL9672267C 1 19961001 A 5315 FLOOR BEAM BOEING 727 727228 NM BS 560 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, FWD CARGO COMPT, LOWER FLANGE OF FLOOR BEAM HAS EXFOLIATED CORROSION AT BS 560, RBL 54. INSTALLED REPAIR PE R SRM 53-10-8, 14 BY 2. 2 L 7 3 4F A3WE 1996110100347 19961101 00347 NM 1996 11 1 DHL9672268C 1 19960912 A 5542 SKIN BOEING 727 727228 NM RUDDER WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, LOWER RUDDER LT SIDE AT FWD SPAR, SKIN WORN THROUGH TO PHENOLOC SUB LAYER MOST OF LENGTH. ACCOMPLISHED RUDD ER REPAIR PER SRM 55-40-3. THREE DOUBLERS, 15.5 BY 12.75, 23.375 BY 12.312, 23.375 BY 13.25. 2 L 7 3 4F A3WE 1996110100348 19961101 00348 NM 1996 11 1 DHL9672269C 1 19960912 A 5542 SKIN BOEING 727 727228 NM RUDDER WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, LOWER RUDDER RT SIDE AT L/E FWD SPAR, SKIN WORN THROUGH TO PHENOLIC SUB LAYER JUST BELOW PANL 9507. INSTA LLED REPAIR PER SRM 55-40-3, 12 BY 9. 2 L 7 3 4F A3WE 1996110100349 19961101 00349 NM 1996 11 1 DHL9672270C 1 19960912 A 5542 SKIN BOEING 727 727228 NM RUDDER TORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, LOWER RUDDER RT SIDE AT L/E SKIN TORN OFF BELOW PANEL 9507. INSTALLED REPAIR PER SRM 55-40-3, 12 BY 23.25 . 2 L 7 3 4F A3WE 1996110100350 19961101 00350 NM 1996 11 1 DHL9672271C 1 19960919 A 5311 FRAME BOEING 727 727228 NM BS 950 CORROSION A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, AFT BAGGAGE COMPT HAS FRAME CORROSION AT STA 950E FLOOR LEVEL AND STR 26R. CUT OUT AREA AND INSTALLED REPAI R PER SRM 51-40-4, 22.5. 2 L 7 3 4F A3WE 1996110100351 19961101 00351 NM 1996 11 1 DHL9672272C 1 19960913 A 5315 FLOOR BEAM BOEING 727 727228 NM BS 1130 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, FLOOR BEAM TOP CHORD STA 1130 RBL 24 HAS CORROSION. CUT OUT FLOOR BEAM TOP CHORD, INSTALLED PER SRM 51-40-4 . REPAIR USED STRAP 12 BY 1, FILLER 1 BY 1.5 AND L-ANGLE 12 BY 2.5 BY 1 LONG. 2 L 7 3 4F A3WE 1996110100352 19961101 00352 NM 1996 11 1 P5CA9600834 1 19961024 A 5350 FAIRING BOEING 747 747122 1384872 NM RT FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 CRACK ABOVE THE ACCORDIAN SEAL STRIKE PLATE ON RIGHT FUSELAGE BODY FAIRING. REPAIRED PER BAC SRM 51-40-09. 2 L 7 4 4F A20WE 1996110100353 19961101 00353 NM 1996 11 1 P5CA9600835 1 19961024 A 5414 SKIN BOEING 747 747122 1384872 NM NR 2 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 CRACK APPROX .25 INCH GOING TO RIVET HOLE AT TOP AFT CORNER OF NR 2 PYLON CUTOUT FOR PANEL 463CL. DYE CHECK CONFIRMED C RACK, EDDY CURRENT CK PER BAC NDT MANUAL PART 6 AND INSTALLED DOUBLER PER BAC SRM 54-30-03. 2 L 7 4 4F A20WE 1996110100354 19961101 00354 NM 1996 11 1 P5CA9600836 1 19961020 A 5320 65B926407 TEE FITTING BOEING 747 747122 1384872 NM NR 4 FUEL TANK CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 DURING INSPECTION FOR CAUSE OF FUEL MIGRATION, FOUND CRACKED TEE FITTING IN NR 4 MAIN TANK. REMOVED WELDED PER COMPONEN T MAINTENANCE MANUAL 28-00-10 AND REINSTALLED TEE FITTING AND LEAK CHECKED OK. 2 L 7 4 4F A20WE 1996110100355 19961101 00355 NM 1996 11 1 P5CA9600837 1 19961024 A 5330 SKIN BOEING 747 747123 1384873 NM FUSELAGE DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 GROUND DAMAGE CAUSED BY TAIL POST JUST FORWARD OF TAIL JACK PAD. REPAIRED PER BOEING SRM 53-30-03 DETAIL 1. 2 L 7 4 4F A20WE 1996110100356 19961101 00356 NM 1996 11 1 P5CA9600838 1 19961025 A 3510 831SG25020R OXY TRANSDUCER BOEING 747 747123 1384873 NM COCKPIT FAILED A P5CA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 859FT 20326 GATE TURNBACK DUE TO CREW O2 PRESSURE READS 0. FOUND INOPERATIVE CREW O2 INDICATION. PLACARDED O2 INDICATION PER MEL 3 5-3. LATER TRANSDUCER REPLACED PER MAINTENANCE MANUAL 35-11-03. 2 L 7 4 4F A20WE 1996110100357 19961101 00357 NM 1996 11 1 P5CA9600839 1 19961025 A 2550 ROLLER TRAY BOEING 747 747123 1384873 NM AFT CARGO DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 ROLLER TRAY DAMAGED AFT CARGO COMPARTMENT. REPLACED DAMAGED SECTION PER BOEING SRM 51-10-01. 2 L 7 4 4F A20WE 1996110100358 19961101 00358 NM 1996 11 1 P5CA9600840 1 19961025 A 5414 SKIN BOEING 747 747123 1384873 NM NR 1 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 CRACK ON PLATE 453DR ON NR 1 PYLON. FABRICATED AND INSTALLED DOUBLER PER BAC SRM 51-30-02 AND 51-40-02. 2 L 7 4 4F A20WE 1996110100359 19961101 00359 NM 1996 11 1 P5CA9600841 1 19961025 A 5280 DOOR BOEING 747 747123 1384873 NM RT MLG DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 DELAMINATION ON RIGHT WING LANDING GEAR LOWER STRUT DOOR AFT BOTTOM EDGE. REPAIRED PER BOEING SRM 51-040-09. 2 L 7 4 4F A20WE 1996110100360 19961101 00360 NM 1996 11 1 P5CA9600842 1 19961025 A 2550 65B6003616 SILL LOCK BOEING 747 747123 1384873 NM CARGO COMPT BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 BROKEN SILL LOCK AFT CARGO DOOR MOST FORWARD. REPLACED PER BOEING MAINTENANCE MANUAL 25-54-00. 2 L 7 4 4F A20WE 1996110100361 19961101 00361 NM 1996 11 1 P5CA9600843 1 19961025 A 3610 PRECOOLER BOEING 747 747123 1384873 NM NR 1 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 CRACK ON NR 1 ENGINE PRECOOLER. WELDED CRACK PER BAC PROCESS 5975. 2 L 7 4 4F A20WE 1996110100362 19961101 00362 NM 1996 11 1 P5CA9600844 1 19961025 A 2150 65B409321 DUCT BOEING 747 747123 1384873 NM NR 3 PACK CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 CRACKED DUCT AT NR 3 PACK SECONDARY HEAT EXCHANGER AT SEAL RETAINER. REPLACED DUCT PER BOEING MAINTENANCE MANUAL 21-51- 06. 2 L 7 4 4F A20WE 1996110100363 19961101 00363 NM 1996 11 1 P5CA9600845 1 19961025 A 3213 STRUT BOEING 747 747123 1384873 NM RT MLG CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LEVEL 1 CORROSION ON FORWARD BASE PORTION OF RIGHT WING GEAR STRUT. REMOVED CORROSION AND REPAINTED PER BAC SRM 51-10-0 1. 2 L 7 4 4F A20WE 1996110100364 19961101 00364 NM 1996 11 1 P5CA9600846 1 19961025 A 2750 65B819922 RETAINER BOEING 747 747123 1384873 NM RT TE FLAP BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 BROKEN WOBBLE RETAINER FOR OUTBOARD FLAP TORQUE TUBE IN RIGHT BODY GEAR WHEEL WELL. REPLACED PER BOEING MAINTENANCE MAN UAL 27-51-20. 2 L 7 4 4F A20WE 1996110100365 19961101 00365 WP 1996 11 1 ARWA9610001 1 19961024 A 2120 C310N620485S2 CLAMP NASI CW0871 DOUG DC8 DC863F 302198F WP AC COMPT LOOSE A ARWA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 661AV 45969 WHILE CLIMBING THROUGH FL 28.0, PNEUMATIC DUCT RUPTURED IN FLIGHT. CABIN PRESSURIZATION CLIMBED TO 10,000 FT. AIRCRAFT RETURNED TO LIMA WITHOUT INCIDENT. DURING TROUBLESHOOTING, FOUND RT SIDE COLD AIR DUCT CLAMP DISCONNECTED AT BULKHEAD. RECONNECTED CLAMP, OPS CHECK OK IAW NASI M/M 21-0-0. IMPROPER INSTALLATION. 2 L 7 4 4F 4A25 1996110100366 19961101 00366 1996 11 1 SRAA961013 3 19961022 A 6110 PROPELLER LKHEED 382 382G 526414U SO NR 4 ENGINE OIL LEAK A A SRAA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 23 905SJ 4472 NR 4 PROP LOW OIL LIGHT CAME ON WITH RPM OUT OF LIMITS, SHUT DOWN ENGINE IN FLIGHT AND AT THE SAME TIME NR 3 ENGINE PROP LOW OIL LIGHT CAME ON. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. FOUND NR 4 PROP LEAKING EXCESSIVELY AT NR 1 AN D NR 2 BLADES, SERVICED ALL FOUR PROPS AND PERFORMED ENGINE RUN, NR 4 PROP HAS SLOW LEAK. PREPARED AIRCRAFT FOR MAINTEN ANCE FERRY TO ANC, AFTER 1.3 HR INTO FLIGHT, NR 4 PROP LOW OIL LIGHT CAME ON AND NR 3 PROP LOW OIL LIGHT CAME ON AFTER 3 .3 HR INTO FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 4 PROP ASSEMBLY, NR 3 PROPELLER AND PUMP HOUSING, ALL WORK DONE IAW SAT J/C 6101, 6101-1 AND OPS CHECKED PER J/C 7101 AND 7101-2. 2 H 7 4 4T A1SO 1996110100378 19961101 00378 CE 1996 11 1 96ZZZX5411 1 19961001 A 3213 PISTON CESSNA 425 425 2076018 CE MLG WORN A DLLA K NONE O OTHER IN INSP/MAINT 1 CE 09 89GC 6203 4250092 THE PISTON, REF NR 20, IS WORN WHERE THE SEAL OR BEARING RIDES WHEN THE AIRCRAFT IS ON THE GROUND, ABOUT 6 INCHES UP FRO M THE BOTTOM. THE WEAR AREA IS ABOUT 2.5 INCHES LONG AND ABOUT ONE-THIRD WAY AROUND THE PISTON ON THE FRONT OUTBOARD SI DE. TOTAL TIME ON AIRCRAFT IS 6,203 HRS. 1 L 7 2 3T RT A7CE 1996110100383 19961101 00383 SW 1996 11 1 96ZZZX5416 1 19960511 A 3260 MCD271111 UPLOCK SW ACT SWRNGN SA226 SA226TC 8780404 SW LT MLG LACK OF LUBE A RAIA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 CE 03 104GS 13494 TC222EE LEFT MAIN GEAR DOWN AND LOCKED INDICATION INTERMITTENT. FOUND LEFT GEAR UP POSITION SWITCH ACTUATOR STICKING. CLEANED AND LUBRICATED SWITCH ACTUATOR. AIRCRAFT TT: 13,494 HRS. 2 L 7 2 4T RT A8SW 1996110100385 19961101 00385 NM 1996 11 1 CA960313010 1 19960228 A 5311 85310025105 FRAME DHAV DHAV DHC8 DHC8102 2809003 NM STA 167 CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 18368 (CAN)DURING FUSELAGE INSPECTION, FRAME FOUND CORRODED. FRAME LOCATED AT STA.X 167 BETWEEN STRINGERS 28S AND 28P. AREA AP PROXIMATELY 2" X 1" COMPLETELY CORRODED AWAY. GENERIC SRM RD8-53-948 MAY APPLY. 2 H 7 2 4T RT A13NM 1996110100387 19961101 00387 CE 1996 11 1 CA960314001 1 19960307 A 3260 MS244201 SWITCH BEECH 115810000652 BEECH 99 99 1154002 CE PWA MLG SQUAT OUT OF ADJ W A UNSCHED LANDING O OTHER CL CLIMB 1 CA ALS3334 (CAN)LANDING GEAR WOULD NOT RETRACT. AIRCRAFT LANDED WITHOUT INCIDENT AND MAINTENANCE FOUND THE SQUAT SWITCH OUT OF ADJU STMENT. SWITCH SERVICED AND AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 3T A14CE 1996110100388 19961101 00388 SW 1996 11 1 CA960315001 1 19960228 A 5320 20603220038 STRAP BELL 206 206B 1181511 SW ALLSN R/H OUTER RADIUS CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN)ON ANNUAL INSPECTION FOUND R/H STRAP CRACKED AS WELL AS SOME DEBONDING OF THE UPPER DECK IN AND AROUND THE R/H BOX BEAM EXTRUSION. POSSIBLY DAMAGE FROM INCIDENT 1000 HOURS EARLIER OF MAST BUMPING. 1 G 7 1 3U H2SW 1996110100389 19961101 00389 NM 1996 11 1 CA960315002 1 19960306 A 2140 322861001 FLANGE BOEING 727 72722 1384002 NM PWA PURGE VALVE CRACKED W A J UNSCHED LANDING DUMP FUEL J M WARNING INDICATION OVER TEMP CL CLIMB 1 CA (CAN)AFTER TAKEOFF THE AFT BODY OVERHEAT LIGHT CAME ON. FUEL DUMPED AND RETURNED TO BLOCKS. CRACK IN FLANGE OF PURGE VAL VE. REPLACED. 2 L 7 3 4F A3WE 1996110100390 19961101 00390 NE 1996 11 1 CA960315003 2 19960307 A 7200 ENGINE BOEING 727 72725 1384006 NM PWA JT8 JT8D7B 52053 NE IGNITER FLANGE DUCT TORN W A K NONE O OTHER IN INSP/MAINT 1 CA 657105 (CAN) DURING A ROUTINE INSPECTION, BROKEN METAL WAS FOUND IN THE COWL OF #3 ENGINE. FURTHER INSPECTION REVEALED AN APPRO XIMATELY 3 SQ.IN. HOLE AND A 8"X4" TEAR AT THE APPROXIMATELY 3 O'CLOCK POSITION OF THE BYPASS DUCT WHERE THE IGNITOR FLA NGE IS MOUNTED. LOOKING FORWARD THROUGH THE HOLE, IT COULD BE SEEN THAT THE DIFFUSER CASE WAS RUPTURED AND THE HEAT SHIE LD BURNT AWAY. THERE WERE NO PILOT REPORTS OF ANY PROBLEMS WITH THE ENGINE EXCEPT A 50 DEGREES HIGHER EGT TEMPERATURE. T HE LAST VISUAL INSPECTION OF THE ENGINE WAS CARRIED OUT 21 HOURS PRIOR. TOTAL TIME SINCE LAST SHOP VISIT WAS 5900 HOURS. 2 L 7 3 4F 4 F A3WE E2EA 1996110100391 19961101 00391 EU 1996 11 1 CA960315004 1 19960222 A 2435 N131858 BRUSHES BRAERO 748 HS7482A 4231001 EU LT ENG STARTER WORN W O OTHER O OTHER TX TAXI/GRND HDL 1 CA 1608 (CAN)PILOT REPORT LH ENGINE WILL NOT TURN OVER AND START BUTTON WILL NOT STAY IN. STARTER REPLACED. BRUSH AND CONNECTOR ASSEMBLY WORN BEYOND LIMITS. 2 L 7 2 3T A24EU 1996110100393 19961101 00393 NM 1996 11 1 CA960315006 1 19960308 A 2510 C036004207505 SPRING AVITECH 39400107 DHAV DHC8 DHC8301 NM PWA CAPTS SEAT BROKEN W K NONE O OTHER TX TAXI/GRND HDL 1 CA 14360 1695 (CAN)CAPTAIN'S SEAT ASSEMBLY NOT POSITIVELY LOCKING IN FORE/AFT POSITION. SEAT UNLOCKED A COUPLE OF TIMES AND HAD TO BE SHAKEN BACK INTO POSITION IN TRACK. COMBINATION OF BOTH SEAT TRACK LOCKING PIN SPRING S BROKEN AND SEAT TRACK LOCKING HO LES FILLED WITH DUST AND DIRT CAUSED SEAT NOT TO POSITIVELY LOCK. BOTH LOCKING PIN SPRINGS REPLACED AND SEAT TRACK CLEAN ED. 2 H 7 2 4T RT A13NM 1996110100394 19961101 00394 WP 1996 11 1 CA960315007 1 19960209 A 7603 90262219 POWER LEVER CVAC 340 340CVAC 242270A WP ALLSN LH WORN W K NONE O OTHER CR CRUISE 1 CA (CAN)LH POWER LEVER REQUIRED TO BE MOVED APPROXIMATELY 4 INCHES BEFORE ENGINE RESPONDED. MAINTENANCE INVESTIGATION REVEA LED THE ARM OF THE BELLCRANK ON CO-ORDINATOR WAS SEVERELY WORN INCLUDING GEAR TEETH ON THE SHAFT. THE LOCK BOLT WAS IN PLACE AND LOCKED WIRED. SUSPECT A LARGE FORCE WAS APPLIED TO THE CONDITION LEVER. CO-ORDINATOR AND LEVER REPLACED. 2 L 7 2 4R 6A6 1996110100395 19961101 00395 SW 1996 11 1 CA960315008 1 19960208 A 3230 2751000175 DOWNLOCK CABLE SWRNGN SWRNGN SA226 SA226AT 8780405 SW LT INB DOWNLOCK BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN)LEFT HAND INBOARD DOWNLOCK ASSIST SPRING CABLE FOUND WITH NUMEROUS BROKEN STRANDS. 2 L 7 2 4T RT A5SW 1996110100396 19961101 00396 SW 1996 11 1 CA960315009 1 19960207 A 3230 2754000123 UPLOCK CABLE SWRNGN SA226 SA226AT 8780405 SW LT EMERG UP LOCK BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN)LEFT EMERGENCY UPLOCK RELEASE CABLE IN AREA OF BATTERY, FOUND DAMAGED WITH MANY STRANDS BROKEN. 2 L 7 2 4T RT A5SW 1996110100397 19961101 00397 SW 1996 11 1 CA960315010 1 19960220 A 7603 C817225 CABLE SWRNGN SA227 SA227AC 8780603 SW RT ENG POWER SEPARATED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN)RIGHT HAND PROP NOT COMING OFF THE LOCKS. INSPECTION FOUND RH ENGINE POWER CABLE END SEPARATED AT OUTER SHEATH SWAG E. CABLE REPLACED. 2 L 7 2 4T RT A8SW 1996110100398 19961101 00398 CE 1996 11 1 CA960315012 1 19960306 A 3233 PUMP MOTOR BEECH 100 A100 1152915 CE LT GEAR FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) ON TAKEOFF THE GEAR FAILED TO RETRACT TO THE LOCKED POSITION. THE CREW SELECTED THE GEAR DOWN AND ONLY THE MAIN GE AR EXTENDED. THE CREW USED THE EMERGENCY PROCEDURES AND EXTENDED THE GEAR. INVESTIGATION FOUND THAT EITHER THE PUMP OR T HE MOTOR APPEARS TO HAVE CAUSED THE FAULT. 1 L 7 2 3T A14CE 1996110100399 19961101 00399 SW 1996 11 1 CA960315013 1 19960312 A 6322 206040301023 BEARING BELL 206 206B 1181511 SW ALLSN AFT OIL COOL FAN ROUGH W K NONE O OTHER IN INSP/MAINT 1 CA (CAN)FOUND AFT OIL COOLER BEARING P/N 206-040-339-009 ROUGH. DISASSEMBLED COOLING FAN ASSEMBLY AND FOUND SPACER P/N 206- 040-351-001 INCORRECTLY INSTALLED IN HANGER ASSEMBLY P/N 206-040-355-001 (NOT THE COR RECT PART). REMOVED SPACER AND INS TALLED SPACER P/N 206-040-351-003 AND NEW BEARING P/N 206-040-339-009. THE CORRECT SPACER PUT TOO MUCH LOAD ON BEARING. 1 G 7 1 3U H2SW 1996110100400 19961101 00400 CE 1996 11 1 CA960315014 1 19960310 A 2750 FLAP MOTOR BEECH BEECH 200 200BEECH 1152920 CE PWA DRIVE SHAFT RIGGING PROBLEM W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA (CAN)PILOT REPORTED A CIRCUIT BREAKER POPPING WHEN THE FLAPS WERE SELECTED. INVESTIGATION FOUND THAT THE FLAP MOTOR INST ALLATION WAS AT FAULT AND TRACED TO AN APPARENT MAINTENANCE MANUAL PRINTING MIXUP. CH APTER 27-50-00, PAGE 205 ISSUED JU NE 24, 1994. THE INBOARD AND OUTBOARD DRIVESHAFTS WERE REVERSED ALLOWING THE FLAP SELECTION TO REVERSE AND CAUSE DAMAGE TO THE ACTUATOR FLEX SHAFT. 1 L 7 2 4T A24CE 1996110100401 19961101 00401 CE 1996 11 1 CA960315016 1 19960307 A 8011 641500R CLUTCH CESSNA 150 150L 2071826 CE CONT STARTER SEIZED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN)DURING TOWING IT WAS NOTICED THAT THE PROP WOULD TURN IN ONE DIRECTION BUT NOT THE OTHER. MAINTENANCE REMOVED THE S TARTER AND FOUND THE CLUTCH SEIZED. 1 H 7 1 3O 3A19 1996110100402 19961101 00402 NM 1996 11 1 CA960315018 1 19960305 A 3244 AHA1648 TIRE BOEING 757 75723A 1384967 NM RROYCE NR 4 AFT MAIN BURST W K NONE O OTHER LD LANDING 1 CA (CAN)#4 AFT MAIN TIRE FOUND BLOWN AFTER LANDING. NOTHING WAS FELT FROM THE COCKPIT BY CREW. PRESUME BRAKE SEIZED FOR AN UNKNOWN REASON. SYSTEMS CHECK SERVICEABLE. WHEELS AND BRAKE REPLACED. 2 L 7 2 4F RT A2NM 1996110100403 19961101 00403 NM 1996 11 1 CA960315019 1 19960306 A 4940 W1002001410 GROUND LEAD BOEING 757 75728A 1384976 NM RROYCE APU START BURNT W K NONE O OTHER IN INSP/MAINT 1 CA 20086 (CAN)APU START GROUNDING LEAD LOOSE AT TERMINAL POST OF GROUNDING BRACKET CAUSING ARCING ELONGATION OF HOLE ON BRACKET. ONE TERMINAL LEAD BURNED. CORROSION AROUND HOLE MAY HAVE CAUSED BAD CONTACT. 2 L 7 2 4F RT A2NM 1996110100404 19961101 00404 EU 1996 11 1 CA960315020 1 19960308 A 5280 14152030401 RIVETS BRAERO BAG JETSTM JETSTM4112 EU AFT DOOR HINGE SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA 2460 (CAN)THREE RIVETS FOUND SHEARED ON THE PANEL CONNECTING THE TWO MAIN LANDING GEAR DOOR HINGES AT AFT MLG DOOR. RIVETS RE PLACED. ONE OTHER AIRCRAFT FOUND WITH SAME PROBLEM. 1 L 7 2 4T RT A196 1996110100406 19961101 00406 NM 1996 11 1 CA960318001 1 19960315 A 3246 1014171 WHEEL BFGOODRICH DHAV DHC8 DHC8102 2809003 NM PWA OUTB HALF CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1121 (CAN)CRACKS FOUND IN OUTBOARD WHEEL HALF USING EDDY CURRENT INSPECITON. 2 H 7 2 4T RT A13NM 1996110100407 19961101 00407 NM 1996 11 1 CA960318002 1 19960315 A 3246 0818 DRIVE LUGS BFGOODRICH 1014182 DHAV DHC8 DHC8102 2809003 NM PWA WHEEL WORN W K NONE O OTHER IN INSP/MAINT 1 CA 0818 (CAN)SEVERAL DRIVE INSERTS FOUND LOOSE AND DRIVE LUGS WORN BEYOND LIMITS 2 H 7 2 4T RT A13NM 1996110100408 19961101 00408 NM 1996 11 1 CA960318003 1 19960315 A 7920 DSC2842 OIL LINE DHAV DHC8 DHC8101 2809002 NM PWA SCAVENGE PUMP CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN)OIL LEAK FROM RIGHT SIDE OF ENGINE NOTED. FOUND OIL LINE FROM SCAVENGE PUMP TO COOLER SPLIT. 2 H 7 2 4T RT A13NM 1996110100410 19961101 00410 EU 1996 11 1 CA960318006 1 19960229 A 2910 AGS9840 PLUG BRAERO 748 HS7482A 4231001 EU RT ENG HYD CRACKED W O OTHER J K WARNING INDICATION FLUID LOSS CL CLIMB 1 CA (CAN)AFTER TAKEOFF PILOT NOTICED LOSS OF HYDRAULIC PRESSURE AND HYDRAULIC FLUID COMING FROM HYDRAULIC BAY IN STARBOARD N ACELLE. ALL PERTINANT EMERGENCY PROCEDURES WERE FOLLOWED BY CREW. MAINTENANCE DISCOVE RED A BLANKING PLUG IN THE END OF THE HYDRAULIC MANIFOLD HAD A HAIR LINE CRACK THAT CAUSED THE LOSS OF HYDRAULIC PRESSURE. PLUG AND ONE HYDRAULIC PUMP REP LACED. 2 L 7 2 3T A24EU 1996110100412 19961101 00412 SW 1996 11 1 CA960320002 1 19960229 A 6320 206040561103 SUNGEAR 206040004107 BELL 206 206L3 1182108 SW M/R GR BOX SPALLED W K NONE O OTHER IN INSP/MAINT 1 CA 2878 (CAN) SCHEDULED 1500 HOUR SPECIAL INSPECTION ON SUNGEAR REVEALED SPALLING OF SPLINES. FURTHER INVESTIGATION REVEALED DA MAGE TO CORRESPONDING INPUT SPIRAL BEVEL GEARSHAFT SPLINES. 1 G 7 1 3U H2SW 1996110100415 19961101 00415 SO 1996 11 1 CA960320010 1 19960313 A 2710 4033901 BELLCRANK ASSY PIPER PIPER PA31 PA31350 7103110 SO RT AILERON CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 10165 (CAN)DURING A SCHEDULED 100 HOUR INSPECTION, MAINTENANCE PERSONNEL DISCOVERED A CRACK IN THE RIGHT AILERON BELLCRANK ASS EMBLY. PART NUMBER 40339-01, REFERENCE FIG. 96, ITEM #4 OF THE PIPER PA31-350 PARTS C ATALOGUE. P/N 761-487 REVISED MARC H 10, 1994. THE CRACK OCCURRED AT THE INTERSECTION OF THE BALANCE CABLE ARM AND THE AILERON ACTUATING PUSH ROD ARM. MAIN TENANCE COULD FIND NO APPARENT CAUSE FOR THIS CRACK AS THE SYSTEM WAS RIGGED PROPERLY, WITH CABLE TENSIONS WITHIN LIMITS . SUBMITTER SPECULATES THAT A SHARP INTERSECTION OF THE TWO ARMS MAY BE A STRESS RISER. 1 L 7 2 3O A20SO 1996110100416 19961101 00416 CE 1996 11 1 CA960320011 1 19960314 A 3233 1153800025 ACTUATOR MOTOR BEECH 1153800025 BEECH 100 A100 1152915 CE PWA GEAR OVERHEATING W K NONE O OTHER IN INSP/MAINT 1 CA 2466 (CAN)TESTING REVEALED THE MOTOR COMMUTATOR HAD A DEAD SPOT AND THERE WAS INDICATION THE UNIT HAD EXPERIENCED OVERHEATING . 1 L 7 2 3T A14CE 1996110100417 19961101 00417 NM 1996 11 1 CA960320012 1 19960307 A 5210 852100099011 UPPER PANEL DHAV 85210003001 DHAV DHC8 DHC8102 2809003 NM PWA AIRSTAIR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 20527 0010061 (CAN)CRACK FOUND ON UPPER PANEL OF AIRSTAIR DOOR ASSEMBLY AND ON EDGE MEMBER. EDGE MEMBER P/N 852210067-107. AIRCRAFT PR E MOD 810689. 2 H 7 2 4T RT A13NM 1996110100419 19961101 00419 GL 1996 11 1 CA960320016 3 19960214 A 6111 T1028NB BLADE HARTZL HCB3TN5G SWRNGN SA226 SA226AT 8780405 SW GARRTT HARTZL HCB3T HCB3TN5 GL RT PROP TIP CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA BV1857 BV3013 (CAN)ONE BLADE TIP ON RH PROP FOUND WITH A ONE-HALF INCH CRACK. PROP REPLACED. 2 L 7 2 4T RT A5SW 6 C P15EA 1996110100420 19961101 00420 NM 1996 11 1 CA960320017 1 19960310 A 3246 L812148 BEARING BFGOODRICH 314353 DHAV DHC8 DHC8102 2809003 NM PWA LH OUTB MLG BROKEN W D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CA 10993 3903 1419 (CAN)DURING TAXI A SLIGHT DRAG NOTED BY PILOT. #1 LEFT HAND OUTBOARD MAINWHEEL BEARING FAILED. IT APPEARED THAT INBOARD BEARING HAD SEIZED AND SPUN ON AXLE CAUSING HEAVY SCORING ON AXLE INBOARD JOURNAL. ASA RESULT INBOARD MAINWHEEL RACE SPU N CAUSING HEAVY DAMAGE TO INNER WHEEL HALF, OUTBOARD BEARING FAILED AND MAINWHEEL TILTED CAUSING BRAKE ASSEMBLY TO CONTA CT AND SCORE MAINWHEEL INNER HALF. LEFT HAND MLG SHOCK STRUT ASSEMBLY, #1 BRAKE ASSEMBLY AND #1 MAINWHEEL ASSEMBLY REPLA CED. 2 H 7 2 4T RT A13NM 1996110100421 19961101 00421 CE 1996 11 1 CA960320018 1 19960312 A 3230 1240016CRO140 HYD FLEX HOSE BEECH 115810000652 BEECH 99 B99 1154004 CE PWA MLG RETRACT RUPTURED W O OTHER J K O WARNING INDICATION FLUID LOSS OTHER CL CLIMB 1 CA ALS3934 (CAN)AFTER TAKEOFF THE GEAR WAS SELECTED UP BUT DID NOT LOCK. AIRCRAFT CONTINUED TO DESTINATION AND GEAR SELECTED DOWN A ND LOCKED WITHOUT INCIDENT. HYDRAULIC GEAR LINE FOUND RUPTURED. RUPTURED LINE REPLACED AND SYSTEM CHECKED OUT SERVICEABL E. 1 L 7 2 3T A14CE 1996110100423 19961101 00423 WP 1996 11 1 CA960320020 2 19960208 A 7321 8950935 DIAPHRAGM WOODWARD 89737515 SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP LEFT HAND FCU BROKEN W K NONE O OTHER AP APPROACH 1 CA 3475 2007609 (CAN)ON APPROACH WITH #1 POWER LEVER RETARDED TO FLIGHT IDLE, #1 ENGINE INDICATED 40 PERCENT TORQUE. IT TOOK ABOUT ONE M INUTE TO SLOWLY REDUCE TO ABOUT 20 PERCENT TORQUE. LEFT HAND FCU P3 DIAPHRAGM REPLACE D. 2 L 7 2 4T 4 T RT A8SW E4WE 1996110100424 19961101 00424 EA 1996 11 1 CA960320021 2 19960312 A 7314 02532310103 FUEL PUMP BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA ENGINE FAULTY W E ENGINE SHUTDOWN X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 CA PCE41919 (CAN)ENGINE STARTED AND FLAMED OUT DURING TAXI. MAINTENANCE REPLACED THE FUEL CONTROL UNIT AND THE FUEL PUMP. ENGINE STA RTED AND FOUND TO BE SERVICEABLE. 1 L 7 2 3T 4 T A14CE E4EA 1996110100425 19961101 00425 NM 1996 11 1 CA960320023 1 19960313 A 3242 170240 INSERTS BFGOODRICH 1014182 DHAV DHC8 DHC8102 2809003 NM PWA #2 BRAKE WORN W K NONE O OTHER IN INSP/MAINT 1 CA 9301 2734 AO80M (CAN)DURING #2 WHEEL REMOVAL ALL 7 BRAKE INSERTS FOUND WORN THROUGH. #2 BRAKE UNIT AND MAIN WHEEL ASSEMBLY REPLACED. 2 H 7 2 4T RT A13NM 1996110100426 19961101 00426 NM 1996 11 1 CA960320024 1 19960313 A 3242 170240 INSERTS BFGOODRICH 1014182 DHAV DHC8 DHC8102 2809003 NM PWA #1 BRAKE WORN W K NONE O OTHER IN INSP/MAINT 1 CA 7005 613 A094M (CAN)ON WHEEL REMOVAL FOUND ALL 7 BRAKE INSERTS WORN THROUGH. #1 BRAKE UNIT AND MAIN WHEEL ASSEMBLY REPLACED. 2 H 7 2 4T RT A13NM 1996110100427 19961101 00427 SO 1996 11 1 CA960320025 1 19960315 A 2140 20D35 EXHAUST JANITROL 20D35 PIPER PA30 PA30 7103002 SO LYC HEATER CRACKED W K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION IN INSP/MAINT 1 CA 437 3691386 (CAN) THE SMELL OF EXHAUST FUMES IN THE CABIN WAS REPORTED DURING HEATER OPERATION. THE CARBON MONOXIDE DETECTOR WAS FOU ND TO HAVE A POSITIVE INDICATION AFTER ABOUT THREE WEEKS. MAINTENANCE WAS CONTINUALLY PERFORMING PRESSURE DECAY TESTS ON THE JANITROL HEATER. THE DECAY TESTS PASSED EVERY TIME AND THE SOURCE OF THE FUMES REMAINED A MYSTERY UNTIL THE HEATER WAS REMOVED FOR REPLACEMENT. A CRACK WAS DISCOVERED ABOUT HALF THE CIRCUMFERENCE OF THE EXHAUST PIPE AND TWO (2) INCHES FROM THE OUTPUT. THIS CRACK WAS HIDDEN WELL INSIDE THE EXHAUST SHROUD AND ALLOWED FUMES TO SEEP INTO THE NOSE COWL. THE SUBMITTER RECOMMENDS THE REMOVAL OF THE HEATER FOR ALL PRESSURE DECAY TESTS AND THE CONTINUED USE OF CO DETECTORS. 1 L 7 2 3O A1EA 1996110100429 19961101 00429 CE 1996 11 1 CA960320027 1 19960311 A 3230 ADIISV1 BLEED VALVE M8101 BEECH 90 C90 1152913 CE PWA EMERG EXT SYS CONTAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA 319 (CAN)WHILE COMPLETING EMERGENCY GEAR SWINGS DURING MAINTENANCE, GEAR DOWN SYSTEM PRESSURIZED, OPENING THE MANUAL NITROGE N VALVE IN COCKPIT, PRESSURE DID NOT HOLD. THE BLEED VALVE WAS REMOVED AND FOUND TO BE CONTAMINATED WITH WATER AND FOREI GN MATERIAL. THE BLEED VALVE WAS CLEANED AND INSTALLED AND THE SYSTEM CHECKET OUT FINE. 1 L 7 2 3T 3A20 1996110100430 19961101 00430 WP 1996 11 1 CA960320501 1 19960102 A 2400 ELECTRICAL SYS DOUG DC9 DC932 3022066 WP PWA COCKPIT BURNIGN SMELL W O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA (CAN)ON ARRIVAL WHILE TAXIING A BURNING SMELL IN THE COCKPIT AREA WAS NOTICED. MAINTENANCE INVESTIGATION COULD NOT FIND SOURCE OF THE PROBLEM AFTER PANELS OPENED AND AIRCRAFT POWERED. 2 L 7 2 4F A6WE 1996110100431 19961101 00431 WP 1996 11 1 CA960320502 1 19960104 A 5610 5887275505 WINDSHIELD DOUG DC9 DC932 3022066 WP PWA CENTRE COCKPIT SHATTERED W O OTHER G MULTIPLE FAILURE CL CLIMB 1 CA (CAN)AFTER TAKEOFF AN EIGHT INCH CRACK APPEARED ON OUTER PANEL OF CENTRE WINDSHIELD. SHORTLY AFTER A LOUD BANG OCCURRED AND OUTER PANEL SHATTERED. CENTRE WINDSHIELD AND HEAT CONTROLLER P/N 3161-1 REPLACED. 2 L 7 2 4F A6WE 1996110100479 19961101 00479 NM 1996 11 1 CALA9601513 1 19961026 A 7931 1163P181 OIL PRESS SW BOEING 737 737222 1384473 NM PWA JT8 JT8D9 52048 NE NR 2 ENGINE CRACKED A CALA E ENGINE SHUTDOWN J K WARNING INDICATION FLUID LOSS AP APPROACH 1 SW 09 12235 19758 666709 THE NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED AND THE ENGINE OIL QUANTITY DROPPED WHILE ON APPROACH. THE 2 ENGINE WAS SHUT DOWN AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE OIL PRESSURE SWITCH CASE CRAC KED AND LEAKING OIL. THE NR 2 ENGINE OIL PRESSURE SWITCH WAS REMOVED AND REPLACED. THE ENGINE WAS SERVICED WITH OIL AN D RUN AT VARIOUS POWER SETTINGS WITH NO LEAKS NOTED. 2 L 7 2 4F 4 F A16WE E2EA 1996110100480 19961101 00480 NM 1996 11 1 CALA9601514 1 19961027 A 7921 MS9388025 O-RING BOEING 727 727243 138408D NM PWA JT8 JT8D9 52048 NE OIL COOLER LEAKING A CALA A E UNSCHED LANDING ENGINE SHUTDOWN K FLUID LOSS TO TAKEOFF 1 SW 09 17407 21270 666799 THE NR 3 ENGINE BEGAN TO LOSE OIL QUANTITY AFTER TAKEOFF. THE NR 3 ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS RETURNED T O EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND PLUG ON FORWARD END OF OIL COOLER LEAKING. THE O-RING PLUG W AS REPLACED. THE NR 3 ENGINE WAS SERVICED TO FULL. A LEAK CHECK WAS PERFORMED AND NO LEAKS WERE NOTED. 2 L 7 3 4F 4 F RT A3WE E2EA 1996110100481 19961101 00481 NM 1996 11 1 CALA9601515 1 19961027 A 2530 8103060000 OVEN FAN BOEING 737 7373T0 1384582 NM AFT GALLEY FAILED A CALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 09 60312 23251 5071 23363 SMOKE APPEARED IN THE AFT GALLEY DURING TAXI OUT. THE AIRCRAFT WAS RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 AFT GALLEY OVEN FAN FROZEN AND OVERHEATED. THE NR 1 AFT GALLEY OVEN WAS REMOVED AND REPLACED, OPERATION OF THE OVEN CHECKED GOOD. ALL AFT GALLEY OVENS WERE OPERATED WITH NO DISCREPANCIES NOTED. 2 L 7 2 4F RT A16WE 1996110100482 19961101 00482 NM 1996 11 1 CALA9601516 1 19961021 A 5312 BULKHEAD BOEING 737 737130 1384435 NM BS 178 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33202 19019 INSPECTION FOUND A 6 INCH CRACK IN BULKHEAD BEHIND STIFFENER ON RT SIDE AT STA 178, WL 218. ALSO, A 1 INCH CRACK WAS FO UND AT WL 230.5, RT SIDE. THE CRACKED AREA AT WL 218 WAS REMOVED AND THE CRACK AT WL 230.5 WAS STOP DRILLED IAW SRM 53- 10-11. REPAIR DOUBLER, FILLER AND SHIMS WERE FABRICATED AND INSTALLED IAW SRM 53-10-11, 51-10-2 AND 51-30-2. 2 L 7 2 4F A16WE 1996110100483 19961101 00483 NM 1996 11 1 CALA9601517 1 19961023 A 5311 FRAME BOEING 737 737130 1384435 NM BS 727 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33202 19019 INSPECTION FOUND A 2 INCH CRACK EXTENDING AFT OF SECOND FASTENER HOLE IN LT BS 727 FRAME CHORD. THE LOWER CHORD SEGMENT WAS REMOVED AND REPLACED IAW CAL WORK CARD JA5310-0163802001. 2 L 7 2 4F A16WE 1996110100484 19961101 00484 NM 1996 11 1 CALA9601518 1 19961022 A 5315 FLOORBEAM BOEING 737 737130 1384435 NM BS 675 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33202 19019 INSPECTION FOUND A 1.5 INCH CRACK IN LOWER RADIUS OF FLOORBEAM AT STA 675, BBL 0. THE LOWER T-CHORD WAS REMOVED, A NEW CHORD WAS FABRICATED AND INSTALLED IAW SRM 51-20-2, 51-30-2 AND BOEING DRAWING NR 65-45410. 2 L 7 2 4F A16WE 1996110100485 19961101 00485 NM 1996 11 1 CALA9601519 1 19961023 A 5320 FITTING BOEING 737 737130 1384435 NM BS 685 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33202 19019 INSPECTION FOUND A 1.5 INCH CRACK IN FRAME FITTING AT BS 685, WL 208, LBL 62. THE FASTENER HOLE WAS COLD WORKED, A REPA IR ANGLE WAS FABRICATED AND INSTALLED IAW ECRA 5310-03346. 2 L 7 2 4F A16WE 1996110100486 19961101 00486 NM 1996 11 1 CALA9601520 1 19961021 A 5330 SKIN BOEING 737 737130 1384435 NM BS 747-727 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33202 19019 INSPECTION FOUND A 1 INCH CRACK IN RT FUSELAGE SKIN AT BS 747 AND AT BS 727A. BOTH CRACKED AREAS WERE CUT OUT, A DOUBLE R REPAIR WAS FABRICATED AND INSTALLED OVER EACH CRACK FROM STA 725 TO 790 IAW SRM 53-30-3. 2 L 7 2 4F A16WE 1996110100487 19961101 00487 NM 1996 11 1 CALA9601521 1 19961023 A 5330 SKIN BOEING 737 737130 1384435 NM BS 188-251.6 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33202 19019 INSPECTION FOUND CRACKS IN SECTION 41 RT FUSELAGE EXTERNAL SKIN FROM BS 188 TO 251.6, WL 207 TO 234. THE CRACK LENGTHS WERE NOT IDENTIFIED. THE SKIN WAS REPAIRED IAW EA 5310-01188. 2 L 7 2 4F A16WE 1996110100488 19961101 00488 WP 1996 11 1 CALA9601522 1 19961026 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 737 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 27522 47524 INSPECTION FOUND LT FRAME AT STA 737 CRACKED IN THREE PLACES. TWO CRACKS WERE 3.125 INCHES LONG AND ONE CRACK WAS 0.25 INCH LONG. THE FRAME WAS REMOVED AND REPLACED IAW ENGINEERING ORDER 1830 AND TASK CARD 05-5310-1-0019. 2 L 7 2 4F A6WE 1996110100489 19961101 00489 WP 1996 11 1 CALA9601523 1 19961024 A 5730 SKIN DOUG DC9 DC932 3022066 WP RT WING CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 27522 47524 INSPECTION FOUND CORROSION ON RT WING SKIN PANEL NR 1244. THE CORRODED AREA WAS CUT OUT, A REPAIR DOUBLER WAS INSTALLED IAW SRM 57-31-1, FIGURE 1. 2 L 7 2 4F A6WE 1996110100490 19961101 00490 1996 11 1 COMA9610310 4 19961025 A 2210 AUTO PILOT EMB 120 EMB120RT SO E/E COMPT MALFUNCTIONED A COMA K NONE L NO TEST UK UNKNOWN 1 SO 01 1110J 120110 DURING AUTO PILOT TEST THE ELEVATOR TRIM RUNS WILD. AUTO PILOT SYSTEM PLACED ON DEFERRED MAINTENANCE LIST. 2 L 7 2 4T RT A31SO 1996110100491 19961101 00491 SO 1996 11 1 COMA9610311 1 19961023 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 263CA 13354 1248 120255 AFT EMERGENCY LIGHTS ARE INOP. REPLACED EMERGENCY BATTERY. 2 L 7 2 4T RT A31SO 1996110100492 19961101 00492 SO 1996 11 1 COMA9610312 1 19961023 A 2752 3203001007 ATUATOR EMB 120 EMB120RT SO R/HRT TE FLAP MALFUNCTION A COMA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 01 179CA 16588 120179 FLAP DISAGREEMENT WARNING DURING LANDING APPROACH. REPLACED THE RT FLAP OUTBD ACTUATOR. 2 L 7 2 4T RT A31SO 1996110100493 19961101 00493 EA 1996 11 1 COMA9660181 1 19961024 A 7732 6233M30A ACCELEROMETER CNDAIR CL600 CL6002B19 EA RT ENGINE MALFUNCTION A COMA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 01 914CA 7012 THE RT ENGINE N1 VIBRATION INDICATOR WAS IN THE CAUTION RANGE AT 85 DEGREES N1. REPLACED THE ENGINE ACCELEROMETER. 2 L 7 2 4F RT A21EA 1996110100494 19961101 00494 EA 1996 11 1 COMA9660182 1 19961024 A 3260 601R572181 PROX SENSOR CNDAIR CL600 CL6002B19 EA NLG DEFECTIVE A COMA K NONE O OTHER AP APPROACH 1 SO 01 948CA 7079 NOSE LANDING GEAR DOORS OPEN MESSAGE ON EICAS AFTER LANDING GEAR EXTENDED. REPLACED THE NLG DOORS PROXIMITY SENSOR WIRI NG HARNESS. 2 L 7 2 4F RT A21EA 1996110100495 19961101 00495 EA 1996 11 1 COMA9660183 1 19961024 A 2612 47259701 FIRE CONTROLLER CNDAIR CL600 CL6002B19 EA E/E COMPT MALFUNCTION A COMA K NONE N FALSE WARNING AP APPROACH 1 SO 01 929CA 3453 796 7035 ALL ENGINE AND APU FIRE WARNINGS AND FAIL LIGHTS CAME ON. REPLACED THE FIRE DETECTION CONTROLLER. 2 L 7 2 4F RT A21EA 1996110100496 19961101 00496 EA 1996 11 1 COMA9660184 1 19961025 A 7830 TR UNIT CNDAIR CL600 CL6002B19 EA RT ENGINE MALFUNCTIONED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 945CA 7069 RT ENGINE THRUST REVERSER UNLOCKED MESSAGE ON EICAS DURING TAKEOFF. SECURED THRUST REVERSER CLOSED AND TRANSFERRED DISC REPANCY TO DEFERRED MAINTENANCE LIST. 2 L 7 2 4F RT A21EA 1996110100497 19961101 00497 EA 1996 11 1 COMA9660185 1 19961023 A 7830 TR UNIT CNDAIR CL600 CL6002B19 EA RT ENGNE MALFUNCTIONED A COMA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 945CA 7069 RT ENGINE THRUST REVERSER UNLOCKED MESSAGE ON EICAS. SECURED THRUST REVERSER CLOSED AND TRANSFERRED TO DEFERRED MAINTEN ANCE LIST. 2 L 7 2 4F RT A21EA 1996110100498 19961101 00498 EA 1996 11 1 COMA9660186 1 19961025 A 2760 270003 PCU CNDAIR CL600 CL6002B19 EA LT SPOILER OUT OF ADJUST A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 914CA 25 25 7012 LT FLIGHT SPOILER IS DEPLOYED 4 DEGREES DURING FLIGHT. FLIGHT SPOILER DEPLOYED CAUTION MESSAGE ON EICAS. ADJUSTED THE LT FLIGHT SPOILER POWER CONTROL UNIT TO M/M SPECIFICATIONS, SYSTEM TEST NORMAL. 2 L 7 2 4F RT A21EA 1996110100499 19961101 00499 NM 1996 11 1 UPS96221468 1 19961015 A 5753 651927015 FLAP TRACK BOEING 727 72722C 138400F NM RT TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-C, RT I/B FLAP TRACK IS CORRODED AT ATTACHMENT TO MLG SUPPORT BEAM. REPAIRED IAW B727-5742-0651. 2 L 7 3 4F A3WE 1996110100500 19961101 00500 NM 1996 11 1 UPS96221470 1 19961025 A 3350 BATTERIES BOEING 727 72722C 138400F NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE N/A, EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES. 2 L 7 3 4F A3WE 1996110100501 19961101 00501 NM 1996 11 1 UPS96221473 1 19961024 A 3350 LIGHT BOEING 727 72727C 138400J NM COCKPIT MALFUNCTIONED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 907UP 19118 INSPECTION TYPE N/A, EMERGENCY EXIT ILLUMINATED AND POPPED OUT OF SOCKET ON LANDING, LIGHT IN COCKPIT. REPLACED LIGHT O VER CABIN DOOR AND OPS CHECK NORMAL. 2 L 7 3 4F A3WE 1996110100502 19961101 00502 NM 1996 11 1 UPS96421302 1 19961008 A 2612 CONNECTOR BOEING 747 747123 1384873 NM NR 2 FIRE DET EXPOSED WIRE A IPXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 677UP 20391 INSPECTION TYPE N/A, LOWER CARGO FIRE DETECTION CAME ON AT 13,000 FT AND WENT OUT WHEN DESCENDING BELOW 10,000 FT. DIDN 'T COME BACK ON FOR REMAINDER OF FLIGHT. FOUND NR 2 LOWER LOBE DETECTOR POWER WIRE BARE AND CONTACTING CANNON PLUG BACK SHELL. REPAIRED WIRE, TESTS GOOD. 2 L 7 4 4F A20WE 1996110100503 19961101 00503 NM 1996 11 1 UPS96421471 1 19961024 A 5753 SKIN BOEING 747 747123F NM LT TE MID FLAP DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE N/A, LEFT I/B MID FLAP HAS AREA OF DELAMINATION IN CENTER ON FLAP 8 FROM ACCORDING SEAL ON BOTTOM AREA 4 BY 1. COVERED WITH SPEED TAPE, DEFERED PER MMOC EO B747-5750-8561-A CONTROL NR D117511 COMPLIED WITH. 2 L 7 4 4F A20WE 1996110100504 19961101 00504 NM 1996 11 1 UPS96421474 1 19961024 A 3350 LIGHT BOEING 747 747121 1384871 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE N/A, EMERGENCY EXIT LIGHT OVER UPPER DECK ESCAPE DOOR INOP. TRANSFERRED TO M117610 PER MEL 33-13 POWER CONTACTS TO LIGHTS ADJUSTED EXIT LIGHT. DEFERRAL CLEARED PLACARD REMOVED. 2 L 7 4 4F A20WE 1996110100505 19961101 00505 NM 1996 11 1 UPS96421476 1 19961015 A 5400 SPAR WEB BOEING 747 747SR46 NM NAC STA 193/196 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE-C, CRACK IN LOWER SPAR WEB, NAC STA 193/196 LT, AT PNU DUCT SUPPORT STIFFENER. REPAIRED LOWER SPAR WEB AT NAC STA 193/196 LT ACC SRM 54-10-03 FIG 2. 2 L 7 4 4F A20WE 1996110100506 19961101 00506 NM 1996 11 1 UPS96421477 1 19961017 A 5711 SPAR WEB BOEING 747 747SR46 NM WS 453 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE-C, MID-SPAR WEB INSPECTION, EO 747-5710-7893 FOUND CRACK IN WEB AT WS 453. CRACK IS APPROX 7 MM, STARTI NG AT FASTENER HOLE FROM SECOND ROW OF FASTENERS THAT ATTACH THE WEB TO THE UPPER CHORD. REPAIRED MID-SPAR WEB AT WS 45 3 ACC EO B747-5710-7893, APPNDIX C. 2 L 7 4 4F A20WE 1996110100507 19961101 00507 NM 1996 11 1 UPS96421478 1 19961021 A 5330 SKIN BOEING 747 747SR46 NM BS 2035-2055 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE-C, PREVIOUS REWORK ON SKIN LAP SPLICE STR 46 BETWEEN BS 2035 AND 2055 LT IS OUT OF LIMITS ACC SRM 53-30- 01 FIG 1. SKIN LAP SPLICE ON STR 46 BETWEEN BS 2035 AND 2055 REPAIRED ACC SRM 53-30-03 FIG 17. 2 L 7 4 4F A20WE 1996110100508 19961101 00508 NM 1996 11 1 UPS96421479 1 19961016 A 5311 FRAME BOEING 747 747SR46 NM BS 2200 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE-C, AREA AFT OF BULK CARGO COMP DURING REPLACEMENT OF FILLER FOUND CRACK IN FRAME INNERFLANGE REINFORCEM ENT ANGLE AT BS 2200, NEAR FRAME STIFFENER AT S-42 RT. REPLACED REINFORCEMENT ANGLE ACCORDING TO SRM 51-30-02. 2 L 7 4 4F A20WE 1996110100509 19961101 00509 NM 1996 11 1 UPS96421480 1 19961015 A 5320 STIFFENER BOEING 747 747SR46 NM BS 2200 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE-C, AREA AFT OF BULK CARGO COMP FOUND CORROSION ON TOP OF FRAME STIFFENER BS 2200 NEAR S-42 RT, JUST I N FRONT OF RT OUTFLOW VALVE. CORROSION DAMAGE OUT OF LIMITS ACC TO SRM 53-10-01. REPLACED SAME STIFFENER ACC TO SRM 51 -30-02. 2 L 7 4 4F A20WE 1996110100510 19961101 00510 WP 1996 11 1 UPS96821472 1 19961023 A 2150 ACM DOUG DC8 DC873F 302199F WP LEFT MALFUNCTIONED A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE N/A, STRONG SMELL OF SKYDROL IN COCKPIT. TRANSFERRED TO N/R CARD 351733/3733, REMOVED ACM DUCTS, WATER SEPARATOR AND CLEANED AND REPLACED DUCTS, INSTALLED NEW SOCK IN WATER SEPARATOR AFTER CLEANING AND REPLACED LT ACM PER M /M 21-55-01. 2 L 7 4 4F RT 4A25 1996110100511 19961101 00511 WP 1996 11 1 UPS96821475 1 19961024 A 7312 FUEL FILTER DOUG DC8 DC871F 302199D WP GE CFM CFM562 GL NR 3 ENG MALFUNCTIONED A IPXA O OTHER X ENGINE FLAMEOUT UK UNKNOWN 1 SO 01 715UP 45915 INSPECTION TYPE N/A, REMOVED AND REPLACED FUEL FILTER ASSY DUE TO ENGINE FLAME-OUT, NR 3. REPLACED FUEL FILTER ASSY, NO CONTAMINATION FOUND REF MM 27-00-00. LEAK CHK'D NR 3 FUEL FILTER AS REQUIRED AND NO LEAKAGE NOTED. 2 L 7 4 4F 4 F RT 4A25 E2GL 1996110100512 19961101 00512 NM 1996 11 1 96FDEA01613 1 19961024 A 5753 6521630188 SKIN BOEING 727 727233 138408A NM TE FOREFLAP DELAMINATION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 NR 0697, RT I/B FOREFLAP HAS TWO LARGE AREAS OF DENTS AND DELAMINATIONS ON LOWER SURFACE. *S/D* RT I/B FOREFLAP WAS RE PAIRED PER FEDEX SRM 51-40-6. 2 L 7 3 4F RT A3WE 1996110100513 19961101 00513 NM 1996 11 1 96FDEA01614 1 19961025 A 5312 6580103 BULKHEAD BOEING 727 72725 1384006 NM BS 950 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 511FE 18283 NR 0507 023, POSSIBLE CRACK ON AFT SIDE OF BS 950 BULKHEAD AT LBL 4 WL 176 AND AT LBL 11, WL 181 TO 184. 2 L 7 3 4F A3WE 1996110100514 19961101 00514 NM 1996 11 1 96FDEA01615 1 19961026 A 5312 6516330 BULKHEAD BOEING 727 72725 1384006 NM BS 870 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 511FE 18283 NR 0509 024, CRACK ON THE AFT SIDE OF THE 870 BULKHEAD AT RBL 9.5 AND WL 157. 2 L 7 3 4F A3WE 1996110100515 19961101 00515 NM 1996 11 1 96FDEA01616 1 19961027 A 5753 652163492 SKIN BOEING 727 727233 138408A NM RT TE AFT FLAP DELAMINATION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 NR 0699 006, RT I/B AFT FLAP HAS LARGE AREA OF DENTS AND DELAMINATIONS ON LOWER SURFACE I/B END *S/D* REPAIRED RT I/B AFT FLAP ON LOWER SURFACE IAW FEDEX SRM 51-40-6. 2 L 7 3 4F RT A3WE 1996110100516 19961101 00516 NM 1996 11 1 96FDEA01617 1 19961025 A 5320 651758866 G-BEAM BOEING 727 727233 138408A NM BS 267 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 NR 0751 009, CORROSION (C53-221-01) ON TOP OF 25 G-BEAM AND 3 SUPPORTING INTERCOSTALS STA 267 LBL 8 STA 267 LBL 9 STA 26 7 LBL 11 AND STA 277 TO 259 LBL 13 WL 208. *S/D* REMOVED AND REPLACED 25 G-BEAM AND 3 SUPPORTING INTERCOSTAL FLOOR SUP PORTS AT STA 277 TO 259.5, LBL 8, STA 267 LBL 8 TO LBL 13 STA 277 TO 259.5 LBL 13, WL 208 AND STA 272 TO 265, LBL 8 TO R BL 22 IAW FEDEX SRM 53-10-1. 2 L 7 3 4F RT A3WE 1996110100517 19961101 00517 NM 1996 11 1 96FDEA01618 1 19961025 A 5320 651627910 BEAM BOEING 727 727233 138408A NM BS 760-850 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 NR 0710, CORROSION (53-224-01,2) ON LONGITUDINAL BEAM AT BS 779 TO BS 793 RBL 45, WL 208 (P/N 65-16279-10). *S/D* REMO VED AND REPLACED LONGITUDINAL BEAM AT BS 740 TO 850 RBL 45 WL 208. 2 L 7 3 4F RT A3WE 1996110100518 19961101 00518 NM 1996 11 1 96FDEA01619 1 19961025 A 5315 65C260184 FLOORBEAM BOEING 727 727233 138408A NM BS 720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 NR 0652, CORROSION (C53-224-01) ON TOP CHORD OF FLOORBEAM BS 720D RBL 23, LBL 3, 15, 20. *S/D* REPAIRED PER FEDEX SRM 53-10-8. 2 L 7 3 4F RT A3WE 1996110100519 19961101 00519 NM 1996 11 1 96FDEA01612 1 19961024 A 5753 6521630187 SKIN BOEING 727 727233 138408A NM LT TE FORE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 NR 0693, LT I/B FORE FLAP HAS TWO LARGE AREAS OF DENTS AND DELAMINATION ON LOWER SURFACE. *S/D* REPAIRED DAMAGED SKIN TO LT I/B FORE FLAP LOWER SURFACE IAW FEDEX SRM 51-40-6. 2 L 7 3 4F RT A3WE 1996110100520 19961101 00520 NM 1996 11 1 DHL96722005 1 19961024 A 2410 CSD BOEING 727 727228 NM NR 2 REQD SERVICE A DHLA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SO 01 722DH 19861 GEN NR 2 HAD 2 LIGHT TRIP EN ROUTE NO FAULT, INDICATIONS ON GEN FAULT PANEL. RESIDUAL VOLTS 14 TO 15 VOLTS AND UNSTABLE FREQS UNSTABLE AT 380 TO 382 CPS. FOUND NR 2 CSD OIL QTY LEVEL AT BOTTOM OF OPERATING BAND. SERVICED CSD PER MM 12-13 -12, CHECKS NORMAL MM 24-10. 2 L 7 3 4F A3WE 1996110100521 19961101 00521 NE 1996 11 1 DHL96722006 2 19961029 A 7200 ENGINE BOEING 727 727228 NM PWA JT8 JT8D7 52053 NE NR 1 VIBRATION A DHLA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 01 722DH 19861 657719 MIDDLE FREQUENCY VIBRATION FELT IN THE NR 1 THRUST LEVER AT ALL POWER SETTINGS ABOVE 1.4 EPR DURING FLIGHT. RETURNED TO DENVER. PERFORMED ENGINE VIBRATION SURVEY ON WING PER MM 72-00 TEST 1, ENGINE WITHIN MANUAL LIMITS. OK FOR CONT SERVI CE. 2 L 7 3 4F 4 F A3WE E2EA 1996110100522 19961101 00522 NE 1996 11 1 DHL96722007 2 19961024 A 7200 ENGINE BOEING 727 727228 NM PWA JT8 JT8D7 52053 NE NR 1 VIBRATION A DHLA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SO 01 722DH 19861 ENGINE NR 1 HAS ABNORMAL VIBRATIONS IN THRUST LEVER AND ENGINE START LEVERS. GROUND RAN NR 1 ENGINE PER JRH 04-02-01, N OT ABNORMAL VIBRATIONS NOTED THROUGHOUT OPERATING RANGE. 2 L 7 3 4F 4 F A3WE E2EA 1996110100523 19961101 00523 NM 1996 11 1 DHL96708006 1 19961022 A 2133 1032801 OUTFLOW VALVE BOEING 727 72725 1384006 NM CABIN FAILED A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 708DH 18275 ON DEPARTURE OUT OF 11,000 FT, HEARD LOUD BUMP FROM REAR OF AIRCRAFT. IMMEDIATELY THE AIRCRAFT BEGAN TO DEPRESSURIZE AN D CABIN ALTITUDE COULD NOT BE CONTROLLED BY ANY MEANS. REMOVED AND DEFERRED OUTFLOW VALVE. 2 L 7 3 4F A3WE 1996110100524 19961101 00524 WP 1996 11 1 CKSA96188 1 19961023 A 5330 SKIN DOUG DC8 DC8F54 3021926 WP BS 480 PUNCTURED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 806CK 45932 ON WALKAROUND, FOUND HOLE IN SIDE OF AIRCRAFT AT STATION 480 JUST AFT OF A-PIT. AIRCRAFT REPAIRED PER SRM 53-4-0, 53-2- 1 WITH A CLASS TWO REPAIR, REFERENCE EA 96-296. REINSPECT WITHIN 12,000 CYCLES, REPETITIVE INSPECT AT 4,000 CYCLES THER EAFTER. 2 L 7 4 4F 4A25 1996110100545 19961101 00545 WP 1996 11 1 CA960320503 1 19960104 A 7603 THROTTLE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE RT ENGINE STIFF W E ENGINE SHUTDOWN O OTHER CR CRUISE 1 CA P657446D (CAN)DURING CRUISE FLIGHT, RIGHT HAND THROTTLE BECAME PROGRESSIVELY STIFF. FINALLY THROTTLE SEIZED AND ENGINE SHUT-DOWN. AIRCRAFT LANDED ON SINGLE ENGINE. MAINTENANCE INVESTIGATION REVEALED WATER LINE AT R H AFT LAVATORY WAS SPLIT ALLOWING WATER TO DROP ON TO RIGHT HAND THRUST REVERSER. HEAT APPLIED TO SECTOR, ICE MELTED. SPLIT LINE REPAIRED AND RIGHT ENGINE THROTTLE AND THRUST REVERSER OPERATIONALLY CHECKED, SYSTEM OKAY. 2 L 7 2 4F 4 F A6WE E2EA 1996110100546 19961101 00546 EA 1996 11 1 CA960320504 1 19960105 A 3230 601R509675 CONTROL PANEL CNDAIR CL600 CL6002B19 EA NLG FAILED W D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 CA 1052 (CAN)AFTER TAKEOFF, NOSE LANDING GEAR DID NOT RETRACT. CHANGED LANDING GEAR CONTROL PANEL AND PSEU. (PSEU P/N 601R50969- 3). 2 L 7 2 4F RT A21EA 1996110100547 19961101 00547 EA 1996 11 1 CA960320505 1 19960105 A 3230 864806 PSEU ELDEC CNDAIR CL600 CL6002B19 EA NLG FAILED W D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 CA 313 (CAN)AFTER TAKEOFF, NOSE LANDING GEAR DID NOT RETRACT. PSEU (PROX., SWITCH ELEC. UNIT) REPLACED. 2 L 7 2 4F RT A21EA 1996110100548 19961101 00548 EU 1996 11 1 CA960320506 1 19960106 A 3246 D230670002 WHEEL ASSY AIRBUS 320 A320211 3930320 EU NLG BEARING FAILED W K NONE O OTHER LD LANDING 1 CA (CAN)AFTER TOUCH DOWN EXCESSIVE NOISE HEARD COMING FROM NOSE WHEEL WELL AREA. MAINTENANCE INVESTIGATION REVEALED LEFT IN BOARD NOSE WHEEL BEARING HAD FAILED. NOSE LANDING GEAR SLIDING TUBE CHANGED ALONG WIT H LEFT AND RIGHT NOSE WHEEL ASSEMB LIES. STEERING SYSTEM TESTED SERVICEABLE. 2 L 7 2 4F RT A28NM 1996110100549 19961101 00549 WP 1996 11 1 CA960320508 1 19960107 A 2130 PRESS LOSS WARN DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE CABIN ILLUMINATED W G B O2 MASK DEPLOYED EMER. DESCENT J WARNING INDICATION CL CLIMB 1 CA P657222D (CAN)DURING CLIMB OUT CABIN PRESSURE LIGHT CAME "ON". CABIN PRESSURE WAS LOST, CABIN ALTITUDE WAS AT 12,000 FEET AND CLI MBING. EMERGENCY DESCENT INITIATED. AIRCRAFT GROUND RUN CARRIED OUT, CABIN PRESSURIZE D AND LEAKED CHECKED, AIR CONDITIO NING SYSTEM AND SECOND SEGMENT CLIMB SWITCHES OPERATIONALLY CHECKED. UNABLE TO DUPLICATE FAULT, AIRCRAFT CHECKED SERVICE ABLE. 2 L 7 2 4F 4 F A6WE E2EA 1996110100550 19961101 00550 EA 1996 11 1 CA960320510 1 19960112 A 3510 RCF6708 REGULATOR EROS CNDAIR CL600 CL6002B19 EA OXY PRESS CONTAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN)OIL CONTAMINATION FOUND IN OXYGEN PRESSURE REGULATOR IN LOWER CHAMBER OF UNIT HOUSING. 2 L 7 2 4F RT A21EA 1996110100551 19961101 00551 EA 1996 11 1 CA960320511 1 19960112 A 3510 RCF6706 REGULATOR EROS CNDAIR CL600 CL6002B19 EA OXYGEN PRESS CONTAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA 2113 (CAN)OIL CONTAMINATION FOUND IN OXYGEN PRESSURE REGULATOR LOWER CHAMBER OF HOUSING. 2 L 7 2 4F RT A21EA 1996110100552 19961101 00552 EU 1996 11 1 CA960320512 1 19960112 A 3510 RCF6705 REGULATOR AIRBUS 320 A320211 3930320 EU OXY PRESS CONTAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN)ON INSPECTION, OIL CONTAMINATION FOUND IN OXYGEN REGULATOR. LOWER HOUSING OF REGULATOR AFFECTED. REGULATOR BEING RE CALLED FOR OVERHAUL. 2 L 7 2 4F RT A28NM 1996110100553 19961101 00553 EU 1996 11 1 CA960320513 1 19960112 A 2780 COMPUTER AIRBUS 320 A320211 3930320 EU SLAT/FLAP LOCKED FAULT W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA (CAN)ON APPROACH SLAT/FLAP LOCKED FAULT INDICATION. MAINTENANCE CHANGED #1 SLAT/FLAP CONTROL COMPUTER (S.F.C.C.) AND INT ERROGATED CENTRAL FAULT DISPLAY SYSTEM (C.F.D.S.). 2 L 7 2 4F RT A28NM 1996110100554 19961101 00554 WP 1996 11 1 CA960320514 1 19960114 A 7620 188352 FUEL LEVER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE RT ENG SOV INOPERATIVE W O OTHER P NO WARNING INDICATION TX TAXI/GRND HDL 1 CA P657717D (CAN)UNABLE TO SHUT DOWN RIGHT ENGINE WITH FUEL SHUT OFF LEVER. FUEL SHUT OFF HANDLE USED. MAINTENANCE ACTION INVOLVED R EPLACING FLEXIBLE EANCO CABLE AT RIGHT ENGINE PYLON. 2 L 7 2 4F 4 F A6WE E2EA 1996110100555 19961101 00555 EA 1996 11 1 CA960320516 1 19960115 A 3260 BRACKET CNDAIR CNDAIR CL600 CL6002B19 EA NLG SENSOR BENT W O OTHER J WARNING INDICATION CL CLIMB 1 CA 375 (CAN)AFTER TAKEOFF DURING LANDING GEAR RETRACTION, NOSE GEAR STAYED DOWN.GEAR 'DISAGREE' AURAL AND 'NOSE DOOR' ON EICAS. NOSE OLEO PROXIMITY SENSOR BRACKET FOUND BENT PUTTING SENSOR OUT OF RANGE. 2 L 7 2 4F RT A21EA 1996110100556 19961101 00556 NM 1996 11 1 CA960320518 1 19960120 A 2540 DRAIN FROZEN BOEING 767 767275 NM LAVATORY FROZEN W K O NONE OTHER K FLUID LOSS LD LANDING 1 CA (CAN)FORARD LAVATORY AND GALLEY DRAINS OVERFLOWED DUE WATER DRAIN HEATER INOPERATIVE. FLOWED INTO ELECTRICAL COMPARTMENT RESULTING IN LOSS OF #1 & #2 EICAS ON LANDING. COMPUTERS REPLACED. DRAINS CLEARED. 2 L 7 2 RT RT A1NM 1996110100557 19961101 00557 1996 11 1 CA960320519 4 19960120 A 2210 B397BAM0407 COMPUTER AIRBUS 320 A320211 3930320 EU #2 FLT AUG INOPERATIVE W D RETURN TO BLOCK P NO WARNING INDICATION CL CLIMB 1 CA (CAN)ON ENGAGING AUTO PILOT AFTER TAKEOFF, RED WARNING LIGHT AND "GEAR NOT DOWN" MESSAGE WITH A QUICK PITCH UP AND DOWN OF AIRCRAFT. AIRCRAFT RETURNED TO BASE. MAINTENANCE ACCOMPLISHED C.F.D.S. TEST OF A.F .S. AND DETERMINED F.A.C. #2 WAS A T FAULT. REPLACED F.A.C. AND GROUND TEST CARRIED OUT. 2 L 7 2 4F RT A28NM 1996110100558 19961101 00558 WP 1996 11 1 CA960320520 1 19960121 A 4900 AUX POWER UNIT DOUG DC9 DC932 3022066 WP PWA APU OIL LEAK W O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA (CAN)DURING PUSH BACK, CABIN FILLED WITH SMOKE, BOTH REAR SMOKE DETECTORS SOUNDED. MAINTENANCE FOUND PROBLEM CAUSED BY A .P.U.AUXILIARY POWER UNIT REPLACED.LEAK AND OPERATIONAL CHECK CARRIED OUT. 2 L 7 2 4F A6WE 1996110100559 19961101 00559 WP 1996 11 1 CA960320521 1 19960121 A 5241 49293611 DOOR ROD ASSY DOUG DC9 DC932 3022066 WP GALLEY DOOR BENT/TWISTED W K NONE O OTHER TX TAXI/GRND HDL 1 CA (CAN)GALLEY DOOR FROZEN; PARTS DAMAGED WHILE FORCING DOOR OPEN. MAINTENANCE INSTALLED NEW FITTING AND ROD ASSEMBLY P/N 3 9166121. 2 L 7 2 4F A6WE 1996110100560 19961101 00560 EA 1996 11 1 CA960320522 1 19960121 A 2160 75065916 SWITCH CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE COMPRESSOR FAILED W C D ABORTED TAKEOFF RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 CA 61 807337 (CAN)TAKEOFF REJECTED AT 100 KNOTS BECAUSE SMOKE IN COCKPIT FROM AIR CONDITIONING. LEFT PACK SUPPLYING HOT AIR AT 96 DEG REES C, UNABLE TO CONTROL IN EITHER AUTO OR MANUAL. CHANGED COMPRESSOR OUTLET TEMPERA TURE SWITCH AND ACM. ACM P/N 78290 -13. 2 L 7 2 4F 4 F RT A21EA E15NE 1996110100561 19961101 00561 WP 1996 11 1 CA960320523 1 19960122 A 3230 5927079507 HOUSING ACTUATOR DOUG DC9 DC932 3022066 WP NOSE LDG GEAR MISSING BOLT W O OTHER J WARNING INDICATION AP APPROACH 1 CA (CAN)WHEN LANDING GEAR SELECTED DOWN ON APPROACH, IT APPEARED NOSE LANDING GEAR DOORS WERE SLOW TO OPEN. THIS CONDITION WAS FOLLOWED BY A LOUD NOISE. SUBSEQUENT MAINTENANCE INVESTIGATION FOUND NOSE LANDING GEAR ACTUATOR UPPER BOLT MISSING. MAINTENANCE ACTION INVOLVED REPLACING HOUSING ACTUATOR, RETRACT ACTUATOR AND INSTALLING NEW BOLT. CHECK RETRACTIONS CARR IED OUT SERVICEABLE. 2 L 7 2 4F A6WE 1996110100562 19961101 00562 EU 1996 11 1 CA960320524 1 19960122 A 5210 ARMING HANDLE AIRBUS 320 A320211 3930320 EU L2 DOOR REQ ADJUSTIMENT W O OTHER J WARNING INDICATION CR CRUISE 1 CA (CAN)L2 DOOR ARMING HANDLE MOVED TO DISARM DURING FLIGHT. IN FLIGHT THE HANDLE GRADUALLY RAISED AND THE SLIDE ARMED INDI CATION SHOWED DISARMED. MAINTENANCE ACTION INVOLVED ADJUSTING TENSION ON ARM/DISARM C ABLE, ADJUSTED PROXIMITY SWITCH TA RGET AND OPERATIONALLY CHECKED. 2 L 7 2 4F RT A28NM 1996110100563 19961101 00563 WP 1996 11 1 CA960320525 1 19960123 A 2150 DUCT DOUG DC9 DC932 3022066 WP LT ACM SEPARATED W D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 CA (CAN)UNABLE TO MAINTAIN PRESSURIZATION WITH ANTI-ICE ON. TO MAINTAIN PRESSURIZATION REQUIRED AN E.P.R. OF 1.6. SUBSEQUEN T MAINTENANCE INVESTIGATION REVEALED DUCT HAD SEPARATED FROM LEFT AIR CYCLING MACHINETO LEFT WATER SEPARATOR. DUCT AND W ATER SEPARATOR SECURED. BOTH PACKS GROUND RUN. 2 L 7 2 4F A6WE 1996110100564 19961101 00564 1996 11 1 CA960320526 4 19960124 A 2312 COMM SYS DOUG DC9 DC932 3022066 WP NR 1&2 COMM VHF INOPERATIVE W O OTHER J WARNING INDICATION CR CRUISE 1 CA (CAN)COMPLETE COMMUNICATION FAILURE FOR 8 MINUTES. ABLE TO RECOVER #2 VHF. MAINTENANCE ACTION INVOLVED CHANGING FIRST OF FICER AND CAPTAINS IMCROPHONES. ALSO CHECKED #1 & #2 VHF FROM BOTH POSITIONS. 2 L 7 2 4F A6WE 1996110100565 19961101 00565 EU 1996 11 1 CA960320527 1 19960124 A 2131 9022157028 PRESS.CONTROLLER AIRBUS 320 A320211 3930320 EU CABIN FAILED W B EMER. DESCENT O OTHER CR CRUISE 1 CA (CAN)AT FLIGHT LEVEL FL370, CABIN ALTITUDE REACHED 8,500 FT., EMERGENCY DESCENT INITIATED, AIRCRAFT LEVELED AT 19,000 FT . AND CABIN ALTITUDE STABILIZED AT 5,000 FT. MAINTENANCE CHANGED #1 CONTROLLER. 2 L 7 2 4F RT A28NM 1996110100566 19961101 00566 EU 1996 11 1 CA960320528 1 19960124 A 2910 HYDRAULIC LINE AIRBUS 320 A320211 3930320 EU LT NR 4 SPOILER LEAKING W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA (CAN)CLASS 1 ECAM MESSAGE "FLIGHT CONTROL FAULT" CARRIED OUT ECAM ACTION, LANDED FLAPLESS. MAINTENANCE INVESTIGATION FOU ND HYDRAULIC LINE TO LEFT #4 SPOILER LEAKING. NEW LINE FABRICATED & INSTALLED. SYSTEM TOPPED AND OPERATIONALLY CHECKED. 2 L 7 2 4F RT A28NM 1996110100567 19961101 00567 WP 1996 11 1 CA960320530 1 19960126 A 2410 976J2522 GENERATOR DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE LT CSD INOPERATIVE W D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CA P656975D (CAN)ON TAKEOFF MASTER CAUTION LIGHT CAME ON WITH LEFT AC BUS OFF, GENERATOR OFF, DC BUS OFF LIGHT ON, AC X TIE LOCKOUT LIGHT ON. LEFT CSD OIL PRESSURE LOW LIGHT ON, CSD DISCONNECTED AND AIRCRAFT RETURNED TO BASE. MAINTENANCE INVESTIGATION REVEALED SCAVENGE FILTER HOUSING BROKEN ON LEFT CSD. LEFT CSD P/N 696233A, GENERATOR, CSD OIL COOLER REPLACED AND GROUN D RUN CARRIED OUT. 2 L 7 2 4F 4 F A6WE E2EA 1996110100568 19961101 00568 EU 1996 11 1 CA960320531 1 19960127 A 2750 793A000003 ACTUATOR AIRBUS 320 A320211 3930320 EU NR 3 FLAP INOPERATIVE W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA (CAN)FLAP CONTROL ECAM MESSAGE; FLAPS LOCKED AND WING TIP BRAKE. FLAPLESS LANDING. MAINTENANCE ACTION RESET WING TIP BRA KE THROUGH C.F.D.S. AND S.F.C.C. #1 AND #2. REPLACED #3 FLAP ACTUATOR. OPERATION CHEC K CARRIED OUT. 2 L 7 2 4F RT A28NM 1996110100569 19961101 00569 EU 1996 11 1 CA960320532 1 19960128 A 5241 D31516101 DOOR MECHANISM AIRBUS 320 A320211 3930320 EU GALLEY DOOR BROKEN W K NONE O OTHER TX TAXI/GRND HDL 1 CA (CAN)R-1 DOOR REPORTED INOPERATIVE ON ARRIVAL. MAINTENANCE INVESTIGATION FOUND BROKEN DOOR ARM/DISARM STRIKER PLATE ON G ALLEY FLOOR AND BOTTLE BLOWN. COPPER SEAL REPLACED, CLEVIS AND DOOR STRIKER REPLACED.DOOR SLIDE REPLACED. 2 L 7 2 4F RT A28NM 1996110100570 19961101 00570 NE 1996 11 1 CA960320533 2 19960129 A 7261 SEAL DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE N1 TACH CUT W A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 CA P657717D (CAN)ONE HALF HOUR AFTER TAKEOFF, LOW PRESSURE LIGHT CAME ON. ENGINE SHUT DOWN. AIRCRAFT RETURNED TO BASE. MAINTENANCE I NVESTIGATION REVEALED N1 TACHOMETER WIRING BOBBIN SEAL CUT. SEAL REPLACED, N1 WIRING RECONNECTED, OIL SERVICED AND AIR CONDITIONING COALESCER BAGS REPLACED. ENGINE GROUND RUN CARRIED OUT. 2 L 7 2 4F 4 F A6WE E2EA 1996110100571 19961101 00571 EU 1996 11 1 CA960320534 1 19960131 A 2780 9028A000401 ACTUATOR AIRBUS 320 A320211 3930320 EU SLAT ROTARY INOPERATIVE W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA (CAN)ON INITIAL FLAP SELECTION DURING APPROACH, ECAM MESSAGE SLATS INOPERATIVE. MAINTENANCE INVESTIGATION FOUND SLAT ROT ARY ACTUATOR 6095CM TRIPPED. SLAT ROTARY ACTUATOR 6095CM REPLACED, S.F.C.C. #1 AND #2TESTED AND FLAP/SLAT OPERATIONALLY CHECKED. 2 L 7 2 4F RT A28NM 1996110100572 19961101 00572 WP 1996 11 1 CA960320535 1 19960131 A 2400 ELECTRICAL SYSTM DOUG DC9 DC932 3022066 WP FLT DECK & CABIN BURNING SMELL W O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA (CAN)ON DEPARTURE TAXIING ELECTRICAL SMELL WAS NOTICED THROUGHOUT AIRCRAFT. GALLEY POWER SWITCHED OFF. E & E COMPARTMENT AND HEAT EXCHANGER AREA CHECKED AND AIR CONDITIONING PACKS RAN ON GROUND. UNABLE TO FIND FAULT. 2 L 7 2 4F A6WE 1996110100573 19961101 00573 EU 1996 11 1 CA960320536 1 19960131 A 2530 25806531 ELECT RECEPTACLE AIRBUS 320 A320211 3930320 EU GALLEY HOT CUP SHORTED W O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 CA (CAN)HOT CUPS AT REAR GALLEY POSITION 527 AND 528 SPARKED AND POPPED CIRCUIT BREAKER. SHORTED RECEPTACLES REPLACED. 2 L 7 2 4F RT A28NM 1996110100574 19961101 00574 WP 1996 11 1 CA960320537 1 19960201 A 3610 ENGINE DUCT DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE 13TH STAGE DUCT BROKEN W E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. J WARNING INDICATION CL CLIMB 1 CA P657726D (CAN)DURING CLIMB AT 4,000 FT RIGHT ENGINE FIRE WARNING ILLUMINATED WITH BELL AND BOTH LOOP LIGHTS ON. ENGINE SHUT DOWN, FIRE CEASED AFTER AGENT 1 DISCHARGED. MAINTENANCE INVESTIGATION REVEALED ENGINE TO P YLON 13TH STAGE DUCT FAILURE AT CL AMP CONNECTION POINT. NEW DUCT AND CLAMP INSTALLED, #1 FIRE EXTINGUISHER BOTTLE REPLACED AND ENGINE GROUND RUN CARRIED O UT. 2 L 7 2 4F 4 F A6WE E2EA 1996110100575 19961101 00575 EA 1996 11 1 CA960320538 1 19960202 A 2170 COALESCER BAG CNDAIR CL600 CL6002B19 EA CABIN AIR COND CONTAMINATED W C D ABORTED TAKEOFF RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 CA 791 (CAN)SMOKE IN CABIN DURING TAKEOFF, REJECTED TAKEOFF AT 95 KNOTS. APPARENTLY DURING DE-ICING, GLYCOL HAD BEEN SPRAYED IN TO INTAKES AND INJESTED BY AIR CONDITIONING SYSTEM.COALESCER BAGS REMOVED AND CLEANED . 2 L 7 2 4F RT A21EA 1996110100576 19961101 00576 WP 1996 11 1 CA960320539 1 19960203 A 3270 59203365 TAIL SKID DOUG DC9 DC932 3022066 WP EMPENNAGE SKID STRIKE W O OTHER O OTHER TO TAKEOFF 1 CA (CAN)TAIL STRIKE OCCURRED DURING TAKEOFF ROLL. MAINTENANCE INSPECTED TAIL SECTION AS PER MAINTENANCE ALTER 32-16 AND MAI NTENANCE MANUAL 32-70-0. TAIL SKID REPLACED. 2 L 7 2 4F A6WE 1996110100577 19961101 00577 EA 1996 11 1 CA960320544 1 19960210 A 2750 FLAP CNDAIR CL600 CL6002B19 EA FORWARD VANE ICED UP W C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 CA 1581 1581 (CAN)TAKEOFF REJECTED AT 80 KNOTS BECAUSE OF FLAP CONFIGURATION WARNING. FOUND HEAVY ICE BUILD UP IN FLAP, AT FORWARD VA NE AREA ON BOTH SIDES. 2 L 7 2 4F RT A21EA 1996110100579 19961101 00579 EA 1996 11 1 CA960320546 1 19960216 A 2920 O-RING CNDAIR CL600 CL6002B19 EA #3 HYDRAULIC FAILED W O OTHER K FLUID LOSS AP APPROACH 1 CA 1620 1620 (CAN)LOST #3 HYDRAULIC SYSTEM ON APPROACH. HIGH PRESSURE MANIFOLD FLUID SAMPLE PLUG FOUND LEAKING. O-RING REPLACED. 2 L 7 2 4F RT A21EA 1996110100580 19961101 00580 NM 1996 11 1 CA960321003 1 19960320 A 3211 102161 DRAG STRUT PIVOT DHAV DHAV DHC8 DHC8102 2809003 NM RT MLG CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 16765 (CAN)PITTING CORROSION FOUND ON RIGHT HAND MLG DRAG STRUT PIVOT PIN. 2 H 7 2 4T RT A13NM 1996110100581 19961101 00581 NM 1996 11 1 CA960321004 1 19960320 A 2730 BOLT DHAV 82760096103 DHAV DHC8 DHC8101 2809002 NM ELEVATOR LOOSE W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 23476 (CAN)INBOARD RH ELEVATOR PULLEY BRACKET LOCATED AT TOP OF STABILIZER FOUND TOP ATTACHING BOLT WITH ONE-EIGHTH INCH CLEAR ANCE UNDER HEAD OF BOLT AND NUT ONLY HALF WAY ON. LIKELY THERE SINCE MANUFACTURE. NO WEAR NOTED AND BOLT STILL SNUG IN HOLE. LOCK NUT HAS GOOD LOCKING TORQUE. 2 H 7 2 4T RT A13NM 1996110100582 19961101 00582 SO 1996 11 1 CA960321005 1 19960318 A 3233 MS28775114 O-RING OZONE OAS29233 PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2B 41532 EA NLG ACTUATOR WORN W O OTHER J K WARNING INDICATION FLUID LOSS TO TAKEOFF 1 CA RL122861 (CAN)THE CREW RETRACTED THE GEAR AND THE CYCLE FAILED TO COMPLETE, RESULTING A GEAR UNSAFE LIGHT. THE GEAR WAS SELECTED DOWN AND FELL BUT WOULD NOT LOCK. THE HAND PUMP WAS USED AND THE GEAR WAS LOCKED INTO THE DOWN POSITION. INVESTIGATION R EVEALED A LEAKING O-RING ON THE NOSE GEAR ACTUATOR RETRACT CIRCUIT. THIS ALLOWED A SMALL AMOUNT OF FLUID TO LEAK OUT ON EVERY CYCLE OF THE GEAR TO THE POINT WHERE THERE WAS INSUFFICIENT FLUID TO COMPLETE THE CYCLE. THE EMERGENCY HAND PUMP D RAWS FLUID FROM DEEPER IN THE RESERVOIR & ALLOWED THE CYCLE TO BE COMPLETED. THE ACTUATOR O-RING WAS REPLACED, RESERVOIR SERVICED AND THE GEAR CHECKED OUT OK. THE AIRCRAFT WAS RETURNED TO SERVICE. 1 L 7 2 3O 3 O A20SO E14EA 1996110100583 19961101 00583 NM 1996 11 1 CA960321007 1 19960310 A 3320 10617825 BALLAST BOEING 737 737242C 1384478 NM CABIN LIGHT BURNT W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA (CAN)AT TOP OF CLIMB FLIGHT ATTENDANT REPORTED ODOR AND FAINT SMOKE IN CABIN. AIRCRAFT RETURNED TO BLOCKS. CEILING LIG HT CB POPPED. REPLACED BURNT LIGHT BALLAST. 2 L 7 2 4F A16WE 1996110100584 19961101 00584 EU 1996 11 1 CA960321008 1 19960321 A 2130 350E5151022 CONCENTRATOR AIRBUS 320 A320211 3930320 EU SDAC NR 1 FAILED W A B UNSCHED LANDING EMER. DESCENT G J MULTIPLE FAILURE WARNING INDICATION CR CRUISE 1 CA 14196 (CAN)DURING FLIGHT, ALL ECAM WARNINGS, MASTER CAUTION, MASTER WARNING BELLS BEGAN CYCLING. PRESSURIZATION CLIMBED, EMERG ENCY DESCENT INITIATED, COULD NOT STOP CYCLING OF WARNINGS OR FAULTS. MAINTENANCE TRO UBLESHOOTING LED TO SDAC #1 FAULT. SDAC REPLACED. SUBSEQUENT REVIEW OF PILOTS REPORT INDICATES THERE MAY NOT HAVE BEEN A TRUE DEPRESSURIZATION PROBLEM AND THE EMERGENCY DESCENT WAS PERFORMED AS A PRECAUTION. AIRBUS ADVISED OF THE INCIDENT. 2 L 7 2 4F RT A28NM 1996110100586 19961101 00586 EA 1996 11 1 CA960321501 1 19960219 A 7603 THROTTLE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE LH ENG FREEZING W O OTHER O OTHER CR CRUISE 1 CA 601 808307 (CAN)LEFT THROTTLE FREEZES DURING FLIGHT. CARRIED OUT CANADAIR CRJ CONCESSION LETTER CO95-196. LUBRICATED THROTTLE TELEF LEX CABLE FROM PYLON TO AFT E & E COMPARTMENT. 2 L 7 2 4F 4 F RT A21EA E15NE 1996110100587 19961101 00587 EU 1996 11 1 CA960321502 1 19960219 A 2780 SLATS AIRBUS 320 A320211 3930320 EU WING LE SEIZED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA (CAN)PRIOR TO ARRIVAL, UNABLE TO EXTEND LEADING EDGE SLATS, LANDING ACCOMPLISHED WITHOUT SLATS. MAINTENANCE ACTION INVOL VED LUBRICATING SLAT PINIONS AND ROLLERS. SYSTEM CHECK CARRIED OUT. 2 L 7 2 4F RT A28NM 1996110100588 19961101 00588 EU 1996 11 1 CA960321503 1 19960221 A 2821 FUEL STRAINER AIRBUS 320 A320211 3930320 EU LEFT PUMPS ICE BLOCKAGE W C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CA 12938 (CAN)LEFT FUEL BOOST PUMPS (#1 & #2) FAULTED ON TAKEOFF, UNABLE TO RESET, NECESSARY TO CROSSFEED. MAINTENANCE ACTION INV OLVED INSTALLING NEW FUEL STRAINERS FOR FUEL PUMPS AS PER PRODUCTION PERMIT #2-28-20/ 351-28-74. MODIFICATION INTRODUCES NEW FUEL PUMP STRAINER WITH A LARGER MESH TO PREVENT ICE BUILD-UP. 2 L 7 2 4F RT A28NM 1996110100591 19961101 00591 EA 1996 11 1 CA960321506 1 19960222 A 3260 BRACKET CNDAIR CNDAIR CL600 CL6002B19 EA NLG PROX SENSOR BENT W O OTHER J WARNING INDICATION TO TAKEOFF 1 CA 2553 (CAN)ON DEPARTURE NOSE LANDING GEAR WOULD NOT RETRACT, WITH GEAR DISAGREE AND NOSE DOOR OPEN MESSAGE. FOUND LANDING GEAR EXTEND PROXIMITY SENSOR TARGET BRACKET BENT. BRACKET REPLACED. 2 L 7 2 4F RT A21EA 1996110100592 19961101 00592 NE 1996 11 1 CA960321509 2 19960224 A 7320 21011404 ENGINE FADEC AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE LT ENG MALFUNCTION W O OTHER P NO WARNING INDICATION LD LANDING 1 CA 731633 (CAN)DURING LANDING ROLL AT 70 KNOTS, LEFT ENGINE SHUT DOWN ON ITS OWN WITH NO ASSOCIATED FAULT. ENGINE STARTED NORMALLY AT THE GATE. MAINTENANCE ACTION INVOLVED TEST MOTORING THE FULL AUTHORITY DIGITAL EN GINE CONTROL (FADEC) AND VISUAL IN SPECTION. NO FURTHER PROBLEMS. 2 L 7 2 4F 4 F RT A28NM E29NE 1996110100593 19961101 00593 EA 1996 11 1 CA960321510 1 19960225 A 2750 FLAP CNDAIR CL600 CL6002B19 EA NR 1 & NR 2 FECU LOCKED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA 1397 (CAN)FLAP LOCKED AT 20 DEGREES ON FINAL APPROACH, WITH FLAP FAIL EICAS MESSAGE. RESET #1 AND #2 FECU CHANNELS. 2 L 7 2 4F RT A21EA 1996110100594 19961101 00594 NE 1996 11 1 CALA9601524 2 19961028 A 7260 GEARBOX BOEING 727 727243 138408D NM PWA JT8 JT8D9 52048 NE NR 3 ENGINE FAILED A CALA A E UNSCHED LANDING ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 09 17407 56534 12122 21270 666799 THE NR 3 ENGINE OIL TEMPERATURE BEGAN TO RISE SHORTLY AFTER TAKEOFF. THE OIL TEMPERATURE RED LINED APPROXIMATELY 13 MIN UTES AFTER TAKEOFF. THE NR 3 ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS DIVERTED TO BOS WHERE IT LANDED WITHOUT INCIDENT . THE ENGINE OIL PRESSURE WAS APPROXIMATELY 50 PSI UNTIL SHUT DOWN. MAINTENANCE FOUND THE ENGINE GEARBOX AT FAULT. TH E NR 3 ENGINE GEARBOX WAS REMOVED AND REPLACED. IN ADDITION, THE FUEL OIL COOLER WAS REPLACED. A POWER ASSURANCE RUN W AS PERFORMED AND ALL PARAMETERS WERE WITHIN LIMITS WITH NO LEAKS NOTED. 2 L 7 3 4F 4 F RT A3WE E2EA 1996110100595 19961101 00595 WP 1996 11 1 CALA9601525 1 19961028 A 2530 8101280000B OVEN DOUG DC10 DC1030 3023501 WP AFT GALLEY INOPERATIVE A CALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 68060 47850 SMOKE BEGAN TO APPEAR FROM THE TOP OF THE NR 625 AFT GALLEY OVEN WHILE INFLIGHT. THE OVEN WAS TURNED OFF AND ASSOCIATED CIRCUIT BREAKERS WERE PULLED. THE SMOKE CEASED AND THE FLIGHT WAS CONTINUED WITHOUT FURTHER PROBLEM. MAINTENANCE PLAC ARDED THE NR 625 AFT GALLEY OVEN INOPERATIVE, NO OTHER DEFECTS WERE NOTED. 2 L 7 3 4F A22WE 1996110100596 19961101 00596 WP 1996 11 1 CALA9601526 1 19961024 A 5350 D29984103 TAILCONE DOUG DC9 DC982 3022082 WP AFT FUSELAGE DEPLOYED A CALA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 09 92874 26203 855 49122 WHEN OPERATIONS ARRIVED AT AIRCRAFT THE TAILCONE WAS FOUND DEPLOYED WITH THE EMERGENCY SLIDE UNRAVELED, BUT NOT INFLATED . MAINTENANCE FOUND THE TAILCONE CRACKED AND THE EVACUATION SLIDE DEPLOYMENT LANYARD CLEVIS END BROKEN. A NEW LANYARD WAS INSTALLED IAW MM 25-62-01. THE EVACUATION SLIDE WAS REMOVED AND REPLACED IAW MM 25-02-01 AND THE TAILCONE WAS REMOV ED AND REPLACED IAW MM 53-53-00, BLOCK 401. IN ADDITION, THE TAILCONE RELEASE CABLE WAS REPLACED DUE TO FRAYING. AN AD JUSTMENT/TEST OF THE TAILCONE RELEASE SYSTEM WAS PERFORMED IAW MM 53-53-00 AND OPERATION CHECKED GOOD. 2 L 7 2 4F A6WE 1996110100597 19961101 00597 NM 1996 11 1 CALA9601527 1 19961027 A 2530 72067002 OVEN BOEING 737 737524 1384721 NM GALLEY CONTAMINATED A CALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 18611 27324 THE FLIGHT ATTENDANT REPORTED SMOKE COMING FROM THE NR 2 OVEN IN FIRST CLASS GALLEY WHILE INFLIGHT. THE OVEN CIRCUITS W ERE DEACTIVATED AND THE SMOKE CEASED. THE FLIGHT WAS CONTINUED WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND COOKING GREA SE IN THE NR 2 FIRST CLASS GALLEY OVEN. THE GREASE WAS REMOVED AND OVEN OPERATION CHECKED GOOD WITH NO SMOKE NOTED. NO OTHER DISCREPANCIES WERE FOUND. 2 L 7 2 4F RT A16WE 1996110100598 19961101 00598 WP 1996 11 1 9622519614 1 19960930 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 851 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 614NW 47128 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND ATTACH FITTING ON FUSELAGE FRAME EXFOLIATED AT BS 851 BETWEEN LONGER ONS 28R TO 27R. FABRICATED NEW ATTACH FITTING AND INSTALLED IN FRAME 851 BETWEEN LONGERONS 28R TO 27R PER SRM 53-10-02 AND 53-10-05. 2 L 7 2 4F A6WE 1996110100599 19961101 00599 WP 1996 11 1 9622529981 1 19961009 A 5330 SKIN DOUG DC9 DC931 3022065 WP PAX DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 994Z 47097 DURING M-CHECK, FOUND A CRACK IN THE FORWARD ENTRY DOOR AFT SIDE AT THE 4TH STOP. REPAIRED SKIN PER EA 99-111030. 2 L 7 2 4F A6WE 1996110100600 19961101 00600 WP 1996 11 1 9622539981 1 19961009 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 617 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 994Z 47097 DURING M-CHECK, FOUND A CRACK IN THE FS 617 FRAME AT THE LEFT SIDE FLOOR BEAM LUG. REPAIRED BEAM (PSE 53.09.015) PER EA 99-11039. 2 L 7 2 4F A6WE 1996110100601 19961101 00601 WP 1996 11 1 9622549960 1 19961011 A 5314 KEEL BEAM WEB DOUG DC9 DC931 3022065 WP BS 622 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 920RW 47163 DURING H-CHECK, FOUND CORROSION ON THE LEFT KEEL WEB AT FS 622. REPLACED WEB (P/N 9910164-191) PER EA 99-111718. 2 L 7 2 4F A6WE 1996110100602 19961101 00602 WP 1996 11 1 9622559854 1 19961014 A 5312 BULKHEAD PANEL DOUG DC9 DC951 3022051 WP BS 83 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 763NC 47716 DURING H-CHECK, FOUND A CRACK IN THE HORIZONTAL PRESSURE PANEL AT FS 83, LEFT SIDE. REPAIRED PANEL (P/N 9910073-3) PER EA 98-11708. 2 L 7 2 4F A6WE 1996110100603 19961101 00603 WP 1996 11 1 9622561227 1 19961016 A 5312 BULKHEAD DOUG DC10 DC1030 3023501 WP BS 1521 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 227NW 46969 DURING T-CHECK, FOUND CORROSION ON THE FORWARD SIDE OF THE FS 1521 CENTER LANDING GEAR WHEEL WELL BULKHEAD FROM LBL 12 T O RBL 12, 18 INCHES ABOVE THE SHELF. REPAIRED THE BULKHEAD PER EA 12-110282. 2 L 7 3 4F A22WE 1996110100604 19961101 00604 WP 1996 11 1 9622579963 1 19961019 A 5320 JAMB DOUBLER DOUG DC9 DC931 3022065 WP VENTRAL DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 913RW 47171 DURING M-CHECK, FOUND A CRACK IN THE AFT VENTRAL DOOR JAMB UPPER LEFT CORNER -13 DOUBLER. REPAIRED DOUBLER PER EA 99-11 1047. 2 L 7 2 4F A6WE 1996110100605 19961101 00605 WP 1996 11 1 9622589851 1 19961021 A 5320 FITTING DOUG DC9 DC951 3022051 WP PAX DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 760NC 47708 DURING M-CHECK, FOUND CRACKS IN THE AFT ENTRY DOOR RIGHT SIDE UPPER AND LOWER STOP FITTINGS. REPLACED FITTINGS PER SRM 51-30-0. 2 L 7 2 4F A6WE 1996110100606 19961101 00606 WP 1996 11 1 96225999779 1 19961022 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 157-180 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9341 473190 DURING M-CHECK, FOUND A CRACK IN THE LONGERON 30 END FITTING BETWEEN FS 157 TO 180. REPLACED FITTING PER SRM 53-02, 53- 30-4. 2 L 7 2 4F A6WE 1996110100607 19961101 00607 WP 1996 11 1 9622629618 1 19961023 A 5754 FITTING DOUG DC9 DC932 3022066 WP NR 1 LE FLAP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 618NW 47433 DURING M-CHECK, FOUND CORROSION ON THE LEFT WING NR 1 SLAT OUTBOARD END FITTING. REPLACED FITTING PER SRM 51-30-2. 2 L 7 2 4F A6WE 1996110100608 19961101 00608 WP 1996 11 1 9622769960 1 19961007 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 169 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 920RW 47163 DURING H-CHECK, FOUND A CRACK IN THE FUSELAGE SKIN AT FS 169 JUST BELOW LONGERON 5R. REPAIRED SKIN (P/N 5921376-1) PER EA 99-111726. 2 L 7 2 4F A6WE 1996110100609 19961101 00609 WP 1996 11 1 9622779852 1 19961014 A 5320 BEAM DOUG DC9 DC951 3022051 WP BS 47 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 761NC 47709 DURING H-CHECK, FOUND CRACKS IN THE FS 47 NOSE LANDING GEAR DOOR CUTOUT BEAMS AT THE LEFT AND RIGHT SIDES. REPAIRED BEA MS (P/N 9910088-107, -108) PER EA 98-111722. 2 L 7 2 4F A6WE 1996110100610 19961101 00610 WP 1996 11 1 9622789852 1 19961017 A 5320 SUPPORT DOUG DC9 DC951 3022051 WP BS 237-256 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 761NC 47709 DURING H-CHECK, FOUND CORROSION IN THE CENTER LINE FLOOR SUPPORT FROM FS 237 TO 256. REPAIRED SUPPORT (P/N 5910760-11) PER EA 98-111738. 2 L 7 2 4F A6WE 1996110100611 19961101 00611 WP 1996 11 1 9622799974 1 19961024 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 218-237 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9338 47347 DURING H-CHECK, FOUND CORROSION ON LONGERON 29R AND ON ITS END FITTING FS 218 TO 237. REPLACED THE FITTING (P/N 4912261 -1) AND REPAIRED THE LONGERON (P/N 2777922-3) PER SRM 51-30-2. 2 L 7 2 4F A6WE 1996110100612 19961101 00612 WP 1996 11 1 9622809753 1 19961024 A 5320 FITTING DOUG DC9 DC941 302207N WP GALLEY DOOR CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 753NW 47117 DURING H-CHECK, FOUND CORROSION ON THE FRAME ATTACH FITTING AT THE LOWER FORWARD CORNER OF THE GALLEY SERVICE DOOR. REP LACED FITTING PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996110100613 19961101 00613 WP 1996 11 1 9622609884 1 19961020 A 5350 RELEASE MECH DOUG DC9 DC951 3022051 WP TAILCONE INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 677MC 47756 DURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE TAILCONE. FOUND THE LOWER CABLE INNER SLEEVE LODGED IN THE CONDUIT. REMOVED THE SLEEVE, CHECKED OK. 2 L 7 2 4F A6WE 1996110100614 19961101 00614 NM 1996 11 1 9622616626 1 19961023 A 3350 BATTERY BOEING 747 747251B 1384892 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 626US 21708 DURING LINE CHECK, FOUND A-ZONE FLOOR PATH AND STAIR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996110100615 19961101 00615 EU 1996 11 1 9622633203 1 19961023 A 3350 321454 POWER SUPPLY AIRBUS 320 A320211 3930320 EU CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 303US 13680 8731 34 DURING LINE MAINTENANCE, THE LEFT AFT EPSU FAULTED THE BATTERY INTERNAL AND EXTERNAL LOADS. REPLACED POWER SUPPLY, OPER ATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996110100616 19961101 00616 WP 1996 11 1 9622649605 1 19961021 A 3231 59151695505 LATCH ASSY DOUG DC9 DC932 3022066 WP LT MLG DOOR FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 605NW 1430 1430 47223 LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDE NT. MAITNENANCE REPLACED LEFT MAIN GEAR DOOR UPLATCH ASSEMBLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996110100617 19961101 00617 1996 11 1 9622652298 4 19961016 A 3442 20704100101 TR UNIT BOEING 727 727251 138408H NM FWD E/E BAY FAILED A NWAA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 01 298US 27953 690 22152 DURING CRUISE FLIGHT, WEATHER RADAR FAILED TO PAINT WEATHER. AIRCRAFT DIVERTED TO DLH AND LANDED WITHOUT INCIDENT. REP LACED TRANSCEIVER AND GROUND TESTED RADAR, OPERATIONAL GROUND CHECK OK. 2 L 7 3 4F A3WE 1996110100618 19961101 00618 NM 1996 11 1 9622662298 1 19961022 A 2780 SWITCH BOEING 727 727251 138408H NM NR 1 LE FLAP FAILED A NWAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 01 298US 22152 ON APPROACH, NR 1 LEADING EDGE SLAT DID NOT EXTEND. AIRCRAFT DIVERTED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED NR 1 LEADING EDGE SLAT SWITCH, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996110100619 19961101 00619 WP 1996 11 1 9622679949 1 19961021 A 3350 FUSE DOUG DC9 DC931 3022065 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8928E 45865 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BLOWN FUSE, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996110100620 19961101 00620 1996 11 1 9622689957 4 19961021 A 2565 113317 SLIDE DOUG DC9 DC931 3022065 WP CABIN DOOR FAILED INSP A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 915RW 7424 7424 47139 DURING PERIODIC CHECK, MAIN CABIN DOOR EVACUATION SLIDE FAILED INSPECTION. REPLACED SLIDE. 2 L 7 2 4F A6WE 1996110100621 19961101 00621 WP 1996 11 1 9622699612 1 19961021 A 3350 6011779 BATTERY PACK DOUG DC9 DC932 3022066 WP LT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 612NW 47436 DURING LINE MAINTENANCE INSPECITON, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996110100622 19961101 00622 WP 1996 11 1 9622709975 1 19961021 A 2780 T-DUCTS DOUG DC9 DC931 3022065 WP LT FLAPS BINDING A NWAA O OTHER J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 GL 01 9339 47382 DURING APPROACH, SLAT DISAGREEMENT LIGHT ILLUMINATED ON SLAT EXTENSION. AIRCRAFT EXPERIENCED A NOTICABLE ROLL TO THE LE FT. COCKPIT OPERATED MANUAL PROCEDURES WERE FOLLOWED AND AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE CLEANED SL AT T-DUCTS, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996110100623 19961101 00623 WP 1996 11 1 9622719972 1 19961022 A 3010 COUPLING DOUG DC9 DC931 3022065 WP RT WING T-DUCT LOOSE A NWAA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 GL 01 9336 47338 EN ROUTE, AIRFOIL ICE PROTECTION PRESSURE ABNORMAL LIGHT ILLUMINATED WITH WING ANTI-ICE ACTIVATED. FLIGHT DIVERTED TO D TW AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND RIGHT T-DUCT COUPLING LOOSE AND LEAKING AIR. TIGHTENED COUPLING, OPE RATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996110100624 19961101 00624 WP 1996 11 1 9622729941 1 19961021 A 3260 DOWNLOCK SW DOUG DC9 DC932 3022066 WP NLG MALFUNCTIONED A NWAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 01 3324L 47103 DURING APPROACH, NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS EXTENDED. CREW EXECUTED GO-AROUND PROCEDURES AND RECYCLED GEAR FOUR TIMES. NORMAL INDICATIONS WERE ACHIEVED ON FOURTH ATTEMPT. AIRCRAFT LANDED WITHOUT INCIDENT. M AINTENANCE RECYCLED NOSE GEAR SEVERAL TIMES WITH NO PROBLEMS FOUND. REPLACED NOSE GEAR DOWNLOCK SWITCH AS A PRECAUTION. 2 L 7 2 4F A6WE 1996110100625 19961101 00625 WP 1996 11 1 9622739972 1 19961024 A 3350 60030451 POWER SUPPLY DOUG DC9 DC931 3022065 WP TAILCONE MALFUNCTIONED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9336 47338 DURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHE CK NORMAL. 2 L 7 2 4F A6WE 1996110100626 19961101 00626 WP 1996 11 1 9622749970 1 19961024 A 3350 60030451 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9334 47247 DURING LINE MAINTENANCE, FOUND AFT OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996110100627 19961101 00627 WP 1996 11 1 9622759970 1 19961024 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9334 47247 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY FLASHLIGHT BY AFT FLIGHT ATTENDANT SEAT INOPERATIVE. REPLACED BATTE RY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996110100628 19961101 00628 WP 1996 11 1 9622819883 1 19961022 A 3010 AUGMENTATION VLV DOUG DC9 DC951 3022051 WP RIGHT MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 671MC 47660 DURING CLIMBOUT, THE RIGHT ICE PROTECTION TEMPERATURE HIGH LIGHT ILLUMINATED. FOLLOWED COM PROCEDURES AND LIGHT WENT OU T. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT AUGMENTATION VALVE AND ICE PROTECTION REGULA TOR VALVE, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996110100629 19961101 00629 WP 1996 11 1 9622829754 1 19961022 A 3350 BATTERY PACK DOUG DC9 DC941 302207N WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 754NW 47178 DURING LINE CHECK, FOUND LEFT FORWARD AND RIGHT REAR OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS , OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996110100630 19961101 00630 WP 1996 11 1 9622839150 1 19961020 A 3350 BATTERY PACK DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8908E 45749 DURING LINE CHECK, FOUND CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED FORWARD OVERHEAD BATTERY PACK AND POWER SUPPLY, O PERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996110100631 19961101 00631 WP 1996 11 1 9622849867 1 19961019 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 760NC 47708 DURING LINE CHECK, FOUND EMERGENCY FLOOR PATH LIGHTING BETWEEN ROWS 9 AND 15 VERY DIM. REPLACED POWER SUPPLY AND BATTER Y, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996110100632 19961101 00632 WP 1996 11 1 9622859872 1 19961024 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 781NC 48121 DURING LINE CHECK, FOUND AISLE EMERGENCY LIGHTS INOPERATIVE BETWEEN ROWS 21 AND 25. REPLACED BOTH BATTERY CELLS, OPERAT IONAL CHECK OK. 2 L 7 2 4F A6WE 1996110100633 19961101 00633 WP 1996 11 1 9622869102 1 19961024 A 3260 DOWNLOCK SW DOUG DC9 DC915 3022036 WP NLG MALFUNCTIONED A NWAA O OTHER N FALSE WARNING DE DESCENT 1 GL 01 92S 47064 ON APPROACH, NOSE GEAR UNSAFE LIGHT ILLUMINATED ON GEAR EXTENSION. RECYCLED GEAR AND ALL INDICATIONS WERE NORMAL. FLIG HT LANDED WITHOUT INCIDENT. MAINTENANCE CYCLED GEAR SEVERAL TIMES BUT COULD NOT DUPLICATE PROBLEM. REPLACED DOWNLOCK S WITCH, GEAR OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996110100634 19961101 00634 EU 1996 11 1 9622873218 1 19961025 A 4920 38002783 APU AIRBUS 320 A320211 3930320 EU TAIL FAILED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 318US 11684 6822 206 SHORTLY AFTER TAKEOFF, STRONG OIL FUMES WERE DETECTED THROUGHOUT THE AIRCRAFT. AIRCRAFT RETURNED TO MSP. GROUND MAINT ENANCE FOUND OIL IN THE APU DUCTS. THE APU WAS REPLACED. 2 L 7 2 4F RT A28NM 1996110100635 19961101 00635 NM 1996 11 1 9622882703 1 19961027 A 2170 COALESCER BAG BOEING 727 727225 1384077 NM CABIN DIRTY A NWAA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 GL 01 8878Z 21451 DURING FLIGHT, THE CABIN ALTITUDE INCREASED TO 13,000 FEET. THERE WAS NO RESPONSE SWITCHING TO MANUAL/STANDBY ON THE AU TO PRESSURIZATION CONTROLLER. DIVERTED TO ATL WITHOUT FURTHER INCIDENT. FOUND THAT THE RIGHT PACK WATER SEPARATOR SOCK WAS DIRTY. REPLACED SOCK, PRESSURIZED AIRCRAFT SEVERAL TIMES WITH THE RIGHT PACK AND OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996110100636 19961101 00636 NM 1996 11 1 9622896307 1 19961024 A 5730 PANEL BOEING 747 747451 1384940 NM LT WING SEPARATED A NWAA A J UNSCHED LANDING DUMP FUEL D INFLIGHT SEPARATION CL CLIMB 1 GL 01 667US 24222 JUST AFTER TAKEOFF, THE UPPER OUTBOARD NACELLE ACCESS PANEL ABOVE THE NR 1 ENGINE SEPARATED 521 FT. NO CONTROL PROBLEMS WERE NOTED. DUMPED 213,000 LBS OF FUEL AND DIVERTED TO MSP WITHOUT FURTHER INCIDENT. REPLACED PANEL (P/N 65814964-39) . 2 L 7 4 4F RT A20WE 1996110100637 19961101 00637 NE 1996 11 1 9622909606 2 19961027 A 7321 7436024 FUEL CONTROL DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7 52053 NE RT ENGINE OUT OF ADJUST A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 01 606NW 4950 47225 653943 WHEN APPLYING POWER FOR TAKEOFF, THE RIGHT ENGINE WOULD NOT REACH TAKEOFF POWER. CREW ABORTED TAKEOFF AND RETURNED TO G ATE. MAINTENANCE TRIMMED THE RIGHT ENGINE, LEAK AND OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F A6WE E2EA 1996110100638 19961101 00638 EA 1996 11 1 COMA9660187 1 19961024 A 3210 171441 ATTACH PIN MESSIER CNDAIR CL600 CL6002B19 EA MLG CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 959CA 7116 FOUND PIN CRACKED, APPROX 1 INCH LONG EXTENDING INBOARD OF LOCKING TAB, DURING DETAILED VISUAL INSPECTION OF SBM-DT17002 -32-10, PAR 2B(2)(C)2. LANDING GEAR PIN HAS BEEN REMOVED FROM SERVICE AND RETURNED TO MANUFACTURER. 2 L 7 2 4F RT A21EA 1996110100639 19961101 00639 1996 11 1 COMA9660188 4 19961024 A 3418 3995100207A STALL COMPUTER CNDAIR CL600 CL6002B19 EA E/ECOMPT MALFUNCTION A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 966CA 5596 7132 STALL FAIL MESSAGE ON EICAS DURING LANDING APPROACH. REPLACED THE STALL PROTECTION COMPUTER. 2 L 7 2 4F RT A21EA 1996110100640 19961101 00640 NE 1996 11 1 COMA9660189 2 19961027 A 7261 ENGINE OIL CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LEFT REQD SERVICE A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 915CA 7013 807421 LEFT ENGINE LOW OIL PRESSURE WARNING AND PRESSURE FLUCTUATIONS. SERVICED ENGINE WITH 5 .25 QUARTS OF OIL. ENGINE OIL P RESSURE RETURNED TO NORMAL. 2 L 7 2 4F 4 F RT A21EA E15NE 1996110100641 19961101 00641 EA 1996 11 1 COMA9660190 1 19961026 A 3297 17300263 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA NLG DEFECTIVE A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 912CA 7011 NLG DOES NOT RETRACT, LANDING GEAR DISAGREE MESSAGE ON EICAS. REPLACED THE NLG DOWNLOCK PROXIMITY SENSOR HARNESS. 2 L 7 2 4F RT A21EA 1996110100642 19961101 00642 EA 1996 11 1 COMA9660191 1 19961027 A 2913 PV304448 HYD PUMP CNDAIR CL600 CL6002B19 EA RT ENGINE LEAKING A COMA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 956CA 7105 NR 2 HYDRAULIC SYSTEM INDICATES ZERO QUANTITY, PRESSURE DROPPED TO 1700 PSI. REPLACED THE NR 2 HYDRAULIC SYSTEM ENGINE DRIVEN PUMP. 2 L 7 2 4F RT A21EA 1996110100643 19961101 00643 NM 1996 11 1 96FDEA01621 1 19961027 A 5320 65588902 WEB BOEING 727 727233 138408A NM BS 277 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 NR 745 013. CORROSION (C53-221-01) ON AFT SIDE OF WEB AND OUTBD CHORD STA 227 RBL 48 WL 190 - 232. REPAIRED CORROSION ON WEB AND OUTBD CHORD STA 227, RBL 48, WL 190-232 PER FEDEX EA 7-5310-31245; SRM 51-30-2, 51-40-2. 2 L 7 3 4F RT A3WE 1996110100644 19961101 00644 NM 1996 11 1 96FDEA01620 1 19961022 A 5315 65208353 FLOOR BEAM BOEING 727 727233 138408A NM BS 1070 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 NR 0186 012. CORROSION (C53-113-01(2)) ON LOWER CHORD OF FLOOR BEAM AT NUTPLATE HOLES BS 1070 LBL 41 - RBL 51 WL 200. REPAIRED LOWER CHORD OF FLOORBEAM AT NUTPLATE HOLES BS 1070, LBL 41-RBL 51, WL 200. PER FEDEX SRM 53-10-8. 2 L 7 3 4F RT A3WE 1996110100645 19961101 00645 WP 1996 11 1 MWEA435 1 19961026 A 5312 2913670IN PIN RECEPTACLE DOUG DC9 DC915 3022036 WP AFT PRESS BLKHD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300 45718 DURING C-CHECK, FOUND AFT PLUG DOOR JAMB ALIGNMENT PIN RECEPTACLE CRACKED AT 9 O'CLOCK POSITION. MTC REMOVED AND REPLAC ED RECEPTACLE IAW DOUGLAS DRAWING 5910163. 2 L 7 2 4F A6WE 1996110100646 19961101 00646 WP 1996 11 1 MWEA618 1 19961027 A 5230 SKIN DOUG DC9 DC915 3022036 WP FWD CARGO DOOR CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300 45718 DURING C-CHECK, FOUND FWD CARGO DOOR SKIN CHAFED BEYOND LIMITS FROM CARGO BARRIER DOOR. MTC INSTALLED REPAIR IAW SRM 52 -05. 2 L 7 2 4F A6WE 1996110100647 19961101 00647 1996 11 1 P5CA9600847 4 19961027 A 3444 ANTENNA BOEING 747 747122 1384872 NM RADIO ALT CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LEVEL 1 CORROSION ON CONNECTOR TO RADIO ALTIMETER ANTENNA. PILOT REPORT FIRST OFFICERS RADIO ALTIMITER CYCLES DURING FL IGHT. CLEANNED CORROSION AND OPERATIONAL CHECKED PER BOEING MAINTENANCE MANUAL 34-33-03. 2 L 7 4 4F A20WE 1996110100648 19961101 00648 NE 1996 11 1 P5CA9600848 2 19961025 A 7250 TURBINE CASE BOEING 747 747123 1384873 NM PWA JT9 JT9D7AH 52054 NE NR 2 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 662336 CRACKED S-RAIL NR 2 ENGINE, TWO PLACES 5 O'CLOCK AND 7 O'CLOCK. WELDED, STRESS RELIEVED AND FLAP PEENED PER PRATT AND W HITNEY MAINTENANCE MANUAL 72-53-01. 2 L 7 4 4F 4 F A20WE E20EA 1996110100649 19961101 00649 NM 1996 11 1 P5CA9600849 1 19961025 A 2550 65B612621 LOCK ASSY BOEING 747 747123 1384873 NM AFT CARGO BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 BROKEN PALLET LOCK AFT CARGO COMPARTMENT. REMOVED AND REPLACED LOCK ASSEMBLY PER BOEING MAINTENANCE MANUAL 25-54-00. 2 L 7 4 4F A20WE 1996110100650 19961101 00650 NE 1996 11 1 P5CA9600850 2 19961025 A 7250 S-RAIL BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE NR 4 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 662964 CRACKED S-RAIL NR 4 ENGINE AT 10 O'CLOCK POSITION. WELD REPAIRED STRESS RELIEVED AND FLAP PEENED PER PRATT AND WHITNEY MAINTENANCE MANUAL 72-53-01. 2 L 7 4 4F 4 F A20WE E20EA 1996110100651 19961101 00651 NM 1996 11 1 P5CA9600851 1 19961025 A 5245 DOOR BOEING 747 747123 1384873 NM RT PACK DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 DELAMINATED RIGHT AFT PACK SERVICE DOOR. REPAIRED PER BOEING SRM 51-40-09 AND 51-40-12. 2 L 7 4 4F A20WE 1996110100652 19961101 00652 NM 1996 11 1 P5CA9600852 1 19961027 A 2750 ROD ENDS BOEING 747 747122 1384872 NM TE FLAPS LACK OF LUBE A P5CA K NONE F FLT CONT AFFECTED DE DESCENT 1 WP 23 852FT 19757 FLAPS ARE EXTREMELY SLOW AND HARD TO MOVE, HANDLE IS SPRINGY AT FLAPS 25, 30 AND FULL UP. RIG CHECKED FLAP CONTROL CAB LES, COMPLETED TENSION CHECK, FOUND ROD ENDS BINDING ON FLAP POWER PACKAGE, CLEANED AND LUBRICATED ROD ENDS AND ALL VISA BLE CABLE RUNS AND PULLEYS OPERATIONAL CHECK GOOD PER MAINTENANCE MANUAL 27-51-00. 2 L 7 4 4F A20WE 1996110100653 19961101 00653 NM 1996 11 1 P5CA9600853 1 19961028 A 5400 65B903475 GUSSET BOEING 747 747122 1384872 NM NR 1 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 CRACKED GUSSET NACELLE STATION 180 NR 1 PYLON AS VIEWED THOUGH ACCESS PANEL 452BL. REPLACED PER BOEING SRM 51-10-01 AND POLAR MA 5430-02:01. 2 L 7 4 4F A20WE 1996110100654 19961101 00654 NM 1996 11 1 P5CA9600854 1 19961008 A 2520 LADDER STEP BOEING 747 747124 1384874 NM UPPER DECK CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 CRACK ON 4TH STEP OF UPPER DECK LADDER. REPAIRED PER BAC SRM 51-40-03. 2 L 7 4 4F A20WE 1996110100655 19961101 00655 NM 1996 11 1 P5CA9600855 1 19961028 A 5414 SKIN BOEING 747 747122 1384872 NM NR 4 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 A .25 INCH CRACK ON NR 4 ENGINE PYLON INBOARD SIDE GOING INTO SCREW ABOVE HORSE SHOE PLATE NACELLE STA 222. REPAIRED PE R BOEING SRM 54-30-03 FIG 35. 2 L 7 4 4F A20WE 1996110100656 19961101 00656 NM 1996 11 1 P5CA9600856 1 19961022 A 2810 FUEL TANK RIBS BOEING 747 747122 1384872 NM RT WING NOT SEALED A A P5CA K NONE O OTHER CR CRUISE 1 WP 23 851FT 19756 FLIGHT REPORT OF UNCOMMANDED TRANSFER OF FUEL INTO NR 4 MAIN FROM NR 4 RESERVE AND INTO NR 3 MAIN FROM NR 4 MAIN TANK. INVESTIGATION REVEALED MISSING SEALANT AT NR 4 RESERVE TANK-J NR 4 MAIN TANK RIB ABOVE NR 4 PYLON AND AT NR 3 TO NR 4 T ANK RIB ABOVE NR 3 PYLON. MODIFICATION PER SB 747-54-2159 COMPLETED 3 FLIGHTS PRIOR. REMOVED OLD SEALANT, RESEALED AND LEAK CHECKED OK PER BOEING MAINTENANCE MANUAL 28-11-00. 2 L 7 4 4F A20WE 1996110100657 19961101 00657 NM 1996 11 1 P5CA9600857 1 19961028 A 5414 SKIN BOEING 747 747122 1384872 NM NR 1 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 CRACK IN SKIN NR 1 PYLON AT NAC STA 180 WL 152, SLOT SEAL AREA. REPAIRED PER BOEING SB 54-2034 REV 4 AND POLAR MA 5430- 02:01. 2 L 7 4 4F A20WE 1996110100658 19961101 00658 WP 1996 11 1 ARWA9610003 1 19961025 A 5320 ANGLE DOUG DC8 DC863F 302198F WP BS 300-320 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND LEVEL 2 CORROSION IN ANGLE FROM STA 300 TO 320 AND L29L NR 2 PIT. REPAIRED ANGLE AND OUTER SKIN, IAW DC-8 SRM 53-2-0 FS 1B AND 53-2-1. 2 L 7 4 4F 4A25 1996110100659 19961101 00659 WP 1996 11 1 ARWA9610004 1 19961025 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 1660 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND LEVEL 1 CORROSION AND MISSING RIVETS AT STA 1660 AND L24L OF FUSELAGE. REPAIRED CORRODED AREA IAW FAA 8110-3 FORM APPROVED DRAWING CF-N661AN-05/96, DATED SEPTEMBER 17, 1996 AND DC-8 SRM 53-2-2 FIG 10 SH 1B4. 2 L 7 4 4F 4A25 1996110100660 19961101 00660 WP 1996 11 1 ARWA9610005 1 19961025 A 5320 FITTING DOUG DC8 DC863F 302198F WP BS 340 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND CRACKED FITTING AT FWD LWR CARGO NR 1 PIT RT TUNNEL STA 340. REMOVED CRACKED FITTING, FABRICATED FITTING PER DAC AUTHORIZATION DATED 09-10-96 FILE C1-P63-ATM/759. TREATED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-20D. 2 L 7 4 4F 4A25 1996110100661 19961101 00661 WP 1996 11 1 ARWA9610006 1 19961025 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 834.5 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND LEVEL 2 CORROSION ON RT SIDE UPPER PLATING OF FUSELAGE STA 834.5 AND 857.125, BETWEEN LONG 11R AND 12R. REPAIRED PLATING IAW DC-8 SRM 53-2-1 FIG 2 SH 5.1. TREATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-8, 51-1-20D A ND 51-1-17. 2 L 7 4 4F 4A25 1996110100662 19961101 00662 WP 1996 11 1 ARWA9610007 1 19961025 A 5320 97540241 FITTING DOUG DC8 DC863F 302198F WP BS 280 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND CRACKED FITTING AT FWD LWR CARGO COMPARTMENT NR 1 PIT LT TUNNEL STA 280. REMOVED CRACKED FITTING, FABRICATED FITTING PER ATTACHED DAC AUTHORIZATION DATED 09-10-96 FILE C1-P63-ATM/151. TREATED AND INSTALLED IAW DC-8 S RM 51-1-8, 51-1-20D. 2 L 7 4 4F 4A25 1996110100663 19961101 00663 WP 1996 11 1 ARWA9610008 1 19961025 A 2750 HOUSING DOUG DC8 DC863F 302198F WP TE FLAP DRUM CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND 3 INCH CRACK AND IMPROPER REPAIR AT FLAP CALBE DRUM HOUSING LOCATED IN LT MAIN WHEEL WELL. REMOVE D PREVIOUS REPAIR, FORMED AND TREATED REPAIR PARTS IAW DC-8 SRM 51-1-4, 51-1-8. INSTALLED DOUBLER IAW DC-8 SRM 53-2-0, FIG 1D SHT 3. 2 L 7 4 4F 4A25 1996110100664 19961101 00664 WP 1996 11 1 ARWA9610009 1 19961025 A 5320 3750940503 FITTING DOUG DC8 DC863F 302198F WP BS 1000 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND CRACKED L21R TO FLOORBEAM JOINT FITTING AT AFT LWR CARGO COMPARTMENT NR 3 PIT STA 1000. REMOVED A ND REPLACED FITTING AT STA 1000 L21R IAW DC-8 SRM 51-1-20D. PREVIOUSLY FABRICATED FITTING PER DAC AUTHORIZATION DATED 0 9-17-96. TILE C1-P63-ATM/154 AND TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1996110100665 19961101 00665 WP 1996 11 1 ARWA9610010 1 19961025 A 5320 3750940503 FITTING DOUG DC8 DC863F 302198F WP BS 1000 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND CRACKED FITTING AT NR 3 PIT FS 1000 AND L21L. REMOVED AND REPLACED FITTING AT STA 1000 L21L IAW D C-8 SRM 51-1-20D. PREVIOUSLY FORMED FITTING PER DAC AUTHORIZATION DATED 09-17-96 FILE C1-P63-ATM/154 AND TREATED IAW DC -8 SRM 51-1-8. 2 L 7 4 4F 4A25 1996110100666 19961101 00666 WP 1996 11 1 ARWA9610011 1 19961025 A 5312 BULKHEAD DR SILL DOUG DC8 DC863F 302198F WP BS 1540 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND LEVEL 2 CORROSION AT AFT LWR CARGO COMPARTMENT BULKHEAD DOOR SILL, STA 1540, LONG 53L. CUT CORROD ED AREA, REPAIRED IAW DC-8 SRM 53-2-0, FIG 2 SHT 4, 6 AND 7. TREATED AND INSTALLED REPAIRED PARTS IAW DC-8 SRM 51-1-8, 51-1-17, 51-1-21. 2 L 7 4 4F 4A25 1996110100667 19961101 00667 WP 1996 11 1 ARWA9610012 1 19961025 A 5320 37540252 FITTING DOUG DC8 DC863F 302198F WP BS 1220 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND CRACKED FITTING AT STA 1220 RT SIDE. REMOVED CRACKED FITTING, FABRICATED FITTING PER DAC AUTHORI ZATION DATED 09-10-96, FILE C1-P63-ATM/151. TREATED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-20D. 2 L 7 4 4F 4A25 1996110100668 19961101 00668 WP 1996 11 1 ARWA9610013 1 19961025 A 5320 36431122 FITTING DOUG DC8 DC863F 302198F WP BS 798 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND CRACKED FITTINGS AT MAIN CARGO COMPARTMENT STA 798 LONG 22R. REMOVED CRACKED FITTING, FABRICATED FITTING PER DAC AUTHORIZATION DATED 09-17-96 FILE C1-P63-ATM/154. TREATED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-20D. 2 L 7 4 4F 4A25 1996110100669 19961101 00669 WP 1996 11 1 ARWA9610014 1 19961025 A 5320 975400283 FITTING DOUG DC8 DC863F 302198F WP BS 1160 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND CORRODED JOINT FITTING AT STA 1160, SUPPORT STRUT. REMOVED CORRODED JOINT FITTING, FABRICATED FIT TING PER DAC AUTHORIZATION DATED 09-17-96 FILE C1-P63-ATM/154. TREATED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-20D. 2 L 7 4 4F 4A25 1996110100670 19961101 00670 WP 1996 11 1 ARWA9610015 1 19961025 A 5320 37540252 FITTING DOUG DC8 DC863F 302198F WP BS 340 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND CRACKED FITTING AT NR 1 PIT STA 340 L26R. REMOVED CRACKED FITTING, FABRICATED FITTING PER DAC AUT HORIZATION DATED 09-10-96 FILE C1-P63-ATM/151. TREATED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-20D. 2 L 7 4 4F 4A25 1996110100671 19961101 00671 WP 1996 11 1 ARWA9610016 1 19961025 A 5320 97540242 FITTING DOUG DC8 DC863F 302198F WP BS 1220 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND CRACKED SUPPORT STRUT AT NR 4 PIT RT SIDE STA 1220. CRACKED SUPPORT WAS REMOVED, FABRICATED PART PER DAC AUTHORIZATION DATED 09-10-96. TREATED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-20D, 51-1-21. 2 L 7 4 4F 4A25 1996110100672 19961101 00672 WP 1996 11 1 ARWA9610017 1 19961025 A 5320 3755822505N FITTING DOUG DC8 DC863F 302198F WP BS 320 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND CORRODED FITTING AT STA 320 FROM L33L TO L34L. REMOVED AND REPLACED CORRODED FITTING AT STA 320 I AW DC-8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1996110100673 19961101 00673 WP 1996 11 1 ARWA9610018 1 19961025 A 5320 47540011 FITTING DOUG DC8 DC863F 302198F WP NR 3 PIT DOOR BROKEN A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND BROKEN FITTINGS AT NR 3 PIT DOOR PROTECTOR COVER. REMOVED AND REPLACED BROKEN FITTINGS AT NR 3 PI T DOOR IAW DC-8 SRM 51-1-21. 2 L 7 4 4F 4A25 1996110100674 19961101 00674 WP 1996 11 1 ARWA9610019 1 19961025 A 5230 2644129 FITTING DOUG DC8 DC863F 302198F WP NR 4 CARGO DOOR BROKEN A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND BROKEN AND WORN FITTINGS AT NR 4 PIT DOOR. DOOR FITTINGS WERE REMOVED AND REPLACED IAW DC-8 SRM 5 1-3-0. 2 L 7 4 4F 4A25 1996110100675 19961101 00675 WP 1996 11 1 ARWA961002 1 19961025 A 5310 STRUCTURE DOUG DC8 DC863F 302198F WP BS 1090 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND LEVEL 2 CORROSION IN LT WHEEL WELL BETWEEN L33L AND L34L FS STA 1090. REPAIRED PLATING IAW FAA 81 10 FORM APPROVED DRAWING CF-N661AV 02/90 DATED 09-09-96. TREATED AND INSTALLED REPAIR PARTS IAW DC-8 SRM 51-1-8, 51-1-1 7, 51-1-21. 2 L 7 4 4F 4A25 1996110100676 19961101 00676 WP 1996 11 1 ARWA9610020 1 19961025 A 5755 3655456 FITTING DOUG DC8 DC863F 302198F WP RT NR 3 SPOILER CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND CRACKED O/B SUPPORT AT RT WING NR 3 SPOILER. REMOVED AND REPLACED FITTING AT NR 3 SPOILER OF RT W ING IAW DC-8 SRM 51-3-0. 2 L 7 4 4F 4A25 1996110100677 19961101 00677 WP 1996 11 1 ARWA9610021 1 19961025 A 5340 4641324 FITTING DOUG DC8 DC863F 302198F WP BS 1690 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND CRACKED FITTING AT MAIN CARGO COMPARTMENT STA 1690 L26L. REMOVED AND REPLACED CRACKED FITTING AT MAIN CARGO IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1996110100678 19961101 00678 WP 1996 11 1 ARWA9610022 1 19961025 A 5320 3755822505N FITTING DOUG DC8 DC863F 302198F WP BS 320 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND CORRODED FITITNG AT STA 320 FROM L33L TO L34L. REMOVED AND REPLACED CORRODED FITTING AT STA 320 I AW DC-8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1996110100679 19961101 00679 WP 1996 11 1 ARWA9610023 1 19961025 A 5320 36410041N FITTING DOUG DC8 DC863F 302198F WP BS 879 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND CRACKED AND CORRODED FITTING AT L24L STA 879. REMOVED AND REPLACED FITTING AT L24L IAW DC-8 SRM 5 1-1-20D. REMOVED CORROSION FROM SURROUNDING AREA, CLEANED AND TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1996110100680 19961101 00680 WP 1996 11 1 ARWA9610024 1 19961025 A 5230 37540211 FITTING DOUG DC8 DC863F 302198F WP NR 3 CARGO DOOR BROKEN A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND BROKEN FITTING ASSY IN UPPER T-BOLT TRUNNION OF NR 3 PIT DOOR. REMOVED AND REPLACED FITTING IN T- BOLT TRUNNION OF NR 3 PIT DOOR IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1996110100681 19961101 00681 WP 1996 11 1 ARWA9610025 1 19961025 A 5230 389406538940632 FITTING DOUG DC8 DC863F 302198F WP CARGO DOOR BROKEN A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND BROKEN AND CRACKED FITTINGS IN NR 3 PIT CROSS SLIDE CARGO DOOR JAMB FRAME. REMOVED AND REPLACED C RACKED FITTINGS IN NR 3 PIT CROSS SLIDE CARGO DOOR JAMB FRAME IAW DC-8 SRM 51-3-0. 2 L 7 4 4F 4A25 1996110100682 19961101 00682 WP 1996 11 1 ARWA9610026 1 19961025 A 5230 37558422N FITTING DOUG DC8 DC863F 302198F WP BS 1220 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND CORRODED FITTING AT DOOR JAMB FRAME STA 1220 L24L. CORRODED FITTING WAS REMOVED AND REPLACED AT D OOR JAMB FRAME IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1996110100683 19961101 00683 WP 1996 11 1 ARWA9610027 1 19961025 A 5230 37558431N21N FITTING DOUG DC8 DC863F 302198F WP BS 1220 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND CORRODED FITTINGS AT NR 3 PIT DOOR JAMB FRAME STA 1220 FROM L32L TO L35L. CORRODED FITTINGS WERE REMOVED AND REPLACED IAW DC-8 SRM 51-1-20D AT STA 1220 NR 3 PIT DOOR JAMB. 2 L 7 4 4F 4A25 1996110100684 19961101 00684 WP 1996 11 1 ARWA9610028 1 19961025 A 5320 26154871 FITTING DOUG DC8 DC863F 302198F WP BS 70 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND CORRODED FITTING AT STA 70 WEB NR 1 PIT. CORRODED FITTING WAS REMOVED, INSTALLED NEW FITTING AT S TA 70 IAW DC-8 SRM 51-3-0. 2 L 7 4 4F 4A25 1996110100685 19961101 00685 WP 1996 11 1 ARWA9610029 1 19961025 A 2830 2652518 FITTING DOUG DC8 DC863F 302198F WP RTWING FUEL DUMP CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND CORRODED FITTING AT RT WING FUEL DUMP CHUTE DOOR. CORRODED FITTING WAS REMOVED AND REPLACED AT RT FUEL DUMP CHUTE IAW DC-8 SRM 28-30-4, 20-16-0. 2 L 7 4 4F 4A25 1996110100686 19961101 00686 WP 1996 11 1 ARWA9610030 1 19961025 A 5320 36169482 FITTING DOUG DC8 DC863F 302198F WP BS 702 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND CRACKED FITTING IN LONG 21R AND 22R AT STA 702. REMOVED AND REPLACED CRACKED FITTING IN LONG 21R AND 22R AT STA 702, IAW DC-8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1996110100687 19961101 00687 WP 1996 11 1 ARWA9610031 1 19961025 A 2830 2652518 FITTING DOUG DC8 DC863F 302198F WP LTWING DUMP CHUT CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND CORRODED FITTING AT LT WING DUMP CHUTE DOOR. CORRODED FITTING WAS REMOVED AND REPLACED IAW DC-8 S RM 51-3-0. 2 L 7 4 4F 4A25 1996110100688 19961101 00688 WP 1996 11 1 ARWA9610032 1 19961025 A 5320 WEB DOUG DC8 DC863F 302198F WP LT MLG WW CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND 2 INCH CRACK IN WEB LT SIDE AT LT MAIN WHEEL WELL. REPAIRED WEB IAW DC-8 SRM 53-2-0, FIG 1B SHT 3 . TREATED AND INSTALLED DOUBLER IAW DC-8 SRM 55-1-8, 55-1-12, 51-1-20D. 2 L 7 4 4F 4A25 1996110100689 19961101 00689 WP 1996 11 1 ARWA9610033 1 19961025 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 340 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND LEVEL 2 CORROSION IN NR 1 PIT DOOR JAMB UPPER SKIN L27R STA 340. CORRODED AREA WAS CUT OUT AND RE PAIRED IAW DC-8 SRM 53-2-0, FIG 1D SHT 3. TREATED AND INSTALLED DOUBLER AND FILLER IAW DC-8 SRM 51-1-8, 51-1-17, 51-1-2 1. 2 L 7 4 4F 4A25 1996110100690 19961101 00690 WP 1996 11 1 ARWA9610034 1 19961025 A 5330 PLATING DOUG DC8 DC863F 302198F WP BS 1690 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND LEVEL 2 CORROSION IN LT WHEEL WELL BETWEEN L33L AND L34L FS 1690. REPAIRED PLATING IAW FAA 8110 F ORM APPROVED DRAWING CF-N661AV-02/96 DATED 09-04-96. TREATED AND INSTALLED REPAIR PARTS IAW DC-8 SRM 51-1-8, 51-1-17, 5 1-1-21. 2 L 7 4 4F 4A25 1996110100691 19961101 00691 WP 1996 11 1 ARWA9610047 1 19961025 A 5320 ANGLE DOUG DC8 DC863F 302198F WP BS 300-320 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND LEVEL 2 CORROSION IN ANGLE FROM STA 300 TO 320 AND L24L NR 4 PIT. REPAIRED ANGLE AND OUTER SKIN I AW DC-8 SRM 53-2-0 FIG 1B AND 53-2-1 FIG 1. INSTALLED REPAIRED PARTS IAW DC-8 SRM 51-1-8, 51-1-17, 51-1-21. 2 L 7 4 4F 4A25 1996110100692 19961101 00692 WP 1996 11 1 ARWA9610048 1 19961025 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 1660 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND LEVEL 1 CORROSION AND MISSING RIVETS AT STA 1660 AND L29L OF FUSELAGE. REPAIRED CORRODED AREA IAW FAA 8110-3 FORM APPROVED DRAWING OF CF-N661AV-05/96 DATED 09-17-96 AND DC-8 SRM 53-2-2, FIG 10 SHT 1, 3 AND 4. 2 L 7 4 4F 4A25 1996110100693 19961101 00693 WP 1996 11 1 ARWA9610049 1 19961025 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 940 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND LEVEL 2 CORROSION ON LT SIDE UPPER PLATING STA 940 BETWEEN L11L AND L13L OF FUSELAGE. REPAIRED PL ATING IAW DC-8 SRM 53-2-1 FIG 7 SH 3. BLENDED OUT AREA PER DC-8 SRM 53-2-0 FIG 1F. INSTALLED DOUBLERS IAW DC-8 SRM 51- 1-20D, 51-1-8 AND 51-1-17. 2 L 7 4 4F 4A25 1996110100694 19961101 00694 WP 1996 11 1 ARWA9610050 1 19961025 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 160 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND LEVEL 2 CORROSION IN NR 1 CARGO COMPARTMENT FRAME BETWEEN L33R AND 34R STA 160. CORRODED FRAME SE CTION WAS REMOVED, TREATED REPAIR PARTS IAW DC-8 SRM 51-1-8. INSTALLED REPAIR AT STA 160 FRAME IAW DC-8 SRM 53-2-0 FIG 2 SHTS 1, 2, 6 AND 7, 51-1-21. 2 L 7 4 4F 4A25 1996110100695 19961101 00695 WP 1996 11 1 ARWA9610051 1 19961025 A 5320 9754002207N FITTING DOUG DC8 DC863F 302198F WP BS 1220 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND CORRODED INTERCOASTAL UPPER FITTING AT NR 3 PIT DOOR STA 1220. REMOVED AND REPLACED CORRODED INTE RCOASTAL UPPER FITTING AT NR 3 PIT DOOR IAW DC-8 SRM 51-1-21 AND 51-3-0. 2 L 7 4 4F 4A25 1996110100696 19961101 00696 WP 1996 11 1 ARWA9610052 1 19961025 A 5720 5769857613CF PAN ASSY DOUG DC8 DC863F 302198F WP WS 526 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 ARROW AIR SICR 7185 PROVED PERMANENT REPAIR OF PAN CRACK AT XS 526 LT WING USING DOUGLAS SKETCH. FORMED PAN PER DAC AUT HORIZATION DATED 9-24-96, DAC DRWAING 5769857. TREATED AND INSTALLED REPAIR PARTS AT XS 526 IAW DC-8 SRM 51-1-21, 51-1- 8 AND 51-1-17. 2 L 7 4 4F 4A25 1996110100697 19961101 00697 WP 1996 11 1 ARWA9610053 1 19961025 A 2750 HOUSING DOUG DC8 DC863F 302198F WP FLAP CABLE DRUM CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND 3 INCH CRACK AND IMPROPER REPAIR AT FLAP CABLE DRUM HOUSING LOCATED IN LT MAIN WHEEL WELL. REMOVE D PREVIOUS REPAIR, FORMED AND TREATED REPAIR PARTS IAW DC-8 SRM 51-1-4. INSTALLED DOUBLER IAW DC-8 SRM 53-2-0 FIG 4D SH 3. 2 L 7 4 4F 4A25 1996110100698 19961101 00698 WP 1996 11 1 ARWA9610054 1 19961025 A 5320 97540242 FITTING DOUG DC8 DC863F 302198F WP BS 340 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 DURING C-CHECK, FOUND CRACKED FITTING AT FWD LWR CARGO NR 1 PIT RT TUNNEL STA 340. REMOVED CRACKED FITTING, FABRICATED FITTING PER DAC AUTHORIZATION DATED 09-10-96 FILE C1-P63-AT/151. TREATED AND INSTALLED IAW DC-8 SRM 51-1-8 AND 51-1-20D . 2 L 7 4 4F 4A25 1996110100699 19961101 00699 EU 1996 11 1 AALA961390 1 19960919 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 77-78 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 90070 513 TUL - FOUND CORROSION AROUND AND IN GALLEY MOUNT HOLE LEFT SIDE, SECOND FLOOR BOARD SUPPORT FROM LEFT. REPLACED FLOOR B OARD SUPPORT SECTION PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1996110100700 19961101 00700 EU 1996 11 1 AALA961392 1 19960919 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 75-76 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 90070 513 TUL - FOUND FLOOR BOARD SUPPORT IMMEDIATELY INBOARD OF L4 DOOR BETWEEN FRAME 75 AND FRAME 76 HAS HEAVY CORROSION. REMOV ED AND REPLACED FLOOR BOARD SUPPORT PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1996110100701 19961101 00701 EU 1996 11 1 AALA961286 1 19960828 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU BS 2241 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 40064 507 TUL - FOUND CORROSION ON NR 8 SEAT TRACK. INSTALLED BEAM SPLICE REPAIR BETWEEN FRAME 34 AND 36 PER SRM 53-10-16. (M) 2 L 7 2 4F RT A35EU 1996110100702 19961101 00702 EU 1996 11 1 AALA961295 1 19960829 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU BS 4587 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 40064 507 TUL - FOUND CORROSION ON CENTER FLOOR BOARD SUPPORT UNDER LAV 'U'. REPLACED FLOOR BOARD SUPPORT PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 1996110100703 19961101 00703 EU 1996 11 1 AALA961290 1 19960828 A 5321 FLOOR BOARD AIRBUS 300 A300B4605R 3930308 EU BS 4972-5043 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 40064 507 TUL - FOUND INBOARD FLOOR BOARD SUPPORT BEAM FOR G-7 GALLEY CORROSION. INSTALLED INBOARD FLOOR BOARD SUPPORT FOR G-7 GA LLEY PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 1996110100704 19961101 00704 EU 1996 11 1 AALA961296 1 19960829 A 5321 FLOOR BOARD AIRBUS 300 A300B4605R 3930308 EU BS 4551-4589 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 40064 507 TUL - FOUND CORROSION TWO PLACES AT FORWARD END OF CENTER FLOOR BOARD SUPPORT UNDER LAV. INSTALLED NEW FLOOR BOARD SUPP ORT UNDER LAV 'V' PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 1996110100705 19961101 00705 EU 1996 11 1 AAL961297 1 19960829 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU BS 2029 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 40064 507 TUL - FOUND CORROSION ON INBOARD LAV 'M' FLOOR SUPPORT. REMOVED AND REPLACED LAV 'M' FLOOR SUPPORT. REMOVED AND REPLAC ED LAV 'M' FLOOR SUPPORT FROM FRAME 31-32 PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 1996110100706 19961101 00706 EU 1996 11 1 AALA961259 1 19960826 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU BS 4740 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 40064 507 TUL - FOUND CORROSION ON FLOOR SUPPORT BEAM NR 2 INSIDE R-4 DOORWAY. INSTALLED STAINLESS STEEL STRAP PER AARD 53-20-00- 2. RESTORED SURFACE FINISH PER SRM 51-21-00. (M) 2 L 7 2 4F RT A35EU 1996110100707 19961101 00707 EU 1996 11 1 AALA961260 1 19960826 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 58 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 40064 507 TUL - FOUND FRAME SUPPORT HAS TWO AREAS OF HEAVY CORROSION AT FRAME 58 ON EITHER SIDE OF 3RD ROLLER TRAY FROM LEFT. SPL ICED IN NEW SECTION OF FRAME SUPPORT PER SRM 53-10-14. (M) 2 L 7 2 4F RT A35EU 1996110100708 19961101 00708 EU 1996 11 1 AALA961251 1 19960823 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 40064 507 TUL - FOUND CORROSION ON NR 8 SEAT TRACK FROM FRAME 30-34. REMOVED AND REPLACED NR 8 SEAT TRACK FROM FRAME NR 30 TO 34 PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 1996110100709 19961101 00709 EU 1996 11 1 AALA961145 1 19960801 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU BS 4574 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14065 508 TUL - FOUND LIGHT CORROSION ON SUPPORT WHERE LAV GOES FROM FRAME APPROX 71-73. REMOVED AND REPLACED CORRODED FLOOR SUPP ORT WITH NEW IN ACCORDANCE WITH SRM 51-72-10-0 TREATED, PAINTED AND PRIMED PER SRM 51-21-00-0. (M) 2 L 7 2 4F RT A35EU 1996110100710 19961101 00710 EU 1996 11 1 AALA961143 1 19960801 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU BS 4630-4740 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14065 508 TUL - FOUND CORROSION ON FLOOR SUPPORT UNDER LAV 'V' BETWEEN FRAME 73 TO FRAME 74. REMOVED AND REPLACED CORRODED FLOOR SUPPORT PER SRM 51-10-00-3, TREATED, PRIMED AND PAINTED PER SRM 51-21-00-0. (M) 2 L 7 2 4F RT A35EU 1996110100711 19961101 00711 WP 1996 11 1 AALA961413 1 19960925 A 5320 CUSP DOUG DC9 DC982 3022082 WP BS 188 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 295AA 49307 TUL - FOUND CORROSION ON CUSP MEMBRANE INBOARD OF ENTRY DOOR AT BS 188. DOUBLER INSTALLED SRM 53-01 PAGE 7, FIG 2. (M) 2 L 7 2 4F A6WE 1996110100712 19961101 00712 WP 1996 11 1 AALA961417 1 19960925 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1309 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 295AA 49307 TUL - FOUND CORROSION AFT LOWER BELT FRAME STATION 1309 LONGERON 29R TO 29L. CUT OUT CORROSION, INSTALLED DOUBLER PER A ARD 53-10-00-17. (M) 2 L 7 2 4F A6WE 1996110100713 19961101 00713 WP 1996 11 1 AALA961415 1 19960923 A 5320 JAMB DOUG DC9 DC982 3022082 WP CARGO DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 484AA 49677 TUL - FOUND CONSTANT AREA BEYOND LIMITS PER AARD 53-10-00-3, CONDITION 5. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-10-00 -3 AND 53-10-00-10. (M) 2 L 7 2 4F A6WE 1996110100714 19961101 00714 WP 1996 11 1 AALA961383 1 19960920 A 5320 SILL DOUG DC9 DC982 3022082 WP CARGO DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 490AA 49683 TUL - FOUND CORROSION ON CARGO DOOR LOWER SILL. REPAIRED PER ESO 80559 DATED 9-18-96. (M) 2 L 7 2 4F A6WE 1996110100715 19961101 00715 WP 1996 11 1 AALA961363 1 19960917 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP BS 1060-1222 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 482AA 49675 TUL - FOUND AFT CARGO LEFT TIE DOWN TRACK HAS CORROSION FROM STATION 1060 TO STATION 1222. REMOVED AND REPLACED AFT CAR GO LEFT TIE-DOWN TRACK FROM STATION 1001 TO 1222. (M) 2 L 7 2 4F A6WE 1996110100716 19961101 00716 NM 1996 11 1 AALA961270 1 19960823 A 5315 141N5131 FLOOR BEAM BOEING 757 757223 1384957 NM BS 405 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 656AA 24614 AFW - FOUND BLENDED GOUGE ON FLOOR BEAM IS BEYOND SRM LIMITS. (M) 2 L 7 2 4F RT A2NM 1996110100717 19961101 00717 NM 1996 11 1 AALA961271 1 19960823 A 5210 146N6201 DOOR PAN BOEING 757 757223 1384957 NM CABIN GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 656AA 24614 AFW - FOUND L4 DOOR PAN HAS GOUGE BEYOND SRM LIMITS. REPAIR PER MRB 757-921. (M) 2 L 7 2 4F RT A2NM 1996110100718 19961101 00718 NM 1996 11 1 AALA961272 1 19960823 A 5320 146N8522 SILL BOEING 757 757223 1384957 NM L2 DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 656AA 24614 AFW - AFTER REMOVING CORROSION, FOUND REMAINING MATERIAL BEYOND SRM LIMITS ON LOWER L2 DOOR SILL. REPAIR PER MRB 757-91 9. (M) 2 L 7 2 4F RT A2NM 1996110100719 19961101 00719 NM 1996 11 1 AALA961273 1 19960823 A 5312 144N2503 BLKHD STIFFENER BOEING 757 757223 1384957 NM BS 1180 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 656AA 24614 AFW - FOUND BLENDED CORROSION BEYOND SRM LIMITS ON BULKHEAD STIFFENER. REPAIR PER MRB 757-917. (M) 2 L 7 2 4F RT A2NM 1996110100720 19961101 00720 NM 1996 11 1 AALA961274 1 19960823 A 5712 113N1511 RIB BOEING 757 757223 1384957 NM BS 817 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 656AA 24614 AFW - AFTER REMOVING CORROSION, FOUND REMAINING METAL BEYOND SRM LIMITS ON RIB. REPAIR PER MRB 757-916. (M) 2 L 7 2 4F RT A2NM 1996110100721 19961101 00721 NM 1996 11 1 AALA961275 1 19960823 A 5315 141N5112 FLOOR BEAM BOEING 757 757223 1384957 NM BS 365 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 656AA 24614 AFW - BLENDED CORROSION, REMAINING METAL IS BEYOND SRM LIMITS ON FLOOR BEAM. REPAIR PER MRB 757-915. (M) 2 L 7 2 4F RT A2NM 1996110100722 19961101 00722 NM 1996 11 1 AALA961276 1 19960823 A 5315 141N5115 FLOOR BEAM BOEING 757 757223 1384957 NM BS 377 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 656AA 24614 AFW - AFTER REMOVING CORROSION, REMAINING METAL IS BEYOND SRM LIMITS ON FLOOR BEAM. REPAIR PER MRB 757-914. (M) 2 L 7 2 4F RT A2NM 1996110100723 19961101 00723 NM 1996 11 1 AALA961277 1 19960823 A 5310 141N5100 STRUCTURE BOEING 757 757223 1384957 NM BS 370 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 656AA 24614 AFW - AFTER REMOVING CORROSION, FOUND REMAINING METAL IS BEYOND SRM LIMITS. REPAIR PER MRB 757-913. (M) 2 L 7 2 4F RT A2NM 1996110100724 19961101 00724 NM 1996 11 1 AALA961298 1 19960828 A 5330 143N3340 SKIN BOEING 757 757223 1384957 NM BS 440 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 661AA 25295 AFW - FOUND FUSELAGE SKIN HAS BLEND OUT STATION 440 BELOW STRINGER 21L. PER MRB 757-925. (M) 2 L 7 2 4F RT A2NM 1996110100725 19961101 00725 WP 1996 11 1 AALA961333 1 19960906 A 5320 99365345 THRESHOLD DOUG DC9 DC982 3022082 WP BS 184 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 298AA 49310 TUL - FOUND CORROSION ON WEB AT FORWARD ENTRY DOOR THRESHOLD. CUT OUT CORRODED AREA, INSTALLED DOUBLER PER SRM 53-01 FI G 2, SHEET 3. (M) 2 L 7 2 4F A6WE 1996110100726 19961101 00726 WP 1996 11 1 AALA961332 1 19960909 A 5347 5584310 CARGO TRACK DOUG DC9 DC982 3022082 WP BS 1212-1250 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 274AA 49271 TUL - FOUND CARGO TRACK CORRODED ON TOP SIDE. REPLACED TIE DOWN. (M) 2 L 7 2 4F A6WE 1996110100727 19961101 00727 WP 1996 11 1 AALA961261 1 19960824 A 5313 STRINGER DOUG DC10 DC1010 3022110 WP BS 879 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 160AA 46710 TUL - FOUND CORROSION BETWEEN STRINGER AND FUSELAGE SKIN AT STATION 879 STRINGER 43L, FUSELAGE SKIN HAD CRACKS BETWEEN F ASTENERS. STRINGER SPLICED PER SRM 53-10-100 VOL 1. (M) 2 L 7 3 4F A22WE 1996110100728 19961101 00728 WP 1996 11 1 AALA961219 1 19960814 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1039 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 134AA 47829 TUL - FOUND CRACK .5 INCH LONG AND BULGE ON FUSELAGE SKIN LEFT SIDE. REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-20-00. (M) 2 L 7 3 4F A22WE 1996110100729 19961101 00729 WP 1996 11 1 AALA961210 1 19960813 A 5320 SHEAR TIE DOUG DC10 DC1030 3023501 WP BS 1119 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 137AA 47847 TUL - FOUND SHEAR TIE HAS SURFACE CORROSION BETWEEN STRINGER 46L AND 47L AT FRAME 1119 FORWARD AND BACK SIDE. INSTALLED SHEAR CLIP SPLICE REPAIR PER SRM 53-30-00 PG 35 FIG 10. (M) 2 L 7 3 4F A22WE 1996110100730 19961101 00730 WP 1996 11 1 AALA961249 1 19960822 A 7120 ENGINE MOUNT DOUG DC10 DC1030 3023501 WP RT ENGINE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 137AA 47847 TUL - BOLT HOLE HAS PITTS IN RIGHT PYLON FORWARD ENGINE MOUNT OUTBOARD BOLT HOLE. REWORKED BOLT HOLE PER ESO 7349 DATED 08-20-96. (M) 2 L 7 3 4F A22WE 1996110100731 19961101 00731 WP 1996 11 1 AALA961262 1 19960824 A 5320 AJC70673 ANGLE DOUG DC10 DC1030 3023501 WP BS 2007 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 137AA 47847 TUL - FOUND UPPER CAP ANGLE (TEE) CRACKED AT 2007 PRESS BULKHEAD AT ATTIC FLOOR LINE 18 INCHES INBOARD OF STRINGER 13 LE FT. REPAIRED PER ESO 7349. (M) 2 L 7 3 4F A22WE 1996110100732 19961101 00732 NM 1996 11 1 AALA961348 1 19960913 A 5330 SKIN BOEING 727 727223 1384074 NM BS 660 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 886AA 21525 TUL - FOUND FUSELAGE SKIN CORRODED 2 INCHES BY 8 INCHES STATION 660, STRINGER 28R TO 27L. CORROSION AREA CUT OUT AND IN STALLED DOUBLER PER SRM 53-30-3 FIG 3. (M) 2 L 7 3 4F A3WE 1996110100733 19961101 00733 NM 1996 11 1 AALA961349 1 19960913 A 5330 SKIN BOEING 727 727223 1384074 NM BS 680 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 886AA 21525 TUL - FOUND BUTT SPLICE CORRODED STATION 680 AT STRINGER 28R TO STRINGER 28L. CORROSION AREA CUT AND DOUBLER INSTALLED PER SRM 53-30-3 FIG 3A PG 14B. (M) 2 L 7 3 4F A3WE 1996110100734 19961101 00734 WP 1996 11 1 AALA961353 1 19960912 A 5320 JAMB DOUG DC9 DC982 3022082 WP BS 1193 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 482AA 49675 TUL - FOUND HORIZONTAL AND VERTICAL CARGO DOOR JAMB BEAM HAS CORROSION. AA REPAIR DOCUMENT 53-10-00-8. (M) 2 L 7 2 4F A6WE 1996110100735 19961101 00735 1996 11 1 AALA961326 4 19960906 A 2565 D29982125 SLIDE DOUG DC9 DC982 3022082 WP ENTRY DOOR LOW PRESSURE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 554AA 53084 TPA - DURING OVERNIGHT CHECK, FORWARD ENTRY DOOR EMERGENCY EVACUATION SLIDE BOTTLE PRESSURE NOTED OUT OF GREEN RANGE. R EPLACED FORWARD ENTRY DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996110100736 19961101 00736 NM 1996 11 1 AALA961330 1 19960907 A 2170 20D102 COALESCER DOUG MD11 MD11 3023602 NM ACM BAY DIRTY A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 1768D 48436 DFW - FLT 901 - AFTER TAKEOFF DFW DURING CLIMB-OUT, BURNING ODOR NOTED IN CABIN AND COCKPIT WITH NO VISIBLE SMOKE. AIRC RAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. CHECKED ALL AIR CYCLE MACHINES WITH NO DEFECTS NOTED. ACCOMPLISHED G ROUND ENGINE RUN TO TAKEOFF POWER WITH NO DEFECTS OR ODOR NOTED. ACCOMPLISHED PACK BURNOUT PROCEDURE AND REPLACED ALL C OALESCER BAGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1996110100737 19961101 00737 EU 1996 11 1 AALA961324 1 19960906 A 3230 715391 VALVE FOKKER F28 F28MK0100 4990807 EU NLG DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 1452B 605G 11464 DFW - FLT 556 - AFTER TAKEOFF DFW WHEN LANDING GEAR RETRACTED, RECEIVED NOSE GEAR ALERT. RECYCLED LANDING GEAR SEVERAL CYCLES AND INDICATIONS NORMAL ON EXTENSION, BUT WIND NOISE EVIDENT FROM NOSE GEAR AREA WHEN GEAR RETRACTED. EXTENDED LA NDING GEAR AND AIRCRAFT RETURNED TO DFW, LANDING WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR DOOR SELECTOR VALVE AND N OSE LANDING GEAR SEQUENCE VALVE. ACCOMPLISHED NOSE LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1996110100738 19961101 00738 EU 1996 11 1 AALA961322 1 19960905 A 2730 6227925303 SERVO FOKKER F28 F28MK0100 4990807 EU LT/RT ELEVATOR DEFECTIVE A A AALA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SW 07 1426A 1593 11411 ORD - FLT 1140 - EN ROUTE OKC/ORD DURING CRUISE AFTER AUTOPILOT 2 DISCONNECTED, BINDING FORCE NOTED IN ELEVATOR WHICH SE EMED TO GET WORSE WHEN TRIMMING THE STABILIZER. ACCOMPLISHED ABNORMAL PROCEDURE FOR JAMMED STABILIZER AND EMERGENCY DEC LARED. AIRCRAFT LANDED ORD WITHOUT INCIDENT. REPLACED LEFT AND RIGHT ELEVATOR SERVO. ADJUSTED SERVO TENSION PER MM AN D ACCOMPLISHED SERVO TEST ON AFCAS PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION. ACCOMPLISHED FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS FOUND. SYSTEM OPERATIONAL CHECKED NORMAL. (M) 2 L 7 2 4F RT 1996110100739 19961101 00739 NM 1996 11 1 AALA961328 1 19960907 A 2530 OVEN BOEING 767 767323 1385205 NM GALLEY DIRTY A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 378AN 25447 BRU - FLT 88 - EN ROUTE ORD/BRU DURING CRUISE, NR 2 OVEN EMITTED SMOKE WHEN DOOR OPENED. NO OTHER ABNORMAL INDICATIONS AND AIRCRAFT PROCEEDED TO BRU, LANDING WITHOUT INCIDENT. CLEANED INTERIOR OF NR 2 OVEN. SYSTEM GROUND CHECKED NORMAL O PERATION WITH NO SMOKE NOTED. (M) 2 L 7 2 4F RT A1NM 1996110100740 19961101 00740 NM 1996 11 1 AALA960933 1 19960616 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 357AA 24038 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 27H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 27H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1996110100741 19961101 00741 NM 1996 11 1 AALA961308 1 19960903 A 3350 A3060698101 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 648AA 24606 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 9 THROUGH 16 INOPERATIVE. RESECURED LOOSE EM ERGENCY FLOOR LIGHT STRIP CONNECTOR BY PAX SEAT ROW 9. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1996110100742 19961101 00742 EU 1996 11 1 AALA961306 1 19960831 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7062A 474 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT BETWEEN PAX SEAT ROWS 20B THROUGH 24B INOPERATIVE. REPLACED EMERGEN CY FLOOR LIGHT STRIP BETWEEN PAX SEAT ROWS 20B THROUGH 24B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996110100743 19961101 00743 EU 1996 11 1 AALA961305 1 19960831 A 3350 A3060698101 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7076A 610 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT LEFT AISLE BY PAX SEAT ROWS 24AB AND 25AB AND DOOR 3 CROSS AISLE INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTOR BY PAX SEAT 24AB. SYSTEM GROUND CHECKED NORMAL OPE RATION. (M) 2 L 7 2 4F RT A35EU 1996110100744 19961101 00744 EU 1996 11 1 AALA961304 1 19960831 A 3350 A3060698101 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 14053 420 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN L3 AND R3 DOORS INOPERATIVE. REPLACED BROKEN EMERGENCY FLO OR LIGHT STRIP CONNECTOR AT L3 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996110100745 19961101 00745 WP 1996 11 1 AALA961242 1 19960819 A 3350 SWITCH COVER DOUG DC10 DC1030 3023501 WP L1 DOOR BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 144AA 47848 DFW - DURING OVERNIGHT MAINTENANCE, FOUND FORWARD FLIGHT ATTENDANT EMERGENCY LIGHT ARMING SWITCH AT THE L1 DOOR REEL HAS BROKEN SPRING. REPLACED SWITCH COVER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A22WE 1996110100746 19961101 00746 NM 1996 11 1 AALA961300 1 19960830 A 3231 69678896 OPERATING ROD BOEING 727 727227 1384078 NM NLG DOOR DEFECTIVE A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 07 717AA 20610 DFW - FLT 1503 - DURING APPROACH TO DFW WHEN LANDING GEAR EXTENDED, NOSE LANDING GEAR DID NOT EXTEND. RECYCLED LANDING GEAR AND NOSE LANDING GEAR EXTENDED NORMALLY. AIRCRAFT LANDED DFW WITHOUT INCIDENT. REPLACED AND RIGGED NOSE LANDING G EAR DOOR OPERATING ROD. ALSO, LUBRICATED NOSE LANDING GEAR. ACCOMPLISHED NOSE LANDING GEAR RETRACTION CHECK WITH NO DE FECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996110100747 19961101 00747 EU 1996 11 1 AALA961302 1 19960830 A 2433 F11QB3121 TRANSFORMER LUCAS AIRBUS 300 A300B4605R 3930308 EU E/E COMPT DEFECTIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 80084 800108 675 RDU - FLT 1169 - EN ROUTE JFK/SJU DURING CRUISE AT FL 310, SMOKE/ODOR NOTED WITHIN 15 SECONDS AFTER TURNING WEATHER RADA R ON. TURNED OFF WEATHER RADAR AND AIRCRAFT DIVETED TO RDU, LANDING WITHOUT INCIDENT. REPLACED NR 1 AND NR 2 TRANSFORM ER/RECTIFIER UNITS. ALSO PRECAUTIONARY REPLACED WEATHER RADAR R/T UNIT. ACCOMPLISHED GROUND ENGINE RUN AND OPERATED PA CKS AND BOTH TRANSFORMER/RECTIFIER UNITS WITH NO SMOKE/ODOR NOTED. SYSTEMS GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996110100748 19961101 00748 EU 1996 11 1 AALA961299 1 19960829 A 3350 A3060698101 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 33069 512 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT RIGHT AISLE BETWEEN PAX SEAT ROWS 10 HJ AND 20 HJ INOPERATIVE. R ESECURED LOOSE EMERGENCY FLOOR LIGHT STRIP CONNECTORS BETWEEN PAX SEAT ROWS 10 HJ AND 20 HJ. SYSTEM GROUND CHECKED NORM AL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996110100749 19961101 00749 NM 1996 11 1 AALA961159 1 19960804 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN BROKEN A AALA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 07 317AA 22319 ORD - FLT 381 - PRIOR TO DEPARTURE ORD, EMERGENCY EXIT LIGHTS AT PAX SEATS 11B AND 24H INOPERATIVE. PLACARDED EMERGENCY EXIT LIGHTS AT PAX SEATS 11B AND 24H AND AIRCRAFT DEPARTED ORD/SFO. SUBSEQUENTLY AT SFO. REPLACED BROKEN EMERGENCY EX IT LIGHT CONNECTORS AT PAX SEATS 11B AND 24H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1996110100750 19961101 00750 WP 1996 11 1 AALA961278 1 19960826 A 3260 R228 RELAY DOUG DC9 DC982 3022082 WP E/E COMPT DEFECTIVE A AALA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 422AA 49334 SEA - FLT 251 - DURING APPROACH TO SEAT WHEN LANDING GEAR EXTENDED, THREE RED LANDING GEAR LIGHTS REMAINED ILLUMINATED W ITH NO GREEN LIGHTS. NOSE LANDING GEAR PIN INDICATED GEAR DOWN. RECYCLED LANDING GEAR AND ALL INDICATIONS RETURNED TO NORMAL WITH THREE GREEN LIGHTS. AIRCRAFT LANDED SEAT WITHOUT INCIDENT. REPLACED LANDING GEAR INTERLOCK RELAY R2-28. A CCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996110100751 19961101 00751 WP 1996 11 1 AALA961279 1 19960826 A 2750 5935973501 ARM ASSY DOUG DC9 DC982 3022082 WP LT TE FLAP BROKEN A A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 498AA 49736 DCA - DURING OVERNIGHT CHECK, LEFT WING INBOARD FLAP ARM ASSEMBLY BROKEN. REPLACED LEFT WING INBOARD FLAP ARM ASSEMBLY. ALSO, REPLACED LEFT WING INBOARD FLAP DRIVE CYLINDER. SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996110100752 19961101 00752 WP 1996 11 1 AALA961282 1 19960828 A 3231 RETRACT MECH DOUG DC9 DC982 3022082 WP NLG DOORS OUT OF ADJUST A AALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 07 227AA 49177 LAX - FLT 1843 - AFTER TAKEOFF LAX WHEN LANDING GEAR RETRACTED, CREW NOTED VIBRATION FROM AREA OF NOSE LANDING GEAR. AI RCRAFT RETURNED TO LAX AND LANDED WITHOUT INCIDENT. AFTER GATE ARRIVAL, NOSE LANDING GEAR DOORS WERE NOTED DOWN. RESEQ UENCED NOSE LANDING GEAR DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996110100753 19961101 00753 NE 1996 11 1 AALA961301 2 19960830 A 7314 925707A3 PUMP DOUG DC10 DC1010 3022110 WP GE CF6 CF66K 30020 NE NR 2 POS DEFECTIVE A AALA E ENGINE SHUTDOWN X ENGINE FLAMEOUT DE DESCENT 1 SW 07 168AA 46938 LAX - FLT 9121 - DURING DESCENT INTO LAX AT FL 140, NR 2 ENGINE FLAMED OUT. ACCOMPLISHED SHUTDOWN OF NR 2 ENGINE AND AI RCRAFT LANDED LAX WITHOUT INCIDENT. REPLACED NR 2 ENGINE MAIN FUEL PUMP AND FUEL CONTROL. ACCOMPLISHED LEAK CHECK AND GROUND ENGINE RUN WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F 4 F A22WE E23EA 1996110100754 19961101 00754 WP 1996 11 1 AALA961280 1 19960827 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 561AA 53091 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRI P BY FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996110100755 19961101 00755 NM 1996 11 1 W8PA960149 1 19961007 A 3350 LIGHT BOEING 737 7373Q8 1384670 NM CABIN LOOSE A W8PA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 03 956WP 24299 EMERGENCY TRACK LIGHTING COMING LOOSE AT ROW 1. SECURED TRACK LIGHTING. (M) 2 L 7 2 4F RT A16WE 1996110100756 19961101 00756 NM 1996 11 1 W8PA960148 1 19961007 A 3350 SOCKET BOEING 737 7373Y0 1384671 NM CABIN DISCONNECTED A W8PA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 03 955WP 24463 EMERGENCY FLOOR TRACK LIGHTS INOP ROW 12-16. FOUND LIGHT SOCKET AT ROW 16 DISCONNECTED. RESECURED. (M) 2 L 7 2 4F RT A16WE 1996110100757 19961101 00757 NM 1996 11 1 W8PA960154 1 19961014 A 3350 LIGHTS BOEING 737 7373Y0 1384671 NM CABIN INOPERATIVE A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 955WP 24463 EMERGENCY TRACK LIGHTS NEED REPAIR, ROW 14. RESECURED TRACK LIGHTING. (M) 2 L 7 2 4F RT A16WE 1996110100758 19961101 00758 NM 1996 11 1 W8PA960155 1 19961015 A 3350 LIGHT BOEING 737 7373Y0 1384671 NM CABIN INOPERATIVE A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 955WP 24463 EMERGENCY EXIT LIGHTING INOP BETWEEN ROWS 2-6. RESEATED LIGHT WIRE. (M) 2 L 7 2 4F RT A16WE 1996110100759 19961101 00759 SW 1996 11 1 MALA965155 1 19961002 A 3260 1EN516 SWITCH SWRNGN SA227 SA227AC 8780603 SW RT MLG FAILED A MALA O OTHER N FALSE WARNING AP APPROACH 1 GL 15 424MA AC639 FLT 3467 - ON APPROACH TO DTW, THE RIGHT INTRANSIT LIGHT FAILED TO ILLUMINATE UPON GEAR EXTENSION. MAINTENANCE REPLACED THE RIGHT INBOARD DOWN POSITION SWITCH. ALL CHECKS SATISFACTORY. (M) 2 L 7 2 4T RT A8SW 1996110100760 19961101 00760 WP 1996 11 1 USAAD96140 1 19961005 A 2150 PACK DOUG DC9 DC931 3022065 WP RIGHT OVERTEMP A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 976VJ 48147 FLT 648 - MYR-CLT - ON CLIMB-OUT, RIGHT PACK OVERTEMP AND SMOKE IN CABIN. DECLARED EMERGENCY. CAPTAIN DETERMINED NO FI RE AND SMOKE DISSIPATED. CAPTAIN ELECTED TO CALL OFF EMERGENCY AND PROCEEDED TO CLT. NO ITEMS WRITTEN IN LOG BY CREW, NO MAINTENANCE ACTIONS TAKEN, NO RECURRANCE OF PROBLEM AS OF 10/17/96. (M) 2 L 7 2 4F A6WE 1996110100761 19961101 00761 WP 1996 11 1 USAAD96137 1 19961006 A 3222 STRUT DOUG DC9 DC931 3022065 WP NLG REQ'D SERVICE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 945VJ 47066 FLT 783 - CLT-ATL - AFTER TAKEOFF, FLIGHT WAS UNABLE TO RETRACT LANDING GEAR. NOSE GEAR UNSAFE LIGHT REMAINED ON. 'AUT O SPOILER DO NOT USE' LIGHT CAME ON. PRESSURIZATION BECAME UNSTABLE. FOLLOWED ABNORMAL PROCEDURES. DID NOT HELP. FLI GHT RETURNED TO CLT WITH NO FURTHER INCIDENTS. NORMAL LANDING. MAINTENANCE FOUND NOSE STRUT NOT EXTENDING FULLY. REMA INED IN GROUND MODE. COMPLETED NOSE GEAR STRUT SERVICE USING A/C ON JACKS PROCEDURE. ALSO DID FULL NOSE GEAR LUBE. SE VERAL GEAR SWINGS PERFORMED. AIRCRAFT FOUND OK FOR SERVICE. (M) 2 L 7 2 4F A6WE 1996110100762 19961101 00762 WP 1996 11 1 USAAD96138 1 19961006 A 3244 TIRE DOUG DC9 DC931 3022065 WP NR 3 MAIN BLOWN A USAA A UNSCHED LANDING D R INFLIGHT SEPARATION PARTIAL RPM/PWR LOSS CL CLIMB 1 EA 19 956VJ 47588 FLT 845 - CLT-SDF, BLEW NR 3 MAIN TIRE ON TAKEOFF. PARTS WENT INTO NR 2 ENGINE CAUSING A SURGE AND ABNORMAL INDICATION. CAPTAIN SHUT DOWN NR 2 ENGINE. CAPTAIN DECLARED AN EMERGENCY. FLIGHT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. M AINTENANCE FOUND RIGHT FLAP DAMAGE ALSO. REPLACED NR 3 AND NR 4 WHEEL ASSEMBLIES. REPLACED NR 2 ENGINE. REPLACED NR 2 FLAP ASSEMBLY. (M) 2 L 7 2 4F A6WE 1996110100763 19961101 00763 WP 1996 11 1 USAAD96139 1 19961006 A 3231 DOOR LATCH DOUG DC9 DC931 3022065 WP NLG NOT LATCHED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 920VJ 48140 FLT 1179 - TRI-CLT - ON CLIMB-OUT CREW GOT A RED NOSE WHEEL LIGHT. NO EMERGENCY DECLARED. FLIGHT RETURNED TO TRI AND L ANDED SAFELY. MAINTENANCE FOUND NOSE GEAR DOORS DID NOT CLOSE COMPLETELY. DOOR LATCHES WERE CHECKED AND OPERATED NORMA LLY. AIRCRAFT WAS RELEASED. (M) 2 L 7 2 4F A6WE 1996110100764 19961101 00764 WP 1996 11 1 USAAD96141 1 19961008 A 2130 LINE DOUG DC9 DC982 3022082 WP FLOW CNTL VLV LOOSE A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 824US 49143 FLT 1189 - LGA-PBI - AT FL 310 CABIN ALT BEGAN CLIMBING 300/400 FEET. CREW DESCENDED AND INCREASED POWER IN AN ATTEMPT TO MAINTAIN PRESS. NO HELP. FINALLY REGAINED PRESSURIZATION CONTROL AT 18,000 FEET AFTER TRYING STANDBY AND THEN MANUA L. CREW DECIDED TO DIVERT TO CLT FOR MAINTENANCE. CABIN PRESSURE REACHED 10500 FEET BUT MASKS DID NOT DEPLOY. NO EMER GENCY DECLARED. FLIGHT CONTINUED TO CLT WITHOUT FURTHER INCIDENT. MAINTENANCE TIGHTENED LINE ON THE LEFT FLOW CONTROL VLV. COMPLIED WITH TEST OF DUAL PRESSURIZATION SYSTEM. LEAK CHECK GOOD ALSO. (M) 2 L 7 2 4F A6WE 1996110100765 19961101 00765 NM 1996 11 1 USAASB96209 1 19961006 A 3350 AD20131A BATTERY PACK BOEING 737 737301 1384611 NM CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 560AU 23514 PIT - THE AFT EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE AFT BATTERY PACK. (M) 2 L 7 2 4F RT A16WE 1996110100766 19961101 00766 NM 1996 11 1 USAASB96206 1 19961006 A 2130 BACC104AD400B CLAMP BOEING 737 7373B7 1384580 NM BS 1016 LOOSE A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 528AU 24410 SFO - FL 453 - CLIMBING TO FL250, CREW COULD NOT MAINTAIN CABIN PRESSURIZATION. RIGHT PACK WAS ALREADY ON MEL. CREW DE SCENDED TO 15,000 FEET. CABIN ALTITUDE DROPPED TO 8000 FEET, BUT CREW COULD NOT CONTROL PRESSURE IN MANUAL. FLIGHT RET URNED TO SFO AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE APU AIR DUCT CLAMP LOOSE AT THE AFT PRESSURE BU LKHEAD, RECONNECTED THE DUCT AND RESECURED THE CLAMP. (M) 2 L 7 2 4F RT A16WE 1996110100767 19961101 00767 NM 1996 11 1 USAASB96207 1 19961006 A 2612 6678 FIRE LOOP BOEING 737 7373B7 1384580 NM RT ENGINE FAULTY A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 533AU 24515 LAS - FL 621 - CREW RECEIVED THE NR 2 ENGINE OVERHEAT DETECT LIGHT IMMEDIATELY AFTER TAKEOFF. LIGHT EXTINGUISHED WHEN P OWER REDUCED ON THAT ENGINE. FLIGHT RETURNED TO LAS AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE CHECKED ALL LOOPS AND WIRING AND REPLACED THE RN 2 ENGINE 'B' LOOP AS A PRECAUTION. (M) 2 L 7 2 4F RT A16WE 1996110100768 19961101 00768 NM 1996 11 1 USAA960664 1 19961004 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 1003 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 224US 21666 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 4 INCH LONG 1 INCH WIDE BS 1003 TO BS 1014 STRINGER. REMOVED DAMAGE AND FABRICATED REPAIR, REPAIRED PER SRM 53-10-2. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996110100769 19961101 00769 NM 1996 11 1 USAA960665 1 19961004 A 5311 FRAME BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 224US 47115 21666 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CRACKED FRAME .75 INCH LONG STATION 727 JUST BELOW STRINGER 13L. INSTAL LED REPAIR DOUBLERS, REPAIRED PER EA 51489. (M) 2 L 7 2 4F A16WE 1996110100770 19961101 00770 NM 1996 11 1 USAA960663 1 19961004 A 5314 KEEL BEAM BOEING 737 737201 1384454 NM BS 727 DAMAGE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 224US 47115 21666 INT - DURING Q-3 CHECK VISUAL INSPECTION FOUND THREE ACCESS PLATE MOUNTING FLANGE HOLES DAMAGED IN KEEL BEAM, RIGHT SIDE KEEL BEAM LOWER CHORD OUTBOARD FLANGE FORWARD OF BS 727. INSTALLED STRAP REPAIR PER EA, REPAIRED PER EA 41514. (M) 2 L 7 2 4F A16WE 1996110100771 19961101 00771 WP 1996 11 1 ASAA9680218 1 19961006 A 3350 SOCKET DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 53016 ANC - PRIOR TO DEPARTURE OF FLT 84, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE . SECURED LIGHT SOCKET AT ROW 3 AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996110100772 19961101 00772 WP 1996 11 1 ASAA9680217 1 19961005 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 53016 SEA - PRIOR TO DEPARTURE OF FLT 85, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE . RECONNECTED ELECTRICAL CONNECTOR AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996110100773 19961101 00773 WP 1996 11 1 ASAA9680216 1 19961004 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 954AS 49387 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996110100774 19961101 00774 WP 1996 11 1 ASAA9680215 1 19961002 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 945AS 49643 PDX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE TAILCONE AREA WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996110100775 19961101 00775 NM 1996 11 1 ASAA9610133 1 19961005 A 3350 8731002142 EXIT SIGN BOEING 737 7372X6C 1384552 NM R2 DOOR INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, THE R2 DOOR EXIT IDENTIFIER WAS FOUND TO BE INOPERATIVE. REPLACED EXIT IDENTIFIER ASSEM BLY AND IDENTIFIER OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996110100776 19961101 00776 NM 1996 11 1 AALA961356 1 19960917 A 5343 TRUNNION FITTING BOEING 727 727227 1384078 NM BS 314 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 718AA 20611 TUL - FOUND CORROSION AT 2 FASTENERS, AFT OUTBOARD END OF LEFT TRUNNION FITTING. OBTAINED ESO 11697, DATED 9-9-96, AARD AND BLENDED AREA, REMOVED CORROSION. HFEC AREA TO CONFIRM DEPTH, TREATED AND PRIMED. (M) 2 L 7 3 4F A3WE 1996110100777 19961101 00777 NM 1996 11 1 AALA961359 1 19960917 A 5532 SKIN BOEING 727 727227 1384078 NM VERT STAB CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 718AA 20611 TUL - FOUND CRACK IN SKIN RIGHT SIDE OF VERT. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 55-30-07-1 PG 3. (M) 2 L 7 3 4F A3WE 1996110100778 19961101 00778 NM 1996 11 1 AALA961424 1 19960925 A 5320 ANGLE BOEING 727 727227 1384078 NM BS 1060-1170 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 717AA 20610 TUL - FOUND LEFT CREASE ANGLE CORRODED STATION 1060 TO 1170. CUT OUT CORRODED AREA AND INSTALLED ANGLE PER SRM 51-10-1 FIG 4. (M) 2 L 7 3 4F A3WE 1996110100779 19961101 00779 NM 1996 11 1 AALA961425 1 19960625 A 5320 DOOR FRAME BOEING 727 727227 1384078 NM BS 377 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 717AA 20610 TUL - FOUND CORROSION ON FRAME 377 ABOVE FLOOR LINE, FORWARD AND AFT SIDES. REMOVED AND REPLACED LOWER SECTION OF DOOR FRAME FORWARD SIDE OF GALLEY DOOR PER SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1996110100780 19961101 00780 NM 1996 11 1 AALA961423 1 19960925 A 5720 SPLICE PLATE BOEING 727 727227 1384078 NM RT WING CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 717AA 20610 TUL - SPLICE PLATE CRACKED ABOVE NR 5 LEFT FLAP ACT. STOP DRILLED CRACKS AND INSTALLED DOUBLER PER SRM 51-40-02 R8-12. (M) 2 L 7 3 4F A3WE 1996110100781 19961101 00781 NM 1996 11 1 AALA961421 1 19960925 A 5321 FLOOR BOEING 727 727227 1384078 NM BS 1170-1176 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 717AA 20610 TUL - FOUND CORROSION ON LEFT AFT LAV FLOOR AT STATION 1170 TO STATION 1176. REMOVED CORROSION AND INSTALLED DOUBLER PE R SRM 51-40-2 PAGES 1-6. (M) 2 L 7 3 4F A3WE 1996110100782 19961101 00782 NM 1996 11 1 AALA961420 1 19960925 A 5330 SKIN BOEING 727 727227 1384078 NM BS 640 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 717AA 20610 TUL - FOUND DENT IN FUSELAGE SKIN STATION 640, STRINGER 25L. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 3. (M) 2 L 7 3 4F A3WE 1996110100783 19961101 00783 NM 1996 11 1 AALA961365 1 19960919 A 5330 SKIN BOEING 727 727223 1384074 NM BS 683 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 847AA 20988 TUL - FOUND CORROSION ON FUSELAGE SKIN UNDER LEVELING COMPOUND OUTBOARD STATION 683, STRINGER 28R. INSTALLED OUTSIDE DO UBLER PER SRM 53-30-3 PAGE 14D. (M) 2 L 7 3 4F A3WE 1996110100784 19961101 00784 NM 1996 11 1 AALA961364 1 19960919 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 540 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 847AA 20988 TUL - FOUND SHEAR TIE CORRODED FORWARD OF STATION 540 OUTBOARD OF STRINGER 26R. REPLACED SHEAR TIE AT STATION 540, OUTB OARD OF STRINGER 26R. (M) 2 L 7 3 4F A3WE 1996110100785 19961101 00785 NM 1996 11 1 AALA961366 1 19960919 A 5330 SKIN BOEING 727 727223 1384074 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 847AA 20988 TUL - FOUND CORROSION AROUND LEFT RAM AIR DOOR ACTUATOR SHAFT HOLE ON FUSELAGE SKIN AT STATION 720B INBOARD OF STRINGER 28L. INSTALLED DOUBLER REPAIR PER SRM 53-30-3 PAGE 5 THROUGH 8 AND SRM 51-20-1, PAGE 12A. (M) 2 L 7 3 4F A3WE 1996110100786 19961101 00786 NM 1996 11 1 AALA961369 1 19960919 A 5311 FRAME BOEING 727 727223 1384074 NM BS 930 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 847AA 20988 TUL - FOUND CRACK IN BELT FRAME AT STATION 930 BETWEEN STRINGER 13-12. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER SRM 53-10-4 FIG 2 PAGE 11. (M) 2 L 7 3 4F A3WE 1996110100787 19961101 00787 NM 1996 11 1 AALA961367 1 19960919 A 5315 FLOOR BEAM BOEING 727 727223 1384074 NM BS 1130 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 847AA 20988 TUL - FOUND CORROSION ON TOP OF FLOOR BEAM STATION 1130 BETWEEN RIGHT, INBOARD AND OUTBOARD SEAT TRACK. REMOVED CORROSI ON PER SRM 51-10-6, REPAIRED FLOOR BEAM PER AARD/MS/MB CHAPTER 53-10-07-1 PAGE 1-3. (M) 2 L 7 3 4F A3WE 1996110100788 19961101 00788 NM 1996 11 1 AALA961371 1 19960919 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 656.5 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 847AA 20988 TUL - 5TH STRINGER AFT TANK STATION 656.5 TOP OF THE CHORD ANGLE FOUND CRACKED. INSTALLED 'Z' ANGLE REPAIR PER SRM 57-1 0-4. (M) 2 L 7 3 4F A3WE 1996110100789 19961101 00789 NM 1996 11 1 AALA961370 1 19960919 A 5311 FRAME BOEING 727 727223 1384074 NM BS 930 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 847AA 20988 TUL - FOUND CRACK IN FRAME STATION 930R AND STRINGER 14R. STOP DRILLED CRACK AND INSTALLED DOUBLER WITH HI-LOC AND SEAL ER SRM 53-10-2 DOUBLER 7075-T6. (M) 2 L 7 3 4F A3WE 1996110100790 19961101 00790 NM 1996 11 1 AALA961372 1 19960919 A 5330 SKIN BOEING 727 727223 1384074 NM BS 460-1030 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 847AA 20988 TUL - FOUND CORROSION UNDER SKIN AT RIGHT STRINGER 14 LAP, FROM STATION 460-1030. REMOVED FASTENERS, CLEANED AND TREATE D SKIN AND INSTALLED NEW FASTENERS PER 53-30-6 FIG 1, PAGE 11. (M) 2 L 7 3 4F A3WE 1996110100791 19961101 00791 NM 1996 11 1 AALA961368 1 19960919 A 5712 STRINGER BOEING 727 727223 1384074 NM WS 656.5 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 847AA 20988 TUL - FOUND TOP WING STRINGER 9 CRACKED AT RIB ATTACHMENT. REPAIRED DAMAGE AREA PER SRM 57-10-4 FIG 2, PAGE 4. (M) 2 L 7 3 4F A3WE 1996110100792 19961101 00792 NM 1996 11 1 AALA961407 1 19960920 A 5210 146N6201 DOOR PAN BOEING 757 757223 1384957 NM R4 DOOR GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 658AA 24616 AFW - AFTER BLENDING GOUGE IN DOOR PAN REMAINING MATERIAL IS BEYOND SRM LIMITS. REPAIRED PER MRB 757-941. (M) 2 L 7 2 4F RT A2NM 1996110100793 19961101 00793 NM 1996 11 1 AALA961406 1 19960920 A 5315 141N5111 FLOOR BEAM BOEING 757 757223 1384957 NM BS 345 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 658AA 24616 AFW - AFTER REMOVING CORROSION THE REMAINING MATERIAL IS BEYOND SRM LIMITS. REPAIRED PER MRB 757-942. (M) 2 L 7 2 4F RT A2NM 1996110100794 19961101 00794 NM 1996 11 1 AALA961405 1 19960920 A 5321 141N5131 FLOOR BOEING 757 757223 1384957 NM BS 418 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 658AA 24616 AFW - AFTER BLENDING CORROSION THE REMAINING MATERIAL IS BEYOND SRM LIMITS. REPAIRED PER MRB 757-943. (M) 2 L 7 2 4F RT A2NM 1996110100795 19961101 00795 NM 1996 11 1 AALA961404 1 19960920 A 5321 141N5161 FLOOR BOEING 757 757223 1384957 NM BS 377 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 658AA 24616 AFW - AFTER BLENDING CORROSION THE REMAINING MATERIAL IS BEYOND SRM LIMITS. REPAIRED PER MRB 757-945. (M) 2 L 7 2 4F RT A2NM 1996110100796 19961101 00796 NM 1996 11 1 AALA961403 1 19960920 A 5315 141N5113 FLOOR BEAM BOEING 757 757223 1384957 NM BS 365 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 658AA 24616 AFW - AFTER BLENDING CORROSION THE REMAINING MATERIAL IS BEYOND SRM LIMITS. REPAIRED PER MRB 757-944. (M) 2 L 7 2 4F RT A2NM 1996110100797 19961101 00797 NM 1996 11 1 AALA961402 1 19960920 A 5320 141N5161 INTERCOSTAL BOEING 757 757223 1384957 NM BS 331 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 658AA 24616 AFW - AFTER BLENDING CORROSION THE REMAINING MATERIAL IS BEYOND SRM LIMITS. REPAIRED PER MRB 757948. (M) 2 L 7 2 4F RT A2NM 1996110100798 19961101 00798 NM 1996 11 1 AALA961400 1 19960920 A 5744 113N1511 HINGE RIB BOEING 757 757223 1384957 NM LT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 658AA 24616 AFW - FOUND LEFT WING AILERON ATTACH HINGE RIB WAS BLENDED TO REMOVE CORROSION, REMAINING MATERIAL IS BEYOND SRM LIMITS. REPAIRED PER MRB 757952. (M) 2 L 7 2 4F RT A2NM 1996110100799 19961101 00799 NM 1996 11 1 AALA961401 1 19960920 A 5210 146N6201 HANDLE PAN BOEING 757 757223 1384957 NM L4 DOOR GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 658AA 24616 AFW - AFTER BLENDING GOUGE ON L-4 DOOR HANDLE PAN, REMAINING MATERIAL IS BEYOND SRM LIMITS. REPAIRED PER MRB 757-950. ( M) 2 L 7 2 4F RT A2NM 1996110100800 19961101 00800 NM 1996 11 1 AALA961399 1 19960920 A 5320 146N8522 SILL BOEING 757 757223 1384957 NM BS 1385-1441 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 658AA 24616 AFW - AFTER BLENDING CORROSION AT AFT CARGO DOOR CUT OUT LOWER SILL, INNER CHORD, MATERIAL REMAINING IS BEYOND SRM LIMIT S. REPAIRED PER MRB 757-953. (M) 2 L 7 2 4F RT A2NM 1996110100801 19961101 00801 NM 1996 11 1 AALA961398 1 19960920 A 5315 146N5089 FLOOR BEAM BOEING 757 757223 1384957 NM BS 1640 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7667A 25301 AFW - FOUND SEVERAL AREAS OF CORROSION BLENDED BEYOND SRM LIMITS ON FLOOR BEAM AT STATION 1640. PER MRB 757-954. (M) 2 L 7 2 4F RT A2NM 1996110100802 19961101 00802 NM 1996 11 1 AALA961362 1 19960716 A 5315 146N5089 FLOOR BEAM BOEING 757 757223 1384957 NM BS 1640 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 664AA 25298 AFW - FOUND FLOOR BEAM WEB AT STATION 1640 AND RBL 24-75 HAS GOUGE, PER SRM 757-949. (M) 2 L 7 2 4F RT A2NM 1996110100803 19961101 00803 NM 1996 11 1 AALA961361 1 19960916 A 5315 146N5089 FLOOR BEAM BOEING 757 757223 1384957 NM BS 1640 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 664AA 25298 AFW - FOUND FLOOR BEAM AT STATION 1640 HAS CORROSION REMOVED ON UPPER SURFACES, PER MRB 757-951. (M) 2 L 7 2 4F RT A2NM 1996110100804 19961101 00804 NM 1996 11 1 AALA961347 1 19960906 A 5210 146N62015 DOOR PAN BOEING 757 757223 1384957 NM L4 DOOR GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 657AM 24615 AFW - FOUND GOUGE AT DOOR PAN IS BEYOND SRM LIMITS. REPAIRED PER MRB 757-935. (M) 2 L 7 2 4F RT A2NM 1996110100805 19961101 00805 NM 1996 11 1 AALA961346 1 19960906 A 5311 146N1015 FRAME BOEING 757 757223 1384957 NM BS 1480 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 657AM 24615 AFW - FOUND AFTER REMOVING CORROSION FROM FRAME THE REMAINING MATERIAL IS BEYOND SRM LIMITS. REPAIRED PER MRB 757-934. (M) 2 L 7 2 4F RT A2NM 1996110100806 19961101 00806 NM 1996 11 1 AALA961345 1 19960906 A 5311 146N8713 FRAME BOEING 757 757223 1384957 NM BS 1645 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 657AM 24615 AFW - AFTER REMOVING CORROSION THE REMAINING MATERIAL IS BEYOND SRM LIMITS. REPAIRED PER MRB 757-933. (M) 2 L 7 2 4F RT A2NM 1996110100807 19961101 00807 NM 1996 11 1 AALA961344 1 19960906 A 5712 113N1511 RIB BOEING 757 757223 1384957 NM LT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 657AM 24615 AFW - FOUND AFTER REMOVING CORROSION THE REMAINING MATERIAL IS BEYOND SRM LIMITS. REPAIRED PER MRB 757-932. (M) 2 L 7 2 4F RT A2NM 1996110100808 19961101 00808 NM 1996 11 1 AALA961343 1 19960906 A 5315 146N5089 FLOOR BEAM BOEING 757 757223 1384957 NM BS 1640 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 657AM 24615 AFW - AFTER REMOVING CORROSION, THE MATERIAL REMAINING IS BEYOND SRM LIMITS. REPAIRED PER MRB 757-931. (M) 2 L 7 2 4F RT A2NM 1996110100809 19961101 00809 NM 1996 11 1 AALA961342 1 19960906 A 5321 141N5160 FLOOR BOEING 757 757223 1384957 NM BS 300 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 657AM 24615 AFW - FOUND AFTER REMOVING CORROSION, THE REMAINING MATERIAL IS BEYOND SRM LIMITS. REPAIRED PER MRB 757-930. (M) 2 L 7 2 4F RT A2NM 1996110100810 19961101 00810 NM 1996 11 1 AALA961340 1 19960906 A 5321 141N5130 FLOOR BOEING 757 757223 1384957 NM BS 417 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 657AM 24615 AFW - AFTER REMOVING CORROSION, FOUND REMAINING MATERIAL IS BEYOND SRM LIMITS. REPAIRED PER MRB 757-929. (M) 2 L 7 2 4F RT A2NM 1996110100811 19961101 00811 NM 1996 11 1 AALA961338 1 19960906 A 5315 141N2932 FLOOR BEAM BOEING 757 757223 1384957 NM BS 324 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 657AM 24615 AFW - AFTER REMOVING CORROSION, FOUND THE REMAINING MATERIAL IS BEYOND SRM LIMITS. REPAIRED PER MRB 757-928. (M) 2 L 7 2 4F RT A2NM 1996110100812 19961101 00812 NM 1996 11 1 AALA961336 1 19960906 A 5315 141N5113 FLOOR BEAM BOEING 757 757223 1384957 NM BS 377 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 657AM 24615 AFW - FOUND AFTER BLENDING CORROSION, REMAINING METAL BEYOND SRM LIMITS. REPAIRED PER MRB 757-926. (M) 2 L 7 2 4F RT A2NM 1996110100813 19961101 00813 NM 1996 11 1 AALA961334 1 19960906 A 5315 141N5112 FLOOR BEAM BOEING 757 757223 1384957 NM BS 365 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 657AM 24615 AFW - FOUND AFTER REMOVING CORROSION, REMAINING METAL THICKNESS IS BEYOND SRM LIMITS. REPAIRED PER MRB 757-927. (M) 2 L 7 2 4F RT A2NM 1996110100814 19961101 00814 NM 1996 11 1 AALA961419 1 19960925 A 5330 SKIN BOEING 727 727227 1384078 NM BS 683 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 717AA 20610 TUL - FOUND DAMAGED SKIN AT BS 683. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 1. (M) 2 L 7 3 4F A3WE 1996110100815 19961101 00815 NM 1996 11 1 AALA961380 1 19960921 A 3230 RETRACT MECH BOEING 727 727223 1384074 NM NLG MALFUNCTIONED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 875AA 21387 MIA - FLT 2157 - AFTER TAKEOFF MIA WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR DID NOT RETRACT. RECYCLED LANDING GEA R WITH SAME RESULTS. EXTENDED LANDING GEAR AND ALL INDICATIONS NORMAL. AIRCRAFT RETURNED TO MIA LANDED WITHOUT INCIDEN T. ACCOMPLISHED LANDING GEAR RETRACTION AND FREE FALL CHECKS WITH NO DEFECTS FOUND. CYCLED LANDING GEAR MULTIPLE CYCLE S AND OPERATION AND ALL LIGHTS INDICATE NORMAL. UNABLE TO DUPLICATE PROBLEM AND AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1996110100816 19961101 00816 NM 1996 11 1 AALA961376 1 19960919 A 2752 240863 HYD MOTOR BOEING 727 727223 1384074 NM TE FLAPS DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 875AA 21387 MIA - FLT 1791 - AFTER TAKEOFF MIA DURING CLIMB-OUT, LOST SYSTEM A HYDRAULIC SYSTEM. MANUALLY LOWERED LANDING GEAR AND AIRCRAFT RETURNED TO MIA, LANDING WITHOUT INCIDENT. REPLACED FLAP HYDRAULIC MOTOR. PRECAUTIONARY REPLACED BOTH ENGINE DRIVE HYDRAULIC PUMPS. ACCOMPLISHED GROUND ENGINE RUN AND SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996110100817 19961101 00817 NM 1996 11 1 AALA961375 1 19960919 A 2121 215201 FAN BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 881AA 21520 DFW - FLT 942 - EN ROUTE MAI/DFW DURING CRUISE, SLIGHT SULPHUR ODOR NOTED FROM GASPER. ACCOMPLISHED ABNORMAL PROCEDURE. WHEN BUS TIE BREAKERS TO GASPER TRIPPED, ODOR DISSIPATED. AIRCRAFT PROCEEDED TO MIA AND LANDED WITHOUT INCIDENT. REP LACED GASPER FAN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996110100818 19961101 00818 1996 11 1 MALA965156 4 19961002 A 3442 071131900 RT UNIT DHAV DHC8 DHC8102 2809003 NM FWD FUSELAGE INTERNAL FAULT A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 828MA 333 FLT 2950 - EN ROUTE FROM DTW, THE WEATHER RADAR 'ANT FLT' ADVISORY LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO DTW DUE TO FORECASTED WEATHER. MAINTENANCE REPLACED THE WEATHER RADAR R/T. ALL CHECKS SATISFACTORY. (M) 2 H 7 2 4T RT A13NM 1996110100819 19961101 00819 SW 1996 11 1 MALA965157 1 19961003 A 3230 RETRACT MECH SWRNGN SA227 SA227AC 8780603 SW NLG MALFUNCTIONED A MALA O OTHER J WARNING INDICATION CR CRUISE 1 GL 15 438MA AC721B FLT 3030- EN ROUTE TO DTW, THE NOSE GEAR BEGAN TO CYCLE IN THE GEAR WELL. THE CREW CYCLED THE GEAR AND THE GEAR REMAINE D UP AND LOCKED. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCEY. ALL ROLLER AND SWITCH ADJUSTMENTS WERE FOUND TO BE SATISFACTORY. MAINTENANCE CLEANED AND LUBED THE UPLIMIT SWITCHES, UPLOCK SHAFT, FITTINGS AND LANDING GEAR. ALL CHE CKS SATISFACTORY. (M) 2 L 7 2 4T RT A8SW 1996110100820 19961101 00820 SW 1996 11 1 MALA965158 1 19961005 A 5753 SKIN SWRNGN SA227 SA227AC 8780603 SW TE FLAP CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 446MA AC693 DURNG AN INSPECTION IN MSP, MAINTENANCE FOUND A CHAF THE LEFT FLAP INBOARD TRAILING EDGE. REPAIRS WERE COMPLETED IAW FA C REPAIR MANUAL 57-90-60 REPAIR NR 1 PAGES 3-6. (M) 2 L 7 2 4T RT A8SW 1996110100821 19961101 00821 SW 1996 11 1 MALA965161 1 19961003 A 5311 FRAME SWRNGN SA227 SA227AC 8780603 SW BS 242 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 423MA AC636 DURING A BLOCK INSPECTION IN MSP, THE LEFT BELT FRAME, FS 242, WL 75.32 WAS FOUND TO BE CRACKED AT THE RELIEF RADIUS, OU TBOARD OF PANEL 403. (M) 2 L 7 2 4T RT A8SW 1996110100822 19961101 00822 SW 1996 11 1 MALA965159 1 19961003 A 5311 FRAME SWRNGN SA227 SA227AC 8780603 SW BS 317 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 423MA AC636 DURING A BLOCK INSPECTION IN MSP, THE RIGHT BELT FRAME AT FS 317 WL 75.32 WAS FOUND TO BE CRACKED AT THE RELIEF RADIUS, OUTBOARD OF PANEL 406. (M) 2 L 7 2 4T RT A8SW 1996110100823 19961101 00823 SW 1996 11 1 MALA965160 1 19961003 A 5311 FRAME SWRNGN SA227 SA227AC 8780603 SW BS 332 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 423MA AC636 DURING A BLOCK INSPECTION IN MSP, THE RIGHT BELT FRAME AT FS 332, WL 75.32 WAS FOUND TO BE CRACKED AT THE RELIEF RADIUS, OUTBOARD OF PANEL 406. (M) 2 L 7 2 4T RT A8SW 1996110100824 19961101 00824 1996 11 1 BDHA9600024 4 19960920 A 2370 89090003211 VOICE RECORDER SWRNGN SA226 SA226TC 8780404 SW FAIL TEST A BDHA K NONE L NO TEST IN INSP/MAINT 1 GL 15 329BA A01302 TC238 MSP - FLT 434 - THE COCKPIT VOICE RECORDER FAILED TO TEST. THE UNIT WAS REMOVED AND SENT TO B/D INSTRUMENTS FOR REPAIR. THIS IS THE EIGHTEENTH PREMATURE FAILURE. AVERAGE TAPE LIFE IS 415 HOURS. THE TAPE REPLACEMENT IS DUE AT 1500 HOURS WITH A 5000 HOUR OVERHAUL. ALL UNITS WERE RECEIVED BACK WITH OVERHAUL PERFORMED. (M) 2 L 7 2 4T RT A8SW 1996110100825 19961101 00825 SW 1996 11 1 BDHA9600023 1 19960909 A 7714 AG34 TACH/GENERATOR SWRNGN SA226 SA226TC 8780404 SW RT ENGINE FAILED A BDHA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 15 328BA TC253 RAP - FLT 434 - THE RIGHT ENGINE RPM WAS ERRATIC IN FLIGHT. THE PROBLEM COULD NOT BE DUPLICATED ON THE GROUND. THE TAC H GENERATOR WAS REMOVED FOR INSPECTION AND THE SHAFT WAS LOOSE FROM A WORN ROLE PIN THE BACK. THE TACH GENERATOR WAS RE PLACED AND ENGINE RUN PERFORMED. THE AIRCRAFT WAS RELEASED. (M) 2 L 7 2 4T RT A8SW 1996110100826 19961101 00826 SW 1996 11 1 BDHA9600021 1 19960906 A 7910 2765020065 OIL TANK SWRNGN SA226 SA226TC 8780404 SW LT ENGINE LEAKING A BDHA O OTHER K FLUID LOSS IN INSP/MAINT 1 GL 15 328BA TC253 MSP - FLT 434 - AFTER ENGINE SHUT DOWN THE LEFT ENGINE STARTED LEAKING OIL. INSPECTION OF THE SYSTEM FOUND THE TAB HAD BROKE OFF AND CHAFED A HOLE IN THE OIL TANK. THE OIL TANK WAS CHANGED AND THE AIRCRAFT WAS RELEASED. (M) 2 L 7 2 4T RT A8SW 1996110100827 19961101 00827 WP 1996 11 1 BDHA9600020 2 19960912 A 7310 39423041 FUEL SHUTOFF SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110U 01514 WP LT ENGINE LEAKS A BDHA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 15 328BA P7806 TC253 MSP - FLT 421 - ON ENGINE SHUT DOWN, THE LEFT ENGINE SMOKED WHEN THE PROP WAS PULLED THROUGH. INSPECTION FOUND THE FUEL SHUTOFF WAS LEAKING FUEL PAST WHEN THE VALVE WAS CLOSED. THE FUEL SHUTOFF WAS REPLACED AND THE AIRCRAFT WAS RELEASED. (M) 2 L 7 2 4T 4 T RT A8SW E4WE 1996110100828 19961101 00828 1996 11 1 BDHA9600019 4 19960913 A 6122 8210260 PROP GOVERNOR SWRNGN SA226 SA226TC 8780404 SW RT ENGINE FAILED A BDHA K NONE O OTHER IN INSP/MAINT 1 GL 15 328BA 2457748A TC253 MSP - FLT 434 - THE RIGHT ENGINE PROP GOVERNOR WAS REMOVED FOR INSPECTION DUE TO CARBON STEEL IN THE SOAP SAMPLE. SLOW BETA LIGHT PROBLEMS WERE ALSO REPORTED. METAL WAS FOUND UNDER THE SCREEN ON THE PROP GOVERNOR. THE PROP GOVERNOR WAS C HANGED AND THE OIL SYSTEM FLUSHED. THE AIRCRAFT WAS RELEASED. (M) 2 L 7 2 4T RT A8SW 1996110100829 19961101 00829 EU 1996 11 1 USAASB96208 2 19961004 A 7530 9971M56P07 VSV ACTUATOR BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU RT ENGINE LEAKING A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 373US 17673 22952 724705 DCA - FLT 2299 - CREW REPORTED SMELLING JET FUEL FUMES IN THE COCKPIT DURING FLIGHT. MAINTENANCE FOUND THE RIGHT ENGINE VSV ACTUATOR LEAKING AND REPLACED IT. (M) 2 L 7 2 4F 4 F RT A16WE E21EU 1996110100830 19961101 00830 NM 1996 11 1 USAASB96205 1 19961003 A 2131 7638101 CONTROLLER BOEING 737 737201 1384454 NM E/E COMPT FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 241US 22230 22443 CLT - FL 8026 - CAPTAIN ADVISED HE LOST AUTO AND STANDBY PRESSURIZATION. MANUAL PRESSURIZATION WAS OK. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE CABIN PRESSURE CONTROLLER. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1996110100831 19961101 00831 1996 11 1 WTAA960174 4 19960915 A 2350 COMM SYS EMB 120 EMB120RT SO COCKPIT MALFUNCTIONED A WTAA O OTHER O OTHER TO TAKEOFF 1 WP 17 120AM 120012 ACV - ON TAKEOFF NR 1 AND NR 2 COMMS REPORTED CARRIER ONLY, NO VOICE. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. M AINTENANCE RERACKED BOTH COMMS AND CLEANED MICROPHONE AND HEADSET JACKS. UNABLE TO DUPLICATE DISCREPANCY. AIRCRAFT RET URNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996110100832 19961101 00832 SO 1996 11 1 WTAA960175 1 19960919 A 7330 5905588 PRESSURE SWITCH EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE FAILED A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 17 271YV 120271 SFO - LEFT FUEL FILTER LIGHT ILLUMINATED DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE DEFFERED I NDICATING SYSTEM PER MEL 73-33-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL BY REPLACING LEFT ENGINE FUEL FILTER LIGHT SWITCH. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1996110100833 19961101 00833 EU 1996 11 1 WTAA960176 1 19961006 A 3260 622800200 UPLOCK SWITCH BAG JETSTM JETSTM3101 1500215 EU LT MLG BROKEN WIRE A WTAA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 17 428UE 806 SFO - LEFT MAIN GEAR INTRANSIT LIGHT REPORTED INTERMITTENT. AIRCRAFT FERRIED TO FAT FOR REPAIR. MAINTENANCE REPAIRED W IRE ON UPLOCK SWITCH. SYSTEM OPERATIONAL CHECK NORMAL DURING GEAR RETRACTION CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996110100834 19961101 00834 EU 1996 11 1 RAIA960937 1 19960927 A 3350 311701 BATTERY PACK BAG JETSTM JETSTM3201 1500217 EU CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 436AM 891 STL - EMERGENCY LIGHTS ARE DEAD. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACKS. (M) 2 L 7 2 4T RT A56EU 1996110100835 19961101 00835 EU 1996 11 1 RAIA960936 1 19960927 A 3060 7826892 BRUSH BLOCK AEROSP ATR72 ATR72202 8680940 EU RT ENGINE FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 722TE 11208 220 STL - FLT 7166 - RIGHT PROPELLER DE-ICE FAULTED. MAINTENANCE REPLACED THE RIGHT PROPELLER DE-ICE BRUSH BLOCK. (M) 2 H 7 2 4T RT A53EU 1996110100836 19961101 00836 EU 1996 11 1 RAIA960939 1 19960930 A 3260 DHE1148A PROX SWITCH AEROSP ATR72 ATR72202 8680940 EU NLG OUT OF ADJUST A RAIA O OTHER N FALSE WARNING LD LANDING 1 CE 03 723TE 895 283 PIA - FLT 7115 - ON FINAL, NOSE GEAR INTRANSIT LIGHT WAS CYCLING. ALL DOWN AND LOCK LIGHTS ILLUMINATED. MAINTENANCE AD JUSTED THE NOSE GEAR DOWN AND LOCK PROX SWITCH. (M) 2 H 7 2 4T RT A53EU 1996110100837 19961101 00837 EU 1996 11 1 RAIA960941 1 19960930 A 3350 ML44 BULB AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 423TE 119 STL - FLT 7240 - EMERGENCY LIGHT IN CABIN DOOR IS INOP. MAINTENANCE REPLACED THE CABIN DOOR EMERGENCY EXIT LIGHT BULB. (M) 2 H 7 2 4T RT A53EU 1996110100838 19961101 00838 EU 1996 11 1 RAIA960940 1 19960930 A 7714 AG34 TACH GENERATOR BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 341TE 5710 950 STL - FLT 7071 - RIGHT RPM INDICATOR DROPPED TO ZERO. MAINTENANCE REPLACED THE RIGHT TACH GENERATOR. (M) 2 L 7 2 4T RT A56EU 1996110100839 19961101 00839 WP 1996 11 1 RAIA961001 2 19961002 A 7310 1379305A119 FUEL HOSE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT ENGINE KINKED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 03 339TE 10597 935 COU - FLT 7028 - LEFT FUEL PRESSURE CAPTION ILLUMINATED. MAINTENANCE REPLACED THE MAIN FUEL FEED LINE AT FUEL CONTROL. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996110100840 19961101 00840 EU 1996 11 1 RAIA960935 1 19960926 A 7332 1103P0645 SWITCH BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT ENGINE INTERMITTENT A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 339TE 9707 935 P66147 SPI - FLT 7083 - LEFT FUEL LOW PRESSURE CAPTION ILLUMINATED. MAINTENANCE REPLACED THE LEFT FUEL LOW PRESS WARNING SWITC H. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996110100841 19961101 00841 EU 1996 11 1 RAIA960931 1 19960924 A 2611 72111211002 SMOKE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU CARGO COMPT FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 552HK 3335 41057 STL - FLT 7458 - POD SMOKE LIGHT ILLUMINATED. MAINTENANCE REPLACED THE POD SMOKE DETECTOR. (M) 2 L 7 2 4T RT A41NM 1996110100842 19961101 00842 NM 1996 11 1 PCAA9600304 1 19960909 A 3234 574205 SELECTOR VALVE DHAV DHC8 DHC8102 2809003 NM LANDING GEAR LEAKING A PCAA O OTHER K FLUID LOSS CR CRUISE 1 EA 13 818EX 17881 17881 235 FLT 3701 - DURING CRUISE NR 2 HYDRAULIC QTY INDICATED ZERO. HYDRAULIC PRESSURE WAS NORMAL. DURING APPROACH GEAR HAD TO BE MANUALLY EXTENDED. INSPECTED AND FOUND LANDING GEAR CONTROL SOLENOID VALVE LEAKING DUE TO TORN PACKING. REPLACED U PPER PACKING. BLED NR 2 HYDRAULIC SYSTEM. COMPLIED WITH INSPECTION OF ENGINE DRIVEN PUMP. GROUND RUN AND LEAK CHECK N ORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1996110100843 19961101 00843 NM 1996 11 1 PCAA9600309 1 19960911 A 3260 7002537 CONTL BOX DHAV DHC8 DHC8102 2809003 NM LT MLG MALFUNCTIONED A PCAA O OTHER P NO WARNING INDICATION AP APPROACH 1 EA 13 815EX 6663 321 FLT 3924 - DURING APPROACH, LEFT MAIN LANDING GEAR UNSAFE ANNUNCIATOR DID NOT ILLUMINATE DURING GEAR EXTENSION. REMOVED AND REPLACED ADVISORY LIGHT CONTROL BOX. RETRACTION AND OPERATIONAL TESTS NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1996110100845 19961101 00845 NM 1996 11 1 PCAA9600311 1 19960914 A 3260 864202 UPLOCK SWITCH DHAV DHC8 DHC8102 2809003 NM NLG FAILED A PCAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 13 825EX 4976 388 FLT 3640 - AFTER GEAR RETRACTION NOSE DOORS INDICATED OPEN. AFTER GEAR WAS CYCLED NOSE GEAR DID NOT SHOW DOWN AND LOCKE D. CREW PERFORMED ALTERNATE EXTENSION AND RETURNED TO PHL WITHOUT INCIDENT. REMOVED AND REPLACED NOSE DRAG STRUT PROXI MITY SWITCH. RETRACTION AND OPERATIONAL TESTS NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1996110100846 19961101 00846 NM 1996 11 1 AWXA960575 1 19960930 A 5330 SKIN BOEING 737 737277 1384570 NM BS 351/303 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 PAE - FLT 7824 - DURING ROUTINE MAINTENANCE CHECK, FOUND CRACKS AT FORWARD ENTRY DOOR LOWER SILL AT BS 351 AND BS 303. R EPAIRED CRACKS PER EO 53-44-01, PART IV. (M) 2 L 7 2 4F RT A16WE 1996110100847 19961101 00847 NM 1996 11 1 AWXA960574 1 19960927 A 5315 FLOOR BEAM BOEING 737 737277 1384570 NM BS 1016 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 PAE - FLT 7834 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION AT BS 1016 ON FLOOR BEAM LBL 11 UPPER SURFACE WL 208. REPAIRED IAW, TCO-PAN-96-1353-RR18110-3 AND EO 2-53-16-43. (M) 2 L 7 2 4F RT A16WE 1996110100848 19961101 00848 NM 1996 11 1 AWXA960573 1 19960926 A 5313 STRINGER BOEING 737 737277 1384570 NM BS 500 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 PAE - FLT 7824 - DURING ROUTINE MAINTENANCE CHECK, FOUND STRINGER LEFT BS 500 B PLUS 6 STRINGER 16 CRACKED. REMOVED, FA BRICATED REPAIR PARTS PER ER 2-53-13-11A AND INSTALLED. (M) 2 L 7 2 4F RT A16WE 1996110100849 19961101 00849 NM 1996 11 1 AWXA960572 1 19960923 A 5330 SKIN BOEING 737 737277 1384570 NM BS 727 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 PAE - FLT 7824 - DURING ROUTINE MAINTENANCE CHECK, FOUND CRACK AT BS 727 A PLUS 5, STRINGER 14R ALONG LOWER FASTENER ROW . CUT OUT DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-30-3, FIG 9. (M) 2 L 7 2 4F RT A16WE 1996110100850 19961101 00850 NM 1996 11 1 AWXA960571 1 19960925 A 5313 STRINGER BOEING 737 737277 1384570 NM BS 907 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 PAE - FLT 7824 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON STRINGER 26L, BS 907. REMOVED, FABRICATED AND INS TALLED PRODUCTION SPLICE AT BS 907, STRINGER 26L AND REPLACED STRINGER 26L FROM BS 910 TO 937. ALL IAW, SRM 53-10-3. ( M) 2 L 7 2 4F RT A16WE 1996110100851 19961101 00851 NM 1996 11 1 AWXA960570 1 19960924 A 5320 SPLICE BOEING 737 737277 1384570 NM BS 907 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 PAE - FLT 7824 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON STRINGER AT BS 907, STRINGER 26R. REMOVED, FABRIC ATED AND INSTALLED PRODUCTION SPLICE ON STRINGER 26R, BS 907 PER SRM 51-30-2. (M) 2 L 7 2 4F RT A16WE 1996110100852 19961101 00852 NM 1996 11 1 AWXA960569 1 19960924 A 5320 SPLICE BOEING 737 737277 1384570 NM BS 907 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 PAE - FLT 7824 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON STRINGER 27 LEFT AT BS 907. REMOVED, FABRICATED A ND INSTALLED STRINGER PRODUCTION SPLICE AT BS 907, STRINGER 27 LEFT PER SRM 51-30-2. (M) 2 L 7 2 4F RT A16WE 1996110100853 19961101 00853 NM 1996 11 1 AWXA960568 1 19960921 A 5320 65C807351 MOPSIL BOEING 737 737277 1384570 NM BS 973/986 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 PAE - FLT 7825 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON R-2 MOPSIL STATION 973 AND 986. REMOVED OLD MOPSI L AND INSTALLED NEW MOPSIL PER SRM 51-10-9. (M) 2 L 7 2 4F RT A16WE 1996110100854 19961101 00854 NM 1996 11 1 AWXA960567 1 19960923 A 5315 FLOOR BEAM BOEING 737 737277 1384570 NM BS 986 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 PAE - FLT 7824 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON UPPER SURFACE OF 986 FLOOR BEAM AT RBL 5 AND LBL 3 , WL 208. CUT OUT DAMAGED PORTION OF UPPER FLOOR BEAM CHORD. REMOVED 2.5 INCH BY 1 INCH AND INSTALLED REPAIR ANGLES AN D FILLER AT BS 986, RBL 6 TO LBL 12, WL 208, PER SRM 53-10-9. (M) 2 L 7 2 4F RT A16WE 1996110100855 19961101 00855 NM 1996 11 1 AWXA960566 1 19960927 A 5315 FLOOR BEAM BOEING 737 737277 1384570 NM BS 208 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION 947 FLOOR BEAM TOP FLANGE, WL 208, RBL 4 AND LBL 4, BOTH TOP AND BOTTO M. FABRICATED, ALODINED AND INSTALLED REPAIR PARTS PER SRM 53-10-9. (M) 2 L 7 2 4F RT A16WE 1996110100856 19961101 00856 NM 1996 11 1 AWXA960565 1 19960927 A 5315 FLOOR BEAM BOEING 737 737277 1384570 NM BS 967 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION IN FLOOR BEAM STATION 967, RBL 15-36, WL 208. REMOVED AND REPLACED DA MAGED SECTION OF FLOOR BEAM BS 967-LBL2-RBL57, SRM 53-10-9. (M) 2 L 7 2 4F RT A16WE 1996110100857 19961101 00857 NM 1996 11 1 AWXA960552 1 19961002 A 3230 655281162 L/G ACCESS UNIT BOEING 737 737277 1384570 NM MLG INOPERATIVE A AWXA K NONE J WARNING INDICATION CL CLIMB 1 WP 28 187AW D00376 22654 LAS - FLT 2059 - UPON GEAR RETRACTION, GEAR HANDLE WOULD NOT COME UP PAST OFF POSITION. RECYCLED DOWN THEN LOCK TO UP. HANDLE OPERATED NORMALLY THE SECOND TIME. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT PER AIB32001. REMOVED AND REPLACED AIR AND GROUND SAFETY PROX SWITCHES PER MM 32-09-200. ALL SYSTEMS FUNCTION CHECKED OK. (M) 2 L 7 2 4F RT A16WE 1996110100858 19961101 00858 NM 1996 11 1 TAOA109602 1 19961006 A 3350 1000677 BATTERY PACK GRIMES BOEING 727 727225 1384077 NM L-1 DOOR DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 919TS 1641 20447 L-1 DOOR OVERHEAD EMERGENCY LAMP INOP. REPLACED BATTERY PACK, OPS CHECK OK PER MM CHAPTER 33-50-00. (M) 2 L 7 3 4F A3WE 1996110100859 19961101 00859 EU 1996 11 1 SIMA962782 1 19961004 A 2424 94511 GCU AEROSP ATR72 ATR72212 EU LEFT FAILED A SIMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 260AE 499217 263 HRL - FLT 3724 - FLIGHT CRWE NOTICED A STRONG ELECTRICAL BURNING SMELL IN THE COCKPIT. AIRCRAFT RETURNED TO GATE, FLIGH T CREW CALLED CFR. NO FIRE WAS FOUND AND PASSENGERS DEPLANED NORMALLY. RAI'D AC GEN BPCU AND GCU. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996110100860 19961101 00860 WP 1996 11 1 96ZZZM1429 1 19961004 A 2910 7650332 HYD LINE DOUG DC8 DC8F54 3021926 WP NR 2 HYD PUMP RUPTURED A FXLA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 19 7046H 46011 ON APPROACH MIA, EXPERIENCED LOSS OF HYDRAULIC QUANTITY. COMPLETED EMERGENCY CHECKLIST AND LANDED MIA WITHOUT INCIDENT. INSPECTION REVEALED RUPTURED HYDRAULIC LINE AT NR 2 HYD PUMP. REPLACED BOTH HYDRAULIC PUMPS AND LINE. AIRCRAFT RETUR NED TO SERVICE. (M) 2 L 7 4 4F 4A25 1996110100861 19961101 00861 NM 1996 11 1 AWXA960557 1 19961005 A 3397 WIRE BOEING 737 73733A 1384673 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 173AW 23632 PHX - FLT 2958 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT INOP AT ROW 13 A, B, C. REPAIRED BROKEN WIRE P ER STANDARD PRACTICES. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 1996110100862 19961101 00862 NM 1996 11 1 AWXA960563 1 19961006 A 3350 831136 LIGHT BOEING 737 737277 1384570 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 184AW 15703 22651 PHX - FLT 2572 - DURING ROUTINE MAINTENANCE CHECK, FOUND RIGHT R-1 EMERGENCY LIGHT OVER DOOR INOP. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A16WE 1996110100863 19961101 00863 NM 1996 11 1 AWXA960560 1 19961007 A 3350 10060091101 LIGHT BOEING 737 737277 1384570 NM CABIN MISSING A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 178AW 22645 DURING ROUTINE MAINTENANCE CEHCK, FOUND EMERGENCY LIGHT AT ROW 1 MISSING. REPLACED LIGHT AT ROW 1. OPERATIONS CHECK GO OD. (M) 2 L 7 2 4F RT A16WE 1996110100864 19961101 00864 NM 1996 11 1 AWXA960561 1 19961007 A 3350 SOCKET BOEING 757 7572G7 1384963 NM CABIN DISCONNECTED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 909AW 24522 PHX - FLT 2209 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT INOP AT ROW 24. RESEAT RECESSED SOCKET AT SEAT CONNECTOR. OPERATIONS CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 1996110100865 19961101 00865 NM 1996 11 1 AWXA960562 1 19961006 A 3397 WIRE BOEING 737 737277 1384570 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 186AW 22653 PHX - FLT 2267 - DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT 2-A EMERGENCY LIGHT INOP. REPAIRED WIRING AT SEAT 2-A. S YSTEM OPERATIONS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996110100866 19961101 00866 EU 1996 11 1 VTZA97021 1 19961029 A 3350 6047051 POWER SUPPLY JETAIR JETSTM JETSTM4101 1500501 EU CABIN INOPERATIVE A VTZA K NONE L NO TEST TX TAXI/GRND HDL 1 EA 27 321UE 41045 FLT 6275 - BWI-BOS - DURING TAXI, EXPERIENCED A DISCREPANCY WITH THE INTERIOR EMERGENCY LIGHTS BECOMING INOPERATIVE. AI RCRAFT RETURNED TO THE GATE AND CONTACTED MAINTENANCE CONTROL. AIRCRAFT WAS FERRIED TO IAD WHERE MAINTENANCE REMOVED AN D REPLACED THE EMERGENCY LIGHT POWER SUPPLY. AIRCRAFT WAS THEN RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1996110100867 19961101 00867 EU 1996 11 1 VTZA97020 1 19961011 A 5270 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGGAGE DOOR DIRTY A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 317UE 41031 FLT 6445 - PWM-BOS - ABORTED TAKEOFF DUE TO BAGGAGE DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO F URTHER PROBLEMS. MAINTENANCE OPENED DMI 40806, MEL 52-30. MX CLOSED MI 40806 BY CLEANING FORWARD DOOR MICROSWITCH, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996110100868 19961101 00868 EU 1996 11 1 VTZA97006 1 19961004 A 5270 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU PAX DOOR DIRTY A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 303UE 41015 FLT 6593 - JFK-IAD - ABORTED TAKEOFF DUE TO MAIN DOOR LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROB LEMS. MAINTENANCE OPENEND DMI 03944 MEL 52-3. MAINTENANCE CLOSED DMI 03944 BY CLEANING MICROSWITCH, OPS CHECK OK. AIR CRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996110100869 19961101 00869 EU 1996 11 1 VTZA96388 1 19960921 A 5270 SWITCH STRIKER JETAIR JETSTM JETSTM4101 1500501 EU CARGO DOOR OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 325UE 41063 FLT 6395 - IAD-RIC - ABORTED TAKEOFF DUE TO BAGGAGE DOOR LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER I NCIDENTS. MAINTENANCE OPENED DMI 17799, MEL 52-30. MAINTENANCE CLOSED DMI 17799 BY ADJUSTING MICROSWITCH STRIKER PIN, O PS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996110100870 19961101 00870 EU 1996 11 1 VTZA96377 1 19960917 A 5270 SWITCH BAG JETSTM JETSTM3201 1500217 EU POD DOOR ADJUSTED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 495UE 818 FLT 6448 - IAD-HVN - DURING TAKEOFF, EXPERIENCED A POD DOOR CAPTION WARNING ILLUMINATION. THE AIRCRAFT RETURNED TO IAD WHERE THE MAINTENANCE ACTIVITY TROUBLESHOT THE PROBLEM AND DEFERRED THE ITEM UNDER MEL 52-1. MAINTENANCE CLOSED DMI 554 18 BY ADJUSTING POD DOOR MICROSWITCH, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996110100871 19961101 00871 EU 1996 11 1 VTZA96384 1 19960922 A 5270 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGGAGE DOOR MOISTURE A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 303UE 41015 FLT NR 6261 - IAD-EWR - ABORTED TAKEOFF DUE TO BAGGAGE DOOR LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHE R PROBLEMS. MAINTENANCE OPENED DMI 03942 MEL 52-3. MAINTENANCE CLOSED DMI 03942 BY REMOVING MOISTURE FROM MICROSWITCH. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996110100872 19961101 00872 EU 1996 11 1 VTZA96387 1 19960921 A 6120 1680640 MONOPOLE BAG JETSTM JETSTM3201 1500217 EU LEFT FAILED A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 370MT 800 FLT 6592 - IAD-AVP - DURING CLIMB, MADE A UNSCHEDULED LANDING DUE TO LEFT EGT FLUCTUATES OF 20 PERCENT, NO FLUCTUATION W ITH SRL OFF. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENT. MANTENANCE OPENED DMI 07255, MEL 77-2 ON SRL, MAINTEN ANCE CLOSED DMI 07255 BY REMOVING AND REPLACING PROP GOV MONOPOLE. OPS CHECK OK, AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996110100873 19961101 00873 1996 11 1 VTZA97023 3 19961014 A 6140 31056294 BETA SWITCH JETAIR JETSTM JETSTM4101 1500501 EU LT PROP FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 27 314UE 41027 FLT 6532 - ORD-IAD - ABORTED TAKEOFF DUE TO LEFT RED BETA LIGHT ILLUMINATED. AIRCRAFT RETURNED TO THE GATE WITH NO FURT HER PROBLEMS. MAINTENANCE REMOVED AND REPLACED BETA PRESSURE SWITCH. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996110100874 19961101 00874 EU 1996 11 1 VTZA97022 1 19961011 A 2550 CARGO NET JETAIR JETSTM JETSTM4101 1500501 EU CARGO DOOR OUT OF POSITION A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 306UE 41020 FLT 6501 - IAD-JFK - ABORTED TAKEOFF AT IAD DUE TO BAGGAGE DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WI TH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED THE DOOR WARNING SYSTEM AND FOUND CARGO NET NOT HOOKED UP, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996110100875 19961101 00875 EU 1996 11 1 VTZA97019 1 19961013 A 3610 F2L226 O-RING JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE FAILURE A VTZA D RETURN TO BLOCK M OVER TEMP TX TAXI/GRND HDL 1 EA 27 302UE 41013 FLT 6276 - IAD-EWR - DURING TAXI, RETURNED TO GATE DUE TO LEFT DUCT FAIL LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE W ITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED O-RING ON BLEED AIR SUPPLY LINE, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1996110100876 19961101 00876 1996 11 1 VTZA97011 4 19961005 A 6122 PROP GOV BAG JETSTM JETSTM3201 1500217 EU RT ENGINE OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 474UE 849 FLT 6508 - ROA-IAD - ABORTED TAKEOFF DUE TO RIGHT ENGINE WOULD NOT MAKE POWER. AIRCRAFT WENT TO GATE WITH NO FURTHER IN CIDENTS. MAINTENANCE INSPECTED AND ADJUSTED PROP GOV HIGH, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE . (M) 2 L 7 2 4T RT A56EU 1996110100877 19961101 00877 EU 1996 11 1 VTZA97010 1 19961004 A 3150 TO WARNING JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT ACTIVATED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 309UE 41022 FLT 2010 - EWR-BOS - ABORTED TAKEOFF DUE TO TAKEOFF CONFIGURATION WARNING ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH N O FURTHER PROBLEMS. MAINTENANCE INSPECTED SYSTEM, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVI CE. (M) 2 L 7 2 4T RT A41NM 1996110100878 19961101 00878 EU 1996 11 1 VTZA97009 1 19961004 A 3260 ATG135022 UPLOCK SWITCH JETAIR JETSTM JETSTM4101 1500501 EU RT MLG FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 322UE 41058 FLT 6365 - IAD-ROC - DURING CLIMB, AN UNSCHEDULED LANDING AT IAD DUE TO LIGHT IN GEAR HANDLE ILLUMINATED. AIRCRAFT RETU RNED TO GATE. MAINTENANCE REMOVED AND REPLACED RIGHT MAIN GEAR UPLOCK SWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR R ETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996110100879 19961101 00879 EU 1996 11 1 VTZA97008 1 19961006 A 3150 TO WARNING JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT ACTIVATED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 319UE 41042 FLT 6225 - IAD-BOS - ABORTED TAKEOFF DUE TO TAKEOFF CONFIGURATION WARNING ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH N O FURTHER PROBLEMS. MAINTENANCE INSPECTED SYSTEM AND RESET GUSTLOCK HANDLE. OPS CHECK OK. AIRCRAFT WAS RELEASED AND A PPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996110100880 19961101 00880 EU 1996 11 1 VTZA97007 1 19961006 A 7722 8974676 HARNESS BAG JETSTM JETSTM3201 1500217 EU LT ENGINE LOSE CONNECTION A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 480UE 894 FLT 6289 - IAD-CMH - DURING CRUISE, MADE AN UNSCHEDULED LANDING DUE TO LEFT ENGINE EGT FLUCTUATION. AIRCRAFT RETURNED T O GATE WITH NO FURTHER PROBLEMS. MAINTENANCE REPAIRED COLD SOLDER AT EGT SOFT HARNESS, OPS CHECK OK. AIRCRAFT WAS RELE ASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996110100881 19961101 00881 EU 1996 11 1 VTZA97005 1 19961003 A 3260 9005EN38 SWITCH BAG JETSTM JETSTM3201 1500217 EU NLG OUT OF ADJUST A VTZA L ABORTED APPROACH N FALSE WARNING LD LANDING 1 EA 27 491UE 911 FLT 918 - LYH-IAD - ABORTED APPROACH DUE TO NOSE GEAR INDICATION OF GREEN LIGHT IN FLIGHT WITH GEAR UP AT 200 FEET ON LA NDING RED LIGHT CAME ON, ABORTED LANDING. AIRCRAFT LANDED AND WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE ADJUS TED NOSE GEAR DOWNLOCK SWITCH, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996110100882 19961101 00882 1996 11 1 VTZA97004 4 19961002 A 2312 7510700807 COMM UNIT JETAIR JETSTM JETSTM4101 1500501 EU NR 1 FAILED A VTZA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 27 309UE 41022 FLT 6340 - EWR-BOS - DURING TAXI OUT, EXPERIENCED THE LOSS OF THE NR 1 COMM SYS FUNCTION. THE A/C RETURNED TO GATE WHER E MX CONTROL AT IAD WAS NOTIFIED. MX CONTROL COORDINATED WITH THE IAD MX DEPART PERSONNEL TO POSITION A MX PERSON AND T HE PARTS TO THE EWR STA TO CORRECT THE DISCREPANCY. IAD MECHANIC ARRIVED AT EWR AND TROUBLESHOT THE DISCREPANCY. THE M ECHANIC THEN REPLACED THE FAILED NR 1 COMM UNIT AND RELEASED THE AIRCRAFT FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1996110100884 19961101 00884 NE 1996 11 1 VTZA97002 2 19961001 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE RIGHT FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 303UE 41015 FLT 6599 - RDU-IAD - DURING TAKEOFF, THE FLIGHT CREW EXPERIENCED A RIGHT ENGINE OIL CONTAMINATION INDICATION. THE AIRCR AFT LANDED AT IAD WHERE THE MAINTENANCE PERSONNEL REMOVED AND INSPECTED THE CHIP DETECTOR AND FOUND 2 SMALL SLIVERS AND 1 MACHINE CHIP ON THE DETECTOR. MAINTENANCE CLEANED THE CHIP DETECTOR AND PERFORMED THE REQUIRED PENALTY RUNS. CHIP DE TECTOR WAS INSPECTED AGAIN AND TWO MORE SLIVERS WERE FOUND. CONTACTED ENGINE MANUFACTURER WHO REQUEST THE ENGINE BE REM OVED FOR INSPECTION. FERRIED AIRCRAFT TO LYNCHBURG FOR ENGINE CHANGE. (M) 2 L 7 2 4T 4 T RT A41NM E18NE 1996110100885 19961101 00885 EU 1996 11 1 VTZA97001 1 19961001 A 2611 72111211000 SMOKE DETECTOR BAG JETSTM JETSTM3201 1500217 EU BAGGAGE COMPT FAILED A VTZA K NONE N FALSE WARNING CR CRUISE 1 EA 27 482UE 897 FLT 6504 - ROA-IAD - DURING CRUISE, EXPERIENCED A SMOKE DETECTOR CAPTION LIGHT ILLUMINATION. AIRCRAFT COMPLETED A NORMA L LANDING (NO EMERGENCY DECLARED) AT IAD WHERE MAINTENANCE INSPECTED THE AFT BAGGAGE AREA AND FOUND NO INDICATION OF PRO BLEM. TROUBLESHOT SYSTEM AND FOUND SMOKE DETECTOR HAD FAILED. REPLACED SMOKE DETECTOR AND RETURNED AIRCRAFT TO SERVICE . (M) 2 L 7 2 4T RT A56EU 1996110100886 19961101 00886 EU 1996 11 1 VTZA96401 1 19960930 A 2751 923FLBU FLAP TRANSMITTER BAG JETSTM JETSTM3201 1500217 EU TE FLAPS DIRTY A VTZA O OTHER F FLT CONT AFFECTED AP APPROACH 1 EA 27 475UE 850 FLT 6901 - ROA-IAD - DURING APPROACH EXPERIENCED A FLAP INDICATION FAILURE. AIRCRAFT COMPLETED A NORMAL LANDING AT IAD WITH FLAPS AT 20 DEGREES AND FLAPS BEING PHHYSICALLY VERIFIED AT THE CORRECT POSITION BY THE FLIGHT CREW THROUGH VISUAL OBSERVATION THROUGH THE CABIN WINDOWS. MAINTENANCE TROUBLESHOT THE SYSTEM AND FOUND THE CONNECTIONS ON THE FLAP POSITI ON INDICATING TRANSMITTER DIRTY. CLEANED CONNECTIONS AND PERFORMED MAINTENANCE OPERATIONAL CHECK OF THE SYSTEM WITH NO FURTHER PROBLEMS. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A56EU 1996110100887 19961101 00887 EU 1996 11 1 VTZA97018 1 19961010 A 5270 SP4594 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGG DOOR LOOSE A VTZA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 27 314UE 41027 FLT 6431 - IAD-RDU - DURING TAKEOFF FLIGHT, EXPERIENCED A BAGGAGE DOOR WARNING LIGHT DURING THE TAKEOFF ROLL. AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE TECHNICIANS FOUND THE FORWARD BAGGAGE BAY DOOR MICROSWITCH LOOSE. SECURED MICROS WITCH AND VERIFIED PROPER ADJUSTMENTS. AIRCRAFT WAS THEN RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1996110100888 19961101 00888 WP 1996 11 1 VTZA97017 2 19961011 A 7320 FUEL CONTROL BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP LT ENGINE OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 27 486UE 905 FLT 900 - LYH-IAD - ABORTED TAKEOFF OF FLIGHT, DUE TO THE LEFT ENGINE SHOWING LOW RPM. AIRCRAFT RETURNED TO THE GATE WH ERE THE MAINTENANCE TECHNICIANS TROUBLESHOT THE DISCREPANCY AND ADJUSTED SCREW 'X' FOR THE LEFT ENGINE. AIRCRAFT WAS RE LEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 3 T RT A56EU E3WE 1996110100889 19961101 00889 1996 11 1 VTZA97015 4 19961009 A 3420 7012100811 RMU JETAIR JETSTM JETSTM4101 1500501 EU NR 1 FAILED A VTZA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 27 321UE 41045 FLT 6590 - IAD-RDU - DURING TAXI, EXPERIENCED A FAILURE OF THE NR 1 RMU SCREEN. SCREEN WENT BLANK. AIRCRAFT RETURNED T O GATE. MAINTENANCE REMOVED AND REPLACED NR 1 RADIO MANAGEMENT UNIT AND PERFORMED FUNCTIONAL CHECK OF THE SYSTEM. FUNC TIONAL CHECK PROVED GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996110100890 19961101 00890 1996 11 1 VTZA97014 3 19961009 A 6140 8659566 BETA SWITCH BAG JETSTM JETSTM3201 1500217 EU RT FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 489UE 908 FLT - 6301 - IAD-ISP - ABORTED TAKEOFF DUE TO RIGHT ENGINE BETA LIGHT. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLE MS. MAINTENANCE REMOVED AND REPLACED RIGHT BETA SWITCH. PERFORMED GROUND OPERATIONAL CHECK. SYSTEM CHECKED OK. AIRCR AFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996110100891 19961101 00891 EU 1996 11 1 VTZA97013 1 19961008 A 5270 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGGAGE DOOR OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 322UE 41058 FLT 6502 - JFK-IAD- ABORTED TAKEOFF DUE TO MAIN BAGGAGE DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND ADJUSTED BAGGAGE DOOR MICROSWITCH. AIRCRAFT WAS RELEASED AND APPROVED F OR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996110100892 19961101 00892 EU 1996 11 1 VTZA97012 1 19961008 A 5230 BAGG NET JETAIR JETSTM JETSTM4101 1500501 EU BAGG DOOR OUT OF POSITION A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 322UE 41058 FLT 6594 - IAD-CLE - ABORTED TAKEOFF DUE TO MAIN BAGGAGE DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE SECURED BAGGAGE RESTRAINT NET. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERV ICE. (M) 2 L 7 2 4T RT A41NM 1996110100893 19961101 00893 EU 1996 11 1 VTZA97024 1 19961015 A 3230 1847F RADIUS ROD BAG JETSTM JETSTM3201 1500217 EU LT MLG FAILED A VTZA L ABORTED APPROACH J WARNING INDICATION LD LANDING 1 EA 27 471UE 821 FLT 6357 - IAD-AVP - DURING APPROACH, ABORTED LANDING DUE TO LEFT MAIN LANDING GEAR DOWNLOCK INTERMITTENT INDICATION. C REW EXPERIENCED A FLICKERING OFF AND ON INDICATION TWICE WITH APPROXIMATELY A 10 SECOND DELAY. FLIGHT CREW RECYCLED LAN DING GEAR AND GOT A SOLID DOWN AND LOCK INDICATION. AIRCRAFT COMPLETED ITS LANDING. MAINTENANCE INSPECTED AIRCRAFT AND FOUND THAT THE LEFT RADIUS HAD AN INTERNAL PROBLEM. MAINTENANCE REMOVED AND REPLACED THE RADIUS ROD, PERFORMED GEAR SW ING AND LEAK CHECK AND RETURNED THE AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996110100894 19961101 00894 EU 1996 11 1 VTZA96402 1 19960929 A 2170 COALESCER BAG JETAIR JETSTM JETSTM4101 1500501 EU LT ACM DIRTY A VTZA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 27 301UE 41012 FLT 941 - LYH-LYH - DURING CLIMB, MADE AN UNSCHEDULED LANDING DUE TO SMOKE IN COCKPIT. AIRCRAFT RETURNED TO LYH WITH NO FURTHER INCIDENTS. MAINTENANCE INSPECTION AND FOUND OIL IN THE LEFT ACM WATER SEPARATOR SOCK. MAINTENANCE CLEANED SOC K. AIRCRAFT WAS RELEASED AND APPROVED FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1996110100895 19961101 00895 NM 1996 11 1 96ZZZM1430 1 19960929 A 2612 87823802 FIRE LOOP CONN BOEING 737 7372L9 1384497 NM E/E COMP DIRTY A ZZDA F ACTIVATE FIRE EXT. N FALSE WARNING LD LANDING 1 SO 15 464AT M00375 21278 DURING LANDING CHECK AFTER ARRIVAL IN OMA, FLT 800, HAD APU FIRE WARNING INDICATION (AUDIBLE AND VISUAL) DURING APU STAR T. APU SHUTDOWN AUTOMATICALLY. CREW PULLED FIRE WARNING SWITCH AND AGENT WAS DISCHARGED. UPON ARRIVAL AT GATE MAINTEN ANCE PERFORMED AN INSPECTION OF THE APU COMPARTMENT AND TAILPIPE AREA. NO EVIDENCE OF FIRE WAS FOUND. MECHANICS MEL'D APU AND FIRE DETECTION SYSTEM. AIRCRAFT WAS RELEASED FOR FLIGHT. AIR TRAM MAINTENANCE CLEANED FIRE LOOP CONNECTORS D18 76 AND 1878. REPLACED FIRE LOOP CONNECTORS D984, D982, D1446 AND 1448. REPLACED FIRE DETECTION UNIT. POST MX RUN OF A PU WAS NORMAL. (M) 2 L 7 2 4F RT A16WE 1996110100896 19961101 00896 NE 1996 11 1 RAIA961006 2 19961006 A 7397 2502 WIRE AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE RT ENGINE CHAFED A RAIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 03 423TE 119 STL - FLT 7480 - RIGHT ENGINE FUEL TEMP INCREASED WITH HIGH OIL TEMP. MAINTENANCE REPAIRED CHAFED WIRE AT FUEL/OIL SWIT CH. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1996110100897 19961101 00897 EU 1996 11 1 RAIA961003 1 19961005 A 3350 ML44 BULB AEROSP ATR72 ATR72202 8680940 EU PAX DOOR FAILED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 721TE 217 STL - FLT 7003 - EMERGENCY LIGHT IN THE MAIN CABIN DOOR IS INOP. MAINTENANCE REPLACED THE DOOR EMERGENCY LIGHT BULB. ( M) 2 H 7 2 4T RT A53EU 1996110100898 19961101 00898 EU 1996 11 1 RAIA961002 1 19961003 A 3350 ML44 BULBS AEROSP ATR72 ATR72202 8680940 EU CABIN FAILED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 722TE 220 STL - FLT 7166 - BOTH EMERGENCY LIGHTS ON THE RIGHT SIDE OF CABIN AND AT PASSENGER DOOR INOP. MAINTENANCE REPLACED RIGH T AND PASSENGER DOOR LIGHT BULBS. (M) 2 H 7 2 4T RT A53EU 1996110100899 19961101 00899 EU 1996 11 1 RAIA961010 1 19961007 A 3610 ASNA214505 CLAMP AEROSP ATR42 ATR42300 8680920 EU RT ENGINE FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 422TE 106 FYV - FLT 7411 - RIGHT ENGINE EGT WENT TO 850 DEGREES CELSIUS FOR 3 SECONDS. MAINTENANCE REPLACED THE RIGHT ENGINE HP B LEED VALVE CLAMP. (M) 2 H 7 2 4T RT A53EU 1996110100900 19961101 00900 EU 1996 11 1 RAIA961009 1 19961006 A 7712 31039402B TORQUE RING BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA E ENGINE SHUTDOWN Y ENGINE STOPPAGE CL CLIMB 1 CE 03 864AE 8639 864 LAX - FLT 4790 - LEFT ENGINE DID NOT RESPOND TO POWER LEVER CONTROL INPUTS. ENGINE WAS SHUTDOWN. MAINTENANCE REPLACED THE LEFT ENGINE TORQUE RING. (M) 2 L 7 2 4T RT A56EU 1996110100901 19961101 00901 EU 1996 11 1 RAIA961008 1 19961007 A 5270 SP4954 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGGAGE DOOR DIRTY A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 551HK 4481 41040 STL - FLT 7506 - BAGGAGE DOOR LIGHT ILLUMINATED AT V1. MAINTENANCE CLEANED THE FORWARD DOOR MICROSWITCH. (M) 2 L 7 2 4T RT A41NM 1996110100903 19961101 00903 EU 1996 11 1 RAIA961004 1 19961004 A 7722 EM340CH EGT WIRE JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE LOOSE A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 564HK 2466 41081 STL - FLT 7506 - RIGHT INTEGRATED ENGINE CONTROL LIGHT CAME ON DURING TAKEOFF. MAINTENANCE REPLACED THE TERMINAL ON THE EGT SHORT LEAD. (M) 2 L 7 2 4T RT A41NM 1996110100904 19961101 00904 EU 1996 11 1 RAIA961011 1 19961008 A 3350 ML44 BULB AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 426TE 228 STL - FLT 7174 - BOTH EMERGENCY EXIT LIGHTS INOP. MAINTENANCE REPLACED BOTH EMERGENCY EXIT LIGHT BULBS. (M) 2 H 7 2 4T RT A53EU 1996110100905 19961101 00905 WP 1996 11 1 RAIA961014 2 19961008 A 7320 8961151 P3 GASKETS BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RT ENGINE LEAKS A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 859AE 11134 859 MRY - FLT 4760 - RIGHT ENGINE WOULD NOT PRODUCE TARGET TORQUE. MAINTENANCE REPLACED THE RIGHT ENGINE P3 GASKETS. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996110100906 19961101 00906 EU 1996 11 1 RAIA961013 1 19961009 A 3610 3038413 DUCT AEROSP ATR42 ATR42300 8680920 EU RT ENGINE A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 422TE LEAKS 106 PIA - FLT 7109 - RIGHT ENGINE ITT HIGH, TARGET TORQUE LOW DURING TAKEOFF. MAINTENANCE REPLACED THE RIGHT BLEED DUCT. ( M) 2 H 7 2 4T RT A53EU 1996110100907 19961101 00907 EU 1996 11 1 RAIA960938 1 19960929 A 5210 1371027C405 ROD BAG JETSTM JETSTM3201 1500217 EU PAX DOOR OUT OF ADJUST A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 427AM 876 STL - FLT 7422 - PASSENGER DOOR LIGHT CAME ON DURING FLIGHT. MAINTENANCE DEFERRED AS PER MEL 52-2 CAT C. MAINTENANCE L ATER CLEARED MEL BY ADJUSTING THE PASSENGER DOOR LINKAGE. (M) 2 L 7 2 4T RT A56EU 1996110100908 19961101 00908 CE 1996 11 1 96ZZZM1431 1 19961006 A 2120 AIR DISTR BEECH 1900 1900C 1154161 CE COCKPIT SMOKE A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 19 199GA UB13 FLT 398A - FLL-MIA - SMOKE COMING OUT OF CAPTAIN AND FIRST OFFICERS ACM VENTS IN FLIGHT. LASTED ABOUT 10 SECONDS. PERF ORMED GROUND RUN UP NO SMOKE NOTED. OPERATED ALL SYSTEMS NO DEFECTS NOTED. POSSIBLE CONDENSATION FROM THE AIR CYCLE MA CHINE AIR CONDITIONING SYSTEM VENTS. 2 L 7 2 4T RT A24CE 1996110100909 19961101 00909 WP 1996 11 1 ASAA9680219 1 19961006 A 3350 6011779 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 935AS 12617 49236 SFO - DURING MAINTENANCE CHECK, THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPL Y AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996110100910 19961101 00910 NM 1996 11 1 ASAA9610131 1 19961002 A 3350 8821004 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - FLT 64 - PRIOR TO DEPARTURE IT WAS REPORTED THAT THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 8 ILLUMINATED WITH S WITCH IN ARMED POSITION AND BUSSES POWERED. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996110100911 19961101 00911 NM 1996 11 1 ASAA9610132 1 19961005 A 3350 8821004 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROW 18. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996110100912 19961101 00912 CE 1996 11 1 96ZZZM1432 1 19960926 A 3297 WIRE BEECH 1900 1900C 1154161 CE NLG BROKEN A AMWA O OTHER O OTHER AP APPROACH 1 CE 07 143AM UC143 COMING INTO OMA, THE NOSE GEAR LIGHT FAILED TO ILLUMINATE UPON NORMAL GEAR EXTENSION. THE CREW PERFORMED AN EMERGENCY G EAR EXTENSION AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A BROKEN WIRE AT THE DOWNLOCK SWITCH, PERFORMED REPAIR AND RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1996110100919 19961101 00919 1996 11 1 WRLA96040 4 19960926 A 2211 4059001907 FLT CONTL COMP DOUG MD11 MD11 3023602 NM NR 1 POSITION FAILED A WRLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 273WA 48519 DURING TAXI OUT FROM DEPARTURE GATE, FLIGHT CREW NOTED FAILURE OF NR 1 FLIGHT CONTROL COMPUTER FCC1. FLIGHT CREW ELECTE D TO RETURN TO GATE FOR MAINTENANCE ACTION. AIRCRAFT RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE PERSONNEL DE-POWER ED AND RE-POWERED AIRCRAFT. RECYCLED BOTH FCC1A AND FCC1B CIRCUIT BREAKERS. FAULT CLEARED. PERFORMED 'RETURN TO SERVI CE' TEST WITH NO FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A22WE 1996110100942 19961101 00942 SO 1996 11 1 RAAA96E8034 1 19961029 A 3350 CA31N BATTERY LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 EXTERNAL EMERGENCY LIGHTS FAILED SERVICE CHECK. REPLACED BATTERY DUE LOW CHARGE. 2 L 7 4 4T 4A22 1996110100943 19961101 00943 WP 1996 11 1 CALA9601528 1 19961029 A 2450 CKT BREAKER DOUG DC9 DC932 3022066 WP LEFT AC BUS FAILED A CALA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 09 18544 47219 THE B-PHASE CIRCUIT BREAKER ON LEFT AC BUS POPPED FOLLOWED BY ALL FORWARD LT, RT AND CENTER FUEL BOOST PUMP CB. THE A-P HASE CIRCUIT BREAKER ON RADIO RACK COOLING FAN POPPED AND LIGHTS ON RT SIDE IN CABIN WENT OUT AS WELL AS CAPT'S INSTRUME NT LIGHTS, VOR AND RADIOS. THE AIRCRAFT WAS RETURNED TO CLE. A CHECK OF ALL BOOST PUMPS, RADIO RACK COOLING FAN AND AL L MISC LIGHTS/EQUIPMENT POWERED BY LT AC BUS WAS PERFORMED AND NO DEFECTS WERE NOTED. A CHECK OF ALL GENERATORS PERFORM ED WITH NO PROBLEMS. MAINTENANCE FOUND THE LT AC BUS B-PHASE CB AT FAULT. THE B-PHASE CB WAS REMOVED AND REPLACED. AL L AC DISTRIBUTION CHECKED GOOD. 2 L 7 2 4F A6WE 1996110100944 19961101 00944 WP 1996 11 1 CALA9601529 1 19961029 A 2910 B-NUT DOUG DC9 DC982 3022082 WP LT HYD SYST LEAKING A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 09 16802 49222 THE LT HYDRAULIC SYSTEM LOST ALL FLUID WHILE AT 26,000 FEET. THE LOSS OF FLUID WAS ACCOMPANIED BY ILLUMINATION OF THE L EFT HYDRAULIC LOW PRESSURE LIGHT. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND B-NUT LOOSE ON LEFT CASE DRAIN FILTER. THE B-NUT WAS SECURED AND THE HYDRAULIC SYSTEM WAS SERVICED. AN ENGINE RUN WAS PERFORMED AND NO LEAKS WERE NOTED. 2 L 7 2 4F A6WE 1996110100945 19961101 00945 WP 1996 11 1 CALA9601530 1 19961025 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 140.038 PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 43537 47112 A MAINTENANCE LIFT TRUCK STRUCK THE FUSELAGE CREATING A HOLE THROUGH SKIN AT STA 140.038, 3 INCHES BELOW LONGERON 20R. T HE HOLE WAS APPROXIMATELY .875 L BY .5 W. THE AREA WAS REPAIRED IAW SRM 53-04 FIGURE 12B PAGE 608A SHEET 15. 2 L 7 2 4F A6WE 1996110100946 19961101 00946 NM 1996 11 1 CALA9601531 1 19961015 A 5522 SKIN BOEING 727 727227 1384078 NM RT ELEVATOR GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76753 21249 INSPECTION FOUND THE RT ELEVATOR LOWER SKIN GOUGED JUST AFT OF NR 2 HINGE. THE GOUGED AREA WAS CUT AWAY. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 55-30-3. 2 L 7 3 4F A3WE 1996110100947 19961101 00947 NM 1996 11 1 CALA9601532 1 19961017 A 5320 ANGLE BOEING 727 727227 1384078 NM BS 1140 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76753 21249 INSPECTION FOUND THE RIGHT AFT LAV FLOOR SUPPORT, JUST AFT OF FORWARD WALL U-CHANNEL CORRODED AT BS 1140. THE SUPPORT A NGLE WAS REMOVED AND A REPLACEMENT WAS FABRICATED AND INSTALLED IAW SRM 51-40-4. 2 L 7 3 4F A3WE 1996110100948 19961101 00948 WP 1996 11 1 9622979180 1 19961029 A 3397 WIRE DOUG DC9 DC914 3022034 WP CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 3312L 45707 DURING LINE CHECK, FOUND AFT AISLE EMERGENCY PATH LIGHTS INOPERATIVE. REPAIRED WIRE AT LOWER SIDEWALL UNDER SEAT 15F, O PERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996110100949 19961101 00949 WP 1996 11 1 9622989869 1 19961026 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 788NC 48100 DURING LINE CHECK, FOUND FORWARD SECTION FLOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY AND POWER SUPPLY, OPERATI ONAL CHECK OK. 2 L 7 2 4F A6WE 1996110100950 19961101 00950 WP 1996 11 1 9622999878 1 19961026 A 3350 LIGHT DOUG DC9 DC951 3022051 WP TAILCONE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 787NC 48149 DURING LINE CHECK, FOUND TAILCONE SPOT LIGHTS INOPERATIVE. REPLACED BULBS AND BATTERIES, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996110100951 19961101 00951 WP 1996 11 1 9623009160 1 19961027 A 3350 BATTERIES DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8903E 45744 DURING LINE CHECK, FOUND RIGHT HAND OVERWING EXIT EMERGENCY LIGHT WILL NOT ILLUMINATE. REPLACED BATTERIES, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996110100952 19961101 00952 WP 1996 11 1 9623019930 1 19961024 A 3260 INDICATION DOUG DC9 DC931 3022065 WP NLG MALFUNCTIONED A NWAA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 01 89S 47042 DURING FLIGHT, RED NOSE GEAR UNSAFE LIGHT DID NOT ILLUMINATE WITH THROTTLES AT FLIGHT IDLE. ON APPROACH, NOSE GEAR GREE N LIGHT DID NOT ILLUMINATE. RECYCLED GEAR TWO TIMES AND NORMAL INDICATIONS WERE ACHIEVED. AIRCRAFT LANDED WITHOUT INCI DENT. MAINTENANCE CYCLED NOSE GEAR SEVERAL TIMES. PROBLEM COULD NOT BE DUPLICATED. REPLACED NOSE GEAR DOWNLOCK SWITCH AS A PRECAUTION. ALSO, REPLACED NOSE GEAR BUNGEE CYLINDER FOR BYPASSING, OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996110100953 19961101 00953 WP 1996 11 1 9623029957 1 19961025 A 3350 LIGHTS DOUG DC9 DC931 3022065 WP TAILCONE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 915RW 47139 DURING PERIODIC CHECK, FOUND TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS AND POWER SUPPLIES, OPERATIO NAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996110100954 19961101 00954 1996 11 1 9623039960 4 19961025 A 2565 113317 SLIDE DOUG DC9 DC931 3022065 WP GALLEY DOOR LOW PRESSURE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 920RW 48293 31 47163 DURING LINE MAINTENANCE INSPECTION, FOUND GALLEY SERVICE DOOR EVACUATION SLIDE LOW ON PRESSURE. REPLACED SLIDE. 2 L 7 2 4F A6WE 1996110100955 19961101 00955 WP 1996 11 1 9623049929 1 19961027 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8923E 45838 DURING LINE MAINTENANCE INSPECTION, FOUND OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN BATTERY PAC K, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996110100956 19961101 00956 WP 1996 11 1 9623059957 1 19961025 A 3350 6011779 BATTERY PACK DOUG DC9 DC931 3022065 WP RT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 915RW 47139 DURING PERIODIC CHECK, FOUND RIGHT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL . 2 L 7 2 4F A6WE 1996110100957 19961101 00957 NE 1996 11 1 9623061151 2 19961028 A 7230 COMPRESSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 1 ENGINE STALLED A NWAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS LD LANDING 1 GL 01 151US 46760 86166 DURING LANDING ROLLOUT, THE NR 1 ENGINE EXPERIENCED REVERSE STALL. THE ENGINE WAS SHUT DOWN AS EGT ROSE OVER 950 DEGREE S WITHIN THIRTY SECONDS. MAINTENANCE PERFORMED BORESCOPE INSPECTION AND NO DISCREPANCIES WERE FOUND. CHECKED REVERSER ACTUATED BLEED SYSTEM AND FOUND NORMAL. AIRCRAFT RETURNED TO SERVICE, THE NR 1 ENGINE ON EIGHTY FLIGHT HOURS MONITOR. 2 L 7 3 4F 4 F A22WE E20EA 1996110100958 19961101 00958 NE 1996 11 1 9623076635 2 19961026 A 7230 COMPRESSOR BOEING 747 747227B 1384888 NM PWA JT9 JT9D7Q 52054 NE NR 3 ENGINE STALLED A NWAA E A J ENGINE SHUTDOWN UNSCHED LANDING DUMP FUEL R PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 01 625US 21682 02242 DURING TAKEOFF ROTATION, THE NR 3 ENGINE EXPERIENCED TWO COMPRESSOR STALLS. AT THE TIME OF STALL, EGT ROSE TO 850 DEGRE ES CELSIUS FOR APPROXIMATELY FIVE MINUTES. EPR WAS 1.60 AND N1 AND N2 FLUCTUATED THEN DROPPED TO THE BOTTOM OF THE SCAL E. CREW SHUT DOWN THE ENGINE, DUMPED 152,000 LBS OF FUEL AND RETURNED TO MSP WITHOUT FURTHER INCIDENT. THE NR 3 ENGINE WAS REPLACED AND FUNCTIONAL CHECK WAS NORMAL. 2 L 7 4 4F 4 F A20WE E3NE 1996110100959 19961101 00959 NM 1996 11 1 9623085513 1 19961026 A 2424 734284A GCU BOEING 757 757251 1384970 NM RT ENGINE MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 513US 31327 19758 23201 AFTER TAKEOFF, THE RIGHT AC BUS OFF LIGHT, BOTH UTILITY BUS LIGHTS AND THE RIGHT GENERATOR CONTROL LIGHT ILLUMINATED. F OLLOWED COCKPIT OPERATING MANUAL PROCEDURES BUT WAS UNABLE TO RESTORE THE RIGHT AC BUS. AIRCRAFT DIVERTED TO SEA AND LA NDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT GENERATOR CONTROL UNIT, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A2NM 1996110100960 19961101 00960 NM 1996 11 1 9623092284 1 19961027 A 3350 BATTERY BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 284US 21323 DURING LINE CHECK, FOUND THE AFT GALLEY EMERGENCY EXIT SIGN WAS INOPERATIVE. REPLACED THE BATTERY PACK AND POWER SUPPLY , CHECKED OK. 2 L 7 3 4F A3WE 1996110100961 19961101 00961 NM 1996 11 1 9623102296 1 19961025 A 3350 LIGHT BOEING 727 727251 138408H NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 296US 21788 DURING SVC1 CHECK, FOUND THE AFT ENTRY DOOR EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE LIGHT ASSEMBLY, CHECKED OK. 2 L 7 3 4F A3WE 1996110100962 19961101 00962 NM 1996 11 1 9623112705 1 19961026 A 3350 BATTERY BOEING 727 727225 1384077 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 802EA 22433 DURING LINE CHECK, FOUND THAT THE EXTERIOR LOWER LEFT AFT EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE BATTERY PACK, C HECKED OK. 2 L 7 3 4F A3WE 1996110100963 19961101 00963 NM 1996 11 1 96FDEA01622 1 19961028 A 5320 65561727 CHORD BOEING 727 727233 138408A NM BS 552 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 NR 0255 014. CRACKED LEVELING COMPOUND AT BS 552, RBL 25, WL 152. UPON FURTHER INVESTIGATION, FOUND CORROSION UNDER L EVELING COMPOUND ON CHORD WHICH IS OUT OF LIMITS. FOUND CORROSION FROM CHORD. CORROSION REMOVAL FOUND TO BE OUT OF LIM ITS. FABRICATED AND INSTALLED REPAIR ANGLE AND SHIM. IAW FED EX EA. 75310-31232. WAS OUT OF LIMITS PER FEDEX SRM 53-1 0-1. 2 L 7 3 4F RT A3WE 1996110100964 19961101 00964 NM 1996 11 1 96FDEA01623 1 19961028 A 5754 651622558 BONDING JUMPER BOEING 727 727233 138408A NM WS 190.0 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 NR 0403 015, CORROSION ON NR 3 K-FLAP BULLNOSE O/B BONDING JUMPER UPPER AND LOWER ATTACH POINTS. *S/D* REPAIRED NR 3 K -FLAP BULLNOSE O/B BONDING JUMPER UPPER ATTACH POINT PER FEDEX SRM 57-50-3 AND THE LOWER ATTACH POINT WAS FOUND TO BE WI THIN LIMITS PER FEDEX SR 27-57-010. 2 L 7 3 4F RT A3WE 1996110100965 19961101 00965 NM 1996 11 1 96FDEA01624 1 19961028 A 5330 65545656 SKIN BOEING 727 727233 138408A NM BS 480 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 NR 0043 016, BS 480, STRINGER 22 RT TO 23 RT THERE ARE GOUGES ON THE OUTER SKIN. *S/D* REPAIRED GOUGES ON OUTER SKIN B S 480 STRINGER 22 RT TO 23 RT PER FEDEX SRM 53-30-3. 2 L 7 3 4F RT A3WE 1996110100966 19961101 00966 NM 1996 11 1 96FDEA01625 1 19961028 A 5320 57177535 WEB BOEING 727 727233 138408A NM BS 225-251 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 NR 0739 017. CORROSION (C53-22-01) UNDER HORIZONTAL WEB AND OUTBOARD CHORD STA 225-251 RBL 45 WL 231 (NR 2 WINDOW LOWE R TRACK SITS ON IT). REMOVED AND REPLACED HORIZONTAL WEB STA 225 TO 251, RBL 45, WL 231. IAW FEDEX SRM 53-10-1. REMO VED CORROSION ON O/B CHORD STA 225 TO 251, RBL 45, WL 231. REWORKED AREA FOUND TO BE WITHIN LIMITS IAW FEDEX SRM 53-10 -1. ALODINED AND PRIMED. 2 L 7 3 4F RT A3WE 1996110100967 19961101 00967 NM 1996 11 1 96FDEA01626 1 19961028 A 5754 651622717B HINGE LUG BOEING 727 727233 138408A NM NR 1 LE FLAP CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 NR 0399 018, CORROSION NR 1 K-FLAP CENTER HINGE LUG AT LOWER BOLT. *S/D* REMOVED CORROSION ON NR 1 K-FLAP CENTER HINGE LUG. REPAIRED IAW FEDEX EA 7-5750-31276A. FUNCTIONAL TESTED NR 1 K-FLAP OK IAW FEDEX M/M 27-81-1. 2 L 7 3 4F RT A3WE 1996110100968 19961101 00968 NM 1996 11 1 96FDEA01627 1 19961028 A 5311 651630822 FRAME BOEING 727 727233 138408A NM BS 243 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 NR 0747 019, CORROSION (C53-221-01) ON WEB FORWARD SIDE OF FRAME STA 243, RBL 48, WL 211 TO 233. *S/D* REPAIRED WEB AT STA 243 FRAME RBL 48 WL 211 TO 233 PER FEDEX SRM 51-40-2. 2 L 7 3 4F RT A3WE 1996110100969 19961101 00969 NM 1996 11 1 SCNA96319 1 19961025 A 2750 CONNECTOR BOEING 727 727282 138408T NM TE FLAPS DIRTY A SCNA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 281SC 21949 SPLIT FLAP INDICATION, INBOARD FLAP INDICATED 3 DEGREES. AIRCRAFT DIVERTED TO TULSA FOR MAINTENANCE. OPERATED BYPASS A CTUATOR DRIVE TO FULL UP, CLEANED AND RECONNECTED BYPASS CANNON PLUG, OPERATED SYSTEM IN BOTH NORMAL AND ALTERNATE THREE TIMES EACH. NO BINDING, ASSYMETRY, OR SPLIT NOTICED AND ALL HARDWARE INTACT. OPERATES NORMAL PER MM 27-51-0. 2 L 7 3 4F RT A3WE 1996110100970 19961101 00970 NM 1996 11 1 CKSA96189 1 19961029 A 2133 OUTFLOW VALVE BOEING 727 727223 1384074 NM CABIN STICKING A CKSA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 23 6806 19481 CABIN OUTFLOW VALVE POSSIBLY STICKING. CABIN CLIMBED IN EXCESS OF 2,000 FT PER MINUTE, MANUAL CONTROL HAS NO EFFECT. C ABIN WENT BACK TO NORMAL, 5 MINUTES LATER LOSS OF CABIN AGAIN, SAME CONDITIONS. CREW DID AN EMERGENCY DESCENT. MAINTEN ANCE TESTED OUTFLOW VALVES, AUTO PRESSURIZATION AND MANUAL PRESSURIZATION IN ACCORDANCE WITH BOEING MM CHAPTER 21-30-0. ALL SYSTEMS OPS CHECKS NORMAL. COULD NOT DUPLICATE. 2 L 7 3 4F A3WE 1996110100971 19961101 00971 SO 1996 11 1 SRAA961015 1 19961028 A 6120 7143253 VALVE LKHEED 382 382G 526414U SO NR 2 PROP DEFECTIVE A SRAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 23 920SJ 4561 DURING FLIGHT, NR 2 ENGINE RPM DECAYED RAPIDLY. SHUT DOWN NR 2 ENGINE AND LANDED WITHOUT INCIDENT. FOUND NR 2 ENGINE V ALVE HOUSING DEFECTIVE. REPLACED NR 2 PROP VALVE HOUSING, PERFORMED ENGINE RUN SYSTEM OPS CHECKED GOOD PER SAT J/C 6103 , 7101 AND 7101-2. 2 H 7 4 4T A1SO 1996110200001 19961102 00001 WP 1996 11 2 AALA961327 1 19960906 A 3320 0200041021 SOCKET DOUG DC9 DC982 3022082 WP CABIN SHORTED A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 476AA 49651 BOS - FLT 630 - EN ROUTE DFW/BOS - DURING CRUISE, F/A NOTED ELECTRICAL ODOR BY PAX SEAT ROW 29DEFT. NO OTHER ABNORMAL I NDICATIONS AND AIRCRAFT PROCEEDED BOS AND LANDED WITHOUT INCIDENT. PLACARDED WINDOW LIGHT LAMPHOULDER (SOCKET) ABOVE PA X SEAT ROW 28-29 DEF. SUBSEQUENTLY REPLACED LAMPHOLDER ABOVE PAX SEAT ROWS 28-29 DEF AT EWR. SYSTEM GROUND CHECKED NOR MAL OPERATIONS WITH NO ELECTRICAL ODOR NOTED. (M) 2 L 7 2 4F A6WE 1996110700001 19961107 00001 EU 1996 11 7 96ZZZX5459 1 19960416 A 3260 1EN16 DOWNLOCK SWITCH FOKKER F27 F27MK500 4990629 EU NLG OUT OF ADJUST A MTNA O OTHER P NO WARNING INDICATION AP APPROACH 1 SO 33 708FE 10372 PWM - ON APPROACH AFTER SELECTING LANDING GEAR DOWN, THE CREW DID NOT RECEIVE NOSE GEAR DOWN INDICATION. THE FLIGHT CRE W PERFORMED ALL EMERGENCY CHECK LISTS AND DECLARED AN EMERGENCY LANDING. THE AIRCRAFT LANDED SAFELY WITH NO FURTHER PRO BLEMS. AFTER TROUBLESHOOTING, MECHANIC FOUND A NOSE LANDING GEAR DOWNLOCK SWITCH REQUIRED ADJUSTMENT. 2 H 7 2 4T A817 1996110700002 19961107 00002 EU 1996 11 7 96ZZZX5460 1 19960430 A 2612 51227105 FIRE LOOP GRAVINER FOKKER F27 F27MK500 4990629 EU RT ENGINE CHAFED A MTNA O A OTHER UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 SO 33 717FE 10455 CHA - ON DEPARTURE, RIGHT ENGINE FIRE WARNING CAME ON. THE FLIGHT CREW PERFORMED THE EMERGENCY PROCEDURES AND THE AIRCR AFT RETURNED TO CHA. AFTER TROUBLESHOOTING, THE MECHANIC FOUND A BAD FIRE WARNING LOOP. THE LOOP WAS REMOVED AND REPLA CED. THE SYSTEM CHECKED GOOD IAW THE FOKKER MM. 2 H 7 2 4T A817 1996110700003 19961107 00003 NE 1996 11 7 96ZZZX5461 2 19960417 A 7260 GD202 DRIVE SHAFT ROTOL FOKKER F27 F27MK500 4990629 EU RROYCE DART DART5327R 54509 NE RIGHT GEARBOX SHEARED A A MTNA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 33 718FE 1339 0C024 10470 GRR - ON DEPARTING REACHING 5,000 FEET ALTITUDE, THE RIGHT GEARBOX OIL PRESSURE LIGHT, ALTERNATOR LIGHT, GENERATOR FAIL LIGHT CAME ON AT THE SAME TIME. THE FLIGHT CREW DID A PRECAUTIONARY ENGINE SHUT DOWN AND RETURNED TO GRR. THE AIRCRAFT LANDED WITHOUT ANY OTHER PROBLEMS. AFTER CHECKING THE MECHANIC, FOUND A SHEARED GEARBOX DRIVE SHAFT. 2 H 7 2 4T 4 T A817 E297 1996110700004 19961107 00004 EU 1996 11 7 VTZA96332 1 19960827 A 5270 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGGAGE DOOR OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 306UE 41020 IAD/BOS - FLT 6290 - DURING TAKEOFF AT 1745 HRS ON 8-27-96, ABORTED TAKEOFF AT IAD DUE TO BAGGAGE DOOR WARNING LIGHT ILL UMINATED. AIRCRAFT RETURNED TO GATE. MAINTENANCE INSPECTED THE DOOR WARNING SYSTEM AND DEFERRED THE SYSTEM UNDER 52-3. PLACARD WAS INSTALLED IN THE AIRCRAFT. MAINTENANCE CLOSED DMI 55368 ON 8-28-96 BY ADJUSTING MICROSWITCH. AIRCRAFT WA S RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1996110700005 19961107 00005 NM 1996 11 7 W8PA960147 1 19961003 A 3350 LENS BOEING 737 7373S3 1384711 NM CABIN MISSING A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 375TA 23787 RIGHT AFT EMERGENCY EXIT LIGHT LENS IS OFF. RE-INSTALLED LENS. (X) 2 L 7 2 4F RT A16WE 1996110700006 19961107 00006 EU 1996 11 7 SIMA962691 1 19960925 A 3350 3012001 BATTERY PACK AEROSP ATR72 ATR72202 8680940 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 252AM 0873 253 ORD - FLT 4281 - EMERGENCY FLOOR LIGHT WILL NOT EXTINGUISH. REPLACED BATTERY PACK. AIRCRAFT WAS RETURNED TO SERVICE. ( X) 2 H 7 2 4T RT A53EU 1996110700007 19961107 00007 EU 1996 11 7 SIMA962661 2 19960922 A 7530 31148921 SWITCHING VALVE AEROSP ATR72 ATR72202 8680940 EU NR 2 ENGINE FAILED A SIMA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 252AM 253 ORD - FLT 4311 - CREW REPORTED STRANGE SMELL, AND SMELL OF SMOKE IN COCKPIT/CABIN. ALSO, GROUND PERSONNEL REPORTED SEEI NG WHITE SMOKE OUT OF RIGHT WHEELWELL. REPLACED P2.5/P3 SWITCHING VALVE. OPS CHECK GOOD WITH NO SMELL OF SMOKE OR STRA NGE SMELL IN COCKPIT OR CABIN. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1996110700008 19961107 00008 EU 1996 11 7 SIMA962772 1 19961003 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 213AT 3365 211 ORD - FLT 4055 - SECTION OF EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK 29WL. OPS CHECK GOOD. AIRCRAFT WAS RE TURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1996110700009 19961107 00009 SW 1996 11 7 96ZZZX5462 1 19960909 A 6220 222310461001 BEARING TORRINGTON BELL 222 222 1182122 SW M/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 30SV 160 47044 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X) 1 G 7 2 3U H9SW 1996110700010 19961107 00010 NE 1996 11 7 96ZZZX5463 2 19960606 A 7250 414129001 ROTOR ASSY BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE POWER TURBINE BLADE SHIFT A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 5188B 570 129 SC12053 7163 LE45757EF FAILED SB LT10172-10-0153. EXCESSIVE IBPT BLADE SHIFT. REPLACED WITH USED UNIT, CORRECTED PROBLEM. H5416Y-001. PART TOTAL CYCLES, 1,218.7. 1 G 7 2 3U 3 U H13EU E5NE10 1996110700011 19961107 00011 NE 1996 11 7 SIMA962791 2 19961005 A 7530 310848501 SWITCHING VALVE AEROSP ATR72 ATR72212 EU PWA PW120 PW127 NE NR 1 ENGINE FAILED A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 4AE 244 ORD - FLT 4323 - DURING TAXI, CABIN BECAME HAZY AND HAD AN ODOR OF SMOKE. NO EMERGENCY DECLARED AND PASSENGERS DEPLANED NORMALLY AT THE GATE AREA. REPLACED NR 1 ENGINE P2.5 P3 SWITCHING VALVE. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SE RVICE. (X) 2 H 7 2 4T 4 T RT A53EU E20NE 1996110700012 19961107 00012 NE 1996 11 7 96ZZZX5464 2 19960814 A 7321 0164448160 FUEL CONTL UNIT SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE MALFUNCTIONED A SQJA K NONE O OTHER IN INSP/MAINT 1 NE 03 68SA 2230 2363 4298 PILOT REPORTS 2 PERCENT NG FLUCTUATION WITH CORRESPONDING FLUCTUATION IN TOT AND TQ. REMOVED FUEL CONTROL TO PERFORM FU NCTIONAL CHECK AT TURBOMECA. P/N OFF 0164448160, S/N OFF B.625B. INSTALLED LOANER. P/N ON 0164448330, S/N ON 460B. ( X) 1 G 7 1 3U 3 U H9EU E19EU 1996110700013 19961107 00013 NE 1996 11 7 MALA965115 2 19960903 A 7260 6068T49P01 SEAL SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE RT ENGINE WORN A MALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 15 112XJ 340A112 FLT 3022 - EN ROUTE FROM DTW, RIGHT ENGINE OIL PRESSURE DEPLETED TO LESS THAN 3 PSI. THE CREW SHUT DOWN THE ENGINE, AND THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE STARTER/GENERATOR DRIVE SEAL. ALL CHECKS SATISFACTORY. (X) 2 L 7 2 4T 4 T RT A52EU E8NE 1996110700014 19961107 00014 WP 1996 11 7 96NK208 1 19960926 A 3260 CONNECTOR DOUG DC9 DC921 302205A WP LT MLG DNLOCK CORROSION A GTIA O A OTHER UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 GL 23 125NK 47302 LOG PAGE 028581. AIR RETURN. AFTER TAKEOFF, GEAR RETRACTED. LEFT MAIN LANDING GEAR INDICATED DOWN WITH NO RED (UNSAFE ) LIGHT. DOOR LIGHT WAS OUT. GEAR INDICATION NORMAL, LANDING NORMAL. CORRECTIVE ACTION: FOUND MINOR CORROSION IN LEF T MAIN GEAR DOWNLOCK SWITCH CONNECTOR. CLEANED CORROSION, SWUNG GEAR IAW DC-9MM, CHAPTER 32-60-0, 4 TIMES, OPS CHECKED GOOD. (X) 2 L 7 2 4F A6WE 1996110700015 19961107 00015 NM 1996 11 7 USAABB96037 1 19961002 A 2421 727792J IDG BOEING 757 7572B7 1384964 NM RT ENGINE FAILED A A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 616AU 4988 27147 ORD - FLT 104 - WHILE EN ROUTE SEA/PHL, CREW RECEIVED THE EICAS MESSAGE 'R GEN DRIVE.' APU GENERATOR WAS ON MEL. FLIGH T DIVERTED TO ORD AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT IDG DUE TO A SHAFT FAILURE. (X) 2 L 7 2 4F RT A2NM 1996110700016 19961107 00016 NE 1996 11 7 96ZZZX5465 2 19960719 A 7250 414129001 ROTOR ASSY BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE POWER TURBINE BLADE SHIFT A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 951AM 459 SC46870 7017 LE45291E FAILED SB LT101-72-10-0153. EXCESSIVE IBPT BLADE SHIFT. REPLACED WITH USED UNIT, CORRECTED PROBLEM. H3046HY-001. PAR T TOTAL CYCLES, 965.0. 1 G 7 2 3U 3 U H13EU E5NE 1996110700017 19961107 00017 NM 1996 11 7 RAAA96B2040 1 19961031 A 5320 65405124 FITTING BOEING 727 72722C 138400F NM BS 487.1 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED INSPECTION PER AD89-16-03, FOUND MAIN CARGO DOOR LATCH SUPPORT FITTING CRACKED, APPROXIMATELY 2 INCHES IN LENGTH, AT BS 487.1. REPLACED WITH P/N 65-93115-4 FITTING PER SB 727-53-A0177. 2 L 7 3 4F A3WE 1996110700018 19961107 00018 NM 1996 11 7 CALA9601533 1 19961011 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 570 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND CORROSION ON STRINGER 27L AT CABLE SUPPORT, STA 570. THE CORRODED SECTION WAS CUT OUT. A SPLICE WAS F ABRICATED AND INSTALLED IAW SRM 53-10-3. 2 L 7 3 4F A3WE 1996110700019 19961107 00019 NM 1996 11 7 CALA9601534 1 19961016 A 5330 SKIN BOEING 727 727232 1384082 NM BS 720 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND FORWARD CARGO COMPARTMENT CIRCUMFERENTIAL TO FUSELAGE SKIN ATTACHMENT CORRODED AT STA 720A BETWEEN STRI NGERS 28R AND 27L. THE CORRODED AREA WAS CUT OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-2. 2 L 7 3 4F A3WE 1996110700020 19961107 00020 NM 1996 11 7 CALA9601535 1 19961010 A 5321 FLOOR BOEING 727 727232 1384082 NM AFT LAV CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND LEFT AFT LAV FLOOR AREA HAD CORROSION IN SEVERAL AREAS AND UNDER MYLAR COVERING. THE FLOOR CORROSION W AS REMOVED. A REPLACEMENT WALL SUPPORT CHANNEL WAS FABRICATED AND INSTALLED IAW SRM 51-10-1. 2 L 7 3 4F A3WE 1996110700021 19961107 00021 NM 1996 11 7 CALA9601536 1 19961010 A 5312 BLKHD FASTENERS BOEING 727 727232 1384082 NM BS 1183 BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND THREE EACH RIVET HEADS BROKEN OFF AT BULKHEAD STA 1183 UPPER AFT WEB, LT SIDE. THE FASTENERS WERE REMOV ED AND REPLACED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996110700022 19961107 00022 NM 1996 11 7 CALA9601537 1 19961010 A 5752 TAB BOEING 727 727232 1384082 NM LT AILERON ERODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND LOWER OUTBOARD TRAILING EDGE OF LEFT INBOARD AILERON TAB ERODED. THE TAB WAS REMOVED AND THE ERODED AR EA WAS CUT OUT. AN ALUMINUM HONEYCOMB HOT BOND REPAIR WAS ACCOMPLISHED IAW SRM 51-40-6. THE TAB WAS BALANCED AND INSTAL LED. 2 L 7 3 4F A3WE 1996110700023 19961107 00023 NM 1996 11 7 CALA9601538 1 19961008 A 5754 SKIN BOEING 727 727232 1384082 NM NR 5 LE FLAP DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND A DENT WITH BONDING MATERIAL REPAIR ERODED IN NR 5 SLAT LEADING EDGE. A DOUBLER WAS FABRICATED AND INS TALLED IAW SRM 57-50-3, FIGURE 1, REPAIR 1. 2 L 7 3 4F A3WE 1996110700024 19961107 00024 NM 1996 11 7 CALA9601539 1 19961009 A 5751 SKIN BOEING 727 727232 1384082 NM RT AILERON DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND RT WING OUTBOARD AILERON LOWER SURFACE OUTBOARD TIP DELAMINATED. THE DELAMINATED AREA WAS CUT OUT AND A HOT BOND REPAIR WAS ACCOMPLISHED IAW SRM'S 51-40-6 AND 51-80-4. 2 L 7 3 4F A3WE 1996110700025 19961107 00025 WP 1996 11 7 9622919618 1 19961025 A 5320 FITTING DOUG DC9 DC932 3022066 WP COCKPIT WINDOW CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 618NW 47433 DURING M-CHECK, FOUND CORROSION ON THE LEFT SLIDING WINDOW LOWER AFT STOP PLATE. REPLACED FITTING AND PLATE PER SRM 51- 30-2. 2 L 7 2 4F A6WE 1996110700026 19961107 00026 WP 1996 11 7 9622929618 1 19961025 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 980-996 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 618NW 47433 DURING M-CHECK, FOUND CORROSION ON THE INTERCOSTAL AND SUPPORT FITTING AT LONGERON 27R, FS 980 - 996. REPLACED BOTH PER SRM 53-01. 2 L 7 2 4F A6WE 1996110700027 19961107 00027 WP 1996 11 7 9622939951 1 19961026 A 5320 FITTING DOUG DC9 DC932 3022066 WP MLG WW CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9347 45827 DURING H-CHECK, FOUND CORROSION ON BOTH THE LEFT AND RIGHT OUTBOARD BATHTUB FITTINGS IN THE MAIN LANDING GEAR WHEELWELLS . REPLACED FITTINGS PER SRM 51-01, PAR.1C. 2 L 7 2 4F A6WE 1996110700028 19961107 00028 WP 1996 11 7 9622949974 1 19961026 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 760 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9338 47347 DURING H-CHECK, FOUND CORROSION ON THE LEFT AND RIGHT SIDE KEEL BEAM FITTINGS AT FS 760 BULKHEAD. REPLACED FITTINGS PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996110700029 19961107 00029 WP 1996 11 7 9622959974 1 19961026 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 694 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9338 47347 DURING H-CHECK, FOUND CORROSION ON THE LONGERON 29L KEEL FITTING AT FS 694. REPLACED FITTING PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996110700030 19961107 00030 WP 1996 11 7 9622969974 1 19961028 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 729 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9338 47347 DURING H-CHECK, FOUND A CRACK IN THE LEFT KEEL FITTING AT FS 729. REPLACED FITTING PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996110700031 19961107 00031 NM 1996 11 7 9623125530 1 19961030 A 7930 OIL FILTER LIGHT BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE NR 1 ENGINE ILLUMINATED A NWAA D E RETURN TO BLOCK ENGINE SHUTDOWN N FALSE WARNING TX TAXI/GRND HDL 1 GL 01 530US 23845 716335 AFTER PUSHBACK, THE NR 1 ENIGNE OIL FILTER MESSAGE WAS DISPLAYED. AIRCRAFT RETURNED TO THE GATE AFTER ENGINE SHUTDOWN A ND RESTART. MESSAGE DID NOT REPEAT. GROUND MAINTENANCE INSPECTED AND REPLACED THE ENGINE OIL FILTER. NO CONTAMINATION WAS FOUND. 2 L 7 2 4F 4 F RT A2NM E17NE 1996110700032 19961107 00032 NM 1996 11 7 9623135512 1 19961029 A 7930 1B7361 SWITCH BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE NR 1 ENGINE MALFUNCTIONED A NWAA D E RETURN TO BLOCK ENGINE SHUTDOWN N FALSE WARNING TX TAXI/GRND HDL 1 GL 01 512US 7330 6672 23200 716466 DURING TAXI OUT, THE NR 1 ENIGNE OIL FILTER MESSAGE WAS DISPLAYED. THE NR 1 ENGINE WAS SHUT DOWN AND THE AIRCRAFT RETUR NED TO THE GATE. MAINTENANCE INSPECTED THE OIL FILTER AND FOUND NO CONTAMINATION. DIFFERENTIAL PRESSURE SWITCH WAS REM OVED AND REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 1996110700033 19961107 00033 WP 1996 11 7 9623149997 1 19961029 A 3231 LINK DOUG DC9 DC931 3022065 WP LT NLG DOOR BROKEN A NWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 01 8933E 47142 A LOUD BANG FOLLOWED BY VIBRATION FROM NOSE GEAR AREA OCCURRED DURING GEAR RETRACTION AFTER TAKEOFF. FLIGHT RETURNED TO RAMP AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT NOSE GEAR DOOR LINK BROKEN. REPLACED LINK. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996110700034 19961107 00034 WP 1996 11 7 9623159917 1 19961030 A 3260 UPLOCK SWITCH DOUG DC9 DC932 3022066 WP LT MLG MALFUNCTIONED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 967N 47573 DURING CLIMBOUT FROM ORD, THE LEFT MAIN GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. COCKPIT OPERATING MANUA L PROCEDURES WERE FOLLOWED AND LIGHT STAYED ON. FLIGHT WAS CONTINUED TO DESTINATION (MSP) AT REDUCED SPEED AND LANDED W ITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT MAIN GEAR UPLOCK SWITCH. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996110700035 19961107 00035 WP 1996 11 7 9623169923 1 19961030 A 3350 60030451 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN MALFUNCTIONED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 927RC 47469 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. OP ERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996110700036 19961107 00036 1996 11 7 9623179977 4 19961029 A 2565 113317 SLIDE DOUG DC9 DC931 3022065 WP CABIN DOOR LOW BATTERY A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9341 36169 5352 47390 DURING PERIODIC CHECK, FOUND MAIN CABIN DOOR EVACUATION SLIDE LIGHT BATTERY INOPERATIVE. REPLACED SLIDE. 2 L 7 2 4F A6WE 1996110700037 19961107 00037 WP 1996 11 7 9623189969 1 19961029 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9333 47246 DURING LINE MAINTENANCE INSPECTION, OVERHEAD EMERGENCY LIGHTING FROM FORWARD GALLEY TO ROW 4 WOULD NOT TEST. REPLACED B ATTERIES IN POWER SUPPLY. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996110700038 19961107 00038 WP 1996 11 7 9623199909 1 19961029 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 959N 47255 AFT EMERGENCY FLASHLIGHT WOULD NOT BLINK. REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996110700039 19961107 00039 SO 1996 11 7 COMA9610313 1 19961029 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 259CA 16775 1910 120252 SEVERAL EMERGENCY LIGHTS ARE DIM OR INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY. 2 L 7 2 4T RT A31SO 1996110700040 19961107 00040 1996 11 7 COMA9610314 4 19961028 A 3425 6226190204 AHC 85 EMB 120 EMB120RT SO E/E COMPT FAILED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 179CA 13802 120179 COPILOT'S AHRS FAILED. REPLACED THE AHC-85. 2 L 7 2 4T RT A31SO 1996110700041 19961107 00041 SO 1996 11 7 COMA9610315 1 19961029 A 5753 KRP138112VT ROLLER EMB 120 EMB120RT SO RT TE FLAP WORN A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 156CA 120156 FLAP DISAGREEMENT WARNING WHEN FLAPS RETRACTED. REPLACED THE RT OUTBOARD FLAP ROLLERS. 2 L 7 2 4T RT A31SO 1996110700042 19961107 00042 1996 11 7 COMA9630154 3 19961029 A 6140 INDICATION SAAB SF340 SF340A 7850100 EU LT PROP MALFUNCTIONED A COMA K NONE N FALSE WARNING TO TAKEOFF 1 SO 01 357CA 340A044 LEFT PROPELLER RPM INDICATED 1380 DURING TAKEOFF ROLL. COULD NOT DUPLICATE DISCREPANCY. 1380 RPM IS IN NORMAL OPERATIN G RANGE. 2 L 7 2 4T RT A52EU 1996110700043 19961107 00043 NM 1996 11 7 UPS96221469 1 19961014 A 5753 RIB BOEING 727 72722C 138400F NM RT TE MID FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE: C. CRACK ON INTERNAL TE RIB AT WBL 210 OF THE RT INBD MID-FLAP. REPAIR PER SRM 51-40-04 FIG 1. 2 L 7 3 4F A3WE 1996110700044 19961107 00044 NM 1996 11 7 UPS96221487 1 19961030 A 5320 6534144128 EXPANSION LINK BOEING 727 72725C 138400H NM BS 858-870 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: SI. CORROSION ON EXPANSION LINK STA 858-870 LBL 25 AROUND EACH NUTPLATE. CORROSION OUT OF LIMITS IAW 53-10-1. REPLACED EXPANSION LINK IAW SRM'S 51-10-1, 51-30-5 OHM 20-50-01 MM 20-50-02, 20-50-03. 2 L 7 3 4F A3WE 1996110700045 19961107 00045 NM 1996 11 7 UPS96221488 1 19961030 A 5313 STRINGER BOEING 727 72725C 138400H NM BS 462-466 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: SI. STR 26L CRACKED AND DENTED BS 462-466. REPAIRED STR 26L STA 462-466 IAW SRM 53-10-3. 2 L 7 3 4F A3WE 1996110700046 19961107 00046 NM 1996 11 7 UPS96221489 1 19961029 A 5711 SPAR BOEING 727 72725C 138400H NM LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: SI. CORROSION L/W LOWER SPAR CHORD IS CORRODED 28 TO 30 OF I/B END AT OUTER RADIUS. REPAIRED SPAR CH ORD (LOWER) IAW TRAMCO EWO 96-2549 (UPS EO FILE NR 727-57-1745). 2 L 7 3 4F A3WE 1996110700047 19961107 00047 NM 1996 11 7 UPS96221490 1 19961029 A 5744 6524646501 HINGE BOEING 727 72725C 138400H NM LT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: SI. L/W I/B AILERON CENTER (WING SIDE) HINGE FITTING IS CORRODED. REPLACED L/W I/B AILERON CENTER (WI NG SIDE) HINGE FITTING IAW MM 27-10-01. 2 L 7 3 4F A3WE 1996110700048 19961107 00048 NM 1996 11 7 UPS96221491 1 19961029 A 5755 659892435 FITTING BOEING 727 72725C 138400H NM NR 1 SPOILER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: SI. WHILE WORKING WINGS 499 CUSTOMER ID NR 598179 FOUND NR 1 SPOILER FITTING TO BE CORRODED. REMOVED AND REPLACED NR 1 SPOILER FITTING IAW MM 27-51-131, 27-61-81. TO BE OPS CHECKED ON NRC 597706. 2 L 7 3 4F A3WE 1996110700049 19961107 00049 NM 1996 11 7 UPS96221492 1 19961029 A 5230 69182036 INTERCOSTAL BOEING 727 72725C 138400H NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: SI. FWD CARGO DOOR AFT HINGE FWD INTERCOSTAL CRACKED. REMOVED AND REPLACED FWD CARGO DOOR AFT HINGE FWD INTERCOSTAL PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996110700050 19961107 00050 NM 1996 11 7 UPS96221493 1 19961028 A 5313 BAC1493508 STRINGER BOEING 727 72725C 138400H NM BS 740-783 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: SI. CORROSION ON STR 7 LEFT FROM BS 740-783. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-1, RE PAIRED PER SRM'S 51-20-51, 51-20-151, 51-30-2. 2 L 7 3 4F A3WE 1996110700051 19961107 00051 NM 1996 11 7 UPS96221494 1 19961028 A 5220 65210818 CASTING BOEING 727 72725C 138400H NM OVER WING EXIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: SI. CORROSION ON RT AFT OVERWING EXIT HANDLE FRAME ASSY CASTING. BEGAN REMOVING CORROSION AND FOUND FRAME CRACKED, REMOVED AND REPLACED FRAME IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1996110700052 19961107 00052 NM 1996 11 7 UPS96221495 1 19961027 A 5753 651859912 CARRIAGE BOEING 727 72725C 138400H NM NR 4 TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: SI. CORROSION NR 4 CARRIAGE HAS CORROSION INSIDE SPINDLE. CORROSION BEYOND ECONOMIC REPAIR, RECEIVED REPLACEMENT CARRIAGE, WILL ADVISE OF REPAIRS. 2 L 7 3 4F A3WE 1996110700053 19961107 00053 NM 1996 11 7 UPS96221496 1 19961027 A 5753 65192029 CARRIAGE BOEING 727 72725C 138400H NM NR 1 TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: SI. CORROSION AROUND THE THRUST WASHER ON NR 1 CARRIAGE. CORROSION FOUND BEYOND ECONOMICAL REPAIR, R ECEIVED REPLACEMENT CARRIAGE, WILL ADVISE OF REPAIRS. 2 L 7 3 4F A3WE 1996110700054 19961107 00054 NM 1996 11 7 UPS96221497 1 19961027 A 5311 FRAME BOEING 727 72725C 138400H NM BS 675 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: SI. CORROSION AT BS 675 ON FRAME AT STR 20A. REMOVED CORRSION, REWORK DEEMED OUT OF LIMITS, IAW SRM 53-10-1, REPAIRED FRAME STA 20 IAW SRM 51-40-2, STR CLIP AT STR 20 ALSO REPLACED. IAW SRM'S 51-30-2, 51-20-1. 2 L 7 3 4F A3WE 1996110700055 19961107 00055 NM 1996 11 7 UPS96221498 1 19961027 A 5753 69192029 CARRIAGE BOEING 727 72725C 138400H NM NR 8 TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE:SI CORROSION ON NO 8 FLAP CARRIAGE HAS BARE METAL AND CORROSION INSIDE SPINDLE CARRIAGE FOUND TO BE BEYOND ECONOMICAL REPAIR, RECEIVED REPLACEMENT CARRIAGE, WILL BE REPLACED ON TC C57-581-04-4D 2 L 7 3 4F A3WE 1996110700056 19961107 00056 NM 1996 11 7 UPS96221499 1 19961025 A 5313 BAC1498130 STRINGER BOEING 727 72725C 138400H NM BS 377 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: SI. CORROSION ON STR 22R BS 377. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-1, REPLACED STR P ER SRM'S 51-40-3, 53-10-3, 53-10-2, 51-40-3, 51-30-2. 2 L 7 3 4F A3WE 1996110700057 19961107 00057 NM 1996 11 7 UPS96221500 1 19961025 A 5315 BAC100246T6 FLOOR BEAM BOEING 727 72725C 138400H NM BS 328 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: SI. CORROSION ON STA 328 FLOORBEAM LBL 3 AND LNL 44 WL 207. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 51-10-6. REPLACED UPPER CHORD FLOOR BEAM PER SRM'S 53-10-8, 51-10-2, 53-10-8. 2 L 7 3 4F A3WE 1996110700058 19961107 00058 NM 1996 11 7 UPS96221501 1 19961025 A 5320 STRAP BOEING 727 72725C 138400H NM BS 385 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: SI. I/B SEAT TRACK SPLICE STRAP CORRODED STA 385 RBL 60.5 WL 206. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-8. REPLACED STRAP PER SRM'S 51-20-1, 51-10-2. 2 L 7 3 4F A3WE 1996110700059 19961107 00059 NM 1996 11 7 UPS96221502 1 19961025 A 5347 BAC15201432 SEAT TRACK BOEING 727 72725C 138400H NM BS 872 EXFOLIATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: SI. SEAT TRACK STA 872 LBL 25 WL 208 IS EXFOLIATED. REMOVED AND REPLACED SEAT TRACK FROM 870-1020 LB L 25 WL 208 IAW 53-10-1, 51-10-1, 51-10-2. 2 L 7 3 4F A3WE 1996110700060 19961107 00060 NM 1996 11 7 UPS96221503 1 19961025 A 5315 FLOOR BEAM BOEING 727 72725C 138400H NM BS 680 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: SI. CORROSION ON STA 680 FLOORBEAM BOTTOM SIDE OF UPPER CHORD LBL 25-RBL 25 WL 207. REMOVED CORROSIO N AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED, WILL ADVISE OF REPAIRS. 2 L 7 3 4F A3WE 1996110700061 19961107 00061 NM 1996 11 7 UPS96221504 1 19961024 A 5320 BAC15061706 STRAP BOEING 727 72725C 138400H NM BS 950-1166 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: SI. CORROSION AROUND NUTPLATE HOLES ON THE BL ZERO STABILIZER STRAP FROM BS 970-1166 WL 199-203. REM OVED CORRODED STABILIZER STRAP FROM BS 950-1160 AND INSTALLED NEW STABILIZER STRAP FROM BS 950-1160, ALL WORK DONE, IAW SRM'S 53-10-1, 51-30-8, 51-30-5, 51-30-2, 51-10-2, 51-10-6, MM 51-20-31. 2 L 7 3 4F A3WE 1996110700062 19961107 00062 NM 1996 11 7 UPS96221505 1 19961023 A 5311 FRAME BOEING 727 72725C 138400H NM BS 227 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: SI. CORROSION ON FRAME WEB STA 227 RBL 44 WL 208 TO 234. CORROSION WAS FOUND OUT OF LIMITS IAW SRM 5 3-10-1, REPAIRED FRAME WEB AT STA 227 IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1996110700063 19961107 00063 NM 1996 11 7 UPS96221506 1 19961023 A 5313 BAC1498143 STRINGER BOEING 727 72725C 138400H NM BS 863 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: SI. STR 4R CRACKED STA 863 RT FLANGE LIP. REPAIRED STR 4R STA 863 IAW SRM 51-30-2, 53-10-1, 53-10-3, AND MM 51-20-21, 51-20-31. 2 L 7 3 4F A3WE 1996110700064 19961107 00064 NM 1996 11 7 UPS96221507 1 19961023 A 5311 FRAME BOEING 727 72725C 138400H NM BS 251 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: SI. CORROSION ON FRAME WEB STA 251 RBL 48 WL 208 TO 228. REMOVED CORROSION. REWORK DEEMED OUT OF LI MITS IAW SRM 53-10-1, REPAIRED 251 FRAME IAW SRM'S 51-40-2 AND 51-30-2. 2 L 7 3 4F A3WE 1996110700065 19961107 00065 NM 1996 11 7 UPS96221508 1 19961021 A 5320 AND101331202 STIFFENER BOEING 727 72725C 138400H NM BS 211.8 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: SI. CORROSION ON STIFFENER BS 211.8 LBL 19 WL 165. FOUND CORROSION OUT OF LIMITS PER SRM 53-10-1, RE PLACED STIFFENER PER SRM'S 51-30-5, 51-30-2, 51-10-6, 51-10-2, 51-20-1. 2 L 7 3 4F A3WE 1996110700066 19961107 00066 NM 1996 11 7 UPS96221509 1 19961020 A 5311 FRAME BOEING 727 72725C 138400H NM BS 211.8 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: SI. CORROSION ON FRAME WEB BS 211.8 LBL 15-26 WL 165. REMOVED CORROSION FROM 211.8 FRAME WEB DOUBLER , REWORK DEEMED OUT OF LIMITS IAW SRM 53-10-1, REPLACED DOUBLER IAW SRM'S 51-30-5, 51-30-2, 51-20-1, ALSO, FOUND STIFFEN ERS TO BE CORRODED. REPLACED STIFFENERS IAW SAME ABOVE REFERENCES. 2 L 7 3 4F A3WE 1996110700067 19961107 00067 NM 1996 11 7 UPS96221510 1 19961020 A 5313 STRINGER BOEING 727 72725C 138400H NM BS 1070-1090 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: SI. CORROSION ON STR 4R STA 1070-1090 AND FRAME 1110-1130. REMOVED CORROSION FROM STR 4R STA 1070-10 90, STA 1110-1130. ALL REWORK WITHIN LIMITS EXCEPT STA 1121-1123, REPAIRED STR 4R 1121-1123 IAW SRM 53-10-3. 2 L 7 3 4F A3WE 1996110700068 19961107 00068 NM 1996 11 7 UPS96221511 1 19961020 A 5313 STRINGER BOEING 727 72725C 138400H NM BS 680-700 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: SI. CORROSION AT STRINGER 12 RIGHT HAND BETWEEN BS 680-700. FOUND CORROSION TO BE OUT OF LIMITS, REP LACED STRINGER PER SRM'S 53-10-1, 51-10-2, 51-10-6, 53-10-2, 53-10-3. 2 L 7 3 4F A3WE 1996110700069 19961107 00069 NM 1996 11 7 UPS96221512 1 19961020 A 5320 69177123 INTERCOSTAL BOEING 727 72725C 138400H NM BS 211.8-219.8 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE: SI. CORROSION ON INTERCOSTAL BS 211.8-219.8 LBL 25 WL 190. FOUND CORROSION TO BE OUT OF LIMITS PER S RM 53-10-1. REMOVED AND REPLACED INTERCOSTAL PER SRM 53-30-2. 2 L 7 3 4F A3WE 1996110700070 19961107 00070 NM 1996 11 7 UPS96221513 1 19961017 A 5311 FRAME BOEING 727 7271A7C 13840X2 NM BS 1203 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 935UP 20143 INSPECTION TYPE: C. LT WEB CRACKED, FRAME 1203, LBL 40 AT WL 220. REMOVED DAMAGED AREA, FABRICATED REPAIR DOUBLER AND FILLER PER SRM 51-40-2 AND INSTALLED REPAIR PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996110700071 19961107 00071 NM 1996 11 7 UPS96221515 1 19961020 A 5754 SKIN BOEING 727 7271A7C 13840X2 NM NR 4 LE SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 935UP 20143 INSPECTION TYPE: C. LT WING NR 4 SLAT SKIN TOP SIDE AT OTBD HOOK HAS SEVERAL CRACKS AROUND FASTENERS. STOP DRILLED CR ACK PER SRM 51-10-1. FABRICATED AND INSTALLED PLATE PER SRM 57-50-3. 2 L 7 3 4F A3WE 1996110700072 19961107 00072 NM 1996 11 7 UPS96421482 1 19961016 A 5210 HINGE ARM BOEING 747 747SR46 NM PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C. M.E.D. 1-L LWR HINGE-ARM: FOUND SMALL CRACK ON FWD FRAME. REPAIRED CRACK AT M.E.D. 1L LWR HINGE-A RM CUTOUT IAW SRM 52-10-02 FIG 12. 2 L 7 4 4F A20WE 1996110700073 19961107 00073 NM 1996 11 7 UPS96421483 1 19961016 A 5210 HANDLE PAN BOEING 747 747SR46 NM PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE: C. FOUND AT MAIN ENTRY DOOR 1 LT, A CRACK IN THE PAN OF THE OUTSIDE DOOR HANDLE. REPLACED PAN OF TH E OUTSIDE DOOR HANDLE 1 LT IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996110700074 19961107 00074 NM 1996 11 7 UPS96521481 1 19961027 A 5751 SKIN BOEING 757 75724APF 1384969 NM RT AILERON DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 407UP 23729 RT AILERON DELAMINATED ON OUTBOARD END TOP OF AILERON. REPAIRED RT AILERON OUTBOARD EDGE IAW EO B757-5760-8740. 2 L 7 2 4F RT A2NM 1996110700075 19961107 00075 WP 1996 11 7 UPS96821484 1 19961006 A 5752 5642831502 TAB DOUG DC8 DC871F 302199D WP RT AILERON DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE: C. RT AILERON CONTROL TAB DELAMINATED. REPLACED TAB ASSY PER MM 27-11-04. 2 L 7 4 4F RT 4A25 1996110700076 19961107 00076 WP 1996 11 7 UPS96821485 1 19961014 A 5713 2613844N STRINGER DOUG DC8 DC871F 302199D WP WS 508 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE: C. RT WING STRINGER 53 JUST INBOARD OF CANT STA 508 IS CRACKED. REPAIRED STRINGER PER SRM 57-2-2, SR M 57-2-0 AND UPS EO. 2 L 7 4 4F RT 4A25 1996110700077 19961107 00077 WP 1996 11 7 UPS96821486 1 19961010 A 5400 58039571 DOUBLER DOUG DC8 DC871F 302199D WP NR 1 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE: C. MOLD LINE DOUBLER HAS APPROX A 1.50 INCH LONG CRACK AT FWD EDGE INSIDE NR 1 PYLON FOOTSTOOL WS XFS 539. REPAIRED PER DOUGLAS DRAWING 5803955 AND UPS EO. 2 L 7 4 4F RT 4A25 1996110700078 19961107 00078 EU 1996 11 7 WWMA9600090 1 19961031 A 2150 7769105 ACM SAAB SF340 340B 7860101 EU RIGHT FAILED A WWMA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 15 356SB 64469 11469 340B356 WHEN THE RIGHT BLEED VALVE IS OPEN, AN OILY SOUR SMELL IS NOTICEABLY EVIDENT IN THE COCKPIT. WHEN THE RIGHT BLEED IS CL OSED, THE ODOR DISSIPATES. INSPECTED RT ENGINE INLET, COMPRESSOR SECTION AND HIGH AND LOW BLEED PORTS, AND FOUND NO SIGN OF OIL. INSPECTED RT ACM AND FOUND SHAFT DIFFICULT TO ROTATE. REPLACED RT ACM IAW SAAB MTX WORK CARD 1753 FCK GOOD. 2 L 7 2 4T RT A52EU 1996110700079 19961107 00079 EU 1996 11 7 WWMA9600089 1 19961030 A 2611 72111121000 DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT DIRTY A WWMA K NONE N FALSE WARNING NR NOT REPORTED 1 WP 15 231LN 340B231 CREW REPORTED INTERMITTENT CARGO SMOKE WARNING LIGHT WITH TRIPLE STROKE CHIME, ONLY WHEN BLEEDS ARE OFF. CLEANED FWD AN D AFT CARGO SMOKE DETECTORS IAW SMM 2613, FCK GOOD. 2 L 7 2 4T RT A52EU 1996110700080 19961107 00080 EU 1996 11 7 WWMA9600088 1 19961026 A 5610 7256100501 WINDSHIELD SAAB SF340 340B 7860101 EU LT COCKPIT CRACKED A WWMA K NONE O OTHER NR NOT REPORTED 1 WP 15 261AE 3082 340B261 CREW REPORTED THE CAPTAIN'S WINDSHIELD HAS NUMEROUS VERTICAL AND HORIZONTAL CRACKS IN THE OUTER PANE. REPLACED CAPTAIN' S WINDSHIELD IAW SAAB AMM. 2 L 7 2 4T RT A52EU 1996110700081 19961107 00081 WP 1996 11 7 WWMA9600091 2 19961022 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LEFT FAILED A WWMA O OTHER X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 WP 15 951AE 6510 689 951 P66362 ON TAXI, THE LEFT ENGINE FLAMED OUT. THE LEFT ENGINE OIL PRESSURE PUMP/FUEL CONTROL DRIVE WOULD NOT ROTATE WHEN THE ENGI NE WAS TURNED. THE ENGINE WAS RETURNED TO OVERHAUL FACILITY FOR REPAIR. 2 L 7 2 4T 4 T RT A56EU E4WE 1996110700082 19961107 00082 NM 1996 11 7 96FDEA01628 1 19961029 A 5320 651594024 BEAM BOEING 727 72722 1384002 NM BS 740 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 150FE 19141 NR 0253 002, WHILE WORKING CUSTOMER CARD NR 0172 FOUND CORROSION ON UPPER SURFACE OF L-ANGLE BS 740 WL 170 LBL 30 TO RBL 25. *S/D* REPAIRED L-ANGLE AT BS 740 WL 170 LBL 30 TO RBL 25 IAW FEDEX EZ 7-5310-31159. 2 L 7 3 4F A3WE 1996110700083 19961107 00083 NM 1996 11 7 96FDEA01629 1 19961029 A 5320 6566127 BEAR STRAP BOEING 727 72722 1384002 NM BS 1110 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 150FE 19141 NR 0108 003, CORROSION IN AFT CARGO BAY ON FWD SIDE OF FRAME ON INTERNAL SURFACE OF BEAR STRAP AT BS 1110 RLB 30 TO 45 W L 146 TO 156. *S/D* REPAIRED BEAR STRAP AT BS 1110 RBL 30 TO 45 WL 146 TO 156 IAW FEDEX EA 7-5330-31236. 2 L 7 3 4F A3WE 1996110700084 19961107 00084 NM 1996 11 7 96FDEA01630 1 19961029 A 5315 652083332 FLOORBEAM BOEING 727 727233 138408A NM BS 1030 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20939 NR 0648 023, CORROSION (C53-224-01) ON FLOORBEAM AT BS 1030 RBL 48 TO RBL 55. *S/D* REMOVED CORROSION FROM FLOORBEAM A T BS 1030 RBL 48 TO RBL 55. BEAM OUT OF LIMITS IAW FEDEX 727 SRM 53-10-1, REPAIRED BEAM IAW FEDEX 727 SRM 53-10-8. 2 L 7 3 4F RT A3WE 1996110700085 19961107 00085 NM 1996 11 7 96FDEA01631 1 19961029 A 5320 651630567 WEB BOEING 727 727233 138408A NM BS 219.8 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 NR 742 122, CORROSION ON AFT SIDE OF WEB STA 219.8 LBL 42 WL 210 TO 232. *S/D* REPAIRED WEB DOUBLER BS 219.8 LBL 42 WL 210 TO 232 PER FEDEX SRM 51-40-2. 2 L 7 3 4F RT A3WE 1996110700086 19961107 00086 NM 1996 11 7 96FDEA01632 1 19961028 A 5320 69157723 INTERCOSTAL BOEING 727 727233 138408A NM BS 219.8-227 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 NR 0119 021, CORROSION (C53-111-01-1) NOSE E-BAY INTERCOSTAL BS 219.8 TO 227 LBL 20 WL 163 TO 167. *S/D* REPLACED INTE RCOSTAL NOSE E-BAY BS 219.8 TO 227 LBL 20 WL 163 TO 167 PER FEDEX SRM 51-10-1. 2 L 7 3 4F RT A3WE 1996110700087 19961107 00087 NM 1996 11 7 96FDEA01633 1 19961029 A 5320 651627910 BEAM BOEING 727 727233 138408A NM BS 740-848 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 NR 0711 020. CORROSION (C53-224-01(2) ON LONGITUDINAL BEAM AT BS 740 TO BS 812 AND BS 825- TO BS 840 RBL 25 WL 208 P/N 65-16279-10. REMOVED AND REPLACED LONGITUDINAL BEAM AT BS 740-850, RBL 25, WL 208. 2 L 7 3 4F RT A3WE 1996110700089 19961107 00089 NM 1996 11 7 96UAL900813 1 19961021 A 3350 BULB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 512UA 24809 EMERGENCY EXIT LIGHT INOP ROW 33 ABC. RELAMPED EMERGENCY EXIT LIGHT. OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996110700090 19961107 00090 NM 1996 11 7 96UAL900824 1 19961021 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 185UA 25395 UPPER DECK LEFT HAND ESCAPE DOOR BATTERY TEST INOP. REPLACED BATTERY PACK. 2 L 7 4 4F 4 F RT A20WE E24NE 1996110700091 19961107 00091 1996 11 7 96UAL900825 4 19961021 A 2310 HF RADIO BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE RIGHT MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 606UA 21867 DIVERTED TO GLA DUE TO BOTH HF RADIOS BEING INOPERABLE. WHEN THE LEFT AND RIGHT HF RADIOS WERE TESTED, THE LEFT HF OPER ATED NORMALLY, AND THE RIGHT HF WOULD TRANSMIT BUT NOT RECEIVE. REPLACED RIGHT TRANSCEIVER, COUPLER, AND RADIO SELECTOR PANEL. SPECIFIC UNIT CAUSING THE PROBLEM IS UNKNOWN. OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 1996110700092 19961107 00092 NM 1996 11 7 96UAL900826 1 19961021 A 2421 745329C IDG BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT ENGINE MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 658UA 27113 DIVERTED TO MIA UNDER AMBER ALERT DUE TO GENERATOR INDICATION PROBLEM. *S/D* THE LEFT ENGINE INTEGRATED DRIVE GENERATO R WAS BELIEVED TO BE AT FAULT. THE LEFT ENGINE IDG WAS REPLACED, OPERATIONS CHECK NORMAL. THE SHOP FOUND NOTHING WRONG WITH THE REMOVED IDG. 2 L 7 2 4F 4 F RT A1NM E24NE 1996110700093 19961107 00093 NM 1996 11 7 96UAL900827 1 19961021 A 3610 BACC10EZ2125BE CLAMP BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE NR 3 ENGINE FAILED A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 154UA 20103 FIRE DETECTION FAULT B-LOOP ON NR 3 ENGINE, RECEIVED INTERMITTENT FIRE WARNING. *S/D* SUSPECT AIR LEAK AT PNEUMATIC DU CT CLAMP. REPLACED DUCT CLAMP, ADDITIONALLY REPLACED PRESSURE RELIEF VALVE AS PRECAUTIONARY. 2 L 7 4 4F 4 F A20WE E20EA 1996110700094 19961107 00094 NM 1996 11 7 96UAL900828 1 19961022 A 2910 BACH6P0260CCN HOSE ASSY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE VERT STAB LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 7264U 21411 RETURNED TO MCO DUE TO HYDRAULIC FLUID LOSS. FLUID IS RUNNING DOWN VERTICAL FIN AND RUDDER. PUMPS RAN FOR 4 MINUTES WI TH ZERO QUANTITY AND PRESSURE. REPLACED LEAKING HYDRAULIC LINE IN LEFT VERTICAL STABILIZER AREA. ALSO, REPLACED BOTH A -HYDRAULIC ENGINE DRIVEN PUMPS AND CASE DRAIN FILTERS. SERVICED SYSTEM, RAN ENGINES AND NOTED NO LEAKS. 2 L 7 3 4F 4 F A3WE E2EA 1996110700095 19961107 00095 WP 1996 11 7 96UAL900829 1 19961022 A 3220 ACG7006501 TQ LINK BUSHING DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NLG BROKEN A UALA O OTHER E VIBRATION/BUFFET LD LANDING 1 WP 29 1859U 47819 SLIGHT NOSE WHEEL SHIMMY ON ROLLOUT DURING LANDING. *S/D* REPLACED LOWER NOSE GEAR TORQUE LINK DUE TO BROKEN BUSHING A T DISCONNECT. 2 L 7 3 4F 4 F A22WE E23EA 1996110700096 19961107 00096 WP 1996 11 7 96UAL900830 1 19961022 A 2130 ABM7012505 CHECK VALVE DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 3 AC SYSTEM FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 1844U 48260 DIVERTED TO HNL WHEN UNABLE TO MAINTAIN CABIN PRESSURE. CHANGED PLANES. *S/D* A DUCT SUPPORT ROD FAILED WHICH CAUSED DUCT MISALIGNMENT AND SUBSEQUENT AIR LOSS. THEN THE BULKHEAD CONDITIONED AIR CHECK VALVE FAILED. THEREFORE, CABIN PRES SURE COULD NOT BE MAINTAINED. THE SUPPORT ROD WAS REPAIRED AND THE CHECK VALVE WAS REPLACED. 2 L 7 3 4F 4 F A22WE E23EA 1996110700097 19961107 00097 NM 1996 11 7 96UAL900831 1 19961022 A 5314 6562125 KEEL BEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE BS 517 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 902UA 16822 25002 A SMALL AMOUNT OF CORROSION WAS FOUND ON THE LEFT HAND KEEL BEAM OUTBOARD HORIZONTAL FLANGE AT STATION 517. THE CORROSIO N HAS BEEN REMOVED AND THE RESULTING BLEND IS APPROXIMATELY .75 INCH LONG BY .50 INCH WIDE, AND APPROXIMATELY .022 INCH DEEP. THE CORRODED AREA WAS BLENDED TO REMOVE ALL EXISTING CORROSION AND STRESS CONCENTRATION AND ROTO PEENED TO IMPROV E THE FUTURE FATIGUE LIFE. THE PART WAS ALODINED, PRIMED WITH TWO COATS OF PRIMER AND CORROSION INHIBITING COMPOUND WAS APPLIED. A BOEING NO TECHNICAL OBJECTION WAS RECEIVED FOR THIS DEVIATION. 2 L 7 2 4F 4 F RT A16WE E2GL 1996110700098 19961107 00098 NM 1996 11 7 96UAL900832 1 19961022 A 5610 5893543110 WINDSHIELD BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE RT COCKPIT CRACKED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 7267U 21414 OUTER PANE OF COPILOT'S WINDSHIELD CRACKED. REPLACED COPILOT'S WINDSHIELD DUE TO A CRACK. CRACK EMANATED FROM ARC IN W INDOW HEAT BUS BAR. 2 L 7 3 4F 4 F A3WE E2EA 1996110700100 19961107 00100 1996 11 7 96UAL900834 4 19961023 A 2210 DPXAMA57335 COUPLER BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE RUDDER CORRODED A UALA O OTHER F FLT CONT AFFECTED DE DESCENT 1 WP 29 9054U 19935 AT FL310 GOT A YAW DAMPER KICK THAT STARTED A OSCILLATION THAT KEPT GETTING STRONGER. AIRCRAFT FELT LIKE IT WANTED TO R OLL TO THE LEFT. TURNED YAW DAMPER OFF, STILL HAD SOME OSCILLATION, RECOVERED WITH AILERON CONTROL. AIRCRAFT NORMAL RE ST OF DESCENT. *S/D* THE MAIN RUDDER POWER CONTROL UNIT AND THE YAW DAMPER COUPLER WERE REPLACED. FURTHER INVESTIGATI ON FOUND CORROSION ON THE D295 BENCH PLUG OF THE YAW DAMPER COUPLER. 2 L 7 2 4F 4 F A16WE E2EA 1996110700101 19961107 00101 NM 1996 11 7 96UAL900835 1 19961025 A 2530 OVEN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE GALLEY FIRE A UALA O OTHER A FLAME/FIRE CR CRUISE 1 WP 29 648UA 25285 A SMALL FIRE OCCURRED IN THE AFT GALLEY OVEN. *S/D* FOOD SPILLED ONTO THE BOTTOM OF THE OVEN INSERT RESULTING IN A SM ALL FIRE. THE FIRE WAS EXTINGUISHED WITH A HALON FIRE EXTINGUISHER. THE OVEN WAS NOT DAMAGED AS A RESULT OF THIS INCID ENT, OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 1996110700102 19961107 00102 NM 1996 11 7 96UAL900836 1 19961025 A 2560 D31038112 SLIDE REGULATOR AIR CRUISERS BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN CORRODED A A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 DURING OVERHAUL OF SLIDE, INFLATION REGULATOR FAILED. REGULATOR AND ASPIRATORS SHOWED SIGNS OF HEAVY CORROSION. DISASS EMBLY OF REGULATOR REVEALED FOD WAS PREVENTING NORMAL OPERATION OF THE REGULATOR. 2 L 7 2 4F 4 F RT A2NM E17NE 1996110700103 19961107 00103 NM 1996 11 7 SRAA961014 1 19961026 A 3230 TILT MECH BOEING 747 747212B 1384886 NM RT MLG MALFUNCTIONED A SRAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 745SJ 20888 DURING FLIGHT202 INTO BOG. THE RIGHT BODY GEAR TILT PRIMARY INDICATING SYSTEM INDICATED GEAR NOT TILT, AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED AIRCRAFT AND FOUND SAFE FOR GEAR DOWN FERRY FLIGHT TO MIA. AIRCRAFT ARRIVED IN MIA WITHOUT INCIDENT. DUE TO LACK OF EQUIPMENT TO ACCOMPLISH REPAIR, AIRCRAFT WAS FERRIED TO MOBILE, AL. AIRCRAFT LANDED AT BFM W ITHOUT INCIDENT. PLACED AIRCRAFT ON JACKS AND PERFORMED RETRACTION TEST, FOUND RIGHT BODY GEAR WOULD NOT TILT, REPLACED RIGHT BODY GEAR TILT SENSOR, ACTUATOR BRACKET, CONDUIT, AND SENSOR BRACKET. SYSTEM OPS CHECKED GOOD. 2 L 7 4 4F A20WE 1996110700106 19961107 00106 CE 1996 11 7 96ZZZX5467 1 19960926 A 5522 9661000611 LOWER SKIN 96610006617 BEECH 58 58 1152740 CE LEFT ELEVATOR CRACKED A P HRMA K NONE O OTHER IN INSP/MAINT 1 NE 01 5565D 1979 TH1552 FOUND LOWER SKIN OF LEFT ELEVATOR CRACKED. THE CRACK RADIATES OUT FROM THE TRAILING EDGE OF THE SKIN FORWARD. IT IS AB OUT 4 INCHES LONG. IT STARTS AT THE OUTBOARD CORNER OF THE CUT-OUT FOR THE TRIM TAB. 1 L 7 2 3O 3A16 1996110700186 19961107 00186 NM 1996 11 7 RAAA96B2041 1 19961031 A 5350 65395031 FAIRING DOOR BOEING 6522554 BOEING 727 72722C 138400F NM BS 740 MISSING A RAAA K NONE D INFLIGHT SEPARATION DE DESCENT 1 AL 03 832RV NSN 19098 ON DESCENT, AT 25,000 FT LOUD BANG SOUNDED IN CARGO COMPARTMENT AREA. CHECKED AREA, APPEARED NORMAL. AFTER LANDING AT AKN FOUND BODY FAIRING SECTION 46 ACCESS DOOR NR 3401 AT BS 740 MISSING. REPLACED ACCESS DOOR NR 3401 AT AKN AND RETURN ED TO ANC. REPLACED ACCESS DOOR NR 3301 DUE IMPACT DAMAGE FROM UNKNOWN SOURCE AND WING TO BODY FAIRING BS 737 TO 780 LT AND RT. 2 L 7 3 4F A3WE 1996110700187 19961107 00187 WP 1996 11 7 CALA9601540 1 19961031 A 2910 7936907603 HYD LINE DOUG DC9 DC982 3022082 WP LT THRUST REVER BROKEN A CALA O OTHER B K J SMOKE/FUMES/ODORS/SPARKS FLUID LOSS WARNING INDICATION LD LANDING 1 SW 09 819NY 49479 THE LEFT HYDRAULIC SYSTEM QUANTITY AND PRESSURE DROPPED TO ZERO AND THE CABIN FILLED WITH SMOKE DURING LANDING ROLLOUT. THE PACKS AND BLEEDS WERE CLOSED AND CABIN DOORS WERE OPENED TO CLEAR SMOKE. THE AIRCRAFT WAS TOWED TO THE GATE. MAIN TENANCE FOUND THE LINE TO THRUST REVERSER LOW PRESSURE SWITCH BROKEN. THE LINE WAS REPLACED AND LEAK CHECK WAS GOOD. 2 L 7 2 4F A6WE 1996110700188 19961107 00188 WP 1996 11 7 CALA9601541 1 19961031 A 3610 5958765503 DUCT DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9 52048 NE NR 2 ENGINE CRACKED A CALA O OTHER J WARNING INDICATION TO TAKEOFF 1 SW 09 14524 47539 665611 THE NR 2 ENGINE FIRE WARNING LIGHT AND BELL ACTIVATED SHORTLY AFTER TAKEOFF. THE FIRE WARNING CEASED AFTER THE ENGINE T HROTTLE WAS RETARDED LESS THAN TEN PERCENT. BOTH FIRE LOOPS TESTED NORMAL AND ALL ENGINE INDICATIONS WERE NORMAL. THE FLIGHT CONTINUED AT NORMAL POWER SETTINGS WITH NO FURTHER OCCURANCE OF FIRE WARNING. MAINTENANCE FOUND THE NR 2 ENGINE 13TH STAGE SADDLE DUCT CRACKED AT ANTI-ICE FLANGE. THE DUCT WAS REPLACED AND LEAK CHECK WAS GOOD. 2 L 7 2 4F 4 F A6WE E2EA 1996110700189 19961107 00189 NM 1996 11 7 CALA9601542 1 19961031 A 2910 65445101708 HYD LINE BOEING 737 737130 1384435 NM RT ENGINE LEAKING A CALA O OTHER K J B FLUID LOSS WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 09 77215 19032 THE A-HYDRAULIC SYSTEM QUANTITY GRADUALLY DECREASED TO 1 GALLON WHILE EN ROUTE. THE A-SYSTEM HYDRAULIC PUMPS WERE TURNE D OFF. WHEN THE PUMPS WERE TURNED ON TO LOWER FLAPS THE SYSTEM FAILED AND SMOKE ENTERED THE CABIN. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND THE A-SYSTEM HYDRAULIC RETURN LINE ON RIGHT ENGINE LEAKING. THE LINE WAS R EPLACED AND LEAK CHECK WAS GOOD. THE HYDRAULIC SYSTEM WAS SERVICED AND BOTH THE LEFT AND RIGHT COALESCER BAGS WERE REMO VED AND REPLACED. 2 L 7 2 4F A16WE 1996110700190 19961107 00190 EU 1996 11 7 9622033203 1 19961023 A 3350 321454 POWER SUPPLY AIRBUS 320 A320211 3930320 EU CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 303US 13680 8731 34 DURING LINE MAINTENANCE, THE LEFT AFT EPSU FAULTED THE BATTERY INTERNAL AND EXTERNAL LOADS. REPLACED POWER SUPPLY, OPER ATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996110700191 19961107 00191 NM 1996 11 7 9623206626 1 19961031 A 3510 OXYGEN SYST BOEING 747 747251B 1384892 NM COCKPIT LEAKING A NWAA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 01 626US 21708 DURING CRUISE, THE FLIGHT CREW'S OXYGEN DEPLETED. AIRCRAFT DIVERTED TO ANC AND LANDED WITHOUT INCIDENT. REPLACED THE C REW OXYGEN CYLINDER, CAPTAIN'S OXYGEN MASK AND FIRST OBSERVER'S OXYGEN PANEL, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996110700192 19961107 00192 EU 1996 11 7 9623213236 1 19961031 A 3350 321430 BATTERY AIRBUS 320 A320212 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 336NW 355 DURING THE LINE MAINTENANCE EMERGENCY LIGHTS TEST, THE FOLLOWING MESSAGES DISPLAYED: INT LOADS AFT L, COMM FWD L, BATTE RY AFT L, EMER L, COMM AFT L. REPLACED AFT LEFT BATTERY PACK, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996110700193 19961107 00193 NM 1996 11 7 9623226307 1 19961031 A 3350 CONNECTOR BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 667US 24222 DURING LINE CHECK, FOUND LEFT FLOOR EMERGENCY LIGHTS INOPERATIVE FROM ROWS 35 TO 43. RECONNECTED LIGHT ASSEMBLY AT ROW 43, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1996110700194 19961107 00194 WP 1996 11 7 9623239102 1 19961030 A 5270 DOOR WARNING DOUG DC9 DC915 3022036 WP CABIN ACTIVATED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 92S 47064 DURING TAKEOFF, THE AFT CABIN DOOR LIGHT ILLUMINATED. AIRCRAFT ABORTED TAKEOFF. VISUALLY INSPECTED AND OPERATIONALLY C HECKED AFT CABIN DOOR. NO DEFECTS FOUND, OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996110700195 19961107 00195 NM 1996 11 7 SWAA961172 1 19961024 A 5320 FRAME BOEING 737 7372H4 138448C NM SERV DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 28SW 21339 DURING SCHEDULED B2 CHECK, FWD SERVICE DOORWAY FWD UPPER STUB FRAME CRACKED .5, JUST FWD OF UPPER STOP ASSEMBLY. REPAIR ED PER SWA RA 1-253-1547. 2 L 7 2 4F A16WE 1996110700196 19961107 00196 1996 11 7 SWAA961173 4 19961024 A 2565 22DD229000131 SLIDE BOEING 737 7372H4 138448C NM R1 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 53SW 21534 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR SLIDE PRESSURE BELOW SERVICEABLE LIMITS. REPLACED SLIDE PER BOEING M/M. 2 L 7 2 4F A16WE 1996110700197 19961107 00197 NM 1996 11 7 SWAA961174 1 19961025 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 440 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED TERMINAL CHECK, FOUND FUSELAGE SKIN PUNCTURED AND TORN AT BS 440 S27L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996110700198 19961107 00198 NM 1996 11 7 SWAA961175 1 19961023 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 907 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 60SW 21812 DURING SCHEDULED D-CHECK, FOUND STRINGERS 21R AND 22R CORRODED AT BS 907. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996110700199 19961107 00199 NM 1996 11 7 SWAA961176 1 19961023 A 5320 WEB BOEING 737 7372H4 138448C NM BS 1148 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 60SW 21812 DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AT BS 1148 S5R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996110700200 19961107 00200 NM 1996 11 7 SWAA961177 1 19961023 A 5320 CHORD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 60SW 21812 DURING SCHEDULED D-CHECK, FOUND BS 178 SIDE CHORD CRACKED ON LEFT SIDE AT WL 200. REPAIRED PER TRAMCO EWO 96-0527. 2 L 7 2 4F A16WE 1996110700201 19961107 00201 NM 1996 11 7 SWAA961178 1 19961023 A 5320 BEAM BOEING 737 7372H4 138448C NM BS 639 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 60SW 21812 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM AT BS 639, LBL 65, WL 208 CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996110700202 19961107 00202 NM 1996 11 7 SWAA961179 1 19961028 A 5330 SKIN BOEING 737 7372H4 138448C NM SERV DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 61SW 21970 DURING SCHEDULED B2 CHECK, FOUND FUSELAGE SKIN CRACKED .25 AT AFT SERVICE DOOR UPPER HINGE CUTOUT. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996110700203 19961107 00203 NM 1996 11 7 SWAA961180 1 19961025 A 2120 AIR DISTR BOEING 737 7372H4 138448C NM AFT GALLEY ODOR A SWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 68SW 22357 ON LANDING, F/A NOTED AN ELECTRICAL TYPE ODOR IN AFT GALLEY. AFT GALLEY C/B'S PULLED. INSPECTED AREA AND COFFEEMAKERS, RESET C/B'S AND NO PROBLEMS NOTED. 2 L 7 2 4F A16WE 1996110700204 19961107 00204 NM 1996 11 7 SWAA961181 1 19961023 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 986.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED A-CHECK, FOUND A FUSELAGE SKIN CRACK AT BS 986.5, JUST BELOW S20L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996110700205 19961107 00205 NM 1996 11 7 SWAA961182 1 19961028 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED C1 CHECK, FOUND A FUSELAGE SKIN CRACK AT AFT LRRA ANTENNA AREA, FWD RIVET. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996110700206 19961107 00206 NM 1996 11 7 SWAA961183 1 19961028 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED C4 CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING AT ROW 3DEF INOP. REPLACED LIGHT ASSEMBLY PER BOEING M/ M. 2 L 7 2 4F RT A16WE 1996110700207 19961107 00207 NM 1996 11 7 SWAA961184 1 19961028 A 5320 STRAP BOEING 737 7373H4 1384600 NM ENTRY DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED C4 CHECK, FOUND FLOORBEAM STRAP UNDERNEATH FWD ENTRY DOOR CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996110700208 19961107 00208 NM 1996 11 7 SWAA961185 1 19961028 A 3350 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 352SW 24888 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY LIGHTS IN AFT GALLEY AREA INOP. REPLACED LEFT AFT BATTERY PACK PER BOEI NG M/M. 2 L 7 2 4F RT A16WE 1996110700209 19961107 00209 NM 1996 11 7 SWAA961186 1 19961025 A 3397 WIRE BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 399SW 27693 DURING PRE-FLIGHT CHECK, FOUND 3 EMERGENCY EXIT TRACK LIGHTS INOP. RESPLICED WIRES AND OP CHECKED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996110700210 19961107 00210 NM 1996 11 7 SWAA961187 1 19961028 A 3397 WIRE BOEING 737 7373T0 1384582 NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 684WN 23941 DURING PRE-FLIGHT CHECK, FOUND EMERGENCY EXIT FLOOR TRACK LIGHTS AT EXIT INOP. REPAIRED BROKEN WIRES AND OP CHECKED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996110700211 19961107 00211 NM 1996 11 7 SWAA961188 1 19961028 A 5330 SKIN BOEING 737 737317 138447P NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE LOWER SKIN CORROSION BULGING BETWEEN BS 727 TO 727A, S28L. REPAIRED PER SWA R A 1-353-1465. 2 L 7 2 4F RT A16WE 1996110700212 19961107 00212 NM 1996 11 7 SWAA961189 1 19961028 A 5330 SKIN BOEING 737 737317 138447P NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CORROSION BULGING BETWEEN FASTENERS AT BS 727 TO 727A AT STRINGER 27R. R EPAIRED PER SWA RA 1-353-1544. 2 L 7 2 4F RT A16WE 1996110700213 19961107 00213 NM 1996 11 7 SWAA961190 1 19961028 A 3350 LIGHTS BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 512SW 24189 DURING WALKAROUND, FOUND EMERGENCY FLOOR TRACK LIGHTING INOP AT ROW 7. RELAMPED AND OP CHECKED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996110700214 19961107 00214 NM 1996 11 7 SWAA961191 1 19961025 A 3350 20131 BATTERY BOEING 737 7375H4 138449D NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 520SW 25319 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996110700215 19961107 00215 EU 1996 11 7 96FDEA01634 1 19961029 A 5230 ACTUATOR ROD AIRBUS 310 A310221 3930310 EU CARGO DOOR SHEARED A FDEA K NONE O OTHER CR CRUISE 1 SO 25 419FE 345 REPORTED BY RAMP PERSONNEL. WHILE OPENING THE MDC DOOR. A LOUD SOUND WAS HEARD. MX DISCOVERED THAT THE MDC DOOR ACTUA TOR ROD-END SHEARED. *S/D* REMOVED AND REPLACED MDC DOOR ACTUATOR PER M/M 52-36-27 AND TESTED PER M/M 52-36-00, CHECK OK. 2 L 7 2 4F RT A35EU 1996110700216 19961107 00216 NM 1996 11 7 96FDEA01635 1 19961021 A 5313 65C2534017 STRINGER BOEING 727 727233 138408A NM BS 720 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 NR 0152 025. CRACKED STRINGER AT BS 720 B AND 3 STRINGER 15 LT. REMOVED AND REPLACED CRACKED STRINGER AT BS 720B PLUS 3 TO 720C STR 15 LT IAW FEDEX SRM 53-10-3 FIG 1 DETAIL II. 2 L 7 3 4F RT A3WE 1996110700217 19961107 00217 NM 1996 11 7 96FDEA01636 1 19961030 A 5313 65C253418 STRINGER BOEING 727 727233 138408A NM BS 720 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 NR 0153 024. CRACKED STRINGER AT STA 720 B PLUS 3 STRINGER 15 RT. REPAIRED STRINGER AT BS 720B PLUS 3 STR 15 RT PER F ED EX SRM 53-10-03. 2 L 7 3 4F RT A3WE 1996110700218 19961107 00218 WP 1996 11 7 96FDEA01637 1 19961031 A 5330 SKIN DOUG DC10 DC1010F 3022111 WP BS 1159 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 050FE 47804 SNRM 00152, FUSELAGE SKIN HAS A 5 INCH CRACK AT STA 1159 STR L-37. *S/D* NDT VERIFIED END OF CRACK, STOP DRILLED CRACK PER EA NR 8-5340-31737. FABRICATED DOUBLER AS PER DAC PRINT 53-40-00. OK TO INSTALL DOUBLER QA-20, INSTALLED REPAIR D OUBLER, REF SRM 53-40-00. 2 L 7 3 4F A22WE 1996110700219 19961107 00219 WP 1996 11 7 96FDEA01602 1 19961023 A 5320 ANB73871 FRAME DOUG DC10 DC1030 3023501 WP CRT MLG DOORWAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 317FE 46835 SNRM N 00335, CENTER GEAR LT DOOR FRAME HAS AN EIGHT INCH CRACK ALONG FORWARD FACE AT THE FORWARD INBOARD CORNER. *S/D* REMOVED DAMAGED BUTT RIB, INSTALLED NEW BUTT RIB, INSTALLED NEW FRAME AS PER SRM 51-00-00 PG 2 ITEM C, COMPLETED 10/31 /96. 2 L 7 3 4F A22WE 1996110700220 19961107 00220 NM 1996 11 7 P5CA9600863 1 19961101 A 2910 65B9017058 LINE BOEING 747 747122 1384872 NM NR 3 HYD SYST WORN A P5CA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 23 850FT 19755 LOSS OF HYDRAULIC FLUID NR 3 HYDRAULIC SYSTEM AFTER TAKEOFF. SYSTEM DEPRESSURIZED AND STABILIZED AT 1.3 GALLONS. ALL SYSTEMS WORKED NORMAL ON APPROACH TO JFK. FOUND HYDRAULIC LINE WORN THROUGH ON NR 3 PYLON IN THE GAP COVER AREA. REPLA CED LINE LEAK CHECKED OK PER MAINTENANCE MANUAL 29-11-00 PAGE 602. 2 L 7 4 4F A20WE 1996110700221 19961107 00221 NM 1996 11 7 P5CA9600864 1 19961101 A 2613 OVERHEAT SENSOR BOEING 747 747132 1384882 NM NR 1 PYLON MALFUNCTIONED A P5CA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 23 857FT 20246 AIR TURNBACK DUE LEFT WING L/E OVERHEAT LIGHT ILLUMINATED DURING CLIMB. LIGHT EXTINGUISHED BY REDUCING THRUST NUMBER 1 ENGINE WITH PYLON VALVE CLOSED. NO PNEUMATIC LEAKS FOUND IN NR 1, NR 2 PYLON OR LEFT WING MANIFOLD. FOUND NR 1 PYLON O VERHEAT DETECTOR INTERMITTENTLY SHORTING. DEACTIVATED PER DISPATCH DEVIATIONS MANUAL. REFERENCE SERVICE BULLETIN 747-2 6-2066. 2 L 7 4 4F A20WE 1996110700222 19961107 00222 WP 1996 11 7 CKSA96190 1 19961028 A 3610 57534301 DUCT DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 1 ENGINE BLOWN A CKSA F ACTIVATE FIRE EXT. J WARNING INDICATION AP APPROACH 1 GL 23 815CK 46151 678969 NR 1 ENGINE FIRE WARNING ON SHORT FINAL. NR 1 BOTTLE DUMPED FIRE DID NOT GO OUT, NR 2 BOTTLE DUMPED FIRE DID NOT GO OUT FOR 3 MINUTES. FIRE WARNING WILL NOT TEST ON NR 1 ENGINE. ENGINE FIRE, SEVERE DAMAGE CHECKLIST WAS ACCOMPLISHED IAW A IA PROCEDURES. FOUND DUCT BLOWN AT TEE FOR HEAT EXCHANGER AT PYLON REVERSER DUCT ASSEMBLY. REMOVED AND REPLACED DUCT A SSEMBLY AND REINSTALLED AS REQUIRED IAW MM 36-20-0. PRESSURE TESTED DUCT WITH APU, NO LEAKS NOTED. REMOVED AND REPLACE D NR 1 ENGINE FIRE BOTTLES, OPS CHECKED ON RUN-UP OK IAW MM CHAPTER 71-20-00 AND TESTED FIRE WARNING. WARNING TEST OK I AW MM 26-10-0, FIRE BOTTLE (P/N 893244) (S/N 25633DH) 1 POS, (S/N 25634DH) 2 POS. 2 L 7 4 4F 4 F 4A25 1E8 1996110700223 19961107 00223 WP 1996 11 7 CKSA96191 1 19961030 A 2750 LOCKOUT CYLINDER DOUG DC8 DC8F54 3021926 WP TE FLAP SYST REQD SERVICE A CKSA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 GL 23 806CK 45932 WHEN 35 DEGREES FLAPS WERE SELECTED, FLAPS CAME DOWN TO 25 DEGREES, MISSED APPROACH. SELECTED FLAPS 35 DEGREES, FLAPS C AME DOWN TO 25 DEGREES UNTIL AIRCRAFT SLOWED TO 145 KIAS, THEN FLAPS LOWERED TO 35 DEGREES. BLED AND SERVICED FLAP LOCK OUT CYLINDER PER MM 27-28-0, FLAPS OPS CHECK NORMAL PER MM 27-24-0. 2 L 7 4 4F 4A25 1996110700224 19961107 00224 WP 1996 11 7 CA960321511 1 19960226 A 2780 SLATS DOUG DC9 DC932 3022066 WP LE DEVICE INOPERATIVE W O OTHER F FLT CONT AFFECTED CL CLIMB 1 CA (CAN)AFTER TAKEOFF UNABLE TO RETRACT SLATS ALSO SLATS LEVER STIFF. MAINTENANCE ACTION INVOLVED LUBRICATING PEDESTAL MECH ANISM AND WHEEL WELL CABLES. SLATS SYSTEM OPERATED SEVERAL TIMES. 2 L 7 2 4F A6WE 1996110700225 19961107 00225 EA 1996 11 7 CA960321513 1 19960227 A 3250 TRANSFORMER CNDAIR CNDAIR CL600 CL6002B19 EA GE RT NLG STEERING OUT OF TOLERANCE W O OTHER O OTHER TX TAXI/GRND HDL 1 CA 228 (CAN)DURING TAXI, TURNING NOSE GEAR TILLER TO LEFT, WHEELS TURNED RIGHT. FOUND RIGHT WHEEL STEERING ROTARY VARIABLE DIF FERENTIAL TRANSFORMER (RVDT) OUT OF TOLERANCE. READJUSTED. 2 L 7 2 4F RT A21EA 1996110700226 19961107 00226 EA 1996 11 7 CA960321514 1 19960302 A 2760 270003 PCU CNDAIR CNDAIR CL600 CL6002B19 EA LEFT INBD SPLR FAILED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA 2606 (CAN)ON APPROACH, SPOILER FAULT MESSAGE ON EICAS. INSPECTION FOUND LEFT INBOARD SPOILERON POWER CONTROL UNIT (PCU) AND E LECTRICAL HARNESS FAILED. HARNESS AND SPOILERON PCU REPLACED. 2 L 7 2 4F RT A21EA 1996110700227 19961107 00227 EU 1996 11 7 CA960321516 2 19960304 A 7530 1216643S5 BLEED VALVE AIRBUS 320 A320211 3930320 EU GE CFM56 CFM565A 13802 NE VBV DRIVE INOPERATIVE W C D ABORTED TAKEOFF RETURN TO BLOCK E VIBRATION/BUFFET TO TAKEOFF 1 CA 731296 (CAN)TAKEOFF REJECTED AT 120 KNOTS BECAUSE OF SEVERE VIBRATION FOLLOWED BY HIGH EGT, UP TO 850 DEGREES CENTIGRADE. MAINT ENANCE INVESTIGATION REVEALED VARIABLE BLEED VALVE (V.B.V.) MOTOR DRIVE SHAFT TO ACTU ATOR SHEARED. V.B.V. MOTOR DRIVE R EPLACED. 2 L 7 2 4F 4 F RT A28NM E29NE 1996110700228 19961107 00228 NM 1996 11 7 CA960325001 1 19960321 A 5751 85740201001 PIN DHAV 85740213102 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE AILERON HINGE CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 120840 (CAN)RIGHT AILERON OUTBOARD HINGE INBOARD HOLE AND HINGE PIN SEVERELY PITTED. PIN AND FITTING REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1996110700229 19961107 00229 NM 1996 11 7 CA960325002 1 19960321 A 3232 82970014007 ACTUATOR DHAV DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE LH MAIN DOOR FAILED W A UNSCHED LANDING J O WARNING INDICATION OTHER CL CLIMB 1 CA 23679 120056 (CAN)LH MAIN LANDING GEAR FAILED TO RETRACT. CENTRE DOOR ACTUATOR HAD FAILED. 2 H 7 2 4T 4 T RT A13NM E20NE 1996110700231 19961107 00231 SO 1996 11 7 CA960325004 1 19960312 A 3230 4027908 SIDE BRACE 4027908 PIPER PA31 PA31350 7103110 SO MLG BRACE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING MAINTENANCE ON THE LEFT HAND MAIN LANDING GEAR, AD 88-05-05, PIPER SB 845A, WAS BEING ACCOMPLISHED WHEN THE FORWARD SIDE BRACE WAS FOUND CRACKED. A DYE PENETRANT INSPECTION REVEALED A CRACK ON ONE OF THE EARS APPROXIMATELY .37 50 INCH IN LENGTH. THIS IS NOT WHERE THE SB STATES A CRACK MIGHT BE. THE SIDE BRACE WAS REPLACED, THUS TERMINATING AD 88-05-05. GEAR SWINGS WERE CARRIED OUT AND THE AIRCRAFT WAS RETURNED TO SERVICE. THE SUBMITTER STATES THAT THE NORMAL METHOD OF AD COMPLIANCE WILL NOT DETECT CRACKS IN THE AREA THAT IS INDICATED. THE RETRACT ARM MUST BE REMOVED. 1 L 7 2 3O A20SO 1996110700232 19961107 00232 SO 1996 11 7 CA960325005 1 19960312 A 3230 41983000 DOWNLOCK PIPER PA31 PA31350 7103110 SO FORWARD TAB SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) WHILE REPLACING THE LEFT HAND MAIN LANDING GEAR SIDE BRACE THE DOWNLOCK WAS REMOVED. INSPECTION REVEALED ONE OF T HE TWO RIVETS SECURING THE TWO TABS TO THE DOWNLOCK HAD SHEARED. TWO USED DOWNLOCKS WERE PURCHASED BUT REJECTED DUE TO A LUMINUM RIVETS BEING INSTALLED SECURING THE TABS. A NEW DOWNLOCK WAS INSTALLED AND GEAR SWINGS CARRIED OUT. THE AIRC RAFT FLEW 5.5 HOURS AND THE DOWNLOCK WAS INSPECTED AND FOUND TO HAVE THE RIVET SHEARED YET AGAIN. SUBMITTER STATES THAT THE NEW DOWNLOCK HAVE ROUND HEAD STEEL RIVETS WHILE THE OLD VERSION HAD FLUSH RIVETS. 1 L 7 2 3O A20SO 1996110700233 19961107 00233 SW 1996 11 7 CA960325006 1 19960315 A 2720 2672002005 ARM SWRNGN 2672019001 SWRNGN SA226 SA226TC 8780404 SW ARSRCH RUDDER CONTROL CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 13734 (CAN)BOTH LH ARMS IN PILOT AND COPILOT RUDDER CONTROL SYSTEM HAVE CRACKS THROUGH MATERIAL. ONE CRACK IS AT MOUNTING SCRE W HOLE. SUBMITTER NOTES THAT INTERFERENCE FIT BETWEEN ARM AND SHAFT DESIGNED IN. IT M AY BE TOO MUCH BUT IS NEEDED TO WO RK ASSEMBLY. 2 L 7 2 4T RT A8SW 1996110700235 19961107 00235 SO 1996 11 7 CA960325008 1 19960320 A 2731 8037M2 TRIM ACTUATOR CALCO 8037M2 LKHEED 382 382G 526414U SO ALLSN ELEV FAILED W A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CA 760 901340 (CAN)ON CLIMB THE ELEVATOR TRIM TAB BECAME UNRESPONSIVE IN NORMAL MODE. AIRCRAFT RETURNED TO BLOCKS. ELEVATOR TRIM TAB A CTUATOR REPLACED. 2 H 7 4 4T A1SO 1996110700237 19961107 00237 NM 1996 11 7 CA960325010 1 19960315 A 3242 214664 BRAKE UNIT BFGOODRICH DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE LEFT HAND SEIZED W K NONE O OTHER TX TAXI/GRND HDL 1 CA 159 LH120584 (CAN)DURING TAXI FOR DEPARTURE LH INBOARD AND OUTBOARD BRAKE ASSEMBLY'S SEIZED. BOTH BRAKE UNITS REPLACED. ON DISASSEMBL Y, PRESSURE PLATES, LININGS AND TORQUE PLATES WERE FOUND OVERHEATED. CYCLES ON #1 WERE 10421 AND ON #2 5543. TSN ON #1 W ERE 8957 AND ON #2 5393. 2 H 7 2 4T 4 T RT A13NM E20NE 1996110700238 19961107 00238 EU 1996 11 7 CA960325013 1 19960314 A 3260 606EN166 SWITCH FOKKER F28 F28MK1000 4990808 EU RT MLG DOOR ADJUSTMENT W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN)AFTER TAKEOFF RH MAIN LANDING GEAR DOOR UNSAFE IN UP POSITION. AIRCRAFT DIVERTED TO MAINTENANCE BASE. RH DOOR UPLOC K POSITION SWITCH ADJUSTED. 2 L 7 2 4F RT A20EU 1996110700239 19961107 00239 WP 1996 11 7 CA960325014 1 19960316 A 5280 1530924147 FIXED DOOR LKHEED 1011 1011385114 WP LT MLG DOOR MISSING W K NONE D INFLIGHT SEPARATION NR NOT REPORTED 1 CA (CAN)LH MAIN LANDING GEAR DOOR MISSING. AIRCRAFT RETURNED TO MAIN BASE. THE UPPER BEAM STILL ATTACHED TO GEAR AND HAD T WO ENDS BROKEN. LOWER FITTING SUPPORT ASSEMBLY STILL ATTACHED WITHOUT DAMAGE. LOWER BEAM MISSING. UNABLE TO DETERMINE WH EN DOOR LOST. PREVIOUS WORK DONE 2 DAYS PREVIOUS. PARTS REPLACED. 2 L 7 3 4F A23WE 1996110700240 19961107 00240 EU 1996 11 7 CA960325015 1 19960308 A 5280 14152030401 RIVETS BAG JETSTM JETSTM4112 EU AFT HINGE LT SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA 2088 (CAN)THREE RIVETS FOUND SHEARED ON THE PANEL CONNECTING THE TWO MAIN LANDING GEAR DOOR HINGES ON AFT LEFT HAND MAIN LAND ING GEAR DOOR. 1 L 7 2 4T RT A196 1996110700241 19961107 00241 CE 1996 11 7 CA960327001 1 19960308 A 5751 122005212 BRACKET CESSNA 122005212 CESSNA 206 U206G 2073356 CE CONT O520 IO520F 17032 SO AILERON CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 9768 247695R (CAN)DURING INSPECTION THE AILERON BRACKET WAS FOUND CRACKED WHERE IT ATTACHES TO THE WING TRAILING EDGE STRUCTURE. 1 H 7 1 3O 3 O A4CE E5CE 1996110700242 19961107 00242 CE 1996 11 7 CA960327002 1 19960308 A 5210 MS203922C13 PIN BEECH BEECH 90 C90 1152913 CE PWA TOP OF DOOR BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 12142 (CAN)ON INSPECTION THE FRONT TOP LATCH WAS FOUND UNSERVICEABLE. THE PIN HOLDING THE LATCH IN PLACE WAS FOUND BROKEN. 1 L 7 2 3T 3A20 1996110700243 19961107 00243 CE 1996 11 7 CA960327003 1 19960308 A 7120 075100330 ENGINE MOUNT CESSNA 075100330 CESSNA 185 A185F 2072821 CE CONT O520 IO520D 17032 SO LORD MOUNT CRACKS W K NONE O OTHER IN INSP/MAINT 1 CA 14400 175705R (CAN)DURING INSPECTION TWO CRACKS WERE FOUND. ONE ON EACH SIDE UNDER THE LORD MOUNT. SUBMITTER SPECULATES THAT WINTER SK I OPERATION MAY HAVE SOMETHING TO DO WITH THE CRACKS. 1 H 7 1 3O 3 O 3A24 E5CE 1996110700244 19961107 00244 CE 1996 11 7 CA960327004 1 19960308 A 5610 9031001P WINDSHIELD BEECH 9031001P BEECH 100 100BEECH 1152916 CE PILOT WINDOW CRACKED W A UNSCHED LANDING O OTHER CR CRUISE 1 CA 8069 94241H3080 (CAN)AT 16,000 FEET THE PILOTS WINDSHIELD CRACKED IN NUMEROUS LOCATIONS. THE OAT WAS REPORTED AT -45 DEGREES. AIRCRAFT R ETURNED TO BASE WITHOUT FURTHER INCIDENT. 1 L 7 2 3T A14CE 1996110700245 19961107 00245 EA 1996 11 7 CA960327005 2 19960308 A 8520 CRANKCASE PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2C 41532 EA LEFT SIDE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1295 1295 L713161A (CAN) ON INSPECTION, A CRACK WAS NOTICED ON THE LEFT SIDE UNDER THE OIL FILLER. IT WAS 2 INCHES LONG AND WENT TOWARDS T HE SECOND CYLINDER BASE. 1 L 7 2 3O 3 O A20SO E14EA 1996110700246 19961107 00246 CE 1996 11 7 CA960327006 1 19960308 A 3242 B302781 TORQUE PLATE CESSNA CESSNA 206 U206G 2073356 CE CONT O520 IO520F 17032 SO TOP PIN LT BRAKE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 2134 247695R (CAN)ON INSPECTION THE TORQUE PLATE OF THE LEFT BRAKE WAS FOUND CRACKED. 1 H 7 1 3O 3 O A4CE E5CE 1996110700247 19961107 00247 CE 1996 11 7 CA960327007 1 19960308 A 2700 PM235 TRIM MOTOR BEECH PM235 BEECH 100 100BEECH 1152916 CE ARMATURE SHORTED W K NONE O OTHER IN INSP/MAINT 1 CA 1900 (CAN)THE TRIM MOTOR WAS NOT WORKING. INSPECTION FOUND THE ARMATURE HAD SHORTED AGAINST THE HOUSING. A NEW ARMATURE WAS I NSTALLED. 1 L 7 2 3T A14CE 1996110700248 19961107 00248 CE 1996 11 7 CA960327008 1 19960308 A 2810 WING TANK CESSNA CESSNA 206 U206G 2073356 CE CONT O520 IO520F 17032 SO OUTBOARD TOP LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 10801 286121R (CAN)INSP FOUND WING TANK LEAKING 1 H 7 1 3O 3 O A4CE E5CE 1996110700249 19961107 00249 CE 1996 11 7 CA960327009 1 19960318 A 7120 75100331 MOUNT CESSNA CESSNA 185 A185F 2072821 CE CONT O520 IO520D 17032 SO ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 14258 175705R (CAN)CRACK FOUND ON THE ENGINE MOUNT BY THE GUSSET PLATE. THE MOUNT WAS REMOVED AND INSPECTED WITH LIQUID PENETRANT AND THE CRACK WAS CONFIRMED. 1 H 7 1 3O 3 O 3A24 E5CE 1996110700250 19961107 00250 CE 1996 11 7 CA960327010 1 19960318 A 5531 07310292 REAR SPAR CESSNA 073100119 CESSNA 185 A185F 2072821 CE RUDDER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 14258 (CAN)DURING AN INSPECTION THE RUDDER SPAR AND ONE DOUBLER WAS FOUND STARTING TO CRACK BETWEEN THE FIRST AND SECOND BOLTS LOCATED AT THE BOTTOM OF THE SPAR. 1 H 7 1 3O 3A24 1996110700251 19961107 00251 CE 1996 11 7 CA960327011 1 19960318 A 5511 07326116 NOSE RIBS CESSNA 12320008 CESSNA 185 A185F 2072821 CE STAB CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 14258 (CAN)DURING INSPECTION THE FIRST TWO RIBS ON THE STABILIZER WERE FOUND CRACKED AND PUSHED IN. 1 H 7 1 3O 3A24 1996110700252 19961107 00252 CE 1996 11 7 CA960327012 1 19960318 A 5510 07120421 BRACKET STAB CESSNA 07120421 CESSNA 185 A185F 2072821 CE HORIZ STAB CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 14258 (CAN)AT INSPECTION THE STABILIZER WAS REMOVED AND THE LEFT BRACKET STABILIZER HINGE WAS FOUND CRACKED FROM THE CENTRE DO WNWARDS. THE RIGHT STABILIZER HINGE WAS GROOVED TO THE POINT OF PART REJECTION AS WEL L AS THE RIGHT ANGLE REINFORCEMENT . 1 H 7 1 3O 3A24 1996110700253 19961107 00253 SW 1996 11 7 CA960327015 1 19960130 A 3212 206073926105 RELIEF VALVE BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL EMERG FLOAT LEAKING W K NONE O OTHER IN INSP/MAINT 1 CA CAE860375 (CAN)VALVE WAS FOUND TO BE LEAKING. UPON REMOVAL AND DISASSEMBLY, DIRT AND CORROSION WAS FOUND TO BE THE CAUSE. SUGGEST A SMALL HOLE BE DRILLED TO ALLOW WATER TO ESCAPE, OR REPOSITION VALVE BY TURNING BODY 90 DEGREES. 1 G 7 1 3U 3 U H2SW E1GL 1996110700255 19961107 00255 SO 1996 11 7 CA960327017 2 19960304 A 8530 641916 CYLINDER CESSNA 150 150M 2071830 CE CONT O200 O200A 17020 SO ENGINE BROKEN ROCKER W O OTHER E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CR CRUISE 1 CA 696 11018A (CAN) PILOT NOTICED A SUDDEN LOSS OF POWER FROM 2400 RPM TO 2200 RPM WITH A SLIGHT VIB AND ROUGHNESS. IT WAS FOUND THAT #1 CYL WAS COLD. WHEN THE ROCKER COVER WAS REMOVED, THE INT, EXH, ROCKER ARMS AND ROCKER ARM SHAFT WERE LAYING INSIDE T HE COVER NO LONGER ATTACHED TO THE HEAD. THE ROCKER ARM BOSSES HAD BEEN TOTALLY BROKEN OFF, CAUSING THE ENG TO RUN ON TH REE CYL. ENG WAS DISMANTLED DUE TO METAL CONTAIMINATION. IT SHOULD BE NOTED THAT AD 94-05-05R1 WAS RECEIVED ONE WEEK EAR LIER WHICH CALLS FOR ROCKER BOSSES TO BE INSP THE NEXT TIME CYL ARE REMOVED. OTHER CYLS WERE CHECKED OK. WALL THICKNESS OF BOSS WAS .090 AND IT SHOULD BE MIN. OF .180 AS STATED IN SB 73-13. 1 H 7 1 3O 3 O 3A19 E252 1996110700256 19961107 00256 CE 1996 11 7 CA960327018 1 19960327 A 2710 2660001152 CONTROL CABLE CESSNA 208 208B 2073701 CE AILERON PULLEY FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA 6450 (CAN) DURING ROUTINE INSPECTION THE AILERON CABLE WAS FOUND FRAYED WHERE IT PASSES THROUGH THE PULLEY ASSEMBLY UNDER THE SCUFF PLATE AREA IN THE COCKPIT. THIS CABLE WAS FOR THE LEFT HAND AILERON. THE CABLE WAS REPLACED WITH A NEW ONE. 1 H 7 1 3T A37CE 1996110700257 19961107 00257 EA 1996 11 7 CA960328002 1 19960316 A 3233 155681 BOLT 155507 DHAV DHC7 DHC7103 2802710 EA RH MLG ACTUATOR SEIZED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA (CAN)RH MAIN LANDING GEAR WOULD NOT RETRACT. CYLINDER LUGS HAD FAILED. SUSPECTED THAT THE BOLT P/N 15568-1 HAD SEIZED IN SIDE OF BUSHING P/N 15513-1. NEW ACTUATOR INSTALLED. 2 H 7 4 4T A20EA 1996110700258 19961107 00258 NE 1996 11 7 CA960328003 1 19960307 A 6320 S6135220173 RING GEAR SKRSKY S61352060004 SKRSKY S61 S61N 8142104 NE MAIN GEARBOX FAILED W K NONE J WARNING INDICATION IN INSP/MAINT 1 CA 639 (CAN)MAIN GEARBOX CHIP LIGHT ALONG WITH AUDIBLE SOUND CHANGE FROM MGB AREA. FOLLOWING SHUTDOWN INSPECTION OF COURSE SCRE EN SHOWED SOME FERROUS AND NON FERROUS PARTICLES. ON DISASSEMBLY IT WAS FOUND THAT THE RING GEAR HAD FAILED. 2 G 7 2 4U 1H15 1996110700259 19961107 00259 NM 1996 11 7 CA960328004 1 19960327 A 2910 727452 CIRCUIT BREAKER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE #1 STDBY HYD FAULTY W O OTHER O OTHER AP APPROACH 1 CA 120854 (CAN)#1 STANDBY HYDRAULIC PUMP WOULD NOT COME ON LINE WHEN SELECTED FOR LANDING. CIRCUIT BREAKER FOUND FAULTY. 2 H 7 2 4T 4 T RT A13NM E20NE 1996110700260 19961107 00260 NM 1996 11 7 CA960328005 1 19960327 A 5343 85310339009 TRUNNIONS DHAV DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NOSE GEAR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 120657 (CAN)NOSE LANDING GEAR TRUNNIONS FOUND CRACKED. NOTED DURING INSPECTION FOR AD CF-92-18R3. MOD KIT 8MK1880-003 INSTALLED . SB A8-53-40 APPLIES. 2 H 7 2 4T 4 T RT A13NM E20NE 1996110700263 19961107 00263 CE 1996 11 7 CA960328008 1 19960319 A 2810 1003810051 FUEL CAP BEECH 99 99 1154002 CE TANK LEAKING W A UNSCHED LANDING K FLUID LOSS TO TAKEOFF 1 CA (CAN)ON ROTATION FUEL BEGAN VENTING FROM CAP. THE CAUSE WAS DETERMINED TO BE THE RETAINER STRAP LOCKING MECHANISM. THE F IX WAS TO REMOVE THE PLASTIC RETAINER AND INSTALL A BRASS CHAIN. 1 L 7 2 3T A14CE 1996110700264 19961107 00264 NE 1996 11 7 CA960329003 2 19960322 A 7200 ENGINE BELL 205 205A1 1181414 SW LYC T53 T5313B 41549 NE ENGINE NR 2 FAILED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA LE07592 (CAN)N2 FAILURE, N2 INDICATOR FLUCTUATED, NR ENGINE WARNING ON. 1 G 7 1 4U 4 U H1SW E17EA 1996110700265 19961107 00265 EU 1996 11 7 CA960401001 1 19960313 A 6220 350A31190703 STARFLEX SNIAS 350 AS350D 8680803 EU LYC LTS101 LTS101600A3 41560 NE MIDDLE OF ARM CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1973 LE43468CE (CAN)STARFLEX FOUND CRACKED IN MIDDLE OF ARM. NEW STAR INSTALLED. 1 G 7 1 3U 3 U H9EU E5NE 1996110700266 19961107 00266 NM 1996 11 7 CA960401004 1 19960326 A 5610 824342001 NUT PLATES PPG NP15790111 DHAV DHC8 DHC8102 2809003 NM PILOTS WINDOW CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 19539 93047H5352 (CAN)DURING REMOVAL OF PILOTS WINDSHIELD SEVERAL NUTS ON THE LOWER ROW CAME AWAY FROM THEIR HOLDERS. NUTS FOUND CORRODED AROUND THE EDGES AND THUS FELL OUT OF THEIR HOLDERS. SOME OF THE SCREW THREADS WERE ALSO CORRODED AT THE THREADS. 2 H 7 2 4T RT A13NM 1996110700267 19961107 00267 WP 1996 11 7 CA960401007 1 19960321 A 2530 CA167072 CONNECTING PLUG LKHEED 1011 1011385115 5265015 WP OVEN L3 CART BURNT W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA (CAN)OVEN AT L3 CART #2 MADE SPARKS AT THE CONNECTOR PLUG. REPLACED. 2 L 7 3 4F A23WE 1996110700268 19961107 00268 NM 1996 11 7 CA960402101 1 19960322 A 2612 FRF61651P PLUG BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE APU FIRE WARN DIRTY W F D ACTIVATE FIRE EXT. RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CA 702660 (CAN)APU FIRE WARNING ON ON GROUND JUST PRIOR TO TAKEOFF. APU HAD BEEN SHUT DOWN FOR 5 MINUTES. APU FIRE HANDLE PULLED S TILL INDICATING FIRE FOR SOME MINUTES. VISUAL CHECK INDICATED NO EVIDENCE OF FIRE. FO UND EXHAUST FIRE DETECTOR PLUG CON TAMINATED BY CARBON AND FLUIDS. CLEANED. 2 L 7 2 4F 4 F A16WE E2EA 1996110700269 19961107 00269 NM 1996 11 7 CA960403101 1 19960401 A 3310 952410214 RELAY BOEING 737 737275 1384485 NM CONTACTS STICKING W A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 CA (CAN)AT 100 KNOTS OVERHEAD PANEL LIGHT ILLUMINATED AS IN THE TEST MODE. TAKEOFF CONTINUED LIGHT TEST SWITCH RECYCLED IN FLIGHT. CB'S RESET IN FLIGHT. OVERHEAD PANEL MODULE P5-6 CONFIRMED DISCRETE LIGHTS ALLON TEST. REPLACED. 2 L 7 2 4F A16WE 1996110700270 19961107 00270 NM 1996 11 7 CA960403102 1 19960322 A 2750 EWB265 BOLT BOEING 737 737275 1384485 NM FLAP SPINDLE BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN)FLAP SPINDLE BEARING AT #7 POSITION BROKEN. BOLT BROKEN IN TWO PLACES. HEAD AND NUT BROKEN OFF ALLOWING SPINDLE TO MOVE FREELY. REPLACED. 2 L 7 2 4F A16WE 1996110700314 19961107 00314 EU 1996 11 7 96ZZZX5541 1 19960531 A 5280 109031214101 DOOR AGUSTA A109 A109C 0260118 EU NLG LT DOOR BROKEN A HQEA K NONE O OTHER NR NOT REPORTED 1 NE 05 100S 948 48 7644 THE LEFT NOSE GEAR DOOR CAME IN CONTACT WITH THE NOSE WHEEL AND BROKE THE LEFT DOOR. AGUSTA SB B.T. 109-84 REV A PERTAI NS TO THIS SUBJECT, BUT WAS PREVIOUSLY PERFORMED ON THIS AIRCRAFT. THIS REPAIR STATION HAS FOUND 2 OTHER AIRCRAFT (A109 C) WITH B.T. 1090-84 REV 1 C/W THAT HAVE BROKEN THE LEFT NOSE GEAR DOOR. FOUND THE NOSE STRUT NITROGEN CHARGE LOW. THI S COULD BE THE CAUSE. INSTALLED NEW LEFT NOSE GEAR DOOR. SERVICED NOSE STRUT WITH HYDRAULIC FLUID AND NITROGEN. PERFO RMED RETRACTION/EXTENSION CHECK. 1 G 7 2 3U H7EU 1996110700315 19961107 00315 EU 1996 11 7 96ZZZX5542 1 19961018 A 5280 109050144101 DOOR AGUSTA A109 A109C 0260118 EU NLG LT DOOR BROKEN A HQEA K NONE O OTHER IN INSP/MAINT 1 NE 05 142HC 164 63 7677 THE LEFT NOSE GEAR DOOR CAME IN CONTACT WITH THE NOSE WHEEL AND BROKE THE LEFT DOOR ACTUATING LEVER ROLLER BEARING AND T HE LEFT DOOR. AGUSTA SB B.T. 109-84 REV A PERTAINS TO THIS SUBJECT, BUT DOES NOT APPLY TO THIS AIRCRAFT S/N. THIS AIRC RAFT WAS MODIFIED AT THE FACTORY. THIS REPAIR STATION HAS FOUND 2 OTHER AIRCRAFT (A109C) WITH B.T. 109-84 REV 1 C/W THA T HAVE BROKEN THE LEFT NOSE GEAR DOOR. THE NOSE STRUT PRESSURE ON THIS AIRCRAFT WAS FOUND TO BE 25 PSI LOW. THIS COULD BE THE CAUSE. INSTALLED NEW LEFT NOSE GEAR DOOR AND LEVER. SERVICED NOSE STRUT WITH NITROGEN. PERFORMED RETRACTION/E XTENSION CHECK. 1 G 7 2 3U H7EU 1996110700316 19961107 00316 EU 1996 11 7 96ZZZX5543 1 19960919 A 5280 109031214101 DOOR AGUSTA A109 A109C 0260118 EU NLG LT DOOR BROKEN A HQEA K NONE O OTHER IN INSP/MAINT 1 NE 05 652DH 118 100 7652 FOUND THE LEFT NOSE GEAR DOOR BROKEN DURING THE 1200 HOUR INSPECTION. THE LEFT NOSE GEAR DOOR CAME IN CONTACT WITH THE NOSE WHEEL AND BROKE THE LEFT DOOR. AGUSTA SB B.T. 109-84 REV A PERTAINS TO THIS SUBJECT, BUT WAS PREVIOUSLY PERFORMED ON THIS ARICRAFT. THE REPAIR STATION HAS FOUND 2 OTHER AIRCRAFT (A109C) WITH B.T. 109-84 REV A C/W THAT HAVE BROKEN THE LEFT NOSE GEAR DOOR. INSTALLED REPAIRED LEFT NOSE GEAR DOOR. PERFORMED RETRACTION/EXTENSION CHECK. 1 G 7 2 3U H7EU 1996110700317 19961107 00317 WP 1996 11 7 CALA9601543 1 19961101 A 4990 3812761M APU DOUG DC9 DC982 3022082 WP A/C TAIL OVERSERVICED A CALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 09 478AC 18434 3861 48063 SMOKE AND ODOR ENTERED THE CABIN SHORTLY AFTER TAKEOFF. BOTH THE SMOKE AND ODOR DISAPPEARED AFTER PULLING THE RECIRCULA TING FAN CIRCUIT BREAKER. MAINTENANCE FOUND NO PROBLEMS WITH THE RECIRCULATING FAN. THE APU WAS CLEANED AND RUN WITH N O LEAKS NOTED. MAINTENANCE REMOVED THE APU BURNER CAN AND FOUND OIL IN TORUS AREA. THE BURNER CAN WAS REINSTALLED, THE COALESCER BAGS WERE CHANGED. THE APU WAS OPERATED WITH PACKS RUNNING TO LEAK CHECK AND CLEAR OUT SMELL FROM APU BEING OVERSERVICED. OPERATION CHECKED GOOD WITH NO LEAKS NOTED. 2 L 7 2 4F A6WE 1996110700318 19961107 00318 WP 1996 11 7 CALA9601544 1 19961102 A 3234 ABH735717 LG HANDLE DOUG DC10 DC1010 3022110 WP COCKPIT LACK OF LUBE A CALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 09 68046 47800 WHEN GEAR WAS LOWERED ON APPROACH, THE THREE GEAR RED UNSAFE LIGHTS ILLUMINATED. ALTERNATE GEAR EXTENSION WAS PERFORMED AND THREE GREEN LIGHTS WERE INDICATED FOR A NORMAL LANDING AT EWR. A SELF TEST OF THE PROXIMITY SWITCH ELECTRONIC BOX WAS PERFORMED WITH NO FAULT LIGHTS INDICATED. THE LANDING GEAR HANDLE ASSEMBLY WAS LUBRICATED, THE GEAR HANDLE WAS CYCL ED SEVERAL TIMES WITH OPERATION AND INDICATIONS CHECKING GOOD. 2 L 7 3 4F A22WE 1996110700319 19961107 00319 WP 1996 11 7 CALA9601545 1 19961102 A 2780 RESTRICTOR DOUG DC9 DC931 3022065 WP TE FLAP CONTL CLOGGED A CALA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SW 09 14564 47490 THE SLATS DID NOT EXTEND SYMMETRICALLY ON APPROACH. A SIGNIFICANT ROLL TO THE RIGHT OCCURRED AT SLATS EXTENDED/FLAPS 5 DEGREES, WHICH TOOK 10 DEGREES LEFT TURN TO COUNTERACT, AND THE BLUE SLAT EXTEND LIGHT TOOK 5 TO 6 SECONDS TO ILLUMINATE . THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT RESTRICTOR ON SLAT CONTROL VALVE CLOGGED. THE REST RICTOR WAS UNCLOGGED. THE SLATS WERE OPERATED WITH HYDRAULIC POWER ON AND OPERATION CHECKED GOOD. ALSO, FREE-FALL WAS PERFORMED AND ALL CHECKS WERE GOOD. 2 L 7 2 4F A6WE 1996110700320 19961107 00320 NM 1996 11 7 9623246309 1 19961102 A 3350 LIGHT BOEING 747 747451 1384940 NM CABIN NOT CONNECTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 669US 24224 DURING LINE CHECK, FOUND FIRST CLASS LEFT FLOOR EMERGENCY LIGHTS INOPERATIVE. RECONNECTED LIGHT ASSEMBLY AT ROW 4, OPER ATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1996110700321 19961107 00321 WP 1996 11 7 9623259979 1 19961103 A 5350 CLIPS DOUG DC9 DC931 3022065 WP TAILCONE OUT OF ADJUST A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9343 47439 DURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR TAILCONE HANDLE FROM THE CLIPS. ADJUSTE D CLIPS. 2 L 7 2 4F A6WE 1996110700322 19961107 00322 WP 1996 11 7 9623269987 1 19961031 A 5350 LATCH ARM DOUG DC9 DC932 3022066 WP TAILCONE WORN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 987US 47458 DURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE EXTERIOR TAILCONE HANDLE FROM THE CLIPS. ALSO, F OUND A WORN UPPER LEFT LATCH ARM AND AN INCORRECT LOWER RIGHT LATCH HOUSING. ADJUSTED THE CLIPS AND REPLACED THE LATCH ARM AND LATCH HOUSING. 2 L 7 2 4F A6WE 1996110700323 19961107 00323 EU 1996 11 7 9623273202 1 19961103 A 3350 321454 POWER SUPPLY AIRBUS 320 A320211 3930320 EU CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 302US 13966 8084 32 DURING LINE MAINTENANCE CHECK OF THE EMERGENCY LIGHTS, THE FORWARD EMERGENCY LIGHTS WOULD NOT ILLUMINATE. REPLACED POWE R SUPPLY, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996110700324 19961107 00324 SO 1996 11 7 COMA9610317 1 19961028 A 5313 12026335013 STRINGER EMB 120 EMB120RT SO BS 3293-3596 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 256CA 120245 C2 INSPECTION FOUND A SMALL AREA OF CORROSION ON FWD FUSELAGE STRINGER 21L BETWEEN FS 3293 AND 3596.5. THE DAMAGED AREA OF THE STRINGER WAS REMOVED AND REPAIRED PER AERODESIGN REPORT NR 1990-3, REV IR, DATED 10-26-96. 2 L 7 2 4T RT A31SO 1996110700325 19961107 00325 SO 1996 11 7 COMA9610316 1 19961028 A 5330 12019230001 SKIN EMB 120 EMB120RT SO FUSELAGE GOUGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 256CA 120245 C2 INSPECTION FOUND THE LOWER FUSELAGE CENTER SECTION SKIN TO BE GOUGED BY THE RIGHT WING DE-ICE PRESSURE REGULATOR. TH E DAMAGED SKIN WAS REPAIRED PER SRM 53-00-01, FIGURE 201, SHEET 3, PAGE 204. THE DE-ICE PRESSURE REGULATOR WAS REPOSITI ONED FOR PROPER CLEARANCE. 2 L 7 2 4T RT A31SO 1996110700326 19961107 00326 EA 1996 11 7 COMA9660192 1 19961103 A 7830 TR UNIT CNDAIR CL600 CL6002B19 EA RT ENGINE MALFUNCTIONED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 945CA 7069 ON CLIMBOUT, RT THRUST REVERSER UNLOCKED MSG CAME ON. REV DID NOT DEPLOY. DEFERRED RT T/R I/A/W MEL 78-30-1 CAT B. 2 L 7 2 4F RT A21EA 1996110700327 19961107 00327 EA 1996 11 7 COMA9660193 1 19961031 A 2760 270003 PCU CNDAIR CL600 CL6002B19 EA LT FLT SPOILER INOPERATIVE A COMA K NONE O OTHER LD LANDING 1 SO 01 946CA 7072 WHITE FLIGHT SPOILER MESSAGE CAME ON AFTER LANDING. REPAIRED LT INBD FLIGHT SPOILER POWER CONTROL UNIT. 2 L 7 2 4F RT A21EA 1996110700328 19961107 00328 SO 1996 11 7 COMA9610318 1 19961031 A 2751 INDICATION EMB 120 EMB120RT SO TE FLAPS MALFUNCTIONED A COMA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 462CA 120264 FLAP DISAGREEMENT AFTER TAKEOFF. INSPECTED FLAPS, NO DEFECTS NOTED. 2 L 7 2 4T RT A31SO 1996110700329 19961107 00329 SO 1996 11 7 COMA9610319 1 19961031 A 3231 12012347001 LATCH EMB 120 EMB120RT SO RT MLG DOOR FAILED A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 268CA 120262 ON POST FLIGHT, FOUND RT O/B FWD GEAR DOOR HANGING DOWN. REPLACED RT O/B DOOR LATCH. 2 L 7 2 4T RT A31SO 1996110700330 19961107 00330 NM 1996 11 7 SWAA961192 1 19961030 A 5320 DOUBLER BOEING 737 7372H4 138448C NM DOOR CUTOUT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 20SW 21337 DURING SCHEDULED 1/2 D-CHECK, FOUND FWD SERVICE DOOR, LOWER AFT CORNER DOUBLER CRACKED. REPLACED DOUBLER PER BOEING SRM . 2 L 7 2 4F A16WE 1996110700331 19961107 00331 NM 1996 11 7 SWAA961193 1 19961030 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 20SW 21337 DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER 16L CRACKED JUST AFT OF SCANNING LIGHT CUTOUT, BS 500B+13, 6 INCHES LONG. R EPAIRED PER SWA ACO 6405-53. 2 L 7 2 4F A16WE 1996110700332 19961107 00332 NM 1996 11 7 SWAA961194 1 19961030 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 20SW 21337 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM T-CAP CORROSION AT BS 344, RBL 1, 2, 7, 9 AND AT LBL 14, 18 AND 22. REPLA CED T-CAPS PER BOEING SRM. 2 L 7 2 4F A16WE 1996110700333 19961107 00333 NM 1996 11 7 SWAA961195 1 19961103 A 3350 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 64SW 22062 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT AT AFT ENTRY DOOR INOP. REPLACED BATTERY PACK PER BOEING M/M . 2 L 7 2 4F A16WE 1996110700334 19961107 00334 NM 1996 11 7 SWAA961196 1 19961029 A 2530 COFFEEMAKER BOEING 737 7372H4 138448C NM AFT GALLEY FAILED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 68SW 22357 AT GATE, NOTED A BURNING ELECTRICAL ODOR AT AFT GALLEY AREA. INSPECTED GALLEY AREAS, REPLACED COFFEEMAKERS AND RESET BR EAKERS PER M/M, ALL NORMAL. 2 L 7 2 4F A16WE 1996110700335 19961107 00335 NM 1996 11 7 SWAA961197 1 19961029 A 5330 SKIN BOEING 737 7373H4 1384600 NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 324SW 23414 AT GATE, FOUND A 4 INCH SKIN CRACK IN AFT CARGO DOOR SKIN. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996110700336 19961107 00336 NM 1996 11 7 SWAA961198 1 19961030 A 2133 322684003 OUTFLOW VALVE BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA B EMER. DESCENT O OTHER CR CRUISE 1 SW 07 350SW 24409 AT 37,000, CABIN ALTITUDE ALERT WARNING SOUNDED. SWITCHING TO MAN OR STANDBY MODES, NO HELP. DESCENDED TO LEVEL WHERE PRESSURE WAS REGAINED. LANDED WITHOUT INCIDENT. FWD OUTFLOW VALVE FAILED TEST. REPLACED VALVE AND SYSTEM CHECKED OK P ER BOEING M/M. 2 L 7 2 4F RT A16WE 1996110700337 19961107 00337 NM 1996 11 7 SWAA961199 1 19961030 A 2120 AIR DISTR BOEING 737 7373H4 1384600 NM COCKPIT ODOR A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 392SW 27379 CREW NOTED JET FUEL SMELL IN COCKPIT EMITTING FROM AIR VENTS. INSPECTION PERFORMED, NO LEAKS NOTED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996110700338 19961107 00338 NM 1996 11 7 SWAA961200 1 19961029 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 624SW 27934 FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT ASSEMBLY BROKEN. REPLACED LIGHT ASSEMBLY PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996110700339 19961107 00339 NM 1996 11 7 SWAA961201 1 19961027 A 3397 WIRE BOEING 737 7373T0 1384582 NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 684WN 23941 FOUND CABIN FLOOR TRACK LIGHTING INOP AT EMERGENCY EXITS. REPAIRED BROKEN WIRES AND MISSING LIGHT SOCKETS PER BOEING M/ M. 2 L 7 2 4F RT A16WE 1996110700340 19961107 00340 NM 1996 11 7 SWAA961202 1 19961029 A 5330 SKIN BOEING 737 7373Q8 1384670 NM BS 500 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D-CHECK, FOUND 2 FUSELAGE SKIN DENTS 2 INCHES APART, AT BS 500C BETWEEN S26 AND 25L. INSTALLED REPAIR PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996110700341 19961107 00341 NM 1996 11 7 SWAA961203 1 19961029 A 5330 SKIN BOEING 737 7373Q8 1384670 NM BS 337 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D-CHECK, FOUND A FUSELAGE SKIN DENT, AT BS 337 AT S25. INSTALLED REPAIR PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996110700342 19961107 00342 NM 1996 11 7 SWAA961204 1 19961029 A 5312 BULKHEAD ANGLE BOEING 737 7373Q8 1384670 NM BS 520 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D-CHECK, FOUND FLOOR TO AFT BULKHEAD SUPPORT ANGLE CORRODED AT BS 520, LBL 24 TO RBL 24. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996110700343 19961107 00343 NM 1996 11 7 SWAA961205 1 19961029 A 5315 FLOORBEAM BOEING 737 7373Q8 1384670 NM BS 270 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 270 AND AT BS 947.5, LBL 6 TO 17. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996110700344 19961107 00344 NM 1996 11 7 SWAA961206 1 19961029 A 5320 SILL BOEING 737 7373Q8 1384670 NM PAX DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR MOPSILL CORRODED AT BS 639, LBL 55, WL 208. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996110700345 19961107 00345 NM 1996 11 7 SWAA961207 1 19961029 A 5320 SUPPORT BOEING 737 7373Q8 1384670 NM BS 847-867 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D-CHECK, FOUND WEB FLOOR SUPPORT CORRODED FROM BS 847 TO 867, WL 156, RBL 26. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996110700346 19961107 00346 NM 1996 11 7 SWAA961208 1 19961029 A 5315 FLOORBEAM BOEING 737 7373Q8 1384670 NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D-CHECK, FOUND TOP CHORD OF FLOORBEAM CORRODED AT BS 344, LBL 7 AND AT RBL 1, WL 208. REPLACED DAMAGED SECTIONS PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996110700347 19961107 00347 NM 1996 11 7 SWAA961209 1 19961029 A 5320 SILL BOEING 737 7373Q8 1384670 NM AFT SERVICE DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D-CHECK, FOUND AFT SERVICE DOOR MOPSILL CORRODED AT BS 913 TO 987, RBL 53, WL 208. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996110700348 19961107 00348 NM 1996 11 7 SWAA961210 1 19961029 A 5320 SUPPORT BOEING 737 7373Q8 1384670 NM BS 204-312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORTS CORRODED AT BS 277 TO 204, LBL 11, WL 208, AT BS 294 TO 312, LBL 11 AND R BL 11, WL 208. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996110700349 19961107 00349 NM 1996 11 7 SWAA961211 1 19961030 A 5330 SKIN BOEING 737 7375H4 138449D NM BS 986.5 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 507SW 24184 DURING SCHEDULED BC2 CHECK, FOUND FUSELAGE SKIN GOUGED 3 PLACES AT 986.5, 16 INCHES BELOW AFT ENTRY DOOR. REPLACED PER BOEING SRM AND TYPICAL REPAIR T1-A53-042. 2 L 7 2 4F RT A16WE 1996110700350 19961107 00350 NM 1996 11 7 UPS96221516 1 19961021 A 5311 FRAME BOEING 727 7271A7C 13840X2 NM BS 1130 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 935UP 20143 INSPECTION TYPE-C, BS 1130 FRAME UPPER FLANGE ABOVE STR 29R IS DENTED AND CRACKED. REMOVED DAMAGE, FABRICATED AND INSTA LLED REPAIR PARTS PER SRM 51-40-3 AND SRM 51-10-6. 2 L 7 3 4F A3WE 1996110700351 19961107 00351 NM 1996 11 7 UPS96221517 1 19961026 A 5347 65234104 SEAT TRACK BOEING 727 7271A7C 13840X2 NM BS 558-585 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 935UP 20143 INSPECTION TYPE-C, THE FWD CARGO AT, RT TRACK BS 558 TO 585 HAS INTERGRANULAR CORROSION AND IS SEVERLY WORN. REMOVED SE AT TRACK AT RT SIDE, FWD CARGO PIT FROM STA 550 TO 680 AND INSTALLED TRACK PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996110700352 19961107 00352 NM 1996 11 7 UPS96221522 1 19961003 A 5712 RIB BOEING 727 72722C 138400F NM WS 686 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE-D, RIB AT LEFT WING STA 686 CRACKED AT LOWER STR 8 ATTACH HOLE. REPLACED RIB ASSY STA 686 PER EO B727-5 710-1325 APPENDIX C. 2 L 7 3 4F A3WE 1996110700353 19961107 00353 NM 1996 11 7 UPS96221523 1 19961001 A 5320 SPLICE BOEING 727 72722C 138400F NM BS 870 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE-D, EDDY CURRENT INSPECTION SHOWS CRACK INDICATION AT BS 870 LT STR 9 SPLICE AFT ROW TOP HOLE AT ABOUT 12 O'CLOCK POSITION. ACCOMPLISHED REPAIR ACC UPS EO B727-5310-8735A. 2 L 7 3 4F A3WE 1996110700354 19961107 00354 NM 1996 11 7 UPS96221524 1 19961004 A 5753 65192028 FLAP CARRIAGE BOEING 727 72722C 138400F NM LT TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYP-D, RUST ON EXTERNAL SURFACE AND INSIDE SPINDLE OF AFT O/B FLAP, O/B CARRIAGE NR 1. REMOVED AND REPLACED WITH OVERHAUL CARRIAGE ASSY IAW MM 27-51-13. 2 L 7 3 4F A3WE 1996110700355 19961107 00355 NM 1996 11 7 UPS96221525 1 19961002 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 720 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE-D, STR 15L CRACKED AT BS 720. REMOVED DAMAGED SECTION OF STRINGER 15L AT BS 720, 13 INCHES LONG. INST ALLED SECTION, BAC 1498-144 PER SRM 53-10-03 FIG 1. 2 L 7 3 4F A3WE 1996110700356 19961107 00356 NM 1996 11 7 UPS96221528 1 19960927 A 5330 SKIN BOEING 727 72722C 138400F NM BS 303 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE-D, FUSELAGE SKIN CORRODED AT FUSELAGE LAP SEAT AT BS 303, STR 24L. LFEC REVEALED MORE THAN 10 PERCENT M ATERIAL LOSS AT BS 295. CUT OUT SECTION OF SKIN 5 BY 3. INSTALLED DOUBLER REPAIR IAW SRM 53-30-03 FIG 14. 2 L 7 3 4F A3WE 1996110700357 19961107 00357 NM 1996 11 7 UPS96221529 1 19961003 A 5313 652988913 STRINGER BOEING 727 72722C 138400F NM BS 360 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE-D, HFEC INSPECTION SHOWS MATERIAL LOSS OF 10 PERCENT AT BS 360 FROM STR 17L TO STR 19L FWD PANEL. CUT O UT DAMAGED SKIN FWD PANEL. REPLACED STR TIE FITTING (P/N 65-29889-13) AT STR 19L. INSTALLED REPAIR DOUBLER PER DRAWING 69-62161 AND PER UPS EO B727-5310-1371E. 2 L 7 3 4F A3WE 1996110700358 19961107 00358 NM 1996 11 7 UPS96221530 1 19961003 A 5330 SKIN BOEING 727 72722C 138400F NM BS 360 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE-D, LFEC INSPECTION SHOWS MATERIAL LOSS OF 10 PERCENT AT BS 360 FWD PANEL FROM STR 10R TO STR 14R. CUT O UT CORRODED SECTION OF FWD SKIN PANEL, INSTALLED FILLER AND EXTERNAL DOUBLER PER DRAWING 69-62161 AND PER UPS EO B727-53 10-1371E. 2 L 7 3 4F A3WE 1996110700359 19961107 00359 NM 1996 11 7 UPS96221531 1 19961104 A 5330 SKIN BOEING 727 72722C 138400F NM BS 259 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE-D, LFEC INSPECTION SHOWS MATERIAL LOSS OF 10 PERCENT AT BS 259, FWD PANEL, FROM STR 19R TO 24R. FABRIC ATED AND INSTALLED REPAIR PER UPS EO B727-5310-1371E. 2 L 7 3 4F A3WE 1996110700360 19961107 00360 NM 1996 11 7 UPS96221532 1 19961104 A 5330 SKIN BOEING 727 72722C 138400F NM BS 259.5 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE-D, LFEC INSPECTION SHOWS MATERIAL LOSS OF 10 PERCENT AT BS 259.5 FWD PANEL, FROM STR 19L TO STR 24L. FA BRICATED AND INSTALLED REPAIR PER UPS EO B727-5310-1371E. 2 L 7 3 4F A3WE 1996110700361 19961107 00361 NM 1996 11 7 UPS96221533 1 19961104 A 5330 SKIN BOEING 727 72722C 138400F NM BS 259.5 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE-D, LFEC INSPECTION SHOWS MATERIAL LOSS OF 10 PERCENT AT BS 259.5 AFT PANEL FROM STR 6L TO STR 10L. FABR ICATED AND INSTALLED REPAIR PER UPS EO B727-5310-1371E. 2 L 7 3 4F A3WE 1996110700362 19961107 00362 NM 1996 11 7 UPS96221534 1 19961104 A 5753 65192028 FLAP CARRIAGE BOEING 727 72722C 138400F NM RT TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE-D, RIGHT O/B FLAP I/B CARRIAGE, NR 7, HAS RUST AROUND SPINDLE. REMOVED AND REPLACED WITH OVERHAULED CAR RIAGE PER MM 27-51-13. 2 L 7 3 4F A3WE 1996110700363 19961107 00363 NM 1996 11 7 UPS96221535 1 19961104 A 5753 651920115 FLAP CARRIAGE BOEING 727 72722C 138400F NM LT TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE-D, RUST ON EXTERNAL SURFACE AND ON SPINDLE OF I/B FLAP I/B CARRIAGE. REMOVED AND REPLACED WITH OVERHAUL ED CARRIAGE MM 27-51-03. 2 L 7 3 4F A3WE 1996110700364 19961107 00364 NM 1996 11 7 UPS96221536 1 19961104 A 5753 651920111 CARRIAGE BOEING 727 72722C 138400F NM LT TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE-D, RUST ON EXTERNAL SURFACE OF LEFT I/B FLAP, O/B CARRIAGE. REPLACED WITH OVERHAULED CARRIAGE PER MM 27 -51-03. 2 L 7 3 4F A3WE 1996110700365 19961107 00365 NM 1996 11 7 UPS96221537 1 19961104 A 5315 FLOORBEAM BOEING 727 72722C 138400F NM BS 344 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE-D, STA 334 FLOORBEAM UPPER CHORD HAS CORROSION FROM LBL 65 TO RBL 24. REPLACED DAMAGED SECTION OF FLOOR BEAM PER SRM 51-10-1, 51-30-2. 2 L 7 3 4F A3WE 1996110700366 19961107 00366 NM 1996 11 7 UPS96221538 1 19961104 A 5753 65192028 FLAP CARRIAGE BOEING 727 72722C 138400F NM LT TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE-D, RUST ON EXTERNAL SURFACES OF LEFT O/B FLAP, I/B CARRIAGE NR 2. REPLACED WITH OVERHAULED CARRIAGE IAW MM 27-51-13. 2 L 7 3 4F A3WE 1996110700367 19961107 00367 NM 1996 11 7 UPS96221539 1 19961104 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 940 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE-D, FUSELAGE STR 18A, RT SIDE CRACKED IN OUTER FLANGE AT BRACKET ATTACH HOLE AT BS 940. REPAIRED STRINGE R PER UPS EO B727-53-1830. 2 L 7 3 4F A3WE 1996110700368 19961107 00368 NM 1996 11 7 UPS96221540 1 19961104 A 5753 65190067 FLAP TRACK BOEING 727 72722C 138400F NM LT TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE-D, LEFT I/B FLAP O/B FLAP TRACK NR 3 HAS RUST IN AREA OF AFT MOUNT PAD AND ON MOUNT PAD ON FALSE SPAR. R EMOVED CORROSION PER EO B727-57-0178. 2 L 7 3 4F A3WE 1996110700369 19961107 00369 NM 1996 11 7 UPS96221541 1 19961104 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 344 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE-SI, CORROSION ON STA 344 FLOORBEAM UPPER CHORD LBL 55 TO RBL 45 WL 207. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED UPPER CHORD, FABRICATED NEW UPPER CHORD AND INSTALLED UPPER CHORD. ALL WORK DONE IAW SRM 53-10- 1, 51-10-1, 51-30-2, 53-10-8 AND MM 51-20-151. 2 L 7 3 4F A3WE 1996110700370 19961107 00370 NM 1996 11 7 UPS96221542 1 19961104 A 5311 FRAME BOEING 727 72722C 138400F NM BS 360 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE-D, TENSION BOLTS CORRODED AT BS 360 FRAME BELOW STR 21. REPAIRED PER UPS EO B727-53-1827. 2 L 7 3 4F A3WE 1996110700371 19961107 00371 NM 1996 11 7 UPS96221543 1 19961104 A 5320 65C1573252 FITTING BOEING 727 72722C 138400F NM BS 940 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE-D, FUSELAGE BS 940 FITTING, HFEC SHOWS CRACK INDICATIONS IN OUTER PORTION OF FITTING BETWEEN UPPER AND L OWER FASTENER HOLES SECOND ROW FROM FRONT AND LOWER FASTENER HOLE IN THIRD ROW FROM FRONT. REPLACED RT SIDE 940 FITTING , INSTALLED REPLACEMENT MOUNT PER UPS E O B727-5310-4501E. 2 L 7 3 4F A3WE 1996110700372 19961107 00372 NM 1996 11 7 UPS96221544 1 19961031 A 5313 BAC1498140 STRINGER BOEING 727 72725C 138400H NM BS 435-475 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE-SI, CORROSION ON STRINGER AND SPLICE STR 24R 435 TO 475. REMOVED CORROSION ON STRINGER AND SPLICE, FOUN D TO BE OUT OF LIMITS. REMOVED OLD STR 24R BS 435 TO 475, INSTALLED NEW STR AND SPLICE ALL WORK DONE IAW SRM 53-10-2, 5 3-10-3, 51-30-2, 51-40-3, 51-10-06. 2 L 7 3 4F A3WE 1996110700373 19961107 00373 NM 1996 11 7 UPS96221545 1 19961103 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 1030 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE-SI, CORROSION STA 1030 FLOORBEAM LBL 5 TO 61 AND RBL 5 TO 30 FWD AFT FLANGES RBL 48 TO 55 FWD FLANGE WL 208 AT NUTPLATE HOLES. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-1, REPAIRED PER EO 96-2563. 2 L 7 3 4F A3WE 1996110700374 19961107 00374 NM 1996 11 7 UPS96221546 1 19961101 A 5320 66147361 EXPANSION LINK BOEING 727 72725C 138400H NM BS 740 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE-SI, EXPANSION LINKS ARE CORRODED AT BS 740 WL 162.5 LBL 36 RBL 12. REMOVED CORRODED LINKS WHICH WERE FO UND TO BE OUT OF LIMITS, INSTALLED NEW EXPANSION LINKS IAW SRM 51-10-1, 51-30-2. 2 L 7 3 4F A3WE 1996110700375 19961107 00375 NM 1996 11 7 UPS96221547 1 19961031 A 5320 65222177 STIFFENER BOEING 727 72725C 138400H NM BS 219.8 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE-SI, CORROSION ON STIFFENER BS 219.8 LBL 15 WL 165. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED STIFFENER PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996110700376 19961107 00376 NM 1996 11 7 UPS96421518 1 19961015 A 5330 SKIN BOEING 747 747SR46 NM BS 1600-1740 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE-C, EXTERNAL SKIN, FOUND BLEND OUT SPOTS AND CORROSION AROUND FASTENER HEADS FROM BS 1600 TO 1740 STR 42 TO 46 LT. SKIN PANEL REPAIRED IAW UPS APPROVAL ENGINEERING FILE NR 747-53-0792. 2 L 7 4 4F A20WE 1996110700377 19961107 00377 NM 1996 11 7 UPS96421519 1 19961021 A 5330 SKIN BOEING 747 747SR46 NM BS 1975/1990 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE-C, EXTERNAL FUSELAGE SKIN, PREVIOUS REWORK ON SKIN LAPSPLICE STR 46 BETWEEN BS 1975 TO 1990 IS OUT OF LI MITS ACC TO SRM 53-30-01 FIG 1. LAPSPLICE ON STR 46 BETWEEN BS 1975 AND 1990 LT REPAIRED ACC SRM 53-30-03 FIG 17. 2 L 7 4 4F A20WE 1996110700378 19961107 00378 NM 1996 11 7 UPS96421520 1 19961021 A 5330 SKIN BOEING 747 747SR46 NM BS 1855/1925 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 680UP 20923 INSPECTION TYPE-C, EXTERNAL FUSELAGE SKIN, PREVIOUS REWORK ON SKIN LAPSPLICE BETWEEN BS 1855 TO 1925 AT STR 46 LT IS OUT OF LIMITS ACC TO SRM 53-30-01 FIG 1. REPAIRED SKIN LAPSPLICE BETWEEN BS 1855 TO 1925 AT STR 46 LT IAW SRM 53-30-03 FIG 17. 2 L 7 4 4F A20WE 1996110700379 19961107 00379 WP 1996 11 7 UPS96821521 1 19961006 A 5755 56551651 SPOILER DOUG DC8 DC871F 302199D WP NR 1 SPOILER DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE-C, LT NR 1 SPOILER DELAMINATED. REPLACED SPOILER ASSY PER MM 27-61-01. 2 L 7 4 4F RT 4A25 1996110700380 19961107 00380 WP 1996 11 7 UPS96821548 1 19961102 A 2120 AIR DISTR DOUG DC8 DC871F 302199D WP COCKPIT ODOR A IPXA G O2 MASK DEPLOYED B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 729UP 46029 INSPECTION TYPE-N/A, 25 MINUTES INTO FLIGHT STRONG ODOR SMELLED LIKE BURNING RUBBER. DONNED OXYGEN MASK, EMERGENCY DECL ARED AND ALL CHECKLIST COMPLIED WITH. SMELL SEEMED STRONGER IN COCKPIT, NO VISIBLE SMOKE. RAN ALL 4 ENGINES, ALL ELEC TRICAL SYSTEMS POWERED UP, BOTH PACKS ON FULL FLOW, CYCLED ENGINE BLEEDS AND COULD NOT DUPLICATE PROBLEM. INSPECTED AIR CONDITION BAYS, LOWER E AND E COMPARTMENTS, RADIO RACKS, C/B PANELS, EQUIPMENT COMPARTMENTS UNDER AND NEXT TO F/E DESK, NO DISCREPANCIES NOTED AT THIS TIME. 2 L 7 4 4F RT 4A25 1996110700381 19961107 00381 NM 1996 11 7 96FDEA01638 1 19961031 A 5330 65545739 SKIN BOEING 727 727233 138408A NM BS 676-679 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 NR 0450 028. CORROSION (C53-111-01(1) ON STR 26 LT AND SPLICE STA 676-679 WL 152 STR 26 LT (FWD BAY). UPON REMOVAL OF STRINGER, FOUND CORROSION ON SKIN AT BS 662. REPAIRED STRINGER AND SKIN BETWEEN BS 650-680, WL 152, STR 26 LT. PER FE DEX SRM 53-30-3, 53-10-3. 2 L 7 3 4F RT A3WE 1996110700382 19961107 00382 NM 1996 11 7 96FDEA01639 1 19961031 A 5320 651627910 BEAM BOEING 727 727233 138408A NM BS 784-810 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 NR 0712 027. CORROSION (C53-224-01(2)) ON LONGITUDINAL BEAM AT BS 784 TO BS 810 LBL 25 WL 208 P/N 65-16279-10. REMOVE D AND REPLACED LONGITUDINAL BEAM BS 784-810 LBL 25, WL 208 PER FEDEX SRM 51-10-1. 2 L 7 3 4F RT A3WE 1996110700383 19961107 00383 WP 1996 11 7 96FDEA01640 1 19961102 A 5312 BULKHEAD PANEL DOUG DC10 DC1030 3023501 WP CTR MLG WW CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 317FE 46835 SNRM N00944, CENTER GEAR WHEEL WELL, LT BULKHEAD ACCESS PANELS 146AN AND 146BN PANEL LAND CORRODED. *S/D* REWORKED PER EA WORK INSTRUCTIONS, EA NR 8-5310-31745, STEPS 1 TO 5 FOR AFT ACCESS PANEL 146 IN, AND STEPS 1 TO 3 FOR FWD ACCESS PA NEL 146BN FWD ACCESS PANEL 146BN. FOLLOW-UP ACTION PERMANENT REPAIR TO BE ACCOMPLISHED DURING NEXT SCHEDULED C-CHECK. 2 L 7 3 4F A22WE 1996110700384 19961107 00384 NM 1996 11 7 96FDEA01641 1 19961031 A 2750 654044 CONTROL VALVE BOEING 727 7272S2F 1384O81 NM TE FLAPS INOPERATIVE A A FDEA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 213FE 22935 INBOARD TRAILING EDGE FLAPS FAILED TO EXTEND, INBOARD ALTERNATE FLAP CIRCUIT BREAKER POPPED WHEN ALTERNATE FLAP SWITCH A CTUATED. REPLACED INBOARD FLAP CONTROL VALVE PER 727-200 MAINTENANCE MANUAL CHAPTER 27-51-51. SERVICED HYDRAULIC SYSTE M, RIGGED SYSTEM PER MAINTENANCE MANUAL. 2 L 7 3 4F A3WE 1996110700385 19961107 00385 WP 1996 11 7 96FDEA01642 1 19961101 A 5714 CTR WING SECTION DOUG DC10 DC1010F 3022111 WP BS 1205 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 050FE 47804 SNRM 211, MAIN CABIN, UPR SURFACE OF CTR WING SECTION CORROSION AT LT SIDE APPROX STA 1205. *S/D* REWORKED PER EA 8-5 710-31746 WORK INSTRUCTIONS. 2 L 7 3 4F A22WE 1996110700386 19961107 00386 WP 1996 11 7 96FDEA01643 1 19961101 A 5714 CTR WING SECTION DOUG DC10 DC1010F 3022111 WP BS 1205 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 050FE 47804 SNRM 222, MAIN CABIN, UPPER SURFACE OF CTR WING SECTION CORROSION AT RT SIDE APPROX STA 1205, SIDEWALL AREA. *S/D* REW ORKED PER EA 8-5710-31746 WORK INSTRUCTIONS. 2 L 7 3 4F A22WE 1996110700387 19961107 00387 WP 1996 11 7 96FDEA01644 1 19961101 A 5714 CTR WING SECTION DOUG DC10 DC1010F 3022111 WP BS 1341 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 050FE 47804 SNRM 227, MAIN CABIN, UPPER SURFACE OF CENTER WING SECTION CORROSION AT LT SIDE APPROX STA 1341, SIDEWALL AREA. *S/D* R EWORKED PER EA 8-5710-31746 WORK INSTRUCTIONS. 2 L 7 3 4F A22WE 1996110700388 19961107 00388 WP 1996 11 7 96FDEA01645 1 19961101 A 5714 CTR WING SECTION DOUG DC10 DC1010F 3022111 WP BS 1185 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 050FE 47804 SNRM 232, MAIN CABIN, UPPER SURFACE OF CENTER WING SECTION CORROSION AT LT SIDE APPROX STA 1185, SIDEWALL AREA. *S/D* R EWORKED PER EA 8-5710-31746 WORK INSTRUCTIONS. 2 L 7 3 4F A22WE 1996110700389 19961107 00389 NM 1996 11 7 96FDEA01646 1 19961031 A 5315 BAC150529222 FLOORBEAM BOEING 727 727233 138408A NM BS 344 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 NR 0635 026. CORROSION (C53-224-01(1) ON 344 BEAM FROM LBL 60 TO RBL 20 WL 208.1. REMOVED CORROSION ON 344 FLOOR BEAM, TOP CHORD FROM LBL 60 TO RBL 20, W/L 208.1. FOUND TO BE OUT OF LIMITS IAW 727 FEDEX SRM 53-10-01. REMOVED AND REPLACE D FLOOR BEAM TOP CHORD AT BS 344 RBL 70 TO 70 IAW FEDEX STANDARD REPAIR DRAWING SR 27-53-007. 2 L 7 3 4F RT A3WE 1996110700390 19961107 00390 WP 1996 11 7 SCNA96320 1 19961026 A 2612 24402534 FIRE LOOP DOUG DC10 DC1030F 3023504 WP NR 2 ENGINE INTERMITTANT A SCNA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 GL 15 602GC 47923 FIRE LOOP-B ON ENGINE NUMBER 2 ILLUMINATED INTERMITTANTLY DURING FLIGHT. TROUBLESHOT SYSTEM PER MM 26-11-03 AND FOUND C ANNON PLUG P1-8004 PUSHED BACK. RESEATED PIN, CLEANED ALL CONNECTIONS AND OPS CHECKED SYSTEM. 2 L 7 3 4F RT A22WE 1996110700391 19961107 00391 WP 1996 11 7 SCNA96321 1 19961027 A 2611 13131 SMOKE DETECTOR DOUG DC10 DC1010 3022110 WP CARGO COMPT INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 573SC 46905 NUMBER 1 CARGO SMOKE DETECTOR DOES NOT TEST. REPLACED BEACON LAMP IN SMOKE DETECTOR AND OPS CHECKED GOOD. 2 L 7 3 4F A22WE 1996110700392 19961107 00392 NM 1996 11 7 SCNA96322 1 19961029 A 2612 106687713 FIRE LOOP BOEING 727 727227 1384078 NM NR 1 ENGINE OUT OF POSITION A SCNA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 GL 15 275AF 22092 NUMBER 1 ENGINE FIRE LOOP DETECTION LIGHT ILLUMINATED INFLIGHT. REPOSITIONED NUMBER 1 ENGINE FIRE LOOP AND OPS CHECKED GOOD. 2 L 7 3 4F A3WE 1996110700393 19961107 00393 WP 1996 11 7 SCNA96323 1 19961101 A 3350 P4010051127 POWER SUPPLY DOUG DC10 DC1010 3022110 WP CABIN INOPERATIVE A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 573SC 46905 FOUND RIGHT FORWARD EMERGENCY FLOOR LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK POWER SUPPLY AND OPS CHECKED GOOD. 2 L 7 3 4F A22WE 1996110700394 19961107 00394 WP 1996 11 7 ARWA9611001 1 19961102 A 3310 BA170 BALLAST DOUG DC8 DC862 3021970 WP COCKPIT FAILED A ARWA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 19 791AL 46150 AIRCRAFT DIVERTED TO SJU. WHILE IN CRUISE AT FL 330, 2150Z, SMOKE WAS NOTED COMING FROM F/O SIDE PANEL. EMERGENCY PROCED URES WERE FOLLOWED AND AN OVERWEIGHT LANDING WAS MADE WITHOUT INCIDENT. TROUBLESHOOTING BY MTX LOCATED A BURNED OUT FLU ORESCENT LIGHT BALLAST. BALLAST WAS REMOVED AND REPLACED, SYS OPS CHECKED NORMAL. OVERWEIGHT LANDING INSPECTION REVEAL ED NO STRUCTURAL DAMAGE. 2 L 7 4 4F 4A25 1996110700395 19961107 00395 WP 1996 11 7 CKSA96192 1 19961101 A 2612 57775621 FIRE LOOP DOUG DC8 DC861 3021952 WP PWA JT3D JT3D3B 52039 NE NR 3 ENGINE CHAFED A CKSA F ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 GL 23 24UA 45963 644561 FIRE WARNING NR 3 ENGINE. DISCHARGED ONE FIRE BOTTLE. RIGHT WING INBOARD FIRE BOTTLE REMOVED. INSPECTED NR 3 ENGINE AN D FOUND NO EVIDENCE OF FIRE. FOUND FIRE LOOP CHAFING. ADJUSTED AND OPS CHECKED GOOD PER DC-8 MM 26-10-1. REPLACED FIR E BOTTLE PER DC-8 MM 26-20-1. 2 L 7 4 4F 4 F 4A25 1E8 1996110700396 19961107 00396 WP 1996 11 7 CKSA96193 1 19961102 A 2612 57775621 FIRE LOOP DOUG DC8 DC861 3021952 WP PWA JT3D JT3D3B 52039 NE NR 3 ENGINE GROUNDED A CKSA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 GL 23 24UA 45963 644561 FIRE WARNING NR 3 ENGINE. THE LIGHT IN HANDLE WENT OUT APPROXIMATELY 45 SECONDS AFTER SHUTDOWN. FIRE BELL AND WARNING LIGHTS REACTIVATED INTERMITTENTLY FOR APPROXIMATELY 5 MINUTES, DID NOT FIRE BOTTLE. INSPECTED NR 3 ENGINE, FOUND NO EVI DENCE OF FIRE. INSPECTED DIFFUSER CASE AND PNEUMATIC SYSTEM FOR POSSIBLE LEAKS AND CRACKS, NONE NOTED. DURING WINDMILL INSPECTION FOUND OIL STRAINER TO BE FREE AND CLEAR OF ANY DIRT OR DELAMINATION. FOUND POSSIBLE GROUNDING IN LOWER FIRE LOOP. ADJUSTED SETTING PER DC-8 MM 26-10-1. RAN ENGINE AT IDLE FOR 10 MINUTES, OPS CHECK GOOD PER DC-8 MM 72-00. 2 L 7 4 4F 4 F 4A25 1E8 1996110700397 19961107 00397 SO 1996 11 7 SRAA961016 1 19961031 A 2910 HYD FITTING LKHEED 382 382E 526413U SO WHEEL WELL LEAKING A SRAA O OTHER K FLUID LOSS CR CRUISE 1 GL 23 908SJ 4300 DURING FLIGHT, UTILITY HYDRAULIC PRESSURE DUMPED, MANUALLY LOWERED GEAR AND LANDED WITHOUT INCIDENT. FOUND NORMAL BRAKE LINE UNDER FLIGHT DECK LEAKING. REPLACED MS FITTING ON HYDRAULIC LINE, SYSTEM OPS CHECKED GOOD PER MM CH 29. 2 H 7 4 4T A1SO 1996110700398 19961107 00398 SO 1996 11 7 SRAA961101 1 19961101 A 2160 GASKET LKHEED 382 382G 526414U SO SHUT OFF VLV BLOWN A SRAA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 GL 23 909SJ 4763 DURING FLIGHT, CARGO COMPARTMENT OVERHEAT LIGHT CAME ON AT FL230. SHUT OFF AIR CONDITIONING SYSTEM PER QUICK REFERENCE HANDBOOK, AIRCRAFT LANDED WITHOUT INCIDENT. FOUND UNDER FLOOR HEAT SHUTOFF VALVE HAD BLOWN GASKET. REPLACED GASKET, SY STEM OPS CHECKED GOOD PER MM CH 21. 2 H 7 4 4T A1SO 1996110700399 19961107 00399 GL 1996 11 7 HEEA968394 2 19961023 A 7260 23030917 BEARING 23035178 BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL GEAR BOX NR 3 MAKING METAL E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 129MR 421 CAG95165 51129 CAE895165 ENGINE REMOVED DUE TO METAL IN OIL. UPON INSPECTION OF GEARBOX PARTS NOTED: (1) METAL SLIVERS ON #3 BEARING INNER RACE (2) CRACKED ROLLER RETAINER & METAL SLIVERS ON #4 BEARING INNER RACE. INSTALLED NEW BEARINGS. SEE MMIR# HEEA0008395 F OR #4 BEARING INFORMATION. 1 G 7 1 3U 3 U H2SW E1GL 1996110700400 19961107 00400 GL 1996 11 7 HEEA968395 2 19961023 A 7260 23030917 BEARING 23035178 BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL GEAR BOX NR 4 MAKING METAL E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 129MR 421 CAG95165 51129 CAE895165 ENGINE REMOVED DUE TO METAL IN OIL. UPON INSPECTION OF GEARBOX PARTS NOTED: (1) METAL SLIVERS ON #3 BEARING INNER RACE (2) CRACKED ROLLER RETAINER & METAL SLIVERS ON #4 BEARING INNER RACE. INSTALLED NEW BEARINGS. SEE MMIR# HEEA0008395 F OR #4 BEARING INFORMATION. 1 G 7 1 3U 3 U H2SW E1GL 1996110700401 19961107 00401 SW 1996 11 7 HEEA968396 1 19961025 A 5313 212030128169S LONGERON ASSY 212030100111 BELL 412 412 1182202 SW TAIL BOOM MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 ADW06010 NEW LONGERON APPEARS TO HAVE HAD ATTACHMENT BOSS PREVIOUSLY MILLED, LEAVING INSUFFICIENT HEIGHT OF BOSS FOR PROPER MILLI NG AFTER INSTALLATION OF PART. 1 G 7 2 4U H4SW 1996110700402 19961107 00402 SW 1996 11 7 HEEA968397 1 19961025 A 6730 222382001105 ACTUATOR ASSY BELL 230 230 1182149 SW PILOT VALVE BINDING E HEEA K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 SW 03 230UN 154 23009 ACTUATOR ASSY PILOT VALVE BINDING, CAUSING FEEDBACK IN CYCLIC. 1 G 7 2 3U NC H9SW 1996110700403 19961107 00403 SW 1996 11 7 HEEA968398 1 19961025 A 6220 206010110105 WASHER 206011100159 BELL 206 206L3 1182108 SW M/R THRUST DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6160Y 204 A2660 51609 THRUST WASHER REMOVED DUE TO TIGHT TRUNNION AND UNABLE TO BALANCE. CHECKED CENTERING AND FOUND WITHIN LIMITS. FOUND TH RUST PLUGS BREAKING DOWN, CAUSING TIGHT TRUNNION. 1 G 7 1 3U H2SW 1996110700404 19961107 00404 EU 1996 11 7 HEEA968399 1 19961025 A 7722 1179405105 INDICATOR BOLKMS 117 BK117A3 5626015 EU COCKPIT TOT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 TOT INDICATOR CHECKED BAD. 1 G 7 2 3U H13EU 1996110700405 19961107 00405 EU 1996 11 7 HEEA968400 1 19961025 A 7722 1179405105 INDICATOR BOLKMS 117 BK117A3 5626015 EU COCKPIT TOT READS HIGH E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 401PH 7050 TOT INDICATOR READS 10-15 PERCENT C HIGH THROUGHOUT RANGE. 1 G 7 2 3U H13EU 1996110700406 19961107 00406 SW 1996 11 7 HEEA968401 1 19961025 A 6710 206001062003 WASHER BELL 206 206L3 1182108 SW M/R CONTROL MIS LUBED E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 SLIDING LUBRICATED SURFACE ON ONE SIDE OF THRUST WASHER UNEVENLY APPLIED. 1 G 7 1 3U H2SW 1996110700407 19961107 00407 SW 1996 11 7 HEEA968402 1 19961025 A 6710 206001144021 TUBE ASSY BELL 206 206L3 1182108 SW CYCLIC JACKSHAFT MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 UNDER CUTS ON TUBE FOR ATTACHMENT TO ELBOW ASSY (P/N 206-001-150-101) USING BOLTS (2 EACH AN4-17A) TOO SHALLOW, NOT ALLO WING BOLT PENETRATION. TUBE REMOVED FROM AIRCRAFT REPAIRED LOCALLY. 1 G 7 1 3U H2SW 1996110700408 19961107 00408 SW 1996 11 7 HEEA968403 1 19961030 A 6220 412010145105 DAMPER SET BELL 412 412 1182202 SW M/R SEPARATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K 1319 36001 DAMPERS SEPARATED CAUSING LEAD AND LAG PROBLEMS. SEE MMIR # HEEA0008403 FOR ADDITIONAL DAMPER SET REPLACED. 1 G 7 2 4U H4SW 1996110700409 19961107 00409 SW 1996 11 7 HEEA968404 1 19961030 A 6220 412010145105 DAMPER SET BELL 412 412 1182202 SW M/R SEPARATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K 1319 36001 DAMPERS SEPARATED CAUSING LEAD AND LAG PROBLEMS. SEE MMIR # HEEA0008404 FOR ADDITIONAL DAMPER SET REPLACED. 1 G 7 2 4U H4SW 1996110700410 19961107 00410 SW 1996 11 7 HEEA968405 1 19961030 A 6510 222044003105 HANGER ASSY BELL 230 230 1182149 SW T/R DRIVE BEARING ROUGH E HEEA K NONE E VIBRATION/BUFFET IN INSP/MAINT 1 SW 03 230UN 3478 23009 HIGH FREQUENCY VIBRATION IN AIRFRAME. FOUND BEARING ROUGH AT T/R DRIVE #3 LOCATION. 1 G 7 2 3U NC H9SW 1996110700411 19961107 00411 EU 1996 11 7 HEEA968406 1 19961030 A 6410 355A12004008 BLADE SNIAS 350 AS350B2 8680813 EU T/R SEPARATION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100R 1480 2862 T/R BLADE TIP SEPARATION AND SB 05.11RS PAN 1C2. 1 G 7 1 3U H9EU 1996110700412 19961107 00412 EU 1996 11 7 HEEA968407 1 19961030 A 6410 355A12004008 BLADES SNIAS 350 AS350B2 8680813 EU T/R WONT BALANCE E HEEA K NONE E VIBRATION/BUFFET IN INSP/MAINT 1 SW 03 60951 1233 2771 AIRCRAFT HAS HIGH FREQUENCY VIBRATION. T/R VIBRATION WAS CHECKED AND FOUND OVER 2 IPS AND COULD NOT BALANCE BELOW .7 IP S. 1 G 7 1 3U H9EU 1996110700413 19961107 00413 SW 1996 11 7 HEEA968408 1 19961030 A 6710 214001970111 ACTUATOR ASSY BELL 214 214ST 1182106 SW M/R DEFECTIVE E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 ACTUATOR ASSY WOULD NOT COMPLETE TEST. 2 G 7 2 4U H10SW 1996110700414 19961107 00414 GL 1996 11 7 HEEA968409 2 19961101 A 7250 6899081 COMBUSTION LINER 23035128 SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL TURBINE DEFECTIVE E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 31219 CAT95259 760230 CAE890431S UPON INSTALLATION OF COMBUSTOR LINER NOTED: UNABLE TO INSTALL FUEL NOZZLE AND IGNITER PLUGS DUE TO MISALIGNMENT. REPLAC ED DISCREPANT PART. 1 G 7 2 3U 3 U H1NE E1GL 1996110700415 19961107 00415 SW 1996 11 7 HEEA968410 1 19961101 A 7810 23032325 COLLECTOR 23035128 BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL EXHAUST CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31077 CAT97841 51520 CAE895129 TURBINE REMOVED DUE TO OVERHAUL. UPON INSPECTION NOTED THE FOLLOWING: EXCESSIVE CRACKS BEYOND SERVICEABLE LIMITS ON EX HAUST COLLECTOR AS MARKED. REPLACED DISCREPANT PART. 1 G 7 1 3U 3 U H2SW E1GL 1996110700416 19961107 00416 SW 1996 11 7 PNSA961001 1 19961018 A 3260 1EN516 SWITCH SWRNGN SA227 SA227AC 8780603 SW LT MLG INTERMITTENT A PNSA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 AL 03 46NE AC746B LT MLG DOWN LIGHT DID NOT ILLUMINATE. CYCLED GEAR, GOT GOOD INDICATION, LANDING OK. REPLACED LT INBD SWITCH. 2 L 7 2 4T RT A8SW 1996110700417 19961107 00417 SW 1996 11 7 PNSA961002 1 19961014 A 5610 2621126008 WINDSHIELD SWRNGN SA227 SA227AC 8780603 SW RT COCKPIT CRACKED A PNSA A UNSCHED LANDING O OTHER CR CRUISE 1 AL 03 2719H AC713B COPILOT WINDSHIELD CRACKED, RETURNED ANC. REPLACED WINDSHIELD. 2 L 7 2 4T RT A8SW 1996110700418 19961107 00418 1996 11 7 PNSA961003 4 19961030 A 3445 TPU66A TCAS SWRNGN SA227 SA227AC 8780603 SW E/E COMPT MALFUNCTIONED A PNSA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 AL 03 41NE AC741B TCAS GAVE FALSE WARNING DURING TAXI. RERACKED COMPUTER, TEST OK. 2 L 7 2 4T RT A8SW 1996110700419 19961107 00419 WP 1996 11 7 CALA9601546 1 19961018 A 5330 SKIN DOUG DC9 DC981 3022081 WP BS 237 IMPACTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16883 48073 INSPECTION FOUND IMPACT DAMAGE TO LT FUSELAGE SKIN, CAUSED BY JETWAY, AT STA 237 AFT OF MAIN CARGO DOOR. NEW SKIN WAS I NSTALLED IAW ECRA 5330-01203, SRM 51-30-2, 51-30-5, 51-20-0. 2 L 7 2 4F A6WE 1996110700420 19961107 00420 WP 1996 11 7 CALA9601547 1 19961014 A 5230 ANGLE DOUG DC9 DC981 3022081 WP CARGO D00R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16883 48073 INSPECTION FOUND A 2 INCH CRACK IN FORWARD BAGGAGE BIN INTERNAL ANGLE AT BOTTOM AFT STOP FITTING. A REPAIR WAS INSTALLE D IAW ECRA 5230-01335. 2 L 7 2 4F A6WE 1996110700421 19961107 00421 WP 1996 11 7 CALA9601548 1 19961015 A 5311 FRAME DOUG DC9 DC981 3022081 WP BS 1463 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16883 48073 INSPECTION FOUND 3 CRACKS IN CANTED FRAME WEB ON RT SIDE AT STA 1463. THE CRACKS WERE .5 TO 1 INCH LENGTH. THE WEB WAS REPLACED IAW SRM 51-30-2, 51-30-5 AND 53-14-4. 2 L 7 2 4F A6WE 1996110700422 19961107 00422 WP 1996 11 7 CALA9601549 1 19961021 A 5320 DOUBLER DOUG DC9 DC981 3022081 WP NLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16883 48073 INSPECTION FOUND A .2187 INCH CRACK IN REPAIR DOUBLER AT NOSE WHEEL WELL LEFT AFT DOOR HINGE CUTOUT. A NEW REPAIR DOUBL ER WAS INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1996110700423 19961107 00423 WP 1996 11 7 CALA9601550 1 19961024 A 5320 ANGLE DOUG DC9 DC981 3022081 WP BS 1155-1212 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16883 48073 INSPECTION FOUND CORROSION ON AFT BAGGAGE BIN Z-ANGLE FROM STA 1155 TO 1212. A REPAIR DOUBLER AND STRAPPER WAS INSTALL ED IAW SRM 53-05, FIGURE 63. 2 L 7 2 4F A6WE 1996110700424 19961107 00424 WP 1996 11 7 CALA9601551 1 19961014 A 5230 DOOR PAN DOUG DC9 DC981 3022081 WP CARGO DOOR CRACKED A CALA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 09 16883 48073 INSPECTION FOUND A .5 INCH CRACK AT BOTTOM FORWARD STOP PAD OF FORWARD BAGGAGE BIN DOOR PAN. A DOUBLER WAS INSTALLED IA W ECRA 65C0123. 2 L 7 2 4F A6WE 1996110700425 19961107 00425 WP 1996 11 7 CALA9601552 1 19961016 A 5320 WEB DOUG DC9 DC981 3022081 WP BS 218 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16883 48073 INSPECTION FOUND CORROSION ON WEB INBOARD OF CUSP AT STA 218, LT SIDE. DOUBLERS WERE INSTALLED IAW ECRA 5310-03343. 2 L 7 2 4F A6WE 1996110700426 19961107 00426 SO 1996 11 7 COMA9610320 1 19961101 A 2132 720159001410 INDICATOR EMB 120 EMB120RT SO INST PANEL MALFUNCTION A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 265CA 120257 CABIN PRESSURIZATION FLUCTUATED 1,500 FT IN AUTO MODE BUT WAS STABLE IN MANUAL. REPLACED THE CABIN PRESSURIZATION TRIPL E INDICATOR SYSTEM, CHECK NORMAL. 2 L 7 2 4T RT A31SO 1996110700427 19961107 00427 SO 1996 11 7 COMA9610321 1 19961101 A 5246 FUEL DOOR EMB 120 EMB120RT SO RT WING NOT LATCHED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 1117H 120117 SERVICE DOOR WARNING ACTIVATED AFTER TAKEOFF. FOUND FUEL SERVICE DOOR UNLATCHED. SECURED DOOR CLOSED AND AIRCRAFT RETU RNED TO SERVICE. 2 L 7 2 4T RT A31SO 1996110700428 19961107 00428 SO 1996 11 7 COMA9610322 1 19961102 A 3230 RETRACT MECH EMB 120 EMB120RT SO LT MLG MALFUNCTIONED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 1117H 120117 LT MLG DID NOT EXTEND ON FIRST ATTEMPT. LANDING GEAR CYCLED 4 TIMES BEFORE A DOWNLOCK INDICATION WAS RECEIVED. COULD N OT DUPLICATE DISCREPANCY. LANDING GEAR WAS INSPECTED AND CYCLED 25 TIMES WITH NO DEFECTS NOTED. 2 L 7 2 4T RT A31SO 1996110700429 19961107 00429 EU 1996 11 7 COMA9630155 1 19961101 A 6120 8542M2 COMPUTER SAAB SF340 SF340A 7850100 EU AUTO COARSEN SYS MALFUNCTION A A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 359CA 13165 520 340A053 AUTO COARSEN WARNING ON CWP DURING TAKEOFF. REPLACED THE AUTO COARSEN COMPUTER. 2 L 7 2 4T RT A52EU 1996110700430 19961107 00430 EU 1996 11 7 COMA9630156 1 19961102 A 2913 4018501 HYD PUMP SAAB SF340 SF340A 7850100 EU NOSE HYD BAY WEAK A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 340SF 18308 489 340A014 HYDRAULIC SYSTEM WARNING ON CWP SYSTEM PRESSURE INDICATED ZERO AND LANDING GEAR INDICATED UNSAFE. REPLACED THE HYDRAULI C SYSTEM PUMP. 2 L 7 2 4T RT A52EU 1996110700431 19961107 00431 NE 1996 11 7 COMA9660194 2 19961102 A 7200 ENGINE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RIGHT MALFUNCTIONED A COMA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 01 914CA 7012 807076 ON CLIMBOUT, RT ENGINE VIBRATION 3.1, 10,000 FT 85 PERCENT. VIBRATION WAS CONTROLLED WITH REDUCTION OF THRUST LEVER, CO CKPIT NOISE WAS LOUDER THAN NORMAL. REPLACED RIGHT ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 1996110700432 19961107 00432 NM 1996 11 7 96FDEA01647 1 19961020 A 5754 652174958 BULLNOSE BOEING 727 727233 138408A NM NR 1 LE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 NR 0397 030. CORROSION (C57-562-01-1) NR 1 K-FLAP BULLNOSE I/B LINKAGE ATTACH POINT. REMOVED AND REPLACED NR 1 K-FLAP BULLNOSE. FUNCTIONAL TESTED. WORK DONE IAW FEDEX M/M 27-81-1. 2 L 7 3 4F RT A3WE 1996110700433 19961107 00433 NM 1996 11 7 96FDEA01648 1 19961104 A 5754 6521750513 BULLNOSE BOEING 727 727233 138408A NM NR 2 LE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 NR 0407 029, CORROSION ON NR 2 K-FLAP BULLNOSE O/B BONDING JUMPER AND LOWER ATTACH POINT. *S/D* REMOVED CORROSION AND REPAIRED NR 2 K-FLAP BULLNOSE O/B BONDING JUMPER ATTACHMENT POINTS IAW FEDEX SRM 57-50-3 AND FEDEX SR 27-57-010. 2 L 7 3 4F RT A3WE 1996110700434 19961107 00434 NM 1996 11 7 96FDEA01649 1 19961104 A 5750 652163479 I/B AFT FLAP BOEING 727 72722 1384002 NM UPR SRF/OB TIE DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 149FE 19087 NR 0151 001 LT WING I/B AFT FLAP HAS TWO AREAS OF DELAMINATION IN O/B AFT HALF SECTION. REPAIRED DAMAGED SKIN TO LT W ING I/B AFT FLAP IAW FEDEX SRM 51-40-6. 2 L 7 3 4F A3WE 1996110700435 19961107 00435 WP 1996 11 7 ABXA9600654 1 19961030 A 3350 43 BULB DOUG DC9 DC941 302207N WP CABIN DEFECTIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 965AX 47498 FIRST OFFICERS EMERGENCY LIGHTING INOPERATIVE. RELAMPED, OPS CHECKED GOOD PER DC-9 MM 33-10-0. 2 L 7 2 4F A6WE 1996110700436 19961107 00436 WP 1996 11 7 ABXA9600655 1 19961031 A 2110 TURBO COMP DOUG DC8 DC862 3021970 WP NR 2 FAILED A ABXA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 23 804AX 45987 ABOUT 15 MINUTES AFTER TURNING ON NR 2 CTC, A BURNT OIL SMELL WAS NOTICED OUT OF THE AIR CONDITIONING VENTS. TURNED OFF NR 2 CTC, SMELL QUIT. DEFERRED NR 2 CTC I/A/W DC-8 MEL 21-1B, CAT C, CODE 11. ALL MAINTENANCE PROCEDURES COMPLIED WIT H, PLACARD INSTALLED DI 804 353 MBCB 11-11-96. 2 L 7 4 4F 4A25 1996110700437 19961107 00437 WP 1996 11 7 MWEA96619 1 19961102 A 2560 591769037 COVER DOUG DC9 DC914 3022034 WP GALLEY DOOR LOOSE A MWEA K NONE O OTHER UK UNKNOWN 1 GL 31 500ME 45711 GALLEY DOOR EMERGENCY ESCAPE SLIDE COVER NEEDS TO BE REINSTALLED. REINSTALLED SLIDE COVER. 2 L 7 2 4F A6WE 1996110700438 19961107 00438 WP 1996 11 7 MWEA96620 1 19961102 A 3350 60030431 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 207ME 47794 FWD OVERWING EMERGENCY EXIT LIGHT ON LT AND RT SIDES VERY DIM. FOUND BATTERY PACK NOT CHARGING. REMOVED AND REPLACED B ATTERIES AND BATTERY PACK FOR FWD OVERWING EXIT LIGHT. 2 L 7 2 4F A6WE 1996110700439 19961107 00439 WP 1996 11 7 SCNA96324 1 19961101 A 3260 MS25237327 LAMP DOUG DC10 DC1010 3022110 WP MLG INDICATOR INOP A SCNA O OTHER P NO WARNING INDICATION DE DESCENT 1 GL 15 573SC 46905 NO INDICATION OF GREEN ON LEFT MAIN GEAR. VISUALLY CONFIRMED GEAR WAS DOWN AND LOCKED, AND PULLED EMERGENCY EXTENSION. FOUND BULB BURNT OUT. REMOVED AND REPLACED. 2 L 7 3 4F A22WE 1996110700440 19961107 00440 WP 1996 11 7 SCNA96325 1 19961016 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 836 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON LEFT HAND CABIN FLOOR STRUCTURE, APPROXIMATELY STATION 836 AND 18 INCHES LE FT OF THE C-LIFT. REMOVED CORROSION, FABRICATED AND INSTALLED A REPAIR PER ENGINEERING ORDER INSTRUCTIONS AND SRM CHAPT ER 51. 2 L 7 3 4F A22WE 1996110700441 19961107 00441 WP 1996 11 7 SCNA96326 1 19961017 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1871 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1871, LBL 40. REMOVED CORRODED SUPPORT, FABRICATED AND INSTALLED A NEW SUPPORT IN ACCORDANCE WITH SRM 51-21-01 AND SRM 51-30-00. 2 L 7 3 4F A22WE 1996110700442 19961107 00442 WP 1996 11 7 SCNA96327 1 19961017 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 1119 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND A CRACK ON THE LOWER FLANGE OF A FRAME AT BS 1119, BETWEEN LONGERONS 49L AND 50R. REMOV ED DAMAGED FLANGE CLIP AND INSTALLED A NEW FLANGE CLIP IN ACCORDANCE WITH SRM 53-30-00 FIGURE 5. 2 L 7 3 4F A22WE 1996110700443 19961107 00443 WP 1996 11 7 SCNA96328 1 19961017 A 5230 AGA38813 ANGLE DOUG DC10 DC1010 3022110 WP CARGO DOOR CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORRODED ANGLE ON INSIDE CORNER OF AFT CARGO DOOR. REMOVED ANGLE, FABRICATED AND INSTAL LED A NEW ANGLE IN ACCORDANCE WITH SRM 51-21-01 AND SRM 5121-02. 2 L 7 3 4F A22WE 1996110700444 19961107 00444 WP 1996 11 7 SCNA96329 1 19961021 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1964 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1964, LBL 64. REMOVED FLOOR SUPPORT, FABRICATED AND IN STALLED A NEW FLOOR SUPPORT IN ACCORDANCE WITH SRM 51-42-00. 2 L 7 3 4F A22WE 1996110700445 19961107 00445 WP 1996 11 7 SCNA96330 1 19961021 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1964 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1964, LBL 46. REMOVED FLOOR SUPPORT, FABRICATED AND IN STALLED A NEW FLOOR SUPPORT IN ACCORDANCE WITH SRM 51-40-00. 2 L 7 3 4F A22WE 1996110700446 19961107 00446 WP 1996 11 7 SCNA96331 1 19961021 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1887 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1887, LBL 33. REMOVED FLOOR SUPPORT, FABRICATED AND IN STALLED A NEW FLOOR SUPPORT IN ACCORDANCE WITH SRM 51-30-00. 2 L 7 3 4F A22WE 1996110700447 19961107 00447 WP 1996 11 7 SCNA96332 1 19961021 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1887 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1887, LBL 45. REMOVED FLOOR SUPPORT, FABRICATED AND IN STALLED A NEW FLOOR SUPPORT IN ACCORDANCE WITH SRM 51-30-00. 2 L 7 3 4F A22WE 1996110700448 19961107 00448 WP 1996 11 7 SCNA96333 1 19961022 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1921 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1921, RBL 20 TO RBL 49. REMOVED FLOOR SUPPORT, FABRICA TED AND INSTALLED A NEW FLOOR SUPPORT IN ACCORDANCE WITH SRM 51-21-00. 2 L 7 3 4F A22WE 1996110700449 19961107 00449 WP 1996 11 7 SCNA96334 1 19961022 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1900-1921 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1900 TO 1921, LBL 13. REMOVED CORRODED SECTION, FABRIC ATED AND INSTALLED A NEW SECTION IN ACCORDANCE WITH SRM 51-30-00. 2 L 7 3 4F A22WE 1996110700450 19961107 00450 WP 1996 11 7 SCNA96335 1 19961022 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP BS 1887-1964 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON SEAT TRACK BETWEEN BS 1887 AND BS 1964, RBL 88 TO RBL 78. REMOVED DAMAGED SECTION OF SEAT TRACK, FABRICATED AND INSTALLED A NEW SEAT TRACK IN ACCORDANCE WITH 53-70-00. 2 L 7 3 4F A22WE 1996110700451 19961107 00451 WP 1996 11 7 SCNA96336 1 19961022 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1923 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1923, LBL 13 TO RBL 13. REMOVED CORRODED SECTION OF SU PPORT, FABRICATED AND INSTALLED A NEW SECTION OF FLOOR SUPPORT IN ACCORDANCE WITH SRM 51-10-00 AND SRM 51-31-00. 2 L 7 3 4F A22WE 1996110700452 19961107 00452 WP 1996 11 7 SCNA96337 1 19961022 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1921 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1921, RBL 13. REMOVED CORRODED SUPPORT, FABRICATED AND INSTALLED A NEW SECTION OF FLOOR SUPPORT IN ACCORDANCE WITH SRM 51-31-00. 2 L 7 3 4F A22WE 1996110700453 19961107 00453 WP 1996 11 7 SCNA96338 1 19961022 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1887-1920 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1887 TO BS 1920, BL 0. REMOVED CORRODED SECTION OF SUP PORT, FABRICATED AND INSTALLED A NEW SECTION OF FLOOR SUPPORT IN ACCORDANCE WITH SRM 51-31-00. 2 L 7 3 4F A22WE 1996110700454 19961107 00454 WP 1996 11 7 SCNA96339 1 19961022 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP BS 1800 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON SEAT TRACK FROM BS 1800, RBL 67 TO BS 1887, RBL 59. REMOVED DAMAGED SECTIO N OF SEAT TRACK, FABRICATED AND INSTALLED NEW SECTION OF SEAT TRACK IN ACCORDANCE WITH SRM 53-70-00. 2 L 7 3 4F A22WE 1996110700455 19961107 00455 WP 1996 11 7 SCNA96340 1 19961022 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP BS 1835 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON SEAT TRACK FROM BS 1835 LBL 65 TO BS 1887, LBL 60. REMOVED DAMAGED SECTION OF SEAT TRACK, FABRICATED AND INSTALLED NEW SECTION OF SEAT TRACK IN ACCORDANCE WITH SRM 53-70-00. 2 L 7 3 4F A22WE 1996110700456 19961107 00456 WP 1996 11 7 SCNA96341 1 19961023 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP BS 1960 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON SEAT TRACK AT BS 1960, LBL 78. REMOVED DAMGED SEAT TRACK SECTION, FABRICAT ED AND INSTALLED A NEW SECTION IN ACCORDANCE WITH SRM 51-31-01. 2 L 7 3 4F A22WE 1996110700457 19961107 00457 WP 1996 11 7 SCNA96342 1 19961024 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP BS 791-840 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON TOP FLANGE OF THE LEFT HAND INBOARD SEAT TRACK AT BS 791 TO 840. REMOVED C ORROSION, FABRICATED AND INSTALLED A REPAIR DOUBLER PER ENGINEERING ORDER. 2 L 7 3 4F A22WE 1996110700458 19961107 00458 NM 1996 11 7 P5CA9600865 1 19961101 A 5280 BRACKET BOEING 747 747122 1384872 NM LT MLG DOOR BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 BROKEN AFT SUPPORT BRACKET FOR THE LEFT WING LANDING GEAR GULL DOOR. REMOVED AND REPLACED BROKEN SUPPORT BRACKET PER BO EING SRM 51-10-01. 2 L 7 4 4F A20WE 1996110700459 19961107 00459 NM 1996 11 7 P5CA9600866 1 19961101 A 7810 SLEEVE BOEING 747 747122 1384872 NM NR 4 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 SMALL CRACK NR 4 ENGINE EXHAUST SLEEVE AT 9 O'CLOCK POSITION. STOP DRILLED CRACK AND FABRICATED DOUBLER AND INSTALLED A S PER BOEING SRM 51-40-02 AND REPLACED LOOSE FASTENERS PER BOEING SRM 51-30-02. 2 L 7 4 4F A20WE 1996110700460 19961107 00460 NM 1996 11 7 P5CA9600867 1 19961103 A 5320 RIVETS BOEING 747 747122 1384872 NM BS 1980/2030 POPPED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 EIGHT POPPED RIVETS AT BULK CARGO DOOR FRAME 5 AT BS 1980 AND 3 AT BS 2030. REPLACED RIVETS PER BOEING SRM 51-30-02. 2 L 7 4 4F A20WE 1996110700461 19961107 00461 NM 1996 11 7 P5CA9600868 1 19961103 A 5330 SKIN BOEING 747 747122 1384872 NM DOOR CUTOUT GOUGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 TWO GOUGES IN FUSELAGE SKIN AT AFT CARGO DOOR CUT AFT SIDE. BLENDED GOUGES PER BOEING SRM 51-10-01. 2 L 7 4 4F A20WE 1996110700462 19961107 00462 NM 1996 11 7 P5CA9600869 1 19961102 A 3610 7289354 BLEED VLV PLATE BOEING 747 747132 1384882 NM NR 3 ENGINE BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 PLATE FOR LOCKOUT OF NR 3 ENGINE HIGH STAGE BLEED VALVE BROKEN. REPLACED BROKEN LOCKOUT PLATE PER BAC MM 36-11-05. 2 L 7 4 4F A20WE 1996110700463 19961107 00463 NE 1996 11 7 P5CA9600870 2 19961102 A 7520 65B9016617 COOLING SHROUD BOEING 747 747132 1384882 NM PWA JT9 JT9D7A 52054 NE NR 2 ENGINE BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 COOLING SHROUD BROKEN ON NR 2 ENGINE GENERATOR. REPLACED NR 2 ENGINE GENERATOR COOLING SHROUD PER BAC MM 75-21-02. 2 L 7 4 4F 4 F A20WE E20EA 1996110700464 19961107 00464 SO 1996 11 7 SRAA961104 1 19961103 A 2150 2037201 COOLING TURBINE LKHEED 382 382G 526414U SO CARGO COMP INOPERATIVE A SRAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 921SJ 4586 ON TAXI OUT, CARGO COMPARTMENT OVERHEAT WARNING LIGHT CAME ON, AIRCRAFT RETURNED TO BLOCK. FOUND CARGO COMPARTMENT COOL ING TURBINE INOPERATIVE, REPLACED COOLING TURBINE, SYSTEM OPS CHECKED GOOD PER M.M. CH 21-00. 2 H 7 4 4T A1SO 1996110700465 19961107 00465 SO 1996 11 7 SRAA961105 1 19961104 A 5320 FITTING LKHEED 382 382G 526414U SO BS 938 CRACKED A SRAA K NONE O OTHER IN INSP/MAINT 1 GL 23 905SJ 4472 POST FLIGHT INSPECTION FOUND THE STRUT BRACE ATTACH FITTING AT STATION 938 CRACKED. REPAIRED AFT FUSELAGE LOWER LONGERO N FITTING AT STATION 938 IAW SRM CH 53-50-26, OPS CHECKED RAMP AND DOOR, SYSTEM OPS CHECKED GOOD. 2 H 7 4 4T A1SO 1996110700468 19961107 00468 CE 1996 11 7 96ZZZX5546 1 19960926 A 3610 600100 PERISEAL 9912056 CESSNA 500 550 2076604 CE LT ENG BLEED BROKEN A A ISYA K NONE N FALSE WARNING NR NOT REPORTED 1 GL 25 8415A 5500484 PILOT REPORTED FIRE WARNING LIGHT CAME ON IN-FLIGHT. THROTTLE WAS REDUCED AND LIGHT WENT OUT. TROUBLESHOT SYSTEM AND F OUND BROKEN PERI-SEAL ON INBOARD SIDE OF LEFT ENGINE ALLOWED BLEED AIR TO BLOW ON FIRE LOOP. NO ADDITIONAL PROBLEM FOUN D. REPLACED 2 PERI-SEALS AND OPS TESTED OK. 1 L 7 2 4F A22CE 1996110700472 19961107 00472 EU 1996 11 7 96ZZZX5550 1 19961007 A 6210 355A11002009 BLADE AEROSP AS355 AS355F1 8680810 EU M/R CRACKED A A M3XA K NONE O OTHER IN INSP/MAINT 1 WP 07 911TM 2578 4488 5059 DURING A SCHEDULED 100-HOUR INSPECTION WHILE CLEANING THE MAIN ROTOR BLADES, A 6 INCH CRACK WAS DISCOVERED ON THE LOWER SURFACE 4 FEET, 6 INCHES FROM THE ROOT END. STARTING 1 INCH FROM THE TRAILING EDGE TRAVELING CORDWISE, BUT DID NOT MEET THE SPAR AREA. NO IDEAS AS TO WHAT CAUSED THE CRACK. IT IS A GOOD IDEA TO REMOVE BLADES IF POSSIBLE WHEN INSPECTING T HEM DUE TO THE DROOP OF THE BLADES WHEN STATIONARY, THE CRACK IS ALMOST IMPOSSIBLE TO SEE. 1 G 7 2 3U H11EU 1996110700484 19961107 00484 NE 1996 11 7 GXPA96004 2 19961021 A 7200 ENGINE HAMFLU HFB320 HFB320 4071204 EU GE CJ610 CJ6105 30006 NE NR 1/NR 2 FLAME OUT A GXPA B EMER. DESCENT X ENGINE FLAMEOUT CR CRUISE 1 GL 23 173GA 1052 A/C WAS EN ROUTE, A/C ALT 33,000 FEET SKIRTING THUNDERSTORMS EXPERIENCED SEVERE TURBULENCE, NR 2 ENGINE FLAMED OUT. STA RTED DESCENT, AIRSTART ON, NR 1 ENGINE FLAMED OUT AT 31,000 FEET. RELIT ENGINES ABOVE 10,000 FEET WITHOUT ANY PROBLEMS. MADE PRECAUTIONARY LANDING. FOUND NO DEFECTS, OPERATIONAL CHECK OK. A/C RETURNED TO SERVICE. (X) 2 L 7 2 4J 4 J A14EU 1E16 1996110700496 19961107 00496 WP 1996 11 7 WRLA96038 1 19960908 A 3222 ACG7023503 UPPER BEARING DOUG DC10 DC1030 3023501 WP NLG STRUT GALLED A A WRLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 9MMAS 46955 DURING CLIMB-OUT, FLT CREW SELECTED L/G 'UP'. NOSE GEAR FAILED TO RETRACT, AND INDICATED 'UNSAFE'. GEAR WAS RE-SELECTE D TO DOWN POSITION. ALL L\G ASSYS TRANSITIONED TO 'DOWN AND LOCKED' POSITION. FLT CREW ELECTED TO RETURN TO POINT OF D EPART (KLAX) FOR MX ACTION. A/C LANDED W/O FURTHER INCIDENT. MAINTENANCE FOUND 'GROUND SENSING BRACKET' BROKEN. SUBMI TTER STATES, MALFUNCTION WAS CAUSED BY THE NOSE STRUT NOT FULLY EXTENDING WHEN LEAVING GROUND. INVESTIGATION OF NOSE ST RUT IDENTIFIED THAT 'UPPER BEARING' WAS GALLED, CAUSING THE INNER CYLINDER TO NOT FULLY EXTEND. UPPER BEARING WAS REPLA CED, NOSE STRUT WAS RESEALED, AND GROUND SENSING BRACKET REPLACED. A/C WAS JACKED AND OPS CHECKED OK. 2 L 7 3 4F A22WE 1996110700497 19961107 00497 EU 1996 11 7 VTZA96399 1 19960928 A 5270 SWITCH BAG JETSTM JETSTM3201 1500217 EU PAX DOOR LACK OF LUBE A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 490UE 909 FLT 6383 - CMH-IAD - DURING CLIMB, MADE A UNSCHEDULED LANDING DUE TO PASSENGER DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MX OPENED DMI 52632, MEL 52-2. MX CLOSED DMI 09-29-96 BY CLEANING AND LUBI NG MICROSWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996110700499 19961107 00499 NE 1996 11 7 VTZA96395 2 19960924 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE RIGHT FAILURE A VTZA K NONE J WARNING INDICATION CR CRUISE 1 EA 27 306UE 41020 P76063 FLT 6182 - TYS-IAD - DURING CRUISE, CONTINUED FLIGHT WITH ONE DISCREPANCY WHICH WAS RIGHT ENGINE OIL CONTAMINATION LIGHT ILLUMINATED IN FLIGHT, ENGINE PARAMETERS NORMAL. AIRCRAFT LANDED AND WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENAN CE REMOVED AND REPLACED RIGHT ENGINE. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 4 T RT A41NM E18NE 1996110700500 19961107 00500 WP 1996 11 7 VTZA96397 2 19960925 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LEFT FAILURE A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 27 471UE 821 P66033 FLT 6363 - LYH-IAD - ABORTED TAKEOFF DUE TO LEFT ENGINE TORQUE LOW ON TAKEOFF. AIRCRAFT LANDED AND RETURNED TO GATE WIT H NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED ENGINE. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVI CE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996110700501 19961107 00501 EA 1996 11 7 HNAA9690566 1 19960919 A 3260 805310 PROXIMITY BOX ELDEC DHAV DHC7 DHC7102 2802708 EA LT MLG FAILED A HNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 07 905HA 17050 PA6347 070 FLT 3084 - DCA-PHL - AFTER GEAR RETRACTION, THE LEFT MAIN RED GEAR LIGHT CYCLES ON AND OFF CONTINUOUSLY. LOUD BANGING N OISE COMING FROM THE NOSE GEAR AREA. THE AIRCRAFT TURNED BACK AND LANDED IN DCA WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 MAIN GEAR PROXIMITY BOX. (M) 2 H 7 4 4T A20EA 1996110700502 19961107 00502 NM 1996 11 7 AALA961313 1 19960904 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 365-418 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - FOUND RIGHT CREASE ANGLE CORRODED STATION 365 TO 418. CUT OUT CORRODED CREASE ANGLE AND REPLACED CREASE ANGLE. ( M) 2 L 7 3 4F A3WE 1996110700503 19961107 00503 NM 1996 11 7 AALA961314 1 19960904 A 5314 KEEL BEAM BOEING 727 727223 1384074 NM BS 800 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - FOUND CORROSION ON BOTTOM O KEEL BEAM STATION 800. REMOVED CORROSION AND INSTALLED WEB REPAIR DOUBLER PER SRM 51- 40-2 PAGE 6 AND EDGE SEALED. (M) 2 L 7 3 4F A3WE 1996110700504 19961107 00504 EU 1996 11 7 AALA961144 1 19960801 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU BS 4514-4585 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14065 508 TUL - RIGHT FLOOR SUPPORT FOUND 2 SPOTS OF CORROSION BETWEEN FR 71 TO FR 72. REMOVED AND REPLACED CORRODED FLOOR SUPPOR T IAW SRM 51-10-00-3. TREATED, PRIMED, AND PAINTED PER SRM 51-21-00-0. (M) 2 L 7 2 4F RT A35EU 1996110700505 19961107 00505 EU 1996 11 7 AALA961418 1 19960903 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 38.1 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 40064 507 TUL - DURING C-CHECK, FOUND CORROSION ON FOUR FASTENER HOLES IN FLOOR SUPPORT FRAME 38.1 AT AFT END OF NR 1 TRACK IN FOR WARD CARGO COMPARTMENT. REMOVED CORRODED SECTION OF FLOOR SUPPORT AND INSTALLED DOUBLER REPAIR PER SRM 53-10-15 AND 51- 10-00-3. (M) 2 L 7 2 4F RT A35EU 1996110700506 19961107 00506 EU 1996 11 7 AALA961416 1 19960829 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU BS 2081 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 40064 507 TUL - FOUND CORROSION ON NR 3 SEAT TRACK AT LAV L. REMOVED AND REPLACED NR 3 SEAT TRACK PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 1996110700507 19961107 00507 EU 1996 11 7 AALA961414 1 19960829 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU BS 2188 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 40064 507 TUL - FOUND CORROSION ON SEAT TRACK NR 3, STATION 2188. REMOVED CORROSION AND INSTALLED ALUMINUM PLUG AND APPLIED PRO S EAL 870 SEALANT PER ESO 3095. (M) 2 L 7 2 4F RT A35EU 1996110700508 19961107 00508 EU 1996 11 7 AALA961319 1 19960904 A 5347 TRACK AIRBUS 300 A300B4605R 3930308 EU CARGO COMPT CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 40064 507 TUL - FOUND CARGO ROLLER TRACK HAS CORROSION AT PAD LOCK ATTACH HOLES AT FRAME 35. SPLICED IN NEW SECTION OF ROLLER TRA Y IAW SRM 53-10-15 FIG 202. (M) 2 L 7 2 4F RT A35EU 1996110700509 19961107 00509 EU 1996 11 7 AALA961382 1 19960919 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FS 29-31 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 90070 513 TUL - FOUND NR 8 SEAT TRACK HAS CORROSION BETWEEN FS 29 AND 31. REPLACED SEAT TRACK FROM FRAME 29-33 PER SRM 51-72-10-0 . (M) 2 L 7 2 4F RT A35EU 1996110700510 19961107 00510 EU 1996 11 7 AALA961384 1 19960919 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FS 31 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 90070 513 TUL - FLIGHT ATTENDANT SEAT TRACK JUST OUTBOARD OF TRACK NR 8 CORROSION AT FRAME 31. REPLACED TRACK PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1996110700511 19961107 00511 EU 1996 11 7 AALA961387 1 19960920 A 5320 TRAY AIRBUS 300 A300B4605R 3930308 EU FRAME 32-38.2 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 90070 513 TUL - FOUND RIGHT OUTBOARD ROLLER TRAY CORRODED FROM UNDERNEATH FROM FRAME 32038.2. SPLICED SECTION OF ROLLER TRAY AS P ER SRM 53-10-15 FIG 202. (M) 2 L 7 2 4F RT A35EU 1996110700512 19961107 00512 EU 1996 11 7 AALA961389 1 19960923 A 5320 ANGLE AIRBUS 300 A300B4605R 3930308 EU FRAME 38.2 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 90070 513 TUL - FOUND UPPER T-ANGLE FRAME 38.2 HOLES ARE CORRODED LEFT SIDE WHERE ROLLER TRACY MOUNTS. SPLICED SECTION OF T-ANGLE AND REPLACED CORNER FITTING PER SRM 53-10-15, 53-10-14, 51-21-00. (M) 2 L 7 2 4F RT A35EU 1996110700513 19961107 00513 EU 1996 11 7 AALA961388 1 19960920 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FRAME 31-32 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 90070 513 TUL - FOUND CORROSION ON TRACK NR 1 BETWEEN 31 AND 32 FRAMES AFT OF FRAME OF L2 DOOR UNDER LAV L. REPLACED SECTION OF T RACK PER SRM 51-74-10-0. (M) 2 L 7 2 4F RT A35EU 1996110700514 19961107 00514 EU 1996 11 7 AALA961391 1 19960919 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 75 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 90070 513 TUL - FOUND SUPPORT AT FR 75 JUST INBOARD OF LEFT AFT DOOR AFT PART OF DOOR OPENING IS CORRODED. REPLACED SECTION OF FL OOR BOARD SUPPORT SECTION PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1996110700515 19961107 00515 EA 1996 11 7 96ZZZM1433 2 19960820 A 7200 ENGINE DHAV DHC7 DHC7102 2802708 EA PWA PT6 PT6A50 52043 EA NR 3 FAILED A CICA O OTHER J WARNING INDICATION AP APPROACH 1 SO 17 4860J 19 PCE86432 FLT 4927 - MIA-PID - PILOT REPORTED NR 3 ENGINE OIL PRESSURE LIGHT ILLUMINATED AND OIL PRESSURE DROPPED. ON FINAL IN TO PID, OIL PRESSURE CONTINUED TO DROP. PILOT SHUT DOWN NR 3 ENGINE. THE AIRCRAFT WAS INSPECTED AND FOUND TO BE SAFE FOR 3 ENGINE FERRY TO FLL MAINTENANCE BASE. UPON ARRIVAL, AT FLL, NR 3 ENGINE OIL CHECK DIP STICK INDICATED NO OIL. ENGIN E WAS REMOVED AND REPLACED. OPERATIONAL CHECK GOOD AND AIRCRAFT RETURNED TO SERVICE. DEFECTIVE ENGINE RETURNED TO OVER HAUL FACILITY FOR REPAIR. 2 H 7 4 4T 4 T A20EA E4EA 1996110700516 19961107 00516 NM 1996 11 7 TAOA099609 1 19960923 A 3350 081691 LIGHT SOCKET BRUCE BOEING 727 727225 1384077 NM CABIN MISSING A TAOA K NONE O OTHER IN INSP/MAINT 1 EA 15 919TS 20447 EMERGENCY PATH LIGHTING, LIGHT SOCKET MISSING AT ROW 26. INSTALLED LIGHT SOCKET ASSEMBLY. (M) 2 L 7 3 4F A3WE 1996110700517 19961107 00517 EU 1996 11 7 AWXA960520 1 19960922 A 3350 321454 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 643AW 1928 315 PHX - FLT 2082 - DURING ROUTINE MAINTENANCE CHECK, FOUND AFT SEAT ROW 26 MOUNTED EMERGENCY LIGHTS INOP. FOUND LEFT MID- CABIN EMERGENCY LIGHT POWER SUPPLY FAILED. REPLACED UNIT. REPLACED L MID-CABIN EMERGENCY LIGHT BATTERY PACK WITH SERVI CEABLE BATTERY. SYSTEM OPS CHECK OK. (M) 2 L 7 2 4F RT A28NM 1996110700518 19961107 00518 EU 1996 11 7 96ZZZM1434 1 19960922 A 3350 321430 BATTERY PACK AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 643AW 5713 315 PHX - FLT 2082 - DURING ROUTINE MAINTENANCE CHECK, FOUND AFT SEAT ROW 26 MOUNTED EMERGENCY LIGHTS INOP. FOUND LEFT MID- CABIN EMERGENCY LIGHT POWER SUPPLY FAILED. REPLACED UNIT. REPLACED L MID-CABIN EMERGENCY LIGHT BATTERY PACK WITH SERVI CEABLE BATTERY. SYSTEM OPS CHECK OK. REFERENCE AWXA960520. 2 L 7 2 4F RT A28NM 1996110700519 19961107 00519 NM 1996 11 7 AWXA960525 1 19960924 A 2751 1817389 FLAP POS XMITTER BOEING 737 7373Q8 1384670 NM LT TE FLAP MALFUNCTIONED A AWXA K NONE F FLT CONT AFFECTED AP APPROACH 1 WP 28 327AW 0711 23507 PDX - FLT 2367 - ASYMMETRICAL FLAPS ON APPROACH INTO PDX RIGHT T/E FLAP AT 10 DEGREES, LEFT T/E FLAP AT 15 DEGREES. RET RACTED TO 10 DEGREES MADE APPROACH AND LANDED AT PDX. EMERGENCY DECLARED. MAINTENANCE FERRY AIRCRAFT TO PHX CHANGED BO TH LEFT AND RIGHT FLAP POSITION TRANSMITTER OPS CHECK OK. (M) 2 L 7 2 4F RT A16WE 1996110700520 19961107 00520 NM 1996 11 7 96ZZZM1435 1 19960924 A 2751 1817389 FLAP POS XMITTER BOEING 737 7373Q8 1384670 NM RT TE FLAP MALFUNCTIONED A AWXA K NONE F FLT CONT AFFECTED AP APPROACH 1 WP 28 327AW 0039 23507 PDX - FLT 2367 - ASYMMETRICAL FLAPS ON APPROACH INTO PDX RIGHT T/E FLAP AT 10 DEGREES, LEFT T/E FLAP AT 15 DEGREES. RET RACTED TO 10 DEGREES MADE APPROACH AND LANDED AT PDX. EMERGENCY DECLARED. MAINTENANCE FERRY AIRCRAFT TO PHX CHANGED BO TH LEFT AND RIGHT FLAP POSITION TRANSMITTER OPS CHECK OK. REFERENCE AWXA960525. 2 L 7 2 4F RT A16WE 1996110700521 19961107 00521 NM 1996 11 7 MZZA96071 1 19960917 A 5330 65545906 SKIN BOEING 727 727224 1384076 NM BS 720 CORROSION A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79744 22253 GUM - DURING B-CHECK, FOUND CORROSION AT LOWER FUSELAGE SKIN BS 720B RAM AIR DOOR CUTOUT AREA. ITEM CLASSIFIED AS MAJOR REPAIR PER ENGINEERING. EC/RA 5330-02438 WAS INITIATED AND AUTHORIZED BY BOEING AND FAA DER. MAINTENANCE REPAIRED COR ROSION AREA AS PER EC/RA 5330-02438. (M) 2 L 7 3 4F A3WE 1996110700522 19961107 00522 NM 1996 11 7 MZZA96072 1 19960903 A 5310 STRUCTURE BOEING 727 727212 138407G NM BS 950 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 86430 21947 TNN - DURING 1/2D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT AT THE F OLLOWING AREAS; FUSELAGE SKIN INNER SURFACE AT BS 950 PLUS 8 BETWEEN STRINGER 28R AND STRINGER 29R, STRINGER 29R KEEL BE AM CHORD OUTBOARD FLANGE AT BS 950 PLUS 4, BS 950 BULKHEAD LOWER CHORD BETWEEN STRINGER 28R AND STRINGER 29R. THE CORRO DED AREAS WAS CLEANED UP AND REPAIRED PER CAL EC/RA 5310-03323. REF HANGAR NON ROUTINE REPAIR ITEM CARD NR 807033 AND 8 07034 SEQ NR 01080 AND 01081. (M) 2 L 7 3 4F A3WE 1996110700523 19961107 00523 NM 1996 11 7 MZZA96077 1 19960930 A 2560 65C1990119 LATCH ASSEMBLY BOEING 727 727212 138407G NM L1 ENTRY DOOR WIRE BROKEN A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 86430 21947 DURING 1/2 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, EXCESSIVE BROKEN WIRES WERE FOUND ON L1 ENTRY DOOR ESCAPE SLIDE L ATCH CABLE. THE DAMAGED ESCAPE SLIDE LATCH ASSEMBLY WAS REMOVED AND REPLACED PER B727 MM 25-60-15. REF HANGAR NON ROUT INE REPAIR ITEM CARD NR 803383 9SEQ NR 02083. (M) 2 L 7 3 4F A3WE 1996110700524 19961107 00524 NM 1996 11 7 MZZA96076 1 19960915 A 5311 FRAME BOEING 727 727212 138407G NM BS 970 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 86430 21947 DURING 1/2D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, 4 INCH LONG CRACK WAS FOUND ON BS 970 FRAME BETWEEN STRINGER 27L A ND STRINGER 26L. THE CRACK WAS STOP DRILLED AND REPAIR PER B727 SRM 53-10-4 FIGURE 1 IN CONJUNCTION WITH CAL ENGINEERIN G AUTHORIZATION 5310-02256 OP 17. REF HANGAR NON ROUTINE REPAIR ITEM CARD NR 804367, SEN NR 01148. (M) 2 L 7 3 4F A3WE 1996110700525 19961107 00525 NM 1996 11 7 MZZA96075 1 19960909 A 3350 EXIT SIGN BOEING 727 727212 138407G NM CABIN BROKEN A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 86430 21947 DURING 1/2 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, BROKEN COVER WAS FOUND ON PASSENGER CABIN AT THE FOLLOWING POSITI ON 'EXIT' SIGN COVER; AFT ENTRY DOOR, L2 CABIN DOOR, L1 CABIN DOOR. THE DAMAGED 'EXIT' SIGN ASSEMBLIED WERE REMOVED AND REPLACED WITH BR9279-105 ASSEMBLIES PER B727 MM 33-50-11 AND OPERATIONAL CHECK FOUND SATISFACTORY. REF HANGAR NON ROUT INE REPAIR ITEM CARD NR 803488, 803486, 803484, SEQ NR 02218, 02216, 02214. (M) 2 L 7 3 4F A3WE 1996110700526 19961107 00526 NE 1996 11 7 AALA960645 2 19960423 A 7532 AC67760 BLEED VALVE BOEING 757 757223 1384957 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE DEFECTIVE A A AALA A E UNSCHED LANDING ENGINE SHUTDOWN X ENGINE FLAMEOUT DE DESCENT 1 SW 07 636AM 24594 31038 LAX - FLT 421 - EN ROUTE DFW/SNA AT START OF DESCENT FROM FL 390 WITH ENG ANTI-ICE ON, POWER WAS REDUCED AND LT ENG EXPE RIENCED FLAMEOUT. ACCOMP ENG SHUTDOWN AND ATTEMPTED RESTART WITH NO SUCCESS. A/C DIVERTED TO LAX AND LANDED W/O INCIDE NT. REPLACED LT ENG. ACCOMP LEAK CHECKS AND GRD ENG RUN WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION . 'IP' BLEED SOLENOID VALVE FOUND TO HAVE A SEIZED PISTON RING AND THE INLET SIDE OF THE VLV EXIHIBITED SIGNS OF EXCESS IVE HEAT AND AIR LEAKED. THE SOLENOID VLV FAILED TO OPEN THE BLEED VLVS, RESULTING IN NON-RECOVERABLE COMPRESSOR STALL. ENGINE PROCESSED THROUGH SHOP FOR RETURN TO SERVICE. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 1996110700527 19961107 00527 EU 1996 11 7 USAAF96102 2 19960922 A 7320 CASC509 FUEL CONTL REG FOKKER F28 F28MK0100 4990807 EU RROYCE SPEY SPEY55515 54521 EU RT ENGINE FAILED A A USAA E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 893US 11373 RIC-PHL - FLT 1150 - AFTER TAKEOFF, NR 2 ENGINE REMAINED AT TAKEOFF POWER. CAPTAIN DISCONNECTED THE AUTOTHROTTLE AND AT TEMPTED TO SLOW ENGINE WITH THROTTLE. THIS DID NOT WORK. ENGINE EXCEEDED N2 LIMIT SO CAPTAIN SHUTDOWN THE ENGINE. FLI GHT RETURNED TO RIC ON ONE ENGINE WITH NO FURTHER INCIDENT. NO EMERGENCY WAS DECLARED ALTHOUGH EMERGENCY EQUIPMENT WAS REQUESTED TO STANDBY. MX REPLACED NR 2 FUEL CONTROL REGULATOR. ALSO, ACCOMP TRIM CHECK. TEST OF AUTO THROTTLE AND TOG A SWITCHES NORMAL. ENGINE RUNUP AND FUNCTIONAL TESTS NORMAL. (M0 2 L 7 2 4F 4 F RT E2EU 1996110700528 19961107 00528 WP 1996 11 7 GTIANK198 1 19960916 A 2612 CONNECTOR DOUG DC9 DC932 3022066 WP B-FIRE LOOP LOOSE A GTIA O OTHER N FALSE WARNING IN INSP/MAINT 1 GL 23 941ML 47131 FOUND ON DAILY, NR 1 ENGINE FIRE DETECTOR B-LOOP INOP. FOUND BAD CONNECTOR FORWARD PYLON B-LOOP. CONNECTOR ON ORDER DE FERRED B-LOOP SYSTEM. NR 1 ENGINE PER MEL 26-1 DMI NR 002701. S/D REMOVED AND REPLACED CONNECTOR AT B-LOOP HARNESS APR ON. OPS CHECK SATISFACTORY. THIS CLEARS DMI NR 2701. (M) 2 L 7 2 4F A6WE 1996110700529 19961107 00529 NM 1996 11 7 96ZZZM1436 1 19960719 A 2612 896768 FIRE LOOP BOEING 737 737214 138446R NM APU EXHAUST CRUSHED A ZZDA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SO 15 460AT 3660 20158 FLT 800 - MCO-OMA - 35 MINS INTO FLT APU FIRE WARNING CAME ON. APU WAS NOT IN USE AT THE TIME. FLT CREW PULLED THR FI RE HANDLE AND DISCHARGED THE FIRE BOTTLE. AN EMERGENCY WAS DECLARED INTO GAINSVILLE, FL. AN UNEVENTFUL LANDING WAS MAD E. MECHANICS OPENED THE APU ACCESS DOOR AND INSPECTED THE APU COMPART AND TAILPIPE AREA FOR EVIDENCE OF FIRE OR OVERHEA T. NO EVIDENCE WAS FOUND. APU AND APU FIRE DETECTION SYSTEM WERE PLACED ON MEL. THE LOOP WAS REPLACED AND FUNCTIONAL CHECK WERE PERFORMED. A CHECK FLT WAS CONDUCTED AND THE APU AND APU FIRE DETECTION SYS PERFORMED NORMAL. APU AND APU F IRE DETECTECTION WERE REMOVED FROM MEL. (M) 2 L 7 2 4F A16WE 1996110700530 19961107 00530 WP 1996 11 7 VTZA96369 2 19960908 A 7313 310411013 FUEL NOZZLE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE3311 01514 WP RT ENGINE FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK X ENGINE FLAMEOUT TO TAKEOFF 1 EA 27 301UE 41012 FLT 6369 - IAD-EWR - ABORTED TAKEOFF DUE TO RIGHT ENGINE FLAME OUT. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS . MAINTENANCE REMOVED AND REPLACED FUEL NOZZLES, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVIC E. (M) 2 L 7 2 4T 3 T RT A41NM E3WE 1996110700531 19961107 00531 WP 1996 11 7 VTZA96367 2 19960909 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP RIGHT LOW POWER A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 EA 27 491UE 911 FLT 6181 - IAD-BWI - ABORTED TAKEOFF DUE TO RIGHT ENGINE WOULD ONLY PRODUCE 94 PERCENT TORQUE. AIRCRAFT RETURNED TO GAT E WITH NO FURTHER PROBLEMS. MAINTENANCE GROUND RAN AIRCRAFT, COULD NOT DUPLICATE, MADE TARGET TORQUE OF 98 PERCENT. AI RCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 3 T RT A56EU E3WE 1996110700532 19961107 00532 EU 1996 11 7 C2XA96IA255 1 19961017 A 2710 S2711009100000 BELLCRANK AEROSP ATR42 ATR42320 8680930 EU LT AILERON RUSTY A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 25811 094 IAH - DURING 3C-CHECK INSPECTION, ROUTINE INSPECTION OF THE AILERON CONTROL SYSTEM FOUND A CONTROL ROD BELLCRANK TO HAVE RUSTY BEARINGS. THE LEFT WING AILERON CONTROL SYSTEM BELLCRANK AT RIB NR 23 WAS REMOVED AND REPLACED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996110700533 19961107 00533 EU 1996 11 7 C2XA96IA254 1 19961017 A 2760 S0001003400000 ROD ASSY AEROSP ATR42 ATR42320 8680930 EU LT SPOILER RUSTY A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 25811 094 IAH - DURING 3C-CHECK INSPECTION, OF THE AILERON CONTROL SYSTEM, THE LEFT SPOILER FEEDBACK ROD WAS FOUND TO HAVE RUSTY B EARINGS AT ROD END. MAINTENANCE REMOVED AND REPLACED THE LEFT SPOILER FEEDBACK ROD AND THE AIRCRAFT WAS APPROVED FOR RE TURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996110700534 19961107 00534 EU 1996 11 7 C2XA96BT011 1 19961008 A 2612 FIRE WARNING AEROSP ATR42 ATR42320 8680930 EU RT ENGINE FALSE WARNING A C2XA D F RETURN TO BLOCK ACTIVATE FIRE EXT. J WARNING INDICATION TX TAXI/GRND HDL 1 SW 09 14819 156 EWR - FLT 3577 - TAXIING FOR TAKEOFF, REPORTED 'RIGHT ENGINE FIRE. DISCHARGED BOTH BOTTLES'. INSPECTED NR 2 ENGINE IAW ATR-42 JIC 70-00-00-SDI-10000-001. NO DEFECTS NOTED, SUSPECT FALSE WARNING DUE TO EXCESSIVE TAILWIND DURING TAXI. REM OVED AND REPLACED BOTH FIRE BOTTLES, CLEANED ENGINES, AND BOTH BOTTLE SQUIBS TEST GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 1996110700535 19961107 00535 1996 11 7 WRLA96043 4 19961018 A 3460 4059050909 FMC DOUG MD11 MD11 3023602 NM COCKPIT MALFUNCTIONED A A WRLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 273WA 48519 DURING INITIAL CLIMB-OUT, FLIGHT CREW EXPERIENCED A DUAL FLIGHT MANAGEMENT COMPUTER FAILURE. PIC ELECTED TO DIVERT TO P OINT OF DEPARTURE. AIRCRAFT RETURNED TO AIRPORT OF DEPARTURE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNE L WERE UNABLE TO DUPLICATE ANY FAULT WITH EITHER FLIGHT MANAGEMENT COMPUTER. PERFORM ALL RETURN TO SERVICE TESTS WITH N O FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A22WE 1996110700536 19961107 00536 NM 1996 11 7 UIEA9612 1 19960918 A 2612 877535 CONNECTOR BOEING 747 747245F 1384897 NM APU COMPARTMENT LOOSE A UIEA K NONE N FALSE WARNING CR CRUISE 1 EA 15 636FE 21764 FLT GT1051 - MIA-POS - DURING CRUISE, APU FIRE WARNING. COMPLETED MEMORY ITEMS. APU INOP. UPON LANDING AT POS, APU 'B ' LOOP FIRE WARNING LIGHT CAME ON. DEFERRED ITEM. FOUND WIRE ON 'B' LOOP TO AFT APU ACCESS DOOR CONNECTOR LOOSE ON PIN . MADE TEMP REPAIR ON ON 9/20/96 AT MIA. ON 9/23/96 AT MIA, REPLACED AFT APU ACCESS DOOR 'B' LOOP CONNECTOR. OPERATIO NAL CHECK NORMAL. (M) 2 L 7 4 4F A20WE 1996110700537 19961107 00537 NM 1996 11 7 UIEA9611 1 19961002 A 3610 CLAMP BOEING 747 747230B 1384889 NM NR 4 ENGINE LOOSE A UIEA K NONE J M WARNING INDICATION OVER TEMP CL CLIMB 1 EA 15 507MC 21380 ATB - FLT EX9880 -DXB/DXB - NR 4 ENGINE, BOTH NACELLE TEMP INDICATORS INDICATED 8.4 ON SCALE AT CLIMB POWER CLOSED BLEED VALVE NO CHANGE. REDUCED THROTTLE TO IDLE, INDICATIONS DROPPED TO 2-2.5, SAME AS NR 1, NR 2, NR 3 ENGINE. AT HIGHER P OWER INDICATIONS FOLLOW THROTTLE. FOUND NACELLE ANTI-ICE TOP ATTACHMENT CLAMP ADRIFT AND LEAKING AIR. CLAMP REMOVED AN D VISUALLY INSPECTED, FOUND NO DAMAGE. CLAMP REINSTALLED AND TORQUED. LEAK CHECK, PERFORMED SATISFACTORILY. (M) 2 L 7 4 4F A20WE 1996110700538 19961107 00538 NM 1996 11 7 HNAA9693469 1 19960927 A 3350 82410165001 CONTROL BOX DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A HNAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 07 934HA 139 FLT 3204 - CLT-CHA - THE FLIGHT ATTENDANT REPORTED THE EMERGENCY LIGHTS WERE FLICKERING WHILE TAXIING. THE AIRCRAFT RET URNED TO THE GATE. REMOVED AND REPLACED THE EMERGENCY LIGHT CONTROL BOX. (M) 2 H 7 2 4T RT A13NM 1996110700539 19961107 00539 EU 1996 11 7 PLGA9610161 1 19960927 A 6120 SWITCH SAAB SF340 SF340A 7850100 EU AUTO COARSEN OUT OF POSITION A PLGA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 NE 05 745BA 340A111 MHT - FLT 4889 - AIRCRAFT DIVERTED TO MHT FOLLOWING SEVERAL POWER INTERRUPTIONS AND EVENTUAL FLAME OUT. INVESTIGATION I NTO THE INCIDENT FOUND THE CAUSE OF THE EVENT TO BE IMPROPER SELECTION OF THE AUTOCOARSEN SYSTEM SWITCH. (M) 2 L 7 2 4T RT A52EU 1996110700540 19961107 00540 NE 1996 11 7 96ZZZM1437 2 19960907 A 7250 BEARING SEAL BOEING 727 72723 1384004 NM PWA JT8 JT8D7B 52053 NE NR 2 ENGINE LOOSE A UHVA E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION CR CRUISE 1 SO 11 1993 45919 45919 18449 654897 AIRCRAFT DEPARTED MEXICO CITY, CANCUN, EN ROUTE NR 2 ENGINE OIL BYPASS LIGHT CAME ON AND ENGINE TEMPERATURE STARTED TO R ISE. NR 2 ENGINE SHUT DOWN, PROCEED TO CANCUN AND LANDED COMPLETE. INVESTIGATION REVEALED OIL SEAL LOOSE IN THE NR 6 B EARING SCAVANGE PUMP HOUSING. RESECURED NR 6 BEARING SEAL, ALL FILTERS REPLACED. CONDUCTED POWER RUN NR 2 ENGINE, NO L EAKS NOTED. (M) 2 L 7 3 4F 4 F A3WE E2EA 1996110700541 19961107 00541 NM 1996 11 7 EISA96195 1 19961011 A 3230 GEAR PINS BOEING 727 727232 1384082 NM LANDING GEAR NOT REMOVED A EISA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 68782 20637 GEAR WOULD NOT RETRACT AFTER TAKEOFF. FOUND GEAR PINS INSTALLED. REMOVED AND STOWED PINS. (M) 2 L 7 3 4F A3WE 1996110700542 19961107 00542 WP 1996 11 7 ASAA9680221 1 19961008 A 3350 014597101 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 8 53016 SEA - FLT 304 - FORWARD SECTION OF EMERGENCY EXIT FLOOR TRACK LIGHTS INOPERATIVE. REPLACED BATTERIES IN SECOND PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996110700543 19961107 00543 WP 1996 11 7 ASAA9680220 1 19961007 A 3350 6030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 946AS 49658 PDX - L-1 AND R-1 DOOR OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996110700544 19961107 00544 NM 1996 11 7 ASAA9640089 1 19961008 A 3397 WIRE BOEING 737 7374S3 1384711 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 786AS 24795 SEA - DURING MAINTENACNE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 15 THROUGH 17 . RECONNECTED WIRING AT ROW 17 AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996110700545 19961107 00545 WP 1996 11 7 ASAA9680239 1 19961021 A 2170 1808492 COALESCERS DOUG DC9 DC983 3022083 WP CABIN INOP A ASAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 01 942AS 53052 PDX - EN ROUTE LAX-PDX - FLT 620 - FLIGHT ATTENDANTS REPORTED HEADACHES, EUPHORIA AND DISORIENTATION DURING CRUISE AT FL 330 AND CABIN ALTITUDE OF 6000 FEET. DESCENDED TO LOWER ALTITUDE, SYMPTONS WERE LESS NOTICEABLE BUT STILL EXISTING. O DOR NOTED SIMILAR TO PLANT NEAR OR IN LEFT AFT LAVATORY. FLIGHT CREW DID NOT EXPERIENCE ANYTHING OUT OF THE ORDINARY WI TH REGARD TO AIR QUALTITY OR ODOR. ACCOMPLISHED AIR QUALITY CHECK PER WS 28525013. REPLACED WATER SEPARATOR COALESCERS AND CLEANED APU INLET AND PANEL AREAS. OPERATED AIR CONDITIONING SYSTEM, NO ODOR OR DEFECT NOTED. (M) 2 L 7 2 4F RT A6WE 1996110700546 19961107 00546 WP 1996 11 7 USAAD96142 1 19961009 A 2133 39245431 REGULATOR VLV DOUG DC9 DC982 3022082 WP LEFT FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 824US 49143 FLT 693 - CLT-PHL - DURING CLIMB FLOW LIGHT ILLUMINATED. LEFT AIRCRAFT SUPPLY PRESSURE 0 PSI. RIGHT SUPPLY 30 PSI. OU TFLOW VALVE MANUALLY CLOSED DID NOT HELP. ON DESCENT LEFT PRESSURE INCREASED. CABIN WAS NEVER ABOVE 8000 FEET. MASKS DID NOT DEPLOY. FLIGHT RETURNED TO CLT FOR MAINTENANCE. MAINTENANCE REPLACED LEFT PILOT PRESSURE REGULATOR VALVE. OPS AND LEAK CHECKS GOOD. (M) 2 L 7 2 4F A6WE 1996110700547 19961107 00547 WP 1996 11 7 USAAD96143 1 19961005 A 3350 6011777LB POWER SUPPLY DOUG DC9 DC931 3022065 WP RT NACELLE FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 927VJ 48154 RIGHT SIDE NACELLE EMERGENCY LIGHT INOP. MAINTENANCE REPLACED POWER PACK. (M) 2 L 7 2 4F A6WE 1996110700548 19961107 00548 NM 1996 11 7 USAA960669 1 19961014 A 5330 SKIN BOEING 737 737201 1384454 NM BS 328 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 252AU 37883 22758 ROA - DURING CX-3 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 1.24 INCH CRACK FORWARD GALLEY DOOR CUT OUT AFT LOWER CORN ER FUSELAGE SKIN STRINGER 17 R, BS 328. REMOVED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 26. (M) 2 L 7 2 4F A16WE 1996110700549 19961107 00549 NM 1996 11 7 USAA960670 1 19961014 A 5330 SKIN BOEING 737 737201 1384454 NM BS 950 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 252AU 22758 ROA - DURING CX-3 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 1.25 INCH CRACK AFT ENTRY DOOR CUT OUT FORWARD LOWER CORNE R FUSELAGE SKIN STRINGER 17L, BL 950. REMOVED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 24. (M) 2 L 7 2 4F A16WE 1996110700550 19961107 00550 NM 1996 11 7 USAASB96119 1 19960628 A 2420 6130200502 HARNESS BOEING 737 737301 1384611 NM NR 2 ENGINE FAILED A A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 558AU 23512 CLT - FLT 337 - WHILE PASSING 18,000 FEET, FLIGHT LOST 2 OF 3 TRANSFORMER RECTIFIERS. FLIGHT RETURNED TO FIELD IN CLT A ND LOST NR 2 MAIN BUS ON 2 NAUTICAL MILE FINAL. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 ENGINE A/C HARNESS. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996110700551 19961107 00551 NM 1996 11 7 USAASB96210 1 19961001 A 3350 20121 POWER SUPPLY BOEING 737 7373B7 1384580 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 384US 22957 CLT - MAINTENANCE FOUND THE LEFT AFT ENTRY DOOR EXTERIOR EMERGENCY ESCAPE SLIDE LIGHT INOP. MAINTENANCE REMOVED AND REP LACED THE POWER SUPPLY IN THE AFT OVERHEAD CABIN. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996110700552 19961107 00552 NM 1996 11 7 USAA960666 1 19961007 A 3350 SKIN BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 36460 22888 ROA - DURING CX-6 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND .25 INCH CRACK FORWARD ENTRY DOOR CUT OUT AFT LOWER CO RNER FUSELAGE SKIN, BONDED DOUBLER AND BEAR STRAP. INSTALLED STRAPS, REPAIRED PER EA 41616 INTERIM REPAIR. (M) 2 L 7 2 4F A16WE 1996110700553 19961107 00553 NM 1996 11 7 TWRA96331 1 19961006 A 3350 363673 LIGHT BOEING 747 747282B 1384860 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 610FF 20501 DURING DAILY CHECK, FOUND UPPER DECK EVAC FLOOR STRIP INOP. REPLACED EMERGENCY LIGHT STRIP IN UPPER DECK. OPS CHECKED OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996110700554 19961107 00554 NM 1996 11 7 TWRA96326 1 19961003 A 3350 S1356B37 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 620FF 11375D 21162 DURING DAILY CHECK, FOUND CEILING MOUNTED EMERGENCY EXIT LIGHT INOP AT L1 DOOR. REMOVED AND REPLACED LIGHT ASSEMBLY AT L1 DOOR. OPS CHECKED NORMAL PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996110700555 19961107 00555 NM 1996 11 7 TWRA96325 1 19961002 A 3350 08163000603 LIGHT BOEING 747 747212B 1384886 NM CABIN MALFUNCTION A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 616FF 21939 DURING DAILY CHECK, FOUND UPPER DECK EGRESS LIGHT STRIP NEED TO BE REPLACED BY GALLEY. REMOVED AND REPLACED UPPER DECK EGRESS LIGHT STRIP PER MM 33-51-00. OPS CHECKED GOOD. (M) 2 L 7 4 4F A20WE 1996110700556 19961107 00556 NM 1996 11 7 TWRA96329 1 19961003 A 3350 S1356B37 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 620FF 21162 DURING DAILY CHECK, FOUND CEILING EMERGENCY EXIT LIGHT INOP AT L1 DOOR. REMOVED AND REPLACED LIGHT ASSEMBLY AT L1 DOOR. OPS CHECKED OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996110700557 19961107 00557 NM 1996 11 7 TWRA96330 1 19961004 A 3350 276001 FUSE BOEING 747 747212B 1384886 NM CABIN BLOWN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 619FF 21316 DURING DAILY CHECK, FUODN L-1 MED OVERHEAD CEILING EVAC LIGHT INOP. REPLACED FUSELAGE, OPS CHECKED NORMAL PER MM 33-51- 00. (M) 2 L 7 4 4F A20WE 1996110700558 19961107 00558 NM 1996 11 7 TWRA96323 1 19960930 A 3350 3004083 LIGHT BOEING 747 747282B 1384860 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 611FF 20502 DURING DAILY CHECK, FOUND RIGHT SIDE OVERWING TO FUSELAGE NR 3 EVAC LIGHT ASSEMBLY. AFT BULB INOP. REMOVED AND REPLACE D LIGHT ASSEMBLY. OPS CHECKED NORMAL PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996110700559 19961107 00559 NM 1996 11 7 TWRA96317 1 19960908 A 3350 276005 FUSE BOEING 747 747212B 1384886 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 6186 21439 DURING DAILY CHECKED, FOUND 'B' AND 'D' ZONE FLOOR EVAC LIGHT INOP. REPLACED FUSELAGE ON BATTERY CHARGER. OPS CHECKED OK PER MM 33-55-00. (M) 2 L 7 4 4F A20WE 1996110700560 19961107 00560 NM 1996 11 7 TWRA96234 1 19960924 A 3397 591215 WIRE BOEING 747 747136 1384883 NM CABIN BROKEN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 606FF 20273 DURING DAILY CHECK, FOUND UPPER DECK FLOOR EVAC STRIP LIGHT IS INOP. FOUND BROKEN WIRE, REPLACED WIRE, OPS CHECKED OK P ER MM 33-59-00 PG 501. (M) 2 L 7 4 4F A20WE 1996110700561 19961107 00561 NM 1996 11 7 TWRA96316 1 19960916 A 3350 S1356B37 LIGHT BOEING 747 747259B NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 EICEO 17118 21730 DURING DAILY CHECK, FOUND 36A CEILING EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED EMERGENCY CEILING LIGHT, AS PER MM 33-51-00. OPS CHECKED NORMAL. (M) 2 L 7 4 4F RT A20WE 1996110700562 19961107 00562 NM 1996 11 7 TWRA96320 1 19960919 A 3350 S1356B37 BATTERY PACK BOEING 747 747259B NM CABIN DISCHARGED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 EICEO 21730 DURING DAILY CHECK, FOUND CEILING LIGHT (EVAC) ABOVE SEAT ROW 60 HJK INOP. REMOVED AND REPLACED BATTERY PACK ASSEMBLY. OPS CHECKED NORMAL PER MM 33-51-00. (M) 2 L 7 4 4F RT A20WE 1996110700563 19961107 00563 NM 1996 11 7 TWRA96321 1 19960924 A 3350 086861 SOCKET BOEING 747 747238B 1384828 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 607PE 20011 DURING DAILY CHECK, FOUND EMERGENCY LIGHT OUT BY SEAT 43C AND 64H. REMOVED AND REPLACED SOCKET SYSTEMS CHECKED NORMAL P ER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996110700564 19961107 00564 NM 1996 11 7 TWRA96319 1 19960919 A 3350 70031243 LIGHT BOEING 747 747259B NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 EICEO 2045 21730 DURING DAILY CHECK, FOUND EXIT SIGN (EVAC) ABOVE SEAT ROW 45HJK INOP. REMOVED AND REPLACED LIGHT. OPS CHECKED OK, PER MM 33-51-00. (M) 2 L 7 4 4F RT A20WE 1996110700565 19961107 00565 NM 1996 11 7 TWRA96333 1 19961015 A 3397 WIRE BOEING 747 747130 1384880 NM CABIN BROKEN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 603FF 19746 EVAC LIGHT OUT NEXT TO SEATS 51C AND 50C. FOUND BROKEN WIRE. RESPLICED, OPS CHECK OK PER 33-51-00. (M) 2 L 7 4 4F A20WE 1996110700566 19961107 00566 NM 1996 11 7 TWRA96332 1 19961011 A 3350 6103991 BATTERY BOEING 747 747282B 1384860 NM CABIN DISCHARGED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 610FF 20501 EVAC SYSTEM OVERWING LEFT SIDE. LAST TWO LIGHT ASSEMBLYS HAVE BOTH LIGHTS OUT. REPLACED BATTERY PACK. OPS CHECK OK PE R MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996110700567 19961107 00567 NM 1996 11 7 TWRA96334 1 19961013 A 3397 WIRE BOEING 747 747282B 1384860 NM CABIN LOOSE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 610FF 20501 EVAC LIGHT STRIP OUT FROM 36 ABC TO 44 ABC AND IN FRONT OF 'L' LAV. CLEANED CONNECTIONS AND SECURED LOOSE WIRE. (M) 2 L 7 4 4F A20WE 1996110700568 19961107 00568 NM 1996 11 7 TWRA96335 1 19961016 A 3350 3004181A LIGHT BOEING 747 747282B 1384860 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 610FF 20501 NR 1 LEFT AND NR 4 LEFT MED UPPER BUSTLE EMERGENCY EVAC LIGHTS INOP REPLACE FAULTY BUSTLE LIGHTS. OPS CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996110700569 19961107 00569 NM 1996 11 7 TWRA96336 1 19961016 A 3350 90083 BATTERY BOEING 747 747282B 1384860 NM CABIN DISCHARGED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 610FF 006 20501 MAIN CABIN CROSSOVER EXIT, EMERGENCY EVAC LIGHT INOP. IN C-ZONE, FORWARD RIGHT SIDE. REPLACED LIGHT ASSEMBLY BATTERY P ACK. OPS CHECK NORMAL PER 33-51-00. (M) 2 L 7 4 4F A20WE 1996110700570 19961107 00570 EU 1996 11 7 SIMA962901 1 19961016 A 3397 WIRE AEROSP ATR42 ATR42300 8680920 EU CABIN BROKEN A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 427MQ 091 ORD - FLT 4309 - EMERGENCY EXIT STAIR LIGHT INOP. REPAIRED BROKEN WIRE ON CANNON PLUG ON PASSENGER DOOR. OPS CHECK GOO D. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996110700571 19961107 00571 EU 1996 11 7 SIMA962871 1 19961013 A 3350 3011151 POWER SUPPLY AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 427MQ 4031 091 ORD - FLT 4045 - THREE FLOOR EMERGENCY LIGHTS INOP AND BOTH FORWARD CABIN EMERGENCY EXITS BOTTOM LIGHTS INOP. RAI'D BAT TERY PACK IN POWER SUPPLY 34WL. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996110700572 19961107 00572 EU 1996 11 7 SIMA962881 1 19961014 A 3350 3011151 BATTERY AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 251AE 250 ORD - FLT 4100 - FORWARD EMERGENCY EXIT LIGHTS INOP. RAI'D BATTERY IN POWER PACK 3WL. OPS CHECK GOOD. AIRCRAFT WAS RE TURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996110700573 19961107 00573 EU 1996 11 7 SIMA962851 1 19961011 A 2910 MS219126 T-FITTING AEROSP ATR42 ATR42300 8680920 EU GREEN HYD SYSTEM FAILED A SIMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 12MQ 012 ORD - FLT 4211 - GREEN SYSTEM HYD LOW LEVEL WARNING CAME ON AFTER TAKEOFF. AIRCRAFT RETURNED TO ORD AND DECLARED EMERGE NCY AND LANDED SAFELY. MAINTENANCE FOUND THE HYD T-FITTING HAD FAILED. REPLACED T-FITTING AND SERVICED HYDRAYULIC SYST EM. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996110700574 19961107 00574 WP 1996 11 7 ORJA9661 1 19961001 A 3350 6011779 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 824RA 53017 OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED OVERWING POWER SUPPLY. OPS CHECKED GOOD. (M) 2 L 7 2 4F A6WE 1996110700575 19961107 00575 WP 1996 11 7 ORJA9663 1 19961005 A 3350 60330431 BATTERY PACK GRIMES DOUG DC9 DC983 3022083 WP DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 836RA 53046 AFT EMERGENCY BATTERY PACK POWER SUPPLY INOP. REMOVED AND REPLACED AFT EMERGENCY BATTERY PACK POWER SUPPLY. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1996110700576 19961107 00576 EU 1996 11 7 M3HA96028 1 19961008 A 3350 3011151 BATTERY AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A M3HA K NONE L NO TEST IN INSP/MAINT 1 WP 13 4202G 2263 050 HNL - AFT EMERGENCY EXIT LIGHT NEAR ENTRANCE DOOR WILL NOT ILLUMINATE. REMOVED AND INSTALLED SERVICEABLE BATT PACK, OPS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1996110700577 19961107 00577 EU 1996 11 7 M3HA96029 1 19961009 A 3350 3011151 BATTERY AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A M3HA K NONE L NO TEST IN INSP/MAINT 1 WP 13 4204G 10466 061 HNL - DURING DAILY AIRCRAFT INSPECTION, FORWARD EMERGENCY LIGHTS OVERHEAD FOUND TO BE INOP. REMOVED AND INSTALLED SERVI CEABLE BATT PACK, OPS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1996110700578 19961107 00578 SW 1996 11 7 MALA965149 1 19960927 A 5320 FRAME SWRNGN SA227 SA227AC 8780603 SW CARGO DOOR CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 436MA AC719B DURING MAINTENANCE IN MSP, FOUND AFT CARGO DOOR FUSELAGE FRAME GAS STRUT MOUNT POST HOLE CRACKED. CRACK WAS REPAIRED IA W FAC ARP 53-20-9503 DATED MARCH 1, 1995. DAMAGE LOCATED AT FS 438 FRAME P/N 27-20085. (M) 2 L 7 2 4T RT A8SW 1996110700579 19961107 00579 NE 1996 11 7 MALA965150 2 19960924 A 7260 1933T39 SEAL SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LEFT ENGINE FAILED A MALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 15 98XJ 340A098 FLT 2907 - AFTER DEPARTURE FROM DTW, THE LEFT OIL PRESSURE GAUGE INDICATED IN THE YELLOW ARC. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE LEFT STARTER/GENERATOR AXIS BB SEAL KIT. ALL CHECKS SATISFACTORY. (M) 2 L 7 2 4T 4 T RT A52EU E8NE6 1996110700580 19961107 00580 EU 1996 11 7 USAA960686 1 19961018 A 5320 WINDOW POST FOKKER F28 F28MK4000 4990810 EU LT COCKPIT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 494US 30043 11167 PIT - DURING UNSCHEDULED MAINTENANCE, FOUND .75 INCH CRACK AT LEFT NR 3 WINDOW POST. DETECTED BY EDDY CURRENT INSPECTIO N, AND SIP REF NR 53-10-18 PG 1, PCI 1488. CUT OUT AFT HROIZONTAL FLANGE. INSTALLED A FILLER AND A BATH TUB REPAIR FIT TING PER EA NR 33552. (M) 2 L 7 2 4F RT A20EU 1996110700581 19961107 00581 EU 1996 11 7 USAA960690 1 19961022 A 5312 BULKHEAD ANGLE FOKKER F28 F28MK4000 4990810 EU FWD PRESS BLKHD CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 483US 59849 11233 PIT - DURING SIP AND B-CHECK, FOUND 4 INCH CRACK IN FRONT PRESSURE BULKHEAD LOWER CONNECTION ANGLE AFT SIDE FRAME 1550 B ETWEEN STRINGER 3 AND 72. DETECTED BY VISUAL/EDDY CURRENT. STOP DRILLED CRACK ENDS AND INSTALLED TWO EXTERNAL DOUBLERS PER SRM 53-02-18 FIG 11. (M) 2 L 7 2 4F RT A20EU 1996110700582 19961107 00582 NM 1996 11 7 USAA960681 1 19961015 A 5315 146N50892 FLOOR BEAM BOEING 757 757225 1384959 NM BS 1640 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 36514 22192 CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND SEVERAL CORRODED AREAS 1 INCH BY 1 INCH STATION 1640 FLOOR BEAM. NEW CH ORD SECTIONS INSTALLED, REPAIRED PER EA 58911 SRM 53-00-51 FIG 201 AND 203. (M) 2 L 7 2 4F RT A2NM 1996110700583 19961107 00583 NM 1996 11 7 USAA960682 1 19961015 A 5315 146N509012 FLOOR BEAM BOEING 757 757225 1384959 NM BS 1664 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 22192 CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORRODED AREAS STATION 1664 FLOOR BEAM. REPLACED UPPER CHORD SECTION, REPAIRED PER SRM 53-00-51, AND SRM 53-00-01. (M) 2 L 7 2 4F RT A2NM 1996110700584 19961107 00584 NM 1996 11 7 USAA960619 1 19960918 A 5320 WEB BOEING 737 7372B7 1384560 NM BS 707 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 282AU 35514 23115 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND FOUR .5 INCH CRACKED WEBS BL 0 BS 707. INSTALLED WEB REPAIR AND FILLERS . REPAIRED PER SRM 51-40-2. (M) 2 L 7 2 4F A16WE 1996110700585 19961107 00585 NM 1996 11 7 USAA960620 1 19960918 A 5320 WEB BOEING 737 7372B7 1384560 NM BS 707 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 282AU 35514 23115 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND THREE .25 INCH CRACKED WEBS LBL 24.5 BS 707. INSTALLED DOUBLER, REPAIRE D PER SRM 51-40-2 FIG 1. (M) 2 L 7 2 4F A16WE 1996110700586 19961107 00586 NM 1996 11 7 USAA960621 1 19960918 A 5320 WEB BOEING 737 7372B7 1384560 NM BS 707 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 282AU 35514 23115 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND TWO .5 INCH CRACKED WEBS RBL 24.5 BS 707. INSTALLED DOUBLER, REPAIRED P ER SRM 51-40-2, FIG 1. (M) 2 L 7 2 4F A16WE 1996110700587 19961107 00587 NM 1996 11 7 USAA960622 1 19960918 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 360 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 282AU 35514 23115 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 2 INCH BY 20 INCH AREA OF HEAVY SURFACE CORROSION FLOOR BE AM STATION 360, RBL 12 TO RBL 56. INSTALLED REPAIR ANGLES, REPAIRED PER TR 53-10-05 C. CORROSION TASK NR C53-107-01, C ORROSION LEVEL 1. (M) 2 L 7 2 4F A16WE 1996110700588 19961107 00588 NM 1996 11 7 USAA960918 1 19960918 A 5320 BEAM BOEING 737 7372B7 1384560 NM BS 674 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 282AU 35514 23115 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACKED BEAM RBL 24.5 BS 674. INSTALLED STIFFENER AND NEW CHANNE L, REPAIRED PER EO 5791G632. (M) 2 L 7 2 4F A16WE 1996110700589 19961107 00589 NM 1996 11 7 USAA960617 1 19960918 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 328 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 282AU 35514 23115 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 2 INCH AND 1.5 INCH BY 6 INCH CORRODED AREAS FLOOR BEAM BS 328 LBL 10 AND LBL 24-30. REPAIR ANGLES AND T-CAP. REPAIRED PER TR 53-10-13. CORROSION TASK NR C53-107-01, CORROSION LEV EL 1. (M) 2 L 7 2 4F A16WE 1996110700590 19961107 00590 NM 1996 11 7 USAA960616 1 19960918 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 986 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 282AU 35514 23115 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORRODED AREA 1 INCH BY 68 INCH FLOOR BEAM BS 986 LBL 18 INCH TO RBL 50 INCH. INSTALLED T-CAP REPAIR AND REPAIRED PER TR 53-10-05C. CORROSION TASK NR C53-107-02, CORROSION LEVEL 1. (M) 2 L 7 2 4F A16WE 1996110700591 19961107 00591 NM 1996 11 7 USAA960615 1 19960918 A 5320 DOOR FRAME BOEING 737 7372B7 1384560 NM BS 317 CORRSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 282AU 35514 23115 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND .25 INCH BY 1 INCH CORROSION DOOR FRAME LONGERONO STATINO 317 STRINGER 2 7R. REMOVED CORROSION AND INSTALLED STRAP DOUBLER PER EA 41489. CORROSION TASK NR C53-107-02, CORROSION LEVEL 1. (M) 2 L 7 2 4F A16WE 1996110700592 19961107 00592 NM 1996 11 7 USAA960614 1 19960918 A 5315 FLOOR BEAM BOEING 737 7372B7 1384560 NM BS 947 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 282AU 35514 23115 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 55 INCH CORRODED AREA FLOOR BEAM BS 947 BL 30 INCH - RBL 25 IN CH. INSTALLED T-CAP REPAIR, REPAIRED TR 53-10-05 C AND SPM. CORROSION TASK NR C53-107-02, CORROSION LEVLE 1. (M) 2 L 7 2 4F A16WE 1996110700593 19961107 00593 NM 1996 11 7 USAA960613 1 19960918 A 5320 BEAM BOEING 737 7372B7 1384560 NM BS 674 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 282AU 35514 23115 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACKED BEAM BS 674 LBL 24.5. INSTALLED STIFFENER AND NEW CHANNE L. REPAIRED PER EO 5791G632. (M) 2 L 7 2 4F A16WE 1996110700594 19961107 00594 WP 1996 11 7 USAAD96145 1 19960927 A 3350 AD20131A BATTERY PACK DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 827US 48049 TAIL COMPARTMENT EMERGENCY LIGHTS DIM. REPLACED BOTH BATTERY PACKS IN RIGHT AFT LAVATORY. (M) 2 L 7 2 4F A6WE 1996110700595 19961107 00595 WP 1996 11 7 USAAD96144 1 19961011 A 3230 39140165505 BUNGEE CYLINDER DOUG DC9 DC931 3022065 WP RT MLG FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 923VJ 48143 FLT 751 - MSP-CLT - AFTER GEAR RETRACTION, RIGHT MAIN UNSAFE LIGHT ILLUMINATED. CAPTAIN RECYCLED GEAR BUT NO HELP. THE N YELLOW GEAR DOOR UP LIGHT ILLUMINATED. OVER JOT CAPTAIN REPORTED 2300 LBS OVER BURN. DECIDED TO LAND AT IND FOR MX. NO EMERGENCY DECLARED. FLIGHT LANDED AT IND WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED RIGHT MAIN GEAR DOWNLOCK B UNGEE. (M) 2 L 7 2 4F A6WE 1996110700596 19961107 00596 NM 1996 11 7 USAASB96190 1 19960803 A 3350 900835A BATTERY PACK BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 286AU 23133 SYR - MAINTENANCE FOUND THE OVERHEAD EMERGENCY LIGHT INOP IN THE FORWARD CABIN. MAINTENANCE REPLACED THE BATTERY PACK A T THE FORWARD OVERHEAD CABIN. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1996110700597 19961107 00597 NM 1996 11 7 USAASB96191 1 19960903 A 3350 6104781 BATTERY PACK BOEING 737 7372B7 1384560 NM CARGO COMPT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 266AU 22878 CLT - MX FOUND THE EXTERIOR LEFT WING EMERGENCY EVACUATION LIGHTS INOP. MAINTENANCE REPLACED THE BATTERY PACK FOR THE L EFT WING EMERGENCY EVACUATION LIGHTS. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1996110700598 19961107 00598 NM 1996 11 7 USAASB96193 1 19960913 A 2130 CIRCUIT BREAKER BOEING 737 7373B7 1384580 NM PRESS SYSTEM TRIPPED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 532AU 24479 PIT - FLT 601 - FLT LOST AUTO AND STANDBY PRESSURIZATION WHILE CLIMBING THROUGH 9000 FEET. CREW MAINTAINED CABIN PRESSU RE IN MANUAL MODE. CAPTAIN ADVISED DISPATCH OF SITUATION AND AFTER CONFERRING WITH MX IT WAS DECIDED TO RETURN THE FLIG HT TO PIT. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE CIRCUIT BRE AKER FOR THE AUTO PRESSURIZATION SYSTEM POPPED. RESET SAME. SYSTEM OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 1996110700599 19961107 00599 NE 1996 11 7 USAAD96128 2 19960915 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE NR 2 FAILED A USAA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 EA 19 817US 48097 708116 FLT 984 - CLT-ORF - AFTER TAKEOFF, THE NR 2 OIL FILTER CLOGGING LIGHT ILLUMINATED. AT IDLE POWER, THE LIGHT REMAINED IL LUMINATED, ACCOMPANIED BY RISING OIL TEMPERATURE AND REDUCED FUEL FLOW. SHUT DOWN NR 2 ENGINE, AND RETURNED TO FIELD. 1 9 MINUTES SINGLE ENGINE TIME. REPLACED NR 2 ENGINE. (M) 2 L 7 2 4F 4 F A6WE E9NE 1996110700600 19961107 00600 WP 1996 11 7 USAAD96127 1 19960910 A 3260 UPLOCK SWITCH DOUG DC9 DC931 3022065 WP LT MLG FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 945VJ 47066 FLT 1203 - PIT-MSP - AFTER DEPARTURE, GOT A LEFT GEAR UNSAFE LIGHT. RETURNED TO PIT. REPLACED LEFT MAIN LANDING GEAR U PLOCK SWITCH. (M) 2 L 7 2 4F A6WE 1996110700601 19961107 00601 NM 1996 11 7 USAABB96029 1 19960910 A 2910 AS11608K0195 HYD LINE BOEING 757 757225 1384959 NM LT MLG WW FAILED A USAA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CL CLIMB 1 EA 19 604AU 22199 LAX - FLT 18 - DURING GEAR RETRACTION ON CLIMB, CREW RECEIVED INDICATION OF LOSS OF HYDRAULIC FLUID/PRESSURE FROM THE LE FT SYSTEM. FLIGHT RETURNED TO FIELD TO LAX AND WAS TOWED TO GATE DUE TO LOSS OF NOSE STEERING. MAINTENANCE REPLACED TH E PRESSURE LINE TO THE LEFT GEAR RETRACT CYCLINDER. (M) 2 L 7 2 4F RT A2NM 1996110700602 19961107 00602 NM 1996 11 7 USAABB96030 1 19960915 A 3260 836003 PSEU BOEING 757 757225 1384959 NM E/E COMPT FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 608AU 7289 22204 MCO - FLT 244 - AFTER TAKEOFF AND DURING GEAR RETRACTION, GREEN INDICATION LIGHTS EXTINGUISHED, DOOR LIGHT REMAINED ON, AND CREW RECEIVED EICAS MESSAGE 'GEAR DISAGREE'. CREW CYCLED THE GEAR. NO CHANGE IN THE SITUATION WAS APPARENT. FLIGHT RETURNED TO MCO AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND TWO FAILED CARDS IN THE PSEU AND REPLACED THE U NIT. (M) 2 L 7 2 4F RT A2NM 1996110700603 19961107 00603 NM 1996 11 7 USAA960667 1 19961011 A 5315 FLOOR BEAM BOEING 737 7374B7 1384702 NM BS 947.5 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 19672 24557 CLT - INSPECTION VISUALLY FOUND LEVEL 2 CORROSION MEASURING 11 INCHES TOTAL AREA AT FLOOR BEAM T-CAP, STATION 947.5 - LB L 9 TO RBL 33. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. CORRODED SECTION REMOVED. REPAIRED ANGLES INSTALLED A S PER USAIR EA NR 58803. (M) 2 L 7 2 4F RT A16WE 1996110700604 19961107 00604 NM 1996 11 7 USAA960668 1 19961011 A 5347 SEAT TRACK BOEING 737 7374B7 1384702 NM BS 328-344 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT - INSPECTION VISUALLY FOUND LEVEL 2 CORROSION MEASURING 16 INCHES TOTAL AREA LOCATED RBL 24, STATINO NR 328-344, SEA T TRACK. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. CORRODED SECTION REMOVED, NEW SECTION INSTALLED AS PER BOEIN G SRM 53-00-52 AND USAIR TYPICAL REPAIR 1, PG 202-205. (M) 2 L 7 2 4F RT A16WE 1996110700605 19961107 00605 WP 1996 11 7 USAAD96146 1 19961016 A 2131 21171802 CONTROLLER DOUG DC9 DC982 3022082 WP NR 1 FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 830US 22632 49443 FLT 417 - PIT-MDT - CLIMBING THROUGH 17,000 FEET, CABIN ALTITUDE CONTROL WHEEL WENT FULL CLOSED AND STARTED TO CHATTER A ND VIBRATE. SELECTED STANDBY WITH NO CHANGE. WENT TO MANUAL AND REGAINED CONTROL OF CABIN PRESSURE. RETURNED TO PIT. FOUND NR 1 PRESSURIZATION CONTROLLER NOT OPERATING. REPLACED CONTROLLER. (M) 2 L 7 2 4F A6WE 1996110700606 19961107 00606 WP 1996 11 7 USAAD96147 1 19961016 A 2424 939D2171 VOLTAGE DOUG DC9 DC931 3022065 WP RIGHT FAILED A USAA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 EA 19 960VJ 6328 47505 FLT 8004 - CHS-SYR - DURING CLIMB-OUT, RIGHT GENERATOR FAILED. STARTED APU. AT FL 300, APU QUIT. DIVERTED TO CLT. FO UND VOLTAGE REGULATOR FAULT ON GENERATOR CONTROL PANEL. REPLACED RIGHT VOLTAGE REGULATOR. (M) 2 L 7 2 4F A6WE 1996110700607 19961107 00607 WP 1996 11 7 USAAD96149 1 19961017 A 3350 110049 BATT CHARGER DOUG DC9 DC931 3022065 WP CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 943VJ 47058 NR 2 SECTION OF FLOOR TRACK LIGHTING INOPERATIVE. REPLACED BATTERY CHARGER FOR EMERGENCY LIGHTS. (M) 2 L 7 2 4F A6WE 1996110700608 19961107 00608 WP 1996 11 7 USAAD96148 1 19961016 A 3350 14597101 BATTERIES DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 802US 48036 FLOOR TRACK LIGHTING ROWS 3-10 INOP. REPLACED BATTERIES IN FORWARD POWER PACK. (M) 2 L 7 2 4F A6WE 1996110700609 19961107 00609 WP 1996 11 7 USAAD96150 1 19961018 A 3350 P4010020 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 920VJ 48140 RIGHT SERVICE DOOR EMERGENCY BATTERY PACK INOPERATIVE. REPLACED BATTERY PACK. (M) 2 L 7 2 4F A6WE 1996110700610 19961107 00610 EU 1996 11 7 VTZA97029 1 19961017 A 7722 8974764 EGT COMPENSATOR BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILURE A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 488UE 907 FLT 6387 - IAD-STR - DURING CLIMB, MADE AN UNSCHEDULED LANDING DUE TO RIGHT ENGINE EGT WENT TO ZERO. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED EGT COMPENSATOR. OPS CHECK OK. AIRCRAFT WAS RELEAS ED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996110700611 19961107 00611 EU 1996 11 7 VTZA97028 1 19961016 A 3233 6158E ACTUATOR BAG JETSTM JETSTM3201 1500217 EU NLG FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 485UE 901 FLT 6194 - IAD-EWR - DURING CLIMB, MADE AN UNSCHEDULED LANDING DUE TO ALL 3 GEAR INTRANSIT LIGHTS REMAINED ILLUMINATED A FTER GEAR SELECTED UP. AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED NLG RE TRACTION JACK. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996110700612 19961107 00612 EU 1996 11 7 VTZA97026 1 19961016 A 2750 51484YMJK83NP SELECTOR BAG JETSTM JETSTM3201 1500217 EU FLAP SYSTEM FAILED A VTZA K NONE J WARNING INDICATION AP APPROACH 1 EA 27 480UE 894 FLT NR 6269 - BUF-IAD - DURING APPROACH, MADE AN UNSCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS FLAPS WOULD NOT GO T O 35 DEGREES SETTING. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED FLAP SELECTOR, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996110700613 19961107 00613 EU 1996 11 7 VTZA97025 1 19961017 A 3260 AIR135022 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU RT MLG FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 312UE 41025 FLT 6499 - IAD-ROA - DURING CLIMB, AN UNSCHEDULED LANDING DUE TO RED GEAR HANDLE LIGHT REMAINED ILLUMINATED WITH GEAR SE LECTED UP. AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED MICROSWITCH, OPS C HECK OK. AIRCRAFT WAS THEN RELEASED AND APPROVED FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1996110700614 19961107 00614 NM 1996 11 7 TAOA109605 1 19961009 A 3350 OL3071BPEGPL LAMP GRIMES BOEING 727 727254 138408L NM CABIN INOPERATIVE A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 915TS 20252 ESCAPE PATH LIGHTING AT ROW 18 ONE LIGHT INOPERATIVE. RELAMPED, OPERATIONAL CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1996110700615 19961107 00615 NM 1996 11 7 TAOA109606 1 19961010 A 5210 766001 SWITCH BOEING 727 727225 1384077 NM L-1 DOOR INOPERATIVE A TAOA O OTHER N FALSE WARNING IN INSP/MAINT 1 EA 15 919TS 20447 FORWARD ENTRY DOOR INDICATES OPEN ON SECOND OFFICERS PANEL. DOOR HANDLE IN CABIN INDICATED CLOSED. VISUALLY CHECKED DO OR, FOUND DOOR SWITCH INOPERATIVE. REMOVED AND REPLACED L-1 DOOR ANNUNCIATOR LIGHT CONTROL SWITCH. OPERATIONAL CHECK N ORMAL IAW MM CHAPTER 52. (M) 2 L 7 3 4F A3WE 1996110700616 19961107 00616 NM 1996 11 7 TAOA109610 1 19961019 A 3350 256005 FUSE BOEING 727 727254 138408L NM CABIN BLOWN A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 915TS 20252 ESCAPE PATH LIGHTING INOPERATIVE FORWARD OF ROW 7. REPLACED BLOWN FUSE IN BATTERY PACK. SYSTEM OPERATION CHECKS NORMAL . (M) 2 L 7 3 4F A3WE 1996110700617 19961107 00617 EU 1996 11 7 SIMA962971 1 19961023 A 2710 14430 INTERCONNECT AEROSP ATR42 ATR42300 8680920 EU TE FLAPS CRACKED A A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 265AE 237 266 DFW - DURIGN COMPLIANCE OF EO E9-2700-001 (AD 93-22-10) REPETITIVE INSPECTION OF AILERON CONTROL SYSTEM. THE FLAP INTER CONNECT ROD APPEARED TO HAVE SEVERAL CRACKS JUST INBOARD OF BEARING SLEEVES. THE INTERCONNECT ROD WAS REPLACED AS A PRE CAUTIONARY STEP. FURTHER INSPECTION AND EVALUATION OF THE ROD WILL CONTINUE BY SIMMONS AND ATR. OPS CHECK SATISFACTORY AS PER GPM. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996110700618 19961107 00618 EU 1996 11 7 SIMA962951 1 19961021 A 3234 F96GA0102 HANDLE AEROSP ATR72 ATR72212 EU LANDING GEAR FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 451AT 666 451 LBB - FLT 3810 - AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO LBB AND LANDED SAFELY. AIRCRAFT RE LOCATED TO DFW PER MEL 32-3 AUTHORITY. MAINTENANCE REPLACED LANDING GEAR SELECTOR HANDLE. PERFORMED LANDING GEAR RETRA CTION/EXTENSION. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996110700619 19961107 00619 1996 11 7 SIMA962921 3 19961018 A 6140 4088T42P01 SENSOR NP SAAB SF340 340B 7860101 EU RT ENGINE FAILED A SIMA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 314AE SIMT1425 340B314 FSM - FLT 3948 - DURING CRUISE FLT, RIGHT ENGINE PROP RPM FLUCTUATED AND RIGHT TQ FLUCTUATED. CREW SHUT DOWN ENGINE AND DIVERTED TO FSM. RAI'D RIGHT ENGINE NP SENSOR. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1996110700620 19961107 00620 NM 1996 11 7 TWRA96340 1 19961017 A 3350 3004185 LIGHT BOEING 747 747282B 1384860 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 610FF 20501 R4 MED EMERGENCY BUSTLE LIGHT INOP. REPLACED EMERGENCY BUSTLE LIGHT ON R4 MED. OPS CHECK OK PER MM 33-51-00 PAGE 501. (M) 2 L 7 4 4F A20WE 1996110700621 19961107 00621 NM 1996 11 7 TWRA96339 1 19961017 A 3350 58801 LIGHT BOEING 747 747282B 1384860 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 610FF 20501 REAR GALLEY EMERGENCY FLOOR STRIP INOP. REPLACED REAR GALLEY FLOOR STRIP. OPS CHECK OK PER 33-51-01. (M) 2 L 7 4 4F A20WE 1996110700622 19961107 00622 NM 1996 11 7 NOCA0796 1 19960919 A 3350 013071 LIGHT BOEING 757 75723A 1384967 NM CABIN INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 757NA 24567 L1 RED LAMP ASSEMBLY INOP AT DOOR 1L. REPLACED LAMP ASSEMBLY, CHECKS OK. (M) 2 L 7 2 4F RT A2NM 1996110700623 19961107 00623 NM 1996 11 7 NOCA0896 1 19960919 A 3350 LIGHT BOEING 757 75723A 1384967 NM CABIN LOOSE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 757NA 24567 RED LIGHT ASSEMBLY E-PATH AT DOOR 1L REQUIRED TO BE RESECURED. SECURED LIGHT ASSEMBLY, CHECKS OK. (M) 2 L 7 2 4F RT A2NM 1996110700624 19961107 00624 CE 1996 11 7 96ZZZM1438 1 19961021 A 3260 IN4007 DIODE BEECH 1900 1900C 1154161 CE LANDING GEAR SHORTED A GUUA O OTHER N FALSE WARNING DE DESCENT 1 SO 19 199GA UB13 FLT 401 - MCO-TPA - GEAR WARNING HORN CAN NOT BE SILENCED WHEN POWER IS REDUCED. RESOLDERED BROKEN WIRE TO, AND REPLACE D, BLOCKING DIODE CR109. 2 L 7 2 4T RT A24CE 1996110700625 19961107 00625 CE 1996 11 7 96ZZZM1439 1 19961020 A 3260 1123640321 PC BOARD BEECH 1900 1900C 1154161 CE LANDING GEAR SHORTED A GUUA O OTHER N FALSE WARNING DE DESCENT 1 SO 19 199GA UB13 FLT 153A - PBI-MIA - GEAR WARNING HORN CANNOT BE SILENCED WHEN POWER IS PULLED BACK FOR DESCENT. REPLACED E175 PC BOARD . GEAR SWING AND OPS CHECK GOOD. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A24CE 1996110700626 19961107 00626 EU 1996 11 7 96ZZZM1440 1 19961021 A 3240 BRAKE SYSTEM STBROS SD3 SD360 8100606 EU MLG REQ'D SERVICE A GUUA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 19 263GA SH3754 FLT 3197 - TPA-TLH - ON TAXI OUT LOST BRAKING AND POWER STEERING, RETURNED TO GATE. INSPECTED SYSTEM DETERMINED IN NEED OF SERVICING. SERVICED SYSTEM, NO DEFECTS NOTED. OPS CHECK ON BOTH SYSTEMS SATISFACTORY ON TAXI AND HIGH SPEED TAXI O PERATIONAL CHECKS. (M) 2 H 7 2 4T A41EU 1996110700627 19961107 00627 WP 1996 11 7 96ZZZM1441 1 19961021 A 3260 H654 SWITCH DOUG DC8 DC8F54 3021926 WP RT MLG DOOR ROLLER MISSING A FXLA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 19 426FB 7617 45667 AFTER TAKEOFF MIA, RIGHT MAIN GEAR LIGHT UNSAFE LIGHT ON AFTER GEAR RETRACTION. FOLLOWED ABNORMAL PROCEDURES AND LIGHT STAYED ON. RETURNED TO MIA AND MADE LANDING WITHOUT INCIDENT. FOUND RIGHT DOOR LATCH SWITCH ROLLER MISSING. REPLACED SWITCH CHECKS OK PER MM 32-7-0, TR 32-146. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 4 4F 4A25 1996110700628 19961107 00628 WP 1996 11 7 96ZZZM1442 1 19961018 A 2197 R263 WIRE DOUG DC8 DC861 3021952 WP COCKPIT LOOSE A FXLA O OTHER N FALSE WARNING CR CRUISE 1 SO 19 27UA 45942 CABIN ALTITUDE WARNING HORN 'ON' DURING CRUISE FLIGHT. CABIN ALTITUDE ABOVE 10,000 FEET AT FL 310 AND MANIFOLD AIR PRES SURE LIGHT 'ON'. ABNORMAL CHECKLIST COMPLETED, CONDITION CONTINUED. FOUND R263 WIRE LOOSE TO GND. TIGHTENED, CHECKED AT ENGINE RUN. PRESSURIZATION IN GROUND MODE, FLIGHT MODE ALL SYSTEMS OPS CHECK NORMAL IAW MM 21-30-0, 32-2-0 AND 36-1- 2. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 4 4F 4A25 1996110700629 19961107 00629 CE 1996 11 7 C2XA96CL034 1 19961016 A 3233 11438004111 ACTUATOR 114810000607 BEECH 1900 1900D 1154162 CE LT MLG BROKEN A C2XA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 09 16540 2279 0361A UE172 CLE - FLT 9363 - THE CREW REPORTED THAT DURING A TRAINING FLIGHT, THE LEFT MAIN LANDING GEAR WOULD NOT INDICATE A DOWN A ND LOCKED CONDITION. THE AIRCRAFT LANDED AT CLE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND FOUND THE LEFT MAIN LANDIG GEAR ACTUATOR ROD END BROKEN AND MINOR DAMAGE TO ADJACENT COMPONENTS. MAINTENANCE REMOVED AND REPLACE D THE LANDING GEAR ACTUATOR IAW B1900D MM 32-10-02, AND REPAIRED AND REPLACED ADJACENT COMPONENTS. AIRCRAFT RELEASED FO R SERVICE. (M) 2 L 7 2 4T RT A24CE 1996110700630 19961107 00630 NE 1996 11 7 C2XA96IA259 3 19961016 A 6114 7827015 HUB AEROSP ATR42 ATR42320 8680930 EU HAMSTD 14SF 14SF5 NE NR 1 ENGINE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 26826 14053 172 IAH - DURING A SCHEDULED MAINTENANCE CHECK, THE LEFT PROPELLER HUB NR 2 AND NR 3 BLADE BORE RETAINING RACES WERE FOUND T O BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RACES, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE (M) 2 H 7 2 4T RT A53EU 6 C P7NE 1996110700631 19961107 00631 EU 1996 11 7 C2XA96IA258 1 19961017 A 5347 S53678001202 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 25811 094 IAH - INSPECTION 3C-CHECK, DURNIG A ROUTINE INSPECTION OF THE CABIN FLOOR SEAT TRACKS, THE RIGHT INBOARD TRACK WAS FOUND TO BE CORRODED BEYOND LIMITS AT THE AFT END. MAINTENANCE REMOVED DAMAGED PORTION OF TRACK, FABRICATED AND INSTALLED A REPAIR SPLICE. THE AIRCRAFT WAS LATER APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996110700632 19961107 00632 EU 1996 11 7 C2XA96IA257 1 19961017 A 5313 S53671300216 STRINGER AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 25811 094 IAH - INSPECTION 3C-CHECK, DURING ROUTINE INSPECTION, FUSELAGE STRINGER NR 15 RIGHT WAS FOUND TO BE CORRODED BETWEEN FRA MES NR 35-38. MAINTENANCE REMOVED DAMAGED PORTION OF STRINGER AND FABRICATED AND INSTALLED A REPLACEMENT STRINGER SECTI ON. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996110700633 19961107 00633 EU 1996 11 7 C2XA96IA256 1 19961017 A 5230 S5237611420501 BRACKET AEROSP ATR42 ATR42320 8680930 EU CARGO DOOR CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 25811 094 IAH - DURING 3C-CHECK INSPECTION, THE FORWARD CARGO DOOR WAS FOUND TO HAVE TWO CRACKS AT THE ACTUATOR ATTACHMENT FITTING . MAINTENANCE REMOVED AND REPLACED THE FITTING AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996110700634 19961107 00634 SO 1996 11 7 ASOA96045 1 19961006 A 2910 12035196001 HYD LINE EMB 120 EMB120RT SO LT ENG RUPTURED A ASOA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 11 237AS 120051 WHILE COMPLETING THE TAKEOFF CHECKLIST DFW-ILE, THE CAPTAIN NOTICED THE LEFT HYDRAULIC PRESSURE GAUGE WAS INDICATING 150 0 LBS. THE ELECTRIC PUMP WAS TURNED ON AND THE PRESSURE RETURNED TO NORMAL. A FEW MINUTES LATER THE PRESSURE DROPPED T O ZERO AND THE CREW PERFORMED THE APPROPRIATE CHECKLISTS, DECLARED AND EMERGENCY AND RETURNED TO DFW. LANDING WAS MADE SAFELY AND WITHOUT INCIDENT. REMOVED AND REPLACED LEFT HYDRAULIC RETURN LINE AND ALSO ENGIEN DRIVE HYDRAULIC PUMP. OPE RATIONAL CNA LEAK CHECKS WERE GOOD AND AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M) 2 L 7 2 4T RT A31SO 1996110700635 19961107 00635 SO 1996 11 7 ASOA96046 1 19961016 A 6120 OIL PUMP EMB 120 EMB120RT SO RT PCU FALIED A A ASOA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 11 130AM 120134 APPROXIMATELY 60 MILES OUT ON APPROACH ICT-DFW, RIGHT NP BEGAN FLUCTUATING FROM 83 PECENT TO 87 PERCENT. ATTEMPTED 100 PERCENT NP, AND NP ROSE TO 101.5 PERCENT. CAPTAIN BROUGHT THE POWER LEVER BACK TO CONTROL THE NP, FLUCTUATION CONTINUE D (WENT TO 105 PERCENT). CREW SHUT DOWN THE RIGHT ENGINE AND DECLARED AND EMERGENCY. AIRCRAFT LANDED UNEVENTFULLY AT D FW. DOWN LOADED FDAU TO CHECK FOR POSSIBLE EXCEEDANCES. NONE NOTED. REMOVED AND REPLACED RIGHT PCU OIL PUMP. OPERATI ONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M) 2 L 7 2 4T RT A31SO 1996110700636 19961107 00636 SO 1996 11 7 ASOA96041 1 19960927 A 6120 78249024 PCU EMB 120 EMB120RT SO LT ENGINE LEAKING A ASOA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SO 11 503AS 120275 EN ROUTE AGS-ATL - THE LEFT ENGINE OIL PRESSURE BEGAN FLUCTUATING FROM 53 TO 65 PSID AND GOT ASSOCIATED MAP AND AURAL WA RNINGS. THE CREW DECLARED AN EMERGENCY AND DIVERTED INTO MCN WHERE LANDING WAS MADE SAFELY AND WITHOUT INCIDENT. FOUND OIL LEAK ON PCU MATING HALVES. REMOVED AND REPLACED PCU AND SERVICED ENGINE WITH 6 QUARTS OF OIL. OPERATIONAL AND LEA K CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M) 2 L 7 2 4T RT A31SO 1996110700637 19961107 00637 SO 1996 11 7 ASOA96042 1 19960928 A 3350 K0201 RELAY EMB 120 EMB120RT SO COCKPIT DEFECTIVE A ASOA O OTHER J S WARNING INDICATION AFFECT SYSTEMS CR CRUISE 1 SO 11 221AS 120020 EN ROUTE ATL-TRI, THE EMERGENCY LIGHT CIRCUIT BREAKER POPPED. THE CREW RESET THE SWITCH, AND IT IMMEDIATELY POPPED AGAI N. MTC CONTROL INSTRUCTED THE CREW TO RETURN TO ATL WHERE LANDING WAS MADE SAFELY AND WITHOUT INCIDENT. REMOVED AND RE PLACED RELAY K0201. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M) 2 L 7 2 4T RT A31SO 1996110700638 19961107 00638 WP 1996 11 7 WTAA960179 2 19961015 A 7200 ENGINE BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110U 01514 WP LEFT BIRD STRIKE A WTAA A UNSCHED LANDING C F.O.D. TO TAKEOFF 1 WP 17 418UE 780 P63281 ACV - BIRD INGESTION REPORTED IN LEFT ENGINE DURNG TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE DUE TO BIRD INGESTION. INSPECTED REMAINDER OF AIRCRAFT FOR DAMAGE, NONE DETECTED. AI RCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A21EU E4WE 1996110700639 19961107 00639 SO 1996 11 7 WTAA960177 1 19961008 A 3260 120011R RELAY BOX EMB 120 EMB120RT SO LT MLG FAILED A WTAA O OTHER N FALSE WARNING CL CLIMB 1 WP 17 122AM 120013 SFO - LEFT MAIN GEAR WARNING ON CLIMB-OUT. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE REPLACED LANDING GEAR RELAY BOX. GEAR RETRACTION SYSTEM OPERATIONAL CHECK NORMAL. TEST FLIGHT SATISFACTORY. AIRCRAFT RETURNED TO SERV ICE. (M) 2 L 7 2 4T RT A31SO 1996110700640 19961107 00640 NM 1996 11 7 WRLA96042 1 19961014 A 2822 608473 BOOST PUMP DOUG MD11 MD11 3023602 NM RT UPPER FAILED A WRLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 278WA 48746 DURING TAXIING OUT, FLIGHT CREW NOTED UPPER AUXILIARY BOOST PUMP FAILED. FLIGHT CREW ELECTED TO RETURN TO GATE. AIRCRA FT RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED RIGHT UPPER AUXILIARY BOOST PUMP. RESET RCCB. OP S CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A22WE 1996110700641 19961107 00641 WP 1996 11 7 GTIA96NK211 1 19961010 A 3350 FUSE DOUG DC9 DC932 3022066 WP CABIN BLOWN A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 12505 45788 AFT SECTION OF EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE. REMOVED AND REPLACED BLOWN FUSE IN BATTERY PACK, OPERATIONAL CHECK GOOD IAW DC-9 MM CH 33-53-01. (M) 2 L 7 2 4F A6WE 1996110700642 19961107 00642 WP 1996 11 7 GRAA9669 1 19960922 A 5610 5912290502 WINDSHIELD DOUG DC9 DC915 3022036 WP RT COCKPIT CRACKED A GRAA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 11 1068T 45782 AT 33,000 MSL, HAD THE FIRST OFFICERS WINDSHIELD CRACK. THE CAPTAIN DIVERTED TO DEN WITHOUT FURTHER INCIDENT. MAINTENA NCE REPLACED THE FIRST OFFICERS WINDSHIELD IAW DC-9 MM 56-10-2, PG 201-213. AIRCRAFT WAS PRESSURIZED AND LEAK CHECKED N ORMAL. NO DEFECTS NOTED. (M) 2 L 7 2 4F A6WE 1996110700643 19961107 00643 NM 1996 11 7 F3LA96043 1 19961016 A 5320 CHORD BOEING 737 737201 1384454 NM BS 727 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 205AU 19421 DURING SERVICE CHECK, INSPECTION REPORTD A .5 INCH CRACK IN OUTER CHORD AT STATION 727, STRINGER 25R. REPAIRED PER BOEI NG TELEX FRO-DEN-96-0090RR AND SRM 51-40-4, FIG 1. (M) 2 L 7 2 4F A16WE 1996110700644 19961107 00644 NM 1996 11 7 F3LA96031 1 19961010 A 5330 SKIN BOEING 737 737201 1384454 NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 205AU 19421 DURING SERVICE CEHCK, INSPECTION REPORTED A .5 INCH CRACK IN THE UPPER FORWARD CORNER OF THE FORWARD ENTRY DOOR CUTOUT. REPAIRED PER BOEING TELEX FRO-DEN-96-0085RR AND SRM 51-10-1. (M) 2 L 7 2 4F A16WE 1996110700645 19961107 00645 WP 1996 11 7 96ZZZM1443 1 19960930 A 2130 DUCT DOUG DC9 DC932 3022066 WP LT COALESCER BAG LOOSE A TWAA O OTHER J WARNING INDICATION CR CRUISE 1 CE 05 922L 47108 STL - DURING CRUISE AT 26,000 FEET, AIRCRAFT CABIN STARTED LOSING PRESSURE. DESCENDED TO 14,000 FEET TO MAINTAIN CABIN PRESSURE. FOUND DUCT SEPARATED FROM REAR OF LEFT WATER SEPARATOR. REATTACHED DUCT, OPERATIONAL AND LEAK CHECKS NORMAL. (M) 2 L 7 2 4F A6WE 1996110700646 19961107 00646 NE 1996 11 7 96ZZZM1444 2 19961002 A 7314 37340126 FUEL PUMP DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7A 52053 NE NR 2 ENGINE FAILED A TWAA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 CE 05 985Z 47491 RSW - DURING CLIMB-OUT NR 2 ENGINE, S/N 2131, SPOOLED DOWN AND AIRCRAFT RETURNED FROM FLIGHT. REMOVED AND REPLACED ENGI NE DRIVEN FUEL PUMP, MFG P/N 373401-26. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F 4 F A6WE E2EA 1996110700647 19961107 00647 NM 1996 11 7 96ZZZM1445 1 19961006 A 3230 691798819 RELEASE ACTUATOR BOEING 727 727231 1384079 NM NLG FAILED A TWAA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 54337 20491 STL - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, NOSE LANDING GEAR WOULD NOT RETRACT. FOUND NOSE LANDING GEAR LOCK RELEASE ACTUATOR TRUNNION BEARING PLATES, MFG P/N 69-17988-19, WORN. REPLACED LOCK ACTUATOR TRUNNION PLATES AND LOCK RE LEASE ACTUATOR, MFG PNM 65-40467-6. NOSE LANDING GEAR OPERATION THEN CHECKED NORMAL. (M) 2 L 7 3 4F A3WE 1996110700648 19961107 00648 NE 1996 11 7 96ZZZM1446 2 19961013 A 7200 ENGINE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7A 52053 NE NR 2 FAILED A TWAA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 984Z 47412 IAD - DURING CLIMB NR 2 ENGINE, S/N 2153, OIL FILTER BYPASS LIGHT ILLUMINATED. REDUCED POWER TO IDLE. FOUND METAL PART ICLES IN OIL FILTER. REPLACED NR 2 ENGINE. ENGINE OPERATION THEN CHECKED NORMAL. (M) 2 L 7 2 4F 4 F A6WE E2EA 1996110700649 19961107 00649 WP 1996 11 7 96ZZZM1447 1 19961008 A 3350 58222 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 991Z 47096 STL - DURING DESCENT, EGRESS LIGHT IN FIRST CLASS ILLUMINATED. FOUND FAULTY BATTERY POWER SUPPLY, MFG P/N 5822-2. REPL ACED BATTERY POWER SUPPLY AND EGRESS LIGHTING SYSTEM OPERATION CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 1996110700650 19961107 00650 WP 1996 11 7 96ZZZM1448 1 19961003 A 3350 0105602001 LENS DOUG DC9 DC983 3022083 WP CABIN BROKEN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9405T 53141 STL - DURING PREFLIGHT, FOUND EGRESS LIGHT LENS COVER TRACK BROKEN, MFG P/N 0105602-001. REPLACED LIGHT TRACK. EGRESS LIGHT SYSTEM AND OPERATION CHECKED NORMAL. (M) 2 L 7 2 4F RT A6WE 1996110700651 19961107 00651 NM 1996 11 7 96ZZZM1449 1 19961004 A 3260 MLCM737AS15 LAMP BOEING 727 727231 1384079 NM RT MLG INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 54342 21629 JFK - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, RIGHT MAIN LANDING GEAR GREEN DOWN AND LOCKED LIGHT DID NOT ILLUMI NATED. VISUALLY CHECKED LANDING GEAR DOWN AND LOCKED. FOUND LAMP, MFG P/N MLCM737AS15, INOPERATIVE. REPLACED BOTH MAI N LANDING GEAR DOWN AND LOCKED LIGHT LAMPS. LANDING GEAR INDICATING LIGHT SYSTEM OPERATION CHECKED NORMAL. (M) 2 L 7 3 4F A3WE 1996110700652 19961107 00652 WP 1996 11 7 96ZZZM1450 1 19961006 A 3350 39164 BATTERY PACK DOUG DC9 DC931 3022065 WP RT NACELLE DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 993Z 47082 STL - DURING OVERNIGHT, FOUND RIGHT NACELLE EMERGENCY LIGHT INOP. FOUND BATTERY PACK MFG P/N 39164, MALFUNCTIONING. RE PLACED BATTERY PACK AND EMERGENCY LIGHT SYSTEM OPERATION CHECKED NORMAL. 2 L 7 2 4F A6WE 1996110700653 19961107 00653 WP 1996 11 7 96ZZZM1451 1 19960930 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 316 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 984Z 47412 STL - DURING OP-15, FOUND A 3 INCH CRACK IN LONGERON 30, STATION 316. REPLACED LONGERON SECTION, STATION 303 TO STATION 380, PER SRM 53-02, FIGURE 14. 2 L 7 2 4F A6WE 1996110700654 19961107 00654 WP 1996 11 7 96ZZZM1452 1 19960927 A 5313 LONGERON DOUG DC9 DC931 3022065 WP LT LAVATORY CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 984Z 47412 STL - DURING OP-15 FOUND CORROSION AT LEFT LAV AREA, LONGERON 18L. REMOVED CORRODED AREA AND REPLACED WITH SPLICE PER S RM 53-05, FIGUER 25. 2 L 7 2 4F A6WE 1996110700655 19961107 00655 WP 1996 11 7 96ZZZM1453 1 19960926 A 5311 FRAME DOUG DC9 DC931 3022065 WP EMER EXIT CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 984Z 47412 STL - DURING OP-15 FOUND A 6 INCH CRACK IN FRAME BEHIND LEFT FORWARD EMERGENCY EXIT DOOR. REPAIRED PER ARA 10400. 2 L 7 2 4F A6WE 1996110700656 19961107 00656 WP 1996 11 7 96ZZZM1454 1 19960922 A 5347 SEAT TRACK DOUG DC9 DC951 3022051 WP BS 1100 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 405EA 47688 STL - DURING OP-15 FOUND CORROSION ON LEFT OUTBOARD SEAT TRACK, STATION 1100. REPLACED SEAT TRACK PER SRM 53-05, FIGURE 4F, SHEET 1. 2 L 7 2 4F A6WE 1996110700657 19961107 00657 WP 1996 11 7 96ZZZM1455 1 19960922 A 5347 SEAT TRACK DOUG DC9 DC951 3022051 WP BS 1100 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 405EA 47688 STL - DURING OP-15, FOUND CORROSION ON RIGHT INBOARD SEAT TRACK, STATION 1100. REPLACED SEAT TRACK PER SRM 53-05, PAGE 10G, FIGURE 4F. 2 L 7 2 4F A6WE 1996110700658 19961107 00658 WP 1996 11 7 96ZZZM1456 1 19960921 A 5330 SKIN DOUG DC9 DC951 3022051 WP BS 655-693 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 405EA 47688 STL - DURING OP-15, FOUND CORROSION ON SKIN AND DOUBLER, LONGERON 30, STATION 655-693. REPAIRED PER SRM 53-04, FIGURE 4 3, SHEET 4. (M) 2 L 7 2 4F A6WE 1996110700659 19961107 00659 WP 1996 11 7 96ZZZM1457 1 19960921 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 855-955 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 984Z 47412 STL - DURING OP-15, FOUND CORROSION, LONGERON 30, STATION 855 TO 955. REPAIRED PER SRM 51-10-4 AND 51-30-5. 2 L 7 2 4F A6WE 1996110700660 19961107 00660 WP 1996 11 7 96ZZZM1458 1 19960920 A 5313 LONGERON DOUG DC9 DC951 3022051 WP BS 1136 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 405EA 47688 STL - DURING OP-15, FOUND A .25 INCH CRACK TOP LEG, LONGERON 16R, STATION 1136. REPAIRED PER ARA 10559 AND SRM CHAPTER 51 STANDARD PRACTICES. (M) 2 L 7 2 4F A6WE 1996110700661 19961107 00661 WP 1996 11 7 96ZZZM1459 1 19960920 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 617 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 984Z 47412 STL - DURIGN OP-15, FOUND A ONE INCH CRACK IN LOWER FLANGE OF LONGERON 6L, STATION 617. REPAIRED PER SRM 53-02, FIGURE 2. (M) 2 L 7 2 4F A6WE 1996110700662 19961107 00662 WP 1996 11 7 96ZZZM1460 1 19960926 A 3350 58222 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 416EA 47751 STL - DURING CRUISE, EGRESS LIGHTS ILLUMINATED. CYCLED SWITCH. FOUND BATTERY POWER SUPPLY WEAK, MFG P/N 5822-2. REPLA CED BATTERY POWER SUPPLY. EGRESS LIGHT SYSTEM OPERATION CHECKED NORMAL. 2 L 7 2 4F A6WE 1996110700663 19961107 00663 WP 1996 11 7 96ZZZM1461 1 19960918 A 5313 LONGERON DOUG DC9 DC951 3022051 WP BS 1136 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 405EA 47688 STL - DURING OP-15 FOUND A .5 INCH CRACK AT TOP AND BOTTOM LEG, LONGERON 16L, STATION 1136. REPAIRED PER ARA 10536. (M ) 2 L 7 2 4F A6WE 1996110700664 19961107 00664 WP 1996 11 7 96ZZZM1462 1 19960918 A 5347 SEAT TRACK DOUG DC9 DC951 3022051 WP BS 1087 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 405EA 47688 STL - DURING OP-15, FOUND CORROSION ON LEFT INBOARD SEAT TRACK, FS 1087. REPLACED SEAT TRACK FROM FS 1022 TO FS 1100 PE R SRM 53-05 AND 51-10-4. 2 L 7 2 4F A6WE 1996110700665 19961107 00665 NM 1996 11 7 96ZZZM1463 1 19960922 A 7930 BYPASS SWITCH BOEING 727 727231 1384079 NM NR 3 ENGINE CLOGGED A TWAA O OTHER N FALSE WARNING CR CRUISE 1 CE 05 52312 19831 MCI - DURING CRUISE SHUT DOWN NR 3 ENGINE DUE TO OIL FILTER BYPASS LIGHT ILLUMINATION. FOUND BYPASS SWITCH BANJO FITTIN G CLOGGED. CLEANED BANJO FITTING. ENGINE OPERATION AND FILTER BYPASS LIGHT OPERATION CHECKED NORMAL. 2 L 7 3 4F A3WE 1996110700666 19961107 00666 WP 1996 11 7 96ZZZM1464 1 19960913 A 5313 LONGERON DOUG DC9 DC951 3022051 WP BS 1151 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 405EA 47688 STL - DURING OP-15, FOUND .25 INCH CRACK ON LOWER LIP OF LONGERON 17R, STATION 1151. REPAIRED PER SRM 53-02, PAGE 3. 2 L 7 2 4F A6WE 1996110700667 19961107 00667 WP 1996 11 7 96ZZZM1465 1 19960924 A 3350 58222 POWER SUPPLY DOUG DC9 DC941 302207N WP CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 935L 47603 STL - DURING CRUISE, EGRESS LIGHTING ILLUMINATED. FOUND WEAK BATTERIES IN POWER SUPPLY, MFG P/N 5822-2. REPLACED POWER SUPPLY. EGRESS LIGHT SYSTEM OPERATION CHECKED NORMAL. 2 L 7 2 4F A6WE 1996110700668 19961107 00668 WP 1996 11 7 96ZZZM1466 1 19960924 A 3350 LIGHTS DOUG DC9 DC951 3022051 WP CABIN MOISTURE CONTAM A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 416EA 47751 STL - DURING CRUISE, EGRESS LIGHTS ILLUMINATED IN AFT END OF CABIN. CYCLED SWITCH TO OFF AND BACK TO ARMED. FOUND MOIS TURE IN LIGHT TRACK. CLEANED AND DRIED TRACK. LIGHT OPERATION CHECKED NORMAL. 2 L 7 2 4F A6WE 1996110700669 19961107 00669 WP 1996 11 7 96ZZZM1467 1 19960918 A 3244 TIRE DOUG DC9 DC982 3022082 WP NR 2 FAILED A TWAA E ENGINE SHUTDOWN D INFLIGHT SEPARATION TO TAKEOFF 1 CE 05 918TW 49367 SFO - DURING TAKEOFF NR 1 ENGINE, S/N 3228, HAD EPR DECREASE FROM 1.93 TO 1.60. SHUT DOWN ENGINE. FOUND NR 2 TIRE RECA P SEPARATED AND ENGINE FAN AND NOSE COWL DAMAGE. REPLACED FOUR EACH FAN BLADES, NOSE COWLING AND NR 1 AND NR 2 MAIN LAN DING GEAR TIRES. ACCOMPLISHED BORESCOPE OF 6TH AND 7TH STAGE COMPRESSOR AND AVM SURVEY. ENGINE OPERATION CHECKED NORMA L. 2 L 7 2 4F A6WE 1996110700670 19961107 00670 NE 1996 11 7 96ZZZM1468 2 19960927 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 1 FAILED A TWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 05 953U 49267 GJT - DURING CRUISE NR 1 ENGINE, S/N 1407, SPOOLED DOWN. AIRCRAFT DIVERTED TO GJT, FOR AN ENGINE CHANGE. 2 L 7 2 4F 4 F A6WE E9NE 1996110700671 19961107 00671 WP 1996 11 7 96ZZZM1469 1 19960927 A 3350 20131A BATTERY PACK DOUG DC9 DC941 302207N WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 935L 47603 STL - DURING CRUISE, EMERGENCY ESCAPE PATH LIGHTING ILLUMINATED AT ROWS 8 THROUGH 12. REMOVED AND REPLACED BATTERY PACK , MFG P/N 2013-1A. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996110700672 19961107 00672 WP 1996 11 7 96ZZZM1470 1 19960923 A 2761 1040T1005 ACTUATOR DOUG DC9 DC932 3022066 WP SPOILER OVERHEATED A TWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 05 995Z 47027 STL - DURING CLIMB AN ELECTRICAL BURNING ODOR EMITTED INTO COCKPIT. FLIGHT RETURNED. FOUND AUTO GROUND SPOILER ACTUATO R OVERHEATED, MFG P/N 1040T100-5. REPLACED GROUND SPOILER ACTUATOR. GROUND SPOILER SYSTEM OPERATION CHECKED NORMAL. 2 L 7 2 4F A6WE 1996110700673 19961107 00673 NE 1996 11 7 96ZZZM1471 2 19960916 A 7510 1552121M FUEL HEAT VLV BOEING 727 727231 1384079 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE STICKING A TWAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 CE 05 54340 20845 STL - DURING CRUISE SHUT DOWN NR 3 ENGINE, S/N 3954, DUE TO HIGH OIL TEMPERATURE. FOUND FUEL HEAT VALVE, MFG P/N 15521 2-1M, STICKING IN THE OPEN POSITION. REPLACED FUEL HEAT VALVE. ENGINE OPERATION THEN CHECKED NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1996110700674 19961107 00674 NM 1996 11 7 AWXA960529 1 19960926 A 3350 HARNESS BOEING 737 737301 1384611 NM CABIN DISCONNECTED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 325AW 23260 PHX - FLT 580 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS INOP. FOUND HARNESS DISCONNECTED AT SEAT ROW. 2 L 7 2 4F RT A16WE 1996110700675 19961107 00675 NM 1996 11 7 AWXA950508 1 19960911 A 3350 1060091101 LIGHT BOEING 737 737277 1384570 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 179AW 22646 PHX - FLT 2446 - DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT 16C EMERGENCY LIGHT BROKEN OFF. REMOVED AND REPLACED EMER GENCY LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A16WE 1996110700676 19961107 00676 NM 1996 11 7 AWXA960551 1 19961001 A 3350 900835A BATTERY BOEING 737 737277 1384570 NM GALLEY DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 180AW 22062 22647 PHX - FLT 7838 - DURING ROUTINE MAINTENANCE CHECK, FOUND AFT GALLEY SIDEWALL EMERGENCY LIGHTS INOP. REMOVED AND REPLACE D BATTERY CARTRIDGE ASSEMBLY. OPERATIONS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996110700677 19961107 00677 NM 1996 11 7 AWXA960553 1 19961002 A 3350 20121 BATTERY CHARGER BOEING 737 7373S3 1384711 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 316AW 23713 PHX - FLT 2491 - DURING ROUTINE MAINTENANCE CHECK, FOUND OVERHEAD R-1 DOOR AND SEAT MOUNTED LIGHTS TO ROW 5 INOP. REMOV ED AND REPLACED BATTERY CHARGER FUSE AT ROW 2 AISLE. OPERATIONS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996110700678 19961107 00678 NM 1996 11 7 AWXA960594 1 19961014 A 2530 416000119 COFFEEMAKER BOEING 757 757225 1384959 NM AFT GALLEY FAILED A AWXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 28 907AW 2444 22691 PHX - FLT 0001 - AFT COFFEEMAKER CIRCUIT BREAKER OUT. FLIGHT ATTENDANT PUSHED IT BACK IN AND SMELLED ELECTRICAL SMOKE. REPLACED COFFEEMAKER. (M) 2 L 7 2 4F RT A2NM 1996110700679 19961107 00679 EA 1996 11 7 96ZZZM1472 1 19960927 A 5330 SKIN DHAV DHC7 DHC7102 2802708 EA BS 781 GOUGED A CICA K NONE O OTHER IN INSP/MAINT 1 SO 17 4860J 25198 19 PBI - AIRCRAFT WAS STRUCK BY A GROUND AIR CONDITIONING CART BEING TOWED BY A TUG. THE STRIKE OCCURRED ONTHE LEFT SIDE R EAR FROM STATION X781. THE DAMAGE IS CLASSIFIED AS A GOUGE. AN DER WAS CONTACTED AND REPAIRS ADE IAW DRAWING NR 96 PAR A 052R0-1 AND M0 NR 53-7-15 AND MO 53-7-14. 2 H 7 4 4T A20EA 1996110700680 19961107 00680 SW 1996 11 7 96ZZZM1473 1 19961001 A 5230 2724010001 SPRING SWRNGN SA227 SA227AC 8780603 SW CARGO DOOR WEAK A SWHA O OTHER J WARNING INDICATION LD LANDING 1 SW 17 373PH AC538 ON SCHEDULED FLT 604, DURING LANDING, THE CAGO DOOR ANNUNCIATOR ILLUMINATED. INVESTIGATION REVEALED THAT UPON ARRIVAL T O THE GATE THE CARGO DOOR HANDLE WAS OPEN APPROXIMATELY 1 INCH. FURTHER INVESTIGATION REVEALED THAT THE CARGO DOOR OVER CENTERING SPRING WAS WEAK. THE CARGO DOOR OVERCENTERING SPRING WAS REPLACED AND OPERATIONAL CHECKED SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A8SW 1996110700681 19961107 00681 WP 1996 11 7 SWHA96001 2 19960131 A 7250 31021069 WHEEL SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP TURBINE SECTION DEFECTIVE A A SWHA K NONE O OTHER IN INSP/MAINT 1 SW 17 718C AC572 P44202C SUMMARY REPORT OF FINDINGS OF TEAR DOWN REPORT OF SEIZED ENGINE, TEARDOWN OF HOT SECTION REVEALED FIRST STAGE TURBINE SH ROUDS WERE WARPED AND ONE SHROUD HAD TIP CURL CAUSING THE SHROUD TO COME IN CONTACT WITH TURBINE WHEEL. SECOND STAGE TU RBINE WHEEL COOLING RIVETS WERE MOVING AFT AND COMING OUT OF TURBINE WHEEL. RIVETS COMING IN CONTACT WITH SECOND STAGE STATOR AIR SEAL WAS DETERMINED TO BE PRIMARY CAUSE OF ENGINE LOCKUP. ALLIED SIGNAL REPORTS THIS A KNOW PROBLEM AND IS C URRENTLY INVESTIGATING THE PROBLEM TO DETERMINE CORRECTIVE ACTION. ENGINE WAS REASSEMBLED WITH NEW SECOND STAGE TURBINE WHEEL AND PASSED ALL TESTS. (M) 2 L 7 2 4T 4 T RT A8SW E4WE 1996110700682 19961107 00682 WP 1996 11 7 GRAA9668 1 19960904 A 8012 39279621 START VALVE DOUG DC9 DC987 3022087 WP RT ENGINE FAILED A GRAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 11 1074T 49727 ON CLIMB-OUT FROM RENO, A/C HAD THE RIGHT ENGINE START VALVE LIGHT ILLUMINATE. THE RIGHT START VALVE WAS PREVIOUSLY DEF ERRED. THE FLIGHT SHUTDOWN AND SECURED THE RIGHT ENGINE. AIRCRAFT RETURNED TO RNO. MAINTENANCE VERIFIED THAT THE RIGH T ENGINE START CONTROL VALVE WAS CLOSED. MX DISCONNECTED AND BAGGED THE RIGHT START CONTROL VALVE CANNON PLUG. AIRCRAF T RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A6WE 1996110700683 19961107 00683 EU 1996 11 7 USAAF96103 1 19961004 A 2131 21185265 CONTROLLER FOKKER F28 F28MK0100 4990807 EU NR 1 FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 850US 11276 AVL-CLT - FLT 1062 - AFTER TAKEOFF, NR 1 AUTOPRESSURE FAILED. NR 2 AUTOPRESSURE WAS ON MEL. CAPTAIN WENT TO MANUAL AND WAS UNABLE TO CONTROL PRESSURE. FLIGHT CLIMBED TO FL060 AND CABIN PRESSURE ALTITUDE CLIMBED 2000 FPM. CREW DESCENDED AND SHUT DOWN PACKS. FLIGHT RETURNED TO AVL WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 2 PRESSURE CONTROLLER, P RIMARY OUTFLOW VALVE, AND RELAY K3515. (M) 2 L 7 2 4F RT 1996110700684 19961107 00684 EU 1996 11 7 96ZZZM1474 1 19961004 A 2133 1037223 OUTFLOW VALVE FOKKER F28 F28MK0100 4990807 EU NR 1 FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 850US 11276 AVL-CLT - FLT 1062 - AFTER TAKEOFF, NR 1 AUTOPRESSURE FAILED. NR 2 AUTOPRESSURE WAS ON MEL. CAPTAIN WENT TO MANUAL AND WAS UNABLE TO CONTROL PRESSURE. FLIGHT CLIMBED TO FL060 AND CABIN PRESSURE ALTITUDE CLIMBED 2000 FPM. CREW DESCENDED AND SHUT DOWN PACKS. FLIGHT RETURNED TO AVL WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 2 PRESSURE CONTROLLER, P RIMARY OUTFLOW VALVE, AND RELAY K3515. REFERENCE USAAF96103. 2 L 7 2 4F RT 1996110700685 19961107 00685 EU 1996 11 7 96ZZZM1475 1 19961004 A 2130 FCA61039 RELAY FOKKER F28 F28MK0100 4990807 EU NR 1 FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 850US 11276 AVL-CLT - FLT 1062 - AFTER TAKEOFF, NR 1 AUTOPRESSURE FAILED. NR 2 AUTOPRESSURE WAS ON MEL. CAPTAIN WENT TO MANUAL AND WAS UNABLE TO CONTROL PRESSURE. FLIGHT CLIMBED TO FL060 AND CABIN PRESSURE ALTITUDE CLIMBED 2000 FPM. CREW DESCENDED AND SHUT DOWN PACKS. FLIGHT RETURNED TO AVL WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 2 PRESSURE CONTROLLER, P RIMARY OUTFLOW VALVE, AND RELAY K3515. REFERENCE USAAF96103. 2 L 7 2 4F RT 1996110700686 19961107 00686 NM 1996 11 7 PCAA9600312 1 19960918 A 3233 8300101 ACTUATOR DHAV DHC8 DHC8102 2809003 NM NLG FAILED A PCAA K NONE O OTHER CL CLIMB 1 EA 13 825EX 388 NOSE AMBER DOOR ANNUNCIATOR STAYED ILLUMINATED AFTER GEAR RETRACTION. REMOVED AND REPLACED NOSE LANDING GEAR DOOR MECHA NICAL SEQUENCE VALVE AND NOSE LANDING GEAR RETRACTION ACTUATOR. SERVICED HYDRAULIC SYSTEM AND PERFORMED RETRACTION TEST . OPERATIONAL AND LEAK CHECK PROVED SATISFACTORY IAW DHC MM CHAPTER 32. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1996110700687 19961107 00687 NM 1996 11 7 96ZZZM1476 1 19960918 A 3230 69210 SEQ VALVE DHAV DHC8 DHC8102 2809003 NM NLG FAILED A PCAA K NONE O OTHER CL CLIMB 1 EA 13 825EX 388 NOSE AMBER DOOR ANNUNCIATOR STAYED ILLUMINATED AFTER GEAR RETRACTION. REMOVED AND REPLACED NOSE LANDING GEAR DOOR MECHA NICAL SEQUENCE VALVE AND NOSE LANDING GEAR RETRACTION ACTUATOR. SERVICED HYDRAULIC SYSTEM AND PERFORMED RETRACTION TEST . OPERATIONAL AND LEAK CHECK PROVED SATISFACTORY IAW DHC MM CHAPTER 32. A/C RETURNED TO SERVICE. REFERENCE PCAA960031 2. 2 H 7 2 4T RT A13NM 1996110700688 19961107 00688 NM 1996 11 7 ASAA9610134 1 19961008 A 3350 8821004 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 12 THROUGH 16 . REPLACD BATTERY AND RECEIVER AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996110700689 19961107 00689 NM 1996 11 7 96ZZZM1477 1 19961008 A 3350 883200312 RECEIVER BOEING 737 7372X6C 1384552 NM CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 12 THROUGH 16 . REPLACD BATTERY AND RECEIVER AND LIGHTS OPERATED NORMALLY. REFERENCE ASAA9610134. 2 L 7 2 4F RT A16WE 1996110700690 19961107 00690 NM 1996 11 7 96ZZZM1478 1 19961001 A 2612 895397 FIRELOOP BOEING 747 747131 1384881 NM NR 4 ENGINE FAILED A TWAA O OTHER N FALSE WARNING CL CLIMB 1 CE 05 93107 19673 FCO - DURING CLIMB, NR 4 ENGINE, S/N 4275, NACELLE TEMPERATURE INDICATED HIGH. CHECKED ENGINE DUCTS FOR AIR LEAKS AND R UPTURES, NONE FOUND. REPLACED LOWER FORWARD AND LOWER AFT FIREWARNING LOOPS, MFG P/N 895397 AND 895398, RESPECTIVELY. P ERFORMED FAN TIEDOWN CHECK, RAN ENGINE AT HIGH POWER FOR NINE MINUTES WHILE MONITORING NACELLE TEMPERATURE, ALL INDICAT IONS NORMAL. 2 L 7 4 4F A20WE 1996110700691 19961107 00691 NM 1996 11 7 96ZZZM1479 1 19961001 A 2612 895398 FIRELOOP BOEING 747 747131 1384881 NM NR 4 ENGINE FAILED A TWAA O OTHER N FALSE WARNING CL CLIMB 1 CE 05 93107 19673 FCO - DURING CLIMB, NR 4 ENGINE, S/N 4275, NACELLE TEMPERATURE INDICATED HIGH. CHECKED ENGINE DUCTS FOR AIR LEAKS AND R UPTURES, NONE FOUND. REPLACED LOWER FORWARD AND LOWER AFT FIREWARNING LOOPS, MFG P/N 895397 AND 895398, RESPECTIVELY. P ERFORMED FAN TIEDOWN CHECK, RAN ENGINE AT HIGH POWER FOR NINE MINUTES WHILE MONITORING NACELLE TEMPERATURE, ALL INDICAT IONS NORMAL. 2 L 7 4 4F A20WE 1996110700692 19961107 00692 NE 1996 11 7 96ZZZM1480 2 19961012 A 7314 3782017 FUEL PUMP DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7A 52053 NE NR 1 ENGINE MALFUNCTIONED A TWAA E ENGINE SHUTDOWN O OTHER CL CLIMB 1 CE 05 991Z 47096 PIT - DURING CLIMB, NR 1 ENGINE, S/N 2106, WOULD NOT RESPOND TO THRUST LEVER MOVEMENT. SHUT DOWN ENGINE. REPLACED ENGI NE DRIVEN FUEL PUMP, MFG P/N 378201-7 AND FUEL CONTROL, MFG P/N 743602-5. ENGINE OPERATION CHECKED NORMAL. 2 L 7 2 4F 4 F A6WE E2EA 1996110700693 19961107 00693 NE 1996 11 7 96ZZZM1481 2 19961012 A 7321 7436025 FUEL CONTROL DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7A 52053 NE NR 1 ENGINE MALFUNCTIONED A TWAA E ENGINE SHUTDOWN O OTHER CL CLIMB 1 CE 05 991Z 47096 PIT - DURING CLIMB, NR 1 ENGINE, S/N 2106, WOULD NOT RESPOND TO THRUST LEVER MOVEMENT. SHUT DOWN ENGINE. REPLACED ENGI NE DRIVEN FUEL PUMP, MFG P/N 378201-7 AND FUEL CONTROL, MFG P/N 743602-5. ENGINE OPERATION CHECKED NORMAL. 2 L 7 2 4F 4 F A6WE E2EA 1996110700694 19961107 00694 SW 1996 11 7 96ZZZX5573 1 19960921 A 5302 206033004177 TAIL BOOM BELL 206 206L4 1182110 SW TR GRBOX LOOSE RIVETS A NYBA K NONE O OTHER IN INSP/MAINT 1 EA 11 125NH 4031 52099 DURING 100-HOUR INSPECTION MECHANIC NOTED 9 EA RIVETS LOOSE BY THE TAIL ROTOR GEARBOX AT STATION 174.105. 1 G 7 1 3U NC H2SW 1996110700695 19961107 00695 WP 1996 11 7 AALA961393 1 19960923 A 5320 593646091 FITTING DOUG DC9 DC982 3022082 WP DOOR OPENING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 295AA 49307 STA 115.5 FORWARD LOWER CORNER OF CARGO DOOR OPENING. CORROSION AROUND HI-LOCK FASTENERS. INSTALLED NEW SUPPORT FITTIN G. TST: 33,327.4. CYCLES, 19,146. (X) 2 L 7 2 4F A6WE 1996110700696 19961107 00696 NE 1996 11 7 96ZZZX5574 2 19960925 A 7250 3031800 CASE BEECH 99 C99 1154006 CE PWA PT6 PT6A36 52043 NE GAS GENERATOR CRACKED A AJZA K NONE O OTHER IN INSP/MAINT 1 WP 19 235AV 14882 3689 U235 PCE38171 DURING SCHEDULED HOT SECTION INSPECTION, MAINTENANCE FOUND GAS GENERATOR CASE CRACKED. CRACK EXTENDS APPROXIMATELY ONE INCH HORIZONTALLY AT THE 2 O'CLOCK POSITION JUST FORWARD OF DIFFUSER TUBE. ENGINE REMOVED FOR REPAIR. 1 L 7 2 3T 4 T A14CE E4EA 1996110700697 19961107 00697 CE 1996 11 7 96ZZZX5575 1 19961007 A 3260 327 LAMP BEECH 1900 1900C 1154161 CE RT MLG FAILED A GUUA O OTHER P NO WARNING INDICATION AP APPROACH 1 SO 19 181GA UB24 FLL/MCO - FLT 420 - PILOT REPORT: RIGHT LANDING GEAR LIGHT INOPERATIVE. DECLARED AN EMERGENCY. AIRCRAFT LANDED WITHOU T INCIDENT. CORRECTIVE: REPLACE RIGHT LANDING GEAR LAMP. PRESS-TO-TEST SATISFACTORILY. 2 L 7 2 4T RT A24CE 1996110700698 19961107 00698 NM 1996 11 7 96ZZZX5576 1 19960910 A 5313 STRINGER BOEING 737 7372L9 1384497 NM BS 520 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 465AT 21528 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND BS 520.0, STR 26L, STRINGER CORRODED. REMOVED THE TRAN SITION PANEL. STR 26L OUT OF LIMITS IAW SRM 51-10-6. CUT OUT A 12 INCH SECTION AT STA 520. FABRICATED REPAIR PARTS IA W SRM 53-10-3. INSTALLED PARTS IAW SRM 51-40-3. REF: NON-ROUTINE 060N1-0432/50774. 2 L 7 2 4F RT A16WE 1996110700699 19961107 00699 NM 1996 11 7 96ZZZX5577 1 19960910 A 5311 FRAME BOEING 737 7372L9 1384497 NM BS 460 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 465AT 21528 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND FRAME AT BS 460.0 BETWEEN STR 20L - STR 21L, AREA HAS T WO EACH CRACKS EMANATING FROM RIVET HOLES AT INNER CORD. FABRICATED FORMED SECTION REPAIR FROM 7075-0 .063 INCH IAW SRM 51-40-3. HEAT TREATED TO T-6 IAW BAC 5602. STOP DRILLED CRACKS. NDT VERIFIED CRACK TERMINATED IAW SRM 51-10-1. INST ALLED FORMED SECTION REPAIR IAW SRM'S 51-40-3, 51-30-2, AND 51-10-2. REF: N/R 060-N1-0467/50795. 2 L 7 2 4F RT A16WE 1996110700700 19961107 00700 NM 1996 11 7 96ZZZX5578 1 19960910 A 5315 FLOOR BEAM BOEING 737 7372L9 1384497 NM BS 312 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 465AT 21528 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND CABIN BS 312 RBL 20 FLOOR BEAM UPPER CAP CORRODED. FAB RICATED FLOOR BEAM REPAIR FROM 7075-T6 .063 INCH L-ANGLE IAW SRM 53-10-09. ALODINED AND PRIMED IAW SRM 51-10-02 AND MM 51-20-11. INSTALLED REPAIR IAW SRM 53-10-09 AND SRM 51-30-01. 2 L 7 2 4F RT A16WE 1996110700701 19961107 00701 NM 1996 11 7 96ZZZX5579 1 19960910 A 5320 ANGLE BOEING 737 7372L9 1384497 NM BS 380 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 465AT 21528 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND BS 380.0 LBL 25 TO RBL 25 FRAME L-ANGLE CORRODED. REMO VED HARDWARE, FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-01, FABRICATED NEW L-ANGLE FROM 7075 .050 INCH, 4 INCHES BY 1.50 INCHES BY 2.1850 INCHES IAW SRM 51-40-3. TREATED AND PRIMED IAW SRM IAW SRM 51-10-2. INSTALLED IAW SRM 51-30-0, NR 1 RAD ALT. OPS CHECKED GOOD IAW MM 34-48-01. 2 L 7 2 4F RT A16WE 1996110700702 19961107 00702 NM 1996 11 7 96ZZZX5580 1 19960910 A 5240 SERVICE DOOR BOEING 737 7372L9 1384497 NM BS 344 CRACKED A ZZDA O OTHER O OTHER IN INSP/MAINT 1 SO 15 465AT 21528 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND RT SERVICE DOOR AFT LOWER CORNER HAS 1.50 INCH LONG CRA CK AT FUSELAGE EXTERIOR SURFACE AT BS 344.0 WL 208.01. FABRICATED 3 DOUBLERS FROM 2024-T-3 .100 INCH, AND 2 FROM 2024-T -3 .063 INCH IAW SRM 53-30-3. TREATED IAW SRM 51-10-2. INSTALLED DOUBLERS IAWSRM 53-30-3. REF: N/R 060N1-0408/50730. 2 L 7 2 4F RT A16WE 1996110700703 19961107 00703 NM 1996 11 7 96ZZZX5581 1 19960908 A 5311 FRAME BOEING 737 7372L9 1384497 NM CARGO COMPT CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 465AT 21528 DURING C-CHECK INSPECTION, REVEALED THAT AFT CARGO COMPARTMENT FRAME HAS CORROSION UNDER NUTPLATES BETWEEN STR 24L AND S TR 25L. REMOVED CORROSION, MATERIAL REMOVAL FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REMOVED NUTPLATES IAW SRM 51-30 -2. FABRICATED FRAME REPAIR, DRILLED AND DEBURRED IAW SRM 51-40-3. CUT OUT CORRODED AREA AND FABRICATED FILLER. DRILL ED AND DEBURRED IAW SRM 51-40-3. ALODINED AND PRIMED IAW SRM 51-10-2 AND MM 51-20-11. INSTALLED FRAME REPAIR, FILLER A ND NUTPLATE IAW 51-30-2. 2 L 7 2 4F RT A16WE 1996110700705 19961107 00705 NM 1996 11 7 96ZZZX5583 1 19961004 A 2450 OVERSPEED BUTTON BOEING 737 737222 1384473 NM NR 1 ENGINE TRIPPED A ZZDA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 SO 15 468AT 19074 MCO/ORF - FLT 640 - AT FL 330, DISCONNECTED NR 1 GENERATOR DUE TO UNDER VOLTAGE. ATTEMPTED TO START APU WITH NO RESPONS E. A DIVERSION WAS MADE INTO JAX. MECHANICS TROUBLESHOT SYSTEM AND SERVICED NR 1 CSD. POST-MAINTENANCE ENGINE RUN REVE ALED NO PROBLEMS WITH NR 1 GENERATOR. MECHANICS RESET OVERPSPEED BUTTON ON M-280 MODULE AND RAN APU. RELEASED AIRCRAFT FOR SERVICE. 2 L 7 2 4F A16WE 1996110700706 19961107 00706 WP 1996 11 7 BDHA9600022 2 19960904 A 7321 89356117 FUEL CONTROL SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP LT ENGINE MALFUNCTIONED A BDHA O OTHER R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 15 328BA 4603 1109554 TC253 MSP - FLT 434 - THE LEFT ENGINE WAS FUEL LIMITED ON TAKEOFF. THE MAX POWER WAS TURNED UP AND A RUN PERFORMED. THE ENGI NE WAS VERY ERRATIC. INSPECTION OF THE FUEL CONTROL FOUND THE MANUAL FUEL VALVE WAS BINDING INSIDE. THE FUEL CONTROL W AS CHANGED AND ENGINE POWER RUN PERFORMED. THE AIRCRAFT WAS RELEASED. (X) 2 L 7 2 4T 4 T RT A8SW E4WE 1996110700707 19961107 00707 NE 1996 11 7 PCAA9600316 2 19960929 A 7320 7863916 HMU DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 ENGINE FAILED A PCAA O OTHER R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 EA 13 EICBJ 13550 2401 215 120774 NR 2 ENGINE TORQUE SLOWLY REDUCING AT 14,000 FEET WITH POWER LEVER AT FIREWALL, TORQUE REDUCED TO 60 PERCENT. REMOVED N R 2 ENGINE OUTBOARD IGNITOR AND 1 OUTBOARD DIFFUSER TUBE, INSPECTED LP AND HP COMPRESSORS AND TURBINES, NO DEFECTS FOUND . INSTALLED IGNITOR, AND DIFFUSER TUBE. REMOVED AND REPLACED HMU AND FUEL PUMP IAW PWC MM, OPERATIONAL AND LEAK CHECKE D GOOD. A/C RETURNED TO SERVICE. (X) 2 H 7 2 4T 4 T RT A13NM E20NE 1996110700716 19961107 00716 NE 1996 11 7 96NK171 2 19960524 A 7320 FUEL CONTROL DOUG DC9 DC932 3022066 WP PWA JT8 JT8D17A 52049 NE LT ENGINE OUT OF ADJUST A GTIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 23 941ML 47131 LOG PAGE 7770. ABORTED TAKEOFF. ON TAKEOFF, LEFT ENGINE DEVELOPED ONLY 1.8 EPR AT 90 PERCENT N1, RIGHT ENGINE DEVELOPED 1.78 EPR AT 88 PERCENT N1, BOTH POWER LEVERS WERE AGAINST THE STOPS. CORRECTIVE ACTION: TRIMMED NR 1 AND NR 2 ENGINES IAW MM 71-00. REFERENCE TRIM CHARTS FIGURE 508. OPS CHK NORMAL. (X) 2 L 7 2 4F 4 F A6WE E2EA 1996110700717 19961107 00717 NE 1996 11 7 96NK197 2 19960905 A 7320 PT2 LINE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D17A 52049 NE NOSE BULLET CLOGGED A GTIA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 23 969ML 47268 LOG PAGE 028762. FLT ORH/UCA DIVERTED ACY - NR 2 EPR GAUGE READS HIGH AT POWER SETTING ABOVE IDLE WITH ALL OTHER ENGINE PARAMETERS MATCHED. CORRECTIVE ACTION: TROUBLESHOT PER MM CHAPTER 77-11-2. FOUND MUD DEBRIS IN NOSE BULLET LINE. RE MOVED DEBRIS AND DID HIGH POWER ENG RUN AT 1.97 EPR AND HIGH SPEED TAXI WITH PILOT. ALL PARAMETERS CHECK GOOD PER MM CH APTER 71-00. (X) 2 L 7 2 4F 4 F A6WE E2EA 1996110700718 19961107 00718 NM 1996 11 7 9623285520 1 19961103 A 7930 OIL FILTER LIGHT BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE NR 1 ENGINE ILLUMINATED A NWAA D E RETURN TO BLOCK ENGINE SHUTDOWN N FALSE WARNING IN INSP/MAINT 1 GL 01 520US 23208 716373 AFTER PUSHBACK, THE NR 1 ENGINE OIL FILTER EICAS MESSAGE WAS DISPLAYED. AIRCRAFT RETURNED TO THE GATE. GROUND MAINTEN ANCE CHECKED MAG PLUGS AND REPLACED MAIN OIL STRAINER. NO CONTAMINATES WERE FOUND. 2 L 7 2 4F 4 F RT A2NM E17NE 1996110700719 19961107 00719 1996 11 7 9623299301 4 19961103 A 3421 VERTICAL GYRO DOUG DC9 DC982 3022082 WP NR 1 MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 301RC 48054 DURING CLIMB, CAPTAIN'S ADI BEGAN PRECESSING, TESTED OK ON PREFLIGHT. AUTO-PILOT DISCONNECTS AND WILL NOT ENGAGE IN NR 1 OR NR 2. REPLACED THE NR 1 VERTICAL GYRO. RAN RTS CHECK ON BOTH NR 1 AND NR 2 AUTO-PILOT AND FLIGHT DIRECTOR. RERAN BOTH ON APU POWER AND BOTH OPERATIONALLY CHECKED GOOD. 2 L 7 2 4F A6WE 1996110700720 19961107 00720 EU 1996 11 7 9623303207 1 19961104 A 3350 321454 POWER SUPPLY AIRBUS 320 A320211 3930320 EU CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 307US 17597 8272 106 DURING LINE MAINTENANCE, FOUND AFT EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED EPSU, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996110700721 19961107 00721 WP 1996 11 7 9623319910 1 19961101 A 3350 60030451 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 960N 47256 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY EXIT LIGHT AT MAIN CABIN DOOR INOPERATIVE. REPLACED POWER SUPPLY AN D BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996110700722 19961107 00722 WP 1996 11 7 9623329941 1 19961031 A 3260 DOWNLOCK BULB DOUG DC9 DC932 3022066 WP RT MLG FAILED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 3324L 47103 DURING APPROACH, THE RIGHT MAIN GEAR DOWNLOCK GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR WAS EXTENDED. RECYCLED GEAR TWO TIMES AND NORMAL INDICATIONS WERE ACHIEVED. CREW REPLACED ONE RIGHT MAIN GEAR GREEN INDICATION BULB. AIRCRAFT LANDED WITHOUT INCIDENT. DISCREPANCY COULD NOT BE DUPLICATED ON GROUND, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996110700723 19961107 00723 WP 1996 11 7 9623339985 1 19961103 A 3260 ROLLER BRACKET DOUG DC9 DC932 3022066 WP LT MLG LOOSE A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 985US 47479 DURING CLIMBOUT, LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. FLIGHT CONTINUED TO DESTINATION AT REDUCED SPEED AND AIRCRAFT LANDED WITHOUT INCIDENT. NO VIBRATION WAS EVER ENCOUNTERED DURING FLIGHT. MAINTENANCE FOUND LEFT MAIN GEAR DOOR LATCH ROLLER BRACKET LOOSE. SECURED BRACKET, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996110700724 19961107 00724 WP 1996 11 7 9623349919 1 19961102 A 3260 INDICATION BULBS DOUG DC9 DC932 3022066 WP NLG FAILED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 941N 47450 DURING APPROACH, NOSE GEAR DOWNLOCK GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR WAS EXTENDED. CREW EXECUTED GO-AROUND PRO CEDURES AND TOWER REPORTED THAT GEAR APPEARED TO BE DOWN AND LOCKED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOU ND NOSE GEAR GREEN INDICATION LIGHT BULBS BURNED OUT. REPLACED BULBS, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996110700725 19961107 00725 WP 1996 11 7 9623359947 1 19961031 A 2421 GENERATION DOUG DC9 DC931 3022065 WP RT ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J H WARNING INDICATION ELECT. POWER LOSS-50 PC TO TAKEOFF 1 GL 01 8938E 47161 DURING TAKEOFF ROLL AT 100 KNOTS, THE RIGHT GENERATOR DROPPED OFF LINE ACCOMPANIED BY AC CROSSTIE LOCKOUT LIGHT ILLUMINA TION. ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE REPLACED VOLTAGE REGULATOR, GENERATOR CONTROL PANEL, BUS CONTR OL PANEL AND CURRENT TRANSFORMER, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996110700726 19961107 00726 WP 1996 11 7 9623369947 1 19961102 A 2420 914F5674 AC RELAY DOUG DC9 DC931 3022065 WP RT GENERATOR FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 GL 01 8938E 18146 4191 47161 AC CROSSTIE LOCKOUT LIGHT ILLUMINATED EN ROUTE. FLIGHT DIVERTED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLAC ED RIGHT GENERATOR AC POWER RELAY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996110700727 19961107 00727 WP 1996 11 7 9623379949 1 19961031 A 3260 DOOR SWITCH DOUG DC9 DC931 3022065 WP LT/RT MLG MALFUNCTIONED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 8928E 45865 DURING APPROACH, LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS EXTENDED. EMERGENCY GEAR EXTENSION PROCEDURES WERE UTILIZED AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT AND RIGHT GEAR DOOR SWITCHES. ALSO, TIGHTENED BOLTS TO THE LEFT DOOR LOCK AND SWITCH STRIKER ASSEMBLY. LEFT GEAR DOOR SKID WAS REPLACED DUE TO DAMAGE INCUR RED ON LANDING, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996110700728 19961107 00728 NM 1996 11 7 9623382703 1 19961103 A 3241 CONNECTOR BOEING 727 727225 1384077 NM LT MLG FAILED A NWAA A UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS AP APPROACH 1 GL 01 8878Z 21451 UPON GEAR EXTENSION, MAIN GEAR OUTBOARD ANTI-SKID INOPERATIVE LIGHT ILLUMINATED. AIRCRAFT DIVERTED TO ORD AND LANDED WI THOUT INCIDENT. REPLACED THE LEFT GEAR DISCONNECT PLUG, OPERATIONAL CHECK NORMAL. 2 L 7 3 4F A3WE 1996110700729 19961107 00729 NM 1996 11 7 9623396302 1 19961104 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 662US 23720 DURING LINE CHECK, FOUND C-ZONE LEFT AND STAIRWAY EMERGENCY TRACK LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND POWER S UPPLY, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1996110700731 19961107 00731 WP 1996 11 7 9623419301 1 19961105 A 7931 OIL PRESS IND DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE LT ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 301RC 48054 708402 DURING TAKEOFF ROLL AT 80 KNOTS, THE LEFT ENGINE OIL PRESSURE INCREASED TO 60 PSI. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE OIL PRESSURE TRANSMITTER, OIL PRESSURE INDICATOR AND ADJUSTED THE PRESSURE RELIEF V ALVE ON THE LEFT ENGINE. LEAK AND OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F A6WE E9NE 1996110700732 19961107 00732 NM 1996 11 7 9623422704 1 19961104 A 2130 AIR MIX VALVE BOEING 727 727225 1384077 NM LEFT MALFUNCTIONED A NWAA B G EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 GL 01 801EA 22432 DURING CRUISE FLIGHT, LEFT AIR MIX VALVE STUCK IN FULL COLD POSITION. LOST CONTROL OF CABIN AT 33,000 FEET. AIRCRAFT M ADE EMERGENCY DESCENT, RECOVERED CABIN AT 11,500 FEET AND OXYGEN MASKS DEPLOYED. PERFORMED MIX VALVE FUNCTIONAL TEST, P RESSURIZED CABIN TO 8 PSI AND PERFORMED PRESSURIZATION SYSTEM TEST. PERFORMED VESSEL LEAKAGE TEST WITH NO EXCESSIVE LEA KAGE FOUND, SYSTEM OPERATIONALLY CHECKED OK. 2 L 7 3 4F A3WE 1996110700733 19961107 00733 1996 11 7 9623431211 4 19961105 A 3418 5293345976 COMPUTER DOUG DC10 DC1030 3023501 WP STALL WARNING FAILED A NWAA A J UNSCHED LANDING DUMP FUEL N FALSE WARNING TO TAKEOFF 1 GL 01 211NW 13278 1735 46868 DURING TAKEOFF, THE STALL WARNING STICK SHAKER ACTIVATED. FLIGHT DUMPED 41,000 POUNDS OF FUEL AND RETURNED TO HNL. MAI NTENANCE REPLACED THE AT/SC COMPUTER AND THE NR 2 AOA SENSOR. 2 L 7 3 4F A22WE 1996110700734 19961107 00734 WP 1996 11 7 9623449941 1 19961104 A 3260 DOWNLOCK SWITCH DOUG DC9 DC932 3022066 WP RT MLG MALFUNCTIONED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 3324L 47103 DURING APPROACH, THE RIGHT MAIN LANDING GEAR GREEN DOWNLOCK LIGHT DID NOT ILLUMINATE ON GEAR EXTENSION. RECYCLED GEAR A ND NORMAL INDICATIONS WERE ACHIEVED. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE RIGHT MAIN GEAR DOWNLOCK SWITCH AN D LANDING GEAR LEVER RELAY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996110700735 19961107 00735 EU 1996 11 7 WWMA9600093 1 19961102 A 2120 AIR DUCT SAAB SF340 340B 7860101 EU CABIN DIRTY A WWMA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 15 356SB 340B356 BAD OIL SMELL IN AIR CONDITIONING DURING CLIMB. INSP LT AND RT ACM AND ASSOCIATED DUCTS. REMOVED FLIGHT DECK OV/HEAD D UCTS AND REMOVED OLD DETERIORATED NAPKINS THAT WERE STUFFED UP IN THERE. CLEANED DUCTS, REINSTALLED AND OPS CK OK IAW S F340B AMM 21-20-00. 2 L 7 2 4T RT A52EU 1996110700736 19961107 00736 EU 1996 11 7 WWMA9600092 1 19961101 A 2612 89905202 FIRE CONTROL BOX SAAB SF340 340B 7860101 EU LEFT FAILED A WWMA K NONE O OTHER CR CRUISE 1 WP 15 341SB 340B341 CIRCUIT BREAKER E1 LEFT ENGINE POPPED OUT IN FLIGHT. REMOVED AND REPLACED LT FIRE DETECTION CONTROL BOX AND FUNCTIONAL CHECKED GOOD I/A/W SAAB AMM 26-21-00. 2 L 7 2 4T RT A52EU 1996110700737 19961107 00737 WP 1996 11 7 96FDEA01650 1 19961105 A 5320 SIDEWALL DOUG DC10 DC1010F 3022111 WP BS 1210 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68050 47804 SNRM 345, CORROSION FOUND ON TOP OF CTR TANK, BELOW MAIN CABIN FLOOR, LT SIDEWALL AREA, STA 1210. *S/D* CLEANED CORROS ION REF SRM 53-00-01. NDT MEASURED REMAINING SKIN THICKNESS. COMPLIED WITH HFEC INSP, NO DEFECTS NOTED. 2 L 7 3 4F A22WE 1996110700738 19961107 00738 EU 1996 11 7 96UAL900773 1 19961007 A 2421 IDG BOLTS SUNSTRAND 740119F AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 ENGINE LOOSE A A UALA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CR CRUISE 1 WP 29 413UA 1260 470 RETURNED TO ORD UNDER AMBER ALERT WITH NR 1 ENGINE GENERATOR FAILURE. *S/D* IDG DID NOT DISCONNECT. ROOT CAUSE WAS DU E TO IDG SCAVENGE PUMP/GOVERNOR HOUSING BOLTS COMING LOOSE. THIS ALLOWED VIBRATION WHICH BROKE THE WIRE STRANDS TO THE DISCONNECT SOLENOID. ALSO, LOOSE BOLTS CAUSED IDG PUMP GEAR TO DISENGAGE AND IDG TO LOOSE OIL PRESSURE CAUSING HIGH OIL TEMP PROMPTING CREW TO SHUT DOWN THE ENGINE. 2 L 7 2 4F 4 F RT A28NM E40NE 1996110700739 19961107 00739 NE 1996 11 7 96UAL900795 2 19961101 A 7321 FUEL CONTL UNIT 7436023 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE MALFUNCTIONED A UALA O OTHER E VIBRATION/BUFFET TO TAKEOFF 1 WP 29 7263U 21410 700296 NR 1 ENGINE NOISY AND VIBRATION ON TAKEOFF. *S/D* LOW FREQUENCY VIBRATION CAUSED THE NOISE AND VIBRATION. THE FUEL CO NTROL UNIT WAS REPLACED AND THERE HAS BEEN NO COMMENTS ON VIBRATIONS SINCE. 2 L 7 3 4F 4 F A3WE E2EA 1996110700740 19961107 00740 NM 1996 11 7 96UAL900804 1 19961014 A 2150 106050619 ACM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN SEIZED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 WP 29 304UA 23665 ON ARRIVAL, CABIN FILLED WITH SMOKE. *S/D* RIGHT AIR CYCLE MACHINE WAS FOUND TO BE SEIZED. REPLACED AIR CYCLE MACHINE , CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1996110700741 19961107 00741 NE 1996 11 7 96UAL900806 2 19961014 A 7230 53A321 FAN BLADES BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT ENGINE DAMAGED A UALA K NONE C F.O.D. NR NOT REPORTED 1 WP 29 650UA 25287 717654 A BIRD STRIKE OCCURRED IN THE RIGHT ENGINE WHICH CAUSED FAN BLADE AND NOSE COWL DAMAGE. *S/D* THE BIRD STRIKE RESULTED IN A COMPLETE REPLACEMENT OF THE FAN BLADE SET. A REPAIR WAS ACCOMPLISHED ON THE NOSE COWL, OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 1996110700742 19961107 00742 NM 1996 11 7 96UAL900809 1 19961014 A 2781 65176342 SWITCH BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 5 LE SLAT FAILED A UALA O OTHER N FALSE WARNING LD LANDING 1 WP 29 7278U 21425 DURING FINAL APPROACH WITH FLAPS AT 5 SPEED 180 KNOTS, AN AMBER LEADING EDGE FLAP LIGHT CAME ON INTERMITTENTLY. THE NUM BER 5 SLAT WAS UNLOCKED. *S/D* REPLACED NR 5 SLAT EXTEND SWITCH, SYSTEM OPERATIONALLY CHECKED OK. 2 L 7 3 4F 4 F A3WE E2EA 1996110700743 19961107 00743 NM 1996 11 7 96UAL900810 1 19961014 A 2751 9660022001 TRANSMITTER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE RT TE FLAPS DEFECTIVE A A UALA K NONE N FALSE WARNING LD LANDING 1 WP 29 7281U 21559 THE FLIGHT CREW REPORTED THE OUTBOARD TRAILING EDGE FLAPS WERE STUCK AT THE 25 DEGREE POSITION. *S/D* ISOLATED PROBLE M TO THE RT OUTBOARD FLAP TRANSMITTER. REPLACED TRANSMITTER AND SYSTEM OPERATIONAL CHECK WAS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1996110700744 19961107 00744 NM 1996 11 7 96UAL900811 1 19961014 A 2780 65618391 IND MODULE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LE FLAPS DEFECTIVE A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 7463U 21917 AIRCRAFT RETURNED TO DEN DUE TO LEADING EDGE DEVICES NOT RETRACTING. *S/D* REPLACED LEADING EDGE INDICATION MODULE M 8 18, SYSTEM CHECKED OK. 2 L 7 3 4F 4 F A3WE E2EA 1996110700745 19961107 00745 NM 1996 11 7 96UAL900822 1 19961018 A 4920 38420722 TURBINE WHEEL BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE TAIL DISINTEGRATED A A UALA K NONE O OTHER NR NOT REPORTED 1 WP 29 997UA 9690 7256 22457 95138 APU MUFFLER AND EXHAUST PIPE REQUIRE REPLACEMENT DUE TO DAMAGE DURING APU FAILURE. *S/D* THE TURBINE WHEEL FAILED CAUS ING UNCONTAINED SEPARATION. THE CAUSE IS BEING ADDRESSED BY INTRODUCTION OF CONTAINMENT AUGMENTATION RING THROUGH SERVI CE BULLETIN 49-A7189 AND COA 0-9223. 2 L 7 2 4F 4 F A16WE E2EA 1996110700746 19961107 00746 NE 1996 11 7 96UAL900837 2 19961028 A 7230 HPC ROTOR PWA PW2037 BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 ENGINE FRACTURE A UALA O OTHER C F.O.D. IN INSP/MAINT 1 WP 29 520UA 18875 7853 24890 726517 NR 2 ENGINE REMOVED FOR HPT T1 BLADE DISTRESS, DISCOVERED DURING BORESCOPE INSPECTION. DISASSEMBLY OF THE ENGINE REVEAL ED FOD DAMAGE THROUGHOUT ALL STAGES OF THE COMPRESSOR 6TH THROUGH 17. *S/D* C6 BLADES OLD STYLE RECEIVED FOD, DEBRIS F ROM C6 BLADES CAUSED ADDITIONAL DAMAGE DOWNSTREAM THROUGH C17. ALL BLADES REPLACED WITH NEW AND OPERATION CHECKS NORMA L. 2 L 7 2 4F 4 F RT A2NM E17NE 1996110700747 19961107 00747 EU 1996 11 7 96UAL900839 1 19961028 A 3260 664700500A4B CONTROL UNIT ULTRA ELECTR 664700500A4B AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RT MLG MALFUNCTIONED A UALA O OTHER N FALSE WARNING DE DESCENT 1 WP 29 423UA 6017 3187 504 RIGHT LANDING GEAR DID NOT DISPLAY GREEN ON GEAR EXTENSION. CYCLED GEAR AND RIGHT GEAR DOOR ECAM DISPLAYED MOMENTARLY F OLLOWED WITH NORMAL 3 GREENS. *S/D* REPLACED LGCIU AND OPERATIONALLY CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 1996110700748 19961107 00748 NM 1996 11 7 96UAL900840 1 19961029 A 7603 INTERLOCK ACT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT THROTTLE FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 541UA 25253 LEFT HAND THROTTLE HAS MECHANICAL STOP SHORT OF FULL MOVEMENT. *S/D* REDUCED THROTTLE MOVEMENT DUE TO THRUST REVERSER INTERLOCK ACTUATOR LOCKED IN EXTENDED POSITION DUE TO OPEN CIRCUIT BREAKER. RESET CIRCUIT BREAKER, OPERATION CHECKS NOR MAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996110700749 19961107 00749 NM 1996 11 7 96UAL900841 1 19961029 A 4900 AS3209014 O-RING BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE APU SATURATED A UALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 922UA 26642 AIRCRAFT RETURNED TO BLOCKS DUE TO SMOKE IN THE CABIN. UNABLE TO CLEAR CABIN WITH ANY PACK BLEED COMBINATION. *S/D* R EMOVED AND REPLACED WATER SOCKS, REPLACED O-RINGS ON BOTH SPEED SENSORS AND APU CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1996110700750 19961107 00750 NM 1996 11 7 96UAL900842 1 19961029 A 2781 AL60F12B12SN CONNECTOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LE FLAP DEFECTIVE A UALA K NONE N FALSE WARNING CR CRUISE 1 WP 29 7289U 21567 LEADING EDGE FLAP AMBER LIGHT ILLUMINATED DURING CRUISE WITH FLAPS UP. SECOND OFFICER FLAP POSITION INDICATOR FOR LEF N R 5 GREEN LIGHT BLINKING OCCASIONALLY. *S/D* REPLACED CONNECTOR AT THE NR 5 LEADING EDGE FLAP SWITCH, SYSTEM CHECKED OK. 2 L 7 3 4F 4 F A3WE E2EA 1996110700751 19961107 00751 NE 1996 11 7 96UAL900843 2 19961029 A 7230 3053556250 BEARING BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE FAILURE A UALA A E UNSCHED LANDING ENGINE SHUTDOWN R E PARTIAL RPM/PWR LOSS VIBRATION/BUFFET CR CRUISE 1 WP 29 951UA 11076 26696 856547 CREW REPORTED NUMBER ONE ENGINE INFLIGHT SHUT DOWN DUE TO LOW OIL PRESSURE. ENGINE STARTED TO CHUG AND VIBRATE. ENGINE WAS SPOOLED DOWN, WOULDN'T RESPOND TO THROTTLE. SHUT DOWN ENGINE, OIL PRESSURE WAS 3 TO 5 POUNDS PER SQUARE INCH WINDM ILLING. *S/D* ENGINE HAD NUMBER FOUR BEARING FAILURE. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A16WE E2GL 1996110700752 19961107 00752 1996 11 7 96UAL900844 4 19961030 A 2565 INFLATE TUBE AIR CRUISERS D28935103 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE DOOR SLIDE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7298U 17528578 21893 DURING TIME CONTROLLED OVERHAUL SLIDE DEVELOPED SEAM LEAK ON INFLATION TUBE. SLIDE SCRAPPED. 2 L 7 3 4F 4 F A3WE E2EA 1996110700753 19961107 00753 WP 1996 11 7 96UAL900845 1 19961030 A 3350 58802 LIGHT DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1858U 46987 EMERGENCY EXIT LIGHTING TEST FAILED. FORWARD SECTION AT FAULT. FOUND FORWARD SECTION LIGHT ASSEMBLY INOPERATIVE AND BR OKEN CABLE NEAR LIGHT CONNECTION. REPLACED LIGHT ASSEMBLY AND REPAIRED CABLE. 2 L 7 3 4F 4 F A22WE E23EA 1996110700754 19961107 00754 NM 1996 11 7 96UAL900846 1 19961030 A 2150 PACKS BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LT/RT FROZEN A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 7261U 21408 AFTER TURNING PACKS ON, RIGHT PACK TRIPPED OFF. COMPRESSOR OUTLET TEMPERATURE IN RED BAND, LEFT PACK WAS APPROACHING Y ELLOW BAND. NOTICED HIGH DUCT TEMPERATURE, DUCT OVERHEAT LT LIGHT AND PACK TRIP OFF. SMOKE FILLED BOTH COCKPIT AND CAB IN. *S/D* AFTER MAINTENANCE THAWED BOTH PACKS THE OPERATIONAL CHECK WAS OK. 2 L 7 3 4F 4 F A3WE E2EA 1996110700755 19961107 00755 NM 1996 11 7 96UAL900847 1 19961030 A 2820 69186128 VENT TUBE ELBOW BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 TANK CRACKED A UALA O OTHER O OTHER CR CRUISE 1 WP 29 7298U 21893 UNCOMMANDED FUEL TRANSFER FROM TANK 3 WHILE X-FEEDING. NR 3 TANK QUANTITY DECREASED 700 POUNDS IN ONE HOUR. *S/D* REP LACED NR 3 TANK VENT TUBE ELBOW. 2 L 7 3 4F 4 F A3WE E2EA 1996110700756 19961107 00756 NM 1996 11 7 96UAL900848 1 19961031 A 3310 2001642600 TRANSFORMER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CONTROL CABIN FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 7272U 21419 SMOKE COMING FROM TOP OF FLIGHT ENGINEER'S PANEL. *S/D* THE SECOND OFFICER TABLE LIGHTS WERE FOUND TO BE OVERHEATED. R EPLACED LIGHTING CONTROL TRANSFORMER. 2 L 7 3 4F 4 F A3WE E2EA 1996110700757 19961107 00757 NM 1996 11 7 96UAL900849 1 19961101 A 3350 LIGHT BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 160UA 21237 EMERGENCY BUSTLE LIGHT IS INOP AT DOOR 1 LEFT LIGHT FAILED. REPLACED SLIDE LIGHT ASSEMBLY. 2 L 7 4 4F 4 F A20WE E20EA 1996110700758 19961107 00758 WP 1996 11 7 96UAL900850 1 19961101 A 2730 TRIM DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL ELEVATOR TAIL HEAVY A UALA C D ABORTED TAKEOFF RETURN TO BLOCK F FLT CONT AFFECTED TO TAKEOFF 1 WP 29 1843U 46636 DURING TAKEOFF ROLL APPROXIMATELY 50 TO 60 KNOTS, AIRCRAFT FELT LIKE IT NEEDED MORE NOSE DOWN TRIM. A UNIT OF TRIM WAS ADDED, AS AIRSPEED INCREASED MORE PRESSURE WAS NEEDED, MORE THAN NORMAL. IT FELT EXTREMELY TAIL HEAVY AND TAKEOFF WAS ABORTED. *S/D* LOAD IN AFT CARGO COMPARTMENT WAS WITHIN LIMITS. CHECKED ELEVATOR AND STABILIZER RIG, BOTH WITHIN LIMI TS. TEST FLIGHT WAS MADE AND OPERATION WAS NORMAL. 2 L 7 3 4F 4 F A22WE E23EA 1996110700759 19961107 00759 NM 1996 11 7 96UAL900851 1 19961101 A 3350 CONNECTOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7261U 21408 FLOOR EMERGENCY LIGHT INOPERATIVE AT DOOR L1. SECURED LOOSE CONNECTION, TESTED GOOD. 2 L 7 3 4F 4 F A3WE E2EA 1996110700760 19961107 00760 NM 1996 11 7 96UAL900852 1 19961102 A 5753 65B1159829 CARRIAGE ASSY BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE TE FORE FLAP FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 4723U 12984 19882 DURING SCHEDULED C-CHECK, THE FORE FLAP ATTACH CLEVIS LUG ON NR 4 TRAILING EDGE FORE FLAP SEQUENCE CARRIAGE UPPER SURFAC E WAS DISCOVERED TO HAVE FAILED. PART FAILED. THE FLAP POSITION NR 4 FORE FLAP SEQUENCE CARRIAGE WAS REPLACED. 2 L 7 4 4F 4 F A20WE E20EA 1996110700762 19961107 00762 NM 1996 11 7 DLM88962389 1 19961024 A 3231 RETRACT MECH 39567851 DOUG MD88 MD88 3023688 NM NLG DOOR MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 929DL 49716 ON T/O, THE NOSE GEAR DOOR ON THE COPILOT'S SIDE DID NOT CLOSE. FLIGHT RETURNED TO CAE. ON RETURN TO CAE, THE RT NOSE GEAR DOOR WAS FOUND OPEN. MTC INSPECTED THE DOOR LOCKING MECHANISM AND FOUND OPERATIONALLY OK FOR SERVICE. 2 L 7 2 4F RT A6WE 1996110700763 19961107 00763 WP 1996 11 7 DLL15962390 1 19961024 A 3350 POWER SUPPLY 516574 LKHEED 1011 10113853 5265020 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 756DR 51062 193Y1185 FIRST CLASS EMERGENCY LIGHTS WERE DISCOVERED TO REMAIN ON FOR AN INSUFFICIANT AMOUNT OF TIME DURING A TEST OF EMERGENCY LIGHTING SYSTEM. TEST WAS REQUIRED AS A LAYOVER CHECK ITEM. THE EMERGENCY LIGHT POWER SUPPLY AT THE R1 CABIN ENTRANCE DOOR WAS REPLACED AND THE SYSTEM THEN OPERATED NORMALLY. 2 L 7 3 4F A23WE 1996110700764 19961107 00764 WP 1996 11 7 DLL10962396 1 19961026 A 3260 327104169 PROX SWITCH LKHEED 1011 10113851 5265010 WP NLG WORN A DALA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SO 27 722DA 38526 193C1147 EAR000 AFTER T/O, UPON GEAR RETRACTION RED DOOR INTRANSIT LIGHT REMAINED ON UP FRONT AND NOSE GEAR OR DOOR LIGHT REMAINED ON AT S/O PANEL. REPLACED UPLOCK AND LT NOSE GEAR DOOR PROX SWITCHES, SWUNG GEAR CHECKS OK. 2 L 7 3 4F A23WE 1996110700765 19961107 00765 WP 1996 11 7 DLL17962397 1 19961026 A 2612 FIRE LOOP LKHEED 1011 10113853 5265020 WP NR 1 ENGINE FAILED A DALA E ENGINE SHUTDOWN N FALSE WARNING TO TAKEOFF 1 SO 27 767DA 32027 193H1209 14714 NR 1 ENG FIRE WARNING AFTER T/O, BOTH A AND B LOOPS ILLUM. CAPTAIN RETARDED NR 1 THROTTLE FIRE WARNING WENT OUT. TEST ED LOOPS AGAIN, NO TEST ON LOOP-B. REPLACED LOWER COMBUSTION CHAMBER MODULE LOOP ASSY, ALL CHECKS GOOD, RAN ENG TO TAKE OFF POWER AND NO DEFECTS. 2 L 7 3 4F A23WE 1996110700766 19961107 00766 WP 1996 11 7 DLL17962398 1 19961026 A 2830 TERMINAL LKHEED 1011 10113853 5265020 WP LT WING SHORTED A DALA J DUMP FUEL J WARNING INDICATION CL CLIMB 1 SO 27 767DA 193H1209 14714 UPON DUMPING OF FUEL NR 1 TANK DUMP VALVE WOULD NOT OPEN. FOUND TERMINALS SHORTED AGAINST EACH OTHER AT NR 13 FUEL PROB E THERMISTER. REPOSITIONED TERMINALS SYSTEM CHECKS NORMAL. 2 L 7 3 4F A23WE 1996110700767 19961107 00767 WP 1996 11 7 DLL14962401 1 19961027 A 3350 5165741 POWER SUPPLY LKHEED 1011 1011385115 5265015 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 736DY 193C1227 14714 EMERGENCY LIGHTS AT L1/R1 DOOR INOP. REPLACED POWER SUPPLY, CK'S GOOD. 2 L 7 3 4F A23WE 1996110700768 19961107 00768 NM 1996 11 7 DL76S962402 1 19961026 A 2422 241002136 INVERTER 7077603 BOEING 767 767332 1382001 NM NR 1 ENGINE MALFUNCTIONED A A DALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TO TAKEOFF 1 SO 27 134DL 339 25123 339 REF LOG A175829 ITM 2, LOST STBY BUSSES 25 MIN AFTER T/O. MID LAV SMOKE DETECTOR WENT OFF W/LIGHT SMOKE IN AREA THEN DI SAPPEARED. REPLACED STBY INVERTER CHKS OK PER MM. CAPT REPORTED, THE DAY BEFORE RANDOM SMOKE DETECTORS IN FRONT AND A FT LAVS WENT OFF THEN STOPPED WITH NO VISIBLE SMOKE IN A/C. THIS STATIC INVERTER (P/N 2410 02136) (S/N 339) IS SUSPECTE D TO HAVE CAUSED PROBLEM. 2 L 7 2 4F RT A1NM 1996110700769 19961107 00769 NM 1996 11 7 DL73E962403 1 19961028 A 2751 1817381 TRANSMITTER BOEING 737 7372S3 NM LT TE FLAPS INOPERATIVE A DALA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 27 367DL 21774 FLAPS FAILED TO EXTEND. REPLACED LT FLAP POS TRANSMITTER AND INDICATOR, OPER CK OK. 2 L 7 2 4F RT A16WE 1996110700770 19961107 00770 WP 1996 11 7 DLL10962405 1 19961028 A 3610 1506776113 DUCT LKHEED 1011 10113851 5265010 WP NR 2 ENGINE RUPTURED A DALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 27 1734D 193C1225 10632 NR 2 ENG PNEUMATIC DUCT RUPTURE AFT OF BAGGAGE BIN WALL IN NR 3 BIN DAMAGING DUMP CHUTE TO AFT LAVATORIES RESULTED IN J- AREA OVHT AND AFT CARGO HOT LIGHT. 2 L 7 3 4F A23WE 1996110700771 19961107 00771 NM 1996 11 7 DLM11962406 1 19961028 A 3350 LIGHTS DOUG MD11 MD11 3023602 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 811DE 48566 10632 EMERGENCY TRACK LIGHTS INOP ON LEFT SIDE AT SEAT ROWS 2 TO 37, 38 TO 40, 41 TO 44, 45 TO 52, 53. RIGHT SIDE AT SEAT ROW S 1 TO 3, 43, 44 TO 46, 47 TO 51. 2 L 7 3 4F RT A22WE 1996110700772 19961107 00772 NM 1996 11 7 DLM11962409 1 19961027 A 3350 CM7839 BULB DOUG MD11 MD11 3023602 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 811DE 48566 10632 EMERGENCY TRACK LIGHTS ON LT SIDE AT ROWS 2, 37, 38, 40, 41, 44, 45, 52, 53 AND RT SIDE AT ROWS 1, 3, 43, 44, 46, 47, 51 OUT. RELAMPED TRACK LIGHTS, OPN CK GOOD ON TEST. 2 L 7 3 4F RT A22WE 1996110700773 19961107 00773 WP 1996 11 7 DLL16962412 1 19961029 A 3244 L1011MAIN TIRES LKHEED 1011 10113853 5265020 WP LT MLG FAILED A DALA F ACTIVATE FIRE EXT. O OTHER LD LANDING 1 SO 27 760DH 193Y1194 ON TOUCHDOWN, LEFT MAIN TIRES BLEW DURING ROLLOUT, BEFORE BRAKE APPLICATION. REPLACED 1 REAR AND 2 REAR WHEEL ASSEMBLIE S PER M/M. 2 L 7 3 4F A23WE 1996110700774 19961107 00774 NM 1996 11 7 DL72S962414 1 19961029 A 5320 WEB BOEING 727 727232 1384082 NM BS 1243 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 419DA 21272 A .75 INCH CRACK AT LIGHTNING HOLE STATION 1243 LT, LOWER TORQUE BOX WEB. INSTALLED DOUBLER PER MM 53-11-0 PG 828. 2 L 7 3 4F A3WE 1996110700775 19961107 00775 NE 1996 11 7 DLM88962415 2 19961030 A 7230 COMPRESSOR DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE DAMAGED A DALA C ABORTED TAKEOFF C F.O.D. TO TAKEOFF 1 SO 27 969DL 16619 53172 725627 LOUD BANG AND EPR DROP ON NR 1 ENGINE WHEN THROTTLES ADVANCED TOWARD TAKEOFF POWER OF 1.87 EPR. AIRSPEED +/- 20KEPR BET WEEN 1.5 AND 1.6 WHEN TAKEOFF ABORTED. NORMAL BRAKING AND EXIT FROM RUNWAY. ENGINE INGESTED FOD, ENGINE CHANGED. 2 L 7 2 4F 4 F RT A6WE E9NE 1996110700776 19961107 00776 WP 1996 11 7 DLL17962418 1 19961030 A 3350 BATTERY PACK LKHEED 1011 10113853 5265020 WP CABIN NOT SEATED A DALA K NONE L NO TEST CR CRUISE 1 SO 27 765DA 193H1206 10632 HALF OF THE EMERGENCY EGRESS PATH LIGHTS INOP. RESEATED BATTERY PACKS, OPS NORMAL. 2 L 7 3 4F A23WE 1996110700777 19961107 00777 NM 1996 11 7 DLM88962419 1 19961031 A 2910 7936913842 HYD LINE 7936913842 DOUG MD88 MD88 3023688 NM TAIL COMPT CRACKED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 918DL 49583 AFTER T/O DURING SLAT RETRACT GOT MASTER CAUTION LIGHT AND RT HYDRAULIC PRESS LOW ON OAP. RT PRESS WAS -0- AND QTY WAS 1 QT. RAN CK LIST AND AFTER FLAP SLATS EXT TO 15 DEGR QTY WAS 3 QTS. AFTER LDG AND FLAPS SLATS WERE RETRACT QTY WENT U P TO 6 QTS. FOUND CRACKED RIGID LINE AT RT ENG FILTER MODULE TO RT ENG PUMP. REPLACED LINE. 2 L 7 2 4F RT A6WE 1996110700778 19961107 00778 NM 1996 11 7 DL72S962423 1 19961031 A 3350 81 BULB BOEING 727 727232 1384082 NM CABIN LOOSE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 470DA 20747 AFT LEFT OVERWING ESCAPE EMERGENCY ESC LIGHT HAD FWD BULB INOP. FOUND BULB SEATED IMPROPERLY. RESEATED BULB, OPS CK NO RMAL. 2 L 7 3 4F A3WE 1996110700779 19961107 00779 NM 1996 11 7 DL757962424 1 19961028 A 5330 SKIN BOEING 757 757232 1384965 NM BS 720 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 603DL 22810 CORROSION WAS FOUND AROUND THE WING SCANNING LIGHT CUTOUT AT STA 720B+10 AND S-15L. THE CORROSION IS WITHIN THE REPAIR LIMITS OF B727 SRM 53-50-5, FIGURE 22 AND WAS BEING REPAIRED BY THAT SECTION. DURING ACCOMPLISHMENT OF THAT REPAIR SEVE N HOLES WERE DRILLED TOO CLOSE TO THE UPPER SKIN OF THE S-14L LAP JOINT FOR INSTALLATION OF FASTENERS IN THE REPAIR DOUB LER, LITTLE OR NO EDGE MARGIN. 2 L 7 2 4F RT A2NM 1996110700780 19961107 00780 NM 1996 11 7 DL757962425 1 19961022 A 5414 311N3450 SKIN BOEING 757 757232 1384965 NM NR 1 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 620DL 22910 THE O/B SKIN OF THE NR 1 ENGINE PYLON WAS FOUND TO HAVE A CRACK CONTINUING BEYOND A PREVIOUS STOP DRILL OUT OF THE UPPER , FWD CORNER OF THE FWD ACCESS OPENING AT NS 112.92. WHEN ROUTED OUT, THE TOTAL LENGTH WAS 1.50 INCH. THE SKIN AT THIS LOCATION IS FABRICATED FROM THREE BONDED 0.080 2024-T3 CLAD SHEETS. THIS CONDITION IS ADDRESSED BY B757 SRM SECTION 54 -41-01, PG 210 AND FOLLOWING. IN ADDITION, THERE WAS A CRACK OUT OF THE FWD SIDE OF THE ACCESS OPENING CENTERED AT NS 1 22.3. AFTER ROUTING OUT, THIS MEASURED .50. 2 L 7 2 4F RT A2NM 1996110700781 19961107 00781 WP 1996 11 7 DLL10962427 1 19961010 A 5311 1505563104 FRAME LKHEED 1011 10113851 5265010 WP BS 1343 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 722DA 193C1147 AFTER BEING INSPECTED PER SI 7-69903-12AD, THE RT SIDE FUSELAGE FRAME WAS FOUND CRACKED AT THE TYPICAL LOCATION OVER THE WL 280.6 LONGERON AND DIRECTLY OVER STR 14. THE CRACK WAS REPAIRED PER THE SI WITH MINOR DEVIATIONS. REV B TO ER/A PR OVIDES FAA APPROVAL. 2 L 7 3 4F A23WE 1996110700782 19961107 00782 WP 1996 11 7 DLL10962428 1 19961011 A 5320 LS13112 PRESS DECK LKHEED 1011 10113851 5265010 WP BS 380 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 722DA 193C1147 THE FUSELAGE HORIZ PRESSURE DECK PANEL WAS FOUND WITH A 1.5 CRACK, LOCATED AT RBL 102, JUST AFT OF FS 378 AND EXTENDS DI AGONALLY I/B AND AFT FROM THE FWD EDGE OF THE PANEL AT THE EXISTING FRAME CUTOUT. THE CRACK EXTENDS OVER A LOWER INTEGR AL PANEL STIFFENER. THE CRACK WAS CUT OUT AND REINFORCED WITH REPAIR DOUBLERS. REV A TO ER/A PROVIDES FAA APPROVAL. 2 L 7 3 4F A23WE 1996110700783 19961107 00783 NM 1996 11 7 DL72E962430 1 19961031 A 3350 LIGHT BOEING 727 727247 138408F NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 282WA 21484 FOUND EMERGENCY EXIT LIGHT ABOVE 1L DOOR WILL NOT COME ON. REPLACED LIGHT EXIT ASSY. 2 L 7 3 4F A3WE 1996110700784 19961107 00784 NE 1996 11 7 DLL10962431 2 19961101 A 7320 FUEL FLOW REG 737003467 LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B NE NR 2 ENGINE MALFUNCTIONED A DALA E ENGINE SHUTDOWN X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 SO 27 719DA B1084 193C1135 10657 ENG NR 2 FLAMED OUT SHORTLY AFTER TAXIING CLEAR OF RUNWAY AFTER LANDING, WAS VERY HARD TO START. REPLACED FFR ON NR 2 E NG, ENG STARTS NORMALLY. PERFORMED CKS PER PFHB, ALL CKS OK. T/O PWR REACHED WITH PLENTY OF ROOM, NO LEAKS. 2 L 7 3 4F 4 F A23WE E12EU 1996110700785 19961107 00785 NM 1996 11 7 DL72S962432 1 19960903 A 5751 652176634 SPAR BOEING 727 727232 1384082 NM RT AILERON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 492DA 21061 10657 REAR SPAR WAS FOUND CRACKED. REPAIRED SPAR PER SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 1996110700786 19961107 00786 NM 1996 11 7 DL72S962434 1 19961101 A 5720 STIFFENER BOEING 727 727232 1384082 NM RT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 401DA 21145 10657 O/B LEADING EDGE SPAR STIFFENER CRACKED AT NR 6 SLAT I/B TRACK. REPLACED STIFFENER PER M/M 57-20-21. 2 L 7 3 4F A3WE 1996110700787 19961107 00787 NM 1996 11 7 DL72L962435 1 19961101 A 3350 37067001 BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 514DA 21430 10657 L-2 AND AFT AIRSTAIR EMERGENCY LIGHTS INOP. REPLACED BATTERIES, CHECKS OK. 2 L 7 3 4F A3WE 1996110700788 19961107 00788 NM 1996 11 7 DL72S962437 1 19961102 A 2782 BRACKET BOEING 727 727232 1384082 NM NR 1 LE SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 407DA 21151 10657 FOUND ON F1 LETTER CK, NR 1 SLAT ACTUATOR ATTACH BRACKETS CRACKED INBD AND OUTBD SIDES. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1996110700789 19961107 00789 NM 1996 11 7 DL72K962438 1 19961029 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 344 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 491DA 21060 10657 TOP OF FLOORBEAM BS 344 RBL 6 TO LBL 36 CORRODED. INSTALLED REPAIR PER SRM 53-10-8. 2 L 7 3 4F A3WE 1996110700790 19961107 00790 NM 1996 11 7 DLM88962439 1 19961103 A 3110 4034234902 FLIGHT MODE ANN DOUG MD88 MD88 3023688 NM LT COCKPIT SHORTED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 986DL 53313 PUNGENT SMOKE IN COCKPIT ON TAXI-OUT, RETURNED TO GATE. FOUND CAPTS FMA CAUSING SMOKE IN COCKPIT. REPLACED CAPTS FMA, ALL INSTRUMENTS CK NORMAL. NO WIRING TROUBLE NOTED. FLIGHT MODE ANNUNCIATOR (DPN 229001002) (P/N 4032434-902) (S/N 911 12590). 2 L 7 2 4F RT A6WE 1996110700791 19961107 00791 NM 1996 11 7 DL72S962440 1 19961103 A 3350 S106 BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 419DA 21272 EMERGENCY LIGHT ABOVE L1 DOOR INOP. REPLACED BATTERIES. 2 L 7 3 4F A3WE 1996110700792 19961107 00792 1996 11 7 DLL10962442 4 19961103 A 3418 AOA SENSOR 0861CAG LKHEED 1011 10113851 5265010 WP LEFT BROKEN A DALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 27 712DA 790079 193C1088 10657 VIOLENT STICK SHAKER WAS EXPERIENCED IMMEDIATELY AFTER TAKEOFF, ACCOMPANIED BY ATS 1 AND 2 FAIL LIGHTS. FOUND AOA SENSO R BROKEN. REPLACED SAME, TESTS NORMAL. 2 L 7 3 4F A23WE 1996110700793 19961107 00793 NM 1996 11 7 DL757962444 1 19961103 A 2910 HYD LINE 271N6123127 BOEING 757 757232 1384965 NM RT MLG WW CRACKED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 673DL 25978 10657 LEFT SYSTEM HYDS STARTED GOING DOWN DURING FLIGHT. 2 L 7 2 4F RT A2NM 1996110700794 19961107 00794 NM 1996 11 7 DLM88962445 1 19961103 A 3350 61020 BATTERY DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 978DL 53259 EMERGENCY FLASHLIGHT FWD F/A LOW BATTERY. REPLACED BATTERY, OPS CKS NORMAL. 2 L 7 2 4F RT A6WE 1996110700795 19961107 00795 NM 1996 11 7 DL72L962446 1 19961103 A 3350 900542 BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 503DA 21305 OVERWING EMERGENCY LIGHT FAILS TO TEST. REPLACED BATTERY PACK RACK, CHECKS NORMAL. 2 L 7 3 4F A3WE 1996110700796 19961107 00796 WP 1996 11 7 DLL16962449 1 19961023 A 5730 1605415101 SKIN LKHEED 1011 10113853 5265020 WP WS 319 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 760DH 193Y1194 10657 SEVERAL CRACKS WERE FOUND IN THE UPPER WING SKIN TO UPPER CAP AND REAR SPAR WEB TO UPPER CAP FASTENER HOLES NEAR IWS 319 . THE CRACKS WERE REMOVED BY OVERSIZING THE FASTENER HOLES. REV B TO ER/A PROVIDES FAA APPROVAL. 2 L 7 3 4F A23WE 1996110700797 19961107 00797 WP 1996 11 7 DLL15962450 1 19961016 A 5712 1606372145 RIB LKHEED 1011 10113853 5265020 WP WS 555 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 753DA 193W1189 10657 THE LT WING IWS 555 RIB UPPER CAP AT STR 10 HAS A CRACK APPROX .875 INCH LENGTH. THE CRACK WAS STOP DRILLED, COLD WORKE D AND EDDY CURRENT INSPECTED. REV B PROVIDES FAA APPROVAL TO ER/A. 2 L 7 3 4F A23WE 1996110700798 19961107 00798 WP 1996 11 7 SCNA96343 1 19961022 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP L1 DOOR CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON SEAT TRACK UNDER L1 DOOR THRESHOLD. REMOVED CORRODED SECTION OF SEAT TRACK , FABRICATED AND INSTALLED NEW SECTION IN ACCORDANCE WITH ENGINEERING AUTHORIZATION. 2 L 7 3 4F A22WE 1996110700799 19961107 00799 WP 1996 11 7 SCNA96344 1 19961022 A 5320 BRACKET DOUG DC10 DC1010 3022110 WP G4 GALLEY CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON G4 GALLEY ATTACH BRACKET. FABRICATED AND INSTALLED A NEW ATTACH BRACKET IN ACCORDANCE WITH SRM 51-21-01. 2 L 7 3 4F A22WE 1996110700800 19961107 00800 WP 1996 11 7 SCNA96345 1 19961024 A 5320 BRACKET DOUG DC10 DC1010 3022110 WP BS 435 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND MOUNTING BRACKET CORRODED AT BS 435 CENTER TIE DOWN FITTING. REMOVED AND REPLACED MOUNT ING BRACKET IN ACCORDANCE WITH SRM 51-30-01. 2 L 7 3 4F A22WE 1996110700801 19961107 00801 WP 1996 11 7 SCNA96346 1 19961027 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1964 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND FLOOR SUPPORT DAMAGED AT BS 1964, RBL 48. REMOVED DAMAGED SUPPORT, FABRICATED AND INSTA LLED A NEW SUPPORT IN ACCORDANCE WITH SRM 53-00-01. 2 L 7 3 4F A22WE 1996110700802 19961107 00802 WP 1996 11 7 SCNA96347 1 19961101 A 5313 STRINGER DOUG DC10 DC1010 3022110 WP BS 1099-1119 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND STRINGER 48L CRACKED BETWEEN BS 1099 AND BS 1119. STOP DRILLED 1 INCH CRACK, FABRICATED AND INSTALLED A REPAIR DOUBLER IN ACCORDANCE WITH SRM 53-00-01. 2 L 7 3 4F A22WE 1996110700803 19961107 00803 1996 11 7 DHL96703004 2 19961030 A 7311 564909 OILCOOLER TUBE BOEING 727 72730C 1384009 NM NR 1 ENGINE GB PULLED LOOSE A DHLA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 703DH 19010 LOST OIL PRESSURE INDICATION ON NR 1 ENGINE FOLLOWED BY QUANTITY DECREASING. ENGINE WINDMILLED FOR 13 TO 14 MINUTES, NO PRESSURE INDICATED. FOUND OIL COOLER IN TUBE ASSY PULLED OUT OF GEARBOX. INSTALLED HELICOILS IN GEARBOX AND INSTALLED LINE, NO LEAKS NOTED. 2 L 7 3 4F A3WE 1996110700804 19961107 00804 NM 1996 11 7 DHL96724007 1 19961101 A 2781 SWITCH BOEING 727 727228 NM NR 1 LE FLAP FAILED A DHLA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 724DH 19862 DURING ROTATION, FWD L/E FLAP AMBER LIGHT ILLUMINATED. CONFIRMED WITH S/O L/E FLAP PANEL. NR 1 L/E FLAP INTRANSIT LIGH T WAS ON AND LIGHT REMAINED ON DURING ALL FLAP SETTINGS. REPLACED NR 1 L/E FLAP SWITCH PER MM 27-80. 2 L 7 3 4F A3WE 1996110700805 19961107 00805 WP 1996 11 7 RRXA96127 1 19960824 A 5311 1616373 FRAME DOUG DC8 DC873F 302199F WP BS 1040 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND FRAME CAP CORRODED PAST LIMITATIONS IAW DC-8 SRM, AT Y=1040 BETWEEN LONGERON 35 LEFT A ND LONGERON 36. REPAIRED FRAME CAP IAW DER APPROVED ENGINEERING SKETCH B21-R08, TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996110700806 19961107 00806 WP 1996 11 7 RRXA96129 1 19960825 A 5311 2705384 FRAME DOUG DC8 DC873F 302199F WP BS 1140 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE UNDER NUTPLATES ON FRAME PAST LIMITATIONS IAW DC-8 SRM, AT Y=1140 BET WEEN LONGERON 33 LEFT AND LONGERON 33 RIGHT. INSTALLED REPAIR IAW DER APPROVED ENGINEERING SKETCH, TREATED AREA IAW DC- 8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996110700807 19961107 00807 WP 1996 11 7 RRXA96128 1 19960824 A 5311 2641520 FRAME DOUG DC8 DC873F 302199F WP BS 1280 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND FRAME CORRODED PAST LIMITATIONS IAW DC-8 SRM, AT Y=1280 BETWEEN LONGERON 27 RIGHT AND LONGERON 29 RIGHT. REPAIRED FRAME BY INSTALLING REPAIR IAW DER APPROVED ENGINEERING SKETCH B21-R07, TREATED AREA IAW DC -8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996110700808 19961107 00808 WP 1996 11 7 RRXA96130 1 19960822 A 5315 2759472 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1360 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND EXFOLIATION CORROSION ON RIGHT SIDE OF VERTICAL FLOORBEAM PAST LIMITATIONS IAW DC-8 SR M, AT Y=1360 AND X-47. INSTALLED SPLICE REPAIR TO FLOORBEAM WEB, IAW DER APPROVED ENGINEERING SKETCH, TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996110700809 19961107 00809 WP 1996 11 7 RRXA96131 1 19960822 A 5315 2759472 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1300 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND EXFOLIATION DAMAGE ON FLOORBEAM PAST LIMITATION IAW DC-8 SRM, AT Y=1300 BETWEEN X-32 A ND X-39. INSTALLED REPAIR DOUBLER AND FILLER IAW DER APPROVED ENGINEERING SKETCH B21-R21, TREATED AREA IAW DC-8 SRM 51- 1-8. 2 L 7 4 4F RT 4A25 1996110700810 19961107 00810 WP 1996 11 7 RRXA96132 1 19960823 A 5313 2772345 LONGERON DOUG DC8 DC873F 302199F WP BS 1640 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND EXFOLIATION CORROSION DAMAGE TO LONGERON 21R PAST LIMITATIONS IAW DC-8 SRM, AT Y=1640. INSTALLED REPAIR IAW DER APPROVED ENGINEERING SKETCH B21-11, TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996110700811 19961107 00811 WP 1996 11 7 RRXA96133 1 19960823 A 5315 2759472 FLOORBEAM DOUG DC8 DC873F 302199F WP BS1580 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND EXFOLIATION CORROSION DAMAGE TO FLOORBEAM PAST LIMITATIONS IAW DC-8 SRM, AT Y=1580 AND X-50. INSTALLED REPAIR IAW DER APPROVED ENGINEERING SKETCH B21-R10, TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996110700812 19961107 00812 WP 1996 11 7 RRXA96134 1 19961014 A 5330 SKIN DOUG DC8 DC8F54 3021926 WP BS 330 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 992CF 45884 DURING A DROP IN MAINTENANCE INSPECTION, FOUND CORROSION DAMAGE TO LAV SERVICE PORT INNER SKIN DOUBLER PAST LIMITATIONS IAW DC-8 SRM, AT Y=330 AND LONGERON 25 RIGHT. INSTALLED REPAIR DOUBLER IAW DER APPROVED ENGINEERING SKETCH B46-R01, TRE ATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1996110700813 19961107 00813 WP 1996 11 7 RRXA96135 1 19960823 A 5315 2759472 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1540 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FLOORBEAM PAST LIMITATIONS IAW DC-8 SRM, AT Y=1540 AND X=+58. INS TALLED REPAIR IAW DER APPROVED ENGINEERING SKETCH B21-R14, TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996110700814 19961107 00814 WP 1996 11 7 RRXA96137 1 19960826 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 640 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO SKIN PAST LIMITATIONS IAW DC-8 SRM, AT Y=640 BETWEEN LONGERON 30 R IGHT AND LONGERON 32 RIGHT. INSTALLED REPAIR IAW DER APPROVED ENGINEERING SKETCH B21-R06, TREATED AREA IAW DC-8 SRM 51- 1-8. 2 L 7 4 4F RT 4A25 1996110700815 19961107 00815 WP 1996 11 7 RRXA96138 1 19960826 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 678 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND SKIN CORRODED PAST LIMITATIONS IAW DC-8 SRM, AT Y=678 TO Y=680 AND BETWEEN LONGERON 30 RIGHT TO 31 RIGHT. INSTALLED REPAIR IAW DER APPROVED ENGINEERING SKETCH B21-R20, TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996110700816 19961107 00816 WP 1996 11 7 RRXA96139 1 19960826 A 5320 WEB DOUG DC8 DC873F 302199F WP BS 275 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND TORQUE BOX WEB CORRODED PAST LIMITATIONS IAW DC-8 SRM, AT Y=275 TO Y=280 AND LONGERON 27 RIGHT. INSTALLED REPAIR IAW DER APPROVED ENGINEERING SKETCH B21-R24, TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996110700817 19961107 00817 WP 1996 11 7 RRXA96140 1 19960824 A 5311 2537716 FRAME DOUG DC8 DC873F 302199F WP BS1120 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND FRAME CORRODED PAST LIMITATIONS IAW DC-8 SRM, AT Y=1120 AND LONGERON 36. INSTALLED RE PAIR IAW DER APPROVED ENGINEERING SKETCH B21-R05, TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996110700818 19961107 00818 WP 1996 11 7 RRXA96141 1 19960824 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 385.25 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND 2 RIGHT WING LEADING EDGE MOUNT SCREW HOLES CRACKED, PAST LIMITATIONS IAW DC-8 SRM, AT XFS 385.250. INSTALLED FILLER AND DOUBLER IAW DER APPROVED ENGINEERING SKETCH B21-R18, TREATED AREA IAW DC-8 SRM 51-1- 8. 2 L 7 4 4F RT 4A25 1996110700819 19961107 00819 WP 1996 11 7 RRXA96142 1 19960823 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 520.168 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND LEFT WING CRACKED IN SKIN PAST LIMITATIONS IAW DC-8 SRM, AT XS 520.168. INSTALLED DOU BLER REPAIR IAW DER APPROVED ENGINEERING SKETCH B21-R23, TREATED AREA IAW DC-8 SRM. 2 L 7 4 4F RT 4A25 1996110700820 19961107 00820 WP 1996 11 7 RRXA96143 1 19960824 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 485/603 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND RIGHT WING LEADING EDGE HAD 5 CRACKS AT MOUNT SCREW HOLES PAST LIMITATION IAW DC-8 SRM , AT XFS 485 TO XFS 603. INSTALLED DOUBLER REPAIR IAW DER APPROVED ENGINEERING SKETCH B21-R17, TREATED AREA IAW DC-8 SR M 51-1-8. 2 L 7 4 4F RT 4A25 1996110700821 19961107 00821 WP 1996 11 7 RRXA96144 1 19960824 A 5311 2750825 FRAME DOUG DC8 DC873F 302199F WP BS 1100 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND FRAME CORRODED PAST LIMITATION IAW DC-8 SRM, AT Y=1100 AND LONGERON 36. INSTALLED REP AIR IAW DER APPROVED ENGINEERING SKETCH B21-R02, TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996110700822 19961107 00822 WP 1996 11 7 RRXA96145 1 19960822 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 300 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND LEFT WING LEADING EDGE SKIN CRACKED PAST LIMITATIONS IAW DC-8 SRM, AT XFS 300. INSTAL LED REPAIR IAW DER APPROVED ENGINEERING SKETCH B21-R01, TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996110700823 19961107 00823 WP 1996 11 7 RRXA96146 1 19960825 A 5311 2750825 FRAME DOUG DC8 DC873F 302199F WP BS 1020 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND FRAME CORRODED PAST LIMITATIONS IAW DC-8 SRM, AT Y=1020 AND BETWEEN LONGERON 35 LEFT T O 35 RIGHT. INSTALLED REPAIR IAW DER APPROVED ENGINEERING SKETCH B21-R09. 2 L 7 4 4F RT 4A25 1996110700824 19961107 00824 WP 1996 11 7 RRXA96147 1 19960827 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1580 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND INTERNAL DOUBLER CORRODED PAST LIMITATIONS IAW DC-8 SRM, AT Y=1580 BETWEEN LONGERON 31 RIGHT TO LONGERON 31 LEFT. SKIN HAD TO CUT AND REMOVED FOR ACCESS AT Y=1580 TO Y=1690 FROM LONGERON 31 RIGHT TO LONGER ON 31 LEFT. REMOVED DAMAGE SECTION OF INTERNAL DOUBLER, FABRICATED AND INSTALLED FILLERS AND REPAIRED DOUBLERS IAW DER APPROVED ENGINEERING SKETCHES B21-R12 AND B21-R13. FABRICATED AND INSTALLED SKIN SPLICE DOUBLERS AT Y=1580 IAW ENGINEER ING SKETCH B21-R03, TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996110700825 19961107 00825 WP 1996 11 7 RRXA96148 1 19960824 A 5320 SCUFF PLATE DOUG DC8 DC873F 302199F WP BS 200-240 DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CARGO DOOR SCUFF PLATING DAMAGED PAST LIMITATIONS IAW DC-8 SRM, AT Y=200 TO Y=240. RE MOVED SCUFF PLATE, FABRICATED NEW SCUFF PLATE AND INSTALLED IAW DC-8 SRM 51-1-20 AND RFTS 96-438. 2 L 7 4 4F RT 4A25 1996110700826 19961107 00826 WP 1996 11 7 RRXA96149 1 19960822 A 5315 2641520 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1360 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND EXFOLIATION ON FLOORBEAM AND WEB TORN PAST LIMITATIONS IAW DC-8 SRM, AT Y=1360. REPAI RED FLOORBEAM WEB BY REPAIR ANGLES AND WEB SPLICE IAW DER APPROVED ENGINEERING SKETCH B21-R22. REMOVED AND TREATED CORR ODED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996110700827 19961107 00827 WP 1996 11 7 RRXA96150 1 19960824 A 5311 2537716 FRAME DOUG DC8 DC873F 302199F WP BS 1120 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND FRAME CORRODED AND PAST LIMITATIONS IAW DC-8 SRM, AT Y=1120 AND LONGERN 36. FABRICATE D AND INSTALLED FILLER AND DOUBLER IAW DER APPROVED ENGINEERING SKETCH B21-R25, TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996110700828 19961107 00828 WP 1996 11 7 RRXA96152 1 19960806 A 5312 BULKHEAD FILLET DOUG DC8 DC873F 302199F WP BS 965-990 GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 961R 46133 DURING A MAINTENANCE VISIT, FOUND FILLET BULKHEAD PANEL LEFT SIDE DAMAGED WEB PAST LIMITATIONS IAW DC-8 SRM, AT Y=965 TO Y=990. FABRICATED NEW WEB AND DOUBLER, INSTALLED IAW REO-02128, TREATED REPAIR AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996110700829 19961107 00829 WP 1996 11 7 RRXA96153 1 19960807 A 5350 3654436402 FILLET DOUG DC8 DC873F 302199F WP CENTER WING DELAMINATED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 961R 46133 DURING A MAINTENANCE VISIT, FOUND CENTER WING FILLET PANEL DELAMINATED, DAMAGE PAST LIMITATION IAW DC-8 SRM, AT PANEL NR 162R. REPAIRED BY FABRICATING NEW FILLET PANEL AND INSTALLING IAW REO-02134 REV IR AND DOUGLAS DRAWING 566752 APPENDIX A, TREATED AREA IAW DC-8 SRM. 2 L 7 4 4F RT 4A25 1996110700830 19961107 00830 WP 1996 11 7 RRXA96155 1 19960806 A 5350 162W FILLET DOUG DC8 DC873F 302199F WP BS 1078 DELAMINATED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 961R 46133 DURING A MAINTENANCE VISIT, FOUND FILLET PANEL NR 162-W DELAMINATED, DAMAGE PAST LIMITATIONS IAW DC-8, AT Y=1058 TO Y=10 78 LEFT SIDE. REPAIRED BY FABRICATING NEW FILLET PANEL IAW REO-02133 REV IR AND DOUGLAS DRAWING 5656352, TREATED AREA I AW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996110700831 19961107 00831 WP 1996 11 7 RRXA96156 1 19960805 A 5730 PLATING DOUG DC8 DC873F 302199F WP WS 450 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 961R 46133 DURING A MAINTENANCE VISIT, FOUND RIGHT WING LOWER SKIN CRACKED PAST LIMITATIONS IAW DC-8 SRM, AT XRS 450. REPAIRED IAW REO-02129, REMOVED DAMAGE, FABRICATED DOUBLER IAW DOUGLAS DRAWING SRO8570013, TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996110700832 19961107 00832 WP 1996 11 7 RRXA96158 1 19960807 A 5320 7075 INTERCOSTAL DOUG DC8 DC873F 302199F WP BS 1000 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 961R 46133 DURING A MAINTENANCE VISIT, FOUND INTERCOSTAL CORRODED PAST LIMITATIONS IAW DC-8 SRM, AT LONGERON 35 LEFT AND Y=1000 TO Y=1060. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW DAC DWG-5779936, TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996110700833 19961107 00833 WP 1996 11 7 RRXA96159 1 19960813 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS1220 SEPARATED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 961R 46133 DURING A MAINTENANCE VISIT, FOUND AFT LOWER FLOOR PANEL MODIFICATION SEPARATING FROM GILL BOARD ON BOTH SIDES OF PANEL, AT Y=1220 TO Y=1320. REPAIRED PANEL BY RESEALING PANEL TO GILL BOARD IAW DAC-DRW 2277-006 REV F, TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996110700834 19961107 00834 WP 1996 11 7 RRXA96160 1 19960807 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS1220 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 961R 46133 DURING A MAINTENANCE VISIT, FOUND FLOOR SUPPORT ANGLE CORRODED PAST LIMITATIONS IAW DC-8 SRM, AT Y=1220 TO Y=1140 AND BE TWEEN LONGERONS 34 AND 35 RIGHT. FABRICATED AND INSTALLED NEW FLOOR SUPPORT ANGLE IAW DC-8 SRM 51-1-4 AND 51-1-24, TREA TED AREA IAW SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996110700835 19961107 00835 WP 1996 11 7 RRXA96161 1 19960807 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1260 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 961R 46133 DURING A MAINTENANCE VISIT, FOUND FRAME CORRODED PAST LIMITATIONS IAW DC-8 SRM 53-2-0, AT Y=1260 AND LONGERON 36. FABRI CATED REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-2-0 AND 51-3-0, TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1996110700836 19961107 00836 WP 1996 11 7 RRXA96162 1 19961103 A 7931 D51P54101 OIL PRESS TUBE DOUG DC8 DC873F 302199F WP NR 3 ENGINE LEAKING A RRXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 15 870TV 46086 AT FL 330, NR 3 ENG LOW OIL PRESSURE LIGHT CAME ON. OIL PRESSURE DROPPED TO 5 PSI AND QUANTITY WENT TO ZERO. ENGINE SH UTDOWN, DIVERTED TO KBOS. MAINTENANCE REPLACED THE LINE FROM THE OIL PRESSURE SWITCH. OPERATIONAL CHECK OF THE OIL SYS TEM WAS GOOD. 2 L 7 4 4F RT 4A25 1996110700838 19961107 00838 1996 11 7 VNAA9610006 4 19961017 A 3442 7008470922 RT UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FWD FUSELAGE FAILED A VNAA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 07 427JS 1925 1925 3039 RADAR FAILED IN FLIGHT, DIVERTED TO CAK FOR REPAIRS. MAINTENANCE REMOVED AND REPLACED THE RADAR UNIT, OPERATIONAL CHECK GOOD. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996110700839 19961107 00839 NE 1996 11 7 VNAA9610007 3 19961018 A 6110 E62127 PROPELLER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT ENGINE PITTED A VNAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 439JS 1891 189 3057 HL210 AIRCRAFT STRUCK BY LIGHTNING DURING CLIMB. AIRCRAFT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. NO INSTRUMENT ATION LOSS OCCURED. UPON INSPECTION, MAINTENANCE DETERMINED THAT THE RT PROPELLER SUSTAINED PITTING ON A BLADE. PROPEL LER WAS REMOVED AND REPLACED, OPERATIONAL CHECK GOOD. AIRCRAFT APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996110700840 19961107 00840 NM 1996 11 7 VNAA9611001 1 19961104 A 3260 870004 PSEU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE E/E COMPT FAILED A VNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 460PS 740 3061 AFTER TAKEOFF, DURING GEAR RETRACTION. TAKEOFF CONFIGURATION HORN AND GEAR UNSAFE INDICATIONS CAME UP ALONG WITH ERRATI C MESSAGES. DECLARED EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PSEU, OPERATI ONAL CHECKED GOOD AND AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. PART TOTAL CYCLES, 629. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996111300001 19961113 00001 EU 1996 11 13 CA960311017 1 19960228 A 3260 1ENN14 SWITCH BRAERO 748 HS7482A 4231001 EU LH MLG DWN LOCK FROZEN W L ABORTED APPROACH O P OTHER NO WARNING INDICATION AP APPROACH 1 CA (CAN)ON APPROACH WHEN GEAR SELECTED DID NOT GET A GEAR IN TRANSIT LIGHT OR A GEAR DOWN AND LOCKED LIGHT FOR THE PORT MAI N LANDING GEAR. TWO MORE SELECTIONS NO SUCCESS. AIRCRAFT RETURNED, EMERGENCY GEAR LOWE RING CARRIED OUT. LH MAIN LANDING GEAR DOWN LOCK MICROSWITCH REPLACED. 2 L 7 2 3T A24EU 1996111300002 19961113 00002 NM 1996 11 13 UPS96221433 1 19961014 A 5753 RIB BOEING 727 72722C 138400F NM RT TE MID FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE: C. RT INBD MID-FLAP CRACK ON INTERSPAR RIB AT WBL 226. REPAIR CARRIED OUT IAW SRM 57-50-4 FIG 6. 2 L 7 3 4F A3WE 1996111300003 19961113 00003 NM 1996 11 13 UPS96221434 1 19961014 A 5753 RIB BOEING 727 72722C 138400F NM RT TE MID FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE: C. RT INBD MID-FLAP CRACK ON INTER SPAR RIB AT STA 230 WBL. REPAIRED PER SRM 57-50-4 FIG 6. 2 L 7 3 4F A3WE 1996111300004 19961113 00004 NM 1996 11 13 UPS96221435 1 19961014 A 5753 RIB BOEING 727 72722C 138400F NM RT TE MID FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE: C. RT INBD MID FLAP CRACKED IN INTER SPAR RIB AT STA 154. REPAIRED PER SRM 57-50-4 FIG 6. 2 L 7 3 4F A3WE 1996111300005 19961113 00005 NM 1996 11 13 UPS96221436 1 19961014 A 5753 RIB BOEING 727 72722C 138400F NM RT TE MID FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE: C. RT INBD MID FLAP CRACKED AT STA WBL 150. REPAIRED PER SRM 57-50-4 FIG 6. 2 L 7 3 4F A3WE 1996111300006 19961113 00006 NM 1996 11 13 CKSA96183 1 19961018 A 5400 112U502G2 SHEAR TIE BOEING 747 747132 1384882 NM WS 670 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 KOSC - DURING C-2 CHECK INSPECTION FOUND: FORWARD NR 3 PYLON SUPPORT STRUT SHEAR TIE CRACKED AT WS 670 IN NR 3 MAIN FUE L TANK 11 INCHES AFT OF FRONT SPAR WEB. REPAIRED IAW SB 747-57-2273 FIGURES 10 AND 11. AD NR 94-15-18 SID TASK CARD NR W-22C. TASK CARD NR 85659. 2 L 7 4 4F A20WE 1996111300008 19961113 00008 NM 1996 11 13 DHL9672213C 1 19960930 A 5753 651920813 SPACER BOEING 727 727228 NM NR 2 FLAP TRACK CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 722DH 19861 AT C-CHECK, NR 2 FLAP TRACK SPACER BLOCK REQUIRES REPAIR. REMOVED AND REPLACED SPACER BLOCK PER S/B 57-125. 2 L 7 3 4F A3WE 1996111300009 19961113 00009 NE 1996 11 13 CA960313006 3 19960306 A 6110 PROPELLER DHAV DHC2 DHC2EVANS 2801832 EA PWA R985 R985AN14B 52008 NE HAMSTD 2D 2D30 NE BLADE PITCH SETTING W K NONE O OTHER IN INSP/MAINT 1 CA 416280 T21871 (CAN)SETTING PITCH ANGLE AT 10.5 DEGREES AS STATED IN TYPE CERTIFICATE DOES NOT ALLOW MAXIMUM RPM WHILE AIRCRAFT STATIC. 1 H 7 1 3O 3 R A806 5E1 5 C P206 1996111300012 19961113 00012 NM 1996 11 13 DLM88962344 1 19961018 A 3510 PBE 4566M37B042N DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE COCKPIT IND POPPED A DALA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 27 963DL E9651837 49982 723951 COCKPIT PBE VISUAL SERVICE IND POPPED. REPLACED MASK, OK FOR SERVICE. 2 L 7 2 4F 4 F RT A6WE E9NE 1996111300013 19961113 00013 NE 1996 11 13 CA960320004 2 19960223 A 7321 3244851 FUEL CONTRL BENDIX 3244851 CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE NR 1 ENG MALFUNCTION W K NONE R PARTIAL RPM/PWR LOSS DE DESCENT 1 CA 1333 1333 B29168 PCE108160 (CAN)ON DESCENT AFTER EXTENDED CRUISE AT 43K, WHEN INCREASING POWER FROM FLIGHT IDLE AT AROUND 20K, #1 ENGINE FAILED TO RESPOND UNTIL A MUCH LOWER ALTITUDE AND WARMER TEMPERATURE REACHED. MINIMUM FUEL FLOWADJUSTED AND FLOWN OK. THREE MONTHS LATER SAME MALFUNCTION OCCURRED. FUEL CONTROL UNIT CHANGED. 2 L 7 2 4F 4 F RT A22CE E25EA 1996111300014 19961113 00014 GL 1996 11 13 CA960320014 2 19960312 A 7310 ENGINE BELL 206 206L 1181522 SW ALLSN 250C 250C20R2 GL 2ND STG NOZZLE DIAPHRAGM CRACK W A B UNSCHED LANDING EMER. DESCENT R PARTIAL RPM/PWR LOSS CR CRUISE 1 CA 2356 CAE295348 (CAN)PILOT ENTERED AUTOROTATION AFTER ENGINE LOST POWER. ENGINE WAS RUNNING AFTER LANDING BUT WOULD NOT PRODUCE POWER. S UBSEQUENT INVESTIGATION REVEALED 2ND STAGE NOZZLE DIAPHRAGM CRACKED. 1 G 7 1 3U 3 U H2SW E4CE 1996111400050 19961114 00050 NM 1996 11 14 CALA9601553 1 19961031 A 5312 BULKHEAD SKIN BOEING 737 737130 1384435 NM BS 178 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 44214 19031 INSPECTION FOUND A .50 INCH CRACK IN STA 178 BULKHEAD SKIN AT WL 233.5 AND A 6 INCH CRACK WAS FOUND AT HORIZONTAL STIFFE NER AT WL 218, RT SIDE. THE CRACKED AREAS WERE CUT OUT. FILLERS AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-1 0-11 AND SRM 51-10-2. 2 L 7 2 4F A16WE 1996111400051 19961114 00051 NM 1996 11 14 CALA9601554 1 19961031 A 5312 BULKHEAD SKIN BOEING 737 737130 1384435 NM BS 178 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 44214 19031 INSPECTION FOUND A 6.5 INCH CRACK IN STA 178 BULKHEAD SKIN PANEL ALONG HORIZONTAL STIFFENER AT WL 218, ON LT SIDE. THE CRACKED AREA WAS CUT OUT. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-11 AND SRM 51-10-2. 2 L 7 2 4F A16WE 1996111400052 19961114 00052 NM 1996 11 14 CALA9601555 1 19961031 A 5330 SKIN BOEING 737 737130 1384435 NM C2 DR CUTOUT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 44214 19031 INSPECTION FOUND A 1 INCH CRACK IN INBOARD SKIN AT LOWER AFT CORNER OF C-2 DOOR CUTOUT. THE CRACKED SECTION OF SKIN WAS REMOVED. A DOUBLER AND TRIPLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2, AND ENGINEERING ORDER RE O-02348. 2 L 7 2 4F A16WE 1996111400053 19961114 00053 NM 1996 11 14 CALA9601556 1 19961030 A 5311 FRAME BOEING 737 737130 1384435 NM BS 520 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 44214 19031 INSPECTION FOUND A 1 INCH CRACK THROUGH NUTPLATE HOLE AT LOWER AFT CORNER OF LT STA 520 WING TO BODY ATTACH FRAME. THE FASTENERS AND EXISTING ANGLE WERE REMOVED. AN ATTACH ANGLE, REPAIR ANGLE, AND CLIPS WERE FABRICATED AND INSTALLED IAW E CRA 5350-01227, SRM 51-10-2, AND SRM 51-30-2. 2 L 7 2 4F A16WE 1996111400054 19961114 00054 WP 1996 11 14 CALA9601557 1 19961104 A 4990 3812761M APU DOUG DC9 DC982 3022082 WP AFT FUSELAGE LEAKING OIL A CALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 478AC 18434 3862 48063 SMOKE WAS REPORTED IN THE AFT AND FORWARD SECTION OF CABIN DURING INITIAL CLIMB OUT OF IAH. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE APU INLET AND BLEED OIL SOAKED. THE APU WAS REMOVED AND R EPLACED. THE APU INLET BOX WAS ALSO DISASSEMBLED AND CLEANED. THE APU INLET DOOR ACTUATOR WAS ALSO REPLACED. A BURN OUT PROCEDURE WAS PERFORMED IAW MM 21-20-02. BOTH WATER SEPARATOR SOCKS WERE REPLACED. BOTH ENGINES AND THE APU WERE R UN WITH LEFT AND RIGHT PACKS OPERATING AND NO SMOKE WAS PRODUCED. PART TOTAL CYCLES, 10,443. 2 L 7 2 4F A6WE 1996111400055 19961114 00055 WP 1996 11 14 CALA9601558 1 19961104 A 2897 BXS700816 WIRE HARNESS DOUG DC9 DC982 3022082 WP WS 70 CHAFED A A CALA O OTHER O OTHER AP APPROACH 1 SW 09 77827 49487 THE AFT LEFT FUEL TANK BOOST PUMP AND FORWARD LEFT FUEL TANK BOOST PUMP CIRCUIT BREAKERS TRIPPED ON FINAL APPROACH TO MI A. THE AFT LEFT FUEL BOOST PUMP CIRCUIT BREAKER COULD NOT BE RESET. THE FORWARD LEFT FUEL TANK BOOST PUMP CIRCUIT BREAKE R WAS RESET, BUT THE LOW FUEL PRESSURE ANNUNCIATOR WAS STILL ILLUMINATED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTE NANCE FOUND WIRE BUNDLE CHAFED AGAINST SLAT ACCESS PANEL NUTPLATE CHANNEL AT LEFT WING STA 70 BETWEEN SLATS ZERO AND ONE . THE WIRING WAS REPAIRED USING RAYCHEM SPLICES IAW STANDARD PRACTICES 20-10-3. ALL ASSOCIATED SYSTEMS CHECKED GOOD. 2 L 7 2 4F A6WE 1996111400056 19961114 00056 NM 1996 11 14 CALA9601559 1 19961103 A 2760 BACC2A3A01853FG CONTROL CABLE BOEING 737 7373T0 1384582 NM FLT SPOILER BROKEN A A CALA O OTHER F FLT CONT AFFECTED DE DESCENT 1 SW 09 14320 23371 FIVE UNITS OF RUDDER LEFT RUDDER TRIM WAS REQUIRED TO COUNTER ADVERSE ROLL TO RIGHT WITH SPEED BRAKES AT FLIGHT DETENT W HILE ON DESCENT INTO LAX. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 3 FLIGHT SPOILER CABLE NUMBER WSA2-3 BROKEN. THE CABLE WAS REPLACED AND THE FLIGHT SPOILERS WERE RIGGED IAW MM 27-61-00. OPERATIONAL CHECKS WERE GO OD. 2 L 7 2 4F RT A16WE 1996111400057 19961114 00057 NM 1996 11 14 CALA9601560 1 19961101 A 5320 SHEAR WEB BOEING 737 737130 1384435 NM BS 664 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 44214 19031 INSPECTION FOUND A 1 INCH CRACK IN INBOARD RADIUS OF SHEAR WEB AT S18A, LT B.S. 664. NEW REPAIR ANGLES WERE INSTALLED I AW BOEING DRAWING NR 65C29228 AND SRM 51-30-2. 2 L 7 2 4F A16WE 1996111400058 19961114 00058 NM 1996 11 14 CALA9601561 1 19961101 A 5312 BULKHEAD SKIN BOEING 737 737130 1384435 NM BS 178 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 44214 19031 INSPECTION FOUND A 6 INCH AND 7 INCH CRACK IN SKIN AT B.S. 178 BULKHEAD. THE CRACKED AREA WAS CUT OUT. DOUBLER AND FILL ERS WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND SRM 53-10-11. 2 L 7 2 4F A16WE 1996111400059 19961114 00059 WP 1996 11 14 CALA9601562 1 19961031 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 200 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12507 47788 INSPECTION FOUND A .8750 INCH CRACK IN SKIN COMING FROM FASTENER HOLE AT STA 200, FOUR INCHES ABOVE L21L. A .1250 INCH CRACK WAS ALSO FOUND IN SKIN AT STA 200, APPROXIMATELY FOUR INCHES ABOVE L20L. THE CRACKS WERE STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5330-02458 AND SRM 53-05, FIGURE 57. 2 L 7 2 4F A6WE 1996111400060 19961114 00060 NE 1996 11 14 CALA9601563 2 19961107 A 7200 805372 VANE CLUSTER DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 1 ENGINE FAILED A CALA A E UNSCHED LANDING ENGINE SHUTDOWN E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SW 09 10834 24462 15155 49494 717436 THE NR 1 ENGINE GAVE OFF A LOUD POP AND ART FIRED DURING CLIMBOUT AT 1,000 FEET. THE ENGINE EPR WAS AT 1.12 AND VIBRATI ON WAS STEADY. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTEN ANCE REMOVED AND REPLACED THE NR 1 ENGINE. *S/D* TEARDOWN REVEALED FAILURE OF T-2 VANE CLUSTER. 2 L 7 2 4F 4 F A6WE E9NE 1996111400061 19961114 00061 WP 1996 11 14 CALA9601564 1 19961106 A 2450 5D000950 BREAKER DOUG DC9 DC982 3022082 WP E/E COMPT TRIPPED A CALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 09 16804 49246 THE A AND B CIRCUIT BREAKER FOR CENTER AFT FUEL BOOST PUMP, FORWARD LEFT FUEL PUMP, AND RECIRCULATING FAN ALL TRIPPED SH ORTLY AFTER TAKEOFF. THE CIRCUIT BREAKERS WERE RESET, BUT TRIPPED AGAIN. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LAN DED WITHOUT INCIDENT. THE CIRCUIT BREAKERS WERE RESET. THE ENGINES WERE RUN AND OPERATION OF BOOST PUMP AND RECIRCULATIN G FAN CHECKED GOOD. THE RIGHT ENGINE GENERATOR CONNECTOR WAS REMOVED FROM FIREWALL AND THE PINS AND RECEPTACLE WERE INS PECTED WITH NO DEFECTS NOTED. MAINTENANCE FOUND NO DISCREPANCIES AND COULD NOT DUPLICATE THE FAILURE. THE B1-740 CIRCUI T BREAKER IN ELECTRICAL EQUIPMENT COMPARTMENT WAS REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. 2 L 7 2 4F A6WE 1996111400062 19961114 00062 WP 1996 11 14 CALA9601565 1 19961005 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 258 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14814 49112 INSPECTION FOUND A 1.5 INCH CRACK AND DENT IN FUSELAGE SKIN AT STA 258 JUST BELOW STRINGER 21R. THE DENT WAS REWORKED A ND THE CRACKED AREA WAS CUT OUT. A FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-04, FIGURE 38, SHEET 21, VIEW I. 2 L 7 2 4F A6WE 1996111400063 19961114 00063 WP 1996 11 14 CALA9601566 1 19961008 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 200-204 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14814 49112 INSPECTION FOUND FLOORBOARD SUPPORT CORRODED AT STA 200-204, LBL 56. THE FLOORBOARD SUPPORT WAS REMOVED AND A REPLACEMEN T PART WAS FABRICATED AND INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1996111400064 19961114 00064 WP 1996 11 14 CALA9601567 1 19961007 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14814 49112 INSPECTION FOUND FLOORBOARD SUPPORT CORRODED AT STA 200, LBL 7 TO RBL 5. THE CORRODED SECTION WAS REMOVED. A NEW SUPPO RT WAS FABRICATED AND INSTALLED IAW SRM 53-14-1 AND SRM 51-30-2. 2 L 7 2 4F A6WE 1996111400065 19961114 00065 WP 1996 11 14 CALA9601568 1 19961007 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14814 49112 INSPECTION FOUND FLOORBOARD SUPPORT CORRODED AT STA 200, RBL 10 TO RBL 44. THE FLOOR SUPPORT WAS REMOVED. A NEW SUPPOR T WAS FABRICATED AND INSTALLED IAW SRM 51-10-3. 2 L 7 2 4F A6WE 1996111400066 19961114 00066 WP 1996 11 14 CALA9601569 1 19961007 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 168 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14814 49112 INSPECTION FOUND FLOORBOARD SUPPORT CORRODED AT STA 168 FROM RBL 10 TO RBL 43. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-10-3 AND SRM 51-10-2. 2 L 7 2 4F A6WE 1996111400067 19961114 00067 WP 1996 11 14 CALA9601570 1 19961008 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 160-200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14814 49112 INSPECTION FOUND FLOORBOARD SUPPORT CORRODED FROM STA 160 TO 200, LBL 44. THE FLOOR SUPPORT WAS REMOVED. A REPLACEMENT PART WAS FABRICATED AND INSTALLED IAW SRM 53-14-1 AND SRM 51-30-2. 2 L 7 2 4F A6WE 1996111400068 19961114 00068 WP 1996 11 14 CALA9601571 1 19961008 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 150-200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14814 49112 INSPECTION FOUND FLOORBOARD SUPPORT CORRODED FROM STA 150-200, LBL 7. THE FLOOR SUPPORT WAS REMOVED. A REPLACEMENT PAR T WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 53-14-1. 2 L 7 2 4F A6WE 1996111400069 19961114 00069 WP 1996 11 14 CALA9601572 1 19961008 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 150-200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14814 49112 INSPECTION FOUND FLOORBOARD SUPPORT CORRODED FROM STA 150 TO 200, RBL 7. THE FLOOR SUPPORT WAS REMOVED. A REPLACEMENT PART WAS FABRICATED AND INSTALLED IAW SRM 53-14-1 AND 51-30-1. 2 L 7 2 4F A6WE 1996111400070 19961114 00070 WP 1996 11 14 CALA9601573 1 19961008 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 218-238 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14814 49112 INSPECTION FOUND FLOORBOARD SUPPORT CORRODED FROM STA 218 TO 238, LBL 14. THE FLOOR SUPPORT WAS REMOVED. A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 53-18-1, FIGURE 11. 2 L 7 2 4F A6WE 1996111400071 19961114 00071 WP 1996 11 14 CALA9601574 1 19961017 A 5320 THRESHOLD DOUG DC9 DC982 3022082 WP LAV SERVICE DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14814 49112 INSPECTION FOUND LT AFT SERVICE DOOR THRESHOLD WEB AT AFT LOWER CORNER CORRODED. THE CORRODED WEB SECTION WAS REMOVED. A NEW WEB REPAIR SECTION WAS FABRICATED AND INSTALLED IAW SRM 51-10-03 AND 53-01, FIGURE 2. 2 L 7 2 4F A6WE 1996111400072 19961114 00072 WP 1996 11 14 CALA9601575 1 19961007 A 5280 BRACE DOUG DC9 DC982 3022082 WP LT MLG DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14814 49112 INSPECTION FOUND A 1.5 INCH CRACK IN LT MLG DOOR CENTER BRACE. THE CENTER BRACE WAS REMOVED IAW SRM 51-30-1. A REPAIR WAS INSTALLED AND THE BRACE WAS REINSTALLED IAW SRM 51-30-1. 2 L 7 2 4F A6WE 1996111400073 19961114 00073 WP 1996 11 14 CALA9601576 1 19961007 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 541 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14814 49112 INSPECTION FOUND FLOORBOARD SUPPORT CORRODED AT FORWARD BULKHEAD OF MID CARGO COMPARTMENT, STA 541, STRINGER 29L TO 28L. THE FLOOR SUPPORT WAS REMOVED IAW SRM 51-30-2. A REPLACEMENT FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-24 -0, FIGURE 9A, SHEETS 2 AND 3, AND SRM 51-30-2. 2 L 7 2 4F A6WE 1996111400074 19961114 00074 WP 1996 11 14 CALA9601577 1 19961007 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 1155 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14814 49112 INSPECTION FOUND FLOOR SUPPORT CORRODED AT F.S. 1155, LBL 18 - 40. THE FLOOR SUPPORT WAS REMOVED AND A SUPPORT ANGLE WA S FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-3. 2 L 7 2 4F A6WE 1996111400075 19961114 00075 WP 1996 11 14 CALA9601578 1 19961006 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 221 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14814 49112 INSPECTION FOUND FLOORBOARD SUPPORT CORRODED AT STA 221, LBL 3. THE FLOOR SUPPORT WAS REMOVED IAW SRM 51-30-2. A REPLA CEMENT PART WAS FABRICATED AND INSTALLED IAW SRM 53-14-1, FIGURE 11 AND 51-30-2. 2 L 7 2 4F A6WE 1996111400076 19961114 00076 NM 1996 11 14 9623452289 1 19961101 A 3350 LIGHT BOEING 727 727251 138408H NM CABIN INOPERATIVE A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 289US 21377 DURING PREFLIGHT, FOUND EMERGENCY LIGHT OVER COCKPIT DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY AND BATTERIES. OPERATIO NAL CHECK NORMAL. 2 L 7 3 4F A3WE 1996111400077 19961114 00077 WP 1996 11 14 9623469922 1 19961105 A 3260 RELAY DOUG DC9 DC932 3022066 WP GEAR WARN LIGHTS MALFUNCTIONED A NWAA O OTHER N FALSE WARNING DE DESCENT 1 GL 01 945N 47664 DURING DESCENT INTO EWR, THE LANDING GEAR WARNING CIRCUIT BREAKER TRIPPED. NO GREEN GEAR DOWNLOCK LIGHTS WERE ILLUMINAT ED AFTER GEAR WAS EXTENDED FOR LANDING. CREW VISUALLY CONFIRMED GEARS TO BE DOWN AND LOCKED THROUGH PERISCOPES. EMERGE NCY EQUIPMENT WAS CALLED OUT ON STANDBY AS A PRECAUTION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE DISCONNECTED AN D RESEATED ALL THREE DOWNLOCK SWITCH CANNON PLUGS AND RESET CIRCUIT BREAKER. LANDING GEAR WARNING LIGHTS DIMMER RELAY W AS ALSO REPLACED. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996111400078 19961114 00078 EU 1996 11 14 9623473229 1 19961106 A 3350 321430 BATTERY AIRBUS 320 A320211 3930320 EU CABIN DISCHARGED A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 329NW 306 PILOT REPORTED THE EMERGENCY EXIT LIGHTS AT DOORS 1L AND 1R WOULD NOT ILLUMINATE WITH ANY SWITCH CONFIGURATION. MAINTEN ANCE TEST FAULTED THE FORWARD LEFT EPSU. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996111400079 19961114 00079 SO 1996 11 14 COMA9610323 1 19961105 A 6123 AUTO FEATHER EMB 120 EMB120RT SO LEFT FAILED TEST A COMA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SO 01 1105G 120105 LEFT AUTOFEATHER FAILED TO TEST. TROUBLESHOT PROBLEM,COULD NOT DUPLICATE. 2 L 7 2 4T RT A31SO 1996111400080 19961114 00080 SO 1996 11 14 COMA9610324 1 19961106 A 2750 120426212507 SELECTOR EMB 120 EMB120RT SO TE FLAPS DEFECTIVE A COMA O OTHER J WARNING INDICATION LD LANDING 1 SO 01 259CA 14596 1294 120252 FLAP CONTROL FAULT WARNING WHEN FLAPS SELECTED UP AFTER LANDING. REPLACED THE FLAP SELECTOR LEVER ASSY. PART TOTAL CYC LES, 14,618. 2 L 7 2 4T RT A31SO 1996111400081 19961114 00081 EU 1996 11 14 COMA9630157 1 19961106 A 6120 8210153 PCU SCBFLG SF34 SF34A 3801351 EU LT PROP MALFUNCTIONED A COMA K NONE O OTHER TO TAKEOFF 1 SO 01 358CA 25123 938 340A047 LEFT PROPELLER RPM INDICATES 1380 DURING TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. 4 RPM IS TOO MINUTE TO PERCEIVE ON THE ANALOG TYPE RPM INDICATOR. THE PROPELLER PITCH CONTROL UNIT WAS REPLACED FOR TROUBLESHOOTING. PART TOTAL CYCLES, 2 8,337. 1 K 0 0 G48EU 1996111400082 19961114 00082 EA 1996 11 14 COMA9660195 1 19961104 A 2170 7536893 COALESCER BAG CNDAIR CL600 CL6002B19 EA LT PACK DIRTY A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 937CA 7044 ON TAXI OUT, NOTICED FAINT BURNING SMELL COMING FROM GASPERS IN COCKPIT. REPLACED COALESCER BAG - OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 1996111400083 19961114 00083 WP 1996 11 14 96FDEA01651 1 19961106 A 3020 ANTI-ICE VALVE DOUG DC10 DC1030F 3023504 WP NR 2 COWL DUCT MALFUNCTIONED A FDEA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 SO 25 307FE 48291 AFTER TAKEOFF, THE NR 2 ANTI-ICE COWL DUCT FAIL LIGHT ILLUMINATED. A NOTE IN THE MEL FOR THE ANTI-ICE WRITE-UP SAID TO REDUCE NR 2 THROTTLE TO IDLE AND USE ONLY IN EMERGENCY CONDITION. COMPLIED. LIGHT WENT OUT WHEN THROTTLE WAS RETARDE D. LIGHT ON APPROXIMATELY 2 MINUTES. REF WRI 30-20/1976 FOR REMOVAL AND REPLACEMENT OF NR 2 ENGINE ANTI-ICE VALVE. NR 2 ENGINE RAN AT TAKEOFF POWER FOR 4 MINUTES PER J.R.H. A/I C.D. FAIL LIGHT REMAINED OUT. CKD NR 2 ANTI-ICE AIR OUTLET SCREEN, FOUND CLEAN. OK FOR SERVICE. 2 L 7 3 4F RT A22WE 1996111400084 19961114 00084 NM 1996 11 14 96FDEA01652 1 19961105 A 5320 65185401 CHORD BOEING 727 72722 1384002 NM BS 740 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 149FE 19087 NR 0039 003, CORROSION ON BS 740 LOWER CHORD RBL 20 AND BLO. *S/D* SPLICED IN A NEW 740 LOWER CHORD IAW FEDEX EA 7-571 0-31288. 2 L 7 3 4F A3WE 1996111400085 19961114 00085 NM 1996 11 14 96FDEA01653 1 19961105 A 5320 651631710 CHORD BOEING 727 72722 1384002 NM BS 351 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 149FE 19087 NR 0041 002, CORROSION (C53-111-03 1/2) IN E-BAY DOGHOUSE ON VERTICAL CHORD AT BS 351 RBL 15 WL 169. *S/D* FOUND CORRO SION TO BE OUT OF LIMITS. REMOVED VERTICAL CHORD, FABRICATED AND INSTALLED NEW VERTICAL CHORD AT BS 351, RBL 15, W/L 16 9 IAW FEDEX SRM 53-10-01. 2 L 7 3 4F A3WE 1996111400086 19961114 00086 NM 1996 11 14 96FDEA01654 1 19961104 A 5315 651631526 FLOORBEAM BOEING 727 727233 138408A NM BS 328 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 NR 0816 32. WHILE WORKING NR 0636 FOUND CORROSION ON BS 328 FLOORBEAM WL 208 LBL 27, 29 AND 45. REPAIRED BS 328 FLOOR BEAM PER FEDEX SR 27-53-017. 2 L 7 3 4F RT A3WE 1996111400087 19961114 00087 NM 1996 11 14 96FDEA01655 1 19961105 A 5320 69436833 SHEAR TIE BOEING 727 727233 138408A NM BS 520 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 NR 0214 31. CORROSION (C53-111-01) ON SHEAR TIE (FWD AND AFT SIDE) AT BS 520 RBL 24 WL 150. REMOVED AND REPLACED SHE AR TIE AT BS 520, RBL 24, WL 150 PER FEDEX SRM 51-10-1. 2 L 7 3 4F RT A3WE 1996111400088 19961114 00088 NM 1996 11 14 96FDEA01601 1 19961021 A 5320 66118092 CLIP BOEING 727 727233 138408A NM BS 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 NR 0151 003. CRACKED STRINGER CLIP AT BS 400 STRINGER NR 15 LT AND NR 2 RT. REPLACED STRINGER CLIPS AT BS 400 STR 15 L AND 2R PER REDEX SRM 53-10-1. 2 L 7 3 4F RT A3WE 1996111400089 19961114 00089 NM 1996 11 14 96FDEA01656 1 19961107 A 2424 GCU BOEING 727 72722 1384002 NM NR 1 GENERATOR WATER CONTAM A FDEA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 SO 25 189FE 19082 NR 1 GENERATOR TRIPPED OFF LINE 2-3 MINUTES AFTER TAKEOFF. BUS TIE WOULD NOT CLOSE PER CHECKLIST. FINALLY DID CLOSE BU T FIELD WOULD THEN NOT CLOSE WITH GOOD RESIDUAL VOLTS. REMOVED AND CLEANED WATER FROM GCU. REINSTALLED, OPS CHECKED NO RMAL PER JRH 8-3. 2 L 7 3 4F A3WE 1996111400090 19961114 00090 WP 1996 11 14 ABXA9600656 1 19961104 A 3350 43 BULB DOUG DC9 DC941 302207N WP CABIN FAILED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 967AX 47509 EMERGENCY LIGHTING WILL NOT COME ON IN THE ARMED (ON) POSITION. RELAMPED AND REPLACED BATTERIES, OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996111400091 19961114 00091 WP 1996 11 14 ABXA9600657 1 19961104 A 3350 43 BULB DOUG DC9 DC941 302207N WP COCKPIT FAILED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 967AX 47509 COCKPIT EMERGENCY LIGHTS, LEFT BULB INOPERATIVE. RELAMPED COCKPIT EMERGENCY LIGHT, LEFT BULB IAW DC-9 M.M. OPS CHECK G OOD. 2 L 7 2 4F A6WE 1996111400092 19961114 00092 NM 1996 11 14 SCNA96348 1 19961031 A 3350 328 LAMP BOEING 727 727259 138408J NM CABIN FAILED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 FOUND RIGHT HAND FORWARD EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP AND OPS CHECKED GOOD. 2 L 7 3 4F A3WE 1996111400093 19961114 00093 WP 1996 11 14 SCNA96349 1 19961015 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 834 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE FOUND CABIN FLOOR STRUCTURE CORRODED FROM C-LIFT TO FLOOR SUPPORT HAT CHANNEL ASSEMBLY, BS 834. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED A SUPPORT ANGLE IN ACCORDANCE WITH SRM 51-31-01. 2 L 7 3 4F A22WE 1996111400094 19961114 00094 WP 1996 11 14 SCNA96350 1 19961020 A 5720 BRACE DOUG DC10 DC1010 3022110 WP WS 130 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE FOUND SUPPORT BRACE CRACKED AT LEFT WING FRONT SPAR, STA XORS 130, INBOARD OF NR 1 SLAT, NR 3 T RACK. REMOVED SUPPORT BRACE, FABRICATED AND INSTALLED A NEW BRACE IN ACCORDANCE WITH SRM 53-00-01. 2 L 7 3 4F A22WE 1996111400095 19961114 00095 WP 1996 11 14 SCNA96351 1 19961017 A 5315 FLOORBEAM DOUG DC10 DC1010 3022110 WP BS 1921 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION AROUND FOUR NUTPLATES ON STATION 1921 FLOOR BEAM, FROM LBL 20 TO LBL 38. REMO VED CORRODED SECTION OF FLOOR BEAM, FABRICATED AND INSTALLED A NEW SECTION OF FLOOR BEAM IN ACCORDANCE WITH SRM 51-31-00 . 2 L 7 3 4F A22WE 1996111400096 19961114 00096 WP 1996 11 14 SCNA96352 1 19961017 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1964 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT JUST FORWARD OF THE FLOOR BEAM AT BS 1964, RBL 22. REMOVED C ORRODED SECTION, FABRICATED AND INSTALLED A NEW SECTION IN ACCORDANCE WITH SRM 51-30-00. 2 L 7 3 4F A22WE 1996111400097 19961114 00097 WP 1996 11 14 SCNA96353 1 19961017 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1871 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BODY STATION 1871, LBL 63. REMOVED DAMAGED SUPPORT, FABRI CATED AND INSTALLED A NEW SUPPORT IN ACCORDANCE WITH SRM 51-30-01. 2 L 7 3 4F A22WE 1996111400098 19961114 00098 WP 1996 11 14 SCNA96354 1 19961017 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1600 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT ON LEFT HAND SIDE AT BS 1600. REMOVED, FABRICATED AND INSTAL LED A NEW FLOOR SUPPORT IN ACCORDANCE WITH SRM 51-30-00. 2 L 7 3 4F A22WE 1996111400099 19961114 00099 WP 1996 11 14 SCNA96355 1 19961019 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1139 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT ANGLE AT AFT END OF FORWARD CARGO COMPARTMENT, BS 1139, RBL 7 TO RBL 22. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 53-00-01. 2 L 7 3 4F A22WE 1996111400100 19961114 00100 WP 1996 11 14 SCNA96356 1 19961021 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1964 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1964 RBL 64. REMOVED CORRODED SUPPORT, FABRICATED AND INSTALLED A NEW SUPPORT IN ACCORDANCE WITH SRM 51-21-03. 2 L 7 3 4F A22WE 1996111400101 19961114 00101 WP 1996 11 14 SCNA96357 1 19961021 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1964 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT BS 1964, RBL 29. REMOVED FLOOR SUPPORT, FABRICATED AND INSTA LLED A NEW FLOOR SUPPORT IN ACCORDANCE WITH SRM 51-30-00. 2 L 7 3 4F A22WE 1996111400102 19961114 00102 WP 1996 11 14 SCNA96358 1 19961021 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1964 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT BS 1964, LBL 29. REMOVED FLOOR SUPPORT, FABRICATED AND INSTA LLED A NEW FLOOR SUPPORT IN ACCORDANCE WITH SRM 51-30-00. 2 L 7 3 4F A22WE 1996111400103 19961114 00103 WP 1996 11 14 SCNA96359 1 19961021 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1964 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT BS 1964, LBL 39. REMOVED FLOOR SUPPORT, FABRICATED AND INSTA LLED A NEW FLOOR SUPPORT IN ACCORDANCE WITH SRM 51-16-01. 2 L 7 3 4F A22WE 1996111400104 19961114 00104 WP 1996 11 14 SCNA96360 1 19961021 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1887 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT BS 1887 LBL 75. REMOVED FLOOR SUPPORT, FABRICATED AND INSTAL LED A NEW FLOOR SUPPORT IN ACCORDANCE WITH SRM 51-30-00. 2 L 7 3 4F A22WE 1996111400105 19961114 00105 WP 1996 11 14 SCNA96361 1 19961021 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1964 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT BS 1964 RBL 46. REMOVED FLOOR SUPPORT, FABRICATED AND INSTAL LED A NEW FLOOR SUPPORT IN ACCORDANCE WITH SRM 51-42-00. 2 L 7 3 4F A22WE 1996111400106 19961114 00106 WP 1996 11 14 SCNA96362 1 19961021 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1835-1837 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT BS 1835 - BS 1837, RBL 39. REMOVED CORRODED SUPPORT, FABRICA TED AND INSTALLED A NEW FLOOR SUPPORT IN ACCORDANCE WITH 51-31-01. 2 L 7 3 4F A22WE 1996111400107 19961114 00107 WP 1996 11 14 SCNA96363 1 19961022 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1871 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1871 RBL 64 TO RBL 90. REMOVED CORRODED SUPPORT, FABRI CATED AND INSTALLED A NEW FLOOR SUPPORT IN ACCORDANCE WITH 51-31-01. 2 L 7 3 4F A22WE 1996111400108 19961114 00108 WP 1996 11 14 SCNA96364 1 19961022 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1921-1964 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1921 TO BS 1964, LBL 18. REMOVED CORRODED SUPPORT, FAB RICATED AND INSTALLED A NEW FLOOR SUPPORT IN ACCORDANCE WITH 51-30-00. 2 L 7 3 4F A22WE 1996111400109 19961114 00109 WP 1996 11 14 SCNA96365 1 19961022 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1901 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1901, LBL 53 TO LBL 86. REMOVED CORRODED SUPPORT, FABR ICATED AND INSTALLED A NEW FLOOR SUPPORT IN ACCORDANCE WITH 53-60-01. 2 L 7 3 4F A22WE 1996111400110 19961114 00110 WP 1996 11 14 SCNA96366 1 19961022 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1835-1887 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1835 TO BS 1887, LBL 40. REMOVED CORRODED SUPPORT, FAB RICATED AND INSTALLED A NEW FLOOR SUPPORT IN ACCORDANCE WITH 51-31-01. 2 L 7 3 4F A22WE 1996111400111 19961114 00111 WP 1996 11 14 SCNA96367 1 19961022 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1887 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE FOUND CORROSION ON FLOOR SUPPORT AT BS 1887, BL ZERO TO RBL 90. REMOVED CORRODED SUPPORT, FABR ICATED AND INSTALLED A NEW FLOOR SUPPORT IN ACCORDANCE WITH 53-60-01. 2 L 7 3 4F A22WE 1996111400112 19961114 00112 WP 1996 11 14 SCNA96368 1 19961022 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1909 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1909, RBL 53 TO RBL 85. REMOVED CORRODED SUPPORT, FABR ICATED AND INSTALLED A NEW FLOOR SUPPORT IN ACCORDANCE WITH 53-60-01. 2 L 7 3 4F A22WE 1996111400113 19961114 00113 NM 1996 11 14 P5CA9600900 1 19961104 A 5280 SKIN BOEING 747 747122 1384872 NM RT MLG DOOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 LEVEL 1 CORROSION ON RIGHT BODY GEAR INBOARD GEAR DOOR SKIN. REMOVED CORROSION PER BAC SRM 51-10-01 AND REPROTECTED PE R BAC SRM 51-10-02. 2 L 7 4 4F A20WE 1996111400114 19961114 00114 NM 1996 11 14 P5CA9600901 1 19961104 A 5280 SKIN BOEING 747 747122 1384872 NM RT MLG DOOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 LEVEL 1 CORROSION ON RIGHT BODY GEAR INBOARD GEAR DOOR TRAILING EDGE SKIN. REMOVED CORROSION PER BAC SRM 51-10-01 AND REPROTECTED PER BAC SRM 51-10-02. 2 L 7 4 4F A20WE 1996111400115 19961114 00115 NM 1996 11 14 P5CA9600902 1 19961104 A 7110 ANGLE BOEING 747 747122 1384872 NM NR 1 ENGINE COWL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 CRACK AND DEFORMATION ON NR 1 CORE COWL HAT SECTION ANGLE. STOP DRILLED AND REPAIRED PER BAC SRM 51-40-01. 2 L 7 4 4F A20WE 1996111400116 19961114 00116 NM 1996 11 14 P5CA9600903 1 19961104 A 2550 BALL MAT TRAY BOEING 747 747122 1384872 NM FWD CARGO BAY DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 DAMAGED BALL MAT TRAY IN FORWARD LOWER CARGO BAY. REPLACED BALL MAT TRAY WITH FABRICATED TRAY PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1996111400117 19961114 00117 WP 1996 11 14 RRXA96163 1 19961105 A 3310 FLUORESCENT BULB DOUG DC8 DC862 3021970 WP LT GLARESHIELD FAILED A RRXA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 15 990CF 46068 ON TAXI IN, SMOKE WAS SEEN FROM UNDER THE GLARESHIELD. MAINTENANCE FOUND THE CAPTAIN'S FLUORESCENT BULB SMOKED. MAIN TENANCE REMOVED AND REPLACED THE CAPTAIN'S FLUORESCENT BULB. NO OTHER DEFECTS NOTED. 2 L 7 4 4F 4A25 1996111400118 19961114 00118 WP 1996 11 14 CALA9601579 1 19961107 A 2910 7936907665 HYD LINE DOUG DC9 DC982 3022082 WP RT TAIL COMPT LEAKING A CALA O OTHER K FLUID LOSS CR CRUISE 1 SW 09 93875 49125 THE AIRCRAFT LOST FLUID FROM THE RT HYDRAULIC SYSTEM WHILE EN ROUTE TO EWR. THE RT SYSTEM WAS SECURED AT 7 QUART LEVEL. THE RT SYSTEM WAS TURNED ON FOR LANDING AND THE HYDRAULIC FLUID DROPPED TO A FINAL LEVEL OF THREE QUARTS. THE AIRCRAF T LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC PRESSURE LINE AT CASE DRAIN FILTER IN RT TAIL COMPARTMENT LE AKING. THE LINE WAS REMOVED AND REPLACED. THE HYDRAULIC SYSTEM WAS SERVICED TO FULL. LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F A6WE 1996111400119 19961114 00119 NM 1996 11 14 CALA9601580 1 19961011 A 5330 SKIN BOEING 727 727232 1384082 NM BS 720 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND LOWER FUSELAGE SKIN CORRODED AT STA 720A, STRINGER 30. THE SKIN WAS REMOVED. A TRIPLER AND DOUBLER RE PAIR WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND EA 65C13568. 2 L 7 3 4F A3WE 1996111400120 19961114 00120 NM 1996 11 14 CALA9601581 1 19961022 A 5321 FLOOR PANEL BOEING 727 727232 1384082 NM BS 1135 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND CABIN FLOOR PANEL LOWER SURFACE CORRODED AT STA 1135, RBL 26. THE CORRODED AREA WAS CUT OUT AND A DOUB LER WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-40-5. 2 L 7 3 4F A3WE 1996111400121 19961114 00121 NM 1996 11 14 CALA9601582 1 19961018 A 5330 SKIN BOEING 727 727232 1384082 NM BS 580 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND SKIN CORRODED BELOW STRINGER 28L AT STA 580. THE CORRODED AREA WAS CUT OUT. A DOUBLER AND STRAP WERE FABRICATED AND INSTALLED IAW SRM 53-30-2 AND 53-30-3. 2 L 7 3 4F A3WE 1996111400122 19961114 00122 NM 1996 11 14 CALA9601583 1 19961012 A 5330 SKIN BOEING 727 727232 1384082 NM BS 670 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND SKIN DOUBLER CORRODED AT LAP SEAM IN FORWARD CARGO PIT AT STA 670, STRINGER 26L. THE CORRODED AREA WAS CUT OUT. REPLACEMENT STRINGER SPLICE, SHEAR TIE, SKIN FILLER, AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-30- 3, 51-30-2, AND 51-10-1. 2 L 7 3 4F A3WE 1996111400123 19961114 00123 NM 1996 11 14 CALA9601584 1 19961011 A 5520 BRACKET BOEING 727 727232 1384082 NM LT ELEVATOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND A .75 INCH CRACK IN LT ELEVATOR NR 3 HINGE ATTACH BRACKET AT HORIZONTAL STABILIZER TRAILING EDGE. THE CRACKED AREA WAS CUT OUT. AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-10-4. 2 L 7 3 4F A3WE 1996111400124 19961114 00124 NM 1996 11 14 CALA9601585 1 19961008 A 5754 RIB BOEING 727 727232 1384082 NM NR 8 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND A 1.5 INCH CRACK IN NR 8 SLAT OUTBOARD RIB WHERE ACTUATOR ATTACHES. A DOUBLER REPAIR WAS INSTALLED IAW SRM 57-50-3. 2 L 7 3 4F A3WE 1996111400125 19961114 00125 NM 1996 11 14 CALA9601586 1 19961012 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 1155 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND STRINGER 20R CORRODED IN AFT CARGO COMPARTMENT AT STA 1155. THE CORRODED AREA OF STRINGER WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-10-3. 2 L 7 3 4F A3WE 1996111400126 19961114 00126 NM 1996 11 14 CALA9601587 1 19961011 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 580 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND CORROSION ON STRINGER 28L BELOW FRAME AT STA 580. THE CORRODED AREA WAS CUT OUT AND A REPAIR WAS FABRI CATED AND INSTALLED IAW SRM 53-10-3. 2 L 7 3 4F A3WE 1996111400127 19961114 00127 NM 1996 11 14 CALA9601588 1 19961015 A 5730 SKIN BOEING 727 727227 1384078 NM RT WING LE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76753 21249 INSPECTION FOUND THE RT WING LEADING EDGE SKIN DENTED WITH A .25 INCH CRACK JUST OUTBOARD OF NR 5 SLAT INBOARD TRACK. T HE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 57-30-4, FIGURE 1. 2 L 7 3 4F A3WE 1996111400128 19961114 00128 NM 1996 11 14 CALA9601589 1 19961015 A 5330 SKIN BOEING 727 727227 1384078 NM BS 416 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76753 21249 INSPECTION FOUND THE RT FUSELAGE SKIN DENTED AT STA 416 JUST BELOW AND AFT OF OXYGEN SERVICE DOOR. THE DENTED AREA WAS CUT OUT. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 1. 2 L 7 3 4F A3WE 1996111400129 19961114 00129 NM 1996 11 14 CALA9601590 1 19961018 A 5240 HINGE HOUSING BOEING 727 727227 1384078 NM L2 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76753 21249 INSPECTION FOUND A .50 INCH CRACK IN L-2 DOOR UPPER HINGE HOUSING. THE HINGE HOUSING WAS REMOVED AND REPLACED IAW SRM 5 1-10-2. 2 L 7 3 4F A3WE 1996111400130 19961114 00130 NM 1996 11 14 CALA9601591 1 19961015 A 5320 INTERCOSTAL BOEING 727 727227 1384078 NM BS 720 BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76753 21249 INSPECTION FOUND INTERCOSTAL BROKEN OUT ALONG TOP AT SCREW HOLES (BELOW FLOOR PANEL NR 49) AT BL ZERO BETWEEN FLOORBEAMS , B.S. 720-720A. THE INTERCOSTAL ANGLE WAS REMOVED AND A REPLACEMENT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 . 2 L 7 3 4F A3WE 1996111400131 19961114 00131 NM 1996 11 14 CALA9601592 1 19961016 A 5320 ANGLE BOEING 727 727227 1384078 NM BS 392 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76753 21249 INSPECTION FOUND FORWARD LAV FLOOR ANGLE CORRODED AT B.S. 392. THE FLOOR ANGLE WAS REMOVED AND A REPLACEMENT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1. 2 L 7 3 4F A3WE 1996111400132 19961114 00132 NM 1996 11 14 CALA9601593 1 19961018 A 5320 INTERCOSTAL BOEING 727 727227 1384078 NM BS 990-1010 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76753 21249 INSPECTION FOUND A 2 INCH CRACK AT SCREW HOLE IN FLOOR SUPPORT INTERCOSTAL BETWEEN FLOORBEAMS AT STA 990-1010, BL ZERO. 2 L 7 3 4F A3WE 1996111400133 19961114 00133 NM 1996 11 14 CALA9601594 1 19961015 A 5330 SKIN BOEING 727 727227 1384078 NM BS 1050 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76753 21249 INSPECTION FOUND A 3 INCH CRACK IN LOWER FUSELAGE SKIN AT STA 1050, STRINGER 27L. THE CRACKED AREA WAS CUT OUT. A FILL ER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 AND 51-40-5. 2 L 7 3 4F A3WE 1996111400134 19961114 00134 NM 1996 11 14 CALA9601595 1 19961023 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 1166 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76753 21249 INSPECTION FOUND STRINGER 24R CORRODED IN AFT CARGO COMPARTMENT AT STA 1166 UNDER CIRCUMFERENTIAL. THE CORRODED SECTION OF STRINGER WAS REMOVED AND A REPLACEMENT WAS FABRICATED AND INSTALLED IAW SRM 53-10-3. 2 L 7 3 4F A3WE 1996111400135 19961114 00135 NM 1996 11 14 CALA9601596 1 19961022 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 1050-1070 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76753 21249 INSPECTION FOUND STRINGER 27L CORRODED FROM STA 1050-1070. THE CORRODED SECTION OF STRINGER WAS CUT OUT. A REPLACEMENT WAS FABRICATED AND INSTALLED IAW SRM 53-10-3. 2 L 7 3 4F A3WE 1996111400136 19961114 00136 NM 1996 11 14 CALA9601597 1 19961015 A 5754 SKIN BOEING 727 727227 1384078 NM NR 4 LE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76753 21249 INSPECTION FOUND A 1 INCH CRACK IN LOWER OUTBOARD AREA OF RT NR 4 LEADING EDGE FLAP AFT SURFACE. THE CRACK WAS STOP DRI LLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-2, AND ECRA 5720-01064. 2 L 7 3 4F A3WE 1996111400137 19961114 00137 NM 1996 11 14 CALA9601598 1 19961015 A 5754 SKIN BOEING 727 727227 1384078 NM NR 4 LE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76753 21249 INSPECTION FOUND THREE 1 INCH CRACKS IN RT NR 4 LEADING EDGE FLAP AFT SURFACE. THE CRACKS WERE STOP DRILLED. DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-2, AND ECRA 5720-01064. 2 L 7 3 4F A3WE 1996111400138 19961114 00138 NM 1996 11 14 CALA9601599 1 19961018 A 5330 SKIN BOEING 727 727227 1384078 NM BS 1010-1030 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76753 21249 INSPECTION FOUND SKIN AND STRINGERS IN AFT CARGO COMPARTMENT CORRODED BETWEEN STA 1010 AND 1030, STRINGERS 30R - 29R. T HE CORRODED AREAS WERE REMOVED. A REPLACEMENT CHANNEL WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1996111400139 19961114 00139 NM 1996 11 14 CALA9601600 1 19961026 A 5330 SKIN BOEING 727 727232 1384082 NM BS 360 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16784 20639 INSPECTION FOUND A .50 INCH CRACK WITH CORROSION IN RT FUSELAGE SKIN AT STA 360, STRINGER 23. A REPAIR DOUBLER WAS INST ALLED IAW SRM 53-30-3. 2 L 7 3 4F A3WE 1996111400140 19961114 00140 NM 1996 11 14 CALA9601601 1 19961109 A 2910 HYD LINE BOEING 737 737130 1384435 NM NR 4 SLAT ACT BROKEN A A CALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 09 77204 19021 THE A-HYDRAULIC SYSTEM PRESSURE AND QUANTITY DROPPED TO ZERO WHEN GEAR WAS LOWERED ON FINAL APPROACH TO CLE. THE FLAPS WERE LOWERED TO 15 DEGREES ELECTRICALLY AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 4 SLAT ACTUA TOR HYDRAULIC LINE BROKEN. THE LINE WAS REMOVED AND REPLACED. BOTH THE NR 1 & NR 2 ENGINE DRIVEN HYDRAULIC PUMPS WERE REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F A16WE 1996111400141 19961114 00141 WP 1996 11 14 CALA9601602 1 19961110 A 3350 EMSE299 BATTERY DOUG DC10 DC1030 3023501 WP CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14063 47864 THE EMERGENCY LIGHTS WOULD NOT TEST IN ARMED POSITION. THE FORWARD BATTERY PACK AND CHARGER AND AFT BATTERY PACK WERE R EMOVED AND REPLACED. A SYSTEM TEST WAS PERFORMED AND OPERATION OF THE EMERGENCY LIGHTS CHECKED NORMAL. 2 L 7 3 4F A22WE 1996111400142 19961114 00142 NM 1996 11 14 CALA9601603 1 19961104 A 5330 SKIN BOEING 737 737130 1384435 NM C2 DOOR CUTOUT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 44214 19031 INSPECTION FOUND A 1 INCH CRACK AT AFT LOWER CORNER OF C-2 DOOR AFT CUTOUT. THE CRACKED AREA WAS CUT OUT AND FILLER AND DOUBLERS WERE INSTALLED IAW ECRA 5330-02460. 2 L 7 2 4F A16WE 1996111400143 19961114 00143 WP 1996 11 14 CALA9601604 1 19961031 A 5310 STRUCTURE DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 938MC 49525 A LAV SERVICE TRUCK STRUCK THE FUSELAGE 29 INCHES BELOW FORWARD EDGE OF SUGAR SCOOP RESULTING IN DAMAGE TO SKIN AND LONG ERON. THE DAMAGED AREA WAS APPROXIMATELY 4 INCHES X 4 INCHES. A CLASS III REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 12B, SHEET 18. A DIP WAS ISSUED TO REPLACE THE REPAIR WITH A CLASS I OR II REPAIR WITHIN 8,000 HOURS AND TO INSPECT THE AREA AT INTERVALS NOT TO EXCEED 3,000 HOURS. 2 L 7 2 4F RT A6WE 1996111400144 19961114 00144 WP 1996 11 14 CALA9601605 1 19961029 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1446 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14889 49118 INSPECTION FOUND .50 INCH CRACKS IN CANTED BELTFRAME AT STA 1446, LONGERONS 3, 4, AND 5R. THE FRAME WAS REPAIRED IAW SR M 53-03. 2 L 7 2 4F A6WE 1996111400145 19961114 00145 NM 1996 11 14 CALA9601606 1 19961101 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17329 23459 INSPECTION FOUND AFT RIGHT LAV WALL FLOORBEAM CORRODED. THE AREA WAS REPAIRED IAW ECRA 5310-03361. 2 L 7 2 4F RT A16WE 1996111400146 19961114 00146 NM 1996 11 14 CALA9601607 1 19961103 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 986-1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17329 23459 INSPECTION FOUND FLOOR SUPPORT INTERCOSTAL CORRODED AT STA 986-1016, LBL 15. THE FLOOR SUPPORT INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-2. 2 L 7 2 4F RT A16WE 1996111400147 19961114 00147 NM 1996 11 14 CALA9601608 1 19961103 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 967-986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17329 23459 INSPECTION FOUND INTERCOSTAL CORRODED BETWEEN STA 967 AND 986, RBL 18.75. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-2 AND 51-40-2. 2 L 7 2 4F RT A16WE 1996111400148 19961114 00148 NM 1996 11 14 CALA9601609 1 19961103 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 947-967 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17329 23459 INSPECTION FOUND FLOOR SUPPORT INTERCOSTAL CORRODED BETWEEN STA 947 AND 967, LBL 17.61. THE FLOOR SUPPORT INTERCOSTAL W AS REMOVED AND REPLACED IAW SRM 51-40-2. 2 L 7 2 4F RT A16WE 1996111400149 19961114 00149 NM 1996 11 14 CALA9601610 1 19961103 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 986.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17329 23459 INSPECTION FOUND FLOORBEAM CORRODED AROUND FASTENER HOLE AT STA 986.5, RBL 40. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310 -03361. 2 L 7 2 4F RT A16WE 1996111400150 19961114 00150 NM 1996 11 14 CALA9601611 1 19961103 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 986.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17329 23459 INSPECTION FOUND RT SIDE AND CENTER OF FLOORBEAM CORRODED AT STA 986.5, RBL 3, RBL 5, AND RBL 15. THE FLOORBEAM WAS REP AIRED IAW ECRA 5310-03361. 2 L 7 2 4F RT A16WE 1996111400151 19961114 00151 NM 1996 11 14 CALA9601612 1 19961102 A 5320 ANGLE BOEING 737 7373T0 1384582 NM BS 986.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17329 23459 INSPECTION FOUND FLOOR SUPPORT ANGLE AT AFT SIDE OF L-2 DOOR FRAME CORRODED AT STA 986.5. THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-2 AND 51-40-2. 2 L 7 2 4F RT A16WE 1996111400152 19961114 00152 NM 1996 11 14 CALA9601613 1 19961103 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17329 23459 INSPECTION FOUND FLOORBEAM AT STA 986, LBL 15 TO DOOR SILL AREA CORRODED. THE AREA WAS REPAIRED IAW ECRA 5310-03361. 2 L 7 2 4F RT A16WE 1996111400153 19961114 00153 NM 1996 11 14 CALA9601614 1 19961103 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 967-986.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17329 23459 INSPECTION FOUND FLOOR SUPPORT INTERCOSTAL CORRODED BETWEEN STA 967-986.5, LBL 17.61. THE FLOOR SUPPORT INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-2. 2 L 7 2 4F RT A16WE 1996111400154 19961114 00154 NM 1996 11 14 CALA9601615 1 19961103 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 947-967 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17329 23459 INSPECTION FOUND INTERCOSTAL CORRODED BETWEEN STA 947-967, RBL 17.61. THE INTERCOSTAL WAS REPLACED IAW SRM 51-40-2. 2 L 7 2 4F RT A16WE 1996111400155 19961114 00155 NM 1996 11 14 CALA9601616 1 19961106 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 995-1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17329 23459 INSPECTION FOUND INTERCOSTAL CORRODED AT NUTPLATE HOLES, STA 995-1016, LBL 37.21. THE INTERCOSTAL WAS REMOVED AND REPLA CED IAW SRM 51-40-2. 2 L 7 2 4F RT A16WE 1996111400156 19961114 00156 NM 1996 11 14 CALA9601617 1 19961103 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 1006 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17329 23459 INSPECTION FOUND UPPER SURFACE OF FLOORBEAM CORRODED AT NUTPLATE HOLE, STA 1006, RBL 20. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-03360. 2 L 7 2 4F RT A16WE 1996111400157 19961114 00157 NM 1996 11 14 CALA9601618 1 19961103 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 967 CORRODED A CALA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 09 17329 23459 INSPECTION FOUND UPPER SURFACE OF FLOORBEAM CORRODED AT STA 967. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-03362. 2 L 7 2 4F RT A16WE 1996111400158 19961114 00158 WP 1996 11 14 9623599978 1 19961106 A 5270 SWITCH DOUG DC9 DC931 3022065 WP AFT STAIR INOPERATIVE A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 9342 47391 AFTER TAKEOFF DTW-GSO, THE AFT STAIRWAY DOOR WARNING LIGHT ILLUMINATED. RETURNED TO DTW WITHOUT FURTHER INCIDENT. REPL ACED THE LEFT AFT STAIR UPLOCK SWITCH. WARNING SYSTEM CHECKED OK. 2 L 7 2 4F A6WE 1996111400159 19961114 00159 EU 1996 11 14 9623603235 1 19961107 A 3350 321454 POWER SUPPLY AIRBUS 320 A320211 3930320 EU CABIN INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 335NW 19110 8101 340 DURING LINE MAINTENANCE CHECK, FOUND BOTH AFT DOOR EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED LEFT AFT EPSU. OPERATION AL CHECK OK. 2 L 7 2 4F RT A28NM 1996111400160 19961114 00160 WP 1996 11 14 9623619882 1 19961107 A 2120 AIR DISTR DOUG DC9 DC951 3022051 WP CABIN ODOR A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 670MC 47659 AFTER TAKEOFF FROM DTW, A BURNING RUBBER/OIL ODOR FILLED AIRCRAFT. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT INSIDE AND OUT AND COULD NOT LOCATE SOURCE OF ODOR. AIRCRAFT WAS APPROVED FOR FURTHER S ERVICE. 2 L 7 2 4F A6WE 1996111400161 19961114 00161 1996 11 14 9623629883 4 19961106 A 3454 5224280105 NAV RECEIVER DOUG DC9 DC951 3022051 WP NR 2 INOPERATIVE A NWAA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 01 671MC 47660 DURING CRUISE TO IND, THE NR 2 VOR BECAME INOPERATIVE. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NAV RECEIVER. OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996111400162 19961114 00162 NM 1996 11 14 9623635515 1 19961108 A 3350 BATTERY PACK BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 515US 23203 DURING PREFLIGHT, FOUND FLOOR LEVEL LIGHTS INOPERATIVE IN FIRST CLASS. REPLACED BATTERY PACK IN FORWARD CEILING. 2 L 7 3 4F A3WE 1996111400163 19961114 00163 NM 1996 11 14 9623642703 1 19961108 A 3350 BATTERY BOEING 727 727225 1384077 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8878Z 21451 EMERGENCY EXIT LIGHT ABOVE BOTTOM AFT AIRSTAIRS INOPERATIVE. REPLACED BATTERY HOLDER AND BATTERY. OPERATIONAL CHECK OK . 2 L 7 3 4F A3WE 1996111400164 19961114 00164 NM 1996 11 14 9623655517 1 19961106 A 3260 LAMP BOEING 727 727251 138408H NM LT MLG FAILED A NWAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 01 517US 23205 ON APPROACH TO MCO, THE LEFT MAIN LANDING GEAR DID NOT INDICATE DOWN AND LOCKED. REPLACED THE LEFT MAIN GEAR INDICATION LAMPS. ALL LIGHTS TESTED NORMALLY. 2 L 7 3 4F A3WE 1996111400165 19961114 00165 NM 1996 11 14 9623662703 1 19961107 A 3240 657276187 BRAKE ASSY BOEING 727 727225 1384077 NM RT MLG FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 8878Z 62 21451 DURING TAKEOFF ROLL, NOISE FROM LEFT MAIN GEAR INCREASED PROPORTIONALLY WITH SPEED OF AIRCRAFT ON TAKEOFF. ABORTED TAKE OFF WITHOUT INCIDENT. INSPECTED TIRES AND BRAKES. REPLACED NR 3 TIRE AND BRAKE ASSEMBLY. PART TOTAL CYCLES, 4,061. 2 L 7 3 4F A3WE 1996111400166 19961114 00166 WP 1996 11 14 9623679980 1 19961107 A 3350 SOCKETS DOUG DC9 DC931 3022065 WP VENTRAL STAIRS CORRODED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9344 47440 DURING LINE MAINTENANCE INSPECTION, FOUND VENTRAL STAIR EMERGENCY LIGHTS WEAK. MAINTENANCE CLEANED CORROSION FROM SOCKE TS. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996111400167 19961114 00167 WP 1996 11 14 9623689606 1 19961107 A 3397 WIRE DOUG DC9 DC932 3022066 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 606NW 47225 DURING PERIODIC CHECK, FOUND EMERGENCY EXIT LIGHT AT ROW 13 INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996111400168 19961114 00168 WP 1996 11 14 9623699918 1 19961106 A 3397 WIRE DOUG DC9 DC932 3022066 WP FA SWITCH PNL MISINSTALLED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 940N 47572 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE FOUND WIRES AT FLIG HT ATTENDANT SWITCH REVERSED. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996111400169 19961114 00169 WP 1996 11 14 9623709940 1 19961106 A 3397 WIRE DOUG DC9 DC932 3022066 WP CABIN MISINSTALLED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3322L 47031 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE FOUND WIRES AT CANN ON PLUG RECEPTACLES R5-4009 PINS L AND M REVERSED. CORRECTED WIRING AT RECEPTACLE. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996111400170 19961114 00170 WP 1996 11 14 9623719985 1 19961106 A 3350 60030451 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 985US 47479 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CH ECK NORMAL. 2 L 7 2 4F A6WE 1996111400171 19961114 00171 1996 11 14 9623729965 4 19961107 A 3442 20671570153 TRANSCEIVER DOUG DC9 DC931 3022065 WP E/E COMPT MALFUNCTIONED A NWAA A UNSCHED LANDING O OTHER UK UNKNOWN 1 GL 01 911RW 38557 3485 47149 WEATHER RADAR SYSTEM FAILED EN ROUTE MSP-PIT. SCREEN DID NOT SHOW RETURNS AND WAS SPOKING WHEN ACTIVATED. FLIGHT DIVER TED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RADAR TRANSCEIVER. OPERATIONAL CHECK NORMAL. AIRCRAFT RET URNED TO SERVICE. 2 L 7 2 4F A6WE 1996111400172 19961114 00172 1996 11 14 9623739984 4 19961106 A 3425 5222782004 HSI DOUG DC9 DC932 3022066 WP LT COCKPIT MALFUNCTIONED A NWAA A UNSCHED LANDING O OTHER UK UNKNOWN 1 GL 01 984US 22736 12073 47383 CAPTAIN'S HORIZONTAL SITUATION INDICATOR BEGAN STICKING ON HEADINGS DURING TURNS. FLIGHT RETURNED TO MSP AND LANDED WIT HOUT INCIDENT. MAINTENANCE REPLACED CAPTAIN'S HORIZONTAL SITUATION INDICATOR. OPERATIONAL CHECK NORMAL. AIRCRAFT RETU RNED TO SERVICE. 2 L 7 2 4F A6WE 1996111400173 19961114 00173 WP 1996 11 14 9623749922 1 19961106 A 2130 94840213 PRESS AMPLIFIER DOUG DC9 DC932 3022066 WP E/E COMPT MALFUNCTIONED A NWAA B EMER. DESCENT J WARNING INDICATION UK UNKNOWN 1 GL 01 945N 25078 1894 47664 LOSS OF CABIN PRESSURIZATION OCCURRED DURING FLIGHT AT 35,000 FEET. CABIN ALTITUDE REACHED 10,000 FEET WITH MASTER WARN ING/CABIN PRESSURE ANNUNCIATOR LIGHTS ILLUMINATED. CAPTAIN DECLARED AN EMERGENCY AND SUCCESSFUL DESCENT WAS MADE TO 16, 000 FEET. FLIGHT CONTINUED TO DESTINATION AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED CABIN PRESSURE AM PLIFIER. OPERATION CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996111400174 19961114 00174 WP 1996 11 14 8512489957 1 19961021 A 5312 BULKHEAD T CAP DOUG DC9 DC931 3022065 WP BS 756 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 915RW 47139 DURING H-CHECK, FOUND CORROSION ON THE FS 756 BULKHEAD T-CAP BETWEEN LONGERONS 29L - 29R. REPAIRED T-CAP (P/N 9958212-3 ) PER EA 99-111734. 2 L 7 2 4F A6WE 1996111400175 19961114 00175 WP 1996 11 14 9623499957 1 19961023 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 965 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 915RW 47139 DURING H-CHECK, FOUND CORROSION ON THE FS 965 FRAME BETWEEN LONGERON 26L - 28R. REPAIRED FRAME (P/N 9912243-105) PER EA 99-111745. 2 L 7 2 4F A6WE 1996111400176 19961114 00176 WP 1996 11 14 9623501161 1 19961025 A 5730 SKIN DOUG DC10 DC1040 3023508 WP WS 611 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 161US 46770 DURING L-CHECK, FOUND A 1.6258 INCH CRACK IN THE RIGHT WING LOWER LEADING EDGE SKIN AT XOS 611. REPAIRED SKIN (P/N ARB2 887-502) PER EA 11-110210. 2 L 7 3 4F A22WE 1996111400177 19961114 00177 WP 1996 11 14 9623519974 1 19961026 A 5320 PRESS PANEL DOUG DC9 DC931 3022065 WP BS 83 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9338 47347 DURING H-CHECK, FOUND CRACKS IN THE NOSE LANDING GEAR HORIZONTAL PRESSURE PANEL AT FS 83, RIGHT SIDE, AND AT FS 110 LEFT SIDE. REPAIRED PANEL (P/N 9910073-3, -313) PER EA 99-111747, 99-111758. 2 L 7 2 4F A6WE 1996111400178 19961114 00178 WP 1996 11 14 9623521161 1 19961027 A 5330 SKIN DOUG DC10 DC1040 3023508 WP BS 587 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 161US 46770 DURING L-CHECK, FOUND A CRACK IN THE FUSELAGE SKIN AT THE LEFT AIR CYCLE MACHINE DOOR JAMB UPPER AFT CORNER, FS 587. RE PAIRED SKIN (P/N ACA 3108) PER EA 11-110287. 2 L 7 3 4F A22WE 1996111400179 19961114 00179 WP 1996 11 14 9623539618 1 19961028 A 5320 FITTING DOUG DC9 DC932 3022066 WP RT COCKPIT CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 618NW 47433 DURING M-CHECK, FOUND CORROSION IN THE FIRST OFFICER'S SLIDING WINDOW LOWER AFT FITTING AND STOP PLATE. REPLACED BOTH P ER SRM 51-30-00. 2 L 7 2 4F A6WE 1996111400180 19961114 00180 WP 1996 11 14 9623541161 1 19961028 A 5320 FITTING DOUG DC10 DC1040 3023508 WP BS 1509 1521 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 161US 46770 DURING L-CHECK, FOUND THE LONGERON 48L, 49L, AND 48R END FITTINGS CORRODED FROM FS 1509 - 1521. REPLACED BOTH FITTINGS. 2 L 7 3 4F A22WE 1996111400181 19961114 00181 WP 1996 11 14 9623559618 1 19961029 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 953 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 618NW 47433 DURING M-CHECK, FOUND CORROSION IN THE FS 935 LEFT SIDE CUSP WEB. REPLACED FRAME END FITTING AND WEB PER SRM 51-10-2, 5 1-30-2, AND 53-01. 2 L 7 2 4F A6WE 1996111400182 19961114 00182 WP 1996 11 14 9623569974 1 19961101 A 5314 KEEL T CAP DOUG DC9 DC931 3022065 WP BS 604 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9338 47347 DURING H-CHECK, FOUND CORROSION IN THE LEFT FORWARD KEEL T-CAP AT THE FS 604 BULKHEAD. REPAIRED T-CAP (P/N 5914865-29) PER EA 99-111756. 2 L 7 2 4F A6WE 1996111400183 19961114 00183 WP 1996 11 14 9623579753 1 19961103 A 5320 PRESS PANEL DOUG DC9 DC941 302207N WP BS 108 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 753NW 47117 DURING H-CHECK, FOUND CRACKS IN THE NOSE LANDING GEAR HORIZONTAL PRESSURE PANEL AT FS 108, LEFT AND RIGHT SIDES AT THE I NBOARD AND OUTBOARD VERTICAL SUPPORTS. REPAIRED PANEL (P/N 9910073-313) PER EA 97-111757. 2 L 7 2 4F A6WE 1996111400184 19961114 00184 WP 1996 11 14 9623589986 1 19961108 A 5315 FLOOR BEAM DOUG DC9 DC932 3022066 WP BS 680 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 986US 47480 DURING H-CHECK, FOUND A 4 INCH CRACK IN THE FS 680 FLOOR BEAM AT THE RIGHT FRAME ATTACH POINT. REPLACED FLOOR BEAM (P/N 9915527-506, PSE 53.09.016) PER SRM 51-30-2, 51-30-5. 2 L 7 2 4F A6WE 1996111400185 19961114 00185 1996 11 14 SWAA961212 4 19961103 A 3417 DADC BOEING 737 7373A4 1384585 NM E/E BAY FAILED A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 677SW 23289 AFTER TAKEOFF, F/O'S AIRSPEED AND ALTIMETER INDICATORS BECAME INOPERATIVE. AIRCRAFT RETURNED TO STL AND MADE AN UNEVEN TFUL LANDING. REPLACED DIGITAL AIR DATA COMPUTER PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996111400186 19961114 00186 NM 1996 11 14 SWAA961213 1 19961104 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 1006 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 20SW 21337 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM HOLE CORROSION AT BS 1006, LBL 18.5, 22.5, 26, AND 28.5. REPAIRED PER BOE ING TI NR A53-014 AND BOEING SRM. 2 L 7 2 4F A16WE 1996111400187 19961114 00187 NM 1996 11 14 SWAA961214 1 19961104 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 1006 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 20SW 21337 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM ATTACHMENT CORROSION AT BS 967, RBL 41. REPAIRED PER BOEING TI NR A53-01 4 AND BOEING SRM. 2 L 7 2 4F A16WE 1996111400188 19961114 00188 NM 1996 11 14 SWAA961215 1 19961104 A 5241 FRAME BOEING 737 7373H4 1384600 NM GALLEY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED D-CHECK, FWD GALLEY DOOR AFT SIDE FRAME CRACKED AT NR 4 STOP FITTING CUTOUT. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996111400189 19961114 00189 NM 1996 11 14 SWAA961216 1 19961104 A 5320 FRAME BOEING 737 7373H4 1384600 NM SERV DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED D-CHECK, FWD SERVICE DOOR FRAME CUT-OUT WEB CRACKED. REPLACED DAMAGED SECTION PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996111400190 19961114 00190 NM 1996 11 14 SWAA961217 1 19961104 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 727-947.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED D-CHECK, FOUND AFT CARGO BAY FLOOR BEAM CORRODED FROM 727-947.5, RBL 13.8, WL 155.5. REPLACED DAMAGED SECTION PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996111400191 19961114 00191 NM 1996 11 14 SWAA961218 1 19961104 A 5320 CHORD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED D-CHECK, FOUND BS 178 SIDE CHORD CRACKED 1 INCH LT SIDE AT APPROXIMATELY WL 195. CUT OUT DAMAGED SECTI ON AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996111400192 19961114 00192 NM 1996 11 14 SWAA961219 1 19961104 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED D-CHECK, FOUND BS 178 PRESSURE WEB CRACKED AT WL 219, RBL 10.7. REPAIRED PER TRAMCO EWO 96-0621. 2 L 7 2 4F RT A16WE 1996111400193 19961114 00193 NM 1996 11 14 SWAA961220 1 19961104 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED D-CHECK, FOUND BS 178 PRESSURE WEB CRACKED 2 PLACES AT WL 201, RBL 4.7, AND AT WL 198, RBL 4.7. REPAIR ED PER TRAMCO EWO 96-0621. 2 L 7 2 4F RT A16WE 1996111400194 19961114 00194 NM 1996 11 14 SWAA961221 1 19961104 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED D-CHECK, FOUND BS 178 PRESSURE WEB CRACKED 2 PLACES AT WL 201, LBL 4.7, AND AT WL 198, LBL 4.7. REPAI RED PER TRAMCO EWO 96-0621. 2 L 7 2 4F RT A16WE 1996111400195 19961114 00195 NM 1996 11 14 SWAA961222 1 19961104 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 814 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED D-CHECK, FOUND FUSELAGE DENTED AT BS 814, LBL 7, WL 146, AT S28L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996111400196 19961114 00196 NM 1996 11 14 SWAA961223 1 19961104 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 390-398 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED D-CHECK, FOUND FUSELAGE DENTED BETWEEN BS 390 AND 398, BETWEEN S24 AND 25R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996111400197 19961114 00197 NM 1996 11 14 SWAA961224 1 19961104 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 415 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED D-CHECK, FOUND FUSELAGE DENTED AT BS 415, BETWEEN S24 AND 26R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996111400198 19961114 00198 NM 1996 11 14 SWAA961225 1 19961104 A 5320 CLIP BOEING 737 7373H4 1384600 NM BS 616/663/639 BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS BROKEN AT BS 616, S1, 2L, 4L, AT BS 663, S10R, S10L, AND AT BS 639, S1, 2R, AND S2L. REPLACED PER BOEING SR. 2 L 7 2 4F RT A16WE 1996111400199 19961114 00199 NM 1996 11 14 SWAA961226 1 19961104 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 1000 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 1000, UNDER S14L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996111400200 19961114 00200 NM 1996 11 14 SWAA961227 1 19961104 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORRODED AT BS 986.5, RBL 26, RBL 4-5, AND AT LBL 3-5, WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996111400201 19961114 00201 NM 1996 11 14 SWAA961228 1 19961104 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 296 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 296, RBL 54, WL 209. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996111400202 19961114 00202 NM 1996 11 14 SWAA961229 1 19961104 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 616 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, RBL 64, WL 202. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996111400203 19961114 00203 NM 1996 11 14 SWAA961230 1 19961104 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED D-CHECK, FOUND CRACKED FLOOR SUPPORT AT BS 540, RBL 2, WL 208. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996111400204 19961114 00204 NM 1996 11 14 SWAA961231 1 19961104 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 500 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996111400205 19961114 00205 NM 1996 11 14 SWAA961232 1 19961104 A 3350 20121 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 399SW 27693 DURING SCHEDULED A2 CHECK, FOUND RT WING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996111400206 19961114 00206 NM 1996 11 14 96FDEA01657 1 19961106 A 5320 65453135 CLIP BOEING 727 727233 138408A NM BS 950 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 NR 0806. FOUND STRINGER CLIP AT BS 950C STRINGER 7 RT TO BE CRACKED. *** S/D *** COMING. 2 L 7 3 4F RT A3WE 1996111400207 19961114 00207 NM 1996 11 14 96FDEA01658 1 19961106 A 5320 6519852157 WINDOW FRAME BOEING 727 727233 138408A NM BS 640-660 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 NR 0128 034. MAIN CABIN RIGHT HAND WINDOW PLUG BS 640-660 HAS EVIDENCE OF CORROSION BETWEEN PLUG AND WINDOW FRAME LOWE R AFT CORNER. *** S/D *** COMING. 2 L 7 3 4F RT A3WE 1996111400208 19961114 00208 NM 1996 11 14 96FDEA01660 1 19961108 A 2611 SMOKE DETECTOR BOEING 727 727233 138408A NM CARGO COMPT MALFUNCTIONED A FDEA O OTHER N FALSE WARNING DE DESCENT 1 SO 25 264FE 21626 ON DESCENT INTO CLE, MAIN CARGO SMOKE DETECTOR NR 2 INDICATOR FLASHED MOMENTARILY AND RANG THE BELL. OPERATIONAL CHECK OF SMOKE DETECTION SYSTEM FOUND NO DEFECTS. 2 L 7 3 4F RT A3WE 1996111400209 19961114 00209 WP 1996 11 14 96FDEA01661 1 19961105 A 5714 CTR WING SECT DOUG DC10 DC1010F 3022111 WP BS 1210 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68050 47804 SNRM 345. CORROSION FOUND ON TOP OF CTR TANK, BELOW MAIN CABIN FLOOR, LT SIDEWALL AREA, STA 1210. CLEANED CORROSION RE F. SRM 57-20-00. COMPLIED WITH HFEC INSP. NO DEFECTS NOTED. MEASURED REMAINING SKIN THICKNESS. REWORKED PER EA 8-57 10-31746 WORK INSTRUCTIONS. 11/08/96. 2 L 7 3 4F A22WE 1996111400210 19961114 00210 EU 1996 11 14 96FDEA01662 1 19961109 A 5210 HANDLE AIRBUS 310 A310203 EU R1 DOOR NOT LATCHED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 414FE 400 OUT OF FL 240 RT DOOR NOT CLOSED IN-FLIGHT. ECAM APPEARED. PRESSURIZATION WAS NOT CONSISTENT. HANDLE WAS IN FULL DOWN POSITION. UPON RETURN TO ORD OUT OF ALT 4,000 FEET, DOOR INDICATION ON ECAM WAS NORMAL. INSPECTED DOOR FOUND ALL STOP S - CAMS- ROLLERS AND TRACKS IN GOOD CONDITION. DOOR OPERATION NORMAL AFTER LUBING INTERIOR HANDLE, ROLLER AND CAM. OK TO CONT. 2 L 7 2 4F RT A35EU 1996111400211 19961114 00211 NM 1996 11 14 96FDEA01663 1 19961111 A 5320 65C8067880 ANGLE BOEING 727 727233 138408A NM BS 312-360 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 NR 640, 035, CORROSION (C53-224-01, 1) ON MOP SILL AT BS 312 TO 360, LBL 62, WL 208.1. *S/D* REMOVED AND REPLACED MOP SILL FROM BS 259 TO 360, LBL 65 WL 208.1 IAW FEDEX SRM 53-10-1, 51-30-2. 2 L 7 3 4F RT A3WE 1996111400212 19961114 00212 NM 1996 11 14 96FDEA01664 1 19961111 A 5754 651622717B BONDING JUMPER BOEING 727 727233 138408A NM NR 1 LE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 NR 398 036, CORROSION (C57-562-01-1) NR 1 K-FLAP BULLNOSE O/B BONDING JUMPER UPPER END LOWER ATTACH POINT. *S/D* REPA IRED NR 1 K-FLAP BULLNOSE O/B BONDING JUMPER UPPER END LOWER ATTACH POINT IAW FEDEX EA 7-5750-31262. 2 L 7 3 4F RT A3WE 1996111400213 19961114 00213 NM 1996 11 14 96FDEA01665 1 19961109 A 5542 657278815 BULLNOSE BOEING 727 727233 138408A NM RUDDER WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 NR 0136 037, UPPER RUDDER BULLNOSE WORN AT CONTACT POINT OF RUDDER TO VERTICAL FIN FAIRING, BEYOND LIMITS. RUDDER REMOV AL AND INSTALL REQUIRED. *S/D* REMOVED UPPER RUDDER, INSTALLED DOUBLER OVER WORN AREA IAW FEDEX SRM 55-40-3 FIG NR 1. REINSTALLED UPPER RUDDER IAW FEDEX M/M 27-20-1. 2 L 7 3 4F RT A3WE 1996111400214 19961114 00214 NM 1996 11 14 96FDEA01666 1 19961109 A 5542 657278810 BULLNOSE BOEING 727 727233 138408A NM RUDDER WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 258FE 20940 NR 0137 038, LOWER RUDDER BULLNOSE WORN AT CONTACT POINT OF RUDDER TO VERTICAL FIN FAIRING, BEYOND LIMITS. RUDDER REMOV AL AND INSTALL REQUIRED). *S/D* REMOVED LOWER RUDDER, INSTALLED DOUBLERS OVER WORN AREAS IAW FEDEX SRM 55-40-3 FIG 1, REINSTALLED RUDDER IAW FEDEX M/M 27-20-1. 2 L 7 3 4F RT A3WE 1996111400215 19961114 00215 NM 1996 11 14 DL73S962451 1 19961105 A 3350 CONTROL SWITCH 15AT48 BOEING 737 737232 1384475 NM COCPIT INOPERATIVE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 315DL 23087 EMERGENCY TRACK LIGHTS CAME ON BY THEMSELVES AND STAYED ON. REPLACED EMERGENCY LIGHT CONTROL SWITCH. OPS CKS GOOD. 2 L 7 2 4F RT A16WE 1996111400216 19961114 00216 NM 1996 11 14 DL72S962452 1 19961105 A 5240 SKIN BOEING 727 727232 1384082 NM R-1 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 485DA 20865 FOUND A .25 INCH CRACK ON THE EXTERNAL SKIN AT R-1 DOOR LWR FWD CORNER. REPAIRED PER M/M 52-12-0, PAR. 10. 2 L 7 3 4F A3WE 1996111400217 19961114 00217 WP 1996 11 14 DLL12962454 1 19961105 A 2150 132L TEMP SENSOR LKHEED 1011 1011385115 5265015 WP NR 3 PACK INOPERATIVE A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 724DA 193C1151 ON DESCENT INTO MCO, F/O COMPLAINED OF BURNING SMELL IN C- ZONE. 2 L 7 3 4F A23WE 1996111400218 19961114 00218 NM 1996 11 14 DL72W962456 1 19961029 A 5330 65C139133 SKIN BOEING 727 727247 138408F NM BS 1050 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 293WA 22111 FOUND CRACK IN THE FUSELAGE SKIN AT STA 1050 JUST OUTBOARD OF STRINGER 28R. DURING REPAIR, DISCOVERED CORROSION ON INB OARD SIDE OF SKIN. REPAIRED PER DAL ER/A 304378-14. 2 L 7 3 4F A3WE 1996111400219 19961114 00219 NM 1996 11 14 DL73E962457 1 19961022 A 5312 BULKHEAD BOEING 737 737247 138448D NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 375DL 23602 DURING INSPECTION PER SI 3-69482-12, STATION 178 BULKHEAD WAS FOUND CRACKED IN SEVERAL LOCATIONS. REPAIR ACCOMPLISHED PER ERA 304293-14 REV B. THE BULKHEAD WEB IS FABRICATED FROM 0.032 CLAD 2024-T3. 2 L 7 2 4F A16WE 1996111400220 19961114 00220 NM 1996 11 14 DL73K962459 1 19961016 A 5312 BULKHEAD BOEING 737 737232 1384475 NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 316DL 23088 STATION 178 BULKHEAD WAS FOUND CRACKED IN SEVERAL LOCATIONS. DAMAGE CUTOUTS ARE 1 INCH X 2 INCH AT RBL 4, WL 200 AND WL 203, AND LBL 4, WL 200, AND A 1 INCH BY 1 INCH AT RBL 7 WL 200. IN ADDITION TO THE WEB CRACKS, THE VERTICAL CHORD HAS A .50 INCH CRACK AT LBL 5.7 AT WL 190. REPAIR ACCOMPLISHED PER ERA 304326-14 REV A. 2 L 7 2 4F RT A16WE 1996111400221 19961114 00221 NM 1996 11 14 DL73K962460 1 19961106 A 3350 LIGHT 0L3071BPEPL BOEING 737 737232 1384475 NM CABIN INOPERATIVE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 322DL 23094 CABIN RT SIDE EMERGENCY LITE INOPERATIVE AT ROW 2D. REPLACED POWER SUPPLY. OPS CHECK OK FOR SERVICE. 2 L 7 2 4F RT A16WE 1996111400222 19961114 00222 NM 1996 11 14 DL72K962461 1 19961019 A 5330 SKIN BOEING 727 727232 1384082 NM R-4 WINDOW CTOUT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 410DA 21222 A .3750 INCH CRACK WAS FOUND IN THE R-4 WINDOW CUTOUT AT THE FWD, LWR EDGE OF THE CUTOUT. REPAIRED PER SRM 53-30-3, FIG 8, REPAIR V. 2 L 7 3 4F A3WE 1996111400223 19961114 00223 NM 1996 11 14 DL72L962464 1 19960110 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 870 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 509DA 21311 FOUND A 1.5 INCH CRACK AT LOWER END OF RT KEEL BEAM ANGLE, STATION 870. REPLACED ANGLE PER SRM 53-10-9. 2 L 7 3 4F A3WE 1996111400224 19961114 00224 NM 1996 11 14 DLM88962466 1 19961107 A 2910 HYD LINE AS15308025 DOUG MD88 MD88 3023688 NM RIGHT WORN A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 985DL 53312 RT HYD FLUID WENT TO 1 QUART AND PRESSURE ZERO CLIMBING THROUGH 14,000 FEET. FOLLOWED CHECKLIST, RETURNED TO ATL. FOUN D FORWARD LINE TO RT HYD HOUSING WORN THROUGH. REPLACED LINE, CHECKED PUMP FILTER FOR METAL, NONE FOUND. REPLACED F ILTER, LEAK AND OP CHECKS NORMAL. GEAR EXTENDED PER EMERGENCY PROCEDURE. DOORS STRUCK GROUND. INSPECTED DOORS, NO DAM AGE FOUND EXCEPT SKIDS WORN. REPLACED BOTH SKIDS. 2 L 7 2 4F RT A6WE 1996111400225 19961114 00225 NM 1996 11 14 DL72P962467 1 19961106 A 5753 652163394 SPAR BOEING 727 727225 1384077 NM NR 4 TE FLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8890Z 21859 NR 4 MID FLAP DAMAGED AT AFT SPAR I/B AFT CORNER, LOWER SIDE. REPAIRED DAMAGE PER MM 57-52-00, FIG. 808. 2 L 7 3 4F A3WE 1996111400226 19961114 00226 NM 1996 11 14 DL72L962468 1 19961107 A 5320 FRAME BOEING 727 727232 1384082 NM C3 DOOR CUTOUT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 509DA 21311 THE UPPER LEG OF THE C3 DOOR CUTOUT FWD FRAME IS CRACKED AT STA 1090, OUTBOARD OF S-27R. REPAIRED PER DAL ER/A 304414- 14AD. 2 L 7 3 4F A3WE 1996111400227 19961114 00227 NM 1996 11 14 DL73S962471 1 19961103 A 5312 651630084 BULKHEAD BOEING 737 737232 1384475 NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 321DL 23093 TWO CRACKS WERE DISCOVERED ON FWD FACE OF THE F.S.178 BLKHDWEB. TWO INDEPENDENT CUTOUTS WERE REQUIRED TO REMOVE THE CRA CKS. FIRST CUTOUT, LOCATED INBD OF THE RBL 5.7 VERTICAL STRAP AT WL 200, MEASURES 4.0 INCH VERTICALLY BY 1.0 INCH INBD/ OTBD. THE SECOND CUTOUT IS LOCATED AT THE LBL 5.7 VERTICAL STRAP AT WL 200 AND MEASURES 4.0 INCHES VERTICALLY BY 1.0 I NCH INBD/OTBD. REPAIRED PER ERA 304394-14 REV A. 2 L 7 2 4F RT A16WE 1996111400228 19961114 00228 NM 1996 11 14 DL72W962472 1 19961107 A 5320 TEE ANGLE BOEING 727 727247 138408F NM PANEL 3348L CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2819W 21057 FOUND CORROSION ON ATTACH ANGLE FOR ACCESS DOOR 3348L. REPAIRED PER MM 53-30-1. 2 L 7 3 4F A3WE 1996111400229 19961114 00229 NM 1996 11 14 DL767962475 1 19961101 A 5330 146T32413 SKIN BOEING 767 767232 1385132 NM BS 1370 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 107DL 22219 THE FUSELAGE SKIN AT F.S.1370 AND STR 39R WAS FOUND CORRODED. THE SKIN WAS CUT OUT AND REPAIRED WITH A DOUBLER. REV. A TO ER/A PROVIDES FAA APPROVAL. 2 L 7 2 4F RT A1NM 1996111400230 19961114 00230 NM 1996 11 14 DL767962476 1 19961103 A 5320 146T8220 DOUBLER BOEING 767 767232 1385132 NM BS 1445-1448 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 107DL 22219 THE FUSELAGE LT SIDE BULK CARGO DOOR INTERNAL BEARSTRAP SURROUND DOUBLER WAS FOUND WITH CORROSION BETWEEN FS 1445 AND 1448, JUST OUTBOARD AND ABOVE THE LOWER SILL OUTER CHORD ATTACHMENT. THE DOUBLER WAS BLENDED AND REINFORCED WITH A SHE ET METAL DOUBLER. REV. B TO ERA PROVIDES FAA APPROVAL. 2 L 7 2 4F RT A1NM 1996111400231 19961114 00231 NM 1996 11 14 DL767962477 1 19961029 A 5330 143T3220 SKIN BOEING 767 767232 1385132 NM BS 676 BL0 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 107DL 22219 THE FUSEALGE SKIN WAS FOUND CORRODED AT F.S. 676 BETWEEN STR'S 39L AND 39R. THE DAMAGE WAS CUT OUT AND REINFORCED WITH A DOUBLER. REV A TO ERA PROVIDES FAA APPROVAL. 2 L 7 2 4F RT A1NM 1996111400232 19961114 00232 WP 1996 11 14 DLL13962478 1 19961025 A 5711 1528390 SPAR CAP LKHEED 1011 10113851 5265010 WP LT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 784DA 193A1038 A FASTENER WAS FOUND CRACKED IN THE LT LOWER SPAR CAP AND SKIN. IT AND THE ADJACENT FASTENER HOLE WERE O/S. THE HOLES WERE COLD-WORKED AND INSTALLED WITH HI-LOKS. 2 L 7 3 4F A23WE 1996111400233 19961114 00233 NM 1996 11 14 DL72P962479 1 19961108 A 5542 657278841X SKIN BOEING 727 727225 1384077 NM RUDDER CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8890Z 21859 FOUND A 2 INCH CRACK IN THE LOWER RUDDER SKIN, MIDWAY CENTER. REPAIRED PER SRM 55-20-3. 2 L 7 3 4F A3WE 1996111400234 19961114 00234 NM 1996 11 14 DL72W962480 1 19961108 A 5320 SIDE WALL BOEING 727 727247 138408F NM BS 277 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2819W 21057 FOUND A .75 INCH CRACK AT RIGH-HAND SIDE WALL OF THE NOSE LANDING GEAR WHEELWELL. REPAIRED PER DAL ER/A 304418-14AD. 2 L 7 3 4F A3WE 1996111400235 19961114 00235 NM 1996 11 14 DL73S962481 1 19961107 A 5312 BULKHEAD BOEING 737 737232 1384475 NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 310DA 23082 STATION 178 BULKHEAD WAS FOUND CRACKED IN SEVERAL LOCATIONS. DAMAGE CUTOUTS ARE: 1INCH BY 2.5 INCH FOR RBL 5, WL 194, A ND 1INCH BY 2.0 INCH FOR LBL 5, WL 194. REPAIRED PER ERA 304373-14 REV A. 2 L 7 2 4F RT A16WE 1996111400236 19961114 00236 NM 1996 11 14 DL767962482 1 19961108 A 7120 BOLT BOEING 767 767232 1385132 NM GE CF680 CF680A2 NE NR 2 ENG MOUNT LOOSE A DALA O OTHER O OTHER IN INSP/MAINT 1 SO 27 115DA 22227 580366 NR 2 ENGINE FWD MOUNT BOLTS LOOSE. RT FWD, 50 INCH/POUNDS. RT AFT, 500 INCH/POUNDS. LT FWD, 500 INCH/POUNDS. LT AFT, 2,000 INC/POUNDS. WHICH IS THE NORMAL TORQUE. NO GAP EXISTS BETWEEN THE MATING SURFACE OF THE FWD ENGINE MOUNTS. B OLTS REPLACED AND TORQUED PER ERA 360634-14. 2 L 7 2 4F 4 F RT A1NM E13NE 1996111400237 19961114 00237 NM 1996 11 14 DL72S962483 1 19961108 A 3350 BATTERY PACK 6013211 BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 519DA 21470 SEVERAL OUTSIDE EMERGENCY LIGHTS INOPERATIVE. C/A REPLACED BATTERY RACK M982. REPLACED BATTERY RACK M982, M955 AND B ATTERY PACK M654. EMERGENCY LIGHTS OPS CHECKED GOOD. 2 L 7 3 4F A3WE 1996111400238 19961114 00238 NM 1996 11 14 DL73K962484 1 19961108 A 3350 BPS73 CHARGER BOEING 737 737232 1384475 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 309DL 23081 SEVERAL EMERGENCY OVERHEAD ASILE LIGHTS INOP. REPLACED CHARGER ASSEMBLY 2 L 7 2 4F RT A16WE 1996111400239 19961114 00239 NM 1996 11 14 DLM11962491 1 19961107 A 2740 42164R13 GEARBOX 42164R13 DOUG MD11 MD11 3023602 NM IAE V2528 V2528D5 NE HORZ STAB TRIM MALFUNCTION A DALA O OTHER F FLT CONT AFFECTED DE DESCENT 1 SO 27 814DE 48769 020007 WHEN SLATS EXTENDED ON DESCENT, UNABLE TO CHANGE STABILIZER TRIM, ELECTRICAL OR MANUALLY. CHANGED A/P NO HELP. WHEN A/P ENGAGED, A STAB OUT OF TRIM DEU WARNING WAS DISPLAYED. CONFIG PAGE SHOWED 1.0 ANU AND AFT PRESSURE NEEDED TO CONTROL A LTITUDE. LANDING AT FFO NORMAL AT 35 DEGREES, FLAPS WITH HIGHER THAN NORMAL BACK PRESSURE NEEDED FOR APPROACH. ADDITIO NAL PARTS INFO DAL 27001480 S/N OFF UNKNOWN. DAL 27001511 S/N OFF DCA 708. DAL 270201800 NO S/N. 2 L 7 3 4F 4 F RT A22WE E40NE 1996111400240 19961114 00240 WP 1996 11 14 SCNA96369 1 19961018 A 5320 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP BS 879 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT ON THE LEFT SIDE OF THE P-LIFT, APPROXIMATELY BS 879, OUTBOA RD SIDE OF THE FLOOR BOARD. REMOVED CORRODED MATERIAL, FABRICATED AND INSTALLED A REPAIR IN ACCORDANCE WITH ENGINEERING AUTHORIZATION INSTRUCTIONS. 2 L 7 3 4F A22WE 1996111400241 19961114 00241 WP 1996 11 14 SCNA96370 1 19961018 A 5320 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP BS 839 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT ON THE LEFT SIDE OF THE P-LIFT, APPROXIMATELY BS 839, INBOARD SIDE OF THE FLOOR BOARD. REMOVED CORRODED MATERIAL, FABRICATED AND INSTALLED A REPAIR IN ACCORDANCE WITH ENGINEERING A UTHORIZATION INSTRUCTIONS. 2 L 7 3 4F A22WE 1996111400242 19961114 00242 WP 1996 11 14 SCNA96371 1 19961019 A 2730 ACTUATOR ROD DOUG DC10 DC1010 3022110 WP LT ELEVATOR CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON THE LEFT HAND ELEVATOR ACTUATOR ROD. REMOVED AND REPLACED LEFT HAND ELEVAT OR ROD IN ACCORDANCE WITH MM 27-33-01. 2 L 7 3 4F A22WE 1996111400243 19961114 00243 WP 1996 11 14 SCNA96372 1 19961021 A 5320 S2929169 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP BS1964 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON THE FLOOR SUPPORT AT BS 1964, RBL 39. REMOVED CORRODED FLOOR SUPPORT, FABR ICATED, AND INSTALLED A NEW FLOOR SUPPORT IN ACCORDANCE WITH SRM 51-30-00. 2 L 7 3 4F A22WE 1996111400244 19961114 00244 WP 1996 11 14 SCNA96373 1 19961022 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP BS 420 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON SEAT TRACK AT BS 420, LBL 53. REMOVED CORROSION, FABRICATED AND INSTALLED A REPAIR IN ACCORDANCE WITH ENGINEERING AUTHORIZATION INSTRUCTIONS. 2 L 7 3 4F A22WE 1996111400245 19961114 00245 WP 1996 11 14 SCNA96374 1 19961103 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1997 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON OVERHEAD GILL LINER SUPPORT AT BS 1997, RBL 18. REMOVED CORROSION, FABRICA TED AND INSTALLED A REPAIR IN ACCORDANCE WITH SRM 53-00-01. 2 L 7 3 4F A22WE 1996111400246 19961114 00246 WP 1996 11 14 SCNA96375 1 19961104 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1361 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 DURING HEAVY MAINTENANCE, FOUND CORROSION ON CENTER WING BOX UPPER SKIN FRM RBL 30 TO RBL 80 AT BS 1361, AT AFT SPAR. O PENED ACCESS TO CENTER WING BOX, REMOVED CORROSION, INSTALLED NEW FASTENERS, AND PERFORMED LEAK CHECKS IN ACCORDANCE WIT H ENGINEERING AUTHORIZATION INSTRUCTIONS. 2 L 7 3 4F A22WE 1996111400247 19961114 00247 NM 1996 11 14 DHL96715004 1 19961105 A 3310 10602041 LIGHT SOCKET BOEING 727 727155C 138404Z NM LT COCKPIT FAILED A DHLA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 01 715DH 19618 CREW SMELLED SMOKE INSIDE THE COCKPIT, BUT WAS NOT ABLE TO LOCATE ITS SOURCE. REMOVED AND REPLACED LEFT HAND UPPER F/E' S DESK TABLE LIGHT SOCKET. OPS CHECK OKAY. 2 L 7 3 4F A3WE 1996111400248 19961114 00248 NM 1996 11 14 DHL96721008 1 19961106 A 3260 656021132 ACCESSORY UNIT BOEING 727 727228 NM LANDING GEAR FAILED A A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 721DH 19545 AFTER TAKEOFF FROM MSP COULD NOT SELECT GEAR LEVER PAST OFF. WENT THROUGH ALT PROC. NR 2 GEAR LEVER WILL NOT GO UP PA ST OFF AND ALT. PROC #3. A/C SYSTEMS IN GROUND MODE - ALL INDICATIONS ARE THE A/C IS STUCK IN GROUND MODE. REPLACED LANDING ACCY UNIT - OPER. TEST CHK. PER MM 32-09-121. OK. AFTER BLOCK IN, SHUT ENGINES DOWN, ON APU, GOT ELECTRICAL SMO KE IN COCKPIT, SHUT DOWN GASPER, PACKS AND APU, SMOKE STOPPED. REF. TO IT-1 PACK COOLING DOORS CLOSED DUE ACCY UNIT FA ILED - OPER. PACKS PER 21-50. OPER. OK. 2 L 7 3 4F A3WE 1996111400249 19961114 00249 NM 1996 11 14 VNAA9611003 1 19961108 A 6123 AUTOFEATHER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ENGINE MALFUNCTIONED A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 07 460PS 3061 AUTOFEATHER DID NOT ARM ITSELF DURING TAKEOFF, ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE PERFORMED GROUND RUN A ND AUTOFEATHER OPERATIONAL CHECK, NO DEFECTS NOTED. AIRCRAFT APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996111400250 19961114 00250 SO 1996 11 14 SRAA961106 1 19961106 A 5320 3431947 STRUT LKHEED 382 382G 526414U SO BS 858 CRACKED A SRAA K NONE O OTHER IN INSP/MAINT 1 GL 23 920SJ 4561 ON POST-FLIGHT INSPECTION, FOUND VERTICAL STRUT BRACE ON RHS AT FUSELAGE STATION 858 CRACKED. REPLACED STRUT ASSEMBLY P ER M.M. CH 53. 2 H 7 4 4T A1SO 1996111400251 19961114 00251 NE 1996 11 14 CA960403103 2 19960326 A 7230 BLADE BOEING 737 737242C 1384478 NM PWA JT8 JT8D9A 52048 NE COMPRESSOR DAMAGED W K NONE C F.O.D. TX TAXI/GRND HDL 1 CA 53161 3665 674383 (CAN)#1 ENGINE FOUND WITH FOD DURING TURN AROUND. TAKEN TO HANGAR, FOD WORK CARD CARRIED OUT. BOROSCOPE DETERMINED ENGIN E BLADE DAMAGE TO THE FIRST STAGE EXTENDED TO 6, 7 AND 13TH STAGES. ENGINE CHANGED, F IRST STAGE VISUAL DAMAGE TO 4 BLOC KS; NICKS AND ONE DEEP L.E. GAUGE. 2 L 7 2 4F 4 F A16WE E2EA 1996111400252 19961114 00252 EA 1996 11 14 CA960404001 2 19960328 A 7260 310063901 RGB BEARING BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA L/H ENG NR 5 MAKING METAL W K NONE J WARNING INDICATION IN INSP/MAINT 1 CA 2882 2882 CPPS60876 (CAN)#1 CHIP DETECTOR (L/H SIDE) IN REDUCTION GEARBOX ILLUMINATED. CHIP DETECTOR WAS INSPECTED, AND SMALL AMOUNT OF META L PARTICLES WERE FOUND. CHIP DETECTOR WAS CLEANED AND RE-INSTALLED INTO GEARBOX ASSEM BLY. THE ENGINE WAS STARTED AND MO NITORED, AND ONCE AGAIN, THE LIGHT ILLUMINATED. THE CHIP DETECTOR WAS REMOVED AND LARGE METAL PARTICLES WERE FOUND. THE RGB WAS REMVOED FROM AIRCRAFT, AND IT WAS DISCOVERED AT THIS POINT THAT #5 BEARING WAS CAUSE OF METAL CONTAMINATION. RGB WILL BE REPAIRED AS PER PRATT & WHITNEY OVERHAUL MANUAL. 3017043 R18 (POST SB 5292) BEARING WILL BE INSTALLED. 1 G 7 1 4U 4 U H4SW E22EA 1996111400253 19961114 00253 CE 1996 11 14 CA960404004 1 19960327 A 7922 53E19600 THERMO VALVE CESSNA 172 172M 2072418 CE LYC O320 O320E2D 41508 EA ENGINE LOOSE NUT W K NONE O OTHER IN INSP/MAINT 1 CA 1190 L3657127A (CAN)INSPECTION AS PER LYCOMING SB 518A FOUND NUT CRIMPED ONLY ON ONE SIDE AND EXTREMELY LOOSE. 1 H 7 1 3O 3 O NT 3A12 E274 1996111400254 19961114 00254 SW 1996 11 14 CA960404006 1 19960322 A 2750 2781032117 LINE SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP FLAP DOWN LINE CHAFED W O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 CA 27280 P54158 (CAN)HYDRAULIC FLUID BEING LOST NOTED BY CREW. INVESTIGATION FOUND THE RIGHT HAND WING ROOT FLAP DOWN LINE HAD CHAFED T HROUGH. THIS IS A 1/4 INCH ALUMINUM LINE. A STAINLESS STEEL REPLACEMENT WAS MADE. THI S LINE IS IN AREA BEHIND AIR CYCLE MACHINE AND HEAT EXCHANGER AND IS DIFFICULT TO INSPECT. OTHER FACTORS POSSIBLY CONTRIBUTING TO LINE WEAR: PROP BALANCE NOT REQUIRED DURING EARLY HISTORY OF AIRCRAFT, AND FLAT HYDRAULIC ACCUMULATOR ALLOWING LINES TO "BUZZ". THERE IS NO EXTE RNAL PRESSURE GAUGE ON ACCUMULATOR THUS PRESSURE CAN ONLY BE CHECKED USING NITROGEN SERVICING BOTTLE. 2 L 7 2 4T 4 T RT A8SW E4WE 1996111400255 19961114 00255 SW 1996 11 14 CA960404010 1 19960314 A 7603 206061745001 CONTROL TUBE BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL THROTTLE CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA CAE820018 (CAN) DURING ANNUAL INSPECTION SLIGHT BULGING AND PITTING FOUND ON THROTTLE CONTROL TUBE. DURING FURTHER INSPECTION THE TUBE BROKE. THE INTERIOR OF THE TUBE WAS FILLED WITH CORROSION AND THE THICKNESS OF THE TUBE WAS EXTREMELY THIN AT THE B RAKE AREA. 1 G 7 1 3U 3 U H2SW E4CE 1996111400256 19961114 00256 EA 1996 11 14 CA960404012 2 19960214 A 8530 PISTON PIN PLUG BEECH 80 65B80 1152812 CE LYC O540 IGSO540A1D 41532 EA #1 CYLINDER DESTROYED W E ENGINE SHUTDOWN Y ENGINE STOPPAGE CR CRUISE 1 CA 31 RL370750 (CAN)LEFT ENGINE FAILED AFTER ONLY 31 HOURS AFTER OVERHAUL. FACTORY NEW CYLINDERS WERE INSTALLED AT OVERHAUL. ENGINE GRA DUALLY LOST RPM. OIL FILTER AND PROP GOVERNOR SCREEN WERE FOUND TOTALLY PLUGGED WITH ALUMINUM FROM THE AFT PISTON PIN P LUG ON THE #1 CYLINDER. PIN WAS CHAMFERRED BY CONTACT WITH THE CYLINDER WALL. UPPER TWO RINGS AND LANDS WERE UNDAMAGED, SO DETONATION IS UNLIKELY. MEASUREMENTS ARE BEING TAKEN TO DETERMINE IF THERE IS A MISALIGNMENT OF CONNECTING ROD BUSHIN GS. 1 L 7 2 3O 3 O 3A20 1E7 1996111400258 19961114 00258 EA 1996 11 14 CA960408502 1 19960301 A 2750 855D1005 SENSOR UNIT EEMCO CNDAIR CL600 CL6002B19 EA LEFT BRAKE FAILED W O OTHER F FLT CONT AFFECTED DE DESCENT 1 CA 250 (CAN)AT 15,000 FEET FLAP FAIL MESSAGE. QRH CHECK LIST COMPLETED. FLAPLESS LANDING CARRIED OUT. CHANGED LEFT BRAKE AND PO SITION SENSOR UNIT. 2 L 7 2 4F RT A21EA 1996111400259 19961114 00259 NM 1996 11 14 CA960408503 1 19960301 A 5540 173U10203 STIFFENER BOEING 747 747433 NM RUDDER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN)LOWER RUDDER, LOWER HINGE STIFFENER FITTING CRACKED. REPLACED. 2 L 7 4 4F RT A20WE 1996111400261 19961114 00261 EA 1996 11 14 CA960408505 1 19960308 A 2750 WIRE CNDAIR CL600 CL6002B19 1900309 EA FLAPS BROKEN W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA 1477 (CAN)ON APPROACH, FLAPS FAIL MESSAGE ON EICAS, FLAPS STOPPED AT 20 DEGREES. PREVIOUS WIRE REPAIR FOUND BROKEN AGAIN. NEW ELECTRICAL HARNESS INSTALLED. 2 L 7 2 4F RT A21EA 1996111400262 19961114 00262 NM 1996 11 14 CA960408507 1 19960318 A 5540 173U0203 STIFFENER BOEING 747 747433 NM RUDDER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN)LOWER RUDDER, LOWER HINGE STIFFENER FITTING CRACKED. REPLACED. 2 L 7 4 4F RT A20WE 1996111400263 19961114 00263 SO 1996 11 14 CA960409001 1 19960402 A 7920 PRESURE LINE LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL NR 2 ENG OIL CRACKED W E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA 500859 (CAN)IN CRUISE, LOW OIL QUANTITY LIGHT ILLUMINATED FOR THE #2 ENGINE. ENGINE WAS SHUT DOWN AND AIRCRAFT LANDED. MAINTENA NCE INVESTIGATION CONFIRMED CRACKED OIL PRESSURE LINE. LINE REPLACED. 2 H 7 4 4T 4 T A1SO E282 1996111400266 19961114 00266 SO 1996 11 14 CA960409026 2 19960325 A 8520 CRANKCASE BEECH 95 95B55 1152729 CE CONT O470 IO470L 17026 SO RT ENG CRACKED W K NONE K FLUID LOSS UK UNKNOWN 1 CA 1787 237685R (CAN)AN OIL LEAK ON THE RIGHT HAND ENGINE WAS REPORTED. A SUBSEQUENT INSPECTION REVEALED A CRACK IN THE CRANKCASE APPROX IMATELY 3 1/2" LONG, FORWARD OF THE #5 CYLINDER. THE CAUSE OF THE CRACK IS NOT KNOWN.ENGINE REPLACED AND AIRCRAFT RETURN ED TO SERVICE. 1 L 7 2 3O 3 O RT 3A16 3E1 1996111400267 19961114 00267 EA 1996 11 14 CA960409028 1 19960327 A 5311 C2FS3203A FRAME DHAV DHC2 DHC2MK1 2800102 EA PWA R985 R985AN14B 52008 NE LOWER TUBE CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 13421 19458 (CAN)IN ACCORDANCE WITH SB 2/49 INSPECTION REVEALED SEVERAL TUBES (5) BELOW MINIMUM REQUIREMENTS. CAGE REMOVED FOR REPA IR. DISASSEMBLY REVEALED FURTHER DAMAGE. TOP LATERAL MEMBERS WERE BENT REARWARD REQUIRING REPAIRS TO INSTRUMENT PANEL CE NTRE SUPPORT MEMBERS. BOTTOM LH LOWER ATTACH BOLT P/N C2FS3871 WAS DEFORMED DUE TO SHEAR LOAD. NO INDICATION OF ACC IDENT. 1 H 7 1 3R 3 R A806 5E1 1996111400268 19961114 00268 1996 11 14 CA960409029 4 19960326 A 6122 6505680 GOVERNOR CVAC 340 340CVAC 242270A WP ALLSN 501D 501D13 03004 GL ALLSN A6441 A6441FN606 GL R/H PROP FLUCTUATES W E ENGINE SHUTDOWN O OTHER AP APPROACH 1 CA 501662 WY12504 (CAN)DURING A FLIGHT TEST, COMING OFF FINAL APPROACH, THE RIGHT HAND PROPELLER STARTED FLUCTUATING BETWEEN 13300 AND 144 00 RPM. THE R/H ENGINE WAS SHUT DOWN AND THE AIRCRAFT LANDED WITHOUT INCIDENT. THE PROPELLER WAS REMOVED AND SENT FOR IN SPECITON/OVERHAUL. 2 L 7 2 4R 4 T 6A6 E282 6 C P898 1996111400269 19961114 00269 EA 1996 11 14 CA960412002 2 19960328 A 7414 10682014 GEAR ELECTROSYS 1038255514 CESSNA 172 172N 2072434 CE LYC O320 O320H2AD 41508 EA LT MAG SHEARED TEETH W A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 CA 433 433 4111555 L212176T (CAN)IN CRUISE, ENGINE SUDDENLY RAN ROUGH AND RPM DROPPED. MAG CHECK INDICATED LEFT MAG DEAD. MAGNETO REMOVED FOR TEST. PLASTIC GEAR HAD 12 TEETH SHEARED OFF. THIS MAG HAD BEEN OVERHAULED BY REPAIR STATIONUT2R226L. 1 H 7 1 3O 3 O NT 3A12 E274 1996111400270 19961114 00270 SW 1996 11 14 CA960412003 1 19960401 A 6322 1321011 FAN BELL 204 204B 1181404 SW LYC T53 T5313B 41549 NE COOLING BEARING FAILED W K NONE E VIBRATION/BUFFET IN INSP/MAINT 1 CA LE07751 (CAN) TURBINE AND FAN ASSEMBLY MAKING NOISE AND VIBRATION. BEARING P/N 9101 PP FOUND DRY. 1 G 7 1 4U 4 U H1SW E17EA 1996111400271 19961114 00271 EU 1996 11 14 CA960412005 1 19960331 A 6210 BLADE AEROSP SA316 SA315B 8680615 EU MAIN ROTOR VIBRATING W K NONE E VIBRATION/BUFFET IN INSP/MAINT 1 CA (CAN)MAIN ROTOR BLADES WERE REMOVED TO DO HIGH VERTICAL VIBRATION. ALTHOUGH TRACK WAS OK, THE VIBRATION SEEMED TO GET PR OGRESSIVELY WORSE. REPLACEMENT BLADES P/N 3160S-13-65-000-00 WERE INSTALLED AND PROBL EM WAS ALLEVIATED. 1 G 7 1 4U H1IN 1996111400272 19961114 00272 SW 1996 11 14 CA960412009 1 19960320 A 7603 C8102413 CABLE SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP LT POWER LEVER BROKEN W O OTHER O OTHER TX TAXI/GRND HDL 1 CA 26551 P54183 (CAN)LEFT HAND POWER LEVER FOUND LOOSE AT START BUT DID NOT AFFECT ENGINE POWER. LEFT POWER LEVER CABLE, INNER RIBBON FO UND BROKEN JUST FORWARD OF THE PEDESTAL. THIS CABLE HAS AN UPPER AND LOWER ASSEMBLY. UPPER ASSEMBLY REPLACED. IN ADDITI ON, CABLE RE-ROUTED TO ALLOW FOR THE LEAST AMOUNT OF FLEX. 2 L 7 2 4T 4 T RT A8SW E4WE 1996111400273 19961114 00273 SW 1996 11 14 CA960412010 1 19960401 A 6220 204011140005 DRAG BRACE BELL 205 205A1 1181414 SW LYC T53 T5313B 41549 NE DRAG BRACE NUT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1904 LEO7186X (CAN) DURING A SCHEDULED 1200 HOUR INSPECTION OF THE DRAG BRACE ASSEMBLY, THE NUT 204-011-144-003 WAS FOUND TO HAVE A LO NGTITUDINAL CRACK ACROSS THE OUTSIDE SURFACE. 1 G 7 1 4U 4 U H1SW E17EA 1996111400274 19961114 00274 SW 1996 11 14 CA960412011 1 19960401 A 6520 2120404621 OUTPUT SHAFT BELL 212040004005 BELL 205 205A1 1181414 SW T/R CONE AREA CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 2609 (CAN)DURING PREMATURE OVERHUAL INCLUDING A MAGNAFLUX OF THE OUTPUT DRIVESHAFT, A CRACK WAS DETECTED ON THE SHAFT IN THE TAIL ROTOR CONE AREA, JUST INBOARD OF THE SPLINES SUPPORTING THE TAIL ROTOR YOKE. THECRACK EXTENDED FOR 0.5 INCHES IN A CIRCUMFERENTIAL DIRECTION AND OUTBOARD ALONG THE SPLINES FROM BOTH ENDS OF CRACK. 1 G 7 1 4U H1SW 1996111400276 19961114 00276 SW 1996 11 14 CA960412013 1 19960308 A 6210 K911001003005 BLADE KAMAN K1200 K1200 05625F6 SW LYC T53 T5317A 41549 NE M/R CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 295 LR81008 (CAN) BLADES ARE MATCHED PAIRS. BLADE 1 - CHORDWISE CRACKS 10 INCHES LONG AT STN. 19 AND 75. BLADE 2 DIAGONAL CRACK AT S TN. 15. CRACKS COULD NOT BEEN SEEN WITH BLADES AT REST AND UNDER OWN WEIGHT. FUTURE INSPECTIONS WILL BE WITH BLADE TIP S UPPORT. 1 G 7 1 4F 4 U NT TR7BO E17EA 1996111400277 19961114 00277 NM 1996 11 14 CA960412014 1 19960327 A 3232 82910016009 ACTUATOR DHAV DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NOSE LDG GEAR FAILED W O OTHER J WARNING INDICATION AP APPROACH 1 CA PCE120542 (CAN)ON APPROACH GEAR SELECTED DOWN BUT NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON. ALTERNATE EXTENSION CARRIED OUT SUCC ESSFULLY. NOSE GEAR DOOR ACTUATOR REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1996111400278 19961114 00278 EA 1996 11 14 CA960412015 1 19960315 A 7720 3028289 T5 HARNESS DHAV DHC6 DHC6300 EA PWA PT6 PT6A27 52043 EA ELECT.TERMINAL GROUNDED W D RETURN TO BLOCK O OTHER CR CRUISE 1 CA PCE40583 (CAN)T5 TEMPERATURE DROPPED TO ZERO WHILE IN CRUISE. ELECTRICAL TERMINAL GROUNDED ON T5 HARNESS. HARNESS REPLACED. 1 H 7 2 3T 4 T A9EA E4EA 1996111400279 19961114 00279 NM 1996 11 14 CA960412016 1 19960308 A 5210 8SC0156 GAS SPRING DHAV 85210002001 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE PAX DOOR LOW PRESSURE W B EMER. DESCENT O OTHER DE DESCENT 1 CA 0010297 PCE120265 (CAN)PASSENGER DOOR MECHANISM UNLOCKED DURING FLIGHT CAUSING A DEPRESSURIZATION. FAILURE WAS DUE TO LOW PRESSURE ON GAS SPRING. 2 H 7 2 4T 4 T RT A13NM E20NE 1996111400281 19961114 00281 EU 1996 11 14 CA960412018 1 19960402 A 2840 MONITOR LIGHT BOLKMS 105 BO105C 5626005 EU ALLSN 250C 250C20B 03013 GL CENTRE CONSOLE CHAFED W K NONE J WARNING INDICATION CR CRUISE 1 CA CAE835696 (CAN) MAIN FUEL PUMP SWITCH MONITOR LIGHT WOULD BE ON INTERMITTENTLY. FOUND WIRES CHAFED AGAINST VERTICAL CONSOLE POST. THIS WAS A COMPANY APPROVED MODIFICATION. 1 G 7 2 3U 3 U H3EU E4CE 1996111400282 19961114 00282 NM 1996 11 14 CA960412019 1 19960313 A 2910 82970410119 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE FIREWALL HYD FAILED W A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 CA 120543 (CAN)IN CLIMB #2 HYDRAULIC QUANTITY INDICATOR BEGAN FALLING. THIS FOLLOWED BY PRESSURE LOSS IN SYSTEM. INSPECTION FOUND A HYDRAULIC LINE FAILURE AT THE FLARE. BRAD ADVISED. 2 H 7 2 4T 4 T RT A13NM E20NE 1996111400283 19961114 00283 EU 1996 11 14 CA960412020 1 19960403 A 3246 DSR46291006 BEARING DUNLOP AHA1837 BAG JETSTM JETSTM4112 EU #4 OUTER MAIN FAILED W A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA RH086 (CAN)PILOT RPORTED ANTI-SKID FAIL CAPTION LIGHT ON DURING TAXI. #4 OUTER MAIN WHEEL BEARING FAILED AND TORE THE ANTI-SKI D TRANSDUCER DRIVE CUP FROM THE HUB CAP. 1 L 7 2 4T RT A196 1996111400284 19961114 00284 SW 1996 11 14 CA960412021 1 19960327 A 2910 70010H060A180 HOSE ASSEMBLY BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL HYD PWR PACK FRACTURED W K NONE O OTHER IN INSP/MAINT 1 CA CAE820757 (CAN)HYDRAULIC LINE FROM MALE QUICK DISCONNECT TO HYDRAULIC POWER PACK (PRESSURE LINE, PACK TO FILTER). LINE FOUND FRACT URED INTERNALLY (FLEX LINE), AT AREA WHERE IT IS CLAMPED TO CABIN ROOF/PYLON FLOOR. 1 G 7 1 3U 3 U H2SW E4CE 1996111400285 19961114 00285 NM 1996 11 14 CA960415001 1 19960411 A 5230 SEAL DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE BAGGAGE DOOR DAMAGED W O OTHER W INADEQUATE Q C CR CRUISE 1 CA 120832 (CAN)PARTIAL LOSS OF PRESSURIZATION CONTROL. BAGGAGE DOOR SEAL FOUND DAMAGED AND LEAKING. 2 H 7 2 4T 4 T RT A13NM E20NE 1996111400286 19961114 00286 NM 1996 11 14 CA960415002 1 19960411 A 5620 85323917001 WINDOW DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE CABIN LH FORWARD CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 120855 (CAN)LEFT HAND FORWARD CABIN WINDOW FOUND CRACKED. 2 H 7 2 4T 4 T RT A13NM E20NE 1996111400287 19961114 00287 EU 1996 11 14 CA960415003 1 19960411 A 5620 HC562H00070 WINDOW BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE LEFT HAND CABIN CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA LF05567A (CAN)PASSENGER WINDOW ON LEFT HAND SIDE IS CRAZED WITH EVIDENCE OF A CRACK DEVELOPING. 2 H 7 4 4F 4 F RT A49EU E6NE 1996111400288 19961114 00288 NM 1996 11 14 CA960415004 1 19960411 A 7921 28E997 OIL COOLER STWARNER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE #2 ENG LEAKING W K NONE J WARNING INDICATION IN INSP/MAINT 1 CA 13559 108 120657 (CAN)#2 ENGINE OIL COOLER LEAKING. REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1996111400289 19961114 00289 NM 1996 11 14 CA960415005 1 19960411 A 2435 23088002A GENERATOR LUCAS DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE #1 START/GEN FAILED W O OTHER H ELECT. POWER LOSS-50 PC CR CRUISE 1 CA 11135 1485 362A 120854 (CAN)#1 DC GENERATOR OFF LINE. STARTER GENERATOR REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1996111400290 19961114 00290 EU 1996 11 14 CA960415006 1 19960411 A 2436 700122490420 CONTROL UNIT PLESSEY BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE #1 DC GENERATOR INTERNAL FAILURE W O OTHER H ELECT. POWER LOSS-50 PC CR CRUISE 1 CA 13942 4495 TE0814 LF05539A (CAN)#1 GENERATOR FAILED. FOUND GENERATOR CONTROL UNIT HAD INTERNAL FAILURE. REPLACED GCU. 2 H 7 4 4F 4 F RT A49EU E6NE 1996111400291 19961114 00291 NM 1996 11 14 CA960415007 1 19960410 A 7603 POWER LEVERS DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE BOTH ENG OVERSPEED W A O L E OTHER ABORTED APPROACH ENGINE SHUTDOWN Y ENGINE STOPPAGE DE DESCENT 1 CA 1178 120165 (CAN)ON APPROACH IN SEVERE TURBULENCE, THE PILOT ATTEMPTED TO REDUCE POWER TO IDLE. BOTH PROPS WENT INTO AN OVERSPEED CO NDITION IN EXCESS OF 1500 RPM. ZERO TORQUE INDICATION. POWER TO #1 ENGINE RECOVERED B UT #2 FAILED AND WAS SHUTDOWN. IT IS BELIEVED THAT TURBULENCE CAUSED THE PILOT TO PULL BOTH POWER LEVERS INTO THE INCORRECT RANGE CAUSING THE OVERSPEED. B OTH ENGINES AND PROPS WERE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1996111400293 19961114 00293 SW 1996 11 14 CA960415010 1 19960215 A 3297 WIRE SWRNGN SA226 SA226TC 8780404 SW UP LOCK HARNESS BROKEN W O OTHER O OTHER CL CLIMB 1 CA (CAN)LANDING GEAR WOULD CYCLE UP AND DOWN AS IT RETRACTED INTO NACELLE. ALSO GEAR CB WOULD BLOW. FOUND BROKEN WIRE IN IN BOARD LH NACELLE UP LOCK HARNESS. CLAMP HAD BEEN MOUNTED UPSIDE DOWN ALLOWING CAM TO INTERFERE WITH HARNESS. WIRE WOULD GROUND AS MAIN GEAR ENTERED NACELLE. 2 L 7 2 4T RT A8SW 1996111400294 19961114 00294 NE 1996 11 14 CA960415011 2 19960410 A 7321 7911006091 EEC AIRBUS 310 A310324 3930206 EU PWA 4152 PW4152 NE NR 2 ENG FAILED W A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 717709 (CAN)ON TAKEOFF AND INITIAL CLIMB, #2 EPR FAIL LIGHT ILLUMINATED INTERMITTENTLY WITH ECAM MESSAGE. AFTER POWER REDUCTION ON #2, LOUD NOISES ASSOCIATED WITH EPR FLUCTUATIONS UNTIL N1 MODE WAS SELECTED IN AC CORDANCE WITH QRH. ONCE THE ENGINE SELECTED IN N1 MODE, ALL READINGS RETURNED TO NORMAL. ELECTRONIC ENGINE CONTROL (EEC) AND FUEL METERING UNIT REPLACED. 2 L 7 2 4F RT A35EU E24NE 1996111400295 19961114 00295 WP 1996 11 14 CA960415013 1 19960328 A 7830 12119041 AIR MOTOR AIRSEARCH 12119041 LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB21122B02 54555 NE NR 1 T/R SEIZED W O OTHER O OTHER LD LANDING 1 CA P1131 10285 (CAN)DURING LANDING AFTER THRUST REVERSER OPERATION, #1 THRUST REVERSER JAMMED IN THE DEPLOY POSITION. UPPER RH COWL TRA NSLATING ROD BENT AND CRACKED. #1 SCREW JACK BENT. BOTH DRIVE CABLES SHEARED AT AIR MOTOR AND MOTOR SEIZED. PARTS REPL ACED. 2 L 7 3 4F 4 F A23WE E12EU 1996111400296 19961114 00296 NM 1996 11 14 CA960415014 1 19960404 A 3510 3800170 OXYGEN LINE BOEING 757 75723A 1384967 NM OBSERV CONSOLE BLOWN W K NONE O OTHER IN INSP/MAINT 1 CA 13260 (CAN)LOW PRESSURE OXYGEN LINE BLOWN. LINE CHAFING ON AN ELECTRICAL WIRE BUNDLE'S TYE WRAP LOCATED ALONG FUSELAGE UNDER FIRST OBSERVER CONSOL, BRADING CUT. REPAIRED. 2 L 7 2 4F RT A2NM 1996111400316 19961114 00316 EA 1996 11 14 96ZZZX5602 2 19961023 A 7230 ENGINE DHAV DHC7 DHC7103 2802710 EA PWA PT6 PT6A50 52043 EA NR 3 OIL LEAK A ROSA A I H UNSCHED LANDING CABIN DEPRESSURIZATION DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 01 54026 106 PCE86466 AIRCRAFT CABIN FILLED WITH VAPOR IMMEDIATLEY AFTER TAKEOFF. ENGINE BLEED AIR WAS SHUT OFF AND CABIN PRESSURIZATION WAS DUMPED. AIRCRAFT RETURNED TO LAS. FOUND NR 3 ENGINE LEAKING OIL FROM COMPRESSOR INTAKE. FERRIED AIRCRAFT TO ABQ FOR E NGINE CHANGE. FURTHER INFORMATION PENDING. 2 H 7 4 4T 4 T A20EA E4EA 1996111400322 19961114 00322 EU 1996 11 14 AWXA960558 1 19961005 A 3350 321420 BATTERY PACK AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 624AW 10872 55 PHX - FLT 146 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS AT ROWS 13, 17, 19, 24, AFT GALLEY AREA AND L-2 AND R-2 DOORS FAILED EMERGENCY BATTERY TEST. REMOVED AND REPLACED BATTERY PACK. REMOVED AND REPLACED BATTERY CHARGER. OPERATIONS CHECKED GOOD. (M) 2 L 7 2 4F RT A28NM 1996111400323 19961114 00323 EU 1996 11 14 96ZZZM1482 1 19961005 A 3350 321420 BATTERY CHARGER AIRBUS 320 A320231 3930325 EU CABIN INOP A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 624AW 0728 55 PHX - FLT 146 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS AT ROWS 13, 17, 19, 24, AFT GALLEY AREA AND L-2 AND R-2 DOORS FAILED BATTERY TEST. REMOVED AND REPLACED BATTERY PACK. REMOVED AND REPLACED BATTERY CHARGER. OPERATIO NS CHECK GOOD. REFERENCE AWXA960558. 2 L 7 2 4F RT A28NM 1996111400324 19961114 00324 NM 1996 11 14 96ZZZM1483 1 19960917 A 2560 80330033 DOOR ASSIST BOTT BOEING 747 747282B 1384860 NM L1 DOOR EMPTY A TWRA K NONE O OTHER NR NOT REPORTED 1 EA 15 611FF 0612 20502 INADVERTENTLY, L1 DOOR WAS OPENED WHILE IN AUTO MODE SLIDE DEPLOYED. PERFORMED INSPECTION PER 5-51-23. REPLACED SLIDE AT L21 DOOR PER TC 25-665-1L AND REPLACED DOOR ASSIST BOTTLE AT L1 DOOR PER WIC 25-615-4-2. OPERATIONAL CHECKED NORMAL. AIRCRAFT RETURN TO SERVICE. REFERENCE TWRA96215. 2 L 7 4 4F A20WE 1996111400325 19961114 00325 WP 1996 11 14 HALA96129 1 19960903 A 3350 CONTROL MODULE DOUG DC10 DC1010 3022110 WP CABIN MALFUNCTIONED A HALA K NONE O OTHER CR CRUISE 1 WP 13 119AA 46519 HNL - FLT 21 - FOUND EMERGENCY FLOOR LIGHTS, CABIN C, RIGHT SIDE CAME ON DURING FLIGHT. REPLACED THR NR 1 CONTROL MODUL E AND THE OPERATIONAL CEHCK WAS OK. (M) 2 L 7 3 4F A22WE 1996111400326 19961114 00326 WP 1996 11 14 ASAA9680230 1 19961014 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 954AS 49387 PAX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS AT ROW 9 WERE FOUND INOPERATIVE. REPLACED THE BATERY PACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996111400327 19961114 00327 WP 1996 11 14 ASAA9680229 1 19961014 A 3350 41B004D07G3 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 932AS 49233 PDX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE TAILCONE AREA WERE FOUND DIM. REPLACED THE BATTERI ES AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996111400328 19961114 00328 WP 1996 11 14 ASAA9680228 1 19961012 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 53016 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. SECURED L OOSE CONNECTOR AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996111400329 19961114 00329 WP 1996 11 14 ASAA9680227 1 19961012 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 53016 SEA - PRIOR TO DEPARTURE OF FLIGHT 85, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERAT IVE. SECURED LOSE CONNECTOR AT ROW 3 AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996111400330 19961114 00330 WP 1996 11 14 ASAA9680226 1 19961010 A 3350 60030431 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 932AS 49233 PDX - DURING MAINTENANCE CHECK, THE OVERWING EMERGENY EXIT LIGHTS WERE FOUND DIM. REPLACED THE POWER SUPPLY AND OPERATE D NORMALLY. (M) 2 L 7 2 4F A6WE 1996111400331 19961114 00331 WP 1996 11 14 ASAA9680225 1 19961011 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 53016 ANC - FLT 204 - CREW REPORTED FIRST CLASS EMERGENCY EXIT FLOOR TRACK LIGHTS INOP IN FIRST CLASS CABIN. RECONNECTED WIRI NG AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996111400332 19961114 00332 WP 1996 11 14 ASAA9680224 1 19961011 A 3350 0200335001 LIGHT DOUG DC9 DC982 3022082 WP TAILCONE INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 933AS 49234 SEA - DURING MAINTENANCE CHECK, THE FIRST OVERHEAD EMERGENCY EXIT LIGHT IN THE TAILCONE AREA WAS FOUND INOPERATIVE AND B ROKEN. REPLACED LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996111400333 19961114 00333 WP 1996 11 14 ASAA9680222 1 19961010 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 967AS 49103 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY EXIT LIGHTS IN FIRST CLASS WERE FOUND INOPERATIVE. REPLACED BATT ERIES AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996111400335 19961114 00335 NM 1996 11 14 ASAA9610135 1 19961010 A 3350 20131A BATTERY BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 ANC - FLT 54 - ONE SECTION OF MID CABIN EMERGENCY EXIT FLOOR TRACK LIGHTS ILLUMINATED DURING FLIGHT. REPLACED BATTERY A ND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1996111400336 19961114 00336 NM 1996 11 14 ASAA9610136 1 19961010 A 3350 8821004 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, THE RIGHT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED BATTERY P ACK AND LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996111400337 19961114 00337 NM 1996 11 14 ASAA9610137 1 19961011 A 3350 8821004 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, NUMEROUS EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED THREE EACH BATTERY PACKS AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996111400338 19961114 00338 SO 1996 11 14 ASOA96047 1 19961019 A 2752 MS312691210S CONNECTOR EMB 120 EMB120RT SO TE FLAP DIRTY A ASOA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SO 11 237AS 120051 IN BOUND TRI-ATL, CREW EXPERIENCED A FLAP CONTROL FAULT. SYSTEM WAS RESET PER THE POH AND APPROXIMATELY 5 MINUTES LATER , THE FAULT LIGHT ILLUMINATED AGAIN. THE CREW CHOSE TO DECLARE AN EMERGENCY AND LANDED ZERO FLAPS IN ATL. LANDING WAS MADE SAFELY AND WITHOUT INCIDENT. CLEANED INBOARD FLAP ACTUATOR CANNON PLUG IAW MM. OPERATIONAL CHECKS WERE GOOD AND A IRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M) 2 L 7 2 4T RT A31SO 1996111400339 19961114 00339 NM 1996 11 14 AWXA960603 1 19961019 A 3350 FUSE BOEING 737 7373S3 1384711 NM CABIN FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 316AW 23713 PHX - FLT 543 - DURING ROUTINE MAINTENANCE CHECK, FOUND FORWARD 4 ROWS OF EMERGENCY LIGHTS INOP. REPLACED BATTERY FUSE, OPS CHECK OK. (M) 2 L 7 2 4F RT A16WE 1996111400340 19961114 00340 NM 1996 11 14 AWXA960601 1 19961019 A 3350 1012721 LIGHT BOEING 737 737301 1384611 NM CABIN INOP A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 325AW 23260 PHX - FLT 28 - DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 22 ABC EMERGENCY EXIT LIGHT INOP ON SEAT. REPLACED LIGHT ASS Y OPS NORMAL. (M) 2 L 7 2 4F RT A16WE 1996111400341 19961114 00341 NM 1996 11 14 AWXA960607 1 19961019 A 3397 WIRE BOEING 737 7372U9 1384498 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 149AW 22575 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 16 SEAT EMERGENCY LIGHT INO. REPAIRED BROKEN WIRE, OPS CHECK GOOD. ( M) 2 L 7 2 4F RT A16WE 1996111400342 19961114 00342 NM 1996 11 14 AWXA960597 1 19961017 A 3350 LIGHT BOEING 737 737277 1384570 NM CABIN LOOSE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 184AW 22651 FLT 2684 - PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT ROW 6C TORN OUT OF SEAT. REPAIRED EMERGEN CY EXIT LIGHT AT ROW 6C. OPS CHECK GOOD AT THIS TIME. (M) 2 L 7 2 4F RT A16WE 1996111400343 19961114 00343 NM 1996 11 14 AWXA960598 1 19961017 A 3350 CONNECTOR BOEING 737 737297 1384480 NM CABIN LOOSE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 147AW 22630 PHX - FLT 2245 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT OVERWING WINDOW EXIT INOP. RECONNECTED CO NNECTOR ON BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1996111400344 19961114 00344 NM 1996 11 14 AWXA960599 1 19961017 A 3350 LIGHT BOEING 737 73733A 1384673 NM CABIN MISSING A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 167AW 23628 PHX - FLT 2440 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT AT ROW 4 RIGHT MISSING FROM BULLNOSE PANEL . REINSTALLED EMERGENCY EXIT LIGHT. OPS CHECK OK. (M) 2 L 7 2 4F RT A16WE 1996111400345 19961114 00345 NM 1996 11 14 AWXA960593 1 19961014 A 3397 WIRE BOEING 737 737277 1384570 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 187AW 22654 PHX - FLT 90 - DURING ROUTINE MAINTENANCE CHECK, FOUND FIRST 5 ROWS OF EMERGENCY LIGHTS REMAIN DIM AT ALL TIMES. FLICKE RED DURING FLIGHT. FOUND OPEN WIRES. REPAIRED WIRES AT ROW 1 AB. OPS NORMAL. (M) 2 L 7 2 4F RT A16WE 1996111400346 19961114 00346 NM 1996 11 14 AWXA960581 1 19961012 A 3397 WIRE BOEING 737 7373G7 1384595 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 160AW 23782 PHX - FLT 2653 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS AT ROW 8 INOP. REPAIRED WIRING. OPS GOOD. ( M) 2 L 7 2 4F RT A16WE 1996111400347 19961114 00347 NM 1996 11 14 AWXA960579 1 19961012 A 3350 FUSE BOEING 737 7373S3 1384711 NM CABIN FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 316AW 23713 PHX - FLT 1265 - DURING ROUTINE MAINTENANCE CHECK, FOUND FORWARD SECTION OF EMERGENCY LIGHTS INOP. REPLACED FUSE AT BAT TERY PACK FORWARD SECTIONS. OP NORMAL. (M) 2 L 7 2 4F RT A16WE 1996111400348 19961114 00348 NM 1996 11 14 AWXA960586 1 19961012 A 3350 LIGHT BOEING 757 757225 1384959 NM CABIN LOOSE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 907AW 22691 PHX - FLT 2260 - DURING ROUTINE MAINTENANCE CEHCK, FOUND EMERGENCY LIGHT AT 3 CD INOP. RESECURED LIGHT. OPS CHECK GOOD . (M) 2 L 7 2 4F RT A2NM 1996111400349 19961114 00349 NM 1996 11 14 AWXA960590 1 19961011 A 3350 LIGHT BOEING 737 7373G7 1384595 NM CABIN LOOSE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 158AW 23780 PHX - FLT 2249 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT ROW 23 LOOSE FROM SEAT. RESECURED LIGHT. (M) 2 L 7 2 4F RT A16WE 1996111400350 19961114 00350 NM 1996 11 14 AWXA960589 1 19961011 A 3350 LIGHT BOEING 737 737277 1384570 NM CABIN LOOSE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 179AW 22646 PHX - FLT 2267 - DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 18 EMERGENCY LIGHTS PULLED LOOSE FROM SEAT. SECURED LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A16WE 1996111400351 19961114 00351 NM 1996 11 14 AWXA960605 1 19961019 A 3350 900542 POWER SUPPLY BOEING 737 7372M8 1384483 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 141AW 21122 21955 PHX - FLT 2887 - DURING ROUTINE MAINTENANCE CHECK, FOUND L-1 AND R-1 EMERGENCY EXIT LIGHTS INOP. REPLACED BOTH FORWARD EMERGENCY EXIT POWER SUPPLY. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1996111400352 19961114 00352 NM 1996 11 14 96ZZZM1484 1 19961019 A 3350 900542 POWER SUPPLY BOEING 737 7372M8 1384483 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 141AW 21122 21955 PHX - FLT 2887 - DURING ROUTINE MAINTENANCE CHECK, FOUND L-1 AND R-1 EMERGENCY EXIT LIGHTS INOP. REPLACED BOTH FORWARD EMERGENCY EXIT POWER SUPPLY. OPS CHECK GOOD. REFERENCE AWXA960605. 2 L 7 2 4F A16WE 1996111400353 19961114 00353 NM 1996 11 14 AWXA960600 1 19961017 A 3350 6013211 POWER SUPPLY BOEING 737 737277 1384570 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 185AW 22652 PHX - FLT 2452 - DURING ROUTINE MAINTENACNE CHECK, FOUND LEFT AND RIGHT AFT EXTERIOR EMERGENCY LIGHTS INOP. REPLACED TH E POWER SUPPLY UNIT FOR THE AFT EXTERIOR EMERGENCY LIGHTS, OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 1996111400354 19961114 00354 NM 1996 11 14 AWXA960592 1 19961014 A 3350 900542 POWER SUPPLY BOEING 737 7372M8 1384483 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 141AW 5080 21955 PHX - FLT 2592 - DURING ROUTINE MAINTENANCE CEHCK, FOUND RIGHT OVERWING EXIT INTERIOR EXIT SIGN ON DOOR FRAME INOP. REP LACED BATTERY POWER CHARGER WITH SERVICEABLE, OPS CHECK NORMAL. (M) 2 L 7 2 4F A16WE 1996111400355 19961114 00355 NM 1996 11 14 AWXA960591 1 19961014 A 3350 831862 BATTERY BOEING 737 7372M8 1384483 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 141AW 22215 21955 PHX - FLT 2550 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT L1 AND R1 DOORS. REMOVED AND REP LACED BATTERY PACK, OPS NORMAL AT THIS TIME. (M) 2 L 7 2 4F A16WE 1996111400356 19961114 00356 NM 1996 11 14 AWXA960585 1 19961011 A 3350 20121 BATTERY CHARGER BOEING 737 7373Y0 1384671 NM L1 DOOR INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 323AW 23684 PHX - FLT 1112 - DURING ROUTINE MAINTENANCE CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTER Y CHARGER, DOOR L1. LIGHTS OP CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996111400357 19961114 00357 EU 1996 11 14 AWXA960540 1 19960928 A 2910 O-RINGS AIRBUS 320 A320231 3930325 EU BOBBIN ASSY FAILED A AWXA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CL CLIMB 1 WP 28 628AW 67 CMH - FLT 2031 - AIR TURN BACK DUE TO LOSS OF GREEN HYDRAULIC SYSTEM. FOUND 2 HYDRAULIC LEAKS IN MAIN LANDING GEAR WHEE L WELL. BOTH LEAKS WERE ON THE GREEN HYDRAULIC SYSTEM MANIFOLD. REPLACD O-RINGS ON BOBBIN ASSEMBLY OF GREEN SYSTEM 3-2 WAY VALVE (CENTER MAIN WHEEL WELL). LEAK CHECKS GOOD. SERVICED AS REQUIRED. (M) 2 L 7 2 4F RT A28NM 1996111400358 19961114 00358 1996 11 14 AWXA960556 4 19961005 A 2565 D30664103 SLIDE AIRBUS 320 A320231 3930325 EU L-1 DOOR DEPLOYED A AWXA K NONE O OTHER TX TAXI/GRND HDL 1 WP 28 633AW A5005 082 CMH - FLT 2860 - L-1 DOOR SLIDE INADVERTENTLY FELL OFF AND PARTIALLY OPENED. REMOVED AND REPLACED L-1 DOOR SLIDE IAW 25 -62-44. OPERATIONS CHECKED GOOD. (M) 2 L 7 2 4F RT A28NM 1996111400359 19961114 00359 NM 1996 11 14 AWXA960595 1 19961015 A 7830 1U1225 ISOLATION VALVE BOEING 737 737277 1384570 NM NR 1 TR UNIT INOP A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 188AW 59019 909 22655 LAS - FLT 2037 - DURING FLIGHT THE ISOLATION VALVE LIGHT ILLUMINATED, A/C DIVETED TO LAS. LIGHT WENT OUT ON LANDING AND REVERSER WORKED NORMALLY. REPLACED NR 1 ISOLATION VALVE, OPS CHECK NORMALLY AT THIS TIME. (M) 2 L 7 2 4F RT A16WE 1996111400360 19961114 00360 NM 1996 11 14 AWXA960583 1 19961011 A 2120 AIR DISTR BOEING 757 7572G7 1384963 NM COCKPIT ODOR A AWXA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 WP 28 910AW 24523 PHX - FLT 7902 - STRONG FUEL SMELL IN COCKPIT JUST AFTER TOUCH AND GO LANDINGS. SMELL ONLY LASTS A FEW SECONDS, BUT WAS SIGNIFICANT. OPERATED BOTH PACKS WITH APU RUNNING. OPERATED BOTH PACKS WITH BOTH ENGINES RUNNING. UNABLE TO DETECT F UEL SMELL IN FLIGHT DECK. (M) 2 L 7 2 4F RT A2NM 1996111400361 19961114 00361 1996 11 14 AWXA960582 4 19961012 A 2565 CABLE BOEING 757 7572S7 1384962 NM ESCAPE SLIDE BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 903AW 23323 PHX - FLT 10 - DURING ROUTINE MAINTENANCE CHECK, FOUND R2 DOOR GIRT BAR RELEASE CABLE BROKEN. REMOVED AND REPLACED CABL E. (M) 2 L 7 2 4F RT A2NM 1996111400362 19961114 00362 NM 1996 11 14 AWXA960564 1 19961007 A 7830 WIRE BOEING 737 737277 1384570 NM NR 2 TR UNIT CHAFED A AWXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 28 189AW 22656 LAS - FLT 134 - DURING TAKEOFF ROLL AT 70 KTS, THE NR 2 ENGINE THRUST REVERSER UNLOCK LIGHT CAME ON WITH NO ACTUAL THRUS T REVERSER DEPLOYMENT. CREW ABORTED TAKEOFF. FOUND CHAFED WIRE IN PYLON AREA NEXT TO THE FEEDBACK CABLE DURING ENGINE CHANGE. REPAIRED WIRES, THRUST REVERSER INDICATION OPERATES GOOD. (M) 2 L 7 2 4F RT A16WE 1996111400363 19961114 00363 EU 1996 11 14 COEA9670102 1 19961011 A 2432 4050A1 BATTERY FOKKER F27 F27MK600 4990706 EU RIGHT OVERHEATED A COEA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 NM 13 701FE L2365 10419 OAK-YVR - NR 2 BATTERY OVERHEAT LIGHT ILLUMINATED. CREW SWITCHED BATTERIES OFFLINE, NR 1 GENERATOR VOLTAGE BECAME ERRAT IC. CREW THEN SELECTED NR 1 GENERATOR OFF AND PROBLEM PERSISTED WITH THE NR 2 GENERATOR. DUE TO IFR WEATHER CONDITIONS CREW ELECTED TO DIVERT TO MFR WHICH WAS VFR. NR 2 BATTERY HAS BEEN REPLACED. OPERATIONAL TEST PERFORMED WITH NO PROBL EMS. AIRCRAFT RETURNED TO SERVICE. DC VOLTAGE ERRATIC WITH BATTERY SWITCH OFF AFTER SWITCHING DC GENERATOR OFF MOMENTA RILY. REMOVED AND REPLACED LEFT DC CONTROL UNIT. GENERATORS PARALLELED. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T A817 1996111400364 19961114 00364 WP 1996 11 14 VJ960001R1 1 19961021 A 2440 DH7ZG RELAY DOUG DC9 DC932 3022066 WP CB PANEL FAILED A A VJ6A K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 11 938VV 47442 WHEN POWER WAS TRANSFERRED FROM EXTERNAL POWER UNIT TO APU, A LOUD ARCING NOISE WAS HEARD FROM BEHIND CAPTAINS SEAT. CA BIN LIGHTS WENT OUT AND GROUND SENSE BUS CONTROL CIRCUIT BREAKER POPPED AND SMOKE APPEARED FROM CIRCUIT BREAKER PANEL. R EMOVED AND REPLACED GROUND SERVICE EXTERNAL POWER RELAY IAW MM SECTION 24-40. PERFORMED A SYSTEM OPERATION CHECK AND SY STEM CHECKED GOOD. (M) 2 L 7 2 4F A6WE 1996111400365 19961114 00365 EU 1996 11 14 PLGA9610201 1 19961020 A 2613 CONNECTOR SAAB SF340 SF340A 7850100 EU RT ENGINE DIRTY A PLGA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NE 05 741BA 340A090 PWM - FLT 4964 - EN ROUTE YOW, THE RIGHT TAIL PIPE HOT WARNING LIGHT ILLUMINATED. THE CREW SECURED THE ENGINE AND DIVER TED TO PWM, LANDING WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT AND FOUND MOISTURE IN THE CANNON PLUG. MAINTENANCE CLEANED THE CONNECTOR, OPERATIONALLY CHECKED THE SYSTEM AND RETURNED THE AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1996111400366 19961114 00366 EU 1996 11 14 USAAF96107 1 19960921 A 2460 41HF60 DIODE FOKKER F28 F28MK0100 4990807 EU DC BUS OVERHEATED A USAA K NONE J WARNING INDICATION AP APPROACH 1 EA 19 887US 11349 FLT 1206 - RDU-PIT, AT 50S OF PIT, CRWE GOT 'EMERGENCY DC BUS FAILED' ON MFDU. COMMUNICATINOS WERE LOST WITH ZOB AND PI T APPROACH. AIRCRAFT SHED SOME ELECTRICAL LOAD AND COMMUNICATION WAS RE-ESTABLISHED. AN EMERGENCY WAS DECLARED AND FLI GHT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND GROUND HANDLING DC BUS BLOCKING DIODE CR3 OVERHEATED. REPLACED CR3. OP ERATIONAL CHECKED GOOD. (M) 2 L 7 2 4F RT 1996111400367 19961114 00367 WP 1996 11 14 USAAD96152 1 19961019 A 7830 TR LATCHES DOUG DC9 DC931 3022065 WP LT ENGINE LACK OF LUBE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 985VJ 47208 FLT 1125 - MDT-CLT - ON ROTATION LEFT ENGINE REVERSE UNLOCK LIGHT CAME ON AND STAYED ON. CONTINUED TAKEOFF AND THEN RET URNED TO FIELD AT MDT. LIGHT WENT OUT WHEN AIRCRAFT LANDED. NO EMERGENCY DECLARED BUT ATC TOWR DID CALL OUT THE EMERGE NCY EQUIPMENT. MAINTENANCE CLEANED AND LUBRICATED UPPER AND LOWER T/R LATCHES. OPERATIONAL CHECK OK. (M) 2 L 7 2 4F A6WE 1996111400368 19961114 00368 WP 1996 11 14 USAAD96151 1 19961020 A 7931 811131 RELIEF VALVE DOUG DC9 DC982 3022082 WP NR 1 ENGINE FAILED A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 822US 49139 FLT 2285 - PBI-DCA - AT CRUISE THE CREW NOTICED HIGH OIL PRESSURE ON NR 1 ENGINE. FLIGHT DIVERTED TO MCO. NO EMEGENCY WAS DECLARED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LEFT OIL PRESSURE RELIEF VALVE. OPERATIONA L CHECK WAS GOOD. (M) 2 L 7 2 4F A6WE 1996111400369 19961114 00369 NM 1996 11 14 USAABB96039 1 19961005 A 2121 FAN BOEING 757 7572B7 1384964 NM CABIN ODOR A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 617AU 27148 ORF - FLT 205 - EN ROUTE CLT-BOS, CAPTAIN REPORTED STRONG SMELL OF SMOKE IN CABIN. THE MID LAVATORY SMOKE DETECTOR ACTI VATED. FLIGHT DIVERTED TO ORF AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE CHECKED THE AIRCRAFT OVER, INCLUDING RU NNING BOTH PACKS FROM THE ENGINES AND THE PAU. NO PROBLEMS WERE FOUND. THE RECIRCULATION FAN AND FILTERS WERE REPLACED AS A PRECAUTION. (M) 2 L 7 2 4F RT A2NM 1996111400370 19961114 00370 EU 1996 11 14 USAAF96104 1 19961014 A 3350 8GS00537605 LAMP FOKKER F28 F28MK0100 4990807 EU CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 851US 11278 EMERGENCY LIGHTS ABOVE EXIT WINDOW INOP. RELAMPED EXIT LIGHT. (M) 2 L 7 2 4F RT 1996111400371 19961114 00371 EU 1996 11 14 USAAF96105 1 19961015 A 5230 HANDLE FOKKER F28 F28MK0100 4990807 EU CARGO DOOR NOT LATCHED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 884US 11338 FLT 915 - CLT-JAX - AFTER TAKEOFF, MID CARGO DOOR WARNING LIGHT ILLUMINATED. FLIGHT RETURNED TO CLT WITH NO FURTHER INC IDENT. MAINTENANCE FOUND DOOR UPPER HANDLE UNLATCHED. CYCLED DOOR OPEN AND CLOSED. LIGHT CHECKED GOOD. DOOR LATCHED PROPERLY. (M) 2 L 7 2 4F RT 1996111400372 19961114 00372 EU 1996 11 14 USAAF96110 1 19961018 A 2840 INDICATION FOKKER F28 F28MK0100 4990807 EU FUEL SYSTEM MALFUNCTIONED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 852US 11280 FLT 582 - ITH-PIT - FLIGHT HAD JUST DEPARTED WHEN CREW RECEIVED FUEL IMBALANCE LIGHT. TANK GAUGES WERE OK. FUEL TOTALI ZER WAS SHOWING FUEL QUANTITY WAS GOING DOWN. CREW DECIDED TO DIVERT TO ELM TO HAVE PROBLEM CHECKED. NO EMERGENCY DECL ARED. FLGIHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED FOR FUEL LEAKS. NONE FOUND. VERIFIED INDICATIONS AGREED WITH TANK CONTENTS USING MAG STICK. PER FORMED BITE CHECK OF SYSTEM. ALL CHECKS OK. AIRCRAFT RETURNED TO SERV ICE. (M) 2 L 7 2 4F RT 1996111400373 19961114 00373 EU 1996 11 14 USAAF96106 1 19961016 A 3230 SENSOR FOKKER F28 F28MK0100 4990807 EU MLG OUT OF ADJUST A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 860US 11295 FLT 388 - RIC-PIT, AFTER TAKEOFF, LANDING GEAR WOULD NOT COME UP. GROUND/FLT ALERT MESSAGE ON MFDU. NO EMERGENCY DECLA RED. FLIGHT RETURNED TO RIC WITHOUT FURTHER INCIDENT. LANDING AND TAXI WAS NORMAL. MAINTENANCE ADJUSTED BOTH AIR/GND SENSORS ON BOTH MAIN GEAR ASSEMBLIES. MULTIPLE GEAR SWINGS PERFORMED. NO PROBLEMS NOTED. (M) 2 L 7 2 4F RT 1996111400374 19961114 00374 EU 1996 11 14 USAAF96108 1 19961018 A 3350 OL3071BPE LAMP FOKKER F28 F28MK4000 4990810 EU CABIN BLOWN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 482US 11231 FOUND FLOOR LEVEL EMERGENCY LIGHTING FIXTURE 8C BROKEN. MAINTENANCE RELAMPED LIGHTING FIXTURE. (M) 2 L 7 2 4F RT A20EU 1996111400375 19961114 00375 EU 1996 11 14 USAAF96109 1 19961012 A 3350 6008905 POWER SUPPLY FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 483US 11233 FOUND FORWARD AND AFT FAIRING EXTERIOR EMERGENCY LIGHTS INOP. MAINTENANCE REPLACED BOTH FORWARD AND AFT POWER SUPPLY. ( M) 2 L 7 2 4F RT A20EU 1996111400376 19961114 00376 EU 1996 11 14 USAA960685 1 19961015 A 5312 BULKHEAD ANGLE FOKKER F28 F28MK4000 4990810 EU FWD PRESS BULKHD CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 488US 20974 11240 PIT - DURING SIP VISIT, SIP REF NR 53-10-06, FOUND 2 CRACKS, ONE 6 INCH AND ONE 3.5 INCH AT CONNECTION ANGLE AT FORWARD PRESSURE BULKHEAD, FRAME 1550 AFT BETWEEN STRINGER NR 72 AND STRINGER NR 3. DETECTED BY VISUAL, DYE PENETRANT AND EDDY CURRENT. STOP DRILLED CRACK ENDS AND INSTALLED TWO EACH DOUBLERS PER SRM 53-02-18 FIG 11. (M) 2 L 7 2 4F RT A20EU 1996111400377 19961114 00377 NM 1996 11 14 AALA961474 1 19961004 A 5320 146N8522 SILL BOEING 757 757223 1384957 NM BS 1382-1441 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 659AA 24617 AFW - FOUND AFT CARGO CUT OUT LOWER SILL INNER CHORD HAS CORROSION BLENDED BEYOND SRM LIMITS. REPAIRED PER MRB 757-965. (M) 2 L 7 2 4F RT A2NM 1996111400378 19961114 00378 NM 1996 11 14 AALA961475 1 19961004 A 5321 141N516153 FLOOR BOEING 757 757223 1384957 NM BS 372 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 659AA 24617 AFW - FOUND FLOOR AT STATION 405 RBL 12 HAD CORROSION BLENDED BEYOND SRM LIMITS. REPAIRED PER MRB 757-967. (M) 2 L 7 2 4F RT A2NM 1996111400379 19961114 00379 NM 1996 11 14 AALA961476 1 19961005 A 5210 146N62016 HANDLE PAN BOEING 757 757223 1384957 NM R4 DOOR GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 628AA 24586 AFW - FOUND R-4 DOOR HANDLE PAN HAS SMALL GOUGE. REF MRB 757-971. REFINISH THE BLEND OUT PER REF C SRM SECTION. (M) 2 L 7 2 4F RT A2NM 1996111400380 19961114 00380 NM 1996 11 14 AALA961489 1 19961009 A 5330 SKIN BOEING 727 727227 1384078 NM DOOR CUT OUT CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 726AA 20733 TUL - FOUND FORWARD ENTRY DOOR UPPER HINGE CUT OUT, SKIN CRACKED APPROX .1875 INCH LONG AT 10 O'CLOCK POSITION. INSTALL ED DOUBLER AS PER SERVICE BULLETIN 727-53-0198. (M) 2 L 7 3 4F A3WE 1996111400381 19961114 00381 NM 1996 11 14 AALA961479 1 19961009 A 5320 CLIP BOEING 727 727223 1384074 NM BS 740 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 706AA 22463 TUL - FOUND CORNER CLIP CORRODED INSIDE DELTA BEAM RIGHT SIDE AT STATION 740. REMOVED AND INSTALLED NEW CLIP PER SRM 51 -10-1. (M) 2 L 7 3 4F A3WE 1996111400382 19961114 00382 NM 1996 11 14 AALA961488 1 19961009 A 5343 TRUNNION BOEING 727 727223 1384074 NM BS 328 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 706AA 22463 TUL - FOUND LEFT NLG TRUNNION CORRODED. REMOVED AND REPLACED LEFT NOSE GEAR TRUNNION ASSEMBLY PER SRM 51-30-2 AND B-727 BP 65-88189. (M) 2 L 7 3 4F A3WE 1996111400383 19961114 00383 NM 1996 11 14 AALA961487 1 19961009 A 5330 SKIN BOEING 727 727223 1384074 NM BS 720 WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 706AA 22463 TUL - FOUND FUSELAGE SKIN CHAFFED AND WORN UNDER WING AND FUSELAGE PANEL 3342, STATION 720D AND 12 INCHES STRINGER 19 LE FT. CUT OUT SECTION AND INSTALLED FILLER AND DOUBLER PER SRM 53-30-3 PAGE 20-23. (M) 2 L 7 3 4F A3WE 1996111400384 19961114 00384 NM 1996 11 14 AALA961486 1 19961009 A 5330 SKIN BOEING 727 727223 1384074 NM BS 720 WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 706AA 22463 TUL - FOUND SKIN LAP 19R WORN BY WING LE FAIRING BEYOND LIMITS. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-3 0-3 FIG 14. (M) 2 L 7 3 4F A3WE 1996111400385 19961114 00385 NM 1996 11 14 AALA961485 1 19961009 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1095 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 706AA 22463 TUL - FOUND FUSELAGE SKIN CRACKED .375 INCH AT RIVET ON LEFT SIDE OF STRINGER 1 AND STATION 1095. REMOVED CRACKED SKIN AND INSTALLED DOUBLER PER SB 53-30-3 FIG 3 PAGES 1-14A. (M) 2 L 7 3 4F A3WE 1996111400386 19961114 00386 NM 1996 11 14 AALA961484 1 19961009 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720-740 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 706AA 22463 TUL - FOUND CORROSION ON STRINGER 28R BETWEEN STRINGER 720E AND 720F 6 INCHES, CORROSION ON STRINGER 28R BETWEEN STRINGE R 720F AND 740 6 INCHES. BLENDED OUT CORROSION AND INSTALLED DOUBLER STRAP PER ESO 11697 DATED 9-9-96 AND 9-11-96. (M) 2 L 7 3 4F A3WE 1996111400387 19961114 00387 NM 1996 11 14 AALA961481 1 19961009 A 5320 CHANNEL BOEING 727 727223 1384074 NM BS 1136 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 708AA 22465 TUL - FOUND FORWARD HAT CHANNEL CORRODED AT I/R EDGE. REPLACED FORWARD HAT CHANNEL PR 51-10-1 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1996111400388 19961114 00388 NM 1996 11 14 AALA961482 1 19961009 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 950 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 706AA 22463 TUL - FOUND CORROSION ON STRINGER 28R AT BS 950E. INSTALLED STRINGER REPAIR PER ESO 11697, DATED 9-11-96. (M) 2 L 7 3 4F A3WE 1996111400389 19961114 00389 NM 1996 11 14 AALA961483 1 19961009 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 910 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 706AA 22463 TUL - FOUND STRINGER CRACKED. INSTALLED STRINGER SPLICE REPAIR PER AA MM 53-10-3. (M) 2 L 7 3 4F A3WE 1996111400390 19961114 00390 WP 1996 11 14 AALA961358 1 19960916 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 1155-1174 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 482AA 49675 TUL - FOUND RIGHT LONGERON CUSP HAS CORROSION STATION 1155 TO 1174 LONGERON 18R ABOVE AFT CX DOOR. INSTALLED DOUBLER ST ATION 1150-1175 PER 53-01 SRM FIG 4 SHEET 3 PAGE 17. (M) 2 L 7 2 4F A6WE 1996111400391 19961114 00391 WP 1996 11 14 AALA961429 1 19960926 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 294-313 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 484AA 49677 TUL - CUSPLINE WEB HAS CORROSION BETWEEN STATION 294 - STATION 313 OUTBOARD NR 6 SEAT TRACK. INSTALLED CUSP DOUBLER OUT BOARD NR 6 SEAT TRACK PER SRM 53-01 FIG 4 SH 3. (M) 2 L 7 2 4F A6WE 1996111400392 19961114 00392 WP 1996 11 14 AALA961439 1 19960930 A 5320 SILL DOUG DC9 DC982 3022082 WP BS 411 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 289AA 49301 TUL - FOUND CORROSION ON HORIZONTAL LEG OF DOOR SILL AREA STATION 411. REPAIRED PER ESO 80559, DATED 9-26-96. (M) 2 L 7 2 4F A6WE 1996111400393 19961114 00393 WP 1996 11 14 AALA961438 1 19960927 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1322 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 295AA 49307 TUL - FOUND FORWARD LOWER ANGLE ON BELT FRAME CORRODED. CORROSION CUT OUT DOUBLER INSTALLED PER SRM 53-03 FIG 2A. (M) 2 L 7 2 4F A6WE 1996111400394 19961114 00394 WP 1996 11 14 AALA961480 1 19961004 A 5320 JAMB BEAM DOUG DC9 DC982 3022082 WP BS 370-427 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 295AA 49307 TUL - FORWARD CARGO DOOR JAMB LOWER BEAM HAS CORROSION STATION 370 TO 427. REPLACED FORWARD CARGO DOOR JAMB BEAM. (M) 2 L 7 2 4F A6WE 1996111400395 19961114 00395 NM 1996 11 14 AALA961459 1 19961007 A 5330 SKIN BOEING 727 727223 1384074 NM BS 420 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 880AA 21519 TUL - FOUND DENT IN FUSELAGE SKIN. CUTOUT DAMAGED AREA. INSTALLED DOUBLER PER SRM 53-30-3 PG 5-8. (M) 2 L 7 3 4F A3WE 1996111400396 19961114 00396 NM 1996 11 14 AALA961464 1 19961007 A 5330 SKIN BOEING 727 727223 1384074 NM BS 830 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 880AA 21519 TUL - FOUND CORROSION ON LEFT PLENNUM CHAMBER SKIN. REMOVED CORROSION AND REPAIRED PER ESO 11697 DATE 10-1-96. (M) 2 L 7 3 4F A3WE 1996111400397 19961114 00397 EU 1996 11 14 WTAA960181 1 19961022 A 5330 SKIN BAG JETSTM JETSTM3101 1500215 EU FWD FUSELAGE BIRDSTRIKE A WTAA O OTHER C F.O.D. NR NOT REPORTED 1 WP 17 417UE 794 LAX - BIRD STRIKE REPORTED TO RIGHT NOSE AREA. MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECTION OF AIRCRAFT. NO DAMAGED DETECTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996111400398 19961114 00398 SO 1996 11 14 WTAA960180 1 19961017 A 5246 12016900010 DOOR EMB 120 EMB120RT SO FUEL SERVICE NOT CLOSED A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 WP 17 284UE 120145 FAT - OUTBOARD FUEL DOOR OPENED DURING TAKEOFF. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND SECURED FU EL DOOR. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996111400399 19961114 00399 EU 1996 11 14 WTAA960178 1 19961015 A 3260 622800200 UPLOCK SWITCH BAG JETSTM JETSTM3101 1500215 EU LT MLG FAILED A WTAA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 17 103XV 747 PDX - LEFT MAIN GEAR INTRANSIT LIGHT REPORTED INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BROKEN TERMINAL ON UPLOCK M ICROSWITCH. GEAR RETRACTION SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996111400400 19961114 00400 NM 1996 11 14 W8PA960161 1 19961025 A 3350 LIGHT BOEING 737 7373Q8 1384670 NM CABIN LOOSE A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 956WP 24299 EMERGENCY EXIT LIGHTING INOP BETWEEN ROWS 16-20. RESEATED LIGHT SOCKET. (M) 2 L 7 2 4F RT A16WE 1996111400401 19961114 00401 WP 1996 11 14 AALA961440 1 19960930 A 5320 SHIM DOUG DC9 DC982 3022082 WP BS 1220-1234 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 289AA 49301 TUL - FOUND CORROSION ON SHIM IN AFT CARGO LONGERON 26R, STATION 1220 TO 1234. REPAIR PER ESO 80559, DATED 9-27-96. (M ) 2 L 7 2 4F A6WE 1996111400403 19961114 00403 WP 1996 11 14 ORJA9667 1 19960909 A 5320 STRAP DOUG DC9 DC982 3022082 WP L-1 DOOR CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 840RA 49424 L-1 DOOR SILL PLATE ATTACHMENT FLOOR STRAP CORRODED. FABRICATED NEW STRAP IAW DEA SRM 51-10-2. TREATED AND PRIMED IAW 51-10-3. INSTALLED WITH SOLID FASTENERS IAW 51-30-1. (M) 2 L 7 2 4F A6WE 1996111400404 19961114 00404 WP 1996 11 14 ORJA9669 1 19961012 A 3350 41B004AD073 BATTERY EA1D13D3 DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 822RA 49932 AFT SECTION OF E-LIGHT FLOOR PATH INOP. REMOVED AND REPLACED APPLICABLE BATTERIES FOR AFT SECTION. E-PATH LIGHTING OPS CHECKS GOOD. (M) 2 L 7 2 4F A6WE 1996111400405 19961114 00405 NM 1996 11 14 GAIA9629 1 19961028 A 2611 SMOKE LIGHT BOEING 727 727251 138408H NM CARGO COMPART MALFUNCTIONED A GAIA K NONE N FALSE WARNING CR CRUISE 1 SW 07 279US 21158 FLT NR 725 - IAH-TOL - PRIOR TO DESCENT INTO TOL, MAIN CARGO CABIN SMOKE DETECTOR LIGHT CAME ON. CHECKED CABIN NO SMOKE NOTED. MAINTENANCE CHECKED SMOKE DETECTOR SYSTEM NO DEFECTS NOTED. SYSTEM OPERATIONAL CHECKED NORMAL. AIRCRAFT RELEA SED FOR FLIGHT. (M) 2 L 7 3 4F A3WE 1996111400406 19961114 00406 NE 1996 11 14 EIAA96047 2 19961018 A 7261 SCAVENGE LINE BOEING 747 747212B 1384886 NM PWA JT9 JT9D7F 52054 NE NR 3 ENGINE LEAKING A EIAA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 NM 09 485EV 59 20712 662479 DURING CLIMB THROUGH FLIGHT LEVEL 100, NR 3 ENGINE QTY SHOWED ZERO, LOW OIL PRESSURE LIGHT CAME ON. SHUTDOWN ENGINE IN FLIGHT. WINDMILLING OIL PRESSURE WAS 5 PSI, WINDMILLING TIME WAS ONE HOUR, MACH .52/IAS 300 KNOTS. FOUND SCAVENGE LINE FROM NR 1 AND NR 2 BEARING LEAKING. BOLTS LOOSE IN GEARBOX AT CONNECTION. REPAIRED ANGLE GEARBOX IAW ECRA NR 662479-7 2-014 BY INSERTION OF HELICOILS PER REPAIR 02 PARA 1. WINDMILLING INSPECTION PERFORMED PER MM 72-00-00. RAN ENGINE AT IDLE FOR 5 MINUTES. LEAK CHECK ALL OK. (M) 2 L 7 4 4F 4 F A20WE E20EA 1996111400407 19961114 00407 NE 1996 11 14 EIAA9646 2 19961021 A 7530 7479555 EVC BOEING 747 747121 1384871 NM PWA JT9 JT9D7AH 52054 NE NR 1 ENGINE MALFUNCTIONED A EIAA O OTHER J WARNING INDICATION AP APPROACH 1 NM 09 480EV 20348 662949 DURING APPROACH, NR 1 ENGINE FAILED TO RESPOND TO THRUST LEVER MOVEMENTS. OIL PRESSURE LIGHT CAME ON. ACCOMPLISHED ENG INE SHUTDOWN PROCEDURE. ENGINE RUN UP, HUNG AT 24 PERCENT. CHECKED EVC AND FOUND ACTUATOR EXTENDED. REPLACED EVC CONT ROL PER MM 75-31-01. TRIM CHECK PER MM 71-00-00. (M) 2 L 7 4 4F 4 F A20WE E20EA 1996111400408 19961114 00408 WP 1996 11 14 EIAA9633 1 19960929 A 3297 WIRE DOUG DC9 DC933F 302207A WP LT MLG BROKEN A EIAA O OTHER N FALSE WARNING CL CLIMB 1 NM 09 933F 47191 SEA - WHEN LANDING GEAR RETRACTED DEPARTING SEA, LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED. ACCOMPLISHED ABNORMAL PRO CEDURE IAW OPS MANUAL WITH NO CHANGE OF INDICATION. LANDING GEAR EXTENDED NORMALLY WITH 3 GREEN AND UNSAFE LIGHTS OUT A T SEAT. ACCOMPLISHED OVERWEIGHT LANDING AFTER DECLARING EMERGENCY. FOUND BROKEN WIRE AT THE LEFT GEAR DOWNLOCKS SWITCH CANNON PLUG PIN NR 7. REPAIRED CANNON PLUG AND TESTED SYSTEM PER MM. ALL CHECKS WERE GOOD. PERFORMED OVERWEIGHT LAND ING INSPECTION. NO PROBLEMS FOUND. (M) 2 L 7 2 4F A6WE 1996111400409 19961114 00409 NM 1996 11 14 EIAA9641 1 19961003 A 5347 63B10047367 SEAT TRACK BOEING 747 747273C 1384896 NM CABIN CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 68923 20653 SAT - SEAT TRACK AT STATION RBL 6 CRACKED. REMOVED DAMAGED SECTION OF THE SEAT TRACK PER SRM 51-30-2. FABRICATED REPAI R SECTION IAW SRM 53-11-25 AND 53-10-5. INSTALLED IAW 51-30-2. (M) 2 L 7 4 4F A20WE 1996111400410 19961114 00410 NM 1996 11 14 EIAA9642 1 19961003 A 5347 SEAT TRACK BOEING 747 747273C 1384896 NM BS 450-530 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 68923 20653 SAT - SEAT TRACK BETWEEN STATION 480 AND 495 AND LBL 6 CRACKED AND CORRODED. REPAIRED DAMAGE SECTION OF TRACK FROM STAT ION 450 TO STATION 530 PER SRM 53-10-05, FIG 1 AT EXISTING SPLICES. (M) 2 L 7 4 4F A20WE 1996111400411 19961114 00411 NM 1996 11 14 EIAA9643 1 19961003 A 5315 FLOOR BEAM BOEING 747 747273C 1384896 NM CABIN CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 68923 20653 SAT - FLOOR BEAM AT STATION 460, LBL 11 THROUGH 24 CRACKED. REMOVED DAMAGED SECTION OF FLOOR BEAM FROM RBL 48 TO LBL 48 . FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-07, FIG 12. (M) 2 L 7 4 4F A20WE 1996111400412 19961114 00412 NM 1996 11 14 EIAA9644 1 19961003 A 5315 FLOOR BEAM BOEING 747 747273C 1384896 NM CABIN CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 68923 20653 SAT - FLOOR BEAM AT STATION 480, LBL 24, THROUGH LBL 29 CORRODED. REMOVED DAMAGED FLOOR BEAM FROM BL 0 TO LBL 72. FABR ICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-07, FIG 12. (M) 2 L 7 4 4F A20WE 1996111400413 19961114 00413 NM 1996 11 14 EIAA9645 1 19961003 A 5347 SEAT TRACK BOEING 747 747273C 1384896 NM BS 480-510 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 68922 20653 SAT - SEAT TRACK AT LBL 69.3, STATION 500 CRACKED AT FRAME ATTACHMENT AREA. REMOVED DAMAGED SEAT TRACK FROM STATION 480 THROUGH 510. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-05, FIG 1. (M) 2 L 7 4 4F A20WE 1996111400414 19961114 00414 NM 1996 11 14 EIAA9640 1 19961003 A 5522 SKIN BOEING 747 747273C 1384896 NM RT TE ELEVATOR CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 68923 20653 SAT - RIGHT INBOARD ELEVATOR TE DAMAGED. REPAIRED DAMAGED AREA PER SRM 51-40-14, PARA 4N FIG 20. SEALED REPAIR PER SRM 51-40-14 AND APPLIED CONDUCTIVE COATING PER SRM 51-24-03. REAPPLIED FINISH PER MM 51-24-03 AND SRM 51-40-14, PARAGRAPH 4N, NR 18. (M) 2 L 7 4 4F A20WE 1996111400415 19961114 00415 NM 1996 11 14 EIAA9639 1 19961003 A 5321 FLOOR BOEING 747 747273C 1384896 NM CABIN CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 68923 20653 SAT - CABIN FLOOR WEB CRACKED AT STATION 520 FORWARD AND AFT, AND CORRODED AT STATION 455, LBL 11. REPAIRED WEB AND INS TALLED DOUBLER PER SRM 51-20-01, 51-40-2, AND 51-10-02. REMOVED CORROSION, TREATED, ALODINED, AND PRIMED PER SRM 51-10- 01. (M) 2 L 7 4 4F A20WE 1996111400416 19961114 00416 WP 1996 11 14 ASAA9680238 1 19961021 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 53016 SEA - PRIOR TO DEPARTURE OF FLT 620, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIV E. REPAIRED TRACK WIRING AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996111400417 19961114 00417 WP 1996 11 14 ASAA9680237 1 19961019 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 974AS 53450 SFO - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996111400418 19961114 00418 WP 1996 11 14 ASAA9680236 1 19961019 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 965AS 53079 PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND DIM. REPLACED THE LIGHT ASSEMBLY AND OPE RATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996111400419 19961114 00419 WP 1996 11 14 ASAA9680235 1 19961019 A 3350 41B004AD07G3 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 943AS 53018 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE AFT CABIN AND THE FORWARD OVERHEAD EMERGENCY LIGHT IN THE TAILCONE AREA WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996111400420 19961114 00420 WP 1996 11 14 ASAA9680234 1 19961017 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 934AS 49235 SJC - FLT 446 - CREW REPORTED AFT CABIN EMERGENCY LIGHTS ILLUMINATED AFTER AIRCRAFT SHUTDOWN COMPLETED. REPLACED BATTER Y PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996111400421 19961114 00421 WP 1996 11 14 ASAA9680233 1 19961017 A 3350 0105610001 LIGHT DOUG DC9 DC983 3022083 WP CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 53016 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE FROM ROW 3 FORWARD. REPLAC ED DAMAGED LIGHT ASSEMBLY AT ROW 3 AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996111400422 19961114 00422 WP 1996 11 14 ASAA9680232 1 19961015 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 979AS 1414 53471 PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996111400423 19961114 00423 WP 1996 11 14 ASAA9680231 1 19961015 A 3350 41B004AD07G3 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 963AS 53077 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 14 TO 16 WERE FOUND INOPERATIVE. REPLACED TH E BATTERIES AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996111400424 19961114 00424 1996 11 14 ASAA9640091 4 19961016 A 3441 HG1050AD05 IRU BOEING 737 7374Q8 NM NR 1 MALFUNCTIONED A A ASAA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 NM 01 754AS 14281 25095 LAX - FLT 582 - DURING DESCENT, CREW REPORTED THAT THE FMC AND BOTH EHSI'S FAILED, NO COMPASS INFORMATION AVAILABLE (EXC EPT THE STANDBY COMPASS), NO TCAS AIRCRAFT SYMBOLS, WARNING FLAGS ON ADI (COMPASS) AND ALL WARNING FLAGS ON EHSI. UNABL E TO RESTORE IN FLIGHT. DIVERTED TO PSP AND LANDED WITHOUT INCIDENT. REPLACED NR 1 IRU AND FERRIED AIRCRAFT TO SEA FOR FURTHER TROUBLESHOOTING. AIRCRAFT OPERATED NORMALLY DURING FERRY FLIGHT. SUBSEQUENTLY REPLACED THE FMC AS PRECAUTIONA RY MEASURE AND SYSTEM OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996111400425 19961114 00425 1996 11 14 96ZZZM1485 4 19961016 A 3460 1689250501 FMC BOEING 737 7374Q8 NM E/E BAY MALFUNCTIONED A A ASAA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 NM 01 754AS 11995 25095 LAX - FLT 582 - DURING DESCENT, CREW REPORTED THAT THE FMC AND BOTH EHSI'S FAILED, NO COMPASS INFORMATION AVAILABLE (EXC EPT THE STANDBY COMPASS), NO TCAS AIRCRAFT SYMBOLS, WARNING FLAGS ON ADI (COMPASS) AND ALL WARNING FLAGS ON EHSI. UNABL E TO RESTORE IN FLIGHT. DIVERTED TO PSP AND LANDED WITHOUT INCIDENT. REPLACED NR 1 IRU AND FERRIED AIRCRAFT TO SEA FOR FURTHER TROUBLESHOOTING. AIRCRAFT OPERATED NORMALLY DURING FERRY FLIGHT. SUBSEQUENTLY REPLACED THE FMC AS PRECAUTIONA RY MEASURE AND SYSTEM OPERATED NORMALLY. REFERENCE ASAA9640091. 2 L 7 2 4F RT A16WE 1996111400426 19961114 00426 WP 1996 11 14 ZIAA969006 1 19961018 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 200 CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 934VV 47488 DURING WALK AROUND INSPECTION, FOUND 1 INCH CRACK ON THE LOWER FUSELAGE AT APPROX STATION 208 ON THE LEFT SIDE FUSELAGE 2ND RIVET ROW ABOVE THE BELLY SKIN LAP SEAM. REPAIRED CRACK AT FUSELAGE STATION 210 LEFT SIDE. FABRICATED FILLER AND D OUBLER AND INSTALLED REPAIR IAW DC-9 SRM 53-04 FIG 37 PG 203 AND 205 SHEET 1 AND 2. (M) 2 L 7 2 4F A6WE 1996111400427 19961114 00427 WP 1996 11 14 96ZZZM1486 1 19960507 A 5414 SKIN DOUG DC9 DC932 3022066 WP NR 2 PYLON CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 940VV 47523 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND SPOTS OF CORROSION ON UNDERSIDE, INBOARD EDGE OF 2 PYLON . REMOVED CORROSION IAW 51-10-3, FOUND SECTION TO BE OUT OF LIMITS IAW 54-01. FABRICATED DOUBLER, TREATED AND PRIMED R EPAIR AND INSTALLED IAW DC9SRM 54-01 FIG 4, 51-10-3, 51-70-2 AND 51-30-2. REBONED DELAMINATION IAW DC9 SRM 51-70-2, 51- 30-2. DIMENSIONS ARE 3 INCHES BY 7.5 INCHES. 2 L 7 2 4F A6WE 1996111400428 19961114 00428 NM 1996 11 14 F3LA96028 1 19961005 A 2730 CONTROLS SYSTEMS BOEING 737 737201 1384454 NM ELEVATOR STIFF A F3LA O OTHER O OTHER AP APPROACH 1 NM 03 205AU 19421 DEN - UPON ARRIVAL, FLIGHT CREW REPORTED ELEVATOR STIFF, ESPECIALLY DURING FLARE. MAINTENANCE CHECKED ALL FLIGHT CONTRO LS FOR MOVEMENT AND POSITION PER MM AND FUOND OK. PERFORMED TEST FLIGHT AND CHECKED OK. (M) 2 L 7 2 4F A16WE 1996111400429 19961114 00429 NM 1996 11 14 F3LA96029 1 19961001 A 5315 FLOOR BEAM BOEING 737 737201 1384454 NM BS 663 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 DURING SERVICE CHECK, INSPECTION REPORTED A 1.25 INCH CRACK IN THE CABIN FLOOR BEAM WEB AT STATION 663, BBL 0. REPAIRED PER BOEING SERVICE BULLETIN 737-57-121D, FIG 4 AND BOEING TELEX M-7272-96-4639. (M) 2 L 7 2 4F A16WE 1996111400430 19961114 00430 NE 1996 11 14 USAASB96214 2 19961021 A 7321 7436024 FUEL CONTROL BOEING 737 7372B7 1384560 NM PWA JT8 JT8D17A 52049 NE NR 2 ENGINE MALFUNCTIONED A A USAA A E UNSCHED LANDING ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 EA 19 274US 22886 EVV - FL 777 - FLIGHT WAS CRUISING AT FL 310 WHEN THE NR 2 ENGINE CAME BACK TO 50 PERCENT POWER OR 2,000 LBS FUEL FLOW. CREW TURNED ON ENGINE HEAT WITH NO EFFECTS ON ENGINE. CREW TURNED ON FUEL HEAT, NR 2 ENGINE WENT PAST NORMAL N1 AND N2 INDICATIONS. CREW HAD NO CONTROL OF THE ENGINE AND SHUT DOWN THE NR 2 ENGINE. CAPTAIN DECLARED AN EMERGENCY AND DIVER TED TO EVV. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. TOTAL SINGLE ENGINE TIME WAS 10 MINUTES. MAINTENANCE REPLACED THE NR 2 ENGINE FUEL CONTROL UNIT AND FUEL PUMP. LEAK CHECK AND ENGINE TRIM RUN GOOD. (M) 2 L 7 2 4F 4 F A16WE E2EA 1996111400431 19961114 00431 NE 1996 11 14 96ZZZM1487 2 19961021 A 7314 378200 FUEL PUMP BOEING 737 7372B7 1384560 NM PWA JT8 JT8D17A 52049 NE NR 2 ENGINE MALFUNCTIONED A A USAA A E UNSCHED LANDING ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 EA 19 274US 22886 EVV - FL 777 - FLIGHT WAS CRUISING AT FL 310 WHEN THE NR 2 ENGINE CAME BACK TO 50 PERCENT POWER OR 2,000 LBS FUEL FLOW. CREW TURNED ON ENGINE HEAT WITH NO EFFECTS ON ENGINE. CREW TURNED ON FUEL HEAT, NR 2 ENGINE WENT PAST NORMAL N1 AND N2 INDICATIONS. CREW HAD NO CONTROL OF THE ENGINE AND SHUT DOWN THE NR 2 ENGINE. CAPTAIN DECLARED AN EMERGENCY AND DIVER TED TO EVV. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. TOTAL SINGLE ENGINE TIME WAS 10 MINUTES. MAINTENANCE REPLACED THE NR 2 ENGINE FUEL CONTROL UNIT AND FUEL PUMP. LEAK CHECK AND ENGINE TRIM RUN GOOD. REFERENCE USAASB96214. 2 L 7 2 4F 4 F A16WE E2EA 1996111400432 19961114 00432 NE 1996 11 14 USAASB96187 2 19960912 A 7260 767043 SEAL BOEING 737 7372B7 1384560 NM PWA JT8 JT8D17A 52049 NE NR 2 ENG GEARBOX LEAKING A USAA A E UNSCHED LANDING ENGINE SHUTDOWN J K WARNING INDICATION FLUID LOSS CL CLIMB 1 EA 19 270AU 22882 BWI - FL 1930 - DURING CLIMB, THE NR 2 ENG LOW OIL PRESS LIGHT ILLUMINATED. THE OIL QTY GAUGE BEGAN DECREASING TO ZERO. CREW SHUT DOWN THE NR 2 ENG. OIL PRESS AT SHUTDOWN WAS 16 PSI. AFTER SHUTDOWN, WINDMILLING OIL PRESS WAS APPROX 15-1 6 PSI. ENG WAS OPERATED FOR APPROX 3 MINS OR LESS AT IDLE PWR. CAPT DECLARED EMERGENCY AND DIVERTED TO BWI, LANDED SAF ELY. TOTAL SINGLE ENGINE TIME WAS 12 MINS. MX FOUND THE N2 TACH GEN GARLOCK SEAL LEAKING ON THE NR 2 ENG ASSY GEARBOX. REPLACED SAME. ALSO, REPLACED THE NR 2 ENG MAIN OIL PUMP, OIL PRESS REGULATING VLV, OIL PRESS IND, OIL FILTER AND THE OIL. OPS CHECK AND LK CHECK NORMAL. (M) 2 L 7 2 4F 4 F A16WE E2EA 1996111400433 19961114 00433 WP 1996 11 14 RAIA961027 2 19961024 A 7320 13711543L401 P3 LINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RT ENGINE CRACKED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CE 03 431AM 881 JLN - FLT 7074 - DURING TAKEOFF RIGHT ENGINE ONLY PRODUCED 90 PERCENT TORQUE. MAINTENANCE REPLACED THE RIGHT ENGINE P3 BLEED LINE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996111400434 19961114 00434 EU 1996 11 14 RAIA961029 1 19961030 A 5311 S53672408228 FRAME AEROSP ATR72 ATR72202 8680940 EU SERVICE DOORWAY CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 723TE 9615 283 STL - CORROSION ON FRAME 37 AT SERVICE DOOR. MAINTENANCE REMOVED CORROSION AND PERFORMED DOUBLER REPAIR. (M) 2 H 7 2 4T RT A53EU 1996111400435 19961114 00435 WP 1996 11 14 HALA96147 1 19961017 A 2740 CONTROL CABLE DOUG DC9 DC951 3022051 WP STAB TRIM BROKEN A HALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 13 EICBH 47796 KOA - FLT 248 - DURING DESCENT INTO KOA, OUT OF TRIM LIGHT CAME ON. STABILIZER TRIM INDICATOR FULL FORWARD AND LOOSE. C OULD NOT MOVE TRIM INDICATOR FORWARD OR AFT. STABILIZER WAS MOVING WHEN TRIM WAS ACTUATED. MANUFACTURED AND REPLACED C ABLE RUN 129. ADJUSTED PER MM 27-40-0. GROUND OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1996111400436 19961114 00436 WP 1996 11 14 HALA96151 1 19961030 A 3350 60030431 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 601AP 12643 47658 HNL - FORWARD EMERGENCY LIGHT INOP. REPLACED POWER BATTERY PACK. OPS CHECK OK. (M) 2 L 7 2 4F A6WE 1996111400437 19961114 00437 WP 1996 11 14 HALA96150 1 19961031 A 3350 60030431 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 601AP 14020 47658 HNL - FORWARD MID CABIN EMERGENCY LIGHTING INOP. REPLACED POWER BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1996111400438 19961114 00438 WP 1996 11 14 HALA96149 1 19961031 A 3350 60030431 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 601AP 9267 47658 HNL - FORWARD CABIN EMERGENCY LIGHTING INOP. REPLACED POWER BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1996111400439 19961114 00439 WP 1996 11 14 ORJA9670 1 19961005 A 5320 DOOR FRAME DOUG DC9 DC983 3022083 WP BS 636-693 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 872RA 49793 LEVEL 2 CORROSION ON MID CARGO COMPARTMENT LOWER DOOR FRAME FROM STATION 636 TO STATION 693. FABRICATED REPAIR PARTS AN D INSTALLED WITH SEALER IAW SRM 53-05, FIGURE 63. (M) 2 L 7 2 4F RT A6WE 1996111400440 19961114 00440 1996 11 14 TSAA9622082 4 19961029 A 2215 75130 SERVO VLV BOEING 737 737297 1384480 NM AILERON MALFUNCTIONED A A TSAA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 WP 13 726AL 22426 FLT 275 - OGG-HNL - AUTOPILOT EXPERIENCED AN UNCOMMANDED ROLL TO THE LEFT. AUTOPILOT WAS SET AS FOLLOWS, AILERON AND EL EV ENGAGED, MAN, HDG OFF. WHILE ESTABILISHED IN A LEFT 15 DEGREES CLIMBING TURN, THE YOKE BEGAN SMALL JERKS LEFT AND RI GHT AND FORWARD AND AFT. AT ABOUT THAT SAME TIME, THE UNCOMMANDED LEFT ROLL BEGAN AT WHICH POINT THE AUTOPILOT WAS DISE NGAGED AND CONTROLS WERE NORMAL. ALSO, WITH HDG SEL, SOMETIMES THE AUTOPILOT WILL ROLL INTO A 4 DEGREES LEFT BANK AND R EMAIN THERE. DEFER PER MEL 22-1, MCDI PLACARD INSTALLED. REMOVED AND REPLACED AILERON SERVO VLV (SYS B) PER MM 22-11-2 1 FOR TROUBLESHOOTING PURPOSES FOR AVIONICS. LEAK CHECK GOOD. AUTOPILOT CHECK OK. REMOVED PLACARD. AIRCRAFT RETURNED 2 L 7 2 4F A16WE 1996111400441 19961114 00441 NM 1996 11 14 TAOA109611 1 19961023 A 2611 824PY SMOKE DETECTOR BOEING 727 727227 1384078 NM AFT LAVATORY FAILED A TAOA K NONE N FALSE WARNING LD LANDING 1 EA 15 925TS 1127 21244 SMOKE ALARM IN LEFT AFT LAVATORY ACTIVATED DURING LANDING, NO SIGNS OF SMOKE OR FIRE. REPLACED LEFT AFT LAVATORY SMOKE DETECTOR, OPERATIONAL CHECKS OK PER MM 26-10-00. (M) 2 L 7 3 4F A3WE 1996111400442 19961114 00442 WP 1996 11 14 Y2PA96086 1 19961016 A 5330 SKIN DOUG DC9 DC915F 3022037 WP FUSELAGE CORRODED A Y2PA K NONE O OTHER IN INSP/MAINT 1 GL 23 194US 64545 47016 YIP - SMALL AREA OF CORROSION NOTED ON THE FORWARD FUSELAGE SKIN, BELOW THE FORWARD BAGGAGE COMPARTMENT OPENING. REMOVA L OF INITIAL CORROSION REVEALED MORE EXTENSIVE (LEVEL 2) AREAS OF CORROSION. REMOVED CORROSION, CLEANED AND TREATED ARE A. FABRICATED AND INSTALLED THE FOLLOWING; INTERNAL FILLER (.050 INCH 2024-T3 MATERIAL), SKIN FILLER (.090 INCH 2024T3 MATERIAL), REPAIR DOUBLER (.063 INC 2024T3 MATERIAL), REPAIR DOUBLER .063 INCH 2024T3 MATERIAL) AND REPAIR TRIPLER (.090 INCH 2024T3 MATERIAL). WORK ACCOMPLISHED PER FLIGHT VEHICLES ENGINEERING AUTHORIZATION NR EA 53-96219. (M) 2 L 7 2 4F A6WE 1996111400443 19961114 00443 WP 1996 11 14 Y2PA96087 1 19961016 A 5311 9911538507 FRAME DOUG DC9 DC915F 3022037 WP FUSELAGE CRACKED A Y2PA K NONE O OTHER IN INSP/MAINT 1 GL 23 194US 47016 YIP - LEFT MAIN FRAME CRACKED BEYOND REPAIRABLE LIMITS. REMOVED AND REPLACED MAIN FRAME. (M) 2 L 7 2 4F A6WE 1996111400444 19961114 00444 WP 1996 11 14 Y2PA96088 1 19961016 A 5330 SKIN DOUG DC9 DC915F 3022037 WP AFT FUSELAGE CANNED A Y2PA K NONE O OTHER IN INSP/MAINT 1 GL 23 194US 47016 YIP - LEFT TAIL SECTION SKIN 'OIL CANNED'. SKIN IS IN THE AREA ADJACENT TO THE AFT AIR STAIRS. SKIN PANEL IS IN AN 'UN PRESSURIZED AREA'. REPLACED SKIN PANEL. (M) 2 L 7 2 4F A6WE 1996111400445 19961114 00445 EU 1996 11 14 SIMA963031 1 19961029 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 EU CABIN FAILED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 451AT 58 451 DFW - FLT 3610 - RAI'D POWER SUPPLY AND BATTERY PACK AT 61WL IAW JIC 33-51 AND OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996111400446 19961114 00446 EU 1996 11 14 96ZZZM1488 1 19961029 A 3350 3012001 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 451AT 58 451 DFW - FLT 3610 - RAI'D POWER SUPPLY AND BATTERY PACK AT 61WL IAW JIC 33-51 AND OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. REFERENCE SIMA963031. 2 H 7 2 4T RT A53EU 1996111400447 19961114 00447 EU 1996 11 14 SIMA963032 1 19961029 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 425MJ 597 425 ORD - FLT 4310 - REMOVED AND REPLACED EMERGENCY POWER SUPPLY AT 43WL IAW ATR 72 JIC 33-51-21. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996111400448 19961114 00448 EU 1996 11 14 SIMA962981 1 19961024 A 2121 011232500 FAN AEROSP ATR72 ATR72212 EU RIGHT FAILED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 322AC A03632 320 FLT 3677 - FLIGHT DIVERTED TO BGS WITH SMELL AND VISIBLE SMOKE IN COCKPIT AND CABIN. EMERGENCY WAS DECLARED AND AIRCRAF T LANDED WITHOUT INCIDENT. AT DFW, TROUBLESHOOTING AND INSPECTION, INCLUDING GROUND RUNS, COULD NOT DUPLICATE PROBLEM, HOWEVER UPON TAXI TO GATE FOR FCF FLIGHT, THE RIGHT RECIRC FAN FAILED FILLING THE COCKPIT WITH SMOKE. MAINTENANCE RETUR NED AIRCRAFT TO HANGAR AND RAI'D THE RECIRC FAN. OPS CHECK GOOD AND RUNS GOOD. NO FCF REQUIRED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996111400449 19961114 00449 NM 1996 11 14 WRLA96046 1 19961025 A 5350 AKC75001 TAILCONE DOUG MD11 MD11 3023602 NM AFT FUSELAGE DAMAGED A A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 273WA 48519 DURING C-CHECK, (UPON COMPLETION OF UNRELATED REPAIRS), TAILCONE WAS BEING RAISED TO 'STOWED' POSITION WHEN A LOUD 'BANG ' WAS HEARD. MAINTENANCE PERSONNEL LOWERED TAIL CONE TO INVESTIGATE. INVESTIGATION FOUND FAILURE OF TAILCONE ACTUATOR ATTACH SUPPORT TO ATTACHING STRUCTURE. MAINTENANCE PERSONNEL REMOVED AND REPLACED TAIL CONE ASSY. AIRCRAFT RETURNED TO SERVICE. DAMAGED TAIL CONE TO BE REPAIRED PER SRM 53-40-00, PAGE 60-64. (M) 2 L 7 3 4F RT A22WE 1996111400450 19961114 00450 NM 1996 11 14 USAASB96211 1 19961006 A 3350 S106 BATTERY PACK BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 281AU 23114 IAH - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT SIGN OVER THE RIGHT FORWARD SERVICE DOOR INOP. MAINTENANCE REPLACED TH E BATTERIES IN THE LIGHT ASSEMBLY OVER THE RIGHT FORWARD SERVICE DOOR. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1996111400451 19961114 00451 NM 1996 11 14 USAASB96215 1 19961024 A 3350 20121 POWER SUPPLY BOEING 737 737301 1384611 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 356US 23559 ALB - MAINTENANCE FOUND THE EMERGENCY LIGHTS IN SEAT ROWS 17 ABC THROUGH 20 ABC INOP. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY IN THE AFT OVERHEAD CABIN. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996111400452 19961114 00452 NM 1996 11 14 AALA961427 1 19960930 A 3397 WIRE BOEING 727 727223 1384074 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 890AA 22006 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PAX SEAT ROW 12 INOPERATIVE. REPAIRED BROKEN EMERGENCY FLOOR LI GHT WIRE BY PAX SEAT ROW 12. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996111400453 19961114 00453 NM 1996 11 14 AALA961426 1 19960927 A 3350 CONNECTOR BOEING 727 727223 1384074 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 715AA 22470 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN AFT SECTION OF MAIN CABIN INOPERATIVE. RESECURED LOOSE CANNON P LUG AT AFT CABIN BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996111400454 19961114 00454 WP 1996 11 14 AALA961494 1 19961008 A 3350 A3060698101 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 438AA 49456 EWR - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PASSENGER SEAT ROW 12D INOPERATIVE. REPLACED BROKEN EMERGENCY F LOOR LIGHT STRIP CONNECTOR BY PAX SEAT ROW 12D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 1996111400455 19961114 00455 WP 1996 11 14 AALA961495 1 19961009 A 3350 A3060698101 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 556AA 53086 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIG HT STRIP CONNECTOR BY FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996111400456 19961114 00456 WP 1996 11 14 AALA961496 1 19961009 A 3350 CONDUCTOR DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 560AA 53090 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT FORWARD END OF MAIN CABIN INOPERATIVE. REPLACED BROKEN/SHORTED FLAT CONDUCTOR WIRE BETWEEN FIRST CLASS CABIN AND MAIN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996111400457 19961114 00457 WP 1996 11 14 AALA961497 1 19961009 A 3350 A3060698101 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 276AA 49273 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIG HT STRIP CONNECTOR BY FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996111400458 19961114 00458 NM 1996 11 14 AALA961507 1 19961013 A 2560 9005225 SQUIB CARTRIDGE BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA O OTHER L NO TEST IN INSP/MAINT 1 SW 07 688AA 25730 GYE - DURING OVERNIGHT CHECK, LEFT AND RIGHT SYSTEM SQUIB TEST FOR OVERWING EMERGENCY EVACUATION SLIDES FAILED TO ILLUMI NATE. AIRCRAFT MAINTENANCE FERRY GYE. REPLACED LEFT AND RIGHT OVERWING EMERGENCY EVACUATION SLIDE SQUIB CARTRIDGES. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1996111400459 19961114 00459 NM 1996 11 14 AALA961455 1 19961006 A 2120 AIR DISTR BOEING 767 767323 1385205 NM GALLEY ODOR A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 351AA 24032 GIG - FLT 904 - EN ROUTE CNF/GIG DURING CRUISE, ELECTRICAL ODOR NOTED IN B/C GALLEY. AIRCRAFT PROCEEDED GIG AND LANDED WITHOUT INCIDENT. CHECKED ALL GALLEY ELECTRICAL FUNCTIONS WITH NO DEFECTS NOTED. CHECKED MAIN WHEEL WELL AREAS, CEILIN G AREA OVER B/C GALLEY AND E/E COMPARTMENT WITH NO DEFECTS FOUND. ACCOMP GROUND ENGINE RUN AND OPERATED PNEUMATIC SYSTE M WITH APU OFF WITH NO DEFECTS FOUND. UNABLE TO DUPLICATE PROBLEM. ACCOMPLISHED FUNCTIONAL CHECK FLIGHT WITH NO DEFECT S FOUND. SYSTEMS OPERATIONAL CHECKED NORMAL AND AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A1NM 1996111400460 19961114 00460 NM 1996 11 14 AALA961508 1 19961011 A 2530 OVEN BOEING 767 767223 1385123 NM GALLEY DIRTY A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 328AA 22328 LHR - FLT 106 - EN ROUTE JFK/LHR DURING CRUISE, FIRST CLASS GALLEY NR 2 OVEN HAD DIRTY INTERIOR CAUSING SMOKE WHEN OVEN DOOR WAS OPENED. NO OTHER ABNORMAL INDICATIONS AND AIRCRAFT PROCEEDED TO LHR AND LANDED WITHOUT INCIDENT. CLEANED INTE RIOR OF FIRST CLASS GALLEY NR 2 OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION WITH NO SMOKE NOTED. (M) 2 L 7 2 4F RT A1NM 1996111400461 19961114 00461 WP 1996 11 14 AALA961452 1 19961003 A 2120 5953625521 DUCT DOUG DC9 DC982 3022082 WP RIGHT DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 499AA 49737 DFW - FLT 701 - AFTER TAKEOFF DFW DURING CLIMB-OUT THROUGH FL 106, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. ACCOMPLISHED ABNORMAL PROCEDURES AND AIRCRAFT RETURNED TO DFW. LIGHT EXTINGUISHED WHEN POWER LEVERS REDUCED DURING DES CENT. AIRCRAFT LANDED DFW WITHOUT INCIDENT. REPLACED RIGHT WATER SEPARATOR DUCT ASSEMBLY. SYSTEM LEAK AND GROUND CHEC KED NORMAL OPERATION. ACCOMPLISHED FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS NOTED. SYSTEM OPERATIONAL CHECKED NORMAL. ( M) 2 L 7 2 4F A6WE 1996111400462 19961114 00462 WP 1996 11 14 AALA961451 1 19961003 A 2161 60714622 CONTROLLER DOUG DC9 DC982 3022082 WP COCKPIT DEFECTIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 411AA 49322 DFW - FLT 1358 - AFTER TAKEOFF DFW DURING INITIAL CLIMB-OUT, CABIN PRESSURIZATION WHEEL BEGAN OSCILLATING AND CABIN TEMP ERATURE BECAME HOT ACCOMPANIED BY FUMES AND SMOKE. AIRCRAFT RETURNED TO DFW AND LANDED OVERWEIGHT WITHOUT INCIDENT. RE PLACED CABIN TEMPERATURE CONTROLLER. ACCOMP GROUND ENGINE RUN WITH PACKS OPERATING AND SYSTEM GROUND CHECKED NORMAL OPE RATION. ACCOMP PACK BURNOUT PROCEDURE. ACCOMP OVERWIGHT LANDING INSPECTION WITH NO DEFECTS FOUND. ACCOMP FUNCTIONAL C HECK FLIGHT WITH NO DEFECTS FOUND. SYSTEM OPERATIONAL CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 1996111400463 19961114 00463 WP 1996 11 14 AALA961493 1 19961009 A 3233 39281375001 CYLINDER DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA O OTHER N FALSE WARNING CL CLIMB 1 SW 07 274AA FAS349 49271 DFW - FLT 1375 - AFTER TAKEOFF LGA WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR RED LIGHT FLICKERED WHILE GEAR WAS COM ING UP AND THEN ILLUMINATED STEADY WITH NO OTHER ABNORMAL INDICATIONS. SELECTED HYDRAULIC PUMPS TO HIGH AND LIGHT EXTIN GUISHED. AIRCRAFT PROCEEDED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR RETRACTION CYLINDER. ACCOM PLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996111400464 19961114 00464 WP 1996 11 14 AALA961477 1 19961007 A 3260 833703 PROX SENSOR ELDEC DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA K NONE N FALSE WARNING CL CLIMB 1 SW 07 479AA 49654 DFW - FLT 1675 - AFTER TAKEOFF TUL WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR RED LIGHT REMAINED ILLUMINATED WITH NO OTHER ABNORMAL INDICATIONS. AIRCRAFT PROCEEDED DFW AND LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR PROXIMITY SWITC H CONTROL UNIT AND PROBLEM CONTINUED DURING LANDING GEAR RETRACTION CHECK. REPLACED NOSE LANDING GEAR UPLOCK PROXIMITY SENSOR. ACCOMPLISHED LANDING GEAR RETRACTION CHECK AND SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996111400465 19961114 00465 WP 1996 11 14 AALA961449 1 19961004 A 5241 CDK21225 DOOR MECHANISM DOUG DC9 DC982 3022082 WP AFT GALLEY SHEARED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 251AA 49270 EWR - DURING OVERNIGHT CHECK, PIN SHEARED IN AFT GALLEY DOOR HANDLE. REPLACED AFT GALLEY DOOR MECHANISM PIN. SYSTEM GR OUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996111400466 19961114 00466 WP 1996 11 14 AALA961453 1 19961004 A 3220 59104475071 GEAR ASSY DOUG DC9 DC983 3022083 WP NLG DAMAGED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 76201 CP1917 53291 ORD - FLT 374 - AFTER TAKEOFF ORD WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR DID NOT RETRACT ACCOMPANIED BY INDICAT IONS THAT AIRCRAFT WAS STILL IN GROUND MODE. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDI NG GEAR ASSEMBLY. ACCOMPLISHED LANDING GEAR RETRACTION CHECK, NOSE GEAR STEERING CHECK, GROUND SENSING SYSTEM CHECK AND ALTERNATE GEAR EXTENSION CHECK WITH NO DEFECTS FOUND. SYSTEMS GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 1996111400467 19961114 00467 WP 1996 11 14 AALA961454 1 19961005 A 2170 21D101 COALESCER DOUG DC9 DC982 3022082 WP CABIN DIRTY A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 463AA 49593 ORD - FLT 1951 - AFTER TAKEOFF ORD DURING CLIMB-OUT, ACRID ELECTRICAL ODOR NOTED IN CABIN AND COCKPIT WITH NO VISIBLE SM OKE. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. OPERATED FANS AND AIR CONDITIONING PACKS WITH NO DEFECTS NO TED. UNABLE TO DUPLICATE ODOR. PRECAUTIONARY REPLACED LEFT AND RIGHT COALESCER BAGS. SYSTEM GROUND CHECKED NORMAL OPE RATION. (M) 2 L 7 2 4F A6WE 1996111400468 19961114 00468 WP 1996 11 14 AALA961445 1 19961002 A 2613 10200074 SENSOR DOUG DC9 DC982 3022082 WP RT PACK DEFECTIVE A AALA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CL CLIMB 1 SW 07 499AA 49737 PBI - FLT 1202 - AFTER TAKEOFF DFW DURING CLIMB-OUT, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. ACCOMPLISHED ABNORMAL PROCEDURES AND LIGHT EXTINGUISHED WHEN RIGHT PACK TURNED OFF. AIRCRAFT PROCEEDED TO PBI AND LANDED WITHOUT INC IDENT. PLACARDED RIGHT PACK DUE TO HIGH TEMPERATURE SENSOR LEAKING. SUBSEQUENTLY REPLACED RIGHT PACK HIGH TEMPERATURE SENSOR AT TPA. ACCOMPLISHED GROUND ENGINE RUN AND SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996111400469 19961114 00469 WP 1996 11 14 AALA961446 1 19961003 A 2160 1297381 THERMOSTAT DOUG DC9 DC982 3022082 WP TAIL COMPT LOOSE A AALA H DEACTIVATE SYST/CIRCUITS J M WARNING INDICATION OVER TEMP CL CLIMB 1 SW 07 499AA 49737 DFW - FLT 2015 - AFTER TAKEOFF TPA DURING CLIMB-OUT AT FL 160, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. ACC OMPLISHED ABNORMAL PROCEDURES AND LIGHT EXTINGUISHED WHEN RIGHT PACK WAS SHUT DOWN. AIRCRAFT PROCEEDED TO DFW AND LANDE D WITHOUT INCIDENT. REPLACED GASKET TO RIGHT PRIMARY HEAT EXCHANGER SUPPLY THERMOSTAT DUE TO THERMOSTAT LOOSE AND GASKE T LEAKING. ACCOMPLISHED GRUOND ENGINE RUN AND SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996111400470 19961114 00470 WP 1996 11 14 AALA961447 1 19961003 A 2613 10200074 SENSOR DOUG DC9 DC982 3022082 WP TAIL COMPT DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 499AA 49737 DFW - FLT 2032 - AFTER TAKEOFF DFW DURING CLIMB-OUT AT FL 135, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. AIR CRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. LIGHT EXTINGUISHED DURING DESCENT. REPLACED LEFT TAIL COMPARTMENT T EMPERATURE SENSOR DUE TO SENSOR TRIPPING AT 150 DEGREES F. ACCOMPLISHED GROUND ENGINE RUN AND SYSTEM LEAK AND GROUND CH ECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996111400471 19961114 00471 EU 1996 11 14 AALA961412 1 19960925 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 14056 463 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT R4 DOOR INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BY R4 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996111400472 19961114 00472 NM 1996 11 14 AALA961408 1 19960923 A 3397 WIRE DOUG MD11 MD11 3023602 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1762B 48552 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PASSENGER SEAT ROW 13C INOPERATIVE. REPAIRED BROKEN EMERGENCY F LOOR LIGHT WIRE BY PAX SEAT 13C. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1996111400473 19961114 00473 WP 1996 11 14 AALA961428 1 19960927 A 5511 SPAR CAP DOUG DC10 DC1030 3023501 WP LT HORIZ STAB CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 163AA 46914 TUL - FOUND LEFT HORIZONTAL STABILIZER AFT SPAR CAP UPPER AFT BARREL NUT HOLE CRACKED. REPAIRED PER ESO 7349 DATED 9/23 /96. (M) 2 L 7 3 4F A22WE 1996111400474 19961114 00474 NM 1996 11 14 AALA961450 1 19961003 A 5320 ABA8312501 SUPPORT DOUG MD11 MD11 3023602 NM BS 450 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1763 48553 TUL - FOUND CENTER AFT GALLEY SUPPORT HAS CORROSION AROUND GALLEY MOUNT HOLE. REMOVED AND REPLACED GALLEY SUPPORT PER S RM 53-00-01 TREATED, PRIMED AND PAINTED PER SRM 51-21-01. (M) 2 L 7 3 4F RT A22WE 1996111400475 19961114 00475 NM 1996 11 14 AALA961466 1 19961004 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 784 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1763 48553 TUL - FOUND NR 7 FLOOR TRACK CORRODED AT LAV DD AFT TIE DOWN. INSTALLED SEAT TRACK PLUG REPAIR PER SRM 53-00-01. (M) 2 L 7 3 4F RT A22WE 1996111400476 19961114 00476 NM 1996 11 14 AALA961456 1 19961007 A 5320 5661223 SUPPORT DOUG MD11 MD11 3023602 NM BS 1890-2007 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1763 48553 TUL - FOUND NR 3 G7 GALLEY FLOOR SUPPORT HAS SEVERAL AREAS OF CORROSION ON THE UPPER SURFACE. FABRICATED A NEW GALLEY F LOOR SUPPORT PER AARD 51-10-00-1 PAGE 1 AND INSTALLED. (M) 2 L 7 3 4F RT A22WE 1996111400477 19961114 00477 NM 1996 11 14 AALA961461 1 19961007 A 5347 TIE DOWN DOUG MD11 MD11 3023602 NM BS 2004-2007 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1763 48553 TUL - AFT TIE DOWN LOG ON G-6 SUPPORT NR 2 HAS CORROSION AT STATION 2000. MANUFACTURED A NEW NR 2 GALLEY SUPPORT FOR GA LLEY NR 6, TREATED, PRIMED AND PAINTED. INSTALLED NEW NR 2 GALLEY SUPPORT PER SRM 53-00-01, VOL I SRM 53-00-01, VOL I A ND SRM 51-10-00-1. (M) 2 L 7 3 4F RT A22WE 1996111400478 19961114 00478 NM 1996 11 14 AALA961463 1 19961007 A 5320 5661223 SUPPORT DOUG MD11 MD11 3023602 NM BS 1890-2007 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1763 48553 TUL - FOUND G-6 NR 1 SUPPORT HAS MULTIPLE AREAS OF MAJOR CORROSION. FABRICATED AND RE-INSTALLED G6 NR 1 STRUCTURE SUPPO RT PER AARD 51-10-00-1 PG 1. (M) 2 L 7 3 4F RT A22WE 1996111400479 19961114 00479 NM 1996 11 14 AALA961434 1 19960926 A 5512 185N0001 SKIN BOEING 757 757223 1384957 NM HORIZ STAB DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 629AA 24587 AFW - LEFT AND RIGHT NR 3 STABILIZER UPPER SKIN PANELS HAVE SEVERAL DENTS, HAIL DAMAGE. PER MRG 757-957. REINSPECT EVE R C-CHECK. (M) 2 L 7 2 4F RT A2NM 1996111400480 19961114 00480 NM 1996 11 14 AALA961435 1 19960926 A 5210 146N6201 HANDLE PAN BOEING 757 757223 1384957 NM R4 DOOR GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 629AA 24587 AFW - FOUND R-4 DOOR HANDLE PAN HAD SMALL GOUGE BLENEDD BEYOND SRM LIMITS. PER MRB 757-959, BLEND OUT AND REFINISHED PE R SRM. (M) 2 L 7 2 4F RT A2NM 1996111400481 19961114 00481 NM 1996 11 14 AALA961448 1 19960929 A 5315 146N5089 FLOOR BEAM BOEING 757 757223 1384957 NM BS 1640 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 663AM 25297 AFW - FOUND FLOOR BEAM AT 1640 HAS CORROSION. PER MRB 757-966. (M) 2 L 7 2 4F RT A2NM 1996111400482 19961114 00482 NM 1996 11 14 AALA961467 1 19961004 A 5321 141N516153 FLOOR BOEING 757 757223 1384957 NM BS 405 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 659AA 24617 AFW - FOUND FLOOR AT STATION 405, RBL 12 HAD CORROSION BLENDED BEYOND LIMITS. REPAIRED PER MRB 757-968. (M) 2 L 7 2 4F RT A2NM 1996111400483 19961114 00483 NM 1996 11 14 AALA961468 1 19961004 A 5315 146N5089 FLOOR BEAM BOEING 757 757223 1384957 NM BS 1640 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 659AA 24617 AFW - FOUND FLOOR BEAM STATION 1640 RBL 30 HAD CORROSION REMOVED BEYOND SRM LIMITS. REPAIRED PER MRB 757-958. (M) 2 L 7 2 4F RT A2NM 1996111400501 19961114 00501 GL 1996 11 14 CALA9601619 2 19961110 A 7261 9634M10P08 GEARBOX BEARING DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 1 ENGINE FAILED A CALA O OTHER Y ENGINE STOPPAGE CR CRUISE 1 SW 09 68043 46902 451220 THE NR 1 ENGINE AUTO SHUTDOWN WHILE CRUISING AT FL 330 EN ROUTE. THE FLIGHT PROCEEDED TO SFO WHERE IT LANDED WITHOUT IN CIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED, A POWER ASSURANCE RUN WAS PERFORMED AND OPERATION CHECKED GOOD. *S/D * TEARDOWN FINDINGS REVEALED THE PRIMARY CAUSE OF ENGINE SHUTDOWN WAS DUE TO INLET GEARBOX DUPLEX BEARING FAILURE. 2 L 7 3 4F 4 F A22WE E23EA 1996111400502 19961114 00502 NM 1996 11 14 CALA9601620 1 19961101 A 5720 CHORD BOEING 727 727227 1384078 NM NR 2 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76753 21249 INSPECTION FOUND A 3 INCH CRACK ON LOWER LEADING EDGE CHORD JUST OUTBOARD OF OUTBOARD TRACK FOR NR 2 LEADING EDGE SLAT. THE CRACK WAS STOP DRILLED, AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-4. 2 L 7 3 4F A3WE 1996111400503 19961114 00503 NM 1996 11 14 CALA9601621 1 19961101 A 5720 CHORD BOEING 727 727227 1384078 NM NR 2 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76753 21249 INSPECTION FOUND A 3.5 INCH CRACK ON LOWER LEADING EDGE CHORD JUST INBOARD OF INBOARD TRACK FOR NR 2 LEADING EDGE SLAT. THE CRACK WAS STOP DRILLED, AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-4. 2 L 7 3 4F A3WE 1996111400504 19961114 00504 NM 1996 11 14 CALA9601622 1 19961016 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 380 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76753 21249 INSPECTION FOUND CORROSION ON TOP OF FLOORBEAM AT BS 380, RBL 48 TO RBL 67. THE CORRODED AREA WAS CUT OUT, A REPAIR WAS INSTALLED IAW SRM 53-10-8, FIGURE 1. 2 L 7 3 4F A3WE 1996111400505 19961114 00505 NM 1996 11 14 CALA9601623 1 19961028 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 1158 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76753 21249 INSPECTION FOUND FLOORBEAM CORRODED AT STA 1158, LBL 49. THE CORRODED AREA WAS CUT OUT, FILLER AND STRAP WERE FABRICATE D AND INSTALLED IAW ECRA 5310-03355. 2 L 7 3 4F A3WE 1996111400506 19961114 00506 NM 1996 11 14 CALA9601624 1 19961015 A 5320 ANGLE BOEING 727 727227 1384078 NM LOWER FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76753 21249 INSPECTION FOUND LOWER BEACON LIGHT PANEL BULGED AT RT EDGE. CORRODED ANGLES WERE REMOVED AND REPLACEMENT ANGLES WERE F ABRICATED AND INSTALLED IAW SRM 51-40-4. 2 L 7 3 4F A3WE 1996111400507 19961114 00507 NM 1996 11 14 CALA9601625 1 19961018 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 1148-1166 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76753 21249 INSPECTION FOUND STRINGER 30 AND SKIN CORRODED BETWEEN STA 1148 TO 1166. THE CORRODED AREA WAS CUT OUT, A STRINGER AND TWO SPLICES WERE FABRICATED AND INSTALLED IAW SRM 53-10-3. 2 L 7 3 4F A3WE 1996111400508 19961114 00508 NM 1996 11 14 CALA9601626 1 19961017 A 5330 SKIN BOEING 727 727227 1384078 NM BS 720 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76753 21249 INSPECTION FOUND FUSELAGE SKIN PANEL BULGED JUST AFT OF RT RAM AIR DOOR ACTUATOR STA 720, STRINGER 28R. THE CORROSION W AS REMOVED, A FILLER AND DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5330-02459. 2 L 7 3 4F A3WE 1996111400509 19961114 00509 NM 1996 11 14 9623906636 1 19961109 A 7931 OIL PRESS LINE BOEING 747 747251B 1384892 NM PWA JT9 JT9D7R4G2 52054 NE NR 1 ENGINE PIN HOLE A NWAA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 636US 23547 15183 ENROUTE, THE NR 1 ENGINE OIL QUANTITY DROPPED TO ZERO. THE OIL PRESSURE FLUCTUATED IN YELLOW BAND FOR FIVE MINUTES THEN DROPPED BELOW THE RED BAND. CREW FOLLOWED COM PROCEDURE, SHUT DOWN THE ENGINE AND CONTINUED FLIGHT TO NRT WITHOUT FURT HER INCIDENT. MAINTENANCE FOUND OIL LEAKING FROM A PIN HOLE IN THE LINE BETWEEN FUEL/OIL COOLER AND THE LOW OIL PRESSUR E SWITCH. REPLACED TUBE ASSEMBLY AND PERFORMED CHECK, UNIT CHECKED NORMAL. 2 L 7 4 4F 4 F A20WE E3NE 1996111400510 19961114 00510 NE 1996 11 14 9623916601 2 19961108 A 7532 PRBC BOEING 747 747151 1384891 NM PWA JT9 JT9D7A 52054 NE NR 4 ENGINE MALFUNCTIONED A NWAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DE DESCENT 1 GL 01 601US 19778 62454 AT TOP OF DESCENT, THE NR 4 ENGINE EXPERIENCED A MILD COMPRESSOR STALL. AS EGT STARTED TO CLIMB TO APPROXIMATELY 850 DE GREES, CREW FOLLOWED COM PROCEDURE, SHUT DOWN THE ENGINE AND ACCOMPLISHED A SUCCESSFUL RESTART AT FL240. FLIGHT CONTINU ED TO NRT WITHOUT FURTHER INCIDENT. BORESCOPE INSPECTION OF 8TH, 9TH AND 15 STAGES OF HPC REVEALED NO DISCREPANCIES. M AINTENANCE CHANGED THE PRBC, CONVERTER VALVE, AND PS4 RESTRICTOR. 2 L 7 4 4F 4 F A20WE E20EA 1996111400511 19961114 00511 EU 1996 11 14 9623923217 1 19961108 A 2920 HYD RESERVOIR AIRBUS 320 A320211 3930320 EU YELLOW HYD SYST LOW FLUID A NWAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 01 317US 197 AS POWER WAS ADVANCED FOR TAKEOFF, RECEIVED HYD-Y RSVR LO LVL MESSAGE. TAKEOFF WAS ABORTED AT 40 KNOTS. AIRCRAFT RETUR NED TO THE GATE WHERE MAINTENANCE SERVICED THE YELLOW HYDRAULIC SYSTEM. 2 L 7 2 4F RT A28NM 1996111400512 19961114 00512 EU 1996 11 14 9623933246 1 19961109 A 3350 321454 POWER SUPPLY AIRBUS 320 A320211 3930320 EU CABIN MALFUNCTIONED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 336NW 14801 7637 400 DURING LINE MAINTENANCE, TEST OF THE EMERGENCY LIGHTS FAULTED INT LOADS FWD-L AND COMM FWD-L. REPLACED EPSU, OPERATIONA L CHECK OK. 2 L 7 2 4F RT A28NM 1996111400513 19961114 00513 WP 1996 11 14 9623949956 1 19961110 A 2810 VENT FLOAT VLV DOUG DC9 DC931 3022065 WP RT WING DIRTY A NWAA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 GL 01 923RW 47183 DURING CLIMB, FUEL WAS SEEN STREAMING FROM RIGHT WING. LOST APPROXIMATELY 1,000 LBS DURING FIRST 30 MINUTES OF FLIGHT. FLIGHT DIVERTED TO DFW AND LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED AND EXERCISED VENT DRAIN FLOAT VALVES, LEAK CH ECK OK. 2 L 7 2 4F A6WE 1996111400514 19961114 00514 WP 1996 11 14 9623959752 1 19961110 A 3260 UNSAFE LIGHT DOUG DC9 DC941 302207N WP LT MLG ILLUMINATED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 752NW 47116 ON DEPARTURE, THE LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. ALL GEAR LIGHTS GREEN WHEN GEAR WAS EXTENDED FOR LANDING. MAINTENANCE INSPECTED AND CHECKED WIRING, UPLATCH ASSEMBLY AND A DJUSTED THE DOOR ROLLER. CYCLED GEAR, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996111400515 19961114 00515 WP 1996 11 14 9623969993 1 19961111 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8986E 47402 DURING LINE CHECK, FOUND EMERGENCY TRACK LIGHTS FROM SEAT 5 AFT WILL NOT GO OUT. FOUND BROKEN GROUND WIRE ABOVE FORWARD GALLEY. REPAIRED WIRE AND ALL LIGHTS OPERATIONALLY CHECKED GOOD. 2 L 7 2 4F A6WE 1996111400516 19961114 00516 WP 1996 11 14 9623979140 1 19961108 A 3350 BATTERY DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 930RC 45729 DURING LINE CHECK, FOUND AFT SECTION OF EMERGENCY LIGHTS FAILED 10 MINUTE TEST. INSTALLED NEW BATTERIES IN BATTERY PACK , OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996111400517 19961114 00517 WP 1996 11 14 9623989152 1 19961103 A 3350 BATTERIES DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8911E 45825 DURING LINE CHECK, FOUND AFT RIGHT HAND AISLE OVERHEAD LIGHT AND TAIL COMPARTMENT OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERIES IN POWER SUPPLY, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996111400518 19961114 00518 WP 1996 11 14 9623999883 1 19961103 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 671MC 47660 DURING LINE CHECK, FOUND OVERHEAD CABIN EMERGENCY LIGHTS AT MID CABIN AREA INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996111400519 19961114 00519 WP 1996 11 14 9624009877 1 19961104 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 786NC 48148 DURING LINE CHECK, FOUND FOUR CEILING LIGHTS AND BOTH OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY POWER SUP PLY B5-33, B5-25 AND B5-26, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996111400520 19961114 00520 NE 1996 11 14 9624011158 2 19961110 A 7230 COMPRESSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20J 52054 NE NR 2 ENGINE STALLED A NWAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DE DESCENT 1 GL 01 158US 46767 86131 AT FL310 WHEN POWER WAS REDUCTED FOR DESCENT, THE NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL. THERE WAS A SUBSEQUENT VI BRATION UNTIL THE ENGINE WAS SHUT DOWN. NO ABNORMAL EGT OR FUEL FLOW INDICATION AT THE TIME OF INCIDENT. FLIGHT CONTIN UED TO DTW WITHOUT FURTHER INCIDENT. INSPECTION OF THE NR 2 ENGINE REVEALED NO DISCREPANCIES. BORESCOPE INSPECTION WIL L BE PERFORMED IN SEA. 2 L 7 3 4F 4 F A22WE E20EA 1996111400521 19961114 00521 NM 1996 11 14 9624022289 1 19961110 A 3350 POWER SUPPLY BOEING 727 727251 138408H NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 289US 21377 DURING PREFLIGHT, FOUND OVERHEAD EMERGENCY LIGHT EXIT SIGN IN FIRST CLASS INOPERATIVE. REPLACED POWER SUPPLY AND BATTER Y PACK, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996111400522 19961114 00522 NM 1996 11 14 9624032704 1 19961110 A 3350 LIGHT BOEING 727 727225 1384077 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 801EA 22432 DURING PREFLIGHT, FOUND RIGHT FORWARD OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996111400523 19961114 00523 NM 1996 11 14 9624042761 1 19961109 A 3350 BATTERY PACK BOEING 727 7272M7 138407S NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 721RW 21200 DURING PREFLIGHT, FOUND COCKPIT EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996111400524 19961114 00524 NM 1996 11 14 9624052285 1 19961111 A 3350 BATTERY PACK BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 285US 21324 DURING PREFLIGHT, FOUND BOTH EMERGENCY EXIT SIGNS ON LEFT SIDE OF AIRCRAFT OVERWING PLUG DOORS INOPERATIVE. REPLACED BA TTERY PACK AND CHARGER, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996111400525 19961114 00525 WP 1996 11 14 9623489957 1 19961021 A 5312 BULKHEAD T CAP DOUG DC9 DC931 3022065 WP BS 756 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 915RW 47139 DURING H-CHECK, FOUND CORROSION ON THE FS 756 BULKHEAD T-CAP BETWEEN LONGERONS 29L TO 29R. REPAIRED T-CAP (P/N 9958212- 3) PER EA 99-111734. 2 L 7 2 4F A6WE 1996111400526 19961114 00526 WP 1996 11 14 9623759854 1 19961011 A 5230 WEB DOUG DC9 DC951 3022051 WP CARGO DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 763NC 47716 DURING H-CHECK, FOUND A CRACK ON THE AFT CARGO DOOR HORIZONTAL BEAM WEB. REPAIRED WEB (P/N 9957665-17) PER EA 98-11724. 2 L 7 2 4F A6WE 1996111400527 19961114 00527 NM 1996 11 14 9623766631 1 19961024 A 5315 FLOORBEAM BOEING 747 747251B 1384892 NM BS 460 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 631US 23111 DURING P-CHECK, FOUND A CRACK IN THE BS 460 UPPER DECK FLOORBEAM WEB AT RBL 55. REPAIRED WEB (P/N 65B10933-34) PER EA 6 6-120426. 2 L 7 4 4F A20WE 1996111400528 19961114 00528 NM 1996 11 14 9623776611 1 19961026 A 5311 FRAME BOEING 747 747251B 1384892 NM BS 400 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 611US 20356 DURING ARMAR VISIT, FOUND CRACKS IN THE BS 400 FRAME INNER CHORD AND WEB AT STR 26R. REPAIRED CHORD AND WEB (P/N 65B079 36-328) PER EA 66-110297. 2 L 7 4 4F A20WE 1996111400529 19961114 00529 NM 1996 11 14 9623786631 1 19961028 A 5753 FITTING BOEING 747 747251B 1384892 NM TE FORE FLAP CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 631US 23111 DURING P-CHECK, FOUND CORROSION ON THE OUTBOARD TRAILING EDGE FORE FLAP INTERIOR SECOND FROM INBOARD ATTACH HOOK FITTING . REPLACED FITTING. 2 L 7 4 4F A20WE 1996111400530 19961114 00530 NM 1996 11 14 9623796631 1 19961029 A 5400 SPAR WEB BOEING 747 747251B 1384892 NM NR 4 PYLON CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 631US 23111 DURING P-CHECK, FOUND A 1.5 INCH CRACK IN THE NR 4 PYLON MID SPAR WEB. REPAIRED WEB (P/N 65B90319-8) PER EA 66-120431. 2 L 7 4 4F A20WE 1996111400531 19961114 00531 WP 1996 11 14 9623809924 1 19961031 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 598-617 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 926RC 47473 DURING H-CHECK, FOUND CORROSION IN THE FUEL TANK TO FUSELAGE ATTACH FITTING BETWEEN FS 598 TO 617. REPLACED FITTING PER SRM 51-10, 51-30. 2 L 7 2 4F A6WE 1996111400532 19961114 00532 WP 1996 11 14 9623819140 1 19961031 A 5320 FITTING DOUG DC9 DC914 3022034 WP BS 491 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 930RC 45729 DURING H-CHECK, FOUND CRACKS IN BOTH THE LONGERON 26L AND 26R END FITTINGS AT FS 491. REPLACED FITTINGS PER SRM 51-30-5 . 2 L 7 2 4F A6WE 1996111400533 19961114 00533 NM 1996 11 14 9623826631 1 19961031 A 5400 FITTING BOEING 747 747251B 1384892 NM NR 2 PYLON CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 631US 23111 DURING P-CHECK, FOUND A CRACK IN THE NR 2 PYLON INBOARD NACELLE STRUT T-FITTING AT NACELLE STATION 300. REPAIRED FITTIN G (P/N 65B90454-2) PER EA 66-120436. 2 L 7 4 4F A20WE 1996111400534 19961114 00534 WP 1996 11 14 9623839140 1 19961104 A 5320 FITTING DOUG DC9 DC914 3022034 WP BS 480 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 930RC 45729 DURING H-CHECK, FOUND THE LONGERON 28L END FITTING CRACKED AT FS 490. REPLACED FITTING PER SRM 51-30-2, 51-30-5. 2 L 7 2 4F A6WE 1996111400535 19961114 00535 WP 1996 11 14 9623849924 1 19961106 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 639 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 926RC 47473 DURING H-CHECK, FOUND A 2 INCH CRACK IN THE FS 639R FRAME LOWER OUTBOARD LEG. REPAIRED FRAME (PSE 53.04.014) PER SRM 51 -10, 51-30, 53-03. 2 L 7 2 4F A6WE 1996111400536 19961114 00536 WP 1996 11 14 9623859924 1 19961106 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 658 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 926RC 47473 DURING H-CHECK, FOUND A 2.5 INCH CRACK IN THE FS 658L FRAME LOWER OUTBOARD LEG. REPAIRED FRAME (PSE 53.09.013) PER SRM 51-30, 53-03. 2 L 7 2 4F A6WE 1996111400537 19961114 00537 WP 1996 11 14 9623869911 1 19961106 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 680 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 961N 47405 DURING M-CHECK, FOUND A CRACK IN THE RBL 42 SEAT TRACK TO FS 680 FLOORBEAM ATTACH FITTING. REPLACED FITTING PER SRM 53- 30-2. 2 L 7 2 4F A6WE 1996111400538 19961114 00538 WP 1996 11 14 9623879140 1 19961106 A 5320 TRAP PANEL DOUG DC9 DC914 3022034 WP LT MLG WW CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 930RC 45729 DURING H-CHECK, FOUND A 3 INCH CRACK IN THE LEFT MAIN LANDING GEAR WHEEL WELL TRAPEZOIDAL PANEL ON THE UPPER OUTBOARD FL ANGE. REPAIRED PER SRM 57-09. 2 L 7 2 4F A6WE 1996111400539 19961114 00539 WP 1996 11 14 9623889911 1 19961108 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 218 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 961N 47405 DURING M-CHECK, FOUND CORROSION IN THE FS 218 CUSP FITTING AT LONGERON 18R. REPLACED FITTING PER 51-10-4, 53-01. 2 L 7 2 4F A6WE 1996111400540 19961114 00540 WP 1996 11 14 9623899872 1 19960817 A 5330 SKIN DOUG DC9 DC951 3022051 WP BS 657 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 781NC 48121 DURING LINE CHECK, FOUND 4 CRACKS IN THE FUSELAGE SKIN AT THE LOWER VHF ANTENNA APPROXIMATELY FS 657 AT LONGERON 30. RE PAIRED SKIN PER SRM 53-04, FIG 12B. 2 L 7 2 4F A6WE 1996111400541 19961114 00541 SO 1996 11 14 COMA9610328 1 19961108 A 5246 12048166003 FASTENER EMB 120 EMB120RT SO FUEL DOOR WORN A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 266CA 120258 SERVICE DOOR WARNING ON AFTER TAKEOFF. REPLACED LATCHES ON FUEL SINGLE POINT SERVICE DOOR AND SECURED DOOR CLOSED. 2 L 7 2 4T RT A31SO 1996111400542 19961114 00542 SO 1996 11 14 COMA9610329 1 19961108 A 6120 30005000052 SIG COND UNIT EMB 120 EMB120RT SO ENGINE MALFUNCTION A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 266CA 11543 120258 AUTO COARSEN SYSTEM DID NOT ARM DURING TAKEOFF. REPLACED THE SIGNAL CONDITIONER UNIT. 2 L 7 2 4T RT A31SO 1996111400543 19961114 00543 WP 1996 11 14 COMA9620017 2 19961110 A 7200 ENGINE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP RIGHT FAILED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 704C 813 AC704 44577 RT ENGINE TORQUE ROLL BACK DURING TAKEOFF. REPLACED RT ENGINE. 2 L 7 2 4T 4 T RT A8SW E4WE 1996111400544 19961114 00544 EA 1996 11 14 COMA9660200 1 19961110 A 2916 73011 HYD RESERVOIR CNDAIR CL600 CL6002B19 EA AFT EQPT BAY LEAKING A COMA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 956CA 5877 665 7105 NR 1 HYDRAULIC SYSTEM QUANTITY INDICATED ZERO. LEAKAGE EVIDENT AT AFT EQUIPMENT BAY. REPLACED THE NR 1 HYDRAULIC RESER VOIR ASSY. 2 L 7 2 4F RT A21EA 1996111400545 19961114 00545 EA 1996 11 14 COMA9660201 1 19961110 A 2760 4916405 SECU CNDAIR CL600 CL6002B19 EA NR 1 SPOILER FAILED A COMA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SO 01 960CA 7117 SPOILERONS FAULT MESSAGE ON EICAS. REPLACED THE NR 1 SPOILER ELECTRONIC CONTROL UNIT. 2 L 7 2 4F RT A21EA 1996111400546 19961114 00546 EA 1996 11 14 COMA9660202 1 19961110 A 2750 857SD10015 FLEX DRIVE CABLE CNDAIR CL600 CL6002B19 EA TE FLAPS CORRODED A COMA O OTHER O OTHER LD LANDING 1 SO 01 940CA 7048 FLAPS FAILED DURING LANDING APPROACH. REPLACED CORRODED FLAP DRIVE FLEX CABLE. 2 L 7 2 4F RT A21EA 1996111400547 19961114 00547 NM 1996 11 14 QXEA9600454 1 19961105 A 3350 8GH0056706 BULB DORNER DO32 DO328100 2996000 NM CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 334PH 3012 EMERGENCY LIGHT IN LAV IS INOP. LAMP REPLACED AND LIGHT OPS CHECKED GOOD. 2 H 7 2 4T RT A45NM 1996111400548 19961114 00548 EU 1996 11 14 QXEA9600455 1 19961106 A 3350 MGG1280 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 450US 11101 CENTER AISLE EMERGENCY EXIT SIGN HAS NUMEROUS BULBS OUT. BULBS WERE REPLACED AND SIGN OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996111400549 19961114 00549 EU 1996 11 14 QXEA9600456 1 19961106 A 3350 MGG1280 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 469US 11096 EXIT SIGN AT ROW 8 HAS SEVERAL LAMPS INOP. BULBS WERE REPLACED AND SIGN OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996111400550 19961114 00550 EU 1996 11 14 QXEA9600457 1 19961108 A 3350 1820 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 466US 11075 EMERGENCY LIGHT AT EXIT 8E IS INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996111400551 19961114 00551 EU 1996 11 14 QXEA9600458 1 19961108 A 2530 180146B COFFEE WARMER FOKKER F28 F28MK1000 4990808 EU GALLEY SHORTED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 469US 11096 BURNING SMELL COMING FROM THE NUMBER TWO COFFEE WARMER. REPLACED COFFEE WARMER AND WARMER OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996111400552 19961114 00552 EU 1996 11 14 QXEA9600459 1 19961110 A 3310 LIGHT BALLAST FOKKER F28 F28MK1000 4990808 EU COCKPIT FAILED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 803PH 11031 BURNT ELECTRICAL SMELL IN COCKPIT, CREW FELT IT WAS LIGHTING BALLEST. SMELL TRACED TO BALLEST FOR WHITE FLOOD LIGHT. L IGHT PLACED ON MEL 33-1. 2 L 7 2 4F RT A20EU 1996111400553 19961114 00553 EU 1996 11 14 QXEA9600460 1 19961110 A 3350 1820 BULB FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 466US 11075 ROW 3 AND 5 OVERHEAD EMERGENCY LIGHTS ARE INOP. BULBS WERE REPLACED AND LIGHTS OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996111400554 19961114 00554 NM 1996 11 14 96FDEA01659 1 19961106 A 2910 HYDRAULIC TUBE DOUG MD11 MD11F 3023600 NM NR 3 ENGINE LEAKING A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 614FE 48528 HYD SYS NR 3 FAIL ALERT DISPLAYED. REMOVED AND REPLACED LEAKING PRESSURE LINE AT NR 3 HYD MANIFOLD. REMOVED AND REPLAC ED HYD FILTERS AND BOTH ENGINE DRIVEN PUMPS. 2 L 7 3 4F RT A22WE 1996111400555 19961114 00555 WP 1996 11 14 ABXA9600662 1 19961106 A 5313 LONGERON DOUG DC9 DC914 3022034 WP BS 408 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 925AX 45728 STATION 408, LONGERON 30 HAS BULGE IN SKIN. REPAIRED IAW DC-9 SRM 53-04, FIG 12B. INTERCOSTAL AT STATION 408, LONGERON 30 IS CORRODED. REPLACED INTERCOSTAL IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 1996111400557 19961114 00557 NE 1996 11 14 ABXA9600663 2 19961107 A 7200 ENGINE DOUG DC8 DC863 302198A WP PWA JT3D JT3D7 52039 NE NR 4 DEFECTIVE A A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 823AX 50168 46122 644128 DURING SERVICE CHECK, FOUND NR 4 ENGINE C1 COMPRESSOR BLADE HAD RUBBED A .75 BY 2.25 INCH HOLE; HOUSING BETWEEN C1 AND C 2 HAD A .25 BY 3 INCH GAP, BOTH AT THE 4 O'CLOCK POSITION. THREE ENGINE FERRIED AIRCRAFT BACK TO ILN. REPLACED NR 4 EN GINE IAW JOB CARD J7002. 2 L 7 4 4F 4 F 4A25 1E8 1996111400558 19961114 00558 WP 1996 11 14 MWEA96624 1 19961109 A 5320 PAN DOUG DC9 DC932 3022066 WP CARGO DOOR JAMB CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 DURING C-CHECK, MAINT SPLICED IN NEW LOWER DOOR JAMB PAN SECTION IN AFT CARGO DOOR CUTOUT WHICH HAD AREA OF CORROSION IA W SRM 53-05, FIG 44. 2 L 7 2 4F A6WE 1996111400559 19961114 00559 WP 1996 11 14 MWEA96625 1 19961111 A 5320 DOOR FRAME DOUG DC9 DC932 3022066 WP AFT CABIN CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 DURING C-CHECK, FOUND CRACK EMANATING FROM UPPER DOOR STOP PAD IN AFT ENTRANCE DOOR FRAME. MAINTENANCE INSTALLED DOUBLE R REPAIR IAW SRM 53-01, FIG 2 SHEET 4. 2 L 7 2 4F A6WE 1996111400560 19961114 00560 WP 1996 11 14 MWEA96626 1 19961111 A 5532 SKIN DOUG DC9 DC932 3022066 WP VERT STAB CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 DURING C-CHECK, FOUND LT VERTICAL STABILIZER SKIN GOUGED UPPER AND LOWER SECTIONS WHERE FAIRINGS CHAFING. REPLACED UPPE R AND LOWER SKIN SECTIONS IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1996111400561 19961114 00561 NM 1996 11 14 SCNA96376 1 19961109 A 3350 900542 POWER SUPPLY BOEING 727 727259 138408J NM CABIN INOPERATIVE A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 289SC 22475 FOUND RIGHT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY PER MM 33-50-71 AND OPS CH ECKED GOOD. 2 L 7 3 4F A3WE 1996111400562 19961114 00562 WP 1996 11 14 SCNA96377 1 19961109 A 3350 110049 BATTERY CHARGER DOUG DC10 DC1010 3022110 WP CABIN INOPERATIVE A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 572SC 46977 FOUND FORWARD RIGHT HAND FLOOR TRACK LIGHTS INOP FROM ROW 1 TO ROW 9. REMOVED AND REPLACED BATTERY CHARGER AND OPS CHEC KED GOOD. 2 L 7 3 4F A22WE 1996111400563 19961114 00563 NE 1996 11 14 SCNA96378 2 19961111 A 7200 ENGINE DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE NR 3 FAILED A SCNA A J UNSCHED LANDING DUMP FUEL B K E SMOKE/FUMES/ODORS/SPARKS FLUID LOSS VIBRATION/BUFFET CL CLIMB 1 GL 15 602GC 47923 455395 DURING CLIMB, EXPERIENCED EXTREME VIBRATION AND NUMBER 3 ENGINE OIL STRAINER CLOG LIGHT ILLUMINATED. RETARDED NUMBER 3 ENGINE THROTTLES AND LIGHT EXTINGUISHED. AFTER SEVERAL MINUTES, OIL PRESSURE DROPPED RAPIDLY, ENGINE FIRE LIGHT ILLUMIN ATED AND SMOKE ENTERED THE CABIN. SHUT DOWN NUMBER 3 ENGINE, DUMPED FUEL AND RETURNED TO SEL. REMOVED AND REPLACED NUM BER 3 ENGINE. 2 L 7 3 4F 4 F RT A22WE E23EA 1996111400564 19961114 00564 NM 1996 11 14 P5CA9600912 1 19961104 A 7110 ANGLE BOEING 747 747122 1384872 NM NR 2 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 CRACKED SKIRT FAIRING ANGLE ON NR 2 ENGINE. REPAIRED PER BAC SRM 51-30-02. 2 L 7 4 4F A20WE 1996111400565 19961114 00565 NM 1996 11 14 P5CA9600913 1 19961104 A 7110 SKIN BOEING 747 747122 1384872 NM NR 2 ENG COWL WORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 WORN LOWER OUTER SKIN ON NR 2 ENGINE FAN COWL. FABRICATED AND INSTALLED DOUBLER PER BAC SRM 51-40-06. 2 L 7 4 4F A20WE 1996111400566 19961114 00566 NM 1996 11 14 P5CA9600914 1 19961104 A 7110 SKIN BOEING 747 747122 1384872 NM NR 2 ENG COWL WORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 WORN OUTER UPPER SKIN ON NR 2 ENGINE FAN COWL. FABRICATED AND INSTALLED DOUBLER PER BAC SRM 51-40-06. 2 L 7 4 4F A20WE 1996111400567 19961114 00567 NM 1996 11 14 P5CA9600915 1 19961104 A 7110 ANGLE BOEING 747 747122 1384872 NM NR 2 ENG COWL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 CRACKED NR 2 ENGINE OUTBOARD CORE COWL ANGLE AT PRECOOLER DOORS. FABRICATED AND INSTALLED NEW ANGLE PER BAC SRM 51-10-0 2. 2 L 7 4 4F A20WE 1996111400568 19961114 00568 NM 1996 11 14 P5CA9600916 1 19961104 A 7110 SKIN BOEING 747 747122 1384872 NM NR 1 ENG COWL WORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 WORN INBOARD TRAILING EDGE SKIN ON NR 1 ENGINE FAN COWL. FABRICATED AND INSTALLED FILLER AND DOUBLER PER BAC SRM 51-40- 06. 2 L 7 4 4F A20WE 1996111400569 19961114 00569 NM 1996 11 14 P5CA9600917 1 19961104 A 5320 STRAPS BOEING 747 747122 1384872 NM NLG WW CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 LEVEL 1 CORROSION ON NOSE LANDING GEAR WHEEL WELL UPPER PRESSURE WEB STRAPS. REMOVED CORROSION PER BAC SRM 51-10-01 AND REPROTECTED PER BAC SRM 51-10-02. 2 L 7 4 4F A20WE 1996111400570 19961114 00570 NM 1996 11 14 P5CA9600918 1 19961104 A 5730 PANEL BOEING 747 747122 1384872 NM LT WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 CRACKED AND DELAMINATED PANEL OUTBOARD OF NR 5 SPOILER ON UPPER LEFT WING. REPAIRED WITH FIBERGLASS OVERLAYS PER BAC SR M 51-40-09 AND REPAINTED PER BAC SRM 51-24-11. 2 L 7 4 4F A20WE 1996111400571 19961114 00571 NM 1996 11 14 P5CA9600919 1 19961104 A 5350 RADOME BOEING 747 747122 1384872 NM FWD FUSELAGE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 DELAMINATED AREAS ON RADOME. REPAIRED PER BAC SRM 51-40-09 AND REPAINTED PER BAC SRM 51-24-11. 2 L 7 4 4F A20WE 1996111400572 19961114 00572 NM 1996 11 14 P5CA9600920 1 19961104 A 5330 SKIN BOEING 747 747122 1384872 NM BS 1800 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 LEVEL 1 CORROSION ON SKIN AROUND ANTENNA AT BS 1800. REMOVED CORROSION PER BAC SRM 51-10-01 AND REPROTECTED PER BAC SRM 51-10-02. 2 L 7 4 4F A20WE 1996111400573 19961114 00573 NM 1996 11 14 P5CA9600921 1 19961105 A 5320 65B611711 FITTING BOEING 747 747122 1384872 NM FWD CARGO BAY BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 BROKEN SIDE RAIL ATTACH FITTING IN FORWARD CARGO BAY ADJACENT TO DOOR. REPLACED RAIL ATTACH FITTING PER BAC MM 25-54-25 . 2 L 7 4 4F A20WE 1996111400574 19961114 00574 NM 1996 11 14 P5CA9600922 1 19961105 A 5522 SKIN BOEING 747 747122 1384872 NM LT ELEVATOR DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 DELAMINATION ON LEFT INBOARD ELEVATOR LOWER SKIN. REPAIRED WITH FIBERGLASS OVERLAYS PER BAC SRM 51-40-09 AND REPAINTED PER BAC SRM 51-24-11. 2 L 7 4 4F A20WE 1996111400575 19961114 00575 NM 1996 11 14 P5CA9600923 1 19961105 A 5522 SKIN BOEING 747 747122 1384872 NM RT ELEVATOR DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 DELAMINATED SKIN ON RIGHT ELEVATOR INBOARD CORNER OF LOWER TRAILING EDGE. REPAIRED WITH FIBERGLASS OVERLAYS PER BAC SRM 51-40-09 AND REPAINTED PER BAC SRM 51-24-11. 2 L 7 4 4F A20WE 1996111400576 19961114 00576 NM 1996 11 14 P5CA9600924 1 19961104 A 5522 SKIN BOEING 747 747122 1384872 NM RT ELEVATOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 CRACK ON RIGHT INBOARD ELEVATOR OUTBOARD TRAILING EDGE LOWER CORNER. REPAIRED WITH FIBERGLASS OVERLAYS PER BAC SRM 51-4 0-09 AND REPAINTED PER BAC SRM 51-24-11. 2 L 7 4 4F A20WE 1996111400577 19961114 00577 NM 1996 11 14 P5CA9600925 1 19961110 A 5522 SKIN BOEING 747 747122 1384872 NM LT ELEVATOR DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 DELAMINATED OUTBOARD TRAILING EDGE CORNER OF LEFT INBOARD ELEVATOR. REPAIRED WITH FIBERGLASS OVERLAYS PER BAC SRM 51-40 -09 AND REPAINTED PER BAC SRM 51-24-11. 2 L 7 4 4F A20WE 1996111400578 19961114 00578 NM 1996 11 14 P5CA9600926 1 19961104 A 5320 DEFLECTOR BOEING 747 747122 1384872 NM BS 2360 BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 BROKEN AIR FLOW DEFLECTOR ON AFT FUSELAGE DRAIN AT BS 2360 RBL 4. REPLACED PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1996111400579 19961114 00579 NM 1996 11 14 P5CA9600927 1 19961110 A 5753 BRACKET BOEING 747 747122 1384872 NM NR 4 TE FLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 BROKEN FORWARD CANOE HANGER BRACKET ON NR 4 FLAP TRACK. REPLACED BRACKET PER BAC MM 27-51-26. 2 L 7 4 4F A20WE 1996111400580 19961114 00580 NM 1996 11 14 P5CA9600928 1 19961105 A 7110 SKIN BOEING 747 747122 1384872 NM NR 3 ENG COWL DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 DAMAGED SKIN ON BOTH AFT CORNERS OF NR 3 ENGINE INBOARD FAN COWL. FABRICATED AND INSTALLED FILLER AND DOUBLERS PER BAC SRM 51-40-06. 2 L 7 4 4F A20WE 1996111400581 19961114 00581 NM 1996 11 14 P5CA9600929 1 19961105 A 7110 SKIN BOEING 747 747122 1384872 NM NR 4 ENG COWL DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 DAMAGED LOWER AFT CORNER SKIN ON NR 4 ENGINE OUTBOARD FAN COWL. FABRICATED AND INSTALLED FILLER AND DOUBLER PER BAC SRM 51-40-06. 2 L 7 4 4F A20WE 1996111400582 19961114 00582 NM 1996 11 14 P5CA9600930 1 19961110 A 7110 RIB BOEING 747 747122 1384872 NM NR 4 ENG COWL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 CRACKED AFT UPPER RIB AND BRACKET ON NR 4 ENGINE OUTBOARD COWL. FABRICATED AND INSTALLED NEW RIB AND BRACKET PER BAC SR M 51-10-01. 2 L 7 4 4F A20WE 1996111400583 19961114 00583 NM 1996 11 14 P5CA9600931 1 19961110 A 5753 BRACKET BOEING 747 747122 1384872 NM NR 4 TE FLAP BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 THREE BROKEN HANGER BRACKETS FOR NR 4 FLAP TRACK CANOE FAIRING. REPLACED BRACKETS PER BAC MM 27-51-26. 2 L 7 4 4F A20WE 1996111400584 19961114 00584 NM 1996 11 14 P5CA9600932 1 19961105 A 7110 CUTOUT BOEING 747 747122 1384872 NM NR 3 ENG COWL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 CRACKED PRECOOLER DOOR CUTOUT ON NR 3 ENGINE INBOARD COWL. FABRICATED AND INSTALLED NEW PART PER BAC SRM 51-10-02. 2 L 7 4 4F A20WE 1996111400585 19961114 00585 NM 1996 11 14 P5CA9600933 1 19961105 A 7110 FLANGE BOEING 747 747122 1384872 NM NR 3 ENG COWL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 CRACKED UPPER FORWARD FLANGE ON NR 3 ENGINE INBOARD COWL. FABRICATED AND INSTALLED NEW FLANGE PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1996111400586 19961114 00586 NM 1996 11 14 P5CA9600934 1 19961110 A 5330 SKIN BOEING 747 747132 1384882 NM BS 2598 DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 DAMAGED SKIN ON AFT FUSELAGE AT BS 2598 FROM S26R TO S42R. REPAIRED PER POLAR AIR MAINTENANCE AUTHORIZATION 5330-12:01. 2 L 7 4 4F A20WE 1996111400587 19961114 00587 1996 11 14 ARWA9611002 4 19961112 A 3442 20709620101 RADAR DOUG DC8 DC863 302198A WP COCKPIT MALFUNCTIONED A ARWA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 19 345JW 46042 RADAR INDICATES 1.5 BY 4 CLUTTER DURING LEVEL FLT, BOTH CAPT AND F/O SCOPES. RETURNED TO SJU WITHOUT INCIDENT. SWAPPED RADAR R/T'S, REMOVED AND REPLACED CAPT'S SCOPE. BOTH SYSTEMS CHECKED GOOD ON THE GROUND PER MM 34-41-1. 2 L 7 4 4F 4A25 1996111400590 19961114 00590 NM 1996 11 14 CKSA96194 1 19961021 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 680 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6811 19486 DURING B-CHECK INSPECTION, FOUND STRINGER 29R CORRODED STA 680. REPAIRED AS PER 727 BOEING SRM 53-10-3 FIGURE NR 1. AD 90-25-03, CORROSION CARD NR C53-113-01 PART 1 OF 2, NON-ROUTINE WORK CARD NR 61464. 2 L 7 3 4F A3WE 1996111400591 19961114 00591 SO 1996 11 14 SRAA961107 1 19961109 A 3230 3881745 BUSHING LKHEED 382 382G 526414U SO RT MLG MISSING A SRAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 23 912SJ 4388 ON APPROACH, RIGHT MAIN LANDING GEAR HAD UNSAFE WARNING INDICATION. FOUND AFT RT MAIN LANDING GEAR SHELF BRACKET BROKEN , TIED DOWN RT GEAR AND DECLARED EMERGENCY FOR LANDING. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED RIGHT MAIN LANDING GEAR SHELF BRACKET, FOUND PIN BUSHING MISSING AND AFT LOWER SHOE BRACKET BROKEN. REPLACED RT AFT SHELF BRACKET AFT BUS HING, ALL RT MLG SHOES ON FORE AND AFT STRUTS. PERFORMED GEAR RETRACTION TEST PER MM CH 32, ALL OPS CHECKED GOOD. 2 H 7 4 4T A1SO 1996111400592 19961114 00592 SO 1996 11 14 CA960416001 2 19960323 A 8530 SA629690 PISTON PIN CONT 653450A5 PIPER PA34 PA34200T 7103406 SO CONT O360 TSIO360EB 17025 SO #4 CYLINDER FRACTURED W K NONE O OTHER IN INSP/MAINT 1 CA 231 OA8524 234298R (CAN)ENGINE TEARDOWN DUE TO METAL CONTAMINATION OF THE OIL. #4 PISTON DISINTEGRATED DUE TO FRACTURE OF PISTON PIN. MAGNA FLUX REVEALS STRESS CRACKING IN ANOTHER PIN. 1 L 7 2 3O 3 O A7SO E9CE 1996111400593 19961114 00593 WP 1996 11 14 CA960416003 2 19960330 A 7322 1390136 DIAPHRAGM SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP R/H ENGINE FC WORN W A O OTHER O OTHER CL CLIMB 1 CA 4558 P54183 (CAN)AFTER TAKEOFF, ENGINE POWER AND TORQUE FELL OFF 50 PERCENT WITH THE POWER LEVER MOVED AFT. SUBSEQUENT INVESTIGATION FOUND THAT THE RIGHT HAND FUEL CONTROL "ROLLING DIAPHRAGM" HAD AN EXCESSIVE LEAK RATE AND WAS REPLACED. ON CAREFUL EXAM INATION, THE "ROLLING DIAPHRAGM" WAS FOUND TO HAVE A HOLE WORN THROUGH. 2 L 7 2 4T 4 T RT A8SW E4WE 1996111400594 19961114 00594 WP 1996 11 14 CA960416004 2 19960403 A 7322 1390136 DIAPHRAGM SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE3313 01514 WP L/H ENGINE WORN W A E O ENGINE SHUTDOWN OTHER R PARTIAL RPM/PWR LOSS AP APPROACH 1 CA 4718 P54214 (CAN)ON APPROACH, ENGINE POWER DROPPED 60 PERCENT. POWER LEVER RESPONSE WAS POOR. SUBSEQUENT INVESTIGATION FOUND THAT TH E LEFT HAND FUEL CONTROL "ROLLING DIAPHRAGM" HAD AN EXCESSIVE LEAK RATE AND WAS REPLA CED. ON CAREFUL EXAMINATION, THE " ROLLING DIAPHRAGM" WAS FOUND TO HAVE A HOLE WORN THROUGH. 2 L 7 2 4T 4 T RT A8SW E4WE 1996111400595 19961114 00595 NM 1996 11 14 CA960416006 1 19960325 A 3241 82970010633 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE #1 NACELLE CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA LH120360 (CAN)DURING WALKAROUND HYDRAULIC FLUID NOTED DRIPPING FROM #1 NACELLE. SYSTEM PRESSURIZED AND FLUID FOUND DRIPPING FROM END OF HYDRAULIC LINE AT ANTI SKID CONTROL VALVE. CRACK NEAR FLARE. 2 H 7 2 4T 4 T RT A13NM E20NE 1996111400596 19961114 00596 1996 11 14 CA960417501 4 19960308 A 3170 6229251002 DATA LINK BOEING 767 767275 NM PWA JT9 JT9D7R4D 52054 NE COCKPIT SHORTED W O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 CA P709631 (CAN)ELECTRICAL SMELL IN COCKPIT DURING DESCENT CB POPPED, RELATED TO ECARS. DATA LINK MODULE REPLACED. 2 L 7 2 RT 4 F RT A1NM E3NE 1996111400597 19961114 00597 EU 1996 11 14 CA960417502 1 19960312 A 2750 FLAPS AIRBUS 320 A320211 3930320 EU WING TE LOCKED W A O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA (CAN)ON FINAL APPROACH, FLAPS LOCKED AT ZERO DEGREES. FLAPLESS LANDING CARRIED OUT. MAINTENANCE CARRIED OUT R.M.A. 27-50 -435 AND 27-50-431. ALL TORQUE LIMITERS INSPECTED AND SYSTEM TESTED. FLAP SYSTEM CHEC K CARRIED OUT. 2 L 7 2 4F RT A28NM 1996111400598 19961114 00598 WP 1996 11 14 CA960417503 1 19960312 A 2530 CA167072 RECEPTACLE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE OVEN ELECT SHORT W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA P657413D (CAN)GALLEY OVEN CIRCUIT BREAKER TRIPPING, GALLEY OVEN SMOKING. MAINTENANCE CHANGED OVEN RECEPTACLE. 2 L 7 2 4F 4 F A6WE E2EA 1996111400599 19961114 00599 WP 1996 11 14 CA960417504 1 19960312 A 2170 COALESCER BAG DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE LT AIR COND CONTAMINATED W O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA P657726D (CAN)AFTER SELECTING LEFT AIR CONDITIONING SUPPLY SWITCH TO "HIGH BLEED OFF" ON GROUND WITH A.P.U. RUNNING, STRONG HEAT ODOUR DETECTED IN CABIN. MAINTENANCE CHANGED LEFT COALESCER BAG. 2 L 7 2 4F 4 F A6WE E2EA 1996111400600 19961114 00600 WP 1996 11 14 CA960417506 1 19960313 A 2170 21700031 COOLING TURBINE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE LT PACK ELECTRICAL SMELL W O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 CA P656975D (CAN)WHEN APU AND LEFT PACK ON, ELECTRICAL SMELL DETECTED IN COCKPIT AND CABIN. MAINTENANCE CHANGED LEFT COALESCER BAG A ND COOLING TURBINE. 2 L 7 2 4F 4 F A6WE E2EA 1996111400601 19961114 00601 WP 1996 11 14 CA960417507 1 19960314 A 4900 AUX.POWER UNIT DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE AIR DIST LEAKING OIL W O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 CA P657270D (CAN)STRONG OIL SMELL IN CABIN WHEN APU USED. MAINTENANCE FOUND APU LEAKING OIL. APU CHANGED. 2 L 7 2 4F 4 F A6WE E2EA 1996111400602 19961114 00602 EU 1996 11 14 CA960417508 1 19960320 A 2121 EVT3454B BLOWER FAN AIRBUS 320 A320211 3930320 EU AIR DIST SEIZED W O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 CA (CAN)BURNING SMELL DETECTED IN COCKPIT, BLOWER AND VENT FANS SHUT OFF. MAINTENANCE FOUND BLOWER FAN SEIZED. DEFECTIVE BL OWER FAN REPLACED. 2 L 7 2 4F RT A28NM 1996111400603 19961114 00603 EU 1996 11 14 CA960417509 1 19960324 A 2750 PROX.SENSOR AIRBUS 320 A320211 3930320 EU FLAP OUT OF RIG W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA (CAN)ON APPROACH WHEN FLAP 2 SELECTED ECAM MESSAGE "F/CTL FLAPS LOCKED ALIGNMENT FAULT". ECAM ACTIONS COMPLETED, LANDING NORMAL. MAINTENANCE FOUND RIGHT FLAP INTERCONNECTING STRUT WITH BOTH SENSORS OUT OF RIG. BOTH PROXIMITY SENSORS RIGGED AS PER M.M. 27-51-44 AND INSPECTION CARRIED OUT ON BOTH FLAPS INTERCONNECTING STRUT. OPERATIONAL CHECK CARRIED OUT. 2 L 7 2 4F RT A28NM 1996111400605 19961114 00605 EU 1996 11 14 CA960417511 1 19960324 A 7603 THRUST LEVER AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE #1 ENGINE FAULT INDICATION W E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 CA 731668 (CAN)ON APPROACH FOLLOWING ECAM MESSAGE "ENGINE #1 THRUST LEVER FAULT" AND "ENGINE #1 FADEC B FAULT", ENGINE SHUT DOWN. FADEC RESET, TEST AND GROUND RUN CARRIED OUT. 2 L 7 2 4F 4 F RT A28NM E29NE 1996111400606 19961114 00606 1996 11 14 CA960417512 4 19960422 A 2370 VIDEO EQUIPMENT BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE CABIN SHOCK W K NONE O OTHER UK UNKNOWN 1 CA P707535 (CAN)TWO FLIGHT ATTENDANTS RECEIVED SHOCKS WHEN OPENING UP CABIN VIDEO SYSTEM. REPAIRED AS PER PERMIT 6-23-6\351-23-360. 2 L 7 2 4F 4 F RT A1NM E3NE 1996111400607 19961114 00607 WP 1996 11 14 CA960417513 1 19960327 A 2530 CA167072 OVEN RECEPTACLE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE GALLEY ELECT SHORT W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA P654059D (CAN)FLIGHT ATTENDANT RECEIVED ELECTRICAL SHOCK OFF GALLEY OVEN AND WAS FOLLOWED BY A BURNING SMELL. MAINTENANCE FOUND P INS ON OVEN BURNT AND OVEN RECEPTACLE DAMAGED. NEW OVEN INSTALLED AND RECEPTACLE CHAN GED. 2 L 7 2 4F 4 F A6WE E2EA 1996111400608 19961114 00608 EU 1996 11 14 CA960417514 1 19960329 A 2752 791A000002 ACTUATOR AIRBUS 320 A320211 3930320 EU LEFT FLAP INOPERATIVE W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA (CAN)ON APPROACH WHEN FLAP 2 SELECTED ECAM MESSAGE "F\CTL FLAPS LOCKED ALIGNMENT FAULT". FLAPLESS LANDING. RMA 27-50-520 CARRIED OUT AND WING TIP BRAKES RESET. ALSO LEFT FLAP ROTARY ACTUATOR CHANGED. 2 L 7 2 4F RT A28NM 1996111400609 19961114 00609 EU 1996 11 14 CA960417515 1 19960330 A 2750 FLAPS AIRBUS 320 A320211 3930320 EU WING TE LOCKED W O OTHER F FLT CONT AFFECTED LD LANDING 1 CA (CAN)FLAP LOCKED, FLAPLESS LANDING CARRIED OUT. MAINTENANCE ACTION INVOLVED CARRYING OUT RMA 27-50-529 AND RESETING BOTH S.F.C.C.'S. OPERATIONAL CHECK CARRIED OUT. 2 L 7 2 4F RT A28NM 1996111400610 19961114 00610 WP 1996 11 14 CA960417516 1 19960401 A 2530 CA167072 OVEN RECEPTACLE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE GALLEY ELECT. SHORT W O OTHER O OTHER DE DESCENT 1 CA P657724D (CAN)WHEN FRIDGE DOOR SLAMMED DURING DESCENT, A LARGE ELECTRICAL ARC JUMPED FROM TROLLEY, STOWED IN AISLE AND HIT THE FL OOR CLOSE TO THE LAVATORY DOOR. PASSENGERS AND CREW VERIFIED THE OCCURRENCE. MAINTENA NCE CHECK FOUND GALLEY OVER #18 RE CEPTACLE DAMAGED. RECEPTACLE REPLACED. 2 L 7 2 4F 4 F A6WE E2EA 1996111400611 19961114 00611 SO 1996 11 14 CA960418001 1 19960410 A 2840 487804 MICRO SWITCHES PIPER PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2C 41532 EA INSTRUMENT PANEL LOOSE SCREWS W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 5000 5000 L463561A (CAN)MICRO SWITCHES ON THE FUEL CONTROL PANEL FOUND LOOSE ON INSPECTION. SUBMITTER SUSPECTS THAT THE PROBLEM WAS FACTORY ORIGINAL. 1 L 7 2 3O 3 O A20SO E14EA 1996111400612 19961114 00612 NE 1996 11 14 CA960418002 2 19960322 A 7200 107006601 RETAINER BELL 205 205A1 1181414 SW LYC T53 T5313B 41549 NE LOCKING TANG BROKEN W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA LE07672 (CAN)LOCKING TANG OF CUP WASHER RETAINER BROKEN. NUT LOST TORQUE AND FELL-OFF FROM GEARSHAFT CAUSING GEAR TO SHIFT AND D ISENGAGE INTERMITTENTLY. NUT AND RETAINER FROUND IN NOSE HOUSING. 1 G 7 1 4U 4 U H1SW E17EA 1996111400613 19961114 00613 SO 1996 11 14 CA960418003 2 19960327 A 7414 10357586 DISTRIBUTOR GEAR BENDIX 101630601 CESSNA 310 310R 2074245 CE CONT O520 IO520M 17032 SO MCAULY ENG MAG FAILED TOOTH W K NONE O OTHER IN INSP/MAINT 1 CA A219114 561748 (CAN)BROKEN TOOTH AND WORN OUT FINGER ON DISTRIBUTOR GEAR. 1 L 7 2 3O 3 O 3A10 E5CE 1996111400615 19961114 00615 CE 1996 11 14 CA960418007 1 19960325 A 3230 GEAR EXTENSION BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA MLG MIS RIGGED W A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS O OTHER AP APPROACH 1 CA PCE50253 (CAN)CREW SELECTED GEAR DOWN AND NOTHING HAPPENED. GEAR WAS EXTENDED MANUALLY AND AIRCRAFT LANDED SAFELY. INVESTIGATION REVEALED THAT THE UNDER FLOOR CIRCUIT BREAKER HAD POPPED DUE TO AN OVERLOAD PLACED ONTHE GEAR MOTOR. THIS OVERLOAD WAS T RACED TO MISRIGGING OF THE GEAR, WHICH WAS RETRACTING TOO FAR INTO THE WHEEL WELLS AND CAUSING THE OVERLOAD. THE MISRIGG ING WAS THOUGHT TO HAVE OCCURRED DUE TO THE AFT CHAIN BEING TOO LOOSE AND POSSIBLY JUMPING OFF THE SPROCKET. 1 L 7 2 3T 4 T A14CE E4EA 1996111400616 19961114 00616 EU 1996 11 14 CA960418008 1 19960401 A 6240 42960 TACH SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ROTOR STICKING W K NONE O OTHER CR CRUISE 1 CA 866 (CAN)ROTOR TACH INDICATION OF 420 RPM (MAX NORM 386 RPM). ALL OTHER INDICATIONS NORMAL. SUBSEQUENT CHECKS FOUND INDICATO R TO BE ERRATIC DUE TO STICKING. 1 G 7 1 3U 3 U H9EU E19EU 1996111400617 19961114 00617 NM 1996 11 14 CA960418011 1 19960324 A 7603 87600518001 CABLE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE LH CONDITION BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 15965 LH120384 (CAN)LEFT HAND LOWER CONDITION LEVER CABLE FOUND FRAYED AND SOME STRANDS BROKEN. AREA ABOUT 6 INCHES FORWARD OF FIREWALL PULLEY. 2 H 7 2 4T 4 T RT A13NM E20NE 1996111400620 19961114 00620 EA 1996 11 14 CA960418015 2 19960409 A 7414 ES10382585 BREAKER POINTS BENDIX D4RN3000 CESSNA 172 172N 2072434 CE LYC O320 O320H2AD 41508 EA MAG CAM FOLLOWER WORN W A UNSCHED LANDING E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CL CLIMB 1 CA 300 4459 RL173076 (CAN)ON THE 100 HOUR INSPECTION, BOTH MAGNETOS HAD BEEN CHECKED FOR CONDITION AND TIMING AS CALLED FOR IN THE CESSNA INS PECTION PROGRAM AND A POST INSPECTION RUN-UP DONE WITH ALL ENGINE PARAMETERS FOUND NORMAL. ON THE FIRST FLIGHT AFTER INS PECTION, A POWER LOSS OCCURRED AT 900 FEET IN THE CLIMB WHICH NECESSITATED AN EMERGENCY LANDING. MAGNETO POINTS CAM FOLL OWER EXCESSIVELY WORN. 1 H 7 1 3O 3 O NT 3A12 E274 1996111400623 19961114 00623 GL 1996 11 14 CA960419001 2 19960410 A 7323 252466712 GOVERNOR AEROSP AS355 AS355F1 8680810 EU ALLSN 250C 250C20F 03013 GL DRIVE SPLINE MISSING W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 1994 CAE840413 (CAN)CIRCLIP AND WASHER SECURING DRIVE GEAR TO GOVERNOR SPLINED DRIVE FOUND MISSING WHEN GOVERNOR REMOVED FOR OVERHAUL. THIS ALLOWS THE DRIVE GEAR TO FLOAT BACK AND FORTH IN THE ENGINE GEARBOX DRIVE. 1 G 7 2 3U 3 U H11EU E4CE 1996111400625 19961114 00625 CE 1996 11 14 CA960419003 1 19960408 A 2140 C10D40M COMBUSTION TUBE JANITROL C10D40M BEECH 99 99 1154002 CE PWA PT6 PT6A20 52043 EA HEATER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1004 11650984M PCE21610 (CAN)DURING A SCHEDULED 500 HOUR HEATER PRESSURE DECAY TEST, LEAKAGE RATE WAS FOUND TO BE EXCESSIVE. UNABLE TO PINPOINT THE EXACT LOCATION DUE TO ACCESS PROBLEMS. HEATER WAS REPLACED AND SENT FOR OVERHAUL. 1 L 7 2 3T 3 T A14CE E4EA 1996111400626 19961114 00626 EA 1996 11 14 CA960419004 2 19960412 A 7414 R16968 MAGNETO BENDIX D6RN3200 PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA LT MAG RT ENG MAG DROP W D RETURN TO BLOCK E VIBRATION/BUFFET TX TAXI/GRND HDL 1 CA R16968 L123968A (CAN)EXCESSIVE MAG DROP, LEFT MAG RIGHT ENGINE, MAGNETO REPLACED WITH SERVICEABLE UNIT 1 L 7 2 3O 3 O A20SO E14EA 1996111400627 19961114 00627 EA 1996 11 14 CA960419005 2 19960403 A 7200 81152 OIL SYSTEM PWA PT6A41 BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA ENGINE CONTAMINATED W C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CA 14107 3641 81152 PCE81152 (CAN)CHIP DETECTOR WARN DURING TAKEOFF, ABORTED. OIL FILTER CONTAMINATED WITH METAL ENGINE REPLACED 1 L 7 2 4T 4 T A24CE E4EA 1996111400628 19961114 00628 EA 1996 11 14 CA960419006 1 19960402 A 5711 C6WM102727 SPAR CAP DHAV C6W100127 DHAV DHC6 DHC6300 EA PWA PT6 PT6A27 52043 EA RH WING SPAR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 18009 461L234 PCE40600 (CAN)CRACK FOUND RUNNING FROM RIVET TO RIVET WHERE THE FORWARD SPAR WEB ATTACHES TO THE CAP. THIS WAS NOTICED THROUGH A LIGHTENING HOLE. SPAR CAP IS ON FORWARD SPAR WHICH SECURES TO THE FORWARD WING ATTACH NOT THE MAIN WING SPAR THAT THE ST RUT ATTACHES TO. 1 H 7 2 3T 4 T A9EA E4EA 1996111400629 19961114 00629 EA 1996 11 14 CA960419007 1 19960411 A 2822 85316 PUMP HYDROAIRE DHAV DHC6 DHC6300 EA PWA PT6 PT6A27 52043 EA NR 1 AFT BOOST BLOCKED INLET W K NONE J L WARNING INDICATION NO TEST IN INSP/MAINT 1 CA 336 H1532A PCE40609 (CAN)DURING PRESTART #1 AFT FUEL BOOST PUMP PRESSURE LIGHT REMAINED ON WHILE TESTING FUEL PUMPS INLET PORTS OF PUMP. FOU ND BLOCKED BY METAL FOIL SELF ADHESIVE LABEL WHICH HAD COME DETACHED FROM THE PUMP. L ABEL FROM PUMP SUPPLIER. PUMP HAD BEEN IN AIRCRAFT FOR 13 MONTHS WITH NO SNAGS. 1 H 7 2 3T 4 T A9EA E4EA 1996111400631 19961114 00631 NE 1996 11 14 CA960419009 2 19960414 A 7321 FUEL CONTROL DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE ENGINE MALFUNCTION W D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CA 9609 LH123141 (CAN)POWER EXCURSION REPORTED ON TAXI-OUT CONFIRMED BY FDR THAT MAXIMUM TORQUE EXCEEDED. PROPELLER ASSEMBLY REPLACED. MF C, ECU AND HARNESS REPLACED PENDING RESULTS OF PWC INVESTIGATION. 2 H 7 2 4T 4 T RT A13NM E20NE 1996111400634 19961114 00634 CE 1996 11 14 CA960422003 1 19960412 A 3201 26410132 MAIN GEAR SPRING CESSNA 208 208B 2073701 CE PWA PT6 PT6A114 52043 NE MATING SURFACES CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 7798 PCE19115 (CAN)THE RIGHT HAND GEAR SPRING WAS BEING REPLACED DUE TO A GOUGE CAUSED BY THE CHAFING OF THE GEAR FAIRING. IT WAS ALSO DISCOVERED THAT THE MATING SURFACES OF THE ATTACHING POINTS WAS CORRODED. SUBMITTER RECOMMENDS A REGULAR LUBRICATION C HECK BE CARRIED OUT. 1 H 7 1 3T 3 T A37CE E4EA 1996111400635 19961114 00635 NM 1996 11 14 CA960422004 1 19960416 A 5320 85310055 WEB DHAV DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NOSE WHEEL WELL CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 22099 LH120360 (CAN)CRACKS FOUND AT X 97.00 AND Z 112.00, Y 0.0, NOSE LANDING GEAR WEB AREA. CRACKS ARE LOCATED 3 INCHES LEFT AND RIGHT OF CENTRE LINE. CRACKS ARE 3 TO 4 INCHES LONG AND ARE RADIATING AFT AT ABOUT A 60 DE GREE ANGLE AND ACROSS AFT OF CROSS STRINGER AT X 97.00. CRACK REPAIRED AS PER R.D. 8-53-039. 2 H 7 2 4T 4 T RT A13NM E20NE 1996111400636 19961114 00636 SO 1996 11 14 CA960422005 1 19960418 A 3260 3674214 MICRO SWITCH 3674214 PIPER PA44 PA44180 7104402 SO LYC O360 O360A1H 41514 EA RT MLG WIRES CUT W A O UNSCHED LANDING OTHER P NO WARNING INDICATION DE DESCENT 1 CA 172 L3465636A (CAN)RIGHT HAND MAIN GEAR SAFE LIGHT FAILED TO ILLUMINATE. SAFE LANDING WAS ACCOMPLISHED AND INVESTIGATION FOUND THE WIR ES ON THE MICRO SWITCH HAD BEEN "SAWED THROUGH" BY A PLASTIC TIE WRAP AS THE GEAR CYC LED. 1 L 7 2 3O 3 O A19S0 E286 1996111400638 19961114 00638 EU 1996 11 14 CA960422007 1 19960417 A 2840 WARNING PANEL BOLKMS 105 BO105C 5626005 EU ALLSN 250C 250C20B 03013 GL CENTRE CONSOLE CHAFED WIRE W K NONE N FALSE WARNING CR CRUISE 1 CA CAE834769 (CAN)THE MAIN FUEL PUMP SWITCH MONITOR LIGHT REMAINED ON WHEN BOOST PUMP WAS ON. AME FOUND WIRE CHAFED ON THE CENTRE CON SOLE, CORNER ANGLE. THIS IS A COMPANY MODIFICATION/INSTALLATION. 1 G 7 2 3U 3 U H3EU E4CE 1996111400639 19961114 00639 SO 1996 11 14 CA960422008 2 19960411 A 8530 CYLINDER HEAD CONT 652955A1 CESSNA 337 337G 2075730 CE CONT O360 IO360G 17025 SO NR 5 CYL CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 902 352436 (CAN)FRONT ENGINE #5 CYLINDER CRACKED APPROXIMATELY 3 INCHES LONG ACROSS THE ROCKER ARM CAVITY AREA. 1 H 7 2 3O 3 O A6CE E1CE 1996111400640 19961114 00640 1996 11 14 CA960422010 4 19960411 A 6113 15573039 BULKHEAD CESSNA CESSNA 337 337G 2075730 CE CONT O360 IO360G 17025 SO MCAULY 2AF34C D2AF34C306 GL PROP SPINNER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 3928 352436 754603 (CAN)FRONT ENGINE SPINNER BULKHEAD ASSEMBLY CRACKED IN NUMEROUS PLACES STARTING AT THE PROP MOUNTING HOLES AND RUNNING T O THE OUTSIDE DIAMETER. 1 H 7 2 3O 3 O A6CE E1CE 5 C P5EA 1996111400641 19961114 00641 NE 1996 11 14 9624065638 2 19961109 A 7261 OIL FILTER BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE NR 2 ENGINE CONTAMINATED A NWAA D E RETURN TO BLOCK ENGINE SHUTDOWN J WARNING INDICATION IN INSP/MAINT 1 GL 01 538US 26485 727167 AFTER PUSHBACK, NR 2 ENGINE OIL FILTER MESSAGE DISPLAYED AFTER ENGINE START. AIRCRAFT RETURNED TO GATE. GROUND MAINTEN ANCE INSPECTED AND REPLACED THE OIL FILTER AND HOUSING. NO CONTAMINATES WERE FOUND. ENGINE RUN AND LEAK CHECK OK. AIR CRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A2NM E17NE 1996111400642 19961114 00642 WP 1996 11 14 9624079920 1 19961110 A 3350 60030451 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 942N 47459 DURING LINE CHECK, FOUND THAT THE INTERIOR OVERWING EMERGENCY EXIT SIGNS WERE INOPERATIVE. REPLACED THE BATTERY PACK/PO WER SUPPLY. CHECKED OK. 2 L 7 2 4F A6WE 1996111400643 19961114 00643 WP 1996 11 14 9624089752 1 19961112 A 3260 DOWNLOCK SWITCH DOUG DC9 DC941 302207N WP LT MLG MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 752NW 47116 AFTER TAKEOFF FROM MSY, THE LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED. FOLLOWED COM PROCEDURE AND DIVERT ED TO MEM. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEFT GEAR UP AND DOWNLOCK SWITCHES. REMOVED, DISASSE MBLED, CLEANED, AND REINSTALLED RESTRICTOR. CYCLED GEAR AT LEAST TEN TIMES. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996111400644 19961114 00644 WP 1996 11 14 9624099977 1 19961110 A 3260 BOLTS DOUG DC9 DC931 3022065 WP RT MLG DOOR LOOSE A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 9341 47390 AFTER TAKEOFF FROM MEM, GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. LIGHT REMAINED ON AFTER FOLLOWI NG COM PROCEDURE. RECYCLED GEAR AND LIGHT EXTINGUISHED. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. FOUND RIG HT MAIN GEAR DOOR ROLLER ATTACH BRACKET BOLTS LOOSE. REPOSITIONED BRACKET AND TIGHTENED BOLTS. GEAR OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996111400645 19961114 00645 WP 1996 11 14 9624119971 1 19961111 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP RT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9335 47337 DURING LINE CHECK, FOUND EMERGENCY ESCAPE LIGHT AT RIGHT ENGINE NACELLE INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY PACK. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996111400646 19961114 00646 WP 1996 11 14 9624129880 1 19961111 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 675MC 47651 DURING LINE CHECK, FOUND TWO OVERWING EMERGENCY LIGHTS WILL NOT ILLUMINATE DURING TEST. REPLACED BATTERIES. OPERATIONA L CHECK OK. 2 L 7 2 4F A6WE 1996111400647 19961114 00647 WP 1996 11 14 9624139959 1 19961112 A 3350 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 919RW 47162 DURING LINE CHECK, FOUND THAT THE TAIL COMPARTMENT EMERGENCY LIGHTS WERE INOPERATIVE. REPAIRED A WIRE SHORTED TO THE CA TWALK. CHECKED OK. 2 L 7 2 4F A6WE 1996111400648 19961114 00648 WP 1996 11 14 9624149971 1 19961111 A 3350 BATTERY DOUG DC9 DC931 3022065 WP RT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9335 47337 DURING LINE CHECK, FOUND THAT THE RIGHT ENGINE NACELLE EMERGENCY LIGHT WAS INOPERATIVE. REPLACED BATTERY PACK AND POWER SUPPLY. CHECKED OK. 2 L 7 2 4F A6WE 1996111400649 19961114 00649 WP 1996 11 14 9624109603 1 19961112 A 3260 SWITCH DOUG DC9 DC932 3022066 WP LT MLG DOOR MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 603NW 47101 DURING CLIMB-OUT OF MEM, GEAR DOOR OPEN LIGHT CAME ON. FOLLOWED COM PROCEDURE AND LIGHT REMAINED ON. RECYCLED GEAR AND LIGHT REMAINED ON. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. REPLACED LEFT GEAR DOOR SWITCH. OPERATIONAL C HECK OK. 2 L 7 2 4F A6WE 1996111400650 19961114 00650 1996 11 14 96FDEA01667 4 19961113 A 3418 STICK SHAKER BOEING 727 727247 138408F NM E/E COMPT ACTIVATED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 233FE 21327 ON TAKEOFF, STALL WARNING STICK SHAKER ACTIVATED AT LIFT OFF. PULLED AND RESET CIRCUIT BREAKER, STALL WARNING CONTINUED . PULLED CIRCUIT BREAKER. INTERROGATED GROUND PROXIMITY WARNING SYSTEM, ANNUNCIATED ANGLE OF ATTACK INOPERATIVE. REPL ACED ANGLE OF ATTACK SENSOR PER MAINTENANCE MANUAL 34-18-51. TESTED STALL WARNING SYSTEM PER MAINTENANCE MANUAL 34-18-0 1 PAGE 501-505 CHECK GOOD. NOTIFIED BY MAINTENANCE OPERATIONS THAT LEFT HAND INBOARD FLAP POSITION TRANSMITTER THAT WAS INSTALLED YESTERDAY HAD SAME PROBLEM ON AIRCRAFT 278. REPLACED AS A PRECAUTION PER MAINTENANCE MANUAL 27-52-2. 2 L 7 3 4F A3WE 1996111400651 19961114 00651 WP 1996 11 14 MWEA96627 1 19961110 A 3350 60030431 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 602ME 48133 DURING C-CHECK, FOUND AFT SECTION OF EMERGENCY LIGHTS IN CABIN CEILING WERE DIM DURING TEST. MAINTENANCE REPLACED BATTE RY POWER SUPPLIES. OPS CHECK GOOD, RETURNED A/C TO SERVICE. 2 L 7 2 4F A6WE 1996111400652 19961114 00652 WP 1996 11 14 MWEA96628 1 19961112 A 3350 101191 LIGHT DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 203ME 47673 DURING SERVICE CHECK FOUND FWD ENTRY EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FWD ENTRY EMERGENCY LIGHT ASSY. OPS CHECK GOOD. RETURNED A/C TO SERVICE. 2 L 7 2 4F A6WE 1996111400653 19961114 00653 WP 1996 11 14 MWEA96629 1 19961112 A 3350 60030451 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 209ME 47730 DURING SERVICE CHECK FOUND TAIL COMPARTMENT WALKWAY EMERGENCY LIGHTS STAY ILLUMUNIATED WHEN POWER IS OFF. MTC REMOVED A ND REPLACED BATTERY POWER SUPPLY. OPS CHECK GOOD. RETURNED A/C TO SERVICE. 2 L 7 2 4F A6WE 1996111400654 19961114 00654 NM 1996 11 14 DLM88962486 1 19961110 A 7430 792055 SWITCH DOUG MD88 MD88 3023688 NM OVERHEAD COCKPIT MALFUNCTIONED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 964DL 49983 WHEN IGNITION SWITCH WAS TURNED TO SYSTEM-B TO TURN ON ENGINE, ANTI-ICE SMOKED. REPLACED IGNITION SELECTOR SWITCH AND I NVERTER RELAY R2-123. 2 L 7 2 4F RT A6WE 1996111400655 19961114 00655 NM 1996 11 14 DLM88962494 1 19961111 A 2133 PRESSURE REG DOUG MD88 MD88 3023688 NM RIGHT MALFUNCTIONED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 27 923DL 49705 ON FINAL APPROACH, GOT SMOKE AND HOT AIR SMELL IN CABIN. BOTH ENGINES AND AIRFOIL ANTI ICE WERE ON . AIR CONDITIONING INDICATIONS WERE NORMAL. C/A: PERFORMED AUG VALVE CHECK PER PFHB. AUG FAILED TEST. REPLACED. THERMOSTAT/ANCPTR/PILO T PRESS REGULATORS, NO HELP. FOUND AUG VALVE MODEL TG, REPLACED SAME. FOUND LEFT PACK PRESSURE REGULATOR BAD. REPLACE D BOTH WATER SEPARATOR BAGS, PRECAUTIONARY. 2 L 7 2 4F RT A6WE 1996111400656 19961114 00656 NE 1996 11 14 DLL10962496 2 19961111 A 7261 BREATHER TUBE 727106575 LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B NE NR 2 ENGINE BROKEN A DALA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SO 27 712DA 193C1088 10270 NR 2 ENGINE HAD OIL LOST IN CRUISE, FOUND OIL BREATHER TUBE BROKEN ABOVE C1 PUMP. 2 L 7 3 4F 4 F A23WE E12EU 1996111400657 19961114 00657 NM 1996 11 14 DL72S962497 1 19961111 A 5320 ANGLE BOEING 727 727232 1384082 NM PANEL 3448R CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 516DA 21432 FOUND CORROSION ON LOWER ATTACH ANGLE FOR ACCESS PANEL 3448R. REPAIRED PER MM 53-30-1. 2 L 7 3 4F A3WE 1996111400658 19961114 00658 NM 1996 11 14 DL72S962498 1 19961111 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 6 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 516DA 21432 FOUND A .50 INCH CRACK NR 6 L/E SLAT COVE SKIN ATTACH ANGLE AT OUTBOARD UPSTOP PAD. REPAIRED PER M/M 57-54-0, PAR. 12. 2 L 7 3 4F A3WE 1996111400659 19961114 00659 NM 1996 11 14 DL72P962502 1 19961107 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM BS 360 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8890Z 21859 10270 FLOOR BEAM STA 360 CORRODED. REPAIRED PER M/M 53-20-11 FIG. 804A. 2 L 7 3 4F A3WE 1996111400660 19961114 00660 NM 1996 11 14 DL72P962503 1 19961108 A 5753 652163395A SKIN BOEING 727 727225 1384077 NM NR 1 TE MID FLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8891Z 21860 10270 INBOARD END OF NR 1 MID-FLAP L/E SKIN DAMAGED, REPAIRED PER MM 57-52-0 FIG 803 REPAIR NR 3. 2 L 7 3 4F A3WE 1996111400661 19961114 00661 NM 1996 11 14 DL72S962506 1 19961017 A 5754 651622296 SKIN BOEING 727 727232 1384082 NM RT LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 526DA 21586 10270 LOWER INBOARD END OF RIGHT WING SLAT WAS CRACKED. REPAIRED PER M/M 57-54-0, FIG. 801. 2 L 7 3 4F A3WE 1996111400662 19961114 00662 NM 1996 11 14 DL72S962507 1 19961017 A 5754 651622292 RIB BOEING 727 727232 1384082 NM RT LE SLAT GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 526DA 21586 10270 RIGHT WING SLAT OUTBOARD TRACK BOLT HOLE DAMAGED. REPAIRED RIB PER M/M 57-54-00, FIG. 809. 2 L 7 3 4F A3WE 1996111400663 19961114 00663 NM 1996 11 14 DL72S962508 1 19961017 A 5754 651622292 RIB BOEING 727 727232 1384082 NM RT LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 526DA 21586 10270 RIB ON RT WING SLAT ACTUATOR WAS FOUND CRACKED. REPAIRED RIB PER M/M 57-54-00, FIG 809. 2 L 7 3 4F A3WE 1996111400664 19961114 00664 NM 1996 11 14 DLM88962509 1 19961111 A 3350 TRACK DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 918DL 49583 EMERGENCY TRACK LIGHTING INOPERATIVE AT FWD CABIN DOOR. REPLACED SECTION OF TRACK WIRING. 2 L 7 2 4F RT A6WE 1996111400665 19961114 00665 1996 11 14 ARWA9611003 4 19961113 A 3442 ANT1S ANTENNA DOUG DC8 DC863 302198A WP FWD FUSELAGE MALFUNCTIONED A ARWA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 19 345JW 46042 EN ROUTE TO ATL FROM SJU, NR 1 RADAR INDICATES NO RETURN WITH LARGE SPIKE DOWN MIDDLE OF DISPLAY. NR 2 RADAR CONSTANTLY SHOWS TEST PATTERN AT ANY SETTING. FLIGHT DIVERTED TO MIA WITHOUT INCIDENT. MAINTENANCE CHANGED RADAR ANTENNA AND SYS TEMS OPS CHECK NORMAL PER M.M. 34-41-1. 2 L 7 4 4F 4A25 1996111400666 19961114 00666 NM 1996 11 14 CKSA96195 1 19961107 A 2782 26344131 DRIVE UNIT BOEING 747 747132 1384882 NM NR 1 LE FLAP WORN A CKSA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 625PL 20247 UHHH-FLT NR 80738: WHEN RETRACTING FLAPS, NR 1 LEADING EDGE FLAP, LEFT SIDE WOULD NOT RETRACT. NR 1 REMAINED INTRANSIT DURING EXTENSION ALSO. REPLACED NR 1 LEFT LEADING EDGE FLAP DRIVE UNIT. OPS CHECKS NORMAL ON GROUND PER MM 27-81-03. 2 L 7 4 4F A20WE 1996111400667 19961114 00667 SO 1996 11 14 SRAA961108 1 19961107 A 2150 GASKET LKHEED 382 382E 526413U SO DIVERTER VLV UNSEATED A SRAA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 GL 23 901SJ 4299 DURING FLIGHT 1005, FOUND RIGHT FORWARD WHEELWELL EXTREMELY HOT WHEN CARGO COMPARTMENT OVERHEAT WARNING LIGHT CAME ON. A IRCRAFT WILL NOT PRESSURIZE PROPERLY, ONLY 7 INCHES PRESSURE AT FL 20.0. TURNED OFF CARGO COMPARTMENT AIR CONDITIONING AND ACCOMPLISHED AIR TURN BACK TO MIA. FOUND GASKET ON DIVERTER VALVE NOT SEATED PROPERLY, REPOSITIONED GASKET. PRESSU RIZED AIRCRAFT, LEAK CHECKED GOOD PER M.M. CH 21.30.00. 2 H 7 4 4T A1SO 1996111400668 19961114 00668 SO 1996 11 14 SRAA961109 1 19961108 A 5320 BEAM LKHEED 382 382G 526414U SO BS 557 CRACKED A SRAA K NONE O OTHER IN INSP/MAINT 1 GL 23 920SJ 4561 POST-FLIGHT INSPECTION AT MHZ FOUND RIGHT WHEELWELL BOW BEAM CRACKED AT STA 557, WL 170. REPAIRED BOW BEAM CRACK PER SR M 53-40-12. 2 H 7 4 4T A1SO 1996112100001 19961121 00001 NM 1996 11 21 AWXA9600667 1 19961111 A 3350 1060091101 LIGHT BOEING 737 737297 1384480 NM CABIN INOP A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 147AW 18575 22630 PHX - FLT 2455 - DURING ROUTINE MAINTENANCE INSPECTION, FOUND L-1 DOOR EMERGENCY EXIT LIGHT (OUTER DOOR) DOES NOT ILLUMI NATE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1996112100002 19961121 00002 NM 1996 11 21 AWXA9600668 1 19961101 A 3397 WIRE BOEING 757 757225 1384959 NM CABIN DISCONNECTED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 915AW 22209 PHX - FLT 8 - DURING ROUTINE SCHEDULED MAINTENANCE, FOUND EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 20. RE-TERMINATED EME RGENCY LIGHT. OPERATIONS CHECK NORMAL. (M) 2 L 7 2 4F RT A2NM 1996112100003 19961121 00003 NE 1996 11 21 AWXA9600669 2 19961110 A 7250 TURBINE BOEING 737 7372E3 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE FAILED A A AWXA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 WP 28 138AW 44161 21475 22792 AIR TURNBACK. WHEN APPLYING TAKEOFF POWER 1 OR 2, MINOR COMPRESSOR STALLS WERE FELT WITH ALL ENGINE INSTRUMENTS INDICAT ING NORMAL SO TAKEOFF WAS CONTINUED. AT ABOUT 12,000 FEET, NR 2 ENGINE HAD RAPID COMPRESSOR STALLS AND EGT WAS RED. SH UTDOWN ENGINE. BORESCOPE PER P AND W TROUBLESHOOTING CHART 72-50. FOUND EVIDENCE OF FOD DAMAGE AT NGV AND MOLTEN METAL AT PLATFORM OF HPT TURBINE. REMOVED AND REPLACED NR 2 ENGINE I.A.W. CARD R5M71005, R5M78002, R5M76001. TRIMMED ENGINE I.A.W. R5M71002. PART TOTAL CYCLES, 33,494. 2 L 7 2 4F 4 F RT A16WE E2EA 1996112100004 19961121 00004 NM 1996 11 21 AWXA9600670 1 19961112 A 3350 6038443M BATTERY SUPPLY BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 178AW 22645 CMH - FLT 400 - DURING ROUTINE MAINTENANCE CHECK, FOUND AFT EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BAT TERY SUPPLY. OPERATIONS CHECK OK. (M) 2 L 7 2 4F RT A16WE 1996112100005 19961121 00005 NM 1996 11 21 AWXA9600671 1 19961025 A 5315 BAC150310281 FLOOR BEAM BOEING 737 73733A 1384673 NM BS 294.5 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 509DC 23636 PAE - FLT 7838 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM STATION 294.5, LBL 12 TO RBL 12, WL 208 . FABRICATED REPAIR AND INSTALLED PER IAW SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1996112100006 19961121 00006 NM 1996 11 21 AWXA9600672 1 19961025 A 5347 BAC1520792 SEAT TRACK BOEING 737 73733A 1384673 NM BS 498-500 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 509DC 23636 PAE - FLT 7838 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION IN SEAT TRACK WELL, STATION 498 TO 500 AND 500 A PLUS 10 INCH, LBL 45, WL 208. REMOVED AND REPLACED SEAT TRACK FROM BS 480-520, LBL 45, WL 208 PER SRM 53-00-52. (M) 2 L 7 2 4F RT A16WE 1996112100007 19961121 00007 NM 1996 11 21 AWXA9600673 1 19961118 A 5315 FLOOR BEAM BOEING 737 73733A 1384673 NM BS 312 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 509DC 23636 PAE - FLT 7838 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM UPPER CHORD BS 312, LBL 15 - RBL 15, WL 208. FABRICATED AND REPAIRED FLOOR BEAM PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1996112100008 19961121 00008 NM 1996 11 21 AWXA9600674 1 19961028 A 5315 FLOOR BEAM BOEING 737 73733A 1384673 NM BS 328 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 509DC 23636 PAE - FLT 7838 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM STATION 328, RBL 24-55, WL 208. REMOVE D, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1996112100009 19961121 00009 NM 1996 11 21 AWXA9600675 1 19961030 A 5313 BAC1506626 STRINGER BOEING 737 73733A 1384673 NM APU DOORWAY CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 509DC 23636 PAE - FLT 7838 - DURING ROUTINE MAINTENANCE CHECK, FOUND TWO AREAS OF CORROSION ON BOTH LOWER CORNERS OF THE APU INLET D OOR OPENING IN APU CAVITY. LOWER STRINGER OUT OF LIMITS. REMOVED AND REPLACED STRINGER PER IAW SRM 51-40-02 AND 52-80- 14. (M) 2 L 7 2 4F RT A16WE 1996112100010 19961121 00010 NM 1996 11 21 AWXA9600676 1 19961030 A 5753 SKIN BOEING 737 73733A 1384673 NM LT TE FOREFLAP DISBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 509DC 23636 PAE - FLT 7838 - DURING ROUTINE MAINTENANCE CHECK, FOUND GRAVEL DAMAGE ON INBOARD END LOWER SURFACE OF L/W INBOARD FOREF LAP. REPAIRED GRAVEL DAMAGE PER IAW SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 1996112100011 19961121 00011 NM 1996 11 21 AWXA9600677 1 19961030 A 5753 SKIN BOEING 737 73733A 1384673 NM RT TE FOREFLAP DISBONDED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 509DC 23636 PAE - FLT 7838 - DURING ROUTINE MAINTENANCE CHECK, FOUND GRAVEL DAMAGE ON LOWER SURFACE INBOARD END, R/W INBOARD FOREFLA P. REPAIRED GRAVEL DAMAGE PER IAW SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 1996112100012 19961121 00012 NM 1996 11 21 AWXA9600678 1 19961102 A 5320 6517688U189 MOPSILL BOEING 737 7373Y0 1384671 NM ENTRY DOOR CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 EICKV 23747 PAE - FLT 7843 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FORWARD ENTRY DOOR MOP SILL. REMOVED MOPSILL AND REPLACED WITH NEW MOPSILL PER SRM 53-10-51, 51-20-01. (M) 2 L 7 2 4F RT A16WE 1996112100013 19961121 00013 NM 1996 11 21 AWXA9600679 1 19961029 A 5315 FLOOR BEAM BOEING 737 7373Y0 1384671 NM BS 312 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 EICKV 23747 PAE - FLT 7843 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORRSION ON FLOOR BEAM BS 312, WL 208, RBL 10, LBL 10. REMOVED , FABRICATED AND REPLACED FLOOR BEAM TOP CAP FROM RBL 20 TO LBL 20, BS 312, WL 208. (M) 2 L 7 2 4F RT A16WE 1996112100014 19961121 00014 NM 1996 11 21 RAAA96B2042 1 19961109 A 3350 86210066 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 ROW 22 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE LOW CHARGE. 2 L 7 3 4F A3WE 1996112100015 19961121 00015 NM 1996 11 21 RAAA96B1011 1 19961101 A 5320 WEB BOEING 727 72722C 138400F NM BS 1223 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S5 INSPECTION PER CARD S5-34103 FOUND .1250 INCH CRACK IN LT LOWER TORQUE BOX INBD WEB AT BS 1223, WL 1 84, LBL 20. REPAIRED PER SRM 51-40-2. 2 L 7 3 4F A3WE 1996112100016 19961121 00016 NM 1996 11 21 RAAA96B1012 1 19961101 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 850-870 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S5 INSPECTION PER CARD S5-21005 FOUND LEFT STRINGER 18A LOWER FLANGE CORRODED AT BS 850-870, WBL 70. RE PAIRED PER BOECOM INSTRUCTION MESSAGE 72-93-1493, REFERENCE BOECOM TELEX 32-9430. 2 L 7 3 4F A3WE 1996112100017 19961121 00017 NM 1996 11 21 RAAA96B1013 1 19961101 A 5753 SPAR CHORD BOEING 727 72722C 138400F NM RT TE MID FLAP CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S5 INSPECTION PER CARD S5-22113 FOUND RT INBD MID FLAP REAR SPAR LOWER CHORD CORRODED AT WBL 79. REPAI RED PER SRM 51-40-2. 2 L 7 3 4F A3WE 1996112100018 19961121 00018 NM 1996 11 21 RAAA96B1014 1 19961101 A 5753 SPAR CHORD BOEING 727 72722C 138400F NM RT TE MID FLAP CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S5 INSPECTION PER CARD S5-22113 FOUND RT INBD MID FLAP REAR SPAR LOWER CHORD CORRODED AT WBL 89. REPAI RED PER SRM 51-40-2. 2 L 7 3 4F A3WE 1996112100019 19961121 00019 NM 1996 11 21 RAAA96B1015 1 19961101 A 5744 651926010 FITTING BOEING 727 72722C 138400F NM WS 693.5 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S5 INSPECTION PER CARD S5-21110, FOUND LT OUTBD AILERON HINGE ASSY SUPPORT FITTING CORRODED AT WS 693.5 . REPLACED FITTING PER SRM 51-10. 2 L 7 3 4F A3WE 1996112100020 19961121 00020 NM 1996 11 21 RAAA96B1016 1 19961101 A 5744 65192591 FITTING BOEING 727 72722C 138400F NM WS 727 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S5 INSPECTION PER CARD S5-21110, FOUND LT OUTBD AILERON HINGE ASSY SUPPORT FITTING CORRODED AT WS 727. REPLACED FITTING PER SRM 51-10. 2 L 7 3 4F A3WE 1996112100021 19961121 00021 NM 1996 11 21 RAAA96B1017 1 19961101 A 5320 WEB BOEING 727 72722C 138400F NM BS 1240 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S5 INSPECTION PER CARD S5-34103 FOUND .25 INCH CRACK IN LT LOWER TORQUE BOX INBD WEB AT LIGHTNING HOLE BS 1240. REPAIRED PER SRM 51-40-2. 2 L 7 3 4F A3WE 1996112100022 19961121 00022 NM 1996 11 21 RAAA96B1018 1 19961101 A 5320 WEB BOEING 727 72722C 138400F NM BS 1306 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S5 INSPECTION PER CARD S5-34103 FOUND .25 INCH CRACK IN LT LOWER TORQUE BOX INBD WEB AT LIGHTNING HOLE BS 1306. REPAIRED PER SRM 51-40-2. 2 L 7 3 4F A3WE 1996112100023 19961121 00023 NM 1996 11 21 RAAA96B1019 1 19961101 A 5720 STIFFENER BOEING 727 72722C 138400F NM LT WING CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S5 INSPECTION OF LT WING LEADING EDGE CAVITY PER CARD S5-22107. FOUND LEADING EDGE RIB LOWER CHORD STI FFENER CORRODED AT SLAT STA. 33. REPLACED STIFFENER PER SRM 51-20-5. 2 L 7 3 4F A3WE 1996112100025 19961121 00025 NM 1996 11 21 RAAA96B1021 1 19961101 A 5713 STRINGER BOEING 727 72722C 138400F NM RT WING CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S5 INSPECTION OF RT WING PER CARD S5-22105, FOUND OUTER WING STR 18R UPPER FLANGE AT WBL 70 OUTBD FLANG E CORRODED BETWEEN BS 846 AND 866. REWORKED UPPER CHORD WBL 70 PER BOEING TELEX 32-9430 RVV-SEA-96-0002RR DATED 10-22-9 6. 2 L 7 3 4F A3WE 1996112100026 19961121 00026 NM 1996 11 21 RAAA96B1022 1 19961101 A 3350 86210066 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 ROW 22 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE LOW CHARGE. 2 L 7 3 4F A3WE 1996112100027 19961121 00027 NM 1996 11 21 RAAA96B1023 1 19961101 A 3350 86210066 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 ROW 17 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE LOW CHARGE. 2 L 7 3 4F A3WE 1996112100028 19961121 00028 NM 1996 11 21 RAAA96B1024 1 19961101 A 3350 86210144 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 RIGHT FWD OVERWING EMERGENCY EXIT EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. 2 L 7 3 4F A3WE 1996112100029 19961121 00029 NM 1996 11 21 RAAA96B1025 1 19961101 A 3350 86210144 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 RIGHT AFT OVERWING EMERGENCY EXIT EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. 2 L 7 3 4F A3WE 1996112100030 19961121 00030 NM 1996 11 21 RAAA96B1026 1 19961101 A 3350 86210144 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 RIGHT SERVICE DOOR EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. 2 L 7 3 4F A3WE 1996112100031 19961121 00031 NM 1996 11 21 RAAA96B2043 1 19961109 A 3350 86210066 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 ROW 17 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE LOW CHARGE. 2 L 7 3 4F A3WE 1996112100032 19961121 00032 NE 1996 11 21 9624342705 2 19961109 A 7230 COMPRESSOR BOEING 727 727225 1384077 NM PWA JT8 JT8D15 52051 NE ENGINE STALLED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 01 802EA 22433 UPON APPLICATION OF TAKEOFF POWER, AN ENGINE STALL OCCURRED. CREW ABORTED TAKEOFF AND RETURNED TO GATE. CREW WAS NOT A BLE TO DETERMINE WHICH ENGINE CAUSED THE STALL. WINDS WERE REPORTED GUSTING AT 24 KNOTS. MAINTENANCE INSPECTED INLETS AND OUTLETS ON ALL THREE ENGINES WHICH CHECKED OK. SUSPECT STALL CAUSED BY CROSSWINDS. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 1996112100033 19961121 00033 WP 1996 11 21 9624359163 1 19961113 A 5610 5887275501 WINDSHIELD DOUG DC9 DC914 3022034 WP COCKPIT CRACKED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 8906E 9999 45747 DURING CLIMB MSP-CVG, THE CENTER WINDSHIELD ARCED AND CRACKED. RETURNED TO MSP WITHOUT FURTHER INCIDENT. REPLACED THE CENTER WINDSHIELD AND HEAT CONTROLLER (CONTROLLER P/N 961-5059-002, S/N 3533). 2 L 7 2 4F A6WE 1996112100034 19961121 00034 WP 1996 11 21 9624369920 1 19961110 A 3350 LIGHT DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 942N 47459 DURING LINE CHECK, FOUND FORWARD INTERIOR OVERWING EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED BATTERIES AND POWER SUP PLY. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996112100035 19961121 00035 EU 1996 11 21 9624403242 1 19961112 A 3260 848401 PROX SENSOR AIRBUS 320 A320212 EU LT MLG FAILED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 342NW 381 DURING CLIMB-OUT AFTER LANDING GEAR RETRACTION, RECEIVED L/G SYS DISAGREE MESSAGE. CYCLED LANDING GEAR AND ALL INDICATI ONS NORMAL. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING REVEALED FAILUR E MESSAGE LT L/G DNLK PROX SENSOR 15GA TGT POS. REPLACED PROXIMITY SENSOR 15GA. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996112100036 19961121 00036 NM 1996 11 21 9624415516 1 19961113 A 3350 BATTERY BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 516US 23204 DURING PREFLIGHT, FOUND EMERGENCY LIGHT AT DOOR 4R INOPERATIVE. REPLACED BATTERY AND POWER SUPPLY. OPERATIONAL CHECK O K. 2 L 7 3 4F A3WE 1996112100037 19961121 00037 SO 1996 11 21 COMA9610330 1 19961113 A 3060 78614423 DEICE LEAD EMB 120 EMB120RT SO RT PROP BROKEN A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 263CA 120255 RIGHT PROPELLER DEICE FAILED. REPLACED ELECTRICAL DEICE LEAD ON RT PROPELLER. 2 L 7 2 4T RT A31SO 1996112100038 19961121 00038 NE 1996 11 21 COMA9630160 2 19961113 A 7321 6055T19P04 FUEL CONTROL SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE RT ENG LEAKING A COMA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 357CA 20148 224 340A044 STRONG FUEL SMELL IN AIRCRAFT AFTER TAKEOFF. REPLACED THE RT ENGINE FUEL CONTROL UNIT. PART TOTAL CYCLES, 23,980. 2 L 7 2 4T 4 T RT A52EU E8NE 1996112100039 19961121 00039 EU 1996 11 21 COMA9630158 1 19961112 A 2731 TRIM ACTUATOR SAAB SF340 SF340A 7850100 EU ELEVATOR FROZEN A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 357CA 340A044 MAIN PITCH TRIM STUCK IN FULL DOWN POSITION. APPLIED WARM GLYCOL TO TRIM ACTUATOR, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1996112100040 19961121 00040 EU 1996 11 21 COMA9630159 1 19961112 A 6120 B NUT SAAB SF340 SF340A 7850100 EU LT ENGINE LOOSE A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 358CA 340A047 AUTO COARSEN WOULD NOT ARM ON TAKEOFF. ABORTED TAKEOFF. FOUND LOOSE B-NUT ON LT ENG. P3 SWITCH, TIGHTEN B-NUT. OPS C HECK GOOD. 2 L 7 2 4T RT A52EU 1996112100041 19961121 00041 EA 1996 11 21 COMA9660203 1 19961111 A 2752 85201009 ACTUATOR CNDAIR CL600 CL6002B19 EA RT TE FLAP MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 940CA 2728 2728 7048 FLAP FAIL MESSAGE WHEN 20 DEGREES SELECTED. FOUND RIGHT INBD FLAP ACTUATORS, INBOARD AND OUTBOARD TO BE THE PROBLEM, REP LACED ACTUATORS, OPS CHECK GOOD. PART TOTAL CYCLES, 1,108. 2 L 7 2 4F RT A21EA 1996112100042 19961121 00042 EA 1996 11 21 COMA9660204 1 19961102 A 5347 601R310329 SEAT TRACK CNDAIR CL600 CL6002B19 EA BS 5590 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 941CA 5346 5346 7050 DURING TASK -53-170-500LBL9 SEAT TRACK CORRODED FROM F.S. 5590 PLUS 9 TO 5590 PLUS 85. REMOVED AND REPLACED SAID SEAT T RACK SECTION. PART TOTAL CYCLES 4,779. 2 L 7 2 4F RT A21EA 1996112100043 19961121 00043 EA 1996 11 21 COMA9660205 1 19961113 A 3020 300013000002 VALVE CNDAIR CL600 CL6002B19 EA LT ENGINE MALFUNCTION A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 962CA 1077 7123 LEFT ENGINE COWL ANTI-ICE INOP MESSAGE ON EICAS. REPLACED THE 14TH STAGE COWL ANTI-ICE VALVE. PART TOTAL CYCLES, 1,023. 2 L 7 2 4F RT A21EA 1996112100044 19961121 00044 1996 11 21 COMA9660206 4 19961113 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA STALL WARNING TRIPPED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 965CA 7131 STALL FAIL MESSAGE ON EICAS. RESET THE STALL WARNING COMPUTER AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1996112100045 19961121 00045 NM 1996 11 21 SWAA961233 1 19961110 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 20SW 21337 DURING SCHEDULED 1/2 D-CHECK, FOUND NR 28 CABIN WINDOW CUTOUT CRACKED IN UPPER AFT CORNER. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996112100046 19961121 00046 NM 1996 11 21 SWAA961234 1 19961110 A 5320 ANGLE BOEING 737 7372H4 138448C NM PAX DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 20SW 21337 DURING SCHEDULED 1/2 D-CHECK, FOUND FWD ENTRY DOOR FRAME ANGLE CRACKED 16 INCHES UP FROM FLOOR APPROX 3 INCHES LONG. RE PAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996112100047 19961121 00047 NM 1996 11 21 SWAA961235 1 19961110 A 5210 SKIN BOEING 737 7372H4 138448C NM PAX DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 20SW 21337 DURING SCHEDULED 1/2 D-CHECK, FOUND FWD ENTRY DOOR INNER SKIN CRACKED IN MIDDLE AREA BOTTOM OF TORQUE TUBE ACCESS CUTOUT . REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996112100048 19961121 00048 NM 1996 11 21 SWAA961236 1 19961110 A 5312 BULKHEAD BOEING 737 7372H4 138448C NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 20SW 21337 DURING SCHEDULED 1/2 D-CHECK, FOUND AFT CARGO FWD PRESSURE BULKHEAD AT BS 727 COMPRESSION CHORD CRACKED IN RADIUS OF LOW ER LEG. REPAIRED PER SWA RA 1-253-1555. 2 L 7 2 4F A16WE 1996112100049 19961121 00049 NM 1996 11 21 SWAA961237 1 19961110 A 3350 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 20SW 20925 DURING SCHEDULED SERVICE CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F A16WE 1996112100050 19961121 00050 NM 1996 11 21 SWAA961238 1 19961108 A 5312 BULKHEAD BOEING 737 7372H4 138448C NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 26SW 21117 DURING SCHEDULED SERVICE VISIT CHECK, FOUND BS 727 BULKHEAD CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996112100051 19961121 00051 NM 1996 11 21 SWAA961239 1 19961113 A 3350 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 55SW 21593 DURING SCHEDULED TERMINAL CHECK, FOUND FUSELAGE EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F A16WE 1996112100052 19961121 00052 1996 11 21 SWAA961240 4 19961111 A 2565 22D22900131 SLIDE BOEING 737 7372H4 138448C NM FWD ENTRY DOOR PRESS LOW A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 83SW 22732 DURING WALKAROUND CHECK, FOUND FWD ENTRY DOOR SLIDE PRESSURE BELOW MINIMUM LIMITS. REPLACED SLIDE PER BOEING M/M. 2 L 7 2 4F A16WE 1996112100053 19961121 00053 NM 1996 11 21 SWAA961241 1 19961111 A 5320 WEB BOEING 737 7372T4 1384492 NM BS 726 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED SV CHECK, FOUND CRACK IN WEB, BS 726, STRINGER 18A, LEFT SIDE. REPAIRED PER BOEING M/M. 2 L 7 2 4F A16WE 1996112100054 19961121 00054 NM 1996 11 21 SWAA961242 1 19961107 A 5511 RIB BOEING 737 7373H4 1384600 NM RT HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED D-CHECK, FOUND RT HORZ STAB L/E RIBS NR 1, 3, 4, 5, 6 AND 7 CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996112100055 19961121 00055 NM 1996 11 21 SWAA961243 1 19961109 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED BC4 CHECK, FOUND EMERGENCY EXIT LIGHT AT ROW 22R INOP. REPLACED LIGHT ASSEMBLY PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996112100056 19961121 00056 NM 1996 11 21 SWAA961244 1 19961107 A 5242 DOOR BOEING 737 7373H4 1384600 NM E/E COMPT OPEN A SWAA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 SW 07 357SW 26594 AFTER TAKEOFF, AIRCRAFT WOULD NOT PRESSURIZE, NO WARNING INDICATION. RETURNED TO HOU AND MADE AN UNEVENTFUL LANDING. I NSPECTED AND FOUND E AND E DOOR OPEN. SECURED DOOR, DEFERRED WARNING LIGHT AND CONTINUED PER MEL 52-2. 2 L 7 2 4F RT A16WE 1996112100057 19961121 00057 NM 1996 11 21 SWAA961245 1 19961110 A 5311 BELTFRAME BOEING 737 7373H4 1384600 NM BS 807 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 385SW 26600 DURING SCHEDULED C2 CHECK, FOUND BELTFRAME CRACKED AT BS 807, AT S29-28R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996112100058 19961121 00058 NM 1996 11 21 SWAA961246 1 19961113 A 3397 WIRE BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 621SW 28037 DURING BOARDING, PASSENGER KICKED FLOOR TRACK LIGHTING COVER AND ASSOCIATED WIRING LOOSE, DISABLING 10 WHITE LIGHTS. RE PLACED COVER, REPAIRED WIRES AND REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996112100059 19961121 00059 NM 1996 11 21 SWAA961247 1 19961110 A 3350 P401002 BATTERY BOEING 737 7373T5 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 692SW 23062 DURING WALKAROUND CHECK, FOUND CABIN AFT UPPER EMERGENCY FLASHLIGHT WOULD NOT CHARGE. REPLACED BATTERY PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996112100060 19961121 00060 NM 1996 11 21 SWAA961248 1 19961111 A 5315 FLOORBEAM BOEING 737 7375H4 138449D NM BS 987 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 521SW 25320 DURING SCHEDULED D-CHECK, FOUND CORROSION AROUND FASTENER HOLE BOTTOM SIDE OF UPPER CHORD OF FLOORBEAM BS 987, RBL 36, W L 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996112100061 19961121 00061 NM 1996 11 21 SWAA961249 1 19961111 A 5230 DOOR BOEING 737 7375H4 138449D NM AFT CARGO DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 521SW 25320 DURING SCHEDULED D-CHECK, FOUND AFT CARGO DOOR OUTER SKIN DENTED WITH A SHARP CREASE, 6 BY .5 BY .04 DEEP. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996112100062 19961121 00062 NM 1996 11 21 SWAA961250 1 19961111 A 3350 LIGHTS BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 505SW 24181 DURING BOARDING, PASSENGER KICKED FLOOR TRACK LIGHTING COVER AND ASSOCIATED WIRING LOOSE, DISABLING 4 WHITE LIGHTS. REP AIRED WIRES AND REPLACED COVER PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996112100063 19961121 00063 NM 1996 11 21 96UAL900807 1 19961014 A 3610 PRESS REG VLV BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT ENGINE MALFUNCTIONED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 29 644UA 25094 ABORTED TAKEOFF DUE TO RIGHT ENGINE PRESSURE REGULATING VALVE EICAS MESSAGE WITH BLEED CAUTION LIGHT. ACCOMPLISHED CHEC K OF ALL VALVES ON THE RIGHT ENGINE. ALL WIRES WERE ALSO INSPECTED AND FOUND SECURE. OPERATIONS CHECK NORMAL. THERE HA VE BEEN NO FURTHER DISCREPANCIES INDICATED. NO PARTS WERE REMOVED. 2 L 7 2 4F 4 F RT A1NM E24NE 1996112100064 19961121 00064 NE 1996 11 21 96UAL900821 2 19961018 A 7320 FUEL CONTROL HAMSTD 7733333 BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LT ENGINE OUT OF ADJUST A UALA K NONE R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 601UA 96392 21862 709610 THE LEFT ENGINE POWER FLUCTUATED DURING CLIMB BETWEEN FLIGHT LEVEL 350 TO 390. THE DISCREPANCY WAS CAUSED BY THE FUEL C ONTROL UNIT BEING OUT OF ADJUSTMENT. CORRECTIVE ACTION TAKEN WAS TO MECHANICALLY ADJUST THE DECELERATION SCHEDULE OF TH E FUEL CONTROL. OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 1996112100065 19961121 00065 NM 1996 11 21 96UAL900854 1 19961104 A 3350 BULB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 567UA 26673 EXTERIOR EMERGENCY EGRESS LIGHT AT DOOR 2L INOPERATIVE. RELAMPED EXTERIOR EMERGENCY EGRESS LIGHT AT DOOR 2L. OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996112100066 19961121 00066 1996 11 21 96UAL900855 4 19961108 A 3197 WIRE BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE CABIN SHORTED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 9022U 19060 AIRCRAFT RETURNED TO ORD DUE TO SMOKE SMELL IN AFT CABIN CEILING AND FLIGHT RECORDER POPPED CIRCUIT BREAKERS. *S/D* FO UND HIGH RESISTANCE SHORT IN WIRING FROM THE RECORDER. REPAIRED WIRE, CHECKS OK. 2 L 7 2 4F 4 F A16WE E2EA 1996112100067 19961121 00067 NM 1996 11 21 96UAL900856 1 19961108 A 2410 3051023010 CSD SEAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE ENGINE LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 311UA 23672 723232 NUMBER ONE ENGINE OIL QUANTITY DROPPED TO 1.5 GALLONS IN FLIGHT. *S/D* THE GEARBOX CONSTANT SPEED DRIVE SEAL WAS FOUND LEAKING. REPLACED DRIVE SEAL, CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1996112100068 19961121 00068 WP 1996 11 21 ABXA9600664 1 19961111 A 3230 RETRACT MECH NIHON YS11 YS11 6310406 WP NLG LACK OF LUBE A ABXA O OTHER P NO WARNING INDICATION DE DESCENT 1 GL 23 914AX 2056 NOSE GEAR HAD TO BE RECYCLED TWICE BEFORE NOSE GEAR DOWN AND LOCKED LIGHT ILLUMINATED. LUBRICATED NOSE LANDNG GEAR AND PERFORMED GEAR SWING. OPS CHECKED GOOD PER YS-11 M.M. 32-60. 2 L 7 2 4T A1PC 1996112100069 19961121 00069 WP 1996 11 21 ABXA9600666 1 19961112 A 3350 41B004AD07G3 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 908AX 47008 ON PRE-DEPARTURE CHECK, FOUND COCKPIT EMERGENCY LIGHTING INOPERATIVE. REPLACED EMERGENCY LIGHTING BATTERIES IAW DC-9 M .M. 33-10-00. 2 L 7 2 4F A6WE 1996112100070 19961121 00070 WP 1996 11 21 ABXA9600665 1 19961112 A 3231 RETRACT MECH DOUG DC8 DC861 3021952 WP RT MLG DOOR OUT OF ADJUST A ABXA O OTHER J WARNING INDICATION TO TAKEOFF 1 GL 23 848AX 46032 AFTER GEAR RETRACTION, GEAR UNSAFE LIGHT REMAINED ILLUMINATED, LANDING GEAR AND DOOR LATCHING INDICATOR INDICATED RIGHT MAIN GEAR DOOR UNLATCHED. AFTER CYCLING GEAR SEVERAL TIMES, GEAR UNSAFE LIGHT EXTINGUISHED AND NOT LATCHED LIGHT EXTING UISHED. ADJUSTED RIGHT MAIN GEAR DOOR PROXIMITY SWITCH DOOR UPLATCH POSITION INTERLOCK CABLE I/A/W DC-8 M.A.B. 32-6. G ROUND OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1996112100071 19961121 00071 NM 1996 11 21 SCNA96379 1 19961111 A 3350 1495X LIGHT BOEING 727 7272J4 1384006 NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 284SC 21438 THE AFT AIRSTAIR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. RELAMPED EMERGENCY LIGHT, OPS CHECKED GOOD. 2 L 7 3 4F RT A3WE 1996112100072 19961121 00072 NM 1996 11 21 SCNA96380 1 19961111 A 3350 1102837 LIGHT BOEING 727 7272A1 138407F NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 286SC 21601 THE AFT AIRSTAIR EMERGENCY EXIT AREA LIGHT WAS FOUND FLICKERING AND DIM. REMOVED AND REPLACED AFT AIRSTAIR LIGHT ASSEMB LY. PERFORMED OPS CHECK, NEW LIGHT OPS CHECKED GOOD. 2 L 7 3 4F A3WE 1996112100073 19961121 00073 NM 1996 11 21 SCNA96381 1 19961112 A 3350 6105771 BATTERY BOEING 727 727227 1384078 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 275AF 22092 BOTH OVERWING FLOOR PROXIMATELY EXIT IDENTIFIERS ARE INOPERATIVE. REMOVED AND REPLACED BATTERY, SYSTEM OPS CHECK GOOD. 2 L 7 3 4F A3WE 1996112100074 19961121 00074 NE 1996 11 21 CKSA96196 2 19961114 A 7200 ENGINE BOEING 727 727223 1384074 NM PWA JT8 JT8D9A 52048 NE NR 2 FLAMEOUT A CKSA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 GL 23 6812 19487 666031 KHUF - FLT 81475: NR 2 ENGINE FLAMEOUT AT CRUISE AT FLIGHT LEVEL 310, DESCENDED TO FLIGHT LEVEL 240. CHECKED RESTART P ARAMETERS WERE NORMAL. RESTARTED NR 2 ENGINE AND ALL ENGINE PARAMETERS, OIL TEMPERATURE, PRESSURE, ETC., WERE ALL NORMA L. REMOVED MAIN FUEL STRAINER, INSPECTED, FOUND NO DEBRIS. REINSTALLED, PERFORMED ENGINE RUN IAW B727 MM 71-00. NO DE FECTS NOTED. COULD NOT DUPLICATE ENGINE FLAMEOUT. ALL PARAMETERS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1996112100075 19961121 00075 NE 1996 11 21 SRAA961110 3 19961113 A 6114 DOME SEAL LKHEED 382 382E 526413U SO HAMSTD 54H 54H6091 NE NR 1 PROP LEAKING A SRAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 23 923SJ 4301 ON CLIMB-OUT FLIGHT 1203 FROM CHS, NR 1 AND NR 3 PROPELLER LOW OIL LIGHTS CAME ON. ACCOMPLISHED AIR TURN BACK TO CHS. F OUND NR 1 PROPELLER LEAKING FLUID OUT OF DOME CAP, REPLACED DOME CAP SEAL AND SERVICED PROP OIL, ALSO SERVICED 1/2 QUART OIL TO NR 3 PROP. BOTH PROPS LEAK CHECKED GOOD. 2 H 7 4 4T A1SO 6 C P906 1996112100076 19961121 00076 SO 1996 11 21 SRAA961030 1 19961013 A 5320 FITTING LKHEED 382 382G 526414U SO BS 1012 CRACKED A SRAA K NONE O OTHER IN INSP/MAINT 1 GL 23 905SJ 45318 4472 DURING C-CHECK, FOUND FITTING AT FUSELAGE STA. 1012 LHS BL 72.70 CRACKED COMPLETELY THROUGH. REMOVED CRACKED FITTING, I NSTALLED NEW T-ANGLE FITTING, FABRICATED AND INSTALLED NEW WEB ASS'Y IAW LAC SRM CHAPTER 53-40-04 PG 10. 2 H 7 4 4T A1SO 1996112100077 19961121 00077 NM 1996 11 21 AWXA9600680 1 19961114 A 3397 WIRE BOEING 737 73733A 1384673 NM CABIN DISCONNECTED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 165AW 23626 DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 2 SEAT MOUNTED EMERGENCY EXIT LIGHT OUT. SPLICED WIRES TO LIGHT, OPERATES N ORMAL AT THIS TIME. 2 L 7 2 4F RT A16WE 1996112100078 19961121 00078 WP 1996 11 21 CALA9601627 1 19961111 A 2530 OVEN DOUG DC9 DC982 3022082 WP AFT GALLEY DIRTY A CALA F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 10801 49127 THE AFT GALLEY OVEN BEGAN TO SMOKE WHILE AT CRUISE PORTION OF FLIGHT. THE AFT HALON FIRE EXTINGUISHER WAS USED IN AFT G ALLEY OVEN AND THE SMOKE CEASED. BURNED PAPER PRODUCTS WERE FOUND INSIDE OVEN. MAINTENANCE FOUND NO DAMAGE TO OVEN AND NO DEFECTS WERE FOUND. THE OVEN WAS CLEANED AND A NEW FIRE EXTINGUISHER WAS INSTALLED. 2 L 7 2 4F A6WE 1996112100079 19961121 00079 NM 1996 11 21 CALA9601628 1 19961114 A 3234 A42006028305 SOLENOID BOEING 737 737217 1384464 NM LANDING GEAR INOPERATIVE A CALA A D UNSCHED LANDING RETURN TO BLOCK O OTHER TO TAKEOFF 1 SW 09 16232 19886 THE GEAR LATCH WOULD NOT RELEASE AFTER TAKEOFF. THE GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. CIRCUIT BREAKERS WE RE PULLED AND RESET IAW QRH PROCEDURES, BUT WITH NO CHANGE. THE AIRCRAFT WAS RETURNED TO GSO WHERE IT LANDED WITHOUT IN CIDENT. MAINTENANCE FOUND THE LANDING GEAR CONTROL LEVER LOCK SOLENOID AT FAULT. THE SOLENOID WAS REMOVED AND REPLACED . 2 L 7 2 4F A16WE 1996112100080 19961121 00080 NM 1996 11 21 CALA9601629 1 19961011 A 5330 SKIN BOEING 727 727232 1384082 NM BS 1223 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND A 3 INCH CRACK IN FUSELAGE SKIN AT STA 1223. THE CRACKED AREA WAS CUT OUT, A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. 2 L 7 3 4F A3WE 1996112100081 19961121 00081 NM 1996 11 21 CALA9601630 1 19961011 A 5330 SKIN BOEING 727 727232 1384082 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND A 1 INCH CRACK AND DENTS IN LT FUSELAGE PANEL JUST BELOW POTABLE WATER SERVICE DOOR. THE DAMAGED AREA WAS CUT OUT, A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1996112100082 19961121 00082 NM 1996 11 21 CALA9601631 1 19961008 A 5754 RIB BOEING 727 727232 1384082 NM NR 5 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND A 1.5 INCH CRACK IN NR 5 SLAT RIB WHERE ACTUATOR ATTACHES. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-50-3, FIGURE 9. 2 L 7 3 4F A3WE 1996112100083 19961121 00083 NM 1996 11 21 CALA9601632 1 19961008 A 5754 RIB BOEING 727 727232 1384082 NM NR 6 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND A .75 INCH CRACK IN NR 6 SLAT RIB WHERE ACTUATOR ATTACHES. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-50-3. 2 L 7 3 4F A3WE 1996112100084 19961121 00084 NM 1996 11 21 CALA9601633 1 19961008 A 5754 RIB BOEING 727 727232 1384082 NM NR 7 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND A .5 INCH CRACK IN NR 7 SLAT OUTBOARD RIB WHERE ACTUATOR ATTACHES. A DOUBLER WAS FABRICATED AND INSTAL LED IAW SRM 57-50-3. 2 L 7 3 4F A3WE 1996112100085 19961121 00085 NM 1996 11 21 CALA9601634 1 19961012 A 5754 RIB BOEING 727 727232 1384082 NM NR 8 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND A 1.25 INCH CRACK IN NR 8 SLAT RIB LOCATED OUTBOARD OF ANTI-ICE DUCT. A DOUBLER WAS FABRICATED AND INS TALLED IAW SRM 57-50-3, FIGURE 9. 2 L 7 3 4F A3WE 1996112100086 19961121 00086 NM 1996 11 21 CALA9601635 1 19961012 A 5754 RIB BOEING 727 727232 1384082 NM NR 2 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND A 1.125 INCH CRACK IN NR 2 SLAT INBOARD TRACK OUTBOARD ATTACH RIB WITH CORROSION AT FORWARD ATTACH HOLE . THE CORROSION WAS REMOVED FROM HOLE, DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 57-30-2. 2 L 7 3 4F A3WE 1996112100087 19961121 00087 NM 1996 11 21 CALA9601636 1 19961022 A 5320 SUPPORT PANEL BOEING 727 727232 1384082 NM BS 337 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND FORWARD LAV FLOOR SUPPORT PANEL CORRODED AT STA 337, RBL 43. THE CORRODED ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-4. 2 L 7 3 4F A3WE 1996112100088 19961121 00088 NM 1996 11 21 CALA9601637 1 19961012 A 5754 RIB BOEING 727 727232 1384082 NM NR 2 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND A 1 INCH CRACK NR 2 SLAT OUTBOARD TRACK OUTBOARD RIB WITH CORROSION AT FORWARD ATTACH BOLT HOLE. CORRO SION WAS REMOVED FROM HOLE, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-30-2. 2 L 7 3 4F A3WE 1996112100089 19961121 00089 NM 1996 11 21 CALA9601638 1 19961012 A 5754 RIB BOEING 727 727232 1384082 NM NR 2 LE SLAT GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND A GOUGE IN INBOARD ATTACH RIB AT FORWARD ATTACH BOLT OF NR 2 SLAT INBOARD TRACK. THE RIB WAS REMOVED A ND REPLACED IAW SRM 51-10-1. 2 L 7 3 4F A3WE 1996112100090 19961121 00090 NM 1996 11 21 CALA9601639 1 19961010 A 5321 FLOOR BOEING 727 727232 1384082 NM AFT LAV CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND RT AFT LAV FLOOR AREA CORRODED IN SEVERAL PLACES. THE CORRODED AREAS WERE CUT OUT, FILLERS AND DOUBLER S WERE FABRICATED AND INSTALLED IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1996112100091 19961121 00091 NM 1996 11 21 CALA9601640 1 19961011 A 5330 SKIN BOEING 727 727232 1384082 NM BS 700 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND CORROSION ON SHEAR TIE AND SKIN AT STA 700 BETWEEN STRINGER 28L AND 28R. THE CORRODED AREA WAS CUT OUT , REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-10-4. 2 L 7 3 4F A3WE 1996112100092 19961121 00092 NM 1996 11 21 CALA9601641 1 19961012 A 5754 RIB BOEING 727 727232 1384082 NM NR 4 LE SLAT GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND THE NR 4 SLAT OUTBOARD TRACK INBOARD ATTACH RIB WITH GOUGES AROUND FORWARD TRACK BOLT HOLE. THE RIB FI TTING WAS REMOVED AND REPLACED IAW SRM 57-30-2. 2 L 7 3 4F A3WE 1996112100093 19961121 00093 NM 1996 11 21 CALA9601642 1 19961011 A 5320 SPLICE BOEING 727 727232 1384082 NM BS 660 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND CORROSION ON STRINGER 28L SPLICE AT STA 660. THE CORRODED SPLICE WAS REMOVED AND A REPLACEMENT WAS FAB RICATED AND INSTALLED IAW SRM 53-10-3. 2 L 7 3 4F A3WE 1996112100094 19961121 00094 WP 1996 11 21 9624159957 1 19961021 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 531 SEVERED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 915RW 47139 DURING H-CHECK, FOUND LONGERON 30 CRACKED COMPLETELY THROUGH AT FS 531. REPAIRED LONGERON (P/N 5920319-504) PER EA 99-1 11743. 2 L 7 2 4F A6WE 1996112100095 19961121 00095 WP 1996 11 21 9624169951 1 19961028 A 5753 SKIN DOUG DC9 DC932 3022066 WP LT TE FLAP DELAMINATED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9347 45827 DURING H-CHECK, FOUND DELAMINATION IN THE LEFT WING FLAP TRAILING EDGE UPPER SKIN AT XFLS 187-235. REPAIRED SKIN (P/N 9 957578-503) PER EA 99-120171. 2 L 7 2 4F A6WE 1996112100096 19961121 00096 NM 1996 11 21 9624176631 1 19961029 A 5315 FLOORBEAM BOEING 747 747251B 1384892 NM BS 1740 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 631US 23111 DURING P-CHECK, FOUND CORROSION ON THE BS 1740 FLOORBEAM UPPER CHORD AT RBL 58. REPAIRED BEAM (P/N 65B26535-7) PER EA 6 6-106423. 2 L 7 4 4F A20WE 1996112100097 19961121 00097 WP 1996 11 21 9624189951 1 19961029 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 786 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9347 45827 DURING H-CHECK, FOUND CORROSION ON THE FS 756 BULKHEAD FRAME T-CHORD AT LONGERON 29L. REPAIRED FRAME (P/N 9958212-3) PE R EA 99-109572. 2 L 7 2 4F A6WE 1996112100098 19961121 00098 WP 1996 11 21 9624199974 1 19961031 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 83 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9338 47347 DURING H-CHECK, FOUND 3 CRACKS .5, .625 AND 1.25 INCH IN THE FS 83 FRAME AT THE LEFT AND RIGHT SIDES. REPAIRED FRAME (P /N 9911505-7) PER EA 99-111786. 2 L 7 2 4F A6WE 1996112100099 19961121 00099 WP 1996 11 21 9624209951 1 19961031 A 5400 FITTING DOUG DC9 DC932 3022066 WP NR 2 PYLON CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9347 45827 DURING H-CHECK, FOUND CORROSION ON THE NR 2 PYLON LOWER FORWARD SURFACE BEAVER TAIL FITTING AND LOWER SPAR CHORD. REPLA CED FITTING AND REMOVED SPAR CORROSION PER EA 99-120169. 2 L 7 2 4F A6WE 1996112100100 19961121 00100 WP 1996 11 21 9624219753 1 19961103 A 5320 PRESS PANEL DOUG DC9 DC941 302207N WP BS 83 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 753NW 47117 DURING H-CHECK, FOUND CRACKS IN THE NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL AT FS 83 LEFT AND RIGHT SIDES . REPAIRED PANEL (P/N 9910073-313) PER EA 97-111775. 2 L 7 2 4F A6WE 1996112100101 19961121 00101 WP 1996 11 21 9624229951 1 19961105 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 579 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9347 45827 DURING H-CHECK, FOUND CORROSION AT LONGERONS 29L AND 29R AT FS 579. REPAIRED LONGERONS (P/N 3920596-1) PER EA 99-120176 , 99-120174. 2 L 7 2 4F A6WE 1996112100102 19961121 00102 WP 1996 11 21 9624239951 1 19961105 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 510 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9347 45827 DURING H-CHECK, FOUND CORROSION ON THE FUSELGE SKIN AND FINGER DOUBLER AT FS 510 FROM LONGERON 29L TO 29R. REPAIRED SKI N (P/N 5911412-191, -55). 2 L 7 2 4F A6WE 1996112100103 19961121 00103 WP 1996 11 21 9624249951 1 19961106 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 218 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9347 45827 DURING H-CHECK, FOUND CORROSION ON THE FS 218 FRAME LOWER CHORD AT LONGERON 30. REPAIRED FRAME (P/N S 2777930-5) PER EA 99-109580. 2 L 7 2 4F A6WE 1996112100104 19961121 00104 NM 1996 11 21 9624255518 1 19961107 A 5315 FLOORBEAM BOEING 757 757251 1384970 NM BS 1661 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 518US 23206 DURING P-CHECK, FOUND CORROSION IN THE BS 1661 FLOORBEAM UPPER CHORD FROM LBL 60, BL 0. REPAIRED CHORD (P/N 146N5090) P ER EA 55-120032. 2 L 7 2 4F RT A2NM 1996112100105 19961121 00105 WP 1996 11 21 9624269618 1 19961111 A 5320 RETAINER DOUG DC9 DC932 3022066 WP RT WINDSHIELD CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 618NW 47433 DURING M-CHECK, FOUND CORROSION IN ONE OF THE FIRST OFFICER'S WINDSHIELD RETAINERS. REPLACED RETAINER (P/N 9957862-506) PER SRM 51-10-03. 2 L 7 2 4F A6WE 1996112100106 19961121 00106 WP 1996 11 21 9624279614 1 19961112 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 832 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 614NW 47128 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE FLOOR SUPPORT FITTING AT FS 832, LONGERON 28R. REP LACED FITTING PER SRM 51-10-3, 51-30-2, 51-30-5. 2 L 7 2 4F A6WE 1996112100107 19961121 00107 WP 1996 11 21 9624289986 1 19961112 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 617 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 986US 47480 DURING H-CHECK, FOUND A CRACK IN THE LONGERON 10R END FITTING AT FS 617. REPLACED FITTING (PSE 53.09.003) PER SRM 51-10 -2. 2 L 7 2 4F A6WE 1996112100108 19961121 00108 WP 1996 11 21 9624299986 1 19961112 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 579 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 986US 47480 DURING H-CHECK, FOUND A CRACK IN THE FS 579 FRAME FITTING BETWEEN THE UPPER FORWARD LUGS. REPAIRED FRAME (PSE 53.09.015 ) PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996112100109 19961121 00109 WP 1996 11 21 9624309986 1 19961112 A 5320 FITTING DOUG DC9 DC932 3022066 WP PAX DOORWAY CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 986US 47480 DURING H-CHECK, FOUND A CRACK IN THE AFT ENTRY DOOR LOWER RIGHT STOP FITTING. REPLACED FITTING PER SRM 51-30-2. 2 L 7 2 4F A6WE 1996112100110 19961121 00110 WP 1996 11 21 9624319986 1 19961112 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 996 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 986US 47480 DURING H-CHECK, FOUND A CRACKED FLOOR STRUCTURE FITTING AT FS 996, LBL 25. REPLACED FITTING (P/N 94FS481223-103) PER SR M 51-30-0. 2 L 7 2 4F A6WE 1996112100111 19961121 00111 EU 1996 11 21 9624323226 1 19961112 A 5230 CASTING AIRBUS 320 A320211 3930320 EU CARGO DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 326US 282 DURING LINE CHECK, FOUND THAT THE FORWARD CARGO DOOR HANDLE ATTACH MECHANISM CASTING WAS BROKEN. REPLACED CASTING. 2 L 7 2 4F RT A28NM 1996112100112 19961121 00112 WP 1996 11 21 9624339953 1 19961112 A 5400 STRAP DOUG DC9 DC931 3022065 WP NR 2 PYLON CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 918RW 47158 DURING LINE CHECK, FOUND A BROKEN NR 2 PYLON UPPER AFT ENGINE MOUNT STRAP. ALSO, FOUND CRACKS IN THE PYLON WEB LOWER CH ANNEL 10 OUTBOARD FROM THE FUSELAGE AT THE LOWER ENGINE MOUNT STRAP AND IN THE UPPER INBOARD PYLON TO FUSELAGE ATTACH AN GLE 15 FORWARD OF THE AFT ENGINE MOIUNT SPAR. REPLACED BOTH THE UPPER AND LOWER AFT ENGINE MOUNT STRAPS PER EA 99-11180 4, REPAIRED THE WEB PER SRM 54-01, FIG 2 AND REPAIRED THE ATTACH ANGLE PER SRM 54-04, FIG 10. 2 L 7 2 4F A6WE 1996112100113 19961121 00113 WP 1996 11 21 9624379986 1 19961113 A 5741 WING ATTACH FTG DOUG DC9 DC932 3022066 WP BS 600 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 986US 47480 DURING H-CHECK, FOUND CORROSION ON THE CENTER WING FITTING AT FS 600 AND LONGERON 19R. REPLACED FITTING PER SRM 51-10, 51-30-1. 2 L 7 2 4F A6WE 1996112100114 19961121 00114 WP 1996 11 21 9624389614 1 19961113 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 851 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 614NW 47128 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE RIGHT CUSP MEMBRANE AND FITTING AT FS 851, LONGERON 18R. REPAIRED CUSP AND REPLACED THE FITTING PER SRM 51-10-03, 51-30-02. 2 L 7 2 4F A6WE 1996112100115 19961121 00115 NM 1996 11 21 9624396622 1 19961113 A 5340 FITTING BOEING 747 747251B 1384892 NM BS 1476 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 622US 21704 DURING P-CHECK, FOUND CORROSION ON THE U-CHANNEL SUPPORT FITTING IN THE LEFT BODY MAIN LANDING GEAR WHEEL WELL FS 1476 O N THE KEEL BEAM TOP PLATE 8 OUTBOARD OF THE INBOARD WALL. REPLACED FITTING PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996112100116 19961121 00116 WP 1996 11 21 9624429870 1 19961111 A 5220 EXIT DOOR DOUG DC9 DC951 3022051 WP CABIN NOT CLOSED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 779NC 48101 DURING CLIMB, FOUND INADEQUATE PRESSURIZATION CONTROL. FOUND THE AFT RIGHT OVERWING EMERGENCY EXIT NOT FULLY CLOSED. R ETURNED TO DTW WITHOUT FURTHER INCIDENT. REINSTALLED AFT RIGHT OVERWING EMERGENCY EXIT, PRESSURIZATION CHECK OK. 2 L 7 2 4F A6WE 1996112100117 19961121 00117 WP 1996 11 21 9624439612 1 19961111 A 2810 FUEL CAP DOUG DC9 DC932 3022066 WP RT WING BROKEN A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK K FLUID LOSS TO TAKEOFF 1 GL 01 612NW 47436 ON TAKEOFF, TOWER NOTICED FUEL VENTING FROM RIGHT WING. TAKEOFF WAS ABORTED AT 90 KTS. MAINTENANCE FOUND OVERWING FUEL CAP BROKEN AND POPPED OFF. INSPECTED CAP FLANGE AND REPLACED CAP. AIRCRAFT REFUELED AND APPROVED SERVICE. 2 L 7 2 4F A6WE 1996112100118 19961121 00118 WP 1996 11 21 9624449973 1 19961108 A 7711 LG80A2 EPR TRANS DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9 52048 NE RT ENGINE INOPERATIVE A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 9337 12251 1183 47346 666311 DURING TAKEOFF ROLL AT 20 KNOTS, THE RIGHT ENGINE EPR INDICATION BECAME INOPERATIVE. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE REPLACED RIGHT ENGINE EPR TRANSMITTER, OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F A6WE E2EA 1996112100119 19961121 00119 NE 1996 11 21 9624451146 2 19961114 A 7230 COMPRESSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20J 52054 NE NR 1 ENGINE STALLED A NWAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DE DESCENT 1 GL 01 146US 46755 86148 DURING POWER REDUCTION AT FL210, THE NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL. AS EGT CLIMBED TO 750 DEGREES, THE ENG INE WAS SHUT DOWN AND RESTARTED. CREW FOLLOWED COCKPIT OPERATING PROCEDURE AND CONTINUED FLIGHT TO PHL WITHOUT FURTHER INCIDENT. VISUAL AND TYPE-A INSPECTION REVEALED NO DISCREPANCIES. BORESCOPE INSPECTION WILL BE DONE WITHIN FOUR CYCLES . 2 L 7 3 4F 4 F A22WE E20EA 1996112100120 19961121 00120 EU 1996 11 21 9624463248 1 19961114 A 3260 INDICATION AIRBUS 320 A320212 EU LANDING GEAR MALFUNCTIONED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 348NW 410 DURING CLIMBOUT AFTER LANDING GEAR RETRACTION, THE LANDING GEAR DID NOT INDICATE UP LOCKED. CYCLED LANDING GEAR HANDLE AND ALL INDICATIONS NORMAL. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED NOSE LA NDING SENSORS, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996112100121 19961121 00121 WP 1996 11 21 9624479965 1 19961113 A 2120 AIR PRESS REG DOUG DC9 DC931 3022065 WP COCKPIT MALFUNCTIONED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 911RW 47149 ON CLIMBOUT, NOTICED A PLASTIC SMELL IN THE COCKPIT. SUPPLY PRESSURE INDICATORS SHOWED LEFT .31, RIGHT .38 PSI. RETURN ED TO NORMAL PRESSURE AND SMELL DISSIPATED. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED A IR PRESSURE REGULATOR. 2 L 7 2 4F A6WE 1996112100122 19961121 00122 NM 1996 11 21 9624482298 1 19961114 A 2131 10251831 CONTROLLER BOEING 727 727251 138408H NM COCKPIT FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 01 298US 45863 19915 22152 DURING CRUISE FLIGHT, AUTOMATIC PRESSURIZATION WOULD NOT MAINTAIN CABIN AT FLIGHT LEVEL. AIRCRAFT RETURNED TO DTW AND L ANDED WITHOUT INCIDENT. REPLACED CABIN PRESSURIZATION CONTROLLER AND PERFORMED AUTOMATIC AND MANUAL PRESSURIZATION TEST , OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996112100123 19961121 00123 WP 1996 11 21 9624499311 1 19961114 A 2150 DUCT DOUG DC9 DC982 3022082 WP ACM LOOSE A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 314RC 49110 ON DEPARTING, UNABLE TO PRESSURIZE CABIN IN AUTO OR MANUAL. FLIGHT RETURNED TO GEG AND LANDED WITHOUT INCIDENT. FOUND DUCT HOSE OFF BETWEEN AIR CYCLE MACHINE AND HEAT EXCHANGER. REINSTALLED DUCT, LEAK AND OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996112100124 19961121 00124 SW 1996 11 21 QXEA9600463 1 19961114 A 2150 ACM SWRNGN SA227 SA227AC 8780603 SW ACM COMPT FAILED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 NM 09 26959 AC662 SMOKE IN CABIN OF A/C AFTER TOUCHDOWN. INSPECTED AND FOUND AIR CYCLE MACHINE FROZEN UP. DEFFERED PER MEL 21-9. 2 L 7 2 4T RT A8SW 1996112100125 19961121 00125 1996 11 21 DHL96742006 4 19961109 A 2310 HF TRANSMITTER BOEING 727 727225 1384077 NM NR 1 MALFUNCTIONED A DHLA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 742DH 21290 HF NR 1 TRANSMITTER INOP, WILL NOT CHANNELIZE. OPEN DEFERRAL 23-3-2 DMI 182 ASSIGNED PER MEL 23-3-2 PLACARD INSTALLED. REMOVED AND REPLACED NR 1 HF TRANSCEIVER AND ANTENNA COUPLER PER MM 23-1-0. 2 L 7 3 4F A3WE 1996112100126 19961121 00126 NM 1996 11 21 P5CA9600949 1 19961114 A 2761 3320550 ACTUATOR BOEING 747 747132 1384882 NM NR 1 SPOILER LEAKING A P5CA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 WP 23 856FT 19897 NR 3 HYDRAULIC SYSTEM FLUID LOSS. AIRCRAFT RETURNED TO MIAMI. ON GROUND FOUND LEAKING NR 1 SPOILER ACTUATOR LEAKING, C RACKED ACTUATOR END CAP. REPLACED PER BOEING MAINTENANCE MANUAL. 2 L 7 4 4F A20WE 1996112100127 19961121 00127 NM 1996 11 21 P5CA9600950 1 19961109 A 5314 KEEL BEAM BOEING 747 747122 1384872 NM FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 LEVEL 1 CORROSION KEEL BEAM PANELS 191GG, 191HH, 191JJ AND 191KK. CLEANED CORROSION ON PANELS 191HH AND 191KK SRM 51-10 -01 AND REPLACED 191GG AND 191JJ FOR CONVENIENCE PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1996112100128 19961121 00128 NM 1996 11 21 P5CA9600951 1 19961012 A 7110 65B915212 NOSE COWL BOEING 747 747122 1384872 NM NR 2 ENGINE DEFORMED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 NR 2 ENGINE NOSE COWL OUTER SKIN FROM 1 TO 3 O'CLOCK POSITION SKIN BULGING FROM SEALANT AND MISSING SCREW. REPLACED EXT ERIOR SKIN IAW BOEING SRM 51-30-02. 2 L 7 4 4F A20WE 1996112100129 19961121 00129 NM 1996 11 21 P5CA9600952 1 19961113 A 7830 SLEEVE BOEING 747 747122 1384872 NM NR 1 ENGINE DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 DEEP LONG DENT NR 1 ENGINE FAN REVERSER SLEEVE AT 7 O'CLOCK POSITION. REPAIRED PER POLAR AIR CARGO MA 7830-01:01 AND BO EING SRM 51-40-06 PARA 3 AND 51-24-11. 2 L 7 4 4F A20WE 1996112100130 19961121 00130 NM 1996 11 21 P5CA9600953 1 19961106 A 5344 65B079223 FITTING BOEING 747 747122 1384872 NM L1 DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 CRACKED LOWER L-1 DOOR LOWER TORQUE TUBE PIVOT HINGE BEARING FITTING. REPLACED FITTING PER BOEING SRM 51-30-03. 2 L 7 4 4F A20WE 1996112100131 19961121 00131 NM 1996 11 21 P5CA9600954 1 19961113 A 5320 BRACKET BOEING 747 747122 1384872 NM KEEL BEAM CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 LEVEL 2 CORROSION KEEL BEAM ACCESS PANELS 191HH AND 191KK 6 INNER ATTACHMENTS BRACKETS. FABRICATED AND REPLACED BRACKET S PER BOEING SRM 51-10-01. 2 L 7 4 4F A20WE 1996112100132 19961121 00132 WP 1996 11 21 ARWA9611004 1 19961115 A 2110 5614845517 COMPRESSOR DOUG DC8 DC862 3021970 WP NR 4 MALFUNCTIONED A ARWA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 19 802BN 45909 AIR TURNBACK, NR 4 TURBO COMPRESSOR OVERHEAT LIGHT ON. UNABLE TO HOLD CABIN ALTITUDE. RETURNED TO MIAMI WITHOUT INCIDEN T. REMOVED AND REPLACED NR 4 T/C, SYS OPS AND FUNCTIONAL TEST OK, IAW MM 21-2-1. 2 L 7 4 4F 4A25 1996112100133 19961121 00133 NM 1996 11 21 CKSA96197 1 19961113 A 3260 MC7711 SWITCH BOEING 727 727223 1384074 NM NLG WORN A CKSA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 6812 19487 LANDING GEAR DOOR WARNING LIGHT STAYED ILLUMINATED AFTER GEAR RETRACTION, WITH NOSE GEAR DOOR LIGHT ON FLIGHT ENGINEER'S PANEL ILLUMINATED. RECYCLED GEAR IAW FLIGHT OPS MANUAL AND LIGHTS REMAINED ILLUMINATED. REMOVED AND REPLACED 2 NOSE G EAR DOOR WARNING SWITCHES AND ADJUSTED, OPS CHECK GOOD. REFERENCE MM 32-62-11 PAGE 402. 2 L 7 3 4F A3WE 1996112100134 19961121 00134 SO 1996 11 21 SRAA961034 1 19961013 A 5330 SKIN LKHEED 382 382G 526414U SO BS 507 CRACKED A SRAA K NONE O OTHER IN INSP/MAINT 1 GL 23 905SJ 45318 4472 DURING C-CK, FOUND UPPER SECTION OF LT MAIN LANDING GEAR WHEEL WELL HAS A CRACK IN INNER SKIN NEAR ATTACH ANGLE ON O/B S IDE AT WL 200 STA 507. CRACK MEASURED 2 INCH LENGTH. FOUND CRACK OUT OF LIMITS, CUT OUT AREA FABRICATED AND INSTALLED FILLER TO EXISTING DOUBLER IAW LAC SRM 51-70-01, 53-60,02 AND 51-140-02. 2 H 7 4 4T A1SO 1996112100135 19961121 00135 NM 1996 11 21 RAAA96B1027 1 19961115 A 2910 BACH30AT08K360 HOSE BOEING 727 72722C 138400F NM LT MLG ACT FAILED A RAAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 AL 03 831RV 19093 ON GEAR RETRACTION AFTER DEPARTURE A-SYSTEM HYD QUANTITY AND PRESSURE WENT TO ZERO. RETURNED TO AKN. REPLACED FAILED L T MLG ACTUATING CYLINDER DOWN SUPPLY HOSE. 2 L 7 3 4F A3WE 1996112100136 19961121 00136 NE 1996 11 21 CALA9601643 2 19961114 A 7314 37190134 FUEL PUMP BOEING 737 7372C0 1384488 NM PWA JT8 JT8D9 52048 NE NR 1 ENGINE FAILED A A CALA A UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 SW 09 14241 19997 9794 20070 674250 THE NR 1 ENGINE FLAMED OUT WHILE CRUISING AT FL 250 EN ROUTE. THE AIRCRAFT WAS DIVERTED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE FUEL PUMP AT FAULT. THE FUEL PUMP WAS REMOVED AND REPLACED, LEAK CHECK WAS GOOD AND ALL PARAMETERS WERE NORMAL DURING ENGINE RUN. 2 L 7 2 4F 4 F A16WE E2EA 1996112100137 19961121 00137 NM 1996 11 21 CALA9601644 1 19961115 A 2430 654980821 RELAY MODULE BOEING 737 737130 1384435 NM COCKPIT BURNT A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 09 24213 8161 8161 19030 SMOKE WITH FUMES WAS OBSERVED COMING FROM ELECTRICAL PANEL BY THE JUMP SEAT ON AIRCRAFT RIGHT ON APPROACH. THE M181 MOD ULE WAS HOT TO TOUCH, THE MODULE WAS REMOVED AND SMELLED BURNT. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENAN CE REMOVED AND REPLACED THE M181 RELAY MODULE. THE MODULE TESTED GOOD AND NO OTHER DISCREPANCIES WERE FOUND. 2 L 7 2 4F A16WE 1996112100138 19961121 00138 WP 1996 11 21 CALA9601645 1 19961116 A 3222 5910448565 SHOCK STRUT DOUG DC9 DC982 3022082 WP NLG LOW PRESSURE A CALA O OTHER J WARNING INDICATION CL CLIMB 1 SW 09 15841 49581 THE LANDING GEAR WOULD NOT RETRACT TO UP AND LOCKED POSITION AFTER TAKEOFF. THE GEAR WAS CYCLED AND RETRACTED TO UP AND LOCKED POSITION AFTER TWO ATTEMPTS. THE AIRCRAFT LANDED NORMALLY AT SEA. MAINTENANCE FOUND THE NOSE STRUT PRESSURE LO W. THE NOSE STRUT WAS SERVICED PER CHART ON NOSE WHEEL WELL AND A DIP WAS ISSUED FOR FULL SERVICE AT NEXT RON. FULL NO SE STRUT SERVICE WAS COMPLIED WITH AT EWR THE FOLLOWING DAY AND THE DIP WAS CLOSED. 2 L 7 2 4F A6WE 1996112100139 19961121 00139 NM 1996 11 21 CALA9601646 1 19961116 A 3350 1102833 LIGHT BOEING 727 727224 1384076 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 79746 22449 THE EMERGENCY EXIT LIGHT AT ROW 8 WAS FOUND INOPERATIVE. THE EMERGENCY EXIT LIGHT ASSEMBLY WAS REMOVED AND REPLACED. 2 L 7 3 4F A3WE 1996112100140 19961121 00140 WP 1996 11 21 CALA9601647 1 19961117 A 2761 1040T1005 ACTUATOR DOUG DC9 DC982 3022082 WP PEDESTAL SHORTED A CALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 83873 21178 115 49121 SMOKE WITH AN ELECTRICAL ODOR BEGAN COMING FROM CENTER PEDESTAL WHILE INFLIGHT. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE SPOILER AUTOMATIC ACTUATOR BURNT AND SHORTING. THE SPOILER AUTOMATIC ACTUATOR WAS REMOVED AND REPLACED AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F A6WE 1996112100141 19961121 00141 WP 1996 11 21 CALA9601648 1 19961117 A 3240 836SD620 BRAKE LIMITER DOUG DC9 DC982 3022082 WP LEFT LEAKING A A CALA A D UNSCHED LANDING RETURN TO BLOCK J K WARNING INDICATION FLUID LOSS CL CLIMB 1 SW 09 69803 22763 9471 49229 THE LT HYDRAULIC SYSTEM QUANTITY DEPLETED DURING CLIMBOUT. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INC IDENT. MAINTENANCE FOUND THE LT HYDRAULIC SYSTEM BRAKE FLUID QUANTITY LIMITER FAILED. THE BRAKE FLUID QUANTITY LIMITER WAS REMOVED AND REPLACED. THE LEFT HYDRAULIC SYSTEM WAS SERVICED TO FULL AND LEAK CHECK WAS GOOD. THE NR 1 AND NR 2 B RAKES WERE BLED, SYSTEM PRESSURE CHECKED NORMAL. 2 L 7 2 4F A6WE 1996112100142 19961121 00142 SO 1996 11 21 COMA9610331 1 19961114 A 7931 APT79100080D OIL PRESS TRANS EMB 120 EMB120RT SO RT ENGINE MALFUNCTIONED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 243CA 120212 ON POWER UP FOR TAKE OFF RIGHT ENGINE OIL PRESSURE WENT UP TO THE RED, 70 PSI. ABORTED TAKEOFF. REPLACED OIL PRESSURE TRANSDUCER, OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 1996112100143 19961121 00143 SO 1996 11 21 COMA9610332 1 19961115 A 5270 WARNING LIGHT EMB 120 EMB120RT SO CARGO DOOR ILLUMINATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 462CA 120264 AFTER TAKEOFF CARGO DOOR WARNING LIGHT ILLUMINATED. TRANSFERRED TO DEFERRED LIST CAT, MEL 52-70-1. 2 L 7 2 4T RT A31SO 1996112100144 19961121 00144 EA 1996 11 21 COMA9660207 1 19961114 A 5270 864202 SENSOR CNDAIR CL600 CL6002B19 EA PAX DOOR FAILED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 960CA 7117 PAX DOOR LATCH CAUTION MESSAGE CAME ON IN FLIGHT. REPLACED PROX SENSOR ON NR 1 LATCH PIN, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 1996112100145 19961121 00145 EA 1996 11 21 COMA9660208 1 19961114 A 3030 785806 ADS CONTROLLER CNDAIR CL600 CL6002B19 EA COCKPIT INOPERATIVE A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 952CA 7092 AFTER TAKEOFF, PITOT BASE HEAT YELLOW MESSAGE CAME ON. RETURNED TO CVG BECAUSE OF ICE CONDITIONS. REPLACED AIR DATA SE NSOR CONTROLLER, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 1996112100146 19961121 00146 1996 11 21 COMA9660209 4 19961115 A 2230 1600980005 ATR CABLE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE ENGINE BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 912CA 6791 7011 807123 AFTER REMOVAL OF ENGINE FOR SCHEDULED ENGINE CHANGE FOUND AUTO THROTTLE RETARD CABLE BROKEN IN TWO, WHERE CABLE CONNECTS TO ATR BELLCRANK. CABLE WAS BROKEN BELOW RIVETED END. 2 L 7 2 4F 4 F RT A21EA E15NE 1996112100147 19961121 00147 1996 11 21 TC8A96067 4 19961114 A 3454 CONNECTOR DOUG DC8 DC862F 3021972 WP NR 2 RMI LOOSE A TC8A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 183SK 45904 NR 2 COMPASS OFF FLAG APPEARED ON TAXI OUT. CLEANED AND RESECURED CANNON PLUG AT CAPTAINS RADIO MAGNETIC DIRECTION INDI CATOR, SYSTEM OPS CHECKS GOOD. 2 L 7 4 4F 4A25 1996112100148 19961121 00148 WP 1996 11 21 SRAA961111 1 19961113 A 5330 SKIN DOUG DC8 DC871F 302199D WP LT WING PUNCTURED A SRAA O OTHER C F.O.D. TO TAKEOFF 1 GL 23 872SJ 46040 ON TAKEOFF, AIRCRAFT HAD BIRD STRIKE. AFTER LANDING AT EBBR, INSPECTED AIRCRAFT AND FOUND BIRD STRIKE CAUSED DAMAGE TO LEFT WING L/E BETWEEN NR 2 PYLON AND FUSELAGE. REPLACED LT WING LANDING LIGHT AND REPAIRED L/E IAW SRM 51 CH 57-2-1. 2 L 7 4 4F RT 4A25 1996112100149 19961121 00149 SO 1996 11 21 SRAA961035 1 19961013 A 5311 FRAME LKHEED 382 382G 526414U SO BS 667 CRACKED A SRAA K NONE O OTHER IN INSP/MAINT 1 GL 23 905SJ 45318 4472 DURING C-CHECK, FOUND RIGHT WHEEL WELL HAS A CRACK IN FRAME STA 667, TOP OF CORNER MEASURED 3 INCHES. STOP DRILLED CRAC K, FABRICATED AND INSTALLED L-ANGLE. REPAIRED IAW LAC SRM 51-140-20 AND 51-60-12A, 51-80-08, AND 51-70-01. 2 H 7 4 4T A1SO 1996112100150 19961121 00150 EU 1996 11 21 CA960422011 1 19960413 A 3240 251130 CONTROL CABLE BAG JETSTM JETSTM4112 EU PARKING BRAKE BROKEN W O OTHER O OTHER NR NOT REPORTED 1 CA 2406 (CAN)CABLE BROKEN NEAR THE FORK END FITTING. 1 L 7 2 4T RT A196 1996112100151 19961121 00151 NE 1996 11 21 CA960423101 2 19960405 A 8530 15373CAI PISTON PWA DHAV DHC3 DHC3 2800202 EA PWA R1340 R134059 52016 NE #6 CYLINDER POUNDED W A UNSCHED LANDING E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CL CLIMB 1 CA 481 P326010 (CAN)POWER LOSS IN THE CLIMB FOLLOWED BY IMMEDIATE LANDING. #6 CYLINDER FAILED DUE TO INGESTION OF METAL DEBRIS WHICH HA D REMAINED IN THE INDUCTION SYSTEM AFTER THE FAILURE OF #2 CYLINDER EXHAUST VALVE ON THE PREVIOUS DAY. 1 H 7 1 3R 3 R A815 5E2 1996112100152 19961121 00152 NE 1996 11 21 CA960423102 2 19960404 A 8530 71167 VALVE PWA DHAV DHC3 DHC3 2800202 EA PWA R1340 R134059 52016 NE NR 2 CYL EXH FAILED W A A UNSCHED LANDING E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CL CLIMB 1 CA 439 P326010 (CAN)ON FIRST POWER REDUCTION AFTER AIRBORNE ON FLOATS, ENGINE LOST POWER. AIRCRAFT LANDED AND WATER TAXIED BACK TO DOCK . #2 CYLINDER EXHAUST VALVE FAILED. HALF OF VALVE FACE WAS MISSING. TOP OF PISTON PEE NED BY VALVE PIECES BOUNCING AROUN D IN CYLINDER. 1 H 7 1 3R 3 R A815 5E2 1996112100153 19961121 00153 NE 1996 11 21 CA960423103 2 19960405 A 8530 77168 CYLINDER PWA 183092 DOUG DC3 DC3C 3021457 WP PWA R1830 R183092 52020 NE #9 DETACHED W E ENGINE SHUTDOWN E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS AP APPROACH 1 CA 77168 77168 (CAN)#1 ENGINE RUNNING ROUGH ON APPROACH #9 CYLINDER PULLED AWAY FROM CRANKCASE ENGINE REPLACED 2 L 7 2 4R 4 R A669 5E4 1996112100154 19961121 00154 NE 1996 11 21 CA960423104 2 19960329 A 8520 CYLINDER DOUG DC3 DC3C 3021457 WP PWA R1830 R183092 52020 NE #9 DETACHED W E ENGINE SHUTDOWN E VIBRATION/BUFFET AP APPROACH 1 CA 444111 (CAN)ON FINAL APPROACH, #2 ENGINE BEGAN TO RUN ROUGH, IDLE POWER SELECTED AND LANDED OK. #9 CYLINDER BROKE AWAY FROM CRA NKCASE. SEVERAL MOUNTING STUDS PULLED. 2 L 7 2 4R 4 R A669 5E4 1996112100155 19961121 00155 NE 1996 11 21 CA960423107 2 19960415 A 7314 378200 PUMP BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE #1 ENG INOPERATIVE W E ENGINE SHUTDOWN O OTHER DE DESCENT 1 CA 39009 4248 707367B (CAN)LOST CONTROL OF POWER SETTINGS ON #1 ENGINE DURING DESCENT, SHUTDOWN BEFORE LANDING. #1 FCU REPLACED, NO CHANGE. OR IGINAL FCU REINSTALLED WITH A NEW FUEL PUMP, OPERATION NORMAL. 2 L 7 2 4F 4 F A16WE E2EA 1996112100156 19961121 00156 NM 1996 11 21 CA960423108 1 19960408 A 7931 SRLOC4N INDICATOR BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE NR 1 OIL PRESS STUCK W A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 CA 38848 22244 7224 707367B (CAN)#1 OIL PRESSURE NOTED AT 38 PSI ON TAKEOFF ROLL. PRESSURE REMAINED STEADY AT 38 PSI AT ALL ENGINE SETTINGS INCLUDIN G IDLE. ENGINE OPERATED AT REDUCED THRUST TILL LANDED. GAUGE REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1996112100157 19961121 00157 NM 1996 11 21 CA960423109 1 19960310 A 5500 FRAMES BOEING 767 767375 NM EMPENNAGE DAMAGED W O OTHER J G WARNING INDICATION MULTIPLE FAILURE LD LANDING 1 CA (CAN)ON LANDING THE TAIL SKID CONTACTED THE RUNWAY. THE IMPACT DROVE THE ACTUATOR UPWARD, SHEARING BOTH PIVOT BEARINGS, THE HYDRAULIC SUPPLY LINE & THE TWO 50 TON SAFETY RETAINER CABLES. THE TOP OF THE ACTUATOR CONTACTED THE LOWER END ON TH E HORIZONTAL STAB JACK SHEARING OFF THE SAFETY RETAINER BOLT. AT THIS POINT THE LOOSE ACTUATOR FELL INTO THE LOWER SECTI ON DAMAGING THE STAB TRIM LIMIT SWITCH/POSITION TRANSMITTER & THE L/H BRACKET OF THE CENTRE STAB TRIM LIMIT SWITCH/POSIT ION TRANSMITTER. THE LOWER FUSELAGE CONTACTED THE RUNWAY REMOVING THE GALLEY DRAIN MAST, CAUSED DAMAGE TO SKIN, FRAMES & STRINGERS. SKIN NOT PENETRATED. 2 L 7 2 4F RT A1NM 1996112100158 19961121 00158 1996 11 21 CA960424001 4 19960416 A 2215 5000023 CONTROL CABLE DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA RUDDER SERVO LOOSE W A K NONE O OTHER IN INSP/MAINT 1 CA PCE40595 (CAN)WHEN INSPECTING THE RUDDER CABLES AND ELEVATOR CABLES FOR CORROSION THE RUDDER SERVO CABLE WAS FOUND TO BE OFF THE PULLEY. ALL LOCKING DEVICES WERE "LOCKED". CABLE WAS SERVICEABLE. 1 H 7 2 3T 4 T RT A9EA E4EA 1996112100159 19961121 00159 EA 1996 11 21 CA960424002 1 19960423 A 2424 CONTROL UNIT 51608002 DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE #1 AC GENERATOR BROKEN WIRE W H DEACTIVATE SYST/CIRCUITS H ELECT. POWER LOSS-50 PC CR CRUISE 1 CA 123151 (CAN)#1 AC GENERATOR WILL NOT STAY ON LINE. FOUND BROKEN WIRE TO GENERATOR CONTROL UNIT. 2 H 7 2 4T 4 T RT A13NM E20NE 1996112100160 19961121 00160 NM 1996 11 21 CA960424003 1 19960423 A 2424 51608002 GCU DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE #2 AC GEN FAILED W H DEACTIVATE SYST/CIRCUITS H ELECT. POWER LOSS-50 PC CL CLIMB 1 CA 14439 734 120226 (CAN)#2 AC GENERATOR FAILED. FOUND GENERATOR CONTROL UNIT (GCU) AT FAULT. 2 H 7 2 4T 4 T RT A13NM E20NE 1996112100161 19961121 00161 NE 1996 11 21 CA960424004 2 19960423 A 7210 OIL FILTER PWA PW123 DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE RGB CLOGGED W K NONE J WARNING INDICATION IN INSP/MAINT 1 CA 10103 PCE126136 PCE126136 (CAN)#1 ENGINE RGB CHIP DETECTOR AND OIL FILTER CLOGGED FLAG WARN. METAL FOUND IN CHIP DETECTOR AND FILTER ENGINE REPL ACED 2 H 7 2 4T 4 T RT A13NM E20NE 1996112100163 19961121 00163 NM 1996 11 21 CA960424006 1 19960417 A 3230 82910010139 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NLG DOWN LINE PIN HOLE W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 120657 (CAN)HYDRAULIC LEAK IN NOSE WHEEL AREA. FOUND PIN HOLE IN NOSE GEAR DOWN LINETO SEQUENCING VALVE. HYDRAULIC LINE REPLACE D. 2 H 7 2 4T 4 T RT A13NM E20NE 1996112100165 19961121 00165 NM 1996 11 21 CA960424019 1 19960419 A 2910 1121521010 FLOW LIMITER BOEING 737 737210C 1384459 NM PWA JT8 JT8D9A 52048 NE A SYS HYD FAILED W K NONE K F FLUID LOSS FLT CONT AFFECTED TX TAXI/GRND HDL 1 CA P678085 (CAN)ON START UP THE HYDRAULIC METERING PISTON FAILED. ALL A SYSTEM HYDRAULIC FLUID LOST. FLOW LIMITER REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1996112100166 19961121 00166 EA 1996 11 21 CA960424501 1 19960401 A 2720 A253171 CONTROL PANEL CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RUDDER/AILERON RUNAWAY W O OTHER F FLT CONT AFFECTED CR CRUISE 1 CA 42028 807343 (CAN)AT FL350, AT CRUISE, RUDDER TRIM RUNAWAY TO FULL DEFLECTION NOSE RIGHT. REPLACED RUDDER/AILERON TRIM CONTROL PANEL. 2 L 7 2 4F 4 F RT A21EA E15NE 1996112100167 19961121 00167 1996 11 21 CA960424502 4 19960401 A 3460 FCU AIRBUS 320 A320211 3930320 EU FLT COMPUTERS INOPERATIVE W O OTHER O OTHER TX TAXI/GRND HDL 1 CA (CAN)ON ARRIVAL BOTH FLIGHT MANAGEMENT GUIDANCE COMPUTERS WERE INOPERATIVE. FULL ATUO LAND CHECK CARRIED OUT. FLIGHT CON TROL UNIT (F.C.U.) RESET. 2 L 7 2 4F RT A28NM 1996112100168 19961121 00168 WP 1996 11 21 CA960424503 1 19960402 A 2170 COALESCER BAGS DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE AIR COND SYS SATURATED W D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA P657518D (CAN)DURING START, SMOKE APPEARED IN AFT CABIN, FORWARD & AFT WASHROOM SMOKE DETECTORS ACTIVATED. UNABLE TO ISOLATE SOUR CE, DISCONTINUED START AND RETURNED TO GATE. MAINTENANCE ACTION INVOLVED REPLACING BOTH AIR CONDITIONING COALESCER BAGS. 2 L 7 2 4F 4 F A6WE E2EA 1996112100169 19961121 00169 NM 1996 11 21 CA960424504 1 19960503 A 2121 732591E COOLING FAN BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE CABIN BURNT W O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 CA P707531 (CAN)SMOKE REPORTED IN COCKPIT & CABIN BEFORE LANDING. EXHAUST COOLING FAN REPLACED. 2 L 7 2 4F 4 F RT A1NM E3NE 1996112100170 19961121 00170 NM 1996 11 21 CA960424505 1 19960403 A 2722 658D1005 TRIM ACTUATOR BOEING 767 767209 NM PWA JT9 JT9D7R4D 52054 NE RUDDER INTERMITTENT W A O OTHER F FLT CONT AFFECTED CR CRUISE 1 CA P707529 (CAN)RUDDER TRIM STUCK LEFT 2 DEGREES, FAILED TO MOVE IN EITHER DIRECTION, AFTER MORE THAN A HALF DOZEN TRIES TRIM START ED WORKING NORMAL. HAPPENED AGAIN THIS TIME LEFT 3 DEGREES TRIM; AFTER SEVERAL TRIES,BEGAN TO MOVE NORMALLY. REPLACED RU DDER TRIM ACTUATOR. 2 L 7 2 4F 4 F RT A1NM E3NE 1996112100171 19961121 00171 NM 1996 11 21 CA960424506 1 19960404 A 2750 FLAP LEVER BOEING 767 767209 NM PWA JT9 JT9D7R4D 52054 NE TE FLAPS ADJUSTED W O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 CA P709637 (CAN)TRAILING EDGE FLAP DISAGREE MESSAGE ON EICAS AND TRAILING LIGHT ILLUMINATED INTERMITTENTLY IN ALL PHASES OF FLIGHT AND ALL FLAP SETTINGS. ADJUSTED FLAP LEVER POSITION TOWARD UPPER TOLERANCE BAND. 2 L 7 2 4F 4 F RT A1NM E3NE 1996112100172 19961121 00172 EA 1996 11 21 CA960425102 1 19960406 A 2730 C3T1413 BRACKET DHAV DHAV DHC3 DHC3 2800202 EA PWA PT6 PT6A135 52043 NE TORQUE TUBE BENT W A K NONE O OTHER IN INSP/MAINT 1 CA PCE92614 (CAN)AIRCRAFT PARKED ON DOCK WITH FLIGHT CONTROL LOCKS ON. ELEVATORS NOTED IN HIGH POSITION. INSPECTION FOUND ELEVATORS MOVEMENT WAS RESTRICTED. ELEVATOR PUSH-ROD WAS HITTING STAB TRIM JACK. UPON FURTHER I NSPECTION IT WAS FOUND THAT THE EL EVATOR TORQUE TUBE PUSH ROD ATTACH BRACKET WAS BENT. OPERATOR SAYS TORQUE BRACKET BENT BECAUSE OF STRONG WINDS. 1 H 7 1 3R 4 T A815 E4EA 1996112100174 19961121 00174 NE 1996 11 21 CA960429002 2 19960419 A 7320 B10358 FCU ALLIED SIGNA 32448094 CESSNA 208 208B 2073701 CE PWA PT6 PT6A114 52043 NE ENG MALFUNCTION W A K NONE O OTHER TX TAXI/GRND HDL 1 CA B10358 PCE19139 (CAN)AFTER THE FIRST START OF THE DAY, WITH THE ENGINE AT IDLE, ADVANCING THE POWER LEVER BROUGHT NO RESPONSE FROM THE E NGINE. NO DEFECT COULD BE FOUND AND ENGINE SUBSEQUENTLY GROUND RUN AND PERFORMANCE RUN CARRIED OUT WITHOUT FAULT. THE AI RCRAFT FLEW THE REMAINDER OF THE DAY UNEVENTFULLY. THE FOLLOWING MORNING, THE SAME PROBLEM OCCURRED ON THE FIRST START. THE FUEL CONTROL UNIT WAS REPLACED. INVESTIGATION AT THE MANUFACTURER REPORTS "THE REPORTED REASON FOR REMOVAL WAS NOT C ONFIRMED IN-HOUSE BENCH TESTS". THIS IS THE SAME FINDINGS FROM THE MANUFACTURER AS FOR AN IDENTICAL SNAG APPROXIMATELY 1 8 MONTHS AGO. 1 H 7 1 3T 3 T A37CE E4EA 1996112100175 19961121 00175 EA 1996 11 21 CA960429004 2 19960226 A 8530 74541 EXHAUST VALVE CESSNA 172 172N 2072434 CE LYC O320 O320H2AD 41508 EA #4 CYL STICKING W K NONE O OTHER IN INSP/MAINT 1 CA 229 RL112076T (CAN)PERFORMING CESSNA SEB92-21 (LYC SB388B), #4 CYLINDER EXHAUST VALVE TO GUIDE CLEARANCE BELOW SPECIFIED. REWORKED IN ACCORDANCE WITH LYCOMING SI 1425. SB WAS NOT DUE FOR ANOTHER 170 HOURS. 1 H 7 1 3O 3 O NT 3A12 E274 1996112100176 19961121 00176 EU 1996 11 21 CA960429005 1 19960404 A 2460 BUSS BAR DORNER DORNER DO228 DO228202 2992030 EU GARRTT TPE331 TPE3315 01514 WP ELECTRICAL SYSTM NOT REMOVED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA P39159 (CAN)DURING TROUBLESHOOTING OF FLAP SYSTEM FOUND A BUSS BAR THAT WAS SUPPOSED TO HAVE BEEN REMOVED DURING SB 228-143 (AT FACTORY). THUS NOT ALLOWING ANY PROTECTION OF THE HYDRAULIC PUMP POWER WIRE. 2 H 7 2 4T 4 T RT A16EU E4WE 1996112100177 19961121 00177 EU 1996 11 21 CA960429006 1 19960404 A 2750 623A000005 BRAKE DORNER DORNER DO228 DO228202 2992030 EU GARRTT TPE331 TPE3315 01514 WP WING TIP BRAKE NOT RELEASING W D RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 CA P39159 (CAN)PART HAD RECENTLY BEEN INSTALLED. INTERMITTENT PROBLEMS OF FLAP CURRENT LIMITER BLOWING FOUND THAT THE ELECTRIC BRA KE ON THE WING TIP BRAKE (SYMNETRY UNIT) WOULD SOMETIMES TAKE UP TO 4 SECONDS TO RELE ASE AFTER THE INITIAL CLICK OF SOL ENOID. TEMPERATURE SENSITIVE. THE COLDER THE UNIT THE LONGER THE BRAKE WOULD TAKE TO RELEASE. THUS WHEN BRAKE WOULD NOT RELEASE THE MOTOR WOULD DRAW LOTS OF CURRENT AND BLOWING THE LIMITER. 2 H 7 2 4T 4 T RT A16EU E4WE 1996112100180 19961121 00180 EU 1996 11 21 CA960429012 1 19960422 A 3244 TIRE BRAERO 748 HS7482A 4231001 EU NLG FLAT W A UNSCHED LANDING O OTHER TO TAKEOFF 1 CA (CAN)AFTER TAKEOFF CREW DETECTED VIBRATION FROM NOSE WHEEL. AIRCRAFT DIVERTED FOR SLOW PASS, NOSE WHEEL FLAT, LANDED WIT HOUT INCIDENT. 2 L 7 2 3T A24EU 1996112100181 19961121 00181 SO 1996 11 21 CA960429201 1 19960331 A 3230 1114 FLUID LINE PIPER 455946 PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA RH MAIN GEAR LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 1046 L523761A (CAN)DURING A 100 HOUR INSPECTION IT WAS FOUND THAT THE RIGHT HAND LANDING GEAR UP LINE WAS LEAKING THROUGH PINHOLES WHE N TESTED UNDER PRESSURE. 1 L 7 2 3O 3 O A20SO E14EA 1996112100182 19961121 00182 EA 1996 11 21 CA960502002 1 19960501 A 3320 1141579 PCU BOARD GRIMES 1010814 DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE SEAT 12A BURNT W K NONE O OTHER IN INSP/MAINT 1 CA 123126 (CAN)PASSENGER SERVICE UNIT CIRCUIT BOARD AT SEAT 12A SHOWS SIGNS OF BURNING. CF-93-01R1 AND SB 8-33-34 APPLY. 2 H 7 2 4T 4 T RT A13NM E20NE 1996112100183 19961121 00183 NM 1996 11 21 CA960502003 1 19960501 A 2910 82950010137 HYDRAULIC LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE LEFT GND SPOILER LEAKING W O OTHER K FLUID LOSS IN INSP/MAINT 1 CA 120305 (CAN)HYDRAULIC LEAK IN VICINITY OF LEFT GROUND SPOILER. LINE LEAKING. 2 H 7 2 4T 4 T RT A13NM E20NE 1996112100184 19961121 00184 NM 1996 11 21 CA960502004 1 19960501 A 3060 3061K2 RELAY DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE PROP DEICE INOPERATIVE W O OTHER J WARNING INDICATION CR CRUISE 1 CA 120855 891001 (CAN)#2 PROPELLER PHASE A BLADES #1 & #2 INDICATE ANTI-ICE "ON" ALL THE TIME. RELAY NOT OPERATING, REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1996112100185 19961121 00185 EA 1996 11 21 CA960502006 2 19960422 A 7414 10357583 DISTRIBUTOR GEAR BENDIX 101630052 BEECH 95 D95A 1153408 CE LYC O360 IO360B1B 41514 EA GEAR AXLE BASE LOOSE ELECTRODE W A K NONE O OTHER IN INSP/MAINT 1 CA 215 712014 L389151A (CAN)THE MAGNETO WAS SENT IN FOR OVERHAUL, 215 HOURS AFTER A 500 HOUR INSPECTION. THE CUSTOMER HAD SNAGGED IT FOR NOT FI RING. INTERNAL INSPECTION FOUND THAT THE ELECTRODE AND AXLE ASSEMBLY HAD COME LOOSE F ROM THE GEAR ITSELF. THE GEAR IS O F THE NEWEST TYPE AND NO REASON FOR THE FAILURE COULD BE FOUND. THE GEAR WAS REPLACED AND THE UNIT RETURNED TO SERVICE. 1 L 7 2 3O 3 O 3A16 1E10 1996112100186 19961121 00186 SW 1996 11 21 CA960502024 1 19960325 A 5320 206031322003 STIFFENER BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL OIL COOL BLOWER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 14691 CAE801518BA (CAN)CRACKS FOUND AT ANCHOR NUT HOLES WHICH MOUNT LEFT SIDE OF OIL COOLER BLOWER TO FUSELAGE. 1 G 7 1 3U 3 U H2SW E4CE 1996112100190 19961121 00190 EA 1996 11 21 CA960502052 1 19960501 A 3246 SCREW WIPLINEINC 6000 DHAV DHC2 DHC2MK3 2800107 EA PWA PT6 PT6A27 52043 EA FLOAT AXLE HEAD BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 1200 PCE40150 (CAN)THE 3/8-16 X 5/8 LG ALLEN STYLE HEAD OF BOLT FOUND FRACTURED ON THE BOTTOM SIDE OF THE HEAD. ONE BOLT OF EACH LANDI NG GEAR AFFECTED. THIS BOLT ATTACHES THE BRAKE ASSEMBLY TO THE FLANGE ON THE FLOAT AX LE. 1 H 7 1 3T 4 T A806 E4EA 1996112100191 19961121 00191 SW 1996 11 21 CA960502053 1 19960422 A 3233 2752010003 ACTUATOR SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP NLG NOISY W O OTHER O OTHER AP APPROACH 1 CA 15534 P54202 (CAN)NOSE GEAR FAILED TO EXTEND. EMERGENCY EXTENSION CARRIED OUT. FROZEN SLUSH ON NOSE GEAR. NLG FAILED TO EXTEND NORMAL LY AFTER WARMING UP IN HANGAR AND GEAR SWINGS CARRIED OUT. SOME SAND CONTAMINATION IN GEAR MECHANISM. LH NLG ACTUATOR IS ONLY ACTUATOR THAT DRIVES THE NLG IN A NORMAL EXTENSION. THIS ACTUATOR WAS NOISY AND SUSPECTED STIFF. ALSO REPLACED THE RESTRICTOR. GEAR PRESSURE WASHED AND ALL FITTINGS LUBRICATED. 2 L 7 2 4T 4 T RT A8SW E4WE 1996112100192 19961121 00192 NM 1996 11 21 CA960502055 1 19960422 A 2530 HEAT TANK 1440A10T DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE GALLEY OVERPRESSURIZED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA 8978 9 LH120339 (CAN)COFFEE MAKER BOILED OVER. CAUSED STEAM IN GALLEY AND FLIGHT DECK AIRCRAFT RETURNED TO LAND. HEATER TANK FOUND OVERP RESSURIZED CAUSING TANK TO CONTACT GALLEY SHELF MELTING CONTACT AREA. 2 H 7 2 4T 4 T RT A13NM E20NE 1996112100193 19961121 00193 NE 1996 11 21 CA960502058 2 19960427 A 7200 ENGINE LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE #3 VIBRATION W E ENGINE SHUTDOWN E VIBRATION/BUFFET CR CRUISE 1 CA 41130 2927 10233 (CAN)#3 ENGINE SHUTDOWN DUE TO VIBRATION ON BOTH CHANNELS DURING CRUISE. NO FAULT FOUND BY MAINTENANCE, LP COMPRESSOR CL EANED, SURVEY TEST 11 FOUND WITHIN LIMITS. 2 L 7 3 4F 4 F A23WE E12EU 1996112100194 19961121 00194 SW 1996 11 21 CA960503103 1 19960404 A 6220 2060101215 LATCH FITTING BELL 206011100021 BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL M/R HUB CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1171 CAE823114 (CAN)DURING OVERHAUL OF MAIN ROTOR HUB ASSEMBLY, A 3/4" CRACK WAS FOUND IN ONE EAR OF LATCH FITTING. TTSN OF MAIN ROTOR HUB WAS 12668 HOURS. 1 G 7 1 3U 3 U H2SW E4CE 1996112100195 19961121 00195 NM 1996 11 21 CA960507002 1 19960425 A 8010 6612 GCU DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE #1 ENGINE STUCK ON W E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. B H SMOKE/FUMES/ODORS/SPARKS ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 CA 6612 120467 (CAN)AFTER STARTUP, GOUND POWER WAS DISCONNECTED AND POWER SWITCHED TO AIRCRAFTAT THIS, A LEFT MAIN BUS FAULT WAS INDICA TEDTHE CREW TRIED A RESET WITH NO SUCCESS AND #1 ENGINE WAS SHUTDOWN AFTER SHUTD OWN, SMOKE WAS SEEN COMING FROM #1 ENG INE, NO FIRE, STARTER STILL ENGAGED AND SMOKING. MAINTENANCE REPLACED #1 GCU AND STARTER GENERATOR. 2 H 7 2 4T 4 T RT A13NM E20NE 1996112100197 19961121 00197 EU 1996 11 21 CA960507004 1 19960415 A 3246 AH52930 WHEEL BRAERO 748 HS7482A 4231001 EU NR 3 WHEEL BROKEN RIM W A UNSCHED LANDING O OTHER CL CLIMB 1 CA (CAN)AFTER TAKEOFF PILOT REPORTED POSSIBLE BLOWN TIRE AND WAS RETURNING. #3 WHEEL HAD BLOWN A SECTION OF INBOARD RIM. RI M HAD 656 CYCLES SINCE LAST OVERHAUL. 2 L 7 2 3T A24EU 1996112100198 19961121 00198 NM 1996 11 21 CA960507006 1 19960426 A 3233 NAS1103B BOLT DHAV 85310340011 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NOSE TRUNNION SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA LH120548 (CAN)DURING CF-92-18R3 (NOSE WHEEL TRUNNION) INSPECTION TOP MOST BOLT ON THE RH ACTUATOR FITING ASSEMBLY WAS FOUND SHEAR ED. 2 H 7 2 4T 4 T RT A13NM E20NE 1996112100199 19961121 00199 NM 1996 11 21 CA960507007 1 19960427 A 3020 DUCT PWA 652673822 BOEING 727 727212 138407G NM PWA JT8 JT8D7B 52053 NE FLANGE ANTI-ICE RUPTURED W J A E DUMP FUEL UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 CA 653716 (CAN)#2 ENGINE ANTI-ICE C.B. TRIPPED AND WOULD NOT RESET. #2 OIL PRESSURE/BYPASS ILUMINATED. #2 SHUTDOWN. AIR SUPPLY DUC T FROM 13TH STAGE TO NOSE COWL ANTI-ICE AND FUEL HEAT HAD RUPTURED AT THE ATTACH FLANGE FOR THE ANTI-ICE VALVE CAUSING T HE WIRING HARNESS DAMAGE BY EXPOSURE TO STAGE 13 AIR. 2 L 7 3 4F 4 F A3WE E2EA 1996112100200 19961121 00200 WP 1996 11 21 CALA9601649 1 19961012 A 5350 CLIPS DOUG DC9 DC981 3022081 WP TAILCONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16883 48073 THE INTERIOR TAILCONE RELEASE HANDLE PULLED FROM CLIPS AT 50 POUNDS. THE CLIPS WERE ADJUSTED IAW MM 53-53-00. 2 L 7 2 4F A6WE 1996112100201 19961121 00201 WP 1996 11 21 CALA9601650 1 19961012 A 5350 CLIPS DOUG DC9 DC981 3022081 WP TAILCONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16883 48073 THE EXTERIOR TAILCONE RELEASE HANDLE PULLED FROM CLIPS AT 20 POUNDS. THE CLIPS WERE ADJUSTED IAW MM 53-53-00. 2 L 7 2 4F A6WE 1996112100202 19961121 00202 NM 1996 11 21 CALA9601651 1 19961109 A 5314 KEEL BEAM BOEING 737 737130 1384435 NM BS 700 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14212 19029 INSPECTION FOUND A 1.5 INCH CRACK IN KEEL BEAM SKIN AT STA 700. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AN D INSTALLED IAW SRM 53-30-3. 2 L 7 2 4F A16WE 1996112100203 19961121 00203 NM 1996 11 21 CALA9601652 1 19961110 A 5312 BULKHEAD BOEING 737 737130 1384435 NM BS 178 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14212 19029 INSPECTION FOUND A 6 INCH CRACK IN BULKHEAD AT STA 178, LT SIDE. THE CRACKED AREA WAS CUT OUT, A REPAIR DOUBLER AND FIL LER WERE FABRICATED AND INSTALLED IAW SRM 53-10-11. 2 L 7 2 4F A16WE 1996112100204 19961121 00204 NM 1996 11 21 CALA9601653 1 19961110 A 5312 BULKHEAD BOEING 737 737130 1384435 NM BS 178 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14212 19029 INSPECTION FOUND A 6 INCH CRACK IN BULKHEAD AT STA 178, RT SIDE. THE CRACKED AREA WAS CUT OUT, A REPAIR DOUBLER AND FIL LER WERE FABRICATED AND INSTALLED IAW SRM 53-10-11. 2 L 7 2 4F A16WE 1996112100205 19961121 00205 NM 1996 11 21 CALA9601654 1 19961029 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 1006 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16310 23361 INSPECTION FOUND FLOORBEAM CORRODED AT STA 1006, LBL 20 TO RBL 20. A NEW UPPER T-FLANGE WAS SPLICED IN IAW SRM 53-00-51 . 2 L 7 2 4F RT A16WE 1996112100206 19961121 00206 NM 1996 11 21 CALA9601655 1 19961022 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM BS 986-1006 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16310 23361 INSPECTION FOUND LT AFT LAV FLOOR SUPPORT ANGLE CORRODED AT STA 986 TO 1006. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 1996112100207 19961121 00207 NM 1996 11 21 CALA9601656 1 19961022 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM CARGO COMPT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16310 23361 INSPECTION FOUND FLOOR SUPPORT CORRODED INBOARD OF DOOR IN AFT PIT. A NEW SECTION OF FLOOR SUPPORT WAS SPLICED IN IAW S RM 53-00-53. 2 L 7 2 4F RT A16WE 1996112100208 19961121 00208 NM 1996 11 21 CALA9601657 1 19961022 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM BS 1006-1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16310 23361 INSPECTION FOUND LT AFT LAV FLOOR SUPPORT CORRODED AT STA 1006 TO 1016. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 1996112100209 19961121 00209 NM 1996 11 21 CALA9601658 1 19961022 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM BS 986-1006 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16310 23361 INSPECTION FOUND RT AFT LAV FLOOR SUPPORT ANGLE CORRODED AT STA 986 TO 1006. THE SUPPORT ANGLE WAS REPAIRED IAW SRM 51- 10-02. 2 L 7 2 4F RT A16WE 1996112100210 19961121 00210 NM 1996 11 21 CALA9601659 1 19961022 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM BS 1006-1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16310 23361 INSPECTION FOUND RT AFT LAV FLOOR SUPPORT ANGLE CORRODED AT STA 1006 TO 1016. THE SUPPORT ANGLE WAS REPLACED IAW SRM 51 -10-02. 2 L 7 2 4F RT A16WE 1996112100211 19961121 00211 NM 1996 11 21 CALA9601660 1 19961020 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 947.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16310 23361 INSPECTION FOUND FLOORBEAM CORRODED AT STA 947.5, LBL 3 TO 8. THE CORRODED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-00-51. 2 L 7 2 4F RT A16WE 1996112100212 19961121 00212 NM 1996 11 21 CALA9601661 1 19961021 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM BS 294.5-312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16310 23361 INSPECTION FOUND FORWARD PASSENGER CABIN FLOOR SUPPORT CORRODED FROM STA 294.5 TO 312, 13 RIGHT OF CENTER AND 15 RIGHT O F CENTER. REPAIRS WERE FABRICATED AND INSTALLED IAW ECRA 5310-03347. 2 L 7 2 4F RT A16WE 1996112100213 19961121 00213 NM 1996 11 21 CALA9601662 1 19961021 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM BS 307 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16310 23361 INSPECTION FOUND FORWARD LAV LT SIDE AFT WALL FLOOR SUPPORT CORRODED AT STA 307. THE FLOOR SUPPORT WAS REMOVED AND REPL ACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 1996112100214 19961121 00214 NM 1996 11 21 CALA9601663 1 19961021 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM BS 294.5-312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16310 23361 INSPECTION FOUND FORWARD PASSENGER CABIN FLOOR SUPPORT CORRODED FROM STA 294.5 TO 312, 11 LEFT OF CENTER. THE FLOOR SUP PORT WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 1996112100215 19961121 00215 NM 1996 11 21 CALA9601664 1 19961021 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM BS 327 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16310 23361 INSPECTION FOUND A .75 INCH CRACK AT AFT END OF FLOOR SUPPORT ON LT SIDE OF FORWARD CABIN NEAR STA 327, 13 INBOARD OF DO OR. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-70-11. 2 L 7 2 4F RT A16WE 1996112100216 19961121 00216 NM 1996 11 21 CALA9601665 1 19961021 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM BS 328-344 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16310 23361 INSPECTION FOUND A 1.5 INCH CRACK AT ONE END OF FLOOR SUPPORT IN FORWARD CABIN ON LT SIDE, WITH CORROSION AT OTHER END, STA 328 TO 344. THE FLOOR SUPPORT WAS REPAIRED IAW SRM 51-70-12. 2 L 7 2 4F RT A16WE 1996112100217 19961121 00217 NM 1996 11 21 CALA9601666 1 19961021 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM BS 328-344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16310 23361 INSPECTION FOUND FORWARD CABIN FLOOR SUPPORT CORRODED BETWEEN STA 328 AND 344, 11 RIGHT OF CENTER. THE FLOOR SUPPORT WA S REPAIRED IAW ECRA 5310-03347. 2 L 7 2 4F RT A16WE 1996112100218 19961121 00218 NM 1996 11 21 CALA9601667 1 19961021 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 294.5/344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16310 23361 INSPECTION FOUND FORWARD CABIN FLOORBEAM CORRODED AROUND SCREW HOLES AT STA 294.5 AND STA 344. THE FLOORBEAM WAS REPAIR ED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 1996112100219 19961121 00219 NM 1996 11 21 CALA9601668 1 19961021 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16310 23361 INSPECTION FOUND FORWARD CABIN FLOORBEAM CORRODED AROUND SCREW HOLES AT STA 312, FROM R-1 DOOR TO 10 LEFT OF CENTER. TH E FLOORBEAM WAS REPAIRED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 1996112100220 19961121 00220 NM 1996 11 21 CALA9601669 1 19961023 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16310 23361 INSPECTION FOUND FORWARD CABIN FLOORBEAM AT STA 328 CORRODED FROM 29 LEFT OF CENTER TO AIRCRAFT CENTERLINE. THE FLOORBEA M WAS REPAIRED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 1996112100221 19961121 00221 NM 1996 11 21 CALA9601670 1 19961020 A 5754 SKIN BOEING 737 7373T0 1384582 NM NR 5 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16310 23361 INSPECTION FOUND A .125 INCH CRACK JUST INBOARD OF ACTUATOR, IN LOWER SKIN OF RT WING NR 5 SLAT PANEL. A DOUBLER WAS IN STALLED IAW ECRA 5750-01159. 2 L 7 2 4F RT A16WE 1996112100222 19961121 00222 NM 1996 11 21 CALA9601671 1 19961022 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 966-986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16310 23361 INSPECTION FOUND INTERCOSTAL CORRODED AT STA 966 TO 986, RBL 15. AN INTERCOSTAL WAS FABRICATED AND INSTALLED IAW ECRA 5 310-03347 AND SRM 51-10-02. 2 L 7 2 4F RT A16WE 1996112100223 19961121 00223 NM 1996 11 21 CALA9601672 1 19961022 A 5320 CHANNEL BOEING 737 7373T0 1384582 NM BS 990 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16310 23361 INSPECTION FOUND LT AFT LAV U-CHANNEL CORRODED AT BS 990. A NEW U-CHANNEL WAS INSTALLED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 1996112100224 19961121 00224 WP 1996 11 21 9624619180 1 19961114 A 2130 SEAL DOUG DC9 DC914 3022034 WP NEG PRESS VLV FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 3317L 45707 ON CLIMBOUT, CABIN PRESSURE LIGHT ILLUMINATED. CABIN ALTITUDE AT 10,200 AND RISING. INITIATED EMERGENCY DESCENT AND FO LLOWED COM PROCEDURE. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. FOUND NEGATIVE PRESSURE VALVE SEAL BAD. REP LACED SEAL, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996112100225 19961121 00225 NM 1996 11 21 9624626302 1 19961116 A 2780 WIRE BOEING 747 747451 1384940 NM LE FLAPS FAILED A NWAA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 GL 01 662US 23720 DURING CLIMB, THE NR 3 LEADING EDGE FLAP DID NOT RETRACT ACCOMPANIED BY A LEADING EDGE FLAP STATUS MESSAGE. AIRCRAFT RE TURNED TO AMS AND LANDED WITHOUT INCIDENT. REPAIRED AN OPEN WIRE FROM THE COCKPIT CIRCUIT BREAKER TO THE LEADING EDGE F LAP CONTROL RELAY, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1996112100226 19961121 00226 NM 1996 11 21 9624636302 1 19961115 A 2782 DRIVE UNIT BOEING 747 747451 1384940 NM NR 3 LE FLAP FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 662US 23720 DURING CLIMB, THE NR 3 LEADING EDGE FLAP DID NOT RETRACT ACCOMPANIED BY A LEADING EDGE FLAP STATUS MESSAGE. AIRCRAFT RE TURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED THE NR 3 LEADING EDGE FLAP DRIVE UNIT AND FOUR RELAYS, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1996112100227 19961121 00227 WP 1996 11 21 9624641154 1 19961115 A 7714 N 1 TRANSMITTER DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 3 ENGINE FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 154US 46763 86175 DURING TAKEOFF ROLLOUT, THE NR 3 ENGINE N1 WOULD NOT REACH TAKEOFF POWER WITH ENGINE FAIL LIGHT ILLUMINATED. THE TAKEOF F WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE NR 3 N1 TRANSMITTER. 2 L 7 3 4F 4 F A22WE E20EA 1996112100228 19961121 00228 EU 1996 11 21 9624653248 1 19961116 A 3230 848401 PROX SENSOR AIRBUS 320 A320212 EU NLG MALFUNCTIONED A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 348NW 410 DURING CLIMBOUT WHILE RETRACTING THE LANDING GEAR, THE NOSE LANDING GEAR WOULD NOT RETRACT. CYCLED LANDING GEAR HANDLE AND ALL INDICATIONS WERE NORMAL. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED N OSE LANDING GEAR PROXIMITY SENSORS 24GA AND 25GA, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996112100229 19961121 00229 EU 1996 11 21 9624663225 1 19961118 A 3350 321454 POWER SUPPLY AIRBUS 320 A320211 3930320 EU CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 325US 20120 8036 281 CIRCUIT BREAKER FOR EMERGENCY LIGHTS ON OVERHEAD PANEL H-5 TRIPPED. RESET UNSUCCESSFULLY. MAINTENANCE REPLACED AFT LEF T EPSU, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996112100230 19961121 00230 WP 1996 11 21 9624679927 1 19961114 A 3350 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8920E 45835 DURING FLIGHT, FOUND THAT THE RIGHT SIDE FLOOR EMERGENCY LIGHTS FROM ROWS 14 TO 17 WERE FLASHING. REPLACED THE BATTERIE S AND POWER SUPPLY AT THE AFT RIGHT EMERGENCY EXIT SIGN, CHECKED OK. 2 L 7 2 4F A6WE 1996112100231 19961121 00231 WP 1996 11 21 9624689752 1 19961117 A 3260 SWITCH STRIKER DOUG DC9 DC941 302207N WP LT MLG OUT OF ADJUST A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 752NW 47116 AFTER TAKEOFF, THE GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. RECYCLED GEAR, LIGHT REMAINED ILLUMINA TED. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEFT SWITCH STRIKER, ADJUSTED AND CYCLED GEAR SEVERAL TIMES, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996112100232 19961121 00232 WP 1996 11 21 9624699957 1 19961117 A 3350 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 915RW 47139 DURING LINE CHECK, FOUND THAT THE EMERGENCY LIGHT AT THE LEFT ENGINE NACELLE WAS INOPERATIVE. REPLACED THE BATTERY PACK AND POWER SUPPLY, CHECKED OK. 2 L 7 2 4F A6WE 1996112100233 19961121 00233 WP 1996 11 21 9624709604 1 19961117 A 3350 NW9A3390463 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 604NW 47222 DURING LINE CHECK, FOUND THAT THE CATWALK EMERGENCY LIGHTS AND THE TAILCONE EXIT SIGN LIGHT WERE INOPERATIVE. REPLACED THE POWER SUPPLY, CHECKED OK. 2 L 7 2 4F A6WE 1996112100234 19961121 00234 WP 1996 11 21 9624719987 1 19961116 A 3350 BATTERY DOUG DC9 DC932 3022066 WP CABIN CONTAMINATED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 987US 47458 DURING LINE CHECK, FOUND THAT THE EMERGENCY SEAT LIGHTS WERE INOPERATIVE. FOUND THE TAILCONE EMERGENCY BATTERY PACK FIL LED WITH DE-ICING FLUID. REPLACED THE BATTERY PACK, CHECKED OK. 2 L 7 2 4F A6WE 1996112100235 19961121 00235 WP 1996 11 21 9624729947 1 19961116 A 3350 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8938E 47161 DURING L-CHECK, FOUND THAT THE LEFT FORWARD OVERWING EVACUATION SLIDE BATTERY FAILED THE CHECK. REPLACED THE SLIDE (P/N 11331-3), (S/N 53). 2 L 7 2 4F A6WE 1996112100236 19961121 00236 WP 1996 11 21 9614739951 1 19961114 A 3260 SWITCH DOUG DC9 DC932 3022066 WP THROTTLE FAILED A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 9347 45827 UPON RAISING GEAR AFTER TAKEOFF, GEAR WARNING HORN SOUNDED CONTINUOUSLY. RECYCLED GEAR SEVERAL TIMES, BOTH CLEAN AND FL APS 15. CYCLED THROTTLES UP AND PUSHED HORN OFF BUTTON, HORN CEASED. FLIGHT CONTINUED TO MSP AND LANDED WITHOUT INCIDE NT. MAINTENANCE CHANGED THROTTLE SWITCH PACK FOR RIGHT THROTTLE, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996112100237 19961121 00237 WP 1996 11 21 9614749983 1 19961117 A 3350 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 983US 47282 DURING LINE CHECK, FOUND THAT THE LAST FOUR ROWS OF EMERGENCY SEAT LIGHTS AND THE AFT LEFT LAV EMERGENCY LIGHT WERE INOP ERATIVE. REPLACED THE BATTERY PACK (P/N 9133-90368-1) AND POWER SUPPLY (P/N BC5-0447-907), CHECKED OK. 2 L 7 2 4F A6WE 1996112100238 19961121 00238 WP 1996 11 21 9624759752 1 19961118 A 3260 UNSAFE LIGHT DOUG DC9 DC941 302207N WP LT MLG ILLUMINATED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 752NW 47116 LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. FOLLOWED COM PROCEDURE AND RECYCLED GEAR. GEAR DOWN INDICATIONS ARE NORMAL BUT LEFT GEAR UNSAFE LIGHT REMAINED ON WITH GEAR UP. FLIGHT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPAIRED WIRING AT S3-65, STUD NR 5. REPLACED STRIKER FOR LEFT SWITCH, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996112100239 19961121 00239 WP 1996 11 21 9624769753 1 19961118 A 3010 HIGH TEMP LIGHT DOUG DC9 DC941 302207N WP RIGHT ILLUMINATED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 753NW 47117 RIGHT ICE PROTECTION TEMPERATURE HIGH LIGHT ILLUMINATED WHEN AIRFOIL ANTI-ICE SELECTED. FLIGHT RETURNED TO DTW AND LAND ED WITHOUT INCIDENT. REPLACED ANTICIPATOR AND THERMOSTAT, RAN STINGER CHECK, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996112100240 19961121 00240 WP 1996 11 21 9624849162 1 19961118 A 2421 GENERATOR DOUG DC9 DC914 3022034 WP RIGHT INOPERATIVE A NWAA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CL CLIMB 1 GL 01 8907E 45748 DURING CLIMBOUT, THE RIGHT GENERATOR OFF LIGHT ILLUMINATED WITH SUBSEQUENT GENERATOR FAILURE. PERFORMED COM PROCEDURE A ND RETURNED TO STL. AIRCRAFT LANDED WITHOUT INCIDENT. RIGHT GENERATOR WAS PLACARDED INOPERATIVE PER MEL 24-1A. 2 L 7 2 4F A6WE 1996112100241 19961121 00241 WP 1996 11 21 9624859964 1 19961116 A 5610 5912290502 WINDSHIELD DOUG DC9 DC931 3022065 WP RT COCKPIT SHATTERED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 912RW 8943 8943 47150 DURING CLIMB, THE FIRST OFFICER'S WINDSHIELD OUTER PANE SHATTERED. RETURNED TO MSP WITHOUT FURTHER INCIDENT. REPLACED WINDSHIELD PER MM 56-10-2, LEAK CHECK OK. 2 L 7 2 4F A6WE 1996112100242 19961121 00242 WP 1996 11 21 9624499913 1 19961114 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 680 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 963N 47415 DURING H-CHECK, FOUND A CRACK IN THE LEFT OUTBOARD SEAT TRACK SUPPORT FITTING AT FS 680. REPLACED FITTING PER SRM 51-30 -5. 2 L 7 2 4F A6WE 1996112100243 19961121 00243 WP 1996 11 21 9624509603 1 19961114 A 5320 FITTING DOUG DC9 DC932 3022066 WP PAX DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 603NW 47101 DURING LINE CHECK, FOUND A CRACK IN THE AFT ENTRY DOOR UPPER RIGHT DOOR STOP FITTING. REPLACED FITTING (P/N 4917923-501 ) PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996112100244 19961121 00244 WP 1996 11 21 9624519760 1 19961021 A 5312 BULKHEAD PANEL DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 760NW 47288 DURING LINE CHECK, FOUND A 3 INCH CRACK IN THE SLANTED PRESSURE PANEL TO FUSELAGE ATTACH ANGLE APPROXIMATELY LBL 24 ABOV E THE REAR SPAR. REPAIRED ANGLE (P/N 9923419-9) PER EA 97-111746. 2 L 7 2 4F A6WE 1996112100245 19961121 00245 WP 1996 11 21 9624529760 1 19961025 A 5315 FLOORBEAM DOUG DC9 DC941 302207N WP BS 1056 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 760NW 47288 DURING H-CHECK, FOUND CORROSION IN THE FS 1056 FLOORBEAM LEFT SIDE. REPAIRED BEAM (P/N 9958187) PER EA 97-111777. 2 L 7 2 4F A6WE 1996112100246 19961121 00246 WP 1996 11 21 9624539993 1 19961029 A 5330 SKIN DOUG DC9 DC931 3022065 WP PAX DOORWAY CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8986E 47402 DURING M-CHECK, FOUND A CRACK IN THE FORWARD ENTRY DOOR JAMB SKIN AT THE AFT SIDE, 4TH STOP FROM THE TOP. REPAIRED SK IN PER EA 99-111046. 2 L 7 2 4F A6WE 1996112100247 19961121 00247 WP 1996 11 21 9624549760 1 19961105 A 5312 BULKHEAD PANEL DOUG DC9 DC941 302207N WP BS 108 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 760NW 47288 DURING H-CHECK, FOUND CRACKS IN THE NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL AT FS 108, LEFT AND RIGHT SID ES, AT BOTH THE INBOARD AND OUTBOARD VERTICAL BEAM ATTACH FITTINGS. REPAIRED PANEL (P/N 9910073-313) PER EA 97-111754. 2 L 7 2 4F A6WE 1996112100248 19961121 00248 WP 1996 11 21 9624559760 1 19961105 A 5313 LONGERON DOUG DC9 DC941 302207N WP BS 794 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 760NW 47288 DURING H-CHECK, FOUND CORROSION AT LONGERON 30 AT FS 794. REPAIRED LONGERON (P/N 5924878-501) PER EA 97-111762. 2 L 7 2 4F A6WE 1996112100249 19961121 00249 WP 1996 11 21 9624569760 1 19961105 A 5315 FLOORBEAM DOUG DC9 DC941 302207N WP BS 1041 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 760NW 47288 DURING H-CHECK, FOUND CORROSION IN THE FS 1041 FLOORBEAM CHORD, RIGHT SIDE. REPAIRED CHORD (P/N 9912243-55) PER EA 97-1 11768. 2 L 7 2 4F A6WE 1996112100250 19961121 00250 WP 1996 11 21 9624579760 1 19961107 A 5313 LONGERON DOUG DC9 DC941 302207N WP BS 531 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 760NW 47288 DURING H-CHECK, FOUND CORROSION ON LONGERON 30 AT FS 531. REPAIRED LONGERON (P/N 5924819-517) PER EA 97-111799. 2 L 7 2 4F A6WE 1996112100251 19961121 00251 WP 1996 11 21 9624589140 1 19961112 A 5312 BULKHEAD PANEL DOUG DC9 DC914 3022034 WP BS 105 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 930RC 45729 DURING H-CHECK, FOUND CRACKS IN THE NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL AT FS 105 AT THE LEFT INBOARD AND OUTBOARD VERTICAL BEAM FITTINGS AND AT THE RIGHT OUTBOARD VERTICAL BEAM FITTING. REPAIRED PANEL (P/N 9910073-313) PER EA 91-111773. 2 L 7 2 4F A6WE 1996112100252 19961121 00252 WP 1996 11 21 9624599986 1 19961115 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 986US 47480 DURING H-CHECK, FOUND A CRACK IN THE FUSELAGE SKIN AT THE FORWARD SERVICE DOOR FORWARD SIDE UPPER AFT ADJUSTOR CUTOUT. R EPAIRED SKIN PER EA 99-111057. 2 L 7 2 4F A6WE 1996112100253 19961121 00253 WP 1996 11 21 9624609986 1 19961115 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 617 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 986US 47480 DURING H-CHECK, FOUND A ONE INCH CRACK IN THE FS 617 FRAME FLANGE AT THE RIGHT SIDE FLOORBEAM LUG. REPAIRED FRAME (PSE 53.09.016, P/N 9919613-502) PER EA DC9-53-068 AND SRM 51-30-2, 51-30-5. 2 L 7 2 4F A6WE 1996112100254 19961121 00254 1996 11 21 COMA9660210 4 19961114 A 2200 8220044001 FLT CNTRL PANEL CNDAIR CL600 CL6002B19 EA COCKPIT MALFUNCTIONED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 914CA 5887 7012 WARNING TONE CAME ON AT LIFT OFF AND DID NOT GO OFF UNTIL FLAP RETRACTION AFTER LANDING. REPLACED FLIGHT CONTROL PANEL, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 1996112100255 19961121 00255 NM 1996 11 21 SWAA961251 1 19961116 A 2720 65C370529 PCU BOEING 737 7373H4 1384600 NM RUDDER FAILED A SWAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 07 314SW 23336 EXPERIENCED UNCOMMANDED YAW INPUT TO THE RIGHT DURING FLIGHT. DISENGAGING YAW DAMPER, NO HELP. AIRCRAFT RETURNED TO PH X AND MADE AN UNEVENTFUL LANDING. REPLACED RUDDER PCU, YAW DAMPER COUPLER AND TEST FLEW PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996112100256 19961121 00256 NE 1996 11 21 SWAA961252 2 19961117 A 7200 ENGINE BOEING 737 7373H4 1384600 NM GE CFM56 CFM563B1 13802 NE NR 2 FAILED A A SWAA A E UNSCHED LANDING ENGINE SHUTDOWN E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SW 07 327SW 25124 23691 721166 CLIMBING THROUGH 18,000, CREW SHUTDOWN NUMBER 2 ENGINE DUE TO HIGH VIBRATION AND HIGH EGT. RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. REPLACED NUMBER 2 ENGINE PER BOEING M/M. 2 L 7 2 4F 4 F RT A16WE E2GL 1996112100257 19961121 00257 NM 1996 11 21 SWAA961253 1 19961115 A 3230 65CC310991 LOCK ACTUATOR BOEING 737 7373H4 1384600 NM NLG FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 600WN 27694 AFTER GEAR RETRACTION, NOSE GEAR EXTENDED WITH GEAR HANDLE IN OFF POSITION. RETURNED TO PHX AND MADE AN UNEVENTFUL LAND ING. REPLACED NOSE GEAR LOCK ACTUATOR, RIGGED GEAR DOORS AND PERFORMED RETRACTION TEST PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996112100258 19961121 00258 NM 1996 11 21 SWAA961254 1 19961115 A 2131 7110025 CONTROLLER BOEING 737 7373H4 1384600 NM E/E BAY FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 307SW 22947 RETURNED DUE TO RT WING/BODY OVERHEAT ILLUMINATING. AFTER ISOLATING SYSTEM, AIRCRAFT WOULD NOT HOLD PRESSURIZATION. RE MOVED AND REPLACED PRESSURE CONTROLLER AND CONTROL PANEL PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996112100259 19961121 00259 NE 1996 11 21 WWMA9600096 2 19961117 A 7530 CLAMP SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE BLEED DEFECTIVE A WWMA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 15 269AE 340B269 AT APPROXIMATELY 200 FT AGL RT ENG LOST PWR, PWR FLUCTATED BRIEFLY BETWEEN 40 TO 90 PERCENT TORQUE. AT 2500 FT ON RETUR N TO FIELD WITH PWR REDUCED TO 30 TO 40 PERCENT THE TORQUE FLUCTATED BETWEEN 0 TO 10 PERCENT. THE ENGINE WAS THEN SHUT DOWN. FOUND HP BLEED LINE HAD CLAMP FAILURE AND HAD SEPARATED. BORESCOPED ENG AND PERFORMED RUNS, ALL CHECKED OK. 2 L 7 2 4T 4 T RT A52EU E8NE 1996112100260 19961121 00260 EU 1996 11 21 WWMA9600095 1 19961112 A 2530 RECEPTICLE SAAB SF340 340B 7860101 EU NR 2 HOT JUG FAILED A WWMA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 WP 15 345SB 340B345 CLIP SECURING NR 2 HOT JUG IS TOO DIFFICULT TO TURN. ALSO, BURNING ODOR COMING FROM NR 2 HOT JUG AREA. LUBED CLIP AND REPLACED HOT JUG RECEPTICLE. 2 L 7 2 4T RT A52EU 1996112100261 19961121 00261 EU 1996 11 21 WWMA9600094 1 19961107 A 2530 RECEPTICLE SAAB SF340 340B 7860101 EU NR 1 HOT JUG FAILED A WWMA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 WP 15 245AE 340B245 HOT WAX SMELL COMING FROM LAV LIGHTING. NR 1 HOT JUG RECEPTICALE AIRFRAME SIDE MELTED. PULLED JUG OUT, COLLARED C/B FO R NR 1 HOT JUG, DEFFERED DUE TO TIME MEL 25-13 AUTHORAZATION NR 110056M CAT D. 2 L 7 2 4T RT A52EU 1996112100262 19961121 00262 WP 1996 11 21 MWEA96631 1 19961116 A 5241 BEAM DOUG DC9 DC932 3022066 WP GALLEY SERV DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 DURING C-CHECK, FOUND GALLEY SERVICE DOOR LOWER BEAM CRACKED IN RADIUS AT FWD END. MAINTENANCE INSTALLED REPAIR IAW SRM 52-05 FIG 25. 2 L 7 2 4F A6WE 1996112100263 19961121 00263 WP 1996 11 21 MWEA96632 1 19961117 A 3350 6011779 POWER SUPPLY DOUG DC9 DC915 3022036 WP LT NACELLE INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 300ME 45718 DURING SERVICE CHECK, FOUND LEFT NACELLE EMERGENCY LIGHT BATTERY PACK INOP. MAINTENANCE REMOVED AND REPLACED LT NACELLE LIGHT BATTERY PACK, OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996112100264 19961121 00264 WP 1996 11 21 MWEA96633 1 19961118 A 3350 100865 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 206ME 47791 DURING A-CHECK, FOUND AFT ACCESSORY COMPARTMENT EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED BATTERY PWR SUP PLY, OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996112100265 19961121 00265 WP 1996 11 21 MWEA96630 1 19961112 A 2424 939D2171 VOLTAGE REG DOUG DC9 DC914 3022034 WP E/E COMPT INOPERATIVE A MWEA D RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TO TAKEOFF 1 GL 31 400ME 45727 PILOT REPORTS LEFT ENGINE GENERATOR DROPPED OFF LINE JUST BEFORE TAKEOFF. RETURNED TO GATE. MAINTENANCE REMOVED AND RE PLACED LT VOLTAGE REGULATOR, OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996112100266 19961121 00266 NM 1996 11 21 DL72P962501 1 19961106 A 5330 SKIN BOEING 727 727225 1384077 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8890Z 21859 LT WING ICE LIGHT MATING FLANGE CORRODED. REPAIRED PER SRM53-30-3. 2 L 7 3 4F A3WE 1996112100267 19961121 00267 NM 1996 11 21 DLM11962505 1 19961112 A 3350 7839 LIGHT DOUG MD11 MD11 3023602 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 804DE 48475 14625 NUMEROUS EMERGENCY FLOOR TRACK LIGHT OUT. REPLACED ALL EMERGENCY FLOOR TRACK LIGHTS THAT WERE OUT. 2 L 7 3 4F RT A22WE 1996112100268 19961121 00268 NM 1996 11 21 DL72S962510 1 19961112 A 5522 SKIN BOEING 727 727232 1384082 NM LT ELEVATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 402DA 21146 FOUND A .5 INCH CRACK IN LT ELEVATOR TOP SKIN, FWD OF OUTBD END OF TAB CUTOUT. REPAIRED PER SRM 55-20-3. 2 L 7 3 4F A3WE 1996112100269 19961121 00269 NM 1996 11 21 DL73K962513 1 19961112 A 3350 3114981 LIGHT BOEING 737 737232 1384475 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 301DL 23073 14625 EXTERIOR EMERGENCY LIGHT AT L1 DOOR INOP. 2 L 7 2 4F RT A16WE 1996112100270 19961121 00270 NM 1996 11 21 DLM11962514 1 19961113 A 2100 RAM AIR INLET ABM7060503 DOUG MD11 MD11 3023602 NM FWD FUSELAGE WORN A DALA K NONE E VIBRATION/BUFFET IN INSP/MAINT 1 SO 27 802DE 48473 14625 THE RAM AIR INLET DOOR AT ALL THREE POSITIONS WAS FOUND TO BE SEVERELY WORN IN SEVERAL PLACES. THESE INCLUDE THE MOUNT POINTS (P/N ABM7060-503) (DP/N 210701279. 2 L 7 3 4F RT A22WE 1996112100271 19961121 00271 NM 1996 11 21 DL72L962516 1 19961113 A 3350 LIGHT 1102833 BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 513DA 10712 21315 LT CENTER OVERWING EMERGENCY LIGHT AND AFT BULLNOSE EMERGENCY LIGHT INOP. REPLACED BATT PACK M955 AND AFT BULLNOSE LIGH T, ASSY OPS CHKS GOOD. 2 L 7 3 4F A3WE 1996112100272 19961121 00272 NM 1996 11 21 DL73S962518 1 19961023 A 7120 MOUNT BOEING 737 737232 1384475 NM ENGINE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 310DA 23082 THE FWD ENGINE MOUNT HAS TWELVE BOLT HOLES THAT ARE USED TO ATTACH TWO COVER PLATES TO EITHER END OF THE MOUNT, SIZE HOL ES PER COVER PLATE. THE TWELVE BOLT HOLES WERE FOUND WITH CORROSION IN THEM. THE BOLT HOLES WERE OVERSIZED TO .400/.40 7 TO REMOVE THE CORROSION. THE ENGINE MOUNT IS MADE FROM 4340 STEEL HEAT TREATED TO 270-300 KSI. THIS ER/A AUTHORIZES THE REPAIR OF THE BOLT HOLES. 2 L 7 2 4F RT A16WE 1996112100273 19961121 00273 NM 1996 11 21 DL73S962519 1 19961114 A 2910 BACH6M0207CKH HOSE BOEING 737 737232 1384475 NM NLG WW RUPTURED A DALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 27 318DL 23090 AFTER 15 TOUCH AND GO LANDINGS THE NOSE GEAR WOULD NOT EXTEND. LANDING GEAR WERE MANUALLY EXTENDED. AFTER THIS WAS ACC OMPLISHED PER THE CHECKLIST, THE A-HYD QTY IND WAS NOTED TO BE ZERO AND THE A-HYD PUMP LOW PRESSURE LIGHTS ILLUMINATED. ACCOMPLISHED A-HYD FAILURE CHECKLIST PER POM. LANDING WAS UNEVENTFUL. FOUND FLEX LINE FOR JURY BRACE ACT RUPTURED. 2 L 7 2 4F RT A16WE 1996112100274 19961121 00274 NM 1996 11 21 DL72W962520 1 19961114 A 2782 ANGLE BOEING 727 727247 138408F NM NR 1 SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 295WA 22532 FOUND THE NR 1 SLAT ACTUATOR INBD ATTACH ANGLE CRACKED. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1996112100275 19961121 00275 NM 1996 11 21 DL72W962521 1 19961114 A 5754 ANGLE BOEING 727 727247 138408F NM NR 1 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 295WA 22532 FOUND THE NR 1 SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED BELOW THE INBD STOP PAD. REPAIRED PER MM 57-50- 4. 2 L 7 3 4F A3WE 1996112100276 19961121 00276 NM 1996 11 21 DL72L962524 1 19961115 A 5720 STIFFENER BOEING 727 727232 1384082 NM LT WING LE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 A 1.75 INCH CRACK NR 3 SLAT I/B TRACK VERTICAL STIFFENER O/B. REPLACED STIFFENER PER MM 57-20-21 PG 813. 2 L 7 3 4F A3WE 1996112100277 19961121 00277 NM 1996 11 21 DLM88962526 1 19961116 A 3320 0200041023 SOCKET DOUG MD88 MD88 3023688 NM CABIN OVERHEAD FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 961DL 49980 BURNING/ELECT ODOR AFT GALLEY CLIMBING THROUGH 10,000 FT, NO SMOKE. FOUND FOUR BULB HOLDER SHORTED AT BULB PINS. REPLA CED THE HOLDER AND BULBS, CK'S OK. 2 L 7 2 4F RT A6WE 1996112100278 19961121 00278 WP 1996 11 21 DLL15962527 1 19961116 A 3350 POWER SUPPLY 5165741 LKHEED 1011 10113853 5265020 WP CABIN INOPERATIVE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 756DR 61368 193Y1185 DURING L/O CK, FOUND AFT CABIN EMERGENCY LIGHTS WOULD NOT REMAIN ON LONG ENOUGH DURING TEST OF THE EMERGENCY LIGHTS. RE PLACED POWER SUPPLY AT R-3 DOOR AND THE LIGHTS CK NORMAL. 2 L 7 3 4F A23WE 1996112100279 19961121 00279 NM 1996 11 21 DL73S962528 1 19961112 A 5312 BULKHEAD BOEING 737 737232 1384475 NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 318DL 23090 THE STATION 178 BULKHEAD WAS FOUND CRACKED IN SEVERAL LOCATIONS. DAMAGE CUTOUTS ARE: 1 DIA AT RBL 5.7, WL 198; 1 BY 1 .5 AT RBL 5.7, WL 201; 1 BY 1.5 AT LBL 5.7, WL 198; 1 BY 2 AT LBL 5.7, WL 201; AND 1 BY 1.5 AT BL 0, WL 188. THE BULK HEAD WEB IS FABRICATED FROM 0.032 CLAD 2024-T3. IN ADDITION, THE VERTICAL STIFFENER AT LBL 5.7 AND WL 184 WAS FOUND CRA CKED. THE RESULTING CUTOUT REMOVES THE FLANGE COMMON TO THE BULKHEAD WEB. THE VERTICAL STIFFENER IS MANUFACTURED FROM 7075-T6 EXTRUSION PER BAC 1505-100361. 2 L 7 2 4F RT A16WE 1996112100280 19961121 00280 NM 1996 11 21 DL72S962529 1 19961114 A 2782 651725613 SUPPORT BOEING 727 727232 1384082 NM NR 1 LE SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 408DA 21152 FOUND CRACK ON THE NR 1 SLAT ACTUATOR SUPPORT STRUCTURE. REPLACED CRACKED WEB IAW DAL ER/A 304444-14AD. 2 L 7 3 4F A3WE 1996112100281 19961121 00281 NM 1996 11 21 DL73S962530 1 19961112 A 5330 654576960 SKIN BOEING 737 737232 1384475 NM BS 379 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 306DL 23078 THE SKIN AT THE COOLING DUCT CUTOUT, BS 379, LBL 2 WAS FOUND CRACKED AT THE AFT EDGE OF THE CUTOUT INTO A FASTENER HOLE. THE CRACK IS APPROXIMATELY 1.5 INCHES IN LENGTH AND IS TYPICAL OF CRACKS DESCRIBED IN BOEING S/B 737-53-1117, REV 1. A PERMANENT REPAIR WILL BE INSTALLED PER THE BOEING S/B. 2 L 7 2 4F RT A16WE 1996112100282 19961121 00282 NM 1996 11 21 DLM88962533 1 19961116 A 3350 20131A BULB DOUG MD88 MD88 3023688 NM CABIN FAILED A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 972DL 53215 F/C EMERGENCY ESCAPE PATH LIGHTING INOP. 2 L 7 2 4F RT A6WE 1996112100283 19961121 00283 NM 1996 11 21 DL76L962534 1 19961116 A 3350 POWER SUPPLY BPS73 BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 173DN 9612 24800 ON L/O, FOUND EMERGENCY PATH LIGHTS BETWEEN ROWS 23 AND 28 BOTH AISLE INOP. REPLACED PWR SUPPLY AT ROW 28A, OPS CK OK. 2 L 7 2 4F RT A1NM 1996112100284 19961121 00284 WP 1996 11 21 DLL10962535 1 19961116 A 2560 257003804 EVAC PANEL LKHEED 1011 10113851 5265010 WP L1 DOOR FAILS TEST A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 716DA 193C1095 DURING H-CHECK, EVAC HORN AT L1 DOOR FAILED TO SOUND WHEN TESTED PER OPN 68111. REPLACED EVAC PANEL AT L1 DOOR, TESTS G OOD PRE OPN. 2 L 7 3 4F A23WE 1996112100285 19961121 00285 NE 1996 11 21 DL73E962536 2 19961117 A 7497 WIRE HARNESS BOEING 737 737247 138448D NM PWA JT8 JT8D15A 52051 NE NR 1 IGN SWITCH CHAFED A A DALA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 380DL 30259 30259 23607 709122 JUST PRIOR TO TAKEOFF, SPARKING AND POPPING FROM WET COMPASS AND IGN SWT SOME SMOKE. FOUND CHAFED WIRE ON NR 1 IGN SWT. REPAIRED WIRE, IGN SWT CKS OK. 2 L 7 2 4F 4 F A16WE E2EA 1996112100286 19961121 00286 NM 1996 11 21 DL72K962537 1 19961112 A 5754 65162255 SKIN BOEING 727 727232 1384082 NM NR 3 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 491DA 21060 FOUND CRACK ON CORNER END OF NR 3 L/E FLAP. REPAIRED PER M/M 57-53-0, PG 804. 2 L 7 3 4F A3WE 1996112100287 19961121 00287 NM 1996 11 21 P5CA9600955 1 19961114 A 5330 SKIN BOEING 747 747124 1384874 NM BS 160 PUNCTURED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FRAME WEB, INNER AND OUTER CHORD AT BS 160 WERE FOUND DAMAGED BETWEEN STRINGER S36L AND S42AL. REPAIRED PER POLAR AIR CARGO MA 5330-13:01 AND 5310-19:01. 2 L 7 4 4F A20WE 1996112100288 19961121 00288 SO 1996 11 21 SRAA961042 1 19961013 A 5320 SUPPORT LKHEED 382 382G 526414U SO BS 697 CORROSION A SRAA K NONE O OTHER IN INSP/MAINT 1 GL 23 905SJ 4472 DURING C-CHECK, FOUND CARGO COMPARTMENT FLOOR PANEL SUPPORT BEAM AT FS 697, RBL 20 HAS CORROSION AT FORWARD AND AFT SID E BEYOND LIMITS. CUT OUT CORRODED SECTION, FABRICATED AND INSTALLED L-ANGLE AND STRAP IAW LAC SRM CH 51-140-22. 2 H 7 4 4T A1SO 1996112100289 19961121 00289 1996 11 21 SRAA961112 3 19961119 A 6110 560501 PROPELLER LKHEED 382 382G 526414U SO NR 2 ENGINE DAMAGED A SRAA K NONE O OTHER IN INSP/MAINT 1 GL 23 920SJ 4561 ON WALKAROUND, FOUND NR 2 PROPELLER HAD DAMAGE AT BLADE CUFFS TRAILING EDGES FROM CONTACTING AFTERBODY FAIRING. ACCOMPL ISH THREE ENGINE FERRY TO MHZ. REPLACED NR 2 PROPELLER ASSEMBLY, AFTERBODY FAIRING PER SAT JOB CARDS 6101, 6101-1, 610 2 AND PERFORMED OPS CHECK PER SAT JOB CARDS 7101, 7101-2. 2 H 7 4 4T A1SO 1996112100290 19961121 00290 1996 11 21 HEEA968411 4 19961104 A 3421 1113034 INDICATOR BELL 412 412 1182202 SW COCKPIT ATTITUDE BALL STICKS E HEEA K NONE I FLT. ATTITUDE INST. NR NOT REPORTED 1 SW 03 33008 36004 ATTITUDE INDICATOR BALL STICKS IN PITCH. 1 G 7 2 4U H4SW 1996112100291 19961121 00291 1996 11 21 HEEA968412 4 19961104 A 3452 071119208 CONTROL BELL 214 214ST 1182106 SW COCKPIT ATC DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 8045T 28101 TRANSPONDER INOPERATIVE. PERFORMED PRELIMINARY INSPECTION, FOUND DIODES CR204 & CR205 SHORTED. ALSO FOUND C214 CAPACITO R BAD. REPLACED CR204, CR205, C214. REPAIRED. ALSO REPLACED PHOTOCELL V101 AND PHOTOCELL LENS P/N 088-00548-0000 AND RETAINING RING P/N 090-0036-04.REPAIRED. BENCH CHECK GOOD. 2 G 7 2 4U H10SW 1996112100292 19961121 00292 1996 11 21 HEEA968413 4 19961104 A 3455 071121009 CONTROL SKRSKY S76 S76A 8143006 NE ADF CONTROL LIGHT INOP E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22342 760096 LIGHTING INOPERATIVE. PERFORMED PRELIMINARY INSPECTION. FOUND 28V BULB DS301 BURNT, REPLACED DS301 BULB. REPAIRED. AL SO REPLACED V301 PHOTOCELL P/N 134-05005-0002. REPAIRED. CHECKED LIGHTING. BENCH CHECK GOOD. 1 G 7 2 3U H1NE 1996112100293 19961121 00293 1996 11 21 HEEA968414 4 19961104 A 3451 066107001 TRANSCEIVER BOLKMS 117 BK117A3 5626015 EU COCKPIT DME INDICATOR INOP E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8765J 7054 DME INDICATOR INOPERATIVE. (COMPONENT DETACHED FROM CIRCUIT BOARD) FOUND C125 CAPACITOR LOOSE IN UNIT. REPLACED C125 C APACITOR. UNIT STILL INOPERATIVE. FOUND L202 COIL HAD BROKEN LEAD AND WAS DETACHED FROM BOARD AT ONE END. CLEANED UP BOARD AND WAS ABLE TO REATTACH L202 TO BOARD. APPLIED SILICON AS SUGGESTED BYMANUFACTURER AND HOLD L202 COIL IN PLACE. CLEANED CORROSION. BENCH CHECK GOOD. 1 G 7 2 3U H13EU 1996112100294 19961121 00294 1996 11 21 HEEA968415 4 19961104 A 3452 066106200 TRANSCEIVER KT76 BOLKMS 105 BO105S 5626006 EU COCKPIT WEAK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 137AE S851 PILOT COMPLAINT OF WEAK SIGNAL. FOUND RECEIVE WEAK AND POWER OUT LOW, ADJUSTED V101. NO HELP. REPLACED V101 CAVITY OS CILLATOR. REPAIRED. ADJUSTED PULSE WIDTH AND FREQUENCY, PLACED IN FREEZER, HEATED AND VIBRATED. BENCH CHECK GOOD. 1 G 7 2 3U H3EU 1996112100295 19961121 00295 1996 11 21 HEEA968416 4 19961104 A 3452 066106200 TRANSCEIVER KT76 BOLKMS 105 BO105S 5626006 EU COCKPIT ATC DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 9190Y S669 TOWER REPORTED INTERMITTENT OPERATION. FOUND POWER OUT LOW, PERFORMED PRELIMINARY INSPECTION. FOUND FUSE F401 BLOWS WHE N UNIT IS TURNED ON. REPLACED V101 CAVITY TUBE V301 PHOTOCELL, ALSO REPLACED R477 RESISTOR. TROUBLESHOT UNIT, FOUND SW ITCH BOARD BEING SHORTED BY LOCKING MECHANISM.REALIGNED SWITCH BOARD AND REPLACED F401 FUSE. REPAIRED. PLACED IN FREEZ ER, HEATED AND VIBRATED. BENCH CHECK GOOD. 1 G 7 2 3U H3EU 1996112100296 19961121 00296 1996 11 21 HEEA968417 4 19961104 A 3452 066106200 TRANSCEIVER KT76 BELL 206 206L3 1182108 SW COCKPIT ATC INOP E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6161A 51611 TRANSCEIVER INOPERATIVE. INTERGRATION LIGHT WILL COME ON BUT IT IS NOT SENDING OUT SIGNAL. FOUND POWER OUT LOW, ADJUSTE D V101. NO HELP. REPLACED V101. REPAIRED. ALSO REPLACED BAD PHOTOCELL V301. REPAIRED. PLACED IT IN FREEZER, HEATED AND VIBRATED. BENCH CHECK GOOD. 1 G 7 1 3U H2SW 1996112100297 19961121 00297 SW 1996 11 21 HEEA968418 1 19961104 A 6320 206040531001 CASE ASSY 206040004107 BELL 206 206L1 1182107 SW XMSN WEB ARMS CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1078D 9882 BMC00541 45397 THREE EACH CRACK INDICATIONS IN WEB ARMS. REPLACED WITH SERVICEABLE PARTS. SEE MMIR # HEEA0008418 THROUGH #8421 FOR ADD ITIONAL PARTS REPLACED. 1 G 7 1 3U H2SW 1996112100298 19961121 00298 SW 1996 11 21 HEEA968419 1 19961104 A 6320 206040540003 SHAFT 206040004107 BELL 206 206L1 1182107 SW XMSN WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1078D BMC00541 45397 SHAFTWORN BEYOND LIMITS (SPLINES). REPLACED WITH SERVICEABLE PARTS. SEE MMIR # HEEA0008418 THROUGH #8421 FOR ADDITIONAL PARTS REPLACED. 1 G 7 1 3U H2SW 1996112100299 19961121 00299 SW 1996 11 21 HEEA968420 1 19961104 A 6320 206040662101 SUN GEAR 206040004107 BELL 206 206L1 1182107 SW XMSN WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1078D BMC00541 45397 SUN GEAR WORN BEYOND LIMITS (SPLINES). REPLACED WITH SERVICEABLE PARTS. SEE MMIR # HEEA0008418 THROUGH #8421 FOR ADDITI ONAL PARTS REPLACED. 1 G 7 1 3U H2SW 1996112100300 19961121 00300 SW 1996 11 21 HEEA968421 1 19961104 A 6320 206040129001 FILTER HOUSING 206040004107 BELL 206 206L1 1182107 SW XMSN PIN HOLE E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 1078D BMC00541 45397 PIN HOLE ON SIDE OF HOUSING. REPLACED WITH SERVICEABLE PARTS. SEE MMIR # HEEA0008418 THROUGH #8421 FOR ADDITIONAL PARTS REPLACED. 1 G 7 1 3U H2SW 1996112100301 19961121 00301 SW 1996 11 21 HEEA968422 1 19961104 A 5320 206033201249 ROOF PANEL BELL 206 206L1 1182107 SW RT FWD MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 3904L 45597 TRANSITION HITS IN SEVERAL AREAS - NO EDGE DISTANCE ON R/H FORWARD OUTER EDGE. AREAS WHERE TRANSITION HITS CABIN STRUCT URE DOES NOT ALLOW PANEL TO SIT FLAT ON BOX BEAM. 1 G 7 1 3U H2SW 1996112100302 19961121 00302 SW 1996 11 21 HEEA968423 1 19961104 A 5320 206033201249 ROOF PANEL BELL 206 206L1 1182107 SW RT AFT OUTB DAMAGED E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 3904L 45597 PANEL CORE CRUSHED AND TORN AS MARKED AROUND INSERTS ON UNDERSIDE OF PANEL. INSERTS AS MARKED ON TOP OF PANEL DO NOT L INE UP WITH ORIGINAL PANEL. INSERTS NOT BONDED. R/H AFT OUTBOARD AS MARKED CUT IN RADIUS. HOLE FOR PLUMB BOB FILLED W ITH ADHESIVE.INSERTS FILLED WITH ADHESIVE. 1 G 7 1 3U H2SW 1996112100303 19961121 00303 1996 11 21 HEEA968424 4 19961104 A 3444 066305401 INDICATOR KI250 BELL 206 206L3 1182108 SW COCKPIT CASE BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8589X 51487 CASE BROKEN AND LOOSE. REPLACED BEZEL, FRONT PLATE; INSTALLED MISSING SPACERS AND LOCKNUTS FOR BEZEL. 1 G 7 1 3U H2SW 1996112100304 19961121 00304 1996 11 21 HEEA968425 4 19961104 A 2312 064100900 TRANSCEIVER KTR905 BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893P 33012 AFTER ONE MINUTE OF OPERATION RADIO TRANSCEIVER QUITS. 1 G 7 2 4U H4SW 1996112100305 19961121 00305 1996 11 21 HEEA968426 4 19961104 A 3454 066400702 RECEIVER KNR632 BELL 412 412 1182202 SW COCKPIT INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893N 33010 RECEIVER INOPERATIVE. UNIT DRAWS EXCESSIVE CURRENT. 1 G 7 2 4U H4SW 1996112100307 19961121 00307 SW 1996 11 21 HEEA968428 1 19961104 A 2436 206075447007 VOLT REGULATOR BELL 206 206L3 1182108 SW DC SYS MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6251V 51404 REG WOULD NOT ADJUST UP OR DOWN. (26.5 VOLTS ALL THE TIME) 1 G 7 1 3U H2SW 1996112100308 19961121 00308 1996 11 21 HEEA968429 4 19961104 A 3455 066104701 RECEIVER SKRSKY S76 S76A 8143006 NE COCKPIT ADF FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31217 760229 ADF NEEDLES STUCK ON PILOT & COPILOT SIDES AND "ANT" MODE VERY WEAK. 1 G 7 2 3U H1NE 1996112100309 19961121 00309 1996 11 21 HEEA968430 4 19961104 A 3455 066104701 RECEIVER BELL 412 412 1182202 SW COCKPIT ADF DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3911L 33023 ADF NEEDLE POINTS 30 DEGREES OR MORE OFF FROM WHERE IT SHOULD. 1 G 7 2 4U H4SW 1996112100310 19961121 00310 1996 11 21 HEEA968431 4 19961104 A 3454 066400700 RECEIVER BELL 412 412 1182202 SW COCKPIT NAV INOP E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893S 33022 VOR/LOC RECEIVER INOPERATIVE. 1 G 7 2 4U H4SW 1996112100312 19961121 00312 1996 11 21 HEEA968433 4 19961104 A 3442 MI5853013 INDICATOR P500 BELL 230 230 1182149 SW COCKPIT MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 236X 23015 "SEC" SCAN SWITCH INTERMITTENT, NOT SWITCHING AT ALL AT TIMES. TIME SINCE REPAIR 0:00. 1 G 7 2 3U NC H9SW 1996112100313 19961121 00313 EU 1996 11 21 HEEA968434 1 19961104 A 6210 10515150 BLADE BOLKMS 105 BO105S 5626006 EU NOSE SHELL CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3520T 6522 S539 BLADE HAS NOSE AND NECK SHELL CRACKED AND SEPARATED. INBOARD LEADING STRIP SEPARATED BEYOND LIMITS. 1 G 7 2 3U H3EU 1996112100314 19961121 00314 EU 1996 11 21 HEEA968435 1 19961106 A 6210 10515150 BLADE BOLKMS 105 BO105S 5626006 EU NOSE SHELL CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3520T 6522 S539 BLADE HAS NOSE AND NECK SHELLS CRACKED WITH SEPARATION. SUSPECTED CRACKED FILLER NEAR MOLD LINE ON LOWER SURFACE. 1 G 7 2 3U H3EU 1996112100315 19961121 00315 EU 1996 11 21 HEEA968436 1 19961106 A 6210 10515150 BLADE BOLKMS 105 BO105S 5626006 EU NOSE SHELL CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3520T 6522 S539 BLADE NOSE AND NECK SHELL CRACKED AND SEPARATED. 1 G 7 2 3U H3EU 1996112100316 19961121 00316 EU 1996 11 21 HEEA968437 1 19961106 A 6210 10515150 BLADE BOLKMS 105 BO105S 5626006 EU NOSE SHELL CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3520T 6522 S539 BLADE NOSE & NECK SHELL CRACKED AND SEPARATED. 1 G 7 2 3U H3EU 1996112100317 19961121 00317 SW 1996 11 21 HEEA968438 1 19961106 A 3213 AB205050403031 CROSSTUBE BELL 412 412 1182202 SW MOUNT PADS CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 CROSSTUBE FRETTING CORROSION UNDER MOUNT PADS WHERE NO DAMAGE IS ALLOWED. SCRIBE MARKS AROUND MOUNT PADS. 1 G 7 2 4U H4SW 1996112100318 19961121 00318 1996 11 21 HEEA968439 4 19961106 A 2312 064101900 TRANSCEIVER BOLKMS 105 BO105S 5626006 EU COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 624MB S751 LED LIGHTS WORK INTERMITTENTLY. 1 G 7 2 3U H3EU 1996112100319 19961121 00319 SW 1996 11 21 HEEA968440 1 19961106 A 7722 206375007103 INDICATOR BELL 206 206L3 1182108 SW COCKPIT TOT STICKS E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 6610C 51425 INDICATOR NEEDLE STICKS AT FIRST START OF DAY. 1 G 7 1 3U H2SW 1996112100320 19961121 00320 SW 1996 11 21 HEEA968441 1 19961106 A 7722 206375007103 INDICATOR BELL 206 206L3 1182108 SW COCKPIT TOT STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 108PH 51334 INDICATOR NEEDLE STICKS ON FIRST START OF DAY. 1 G 7 1 3U H2SW 1996112100321 19961121 00321 1996 11 21 HEEA968442 4 19961106 A 3442 MI5853011 INDICATOR P500 SKRSKY S76 S76A 8143006 NE COCKPIT MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 278X 760440 RADAR DISPLAY BLURRY AND GLITCHES AFTER WARM UP. 1 G 7 2 3U H1NE 1996112100322 19961121 00322 1996 11 21 HEEA968443 4 19961106 A 3442 MI5853011 INDICATOR P500 SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 278X 760440 RADAR INTERMITTENTLY IN CYCLE MODE ALL THE TIME, REGARDLESS OF MODE SELECTED. 1 G 7 2 3U H1NE 1996112100323 19961121 00323 NE 1996 11 21 HEEA968444 1 19961106 A 6210 7615009000046A BLADE SKRSKY S76 S76A 8143006 NE TIP RIB SEPARATION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545X 11893 760050 SEPARATION IN THE SKIN NEAR THE TIP RIB AREA WITH CRACKS IN THE SKIN JUST BELOW THE SPAR ON THE LOWER SIDE. 1 G 7 2 3U H1NE 1996112100324 19961121 00324 NE 1996 11 21 HEEA968445 1 19961106 A 6210 7615009100041 BLADE SKRSKY S76 S76A 8143006 NE TIP RIB CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31217 9656 760229 TIP RIB CRACKED. THE NICKEL STRIP HAS SEVERAL AREAS OF SEPARATION. 1 G 7 2 3U H1NE 1996112100325 19961121 00325 1996 11 21 HEEA968446 4 19961106 A 3455 066104701 RECEIVER BELL 212 212 1181420 SW COCKPIT ADF FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 102PH 30899 RECEIVER WILL NOT RECEIVE STATIONS. 1 G 7 1 4U H4SW 1996112100326 19961121 00326 1996 11 21 HEEA968447 4 19961106 A 3455 066104701 RECEIVER BELL 412 412 1182202 SW COCKPIT ADF DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3893P 33012 STATIC ON LOW WATT STATIONS AND RECEIVER SCRATCHY. 1 G 7 2 4U H4SW 1996112100327 19961121 00327 1996 11 21 HEEA968448 4 19961106 A 2210 7000299901 CONTROL BELL 412 412 1182202 SW COCKPIT AP DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22347 36005 ATT. LIGHT INOPERATIVE ONLY WHEN #2 HP IS ENGAGED. TIME SINCE REPAIR 701:20. 1 G 7 2 4U H4SW 1996112100328 19961121 00328 1996 11 21 HEEA968449 4 19961106 A 3442 MI5852013 INDICATOR P4001 SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 792CH 760193 BROKEN PICTURE, CONSTANT FLUCTUATION AND WARNING ROW INOPERATIVE. SMELLS BURNT; NO DISPLAY. 1 G 7 2 3U H1NE 1996112100329 19961121 00329 1996 11 21 HEEA968450 4 19961106 A 3455 066104701 RECEIVER SKRSKY S76 S76A 8143006 NE COCKPIT INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 4253S 760035 ADF INOPERATIVE, NO RECEPTION, NO POINTING TO STATIONS. 1 G 7 2 3U H1NE 1996112100330 19961121 00330 1996 11 21 HEEA968451 4 19961106 A 3431 066401018 RNAV BELL 214 214ST 1182106 SW COCKPIT MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5748M 28102 GS NEEDLE DEFLECTS UP. WITH ONLY VOR SIGNAL APPLIED. 2 G 7 2 4U H10SW 1996112100331 19961121 00331 1996 11 21 HEEA968452 4 19961106 A 3425 1113025 INDICATOR BELL 212 212 1181420 SW COCKPIT HSI DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1079U 31122 HSI INDICATOR COURSE SELECT KNOB HARD TO TURN. TIME SINCE REPAIR 237:35. 1 G 7 1 4U H4SW 1996112100332 19961121 00332 SW 1996 11 21 HEEA968453 1 19961106 A 7722 35712519127 INDICATOR BELL 206 206B 1181511 SW COCKPIT TOT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2278V 3632 NEEDLE HAS STICKY OPERATION THROUGH 500 DEGRES. 1 G 7 1 3U H2SW 1996112100333 19961121 00333 SW 1996 11 21 HEEA968454 1 19961106 A 7722 206375007103 INDICATOR BELL 206 206L1 1182107 SW COCKPIT TOT STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2135V 45657 NEEDLE STICKS AT FIRST START OF DAY. TIME SINCE REPAIR 85:25. 1 G 7 1 3U H2SW 1996112100334 19961121 00334 SW 1996 11 21 HEEA968455 1 19961106 A 7722 206375006101 INDICATOR BELL 206 206L1 1182107 SW COCKPIT TOT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 10814 45415 NEEDLE HAS STICKY OPERATION. 1 G 7 1 3U H2SW 1996112100335 19961121 00335 EU 1996 11 21 HEEA968456 1 19961106 A 7160 350A54108004 INTAKE AIR SNIAS 350 AS350B2 8680813 EU ENGINE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 3737 2771 ENGINE AIR INTAKE CRACKED. 1 G 7 1 3U H9EU 1996112100336 19961121 00336 EU 1996 11 21 HEEA968457 1 19961106 A 3213 1055000134 SKID SHOE BOLKMS 105 BO105S 5626006 EU MLG WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7170D S840 SKID PROTECTIVE PLATES WORN THROUGH HARDENED METAL TO AND THROUGH BASE METAL. REPLACED WITH SERVICEABLE SKID PROTECTIVE PLATES. 1 G 7 2 3U H3EU 1996112100337 19961121 00337 EU 1996 11 21 HEEA968458 1 19961106 A 2435 150SG122Q GENERATOR SNIAS 350 AS350B2 8680813 EU START/GEN FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6095S 433 2777 START/GENERATOR NO STARTS AND NO GEN. 1 G 7 1 3U H9EU 1996112100338 19961121 00338 EU 1996 11 21 HEEA968459 1 19961106 A 7923 209072433101 VALVE BOLKMS 105 BO105S 5626006 EU OIL SOV DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 9190Y S669 INTERMITTENT OPERATION. INSPECTED BY ACCESSORY OVERHAUL SHOP AND FOUND VALVE TO BE INOPERATIVE. 1 G 7 2 3U H3EU 1996112100339 19961121 00339 SW 1996 11 21 HEEA968460 1 19961106 A 2436 206075447007 VOLT REGULATOR BELL 206 206L1 1182107 SW DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2135V 45657 WHEN INSTALLED ON AIRCRAFT, VOLTAGE REGULATOR WOULD NOT FUNCTION. TIME SINCE REPAIR 0:00. 1 G 7 1 3U H2SW 1996112100340 19961121 00340 SW 1996 11 21 HEEA968461 1 19961106 A 2436 206075447007 VOLT REGULATOR BELL 206 206L1 1182107 SW DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2135V 45657 WHEN INSTALLED ON AIRCRAFT, VOLTAGE REGULATOR WOULD NOT FUNCTION. 1 G 7 1 3U H2SW 1996112100341 19961121 00341 1996 11 21 HEEA968462 4 19961106 A 3442 MI5852013 INDICATOR P4001 SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 760035 BAD MEMORY BOARD, AND R132 HIGH VOLTAGE POT. BROKEN ON VIDEO BOARD. 1 G 7 2 3U H1NE 1996112100342 19961121 00342 NE 1996 11 21 HEEA968463 1 19961106 A 6210 7615009043050 TIP CAP SKRSKY S76 S76A 8143006 NE MR BLADE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545X 760050 TIP CAP HAS ABRASION STRIP CRACKED WITH SEPARATION. FIBERGLASS BROKEN BETWEEN THE DOUBLER ON THE UPPER SURFACE. 1 G 7 2 3U H1NE 1996112100343 19961121 00343 NE 1996 11 21 HEEA968465 1 19961106 A 6210 7615009100051 BLADE SKRSKY S76 S76A 8143006 NE M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545K 8458 760047 BLADE TRIM TAB CRACKED ON THE LOWER SURFACE. 1 G 7 2 3U H1NE 1996112100344 19961121 00344 EU 1996 11 21 HEEA968466 1 19961106 A 6210 10515150 BLADE BOLKMS 105 BO105S 5626006 EU NOSE SHELL CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81832 3847 S828 NOSE AND NECK SHELLS CRACKED AND SEPARATED. 1 G 7 2 3U H3EU 1996112100345 19961121 00345 SW 1996 11 21 HEEA968467 1 19961106 A 6210 212015501115 BLADE BELL 212 212 1181420 SW M/R DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5736J 9 31140 TOO LIGHT TO BALANCE. BLADE BOLT HOLE WAS MAX. OUT, STILL WITH NO SUCCESS. 1 G 7 1 4U H4SW 1996112100346 19961121 00346 1996 11 21 HEEA968468 4 19961106 A 2312 071121525 CONTROL UNIT BOLKMS 105 BO105S 5626006 EU COCKPIT SHAFT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 54191 S804 SELECTOR CONTROL KNOB AND SHAFT PULLED OUT OF CONTROL. PERFORMED PRELIMINARY INSPECTION, FOUND RETAINING RING MISSING. I NSTALLED NEW RETAINING RING P/N 090-0036-04. REPAIRED. BENCH CHECK GOOD. 1 G 7 2 3U H3EU 1996112100347 19961121 00347 1996 11 21 HEEA968469 4 19961106 A 3452 066106200 TRANSCEIVER KT76 SNIAS 350 AS350B2 8680813 EU COCKPIT ATC INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100U 2863 TRANSCEIVER INOPERATIVE. FOUND V101 CAVITY DRAWING EXCESSIVE CURRENT. REPLACED V101 CAVITY OSCILLATOR. ALSO REPLACED R M401 AND RM402 RESISTOR CAPACITOR NETWORKS TO COMPLY WITH MOD 7 AND INSTALLED HEAT SINK ON Q415 TRANSISTOR TO COMPLY WIT H MOD 6. INSPECTED AND BENCH CHECKGOOD. 1 G 7 1 3U H9EU 1996112100348 19961121 00348 1996 11 21 HEEA968470 4 19961106 A 2312 071121570 CONTROL BOLKMS 105 BO105S 5626006 EU COCKPIT COMM 2 DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4302G S853 FREQUENCY LIGHT STAYS ON DIM. PERFORMED PRELIMINARY INSPECTION, TROUBLESHOT AND REPLACED V101 PHOTOCELL, REPAIRED. BENC H CHECK GOOD. 1 G 7 2 3U H3EU 1996112100349 19961121 00349 1996 11 21 HEEA968471 4 19961106 A 3452 066106200 TRANSCEIVER KT76 BELL 206 206B 1181511 SW COCKPIT ATC DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2145C 3456 WHEN FIRST DIGIT IS SELECTED AS "6" SOMETIMES "5" AND SOMETIMES "7" ARE TRANSMITTED INSTEAD. CLEANED CONTACTS AND WAFERS , REPAIRED, ALSO REPLACED V301 PHOTOCELL AND DETERIORATED R477 RESISTOR AND FOUND FREQUENCY AND POWER WOULD NOT ADJUST T O SPECS. REPLACED V101 OSCILLATOR. REPAIRED. BENCH CHECK GOOD. 1 G 7 1 3U H2SW 1996112100350 19961121 00350 GL 1996 11 21 HEEA968472 2 19961113 A 7250 6899170 FRONT SUPPORT 23033191 BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL ENG TURB DEFECTIVE E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 5737T CAC70437 45454 CAE860520 RECEIVING INSPECTION REVEALED: DEPTH BELOW SPECS ON FRONT SUPPORT FORWARD #1 BEARING HOUSING BORE. ALSO REMOVED SPUR A DAPTER GEARSHAFT DUE TO METAL DEPOSIT ON ONE SPUR ADAPTER GEARSHAFT GEARTOOTH. INSTALLED A NEW FRONT SUPPORT AND NEW SPU R ADAPTER GEARSHAFT. SUBMITTAL FOR CREDIT AND SHIPPING ACCOMPLISHED ON AFA#29333A. SEE MMIR# HEEA0008473 FOR SPUR ADAP TER GEARSHAFT INFORMATION. 1 G 7 1 3U 3 U H2SW E1GL 1996112100351 19961121 00351 GL 1996 11 21 HEEA968473 2 19961113 A 7250 23056634 GEARSHAFT 23033191 BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL SPUR ADAPTER DEFECTIVE E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 5737T CAC70437 45454 CAE860520 RECEIVING INSPECTION REVEALED: METAL DEPOSIT ON ONE SPUR ADAPTER GEARSHAFT GEARTOOTH. ALSO REMOVED FRONT SUPPORT DUE TO DEPTH BELOW SPECS ON FRONT SUPPORT FORWARD #1 BEARING HOUSING BORE. INSTALLED A NEW FRONT SUPPORT AND NEW SPUR ADAPT ER GEARSHAFT. SUBMITTAL FOR CREDIT AND SHIPPING ACCOMPLISHED ON AFA#29333A. SEE MMIR# HEEA0008472 FOR FRONT SUPPORT I NFORMATION. 1 G 7 1 3U 3 U H2SW E1GL 1996112100353 19961121 00353 GL 1996 11 21 HEEA968475 2 19961113 A 7260 6876925 TUBE ASSY. 6894171 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL GEARBOX OUT OF SPEC E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 967MB 4212 CAG38539 S737 CAE835716 ENGINE REMOVED DUE TO AFT T/M LEAKS. UPON INSPECTION OF GEARBOX PARTS NOTED THE FOLLOWING: TUBE FAILED DIMENSIONAL CHE CK PER CEB 1307. INSTALLED NEW TUBE. 1 G 7 2 3U 3 U H3EU E4CE 1996112100354 19961121 00354 GL 1996 11 21 HEEA968476 2 19961113 A 7260 6876925 TUBE ASSY. 6894171 BELL 206 206B3 1181506 SW ALLSN 250C 250C20B 03013 GL GEARBOX OUT OF SPEC E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2268A CAG34494 3602 CAE830384 ENGINE REMOVED DUE TO MAKING METAL. UPON INSPECTION OF GEARBOX PARTS NOTED THE FOLLOWING: TUBE FAILED DIMENSIONAL CHEC K PER CEB 1307. INSTALLED NEW TUBE. 1 G 7 1 3U 3 U H2SW E4CE 1996112100355 19961121 00355 GL 1996 11 21 HEEA968477 2 19961113 A 7210 6898977 COUPLING 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENGINE FAILED INSP E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 9190Y 116 CAT33140 S669 CAE834012 TURBINE REMOVED DUE TO 1750 HOUR INSPECTION DUE. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: FAILED NO-GO GU AGE INSPECTION ON N1 COUPLING INTERNAL SPLINES. INSTALLED NEW PART. 1 G 7 2 3U 3 U H3EU E4CE 1996112100356 19961121 00356 GL 1996 11 21 HEEA968478 2 19961113 A 7230 23056634 GEARSHAFT 23033193 BELL 206 206L1 1182107 SW ALLSN 250C 250C30P 03013 GL ENG COMP DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1076Y 988 CAC90513 45380 CAE895023 ENGINE REMOVED DUE TO IMPELLER RETIREMENT. UPON INSPECTION OF COMPRESSOR PARTS NOTED THE FOLLOWING: FAILED GO,NO-GO GU AGE INSPECTION ON SPUR ADAPTER GEARSHAFT FORWARD AND AFT SPLINES. INSTALLED NEW PART. 1 G 7 1 3U 3 U H2SW E1GL 1996112100357 19961121 00357 GL 1996 11 21 HEEA968479 2 19961113 A 7230 23056634 GEARSHAFT 23033191 BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL SPUR ADAPTER WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2125M 865 CAC70540 45649 CAE860085 ENGINE REMOVED DUE TO LOW POWER. UPON INSPECTION OF COMPRESSOR PARTS NOTED THE FOLLOWING: FAILED GO,NO-GO GUAGE INSPEC TION ON SPUR ADAPTER GEARSHAFT AFT SPLINES. INSTALLED NEW PART. 1 G 7 1 3U 3 U H2SW E1GL 1996112100358 19961121 00358 GL 1996 11 21 HEEA968480 2 19961113 A 7250 6886407 WHEEL 6898735 BELL 206 206B3 1181506 SW ALLSN 250C 250C20B 03013 GL 1ST STAGE DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 104PH 1715 CAT25180 3622 CAE270042 TURBINE REMOVED DUE TO 1750 HOUR INSPECTION. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: MINOR SULFIDATION O N ALL 1ST STAGE WHEEL BLADES. SCRAPPED 1ST STAGE WHEEL. 1 G 7 1 3U 3 U H2SW E4CE 1996112100359 19961121 00359 SW 1996 11 21 MALA965152 1 19960927 A 5712 RIB SWRNGN SA227 SA227AC 8780603 SW WS 27.103 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 26863 AC650B DURING SCHEDULED MAINTENANCE IN MSP, MECHANICS FOUND RIGHT INBOARD FLAP END COVE RIB AT WS 27.103 CRACKED IN BEND AT UPP ER AFT CORNER ABOVE FLAP POT MOUNT. COMPLETED REPAIR BY INSTALLING A DOUBLER IAW AERO TECH DESIGNS EO 01-96097 DATED SE PT 27, 1996. (M) 2 L 7 2 4T RT A8SW 1996112100360 19961121 00360 NM 1996 11 21 MALA965165 1 19961012 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN LOOSE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 822MA 326 FLT 3319 - DURING THE PREFLIGHT INSPECTION, THE FLIGHT ATTENDANT FOUND TWO FLOOR TRACK LIGHTS TO BE INOPERATIVE. MAINTE NANCE RESECURED A PIN INTO A CONNON PLUG TO THE RIGHT FORWARD EMERGENCY BATTERY PACK CONTROL HEAD. OPS CHECK IS SATISFA CTORY. (M) 2 H 7 2 4T RT A13NM 1996112100361 19961121 00361 SW 1996 11 21 MALA965162 1 19961005 A 5753 SKIN SWRNGN SA227 SA227AC 8780603 SW LT TE FLAP CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 446MA AC693 DURING AN INSPECTION IN MSP, MAINTENANCE FOUND A CHAFF IN THE LEFT FLAP INBOARD TRAILING EDGE. REPAIRS WERE COMPLETED I AW FAC STRUCTURAL REPAIR MANUAL 57-90-60 PAGES 3-6. (M) 2 L 7 2 4T RT A8SW 1996112100362 19961121 00362 1996 11 21 RAIA961022 4 19961018 A 3425 7003360944 AHRS COMPUTER AEROSP ATR42 ATR42300 8680920 EU NR 2 FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 421TE 12370 102 STL - FLT 7152 - NR 2 AHRS FAILED. MAINTENANCE REPLACED THE NR 2 AHRS COMPUTER. (M) 2 H 7 2 4T RT A53EU 1996112100363 19961121 00363 EU 1996 11 21 RAIA961021 1 19961018 A 2913 POV304426 HYDRAULIC PUMP BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 866AE 11548 11548 866 FAT - FLT 4750 - LEFT HYDRAULIC PUMP PRESSURE DROPS TO ZERO. MAINTENANCE REPLACED THE LEFT HYDRAULIC PUMP. (M) 2 L 7 2 4T RT A56EU 1996112100364 19961121 00364 WP 1996 11 21 RAIA961019 2 19961015 A 7530 896115 GASKET BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP NR 2 ENGINE LEAKING A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK J R WARNING INDICATION PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CE 03 342TE 1213 954 66178 STL - FLT 7050 - NR 2 ENGINE WOULD NOT PRODUCE REQUIRED TORQUE. REPLACED ENGINE BLEED AIR GASKETS. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996112100365 19961121 00365 EU 1996 11 21 RAIA961018 1 19961015 A 3230 7445B RELIEF VALVE JETAIR JETSTM JETSTM4101 1500501 EU LANDING GEAR TRIPPED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 568HK 1106 41086 DCA - FLT 7742 - LANDING GEAR WOULD NOT RETRACT. RESET GEAR PRESSURE RELIEF VALVE. (M) 2 L 7 2 4T RT A41NM 1996112100366 19961121 00366 WP 1996 11 21 RAIA961017 2 19961012 A 7321 89778025 FUEL CONTROL BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP NR 2 ENGINE FAILED A A RAIA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 CE 03 422AM 6975 856 66176 PAH - FLT 7365 - NR 2 ENGINE TORQUE FLUCTUATES. REMOVED AND REPLACED FUEL CONTROL. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996112100367 19961121 00367 1996 11 21 RAIA961016 4 19961012 A 3416 066306202 ALTIMETER BAG JETSTM JETSTM3201 1500217 EU NR 1 FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 426AM 6900 874 STL - FLT 7086 - SPLIT IN ALTIMETERS. REMOVED AND REPLACED NR 1 ALTIMETER. (M) 2 L 7 2 4T RT A56EU 1996112100368 19961121 00368 EU 1996 11 21 RAIA961015 1 19961010 A 7931 41SG107150G14 TRANSMITTER BAG JETSTM JETSTM3201 1500217 EU NR 1 ENGINE FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 337TE 1211 929 AFTER TAKEOFF NR 1 OIL PRESSURE INCREASED TO 120 PSI. REPLACED OIL PRESSURE TRANSMITTER. (M) 2 L 7 2 4T RT A56EU 1996112100369 19961121 00369 EU 1996 11 21 RAIA961012 1 19961008 A 7712 31024766 TQ SIGNAL COND BAG JETSTM JETSTM3201 1500217 EU RT ENGINE OUT OF ADJUST A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CE 03 859AE 11941 11941 859 MRY - FLT 4760 - RIGHT ENGINE WOULD NOT PRODUCE TARGET TORQUE. MAINTENANCE ADJUSTED THE TORQUE SIGNAL CONDITIONER. (M) 2 L 7 2 4T RT A56EU 1996112100370 19961121 00370 NE 1996 11 21 RAIA961020 2 19961016 A 7532 E0195FK1814CN CONNECTOR AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE RT ENGINE CONTAMINATED A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 425TE 17460 125 STL - FLT 7398 - NR 2 BLEED FAULTED, AND WOULD NOT RESET. MAINTENANCE CLEANED OIL FROM THE NR 2 ENGINE BLEED VALVE CANN ON PLUG. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1996112100371 19961121 00371 EU 1996 11 21 RAIA961005 1 19961006 A 5270 SP4954 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGGAGE DOOR OUT OF ADJUST A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 557HK 1578 41074 ORF - FLT 7786 - MAIN BAGGAGE BAY DOOR LIGHT ILLUMINATED DURING TAKEOFF. LIGHT EXTINGUISHED ON TAXI BACK TO GATE. MAIN TENANCE ADJUSTED THE FORWARD MICROSWITCH. (M) 2 L 7 2 4T RT A41NM 1996112100372 19961121 00372 EU 1996 11 21 RAIA961025 1 19961022 A 2435 NSA8203113 O-RING AEROSP ATR42 ATR42300 8680920 EU RT ENGINE LEAKING A RAIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 03 EICBK 199 PIA - FLT 7541 - RIGHT ENGINE OIL PSI LOW WARNING ILLUMINATED, AND GAUGE INDICATED LOW OIL PRESSURE. MAINTENANCE REPLAC ED THE STARTER/GENERATOR SHAFT O-RING. (M) 2 H 7 2 4T RT A53EU 1996112100373 19961121 00373 EU 1996 11 21 RAIA961026 1 19961025 A 5330 SPECL156T4040 SKIN BAG JETSTM JETSTM3201 1500217 EU BS 148-114R PUNCTURED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 337TE 929 REPAIRED PUNCTURE IN FUSELAGE SKIN ON RIGHT SIDE AT STATION 148 AT STRINGER 114R. REPAIR PERFORMED IAW SRM 51-50-21. ( M) 2 L 7 2 4T RT A56EU 1996112100374 19961121 00374 EU 1996 11 21 RAIA961040 1 19961030 A 5313 NTA46356 STRINGER AEROSP ATR72 ATR72202 8680940 EU FRAME 24-25 CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 723TE 9615 283 STL - CORROSION ON STRINGER 21L AND 21R BETWEEN FRAMES 24 AND 25. MAINTENANCE REPLACED STRINGER 21L AND 21R. (M) 2 H 7 2 4T RT A53EU 1996112100375 19961121 00375 EU 1996 11 21 RAIA961039 1 19961030 A 5315 S53672407252 FLOOR BEAM AEROSP ATR72 ATR72202 8680940 EU FRAME 33 CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 723TE 9615 283 STL - CORROSION ON FLOOR BEAM AT FRAME 33. MAINTENANCE REPLACED THE FLOOR BEAM AT FRAME 33. (M) 2 H 7 2 4T RT A53EU 1996112100376 19961121 00376 EU 1996 11 21 RAIA961038 1 19961030 A 5320 S00030121100000 DEPRESSOR AEROSP ATR72 ATR72202 8680940 EU SERV DOOR CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 723TE 9615 283 STL - CORROSION AT SERVICE DOOR SEAL DEPRESSOR. MAINTENANCE REPLACED THE SERVICE DOOR SEAL DEPRESSOR. (M) 2 H 7 2 4T RT A53EU 1996112100377 19961121 00377 EU 1996 11 21 RAIA961036 1 19961030 A 5347 S53678001225 SEAT TRACK AEROSP ATR72 ATR72202 8680940 EU CABIN CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 723TE 9615 283 STL - CORROSION ON RIGHT OUTBOARD SEAT TRACK AT GALLEY ATTACH POINTS. MAINTENANCE REPLACED THE RIGHT OUTBOARD SEAT TRAC K. (M) 2 H 7 2 4T RT A53EU 1996112100378 19961121 00378 EU 1996 11 21 RAIA961035 1 19961030 A 5320 S53672408228 DOUBLER AEROSP ATR72 ATR72202 8680940 EU FRAME 39 CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 723TE 9615 283 STL - FOUND CORROSION ON DOUBLER AT FRAME 39. MAINTENANCE REPLACED DOUBLER ON FRAME 39. (M) 2 H 7 2 4T RT A53EU 1996112100379 19961121 00379 EU 1996 11 21 RAIA961034 1 19961030 A 5315 S536712572040270 FLOOR BEAM AEROSP ATR72 ATR72202 8680940 EU FRAME 36-39 CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 723TE 9615 283 STL - FOUND CORROSION AT SERVICE DOOR TORQUE BOX BEAMS BETWEEN FRAMES 36 AND 39. MAINTENANCE REPLACED FLOOR BEAM BETWEE N FRAMES 36-39. (M) 2 H 7 2 4T RT A53EU 1996112100380 19961121 00380 EU 1996 11 21 RAIA961033 1 19961030 A 5210 S536770206200 SKIN AEROSP ATR72 ATR72202 8680940 EU PAX DOOR CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 723TE 9615 283 STL - FOUND CORROSION ON PASSENGER DOOR TORQUE BOX SKIN. MAINTENANCE REPLACED THE PAX DOOR TORQUE BOX SKIN. (M) 2 H 7 2 4T RT A53EU 1996112100381 19961121 00381 EU 1996 11 21 RAIA961032 1 19961030 A 5240 S536720206200 SKIN AEROSP ATR72 ATR72202 8680940 EU SERV DOOR CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 723TE 283 STL - FOUND CORROSION ON SERVICE DOOR TORQUE BOX SKIN. MAINTENANCE REPLACED THE TORQUE BOX SKIN AT SERVICE DOOR. (M) 2 H 7 2 4T RT A53EU 1996112100382 19961121 00382 EU 1996 11 21 RAIA961031 1 19961030 A 5320 S53671257209 INTERCOSTAL AEROSP ATR72 ATR72202 8680940 EU FRAME 35-40 CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 723TE 9615 283 STL - FOUND CORROSION ON INTERCOSTAL ON STRINGER 17R. MAINTENANCE REPLACED INTERCOSTAL ON STRINGER 17R. (M) 2 H 7 2 4T RT A53EU 1996112100383 19961121 00383 EU 1996 11 21 RAIA961030 1 19961030 A 5315 S53672406200 FLOOR BEAM AEROSP ATR72 ATR72202 8680940 EU FRAME 36-39 CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 723TE 9615 283 STL - FLOOR BEAM FROM FRAME 36 TO FRAME 39 HAS CORROSION. MAINTENANCE REPLACED THE FLOOR BEAM FROM FRAME 36 TO 39. (M) 2 H 7 2 4T RT A53EU 1996112100384 19961121 00384 WP 1996 11 21 RAIA961024 2 19961022 A 7320 8974575 BYPASS VALVE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT ENGINE STICKING A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 03 342TE 10298 10298 954 P66079 STL - FLT 7050 - LEFT ENGINE ON TAKEOFF ROLL DROPPED TO 80 PERCENT TORQUE. MAINTENANCE REPLACED THE LEFT ENGINE BYPASS VALVE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996112100385 19961121 00385 EU 1996 11 21 VTZA97044 1 19961028 A 7997 WIRE JETAIR JETSTM JETSTM4101 1500501 EU RT OIL COOLER BROKEN A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 321UE 41045 FLT 6477 - IAD - CHS - DURING CLIMB, EXPERIENCED A FAILURE OF THE RIGHT OIL COOLER FLAP NO CLOSING. AIRCRAFT RETURNED T O IAD AND THE GATE. MAINTENANCE INSPECTED THE AIRCRAFT DISCREPANCY AND FOUND THAT A WIRE HAD BROKEN AT THE FLAP COOLER ACTUATOR. MAINTENANCE REPAIRED THE BROKEN WIRE AND PERFORMED A FUNCTIONAL CHECK OF THE SYSTEM. AIRCRAFT WAS THEN RELEA SED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996112100386 19961121 00386 EU 1996 11 21 VTZA97045 1 19961029 A 3260 ATG135022 UPLOCK SWITCH JETAIR JETSTM JETSTM4101 1500501 EU RT MLG FAILED A VTZA A D UNSCHED LANDING RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 EA 27 316UE 41055 PIT-IAD - FLT 6329 - DURING CLIMB THE CREW EXPERIENCED A RED GEAR HANDLE ILLUMINATION THAT WOULD NOT EXINGUISH. ALL INT RANSIT AND DOWNLOCK INDICATIONS WERE NORMAL. THE AIRCRAFT RETURNED TO PIT. MAINTENANCE CONTROL WAS NOTIFIED AND ASSIST ED IN THE TROUBLESHOOTING OF THE DISCREPANCY. THE AIRCRAFT WAS FERRIED TO IAD WHERE THE MAINTENANCE PERSONNEL FOUND THA T THE RIGHT MAIN LANDING GEAR STANDBY UPLOCK MICROSWITCH HAD FAILED. THE MICROSWITCH WAS REPLACED AND ALL REQUIRED CHEC KS WERE ACCOMPLISHED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1996112100387 19961121 00387 EU 1996 11 21 VTZA97043 1 19961027 A 2150 1718D000 ACM JETAIR JETSTM JETSTM4101 1500501 EU LEFT MALFUNCTIONED A VTZA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 27 303UE 41015 FLT 6506 - IAD-BOS - DURING TAXI OUT, AIRCRAFT EXPERIENCED A DUCT OVERTEMP LIGHT ILLUMINATION. AIRCRAFT RETUREND TO THE GATE WHERE MAINTENANCE TROUBLESHOT THE DISCREPANCY AND FOUND THAT THE ACM HAD BECOME STUCK. MAINTENANCE FREED THE ACM AND RETURNED AND RELEASED THE AIRCRAFT FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1996112100388 19961121 00388 EU 1996 11 21 VTZA97042 1 19961025 A 3240 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU PARKING BRAKE OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 436JX 41036 FLT 6418 - IAD-BOS - TAKEOFF ABORTED DUE TO TAKEOFF CONFIGURATION WARNING INDICATION. AIRCRAFT RETURNED TO THE GATE WHE RE MAINTENANCE FOUND THE PARKING BRAKE SYSTEM WAS AT FAULT. MAINTENANCE ADJUSTED THE PARKING BRAKE MICROSWITCH. AIRCRA FT SYSTEM WAS THEN OPERATIONALL CHECKED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1996112100389 19961121 00389 EU 1996 11 21 VTZA97040 1 19961024 A 2435 23079009 STARTER GEN BAG JETSTM JETSTM3201 1500217 EU RIGHT LOOSE WIRE A VTZA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 27 486UE 905 FLT 6448 - HVN - IAD - DURING TAXI, RIGHT STARTER GENERATOR FAILED. AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE INS PECTED STARTER GENERATOR AND COULD NOT DUPLICATE. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. UPON TAXII NG OUT AGAIN, US AIR PILOT SAW SMOKE COMING FROM STARTER/GEN VENT. AIRCRAFT TAXIIED BACK TO GATE WHERE MAINTENANCE INSP ECTED AND FOUND LOOSE WIRE. MAINTENANCE REMOVED AND REPLACD STARTER GENERATOR, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996112100390 19961121 00390 EU 1996 11 21 VTZA97041 1 19961024 A 7603 CONDITION LEVER JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT LOOSE A VTZA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 27 319UE 41042 FLT 6276 - IAD-EWR - ABORTED TAKEOFF DUE TO TAKEOFF CONFIGURATION WARNING ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH N O FURTHER PROBLEMS. MAINTENANCE INSPECTED SYSTEM AND FOUND CONDITION LEVER FRICTION LOCK LOOSE AND TIGHTEN, OPS CHECK O K. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996112100391 19961121 00391 EU 1996 11 21 VTZA97039 1 19961023 A 2722 4006719904 SERVO JETAIR JETSTM JETSTM4101 1500501 EU RUDDER FAILED A VTZA K NONE F FLT CONT AFFECTED AP APPROACH 1 EA 27 436JX 41036 FLT 6559 - IAD- ORF - DURING APPROACH, MADE AN UNSCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS GRINDING NOISE FROM RU DDER CONTROLS. AIRCRAFT LANDED AT ORF WITH NO FURTHER INCIDENTS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED RUDDER SERVO, OP CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1996112100392 19961121 00392 EU 1996 11 21 VTZA97038 1 19961022 A 3260 AIR132254 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU RT MLG FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 313UE 41026 FLT 6369 - RDU-IAD - DURING CLIMB MADE AN UNSCHEDULED LANDING DUE TO RIGHT MAIN GEAR INTRANSIT LIGHT REMAINED ILLUMINATE D AFTER GEAR RETRACTED. AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED MICRO SWITCH. OPS CHECK OK. AIRCRAFT WAS THEN RELEASED AND APPROVED FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1996112100393 19961121 00393 1996 11 21 VTZA97037 4 19961021 A 3418 C771076 LIFT TRANSDUCER BAG JETSTM JETSTM3201 1500217 EU LEFT FAILURE A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 474UE 849 FLT 6436 - IAD-CLE - ABORTED TAKEOFF DUE TO LEFT STALL CAPTION ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER P ROBLEMS. MAINTENANCE REMOVED AND REPLACED LIFT TRANSDUCER, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996112100394 19961121 00394 EU 1996 11 21 VTZA97036 1 19961021 A 7110 COWL JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE LOOSE A VTZA A D UNSCHED LANDING RETURN TO BLOCK O OTHER CL CLIMB 1 EA 27 322UE 41058 FLT 6198 - IAD-BDL - DURING CLIMB MADE AN UNSCHEDULED LANDING DUE TO RIGHT ENGINE INBOARD COWL CAME LOOSE. AIRCRAFT RET URNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE RESECURED COWL. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO S ERVICE. (M) 2 L 7 2 4T RT A41NM 1996112100395 19961121 00395 1996 11 21 VTZA97035 4 19961021 A 3420 4318166 RMU JETAIR JETSTM JETSTM4101 1500501 EU RIGHT FAILED A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 312UE 41025 FLT 6356 - PWM-BOS - DURING CLIMB, MADE AN UNSCHEDULED LANDING DUE TO RIGHT RMU FAILED. AIRCRAFT RETURNED TO THE GATE W ITH NO FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED RMU, OPS CHECK OK. AIRCRAFT WAS THEN RELEASED AND APPROVED F OR SERVICE. (M) 2 L 7 2 4T RT A41NM 1996112100396 19961121 00396 1996 11 21 VTZA97034 4 19961020 A 3413 066500012704 VSI BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 492UE 790 FLT 6382 - JFK-BOS - DURING CRUISE MADE AN UNSCHEDULED LANDING DUE TO TCAS DISPLAY WENT DEAD. AIRCRAFT WENT TO GATE WIT H NO FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED VSI, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETU RN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996112100397 19961121 00397 1996 11 21 VTZA97033 4 19961020 A 3414 3996882236 ASI BAG JETSTM JETSTM3201 1500217 EU LT COCKPIT FAILED A A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 27 484UE 899 FLT 6231 - IAD-PHL - ABORTED TAKEOFF DUE TO CAPTAINS ASI FAILED. AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS . MAINTENANCE REMOVED AND REPLACED ASI. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996112100398 19961121 00398 EU 1996 11 21 VTZA97032 1 19961016 A 7712 8974573 TTL VALVE BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 EA 27 477UE 890 FLT 6494 - ROS-IAD - DURING DESCENT, MADE AN UNSCHEDULED LANDING DUE TO RIGHT ENGINE TORQUE, RPM AND EGT FELL OFF. AIRC RAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED TTL VLV. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996112100399 19961121 00399 1996 11 21 VTZA97030 4 19961018 A 3442 7008470922 RT UNIT JETAIR JETSTM JETSTM4101 1500501 EU RADAR SYSTEM FAILED A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 306UE 41020 FLT 6563 - IAD-RDU - DURING CLIMB, MADE AN UNSCHEDULED LANDING DUE TO RADAR FAILED ON CLIMB-OUT. AIRCRAFT RETURNED TO G ATE WITH NO FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED RADAR R/T UNIT, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996112100400 19961121 00400 EU 1996 11 21 VTZA97027 1 19961016 A 5270 DOOR WARNING BAG JETSTM JETSTM3201 1500217 EU BAGG COMPARTMENT MALFUNCTIONED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 495UE 818 FLT 6475 - IAD-SCE - ABORTED TAKEOFF DUE POD DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED POD DOOR AND OPENED DMI 55422, MEL 52-10. AIRCRAFT WAS RELEASED AND APPROVED FOR RETUR N TO SERVICE. MAINTENANCE CLOSED DMI 55422 ON 10-17-96 BY REPAIRING CONNECTION ON DOOR MICROSWITCH. OPS CHECK OK. AIR CRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996112100401 19961121 00401 EU 1996 11 21 VTZA97016 1 19961009 A 7931 1241012 PRESS TRANSDUCER JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 318UE 41041 FLT 6567 - BOS-EWR - DURING CRUISE FLT, EXPERIENCED A FLUCTUATION OF THE RT OIL PRESS INDICATOR. FLT CREW DECLARED EMER GENCY, SHUT DOWN RT ENG AND RETURNED TO BOS. FLT CREW MISINTERPRETED QRH, AS NO OTHER INDICATIONS WERE AFFECTED. A/C L ANDED AT BOS WHERE THE SYSTEM WAS CHECKED AND FOUND TO BE ONLY AND ERRATIC INDICATOR. VISUALLY CHECKED ENG OIL LEVEL AN D PERFORMED GROUND RUNS TO VERIFY CORRECT ENGINE OIL PSI CAPTION OPERATION. GROUND RUNS PROVED GOOD. DEFERRED OIL PRES S INDICATOR IAW J-4100 MEL NR 79-3. CLOSED DMI 08358 ON 10-10-96. MX R/R OIL PRESS TRANSDUCER, OPS CHECK OK. A/C RELE ASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996112100402 19961121 00402 EU 1996 11 21 VTZA96400 1 19960929 A 5270 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGGAGE DOOR OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 317UE 41031 FLT 6450 - CLE-IAD - ABORTED TAKEOFF DUE TO BAGGAGE DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO F URTHER INCIDENT. MAINTENANCE OPENED DMI 40804, MEL 52-3. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE MAI NTENANCE CLOSED DMI 40804 BY ADJUSTING AFT MICROSWITCH, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996112100403 19961121 00403 NE 1996 11 21 EISA96196 2 19961022 A 7261 FITTING BOEING 727 727221 1384071 NM PWA JT8 JT8D17 52049 NE NR 3 ENGINE LOOSE A EISA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 07 368PA 678665 22540 678665 ENGINE NR 3 OIL QTY BEGAN RAPIDLY DROPPING ON APPROACH AND OIL TEMPERATURE ENTERED YELLOW BAND. ENGINE SHUTDOWN ACCOMPL ISHED APPROXIMATELY 1/4 GALLON REMAINING UPON LANDING. OIL SYSTEM INSPECTED, BANJO FITTING ON SYSTEM RETURN FOUND LOOSE . THREAD PITCH CHECKED AND FOUND SATISFACTORY, FITTING REPACKED. ENGINE RUN AND LEAK CHECK GOOD. (M) 2 L 7 3 4F 4 F A3WE E2EA 1996112100404 19961121 00404 NM 1996 11 21 GAIA9630 1 19961031 A 3350 1000679 LIGHT BOEING 727 727223 1384074 NM COCKPIT INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 6809 19484 DURING PS CHECK AT CGK, COCKPIT EMERGENCY LIGHT TESTED INTERMITTENTLY. REPLACED COCKPIT EMERGENCY EXIT LIGHT MODULE. S YSTEM TESTED NORMALLY. AIRCRAFT RELEASED FOR FLIGHT. (M) 2 L 7 3 4F A3WE 1996112100405 19961121 00405 EU 1996 11 21 M3HA96031 1 19961019 A 3230 CIRCUIT BREAKER AEROSP ATR42 ATR42300 8680920 EU LANDING GEAR TRIPPED A M3HA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 4209G 129 HNL - FLT 702 - CREW REPORTED, AFTER TAKEOFF FROM HNL, GEARS WILL NOT RETRACT, WOW SYSTEM NR 2 CIRCUIT BREAKER POPPED. AIRCRAFT RETURN TO HNL FOR INVESTIGATION, HMC GB. RERACKED PSEU, OPS CHECK GOOD, PERFORMED GEAR SWING SEVERAL TIMES, I AW JIC 32-31-00. (M) 2 H 7 2 4T RT A53EU 1996112100406 19961121 00406 WP 1996 11 21 GTIA96NK212 1 19961027 A 3350 60030431 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 12536 47113 FORWARD RIGHT AND LEFT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY POWER SUPPLY, OPS CHECKS GOOD IAW 33-53-0. (M) 2 L 7 2 4F A6WE 1996112100407 19961121 00407 SO 1996 11 21 C2XA96IA261 1 19961021 A 5315 12006158002 FLOOR BEAM EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16731 120190 IAH - DURING C-CHECK INSPECTION, THE FLOOR SUPPORT FROM FRAME 39 TO 44 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AN D REPLACED THE AFFECTED FLOOR BEAM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996112100408 19961121 00408 SO 1996 11 21 C2XA96IA260 1 19961021 A 5320 12004149002 T-PROFILE EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16731 120190 IAH - DURING C-CHECK INSPECTION, THE T-PROFILE FROM FRAME 36 TO 38 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND RE PLACED THE AFFECTED T-PROFILE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996112100409 19961121 00409 EU 1996 11 21 C2XA96BT015 1 19961027 A 2611 A300B09606031B SELECTOR SWITCH AEROSP ATR42 ATR42320 8680930 EU LT EQUIP PNL DIRTY A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 09 14832 187 EWR - INBOUND TO EWR FLIGHT 3549 CREW REPORTED AFT SMOKE LIGHT ILLUMINATED ON CAP WITH AFT CARGO LIGHT ON FLIGHT ATTENDA NTS PANEL. NO SMOKE OR FIRE PRESENT. ALSO NOTED, PULLED LAV FLUSH MOTOR AND CVR CIRCUIT BREAKER FOLLOWING AFT SMOKE LI GHT IN FLIGHT. CLEANED ROTARY TEST SWITCH ON CAPTAINS MAINTENANCE PANEL AND OPS CHECKED GOOD IAW 26-15-00 OPT 10020-002 AND 26-15-00 OPT 10030-002 ALSO, RESET BREAKERS THAT WERE PULLED OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A53EU 1996112100410 19961121 00410 NE 1996 11 21 C2XA96CL035 2 19961026 A 7321 7898414005 EEC EMB 120 EMB120RT SO PWA 118 PW118 NE NR 2 ENGINE FAILED A C2XA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 09 12709 10276 120101 89123365 CLE - FLT 3003 - CREW REPORTED THAT AT 17,500 FEET THEY COULD NOT GET MORE THAN 4 PERCENT TORQUE AND 700 DEGREES EGT WIT H POWER LEVER FULL FORWARD. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED THE NR 1 ENGINE ELECTRONIC ENGINE CONTROL IAW EMB 120 MM 73-22-00, ALL OPERATIONAL CHECKS WERE GOOD IAW EMB 120MM 71-00-00. A IRCRAFT RELEASED FOR SERVICE (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1996112100411 19961121 00411 EU 1996 11 21 C2XA96BT014 1 19961027 A 2421 200322 GENERATOR AEROSP ATR42 ATR42320 8680930 EU NR 2 ENGINE FAILED A C2XA O OTHER H ELECT. POWER LOSS-50 PC IN INSP/MAINT 1 SW 09 86842 14011 286 EWR - FLT 3615 - ARRIVED EWR WITH NR 2 ACW GENERATOR INOP, PREVIOUSLY MEL'D. FOUND ACW GENERATOR FAN BLADES SHEARED. R EMOVED AND REPLACED ACW GENERATOR OPERATIONAL CHECKS GOOD IN REFERENCE WITH ATR JIC 24-22-61 RAI 10000-005. AIRCRAFT RE TURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996112100412 19961121 00412 EU 1996 11 21 C2XA96B1012 1 19961025 A 3397 WIRE AEROSP ATR42 ATR42320 8680930 EU NAV LIGHTS FAILED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 15816 105 EWR - FLT 3512 - FLIGHT CREW REPORTED STRONG BURING SMELL IN COCKPIT. AIRCRAFT AIR RETURNED TO EWR UNEVENTFULLY. MAINT ENANCE FOUND C/B TO NORMAL NAV LIGHTS BURNED AND WIRE GOING TO C/B BURNED. REPLACED C/B FOR BEACON NORMAL AND NAV LIGHT S NORMAL POWER SUPPLY. REPAIRED WIRE BETWEEN NAV NORMAL C/B AND LOGO NORMAL C/B IAW ATR-42 WIRING MANUAL AND CHAP 20 ST ANDARD PRACTICES. OPS CHECKS GOOD, NO ACRID SMELL NOTED. (M) 2 H 7 2 4T RT A53EU 1996112100413 19961121 00413 EU 1996 11 21 C2XA96BT013 1 19961028 A 2710 52211001100000 DRIVE CABLE AEROSP ATR42 ATR42320 8680930 EU AILERON BROKEN A A C2XA K NONE F FLT CONT AFFECTED AP APPROACH 1 SW 09 15816 15964 105 BTV - INBOUND FLIGHT 3682, CAPTAIN REPORTED 'YOKE MOVEMENT FEELS RESTRICTED. CAN'T GET FULL DEFLECTION OF RIGHT AILERON '. AIRCRAFT LANDED WITHOUT PROBLEM. UPON INSPECTION FOUND THE AILERON TRIM SERVO DRIVE CABLES BROKEN AND SERVO DRIVE B INDING. REMOVED AND REPLACED AUTOPILOT ROLL SERVO AND CABLES IAW ATR 42 JIC 22-13-71 RAI 10000-002. OPS CHECK GOOD. A IRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996112100414 19961121 00414 EU 1996 11 21 C2XA96BT016 1 19961029 A 3222 D226981003 STRUT ASSY AEROSP ATR42 ATR42320 8680930 EU NLG WORN/PLAY A C2XA O OTHER J WARNING INDICATION UK UNKNOWN 1 SW 09 18814 19084 103 EWR - FLT 3447 - REPORTED LANDING GEAR WOULD NOT LOCK IN THE UP POSITION. AIRCRAFT WAS RELEASED IAW MEL 32-31-3 PLACARD NR 896767. AIRCRAFT RETURNED TO SERVICE. AIRCRAFT RON BTB MAINTENANCE FOUND EXCESSIVE PLAY IN SHOCK ABSORBER CAUSING NOSE GEAR TO NOT RETRACT. REMOVED AND REPLACED NOSE LANDING GEAR LEG ASSEMBLY. ALL OPERATIONAL AND LEAKAGE CHECKS GOOD IAW ATR 42 MM 32-21-00 RAI 10000-003. MEL CLEARED AND AIRCRAFT RELEASED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996112100415 19961121 00415 EU 1996 11 21 C2XA96IA271 1 19961028 A 5315 S35672407202 FLOOR BEAM AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 21837 202 IAH - DURING C-CHECK INSPECTION, FOUND FRAME NR 38 FLOOR BEAM TO HAVE CORROSION. INSTALLED DOUBLER TO AFFECTED AREA. A IRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996112100416 19961121 00416 EU 1996 11 21 C2XA96IA272 1 19961028 A 5315 S53672408202 FRAME AEROSP ATR42 ATR42320 8680930 EU CABIN FLOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 21837 202 IAH - DURING C-CHECK INSPECTION, FOUND FRAME NR 39 FLOOR BEAM TO HAVE CORROSION. INSTALLED DOUBLER TO AFFECTED AREA. A IRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996112100417 19961121 00417 EU 1996 11 21 C2XA96IA273 1 19961028 A 5315 S53672406208 FLOOR BEAM AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 21837 202 IAH - DURING C-CHECK INSPECTION, FOUND FRAME NR 36 FLOOR BEAM TO HAVE CORROSION. INSTALLED DOUBLER TO AFFECTED AREA. A IRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996112100418 19961121 00418 EU 1996 11 21 C2XA96IA274 1 19961028 A 5347 S53678001202 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 21837 202 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT AFT INBOARD SEAT TRACK TO HAVE CORROSION. REMOVED AND REPLACED AFFECTED AR EA OF SEAT TRACK. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996112100419 19961121 00419 EU 1996 11 21 C2XA96IA275 1 19961028 A 5347 S53678001201 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 21837 202 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT AFT OUTBOARD SEAT TRACK TO HAVE CORROSION. REMOVED AND REPLACED AFFECTED A REA OF SEAT TRACK. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996112100420 19961121 00420 EU 1996 11 21 C2XA96IA276 1 19961028 A 5347 S53678001212 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 21837 202 IAH - DURING C-CHECK INSPECTION, FOUND FLIGHT ATTENDANTS LEFT SIDE SEAT TRACK TO BE CORRODED. REMOVED AND REPLACED AFFE CTED AREA OF SEAT TRACK. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996112100421 19961121 00421 EU 1996 11 21 C2XA96IA277 1 19961028 A 5347 S53678001214 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 21837 202 IAH - DURING C-CHECK INSPECTION, FOUND FLIGHT ATTENDANTS RIGHT SIDE SEAT TRACK TO BE CORRODED. REMOVED AND REPLACED AFF ECTED AREA OF SEAT TRACK. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996112100422 19961121 00422 EU 1996 11 21 AWXA960614 1 19961024 A 3350 321430 BATTERY AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 639AW 471 PHX - FLT 2284 - DURING ROUTINE MAINTENANCE CHECK, FOUND LEFT OVERHEAD EMERGENCY LIGHT BATTERY PACK FAULTED. REPLACED B ATTERY PACK, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A28NM 1996112100423 19961121 00423 EU 1996 11 21 AWXA960604 1 19961019 A 3350 321430 BATTERY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 636AW 2876 098 PHX - FLT 2541 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT SYSTEM FAILS BATTERY AT 11WL AND 10WL. RE PLACED BOTH BATTERY SYSTEM, OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A28NM 1996112100424 19961121 00424 EU 1996 11 21 96ZZZM1489 1 19961019 A 3350 321430 BATTERY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 636AW 2876 098 PHX - FLT 2541 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT SYSTEM FAILS BATTERY AT 11WL AND 10WL. RE PLACED BOTH BATTERY SYSTEM, OPS CHECK NORMAL. REFERENCE AWXA960604. 2 L 7 2 4F RT A28NM 1996112100425 19961121 00425 EU 1996 11 21 AWXA960584 1 19961011 A 3350 CONNECTOR AIRBUS 320 A320231 3930325 EU CABIN FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 633AW 082 PHX - FLT 0007 - DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 16 LEFT EMERGENCY EXIT FLOOR PATH LIGHT INOP. REPLACED CON NECTOR. OPS CHECK OK. (M) 2 L 7 2 4F RT A28NM 1996112100426 19961121 00426 EU 1996 11 21 AWXA960587 1 19961011 A 3350 321430 BATTERY PACK AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 643AW 315 PHX - FLT 1236 - DURING ROUTINE MAINTENANCE CHECK, FOUND FORWARD SECTION L1 AND R1 EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A28NM 1996112100427 19961121 00427 EU 1996 11 21 AWXA960588 1 19961011 A 3350 321454 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 643AW 315 PHX - FLT 1236 - DURING ROUTINE MAINTENANCE CHECK, FOUND BATTERY PACK AT LEFT EMERGENCY EXIT HATCHES FAULTS WHEN TESTED. REMOVED AND REPLACED POWER SUPPLY. (M) 2 L 7 2 4F RT A28NM 1996112100428 19961121 00428 NM 1996 11 21 AWXA960609 1 19961021 A 3350 LIGHT BRACKET BOEING 757 757225 1384959 NM CABIN FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 907AW 22691 DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT OUT ON BULL NOSE ROW 3 DC. INSTALLED NEW LIGHT BRACKET AND REIN STALLED EMERGENCY LIGHT. OPERATIONS CHECK OK. (M) 2 L 7 2 4F RT A2NM 1996112100429 19961121 00429 NE 1996 11 21 AWXA960608 2 19961112 A 7510 320115 FUEL HEAT VLV BOEING 737 737297 1384480 NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE LOOSE WIRING A AWXA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 WP 28 147AW 10584 22630 TUS - FLT 2062 - PILOT SHUT DOWN NR 1 ENGINE DUE TO HIGH OIL TEMP. PILOT CYCLED FUEL HEAT VALVE SUSPECTING IT MAY BE PA RTIALLY OPEN, VALVE APPARENTLY FAILED TO CLOSE AS INDICATED BY DISAGREE LIGHT WHEN SELECTED OFF. COULD NOT REMEDY THE H IGH OIL TEMP SO ENGINE WAS SHUT DOWN. AIRCRAFT MADE A SMOOTH OVERWEIGHT LANDING. PLACED THE NR 1 FUEL HEAT VALVE ON ME L. REPAIRED WIRING TO THE NR 1 FUEL HEAT VLV. MEL CLEARED. (M) 2 L 7 2 4F 4 F A16WE E2EA 1996112100430 19961121 00430 NM 1996 11 21 AWXA960596 1 19961015 A 3397 WIRE BOEING 737 737277 1384570 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 180AW 22647 PHX - FLT 2245 - DURING ROUTINE MAINTENANCE CHECK, FUOND EMERGENCY LIGHT WIRE BROKEN AT SEAT 14. REPAIRED WIRE. (M) 2 L 7 2 4F RT A16WE 1996112100431 19961121 00431 NM 1996 11 21 AWXA960610 1 19961019 A 3350 335001 LIGHT BOEING 737 73733A 1384673 NM CABIN LOOSE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 166AW 23627 PHX - FLT 2667 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT AT ROW 13 LEFT IN OVERHEAD BIN BOW NOSE HAS COM E LOOSE. PLACED ON MEL 33-15. RESECURED LIGHT ASSEMBLY. OPERATIONS CHECK GOOD. MEL CLEARED. (M) 2 L 7 2 4F RT A16WE 1996112100432 19961121 00432 NM 1996 11 21 AWXA960611 1 19961023 A 3350 335001 LIGHT BOEING 737 737277 1384570 NM CABIN LOOSE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 184AW 22651 LAS - FLT 134 - DURING ROUTINE MAINTENANCE CHECK, FOUND LIGHT ON SEAT 6C IS LOOSE AND HANGING BY THE WIRING. PLACED ON MEL 33-19. REPLACED EMERGENCY LIGHT AT ROW 6 A, B, C. MEL CLEARED. (M) 2 L 7 2 4F RT A16WE 1996112100433 19961121 00433 NM 1996 11 21 AWXA960606 1 19961018 A 3350 CONNECTOR BOEING 737 73733A 1384673 NM CABIN FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 168AW 23629 PHX - FLT 2842 - DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT MOUNTED EMERGENCY EXIT LIGHT INOP AT ROW 21. RELAMP NO HE LP PLACED ON MEL 33-19. REPAIRED CONNECTOR AS REQUIRED. OPERATES NORMALLY. MEL CLEARED. (M) 2 L 7 2 4F RT A16WE 1996112100434 19961121 00434 NM 1996 11 21 AWXA960612 1 19961023 A 2612 3500838 CIRCUIT CARD BOEING 757 7572S7 1384962 NM WHEEL WELL FAILED A AWXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 28 903AW K660295 23323 ORD - FLT 2011 - PIREP REPORTED WHEEL WELL FIRE WARNING LIGHT, IN CURISE AT 350 FL (EICAS BELLS AND ASSOCIATED WARNINGS) AIR SPEED OK, GEAR DROPPED AND ALL WARNINGS EXTINGUISHED. AIRCRAFT DIVERTED INTO ORD. LANDED OVERWEIGHT WITH NO OTHER FIRE WARNING INDICATIONS. PERFORMED WHEEL WELL FIRE DETECTION BITE. NO DEFECTS FOUND. VISUALLY INSPECTED GEAR WELLS, NO DEFECTS NOTED. REPLACED CIRCUIT CARD (DUCT LEAK DETECTION) SYSTEM TEST GOOD. OVERWEIGHT LANDING INSPECTION COMPLET ED WITH NO DEFECTS NOTED. (M) 2 L 7 2 4F RT A2NM 1996112100435 19961121 00435 1996 11 21 96ZZZM1490 4 19961006 A 3421 WIRE BFGOODRICH PS055A DHAV DHC7 DHC7102 2802708 EA POWER SUPPLY FRAYED A CICA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 17 4860J 1144 19 FLT 4903 - FLL-PID - UPON LANDING, PILOT REPORTED SMOKE AND ELECTRICAL BURNING SMELL COMING FROM BEHIND AND LEFT OF CAPT AINS SEAT. INSPECTION FOUND FAULTY WIRES, FRAYED AND LOOSE ATTACHED TO STANDBY ATTITUDE INDICATOR POWER SUPPLY. WIRES SECURED, CIRCUIT BREAKER SECURED. RAN ENGINES, NO SMELL OR SMOKE NOTED. AIRCRAFT FOUND SAFE FOR FERRY FLIGHT TO FLL. M AINTENANCE REPLACED WIRING AND POWER SUPPLY. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 4 4T A20EA 1996112100436 19961121 00436 1996 11 21 96ZZZM1491 4 19961007 A 2350 WC150PA6 SWITCH DHAV DHC7 DHC7102 2802708 EA TILLER WORN A CICA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SO 17 234SL 24 FLT NR 4920 - PID-PBI - PILOT REPORTS TILLER MIC IS STUCK IN THE OPEN POSITION. THE AIRCRAFT WAS INSPECTED AND FOUND TO BE IN SAFE CONDITION FOR FERRY FLIGHT TO FLL MAINTENANCE BASE. MAINTENANCE REMOVED AND REPLACED PUSH TO TALK SWITCH ON TILLER. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 4 4T A20EA 1996112100437 19961121 00437 EA 1996 11 21 96ZZZM1492 1 19961007 A 7921 5D95500 OIL COOLER DHAV DHC7 DHC7102 2802708 EA NR 3 ENGINE FAILURE A CICA E A ENGINE SHUTDOWN UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 SO 17 234SL 24 FLT NR 4922 - PID-PBI - PILOT REPORTED DURING CLIMB-OUT NR 3 OIL TEMPERATURE ABOVE RED LINE. DID PRECAUTIONARY SHUT DOW N OF NR 3 ENGINE AND RETURNED TO PID. INSPECTION REVEALED SLUDGE IN THE VERNATHERM. THE VERNATHERM WAS REPLACED AND NR 3 ENGINE WAS RUN. PROBLEM STILL EXISTED. THE OIL COOLER WAS THEN REPLACED. ENGINE WAS RUN AND OPS CHECKED GOOD. NO LEAKS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 4 4T A20EA 1996112100438 19961121 00438 EA 1996 11 21 96ZZZM1493 1 19961009 A 3230 62380 SEQ VALVE 75280105004 DHAV DHC7 DHC7102 2802708 EA NLG LEAKING A CICA K NONE J WARNING INDICATION DE DESCENT 1 SO 17 8041D 026 FLT 4918 - PID-MIA - PILOT REPORTED NOSE WHEEL LANDING GEAR LIGHT WAS RED AND TRANSIT LIGHT ON IN FLIGHT. UPON ARRIVAL AT MIA THE AIRCRAFT WAS INSPECTED AND FOUND TO BE SAFE FOR GEAR DOWN FERRY FLIGHT TO FLL. MX FOUND NOSE GEAR DOORS WOUL D NOT FULLY RETRACT. FOUND SEQUENCE VALVE LEAKING. REPLACED VALVE AND REPAIRED DENT IN NOSE GEAR DOORS, SWUNG GEAR TEN TIMES OPERATED CORRECTLY WITH NO DISCREPANCIES NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 4 4T A20EA 1996112100439 19961121 00439 CE 1996 11 21 GLBA96197 1 19961009 A 3230 RETRACT MECH BEECH 1900 1900C 1154161 CE LANDING GEAR MALFUNCTIONED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 96UE UC96 SPI - GEAR FAILED TO RETRACT. MAINTENANCE CYCLED GEAR 20 TIMES WITHOUT DUPLICATION. WIRING INSPECTION AND FUNCTION CHE CK REVEALED NO DISCREPANCIES. (M) 2 L 7 2 4T RT A24CE 1996112100440 19961121 00440 CE 1996 11 21 GLBA96187 1 19960909 A 3297 WIRE BEECH 1900 1900C 1154161 CE RT MLG WW BROKEN A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 123UE UC123 ORD - LANDING GEAR WOULD NOT RETRACT. MAINTENANCE REPAIRED BROKEN WIRE IN RIGHT WHEEL WELL. TEST FLIGHT SATISFACTORY. (M) 2 L 7 2 4T RT A24CE 1996112100441 19961121 00441 SO 1996 11 21 GLBA96188 1 19960912 A 3230 922FS2A6N2735A PROX SENSOR EMB 120 EMB120RT SO RT MLG FAILED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 452UE 120096 ORD - GEAR WON'T RETRACT. MAINTENANCE REMOVED AND REPLACED RIGHT MAIN LANDING GEAR PROXIMITY SENSOR. LANDING GEAR OPER ATES NORMALLY. (M) 2 L 7 2 4T RT A31SO 1996112100442 19961121 00442 SO 1996 11 21 GLBA96185 1 19960906 A 3231 SEQ VALVE EMB 120 EMB120ER 3260203 SO GEAR DOOR DIRTY A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 293UX 120293 CIU - GEAR WOULD NOT RETRACT. FOUND FORWARD GEAR DOOR SEQUENCE VALVES STICKING. CLEANED ALL SEQUENCE VALVES AND TEST F LIGHT SATISFACTORY. (M) 2 L 7 2 4T RT A31SO 1996112100443 19961121 00443 SO 1996 11 21 GLBA96186 1 19960908 A 3230 SEQ VALVE EMB 120 EMB120ER 3260203 SO GEAR DOOR DIRTY A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 293UX 120293 CIU - LANDING GEAR WOULD NOT RETRACT. MAINTENANCE CLEANED ALL FORWARD GEAR DOOR SEQUENCE VALVES. TEST FLIGHT SATISFACT ORY. (M) 2 L 7 2 4T RT A31SO 1996112100444 19961121 00444 SO 1996 11 21 GLBA96184 1 19960830 A 3230 1202050500001 PROX SWITCH EMB 120 EMB120RT SO RT MLG INOPERATIVE A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 267UE 120071 MQT - LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. MAINTENANCE REMOVED AND REPLACED RIGHT MAIN PROXIMITY SWITCH. OPS NORMAL. (M) 2 L 7 2 4T RT A31SO 1996112100445 19961121 00445 CE 1996 11 21 GLBA96189 1 19960919 A 5270 SWITCH BEECH 1900 1900C 1154161 CE CARGO DOOR OUT OF ADJUST A GLBA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 01 145GL UC145 DEN - AFT CABIN DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT. MAINTENANCE ADJUSTED CARGO DOOR ANNUNCIATOR MICROSWITCH, OPS NO RMAL. (M) 2 L 7 2 4T RT A24CE 1996112100446 19961121 00446 SO 1996 11 21 GLBA96190 1 19960919 A 3231 SEQ VALVE EMB 120 EMB120ER 3260203 SO LANDING GEAR DIRTY A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 293UX 120293 CIU - GEAR WOULD NOT RETRACT. MAINTENANCE CLEANED ALL SIX SEQUENCE VALVES, TEST FLIGHT SATISFACTORY. (M) 2 L 7 2 4T RT A31SO 1996112100447 19961121 00447 SO 1996 11 21 GLBA96191 1 19960925 A 3231 LATCH EMB 120 EMB120RT SO RT MLG DOOR LOOSE A GLBA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 CE 01 451UE 120108 ORD - RIGHT MAIN, OUTBOARD, FORWARD GEAR DOOR WOULD NOT CLOSE. MAINTENANCE RESECURED DOOR LATCH PROPERLY AND OPERATIONA L CHECKS GOOD ON GROUND. (M) 2 L 7 2 4T RT A31SO 1996112100448 19961121 00448 CE 1996 11 21 GLBA96192 1 19960926 A 3620 BLEED AIR LIGHT BEECH 1900 1900C 1154161 CE LEFT ILLUMINATED A GLBA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 01 170GL UE170 RDU - LEFT BLEED AIR FAIL ANNUNCIATOR ILLUMINATED IN FLIGHT. MAINTENANCE MEL'D SYSTEM. (M) 2 L 7 2 4T RT A24CE 1996112100449 19961121 00449 SO 1996 11 21 GLBA96198 1 19961011 A 3230 ACTUATOR EMB 120 EMB120RT SO LT/RT MLG OUT OF ADJUST A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 128AM 120109 ORD - LEFT MAIN LANDING GEAR WILL NOT RETRACT. BOTH A AND B RED LIGHTS REMAIN ON AFTER GEAR SELECTED UP. MAINTENANCE A DJUSTED LEFT AND RIGHT MLG ACTUATORS AND UPLOCK INDICATOR SWITCHES. TEST FLIGHT SATISFACTORY. (M) 2 L 7 2 4T RT A31SO 1996112100450 19961121 00450 CE 1996 11 21 GLBA96199 1 19961011 A 3230 SWITCH BEECH 1900 1900C 1154161 CE RT MLG OUT OF ADJUST A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 96UE UC96 ORD - GEAR FAILED TO RETRACT ON TAKEOFF. MAINTENANCE INSPECTED AND FOUND RIGHT LANDING GEAR SAFETY SWITCH OUT OF ADJUST MENT. READJUSTED SWITCH AND OPERATES NORMALLY. (M) 2 L 7 2 4T RT A24CE 1996112100451 19961121 00451 SO 1996 11 21 GLBA96194 1 19961002 A 3230 RETRACT MECH EMB 120 EMB120ER 3260203 SO LANDING GEAR MALFUNCTIONED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 293UX 120293 CIU - LANDING GEAR WOULD NOT RETRACT. MAINTENANCE INSPECTED GEAR SYSTEM WITH NO FAULTS NOTED. TEST FLIGHT SATISFACTORY . CYCLED GEAR AGAIN ON GROUND WITH NOT DISCREPANCIES. (M) 2 L 7 2 4T RT A31SO 1996112100452 19961121 00452 CE 1996 11 21 GLBA96195 1 19961002 A 6120 BETA CABLES BEECH 1900 1900C 1154161 CE RT PROP OUT OF ADJUST A GLBA O OTHER O OTHER CR CRUISE 1 CE 01 86UE UC86 ORD - RIGHT PROP SURGES IN AND OUT OF FEATHER WHEN POWER IS INCREASED IN FLIGHT. MAINTENANCE ADJUSTED BETA CABLE AND OP ERATION CHECKS NORMAL. (M) 2 L 7 2 4T RT A24CE 1996112100453 19961121 00453 SO 1996 11 21 GLBA96196 1 19961009 A 3231 DOOR EMB 120 EMB120ER 3260203 SO NLG NOT LATCHED A GLBA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 CE 01 297UX 120297 CIU - NOSE GEAR LIGHT WOULD NOT EXTINGUISH ON GEAR RETRACTION. MAINTENANCE FOUND RIGHT FORWARD NOSE LANDING GEAR DOOR U NLATCHED FROM ACTUATOR. RELATCHED DOOR, GROUND OPS GOOD. (M) 2 L 7 2 4T RT A31SO 1996112100454 19961121 00454 SO 1996 11 21 GLBA96193 1 19961001 A 3231 SEQ VALVE EMB 120 EMB120ER 3260203 SO LANDING GEAR DIRTY A GLBA O OTHER J WARNING INDICATION CL CLIMB 1 CE 01 293UX 120293 CIU - GEAR WOULD NOT RETRACT AFTER TAKEOFF. MAINTENANCE INSPECTED AND CLEANED SEQUENCE VALVES ON LANDING GEAR DOORS. I NSPECTED ALL WIRING AND HYDRAULIC TUBING. OPERATES NORMALLY, COULD NOT DUPLICATE. (M) 2 L 7 2 4T RT A31SO 1996112100455 19961121 00455 SW 1996 11 21 MALA965168 1 19961023 A 5320 CHANNEL SWRNGN SA227 SA227AC 8780603 SW BS 293 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 2692P AC658B DURING AN INSPECTION IN MSP, MAINTENANCE FOUND THE LEFT FLOOR BOARD SUPPORT 'Z' CHANNEL CRACKED APPROXIMATELY .375 INCH FROM FASTENER HOLE TO CHANNEL EDGE AT FS 293 (P/N 27-20025). REPAIRS COMPLETED BY INSTALLATION OF A REPAIR DOUBLER PER FAC SRM 56-90-20 PAGES 67-69 REV JAN 18/93. (M) 2 L 7 2 4T RT A8SW 1996112100456 19961121 00456 EU 1996 11 21 MALA965170 1 19961023 A 2613 899253 DETECTORS SAAB SF340 SF340A 7850100 EU RT NACELLE FAILED A MALA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 GL 15 107AE 340A107 FLT 2973 - AFTER TAKEOFF FROM ESC, THE RIGHT TAIL PIPE HOT LIGHT ILLUMINATED. THE CREW RETARDED THE POWER LEVERS AND TH E LIGHT REMAINED ON. THE CREW SHUT DOWN THE ENGINE, AND THE LIGHT WOULD INTERMITTENTLY ILLUMINATE. MAINTENANCE REPLACE D THE OVERHEAT DETECTORS IN THE RIGHT AFT FAIRING. ALL CHECKS SATISFACTORY. (M) 2 L 7 2 4T RT A52EU 1996112100457 19961121 00457 SW 1996 11 21 MALA965169 1 19961023 A 5712 RIB SWRNGN SA227 SA227AC 8780603 SW WS 39 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 2692P AC658B DURING AN INSPECTION IN MSP, MAINTENANCE FOUND AT RIGHT WS 39 WING RIB FORWARD LOWER CUTOUT A .250 CRACK ON AFT SIDE AND .50 CRACK ON LOWER SIDE OF CUTOUT, P/N 27-31020. REPAIRS COMPLETED BY INSTALLATION OF A REPAIR DOUBLER PER AEROTECH DE SIGNS EA01-96108 DATED OCT 23/96. (M) 2 L 7 2 4T RT A8SW 1996112100458 19961121 00458 WP 1996 11 21 MALA965171 2 19961025 A 7230 3407051 COMPRESSOR SEAL SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP RT ENGINE FAILED A MALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 15 422MA AC635 FLT 3094 - ON CLIMB-OUT FROM MSP, THE CREW NOTED A BAD ODOR FROM THE BLEED AIR SYSTEM AND A HAZE IN THE CABIN. THE AIRC RAFT RETURNED TO MSP. MAINTENANCE REPLACED THE RIGHT ENGINE COMPRESSOR SEAL. ALL CHECKS SATISFACTORY. (M) 2 L 7 2 4T 4 T RT A8SW E4WE 1996112100459 19961121 00459 WP 1996 11 21 ORJA9673 1 19961029 A 3350 41B004AD073 BATTERY EA1D13D3 DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 823RA 49889 EMERGENCY LIGHTS FROM FORWARD GALLEY TO ROW 3 ARE OUT. REPLACED FUSE AND BATTERIES AT FORWARD LEFT CHARGER. LIGHTS CHE CK GOOD, ALSO REPLACED FUSE. (M) 2 L 7 2 4F A6WE 1996112100460 19961121 00460 WP 1996 11 21 96ZZZM1494 1 19961013 A 3230 37760735001 BOGIE CYLINDER DOUG DC8 DC861 3021952 WP LT MLG DAMAGED A FXLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 27UA 45942 A/C RETURNED TO MIAMI FOR RED GEAR LIGHT STAYS ON AFTER GEAR RETRACTION. FOUND LEFT BOGIE UNLOCK CYLINDER DAMAGED. REM OVED AND REPLACED BOGIE CONTROL VALVE IAW MM 32-53-1 AND ALSO REMOVED AND REPLACED LEFT BOGIE CYLINDER ACTUATOR IAW MM 3 2-53-2. OPS CHECK FOUND GOOD. PERFORMED LANDING GEAR SWING, CHECKED INDICATION LIGHTS IAW MM 32-11-1. OPS CHECK FOUND NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 4 4F 4A25 1996112100461 19961121 00461 EU 1996 11 21 JBXA00021 1 19961024 A 2131 CONTROLLER FOKKER F28 F28MK0100 4990807 EU NR 2 MALFUNCTIONED A JBXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 131ML 11323 FLL - FLT 301 - WHILE EN ROUTE TO RDU, CREW REPORTED HAVING PROBLEMS GETTING AIRCRAFT TO PRESSURIZE AND RETURNED TO FLL. MX FOUND THAT PRESSURE CONTROLLER NR 2 HAD FAULTED. AFTER RESETTING THE CONTROLLER, AIRCRAFT WOULD NOT PRESSURIZE ON THE GROUND PLACED MEL 21-30-1 DMI NR 02369 ON AIRCRAFT AND RETURNED TO RDU UNPRESSURIZED. MIDWAY, MAINTENANCE PERFORMED OPERATIONAL CHECK OF SYSTEM WITH NO FAULTS FOUND, CLEARED DMI. (M) 2 L 7 2 4F RT 1996112100462 19961121 00462 NM 1996 11 21 IXKA9600082 1 19961029 A 3610 12355814 CHECK VALVE BOEING 727 727225 1384077 NM NR 1 STRUT BROKEN A IXKA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 25 356PA 07125 20626 NR 1 ENGINE STRUT OVERHEAT ON TAKEOFF. REMOVED AND REPLACED 8TH STAGE CHECK VALVE PER MM 36-10-21. (M) 2 L 7 3 4F A3WE 1996112100463 19961121 00463 WP 1996 11 21 GRAA9674 1 19961019 A 3350 0816300609 COVER DOUG DC9 DC987 3022087 WP CABIN MISSING A GRAA K NONE L NO TEST IN INSP/MAINT 1 WP 11 750RA 49777 LINE MAINTENANCE AT IFP, FOUND THE EMERGENCY TRACK LIGHT COVER MISSING AT ROW 8. MAINTENANCE REPLACED THE EMERGENCY TRA CK LIGHT COVER. OPERATIONAL CHECKED NORMAL. NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A6WE 1996112100464 19961121 00464 1996 11 21 96ZZZM1495 4 19961101 A 3454 6341022001 CONNECTOR FRCHLD SA227 SA227DC 3377521 SW AVIONICS LOOSE A EQGA H DEACTIVATE SYST/CIRCUITS O OTHER AP APPROACH 1 SW 19 847LS 7045 DC847B A/C DIVERTED TO HOT DUE TO RADAR MALFUNCTION. ON APPROACH , THE CAPT REPORTED BOTH VOR'S WERE NOT FUNCTIONING PROPERLY AND THE CEILING WAS TOO LOW FOR AN ADF APPROACH, CAPT ASKED MEM CTR FOR VECTORS TO NEAREST VFR AIRPORT AND DIVERTED TO F SM. AN AVIONICS SHOP CHECKED OUT THE VOR'S AND COULD NOT FIND ANY FAULTS WITH THE SYS AND RETURNED THE A/C TO SERV. AF TER THE WEATHER IMPROVED, THE CAPT REPOSITIONED THE A/C TO HOT. AFTER LANDING IN HOT, THE CAPT REPORTED THAT THE VORS W ERE ACTING UP AGAIN. THROUGH EXTENSIVE T/S WITH NAV401 TEST BOX, A BARREL ON THE COAX SPLITTER WAS FOUND TO BE LOOSE. T HE BARREL WAS REPAIRED AND THE A/C WAS RETURNED TO SERV. 2 L 7 2 4T RT A18SW 1996112100465 19961121 00465 SO 1996 11 21 ZIAA96039 1 19961011 A 3242 2697 BRAKE ASSEMBLY BFGOODRICH LKHEED 188 188C 5262604 SO NR 2 MLG LEAKING A ZIAA O OTHER A K FLAME/FIRE FLUID LOSS LD LANDING 1 GL 23 290F 2250 188C1133 DFW - UPON ARRIVAL DFW, CAPTAIN REPORTED BRIEF LEFT BRAKE FIRE. FOUND NR 2 BRAKE LEAKING. REPLACED NR 2 BRAKE ASSEMBLY AND BRAKE ATTACHING BOLTS. BLED BRAKE SYSTEM, NO LEAKS NOTED. SYSTEM FUNCTIONS NORMAL. (M) 2 L 7 4 4T 4A22 1996112100466 19961121 00466 NM 1996 11 21 AWXA960644 1 19961027 A 3350 PIN BOEING 757 7572S7 1384962 NM CABIN UNSEATED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 902AW 23322 PHX - FLT 25 - DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 32 R SEAT MOUNTED EMERGENCY LIGHT INOP. FOUND PIN NOT SEATED AT SEAT 32C. RESEATED PIN. OPERATIONS CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 1996112100467 19961121 00467 NM 1996 11 21 AWXA960632 1 19961010 A 5320 WEB BOEING 737 737277 1384570 NM BS 709-727 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 PAE - FLT 7837 - DURING ROUTINE MAINTENANCE CHECK, FOUND SHEAR WEB ON LEFT SIDE CRACKED FROM BS 709 - BS 727 AT STRINGER 18A. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-30-2, ER 2-53-15-51, TCO-PAN-1433RR-1449RR8110-3. (M) 2 L 7 2 4F RT A16WE 1996112100468 19961121 00468 NM 1996 11 21 AWXA960631 1 19961010 A 5320 654681287 INTERCOSTAL BOEING 737 737277 1384570 NM BS 1013 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 PAE - FLT 7837 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION AT FASTENER HOLE ON INTERCOSTAL STATION 1013, LBL 40. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-30-2. (M) 2 L 7 2 4F RT A16WE 1996112100469 19961121 00469 NM 1996 11 21 AWXA960630 1 19961010 A 5320 WEB BOEING 737 737277 1384570 NM BS 987-1006 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 PAE - FLT 7837 - DURING ROUTINE MAINTENANCE CHECK, FOUND WEB UNDER MOPSILL BS 987-1006, LBL 55 CORRODED. REMOVED, FABRI CATED AND INSTALLED NEW WEB IAW SRM 51-30-2, 51-10-1, 51-10-2. (M) 2 L 7 2 4F RT A16WE 1996112100470 19961121 00470 NM 1996 11 21 AWXA960629 1 19961010 A 5320 PLATE BOEING 737 737277 1384570 NM BS 997-1006 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 PAE - FLT 7837 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON INTERCOSTAL STATION 997-1006, LBL 10 ON SPACER PLA TE. REMOVED, FABRICATED AND INSTALLED SPACER PLATE ON INTERCOSTAL AT STATION 997-1006, LBL 10. (M) 2 L 7 2 4F RT A16WE 1996112100471 19961121 00471 NM 1996 11 21 AWXA960628 1 19961005 A 5320 65C2084438 INTERCOSTAL BOEING 737 737277 1384570 NM BS 947 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 PAE - FLT 7837 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION AROUND FASTENER HOLES INTERCOSTAL STATION 947-967, RB L 18, WL 208. REMOVED CORRODED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL IAW SRM 51-10-1, 51-30-2 AND SRM 53-10-1. (M) 2 L 7 2 4F RT A16WE 1996112100472 19961121 00472 NM 1996 11 21 AWXA960627 1 19961005 A 5320 6SC2084438 INTERCOSTAL BOEING 737 737277 1384570 NM BS 947-967 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 PAE - FLT 7837 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION AROUND FASTENER HOLES OF INTERCOSTAL STATION 947 TO 9 67, RBL 10, WL 208. REMOVED AND REPLACED WITH NEW INTERCOSTAL AT BS 947-967, RBL 30, WL 208 PER SRM 51-10-1 AND 51-30-2 . (M) 2 L 7 2 4F RT A16WE 1996112100473 19961121 00473 NM 1996 11 21 AWXA960626 1 19961009 A 5315 BAC1505100617 FLOOR BEAM BOEING 737 737277 1384570 NM BS 987 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 PAE - FLT 7837 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM STATION 987, LBL 15, RBL 3 AND RBL 30-3 5. REMOVED AND REPLACED UPPER CHORD OF FLOOR BEAM FROM LBL 55 TO RBL 55, BS 987, WL 208, PER SRM 51-30-2 AND ER 2-53-15 -36, TCO-PAN-96-141RR, 8110-3. (M) 2 L 7 2 4F RT A16WE 1996112100474 19961121 00474 NM 1996 11 21 AWXA960625 1 19961010 A 5320 65C807361 MOPSILL BOEING 737 737277 1384570 NM BS 950-1006 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 PAE - FLT 7837 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON MOPSILL RIGHT STATION 950-1006, WL 208. REMOVED A ND REPLACED MOPSILL (CHORD) PER SRM 53-10-1, 51-30-2, 51-10-1. (M) 2 L 7 2 4F RT A16WE 1996112100475 19961121 00475 NM 1996 11 21 AWXA960624 1 19961007 A 5320 65C8073S116 THRESHOLD BOEING 737 737277 1384570 NM BS 954-991 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 PAE - FLT 7837 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON MOP SILL LEFT BS 954-991, WL 208. REMOVED DAMAGED MOPSILL AND INSTALLED NEW MOPSILL IAW SRM 51-10-1, 51-30-2. (M) 2 L 7 2 4F RT A16WE 1996112100476 19961121 00476 NM 1996 11 21 AWXA960623 1 19961007 A 5315 FLOOR BEAM BOEING 737 737277 1384570 NM BS 967 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 PAE - FLT 7837 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM 967, RBL 15-55, WL 208. REPAIRED PER S RM 53-10-9 BY FABRICATING AND INSTALLING UPPER CHORD. (M) 2 L 7 2 4F RT A16WE 1996112100477 19961121 00477 NM 1996 11 21 AWXA960622 1 19961005 A 5313 STRINGER BOEING 737 737277 1384570 NM BS 907 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 FLT 7837 - PAE - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION AT BS 907, STRINGER 27R AT STRINGER SPLICE. REPAIRED STRINGER 27 RIGHT, BS 887-927 AS PER SRM 53-10-3. (M) 2 L 7 2 4F RT A16WE 1996112100478 19961121 00478 NM 1996 11 21 AWXA960621 1 19961005 A 5313 STRINGER BOEING 737 737277 1384570 NM BS 949 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 PAE - FLT 7837 - DURING ROUTINE MAINTENANCE CHECK, FOUND STRINGER 27 LEFT AT BS 949 CORRODED. REMOVED, FABRICATED AND I NSTALLED REPAIR PARTS PER SRM 53-10-3. (M) 2 L 7 2 4F RT A16WE 1996112100479 19961121 00479 NM 1996 11 21 AWXA960619 1 19960926 A 5347 654N02438 SEAT TRACK BOEING 757 7572S7 1384962 NM BS 397 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 PAE - FLT 7825 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON SEAT TRACK BS 397, RBL 45, WL 208. REMOVED AND RE PLACED SEAT TRACK PER IAW SRM 51-40-02 AND SRM 51-40-00. (M) 2 L 7 2 4F RT A2NM 1996112100480 19961121 00480 NM 1996 11 21 AWXA960618 1 19960926 A 5315 FLOOR BEAM BOEING 757 7572S7 1384962 NM BS 377 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 PAE - FLT 7825 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM BS 377, RBL 2, WL 208. FABRICATED, ALO DINED, PRIMED AND INSTALLED REPAIR PARTS PER SRM 53-00-51 AND 51-20-01. (M) 2 L 7 2 4F RT A2NM 1996112100481 19961121 00481 NM 1996 11 21 AWXA960617 1 19960926 A 5347 SEAT TRACK BOEING 757 7572S7 1384962 NM BS 397 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 PAE - FLT 7825 - DURING ROUTINE MAINTENANCE CEHCK, FOUND CORROSION ON SEAT TRACK BS 397, RBL 24, WL 208. REMOVED AND IN STALLED REPAIR PARTS PER SRM 51-40-02. (M) 2 L 7 2 4F RT A2NM 1996112100482 19961121 00482 NM 1996 11 21 AWXA960616 1 19960926 A 5315 FLOOR BEAM BOEING 757 7572S7 1384962 NM BS 324 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 PAE - FLT 7825 - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR BEAM AT STATION 324 HAS CORROSION AT RBL 51 TO RBL 65, WL 208. FABRICATED, ALODINED, PRIMED AND INSTALLED PARTS PER ER 5-23-12-06 AND TCO PAN 96-1358RR-8110-3. (M) 2 L 7 2 4F RT A2NM 1996112100483 19961121 00483 NM 1996 11 21 AWXA960615 1 19960924 A 5330 SKIN BOEING 757 7572S7 1384962 NM BS 1500-1520 DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 906AW 23568 PAE - FLT 7825 - DURING ROUTINE MAINTENANCE CHECK, FOUND TWO DENTS IN SKIN ON LEFT AFT FUSELAGE BETWEEN BS 1500 AND 1520 , BETWEEN STRINGER 26L AND STRINGER 27L. CUT OUT DAMAGE, FABRICATED PARTS AND INSTALLED PER SRM 53-00-01 AND ER 5-53-35 -02. (M) 2 L 7 2 4F RT A2NM 1996112100484 19961121 00484 NM 1996 11 21 AWXA960613 1 19961025 A 2760 285T0017103 POWER SUPPLY BOEING 757 7572G7 1384963 NM NR 2 RIGHT FAILED A AWXA O OTHER F FLT CONT AFFECTED AP APPROACH 1 WP 28 909AW 29357 D02194 24522 PHX - FLT 25 - AIRCRAFT ROLLED TO THE LEFT UPON SELECTING FLAPS 30 DEGREES (WENT DIRECTLY FROM 20 TO 30 DEGREES). APPRO XIMATELY 4 DEGREES OF RIGHT AILERON WAS REQUIRED TO HOLD WINGS LEVEL. FLAPS 20 WAS SELECTED AND GROUND PROX FLAP OVERRI DE WAS SELECTED. ROLL DISAPPEARED AND A NORMAL LANDING WAS MADE. RESET SPOILER ACTUATOR RVDT NULL PER 27-61-00. REPLA CED CSEU 2R FOR EICAS MESSAGE. SYSTEM OPS CHECK GOOD SPOILER NR 3 IS NOW NULLED IN LIMITS OK FOR SERVICE. (M) 2 L 7 2 4F RT A2NM 1996112100485 19961121 00485 1996 11 21 ASAA9680223 4 19961010 A 2565 D37013111 INFLATION BOTTLE DOUG DC9 DC982 3022082 WP L-2 DOOR SLIDE LOW PRESSURE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 956AS 15211 48079 PDX - DURING MAINTENANCE CHECK, THE L-2 DOOR EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. REPLACED EVACUAT ION SLIDE ASSEMBLY. (M) 2 L 7 2 4F A6WE 1996112100486 19961121 00486 WP 1996 11 21 ASAA9680244 1 19961026 A 5320 DOOR JAMB DOUG DC9 DC983 3022083 WP BS 1212 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 964AS 53078 OAK - DURNG 15K CHECK, CORROSION WAS FOUND ON THE AFT CARGO COMPARTMENT DOOR JAMB TORQUE BOX WEB AT Y1212. REMOVED DAMA GED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM AND ASA EA 5310-01498. (M) 2 L 7 2 4F RT A6WE 1996112100487 19961121 00487 WP 1996 11 21 ASAA9680245 1 19961028 A 2612 FIRE WARNING DOUG DC9 DC983 3022083 WP APU SOUNDED A ASAA K NONE N FALSE WARNING DE DESCENT 1 NM 01 974AS 53450 GEG - FLT 305 - CREW REPORTED, APU AURAL FIRE WARNING SOUNDED DESCENDING THROUGH 8500 FEET IN RAIN, NO VISUAL INDICATION NOTED. PERFORMED APU/ENGINE FIRE WARNING TEST, NO FAULT FOUND. (M) 2 L 7 2 4F RT A6WE 1996112100488 19961121 00488 WP 1996 11 21 ASAA9680246 1 19961029 A 5210 4928806501 HOLD OPEN HOOK DOUG DC9 DC983 3022083 WP L-1 DOOR INOPERATIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PDX - DURING MAINTENANCE CHECK, THE L-1 DOOR WOULD NOT LATCH IN THE OPEN POSITION. REPLACED HOLD OPEN HOOK AND DOOR LAT CHED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996112100489 19961121 00489 WP 1996 11 21 ASAA9680243 1 19961026 A 3350 41B004AD07G3 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 948AS 53021 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE BAT TERIES AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996112100490 19961121 00490 WP 1996 11 21 ASAA9680242 1 19961025 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 53016 SAN - PRIOR TO DEPARTURE OF FLIGHT 343, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERA TIVE. RECONNECTED TRACK WIRING AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996112100491 19961121 00491 WP 1996 11 21 ASAA9680241 1 19961025 A 3350 6011779 POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 958AS 48654 53024 PDX - DURING MAINTENANCE CHECK, THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPL Y AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996112100492 19961121 00492 WP 1996 11 21 ASAA9680240 1 19961023 A 3350 20131A BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 954AS 49387 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996112100493 19961121 00493 NM 1996 11 21 ASAA9640093 1 19961026 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 773AS 25106 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 14-17. RECON NECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996112100494 19961121 00494 NM 1996 11 21 ASAA9640092 1 19961019 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 773AS 25106 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE ROWS 15-17. RECONNECTED WI RING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996112100495 19961121 00495 NM 1996 11 21 ASAA9610138 1 19961019 A 3350 86210151 BATTERY BOEING 737 7372X6C 1384552 NM CARGO COMPT DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE ON PALLET 7-5. REPLA CED BATTERY AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996112100496 19961121 00496 SO 1996 11 21 C2XA96IA270 1 19961021 A 5347 12026863007 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16731 120190 IAH - DURING C-CHECK INSPECTION, THE LEFT SIDE WALL SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLAC ED THE AFFECTED PORTION OF SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996112100497 19961121 00497 SO 1996 11 21 C2XA96IA269 1 19961021 A 5347 12015997003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16731 120190 IAH - DURING C-CHECK INSPECTION, FOUND THE RIGHT SIDEWALL SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996112100498 19961121 00498 SO 1996 11 21 C2XA96IA268 1 19961021 A 5347 12026865009 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16731 120190 IAH - DURING C-CHECK INSPECTION, THE RIGHT FLOOR AFT SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLA CED THE AFFECTED PORTION OF SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996112100499 19961121 00499 SO 1996 11 21 C2XA96IA267 1 19961021 A 5347 12016000003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16731 120190 IAH - DURING C-CHECK INSPECTION, THE RIGHT FLOOR FORWARD SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND R EPLACED THE AFFECTED PORTION OF SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996112100500 19961121 00500 SO 1996 11 21 C2XA96IA266 1 19961021 A 5347 12026864007 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16731 120190 IAH - DURING C-CHECK INSPECTION, THE LEFT AFT FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLAC ED THE AFFECTED PORTION OF SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996112100501 19961121 00501 SO 1996 11 21 C2XA96IA265 1 19961021 A 5347 12015995003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16731 120190 IAH - DURING C-CHECK INSPECTION, THE LEFT FLOOR FORWARD SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND RE PLACED THE AFFECTED PORTION OF SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996112100502 19961121 00502 SO 1996 11 21 C2XA96IA264 1 19961021 A 5315 12009846001 FLOOR BEAM EMB 120 EMB120RT SO CABIN CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16731 120190 IAH - DURING C-CHECK INSPECTION, THE FLOOR SUPPORT AT FRAME 16 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACD THE AFFECTED FLOOR BEAM AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996112100503 19961121 00503 SO 1996 11 21 C2XA96IA263 1 19961021 A 5320 12006158003 BUTTSTRAP EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16731 120190 IAH - DURING C-CHECK INSPECTION, THE CENTER BUTTSTRAP FROM FRAME 35 TO 44 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996112100504 19961121 00504 SO 1996 11 21 C2XA96IA262 1 19961021 A 5320 12006159001 BUTTSTRAP EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16731 120190 IAH - DURING C-CHECK INSPECTION, THE RIGHT BUTTSTRAP FROM FRAME 33 TO 44 WAS FOUND CORRODED. MAINTENANCE REMOVED AND RE PLACED THE AFFECTED BUTTSTRAP AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996112100505 19961121 00505 NM 1996 11 21 USAA960677 1 19961018 A 5320 WEB BOEING 737 737201 1384454 NM BS 706 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 225US 47563 21667 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND TWO CRACKS APPROX 1 INCH LONG EACH IN VERTICAL WEB STATION 706 LBL 24. I NSTALLED DOUBLER AND ANGLES, REPAIRED PER SRM 51-40-2. (M) 2 L 7 2 4F A16WE 1996112100506 19961121 00506 NM 1996 11 21 USAA960678 1 19961018 A 5311 FRAME BOEING 737 737201 1384454 NM BS 767 CRACK A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 225US 47563 21667 DURING Q-4 CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK FRAME STATION 767 AT STRINGER 21 LEFT. INSTALLED DOUBLER, REPAIR ED PER SRM 53-10-4. (M) 2 L 7 2 4F A16WE 1996112100507 19961121 00507 NM 1996 11 21 USAA960679 1 19961018 A 5330 SKIN BOEING 737 737201 1384454 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 225US 47563 21667 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1.24 INCH CRACK EXT SKIN LBL 3 BS 380. INSTALLED DOUBLER, REPAIRED PER TR 53-30-04. (M) 2 L 7 2 4F A16WE 1996112100508 19961121 00508 NM 1996 11 21 USAA960680 1 19961018 A 5313 1125653 STRINGER BOEING 737 737201 1384454 NM BS 947.5 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 225US 46563 21667 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION APPROX 2 INCH BY 2 INCH STATION 947.5 STRINGER 27L. REPLACED STRINGER FROM STATION 940 TO 1016, REPAIRED PER SRM 53-10-3. CORROSION TASK NR 53-202-01, CORROSION LEVEL 1. (M) 2 L 7 2 4F A16WE 1996112100509 19961121 00509 NM 1996 11 21 USAA960672 1 19961018 A 5330 SKIN BOEING 737 737201 1384454 NM BS 754 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 225US 21667 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1.25 INCH CRACK BS 754 ABOVE STRINGER 18R FUSELAGE SKIN. INSTALLED DOUB LER, REPAIRED PER SRM 53-30-3 FIG 6 AND EA 58706. (M) 2 L 7 2 4F A16WE 1996112100510 19961121 00510 NM 1996 11 21 USAA960675 1 19961018 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 225US 47563 21667 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2.875 INCH CRACK IN SKIN BS 727B AT STRINGER 17R. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER. REPAIRED PER SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1996112100511 19961121 00511 WP 1996 11 21 USAAD96153 1 19961027 A 3350 14597101 BATTERIES DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 805US 48053 FORWARD SECTION OF CABIN EMERGENCY LIGHTS STAY ON WHEN BATTERY SWITCH IS SELECTED OFF. REPLACED BATTERIES IN CEILING BA TTERY PACK. (M) 2 L 7 2 4F A6WE 1996112100512 19961121 00512 WP 1996 11 21 USAAD96154 1 19961018 A 3350 P4010020 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 920VJ 48140 RIGHT SERVICE DOOR EMERGENCY BATTERY PACK INOPERATIVE. REPLACED BATTERY PACK. (M) 2 L 7 2 4F A6WE 1996112100513 19961121 00513 WP 1996 11 21 USAAD96155 1 19961028 A 3350 P4010020 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 939VJ 48120 GALLEY DOOR FORWARD EVACUATION SLIDE LIGHT INOPERATIVE. REPLACED BATTERY PACK. (M) 2 L 7 2 4F A6WE 1996112100514 19961121 00514 WP 1996 11 21 USAAD96156 1 19961030 A 3350 60030451LB POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 973VJ 47099 FORWARD AND AFT OVERWING EMERGENCY DOOR LIGHTS INOPERATIVE. REPLACED BOTH POWER SUPPLIES. (M) 2 L 7 2 4F A6WE 1996112100515 19961121 00515 WP 1996 11 21 USAAD96157 1 19961027 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 830US 49443 FORWARD OVERWING EXIT FLOOR LEVEL EMERGENCY LIGHT (RED) INOPERATIVE. REPAIRED BROKEN WIRE TO LIGHT. (M) 2 L 7 2 4F A6WE 1996112100516 19961121 00516 WP 1996 11 21 USAA960711 1 19961030 A 5330 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 967VJ 75545 47375 PIT - DURING Q-1 CHECK, FOUND CORROSION ON SKIN UNDER NR 1 ADF ANTENNA. SEALANT MISSING AND EVIDENCE OF CORROSION UNDER NEATH (LEVEL 1 AND SUSPECT LEVEL 2). SPLICED REPAIR PER EA 33764 SKIN SPLICE REPAIR. CORROSION LEVEL 2, CORROSION TASK NR C50-53306. (M) 2 L 7 2 4F A6WE 1996112100517 19961121 00517 WP 1996 11 21 USAA960712 1 19961030 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 718 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 934VJ 42984 48114 PIT - DURING C-4, FOUND 1.25 INCH CRACK IN LONGERON 3L AT STATION 718 AT ATTACHING BOLT HOLE. CUT OUT DAMAGED SECTION O F LONGERON AND SPLICED IN NEW SECTION PER TYPICAL REPAIR 53-10-17. (M) 2 L 7 2 4F A6WE 1996112100518 19961121 00518 WP 1996 11 21 USAA960713 1 19961030 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 756 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 934VJ 42984 48114 PIT - DURING C-4, FOUND A .5 INCH AND .75 INCH CRACK IN LONGERON 2R AT STATION 756 AT ATTACHING BOLT HOLES. CUT OUT DAM AGED SECTION OF THE LONGERON AND SPLICED IN A NEW SECTION PER TYPICAL REPAIR 53-10-17. (M) 2 L 7 2 4F A6WE 1996112100519 19961121 00519 WP 1996 11 21 USAA960714 1 19961030 A 5330 SKIN DOUG DC9 DC931 3022065 WP AIR STAIR CUTOUT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 934VJ 42984 48114 PIT - DURING C-4, FOUND .5 INCH CRACK IN SKIN AT FORWARD AIR STAIR CUT OUT AFT LOWER CORNER. ROUTED OUT CRACKED AREA OF SKIN AND INSTALLED A SHIM, FILLER AND A DOUBELR PER SRM 53-05 FIG 57A SHEET NR 1. (M) 2 L 7 2 4F A6WE 1996112100520 19961121 00520 WP 1996 11 21 USAA960691 1 19961025 A 5320 591014211 WEB DOUG DC9 DC931 3022065 WP BS 362.5-436 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 967VJ 76507 47375 PIT - DURING Q-1 CHECK, FOUND 1 INCH BY 8 INCH CORRODED AREA AT LOWER EDGE OF CARGO DOOR WEB STATION 362.5 TO 436 28L TO 29L. REPLACED WEB WITH IDENTICAL PART NR 5910142-11. CORROSION LEVEL 1, CORROSION TASK NR C51-5330. (M) 2 L 7 2 4F A6WE 1996112100521 19961121 00521 WP 1996 11 21 USAA960696 1 19961028 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 427 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 958VJ 59849 47351 PIT - DURING Q-4/C-6 CHECK, FOUND .375 INCH CRACK IN SKIN AT DOOR JAMB FS 427 R27. INSTALLED DOUBLERS PER SRO DWG 95301 17. (M) 2 L 7 2 4F A6WE 1996112100522 19961121 00522 WP 1996 11 21 USAA960697 1 19961028 A 5320 CUSP DOUG DC9 DC931 3022065 WP BS 658-680 DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 958VJ 59849 47351 PIT - DURING Q-4/C-6 CHECK, FOUND HOLE MADE IN CUSP MEMBRANE BETWEEN STATION 658-680 (20 INCH) SECTION. REPLACED SECTIO N OF SKIN AREA FROM FACTORY SPLICE TO FACTORY SPLICE. (M) 2 L 7 2 4F A6WE 1996112100523 19961121 00523 WP 1996 11 21 USAA960698 1 19961028 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 229 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 958VJ 59849 47351 PIT - DURING Q-4/C-6 CHECK, FOUND LONGERON CRACKED AT 23R AT STATION 229. INSTALLED SPLICE PER SRM 53-02 FIG 2. (M) 2 L 7 2 4F A6WE 1996112100524 19961121 00524 WP 1996 11 21 USAA960699 1 19961028 A 5313 2777922 LONGERON DOUG DC9 DC931 3022065 WP STATION 639 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 958VJ 59849 47351 PIT - DURING Q-4/C-6 CHECK, FOUND SEVERAL CRACKS BETWEEN STATION 639 AND STATION 737. SPLICED IN LONGERON FROM STATION 639 TO STATIO N737 PER SRM 53-02 FIG 2. (M) 2 L 7 2 4F A6WE 1996112100525 19961121 00525 WP 1996 11 21 USAA960700 1 19961028 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 522 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 958VJ 59849 47351 PIT - DURING Q-4/C-6 CHECK, FOUND 1 INCH CRACK AT FASTENERS AT STATION 522, 17L LONGERON. REPLACED 20 INCH PIECE OF LON GERON AND DOUBLERS INSTALLED PER SRM 53-10-17 TYPICAL REPAIR. (M) 2 L 7 2 4F A6WE 1996112100526 19961121 00526 WP 1996 11 21 USAA960701 1 19961028 A 5320 CUSP DOUG DC9 DC931 3022065 WP BS 598 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 958VJ 59849 47351 PIT - DURING Q-4/C-6 CHECK, FOUND 4 INCH CRACK IN CUSP MEMBRANE AT STATION 598 18R. REPLACED SECTION OF METAL REMOVED A T FACTORY SPLICE PER EA 33707. (M) 2 L 7 2 4F A6WE 1996112100527 19961121 00527 WP 1996 11 21 USAA960702 1 19961028 A 5730 SKIN DOUG DC9 DC931 3022065 WP WS 214 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 958VJ 59849 47351 PIT - DURIGN Q-4/C-6 CHECK, FOUND 4 INCH CRACK RIGHT WING AT XRS 214 OUTBOARD NR 5 SLAT TRACK CUT OUT RIGHT WING LEADING EDGE. 12 INCH BY 7 INCH DOUBLER REPAIR INSTALLED PER SRM 57-06 FIG 4. (M) 2 L 7 2 4F A6WE 1996112100528 19961121 00528 WP 1996 11 21 USAA960703 1 19961028 A 5530 ANGLE DOUG DC9 DC931 3022065 WP VERTICAL STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 958VJ 59849 47351 PIT - DURING Q-4/C-6 CHECK, FOUND 1.25 INCH CRACK IN RIGHT DRAG ANGLE AT FS 1132 VERTICAL FIN DRAG ANGLE. INSTALLED DOU BLERS PER SRM 53-05 FIG 23 AND 23A. (M) 2 L 7 2 4F A6WE 1996112100529 19961121 00529 WP 1996 11 21 USAA960704 1 19961028 A 5530 ANGLE DOUG DC9 DC931 3022065 WP VERT STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 958VJ 59849 47351 PIT - DURING Q-4/C-6 CHECK, FOUND 1.5 INCH CRACK IN LEFT VERTICAL FIN DRAG ANGLE AT FS 1132. INSTALLED REPAIR DOUBLERS PER SRM 53-05 FIG 23 AND 23A. (M) 2 L 7 2 4F A6WE 1996112100530 19961121 00530 WP 1996 11 21 USAA960705 1 19961028 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 1095 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 958VJ 59849 47351 PIT - DURING Q-4/C-6 CHECK, FOUND .75 INCH CRACK IN FUSELAGE SKIN RIGHT FS 1095 BETWEEN LONGERON R3/R4. INSTALLED DOUBL ER REPAIR PER SRM 53-04 FIG 27. (M) 2 L 7 2 4F A6WE 1996112100531 19961121 00531 WP 1996 11 21 USAA960706 1 19961028 A 5530 ANGLE DOUG DC9 DC931 3022065 WP VERT STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 958VJ 59849 47351 PIT - DURING Q-4/C-6 CHECK, FOUND 1.5 INCH CRACK IN LEFT DRAG ANGLE AT FS 1095 LEFT VERTICAL FIN. INSTALLED DOUBLER PER SRM 53-05 FIG 23B. (M) 2 L 7 2 4F A6WE 1996112100532 19961121 00532 WP 1996 11 21 USAA960707 1 19961028 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 1038 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 958VJ 59849 47351 PIT - DURING Q-4/C-6 CHECK, FOUND .75 INCH CRACK IN RIGHT FUSELAGE SKIN FS 1038 LONGERON R14. INSTALLED DOUBLER PER SRM 53-04 FIG 18. (M) 2 L 7 2 4F A6WE 1996112100533 19961121 00533 WP 1996 11 21 USAA960708 1 19961028 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 1095 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 958VJ 59849 47351 PIT - DURING Q-4/C-6 CHECK, FOUND 1 INCH CRACK IN FUSELAGE SKIN LEFT FS 2095 LONGERON L3/L4. INSTALLED DOUBLER REPAIR P ER EA 33693. (M) 2 L 7 2 4F A6WE 1996112100534 19961121 00534 NM 1996 11 21 AWXA9600681 1 19961115 A 3350 106009139 LIGHT BOEING 737 737277 1384570 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 184AW 22651 DURING ROUTINE MAINTENANCE CHECK, FOUND L-1 DOOR O/H EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY, OPERATIONS CHECK GOOD. 2 L 7 2 4F RT A16WE 1996112100535 19961121 00535 NM 1996 11 21 AWXA9600682 1 19961116 A 3350 831862 BATTERY BOEING 737 737275 1384485 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 CGAPW 20922 DURING ROUTINE MAINTENANCE CHECK, FOUND R-1 AND R-2 DOOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED POWER SUPPL Y UNIT. REMOVED AND REPLACED BATTERY, OPERATIONS CHECK GOOD. POWER SUPPLY UNIT INOP CABIN. 2 L 7 2 4F A16WE 1996112100536 19961121 00536 NM 1996 11 21 AWXA9600683 1 19961115 A 3397 WIRE BOEING 737 737301 1384611 NM CABIN SHORTED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 326AW 23258 DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS OUT AT ROW 17. REMOVED AND REPLACED BATTERY ASSEMBLY. REMOVED AND REPLACED OPEN FUSE IN EMERGENCY BATTERY CHARGER ASSEMBLY. REPAIRED SHORTED WIRES UNDER SEAT AT ROW 21, LIGHTS CHEC K GOOD. 2 L 7 2 4F RT A16WE 1996112100537 19961121 00537 NM 1996 11 21 AWXA9600684 1 19961114 A 5347 GALLEY TRACK BOEING 737 73733A 1384673 NM BS 328 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 509DC 23636 PAE - FLT 7838 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON OUTBOARD GALLEY TRACK STATION 328, RBL 55, WL 208. INSTALLED FABRICATED SEAT TRACK AT BS 328-360, RBL 55, WL 208 PER 53-10-5. (M) 2 L 7 2 4F RT A16WE 1996112100538 19961121 00538 NM 1996 11 21 AWXA9600685 1 19961114 A 5347 SEAT TRACK BOEING 737 73733A 1384673 NM BS 328 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 509DC 23636 PAE - FLT 7838 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON SEAT TRACK FLANGE STATION 328, RBL 45, WL 208. IN STALLED FABRICATED SEAT TRACK AT BS 328-344, WL 208, RBL 45, PER 53-10-5. (M) 2 L 7 2 4F RT A16WE 1996112100539 19961121 00539 NM 1996 11 21 AWXA9600686 1 19961114 A 5347 GALLEY TRACK BOEING 737 73733A 1384673 NM BS 294.5 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 509DC 23636 PAE - FLT 7838 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON INBOARD GALLEY TRACK STATION 294.5, WL 208, RBL 16 . INSTALLED FABRICATED SEAT TRACK AT BS 277-294.5, WL 208, RBL 26 PER 53-10-5. (M) 2 L 7 2 4F RT A16WE 1996112100540 19961121 00540 WP 1996 11 21 CALA9601673 1 19961031 A 5320 BRACKET DOUG DC9 DC982 3022082 WP BS 864 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16807 49261 INSPECTION FOUND A 1.5 CRACK BRACKET AT LT SIDE JUST BOTTOM/CENTER OF FUSELAGE FORWARD OF STA 864. THE BRACKET WAS REMO VED AND A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 1996112100541 19961121 00541 WP 1996 11 21 CALA9601674 1 19961101 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 389 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16807 49261 INSPECTION FOUND A DENT IN FUSELAGE SKIN BELOW CARGO DOOR AT STA 389, LONGERON 29R. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, SHEET 19. 2 L 7 2 4F A6WE 1996112100542 19961121 00542 WP 1996 11 21 CALA9601675 1 19961106 A 5542 SKIN DOUG DC9 DC982 3022082 WP RT RUDDER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16807 49261 INSPECTION FOUND A .75 INCH CRACK IN RT SIDE OF RUDDER SKIN. THE CRACKED AREA WAS CUT OUT, A REPAIR DOUBLER WAS INSTAL LED IAW SRM 55-01, FIGURE 4, SHEET 2. 2 L 7 2 4F A6WE 1996112100543 19961121 00543 WP 1996 11 21 CALA9601676 1 19961031 A 5730 99579651 PANEL DOUG DC9 DC982 3022082 WP LT WING TE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16807 49261 INSPECTION FOUND A 1 INCH CRACK AND CHAFING IN LT WING LOWER TRAILING EDGE PANEL NR 1510. THE AREA WAS REPAIRED IAW SRM 51-70-01. 2 L 7 2 4F A6WE 1996112100544 19961121 00544 WP 1996 11 21 CALA9601677 1 19961102 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 984-1003 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16807 49261 INSPECTION FOUND A .5 INCH CRACK IN LONGERON 20R AT STA 984 TO 1003. THE CRACK WAS ROUTED OUT AND A DOUBLER WAS INSTALL ED IAW ECRA 5310-03363. 2 L 7 2 4F A6WE 1996112100545 19961121 00545 WP 1996 11 21 CALA9601678 1 19961101 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16807 49261 INSPECTION FOUND FLOOR SUPPORT CORRODED AT FORWARD ENTRY UNDER PANEL H. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLE D IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1996112100546 19961121 00546 WP 1996 11 21 CALA9601679 1 19961101 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16807 49261 INSPECTION FOUND FLOOR SUPPORT CORRODED AT FORWARD ENTRY UNDER PANEL G. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLE D IAW SRM 51-10-1 AND 51-30-1. 2 L 7 2 4F A6WE 1996112100547 19961121 00547 WP 1996 11 21 CALA9601680 1 19961101 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16807 49261 INSPECTION FOUND FLOOR SUPPORT CORRODED AT FORWARD ENTRY UNDER MAIN CABIN DOOR THRESHOLD. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1996112100548 19961121 00548 WP 1996 11 21 CALA9601681 1 19961030 A 5350 4913354501 LOCK PIN DOUG DC9 DC982 3022082 WP TAILCONE WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16807 49261 THE TAILCONE HUNG UP ON UPPER RIGHT LATCH DURING DROP TEST. MAINTENANCE FOUND UPPER RIGHT BAYONET LOCK PIN WORN. THE L OCK PIN WAS REPLACED AND THE TAILCONE WAS ADJUSTED IAW MM 53-53-00. 2 L 7 2 4F A6WE 1996112100549 19961121 00549 WP 1996 11 21 CALA9601682 1 19961106 A 5240 SKIN DOUG DC9 DC982 3022082 WP AFT SERVICE DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16894 49393 INSPECTION FOUND A 1 INCH CRACK IN AFT SERVICE DOOR SKIN ABOVE AND BELOW HOLD OPEN HOOK. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5230-01340 AND SRM 52-01. 2 L 7 2 4F A6WE 1996112100550 19961121 00550 WP 1996 11 21 ABXA9600667 1 19961115 A 3260 CONNECTOR DOUG DC9 DC931 3022065 WP RT MLG CORRODED A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 908AX 47008 RIGHT GEAR UNSAFE LIGHT CAME ON DURING UPLATCH CHECK, RECYCLED GEAR, LIGHT WAS STILL ON, RIGHT HYDRAULIC SYSTEM 3000 PSI .\N\N\N\N\NCLEANED WIRING TERMINALS AT TERMINAL STRIP IN RIGHT WING ROOT. LUBRICATED GEAR. PERFORMED GEAR INDICATION TES T IAW DC-9 SUPP M.M. 32-60-01. 2 L 7 2 4F A6WE 1996112100551 19961121 00551 WP 1996 11 21 MWEA96634 1 19961118 A 3350 60030431 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 209ME 47730 DURING SERVICE CHECK FOUND AF FLT ATTEND EMERGENCY LIGHT IN CEILING REMAINED ON WITH PWR OFF. REMOVED AND REPLACED AFT EMERGENCY LIGHT BATTERY PACK. 2 L 7 2 4F A6WE 1996112100552 19961121 00552 WP 1996 11 21 MWEA96635 1 19961118 A 5730 SKIN DOUG DC9 DC914 3022034 WP WS 80 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 RIGHT WING LEADING EDGE SUSTAINED DAMAGE AT APPROX XFS 80 AFTER RAMP VEHICLE CAME IN CONTACT. INSTALLED DOUBLER REPAIR IAW SRM 57-06 FIG 2. 2 L 7 2 4F A6WE 1996112100553 19961121 00553 WP 1996 11 21 SCNA96382 1 19961117 A 2611 13131 SMOKE DETECTOR DOUG DC10 DC1015 3022118 WP CARGO COMPT FAILED A SCNA K NONE L NO TEST UK UNKNOWN 1 GL 15 151SY 48295 THE NUMBER 1 SMOKE DETECTOR WOULD NOT TEST. FOUND LAMP BURNED OUT ON NUMBER 1 AFT CENTER CARGO SMOKE DETECTOR. RELAMPE D AND DETECTOR, TESTED GOOD. 2 L 7 3 4F A22WE 1996112100554 19961121 00554 WP 1996 11 21 SCNA96383 1 19961115 A 3350 0816901 PIGTAIL DOUG DC10 DC1010 3022110 WP CABIN SHORTED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 571SC 46645 THE LEFT FORWARD EMERGENCY TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. FOUND THE EMERGENCY LIGHT PIGTAIL SHORTED AT THE SECOND MODULE FROM THE LEFT, AFT SIDE OF THE LEFT FORWARD EMERGENCY TRACK LIGHTING STRIP. 2 L 7 3 4F A22WE 1996112100555 19961121 00555 NM 1996 11 21 SCNA96384 1 19961115 A 3350 S106 BATTERIES BOEING 727 727227 1384078 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 275AF 22092 THE AFT AIRSTAIR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE BATTERIES IN THE AFT AIRSTAIR EM ERGENCY LIGHT, LIGHT OPS CHECKED GOOD. 2 L 7 3 4F A3WE 1996112100556 19961121 00556 NM 1996 11 21 SCNA96385 1 19961118 A 5313 65564418 STRINGER BOEING 727 727282 138408T NM BS 950 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 281SC 21949 DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON STRINGER 29R BETWEEN STATION 950A AND STATION 950C. REPAIR WAS A CCOMPLISHED PER ENGINEERING AUTHORIZATION INSTRUCTIONS. 2 L 7 3 4F RT A3WE 1996112100557 19961121 00557 SO 1996 11 21 SRAA961049 1 19961013 A 5320 SUPPORT LKHEED 382 382G 526414U SO BS 275 CORROSION A SRAA K NONE O OTHER IN INSP/MAINT 1 GL 23 905SJ 4472 DURING C-CHECK, FOUND CARGO COMPARTMENT FLOOR PANEL SUPPORT BEAM AT FS 275, LBL 40 HAS CORROSION AT FORWARD AND AFT SI DE BEYOND LIMITS. CUT OUT CORRODED SECTION, FABRICATED AND INSTALLED L-ANGLE AND STRAP IAW LAC SRM CHAPTER 51-140-22 AN D 51-70-1. 2 H 7 4 4T A1SO 1996112500001 19961125 00001 NM 1996 11 25 DHL96712005 1 19961113 A 5350 RADOME BOEING 727 72729 1384007 NM FWD FUSELAGE POPPED A DHLA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 01 712DH 19401 DURING TAKEOFF ROLL IMMEDIATELY PRIOR TO ROTATION, CREW HEARD A POP, F/O FELT AND IMPACT UNDER HIS FEET. BURNED RUBBER SMELL IN COCKPIT LASTED 5 MINUTES AND GEAR RETRACTION WAS NORMAL. NO GEAR WARNING OR OTHER ABNORMAL INDICATIONS WERE NO TED. PERFORMED ABNOMRAL NOISE CHECK, INSPECTED RADOME, NOSE W/W, FWD AND AFT E AND E BAYS, WING LEADING EDGES AND FUSEL AGE LOWER SKIN AND NO ABNORMALITIES WERE FOUND. ABNORMAL NOISE CHECK PERFROMED IAW DHL B727 MM 5-51-311. 2 L 7 3 4F A3WE 1996112500002 19961125 00002 1996 11 25 TWRA96315 4 19960917 A 2565 D330440103 SLIDE BOEING 747 747282B 1384860 NM L1 DOOR DEPLOYED A TWRA K NONE O OTHER NR NOT REPORTED 1 EA 15 611FF 0612 20502 INADVERTENTLY, L1 DOOR WAS OPENED WHILE IN AUTO MODE SLIDE DEPLOYED. PERFORMED INSPECTION PER 5-51-23. REPLACED SLIDE AT L21 DOOR PER TC 25-665-1L AND REPLACED DOOR ASSIST BOTTLE AT L1 DOOR PER WIC 25-615-4-2. OPERATIONAL CHECKED NORMAL. AIRCRAFT RETURN TO SERVICE. (M) 2 L 7 4 4F A20WE 1996112700001 19961127 00001 NM 1996 11 27 CA960507011 1 19960407 A 3222 29685 BEARING BFGOODRICH 314232 BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE NLG DISINTEGRATED W K NONE O OTHER TX TAXI/GRND HDL 1 CA 209 30692 (CAN)BEARING FAILURE, BEARING ON NOSE WHEEL ASSEMBLY DISINTEGRATED. WHEEL BEARING AND AXLE REPLACED. 2 L 7 2 4F 4 F RT A2NM E12EU 1996112700004 19961127 00004 SW 1996 11 27 CA960507018 1 19960423 A 7714 32005023 INDICATOR BELL 206 206L1 1182107 SW ALLSN 250C 250C30P 03013 GL NG TACH NOT INDICATING W A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CA CAE890130S (CAN)PILOT REPORTED ENGINE OUT HORN AND ENGINE OUT LIGHT. NG TACH INDICATOR NOT INDICATING. ALL OTHER GAUGES READING NOR MAL. 1 G 7 1 3U 3 U H2SW E1GL 1996112700005 19961127 00005 NM 1996 11 27 CA960508001 1 19960507 A 7930 310573501A REGULATOR DHAV DHC8 DHC8101 2809002 NM PWA PW120 PW123 NE NR 1 ENG OIL FLUCTUATING W A O UNSCHED LANDING OTHER O J OTHER WARNING INDICATION CL CLIMB 1 CA PCE120057 (CAN)ON TAKEOFF, OIL PRESSURE ON #1 ENGINE FLUCTUATED BELOW 40 PSI. WITH POWER LEVER AT FLIGHT IDLE AND CONDITION LEVER MOVING TO MINIMUM, OIL PRESSURE RETURNED TO NORMAL. WITH THE CONDITION LEVER TO MAX A ND POWER LEVER ADVANCING THROUGH 6 5 PERCENT TORQUE, FLUCTUATIONS REAPPEARED. POWER LEVER REDUCED BELOW 65 PECENT AND OIL PRESSURE STABILIZED. RETURNED TO AIRPORT WITH #1 ENGINE AT REDUCED POWER. OIL PRESSURE REGULATOR REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1996112700006 19961127 00006 NM 1996 11 27 CA960508002 1 19960507 A 2913 311435001 SEAL DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE ENG HYD PUMP LEAKING W A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 CA 120144 (CAN)AIRCRAFT RETUNED TO LAND WITH FLIGHT CREW REPORTING #2 ENGINE COWL GETTING COVERED IN OIL. ENGINE DRIVEN HYDRAULIC PUMP OIL SEAL LEAKING. 2 H 7 2 4T 4 T RT A13NM E20NE 1996112700007 19961127 00007 NE 1996 11 27 CA960508003 3 19960504 A 6110 N212585 PROPELLER HAMSTD 54H60117 LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL HAMSTD 54H 54H60117 NE #4 ENG FAILED W A E ENGINE SHUTDOWN O OTHER CR CRUISE 1 CA N212585 500859 N212585 (CAN)IN CRUISE, #4 PROPELLER PITCH LOCKED ENGINE SHUTDOWN. UNDER INVESTIGATION 2 H 7 4 4T 4 T A1SO E282 6 C P906 1996112700008 19961127 00008 SO 1996 11 27 CA960508005 1 19960503 A 6120 582855 VALVE HOUSING HAMSTD 54H60117 LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL HAMSTD 54H 54H60117 NE #4 ENG PROP MALFUNCTION W A O OTHER R PARTIAL RPM/PWR LOSS AP APPROACH 1 CA 765 N212585 500859 N212585 (CAN)ON APPROACH, TORQUE ON #4 ENGINE COULD NOT BE REDUCED BELOW 5000 LBS. ON LANDING, PROP FAILED TO GO INTO BETA RANGE , ENGINE SHUTDOWN. #4 VALVE HOUSING REPLACED. 2 H 7 4 4T 4 T A1SO E282 6 C P906 1996112700009 19961127 00009 EU 1996 11 27 CA960508006 1 19960430 A 5742 1415762930 BRACKET BRAERO 14157629402 BAG JETSTM JETSTM4112 EU MCAULY 2D34C B2D34C202 GL RH CONE CRACKED W K NONE E VIBRATION/BUFFET CL CLIMB 1 CA 950511 (CAN)VIBRATION FELT ON CLIMB OUT. INSPECTION REVEALED RH FAIRING (CONE) P/N 1417836-201 LOOSE. ATTACHMENT BRACKET (P/N 14157629-30 AND 32) WERE FOUND CRACKED, WITH LOOSE AND WORKING RIVETS. UPON REMOVAL O F THE BRACKETS ELONGATED HOLES, CH AFED AND CRACKED SKIN. REPAIRS AS PER JETSTREAM T.O.R. #0259 AND SRM 51-70-03. REST OF FLEET TO BE CHECKED. 1 L 7 2 4T RT A196 5 C P7EA 1996112700013 19961127 00013 EA 1996 11 27 CA960510103 2 19960509 A 8520 LW17760 CRANKSHAFT LYC TIO540J2BD PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA NR 2&3 CYL AREA BROKEN W A A E UNSCHED LANDING ENGINE SHUTDOWN Y ENGINE STOPPAGE CR CRUISE 1 CA 1549 L537161A (CAN)IN CRUISE, ENGINE RUNNING ROUGH AND LOSING POWER. ENGINE SHUTDOWN. MAINTENANCE FOUND THAT TURNING PROP BY HAND RESU LTED IN NO ROTATION ON 3,4,5 & 6 CYLINDERS INDICATING A BROKEN CRANKSHAFT. ENGINE ROUTED TO SHOP FOR FURTHER INVESTIGATI ON. 1 L 7 2 3O 3 O A20SO E14EA 1996112700021 19961127 00021 NM 1996 11 27 CA960513010 1 19960508 A 5542 SKIN DHAV 85540001001 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE RUDDER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 17118 120305 (CAN)CRACK FOUND AT LH FORE RUDDER SKIN AT REAR SPAR AND UPPER STIFFENER P/N 85540025. REPAIRED AS PER SRM 8-55-335. 2 H 7 2 4T 4 T RT A13NM E20NE 1996112700022 19961127 00022 NM 1996 11 27 CA960513011 1 19960508 A 2430 747 WIRE LUCAS 23088002A DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE START/GEN SYS CHAFED W H DEACTIVATE SYST/CIRCUITS H ELECT. POWER LOSS-50 PC CR CRUISE 1 CA 747 120305 (CAN)#1 DC GENERATOR FAILED AND #1 STARTER HAS TO BE MANUALLY DE-SELECTED. PROBLEM TRACED TO CHAFED WIRES #71D20 AND 78A 20 2 H 7 2 4T 4 T RT A13NM E20NE 1996112700023 19961127 00023 NM 1996 11 27 CA960513012 1 19960508 A 3246 L713049 BEARING DUNLOP 314353 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE #3 WHEEL DAMAGED W O OTHER E VIBRATION/BUFFET LD LANDING 1 CA 1983 120657 (CAN)WHEEL VIBRATION NOTED ON LANDING. #3 BRAKE AND WHEEL REPLACED DUE TO SOME DAMAGE FOUND IN THE INNER BEARING CAGE. I T IS FELT THE DAMAGE TO THE BEARING CAGE WAS NOT SUFFICIENT TO CAUSE NOTICEABLE VIBRA TION. VIBRATION LIKELY CAUSED BY A N IMBALANCE. 2 H 7 2 4T 4 T RT A13NM E20NE 1996112700024 19961127 00024 EU 1996 11 27 CA960513013 1 19960509 A 5610 NF20216245 WINSHIELD BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE CAPTAINS CRACKED W O OTHER O OTHER DE DESCENT 1 CA 1188 LF05567A (CAN)CAPTAIN'S "A" PANEL WINDSHIELD CRACKED ON DESCENT THROUGH 4,000 FEET. 2 H 7 4 4F 4 F RT A49EU E6NE 1996112700026 19961127 00026 EU 1996 11 27 CA960513026 1 19960513 A 5230 DOOR AIRBUS 310 A310324 3930206 EU PWA 4152 PW4152 NE CARGO UNSAFE WARNING W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 717738 (CAN)DURING TAKEOFF ROLL ECAM WARNING AND MASTER CAUTION INDICATING OPEN CARGO DOOR. TAKEOFF ABORTED. MAINTENANCE CHECK REVEALED BAGGAGE NOT SECURED BY CARGO NETS IN BULK CARGO HOLD. AS A RESULT DURING TAK EOFF ROLL THE BAGGAGE FELL ON CARG O DOOR RETRACT REELS CAUSING UPWARD PRESSURE ON CARGO DOOR CAUSING UNSAFE INDICATION. BAGGAGE SECURED NO FURTHER INDICAT IONS. MAINTENANCE INSPECTION INITIATED AT EVERY STATION AS PART OF PREFLIGHT TO ENSURE CARGO NETS SECURED BAGGAGE BEFORE CLOSING DOOR. 2 L 7 2 4F RT A35EU E24NE 1996112700027 19961127 00027 EU 1996 11 27 CA960513028 1 19960501 A 2620 WIRE BRAERO BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE OVERHEAD PANEL CHAFED W A F ACTIVATE FIRE EXT. A FLAME/FIRE IN INSP/MAINT 1 CA LF05482A (CAN)#4 ENGINE VIBRATING & BELCHING FLAMES FROM EXHAUST. DURING SHUTDOWN, CREW PULLED #4 FIRE HANDLE, #1 CIRCUIT AND FIR ED HALON BOTTLE. MAINTENANCE CONFIRMED THAT BOTTLE WAS DISCHARGED, HOWEVER, DISCHARGE DISC LENS ON NOSE COWL REMAINED "G REEN" AND PILOT DID NOT GET A MWS CAUTION ON FORWARD PANEL, NOR ANNUNCIATION OF "#1 USED" ON OVERHEAD ANNUNCIATOR PANEL. CIRCUIT BREAKER C20 "EXT #1 + APU USED ANNUNCIATOR" FOUND POPPED AND CHAFED WIRE FOR #4 FIRE HANDLE MICROSWITCH IN OVER HEAD EXTINGUISHER PANEL. REF: WIRING MANUAL 26-21-00, FIG.2, PAGE 101, MICROSWITCH "4W87" WIRING. 2 H 7 4 4F 4 F RT A49EU E6NE 1996112700028 19961127 00028 WP 1996 11 27 CA960514101 1 19960328 A 2710 54913801CT14008 CONTROL CABLE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE CONTROL COLUMN BROKEN W A K NONE O OTHER IN INSP/MAINT 1 CA 455931 (CAN)WHILE CYCLING AILERON CONTROLS FOR INVESTIGATION OF A HYDRAULIC LEAK, THE CAPTAINS CONTROL WHEEL WOULD NOT RETURN T O THE CENTRE POSITION. FURTHER INVESTIGATION REVEALED THE AILERON DOWN CABLE RUN #7 BROKE INSIDE THE CONTROL COLUMN. A L SO THE AILERON "UP" CABLE RUN #8 WAS FOUND CHAFED. CABLES REPLACED AND RIGGED AS PER M.M. 27-10-00. A FLEET CAMPAIG N WAS INITIATED TO INSPECT THE REMAINING DC10'S IN CANADIAN FLEET. 2 L 7 3 4F 4 F A22WE E23EA 1996112700029 19961127 00029 NM 1996 11 27 CA960514102 1 19960426 A 2910 6544510721 TUBE ASSEMBLY BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE A SYS HYD CHAFED W A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS J K WARNING INDICATION FLUID LOSS CL CLIMB 1 CA 707346 (CAN)AFTER DEPARTURE AIRCRAFT EXPERIENCED LOSS OF "A" SYSTEM HYDRAULICS AND RETURNED TO BLOCKS. "A" SYSTEM HYDRAULIC LIN E ABOVE THE L/H MAIN LANDING GEAR CHAFED THROUGH AND WEARING INTO THE 13TH STAGE RESERVOIR PRESSURE LINE. TEMPORARY REPA IR. LINE TO BE REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1996112700032 19961127 00032 EA 1996 11 27 CA960515001 1 19960502 A 2711 C6CW108727 ROD DHAV DHAV DHC6 DHC6300 EA PWA PT6 PT6A27 52043 EA AIL SERVO TAB CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 12145 PCE40610 (CAN)ON EMMA INSPECTION #28 THE AILERON SERVO TAB ROD ON THE R/H SIDE WAS FOUND TO HAVE A CRACK AT THE ADJUSTABLE END OF THE ROD. 1 H 7 2 3T 4 T A9EA E4EA 1996112700033 19961127 00033 SO 1996 11 27 CA960515008 2 19960116 A 8520 646437 CONNECTING ROD CESSNA 404 404CESSNA 2075901 CE CONT O520 GTSIO520M 17032 SO MCAULY #2 CYLINDER FRACTURED W E B A ENGINE SHUTDOWN EMER. DESCENT UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 CA 706 606587 (CAN)IN CRUISE, #2 ENGINE STOPPED SUDDENLY. #2 CONNECTING ROD FAILURE DUE TO BEARING SHELLS ROTATING IN BIG END AND OVER HEATING. 1 L 7 2 3O 3 O A25CE E7CE 1996112700034 19961127 00034 NM 1996 11 27 CA960515010 1 19960509 A 5541 85540127101 RIB DHAV 85540001003 DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE RUDDER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 14391 CAP0147 LH123046 (CAN)DURING REPAIR OF RUDDER TO REPLACE CENTRE HINGE FITTING, FOUND UPPER ADJACENT RIB CRACKED BETWEEN TWO RIVETS ALONG FORWARD RIVET ROW. REPAIR ACCOMPLISHED AS PER STRUCTURAL REPAIR MANUAL (SRM). 2 H 7 2 4T 4 T RT A13NM E20NE 1996112700035 19961127 00035 NM 1996 11 27 CA960515011 1 19960506 A 3231 83200506003 CONTROL CABLE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE LANDING GEAR BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 19847 LH121075 (CAN)FOR FLIGHT CREW TO DO AIRCRAFT ACCEPTANCE TEST MAIN LANDING GEAR DOORS MUST BE OPENED. WHEN FLIGHT CREW PULLED THE ALTERNATE EXTENSION CABLE THE CABLE BROKE. 2 H 7 2 4T 4 T RT A13NM E20NE 1996112700036 19961127 00036 NM 1996 11 27 CA960515014 1 19960505 A 2130 7612608 CONTROLER BOEING 727 727217 NM PWA JT8 JT8D17 52049 NE PRESS OUTFLOW INTERMITTENT W I CABIN DEPRESSURIZATION J WARNING INDICATION DE DESCENT 1 CA 688240 (CAN)PRESSURIZATION LOST ON DESCENT THROUGH 5,000 FEET.OUTFLOW VALVE MANUALLY CLOSED. PRESSURIZATION CONTROLLER REPLACED . 2 L 7 3 4F 4 F RT A3WE E2EA 1996112700037 19961127 00037 NM 1996 11 27 CA960515015 1 19960426 A 3246 2605759 WHEEL HALF BENDIX 26045611 BOEING 727 727217 NM PWA JT8 JT8D17 52049 NE DRIVE KEY LOBE CRACKED W O OTHER O OTHER IN INSP/MAINT 1 CA 306 HS440 688240 (CAN)BEFORE DEPARTURE #1 WHEEL ASSEMBLY FOUND DEFLATED. BOTH #1 AND #2 WHEELS REPLACED. SHOP INVESTIGATION REVEALED THAT THE INBOARD HALF WAS CRACKED AND LOST AIR PRESSURE. THE CRACK IS IN THE AREA AT THE END OF THE BRAKE DRIVE KEY SEAT RA DIUS. 2 L 7 3 4F 4 F RT A3WE E2EA 1996112700038 19961127 00038 WP 1996 11 27 CA960515101 1 19960407 A 2611 SMOKE DETECTOR DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE LAV.E ALARM ACTIVATED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 517866 (CAN)TAKEOFF REJECTED AFTER SMOKE DETECTOR SOUNDED IN LAV. E. SMOKE DETECTOR RESET. THERE WERE NO FURTHER INDICATIONS. B RAKE TEMP PEAKED AT 400 DEGREES "C". INVESTIGATION REVEALED ALARM ACTIVATED DUE TO PASSENGER SMOKING IN ADJACENT LAV. SM OKE DETECTORS OF LAVATORIES TESTED AND UNIT AT LAV. "E" REPLACED. ALSO REJECTED TAKEOFF AND HIGH ENERGY STOP INSPECTION CARRIED OUT. 2 L 7 3 4F 4 F A22WE E23EA 1996112700039 19961127 00039 NM 1996 11 27 CA960515102 1 19960501 A 5330 149T762331ACC PANEL BOEING 767 767375 NM 195CL MISSING W K NONE D INFLIGHT SEPARATION IN INSP/MAINT 1 CA (CAN) DURING LAYOVER CHECK FOUND FAIRING ACCESS PANEL 195CL MISSING. FOUR ANCHOR NUTS FOUND DAMAGED. REPAIRED. 2 L 7 2 4F RT A1NM 1996112700040 19961127 00040 WP 1996 11 27 CA960515501 1 19960404 A 2150 21700031 COOLING TURBINE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE CABIN AIR FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA P657342D (CAN)DURING OPERATION OF LEFT AIR CONDITIONING SYSTEM ON GROUND, CABIN FILLED WITH SMOKE SUFFICIENT TO CAUSE SMOKE ALARM DETECTOR TO ACTIVATE. COOLING TURBINE REPLACED AND BOTH COALESCER BAGS. 2 L 7 2 4F 4 F A6WE E2EA 1996112700041 19961127 00041 NM 1996 11 27 CA960515502 1 19960404 A 5753 BAC1328AK04030 DOOR BOEING 767 767333 NM PWA 4060 PW4060 52119 NE LT TE FLAP INBD MISSING W K NONE F FLT CONT AFFECTED TX TAXI/GRND HDL 1 CA P724695 (CAN)PRIOR TO DEPARTURE CREW FOUND LEFT WING TRAILING EDGE FLAP INBOARD SIDE BODY DOOR MISSING. REPAIRED AS PER M.M. 27- 51-03-20. 2 L 7 2 4F 4 F RT A1NM E24NE 1996112700042 19961127 00042 EA 1996 11 27 CA960515503 1 19960416 A 3234 CONTROL HANDLE CNDAIR CL600 CL6002B19 EA MLG FAILED W O OTHER J WARNING INDICATION CL CLIMB 1 CA 1111 (CAN)UNABLE TO RETRACT LANDING GEAR AFTER SEVERAL ATTEMPTS. FOUND LANDING GEAR CONTROL HANDLE AT FAULT. 2 L 7 2 4F RT A21EA 1996112700043 19961127 00043 EU 1996 11 27 CA960517102 1 19960511 A 2610 SMOKE ALARM SYS AIRBUS 320 A320211 3930320 EU AFT CARGO ACTIVATED W E D F ENGINE SHUTDOWN RETURN TO BLOCK ACTIVATE FIRE EXT. J WARNING INDICATION TX TAXI/GRND HDL 1 CA (CAN)AFTER ENGINE START, ECAM MESSAGE, AFT CARGO SMOKE ALARM ACTIVATED. FIRE EXTINGUISHER BOTTLED DISCHARGED. MAINTENANC E INVESTIGATION UNABLE TO FIND EVIDENCE OF SMOKE OR FIRE IN AFT CARGO COMPARTMENT. FU RTHER INVESTIGATION REVEALED SMOKE /FUMES FROM AIRCRAFT ENGINE ENTERED CARGO COMPARTMENT WHEN CARGO DOOR WAS OPEN CAUSING ALARM TO BE ACTIVATED. 2 L 7 2 4F RT A28NM 1996112700044 19961127 00044 WP 1996 11 27 CA960521001 2 19960509 A 7240 31032153 INNER RING SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP COMBUST CHAMBER CRACKED W A E A ENGINE SHUTDOWN UNSCHED LANDING G Y MULTIPLE FAILURE ENGINE STOPPAGE CL CLIMB 1 CA 3194 11392 P54082 (CAN) ONE MINUTE AFTER TAKEOFF, THE LEFT ENGINE WAS SHUT DOWN AND AUTO FEATHERED. THE DISASSEMBLY AND EXAMINATION OF THE ENGINE REVEALED THE REAR TURBINE CARRIER CRACKED, ALL FIRST STAGE TURBINE BLADES BROKEN. COMBUSTION CHAMBER INNER RING CRACKED 350 DEGREES. THE COMBUSTION CHAMBER INNER RING CRACKED RADIALLY APPROXIMATELY 90 PERCENT OF THE CIRCUMFERENCE. T HIS ALLOWED HOT COMBUSTION GASES TO IMPINAGE UPON THE TRANSITION LINER CAUSING BURN THROUGH, SUBSEQUENT OVERHEATING AND FAILURE OF THE SECOND STAGE COMPRESSOR. PIECES OF LINER ETC. DAMAGED THE TURBINE WHEELS. THE FINAL RESULT WAS SUDDEN FAI LURE. 2 L 7 2 4T 4 T RT A8SW E4WE 1996112700055 19961127 00055 EU 1996 11 27 CA960522001 1 19960425 A 3232 1252515 DOOR ACTUATR FOKKER F28 F28MK1000 4990808 EU RT MLG LEAKING W A D UNSCHED LANDING RETURN TO BLOCK J K WARNING INDICATION FLUID LOSS TO TAKEOFF 1 CA 39647 (CAN)AFTER TAKEOFF CREW NOTICED R/H MAIN LANDING GEAR LIGHT REMAINED ON, SHORTLY AFTERWARDS MLG FELL OUT OF HOLE. ALTERN ATE EXTENSION CARRIED OUT AND RETURNED TO BLOCKS. ON LANDING CREW NOTICED THE UTILITYSYSTEM WAS DELETED OF FLUID, AIRCRA FT TOWED OFF RUNWAY. R/H FORWARD DOOR ACTUATOR WAS LEAKING, REPLACED. 2 L 7 2 4F RT A20EU 1996112700056 19961127 00056 NE 1996 11 27 CA960522002 2 19960508 A 8530 CYLINDER DOUG DC3 DC3CS1C3G 3021458 WP PWA R1830 R183092 52020 NE NR 1 EXH EAR CRACKED W A UNSCHED LANDING E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CL CLIMB 1 CA 41 CP360587 (CAN)SHORTLY AFTER TAKEOFF, #1 ENGINE BEGAN TO SHAKE AND MISS. AIRCRAFT RETURNED WHERE #1 CYLINDER WAS FOUND CRACKED ACR OSS THE EXHAUST EAR. THIS CYLINDER APPEARS TO HAVE BEEN PREVIOUSLY REPAIRED BY WELDIN G. 2 L 7 2 4R 4 R A669 5E4 1996112700058 19961127 00058 EA 1996 11 27 CA960522007 1 19960514 A 2730 C3CF1935 CONTROL CABLE DHAV DHC3 DHC3 2800202 EA ELEVATOR CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 17907 (CAN) TWO ELEVATOR CABLES RUNNING IN THE FUSELAGE LOWER RIGHT HAND SECTION UNDER THE FLOOR FOUND BADLY CORRODED AT STA. 310, AFT OF REAR BAGGAGE COMPARTMENT BULKHEAD. OTHER P/N C3CF195-7. THIS AREA IS ALSO BELOW AND AFT OF BATTERY RACK. BOT H CABLES REPLACED. THEY WERE NOT FRAYED. AIRCRAFT OPERATED IN SALT WATER FOR LAST THREE YEARS. BATTERY ALSO LOCATED IN A REA. 1 H 7 1 3R A815 1996112700059 19961127 00059 EA 1996 11 27 CA960522008 1 19960513 A 2710 C2CF1197 LINKS X1282 DHAV DHC2 DHC2MK1 2800102 EA PWA R985 R985AN14B 52008 NE AIL CONTROL DAMAGED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 12760 JP215208 (CAN) INSPECTION OF FLIGHT CONTROLS IN ACCORDANCE WITH SB A2/51. SPECIAL INSPECTION OF LINK STOP IN AILERON CONTROL CHAI N. LINKS #C2CF1197 AND C2CF1198 HAVE BEEN DAMAGED BY MAINTENANCE PERSONNEL, PROBABLY WITH VISE GRIP PLIERS. VERY DEEP SC RATCHES FOUND ON THE SHANK AREA OF ONE OF THE LINKS. BOTH LINKS REPLACED. 1 H 7 1 3R 3 R A806 5E1 1996112700060 19961127 00060 SO 1996 11 27 CA960522009 2 19960503 A 8530 CYLINDER CESSNA 150 150M 2071830 CE CONT O200 O200A 17020 SO NR 2 RKR BOSS CRACKED W A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 CA 1120 255856A48 (CAN)IN THE CIRCUIT, PILOT REPORTED AN ENGINE VIBRATION. #2 CYLINDER ROCKER SHAFT BOSS CRACKED. 1 H 7 1 3O 3 O 3A19 E252 1996112700063 19961127 00063 NM 1996 11 27 CA960524002 1 19960522 A 2920 82970010401 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE #2 NACELLE HYD CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 120056 (CAN) HYDRAULIC LEAK IN #2 NACELLE DOWN PRESSURE TUBE FROM A PIN HOLE OR CRACK. 2 H 7 2 4T 4 T RT A13NM E20NE 1996112700064 19961127 00064 NM 1996 11 27 CA960524003 1 19960522 A 2910 82970010121 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE #1 ENG NACELLE LEAKING W O OTHER K FLUID LOSS IN INSP/MAINT 1 CA 120083 (CAN) HYDRAULIC LEAK FROM #1 ENGINE NACELLE. HYDRAULIC LINE BETWEEN ANTI-SKID CONTROL AND RETURN MANIFOLD. 2 H 7 2 4T 4 T RT A13NM E20NE 1996112700065 19961127 00065 EA 1996 11 27 CA960524004 1 19960522 A 7500 BLEED AIR DHAV DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE #1 ENGINE OIL CONTAMINATED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA 9709 123136 (CAN) FLIGHT CREW REPORTED WHEN #1 ENGINE BLEED AIR SELECTED ON CABIN FILLS WITH HAZE OF SMOKE AND FUMES. PROBLEM TRACED TO OIL IN BLEED AIR FROM #1 ENGINE. ENGINE REPLACED. PROBLEM TO BE CHECKED. 2 H 7 2 4T 4 T RT A13NM E20NE 1996112700066 19961127 00066 EU 1996 11 27 CA960524005 1 19960409 A 2421 740119F IDG AIRBUS 320 A320211 3930320 EU #1 ENGINE PISTON SHATTERED W D H RETURN TO BLOCK DEACTIVATE SYST/CIRCUITS J WARNING INDICATION TO TAKEOFF 1 CA (CAN) REJECTED TAKEOFF DUE TO #1 I.D.G. LOW OIL PRESSURE. ECAM MESSAGE. AIRCRAFT RETURNED TO RAMP. I.D.G. REPLACED. UPON INVESTIGATION FOUND 2 PISTONS IN VARIABLE DISPLACEMENT PUMPS (1 INCH EACH PUMP) SHATTERED. MAIN SPLINED DRIVE SHAFT SHE ARED. UNABLE TO DETERMINE CAUSE OF FAILURE FOR DRIVE SHAFT. 2 L 7 2 4F RT A28NM 1996112700067 19961127 00067 NM 1996 11 27 CA960524006 1 19960408 A 7931 SRL0C4N GAUGE BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE ENG OIL PRESS FAILED W A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CA 707370 (CAN)ENGINE POWER REDUCED AND AIR TURN BACK DUE TO ENGINE OIL PRESSURE INDICATING IN THE AMBER RANGE. MAINTENANCE CONFIR MED AS GAUGE FAILURE. 2 L 7 2 4F 4 F A16WE E2EA 1996112700068 19961127 00068 1996 11 27 CA960524007 4 19960501 A 2565 5A28514 REGULATOR BFGOODRICH 7A147911 BOEING 747 747475 NM SLIDE RAFT OUT OF TOLERANCE W K NONE L NO TEST IN INSP/MAINT 1 CA 0307 (CAN)DURING A SAMPLE DEPLOYMENT OF A SLIDE/RAFT FROM A 747 PASSENGER DOOR, THE SLIDE/RAFT FAILED TO DEPLOY. THE INFLATIO N CYLINDER REGULATOR WAS SENT TO THE MANUFACTURER FOR EXAMINATION. THE EXAMINATION SH OWED THAT THE INFLATION CYLINDER R EGULATOR AND TEMPERATURE COMPENSATOR WERE OUT OF TOLERANCE. THIS INFLATION HAD ONE PREVIOUS INFLATION. 2 L 7 4 4F RT A20WE 1996112700069 19961127 00069 NM 1996 11 27 CA960524009 1 19960410 A 2612 65528087 MODULE FENWAL 65528087 BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE FIRE DET FAILED W C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CA D00048 707350 (CAN)ABORTED TAKEOFF DUE TO FIRE WARNING ON FORWARD PANEL. AIRCRAFT RETURNED TO GATE. FDU, DIMMER UNIT AND ACCESSORY COM PARTMENT OVERHEAT MODULE REPLACED. ACCESSORY COMPARTMENT OVERHEAT MODULE FAILED CURE INSPECTION. FDU AND DIMMER UNIT FO UND NO FAULT ON SHOP CHECK. 2 L 7 2 4F 4 F A16WE E2EA 1996112700070 19961127 00070 EU 1996 11 27 CA960524010 1 19960516 A 2810 HIGH LOCK BOLTS BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE LH WING ROOT LOOSE W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 17749 LF05567A (CAN) FUEL LEAK NOTED AT LEFT HAND WING ROOT AT REAR SPAR.HIGH LOCK BOLTS "A", "B", "C", REPLACED WITH MS21250 BOLTS AS PER HC536H9156. 2 H 7 4 4F 4 F RT A49EU E6NE 1996112700071 19961127 00071 NM 1996 11 27 CA960524011 1 19960516 A 2435 03601023 BEARING LUCAS 23088002A DHAV DHC8 DHC8101 2809002 NM PWA PW120 PW123 NE NR 2 START/GEN FAILED W O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION IN INSP/MAINT 1 CA 8010 1048 607A 123138 (CAN) #2 DC GENERATOR CAUTION LIGHT ON. UNABLE TO RESET. STARTER GENERATOR REPLACED. BEARING SUFFERED PREMATURE FAILURE. 2 H 7 2 4T 4 T RT A13NM E20NE 1996112700075 19961127 00075 NE 1996 11 27 CA960524015 2 19960509 A 7261 657262 OIL SYSTEM PWA JT8D7B BOEING 727 72725 1384006 NM PWA JT8 JT8D7B 52053 NE NR 2 ENG OIL LEAK W A E UNSCHED LANDING ENGINE SHUTDOWN J K WARNING INDICATION FLUID LOSS CL CLIMB 1 CA 45470 657262 657262 (CAN)ON CLIMBOUT, #2 ENGINE OIL PRESSURE DROPPING, ENGINE SHUTDOWN INTERNAL OIL LEAK TOWARD THE AFT OF ENGINE. FOLLOW- UP COMING 2 L 7 3 4F 4 F A3WE E2EA 1996112700078 19961127 00078 EA 1996 11 27 CA960524019 2 19960503 A 8520 69796 DOWEL LYC LW13812 CESSNA 172 172M 2072418 CE LYC O320 O320E2D 41508 EA #2 MAIN BEARING SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA 4498 792 L4124727A (CAN)METAL CONTAMINATION IN THE OIL FILTER AT 50 HOUR INSPECTION. SOURCE OF METAL IS #3 CONROD BEARING AND #2 MAIN BEARI NG. MAIN BEARING DOWEL PIN SEHARED AND CAUSED F.O.D. TO MAIN AND CONROD BEARINGS. ALL MAIN BEARING DOWELS RENEWED. 1 H 7 1 3O 3 O NT 3A12 E274 1996112700079 19961127 00079 NM 1996 11 27 CA960524020 1 19960413 A 6120 87600518001 CONTROL CABLE DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE FIREWALL PULLEY FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA PCE124460 (CAN)ON DAILY INSPECTION OF ENGINE, #1 ENGINE PROP/CONDITION CABLE CHAFED AND FRAYED AT ENGINE FIRE WALL PULLEY. LOWER C ABLE P/N 87600518-001 REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1996112700080 19961127 00080 EU 1996 11 27 CA960524021 1 19960318 A 2841 INDICATOR FOKKER F28 F28MK1000 4990808 EU FUEL QTY MALFUNCTION W A UNSCHED LANDING O OTHER CR CRUISE 1 CA (CAN)26 MINUTES AFTER TAKEOFF AT FL330 A 1100 LB FUEL IMBALANCE WAS DETECTED. CROSS BALANCING WAS IMPLEMENTED, LEFT AND RIGHT COUNTERS SHOWING EQUAL AMOUNTS OF FUEL IN BOTH TANKS. AIRCRAFT DIVERTED, LANDEDWITHOUT INCIDENT. TANKS WERE DIPPED AND A 2000 LB DIFFERENCE WAS DETECTED. FUEL QUANTITY GAUGE REPLACED. 2 L 7 2 4F RT A20EU 1996112700081 19961127 00081 CE 1996 11 27 CA960524022 1 19960510 A 5712 RIB CESSNA 421 421B 2076014 CE CONT O520 GTSIO520H 17032 SO MCAULY 3AF34C 3AF34C92 GL L/H WING TIP RIVETS SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA 3960 600100 779641 (CAN) LEFT WING OUTBOARD END RIB JOINT TO REAR WING SPAR ATTACH POINT SHEARED BOTH RIVETS. THIS PERMITTED TIP TANK VERTI CAL MOVEMENT WHICH LED TO CRACK IN WING SKIN. THIS IDENTICAL PROBLEM IS REPORTED TO HAVE ALSO HAPPENED IN A 414 AND THE SUBMITTER SUGGESTS THAT IT MAY BE POSSIBLE ON ALL CESSNA TIP TANK AIRCRAFT. THE SUBMITTER ALSO SUGGESTS THE CAUSE MAY HA VE BEEN FROM A HARD LANDING. 1 L 7 2 3O 3 O A7CE E7CE 5 C P22EA 1996112700083 19961127 00083 EA 1996 11 27 CA960524024 1 19960508 A 3060 KCD4N RELAY DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE PROP HEAT STUCK CLOSED W A H DEACTIVATE SYST/CIRCUITS M P OVER TEMP NO WARNING INDICATION DE DESCENT 1 CA 11027 123018 (CAN) PROP HEAT RELAY STUCK CLOSED, ALLOWING AC POWER TO PROP HEAT ALL THE TIME. 2 H 7 2 4T 4 T RT A13NM E20NE 1996112700084 19961127 00084 NM 1996 11 27 CA960524025 1 19960509 A 3340 A35541 SOCKET GRIMES DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE WING INSPECTION SHORTED W K NONE O OTHER IN INSP/MAINT 1 CA 123046 (CAN) RIGHT WING INSPECTION LIGHT CIRCUIT BREAKER FOUND POPPED. INVESTIGATION REVEALED A SHORT IN RIGHT LOWER NACELLE CO WLING WING INSPECTION LIGHT SOCKET. SOLDER FROM CONTACT ASSEMBLY CENTRE CONTACT FOUND MELTED AND HAD FLOWED ACROSS TO SO CKET BASE ASSEMBLY GROUND. 2 H 7 2 4T 4 T RT A13NM E20NE 1996112700085 19961127 00085 EA 1996 11 27 CA960524028 2 19960515 A 7322 A45508 FCU BENDIX 324475520 BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA NR 2 ENG LOW POWER W A K NONE R PARTIAL RPM/PWR LOSS CR CRUISE 1 CA A45508 PCE80636 (CAN)#2 ENGINE UNABLE TO REACH MAXIMUM CRUISE TORQUE ABOVE 18,000 FEET, ALL ENGINE PARAMETERS NORMAL ON GROUND FCU CHAN GED. SAME PROBLEM AGAIN ABOVE 15,000 FEET: NG 3 5 PERCENT LOW, TORQUE 150 LBS LOW ANDTHE TOP ONE INCH OF THROTTLE MOVEME NT HAD NO EFFECT ON POWER. ALL AIR AND FUEL LINES INSPECTED, ENGINE BOROSCOPED AND BLEED VALVES CHECKED OK. FCU AGAIN RE PLACED, ENGINE PERFORMANCE NORMAL. 1 L 7 2 4T 4 T A24CE E4EA 1996112700089 19961127 00089 NE 1996 11 27 CA960527009 2 19960518 A 7230 ANULUS SEAL RROYCE BOEING 757 75723A 1384967 NM RROYCE RB211 RB211535E4 54555 NE BETWEEN N1 BLADE OUT OF POSITION W A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 CA 3649 30863 (CAN)IN CRUISE DURING ICING CONDITIONS, #1 ENGINE VIBRATION WENT UP TO 2.5 UNITS. MAINTENANCE FOUND ANULUS FILLER SEAL O UT OF POSITION BETWEEN N1 BLADES. SEAL RESEATED PER MAINTENANCE MANUAL. 2 L 7 2 4F 4 F RT A2NM E12EU 1996112700091 19961127 00091 SW 1996 11 27 CA960527011 1 19960514 A 3213 ED124061 TORQUE LINKSHAFT GULSTM 690TP 690D 3970405 SW GARRTT TPE331 TPE3315 01514 WP ROTOL R306 R306382F7 GL R/H MLG BROKEN W A O OTHER O OTHER LD LANDING 1 CA P40493 106746 (CAN)ON ROLL OUT ON LANDING, THE AIRCRAFT'S R/H TIRE BLEW. FURTHER INSPECTION REVEALED THAT THE TORQUE LINK SHAFT WAS AL SO BROKEN. 1 H 7 2 3T 4 T 2A4 E4WE 6 C P8EU 1996112700092 19961127 00092 NM 1996 11 27 CA960528101 1 19960516 A 2432 TYPECA72720 CELL MARATHON 25582003 BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE BATTERY MELTED W K NONE O B OTHER SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA 2803 2775 9402058 708821 (CAN) BATTERY CHARGER CIRCUIT BREAKER POPPED AND BATTERY HOT TO TOUCH. ON GROUND A VERY NOTICEABLE ELECTRICAL SMELL WAS NOTED. REPLACED 60 AMP BATTERY CHARGER. SMELL STILL EXISTS NEAR BATTERY. BATTERY ALSO RE PLACED. 2 L 7 2 4F 4 F A16WE E2EA 1996112700093 19961127 00093 NM 1996 11 27 CA960528102 1 19960516 A 2530 3510001601 COFFEE MAKER AIRCRFTPRDTS 3510001601 BOEING 767 767375 NM AFT GALLEY BURNT W O H OTHER DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA 0104 (CAN)AFT GALLEY COFFEE MAKER SPARKING AND FLASH FOLLOWED BY SMOKE. CBS PULLED AND UNIT REPLACED. 2 L 7 2 4F RT A1NM 1996112700096 19961127 00096 WP 1996 11 27 CALA9601683 1 19961118 A 3350 110049 FUSE DOUG DC9 DC982 3022082 WP GALLEY DR BLOWN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 76823 49483 INSPECTION FOUND THE EMERGENCY EXIT LOCATOR SIGN AT AFT GALLEY DOOR INOPERATIVE. MAINTENANCE FOUND A BLOWN FUSE IN POWE R SUPPLY. THE FUSE WAS REPLACED AND OPERATION OF THE EXIT SIGN WAS RESTORED. 2 L 7 2 4F A6WE 1996112700097 19961127 00097 WP 1996 11 27 CALA9601684 1 19961118 A 3350 41B004AD073 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 76823 49483 INSPECTION FOUND THE CEILING EMERGENCY LIGHT INOPERATIVE AT ROW 28 TO 30. THE BATTERIES WERE REPLACED AND OPERATION OF THE LIGHT WAS RESTORED. 2 L 7 2 4F A6WE 1996112700098 19961127 00098 WP 1996 11 27 CALA9601685 1 19961118 A 3350 41B004AD073 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 76823 49483 INSPECTION FOUND THE EMERGENCY CEILING LIGHT INOPERATIVE AT ROW 12 TO 16. THE BATTERIES WERE REPLACED AND OPERATION OF THE LIGHT WAS RESTORED. 2 L 7 2 4F A6WE 1996112700099 19961127 00099 NM 1996 11 27 CALA9601686 1 19961031 A 2782 ACTUATOR MOUNT BOEING 727 727243 138408D NM NR 2 LE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND A .5 INCH CRACK IN NR 2 KREUGER FLAP ACTUATOR MOUNT. THE CRACK WAS LOCATED BELOW AND FORWARD OF INBOAR D AND OUTBOARD LOWER MOUNT BOLTS. THE CRACK WAS STOP DRILLED, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53- 10-1 AND 51-40-3. 2 L 7 3 4F RT A3WE 1996112700100 19961127 00100 NM 1996 11 27 CALA9601687 1 19961106 A 5330 SKIN BOEING 727 727243 138408D NM BS 970 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND SKIN CORRODED UNDER WEB IN AFT CARGO COMPARTMENT AT STA 970, STRINGER 28L. THE CORRODED AREA OF SKIN W AS CUT OUT, FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3. 2 L 7 3 4F RT A3WE 1996112700101 19961127 00101 NM 1996 11 27 CALA9601688 1 19961031 A 5730 SKIN BOEING 727 727243 138408D NM WING LE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND A .5 INCH CRACK IN WING LEADING EDGE SKIN AT TOP OF CUTOUT FOR NR 3 SLAT OUTBOARD TRACK. THE CRACK WAS STOP DRILLED, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-30-4. 2 L 7 3 4F RT A3WE 1996112700102 19961127 00102 NM 1996 11 27 CALA9601689 1 19961105 A 5313 STRINGER BOEING 727 727243 138408D NM BS 965 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND STRINGER 28L CORRODED AT STA 965 IN AFT CARGO COMPARTMENT. THE CORRODED SECTION OF STRINGER WAS CUT OU T, A REPLACEMENT STRINGER AND SPLICE WERE FABRICATED AND INSTALLED IAW SRM 53-10-3. 2 L 7 3 4F RT A3WE 1996112700103 19961127 00103 WP 1996 11 27 CALA9601690 1 19961119 A 2433 6RW176YN3 TR UNIT DOUG DC9 DC932 3022066 WP E/E COMPT FAILED A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 09 17557 47424 WHEN CREW ENTERED AIRCRAFT AT GATE, WITH EXTERNAL POWER ON, THEY NOTICED SMOKE IN COCKPIT AND CABIN. THE NR 2 TRANSFORM ER RECTIFIER CIRCUIT BREAKER WAS POPPED AND WOULD NOT RESET. EXAMINATION OF THE NR 2 TRANSFORMER RECTIFIER FOUND IT BUR NT. THE NR 2 TRANSFORMER RECTIFIER WAS REMOVED AND REPLACED, OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F A6WE 1996112700104 19961127 00104 NM 1996 11 27 CALA9601691 1 19961031 A 3350 20131A BATTERY PACK BOEING 727 727243 138408D NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND EMERGENCY PATH LIGHTS INOPERATIVE AT ROW 12 AND ROW 15 TO 23. A BROKEN WIRE WAS REPAIRED IN FORWARD SE CTION AND THE FORWARD BATTERY PACK WAS REPLACED. 2 L 7 3 4F RT A3WE 1996112700105 19961127 00105 NM 1996 11 27 CALA9601692 1 19961101 A 5330 SKIN BOEING 727 727243 138408D NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND A .5 AND 1 INCH CRACK IN RT FUSELAGE SKIN JUST BELOW PANEL NR 9516, RT SIDE NR 2 ENGINE INLET. THE CRA CKS WERE STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-30-3. 2 L 7 3 4F RT A3WE 1996112700106 19961127 00106 NM 1996 11 27 CALA9601693 1 19961031 A 5753 SKIN BOEING 727 727243 138408D NM LT TE FOREFLAP DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND TOP OF LT INBOARD FOREFLAP DELAMINATED AT MID SPAN. THE DELAMINATED AREA WAS CUT OUT, NEW CORE, FILLER AND DOUBLER WERE FABRICATED AND A HOT BOND REPAIR WAS ACCOMPLISHED IAW SRM 51-40-6. 2 L 7 3 4F RT A3WE 1996112700107 19961127 00107 WP 1996 11 27 9624739951 1 19961114 A 3260 SWITCH PACK DOUG DC9 DC932 3022066 WP RT THROTTLE FAILED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 9347 45827 UPON RAISING GEAR AFTER TAKEOFF, GEAR WARNING HORN SOUNDED CONTINUOUSLY. RECYCLED GEAR SEVERAL TIMES, BOTH CLEAN AND FL APS 15. CYCLED THROTTLES UP AND PUSHED HORN OFF BUTTON, HORN CEASED. FLIGHT CONTINUED TO MSP AND LANDED WITHOUT INCIDE NT. MAINTENANCE CHANGED THROTTLE SWITCH PACK FOR RIGHT THROTTLE, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996112700108 19961127 00108 WP 1996 11 27 9624749983 1 19961117 A 3350 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 983US 47282 DURING LINE CHECK, FOUND THAT THE LAST FOUR ROWS OF EMERGENCY SEAT LIGHTS AND THE AFT LEFT LAV EMERGENCY LIGHT WERE INOP ERATIVE. REPLACED THE BATTERY PACK (P/N 9133-90368-1) AND POWER SUPPLY (P/N BC5-0447-907, CHECKED OK. 2 L 7 2 4F A6WE 1996112700109 19961127 00109 EU 1996 11 27 9624873242 1 19961119 A 3350 321454 POWER SUPPLY AIRBUS 320 A320212 EU CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 342NW 12672 7991 381 DURING LINE MAINTENANCE, THE EMERGENCY LIGHT ASSOCIATED WITH EPSU 11WL WAS INOPERATIVE. REPLACED EPSU, OPERATIONAL CHEC K OK. 2 L 7 2 4F RT A28NM 1996112700110 19961127 00110 NM 1996 11 27 9624882705 1 19961115 A 2781 SWITCH BOEING 727 727225 1384077 NM NR 4 LE FLAP FAILED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 802EA 22433 DURING TAKEOFF, THE NR 4 LEADING EDGE SLAT INDICATED STILL DOWN ON SLAT/FLAP RETRACTION. AIRCRAFT RETURNED TO MSP AND L ANDED WITHOUT INCIDENT. REPLACED THE NR 4 LEADING EDGE SWITCH S-205. PERFORMED OPERATIONAL CHECK OF SLAT/FLAP INDICATI ON SYSTEM, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996112700111 19961127 00111 NM 1996 11 27 9624896716 1 19961116 A 7722 EGT WIRE BOEING 747 747251F 1384898 NM PWA JT9 JT9D7F 52054 NE NR 1 ENGINE FAILED A A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 616US 21120 62954 DURING TAKEOFF ROLLOUT, THE NR 1 ENGINE EGT GAUGE INDICATED APPROXIMATELY 400 DEGREES WHILE OTHERS INDICATED 750 DEGREES . THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A PREVIOUS LY REPAIRED WIRE FORWARD OF A JUNCTION BOX MELTED. REPAIRED THE WIRE AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4 F A20WE E20EA 1996112700112 19961127 00112 WP 1996 11 27 9624909752 1 19961119 A 3260 SWITCH BRACKET DOUG DC9 DC941 302207N WP LT MLG FAILED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 752NW 47116 AFTER TAKEOFF AND GEAR RETRACTION, LEFT GEAR UNSAFE LIGHT ILLUMINATED. PERFORMED COM PROCEDURE AND GEAR UPLATCH CHECK, GEAR DOOR LIGHT MOMENTARILY ILLUMINATED THEN EXTINGUISHED ALONG WITH GEAR UNSAFE LIGHT. FLIGHT RETURNED TO MSP AND LAND ED WITHOUT INCIDENT. MAINTENANCE ADJUSTED BRACKET AND ROLLER AND LINK ASSEMBLY, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996112700113 19961127 00113 NM 1996 11 27 9624915501 1 19961116 A 3350 POWER SUPPLY BOEING 727 727251 138408H NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 501US 23190 DURING PREFLIGHT, FOUND DOOR 4L EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY POWER SUPPLY, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996112700114 19961127 00114 NM 1996 11 27 9624922761 1 19961115 A 3350 BATTERY PACK BOEING 727 7272M7 138407S NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 721RW 21200 DURING PREFLIGHT, FOUND MAIN CABIN DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY BATTERY PACK, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996112700115 19961127 00115 1996 11 27 9624939759 4 19961119 A 3425 5223700004 ADI INDICATOR DOUG DC9 DC941 302207N WP LT COCKPIT FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 759NW 33522 1545 47287 AFTER TAKEOFF, CAPTAIN'S ATTITUDE GYRO CIRCUIT BREAKER POPPED. RESET AND POPPED AGAIN. FLIGHT RETURNED TO DTW AND LAND ED WITHOUT INCIDENT. REPLACED NR 1 ADI AND NR 1 AMPLIFIER, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996112700116 19961127 00116 WP 1996 11 27 9624869913 1 19961114 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 680 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 963N 47415 DURING H-CHECK, FOUND A CRACK IN THE LEFT OUTBOARD SEAT TRACK SUPPORT FITTING AT FS 680. REPLACED FITTING PER SRM 51-30 -5. 2 L 7 2 4F A6WE 1996112700117 19961127 00117 NM 1996 11 27 9624776622 1 19961031 A 5320 ANGLE BOEING 747 747251B 1384892 NM BS 460 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 622US 21704 DURING P-CHECK, FOUND A CRACK IN THE 1L MAIN ENTRY DOOR CUTOUT UPPER SILL OUTBOARD ANGLE BS 460. REPAIRED SILL (P/N 65B 08301-1) PER EA 66-120437. 2 L 7 4 4F A20WE 1996112700118 19961127 00118 EU 1996 11 27 9624783205 1 19961109 A 5313 STRINGER AIRBUS 320 A320211 3930320 EU BS 32571 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 305US 41 DURING 1C1 CHECK, FOUND CORROSION ON THE LBL 1162 FLOOR STRINGER AT FRAME 68. REPAIRED STRINGER PER EA 32-106179. 2 L 7 2 4F RT A28NM 1996112700119 19961127 00119 EU 1996 11 27 9624793222 1 19961110 A 5315 FLOORBEAM AIRBUS 320 A320211 3930320 EU BS 8077 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 322US 263 DURING 1L CHECK, FOUND CORROSION ON THE FRAME 20 FLOORBEAM AT RBL 1640. REPAIRED BEAM (P/N D53112785201) PER EA 32-1061 67. 2 L 7 2 4F RT A28NM 1996112700120 19961127 00120 WP 1996 11 27 9624809982 1 19961116 A 5753 VANE DOUG DC9 DC932 3022066 WP RT TE FLAP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 982US 45790 DURING LINE CHECK, FOUND A BROKEN CASTING IN THE RIGHT WING AFT MOVEABLE VANE INBOARD END. REPLACED VANE PER MM 27-51-2 PG 505. 2 L 7 2 4F A6WE 1996112700121 19961127 00121 WP 1996 11 27 9624819996 1 19961118 A 5312 BULKHEAD FITTING DOUG DC9 DC931 3022065 WP BS 756 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8932E 47141 DURING H-CHECK, FOUND CRACKS IN FS 756 CENTER LINE BULKHEAD FITTINGS: SECOND, THIRD AND FOURTH FROM THE TOP. REPLACED ALL FITTINGS (P/N 9958212-37) PER SRM 51-30-5. 2 L 7 2 4F A6WE 1996112700122 19961127 00122 WP 1996 11 27 9624829923 1 19961118 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 605 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 927RC 47469 DURING H-CHECK, FOUND CORROSION ON THE KEEL LONGERON END FITTINGS 29L AND 29.5L, FORWARD END FS 605. REPLACED FITTINGS PER SRM 51-30-5 AND DWG 5911418-505. 2 L 7 2 4F A6WE 1996112700123 19961127 00123 NM 1996 11 27 9624836608 1 19961118 A 5320 FITTING BOEING 747 747151 1384891 NM BS 2355 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 608US 19785 DURING P-CHECK, FOUND CORROSION IN THE FLOOR STRUCTURE TIE-DOWN FITTING AT BS 2355, LBL 15. REPLACED FITTING. 2 L 7 4 4F A20WE 1996112700124 19961127 00124 NM 1996 11 27 9624946631 1 19961119 A 5320 FITTING BOEING 747 747251B 1384892 NM BS 1920 BROKEN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 631US 23111 DURING LINE CHECK, FOUND THE LOWER FITTING ON THE RIGHT DOOR POST IN THE AFT CARGO BAY BROKEN. REMOVED AND REPLACED FIT TING PER SRM 51-10-01 PG 18, PARA 4. 2 L 7 4 4F A20WE 1996112700125 19961127 00125 1996 11 27 COMA9610333 2 19961119 A 7321 EEC EMB 120 EMB120RT SO NR 1 ENGINE OUT OF ADJUST A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 244CA 120217 ON INITIAL CLIMBOUT, THE NR 1 ENGINE TORQUE FLUCTUATED FROM 92 PERCENT TO 100 PERCENT. WHEN POWER WAS REDUCED THE FLUCT UATION WAS FROM 72 PERCENT TO 90 PERCENT, OPERATION BECAME NORMAL SHORTLY. TRANSFERRED TO DEFERRED LIST CAT C, MEL 73-2 1-1, EXPIRES 11-29-96. BOTH EEC TURNED TO MANUAL. 2 L 7 2 4T RT A31SO 1996112700126 19961127 00126 NM 1996 11 27 SWAA961255 1 19961119 A 3350 900835A BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 20SW 21337 DURING SCHEDULED 1/2 D-CHECK, FOUND 7 CABIN FLOOR TRACK LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F A16WE 1996112700127 19961127 00127 NM 1996 11 27 SWAA961256 1 19961118 A 3350 1000679 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 64SW 21722 DURING SCHEDULED TERMINAL CHECK, RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER BOEING M/M. 2 L 7 2 4F A16WE 1996112700128 19961127 00128 NM 1996 11 27 SWAA961257 1 19961115 A 5330 SKIN BOEING 737 7372T4 1384492 NM BS 750 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED TERMINAL CHECK, FOUND FUSELAGE SKIN CRACK ON RT SIDE ABOVE WING FAIRING AT BS 750. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996112700129 19961127 00129 NM 1996 11 27 SWAA961258 1 19961115 A 5330 SKIN BOEING 737 7373H4 1384600 NM SERV DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOOR LOWER AFT SKIN CUTOUT CRACKED AT BS 328, RBL 65, WL 210. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996112700130 19961127 00130 NM 1996 11 27 SWAA961259 1 19961115 A 5320 CLIP BOEING 737 7373H4 1384600 NM BS 500/663/908 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 663, S10R AT BS 500D, S19R AND AT BS 908, S4L. REPLACED PE R BOEING SRM. 2 L 7 2 4F RT A16WE 1996112700131 19961127 00131 NM 1996 11 27 SWAA961260 1 19961115 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 335 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED D-CHECK, FOUND STRINGER 8R DAMAGED AT BS 335. REPLACED DAMAGED SECTION PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996112700132 19961127 00132 NM 1996 11 27 SWAA961261 1 19961115 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 907/400 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT HAT SECTION ANGLE AT BS 907, BETWEEN S9 AND 8L, AND AT BS 400, BETWEEN S9 AND 8L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996112700133 19961127 00133 NM 1996 11 27 SWAA961262 1 19961115 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 927 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED D-CHECK, FOUND UPPER ATTACH ANGLE ON SHEAR WEB CRACKED AT BS 927 TO 947. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996112700134 19961127 00134 NM 1996 11 27 SWAA961263 1 19961115 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 986-994 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 986 TO 994, WL 208. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996112700135 19961127 00135 NM 1996 11 27 SWAA961264 1 19961115 A 5320 MOPSILL BOEING 737 7373H4 1384600 NM BS 947-986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED D- CHECK, FOUND AFT GALLEY DOORWAY MOPSILL CORRODED FROM BS 947 TO 986 AND AT FWD SERVICE DOOR MOPSILL FROM BS 294 TO 338. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996112700136 19961127 00136 NM 1996 11 27 SWAA961265 1 19961115 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 637 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED D-CHECK, WEB CRACKED BELOW LEFT EMERGENCY EXIT CUTOUT AT BS 637. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996112700137 19961127 00137 NM 1996 11 27 SWAA961266 1 19961115 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 368 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED D-CHECK, FUSELAGE SKIN GOUGED AT BS 368, BELOW S4L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996112700138 19961127 00138 NM 1996 11 27 SWAA961267 1 19961115 A 5320 CHANNEL BOEING 737 7373H4 1384600 NM BS 727/772 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CHANNELS CORRODED AT BS 727D PLUS 5 AND AT 772, LBL 12.5, LBL 3, 8 , 12.5, 8.10. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996112700139 19961127 00139 NM 1996 11 27 SWAA961268 1 19961115 A 5312 BULKHEAD WEB BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED D-CHECK, FOUND BULKHEAD BS 178 PRESSURE WEB CRACKED AT RBL 4.7. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996112700140 19961127 00140 NM 1996 11 27 SWAA961269 1 19961115 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 360-380 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED D-CHECK, FOUND MULTIPLE FUSELAGE SKIN DENTS AT FROM BS 360 TO 380, BETWEEN S17 AND 19L. REPAIRED PER B OEING SRM. 2 L 7 2 4F RT A16WE 1996112700141 19961127 00141 NM 1996 11 27 SWAA961270 1 19961115 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED D-CHECK, FOUND BS 178 SIDE CHORD LT AND RT SIDES CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996112700142 19961127 00142 NM 1996 11 27 SWAA961271 1 19961115 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 834/331 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED D-CHECK, FOUND FUSLAGE SKIN DENTED AT BS 834, RBL 8, BETWEEN S26 TO 27 AND AT BS 331 BETWEEN S21 AND 22 . REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996112700143 19961127 00143 NM 1996 11 27 SWAA961272 1 19961115 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 400-420/500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED D-CHECK, FOUND FLOOR TO SIDEWALL SUPPORT PLATE CORRODED AROUND NUTPLATE HOLES AT BS 500 TO 500A AND BS 420 TO 400. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996112700144 19961127 00144 NM 1996 11 27 SWAA961273 1 19961115 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 312, WL 208 AND AT BS 344, WL 208.1. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996112700145 19961127 00145 NM 1996 11 27 SWAA961274 1 19961115 A 3350 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED A1 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996112700146 19961127 00146 NM 1996 11 27 SWAA961275 1 19961116 A 5330 SKIN BOEING 737 7373H4 1384600 NM DOOR CUTOUT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 330SW 23694 DURING SCHEDULED C1 CHECK, FOUND FWD GALLEY DOOR UPPER HINGE CUTOUT CRACKED AT LOWER AFT CORNER. REPAIRED PER SWA RA 1- 352-0257. 2 L 7 2 4F RT A16WE 1996112700147 19961127 00147 NM 1996 11 27 SWAA961276 1 19961114 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 880 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 880, ABOVE S25R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996112700148 19961127 00148 NM 1996 11 27 SWAA961277 1 19961116 A 5320 FRAME BOEING 737 7373H4 1384600 NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED TERMINAL CHECK, FOUND FWD SERVICE DOORWAY UPPER STUB FRAME CRACKED. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996112700149 19961127 00149 1996 11 27 SWAA961278 4 19961116 A 2565 0250084 SLIDE BOEING 737 7373H4 1384600 NM FWD GALLEY DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED RON, GALLEY DOOR SLIDE DEPLOYED. REPLACED SLIDE PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996112700150 19961127 00150 NM 1996 11 27 SWAA961279 1 19961115 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 600SW 27694 DURING SCHEDULED BC3 CHECK, FOUND FUSELAGE SKIN GOUGED 3 FT LONG AND 2 WIDE, 33 AFT OF FWD CARGO DOOR AND APPROX 11 INCH ES BELOW MAIN DECK FLOORBEAMS. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996112700151 19961127 00151 NM 1996 11 27 SWAA961280 1 19961117 A 3350 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 621SW 28037 DURING WALKAROUND, FOUND FLOOR TRACK LIGHTING INOP AT ROWS 14 THROUGH 18. REPLACED POWER SUPPLIES AND OP CHECKED PER BO EING M/M. 2 L 7 2 4F RT A16WE 1996112700152 19961127 00152 1996 11 27 SWAA961281 4 19961114 A 2565 D31354125 SLIDE BOEING 737 7373G7 1384595 NM AFT SERVICE DR LOW PRESS A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED TERMINAL CHECK, FOUND AFT SERVICE DOOR ESCAPE SLIDE PRESSURE LOW. REPLACED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996112700153 19961127 00153 NM 1996 11 27 SWAA961282 1 19961114 A 5320 WEB BOEING 737 7373Y0 1384671 NM DOOR STOP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 699SW 23826 DURING SCHEDULED C3 CHECK, FOUND UPPER FWD DOOR STOP CRACKED IN WEB. REPAIRED PER SWA RA 1-353-1558. 2 L 7 2 4F RT A16WE 1996112700154 19961127 00154 1996 11 27 SWAA961283 4 19961119 A 2565 1061323433 SLIDE BOEING 737 7375H4 138449D NM SERVICE DOOR LOW PRESS A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 524SW 26566 DURING SCHEDULED RON CHECK, FOUND AFT SERVICE DOOR ESCAPE SLIDE PRESSURE LOW. REPLACED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996112700155 19961127 00155 NM 1996 11 27 96FDEA01668 1 19961025 A 5751 CASTING BOEING 727 72725C 138400H NM LT AILERON CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 117FE 19299 NR 0932, LT OUTBOARD AILERON NR 2 HINGE CASTING HAS CORROSION AT LOWER HINGE HOLES. REMOVED AND REPLACED CASTING PER SR M 51-10-01, (P/N 5700200) HINGE ASSY. 2 L 7 3 4F A3WE 1996112700156 19961127 00156 NM 1996 11 27 96FDEA01669 1 19961105 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 580 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 117FE 19299 MAIN CARGO COMPARTMENT STA 580 FLOORBEAM RBL 45 FROM C/L, UPPER CHORD OF BEAM CORRODED AFT SIDE AT FASTENERS ON FLOORBEA M. CORROSION REMOVED, THICKNESS LESS THAN ALLOWABLE LIMITS AFTER REPAIR. INSTALLED STRAP PER AARD 53-10-07-2 FIGURE 1. REPAIR INSTALLED AFTER ALODING AND PAINT, WET WITH SEALER AT ASSEMBLY. 2 L 7 3 4F A3WE 1996112700157 19961127 00157 NM 1996 11 27 96FDEA01670 1 19961025 A 5751 5694420 CASTING BOEING 727 72725C 138400H NM LT AILERON CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 117FE 19299 LT AILERON NR 3 HINGE CASTING HAS CORROSION AT HINGE PIN AREA. REMOVED AND REPLACED CASTING PER 51-10-1 SRM. 2 L 7 3 4F A3WE 1996112700158 19961127 00158 NM 1996 11 27 96FDEA01671 1 19961029 A 5311 FRAME BOEING 727 72725C 138400H NM BS 440 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 117FE 19299 STA 440 FRAME IS CRACKED AT STR 9 LT. TRIMMED OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-10-4 FIG 2 PAGE 7 TO 11. 2 L 7 3 4F A3WE 1996112700159 19961127 00159 NM 1996 11 27 96FDEA01672 1 19961114 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 640 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 117FE 19299 MAIN CARGO FLOORBEAM STA 640 RBL 45 TO 60 HAS CORROSION AND PREVIOUS REPAIR DOES NOT COVER DAMAGE AREA. REMOVED TOP CHO RD OF BS 640 FLOORBEAM FROM RBL 19 TO RT OUTBOARD SKIN, FABRICATED NEW TOP CHORD AND REPAIR ANGLES AND STRAPS PER SRM 53 -10-8 FIG 5. 2 L 7 3 4F A3WE 1996112700160 19961127 00160 NM 1996 11 27 FDEA01673 1 19961115 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 640 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 117FE 19299 CORROSION ON VERTICAL WEB OF BS 640 FLOORBEAM RBL 52 THROUGH RBL 61 AFT SIDE UNDER TOP CHORD. REMOVED CORROSION FROM VE RTICAL WEB OF BS 640 FLOORBEAM RBL 52 THROUGH RBL 61. AFT SIDE FABRICATED, REPAIR DOUBLER FOR BS 640 FLOORBEAM VERTICAL WEB 17 RBL 52 TO RBL 61 AFT SIDE, PER SRM 51-40-2, M/M 51-20-0. 2 L 7 3 4F A3WE 1996112700161 19961127 00161 NM 1996 11 27 96FDEA01674 1 19961028 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 560 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 117FE 19299 FUSELAGE UPPER LOBE; CORROSION ON FLOORBEAM BETWEEN LBL 0 TO LBL 26 SEAT TRACKS STA 560. REMOVED CORROSION PER SRM 51- 10-6, ALODINED AND PRIMED AREA, FABRICATED AND INSTALLED STRAP REPAIR LBL 0 TO LBL 26 STA 560 AS PER EA 7-5310-78928. I NSTALLED ADDITIONAL FASTENERS AS REQUIRED. 2 L 7 3 4F A3WE 1996112700162 19961127 00162 NM 1996 11 27 96FDEA01675 1 19961028 A 5720 CHORD BOEING 727 72725C 138400H NM BS 870 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 117FE 19299 CENTER WING AFT WEB UPPER CHORD BULGED AND CORROSION EMANTING FROM BETWEEN WEB AND CHORD AT STA 870 W/L 190 LBL 30. REM OVED CORRODED WEB AND UPPER CHORD STA 870 LBL 70 RBL 70. INSTALLED REPAIR PER ESO 11697 DATED 9-10-96, PER SRM 57-10-00 . 2 L 7 3 4F A3WE 1996112700163 19961127 00163 NM 1996 11 27 96FDEA01676 1 19961103 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 117FE 19299 UPPER LOBE FLOORBEAM HAS CORROSION STA 400 RBL 27 TO RBL 35. INSTALLED REPAIR STRAP TO FLOORBEAM PER SRM 53-10-8. 2 L 7 3 4F A3WE 1996112700164 19961127 00164 NM 1996 11 27 96FDEA01677 1 19961101 A 5320 FITTING BOEING 727 72725C 138400H NM BS 870 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 117FE 19299 STR 4R END FITTING CRACKED AT STATION 870 FWD SIDE. REMOVED AND REPLACED STR END FITTING PER 51-10-01. 2 L 7 3 4F A3WE 1996112700165 19961127 00165 NM 1996 11 27 96FDEA01678 1 19961114 A 5511 RIB BOEING 727 72725C 138400H NM HORIZ STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 117FE 19299 HORZ STAB RT SIDE RIB CRACKED, FWD UPPER CHORD, I/B SIDE STA 17.20. REMOVED AND REPLACED CHORD RIB PER EA 7-5510-20214. 2 L 7 3 4F A3WE 1996112700166 19961127 00166 NM 1996 11 27 96FDEA01679 1 19961114 A 5320 FITTING BOEING 727 72725C 138400H NM BS 870 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 117FE 19299 UPPER LOBE; END FITTING CRACK FWD OF STA 870 STR 2R. REMOVED AND REPLACED STR 2R END FITTING FWD OF STA 870 PER 51-10-1 SRM. 2 L 7 3 4F A3WE 1996112700167 19961127 00167 NM 1996 11 27 96FDEA01680 1 19961115 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 312 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 117FE 19299 CORROSION ON UPPER FLANG OF FLOORBEAM STA 312 LBL 4. CUT OUT CORROSION ALONG WITH CORROSION AND DAMAGE FROM NR 0708 AND NR 1434 OF INST DOUBLER PER SRM 53-10-8 FIG 7 FROM LBL 29 TO RBL 9. 2 L 7 3 4F A3WE 1996112700168 19961127 00168 NM 1996 11 27 96FDEA01681 1 19961021 A 5720 VERT STIFFENER BOEING 727 72725C 138400H NM BS 868 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 117FE 19299 VERTICAL STIFFINER ON CENTER WING AFT WEB AFT SIDED CRACKED APPROX 4 INCHES AT UPPER END STA 868 RBL 40 WL 190. REMOVED STIFFENER AND INSTALLED NEW STIFFENER PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996112700169 19961127 00169 NM 1996 11 27 96FDEA01682 1 19961119 A 3260 DOWNLOCK SWITCH BOEING 727 727173C 1384059 NM NLG MALFUNCTIONED A FDEA O OTHER N FALSE WARNING AP APPROACH 1 SO 25 199FE 19509 ON INITIAL LANDING GEAR EXTENSION THE NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE. A VISUAL SCAN OF THE ALIGNMENT MARKS IN DICATED THAT THE GEAR WAS DOWN. RECYCLED GEAR AS PER NOSE EXTENSION FAILURE PROCEDURES AND THE NOSE GEAR GREEN LIGHT IL LUMINATED NORMALLY. INSPECTED DOWNLOCK SWITCH AND BRACKET AS PER M/M 32-21-41. FOUND MOISTURE IN CONNECTOR. CLEANED, REINSTALLED AND SAFETIED CONNECTOR, OPERATIONAL CHECK GOOD. 2 L 7 3 4F A3WE 1996112700170 19961127 00170 NM 1996 11 27 96FDEA01683 1 19961120 A 2781 CONNECTOR BOEING 727 727227 1384078 NM NR 2 LE FLAP DIRTY A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 490FE 21483 AFTER TAKEOFF AND CLEAR UP, SHORTLY THEREAFTER THE AMBER LEADING EDGE FLAPS LIGHT CAME ON. RAN CHECKLIST, NO HELP. THE NR 2 LEADING EDGE FLAP WAS AMBER ON SECOND OFFICER'S POSITION INDICATOR. RETURNED FOR LANDING. CLEANED CANNON PLUG ON THE NR 2 LEADING EDGE FLAP POSITION INDICATING SWITCH. SYSTEM TESTED NORMALLY. ALL DONE PER MAINTENANCE CONTROL AND M AINTENANCE MANUAL 27-82-0 PAGE 101. 2 L 7 3 4F A3WE 1996112700171 19961127 00171 EU 1996 11 27 96FDEA01684 1 19961120 A 7830 TR COWL AIRBUS 310 A310221 3930310 EU NR 2 ENGINE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 448FE 260 UPON ARRIVAL, DURING WALKAROUND FOUND APPROX 18 DIA HOLE ON AFT INBD EDGE OF NR 2 ENGINE FAN COWL. ALSO, NOTED SEVERE D ISCOLORATION ON INBD REVERSER HALF WITH BURN STREAKS AND STRUCTURAL DAMAGE TO THE REVERSER. *S/D* REMOVED AND REPLACED GROUND THRUST REV CHECK VALVE AND LEAK CHECKED. REMOVED AND REPLACED INBD THRUST REV COWL AND INBD FAN COWL M/M PER 71 -13-03. RIG CHECKED THRUST REV PER M/M 78-32-03. PERFORMED COWL LOAD SHARE ADJ/TEST PER M/M 71-13-03. 2 L 7 2 4F RT A35EU 1996112700172 19961127 00172 NM 1996 11 27 96FDEA01685 1 19961121 A 3231 MECHANISM BOEING 727 727233 138408A NM NLG DOOR OUT OF ADJUST A FDEA O OTHER E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 25 276FE 22041 AFTER LANDING GEAR RETRACTION DOORS LIGHT ON FORWARD PANEL AND NOSE GEAR DOOR LIGHT ON SECOND OFFICER'S PANEL REMAINS IL LUMINATED WHILE GEAR HANDLE WAS IN UP POSITION. LANDING GEAR WAS RECYCLED WITH NO EFFECT. INCREASED NOISE IN COCKPIT S UGGEST THAT THE NOSE GEAR DOORS ARE NOT COMPLETELY CLOSED. CHECKED ADJUSTMENT OF NOSE GEAR DOOR LOCK SWITCHES, CLEANED SWITCHES. DOOR LIGHTS OPERATIONAL CHECK NORMAL WITH DOORS IN CLOSE AND OPEN POSITIONS AS PER MAINTENANCE MANUAL 32-62-1 1. OPENED AND CLOSED DOORS SEVERAL TIMES, DOORS AND SWITCHES OPERATIONAL CHECKED NORMAL OK FOR SERVICE. 2 L 7 3 4F RT A3WE 1996112700173 19961127 00173 WP 1996 11 27 96FDEA01686 1 19961120 A 3244 NCG620513 TIRE DOUG DC10 DC1030 3023501 WP NLG FAILED A A FDEA A UNSCHED LANDING D C INFLIGHT SEPARATION F.O.D. TO TAKEOFF 1 SO 25 313FE 48311 AT LIFT OFF, A LOUD BANG WAS IN THE COCKPIT, AT THE SAME TIME ALL 3 INS UNITS FAILED. DUE TO WEATHER AT NARITA AIRCRAF T WAS DIVERTED TO OSAKA. ON LANDING FOUND RIGHT NOSE GEAR TIRE TREAD HAD COME OFF AND DAMAGED LOWER FUSELAGE AREA. NO INS READINGS DUE TO IN FLIGHT FAILURE. REMOVED AND REPLACED BOTH NOSE TIRE AND WHEEL ASSEMBLIES PER MAINTENANCE MANUAL 32-42-01. REPLACED BENT ROD ASSEMBLY (P/N ACG7177-1), HANDLE (P/N ACG715-1) AND BRACKET (P/N ACG7176-1) ON STEERING BYP ASS SYSTEM PER MAINTENANCE MANUAL 32-52-05. ALSO, REPLACED BENT GROUND SENSE ROD AND INSPECTED. INTERIM REPAIRED LOWER FUSELAGE DAMAGE PER ENGINEERING AUTHORIZATION 8-5310-32013. 2 L 7 3 4F A22WE 1996112700174 19961127 00174 WP 1996 11 27 ARWA9611005 1 19961120 A 7931 420491C OIL PRESS SWITCH DOUG DC8 DC863F 302198F WP NR 2 ENGINE MALFUNCTIONED A ARWA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SO 19 441J 45988 NR 2 ENGINE OIL PRESSURE LIGHT CAME ON. RETARDED THROTTLE, LIGHT STAYED ON. SHUT DOWN ENGINE AS PER ABNORMAL CHECKLIST , TIME 1430Z, OIL PRESSURE 24 PSI. REMOVED AND REPLACED MAIN OIL FILTER, OLD ONE FOUND NORMAL. PRECAUTIONARY REMOVED A ND REPLACED DIFFERENTIAL OIL PRESSURE SW, PRESSURE LIGHT SW EINGINE RUN-UP OIL PRESSURE AND TEMP CHECKED NORMAL PER MM 7 9-20-7, 79-32-2 AND 79-33-1. 2 L 7 4 4F 4A25 1996112700175 19961127 00175 NM 1996 11 27 VNAA9611004 1 19961111 A 2150 CIRCUIT BREAKER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LEFT TRIPPED A VNAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 436JS 3052 ON TAXI OUT, LT BLEED SHUTOFF VALVE FAIL AND LT PACK OVERHEAT MESSAGES APPEARED, SMOKE WAS APPARENT IN CABIN. AIRCRAFT RETURNED TO GATE. UPON INSPECTION, MAINTENANCE FOUND THAT THE CIRCUIT BREAKER FOR THE LT HX FAN HAD TRIPPED. MAINTENAN CE RESET THE CIRCUIT BREAKER AND PERFORMED GROUND RUNS, OPERATIONAL CHECK GOOD. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996112700176 19961127 00176 NM 1996 11 27 VNAA9611005 1 19961114 A 3234 7178011 CONTROL LEVER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT FAILED A VNAA K NONE J WARNING INDICATION CL CLIMB 1 GL 07 437JS 2496 3055 LANDING GEAR WOULD NOT RETRACT, CONTINUED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER, GEAR OPERATIONAL CHECKED GOOD. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996112700177 19961127 00177 NM 1996 11 27 VNAA9611006 1 19961121 A 6120 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT PROP DIRTY A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 07 458PS 3068 LT PROP LOW PITCH CAS MESSAGE CAME ON AND ENGINE FLUX WHEN POWER LEVERS WERE ADVANCED. MAINTENANCE CLEANED THE CONNECTO RS ON THE LT PCU AND ECU, PERFORMED GROUND RUN, OPERATIONAL CHECK GOOD. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996112700178 19961127 00178 NM 1996 11 27 SRAA961113 1 19961120 A 7931 OIL PRESS LINE BOEING 747 747212B 1384886 NM NR 1 ENGINE LOOSE A SRAA E ENGINE SHUTDOWN K FLUID LOSS AP APPROACH 1 GL 23 745SJ 20888 DURING DESCENT, NR 1 ENGINE HAD RAPID QUANTITY AND PRESSURE DROP. SHUT DOWN NR 1 ENGINE PER AOM PROCEDURES AND LANDED W ITHOUT INCIDENT. FOUND MAIN OIL PRESSURE LINE POPPED OUT OF COUPLING BRACKET AND RETAINING BOLTS SHEARED OFF. REMOVED BROKEN STUDS AND INSTALLED THREE HELICOILS REPAIR PER BOEING MM CH 79-21-00 AND 71-21-03. INSPECTED OIL FILTER AND CHIP DETECTOR NO DEFECTS NOTED, ACCOMPLISHED ENGINE RUN, OPS CHECKED AND LEAK CHECKED GOOD. 2 L 7 4 4F A20WE 1996112700179 19961127 00179 WP 1996 11 27 IXXA9600166 1 19961121 A 5242 861583849 DOOR DOUG DC8 DC862 3021970 WP E/E COMPT NOT CLOSED A IXXA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 GL 23 8969U 46070 ON TAKEOFF, THE AIRCRAFT WOULD NOT PRESSURIZE ACCOMPANIED BY A LOUD BANG AND THE NR 3 TURBO COMPRESSOR STALLING. THE FL IGHT RETURNED TO LPLA. MAINTENANCE FOUND THE FORWARD ACCESSORY COMPARTMENT DOOR AJAR. THE DOOR WAS RESEATED AND A GROU ND PRESSURIZATION CHECK WAS ACCOMPLISHED. THE TURBO COMPRESSOR DUCTING WAS CHECKED WITH NO DEFECTS FOUND. 2 L 7 4 4F 4A25 1996112700180 19961127 00180 WP 1996 11 27 IXXA9600167 1 19961121 A 2110 543C51 CLAMP DOUG DC8 DC862 3021970 WP RT TURBO COMP LOOSE A IXXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 8969U 46070 ON CLIMBOUT, AIRCRAFT WOULD NOT PRESSURIZE ABOVE 10,000 FEET CABIN ALTITUDE. AIRCRAFT RETURNED TO LPLA FOR AN UNEVENTFU L LANDING. MAINTENANCE FOUND DUCT CLAMP FROM THE RIGHT TURBO COMPRESSOR SYSTEM TO THE HEAT EXCHANGER LOOSE. MAINTENANC E SECURED THE LOOSE CLAMP AND PRESSURIZED THE AIRCRAFT ON THE GROUND PRIOR TO RETURNING THE AIRCRAFT TO SERVICE. 2 L 7 4 4F 4A25 1996112700181 19961127 00181 NM 1996 11 27 CALA9601694 1 19961031 A 5751 SKIN BOEING 727 727243 138408D NM LT AILERON DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND OUTBOARD TRAILING EDGE CORNER OF LEFT OUTBOARD AILERON DELAMINATED. THE DELAMINATED AREA WAS CUT OUT A ND A HOT BOND REPAIR WAS INSTALLED IAW SRM 51-40-6. 2 L 7 3 4F RT A3WE 1996112700182 19961127 00182 NM 1996 11 27 CALA9601695 1 19961031 A 5752 SKIN BOEING 727 727243 138408D NM LT AILERON TAB SEPARATING A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND LT OUTBOARD AILERON TAB SEPARATING AT OUTBOARD TRAILING EDGE. THE SEPARATING AREA WAS CUT OUT AND A HO T BOND REPAIR WAS ACCOMPLISHED IAW SRM 51-40-6. 2 L 7 3 4F RT A3WE 1996112700183 19961127 00183 NM 1996 11 27 CALA9601696 1 19961103 A 5754 RIB BOEING 727 727243 138408D NM NR 3 LE SLAT ACT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND A .75 INCH CRACK IN NR 3 SLAT ACTUATOR INBOARD ATTACH RIB. A REPAIR PART WAS FABRICATED, HEAT TREATED AND INSTALLED IAW SRM 51-40-3 AND 51-30-2. 2 L 7 3 4F RT A3WE 1996112700184 19961127 00184 NM 1996 11 27 CALA9601697 1 19961103 A 5754 RIB BOEING 727 727243 138408D NM NR 3 LE SLAT ACT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND A 1 INCH CRACK IN NR 3 SLAT ACTUATOR OUTBOARD ATTACH RIB. THE CRACK WAS STOP DRILLED, AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-40-3. 2 L 7 3 4F RT A3WE 1996112700185 19961127 00185 NM 1996 11 27 CALA9601698 1 19961031 A 5712 RIB BOEING 727 727243 138408D NM RT WING LE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND A 2 INCH CRACK AT UPPER EDGE OF RT WING LEADING EDGE RIB, SLAT STA 0. THE CRACK WAS STOP DRILLED, A WE B REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-20-1. 2 L 7 3 4F RT A3WE 1996112700186 19961127 00186 NM 1996 11 27 CALA9601699 1 19961101 A 5753 SKIN BOEING 727 727243 138408D NM RT TE FOREFLAP GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND RT WING OUTBOARD FOREFLAP INBOARD LOWER SURFACE GOUGED AND DELAMINATED. THE DAMAGED AREA WAS CUT OUT, FILLER AND DOUBLER WERE FABRICATED AND A HOT BOND REPAIR WAS ACCOMPLISHED IAW SRM 51-40-6. 2 L 7 3 4F RT A3WE 1996112700187 19961127 00187 NM 1996 11 27 CALA9601700 1 19961113 A 5755 ANGLE BOEING 727 727243 138408D NM NR 11 SPOILER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND RT WING NR 11 SPOILER ACTUATOR SUPPORT FITTING INBOARD ATTACH ANGLE CRACKED. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F RT A3WE 1996112700188 19961127 00188 NM 1996 11 27 CALA9601701 1 19961113 A 3350 110049 POWER SUPPLY BOEING 737 7373T0 1384582 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 10323 23374 WHEN GROUND TEST SWITCH FOR EMERGENCY TRACK LIGHTS WAS PLACED IN TEST POSITION FROM COCKPIT OR FLIGHT ATTENDANT POSITION , THE AFT GALLEY AND LAST FOUR CABIN ROWS DID NOT TEST. MAINTENANCE FOUND THE BATTERY CHARGER POWER SUPPLY AT FAULT. T HE AFT POWER SUPPLY WAS REMOVED AND REPLACED. 2 L 7 2 4F RT A16WE 1996112700189 19961127 00189 WP 1996 11 27 9624959956 1 19961031 A 5280 DOORS DOUG DC9 DC931 3022065 WP NLG DAMAGED A NWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 01 923RW 47188 VIBRATION AND NOISE COMING FROM NOSE GEAR AREA AFTER TAKEOFF. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAIN TENANCE FOUND LEFT AND RIGHT FORWARD NOSE GEAR DOORS DAMAGED. REMOVED, REPAIRED AND REINSTALLED DOORS. OPERATIONAL CHE CK NORMAL. 2 L 7 2 4F A6WE 1996112700190 19961127 00190 WP 1996 11 27 9624969956 1 19961026 A 3231 DOORS DOUG DC9 DC931 3022065 WP NLG NOT LATCHED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 923RW 47183 FORWARD NOSE LANDING GEAR DOOR FAILED TO CLOSE AFTER TAKEOFF. FLIGHT RETURNED TO MSN AND LANDED WITHOUT INCIDENT. MAIN TENANCE FOUND FORWARD NOSE GEAR DOORS UNLATCHED. SECURED DOORS TO PROPER LATCHED POSITION. 2 L 7 2 4F A6WE 1996112700191 19961127 00191 NM 1996 11 27 9624975528 1 19961120 A 7932 CONNECTOR BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE NR 2 ENGINE MISINSTALLED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 528US 23843 716457 AFTER TAKEOFF, ENGINE NR 2 OIL QUANTITY INDICATED 0. AIRCRAFT RETURNED TO DEPARTURE AIRPORT. GROUND MAINTENANCE FOUND OIL LEVEL FULL AND NO OIL LEAKS NOTED. CANNON PLUG ON TRANSMITTER WAS FOUND OVER TORQUED WHICH CAUSED PINS TO UNSEAT FR OM RUBBER GROMMET. THE CANNON PLUG PINS WERE RESEATED AND CANNON PLUG REINSTALLED. OIL QUANTITY INDICATION CHECKED NOR MAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996112700192 19961127 00192 WP 1996 11 27 9624989906 1 19961120 A 3397 WIRE DOUG DC9 DC931 3022065 WP ROW 18 BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 956N 47252 DURING PERIODIC CHECK, FOUND EMERGENCY AT ROW 18 INOPERATIVE. REPAIRED BROKEN WIRE, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996112700193 19961127 00193 WP 1996 11 27 9624999933 1 19961119 A 3260 SWITCH DOUG DC9 DC931 3022065 WP NLG OUT OF ADJUST A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 1334U 47280 DURING APPROACH, NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. RECYCLED GEAR AND NORMAL INDICA TIONS WERE ACHIEVED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED NOSE GEAR LOCK SWITCH ACTUATING BOLT. OPE RATIONAL CHECK NORMAL ON GEAR SWING. 2 L 7 2 4F A6WE 1996112700194 19961127 00194 NM 1996 11 27 9625012293 1 19961120 A 3350 BATTERY PACK BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 293US 21504 DURING PREFLIGHT, FOUND LEFT FORWARD AND AFT EMERGENCY LIGHTS INOPERATIVE. REPLACED BOTH BATTERY PACKS, FORWARD AND AFT , OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996112700195 19961127 00195 1996 11 27 9625029913 4 19961119 A 2565 113317 SLIDE DOUG DC9 DC931 3022065 WP PAX DOOR FAILED TEST A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 963N 38006 4273 47415 DURING PERIODIC CHECK, FORWARD ENTRY EVACUATION SLIDE FAILED BATTERY TEST. REPLACED SLIDE. 2 L 7 2 4F A6WE 1996112700196 19961127 00196 WP 1996 11 27 9625039930 1 19961119 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 89S 47042 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPER ATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996112700197 19961127 00197 WP 1996 11 27 9625049940 1 19961119 A 3411 PITOT LINE DOUG DC9 DC932 3022066 WP RUDDER BLOCKED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 3322L 47031 RUDDER TRAVEL UNRESTRICTED LIGHT REMAINED ON AFTER TAKEOFF. FLIGHT DIVERTED TO DTW AND LANDED WITHOUT INCIDENT. MAINTE NANCE FOUND PITOT LINE TO RUDDER LIMITER PROBE BLOCKED WITH ICE. DRAINED WATER FROM TRAP. REPLACED RUDDER TRAVEL UNRES TRICTED LIGHT SWITCH, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996112700198 19961127 00198 WP 1996 11 27 9625059874 1 19961118 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP ROW 16 DISCHARGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 783NC 48108 DURING LINE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE AT ROW 16 EXIT SIGN FOR OVERWING DOOR. REPLACED BATTERIES AN D OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A6WE 1996112700199 19961127 00199 WP 1996 11 27 9625069104 1 19961119 A 2410 CSD DOUG DC9 DC915 3022036 WP NR 2 ENGINE FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 94S 47204 DURING CLIMBOUT AT ABOUT 3,000 FT EXPERIENCED WHAT APPEARED TO BE INTERMITTANT POWER INTERRUPTIONS. FLASHING ANNUNCIATO R LIGHTS AND CLICKING SOUNDS COMING FROM CIRCUIT BREAKER PANEL LOWER AREA OR E & E COMPARTMENT. RIGHT GENERATOR VOLTS N ORMAL BUT CYCLES JUST BELOW 380 AT 390-395. FOLLOWED COM AND RETURNED TO MEM. FLIGHT LANDED WITHOUT INCIDENT. MAINTEN ANCE REPLACED NR 2 CSD, OPERATION CHECKS GOOD. 2 L 7 2 4F A6WE 1996112700200 19961127 00200 WP 1996 11 27 9625079601 1 19961107 A 2150 CLAMP DOUG DC9 DC932 3022066 WP LT ACM BROKEN A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 601NW 47038 LOSS OF PRESSURIZATION OCCURRED AFTER TAKEOFF. CREW DECLARED AN EMERGENCY AND FLIGHT WAS RETURNED TO DTW. AIRCRAFT LAN DED WITHOUT INCIDENT. MAINTENANCE FOUND BROKEN CLAMP ON LEFT AIR CYCLE MACHINE OUTLET DUCT. REPLACED CLAMP, OPERATIONA L CHECK NORMAL. 2 L 7 2 4F A6WE 1996112700201 19961127 00201 NM 1996 11 27 9625082717 1 19961120 A 3350 BATTERY PACK BOEING 727 7272S7 138407Z NM CABIN DISCHARGED A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 721RC 22492 DURING PREFLIGHT, FOUND AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996112700202 19961127 00202 1996 11 27 9625099866 4 19961119 A 3425 5223700004 ADI DOUG DC9 DC951 3022051 WP NR 2 MALFUNCTIONED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 775NC 34364 2942 47785 FIRST OFFICER'S ADI INDICATED TURN 30 DEGREE ANGLE WHEN LEVEL. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAI NTENANCE REPLACED NR 2 ADI, OPERATION CHECKS GOOD. 2 L 7 2 4F RT A6WE 1996112700203 19961127 00203 NM 1996 11 27 9625002710 1 19961118 A 3350 BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 820EA 22557 DURING PREFLIGHT, FOUND FORWARD SECTION OF EMERGENCY PATHWAY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHE CK OK. 2 L 7 3 4F A3WE 1996112700204 19961127 00204 EU 1996 11 27 WWMA9600098 1 19961120 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT DIRTY A WWMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 15 231LN 340B231 CARGO SMOKE LIGHT ILLUMINATED AFTER TAKEOFF, THE AIRCRAFT RETURNED TO FIELD WITHOUT INCIDENT. MAINTENANCE CLEANED BOTH CARGO SMOKE DETECTORS AND RERACKED THE WARNING ELECTRONIC UNIT. 2 L 7 2 4T RT A52EU 1996112700205 19961127 00205 EU 1996 11 27 WWMA9600097 1 19961120 A 2170 471749 FILTER SAAB SF340 340B 7860101 EU COCKPIT DIRTY A WWMA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 15 356SB 340B356 CREW REPORTED WHEN REDUCING POWER FOR DESCENT THE COCKPIT AIR BEGAN TO SMELL. MAINTENANCE PERFORMED VISUAL INSPECTION O F THE LEFT AIR CYCLE MACHINE AND THE ENGINE BLEED AIR CONNECTIONS. THE COCKPIT AIR DISTRIBUTION AIR FILTER WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 1996112700206 19961127 00206 EU 1996 11 27 96FDEA01687 1 19961121 A 2133 REGULATOR AIRBUS 310 A310221 3930310 EU NR 2 ENGINE MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 419FE 345 AFTER NR 2 ENG START CABIN AUTO PRESS NR 2 AND NR 2 REGULATOR FAIL, NR 1 SYS OK. AFTER TAKEOFF UNABLE TO PRESSURIZE CAB IN IN AUTO OR MANUAL. THE OVERRIDE AND ECAM OUTFLOW VALVE POSITION INDICATED CLOSED. RESET NR 2 AUTO FLOW VALVE AND CO NTROLLER C/B'S. ALSO, PERFORMED NR 2 CPC, BITE CHK NORMAL. ALL TESTS PASSED AND ALL FAULT LIGHTS RESET TO NORMAL POSIT IONS. 2 L 7 2 4F RT A35EU 1996112700207 19961127 00207 NM 1996 11 27 96FDEA01688 1 19961122 A 3260 POSITION SWITCH BOEING 727 727233 138408A NM NLG OUT OF ADJUST A FDEA O OTHER N FALSE WARNING AP APPROACH 1 SO 25 276FE 22041 ON FINAL, GEAR HANDLE DOWN NO GREEN NOSE GEAR LIGHTS ILLUMINATED. RECYCLED GEAR UP AND DOWN AGAIN GREEN GEAR LIGHT ILLU MINATED NORMALLY. ACCOMPLISHED NOSE GEAR LOCK AND POSITION SWITCHES ADJUSTMENT AND TEST PER MAINTENANCE MANUAL 32-61-71 PAGE 501 TO 502. NO DEFECTS NOTED, LIGHTS CHECKED NORMAL. 2 L 7 3 4F RT A3WE 1996112700208 19961127 00208 NM 1996 11 27 96FDEA01689 1 19961122 A 2612 FIRE WARNING BOEING 727 727225 1384077 NM GLARE SHIELD ACTIVATED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 465FE 21289 ON CLIMBOUT, THE FIRE WARNING BELL AND FORWARD FIRE WARNING LIGHTS ON THE GLARE SHIELD MOMENTARILY ILLUMINATED, THEN IMM EDIATELY EXTINGUISHED. NO OTHER LIGHT WAS OBSERVED. TESTED THE FIRE WARNING AND SMOKE DETECTION SYSTEMS AND THEY CHEC KED NORMAL. NO FURTHER INDICATIONS WERE OBSERVED. PERFORMED ENGINE FIREWALL AND WHEEL WELL FIRE TEST PER JET RUN HANDB OOK CHAPTER 5. PERFORMED MAIN CARGO SMOKE TEST, ALL TEST NORMAL. 2 L 7 3 4F A3WE 1996112700209 19961127 00209 WP 1996 11 27 96FDEA01690 1 19961122 A 3010 PICCOLO TUBE DOUG DC10 DC1030F 3023504 WP NR 5 LE SLAT LEAKING A FDEA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 SO 25 315FE 48313 AIRCRAFT WING ANTI-ICE SET UP FOR USE ON TAKEOFF, ABOUT 10 TO 15 SECONDS AFTER LIFT OFF. NR 1 MANIFOLD FAIL LIGHT ILLUM INATED. TURNING OFF WING ANTI-ICE TURNED OFF MANIFOLD FAIL LIGHT. TROUBLESHOT SYSTEM FOUND NR 5 LEFT HAND SLAT PICCOLO TUBE OUTBOARD END LEAKING. REMOVED PICCOLO TUBE FROM NR 5 SLAT, REPAIRED AS PER ENGINEERING AUTHORIZATION 8-3010-32015 , INSTALLED IN AIRCRAFT. PRESSURE CHECK GOOD, OPERATED SLATS AND WING ANTI-ICE SEVERAL TIMES AND FUNCTIONAL CHECK WAS G OOD. 2 L 7 3 4F RT A22WE 1996112700210 19961127 00210 NM 1996 11 27 96UAL900857 1 19961111 A 3350 M1197 BATTERY BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN DISCHARGED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 378UA 24653 EMERGENCY EXIT SIGN AT DOOR NUMBER TWO RIGHT HAND AND AFT CABIN EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK, CHECKS OK . 2 L 7 2 4F 4 F RT A16WE E2GL 1996112700211 19961127 00211 NM 1996 11 27 96UAL900858 1 19961111 A 3350 900835A BATTERY PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7287U 21565 TWO RIGHT OVERWING EMERGENCY EXIT LIGHTS ABOVE BOTH EXITS INOPERATIVE. *S/D* BATTERY DISCHARGED, REPLACED BATTERY PACK . 2 L 7 3 4F 4 F A3WE E2EA 1996112700212 19961127 00212 NM 1996 11 27 96UAL900859 1 19961111 A 3350 STRIP BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN LOOSE A UALA O OTHER L NO TEST IN INSP/MAINT 1 WP 29 7287U 21565 ORANGE COLOR EEL LIGHTING STRIP LOOSE AT ROW 14 ABC. REPLACED ORANGE EEL STRIP COVER WHICH SECURES EEL STRIP IN ITS TRA CK. 2 L 7 3 4F 4 F A3WE E2EA 1996112700213 19961127 00213 NM 1996 11 27 96UAL900860 1 19961111 A 5620 WINDOW BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7261U 21408 WINDOW 8L NEXT TO SEAT 4A HAS EVIDENCE OF CRACK. *S/D* CHECKED WINDOW AND FOUND A SCRATCH, NOT A CRACK OR FRACTURE. 2 L 7 3 4F 4 F A3WE E2EA 1996112700214 19961127 00214 NM 1996 11 27 96UAL900861 1 19961112 A 3350 BATTERY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 558UA 26654 EMERGENCY EGRESS LIGHTING INOP ROWS 16 TO 23. REPLACED BATTERY PACK, OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996112700215 19961127 00215 NM 1996 11 27 96UAL900862 1 19961112 A 2140 HEATER COX & COMPAN 28311 BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE COCKPIT MALFUNCTIONED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 618UA 197 21878 DIVERTED TO DEN UNDER AMBER ALERT WITH SMOKE IN THE COCKPIT. *S/D* THE FIRST OFFICER'S SHOULDER HEATER OVERHEATED. TH E HEATER WAS REPLACED, OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 1996112700216 19961127 00216 NE 1996 11 27 96UAL900863 2 19961112 A 7321 78017013 EEC BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE RT ENGINE FAILED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 WP 29 604UA 21865 707518 ABORTED TAKEOFF AT 80 KNOTS DUE TO RIGHT ENGINE OVER TEMP CONDITION. *S/D* A FAULTY ELECTRONIC ENGINE CONTROL UNIT HAD JUST BEEN INSTALLED ON THE RIGHT ENGINE BEFORE THE OVER TEMP DISCREPANCY OCCURRED. THE EEC WAS REPLACED, OPERATIONS C HECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 1996112700217 19961127 00217 NM 1996 11 27 96UAL900864 1 19961112 A 2140 HEATER COX & COMPAN 28311 BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE COCKPIT MALFUNCTIONED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 618UA 197 21878 DIVERTED TO ORD DUE TO AN ELECTRICAL ODOR IN THE COCKPIT. *S/D* THE FIRST OFFICER'S SHOULDER HEATER OVERHEATED. THE H EATER WAS REPLACED, OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 1996112700218 19961127 00218 NM 1996 11 27 96UAL900865 1 19961112 A 7933 A53209014 O-RING BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE NR 1 ENGINE CUT A UALA A E UNSCHED LANDING ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 105UA 26473 724186PW NR 1 ENGINE OIL QUANTITY SLOWLY DROPPED TO ZERO. SHUT DOWN ENGINE AND RETURNED TO HNL. REPLACED ENGINE. AT ENGINE DISA SSEMBLY, FOUND OIL LEAK AT NR 3 BEARING SCAVENGE OIL TEMP PROBE. O-RING WAS DAMAGED. REPLACED PROBE AND O-RING. 2 L 7 4 4F 4 F RT A20WE E24NE 1996112700219 19961127 00219 NM 1996 11 27 96UAL900866 1 19961112 A 2720 69427332 BUSHING BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE RUDDER BROKEN A UALA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 WP 29 941UA 26676 CAPTAIN AND FIRST OFFICERS RUDDER PEDALS HAVE FEEDBACK OR RESISTANCE IN LAST TWO INCHES OF TRAVEL ON THE RIGHT SIDE, THE LEFT SIDE IS NORMAL. FOUND RUDDER POWER CONTROL UNIT FORWARD MANIFOLD CLEVIS BOLT GUIDE BUSHING BROKEN. RUDDER CONTRO L ACTUATOR FORWARD SUPPORT BRACKET MISALIGNED AND BUSHING BROKEN. 2 L 7 2 4F 4 F RT A16WE E2GL 1996112700220 19961127 00220 NM 1996 11 27 96UAL900867 1 19961113 A 3350 5603325 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 578UA 26694 EMERGENCY EGRESS LIGHTING IN FRONT OF AFT LAV INOP. REPLACED EMERGENCY EGRESS LIGHT ASSEMBLY, OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996112700221 19961127 00221 NM 1996 11 27 96UAL900868 1 19961113 A 3397 58791 WIRE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7273U 21420 EEL LIGHTS INOPERATIVE ROWS 26 THROUGH 28. *S/D* FEEDER CABLE ASSEMBLY FROM POWER SUPPLY BATTERY TO AFT CABIN SECTION EEL LIGHTING DAMAGED. CABLE REPLACED AND EEL SYSTEM, OPERATED NORMALLY. 2 L 7 3 4F 4 F A3WE E2EA 1996112700222 19961127 00222 WP 1996 11 27 96UAL900869 1 19961113 A 3350 POWER LEAD DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1812U 46611 EEL LIGHTS LT SIDE FORWARD GALLEY INOPERATIVE. SECURED POWER FEEDER LEAD AT STRIP, CHECKS OK. 2 L 7 3 4F 4 F A22WE E23EA 1996112700223 19961127 00223 NM 1996 11 27 96UAL900870 1 19961113 A 5610 5893543110 WINDSHIELD BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE RT COCKPIT CRACKED A UALA A UNSCHED LANDING C F.O.D. TO TAKEOFF 1 WP 29 7265U 21412 FIRST OFFICERS FORWARD WINDSHIELD SHATTERED DUE TO BIRD STRIKE ON TAKEOFF. RETURNED TO ORD. *S/D* REPLACED WINDOW. 2 L 7 3 4F 4 F A3WE E2EA 1996112700224 19961127 00224 1996 11 27 96UAL900871 4 19961114 A 2565 D30654122 INFLATION TUBE AIRCRUISERS BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SLIDE CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 577UA 26693 DURING TIME CONTROLLED OVERHAUL, SLIDE UNIT INFLATABLE SHOWS CHAFE DAMAGE CAUSED BY THE PRESSURE RELIEF VALVE SCREWS. H OLES ARE WORN THROUGH THE CHAFE COVER (2) AND THROUGH THE TOP INFLATION TUBE (5 HOLES). EACH HOLE IS .25 INCH IN DIAME TER. PATCH PER MANUFACTURERS MANUAL. REPLACED CHAFE COVER WITH NEW COVER, OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996112700225 19961127 00225 NM 1996 11 27 96UAL900872 1 19961114 A 5315 65C33948 FLOORBEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE BS 947 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 901UA 25001 THE RT UPPER CHORD OF THE FLOOR BEAM AT BS 947, WAS FOUND CORRODED AROUND THE FLOOR PANELS ATTACHMENT HOLES. THE CORROSI ON EXTENDS FROM THE RT TO LT BL 22.2. THE CORROSION DEPTH IS IN SOME LOCATIONS MORE THAN HALF THE FLANGE THICKNESS. TH E CORROSION WAS REMOVED BY CUTTING THE HORIZONTAL FLANGE FROM THE MOST RT HAND END, TO THE LT BL 22.2. A REPAIR T-SECT ION WAS MANUFACTURED AND ATTACHED TO THE VERTICAL FLANGE OF THE FLOORBEAM. AN ENGINEERING VARIATION AUTHORITY WAS ISSUE D WITH BOEING NO TECHNICAL OBJECTION RECEIVED. 2 L 7 2 4F 4 F RT A16WE E2GL 1996112700226 19961127 00226 1996 11 27 96UAL900873 4 19961114 A 2565 D28935103 SLIDE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE DOOR 2L LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7462U 21916 DURING TIME CONTROLLED OVERHAUL SLIDE DEVELOPED A SEAM LEAK ON INFLATION TUBE. SLIDE SCRAPPED. 2 L 7 3 4F 4 F A3WE E2EA 1996112700227 19961127 00227 1996 11 27 96UAL900874 4 19961114 A 2565 D28935103 SLIDE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE DOOR 1L LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7454U 21908 DURING TIME CONTROLLED OVERHAUL SLIDE DEVELOPED SEAM LEAK ON INFLATION TUBE. SLIDE SCRAPPED. 2 L 7 3 4F 4 F A3WE E2EA 1996112700228 19961127 00228 1996 11 27 96UAL900875 4 19961114 A 2565 D28935103 SLIDE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE DOOR 2L LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7268U 21415 DURING TIME CONTROLLED OVERHAUL SLIDE DEVELOPED SEAM LEAK ON INFLATION TUBE. SLIDE SCRAPPED. 2 L 7 3 4F 4 F A3WE E2EA 1996112700230 19961127 00230 NM 1996 11 27 96UAL900877 1 19961115 A 2720 69427332 BUSHING BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE RUDDER BROKEN A UALA K NONE F FLT CONT AFFECTED NR NOT REPORTED 1 WP 29 943UA 26680 CREW REPORTS WHILE DOING FLIGHT CONTROL CHECK, FOUND RUDDER HAS A BINDING OR GRINDING FEEL WHEN DISPLACED TO RIGHT THE L AST FEW INCHES OF FULL TRAVEL. THE RUDDER POWER CONTROL UNIT FORWARD MANIFOLD CLEVIS BOLT GUIDE BUSHING WAS BROKEN. R EPLACED BUSHING. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 1996112700231 19961127 00231 WP 1996 11 27 ABXA9600668 1 19961120 A 3231 CF252A0453 BUSHING DOUG DC9 DC931 3022065 WP RT MLG DOOR WORN A ABXA O OTHER N FALSE WARNING TO TAKEOFF 1 GL 23 908AX 47008 RIGHT GEAR UNSAFE LIGHT WOULD NOT GO OUT IN FLIGHT. COMPLETED ABNORMAL PROCEDURE BUT GEAR LIGHT WOULD NOT GO OUT. REPL ACED RIGHT MAIN LANDING GEAR DOOR HINGE BUSHING AND ADJUSTED THE MAIN LANDING GEAR DOOR LATCH ASSEMBLY IAW DC-9 MM 32-31 -4. 2 L 7 2 4F A6WE 1996112700232 19961127 00232 WP 1996 11 27 ABXA9600669 1 19961121 A 3350 60030431 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN DEFECTIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 903AX 4395 47427 EMERGENCY LIGHTING STAYS ON WHEN POWER IS REMOVED FROM AIRCRAFT. REPLACED EMERGENCY LIGHT POWER SUPPLY IAW DC-9 SUPP MM 33-53-00. 2 L 7 2 4F A6WE 1996112700233 19961127 00233 NE 1996 11 27 SWIA95768 2 19961015 A 7200 ENGINE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RIGHT FAILED A SWIA C D E F ABORTED TAKEOFF RETURN TO BLOCK ENGINE SHUTDOWN ACTIVATE FIRE EXT. A J FLAME/FIRE WARNING INDICATION TO TAKEOFF 1 NM 07 411SW 7067 DURING TAKEOFF, RT ENGINE ITT WENT TO RED LINE. ABORTED TAKEOFF, TOWER REPORTED FLAMES FROM RT ENGINE. PERFORMED ENGIN E FIRE PROCEDURE. REPLACED RT ENGINE WITH REPAIRED ASSY, OPS CKS AND LEAKS CKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 1996112700234 19961127 00234 SO 1996 11 27 SWIA95769 1 19961026 A 5610 WINDSHIELD EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT COCKPIT FAILED A SWIA K NONE O OTHER CL CLIMB 1 NM 07 234SW 120308 PILOTS CAPT WINDSCREEN SHATTERED, OUTER LAYER DURING CLIMBOUT. REPLACED LT WINDSCREEN IAW MM 56-10-01. 2 L 7 2 4T 4 T RT A31SO E20NE 1996112700235 19961127 00235 SO 1996 11 27 SWIA95770 1 19961027 A 7712 311694201 TORQUE SENSOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT ENGINE FAILED A SWIA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 NM 07 235SW 120310 AT 2,300 FT, THE TORQUE GAUGE BECAME ERRATIC AND TWO SECONDS LATER THE LT ENGINE AUTO FEATHERED. REPLACED TORQUE SENSOR WITH SERVICEABLE UNIT, RAN ENGINE OPS CKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1996112700236 19961127 00236 SO 1996 11 27 SWIA95771 1 19961030 A 3260 SENSOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT MLG MALFUNCTIONED A SWIA O OTHER N FALSE WARNING CR CRUISE 1 NM 07 186SW 120034 RT MAIN A GEAR DOWN LIGHT CAME ON IN FLT, USED OVERRIDE TO GET GEAR DOWN. PERFORMED GEAR SWING SEVERAL TIMES WITHOUT DU PLICATING MALFUNCTION. REPLACED A-SYSTEM RT MLG GEAR SENSORS AND Y-HARNESS AND SYSTEM OPS CKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1996112700237 19961127 00237 EA 1996 11 27 SWIA95772 1 19961109 A 2613 OVERHEAT ELEMENT CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LT ENGINE FAILED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 403SW 7028 LT 14TH DUCT WARNING AND BLEED AIR DUCT AURAL AFTER TAKEOFF. WARNING DID NOT EXTINGUISH WITH LT 14TH BLEED CLOSED, WARN INGS EXTINGUISHED LT POWER REDUCTION BELOW 79 PERCENT N1. CONTINUED FLIGHT USING PARTIAL LT POWER. REMOVED AND REPLACE D LT 14TH STAGE SENSING ELEMENT, RAN A/C LEAK CKS OF 14TH STAGE BLEED AIR. 2 L 7 2 4F 4 F RT A21EA E15NE 1996112700238 19961127 00238 SW 1996 11 27 SWIA95773 1 19961111 A 3260 UPLOCK ROLLER SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP RT MLG MISSING A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 2725D AC723 ON GEAR RETRACTION RT MAIN INTRANSIT LIGHT WOULD NOT EXTINGUISH. FOUND UPLOCK ROLLER MISSING ON RT MAIN STRUT. INSTALL ED NEW UPLOCK ROLLER AND TARGET, ADJUSTED UPLOCK SWITCHES TO TARGET, CYCLED GEAR NUMEROUS TIMES, OPS CKS GOOD MM 32-00-0 0. 2 L 7 2 4T 4 T RT A8SW E4WE 1996112700239 19961127 00239 SO 1996 11 27 SWIA95774 1 19961112 A 3260 PROX SENSOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE NLG MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 199SW 120237 AURAL WARNING UNIT WENT OFF INFLIGHT WITH THE FOLLOWING BRAKES, TRIM FLAPS AUTOFEATHER. REPLACED NOSE GEAR AIR/GROUND P ROX SENSOR CYCLED GEAR SEVERAL TIMES, OPS CKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1996112700240 19961127 00240 EA 1996 11 27 SWIA95775 1 19961114 A 3320 BR95005 BALLAST CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE CABIN FAILED A A SWIA C D ABORTED TAKEOFF RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 NM 07 411SW 7067 FLIGHT ATTENDANT REPORTED SMOKE COMING FROM ROW 8 OVERHEAD BIN AND VENTS. MOSTLY DISSIPATED BY LANDING. VERY STRONG EL ECTRICAL SMELL, BURNING IN SEVERAL PLACES ABOVE OVERHEAD BINS. FOUND LIGHT BALLAST FOR UPPER CABIN LIGHTING OVER ROW 8 ON RT SIDE OVERHEATED AND BURNED. REPLACED LIGHTING BALLAST WITH NEW ONE, CKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 1996112700241 19961127 00241 SO 1996 11 27 SWIA95776 1 19961117 A 7332 CONNECTOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LEFT MALFUNCTIONED A SWIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 07 186SW 120034 LT LOW PRESSURE LIGHT ILLUMINATE STEADY ON TAXI OUT. COMPLIED WITH QRH LOW PRESSURE LIGHT STILL ILLUMINATED. REPLACED FUEL LOW PRESSURE SWITCH CANNON PLUG, OPS CKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1996112700242 19961127 00242 SW 1996 11 27 SWIA95777 1 19961118 A 3230 RETRACT MECH SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP LT MLG OUT OF ADJUST A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 2702Z AC669 LT MAIN GEAR WOULD NOT RETRACT. JACKED A/C AND OPS CHECKED LANDING GEAR SYSTEM. ONLY FOUND FAULT WITH THE LT MAIN LAND ING GEAR NOT FULLY ENGAGING IN UPLOCK HOOK. ADJUSTED LT MAIN ACTUATORS AS PER MM 32-00-00, ADJUST AND TEST OPS CKS GOOD AT THIS TIME. 2 L 7 2 4T 4 T RT A8SW E4WE 1996112700243 19961127 00243 SW 1996 11 27 SWIA95778 1 19961118 A 2432 RELAY SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP DC ELECT SYST FAILED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 3117A AC600 BATT FAULT LIGHT ILLUMINATED INFLIGHT AND BOTH BATT DISC LIGHTS CAME ON. RESET BATTERIES AND SAME PROBLEM OCCURRED AGAI N. REPLACED BATT FEEDER FAULT RELAY, RAN ENGINES AND OPS CKS GOOD. 2 L 7 2 4T 4 T RT A8SW E4WE 1996112700244 19961127 00244 SO 1996 11 27 SWIA95779 1 19961119 A 3150 BREAKER EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE AURAL WARNING TRIPPED A SWIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 NM 07 186SW 120034 AURAL WARNING BREAKER POPPED, RESET AS PER CHECKLIST. AURAL WARNING MAP ANNUNICATOR ILLUMINATED, BREAKER STAYED RESET. INSTALLED SERVICEABLE BACK UP BATTERY, RERACKED AURAL WARNING UNIT AND CHECKED CONNECTIONS PINS, POWERED UP A/C AND ALL CKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1996112700245 19961127 00245 WP 1996 11 27 ARWA9611006 1 19961122 A 2424 CONNECTOR DOUG DC8 DC863 302198A WP NR 4 GNS LOOSE A ARWA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SO 19 345JW 46042 AIR TURNBACK ON ROTATION, NR 4 GENERATOR WARNING. DID A GO-AROUND AND LANDED WITHOUT INCIDENT. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION, NO DEFECTS NOTED. FOUND NR 4 GCU CENTER CANNON PLUG LOOSE. RECONNECTED, RAN ALL ENGINES AND CHECK ED ELECTRICAL SYSTEM, OPS FOUND ALL NORMAL PER MM 24-10-0. 2 L 7 4 4F 4A25 1996112700246 19961127 00246 WP 1996 11 27 ARWA9611007 1 19961122 A 2910 O-RING DOUG DC8 DC863 302198A WP SLOT CONTROL VLV LEAKING A ARWA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 19 345JW 46042 INFLIGHT EMERGENCY DECLARED, TOTAL LOSS OF HYD FLUID. FOUND SLOT CONTROL VALVE AT HYD MANIFOLD BASE SEAL LEAKING. REMO VED AND REPLACED O-RING, SERVICED MAIN HYD SYSTEM, BLED ALL HYD SYSTEM. REPLACED CASE DRAIN FILTERS FOR LT AND RT HYD P UMPS. REPLACED MAIN HYD SYSTEM DUAL FILTERS, CHECKED FOR LEAKS. ALL NORMAL PER IAW MM 29-10-15 AND 27-80-4. 2 L 7 4 4F 4A25 1996112700255 19961127 00255 CE 1996 11 27 96ZZZX5633 1 19960912 A 2497 WIRE BEECH 18 G18S 1151010 CE COCKPIT SHORTED A A UATA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 AL 03 151H 10341 BA476 PILOT SMELLED SMOKE IN COCKPIT DURING TAKEOFF. WIRE NR 176 CHAFED ON THE DEFROST SCAT HOSE UNTIL SHORTING ITSELF. WIRE NR 176 ALSO MELTED THE INSULATION ON WIRE NR 177. BOTH WIRES AND SCAT HOSE WERE REPLACED. ALSO, WIRE NR 947 CHAFED ON DEFROST SCAT HOSE AND SHORTED BURNING THE INSULATION OFF DOWN TO THE REGULATOR. BOTH WIRE AND REGULATOR WERE REPLACED. ELECTRICAL SYSTEM FUNCTIONALLY TESTED IN ALL CIRCUITS AND NO OTHER DISCREPANCIES FOUND. 1 L 7 2 3R A765 1996112700273 19961127 00273 1996 11 27 96ZZZX5651 4 19961028 A 2562 MN1300 BATTERY ACK E01ELT PIPER PA28 PA28140 7102802 SO ELT LEAKING A LECA K NONE O OTHER IN INSP/MAINT 1 NE 05 5564U 8283 2826291 DURING ANNUAL INSPECTION, BATTERIES INSIDE ELT WERE FOUND TO BE LEAKING. ACID LEAKED INTO ELT CIRCUIT BOARD AND CORRODE D THE BOARD. GROUND WIRE OF ELT WAS CORRODED OFF. SUBMITTER RECOMMENDS USE OF DURACELL BATTERY POWERED ELT BE DISCONTI NUED, OR BATTERY MFG SEAL THE BATTERIES. BATTERY INSTALLED ELT 4-13-93. ELT INSTALLED AIRCRAFT 4-13-93. 1 L 7 1 3O 2A13 1996112700279 19961127 00279 SO 1996 11 27 96ZZZX5657 2 19961101 A 7414 10357426 BLOCK ASSY 101630203 CESSNA 402 402B 207590P CE CONT O520 TSIO520EB 17040 SO MAG DIST GEAR TEETH MISSING A OEZA K NONE E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 WP 19 773EA 869 E239506ER 402B0544 275398R PILOT REPORTED THAT ABOUT EVERY 20 MINUTES, THE RT ENGINE WOULD RUN ROUGH FOR A SECOND. FOUND DISTRIBUTOR GEAR TEETH MI SSING FROM DISTRIBUTOR BLOCK ASSY. REPLACED MAGNETO WITH NEW. 1 L 7 2 3O 3 O A7CE E8CE 1996112700280 19961127 00280 CE 1996 11 27 96ZZZX5658 1 19961028 A 3310 POST LIGHT CESSNA 402 402C 207590R CE COPILOT PANEL SHORTED A GNBA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 01 747WS 402C0080 PILOT REPORTED SEEING A SMALL AMOUNT OF SMOKE FROM UNDER COPILOT'S INSTRUMENT PANEL AND SMELLING SOMETHING 'ELECTRICAL' BURNING. UPON INSPECTION, A POST LIGHT WAS FOUND SHORTED. NO CIRCUIT BREAKERS TRIPPED. A VERY THIN SPRING INSIDE THE SCREW ON CONNECTOR BURNED THROUGH AND STOPPED CURRENT FLOW. THIS SPRING APPEARS TO BE A CIRCUIT PROTECTION DEVICE. 1 L 7 2 3O A7CE 1996112700282 19961127 00282 NM 1996 11 27 320796 1 19961002 A 3230 RETRACT MECH BOEING 737 7372L9 1384497 NM LANDING GEAR MALFUNCTIONED A ZZDA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 15 465AT 21528 ON TAKEOFF, LANDING GEAR HANDLE WOULD NOT RETRACT. MADE A LOW PASS FOR A TOWER VISUAL CHECK. REFERRED TO NON-NORMAL PR OCEDURES CHECK LIST. RESET LEVER LATCH AND LIGHT BREAKER. ALL INDICATIONS WERE NORMAL. USED QRH PROCEDURES AND NORMA L PROCEDURES CHECK LISTS. PERFORMED A NORMAL LANDING. MAINTENANCE PERFORMED A PRECAUTIONARY GEAR EXTENSION AND RETRACT ION PER BOEING MM 32-32-00 AND 32-33-00. FOUND NO DEFECTS. RETURNED AIRCRAFT TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1996112700285 19961127 00285 EU 1996 11 27 96ZZZX5660 1 19960517 A 6210 10513103505 PIN BOLKMS 117 BK117B1 5626012 EU BLADE WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 10UM 566 18255 7231 BLADE PIN WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996112700286 19961127 00286 EU 1996 11 27 96ZZZX5661 1 19960517 A 6210 10513103505 PIN BOLKMS 117 BK117B1 5626012 EU BLADE WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 10UM 566 180720 7231 BLADE PIN WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996112700287 19961127 00287 EU 1996 11 27 96ZZZX5662 1 19960517 A 6210 10513103505 PIN BOLKMS 117 BK117B1 5626012 EU BLADE WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 10UM 566 181312 7231 BLADE PIN WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996112700288 19961127 00288 EU 1996 11 27 96ZZZX5663 1 19960517 A 6210 10513103505 PIN BOLKMS 117 BK117B1 5626012 EU BLADE WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 10UM 566 81270 7231 BLADE PIN WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996112700289 19961127 00289 EU 1996 11 27 96ZZZX5664 1 19960718 A 6420 1053170023 BEARING BOLKMS 117 BK117B1 5626012 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 10UM 417 7231 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996112700290 19961127 00290 EU 1996 11 27 96ZZZX5665 1 19960703 A 7810 59528AELPSW3 CLAMP BOLKMS 105 BO105CBS 5626008 EU EXH CRACKED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 105NC 337 790 CLAMP CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H3EU 1996112700291 19961127 00291 EU 1996 11 27 96ZZZX5666 1 19960717 A 6210 10513103505 PIN BOLKMS 117 BK117B1 5626012 EU BLADE WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 17SJ 243 181692 7230 BLADE PIN WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996112700292 19961127 00292 EU 1996 11 27 96ZZZX5667 1 19960627 A 6420 ABWT82008 BEARING BOLKMS 117 BK117A4 5626017 EU T/R HEAD WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 118LF 374 7137 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW 2 EACH UNITS, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996112700293 19961127 00293 EU 1996 11 27 96ZZZX5668 1 19960424 A 6420 1053170023 BEARING BOLKMS 117 BK117A4 5626017 EU T/R HEAD WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 117CW 121 7125 T/R HEAD BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996112700294 19961127 00294 EU 1996 11 27 96ZZZX5669 1 19960731 A 6230 1051011305 BELLOWS BOLKMS 117 BK117A3 5626015 EU M/R MAST TORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 158BK 211 7058 BELLOWS IS TORN AROUND CLAMP AND FOLD AREAS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM 1 G 7 2 3U H13EU 1996112700295 19961127 00295 EU 1996 11 27 96ZZZX5670 1 19960913 A 6230 1051011305 BELLOWS BOLKMS 117 BK117B1 5626012 EU M/R MAST TORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 417BK 409 7143 BELLOWS IS TORN AROUND CLAMP AND FOLD AREAS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996112700296 19961127 00296 1996 11 27 96ZZZX5671 4 19961003 A 3120 B1794127000A CLOCK BOLKMS 117 BK117B1 5626012 EU COCKPIT FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 417BK 241 704097 7143 CLOCK SECOND HAND OPERATES FOR ONLY A COUPLE OF MINUTES BEFORE STOPPING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996112700297 19961127 00297 EU 1996 11 27 96ZZZX5672 1 19960516 A 6230 1051011305 BELLOWS BOLKMS 117 BK117A3 5626015 EU M/R MAST TORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 424MB 340 7082 BELLOWS IS TORN AROUND CLAMP AND FOLD AREAS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996112700298 19961127 00298 EU 1996 11 27 96ZZZX5673 1 19960712 A 6420 1053170023 BEARING BOLKMS 117 BK117B1 5626012 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 5194C 244 7169 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996112700299 19961127 00299 EU 1996 11 27 96ZZZX5674 1 19960609 A 6420 1053170018 FITTED BOLT BOLKMS 117 BK117B1 5626012 EU T/R HEAD WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 5188B 302 7163 FITTED BOLT WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996112700300 19961127 00300 EU 1996 11 27 96ZZZX5675 1 19961002 A 6420 10531717 BOLT BOLKMS 117 BK117B1 5626012 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 5188B 464 7163 BOLT WORN BEYOND SERVICEABLE LIMITS. REPLACED WTIH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996112700301 19961127 00301 EU 1996 11 27 96ZZZX5676 1 19960830 A 3340 11796135 LIGHT BOLKMS 117 BK117B1 5626012 EU ANTI COLL FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 5188B 7 1278642 7163 LIGHT BULB WILL NOT FLASH. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996112700302 19961127 00302 EU 1996 11 27 96ZZZX5677 1 19960417 A 6220 10515876 BUSHING BOLKMS 117 BK117A4 5626017 EU M/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 586BH 122 7129 VIB ABSORBER BUSHING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 4 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996112700303 19961127 00303 EU 1996 11 27 96ZZZX5678 1 19960925 A 6420 1053170023 BEARING BOLKMS 117 BK117A4 5626017 EU T/R HEAD WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 586BH 203 7129 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996112700304 19961127 00304 EU 1996 11 27 96ZZZX5679 1 19960330 A 6300 8500311101 INDICATOR BOLKMS 117 BK117A4 5626017 EU POP UP MALFUNCTION A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 586BH 7129 INDICATOR POP-UP WILL NOT RESET. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996112700305 19961127 00305 EU 1996 11 27 96ZZZX5680 1 19960623 A 6230 1051011305 BELLOWS BOLKMS 117 BK117B1 5626012 EU M/R MAST TORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 7060G 724 7173 BELLOWS IS TORN AROUND CLAMP AND FOLD AREAS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996112700306 19961127 00306 EU 1996 11 27 96ZZZX5681 1 19960723 A 7711 DK040 TRANSMITTER BOLKMS 105 BO105CBS 5626008 EU EPR PRESS DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 825LF 313 7587 796 TRANSMITTER DEFECTIVE. HIGH PRESSURE READINGS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H3EU 1996112700307 19961127 00307 EU 1996 11 27 96ZZZX5682 1 19960728 A 6230 1051011305 BELLOWS BOLKMS 117 BK117A4 5626017 EU M/R MAST TORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911BY 661 7127 BELLOWS IS TORN AROUND CLAMP AND FOLD AREAS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996112700308 19961127 00308 EU 1996 11 27 96ZZZX5683 1 19960728 A 6420 1053170018 FITTED BOLT BOLKMS 117 BK117A4 5626017 EU T/R HEAD WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911BY 343 7127 FITTED BOLT WORN BEYOND SERVICEABLE LIMITS. REPLACED WTIH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996112700309 19961127 00309 EU 1996 11 27 96ZZZX5684 1 19960728 A 6420 1053170023 BEARING BOLKMS 117 BK117A4 5626017 EU T/R HEAD WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911BY 343 7127 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996112700310 19961127 00310 EU 1996 11 27 96ZZZX5685 1 19960728 A 6410 134616P BUSHING BOLKMS 117 BK117A4 5626017 EU T/R BLADE WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911BY 478 7127 BUSHING TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996112700311 19961127 00311 EU 1996 11 27 96ZZZX5686 1 19960728 A 6410 134617P BUSHING BOLKMS 117 BK117A4 5626017 EU T/R BLADE WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911BY 478 7127 BUSHING TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH, 2 EACH NEW UNITS CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996112700312 19961127 00312 EU 1996 11 27 96ZZZX5687 1 19960419 A 3340 2LA00162500 LIGHT SOCKET BOLKMS 117 BK117A4 5626017 EU TAIL WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911BY 400 7127 LAMP WILL NOT REMAIN ILLUMINATED BECAUSE SOCKET IS WORN. SOCKET IS TOO LOOSE TO GET PROPER CONTACT WITH LAMP. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1996112700313 19961127 00313 EU 1996 11 27 96ZZZX5688 1 19960802 A 2840 DK042 TRANSMITTER BOLKMS 105 BO105CBS 5626008 EU FUEL PRESS INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911BH 182 11584 685 FUEL PRESS UNIT INOPERATIVE. HIGH PRESSURE READING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H3EU 1996112700314 19961127 00314 NE 1996 11 27 96ZZZX5689 2 19961020 A 7420 3038221 CABLE ASSY DOUG MD900 MD900 3027375 NM PWA PW206 PW206A NE RT ENG IGNITER WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 865 90000012 PCE206042 IGNITER CABLE ASSY WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW 2 EACH UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U NC H19NM E42NE 1996112700315 19961127 00315 NE 1996 11 27 96ZZZX5690 2 19961020 A 7420 3038221 CABLE ASSY DOUG MD900 MD900 3027375 NM PWA PW206 PW206A NE LT ENG IGNITER WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 888 90000012 PCE206018 IGNITER CABLE ASSY WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW 2 EACH UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U NC H19NM E42NE 1996112700332 19961127 00332 NM 1996 11 27 AWXA9600687 1 19961110 A 5315 FLOOR BEAM BOEING 737 7373S3 1384711 NM BS 294.5 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 PAE - FLT 7700 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON BOTTOM SIDE OF BS 294.5, FLOOR BEAM RBL 45. REMOV ED, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-51 AND 51-40-02. (M) 2 L 7 2 4F RT A16WE 1996112700333 19961127 00333 NM 1996 11 27 AWXA9600688 1 19961110 A 5315 FLOOR BEAM BOEING 737 7373S3 1384711 NM BS 328 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 PAE - FLT 7700 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON BS 328, FLOOR BEAM LBL 55 TO RBL 55, WL 208. REMO VED, MANUFACTURED AND REPLACED UPPER CHORD OF FLOOR BEAM PER SRM 53-10-5. (M) 2 L 7 2 4F RT A16WE 1996112700334 19961127 00334 NM 1996 11 27 AWXA9600689 1 19961107 A 5315 FLOOR BEAM BOEING 737 7373S3 1384711 NM BS 312 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 PAE - FLT 7700 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM AT BS 312, LBL 10 TO BL 0. REMOVED TOP CHORD FROM FLOOR BEAM AT BS 312, LBL 19 TO RBL 15 AND SPLICED IN MANUFACTURED TOP CHORD, IAW SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1996112700335 19961127 00335 NM 1996 11 27 AWXA9600690 1 19961109 A 2761 654494714 ACTUATOR BOEING 737 7373S3 1384711 NM NR 4 SPOILER BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 0873 23713 PAE - FLT 7700 - DURING ROUTINE MAINTENANCE CHECK, FOUND NR 4 INBOARD SPOILER ACTUATOR MOUNT CASTING BROKEN OFF. REMOVE D AND REPLACED NR 4 INBOARD SPOILER ACTUATOR, IAW MM 27-62-71. (M) 2 L 7 2 4F RT A16WE 1996112700336 19961127 00336 NM 1996 11 27 AWXA9600691 1 19961114 A 3397 WIRE BOEING 737 7373S3 1384711 NM BS 400 MISWIRED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 316AW 23713 DURING ROUTINE MAINTENANCE CHECK, FOUND EXIT LIGHTS IN AFT GALLEY OVERHEAD AND OVERWING INOPERATIVE. FOUND WIRES MISS-W IRED AT D2956 AND AT THE BATTERY PACK DURING C-CHECK. REWIRED PER EO 33-50-16. 2 L 7 2 4F RT A16WE 1996112700337 19961127 00337 NM 1996 11 27 AWXA9600692 1 19961114 A 3350 CONNECTOR BOEING 737 7373S3 1384711 NM BS 400 MISWIRED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT PROXIMITY LIGHTS AT ROWS 4, 5, 7, 9, 10, 14, 15, 16 AND 20 INOPERATIVE. FO UND CONNECTOR D2956 WIRED WRONG AT C-CHECK. REWIRED AND FUNCTIONALLY CHECKED GOOD. REWORKED PER EO 33-50-16. 2 L 7 2 4F RT A16WE 1996112700338 19961127 00338 NM 1996 11 27 AWXA9600693 1 19961110 A 5320 6517688U180 SILL BOEING 737 7373S3 1384711 NM FWD ENTRY CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 PAE - FLT 7700 - DURING ROUTINE MAINTENANCE CHECK, FOUND FORWARD ENTRY DOOR MOPSILL CORRODED. REPAIRED MOPSILL, IAW, SR M 53-10-15, SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 1996112700339 19961127 00339 NM 1996 11 27 AWXA9600694 1 19961109 A 2761 BACB30LJ820 BOLT BOEING 737 7373S3 1384711 NM NR 4 SPOILER BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 PAE - FLT 7700 - DURING ROUTINE MAINTENANCE CHECK, FOUND NR 4 SPOILER OUTBOARD ACTUATOR LINKAGE PIVOT BOLT BROKEN. REMO VED BROKEN BOLT AND INSTALLED NEW BOLT PER MM 27-62-82. (M) 2 L 7 2 4F RT A16WE 1996112700340 19961127 00340 NM 1996 11 27 AWXA9600695 1 19961111 A 5312 BULKHEAD BOEING 737 7373S3 1384711 NM BS 178 DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 PAE - FLT 7806 - DURING ROUTINE MAINTENANCE CHECK, FOUND BS 178 PRESSURE BULKHEAD DENTED, WL 187, RBL 12. REMOVED DAMAG ED SECTION, FABRICATED AND INSTALLED REPAIR PIECES, IAW ER 2-53-12-31, TCO-PAN-96-1636RR. (M) 2 L 7 2 4F RT A16WE 1996112700341 19961127 00341 NM 1996 11 27 AWXA9600696 1 19961111 A 5313 STRINGER BOEING 737 7373S3 1384711 NM BS 727 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 316AW 23713 PAE - FLT 7806 - DURING ROUTINE MAINTENANCE CHECK, FOUND CRACK AT 4TH HOLE FORWARD FROM PRESSURE BULKHEAD AT BS 727, STR INGER 18A. PERFORMED REPAIR IAW, ER 2-53-15-52, TCO-PAN-96-1622RR AND 8110-3. (M) 2 L 7 2 4F RT A16WE 1996112700342 19961127 00342 NM 1996 11 27 AWXA9600697 1 19961111 A 5313 STRINGER BOEING 737 737277 1384570 NM BS 747 DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 188AW 22655 DURING ROUTINE MAINTENANCE CHECK, FOUND BLIND FASTENER DRILLED INTO RADIUS OF STRINGER AT BS 747, STR 3 LT. REMOVED FAS TENER, DAMAGED SKIN, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-30-3. 2 L 7 2 4F RT A16WE 1996112700343 19961127 00343 NM 1996 11 27 AWXA9600698 1 19961109 A 5730 SKIN BOEING 737 737277 1384570 NM LT WING LE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 188AW 22655 DURING ROUTINE MAINTENANCE CHECK, FOUND LT WING L/E SKIN UPPER SURFACE CORRODED AND CRACKED AT NR 3 SLAT ACTUATOR, 3 INC HES ABOVE CUTOUT. INSTALLED REPAIR ON LT WING L/E SKIN UPPER SURFACE 3 INCHES ABOVE NR 3 SLAT ACTUATOR CUTOUT IAW SRM 5 7-30-4. 2 L 7 2 4F RT A16WE 1996112700344 19961127 00344 NM 1996 11 27 AWXA9600699 1 19961109 A 2761 65448517 ACTUATOR BOEING 737 737277 1384570 NM NR 4 SPOILER BROKEN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 188AW 22655 DURING ROUTINE MAINTENANCE CHECK, FOUND NR 4 SPOILER O/B ACTUATOR HAS BROKEN ATTACH LUG ON BOTTOM OF ACTUATOR. REMOVED AND REPLACED ACTUATOR IAW AWA TASK CARD R3M27017. 2 L 7 2 4F RT A16WE 1996112700345 19961127 00345 NM 1996 11 27 AWXA9600700 1 19961109 A 5347 GALLEY TRACK BOEING 737 737277 1384570 NM BS 990 CORROSION A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 188AW 22655 DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON AFT GALLEY TRACK I/B STA 990 WL 208 RBL 18. FABRICATED REPAIR STRA P AND INSTALLED PER ER 2-53-43-04 TCO-PAN-96-1612RR, 8110-3. 2 L 7 2 4F RT A16WE 1996112700346 19961127 00346 NM 1996 11 27 AWXA9600701 1 19961107 A 5315 BAC1505100617 FLOORBEAM BOEING 737 737277 1384570 NM BS 967 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 188AW 22655 DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOORBEAM BS 967 RBL 12 TO 18, 55. REMOVED UPPER CHORD FROM FLOORB EAM, BS 967 RBL 55 TO LBL 5. FABRICATED AND INSTALLED REPAIR CHORD IAW AWA ER 2-53-16-44, TCO-PAN-96-1620RR 8110-3. 2 L 7 2 4F RT A16WE 1996112700347 19961127 00347 NM 1996 11 27 AWXA9600702 1 19961107 A 5315 FLOORBEAM BOEING 737 737277 1384570 NM BS 987 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 188AW 22655 DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOORBEAM STA 987 RBL 16.45 WL 208. REPAIRED FLOORBEAM STA 987 PER ER 2-53-16-44 TCO-PAN-96-1620RR, 8110-3. 2 L 7 2 4F RT A16WE 1996112700348 19961127 00348 NM 1996 11 27 AWXA9600703 1 19961110 A 5320 SHEAR TIE BOEING 737 737277 1384570 NM BS 727 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 188AW 22655 DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON SHEAR TIE AT BS 727B, LBL 0 TO LBL 6. REPAIRED DAMAGED SHEER TIE, ALL WORK DONE IAW SRM 53-10-4, 51-10-1. 2 L 7 2 4F RT A16WE 1996112700349 19961127 00349 NM 1996 11 27 AWXA9600704 1 19961110 A 5320 SHEAR TIE BOEING 737 737277 1384570 NM BS 767 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 188AW 22655 DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON SHEAR TIE AT BS 767, LBL 6 FWD AND AFT SIDE. REMOVED, FABRICATED A ND INSTALLED REPAIR PARTS PER SRM 53-10-4. 2 L 7 2 4F RT A16WE 1996112700350 19961127 00350 NM 1996 11 27 AWXA9600705 1 19961110 A 5315 FLOORBEAM BOEING 737 737277 1384570 NM BS 847 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 188AW 22655 DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOORBEAM LBL 3, WL 208, BS 847. REMOVED DAMAGED PORTION OF UPPER CHORD, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-10-9. 2 L 7 2 4F RT A16WE 1996112700351 19961127 00351 NM 1996 11 27 AWXA9600706 1 19961120 A 3397 WIRE BOEING 737 7373G7 1384595 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 155AW 23777 DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 2 TO 5 FLOOR PROXIMITY EMERGENCY LIGHTING INOPERATIVE. REPAIRED BROKEN WIRE , OPERATIONS CHECK GOOD. 2 L 7 2 4F RT A16WE 1996112700352 19961127 00352 WP 1996 11 27 CALA9601702 1 19961122 A 2750 49561601 SPRING DOUG DC9 DC982 3022082 WP FLAP HANDLE BROKEN A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 16815 49113 THE FLAPS WOULD NOT FULLY RETRACT AFTER TAKEOFF. THE FLAP HANDLE WOULD NOT STAY IN THE RETRACT POSITION. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE FLAP HANDLE CONTROL SPRING BROKEN. THE SPR ING WAS REMOVED AND REPLACED, AN OPERATIONAL CHECK OF THE FLAPS WAS GOOD. 2 L 7 2 4F A6WE 1996112700353 19961127 00353 NM 1996 11 27 CALA9601703 1 19961124 A 3020 652673822 DUCT BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE BROKEN A CALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 09 27783 20638 685586 THE NR 3 FIRE LIGHT AND BELL ACTIVATED IN FLIGHT. THE ENGINE THROTTLE WAS REDUCED TO IDLE AND THE WARNING CEASED. WHEN THE THROTTLE WAS INCREASED THE LIGHT CAME ON AGAIN. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE DUCT FROM 13TH STAGE BLEED TO COWL ANTI-ICE BROKEN. THE DUCT WAS REPLACED AND OPERATIONAL CHECK S WERE GOOD. 2 L 7 3 4F 4 F A3WE E2EA 1996112700354 19961127 00354 NE 1996 11 27 CALA9601704 2 19961123 A 7314 35820134 FUEL PUMP BOEING 737 737217 1384464 NM PWA JT8 JT8D9 52048 NE NR 3 ENGINE INOPERATIVE A A CALA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 SW 09 12230 19884 665378 THE NR 2 ENGINE FLAMED OUT DURING CLIMB AT 900 FEET AGL. THE AIRCRAFT WAS RETURNED TO CHS WHERE IT LANDED WITHOUT INCID ENT. MAINTENANCE FOUND THE NR 2 ENGINE FUEL PUMP AT FAULT. THE FUEL PUMP WAS REMOVED AND REPLACED IAW MM 73-11-1. A P OWER ASSURANCE RUN WAS PERFORMED AND OPERATIONAL AND LEAK CHECKS WERE GOOD. 2 L 7 2 4F 4 F A16WE E2EA 1996112700355 19961127 00355 WP 1996 11 27 CALA9601705 1 19961120 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 69 DAMAGED A CALA A UNSCHED LANDING C F.O.D. CL CLIMB 1 SW 09 58545 47094 THE AIRCRAFT STRUCK A FLOCK OF BIRDS DURING CLIMBOUT BETWEEN 2,500 TO 3,000 FEET. THE AIRCRAFT WAS RETURNED TO CLE. MA INTENANCE DISCOVERED IMPACT DAMAGE TO FUSELAGE SKIN, APPROXIMATELY 2 FEET BY 2 INCHES IN AREA, TWO FEET AFT OF RADOME ON LT FORWARD LOWER SKIN PANEL AT STA 69. THE AREA WAS REPAIRED IAW ECRA 5330-02468 AND A DIP WAS ISSUED FOR ONE YEAR EVA LUATION BY DACO ENGINEERING. IN ADDITION, CABIN WINDOWS NR 1, NR 2 AND NR 3 ON LT SIDE WERE REPLACED DUE TO DAMAGE CAUS ED BY THE BIRD STRIKE. LEAK CHECK WAS GOOD IAW MM 56-20-00. THE NR 1 ENGINE WAS BORESCOPED AND NO DAMAGE WAS FOUND. 2 L 7 2 4F A6WE 1996112700356 19961127 00356 NE 1996 11 27 9625109987 2 19961120 A 7230 COMPRESSOR DOUG DC9 DC932 3022066 WP PWA JT8 JT8D17 52049 NE ENGINE STALLED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 01 987US 47458 696761 DURING TAKEOFF ROLL, ONE OR MORE ENGINES EXPERIENCED COMPRESSOR STALLS. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE INSPECTED BOTH ENGINES, PERFORMED OPERATIONAL CHECK AND CHECKED OK. COULD NOT DUPLICATE STALLS. 2 L 7 2 4F 4 F A6WE E2EA 1996112700357 19961127 00357 WP 1996 11 27 9625119908 1 19961121 A 7714 N1 INDICATION DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9 52048 NE RT ENGINE LOW A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 01 958N 47254 656968 AS POWER WAS APPLIED FOR TAKEOFF THE RIGHT ENGINE N1 INDICATION WAS LOW. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MA INTENANCE RAN BOTH ENGINES TO TAKEOFF SETTINGS AND ALL INDICTIONS WERE NORMAL. 2 L 7 2 4F 4 F A6WE E2EA 1996112700358 19961127 00358 WP 1996 11 27 9625129856 1 19961121 A 7711 5910297501 NOSE DOME DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE LT ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 765NC 47718 696739 AS POWER WAS APPLIED FOR TAKEOFF LEFT ENGINE EPR INDICATION WAS ABNORMALLY HIGH. CREW ABORTED TAKEOFF AND RETURNED TO G ATE. MAINTENANCE REPLACED LEFT ENGINE NOSE DOME AND EPR TRANSMITTER. RAN ENGINES TO TAKEOFF AND PART POWER SETTINGS, A LL INDICATIONS WERE NORMAL. 2 L 7 2 4F 4 F RT A6WE E2EA 1996112700359 19961127 00359 WP 1996 11 27 9625139961 1 19961121 A 3350 60030451 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 924RW 47185 DURING LINE MAINTENANCE INSPECTION, FOUND AFT OVERWING EXIT AND SEVERAL OVERHEAD CABIN EMERGENCY LIGHTS INOPERATIVE. RE PLACED BATTERY PACKS, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996112700360 19961127 00360 WP 1996 11 27 9625149995 1 19961121 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP TAILCONE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8978E 47327 DURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERIES, O PERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996112700361 19961127 00361 NM 1996 11 27 9625156739 1 19961124 A 3230 69B8035B27 DOWNLOCK ACT BOEING 747 747251F 1384898 NM LT MLG MALFUNCTIONED A A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 639US 45356 2769 23887 DURING APPROACH, THE LEFT WING LANDING GEAR DID NOT FULLY EXTEND. CREW FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND THE AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED LEFT WING LANDING GEAR DOWNLOCK ACTUATOR, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996112700362 19961127 00362 NM 1996 11 27 9625162716 1 19961123 A 7711 EPR SYST BOEING 727 7272S7 138407Z NM PWA JT8 JT8D17 52049 NE LT ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 720RC 22491 688216 AS POWER WAS APPLIED FOR TAKEOFF, LEFT ENGINE EPR INDICATION WAS LOW. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINT ENANCE INSPECTED LEFT ENGINE AND PLACED EPR SYSTEM ON MEL. 2 L 7 3 4F 4 F A3WE E2EA 1996112700363 19961127 00363 SO 1996 11 27 COMA9610334 1 19961120 A 3250 2050000002 POTENTIOMETER EMB 120 EMB120RT SO NLG MALFUNCTION A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 247CA 120255 CLUNKING SOUND AND UNCOMMANDED MOVEMENT FROM NOSE WHEEL STEERING SYSTEM. REPLACED THE NWS FEEDBACK POTENTIOMETER. 2 L 7 2 4T RT A31SO 1996112700364 19961127 00364 EU 1996 11 27 WWMA9600099 1 19961124 A 2120 AIR DISTRIBUTION SAAB SF340 340B 7860101 EU CABIN ODOR A WWMA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 15 319AE 340B319 CREW REPORTED AN INFO TO MAINTENANCE ITEM OF FAINT COMPRESSOR WASH ODORS FROM BOTH BLEEDS ESPECIALLY IN HP SETTINGS. OD ORS DISSIPATED EN ROUTE. MAINTENANCE NOTED INFO AND INFORMED THE STATION THAT PERFORMED THE COMPRESSOR WASH TO GROUND R UN THE AIRCRAFT LONGER. 2 L 7 2 4T RT A52EU 1996112700365 19961127 00365 NM 1996 11 27 SCNA96386 1 19961121 A 3397 1000677 WIRE BOEING 727 727259 138408J NM CABIN BROKEN A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 THE CEILING MOUNTED EMERGENCY EXIT SIGN AT THE L-2 DOOR WAS FOUND TO BE INOPERATIVE. FOUND BROKEN WIRE AT CONNECTOR TO SIGN. REPINNED CONNECTOR AND LIGHT TESTED GOOD IAW MM 33-50-91. 2 L 7 3 4F A3WE 1996112700366 19961127 00366 NM 1996 11 27 SCNA96387 1 19961121 A 3350 1495 BULB BOEING 727 7272J4 1384006 NM AFT AIRSTAIR FAILED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 284SC 21438 TWO EMERGENCY LIGHTS WERE FOUND INOPERATIVE AT THE AFT AIRSTAIRS. RELAMPED TWO EMERGENCY LIGHTS AND LIGHTS TESTED GOOD. 2 L 7 3 4F RT A3WE 1996112700367 19961127 00367 NM 1996 11 27 P5CA9600956 1 19961122 A 5280 BRACKET BOEING 747 747132 1384882 NM RT MLG DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACKED BRACKET RIGHT WING LANDING GEAR STRUT DOOR AFT BRACKET. REMOVED FABRICATED AND INSTALLED BRACKET PER BOEING SRM 51-10-01 AND 51-30-02. 2 L 7 4 4F A20WE 1996112700368 19961127 00368 NE 1996 11 27 P5CA9600957 2 19961120 A 7230 771841770931 FAN BLADE BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE NR 1 ENGINE BENT A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 663071 ON PREFLIGHT, FOUND 5 DAMAGED 1ST STAGE FAN BLADES. BLENDED 2 BLADES PER MAINTENANCE MANUAL 72-31-02, REPLACED 3 BLADES AND MATCHED SET PER MAINTENANCE MANUAL 72-31-02. 2 L 7 4 4F 4 F A20WE E20EA 1996112700369 19961127 00369 NM 1996 11 27 P5CA9600958 1 19961122 A 5230 FITTING BOEING 747 747132 1384882 NM CARGO DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACKED AFT CARGO DOOR LIFT ACTUATOR MOUNT FITTING .75 INCH CRACK OUT OF NR 7 BOLT HOLE. REPAIRED PER POLAR AIR CARGO M AINTENANCE AUTHORIZATION 5310-17:01. 2 L 7 4 4F A20WE 1996112700370 19961127 00370 NM 1996 11 27 P5CA9600959 1 19961118 A 5280 DOOR STOP BOEING 747 747132 1384882 NM LANDING GEAR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACKED DOOR STOP ON LOWER BODY GEAR ADJUSTMENT TO SIDE BRACE. REPLACED STOP PER BOEING MAINTENANCE MANUAL 32-14-00. 2 L 7 4 4F A20WE 1996112700371 19961127 00371 NM 1996 11 27 P5CA9600960 1 19961122 A 5753 SKIN BOEING 747 747132 1384882 NM NR 2 LE FLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 SKIN SEPARATING ON LEFT WING INBOARD FLAP LEFT TOP CORNER INBOARD SIDE. REPAIRED PER BOEING SRM 51-40-15. 2 L 7 4 4F A20WE 1996112700372 19961127 00372 NE 1996 11 27 P5CA9600961 2 19961122 A 7261 BREATHER TUBE BOEING 747 747132 1384882 NM PWA JT9 JT9D7A 52054 NE NR 2 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACKED BREATHER TUBE DUCT ON NR 2 ENGINE INBOARD CORE COWL. WELD REPAIRED PER BAC 5975. 2 L 7 4 4F 4 F A20WE E20EA 1996112700373 19961127 00373 NM 1996 11 27 P5CA9600962 1 19961122 A 7110 ANGLE BOEING 747 747132 1384882 NM NR 4 ENGINE COWL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 THREE CRACKED ANGLES NR 4 ENGINE INBOARD CORE COWL UPPER INNER ANGLES. FABRICATED AND INSTALLED ANGLES PER BOEING SRM 5 1-10-01 AND 51-30-02. 2 L 7 4 4F A20WE 1996112700374 19961127 00374 NM 1996 11 27 P5CA9600963 1 19961122 A 5730 PANEL BOEING 747 747132 1384882 NM RT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 DELAMINATED PANEL RIGHT WING UPPER LEADING EDGE JUST INBOARD OF NR 3 ENGINE. REPAIRED PER BOEING SRM 51-40-09. 2 L 7 4 4F A20WE 1996112700375 19961127 00375 NM 1996 11 27 P5CA9600964 1 19961122 A 5730 PANEL BOEING 747 747132 1384882 NM RT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 DELAMINATED PANEL RIGHT WING UPPER GAP PANEL AT NR 3 PYLON. REPAIRED PER BOEING SRM 51-40-09. 2 L 7 4 4F A20WE 1996112700376 19961127 00376 NM 1996 11 27 P5CA9600965 1 19961122 A 5330 SKIN BOEING 747 747132 1384882 NM EMPENAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 SEVERAL SKIN CRACKS BETWEEN RIVETS ON LEFT SIDE OF TAILCONE EXTERIOR ABOVE APU EXHAUST DUCT. REMOVED AND REPLACED SKIN SECTION PER BOEING SRM 51-10-01 AND 51-30-02. 2 L 7 4 4F A20WE 1996112700377 19961127 00377 NM 1996 11 27 P5CA9600966 1 19961118 A 5754 BRACKET BOEING 747 747132 1384882 NM NR 11 LE FLAP BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEFT WING LEADING EDGE FLAP NR 11 HAS BROKEN BRACKET ON CONNECTION ROD FROM BULLNOSE TO SLAT. REMOVED AND REPLACED BRAC KET PER BOEING SRM 51-10-01. 2 L 7 4 4F A20WE 1996112700378 19961127 00378 1996 11 27 SRAA961114 4 19961121 A 3414 SK40LC AIR SPEED IND LKHEED 382 382E 526413U SO COCKPIT INOPERATIVE A SRAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 23 522SJ 4362 ON TAKEOFF ROLL, F/O'S AIRSPEED INDICATOR STUCK AT 50 KIAS WITH CAPTAIN'S INDICATOR READING 70 KIAS. ABORTED TAKEOFF WI THOUT INCIDENT. PERFORMED PITOT STATIC CHECK, NO FAULT FOUND. REPLACED F/O'S AIR SPEED IND, SYSTEM OPS CHECKED GOOD IA W CH 34. 2 H 7 4 4T A1SO 1996112700379 19961127 00379 NM 1996 11 27 SRAA961115 1 19961104 A 3350 P4010021 BATTERY BOEING 747 747246F NM CABIN DISCHARGED A SRAA K NONE L NO TEST IN INSP/MAINT 1 GL 23 741SJ 22063 DURING ROUTINE MAINTENANCE, FOUND UPPER DECK EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTE RY, OPS CHECKED GOOD PER MM 25-00. 2 L 7 4 4F A20WE 1996112700380 19961127 00380 WP 1996 11 27 HALA96155 1 19961103 A 3350 6011777 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 673MC 47726 HNL - FLT 767 - THE AFT CABIN EMERGENCY FLOOR LIGHTS ARE DIM. REPLACED THE BATTERY PACK AND THE OPERATIONAL CHECK WAS G OOD. (M) 2 L 7 2 4F A6WE 1996112700381 19961127 00381 WP 1996 11 27 HALA96154 1 19961102 A 3350 P4010049 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 669HA 8668 47654 HNL - DURING CHECK, FOUND THE FORWARD FLOOR LIGHT TRACK DIM. REPLACED THE BATTERY PACK AND THE OPERATIONAL CHECK WAS GO OD. (M) 2 L 7 2 4F A6WE 1996112700382 19961127 00382 CE 1996 11 27 COEA9685901 1 19961031 A 5542 263306318 SKIN CESSNA 208 208 2073702 CE RUDDER CRACKED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 859FE 208B0181 A ONE INCH CRACK IN THE RUDDER TRAILING EDGE WAS DISCOVERED DURING THE PREFLIGHT WALK AROUND CHECK IN IFP. REASON UNKNO WN. AIRCRAFT WAS GROUNDED. INSTALLED A COMPLETE SERVICEABLE RUDDER ASSEMBLY. OPERATIONAL CHECK FLIGHT WAS GOOD. (M) 1 H 7 1 3T NT A37CE 1996112700383 19961127 00383 EU 1996 11 27 COEA9671102 1 19961029 A 5713 0146000065 STRINGER FOKKER F27 F27MK500 4990629 EU WS 10760 CRACKED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 711FE 10383 SIP 57-30-04 PAGE 1 X-RAY INSPECTION REVEALED CRACK ON AFT FLANGE OF STRINGER 6, AT NR 8 RIVET FROM LOWER SKIN SPLICE ED GE WS 10760, LEFT WING. CRACK WAS APPROXIMATELY .4 OF AN INCH IN LENGTH. REPAIRED IAW F27 SRM CHAPTER 57-13-20 PAGE 14 , FIG 8, SHEET 3 OF 3. (M) 2 H 7 2 4T A817 1996112700384 19961127 00384 NM 1996 11 27 TAOA109612 1 19961023 A 3610 12355614 CHECK VALVE BOEING 727 727225 1384077 NM NR 1 ENGINE LEAKING A TAOA O OTHER J M WARNING INDICATION OVER TEMP CL CLIMB 1 EA 15 919TS 20447 FLT 6090 - LGA-BOS - EXPERIENCED NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED ON CLIMB-OUT. REDUCED POWER, LIGHT WENT O UT FOR REMAINDER OF FLIGHT. FOUND 6TH STAGE CHECK VALVE LEAKING. REPLACED 6TH STAGE CHECKED VALVE. (M) 2 L 7 3 4F A3WE 1996112700385 19961127 00385 EU 1996 11 27 PLGA9610281 1 19961028 A 2910 L38710SA SWIVEL SAAB SF340 SF340A 7850100 EU RT MLG BROKEN A PLGA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NE 05 744BA 340A105 PSM - FLT 4851 - AFTER DEPARTING PWM EN ROUTE TO LGA, THE CREW NOTED THE HYDRAULIC PUMP RUNNING CONTINOUSLY. THE CREW S ELECTED THE HYDRAULIC PUMP OFF AND NOTED MAIN PRESSURE AND QUANTITY AT ZERO. THE CREW SELECTED GEAR DOWN, PUMPED THE GE AR DOWN AND DIVERTED TO PSM, LANDING WITHOUT INCIDENT. PSM MAINTENANCE REMOVED AND REPLACED THE RIGHT MLG DOWNLOCK ACTU ATOR SWIVEL, REPLENISHED THE HYDRAULIC SYSTEM AND RETURNED THE AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1996112700386 19961127 00386 CE 1996 11 27 96ZZZM1519 1 19961027 A 7712 TORQUE GAUGE BEECH 1900 1900C 1154161 CE RT ENGINE MALFUNCTIONED A MASA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 01 144YV UC144 CLIMB-OUT OF FMN AT 1500 FEET, RIGHT ENGINE TORQUE SURGED FROM 500 TO 800 LBS. FEATHERED RIGHT ENGINE, RETURNED TO GATE AND NO FURTHER INCIDENT. COULD NOT DUPLICATE ON THE GROUND, SWAPPED TORQUE GAUGES AND PERFORMED TEST FLIGHT. TEST FLI GHT WAS SATISFACTORY AND AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A24CE 1996112700387 19961127 00387 CE 1996 11 27 96ZZZM1520 1 19961005 A 6120 310047503 BETA CABLE BEECH 1900 1900D 1154162 CE LT ENGINE BINDING A MASA E ENGINE SHUTDOWN X ENGINE FLAMEOUT TO TAKEOFF 1 SW 01 35YV 8525 UE35 JUST AFTER TAKEOFF FROM GALLUP, LEFT ENGINE LOST POWER. RETURNED TO GATE. MAINTENANCE FOUND LEFT BETA CABLE BOUND UP A ND CAUSED BETA VALVE TO COME OUT OF RIG. REPLACED BETA CABLE AND RIGGED. (M) 2 L 7 2 4T RT A24CE 1996112700388 19961127 00388 NM 1996 11 27 TAOA109615 1 19961031 A 5712 RIB BOEING 727 727225 1384077 NM BS 760.95 CRACKED A TAOA K NONE O OTHER IN INSP/MAINT 1 EA 15 923TS 20441 AD NR 94-07-08 INSPECTION OF THE LEFT SIDE BL 70.5 WING RIB UPPER CHORD REVEALED CRACKS IN THE FORWARD TWO FASTENER HOLE S COMMON TO THE BS 760.95 FRAME. THE CRACK EXTENDS SLIGHTLY INTO THE HORIZONTAL FLANGE. CORROSION WAS ALSO DETECTED ON THE INNER SURFACE OF THE VERTICAL FLANGE AROUND THE CRACKED FASTENER HOLES. ENGINEERING AUTHORIZATION NR S1485 ACCOMPL ISHED. TRIMMED OUT CRACKED/CORRODED SECTION OF VERTICAL FLANGE AND STOP DRILLED LOWER END OF CRACK, INSPECTED SLOTTED A REA AND TRIMMED AREA TO ENSURE NO ADDITIONAL DAMAGE IS PRESENT. (M) 2 L 7 3 4F A3WE 1996112700389 19961127 00389 NM 1996 11 27 TWRA96350 1 19961029 A 3350 3004093 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 619FF TOW2389 21316 DURING DAILY CHECK, FOUND LEFT SIDE BOTTOM OVERWING LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY. OPS CHECKED NORMA L PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996112700390 19961127 00390 NM 1996 11 27 TAOA119601 1 19961106 A 3350 312010 FUSE BOEING 727 727225 1384077 NM CABIN BLOWN A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 923TS 20441 L-1 AND R-1 EMERGENCY EXIT IDENTIFIER LIGHTS INOP. REPLACED FUSE IN FORWARD BATTERY PACK, OPS CHECK OK. (M) 2 L 7 3 4F A3WE 1996112700391 19961127 00391 NM 1996 11 27 TWAA9613201 1 19961028 A 2612 895312 FIRELOOP BOEING 747 747257B 1384853 NM APU MALFUNCTIONED A TWAA O OTHER N FALSE WARNING CR CRUISE 1 CE 05 303TW 20116 LGW - DURING CRUISE THE APU FIREWARNING LIGHT ILLUMINATED AND BELL SOUNDED WITH APU SHUTDOWN. REMOVED AND REPLACED APU DOOR FIREWARNING LOOP, MFG P/N 895312, AND THE FIRE BOTTLE, MFG P/N 34505501M. OPERATIONAL CHECK NORMAL. (M) 2 L 7 4 4F A20WE 1996112700392 19961127 00392 NM 1996 11 27 TWAA9613202 1 19961028 A 7603 315T304013 TORQUE BOX BOEING 767 767231 1385131 NM NR 1 ENGINE MALFUNCTIONED A TWAA O OTHER O OTHER CL CLIMB 1 CE 05 608TW 22571 JFK - FLT 741 - DURING CLIMB-OUT, THE NR 1 ENGINE THRUST LEVER WAS DIFFICULT TO MOVE. REMOVED AND REPLACED LOWER TORQUE BOX, MFG P/N 315T3040-13 AND THE LOWER TELEFLEX CABLE, MFG P/N 580-299-101. OPERATIONAL CHECK AND ENGINE RUN NORMAL. ( M) 2 L 7 2 4F RT A1NM 1996112700393 19961127 00393 NM 1996 11 27 TWAA9613203 1 19961029 A 3610 652673831 CROSSOVER PIPE BOEING 727 727231 1384079 NM NR 1 ENGINE DAMAGED A TWAA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 54336 20490 STL - DURING CLIMB-OUT THE NR 1 ENGINE FIREWARNING ILLUMINATED, POWER WAS REDUCED TO IDLE, THE LIGHT WENT OUT. REMOVED AND REPLACED THE CROSSOVER PIPE, MFG P/N 65-26738-31, FROM THE 6TH STAGE TO THE CONSTANT SPEED DRIVE AND SUPPLEMENTAL AN TI-ICE VALVE DUE TO A HOLE. ENGINE RUN AND LEAK CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1996112700394 19961127 00394 NE 1996 11 27 TWAA9613402 2 19961103 A 7230 COMPRESSOR DOUG DC9 DC983 3022083 WP PWA JT8 JT8D217C 52053 NE NR 1 ENG STALL A TWAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 CE 05 9404V 53140 SFO - DURING CLIMB NR 1 ENGINE, S/N 3210, EXPERIENCE A COMPRESSOR STALL AND VIBRATION. SHUT DOWN ENGINE. CHECKED ENGIN E INLET AND EXHAUST, BORESCOPE OF 6TH AND 7TH STAGE COMPRESSOR, CHECKED 8TH AND 16TH STAGE BLEED AIR DUCT END CAPS, CHEC KED ALL MAGNET CHIP DETECTORS AND OIL FILTER. ALL CHECKS WERE NORMAL. ENGINE PERFORMANCE RUNUP CHECKED NORMAL. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 1996112700395 19961127 00395 WP 1996 11 27 TWAA9613304 1 19961026 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 598 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 988Z 47134 STL - DURING SPECIAL CHECK, FOUND END FITTING OF LONGERON 30 CRACKED, STATION 598. REPLACED FITTING PER SRM 51-00 AND T WA STANDARD PRACTICES. (M) 2 L 7 2 4F A6WE 1996112700396 19961127 00396 WP 1996 11 27 TWAA9613301 1 19961031 A 3241 CONNECTOR DOUG DC9 DC982 3022082 WP ANTI-SKID CORRODED A TWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 05 902TW 49153 STL - ABORTED TAKEOFF AT 50 KNOTS DUE TO A WHEEL NOT TURNING LIGHT ILLUMINATION. CLEANED CORROSION FROM THE ANTI-SKID V ALVE CONNECTOR. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F A6WE 1996112700397 19961127 00397 NM 1996 11 27 TWAA9613302 1 19961031 A 3260 DOWNLOCK SWITCH BOEING 727 727231 1384079 NM RT MLG FAILED A TWAA O OTHER N FALSE WARNING AP APPROACH 1 CE 05 54342 21629 STL - DURING APPROACH, FOLLOWING GEAR EXTENSION THE RIGHT MAIN GEAR UNSAFE LIGHT ILLUMINATED. REMOVED AND REPLACED RIGH T GEAR DOWN LOCK SWITCH DUE TO WEAR, MFG P/N H10-1026-2. (M) 2 L 7 3 4F A3WE 1996112700398 19961127 00398 NE 1996 11 27 TWAA9613303 2 19961030 A 7200 ENGINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D217C 52053 NE NR 2 FAILED A TWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 05 EICIW 49785 1212 STL - FLT 391 - DURING CLIMB, NR 2 ENGINE, FAILED. THROTTLE WAS RETARDED TO IDLE RESULTING IN AN ENGINE CHANGE. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 1996112700399 19961127 00399 WP 1996 11 27 TWAA9613305 1 19961030 A 5320 FITTING DOUG DC9 DC951 3022051 WP BS 732.5 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 410EA 47731 STL - DURING SPECIAL CHECK, FOND A TWO INCH CRACK IN LONGERON 29R FITTING, STATION 732.5 FORWARD SIDE. REMOVED AND REPL ACED FITTING PER SRM 51-30-5 AND TWA STANDARD PRACTICES. (M) 2 L 7 2 4F A6WE 1996112700400 19961127 00400 NM 1996 11 27 TWAA9613401 1 19961102 A 3230 RETRACT MECH BOEING 727 727231 1384079 NM RT MLG LACK OF LUBE A TWAA O OTHER J WARNING INDICATION AP APPROACH 1 CE 05 54342 21629 DTW - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED. CYCLED LANDING GEAR AND USED MANUAL EXTENSION SYSTEM. LUBRICATED LANDING GEAR AND CYCLED LANDING GEAR. LANDING GEAR OPERATIO N AND INDICATION SYSTEM CHECKED NORMAL. (M) 2 L 7 3 4F A3WE 1996112700401 19961127 00401 WP 1996 11 27 96ZZZM1521 1 19961011 A 5712 RIB DOUG DC9 DC982 3022082 WP WS 331 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 959U 49704 MCI - DURING OP-16, FOUND A ONE INCH CRACK IN UPPER RADIUS OF RIGHT WING LE RIB AFT UPPER END, STATION 331. REPLACED LE RIB PER SRM 51-01 AND TWA STANDARD PRACTICES. (M) 2 L 7 2 4F A6WE 1996112700402 19961127 00402 WP 1996 11 27 96ZZZM1522 1 19961011 A 5320 CLIP DOUG DC9 DC982 3022082 WP BS 1211-1329 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 959U 49704 MCI - DURING OP-16, FOUND CORROSION AT CLIP NUT HOLES OF RIGHT CARGO TRACK IN AFT CARGO BIN, FS 1211 TO FS 1329. REPLAC ED TRACK PR SRM 51-01, PAGE 1. 2 L 7 2 4F A6WE 1996112700403 19961127 00403 WP 1996 11 27 96ZZZM1523 1 19961011 A 5312 BULKHEAD SUPPORT DOUG DC9 DC982 3022082 WP BS 1322 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 959U 49704 MCI - DURING OP-16, FOUND CORROSION ON BULKHEAD FLOOR SUPPORT, FS 1322. INSTALLED NEW SUPPORT PER SRM 51-01 AND TWA STA NDARD PRACTICES. 2 L 7 2 4F A6WE 1996112700404 19961127 00404 WP 1996 11 27 96ZZZM1524 1 19961011 A 5712 RIB DOUG DC9 DC982 3022082 WP WS 312 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 959U 49704 MCI - DURING OP-16, FOUND A 1 INCH CRACK IN UPPER RADIUS OF RIGHT WING LE RIB U PPER END, STATION 312. REPLACED LE RIB PER SRM 51-01 AND TWA STANDARD PRACTICES. 2 L 7 2 4F A6WE 1996112700405 19961127 00405 WP 1996 11 27 96ZZZM1525 1 19961011 A 5720 SPLICE DOUG DC9 DC982 3022082 WP WS 164 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 959U 49704 MCI - DURING OP-16, FOUND A 1 INCH CRACK IN RIGHT WING LE SPLICE PLATE, STATION 164. REPAIRED PER SSRM 57-40-103. 2 L 7 2 4F A6WE 1996112700406 19961127 00406 WP 1996 11 27 96ZZZM1526 1 19961021 A 3231 RETRACT MECH DOUG DC9 DC951 3022051 WP NLG DOOR LACK OF LUBE A TWAA O OTHER E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 CE 05 411EA 47732 STL - AFTER TAKEOFF HAD VIBRATION FROM NOSE LANDING GEAR DOORS AFTER LANDING GEAR RETRACTION. CYCLED LANDING GEAR. FOU ND RIGHT NOSE LANDING GEAR DOOR BUNGEE LINK, MFG P/N 3956785-1, DRY AND DIRTY. CLEANED AD LUBRICATED BUNGEE LINK. NOSE LANDING GEAR DOOR OPERATION CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 1996112700407 19961127 00407 WP 1996 11 27 96ZZZM1527 1 19961021 A 3297 WIRE LKHEED 1011 10113851 5265010 WP LT MLG BROKEN A TWAA O OTHER N FALSE WARNING AP APPROACH 1 CE 05 31013 193B1035 STL - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED LEFT MAIN LANDING GEAR DID NOT INDICATE DOWN AND LOCKED. CYCLED LA NDING GEAR AND RELAMPED INDICATOR. FOUND BROKEN WIRE AT PIN 4 OF LIGHT BASE, MFG P/N 10648LD3. REPAIRED BROKEN WIRE AN D REPLACED LIGHT BASE. LANDING GEAR OPERATION AND INDICATION CHECKED NORMAL. (M) 2 L 7 3 4F A23WE 1996112700408 19961127 00408 WP 1996 11 27 TWAA9613003 1 19961027 A 3350 58222 POWER SUPPLY DOUG DC9 DC915 3022036 WP CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 971Z 45773 STL - EMERGENCY EGRESS LIGHTS AT ROWS 2.5 INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY, MFG P/N 5822-2. OPERATION CH ECK NORMAL. (M) 2 L 7 2 4F A6WE 1996112700409 19961127 00409 WP 1996 11 27 TWAA9613004 1 19961028 A 3350 LIGHT DOUG DC9 DC941 302207N WP CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 934L 47618 STL - EMERGENCY ESCAPE PAHT LIGHTING ILLUMINATED DURING FLIGHT. CLEANED MOISTURE FROM LIGHT TRACK, OPERATIONAL CHECK NO RMAL. (M) 2 L 7 2 4F A6WE 1996112700410 19961127 00410 WP 1996 11 27 TWAA9613005 1 19961014 A 5347 TRACK DOUG DC9 DC982 3022082 WP BS 1290 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 959U 49704 MCI - DURING OP-16, FOUND CORROSION ON FLOOR TRACK, STATION 1290, LBL 21. REMOVED CORRODED TRACK AND INSTALLED NEW TRAC K PER SRM 53-05, PAGE 4. (M) 2 L 7 2 4F A6WE 1996112700411 19961127 00411 WP 1996 11 27 TWAA9613006 1 19961014 A 5315 FLOOR BEAM DOUG DC9 DC982 3022082 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 959U 49704 MCI - DURING OP-16, FOUND CORROSION ON CABIN LOWER FLOOR BEAM. INSTALLED NEW ANGLE PER SRM 51-01, PAGE 1, ITEM C. (M) 2 L 7 2 4F A6WE 1996112700412 19961127 00412 WP 1996 11 27 TWAA9613001 1 19961027 A 2150 DUCT DOUG DC9 DC983 3022083 WP LT PACK FAILED A TWAA O OTHER J WARNING INDICATION TO TAKEOFF 1 CE 05 9413T 53188 JFK - DURING TAKEOFF TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. REINSTALLED SEPARATED RUBBER DUCT AT LEFT PAC K. ENGINE RUNS AND LEAKS CHECKS NORMAL. (M) 2 L 7 2 4F RT A6WE 1996112700413 19961127 00413 WP 1996 11 27 96ZZZM1528 1 19961011 A 5320 FORMER DOUG DC9 DC982 3022082 WP BS 1287 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 959U 49704 MCI - DURING OP-16, FOUND CORROSION ON FORMER CAP WEB FOOT, FS 1287, RBL 5 TO LBL 20. CUT OUT AND REMOVED CORRODED AREA INSTALLED REPAIR PER SRM 53-03, FIGURE 2A, VIEW Q. (M) 2 L 7 2 4F A6WE 1996112700414 19961127 00414 NM 1996 11 27 TWAA9613002 1 19961027 A 2780 RETRACT MECH BOEING 767 767231 1385131 NM LE FLAPS MALFUNCTIONED A TWAA O OTHER J WARNING INDICATION TO TAKEOFF 1 CE 05 604TW 22567 LAX - DURING TAKEOFF LEADING EDGE FLAPS WOULD NOT RETRACT. PERFORMED BITE CHECK, CHECKED ALL 24 LEADING EDGE FLAP SENSO RS, OPERATED FLAPS SEVERAL CYCLES. ALL CHECKS NORMAL. (M) 2 L 7 2 4F RT A1NM 1996112700415 19961127 00415 WP 1996 11 27 96ZZZM1529 1 19961011 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1250 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 959U 49704 MCI - DURING OP-16, FOUND CORROSION ON FRAME, LONGERON 28R TO LONGERON 28L, STATION 1250. REMOVED CORROSION PER SRM 51- 10-03, AND REPAIRED PER SRM 53-03, FIGURE 2A, VIEW Q, AND TWA STANDARD PRACTICES. (M) 2 L 7 2 4F A6WE 1996112700416 19961127 00416 WP 1996 11 27 TWAA9613010 1 19961014 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 769 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 959U 49704 MCI - DURING OP-16, FOUND CORROSION ON RIGHT SIDE OF FUSELAGE SKIN ABOVE LONGERON 29R, FS 769. REPAIRED PER SRM 53-543 AND TWA STANDARD PRACTICES. (M) 2 L 7 2 4F A6WE 1996112700417 19961127 00417 WP 1996 11 27 TWAA9613009 1 19961014 A 5321 FLOOR DOUG DC9 DC982 3022082 WP BS 1208 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 959U 49704 MCI - DURING OP-16, FOUND HOLE IN CABIN FLOOR MEMBRANE ADJACENT TO LEFT SIDEWALL, FS 1208. INSTALLED REPAIR PER SRM 53- 01, APGE 17, FIGURE 4. (M) 2 L 7 2 4F A6WE 1996112700418 19961127 00418 WP 1996 11 27 TWAA9613011 1 19961014 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 807-820 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 959U 49704 MCI - DURING OP-16, FOUND CORROSION ON LOWER FUSELAGE SKIN, STATION 807-820, RBL 5. REPAIRED PER SRM 53-04, FIGURE 53. (M) 2 L 7 2 4F A6WE 1996112700419 19961127 00419 WP 1996 11 27 TWAA9613007 1 19961014 A 5312 BULKHEAD PANEL DOUG DC9 DC982 3022082 WP BS 1322 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 959U 49704 MCI - DURING OP-16, FOUND CORROSION ON ALL SUPPORTS ON VERTICAL BULKHEAD PANEL, FS 1322. REMOVED CORROSION PER SRM 91-0 1-3, AND REPLACED PARTS PER SRM 51-10. (M) 2 L 7 2 4F A6WE 1996112700420 19961127 00420 WP 1996 11 27 TWAA9613008 1 19961014 A 5347 TRACK DOUG DC9 DC982 3022082 WP BS 1300 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 959U 49704 MCI - DURING OP-16, FOUND CORROSION ON NR 2 FLOOR TRACK, STATION 1300. REPLACED CORRODED SECTION OF TRACK PER SRM 53-05 , FIGURE 4F. (M) 2 L 7 2 4F A6WE 1996112700421 19961127 00421 WP 1996 11 27 96ZZZM1530 1 19961014 A 5320 FORMER DOUG DC9 DC982 3022082 WP BS 1322 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 959U 49704 MCI - DURING OP-16, FOUND CORROSION ON FORMER WEB AND CAP, LONGERON 27L TO LONGERON 28R, STATION 1322. REMOVED CORROSIO N PER SRM 51-10-3 AND REPAIRED PER SRM 53-03 AND TWA STANDARD PRACTICES. (M) 2 L 7 2 4F A6WE 1996112700422 19961127 00422 WP 1996 11 27 96ZZZM1531 1 19961014 A 5347 TRACK DOUG DC9 DC982 3022082 WP BS 1280 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 959U 49704 MCI - DURING OP-16, FOUND CORROSION ON LEFT OUTBOARD GALLEY TIEDOWN TRACK, STATION 1280. REPLACED GALLEY TIEDOWN TRACK PER SRM 51-01. 2 L 7 2 4F A6WE 1996112700423 19961127 00423 WP 1996 11 27 96ZZZM1532 1 19961014 A 5531 RIB DOUG DC9 DC982 3022082 WP VERT STAB CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 959U 49704 MCI - DURING OP-16, FOUND LOWER LEADING EDGE PANEL VERTICAL STABILIZER LOWER ENDS OF RIBS CRACKED, LEFT AND RIGHT SIDE. REPAIRED PER SRM 55-30-102, FIGURE 201. 2 L 7 2 4F A6WE 1996112700424 19961127 00424 WP 1996 11 27 96ZZZM1533 1 19961014 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 824 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 959U 49704 MCI - DURING OP-16, FOUND CORROSION ON CENTERLINE FUSELAGE SKIN, LONGERON 30, FS 824. REMOVED CORROSION PER SRM 51-10-0 3 AND INSTALLED DOUBLER PER SRM 53-04, PAGE 321 AND ARA 10722. 2 L 7 2 4F A6WE 1996112700425 19961127 00425 WP 1996 11 27 96ZZZM1534 1 19961016 A 3350 CONNECTOR DOUG DC9 DC931 3022065 WP CABIN DIRTY A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 982PS 47251 STL - DURING APPROACH EGRESS LIGHTS IN AFT CABIN WOULD INTERMITTENTLY ILLUMINATE. FOUND DIRTY FLEX CABLE CONNECTOR, MFG P/N 5853-1. CLEANED CABLE CONNECTOR AND SECURED CONNECTOR. EGRESS LIGHT SYSTEM OPERATION CHECKED NORMAL. 2 L 7 2 4F A6WE 1996112700426 19961127 00426 WP 1996 11 27 96ZZZM1535 1 19961014 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1271 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 959U 49704 MCI - DURING OP-16, FOUND CORROSION IN AFT CARGO COMPARTMENT LONGERON 17L TO LONGERON 27R FRAME, FS 1271. REMOVED CORRO SION PER SRM 51-10-3 AND INSTALLED REPAIR PER SRM 53-03, PAGE 4E, VIEW Q. (M) 2 L 7 2 4F A6WE 1996112700427 19961127 00427 NM 1996 11 27 TWAA9613101 1 19961029 A 3350 S106CD BATTERIES BOEING 727 727231 1384079 NM CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 54326 20233 LGA - FLT 293 - DURING ROUTINE LAYOVER MAINTENANCE, THE EMERGENCY EXIT LIGHT OVER THE LEFT FORWARD OVERWING EXIT WAS INO PERATIVE. REMOVED AND REPLACED BATTERIES, MFG P/N S106CD. OPERATIONAL CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1996112700428 19961127 00428 NM 1996 11 27 USAASB96212 1 19961020 A 2433 2299 TR UNIT BOEING 737 737201 1384454 NM E/E COMP FAILED A USAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 EA 19 241US 22443 ITH - FLT 2075 - CLIMBING THROUGH 12,000 FT, THE CABIN PRESS WARNING HORN SOUNDED. DESCENDED TO 10,000 FT AND WENT TO S TANDBY. CHECKED FOR C/B'S POPPED AND FOUND THE E/E COOLING FAN C/B POPPED. SWITCHED TO ALTERNATE FAN AT WHICH TIME FLT ATTENDANTS REPORTED SMOKE IN CABIN. CAPT TURNED ALTERNATE FAN BACK TO NORMAL AND DIVERTED TO ITH. AN EMERG WAS DECLAR ED. THE FLT LANDED W/O FURTHER INCIDENT. MX ACCOMP PRESS CHECK PER MM 21-31-00. OPS CHECK GOOD WITH NO FAULTS FOUND. SMOKE IN CABIN CAUSED BY BURNED UP NR 1 TRANSFORMER RECTIFIER UNIT. REPLACED SAME. OPS CHECK GOOD. COOLING FAN CHECK S OK IN NORMAL AND ALTERNATE. (M) 2 L 7 2 4F A16WE 1996112700429 19961127 00429 NM 1996 11 27 USAA960673 1 19961018 A 5240 FRAME BOEING 737 737201 1384454 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 225US 47563 21667 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 CRACKS .25 INCH AND .375 INCH FORWARD SERVICE DOOR AFT FRAME 1 AT NR 3 STOP, 1 AT NR 4 STOP. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-3. (M) 2 L 7 2 4F A16WE 1996112700430 19961127 00430 NM 1996 11 27 USAA960671 1 19961018 A 5314 KEEL BEAM BOEING 737 737201 1384454 NM BS 720-725 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 225US 47563 21667 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 3 SCREW HOLES CORRODED .25 INCH AROUND OPENINGS, BS 720-725 RIGHT FLANGE UPPER SIDE KEEL BEAM. INSTALLED DOUBLER AFTER SPOT FACING, REPAIRED PER EA NR 41637. CORROSION TASK NR C53-212-01, CO RROSION LEVEL 1. (M) 2 L 7 2 4F A16WE 1996112700431 19961127 00431 NM 1996 11 27 USAA960687 1 19961021 A 5330 SKIN BOEING 737 737201 1384454 NM BS 328 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 228US 21817 ROA - DURING CX-5 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 2 CRACKS 3.1875 INCH AND .5 INCH FORWARD GALLEY DOOR CUT O UT AFT LOWER CORNER (STRINGER 17R BS 328) FUSELAGE SKIN. INSTALLED TRIPLER, REPAIRED PER SRM 53-30-3 FIG 26. (M) 2 L 7 2 4F A16WE 1996112700432 19961127 00432 NM 1996 11 27 USAA960688 1 19961021 A 5330 SKIN BOEING 737 737201 1384454 NM BS 857 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 228US 45886 21817 ROA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND 1.375 INCH CRACK AFT GALLEY DOOR CUT OUT FORWARD LOWER CORNER (STRINGER 17 R BS 857) FUSELAGE SKIN. INSTALLED TRIPLER, REPAIRED PER SRM 53-30-3 FIG 24, EA 58949. (M) 2 L 7 2 4F A16WE 1996112700433 19961127 00433 NM 1996 11 27 USAA960689 1 19961020 A 5330 SKIN BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 235US 41654 22275 INT - DURING B-CHECK, EDDY CURRENT INSPECTION, FOUND .120 INCH CRACK LOWER FORWARD CORNER OF FORWARD SERVICE DOOR LOWER CUT OUT IN RADIUS SKIN. INSTALLED DOUBLER AND REWORKED PER EA AND SRM. REPAIRED PER EA 41649, SRM 53-30-3 FIG 32. (M) 2 L 7 2 4F A16WE 1996112700434 19961127 00434 NM 1996 11 27 USAA960674 1 19961018 A 5320 FORMER BOEING 737 737201 1384454 NM BS 500 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 225US 47563 21667 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH STATION 500 A STRINGER 26 R FORMER. INSTALLE D DOUBLER REPAIR, REPAIRED PER SRM 51-40-3, CORROSION TASK NR C53-208-01, CORROSION LEVEL 1. (M) 2 L 7 2 4F A16WE 1996112700435 19961127 00435 NM 1996 11 27 USAA960676 1 19961018 A 5320 WEB BOEING 737 737201 1384454 NM BS 706 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 225US 47563 21667 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CRACKS APPROXIMATELY 1 INCH LONG IN VERTICAL WEB STATION 706 RBL 24. IN STALLED DOUBLER, REPAIRED PER SRM 51-40-2. (M) 2 L 7 2 4F A16WE 1996112700436 19961127 00436 EU 1996 11 27 RAIA961037 1 19961030 A 5347 S53678001225 SEAT TRACK AEROSP ATR72 ATR72202 8680940 EU CABIN CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 723TE 9615 283 STL - AFT CORROSION ON FLIGHT ATTENDANTS AFT SEAT TRACK. MAINTENANCE REPLACED THE AFT FLIGHT ATTENDANT SEAT TRACK. (M) 2 H 7 2 4T RT A53EU 1996112700437 19961127 00437 WP 1996 11 27 USAA960709 1 19961028 A 5730 SKIN DOUG DC9 DC931 3022065 WP LT WING CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 958VJ 59849 47351 PIT - DURING Q-4/C-6 CHECK, FOUND LEVEL II CORROSION AT NR 1 SLAT TRACK CUT OUT OUTBOARD LEADING EDGE OF LEFT WING. CUT OUT CORRODED AREA AND INSTALLED DOUBLER 9 INCH BY 7.5 INCH PER SRM 57-06 FIG 4. CORROSION LEVEL 2, COROSION TASK NR C1 1-57300. (M) 2 L 7 2 4F A6WE 1996112700438 19961127 00438 WP 1996 11 27 USAA960710 1 19961028 A 5315 9915561 FLOOR BEAM DOUG DC9 DC931 3022065 WP BS 996 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 958VJ 59849 47351 PIT - DURING Q-4/C-6 CHECK, FOUND LEVEL 2 CORROSION AT STATION 996 FLOOR BEAM. INSTALLED NEW BEAM AND MFG DOUBLERS PER SRM 53-05 PAGE 212A FIG 72. CORROSION LEVEL 2. CORROSION TASK NR C58-53300. (M) 2 L 7 2 4F A6WE 1996112700439 19961127 00439 NM 1996 11 27 USAA960692 1 19961027 A 5313 STRINGER BOEING 737 7374B7 1384702 NM BS 747-767 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 19567 24560 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION .5 INCH BY .5 INCH AND 4 INCH CRACK AT STATION 747 TO STATION 767, ABOVE STRINGER 26R. INSTALLED SPLICE AND REPAIRED PER SRM 53-00-53. CORROSION TASK NR C53-208-11, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1996112700440 19961127 00440 NM 1996 11 27 USAASB96216 1 19961024 A 2910 NAS161212 PACKING BOEING 737 737401 1384701 NM 'A' HYD SYSTEM FAILED A USAA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CR CRUISE 1 EA 19 404US 23886 MIA - FLT 1876 - DURING CRUISE, SYS 'A' HYD QTY DECREASED TO ONE QUARTER MARK. SYS 'A' LOW PRESS LITE ILLUMINATED ON EN G NR 1 HYD PUMP. CREW SHUT OFF NR 1 ENGINE DRIVEN HYDRAULIC PUMP. SHORTLY AFTER, SYSTEM 'A' HYDRAULIC QTY DECREASED TO ZERO AND SYSTEM 'A' PRESS READ NORMAL. CREW DECIDED TO DIVERT TO MIA. FLT LANDED WITHOUT FURTHER INCIDENT. ALL SYSTE MS ON SYSTEM 'A' HYDRAULIC SIDE FUNCTIONED NORMAL FOR LANDING. MAINTENANCE FOUND LEAK AT UNION ON PRESSURE INLET SIDE O F 'A' SYSTEM HYDRAULIC MODULE. REPLACED PACKING AND SERVICED 'A' SYSTEM TO PROPER LEVEL. LEAK CHECK GOOD. RAN ENGINES TO CHECK OPERATION OF FLIGHT CONTROLS. ALL FUNCTION NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996112700441 19961127 00441 NE 1996 11 27 USAASB96217 2 19961024 A 7200 ENGINE BOEING 737 737201 1384454 NM PWA JT8 JT8D15A 52051 NE LEFT FAILED A A USAA A E UNSCHED LANDING ENGINE SHUTDOWN E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CL CLIMB 1 EA 19 256AU 30396 22798 708959 BDL - FLT 268 - AT FL 285, CAPTAIN HEARD A LOUD BANG. THE NR 1 ENGINE THEN SHOWED INDICATIONS OF LOW POWER. AS A PRECA UTION, THE NR 1 ENGINE WAS SHUT DOWN AND THE FLIGHT DIVERTED TO BDL. CAPT DID DECLARE AN EMERGENCY. FLIGHT LANDED WITH OUT FURTHER INCIDENT. TOTAL SINGLE ENGINE TIME WAS 10 MINUTES. MAINTENANCE REPLACED THE NR 1 ENGINE ASSEMBLY PER JOB C ARD. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F 4 F A16WE E2EA 1996112700442 19961127 00442 EU 1996 11 27 USAAF96111 1 19961026 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 881US 11333 DURING OVERNIGHT MAINTENANCE CHECK, MECHANIC FOUND FIRST CLASS FLOOR LEVEL EMERGENCY LIGHTING INOP. MAINTENANCE REPLACE D BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT 1996112700443 19961127 00443 EU 1996 11 27 USAAF96113 1 19961101 A 3350 CONNECTOR FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 488US 11240 DURING OVERNIGHT MAINTENANCE CHECK, FOUND SEAT LEVEL EMERGENCY LIGHTS INOP BETWEEN ROW 6 AND 9. MAINTENANCE REPAIRED CO NNECTOR, ROW 8 LEFT SIDE. (M) 2 L 7 2 4F RT A20EU 1996112700444 19961127 00444 EU 1996 11 27 USAAF96112 1 19961021 A 3350 6008905 BATTERY PACK FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 483US 11233 DURING MAINTENANCE B-CHECK, SEVERAL CABIN CEILING EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE REPLACED RIGHT FOR WARD BATTERY PACK AND BATTERIES. (M) 2 L 7 2 4F RT A20EU 1996112700445 19961127 00445 NM 1996 11 27 W8PA960160 1 19961016 A 5523 SKIN BOEING 737 7373B7 1384580 NM LT ELEV TAB DELAMINATED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 509AU 23384 LEFT ELEVATOR CONTROL TAB LEADING EDGE DELAMINATED AROUND INBOARD FITTING. REPAIRED LEFT ELEVATOR INBOARD LEADING EDGE ALL WORK DONE. (M) 2 L 7 2 4F RT A16WE 1996112700446 19961127 00446 NM 1996 11 27 W8PA960158 1 19961015 A 5347 SEAT TRACK BOEING 737 7373B7 1384580 NM BS 346 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 509AU 23384 DURING C-CHECK, THE LBL 20 SEAT TRACK IS CORRODED BS 346 - BS 352, WL 208. REMOVED DAMAGED SEAT RACK. FABRICATED, ALOD INED, PRIMED, PAINTED AND INSTALLED NEW SEAT TRACK. (M) 2 L 7 2 4F RT A16WE 1996112700447 19961127 00447 NM 1996 11 27 W8PA960157 1 19961021 A 3350 BULBS BOEING 737 7373Q8 1384670 NM CABIN FAILED A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 956WP 24299 EMERGENCY EXIT LIGHTING ROWS 18-21 INOP. SECURED SEVERAL LOOSE CONNECTORS AND REPLACED BAD BULBS. (M) 2 L 7 2 4F RT A16WE 1996112700448 19961127 00448 NM 1996 11 27 W8PA960159 1 19961015 A 5347 SEAT TRACK BOEING 737 7373B7 1384580 NM BS 346 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 509AU 23384 DURING C-CHECK, THE LBL 40 SEAT TRACK IS CORRODED BS 346 - BS 351, WL 208. CORROSION FOUND TO BE OUT OF LIMITS. REMOVE D DAMAGED SEAT TRACK, FABRICATED, ALODINED, PRIMED, PAINTED AND INSTALLED NEW SEAT TRACK. (M) 2 L 7 2 4F RT A16WE 1996112700449 19961127 00449 NM 1996 11 27 W8PA960166 1 19961106 A 3397 WIRE BOEING 737 7373Y0 1384671 NM CABIN LOOSE A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 955WP 24463 FOUND TRACK LIGHTING IN CABIN DAMAGED AT ROWS 12, 14, 18. FOUND WIRE DISCONNECTED. RECONNECTED AND SECURED LIGHTING. ( M) 2 L 7 2 4F RT A16WE 1996112700450 19961127 00450 NM 1996 11 27 W8PA960165 1 19961108 A 3350 LIGHT BOEING 737 7373Y0 1384671 NM CABIN INOPERATIVE A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 955WP 24463 EMERGENCY FLOOR TRACK LIGHT AT ROW 18 IINOP. RELAMPED EMERGENCY LIGHT AT ROW 18. (M) 2 L 7 2 4F RT A16WE 1996112700451 19961127 00451 WP 1996 11 27 96ZZZM1536 1 19961018 A 3231 269003213 LOCK ACTUATOR 269002121 LKHEED 1011 10113851 5265010 WP LT MLG DOOR FAILED A WRNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 311EA DA55 193A1012 MAIN GEAR DOOR LIGHT AND RED INTRANSIT LIGHT CAME ON DURING CLIMB-OUT. AIRCRAFT RETURNED TO AIRPORT. LANDING NORMAL. R EMOVED AND REPLACED MAIN GEAR DOOR LOCK ACTUATOR IAW 32-33-08 OF THE MM. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVIC E. (M) 2 L 7 3 4F A23WE 1996112700452 19961127 00452 EU 1996 11 27 VTZA97047 1 19961030 A 7722 8974764 EGT COMP RES BAG JETSTM JETSTM3201 1500217 EU LT ENGINE OUT OF ADJUST A VTZA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 27 491UE 911 FLT 6273 - IAD-LYH - ABORTED TAKEOFF DUE TO BOTH ENGINES NOT MAKING TARGET TORQUE. AIRCRAFT RETURNED TO THE GATE WHERE THE MAINTENANCE DEPARTMENT TROUBLESHOT THE DISCPREPANCY AND FOUND THAT THE LEFT ENGINE NEEDED THE EGT COMP RESISTOR ADJU STED. THE RIGHT ENGINE HAD NO DISCREPANCY NOTED DURING ENGINE RUNS. MAINTENANCE ADJUSTED THE LEFT EGT COMP RESISTOR AN D PERFORMED ENGINE RUNS ON BOTH ENGINES IAW MM. AIRCRAFT WAS THEN RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A56EU 1996112700453 19961127 00453 EU 1996 11 27 VTZA97046 1 19961031 A 3231 A103GS NUT BAG JETSTM JETSTM3201 1500217 EU LT MLG DOOR LOOSE A VTZA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 27 483UE 898 FLT 6152 - BGM-IAD - DURING CLIMB-OUT, EXPERIENCED A SLIGHT VIBRATION. AIRCRAFT RETURNED TO BGM WHERE MAINTENANCE INSPE CTED THE NOSE GEAR DOORS AND FOUND THE ATTACHING HARDWARE FOR THE LEFT GEAR RETRACTION ARM LOOSE. MAINTENANCE TIGHTENED THE ATTACHING HARDWARE AND PERFORMED THE REQUIRED MAINTENANCE CHECKS. AIRCRAFT WAS THEN RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A56EU 1996112700454 19961127 00454 1996 11 27 VTZA97048 4 19961102 A 3425 7004545911 AHRS JETAIR JETSTM JETSTM4101 1500501 EU LEFT FAILED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 303UE 41015 FLT 6470 - EWR-RIC - DURING CRUISE, AN UNSCHEDULED LANDING DUE TO HEADING COMPARATOR LIGHT ILLUMINATED. AIRCRAFT RETURN ED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED LEFT AHRS, OPS CHECK OK. AIRCRAFT WAS RELEASED A ND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996112700455 19961127 00455 EU 1996 11 27 SIMA963051 1 19961031 A 3350 3011151 BATTERY AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 209AT 3633 0209 SGF - EMERGENCY FLOOR LIGHTS 2, 4, 6, AND LOWER FORWARD SIGNS INOP. RAI'D EMERGENCY FLOOR LIGHT BATTERY FOR 2, 4, 6, AN D LOWER FORWARD EMERGENCY SIGNS. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996112700456 19961127 00456 WP 1996 11 27 ORJA9683 1 19961030 A 3246 26088911 WHEEL DOUG DC9 DC983 3022083 WP LT MLG BROKEN A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 834RA 4750 53124 NR 1 MAIN MOUNT HAS BROKEN THROUGH BOLT, DISCOVERED DURING WALK AROUND IN SEATTLE. LOANER TIRE OBTAINED FROM AMERICAN A IRLINES. REMOVED AND REPLACED NR 1 MAIN WHEEL/TIRE ASSEMBLY PER MM. (M) 2 L 7 2 4F RT A6WE 1996112700457 19961127 00457 WP 1996 11 27 ORJA9681 1 19960928 A 5347 SR095301157001 TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 842RA 49604 FOUND TRACK X-22 AND X-44 FROM STATION 200-237 HAS LEVEL 2 CORROSION. REPAIRED SEAT TRACKS IAW SRM 53-05, FIGURE 4. TR EATED AND PRIMED IAW SRM 51-10-3. INSTALLED TRACK IAW SRM 51-30-2 AND 51-30-5. (M) 2 L 7 2 4F A6WE 1996112700458 19961127 00458 WP 1996 11 27 ORJA9680 1 19960927 A 5320 FASTENERS DOUG DC9 DC982 3022082 WP CABIN CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 842RA 49604 CABIN WINDOW RIGHT NR 29 HAS CORROSION ON FORWARD CENTER NUT PLATE AND FORWARD UPPER NUTS UNDER LONGERON 11. REPLACED C ORRODED FASTENERS AS NECESSARY. ALL WORK DONE IAW SRM 51-10-3 AND SRM 51-30-2. TREATED AND PRIMED IAW SRM 51-10-3. (M ) 2 L 7 2 4F A6WE 1996112700459 19961127 00459 WP 1996 11 27 ORJA9679 1 19961003 A 5321 FLOOR DOUG DC9 DC982 3022082 WP CARGO PIT CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 842RA 49604 FLOOR PANEL IN AFT CARGO PIT HAS EXFOLIATION CORROSION. FABRICATED NEW FLOOR PANEL, DRILLED, TREATED, AND PRIMED IAW SR M 51-10-2, 51-10-3, 51-10-4. (M) 2 L 7 2 4F A6WE 1996112700460 19961127 00460 WP 1996 11 27 ORJA9676 1 19960927 A 5347 TRACK DOUG DC9 DC982 3022082 WP CARGO PIT CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 842RA 49604 AFT CARGO COMPARTMENT X16L TIE DOWN TRACK HAS CORROSION AT STATION 946 - 1030 AND STATION 1096. REMOVED AND REPLACED TR ACK SECTIONS IAW SRM 51-30-1 AND TREATED IAW SRM 51-10-3. (M) 2 L 7 2 4F A6WE 1996112700461 19961127 00461 WP 1996 11 27 ORJA9675 1 19960920 A 5347 TRACK DOUG DC9 DC982 3022082 WP CARGO PIT CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 842RA 49604 MID CARGO PIT HAS LEVEL 2 CORROSION AT STATION 693 - 787 ON RIGHT TIE-DOWN TRACK. REMOVED AND REPLACED TRACK IAW SRM 51 -10-4 AND 51-30-1. (M) 2 L 7 2 4F A6WE 1996112700462 19961127 00462 WP 1996 11 27 ORJA9674 1 19960927 A 5347 TRACK DOUG DC9 DC982 3022082 WP CARGO PIT CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 842RA 49604 FORWARD PIT STATION 370-522 LEFT TIE-DOWN TRACK HAS LEVEL 2 SURFACE CORROSION. REMOVED AND REPLACED DAMAGED TRACK SECTI ON IAW SRM 51-10-4 AND 51-30-1 AND 51-30-2. (M) 2 L 7 2 4F A6WE 1996112700463 19961127 00463 WP 1996 11 27 GRAA9673 1 19961019 A 3350 0816300609 COVER DOUG DC9 DC987 3022087 WP CABIN LOOSE A GRAA K NONE O OTHER IN INSP/MAINT 1 WP 11 750RA 49777 LINE MAINTENANCE AT IFP, FOUND THE FORWARD EMERGENCY TRACK LIGHT COVER LOOSE. MAINTENANCE RESECURED THE FORWARD EMERGEN CY TRACK LIGHT COVER. OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM WAS PERFORMED. NO DEFECTS NOTED. THE AIRCRAFT W AS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A6WE 1996112700464 19961127 00464 WP 1996 11 27 ORJA9672 1 19961029 A 3350 GROUND DOUG DC9 DC987 3022087 WP CABIN LOOSE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 752RA 49780 MID CABIN EMERGENCY CEILING LIGHT INOP. RELAMPED, NO HELP. FOUND LOOSE GROUND STUD AT 5225. TIGHTENED STUD. OPS NORM AL. (M) 2 L 7 2 4F RT A6WE 1996112700465 19961127 00465 NM 1996 11 27 AALA961469 1 19961004 A 5321 141N516154 FLOOR BOEING 757 757223 1384957 NM BS 405 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 659AA 24617 AFW - FOUND FLOOR AT STATION 405, RBL 59, HAD CORROSION BLENDED BEYOND SRM LIMITS. REPAIRED PER MRB 757-960. (M) 2 L 7 2 4F RT A2NM 1996112700466 19961127 00466 NM 1996 11 27 AALA961470 1 19961004 A 5320 141N832258 ANGLE BOEING 757 757223 1384957 NM BS 374 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 659AA 24617 AFW - FOUND FLOOR STRUCTURE ANGLE AT L-1 DOOR STATION 374 LBL 63 HAD CORROSION BLENDED BEYOND SRM LIMITS. REPAIRED PER MRB 757-961. (M) 2 L 7 2 4F RT A2NM 1996112700467 19961127 00467 NM 1996 11 27 AALA961471 1 19961004 A 5315 141N5113 FLOOR BEAM BOEING 757 757223 1384957 NM BS 377 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 659AA 24617 AFW - FOUND FLOOR BEAM AT STATION 377 LBL 48 HAD CORROSION REMOVED BEYOND SRM LIMITS. REPAIRED PER MRB 757-962. (M) 2 L 7 2 4F RT A2NM 1996112700468 19961127 00468 NM 1996 11 27 AALA961472 1 19961004 A 5311 143N1018 FRAME BOEING 757 757223 1384957 NM BS 780 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 659AA 24617 AFW - FOUND FRAME AT STATION 780 NEAR STRINGER 24L HAD A SMALL CRACK INBOARD FLANGE. REPAIRED PER MRB 757-963. (M) 2 L 7 2 4F RT A2NM 1996112700469 19961127 00469 NM 1996 11 27 AALA961473 1 19961004 A 5311 146N1008 FRAME BOEING 757 757223 1384957 NM BS 1340 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 659AA 24617 AFW - FOUND FRAME AT STATION 1340 BETWEEN STRINGER 25L AND STRINGER 26L HAD SMALL GOUGE BLENDED BEYOND SRM LIMITS. REPA IRED PER MRB 757-964. (M) 2 L 7 2 4F RT A2NM 1996112700470 19961127 00470 NM 1996 11 27 USAA960724 1 19960829 A 5330 SKIN BOEING 757 75723APF 1384966 NM STA 345 DENT A CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 572CA 24601 24868 CLT - INSPECTION VISUALLY FOUND A 1 INCH DENT IN SKIN LOCATED AT FRAME STATION 345 LEFT ZONE 838. REMOVED DAMAGE AND IN STALLED REPAIR ANGLE AND FILLER AS PER SRM 53-00-07. (M) 2 L 7 2 4F RT A2NM 1996112700471 19961127 00471 NM 1996 11 27 USAA960723 1 19960829 A 5330 SKIN BOEING 757 75723APF 1384966 NM STA 1480 DENT A CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 572CA 24601 24868 CLT INSPECTION VISUALLY FOUND A 1 INCH DENT IN SKIN LOCATED AT STATION 1480, ABOVE STRINGER 26L. DAMAGE CUTOUT AND INST ALLED REPAIR ANGLE AND FILLER AS PER SRM 51-70-11. (M) 2 L 7 2 4F RT A2NM 1996112700472 19961127 00472 NM 1996 11 27 USAA960722 1 19960829 A 5330 SKIN BOEING 757 75723APF 1384966 NM BS 1520 DENT A CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 572CA 24601 24868 CLT - INSPECTION VISUALLY FOUND A 1 INCH DENT IN SKIN LOCATED AT STATION 1520 ABOVE STRINGER 26R. DAMAGED REMOVED AND I NSTALLED REPAIR ANGLE AND FILLER AS PER SRM 51-70-11. (M) 2 L 7 2 4F RT A2NM 1996112700473 19961127 00473 WP 1996 11 27 HAL960073 1 19960930 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1921 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 148AA 72741 46703 FLOOR SUPPORT LOCATED IN FRONT OF LAV NR 6 IS CORRODED. REMOVED FLOOR SUPPORT AND INSTALLED NEW FLOOR SUPPORT PER AARD 51-01-00-05, PAGE 1 AND 2. (M) 2 L 7 3 4F A22WE 1996112700474 19961127 00474 WP 1996 11 27 HAL960072 1 19960930 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1900 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 148AA 72741 46703 FLOOR SUPPORT FORWARD OF COFFEE BAR CORRODED. REMOVED AND INSTALLED NEW FLOOR SUPPORT PER AARD 51-01-00-05, PAGE 1 AND 2. (M) 2 L 7 3 4F A22WE 1996112700475 19961127 00475 WP 1996 11 27 HAL960071 1 19960930 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1900 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 148AA 72741 46703 INBOARD FLOOR SUPPORT FOR COFFEE BAR CORRODED. REMOVED FLOOR SUPPORT AND INSTALLED NEW FLOOR SUPPORT PER AARD 51-10-00- 05, PAGE 1 AND 2. (M) 2 L 7 3 4F A22WE 1996112700476 19961127 00476 WP 1996 11 27 HAL960095 1 19961031 A 5720 AVB09831 DOUBLER DOUG DC10 DC1010 3022110 WP WS 264 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 116AA 75042 46516 UNDERSIDE OF LEFT WING JUST OUTBOARD OF MLG STRUT DOOR TAPER LOCK FASTENER HEAD CORRODED. INSTALLED DOUBLER (ESO 7349) CORROSION PROTECT THE RE-WORKED AREA PER SRM VOL 2 CHAPTER 51-21-01. (M) 2 L 7 3 4F A22WE 1996112700477 19961127 00477 WP 1996 11 27 HAL960092 1 19961028 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 999 CORROSION A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 116AA 75042 46516 CORROSION ON BELT FRAME STATION 999 AFT SIDE BETWEEN LONGERONS 49R AND 48L. REMOVED CORRODED SECTION OF LOWER FRAME 'J' ANGLE AND INSTALLED SPLICE REPAIR PER SRM 51-22-00 AND 53-30-00. (M) 2 L 7 3 4F A22WE 1996112700478 19961127 00478 WP 1996 11 27 HAL960099 1 19961105 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 1278 CORROSION A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 116AA 75043 46516 CORROSION AND CRACKS ON FRAME AT STATION 1278 BETWEEN LONGERONS 52L AND 52R. REMOVED CORROSION PER SRM 51-21-01 AND INS TALLED DOUBLER PER SRM 51-00-01 PAGE 124D. (M) 2 L 7 3 4F A22WE 1996112700479 19961127 00479 WP 1996 11 27 HAL96058 1 19960909 A 5315 ACA0031507 FLOOR BEAM DOUG DC10 DC1010 3022110 WP BS 1501 CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 153AA 68464 46708 DURING CHECK, FOUND 3 CRACKS IN AFT FLOOR BEAM LOWER CAP STATION Y 1501, AT STATION X EACH CRACK IS APPROX 1 INCH LONG. INSTALLED FABRICATED DOUBLERS IAW ESO 7349 DATED 9-6-96. (M) 2 L 7 3 4F A22WE 1996112700480 19961127 00480 WP 1996 11 27 HAL960059 1 19960909 A 5720 ANGLE DOUG DC10 DC1010 3022110 WP RT WS 164 CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 153AA 46708 FOUND CORROSION AND METAL SPLIT AT TOP OF VERTICAL SUPPORT ON FALSE REAR SPAR 3 FEET FROM WHEEL WELL ON THE RIGHT TRAILI NG EDGE. REMOVED CORROSION AND INSTALLED REPAIR ANGLE PER ESO 7349 DATED 9-4-96. (M) 2 L 7 3 4F A22WE 1996112700481 19961127 00481 WP 1996 11 27 HAL960056 1 19960903 A 5347 S492925215200 CARGO TRACK DOUG DC10 DC1010 3022110 WP BS 1020 CORROSION A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 153AA 68464 46708 DURING CHECK, FOUND CORROSION ON CENTER ROLLER TRACK AT STATION 979 TO STATION 1099. FABRICATED NEW ROLLER TRACK AND IN STALLED PER SRM 51-10-00-1. (M) 2 L 7 3 4F A22WE 1996112700482 19961127 00482 WP 1996 11 27 HAL960055 1 19960903 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 959 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 153AA 68464 46708 DURING CHECK, FOUND CORROSION ON BOTTOM OF FLOOR BEAM VERTICAL SUPPORT 19 INCHES RIGHT OF CENTER LINE AT FRAME ATTACH PO INT. REPLACED VERTICAL SUPPORT AS PER SRM 51-01-00-05. (M) 2 L 7 3 4F A22WE 1996112700483 19961127 00483 EA 1996 11 27 96ZZZM1537 2 19961112 A 7200 ENGINE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA RIGHT FLUCTUATING A GUUA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 196GA 12735 UB31 PCE32582 FLT 401 - EYW-TPA - DURING CLIMB-OUT, RIGHT TORQUE FLUCTUATING SHUT DOWN ENGINE. DECLARED AN EMERGENCY AND RETURNED TO EWY AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RIGHT ENGINE. (M) 2 L 7 2 4T 4 T RT A24CE E4EA 1996112700484 19961127 00484 WP 1996 11 27 96ZZZM1538 1 19960712 A 2752 BRACKET DOUG DC8 DC861 3021952 WP RT TE FLAP BROKEN A A FXLA O OTHER F FLT CONT AFFECTED CL CLIMB 1 SO 19 27UA 45942 DURING FLIGHT FROM SJO, SPLIT FLAPS INDICATED BY 10 DEGREES AND FELT IN CONTROLS. UPON ARRIVAL AT MIAMI INSPECTED AND C HECKED FLAP SYSTEM AND FOUND RIGHT INBOARD FLAP ACTUATOR SWIVEL BRACKET BROKEN. REMOVED AND REPLACED INBOARD FLAP ACTUA TOR ASSEMBLY P/N 27800853, IAW MM 27-51-9 AND BLED SYSTEM IAW MM 27-51-12. SYSTEM CHECKED NORMAL. ALSO, PERFORMED TEST FLIGHT ON AIRCRAFT. SYSTEM CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 4 4F 4A25 1996112700485 19961127 00485 WP 1996 11 27 96ZZZM1539 1 19961030 A 5312 BULKHEAD TEE DOUG DC8 DC861 3021952 WP BS 1766 CRACKED A FXLA O OTHER O OTHER IN INSP/MAINT 1 SO 19 30UA 45888 DURING INSPECTION OF AFT PRESSURE BULKHEAD AT STATION Y=1766 IAW PSI 53.08.009/010C AND NDI 53-10-18, FOUND TWO CRACKS A T CORNER RADIUS OF THE TEE CAP AT LONGERON 10 RIGHT AND LONGERON 10 LEFT. REPAIRED CRACKS BY INSTALLING A REPAIR ANGLE IAW SRM 53-2-5 PAGE 15 AND 16. (M) 2 L 7 4 4F 4A25 1996112700486 19961127 00486 WP 1996 11 27 96ZZZM1540 1 19961008 A 3210 5719124508 BOGIE BEAM DOUG DC8 DC8F55 3021928 WP RT MLG CRACKED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 55FB 15349 45678 DURING C-CHECK INSPECTION, FOUND RIGHT MAIN GEAR FORWARD BOGIE BEAM CRACKED LEFT LUG. REMOVED AND REPLACED RIGHT MAIN G EAR FORWARD BOGIE BEAM P/N ON 5719124-508 S/N ON 325-046, WO 2951 NR 0-0116, OH BY ARR WO 295153 P/N OFF 5719124-508. ( M) 2 L 7 4 4F 4A25 1996112700487 19961127 00487 WP 1996 11 27 ASAA9680248 1 19961106 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 940AS 22816 49825 PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996112700488 19961127 00488 NM 1996 11 27 ASAA9640094 1 19961102 A 3350 8821004 BATTERY PACKS BOEING 737 7374Q8 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 764AS 25101 SEA - DURING MAINTENANCE CEHCK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 11, 14, 15 AN D 18. REPLACED BATTERY PACKS AT ROWS 11,14, AND 18 AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996112700489 19961127 00489 NM 1996 11 27 ASAA9610139 1 19961103 A 3350 86210144 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, THE R1 DOOR EMERGENCY EXIT IDENTIFIER WAS FOUND TO BE INOPERATIVE. REPLACED BATTERY PAC K AND SIGN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996112700490 19961127 00490 NM 1996 11 27 BJNA961102 1 19961119 A 5730 SKIN BOEING 737 737214 138446R NM WS 425 CRACKED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 457TM 52149 20156 RIGHT WING NR 4 SLAT AUXILLARY TRACK CUTOUT HAS .5 INCH LONG CRACK CENTER OF CUTOUT WSL 425. MECHANICALLY BLENDED CRACK EC VERIFIED NO FURTHER CRACKS. AFTER EVALUATION DETERMINED NOT TO BE ON SDR. (M) 2 L 7 2 4F A16WE 1996112700491 19961127 00491 NM 1996 11 27 BJNA961104 1 19961119 A 5730 1A14173 SKIN BOEING 737 737214 138446R NM RT WING CRACKED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 457TM 52149 20156 RIGHT WIND NR 4 SLAT INBOARD AUXILLARY TRACK CUT OUT, SKIN HAS .5 INCH LONG CRACK WBL 254. CUT OUT CRACKED FABRICATED A ND INSTALLED FILLER AND DOUBLER IAW B737 SRM 57-30-4 AND 57-50-1 FIG 2. (M) 2 L 7 2 4F A16WE 1996112700492 19961127 00492 WP 1996 11 27 ORJA9686 1 19961029 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP BS 480 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 833RA 53045 SEAT TRACK 54 RIGHT AT STATION 480 CORRODED OUT OF LIMITS. REPLACED AFFECTED SECTION IAW SRM 53-05, FIGURE 4-F. REFERE NCE AAR N/R 2000-0016. (M) 2 L 7 2 4F RT A6WE 1996112700493 19961127 00493 WP 1996 11 27 ORJA9687 1 19961103 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP BS 560 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 833RA 53045 SEAT TRACK 54 LEFT CORRODED OUT OF LIMITS AT FUSELAGE STATION 560. REPLACED AFFECTED SECTION OF TRACK IAW SRM 53-05, FI GURE 4-F. REFERENCE AAR N/R 2000-0016. (M) 2 L 7 2 4F RT A6WE 1996112700494 19961127 00494 WP 1996 11 27 ORJA9688 1 19961103 A 5347 TRACK DOUG DC9 DC983 3022083 WP BS 1041 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 833RA 53045 SEAT TRACK 54 RIGHT AT FUSELAGE STATION 1041 CORRODED OUT OF LIMITS. REPLACED AFFECTED SECTION IAW STR 53-05, FIGURE 4- F. REFERENCE AAR N/R 2000-0016. (M) 2 L 7 2 4F RT A6WE 1996112700495 19961127 00495 WP 1996 11 27 ORJA9689 1 19961103 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP BS 446 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 833RA 53045 SEAT TRACK 54.5 RIGHT AT FUSELAGE STATION 446 CORRODED OUT OF LIMITS. REPLACED AFFECTED SECTION OF TRACK IAW SRM 53-05, FIGURE 4-F. REFERENCE AAR 2000-0016. (M) 2 L 7 2 4F RT A6WE 1996112700496 19961127 00496 WP 1996 11 27 ORJA9690 1 19961103 A 5320 STRAP DOUG DC9 DC983 3022083 WP FORWARD ENTRY CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 833RA 53045 STRAP CORRODED IN FORWARD ENTRYWAY, THRESHOLD AREA. REMOVED OLD SHIM, FABRICATED AND INSTALLED NEW SHIM IAW SRM 51-10-2 , 51-10-3, 51-10-4, 51-30-1, AND MM 20-20-02 AND MM 20-20-03. REFERENCE AAR N/R 2000-0018. (M) 2 L 7 2 4F RT A6WE 1996112700497 19961127 00497 WP 1996 11 27 ORJA9691 1 19961030 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP BS 750. CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 833RA 53045 SEAT RACK X-54 RIGHT AT STATION 750 OUT OF LIMITS IAW SRM 53-04. REMOVED DAMAGED SEAT TRACK AND SPLICED IN NEW SECTION IAW SRM 53-05. REFERENCE AAR N/R 2000-0016. (M) 2 L 7 2 4F RT A6WE 1996112700498 19961127 00498 WP 1996 11 27 ORJA9692 1 19961029 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP CABIN CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 833RA 53045 SEAT TRACK X-54 AT STATION 496 INBOARD FLANGE OUT OF LIMITS IAW SRM 53-05, PAGE 8R. REMOVED DAMAGED TRACK AND REPLACED WITH NEW TRACK IAW SRM 53-05. REFERENCE AAR N/N 2000-0016. (M) 2 L 7 2 4F RT A6WE 1996112700499 19961127 00499 WP 1996 11 27 ORJA9693 1 19961028 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP BS 1136 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 833RA 53045 STUB TRACK CORRODED X-35 STATION 1136 LEFT. REPLACED STUB TRACK IAW 51-00 AND 51-10-3. REFERENCE AAR N/R 2000-0016. ( M) 2 L 7 2 4F RT A6WE 1996112700500 19961127 00500 WP 1996 11 27 ORJA9694 1 19961103 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP CABIN CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 833RA 53045 CABIN SEAT TRACK INBOARD LIP CORRODED BEYOND LIMITS, SEAT TRACK 22 RIGHT AT FUSELAGE STATION 1231. REPLACED AFFECTED SE CTION OF TRACK IAW SRM 53-05, FIGURE 4-F. REFERENCE AAR N/R 2000-0016. (M) 2 L 7 2 4F RT A6WE 1996112700501 19961127 00501 WP 1996 11 27 ORJA9695 1 19961103 A 5321 FLOOR BOARD DOUG DC9 DC983 3022083 WP FORWARD LAV CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 833RA 53045 FORWARD LAV FLOOR BOARD INBOARD EDGE CORRODED. CUT OUT DAMAGED AREA AND REPLACED HONEYCOMB IAW SRM 51-90-0, 51-70-2, 51 -70-1. REFERENCE AAR N/R 2000-0055. (M) 2 L 7 2 4F RT A6WE 1996112700502 19961127 00502 WP 1996 11 27 ORJA9698 1 19961105 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 873RA 53093 OVER THE WING LIGHT ON EMERGENCY LIGHTS SYSTEM OUT. REMOVED AND REPLACED POWER SUPPLY SYSTEM. OPS GOOD. (M) 2 L 7 2 4F RT A6WE 1996112700503 19961127 00503 WP 1996 11 27 ORJA9697 1 19961106 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP TAILCONE DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 833RA 53045 TAILCONE EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK IN TAILCONE EMERGENCY LIGHTS. OPS NORMAL. (M) 2 L 7 2 4F RT A6WE 1996112700504 19961127 00504 WP 1996 11 27 ORJA9696 1 19961106 A 3350 41B004AD073 BATTERY EA1D13D3 DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 833RA 53045 EMERGENCY LIGHTS ROWS 1 AND 2 INOP. REMOVED AND REPLACED BATTERY PACKS FOR ROWS 1 AND 2. OPS NORMAL. (M) 2 L 7 2 4F RT A6WE 1996112700505 19961127 00505 WP 1996 11 27 96ZZZM1541 1 19960311 A 5313 A6A7422 LONGERON DOUG DC10 DC1030 3023501 WP BS 1801 CORRODED B ZJ4R K NONE O OTHER IN INSP/MAINT 1 SO 13 228NW 75849 75849 46578 FOUND SEVERE EXFOLIATION ON LONGERON STRAP 36RT NEAR FS 1801 CENTER CARGO COMPARTMENT. REMOVED AND REPLACED 2 ANGLES AN D 1 STRAP ON LONGERON 36RT SPLICE AT FS 1801 CENTER CARGO COMPARTMENT IAW SRM 53-00-01 AND 51-33-01. (M) 2 L 7 3 4F A22WE 1996112700506 19961127 00506 WP 1996 11 27 EIAA9651 1 19961030 A 5320 CHANNEL DOUG DC9 DC932F 3022067 WP BS 90 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 48522 47220 SAT - 'J' CHANNEL CORRODED FS 90 LBL 6 TO LBL 12 NOSE WHEEL WELL. REMOVED, FABRICATED AND INSTALLED 'J' CHANNEL PER SRM 51-00, 51-30-2 AND 51-30-3. (M) 2 L 7 2 4F A6WE 1996112700507 19961127 00507 WP 1996 11 27 EIAA9652 1 19961030 A 5311 FRAME DOUG DC9 DC932F 3022067 WP FRAME 1168 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 48522 47220 SAT - AFT ACCESSORY COMPARTMENT FRAME 1168 WEB AT 1 O'CLOCK IS CRACKED. REMOVED, FABRICATED AND INSTALLED CRACKED WEB A NGLE PER SRM 53-10-4 FIG 4 AND SRM 51-30-0. (M) 2 L 7 2 4F A6WE 1996112700508 19961127 00508 WP 1996 11 27 EIAA9653 1 19961030 A 5312 BULKHEAD WEB DOUG DC9 DC932F 3022067 WP BS 37 GOUGE A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 48522 47220 SAT - FOUND FUSELAGE STATION 37 BULKHEAD WEB GOUGED AT STRINGER 18R. REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 1 AND FIG 2. (M) 2 L 7 2 4F A6WE 1996112700509 19961127 00509 WP 1996 11 27 EIAA9654 1 19961030 A 5312 BULKHEAD DOUG DC9 DC932F 3022067 WP BS 37 GOUGE A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 48522 47220 SAT - FOUND FUSELAGE STATION 37 BULKHEAD WEB GOUGED AT STRINGER 18L. REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 4 ITEM 4. (M) 2 L 7 2 4F A6WE 1996112700510 19961127 00510 WP 1996 11 27 EIAA9655 1 19961030 A 5320 WEB DOUG DC9 DC932F 3022067 WP BS 737 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 48522 47220 SAT - FOUND RIGHT MAIN LANDING GEAR WHEEL WELL FS 737 RBL 52 AT STRINGER 18R WEB IS CRACKED. FABRICATED AND INSTALLED D OUBLER REPAIR PER SRM 53-01 FIG 4 AND SRM 51-30-2. (M) 2 L 7 2 4F A6WE 1996112700511 19961127 00511 WP 1996 11 27 EIAA9656 1 19961030 A 5320 591036749 CHANNEL DOUG DC9 DC932F 3022067 WP ACCESSORY COMP CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 48522 47220 SAT - AFT ACCESSORY COMPARTMENT PLUG DOOR LOWER SEALING CHANNEL FRAME IS CRACKED. REMOVED AND INSTALLED NEW SEAL CHANNE L FRAME IAW SRM 51-00 AND SRM 51-30-2. (M) 2 L 7 2 4F A6WE 1996112700512 19961127 00512 WP 1996 11 27 EIAA9657 1 19961030 A 5313 LONGERON DOUG DC9 DC932F 3022067 WP BS 963 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 48522 47220 SAT - LONGERON 28R HAS EXFOLIATION CORROSION AT STATION 963 BEYOND LIMITS. REMOVED LONGERON 28R FROM FS 945-996 IAW SRM 53-11-3 FIG 4 AND 51-10-1 FABRICATED LONGERON AND INSTALLED IAW SRM 53-11-3 FIG 4 AND 51-10-1 FIG 15. (M) 2 L 7 2 4F A6WE 1996112700513 19961127 00513 WP 1996 11 27 EIAA9658 1 19961030 A 7830 DOUBLER DOUG DC9 DC932F 3022067 WP LEFT ENGINE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 48522 47220 SAT - FOUND LEFT ENGINE UPPER THRUST REVERSER BUCKET DOUBLER CRACKED AT OUTBOARD FORWARD END. CUT OUT DAMAGED AREA PER OHM 78-30-1 FIG 404. FABRICATED REPAIR DOUBLER PER SRM 54-01 AND INSTALLED PER SRM 51-00 AND 51-30-2. (M) 2 L 7 2 4F A6WE 1996112700543 19961127 00543 CE 1996 11 27 96ZZZX5736 1 19961101 A 5610 55112856 WINDOW CESSNA 500 550 2076604 CE COCKPIT RT SIDE CRACKED A S ISYA K NONE O OTHER IN INSP/MAINT 1 GL 25 84EA 6107 5500484 DURING PRISM INSPECTION OF CO-PILOT'S WINDOW, FOUND 4 FASTENER HOLES CRACKED AT UPPER FORWARD. CRACK CONNECTS CENTER 2 FASTENERS. WINDOW IS TO BE REPLACED. 1 L 7 2 4F A22CE 1996112700554 19961127 00554 NM 1996 11 27 AWXA9600708 1 19961123 A 3397 WIRE BOEING 737 73733A 1384673 NM CABIN FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 164AW 23625 DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT AT 6C INOPERATIVE. REPAIRED WIRING AT SEAT 6C EMERGENCY LIGH, O PERATIONS CHECK GOOD. 2 L 7 2 4F RT A16WE 1996112700555 19961127 00555 EU 1996 11 27 AWXA9600709 1 19961121 A 3260 SENSOR AIRBUS 320 A320231 3930325 EU LT MLG DOOR OUT OF ADJUST A AWXA O OTHER E VIBRATION/BUFFET CL CLIMB 1 WP 28 636AW 098 LANDING GEAR NEEDED TO BE RECYCLED AFTER TAKEOFF TO GET IT UP AND LOCKED. COULD FEEL VIBRATION INDICATING THAT IT WAS N OT UP AND LOCKED UNTIL RECYCLED. FOUND LT MLG DOOR PROXIMITY SENSOR TO BE OUT ADJUSTMENT. ADJUSTED SENSOR PER MM 32-31 -73 PG 608 ITEM 5. SWUNG LANDING GEAR SEVERAL TIMES WITH NO DEFECTS NOTED. 2 L 7 2 4F RT A28NM 1996112700556 19961127 00556 EU 1996 11 27 AWXA9600710 1 19961123 A 2910 FLUID AIRBUS 320 A320231 3930325 EU GREEN HYD SYSTEM DEPLETED A AWXA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 WP 28 621AW 053 ON APPROACH, GREEN SYSTEM LOW HYDRAULIC QUANTITY DISPLAYED. CREW FOLLOWED ECAM PROCEDURES AND SHUT DOWN PUMP. GEAR WAS STILL UP WHEN WARNING OCCURRED, EMERGENCY DECLARED. GREEN HYDRAULIC SYSTEM SERVICED WITH 2 GALLONS, RESET GEAR FROM MA NUAL EXTENSION. 2 L 7 2 4F RT A28NM 1996112700557 19961127 00557 NM 1996 11 27 AWXA9600711 1 19961124 A 3350 LIGHT BOEING 737 737277 1384570 NM CABIN LOOSE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 188AW 22655 DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 4 EMERGENCY LIGHT INOPERATIVE. RESECURED ROW 4 EMERGENCY EXIT LIGHT, OPERAT IONS CHECK GOOD. 2 L 7 2 4F RT A16WE 1996112700558 19961127 00558 NM 1996 11 27 AWXA9600712 1 19961125 A 3397 WIRE BOEING 737 73733A 1384673 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 168AW 23629 DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 2 EMERGENCY LIGHT INOPERATIVE. SPLICED BROKEN WIRES, OPERATIONS CHECK GOOD. 2 L 7 2 4F RT A16WE 1996112700559 19961127 00559 NM 1996 11 27 AWXA9600713 1 19961124 A 3397 WIRE BOEING 737 7373G7 1384595 NM CABIN SHORTED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 303AW 24010 DURING ROUTINE MAINTENANCE CHECK, FOUND ROWS 19 TO 22 EMERGENCY TRACK LIGHTS OUT. WIRE HARNESS SHORTED OUT AT SEAT ROW 20. REPAIRED HARNESS, OPERATIONS CHECK GOOD. 2 L 7 2 4F RT A16WE 1996112700560 19961127 00560 NM 1996 11 27 AWXA9600714 1 19961125 A 3350 1060091101 LIGHT BOEING 737 737277 1384570 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 185AW 22652 DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT MOUNTED EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 18. REPLACED LIGHT ASSEMBL Y. 2 L 7 2 4F RT A16WE 1996112700561 19961127 00561 SO 1996 11 27 RAAA96E9015 1 19961125 A 3350 8621014 BATTERY PACK INTVLV 873100112 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 1471 188C2007 RT FWD OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. REPLACED BATTERY PACK AND LIGHT ASSEMBLY. 2 L 7 4 4T 4A22 1996112700562 19961127 00562 WP 1996 11 27 CALA9601706 1 19961115 A 5730 SKIN DOUG DC9 DC982 3022082 WP RT WING LE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10801 49127 INSPECTION FOUND A 3.5 INCH CRACK IN RT WING LOWER LEADING EDGE SKIN JUST OUTBOARD OF NR 7 SLAT TRACK. THE SKIN WAS REP AIRED IAW ECRA 5730-01468. 2 L 7 2 4F A6WE 1996112700563 19961127 00563 NM 1996 11 27 CALA9601707 1 19961115 A 5230 SKIN BOEING 737 737130 1384435 NM C 1 CARGO DR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14212 19029 INSPECTION FOUND LOWER 6 SECTION OF C-1 CARGO DOOR SKIN DENTED, SCRATCHED AND GOUGED AT STA 178. THE DAMAGED SKIN WAS R EMOVED AND REPLACED WITH NEW SKIN IAW SRM 52-30-2 AND 51-30-2. 2 L 7 2 4F A16WE 1996112700564 19961127 00564 WP 1996 11 27 CALA9601708 1 19961115 A 5720 ANGLE DOUG DC9 DC982 3022082 WP NR 2 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10801 49127 INSPECTION FOUND A 1.25 INCH CRACK IN LT WING LEADING EDGE RIB LOWER ATTACH ANGLE JUST OUTBOARD OF NR 2 SLAT TRACK. A N EW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 1996112700565 19961127 00565 WP 1996 11 27 CALA9601709 1 19961120 A 5522 SKIN DOUG DC10 DC1030 3023501 WP RT ELEVATOR TORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND INBOARD AFT CORNER OF RT OUTBOARD ELEVATOR SKIN TORN WITH SKIN PULLING THROUGH FASTENERS. A CLASS-B RE PAIR WAS INSTALLED IAW SRM 55-22-00, PAGE 4. A DIP WAS ISSUED TO REINSPECT THE AREA AT EACH B-CHECK AND INSTALL A-CLASS 1 REPAIR WITHIN 12,000 HOURS. 2 L 7 3 4F A22WE 1996112700566 19961127 00566 WP 1996 11 27 CALA9601710 1 19961114 A 5350 CLIPS DOUG DC9 DC982 3022082 WP TAILCONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10801 49127 THE TAILCONE INTERIOR AND EXTERIOR RELEASE HANDLE PULL FROM CLIPS WAS LESS THAN 25 POUNDS AND LESS THAN 10 POUNDS, RESPE CTIVELY. THE HANDLE RETAINER CLIPS WERE ADJUSTED IAW MM 53-53-00. 2 L 7 2 4F A6WE 1996112700567 19961127 00567 WP 1996 11 27 CALA9601711 1 19961114 A 5350 CABLES DOUG DC9 DC982 3022082 WP TAILCONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10801 49127 THE TAILCONE RELEASE HANDLE PULL WAS HIGH AT BOTH THE INTERIOR AND EXTERIOR HANDLES AND THE TAILCONE FAILED TO DROP FROM AIRCRAFT. THE TAILCONE RELEASE SYSTEM CABLES WERE ADJUSTED IAW MM 53-53-00, PAGE 501. 2 L 7 2 4F A6WE 1996112700568 19961127 00568 EU 1996 11 27 9625173210 1 19961124 A 2720 FEEL SOLENOID AIRBUS 320 A320211 3930320 EU RUDDER FAILED A NWAA K NONE F FLT CONT AFFECTED AP APPROACH 1 GL 01 310NW 121 DURING FINAL APPROACH IN LIGHT ICING CONDITIONS, THE RUDDER PEDALS WERE RESTRICTED IN THE NEUTRAL POSITION. WING AND EN GINE ANTI-ICE WERE OPERATING AT THE TIME. AUTO PILOT WAS NOT ENGAGED. AIRCRAFT LANDED WITHOUT INCIDENT. RUDDER MOVEME NT RETURNED TO NORMAL DURING TAXI. MAINTENANCE REPLACED THE RUDDER ARTIFICIAL FEEL SOLENOID, OPS CHECKED OK. 2 L 7 2 4F RT A28NM 1996112700569 19961127 00569 WP 1996 11 27 9625189930 1 19961125 A 7711 LG80A2 EPR TRANSMITTER DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9A 52048 NE RT ENGINE FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 89S 29699 481 47042 657284 AS POWER WAS APPLIED FOR TAKEOFF THE RIGHT ENGINE EPR INDICATION WAS INOPERATIVE. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE REPLACED THE RIGHT ENGINE EPR TRANSMITTER, OPERATIONAL CHECK WAS OK. 2 L 7 2 4F 4 F A6WE E2EA 1996112700570 19961127 00570 WP 1996 11 27 9625199995 1 19961124 A 4900 GTCP8598DCA APU DOUG DC9 DC931 3022065 WP MLG WW MALFUNCTIONED A NWAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 01 8978E 56236 3175 47327 DURING TAXI OUT, SMOKE WAS NOTICED IN AFT CABIN AREA. SHORTLY THEREAFTER, APU AUTO SHUTDOWN. AC WAS TOWED BACK TO THE GATE. SOURCE OF SMOKE WAS ISOLATED TO THE APU. APU REMOVED AND REPLACED, AC RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996112700572 19961127 00572 WP 1996 11 27 9625219956 1 19961123 A 3350 60030451 BATTERY PACK DOUG DC9 DC931 3022065 WP COCKPIT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 923RW 47183 DURING PREFLIGHT CHECK, FOUND COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996112700573 19961127 00573 WP 1996 11 27 9625229967 1 19961122 A 3350 6011779 BATTERY PACK DOUG DC9 DC931 3022065 WP LT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9331 47263 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996112700574 19961127 00574 WP 1996 11 27 9625239957 1 19961123 A 3350 6011779 BATTERY PACK DOUG DC9 DC931 3022065 WP LT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 915RW 47139 DURING PERIODIC CHECK, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996112700575 19961127 00575 NM 1996 11 27 9625242708 1 19961122 A 7711 EPR INDICATION BOEING 727 727225 1384077 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE LOW A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 817EA 22554 695251 AS POWER WAS APPLIED FOR TAKEOFF, NUMBER THREE ENGINE EPR INDICATION WAS LOW. CREW ABORTED TAKEOFF AND RETURNED TO GATE . MAINTENANCE TRIMMED NUMBER THREE ENGINE AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 1996112700576 19961127 00576 EU 1996 11 27 9625253241 1 19961123 A 3350 321430 BATTERY AIRBUS 320 A320212 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 341NW 380 DURING LINE MAINTENANCE CHECK, THE EMERGENCY LIGHTS TEST FAULTED AFT LEFT UNIT. REPLACED BATTERY PACK, OPS CHECK OK. 2 L 7 2 4F RT A28NM 1996112700577 19961127 00577 WP 1996 11 27 9625269986 1 19961124 A 3350 60030451 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 986US 47480 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 5 AND 9 INOPERATIVE. REPLACED POWER SU PPLY AND BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996112700578 19961127 00578 NM 1996 11 27 9625272708 1 19961122 A 7711 EPR INDICATION BOEING 727 727225 1384077 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE LOW A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 817EA 22554 700029 AS POWER WAS APPLIED FOR TAKEOFF NUMBER ONE ENGINE EPR INDICATION WAS LOW. CREW ABORTED TAKEOFF AND RETURNED TO GATE. M AINTENANCE TRIMMED NUMBER ONE ENGINE AND A/C WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 1996112700579 19961127 00579 EU 1996 11 27 9625283204 1 19961124 A 5610 NP1653132 WINDOW AIRBUS 320 A320211 3930320 EU FLIGHT DECK SHATTERED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 304US 6346 40 DURING CLIMBOUT AT 16,000 FEET THE FIRST OFFICER'S NR 3 WINDOW OUTER PANE SHATTERED. AIRCRAFT DIVERTED TO MSP AND LANDE D WITHOUT INCIDENT. MAINTENANCE REPLACED WINDOW, OPS CHECK OK. 2 L 7 2 4F RT A28NM 1996112700580 19961127 00580 WP 1996 11 27 9625299150 1 19961121 A 3222 STRUT DOUG DC9 DC914 3022034 WP NLG REQD SERVICE A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 8908E 45749 UPON TAKEOFF, LANDING GEAR WOULD NOT RETRACT. PULLED GROUND CONTROL CIRCUIT BREAKER'S PER COM. FLIGHT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE SERVICED NOSE STRUT AND INSPECTED GEAR CONTROL LEVER, ANTI RETRACTION LATCH AN D GROUND SENSING CONTROL MECHANSIM. GEAR CYCLED SEVERAL TIMES AND OPERATION CHECKS GOOD. 2 L 7 2 4F A6WE 1996112700581 19961127 00581 1996 11 27 9625309885 4 19961121 A 3421 DIRECTIONAL GYRO DOUG DC9 DC951 3022051 WP NR 1 MALFUNCTIONED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 401EA 47682 AFTER TAKEOFF, CAPTAIN'S NR 1 RMI CARD INTERMITTANT AND FIRST OFFICER'S HSI COMPASS FLAG IN VIEW CONSTANTLY. FLIGHT RET URNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE CHANGED NR 1 DIRECTIONAL GYRO, NR 1 RMI AND NR 1 SERVO AND OPERAT ION CHECKS GOOD. 2 L 7 2 4F A6WE 1996112700582 19961127 00582 WP 1996 11 27 9625319753 1 19961123 A 3010 AUGMENTATION VLV DOUG DC9 DC941 302207N WP RIGHT FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 753NW 47117 ON CLIMBOUT WITH AIRFOIL ANTI-ICE ON, THE RIGHT ICE PROTECT TEMPERATURE HIGH WARNING LIGHT ILLUMINATED. PERFORMED COM P ROCEDURE AND LIGHT EXTINGUISHED. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT AU GMENTATION VALVE, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996112700583 19961127 00583 WP 1996 11 27 9625329993 1 19961123 A 2410 696233B CSD DOUG DC9 DC931 3022065 WP LT ENGINE MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 8986E 44216 15903 47402 LEFT CSD OIL PRESSURE LOW LIGHT ILLUMINATED DURING CLIMBOUT. FLIGHT DIVERTED TO DTW AND LANDED WITHOUT INCIDENT. MAINT ENANCE REPLACED CSD, GENERATOR AND CSD COOLER, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996112700584 19961127 00584 SO 1996 11 27 COMA9610335 1 19961121 A 6120 30005000052 SIG COND UNIT EMB 120 EMB120RT SO RIGHT MALFUNCTION A COMA K NONE J WARNING INDICATION CL CLIMB 1 SO 01 266CA 10680 85 120258 AUTOFEATHER WARNING SOUNDED AFTER TAKEOFF. REPLACED THE RT SIGNAL CONDITIONER UNIT. 2 L 7 2 4T RT A31SO 1996112700585 19961127 00585 SO 1996 11 27 COMA9610336 1 19961122 A 3150 PROX SENSOR EMB 120 EMB120RT SO ELEV TRIM MALFUNCTIONED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 462CA 120264 TRIM AURAL WARNING SOUNDED DURING TAKEOFF. REPAIRED WIRING AT ELEVATOR TRIM PROXIMITY SENSOR. 2 L 7 2 4T RT A31SO 1996112700586 19961127 00586 SO 1996 11 27 COMA9610337 1 19961122 A 5280 12012347001 LATCH EMB 120 EMB120RT SO LT MLG DOOR BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 258CA 120247 LT MLG DOOR FOUND HANGING OPEN DURING POST FLIGHT INSPECTION. REPLACED BROKEN GEAR DOOR LATCH ASSY. 2 L 7 2 4T RT A31SO 1996112700587 19961127 00587 EA 1996 11 27 COMA9660211 1 19961125 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA RT TE FLAP SHORTED A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 962CA 1169 7123 FLAPS FAILED AT 12 DEGREES DURING TAXI OPS. REPLACED THE RT FLAP BRAKE AND POSITION SENSOR UNIT. 2 L 7 2 4F RT A21EA 1996112700588 19961127 00588 EA 1996 11 27 COMA9660212 1 19961121 A 3230 16400105 DRAG BRACE CNDAIR CL600 CL6002B19 EA NLG MALFUNCTION A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 912CA 3387 172 7011 NOSE LANDING GEAR DISAGREE MESSAGE ON EICAS NLG DID NOT RETRACT. REPLACED THE NLG DRAG BRACE ASSY. 2 L 7 2 4F RT A21EA 1996112700589 19961127 00589 EA 1996 11 27 COMA9660213 1 19961125 A 3230 16400103 DRAG BRACE CNDAIR CL600 CL6002B19 EA NLG MALFUNCTION A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 915CA 6874 6500 7013 NOSE LANDING GEAR DID NOT RETRACT. DOWN LOCK IS NOT RELEASING. REPLACED THE NLG DRAG BRACE ASSY, RETRACT SYSTEM CHECKS SATISFACTORY. 2 L 7 2 4F RT A21EA 1996112700590 19961127 00590 EA 1996 11 27 COMA9660214 1 19961125 A 5210 DOOR CNDAIR CL600 CL6002B19 EA CABIN FOD A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 960CA 7117 CABIN DOOR WARNING ON DURING FLIGHT. REMOVED 5 CENT FOD 1 US NICKEL FROM DOOR FRAME. DOOR WARNING CHECK SATISFACTORY. 2 L 7 2 4F RT A21EA 1996112700591 19961127 00591 1996 11 27 COMA9660215 4 19961125 A 3442 6229302003 RT UNIT CNDAIR CL600 CL6002B19 EA RADAR COMPT FAILED A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 956CA 1029 329 7105 RADAR FAILED. REPLACED THE RADAR UNIT. 2 L 7 2 4F RT A21EA 1996112700592 19961127 00592 EU 1996 11 27 QXEA9600465 1 19961122 A 3350 1315 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 462AU 11054 LEFT HAND WING FAIRING EMERGENCY LIGHT IS INOP. LAMP REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996112700593 19961127 00593 EU 1996 11 27 QXEA9600466 1 19961122 A 3350 1820 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 450US 11101 LEFT-HAND OVERWING EMERGENCY EXIT LIGHT IS INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED. 2 L 7 2 4F RT A20EU 1996112700594 19961127 00594 EU 1996 11 27 QXEA9600467 1 19961122 A 3350 1820 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 450US 11101 NUMEROUS EMERGENCY LIGHTS IN CABIN OVERHEAD ARE INOP. THREE BULBS WERE REPLACED AND LIGHTS OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996112700595 19961127 00595 EU 1996 11 27 QXEA9600468 1 19961122 A 3350 1012721 BULB FOKKER FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 487US 11238 EMERGENCY LIGHT AT SEAT 9A IS INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996112700596 19961127 00596 EU 1996 11 27 QXEA9600469 1 19961123 A 3350 1012721 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 462AU 11054 EMERGENCY LIGHTS ARE OUT AT ROWS 10 THROUGH 12. BULBS WERE REPLACED AND LIGHTS OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996112700597 19961127 00597 EU 1996 11 27 QXEA9600470 1 19961124 A 3350 1820 BULB FOKKER FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 484US 11234 LEFT HAND EMERGENCY EXIT HAS ONE EMERGENCY LIGHT OUT. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996112700598 19961127 00598 NM 1996 11 27 96FDEA01691 1 19961125 A 3260 189915 AIR GRD SENSOR BOEING 727 727227 1384078 NM LT MLG WW DEFECTIVE A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 482FE 21464 ON TAKEOFF, GEAR HANDLE WOULD NOT RAISE ABOVE OFF POSITION, HAD 3 GREEN INDICATION, TAIL SKID AND 3 RED LIGHT. WHEN FLA PS RAISED FROM 5 TO 2, HAD INTERMITTENT HORN. FLAPS RETURNED TO 5 AND GEAR HANDLE DOWN WITH RESULTING 3 GREEN LIGHTS. C HECKLIST PROCEDURES FOR LEVER LATCH FAILURE FOLLOWED. LANDED OK AT MEMPHIS. FOUND AIR SENSE SENSOR IN LEFT HAND WHEEL WELL BAD. REPLACED SENSOR, REPLACED LANDING GEAR ACCESSORY UNIT BAD. REPLACED SOLENDID PRECAUTIONARY. SYSTEM CHECK NO RMAL OK TO CONTINUE. 2 L 7 3 4F A3WE 1996112700599 19961127 00599 WP 1996 11 27 ABXA9600670 1 19961121 A 3231 45973345501 ROLLER ASSY DOUG DC9 DC931 3022065 WP LT MLG DOOR DEFECTIVE A ABXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 908AX 47008 DURING GEAR UPLATCH CHECK, LEFT GEAR UNSAFE LIGHT ILLUMINATED AND COULD NOT BE EXTINGUISHED USING THE ABNORMAL PROCEDURE . REPLACED LEFT MAIN LANDING GEAR DOOR LATCH ROLLER ASSEMBLY IAW DC9 OHM 32-11-5, OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1996112700600 19961127 00600 WP 1996 11 27 ABXA9600672 1 19961122 A 2612 3771523 FIRE LOOP DOUG DC8 DC861 3021952 WP PWA JT3D JT3D3B 52039 NE NR 2 ENGINE DEFECTIVE A ABXA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 851AX 45940 669528 INFLIGHT, MASTER FIRE WARNING AND BELL. NO LIGHTS IN LEVER ILLUMINATED. FIRE WARNING TESTED, NR 2 ENGINE WOULD NOT TES T, TRIED SEVERAL TIMES. SECURED ENGINE NR 2, FUEL DUMPED. CHECKED FIRE LOOPS AND WIRES TO NR 2 ENGINE DETECTOR AMP, NO PROBLEMS FOUND. REPLACED NR 2 LOOP FOR TROUBLESHOOTING, SYSTEM OPS CHECKED GOOD. 2 L 7 4 4F 4 F 4A25 1E8 1996112700601 19961127 00601 WP 1996 11 27 ABXA9600673 1 19961121 A 2110 5614845517 COMPRESSOR DOUG DC8 DC863F 302198F WP NR 3 FAILED A ABXA O OTHER O OTHER CR CRUISE 1 GL 23 816AX 46093 AFTER 3 HOURS AT CRUISE, NR 3 CTC BEGAN TO SURGE FROM 10,000 RPM TO 35,000 RPM, ACCOMPANIED BY A BURNING ODOR FROM THE A IR CONDITIONING SYSTEM. SHUTDOWN NR 3 CTC, COMPRESSOR NR 3 OVERHEAT LIGHT DID NOT COME ON. VERIFIED NR 3 CTC BAD, DEFE RRED IAW DC-8 MEL 21-1 DI 816 348, PLACARDED. 2 L 7 4 4F 4A25 1996112700602 19961127 00602 NM 1996 11 27 SRAA961116 1 19961120 A 2740 HORIZ STAB BOEING 747 747246F NM EMPENAGE OUT OF POSITION A SRAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 23 741SJ 22063 DURING TAKEOFF ROLLOUT, TAKEOFF WARNING HORN CAME ON AT 90 KIAS WITH ALL CONDITIONS NORMAL. REJECTED TAKEOFF WITHOUT IN CIDENT. TROUBLESHOT AND FOUND HORIZONTAL STABILIZER SETTING OF 7.5 UNIT TO BE AT EDGE OF MID SCALE GREEN BAND, CAUSING TAKEOFF WARNING HORN TO COME ON WHEN WEIGHT IS REDUCED AT THE NOSE. READJUST HORIZ STABILIZER TRIM, SYSTEM OPS CHECKED GOOD PER MM CH 27-48-00. 2 L 7 4 4F A20WE 1996120300001 19961203 00001 NM 1996 12 3 P5CA9600871 1 19961022 A 5347 SEAT TRACK BOEING 747 747249F 1384849 NM BS 1260-1280 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEVEL 1 CORROSION ON MAIN DECK SEAT TRACK FLANGE UNDERSIDE AT BS 1260 TO BS 1280 LBL 97. CORROSION REMOVED PER BAC SRM AND REPROTECTED PER BAC MM 51-24-11. 2 L 7 4 4F A20WE 1996120300002 19961203 00002 NM 1996 12 3 P5CA9600872 1 19961022 A 5320 FITTING BOEING 747 747249F 1384849 NM BS 1922 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEVEL 1 CORROSION ON TIE DOWN TRACK FITTING ON MAIN DECK AT BS 1922 LBL 50 TO LBL 58. CORROSION REMOVED PER BAC SRM 51- 10-01 AND REPROTECTED PER BAC MM 51-24-11. 2 L 7 4 4F A20WE 1996120300003 19961203 00003 NM 1996 12 3 P5CA9600873 1 19961022 A 5320 BEAM BOEING 747 747249F 1384849 NM BS 1400 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEVEL 1 CORROSION TO POWER DRIVE UNIT SUPPORT BEAM ON MAIN DECK AT BS 1480 LBL 50. REMOVED CORROSION PER BAC SRM 51-10- 01 AND REPROTECTED PER BAC MM 51-24-11. 2 L 7 4 4F A20WE 1996120300004 19961203 00004 NM 1996 12 3 P5CA9600874 1 19961022 A 5320 SUPPORT BOEING 747 747249F 1384849 NM BS 1420 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEVEL 1 CORROSION TO MAIN DECK FLOOR BEAM SUPPORT AT BS 1420 LBL 57. REMOVED CORROSION PER BAC SRM 51-10-01 AND REPROTE CTED PER BAC MM 51-24-11. 2 L 7 4 4F A20WE 1996120300005 19961203 00005 NM 1996 12 3 P5CA9600875 1 19961022 A 5320 SUPPORT BOEING 747 747249F 1384849 NM BS 477 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEVEL 1 CORROSION ON MAIN DECK LONGITUDINAL FLOOR SUPPORT UNDERSIDE AT BS 477 LEFT OUTBOARD. REMOVED CORROSION PER BAC SRM 51-10-01 AND REPROTECTED PER BAC MM 51-24-11. 2 L 7 4 4F A20WE 1996120300006 19961203 00006 NM 1996 12 3 P5CA9600876 1 19961022 A 5320 FITTING BOEING 747 747249F 1384849 NM BS 1918 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEVEL 1 CORROSION TO MAIN DECK CARGO DOOR SILL PLATE SUPPORT FITTING AT BS 1918 LBL 95 TO LBL 100. REMOVED CORROSION PE R BAC SRM 51-10-01 AND REPROTECTED PER BAC MM 51-24-11. 2 L 7 4 4F A20WE 1996120300007 19961203 00007 NM 1996 12 3 P5CA9600877 1 19961022 A 5315 FLOOR BEAM BOEING 747 747249F 1384849 NM BS 1860 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEVEL 1 CORROSION ON MAIN DECK FLOOR BEAM AT BS 1860 LBL 85 TO LBL 95. REMOVED CORROSION PER BAC SRM 51-10-01 AND REPR OTECTED PER BAC MM 51-24-11. 2 L 7 4 4F A20WE 1996120300008 19961203 00008 NM 1996 12 3 P5CA9600878 1 19961022 A 5320 SUPPORT BOEING 747 747249F 1384849 NM BS 1940 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEVEL 1 CORROSION TO MAIN DECK FLOOR SUPPORT AT BS 1940 LBL 60 TO LBL 75. REMOVED PER BAC SRM 51-10-01 AND REPROTECTED PER BAC MM 51-24-11. 2 L 7 4 4F A20WE 1996120300009 19961203 00009 NM 1996 12 3 P5CA9600879 1 19961022 A 5320 SUPPORT BOEING 747 747249F 1384849 NM BS 1840 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEVEL 1 CORROSION ON MAIN DECK FLOOR SUPPORT AT BS 1840 LBL 31 TO LBL 38. REMOVED CORROSION PER BAC SRM 51-10-01 AND R EPROTECTED PER BAC MM 51-24-11. 2 L 7 4 4F A20WE 1996120300010 19961203 00010 NM 1996 12 3 P5CA9600880 1 19961022 A 5320 SUPPORT BOEING 747 747249F 1384849 NM BS 1800 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEVEL 1 CORROSION ON DECK FLOOR SUPPORT AT BS 1800 FROM LBL 11 TO RBL 11. REMOVED CORROSION PER BAC SRM 51-10-01 AND RE PROTECTED PER BAC MM 51-24-11. 2 L 7 4 4F A20WE 1996120300011 19961203 00011 NM 1996 12 3 P5CA9600881 1 19961022 A 5320 SUPPORT BOEING 747 747249F 1384849 NM BS 1800 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEVEL 1 CORROSION ON MAIN DECK FLOOR SUPPORT AT BS 1800 RBL 11. REMOVED CORROSION PER BAC SRM 51-10-01 AND REPROTECTED PER BAC MM 51-24-11. 2 L 7 4 4F A20WE 1996120300012 19961203 00012 NM 1996 12 3 P5CA9600882 1 19961022 A 5320 SUPPORT BOEING 747 747249F 1384849 NM BS 1960 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEVEL 1 CORROSION TO UPPER AND LOWER SURFACES OF MAIN DECK FLOOR SUPPORT AT BS 1960 RBL 12 TO 14. REMOVED CORROSION PER BAC SRM 51-10-01 AND REPROTECTED PER BAC MM 51-24-11. 2 L 7 4 4F A20WE 1996120300013 19961203 00013 NM 1996 12 3 P5CA9600883 1 19961022 A 5320 SUPPORT BOEING 747 747249F 1384849 NM BS 400-460 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEVEL 1 CORROSION ON MAIN DECK LONGITUDINAL FLOOR SUPPORT AT BS 400 TO 460 LEFT OUTBOARD. REMOVED CORROSION PER BAC SR M 51-10-01 AND REPROTECTED PER BAC MM 51-24-11. 2 L 7 4 4F A20WE 1996120300014 19961203 00014 NM 1996 12 3 P5CA9600884 1 19961022 A 5320 SUPPORT BOEING 747 747249F 1384849 NM BS 1900 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEVEL 1 CORROSION ON MAIN DECK FLOOR SUPPORT LOWER SURFACE AT BS 1900 RBL 74. REMOVED CORROSION PER BAC SRM 51-10-01 A ND REPROTECTED PER BAC MM 51-24-11. 2 L 7 4 4F A20WE 1996120300015 19961203 00015 NM 1996 12 3 P5CA9600885 1 19961022 A 5320 SUPPORT BOEING 747 747249F 1384849 NM BS 1760-1766 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEVEL 1 CORROSION ON MAIN DECK FLOOR SUPPORT AT BS 1760 TO 1766 RBL 105. REMOVED CORROSION PER BAC SRM 51-10-01 AND RE PROTECTED PER BAC MM 51-24-11. 2 L 7 4 4F A20WE 1996120300016 19961203 00016 NM 1996 12 3 P5CA9600886 1 19961022 A 5347 SEAT TRACK BOEING 747 747249F 1384849 NM BS 1720 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEVEL 1 CORROSION ON MAIN DECK SEAT TRACK AT BS 1720 LBL 53 TO 58. REMOVED CORROSION PER BAC SRM 51-10-01 AND REPROTEC TED PER BAC MM 51-24-11. 2 L 7 4 4F A20WE 1996120300017 19961203 00017 NM 1996 12 3 P5CA9600887 1 19961022 A 5320 SUPPORT BOEING 747 747249F 1384849 NM BS 1740 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEVEL 1 CORROSION ON MAIN DECK FLOOR SUPPORT AT BS 1740 LBL 33. REMOVED CORROSION PER BAC SRM 51-10-01 AND REPROTECTED PER BAC MM 51-24-11. 2 L 7 4 4F A20WE 1996120300018 19961203 00018 NM 1996 12 3 P5CA9600888 1 19961022 A 5320 SUPPORT BOEING 747 747249F 1384849 NM BS 1660 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEVEL 1 CORROSION ON MAIN DECK FLOOR SUPPORT AT BS 1660 LBL 98 TO 110. REMOVED CORROSION PER BAC SRM 51-10-01 AND REPR OTECTED PER BAC MM 51-24-11. 2 L 7 4 4F A20WE 1996120300019 19961203 00019 NM 1996 12 3 P5CA9600889 1 19961022 A 5330 SKIN BOEING 747 747249F 1384849 NM BS 400-500 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEVEL 1 CORROSION ON FUSELAGE EXTERNAL SKIN AT BS 400 TO 500 S41R TO S44R. REMOVED CORROSION PER BAC SRM 51-10-01 AND REPROTECTED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1996120300020 19961203 00020 NM 1996 12 3 P5CA9600890 1 19961022 A 5330 SKIN BOEING 747 747249F 1384849 NM BS 400 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEVEL 1 CORROSION ON FUSELAGE EXTERNAL SKIN AT BS 400 S41R TO S42R. REMOVED CORROSION PER BAC SRM 51-10-01 AND REPROTEC TED PER BAC SRM 51-10-02. 2 L 7 4 4F A20WE 1996120300021 19961203 00021 NM 1996 12 3 P5CA9600891 1 19961022 A 5347 SEAT TRACK BOEING 747 747249F 1384849 NM BS 1830 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEVEL 2 CORROSION ON MAIN DECK SEAT TRACK AT BS 1830 RBL 56. REPAIRED PER BAC SRM 53-10-05 FIG. 1. 2 L 7 4 4F A20WE 1996120300022 19961203 00022 NM 1996 12 3 P5CA9600892 1 19961022 A 5320 SUPPORT BOEING 747 747249F 1384849 NM BS 1920 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEVEL 2 CORROSION ON MAIN DECK FLOOR SUPPORT AT BS 1920 LBL 80 TO 88. REPAIRED PER BAC SRM 51-40-04 FIG 3. 2 L 7 4 4F A20WE 1996120300023 19961203 00023 NM 1996 12 3 P5CA9600893 1 19961022 A 5320 SUPPORT BOEING 747 747249F 1384849 NM BS 1920 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEVEL 2 CORROSION ON MAIN DECK FLOOR SUPPORT AT BS 1920 RBL 100. REPAIRED PER BAC SRM 51-40-04 FIG. 3. 2 L 7 4 4F A20WE 1996120300024 19961203 00024 NM 1996 12 3 P5CA9600894 1 19961022 A 5347 65B621791 SEAT TRACK BOEING 747 747249F 1384849 NM BS 300 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEVEL 2 CORROSION ON MAIN DECK SEAT TRACK AT BS 300 LBL 42. REPLACED SEAT TRACK PER BAC SRM 51-10-07. 2 L 7 4 4F A20WE 1996120300025 19961203 00025 NM 1996 12 3 P5CA9600895 1 19961023 A 5347 65B621171 SEAT TRACK BOEING 747 747249F 1384849 NM BS 420 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEVEL 2 CORROSION ON MAIN DECK SEAT TRACK AT BS 420 LBL 11. REPLACED SEAT TRACK PER BAC SRM 51-10-07. 2 L 7 4 4F A20WE 1996120300026 19961203 00026 NM 1996 12 3 P5CA9600896 1 19961025 A 5320 SUPPORT BOEING 747 747249F 1384849 NM BS 1284 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEVEL 1 CORROSION ON KEEL BEAM ACCESS PANEL SUPPORT BEAM AT BS 1284. LBL 12 TO RBL 12. REMOVED CORROSION PER BAC SRM 51-10-01 AND REPROTECTED PER BAC MM 51-24-11. 2 L 7 4 4F A20WE 1996120300027 19961203 00027 NM 1996 12 3 P5CA9600897 1 19961025 A 5320 SUPPORT BOEING 747 747249F 1384849 NM BS 1304 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEVEL 1 CORROSION ON KEEL BEAM ACCESS PANEL SUPPORT BEAM AT BS 1304 LBL 12. REMOVED CORROSION PER BAC SRM 51-10-01 AND REPROTECTED PER BAC MM 51-24-11. 2 L 7 4 4F A20WE 1996120300028 19961203 00028 NM 1996 12 3 P5CA9600898 1 19961025 A 5320 SUPPORT BOEING 747 747249F 1384849 NM BS 1326 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEVEL 1 CORROSION ON KEEL BEAM ACCESS PANEL SUPPORT BEAM AT BS 1326 LBL 12 TO RBL 12. REMOVED CORROSION PER BAC SRM 51 -10-01 AND REPROTECTED PER BAC MM 51-24-11. 2 L 7 4 4F A20WE 1996120300029 19961203 00029 NM 1996 12 3 P5CA9600899 1 19961025 A 5320 SUPPORT BOEING 747 747249F 1384849 NM BS 1340 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LEVEL 1 CORROSION ON KEEL BEAM ACCESS PANEL SUPPORT BEAM AT BS 1340 LBL 12 TO RBL 12. REMOVED CORROSION PER BAC SRM 51 -10-01 AND REPROTECTED PER BAC MM 51-24-11. 2 L 7 4 4F A20WE 1996120300030 19961203 00030 NM 1996 12 3 VNAA9611002 1 19961106 A 5101 STRUCTURE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE AIRFRAME BIRDSTRIKE A VNAA A UNSCHED LANDING C F.O.D. CL CLIMB 1 GL 07 422JS 3018 JUST AFTER TAKEOFF, FLEW THROUGH A FLOCK OF BIRDS, HEARD 3 STRIKES. RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTE NANCE PERFORMED A BIRD STRIKE AND OVERWEIGHT LANDING INSPECTION. NO DEFECTS WERE NOTED AND THE AIRCRAFT WAS APPROVED FO R RETURN TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 1996120300031 19961203 00031 SW 1996 12 3 CA960404014 1 19960326 A 7120 206063106005 ENGINE MOUNT BELL 206 206L 1181522 SW ALLSN 250C 250C20 03013 GL LEFT HAND CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA CAE295348 (CAN) COLLET WAS MISSING FROM HIGH LOCK. WHEN HIGH LOCK REMOVED IT WAS FOUND COMPLETELY CORRODED AND CORROSION COULD BE SHAKEN OUT OF HOLE. AIRCRAFT HOURS 11806. 1 G 7 1 3U 3 U H2SW E4CE 1996120300032 19961203 00032 GL 1996 12 3 CA960404015 2 19960325 A 7510 23034755 TUBE BELL 206 206L 1181522 SW ALLSN 250C 250C20 03013 GL ANTI-ICE WORN W K NONE O OTHER IN INSP/MAINT 1 CA 2359 CAE295348 (CAN) TUBE PARTIALLY WORN DUE TO CONTACT WITH HEATER HOSE. TUBE REPLACED, HEATER HOSE RELOCATED. 1 G 7 1 3U 3 U H2SW E4CE 1996120300033 19961203 00033 GL 1996 12 3 CA960412007 3 19960322 A 6110 57B083037 START LOCK PIN SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP HARTZL HCB3T HCB3TN5 GL PROP SPLIT PIN PULLED THROUGH W K NONE O OTHER IN INSP/MAINT 1 CA 18492 905 P54183 BV4296 (CAN)ON ROUTINE PHASE INSPECTION, THE SPLIT PINS WERE FOUND TO BE PULLING THROUGH THE ENDS OF THE START LOCKS. NEW START LOCKS P/N 57B08030-37 NOW SUPPLIED BY HARTZELL HAS A THICKER END WALL ALTHOUGH THE P/N HAS NOT BEEN CHANGED. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C P15EA 1996120300035 19961203 00035 NM 1996 12 3 DL76L962522 1 19961114 A 4920 380029816 APU BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE TAIL FAILED A DALA O OTHER A FLAME/FIRE IN INSP/MAINT 1 SO 27 175DN 24803 P1532 DURING GROUND OPERATIONS, APU AUTO SHUTDOWN DUE WITH TAILPIPE FIRE. INSPECTION REVEALED GEARBOX OIL IN TAILPIPE CAUSING FIRE. REPLACED APU. 2 L 7 2 4F 4 F RT A1NM E24NE 1996120300036 19961203 00036 NM 1996 12 3 DL73S962531 1 19961113 A 5315 6545410223 FLOOR BEAM BOEING 737 737232 1384475 NM BS 664 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 306DL 23078 THE BL 0.07 FLOORBEAM UPPER CAP OF THE WING CENTER SECTION IS CRACKED ALL THE WAY THROUGH THE CAP JUST FORWARD OF FS 664 AT A NUTPLATE HOLE. NO CRACKS WERE FOUND IN THE WEB. THE CRACK IS TYPICAL PER BOEING SERVICE BULLETIN 737-57-1210. T HE ER/A WILL INSTALL THE SERVICE BULLETIN REPAIR FOR THIS CONDITION. 2 L 7 2 4F RT A16WE 1996120300037 19961203 00037 WP 1996 12 3 RAIA961028 2 19961030 A 7320 8976921 FILTER BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP NR 2 ENG DIRTY A RAIA E ENGINE SHUTDOWN O OTHER AP APPROACH 1 CE 03 422AM 173 856 961026 PAH - FLT 7365 - ON APPROACH NR 2 ENGINE STARTED SURGING. ENGINE WAS SHUT DOWN. REPLACED ENGINE FUEL CONTROL FILTER. ( M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996120300045 19961203 00045 SO 1996 12 3 CA960328009 2 19960228 A 8520 CAMSHAFT CESSNA 188 A188B 2073005 CE CONT O550 IO550* SO ENGINE SPALLED W K NONE O OTHER IN INSP/MAINT 1 CA 162 284028 (CAN) DURING INSPECTION AND UPON DISMANTLING, #3 & #4 INTAKE LOBES, #5 EXHAUST LOBE, AND #5 & #6 INTAKE LOBES ON CAMSHAF T WERE SPALLED. TWO LOBES WERE SPALLED OVER ENTIRE FACE AND TWO WERE SPALLED ONLY IN THE CENTRE. TWO LIFTERS WERE CORROD ED BADLY. ALL MAIN BEARING INSERTS AND ALL CONNECTING ROD BEARING INSERTS WERE METAL CONTAMINATED. 1 L 7 1 3O 3 O A9CE E3SO 1996120300046 19961203 00046 SO 1996 12 3 CA960328010 2 19960228 A 8520 CAMSHAFT CESSNA 188 A188B 2073005 CE CONT O550 IO550* SO ENGINE SPALLED W K NONE P NO WARNING INDICATION IN INSP/MAINT 1 CA 208 284027R (CAN) DURING INSPECTION AND UPON DISMANTLING, #5 AND #1 EXHAUST LOBE, AND #3 AND #4 INTAKE LOBES ON CAMSHAFT WERE SPALLE D. THE LIFTERS CONTACTING THE SPALLED LOBES WERE ALSO SPALLED. #2 EXHAUST LIFTER, #4 EXHAUST LIFTER AND #6 INTAKE LIFTER WERE CORROSIVELY PITTED. ALL MAIN BEARING INSERTS AND ALL CONNECTING ROD BEARING INSERTS WERE METAL CONTAMINATED. 1 L 7 1 3O 3 O A9CE E3SO 1996120300047 19961203 00047 NM 1996 12 3 DL757962422 1 19961030 A 4910 INLET DOOR BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE APU LOCKED CLOSED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 680DA 19669 26956 P344 APU QUIT IN FLIGHT, COULD NOT RESTART DUE TO INLET DOOR FAULT LEFT ENGINE GENERATOR ON MCO. ELP LOCKED INLET DOOR OPEN PER MEL 49-15-01B. 2 L 7 2 4F 4 F RT A2NM E17NE 1996120500040 19961205 00040 NE 1996 12 5 IXXA9600168 2 19961127 A 7250 9026M70G01 TURBINE BLADES DOUG DC8 DC871 302199A WP GE CFM56 CFM562C1 13802 NE NR 2 ENGINE DAMAGED A IXXA E A ENGINE SHUTDOWN UNSCHED LANDING E X VIBRATION/BUFFET ENGINE FLAMEOUT CL CLIMB 1 GL 23 820BX 27692 13485 46065 693387 SHORTLY AFTER ROTATION DEPARTING FLL, THE NUMBER 2 ENGINE EXPERIENCED A HEAVY COMPRESSOR STALL. THE ENGINE REPORTILY FL AMED OUT. THE CREW SECURED THE ENGINE IAW COMPANY PROCEDURES AND RETURNED TO FLL. GROUND INSPECTION BY MAINTENANCE FOU ND METAL IN THE TAILPIPE ACCOMPANIED BY DAMAGED TURBINE BLADES. THE ENGINE REQUIRED REPLACEMENT. 2 L 7 4 4F 4 F 4A25 E2GL 1996120500041 19961205 00041 NM 1996 12 5 AWXA9600715 1 19961126 A 3397 WIRE BOEING 737 737277 1384570 NM CABIN DISCONNECTED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 179AW 22646 DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 6 LT EMERGENCY LIGHT INOPERATIVE. RESPLICED WIRES, OPERATIONS CHECK GOOD. 2 L 7 2 4F RT A16WE 1996120500042 19961205 00042 NM 1996 12 5 AWXA9600716 1 19961126 A 3350 831136 LIGHT BOEING 737 7373G7 1384595 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 154AW 23776 DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 17 FLOOR PROXIMITY EMERGENCY LIGHT INOP. REPLACED ROW 17 FLOOR PROXIMITY LI GHT ASSEMBLY, FUNCTION CHECK NORMAL. 2 L 7 2 4F RT A16WE 1996120500043 19961205 00043 NM 1996 12 5 CALA9601712 1 19961125 A 4930 3602310281 FUEL CONTROL GTCP85129 BOEING 737 7372C0 1384488 NM APU INOPERATIVE A A CALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 09 10242 10551 10551 P34462 20071 THE NR 1 GENERATOR FAILED WHILE EN ROUTE. THE APU WAS STARTED AND THE FIRE WARNING BELL SOUNDED WITH THE RED APU FIRE H ANDLE ILLUMINATED. THE APU START SWITCH WAS PLACED TO OFF AND THE FIRE WARNING SYSTEM TESTED GOOD. THE AIRCRAFT WAS DI VERTED TO CMH WHERE IT LANDED WITHOUT INCIDENT. TROUBLESHOOTING BY MAINTENANCE FOUND THE APU TORCHING ON START. THE A PU FUEL CONTROL AND COMBUSTOR WERE REPLACED. THE APU TAILPIPE FIRELOOP HARNESS AND EGT WIRE HARNESS WERE FOUND BURNT. B OTH HARNESSES WERE REPLACED. THE EGT THERMOCOUPLE WAS REPLACED AS A PRECAUTIONARY MEASURE, OPERATION OF THE APU CHECKED GOOD. IN ADDITION, THE NR 1 GENERATOR WAS REPLACED. 2 L 7 2 4F A16WE 1996120500044 19961205 00044 NM 1996 12 5 9625336622 1 19961114 A 5347 SEAT TRACK BOEING 747 747251B 1384892 NM BS 1250 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 622US 21704 DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE UPPER SURFACE OF THE OUTBOARD FLANGE OF THE CROWNLESS SEAT TRACK. REP AIRED PER EA 66-120446. 2 L 7 4 4F A20WE 1996120500045 19961205 00045 NM 1996 12 5 9625346622 1 19961109 A 5315 65B226343 FLOORBEAM BOEING 747 747251B 1384892 NM BS 1720 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 622US 21704 DURING PERIODIC CHECK, FOUND MAIN DECK FLOOR BEAM CORRODED ON THE UPPER SURFACE OF UPPER CHORD. REPAIRED PER EA 66-1204 40. 2 L 7 4 4F A20WE 1996120500046 19961205 00046 WP 1996 12 5 9625359604 1 19961122 A 3260 CONNECTOR DOUG DC9 DC932 3022066 WP RT MLG LOOSE A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 604NW 47222 RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. RECYCLED GEAR AND NORMAL INDICATIONS WERE ACHIE VED. ON APPROACH, SPOILERS WOULD NOT ARM. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND RIGHT MAIN GEAR UPLOCK SWITCH CANNON PLUG LOOSE. SECURED PLUG, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996120500047 19961205 00047 WP 1996 12 5 9625369604 1 19961125 A 3260 DOWNLOCK SWITCH DOUG DC9 DC932 3022066 WP RT MLG MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 604NW 47222 RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. FLIGHT RETURNED TO MSP AND LANDED WITHOUT IN CIDENT. MAINTENANCE REPLACED DOWNLOCK SWITCH, CLEANED AND LUBED UPLOCK MECHANISM AND REPLACED LOOSE RIVETS FOR SEQUENCE MECHANISM ON DOOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996120500048 19961205 00048 EU 1996 12 5 9625373238 1 19961126 A 5610 NP1653132 WINDOW AIRBUS 320 A320212 EU COCKPIT DELAMINATED A NWAA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 GL 01 338NW 13885 360 DURING CLIMBOUT AT 25,500 FEET, THE FIRST OFFICER'S NR 3 WINDOW OUTER PANE DELAMINATED AND SEPARATED FROM THE MIDDLE PAN E. AIRCRAFT RETURNED TO BOS AND ACCOMPLISHED AN UNEVENTFUL OVERWEIGHT LANDING. MAINTENANCE REPLACED THE FIRST OFFICER' S NR 3 WINDOW. 2 L 7 2 4F RT A28NM 1996120500049 19961205 00049 EU 1996 12 5 9625383213 1 19961126 A 3350 100865 POWER SUPPLY AIRBUS 320 A320211 3930320 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 313US 153 DURING LINE MAINTENANCE ALL OF FIRST CLASS EMERGENCY FLOOR PROXIMITY LIGHTS FOUND INOPERATIVE. MAINTENANCE REPLACED POW ER SUPPLY 110WL-1, OPS CHECKED OK. 2 L 7 2 4F RT A28NM 1996120500050 19961205 00050 EU 1996 12 5 WWMA9600100 1 19961126 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT DIRTY A WWMA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 WP 15 354SB 340B354 DURING TAXI, THE CARGO SMOKE LIGHT CAME ON. IT STAYED ON FOR AT LEAST ONE MINUTE THEN WENT OFF, THIS SEQUENCE HAPPENED REPEATEDLY UNTIL ENGINE SHUTDOWN UPON RETURNING TO THE GATE. MAINTENANCE CLEANED BOTH CARGO SMOKE DETECTORS AND RETURNE D THE AIRCRAFT TO SERVICE. 2 L 7 2 4T RT A52EU 1996120500051 19961205 00051 NM 1996 12 5 96FDEA01692 1 19961123 A 5270 211FW104 SWITCH BOEING 727 727233 138408A NM CARGO DOOR MALFUNCTIONED A FDEA B EMER. DESCENT N FALSE WARNING CL CLIMB 1 SO 25 269FE 21675 AT FLIGHT LEVEL 290 CLIMBING TO FLIGHT LEVEL 310, PRESSURIZATION NORMAL, MAIN CARGO DOOR LIGHT ILLUMINATED. PRECAUTIONA RY DESCENT TO 10,000 FT, SLOWED TO 250 KNOTS PER RED TAB PROCEDURES. ALSO, DEPRESSURIZED THE AIRCRAFT, HAD BULKHEAD CAR GO DOOR UNLOCKED LIGHT ILLUMINATED, PRESSURIZATION WAS NORMAL DURING ENTIRE PROCEDURE. DOOR LIGHT REMAINED ON DURING TH E REST OF FLIGHT LEVEL. TROUBLESHOT DOWN TO S9035 LATCH WARNING PROXIMITY SENSOR. INSTALLED NEW SWITCH ADJUSTED PER MA INTENANCE MANUAL 52-34-9 PAGE 513, OPERATIONAL CHECK GOOD. 2 L 7 3 4F RT A3WE 1996120500053 19961205 00053 NM 1996 12 5 96FDEA01694 1 19961127 A 2780 SWITCH SPACER BOEING 727 72722 1384002 NM NR 2 LE FLAP MISSING A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 168FE 18865 NR 2 LEADING EDGE FLAP FAILED TO RETRACT AFTER TAKEOFF. FOLLOWED CHECKLIST WITH NO RESULTS, RETURNED TO PORTLAND. REMO VED AND REPLACED NR 2 FLAP SWITCH, FOUND SPACER MISSING. INSTALLED SPACER, OPERATIONAL CHECK SEVERAL TIMES OPERATIONAL CHECK GOOD PER MAINTENANCE MANUAL 27-81-0. 2 L 7 3 4F A3WE 1996120500054 19961205 00054 WP 1996 12 5 ABXA9600671 1 19961122 A 3260 UNSAFE LIGHT DOUG DC9 DC931 3022065 WP LT MLG ILLUMINATED A ABXA K NONE N FALSE WARNING CL CLIMB 1 GL 23 908AX 47008 UPON GEAR RETRACTION, LEFT GEAR UNSAFE LIGHT WOULD NOT EXTINGUISH. FERRIED AIRCRAFT FROM MEM TO ILN. WORK IN PROGRESS AT THIS TIME. 2 L 7 2 4F A6WE 1996120500055 19961205 00055 WP 1996 12 5 ABXA9600674 1 19961125 A 3350 60030451 POWER SUPPLY DOUG DC9 DC941 302207N WP CABIN DEFECTIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 956AX 2350 47620 EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY IAW DC-9 MM 33-53-0. 2 L 7 2 4F A6WE 1996120500056 19961205 00056 WP 1996 12 5 ABXA9600675 1 19961126 A 3350 60030431 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN DEFECTIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 924AX 1919 47403 EMERGENCY LIGHTS CAME ON WHEN POWER IS REMOVED FROM AIRCRAFT. REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY IAW DC-9 MM 33-53-0. 2 L 7 2 4F A6WE 1996120500057 19961205 00057 WP 1996 12 5 ABXA9600676 1 19961127 A 2612 3771523 FIRE LOOP DOUG DC8 DC861 3021952 WP PWA JT3D JT3D3B 52039 NE NR 2 ENGINE MALFUNCTIONED A ABXA K NONE N FALSE WARNING DE DESCENT 1 GL 23 851AX 45940 669528 CREW REPORTED, THEY EXPERIENCED A BRIEF FIRE BELL AND MASTER FIRE WARNING LIGHT ON DESCENT. UNABLE TO VERIFY WHICH ENGI NE, SUSPECT NR 2 ENGINE DUE TO PREVIOUS HISTORY. CHECKED ALL ENGINE FIRE SENSING ELEMENTS IAW DC-8 MM 26-10-1, ALL TEST ED GOOD. REPLACED NR 2 LOWER FIRE SENSING LOOP IAW DC-8 MM 26-10-1. ALL ENGINE FIRE WARNING SYSTEMS AND INDICATIONS OP ERATE NORMALLY IAW DC-8 MM. 2 L 7 4 4F 4 F 4A25 1E8 1996120500059 19961205 00059 NM 1996 12 5 DL72S962539 1 19961117 A 3350 RPS1 POWER SUPPLY BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 528DA 21702 ESCAPE PATH LIGHTING INOP BETWEEN ROWS 27 AND 35. FOUND WIRES SHORTED IN TRACK LIGHTING. SPLICED WIRES AND REPLACED BA TT PACK M9027, CKS OK. 2 L 7 3 4F A3WE 1996120500060 19961205 00060 NM 1996 12 5 DLM11962541 1 19961118 A 3397 WIRE DOUG MD11 MD11 3023602 NM CABIN BROKEN A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 803DE 48474 A/C LOST ELECTRICAL POWER AT GATE WITH PASSENGERS ON BOARD. RIGHT SIDE EMERGENCY LIGHTS AT ROW 30 TO 36 FLOOR LIGHTS IN OPERATIVE. REPAIRED BROKEN WIRE FOUND IN FLOOR TRACK WIRING. 2 L 7 3 4F RT A22WE 1996120500061 19961205 00061 NM 1996 12 5 DL76L962544 1 19961118 A 3350 BPS73 POWER SUPPLY BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 174DN 24802 ON LAYOVER, EMERGENCY PATH LIGHT AT SEAT 24 TO 27 BOTH SIDE INOP. REPLACED EMERGENCY LIGHT POWER SUPPLY OPS CHK NORMAL. 2 L 7 2 4F RT A1NM 1996120500062 19961205 00062 NE 1996 12 5 DLL10962547 2 19961119 A 7200 ENGINE FFR101MK14 LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B NE NR 2 MALFUNCTIONED A DALA E ENGINE SHUTDOWN X ENGINE FLAMEOUT CL CLIMB 1 SO 27 719DA B616 193C1135 10657 NR 2 ENG EPR GRADUALLY ROLLED BACK ON CLIMBOUT. OTHER ENGINE PARAMETERS FOLLOWED, FUEL AMP NO HELP. 2 L 7 3 4F 4 F A23WE E12EU 1996120500063 19961205 00063 NM 1996 12 5 DL72W962548 1 19961119 A 2170 COALESCER BAG 22D10 BOEING 727 727247 138408F NM LEFT PACK DIRTY A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 2810W 20648 AT FL 11,000 WITH LT PACK ONLY ON F/AS REPORTED, SMOKE IN CABIN COMING FROM OVHD VENTS. REPLACED LT WATER SEPARATOR BAG , RAN NR 1 ENG AND OPERATED BOTH PACKS. ALL OK, NO SMOKE. 2 L 7 3 4F A3WE 1996120500064 19961205 00064 NM 1996 12 5 DLM90962550 1 19961119 A 3350 P2070003001 LIGHT DOUG MD90 MD9030 3023690 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 903DA 53383 MID CABIN EMERGENCY FLASHLIGHT INOP. REPLACED FLASHLIGHT. 2 L 7 2 4F RT A6WE 1996120500065 19961205 00065 WP 1996 12 5 DLL13962554 1 19961120 A 2560 MEGAPHONE MV10S LKHEED 1011 10113851 5265010 WP 4L DOOR MALFUNCTIONED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 790DL 193A1143 MEGAPHONE WEAK AT 4L. 2 L 7 3 4F A23WE 1996120500066 19961205 00066 NM 1996 12 5 DL72S962556 1 19961120 A 3350 POWER SUPPLY RPS1 BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 420DA 21273 FLOOR EMERGENCY PATH LIGHTING OUT IN FIRST CLASS AND COACH. REPLACED DIODE IN FWD EMERGENCY LIGHTING POWER SUPPLY, OPS CK GOOD. 2 L 7 3 4F A3WE 1996120500067 19961205 00067 NM 1996 12 5 DLM11962557 1 19961020 A 2622 FIRE BOTTLE 51211 DOUG MD11 MD11 3023602 NM 4L DOOR LOW CHARGE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 813DE 48600 HALON FIRE BOTTLE AT 4L IS LOW. 2 L 7 3 4F RT A22WE 1996120500068 19961205 00068 NM 1996 12 5 DL76L962558 1 19961121 A 2120 AIR DISTRIBUTION BOEING 767 767332 1382001 NM CABIN ODOR A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 171DN 24759 BURNING ODOR REPORTED BY FLIGHT ATTENDANT AND PAX FROM SEATS 24 F/G. NO ODOR FOUND AND COULD NOT DUPLICATE. 2 L 7 2 4F RT A1NM 1996120500069 19961205 00069 NM 1996 12 5 DL72S962559 1 19961121 A 5530 STRINGER BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 528DA 21702 STRINGER CRACKED ON VERT STAB STR 9 STA 44 RT SIDE. REPAIRED PER M/M 55-30-0 FIG 803. 2 L 7 3 4F A3WE 1996120500070 19961205 00070 NM 1996 12 5 DL72S962560 1 19961121 A 5530 STRINGER BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 528DA 21702 STRINGER CRACKED ON VERT STAB STA 157.2 STR 4 LT. REPAIRED PER M/M 55-30-0 FIG 803. 2 L 7 3 4F A3WE 1996120500071 19961205 00071 NM 1996 12 5 DLM88962561 1 19961121 A 3350 61020 BATTERY DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 914DE 49957 AFT CABIN FLASHLIGHT INOP. REPLACED BATTERY. 2 L 7 2 4F RT A6WE 1996120500072 19961205 00072 NM 1996 12 5 DL72S962562 1 19961121 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 517DA 21433 LEFT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK, CHECKS GOOD. 2 L 7 3 4F A3WE 1996120500073 19961205 00073 NM 1996 12 5 DL72K962563 1 19961111 A 5711 SPAR STIFFENER BOEING 727 727232 1384082 NM NR 3 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 481DA 20861 LE SPAR STIFFENER CRACKED AT NR 3 SLAT INBD TRACK. REPAIRED PER M/M 57-20-21. 2 L 7 3 4F A3WE 1996120500074 19961205 00074 NM 1996 12 5 DL72P962564 1 19961106 A 5531 RIB BOEING 727 727225 1384077 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8890Z 21859 VERTICAL RIB INSIDE PLATE 9504 CRACKED LEFT AND RIGHT SIDE JUST ABOVE S-DUCT. REPAIRED PER SRM 53-10-4. 2 L 7 3 4F A3WE 1996120500075 19961205 00075 WP 1996 12 5 DLL13962565 1 19961122 A 3350 LIGHT P4010021 LKHEED 1011 10113851 5265010 WP 2R DOOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 783DL 193A1009 EMERGENCY FLASHLIGHT AT 2R INBD INOP. 2 L 7 3 4F A23WE 1996120500076 19961205 00076 1996 12 5 DLM88962566 4 19961122 A 3460 DFGC 4034241971 DOUG MD88 MD88 3023688 NM E/E COMP FAILED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK G MULTIPLE FAILURE TO TAKEOFF 1 SO 27 946DL 91062575 49819 DURING T/O ROLL, LOST ALL FLT GUID DISPLAY, NR 1 PFD F/D WITH FAIL LIGHTS .A/T KICKED OFF MACH TRIM, YAW DAMP AND WINDS HEAR INOP LIGHTS ILLUM ON AOP. NO C/BS POPPED, REJECTED T/O AT 120 KTS 35 DEG F, AT CVG 890MSL. MAX BRK TEMP OF 285, N O OVHT BRK LIGHT. REPLACED NR 1 DFGC, RAN RTS CKTS GOOD. 2 L 7 2 4F RT A6WE 1996120500077 19961205 00077 NM 1996 12 5 DL72S962568 1 19961123 A 3350 MS1557081 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 515DA 21431 R2 SERVICE DOOR EMERGENCY LIGHT INOP. REPLACED LIGHT, CHECKS GOOD. 2 L 7 3 4F A3WE 1996120500078 19961205 00078 NM 1996 12 5 DL72K962569 1 19961111 A 2782 ACTUATOR BRACKET BOEING 727 727232 1384082 NM NR 1 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 481DA 20861 O/B ACTUATOR ATTACH BRACKET CRACKED AT UPPER CORNER NR 1 L/E FLAP. INSTALLED REPAIR DOUBLER PER M/M 57-20-21. 2 L 7 3 4F A3WE 1996120500081 19961205 00081 NM 1996 12 5 DL73S962573 1 19961118 A 3397 WIRE BOEING 737 737232 1384475 NM PWA 4060 PW4060 52119 NE CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 315DL 23087 724150 EMERGENCY TRACK LIGHTING INOP FWD AND AFT CABIN. REPLACED CHARGER BASE AND BATTERY PACKS, NO HELP. FOUND BROKEN WIRE I N LIGHTING TRACK THAT AFFECTED MOST FWD AND AFT LIGHT SEGMENTS. 2 L 7 2 4F 4 F RT A16WE E24NE 1996120500082 19961205 00082 NM 1996 12 5 DL76L962574 1 19961123 A 3260 GEAR LIGHT 849704 BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE COCKPIT MALFUNCTIONED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 171DN 511 24759 724150 AFTER T/O, WHEN GEAR HANDLE WAS RAISED, LANDING GEAR GREEN LIGHTS STAYED ON, TAIL SKID LIGHT ON, CAPTS PITOT, RT AUX PIT OT AND TAT LIGHTS ON. EICAS STATUS PAGE INDICATED LANDING GEAR MONITOR, NOSE AIR/GND DISAGREE, A/G DISAGREE AND ICE DET MSGS. RESEATED ASSOCIATED CARDS, CHECKED OK. 2 L 7 2 4F 4 F RT A1NM E24NE 1996120500083 19961205 00083 WP 1996 12 5 DLL15962575 1 19961123 A 7732 A24000004 VIB MONITOR A24000004 LKHEED 1011 10113853 5265020 WP NR 2 ENGINE MALFUNCTIONED A DALA E ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 SO 27 755DL 0293 193Y1184 14625 NR 2 ENGINE WAS SHUTDOWN ON DESCENT APPROX 20K FT. HIGH VIBS BOTH CHANNELS 2.6 VIBS. NO OTHER ABNORMAL ENGINE INDICATI ONS, NO ICING PRESENT. REPLACED ENG VIB MONITOR, RAN ENGINES PER PFHB TEST. CK'D CHIP DETECTORS, FILTERS, INLET AND EX HAUST. BORESCOPED HPT AND NOZZLE GUIDE VANES, ALL OK. 2 L 7 3 4F A23WE 1996120500084 19961205 00084 NM 1996 12 5 DL757962576 1 19961124 A 3350 P2070003 BATTERY BOEING 757 757232 1384965 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 633DL 23614 14625 MID CABIN EMERGENCY FLASHLIGHT WON'T TEST. REPLACED FLASHLIGHT AND BATTERY OP CK OK. 2 L 7 2 4F RT A2NM 1996120500085 19961205 00085 NE 1996 12 5 DL757962577 2 19961124 A 7200 ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 FAILED A A DALA O OTHER X ENGINE FLAMEOUT DE DESCENT 1 SO 27 662DN 20635 24991 716549 ON DESCENT AT APPROX FL240, THE RIGHT ENGINE FLAMED OUT WITH A SUDDEN YAW MOVEMENT. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. DURING INSPECTION SMALL PIECES OF METAL WERE FOUND IN THE EXHAUST SECTION. 2 L 7 2 4F 4 F RT A2NM E17NE 1996120500086 19961205 00086 NM 1996 12 5 DLM11962580 1 19961124 A 3350 6044113 BATTERY DOUG MD11 MD11 3023602 NM CABIN DISCHARGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 806DE 48477 EMERGENCY LIGHT SYSTEM FAULTS BATTERY PACK NR 3 AND NR 6. 2 L 7 3 4F RT A22WE 1996120500087 19961205 00087 NM 1996 12 5 DLM11962581 1 19961124 A 3350 6044113 BATTERY DOUG MD11 MD11 3023602 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 806DE 48477 EMERGENCY LIGHT SYSTEM FAULTED BATTERY PACK NR 3 AND NR 6. 2 L 7 3 4F RT A22WE 1996120500088 19961205 00088 NM 1996 12 5 DL72S962582 1 19961125 A 7933 OIL TEMP BULB BOEING 727 727232 1384082 NM NR 3 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 27 515DA 43962 21431 695277 SHUTDOWN NR 3 ENGINE AT 1505Z DUE TO HIGH ENGINE OIL TEMP. LANDED ORD 1531Z, ALL OTHER INDICATIONS WERE NORMAL. ENGINE SHUTDOWN LESS THAN 30 MINUTES. NECESSARY TO REPLACE NR 3 ENGINE OIL TEMP BULB. INSPECTED ENGINE PER MM 72-00 PG 212L. RAN ENGINE, ALL INDICATIONS NORMAL. 2 L 7 3 4F A3WE 1996120500089 19961205 00089 NE 1996 12 5 DLM11962583 2 19961125 A 7200 ENGINE DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE NR 3 MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 809DE 12849 48480 723906 NR 3 ENGINE SURGED ON T/O AND EGT WENT TO 710 DEGREES. ENG PARAMETERS RETURNED TO NORMAL AFTER POWER REDUCTION. AIRCRA FT FERRIED TO ATL FOR ENGINE CHANGE. 2 L 7 3 4F 4 F RT A22WE E24NE 1996120500090 19961205 00090 NM 1996 12 5 DLM88962584 1 19961125 A 3320 BALLAST DOUG MD88 MD88 3023688 NM CABIN BURNED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 949DL 49880 JUST BEFORE PUSHBACK, THE SIDE WALL LIGHT, CAPT SIDE OF FIRST CLASS BURNED OUT, RELEASING A FAINT ELECTRICAL SMOKE SMELL . DISCONNECTED BALLAST AT 1 AB FWD TO MCO 25-00-12. INSPECTED AREA FOR DAMAGE, NONE FOUND. 2 L 7 2 4F RT A6WE 1996120500091 19961205 00091 NM 1996 12 5 DL72S962586 1 19961125 A 5610 WINDOW BOEING 727 727232 1384082 NM COCKPIT SHATTERED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 477DA 20754 AT FL 310 R2 WINDOW OUTER PANE CRACKED. DIVERTED TO MCO. 2 L 7 3 4F A3WE 1996120500092 19961205 00092 NM 1996 12 5 DL72S962587 1 19961113 A 5320 CHORD BOEING 727 727232 1384082 NM NLG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 408DA 21152 AT MID VISIT, THE NLG LT LWR CHORD WAS FOUND TO BE CORRODED. CORROSION WAS REMOVED AND REPAIR ACCOMPLISHED PER SRM 53-1 0-4. 2 L 7 3 4F A3WE 1996120500093 19961205 00093 NM 1996 12 5 DL72S962588 1 19961112 A 5312 BULKHEAD SUPPORT BOEING 727 727232 1384082 NM C1 BIN WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 408DA 21152 AT MID VISIT, THE VERT SUPPORT BEAMS FOR AFT C1 BIN BULKHEAD WERE FOUND TO BE WORN. THEY WERE REPAIRED PER SRM 53-10-9. 2 L 7 3 4F A3WE 1996120500094 19961205 00094 NM 1996 12 5 DL72S962589 1 19961125 A 2782 BRACKET BOEING 727 727232 1384082 NM NR 2 LE SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 527DA 21587 FOUND ON E1 LETTER CK, NR 2 INBD AND OUTBD SLAT ACTUATOR ATTACH BRACKETS CRACKED. REPAIRED PER MM 57-40-0. 2 L 7 3 4F A3WE 1996120500095 19961205 00095 NM 1996 12 5 DL733962590 1 19961125 A 3350 LIGHT OL3071BEGPL BOEING 737 737347 1384647 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 3301 23181 2ND EMERGENCY TRACK LIGHT INOP IN Y/C. RELAMPED OPS CKS NML. 2 L 7 2 4F RT A16WE 1996120500096 19961205 00096 NM 1996 12 5 DL757962591 1 19961125 A 2913 HYD PUMP TC125UK06Y BOEING 757 757232 1384965 NM LT ENGINE LEAKING A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 620DL 22910 LEFT HYD QTY DECREASED IN FLT WITH BOTH LEFT ELEC AND ENG PUMPS OFF AND PTU CB. PULLED, LOSS WAS SLOWED CONSIDERABLY. F OUND LEFT ENG PUMP PRESSURE FILTER DIFFERENTIAL BUTTON ASSY LEAKING. REPLACED BUTTON ASSY, LEFT PRESSURE AND CASE DRAIN FILTERS. NO CONTAMINATION FOUND, LEAK CKS OK (P/N 291201356). 2 L 7 2 4F RT A2NM 1996120500097 19961205 00097 WP 1996 12 5 SCNA96388 1 19961124 A 3350 EMBS1392T POWER SUPPLY DOUG DC10 DC1010 3022110 WP CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 571SC 46645 THE OVERWING EMERGENCY LIGHT POWER SUPPLY FAILED TO TEST. REMOVED AND REPLACED POWER SUPPLY AND OPS CHECKED NORMAL. 2 L 7 3 4F A22WE 1996120500098 19961205 00098 NM 1996 12 5 SCNA96389 1 19961126 A 3350 1102833 LIGHT BOEING 727 727282 138408T NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 281SC 21949 FOUND AFT SELF CONTAINED EMERGENCY LIGHT BATTERIES DISCHARGED AND LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT. 2 L 7 3 4F RT A3WE 1996120500099 19961205 00099 WP 1996 12 5 SCNA96390 1 19961107 A 3211 ARG7040529 BUSHING DOUG DC10 DC1010 3022110 WP RT MLG CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 572SC 46977 DURING HEAVY MAINTENANCE, FOUND RIGHT HAND MAIN LANDING GEAR FORWARD TRUNNION GEAR LUG INNER BUSHINGS PITTED. REMOVED R IGHT HAND MAIN LANDING GEAR FORWARD TRUNNION GEAR LUG INNER BUSHINGS. INSPECTED BORE AND FOUND TO BE WITHIN ORIGINAL HO LE SIZE LIMITS AND INSTALLED NEW BUSHINGS PER CMM 32-11-04. 2 L 7 3 4F A22WE 1996120500100 19961205 00100 WP 1996 12 5 SCNA96391 1 19961117 A 5230 SPOOL BOLT DOUG DC10 DC1010 3022110 WP CARGO DOOR CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 572SC 46977 DURING HEAVY MAINTENANCE, FOUND CENTER PIT AFT LATCH SPOOL MOUNT HAS CORROSION AT SPOOL MOUNT BOLT INNER SURFACE. REMOV ED CORROSION BY OVERSIZING HOLES TO 1.089 DIAMETER. FABRICATED SLEEVE FROM 17-4 AND CADMIUM PLATED IN ACCORDANCE WITH S RM 52-10-00, FIGURE 9. 2 L 7 3 4F A22WE 1996120500101 19961205 00101 WP 1996 12 5 SCNA96392 1 19961113 A 5320 PRESSURE WEB DOUG DC10 DC1010 3022110 WP BS 1156 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 572SC 46977 DURING HEAVY MAINTENANCE, FOUND A 19 INCH CRACK IN THE LOWER FORWARD PRESSURE BARREL OF THE CENTER ACCESSORY COMPARTMENT BAY AT BS 1156. THE CRACK PROTRUDES 5.25 INCHES UP FROM A LIGHTENING HOLE AND 13.7 INCHES DOWNWARD FROM LIGHTENING HOL E TO THE 11TH TOP FASTENER IN THE PRESSURE WEB. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLERS IN ACCORDA NCE WITH SRM 53-40-00. 2 L 7 3 4F A22WE 1996120500102 19961205 00102 WP 1996 12 5 SCNA96393 1 19961119 A 5320 WEB DOUG DC10 DC1010 3022110 WP BS 1780 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 572SC 46977 DURING HEAVY MAINTENANCE, FOUND THE LOAD BAR TRACK WEB CRACKED AT BS 1780. STOP DRILLED CRACK, FABRICATED AND INSTALLED A DOUBLER IN ACCORDANCE WITH SRM 53-00-01 FIGURE 4 SHEET 2. 2 L 7 3 4F A22WE 1996120500103 19961205 00103 WP 1996 12 5 SCNA96394 1 19961116 A 5753 WEDGE DOUG DC10 DC1010 3022110 WP RT TE FLAP DELAMINATED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 572SC 46977 DURING HEAVY MAINTENANCE, FOUND RIGHT INBOARD FLAP TRAILING EDGE WEDGE DELAMINATED. REMOVED PREVIOUS REPAIR AND REPLACE D WITH A NEW REPAIR IN ACCORDANCE WITH SRM 57-20-00 PARAGRAPH 2 A (1) (5) USING 151 CLOTH AND ADHESIVE 50A. 2 L 7 3 4F A22WE 1996120500104 19961205 00104 WP 1996 12 5 SCNA96395 1 19961119 A 5320 SHEAR TIE DOUG DC10 DC1010 3022110 WP BS 1039 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 572SC 46977 DURING HEAVY MAINTENANCE, FOUND SHEAR TIES LEGS CORRODED AT LONGERON 52, BS 1039. REMOVED CORRODED SHEAR TIES, CLEANED SKIN, FABRICATED AND INSTALLED NEW SHEAR TIES IN ACCORDANCE WITH SRM 53-15-01. 2 L 7 3 4F A22WE 1996120500105 19961205 00105 NE 1996 12 5 DHL96707004 2 19961121 A 7220 65196842 INLET BULLET BOEING 727 72722 1384002 NM PWA JT8 JT8D7B 52053 NE NR 3 ENGINE MALFUNCTIONED A DHLA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 01 707DH 18321 18321 REJECTED TO NR 3 ENGINE, NOT MAKING TARGET EPR WITH ENGINE A/I ON. PARAMETERS ON ENGINE NR 1 WERE EPR 2.00 NI 96 PERCEN T EGT 520 N2 93.5 F/F 9,500. ENGINE NR 3 PARAMETER WERE EPR 1.86 WITH A/I OFF NR 1 AND NR 3 ENGINE NORMAL. REMOVED AND REPLACED NR 3 ENGINE INLET BULLETT, GROUND RUN OK. 2 L 7 3 4F 4 F A3WE E2EA 1996120500106 19961205 00106 NM 1996 12 5 P5CA9600967 1 19961123 A 5730 PANEL BOEING 747 747122 1384872 NM LT WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 A 4 INCH CRACK IN LEFT WING LOWER PANEL FORWARD OF WING LANDING GEAR DOOR CUTOUT. REPAIRED PER BOEING SRM 51-40-06. 2 L 7 4 4F A20WE 1996120500107 19961205 00107 NM 1996 12 5 P5CA9600968 1 19961122 A 5400 FAIRING BOEING 747 747132 1384882 NM NR 4 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACKED AND BENT NR 4 ENGINE FORWARD FAIRING RIGHT HAND FORWARD CORNER. REPAIRED PER BOEING SRM 51-40-02. 2 L 7 4 4F A20WE 1996120500108 19961205 00108 NM 1996 12 5 P5CA9600970 1 19961123 A 5753 65B019837 BRACKET BOEING 747 747123 1384873 NM LT TE FLAP BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 ON ARRIVAL AND WALK AROUND, FOUND NR 1 FLAP INBOARD CANOE LOOSE AND HANGING DOWN. REMOVED CANOE AND DISPATCHED AIRCRAFT PER CDL 27-51. REPLACED FITTING AT JFK PER BOEING MAINTENANCE MANUAL 27-52-06 ANF 27-51-31. 2 L 7 4 4F A20WE 1996120500109 19961205 00109 NM 1996 12 5 P5CA9600971 1 19961127 A 5730 PANEL BOEING 747 747122 1384872 NM RT WING CREASED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 RIGHT UNDERWING FIBERGLASS PANEL AFT OF OUTBOARD LANDING LIGHT HAS A CREASE APPROXIMATELY 4 INCHES LONG BY .25 INCH DEEP WING STATION 294.600. REPAIRED PER BOEING SRM 51-40-07. 2 L 7 4 4F A20WE 1996120500110 19961205 00110 NE 1996 12 5 P5CA9600972 2 19961126 A 7320 PT2 SENSOR BOEING 747 747132 1384882 NM PWA JT9 JT9D7A 52054 NE NR 4 ENGINE CONTAMINATED A P5CA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 23 856FT 19897 662570 NR 4 ENGINE HAD NO THRUST LEVER RESPONSE WHEN AIRCRAFT READY FOR TAKEOFF. CHECKED ENGINE CONTROL LINKAGE, ALL CHECKED G OOD. CHECKED PS4 LINE CHECKS GOOD. CHECKED PT2 SENSOR AND LINE CHECKED GOOD. APPLIED HEAT PER MAINTENANCE MANUAL 71-0 0-00 PAGE 262, RAN ENGINE AND LEAK CHECK AND RUN UP ALL CHECKED GOOD PER MAINTENANCE MANUAL 71-00-00. SUSPECT DE-ICING FLUID GOT INTO PT2 SENSOR. 2 L 7 4 4F 4 F A20WE E20EA 1996120500111 19961205 00111 SO 1996 12 5 SRAA961117 1 19961125 A 3246 WHEEL LKHEED 382 382G 526414U SO LT MLG FAILED A A SRAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 905SJ 4472 DURING TAXI OUT, THE LEFT FRONT MAIN WHEEL BLEW DUE TO FLANGE SEPARATION. AIRCRAFT RETURNED TO BLOCK. FOUND LEFT MLG O UTER DOOR DAMAGED, VERIFIED WHEEL FAILURE. REMOVED AND REPLACED LEFT FWD MAIN WHEEL ASSY. REMOVED LT MLG OUTER AND INN ER DOOR PER AFM 1 TO 16. INSPECTED AIRCRAFT AND NO OTHER DAMAGE NOTED. 2 H 7 4 4T A1SO 1996120500112 19961205 00112 SO 1996 12 5 SRAA1066 1 19961013 A 5320 SUPPORT BEAM LKHEED 382 382G 526414U SO BS 497 CORROSION A SRAA K NONE O OTHER IN INSP/MAINT 1 GL 23 905SJ 45318 4472 DURING C-CHECK, FOUND CARGO COMPARTMENT FLOOR PANEL SUPPORT BEAM AT FS.497, LBL 40 AND 20 HAS CORROSION AT FORWARD AND A FT SIDE BEYOND LIMITS. CUT OUT CORRODED SECTION, FABRICATED AND INSTALLED SECTION UPPER CAP, 2 L-ANGLES, STRAPS AND FI LLER IAW LAC SRM CHAPTER 51-140-22. 2 H 7 4 4T A1SO 1996120500121 19961205 00121 NE 1996 12 5 M3HA96030 3 19961015 A 6114 8022631 SEALS AEROSP ATR42 ATR42300 8680920 EU HAMSTD 14SF 14SF5 NE PROP HUB BROKEN A M3HA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 13 4211G 178 HNL - WHEN SETTING TAKEOFF POWER, PILOT NOTED AND FELT 3 TORQUE FLUCTUATIONS FROM 80 PERCENT TORQUE TO 90 PERCENT TORQUE . (TEN PERCENT TORQUE FLUCTUATION) ON NR 1 ENGINE. REMOVED AND INSTALLED SERVICEABLE 'L' SEALS ON TRANSFER TUBE AND RE INDEXED PROPELLER BLADES. A/C RIGGING CHECK GOOD. (X) 2 H 7 2 4T RT A53EU 6 C P7NE 1996120500122 19961205 00122 WP 1996 12 5 96ZZZX5795 1 19960925 A 3231 S10361 LINK ROD DOUG DC8 DC8F54 3021926 WP NLG DOOR WORN A FXLA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 19 54FA 45637 AFTER TAKEOFF MIAMI AND GEAR RETRACTION, EXPERIENCED VIBRATION IN NOSE GEAR AREA. RETURNED TO MIA. MADE LANDING WITHOU T INCIDENT. INSPECTION REVEALED LEFT NOSE LANDING GEAR DOOR OPEN AND FORWARD DOOR LINK STRUT WOULD NOT LOCK DOOR IN UP POSITION. REPLACED LINK AND RETURNED AIRCRAFT TO SERVICE. 2 L 7 4 4F 4A25 1996120500124 19961205 00124 WP 1996 12 5 AALA961436 1 19960926 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 460 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 479AA 49654 TUL - LIGHTNING STRIKE IN FUSELAGE SKIN STILL INDICATING CRACK. INSTALLED DOUBLER PER SRM 53-04, FIG 38. TST: 23,322. 43 HRS. CYCLES, 13,207. ( X) 2 L 7 2 4F A6WE 1996120500125 19961205 00125 NM 1996 12 5 GAIA9631 1 19961113 A 3350 1000679 LIGHT ASSY BOEING 727 727223 1384074 NM L1 DOOR INOPERATIVE A GAIA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 07 6833 20186 EMERGENCY LIGHT AT MAIN ENTRY DOOR WILL NOT ARM WITH SWITCH ON. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY. (X) 2 L 7 3 4F A3WE 1996120500126 19961205 00126 EU 1996 12 5 SIMA963111 1 19961106 A 3350 3011180 POWER PACK AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 12MQ 1316 012 ORD - FLT 4005 - FORWARD STRIP OF EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY 29WL. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1996120500127 19961205 00127 WP 1996 12 5 96NK214 1 19961031 A 5610 WINDOW DOUG DC9 DC932 3022066 WP CAPT DELAMINATED A GTIA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 23 12536 47113 LOG PAGE NR 028273, ITEM NR P782. CLIMBING THROUGH 10,000 FEET, HEARD LOUD BANG. RT DV WINDOW APPEARED TO DELAMINATE A T FWD EDGE. RETURNED TO DTW. INSP F/O'S (CAPT) CLEARVIEW WINDOW AND FOUND ROUGH EDGE DELAMINATED ON FWD EDGE OF WINDOW , NO CORRECTIVE ACTION REQUIRED IAW DC-9 MM CH 56-00-0, CODE 1. CHECKED EXTERIOR OF AIRCRAFT AROUND SURROUNDING AREAS, NO DEFECTS FOUND. CLEARVIEW WINDOW LOCKING, LATCHING MECHANISM OPERATES NORMALLY, NO DEFECTS FOUND. (X) 2 L 7 2 4F A6WE 1996120500128 19961205 00128 WP 1996 12 5 96NK215 1 19961106 A 3350 1001191 LIGHT ASSY DOUG DC9 DC932 3022066 WP FWD ENTRY INOP A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 947ML 47514 LOG PAGE 027664. FWD ENTRY DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY. OPS NORMA L IAW MM 33-53. (X) 2 L 7 2 4F A6WE 1996120500129 19961205 00129 WP 1996 12 5 96ZZZX5797 1 19961029 A 2782 391357 PDU MOTOR SUNDSTRANDEM 672164115 LKHEED 1011 10113851 5265010 WP WBL 116.48 SLAT CRACKED A WRNA H O DEACTIVATE SYST/CIRCUITS OTHER J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SO 05 311EA 137 193A1012 A-HYD RESERVOIR QTY LOW AND LOW QTY LIGHT ON. TURNED OFF HYD PUMP - LEAK STOPPED. AIRCRAFT LANDED NORMAL. FOUND SLAT A-SYS PDU HYD MOTOR HOUSING CRACKED. REMOVED AND REPLACED MOTOR IAW MM 27-80-10. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A23WE 1996120500130 19961205 00130 WP 1996 12 5 96ZZZX5798 1 19961030 A 2910 1551382105 LINE LKHEED 1011 10113851 5265010 WP NR 1 PYLON HYD CRACKED A WRNA H O DEACTIVATE SYST/CIRCUITS OTHER K FLUID LOSS CR CRUISE 1 SO 05 311EA 193A1012 A-HYD SYS RAPIDLY DEPLETED AT 33,000 FEET. SYS SHUTDOWN IAW FLIGHT MANUAL. AIRCRAFT LANDED NORMALLY. FOUND HYD LINE I N NR 1 PYLON AREA LEAKING. REPAIRED LINE IAW REV MM ATA 20. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A23WE 1996120500131 19961205 00131 EU 1996 12 5 96ZZZX5799 1 19961029 A 3350 3011151 PACK BATTERY AEROSP ATR42 ATR42300 8680920 EU CABIN 29 WL DISCHARGED A M3HA K NONE O OTHER TX TAXI/GRND HDL 1 WP 13 4204G 243 10468 061 HNL - 2 FWD TRACK LIGHTS ARE OUT WITH A/C POWER OFF. REPLACED SERVICEABLE EMERGENCY BATTERY PACK AT 29 WL. 2 H 7 2 4T RT A53EU 1996120500132 19961205 00132 NM 1996 12 5 PCAA9600314 1 19960926 A 6120 7901802 PROP ACTUATOR DHAV DHC8 DHC8102 2809003 NM NR 2 ENGINE FAILED A PCAA E ENGINE SHUTDOWN J K WARNING INDICATION FLUID LOSS NR NOT REPORTED 1 EA 13 977HA 11373 2422 000881 220 NR 2 ENG OIL PRESSURE LOW, SHUT DOWN ENGINE IN FLIGHT. INSPECTED AND FOUND ENGINE PRESSURIZING PROPELLER HUB CAUSING LE AK OUT OF BLADE SEAL. REMOVED ACTUATOR, REPLACED SEALS, REPLACED ACTUATOR. REPLACED 4 BLADE SEALS. LOW OIL PRESSURE I NSPECTION PERFORMED IAW PWC MM. GROUND ENGINE RUN AND TEST FLIGHT PROVED SATISFACTORY. A/C RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A13NM 1996120500133 19961205 00133 NE 1996 12 5 PCAA9600313 2 19960926 A 7261 O-RING DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 PROP FAILED A PCAA E ENGINE SHUTDOWN J K WARNING INDICATION FLUID LOSS NR NOT REPORTED 1 EA 13 977HA 220 120053 NR 2 ENGINE OIL PRESS LOW, SHUT DOWN ENGINE IN FLIGHT. REMOVED PROPELLER, REPLACED O-RINGS ON TRANSFER TUBE AND PROPELL ER ASSEMBLY. REINSTALLED ASSEMBLY. COMPLETED INSPECTION FOR LOSS OF OIL PRESS IAW PWC MM. RAN AIRCRAFT AT ALL PARAMET ERS, NO LEAKS DETECTED. A/C RETURNED TO SERVICE. (X) 2 H 7 2 4T 4 T RT A13NM E20NE 1996120500135 19961205 00135 WP 1996 12 5 ZIAA961101 1 19961031 A 5751 2024T3AL SKIN DOUG DC8 DC862 3021970 WP RT OTBD AIL CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 66430 45922 MCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED RT OT BD AILERON LOWER SURFACE CORROSION. REPAIRED IAW DWG A74-R05. (X) 2 L 7 4 4F 4A25 1996120500136 19961205 00136 WP 1996 12 5 ZIAA961102 1 19961031 A 5311 2750825 FRAME DOUG DC8 DC862 3021970 WP FS 1080 35 L/R CORROSION A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 MCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED CORROS ION ON FUSELAGE FRAME FS 1080 35 L\R. REPAIRED IAW SRM 51-1-8; DWG A74-R27. (X) 2 L 7 4 4F 4A25 1996120500137 19961205 00137 WP 1996 12 5 ZIAA961103 1 19961031 A 5311 2537716 FRAME DOUG DC8 DC862 3021970 WP FS 1020 CL CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 MCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED CORROS ION ON FUSELAGE FRAME FS 1020 CL. REPAIRED IAW DWG A74-R03. (X) 2 L 7 4 4F 4A25 1996120500138 19961205 00138 WP 1996 12 5 ZIAA961104 1 19961031 A 5311 2537716 FRAME DOUG DC8 DC862 3021970 WP FS 1100 35/36 CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 MCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVALED CORROSI ON ON FUSELAGE FRAME FS 1100 35/36. REPAIRED IAW A74-404. (X) 2 L 7 4 4F 4A25 1996120500139 19961205 00139 WP 1996 12 5 ZIAA961105 1 19961031 A 5313 2750826 LONGERON DOUG DC8 DC862 3021970 WP FS 1090 CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 MCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED LONGER ON CRACKED. FS 1090 L35R. REPAIRED IAW DWG A74-R35. (X) 2 L 7 4 4F 4A25 1996120500140 19961205 00140 WP 1996 12 5 ZIAA961106 1 19961031 A 5313 2750826 LONGERON DOUG DC8 DC862 3021970 WP FS 1190 34R CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 MCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED LONGER ON CRACKED. FS 1190 34R. REPAIRED IAW DWG A74-R35. (X) 2 L 7 4 4F 4A25 1996120500141 19961205 00141 WP 1996 12 5 ZIAA961107 1 19961031 A 5313 2750826 LONGERON DOUG DC8 DC862 3021970 WP FS 1190 36 CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 MCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED LONGER ON CRACKED. FS 1190 36. REPAIRED IAW DWG A74-R35. (X) 2 L 7 4 4F 4A25 1996120500142 19961205 00142 WP 1996 12 5 ZIAA961108 1 19961031 A 5314 SUPPORT DOUG DC8 DC862 3021970 WP KEEL FS 920 CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 MCH - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED FUSELA GE KEEL VERT SUPPORT CRACKED. REPAIRED IAW SRM 51-1-8 AND 51-1-120D. (X) 2 L 7 4 4F 4A25 1996120500143 19961205 00143 WP 1996 12 5 ZIAA961109 1 19961031 A 5315 2616243 FLOOR BEAM DOUG DC8 DC862 3021970 WP FS 880 BL 60L CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 MCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED FUSELA GE FLOOR BEAM CRACKED. REPAIRED IAW DWG 174-R20. (X) 2 L 7 4 4F 4A25 1996120500144 19961205 00144 WP 1996 12 5 ZIAA961110 1 19961031 A 5320 FRAME DOUG DC8 DC862 3021970 WP LT WINDOW CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 MCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED LT WIN DOW FRAME CORRODED. FS 1320-1340. REPAIRED IAW DWG A74-R28; SRM 51-1-20D/-21. (X) 2 L 7 4 4F 4A25 1996120500145 19961205 00145 WP 1996 12 5 ZIAA961111 1 19961031 A 5320 WINDOW LAND DOUG DC8 DC862 3021970 WP LT WINDOW CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64403 45922 MCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED LT WIN DOW LAND CORRODED. FS 879-900. REPAIRED IAW DWG A74-R28; SRM 51-1-20D/-21. (X) 2 L 7 4 4F 4A25 1996120500146 19961205 00146 WP 1996 12 5 ZIAA961112 1 19961031 A 5320 FRAME DOUG DC8 DC862 3021970 WP RT WINDOW CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 MCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED RT WIN DOW FRAME CORRODED. FS 1000-1020. REPAIRED IAW DWG A74-R28; SRM 51-1-20D-21. (X) 2 L 7 4 4F 4A25 1996120500147 19961205 00147 WP 1996 12 5 ZIAA961113 1 19961031 A 5320 FRAME DOUG DC8 DC862 3021970 WP RT WINDOW CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 MCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED RT WIN DOW FRAME CORRODED. FS 1040-1060. REPAIRED IAW DWG A74-R28; SRM 51-1-20D-21. (X) 2 L 7 4 4F 4A25 1996120500148 19961205 00148 WP 1996 12 5 ZIAA961114 1 19961031 A 5320 FRAME DOUG DC8 DC862 3021970 WP RT WINDOW CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 MCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED RT WIN DOW FRAME CORRODED. FS 1240-1260. REPAIRED IAW DWG A74-R28; SRM 51-1-20D/21. (X) 2 L 7 4 4F 4A25 1996120500149 19961205 00149 WP 1996 12 5 ZIAA961115 1 19961031 A 5320 FRAME DOUG DC8 DC862 3021970 WP RT WINDOW CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 MCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED RT WIN DOW FRAME CORRODED. FS 1240-1260. REPAIRED IAW DWG A74-R28; SRM 51-1-20D/21. (X) 2 L 7 4 4F 4A25 1996120500150 19961205 00150 WP 1996 12 5 ZIAA961116 1 19961031 A 5330 SKIN DOUG DC8 DC862 3021970 WP FS 1085 33/35R CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 MCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED FUSEL AGE SKIN CORRODED FS 1085 33/35R. REPAIRED IAW SRM 51-1-20D/21. (X) 2 L 7 4 4F 4A25 1996120500151 19961205 00151 WP 1996 12 5 ZIAA961117 1 19961031 A 5330 SKIN DOUG DC8 DC862 3021970 WP FS 1190 33/35R CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 MCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED FUSELA GE SKIN CORRODED. FS 1190 33/35R. REPAIRED IAW SRM 51-1-20D/21. (X) 2 L 7 4 4F 4A25 1996120500152 19961205 00152 WP 1996 12 5 ZIAA961118 1 19961031 A 5330 2537717 SKIN DOUG DC8 DC862 3021970 WP FS 440-460 RT CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 MCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED FUSELA GE SKIN CORRODED. FS 440-460 RT. REPAIRED IAW DWG A74-R15. (X) 2 L 7 4 4F 4A25 1996120500153 19961205 00153 WP 1996 12 5 ZIAA961119 1 19961031 A 5512 SKIN DOUG DC8 DC862 3021970 WP HORZ STAB LT BULGING A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 MCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED HORIZ STAB LOWER SKIN LT AT 2ND ELEV HINGE CORRODED. REPAIRED IAW DWG A74-R32. (X) 2 L 7 4 4F 4A25 1996120500154 19961205 00154 WP 1996 12 5 ZIAA961120 1 19961031 A 5512 SKIN DOUG DC8 DC862 3021970 WP HORZ STAB LT BULGING A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 MCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED HORIZ STAB UPPER SKIN LT AT 2ND ELEV HINGE CORRODED. REPAIRED IAW DWG A74-R32. (X) 2 L 7 4 4F 4A25 1996120500155 19961205 00155 WP 1996 12 5 ZIAA961121 1 19961031 A 5521 FLANGE DOUG DC8 DC862 3021970 WP RT ELEV CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 MCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED RT ELE V LOWER AFT FLANGE CORRODED. REPAIRED IAW DWG A74-426; SRM 51-1-21. (X) 2 L 7 4 4F 4A25 1996120500156 19961205 00156 WP 1996 12 5 ZIAA961122 1 19961031 A 5532 SKIN DOUG DC8 DC862 3021970 WP ZR45 CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 MCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED VERT S TAB LT SKIN CORRODED. ZR45. REPAIRED IAW DWG A74-R29; SRM 51-1-8. (X) 2 L 7 4 4F 4A25 1996120500157 19961205 00157 WP 1996 12 5 ZIAA961123 1 19961031 A 5542 SKIN DOUG DC8 DC862 3021970 WP RUD LWR WELL DAMAGED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 64430 45922 MCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED RUDDER STRUCTURE LT SKIN LWR WELL DAMAGED. REPAIRED IAW DWG A74-R25. (X) 2 L 7 4 4F 4A25 1996120500158 19961205 00158 WP 1996 12 5 ZIAA961124 1 19961031 A 5720 ANGLE DOUG DC8 DC862 3021970 WP XW428 CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 MCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED WING S TRUCTURE L-ANGLE XW428 CORRODED. REPAIRED IAW DWG A74-R23. (X) 2 L 7 4 4F 4A25 1996120500159 19961205 00159 WP 1996 12 5 ZIAA61125 1 19961031 A 5730 SKIN DOUG DC8 DC862 3021970 WP XRS162-263 CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 MCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED WING S TRUCTURE UPPER SKIN XRS612-263 CRACKED. (X) 2 L 7 4 4F 4A25 1996120500160 19961205 00160 WP 1996 12 5 ZIAA961126 1 19961031 A 5730 SKIN DOUG DC8 DC862 3021970 WP LT XWR85-XFS566 CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 MCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED WING S TRUCTURE UPPER SKIN LT XW485-XFS 566 CORRODED. REPAIRED IAW DWG A74-R22. (X) 2 L 7 4 4F 4A25 1996120500161 19961205 00161 WP 1996 12 5 ZIAA961127 1 19961031 A 5720 FLANGE DOUG DC8 DC862 3021970 WP LT XFS 525-560 CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 MCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED WING S TRUCTURE LT FLANGE, LT XFS 525-560 CORRODED. REPAIRED IAW DWG A74-R24. (X) 2 L 7 4 4F 4A25 1996120500162 19961205 00162 WP 1996 12 5 ZIAA961128 1 19961031 A 5730 SKIN DOUG DC8 DC862 3021970 WP LE RT XFS 260 CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 MCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED WING S TRUCTURE SKIN LE RT CTR RT XFS 260 CORRODED. REPAIRED IAW DWG A74-R38. (X) 2 L 7 4 4F 4A25 1996120500163 19961205 00163 WP 1996 12 5 ZIAA961129 1 19961031 A 5730 SKIN DOUG DC8 DC862 3021970 WP RT XFS 139 CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 MCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED WING S TRUCTURE LE UPPER SKIN RT XFS 139 CORRODED. REPAIRED IAW DWG A74-R30. (X) 2 L 7 4 4F 4A25 1996120500164 19961205 00164 WP 1996 12 5 ZIAA961130 1 19961031 A 5730 SKIN DOUG DC8 DC862 3021970 WP RT XFS 172-292 CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 MCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED WING S TRUCTURE LE UPPER SKIN RT XFS 172-292 CORRODED. REPAIRED IAW DWG A74-R31. (X) 2 L 7 4 4F 4A25 1996120500165 19961205 00165 WP 1996 12 5 ZIAA961131 1 19961031 A 5730 SKIN DOUG DC8 DC862 3021970 WP RT XFS 164-207 CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 MCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED WING S TRUCTURE LE UPPER SKIN XFS 164-207 CORRODED. REPAIRED IAW DWG A74-R19; SRM 51-1-8. (X) 2 L 7 4 4F 4A25 1996120500166 19961205 00166 WP 1996 12 5 ZIAA961132 1 19961031 A 5730 SKIN DOUG DC8 DC862 3021970 WP LT XFS 566-603 CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 MCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED WING S TRUCTURE LE LOWER SKIN LT XFS 566-603 CORRODED. REPAIRED IAW DWG A74-R08/R09. (X) 2 L 7 4 4F 4A25 1996120500167 19961205 00167 WP 1996 12 5 ZIAA961133 1 19961031 A 5730 SKIN DOUG DC8 DC862 3021970 WP LT XFS 710-746 CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 MCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED WING S TRUCTURE LE UPPER SKIN LT XFS 710-746 CORRODED. REPAIRED IAW DWG A74-R18. (X) 2 L 7 4 4F 4A25 1996120500168 19961205 00168 WP 1996 12 5 ZIAA961134 1 19961031 A 5730 SKIN DOUG DC8 DC862 3021970 WP LT XFS 285-309 CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 MCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED WING S TRUCTURE LE UPPER SKIN LT XFS 285-309 CORRODED. REPAIRED IAW DWG A74-R07/R21. (X) 2 L 7 4 4F 4A25 1996120500169 19961205 00169 WP 1996 12 5 ZIAA961135 1 19961031 A 5730 SKIN DOUG DC8 DC862 3021970 WP LT XFS 560-575 CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 MCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED WING S TRUCTURE LE UPPER SKIN LT XFS 560-575 CORRODED. REPAIRED IAW DWG A74-R17; SRM 51-1-8. (X) 2 L 7 4 4F 4A25 1996120500170 19961205 00170 WP 1996 12 5 ZIAA961136 1 19961031 A 5720 HOIST POINT DOUG DC8 DC862 3021970 WP LT WS672-720-803 CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 MCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED WING S TRUCTURE LE HOIST POINT LT WS 672-720-803 CORRODED. REPAIRED IAW DWG A74-R06. (X) 2 L 7 4 4F 4A25 1996120500171 19961205 00171 WP 1996 12 5 ZIAA961137 1 19961031 A 7810 57505151 NOZZLE DOUG DC8 DC862 3021970 WP NR 2 OUT OF ROUND A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 MCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED NR 2 N OZZLE OUT OF ROUND, 10-12 O'CLOCK. REPAIRED IAW DWG A74-R01. (X) 2 L 7 4 4F 4A25 1996120500172 19961205 00172 WP 1996 12 5 ZIAA961138 1 19961031 A 7810 57505151 NOZZLE DOUG DC8 DC862 3021970 WP NR 4 CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 MCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED NR 4 N OZZLE CRACKED, 6 O'CLOCK. REPAIRED IAW DWG A74-R11. (X) 2 L 7 4 4F 4A25 1996120500173 19961205 00173 SW 1996 12 5 HEEA968481 1 19961118 A 6220 412010427101 BEARING 412010405109 BELL 412 412 1182202 SW M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911AR 493 A842 33111 BEARING WORN BEYOND LIMITS PER MANUFACTURER. PARTS SCRAPPED LOCALLY. 1 G 7 2 4U H4SW 1996120500174 19961205 00174 SW 1996 12 5 HEEA968482 1 19961118 A 6220 412010427101 BEARING 412010405109 BELL 412 412 1182202 SW M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911AR 493 A950 33111 BEARING WORN BEYOND LIMITS PER MANUFACTURER. PARTS SCRAPPED LOCALLY. 1 G 7 2 4U H4SW 1996120500175 19961205 00175 SW 1996 12 5 HEEA968483 1 19961118 A 6220 412010427101 BEARING 412010405109 BELL 412 412 1182202 SW M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911FD 161 A783 33056 BEARING WORN BEYOND LIMITS PER MANUFACTURER. PARTS SCRAPPED LOCALLY. 1 G 7 2 4U H4SW 1996120500176 19961205 00176 SW 1996 12 5 HEEA968484 1 19961118 A 6220 412010427101 BEARING 412010405109 BELL 412 412 1182202 SW M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911FD 1101 A40 33056 BEARING WORN BEYOND LIMITS PER MANUFACTURER. PARTS SCRAPPED LOCALLY. 1 G 7 2 4U H4SW 1996120500177 19961205 00177 SW 1996 12 5 HEEA968485 1 19961118 A 6220 206011147005 STRAP 206011100021 BELL 206 206B3 1181506 SW M/R REQ REPLACEMENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 103PH 191 A101522 3000 STRAP S/N BTFS-17845 AND S/N BTFS-17803 WERE REMOVED DUE TO 2 YEAR RETIREMENT AS PER AD 78-11-02R1. REPLACED WITH -007 STRAPS. 1 G 7 1 3U H2SW 1996120500178 19961205 00178 1996 12 5 HEEA968487 4 19961118 A 3421 200DCL28 GYRO BELL 407 407 SW COCKPIT VG PRECESSES E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407PH 516 53003 GYRO UNIT PRECESSING EXCESSIVELY. 1 G 7 1 3U O H2SW 1996120500179 19961205 00179 SW 1996 12 5 HEEA968488 1 19961118 A 2435 214060056103 STARTER BELL 214 214ST 1182106 SW START/GEN SLIPPING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 523 28106 STARTER CLUTCH HAS EXCESSIVE SLIPPAGE TORQUE (OVER 375 IN. LBS) AND EXCESSIVE END PLAY (OVER .010) 2 G 7 2 4U H10SW 1996120500180 19961205 00180 NE 1996 12 5 HEEA968489 1 19961120 A 6320 7635109011106 BEVEL GEAR 763510950004 SKRSKY S76 S76A 8143006 NE M/R GR BOX EXCESS WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31219 8129 A08100286 760230 EXCESSIVE WEAR ON CONVEX SIDE OF GEAR TEETH. REPLACED WITH SERVICEABLE PART. SEE MMIR# HEEA0008490 FOR PINION ALSO REPL ACED. 1 G 7 2 3U H1NE 1996120500181 19961205 00181 NE 1996 12 5 HEEA968490 1 19961120 A 6320 7635109132102 PINION 763510950004 SKRSKY S76 S76A 8143006 NE M/R GR BOX EXCESS WEAR E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31219 A08100286 760230 EXCESSIVE WEAR ON CONVEX SIDE OF GEAR TEETH. REPLACED WITH SERVICEABLE PART. SEE MMIR# HEEA0008489 FOR PINION ALSO REPL ACED. 1 G 7 2 3U H1NE 1996120500182 19961205 00182 EU 1996 12 5 HEEA968491 1 19961120 A 6310 4638202007 CLUTCH 4638001001 BOLKMS 105 BO105S 5626006 EU FREEWHEEL WORN EXCESSIVELY E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 624MB 1883 306 S751 INNER CAGE WORN BEYOND LIMITS AT 600 HOUR INSPECTION. REPLACED WITH SERVICEABLE CLUTCH ASSEMBLY. 1 G 7 2 3U H3EU 1996120500183 19961205 00183 1996 12 5 HEEA968492 4 19961120 A 2312 064100900 TRANSCEIVER KTR905 SKRSKY S76 S76A 8143006 NE COCKPIT VHF MALFUNCTION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1546G 760076 INTERMITTENTLY INOPERATIVE. RECEIVERS HAVE POPPING NOISE. 1 G 7 2 3U H1NE 1996120500184 19961205 00184 1996 12 5 HEEA968493 4 19961120 A 3457 0110005400 GPS 150 GARMIN BELL 206 206L3 1182108 SW COCKPIT GPS DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 363BH 51345 TAKES 45 MINUTES BEFORE GPS IS WORKING. SENT TO GARMIN INTERNATIONAL FOR INSPECTION AND REPAIR. 1 G 7 1 3U H2SW 1996120500185 19961205 00185 SW 1996 12 5 HEEA968495 1 19961120 A 6240 206075545005 SENSOR BELL 206 206L1 1182107 SW ROTOR RPM DEFECTIVE E HEEA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SW 03 5742H 45476 SENSOR DEFECTIVE. LOW ROTOR LIGHT WILL NOT COME ON. REPLACED WITH SERVICEABLE SENSOR. 1 G 7 1 3U H2SW 1996120500186 19961205 00186 SW 1996 12 5 HEEA968496 1 19961120 A 5321 412030324101 PANEL BELL 412 412 1182202 SW FLOOR RT SEPARATION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3911L 33023 LOWER SIDE OF PANEL HAS SEPARATED COVERS FOR TIE DOWN RING AND SEPARATION ON SLANTED PROTECTIVE COVER OF PANEL. 1 G 7 2 4U H4SW 1996120500187 19961205 00187 SW 1996 12 5 HEEA968497 1 19961120 A 5320 212030010123A PANEL BELL 412 412 1182202 SW ROOF MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 3911L 33023 PANEL DOES NOT FIT AIRFRAME DUE TO HAVING THE WRONG CONTOUR. IT SHOULD HAVE A CONVEX CURVE SHAPE WHEN LOOKING FROM TOP VIEW. 1 G 7 2 4U H4SW 1996120500188 19961205 00188 1996 12 5 HEEA968498 4 19961121 A 2370 9806019001 CVR SKRSKY S76 S76A 8143006 NE COCKPIT WONT TEST E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 1545X 3409 760050 CVR WILL NOT TEST PROPERLY. 1 G 7 2 3U H1NE 1996120500189 19961205 00189 1996 12 5 HEEA968499 4 19961121 A 2312 064105430 TRANSCEIVER BELL 206 206L3 1182108 SW COCKPIT VHF INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3107N 51512 RADIO INOPERATIVE. POWER APPLIED TO THE WRONG CONTACTS, LOUD POPPING SOUND HEARD. 1 G 7 1 3U H2SW 1996120500190 19961205 00190 SW 1996 12 5 HEEA968500 1 19961121 A 5260 FYLM735023 MOTOR ASSY SYLC502281 BELL 412 412 1182202 SW STEP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893P 003 33012 STEP WILL NOT RAISE OR LOWER. THIS UNIT WAS DISASSEMBLED AND INSPECTED BY THE ACCESSORY SHOP. A BURNT SPOT ON THE ARMA TURE WAS FOUND TO BE THE PROBLEM. MOTOR AS REPAIRED ON 7-31-96 UNDER NO. MGR. 91072. INSTALLED IN ACTUATOR S/N 003 ON 8-7-96. 1 G 7 2 4U H4SW 1996120500191 19961205 00191 1996 12 5 HEEA968501 4 19961121 A 3454 066303800 RMI KING KI229 BOLKMS 105 BO105S 5626006 EU COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 818SH S753 COMPASS CARD WON'T TURN AND VOR NEEDLE INTERMITTENT. 1 G 7 2 3U H3EU 1996120500192 19961205 00192 1996 12 5 HEEA968502 4 19961121 A 3453 27010045 ANTENNA BELL 412 412 1182202 SW LORAN ANTENNA DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22608 33075 TROUBLESHOOTING LORAN ADVISORY LIGHT STAYING ON. 1 G 7 2 4U H4SW 1996120500193 19961205 00193 EU 1996 12 5 HEEA968503 1 19961121 A 6310 4638202007 CLUTCH BOLKMS 105 BO105S 5626006 EU FREEWHEEL RUST E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 FREEWHEEL CLUTCH HAS RUST ON SPRAGS. 1 G 7 2 3U H3EU 1996120500194 19961205 00194 SW 1996 12 5 HEEA968504 1 19961121 A 3213 206327002 SKID TUBE BELL 206 206B3 1181506 SW SADDLE MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 39122 3312 BOLT HOLE IN TOP OF AFT SKID TUBE SADDLE, WAS NOT LINED UP, WOULD NOT MATCH WITH CROSS TUBE MOUNT HOLE. 1 G 7 1 3U H2SW 1996120500195 19961205 00195 EU 1996 12 5 HEEA968506 1 19961121 A 6520 4619210902 GEAR SPLINES 4619002003 BOLKMS 105 BO105S 5626006 EU T/R GEARBOX WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3534T 340 S112 BEVEL GEAR INTERNAL SPLINES WORN. (PINION S/N 879 - BEVEL GEAR S/N 770) REPLACED WITH SERVICEABLE GEARSET. 1 G 7 2 3U H3EU 1996120500196 19961205 00196 EU 1996 12 5 HEEA968507 1 19961121 A 6520 4619210902 BEVEL GEAR SET 4619002003 BOLKMS 105 BO105S 5626006 EU T/R GR BOX TEETH WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911BR 3626 1083 S719 GEAR TEETH WEARING AND PITTING. INTERNAL SPLINES WORN. REPLACED WITH SERVICEABLE GEARSET. 1 G 7 2 3U H3EU 1996120500197 19961205 00197 1996 12 5 HEEA968508 4 19961121 A 3455 066107700 RECEIVER BELL 412 412 1182202 SW COCKPIT ADF INTERMITTENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 21498 36003 RECEIVER INTERMITTENT. PERFORMED PRELIMINARY INSPECTION. FOUND EXCESSIVE CORROSION ON CONN. J8061, REPLACED CONN. J8061 . ONE EACH SPACER AND ONE EACH PLATE. ALSO REPLACED MISSING SCREW. REPAIRED, TESTED, ADJUSTED POT. R374 AND CLEANED H EADERS. BENCH CHECK GOOD. 1 G 7 2 4U H4SW 1996120500198 19961205 00198 SW 1996 12 5 HEEA968509 1 19961121 A 2435 214060056103 STARTER BELL 214 214ST 1182106 SW ENG FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5748M 523 28102 STARTER WON'T ENGAGE AND FINALLY INTERMITTENT OPERATION. 2 G 7 2 4U H10SW 1996120500199 19961205 00199 EU 1996 12 5 HEEA968510 1 19961121 A 6520 4619210902 BEVEL GEAR SET 4619002003 BOLKMS 105 BO105S 5626006 EU T/R GR BOX SCUFFED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 205UC 60 598 S668 BEVEL GEAR SET SCUFFED CAUSING METAL IN OIL. 1 G 7 2 3U H3EU 1996120500200 19961205 00200 EU 1996 12 5 HEEA968511 1 19961121 A 6210 10587214 BLADE BOLKMS 105 BO105S 5626006 EU M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3534T 7605 S112 BLADE IS CRACKED. (NOSE AND NECK SHELLS CRACKED AND SEPARATED) 1 G 7 2 3U H3EU 1996120500201 19961205 00201 EU 1996 12 5 HEEA968512 1 19961121 A 6210 10587214 BLADE BOLKMS 105 BO105S 5626006 EU M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3534T 7605 S112 BLADE IS CRACKED. (NOSE AND NECK SHELLS CRACKED AND SEPARATED) 1 G 7 2 3U H3EU 1996120500202 19961205 00202 EU 1996 12 5 HEEA968513 1 19961121 A 6210 10587214 BLADE BOLKMS 105 BO105S 5626006 EU M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3534T 7605 S112 BLADE IS CRACKED. (NOSE AND NECK SHELLS CRACKED AND SEPARATED) 1 G 7 2 3U H3EU 1996120500203 19961205 00203 EU 1996 12 5 HEEA968514 1 19961121 A 2844 642792002 TRANSMITTER SNIAS 350 AS350B2 8680813 EU FUEL SYS DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 350BZ 1783 2653 TRANSMITTER CAUSED FUEL PRESSURE INDICATOR TO PEG FULL SCALE WHEN BATTERY IS TURNED ON. 1 G 7 1 3U H9EU 1996120500204 19961205 00204 EU 1996 12 5 HEEA968515 1 19961121 A 2844 642792002 TRANSMITTER SNIAS 350 AS350B2 8680813 EU FUEL PRESS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 1710 2771 GAUGE NOT INDICATING PRESSURE WITH BOOST PUMPS ON. 1 G 7 1 3U H9EU 1996120500205 19961205 00205 EU 1996 12 5 HEEA968516 1 19961121 A 6210 10587214 BLADE BOLKMS 105 BO105S 5626006 EU M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3533T 9674 S111 BLADE IS CRACKED. (NOSE AND NECK SHELLS CRACKED AND SEPARATED) 1 G 7 2 3U H3EU 1996120500206 19961205 00206 EU 1996 12 5 HEEA968517 1 19961121 A 6210 10587214 BLADE BOLKMS 105 BO105S 5626006 EU M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3533T 9674 S111 BLADE IS CRACKED. (NOSE AND NECK SHELLS CRACKED AND SEPARATED) SENT TO COMPOSITE TECHNICS FOR INSPECTION AND REPAIR. 1 G 7 2 3U H3EU 1996120500207 19961205 00207 EU 1996 12 5 HEEA968518 1 19961121 A 6210 10587214 BLADE BOLKMS 105 BO105S 5626006 EU M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3534T 7605 S112 BLADE IS CRACKED. (NOSE AND NECK SHELLS CRACKED AND SEPARATED) 1 G 7 2 3U H3EU 1996120500208 19961205 00208 1996 12 5 HEEA968519 4 19961121 A 3454 066107800 RECEIVER SKRSKY S76 S76A 8143006 NE NAV COMM DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 15460 760223 DEVIATION BAR ABOUT 20 DEGREES OFF FROM SELECTED BEARING. 1 G 7 2 3U H1NE 1996120500209 19961205 00209 EU 1996 12 5 HEEA968520 1 19961121 A 6520 350A33200405 SPIDER SNIAS 350 AS350B2 8680813 EU T/R SEAL TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 1376 2771 T/R SPIDER SEAL TORN. 1 G 7 1 3U H9EU 1996120500210 19961205 00210 SW 1996 12 5 HEEA968521 1 19961121 A 6320 206040530001 CASE ASSY 206040004107 BELL 206 206L3 1182108 SW M/R FAULTY E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 3116P A17 51530 S/N ON MAIN CASE DOES NOT MATCH WITH S/N ON ACC. DRIVE HOUSING. MAIN CASE S/N A000180 AND ACC. DRIVE HOUSING S/N A100. 1 G 7 1 3U H2SW 1996120500211 19961205 00211 SW 1996 12 5 HEEA968522 1 19961121 A 5260 FYLM735023 MOTOR ASSY SYLC502281 BELL 412 412 1182202 SW STEP INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 108X 1018 33115 INOPERATIVE. THIS UNIT WAS DISASSEMBLED AND INSPECTED BY THE ACCESSORY SHOP. A BURNT SPOT ON THE ARMATURE WAS FOUND TO BE THE PROBLEM. S/N 2237 WAS REPAIRED BY BARBER COLMAN ON 4-24-96 UNDER NO. MGR 90342. INSTALLED IN ACTUATOR S/N 1018 ON 8-7-96. 1 G 7 2 4U H4SW 1996120500212 19961205 00212 SW 1996 12 5 HEEA968523 1 19961121 A 6210 412015300109 BLADE BELL 412 412 1182202 SW M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22608 4620 33075 BLADE IS CRACKED. (CRACK IN THE UPPER SKIN AT STATION 83.5" RUNNING IN A 45 DEGREE DIRECTION. 1 G 7 2 4U H4SW 1996120500213 19961205 00213 1996 12 5 HEEA968524 4 19961121 A 3416 5035P2P44 ALTIMETER SKRSKY S76 S76A 8143006 NE COCKPIT ENCODER NEEDLE ERROR E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546G 760076 ENCODE ALTIMETER NEEDLE HAS EXCESSIVE FRICTION ERROR. 1 G 7 2 3U H1NE 1996120500214 19961205 00214 NE 1996 12 5 HEEA968525 1 19961121 A 6410 7610105101041 BLADE SKRSKY S76 S76A 8143006 NE T/R SEPARATION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31217 11074 760229 PADDLE "B" OF THIS ASSEMBLY HAS SEPARATION ON THE EXTREME TRAILING EDGE PRIMARY RUBBER ERRODED THROUGH ON PADDLE "B". 1 G 7 2 3U H1NE 1996120500215 19961205 00215 GL 1996 12 5 HEEA968526 2 19961121 A 7314 3881005 PUMP BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL FUEL LEAKAGE E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 16938 10776 45157 PUMP EXCESSIVE DRAIN LEAKAGE. 1 G 7 1 3U 3 U H2SW E1GL 1996120500216 19961205 00216 1996 12 5 HEEA968527 4 19961121 A 3453 25410036 7000 RCU BELL 412 412 1182202 SW LORAN FAIL SELF TEST E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22608 33075 7000 RCU WILL NOT GO THROUGH SELF TEST. SHOWS OSCILLATOR ERROR. 1 G 7 2 4U H4SW 1996120500217 19961205 00217 1996 12 5 HEEA968528 4 19961121 A 3442 MI585202 ANT PEDESTAL BELL 212 212 1181420 SW RADAR DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3131S 30953 "ANT" LIGHT FLASHES ON INDICATOR AND WILL NOT PAINT TARGET. 1 G 7 1 4U H4SW 1996120500218 19961205 00218 1996 12 5 HEEA968530 4 19961121 A 3444 0710111400 ANTENNA KA131 BELL 206 206L3 1182108 SW RADAR ALTIMETER FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3107N 51512 RADAR ALTIMETER INOPERATIVE. NO ACCURACY, JUST FLUCTUATES. 1 G 7 1 3U H2SW 1996120500219 19961205 00219 1996 12 5 HEEA968531 4 19961121 A 3457 0110014700 ANTENNA GA56 BELL 206 206L3 1182108 SW COCKPIT GPS DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 108PH 51334 GPS CANNOT FIND SATELLITE AND ANT ATTACH FITTING IS LOOSE. 1 G 7 1 3U H2SW 1996120500220 19961205 00220 SW 1996 12 5 HEEA968532 1 19961121 A 5320 206032117069 PANEL ASSY BELL 206 206L1 1182107 SW CABIN MIS MFG E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3904L 45597 AFT EDGE OF PANEL WAS TRIMMED OFF OF NEW PANEL APPROXIMATELY 5/8". INSERT IN CORNER OF PANEL NOT IN CORRECT LOCATION. 1 G 7 1 3U H2SW 1996120500221 19961205 00221 SW 1996 12 5 HEEA968533 1 19961121 A 6710 206001191001 TUBE ASSY BELL 206 206L1 1182107 SW M/R CONTROL CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5007Q 45187 FOUR EACH CRACKS AT CLEVIS END OF TUBE APPROXIMATELY 1/2" TO 3/4" LONG. REPLACED WITH SERVICEABLE TUBE. 1 G 7 1 3U H2SW 1996120500222 19961205 00222 SW 1996 12 5 HEEA968534 1 19961121 A 6220 412010182101 BEARING BELL 412 412 1182202 SW M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 294 33113 SHOULDER ON ONE SIDE OF BEARING WORN EXCESSIVELY. REPLACED ROD END (AND PITCH HORN BUSHING). 1 G 7 2 4U H4SW 1996120500223 19961205 00223 SW 1996 12 5 HEEA968535 1 19961121 A 6220 412010182101 BEARING BELL 412 412 1182202 SW M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7128R 825 36007 SHOULDER ON ONE SIDE OF BEARING WORN EXCESSIVELY. REPLACED ROD END (AND PITCH HORN BUSHING). 1 G 7 2 4U H4SW 1996120500225 19961205 00225 GL 1996 12 5 HEEA968537 2 19961121 A 7250 23060450 NOZZLE 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL NR 1 VANE CRACKED E HEEA K NONE R PARTIAL RPM/PWR LOSS IN INSP/MAINT 1 SW 03 5421E 443 CAT38001F S806 CAE833901 ENGINE REMOVED DUE TO AFT T/M LEAKS. TURBINE DISASSEMBLED DUE TO LOW POWER ON TEST RUN. UPON INSPECTION OF TURBINE PAR TS NOTED THE FOLLOWING: CRACKED AND BOWED BEYOND SERVICEABLE LIMITS ON #1 NOZZLE VANES. INSTALLED A STANDARD AERO OVERH AULED #1 NOZZLE. 1 G 7 2 3U 3 U H3EU E4CE 1996120500226 19961205 00226 SW 1996 12 5 HEEA968538 1 19961121 A 7810 230063301102 EXHAUST STACK BELL 230 230 1182149 SW ENGINE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 3430 23009 EXHAUST DUCT CRACKED. 1 G 7 2 3U NC H9SW 1996120500227 19961205 00227 EU 1996 12 5 HEEA968539 1 19961122 A 6220 113944P BEARING 10531821 BOLKMS 105 BO105S 5626006 EU PC LINK FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 86CH NA S557 BEARING INNER RACE CAME COMPLETELY OUT OF BEARING. INSTALLED SERVICEABLE P/C LINK. ONE P/C LINK SCRAPPED CAUSED BY BEAR ING FAILURE. 1 G 7 2 3U H3EU 1996120500228 19961205 00228 EU 1996 12 5 HEEA968540 1 19961122 A 6710 10541506 CONTROL ROD BOLKMS 105 BO105S 5626006 EU M/R CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81832 S828 EXCESSIVE CORROSION ON CONTROL TUBE WHICH WAS COVERED BY HEAT SHRINK. SCRAPPED TUBE AND REPLACED WITH SERVICEABLE TUBE. 1 G 7 2 3U H3EU 1996120500229 19961205 00229 EU 1996 12 5 HEEA968541 1 19961122 A 7120 10560386 BUSHING BOLKMS 105 BO105S 5626006 EU ENG MOUNT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81832 S828 SEPARATION OF ELASTOMERIC FROM BUSHING ASSY. REMOVED AND REPLACED WITH SERVICEABLE BUSHING. 1 G 7 2 3U H3EU 1996120500230 19961205 00230 EU 1996 12 5 HEEA968542 1 19961122 A 3213 10550012 CROSS TUBE ASSY BOLKMS 105 BO105S 5626006 EU SKID SHOE CORROSION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7170D S840 CORROSION PITS BEYOND LIMITS WHERE SKID SHOE MOUNTS. REPLACED WITH SERVICEABLE CROSSTUBE. 1 G 7 2 3U H3EU 1996120500231 19961205 00231 EU 1996 12 5 HEEA968543 1 19961122 A 6710 10541488 CONTROL ROD BOLKMS 105 BO105S 5626006 EU M/R CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7170D S840 CORROSION BEYOND LIMITS ON COLLARS AND ON INTERIOR OF COLLARS. REPLACED WITH SERVICEABLE CONTROL TUBE. 1 G 7 2 3U H3EU 1996120500232 19961205 00232 1996 12 5 HEEA968544 4 19961122 A 3420 5050010902 GYRO 200 SNIAS 350 AS350B2 8680813 EU COCKPIT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 60951 2771 SPINS IN FLIGHT. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H9EU 1996120500233 19961205 00233 EU 1996 12 5 HEEA968545 1 19961122 A 7712 53516 TRANSMITTER SNIAS 350 AS350B2 8680813 EU ENG TORQUE DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 2771 TORQUE GAUGE READS 4% HIGH. REPLACED WITH SERVICEABLE TRANSMITTER. 1 G 7 1 3U H9EU 1996120500234 19961205 00234 EU 1996 12 5 HEEA968546 1 19961122 A 5210 350A2510842101 SLEEVE ASSY SNIAS 350 AS350B2 8680813 EU DOOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 2771 SLEEVE ASSY WORN. REPLACED WITH SERVICEABLE SLEEVE ASSEMBLY. 1 G 7 1 3U H9EU 1996120500235 19961205 00235 EU 1996 12 5 HEEA968547 1 19961122 A 6400 AUAS405058 SEAL LIP 350A33200402 SNIAS 350 AS350B2 8680813 EU T/R DETERIORATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100R NA 2862 RUBBER DETERIORATED. REPLACED WITH NEW SEAL. 1 G 7 1 3U H9EU 1996120500236 19961205 00236 EU 1996 12 5 HEEA968548 1 19961122 A 6420 350A33211905 BODY SNIAS 350 AS350B2 8680813 EU T/R BEARING FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 2771 BEARINGS SEPARATED. REPLACED WITH SERVICEABLE T/R YOKE ASSEMBLY. 1 G 7 1 3U H9EU 1996120500237 19961205 00237 NE 1996 12 5 HEEA968549 1 19961122 A 5551 7620904004043 FITTING SKRSKY S76 S76A 8143006 NE HORIZ STAB PITTED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22342 12094 760096 PART IS PITTED. (EXCESSIVE CORROSION PITTING IN RADIUS OF HORIZONTAL STABILIZER MATING SURFACE. DEEPEST PIT MEASURES . 039". REPLACED STABILIZER SUPPORT FITTING. 1 G 7 2 3U H1NE 1996120500238 19961205 00238 1996 12 5 HEEA968550 4 19961122 A 3453 453105004 SWITCH ARNAV BELL 412 412 1182202 SW LORAN STICKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 108X 33115 ENTER SWITCH STICKING. 1 G 7 2 4U H4SW 1996120500239 19961205 00239 SW 1996 12 5 HEEA968551 1 19961122 A 7714 212075037101 INDICATOR BELL 412 412 1182202 SW ENG N1 NEEDLE LOOSE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 NEEDLE IS LOOSE ON SHAFT. THIS UNIT WAS REPAIRED ON 8-1-96. 1 G 7 2 4U H4SW 1996120500240 19961205 00240 1996 12 5 HEEA968552 4 19961122 A 3450 066401018 RNAV BELL 214 214ST 1182106 SW COCKPIT MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5748M 28102 REMOTE RNAV ANNUCIATOR LIGHT ALWAYS ILLUMINATED WHEN UNIT IS TURNED ON. SENT TO THE RADIO SHOP FOR INSPECTION AND REPAIR . 2 G 7 2 4U H10SW 1996120500241 19961205 00241 NM 1996 12 5 CALA9601713 1 19961129 A 2910 654685860 HYD LINE BOEING 737 737130 1384435 NM NR 2 ENGINE LEAKING A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 59207 19024 THE AIRCRAFT LOST A-SYSTEM HYDRAULIC QUANTITY AND PRESSURE WHILE EN ROUTE. THE AIRCRAFT WAS DIVERTED TO GSO WHERE IT LA NDED WITHOUT INCIDENT. MAINTENANCE FOUND HYDRAULIC PRESSURE LINE ON TOP OF NR 2 ENGINE LEAKING. THE LINE WAS REPLACED USING A FLEX LINE AND A DIP WAS ISSUED TO REPLACE THE FLEX LINE WITHIN 1,200 HOURS OR 500 FLIGHTS. THE HYDRAULIC SYSTEM WAS SERVICED AND BLED, LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F A16WE 1996120500242 19961205 00242 NM 1996 12 5 CALA9601714 1 19961127 A 3397 WIRE BOEING 757 757224 1384958 NM CABIN BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 12109 27299 INSPECTION FOUND AISLE EMERGENCY LIGHTING INOPERATIVE FROM ROWS 15 ABC TO 25 ABC. MAINTENANCE FOUND A BROKEN WIRE. THE WIRE WAS REPAIRED AND THE LIGHTS WERE TESTED IAW MM 33-51-00, PAGES 501 AND 503. 2 L 7 2 4F RT A2NM 1996120500243 19961205 00243 NM 1996 12 5 CALA9601715 1 19961125 A 5330 SKIN BOEING 727 727232 1384082 NM BS 720 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A .75 INCH CRACK ON FUSELAGE SKIN LAP JOINT AT STA 720, STRINGER 26R. A REPAIR WAS FABRICATED AND INST ALLED IAW SRM 51-10-6 AND 53-30-3. 2 L 7 3 4F A3WE 1996120500244 19961205 00244 WP 1996 12 5 9625399860 1 19961126 A 2432 BATTERY CHARGER DOUG DC9 DC951 3022051 WP E/E COMPT FAILED A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 01 769NC 47757 AT GATE, PUSH BACK DRIVER INFORMED COCKPIT OF SMOKE COMING FROM NOSE WHEEL WELL E AND E COMPARTMENT. PASSENGERS DEPLANE D, FOUND BATTERIES AND CHARGER HOT TO TOUCH. REPLACED BATTERIES, CHARGER AND TEMP SENSOR AND OPERATION CHECKS GOOD. 2 L 7 2 4F A6WE 1996120500245 19961205 00245 NM 1996 12 5 9625402767 1 19961126 A 2130 56697 VALVE BOEING 727 7272M7 138407S NM E/E COMPT MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 727RW 16555 1057 26156 DURING CLIMB, COULD NOT CONTROL CABIN PRESSURIZATION. RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED EQUIPMENT COOLING AIR SHUTOFF VALVE. PERFORMED PRESSURIZATION CHECK, CHECKED OK. 2 L 7 3 4F A3WE 1996120500246 19961205 00246 NM 1996 12 5 9625415504 1 19961126 A 3150 WARNING BELL BOEING 757 757251 1384970 NM COCKPIT SOUNDED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 504US 23193 DURING TAKEOFF ROTATION, WARNING BELL SOUNDED WITH NO LIGHT INDICATION. AIRCRAFT RETURNED TO TPA AND LANDED WITHOUT INC IDENT. MAINTENANCE PERFORMED AURAL WARNING TEST, CHECKED OK. 2 L 7 2 4F RT A2NM 1996120500247 19961205 00247 WP 1996 12 5 9625429150 1 19961125 A 3222 STRUT BEARING DOUG DC9 DC914 3022034 WP NLG FAILED A A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 8908E 45749 ON TAKEOFF, UNABLE TO RETRACT LANDING GEAR. PERFORMED COCKPIT OPERATING MANUAL (COM), NOSE STEERING WAS ACTIVE. CONTIN UED FLIGHT TO DTW WITH GEAR IN DOWN POSITION. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE JACKED AIRCRAFT AND FOUND NO SE STRUT CONTAMINATED WITH METAL FROM DISINTEGRATED BEARING. REPLACED LOWER SHOCK STRUT ASSEMBLY, OPERATIONAL CHECKED G EAR, RETRACT AND GROUND SHIFT FUNCTIONS NORMAL. GEAR OPERATION CHECKS GOOD. 2 L 7 2 4F A6WE 1996120500248 19961205 00248 NM 1996 12 5 9625435523 1 19961120 A 2120 AIR DISTR BOEING 757 757251 1384970 NM CABIN ODOR A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 523US 23617 DURING FLIGHT SEVERAL PASSENGER'S REPORTED A BURNING SMELL IN THE AFT END OF AIRCRAFT. DIVERTED TO MSP AND LANDED WITH OUT INCIDENT. MAINTENANCE PERFORMED CHECK OF AFT CARGO, PACK BAYS, WHEEL WELLS AND TIRES. NO DISCREPANCIES NOTED. PUL LED AND COLLARED WATER COMPRESSOR CIRCUIT BREAKER PRECAUTIONARY. 2 L 7 2 4F RT A2NM 1996120500249 19961205 00249 WP 1996 12 5 9625449927 1 19961125 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8920E 45835 DURING LINE MAINTENANCE INSPECTION, FOUND AFT CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIO NAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996120500250 19961205 00250 WP 1996 12 5 9625459998 1 19961125 A 3350 60030451 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8934E 47143 EMERGENCY LIGHTS ILLUMINATED AND EMERGENCY LIGHTS ARM AND CHARGE CIRCUIT BREAKER POPPED IN FLIGHT. TURNED LIGHTS OFF AN D REARMED AND RESET CIRCUIT BREAKER. BREAKER POPPED AGAIN AND LIGHTS ILLUMINATED. REPLACED AFT EMERGENCY LIGHT BATTERY PACK POWER SUPPLY ABOVE AFT RIGHT LAVATORY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996120500251 19961205 00251 WP 1996 12 5 9625469990 1 19961125 A 3297 WIRE DOUG DC9 DC931 3022065 WP RT MLG IND CHAFED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 895OE 47186 RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. RECYCLED GEAR WITH NO HELP. FLIGHT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LANDING GEAR LEVER MECHANISM RUBBING AGAINST WIRE TO LIGHT BEHIN D PANEL. REPAIRED AND REPOSITIONED WIRE BUNDLE. ALSO, FOUND BROKEN WIRE TO RIGHT MAIN GEAR UPLOCK SWITCH PIN 5. REPAI RED WIRE, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996120500252 19961205 00252 WP 1996 12 5 9625479993 1 19961122 A 3222 STRUT DOUG DC9 DC931 3022065 WP NLG REQD SERVICE A NWAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 01 8986E 47402 GROUND SHIFT FAILURE OCCURRED ON APPROACH INTO DTW. CREW EXECUTED GO-AROUND PROCEDURES AND SYSTEM OPERATED NORMALLY ON SECOND APPROACH. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED AND SERVICED NOSE LANDING GEAR STRUT, OPERATION AL CHECK NORMAL. 2 L 7 2 4F A6WE 1996120500253 19961205 00253 NE 1996 12 5 9625485515 2 19961125 A 7530 185885 BELLCRANK BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE NR 2 ENGINE FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J M WARNING INDICATION OVER TEMP TO TAKEOFF 1 GL 01 515US 492 23203 716369 DURING TAKEOFF ROLL, ENGINE NR 2 EGT AND N2 REACHED LIMITS WELL BEFORE ENGINE NR 1. THRUST REDUCED AND TAKEOFF ABORTED. MAINTENANCE FOUND THE 2.5 BLEED INOPERATIVE AND THE 2.5 BLEED BELL CRANK FRACTURED IN TWO. BELLCRANK REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 1996120500254 19961205 00254 EA 1996 12 5 COMA9660216 1 19961126 A 2751 WIRE CNDAIR CL600 CL6002B19 1900309 EA RT TE FLAP CHAFED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 962CA 7123 FLAPS FAIL MESSAGE ON EICAS AFTER TAKEOFF. REPAIRED CHAFED WIRE HARNESS AT RT BRAKE AND POSITION SENSOR. 2 L 7 2 4F RT A21EA 1996120500255 19961205 00255 NM 1996 12 5 UPS96221691 1 19961112 A 5311 FRAME BOEING 727 72725C 138400H NM BS 1050 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE-C, AFT PIT BS 1050 APPROX RBL 3, THE FRAME APPEARS CRACKED IN THE RADIUS OF THE UPPER FLANGE. CUT OUT D AMAGED AREA AS REQUIRED, FABRICATED PARTS AND INSTALLED IAW SRM 51-40-3. 2 L 7 3 4F A3WE 1996120500256 19961205 00256 NM 1996 12 5 UPS96221692 1 19961023 A 5320 SHEAR TIE BOEING 727 72725C 138400H NM BS 351.2 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE-C, FRAME 351.2 EXFOLIATED ABOVE STR 25R, DETERMINED TO BE ON SHEAR TIE AND NOT ON FRAME. REMOVED DISCRE PANT AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-40-2, 53-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 1996120500257 19961205 00257 NM 1996 12 5 UPS96221694 1 19961030 A 5315 FLOORBEAM BOEING 727 72725C 138400H NM BS 344 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE-C, FLOORBEAM STA 344 RBL 18 UPPER CHORD FWD FLANGE CORRODED BEYOND LIMITS. REMOVED DAMAGED SECTION OF C HORD, FABRICATED AND INSTALLED REPAIR SECTION USING EXISTING SPLICE IAW SRM 51-30-2, 51-40-2. 2 L 7 3 4F A3WE 1996120500258 19961205 00258 NM 1996 12 5 UPS96221695 1 19961102 A 5530 CHORD BOEING 727 72725C 138400H NM VERTICAL STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE-C, VERTICAL STAB RT LOWER TORQUE BOX CHORD CORRODED AND CRACKED. REMOVED DAMAGED SECTION OF CHORD, FABR ICATED AND INSTALLED REPAIR PARTS IAW DHC SK947-123 AND SRM 51-30-2 REF ENGINEERING FLIE NR 727-55-0338. 2 L 7 3 4F A3WE 1996120500259 19961205 00259 NM 1996 12 5 UPS96221696 1 19961122 A 5320 SHEAR TIE BOEING 727 72725C 138400H NM BS 351.2 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE-C, SHEAR TIE AT STA 351.2, STR 22R WAS FOUND TO BE CORRODED BEYOND LIMITS. CUT OUT DAMAGED SECTION OF S HEAR TIE AT BS 351.2, STR 22R, FABRICATED AND INSTALLED REPAIR IAW SRM 53-10-2 AND 51-40-3. 2 L 7 3 4F A3WE 1996120500260 19961205 00260 NM 1996 12 5 UPS96221699 1 19961024 A 5330 SKIN BOEING 727 72725C 138400H NM BS 1096-1112 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE-C, FUSELAGE SKIN AND INTERNAL DOUBLER BS 1096 TO 1112 STR 18R TO 20R CORRODED BEYOND LIMITS ON UPS NRC 5 88666. FABRICATED REPAIR SKINS AND SPLICE DOUBLER IAW SK 974-957. INSTALLED REPAIR SKINS AND DOUBLER IAW DHC SK 947-95 7 REF ENGINEERING FILE NR 727-53-1841. 2 L 7 3 4F A3WE 1996120500261 19961205 00261 NM 1996 12 5 UPS96421689 1 19961130 A 2611 SMOKE DETECTOR BOEING 747 747123 1384873 NM CARGO COMPT INOPERATIVE A IPXA A F UNSCHED LANDING ACTIVATE FIRE EXT. J N WARNING INDICATION FALSE WARNING CR CRUISE 1 SO 01 673UP 20325 AFT CARGO FIRE WARN LIGHT WITH BELL. ACCOMPLISHED AFT CARGO FIRE CHK LIST PRIOR TO LANDING. REMOVED AND REPLACED LWR C ARGO COMPT NR 6 SMOKE DETECTOR PER B747MM. OPS CK NORMAL, THIS CLEARS M119730. 2 L 7 4 4F A20WE 1996120500262 19961205 00262 NM 1996 12 5 UPS96421693 1 19961121 A 5311 FRAME BOEING 747 747123 1384873 NM BS 1500 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE-C, AFT CARGO COMP FOUND CRACK IN FRAME INNER FLANGE BS 1500, S-40RT. STOP DRILLED CRACK AND REPAIRED FR AME INNER FLANGE ACC SRM 53-10-04 FIG 66. 2 L 7 4 4F A20WE 1996120500263 19961205 00263 NM 1996 12 5 UPS96421697 1 19961126 A 5311 FRAME BOEING 747 747123 1384873 NM BS 1740 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE-C, AFT CARGO COMP, DURING INSPECTION PER EO B747-5310-0180D, FOUND DENTS IN FRAME INNER FLANGE AND DEFOR MED FRAME WEB AT BS 1740, BETWEEN S-38 AND 40RT. REMOVED DAMAGED SECTION OF FRAME INNER FLANGE AND REPAIRED FRAME INNER FLANGE ACC SRM 51-40-0. 2 L 7 4 4F A20WE 1996120500264 19961205 00264 NM 1996 12 5 UPS96421698 1 19961121 A 5320 WEB BOEING 747 747123 1384873 NM BS 2160 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE-C, FOUND A HOLE IN WEB AT STA 2160 LT LOWER SIDE IN BULK CARGO COMPARTMENT. REMOVED DAMAGED SECTION OF WEB AND REPAIRED WEB ACC TO SRM 51-40-02. 2 L 7 4 4F A20WE 1996120500265 19961205 00265 NM 1996 12 5 UPS96421700 1 19961121 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM BS 255 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE-C, SEAT TRACK AT BS 255 AT LBL 53 IS CORRODED, CORROSION BEYOND LIMITS. REPLACED DAMAGE SEAT TRACK FROM BS 310 AT LBL ACC SRM 53-10-05 FIG 1. 2 L 7 4 4F A20WE 1996120500266 19961205 00266 NM 1996 12 5 UPS96421701 1 19961201 A 3350 60B5003737 LIGHT BOEING 747 747121 1384871 NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 691UP 19641 INSPECTION TYPE-N/A, COCKPIT EMERGENCY LIGHT ABOVE STAIRWAY INOP. REMOVED AND REPLACED LIGHT, OPS CHECKS GOOD (P/N 60B5 0037-37) (S/N 19567) OFF, (P/N 60B50037-37) (S/N 33648) ON. 2 L 7 4 4F A20WE 1996120500267 19961205 00267 NM 1996 12 5 UPS96421702 1 19961127 A 3350 LIGHT BOEING 747 747121 1384871 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE-N/A, FWD EMERGENCY EXIT LIGHT UPPER CREW SVC DOOR INOP. RELAMPED, OPS CKS OK. 2 L 7 4 4F A20WE 1996120500268 19961205 00268 NM 1996 12 5 UPS96421703 1 19961130 A 2621 35207920M11 FIRE BOTTLES BOEING 747 747123 1384873 NM CARGO COMPT DISCHARGED A IPXA O OTHER N FALSE WARNING IN INSP/MAINT 1 SO 01 673UP 20325 BOTH LOWER CARGO COMPT. FIRE BOTTLES DISCHARGED AND LIGHTS ARE ILLUMINATED. REPLACED BOTH FIRE BOTTLES PER MM 26-20. P /N ON 35207900M-11, OFF 35207920M-11, P/N ON 34907900M12, S/N ON 00691R1, OFF 00686R1, S/N OFF 02899531 OFF K87. 2 L 7 4 4F A20WE 1996120500269 19961205 00269 1996 12 5 UPS96821704 4 19961129 A 2564 LIFE RAFT DOUG DC8 DC873F 302199F WP CABIN DEPLOYED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE-N/A, AFT LIFE RAFT PARTIALLY DEPLOYED. REMOVED AND REPLACED AFT LIFE RAFT ASSY UNDER COURIER SEATS. 2 L 7 4 4F RT 4A25 1996120500270 19961205 00270 WP 1996 12 5 96640 1 19961126 A 3350 60030431 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 502ME 48132 DURING A CHECK, FOUND BOTH OVERWING EMERGENCY EXIT FWD SIGNS WOULD NOT ILLUMINATE. REMOVED AND REPLACED OVERWING EXIT S IGN BATTERY POWER SUPPLY, OPS CHK GOOD. 2 L 7 2 4F A6WE 1996120500271 19961205 00271 WP 1996 12 5 96641 1 19961126 A 3350 100865 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 206ME 47791 DURING SERVICE CHECK, FOUND AFT EMERGENCY LIGHTS WOULD NOT TEST. REMOVED AND REPLACED BATTERY PWR SUPPLY, OPS CHECK GOO D. 2 L 7 2 4F A6WE 1996120500272 19961205 00272 WP 1996 12 5 96642 1 19961127 A 2910 HYDRAULIC LINE DOUG DC9 DC932 3022066 WP ACCESORY COMPT LOOSE A MWEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 31 207ME 47794 PILOT REPORTS, POSSIBLE SMOKE OR MIST IN CABIN WHILE OPERATING RT PACK WITH APU. FOUND LEAKING HYDRAULIC LINE IN AFT AC CESSORY COMPARTMENT NEAR APU INTAKE. TIGHTENED LINE, CLEANED AIRBOX AND APU DOORS, RAN APU AND RT PACK AND NO SMOKE OR MIST PRESENT. 2 L 7 2 4F A6WE 1996120500273 19961205 00273 WP 1996 12 5 96643 1 19961129 A 5730 SKIN DOUG DC9 DC932 3022066 WP WS 247 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 DURING C-CHECK, FOUND SKIN CRACKED ON LOWER SIDE OF LEADING EDGE NEAR INBD END OF FUELING PANEL AT STA XFS 247. INSTALL ED DOUBLER REPAIR IAW DAC TELEX MISC/K5L. 2 L 7 2 4F A6WE 1996120500274 19961205 00274 NM 1996 12 5 DHL9672001C 1 19961031 A 5754 692848112 RIB BOEING 727 727228 NM NR 6 LE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, NR 6 SLAT O/B RIB CRACKED. REPLACED RIB PER SRM 51-10-1 AND 57-30-7. 2 L 7 3 4F A3WE 1996120500275 19961205 00275 NM 1996 12 5 DHL9672002C 1 19961020 A 5730 SKIN BOEING 727 727228 NM LT WING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, SKIN DAMAGED ON LEFT WING INBD OF NR 2 L/E SLAT. CUT OUT DAMAGED AREA, INSTALLED FLUSH DOUBLER REPAIR PER S RM 57-30-4, FILLER 6 BY 3.5, DOUBLER 8 BY 7. 2 L 7 3 4F A3WE 1996120500276 19961205 00276 NM 1996 12 5 DHL9672003C 1 19961022 A 5754 FITTING BOEING 727 727228 NM NR 4 LE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, LEFT WING L/E NR 4 SLAT ON I/B FLANGE CRACKED. STOP DRILLED CRACK, INSTALLED DOUBLER REPAIR PER SRM 57-50- 3, 3 BY 3. 2 L 7 3 4F A3WE 1996120500277 19961205 00277 NM 1996 12 5 DHL9672004C 1 19961022 A 5730 SKIN BOEING 727 727228 NM WS 171.5 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, LEFT UPPER LEADING EDGE HAS DEEP DENT ABOUT WS 171.5. CUT OUT DAMAGED AREA PER SRM 57-30-4, INSTALLED DOUBL ER REPAIR PER SRM 57-30-4 5 BY 5, FILLER 2 BY 3. 2 L 7 3 4F A3WE 1996120500278 19961205 00278 NM 1996 12 5 DHL9672005C 1 19961022 A 5730 PANEL BOEING 727 727228 NM LT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, LEFT WING UPPER T/E PANEL JUST FWD OF NR 7 SPOILER HAS CORROSION AT AFT CENTER EDGE. REPLACED PANEL PER SRM 51-10-1, 89 BY 12. 2 L 7 3 4F A3WE 1996120500279 19961205 00279 NM 1996 12 5 DHL9672006C 1 19961025 A 5712 RIB BOEING 727 727228 NM WS 629 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, LEFT WING INSPECTION REVEALED CRACK AT WING RIB STA 629, ATTACH FLANGE AT S-2 LOWER SIDE. STOP DRILLED CRA CK, ACCOMPLISHED HFEC OF STOP HOLE, ENLARGED STOP HOLE ADDITIONAL .062 PER S/B 57-0127. INSTALLED ANGLE REPAIR PER SRM 57-10-5 AND S/B 57-0127, 10 BY 3. 2 L 7 3 4F A3WE 1996120500280 19961205 00280 NM 1996 12 5 DHL9672007C 1 19961026 A 5712 RIB BOEING 727 727228 NM WS 686.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, INSPECTION OF LEFT WING REVEALED CRACK AT WING RIB STA 686.5 S-2 LOWER ATTACH FASTENER HOLE. STOP DRILLED C RACK, HFEC OF HOLE, ENLARGED HOLE ADDITIONAL .062 PER S/B 57-0127 AND ACCOMPLISHED REPAIR PER SRM 57-10-5 AND S/B 57-012 7, REPAIR 9 BY 3.125. 2 L 7 3 4F A3WE 1996120500281 19961205 00281 NM 1996 12 5 DHL9672008C 1 19961029 A 5712 RIB BOEING 727 727228 NM WS 601.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, FOUND CRACK AT WING RIB STA 601.5 AT S-3 LOWER FASTENER ATTACH HOLE. STOP DRILLED CRACK, HFEC OF STOP DRILL OK. ENLARGED STOP HOLE ADDITIONAL .062 PER S/B 57-0127, ACCOMPLIHED REPAIR PER SRM 57-10-5, REPAIR 9 BY 3.125. 2 L 7 3 4F A3WE 1996120500282 19961205 00282 NM 1996 12 5 DHL9672009C 1 19961030 A 5712 RIB BOEING 727 727228 NM WS 656.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, CRACK INDICATION FOUND AT LEFT WING RIB STA 656.5 AT S-2 LOWER ATTACH FASTENER HOLE OLD REPAIR. REMOVED OLD REPAIR, INSTALLED ANGLE REPAIR AT WING RIB PER SRM 57-10-5. 2 L 7 3 4F A3WE 1996120500283 19961205 00283 NM 1996 12 5 DHL9672010C 1 19961031 A 5754 692848111 RIB BOEING 727 727228 NM NR 3 LE SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, NR 3 SLAT I/B RIB CRACKED. REMOVED AND REPLACED RIB PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996120500284 19961205 00284 NM 1996 12 5 DHL9672011C 1 19961021 A 5712 RIB BOEING 727 727228 NM WS 349 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, RIB CRACKED JUST FWD OF TOP CHORD FWD SPAR AT STA 349, RIGHT WING. STOP DRILLED CRACK, DYE PEN INSP. INSTA LLED ANGLE REPAIR PER SRM 51-40-3, REPAIR 6 BY 1.5. 2 L 7 3 4F A3WE 1996120500285 19961205 00285 NM 1996 12 5 DHL9672012C 1 19961021 A 5754 ANGLE BOEING 727 727228 NM NR 5 LE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, NR 5 SLAT OUTBD END LOWER SKIN ANGLE TO OUTBD RIB CRACKED. CUT OUT DAMAGED AREA, INSTALLED ANGLE REPAIR PER SRM 51-40-4, REPAIR 1 BY 12 BY 3.5. 2 L 7 3 4F A3WE 1996120500286 19961205 00286 NM 1996 12 5 DHL9672013C 1 19961021 A 5712 RIB BOEING 727 727228 NM WS 601.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, INSPECTION REVEALED CRACK INDICATION AT WING RIB STA 601.5 AT S-2 LOWER ATTACH FASTENER HOLE. STOP DRILLED CRACK PER 57-0127. HFEC INSPECTION OF STOP HOLE, ENLARGED HOLE AN ADDITIONAL .062 PER S/B 57-0127. INSTALLED WING RIB REPAIR 10 BY 2 PER SRM 57-0127 AND SRM 57-10-5. 2 L 7 3 4F A3WE 1996120500287 19961205 00287 NM 1996 12 5 DHL9672014C 1 19961030 A 5330 SKIN BOEING 727 727228 NM BS 985 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, FUSELAGE EXTERNAL SKIN CRACKED AT BS 985 S-25L. CUT OUT DAMAGED SKIN, INSTALLED FLUSH REPAIR PER SRM 53-30- 3 21 BY 7. 2 L 7 3 4F A3WE 1996120500288 19961205 00288 NM 1996 12 5 DHL9672015C 1 19961028 A 5720 STIFFENER BOEING 727 727228 NM BS 740 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, WING CENTER SECTION INTERIOR STIFFENER, RBL 51 FS 740 CRACKED AT LOWER AREA. REPLACED STIFFENER PER SRM 51- 30-2, 34 INCHES LONG. 2 L 7 3 4F A3WE 1996120500289 19961205 00289 NM 1996 12 5 DHL9672016C 1 19961024 A 5315 BAC1518359 FLOORBEAM BOEING 727 727228 NM BS 420 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, FLOORBEAM STA 420 LBL 62 CORRODED. REPLACED FLOORBEAM PER SRM 51-10-1, 24 INCHES LONG. 2 L 7 3 4F A3WE 1996120500290 19961205 00290 NM 1996 12 5 DHL9672017C 1 19961028 A 5230 SKIN BOEING 727 727228 NM NR 2 CARGO DOOR CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, NR 2 CARGO DOOR INTERIOR SKIN CORRODED ON LOWER STRAP 24 INCHES FROM FWD EDGE AND 24 INCHES FROM LOWER EDGE. REMOVED AND RPLACED DOOR STRAP PER SRM 51-10-1, 1 BY 32. 2 L 7 3 4F A3WE 1996120500291 19961205 00291 NM 1996 12 5 DHL9672018C 1 19961023 A 5210 SKIN BOEING 727 727228 NM PAX DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, FWD ENTRY DOOR HAS SKIN STOP DRILLED CRACK AT LOWER AFT HINGE CUTOUT AND DAMAGE AT FWD UPPER AREA. STOP DRI LLED CRACK, INSTALLED EXTERNAL DOUBLER REPAIR PER SRM 52-00-3, 8 BY 6. 2 L 7 3 4F A3WE 1996120500292 19961205 00292 NM 1996 12 5 DHL9672019C 1 19961031 A 5754 692848212 RIB BOEING 727 727228 NM NR 6 LE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, NR 6 SLAT I/B RIB CRACKED. REPLACED RIB PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996120500293 19961205 00293 NM 1996 12 5 DHL9672020C 1 19961024 A 5330 SKIN BOEING 727 727228 NM BS 328 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, LAP SEAM AT STA 328, STR 24R HAS BULGING AROUND RIVETS. REMOVED FASTENERS AT LAP SEAM. CHECKED INNER SIDE OF SKIN, FOUND NO EVIDENCE OF CORROSION. PERFORMED HFEC AT UPPER ROW, NO DEFECTS NOTED. FOUND CRACK AT ATTACH ANGLE RT SIDE BS 328. CUT OUT DAMAGED SKIN AT STA 328. INSTALLED SKIN REPAIR PER SRM 53-30-3, FILLER 3.53 BY 2, DOUBLER 8 X 7. 2 L 7 3 4F A3WE 1996120500294 19961205 00294 NM 1996 12 5 DHL9672021C 1 19961102 A 5315 FLOORBEAM BOEING 727 727228 NM BS 400 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, CABIN FLOORBEAM AT BS 400 LBL 12 HAS HEAVY CORROSION. CUT OUT DAMAGED AREA OF FLOORBEAM, INSTALLED FLOORBEA M REPAIR PER SRM 53-1-8, REPAIR 13.5 LONG. 2 L 7 3 4F A3WE 1996120500295 19961205 00295 NM 1996 12 5 DHL9672022C 1 19961029 A 5712 RIB BOEING 727 727228 NM WS 738.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, INSPECTION FOUND CRACK AT WING RIB STA 738.5 STRINGER 2 LOWER AT ATTACH FASTENER HOLE. STOP DRILLED CRACK, HFEC STOP DRILL, ENLARGED HOLE ADDITIONAL .062 PER S/B 57-127. ACCOMPLISHED REPAIR PER SRM 57-10-5 AND S/B 57-0127, REP AIR 7 BY 3 . 2 L 7 3 4F A3WE 1996120500296 19961205 00296 NM 1996 12 5 DHL9672023C 1 19961101 A 5347 SEAT TRACK BOEING 727 727228 NM BS 1070 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, CABIN SEAT TRACK STA 1070 LBL 48 FLANGE CORRODED. REMOVED AND REPLACED SEAT TRACK FROM STA 1030 TO 1070 PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996120500297 19961205 00297 NM 1996 12 5 DHL9672024C 1 19961028 A 5347 BAC1520792 SEAT TRACK BOEING 727 727228 NM BS 947-939 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, CORROSION AROUND FASTENER HOLES ON SEAT TRACK O/B FLANGE LBL 45 FROM STA 947 TO 939. REMOVED AND REPLACED S EAT TRACK FROM BS 870 TO BS 950 PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996120500298 19961205 00298 NM 1996 12 5 DHL9672025C 1 19961025 A 5347 SEAT TRACK BOEING 727 727228 NM BS 680 CORROSION A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, FOUND CORROSION ON SEAT TRACK FLANGE STA 680 LBL 47. REMOVED AND REPLACED SEAT TRACK FROM STA 660 TO 690 PE R SRM 51-10-1. 2 L 7 3 4F A3WE 1996120500299 19961205 00299 NM 1996 12 5 DHL9672026C 1 19961025 A 5347 BAC1520792 SEAT TRACK BOEING 727 727228 NM BS 680 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, FOUND CORROSION ON SEAT TRACK STA 680 RBL 45. CUT OUT AND INSTALLED SEAT TRACK FROM BS 650 TO 690 PER SRM 5 3-10-5. 2 L 7 3 4F A3WE 1996120500300 19961205 00300 NM 1996 12 5 DHL9672027C 1 19961025 A 5347 SEAT TRACK BOEING 727 727228 NM BS 360-400 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, CORROSION AND CRACK ON SEAT TRACK LBL 50.5 STA 360 TO 400. REMOVED AND REPLACED SEAT TRACK FROM STA 360 TO 460 PER SRM 51-30-2. 2 L 7 3 4F A3WE 1996120500301 19961205 00301 NM 1996 12 5 DHL9672028C 1 19961021 A 5330 SKIN BOEING 727 727228 NM BS 294 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, FOUND BULGING AROUND RIVETS ON LAP SEAM STR 24R APPROX FS 294. REMOVED FASTENERS AT LAP SEAM STR 24 RT FROM BS 280 TO BS 328. PERFORMED HFEC, FOUND SKIN CRACK AT ATTACH ANGLE BELOW STR 24RT BS 294.5. CUT OUT DAMAGED SKIN 3.5 BY 2. INSTALLED EXTERNAL DOUBLER SKIN REPAIR PER SRM 53-30-3, 11 BY 9.75. 2 L 7 3 4F A3WE 1996120500302 19961205 00302 NM 1996 12 5 DHL9672029C 1 19961021 A 2782 ANGLE BOEING 727 727228 NM NR 8 SLAT ACT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, NR 8 SLAT ACTUATOR TRUNNION, OUTBD VERTICAL SUPPORT ANGLE IS CRACKED JUST UNDER LOWER ATTACH BOLT TO TRUNNIO N. REMOVED AND REPLACED OUTBD VERTICAL SUPPORT ANGLE AT NR 8 SLAT ACTUATOR TRUNNION PER SRM 51-10-1, 9 BY 4.5. 2 L 7 3 4F A3WE 1996120500303 19961205 00303 NM 1996 12 5 DHL9672030C 1 19961020 A 2782 BRACKET BOEING 727 727228 NM NR 1 SLAT ACT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, NR 1 SLAT ACTUATOR I/B MOUNT CRACKED. REMOVED AND REPLACED INBOARD MOUNT BRACKET PER SRM 51-10-1 AND 51-30- 3, REPAIR 7.5 BY 5. 2 L 7 3 4F A3WE 1996120500304 19961205 00304 NM 1996 12 5 DHL9672031C 1 19961022 A 2760 65192228 CASTING BOEING 727 727228 NM NR 8 SPOILER ACT CRACKED A A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, NR 8 SPOILER CENTER HINGE ACTUATOR LINKAGE AFT END BROKEN OFF. INSTALLED NEW CASTING PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996120500305 19961205 00305 NM 1996 12 5 DHL9672032C 1 19961022 A 5712 RIB BOEING 727 727228 NM WS 686.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, RIGHT WING RIB AT STA 686.5 HAS CRACK AT ATTACH POINT. STOP DRILLED CRACK AND PERFORMED HFEC ISNP. INSTAL LED RIB REPAIR PER SRM 57-10-5, REPAIR 3 BY 10. 2 L 7 3 4F A3WE 1996120500306 19961205 00306 NM 1996 12 5 DHL9672033C 1 19961024 A 5712 RIB BOEING 727 727228 NM WS 629 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, RIGHT WING RIB STA 629, LOWER FLANGE AT STR 6 CRACKED. STOP DRILLED CRACK, HFEC INSTALLED REPAIR PER SRM 57 -10-5, 3 BY 10. 2 L 7 3 4F A3WE 1996120500307 19961205 00307 NM 1996 12 5 DHL9672034C 1 19961022 A 5320 ANGLE BOEING 727 727228 NM BS 560 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, FWD LOWER CARGO DOOR CUTOUT FRAME ANGLE HAS CORROSION AT BS 560 BETWEEN STR 24R AND 25R. REMOVED FRAME ANGL E AND INSTALLED NEW ANGLE PER SRM 51-40-2, REPAIR 2 BY 2. 2 L 7 3 4F A3WE 1996120500308 19961205 00308 NM 1996 12 5 DHL9672035C 1 19961023 A 5720 STIFFENER BOEING 727 727228 NM BS 740 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, WING CENTER SECTION INTERIOR UPPER STIFFENER ATTACH ANGLE CRACKED LBL 24, BS 740. REMOVED AND REPLACED ANGL E PER SRM 51-30-2, 3 BY 3.5. 2 L 7 3 4F A3WE 1996120500309 19961205 00309 NM 1996 12 5 DHL9672036C 1 19961021 A 5320 WEB BOEING 727 727228 NM BS 326 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, FLOOR SUPPORT WEB AT STA 326 AT LBL 40 CORRODED. REMOVED AND REPLACED SUPPORT WEB PER SRM 51-10-1, 20 INCHE S LONG. 2 L 7 3 4F A3WE 1996120500310 19961205 00310 NM 1996 12 5 DHL9672037C 1 19961028 A 5320 VERICAL WEB BOEING 727 727228 NM BS 870 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, FOUND CORROSION AT SEAT TRACK LOWER VERT WEB BEAM END AT ATTACHING FITTING INBD SIDE AT LBL 45 STA 870. REM OVED AND REPLACED VERTICAL WEB AND ATTACH FITTING PER SRM 51-10-1. 2 L 7 3 4F A3WE 1996120500311 19961205 00311 NM 1996 12 5 DHL9672038C 1 19961024 A 2120 PLENUM CHAMBER BOEING 727 727228 NM RIGHT CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, CORROSION WAS FOUND ON UPPER WALL OF RAM AIR PLENUM CHAMBER OVER PRIMARY HEAT EXCHANGER. REMOVED HEAT EXCHA NGER FOR ACCESS, REMOVED EXISTING DOUBLER, INSTALLED REPAIR PER ENGINEERING ORDER PMSI-135D-1. INSTALLED DOUBLER 15 BY 3.75, DOUBLER 19.5 BY 6.5, TRIPLER 24 BY 6.5 . INSTALLED FIBERGLASS REPAIR PER SRM 51-40-8 ON RAM AIR DUCT. INSTALLED L-ANGLE PER SRM 51-20-4. 2 L 7 3 4F A3WE 1996120500312 19961205 00312 NM 1996 12 5 DHL9672039C 1 19961031 A 2782 MOUNT BOEING 727 727228 NM NR 2 LE FLAP ACT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, NR 2 LEADING EDGE FLAP ACTUATOR MOUNT O/B SIDE BOTH CORNERS CRACKED. REPLACED BRACKET PER SRM 51-10-1 AND 5 1-30-2, REPAIR 6 BY 8 . 2 L 7 3 4F A3WE 1996120500313 19961205 00313 NM 1996 12 5 DHL9672040C 1 19961101 A 5330 SKIN BOEING 727 727228 NM BS 950 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, FOUND CORROSION ON INNER SKIN SURFACE AT DRAIN VALVE BETWEEN 28 TO 29R, FWD OF 950. INSTALLED DOUBLER PER S RM 53-30-3 36 BY 15, FILLER 20.5 BY 12. 2 L 7 3 4F A3WE 1996120500314 19961205 00314 NM 1996 12 5 DHL9672041C 1 19961105 A 5330 SKIN BOEING 727 727228 NM BS 950 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, FOUND CHORD ANGLE CORRODED IN AFT BAGGAGE COMP STA 950 RBL 15. REMOVED FASTENERS, CUT OUT SKIN 20.5 BY 12, REMOVED CORRODED CHORD ANGLE AND ATTACH STRAP TO L-ANGLE. INSTALLED REPAIR STRAP BETWEEN STR 28R AND 26R, INSTALLED NE W CHORD ANGLE PER SRM 51-10-1, INSTALLED DOUBLER PER SRM 53-30-3 36 BY 15, FILLER 20.5 BY 12. 2 L 7 3 4F A3WE 1996120500315 19961205 00315 NM 1996 12 5 DHL9672042C 1 19961008 A 5712 RIB BOEING 727 727228 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, HFEC ON LEFT WING RIB UPPER CHORD, CRACKS AT BL 70.5. STOP DRILLED HOLE, HFEC ON STOP HOLE AND COMMON FAST ENERS HOLES, NOT CRACKS NOTED. INSTALLED PREVENTATIVE MODIFICATION PER S/B 57-0112 AND DRAWING 65-33202. 2 L 7 3 4F A3WE 1996120500316 19961205 00316 NM 1996 12 5 DHL9672043C 1 19961008 A 5712 RIB BOEING 727 727228 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, CRACKS NOTED ON RIGHT WING UPPER CHORD BL 70.5. STOP DRILLED CRACK, HFEC STOP HOLE AND HOLES COMMON TO FAST ENERS. INSTALLED WING REPAIR PER S/B 57-112. 2 L 7 3 4F A3WE 1996120500317 19961205 00317 NM 1996 12 5 DHL9672044C 1 19961022 A 5711 SPAR BOEING 727 727228 NM WS 519 CORROSION A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C-CHECK, LEFT WING L/E SPAR LOWER CHORD HAS EXFOLIATION CORROSION JUST FWD AND I/B OF NR 3 SLAT, WS 519. REMOVED COR ROSION, FOUND OUT OF LIMITS. INSTALLED REPAIR PER SRM 57-10-6 AND S/B 57-145, DOUBLER 12 BY 4. 2 L 7 3 4F A3WE 1996120500349 19961205 00349 SO 1996 12 5 96ZZZX5832 1 19961113 A 3320 BC10047005 LUMINARE BRUCE BR99002 EMB 120 EMB120ER 3260203 SO CABIN LIGHT BURN DAMAGE A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 197SW 120186 AIRCRAFT HAD REPORTED AN ELECTRICAL ODOR IN THE CABIN NEAR ROW 6. THE MECHANIC INSPECTED THE CABIN TO PINPOINT THE ORIG IN OF THE SMELL. HE FOUND A BURNT SPOT ON THE OVERHEAD PANEL ABOVE SEAT 5A. AFTER REMOVING THE PANEL, HE DISCOVERED A BURNT SOCKET ON THE LUMINARIES. THIS LUMINARY HAD SERVICE LETTER SL-BC5-0618-901-33-01 INSTALLED ON 8-31-96. THERE HAS BEEN NO MAINTENANCE PERFORMED IN THAT LOCATION SINCE THE INSTALLATION OF THE SERVICE LETTER. IN LATER DISCUSSION WITH THE MECHANIC ON THE CONDITION OF THE LAMP AND SOCKET WHEN DISCOVERED. IT WAS MENTIONED THE LAMP END WAS NOT DAMAGED OR DISCOLORED. 2 L 7 2 4T RT A31SO 1996120500350 19961205 00350 CE 1996 12 5 96ZZZX5833 1 19961101 A 5610 10138402517 WINDOW BEECH 90 F90 1152909 CE PILOT SIDE FRACTURED A A BR7A A UNSCHED LANDING O OTHER CR CRUISE 1 EA 09 66BS 1766 LA40 NOV. 1, 1996: CRUISE FLIGHT @ FL 230, OUTER LAMINATION OF PILOT WINDSHIELD FRACTURED 2-3 INCHES INBOARD OF CENTER POST. FRACTURE WAS VERTICAL THE ENTIRE HEIGHT OF WINDSHIELD. INNER LAMINATION NOT AFFECTED. PRECAUTIONARY LANDING MADE WI THOUT INCIDENT. WINDSHIELD HEAT WAS ACTIVE FOR 20-30 MINUTES PRIOR TO FAILURE. SECOND FAILURE OF WINDSHIELD ASSY. 1ST FAILURE OCCURRED 10-17-88 @ 1384 TSN. 2ND FAILURE @ 3150 TSN. 1 L 7 2 4T A31CE 1996120500358 19961205 00358 NE 1996 12 5 CA960529004 2 19960515 A 7320 3029592C FUEL CONTRL UNIT CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE PC AIR BLOCKED ORIFICE W A K NONE O OTHER CL CLIMB 1 CA 1757 PCE71716 (CAN)DURING A SIMULATED ENGINE FAILURE, THE #2 ENGINE RETARDED TO IDLE. AFTER THE EXERCISE TERMINATED, THE THROTTLE WAS ADVANCED TO RESTORE POWER BUT THE ENGINE FAILED TO RESPOND. BLOCKED PC AIR ORIFICE INTHE FCU. THIS ENGINE HAD UNDERGONE HOT SECTION INSPECTION 3.8 HOURS PREVIOUS DURING WHICH DIFFUSER TUBES WERE REPLACED. SWARF RESULTING FROM THE GRINDING O PERAITON IS BELIEVED TO BE THE SOURCE OF THE BLOCKING MATERIAL. 1 L 7 2 4F 4 F A22CE E1NE 1996120500359 19961205 00359 EA 1996 12 5 CA960529006 1 19960509 A 3222 713381 TORQUE ARM HEROUX 7110011 DHAV DHC6 DHC6300 EA PWA PT6 PT6A27 52043 EA NLG LOWER BROKEN W O OTHER O OTHER TX TAXI/GRND HDL 1 CA H687 PCE42054 (CAN) AFTER LANDING THE WHEEL SKI EQUIPPED NOSE GEAR LOWER TORQUE ARM BROKE. DURING ROLL OUT THE COMBINATION OF SKI SHIM MY AND FULL EXTENSION OF THE NOSE OLEO WHICH WOULD PREVENT SHIMMY DAMPENING INDUCED FORCES BEYOND THE TORQUE LINK DESIGN . 1 H 7 2 3T 4 T A9EA E4EA 1996120500363 19961205 00363 SO 1996 12 5 CA960529012 2 19960504 A 8520 629340 CONROD BOLT CESSNA 207 207A 2073604 CE CONT O520 IO520F 17032 SO MCAULY D3A34 D3A34C404 GL #2 ROD FAILED W C D ABORTED TAKEOFF RETURN TO BLOCK E R K VIBRATION/BUFFET PARTIAL RPM/PWR LOSS FLUID LOSS TO TAKEOFF 1 CA 1429 810084R 811665 (CAN)ON POWER APPLICATION FOR TAKEOFF, SEVERE VIBRATION FROM ENGINE. POWER REDUCED AND ENGINE STOPPED. #2 CONNECTING ROD FAILED AND EXITED THE TOP OF CASE. CONROD CAP BOLTS FAILED. 1 H 7 1 3O 3 O A16CE E5CE 5 C P47GL 1996120500364 19961205 00364 NE 1996 12 5 CA960529014 2 19960521 A 7322 32448094 FUEL CONTRL UNIT CESSNA 208 208B 2073701 CE PWA PT6 PT6A114 52043 NE CASE DRAIN LEAKING W K NONE O OTHER IN INSP/MAINT 1 CA 1498 PCE19255 (CAN)ON INSPECTION, BLUE DYE NOTICED FROM FCU VENT INDICATING FUEL LEAKAGE INTO BEARING AREA. 1 H 7 1 3T 3 T A37CE E4EA 1996120500365 19961205 00365 EA 1996 12 5 CA960530001 2 19960401 A 8520 CRANKCASE PIPER PA44 PA44180 7104402 SO LYC O360 O360E1A6 41514 EA #3 CYLINDER BASE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1274 RL43572T (CAN)CRANKCASE CRACKED AT #3 CYLINDER POSITION. 1 L 7 2 3O 3 O A19S0 E286 1996120500369 19961205 00369 NE 1996 12 5 CA960604004 2 19960429 A 8540 OIL SYSTEM PWA 121510 DOUG DC3 DC3CS1C3G 3021458 WP PWA R1830 R183092 52020 NE ENG OIL CONTAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA A77295 (CAN)MICARTA MATERIAL FOUND OIL SCREEN, SUSPECT FAILURE OF IMPELLER SHAFT BEARING. AWAITING STRIP REPORT. 2 L 7 2 4R 4 R A669 5E4 1996120500370 19961205 00370 EA 1996 12 5 CA960604005 2 19960604 A 8520 74801M10 BEARING BEECH 60 B60 1153605 CE LYC O541 TIO541E1C4 41536 EA CRANKSHAFT #1 BR SCORED W A K NONE O OTHER IN INSP/MAINT 1 CA 34 L154159 (CAN)PROP WENT INTO FEATHER AT ENGINE IDLE. PROP CONTROL OIL LEAK TEST PERFORMED PER LYCOMING S.L. 1462, NOT WITHIN LIMI TS. NON FERROUS METAL IN FILTERS. ENGINE REPLACED. TEARDOWN REVEALED FRONT CRANKSHAFT BEARING BADLY WORN DUE TO AN APPAR ENT OUT OF ROUND CONDITION. 1 L 7 2 3O 3 O A12CE E10EA 1996120500373 19961205 00373 EA 1996 12 5 CA960604008 1 19960527 A 5752 85740335102 AIL TAB BRACKET DHAV 85740483003 DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE RT OUTB BUSHING WORN W K NONE O OTHER IN INSP/MAINT 1 CA 11128 0030043 123018 (CAN) RH AILERON TRIM TAB, OUTBOARD HINGE POINT FOUND WITH EXCESSIVE PLAY. HINGE BRACKET ON AILERON TRAILING EDGE OUTBOA RD BUSHING HOLE ELONGATED. 2 H 7 2 4T 4 T RT A13NM E20NE 1996120500374 19961205 00374 WP 1996 12 5 CA960604010 1 19960519 A 7110 LK73720 FAIRING RROYCE LK73720 LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB21122B NE NR 1 ENG MISSING W K NONE D INFLIGHT SEPARATION IN INSP/MAINT 1 CA 10171 (CAN) ON ROUTINE INSPECTION, NR 1 ENGINE GAS GENERATOR FAIRING LOWER PORTION MISSING AND ADJACENT FAIRINGS DAMAGED. 2 L 7 3 4F 4 F A23WE E12EU 1996120500375 19961205 00375 NM 1996 12 5 CA960604013 1 19960531 A 3246 1014171 WHEEL HALF DUNLOP 314353 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE OUTBOARD CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 356 0195 120144 (CAN) DURING EDDY CURRENT INSPECTION OUTBOARD WHEEL HALF FOUND CRACKED. 0.75 INCHES ABOVE BEAD AREA IN BARREL. 2 H 7 2 4T 4 T RT A13NM E20NE 1996120500376 19961205 00376 NM 1996 12 5 CA960604014 1 19960531 A 3231 SENSOR DHAV DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE LEFT MLG DOOR OUT OF ADJUST W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 120083 (CAN) LEFT MAIN LANDING GEAR FORWARD DOOR AMBER CAUTION LIGHT REMAINED ON AFTER GEAR SLECTED UP. DOOR VISUALLY CONFIRMED OPEN. GEAR WOULD NOT EXTEND WITH NORMAL SELECTION. ALTERNATE EXTENSION CARRIED OUT. GEAR DOOR SENSOR GAP TOO WIDE, ALSO DOOR ROD ADJUSTED. 2 H 7 2 4T 4 T RT A13NM E20NE 1996120500377 19961205 00377 1996 12 5 CA960604015 4 19960524 A 2210 2588880901 YAW DAMPER BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE AUTO PILOT INTERMITTENT W A H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED AP APPROACH 1 CA 702782 (CAN) ON APPROACH WITH 40 UNITS OF FLAPS SELECTED AIRCRAFT HAD EXCESSIVE YAW TO THE RIGHT AND LEFT. AIRCRAFT STABILIZED WHEN YAW DAMPER SELECTED OFF. AUTOPILOT OFF/ALT 1200 AGL/WIND 10/TEMP 18 DEGREES. REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1996120500378 19961205 00378 NM 1996 12 5 CA960604016 1 19960520 A 2912 SEAL BOEING 737 7372T7 NM PWA JT8 JT8D17 52049 NE HYD FILTER LEAKING W A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 CA 708808 (CAN) AFTER TAKEOFF WITH THE LANDING GEAR AND FLAPS UP, THE HYDRAULIC QUANTITY WAS 3.0 GALLONS. ONE HOUR INTO FLIGHT HYD RAULIC QUANTITY WAS 1.8 GALLONS. SEVENTEEN MINUTES LATER QUANTITY WAS 1.5. QUANTITY DROPPED 1.4 GALLONS IN 10 MINUTES. A IRCRAFT DIVERTED. ON APPROACH GEAR AND FLAPS UP QUANTITY 1.0 GALLONS, FLAPS/GEAR DOWN QUANTITY AT 0.8 GALLONS. HIGH PRES SURE FILTER 'O' RING REPLACED 'A' SYSTEM. 2 L 7 2 4F 4 F RT A16WE E2EA 1996120500379 19961205 00379 NM 1996 12 5 CA960604017 1 19960521 A 5300 AIRFRAME DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE PROP AIL & ELEV LIGHTNING STRIKE W K NONE C F.O.D. DE DESCENT 1 CA 17212 120584 (CAN) ON DESCENT AIRCRAFT HIT BY LIGHTNING. INSPECTION REVEALED THE LH PROP #1,2,4 BLADE HAD ARC MARKINGS ALONG THE AFT EDGE OF STAINLESS SHEATH ON FACE OF BLADES. #4 BLADE ALSO HAD TIP AND HEATER ELEMENT DAMAGE. RH PROP #1,3,4 BLADE HAD TI P ARCING AND #1 BLADE ALSO HAD A SMALL BLISTER ON FACE SIDE OF BLADE APPROXIMATELY 2 INCHES FROM TIP. TAIL STROBE LIGHT WAS FOUND BURNT. RADOME HAD SEVERAL SMALL PINHOLE BURN MARKS & ATTACHMENT SCREWS ARCED. OUTBOARD STATIC WICK BRACKET ON RH ELEVATOR HAD BURNT RIVETS. LH INBOARD FLAP HAD A RIVET BLOWN OUT 3/4" BEHIND REAR SPAR AT STA. Y81.67. 2 H 7 2 4T 4 T RT A13NM E20NE 1996120500382 19961205 00382 EA 1996 12 5 CA960605007 1 19960530 A 3246 WAL96 EYE BOLT EDO 557170A DHAV DHC3 DHC3 2800202 EA FLOATS ELONGATED W A K NONE O OTHER IN INSP/MAINT 1 CA 10000 977 (CAN) DURING ANNUAL INSPECTION OF FLOAT INSTALLATION, 2 OF 8 EYE BOLTS ATTACHING SPREADER BARS WERE FOUND BADLY ELONGATE D. SUSPECT CAUSE - CONSIDERED POOR MAINTENANCE AS SOME AME'S ARE TRYING TO REMOVE FLOAT ASSEMBLIES TIED TOGETHER WITH TH E SPREADER BARS. THEY NEED TO BE REMOVE INDIVIDUALLY. EYE BOLTS, BRACKETS AND SPREADERS ARE NOT DESIGNED TO HOLD FLOATS TOGETHER WHEN OFF AIRCRAFT. EXTREME BENDING AND SHEAR LOADS ARE APPLIED TO THOSE PARTS WHEN REMOVAL AND INSTALLATION OF THE FLOATS IS NOT CARRIED OUT PROPERLY. 1 H 7 1 3R A815 1996120500385 19961205 00385 SW 1996 12 5 CA960606003 1 19960530 A 2710 2771004073 LINKAGE SWRNGN SWRNGN SA227 SA227AC 8780603 SW AILERON CRACKED W A K NONE O OTHER IN INSP/MAINT 1 CA (CAN) AILERON LINKAGE ASSEMBLY FOUND CRACKED. IT IS SUSPECTED THAT LINKAGE HAD FILLED WITH FLUIDS AND THEN FROZE CAUSING IT SWELL AND CRACK. DRAIN HOLE FOUND FILLED WITH UNKNOWN SEALANT. 2 L 7 2 4T RT A8SW 1996120500387 19961205 00387 NM 1996 12 5 CA960606005 1 19960529 A 6123 M832481111 O-RING HAMSTD 8148291 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE PROP XSFER TUBE WORN W K NONE O OTHER IN INSP/MAINT 1 CA 1023 1023 LH120825 LH342 (CAN)DURING GROUND RUN, PROPELLER TOOK TOO LONG TO COME OUT OF FEATHER. "O" RINGS ON TRANSFER TUBES WORN AND DAMAGED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1996120500388 19961205 00388 EU 1996 12 5 CA960606010 1 19960527 A 5320 1412 FASTENER BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE MLG RH WELL SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA 15558 LF05741A (CAN) DURING ROUTINE INSPECTION OF MAIN LANDING GEAR RIGHT HAND WHEEL WELL FOUND 2 HYLOK FASTENERS SHEARED. 2 H 7 4 4F 4 F RT A49EU E6NE 1996120500389 19961205 00389 EA 1996 12 5 CA960610003 1 19960527 A 3230 858601 PSEU DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE NOSE GEAR FAILED W O OTHER J WARNING INDICATION NR NOT REPORTED 1 CA 5919 76 123029 (CAN) CREW ADVISED THAT A LANDING GEAR INOPERATIVE LIGHT WAS ON. ALTERNATE SELECTION TRIED BUT NO GOOD AS NOSE GEAR DID NOT COME DOWN.GEAR APPEARED TO BE HUNG UP ON DOORS. CREW RE-PULLED CABLE WHICH WAS SUCCESSFUL. THIS DIFFICULTY DUE TO SE QUENCING PROBLEM OF GEAR DOORS, BECAUSE OF FAILURE OF PROXIMITY SENSORS ELECTRONIC CONTROL (PSEU). 2 H 7 2 4T 4 T RT A13NM E20NE 1996120500391 19961205 00391 SW 1996 12 5 CA960610006 1 19960521 A 3243 35021834 SPRING WASHER A596 SWRNGN SA226 SA226TC 8780404 SW ARSRCH LEFT BRAKE VLV BROKEN W A O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA 12901 03453 (CAN) ON LANDING AIRCRAFT PULLED TO THE LEFT AND POWER WAS REQUIRED TO CLEAR RUNWAY. SMOKE NOTED COMING FROM LH BRAKES. LEFT HAND BRAKE WAS VERY HOT AND LEAKING FLUID. BOTH LH ASSEMBLIES AND WHEELS WERE REPLACED. CAPTAINS BRAKE MASTER CYLIN DER ASSEMBLY WAS REPLACED. ON DISASSEMBLY OF THE BRAKE THE VALVE RETURN SPRING WASHER WAS FOUND BROKEN IN HALF. THIS ALL OWED A HYDRAULIC LOCK TO DEVELOP. AS THE FLUID HEATED ADDITIONAL BRAKE PRESSURE WAS GENERATED. 2 L 7 2 4T RT A8SW 1996120500392 19961205 00392 SW 1996 12 5 CA960610007 1 19960603 A 7603 MS20392211 PIN SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP POWER LEVER FALLEN OUT W A E ENGINE SHUTDOWN G MULTIPLE FAILURE DE DESCENT 1 CA 26855 P54183 (CAN)ON DESCENT CREW UNABLE TO REDUCE POWER ON RH ENGINE BELOW 70 PERCENT. POWER LEVER JAMMED, BUT ABLE TO MOVE FREELY B ETWEEN 70 AND 100 PERCENT. ENGINE SHUTDOWN, BUT PROP WOULD NOT FEATHER. AIRCRAFT LANDED OK AT HIGHER THAN NORMAL SPEED. INSPECTION FOUND PIN SECURING STOP AND FEATHER PUSH PULL TO THE BELLCRANK ASSEMBLY (P/N 27-61002-001) HAD FALLEN OUT. CO TTER PIN HOLDING PIN HAD WORN THROUGH ALLOWING PIN TO FALL OUT. PIN HAD FALLEN BESIDE HYDRAULIC PUMP CAUSING POWER LEVER TO JAM AT 70 PERCENT POSITION. ALL FLEET TO BE EXAMINED. STEEL COTTER PINS TO BE REPLACED WITH STAINLESS STEEL PINS. 2 L 7 2 4T 4 T RT A8SW E4WE 1996120500393 19961205 00393 SW 1996 12 5 CA960610008 1 19960531 A 2740 L0316 MOTOR SIMMONDS DL5040M5 SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP PITCH TRIM FAILED W O OTHER O OTHER CR CRUISE 1 CA 2300 L0316 P54202 (CAN) THE COPILOTS PITCH TRIM ACTUATOR DROVE SLOWER THAN NORMAL AND POPPED THE CIRCUIT BREAKER. THE PITCH TRIM ACTUATOR REPLACED. ACTUATOR DID NOT HAVE THE NUTS AND SHAFT REPLACED WITH NEW PARTS AT THE LAST OVERHAUL AS REQUIRED BY AD 93-15- 02R1. THEREFORE THIS ASSEMBLY WAS SCHEDULED FOR OVERHAUL AT 3000 HOURS. 2 L 7 2 4T 4 T RT A8SW E4WE 1996120500395 19961205 00395 WP 1996 12 5 CA960610012 1 19960530 A 2910 1496452 MOTOR ASSY WHITTAKER 1496452 LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE HYD SOV ASSY LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 67 10292 (CAN) HYDRAULIC SHUTOFF VALVE AND MOTOR ASSEMBLY IS USED AS A FUSE FOR "A" SYSTEM RUDDER SYSTEM. FOR UNKNOWN REASON MOTO R HAS BEEN SPLIT FROM THE VALVE, CAUSING HYDRAULIC LEAK AND LOSS OF "A" SYSTEM FLUID. HAPPENED ON LANDING. REPLACED. 2 L 7 3 4F 4 F A23WE E12EU 1996120500398 19961205 00398 SO 1996 12 5 CA960611002 2 19960526 A 8520 CONROD CESSNA 310 310 2074202 CE CONT O470 O470B 17026 SO LEFT ENG BROKEN W A E UNSCHED LANDING ENGINE SHUTDOWN E R K VIBRATION/BUFFET PARTIAL RPM/PWR LOSS FLUID LOSS CR CRUISE 1 CA 1200 506956BR (CAN)IN CRUISE, LEFT ENGINE LOST POWER AND VIBRATED, SHUTDOWN. HOLE APPROXIMATELY 6 INCHES DIAMETER IN CRANKCASE. CONROD FAILED. 1 L 7 2 3O 3 O RT 3A10 E273 1996120500399 19961205 00399 EA 1996 12 5 CA960611003 1 19960604 A 3246 258240861 TORSION BAR BRSTOL 5500 DHAV DHC6 DHC6300 EA PWA PT6 PT6A27 52043 EA LH MAIN SKI FRACTURED W A K NONE O OTHER CL CLIMB 1 CA BA090 PCE40320 (CAN)AFTER TAKEOFF AND SELECTING SKI BUCKETS UP, THE PILOT OBSERVED THE L/H MAIN SKI HAD AN APPROXIMATE 15 DEGREE NOSE D OWN ATTITUDE. THE AFT TORSION BAR WAS FOUND FRACTURED. PRIOR TO DISCOVERY OF FAILED ROD, THE AIRCRAFT HAD BEEN STUCK AND TOOK A LOT OF EFFORT TO FREE. UNUSUAL LOADING MAY HAVE OCCURRED CONTRIBUTING TO THE FAILURE. CRACK ABOUT 3/8 INCHES HAD APPARENTLY PREVIOUSLY EXISTED. MAGNAFLUX INSPECTION ADDED TO THE 600 HOUR INSPECTION. 1 H 7 2 3T 4 T A9EA E4EA 1996120500400 19961205 00400 NM 1996 12 5 CA960611005 1 19960603 A 2910 82970410119 HYDRAULIC LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE WHEEL WELL CHAFED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA LH121075 (CAN)HYDRAULIC FLUID FOUND DRIPPING FROM LEFT WHEEL WELL. LINE FOUND CHAFED BETWEEN FIREWALL AND PRESSURE MANIFOLD. FLEX LINE INSTALLED. 2 H 7 2 4T 4 T RT A13NM E20NE 1996120500402 19961205 00402 NM 1996 12 5 CA960611007 1 19960509 A 3250 89925 LINK ROTOL DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NOSE WHEEL BROKEN W K NONE O OTHER TX TAXI/GRND HDL 1 CA PCE120358 (CAN)THE NOSE WHEEL STEERING WENT BEYOND THE STEERING LIMIT IN THE CORRECT DIRECTION. THE ADJUSTABLE FEMALE LINK BROKE A S A RESULT. 2 H 7 2 4T 4 T RT A13NM E20NE 1996120500404 19961205 00404 EA 1996 12 5 CA960612001 1 19960604 A 2760 82950010271 TUBE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE ROLL SPOILER BROKEN W H DEACTIVATE SYST/CIRCUITS K FLUID LOSS CR CRUISE 1 CA 123138 (CAN)LOSS OF #1 HYDRAULIC PRESSURE AND QUANTITY. FOUND RH INBOARD ROLL SPOILER LINE AT ACTUATOR BROKEN. 2 H 7 2 4T 4 T RT A13NM E20NE 1996120500405 19961205 00405 NE 1996 12 5 CA960612002 2 19960606 A 7210 BEARING DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE ENGINE MAKING METAL W K NONE J WARNING INDICATION IN INSP/MAINT 1 CA 17891 10908 120144 (CAN)METAL FLAKES FOUND ON RGB CHIP DETECTOR. ANALYSIS SHOWED IT TO BE M-50 BEARING MATERIAL. 2 H 7 2 4T 4 T RT A13NM E20NE 1996120500406 19961205 00406 NM 1996 12 5 CA960612003 1 19960605 A 2421 739515B GENERATOR BOEING 767 767375 NM LT RT IDG FAILED W H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION TX TAXI/GRND HDL 1 CA (CAN) ON RAMP, AFTER START, INTERMITTENT STATUS APPEARED "LIDG TEMP SENS". STATUS WENT OUT AND DID NOT OCCUR AGAIN. ON C LIMB OUT "RIDG TEMP SENS" STATUS MESSAGE INTERMITTENTLY ILLUMINATED AND WENT OUT. FIVE HOURS LATER "RIDG TEMP SENS" REAP PEARED ALONG WITH EICAS MESSAGE "R GEN DRIVE". RIGHT GENERATOR DRIVE DISCONNECTED AND APU STARTED. AIRCRAFT LANDED, MEL APPLIED, AIRCRAFT CONTINUED FLIGHT. IN CRUISE "LIDG TEMP SENS" APPEARED THEN LATER EICAS MESSAGE "L GEN DRIVE". REPLACED BOTH INTEGRATED DRIVE GENERATORS. 2 L 7 2 4F RT A1NM 1996120500407 19961205 00407 WP 1996 12 5 MWEA96637 1 19961122 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 756 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 DURING INSPECTION, FOUND LONGERON 2R CRACKED AT STA 756. MAINTENANCE INSTALLED SPLICE REPAIR IAW DOUGLAS SERVICE REWORK DRAWING NUMBER SR09530128. 2 L 7 2 4F A6WE 1996120500408 19961205 00408 WP 1996 12 5 MWEA96638 1 19961122 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 DURING INSPECTION, FOUND CRACK IN FUSELAGE SKIN AT LOWER AFT CORNER OF FWD AIRSTAIR DOOR CUTOUT. INSTALLED TEMPORARY RE PAIR IAW SRM 53-05 FIG 57A SHEET 2. WILL INSTALL PERMANENT REPAIR AT D-CHECK. 2 L 7 2 4F A6WE 1996120500409 19961205 00409 WP 1996 12 5 MWEA96639 1 19961124 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 1132 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 DURING C-CHECK, FOUND SKIN CRACKED AT STA 1132 ON LEFT SIDE NEAR RAIN GUTTER. INSTALLED SKIN SPLICE REPAIR IAW SRM 53-0 1 FIG 2 SHEET 3. 2 L 7 2 4F A6WE 1996120500410 19961205 00410 NM 1996 12 5 AWXA9600717 1 19961127 A 3397 WIRE BOEING 737 7373G7 1384595 NM CABIN LOOSE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 158AW 23780 DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT AT SEAT 19 INOPERATIVE. FOUND WIRE PULLED OUT OF SPLICE. R EPAIRED AS NEEDED, OPS CHECK GOOD STC - SA3432NM. 2 L 7 2 4F RT A16WE 1996120500411 19961205 00411 NM 1996 12 5 AWXA9600718 1 19961129 A 2721 CONNECTOR BOEING 757 7572S7 1384962 NM RUDDER TRIM DIRTY A AWXA K NONE F FLT CONT AFFECTED AP APPROACH 1 WP 28 901AW 23321 CREW REPORT ON FINAL, FIRST OFFICER REQUESTED CAPTAIN TO RETURN RUDDER TRIM TO ZERO. CAPTAIN REPORTED WITH TRIM AT 1.5 UNITS TO RIGHT, THE RUDDER TRIM WOULD NOT RESET. CAPTAIN SELECTED TO LEFT, NO MOVEMENT, RESELECTED TO RIGHT, NO MOVEMEN T. AIRCRAFT LANDED WITHOUT INCIDENT. CLEANED AND RESEATED THE C/PS ON THE AILERON AND RUDDER TRIM PANEL. OPERATIONS C HECK OK, NO FURTHER PROBLEMS. 2 L 7 2 4F RT A2NM 1996120500412 19961205 00412 EU 1996 12 5 AWXA9600719 1 19961129 A 3231 RETRACT MECH AIRBUS 320 A320231 3930325 EU MLG DOOR MALFUNCTIONED A AWXA O OTHER J WARNING INDICATION CL CLIMB 1 WP 28 636AW 098 ON TAKEOFF GEAR RETRACTION, ECAM L/G DOOR NOT OPEN. RECYCLED GEAR AND OPERATED NORMALLY. 2 L 7 2 4F RT A28NM 1996120500413 19961205 00413 1996 12 5 AWXA9600720 2 19961128 A 7321 79830015046 EEC AIRBUS 320 A320231 3930325 EU NR 2 ENGINE MALFUNCTIONED A AWXA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 WP 28 634AW 15226 4988 091 GOING THROUGH ABOUT 12,000 FEET AT ABOUT 280 KTS AND ACCELERATING, ECAM MESSAGE OF THRUST REVERSER NR 2 UNLOCKED CAME UP . ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNED TO PHX. REMOVED AND REPLACED NR 2 EEC. CYCLED THRUST REVERSER WITH ENGIN E RUNNING SEVERAL TIMES, ALL INDICATIONS NORMAL. 2 L 7 2 4F RT A28NM 1996120500414 19961205 00414 NM 1996 12 5 AWXA9600721 1 19961117 A 5320 6517688U165 MOPSILL BOEING 737 7373G7 1384595 NM PAX DOOR WAY CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 DURING ROUTINE MAINTENANCE CHECK, FOUND FWD ENTRY MOPSILL CORRODED BEYOND LIMITS, FWD ENTRY DOOR CUTOUT, WL 108. REMOVE D AND REPLACED MOPSILL PER SRM 53-10-15, 51-40-2. 2 L 7 2 4F RT A16WE 1996120500415 19961205 00415 NM 1996 12 5 AWXA9600722 1 19961118 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 520 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 DURING ROUTINE MAINTENANCE CHECK, FOUND BS 520 FLOORBEAM IS CRACKED IN RADIUS AT RBL 24.75. REPAIRED EXPANSION LINK AT STA 520, RBL 15 PER ER 3-53-13-11, TCO-PAN-96-1661RR AND 8110-3. 2 L 7 2 4F RT A16WE 1996120500416 19961205 00416 NM 1996 12 5 AWXA9600723 1 19961115 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 312 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 306AW 24633 DURING ROUTINE MAINTENANCE CHECK, FOUND FLOORBEAM STA 312 IS CORRODED LBL 10 TO LBL 45, WL 208. REMOVED UPPER CHORD OF BEAM FROM RBL 27 TO LBL 55, FABRICATED NEW CHORD AND INSTALLED REPAIR PARTS PER SRM 53-10-51, FIG 205. 2 L 7 2 4F RT A16WE 1996120500417 19961205 00417 1996 12 5 CALA9601716 4 19961202 A 2565 11331DGDME SLIDE DOUG DC9 DC932 3022066 WP L1 DOOR LOW PRESSURE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18513 23051 2674 48112 INSPECTION FOUND THE L-1 DOOR EMERGENCY SLIDE PRESSURE LOW. THE SLIDE WAS REMOVED AND REPLACED. 2 L 7 2 4F A6WE 1996120500418 19961205 00418 NE 1996 12 5 CALA9601717 2 19961201 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 1 FOD A A CALA A UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 SW 09 71828 49488 717444 THE NR 1 ENG AUTO SHUTDOWN WHILE CRUISING AT 31,000 FT. THE A/C WAS DIVERTED TO PHX WHERE IT LANDED WITHOUT INCIDENT. I NSPECTION FOUND ICE BUILD-UP IN FORWARD LAV PANEL. BLUE ICE WAS SUSPECTED AS CAUSE OF ENGINE FAILURE. THE 6TH, 7TH, 8TH AND 13TH STAGES OF NR 1 ENG COMPRESSOR WERE BORESCOPED WITH NO DAMAGE FOUND. THE NR 1 ENG WAS RUN TO TAKEOFF POWER AND ALL PARAMETERS WERE NORMAL. THE FORWARD LAV WAS FLUSHED SEVERAL TIMES AND SERVICED WITH BLUE WATER, NO LEAKS WERE DETEC TED. NO SPECIFIC PART WAS IDENTIFIED AS FAILED. THE FILL CHECK VALVE, TOILET TANK DRAIN VALVE, LAV FLUSH MOTOR AND LAV WASTE DRAIN VALVE WERE REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. 2 L 7 2 4F 4 F A6WE E9NE 1996120500419 19961205 00419 SW 1996 12 5 COMA9620018 1 19961202 A 7712 2719158007 TQ INDICATOR SWRNGN SA227 SA227AC 8780603 SW INST PANEL DEFECTIVE A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 703CA 10271 667 AC703 LEFT ENGINE TORQUE INDICATOR FAILED DURING TAKEOFF, CIRCUIT BREAKER TRIPPED. REPLACED TORQUE INDICATOR. 2 L 7 2 4T RT A8SW 1996120500420 19961205 00420 EU 1996 12 5 COMA9630161 1 19961202 A 3260 INTRANSIT LIGHT SAAB SF340 SF340A 7850100 EU LANDING GEAR MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 357CA 340A044 LANDING GEAR INTRANSIT LIGHT REMAINED ON AFTER GEAR RETRACTION. COULD NOT DUPLICATE DISCREPANCY. INSPECTION AND OPERAT IONAL CHECKS OF LANDING GEAR SATISFACTORY. 2 L 7 2 4T RT A52EU 1996120500421 19961205 00421 EA 1996 12 5 COMA9660217 1 19961202 A 3510 MF100801 MASK CNDAIR CL600 CL6002B19 EA COPILOT WILL NOT TEST A COMA K NONE O OTHER CR CRUISE 1 SO 01 958CA 7111 COPILOTS OXYGEN MASK DOES NOT TEST PROPERLY. REPLACED OXYGEN MASK. 2 L 7 2 4F RT A21EA 1996120500422 19961205 00422 NM 1996 12 5 96UAL900774 1 19961007 A 5411 313W3750 FRAME BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 2 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 767UA 26918 NR 2 PYLON STRUT AFT FAIRING FRAME NR 5 INBOARD ATTACH FITTING CRACKED. *S/D* FITTING WAS ADJACENT TO PREVIOUSLY REPLA CED FITTING. SUSPECT PRELOAD CONDITION INTRODUCED DURING REPLACEMENT. DAMAGED FITTING REPLACED AND SENT TO BOEING FOR ANALYSIS. REPLACEMENT ANGLE SHIMMED TO AVOID PRELOAD CONDITION. 2 L 7 2 4F 4 F RT T0001SE E46NE 1996120500423 19961205 00423 1996 12 5 96UAL900878 4 19961119 A 2565 7A1323107 SLIDE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN FAILED TEST A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 184UA 394 25380 SLIDE REMOVED FOR INADVERTANT DEPLOYMENT. DURING OVERHAUL, SLIDE FAILED AIR RETENTION TEST DUE TO POROSITY. SCRAPPED S LIDE AND INSTALLED NEW SLIDE. 2 L 7 4 4F 4 F RT A20WE E24NE 1996120500424 19961205 00424 NE 1996 12 5 96UAL900879 2 19961119 A 7230 FAN ROTOR DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 1 ENGINE OUT OF BALANCE A UALA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 WP 29 1853U 47812 NR 1 ENGINE VIBRATES STARTING AROUND 92 PERCENT N1 AND INCREASES IN INTENSITY. AROUND 95-96 PERCENT NI, IT APPEARS TO H AVE A PHASE OR OUT OF SYNC. BEAT. TURNING OFF BLEEDS, HYDRAULIC OR ELECTRICAL POWER HAS NO EFFECT. VIBRATION WAS ISOL ATED TO THE FAN ROTOR. TRIM BALANCE OF THE FAN WAS PERFORMED REDUCING THE VIBRATION LEVEL TO WITHIN ACCEPTABLE LIMITS. 2 L 7 3 4F 4 F A22WE E23EA 1996120500425 19961205 00425 WP 1996 12 5 96UAL900880 1 19961119 A 2760 4913802BT06328 CONTROL CABLE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE LT SPOILER BROKEN A UALA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 WP 29 1858U 46987 ON FLIGHT CHECK DURING TAXI OUT, LEFT HAND SPOILER INDICATED ONLY PARTIAL EXTENSION. *S/D* FOUND SPOILER CABLE 11B, LT SPOILER 1, 4 AND 5 UP BROKEN. REPLACED CABLE. 2 L 7 3 4F 4 F A22WE E23EA 1996120500426 19961205 00426 NM 1996 12 5 96UAL900881 1 19961119 A 2150 213W212010 DUCT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LT PACK CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 773UA 26929 LEFT AIR CONDITIONING PACK INLET DUCT HAS HOLE 2.5 INCHES LONG BY 1 INCH WIDE. HOLE IS AT THE END OF A FOUR INCH LONG C RACK EXTENDING FROM WELDED BOSS. *S/D* FAILURE ATTRIBUTED TO FATIGUE CRACK ASSOCIATED WITH PITTING CAUSED BY ELECTRIC WELDING ARC STRIKE DURING MANUFACTURE. PROCESS CHANGES HAVE BEEN IMPLEMENTED TO AVOID FUTURE PROBLEMS. FLEETWIDE INSPE CTION PROJECT INITIATED TO ADDRESS SUSPECT PARTS. 2 L 7 2 4F 4 F RT T0001SE E46NE 1996120500427 19961205 00427 NM 1996 12 5 96UAL900882 1 19961119 A 3350 P4010021 BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7275U 21422 FORWARD CABIN LEFT OUTBOARD EMERGENCY FLASHLIGHT RED LIGHT DOES NOT BLINK. *S/D* BATTERY DISCHARGED. REPLACED BATTERY ASSEMBLY. 2 L 7 3 4F 4 F A3WE E2EA 1996120500428 19961205 00428 NM 1996 12 5 96UAL900883 1 19961119 A 2710 CONTROL SYST BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE AILERONS OUT OF ADJUST A UALA K NONE O OTHER NR NOT REPORTED 1 WP 29 7291U 21569 AILERON CONTROL WHEEL FORCES HAVE EXCESSIVE DEAD BAND OR LACK OF FEEL EITHER SIDE OF NEUTRAL IN LANDING CONFIGURATION. E SPECIALLY NOTICEABLE, ALSO STIFF. *S/D* AILERON SYSTEM RERIGGED. AIRCRAFT TEST FLOWN AND THERE WAS NO EVIDENCE OF A D EAD BAND OR STIFFNESS IN THE AILERON SYSTEM. 2 L 7 3 4F 4 F A3WE E2EA 1996120500429 19961205 00429 WP 1996 12 5 96UAL900884 1 19961119 A 5270 WARNING SYST DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE CARGO DOOR INOPERATIVE A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 1859U 47819 CENTER CARGO DOOR A-LOOP INDICATING SYSTEM INOPERATIVE. *S/D* CYCLED DOOR SEVERAL TIMES AND COULD NOT DUPLICATE. 2 L 7 3 4F 4 F A22WE E23EA 1996120500430 19961205 00430 NM 1996 12 5 96UAL900885 1 19961119 A 3350 M955 BATTERY PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7290U 21568 LEFT AFT EXTERIOR OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK. 2 L 7 3 4F 4 F A3WE E2EA 1996120500431 19961205 00431 WP 1996 12 5 96UAL900886 1 19961119 A 2170 21D10011 COALESCER BAGS DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE CABIN DIRTY A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 1858U 46987 VERY STRONG ODOR IN CABIN AFTER TAKEOFF WITH PNEUMATIC AND RECIRCULATION FANS ON. REPLACED COALESCER BAGS, ACCOMPLISHED ENGINE RUN AND THERE WAS NO SMELL. 2 L 7 3 4F 4 F A22WE E23EA 1996120500432 19961205 00432 NM 1996 12 5 96UAL900887 1 19961119 A 2612 17051 FIRE LOOP LINDBERG BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE NR 2 ENGINE DEFECTIVE A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 9038U 19076 TWENTY MILES OUT OF GRR HAD FIRE WARNING FLICKER ON NUMBER TWO ENGINE. ON FINAL 2 MILES OUT, FIRE WARING LIGHT CAME ON SOLID AND NUMBER TWO ENGINE EXHAUST GAS TEMPERATURE APPEARED TO START RISING. SHUT DOWN NUMBER TWO ENGINE AND FIRED BOT TLES, EVACUATED AIRCRAFT ON RUNWAY. *S/D* FOUND NR 2 ENGINE FIRE DETECTION LOWER LOOP DEFECTIVE. FOUND ELEMENT FAILED INTERNALLY. REPLACED NR 2 ENGINE FIRE DETECTION LOWER LOOP AND TESTED SYSTEM, CHECKS OK. 2 L 7 2 4F 4 F A16WE E2EA 1996120500433 19961205 00433 NM 1996 12 5 96UAL900888 1 19961119 A 2910 BACH5R0260DDN HOSE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE B HYD SYSTEM LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 7466U 21920 AFTER TAKEOFF HAD SUDDEN LOSS OF B-HYDRAULIC SYSTEM. RETURNED TO DEN. FOUND B-SYSTEM HYDRAULIC RETURN LINE LEAKING. A LSO, FOUND FLEX LINE ON RIGHT SIDE OF ELEVATOR PCU LEAKING. REPLACED BOTH LINES. ALSO, REPLACED BOTH NR 1 AND NR 2 MOT OR DRIVEN HYDRAULIC PUMPS AND CASE DRAIN FILTERS. 2 L 7 3 4F 4 F A3WE E2EA 1996120500434 19961205 00434 NM 1996 12 5 96UAL900889 1 19961119 A 4920 36069821 TURBINE WHEEL BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE APU CRACKED A UALA K NONE O OTHER NR NOT REPORTED 1 WP 29 7294U 6490 21572 LOUVER ASSEMBLY AND EXHAUST DUCTS DAMAGED WHEN TURBINE BROKE OFF FROM THE APU. *S/D* UNITED NO LONGER USES (P/N 360698 2-1) AND NOW USES(P/N 3842072-2 OR - 3). THE PROBLEM HAS BEEN ADDRESSED AND ALL MEANS OF INSPECTION AND REPAIR OF SADDL E CRACKS ARE IN PLACE. THE 98CK APU BEING INSTALLED ON 727-222 AIRPLANES HAS TAILPIPES WITH CENTER BODIES INSTALLED TO PREVENT RELEASE OF SHRAPNEL IN CASE OF TURBINE WHEEL DISPERSEMENT. 2 L 7 3 4F 4 F A3WE E2EA 1996120500435 19961205 00435 WP 1996 12 5 96UAL900890 1 19961119 A 3350 582215 BATTERY PACK DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN DISCHARGED A UALA K NONE L NO TEST DE DESCENT 1 WP 29 1838U 46632 EMERGENCY LIGHTS IN BACK OF AIRPLANE CAME ON AFTER DESCENT. *S/D* REPLACED AFT BATTERY PACK. 2 L 7 3 4F 4 F A22WE E23EA 1996120500436 19961205 00436 NM 1996 12 5 96UAL900891 1 19961119 A 5610 WINDOW BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LT COCKPIT AIR LEAK A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 346UA 24250 AIRCRAFT FAILED TO PRESSURIZE AFTER TAKEOFF AND CAPTAIN'S SLIDING WINDOW NOISY. PRESSURIZED AIRCRAFT TO 6 PSI, NO LEAK S. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 1996120500437 19961205 00437 NM 1996 12 5 96UAL900892 1 19961121 A 3010 285W0020101 ASG CARD BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE ANTI-ICE SYST MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 776UA 26937 CREW REPORTS EICAS MESSAGE FOR WING ANTI-ICE THREE HOURS AFTER DEPARTURE. RETURNED TO IAD. *S/D* REPLACED AIRFOIL AND COWL ICE PROTECTION SYSTEM CARD, PASSED TEST. PROBLEM REOCCURRED SEVERAL FLIGHTS LATER. REPLACED POWER SUPPLY UNIT LI NEAR MONITOR A3 PER AMM 31-09-01 AND LEFT ARINC SIGNAL GATE (ASG) CARD PER AMM 31-09-02. 2 L 7 2 4F 4 F RT T0001SE E46NE 1996120500438 19961205 00438 NM 1996 12 5 96UAL900893 1 19961121 A 3233 65B015028 ACTUATOR BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE RT MLG CORRODED A UALA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 WP 29 165UA 21658 AFTER TAKEOFF, GEAR COULD NOT BE RETRACTED. RETURNED TO FIELD. MAINTENANCE FOUND RIGHT BODY GEAR RETRACT ACTUATOR FAIL ED. ACTUATOR ROD END PULLED FREE FROM PISTON HOUSING DUE TO STRIPPED THREADS WHICH WERE CORRODED. REPLACED RIGHT BODY GEAR ACTUATOR. 2 L 7 4 4F 4 F A20WE E20EA 1996120500439 19961205 00439 1996 12 5 96UAL900894 4 19961121 A 2565 HOSE BFGOODRICH 5LD23102400 DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL SLIDE CRACKED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 1811U N0079 46610 SLIDE WAS INADVERTANTLY DEPLOYED AND THE SLIDE PORTION OF THE SLIDE/RAMP DID NOT FULLY INFLATE. THE SLIDE INFLATION HOS ES WERE FOUND TO BE BROKEN IN SEVERAL PLACES AND METAL FITTING WAS CRACKED. REPLACED HOSES AND SLIDE INFLATED SATISFACT ORILY. SENT HOSES TO VENDOR FOR ANALYSIS. 2 L 7 3 4F 4 F A22WE E23EA 1996120500440 19961205 00440 NM 1996 12 5 96UAL900895 1 19961121 A 2150 32021221 CHECK VALVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT PACK FAILED A UALA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 WP 29 657UA 27112 THE RIGHT PACK WAS NOISY AND CAUSING A VIBRATION IN THE FORWARD CABIN DURING THE FLIGHT. THE AIRCRAFT DIVERTED TO JFK. *S/D* THE NOISE AND VIBRATION WAS CAUSED BY A LOOSE FLAPPER IN THE SUPPLY FAN CHECK VALVE. THE CHECK VALVE WAS REPLAC ED PER MM 21-58-02, OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 1996120500441 19961205 00441 1996 12 5 96UAL900896 4 19961122 A 3414 405112 SWITCH GUARD BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE E/E BAY MISALIGNED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 602UA 21863 DIVERTED TO DEN DUE TO THE CAPTAIN AND FIRST OFFICER'S VMO-MACH WARNING INDICATOR BOTH STUCK AT 265 KNOTS. *S/D* THE V MO-MACH ALT GUARD SWITCH WAS FOUND SAFETIED IN THE ALT POSITION. REPOSITIONED SWITCH TO NORMAL, OPERATIONS CHECK NORMAL . 2 L 7 2 4F 4 F RT A1NM E3NE 1996120500442 19961205 00442 NM 1996 12 5 96UAL900897 1 19961125 A 2750 Y35A RVDT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FLIGHT DECK FAILED A UALA K NONE F FLT CONT AFFECTED LD LANDING 1 WP 29 660UA 27115 LANDED IN SFO UNDER AMBER ALERT DUE TO FLAP EXTENSION PROBLEM. *S/D* THE ROTARY VARIABLE DIFFERENTIAL TRANSFORMER FLAP LEVER FAILED. REPLACED ROTARY VARIABLE DIFFERENTIAL TRANSFORMER PER MM 27-51-26, OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 1996120500443 19961205 00443 NM 1996 12 5 96UAL900898 1 19961125 A 3350 CONNECTOR BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 610UA 21871 TWENTY-FIVE PERCENT OF EMERGENCY EXIT LIGHTS FOUND INOPERABLE IN THE AFT CABIN. SECURED LOOSE EEL STRIP CONNECTION, OPE RATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 1996120500444 19961205 00444 NM 1996 12 5 96UAL900899 1 19961125 A 2421 GENERATOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RIGHT MALFUNCTIONED A UALA O OTHER J H WARNING INDICATION ELECT. POWER LOSS-50 PC CL CLIMB 1 WP 29 769UA 26921 DURING CLIMB, RIGHT GENERATOR OFF LIGHT ILLUMINATED. ATTEMPTED ONE RESET PER HANDBOOK, DID NOT RESET. STARTED APU AND CONTINUED. 2 L 7 2 4F 4 F RT T0001SE E46NE 1996120500445 19961205 00445 NE 1996 12 5 96UAL900900 2 19961125 A 7230 COMPRESSOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 3 ENGINE STALLED A UALA A E J UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 29 186UA 26875 724376 NR 3 ENGINE STALLED ON TAKEOFF JUST AFTER LIFTOFF. A/C RETURNED TO FIELD. NO VISIBLE DAMAGE. NO CONTROL SYSTEM FAULT S. SURGE IS ATTRIBUTED TO POOR N2 COMPRESSOR PERFORMANCE. ENGINE TO BE REFURBISHED. ENGINE REPLACED. 2 L 7 4 4F 4 F RT A20WE E24NE 1996120500446 19961205 00446 NE 1996 12 5 96UAL900901 2 19961125 A 7200 ENGINE BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE NR 1 MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 9007U 19045 NR ONE ENGINE OIL FILTER BYPASS LIGHT CAME ON AFTER TAKEOFF. RETARDED THROTTLE AND LIGHT WENT OUT. RETURNED TO ORD. R EPLACED NR 1 ENGINE DUE TO CHRONIC OIL FILTER BYPASS LIGHT. REPLACED F/O COOLER AND OIL TANK. OPS CHECK GOOD. 2 L 7 2 4F 4 F A16WE E2EA 1996120500447 19961205 00447 NM 1996 12 5 96UAL900902 1 19961126 A 3230 6544625 LOCK ACTUATOR BOEING 737 737291 138448W NM PWA JT8 JT8D9A 52048 NE NLG FAILED A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 979UA 21544 WHEN GEAR HANDLE PUT IN THE UP POSITION, GOT NOSE LANDING GEAR UNSAFE LIGHT. NOSE LANDING GEAR DID NOT RETRACT, CYCLED HANDLE AND NO HELP. NOSE GEAR WAS STUCK DOWN AND LOCKED. *S/D* LOWER END OF THE NLG LOCK ACTUATOR FRACTURED. REPLACE D ACTUATOR AND ACCOMPLISHED NLG RETRACTION TEST, OPS CHECK GOOD. 2 L 7 2 4F 4 F A16WE E2EA 1996120500448 19961205 00448 NM 1996 12 5 96UAL900903 1 19961126 A 2760 69268661 ROD END BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 10 SPOILER OUT OF ADJUST A UALA O OTHER F FLT CONT AFFECTED CR CRUISE 1 WP 29 7259U 21406 AIRCRAFT REQUIRES 2 DEGREES LEFT WING DOWN AILERON TRIM FOR STRAIGHT AND LEVEL FLIGHT WITH ZERO DEGREE RUDDER TRIM. *S/ D* FOUND THAT AIRCRAFT WAS EXPERIENCING SPOILER FLOAT ON THE NR 10 FLIGHT SPOILER. REPLACED AND ADJUSTED ROD END, TRI M IMBALANCE ELIMINATED. 2 L 7 3 4F 4 F A3WE E2EA 1996120500449 19961205 00449 NE 1996 12 5 96UAL900905 2 19961127 A 7230 COMPRESSOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 1 ENGINE STALLED A UALA A E J UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL J M WARNING INDICATION OVER TEMP CL CLIMB 1 WP 29 190UA 26879 717604 AFTER TAKEOFF, NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL AND HIGH EGT. SHUT DOWN ENGINE, DUMPED FUEL AND RETURNED TO F IELD. *S/D* ENGINE REPLACED, NO VISIBLE DAMAGE FOUND, NO CONTROL SYSTEM FAULTS. COMPRESSOR STALL ATTRIBUTED TO LOW N2 COMPRESSOR PERFORMANCE. ENGINE REFURBISHED. 2 L 7 4 4F 4 F RT A20WE E24NE 1996120500451 19961205 00451 WP 1996 12 5 96UAL900907 1 19961127 A 5297 WIRE DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL 3 L DOOR FAILED A UALA O OTHER L NO TEST IN INSP/MAINT 1 WP 29 1825U 46624 DOOR 3L NO TEST LIGHT, INOPERATIVE. REPAIRED BROKEN WIRE, CHECKS OK. 2 L 7 3 4F 4 F A22WE E23EA 1996120500452 19961205 00452 WP 1996 12 5 96UAL900908 1 19961127 A 3240 JAD9F008 RELAY DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE BRAKE VALVE INOPERATIVE A UALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 29 1857U 46986 ON CLEARING RUNWAY COULD NOT TAXI BECAUSE OF LOCKED BRAKES . FOUND PARKING BRAKE VALVE NOT GETTING POWER TO OPEN VALVE. REPLACED PARKING BRAKE MOTOR VALVE RELAY. SYSTEM CHECKED OKAY. 2 L 7 3 4F 4 F A22WE E23EA 1996120500453 19961205 00453 WP 1996 12 5 96UAL900909 1 19961127 A 2120 AIR DISTR DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 1825U 46624 PUNGENT ODOR-SMOKE IN AIRCRAFT ON ENGINE PNEUMATICS AFTER ENGINE START. SHOP MECHANIC REPLACED APU COOLING FAN. UNIT W AS NOT LEAKING OIL AND WAS NOT THE CAUSE OF ODOR-SMOKE IN CABIN. SUSPECT DE-ICING FLUID INGESTION THROUGH APU. 2 L 7 3 4F 4 F A22WE E23EA 1996120500454 19961205 00454 WP 1996 12 5 SCNA96396 1 19961107 A 3211 ARG7696 BEARING DOUG DC10 DC1010 3022110 WP LT MLG SCORED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 572SC 46977 DURING HEAVY MAINTENANCE, FOUND LEFT HAND MAIN LANDING GEAR UPPER BEARING ASSEMBLY SCORED AND GOUGED. REMOVED AND REPLA CED LEFT HAND MAIN LANDING GEAR UPPER BEARING ASSEMBLY IN ACCORDANCE WITH CMM 32-11-04. 2 L 7 3 4F A22WE 1996120500455 19961205 00455 WP 1996 12 5 SCNA96397 1 19961119 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP CARGO COMPT CORRODED A SCNA K - NONE O OTHER IN INSP/MAINT 1 GL 15 572SC 46977 DURING HEAVY MAINTENANCE FOUND AFT CARGO PIT LEFT HAND FORWARD OUTBOARD CARGO TRACK HAS EXFOLIATION CORROSION. REMOVED AND REPLACED SEAT TRACK IN ACCORDANCE WITH SRM 51-33-01 AND 53-70-00 FIGURE 2. 2 L 7 3 4F A22WE 1996120500456 19961205 00456 WP 1996 12 5 SCNA96398 1 19961119 A 5320 SPLICE DOUG DC10 DC1010 3022110 WP BS 1801-1821 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 572SC 46977 DURING HEAVY MAINTENANCE, FOUND LONGERON 46R SPLICE CORRODED BETWEEN FRAMES AT BS 1801 THROUGH BS 1821. REMOVED LONGERO N SPLICE, FABRICATED AND INSTALLED A NEW SPLICE IN ACCORDANCE WITH SRM 51-33-01. 2 L 7 3 4F A22WE 1996120500457 19961205 00457 NM 1996 12 5 SCNA96399 1 19961126 A 3350 900542 POWER SUPPLY BOEING 727 7272J4 1384006 NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 FOUND RIGHT FORWARD AND AFT OVERWING EMERGENCY EXIT SIGNS INOP. REMOVED AND REPLACED RIGHT FORWARD AND AFT OVERWING EME RGENCY EXIT POWER SUPPLY AND OPS CHECKED GOOD. 2 L 7 3 4F RT A3WE 1996120500458 19961205 00458 NM 1996 12 5 SCNA96400 1 19961126 A 3397 WIRE BOEING 727 7272J4 1384006 NM CABIN OPEN A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 FOUND AFT FLOOR TRACK LIGHTS INOP NEAR GALLEY. REPAIRED WIRING IN TRACK AND OPS CHECKED GOOD. 2 L 7 3 4F RT A3WE 1996120500459 19961205 00459 NM 1996 12 5 SCNA96401 1 19961130 A 3350 S106 BATTERIES BOEING 727 7272A1 138407F NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 286SC 21601 FOUND CEILING MOUNTED EMERGENCY AREA LIGHT IN FORWARD CABIN INOP. REMOVED AND REPLACED BATTERIES FOR AREA LIGHT IN ACCO RDANCE WITH MM 33-50-81 AND OPS CHECKED NORMAL. 2 L 7 3 4F A3WE 1996120500460 19961205 00460 WP 1996 12 5 DHL96805006 1 19961127 A 2711 YP212 BOLT DOUG DC8 DC873F 302199F WP AILERON TAB LOOSE A DHLA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 805DH 46125 NEED 1.5 UNITS OF AILERON AND 1 UNIT OF RUDDER TRIM FOR LEVEL FLIGHT. FOUND BOLT LOOSE ON LT AILERON TAB. TIGHTENED BO LT, OPS CHECK OK. 2 L 7 4 4F RT 4A25 1996120500461 19961205 00461 NM 1996 12 5 DHL96703005 1 19961126 A 2782 1U109592 ACTUATOR BOEING 727 72730C 1384009 NM NR 1 LE SLAT FAILED A A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 703DH 19010 NR 1 L/E WOULD NOT RETRACT WHEN FLAPS SELECTED FROM ZERO. REMOVED AND REPLACED L/E SLAT ACTUATOR OPS AND LEAK CHECK OK. 2 L 7 3 4F A3WE 1996120500462 19961205 00462 WP 1996 12 5 DHL96802006 1 19961201 A 3260 6F83402 STRIKER PLATE DOUG DC8 DC873F 302199F WP RT MLG BROKEN A DHLA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 802DH 46076 RIGHT GEAR DOOR UNSAFE LIGHT CAME ON WHILE PERFORMING GEAR CHECK. REMOVED AND REPLACED BROKEN RIGHT HAND MAIN LANDING G EAR DOOR SWITCH STRIKER PLATE. 2 L 7 4 4F RT 4A25 1996120500463 19961205 00463 1996 12 5 DHL96803005 4 19961129 A 3442 20671570153 RT UNIT DOUG DC8 DC873F 302199F WP E/E COMPT MALFUNCTIONED A DHLA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 803DH 46123 CAPTAINS RADAR SCREEN IS SPOKING AT 12:30 POSITION FIRST OFFICERS RADAR SCREEN IS COMPLETELY CLOUDED UNABLE TO PAINT GRO UND ON EITHER SCREEN. REMOVED AND REPLACED RADAR RT UNIT, OPS CKD PER MM 34-41-0. 2 L 7 4 4F RT 4A25 1996120500464 19961205 00464 1996 12 5 DHL96803006 4 19961130 A 3442 2067565680501 ANTENNA DOUG DC8 DC873F 302199F WP FWD FUSELAGE MALFUNCTIONED A DHLA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 803DH 46123 CAPT AND FIRST OFFICER RADAR INDICATOR SPOKE AT 11:30 POSITION. RADAR WILL NOT PAINT RETURNS ON GROUND WHILE IN AIR. T EST INDICATIONS NORMAL WHILE IN AIR AND ON GROUND. REMOVED AND REPLACED RADAR R/T PER MM 34-45-0. REMOVED AND REPLACED RADAR ANT PER MM 34-45-1, OPS CK RADAR SYS PER MM 34-45-0. 2 L 7 4 4F RT 4A25 1996120500465 19961205 00465 NE 1996 12 5 P5CA9600973 2 19961130 A 7200 3440330A221 ENGINE BOEING 747 747132 1384882 NM PWA JT9 JT9D7A 52054 NE NR 3 MALFUNCTIONED A A P5CA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 23 857FT 20246 662376 WHEN THROTTLES REDUCED FOR DESCENT, OIL QUANTITY DROPPED TO ZERO AND PRESSURE DROPPED TO 30 PSI OIL PRESSURE STAYED ABOV E 20 PSI REST OF FLIGHT, AFTER ENGINE SHUT DOWN IAW ALTERNATE PROCEDURES. AFTER SHUT DOWN OIL QUANTITY CAME BACK TO 4.2 GALLONS. RESTARTED OIL PRESSURE OK 44 PSI, THEN OIL QUANTITY DROPPED TO 1 GALLON PRESSURE FLUCTUATED 34 TO 39 PSI. MO TORED ENGINE OIL TANK SERVICED WITH 2 QUARTS OF OIL, CHECKED OIL FILTER, NO CONTAMINATION. CHECKED CHIP DETECTORS, NO C ONTAMINATION. REPLACED OIL PRESSURE TRANSMITTER PRECAUTIONARY PER M/M 79-31-00. RUNUP AND ALL PARAMETERS NORMAL PER M/ M 71-00-00. POLAR REPLACED ENGINE LATER DUE TO REPEAT OF PROBLEM. 2 L 7 4 4F 4 F A20WE E20EA 1996120500467 19961205 00467 NM 1996 12 5 P5CA9600975 1 19961130 A 5753 SKIN BOEING 747 747122 1384872 NM RT TE FLAP MISSING A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 RIGHT OUTBOARD TRAILING EDGE FLAP LOWER SURFACE OF MID-FLAP LEADING EDGE HAS APPROXIMATELY 2.5 INCH BY 3 FOOT SECTION OF SKIN MISSING WITH EXPOSED HONEY COMB DAMAGED AND PROTRUDING, AREA SURROUNDING THE MISSING MATERIAL SOFT. REPAIRED PER BOEING SRM 51-40-07. 2 L 7 4 4F A20WE 1996120500468 19961205 00468 NM 1996 12 5 P5CA9600976 1 19961123 A 5730 PANEL BOEING 747 747122 1384872 NM LT WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 A 4 INCH CRACK ON LEFT WING LOWER, PANEL FORWARD OF WING GEAR DOOR CUTOUT. REPAIRED PER BOEING SRM 51-40-06. 2 L 7 4 4F A20WE 1996120500469 19961205 00469 WP 1996 12 5 RRXA96165 1 19961120 A 3310 LIGHT BALLAST DOUG DC8 DC873 302199C WP COCKPIT FAILED A RRXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 15 105WP 46095 DURING FLIGHT, THE FLT CREW OBSERVED AN INTERMITTENT SMELL OF HOT ELECTRICAL WIRING. MAINTENANCE TRANSFERRED THE GLARES HIELD LIGHTING BALLAST TO THE DMI LIST IAW MEL 33-1. MAINTENANCE REMOVED AND REPLACED THE FLUORESCENT BALLAST, OPERATIO NAL CHECK OF LIGHTING SYSTEM WAS GOOD. 2 L 7 4 4F RT 4A25 1996120500470 19961205 00470 WP 1996 12 5 RRXA96166 1 19961130 A 2910 HYD LINE DOUG DC8 DC873F 302199F WP RUDDER FAILED A RRXA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 15 961R 46133 AFTER LEVEL OFF HYD QTY WENT FROM FULL TO THE 'A', SLOW LEAK REST OF FLIGHT. ON DESCENT AND LANDING QTY WENT TO BOTTOM OF NORMAL. RAN LOSS OF HYD QTY CHECKLIST, N961R TOWED TO RAMP. MAINTENANCE REMOVED AND REPLACED FLEX LINE TO RUDDER AU X PUMP IAW DC8 MM 29-00. 2 L 7 4 4F RT 4A25 1996120500471 19961205 00471 WP 1996 12 5 ARWA9611008 1 19961129 A 2120 S43C51 CLAMP DOUG DC8 DC862 3021970 WP CABIN LOOSE A ARWA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 19 1808E 46105 DURING EARLY CLIMB, HEARD A BANG BELOW THE FLOOR. CABIN RATE OF CLIMB WENT TO 2,000 FPM UP. UNABLE TO PRESSURIZE ACFT. FOUND LOOSE CLAMP ON DELIVERY DUCT, SECURED SAME. PRESSURIZED ACFT, OPS NORMAL IAW 21-30. 2 L 7 4 4F 4A25 1996120500472 19961205 00472 1996 12 5 ARWA9612001 4 19961201 A 3418 C267072 LIFT TRANSDUCER DOUG DC8 DC863F 302198F WP RT WING INOPERATIVE A ARWA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 19 441J 45988 ON TAKEOFF, STALL SHAKER CAME ON, TWICE. ABORTED TAKEOFF AT 298,000 LBS. REMOVED AND REPLACED LIFT TRANSDUCER PER MM 3 4-16-0. ADJUSTMENT TEST 501, CODE 2, UNABLE TO DUPLICATE FAIL, FOUND NORMAL. PERFORMED OVERWEIGHT LANDING INSP, NO STR UCTURAL DEFECTS NOTED. 2 L 7 4 4F 4A25 1996120500473 19961205 00473 WP 1996 12 5 CKSA96198 1 19961124 A 5751 DOUBLER DOUG DC8 DC863F 302198F WP RT AILERON DENTED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND RIGHT WING AILERON HAS DENT ON UPPER LEADING EDGE. REPAIRED RIGHT HAND OUTBOARD AILE RON BY INSTALLING DOUBLER IAW EA 96-326 EER D8-05081 AND AIA 8110-3. CORROSION CARD NR 111R-0551, NON-ROUTINE TASK CARD NR 87357. 2 L 7 4 4F 4A25 1996120500474 19961205 00474 WP 1996 12 5 CKSA96199 1 19961124 A 5730 SKIN DOUG DC8 DC863F 302198F WP RT WING CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND RIGHT UPPER WING INBOARD SLOT LEADING EDGE HAS CORROSION AROUND FRONT SPAR SCREWS. R EPAIRED DAMAGED SKIN, INSTALLED REPAIR IAW DC-8 SRM 57-2-1. CORROSION CARD NR 121R-0552, NON-ROUTINE TASK CARD NR 87402 . 2 L 7 4 4F 4A25 1996120500475 19961205 00475 WP 1996 12 5 CKSA96200 1 19961124 A 5711 SPAR DOUG DC8 DC863F 302198F WP RT WING CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND RIGHT UPPER WING SPAR HAS CORROSION. REPAIRED IAW DC-8 SRM 57-2-1 FIGURE 38. CORROS ION CARD NR 121R-0552 AND 112R-0551, NON-ROUTINE TASK CARD NR 87403. 2 L 7 4 4F 4A25 1996120500476 19961205 00476 WP 1996 12 5 CKSA96201 1 19961124 A 5320 INTERCOSTAL DOUG DC8 DC863F 302198F WP BS 1360 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND FS 1360 STRINGER 31R INTERCOSTAL CORRODED. REMOVED AND REPLACED FS 1360 STRINGER 31R INTERCOSTAL IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88475. 2 L 7 4 4F 4A25 1996120500477 19961205 00477 WP 1996 12 5 CKSA96202 1 19961124 A 5210 FRAME DOUG DC8 DC863F 302198F WP ENTRY DOOR CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND FORWARD ENTRY DOOR CORROSION ON SECOND FRAME FROM BOTTOM AFT LOWER CORNER INSIDE. RE PAIRED FRAME IAW DC-8 SRM 52-2-0 FIGURE 2. TREATED AND PRIMED. C-4 CHECK WORK CARD NR 3043, NON-ROUTINE TASK CARD NR 8 7497. 2 L 7 4 4F 4A25 1996120500478 19961205 00478 WP 1996 12 5 CKSA96203 1 19961124 A 5730 PANEL DOUG DC8 DC863F 302198F WP WS 172 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND STA XRS 172 LEFT HAND UPPER WING LEADING EDGE PANEL AT FORWARD SPAR HAS CORROSION ARO UND SCREWS. REPAIRED IAW DC-8 SRM 57-2-1 FIGURE 38. CORROSION CARD NR 116L-055, NON-ROUTINE TASK CARD NR 87345. 2 L 7 4 4F 4A25 1996120500479 19961205 00479 WP 1996 12 5 CKSA96204 1 19961124 A 5330 SKIN DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND FREON COOLING EXHAUST PORT AFT LOWER CORNER SKIN CRACKED. REPAIRED FREON SYSTEM EXHA UST DOOR SKIN WITH DOUBLER REPAIR IAW DC-8 SRM 53-2-0 FIGURE 13 VIEW R 7011. C-4 CHECK WORK CARD NR 3097, NON-ROUTINE T ASK CARD NR 87277. 2 L 7 4 4F 4A25 1996120500480 19961205 00480 WP 1996 12 5 CKSA96205 1 19961124 A 5320 37558452 FITTING DOUG DC8 DC863F 302198F WP BS 1228 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND BATHTUB FITTING AT FS 1228 STRINGER 35L TO STRINGER 34L CORRODED. REMOVED AND REPLAC ED FITTING IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88118. 2 L 7 4 4F 4A25 1996120500481 19961205 00481 WP 1996 12 5 CKSA96206 1 19961124 A 5320 37558452 FITTING DOUG DC8 DC863F 302198F WP BS 1160 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND BATHTUB FITTING AT FS 1160 STRINGER 35R TO STRINGER 36R CORRODED. REMOVED AND REPLAC ED FITTING IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88117. 2 L 7 4 4F 4A25 1996120500482 19961205 00482 WP 1996 12 5 CKSA96207 1 19961124 A 5320 3755843502 FITTING DOUG DC8 DC863F 302198F WP BS 1200 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND BATHTUB FITTING FS 1200 STRINGER 34R TO STRINGER 35R CORRODED. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88119. 2 L 7 4 4F 4A25 1996120500483 19961205 00483 WP 1996 12 5 CKSA96208 1 19961124 A 5320 3755843501 FITTING DOUG DC8 DC863F 302198F WP BS 1220 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, BATHTUB FITTING AT FS 1220 STRINGER 34R TO STRINGER 35R CORRODED. REMOVED AND REPLACED FIT TING IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88116. 2 L 7 4 4F 4A25 1996120500484 19961205 00484 WP 1996 12 5 CKSA96209 1 19961124 A 5320 37558451 FITTING DOUG DC8 DC863F 302198F WP BS 1152 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND BATHTUB FITTING AT FS 1152 STRINGER 35L TO STRINGER 36L CORRODED. REMOVED AND REPLAC ED FITTING IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88115. 2 L 7 4 4F 4A25 1996120500485 19961205 00485 WP 1996 12 5 CKSA96210 1 19961124 A 5320 37558412 FITTING DOUG DC8 DC863F 302198F WP BS 1200 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND BATHTUB FITTING AT FS 1200 STRINGER 33R TO STRINGER 34R CORRODED. REMOVED AND REPLAC ED FITTING IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88114. 2 L 7 4 4F 4A25 1996120500486 19961205 00486 WP 1996 12 5 CKSA96211 1 19961124 A 5320 37558411 FITTING DOUG DC8 DC863F 302198F WP BS 1200 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND BATHTUB FITTING AT FS 1200 STRINGER 33R TO STRINGER 34R CORRODED. REMOVED AND REPLAC ED DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88113. 2 L 7 4 4F 4A25 1996120500487 19961205 00487 WP 1996 12 5 CKSA96212 1 19961124 A 5320 37558452 FITTING DOUG DC8 DC863F 302198F WP BS 1228 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND BATHTUB FITTING AT FS 1228 STRINGER 35L TO STRINGER 36L CORRODED. REMOVED AND REPLAC ED BATHTUB FITTING IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88112. 2 L 7 4 4F 4A25 1996120500488 19961205 00488 WP 1996 12 5 CKSA96213 1 19961124 A 5320 37558451 FITTING DOUG DC8 DC863F 302198F WP BS 1220 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND BATHTUB FITTING AT FS 1220 STRINGER 35R TO STRINGER 36R CORRODED. REMOVED AND REPLAC ED FITTING IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88111. 2 L 7 4 4F 4A25 1996120500489 19961205 00489 WP 1996 12 5 CKSA96214 1 19961124 A 5320 37558451 FITTING DOUG DC8 DC863F 302198F WP BS 1226 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND BATHTUB FITTING AT FS 1226 STRINGER 36R TO STRINGER 35R CORRODED. REMOVED AND REPLAC ED FITTING IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88110. 2 L 7 4 4F 4A25 1996120500490 19961205 00490 WP 1996 12 5 CKSA96215 1 19961124 A 5320 3755822513 FITTING DOUG DC8 DC863F 302198F WP BS 1180 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND BATHTUB FITTING AT FS 1180 STRINGER 35R TO STRINGER 34R CORRODED. REMOVED AND REPLAC ED FITTING IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88109. 2 L 7 4 4F 4A25 1996120500491 19961205 00491 WP 1996 12 5 CKSA96216 1 19961124 A 5320 37558451 FITTING DOUG DC8 DC863F 302198F WP BS 1160 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND BATHTUB FITTING FS 1120 STRINGER 36L CORRODED. REMOVED AND REPLACED BATHTUB FITTING IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88120. 2 L 7 4 4F 4A25 1996120500492 19961205 00492 WP 1996 12 5 CKSA96217 1 19961124 A 5320 37558451 FITTING DOUG DC8 DC863F 302198F WP BS 1220 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND BATHTUB FITTING AT FS 1220 STRINGER 35L TO STRINGER 34L CORRODED. REMOVED AND REPLAC ED FITTING IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88121. 2 L 7 4 4F 4A25 1996120500493 19961205 00493 WP 1996 12 5 CKSA96218 1 19961124 A 5320 37558411 FITTING DOUG DC8 DC863F 302198F WP BS 1180 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND BATHTUB FITTING AT FS 1180 STRINGER 33R TO STRINGER 34R CORRODED. REMOVED AND REPLAC ED BATHTUB FITTING IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88127. 2 L 7 4 4F 4A25 1996120500494 19961205 00494 WP 1996 12 5 CKSA96219 1 19961124 A 5320 3755842504 FITTING DOUG DC8 DC863F 302198F WP BS 1200 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND BATHTUB FITTING AT FS 1200 STRINGER 33L TO STRINGER 32L CORRODED. REMOVED AND REPLAC ED BATHTUB FITTING IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88133. 2 L 7 4 4F 4A25 1996120500495 19961205 00495 WP 1996 12 5 CKSA96220 1 19961124 A 5320 37558461 FITTING DOUG DC8 DC863F 302198F WP BS 1220 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND BATHTUB FITTING AT FS 1220 STRINGER 31 CORRODED. REMOVED AND REPLACED FITTING IAW DC -8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88134. 2 L 7 4 4F 4A25 1996120500496 19961205 00496 WP 1996 12 5 CKSA96221 1 19961124 A 5320 37558452 FITTING DOUG DC8 DC863F 302198F WP BS 1160 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND BATHTUB FITTING AT FS 1160 STRINGER 33R TO STRINGER 34R CORRODED. REMOVED AND REPLAC ED FITTING IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88135. 2 L 7 4 4F 4A25 1996120500497 19961205 00497 WP 1996 12 5 CKSA96222 1 19961124 A 5320 37558411 FITTING DOUG DC8 DC863F 302198F WP BS 1220 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND FITTING CORRODED AT FS 1220 STRINGER 33R TO STRINGER 34R. REMOVED AND REPLACED FITTI NG IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88137. 2 L 7 4 4F 4A25 1996120500498 19961205 00498 WP 1996 12 5 CKSA96223 1 19961124 A 5320 37558401 FITTING DOUG DC8 DC863F 302198F WP BS 1220 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND FITTING AT FS 1220 STRINGER 33R CORRODED. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88139. 2 L 7 4 4F 4A25 1996120500499 19961205 00499 WP 1996 12 5 CKSA96224 1 19961124 A 5510 DOUBLER DOUG DC8 DC863F 302198F WP LT HORIZ STAB CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER LEADING EDGE AT STA XFS185 CORRODED. REPAIRED CORROSION D AMAGE IAW SKETCH AIA/E/2404 AND EA 96-326 AND 8110-3. C-4 CHECK WORK CARD NR 4001 1OF1, NON-ROUTINE TASK CARD NR 87530. 2 L 7 4 4F 4A25 1996120500500 19961205 00500 WP 1996 12 5 CKSA96225 1 19961124 A 5730 SKIN DOUG DC8 DC863F 302198F WP WS 329-405 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND RIGHT WING TOP LEADING EDGE XFS329.000 TO 405.000 HAS CORROSION AROUND LEADING EDGE S CREWS. REMOVED CORRODED AREA AROUND SPAR SCREW IAW DC-8 SRM 51-1-8. INSTALLED UPPER WING LEADING EDGE SURFACE REPAIR I AW DC-8 SRM 57-2-1 FIGURE 38. REPAIR DEVIATION APPROVED IAW EA 96-326, AIA EER D8-05085 AND AIA 8110-3 DATED 11-15-96. CORROSION CARD NR 115R-0551, 116R-0551, NON-ROUTINE TASK CARD NR 87390. 2 L 7 4 4F 4A25 1996120500501 19961205 00501 WP 1996 12 5 CKSA96226 1 19961124 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 1600 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND FS 1600 LONGERON 28R BULGE IN REPAIR. REPAIRED IAW DC-8 SRM 53-2-1 FIGURE 7 CLASS II REPAIR INTIAL INSPECTION DUE 12,000 CYCLES REPETITIVE 4,000 CYCLES REPLACEMENT AT 24,000 CYCLES IAW 53-2-1 FIGURE 5. I AW 51-5-5 OK TO TREAT, PRIME AND INSTALL REPAIR, NO CORROSION FOUND. NON-ROUTINE TASK CARD NR 87474. 2 L 7 4 4F 4A25 1996120500502 19961205 00502 WP 1996 12 5 CKSA96227 1 19961124 A 5730 SKIN DOUG DC8 DC863F 302198F WP WS 566.25-710 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND RIGHT UPPER WING LEADING EDGE FROM XFS566.250 TO 710.000 HAS CORROSION AT ATTACHING S CREWS TO SPAR. REMOVED CORROSION AND INSTALLED DOUBLER IAW DC-8 SRM 57-2-1 FIGURE 38 AND AIA SKETCH AIA/E/2390. REPAIR ACCOMPLISHED IAW EA 96-326 AND AIA 8110-3 DATED 11-15-96. CORROSION CARD NR 117R-0551, 109R-0551. NON-ROUTINE TASK CA RD NR 87737. 2 L 7 4 4F 4A25 1996120500503 19961205 00503 WP 1996 12 5 CKSA96228 1 19961124 A 5320 FITTING DOUG DC8 DC863F 302198F WP BS 1690-1680 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND STRINGER END FITTING CORRODED STA 1690 TO 1680 STRINGER 26R. REMOVED AND REPLACED EN D FITTING IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5600-0551. NON-ROUTINE TASK CARD NR 88150. 2 L 7 4 4F 4A25 1996120500504 19961205 00504 WP 1996 12 5 CKSA96229 1 19961124 A 5531 SPAR DOUG DC8 DC863F 302198F WP VERT STAB CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND LEFT VERTICAL STAB REAR SPAR CORRODED AT STA ZR132. REPAIRED IAW AIA/E/2386 SKETCH N R C-4 CHECK WORK CARD NR 3014. NON-ROUTINE TASK CARD NR 87304. 2 L 7 4 4F 4A25 1996120500505 19961205 00505 WP 1996 12 5 CKSA96230 1 19961124 A 5730 SKIN DOUG DC8 DC863F 302198F WP WS 310.25-329 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND RIGHT WING LEADING EDGE XFS 310.250 TO 329.000 APPROXIMATELY HAS BULGING SKIN AT SPAR . REMOVED CORROSION BY CUTTING SKIN FROM XFS291.5 TO XFS400 AND FABRICATED FILLER AND DOUBLER PER SRM 57-2-1. CORROSIO N CARD NR 116R-0551, NON-ROUTINE TASK CARD NR 87389. 2 L 7 4 4F 4A25 1996120500506 19961205 00506 WP 1996 12 5 CKSA96231 1 19961124 A 5730 SKIN DOUG DC8 DC863F 302198F WP RT WING CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND RIGHT UPPER WING INBOARD LEADING EDGE HAS LIGHT CORROSION AND BARE METAL AROUND LEADI NG EDGE SCREWS. REPAIRED IAW AIA EA SKETCH NR 2389 EA 96-326 AND AIA 8110-3 DATED 11-15-96. CORROSION CARD NR 124R-055 1, 123R-0551, 121R-0552, NON-ROUTINE TASK CARD NR 87391. 2 L 7 4 4F 4A25 1996120500507 19961205 00507 WP 1996 12 5 CKSA96232 1 19961124 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 1660 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND FS 1660 BULGE IN SKIN BELOW LEFT HAND AFT ENTRY DOOR. REMOVED CORROSION AND TREATED THE AREA IAW SRM 51-1-8 AND INSTALLED DOUBLER REPAIR IAW SRM 53-2-0 FIGURE 18. C-4 CHECK WORK CARD 3097, NON-ROUTINE TA SK CARD NR 87246. 2 L 7 4 4F 4A25 1996120500508 19961205 00508 WP 1996 12 5 CKSA96233 1 19961124 A 5320 INTERCOSTAL DOUG DC8 DC863F 302198F WP BS 1020-1040 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND INTERCOSTAL CORRODED ON ENDS STA 1020 TO STA 1040. REMOVED AND REPLACED INTERCOSTAL STA 1020 TO STA 1040 STRINGER 34R IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88474. 2 L 7 4 4F 4A25 1996120500509 19961205 00509 WP 1996 12 5 CKSA96234 1 19961124 A 5320 WEB DOUG DC8 DC863F 302198F WP NLG WW CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND RIGHT HAND NOSE TUNNEL PUNCTURED IN PRESSURE WEB AT FS 12. CUT DAMAGED AREA OUT, REP AIRED IAW SRM 53-2-1 FIGURE 7. C-4 CHECK WORK CARD NR 3006, NON-ROUTINE TASK CARD NR 88102. 2 L 7 4 4F 4A25 1996120500510 19961205 00510 WP 1996 12 5 CKSA96235 1 19961124 A 5720 46487722 FITTING DOUG DC8 DC863F 302198F WP WS 69.5 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND UPPER STA XW69.5 SHEAR TIE FITTING CRACKED BELOW PRESSURE DECK. REMOVED AND REPLACED FITTING IAW DC-8 SRM. C-4 CHECK WORK CARD NR 3010, NON-ROUTINE TASK CARD NR 88076. 2 L 7 4 4F 4A25 1996120500511 19961205 00511 WP 1996 12 5 CKSA96236 1 19961124 A 5320 37517382 STRAP DOUG DC8 DC863F 302198F WP BS 850 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND HEAVY CORROSION ON STRAP AND STRUCTURE FORWARD OF LONGERON 24 FORWARD ATTACH POINT BA RREL NUT STA 850. REMOVED AND REPLACED STRAP AND STRUCTURE IAW DC-8 SRM 51-1-20D. C-4 CHECK CARD NR 3010, NON-ROUTINE TASK CARD NR 87585. 2 L 7 4 4F 4A25 1996120500512 19961205 00512 WP 1996 12 5 CKSA96237 1 19961124 A 5320 36410042 FITTING DOUG DC8 DC863F 302198F WP BS 879 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND EXFOLIATION CORROSION ON FORWARD SIDE OF RIGHT HAND LONGERON 24 VERTICAL FITTING STA 879. REPLACED BY REPAIR FITTING IAW DC-8 SRM 53-2-0 FIGURE 8 C-4 CHECK CARD NR 3010, NON-ROUTINE TASK CARD NR 87902. 2 L 7 4 4F 4A25 1996120500513 19961205 00513 WP 1996 12 5 CKSA96238 1 19961124 A 5312 4615394 BULKHEAD FITTING DOUG DC8 DC863F 302198F WP BS 857 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND LEFT HAND WHEEL WELL 857 BULKHEAD 69.5 UPPER FITTING CORRODED. REPAIRED IAW DOUGLAS DRAWING NR J060192. C-4 CHECK CARD NR 3010, NON-ROUTINE TASK CARD NR 88042. 2 L 7 4 4F 4A25 1996120500514 19961205 00514 WP 1996 12 5 CKSA96239 1 19961124 A 5347 83000034 SEAT TRACK DOUG DC8 DC863F 302198F WP LT COCKPIT WORN A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND HOLES IN CAPTAINS LEFT HAND AND RIGHT HAND CHAIR TRACK ARE WORN. REPAIRED ONE AND RE PLACED ONE SEAT CHAIR TRACK IAW SRM 53-2-3 AND 51-3-0. C-4 CHECK CARD NR 3010, NON-ROUTINE TASK CARD NR 87521. 2 L 7 4 4F 4A25 1996120500515 19961205 00515 WP 1996 12 5 CKSA96240 1 19961124 A 5320 4758514509 FITTING DOUG DC8 DC863F 302198F WP BS 1240 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND C-PIT DOOR JAMB FITTING CRACKED STA 1240 LONGERON 32R. REMOVED AND REPLACED DOOR JAM B FITTING IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88026. 2 L 7 4 4F 4A25 1996120500516 19961205 00516 WP 1996 12 5 CKSA96241 1 19961124 A 5320 37549301 FITTING DOUG DC8 DC863F 302198F WP NR 2 DOOR CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND NR 2 DOOR LATCH BACKUP FITTING CORRODED AND CRACKED. REMOVED AND REPLACED CORRODED F ITTING IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88140. 2 L 7 4 4F 4A25 1996120500517 19961205 00517 WP 1996 12 5 CKSA96242 1 19961124 A 5320 37540232 FITTING DOUG DC8 DC863F 302198F WP NR 3 DOOR CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND NR 3 DOOR LATCH BACKUP FITTING HAS CORROSION. REMOVED AND REPLACED CORRODED DOOR LAT CH IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88141. 2 L 7 4 4F 4A25 1996120500518 19961205 00518 WP 1996 12 5 CKSA96243 1 19961124 A 5320 4758514510 FITTING DOUG DC8 DC863F 302198F WP BS 1140 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND FITTING CRACKED STA 1140 L32R. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-0. CO RROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88145. 2 L 7 4 4F 4A25 1996120500519 19961205 00519 WP 1996 12 5 CKSA96244 1 19961124 A 5320 475814501 FITTING DOUG DC8 DC863F 302198F WP BS 1140 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND FITTING CRACKED STA 1140 LONGERON 32R TO LONGERON 33R. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88146. 2 L 7 4 4F 4A25 1996120500520 19961205 00520 WP 1996 12 5 CKSA96245 1 19961124 A 5320 47585141 FITTING DOUG DC8 DC863F 302198F WP BS 1160 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND DOOR JAMB FITTING CRACKED STA 1160 STRINGER 29R TO STRINGER 32R. REMOVED AND REPLACE D FITTING IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88154. 2 L 7 4 4F 4A25 1996120500521 19961205 00521 WP 1996 12 5 CKSA96246 1 19961124 A 5320 37558451 FITTING DOUG DC8 DC863F 302198F WP BS 1155 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND BATHTUB FITTING CORRODED STA 1155 STRINGER 34L TO STRINGER 35L. REMOVED AND REPLACED BATHTUB FITTING AT FS 1155 STRINGER 34L TO STRINGER 35L. CORROSION CARD NR 5590-055, NON-ROUTINE TASK CARD NR 88155. 2 L 7 4 4F 4A25 1996120500522 19961205 00522 WP 1996 12 5 CKSA96247 1 19961124 A 5320 37558411 FITTING DOUG DC8 DC863F 302198F WP BS 1155 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND BATHTUB FITTING CORRODED STA 1155 STRINGER 34R TO STRINGER 33R. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88156. 2 L 7 4 4F 4A25 1996120500523 19961205 00523 WP 1996 12 5 CKSA96248 1 19961124 A 5320 37558401 FITTING DOUG DC8 DC863F 302198F WP BS 1160 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND BATHTUB FITTING CORRODED STA 1160 STRINGER 32R TO STRINGER 33R. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0115, NON-ROUTINE TASK CARD NR 88157. 2 L 7 4 4F 4A25 1996120500524 19961205 00524 WP 1996 12 5 CKSA96249 1 19961124 A 5320 37558401 FITTING DOUG DC8 DC863F 302198F WP BS1155 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND BATHTUB FITTING CORRODED STA 1155 STRINGER 32R TO STRINGER 33R. REMOVED AND REPLACED AS PER DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88158. 2 L 7 4 4F 4A25 1996120500525 19961205 00525 WP 1996 12 5 CKSA96250 1 19961124 A 5320 37558451 FITTING DOUG DC8 DC863F 302198F WP BS 1155 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND BATHTUB FITTING CORRODED STA 1155 STRINGER 36R TO STRINGER 35R. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88159. 2 L 7 4 4F 4A25 1996120500527 19961205 00527 WP 1996 12 5 CKSA96252 1 19961124 A 5320 3755843501 FITTING DOUG DC8 DC863F 302198F WP BS 1155 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND BATHTUB FITTING STA 1155 STRINGER 34R TO STRINGER 35R CORRODED. REMOVED AND REPLACED BATHTUB FITTING IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88160. 2 L 7 4 4F 4A25 1996120500528 19961205 00528 WP 1996 12 5 CKSA96253 1 19961124 A 5320 4758514505 FITTING DOUG DC8 DC863F 302198F WP CARGO DOORWAY CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND C-PIT DOOR JAMB FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-0. C ORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88024. 2 L 7 4 4F 4A25 1996120500529 19961205 00529 WP 1996 12 5 CKSA96254 1 19961124 A 5320 4756514512 FITTING DOUG DC8 DC863F 302198F WP BS 1260 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND C-PIT DOOR JAMB FITTING CRACKED STA 1260 LONGERON 32R. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88025. 2 L 7 4 4F 4A25 1996120500530 19961205 00530 WP 1996 12 5 CKSA96255 1 19961124 A 5320 37558452 FITTING DOUG DC8 DC863F 302198F WP BS 1160 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND BATHTUB FITTING CORRODED STA 1160 STRINGER 33L TO STRINGER 34L. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88361. 2 L 7 4 4F 4A25 1996120500531 19961205 00531 WP 1996 12 5 CKSA96256 1 19961124 A 5320 4758514519 FITTING DOUG DC8 DC863F 302198F WP BS 1220 L32R CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND C-PIT FITTING CRACKED STA 1220 LONGERON 32R. REMOVED AND REPLACED FITTING IAW DC-8 S RM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88028. 2 L 7 4 4F 4A25 1996120500532 19961205 00532 WP 1996 12 5 CKSA96257 1 19961124 A 5320 37385702 FITTING DOUG DC8 DC863F 302198F WP BS 1220 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND C-PIT FITTING CRACKED STA 1220 STRINGER 35R. REMOVED AND REPLACED FITTING IAW DC-8 S RM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88029. 2 L 7 4 4F 4A25 1996120500533 19961205 00533 WP 1996 12 5 CKSA96258 1 19961124 A 5320 4758514511B FITTING DOUG DC8 DC863F 302198F WP BS 1280 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND C-PIT FITTING CRACKED STA 1280 LONGERON 32R. REMOVED AND REPLACED FITTING IAW DC-8 S RM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88030. 2 L 7 4 4F 4A25 1996120500534 19961205 00534 WP 1996 12 5 CKSA96259 1 19961124 A 5320 4758514520 FITTING DOUG DC8 DC863F 302198F WP BS 1220 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND C-PIT FITTING CRACKED STA 1220 LONGERON 33R. REMOVED AND REPLACED FITTING IAW DC-8 S RM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88031. 2 L 7 4 4F 4A25 1996120500535 19961205 00535 WP 1996 12 5 CKSA96260 1 19961124 A 5320 3754021 FITTING DOUG DC8 DC863F 302198F WP CARGO COMPT CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND NR 2 T-BOLT FITTING CORRODED C-PIT STRINGER 32R. REMOVED AND REPLACED FITTING IAW DC -8 SRM 51-1-0. CORROSION CARD NR 5590-055, NON-ROUTINE TASK CARD NR 88362. 2 L 7 4 4F 4A25 1996120500536 19961205 00536 WP 1996 12 5 CKSA96261 1 19961124 A 5320 3754021 FITTING DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND T-BOLT FITTING CORRODED STRINGER 32R. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1 -0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88363. 2 L 7 4 4F 4A25 1996120500537 19961205 00537 WP 1996 12 5 CKSA96262 1 19961124 A 5320 37558401 FITTING DOUG DC8 DC863F 302198F WP BS 1226 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND BATHTUB FITTING CORRODED STA 1226 STRINGER 32R TO STRINGER 33R. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88364. 2 L 7 4 4F 4A25 1996120500538 19961205 00538 WP 1996 12 5 CKSA96263 1 19961124 A 5320 3755840 FITTING DOUG DC8 DC863F 302198F WP BS 1220 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND BATHTUB FITTING CORRODED STA 1220 STRINGER 32R TO STRINGER 33R. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88365. 2 L 7 4 4F 4A25 1996120500539 19961205 00539 WP 1996 12 5 CKSA96264 1 19961124 A 5320 5894282501 FITTING DOUG DC8 DC863F 302198F WP NR 5 DOORWAY CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND NR 5 DOOR LATCH SUPPORT FITTING CRACKED AND CORRODED. REMOVED AND REPLACED FITTING I AW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88368. 2 L 7 4 4F 4A25 1996120500540 19961205 00540 WP 1996 12 5 CKSA96265 1 19961124 A 5320 37540231 FITTING DOUG DC8 DC863F 302198F WP NR 1 DOORWAY CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND NR 1 DOOR LATCH AFT SUPPORT CORRODED. REMOVED AND REPLACED AS PER DC-8 SRM 51-1-0. C ORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88369. 2 L 7 4 4F 4A25 1996120500541 19961205 00541 WP 1996 12 5 CKSA96266 1 19961124 A 5320 3754021 FITTING DOUG DC8 DC863F 302198F WP CARGO COMPT CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND NR 5 T-BOLT BRACKET CORRODED C-PIT. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-0 . CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88373. 2 L 7 4 4F 4A25 1996120500542 19961205 00542 WP 1996 12 5 CKSA96267 1 19961124 A 5320 37540233 BRACKET DOUG DC8 DC863F 302198F WP CARGO COMPT CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND NR 5 AFT BRACKET SUPPORT C-PIT CORRODED. REMOVED AND REPLACED CORRODED BRACKET SUPPO RT IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88374. 2 L 7 4 4F 4A25 1996120500543 19961205 00543 WP 1996 12 5 CKSA96268 1 19961124 A 5320 37549302 BRACKET DOUG DC8 DC863F 302198F WP CARGO COMPT CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND NR 4 DOOR LATCH AFT BRACKET C-PIT CORRODED AND CRACKED. REMOVED AND REPLACED AS PER DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88380. 2 L 7 4 4F 4A25 1996120500544 19961205 00544 WP 1996 12 5 CKSA96269 1 19961124 A 5320 37558421 FITTING DOUG DC8 DC863F 302198F WP BS 1160 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND FITTING STA 1160 STRINGER 31L TO STRINGER 30L CORRODED. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88388. 2 L 7 4 4F 4A25 1996120500545 19961205 00545 WP 1996 12 5 CKSA96270 1 19961124 A 5320 37558472 FITTING DOUG DC8 DC863F 302198F WP BS 1160 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND FITTING CRACKED FORWARD OF C-PIT DOOR STA 1160. REMOVED AND REPLACED FITTING IAW DC- 8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88075. 2 L 7 4 4F 4A25 1996120500546 19961205 00546 WP 1996 12 5 CKSA96271 1 19961124 A 5320 4758514515 FITTING DOUG DC8 DC863F 302198F WP BS 1140 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND STA 1140 LONGERON 35L FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51- 1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88148. 2 L 7 4 4F 4A25 1996120500547 19961205 00547 WP 1996 12 5 CKSA96272 1 19961124 A 5320 4758514512 FITTING DOUG DC8 DC863F 302198F WP BS 1160 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND STA 1160 LONGERON 32R CRACKED. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-0. CO RROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88149. 2 L 7 4 4F 4A25 1996120500548 19961205 00548 WP 1996 12 5 CKSA96273 1 19961124 A 5320 37592582 FITTING DOUG DC8 DC863F 302198F WP BS 1280-1300 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND LONGERON SPLICE FITTING CRACKED STA 1280 TO STA 1300. REMOVED AND REPLACED FITTING I AW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88420. 2 L 7 4 4F 4A25 1996120500549 19961205 00549 WP 1996 12 5 CKSA96274 1 19961124 A 5320 47585141 FITTING DOUG DC8 DC863F 302198F WP BS 1240 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND FITTING CRACKED STA 1240 STRINGER 35R. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51- 1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88422. 2 L 7 4 4F 4A25 1996120500550 19961205 00550 WP 1996 12 5 CKSA96275 1 19961124 A 5320 37584981 FITTING DOUG DC8 DC863F 302198F WP BS 1260 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND FITTING STA 1260 LONGERON 35 CRACKED. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1 -0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88458. 2 L 7 4 4F 4A25 1996120500551 19961205 00551 WP 1996 12 5 CKSA96276 1 19961124 A 5320 37558451 FITTING DOUG DC8 DC863F 302198F WP BS 1240 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND FITTING STA 1240 LONGERON 33R CRACKED. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51- 1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88459. 2 L 7 4 4F 4A25 1996120500552 19961205 00552 WP 1996 12 5 CKSA96277 1 19961124 A 5320 4758514502 FITTING DOUG DC8 DC863F 302198F WP BS 1225-1240 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND BRACKET CRACKED AT STA 1225 TO 1240 STRINGER 35L. REMOVED AND REPLACED FITTING IAW D C-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88491. 2 L 7 4 4F 4A25 1996120500553 19961205 00553 WP 1996 12 5 CKSA96278 1 19961124 A 5320 2646348501 ANGLE DOUG DC8 DC863F 302198F WP BS 902 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND PRESSURE FLOOR T-CHORD CORRODED THROUGH ABOVE LEFT HAND LONGERON 24 FORWARD OF VERTIC AL SUPPORT FITTING STA 902. REPAIRED ANGLE IAW AIA SKETCH NR AIA/E/2381, AIA EA 96-326 AND AIA 8110-3 DATED 11-15-96. C -4 CHECK WORK CARD NR 3010, NON-ROUTINE TASK CARD NR 87582. 2 L 7 4 4F 4A25 1996120500554 19961205 00554 WP 1996 12 5 CKSA96279 1 19961124 A 5753 565239680 RIB DOUG DC8 DC863F 302198F WP TE FLAP WORN A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND INBOARD FLAP RIB WORN THROUGH CORNER AT FLAP SPLIT ON LOWER AFT SURFACE. REPAIRED IA W AIA EER D8-05080 EA 96-325 PRIMED IAW SRM 51-1-8. CORROSION CARD NR 115L-0551, NON-ROUTINE TASK CARD NR 87365. 2 L 7 4 4F 4A25 1996120500555 19961205 00555 WP 1996 12 5 CKSA96280 1 19961124 A 7110 AN1225835764001 COWL FLANGE DOUG DC8 DC863F 302198F WP NR 1 ENGINE BROKEN A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND NR 1 NOSE COWL FLANGE BROKEN AND FLANGE HOLES WORN. REPAIRED BROKEN COWL FLANGE IAW EER D8-05086, AIA EA 96-326, AND AIA 8110-3 DATED 11-15-96. INSERTED WASHERS AT WORN HOLES IAW BURBANK AERO CORP II MM 71-1-0. C-4 CHECK WORK CARD NR 7106, NON-ROUTINE TASK CARD NR 87411. 2 L 7 4 4F 4A25 1996120500556 19961205 00556 WP 1996 12 5 CKSA96281 1 19961124 A 5330 SKIN DOUG DC8 DC863F 302198F WP FS 680 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND FS 680 STRINGER 34R CORROSION ON SKIN. REMOVED CORROSION, REPAIRED IAW EA96-326, AIA SKETCH AIA/E/2393, AND 8110-3 DATED 11-15-96. C-4 CHECK WORK CARD NR 3014, NON-ROUTINE TASK CARD NR 87952. 2 L 7 4 4F 4A25 1996120500557 19961205 00557 WP 1996 12 5 CKSA96282 1 19961124 A 5330 SKIN DOUG DC8 DC863F 302198F WP FS 690 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND FS 1690 LONGERON 23 RIGHT SURFACE CORROSION ON SKIN. REMOVED DAMAGED SKIN, INSTALLED REPAIR IAW EA 96-326, AIA SKETCH AIA/E/2394, AND AIA 8110-3 DATED 11-15-96. C-4 CHECK WORK CARD NR 3014, NON-ROUTINE T ASK CARD NR 87265. 2 L 7 4 4F 4A25 1996120500558 19961205 00558 WP 1996 12 5 CKSA96283 1 19961124 A 7830 2219T62 GRIPPER DOUG DC8 DC863F 302198F WP NR 2 ENG TR UNIT DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND NR 2 T/R STRINGER GRIPPER STOP TUBE AFT END DAMAGED. REPAIRED GRIPPER STOP TUBE AFT END IAW EA 96-326 AIA EER D8-05084 AND 8110-3 DATED 11-15-96. C-4 CHECK WORK CARD NR 7208, NON-ROUTINE TASK CARD NR 87 946. 2 L 7 4 4F 4A25 1996120500559 19961205 00559 WP 1996 12 5 CKSA96284 1 19961124 A 5720 ANGLE DOUG DC8 DC863F 302198F WP WING LE CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND WING LEADING EDGE ANGLE CRACKED JUST INBOARD OF NR 4 PYLON SLOT PANEL. REMOVED CRACK ED ANGLE MANUFACTURED AND INSTALLED IAW DC-8 SRM 51-1-21 AND AIA EA 96-326 AIA EER D8-05088 AND 8110-3 DATED 11-15-96. C ORROSION CARD NR 115L-0551, NON-ROUTINE TASK CARD NR 88412. 2 L 7 4 4F 4A25 1996120500560 19961205 00560 WP 1996 12 5 CKSA96285 1 19961124 A 5240 DOOR PLUG DOUG DC8 DC863F 302198F WP BS 45 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND STA 45 LONGERON 30R GROUND A/C SERVICE PANEL HAS CORROSION. INSTALLED GROUND A/C SER VICE DOOR PLUG IAW EA 96-326 SKETCH AIA/E/2378 AND AIA 8110-3 DATED 11-15-96. C-4 CHECK WORK CARD NR 3006, NON-ROUTINE TASK CARD NR 86927. 2 L 7 4 4F 4A25 1996120500561 19961205 00561 WP 1996 12 5 CKSA96286 1 19961124 A 5730 SKIN DOUG DC8 DC863F 302198F WP WS 693 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND CORROSION ON WING UPPER PLATING STA XRS693 BEYOND SRM LIMIT. REPAIRED IAW AIA EA SKE TCH NR AIA/E/2397 EA 96-326 AND AIA 8110-3 DATED 11-15-96. CORROSION CARD NR 115L-0551, NON-ROUTINE TASK CARD NR 88451. 2 L 7 4 4F 4A25 1996120500562 19961205 00562 WP 1996 12 5 CKSA96287 1 19961124 A 5531 SPAR DOUG DC8 DC863F 302198F WP VERT STAB CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND LEFT VERTICAL STABILIZER REAR SPAR CORRODED AT STA ZR180. REPAIRED IAW SKETCH AIA/E/ 2386 TREATED AND PRIMED IAW DC-8 SRM 51-1-8. REPAIR ACCOMPLISHED IAW EA 96-326 AND AIA 8110-3 DATED 11-15-96. CORROSIO N CARD NR 6000-0551, NON-ROUTINE TASK CARD NR 88461. 2 L 7 4 4F 4A25 1996120500563 19961205 00563 WP 1996 12 5 CKSA96288 1 19961124 A 5542 SKIN DOUG DC8 DC863F 302198F WP RUDDER DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND TOP OF RUDDER 2 LIGHTNING STRIKES STA ZR320 LEFT SIDE. REPAIRED IAW SKETCH NR AIA/E/ 2396 TREATED AND PRIMED METAL IAW DC-8 SRM 51-1-8. REPAIR ACCOMPLISHED IAW EA 96-326 AND AIA 8110-3 DATED 11-15-96. C- 4 CHECK CARD NR 3014, NON-ROUTINE TASK CARD NR 87301. 2 L 7 4 4F 4A25 1996120500564 19961205 00564 WP 1996 12 5 CKSA96289 1 19961124 A 5542 SKIN DOUG DC8 DC863F 302198F WP RUDDER DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND RIGHT SIDE OF RUDDER HAS HOLE IN SKIN AT STA ZR217. REPAIRED IAW SKETCH NR AIA/E/240 2 TREAT AND PRIMED METAL IAW DC-8 SRM 51-1-8 REPAIR ACCOMPLISHED IAW EA 96-326 AND 8110-3 DATED 11-15-96. C-4 CHECK CAR D NR 3014, NON-ROUTINE TASK CARD NR 87313. 2 L 7 4 4F 4A25 1996120500565 19961205 00565 WP 1996 12 5 CKSA96290 1 19961124 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 1390 DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND STA 1390 SKIN DAMAGE BETWEEN LONGERON 32R TO LONGERON 34R. REMOVED DAMAGED SKIN, INS TALLED REPAIR IAW EA 96-326 SKETCH AIA/E/2380 AND 8110-3 DATED 11-15-96. C-4 CHECK CARD NR 3097, NON-ROUTINE TASK CARD NR 86926. 2 L 7 4 4F 4A25 1996120500566 19961205 00566 WP 1996 12 5 CKSA96291 1 19961124 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 1390 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND FS 1390 LONGERON 31 RIGHT BULGE IN SKIN. REMOVED CORRODED SECTION OF SKIN, INSTALLED REPAIR IAW EA 96-326, SKETCH AIA/E/2380 AND 8110-3 DATED 11-15-96. C-4 CHECK CARD NR 3097, NON-ROUTINE TASK CARD NR 87 268. 2 L 7 4 4F 4A25 1996120500567 19961205 00567 WP 1996 12 5 CKSA96292 1 19961124 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1140 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND LOWER FLANGE OF FRAME CORRODED STA 1140 LONGERON 33R. REMOVED DAMAGE, INSTALLED DOUB LER REPAIR IAW AIA DWG AIA/E/2405 REV O DATED 11-14-96. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88523. 2 L 7 4 4F 4A25 1996120500568 19961205 00568 WP 1996 12 5 CKSA96293 1 19961124 A 5320 WEB DOUG DC8 DC863F 302198F WP BS 1220 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND FS 1220 STRINGER 33R WEB CORRODED. REMOVED CORROSION ON WEB AND REPAIRED IAW AIA SKE TCH AIA/E/2398 REV O SHEET 1 THROUGH 8 DATED 11-11-96. CORROSION CHECK CARD NR 5590-055, NON-ROUTINE TASK CARD NR 87959 . 2 L 7 4 4F 4A25 1996120500569 19961205 00569 WP 1996 12 5 CKSA96294 1 19961124 A 5313 2753715 LONGERON DOUG DC8 DC863F 302198F WP BS 1260-1280 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND STRINGER 36 TOP FLANGE IS CRACKED AT FACTORY SPLICE BETWEEN STA 1260 TO STA 1280. RE PAIRED IAW EA 96-326 SKETCH AIA/E/2408. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88143. 2 L 7 4 4F 4A25 1996120500570 19961205 00570 WP 1996 12 5 CKSA96295 1 19961124 A 5320 ANGLE DOUG DC8 DC863F 302198F WP BS 1220 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND DOOR FRAME ANGLE CRACKED AT FS 1220 TO DOOR. INSTALLED DOUBLER REPAIR IAW DC-8 SRM 5 3-2-0 FIGURE 1B. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 87960. 2 L 7 4 4F 4A25 1996120500571 19961205 00571 WP 1996 12 5 CKSA96296 1 19961124 A 5320 3754066501 INTERCOSTAL DOUG DC8 DC863F 302198F WP BS 1220 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND INTERCOSTAL END FITTING CRACKED STA 1220 LONGERON 33R. REMOVED AND REPLACED INTERCOS TAL END FITTING IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 89082. 2 L 7 4 4F 4A25 1996120500572 19961205 00572 WP 1996 12 5 CKSA96297 1 19961124 A 5320 ANGLE DOUG DC8 DC863F 302198F WP BS 1160 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND STRINGER 26L FS 1160 VERTICAL STIFFENER ANGLE CRACKED. REPLACED IAW SRM 51-1-0. COR ROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88046. 2 L 7 4 4F 4A25 1996120500573 19961205 00573 WP 1996 12 5 CKSA96298 1 19961124 A 5320 2611534 DOOR FRAME DOUG DC8 DC863F 302198F WP CARGO DOORWAY CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND D-PIT DOOR FRAME FORWARD AT LIGHT SWITCH CORRODED. REMOVED CORROSION, INSTALLED DOUB LER REPAIR IAW DC-8 SRM 53-2-0 FIGURE 2 SHEET 4. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88541. 2 L 7 4 4F 4A25 1996120500574 19961205 00574 WP 1996 12 5 CKSA96299 1 19961124 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 1260 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND EXTERNAL SKIN HAS CORROSION STA 1260 LONGERON 36. REMOVED CORROSION AND INSTALLED DO UBLER REPAIR IAW DC-8 SRM 53-2-1 FIGURE 7 SHEET 3. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 89076. 2 L 7 4 4F 4A25 1996120500575 19961205 00575 WP 1996 12 5 CKSA96300 1 19961124 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 1240-1260 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND FS 1240 TO FS 1260 SKIN CORRODED AT STRINGER 36. REMOVED CORRODED SKIN, INSTALLED RE PAIR IAW AIA SKETCH AIA/E/2398 REV O SHEET 01 THROUGH 08 DATED 11-11-96. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88433. 2 L 7 4 4F 4A25 1996120500576 19961205 00576 WP 1996 12 5 CKSA96301 1 19961124 A 5311 2357716 FRAME DOUG DC8 DC863F 302198F WP BS 1360 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND STA 1360 STRINGER 35L THROUGH STRINGER 35R FRAME CORRODED. REPAIRED IAW DC-8 SRM 53- 2-0 FIGURE 2. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88540. 2 L 7 4 4F 4A25 1996120500577 19961205 00577 WP 1996 12 5 CKSA96302 1 19961124 A 5320 3754914501 FITTING DOUG DC8 DC863F 302198F WP BS 1220-1240 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND FS 1220 TO 1240 STRINGER 31R CORRODED INCLUDING END FITTING. REMOVED AND REPLACED EN D FITTING IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 87967. 2 L 7 4 4F 4A25 1996120500578 19961205 00578 WP 1996 12 5 CKSA96303 1 19961124 A 5320 DOUBLER DOUG DC8 DC863F 302198F WP BS 1240 DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND FINGER DOUBLER DAMAGED AT STRINGER 31L FS 1240 C-PIT. REMOVED AND REPLACED FINGER DO UBLER IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88428. 2 L 7 4 4F 4A25 1996120500579 19961205 00579 WP 1996 12 5 CKSA96304 1 19961124 A 5320 975494961 INTERCOSTAL DOUG DC8 DC863F 302198F WP BS 1140 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND INTERCOSTAL HAS CORROSION STA 1140 LONGERON 33R. REMOVED AND REPLACED INTERCOSTAL IA W DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88476. 2 L 7 4 4F 4A25 1996120500580 19961205 00580 WP 1996 12 5 CKSA96305 1 19961124 A 5320 4755847502 FITTING DOUG DC8 DC863F 302198F WP BS 1230 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND FS 1230 MAIN SHEAR TIE FITTING CRACKED STRINGER 31R. REMOVED AND REPLACED FITTING IA W DC-8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 87966. 2 L 7 4 4F 4A25 1996120500581 19961205 00581 WP 1996 12 5 CKSA96306 1 19961124 A 5320 ANGLE DOUG DC8 DC863F 302198F WP BS 1240 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND FS 1240 FRAME ATTACH ANGLE BLOWN OUT AT STRINGER 32R. REPAIRED FRAME ATTACH ANGLE IA W DC-8 SRM 53-2-0. CORROSION CARD NR 5590-055, NON-ROUTINE TASK CARD NR 87646. 2 L 7 4 4F 4A25 1996120500582 19961205 00582 WP 1996 12 5 CKSA96307 1 19961124 A 5311 2754646 FRAME DOUG DC8 DC863F 302198F WP BS 1240 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND AFT SIDE OF FRAME CORRODED STA 1240 STRINGER 33R. INSTALLED DOUBLER REPAIR IAW AIA D RAWING AIA/E/2401 REV 0 DATED 11-12-96. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88427. 2 L 7 4 4F 4A25 1996120500583 19961205 00583 WP 1996 12 5 CKSA96308 1 19961124 A 5311 2750825 FRAME DOUG DC8 DC863F 302198F WP BS 1260 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND FS 1260 FRAME CORRODED STRINGER 34R THROUGH STRINGER 34L. REMOVED DAMAGE AND INSTALL ED REPAIR IAW DC-8 SRM 53-2-0 FIGURE 2 SHEET 5. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88432. 2 L 7 4 4F 4A25 1996120500584 19961205 00584 WP 1996 12 5 CKSA96309 1 19961124 A 5320 81130487654 SHEAR TIE DOUG DC8 DC863F 302198F WP BS 1260 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND FS 1260 SHEAR TIE CORRODED AT STRINGER 33R. REPLACED SHEAR TIE IAW DC-8 SRM 51-1-0 A ND D8-05072 AND EA 96-326 AND 8110-3 DATED 11-15-96. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88434. 2 L 7 4 4F 4A25 1996120500585 19961205 00585 WP 1996 12 5 CKSA96310 1 19961124 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 1140-1240 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND CORROSION ON INNER SKIN FROM FS 1140 THROUGH FS 1240 STRINGER 31L TO STRINGER 31R. R EMOVED CORROSION AND INSTALLED REPAIR IAW AIA SKETCH AIA/E/2398 REV 0 SHEET 01 THROUGH 08 DATED 11-11-96. CORROSION CAR D NR 5590-0551, NON-ROUTINE TASK CARD NR 88386. 2 L 7 4 4F 4A25 1996120500586 19961205 00586 WP 1996 12 5 CKSA96311 1 19961124 A 5320 97549491 INTERCOSTAL DOUG DC8 DC863F 302198F WP BS 1240-1260 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND INTERCOSTAL CRACKED STA 1240 TO STA 1260 LONGERON 33L. REPAIRED IAW 51-1-20 DC-8 SRM . CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88490. 2 L 7 4 4F 4A25 1996120500587 19961205 00587 WP 1996 12 5 CKSA96312 1 19961124 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 1240-1260 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND REPLACE FS 1240 THROUGH FS 1260 STRINGER 33L TO STRINGER 33R INNER SKIN. REPAIRED IA W EA 96-326 SKETCH AIA/E/2398. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88524. 2 L 7 4 4F 4A25 1996120500588 19961205 00588 WP 1996 12 5 CKSA96313 1 19961124 A 5330 SKIN DOUG DC8 DC863F 302198F WP CARGO DOORWAY CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND FUSELAGE SKIN CRACKED AT FORWARD LOWER CORNER OF CARGO DOOR. INSTALLED REPAIR IAW EA 96-326 SKETCH AIA/E/2387 AND AIA 8110-3 DATED 11-15-96. C-4 CHECK CARD NR 309, NON-ROUTINE TASK CARD NR 87473. 2 L 7 4 4F 4A25 1996120500589 19961205 00589 WP 1996 12 5 CKSA96314 1 19961124 A 5320 4758514511 FITTING DOUG DC8 DC863F 302198F WP BS 1260 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND C-PIT FITTING CRACKED STA 1260 LONGERON 32R. REMOVED AND REPLACED FITTING IAW DC-8 S RM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88027. 2 L 7 4 4F 4A25 1996120500590 19961205 00590 WP 1996 12 5 CKSA96315 1 19961124 A 5320 37558401 FITTING DOUG DC8 DC863F 302198F WP BS 1220 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND BATHTUB FITTING CORRODED STA 1220 STRINGER 32R THROUGH STRINGER 33R. REMOVED AND REP LACED CORRODED FITTING IAW DC-8 SRM 51-1-0. CORROSION CARD NR 5590-055, NON-ROUTINE TASK CARD NR 88151. 2 L 7 4 4F 4A25 1996120500591 19961205 00591 WP 1996 12 5 CKSA96316 1 19961124 A 5320 3754914501 FITTING DOUG DC8 DC863F 302198F WP BS 879 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND INTERCOSTAL FITTING CRACKED STA 879 RIGHT HAND SIDE. REMOVED AND REPLACED IAW DC-8 S RM 51-1-0. C-4 CHECK CARD NR 3010, NON-ROUTINE TASK CARD NR 88492. 2 L 7 4 4F 4A25 1996120500592 19961205 00592 WP 1996 12 5 CKSA96317 1 19961124 A 5320 SPLICE DOUG DC8 DC863F 302198F WP BS 1280-1300 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND LONGERON SPLICE CRACKED STA 1280 THROUGH STA 1300 LONGERON 36. REPAIRED IAW EA 96-32 6 AIA/E/2407, CORROSION CARD NR 5590-055, NON-ROUTINE TASK CARD NR 88502. 2 L 7 4 4F 4A25 1996120500593 19961205 00593 WP 1996 12 5 CKSA96318 1 19961124 A 5320 37592582 SPLICE DOUG DC8 DC863F 302198F WP BS 1260-1280 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND LONGERON SPLICE FITTING CRACKED STA 1260 TO 1280 STRINGER 35R. REPAIRED IAW AIA DRAW ING AIA/E/2407, EER D8-05103, EA 96-326 AND 8110-3 DATED 11-15-96. CORROSION CARD NR 5564-0051, NON-ROUTINE TASK CARD N R 88421. 2 L 7 4 4F 4A25 1996120500594 19961205 00594 WP 1996 12 5 CKSA96319 1 19961124 A 5312 BULKHEAD ANGLE DOUG DC8 DC863F 302198F WP BS 1766 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND FS 1766 AFT PRESSURE BULKHEAD RIGHT HAND HORIZONTAL SUPPORT ANGLE ATTACHING TRANSVERS E FLOORBEAM CORRODED. REMOVED AND REPLACED ANGLE IAW DC-8 SRM 51-1-0 AND INSTALLED FASTENERS IAW DC-8 SRM 51-1-21. COR ROSION CARD NR 5600-0551, NON-ROUTINE TASK CARD NR 88080. 2 L 7 4 4F 4A25 1996120500595 19961205 00595 WP 1996 12 5 CKSA96320 1 19961124 A 5320 WEB DOUG DC8 DC863F 302198F WP BS 32 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND RIGHT HAND NOSE TUNNEL FS 32 CORRODED AT UPPER WEB. CUT OUT DAMAGED AREA AND REPAIRE D IAW SRM 53-2-1. C-4 CHECK WORK CARD NR 3006, NON-ROUTINE TASK CARD NR 88043. 2 L 7 4 4F 4A25 1996120500596 19961205 00596 WP 1996 12 5 CKSA96321 1 19961124 A 5320 37517382 ANGLE DOUG DC8 DC863F 302198F WP RT MLG WW CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND RIGHT WHEEL WELL DOG HOUSE ANGLE CORRODED. REPAIRED ANGLE IAW AIA ENGINEERING SKETCH AIA/E/2379, EA 96-326 AND AIA 8110-3 DATED 11-15-96. C-4 CHECK WORK CARD NR 3010, NON-ROUTINE TASK CARD NR 87586. 2 L 7 4 4F 4A25 1996120500597 19961205 00597 WP 1996 12 5 CKSA96322 1 19961124 A 5753 SKIN DOUG DC8 DC863F 302198F WP LT WING TE CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND LEFT HAND TRAILING EDGE WING JUST OUTBOARD OF OUTBOARD AILERON IS CRACKED IN RADIUS. STOP DRILLED CRACK, FABRICATED REPAIR AS PER AIA EER D8-05082. TREATED AND PRIMED AS PER SRM 51-1-8 AND INSTALLED REPA IR IAW AIA EER D8-05082. CORROSION CARD NR 115L-0551, NON-ROUTINE TASK CARD NR 87286. 2 L 7 4 4F 4A25 1996120500598 19961205 00598 WP 1996 12 5 CKSA96323 1 19961124 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 1660 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND FS 1660 LONGERON 11L CORROSION ON SKIN AROUND SCREW. INSTALLED DOUBLER REPAIR IAW DC -8 SRM 53-2-0 FIGURE 18 SHEET 3. C-4 CHECK WORK CARD NR 3099, NON-ROUTINE TASK CARD NR 87250. 2 L 7 4 4F 4A25 1996120500599 19961205 00599 SO 1996 12 5 SRAA961201 1 19961202 A 2140 CLAMP LKHEED 382 382B 5264104 SO DIVERTER VLV LOOSE A SRAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 916SJ 4134 AFTER TAKEOFF, CARGO COMPARTMENT OVERHEAT LIGHT CAME ON, ACCOMPLISHED AIR TURNBACK TO MHZ WITHOUT INCIDENT. FOUND CLAMP ON CARGO COMPARTMENT DIVERTER VALVE NOT SECURED. TIGHTENED CLAMP AND PERFORMED OPS CHECK PER MM CH 21. 2 H 7 4 4T A1SO 1996120500600 19961205 00600 SO 1996 12 5 SRAA1070 1 19961013 A 5320 SUPPORT BEAM LKHEED 382 382G 526414U SO BS 537 CORROSION A SRAA O OTHER O OTHER IN INSP/MAINT 1 GL 23 905SJ 4472 DURING C-CHECK, FOUND CARGO COMPARTMENT FLOOR PANEL SUPPORT BEAM AT FS 537, RBL 20 HAS CORROSION AT FOWARD AND AFT SIDE BEYOND LIMITS. CUT OUT CORRODED SECTION, FABRICATED AND INSTALLED L-ANGLE, FILLER, STRAP AND DOUBLER IAW LAC SRM CHAPTE R 51-140-22. 2 H 7 4 4T A1SO 1996120500601 19961205 00601 1996 12 5 HEEA968553 4 19961125 A 3453 25410036 7000 RCU BELL 412 412 1182202 SW COCKPIT LORAN DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22608 33075 COMES UP CODE 5. ADVISORY LIGHT STAYS ON. 1 G 7 2 4U H4SW 1996120500602 19961205 00602 SW 1996 12 5 HEEA968554 1 19961125 A 6220 412010124109 BOLT 412010100193 BELL 412 412 1182202 SW M/R FLAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893S 976 976 AAD00020 33022 TUNGSTEN COATING FLAKING FROM BOLT. SENT TO BELL HELICOPTER TEXTRON FOR INSPECTION AND REPAIR. 1 G 7 2 4U H4SW 1996120500603 19961205 00603 EU 1996 12 5 HEEA968555 1 19961125 A 6310 4638202007 CLUTCH 4638001001 BOLKMS 105 BO105S 5626006 EU FREEWHEEL WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6607K 1685 917 S841 FREEWHEEL CLUTCH INNER CAGE WORN BEYOND LIMITS. REPLACED WITH SERVICEABLE CLUTCH. 1 G 7 2 3U H3EU 1996120500604 19961205 00604 EU 1996 12 5 HEEA968556 1 19961125 A 6310 4638202007 CLUTCH 4638001001 BOLKMS 105 BO105S 5626006 EU FREEWHEEL WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3533T 1481 627 S111 FREEWHEEL CLUTCH INNER CAGE WORN BEYOND LIMITS. REPLACED WITH SERVICEABLE CLUTCH. 1 G 7 2 3U H3EU 1996120500605 19961205 00605 EU 1996 12 5 HEEA968557 1 19961125 A 2432 30402002 BATTERY AEROSP AS355 AS355F2 8680812 EU DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6040U 5474 BATTERY WEAK. INSPECTED BY ACCESSORY SHOP AND FOUND BATTERY WOULD NOT PASS CAPACITY TEST. BATTERY PUT INTO SERVICE 7-1 2-95. 1 G 7 2 3U H11EU 1996120500606 19961205 00606 SW 1996 12 5 HEEA968558 1 19961125 A 2432 3055401C BATTERY BELL 206 206L1 1182107 SW DC SYS DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5748Q 45499 BATTERY INSPECTED BY ACCESSORY SHOP AND FOUND BATTERY WOULD NOT PASS CAPACITY TEST. BATTERY PUT INTO SERVICE 2-27-95. 1 G 7 1 3U H2SW 1996120500607 19961205 00607 1996 12 5 HEEA968559 4 19961125 A 3454 071121627 NAV CONTROL BELL 214 214ST 1182106 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 NAV NUMBERS ARE VERY DIM. REPLACED V101 PHOTOCELL. REPAIRED. BENCH CHECK GOOD. 2 G 7 2 4U H10SW 1996120500608 19961205 00608 1996 12 5 HEEA968560 4 19961125 A 3452 066106200 TRANSCEIVER KT76 BELL 206 206L4 1182110 SW COCKPIT ATC DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 62127 52023 DOESN'T REPORT CODE PROPERLY. PERFORMED PRELIMINARY INSPECTION, CLEANED WAFER SWITCHES, REPAIRED. REPLACED R477 RESISTO R DUE TO BEING DETERIORATED. REPAIRED. ALSO REPLACED BLOWN FUSE (F401). REPAIRED. BENCH CHECK GOOD. 1 G 7 1 3U NC H2SW 1996120500609 19961205 00609 NE 1996 12 5 HEEA968561 1 19961125 A 7712 7645001078106 INDICATOR SKRSKY S76 S76A 8143006 NE DUAL TORQUE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 760035 INSTALLED GAUGE IN AIRCRAFT BUT #2 NEEDLE WOULD NOT WORK. 1 G 7 2 3U H1NE 1996120500610 19961205 00610 SW 1996 12 5 HEEA968562 1 19961125 A 2840 206075186005 INDICATOR BELL 206 206L1 1182107 SW COCKPIT STUCK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2764F 45279 LOAD NEEDLE STUCK ON HIGH SIDE. TIME SINCE REPAIR 0:00. 1 G 7 1 3U H2SW 1996120500611 19961205 00611 SW 1996 12 5 HEEA968563 1 19961125 A 6320 206040530001 CASE ASSY 206040004101 BELL 206 206L1 1182107 SW MAIN GR BOX CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 10761 BMC45037 45381 TRANSMISSION OVERHAUL DUE. UPON INSPECTION OF PARTS NOTED: CORROSION ON I/P FLANGE SURFACE AND SURFACE WHERE CENTER CA SE SEATS. REPLACED WITH SERVICEABLE PARTS. SEE MMIR# HEEA0008563 THROUGH HEEA0008566 FOR PARTS REPLACED. 1 G 7 1 3U H2SW 1996120500612 19961205 00612 SW 1996 12 5 HEEA968564 1 19961125 A 6320 206040531001 CASE ASSY 206040004101 BELL 206 206L1 1182107 SW M/R GR BOX CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 10761 BMC45037 45381 TRANSMISSION OVERHAUL DUE. UPON INSPECTION OF PARTS NOTED: CORROSION IN ORING GROOVE. REPLACED WITH SERVICEABLE PARTS. SEE MMIR# HEEA0008563 THROUGH HEEA0008566 FOR PARTS REPLACED. 1 G 7 1 3U H2SW 1996120500613 19961205 00613 SW 1996 12 5 HEEA968565 1 19961125 A 6320 206040052009 HOUSING 206040004101 BELL 206 206L1 1182107 SW M/R GR BOX CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 10761 BMC45037 45381 TRANSMISSION OVERHAUL DUE. UPON INSPECTION OF PARTS NOTED: CORROSION IN BOLT HOLE. REPLACED WITH SERVICEABLE PARTS. S EE MMIR# HEEA0008563 THROUGH HEEA0008566 FOR PARTS REPLACED. 1 G 7 1 3U H2SW 1996120500614 19961205 00614 SW 1996 12 5 HEEA968566 1 19961125 A 6320 206040540003 SHAFT 206040004101 BELL 206 206L1 1182107 SW M/R GR BOX CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 10761 BMC45037 45381 TRANSMISSION OVERHAUL DUE. UPON INSPECTION OF PARTS NOTED:CORRODED SPLINES BEYOND LIMITS. REPLACED WITH SERVICEABLE PAR TS. SEE MMIR# HEEA0008563 THROUGH HEEA0008566 FOR PARTS REPLACED. 1 G 7 1 3U H2SW 1996120500615 19961205 00615 EU 1996 12 5 HEEA968567 1 19961125 A 3213 1055070106 RUBBER RING BOLKMS 105 BO105S 5626006 EU SKID DETERIORATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7170D S840 RUBBER DETERIORATED AND CRACKING. REPLACED WITH NEW RUBBER RINGS. 1 G 7 2 3U H3EU 1996120500616 19961205 00616 EU 1996 12 5 HEEA968568 1 19961125 A 6220 10513142 ROD END ASSY BOLKMS 105 BO105S 5626006 EU M/R CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7170D S840 CORROSION PITS ON ROD ENDS. REPLACED WITH SERVICEABLE ROD ENDS. 1 G 7 2 3U H3EU 1996120500617 19961205 00617 EU 1996 12 5 HEEA968569 1 19961125 A 6220 1051310123 BOLT BOLKMS 105 BO105S 5626006 EU M/R SCORED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7170D S840 SCORING ON SHANK. REPLACED WITH SERVICEABLE BOLT. 1 G 7 2 3U H3EU 1996120500618 19961205 00618 EU 1996 12 5 HEEA968570 1 19961125 A 5210 350A25101722 STRICKER SNIAS 350 AS350B2 8680813 EU LT DOOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 2771 STRICKER WORN. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H9EU 1996120500619 19961205 00619 EU 1996 12 5 HEEA968571 1 19961125 A 5210 350A25107320 LOCK SNIAS 350 AS350B2 8680813 EU LT DOOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 2771 WORN. REPLACED WITH SERVICEABLE LOCK. 1 G 7 1 3U H9EU 1996120500620 19961205 00620 EU 1996 12 5 HEEA968572 1 19961125 A 3150 6082TYTX3 WARNING AUDIO SNIAS 350 AS350B2 8680813 EU ROTOR HORN INOPERATIVE E HEEA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SW 03 60951 2771 ROTOR HORN DOES NOT BLOW. REPLACED WITH SERVICEABLE HORN. 1 G 7 1 3U H9EU 1996120500621 19961205 00621 EU 1996 12 5 HEEA968573 1 19961125 A 7603 TLH52L450 TELEFLEX CABLE BOLKMS 105 BO105S 5626006 EU THROTTLE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7170D S840 CABLE WORN BEYOND LIMITS. REPLACED WITH NEW TELEFLEX CABLE. 1 G 7 2 3U H3EU 1996120500622 19961205 00622 EU 1996 12 5 HEEA968574 1 19961125 A 7603 TLH52L535 TELEFLEX CABLE BOLKMS 105 BO105S 5626006 EU THROTTLE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7170D S840 CABLE WORN BEYOND LIMITS. REPLACED WITH NEW TELEFLEX CABLE. 1 G 7 2 3U H3EU 1996120500623 19961205 00623 EU 1996 12 5 HEEA968577 1 19961125 A 7110 153181 HSD COLLAR BOLKMS 105 BO105S 5626006 EU COWL CHAFED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7170D S840 EXHAUST STACK CLAMP CHAFED THROUGH INNER RING. REPLACED INNER RING WITH SERVICEABLE ONE AND MAKE SURE EXHAUST STACK CLAM P DOES NOT CHAFE. 1 G 7 2 3U H3EU 1996120500624 19961205 00624 EU 1996 12 5 HEEA968578 1 19961125 A 7810 4606AH EXHAUST CLAMP BOLKMS 105 BO105S 5626006 EU EXHAUSY SYS CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7170D S840 T-BOLT HAVE CORROSION PITS, CHAFED T-BOLTS AND CRACKS. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1996120500625 19961205 00625 EU 1996 12 5 HEEA968579 1 19961125 A 7603 TLH452L46 THROTTLE ROD BOLKMS 105 BO105S 5626006 EU ENG WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7170D S840 WORN BEYOND LIMITS. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1996120500626 19961205 00626 EU 1996 12 5 HEEA968580 1 19961125 A 7810 4606AH CLAMP BOLKMS 105 BO105S 5626006 EU EXHAUST WELD FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3520T S539 CLAMPS HAVE BROKEN SPOT WELDS AND ARE CRACKED. REMOVED PART AND INSTALLED SERVICEABLE PARTS. 1 G 7 2 3U H3EU 1996120500627 19961205 00627 EU 1996 12 5 HEEA968581 1 19961125 A 7712 305731365 INDICATOR SNIAS 350 AS350B2 8680813 EU ENG TORQUE WONT CALIB E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100U 1695 2863 TORQUE IND WON'T CALIBRATE. 1 G 7 1 3U H9EU 1996120500628 19961205 00628 EU 1996 12 5 HEEA968583 1 19961125 A 6400 355A09103601 BEARING SNIAS 350 AS350B2 8680813 EU T/R UNBONDED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100U 609 2863 BEARING UNBONDED. 1 G 7 1 3U H9EU 1996120500629 19961205 00629 SW 1996 12 5 HEEA968585 1 19961125 A 6230 299402023D SEAL 412040366105 BELL 412 412 1182202 SW M/R MAST LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911PB 1043 A118 33186 SEAL LEAKING. 1 G 7 2 4U H4SW 1996120500630 19961205 00630 GL 1996 12 5 HEEA968586 2 19961125 A 7250 6886407 WHEEL 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL TURB 1ST STG FAILED E HEEA K NONE T ENGINE CASE PENETRATION NR NOT REPORTED 1 SW 03 911FL 437 CAT40303 S717 CAE831144 ENGINE REMOVED DUE TO TURBINE WHEEL FAILURE. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: #1 WHEEL EXHIBITS A RIM FAILURE. CRACK ORIGINATED AT RIM AND PROGRESSED ON THE LEADING EDGE SIDE 3/8" UNTIL OVERLOAD, PROGRESSING AROUND A 1/16" X 1/4" CASTING FLAW 5/8" FROM THE TRAILING EDGE CENTER OF WHEEL. FLAW IS SMOOTH TEXTURED AND APPEARS TO BE A 1/4" CIRCULAR PLUG INSERT. 45% OF WHEEL NOT RECOVERABLE DUE TO EXITING THROUGH GP SECTION AND A/C COWLING. 1 G 7 2 3U 3 U H3EU E4CE 1996120500631 19961205 00631 GL 1996 12 5 HEEA968587 2 19961125 A 7250 6886407 WHEEL 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL TURB 1ST STG DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 54197 1404 CAT40338 S805 CAE830763 ENGINE REMOVED DUE TO COMPRESSOR OVERHAUL. PERFORMED HOT END INSPECTION ON TURBINE DUE TO COMPRESSOR FOD. UPON INSPECT ION OF TURBINE NOTED MINOR SULFIDATION ON ALL #1 WHEEL BLADES. SCRAPPED 1ST STAGE WHEEL. 1 G 7 2 3U 3 U H3EU E4CE 1996120500632 19961205 00632 EU 1996 12 5 HEEA968591 1 19961125 A 6520 4619002003 GEAR BOX BOLKMS 105 BO105S 5626006 EU INTERMED GR BOX MAKING METAL E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 50293 3481 S677 INTERMEDIATE GR BOX MAKES METAL. 1 G 7 2 3U H3EU 1996120500633 19961205 00633 SW 1996 12 5 HEEA968592 1 19961125 A 6230 214010411111 SLEEVE 214010501115 BELL 214 214ST 1182106 SW M/R BEARING FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5748M 2251 A291 28102 BEARING SET SPINNING ( GROOVED BEYOND LIMITS) 2 G 7 2 4U H10SW 1996120500634 19961205 00634 SW 1996 12 5 HEEA968593 1 19961125 A 6230 214010418001 NUT 214010501115 BELL 214 214ST 1182106 SW M/R BEARING SET WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5748M 2251 A291 28102 BEARING SET SPINNING (WORN) 2 G 7 2 4U H10SW 1996120500635 19961205 00635 SW 1996 12 5 HEEA968594 1 19961125 A 6230 214010482001 BEARING SET 214010501115 BELL 214 214ST 1182106 SW M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5748M 2251 A291 28102 BEARING SET SPINNING (WORN) 2 G 7 2 4U H10SW 1996120500636 19961205 00636 SW 1996 12 5 HEEA968595 1 19961127 A 6220 214010104121 GRIP 214010100207 BELL 214 214ST 1182106 SW M/R CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 745H 3450 A272 28200 CORROSION ON GRIP TANGS BEYOND LIMITS. 2 G 7 2 4U H10SW 1996120500637 19961205 00637 SW 1996 12 5 HEEA968596 1 19961127 A 5302 206032308103S FRAME BELL 206 206L3 1182108 SW TB MOUNT CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3107N 1603 51512 FRAME IS CRACKED. (CRACKED TAILBOOM MOUNT RING) 1 G 7 1 3U H2SW 1996120500638 19961205 00638 SW 1996 12 5 HEEA968597 1 19961129 A 5260 212075418103 ACTUATOR BELL 412 412 1182202 SW STEP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D 33076 WILL NOT RETRACT - POPS CIRCUIT BREAKER. INSPECTED BY ACCESSORY OVERHAUL SHOP AND FOUND EXTEND TRAVEL TOO SHORT 5.578" SHOULD BE BETWEEN 5.620" - 5.680". 1 G 7 2 4U H4SW 1996120500639 19961205 00639 SW 1996 12 5 96ZZZX5841 1 19961030 A 6210 206015001107 BLADE BELL 206 206L4 1182110 SW M/R WORN A A NYBA K NONE O OTHER IN INSP/MAINT 1 EA 11 125NH 1838 A149 52099 DURING NORMAL AIRCRAFT USAGE NEW YORK HELICOPTER HAS NOTED THE LEADING EDGE OF THE MAIN ROTOR BLADE IS EXPERIENCING ABNO RMAL WEAR IN THE FORM OF SCALING/SPLINTERING ON A MODERATE LEVEL. NEW YORK HELICOPTER IS AWAITING RECOMMENDATIONS FROM BELL HELICOPTER TEXTRON ON THIS MATTER. THIS HAS BEEN THE SECOND BLADE WHICH HAS EXPERIENCED EXFOLIATON OF THE LEADING EDGE. NEW YORK HELICOPTER BELIEVES THIS TO BE A SAFETY ISSUE WITH THE BLADE INTEGRITY AND BLADE PERFORMANCE DIGRESSION. ABOVE BLADE PREVIOUSLY REPAIRED FOR EXFOLIATION BY BELL HELICOPTER TEXTRON CPR NR 07587200. 1 G 7 1 3U NC H2SW 1996120500641 19961205 00641 EU 1996 12 5 96ZZZX5843 1 19960627 A 6230 1051011305 BELLOWS BOLKMS 105 BO105LSA3 5626020 EU M/R MAST TORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 202LF 430 2014 BELLOWS IS TORN AROUND CLAMP AND FOLD AREAS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H3AU 1996120500642 19961205 00642 EU 1996 12 5 96ZZZX5844 1 19960426 A 6210 10513103505 BLADE PIN BOLKMS 105 BO105LSA3 5626020 EU M/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 202LF 289 2014 BLADE PIN WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H3AU 1996120500643 19961205 00643 EU 1996 12 5 96ZZZX5845 1 19960510 A 6410 134616P BUSHING BOLKMS 105 BO105LSA3 5626020 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 202LF 327 2014 TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U H3AU 1996120500644 19961205 00644 EU 1996 12 5 96ZZZX5846 1 19960510 A 6410 134617P BUSHING BOLKMS 105 BO105LSA3 5626020 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 202LF 327 2014 TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U H3AU 1996120500645 19961205 00645 EU 1996 12 5 96ZZZX5847 1 19960413 A 6420 1053170023 BEARING BOLKMS 105 BO105LSA3 5626020 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 203LF 382 2015 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW 2 EACH UNITS, CORRECTED PROBLEM. 1 G 7 2 3U H3AU 1996120500646 19961205 00646 EU 1996 12 5 96ZZZX5848 1 19960520 A 6410 134616P BUSHING BOLKMS 105 BO105LSA3 5626020 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 203LF 420 2015 TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U H3AU 1996120500647 19961205 00647 EU 1996 12 5 96ZZZX5849 1 19960520 A 6410 134617P BUSHING BOLKMS 105 BO105LSA3 5626020 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 203LF 420 2015 TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U H3AU 1996120500648 19961205 00648 EU 1996 12 5 96ZZZX5850 1 19960816 A 6220 704A33633156 SPHERICAL STOP SNIAS 350 AS350B2 8680813 EU M/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 6099P 534 3172 2818 SPHERICAL STOP ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996120500649 19961205 00649 EU 1996 12 5 96ZZZX5851 1 19960819 A 6220 740A33633156 SPHERICAL STOP SNIAS 350 AS350B2 8680813 EU M/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 6099P 534 3171 2818 SPHERICAL STOP ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996120500650 19961205 00650 EU 1996 12 5 96ZZZX5852 1 19960817 A 6410 704A33633171 LAMINATED HINGE SNIAS 350 AS350D 8680803 EU T/R PINK WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 779LF 80 1621 HINGE ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, FROM KIT 350A33-2153-00 CORRECTED PR OBLEM. 1 G 7 1 3U H9EU 1996120500651 19961205 00651 EU 1996 12 5 96ZZZX5853 1 19960709 A 6410 704A33633171 LAMINATED HINGE SNIAS 350 AS350D 8680803 EU T/R YELLOW WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 779LF 224 1621 HINGE ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECTED PROBLEM . 1 G 7 1 3U H9EU 1996120500652 19961205 00652 EU 1996 12 5 96ZZZX5854 1 19960903 A 6220 117775P BALL JOINT SNIAS 350 AS350B2 8680813 EU STARFLEX WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911LR 588 2404 TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 3 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996120500653 19961205 00653 EU 1996 12 5 96ZZZX5855 1 19960602 A 6410 704A33633116 LAMINATE BEARING SNIAS 350 AS350B2 8680813 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911LR 305 2404 LAMINATED BEARING ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 4 EACH NEW UNITS FROM KIT 355A09-1036-00, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996120500654 19961205 00654 EU 1996 12 5 96ZZZX5856 1 19960602 A 6410 704A33633171 LAMIANTED HINGE SNIAS 350 AS350B2 8680813 EU T/R GREEN WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911LR 169 2404 LAMINATED HINGE ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CO RRECTED PROBLEM. 1 G 7 1 3U H9EU 1996120500655 19961205 00655 EU 1996 12 5 96ZZZX5857 1 19960905 A 6410 704A33633171 LAMIANTED HINGE SNIAS 350 AS350B2 8680813 EU T/R YELLOW WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911LR 159 2404 LAMINATED HINGE ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CO RRECTED PROBLEM. 1 G 7 1 3U H9EU 1996120500656 19961205 00656 EU 1996 12 5 96ZZZX5858 1 19960712 A 6410 704A33633171 LAMINATED HINGE SNIAS 350 AS350B2 8680813 EU T/R WHITE WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 92LG 67 2575 LAMINATED HINGE ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CO RRECTED PROBLEM. 1 G 7 1 3U H9EU 1996120500657 19961205 00657 EU 1996 12 5 96ZZZX5859 1 19960925 A 6410 704A33633116 LAMINATE BEARING SNIAS 350 AS350B2 8680813 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 94LG 344 2728 LAMINATED BEARING ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 4 EACH NEW UNITS FROM KIT 355A09-1036-00, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996120500658 19961205 00658 EU 1996 12 5 96ZZZX5860 1 19960925 A 6410 704A33633171 LAMINATED HINGE SNIAS 350 AS350B2 8680813 EU T/R PINK WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 94LG 344 2728 LAMINATED HINGE ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CO RRECTED PROBLEM. 1 G 7 1 3U H9EU 1996120500659 19961205 00659 EU 1996 12 5 96ZZZX5861 1 19961010 A 5410 350A5801100801 FIREWALL SNIAS 350 AS350B2 8680813 EU ENG CRACKED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 96LG 868 2817 FIREWALL CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996120500660 19961205 00660 EU 1996 12 5 96ZZZX5862 1 19960605 A 6240 50071550020 SENSOR SNIAS 350 AS350B2 8680813 EU M/R TACH INTERMITTENT A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 96LG 649 1933 2817 TACH SENSOR UNIT OPERATES INTERMITTENTLY. CAUSED BY SHORT ON CANNON PLUG SIDE. REPLACED WITH NEW UNIT, CORRECTED PROBL EM. 1 G 7 1 3U H9EU 1996120500661 19961205 00661 EU 1996 12 5 96ZZZX5863 1 19960625 A 7931 642790041 TRANSMITTER SNIAS 350 AS350B2 8680813 EU ENG OIL DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 96LG 649 717 2817 TRANSMITTER GIVES INACCURATE OIL PRESSURE READINGS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996120500662 19961205 00662 EU 1996 12 5 96ZZZX5864 1 19960625 A 7931 642790041 TRANSMITTER SNIAS 350 AS350B2 8680813 EU ENG OIL FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 96LG 48 1536 2817 WITH BATTERY ON, GAUGE GOES TO 10 BARS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996120500663 19961205 00663 EU 1996 12 5 96ZZZX5865 1 19960808 A 6410 704A33633171 LAMINATED HINGE SNIAS 350 AS350B2 8680813 EU T/R PINK WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 96LG 264 2817 LAMINATED HINGE ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, C ORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996120500664 19961205 00664 EU 1996 12 5 96ZZZX5866 1 19960809 A 2510 AFG0582730 HARNESS SNIAS 350 AS350B2 8680813 EU COCKPIT SAFETY MALFUNCTION A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 96LG 749 24262 2817 INERTIA SAFETY HARNESS WILL NOT RETRACT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996120500665 19961205 00665 EU 1996 12 5 96ZZZX5867 1 19960723 A 6320 1B675 DETECTOR SNIAS 350 AS350B2 8680813 EU MGB MALFUNCTION A R7MA K NONE N FALSE WARNING IN INSP/MAINT 1 NM 11 6099P 886 2818 MGB WARNING LIGHT COMES ON VERY DIMLY WHEN BATTERY IS SWITCHED ON. THEN LIGHT GOES OUT AFTER 2 TO 3 SECONDS. REPLACED W ITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996120500666 19961205 00666 EU 1996 12 5 96ZZZX5868 1 19960819 A 6220 704A33633156 SPHERICAL STOP SNIAS 350 AS350B2 8680813 EU M/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 6099P 534 3153 2818 SPHERICAL STOP ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1996120500667 19961205 00667 1996 12 5 96ZZZX5869 4 19960925 A 2211 117884141 COMPUTER BOLKMS 117 BK117A4 5626017 EU YAW CSAS SHORTED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 586BH 204 1187051 7129 YAW CSAS COMPUTER INTERNAL SHORT. 1 G 7 2 3U H13EU 1996120500669 19961205 00669 NM 1996 12 5 USAASB96213 1 19961020 A 2150 PACK BOEING 737 737301 1384611 NM RIGHT FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 591US 23936 DEN - FLT 122 - CAPTAIN REPORTED HE WAS UNABLE TO PRESSURIZE THE AIRCRAFT IN CLIMB-OUT. RETURNED TO FIELD AT DEN. THE F LIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE RT PACK FROZEN AND REPLACED THE RT 35 DEGREE TEMP SENSOR ( PN B7040-2), S/O VALVE (PN 321942-1-1), AND CONTROLLER (PN 607510-3). RAN ENGINES AND FOUND LT PRSOV BACKING DOWN AT HI GH POWER WHICH LED TO REPLACEMENT OF LT HIGH STAGE REGULATOR (PN 107484-5), PRSOV REGULATOR (PN 107492-2), AND PRECOOLER CONTROL VALVE (PN 3289562-5). RAN ENGINES, SYSTEM CHECKS OK. (X) 2 L 7 2 4F RT A16WE 1996120500670 19961205 00670 CE 1996 12 5 GLBA96201 1 19961013 A 3610 PACKING BEECH 1900 1900D 1154162 CE RT BLEED AIR FAILED A GLBA O OTHER J WARNING INDICATION CR CRUISE 1 CE 01 211UX UE211 ISN - RIGHT BLEED AIR FAIL ILLUMINATED IN-FLIGHT. MAINTENANCE REPLACED PACKINGS IN RIGHT DUCT ASSY AND REPAIRED EVA TUB ING. SYSTEM OPERATED NORMALLY. (X) 2 L 7 2 4T RT A24CE 1996120500671 19961205 00671 WP 1996 12 5 96ZZZX5871 1 19961008 A 5400 58950815 SPAR DOUG DC8 DC8F54 3021926 WP NR 1 PYLON CRACKED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 57FB 45669 DURING C-CHECK INSPECTION, FOUND NR 1 PYLON UPPER OUTBOARD SPAR CRACKED. REMOVED AND REPLACED NR 1 PYLON UPPER OUTBOARD SPAR IAW DOUGLAS DRAWING 5895081. (X) 2 L 7 4 4F 4A25 1996120500672 19961205 00672 EU 1996 12 5 AWXA960642 1 19961028 A 3350 321454 POWER SUPPLY AIRBUS 320 A320232 3930326 EU CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 641AW 2400 453 PHX - FLT 2245 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS FAIL TEST PER CARD 18M05302. REMOVED AN D REPLACED L1 DOOR EMERGENCY LIGHT POWER SUPPLY. OPERATIONS CHECK GOOD PER 18M05302. (X) 2 L 7 2 4F RT A28NM 1996120500673 19961205 00673 NM 1996 12 5 AWXA960620 1 19961008 A 5315 FLOOR BEAM BOEING 737 737277 1384570 NM BS 1016 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 184AW 22651 PAE - FLT 7837 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM BS 1016, LBL 26. REMOVED CORRODED FLOO R BEAM, FABRICATED REPAIR PARTS, AND INSTALLED PER E.R. 2-53-15-50, TCO-PAN-96-1408RR-8110-3. (X) 2 L 7 2 4F RT A16WE 1996120500674 19961205 00674 CE 1996 12 5 96ZZZX5872 1 19961029 A 7920 330997F120414 OIL LINE 1143890005 BEECH 1900 1900C 1154161 CE LT ENGINE LOOSE A MASA E ENGINE SHUTDOWN K J Y FLUID LOSS WARNING INDICATION ENGINE STOPPAGE AP APPROACH 1 SW 01 156YV UC156 LEFT ENGINE FAILED 1 MINUTE FROM TOUCH DOWN AT ABQ. SECURED ENGINE AND LANDED WITHOUT INCIDENT. DURING INVESTIGATION F OUND ONE OIL LINE TO THE OIL COOLER LOOSE. 2 L 7 2 4T RT A24CE 1996120500675 19961205 00675 NE 1996 12 5 96ZZZX5873 2 19961019 A 7261 8477601 OIL LINE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9A 52048 NE NR 1 ENGINE CRACKED A TWAA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 05 921L 47107 CMH - FLT 425 - DURING CRUISE, SHUT DOWN NR 1 ENGINE, SN 2146, DUE TO LOSS OF OIL QUANTITY. FOUND CRACKED OIL LINE, MFG PN 814776-01. REPLACED OIL LINE, SERVICED ENGINE OIL. ENGINE OPERATION CHECKED NORMAL. ENGINE TOTAL TIME: 58,369 HO URS; 68,640 CYCLES. CHECK C- 11-13-95 - STL. 2 L 7 2 4F 4 F A6WE E2EA 1996120500676 19961205 00676 WP 1996 12 5 EIAA9659 1 19961030 A 5320 INTERCOSTAL DOUG DC9 DC932F 3022067 WP BS 718-737 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 47220 SAT - FLOOR SUPPORT INTERCOSTAL RB 153 STATION 718 TO 737 CRACKED. FABRICATED REPLACEMENT INTERCOSTAL WEB STATION 718 T O 737 RBL 53 PER SRM 51-10-1 AND 51-30-2. (M) 2 L 7 2 4F A6WE 1996120500677 19961205 00677 WP 1996 12 5 EIAA9660 1 19961030 A 5320 INTERCOSTAL DOUG DC9 DC932F 3022067 WP FR 579 - 598 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 47220 SAT - CORROSION ON TOP FLANGE OF INTERCOSTAL FRAME 579 TO 598 BETWEEN STRINGER 27R AND 28R IS OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER FR 579 TO 598 INTERCOSTAL BETWEEN STRINBER 27R AND 28R PER SRM. (M) 2 L 7 2 4F A6WE 1996120500678 19961205 00678 WP 1996 12 5 EIAA9661 1 19961030 A 5320 5931960511 FITTING DOUG DC9 DC932F 3022067 WP BS 718 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 47220 SAT - LEFT WHEEL WELL TO KEEL BEAM ATTACH FITTING STATION 718 IS CRACKED. CRACK EMANATES FROM THE FORWARD VERTICAL BOLT HOLE FORWARD IN THE HORIZONTAL FLANGE OF THE FITTING. REMOVED AND REPLACED FITTING IAW SRM 51-30-2 AND 51-20-0. (M) 2 L 7 2 4F A6WE 1996120500679 19961205 00679 WP 1996 12 5 EIAA9662 1 19961030 A 5320 INTERCOSTAL DOUG DC9 DC932F 3022067 WP BS 945-965 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 48522 47220 SAT - AFT BAG BIN BS 945-965 INTERCOSTAL AT STATION 28R HAS EXFOLIATION CORROSION. REMOVED, FABRICATED AND INSTALLED RE PLACEMENT INTERCOSTAL IAW SRM 51-11-3 AND 51-30-2. (M) 2 L 7 2 4F A6WE 1996120500680 19961205 00680 WP 1996 12 5 EIAA9663 1 19961030 A 5311 9919682N FRAME DOUG DC9 DC932F 3022067 WP FR 718 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 48522 47220 SAT - FRAME 718 RIGHT IS CRACKED BEYOND SERVICABLE LIMITS OF S/B 53-131. REMOVED AND REPLACED FRAME PER S/B 53-131 AND SRM 51-30-2. INTERCOSTAL IAW SRM 53-11-3 AND 51-30-2. (M) 2 L 7 2 4F A6WE 1996120500681 19961205 00681 WP 1996 12 5 EIAA9664 1 19961030 A 5311 FRAME DOUG DC9 DC932F 3022067 WP FRAME 1038 CHAFFED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 48522 47220 SAT - FRAME 1038 AT STRINGER 5L HAS A HOLE CHAFFED IN FRAME WEB BY LEFT AIR CONDITIONING PACKAGE ROTARY ACTUATOR. FABRI CATED AND INSTALLED WEB DOUBLER REPAIR FRAME 1038 STRINGER 5L PER SRM 53-11 FIG 1. (M) 2 L 7 2 4F A6WE 1996120500682 19961205 00682 WP 1996 12 5 EIAA9665 1 19961030 A 5320 ANGLE DOUG DC9 DC932F 3022067 WP FS 996 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 48522 47220 SAT - CORRODED FLOOR SUPPORT ANGLE AT AFT CARGO STATION 996 STRINGER 25L-25R. FABRICATED NEW ANGLES AND INSTALLED PER S RM 53-01 FIG 2 AND 51-30-2. (M) 2 L 7 2 4F A6WE 1996120500683 19961205 00683 WP 1996 12 5 EIAA9666 1 19961030 A 5311 FRAME DOUG DC9 DC932F 3022067 WP FR 274 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 48522 47220 SAT - FRAME 274 LOWR FLAGNE CRACKED AT ATTACHMENT POINT STRINGER 29L AND 29R. FABRICATED NEW ANGLES AND FILLERS AND INS TALLED PER SRM 51-10-3 FIG 5, 51-10-3 AND 51-30-2. (M) 2 L 7 2 4F A6WE 1996120500684 19961205 00684 WP 1996 12 5 EIAA9667 1 19961030 A 5320 5912494501 JAMB DOUG DC9 DC932F 3022067 WP BS 370-427 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 48522 47220 SAT - CORRODED FORWARD CARGO LOWER DOOR JAMB AT STATION 370-427. FABRICATED NEW SECTION AND INSTALLED PER SRM 53-05 FIG 44, 51-30-2 AND 51-10-3. (M) 2 L 7 2 4F A6WE 1996120500685 19961205 00685 SO 1996 12 5 96ZZZM1542 1 19961108 A 2913 1159SCH20041 HYD PUMP GULSTM G1159 GIV 3980115 SO LT ENGINE FAILED A YNOA O OTHER J WARNING INDICATION CR CRUISE 1 EA 11 917W 1158 EN ROUTE FROM LAGUARDIA TO NICE FRANCE ON AN FAR PART 91 FLT, WHEN DURING CRUISE CONFIGURATION COMBINED HYD PRESSURE WAS LOST. THE FLIGHT CREW CONTINEUD TO DESTINATION DEPLOYING THE LANDING GEAR USING THE ALTERNATE SYSTEM AND LANDED WITHOU T INCIDENT. MAINTENANCE AUDITED AND AUTHORIZED A LOCAL MAINTENANCE AGENCY AND REPAIRS WERE COORDINATED RETURNING THE AI RCRAFT TO SERVICE. (M) 2 L 7 2 4F RT A12EA 1996120500686 19961205 00686 WP 1996 12 5 ORJA9685 1 19961103 A 5320 ANGLE DOUG DC9 DC983 3022083 WP FORWARD LAV CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 833RA 53045 FOUND CORROSION ON LOWER FORWARD ANGLE FORWARD LAVATORY. FABRICATED AND INSTALLED ANGLE IAW EA 13-25, EA 006, DATED 11/ 05/96, APPROVED BY 8110.3, DATED 11/06/96. REF AAR N/R 2000-0055. (M) 2 L 7 2 4F RT A6WE 1996120500687 19961205 00687 EA 1996 12 5 96ZZZM1543 1 19961111 A 2910 DSC187A40126 FLEX LINE 729500615009 DHAV DHC7 DHC7102 2802708 EA NR 1 HYD SYSTEM HOLE A CICA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION LD LANDING 1 SO 17 703MG DHC266 103 FLT 4920 - PID-PBI - PILOT REPORTED NR 1 HYD SYSTEM LOSS OF FLUID AND PRESSURE. PILOT REPORTED EMERGENCY TO PBI. PILOT LANDED AIRCRAFT AND TAXIED TO THE GATE AND PASSENGERS DEPLANED. MAINTENANCE INSPECTION FOUND LEFT INBOARD GROUND SPOIL ER HYDRAULIC LINE TO ACTUATOR RUPTURED. REPLACED LINE AND SERVICED HYD SYSTEM. OPERATION CHECKED AIRCRAFT SYSTEM AND L EAK CHECKED. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 4 4T A20EA 1996120500688 19961205 00688 NM 1996 12 5 96ZZZM1544 1 19961111 A 5240 001A711E1400008 DOOR DORNER DO32 DO328100 2996000 NM RT NACELLE DAMAGED A A EQGA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 SW 19 350AD 2459 2459 1110 3050 AFTER DEPARTING DFW EN ROUTE TO CUU, IT WAS NOTED THAT THE RIGHT ENGINE INBOARD COWLING LEADING EDGE PEELED BACK FROM TH E FRAME AND A PIECE BROKEN OFF. CAPTAIN MADE AN EMERGENCY LANDING AT DFW WITHOUT INCIDENT. AFTER LANDING, THE COWLING DOOR WAS INSPECTED AND THE SPOT WELDS ALONG THE LEADING EDGE AND THE BOTTOM OF THE DOOR ALONG WITH SEVERAL OTHERS ON THE FRAME WERE FOUND TO BE DEFECTIVE AND NOT HOLDING. THE DOOR WILL BE RETURNED TO DORNIER FOR ANALYSIS. A REPLACEMENT DO OR WILL BE INSTALLED AND THE AIRCRAFT WILL BE RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A45NM 1996120500689 19961205 00689 WP 1996 12 5 EIAA9668 1 19961030 A 5311 FRAME DOUG DC9 DC932F 3022067 WP CARGO COMPT CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 48522 47220 SAT - AFT CARGO HAS CRACKS IN FRAME 908-937 UPPER CEILING WEB AT STRIGNER 19L ABOVE AFT CARGO DOOR LIGHT. STOP DRILLED CRACKS, PERFORMED EDDY CURRENT INSPECTION ON STOP DRILL HOLES, FABRICATED DOUBLER AND INSTALLED PER SRM 51-10-3, 53-11-3 FIGURE 1, 2 AND 3, 53-01 FIGURE 3 SHEET 1, 2 AND 3 AND NDTS PM 06-00-07. (M) 2 L 7 2 4F A6WE 1996120500690 19961205 00690 WP 1996 12 5 EIAA9669 1 19961030 A 5320 ANGLE DOUG DC9 DC932F 3022067 WP BS 598 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 48522 47220 SAT - FORWARD CARGO COMPARTMENT STATION 598, STRINGER 28R HORIZONTAL AND VERTICAL PANEL SUPPORT ANGLES ARE CRACKED. FAB RICATED AND INSTALLED HORIZONTAL ANGLE IAW SRM 51-30-0, FIGURE 76 SHEET 1 AND 3. REMOVED DAMAGED AREA ON VERTICAL ANGLE IAW SRM 53-01 FIGURE 2 SHEET 4. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-30-2, 53-01 FIGURE 2 SHEET 4 AND 53-2 1-0 FIGURE 7C SHEET 1 AND 3. (M) 2 L 7 2 4F A6WE 1996120500691 19961205 00691 WP 1996 12 5 EIAA9670 1 19961030 A 5320 FLOOR SUPPORT DOUG DC9 DC932F 3022067 WP BS 218-285 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 48522 47220 SAT - FORWARD CARGO COMPARTMENT FRAME 362 TO FORWARD BULKHEAD HAS LIGHT SURFACE CORROSION ON FLOOR SUPPORT AT STATION 28 R. REMOVED FLOOR SUPPORT, FABRICATED AND INSTALLED REPLACEMENT CHANNEL LE IAW SRM 51-30-2 FROM STATION 218 TO 285, FROM AREA 285 TO 362. REMOVED CORROSION IAW SRM 51-10-3, AREA FROM STATION 285 TO 362 WITHIN LIMITS. (M) 2 L 7 2 4F A6WE 1996120500692 19961205 00692 WP 1996 12 5 EIAA9671 1 19961030 A 5320 FLOOR SUPPORT DOUG DC9 DC932F 3022067 WP BS 996 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 48522 47220 SAT - FS 996 LOWER SUPPORT ANGLE HAS EXFOLIATION CORROSION FROM LONGERON 25L TO 25R. FABRICATED AND INSTALLED FLOOR SUP PORT ANGLE FS 996 FROM LONGERON 26L TO 29R PER SRM 53-01 FIG 2 AND SRM 53-11-3. (M) 2 L 7 2 4F A6WE 1996120500693 19961205 00693 WP 1996 12 5 EIAA9672 1 19961030 A 5311 FRAME DOUG DC9 DC932F 3022067 WP BS 237 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 48522 47220 SAT - FRAME 237 LONGERON 24R CORRODED. FABRICATED AND INSTALLED REPAIR SPLICE TO FRAME BS 237 LONGERON 24R PER SRM 53-0 3 FIGURE 2A. (M) 2 L 7 2 4F A6WE 1996120500694 19961205 00694 WP 1996 12 5 EIAA9673 1 19961030 A 5312 BULKHEAD CHORD DOUG DC9 DC932F 3022067 WP BS 756 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 48522 47220 SAT - BULKHEAD 756 UPPER T-CHORD CORRODED LBL 22 TO LBL 31. FABRICATED AND INSTALLED BULKHEAD T-CHORD SECTION BS 756 LB L 22 TO LBL 31 PER SRM 53-01 FIG 2, 51-10-3 AND 53-14-3. (M) 2 L 7 2 4F A6WE 1996120500695 19961205 00695 WP 1996 12 5 EIAA9674 1 19961030 A 5347 TIE DOWN RAILS DOUG DC9 DC932F 3022067 WP BS 756-900 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 48522 47220 SAT - AFT CARGO BAY LEFT AND RIGHT TIE DOWN RAILS BS 756 TO 900 CORRODED. FABRICATED AND INSTALLED TIE DOWN RAILS PER S RM 53-21-0 FIGURE 8 AND 51-30-2. (M) 2 L 7 2 4F A6WE 1996120500696 19961205 00696 WP 1996 12 5 EIAA9675 1 19961030 A 5321 FLOOR PANEL DOUG DC9 DC932F 3022067 WP CARGO BAY CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 48522 47220 SAT - FORWARD CARGO BAY FLOOR PANEL NR 3 IS CORRODED. REPAIRED FLOOR PANEL PER SRM 51-70-2. (M) 2 L 7 2 4F A6WE 1996120500697 19961205 00697 WP 1996 12 5 EIAA9676 1 19961030 A 5320 SUPPORT DOUG DC9 DC932F 3022067 WP BS 218-285 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 48522 47220 SAT - FORWARD CARGO BAY FRAME 362 FLOOR SUPPORT IS CORRODED AT STRINGER 28R. FABRICATED AND INSTALLED FLOOR SUPPORT CHA NNEL FROM BS 218 TO 285 AND 285 TO 362 PER SRM 53-21-0, 53-01 FIGURE 2 AND 51-21-3. (M) 2 L 7 2 4F A6WE 1996120500698 19961205 00698 WP 1996 12 5 EIAA9677 1 19961030 A 5320 59220291 FLOOR STRUT DOUG DC9 DC932F 3022067 WP FR 237 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 48522 47220 SAT - FORWARD CARGO BAYFRAME 237 FLOOR SUPPORT STRUT AT LONGERON 24R IS CRACKED. REMOVED, FABRICATED AND INSTALLED FLOO R SUPPORT STRUT AT FR 237 LONGERON 24R PER DAC DRAWING 5922079 AND SRM 51-30-2. (M) 2 L 7 2 4F A6WE 1996120500699 19961205 00699 WP 1996 12 5 EIAA9678 1 19961030 A 5320 FITTING DOUG DC9 DC932F 3022067 WP FR 237 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 48522 47220 SAT - FORWARD CARGO BAYFRAME 237 FLOOR SUPPORT FITTING AT LONGERON 24R IS CRACKED. REMOVED AND REPLACED FITTING PER SRM 51-30-2. (M) 2 L 7 2 4F A6WE 1996120500700 19961205 00700 WP 1996 12 5 EIAA9650 1 19961030 A 5320 INTERCOSTAL DOUG DC9 DC932F 3022067 WP BS 218/237 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 48522 47220 SAT - FORWARD CARGO BAY INTERCOSTAL BETWEEN STATION 218 AND 237 AT STRINGER 27R/28R CORRODED. REMOVED, FABRICATED AND I NSTALLED INTERCOSTAL PER SRM 53-11-2 FIG 1D AND SRM 53-10-1 FIG 3. (M) 2 L 7 2 4F A6WE 1996120500701 19961205 00701 WP 1996 12 5 EIAA9679 1 19961101 A 5320 ANGLES DOUG DC9 DC932F 3022067 WP BS 598 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 48522 47220 SAT - FORWARD CARGO BAY BS 598 STRINGER 28R BOTH HORIZONTAL AND VERTICAL PANEL SUPPORT ANGLES ARE CRACKED. FABRICATED A ND INSTALLED HORIZONTAL ANGLE PER SRM 51-30-2, 53-21-0 FIG 7C SHEET 1 AND 3. FABRICATED AND INSTALLED VERTICLE ANGLE PE R SRM 51-30-2, 53-01 FIG 2 SHEET 4 AND SRM 53-21-0 FIG 7C SHEET 1/3. SECOND STRUCTURE. (M) 2 L 7 2 4F A6WE 1996120500702 19961205 00702 WP 1996 12 5 EIAA9680 1 19961101 A 5330 SKIN DOUG DC9 DC915F 3022037 WP BS 642 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 916F 49920 47044 MZJ - EXFOLIATION CORROSION WAS FOUND ON THE LOWER FUSELAGE EXTERNAL SKIIN AT BS 642, LONGERON 30, AND BL 0.000. CORROD ED AREA MEASURES 5.25 INCH LONG AND 4.90 INCH WIDTH. TWO EXTERNAL FINGER REPAIR DOUBLERS FABRICATED AND INSTALLED ON TR IMMED OUT AREA. AN EXTERNAL REPAIR DOUBLER FABRICATED AND INSTALLED. APPROVAL SOURCES, DOUGLAS TELEX NR MISC6900/AJC A ND 8110-3 DATED 30 SEPT 1996 REF ECRA NR 916-53-016-2. (M) 2 L 7 2 4F A6WE 1996120500703 19961205 00703 NM 1996 12 5 EIAA9681 1 19961104 A 5753 SKIN BOEING 747 747273C 1384896 NM TE FLAP DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 JFK - OUTBOARD FLAP DAMAGED FROM LEADING EDGE TO END CAP. (M) 2 L 7 4 4F A20WE 1996120500704 19961205 00704 WP 1996 12 5 REXA96058 2 19961023 A 7321 8778024 FUEL CONTROL WOODWARD BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110U 01514 WP LT ENGINE INOP A REXA C D ABORTED TAKEOFF RETURN TO BLOCK E VIBRATION/BUFFET CR CRUISE 1 SO 25 317PX 1711094 688 P63088 LEFT ENGINE WON'T MAKE TARGET TORQUE. REMOVED AND REPLACED LEFT FUEL CONTROL UNIT IAW GARRETT MM. OPS CHECK GOOD. OK FOR SERVICE. (M) 2 L 7 2 4T 4 T RT A21EU E4WE 1996120500705 19961205 00705 1996 12 5 REXA96057 4 19961021 A 3413 66500012804 VSI INDICATOR SAAB SF340 340B 7860101 EU RT COCKPIT SHORTED A REXA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 25 365PX 4299 340B265 FIRST OFFICER'S VSI/TCAS INOP. REMOVED AND REPLACED VSI/TCAS IND IAW AMM. PERFORMED PITOT/STATIC LEAK CHECK IAW AMM. O PS CHECK AND LEAK CHECK GOOD. OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1996120500706 19961205 00706 EU 1996 12 5 REXA96056 1 19961020 A 7722 897469621888 WIRE HARNESS BAG JETSTM JETSTM3101 1500215 EU LT ENGINE BROKEN A REXA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 25 309PX 676 LEFT ENGINE EGT HAD EXTREME TEMP FLUCTUATIONS ON TAKEOFF ROLL. REMOVED AND REPLACED LEFT ENGINE EGT HARNESS BECAUSE OF DISLOCATED TERMINAL END RAN A/C OPS CHECK GOOD. (M) 2 L 7 2 4T RT A21EU 1996120500707 19961205 00707 EU 1996 12 5 REXA96055 1 19961020 A 7712 TQ INDICATION BAG JETSTM JETSTM3101 1500215 EU LT ENGINE FLUCTUATED A REXA O OTHER N FALSE WARNING TO TAKEOFF 1 SO 25 309PX 676 ON TAKEOFF, LT ENG HAD ERRATIC TQ AND EGT IND. TQ FLUCTUATED FROM 100 PERCENT TO 70 PERCENT WITH EGT FLUCTUATING FROM 6 40 TO 500 WITH CORRESPONDING LOSS OF ENGINE PERFORMANCE LAST APPROX 5 MINUTES, THEN STABILIZED BY ITSELF APPROX 3 MINUTE S LATER EGT FLUCTUATED FROM 600/200. INSPECTED EGT PIGTAIL, CANNON PLUGS, WIRES, COMP RESISTOR, AND FOUND NO DISCREPANC IES, GROUND RAN AND OPS CHECKED ALL SYSTEMS. NO DEFECTS NOTED. A/C OK FOR CONTINUED SERVICE. (M) 2 L 7 2 4T RT A21EU 1996120500708 19961205 00708 EU 1996 12 5 REXA96054 1 19961018 A 2910 GPP125012 HYD SWITCH SAAB SF340 SF340A 7850100 EU HYD BAY SHORTED A REXA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 25 341PX 9247722 340A142 DURING TAXI, HYDRAULIC MAIN ACCUMULATOR BLEEDS DOWN RAPIDILY, AS DOES OUTBOARD, INBOARD BRAKE ACCUMULATORS. FREED STICK Y CHECK VALVES ON HYDRAULIC MANIFOLD. LEAKAGE RATE TEST GOOD IAW 290000. REMOVED AND REPLACED HYDRAULIC PRESSURE SWITC H IAW AMM 29-10-45. (M) 2 L 7 2 4T RT A52EU 1996120500709 19961205 00709 EU 1996 12 5 REXA96053 1 19961018 A 7933 4053T73P01 TEMP BULB SAAB SF340 340B 7860101 EU LT PGB SHORTED A REXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 370PX LEW51924 340B300 LT PGB OIL TEMPERATURE ENTERED RED ARC. FERRIED TO MEMPHIS. REMOVED AND REPLACED TEMP BULB. (M) 2 L 7 2 4T RT A52EU 1996120500710 19961205 00710 EU 1996 12 5 REXA96052 1 19960809 A 7920 NAM1300112 SNAP RING BAG JETSTM JETSTM3101 1500215 EU LT ENGINE BROKEN A REXA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. A FLAME/FIRE TO TAKEOFF 1 SO 25 316PX 687 LEFT OIL LIGHT CAME ON DURING TAKEOFF ROLL. ENGINE FLAMED OUT, ABORTED DURING TAKEOFF. WHILE TAXIING IN, FIRE WAS SEEN BY PAX ON LEFT ENGINE. EVACUATED AIRCRAFT AND FIRED BOTH FIRE BOTTLES. FOUND OIL LEAK ON LEFT ENGINE, OIL COOLER THER MOSTAT POPPED OUT. INSTALLED NEW O-RING AND SNAP-RING. RAN A/C AND LEAK CHECKED GOOD. OK FOR CONTINUED SERVICE. (M) 2 L 7 2 4T RT A21EU 1996120500711 19961205 00711 EU 1996 12 5 REXA96048 1 19961018 A 5350 NOSE CONE SAAB SF340 SF340A 7850100 EU FORWARD FUSELAGE BIRD STRIKE A REXA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 25 347AM 340A039 ABORTED TAKEOFF DUE TO BIRD STRIKE, RETURNED TO GATE FOR INSPECTION. INSPECTED NOSE AND NOSE CONE, NO VISUAL DAMAGE NOT ED. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1996120500712 19961205 00712 NE 1996 12 5 REXA96034 2 19960726 A 7260 CHIP DET 004WS00 SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LT ENGINE SHORTED A REXA A UNSCHED LANDING N FALSE WARNING IN INSP/MAINT 1 SO 25 401BH 1078 340A057 LEFT CHIP LIGHT ON (ENGINE) AND BYTE LIGHT ILLUMINATED. VISUALLY INSPECTED LEFT ENGINE CHIP DETECTOR. NO CHIPS NOTED. REPLACED WEU. OPS CHECKED GOOD. AIRCRAFT OK FOR SVC. (M) 2 L 7 2 4T 4 T RT A52EU E8NE6 1996120500713 19961205 00713 NM 1996 12 5 EIAA9649 1 19961027 A 3211 65B012473 TRUNNION FORK BOEING 747 747SR46 NM LEFT MLG WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 478EV 21033 JFK - DURING LEFT WING LANDING GEAR JURY STRUT REPLACEMENT MAINTENANCE, (REF M20'S 002 AND 003), NOTED SOME END PLAY AT THE FORWARD TRUNNION FORK BEARING. REMOVED TRUNNION FORK AND BEARING AND INSTALLED REPLACEMENT FORK AND BEARING. PERFO RMED GEAR RETRACTION CHECK. REF 32-11-19/32-32-00. (M) 2 L 7 4 4F A20WE 1996120500714 19961205 00714 NE 1996 12 5 EIAA9648 2 19961024 A 7200 ENGINE BOEING 747 747273C 1384896 NM PWA JT9 JT9D7J 52054 NE NR 3 MALFUNCTIONED A A EIAA O OTHER J WARNING INDICATION TO TAKEOFF 1 NM 09 471EV 20651 686107 SBEG - DURING TAKEOFF ROLL NR 3 ENIGNE POWER ROLLED BACK FROM 1.42 EPR TO 1.31 EPR. FOLLOWED BY AN EGT DECREASE FROM 85 0 TO 813 AND N-1 DECREASED FROM 95 PERCENT TO 88 PERCENT. AFTER ADVANCING THRUST LEVER APPROX 1.5 KNOB WIDTHS, ENGINE R ECOVERED. NO DEFECTS DETERMINED AT THIS TIME. FURTHER INVESTIGATION IS UNDERWAY. THREE ENGINE FERREID TO JFK FOR MAIN TENANCE. (M) 2 L 7 4 4F 4 F A20WE E20EA 1996120500715 19961205 00715 EU 1996 12 5 USAAF96114 1 19961103 A 5610 D20543405 WINDSHIELD FOKKER F28 F28MK0100 4990807 EU LT COCKPIT CRACKED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 866US 11310 FLT 511 - PIT-GSO - AFTER TAKEOFF, AT APPROXIMATELY 6500 FEET, A BIRD HIT THE CAPTAINS WINDSHIELD AND IT CRACKED. THE F LIGHT RETURNED TO PIT WITHOUT INCIDENT. NO EMEGENCY DECLARED. MAINTENANCE REPLACED THE WINDSHIELD. (M) 2 L 7 2 4F RT 1996120500716 19961205 00716 NM 1996 12 5 USAA960721 1 19961030 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 947-967 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 261AU 35361 22867 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOND 2 INCH BY 12 INCH CORRODED AREA BS 947 TO 967 STRINGER 25R. REMOVED CORR ODED STRINGER RADIUS FILLER AND SPLICED IN NEWE RADIUS FILLER (ACTUAL STRINGER NOT AFFECTED BY CORROSION) LESS THAN ONE POUND ADDED. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996120500717 19961205 00717 NM 1996 12 5 USAA960716 1 19961030 A 5230 ANGLE BOEING 737 737201 1384454 NM CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 261AU 35316 22867 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK FORWARD CARGO DOOR AT LOWER AFT CORNER STOP FITTING, SKIN TO WEB ATTACH ANGLE. FABRICATED AND INSTALLED REPAIR ANGLES, REPAIRED PER SRM 51-40-4. (M) 2 L 7 2 4F A16WE 1996120500718 19961205 00718 NM 1996 12 5 USAA960717 1 19961030 A 5312 BULKHEAD SKIN BOEING 737 737201 1384454 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 261AU 35316 22867 INT - DURING Q-4 CHECK VISUAL INSPECTION FOUND 1.5 INCH CRACK 178 BULKHEAD SKIN RBBL 5 INCH WL 202. STOP DRILLED CRACK AND INSTALLED DOUBLER, REPAIRED PER T/R 53-10-11. (M) 2 L 7 2 4F A16WE 1996120500719 19961205 00719 NM 1996 12 5 USAA960718 1 19961030 A 5312 BULKHEAD SKIN BOEING 737 737201 1384454 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 261AU 35316 22867 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK BS 178 BULKHEAD SKIN RBBL 5 INCH WL 199. STOP DRILLED CR ACK AND INSTALLED DOUBLER, REPAIRED PER T/R 53-10-11. (M) 2 L 7 2 4F A16WE 1996120500720 19961205 00720 NM 1996 12 5 USAA960719 1 19961030 A 5312 BULKHEAD SKIN BOEING 737 737201 1384454 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 261AU 35316 22867 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1. 5INCH CRACK BS 178 BULKHEAD SKIN LBBL 5 INCH WL 202. STOP DRILLED CR ACK AND INSTALLED DOUBLER, REPAIRED PER T/R 53-10-11. (M) 2 L 7 2 4F A16WE 1996120500721 19961205 00721 NM 1996 12 5 USAA960720 1 19961030 A 5315 FLOOR BEAM BOEING 737 737201 1384454 NM BS 328 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 261AU 35316 22867 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 100 INCH CORROSION BS 328 LBBL 50 INCH THROUGH RBBL 50 INCH FL OOR BEAM T-CAP. FABRICATED NEW T-CAP AND SPLICE, REPAIRED PER TR 53-10-13. CORROSION TASK NR C53-107-02, CORROSION LEV EL 2. (M) 2 L 7 2 4F A16WE 1996120500722 19961205 00722 NM 1996 12 5 USAA960693 1 19961026 A 5330 SKIN BOEING 737 737201 1384454 NM BS 797 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 240AU 41392 22355 ROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 6 INCH CORROSION STRINGER 26R BS 797 FUSELAGE SKIN. REMOVED CORROSION AND INSTALLED DOUBLER. REPAIRED PER SRM 53-30-3 FIG 6. CORROSION TASK NR C53-100-01, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1996120500723 19961205 00723 NM 1996 12 5 USAABB96040 1 19961015 A 2130 S210U1222 OVERPRESSURE SW BOEING 767 767201 1385125 NM RT PYLON FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 647US 23899 PHL - FLT 894 - FLIGHT RETURNED TO FIELD TO PHL DUE TO THE EICAS MESSAGE 'R ENG PRV', THE RIGHT ENGINE 'BLEED' LIGHT ILL UMINATING, AND THE RIGHT DUCT PRESSURE INDICATING ZERO. FLIGHT LANDING WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE PRV, PRV CONTROLLER, A BLEED CARD AND THE OVERPRESSURE SWITCH (S735). THE SWITCH FIXED THE PROBLEM. (M) 2 L 7 2 4F RT A1NM 1996120500724 19961205 00724 NE 1996 12 5 USAAD96158 2 19961101 A 7200 ENGINE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9A 52048 NE LEFT FAILED A USAA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 EA 19 967VJ 38126 47375 674479 FLT 451 - DCA-YUL - DURING CRUISE AT FL 330, LEFT ENGINE EPR DECREASED TO 1.2, N1 AND N2 DROPPED TO APPROXIMATELY 40 PER CENT, HEARD THREE LOUD BANGS. TURNED ON LEFT FUEL PUMP AND ANTI-ICE SWITCH, LEFT ENGINE RETURNED TO NORMAL. DIVERTED T O BOS AS PRECAUTIONARY. REPLACED ENGINE. (M) 2 L 7 2 4F 4 F A6WE E2EA 1996120500725 19961205 00725 NM 1996 12 5 USAASB96222 1 19961105 A 3230 RETRACT MECH BOEING 737 737301 1384611 NM LANDING GEAR MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 354US 23557 PVD - FL 2026 - GEAR LEVER WOULD NOT MOVE TO RAISE POSITION. CREW DID NOT TRY OVERRIDE. FLIGHT RETURNED TO PVD AND LAN DED WIHT NO FURTHER INCIDENT. MAINTENANCE COULD NOT DUPLICATE THE PROBLEM. SYSTEM OPERATED NORMALLY. BELIEVE PROBLEM TO BE A POPPED CIRCUIT BREAKER. (M) 2 L 7 2 4F RT A16WE 1996120500726 19961205 00726 NM 1996 12 5 USAASB96223 1 19961107 A 3260 1061226211 CIRCUIT CARDS BOEING 737 7373B7 1384580 NM LANDING GEAR FAILED A USAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 EA 19 383US 22956 IND - FL 2284 - UPON GEAR EXTENSION, RED NOSE GEAR UNSAFE LIGHT ILLUMINATED. CREW PERFORMED GO AROUND AND CYCLED THE GE AR FOUR TIMES, RESULTING IN THERE GREEN LIGHTS. FLIGHT LANDED AT IND. MAINTENANCE AT IND REPLACED TWO CARDS, M1214 AND M983. (M) 2 L 7 2 4F RT A16WE 1996120500727 19961205 00727 NM 1996 12 5 96ZZZM1545 1 19961107 A 3260 655825029 CIRCUIT CARDS BOEING 737 7373B7 1384580 NM LANDING GEAR FAILED A USAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 EA 19 383US 22956 IND - FL 2284 - UPON GEAR EXTENSION, RED NOSE GEAR UNSAFE LIGHT ILLUMINATED. CREW PERFORMED GO AROUND AND CYCLED THE GE AR FOUR TIMES, RESULTING IN THREE GREEN LIGHTS. FLIGHT LANDED AT IND. MAINTENANCE AT IND REPLACED TWO CARDS, M1214 AND M983. (M) 2 L 7 2 4F RT A16WE 1996120500728 19961205 00728 NM 1996 12 5 TWRA96343 1 19961021 A 7800 65B979041 EXHAUST SLEEVE BOEING 747 747212B 1384886 NM NR 4 ENGINE SEPARATED A A TWRA A E UNSCHED LANDING ENGINE SHUTDOWN O OTHER CL CLIMB 1 EA 15 619FF 34 21316 DURNIG CLIMB NR 4 ENGINE COMPRESSOR STALLED AND SPOOLED DOWN, EGT WNE TO 980 DEGREES CELSIUS. AFTER STALL INFLIGHT ENGI NE FAILURE/SHUTDOWN CHECKLIST PERFORMED. MAINTENANCE FOUND PT-2 LINE CHAFED TO PRBC. REPLACED LINE, OPS CHECKED NORMA L ON RUN UP PER 72-00-00 AND 75-32-00. ALSO, FOUND EXHAUST SLEEVE SEPARTATED. REMOVED AND REPLACED EXHAUST SLEEVE PER WI 78-364, OPS CHECKED NORMAL ON RUN UP PER MM 72-00-00. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 4 4F A20WE 1996120500729 19961205 00729 NE 1996 12 5 TWRA96322 2 19960928 A 7200 ENGINE BOEING 747 747130 1384880 NM PWA JT9 JT9D7A 52054 NE NR 1 FAILED A A TWRA E ENGINE SHUTDOWN J M WARNING INDICATION OVER TEMP CL CLIMB 1 EA 15 603FF 61032 19746 662818 DURING CLIMB FLIGHT LEVEL 220, AIRCRAFT SHOOK AND LOUD BANG NR 1 ENGINE EGT WENT TO 905 DEGREES CELSIUS. THRUST LEVER R ETARDED AND ENGINE SHUTDOWN PER INFLIGHT FAILURE. ACCOMPLISHED CONDITION INSPECTION PER MM 5-51-39, PHASE ONE PARAGRAPH S A AND B NR DEFECTS NOTED. REMOVED ENGINE S/N 662818 AND INSTALLED ENGINE S/N 685870 IAW MM 71-00-02 AND 71-00-07 AND WIC 71-002, RUN UP AND LEAK CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 4 4F 4 F A20WE E20EA 1996120500730 19961205 00730 NE 1996 12 5 TWRA96328 2 19961007 A 7200 ENGINE BOEING 747 747282B 1384860 NM PWA JT9 JT9D7A 52054 NE NR 4 FAILED A A TWRA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 EA 15 611FF 68139 20502 662574 AFTER T/O 30 MINS IN FLT, WHILE CLIMBING THRU FL 350, LOST PWR ON NR 4 ENG. EGT DROPPED TO 480 DEG CELSIUS, N1 AND N2 A PPROX 75 PERCENT, FUEL FLOW 300. NORMAL OIL PRESS WITH POSITIVE FUEL PRESS. ACCOMP UNSCHEDULED THRUST LOSS OR ABNORMAL RESPONSE TO THRUST LEVER ADVANCEMENT 3-21-9. ENG WAS SHUT DOWN AS PER PROCEDURE. ALL WINDMILLING PARAMETERS NORMAL. N ORMAL RELITE AND ALL PARAMETERS AND ENG OPS FOR REMAINDER OF FLT NORMAL. PERFORMED FP12 CHECK, PRESS OK AT 700 PSI BORO SCOPED ENG, REPLACED TT2 SENSOR PER 73-11-05. OPS NORM. R/R FUEL PUMP PER TC 73-154. R/R FUEL CONTL PER TC 73-251. RU N UP AND LEAK CHECK NORMAL PER MM 72-00-00. A/C RETURN TO SERVICE. (M) 2 L 7 4 4F 4 F A20WE E20EA 1996120500731 19961205 00731 NM 1996 12 5 TWRA96346 1 19961022 A 3350 900835A BATTERY PACK BOEING 747 747212B 1384886 NM CABIN DISCHARGED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 619FF 14933 21316 DURING DAILY CHECK, FOUND EXIT SIGN ABOVE SEAT 19H AND 2R MED COMES ON FOR A SECOND THEN SHUTS OFF. FOUND BATTERY DOES NOT HOLD CHARGE. REMOVED AND REPLACED BATTERY PACK AS PER MM 33-51-30. OPERATIONAL CHECK NORMAL. (M) 2 L 7 4 4F A20WE 1996120500732 19961205 00732 NM 1996 12 5 TWRA96341 1 19961018 A 3350 362624 LIGHT BOEING 747 747282B 1384860 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 611FF 20502 DURING DAILY CHECK, FOUND LIGHT STRIP AT SEAT 7A NOT ILLUMINATING. REPLACED STRIP AT SEAT 7A. OPS CHECKED NORMAL PER M M 33-59-00. (M) 2 L 7 4 4F A20WE 1996120500733 19961205 00733 NE 1996 12 5 TWRA96344 2 19961023 A 7314 38690113 FUEL PUMP BOEING 747 747212B 1384886 NM PWA JT9 JT9D7Q 52054 NE NR 2 ENG MALFUNCTION A A TWRA A E UNSCHED LANDING ENGINE SHUTDOWN E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CR CRUISE 1 EA 15 616FF 96108 21939 702083 DURING CRUISE, AT FL 390, NR 2 ENGINE EMITTED A LOW BOOMING NOISE FOLLOWED BY A RUMBLE AND VIBRATION. DECREASE IN EPR, N1, N2, EGT TO 300 DEGREES CELSIUS AND FUEL FLOW ZERO. ACCOMPLISHED ENGINE SHUT DOWN PER CHECKLIST. ATTEMPTED TWO REST ARTS, BOTH UNSUCCESSFUL. OIL PRESSURE REMAINED AT 13 PSI. REMOVED AND REPLACED FUEL PUMP AND FUEL CONTROL UNIT AS PER MM 73-11-001 PAGE 401 AND MM 73-21-01 PAGE 401. OPS CHECKED NORMAL. (M) 2 L 7 4 4F 4 F A20WE E3NE 1996120500734 19961205 00734 NE 1996 12 5 96ZZZM1546 2 19961023 A 7321 780001 FUEL CONTL BOEING 747 747212B 1384886 NM PWA JT9 JT9D7Q 52054 NE NR 2 ENG MALFUNCTION A A TWRA A E UNSCHED LANDING ENGINE SHUTDOWN E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CR CRUISE 1 EA 15 616FF 96108 21939 702083 DURING CRUISE, AT FL 390, NR 2 ENGINE EMITTED A LOW BOOMING NOISE FOLLOWED BY A RUMBLE AND VIBRATION. DECREASE IN EPR, N1, N2, EGT TO 300 DEGREES CELSIUS AND FUEL FLOW ZERO. ACCOMPLISHED ENGINE SHUT DOWN PER CHECKLIST. ATTEMPTED TWO REST ARTS, BOTH UNSUCCESSFUL. OIL PRESSURE REMAINED AT 13 PSI. REMOVED AND REPLACED FUEL PUMP AND FUEL CONTROL UNIT AS PER MM 73-11-001 PAGE 401 AND MM 73-21-01 PAGE 401. OPS CHECKED NORMAL. (M) 2 L 7 4 4F 4 F A20WE E3NE 1996120500735 19961205 00735 NM 1996 12 5 TWRA96342 1 19961020 A 3350 S1356A36 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 620FF 5926 21162 DURING DAILY CHECK, FOUND NR 1 LEFT CEILING EMERGENCY LIGHT INOP. REPLACED CEILING LIGHT ASSEMBLY AT NR 1 LEFT. OPS CH ECKED NORMAL PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996120500736 19961205 00736 NM 1996 12 5 TWRA96348 1 19961026 A 3350 S1356B37 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 25202 21937 DURING DAILY CHECK, FOUND 5L MED EVAC LIGHT INOP. REPLACED CEILING EVAC LIGHT. OPS CHECKED NORMAL PER MM 33-51-00. (M ) 2 L 7 4 4F A20WE 1996120500737 19961205 00737 1996 12 5 VTZA97049 4 19961104 A 3445 TCWS JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT ACTIVATED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 323UE 41059 FLT 6323 - IAD- RDU - ABORTED TAKEOFF DUE TO TCWS. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INS PECTED, RESET AND TESTED SYSTEM, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996120500738 19961205 00738 CE 1996 12 5 96ZZZM1547 1 19960912 A 5610 114504315 WINDSHIELD PPG 10138402518 BEECH 1900 1900D 1154162 CE RT COCKPIT CRACKED A MASA K NONE O OTHER NR NOT REPORTED 1 SW 01 125YV 96206H3213 UE125 CO-PILOT WINDSHIELD CRACKED IN SEVERAL PLACES. DURING FLIGHT, WEATHER PLUS 12 DEGREES CELSIUS AT 4,000 FEET. 2 L 7 2 4T RT A24CE 1996120500739 19961205 00739 NM 1996 12 5 HNAA9692872 1 19961030 A 3350 POWER SUPPLIES DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 928HA 120 FLT 3108 - GSO-BWI - DURING PREFLIGHT CHECKS, FOUND THE FORWARD CEILING EMERGENCY DOWN LIGHT INOP. SWAPPED PS1 AND PS2 POWER SUPPLIES. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 1996120500740 19961205 00740 NM 1996 12 5 HNAA9698973 1 19961030 A 2120 AIR DISTR DHAV DHC8 DHC8201 2809001 NM COCKPIT SMOKING A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 07 989HA 427 FLT 3448 - TPA-TLH - CREW REPORTS SMOKE IN COCKPIT IN CRUISE WHEN REDUCING POWER TO 20 PERCENT. WHEN BLEEDS ARE TURNED OFF, NO SMOKE IS VISIBLE. THE AIRCRAFT CONTINUED ON TO TLH AND LANDED WITHOUT INCIDENT. CHECKED OIL LEVEL, OIL LEVELS GOOD. OIL PRESSURES ON BOTH ENGINES WERE FOUND NORMAL. VISUALLY INSPECTED AIR SWITCHING VALVES ON BOTH ENGINES, VALVES CHECKED GOOD. COULD NOT DUPLICATE. (M) 2 H 7 2 4T RT A13NM 1996120500741 19961205 00741 WP 1996 12 5 ORJA9665 1 19960904 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1115-1120 CORRODED A L ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 840RA 49424 VARIOUS CORROSION SPOTS FOUND ON SEAT TRACKS IN AFT CABIN AREA. REFERENCE ATTACHED NON-ROUTINE CARDS 20000069/70. REMO VED WORN AND CORRODED SEAT TRACKS AND REPLACED WITH NEW SEAT TRACKS, INSTALLED IAW DC9 SRM 53-05 PG 105. (M) 2 L 7 2 4F A6WE 1996120500742 19961205 00742 WP 1996 12 5 96ZZZM1548 1 19960904 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1287-1309 CORRODED A L ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 840RA 49424 VARIOUS CORROSION SPOTS FOUND ON SEAT TRACKS IN AFT CABIN AREA. REFERENCE ATTACHED NON-ROUTINE CARDS 20000069/70. REMO VED WORN AND CORRODED SEAT TRACKS AND REPLACED WITH NEW SEAT TRACKS, INSTALLED IAW DC9 SRM 53-05 PG 105. (M) 2 L 7 2 4F A6WE 1996120500743 19961205 00743 WP 1996 12 5 ORJA9664 1 19960908 A 5310 STRUCTURE DOUG DC9 DC982 3022082 WP AFT CARGO PIT CORRODED A L ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 840RA 49424 VARIOUS CORROSION SPOTS FOUND ON STRUCTURE AND TIE DOWN TRACKS IN AFT CARGO PIT. REFERENENCE NON-ROUTINE CARDS 10000116 /128/131/132/133/134. REWORKED CORRO DED STRUCTURE, REMOVED AND REPLACED WORN AND CORRODED TIE DOWN TRACKS IAW DC9 SRM 51-30-1. (M) 2 L 7 2 4F A6WE 1996120500744 19961205 00744 WP 1996 12 5 96ZZZM1549 1 19960908 A 5347 TIE DOWN TRACK DOUG DC9 DC982 3022082 WP AFT CARGO PIT CORRODED A L ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 840RA 49424 VARIOUS CORROSION SPOTS FOUND ON STRUCTURE AND TIE DOWN TRACKS IN AFT CARGO PIT. SEE ATTACHED NON-ROUTINE CARDS 1000011 6/128/131/132/133/134. REWORKED CORRODED STRUCTURE, REMOVED AND REPLACED WORN AND CORRODED TIE DOWN TRACKS IAW DC9 SRM 51-30-1. (M) 2 L 7 2 4F A6WE 1996120500745 19961205 00745 WP 1996 12 5 ORJA9666 1 19960906 A 5310 STRUCTURES DOUG DC9 DC982 3022082 WP MID CARGO COMPT CORRODED A L ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 840RA 49424 VARIOUS CORROSION SPOTS FOUND ON STRUCTURE AND TIE DOWN TRACKS IN MID CARGO PIT. REFERENCE NON-ROUTINE FORMS 10000081/8 5/88/89/96. REWORKED CORRODED STRUCTURE, REMOVED AND REPLACED WORN AND CORRODED TIE DOWN TRACKS IAW DC9 SRM 51-30-1. ( M) 2 L 7 2 4F A6WE 1996120500746 19961205 00746 WP 1996 12 5 96ZZZM1550 1 19960906 A 5347 TIE DOWN TRACKS DOUG DC9 DC982 3022082 WP MID CARGO COMPT CORRODED A L ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 840RA 49424 VARIOUS CORROSION SPOTS FOUND ON STRUCTURE AND TIE DOWN TRACKS IN MID CARGO PIT. REFERENCE NON-ROUTINE FORMS 10000081/8 5/88/89/96. REWORKED CORRODED STRUCTURE, REMOVED AND REPLACED WORN AND CORRODED TIE DOWN TRACKS IAW DC9 SRM 51-30-1. ( M) 2 L 7 2 4F A6WE 1996120500747 19961205 00747 CE 1996 12 5 GLBA96203 1 19961016 A 3230 44EN496 SQUAT SWITCH BEECH 1900 1900C 1154161 CE RT MLG FAILED A GLBA O OTHER J WARNING INDICATION CL CLIMB 1 CE 01 96UE UC96 MDW - GEAR WOULD NOT RETRACT. MAINTENANCE REMOVED AND REPLACED RIGHT SQUAT SWITCH, CYCLED GEAR, CHECKED GOOD. (M) 2 L 7 2 4T RT A24CE 1996120500748 19961205 00748 SO 1996 12 5 GLBA96202 1 19961013 A 3230 PROX SWITCH EMB 120 EMB120ER 3260203 SO MLG FAILED A GLBA O OTHER J WARNING INDICATION CL CLIMB 1 CE 01 293UX 120293 DEN - LANDING GEAR WOULD NOT RETRACT. MAINTENANCE REPLACED MAIN LANDING GEAR PROX SWITCH. (M) 2 L 7 2 4T RT A31SO 1996120500749 19961205 00749 EU 1996 12 5 RAIA961041 1 19961030 A 7712 3036927 TQ SIG COND AEROSP ATR42 ATR42300 8680920 EU RT ENGINE MALFUNCTIONED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 421TE 9355 102 STL - FLT 7136 - FDAU TORQUE BUGS FLUCTUATED ON RIGHT ENGINE. ONLY AN INDICATION PROBLEM. MAINTENANCE REPLACED THE RIG HT TORQUE SIGNAL CONDITIONER. (M) 2 H 7 2 4T RT A53EU 1996120500750 19961205 00750 EU 1996 12 5 RAIA961042 1 19961031 A 7722 8974696 CONNECTOR BAG JETSTM JETSTM3201 1500217 EU LT ENGINE LOOSE A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 435AM 8883 889 STL - FLT 7496 - LEFT EGT ERRATIC, SRL ON AND OFF. MAINTENANCE REPLACED THE LEFT EGT SHORTLEAD, P/N 8974696. (M) 2 L 7 2 4T RT A56EU 1996120500751 19961205 00751 EU 1996 12 5 RAIA961023 1 19961021 A 5270 SP4954 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGG DOOR OUT OF ADJUST A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 03 556HK 2452 41073 JFK - FLT 7724 - BAGGAGE DOOR CAPTION ILLUMINATED DURING TAKEOFF. ADJUSTED MICROSWITCH. (M) 2 L 7 2 4T RT A41NM 1996120500752 19961205 00752 EU 1996 12 5 RAIA961101 1 19961101 A 5240 14153133217 DOOR JETAIR JETSTM JETSTM4101 1500501 EU LAV SERVICE MISSING A RAIA K NONE D INFLIGHT SEPARATION IN INSP/MAINT 1 CE 03 553HK 3151 41066 JFK - FLT 660 - ON POST FLIGHT FOUND THE LAVATORY SERVICE DOOR MISSING. MAINTENANCE REPLACED THE LAVATORY SERVICE DOOR. (M) 2 L 7 2 4T RT A41NM 1996120500753 19961205 00753 EU 1996 12 5 RAIA961103 1 19961104 A 7600 GCL3P CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU WING/FUSE LOOSE A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 03 563HK 1693 41079 JFK - FLT 7753 - NR 1 IEC FAULTED ON TAKEOFF. SECURED PIN 55 IN WING TO FUSELAGE CANNON PLUG. (M) 2 L 7 2 4T RT A41NM 1996120500754 19961205 00754 WP 1996 12 5 RAIA961104 2 19961104 A 7320 8975481 X-SCREW BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT ENGINE OUT OF ADJUST A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 343TE 8453 955 66158 BMI - FLT 7325 - LEFT ENGINE RPM 98.8 PERCENT. ADJUSTED SCREW X (PROP GOV HIGH). (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996120500755 19961205 00755 WP 1996 12 5 RAIA961108 2 19961107 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP NR 2 FAILED A RAIA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 CE 03 862AE 10351 862 66146 SBA - FLT 4743 - IN FLT NR 2 ENGINE FUEL PRESSURE DROPPED AND ENGINE SHUT DOWN. REMOVED AND REPLACED ENGINE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996120500756 19961205 00756 EU 1996 12 5 RAIA961109 1 19961108 A 3350 167006 BULB AEROSP ATR72 ATR72202 8680940 EU CABIN FAILED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 721TE 217 STL - FORWARD BULB IN EMERGENCY ESCAPE PATH LIGHTING INOP. MAINTENANCE REPLACED THE FORWARD LIGHT BULB. (M) 2 H 7 2 4T RT A53EU 1996120500757 19961205 00757 EU 1996 12 5 RAIA961114 1 19961113 A 3060 66000218 BRUSH BLOCK BAG JETSTM JETSTM3201 1500217 EU RT PROP FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 03 430AM 12093 880 STL - FLT 7330 - DURING TAKEOFF, RIGHT PROP DE-ICE FAILED. MAINTENANCE REPLACED THE RIGHT PROP DE-ICE BRUSH BLOCK. (M) 2 L 7 2 4T RT A56EU 1996120500758 19961205 00758 EU 1996 12 5 PLGA9611091 1 19961109 A 3020 FAIL LIGHT SAAB SF340 340B 7860101 EU RT INTAKE HEAT ILLUMINATED A PLGA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NE 05 365BE 340B299 LGA - FLT 4494 - EN ROUTE TO BOS FROM ISP, THE RIGHT INTAKE HEAT FAIL LIGHT ILLUNMINATED. THE AIRCRAFT RETURNED TO ISP, LANDING WITHOUT INCIDENT. MAINTENANCE CYCLED THE WHEEL WELL CIRCUIT BREAKERS, OPERATIONALLY TESTED THE SYSTEM AND RETU RNED THE AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1996120500759 19961205 00759 EU 1996 12 5 PLGA9611011 1 19961101 A 3020 CONNECTORS SAAB SF340 SF340A 7850100 EU LT INTAKE HEAT DIRTY A PLGA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NE 05 346BE 340A150 LGA - FLT 4300 - EN ROUTE TO DCA FROM BOS, THE LEFT INTAKE HEAT FAIL LIGHT ILLUMINATED. THE AIRCRAFT DIVERTED TO LGA LA NDING WITHOUT INCIDENT. LGA MAINTENANCE INSPECTED THE AIRCRAFT, FINDING OIL IN SEVERAL OF THE LOWER DUCT CONNECTORS. M AINTENANCE CLEANED THE CONNECTORS AND REPLACED THE LOAD MONITOR FOR PRECAUTIONARY REASONS. THE SYSTEM OPERATIONAL CHECK ED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1996120500760 19961205 00760 EU 1996 12 5 PLGA9610312 1 19961031 A 3260 D49412001 CONTL BOX SAAB SF340 SF340A 7850100 EU E/E COMPT MALFUNCTIONED A PLGA O OTHER N FALSE WARNING AP APPROACH 1 NE 05 741BA 3150690 340A090 PVD - FLT 4782 - DURING APPROACH WHEN THE GEAR WAS SELECTED DOWN THE N/G AND LT MAIN GEAR GREEN DOWN AND LOCKED IND DID NOT ILLUMINATE. THE CREW CYCLED THE GEAR ONCE AND THE N/G LIGHT DID ILLUMINATE BUT LT MAIN LIGHT STILL DID NOT ILLUMINA TE. THE GEAR WAS PUMPED DOWN BUT THE LT MAIN LIGHT FAILED ILLUMINATE. CREW VERIFIED WITH FLAPS DOWN THAT THERE WAS NO CONFIG WARNING. A REPOSITIONING CAPTAIN CHECKED THE MAIN GEAR FROM THE CABIN AND THEY APPEARED DOWN AND LOCKED. THE A/ C LANDED W/O INCIDENT. MX INSPECT THE WIRING AND DOWN LOCK SWITCHES. MX CLEANED AND LUBED THE DOWN LOCK SWITCHES. L/G CONTL BOX WAS ALSO R/R. MX PERFORMED AN OPS CHECK OF THE SYS AND NO FAULT WAS FOUND. A/C RELEASED TO SERV. (M) 2 L 7 2 4T RT A52EU 1996120500761 19961205 00761 CE 1996 12 5 96ZZZM1551 1 19961005 A 3220 998201109 PIN BEECH 1900 1900D 1154162 CE NLG BACKED OUT A A MASA K NONE O OTHER TX TAXI/GRND HDL 1 SW 01 4ZV 7837 UE4 961005 NOSE GEAR COLLAPSED ON TAXI. CLEAR VFR DAY. NOSE DRAG LEG UPPER PIN BACKED OUT. ISSUED FLEET CAMPAIGN DIRECTIVE TO IN SPECT ENTIRE FLEET FOR UPPER DRAG LEG PIN INSTALLATION. (M) 2 L 7 2 4T RT A24CE 1996120500762 19961205 00762 WP 1996 12 5 GTIA96NK218 1 19961114 A 3350 BULBS DOUG DC9 DC931 3022065 WP CABIN CORRODED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 934ML 47526 NUMEROUS CABIN EMERGENCY LIGHTS INOP. CLEANED SOCKETS AND REMOVED AND REPLACED CORRODED BULBS. (M) 2 L 7 2 4F A6WE 1996120500764 19961205 00764 WP 1996 12 5 IXXA96164 1 19961112 A 3310 16435 LIGHT BALLAST DOUG DC8 DC863F 302198F WP COCKPIT OVERHEATED A IXXA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 11 870BX 46036 EN ROUTE IND TO LRD, AN ELECTRICAL BURNING SMELL WAS PRESENT IN THE COCKPIT. THE CREW REPORTED THE SMELL DISIPATED WHEN THE WHITE COCKPIT LIGHTING WAS TURNED OFF. MAINTENANCE DEFERRED THE COCKPIT WHITE LIGHTING, ATTRIBUTING THE SMELL TO T HE CONTROL BALLAST. (M) 2 L 7 4 4F 4A25 1996120500765 19961205 00765 WP 1996 12 5 IXXA96163 1 19961110 A 2110 543C51 COMPRESSOR CLAMP DOUG DC8 DC863 302198A WP NR 2 ENGINE LOOSE A IXXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 11 868BX 46034 EN ROUTE TOL TO LAX, PRESSURIZATION WAS LOST AND THE AIRCRAFT DIVERTED TO DEN. MAINTENANCE FOUND AND SECURED A TURBO CO MPRESSOR OUTLET DUCT CLAMP. PRIOR TO RELEASE FOR FLIGHT, THE CREW OXYGEN WAS SERVICED AND AN OVERWEIGHT LANDING INSPECT ION WAS ACCOMPLISHED. (M) 2 L 7 4 4F 4A25 1996120500766 19961205 00766 NE 1996 12 5 IXXA96162 2 19961107 A 7200 9026M70G01 ENGINE DOUG DC8 DC871 302199A WP GE CFM56 CFM562C1 13802 NE NR 3 FAILED A IXXA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SW 11 829BX 24771 45994 EN ROUTE TOL TO DEN, THE NR 3 ENGINE WAS SHUT DOWN DUE TO FLUCTUATING FUEL FLOW AND SUBSEQUENT FLUCTUATING N1. MAINTENA NCE INSPECTED THE ENGINE AND FOUND THE N1 AND N2 SPOOLS DRAGGING TOGETHER. THE ENGINE WAS REMOVED AND REPLACED. PRELIM INARY INDICATIONS ARE A FAILURE OF THE NR 4 BEARING. (M) 2 L 7 4 4F 4 F 4A25 E2GL 1996120500767 19961205 00767 NE 1996 12 5 IXXA96161 2 19961018 A 7320 MEC SENSE LINE DOUG DC8 DC871 302199A WP GE CFM56 CFM562C1 13802 NE NR 4 ENGINE OBSTRUCTED A IXXA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 SW 11 822BX 23556 45813 693341 EN ROUTE OAK TO TOL AT FL 37, SAT MINUS 48, FUEL QTY OF RESPECTIVE TANK 8000 LBS, NR 4 ENGINE FLAMED OUT. CREW ACCOMPLI SHED SUCCESSFUL RESTART IAW COMPANY PROCEDURES. FLIGHT CONTINUED WITH NO FURTHER EVENTS. MAINTENANCE TROUBLESHOT THE E VENT IAW CFMI MM FAULT 57. MAINTENANCE FOUND AND CLEANED AND OBSTRUCTION FROM THE CDP AND CBP LINES, REPLACED THE ENGIN E FUEL FILTER, AND OPERATIONALLY CHECKED THE ENGINE PRIOR TO RETURNING THE AIRCRAFT TO SERVICE. (M) 2 L 7 4 4F 4 F 4A25 E2GL 1996120500768 19961205 00768 WP 1996 12 5 IXXA96160 1 19961009 A 3230 510361 TELESCOPING LINK DOUG DC8 DC863 302198A WP NLG LACK OF LUBE A IXXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 11 869BX 46035 AFTER DEPARTURE FROM ELP AND SUBSEQUENT GEAR RETRACTION, VIBRATION AND AIR NOISE WERE NOTED IN THE NOSE AREA OF THE AIRC RAFT. THE FLIGHT CREW VISUALLY CONFIRMED THE NOSE LANDING GEAR RETRACTION. THE CREW THEN RECYCLED THE GEAR AND THE NOI SE CONTINUED. THE AIRCRAFT RETURNED TO ELP. MAINTENANCE CLEANED AND LUBED THE RIGHT NOSE GEAR TELESCOPING LINK AND RET URNED THE AIRCRAFT TO SERVICE. (M) 2 L 7 4 4F 4A25 1996120500769 19961205 00769 WP 1996 12 5 GTIA96NK217 1 19961105 A 5720 99194022 TRAPEZOIDAL PNL DOUG DC9 DC932 3022066 WP RIGHT CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 941ML 47131 DURING INSPECTION OF LEFT AND RIGHT TRAPEZOIDAL PANEL PER SERVICE BULLETIN 53-182 RIGHT TRAP PANEL CRACKED EXTENDING FRO M LEADING EDGE OF PANEL TO SECOND FASTENER. EDDY CURRENT BOLT HOLE INSPECTION CONFIRMS CRACK IS ONLY FROM FIRST HOLE TO FRONT EDGE OF PANEL LENGTH 1 INCH ROUTED OUT CRACK PER S/B 53-100. (M) 2 L 7 2 4F A6WE 1996120500770 19961205 00770 WP 1996 12 5 GTIA96NK216 1 19961105 A 5720 99194021 TRAPEZOIDAL PNL DOUG DC9 DC932 3022066 WP LEFT CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 941ML 47131 DURING INSPECTION OF LEFT AND RIGHT TRAPEZOIDAL PANEL PER S/B 53-182. LEFT TRAP PANEL CRACKED EXTENDED BEYOND EXISTING APPROVED SRM 57-09 FIGURE 6 SHEET 4 REPAIR IT RUNS PAST 4 FASTENER. DAC NOTIFIED ROUTED OUT CRACKED AREA .090 PAST AFT EDGE OF 4TH HOLE. EDDY CURRENT AND ULTRASOUND CONFIRM CRACK COMPLETELY REMOVED. LEFT TRAP PANEL PLACED ON WATCH WITH 4 00 HOUR VISUAL INSPECTION AND REPLACE AT C-CHECK BUT NOT TO EXCEED 1500 HRS. (M) 2 L 7 2 4F A6WE 1996120500771 19961205 00771 WP 1996 12 5 HALA960053 1 19960903 A 5720 WEB DOUG DC10 DC1010 3022110 WP CEN WING BOX CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 153AA 68464 46708 DURING CHECK, FOUND CRACK ON WEB 46 RIGHT INBOARD OF ACCESS DOOR 142AZ ON THE INBOARD SIDE OF WEB APPROX 18 INCHES AFT T HE FORWARD BULKHEAD. INSTALLED DOUBLER PER SRM 51-00-01. (M) 2 L 7 3 4F A22WE 1996120500772 19961205 00772 WP 1996 12 5 HALA960052 1 19960903 A 5320 5585682 ROLLER TRACK DOUG DC10 DC1010 3022110 WP BS 845 CORROSION A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 153AA 46708 FOUND CORROSION ON TOP SIDE OF INBOARD RIGHT ROLLER TRACK, STATION 824 TO STATION 859. REMOVED AND REPLACED RIGHT ROLLE R TRACK STARTING AT AT STATION 824 PER SRM 51-01-00-05. (M) 2 L 7 3 4F A22WE 1996120500773 19961205 00773 WP 1996 12 5 HAL960051 1 19960903 A 5720 ARB1263 DOUBLER DOUG DC10 DC1010 3022110 WP WS 264 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 153AA 68464 46708 DURING CHECK, FOUND THE LOWER LEFT LEADING EDGE SACRIFICIAL DOUBLER CORRODED WHERE THE INBOARD LATCH FOR ACCESS PANEL 51 7AB CONTACTS IT. INSTALLED DOUBLER AFTER CORROSION REMOVAL PER SRM 57-10-00, FIGURE 19. (M) 2 L 7 3 4F A22WE 1996120500774 19961205 00774 WP 1996 12 5 HAL960046 1 19960903 A 5320 5635778 FITTING DOUG DC10 DC1010 3022110 WP BS 795 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 153AA 68464 46708 DURING CHECK, FOUND STRINGER 52 TERMINAL FITTING CORRODED BETWEEN STATION 795 AND 798 AS MARKED. REMOVED AND REPLACED S TRINGER TERMINAL FITTING AT STATION 795 PER SRM 51-01-00-05. (M) 2 L 7 3 4F A22WE 1996120500775 19961205 00775 WP 1996 12 5 HAL960044 1 19960903 A 5320 ANGLE DOUG DC10 DC1010 3022110 WP BS 1841 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 153AA 68464 46708 DURING CHECK, FOUND CORROSION ON SURFACE OF BELT FRAME AT STATION 1841. CORROSION WAS ON THE LOWER 'J' ANGLE LIP. REMO VED AND REPLACED THE LOWER 'I' ANGLE WITH SPLICE, ALODINED AND PAINTED AREA PER 53-30-00 PG 31, FIG 8 OF THE SRM. (M) 2 L 7 3 4F A22WE 1996120500776 19961205 00776 WP 1996 12 5 HAL960045 1 19960903 A 5320 ANGLE DOUG DC10 DC1010 3022110 WP BS 979 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 153AA 68464 46708 DURING CHECK, FOUND CORROSION ON THE BELT FRAME ANGLE STATION 979, AFT SIDE, FROM STRINGER 51 RIGHT TO STRINGER 51 LEFT. CUT OUT CORRODED ANGLE AND INSTALLED NEW CHANNEL. REPAIR PER SRM 53-30-00. (M) 2 L 7 3 4F A22WE 1996120500777 19961205 00777 WP 1996 12 5 HAL960076 1 19961002 A 5320 FRAME STRAP DOUG DC10 DC1010 3022110 WP R2 DOOR CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 148AA 72741 46703 CORROSION ON THE UPPER EAR OF THE FUSELAGE FRAME STRAP ABOVE R2 DOOR. REMOVED CORROSION AND INSTALLED A STRAP OVER THE AREA PER ESO 7349 DATED 10-1-96. (M) 2 L 7 3 4F A22WE 1996120500778 19961205 00778 WP 1996 12 5 HAL960078 1 19961001 A 5311 ADA01449 FRAME DOUG DC10 DC1010 3022110 WP BS 979 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 148AA 72741 46703 WEB AT FRAME 979 HAS CORROSION BETWEEN LAYERS OF FRAME 6 INCHES ABOVE THE BELLY AND CRACKED 2 PLACES AT STRINGER 50L. I NSTALLED REPLACEMENT WEB AT STATION 979 LEFT SIDE PER ESO 7349 DATED 9-27-96 AND SRM VOL NR 51-21-01 AND SRM VOL NR 51-3 1-01. (M) 2 L 7 3 4F A22WE 1996120500779 19961205 00779 WP 1996 12 5 HALA960084 1 19961005 A 5720 ARC0311 FALSE SPAR DOUG DC10 DC1010 3022110 WP LT WING TE CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 148AA 72741 46703 CORROSION ON AFT SIDE OF FALSE SPAR JUST OUTBOARD OF NR 1 SPOILER ACT. REMOVED AND REPLACED 8 FOOT SECTION OF FALSE SPA R PER AARD 51-01-00-05 AND ESO 7349 DATED 10-4-96. (M) 2 L 7 3 4F A22WE 1996120500780 19961205 00780 WP 1996 12 5 HAL960083 1 19961004 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 1059-1079 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 148AA 72741 46703 CORROSION ON STRINGER 52 BETWEEN STATION 1059 AND 1079. SPLICED NEW SECTION AT LONGERON FROM STATION 1072-1079 AS PER A ARD 51-10-00-05. (M) 2 L 7 3 4F A22WE 1996120500781 19961205 00781 WP 1996 12 5 HAL960082 1 19961004 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 1039-1059 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 148AA 72741 46703 FOUND STRINGER 52 BETWEEN STATION 1039-1059 HAS SURFACE CORROSION. SPLICED NEW SECTION AT LONGERON FROM STATION 1053-10 59 AS PER AARD 51-01-00-05 AND SRM 51-21-01. (M) 2 L 7 3 4F A22WE 1996120500782 19961205 00782 WP 1996 12 5 HAL960081 1 19961004 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1480-1531 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 148AA 72741 46703 CORROSION ON SKIN, BELLY BETWEEN LANDING GEAR. FABRICATED AND INSTALLED DOUBLER FROM LONGERON 50R TO 50L AND FROM STATI ON 1461 TO 1531 IAW ESO 7349 DATED 9-23-96. (M) 2 L 7 3 4F A22WE 1996120500783 19961205 00783 WP 1996 12 5 HAL960080 1 19961004 A 5320 DOOR JAMB DOUG DC10 DC1010 3022110 WP BS 1305 CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 148AA 74741 46703 CRACK IN AFT DOOR JAMB WEB AT NR 8 ACCESS HOLE. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM VOL 1 53-50-00 PAGE 69 . (M) 2 L 7 3 4F A22WE 1996120500784 19961205 00784 WP 1996 12 5 HAL960079 1 19961008 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1661 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 148AA 72741 46703 LOWER FUSELAGE SKIN BULGED AND CRACKED FROM CORROSION AT STATION 1661 BETWEEN LONGERON 43L AND 44L. REMOVED CORROSION S RM 51-21-01. INSTALLED DOUBLERS PER SRM 53-20-00 VOL 1. (M) 2 L 7 3 4F A22WE 1996120500785 19961205 00785 WP 1996 12 5 HAL960087 1 19961007 A 5720 ARC0292 FALSE SPAR CAP DOUG DC10 DC1010 3022110 WP WS 320-224 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 148AA 46703 DURING C-CHECK, FOUND CORROSION ON LEFT WING FUSELAGE SPAR UPPER CAP AT STATION XW=320 TO XW=224. REMOVED AND REPLACED EIGHT FOOT SECTION OF FALSE SPAR PER AARD 51-01-00-05, 51-35-01 VOL 2 AND ESO 7349 DATED 10-4-96. (M) 2 L 7 3 4F A22WE 1996120500786 19961205 00786 WP 1996 12 5 HAL960061 1 19960919 A 5320 SHEAR TIE DOUG DC10 DC1010 3022110 WP BS 899 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 148AA 72741 46703 SHEAR TIE HEAVY CORROSION AT STATION 899 BETWEEN STRINGER 52L AND 51L. INSTALLED NEW SHEAR TIE SECTION BETWEEN STRINGER 52L AND 51L PER SRM VOL 1 53-30-00 AND 53-30-00-10. (M) 2 L 7 3 4F A22WE 1996120500787 19961205 00787 WP 1996 12 5 HAL960066 1 19960930 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 759 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 148AA 72741 46703 CORROSION ON FLOOR BOARD SUPPORT FORWARD CARGO COMPARTMENT INBOARD NR 1 ROLLER TRAY. REPLACED FLOOR BOARD SUPPORT PER S RM 51-10-00. (M) 2 L 7 3 4F A22WE 1996120500788 19961205 00788 WP 1996 12 5 HAL960065 1 19960930 A 5320 SHEAR TIE DOUG DC10 DC1010 3022110 WP BS 1964 BROKEN A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 148AA 72741 46703 SHEAR TIE CORRODED, BROKEN OFF BETWEEN STRINGER 52 AND 51R. INSTALLED SHEAR TIE CLIP REPAIR PER SRM 53-30-00, FIG 10. ( M) 2 L 7 3 4F A22WE 1996120500789 19961205 00789 WP 1996 12 5 HAL960064 1 19960926 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 550 CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 148AA 72741 46703 CRACK IN LONGERON NR 33 RIGHT AT STATION 550. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-10-00 PAGE 1-5. (M) 2 L 7 3 4F A22WE 1996120500790 19961205 00790 WP 1996 12 5 HAL960063 1 19960924 A 5313 STRINGER DOUG DC10 DC1010 3022110 WP BS 999-1019 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 148AA 72741 46703 HEAVY CORROSION ON STRINGER 52 FROM STATION 999 TO STATION 1019. SPLICED IN NEW SECTION OF STRINGER FROM STATION 989 TO 1101 PER SRM 51-10-00. (M) 2 L 7 3 4F A22WE 1996120500791 19961205 00791 WP 1996 12 5 HAL960094 1 19961101 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 1139-1156 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 116AA 75042 46516 LONGERON 52 FROM STATION 1139 TO 1156 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED LONGERON PER SRM 51-01-00-05. (M ) 2 L 7 3 4F A22WE 1996120500792 19961205 00792 WP 1996 12 5 HAL960096 1 19961031 A 5313 STRINGER DOUG DC10 DC1010 3022110 WP BS 560 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 116AA 75042 46516 STRINGER 48L CORRODED AT LOWER FLANGE FAST HOLES. CLEANED CORROSION AND ADDED STRAP TO 48L PER SRM 51-00-01 PAGE 10, SR M 51-01-00-03 PAGE 1 FIG 1A (SHEET 1) FIG 80 SHEET 1, FIG 1 SHEET 6. (M) 2 L 7 3 4F A22WE 1996120500793 19961205 00793 WP 1996 12 5 HAL960090 1 19961021 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1621 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 116AA 46516 LEFT FLOOR SUPPORT FRAME HAS CORROSION AT STATION 1621 UNDER NR 1 ROLLER TRACK. INSTALLED DOUBLER AT STATION 1621 ON LE FT END OF FLOOR SUPPORT FRAME UNDER ROLLER TRACK REF SRM 53-30-00. (M) 2 L 7 3 4F A22WE 1996120500794 19961205 00794 WP 1996 12 5 HAL960091 1 19961022 A 5347 S4929405 SEAT TRACK DOUG DC10 DC1010 3022110 WP BS 439-469 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 116AA 75042 46516 DEEP CORROSION 3.5 INCHES ALONG INBOARD SIDE OF NR 4 SEAT TRACK LOCATED BETWEEN STATION 439 AND STATION 469, A ZONE CABI N FLOOR. REMOVED AND REPLACED NR 4 SEAT TRACK AT LOCATION BETWEEN STATION 439 AND 469 AARD 51-01-00-05. (M) 2 L 7 3 4F A22WE 1996120500795 19961205 00795 WP 1996 12 5 HAL960100 1 19961105 A 5320 LAV PAN DOUG DC10 DC1010 3022110 WP BS 795 CORROSION A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 116AA 75042 46516 MID LAVATORY FLOOR PAN HAS CORROSION ON FORWARD SIDE. REMOVED AND REPLACED PAN IAW ESO 7349. (M) 2 L 7 3 4F A22WE 1996120500796 19961205 00796 WP 1996 12 5 HAL960075 1 19961001 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 1099 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 148AA 72741 46703 HEAVY CORROSION ON STRINGER R43 STATION 1099 TO STATION 1119. CUT OUT DAMAGE, INSTALLED STRINGER REPAIR PER AARD 51-10- 00-1 SRM 53-10-00. (M) 2 L 7 3 4F A22WE 1996120500797 19961205 00797 WP 1996 12 5 HAL960074 1 19961001 A 5320 INTERCOSTAL DOUG DC10 DC1010 3022110 WP BS 1099 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 148AA 72741 46703 FOUND CORROSION ON INTERCOSTAL AT L 43R STATION 1099 TO STATION 1119. INSTALLED NEW INTERCOSTAL PER AARD 51-10-00-1. ( M) 2 L 7 3 4F A22WE 1996120500798 19961205 00798 WP 1996 12 5 HAL960069 1 19960930 A 5320 ROLLER TRAY DOUG DC10 DC1010 3022110 WP BS 859-879 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 148AA 72741 72741 46703 NR 4 ROLLER TRAY HAS HEAVY CORROSION BOTTOM SIDE AT STATION 859 TO 879. REPLACED ROLLER TRAY FROM STATION 879 TO 795 PE R SRM 51-01-00-05. (M) 2 L 7 3 4F A22WE 1996120500799 19961205 00799 WP 1996 12 5 HAL960068 1 19960930 A 5320 ROLLER TRAY DOUG DC10 DC1010 3022110 WP BS 815-825 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 148AA 72741 46703 SURFACE CORROSION ON OUTBOARD LIP OF NR 4 RIGHT ROLLER TRAY BETWEEN FRAME STATION 815 AND 825. REPLACED ROLLER TRAY FRO M STATION 879 TO 795 PER SRM 51-01-00-05. (M) 2 L 7 3 4F A22WE 1996120500800 19961205 00800 EU 1996 12 5 USAAF96116 1 19961110 A 2730 234387 BYPASS SWITCH FOKKER F28 F28MK0100 4990807 EU ELEVATOR CONTL FAILED A USAA A UNSCHED LANDING C J F.O.D. WARNING INDICATION CL CLIMB 1 EA 19 865US 11308 FLT 2341 - PIT-RSW - UPON CLIMB-OUT AT 7500 FEET, AIRCRAFT ENCOUNTERED LIGHTNING AND HEARD LOUD THUNDER IN AIRCRAFT. CA PTAIN HAD A DOUBLE FAULT ON ELEVATOR. RETURNED TO PIT WITH MANUAL REVERSION LANDED WITHOUT FURTHER INCIDENT. MAINTENAN CE PERFORMED LIGHTNING STRIKE INSPECTION. REPAIRED LEFT HORIZONTAL STABILIZER TIP FAIRING PER EA. ALSO, REPLACED BOTH ELEVATOR BOOST BYPASS SWITCHES DUE TO FAILURE. (M) 2 L 7 2 4F RT 1996120500801 19961205 00801 EU 1996 12 5 USAAF96115 1 19961105 A 3350 MGG175008 BULB FOKKER F28 F28MK0100 4990807 EU CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 882US 11334 EMERGENCY EXIT LIGHT AT 12A IS OUT OF SERVICE. MAINTENANCE RELAMPED EXIT LIGHT. (M) 2 L 7 2 4F RT 1996120500802 19961205 00802 NM 1996 12 5 USAA960715 1 19961030 A 5312 BULKHEAD SKIN BOEING 737 737201 1384454 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 261AU 35316 22867 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK BS 178 BULKHEAD SKIN LBBL 5 INCH WL 199. STOP DRILLED C RACK AND INSTALLED DOUBLER, REPAIRED PER T/R 53-10-11. (M) 2 L 7 2 4F A16WE 1996120500803 19961205 00803 NM 1996 12 5 USAASB96224 1 19961108 A 3350 FUSE BOEING 737 737401 1384701 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 405US 23885 ROC - LAST TWO ROWS OF FLOOR LEVEL LIGHTING AND AFT RIGHT SLIDE LIGHT INOPERATIVE. MAINTENANCE REPLACED A BAD FUSE IN T HE POWER SUPPLY. (M) 2 L 7 2 4F RT A16WE 1996120500804 19961205 00804 NM 1996 12 5 USAABB96044 1 19961102 A 4990 380029815 APU BOEING 757 7572B7 1384964 NM APU BAY OIL LEAK A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 617AU 16486 27148 CLT - FL 433 - EN ROUTE PHL-TPA, CREW NOTED LIGHT OIL MIST AND SMELL IN CABIN AND COCKPIT. FLIGHT DIVERTED TO CLT AND L ANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE APU AND RAN BOTH PACKS AT FULL HOT TO CLEAR THE SYSTEM. (M) 2 L 7 2 4F RT A2NM 1996120500805 19961205 00805 NM 1996 12 5 USAABB96042 1 19961031 A 2421 S281T00138 IDG BOEING 757 7572B7 1384964 NM RT ENGINE FAILED A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 617AU 11916 27148 MSP - FLT 114 - EN ROUTE SEA-PIT, CREW RECEIVED E/M 'R GEN DRIVE' AND DRIVE LIGHT. CREW DISCONNECTED THE IDG AND STARTE D THE APU. APPROXIMATELY ONE AND ONE-HALF HOURS LATER, THE CREW RECEIVED THE E/M 'APU OIL QTY' AND THE OIL QTY READ 'AD D'. APPROXIMATELY TWENTY MINUTES LATER, THE APU PERFORMED AND AUTO SHUTDOWN DUE TO LOW OIL PRESSURE. FLIGHT DIVERTED T O MSP AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE RIGHT IDG DPI EXTENDED AND PROGRAMMED IT FOR REPLACEME NT. THE APU WAS SERVICED WITH OIL, APU STARTED, AND THE AIRCRAFT RELEASED FOR FLIGHT. (M) 2 L 7 2 4F RT A2NM 1996120500806 19961205 00806 NM 1996 12 5 USAABB96045 1 19961105 A 3350 8731002511 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 612AU 27124 LAX - FOUND THREE EMERGENCY EXIT IDENTIFIERS INOPERATIVE AT DOORS R1, R2, AND R4. MAINTENANCE REPLACED THE IDENTIFIERS. (M) 2 L 7 2 4F RT A2NM 1996120500807 19961205 00807 NM 1996 12 5 USAABB96043 1 19961101 A 4990 32895141 OIL SHUTOFF VLV BOEING 757 7572B7 1384964 NM APU LEAKING A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 617AU 16476 27148 MCI - FLT 29 - EN ROUTE BWI-LAX WITH THE LEFT IDG ON MEL, CREW RECEIVED APU LOW QUANTITY INDICATIONS. APU PERFORMED AUT O SHUT DOWN NEAR DSM. FLIGHT DIVERTED TO MCI AND LANDED WITH NO FURTHER INCIDENT. THE APU WAS SERVICED AND THE AIRCRAF T RELEASED FOR A MAINTENANCE FERRY FLIGHT TO PHL. EN ROUTE, THE SAME PROBLEM REOCCURRED AND THE FLIGHT DIVERTED TO PIT. MAINTENANCE IN PIT REPLACED THE APU GEARBOX OIL SHUTOFF VALVE. (M) 2 L 7 2 4F RT A2NM 1996120500808 19961205 00808 SO 1996 12 5 WTAA960190 1 19961110 A 7712 30005000026 TQ SIG COND EMB 120 EMB120RT SO LT ENGINE FAILED A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 WP 17 284UE 120145 MRY - LEFT ENGINE BEGINS TO AUTO FEATHER WITH POWER LEVER ADVANCED. TAKEOFF ABORTED. AIRCRAFT RELEASED FOR ONE TIME FE RRY FLIGHT TO FAT. MAINTENANCE REMOVED AND REPLACED LEFT TORQUE SIGNAL CONDITIONER. OPERATIONAL CHECK SATISFACTORY. A IRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996120500809 19961205 00809 1996 12 5 WTAA960182 3 19961027 A 6140 8659566 BETA SWITCH BAG JETSTM JETSTM3101 1500215 EU RT ENGINE FAILED A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 17 418UE 780 LAX - RIGHT BETA LIGHT ILLUMINATED ON TAKEOFF. TAKEOFF ABORTED WITHOUT INCIDENT. REPLACED RIGHT BETA SWITCH. OPERATIO NAL AND LEAK CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996120500810 19961205 00810 EU 1996 12 5 WTAA960187 1 19961101 A 2424 51539002A GEN CONTL UNIT BAG JETSTM JETSTM3101 1500215 EU RIGHT FAILED A WTAA C ABORTED TAKEOFF H ELECT. POWER LOSS-50 PC TO TAKEOFF 1 WP 17 403UE 743 SMF - RIGHT GENERATOR CONTROL UNIT FAILED DURING TAKEOFF. TAKEOFF ABORTED. AIRCRAFT FERRIED TO SFO. MAINTENANCE REPLA CED RIGHT GENERATOR CONTROL UNIT. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996120500811 19961205 00811 EU 1996 12 5 WTAA960184 1 19961101 A 7714 AG34 TACH GENERATOR BAG JETSTM JETSTM3101 1500215 EU LT ENGINE FAILED A WTAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 17 417UE 794 IPL - LEFT ENGINE RPM INDICATION FAILED ON TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. FERRIED AIRCRAFT TO LAX. MAINTENANCE REPLACED LEFT TACHOMETER GENERATOR. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4T RT A21EU 1996120500812 19961205 00812 EU 1996 12 5 WTAA960186 1 19961103 A 5330 SKIN BAG JETSTM JETSTM3101 1500215 EU FUSELAGE BIRDSTRIKE A WTAA K NONE C F.O.D. AP APPROACH 1 WP 17 403UE 743 STS - REPORTED BIRD STRIKE TO POD DURING APPROACH. MAINTENANCE INSPECTED AIRCRAFT FOR DAMAGE, NO DAMAGE NOTED. AIRCRAF T RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996120500813 19961205 00813 EU 1996 12 5 WTAA960183 1 19961028 A 5610 WINDSHIELD BAG JETSTM JETSTM3101 1500215 EU COCKPIT BIRDSTRIKE A WTAA K NONE C F.O.D. CR CRUISE 1 WP 17 107XV 723 LAX - BIRD STRIKE REPORTED TO CENTER WINDSCREEN. MAINTENANCE INSPECTED AIRCRAFT AND CLEANED CENTER WINDSCREEN. NO DAMA GE NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996120500814 19961205 00814 SO 1996 12 5 WTAA960189 1 19961106 A 5246 PE2506820202 CAMLOCK EMB 120 EMB120RT SO RT FUEL DOOR FAILED A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 17 284UE 120145 FAT - DOOR WARNING LIGHT ILLUMINATED PRIOR TO TAKEOFF. TAKEOFF ABORTED. MAINTENANCE REPLACED FUELING DOOR CAMLOCK. OP ERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996120500815 19961205 00815 SO 1996 12 5 WTAA960188 1 19961104 A 3260 85106R106P50 CONNECTOR EMB 120 EMB120RT SO RT MLG BROKEN WIRE A WTAA O OTHER J WARNING INDICATION CL CLIMB 1 WP 17 275UE 120058 FAT - LANDING GEAR FAILED TO RETRACT ON TAKEOFF, GEAR LEVER LOCKED IN DOWN POSITION. AIRCRAFT RETURNED TO FAT. MAINTEN ANCE REPAIRED BROKEN WIRE ON RIGHT GEAR PROXIMITY SENSOR WIRE HARNESS CANNON PLUG. LANDING GEAR FUNCTIONAL CHECK NORMAL . AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996120500816 19961205 00816 NE 1996 12 5 WTAA960185 2 19961102 A 7260 310098601 DRIVE GEAR EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE FAILED A A WTAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 WP 17 122AM 120013 115135 MRY - EN ROUTE SFO TO SBA RIGHT ENGINE POWER LOSS REPORTED. CREW SECURED RIGHT ENGINE. DIVERTED TO MRY, LANDING WITHOU T INCIDENT. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE DUE TO INTERNAL FUEL PUMP DRIVE GEAR FAILURE. AIRCRAFT RETUR NED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1996120500817 19961205 00817 NM 1996 12 5 WRLA96048 1 19961106 A 7110 COWL DOUG MD11 MD11 3023602 NM NR 3 ENGINE DAMAGED A A WRLA O OTHER O OTHER LD LANDING 1 EA 27 271WA 48518 DURING LANDING AT SAEZ A/C WAS UNABLE TO STOP ON THE RUNWAY. A/C CONTINUED OFF THE RUNWAY SURFACE AND STOPPED APPROXIMA TELY 450 FT PAST THE END OF RUNWAY. NO INJURIES WERE SUSTAINED. GRD PERSONNEL WERE UNABLE TO POSITION MOBILE STAIRWAYS TO AIRCRAFT, HEAVY MUD AROUND AIRCRAFT. TO DEPLANE PASSENGERS, MX REP ABOARD A/C DEPLOYED THE L2 SLIDE RAFT AND PASSEN GERS WERE DEPLANED VIA SLIDE. MX INSPECTED A/C FOR DAMAGE, AND FOUND DAMAGE TO THE NR 3 ENG NOSE COWL, AND NR 3 ENG ING ESTED FOREIGN OBJECTS SUSTAINING DAMAGE TO COMPRESSOR AREA. INSPECT OF A/C NOTED NO STRUCTURAL DAMAGE OTHER THAN NOSE C OWL. (M) 2 L 7 3 4F RT A22WE 1996120500818 19961205 00818 1996 12 5 WRLA96049 4 19961106 A 3417 ADC DOUG MD11 MD11 3023602 NM E/E COMPT MALFUNCTIONED A A WRLA L ABORTED APPROACH G MULTIPLE FAILURE AP APPROACH 1 EA 27 271WA 48518 DURING APPROACH AT SAEZ, FLT CREW ENCOUNTERED MULTIPLE FAULTS (ENGINES NR 1, 2, AND 3 SELECT FADEC ALTERNATE LEVEL 2, SE LECT ELEVATOR FEEL MAN, SELECT FLAP LIMIT OVERRIDE, WINDSHEAR DETECTION FAIL). A/C WAS ENCOUNTERING HEAVY TURBULENCE WI TH HEAVY PRECIPITATION. A/C WAS EXPERIENCING AERODYNAMIC VIBRATION AS FLAPS WERE DEPLOYED TO 35 DEGREES. FLT CREW INIT IATED A 'MISSED APPROACH'. FLT CREW INITIATED A SECOND APPROACH TO AIRPORT. NOTED FAULTS AND VIB CONTINUED DURING SECO ND APPROACH. A/C LANDED, BUT WAS UNABLE TO STOP, A/C STOPPED 450 FT OFF THE END OF THE RUNWAY. NO INJURIES NOTED. (M ) 2 L 7 3 4F RT A22WE 1996120500819 19961205 00819 NE 1996 12 5 WRLA96047 2 19961111 A 7230 54A831 FAN BLADE DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE NR 1 ENG BIRD STRIKE A A WRLA A UNSCHED LANDING E C VIBRATION/BUFFET F.O.D. TO TAKEOFF 1 EA 27 274WA 48633 DURING TAKEOFF, FLT CREW NOTICED FLOCK OF BIRDS IN AREA OF FLIGHT PATH, SHORTLY AFTER CREW NOTICED NR 1 ENGINE HAVING EX CESIVE VIBRATION. BIRD INGESTED INTO NR 1 ENGINE. FLIGHT CREW ELECTED TO RETURN TO POINT OF DEPARTURE FOR REPAIRS. AI RCRAFT LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED NR 1 ENGINE AND FOUND 1 FAN BLADE BENT AND CUT 6 INCHES FROM END O F BLADE. BIRD TRAVELED THROUGH BYPASS/SECONDARY STAGE OF ENGINE. FAN BLADE WAS REPLACED PER MM 72-31-02, BOROSCOPE INS PECTION IAW MM 72-00-00. NO DEFECTS NOTED. ENG RUN UP TEST ACCOMP, ALL IND NORMAL. A/C RETURNED TO SERVICE. (M) 2 L 7 3 4F 4 F RT A22WE E24NE 1996120500820 19961205 00820 1996 12 5 96ZZZM1552 4 19961101 A 2565 3HT3000 CYLINDER 415670014 CVAC 340 34031 2422704 WP SERV DOOR LOW PRESSURE A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 07 73153 131 179 DURING SCHEDULED CHECK, THE EVACUATION SLIDE CYLINDER PRESSURE WAS FOUND BELOW LIMITS. THE EVACUATION SLIDE/CYLINDER AS SEMBLY WAS REPLACED. 2 L 7 2 4R 6A6 1996120500821 19961205 00821 WP 1996 12 5 96ZZZM1553 1 19961009 A 5330 SKIN CVAC 440 440 2422902 WP FUSELAGE CRACKED A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 07 73166 374 DURING ACCOMPLISHMENT OF SID ITEM 53-2-1 AND .5 INCH LONG CRACK WAS FOUND IN THE FUSELAGE SKIN FROM RIVET TOWARDS CENTER OF LEFT NR 3 EMERGENCY EXIT OPENING, LOWER AFT CORNER. A PATCH WAS FABRICATED AND INSTALLED AS PER VIEW 'A' OF CV 640( 340D) SB NR 53-1. 2 L 7 2 4R 6A6 1996120500822 19961205 00822 WP 1996 12 5 VTZA97052 2 19961105 A 7321 31059005 FUEL CONTL UNIT JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE3311 01514 WP RT ENGINE FAILURE A A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 321UE 41045 FLT 6516 - RIC-EWR - ABORTED TAKEOFF DUE TO RIGHT RPM 85 PERCENT, RIGHT RED BETA LIGHT ILLUMINATED. AIRCRAFT RETURNED T O GATE WITH NO FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED FUEL CONTROL UNIT, OPS CHECK OK. AIRCRAFT WAS RELEAS ED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 3 T RT A41NM E3WE 1996120500823 19961205 00823 EU 1996 12 5 VTZA97051 1 19961106 A 5270 DOOR WARNING JETAIR JETSTM JETSTM4101 1500501 EU BAGG COMPT ACTIVATED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 324UE 41017 FLT 6186 - LYH-IAD - ABORTED TAKEOFF DUE TO MAIN BAGGAGE DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MX OPENED DMI 57952, MEL 52-3. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996120500824 19961205 00824 NM 1996 12 5 TWRA96352 1 19961103 A 3350 LIGHT BOEING 747 747212B 1384886 NM CABIN MISSING A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND SEAT 51H EVAC LIGHT MISSING. REPLACED SOCKET, BULB AND LENS ASSEMBLY. SYSTEM OPS CHECKED NOR MAL AS PER MM 33-51-00 PAGE 501. (M) 2 L 7 4 4F A20WE 1996120500825 19961205 00825 NM 1996 12 5 TWRA96351 1 19961103 A 3350 362622 LIGHT BOEING 747 747136 1384883 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 606FF 20273 DURING DAILY CHECK, FOUND EVAC STRIP, UPPER DECK RIGHT SIDE AFT PART ARE OUT. REPLACED EVAC STRIP. OPS CHECKED NORMAL PER 33-51-00. (M) 2 L 7 4 4F A20WE 1996120500826 19961205 00826 NM 1996 12 5 TWRA96347 1 19961028 A 5400 6883314 HIGH LOCK BOLTS BOEING 747 747212B 1384886 NM NR 4 PYLON SHEARD OFF A TWRA K NONE O OTHER IN INSP/MAINT 1 EA 15 620FF 21162 DURING 'B' SERVICE AT JFK, MX FOUND FOUR HIGH LOCKS BOLT HEADS SHEARED OFF AT NR 4 PYLON UPPER CLEVIS AFT INBOARD SIDE. REMOVED FASTENER. PERFORMED HIGH FREQ EDDY CURRENT INSPECTION AND BOROSCOPED HOLE. FOUND NO CORROSION OR CRACKS. PRI MED FASTENER HOLE AND INSTALLED NEW FASTENER PER SRM 51-30-02. EA 54-073 AND SB 54-2118. A/C RETURN TO SERVICE. (M) 2 L 7 4 4F A20WE 1996120500827 19961205 00827 NM 1996 12 5 TWRA96353 1 19961031 A 3350 S1356B37 LIGHT BOEING 747 747282B 1384860 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 611FF 11051 20502 DURING DAILY CHECK, FOUND RIGHT SIDE AISLE CEILING EMERGENCY LIGHT INOP, ADJACENT TO SEAT 64 HJK. REMOVED AND REPLACED LIGHT ASSEMBLY AS PER MM 33-51-00. OPS CHECKED NORMAL. (M) 2 L 7 4 4F A20WE 1996120500828 19961205 00828 EU 1996 12 5 SIMA963191 1 19961114 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 135MQ 135 ORD - FLT 4055 - FLOOR PATH EMERGENCY LIGHTING INOP. RAI'D BATTERY PACKS AT 29WL (S/N 3522) AND 3WL (S/N 4032). SYSTEM OPS CHECKS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996120500829 19961205 00829 EU 1996 12 5 SIMA963169 1 19961111 A 3350 330151 POWER PACK SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 375AE 1101 340B375 DFW - FLT 3559 - MIDDLE CABIN LEFT SIGN BETWEEN ROW 7 AND 8 INOP. RAI'D POWER PACK 23LM FOR ROW 7 AND 8 AND PERFORMED O PERATIONAL CHECK. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1996120500830 19961205 00830 EU 1996 12 5 SIMA963168 1 19961111 A 5347 453776000 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 971NA 017 MQT - MAINTENANCE PERFORMING AN IMBV INSPECTION, FOUND CORROSION ON THE LEFT FORWARD OUTBOARD SEAT TRACK. MAINTENANCE R EMOVED AND REPLACED SEAT TRACK IAW EO 4-53-077. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996120500831 19961205 00831 EU 1996 12 5 SIMA963167 1 19961111 A 5347 453776000 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 971NA 017 MQT - MAINTENANCE PERFORMING AN IMBV INSPECTION, FOUND CORROSION ON THE RIGHT FORWARD OUTBOARD SEAT TRACK. MAINTENANCE REMOVED ADN REPLACED SEAT TRACK IAW EO 4-53-077. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996120500832 19961205 00832 EU 1996 12 5 SIMA963166 1 19961111 A 5347 45307712000 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 971NA 017 MQT - MAINTENANCE PERFORMING AN IMBV INSPECTION, FOUND CORROSION ON LEFT AFT SEAT TRACK OF FRAME 39. MAINTENANCE REMOVE D AND REPLACED SEAT TRACK IAW EO E95300-002. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996120500833 19961205 00833 EU 1996 12 5 SIMA963165 1 19961111 A 5315 S5367240521201 FLOOR BEAM AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 971NA 017 MQT - MAINTENANCE PERFORMING AN IMBV INSPECTION, FOUND CORROSION ON FLOOR BEAM 36. MAINTENANCE REMOVED REPLACED FLOOR B EAM IAW EO E9-5300-004. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996120500834 19961205 00834 EU 1996 12 5 SIMA963164 1 19961111 A 5320 S53671257229 GUSSET AEROSP ATR42 ATR42300 8680920 EU RT MLG WW CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 971NA 017 MQT - MAINTENANCE PERFORMING AN IMBV INSPECTION, FOUND A CRACK IN THE RIGHT WHEEL WELL GUSSET AT FRAME 25, STRINGER 14. MAINTENANCE REPAIRED GUSSET WITH A STAINSTEEL DOUBLER IAW EO E1-5300-190. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996120500835 19961205 00835 EU 1996 12 5 SIMA963163 1 19961111 A 5320 DOUBLER AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 971NA 017 MAINTENANCE PERFORMING AN IMBV INSPECTION, FOUND CORROSION AROUND 5 HI-LOKS ON A DOUBLER LOCATED AT FRAME 25 BETWEEN STR INGER 14 AND 15 ON RIGHT SIDE OF AIRCRAFT. MAINTENANCE REMOVED CORROSION BY SPOT FACING BLENDING AND APPLYING ALODINE I AW EO E1-5300-195. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996120500836 19961205 00836 EU 1996 12 5 SIMA963162 1 19961111 A 5320 13S53371213200 WINDOW FRAME AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 971NA 017 MQT - MAINTENANCE PERFORMING AN IMBV INSPECTION, FOUND CORROSION BEYOND LIMITS ON THE WINDOWS FRAME RIGHT SIDE NR 3 THRU 18, AND LEFT SIDE NR 2 THRU 12, AND 14 THRU 17. MAINTENANCE REMOVED AND REPLACED ABOVE NUMBERED WINDOWS IAW SRM 51-25- 04. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996120500837 19961205 00837 EU 1996 12 5 SIMA963161 1 19961111 A 5330 SKIN AEROSP ATR42 ATR42300 8680920 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 971NA 017 MQT - MAINTENANCE PERFORMING AN IMBV, FOUND A DENT RIGHT SIDE OF AIRCRAFT BETWEEN FRAME FRAME 41 AND 42. MAINTENANCE RE PAIRED DENT WITH SKIN PATCH IAW EO E1-5300-178. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996120500838 19961205 00838 EU 1996 12 5 SIMA963141 1 19961109 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 213AT 4207 211 ORD - FLT 4087 - SEVERAL FLOOR EMERGENCY LIGHTS INOP. RAI'D POWER PACK AT LOCATION 29WL. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996120500839 19961205 00839 EU 1996 12 5 REXA96066 1 19961029 A 7722 6058T27P01 ITT HARNESS SAAB SF340 SF340A 7850100 EU RT ENGINE SHORTED A REXA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 25 327PX CJWS0699 340A059 ABORTED TAKEOFF WITH A ITT INDICATION RIGHT OF 944 DEGREES CELSIUS, 108 PERCENT TORQUE BLEEDS OFF, ANTI-ICE ON. GROUND RAN AIRCRAFT. FOUND ITT FLUCTUATING. REMOVED AND REPLACED RIGHT YELLOW HARNESS. GROUND RAN AIRCRAFT AGAIN. NO DEFECT S NOTED. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1996120500840 19961205 00840 EU 1996 12 5 REXA96064 1 19961027 A 7931 IPTE1191000200D1 TRANSDUCER SAAB SF340 SF340A 7850100 EU RT ENGINE FAILED A REXA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SO 25 406BH 55471448 340A074 PERFORMED A PRECAUTIONARY SHUTDOWN ON RIGHT ENGINE, OIL PRESSURE AND GAUGE. REMOVED AND REPLACED RIGHT PGB OIL TRANSDUC ER IAW GEMM. GROUND RUNS GOOD. OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1996120500841 19961205 00841 EU 1996 12 5 REXA96063 1 19961028 A 6120 1375759003 ROD ENDS BAG JETSTM JETSTM3101 1500215 EU RT PROP GOV WORN A REXA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 318PX 689 RIGHT RPM REMAINED HIGH IN FLIGHT. ADJUSTED ROD LENGTH ON PROPELLER GOVERNOR. OPS CHECK GOOD ON GROUND RUN. (M) 2 L 7 2 4T RT A21EU 1996120500842 19961205 00842 EU 1996 12 5 REXA96061 1 19961023 A 2720 522834 TRIM INDICATOR SAAB SF340 SF340A 7850100 EU COCKPIT DRIFTING A REXA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 922MA 11850082 340A077 REQUIRES FULL RIGHT RUDDER TRIM AT SLOW AIRSPEEDS, 3 UNITS AT CRUISE AT SLOW AIRSPEEDS, A/C REQ'S FULL RIGHT RUDDER TRIM TO CENTER THE BALL AT CRUISE SPEEDS. THE TRIM IND STILL SHOWS 3 UNITS RIGHT WHEN YAW DAMPER IS ENGAGED, YELLOW RUDDER FLAG IS ANNUNCIATED IN EHSI. INSPECTED RUDDER AND TAB, NO DEFECTS NOTED. REPLACED TRIM INDICATOR. (M) 2 L 7 2 4T RT A52EU 1996120500843 19961205 00843 EU 1996 12 5 REXA96060 1 19961023 A 2435 23080031 STARTER/GEN LUCAS SAAB SF340 SF340A 7850100 EU RIGHT FAILED A REXA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CL CLIMB 1 SO 25 324PX 3698 340A048 RIGHT GENERATOR LIGHT CAME ON DURING CLIMB-OUT AT MSP. REMOVED AND REPLACED RIGHT STARTER/GENERATOR IAW SAAB MM 24-31-0 5. F/C IS GOOD. (M) 2 L 7 2 4T RT A52EU 1996120500844 19961205 00844 CE 1996 12 5 GLBA96211 1 19961023 A 2720 YAW SENSOR BEECH 1900 1900D 1154162 CE RUDDER MALFUNCTIONED A A GLBA O OTHER F FLT CONT AFFECTED CR CRUISE 1 CE 01 169GL UE169 RDU - TWO HARD UNCOMMANDED RUDDER TURNS WITH AUTOPILOT ENGAGED. TURNED OFF RUDDER BOOST. MAINTENANCE SECURED CANNON PL UG AT YAW RATE SENSOR. (M) 2 L 7 2 4T RT A24CE 1996120500845 19961205 00845 WP 1996 12 5 9625499102 1 19961130 A 3222 STRUT DOUG DC9 DC915 3022036 WP NLG REQD SERVICE A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 92S 47064 ON TAKEOFF, COULD NOT RETRACT MAIN LANDING GEAR. FOLLOWED COCKPIT OPERATING MANUAL (COM), TAKEOFF WARNING HORN CAME ON, NO AUTO PRESSURIZATION. PULLED GROUND SHIFT CIRCUIT BREAKER'S GEAR CHECKS NORMAL. FLIGHT RETURNED TO MSP AND LANDED W ITHOUT INCIDENT. MAINTENANCE SERVICED NOSE STRUT, LUBED NOSE GEAR AND GROUND SHIFT MECHANISM, OPERATION CHECKS GOOD. 2 L 7 2 4F A6WE 1996120500846 19961205 00846 EU 1996 12 5 9625503202 1 19961201 A 2750 RETRACT SYST AIRBUS 320 A320211 3930320 EU TE FLAPS LOCKED UP A A NWAA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 01 302US 32 DURING APPROACH WHEN SELECTING FLAPS 2, RECEIVED F/CTL FLAPS LOCKED ALIGNMENT FAULT COMPLETED COCKPIT OPERATING MANUAL P ROCEDURES AND LANDED WITH FLAPS 0. LANDING WAS ACCOMPLISHED WITHOUT INCIDENT. MAINTENANCE RESET NR 1 AND NR 2 SLAT FLA P CONTROL COMPUTERS, OK AT THIS TIME. 2 L 7 2 4F RT A28NM 1996120500847 19961205 00847 WP 1996 12 5 9625519852 1 19961201 A 3350 BATTERY DOUG DC9 DC951 3022051 WP TAILCONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 761NC 47709 DURING LINE CHECK, FOUND EMERGENCY SPOTLIGHT FOR INTERIOR TAILCONE DIM. REPLACED BATTERIES, OPERATION CHECKS GOOD. 2 L 7 2 4F A6WE 1996120500848 19961205 00848 WP 1996 12 5 9625529852 1 19961201 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 761NC 47709 DURING LINE CHECK, FOUND ALL CATWALK PATHWAY LIGHTING INOPERATIVE. REPLACED BATTERIES AND OPERATION CHECKS GOOD. 2 L 7 2 4F A6WE 1996120500849 19961205 00849 WP 1996 12 5 9625539152 1 19961129 A 3350 BATTERY DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8911E 45825 DURING LINE CHECK, FOUND FLOOR PROXIMITY LIGHTS FROM ROW 2 TO ROW 7 STAY ON FOR ONLY TEN SECONDS. REPLACED BATTERY AND OPERATION CHECKS GOOD. 2 L 7 2 4F A6WE 1996120500850 19961205 00850 NE 1996 12 5 9625549956 2 19961128 A 7200 ENGINE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D15 52051 NE RIGHT FAILED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN E K J VIBRATION/BUFFET FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 923RW 47183 657151 DURING CLIMB, THE RIGHT ENGINE BEGAN VIBRATING AND OIL PRESSURE, OIL QUANTITY DROPPED TO ZERO. CREW SHUTDOWN THE RIGHT ENGINE AND RETURNED TO BIL WHERE THEY LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE, OPS CHECK OK. 2 L 7 2 4F 4 F A6WE E2EA 1996120500851 19961205 00851 NE 1996 12 5 9625559917 2 19961201 A 7314 FUEL PUMP DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9A 52048 NE NR 1 ENGINE FAILED A A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 967N 47573 DURING TAKEOFF ROLL, A/C EXPERIENCED A UNDETERMINED ENGINE STALL. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENAN CE INSPECTED ENGINE INLETS, OUTLETS AND PS3 SCREENS ON BOTH ENGINES. THE NUMBER ONE ENGINE FUEL PUMP ASSEMBLY WAS REPLA CED, OPS AND LEAK CHECK OK. 2 L 7 2 4F 4 F A6WE E2EA 1996120500852 19961205 00852 WP 1996 12 5 9625569307 1 19961201 A 2420 976J2544 GEN CONTL PANEL DOUG DC9 DC982 3022082 WP LEFT MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 GL 01 309RC 37192 2402 48088 ON TAKEOFF, AC LOCKOUT WARNING ILLUMINATED WITH AC BUS OFF. FOLLOWED COM PROCEDURE AND RETURNED TO MSP. FLIGHT LANDED WITHOUT INCIDENT. REPLACED LEFT GENERATOR CONTROL PANEL. RAN BOTH ENGINE, APU AND EXTERNAL POWER AND ALL BUSES OPERATE NORMAL. 2 L 7 2 4F A6WE 1996120500853 19961205 00853 NE 1996 12 5 9625579938 2 19961129 A 7200 ENGINE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7 52053 NE RIGHT FAILED A A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 1798U 47369 655220 DURING CLIMB, THE RIGHT ENGINE OIL QUANTITY BEGAN DECREASING WITH ASSOCIATED SMOKE REPORTED IN THE CABIN. A/C RETURNED TO DTW AND LANDED WITHOUT FURTHER INCIDENT. CREW SHUTDOWN THE RIGHT ENGINE AFTER LANDING. MAINTENANCE REPLACED THE RIG HT ENGINE. 2 L 7 2 4F 4 F A6WE E2EA 1996120500854 19961205 00854 WP 1996 12 5 9625589931 1 19961128 A 3260 SWITCH DOUG DC9 DC931 3022065 WP LT MLG DOOR DIRTY A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 90S 47244 LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR RETRACTION. COCKPIT OPERATING MANUAL PROCEDURES WERE FOLLOWED AND A IRCRAFT CONTINUED TO DESTINATION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENACE CLEANED LEFT MAIN GEAR SWITCH AND ADJUS TED STRIKER BOLT, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996120500855 19961205 00855 WP 1996 12 5 9625599954 1 19961128 A 2410 CSD DOUG DC9 DC931 3022065 WP RT ENGINE MALFUNCTIONED A NWAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 01 921RW 47164 GENERATOR OFF AND AC BUS OFF LIGHTS ILLUMINATED AT BEGINNING OF TAKEOFF ROLL. CREW ABORTED TAKEOFF AND RETURNED TO GATE . MAINTENANCE REPLACED RIGHT GENERATOR, CSD AND CSD OIL COOLER AND OPERATIONAL CHECK LEAK CHECK NORMAL. 2 L 7 2 4F A6WE 1996120500856 19961205 00856 EU 1996 12 5 9625603219 1 19961202 A 2782 830A000002 ACTUATOR AIRBUS 320 A320211 3930320 EU LT/RT LE SLATS MALFUNCTIONED A A NWAA O OTHER F FLT CONT AFFECTED UK UNKNOWN 1 GL 01 319US 208 EXPERIENCED F/CTL SLATS FAULT' ACCOMPANIED BY SLATS LOCKED DURING HEAVY ICING. AIRCRAFT DID NOT SWITCH TO ALTERNATE LAW . AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BOTH LEFT AND RIGHT WING NR 2 SLAT ACTUATOR TORQUE LIMITERS POPP ED. REPLACED BOTH SLAT ACTUATORS, OPS CHECKED OK. 2 L 7 2 4F RT A28NM 1996120500857 19961205 00857 WP 1996 12 5 9625619931 1 19961128 A 3260 SWITCH STRIKER DOUG DC9 DC931 3022065 WP LT MLG DOOR OUT OF ADJUST A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 90S 47244 LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR RETRACTION. RECYCLED GEAR WITH NO HELP. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED LEFT MAIN GEAR DOOR SWITCH STRIKER, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996120500858 19961205 00858 WP 1996 12 5 9625629931 1 19961130 A 3260 SWITCH DOUG DC9 DC931 3022065 WP RT MLG DOOR MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 90S 47244 LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR RETRACTION. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MA INTENANCE REPLACED RIGHT MAIN GEAR DOOR SWITCH AND ADJUSTED RIGHT GEAR DOOR LATCH, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996120500859 19961205 00859 NM 1996 12 5 9625632707 1 19961128 A 2742 12970006 ACTUATOR BOEING 727 727225 1384077 NM STAB TRIM INOPERATIVE A NWAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 01 816EA 34631 134 22553 DURING CLIMBOUT, MAIN ELECTRIC STABILIZER TRIM WENT INOPERATIVE. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED STABILIZER TRIM ACTUATOR, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996120500860 19961205 00860 NM 1996 12 5 9625642708 1 19961201 A 3350 BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 817EA 22554 DURING PREFLIGHT, FOUND LEFT OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS M-1090, OPERATIONAL CHECK OK . 2 L 7 3 4F A3WE 1996120500861 19961205 00861 WP 1996 12 5 9625659955 1 19961129 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN CROSSED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 922RW 47182 DURING LINE MAINTENANCE INSPECTION, FOUND CABIN EMERGENCY LIGHT INOPERATIVE. FOUND EMERGENCY AND STANDBY LIGHT WIRES CR OSSED. CORRECTED WIRING, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996120500862 19961205 00862 WP 1996 12 5 9625669604 1 19961129 A 3260 UPLOCK SWITCH DOUG DC9 DC932 3022066 WP RT MLG MALFUNCTIONED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 604NW 47222 RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. RECYCLED GEAR AND NORMAL INDICATIONS WERE ACHIE VED. REPLACED RIGHT MAIN GEAR UPLOCK SWITCH AND CONNECTOR, OPERATIONAL CHECK NORMAL ON GEAR SWING. 2 L 7 2 4F A6WE 1996120500863 19961205 00863 NM 1996 12 5 9625676302 1 19961129 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 662US 23720 DURING LINE CHECK, FOUND FLOOR EMERGENCY LIGHTS INOPERATIVE FROM ROWS 36HJK TO 40HKJ. REPAIRED WIRE, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1996120500864 19961205 00864 WP 1996 12 5 9625689942 1 19961130 A 3350 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 3991C 47175 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT AND RIGHT AFT OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTE RIES IN PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996120500865 19961205 00865 WP 1996 12 5 9625699916 1 19961130 A 3350 60030451 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 949N 47566 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 16 AND 20 INOPERATIVE. REPLACED BATTER Y PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996120500866 19961205 00866 WP 1996 12 5 9625709903 1 19961129 A 3350 BATTERY DOUG DC9 DC931 3022065 WP COCKPIT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 953N 47083 DURING LINE MAINTENANCE INSPECTION, FOUND COCKPIT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY BATTERIE S, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996120500867 19961205 00867 WP 1996 12 5 9625719604 1 19961130 A 3231 LATCH ASSEMBLY DOUG DC9 DC932 3022066 WP RT MLG DOOR OUT OF ADJUST A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 604NW 47222 DURING CLIMB, RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. RECYCLED GEAR AND NORMAL INDICATI ONS WERE ACHIEVED. FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED RIGHT MAIN GEAR D OOR LATCH MECHANSIM. OPERATIONAL CHECK NORMAL ON GEAR SWING. 2 L 7 2 4F A6WE 1996120500868 19961205 00868 WP 1996 12 5 9625729996 1 19961129 A 2150 CLAMP DOUG DC9 DC931 3022065 WP RT ACM BROKEN A NWAA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 GL 01 8932E 47141 LOSS OF CABIN PRESSURIZATION OCCURRED AT 25,000 FEET EN ROUTE. OXYGEN MASKS WERE DEPLOYED THROUGHOUT CABIN AND DESCENT WAS MADE TO 10,000 FEET. FLIGHT DIVERTED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BROKEN CLAMP AND DUCT L EAK AT RIGHT AIR CYCLE MACHINE TURBINE DISCHARGE. REPLACED CLAMP, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996120500869 19961205 00869 WP 1996 12 5 9625739996 1 19961130 A 3260 DOWNLOCK SWITCH DOUG DC9 DC931 3022065 WP NLG MALFUNCTIONED A NWAA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 01 8932E 47141 DURING APPROACH, NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMNATE AFTER GEAR EXTENSION. RECYCLED GEAR THREE TIMES BEFORE NORMAL INDICATIONS WERE ACHIEVED. AIRCRAFT LANDED WITHOUT INCIDENT. FERRIED AIRCRAFT FROM GRR TO DTW. MAINTENANCE RE PLACED NOSE GEAR DOWNLOCK SWITCH, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996120500870 19961205 00870 WP 1996 12 5 9625749977 1 19961130 A 3260 SWITCH DOUG DC9 DC931 3022065 WP LT MLG DOOR MALFUNCTIONED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 9341 47390 LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR RETRACTION. FLIGHT CONTINUED TO DESTINATION. EMERGENCY GEAR EXTENS ION PROCEDURES WERE UTILIZED AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEFT MAIN GEAR DOOR SWITCH, OPE RATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996120500871 19961205 00871 WP 1996 12 5 9625751147 1 19961202 A 7711 PT 7 LINE DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20J 52054 NE NR 3 ENGINE BROKEN A NWAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 01 147US 46756 86126 DURING TAKEOFF ROLLOUT, THE NR 3 ENGINE EXHIBITED LOWER POWER. THE TAKEOFF WAS ABORTED AND A/C RETURNED TO GATE. MAINT ENANCE FOUND A BROKEN PT7 LINE BETWEEN 6 AND 8 O'CLOCK POSITION. REPAIR WAS DEFERRED PER MEL 77-3. 2 L 7 3 4F 4 F A22WE E20EA 1996120500872 19961205 00872 1996 12 5 9625209924 4 19961122 A 2565 113317 SLIDE DOUG DC9 DC932 3022066 WP FWD SERV DOOR LOW BATTERY A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 926RC 37194 5067 47473 DURING PERIODIC CHECK, FOUND FORWARD GALLEY SERVICE DOOR EVACUATION SLIDE BATTERY PACK INOPERATIVE. REPLACED SLIDE. 2 L 7 2 4F A6WE 1996120500873 19961205 00873 NM 1996 12 5 SWAA961284 1 19961121 A 3350 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 369SW 26580 DURING WALKAROUND, FOUND AFT UPPER CABIN FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996120500874 19961205 00874 NM 1996 12 5 SWAA961285 1 19961126 A 3350 LIGHT BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED TERMINAL CHECK, FOUND FWD SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHT SIGN INOP. REMOVED AND REPLACED L IGHT ASSEMBLY PER BOEING M/M. 2 L 7 2 4F A16WE 1996120500875 19961205 00875 NM 1996 12 5 SWAA961286 1 19961129 A 2120 AIR DISTR BOEING 737 7373H4 1384600 NM AFT GALLEY ODOR A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 358SW 26595 JUST AFTER PUSHBACK, PASSENGER AND F/A NOTED A BURNING SMELL AT AFT GALLEY AREA. OPENED AND INSPECTED AFT AREA PLUS, RA N ENGINES, AND TURNED OFF APU. SMELL DISSIPATED, CONTINUED UNDER MEL. 2 L 7 2 4F RT A16WE 1996120500876 19961205 00876 NM 1996 12 5 SWAA961287 1 19961129 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 621SW 28037 DURING SCHEDULED RON CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT ROW 11. RESECURED LIGHT ASSEMBLY WIRE TERMINAL AND OP C HECKED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996120500877 19961205 00877 NM 1996 12 5 SWAA961288 1 19961129 A 3397 WIRE BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 635SW 27710 DURING SCHEDULED A2 CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOP AT MID CABIN AREA. RESECURED LIGHT WIRES AND OP CH ECKED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996120500878 19961205 00878 NM 1996 12 5 SWAA961289 1 19961202 A 5330 SKIN BOEING 737 7372H4 138448C NM CARGO DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 51SW 21448 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN AT LOWER FWD CORNER OF AFT CARGO DOOR CUTOUT CRACKED 3 INCHES. REPAIRED PER SWA RA 1-253-1551 AND BOEING SRM. 2 L 7 2 4F A16WE 1996120500879 19961205 00879 NM 1996 12 5 SWAA961290 1 19961126 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 291.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 64SW 22062 DURING SCHEDULED D-CHECK, FOUND BS 291.5 FRAME WEB CRACKED AT WL 235 AND WL 241. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996120500880 19961205 00880 NM 1996 12 5 SWAA961291 1 19961126 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 298 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 64SW 22062 DURING SCHEDULED D-CHECK, FOUND BS 298 FWD GALLEY DOORWAY FWD CUTOUT FRAME CRACKED AT WL 260. REPLACED DAMAGED SECTION PER BOEING SRM. 2 L 7 2 4F A16WE 1996120500881 19961205 00881 NM 1996 12 5 SWAA961292 1 19961126 A 3350 BATTERIES BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 67SW 22356 DURING SCHEDULED SERVICE CHECK, FOUND FWD GALLEY EMERGENCY FLASHLIGHT BATTERIES WEAK. REPLACED BATTERIES PER BOEING M/M . 2 L 7 2 4F A16WE 1996120500882 19961205 00882 NM 1996 12 5 SWAA961293 1 19961129 A 5320 SPLICES BOEING 737 7372H4 138448C NM BS 907 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 91SW 22963 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICES CORRODED AT BS 907, STRINGERS 25L AND 26L, WL 158. REPLACED SPLICES PE R BOEING SRM. 2 L 7 2 4F A16WE 1996120500883 19961205 00883 NM 1996 12 5 SWAA961294 1 19961129 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 91SW 22963 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CORROSION AT BS 727 KEEL BEAM AREA LBL 10 TO RBL 10. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996120500884 19961205 00884 NM 1996 12 5 SWAA961295 1 19961129 A 5320 TIES BOEING 737 7372H4 138448C NM BS 360 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 91SW 22963 DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER TIES AT BS 360, STR 14L AND 15L. REPLACED TIES PER BOEING SRM. 2 L 7 2 4F A16WE 1996120500885 19961205 00885 NM 1996 12 5 SWAA961296 1 19961129 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 520 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 91SW 22963 DURING SCHEDULED D-CHECK, FOUND STRINGER 16R AT BS 520 CRACKED. REPLACED STRINGER PER BOEING SRM. 2 L 7 2 4F A16WE 1996120500886 19961205 00886 NM 1996 12 5 SWAA961297 1 19961129 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 616 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 91SW 22963 DURING SCHEDULED D-CHECK, FOUND I/B CHORD OF FRAME AT BS 616 CRACKED, LBL 69, WL 209. REPLACED I/B CHORD OF FRAME PER BOEING SRM. 2 L 7 2 4F A16WE 1996120500887 19961205 00887 NM 1996 12 5 SWAA961298 1 19961129 A 5320 MOPSILL BOEING 737 7372H4 138448C NM BS 957-986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 91SW 22963 DURING SCHEDULED D-CHECK, FOUND AFT SERVICE DOOR MOPSILL CORRODED AT BS 957 TO 986, RBL 53, WL 208. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996120500888 19961205 00888 NM 1996 12 5 SWAA961299 1 19961129 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 91SW 22963 DURING SCHEDULED D-CHECK, FOUND WALL SUPPORT ANGLE CORRODED AT BS 1016. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996120500889 19961205 00889 NM 1996 12 5 SWAA961300 1 19961129 A 5320 SUPPORT BOEING 737 7372H4 138448C NM BS 994-1006 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 91SW 22963 DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 994 TO 1006. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996120500890 19961205 00890 NM 1996 12 5 SWAA961301 1 19961129 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 91SW 22963 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 43, WL 208. REPAIRED PER EWO 96-0709. 2 L 7 2 4F A16WE 1996120500891 19961205 00891 NM 1996 12 5 SWAA961302 1 19961129 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 91SW 22963 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED ON UPPER CHORD AT BS 986 RBL 45 TO LBL 18, WL 208. REPAIRED PER EWO 96-0709. 2 L 7 2 4F A16WE 1996120500892 19961205 00892 NM 1996 12 5 SWAA961303 1 19961129 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 967 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 91SW 22963 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED ON UPPER CHORD AT BS 967, RBL 27.5 TO LBL 55, WL 208. REPAIRED PER BOEING TI T1-A53-014. 2 L 7 2 4F A16WE 1996120500893 19961205 00893 NM 1996 12 5 SWAA961304 1 19961129 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 91SW 22963 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED ON UPPER CHORD AT BS 947, RBL 20 TO RBL 54, WL 208. REPAIRED PER BO EING SRM. 2 L 7 2 4F A16WE 1996120500894 19961205 00894 NM 1996 12 5 SWAA961305 1 19961129 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 294 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 91SW 22963 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED ON UPPER CHORD AT BS 294, WL 208. REPLACED UPPER T-CHORD PER BOEING SRM. 2 L 7 2 4F A16WE 1996120500895 19961205 00895 NM 1996 12 5 SWAA961306 1 19961129 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 310 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 91SW 22963 DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR UPPER FWD CLOSE OUT ATTACH ANGLE CRACKED AT BS 310, WL 281. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996120500896 19961205 00896 NM 1996 12 5 SWAA961307 1 19961129 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 312 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 91SW 22963 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 312, LBL 33, WL 283. REPLACED CRACKED SECTION PER BOEING SRM. 2 L 7 2 4F A16WE 1996120500897 19961205 00897 NM 1996 12 5 SWAA961308 1 19961129 A 5320 CHANNEL BOEING 737 7372H4 138448C NM BS 270 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 91SW 22963 DURING SCHEDULED D-CHECK, FOUND Z-CHANNEL CRACKED AT BS 270, RBL 8 TO LBL 8. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996120500898 19961205 00898 NM 1996 12 5 SWAA961309 1 19961129 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 91SW 22963 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED ON UPPER FLANGE AT BS 312, LBL 8 TO RBL 55, WL 208. REPAIRED PER BO EING SRM. 2 L 7 2 4F A16WE 1996120500899 19961205 00899 NM 1996 12 5 SWAA961310 1 19961129 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 91SW 22963 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED ON UPPER FLANGE AT BS 328, RBL 12 TO RBL 58, WL 208. REPAIRED PER B OEING SRM. 2 L 7 2 4F A16WE 1996120500900 19961205 00900 NM 1996 12 5 SWAA961311 1 19961129 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 91SW 22963 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED ON UPPER FLANGE AT BS 344, RBL 10 TO LBL 54, WL 208. REPAIRED PER B OEING SRM. 2 L 7 2 4F A16WE 1996120500901 19961205 00901 NM 1996 12 5 SWAA961312 1 19961129 A 5320 SHEAR TIE BOEING 737 7372H4 138448C NM BS 967 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 91SW 22963 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 967, LBL 50. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996120500902 19961205 00902 NM 1996 12 5 SWAA961313 1 19961129 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 1074 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 91SW 22963 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 1074 GOUGED AT BS 1074. REPLACED DAMAGED SECTION PER BOEING SRM. 2 L 7 2 4F A16WE 1996120500903 19961205 00903 NM 1996 12 5 SWAA961314 1 19961129 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 1074 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 91SW 22963 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 1074 GOUGED AT BS 1074. REPLACED DAMAGED SECTION PER BOEING SRM. 2 L 7 2 4F A16WE 1996120500904 19961205 00904 NM 1996 12 5 SWAA961315 1 19961129 A 5312 BULKHEAD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 91SW 22963 DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT LBL 11 TO 13.5 AND AT LBL 16 TO 17. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996120500905 19961205 00905 NM 1996 12 5 SWAA961316 1 19961129 A 5320 DOUBLER BOEING 737 7372H4 138448C NM FWD GALLEY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 91SW 22963 DURING SCHEDULED D-CHECK, FOUND FWD GALLEY DOOR LOWER AFT STOP FITTING INNER DOUBLER CRACKED. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996120500906 19961205 00906 NM 1996 12 5 SWAA961317 1 19961129 A 3350 6104781 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 91SW 22963 DURING SCHEDULED D-CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F A16WE 1996120500907 19961205 00907 NM 1996 12 5 SWAA961318 1 19961129 A 5320 WEB BOEING 737 7372H4 138448C NM BS 440 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 92SW 22964 DURING SCHEDULED 1/2 D-CHECK, FOUND WEB DAMAGED AND CRACKED AT BS 440, S24R. REPLACED WEB PER BOEING SRM. 2 L 7 2 4F A16WE 1996120500908 19961205 00908 NM 1996 12 5 SWAA961319 1 19961129 A 5320 CLIP BOEING 737 7372H4 138448C NM BS 1138 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 92SW 22964 DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER CLIP CRACKED AT S12L, BS 1138. REPLACED CLIP PER BOEING SRM. 2 L 7 2 4F A16WE 1996120500909 19961205 00909 NM 1996 12 5 SWAA961320 1 19961126 A 5230 SKIN BOEING 737 7372H4 138448C NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 94SW 23053 DURING SCHEDULED C2 CHECK, FOUND AFT RADIUS OF AFT CARGO DOOR HANDLE CUTOUT CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996120500910 19961205 00910 NM 1996 12 5 SWAA961321 1 19961201 A 2612 FIRE LIGHT BOEING 737 7372H4 138448C NM APU ILLUMINATED A SWAA F ACTIVATE FIRE EXT. N FALSE WARNING LD LANDING 1 SW 07 102SW 23108 AT TOUCHDOWN, APU FIRE DETECT INOP LIGHT FLICKERED. APU FIRE HANDLE AND BELL ACTIVATED. APU WAS SHUTDOWN. INSPECTED W ITH NO EVIDENCE OF FIRE OR OVERHEAT CONDITIONS. CONTINUED PER MEL 26-6. 2 L 7 2 4F A16WE 1996120500911 19961205 00911 NM 1996 12 5 SWAA961322 1 19961123 A 3241 0320017 VALVE BOEING 737 7372T4 1384492 NM RT MLG INOPERATIVE A SWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 722WN 22698 IN ROUTE, I/B ANTI-SKID INOP LIGHT ILLUMINATED. UNABLE TO CONTINUE TO DESTINATION, DIVERTED TO STL AND MADE AN UNEVENTF UL LANDING. REPLACED RIGHT I/B ANTI-SKID VALVE PER BOEING M/M. 2 L 7 2 4F A16WE 1996120500912 19961205 00912 NM 1996 12 5 SWAA961323 1 19961127 A 3350 FUSE BOEING 737 7373H4 1384600 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED BC3 CHECK, FOUND CABIN BULLNOSE EMERGENCY EXIT LIGHTS ABOVE ROWS 22 AND 18 INOP. REPLACED BULB SOCKET AND BATTERY PACK FUSE PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996120500913 19961205 00913 NM 1996 12 5 SWAA961324 1 19961127 A 3350 BULB BOEING 737 7373H4 1384600 NM COCKPIT FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED BC3 CHECK, FOUND COCKPIT EMERGENCY LIGHTING VERY DIM. RELAMPED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996120500914 19961205 00914 NM 1996 12 5 SWAA961325 1 19961127 A 3350 LAMP BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED BC3 CHECK, FOUND CABIN AFT RED EMERGENCY FLOOR TRACK LIGHT INOP. REPLACED 2 LAMPS PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996120500915 19961205 00915 NM 1996 12 5 SWAA961326 1 19961130 A 3350 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN FLOOR LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996120500916 19961205 00916 NM 1996 12 5 SWAA961329 1 19961127 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 194 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673AA 23251 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN DENTED 6 INCHES ABOVE STRINGER 24 AT FRAME, BS 194. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996120500917 19961205 00917 NM 1996 12 5 SWAA961330 1 19961127 A 3350 604221 SUPPLY BOEING 737 7373Y0 1384671 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 682SW 23496 DURING SCHEDULED RON CHECK, FOUND FWD ENTRY EMERGENCY LIGHTING INOP. REPLACED BATTERY POWER SUPPLY AND OP CHECKED PER B OEING M/M. 2 L 7 2 4F RT A16WE 1996120500918 19961205 00918 NM 1996 12 5 SWAA961331 1 19961130 A 2841 INDICATOR BOEING 737 7375H4 138449D NM RIGHT INOPERATIVE A SWAA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 505SW 24182 RIGHT WING FUEL QUANTITY BEGAN DROPPING DURING FLIGHT CAUSING THE INABILITY TO MAINTAIN BALANCED FUEL LOAD. AIRCRAFT DI VERTED TO CLE AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND RT MAIN FUEL QUANTITY INDICATOR INOP. REPLACED PER B OEING M/M. 2 L 7 2 4F RT A16WE 1996120500919 19961205 00919 NM 1996 12 5 SWAA961332 1 19961125 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 727D PLUS 5, WL 156, RBL 6. REPLACED CORRODED SECTION PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996120500920 19961205 00920 NM 1996 12 5 SWAA961333 1 19961129 A 5320 DOUBLER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED BC2 CHECK, FOUND EXTERNAL DOUBLER CRACKED AT UPPER LT PITOT PROBE AREA, BS 219 TO 235, S15L TO 16L. RE PLACED DOUBLER PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996120500921 19961205 00921 NM 1996 12 5 SWAA961334 1 19961129 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 1074 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 91SW 22963 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 1074 GOUGED AT BS 1074. REPLACED DAMAGED SECTION PER BOEING SRM. 2 L 7 2 4F A16WE 1996120500922 19961205 00922 EU 1996 12 5 QXEA9600471 1 19961129 A 3350 1820 BULB FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 469US 11096 LEFT HAND OVERWING EMERGENCY EXIT LIGHT WAS INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996120500923 19961205 00923 NM 1996 12 5 QXEA9600472 1 19961129 A 3230 11300105 UPLOCK ACTUATOR DHAV DHAV DHC8 DHC8102 2809003 NM LT MLG INOPERATIVE A QXEA O OTHER J WARNING INDICATION AP APPROACH 1 NM 09 816PH 9739 54 ALTERNATE GEAR EXTENSION PERFORMED BECAUSE LEFT MAIN GEAR REMAINED IN THE WHEEL WELL DURING NORMAL GEAR EXTENSION. LEFT MAIN GEAR EXTENDED USING ALTERNATE METHOD. AIRCRAFT LANDED IN PDX WITHOUT FURTHER PROBLEMS. LEFT HAND UPLOCK ACTUATOR REPLACED IAW MAINTENANCE MANUAL, UPLOCK ROLLER LUBED AND GEAR OPS CHECKED GOOD ON GEAR SWING. 2 H 7 2 4T RT A13NM 1996120500924 19961205 00924 EU 1996 12 5 QXEA9600473 1 19961129 A 3350 6008905 POWER SUPPLY FOKKER FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 484US 11234 THE FOUR OVER WING EMERGENCY EXIT SIGNS ARE INOP. EMERGENCY EXIT SIGN POWER SUPPLY WAS REPLACED AND THE EXIT SIGNS OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996120500925 19961205 00925 EU 1996 12 5 QXEA9600474 1 19961130 A 3350 1012721 BULB FOKKER FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 487US 11238 EMERGENCY EXIT LIGHT AT SEAT 8A IS INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996120500926 19961205 00926 EU 1996 12 5 QXEA9600475 1 19961130 A 3350 2TC125 BREAKER FOKKER FOKKER F28 F28MK4000 4990810 EU COCKPIT TRIPPED A QXEA K NONE L NO TEST CR CRUISE 1 NM 09 490US 11152 EMERGENCY LIGHTS CAME ON IN FLIGHT AND CREW WAS UNABLE TO EXTINGUISH. AUTO EVAC CIRCUIT BREAKER FOUND POPPED. BREAKER WAS RESET AND LIGHTS OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996120500927 19961205 00927 NM 1996 12 5 QXEA9600476 1 19961130 A 5610 001A561A0000200 WINDSHIELD DORNER DO32 DO328100 2996000 NM LT COCKPIT CRACKED A QXEA K NONE O OTHER AP APPROACH 1 NM 09 332PH 6391 3010 PILOTS WINDSHIELD STARTED ARCING AND CRACKING UP THE CENTER OF THE WINDSHIELD. WINDSHIELD HEAT SWITCHED OFF AND AIRCRA FT LANDED IN BTM WITHOUT FURTHER PROBLEMS. PILOTS WINDSHIELD REPLACED IAW MAINTENANCE MANUAL. WINDSHIELD HEAT CONTROLL ER REPLACED AS A PRECAUTIONAY MEASURE. WINDSHIELD HEAT OPS CHECKED GOOD. 2 H 7 2 4T RT A45NM 1996120500928 19961205 00928 WP 1996 12 5 RRXA96167 1 19961127 A 2110 TURBO COMP DOUG DC8 DC862F 3021972 WP NR 2 FAILED A RRXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 15 996CF 46162 NR 2 TURBO COMPRESSOR HAD LOUD GRINDING NOISE AND SENT BURNING ODOR INTO COCKPIT. MAINTENANCE REMOVED AND REPLACED NR 2 TC, OPERATIONAL CHECK OF THE TC SYSTEM WAS GOOD. 2 L 7 4 4F 4A25 1996120500929 19961205 00929 NE 1996 12 5 TC8A96068 2 19961201 A 7532 563883 BLEED VALVE DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3B 52039 NE NR 2 ENGINE FAILED A TC8A C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 23 181SK 1585 45910 669173 NUMBER TWO ENGINE FAILED TO DEVELOPE T/O THRUST, AIRPLANE RETURNED TO CARGO RAMP. FOUND NUMBER TWO ENGINE BLEED VALVE A T FAULT. REMOVED AND REPLACED THE SAME IN ACCORDANCE WITH MAINT MANUAL 75-30-3, ENGINE RUN-UP ACCOMPLISHED, GROUND CHEC KS NORMAL. 2 L 7 4 4F 4 F 4A25 1E8 1996120500930 19961205 00930 SO 1996 12 5 SRAA1074 1 19961013 A 5315 FLOORBEAM LKHEED 382 382G 526414U SO BS 737 CORROSION A SRAA K NONE O OTHER IN INSP/MAINT 1 GL 23 905SJ 45318 4472 DURING C-CHECK, FOUND CORROSION ON CARGO COMPARTMENT FLOORBEAM AT TIE DOWN MOUNT HOLES FS 737E BL 0. REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. CUT OUT CORRODED AREA, FABRICATED AND INSTALLED L-ANGLE AND STRAP IAW LAC SRM 51-140-22. 2 H 7 4 4T A1SO 1996120500931 19961205 00931 NM 1996 12 5 SWAA961328 1 19961127 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 787 CREASED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 606SW 27926 DURING SCHEDULED RON, FOUND WINDOW FRAME SKIN CREASED AT BS 787, BETWEEN NR 30 AND 31 WINDOWS, RIGHT SIDE. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996121000004 19961210 00004 EU 1996 12 10 CA960522004 2 19960418 A 7323 B5039 GOVERNOR LUCAS LPG127 FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU ENGINE REQ ADJUST W C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CA B5039 9007 (CAN)AIRCRAFT FAILED TO MAKE 100 PERCENT RATED THRUST ON TAKEOFF, TAKEOFF REJECTED LP GOVERNOR ADJUSTED TO 102 PERCENT 2 L 7 2 4F 4 F RT A20EU E2EU 1996121200001 19961212 00001 SO 1996 12 12 PNSA961101 1 19961102 A 2731 6353000 CONTROLS PIPER PA32 PA32301 7103207 SO ELEVATOR TRIM LACK OF LUBE A PNSA A UNSCHED LANDING O OTHER CL CLIMB 1 AL 03 8305H 328106017 ELEVATOR TRIM STIFF. RETURNED TO AIRPORT. 1 L 7 1 3O A3SO 1996121200002 19961212 00002 SW 1996 12 12 PNSA961102 1 19961107 A 5210 DOOR SEAL SWRNGN SA227 SA227AC 8780603 SW PAD DOOR CONTAMINATED A PNSA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 46NE AC746B A/C WOULD NOT PRESSURIZE. RETURNED TO GATE, PURGED WATER FROM DOOR SEAL. OPS CK OK. 2 L 7 2 4T RT A8SW 1996121200003 19961212 00003 SW 1996 12 12 PNSA961103 1 19961119 A 3230 NAS77A843 UPLOCK BUSHING SWRNGN SA227 SA227AC 8780603 SW NLG LACK OF LUBE A PNSA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 41NE AC741B NOSE GEAR WOULD NOT LOCK UP. RETURNED TO GATE, LUBED UPLOCK BUSHING. 2 L 7 2 4T RT A8SW 1996121200004 19961212 00004 SO 1996 12 12 PNSA961104 1 19961122 A 2731 6353000 CONTROLS PIPER PA32 PA32301 7103207 SO ELEVATOR TRIM FROZEN A PNSA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 AL 03 8305H 328106017 ELEVATOR TRIM FROZEN, THAWED ICE, LUBED DRUM, CHECKS OK. 1 L 7 1 3O A3SO 1996121200005 19961212 00005 SO 1996 12 12 PNSA961105 1 19961125 A 2432 G35 BATTERY PIPER PA32 PA32301 7103207 SO BATTERY COMPT DISCHARGED A PNSA D RETURN TO BLOCK O OTHER IN INSP/MAINT 1 AL 03 8327S 1045 328106039 PILOT REPORTED ENGINE NO START, REPLACED BATTERY, NO OTHER FAULT FOUND. 1 L 7 1 3O A3SO 1996121200006 19961212 00006 SO 1996 12 12 RAAA96E8035 1 19961203 A 3350 100053 LIGHT LKHEED 188 188C 5262604 SO CABIN FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 LT FWD OVERWING EMERGENCY EXIT PULLDOWN LIGHT FAILED SERVICE CHECK. CHANGED LIGHT ASSY. 2 L 7 4 4T 4A22 1996121200007 19961212 00007 NM 1996 12 12 CALA9601724 1 19961203 A 3260 189915 SENSOR BOEING 737 737130 1384435 NM LANDING GEAR OUT OF ADJUST A CALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 14211 19028 THE GEAR HANDLE WOULD NOT MOVE PAST THE OFF POSITION AFTER TAKEOFF FROM PHL. CYCLING OF THE GEAR LIGHT CIRCUIT BREAKER MADE NO CHANGE. THE AIRCRAFT WAS RETURNED TO PHL WHERE IT LANDED WITHOUT INCIDENT (THE AIRCRAFT HAD AIR RETURNED THE DA Y BEFORE FOR THE GEAR NOT RETRACTING; AT THAT TIME, THE LANDING GEAR ACCESSORY UNIT WAS REPLACED AS CORRECTIVE ACTION). MAINTENANCE FOUND THE LANDING GEAR AIR SAFETY SENSOR GAP OUT OF ADJUSTMENT. THE AIR SAFETY SENSOR WAS ADJUSTED AND TES TED PER MM 32-09-200, PAGE 501. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F A16WE 1996121200008 19961212 00008 WP 1996 12 12 CALA9601725 1 19961203 A 3231 APH7204511 CONTROL CABLE DOUG DC10 DC1030 3023501 WP RT MLG DOOR BROKEN A CALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 09 13067 47866 THE AIRCRAFT ARRIVED IN EWR WITH THE RT MLG DOOR HANGING DOWN. MAINTENANCE FOUND THE RT MLG DOOR FOLLOW-UP CABLE BROKEN . THE CABLE WAS REMOVED AND REPLACED AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 3 4F A22WE 1996121200009 19961212 00009 NM 1996 12 12 9625766603 1 19961205 A 2910 HYD LINE BOEING 747 747151 1384891 NM NR 4 HYD SYST LEAKING A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 603US 19780 DURING CLIMB, THE HYDRAULIC FLUID IN THE NR 4 HYDRAULIC SYSTEM DECREASED. AIRCRAFT RETURNED TO NRT AND LANDED WITHOUT I NCIDENT. SECURED HYDRAULIC LINE ON NR 4 AIR DRIVEN PUMP AUTO PRESSURE CONTROL SWITCH. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996121200010 19961212 00010 WP 1996 12 12 9625779851 1 19961202 A 2421 GENERATOR DOUG DC9 DC951 3022051 WP APU FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 01 760NC 47708 IN CRUISE FROM ALB TO DTW, LEFT GENERATOR WENT OFF LINE. APU GENERATOR INOPERATIVE IN FLIGHT. FLIGHT DIVERTED TO SYR A ND LANDED WITHOUT INCIDENT. MAINTENANCE RESET GENERATOR ON GROUND AND OPS CHECKED OK. SIMULATED FLIGHT MODE AND OPERAT ION CHECKS OK. 2 L 7 2 4F A6WE 1996121200011 19961212 00011 WP 1996 12 12 9625789991 1 19961203 A 5350 CLIPS DOUG DC9 DC931 3022065 WP TAILCONE OUT OF ADJUST A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8957E 47215 DURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR TAIL CONE HANDLE FROM CLIPS. MAINTE NANCE ADJUSTED CLIPS. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996121200012 19961212 00012 WP 1996 12 12 9625799941 4 19961203 A 2565 113317 SLIDE DOUG DC9 DC932 3022066 WP PAX DOOR LOW PRESSURE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 3324L 5507 1014 47103 DURING LINE MAINTENANCE INSPECTION, FOUND MAIN CABIN DOOR EVACUATION SLIDE LOW ON PRESSURE. REPLACED SLIDE. 2 L 7 2 4F A6WE 1996121200013 19961212 00013 WP 1996 12 12 9625809909 1 19961202 A 3350 CONNECTOR DOUG DC9 DC931 3022065 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 959N 47255 DURING LINE MAINTENANCE INSPECTION, FOUND OVERWING EXIT EMERGENCY LIGHTS DIM. MAINTENANCE REPAIRED GROUND TERMINAL CONN ECTION. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996121200014 19961212 00014 WP 1996 12 12 9625819942 1 19961202 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 3991C 47175 DURING LINE MAINTENANCE INSPECTION, FOUND MID-CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES. OPERATI ONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996121200015 19961212 00015 WP 1996 12 12 9625829967 1 19961203 A 3350 CONNECTOR DOUG DC9 DC931 3022065 WP CABIN NOT SEATED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9331 47263 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS BETWEEN ROWS 14 AND 17 INOPERATIVE. MAINTENANCE RESEATED CON NECTION AT ROW 14. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996121200016 19961212 00016 WP 1996 12 12 9625839987 1 19961202 A 3350 60030451 BATTERY PACKS DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 987US 47458 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATT ERY PACKS. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996121200017 19961212 00017 WP 1996 12 12 9625849993 1 19961202 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8986E 47402 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS WEAK. REPLACED BATTERIES AT GALLEY DOOR POWER SUPPLY. OPERA TIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996121200018 19961212 00018 WP 1996 12 12 9625859906 1 19961203 A 2820 O-RING DOUG DC9 DC931 3022065 WP LT WING BROKEN A NWAA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 GL 01 956N 47252 FUEL LEAKING FROM LEFT WING AFTER TAKEOFF. FLIGHT RETURNED TO MIA AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LEAK AT DUCT CONNECTION BETWEEN CROSSFEED VALVE AND FORWARD RIGHT FUEL PUMP. REPLACED O-RINGS. OPERATIONAL CHECK NORMAL. A IRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996121200019 19961212 00019 WP 1996 12 12 9625869602 1 19961202 A 3260 CONNECTOR DOUG DC9 DC932 3022066 WP NLG DAMAGED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 602NW 47046 DURING CLIMBOUT FROM MSN, NOSE LANDING GEAR GREEN LIGHT REMAINED ON AFTER GEAR RETRACTION. RECYCLED GEAR AND LIGHT EXTI NGUISHED AFTER APPROXIMATELY FIVE MINUTES. FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE RE PLACED NOSE GEAR LOCK SWITCH CONNECTOR DUE TO DAMAGED BACKSHELL. ALSO REPLACED LOCK SWITCH AND UPLIMIT SWITCH. OPERATI ONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996121200020 19961212 00020 NM 1996 12 12 9625876608 1 19961126 A 5320 65B046431 SILL BOEING 747 747151 1384891 NM BS 1809 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 608US 19785 DURING PCK, FOUND TWO CRACKS IN THE AFT CARGO DOOR LOWER MAIN SILL OUTBOARD CHORD. SEVERED CHORD AND INSTALLED NEW DOUB LERS MADE FROM 2024-T3, .160 INCH AND .250 INCH PER EA 66-120453. 2 L 7 4 4F A20WE 1996121200021 19961212 00021 NM 1996 12 12 9625896740 1 19961127 A 5320 BEAM BOEING 747 747251F 1384898 NM CARGO COMPT CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 640US 23888 DURING LINE CHECK, FOUND CRACK IN AFT CARGO COMPARTMENT VERTICAL BEAM AT AFT EDGE OF DOOR OPENING. REPAIRED PER EA 67-3 3556. 2 L 7 4 4F A20WE 1996121200022 19961212 00022 WP 1996 12 12 9625909980 1 19961204 A 5330 SKIN DOUG DC9 DC931 3022065 WP FS 676-698 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9344 47440 DURING PERIODIC CHECK, FOUND SKIN AT RIGHT KEEL CORRODED BETWEEN FS 676 AND FS 698. REPLACED SKIN AND INSTALLED DOUBLER AND SHIMS PER EA 99-111913. L/P 0899472. 2 L 7 2 4F A6WE 1996121200023 19961212 00023 WP 1996 12 12 9625919914 1 19961204 A 5320 PRESS PANEL DOUG DC9 DC931 3022065 WP FS 83 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 964N 47416 DURING PERIODIC CHECK, FOUND NOSE WHEELWELL PRESSURE PANEL CRACKED APPROXIMATELY 2 INCHES AT RIGHT SIDE FRAME ATTACH POI NT, F.S. 83. REPAIRED PER EA 99-111235. L/P 0899335. 2 L 7 2 4F A6WE 1996121200024 19961212 00024 NM 1996 12 12 9625886608 1 19961127 A 5347 SEAT TRACK BOEING 747 747151 1384891 NM BS 452-458 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 608US 19785 DURING PCK, FOUND CORROSION ON SEAT TRACK FLANGE, LEFT SIDE 28 INBOARD. REPAIRED PER EA 66-120462. 2 L 7 4 4F A20WE 1996121200025 19961212 00025 WP 1996 12 12 9625929952 1 19961204 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 598 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 916RW 47144 DURING PERIODIC CHECK, FOUND LOWER FLANGE OF FUSELAGE FRAME CRACKED FS 598, LONGERON 30L. REPAIRED PER EA 99-120158. L /P 0899286. 2 L 7 2 4F A6WE 1996121200026 19961212 00026 WP 1996 12 12 9625939952 1 19961204 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 529-584 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 916RW 47144 DURING PERIODIC CHECK, FOUND CORROSION ON BELLY SKIN FROM FS 529 TO FS 584, LONGERONS 26L TO 26R. INSTALLED REPLACEMENT SKIN PER EA 99-120159. L/P 0899331. 2 L 7 2 4F A6WE 1996121200027 19961212 00027 WP 1996 12 12 9625949980 1 19961203 A 5320 PRESSURE PANEL DOUG DC9 DC931 3022065 WP BS 110 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9344 47440 DURING PERIODIC CHECK, FOUND NOSE WHEELWELL PRESSURE PANEL CRACKED AT FS 110, LEFT AND RIGHT AT INBOARD AND OUTBOARD TOP VERTICAL SUPPORT. REPAIRED PER EA 99-111906. L/P 0898978, 0898972, 0898965. 2 L 7 2 4F A6WE 1996121200028 19961212 00028 WP 1996 12 12 9625959980 1 19961203 A 5320 PRESSURE PANEL DOUG DC9 DC931 3022065 WP BS 83 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9344 47440 DURING PERIODIC CHECK, FOUND NOSE WHEELWELL PRESSURE PANEL CRACKED AT FS 83, LEFT AND RIGHT SIDE. REPAIRED PER EA 99-11 1904. L/P 0899110, 0899101. 2 L 7 2 4F A6WE 1996121200029 19961212 00029 SO 1996 12 12 COMA9610339 1 19961204 A 5246 12047700001 FUEL DOOR EMB 120 EMB120RT SO R/H WING NOT CLOSED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 462CA 120264 SERVICE DOOR WARNING DURING TAKEOFF. FOUND FUEL SERVICE DOOR OPEN - SECURED DOOR CLOSED AND AIRCRAFT CONTINUED SERVICE. 2 L 7 2 4T RT A31SO 1996121200030 19961212 00030 1996 12 12 COMA9660218 4 19961202 A 3422 6225812606 FLUX VALVE CNDAIR CL600 CL6002B19 EA LEFT MALFUNCTION A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 914CA 8934 7012 COPILOT'S HSI HEADING DRIFTS 10 DEGREES TO 15 DEGREES, RED HEADING FLAG IN VIEW. REPLACED THE LT FLUX DETECTOR. PART T OTAL CYCLES, 8,180. 2 L 7 2 4F RT A21EA 1996121200031 19961212 00031 NE 1996 12 12 COMA9660219 2 19961204 A 7321 EEC CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LT ENGINE MALFUNCTIONED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 920CA 7022 LEFT ENGINE WOULD NOT ACCELERATE ABOVE 52 DEGREES WITH THE SPEED SWITCHES ON. TRANSFERRED THE ELECTRONIC ENGINE CONTROL SYSTEM TO DEFERRED MAINTENANCE LIST. AIRCRAFT CONTINUED SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 1996121200032 19961212 00032 NM 1996 12 12 UPS96221729 1 19961204 A 3350 BULB BOEING 727 72751C 1384015 NM CABIN LOOSE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 903UP 18945 INSPECTION TYPE: EMERGENCY EXIT LIGHT OVER DOOR FLICKERING ON AND OFF WHEN CHECKED. FOUND LAMP LOOSE, TIGHTENED. OPS CHK O.K. 2 L 7 3 4F A3WE 1996121200033 19961212 00033 NM 1996 12 12 UPS96421705 1 19961121 A 5320 DOUBLER BOEING 747 747123 1384873 NM BS 310 MISINSTALLED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C. EXISTING REPAIR INCORRECT. INSTALLED ACC. EO B747-5330-1431C APPX 9.6 STEP 4 AND APPX. 8.5 STEP 2 AT BS 310 STR 8A LT. INSTALLED DOUBLER AT BS 310 STR 8A LT ACC TO EO B747-5330-1431 APPX. 8.5 AND APPX. 8.6. 2 L 7 4 4F A20WE 1996121200034 19961212 00034 NM 1996 12 12 UPS96421706 1 19961127 A 5730 SKIN BOEING 747 747123 1384873 NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C. FOUND CORROSION BETWEEN THE UPPER FRONT SPAR CHORD AND UPPER WING SKIN AT RT ILES 847.50. REMOVED FASTENERS ON WING SKIN ACC. SRM 51-30-02. REMOVED CORROSION ON WING SKIN ACC. SRM 51-10-01 WING SKIN OUT OF LIMITS ACC . SRM 57-30-01 FIG. 1. REPAIRED WING SKIN ACC KLM DFX 96-241. APPROVED PER UPS EFN 747-57-0347. 2 L 7 4 4F A20WE 1996121200035 19961212 00035 NM 1996 12 12 UPS96421707 1 19961129 A 5320 PLATE BOEING 747 747123 1384873 NM BS 140 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C. FOUND WEB FLOOR STRUCTURE PLATE CRACKED AT BS 140 LBL 40. REPAIRED WEB FLOOR STRUCTURE PLATE BETW EEN BS 140 AND 150 LBL. 40 ACC. SRM 51-40-02. 2 L 7 4 4F A20WE 1996121200036 19961212 00036 NM 1996 12 12 UPS96421708 1 19961121 A 5320 CHORD BOEING 747 747123 1384873 NM BS 220 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C. FOUND CORROSION ON UPPER CHORD AT BS 220 AT LBL 59. REMOVED CORROSION ON UPPER CHORD ON BS 220 LB L 59 ACC. SRM 51-10-01. CORROSION NOT IN LIMITS ACC. SRM 53-10-01. REPAIRED UPPER CHORD FROM LBL 58 TO LBL 82 ACC. SRM 53-10-07 FIG. 8. 2 L 7 4 4F A20WE 1996121200037 19961212 00037 NM 1996 12 12 UPS96421710 1 19961125 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM BS 220-250 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C. FOUND CORROSION ON SEAT RACK ON BS 220 TO BS 250 AT RBL 52. REMOVED CORROSION AT SEAT TRACK ON B S 220 TO BS 250 AT RBL 52 ACC SRM 51-10-01 CORROSION NOT IN LIMITS ACC. SRM 53-10-01. REPAIRED SEAT TRACK FROM BS 210 T O BS 290 ACC. SRM. 53-10-05 FIG. 1. 2 L 7 4 4F A20WE 1996121200038 19961212 00038 NM 1996 12 12 UPS96421711 1 19961121 A 5320 WEB BOEING 747 747123 1384873 NM BS 280 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C. CORROSION BETWEEN WEB AND FLOOR BEAM UPPER CHORD AT BS 280 BETWEEN RBL 20 AND LBL 20. CORROSION ON WEB AT LBL 10 OUT OF LIMITS AFTER REWORK. REPAIRED I.A.W. SRM 51-40-02 FIG. 1. 2 L 7 4 4F A20WE 1996121200039 19961212 00039 NM 1996 12 12 UPS96421712 1 19961121 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM BS400/440 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C. SEAT TRACK RBL 11.33 CORRODED AT BS 400 AND BS 440. REPAIRED SEAT TRACK AT BS 370 TO BS 410 RBL 1 1.33 ACC. SRM 53-10-05 FIG. 1. 2 L 7 4 4F A20WE 1996121200040 19961212 00040 NM 1996 12 12 UPS96421713 1 19961121 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM BS 460 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C. SEAT TRACK CORRODED AT BS 460 AT RBL 90. REMOVED CORROSION ON SEAT TRACK ACC. SRM 510-10-01. COR ROSION NOT IN LIMITS ACC. SRM 53-10-01. REPAIRED SEAT TRACK FROM BS 410 TO BS 460 AT RBL 90 ACCORDING SRM 53-10-05. 2 L 7 4 4F A20WE 1996121200041 19961212 00041 NM 1996 12 12 UPS96421714 1 19961127 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM BS 440/475/500 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C. SEAT TRACK LBL 11.33 IS CORRODED AT BS 440, 475 AND 500. DAMAGE EXCEEDED ALLOWABLE LIMITS IAW SR M 53-10-01. REPLACED SEAT TRACK PARTLY FROM BS 390 TO BS 520 IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996121200042 19961212 00042 NM 1996 12 12 UPS96421715 1 19961128 A 5320 TRUSS FITTING BOEING 747 747123 1384873 NM BS 1880 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C. FOUND IN AFT CARGO COMP. THE FWD TRUSS FITTING CRACKED IN THE EDGE FROM LATCH SUPPORT STRUCTURE P OS. NR 14. REPLACED BOTH LATCH SUPPORT AND TRUSS FITTINGS ACC. EO B747-5340-0191A APPX. D AT POS. NR 14 (INSTALLED/REPL ACED PER TOPKIT 63B12792-13). 2 L 7 4 4F A20WE 1996121200043 19961212 00043 NM 1996 12 12 UPS96421716 1 19961126 A 5320 TRUSS FITTING BOEING 747 747123 1384873 NM BS 650 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C. FWD CARGO COMP. LOWER DOORWAY SILL. FOUND TYPE 'B' CRACK IN LOWER FLANGE OF FWD TRUSS FITTING OF POS. NR 7 LATCH SUPPORT FITTING. REPLACED BOTH LATCH SUPPORT AND TRUSS FITTINGS P/N TOPKIT 63B12792-20 ACC. EO B747-534 0-0191 APPX. D AT POS NR 7. 2 L 7 4 4F A20WE 1996121200044 19961212 00044 NM 1996 12 12 UPS96421717 1 19961125 A 5315 FLOOR BEAM BOEING 747 747123 1384873 NM BS 380 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C. SEVERAL SMALL HOLES DRILLED IN FLOOR BEAM UPPER CHORD AT BS 380 BETWEEN LBL 61 AND LBL 81. REPAIR ED FLOOR BEAM UPPER CHORD ON BS 580 BETWEEN LBL 61 AND LBL 81 ACCORDING SRM 51-40-04 FIG.1. 2 L 7 4 4F A20WE 1996121200045 19961212 00045 NM 1996 12 12 UPS96421718 1 19961125 A 5320 SHEAR TIE BOEING 747 747123 1384873 NM BS 1540 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C. FRAME TO SKIN SHEAR TIE BS 1540 HAS EDGE CRACK BETWEEN STR 21 AND 23 LT. REPLACED SHEAR TIE AT BS 1540 STR 21 AND STR 23 LT ACC SRM 51-30-02. 2 L 7 4 4F A20WE 1996121200046 19961212 00046 NM 1996 12 12 UPS96421719 1 19961128 A 5311 FRAME BOEING 747 747123 1384873 NM BS 1660 SEVERED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C. FUSELAGE FRAME BS 1660 IS 75 PERCENT SEVERED BETWEEN STR 13 AND 14 LT. REPLACED FRAME AT BS 1660 LT FROM STR 13 TO STR 17 ACCORDING SRM 51-30-02 AND SIM 65B01777-401. 2 L 7 4 4F A20WE 1996121200047 19961212 00047 NM 1996 12 12 UPS96421720 1 19961121 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C. MED NR 5 LT FWD FRAME WEB CRACKED WL 250 APPROX. REPLACED FRAME WEB AT MED 5 LT WL 250 APPROX. AC CORDING SRM 51-30-02. 2 L 7 4 4F A20WE 1996121200048 19961212 00048 NM 1996 12 12 UPS96421721 1 19961121 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C. MED 5 RT FORWARD FRAME WEB CRACKED WL 250 APPROX. REPLACED WEB AT MED 5 RT WL 250 APPROX. ACCORDI NG SRM 51-30-02. 2 L 7 4 4F A20WE 1996121200049 19961212 00049 NM 1996 12 12 UPS96421722 1 19961125 A 5320 SHEAR TIE BOEING 747 747123 1384873 NM BS 1540 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C. AT BS 1500 AND 1540 SHEAR TIE CRACKED BETWEEN STR 21/22 RT. REPLACED SHEAR TIE AT BS 1500 AND 1 540 BETWEEN STR 21/22 RT ACC. SRM 51-30-02. 2 L 7 4 4F A20WE 1996121200050 19961212 00050 NM 1996 12 12 UPS96421723 1 19961125 A 5320 SHEAR TIE BOEING 747 747123 1384873 NM BS 1060 BENT A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C. FOUND SHEAR TIE BENT AT BS 1060 BETWEEN STR 2 AND 3 RT. REPAIRED SHEAR TIE AT BS 1060 AT STR 2 A ND 3 RT, ACCORDING SRM 51-20-01. 2 L 7 4 4F A20WE 1996121200051 19961212 00051 NM 1996 12 12 UPS96421724 1 19961128 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM BS 990 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C. MAIN DECK INTERIOR BS 990 RBL 98 SEAT TRACK CORRODED/CRACKED. REPAIRED SEAT TRACK FROM BS 990 TO 1070 RBL 98 I.A.W. SRM 53-10-05 FIG. 34. 2 L 7 4 4F A20WE 1996121200052 19961212 00052 NM 1996 12 12 UPS96421725 1 19961119 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM BS 1000/1265 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C. MAIN DECK INTERIOR: BETWEEN BS 1000 AND BS 1265 RBL 33 SEAT TRACK CORRODED/CRACKED. CORROSION C RACKS EXCEEDING AND ALLOWABLE LIMITS I.A.W. SRM 53-10-01. REPLACED SEAT TRACK I.A.W. SRM 53-10-05 FIG.34. 2 L 7 4 4F A20WE 1996121200053 19961212 00053 NM 1996 12 12 UPS96421726 1 19961119 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM BS 1100 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C. MAIN DECK INTERIOR: BS 1100 RBL 11, SEAT TRACK CROWN DAMAGED. REPAIRED SEAT TRACK FROM BS 1090 T O BS 1110 AT RBL 11 ACC. SRM 53-10-05 FIG. 34. 2 L 7 4 4F A20WE 1996121200054 19961212 00054 NM 1996 12 12 UPS96421727 1 19961119 A 5730 65B01100 SKIN BOEING 747 747123 1384873 NM BS 1100 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C. EXTERIOR SURFACE OF WING CENTER SECTION UPPER SKIN BS 1100 RBL 93 SKIN CORRODED. REWORKED CORROSI ON IAW SRM 51-10-01. DAMAGE AFTER REWORK OUT-OF-LIMITS IAW SRM 57-30-01. REPAIRED CENTER WING UPPER SKIN IAW DFX 96-24 3/EFN 747-57-0346 AND REF. UPS-AMS-96-0262RE. 2 L 7 4 4F A20WE 1996121200055 19961212 00055 NM 1996 12 12 UPS96421728 1 19961119 A 5730 65B01100 SKIN BOEING 747 747123 1384873 NM BS 1100 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C. EXTERIOR SURFACE OF WING CENTER SECTION UPPER SKIN BS 1100 RBL 117 SKIN CORRODED. REWORKED CORROS ION IAW SRM 51-10-01. DAMAGE AFTER REWORK OUT-OF-LIMITS IAW SRM 57-30-01. REPAIRED CENTER WING UPPER SKIN IAW KLM DFX 96-243/EFN 747-57-0346 AND REF. UPS-AMS-96-0262RE. 2 L 7 4 4F A20WE 1996121200056 19961212 00056 NM 1996 12 12 UPS96421730 1 19961119 A 5320 FILLER BOEING 747 747123 1384873 NM BS 1240 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C. CENTER SECTION UPPER SKIN: BS 1240 LT REAR SPAR UPPER SPLICE PLATE FILLER CORRODED. REMOVED CORR OSION AT BS 1240 LT REAR SPAR UPPER SPLICE FILLER ACC. SRM 51-10-01, OUT-OF-LIMITS ACC. SRM 53-10-01. REPLACED FILLER A CC. SRM 51-10-10. 2 L 7 4 4F A20WE 1996121200057 19961212 00057 NM 1996 12 12 UPS96421731 1 19961121 A 5210 65B0989217 GATE ASSY BOEING 747 747123 1384873 NM MED 5 LT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C. FOUND LOWER GATE OF DOOR 5 LT CORRODED. DAMAGE EXCEEDED ALLOWABLE LIMITS IAW SRM 52-00-02. REPLA CED LOWER GATE OF DOOR 5 LT IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996121200058 19961212 00058 NM 1996 12 12 UPS96421732 1 19961121 A 5312 015U040020 BULKHEAD CHORD BOEING 747 747123 1384873 NM BS 1000 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C. FWD CARGO COMPARTMENT: AFTER HFEC INSPECTION, FOUND BULKHEAD CHORD STA 1000 CRACKED BETWEEN STR 4 6/47 RT, CRACK LENGTH APPROX. 40MM. REPLACED LWR CHORD SEGMENT AT BS 1000 ACC. EO B747-5310-5301-E PER SALES ORDER NR 69494-20. 2 L 7 4 4F A20WE 1996121200059 19961212 00059 NM 1996 12 12 UPS96421735 1 19961126 A 5311 FRAME BOEING 747 747123 1384873 NM BS 980 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE: C. FOUND DURING REPLACEMENT OF BSTA 1000 LOWER CHORD (EO B747-5310-5301E) CORROSION ON WEB OF FRAME B STA 980 NEAR STR 46 LT AFT SIDE OF FRAME. CORRODED PART OF WEB IS OUT OF LIMITS ACC. SRM 53-10-01 ITEM 1 NOTE B. REMOV ED CORRODED PART OF WEB, CUT OUT IS 2 SQUARE INCH. REPAIRED FRAME ACC. SRM 53-10-04 FIG. 52 DETAIL 2. 2 L 7 4 4F A20WE 1996121200060 19961212 00060 NM 1996 12 12 UPS96621709 1 19961130 A 7830 THRUST REVERSER BOEING 767 76734AF 1385212 NM RT ENGINE MALFUNCTIONED A IPXA O OTHER O OTHER LD LANDING 1 SO 01 304UP 27242 LANDED 6R. BRAKING ACTION FAIR TO POOR. AFTER SLOWING TO TAXI SPEED, CAME OUT OF REVERSE. RT REVERSER DID NOT STOW. A DVANCED THROTTLES TO MAINTAIN SPEED. LOST DIRECTIONAL CONTROL, STAYED ON RUNWAY, NO DAMAGE. IT WAS NECESSARY TO BE TOW ED DUE TO SLICK SURFACES. RESET REVERSER RELAY MODULE. RAN RT ENG, DEPLOYED REVERSER SEVERAL TIMES. OPS CHECK NORMAL. 2 L 7 2 4F RT A1NM 1996121200061 19961212 00061 WP 1996 12 12 UPS96821734 1 19961201 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 597 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 LT WING - 2.50 INCH CRACK IN LOWER SURFACE OF LEADING EDGE SKIN - STA XFS 597.000, OTBD OF NR 1 PYLON. STOP DRILLED CRA CKS (26700/QC15650). FABRICATED DOUBLER AND INSTALLED SAME PER EO NR DC8-5720-4087. 2 L 7 4 4F RT 4A25 1996121200062 19961212 00062 WP 1996 12 12 MWEA96644 1 19961204 A 3397 WIRE DOUG DC9 DC914 3022034 WP CABIN BROKEN A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 500ME 45711 DURING SERVICE CHECK, FOUND BROKEN WIRE ON LAST RED LIGHT ON EMERGENCY FLOOR TRACK LIGHTING -- MAINTENANCE REPAIRED WI RE AND PERFORMED OPS CHECK IAW DAC MM 33-50-00 RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996121200063 19961212 00063 NM 1996 12 12 SCNA96402 1 19961202 A 3260 SENSOR BOEING 727 7272J4 1384006 NM NLG INTERMITTENT A SCNA O OTHER N FALSE WARNING CL CLIMB 1 GL 15 285SC 21676 ON GEAR RETRACTION, NOSE GEAR RED WARNING LIGHT REMAINED ON, RECYCLED GEAR AND OPS NORMAL. CLEANED NOSE GEAR POSITION A ND LOCK SWITCHES, SWUNG NOSE GEAR AND OPS CHECKED NORMAL. 2 L 7 3 4F RT A3WE 1996121200064 19961212 00064 1996 12 12 P5CA9600977 4 19961204 A 3414 A4321710002 AIR SPEED IND BOEING 747 747123 1384873 NM COCKPIT MALFUNCTIONED A P5CA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 WP 23 858FT 20109 CAPTAIN'S AIR SPEED INDICATOR FROZE AT 70 KNOTS INDICATED AIR SPEED DURING TAKEOFF ABORTED TAKEOFF AT APPROXIMATELY 90 T O 100 KNOTS INDICATED AIR SPEED. REMOVED AND REPLACED CAPTAIN'S AIR SPEED INDICATOR PER MAINTENANCE MANUAL 34-13-05. O PERATIONAL CHECK OK, NO LEAKS. FOUND PER MAINTENANCE MANUAL 34-11-00. 2 L 7 4 4F A20WE 1996121200065 19961212 00065 NM 1996 12 12 P5CA9600978 1 19961201 A 5400 RIVET BOEING 747 747132 1384882 NM NR 3 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 CRACKED RIVET ON LOWER SLOT SEAL (NACELLE STATION 180 WATER LINE 124) RIGHT SIDE NR 3 PYLON. REPLACED RIVET PER BOEING SRM 51-30-02. 2 L 7 4 4F A20WE 1996121200066 19961212 00066 SO 1996 12 12 SRAA961083 1 19961013 A 5320 SUPPORT BEAM LKHEED 382 382G 526414U SO BS 297O CORROSION A SRAA K NONE O OTHER IN INSP/MAINT 1 GL 23 905SJ 45318 4472 DURING C-CHECK FOUND CARGO COMPARTMENT FLOOR PANEL SUPPORT BEAM AT FS 297OE, BL ZERO HAS CORROSION AT FORWARD AND AFT SI DE OF UPPER CAP BEYOND LIMITS. CUT OUT CORRODED SECTION, FABRICATED AND INSTALLED NEW FILLER L-ANGLE AND STRAP IAW LAC SRM CHAPTER 51-140-22. 2 H 7 4 4T A1SO 1996121200067 19961212 00067 WP 1996 12 12 SRAA961118 1 19961129 A 7931 12584 SWITCH DOUG DC8 DC873F 302199F WP NR 4 ENGINE DEFECTIVE A SRAA A E J UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL N FALSE WARNING CL CLIMB 1 GL 23 873SJ 46091 ON CLIMB-OUT OF SHANHAI ON FLIGHT 7875, NR 4 ENGINE OIL PRESSURE LIGHT CAME ON. SHUT DOWN NR 4 ENGINE AS PRECAUTIONARY, DUMPED FUEL AND LANDED AT HKG WITHOUT INCIDENT. INSPECTED OIL FILTER, NO CONTAMINATION FOUND, SUSPECT OIL PRESSURE DIF FERENTIAL SWITCH AT FAULT, DEFERRED SWITCH PER MEL 79-7. UNIT WAS REPLACED AT SIN, SYSTEM OPS CHECKED GOOD PER M.M. CH 79. 2 L 7 4 4F RT 4A25 1996121200068 19961212 00068 SO 1996 12 12 SRAA961081 1 19961013 A 5320 ANGLE LKHEED 382 382G 526414U SO BS 507 CRACKED A SRAA K NONE O OTHER IN INSP/MAINT 1 GL 23 905SJ 45318 4472 DURING C-CHECK, FOUND A 2 INCH CRACK AT ACCESS PANEL SUPPORT ANGLE IN UPPER LEFT MLG WHEELWELL O/B SIDE OF WL 200, FS 50 7. CUT OUT CRACKED AREA, FABRICATED A FILLER TO EXISTING DOUBLER IAW LAC SRM 51-70-01, 53-60-02 AND 51-140-02. 2 H 7 4 4T A1SO 1996121200099 19961212 00099 SO 1996 12 12 96ZZZX5904 2 19961119 A 8500 ENGINE PIPER PA34 PA34200T 7103406 SO CONT O360 TSIO360EB 17025 SO RT ENG ROUGHNESS A A C2SA A UNSCHED LANDING E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CL CLIMB 1 CE 01 24KG 348070309 312526 UPON ROTATION, ENGINE ROUGHNESS WAS NOTED BY PILOT. TOWER REPORTED SMOKE FROM RIGHT ENGINE. LANDING PATTERN WAS ENTERE D IMMEDIATELY, AND UNEVENTFUL LANDING MADE. MAINTENANCE COULD NOT DUPLICATE PROBLEM ON GROUND. RUN-UPS AND ENGINE INSP ECTIONS SHOWED NO VISUAL EXTERNAL DEFECTS. MAINTENANCE INVESTIGATIONS ARE CONTINUING INTO THE PROBLEM. OCCURRED NOV 19 , 1996. 1 L 7 2 3O 3 O A7SO E9CE 1996121200103 19961212 00103 CE 1996 12 12 96ZZZX5909 1 19961119 A 3231 08411065 BELLCRANK CESSNA 310 310R 2074245 CE MLG BROKEN A CWTA K NONE O OTHER IN INSP/MAINT 1 GL 05 3291M 5144 310R1896 INSP FOUND INNER GEAR DOOR NOT CLOSED. FURTHER INSP REVEALED GEAR DOOR BELLCRANK BROKEN AT CURVE. 1 L 7 2 3O 3A10 1996121200114 19961212 00114 NM 1996 12 12 96ZZZX5914 1 19960823 A 5315 652083830 FLOOR BEAM BOEING 727 727251 138408H NM BS 1130 CORROSION B EF2R K NONE O OTHER IN INSP/MAINT 1 SW 05 280US 21159 FS 1130 FLOOR BEAM LOWER CAP HAS HEAVY CORROSION ON LBL 50 INCH TO RBL 60 INCH INSIDE AFT BAG BIN. REPAIRED FLOOR BEAM PER DALFORT AVIATION XEA NR X1-53-689, REVISION 1. 2 L 7 3 4F A3WE 1996121200115 19961212 00115 NM 1996 12 12 TAOA109608 1 19961011 A 5530 651680221 FITTING BOEING 727 727227 1384078 NM VERT STAB EXCEEDED LIMITS A TAOA K NONE O OTHER IN INSP/MAINT 1 EA 15 926TS 20774 DURING D-CHECK, THE VERTICAL STABILZIER TENSION TIES REQUIRED REWORK ACCORDING TO BOEING SB 55-0071. THE REWORK DIMENSI ONS SET FORTH EXCEEDED THE SB LIMITS. REWORK DIMENSIONS WERE APPROVED BY BOEING. (X) 2 L 7 3 4F A3WE 1996121200116 19961212 00116 NM 1996 12 12 TAOA109609 1 19961018 A 7931 42D107A2 SWITCH BOEING 727 727227 1384078 NM NR 3 ENG OIL FAILED A TAOA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 EA 15 926TS 2962 20774 NR 3 ENGINE LOW OIL PRESSURE/FILTER BYPASS LIGHT CAME ON. FOLLOWED ABNORMAL CHECKLIST NO HELP. ENGINE SHUT DOWN AS A P RECAUTION. OIL PRESSURE STAYED AT 15 PLUS PSI AFTER SHUT DOWN. CHECKED MAIN ENGINE OIL FILTER-CHECKS OK. REPLACED OIL FILTER AND REPLACED NR 3 LOW OIL PRESSURE SWITCH, LEAK AND OPS CHECK OK PER MM CHAPTER 79-33-0 AND MM CHAPTER 79-33-01. (X) 2 L 7 3 4F A3WE 1996121200117 19961212 00117 CE 1996 12 12 96ZZZX5915 1 19960719 A 2130 1304061 SAFETY VALVE LEAR 24 24D 5170311 CE CABIN CRACKED A MFGA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 11 249RA 2219 249 THE AIRCRAFT WAS AT 41,000 FEET WHEN IT HAD A LOSS OF CABIN PRESSURIZATION. THE CABIN WAS CLIMBING AT A RATE OF 800 FEE T PER MINUTE. THE FLIGHT CREW DESCENDED THE AIRCRAFT TO AN ALTITUDE OF 8,000 FEET AND PROCEEDED TO THE DESTINATION. UP ON INSPECTION OF THE OUTFLOW AND SAFETY VALVE P/N 130406-1, IT WAS FOUND THAT THE SAFETY VALVE HAS CRACKED. BOTH THE SA FETY AND OUTFLOW VALVE ARE RESTRICTED TO 41,000 FEET BY AD-95-20-03, SUPERSEDES (94-26-01). 2 L 7 2 4J A10CE 1996121200118 19961212 00118 EU 1996 12 12 96ZZZX5916 1 19961005 A 3350 CONNECTOR STBROS SD3 SD360 8100606 EU CABIN LOOSE A GUUA K NONE L NO TEST IN INSP/MAINT 1 SO 19 262GA SH3749 AT SCHEDULED MAINTENANCE VISIT, DETERMINED EMERGENCY FLOOR LIGHT AT ROW 10 TO BE INOPERATIVE. RESECURED CONNECTOR, OPER ATIONAL CHECK SATISFACTORY. 2 H 7 2 4T A41EU 1996121200119 19961212 00119 EU 1996 12 12 96ZZZX5917 1 19961020 A 5330 SKIN STBROS SD3 SD360 8100606 EU BS 186.5 DAMAGED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 262GA SH3749 ON PRE-FLIGHT INSPECTION FOUND GROUND EQUIPMENT DAMAGE OF THE RIGHT FUSELAGE AT STA 186.5. REMOVED DAMAGED AREA, INSTAL LED INNER CORREGATED SKIN AND OUTER SKIN DOUBLERS PER THE SRM. 2 H 7 2 4T A41EU 1996121200120 19961212 00120 WP 1996 12 12 96ZZZX5918 1 19961003 A 3350 0105602001 LIGHT DOUG DC9 DC983 3022083 WP CABIN BROKEN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9414W 53189 STL - FLT 202 - DURING OVERNIGHT INSPECTION EGRESS LIGHTING TRACK FOUND BROKEN WITH EXPOSED WIRING, MFG P/N 0105602-001, AT SEAT ROW 33. REPLACED LIGHT TRACK. EGRESS LIGHT SYSTEM OPERATION CHECKED NORMAL. CHECK C - 10-5-95 - NEW AIRCRAFT . 2 L 7 2 4F RT A6WE 1996121200121 19961212 00121 WP 1996 12 12 96ZZZX5919 1 19961003 A 3350 0105607301 LENS DOUG DC9 DC983 3022083 WP CABIN MISSING A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9414W 53189 STL - FLT 202 - DURING PRE-FLIGHT EGRESS LIGHTING RED LENS AT SEAT ROW 31 INOPERATIVE AND MISSING. REPAIRED RED LENS, M FG P/N 0105607-301, AND REPLACED COVER, MFG P/N 008PA57. EGRESS LIGHT SYSTEM OPERATION CHECKED NORMAL. CHECK C - 10-5- 95 - NEW AIRCRAFT. 2 L 7 2 4F RT A6WE 1996121200122 19961212 00122 NM 1996 12 12 96ZZZX5920 1 19961007 A 3397 210701979620 WIRE BOEING 747 747206B 1384856 NM CABIN OPEN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 306TW 20398 STL - FLT 1 - DURING PRE-FLIGHT, UPPER DECK EGRESS LIGHTS WERE INOPERATIVE. FOUND OPEN WIRE 21070-19796-20 TO CONNECTOR D3272J. ACCOMPLISHED AIRWORTHY REPAIR TO WIRING. EGRESS LIGHT SYSTEM OPERATION CHECKED NORMAL. CHECK C-1 - 4-13-96 - SBA. 2 L 7 4 4F RT A20WE 1996121200123 19961212 00123 WP 1996 12 12 AALA961443 1 19961002 A 3231 DOOR DOUG DC9 DC982 3022082 WP NLG LACK OF LUBE A AALA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SW 07 223AA 49173 LAX - FLT 0550 - AFTER TAKEOFF LAX WHEN LANDING GEAR RETRACTED, VIBRATION NOTED FROM AREA OF NOSE LANDING GEAR. EXTENDE D LANDING GEAR AND AIRCRAFT RETURNED TO LAX, LANDING WITHOUT INCIDENT. LT NOSE LANDING GEAR DOOR FOUND OPEN AT GATE ARR IVAL. CHECKED ALL NOSE LANDING GEAR DOOR LINKAGE AND LATCHING MECHANISM WITH NO DEFECTS FOUND. PRECAUTIONARY LUBRICATE D GEAR DOOR HINGES AND ACTUATOR. ACCOMPLISHED NOSE LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1996121200124 19961212 00124 WP 1996 12 12 ORJA9668 1 19961011 A 3397 WIRE DOUG DC9 DC987 3022087 WP CABIN FAILED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 753RA 49587 EMERGENCY EXIT TRACK LIGHT OUT AT SEAT ROW 22. REPAIRED WIRING. OPS GOOD. (X) 2 L 7 2 4F RT A6WE 1996121200125 19961212 00125 WP 1996 12 12 ORJA9659 1 19960927 A 3350 60030431 POWER PACK DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 881RA 15831 49941 EMERGENCY LIGHTS BATTERY LOW. REPLACED FORWARD EMERGENCY-LIGHT POWER SUPPLY PER MD-80 MM. OPS CHECK GOOD. (X) 2 L 7 2 4F RT A6WE 1996121200126 19961212 00126 WP 1996 12 12 ORJA9671 1 19961022 A 3350 670030431 POWER PACK DOUG DC9 DC983 3022083 WP COCKPIT INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 881RA 15831 49941 COCKPIT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPlaCED BATTERIES TO COCKPIT OVERHEAD EMERGENCY-LIGHT BATTERY PACK. OP S NORMAL. (X) 2 L 7 2 4F RT A6WE 1996121200127 19961212 00127 NM 1996 12 12 ORJA9660 1 19960927 A 3260 INDICATION DOUG MD90 MD9030 3023690 NM NLG MALFUNCTIONED A ORJA O OTHER N FALSE WARNING AP APPROACH 1 WP 11 903RA 53551 NOSE LANDING GEAR GREEN LIGHT DID NOT COME ON UNTIL THE FOURTH ATTEMPT TO LOWER GEAR; EVEN TRIED EMERGENCY GEAR LEVER. N OSE LANDING GEAR INDICATOR ONLY CAME UP 2/3 UNTIL GEAR FINALLY LOCKED DOWN ON FOURTH TRY. INSTALLED BOTH LEFT AND RIGHT MAIN LANDING GEAR LOCK PINS. PERFORMED GEAR SWING PER MM 07-11-00. NO DEFECTS NOTED; OPS NORMAL. REMOVED BOTH LEFT A ND RIGHT MAIN LANDING GEAR LOCK PINS AND STOWED LOCK PINS IN COCKPIT. (X) 2 L 7 2 4F RT A6WE 1996121200128 19961212 00128 EU 1996 12 12 SIMA962861 1 19961012 A 3350 F1AL250W FUSE AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 233RM 235 ORD - FLT 42886 - SEVERAL EMERGENCY EGRESS FLOOR LIGHTS INOPERATIVE. REPLACED FUSE IN POWER SUPPLY 3WL. OPS CHECK GOOD . AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1996121200130 19961212 00130 NM 1996 12 12 GAIA9625 1 19960924 A 3350 LIG5192 BATTERY PACK BOEING 727 727223 1384074 NM COCKPIT DISCHARGED A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 855AA 20996 COCKPIT EMERGENCY EXIT LIGHT BATTERY PACK FOUND DEAD DURING 'PS' CHECK. THE LIGHT ASSEMBLY WAS CHANGED, OPS CHECKED AND SIGNED OFF. (X) 2 L 7 3 4F A3WE 1996121200131 19961212 00131 NM 1996 12 12 W8PA960146 1 19961003 A 3350 20131A BATTERY BOEING 737 7373S3 1384711 NM CABIN DISCHARGED A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 375TA 18903 23787 FLOOR TRACK LIGHTING INOP FROM ROWS 14 THROUGH 20. REMOVED AND REPLACED BATTERY ASSY. (X) 2 L 7 2 4F RT A16WE 1996121200132 19961212 00132 CE 1996 12 12 NSVA96004 1 19961028 A 2510 6226200002 CONTROL PANEL COLLINS HCP74 BEECH 1900 1900C 1154161 CE CONSOLE SHORTED A NSVA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 27 129CJ 1741 UC129 EN ROUTE, SMOKE WAS OBSERVED COMING FROM CENTER CONSOLE. EXECUTED EMERGENCY PROCEDURES FOR SMOKE IN THE COCKPIT. DECLA RED EMERGENCY AND EXECUTED AN UNEVENTFUL LANDING. PRIOR TO LANDING, THE SOURCE OF SMOKE CEASED AND THE SMOKE DISSIPATED . (X) 2 L 7 2 4T RT A24CE 1996121200134 19961212 00134 CE 1996 12 12 96ZZZX5923 1 19961005 A 3610 19357222 O-RING BEECH 1900 1900D 1154162 CE LT WING CRACKED A AMWA O OTHER J WARNING INDICATION CR CRUISE 1 CE 07 233YV 254 UE233 FLT 5636 - LT BLEED AIR FAIL LIGHT CAME ON IN-FLIGHT. MAINTENANCE FOUND FOUR SEALS BRITTLE AND CRACKED BETWEEN FUSELAGE AND ACM WHICH MELTED HOLE IN EVA TUBING. AIRCRAFT TOTAL TIME 254 HOURS. 2 L 7 2 4T RT A24CE 1996121200135 19961212 00135 1996 12 12 96ZZZX5924 3 19960912 A 6112 4E259810 DEICE BOOT SWRNGN SA227 SA227AC 8780603 SW RT PROPELLER LOOSE A SWHA K NONE E VIBRATION/BUFFET CR CRUISE 1 SW 17 373PH 22017 63 AC538 ON SCHEDULED FLIGHT 103, FROM AUS TO CRP, THE CREW NOTICED A SLIGHT VIBRATION. IT WAS DETERMINED THAT IT WAS MOST LIKEL Y COMING FROM THE RT ENGINE. ALL ENGINE PARAMETERS WERE NORMAL AND THE FLIGHT CONT. DURING THE POST-FLIGHT INSPECTION, THE CREW FOUND THAT APPROXIMATELY 6 INCHES OF ONE DE-ICE BOOT, ON THE RT PROPELLER HAD COME LOOSE FROM THE BLADE. THE AIRCRAFT WAS FERRIED TO AUS. THE DE-ICE BOOT WAS REPLACED AND OPERATIONAL CHECKED SATISFACTORY. THE AIRCRAFT WAS RETUR NED TO SERVICE. 2 L 7 2 4T RT A8SW 1996121200136 19961212 00136 NM 1996 12 12 GAIA9628 1 19961020 A 3350 1000679 LIGHT BOEING 727 727223 1384074 NM L1 DOOR INOPERATIVE A GAIA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 07 855AA 20996 PORTABLE EMERGENCY LIGHT AT MAIN ENTRY DOOR WILL NOT ALWAYS COME ON WHEN MAIN ARM SWITCH IS ON. REMOVED AND REPLACED EM ERGENCY EXIT LIGHT ASSY. (X) 2 L 7 3 4F A3WE 1996121200137 19961212 00137 WP 1996 12 12 GAIA9626 1 19960924 A 5230 726430B RELAY CVAC 640 640340D 2422814 WP BELLY COMPT STUCK A GAIA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 07 860FW 10 FLT 484 - ON APPROACH INTO PIT, FLIGHT CREW NOTED SMOKE IN COCKPIT BRINGING THE GEAR UP OR DOWN, BUT GOES AWAY IN-FLIGHT . AFTER LANDING IN PIT, THE FLIGHT CREW NOTED THE RELAY FOR THE CARGO DOOR HYDRAULIC POWER PACK HAD STUCK IN THE CLOSED POSITION ALLOWING THE HYDRAULIC PUMP MOTOR TO REMAIN ON AND OVER HEAT. A NEW LEACH RELAY P/N 7264-30B AND HYDRAULIC PO WER PACK P/N 7-1261-5, WAS INSTALLED, NO OTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A793 1996121200138 19961212 00138 SO 1996 12 12 96ZZZX5925 2 19961014 A 8520 629726A3 CAMSHAFT CESSNA 310 310R 2074245 CE CONT O520 IO520M 17032 SO RT ENGINE BROKEN A OVEA E ENGINE SHUTDOWN K T Z FLUID LOSS ENGINE CASE PENETRATION SIGNIFICANT FAILURE REPORT AP APPROACH 1 NE 05 87397 1595 310R0545 565546 PWN/AUG - FLT 32 - INBOUND, FLT CREW NOTICED FUEL FLOW FLUCTUATING, THEN PROP (RT ) FEATHERED. OIL OBSERVED COMING FROM INBD NOSE COWLING . UNEVENTFUL LANDING MADE AT AUG. INSP FND GOV DAMAGED, LT NOSE CASE FROM GOV PAD TO NR 6 CYL BROKE N AWAY. CAMSHAFT FND BROKEN BETWEEN NR 2 AND 4 CYLS AND NR 6 CYL CONNECTING ROD BROKEN. CAUSE PENDING TEAR-DOWN REPORT . APPROVED TBO 1700 HRS. TCM TEAR-DOWN REPORT FND NR 6 CYL HAD HYDROSTATIC LOCKING, BUCKLING CONNECTING ROD CAUSING IT TO FRACTURE IN FATIGUE. ALL DAMAGE OBSERVED TO HSI ENG WAS RESULT OF CONNECTING ROD SEPARATION, THE ENG DISREGARDING D AMAGE BY CONNECTING ROD, APPEARED NORMAL IN EVERY ASPECT. OPER IS TRAINING FLT CREWS. REF: OPER CNTRL NR 96ZZZX5926. 1 L 7 2 3O 3 O 3A10 E5CE 1996121200139 19961212 00139 SO 1996 12 12 96ZZZX5926 2 19961014 A 8520 632041F CONNECTING ROD CESSNA 310 310R 2074245 CE CONT O520 IO520M 17032 SO ENG NR 6 CYL BROKEN A OVEA E ENGINE SHUTDOWN K T Z FLUID LOSS ENGINE CASE PENETRATION SIGNIFICANT FAILURE REPORT AP APPROACH 1 NE 05 87397 1595 310R0545 565546 PWN/AUG - FLT 32 - INBOUND, FLT CREW NOTICED FUEL FLOW FLUCTUATING, THEN PROP (RT ) FEATHERED. OIL OBSERVED COMING FROM INBD NOSE COWLING . UNEVENTFUL LANDING MADE AT AUG. INSP FND GOV DAMAGED, LT NOSE CASE FROM GOV PAD TO NR 6 CYL BROKE N AWAY. CAMSHAFT FND BROKEN BETWEEN NR 2 AND 4 CYLS AND NR 6 CYL CONNECTING ROD BROKEN. CAUSE PENDING TEAR-DOWN REPORT . APPROVED TBO 1700 HRS. TCM TEAR-DOWN REPORT FND NR 6 CYL HAD HYDROSTATIC LOCKING, BUCKLING CONNECTING ROD CAUSING IT TO FRACTURE IN FATIGUE. ALL DAMAGE OBSERVED TO THIS ENG WAS RESULT OF CONNECTING ROD SEPARATION, THE ENG DISREGARDING DAMAGE BY CONNECTING ROD, APPEARED NORMAL IN EVERY ASPECT. OPER IS TRAINING FLT CREWS. REF: OPER CNTRL NR 96ZZZX5925. 1 L 7 2 3O 3 O 3A10 E5CE 1996121200140 19961212 00140 NM 1996 12 12 HNAA9699270 1 19961013 A 7712 311555701 TORQUE PROBE DHAV DHC8 DHC8201 2809001 NM NR 2 ENGINE FAILED A HNAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 07 992HA 896 MM0544 432 FLL/TPA - FLT 3438 - ON TAKEOFF ROLL, THE NR 2 AUTOFEATHER ACTIVATED. THE TAKEOFF WAS ABORTED AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED THE NR 2 ENGINE TORQUE PROBE AND TORQUE SENSOR CONTROL UNIT (TSCU). REF ERENCE: OPERATOR CONTROL NR 96ZZZX5927. (X) 2 H 7 2 4T RT A13NM 1996121200141 19961212 00141 NM 1996 12 12 96ZZZX5927 1 19961013 A 7712 30005000051 TSCU DHAV DHC8 DHC8201 2809001 NM NR 2 ENGINE FAILED A HNAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 07 992HA 31 MM4865 432 FLL/TPA - FLT 3438 - ON TAKEOFF ROLL, THE NR 2 AUTOFEATHER ACTIVATED. THE TAKEOFF WAS ABORTED AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED THE NR 2 ENGINE TORQUE PROBE AND TORQUE SENSOR CONTROL UNIT (TSCU). REF ERENCE: OPERATOR CONTROL NR HNAA9699270. 2 H 7 2 4T RT A13NM 1996121200142 19961212 00142 NE 1996 12 12 PCAA9600315 2 19960928 A 7321 7898426008 ELECT ENG CONTL DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 ENGINE MALFUNCTIONED A PCAA O OTHER O OTHER NR NOT REPORTED 1 EA 13 EICBJ 17067 054126 215 121144 NR 1 TORQUE GAUGE WENT FROM 92 PERCENT TO ZERO. POWER UPTRIM WAS CYCLING ON AND OFF. REMOVED AND REPLACED NR 1 ECU, TS CU, AND TORQUE PROBE. GROUND RUN AND TEST FLIGHT PROVED SATISFACTORY. A/C RETURNED TO SERVICE. REFERENCE: OPERATOR C ONTROL NR. 96ZZZX5928 AND 96ZZZX5929. (X) 2 H 7 2 4T 4 T RT A13NM E20NE 1996121200143 19961212 00143 NM 1996 12 12 96ZZZX5928 1 19960928 A 7712 3036774B TQ SIG COND UNIT DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 ENGINE MALFUNCTIONED A PCAA O OTHER O OTHER NR NOT REPORTED 1 EA 13 EICBJ 11377 003467 215 121144 NR 1 TORQUE GAUGE WENT FROM 92 PERCENT TO ZERO. POWER UPTRIM WAS CYCLING ON AND OFF. REMOVED AND REPLACED NR 1 ECU, TS CU, AND TORQUE PROBE. GROUND RUN AND TEST FLIGHT PROVED SATISFACTORY. A/C RETURNED TO SERVICE. REFERENCE: OPERATOR C ONTROL NR PCAA9600315 AND 96ZZZX5929. 2 H 7 2 4T 4 T RT A13NM E20NE 1996121200144 19961212 00144 NM 1996 12 12 96ZZZX5929 1 19960928 A 7712 311197801 TQ PROBE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 ENGINE MALFUNCTIONED A PCAA O OTHER O OTHER NR NOT REPORTED 1 EA 13 EICBJ 11A689 215 121144 NR 1 TORQUE GAUGE WENT FROM 92 PERCENT TO ZERO. POWER UPTRIM WAS CYCLING ON AND OFF. REMOVED AND REPLACED NR 1 ECU, TS CU, AND TORQUE PROBE. GROUND RUN AND TEST FLIGHT PROVED SATISFACTORY. A/C RETURNED TO SERVICE. REFERENCE: OPERATOR C ONTROL NR PCAA9600315 AND 96ZZZX5928. 2 H 7 2 4T 4 T RT A13NM E20NE 1996121200145 19961212 00145 EU 1996 12 12 96ZZZX5930 1 19960914 A 7603 8187 ACTUATOR AEROSP SA365 AS365N2 8680815 EU ENG CONT INOPERATIVE A ZYWA K NONE O OTHER IN INSP/MAINT 1 GL 09 365WM 1208 692 6429 PART IS INOPERATIVE. HAS LIMITED TRAVEL RANGE. REMOVED AND REPLACED ACTUATOR. 1 G 7 2 3U RT H10EU 1996121200146 19961212 00146 EU 1996 12 12 96ZZZX5931 1 19960520 A 2844 81071370010 TRANSMITTER AEROSP SA365 AS365N2 8680815 EU FUEL PRESS FLUCTUATES A ZYWA K NONE O OTHER IN INSP/MAINT 1 GL 09 365WM 952 481 6429 PRESSURE READING FLUCTUATES. REMOVE AND REPLACE TRANSMITTER. 1 G 7 2 3U RT H10EU 1996121200147 19961212 00147 EU 1996 12 12 96ZZZX5932 1 19960828 A 3340 34258M011 LIGHT AEROSP SA365 SA365N 8680669 EU ANTI COLL INOPERATIVE A ZYWA K NONE O OTHER IN INSP/MAINT 1 GL 09 365SJ 562 1573 6018 ANTI-COLLISION LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT. 1 G 7 2 3U H10EU 1996121200148 19961212 00148 EU 1996 12 12 96ZZZX5933 1 19961016 A 2436 D19035 REGULATOR AEROSP SA365 SA365N 8680669 EU DC SYS DEFECTIVE A ZYWA K NONE H ELECT. POWER LOSS-50 PC IN INSP/MAINT 1 GL 09 365SJ 3056 4496027 6018 NR 2 GEN FALLS OFF LINE. REMOVED AND REPLACED VOLT REG. 1 G 7 2 3U H10EU 1996121200149 19961212 00149 EU 1996 12 12 96ZZZX5934 1 19960917 A 2842 647600251 SWITCH AEROSP SA365 SA365N 8680669 EU FUEL SYS DEFECTIVE A ZYWA K NONE O OTHER IN INSP/MAINT 1 GL 09 365SJ 3053 6018 FLUSH Q LIGHT INTERMITTENT. REMOVED AND REPLACED FLUSH SWITCH. 1 G 7 2 3U H10EU 1996121200150 19961212 00150 EU 1996 12 12 96ZZZX5935 1 19961004 A 6320 4638001001 TRANSMISSION BOLKMS 105 BO105CBS 5626008 EU M/R MAKING METAL A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 105LC 4340 1872 1053 S789 TRANSMISSION REMOVED DUE TO METAL CONTAMINATION IN THE OIL. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H3EU 1996121200151 19961212 00151 NE 1996 12 12 96ZZZX5936 2 19961104 A 7200 400100025 ENGINE BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE RT NR 2 BEARING FAILED A R7MA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 11 71703 3985 976 7227 LE45549E PILOTS REPORT: WTH BOTH ENGINES AT GROUND IDLE AND ENGINE INDICATION NORMAL, ADVANCED THE POWER LEVERS SLIGHTLY PAST TH E GROUND IDLE POSITION WHEN A LOUD GRINDING NOISE WAS HEARD WITH RAPID N1 ACCELERATION, RISING TURBINE OUTLET TEMPERATUR E AND DECREASING N2 ON THE NR 2 ENGINE. EMERGENCY ENGINE SHUTDOWN PROCEDURES WERE PERFORMED AND THE MEDICAL CREW EXITED THE AIRCRAFT. SMOKE AND SPARKS WERE WITNESSED COMING FROM THE NR 2 ENGINE EXHAUST BY THE MEDICAL CREW. MECHANIC WAS N OTIFIED AND ASSESSED INTERNAL BEARING FAILURE. 1 G 7 2 3U 3 U H13EU E5NE10 1996121200152 19961212 00152 NE 1996 12 12 96ZZZX5937 2 19961104 A 7230 430151101 BEARING BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE NR 2 ENG FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 71703 976 42867 7227 LE45549E RT ENG NR 2 BEARING FAILED. 1 ROLLER REMAINS IMBEDDED WITHIN REMAINS OF BEARING CAGE. 1 G 7 2 3U 3 U H13EU E5NE10 1996121200153 19961212 00153 NE 1996 12 12 96ZZZX5938 2 19961104 A 7250 414144001 BEARING BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE NR 2 ENG DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 71703 976 42259 7227 LE45549E SECONDARY DAMAGE DUE TO NR 2 BEARING FAILURE. 1 G 7 2 3U 3 U H13EU E5NE10 1996121200154 19961212 00154 NE 1996 12 12 96ZZZX5939 2 19961104 A 7250 430124202 BEARING BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE RT ENG NR 3 DAMAGE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 71703 976 3901 7227 LE45549E SECONDARY DAMAGE DUE TO NR 2 BEARING FAILURE. 1 G 7 2 3U 3 U H13EU E5NE10 1996121200159 19961212 00159 NM 1996 12 12 AWXA9600724 1 19961201 A 3350 FUSE BOEING 737 73733A 1384673 NM CABIN BLOWN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 165AW 23626 DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS INOP ROW 1 TO 5. REPLACED FUSE IN POWER UNIT, LIGHTS FUNCTION NORMALLY. 2 L 7 2 4F RT A16WE 1996121200160 19961212 00160 NM 1996 12 12 AWXA9600725 1 19961202 A 3397 WIRE BOEING 757 7572S7 1384962 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 902AW 23322 DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT 31 A, B, C EMERGENCY LIGHT INOPERATIVE. RECONNECTED WIRING, OPERATIONS CHE CK GOOD. 2 L 7 2 4F RT A2NM 1996121200161 19961212 00161 NM 1996 12 12 AWXA9600726 1 19961203 A 3397 WIRE BOEING 757 7572G7 1384963 NM CABIN DISCONNECTED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 909AW 24522 DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT AT ROW 29 INOPERATIVE. RECONNECTED EMERGENCY LIGHT AT ROW 19, O PERATIONS CHECK GOOD. 2 L 7 2 4F RT A2NM 1996121200162 19961212 00162 NM 1996 12 12 AWXA9600727 1 19961204 A 3350 SWITCH BOEING 757 7572S7 1384962 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 902AW 23322 DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY TEST BUTTON ON FWD CSR SEAT INOPERATIVE. REMOVED AND REPLACED THE FWD ATTENDANT'S PANEL EMERGENCY LIGHT SWITCH, SYSTEM OPERATIONS CHECK NORMAL. 2 L 7 2 4F RT A2NM 1996121200163 19961212 00163 NM 1996 12 12 AWXA9600728 1 19961203 A 7711 LG80A6SERIES4 EPR TRANSMITTER BOEING 737 737277 1384570 NM NR 1 ENGINE MALFUNCTIONED A AWXA O OTHER N FALSE WARNING CR CRUISE 1 WP 28 185AW 22652 AFTER LEVEL OFF AT 28,000 AUTO THROTTLES ENGAGED, ENGINES INCREASED THRUST USING AUTO THROTTLE. NR 1 ENGINE EPR INCREA SED TO APPROX 2.15. DISCONNECTED AUTO THROTTLES, MATCHED UP N1'S THROTTLE SPLIT. NR 1 ENGINE APPROX 2.20, NR 2 EPR 1.8 5. UNABLE TO HOLD AIRSPEED WITH N1'S MATCHED, EMERGENCY DECLARED. REMOVED AND REPLACED EPR PT2 FLEX LINE UNDER DOG HOU SE, BLEW MOISTURE OUT OF EPR LINES. LEAK CHECK EPR SYSTEM, CHECK OK. REMOVED AND REPLACED NOSE DOME. RAN ENGINE. EPR SYSTEM CHECKS OK. REMOVED AND REPLACED NR 1 ENGINE EPR TRANSMITTER PER MM 77-11-21 AS PRECAUTION. 2 L 7 2 4F RT A16WE 1996121200164 19961212 00164 NM 1996 12 12 AWXA9600729 1 19961204 A 3350 SWITCH BOEING 757 7572S7 1384962 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 902AW 23322 DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY TEST BUTTON ON FORWARD CSR SEAT INOPERATIVE. REMOVED AND REPLACED THE FORWARD ATTENDENT'S PANEL EMERGENCY LIGHT SWITCH, SYSTEM OPERATIONS CHECKED NORMAL. 2 L 7 2 4F RT A2NM 1996121200165 19961212 00165 NM 1996 12 12 AWXA9600730 1 19961204 A 3397 WIRE BOEING 757 757225 1384959 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 914AW 22208 DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT EMERGENCY LIGHT OUT AT ROW 7. WIRE BROKEN AT FLOOR TRACK. REPAIRED WIRE, OPERATIONS CHECK GOOD,STC - SA3143NM. 2 L 7 2 4F RT A2NM 1996121200166 19961212 00166 NM 1996 12 12 RAAA96B2044 1 19961206 A 3350 GE81 LAMP BOEING 727 72722C 138400F NM CABIN FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 CENTER LEFT WING EXTERNAL EMERGENCY LIGHT FAILED SERVICE CHECK. REPLACED 2 LAMPS. 2 L 7 3 4F A3WE 1996121200167 19961212 00167 NM 1996 12 12 CALA9601726 1 19961105 A 5320 WEB BOEING 737 7372C0 1384488 NM BS 664 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73243 20072 INSPECTION FOUND A CRACK IN LT MLG WHEEL WELL UPPER PRESSURE WEB AT LT FORWARD CORNER JUST AFT OF STA 664. LENGTH OF CR ACK NOT IDENTIFIED. THE WEB WAS REMOVED AND A NEW PART WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-2, AND 53-10 -2, FIGURE 3. 2 L 7 2 4F A16WE 1996121200168 19961212 00168 NM 1996 12 12 CALA9601727 1 19961031 A 5320 SUPPORT BOEING 737 7372C0 1384488 NM BS 887 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73243 20072 INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 887, RBL 60. THE CORRODED AREA WAS REMOVED, REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-30-2, 51-10-2 AND 53-10-2. 2 L 7 2 4F A16WE 1996121200169 19961212 00169 NM 1996 12 12 CALA9601728 1 19961031 A 5230 SKIN BOEING 737 7372C0 1384488 NM CARGO DOOR CREASED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73243 20072 INSPECTION FOUND AFT CARGO DOOR EXTERNAL SKIN CREASED AND OIL CANNED. THE DAMAGED AREA WAS REMOVED, A DOUBLER WAS FABRI CATED AND INSTALLED IAW SRM 52-00-3 FIGURE 6, 52-30-3 AND 51-10-6. 2 L 7 2 4F A16WE 1996121200170 19961212 00170 WP 1996 12 12 CALA9601729 1 19961128 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP BS 1338 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 INSPECTION FOUND CORROSION UNDER CASTING ON FLOORBEAM WEB AT STA 1338, LBL 45 TO LBL 54. THE CORROSION WAS REMOVED AND A DOUBLER WAS INSTALLED IAW ECRA 5310-03372. 2 L 7 2 4F A6WE 1996121200171 19961212 00171 WP 1996 12 12 CALA9601730 1 19961128 A 5311 FLOOR FRAME DOUG DC9 DC982 3022082 WP BS 1338 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 INSPECTION FOUND CORROSION AROUND FASTENER HOLE ON FLOOR FRAME AT STA 1338, LBL 45. THE CORRODED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 53-05, FIGURE 20A PAGE 31. 2 L 7 2 4F A6WE 1996121200172 19961212 00172 NM 1996 12 12 CALA9601731 1 19961119 A 5753 SKIN BOEING 727 727232 1384082 NM TE MIDFLAP DAMAGED A CALA K NONE O OTHER LD LANDING 1 SW 09 10791 20645 THE RT INBOARD TRAILING EDGE MID FLAP LOWER SKIN SUSTAINED DAMAGE WHEN THE RT MLG TIRE BLEW. THE MID FLAP WAS REPAIRED IAW ECRA 5750-02565. 2 L 7 3 4F A3WE 1996121200173 19961212 00173 WP 1996 12 12 9625969941 1 19961204 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 3324L 47103 DURING LINE MAINTENANCE INSPECTION, FOUND FAIL COMPARTMENT FLOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, O PERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996121200174 19961212 00174 WP 1996 12 12 9625979978 1 19961204 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9342 47391 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN PACK, OPERA TIONAL CHECK OK. 2 L 7 2 4F A6WE 1996121200175 19961212 00175 EU 1996 12 12 9625983233 1 19961204 A 2761 31077050 ACTUATOR AIRBUS 320 A320212 EU NR 2 SPOILER LEAKING A NWAA K NONE F K FLT CONT AFFECTED FLUID LOSS LD LANDING 1 GL 01 333NW 329 THE RIGHT WING NR 2 SPOILER ACTUATOR FAILED TO EXTEND ON LANDING. THE LANDING WAS ACCOMPLISHED WITHOUT INCIDENT. DURIN G TAXI INTO GATE THE YELLOW HYDRAULIC SYSTEM FLUID DEPLETED. MAINTENANCE REPLACED THE RIGHT WING NR 2 SPOILER ACTUATOR, LEAK AND OPS CHECK OK. 2 L 7 2 4F RT A28NM 1996121200176 19961212 00176 NM 1996 12 12 9625996303 1 19961204 A 3350 LIGHT BOEING 747 747451 1384940 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 663US 23818 DURING LINE CHECK, FOUND EMERGENCY FLOOR PATH LIGHTING INOPERATIVE AT DR 2L TO ROW 21L, ROW 35L TO 43L, ROW 21R TO 23R. REINSTALLED CONNECTOR AND LIGHTS, REPLACED LIGHT MODULE, REPAIRED WIRING AND OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1996121200177 19961212 00177 NM 1996 12 12 9626006301 1 19961201 A 3350 CONNECTOR BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 661US 23719 DURING LINE CHECK, FOUND 2 RT, 2 LT AND 3 LT FLOOR EMERGENCY LIGHTS INOPERATIVE. RECONNECTED LIGHT, OPERATIONAL CHECK G OOD. 2 L 7 4 4F RT A20WE 1996121200178 19961212 00178 WP 1996 12 12 9626019905 1 19961204 A 3231 BOLT DOUG DC9 DC931 3022065 WP RT MLG DOOR MISINSTALLED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 955N 47160 RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. RECYCLED GEAR AND LIGHT STAYED ON. MAINTENANCE FOUND BOLT HEAD ON ROLLER AND LINK ASSEMBLY HITTING ON FORWARD EDGE OF RIGHT WHEEL WELL APPROXIMATELY 1.5 INCHES ABOVE DOOR SWITCH. REMOVED WASHER FROM UNDER BOLT HEAD AND CHECKED ADJUSTMENTS, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996121200179 19961212 00179 EU 1996 12 12 9626023243 1 19961202 A 2761 31077050 ACTUATOR AIRBUS 320 A320212 EU NR 3 SPOILER LEAKING A NWAA O OTHER K J FLUID LOSS WARNING INDICATION UK UNKNOWN 1 GL 01 343NW 387 HYD-B RSVR LO LVL ANNUNCIATED. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND LANDED WITHOUT INCIDENT. MAINTENANCE F OUND THE NR 3 SPOILER ACTUATOR LEAKING. REPLACED THE SAME, LEAK OPS CHECK OK. 2 L 7 2 4F RT A28NM 1996121200180 19961212 00180 NM 1996 12 12 QXEA9600477 1 19961203 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT INOPERATIVE A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 840PH 74 COCKPIT OVERHEAD EMERGENCY LIGHT IS INOP. LIGHT ASSY REPLACED AND LIGHT OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 1996121200181 19961212 00181 SW 1996 12 12 QXEA9600478 1 19961203 A 3260 GEAR LIGHT SWRNGN SA227 SA227AC 8780603 SW NLG MALFUNCTIONED A QXEA O OTHER P NO WARNING INDICATION AP APPROACH 1 NM 09 26932 AC660 NOSE GEAR DOWN AND LOCKED LIGHT DID NOT ILLUMINATE AFTER SELECTING GEAR DOWN. GEAR WAS CYCLED SEVERAL TIMES WITH THE SA ME RESULT. ALTERNATE GEAR EXTENSION PERFORMED AND DOWN AND LOCKED LIGHT ILLUMINATED. AIRCRAFT LANDED IN GEG WITHOUT FU RTHER PROBLEMS. AIRCRAFT FERRIED EDX FOR REPAIR. 2 L 7 2 4T RT A8SW 1996121200182 19961212 00182 EU 1996 12 12 QXEA9600479 1 19961205 A 3350 1820 BULB FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 478US 11227 NUMBER FIVE AND SIX EMERGENCY LIGHTS IN CABIN OVERHEAD ARE INOP. BULBS WERE REPLACED AND LIGHTS OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996121200183 19961212 00183 EU 1996 12 12 QXEA9600480 2 19961204 A 7261 ENGINE OIL FOKKER F28 F28MK4000 4990810 EU RROYCE SPEY SPEY55515 54521 EU NR 2 ENGINE OVER SERVICED A QXEA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 478US 11227 SMOKE SMELL IN AFT AREA OF CABIN REPORTED BY A PASSENGER AND LEFT LAV SMOKE DETECTOR ALARM SOUNDED ON TAXI OUT. AIRCRAF T RETURNED TO GATE. NUMBER TWO ENGINE FOUND OVER SERVICED BY TWO QUARTS ON THE ENGINE OIL. ENGINE OIL SERVICED TO NORM AL LEVEL. ENGINE GROUND RUN PERFORMED AND BLEED AIR CHECK GOOD. 2 L 7 2 4F 4 F RT A20EU E2EU 1996121200184 19961212 00184 EU 1996 12 12 96FDEA01696 1 19961205 A 2131 CONTROLLER AIRBUS 310 A310221 3930310 EU CABIN MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 419FE 345 CLIMBOUT APPROX 8,000 FT, RECEIVED RED ECAM WARNING LWR ACCESS DOOR NOT CLOSED, FOLLOWED BY EXCESSIVE CABIN RATE. ACCOM PLISHED ECAM. CABIN RATE CLIMBED AT SAME RATE AND ALTITUDE AS A/C DESCENDED TO 10,000 FT MADE PRECAUTIONARY LANDING KUL . LONG HISTORY OF PRESS PROBLEMS WITH A/C. CABIN PRESSURIZATION CONTROLLER NR 2 SELECTED OFF BY CREW. SELECTED NR 2 C PC ON AND ALL ECAM INDICATIONS NORMAL. PERFORMED BITE TEST ON BOTH CPCS WITH NO FAULTS. CHECKED BOTH LOWER ACCESS DOOR S AND FOUND CLOSED. ADJUSTED INDICATION STRIKER ON FWD DOOR AND ECAM DOOR INDICATION NORMAL. PRESSURIZED CABIN TO 4 PS I DIFFERENTIAL. 2 L 7 2 4F RT A35EU 1996121200185 19961212 00185 NM 1996 12 12 96FDEA01695 1 19961203 A 3230 ARG70765511 TRIM CYLINDER DOUG MD11 MD11F 3023600 NM LANDING GEAR MALFUNCTIONED A FDEA A J UNSCHED LANDING DUMP FUEL K FLUID LOSS CL CLIMB 1 SO 25 603FE 48459 AFTER TAKEOFF, GEAR HANDLE WOULD NOT RAISE TO RETRACT THE GEAR. REMOVED AND REPLACED THE BOGIE TRIM CYCLINDER, OPS CHEC K GOOD. 2 L 7 3 4F RT A22WE 1996121200186 19961212 00186 WP 1996 12 12 MWEA96645 1 19961205 A 5522 SKIN DOUG DC9 DC932 3022066 WP LT ELEVATOR DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 WHILE BEING DE-ICED, THE VEHICLE CAME IN CONTACT WITH THE LEFT ELEVATOR TRAILING EDGE OUTBD END. REMOVED AND REPLACED LEFT ELEVATOR TRAILING EDGE SECTION IAW SRM 51-30. 2 L 7 2 4F A6WE 1996121200187 19961212 00187 NM 1996 12 12 SCNA96403 1 19961203 A 5311 FRAME BOEING 727 7272J4 1384006 NM BS 328 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 288SC 20765 DURING INSPECTION, CORROSION DAMAGE WAS DISCOVERED ON THE FUSELAGE SKIN AT BS 328 RT, JUST OUTBOARD OF THE NLG WHEEL WEL L CUTOUT. ALSO, CORROSION WAS FOUND ON THE BS 328 FRAME AND THE LOWER STIFFENER FOR THE NOSE LANDING GEAR WHEEL WELL SI DE PANEL. THE FUSELAGE AND FRAME WERE REPAIRED IN ACCORDANCE WITH THE SRM AND THE STIFFENER WAS REPAIRED IN ACCORDANCE WITH AN ENGINEERING AUTHORIZATION. 2 L 7 3 4F RT A3WE 1996121200188 19961212 00188 WP 1996 12 12 SCNA96404 1 19961114 A 5315 FLOORBEAM DOUG DC10 DC1010 3022110 WP BS 1601 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 572SC 46977 DURING HEAVY MAINTENANCE, FOUND CORROSION AROUND NUTPLATE HOLES ON CENTER CARGO BAY FLOORBEAM AT BS 1601, LBL 20. REMOV ED DAMAGED SUPPORT, FABRICATED AND INSTALLED NEW SUPPORT IN ACCORDANCE WITH SRM 53-15-01 AND 51-33-01. 2 L 7 3 4F A22WE 1996121200189 19961212 00189 WP 1996 12 12 SCNA96405 1 19961114 A 5320 FLOOR SUPPORT DOUG DC10 DC1010 3022110 WP BS 600 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 572SC 46977 DURING HEAVY MAINTENANCE, FOUND CORROSION AROUND NUTPLATE HOLES FLOOR SUPPORT AT BS 60, BL 0 TO BL 29. REMOVED DAMAGED FLOOR SUPPORT, FABRICATED AND INSTALLED NEW FLOOR SUPPORT IN ACCORDANCE WITH SRM 51-30-00. 2 L 7 3 4F A22WE 1996121200190 19961212 00190 WP 1996 12 12 SCNA96406 1 19961115 A 5512 SKIN DOUG DC10 DC1010 3022110 WP LT HORIZ STAB GOUGED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 572SC 46977 DURING HEAVY MAINTENANCE, FOUND GOUGE ON LEADING EDGE OF LEFT HAND HORIZONTAL STABILIZER, APPROXIMATELY 13 FEET OUTBOARD OF FUSELAGE. REMOVED DAMAGED MATERIAL, FABRICATED AND INSTALLED A FILLER AND DOUBLER IN ACCORDANCE WITH SRM 55-10-1 FI GURE 13. 2 L 7 3 4F A22WE 1996121200191 19961212 00191 WP 1996 12 12 SCNA96407 1 19961115 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 1787 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 572SC 46977 DURING HEAVY MAINTENANCE, FOUND CORROSION ON REINFORCING CHANEL FOR FRAME 1787, BETWEEN LONGERON 50L AND 50R. FABRICATE D AND INSTALLED A NEW FRAME CAP IN ACCORDANCE WITH SRM 53-30-00, PAGES 15 AND 16. 2 L 7 3 4F A22WE 1996121200192 19961212 00192 WP 1996 12 12 SCNA96408 1 19961115 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 899 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 572SC 46977 DURING HEAVY MAINTENANCE, FOUND CORROSION ON FRAME AT BS 899 BETWEEN LONGERON 51L AND 51R. REMOVED DAMAGED MATERIAL, FA BRICATED AND INSTALLED A FRAME CAP IN ACCORDANCE WITH SRM 53-30-00 PAGE 31. 2 L 7 3 4F A22WE 1996121200193 19961212 00193 WP 1996 12 12 SCNA96409 1 19961115 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 939 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 572SC 46977 DURING HEAVY MAINTENANCE, FOUND CORROSION ON FRAME AT BS 939 BETWEEN LONGERON 50L AND 50R. REMOVED DAMAGED MATERIAL, FA BRICATED AND INSTALLED A FRAME CAP IN ACCORDANCE WITH SRM 53-30-00. 2 L 7 3 4F A22WE 1996121200194 19961212 00194 WP 1996 12 12 SCNA96410 1 19961116 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 775-889 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 572SC 46977 DURING HEAVY MAINTENANCE, FOUND CORROSION AROUND FASTENER HOLES ON LONGERON 51R FROM BS 775 TO BS 889. FABRICATED AND S PLICED IN NEW LONGERON SECTION IN ACCORDANCE WITH SRM 51-30-01. 2 L 7 3 4F A22WE 1996121200195 19961212 00195 WP 1996 12 12 SCNA96411 1 19961116 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 1942 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 572SC 46977 DURING HEAVY MAINTENANCE, FOUND CORROSION ON FRAME 1942 BETWEEN LONGERON 51L AND 49R. REMOVED DAMAGED MATERIAL, FABRICA TED AND INSTALLED REPAIR IN ACCORDANCE WITH SRM 53-00-00 FIGURE 5. 2 L 7 3 4F A22WE 1996121200196 19961212 00196 WP 1996 12 12 SCNA96412 1 19961116 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 775-850 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 572SC 46977 DURING HEAVY MAINTENANCE, FOUND CORROSION AROUND RIVET HOLES ON LONGERON 50L BETWEEN BS 775 AND BS 850. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED A REPAIR SECTION IN ACCORDANCE WITH SRM 53-10-00. 2 L 7 3 4F A22WE 1996121200197 19961212 00197 WP 1996 12 12 SCNA96414 1 19961116 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 1902 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 572SC 46977 DURING HEAVY MAINTENANCE, FOUND CORROSION AROUND NUTPLATE HOLES ON FRAME 1902. REMOVED CORROSION, FABRICATED AND INSTAL LED DOUBLERS IN ACCORDANCE WITH SRM 53-00-01 FIGURE 2. 2 L 7 3 4F A22WE 1996121200198 19961212 00198 WP 1996 12 12 SCNA96415 1 19961116 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 775-889 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 572SC 46977 DURING HEAVY MAINTENANCE, FOUND CORROSION AROUND FASTENER HOLES ON LONGERON 52 BETWEEN BS 775 AND 889. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR SECTION AND SPLICES IN ACCORDANCE WITH SRM 51-30-00. 2 L 7 3 4F A22WE 1996121200199 19961212 00199 WP 1996 12 12 SCNA96416 1 19961116 A 5320 INTERCOSTAL DOUG DC10 DC1010 3022110 WP BS 1721-1741 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 572SC 46977 DURING HEAVY MAINTENANCE, FOUND CORROSION ON WEBS AND AREA AROUND DOME NUTS THAT ATTACH THE ADF ANTENNA BETWEEN LONGERON S 51R AND 52, BS 1721 TO 1741. REMOVED AND REPLACED INTERCOSTAL IN ACCORDANCE WITH SRM 51-31-01. 2 L 7 3 4F A22WE 1996121200200 19961212 00200 WP 1996 12 12 SCNA96417 1 19961120 A 5320 NCA6042174 STIFFENER DOUG DC10 DC1010 3022110 WP BS 475 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 572SC 46977 DURING HEAVY MAINTENANCE, FOUND CORROSION AT FRAME AND SKIN INTERSECTION AT BS 475 FROM LONGERON 44L TO 44R. REMOVED CO RROSION, REMOVED AND REPLACED STIFFENER IN ACCORDANCE WITH SRM 51-21-01, 51-31-01 AND 51-35-01. 2 L 7 3 4F A22WE 1996121200201 19961212 00201 WP 1996 12 12 SCNA96418 1 19961127 A 5320 SPLICE DOUG DC10 DC1010 3022110 WP BS 890 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 572SC 46977 DURING HEAVY MAINTENANCE, FOUND LONGERON 52 SPLICE CRACKED AND CORRODED AT BS 890. FABRICATED AND INSTALLED NEW SPLICE IN ACCORDANCE WITH SRM 53-10-00. 2 L 7 3 4F A22WE 1996121200202 19961212 00202 WP 1996 12 12 SCNA96419 1 19961130 A 3350 LIGHTING DOUG DC10 DC1010 3022110 WP CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 572SC 46977 FOUND AFT CABIN TRACK LIGHTING LOOSE AND BROKEN WIRES ON THE RIGHT HAND SIDE. SECURED TRACK, REPAIRED WIRES AND OPS CHE CKED IN ACCORDANCE WITH MM 33-50-00. 2 L 7 3 4F A22WE 1996121200203 19961212 00203 WP 1996 12 12 SCNA96420 1 19961201 A 3350 EMBS1392 POWER SUPPLY DOUG DC10 DC1010 3022110 WP CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 572SC 46977 FOUND EMERGENCY LIGHT CHARGE AND STANDBY BREAKERS OPEN. REMOVED AND REPLACED LEFT HAND OVERWING BATTERY POWER SUPPLY AN D OPS CHECKED GOOD IN ACCORDANCE WITH MM 33-51-01. 2 L 7 3 4F A22WE 1996121200204 19961212 00204 NM 1996 12 12 SCNA96421 1 19961203 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM AIRSTAIR DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 282SC 22558 FOUND AFT AIRSTAIR EMERGENCY EXIT LIGHT FLICKERING. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK IN ACCORDANC E WITH MM 33-50-61 AND OPS CHECKED NORMAL. 2 L 7 3 4F A3WE 1996121200205 19961212 00205 NM 1996 12 12 SCNA96422 1 19961203 A 3231 RETRACT MECH BOEING 727 727225 1384077 NM NLG DOORS MALFUNCTIONED A SCNA K NONE J WARNING INDICATION NR NOT REPORTED 1 GL 15 282SC 22558 NOSE GEAR DOOR LIGHT ON INTERMITTENTLY. ADJUSTED DOORS PER MM 32-22-1 PAGE 507 STEP 12, OPS CHECKED NORMAL. 2 L 7 3 4F A3WE 1996121200206 19961212 00206 WP 1996 12 12 RRXA96168 1 19961204 A 2910 HYD LINE DOUG DC8 DC8F54 3021926 WP NR 3 ENGINE FAILED A RRXA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 15 992CF 45884 DURING CRUISE HYDRAULIC QUANTITY DROPPED TO AUX LEVEL. HYDRAULIC LOSS QRH PROCEDURE WAS CALLED OUT. MAINTENANCE REMOVE D AND REPLACED THE RETURN LINE TO THE NR 3 ENGINE HYDRAULIC PUMP, OPERATIONAL CHECK OF THE SYSTEM WAS GOOD. 2 L 7 4 4F 4A25 1996121200207 19961212 00207 WP 1996 12 12 CKSA96324 1 19961121 A 5330 SKIN DOUG DC8 DC8F55 3021928 WP BS 550-556 DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING B-CHECK INSPECTION, FOUND SKIN PUNCTURED, ON BOTTOM B-PIT ON FUSELAGE 12 BELOW DOOR SILL. REMOVED DAMAGED MATERI AL AND REPAIRED IAW AIA ENGINEERING SKETCH NR AIA/E/2413, FAA/DER APPROVED ON FORM 8110-3 DATED 11-19-96. NON-ROUTINE T ASK CARD NR 89763. 2 L 7 4 4F 4A25 1996121200209 19961212 00209 NM 1996 12 12 CA960612024 1 19960526 A 3231 82910010193 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NOSE GEAR DOOR LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 19773 PCE120358 (CAN)HYDRAULIC FLUID FOUND AT NOSE BAY AND ON NOSE LANDING GEAR DOOR. LEAK CHECK FOUND A PIN HOLE ON THE LINE SURROUNDED BY SMALL CORROSION AREA. 2 H 7 2 4T 4 T RT A13NM E20NE 1996121200237 19961212 00237 NE 1996 12 12 CA960614001 2 19960614 A 7210 120373 RED GR BOX PWA DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE CHIP DETECTOR MAKING METAL W A K NONE O OTHER IN INSP/MAINT 1 CA 17891 10907 120373 120373 (CAN)METAL ON RH REDUCTION GEAR BOX CHIP DETECTOR. METAL ANALYSED AS BEARING MATERIAL. ENGINE REMOVED FOR REPAIR 2 H 7 2 4T 4 T RT A13NM E20NE 1996121200238 19961212 00238 NM 1996 12 12 CA960614002 1 19960614 A 2750 745583A DRIVE DHAV DHAV DHC8 DHC8301 NM PWA 120 PW120A NE FLAP SEC DRIVE DAMAGED W A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CA 121164 (CAN)AFTER TAKEOFF FLAPS FAILED TO RETRACT FROM 10 DEGREES. FLEX SECONDARY DRIVE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1996121200239 19961212 00239 NM 1996 12 12 CA960614003 1 19960614 A 2761 82950011005 ACTUATOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE SPOILER BYPASSING W O OTHER J WARNING INDICATION IN INSP/MAINT 1 CA 17373 120305 (CAN) GENERAL VIBRATION AND BUZZING DURING AND AFTER ENGINE START CYCLE. #2 ENGINE HYDRAULIC PRESSURE AT 1100 TO 1200 PS I ONLY. CAUTION LIGHT ON. LH INBOARD GROUND SPOILER ACTUATOR FAILED. SB 8-27-62 COVERS MODIFICATION OF THIS P/N UNIT. 2 H 7 2 4T 4 T RT A13NM E20NE 1996121200240 19961212 00240 SO 1996 12 12 CA960614006 2 19960605 A 8530 637781 VALVE CONT 6423430 CESSNA 421 421C 2076016 CE CONT O520 GTSIO520L 17032 SO MCAULY 3FF32 3FF32C501 GL NR 3 CYL EXH BROKEN STEM W O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 CA 1006 7785MS410 604432 802942 (CAN)#3 CYLINDER EXHAUST VALVE STEM BROKEN JUST BELOW THE HEAD. 1 L 7 2 3O 3 O A7CE E7CE 5 C P45GL 1996121200241 19961212 00241 NM 1996 12 12 CA960614008 1 19960609 A 7830 52754031 CABLE BOEING 757 757236 NM RROYCE RB211 RB211535E4 54555 NE THRUST REV BROKEN W A D RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CA 30739 (CAN) AIRCRAFT HAD TO REJECT TAKEOFF DUE TO ENGINE NOT REACHING TO POWER BECAUSED OF THROTTLE JAM. THRUST REVERSER CABLE BROKEN RESULTING A FEEDBACK CABLE CAM IN UNLOCK POSITION. CAM REPOSITIONED AND THRUST REVERSER DEACTIVATED AS PER MM AN D RELEASED AS PER MEL. 2 L 7 2 4F 4 F RT A2NM E12EU 1996121200243 19961212 00243 SO 1996 12 12 CA960614013 2 19960601 A 8530 639274 CYLINDER CESSNA 210 210J 2073439 CE CONT O520 IO520J 17032 SO NR 2 HEAD CRACKED W A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 CA 308 553574 (CAN)ROUGH RUNNING ENGINE WITH A SLIGHT POWER LOSS. #2 CYLINDER HAD A SMALL HOLE IN THE HEAD AND SEVERAL CRACKS RADIATIN G FROM BOTH PLUG HOLES, ALSO, A 6 INCH CRACK AROUND THE HEAD AT THE TOP OF THE BARREL . 1 H 7 1 3O 3 O 3A21 E5CE 1996121200254 19961212 00254 CE 1996 12 12 CA960617201 1 19960605 A 2435 BRUSHES LEAR 25 25B 5170511 CE GE CJ610 CJ6106 30006 NE STARTER GEN WORN W H DEACTIVATE SYST/CIRCUITS H ELECT. POWER LOSS-50 PC DE DESCENT 1 CA 170 241C210A (CAN)PRE MATURE BRUSH WEAR. 2 L 7 2 4J 4 J A10CE 1E16 1996121200255 19961212 00255 NE 1996 12 12 CA960618201 2 19960530 A 8510 17187 SNAP RING PWA 109268 DOUG DC4 C54EDC 3021528 WP PWA R2000 R20004 52023 NE GOV GEARSHAFT DISLODGED W E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 749 S3376F P107335 (CAN) IN CRUISE, #3 ENGINE RPM STARTED TO INCREASE, COULD NOT BE REDUCED BY PROPELLER CONTROL, ENGINE SHUTDOWN BEFORE RP M REACHED 2700. SNAP RING POPPED OUT OF ITS GROOVE ON THE PROP GOVERNOR GEARSHAFT P/N 46050, ALLOWING THE SHAFT TO DROP DOWN AND DISENGAGE THE GOVERNOR. 2 L 7 4 4R 4 R A762 5E5 1996121200256 19961212 00256 NM 1996 12 12 CA960619001 1 19960603 A 7930 OIL PRESSURE BOEING 727 72725 1384006 NM PWA JT8 JT8D7 52053 NE #1 ENGINE LOW W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 653417 (CAN) #1 ENGINE OIL PRESSURE LOW ON TAKEOFF, ABORTED. NO FAULT FOUND. 2 L 7 3 4F 4 F A3WE E2EA 1996121200257 19961212 00257 NM 1996 12 12 CA960619003 1 19960618 A 3244 93077031 TREAD DUNLOP 265X813 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE MLG TIRE SEPARATED W A UNSCHED LANDING O OTHER TO TAKEOFF 1 CA 93077031 120442 (CAN)TREAD SEPARATED FROM TIRE CARCASS ON TAKEOFFBOTH TIRES REPLACED TIRE ON SECOND RECAP 2 H 7 2 4T 4 T RT A13NM E20NE 1996121200258 19961212 00258 NE 1996 12 12 CA960619006 2 19960501 A 7420 955016860 IGNITOR CABLE SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE MOISTURE W K NONE O OTHER IN INSP/MAINT 1 CA 835 (CAN)NO IGNITION, MOISTURE NOTICED IN IGNITOR TIPS. TWO IGNITORS AND CABLE ASSEMBLIES REPLACED. 953.6 HOURS THIS INSTALL LATION. AIRCRAFT RETURNED TO SERVICE. 1 G 7 1 3U 3 U H9EU E19EU 1996121200259 19961212 00259 NE 1996 12 12 CA960619007 2 19960417 A 7322 306001 FUEL FILTER SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE CANNON PLUG AREA LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 48 451 (CAN)FUEL FILTER ASSEMBLY WAS LEAKING OUT OF ELECTRICAL CONNECTION. UNIT REPLACED, AIRCRAFT RETURNED TO SERVICE. 1 G 7 1 3U 3 U H9EU E19EU 1996121200260 19961212 00260 GL 1996 12 12 CA960619008 2 19960422 A 7230 6890550 COMPRESSOR BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE SEIZED W K NONE O OTHER IN INSP/MAINT 1 CA 13008 1 CAE830542 (CAN)AFTER FLIGHT TEST, PILOT WAS UNABLE TO RESTART ENGINE. TROUBLESHOOTING DETERMINED COMPRESSOR ASSEMBLY WAS SEIZED. U NIT REPLACED AND AIRCRAFT RETURNED TO SERVICE. TIME THIS INSTALLATION, 0.3 HOURS. 1 G 7 1 3U 3 U H2SW E4CE 1996121200262 19961212 00262 NM 1996 12 12 CA960619039 1 19960612 A 2131 IN4964 ZENER DIODE AIRESRCH 21178041 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE POWER BOARD BURNT W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA 213 213 108482 120584 (CAN)CREW NOTED ELECTRICAL BURNING SMELL IN FLIGHT COMPARTMENT AND CABIN. CABIN PRESSURE CONTROLLER FOUND SHORTED INTERN ALLY, PRODUCING THE SMELL. THE ZENER DIODE VR3 ON THE POWER CIRCUIT BOARD HAD OVERHEA TED AND BURNT THE CIRCUIT BOARD AN D CLEAR BLACK COAT EMITTING INTENSE "BURNT PLASTIC" ODOUR. 2 H 7 2 4T 4 T RT A13NM E20NE 1996121200263 19961212 00263 NE 1996 12 12 CA960619040 2 19960612 A 7323 MICRO SWITCH DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE NP UNDERSPD GOV FAILED W E ENGINE SHUTDOWN O OTHER TX TAXI/GRND HDL 1 CA 10384 123020 (CAN) ON #1 ENGINE SHUTDOWN, ENGINE OVERTORQUE OCCURRED, ENGINE SHUTDOWN WITH "T" HANDLE. NP UNDERSPEED GOVERNING MICROS WITCH FAILED. 2 H 7 2 4T 4 T RT A13NM E20NE 1996121200266 19961212 00266 EA 1996 12 12 CA960620003 1 19960610 A 2910 72980010217 LINE DHAV DHC7 DHC7103 2802710 EA PWA PT6 PT6A50 52043 EA HAMSTD 24PF 24PF305 GL #1 HYD SYS CRACKED W K NONE K FLUID LOSS TO TAKEOFF 1 CA PCE86334 237121 (CAN) ON TAKEOFF HYDRAULIC PRESSURE WAS LOST AND HYDRAULIC QUANTITY SOON FOLLOWED ON SYSTEM #1. THE AIRCRAFT CONTINUED H OME ON 4 ENGINES. A CRACKED HYDRAULIC LINE FOUND. 2 H 7 4 4T 4 T A20EA E4EA 6 C P1NE 1996121200267 19961212 00267 1996 12 12 CA960620004 4 19960604 A 3420 7003360941 AHRS HONEYWELL DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE #2 SYS FAILED W K NONE I FLT. ATTITUDE INST. CR CRUISE 1 CA 89061385 123052 (CAN) #2 ATTITUDE AND HEADING REFERENCE SYSTEM (AHRS) FAILED IN FLIGHT. EADI ATTITUDE INFO TOPPLES. CYCLING THE #2 AHRS AND #2 AHRS CIRCUIT BREAKERS WOULD BRING AHRS BACK ON LINE. UNIT REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1996121200270 19961212 00270 NM 1996 12 12 CA960620017 1 19960604 A 2910 82950010175 HYDRAULIC TUBE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE LH SPOILER AREA CRACKED W K NONE K FLUID LOSS NR NOT REPORTED 1 CA 17110 120386 (CAN) HYDRAULIC TUBE LEAK LH WING REAR SPAR NEAR OUTBOARD FLIGHT SPOILER ACTUATOR. 2 H 7 2 4T 4 T RT A13NM E20NE 1996121200272 19961212 00272 NE 1996 12 12 CA960620023 2 19960607 A 8530 VALVE SEAT PWA 399359 DHAV DHC3 DHC3 2800202 EA PWA R1340 S3H1G 52016 NE CYL HEAD EXH DETACHED W K NONE R PARTIAL RPM/PWR LOSS LD LANDING 1 CA 430 22910 (CAN) PILOT REPORTED LOW ENGINE POWER AND SUCKING SOUND ON SHUTDOWN. #3 CYLINDER EXHAUST VALVE SEAT OUT OF POSITION KEEP ING VALVE OPEN. 1 H 7 1 3R 3 R A815 E142 1996121200273 19961212 00273 SO 1996 12 12 CA960620024 1 19960606 A 5751 4A25108701 SUPPORT EMB EMB 110 EMB110P1 3260122 SO PWA PT6 PT6A34 52043 EA LEFT AIL CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 16721 PCE56946 (CAN) LEFT AILERON BRACKET, CENTRE SUPPORT CRACKED, ON CENTRE AILERON SPAR. 1 L 7 2 4T 4 T A21SO E4EA 1996121200274 19961212 00274 NM 1996 12 12 CA960620027 1 19960612 A 3297 WIRE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NLG CHAFED W K NONE N FALSE WARNING NR NOT REPORTED 1 CA 22579 120550 (CAN) NOSE LANDING GEAR ADVISORY GREEN LIGHT COMES ON INTERMITTENTLY IN FLIGHT. WIRE 3261-56A22 AND 3261-52A22 WERE FOUN D CHAFED. THESE WIRES ARE LOCATED ON THE BACK OF THE ADVISORY CONTROL BOX, 12 INCHES FROM THE CONNECTOR 3313-P1A. CHAFIN G RESULTED FROM WIRE RUBBING AGAINST THE PITOT TUBING. 2 H 7 2 4T 4 T RT A13NM E20NE 1996121200275 19961212 00275 NE 1996 12 12 CA960620028 2 19960603 A 7414 SHAFT BOSCH DHAV DHC2 DHC2MK1 2800102 EA PWA R985 R985AN14B 52008 NE RT MAG DRIVE BROKEN W D RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 CA 200320 (CAN) ON ENGINE RUNUP, DURING MAGNETO CHECK, ENGINE VIBRATION ON THE RIGHT MAGNETO. MAGNETO DRIVESHAFT BROKEN. 1 H 7 1 3R 3 R A806 5E1 1996121200277 19961212 00277 EU 1996 12 12 CA960620030 1 19960621 A 2510 AN515A BOLT 168672 BAG JETSTM JETSTM4112 EU MCAULY 2D34C B2D34C202 GL CAPTAINS BELT LOOSE W D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CA 2698 950511 (CAN) DURING TAXI FOR TAKEOFF, THE CAPTAINS RIGHT HAND LAP BELT CAME DETACHED FROM THE SEAT. MAINTENANCE FOUND THAT THE BOLT RETAINING THE LAP BELT LINK TO THE SEAT HAD BACKED OUT. ALL AIRCRAFT IN FLEET INSPECTED. 1 L 7 2 4T RT A196 5 C P7EA 1996121200280 19961212 00280 SW 1996 12 12 CA960625005 1 19960611 A 3260 2686026005 INDICATOR SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP GEAR/FLAP STUCK W K NONE N FALSE WARNING AP APPROACH 1 CA 15746 P54202 (CAN) ON APPROACH, CREW DID NOT GET RH GEAR DOWN AND LOCKED INDICATION. EMERGENCY EXTENSION USED OKAY. INVESTIGATION FOU ND THAT THE RIGHT GEAR WAS FUNCTIONING NORMALLY BUT THAT THE RIGHT GEAR INDICATOR WAS STICKING AND NEEDED TO BE TAPPED. GAUGE REPLACED. 2 L 7 2 4T 4 T RT A8SW E4WE 1996121200281 19961212 00281 EA 1996 12 12 CA960625006 1 19960511 A 2750 SKA1043 VALVE SYNCRO DHAV DHC6 DHC6300 EA PWA PT6 PT6A27 52043 EA FLAP SELECTOR LEAKING W K NONE O OTHER IN INSP/MAINT 1 CA 9 295 PCE41677 (CAN) FLAP SELECTOR VALVE HAD BEEN REPLACED. DURING TESTING AND RIGGING OF SYSTEM, SYSTEM PRESSURE DROPPED AND THE FLAPS DROOPED WITHIN A HALF HOUR. THE SELECTOR CABLES WERE DISCONNECTED AND THE VALVE WAS OPERATED MANUALLY. IT WAS DETERMINE D THAT VALVE WAS LEAKING INTERNALLY. THIS HAD BEEN A REPAIRED ITEM WHICH HAD BEEN REPAIRED AND CHECKED FOR SAME PROBLEM. 1 H 7 2 3T 4 T A9EA E4EA 1996121200282 19961212 00282 EA 1996 12 12 CA960625007 1 19960524 A 2750 SKA1043 VALVE SYNCRO DHAV DHC6 DHC6300 EA PWA PT6 PT6A27 52043 EA FLAP SELECTOR LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 20 691 PCE41677 (CAN) SECOND SELECTOR VALVE INSTALLED IN 14 DAYS. ON DI A SMALL AMOUNT OF FLUID NOTED ON CABIN FLOOR. INSPECTION OF OVER HEAD PANEL REVEALED A LOT OF HYDRAULIC FLUID HAD CONTAMINATED CENTRE LIGHT PANEL FROM STA. 111.0 TO STA. 332.0. HYDRAULI C PRESSURE PUT ON AIRCRAFT AND FLAP SELECTOR CYCLED TO FULL DOWN POSITION. AS SOON AS FLAPS STARTED DOWN HYDRAULIC FLUID STREAMED OUT OF THE LOWER RH POPPET VALVE COVER. COVER REMOVED AND NEW 'O' RINGS INSTALLED, BUT VALVE STILL LEAKED. VAL VE REPLACED. 1 H 7 2 3T 4 T A9EA E4EA 1996121200283 19961212 00283 EA 1996 12 12 CA960625008 1 19960617 A 5280 215330013 SKIN CNDAIR CNDAIR CL215 CL2151A10 EA RH DOOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1479 (CAN) NOSE LANDING GEAR DOOR SKIN FOUND CRACKED AT TRAILING EDGES OF BOTH DOORS. SRM 51-64-10. LEFT DOOR P/N 215-33001-2 . 2 H 7 2 4R A14EA 1996121200284 19961212 00284 EA 1996 12 12 CA960625009 1 19960616 A 5322 BULKHEAD CNDAIR 215260522 CNDAIR CL215 CL2151A10 EA FS 371.5 CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1479 1479 (CAN) WATER TANK BULKHEAD AT FUSELAGE STA. 371.5 FOUND CRACKED AT LUG ATTACHMENT AREA, CAUSING WATER DOORS TO BE OUT OF RIG. REPAIRED AS PER DECA ENGINEERING ORDER. 2 H 7 2 4R A14EA 1996121200285 19961212 00285 EA 1996 12 12 CA960625010 1 19960622 A 5280 SKIN CNDAIR 215330013 CNDAIR CL215 CL2151A10 EA LT RT NLG DOOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1548 (CAN) NOSE LANDING GEAR DOORS EXTERIOR SKINS FOUND CRACKED ON INSPECTION AT TRAILING EDGES, BOTH DOORS. LEFT DOOR P/N 21 5-33001-2. 2 H 7 2 4R A14EA 1996121200286 19961212 00286 NE 1996 12 12 CA960625014 3 19960615 A 6114 7827015 PROP HUB DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE #4 BLADE SLEEVE MOVING W K NONE O OTHER IN INSP/MAINT 1 CA 20073 1678 120358 870508 (CAN) AFTER REMOVING THE #4 PROPELLER BLADE INSPECITON REVEALED THE SLEEVE/BUSHING WAS STARTING TO DISLODGE. THE PROPELL ER WAS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1996121200290 19961212 00290 EA 1996 12 12 CA960626002 2 19960606 A 8520 11B200511SL CRANKCASE BEECH 95 D95A 1153408 CE LYC O360 IO360B1B 41514 EA UNDER FWD BAFFLE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1037 L531351A (CAN) WHILE REMOVING THE #2 ENGINE TO FACILITATE REPLACEMENT OF A CRACKED ENGINE MOUNT, A 6" CRACK WAS FOUND ON THE CRAN KCASE, JUST AFT OF THE PROP UNDER THE FORWARD BAFFLE. THE ENGINE WAS REPLACED. 1 L 7 2 3O 3 O 3A16 1E10 1996121200291 19961212 00291 EA 1996 12 12 CA960626003 1 19960615 A 5413 C6W15125141 LONGERON DHAV DHAV DHC6 DHC6300 EA PWA PT6 PT6A27 52043 EA AFT OF ENG MT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 8309 PCE40096 (CAN) STARBOARD ENGINE NACELLE LONGERON FOUND CRACKED. CRACK WAS ABOUT 10 INCHES AFT OF THE ENGINE MOUNT. CRACK IS DESCR IBED IN SB 509 AND AD CF-81-07R4. 1 H 7 2 3T 4 T A9EA E4EA 1996121200292 19961212 00292 EA 1996 12 12 CA960626004 1 19960514 A 2720 C3CF1995 CONTROL CABLE DHAV DHC3 DHC3 2800202 EA RUDDER CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) RUDDER CONTROL CABLES RUNNING UNDER FLOOR IN LOWER RIGHT HAND SECTION FOUND BADLY CORRODED (INCLUDES P/N C3CF197-5 ) AT STA. 310, AND AFT OF REAR BAGGAGE COMPARTMENT BULKHEAD. THIS AREA ALSO BELOW AND AFT OF BATTERY RACK. AIRCRAFT HAD BEEN OPERATED IN SALT WATER FOR LAST THREE YEARS. 1 H 7 1 3R A815 1996121200293 19961212 00293 EU 1996 12 12 CA960626101 1 19960607 A 5210 NSA81450810 DOOR BUSHING AIRBUS D52111010034 AIRBUS 320 A320211 3930320 EU DOOR L2 LOOSE W D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CA (CAN) DOOR L2 WOULD NOT ARM ON PUSH BACK. MAINTENANCE INVESTIGATION REVEALED BUSHING PUSHED INTO LINING OF THE DOOR. FIT TING REPLACED. 2 L 7 2 4F RT A28NM 1996121200295 19961212 00295 NM 1996 12 12 CA960703006 1 19960601 A 5610 NP15790214 WINDOW TRIPLEX DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE RH COCKPIT NOISY W K NONE O OTHER IN INSP/MAINT 1 CA 3220993 120691 (CAN) PILOT REPORTED RIGHT HAND SIDE WINDOW MADE SQUEALING NOISE. WINDOW RETORQUED BUT PROBLEM STILL THERE. WINDOW REPLA CED. 2 H 7 2 4T 4 T RT A13NM E20NE 1996121200296 19961212 00296 EA 1996 12 12 CA960703011 1 19960603 A 2910 SELECTOR VALVE PARKERHANFIN 50420101 CNDAIR CL215 CL2151A10 EA WATER BOMB SYSTM BLOWN W A O UNSCHED LANDING OTHER K FLUID LOSS NR NOT REPORTED 1 CA 194 (CAN) AIRCRAFT LOST MAIN HYDRAULIC SYSTEM. LANDED USING EMERGENCY SYSTEM. WATER BOMBING PROBE SELECTOR VALVE REMOVED AND FOUND THAT THE REAR SCREW PLUG SEAL AND PLASTIC BACK UP RING HAD BLOWN OUT CAUSING HYDRAULIC PRESSURE LOSS. UNIT SENT T O OVERHAUL AGENT WHO SAID THAT 'O' RING HAD BEEN CUT BUT UNIT STILL PASSED THEIR HIGH PRESSURE TEST. 2 H 7 2 4R A14EA 1996121200299 19961212 00299 EA 1996 12 12 CA960703014 1 19960528 A 5312 C2FS533 BULKHEAD DHAV DHAV DHC2 DHC2MK3 2800107 EA PWA PT6 PT6A27 52043 EA AFT FS288 CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 9944 PCE51004 (CAN) AFT FULL BULKHEAD AT STA. 228 FOUND CRACKED ON BOTH LEFT AND RIGHT SIDES WHERE THE RUDDER CONTROL RODS PASS THROUG H THE BULKHEAD. CRACKS RADIATE FROM HOLES 3/32" TO 1/2" TOWARDS THE VERTICAL STAB ATTACHMENT. TWO OTHER AIRCRAFT WERE FO UND WITH SAME PROBLEMS. 1 H 7 1 3T 4 T A806 E4EA 1996121200300 19961212 00300 NM 1996 12 12 CA960703015 1 19960612 A 2760 WIRE 82740061016 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE RH UPPER SEVERED W K NONE O OTHER IN INSP/MAINT 1 CA 6049 120094 (CAN) AT 18 MONTH WING INSPECTION, AFT SPAR AREA ONE WIRE ON FLIGHT SPOILER CLUTCH FOUND BROKEN. IF ONE OF TWO SPOILER A CTUATORS JAMS, THE CLUTCH MAKES A SWITCH (P/N KX511), AND IN TURN WARNS THE PILOT OF AN ACTUATOR JAM PROBLEM. 2 H 7 2 4T 4 T RT A13NM E20NE 1996121200301 19961212 00301 NE 1996 12 12 CA960703016 2 19960623 A 8520 76270F FRONT CAM PWA CNDAIR CL215 CL2151A10 EA PWA R2800 CA3 52026 NE #2 ENGINE DAMAGED CAM W K NONE E VIBRATION/BUFFET TX TAXI/GRND HDL 1 CA 607 P35185 (CAN) ENGINE RUNNING ROUGH AND BACKFIRING ON INITIAL START-UP. INVESTIGATION REVEALED FRONT CAM MISSING PART OF A LOBE. FRONT CAM REPLACED AND AIRCRAFT TEST FLOWN SATISFACTORILY. 2 H 7 2 4R 4 R A14EA E231 1996121200302 19961212 00302 NM 1996 12 12 CA960703017 1 19960619 A 2910 12400110C0720 FLEX LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE #1 PRESSURE MANI CHAFED W D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 CA 121075 (CAN) A FLEX LINE IN THE LEFT WHEEL WELL CONNETING TO #1 SYSTEM PRESSURE MANIFOLD RUPTURED DUE TO CHAFING ON AN ADELL CL AMP. 2 H 7 2 4T 4 T RT A13NM E20NE 1996121200305 19961212 00305 NM 1996 12 12 CA960703029 1 19960617 A 2421 31708001A GENERATOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE #2 AC SYS FAILED W D RETURN TO BLOCK H ELECT. POWER LOSS-50 PC NR NOT REPORTED 1 CA 6660 701 120786 (CAN) ON DEPARTURE, #2 AC GENERATOR WENT OFF LINE AND COULD NOT BE RESET. GENERATOR REPLACED. SB 8-24-52 MAY APPLY HERE. 2 H 7 2 4T 4 T RT A13NM E20NE 1996121200306 19961212 00306 NE 1996 12 12 CA960703030 2 19960605 A 7314 5006488B FUEL PUMP DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE #2 ENG FAILED W A UNSCHED LANDING J X WARNING INDICATION ENGINE FLAMEOUT CR CRUISE 1 CA 20289 2680 647 120760 (CAN) #2 FUEL PRESSURE LIGHT AND #2 ENGINE 'MANUAL' LIGHT ON WITH AN ACCOMPANYING POWER ROLL-OFF. LANDING OK. FUEL PUMP REMOVED AND INTERNAL SPLINE COUPLING ROTOR FOUND LOOSE AND PUMP ROUGH RUNNING. 2 H 7 2 4T 4 T RT A13NM E20NE 1996121200307 19961212 00307 NM 1996 12 12 CA960703031 1 19960626 A 7603 87600520001 CABLE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE RT HAND COND FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA 14865 120339 (CAN) FOUND RH CONDITION LEVER CABLE FRAYED BEYOND LIMITS AT ENGINE FIREWALL PULLEY. 2 H 7 2 4T 4 T RT A13NM E20NE 1996121200308 19961212 00308 NM 1996 12 12 CA960703032 1 19960619 A 2760 MS2467715 BOLT 659603 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE FLIGHT SPOILER BROKEN W K NONE K FLUID LOSS DE DESCENT 1 CA 120358 (CAN) TWO BOLTS HAD HEAD SHEARED OFF FROM THE COVER OF THE FLIGHT SPOILER UNLOAD VALVE. THIS ALLOWED HYDRAULIC FLUID TO LEAK FROM #2 SYSTEM COMPLETELY DRAINING HYDRAULIC SYSTEM. 2 H 7 2 4T 4 T RT A13NM E20NE 1996121200309 19961212 00309 SO 1996 12 12 CA960704001 1 19960623 A 8120 IW12463 TURBOCHARGER PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA TURBINE SHAFT BEARING WORN W A C D E ABORTED TAKEOFF RETURN TO BLOCK ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 CA 930 E10122 L766761A (CAN) DURING TAKEOFF ROLL THE LEFT HAND ENGINE BEGAN TO LOOSE POWER. THE PILOT WAS INFORMED BY THE TOWER THAT BLACK SMOK E WAS COMING FROM THE LEFT HAND ENGINE. THE TAKEOFF WAS ABORTED AND THE LEFT HAND ENGINE WAS SHUTDOWN. POST FLIGHT INVES TIGATION FOUND OIL INSIDE THE TURBOCHARGER AND THE TURBINE WHEEL HAD APPROXIMATELY 1/4" OF MOVEMENT. A BEARING ON THE TU RBINE SHAFT WAS FOUND WORN. THE TURBOCHARGER WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 3O 3 O A20SO E14EA 1996121200310 19961212 00310 NE 1996 12 12 CA960704004 2 19960623 A 8520 76270F FRONT CAM CNDAIR CL215 CL2151A10 EA PWA R2800 CA3 52026 NE ENGINE DAMAGED LOBE W K NONE E VIBRATION/BUFFET TX TAXI/GRND HDL 1 CA 607 P35185 (CAN) ENGINE RUNNING ROUGH AND BACKFIRING ON INITIAL STARTUP. INVESTIGATION REVEALED FRONT CAM MISSING PART OF A LOBE. F RONT CAM REPLACED AND AIRCRAFT TEST FLOWN SERVICEABLE. 2 H 7 2 4R 4 R A14EA E231 1996121200312 19961212 00312 EA 1996 12 12 CA960704006 1 19960622 A 5280 1103 SKIN CNDAIR 21533001 CNDAIR CL215 CL2151A10 EA NLG DOOR TE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1548 1103 (CAN) NOSE LANDING GEAR DOOR EXTERIOR SKINS FOUND CRACKED AT TRAILING EDGES, BOTH DOORS REPAIRED IN ACCORDANCE WITH SRM 2 H 7 2 4R A14EA 1996121200313 19961212 00313 EA 1996 12 12 CA960704007 1 19960617 A 5280 1090 SKIN CNDAIR 21533001 CNDAIR CL215 CL2151A10 EA NLG DOOR TE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1479 1090 (CAN) NOSE LANDING GEAR DOOR EXTERIOR SKINS FOUND CRACKED ON TRAILING EDGE OF BOTH DOORSDOORS REPLACED IN ACCORDANCE WIT H SRM 2 H 7 2 4R A14EA 1996121200314 19961212 00314 EA 1996 12 12 CA960704008 1 19960615 A 5413 C6W15125141 LONGERON DHAV DHAV DHC6 DHC6300 EA PWA PT6 PT6A27 52043 EA RH INBOARD CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 8309 PCE40096 (CAN) STARBOARD ENGINE NACELLE LONGERON CRACKED. CRACK WAS APPROXIMATELY 10" AFT OF ENGINE MOUNT. CRACK FOUND IN AREA DE SCRIBED IN SB 509 AND AD CF-81-07R4. 1 H 7 2 3T 4 T A9EA E4EA 1996121200315 19961212 00315 CE 1996 12 12 CA960708002 1 19960627 A 3230 5045010 TORQUE TUBE CESSNA 401 401 207590C CE MCAULY 3AF32C 3AF32C87 GL R/H MAIN GEAR FRACTURED W A A UNSCHED LANDING J WARNING INDICATION LD LANDING 1 CA 9921 694701 (CAN) ON GEAR UP SELECTION AFTER TAKEOFF, A LOUD BANG WAS HEARD. THE AIRCRAFT CONTINUED AND AFTER GEAR DOWN SELECTION, T HE R/H MAIN GEAR FAILED TO INDICATE LOCKED. AIRCRAFT LANDED WITHOUT INCIDENT. IT APPEARED THAT TORQUE TUBE MAY HAVE BEEN CRACKED PREVIOUSLY AT ATTACH POINT FOR THE OPERATING ROD. A FLEET INSPECTION WAS COMPLETED WITH NO OTHER DEFECTS NOTED. PART IS INSPECTED AT EACH #3 CHECK EVERY 200 HOURS. 1 L 7 2 3O A7CE 5 C P22EA 1996121200316 19961212 00316 EA 1996 12 12 CA960708003 1 19960612 A 5523 C3TE134 SERVO TAB DHAV C3TE1106 DHAV DHC3 DHC3 2800202 EA PWA PT6 PT6A135 52043 NE RT ELEV TE RIPPED W A B EMER. DESCENT E VIBRATION/BUFFET CR CRUISE 1 CA FW372 PCE92739 (CAN) SLIGHT FLUTTER ON FINAL STAGE OF CLIMB. SEVERE FLUTTER AFTER LEVEL OUT IN CRUISE. INVESTIGATION FOUND THE RIGHT HA ND ELEVATOR SERVO TAB CONNECTING ROD ARM BORKEN OFF THE SERVO TAB. TAB WAS BENT AND BROKEN BUT STILL ATTACHED. TRAILING EDGE OF ELEVATOR SKIN LOOSE. CENTRE SPAR OF ELEVATOR BROKEN. SRVO TAB HAS SKIN SPLIT 7" FROM INBOARD END. SKIN ON TRAIL ING EDGE BENT UP 1 3/4", THEN STRAIGHT FOR 6", THEN TRAILING EDGE BENT DOWN FOR 2 7/16" AND THEN STRAIGHT UNTIL ACTUATIN G ATTACH POINT, WHERE ACTUATING ARM IS RIPPED OUT OF TAB. TAB APPEARS TO HAVE BEEN BENT UP ON TRAILING EDGE. 1 H 7 1 3R 4 T A815 E4EA 1996121200317 19961212 00317 NM 1996 12 12 CA960708004 1 19960701 A 5751 85711596053 BRACKET DHAV DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE LT RT AIL QUAD CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 123141 (CAN) BOTH LEFT AND RIGHT AILERON TERMINAL QUADRANT BRACKETS FOUND CRACKED AT LOWER ATTACHMENTS WHERE QUADRANT ATTACHES. ALSO P/N 85711596056. 2 H 7 2 4T 4 T RT A13NM E20NE 1996121200318 19961212 00318 EA 1996 12 12 CA960708006 1 19960620 A 5510 2152300385 STABILIZER CNDAIR 21523001882 CNDAIR CL215 CL2151A10 EA STA 120 LE CUT W K NONE O OTHER IN INSP/MAINT 1 CA 1597 (CAN) DAMAGE FOUND ON LEADING EDGE OF RIGHT HAND HORIZONTAL STABILIZER AT STATION 120. FURTHER INVESTIGATION FOUND UPPER AND LOWER EXHAUST CLAMP ASSEMBLIES ON CYLINDER 16 AND 17 HAD COME OFF DURING FLIGHT AND CUT LEADING EDGE STABILIZER 2.5 ". 2 H 7 2 4R A14EA 1996121200320 19961212 00320 NM 1996 12 12 CA960708008 1 19960628 A 3320 BA080061 BALLAST DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE ROW 8AB BURNT W K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA 120825 (CAN) CREW REPORTED CABIN ELECTRICAL SMELL. INVESTIGATION FOUND LIGHTING BALLAST AT ROW 8AB SHORTED. 2 H 7 2 4T 4 T RT A13NM E20NE 1996121200321 19961212 00321 NM 1996 12 12 CA960708009 1 19960701 A 3230 54C546349 SEQUENCE VALVE RONSON DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE NOSE WHEEL WELL LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 0280 123046 (CAN) CREW NOTICED HYDRAULIC FLUID LEAKING FROM NOSE WHEEL WELL. NOSE LANDING GEAR SEQUENCE VALVE FOUND LEAKING FROM A C RACK IN THE BODY. 2 H 7 2 4T 4 T RT A13NM E20NE 1996121200322 19961212 00322 EA 1996 12 12 CA960709004 1 19960704 A 5311 2CFS3282A STRUT DHAV DHAV DHC2 DHC2MK1 2800102 EA PWA R985 R985AN14B 52008 NE RIGHT HAND CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 14910 JP205745 (CAN) UPPER AND OUTBOARD SURFACE OF RIGHT HAND STRUT CORRODED ITS ENTIRE LENGTH UNDER WINDSHIELD RETAINING SIDE P/N C2FC 142ND. TUBE CORRODED THROUGH UPPER OUTBAORD CORNER 1 1/2" LONG APPROXIMATELY MIDWAY OF WINDSHIELD SIDE. SEVERE RUST AT O THER LOCATIONS. 1 H 7 1 3R 3 R A806 5E1 1996121200324 19961212 00324 EA 1996 12 12 CA960709006 2 19960614 A 8530 VALVE LIFTER PIPER PA32 PA32300 7103212 SO LYC O540 IO540K1A5 41532 EA #2 CYL EXHAUST BROKEN W A O OTHER E VIBRATION/BUFFET CR CRUISE 1 CA 15 L482048 (CAN) ROUGH ENGINE RUNNING LED TO INSPECTION WHICH REVEALED #2 CYLINDER EXHAUST VALVE LIFTER WAS BROKEN. ENGINE WAS REMO VED AND SENT TO R&O WHERE FAILURE WAS ATTRIBUTED TO MISASSEMBLY OF VALVE ROCKER ARMS, INTAKE FOR EXHAUST AND VICE VERSA, THIS CONDITION ALSO AFFECTED #3 CYLINDER. THE ENGINE WAS REPAIRED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1 L 7 1 3O 3 O A3SO 1E4 1996121200325 19961212 00325 WP 1996 12 12 CA960709008 1 19960629 A 2910 ER8334D ELBOW FITTING CVAC 340 340CVAC 242270A WP ALLSN 501D 501D13 03004 GL RH MLG HYD BROKEN W B EMER. DESCENT J K WARNING INDICATION FLUID LOSS CL CLIMB 1 CA 501662 (CAN) AFTER TAKEOFF DURING CLIMB AND FLAPS RETRACTED, ENGINE DRIVEN HYDRUALIC FAIL LIGHT ILLUMINATED. HYDRAULIC FLUID LE VEL INDICATED EMPTY. FLAPS EXTENDED USING D.C. PUMP AND LANDING GEAR EXTENDED USING EMERGENCY FREE FALL PROCEDURES. MAIN TENANCE INVESTIGATION REVEALED THAT AN ELBOW FITTING HAD BROKEN ON THE RH MAIN LANDING GEAR UPLINE. FITTING REPLACED. 2 L 7 2 4R 4 T 6A6 E282 1996121200326 19961212 00326 NM 1996 12 12 CA960709010 1 19960628 A 7170 82821013107 DRAIN LINE DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE #1 ENGINE NACELL CHAFED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 123141 (CAN) CREW ON WALKAROUND FOUND A FUEL LEAK IN #1 ENGINE NACELLE. SOURCE WAS A DRAIN LINE WHICH HAD CHAFED THROUGH. 2 H 7 2 4T 4 T RT A13NM E20NE 1996121200328 19961212 00328 EA 1996 12 12 CA960709012 1 19960628 A 2822 TF9005 FUEL PUMP TMPSON DHAV DHC3 DHC3 2800202 EA PWA R1340 R1340AN1 52016 NE ENG FUEL LOW PRESSURE W C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CA 494 TF209612 P327203 (CAN) FUEL PRESSURE DROPPED TO ZERO ON TAKEOFF RUN. PUMP SENT TO OVERHAUL. 1 H 7 1 3R 3 R A815 5E2 1996121200330 19961212 00330 EU 1996 12 12 CA960711004 1 19960705 A 2910 HDS1127710 O-RING 3549H1 BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE GREEN HYD SYS LEAKING W D RETURN TO BLOCK B K SMOKE/FUMES/ODORS/SPARKS FLUID LOSS TX TAXI/GRND HDL 1 CA 17823 17823 LF05627A (CAN) WHILE AIRCRAFT WAS TAXIING FOR TAKEOFF AN O-RING ON THE GREEN HYDRAULIC SYSTEM HIGH PRESSURE FILTER FAILED ALLOWIN G FUMES INTO THE CABIN. AIRCRAFT EVACUATED. O-RING FROM AREA WHICH DOES NOT REQUIRE ONGOING MAINTENANCE AND IS BELIEVED TO BE ORIGINAL. ON REMOVAL SHAPE OF O-RING INDICATED IT WAS INSTALLED PINCHED ON ONE SIDE AND THROUGH TIME WORKED ITS WA Y OUT TO A POINT WHERE A TINY LEAK OCCURRED CAUSING FINE MIST WHICH FOUND ITS WAY INTO THE CABIN. 2 H 7 4 4F 4 F RT A49EU E6NE 1996121200331 19961212 00331 NM 1996 12 12 CA960711005 1 19960705 A 2761 82950010307 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE ROLL SPOILER CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 120083 (CAN) HYDRAULIC LEAK FROM RIGHT HAND FLAP AREA. LINE TO ROLL SPOILER ACTUATOR FOUND LEAKING. 2 H 7 2 4T 4 T RT A13NM E20NE 1996121200332 19961212 00332 NE 1996 12 12 CA960711006 2 19960710 A 7261 42D107A1 SWITCH OIL PRESS BOEING 737 737275 1384485 NM PWA JT8 JT8D17A 52049 NE ENG OIL SYSTEM DEFECTIVE W A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 CA 20475 P707411B (CAN) #2 ENGINE WAS SHUTDOWN IN FLIGHT, AIRCRAFT DIVERTED, DUE TO ENGINE OIL FILTER BYPASS LIGHT ON. OIL BYPASS PRESSURE SWITCH REPLACED. FURTHER TROUBLESHOOTING TO BE CARRIED OUT AS FILTER BYPASS LIGHT DID NOT GO OUT ON ENGINE START UP. 2 L 7 2 4F 4 F A16WE E2EA 1996121200335 19961212 00335 EU 1996 12 12 CA960711016 1 19960622 A 2613 TEMP SWITCH GRAVINER BRAERO 748 HS7482A 4231001 EU ENG OHEAT FAULTY W E ENGINE SHUTDOWN L M NO TEST OVER TEMP DE DESCENT 1 CA (CAN) PILOT REPORT INDICATED THE ENGINE OVERHEAT LIGHT ILLUMINATED IN FLIGHT, BUT ALL OTHER PARAMETERS WERE NORMAL. STAN DARD EMERGENCY PROCEDURES WERE FOLLOWED AND THE ENGINE WAS SHUTDOWN. MAINTENANCE CHECKED OUT THE SYSTEM AND REPLACED THE OVERHEAT DETECTOR. GROUND RUNS WERE CARRIED OUT SERVICEABLE AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 3T A24EU 1996121200336 19961212 00336 EA 1996 12 12 CA960712102 2 19960704 A 7313 LW11218 FUEL INJECTOR PIPER PA60 PA60600 7106001 NM LYC O540 IO540G1B5 41532 EA ENG LOOSE HARDWARE W K NONE O OTHER IN INSP/MAINT 1 CA L1298648A (CAN) DURING ROUTINE INSPECTION OF AN AEROSTAR FUEL INJECTOR, SECURING HARDWARE (PAL-NUTS) WERE FOUND TO BE MISSING OR LOOSE. 1 M 7 2 3O 3 O RT A17WE 1E4 1996121200338 19961212 00338 WP 1996 12 12 CA960715007 1 19960704 A 2421 729641A GENERATOR LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB21122B02 54555 NE #1 ENG IDG FAULTY W K NONE J WARNING INDICATION CR CRUISE 1 CA 460 10171 (CAN) TWO HOURS AFTER TAKEOFF #1 ENGINE IDG LOW PRESSURE LIGHT CAME ON. GENERATOR VOLTAGE AND FREQUENCY WENT TO ZERO. PO ST FLIGHT MAINTENANCE CHECK FOUND IDG OVERHEATED. IDG AND OIL COOLER REPLACED. 2 L 7 3 4F 4 F A23WE E12EU 1996121200339 19961212 00339 CE 1996 12 12 CA960715011 1 19960701 A 2434 633962 ALTERNATOR CESSNA 337 337G 2075730 CE CONT O360 IO360G 17025 SO DRIVE SHAFT BROKEN SHAFT W A K NONE H ELECT. POWER LOSS-50 PC CR CRUISE 1 CA 1172 352415 (CAN) THE ALTERNATOR DRIVE SHAFT FAILED AT THE BASE OF THE ALTERNATOR. THIS SHAFT APPEARED TO BE CRACKED OR HAD A PREVIO US FLAW. THIS ALLOWED THE REMAINING SHAFT AND DRIVE GEAR TO MOVE FORWARD RUBBING ON THE CAM GEAR. THE RUBBER BUSHING, P/ N 632050, AND METAL RETAINER, P/N 352030, WERE TOTALLY DESTROYED. THE OIL FILTER WAS REMOVED AND FOUND FREE OF CONTAMINA TES. THE ENGINE SCREEN WAS REMOVED AND FOUND FULL OF RUBBER AND METAL DEBRIS. THE ENGINE HAS BEEN REMOVED DUE TO OIL SYS TEM CONTAMINATION. 1 H 7 2 3O 3 O A6CE E1CE 1996121200342 19961212 00342 GL 1996 12 12 CA960719103 1 19960708 A 7500 6876294 LINE HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL FCU CRACKED W K NONE R PARTIAL RPM/PWR LOSS IN INSP/MAINT 1 CA 9123 CAE830700 (CAN) AT LOWER POWER SETTINGS, ENGINE UNDER SPEC FOR POWER. AT HIGHER POWER SETTINGS (MAX TORQUE) ENGINE ON SPEC FOR PO WER. FOUND RIGID LINE BETWEEN BLEED VALVE AND ENGINE COMPRESSOR CRACKED ALL THE WAY AROUND THE TUBE UNDER THE 'B' NUT. LINE REPLACED. 1 G 7 1 3U 3 U H3WE E4CE 1996121200344 19961212 00344 EA 1996 12 12 CA960722003 1 19960708 A 7930 02871228 GAUGE OIL PRESS DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE #2 ENGINE FAULTY W D C RETURN TO BLOCK ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CA 02871228 123135 (CAN) PILOT REPORTED LOW OIL PRESSURE INDICATION ON #2 ENGINE ON TAKEOFF ROLL MAINTENANCE REPLACED THE #2 ENGINE DUAL O IL PRESSURE/TEMPERATURE GAUGE, S/N "ON" 06890149, S/N "OFF" 02871228GROUND RUN FUNCTIONAL TEST SATISFACTORY, AIRCRAFT RE TURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 1996121200345 19961212 00345 EA 1996 12 12 CA960722005 2 19960714 A 7200 ENGINE BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA #1 ENGINE MAKING METAL W A K NONE O OTHER CR CRUISE 1 CA PCE50944 (CAN) DURING FLIGHT THE #1 ENGINE OIL PRESSURE WAS LOWER AND THE OIL TEMPERATURE HIGHER THAN NORMAL, WITH THE TORQUE IND ICATION FLUCTUATING. THE ENGINE OIL SCREEN WAS PULLED AND FOUND CONTAMINATED WITH BRASS/BRONZE AND STEEL FLECKS OF METAL . ENGINE WAS REMOVED FOR TEARDOWN INVESTIGATION. STRIP REPORT WILL FOLLOW. 1 L 7 2 3T 4 T A14CE E4EA 1996121200347 19961212 00347 NE 1996 12 12 CA960723014 2 19960628 A 8530 CYLINDER DHAV DHC3 DHC3 2800202 EA PWA R1340 R134051 52016 NE NR 1 CRACKED W K NONE E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 CA 239 B12081 419736 (CAN) ENGINE EXPERIENCING BACKFIRING AND LOSS OF POWER. INVESTIGATION FOUND NR 1 CYLINDER HEAD CRACKED AROUND THE ROCKE R BOX COVER. 1 H 7 1 3R 3 R A815 5E2 1996121200348 19961212 00348 NM 1996 12 12 CA960724005 1 19960718 A 2435 STARTER BOEING 727 727217 NM PWA JT8 JT8D17 52049 NE #2 ENGINE DISINTEGRATED W A A E F UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. A FLAME/FIRE CL CLIMB 1 CA 120 688735 (CAN) 5-8 MINUTES AFTER TAKEOFF THE #2 ENGINE FIRE ALARM SOUNDED, THE FIRST FIRE BOTTLE WAS DISCHARGED. WARNING LIGHT DI D NOT GO OUT SO SECOND FIRE BOTTLE WAS DISCHARGED 30 SECONDS LATER. LIGHT WENT OUT AFTER 5 MINUTES. AIRCRAFT DECLARED EM ERGENCY LANDING AND RETURNED TO POINT OF DEPARTURE. POST FLIGHT INSPECTION OF #2 ENGINE FOUND LOWER HALF FROM 6 O'CLOCK TO 8 O'CLOCK POSITION COMPONENTS (IGNITER BOX, GEARBOX, EXCITER, OIL COOLER, ASSOCIATED WIRING, LINES, ETC.) WERE BURNT. THE #2 ENGINE STARTER WAS FOUND DISINTEGRATED AND THE IMPELLER HOUSING HAD BURST. ENGINE WAS REMOVED FOR INVESTIGATION AND REPAIR. #2 ENGINE UPPER SUPPORT STRUCTURE SHOW SIGNS OF BURNING. AIRCRAFT IS STILL UNDER INVESTIGATION. 2 L 7 3 4F 4 F RT A3WE E2EA 1996121200355 19961212 00355 SO 1996 12 12 96ZZZX5951 1 19961008 A 3244 0613210 TIRE PIPER PA23 PA23250 7102308 SO LT MLG BLOWN A VLLA O OTHER O OTHER LD LANDING 1 GL 05 62650 282 4222000399 277654115 AFTER LANDING, PILOT APPLIED BRAKES. LT MAIN WHEEL LOCKED UNTIL TIRE WORE THROUGH TO TUBE AND LOST ITS AIR CHARGE. A V ISUAL AND OPERATIONAL CHECK OF BRAKES FOUND NO PROBLEMS. BRAKES WERE TESTED DURING TAXIING AND WERE FOUND SATISFACTORY. 1 L 7 2 3O 1A10 1996121200362 19961212 00362 CE 1996 12 12 96ZZZX5958 1 19961114 A 2810 082340063 BULKHEAD CESSNA 402 402B 207590P CE LT MAIN TANK CRACKED A OEZA K NONE O OTHER IN INSP/MAINT 1 WP 19 765EA 14032 402B0314 DURING WING INSPECTION, FOUND LEFT MAIN FUEL TANK AFT BULKHEAD HAD CRACKED. REPLACED BULKHEAD WITH NEW FROM CESSNA. SU SPECT THE REASON FOR THE FAILURE IS THE RELATIVE HIGH TIME OF THE AIRPLANE. 1 L 7 2 3O A7CE 1996121200377 19961212 00377 CE 1996 12 12 96ZZZX5974 1 19961101 A 3297 WIRE LEAR 25 25 5170506 CE THROTTLE QUAD DEFECTIVE A KKFA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 28CK 045 LANDING GEAR UNSAFE LIGHTS STAYED ON WITH GEAR UP. REPAIRED SWITCH WIRES AND ROLLERS IN THROTTLE QUADRANT. CLEANED ARE A. CYCLED GEAR, OPS CHECK GOOD. 2 L 7 2 4J A10CE 1996121200383 19961212 00383 1996 12 12 96ZZZX5980 4 19961121 A 3452 066011415101 TRANSPONDER CESSNA 208 208B 2073701 CE COCKPIT INOPERATIVE A AWHA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 17 744FX 405 2172 208B0492 PILOT REPORTED ELECTRICAL SMELL IN COCKPIT, NO VISIBLE SMOKE. HE DECLARED AN EMERGENCY AND PROCEEDED TO ISOLATE, ELECTR ICAL SYSTEMS. LANDING WAS UNEVENTFUL. MAINTENANCE INSPECTED THE AIRCRAFT WIRING, CIRCUIT BREAKERS, AND SWITCHES AND CO ULD FIND NO DISCREPANCIES. THE NR 2 TRANSPONDER WAS FOUND TO BE INOPERATIVE. THE FAULTY TRANSPONDER WAS REPLACED AND C ERTIFIED. THE AIRCRAFT WAS TEST FLOWN WITH NO DISCREPANCIES NOTED. THE AIRCRAFT IS RETURNED TO SERVICE. 1 H 7 1 3T A37CE 1996121200386 19961212 00386 NM 1996 12 12 RAAA96B2045 1 19961208 A 3530 4566M37B042NM PBE BOEING 727 72722C 138400F NM COCKPIT FAILED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SERVICE CHECK, FOUND COCKPIT PBE RED INDICATOR PIN PROTRUDING. CHANGED PBE DUE SEAL FAILURE. 2 L 7 3 4F A3WE 1996121200387 19961212 00387 SO 1996 12 12 RAAA96E4016 1 19961206 A 5311 FRAME LKHEED 188 188C 5262604 SO BS 939 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 3 CHECK, FOUND FS 939 SHEAR TIE CORRODED AT STRINGER 44 TO 45. REPAIRED PER SRM 53-2-3, FIG 2. 2 L 7 4 4T 4A22 1996121200388 19961212 00388 SO 1996 12 12 RAAA96E4017 1 19961206 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 135 BROKEN A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 3 CHECK, FOUND FS 135 FLOORBEAM UPPER CHORD BROKEN AT FASTENER HOLE AT LBL 40. REPAIRED PER SRM 51- 3-8, FIG 1. 2 L 7 4 4T 4A22 1996121200389 19961212 00389 SO 1996 12 12 RAAA96E4018 1 19961206 A 5720 DOUBLER LKHEED 188 188C 5262604 SO WS 151 DEBONDED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 3 CHECK, FOUND FUEL SEEP FROM RIGHT WING PREVIOUS REPAIR WS 151 AT NR 1 PLANK. REPLACED REPAIR DOUB LERS PER S/B 653 AND LAC DRAWING NR 841441. 2 L 7 4 4T 4A22 1996121200390 19961212 00390 SO 1996 12 12 RAAA96E4019 1 19961206 A 5720 DOUBLER LKHEED 188 188C 5262604 SO WS 79 DEBONDED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 3 CHECK, FOUND FUEL SEEP FROM RIGHT WING PREVIOUS REPAIR WS 79 AT NR 1 PLANK. REPAIRED PER SRM 57-2 -1, PG 23. 2 L 7 4 4T 4A22 1996121200391 19961212 00391 SO 1996 12 12 RAAA96E4020 1 19961206 A 5330 SKIN LKHEED 188 188C 5262604 SO BS 146 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 3 CHECK, FOUND FUSELAGE SKIN CORRODED FS 146 AT S-15. REPAIRED PER SRM 53-2-1, FIG 2. 2 L 7 4 4T 4A22 1996121200392 19961212 00392 SO 1996 12 12 RAAA96E4021 1 19961206 A 5330 SKIN LKHEED 188 188C 5262604 SO BS 245-255 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 3 CHECK, FOUND FUSELAGE SKIN CORRODED UNDER PREVIOUS REPAIR FS 245 TO 255, S-23 TO S-31. REPLACED F USELAGE SKIN FROM FS 236 TO 274 AND S-23 TO S-31 PER SRM 51-2-9. REPAIRED FWD CARGO COMPT DOOR CUTOUT SKIN PER SRM 53-2 -1, FIG 2, SHEET 6. 2 L 7 4 4T 4A22 1996121200393 19961212 00393 SO 1996 12 12 RAAA96E4022 1 19961206 A 3350 S102 BATTERY PACK LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST CR CRUISE 1 AL 03 9744C 188C1140 MAIN CABIN DOOR EMERGENCY PULLDOWN LIGHT ASSY FLASHED ON AND OFF DURING FLIGHT. REPLACED BATTERY PACK DUE FAILED. 2 L 7 4 4T 4A22 1996121200394 19961212 00394 SO 1996 12 12 RAAA96E4023 1 19961207 A 3350 S102 BATTERY PACK LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 9744C 188C1140 RT AFT EMERGENCY EXIT PULLDOWN LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE LOW CHARGE. 2 L 7 4 4T 4A22 1996121200395 19961212 00395 SO 1996 12 12 RAAA96E8036 1 19961206 A 3211 HSP36102 BEARING MENASCO 80579425 LKHEED 188 188C 5262604 SO RT MLG CONTAMINATED A A RAAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 178RV A2095 188C2010 ON CLIMBOUT, CREW NOTED LANDING GEAR SLOW TO RETRACT AND UNSAFE LIGHT ON RT MLG. LDG CONTROL HANDLE TO NEUTRAL POSITION . CYCLED, LDG CONTROL HANDLE TO DOWN WITH 3 SAFE LIGHTS. RETURNED TO ANC AND LANDED OVERWEIGHT WITHOUT INCIDENT. ACCO MPLISHED OVERWEIGHT LANDING INSPECTION. REPLACED BOTH RT MLG FWD DOORS DUE DAMAGE FROM RAPID CYCLING OF LDG. REPLACED RT MLG DOOR ACTUATOR DUE LEAK AT VENT. REPLACED NR 1 HYD SYS PRESSURE LINE DUE LEAK. LUBED LDG, GEAR RETRACTION TEST N ORMAL. SUSPECT FROZEN MOISTURE IN RT MLG INBD TRUNNION BEARING DUE WATER EXPELLED WHEN LUBED. 2 L 7 4 4T 4A22 1996121200396 19961212 00396 NM 1996 12 12 CALA9601732 1 19961205 A 2910 6544510696 HYD LINE BOEING 737 737222 1384473 NM A-HYD SYST RUPTURED A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 12235 19758 THE A-SYSTEM HYDRAULIC QUANTITY WAS LOST APPROXIMATELY 15 MINUTES INTO FLIGHT. THE LOSS WAS ACCOMPANIED BY ILLUMINATION OF THE NR 1 AND NR 2 PUMP LOW PRESSURE LIGHTS. THE LOSS OF HYD SYSTEM-A QTY CHECKLIST WAS COMPLETED AND THE AIRCRAFT W AS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A-SYSTEM PRESSURE HYDRAULIC FLEX LINE IN THE LT FLAP WELL INBOARD OF ENGINE PYLON RUPTURED. THE LINE WAS REMOVED AND REPLACED AND LEAK CHECK WAS GOOD. 2 L 7 2 4F A16WE 1996121200397 19961212 00397 NM 1996 12 12 CALA9601733 1 19961125 A 5330 PANEL BOEING 727 727224 1384076 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79746 22449 INSPECTION FOUND AREA AROUND AFT LAVATORY SERVICE PANEL FILL AND DRAIN PIPE BULGED WITH CORROSION. THE PAN AND DOUBLER WERE REMOVED, A REPLACEMENT DOUBLER AND ANGLE WERE FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-10-6, 51-20-2 AND 51-30- 2. 2 L 7 3 4F A3WE 1996121200398 19961212 00398 NM 1996 12 12 CALA9601734 1 19961122 A 5523 SKIN BOEING 727 727224 1384076 NM LT ELEV TAB DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79746 22449 INSPECTION FOUND LT ELEVATOR CONTROL TAB UPPER SKIN DELAMINATED. A FIBERGLASS OVERLAY REPAIR WAS ACCOMPLISHED IAW SRM 5 1-40-6. 2 L 7 3 4F A3WE 1996121200399 19961212 00399 NM 1996 12 12 CALA9601735 1 19961122 A 5522 SKIN BOEING 727 727224 1384076 NM RT ELEVATOR PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79746 22449 INSPECTION FOUND RT ELEVATOR UPPER SKIN HAD A HOLE AND LOOSE RIVETS JUST FORWARD OF INBOARD CONTROL TAB. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 55-20-3. 2 L 7 3 4F A3WE 1996121200400 19961212 00400 NM 1996 12 12 CALA9601736 1 19961122 A 5730 SKIN BOEING 727 727224 1384076 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79746 22449 INSPECTION FOUND A .75 INCH CRACK IN LT WING FIXED LEADING EDGE AT CUTOUT WHERE NR 3 SLAT OUTBOARD TRACK INSERTS. THE C RACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-30-4. 2 L 7 3 4F A3WE 1996121200401 19961212 00401 NM 1996 12 12 CALA9601737 1 19961122 A 5720 ANGLE BOEING 727 727224 1384076 NM WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79746 22449 INSPECTION FOUND A 2.6 INCH CRACK AT ANGLE BELOW INBOARD STOP FITTING AT NR 3 SLAT. THE CRACK WAS STOP DRILLED, AN EXTR UDED ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-4. 2 L 7 3 4F A3WE 1996121200402 19961212 00402 NM 1996 12 12 CALA9601738 1 19961122 A 5720 DOUBLER BOEING 727 727224 1384076 NM RT WING TIP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79746 22449 INSPECTION FOUND A .75 INCH CRACK IN RT WING TIP TRAILING EDGE LOWER DOUBLER. THE DOUBLER WAS REMOVED AND A REPLACEMENT WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1996121200403 19961212 00403 NM 1996 12 12 CALA9601739 1 19961122 A 5754 RIB BOEING 727 727224 1384076 NM NR 5 SLAT ACT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79746 22449 INSPECTION FOUND A 1 INCH CRACK IN RT WING NR 5 SLAT ACTUATOR OUTBOARD ATTACH RIB AND A .5 INCH CRACK IN INBOARD ATTACH RIB OF NR 5 SLAT ACTUATOR. THE CRACKS WERE STOP DRILLED, ANGLE REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 51-40-3. 2 L 7 3 4F A3WE 1996121200404 19961212 00404 NM 1996 12 12 CALA9601740 1 19961122 A 5754 RIB BOEING 727 727224 1384076 NM NR 6 SLAT ACT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79746 22449 INSPECTION FOUND A .5 INCH CRACK IN RT WING NR 6 SLAT OUTBOARD TRACK INBOARD ATTACH RIB AND A .5 INCH CRACK IN INBOARD T RACK OUTBOARD ATTACH RIB OF NR 6 SLAT. THE CRACKS WERE STOP DRILLED, DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51- 40-3. 2 L 7 3 4F A3WE 1996121200405 19961212 00405 NM 1996 12 12 CALA9601741 1 19961119 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 294.5-312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17316 23367 INSPECTION FOUND INTERCOSTAL CORRODED BETWEEN STA 294.5 AND 312, RBL 12. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW S RM 51-10-02. 2 L 7 2 4F RT A16WE 1996121200406 19961212 00406 NM 1996 12 12 CALA9601742 1 19961119 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 328-344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17316 23367 INSPECTION FOUND INTERCOSTAL CORRODED BETWEEN STA 328 AND 344, RBL 10. REPAIRED IAW ECRA 5310-03368. 2 L 7 2 4F RT A16WE 1996121200407 19961212 00407 NM 1996 12 12 CALA9601743 1 19961118 A 5754 SKIN BOEING 737 7373T0 1384582 NM NR 1 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17316 23367 INSPECTION FOUND .25 INCH CRACKS AROUND RIVET HEADS OF LT WING NR 1 SLAT SKIN NEAR ACTUATOR. REPAIRED IAW ECRA 5700-011 59. 2 L 7 2 4F RT A16WE 1996121200408 19961212 00408 NM 1996 12 12 CALA9601744 1 19961119 A 5320 ANGLE BOEING 737 7373T0 1384582 NM BS 540 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17316 23367 INSPECTION FOUND A 2 INCH CRACK ON ANGLE BRACKET AT FUSELAGE STA 540, STRINGER 23L. A NEW PART WAS INSTALLED IAW SRM 51 -70-11. 2 L 7 2 4F RT A16WE 1996121200409 19961212 00409 NM 1996 12 12 CALA9601745 1 19961119 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 294.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17316 23367 INSPECTION FOUND CORROSION ON INTERCOSTAL JUST AFT OF STA 294.5, RBL 17. REPAIRED IAW ECRA 5310-03368. 2 L 7 2 4F RT A16WE 1996121200410 19961212 00410 NM 1996 12 12 CALA9601746 1 19961119 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 294.5-277 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17316 23367 INSPECTION FOUND INTERCOSTAL CORRODED BETWEEN STA 294.5 AND 277, LBL 10. AN ANGLE REPAIR WAS INSTALLED IAW ECRA 5310-03 368. 2 L 7 2 4F RT A16WE 1996121200411 19961212 00411 NM 1996 12 12 CALA9601747 1 19961123 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 1006 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17316 23367 INSPECTION FOUND FLOORBEAM CORRODED AROUND FASTENER HOLES AT STA 1006, RBL 10. REPAIRED USING DOUBLERS IAW SRM 53-30-51 . 2 L 7 2 4F RT A16WE 1996121200412 19961212 00412 NM 1996 12 12 CALA9601748 1 19961119 A 5311 FRAME BOEING 737 7373T0 1384582 NM BS 847 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17316 23367 INSPECTION FOUND AFT CARGO COMPARTMENT AFT DOOR FRAME CORRODED ON FORWARD SIDE AT STA 847, STRINGER 24R TO 26R. THE COR RODED AREA WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-70-11. 2 L 7 2 4F RT A16WE 1996121200413 19961212 00413 NM 1996 12 12 CALA9601749 1 19961124 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM BS 986-1006 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17316 23367 INSPECTION FOUND RT AFT LAV FLOOR SUPPORT CORRODED AT NUTPLATE HOLE STA 986 TO 1006. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 1996121200414 19961212 00414 NM 1996 12 12 CALA9601750 1 19961119 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 312-328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17316 23367 INSPECTION FOUND INTERCOSTALS CORRODED BETWEEN STA 312 TO 328, LBL10 AND RBL 10. THE INTERCOSTALS WERE REMOVED AND REPL ACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 1996121200415 19961212 00415 NM 1996 12 12 CALA9601751 1 19961119 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17316 23367 INSPECTION FOUND CORROSION IN SEVERAL PLACES ON FLOORBEAM AT R-1 DOOR, STA 328. A FLOORBEAM AND SPLICE REPAIR WAS INSTA LLED IAW SRM 51-10-51. 2 L 7 2 4F RT A16WE 1996121200416 19961212 00416 NM 1996 12 12 CALA9601752 1 19961119 A 5320 STRAP BOEING 737 7373T0 1384582 NM BS 1020 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17316 23367 INSPECTION FOUND LT AFT LAV STRAP CORRODED AT BS 1020, LBL 18.32. REPAIRED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 1996121200417 19961212 00417 NM 1996 12 12 CALA9601753 1 19961119 A 5320 STRAP BOEING 737 7373T0 1384582 NM BS 1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17316 23367 INSPECTION FOUND LT AFT LAV STRAP CORRODED AT BS 1016, LBL 3. REPAIRED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 1996121200418 19961212 00418 NM 1996 12 12 CALA9601754 1 19961119 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM BS 1006-1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17316 23367 INSPECTION FOUND LT AFT LAV FLOOR SUPPORT CORRODED AT BS 1006 TO 1016. REPAIRED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 1996121200419 19961212 00419 NM 1996 12 12 CALA9601755 1 19961119 A 5320 CHANNEL BOEING 737 7373T0 1384582 NM BS 990 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17316 23367 INSPECTION FOUND RT AFT LAV U-CHANNEL CORRODED AT BS 990. A NEW U-CHANNEL WAS INSTALLED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 1996121200420 19961212 00420 NM 1996 12 12 CALA9601756 1 19961119 A 5320 STRAP BOEING 737 7373T0 1384582 NM BS 1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17316 23367 INSPECTION FOUND RT AFT LAV STRAP CORRODED AT BS 1016, RBL 27. REPAIRED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 1996121200421 19961212 00421 NM 1996 12 12 CALA9601757 1 19961119 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM BS 1006-1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17316 23367 INSPECTION FOUND RT AFT LAV FLOOR SUPPORT CORRODED AT NUTPLATE, BS 1006 TO 1016. THE FLOOR SUPPORT WAS REMOVED AND REPL ACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 1996121200422 19961212 00422 NM 1996 12 12 CALA9601758 1 19961119 A 5320 STRAP BOEING 737 7373T0 1384582 NM BS 1020 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17316 23367 INSPECTION FOUND LT AFT LAV STRAP CORRODED AT BS 1020, LBL 27.85. REPAIRED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 1996121200423 19961212 00423 NM 1996 12 12 CALA9601759 1 19961119 A 5320 STRAP BOEING 737 7373T0 1384582 NM BS 1020 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17316 23367 INSPECTION FOUND RT AFT LAV STRAP CORRODED AT NUTPLATE, BS 1020, RBL 3. REPAIRED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 1996121200424 19961212 00424 NM 1996 12 12 CALA9601760 1 19961119 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM BS 986-1006 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17316 23367 INSPECTION FOUND LT AFT LAV FLOOR SUPPORT CORRODED FROM BS 986 TO 1006. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 1996121200425 19961212 00425 WP 1996 12 12 9626031228 1 19961209 A 3620 PNEU IND SYST DOUG DC10 DC1030 3023501 WP NR 2 MALFUNCTIONED A NWAA A J UNSCHED LANDING DUMP FUEL N FALSE WARNING CR CRUISE 1 GL 01 228NW 46578 DURING CRUISE, THE NR 2 MANIFOLD FAIL LIGHT ILLUMINATED. FLIGHT DIVERTED TO NRT AND DUMPED 30,000 LBS OF FUEL. NR 2 PN EUMATIC INDICATION SYSTEM WAS PLACED ON MEL 36-1D AND 36-10A. 2 L 7 3 4F A22WE 1996121200426 19961212 00426 NE 1996 12 12 9626046739 2 19961204 A 7520 TCC DUCT BOEING 747 747251F 1384898 NM PWA JT9 JT9D7Q 52054 NE NR 1 ENGINE BLOWN A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 639US 23887 702058 DURING CLIMB, THE NR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED. CREW SHUT DOWN THE NR 1 ENGINE AND DISCHARGED THE FIRE BO TTLE. AIRCRAFT RETURNED TO NRT AND LANDED WITHOUT INCIDENT. FOUND THE TURBINE CASE COOLING DUCT BLOWN. REPLACED THE N R 1 ENGINE, OPEATIONAL CHECK GOOD. 2 L 7 4 4F 4 F A20WE E3NE 1996121200427 19961212 00427 NM 1996 12 12 9626052705 1 19961203 A 3010 ANTI-ICE DUCT BOEING 727 727225 1384077 NM AFT FUSELAGE FAILED A NWAA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 GL 01 802EA 22433 DURING CLIMB SHORTLY AFTER WING ANTI-ICE WAS TURNED ON, A THUMP WAS HEARD IN THE TAIL COMPARTMENT FOLLOWED BY A LOWER AF T BODY OVERHEAT INDICATION. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED BLOWN ANTI-ICE DUCT ON LEFT SIDE OF AFT VENTRAL AIRSTAIR COMPARTMENT. OPERATIONAL CHECK OF ANTI-ICE SYSTEM CHECKED NORMAL. 2 L 7 3 4F A3WE 1996121200428 19961212 00428 NM 1996 12 12 9626062707 1 19961205 A 2530 OVEN BOEING 727 727225 1384077 NM GALLEY SMOKING A NWAA A J H UNSCHED LANDING DUMP FUEL DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 816EA 22553 DURING CLIMB, FLIGHT ATTENDANT REPORTED SMOKE COMING FROM FIRST CLASS GALLEY OVENS. AIRCRAFT DUMPED FUEL AND RETURNED T O FLL AND LANDED WITHOUT INCIDENT. MAINTENANCE DEACTIVATED FIRST CLASS GALLEY OVENS BY PULLING CIRCUIT BREAKERS. OVENS WERE PLACED ON MEL. 2 L 7 3 4F A3WE 1996121200429 19961212 00429 NM 1996 12 12 9626072298 1 19961205 A 3010 ANTI-ICE DUCT BOEING 727 727251 138408H NM AFT FUSELAGE FAILED A NWAA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 GL 01 298US 22152 DURING CLIMB, A LOUD BANG WAS HEARD IN THE AFT VENTRAL STAIRS FOLLOWED BY A LOWER AFT BODY OVERHEAT INDICATION. AIRCRAF T DUMPED FUEL AND RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED TWO RUPTURED DUCTS IN AFT VENTRAL STAIR AREA AN D PT2 LINES. PERFORMED LEAK CHECK OF PITOT STATIC SYSTEM AND PNEUMATIC SYSTEM, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996121200430 19961212 00430 WP 1996 12 12 9626089163 1 19961203 A 3260 POSITION SWITCH DOUG DC9 DC914 3022034 WP RT MLG MALFUNCTIONED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 8906E 45747 ON APPROACH, GREEN LIGHT ON RIGHT MAIN GEAR DID NOT ILLUMINATE AFTER GEAR EXTENDED. RECYCLED GEAR WITH STILL NO GREEN A ND NO RED INTRANSIT LIGHT. FOLLOWED COM PROCEDURE AND GREEN LIGHT ILLUMINATED. FLIGHT LANDED WITHOUT INCIDENT. REPLAC ED BOTH RIGHT MAIN GEAR POSITION SWITCHES, SYSTEM FUNCTIONALLY TESTED OK. 2 L 7 2 4F A6WE 1996121200431 19961212 00431 NE 1996 12 12 9626096729 2 19961207 A 7320 PS4 LINE BOEING 747 747251F 1384898 NM PWA JT9 JT9D7F 52054 NE NR 2 ENIGNE RUPTURED A NWAA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 GL 01 251F 22388 689563 DURING CRUISE, THE NR 2 ENGINE FAILED TO OBTAIN NORMAL POWER. AIRCRAFT RETURNED TO ANC AND LANDED WITHOUT INCIDENT. R EPLACED PS4 LINE BETWEEN ENGINE CASE AND COMPRESSOR BLEED CONTROL, OPERATIONAL CHECK OK. 2 L 7 4 4F 4 F A20WE E20EA 1996121200432 19961212 00432 EU 1996 12 12 9626103237 1 19961207 A 3242 BRAKES AIRBUS 320 A320212 EU RT MLG DRAGGING A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 337NW 358 DURING TAKEOFF ROLL, RECEIVED BRAKES HOT MESSAGE AND ACCELERATION SEEMED SLUGGISH. TAKEOFF WAS ABORTED AT 80 KNOTS. AI RCRAFT RETURNED TO THE GATE WHERE MAINTENANCE FOUND THE NR 3 TIRE DEFLATED. REPLACED BOTH RIGHT MAIN LANDING GEAR WHEEL S AND BLED THE BRAKE SYSTEM, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996121200433 19961212 00433 NM 1996 12 12 UPS96221737 1 19961205 A 2150 65235792 MIX VALVE BOEING 727 72730C 1384009 NM LT PACK INOPERATIVE A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 01 919UP 19012 INSPECTION TYPE-N/A, FUMES SMELLED IN COCKPIT LIKE BURNING RUBBER. CHECKED CARGO AREA AND NO FUMES DETECTED. *S/D* RE MOVED AND REPLACED LEFT PACK MIX VALVE DUCT (P/N 65-23579-2) OPS CHECK LEFT PACK OK. THIS CLEARS M120048 PLACARD REMOVE D. 2 L 7 3 4F A3WE 1996121200434 19961212 00434 NM 1996 12 12 UPS96421736 1 19961207 A 3350 LIGHT BOEING 747 747123 1384873 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE-N/A, EMERGENCY LIGHTS ON THE MAIN DECK L-1 DOOR OVERHEAD INOP. RELAMPED OVERHEAD EMERGENCY LIGHTS ON TH E L-1 DOOR, CHECKS GOOD. 2 L 7 4 4F A20WE 1996121200435 19961212 00435 NM 1996 12 12 UPS96421738 1 19961209 A 3350 69B461024 LIGHT BOEING 747 747123 1384873 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE-N/A, EMERGENCY LIGHTS UNARMED LIGHT REMAINS ON AND EXIT LIGHTS ARE ILLUMINATED WITH SWITCH IN ARMED. RE PLACED MODULE ASSY EMERGENCY DTR, CHECK DONE (P/N 69B46010-24) (S/N D00407) ON, (P/N 69B46010-24) (S/N D00196) OFF. 2 L 7 4 4F A20WE 1996121200436 19961212 00436 EU 1996 12 12 WWMA9600104 1 19961207 A 2611 72111211000 DETECTOR SAAB SF340 340B 7860101 EU GALLEY DEFECTIVE A WWMA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 15 340RC 7552 340B340 CREW REPORTED A CONTINOUS AVIONICS SMOKE ALARM, NO SMOKE WAS DETECTED OR SMELL NOTED. MAINTENANCE REPLACED THE AVIONICS SMOKE DETECTOR. 2 L 7 2 4T RT A52EU 1996121200437 19961212 00437 EU 1996 12 12 WWMA9600103 1 19961206 A 2131 21179662 CONTROLLER SAAB SF340 340B 7860101 EU CABIN DEFECTIVE A WWMA O OTHER J WARNING INDICATION CR CRUISE 1 WP 15 280AE 340B280 CABIN PRESSURIZATION FAILED AT FLIGHT LEVEL 180. MAINTENANCE REPLACED THE CABIN PRESSURE CONTROLLER. 2 L 7 2 4T RT A52EU 1996121200438 19961212 00438 EU 1996 12 12 WWMA9600102 1 19961205 A 3320 BV033000250 LIGHT SOCKET SAAB SF340 340B 7860101 EU CABIN DEFECTIVE A WWMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 15 307AE 340B307 AIRCRAFT RETURNED TO FIELD DUE TO A SMOKE ODOR IN THE CABIN. THE FLIGHT ATTENDENT REPORTED SMOKE CAME FROM CABIN AROUND SEAT 3A. MAINTENANCE REPLACED FORWARD LIGHT SOCKET AT SEAT 4A. 2 L 7 2 4T RT A52EU 1996121200439 19961212 00439 NE 1996 12 12 WWMA9600101 2 19961203 A 7250 TURBINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE FAILED A A WWMA A E UNSCHED LANDING ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 15 324AE 12168 1175 340B324 GEE785510 RIGHT ENGINE OIL PRESSURE DECREASED TO NEAR ZERO IN FLIGHT. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT RETURNED TO FIELD WITHOUT INCIDENT. MAINTENANCE FOUND THE RIGHT ENGINE TO BE 4 QUARTS LOW OF OIL. NO LEAKS WERE NOTED BUT A LARGE AMOUN T OF OIL WAS FOUND IN THE TAILPIPE THAT APPEARED TO BE COMING OUT OF THE ENGINE TURBINE SECTION. THE ENGINE WAS REPLACE D. 2 L 7 2 4T 4 T RT A52EU E8NE 1996121200440 19961212 00440 NM 1996 12 12 96FDEA01697 1 19961207 A 2761 ACTUATOR BOEING 727 727233 138408A NM NR 13 SPOILER FAILED A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 220FE 20934 A SYSTEM HYDRAULIC PRESSURE WENT TO ZERO IN FLIGHT. A SYSTEM LOW PRESSURE LIGHT ILLUMINATED. PERFORMED EMERGENCY PROCE DURES, HAND CRANKED GEAR DOWN. CLOSED HYDRAULIC FLUID SHUTOFF VALVES, USED ALTERNATE FLAPS AND SHUT OFF ALL A-SYSTEM CO MPONENTS. TOWED BACK INTO THE PARKING AREA. FOUND NR 13 SPOILER ACTUATOR HAD A CUT ON RING. REPLACED SAME, LEAK AND O PERATIONAL CHECKED GOOD. 2 L 7 3 4F RT A3WE 1996121200441 19961212 00441 1996 12 12 96FDEA01698 4 19961206 A 2350 G3617 AUDIO PANEL DOUG DC10 DC1010 3022110 WP RT COCKPIT BURNT A FDEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SO 25 68058 46705 AIR TURNBACK, RETURNED TO DFW. SMOKE IN COCKPIT, APPEARS TO BE COMING FROM SECOND OFFICER'S AUDIO PANEL. ALL FIRE AND SMOKE CHECK LIST DONE. FOUND SECOND OFFICER'S AUDIO CONTROL PANEL BURNT INSIDE. USED AUDIO PANEL FROM ELECTRONIC COMPA RTMENT, FUNCTIONAL CHECKS OK. 2 L 7 3 4F A22WE 1996121200442 19961212 00442 NM 1996 12 12 96FDEA01699 1 19961207 A 5610 WINDOW BOEING 727 727277 138408S NM LT COCKPIT FAILED SEALER A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 242FE 21178 PASSING THROUGH 10,000 FT WITH CABIN AT 30 PSI AIR SPEED GOING THROUGH 300 KTS A LOUD NOISE FOLLOWED BY A WHISTLING CAME FROM CAPTAINS L1 WINDOW LEFT SIDE. FOUND TAPE HAD COME OFF OUTSIDE OF L 1 WINDOW EXPOSING UNCURED SEALANT. CLEANED SE ALANT FROM A/C FUSELAGE, RESEALED AND APPLIED HUFFER HEAT FOR 2.5 HOURS. RETAPED SEALANT, OK FOR FLIGHT. 2 L 7 3 4F RT A3WE 1996121200443 19961212 00443 WP 1996 12 12 SCNA96424 1 19961208 A 3260 802530 PROX ELEC UNIT DOUG DC10 DC1010 3022110 WP LANDING GEAR FAILED A SCNA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 15 573SC 46905 ALL THREE GEAR UNSAFE LIGHTS ILLUMINATED AFTER GEAR RETRACTION. REPOSITIONSED WIRE BUNDLE INTERFERING WITH HANDLE INTER LOCK SWITCH, REMOVED AND REPLACED PROXIMITY ELECTRONICS UNIT AND RELAY R2-5083. PERFORMED SYSTEM TEST IN ACCORDANCE WIT H MM 32-60-00. 2 L 7 3 4F A22WE 1996121200444 19961212 00444 WP 1996 12 12 SCNA96425 1 19961115 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 735 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 572SC 46977 DURING HEAVY MAINTENANCE, FOUND CORROSION AROUND FLOORBOARD SUPPORT NUT CLIP HOLES IN LOWER GALLEY, BS 735 LBL 8. REMOV ED CORROSION, FABRICATED AND INSTALLED REPAIR DOUBLERS IN ACCORDANCE WITH SRM 53-00-01. 2 L 7 3 4F A22WE 1996121200445 19961212 00445 WP 1996 12 12 SCNA96423 1 19961206 A 3830 1600157 PUMP DOUG DC10 DC1010 3022110 WP NR 3 LAVATORY FAILED A SCNA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 573SC 46905 INFLIGHT, SMOKE WAS REPORTED IN AFT LAV, DISCHARGED TWO FIRE EXTINGUISHERS. DIVERTED TO MSP AND DUMPED FUEL. REMOVED A ND REPLACED AFT LAV PUMP AND OPS CHECKED NORMAL. 2 L 7 3 4F A22WE 1996121200446 19961212 00446 WP 1996 12 12 SCNA96426 1 19961115 A 5320 DOUBLER DOUG DC10 DC1010 3022110 WP BS 1029 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 572SC 46977 DURING HEAVY MAINTENANCE, FOUND CORROSION ON ANTENNA DOUBLER AT BS 1029 BETWEEN LONGERON 51R AND 52. REMOVED LOWER ANTE NNA DOUBLER, FABRICATED AND INSTALLED A NEW DOUBLER IN ACCORDANCE WITH SRM 53-20-00, PAGES 74 TO 84. 2 L 7 3 4F A22WE 1996121200447 19961212 00447 WP 1996 12 12 SCNA96427 1 19961116 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 775/899 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 572SC 46977 DURING HEAVY MAINTENANCE, FOUND CORROSION ON LONGERON 50 BETWEEN BS 775 AND BS 899. REMOVED CORRODED SECTION OF LONGERO N, FABRICATED AND INSTALLED A SPLICED SECTION OF LONGERON IN ACCORDANCE WITH SRM 53-10-00. 2 L 7 3 4F A22WE 1996121200448 19961212 00448 SO 1996 12 12 SRAA961088 1 19961013 A 5311 FRAME LKHEED 382 382G 526414U SO BS 444 CORROSION A SRAA K NONE O OTHER IN INSP/MAINT 1 GL 23 905SJ 45318 4472 DURING C-CHECK, FOUND LEVEL 1 CORROSION AT RT O/B CARGO COMPARTMENT Z-FRAME AT FS 444, BL 61, WL 146. CUT OFF CORRODED END OF RING SEGMENT, FABRICATED FORMED AND INSTALLED 2 L-ANGLES AND 1 Z-FILLER IAW LAC SRM 51-140-21. 2 H 7 4 4T A1SO 1996121200449 19961212 00449 SO 1996 12 12 SRAA961202 1 19961203 A 3350 BATTERIES LKHEED 382 382G 526414U SO CABIN DISCHARGED A SRAA K NONE L NO TEST IN INSP/MAINT 1 GL 23 906SJ 4477 DURING PREFLIGHT INSPECTION, FOUND EMERGENCY EXIT LIGHTS WEAK. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERIES IAW MM CH 33, OPS CHECKED GOOD. 2 H 7 4 4T A1SO 1996121200451 19961212 00451 SW 1996 12 12 HEEA968600 1 19961203 A 6330 222331617101 ISOLATION MOUNT BELL 230 230 1182149 SW M/R GR BOX SEPARATION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 501 23009 RUBBER SEPARATED FROM CENTER SECTION. 1 G 7 2 3U NC H9SW 1996121200452 19961212 00452 SW 1996 12 12 HEEA968601 1 19961203 A 6330 222331618105 ISOLATION MOUNT BELL 230 230 1182149 SW M/R GR BOX DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 280 23009 TEFLON COMING OUT OF THE BEARING. 1 G 7 2 3U NC H9SW 1996121200453 19961212 00453 GL 1996 12 12 HEEA968602 2 19961203 A 7230 23038162 SHROUD HOUSING 23033193 BELL 206 206L1 1182107 SW ALLSN 250C 250C30P 03013 GL ENGINE UNDER SIZE E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 5007N CAC91062 45184 CAE895174 RECEIVING INSPECTION REVEALED; UNDERSIZED THROAT CLEARANCE ON SHROUD HOUSING. INSTALLED A NEW SHROUD HOUSING. 1 G 7 1 3U 3 U H2SW E1GL 1996121200454 19961212 00454 GL 1996 12 12 HEEA968603 2 19961203 A 7240 6899081 COMB LINER BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL ENGINE MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 6610E 51424 WHILE INSTALLING NEW COMBUSTION LINER FOR TROUBLESHOOTING TORQUE FLUX AT HIGH POWER SETTINGS. WAS UNABLE TO INSTALL IGN ITOR - DUMMY PLUG AND FUEL NOZZLE AT SAME TIME. FOUND MISALIGNMENT BETWEEN ALIGNMENT PIN AND IGNITOR BOSS (APPROX. 1/4" )WHEN COMPARED WITH OLD COMBUSTION LINER. LINER OVERHAULED ON DALLAS AIRMOTIVE W/O# LF0776. 1 G 7 1 3U 3 U H2SW E1GL 1996121200455 19961212 00455 SW 1996 12 12 HEEA968604 1 19961203 A 6730 212076005105 CYL INDER ASSY BELL 412 412 1182202 SW M/R CONTROL REQ OVERHAUL E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911PB 2023 33186 NEEDS OVERHAUL. 1 G 7 2 4U H4SW 1996121200456 19961212 00456 SW 1996 12 12 HEEA968605 1 19961203 A 6730 212076005105 CYLINDER BELL 412 412 1182202 SW M/R CONTROL REQ OVERHAUL E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911PB 1919 33186 NEEDS OVERHAUL. 1 G 7 2 4U H4SW 1996121200457 19961212 00457 SW 1996 12 12 HEEA968606 1 19961203 A 6730 212076005105 CYLINDER ASSY BELL 412 412 1182202 SW M/R CONTROL LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 911PB 2618 33186 SERVO TESTED PRIOR TO REPAIR. SERVO LEAKING AT BOTH ENDS OF UPPER AND LOWER CYLINDERS. LEAKING INTERNALLY IN NEUTRAL P OSITION IN BOTH CYLINDERS AND LEAKING EXTERNALLY AT BOTH LOWER PILOT VALVES. 1 G 7 2 4U H4SW 1996121200458 19961212 00458 GL 1996 12 12 HEEA968607 2 19961203 A 7250 23034775 SUPPORT 23035128 BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL ENG GP SEAL DEFECTIVE E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 42EA CAT97885 51542 CAE895606 RECEIVING INSPECTION REVEALED: COATING LIFTING ON G.P. SUPPORT SEAL BORE ID. INSTALLED A DALLAS AIRMOTIVE OVERHAULED G. P. SUPPORT. 1 G 7 1 3U 3 U H2SW E1GL 1996121200459 19961212 00459 EU 1996 12 12 HEEA968608 1 19961204 A 6720 350A33214501 ROD SNIAS 350 AS350B2 8680813 EU PITCH CONTROL WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6097Z 2042 2820 PITCH CONTROL ROD IS WORN EXCESSIVELY. (WORN SPHERICAL BEARINGS) 1 G 7 1 3U H9EU 1996121200460 19961212 00460 EU 1996 12 12 HEEA968609 1 19961204 A 6720 350A33214501 ROD SNIAS 350 AS350B2 8680813 EU PITCH CONTROL WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100R 1411 2862 PITCH CONTROL ROD IS WORN EXCESSIVELY. (WORN SPHERICAL BEARINGS) SERIAL NUMBERS REMOVED PMA8787 AND PMA8784. 1 G 7 1 3U H9EU 1996121200461 19961212 00461 SW 1996 12 12 HEEA968610 1 19961204 A 6320 204040701103 GEAR 412040002113 BELL 412 412 1182202 SW M/R GR BOX PITTED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911PB 3095 A133 33186 PITTING ON MATING SURFACE BEYOND ACCEPTABLE LIMITS. 1 G 7 2 4U H4SW 1996121200462 19961212 00462 SW 1996 12 12 HEEA968611 1 19961204 A 6320 204040305001 SLEEVE ASSY 412040002113 BELL 412 412 1182202 SW M/R GR BOX DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911PB 3095 A133 33186 DAMAGED THREADS IN JACK OUT HOLE. 1 G 7 2 4U H4SW 1996121200463 19961212 00463 SW 1996 12 12 HEEA968612 1 19961204 A 6230 412040366105 MAST ASSY BELL 412 412 1182202 SW M/R SEAL LEAK E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 911PB 3095 33186 MAST ASSY SEAL LEAK. 1 G 7 2 4U H4SW 1996121200464 19961212 00464 GL 1996 12 12 HEEA968613 2 19961204 A 7260 6876925 TUBE ASSY. 6894171 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL GR BOX FAILED CHECK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3533T CAG33634 S111 CAE800850 ENGINE REMOVED DUE TO COMPRESSOR OVERHAUL. GEARBOX REPAIRED DUE TO WORN COMPRESSOR BORE. UPON INSPECTION OF GEARBOX PA RTS NOTED THE FOLLOWING: TUBE ASSEMBLY FAILED DIMENSIONAL CHECK PER CEB1307. INSTALLED A NEW TUBE. 1 G 7 2 3U 3 U H3EU E4CE 1996121200465 19961212 00465 SW 1996 12 12 HEEA968614 1 19961204 A 6400 206010777001 WASHER BELL 206 206L1 1182107 SW T/R BUMPER WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2251A 60 45755 RUBBER BUMPER HAS WORN OUT PREMATURELY. 1 G 7 1 3U H2SW 1996121200466 19961212 00466 SW 1996 12 12 HEEA968615 1 19961204 A 6400 206010777001 WASHER BELL 206 206L1 1182107 SW T/R BUMPER WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2251A 32 45755 TAIL ROTOR RUBBER BUMPER HAS WORN THROUGH AT ACCELERATED RATE. THESE ARE THE BLACK RUBBER BUMPERS. 1 G 7 1 3U H2SW 1996121200468 19961212 00468 CE 1996 12 12 96ZZZX5983 1 19961012 A 3260 YZR31 SWITCH BEECH 18 G18S 1151010 CE LANDING GEAR OUT OF ADJUST A UATA O OTHER P NO WARNING INDICATION LD LANDING 1 AL 03 151H BA476 PILOT LANDED AIRCRAFT WITH LANDING GEAR UP. FOUND LANDING GEAR WARNING HORN SWITCH SET AT TOO LOW OF A THROTTLE SETTING . 1 L 7 2 3R A765 1996121200469 19961212 00469 NM 1996 12 12 96ZZZX5984 1 19961114 A 5330 SKIN BOEING 737 7372P6 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 EICKW 21677 ON WALK-AROUND, CREW FOUND 5 INCH CRACK IN SKIN AT STA 787, STR 18L. INSTALLED DOUBLER PER SRM 53-30-6, FIG 6. 2 L 7 2 4F RT A16WE 1996121200470 19961212 00470 EU 1996 12 12 96ZZZX5985 1 19961023 A 2460 2410AM RELAY ECE AMD FALC20 FALCOND 2720304 EU DC POWER BOX FAILED A DKAA O OTHER J H WARNING INDICATION ELECT. POWER LOSS-50 PC DE DESCENT 1 GL 23 192R 13731 192 AIRCRAFT WENT INTO LOAD SHED. REPLACED 14P RELAY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE (MEM). 2 L 7 2 4F A7EU 1996121200471 19961212 00471 EU 1996 12 12 96ZZZX5986 1 19961008 A 5230 BRACKET AMD FALC20 FALCOND 2720304 EU CARGO DOOR CRACKED A DKAA K NONE O OTHER IN INSP/MAINT 1 GL 23 192R 192 AIRCRAFT CARGO DOOR ROTATING LATCH SUPPORT STRUCTURES (BOTTOM ROW) FOUND CRACKED DURING NUMBER CHECK INSPECTION. 2 L 7 2 4F A7EU 1996121200472 19961212 00472 EU 1996 12 12 AWXA960580 1 19961012 A 2761 31077050 SPOILER ACTUATOR AIRBUS 320 A320231 3930325 EU NR 3 SPOILER MALFUNCTIONED A AWXA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 WP 28 644AW 10096 L2072 317 PHX - FLT 2050 - ON LANDING, LOST BLUE HYDRAULIC SYSTEM. NR 3 SPOILER FAULTED UP. BLUE RESERVOIR LOW LEVEL. REMOVED A ND REPLACED NR 3 SPOILER ACTUATOR. OPS CHECK NORMAL. PART TOTAL CYCLES 5060. (X) 2 L 7 2 4F RT A28NM 1996121200473 19961212 00473 EU 1996 12 12 AWXA960602 1 19961019 A 3350 321454 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 618AW 1565 304 PHX - FLT 2209 - DURING ROUTINE MAINTENANCE CHECK, FOUND FORWARD SECTION EMERGENCY LIGHTS INOPERATIVE. REPLACED FORWARD LEFT EMERGENCY EXIT POWER SUPPLY AND EMERGENCY EXIT LIGHT BATTERY. OPS CHECK OK. (X) 2 L 7 2 4F RT A28NM 1996121200474 19961212 00474 1996 12 12 MALA965172 4 19961023 A 3425 6225190113 AHARS COMPUTER SAAB SF340 SF340A 7850100 EU COCKPIT FAILED A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 103XJ 340A103 FLT 3006 - ON CLIMB-OUT FROM DTW, THE FIRST OFFICER'S EADI AND EHSI WENT BLANK. THE AIRCRAFT RETURNED TO DTW. MAINTENA NCE REPLACED THE NR 2 AHRS COMPUTER. ALL CHECKS SATISFACTORY. (X) 2 L 7 2 4T RT A52EU 1996121200475 19961212 00475 EU 1996 12 12 MALA965151 1 19960928 A 2613 CONNECTOR SAAB SF340 SF340A 7850100 EU LT ENGINE CORRODED A MALA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 GL 15 103XJ 340A103 FLT 3157 - ON CLIMB-OUT FROM DTW, THE LEFT TAIL PIPE HOT LIGHT ILLUMINATED. THE CREW RETARDED THE POWER LEVER TO FLIGH T IDLE AND THE LIGHT REMAINED ILLUMINATED. THE CREW SHUT DOWN THE ENGINE AND RETURNED TO DTW. MAINTENANCE FOUND CANNON PLUG 161VP P10 PINS 1 AND 2 CORRODED TOGETHER. REPLACED THE CANNON PLUGS. ALL CHECKS SATISFACTORY. (X) 2 L 7 2 4T RT A52EU 1996121200476 19961212 00476 CE 1996 12 12 96ZZZX5987 1 19961016 A 2120 AIR DISTR BEECH 1900 1900D 1154162 CE COCKPIT ODOR A MASA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 01 240YV UE240 ON FINAL APPROACH, PILOT REPORTED SMELLING A BURNING ODOR. MECHANIC INSPECTED, FOUND AIRCRAFT SAFE FOR FERRY FLIGHT TO DENVER. MECHANIC IN DENVER INSPECTED, REMOVED FLOOR PANELS AND PERFORMED GROUND RUNS WITH BLEED OFF AND ON. RAN FLAPS. COULD NOT DUPLICATE DISCREPANCY. 2 L 7 2 4T RT A24CE 1996121200477 19961212 00477 NM 1996 12 12 USAA960726 1 19960910 A 5310 STRUCTURE BOEING 737 737247 138448D NM BS 268.25 CORROSION A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 487GS 46002 19600 CLT - INSPECTION VISUALLY FOUND A 1 INCH CORRODED AREA LOCATED AT BS 268.25 AT LBL 20 AND RBL 20 AT WL 186. CORROSION T ASK NR: C53-202-01. CORROSION LEVEL: 2. INSTALLED REPAIR ANGLES AND FILLERS PER EA 588005A. (X) 2 L 7 2 4F A16WE 1996121200478 19961212 00478 NM 1996 12 12 USAA960731 1 19960910 A 5330 SKIN BOEING 737 737247 138448D NM FUSELAGE DISBOND A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 487GS 46002 19600 CLT - INSPECTION VISUALLY FOUND A 1 INCH BY 11 INCH DELAMINATED AREA LOCATED AT RT OVERWING EMERGENCY EXIT CUT OUT. INS TALLED FASTENER PER BOEING SB 73 7-58-1076. (X) 2 L 7 2 4F A16WE 1996121200479 19961212 00479 NM 1996 12 12 USAA960728 1 19960910 A 5330 SKIN BOEING 737 737247 138448D NM BS 259.5-277 CORROSION A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 487GS 46002 19600 CLT - INSPECTION VISUALLY FOUND SKIN WITH LEVEL 2 CORRODED AREA MEASURING 8 INCHES BY 10 INCHES LOCATED AT BS 259.5 - BS 277 AT S23R (BOTTOM OF FORWARD LAVATORY SERVICE PANEL). INSP CARD NR: A-06A-2. CORROSION LEVEL: 2. INSTALLED DOUBL ER PER BOEING SRM 53-30-3. (X) 2 L 7 2 4F A16WE 1996121200480 19961212 00480 NM 1996 12 12 USAA960725 1 19960910 A 5311 FRAME BOEING 737 737247 138448D NM STA 500 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 487GS 46002 19600 CLT - INSPECTION VISUALLY FOUND A 2 INCH CRACK LOCATED AT UPPER FLANGE OF FUSELAGE FRAME STA 500 ATTACH TO RT TRANSITION ANGLE. INSTALLED FILLER AND DOUBLER AND RIVET INSTALLATION PER BOEING SRM 51-40-3. (X) 2 L 7 2 4F A16WE 1996121200481 19961212 00481 NM 1996 12 12 USAA960729 1 19960910 A 5330 SKIN BOEING 737 737247 138448D NM STA 276 CORROSION A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 487GS 46002 19600 CLT - INSPECTION VISUALLY FOUND SKIN WITH LEVEL 2, 2 INCH BY 4 INCH, CORRODED AREA LOCATED AT NLG W/W, STA 276, RBL 13. CORROSION TASK NR: C53-100-01. CORROSION LEVEL: 2. FABRICATED PART, SAME AS REMOVED, AND INSTALLED PER BOEING SRM 5 3-10-2. (X) 2 L 7 2 4F A16WE 1996121200482 19961212 00482 NM 1996 12 12 USAA960727 1 19960910 A 5311 FRAME BOEING 737 737247 138448D NM BS 500 CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 487GS 46002 19600 CLT - INSPECTION VISUALLY FOUND A 1 INCH CRACK LOCATED AT BS 500B FRAME INNER CHORD (FORMED SECTION AT S24R). INSTALLED DOUBLER PER BOEING SRM 51-40-03, FIG 1. (X) 2 L 7 2 4F A16WE 1996121200483 19961212 00483 CE 1996 12 12 96ZZZX5988 1 19961101 A 3260 WARNING LIGHT BEECH 1900 1900C 1154161 CE LANDING GEAR MALFUNCTIONED A GUUA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 SO 19 153GA UB34 EYW/MIA - FLT 403 - PILOT REPORT: WHEELS WARNING LIGHT WILL NOT COME ON IN-FLIGHT. SYSTEM FUNCTIONS PROPERLY WHEN RETAR DING POWER LEVERS BACK TO ACTUATE WARNING HORN. 2 L 7 2 4T RT A24CE 1996121200484 19961212 00484 EU 1996 12 12 96ZZZX5989 1 19961029 A 3260 638 ANN LAMPS STBROS SD3 SD360 8100606 EU COCKPIT FAILED A GUUA O OTHER P NO WARNING INDICATION AP APPROACH 1 SO 19 261GA SH3745 MIA/MIA - FLT 104 - PILOT REPORT: ON TRAINING FLIGHT, RIGHT MAIN GEAR GREEN DOWN INDICATION INOPERABLE WHEN GEAR IS SEL ECTED DOWN. REPLACED ANNUNCIATOR LAMPS. 2 H 7 2 4T A41EU 1996121200485 19961212 00485 NE 1996 12 12 96ZZZX5990 2 19961002 A 7414 MAGNETO DHAV DHC4 DHC4A 2800304 EA PWA R2000 R20007M2 52023 NE RIGHT FAILED A A G2OC E ENGINE SHUTDOWN Y ENGINE STOPPAGE CR CRUISE 1 AL 03 800NC 98 P107895 WHILE RETURNING, IN-FLIGHT, ENGINE RT MAGNETO QUIT WORKING. FURTHER INSPECTION. FOUND MAG HAD FAILED DUE TO TIMING GEA RS HAVING ROTATED CAUSING MAG TO LOSE ITS TIMING. MAG WAS PROPERLY SAFTIED WITH COTTER KEY STILL IN PLACE. FAILURE WAS CAUSED BY A BUSHING LOCATED IN THE BASE OF THE MAGNETO. THIS IS THE SECOND SUCH FAILURE IN 6 MONTHS AND 500 HOURS OF F LYING. 2 H 7 2 4R 4 R 1A19 5E5 1996121200486 19961212 00486 WP 1996 12 12 ORJA9682 1 19961031 A 3397 WIRE DOUG DC9 DC987 3022087 WP CABIN BROKEN A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 753RA 49587 EMERGENCY LIGHTS OUT AT 6-DEF AND 15-DEF. AT 6-DEF REPINNED CONNECTOR. OPS CHECK NORMAL. AT 15-DEF REPAIRED WIRE BY S PLICE. OPS CHECK NORMAL. (X) 2 L 7 2 4F RT A6WE 1996121200487 19961212 00487 EU 1996 12 12 COEA9622201 2 19961018 A 7200 ENGINE FRCHLD F27 F27F 3373008 EA RROYCE DART DART5297E 54507 EU LEFT FAILED A A COEA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 NM 13 222DG 18738 4751 31 13517 OAK/YVR - WHILE EN ROUTE WITH MODERATE TURBULENCE AND MODERATE ICING CONDITIONS, LT ENGINE AUTOFEATHERED IN CRUISE. CRE W INITIATED AIRSTART PROCEDURES. ENGINE WAS BACK ON-LINE WITH NO PROBLEMS. ENGINE PERFORMED THROUGH THE REMAINDER OF T HE FLIGHT WITH NO RECURRENCE. MAINTENANCE INSPECTED ENGINE INTAKE AND EXHAUST, IGNITIION SYSTEM AND GROUND RUN CARRIED OUT. FOUND SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T 4 T 7A1 E297 1996121200488 19961212 00488 WP 1996 12 12 ORJA9684 1 19961031 A 3350 41B004AD073 BATTERY EA1D13D3 DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 881RA 49941 OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 19 AND 22 ARE INOPERATIVE. REMOVED AND REPLACED BATTERIES. OPS NORMAL. (X) 2 L 7 2 4F RT A6WE 1996121200489 19961212 00489 EU 1996 12 12 JBXA00020 1 19961018 A 3020 DEICE SYST FOKKER F28 F28MK0100 4990807 EU NR 1 ENGINE MALFUNCTIONED A JBXA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SO 05 107ML 11450 DCA - WHILE EN ROUTE, AIRCRAFT PUT IN HOLD BY ATC. ICING CONDITIONS ENCOUNTERED. ENGINE ONE VIBRATION GAUGE WENT INTO AMBER AND ABOVE WHILE IN ICING CONDITIONS. COULD NOT BRING THRUST LEVER ABOVE FLT IDLE WITHOUT VIB. GOING BACK INTO AMB ER RANGE. RETURNED TO RDU. ICE CAUSING VIB MELTED PASSING 8,000 FEET. ICING VIB OCCURRED AT 21,200 FEET. PERFORMED E NGINE RUN ON NR 1 ENGINE IAW AMM 71-00-00 VIBS. WITHIN LIMITS. (X) 2 L 7 2 4F RT 1996121200490 19961212 00490 CE 1996 12 12 GLBA96200 1 19961011 A 3610 PACKING BEECH 1900 1900D 1154162 CE BLEED AIR MISSING A GLBA O OTHER J WARNING INDICATION CR CRUISE 1 CE 01 208GL UE208 HON - RIGHT BLEED AIR FAIL ILLUMINATED AND LEFT BLEED WILL NOT HOLD PRESSURE. MAINTENANCE FOUND PACKINGS MISSING IN BLE ED DUCT ASSY ON LEFT SIDE. INSTALLED PACKINGS, REPAIRED EVA TUBING AND OPERATED NORMALLY. (X) 2 L 7 2 4T RT A24CE 1996121200491 19961212 00491 WP 1996 12 12 96NK213 1 19961028 A 2150 PACK DOUG DC9 DC941 302207N WP RIGHT SMOKING A GTIA O J OTHER DUMP FUEL B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 23 130NK 47604 LOG PAGE NR 028018. ITEM NR P287. AT 18,000 FEET IN DESCENT, BOTH SMOKE DETECTORS WENT OFF. COULD SMELL ELECTRICAL SM OKE (STINKY AND HAZY IN BACK). INSPECTION THE SUSPECT LOCATION OF THE SMOKE-RUNNING RIGHT PACK, BLEW SMOKE FROM PACK. I TEM DEFERRED BY WANER AVIATION (FLL). ACTUAL LOG SHEET PENDING - WILL SEND MRR FOLLOW-UP REPORT ASAP. (X) 2 L 7 2 4F A6WE 1996121200494 19961212 00494 1996 12 12 VTZA97031 4 19961018 A 3425 4020531574 ADI BAG JETSTM JETSTM3101 1500215 EU RT COCKPIT FAILED A VTZA K NONE O OTHER CR CRUISE 1 EA 27 473UE 828 LYH/IAD AT 1500 HOURS ON 10-18-96, DURING CRUISE. LANDED AT IAD WITH ONE DISCREPANCY WHICH WAS FO'S ADI 5 DEGREES TILT UP. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED ADI, OPS CHECK OK. AIRCRAFT WAS R ELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A21EU 1996121200499 19961212 00499 EU 1996 12 12 CA960212002 1 19960208 A 4950 APU BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE APU BLEED OIL IN AIR DIST W D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA 2700 LF05539A (CAN) AIRCRAFT RETURNED TO GATE DUE TO SMOKE IN CABIN AND FLIGHT DECK. CAUSE FOUND TO BE COMING FROM AIR CONDITIONING UN IT WHEN APU BLEED AIR USED. APU REPLACED. 2 H 7 4 4F 4 F RT A49EU E6NE 1996121200501 19961212 00501 CE 1996 12 12 CA960212014 1 19960131 A 2810 FUEL SYSTEM BEECH 95 95B55 1152729 CE CONT O470 IO470L 17026 SO FUEL SUMPS ICE CRYSTALS W A C A ABORTED TAKEOFF UNSCHED LANDING O R OTHER PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CA 237685R (CAN) ON THE TAKEOFF ROLL, THE R/H ENGINE FAILED TO DEVELOP FULL POWER. THE TAKEOFF WAS ABORTED AND A GROUND RUN PERFORM ED. A SECOND TAKEOFF WAS ATTEMPTED, THIS TIME DEVELOPING FULL POWER, BUT ONCE AGAIN WHEN AIRBORNE BEGAN TO LOSE POWER. T HE AIRCRAFT LANDED WITHOUT INCIDENT. A SUBSEQUENT INSPECTION AND GROUND RUN COULD FIND NO FAULT, BUT WATER AND ICE CRYST ALS WERE FOUND IN THE FUEL SUMPS. THE SUMPS WERE DRAINERD AND A TEST FLIGHT FOUND THE AIRCRAFT FUNCTIONING NORMALLY. 1 L 7 2 3O 3 O RT 3A16 3E1 1996121200502 19961212 00502 EU 1996 12 12 CA960212030 1 19960203 A 6130 3036007 SEAL AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE HAMSTD 14SF 14SF5 NE REDUCTION GEARBX DAMAGED W A D E H UNSCHED LANDING RETURN TO BLOCK ENGINE SHUTDOWN DEACTIVATE SYST/CIRCUITS J K WARNING INDICATION FLUID LOSS CL CLIMB 1 CA 120619 890205 (CAN) THE PROP BRAKE HAD TO BE REMOVED AND DURING THE REMOVAL, THE PROP BRAKE FLANGE SEAL WAS DISTURBED. THE LATTER BEGA N TO LEAK OIL ON THE NEXT FLIGHT. THE ENGINE HAD TO BE SHUT DOWN DUE TO LOW OIL LEVEL. THE SEAL WAS REPLACED, RUN-UP CAR RIED OUT AND FOUND SERVICEABLE. 2 H 7 2 4T 4 T RT A53EU E20NE 6 C P7NE 1996121200506 19961212 00506 NE 1996 12 12 CA960212201 2 19960121 A 8520 164448 STUDS DOUG DC4 C54A 3021512 WP PWA R2000 R20007M2 52023 NE #6 CYLINDER BROKEN W E ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 CA 1172 P107846 (CAN) VISIBLE OIL LEAK IN FLIGHT. ENGINE SHUT DOWN. INSPECTION DISCLOSED THAT THE 24 CYLINDER HOLD DOWN STUDS FOR #6 CYL INDER HAD FAILED. APPROXIMATELY 50 PERCENT HAD BROKEN AND THE OTHER 50 PERCENT HAD PULLED OUT OF THE CRANKCASE. 2 L 7 4 4R 4 R A762 5E5 1996121200507 19961212 00507 NE 1996 12 12 CA960214001 3 19960213 A 6111 SFA13M1OA BLADE DHAV DHC8 DHC8101 2809002 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE #1 BLADE FAILED TEST W K NONE O OTHER IN INSP/MAINT 1 CA 5805 123138 910323 (CAN) #1 BALDE #1 PROP FAILED SHEAR WAVE TEST AS PER SB 14SF-61-A95. BLADE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1996121200508 19961212 00508 NE 1996 12 12 CA960214002 3 19960213 A 6111 SFA13G1OA BLADE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE #1 AND #2 BLADE FAILED TEST W K NONE O OTHER IN INSP/MAINT 1 CA 16229 8969 120083 890915 (CAN) #1 AND #2 BLADES FAILED SHEAR WAVE TEST AS PER SB 14SF-61-A95. BLADE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1996121200509 19961212 00509 NE 1996 12 12 CA960214003 3 19960213 A 6111 SFA13M1OA BLADE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE #1 AND #2 BLADE FAILED TEST W O OTHER O OTHER IN INSP/MAINT 1 CA 16848 7687 120760 9527 (CAN) #1 AND #2 PROP BLADES FAILED SHEAR WAVE TEST AS PER SB 14SF-61-A95. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1996121200510 19961212 00510 NE 1996 12 12 CA960214004 3 19960213 A 6111 14SF13M1OA BLADE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE #2 AND #4 BLADES FAILED TEST W K NONE O OTHER IN INSP/MAINT 1 CA 2186 120760 9527 (CAN) #2 AND #4 BLADES FAILED SHEAR WAVE TEST AS PER SB 14SF-61-A95. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1996121200511 19961212 00511 NE 1996 12 12 CA960214005 3 19960213 A 6111 SFA13N10A BLADE DHAV DHC8 DHC8301 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE FAILED TEST W K NONE O OTHER IN INSP/MAINT 1 CA 8927 121164 870626 (CAN) BLADE FAILED SHEAR WAVE TEST AS PER SB 14SF-61-A95. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1996121200515 19961212 00515 NE 1996 12 12 CA960312002 3 19960308 A 6111 SFA13G1OA BLADE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE #1 AND #2 FAILED TEST W K NONE O OTHER IN INSP/MAINT 1 CA 15460 7760 120657 841104 (CAN) #1 PROP BLADE FAILED SHEAR WAVE TEST AS PER SB 14SF-61-A95. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1996121200516 19961212 00516 NE 1996 12 12 CA960312004 3 19960308 A 6111 SFA13N10A BLADE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE #2 BLADE #1 PROP FAILED TEST W K NONE O OTHER IN INSP/MAINT 1 CA 10242 1625 123132 901161 (CAN) #2 BLADE #1 PROP FAILED SHEAR WAVE TEST AS PER SB 14SF-61-A95. BLADE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1996121200517 19961212 00517 EA 1996 12 12 CA960312009 2 19960219 A 7210 3017680 RED GEARBX BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA ENGINE MIS ASSEMBLY W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 10504 2592 CPPS6063 (CAN) GEARBOX WAS RECEIVED DIRECTLY FROM MANUFACTURER WITH SEVERAL DISCREPANCIES IN QUALITY OF ASSEMBLY. THE TWO COUPLIN GS P/N 3024973 BETWEEN C-BOX AND GOVERNORS WERE NOT INSTALLED PROPERLY (COMPLETELY MISSING). ELBOW MS9194-04 ON TOP OF G OVERNOR WAS JAMMED INTO OIL MOUNTING FLANGE. SEVERAL LINE NUTS (B-NUTS) WERE LOCKWIRED BACKWARDS. 1 HELICOIL WAS NOT COM PLETELY INSTALLED. THE PREVIOUS DEFECTS WERE NOTICED AND RECTIFIED BEFORE INSTALLATION ON HELICOPTER. MANUFACTURER HAS B EEN INFORMED. 1 G 7 1 4U 4 U H4SW E22EA 1996121200518 19961212 00518 EA 1996 12 12 CA960312019 2 19960219 A 7210 3024780 BEARING BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA #5 BEARING WRONG PART W O OTHER W INADEQUATE Q C IN INSP/MAINT 1 CA 41 CPPS6063 (CAN) THIS GEARBOX HAD AN UNAPPROVED BEARING INSTALLED IN IT FROM OVERHAUL. THE GEARBOX WAS REPLACED PRIOR TO NEXT FLIGH T TO COMPLY WITH A LETTER RECEIVED FROM TRANSPORT CANADA. ASSEMBLY REPLACED, AND AIRCRAFT RETURNED TO SERVICE. 1 G 7 1 4U 4 U H4SW E22EA 1996121200519 19961212 00519 NE 1996 12 12 CA960321002 2 19960320 A 7230 SEAL BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE #3 ENGINE LEAKING W O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA LF05567A (CAN) AFTER TAKEOFF, SMELL OF OIL IN COCKPIT AND CABIN FOR TWO MINUTES. OIL FOUND LEAKING FROM #1 SEAL #3 ENGINE. #2 AIR PACK MADE INOPERATIVE AS PER MEL. 2 H 7 4 4F 4 F RT A49EU E6NE 1996121200520 19961212 00520 EA 1996 12 12 CA960321006 2 19960222 A 8520 5015 STUDS PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2B 41532 EA #5 CYLINDER BROKEN W A E O ENGINE SHUTDOWN OTHER E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CR CRUISE 1 CA L803061A (CAN) DURING CRUISE FLIGHT, RIGHT ENGINE BEGAN TO RUN ROUGH. INVESTIGATION REVEALED 4 BROKEN STUDS 1-P/N 5015, 2-P/N 38- 13, 1-P/N 69679 ON THE BOTTOM FLANGE OF #5 CYLINDER. MOVEMENT OF THE CYLINDER CAUSED THE INDUCTION PIPE SEAL P/N 72711 T O DISLOCATE, CAUSING A LARGE INDUCTION AIR LEAK. THE ENGINE WAS REPLACED. 1 L 7 2 3O 3 O A20SO E14EA 1996121200521 19961212 00521 NE 1996 12 12 CA960321009 2 19960307 A 7314 358200 FUEL PUMP BOEING 737 737210C 1384459 NM PWA JT8 JT8D9A 52048 NE ENGINE FAILED SHAFT W A E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CL CLIMB 1 CA 5159 665654 (CAN) DURING CLIMB, #2 ENGINE WOULD NOT RESPOND TO ANY POWER LEVER ADJUSTMENT. THE ENGINE SHUT DOWN IN FLIGHT AND THE AI RCRAFT LANDED SAFELY. MAINTENANCE INVESTIGATION FOUND THE FUEL PUMP WENT TO AN AUTO ACCELERATION CONDITION DUE TO A DAMA GED DRIVE SHAFT. THE FUEL PUMP WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F A16WE E2EA 1996121200522 19961212 00522 EU 1996 12 12 CA960401003 1 19960321 A 3222 30011150 TAB WASHER MORAVN K237 ZLIN 242 Z242L 9970204 EU NOSE GEAR FORK LOST W A K NONE O OTHER TX TAXI/GRND HDL 1 CA 220 4519 (CAN) WHILE TOWING THE AIRCRAFT IT WAS NOTED THAT RIGHT HAND AXLE RETAINING BOLT AND TAB WASHER WERE MISSING. THIS ALLOW ED THE NOSE WHEEL TO REPOSITION ABOUT 3/4 INCH TO THE LEFT. INSPECTION FOUND THE NOSE WHEEL SERVICEABLE. SUBMITTER SPECU LATES THAT THE LOCKING TAB MAY HAVE BEEN DAMAGED AND ALLOWED THE BOLT TO BACK OUT. 1 L 7 1 3O 0 A76EU 1996121200523 19961212 00523 CE 1996 12 12 CA960404005 1 19960327 A 5511 STABILIZER CESSNA 172 172M 2072418 CE HORIZ STAB CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 7355 (CAN) INSPECTION PER SE 1394-8 FOUND SPAR AND SKIN CRACKED. 1 H 7 1 3O NT 3A12 1996121200524 19961212 00524 CE 1996 12 12 CA960404007 1 19960319 A 3244 22X675108190 TIRE PARKER HANNI 04020400 BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA SIDEWALL BULGED W K NONE O OTHER IN INSP/MAINT 1 CA 862 500530304 PCE81939 (CAN) WHILE PERFORMING A DAILY INSPECTION ON THE NOSE GEAR A BULGE WAS NOTICED IN THE TIRE TREAD GROOVE. CLOSER OBSERVAT ION OF THE FIRST TREAD GROOVE REVEALED A DISTORTED PORTION. SUBMITTER SUSPECTS THE INTERNAL CORDS MAY HAVE RUPTURED. THE RE ARE FOUR ADDITIONAL ITEMS IN THE SDR DATA BASE. 1 L 7 2 4T 4 T A24CE E4EA 1996121200525 19961212 00525 CE 1996 12 12 CA960404008 1 19960323 A 3244 22X675108190 TIRE PARKER HANNI 04020300 BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA TREAD BULGED W K NONE O OTHER IN INSP/MAINT 1 CA 813 1480 PCE81939 (CAN) BULGE ON LEFT INBOARD MAIN WHEEL TIRE TREAD NOTICED WHILE CARRYING OUT A DAILY INSPECTION. INSPECTION OF BULGED AR EA SEEMS TO INDICATE A SEPARATION IN THE FIRST TREAD GROOVE AND PART OF THE SIDE WALL. THERE ARE A TOTAL OF FIVE OCCURRE NCES OF THIS NATURE ON THE SDR DATABASE. 1 L 7 2 4T 4 T A24CE E4EA 1996121200526 19961212 00526 CE 1996 12 12 CA960404009 1 19960321 A 3211 501202011 SUPPORT BEECH 115810000605 BEECH 99 99 1154002 CE PWA PT6 PT6A27 52043 EA MLG DRAG LEG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA PCE40943 (CAN) DURING A DETAILED INSPECTION CRACKS WERE FOUND ON BOTH DRAG LEG SUPPORTS. NEW SUPPORTS INSTALLED AS PER BEECH SB 2 532. 1 L 7 2 3T 4 T A14CE E4EA 1996121200527 19961212 00527 SO 1996 12 12 CA960404013 1 19960325 A 3260 INDICATOR PIPER PA31 PA31350 7103110 SO MLG BROKEN WIRE W O OTHER N FALSE WARNING AP APPROACH 1 CA (CAN) ON APPROACH THE PILOT NOTICED THE MAIN LANDING GEAR RED TRANSIT LIGHT WAS LIT. AFTER LANDING, AN INDEPTH CHECK WAS MADE AND A BROKEN WIRE WAS FOUND. 1 L 7 2 3O A20SO 1996121200528 19961212 00528 CE 1996 12 12 CA960409027 1 19960328 A 7160 59550538 AFT VANE ASSY CESSNA 26580086 CESSNA 208 208B 2073701 CE PWA PT6 PT6A114 52043 NE INERTIAL SEP CRACKED W K NONE O OTHER CR CRUISE 1 CA 5981 PCE19139 (CAN PILOT REPORTED THAT WHILE IN CRUISE FLIGHT AN ATTEMPT WAS MADE TO RETRACT THE INERTIAL SEPARATOR. IT WAS FOUND THA T HE COULD NOT PUSH THE HANDLE IN. THE FLIGHT WAS COMPLETED WITHOUT INCIDENT AND MAINTENANCE FOUND THE SHAFT OF THE AFT VANE ASSEMBLY HAD CRACKED AT THE LOWER END AND WAS CAUSING THE INERTIAL SEPARATOR TO BIND. MAINTENANCE REPLACED THE VANE ASSEMBLY AND THE AIRCRAFT RETURNED TO SERVICE. 1 H 7 1 3T 3 T A37CE E4EA 1996121200529 19961212 00529 1996 12 12 CA960412001 4 19960401 A 3418 S24881 STALL WARN CESSNA 07133481 CESSNA 172 172P 2072436 CE MCAULY 1C160 1C160DTM GL STALL WARN SYS DEFECTIVE W D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CA BA026 (CAN) THE STALL WARNING REED WAS REPLACED DUE TO INTERMITTENT ACTIVATION IN THE STALL CONDITION. THE NEW REED ACTIVATED 2.6 HOURS LATER. THIS REED WAS REPLACED AND ANOTHER INSTALLED ONLY TO SOUND ANOTHER 1.3 HOURS INTO ITS SERVICE LIFE. IT WAS DISCOVERED THAT BOTH REEDS WOULD SOUND IN EITHER SUCTION OR PRESSURE TESTS. THE REED WAS REPLACED WITH A SERVICEABLE REED THAT SOUNDS ONLY IN SUCTION. 1 H 7 1 3O NT 3A12 5 N P910 1996121200530 19961212 00530 CE 1996 12 12 CA960412004 1 19960325 A 7110 H296K1135 LATCH ASSY BEECH 100 100BEECH 1152916 CE PWA PT6 PT6A28 EA COWL BROKEN HOOK W K NONE O OTHER IN INSP/MAINT 1 CA 50054 (CAN) HOOK BROKEN WHEN LATCHING COWL AFTER CHECKING OIL. SKETCH SHOWS BREAK OCCURRING ON THE HOOK PORTION OF THE ASSEMBL Y. 1 L 7 2 3T 4 T A14CE E4EA 1996121200531 19961212 00531 CE 1996 12 12 CA960412008 1 19960328 A 3246 5030001121 WHEEL HALF BEECH 5030001141 BEECH 90 C90 1152913 CE PWA PT6 PT6A28 EA BOLT HOLES CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 10172 A2754 PCE42311 (CAN) THE NOSE WHEEL WAS REMOVED FOR TIRE REPLACEMENT. THE WHEEL WAS DISASSEMBLED AND CLEANED AND READIED FOR INSPECTION . A MODERATE AMOUNT OF CORROSION WAS FOUND AND THE WHEEL HALF WAS DYE PENETRANT INSPECTED AND TWO CRACKS WERE FOUND LEAD ING AWAY FROM ONE OF THE BOLT HOLES. A VISUAL CRACK WAS NOTED AT ANOTHER OF THE BOLT HOLES. 1 L 7 2 3T 4 T 3A20 E4EA 1996121200532 19961212 00532 CE 1996 12 12 CA960418006 1 19960409 A 5711 50120151128 SPAR CAP BEECH 50120151618 BEECH 99 99A 1154003 CE PWA PT6 PT6A28 EA R/H WHEEL WELL CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 23000 50754 (CAN) SPAR CAP FOUND CRACKED IN THE RIGHT HAND WHEEL WELL. SECONDARY DAMAGE FOUND TO BE CRACKED SPLICE PLATES. 1 L 7 2 3T 4 T A14CE E4EA 1996121200534 19961212 00534 CE 1996 12 12 CA960423106 1 19960323 A 3246 10B29901 SHAFT PIVOT FEDERAL C3600 CESSNA 185 A185F 2072821 CE MCAULY D3A34 D3A34C403 GL WHEEL SKI BROKEN W A O OTHER O OTHER TX TAXI/GRND HDL 1 CA 108 805506 (CAN) WHILE TAXI TURNING, THE HYDRAULIC WHEEL SKI RIGHT HAND SHAFT PIVOT FRACTURED. THE FRACTURED OCCURRED AT THE STEP T RANSITION TO THE KEYWAYS. THIS ALLOWED THE SKI TO DEPART THE AIRCRAFT. THE SUBMITTER STATES THAT THE SHAFT DESIGN HAS LE FT SHARP EDGES AND SUBSEQUENT STRESS RISER IN THE STEP AREA. 1 H 7 1 3O 3A24 5 C P47GL 1996121200539 19961212 00539 SO 1996 12 12 CA960425101 1 19960311 A 2720 4004009 TORQUE TUBE PIPER 4004634 PIPER PA31 PA31350 7103110 SO RUDDER CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 9183 315302 (CAN) RUDDER TORQUE TUBE ASSEMBLY AND THE RIBS TO WHICH THE ASSEMBLY ATTACHES WERE FOUND TO BE CORRODED DUE TO WATER ENT RAPMENT. 1 L 7 2 3O A20SO 1996121200540 19961212 00540 CE 1996 12 12 CA960429003 1 19960301 A 2823 98510662 VALVE COVER CESSNA 98510674 CESSNA 172 172N 2072434 CE LYC O320 O320H2AD 41508 EA FUEL SELECT WORN W C D ABORTED TAKEOFF RETURN TO BLOCK O R OTHER PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CA 8274 RL112076T (CAN) AIRCRAFT LOST POWER ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED. WHEN THE FUEL SELECTOR WAS MOVED THE POWER WAS RESTO RED. INSPECTION OF THE VALVE SHOWED WEAR TRACKS BETWEEN THE DETENT LOCKING HOLES SO THAT POSITIONING OF THE SELECTOR HAN DLE WAS NOT IN THE PRECISE DETENT SPOT. VALVE WAS REWORKED AND A NEW VALVE WAS ORDERED. 1 H 7 1 3O 3 O NT 3A12 E274 1996121200542 19961212 00542 SO 1996 12 12 CA960430201 2 19960119 A 8520 CRANKSHAFT CESSNA 206 U206F 2073333 CE CONT O520 IO520F 17032 SO MCAULY 2A34C D2A34C58 GL MAIN BEARINGS FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 35 286376R 741571 (CAN) FOUND CRACK IN CRANKCASE AT #2 CYLINDER. #4 CONNECTING ROD DEPARTED CRANKSHAFT CAUSING INTERNAL ENGINE DAMAGE. DIS ASSEMBLY OF ENGINE FOUND ALL MAIN BEARING BABBITT OVERLAYS WERE SMEARED FROM OIL STARVATION. ALL CONNECTING ROD BEARINGS SMEARED FROM LUB DISTRESS. #3 & #4 CONNECTING RODS WERE OFF THE CRANKSHAFT. ROD BOLTS BROKEN FROM THERMAL HEATING DUE T O OIL STARVATION. OIL PUMP EXHIBITED VERY LITTLE DAMAGE TO THE CAVITY WALLS, INDICATING LITTLE OR NO CIRCULATION AS THE BEARINGS WERE BEING DAMAGED. ALL OIL PASSAGES WERE VERIFIED OPEN. OIL PUMP APPEARS FUNCTION. REASON FOR OIL STARVATION N OT DETERMINED FROM EXAMINATION OF THIS EXHIBIT. NO OIL LEAK PATHS WERE FOUND. 1 H 7 1 3O 3 O A4CE E5CE 5 C P3EA 1996121200543 19961212 00543 SW 1996 12 12 CA960502014 1 19960228 A 6710 206001342001 CYCLIC TUBE BELL 206 206L 1181522 SW ALLSN 250C 250C20B 03013 GL UPPER BOLT SLOT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 830805 (CAN) DYE PENETRANT INSPECTION REVEALED A SMALL CRACK IN UPPER MOUNTING BOLT SLOT. R/H SIDE OF OUTER TUBE. 1 G 7 1 3U 3 U H2SW E4CE 1996121200544 19961212 00544 EU 1996 12 12 CA960502015 1 19960216 A 6730 AC67244 SERVO SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE RT HYD SERVO ROUGH W O OTHER E VIBRATION/BUFFET CR CRUISE 1 CA 1679 878 (CAN) R/H HYDRAULIC SERVO COUPLING WITH COLLECTIVE SERVO IN ROUGH FLIGHT CONDITIONS. 1 G 7 1 3U 3 U H9EU E19EU 1996121200545 19961212 00545 EU 1996 12 12 CA960502016 1 19960227 A 5210 350A7500500003 DOOR SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE LOWER WINDOW INCORRECT ASSY W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 7720 835 (CAN) DOOR WOULD NOT CLOSE PROPERLY. LOWER WINDOW WAS NOT INSTALLED AS PER SB 52.08 1 G 7 1 3U 3 U H9EU E19EU 1996121200546 19961212 00546 NM 1996 12 12 CALA9601761 1 19961119 A 5320 SUBFLOOR BOEING 737 7373T0 1384582 NM BS 1026 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17316 23367 INSPECTION FOUND LT AFT LAV SUBFLOOR CORRODED AT BS 1026. REPAIRED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 1996121200547 19961212 00547 NM 1996 12 12 CALA9601762 1 19961119 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 967-986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17316 23367 INSPECTION FOUND INTERCOSTALS CORRODED FROM BS 967 TO 986, AT LBL 18 AND RBL 18. THE INTERCOSTALS WERE REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 1996121200548 19961212 00548 NM 1996 12 12 CALA9601763 1 19961119 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 947-967 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17316 23367 INSPECTION FOUND INTERCOSTALS CORRODED FROM BS 947 TO BS 967, AT LBL 18 AND RBL 18. THE INTERCOSTALS WERE REPLACED IAW SRM 51-10-02 AND ECRA 5310-03368. 2 L 7 2 4F RT A16WE 1996121200549 19961212 00549 NM 1996 12 12 CALA9601764 1 19961125 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM BS 950 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17316 23367 INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 950, RBL 40. REPAIRED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 1996121200550 19961212 00550 NM 1996 12 12 CALA9601765 1 19961119 A 5210 ANGLE BOEING 737 7373T0 1384582 NM R-2 DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17316 23367 INSPECTION FOUND R-2 DOOR Z-ANGLE CORRODED. A NEW Z-ANGLE WAS INSTALLED IAW SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A16WE 1996121200551 19961212 00551 NM 1996 12 12 CALA9601766 1 19961120 A 5320 ANGLE BOEING 737 7373T0 1384582 NM BS 787-847 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17316 23367 INSPECTION FOUND AFT CARGO CENTER FLOOR RIGHT SIDE AND CENTER ATTACH ANGLES CORRODED AROUND NUT PLATES BETWEEN STA 787 T O 847. REPAIRED IAW SRM 51-10-02 AND 53-00-53. 2 L 7 2 4F RT A16WE 1996121200552 19961212 00552 NM 1996 12 12 CALA9601767 1 19961209 A 2730 6595600642 CONTROL MODULE BOEING 727 727243 138408D NM ELEVATOR INOPERATIVE A CALA O OTHER K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SW 09 578PE 21661 THE AIRCRAFT LOST A-SYSTEM HYDRAULIC PRESSURE AND QUANTITY APPROXIMATELY 10 MINUTES AFTER TAKEOFF. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE A-SYSTEM ELEVATOR CONTROL MODULE AT FAULT. THE ELEVATOR CONTROL MODULE WAS REP LACED. THE NR 1 ENGINE DRIVEN PUMP WAS ALSO REPLACED DUE TO FAILURE. LEAK AND OPERATIONAL CHECKS WERE NORMAL. 2 L 7 3 4F RT A3WE 1996121200553 19961212 00553 NM 1996 12 12 CALA9601768 1 19961209 A 2450 734285E BUS PWR CONTL BOEING 757 757224 1384958 NM E/E COMPT INOPERATIVE A CALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 09 14114 6052 6052 27556 THE CREW RECEIVED EICAS MESSAGES, NOSE GEAR AIR GRND, RT PROBE HEAT, ANTI-SKID, RECIRC FANS AND HYD PUMPS AND EMERGENCY LIGHTS ILLUMINATED IN FLIGHT. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND RT DC BUS SEC 1 C/B TRIPPED. THE CIRCUIT BREAKER WAS RESET AND ALL SYSTEMS CHECKED NORMAL. THE BUS POWER CONTROL UNIT WAS REPLACED. BITE CHECK SHOWED RT GCU SERIAL LINK FAULT. THE RIGHT GCU WAS REPLACED, AN ENGINE RUN WAS ACCOMPLISHED AND ALL SYSTEMS CHECKED NORMAL. 2 L 7 2 4F RT A2NM 1996121200554 19961212 00554 NM 1996 12 12 CALA9601769 1 19961206 A 5320 WEB BOEING 737 737130 1384435 NM AFT LAV CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16201 19018 INSPECTION FOUND AFT LAV LT PAN CORRODED AROUND DUMP CHUTE AND CENTER SUBSTRUCTURE CHANNEL CORRODED AT UPPER SURFACE. T HE FLOOR WEB AND CENTER CHANNEL WERE REMOVED, A REPLACEMENT WEB AND CHANNEL WERE FABRICATED AND INSTALLED IAW SRM 51-30- 2, 51-10-2 AND 51-10-6. 2 L 7 2 4F A16WE 1996121200555 19961212 00555 NM 1996 12 12 CALA9601770 1 19961204 A 5320 STIFFENER BOEING 737 737130 1384435 NM BS 285.62 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16201 19018 INSPECTION FOUND STA 285.62 NOSE WHEEL WELL RT VERTICAL STIFFENER CORRODED 3 INCHES FROM LOWER END AND 2 INCHES FROM UPP ER END. THE VERTICAL STIFFENER WAS REMOVED, A REPLACEMENT STIFFENER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10 -2 AND BAC DRAWING 65-45819. 2 L 7 2 4F A16WE 1996121200556 19961212 00556 NM 1996 12 12 CALA9601771 1 19961207 A 5320 INTERCOSTAL BOEING 737 737130 1384435 NM BS 357 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16201 19018 INSPECTION FOUND A 1.5 INCH CRACK IN INTERCOSTAL AT STA 357, STRINGER 16L. A REPAIR DOUBLER WAS FABRICATED AND INSTALLE D IAW SRM 51-40-2 AND 51-30-2. 2 L 7 2 4F A16WE 1996121200557 19961212 00557 NM 1996 12 12 CALA9601772 1 19961207 A 5315 FLOORBEAM BOEING 737 737130 1384435 NM BS 328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16201 19018 INSPECTION FOUND FLOORBEAM UPPER T-CAP CORRODED AT STA 328, RBL 10 TO RBL 46. THE UPPER T-CAP WAS REMOVED, A NEW UPPER T-CAP WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-2. 2 L 7 2 4F A16WE 1996121200558 19961212 00558 WP 1996 12 12 CALA9601773 1 19961125 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 218-237 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND SEVERAL DENTS IN FUSELAGE SKIN AT STA 218 TO 237, LONGERON 14L TO 18L. NEW SKIN AND DOUBLERS WERE INST ALLED IAW ECRA 5330-02445 AND ECRA 5330-02471. 2 L 7 2 4F A6WE 1996121200559 19961212 00559 WP 1996 12 12 CALA9601774 1 19961125 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 1155-1211 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND FLOOR SUPPORT ANGLE CORRODED FROM STA 1155 TO 1211, LONGERON 29R. THE FLOOR SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-1. 2 L 7 2 4F A6WE 1996121200560 19961212 00560 WP 1996 12 12 CALA9601775 1 19961124 A 5320 CHANNEL DOUG DC9 DC982 3022082 WP BAGGAGE COMPT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND AFT BAGGAGE BIN DOOR THRESHOLD Z-CHANNEL CORRODED. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-05, FIGUR E 63. 2 L 7 2 4F A6WE 1996121200561 19961212 00561 WP 1996 12 12 CALA9601776 1 19961124 A 5542 SKIN DOUG DC9 DC982 3022082 WP RUDDER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND TOP LT SIDE OF RUDDER SKIN BENT WITH A 2 INCH CRACK. THE CRACKED AREA OF SKIN WAS CUT OUT AND A DOUBLE R WAS INSTALLED IAW SRM 55-01. 2 L 7 2 4F A6WE 1996121200562 19961212 00562 NM 1996 12 12 9626116301 1 19961209 A 3697 WIRE BOEING 747 747451 1384940 NM NR 1 ENG BLEED BROKEN A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 661US 23719 DURING TAKEOFF, AN ENG 1 BLEED EICAS MESSAGE DISPLAYED. AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE. REPAIRED BR OKEN WIRE ON TERMINAL NR 1 ON THE PNEUMATIC HIGH PRESSURE SHUTOFF VALVE, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1996121200563 19961212 00563 NE 1996 12 12 COMA9620019 3 19961207 A 6112 PROP DE-ICE SWRNGN SA227 SA227AC 8780603 SW MCAULY 4HFR34 4HFR34C652 NE RIGHT FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 703CA AC703 881381 RIGHT PROP DE-ICE INDICATES APPROXIMATELY 20 AMPS DURING ONE CYCLE. REPLACED RIGHT PROP, OPS CHECK GOOD. 2 L 7 2 4T RT A8SW 6 C 3PNE 1996121200564 19961212 00564 SO 1996 12 12 COMA9610340 1 19961209 A 5330 12019230001 SKIN EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 156CA 120156 DURING 2C INSPECTION, FOUND FUSELAGE BELLY SKIN SEVERELY CORRODED AT FRAME 23. THE DAMAGE WAS REPAIRED PER EMB120 SRM 5 3-00-01, FIG 202. 2 L 7 2 4T RT A31SO 1996121200565 19961212 00565 SO 1996 12 12 COMA9610341 1 19961209 A 5320 12005226001 CROSSBEAM EMB 120 EMB120RT SO FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 156CA 120156 DURING 2C INSPECTION, FOUND FUSELAGE FLOOR SUPPORT CROSSBEAM AT FRAME 20 WAS CRACKED BY MAINTENANCE PERSONNEL. THE CROS SBEAM WAS REPAIRED PER ERODESIGN REPORT NR 2117-1, REV IR, DATED 12-3-96. 2 L 7 2 4T RT A31SO 1996121200566 19961212 00566 SO 1996 12 12 COMA9610342 1 19961209 A 5320 12006664004 SILL EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 156CA 120156 DURING 2C INSPECTION, FOUND FUSELAGE CENTER SECTION FLOOR SUPPORT STRUCTURE RT SILL CORRODED. REPLACED RT SILL WITH NEW PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51. 2 L 7 2 4T RT A31SO 1996121200567 19961212 00567 SO 1996 12 12 COMA9610343 1 19961209 A 5320 12013133001 SUPPORT SECTION EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 156CA 120156 DURING 2C INSPECTION, FOUND FUSELAGE FWD RT SIDEWALL SEAT TRACK SUPPORTING SECTION CORRODED. REPLACED RT SUPPORT SECTIO N WITH NEW PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51. 2 L 7 2 4T RT A31SO 1996121200568 19961212 00568 SO 1996 12 12 COMA9610344 1 19961209 A 5320 12013136001 SUPPORT SECTION EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 156CA 120156 DURING 2C INSPECTION, FOUND FUSELAGE FWD LT SIDEWALL SEAT TRACK SUPPORTING SECTION CORRODED. REPLACED SUPPORTING SECTIO N WITH NEW PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51. 2 L 7 2 4T RT A31SO 1996121200569 19961212 00569 SO 1996 12 12 COMA9610345 1 19961209 A 5320 12007089003 BUTT STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 156CA 120156 DURING 2C INSPECTION, FOUND FUSELAGE FWD FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP CORRODED. REPLACED CENTER BUTT STRAP WITH NEW PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51. 2 L 7 2 4T RT A31SO 1996121200570 19961212 00570 SO 1996 12 12 COMA9610346 1 19961209 A 5320 12004149002 CROSSBEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 156CA 120156 DURING 2C INSPECTION, FOUND FUSELAGE FLOOR SUPPORT RT CROSSBEAM AT FRAME 16 HAD CORROSION. REPLACED RT CROSSBEAM WITH N EW PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51. 2 L 7 2 4T RT A31SO 1996121200571 19961212 00571 SO 1996 12 12 COMA9610347 1 19961209 A 5313 12006173003 STRINGER EMB 120 EMB120RT SO BS 4088 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 156CA 120156 DURING 2C INSPECTION, FOUND FUSELAGE STRINGER 18L CORRODED AT FWD END, FS 4088.0. REPAIRED STRINGER PER AERODESIGN REPO RT NR 1990-2, REV IR DATED 9-15-96. 2 L 7 2 4T RT A31SO 1996121200572 19961212 00572 SO 1996 12 12 COMA9610348 1 19961209 A 5320 12027289001 BUTT STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 156CA 120156 DURING 2C INSPECTION, FOUND FUSELAGE FWD FLOOR SUPPORT STRUCTURE LT BUTT STRAP CORRODED. REPLACED LT BUTT STRAP WITH NE W PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51 AND AERODESIGN REPORT 31671-2, REV IR, DATED 12-4-96. 2 L 7 2 4T RT A31SO 1996121200573 19961212 00573 SO 1996 12 12 COMA9610349 1 19961209 A 5320 12005802001 SILL EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 156CA 120156 DURING 2C INSPECTION, FOUND FUSELAGE FWD FLOOR SUPPORT STRUCTURE LT SILL CORRODED. REPLACED LT SILL PER EMB120 SRM STAN DARD PRACTICES, CHAPTER 51. 2 L 7 2 4T RT A31SO 1996121200574 19961212 00574 SO 1996 12 12 COMA9610350 1 19961209 A 5320 12014241001 CROSSBEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 156CA 120156 DURING 2C INSPECTION, FOUND FUSELAGE FWD FLOOR SUPPORT LT CROSSBEAM CORRODED. REPLACED CROSSBEAM WITH NEW PART PER EMB1 20 SRM STANDARD PRACTICES, CHAPTER 51. 2 L 7 2 4T RT A31SO 1996121200575 19961212 00575 SO 1996 12 12 COMA9610351 1 19961209 A 5320 12026671001 BUTT STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 156CA 120156 DURING 2C INSPECTION, FOUND FWD FUSELAGE FLOOR SUPPORT STRUCTURE LT BUTT STRAP CORRODED. REPLACED LT BUTT STRAP WITH NE W PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51. 2 L 7 2 4T RT A31SO 1996121200576 19961212 00576 SO 1996 12 12 COMA9610352 1 19961209 A 5320 12005805003 BUTT STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 156CA 120156 DURING 2C INSPECTION, FOUND FUSELAGE FWD CENTER FLOOR SUPPORT STRUCTURE BUTT STRAP CORRODED. REPLACED CENTER BUTT STRAP WITH NEW PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51. 2 L 7 2 4T RT A31SO 1996121200577 19961212 00577 SO 1996 12 12 COMA9610353 1 19961209 A 5320 12005803003 BUTT STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 156CA 120156 DURING 2C INSPECTION, FOUND FUSELAGE FWD FLOOR STRUCTURE RT BUTT STRAP CORRODED. REPLACED BUTT STRAP WITH NEW PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51. 2 L 7 2 4T RT A31SO 1996121200578 19961212 00578 SO 1996 12 12 COMA9610354 1 19961209 A 5320 12005803001 SILL EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 156CA 120156 DURING 2C INSPECTION, FOUND FUSELAGE FWD FLOOR STRUCTURE RT SILL CORRODED. REPLACED SILL WITH NEW PART PER EMB120 SRM S TANDARD PRACTICES CHAPTER 51. 2 L 7 2 4T RT A31SO 1996121200579 19961212 00579 SO 1996 12 12 COMA9610355 1 19961209 A 5330 12006631001 SKIN EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 156CA 120156 DURING 2C INSPECTION, FOUND FUSELAGE INNER SKIN FOUND CORRODED AT PAX DOOR CUTOUT, BENEATH BOTTOM FWD DOOR CUTOUT REINFO RCEMENT DOUBLER. THE DAMGE WAS REPAIRED PER AERODESIGN REPORT NR 2118-1, REV IR, DATED 12-3-96. 2 L 7 2 4T RT A31SO 1996121200580 19961212 00580 SO 1996 12 12 COMA9610356 1 19961206 A 3233 ACTUATOR EMB 120 EMB120RT SO RT MLG OUT OF ADJUST A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 257CA 120248 AFTER TAKEOFF, RIGHT MAIN LANDING GEAR WOULD NOT RETRACT. RETURN TO AIRPORT. ADJUSTED RIGHT MAIN LANDING GEAR ACTUATOR , OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 1996121200581 19961212 00581 SO 1996 12 12 COMA9610357 1 19961208 A 3260 922FS2A6NZ735 PROX SENSOR EMB 120 EMB120RT SO LT MLG INOPERATIVE A COMA K NONE J WARNING INDICATION TO TAKEOFF 1 SO 01 189CA 120189 LANDING GEAR WILL NOT RETRACT, HANDLE WILL NOT MOVE TO UP POSITION. REPLACED LEFT STRUT PROX SENSOR, OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 1996121200582 19961212 00582 EA 1996 12 12 COMA9660220 1 19961209 A 3010 124112450 THERMAL SWITCH CNDAIR CL600 CL6002B19 EA RT WING FAILED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 915CA 7013 RT WING ANTI-ICE WARNING CAME ON. REPLACED FOUR SENSORS FOR RT WING. 2 L 7 2 4F RT A21EA 1996121200583 19961212 00583 EA 1996 12 12 COMA9660221 1 19961209 A 2761 270003 PCU CNDAIR CL600 CL6002B19 EA LT FLT SPOILER FAILED A COMA K NONE J WARNING INDICATION UK UNKNOWN 1 SO 01 943CA 7062 FLIGHT SPOILER CAUTION MESSAGE ON. REPLACED LEFT OUTBOARD FLIGHT SPOILER POWER CONTROL UNIT. 2 L 7 2 4F RT A21EA 1996121200584 19961212 00584 WP 1996 12 12 QXEA9600439 2 19961021 A 7260 31030351 BEARING SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP NR 2 ENGINE FAILED A A QXEA A UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 NM 09 386PH AC597 P44257 DURING FLIGHT 19,000 FT WITH CLEAR CONDITIONS AND NO ICE, THE NR 2 ENGINE FLAMED OUT. NO ABNORMAL INDICATIONS PRIOR TO FLAME-OUT. AIRSTART WAS UNSUCCESSFUL, NO FUEL FLOW. AIRCRAFT MADE AN UNSCHEDULED LANDING IN FCA WITHOUT FURTHER PROBLE M. NR 2 ENGINE REPLACED IAW MM AND ENGINE OPS CHECKED GOOD ON GROUND RUN. AIRCRAFT RETURNED TO SERVICE. ENGINE TEARDO WN REVEALED THE SECOND IDLER GEAR BEARING WAS FOUND TO BE COMING APART. WHEN BEARING FAILED IT UNCOUPLED THE FUEL CONTR OL DRIVE GEAR. THE MOST LIKELY CAUSE OF THE BEARING FAILURE WAS A DENTED BALL OR A MATERIAL FLAW, THE EXACT CAUSE CAN N OT BE DETERMINED DUE TO THE EXTENSIVE SECONDARY DAMAGE. 2 L 7 2 4T 4 T RT A8SW E4WE 1996121200585 19961212 00585 WP 1996 12 12 ABXA9600677 1 19961123 A 3260 GEAR INDICATION DOUG DC8 DC861 3021952 WP NLG MALFUNCTIONED A ABXA O OTHER N FALSE WARNING AP APPROACH 1 GL 23 853AX 46037 ON FIRST GEAR EXTENSION ATTEMPT, NOSE GEAR GREEN LIGHT WOULD NOT COME ON. RECYCLED GEAR, HAD A GOOD INDICATION ON SECON D TRY. AIRCRAFT JACKED AND GEAR SWING COMPLIED WITH, NO DEFECTS NOTED IAW DC-8 MM 32-60-0. 2 L 7 4 4F 4A25 1996121200586 19961212 00586 WP 1996 12 12 ABXA9600678 1 19961205 A 3260 GEAR INDICATION DOUG DC8 DC861 3021952 WP NLG MALFUNCTIONED A ABXA O OTHER N FALSE WARNING AP APPROACH 1 GL 23 853AX 46073 ON FINAL WHEN GEAR HANDLE PUT IN DOWN POSITION, NO NOSE GEAR GREEN LIGHT, HAD GEAR UNSAFE LIGHT. RECYCLED GEAR, GOT NOR MAL INDICATION. PERFORMED ADJUSTMENT TEST OF NOSE LANDING GEAR SYSTEM IAW DC-8 MM 32-31-0. OPERATIONAL CHECK OF INDICA TION AND MECHANICAL SYSTEMS CHECKED NORMAL ON SEVERAL GEAR SWINGS. 2 L 7 4 4F 4A25 1996121200587 19961212 00587 WP 1996 12 12 MWEA96646 1 19961207 A 5330 SKIN DOUG DC9 DC915 3022036 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 DURING INSPECTION, FOUND SKIN AROUND LAV SERVICE PORT HAS SMALL AREA OF CORROSION BEYOND LIMIT. BLENDED CORROSION AND I NSTALLED DOUBLER REPAIR IAW SRM 53-01 FIG 2 SHT 3. 2 L 7 2 4F A6WE 1996121200588 19961212 00588 WP 1996 12 12 MWEA96647 1 19961207 A 2560 113317 EVAC SLIDE DOUG DC9 DC932 3022066 WP FWD ENTRY DOOR FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 602ME 48133 CREW REPORTS, FWD ENTRY DOOR EVACUATION SLIDE FELL OFF. REINSTALLED FWD ENTRY DOOR EVACUATION SLIDE. 2 L 7 2 4F A6WE 1996121200589 19961212 00589 WP 1996 12 12 MWEA96648 1 19961207 A 2560 113317 EVAC SLIDE DOUG DC9 DC932 3022066 WP FWD ENTRY DOOR FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 209ME 47730 CREW REPORTS, FWD ENTRY DOOR EVACUATION SLIDE FELL OFF. REINSTALLED FWD ENTRY DOOR EVACUATION SLIDE. 2 L 7 2 4F A6WE 1996121200590 19961212 00590 WP 1996 12 12 MWEA96649 1 19961208 A 2560 113317 EVAC SLIDE DOUG DC9 DC932 3022066 WP FWD GALLEY DOOR FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 401ME 47133 CREW REPORTS, FWD GALLEY DOOR EVACUATION SLIDE FELL OFF DOOR. REINSTALLED FWD GALLEY DOOR EVACUATION SLIDE. 2 L 7 2 4F A6WE 1996121200591 19961212 00591 NM 1996 12 12 DLM88962592 1 19961126 A 3350 07912 BULB DOUG MD88 MD88 3023688 NM CABIN MISSING A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 960DL 49979 EMERGENCY TRACK LIGHT BULB AND COVER MISSING AT 4C. INST NEW BULB AND MODULE, CK'S OK (P/N 0L3071BPEGPL). 2 L 7 2 4F RT A6WE 1996121200592 19961212 00592 WP 1996 12 12 DLL14962594 1 19961126 A 7110 UL12586 CORE COWL LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB211524B4 54555 NE NR 3 ENGINE MISSING A DALA K NONE D INFLIGHT SEPARATION NR NOT REPORTED 1 SO 27 1738D 193C1234 14874 RIGHT CENTER SECTION CORE COWL MISSING ON ARRIVAL. INSTALLED BOTH GENERATOR FAIRINGS AND LOWER HOT SECTION FAIRING. RA N ENGINE, ALL SYSTEMS OK. 2 L 7 3 4F 4 F A23WE E12EU 1996121200593 19961212 00593 NM 1996 12 12 DL72E962598 1 19961126 A 2782 BRACKET BOEING 727 727247 138408F NM NR1 LE FLAP ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 283WA 21485 FOUND ON A1 LETTER CK, NR 1 L/E FLAP ACTUATOR I/B ATTACH BRACKET CRACKED. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1996121200594 19961212 00594 NM 1996 12 12 DLM88962599 1 19961127 A 2170 21D101 WATER SEPARATOR DOUG MD88 MD88 3023688 NM CABIN DIRTY A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 954DL 49885 F/A REPORTED, LAV SMOKE ALARM ON F/O SIDE WENT OFF AND WOULD NOT STOP. SMELLED SMOKE LATER, REPORTED IT SMELLED ELECTRI CAL. INSPECTED RIGHT AFT LAV, NOTHING FOUND. REPLACED SMOKE DETECTOR, WATER SEPARATOR BAGS AND PERFORMED CROSS OVER D UCT BURNOUT PROCEDURE PER M/M 36-10-00 PG 507 TO 508, RAN PACKS AND ALL CHECKS OK. 2 L 7 2 4F RT A6WE 1996121200595 19961212 00595 WP 1996 12 12 DLL10962600 1 19961124 A 5320 PRESS PANEL LKHEED 1011 10113851 5265010 WP BS 1212 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 728DA 193C1173 CORROSION ON FS 1212 BELOW CANTED PRESSURE PANEL IN RIGHT W/WAT APPROX RBL 96.5, NON-ROUTINE CARD 3. REMOVED VERT STIFF NER AT RBL 96, FABRICATED DOUBLER AND FILLER, REMOVED CORROSION. HFEC INSP OF BLENDED AREA OK. ROTO PEENED BLENDED ARE A PER PS 900-4 NR 5, FABRICATED SHIMS, CONT ON NR 16, DRILLED TREATED AND PAINTED FILLERS AND FITTING. TREATED AND PAIN TED EFFECTED AREA ON WEB, GOT OK TO INSTALL PER QA. INSTALLED AND FINISHED REPAIR, INSTALLATION OK PER QA. 2 L 7 3 4F A23WE 1996121200596 19961212 00596 WP 1996 12 12 DLL10962601 1 19961128 A 3350 POWER PACK 5165741 LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 721DA 62822 193C1139 DURING L/O CK, FOUND EMERGENCY LIGHTS INOP AT L-1 CABIN DOOR. REPLACED POWER PACK AT L-1 DOOR, OPS CKS OK. 2 L 7 3 4F A23WE 1996121200597 19961212 00597 NM 1996 12 12 DL72W962602 1 19961128 A 3350 BATTERY PACK 900542 BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 292WA NA 22110 DURING L/O CK, FOUND RIGHT SIDE OVERWING EXIT LIGHTS INOP. REPLACED BATTERY PACK, OPS CKS OK. 2 L 7 3 4F A3WE 1996121200598 19961212 00598 NM 1996 12 12 DL72E962603 1 19961127 A 2150 PACKS BOEING 727 727247 138408F NM LT/RT MALFUNCTIONED A DALA B H EMER. DESCENT DEACTIVATE SYST/CIRCUITS G MULTIPLE FAILURE CR CRUISE 1 SO 27 830WA 21482 DOUBLE PACK TRIP OFF AT FL370, MIX VALVES IN MID RANGE. PACKS RECOVERED AND OPERATED NORMALLY AFTER BEING TURNED OFF AN D THEN BACK ON AT FL240. PERFORMED PACK TRIP CHECK PER M/M 21-11-00, CHECKED OK. 2 L 7 3 4F A3WE 1996121200599 19961212 00599 WP 1996 12 12 DLL16962604 1 19961128 A 7603 THROTTLE LEVER LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE NR 3 ENGINE STUCK A DALA E ENGINE SHUTDOWN O OTHER DE DESCENT 1 SO 27 762DA 49328 193Y1210 14733 NR 3 THROTTLE WILL NOT RETARD PAST 2.2 UNITS ON DESCENT. ALSO, STIFF TO MOVE FWD BUT WILL MOVE FWD, HAD TO SHUT DOWN NR 3 ENG. NIL FAULT OR WEAR FOUND THROTTLE MOVEMENT CHECKED THROUGH COMPLETE RANGE AND FOUND NORMAL WITH NO EXCESSIVE FOR CE REQUIRED. BASIC RIG CHECK OUT AND IDLE TO STOP CHECK OK. 2 L 7 3 4F 4 F A23WE E12EU 1996121200600 19961212 00600 NM 1996 12 12 DL72S962607 1 19961121 A 5330 6518420282 SKIN BOEING 727 727232 1384082 NM L1 DOOR CUTOUT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 408DA 21152 FOUND A GOUGE IN THE LOWER FUSELAGE SKIN JUST AFT OF THE L-1 DOOR. REPAIRED PER DAL EO 4-60829-3 AND ER/A 30446-14, REV A. 2 L 7 3 4F A3WE 1996121200601 19961212 00601 NM 1996 12 12 DL72P962608 1 19961120 A 5730 65877411 SKIN BOEING 727 727225 1384077 NM BS 830-840 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8890Z 21859 FOUND CORROSION ON THE LOWER SKIN BETWEEN S-4C AND S-3C AND BETWEEN BS 830 AND BS 840. REPAIRED IN ACCORDANCE WITH DAL ER/A 304410-14AD, REV B. 2 L 7 3 4F A3WE 1996121200602 19961212 00602 NM 1996 12 12 DL73K962609 1 19961120 A 5312 BULKHEAD BOEING 737 737232 1384475 NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 306DL 23078 THE STATION 178 BULKHEAD WAS FOUND CRACKED IN SEVERAL LOCATIONS. DAMAGE CUTOUTS ARE: 1 X 1.75 AT RBL 5.7, WL 198; 1 X 1 AT RBL 5.7, WL 201; 1 X 1 AT LBL 5.7, WL 198; 1 X 1 AT LBL 5.8, WL 201; 1 X 1.75 AT LBL 5.7, WL 201. THE BULKHEAD WEB IS FABRICATED FROM 0.032 CLAD 2024-T3. IN ADDITION, THE VERTICAL STIFFENER AT LBL 5.7 WL 184 WAS FOUND CRACKED. T HE RESULTING CUTOUT REMOVES THE FLANGE COMMON TO THE BULKHEAD WEB. THE VERTICAL STIFFENER IS MANUFACTURED FROM 7075-T6 EXTRUSION PER BAC1505-100361. REPAIRED PER DAL ER/A 304439-14, REV A. 2 L 7 2 4F RT A16WE 1996121200603 19961212 00603 NM 1996 12 12 DL72S962610 1 19961130 A 3350 BATTERY PACK RPS1 BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 420DA 21273 F/C EMERGENCY TRACK LIGHTS INOP. REPLACED CHARGER AND BATTERY. 2 L 7 3 4F A3WE 1996121200604 19961212 00604 NM 1996 12 12 DL757962612 1 19961130 A 2120 AIR DISTR BOEING 757 757232 1384965 NM CABIN ODOR A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 646DL 24217 RETURNED DUE TO SMELL OF BURNING RUBBER ON TAKEOFF IN COCKPIT AND MID PORTION OF CABIN. CKD E/E COMP, CARGO COMP AND WH EEL WELL AREAS AND NO DISCREPANCIES NOTED. RAN BOTH ENGS AND OPERATED PACKS FROM ENG BLEEDS, FOUND NO ODOR. 2 L 7 2 4F RT A2NM 1996121200605 19961212 00605 NM 1996 12 12 DL72L962613 1 19961201 A 3397 WIRE HARNESS BOEING 727 727232 1384082 NM CABIN BURNED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 513DA 21315 DURING TAXI OUT, THE LEFT AFT CEILING PASSENGER CABIN LIGHTING CIRCUIT BREAKER POPPED. UNABLE TO RESET. FLIGHT ATTENDA NT REPORTED A SMOKE SMELL. RETURNED TO GATE. REPAIRED BURNED WIRE BUNDLE ABOVE CEILING PANEL AT SEAT 10ABC PER BOEING WIRING PRACTICES MANUAL 20-00-13 AND WIRING DIAGRAM 33-22-01, PG 5, SHEET 1, SYSTEM CHECKS NORMAL. 2 L 7 3 4F A3WE 1996121200606 19961212 00606 WP 1996 12 12 DLL10962614 1 19961122 A 5312 BULKHEAD LKHEED 1011 10113851 5265010 WP BS 1212 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 712DA 193C1088 BS 1212 BULKHEAD WAS FOUND CRACKED AT LBL 30 AND RBL 6. THE CRACKS MEASURED 1 AND 8 RESPECTIVELY. DURING REPAIR THE TE E STIFFENER AND THE UPPER CAP WERE MISDRILLED. THE HOLES ARE BUSHED TO FIRST OVERSIZE AND THE RBL 6 LOCATION REQUIRED A CHANGE TO THE DOUBLER PROFILE. INSTALLED DOUBLER. 2 L 7 3 4F A23WE 1996121200607 19961212 00607 WP 1996 12 12 DLL15962615 1 19961118 A 5330 SKIN LKHEED 1011 10113853 5265020 WP BS 639 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 754DL 193Y1181 THE FUSELAGE SKIN WAS SEVERLY CORRODED AND CRACKED BETS FS 629 TO 659 AND STR 32 TO 34, DIMENSIONS: 30 X 20. THIS WAS R EPAIRED BY TRIMMING THE SKIN TO REMOVE ALL CORROSION AND REPAIRING SKIN AND STRAPS SIMILAR TO L1011 SRM 53-31-00. 2 L 7 3 4F A23WE 1996121200608 19961212 00608 WP 1996 12 12 DLL12962616 1 19961117 A 5312 1504400113 BULKHEAD LKHEED 1011 1011385115 5265015 WP BS 1212 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 724DA 193C1151 A CRACK WAS FOUND AT FS 1212 BULKHEAD RBL 42.5. THE CRACK WAS TRIMMED OUT, FILLED AND REINFORCED. REVISION A: CORRECT ED FASTENER PATTERN ON FIGURE 1, CHANGED RESTRICITONS TO 12 MONTHS. REVISION B: ADDED FAA APPROVAL. 2 L 7 3 4F A23WE 1996121200609 19961212 00609 WP 1996 12 12 DLL10962619 1 19961202 A 5230 SEAL 1522481133 LKHEED 1011 10113851 5265010 WP CARGO DOOR MISSING A DALA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 27 716DA NA 193C1095 AT 27,000 FT IN CRUISE, CABIN STARTED CLIMBING AT 7,200 FPM EMERGENCY DESCENT INITIATED. ALL CHECKLIST COMPLIED WITH. A T 7,000 FT CABIN CONTROL WAS RE-ESTABLISHED. FOUND C-2 CARGO UPPER DOOR SEAL MISSING. REPLACED TOP SECTION FROM TOP CO RNER TO TOP CORNER. PRESSURIZED A/C, OPN NORMAL. 2 L 7 3 4F A23WE 1996121200610 19961212 00610 NM 1996 12 12 DL75A962620 1 19961201 A 3350 BATTERY PACK BOEING 757 757212 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 750AT NA 23126 FIRST CLASS TRACK LIGHTING INOP. REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CHK NML. 2 L 7 2 4F RT A2NM 1996121200611 19961212 00611 1996 12 12 DL76L962621 4 19961130 A 3460 CDU 4058650931 BOEING 767 767332 1382001 NM COCKPIT MALFUNCTIONED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 180DN 95032474 25985 F/O CDU SCREEN FAILED, UNABLE TO FLY TRACK. DIVERTED TO JFK. REPLACED NR 2 FMS CDU, OPS NOW NORMAL. 2 L 7 2 4F RT A1NM 1996121200612 19961212 00612 NM 1996 12 12 DL72S962622 1 19961202 A 5720 STIFFENER BOEING 727 727232 1384082 NM RT WING SPAR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 482DA 20862 FOUND ON C1 LETTER CK, 2 INCH CRACK IN WING FWD SPAR STIFFNER AT THE NR 7 SLAT INBD TRACK. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1996121200613 19961212 00613 NM 1996 12 12 DLM88962623 1 19961202 A 3350 BATTERY PACK 6011779 DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 909DE 861 53418 LEFT AND RIGHT EMERGENCY EXIT LIGHTS INOP. REPLACED POWER SUPPLY AND BATTERY PACK, SYSTEM CHECKS NORMAL. 2 L 7 2 4F RT A6WE 1996121200614 19961212 00614 NM 1996 12 12 DL73K962625 1 19961202 A 3350 BATTERY PACK 20131A BOEING 737 737232 1384475 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 321DL NA 23093 ON L/O, FOUND MID CABIN OVERHEAT EMERGENCY LIGHT AND LIGHT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK, CKS NO RMAL. 2 L 7 2 4F RT A16WE 1996121200615 19961212 00615 NM 1996 12 12 DL767962628 1 19961203 A 2422 INVERTER 111101020 BOEING 767 767232 1385132 NM E/E COMP FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 109DL 006 22221 HAD STATIC INVERTER MSG ON EICAS FOLLOWED BY SMELL OF SMOKE. A/C DIVERTED INTO BIS. STATIC INVERTER WAS REPLACED AND F LT CONTINUED ON TO PDX. 2 L 7 2 4F RT A1NM 1996121200616 19961212 00616 NM 1996 12 12 DL72E962629 1 19961203 A 7997 WIRE BOEING 727 727247 138408F NM NR 2 ENGINE DAMAGED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 830WA 21482 NR 2 ENGINE OIL TEMP GUAGE PEGGED OUT HIGH DURING CLIMB AND CRUISE. PULLING THE THROTTLE TO IDLE MADE THE GUAGE FLUCTUA TE BETWEEN THE YELLOW AND RED RADIAL. REMOVED AND REPLACED OIL TEMP BULB AND TEMP IND, NO HELP. REINSTALLED ORIGIND. D URING INSP, FOUND BROKEN GROUNDING WIRE. REPAIRED WIRE, RAN NR 2 ENG PER PFHB AND OIL TEMP IND NORMAL. 2 L 7 3 4F A3WE 1996121200617 19961212 00617 NM 1996 12 12 DL72S962631 1 19961203 A 3350 6104789 BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 519DA 21470 ON LAYOVER, FOUND L1 DOOR SLIDE LIGHT INOP. REPLACED BATTERY PACK, CHECKS OK. 2 L 7 3 4F A3WE 1996121200618 19961212 00618 NM 1996 12 12 DL73E962632 1 19961204 A 2150 RELAY 655281025 BOEING 737 737247 138448D NM E/E COMPT MALFUNCTIONED A DALA D RETURN TO BLOCK O OTHER CL CLIMB 1 SO 27 237WA D00356 23185 DID NOT PRESS AFTER T/O, OUTFLOW VALVE FULL CLOSED. NOTICED PACKS NOT RUNNING. RERACKED AIRCOND RELAY UNIT, OPN NRML. REPLACED AIRCOND RELAY UNIT, OPN NORMAL AND PAC OPN NORMAL. 2 L 7 2 4F A16WE 1996121200619 19961212 00619 NM 1996 12 12 DL72K962633 1 19961204 A 5754 651622295 SKIN BOEING 727 727232 1384082 NM RT LE FLAPS CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 472DA 20749 LOWER SKIN CRACKED AT O/B END. REPAIRED SKIN PER M/M 57-54-00 FIG 801. 2 L 7 3 4F A3WE 1996121200621 19961212 00621 NM 1996 12 12 DL72S962637 1 19961202 A 3350 079123 BULB 079123 BOEING 727 727232 1384082 NM CABIN MISSING A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 538DA NA 22076 EMERGENCY PATH LIGHTS MISSING LENSES IN AFT CABIN AND ONE LIGHT HAS WIRE DAMAGED. REPLACED MISSING LENSES AND REPLACED ONE BULB AND SOCKET ASSY, OPS CKS OK. 2 L 7 3 4F A3WE 1996121200622 19961212 00622 NM 1996 12 12 DL72K962639 1 19961204 A 3213 STRUT 655790120 BOEING 727 727232 1384082 NM RT MLG CRACKED A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 412DA 1M25 21232 RT MLG UNSAFE LIGHT ILLUMINATED ON ROLLOUT AT APPROX 70 KNOTS. FOUND RT MLG CYLINDER CRACKED IN HALF. REPLACED CYLINDE R. 2 L 7 3 4F A3WE 1996121200623 19961212 00623 WP 1996 12 12 DLL15962640 1 19961204 A 3350 LIGHT LKHEED 1011 10113853 5265020 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 752DA 193W1172 ON CABIN CHECK FOUND LEFT PATH LIGHT AT SEATS 35, 25, 21 INOP AND COVER MISSING. INSTALLED COVERS AND BULBS, OPS OK. 2 L 7 3 4F A23WE 1996121200624 19961212 00624 NM 1996 12 12 DL72S962641 1 19961204 A 3350 BATTERY PACK 6104789 BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 400DA NA 21144 L1 AND R1 DOOR EMERGENCY EXTERIOR LIGHTS INOP. REPLACED BATTERY, CHECKS NORMAL. 2 L 7 3 4F A3WE 1996121200625 19961212 00625 NM 1996 12 12 DLM88962645 1 19961205 A 3350 LIGHT DOUG MD88 MD88 3023688 NM CABIN MISSING A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 912DE 49997 EMERGENCY TRACK LIGHT MISSING AT SEAT 1 CD. INSTALLED BULB AND LENS, OPS CHK NORMAL. 2 L 7 2 4F RT A6WE 1996121200626 19961212 00626 NM 1996 12 12 DLM88962649 1 19961205 A 3350 LIGHT DOUG MD88 MD88 3023688 NM CABIN MISSING A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 912DE 49997 ONE WHITE TRACK LIGHT MISSING AT SEAT 1 CD. INSTALLED BULB AND LENS IN TRACK LIGHT AT 1 CD. 2 L 7 2 4F RT A6WE 1996121200627 19961212 00627 NM 1996 12 12 DL72W962650 1 19961125 A 5210 FRAME BOEING 727 727247 138408F NM R2 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2821W 21059 A .375 INCH CRACK R-2 DOOR FRAME AT UPPER HINGE CUTOUT. REMOVED DOOR FROM A/C, REPAIRED DOOR FRAME PER SRM 52-40-2. 2 L 7 3 4F A3WE 1996121200628 19961212 00628 NM 1996 12 12 DL72W962651 1 19961202 A 5210 FRAME BOEING 727 727247 138408F NM R1 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2821W 21059 R-1 DOORS 550 HAS A 1.5 INCH CRACK IN AFT LOWER FRAME AT CUTOUT FOR LOCK MECHANISM. DRILLED UP REPAIR DOUBLER PER M/M 5 2-12-0 PG 807, INSTALLED DOUBLER PER M/M 52-12-0 PG 807, CLOSED WEB. 2 L 7 3 4F A3WE 1996121200629 19961212 00629 NM 1996 12 12 DLM88962652 1 19961205 A 2420 780029700 WIRE DOUG MD88 MD88 3023688 NM CARGO COMPT WORN A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 901DL 49532 FIRE DAMAGE FWD CARGO BIN AT STA 225 UNDER LT SLANT PANEL, FOUND 6 HOLE BURNED IN PLASTIC DRIP SHIELD. ALSO, FIBERGLASS FLOOR PANEL SIDEWALL MOUNTED PNEUMATIC DUCT AND WIRING CHARRED. REMOVED PNEU DUCT FOR VISUAL INSP OF STRUCTURE, INSPEC TED SKIN, STRC FRAME AND STRUCTURE, NO HEAT DAMAGE. CAUSE OF DAMAGE FOUND TO BE GENERATOR FEEDER CABLE. REPLACED FEEDE R CABLE ON NR 500. 2 L 7 2 4F RT A6WE 1996121200630 19961212 00630 NM 1996 12 12 DL72K962653 1 19961206 A 3350 BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 412DA 21232 L-2, R-2 EMERGENCY SLIDE LIGHT INOP. REPLACED L-2 , R-2 EMERGENCY SLIDE LIGHT BATTERY PACK, CHECKS NORMAL. 2 L 7 3 4F A3WE 1996121200631 19961212 00631 NM 1996 12 12 DL72S962654 1 19961206 A 3350 POWER SUPPLY BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 407DA 21151 LEFT AFT OVERWING EMERGENCY LIGHT INOP. REPLACED POWER SUPPLY, OPS CHECKS GOOD. 2 L 7 3 4F A3WE 1996121200632 19961212 00632 NM 1996 12 12 DL72S962655 1 19961205 A 3244 B727M TIRE BOEING 727 727232 1384082 NM RT MLG FAILED A DALA K NONE O OTHER TO TAKEOFF 1 SO 27 533DA 22046 NR 4 BLEW ON T/O. REPLACED NR 3, 4 MAIN WHEEL ASSY. A/C FERRIED TO DFW ACCT OF DAMAGE TO RT INBD MID FLAP AND RT MAIN GEAR WING DOOR. 2 L 7 3 4F A3WE 1996121200633 19961212 00633 NM 1996 12 12 DL72L962658 1 19961206 A 3350 079123 LENS BOEING 727 727232 1384082 NM CABIN MISSING A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 502DA 21304 ONE EMERGENCY EXIT RED TRACK LIGHT INOP. LENS MISSING NEAR AFT GALLEY. INSTALLED NEW LENS, OPN CKS NORMAL. 2 L 7 3 4F A3WE 1996121200634 19961212 00634 NM 1996 12 12 DL72W962659 1 19961206 A 5754 ANGLE BOEING 727 727247 138408F NM NR 2 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2814W 20870 FOUND DURING A-2 LETTER CHECK, 2 INCH CRACK NR 2 L/E SLAT COVE SKIN ATTACH ANGLE AT O/B UPSTOP PAD. REPAIRED PER M/M 57 -54-0PAR 12. 2 L 7 3 4F A3WE 1996121200635 19961212 00635 NM 1996 12 12 DL733962660 1 19961207 A 5400 311A106597 ACCESS PANEL BOEING 737 737347 1384647 NM NR 2 ENGINE MISSING A DALA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 SO 27 305WA 23346 721456 ACCESS PANEL ON TOP OF STARBOARD ENGINE CAME OFF AFTER TAKEOFF. FOUND PANEL 5727R MISSING. INSTALLED NEW PANEL, INSPEC TED A/C AND FOUND NO OTHER DAMAGE MADE BY PANEL. 2 L 7 2 4F RT A16WE 1996121200637 19961212 00637 WP 1996 12 12 DLL10962664 1 19961202 A 5312 1642621 BULKHEAD LKHEED 1011 10113851 5265010 WP BS 499 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 722DA 193C1147 DURING INSPECTION OF THE FS 499 BULKHEAD, ADDITIONAL CRACKS WERE FOUND. ORIGINALLY THIS LOCATION HAD BEEN MODIFIED PER A LAX SB. 2 L 7 3 4F A23WE 1996121200638 19961212 00638 WP 1996 12 12 DLL17962665 1 19961201 A 5311 FRAME LKHEED 1011 10113853 5265020 WP BS 983 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 768DL 193H1216 DURING AN INSPECTION PER DAL SI 7-63916-12AD, A CRACK WAS FOUND IN THE HORIZONTAL STIFFENING FLANGE. 2 L 7 3 4F A23WE 1996121200639 19961212 00639 WP 1996 12 12 DLL13962666 1 19961126 A 5320 SUPPORT FITTING LKHEED 1011 10113851 5265010 WP BS 449 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 789DL 193A1142 FURTHER CRACKING WAS FOUND IN BOTH THE LT AND RT NLG SHOCK STRUT SUPPORT FITTINGS. 2 L 7 3 4F A23WE 1996121200640 19961212 00640 WP 1996 12 12 DLL17962667 1 19961208 A 3350 BULB LKHEED 1011 10113853 5265020 WP CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 767DA 193H1209 LT EMERGENCY PASS LIGHTS ROW 33 AND 30 OUT. RELAMPED PASS LIGHTS AT ROW 33 AND 30, OPS CHECK OK. 2 L 7 3 4F A23WE 1996121200641 19961212 00641 NM 1996 12 12 SCNA96428 1 19961207 A 3350 328 LAMP BOEING 727 7272A1 138407F NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 286SC 21601 FOUND RIGHT AFT SERVICE DOOR EMERGENCY LIGHT INOP. CLEANED SOCKET, RELAMPED FIXTURE AND OPS CHECKED GOOD. 2 L 7 3 4F A3WE 1996121200642 19961212 00642 WP 1996 12 12 SCNA96429 1 19961115 A 5312 BULKHEAD TEE DOUG DC10 DC1010 3022110 WP FWD PRESS BLKHD DAMAGED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 572SC 46977 DURING HEAVY MAINTENANCE, FOUND FORWARD PRESSURE BULKHEAD TEE SUPPORT FOR HINGES WITH TWO LIGHTNING STRIKES. REMOVED TE E, FABRICATED AND INSTALLED A NEW TEE IN ACCORDANCE WITH SRM 51-30-2 AND DRAWING NBA6054. CLOSED AREA AND LEAK CHECKED GOOD. 2 L 7 3 4F A22WE 1996121200643 19961212 00643 WP 1996 12 12 SCNA96430 1 19961117 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 816 CUT A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 572SC 46977 DURING HEAVY MAINTENANCE, FOUND CUT IN FUSELAGE SKIN AT BS 816, BETWEEN LONGERON 50R AND 51R. CUT OUT DAMAGE, FABRICATE D AND INSTALLED DOUBLER AND SKIN FILLER IN ACCORDANCE WITH SRM 53-20-00 FIGURE 13 SHEET 8. 2 L 7 3 4F A22WE 1996121200644 19961212 00644 NM 1996 12 12 P5CA9600979 1 19961207 A 5230 65B073296 CONTROL ROD BOEING 747 747122 1384872 NM CARGO DOOR BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 MAIN DECK CARGO DOOR WOULD NOT CLOSE NORMALLY AFTER CARGO LOADING. FOUND FORWARD PULL IN HOOK CONTROL ROD BROKEN. REPL ACED ROD PER M/M 52-32-00. 2 L 7 4 4F A20WE 1996121200645 19961212 00645 NM 1996 12 12 P5CA9600980 1 19961206 A 3244 TIRES BOEING 747 747122 1384872 NM NR 2/4 FLAT A P5CA K NONE O OTHER LD LANDING 1 WP 23 850FT 19755 ON WALKAROUND CHECK, FOUND NR 2 AND NR 4 TIRES FLAT. REPLACED NR 1, 2, 3 AND 4 TIRES PER MAINTENANCE MANUAL 32-45-01. C OMPLETED BRAKE ANTI-SKID OPERATIONAL CHECK PER M/M 32-42-00, ALL CHECKS SATISFACTORY. 2 L 7 4 4F A20WE 1996121200646 19961212 00646 NM 1996 12 12 P5CA9600981 1 19961208 A 5320 ACCESS PANEL BOEING 747 747122 1384872 NM FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 ACCESS PANEL 191ML FORWARD HINGE AREA UNDER HINGE CRACKED FIBERGLASS. REPAIRED PER BOEING SRM 51-40-09. 2 L 7 4 4F A20WE 1996121200647 19961212 00647 WP 1996 12 12 TC8A96069 1 19961207 A 3297 WIRE DOUG DC8 DC851 3021920 WP ANTI-SKID SYST FAILED A TC8A O OTHER O OTHER TX TAXI/GRND HDL 1 GL 23 805CK 45649 ANTI-SKID SWITCH ON, BRAKES INOP AT TAXI SPEEDS. ANTI-SKID WIRING REPAIRED AT PIN 32 ON CONTROL BOX. OPERATION OF BRAK ES AND ANTI-SKID NORMAL, REF WDM 32-03-00 PAGE 39. 2 L 7 4 4F 4A25 1996121200648 19961212 00648 NM 1996 12 12 SRAA961204 1 19961207 A 5270 SWITCH BOEING 747 747212B 1384886 NM CARGO DOOR OUT OF ADJUST A SRAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 745SJ 20888 AFTER TAKEOFF, MAIN CARGO DOOR WARNING LIGHT ILLUMINATED. ACCOMPLISHED AIR TURNBACK TO MIA. ADJUSTED MAIN CARGO DOOR L ATCH DRIVE UNIT CLOSE SWITCH IAW CH 52-31-00, PRESSURIZED AIRCRAFT ON GROUND, SYSTEM OPS CHECKED GOOD. 2 L 7 4 4F A20WE 1996121200684 19961212 00684 WP 1996 12 12 96ZZZX6032 1 19961027 A 2520 11070893 SEAT HARNESS DOUG DC10 DC1030 3023501 WP CABIN FAILED A L2KA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 17 832LA 46931 MCO/LGW - FLT 504 - DURING TAXI, THE PILOT REPORTED F/A AT R2 DOOR COULD NOT RELEASE HER SEAT BELT HARNESS. THE CAPTAIN RETURNED BACK TO BLOCKS AND THE HARNESS WAS CUT TO FREE THE F/A. MAINTENANCE DEFERRED THE R2 F/A JUMP SEAT PER MEL 25- 23. AIRCRAFT RELEASED TO SERVICE. 2 L 7 3 4F A22WE 1996121200685 19961212 00685 WP 1996 12 12 96ZZZX6033 1 19961027 A 5247 NAA605635 APU DOOR DOUG DC10 DC1030 3023501 WP TAIL UNLATCHED A L2KA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 17 833LA 99893 46937 MCO/LGW - FLT 504 - PILOT REPORTED 'AIRFRAME VIBRATION FELT IN FLOOR AND FLIGHT CONTROLS ABOVE 180 KNOTS ON TAKEOFF, CLI MB, CRUISE AT FL 270 AND DESCENT. IT NOTICEABLY DECREASED AFTER FLAPS LOWERED TO 22 DEGREES AND SLOWING BELOW 175 KNOTS .' THE CAPTAIN RETURNED BACK TO MCO AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RELATCHED THE APU SERVICE DOOR. A TEST FLIGHT WAS FLOWN WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A22WE 1996121200689 19961212 00689 CE 1996 12 12 96ZZZX6037 1 19961115 A 5620 1014400424 WINDOW BEECH 200 200BEECH 1152920 CE RT AFT BAG COMP FAILED A S GONA O OTHER O OTHER NR NOT REPORTED 1 SW 01 131PA BB161 RT REAR WINDOW IN BAGGAGE COMPARTMENT FAILED. WINDOW BROKE IN HALF, LOWER HALF BLEW OUT LARGE PIECE. 1 L 7 2 4T A24CE 1996121200691 19961212 00691 CE 1996 12 12 GLBA96210 1 19961029 A 3040 WIPERS BEECH 1900 1900C 1154161 CE WINDSHIELD MALFUNCTIONED A GLBA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 01 101UE UC101 ORD - WINDSHIELD WIPERS DO NOT WORK WITH SWITCH IN SLOW MODE, NO OPERATION AND STRONG SMELL OF ELECTRICAL ODOR. OVERHEA D PANEL EXTREMELY HOT. MAINTENANCE INSPECTED ELECTRICAL SYSTEM AND OPERATIONS OF WIPERS OK IN ALL MODES. NO OVERHEAT O F PANELS. (M) 2 L 7 2 4T RT A24CE 1996121200692 19961212 00692 CE 1996 12 12 GLBA96209 1 19961024 A 6120 8210212D PROP GOVERNOR BEECH 1900 1900C 1154161 CE RT PROP MALFUNCTIONED A GLBA O OTHER O OTHER LD LANDING 1 CE 01 45GL UC45 BMG - DURING LANDING AT 110 KTS THE RIGHT PROP RPM DECREASES TO 900 AND THE LEFT STAYS AT 1400. RIGHT TORQUE INCREASES SLIGHTLY AND AIRCRAFT YAWS HEAVY TO THE LEFT. MAINTENANCE CLEANED LOW PITCH SOLENOIDS. LUBED PROP AND BETA CABLES. RE MOVED ADN REPLACED RIGHT PRIMARY GOVERNOR. (M) 2 L 7 2 4T RT A24CE 1996121200693 19961212 00693 SO 1996 12 12 GLBA96207 1 19961023 A 5730 PANEL EMB 120 EMB120RT SO LT WING LEAKING A GLBA O OTHER K FLUID LOSS IN INSP/MAINT 1 CE 01 281UE 120092 DEN - FUEL LEAK AT LEFT INBOARD WING DEFUEL PANEL. MAINTENANCE SECURED SCREWS ON PANEL. (M) 2 L 7 2 4T RT A31SO 1996121200694 19961212 00694 NE 1996 12 12 GLBA96206 2 19961010 A 7200 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE LEFT FAILED A GLBA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 CE 01 451UE 7650 120108 DLH - LOST NR 1 ENGINE SHORTLY AFTER TAKEOFF. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE. OPERATIONAL AND PERFORMANC E CHECKS GOOD. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1996121200695 19961212 00695 CE 1996 12 12 GLBA96205 1 19961018 A 6120 PROP CONTL SYST BEECH 1900 1900C 1154161 CE LT ENGINE MALFUNCTIONED A GLBA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 01 60UE UC60 SPI - LEFT ENGINE FEATHERED ON TAKEOFF AND WOULD NOT COME OUT OF FEATHER. MAINTENANCE RIGGED LOW PITCH SOLENOID, LOST M OTION LINK, SHORTED BETA CABLE AND VERIFIED BETA VALVE RIGGING. GROUND CHECKS GOOD. (M) 2 L 7 2 4T RT A24CE 1996121200696 19961212 00696 1996 12 12 VTZA97054 3 19961107 A 6140 31056294 BETA SWITCH DOUG DC9 DC914 3022034 WP LT ENGINE FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 600ME 45725 FLT 6484 - JFK-BOS - ABORTED TAKEOFF DUE TO LEFT ENGINE RED BETA LIGHT ILLUMINATED AND RIGHT PAC O/T LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED BETA SWITCH AND COULD NOT DUPLICA TE O/T, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F A6WE 1996121200697 19961212 00697 EU 1996 12 12 VTZA97053 1 19961107 A 7712 CONNECTOR BAG JETSTM JETSTM3201 1500217 EU LT ENGINE DIRTY A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 481UE 895 FLT 6549 - CLE-IAD - MADE AN UNSCHEDULED LANDING DUE TO LEFT ENGINE TORQUE FLUCTUATIONS AND SURGE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE CLEANED LEFT ENGINE STRAIN GAUGE CANNON PLUG AND SWAPPED TORQUE SIGNAL CON DITIONER BRIDGES, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996121200698 19961212 00698 NE 1996 12 12 TWRA96358 2 19961114 A 7260 773190 ANGLE GEARBOX BOEING 747 747212B 1384886 NM PWA JT9 JT9D7Q 52054 NE NR 1 ENGINE LEAKING A TWRA A E UNSCHED LANDING ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 EA 15 616FF EO2095 21939 702332 DURING CRUISE FLT LEVEL 330, NR 1 ENG OIL QTY, OIL PRESS DROP TO ZERO. OIL PRESS LIGHT CAME ON. ENG WAS SHUTDOWN IAW C HECKLIST. ENGINE WITH POSITIVE OIL PRESSURE. MAINTENANCE FOUND ANGLE GEAR BOX OIL SCAVENGE LINE FITTING LOOSE ON ANGLE GEAR BOX. REMOVED AND REPLACED ANGLE GEAR BOX PER WI 72-653 AND MM 72-61-00. RAN ENGINE, OPS AND LEAK CHECKED NORMAL. AIRCRAFT RETURN TO SERVICE. (M) 2 L 7 4 4F 4 F A20WE E3NE 1996121200699 19961212 00699 NM 1996 12 12 96ZZZM1554 1 19961109 A 3350 90084 BATTERY CHARGER BOEING 747 747212B 1384886 NM CABIN MALFUNCTIONED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 616FF 21939 DURING DAILY CHECK, RIGHT SIDE OVERWING EVAC LIGHTS, FORWARD ARE BLINKING. REPLACED BATTERY PACK, BATTERY CHARGER AND F USE. OPS CHECKED NORMAL AS PER MM 33-51-00 PAGE 501. REFERENCE TWRA96358 2 L 7 4 4F A20WE 1996121200700 19961212 00700 NM 1996 12 12 96ZZZM1555 1 19961109 A 3350 276005 FUSE BOEING 747 747212B 1384886 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 616FF 21939 DURING DAILY CHECK, RIGHT SIDE OVERWING EVAC LIGHTS, FORWARD ARE BLINKING. REPLACED BATTERY PACK, BATTERY CHARGER AND F USE. OPS CHECKED NORMAL AS PER MM 33-51-00 PAGE 501. REFERENCE TWRA96358. 2 L 7 4 4F A20WE 1996121200701 19961212 00701 NM 1996 12 12 TWRA96355 1 19961110 A 3350 3004181A LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 616FF 528 21939 DURING DAILY CHECK, FOUND L2 MED UPPER BUSTLE LIGHT INOP. REMOVED AND REPLACED BUSTLE LIGHT. OPS CHECKED NORMAL AS PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996121200702 19961212 00702 EU 1996 12 12 VTZA97050 1 19961106 A 5270 DOOR WARNING BAG JETSTM JETSTM3201 1500217 EU BAGG COMPT MALFUNCTIONED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 493UE 805 FLT 6332 - IAD-PIT - MADE AN UNSCHEDULED LANDING DUE TO POD DOOR LIGHT ILLUMINATED AND ATC SAID POD DOOR OPENED. AIRCRA FT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED DOOR AND FOUND SECURED ALSO INSPECTED HINGES AND SH OOT BOLTS. MAINTENANCE OPENED DMI 05774, MEL 52-2 ON POD DOOR CAPTION LIGHT. AIRCRAFT WAS RELEASED AND RETURNED TO SER VICE. (M) 2 L 7 2 4T RT A56EU 1996121200703 19961212 00703 NM 1996 12 12 EISA96261 1 19960915 A 5320 CHORD BOEING 727 72725 1384006 NM BS 760.95 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 RIGHT PLUS CHORD CRACKED AT FS 760.95 RBL 70.5. STOP DRILLED CRACK AND INSTALLED REPAIR PER SB 727-57-0112. (M) 2 L 7 3 4F A3WE 1996121200704 19961212 00704 NM 1996 12 12 EISA96260 1 19960915 A 5330 SKIN BOEING 727 72725 1384006 NM BS 303 CORROSION A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FUSELAGE SKIN CORROSION AT FS 303 LEFT SIDE, JUST BELOW FORWARD AIRSTAIR DOOR. REMOVED AND REPLACED DAMAGED SKIN PER SR M 51-10-06 FROM STATION 259 TO 360. (M) 2 L 7 3 4F A3WE 1996121200705 19961212 00705 NM 1996 12 12 EISA96259 1 19960915 A 5270 WIRE BOEING 727 72725 1384006 NM MAIN CARGO DOOR MISINSTALLED A EISA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 300NE 18974 DURING INSTALLATION OF SERVICE BULLETIN NR 727-2-008 ON MAIN CARGO DOOR FOUND WIRING TO NOT BE IN CONFORMITY WITH WIRING PRINT NR AE727-2-008. REWIRED MCD PER AERONAUTICAL ENGINEERS PRINT NR 727-2-008 AND STC SA 179750. (M) 2 L 7 3 4F A3WE 1996121200706 19961212 00706 NM 1996 12 12 EISA96258 1 19960915 A 5712 RIB BOEING 727 72725 1384006 NM WS 629.5 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND WING RIB CRACKED IN TWO PLACES AT RIGHT WS 629.5. INSTALLED REPAIR PER SRM 57-10-05. (M) 2 L 7 3 4F A3WE 1996121200707 19961212 00707 NM 1996 12 12 EISA96257 1 19960915 A 5712 RIB BOEING 727 72725 1384006 NM WS 629.5 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND RIB CRACKED IN THREE PLACES AT LT WS 629.5. INSTALLED NEW RIB PER SB 57-017. (M) 2 L 7 3 4F A3WE 1996121200708 19961212 00708 NM 1996 12 12 EISA96256 1 19960915 A 5712 RIB BOEING 727 72725 1384006 NM WS 601.5 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND WING RIB CRACKED AT RT WS 601.5. REMOVED AND REPLACED DAMAGED RIB PER SB 727-57A-159. (M) 2 L 7 3 4F A3WE 1996121200709 19961212 00709 NM 1996 12 12 EISA96255 1 19960915 A 5712 RIB BOEING 727 72725 1384006 NM WS 546.5 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND WING RIB CRACKED AT RT WS 546.5. FABRICATED AND INSTALLED REPAIR CHANNEL PER 57-10-05. (M) 2 L 7 3 4F A3WE 1996121200710 19961212 00710 NM 1996 12 12 EISA96254 1 19960915 A 5713 STRINGER BOEING 727 72725 1384006 NM WS 546.5 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND STRINGER CRACKED, 3RD UPPER, FORWARD OF REAR SPAR LEFT WS 546.5. STOP DRILLED CRACK AND INSTALLED REPAIR PER SB 7 27-57-129. (M) 2 L 7 3 4F A3WE 1996121200711 19961212 00711 NM 1996 12 12 EISA96253 1 19960915 A 5712 RIB BOEING 727 72725 1384006 NM WS 601.5 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND THREE CRACKS IN WING RIB AT LEFT WS 601.5. FABRICATED AND INSTALLED REPAIR PER SRM 57-10-00. (M) 2 L 7 3 4F A3WE 1996121200712 19961212 00712 NM 1996 12 12 EISA96252 1 19960915 A 5311 FRAME BOEING 727 72725 1384006 NM BS 783.95 MISDRILLED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND FUSELAGE FRAME MISDRILLED AT BS 783.95, LEFT, 4TH FASTENER HOLE UP FROM CABIN FLOOR. INSTALLED REPAIR KIT PER SB 727-53-0197. (M) 2 L 7 3 4F A3WE 1996121200713 19961212 00713 NM 1996 12 12 EISA96251 1 19960915 A 5311 FRAME BOEING 727 72725 1384006 NM BS 825.95 MISDRILLED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND FUSELAGE FRAME MISDRILLED AT BS 825.95, LEFT, 4TH FASTENER HOLE UP FROM CABIN FLOOR. HOLE TO FIRST OVERSIZE AND I NSTALLED REPAIR STRAP PER SB 727-53-0197. (M) 2 L 7 3 4F A3WE 1996121200714 19961212 00714 NM 1996 12 12 EISA96250 1 19960915 A 5311 FRAME BOEING 727 72725 1384006 NM BS 760.95 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND FUSELAGE FRAME CRACKED AT BS 760.95 RIGHT, 4TH FASTENER HOLE UP FROM CABIN FLOOR. INSTALLED REPAIR KIT PER SB 53- 0197. (M) 2 L 7 3 4F A3WE 1996121200715 19961212 00715 NM 1996 12 12 EISA96249 1 19960915 A 2782 ANGLE BOEING 727 72725 1384006 NM NR 2 LE FLAP ACT CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 NR 2 LE FLAP ACTUATOR MOUNT, INBOARD UPPER ANGLE CRACKED. FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-10-0 AND 51-12- 1. (M) 2 L 7 3 4F A3WE 1996121200716 19961212 00716 NM 1996 12 12 EISA96248 1 19960915 A 5712 RIB BOEING 727 72725 1384006 NM WS 300 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND RIGHT WING LEADING EDGE RIB CRACKED AT WS 330. FABRICATED AND INSTALLED DOUBLER PER SRM 51-30-02. (M) 2 L 7 3 4F A3WE 1996121200717 19961212 00717 NM 1996 12 12 EISA96247 1 19960915 A 5241 ANGLE BOEING 727 72725 1384006 NM GALLEY DOOR CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND GALLEY SERVICE DOOR ANGLE CRACKED AT BOTTOM LOWER FRAME AT FORWARD END. REPLACED ANGLE PER SRM 51-30-02. (M) 2 L 7 3 4F A3WE 1996121200718 19961212 00718 NM 1996 12 12 EISA96246 1 19960915 A 5210 ANGLE BOEING 727 72725 1384006 NM PAX DOOR CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND FORWARD ENTRY DOOR LOWER FRAME CORNER AFT ANGLE HAS EXFOLIATING CORROSION. REMOVED AND REPLACED ANGLE PER SRM 51- 10-01. (M) 2 L 7 3 4F A3WE 1996121200719 19961212 00719 NM 1996 12 12 EISA96245 1 19960915 A 5210 FRAME BOEING 727 72725 1384006 NM PAX DOOR CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND 3.25 INCH CRACK IN FRAME OF FORWARD ENTRY DOOR AS SEEN FROM 2ND LIGHTENING HOLE FROM AFT, 6, UP FROM LOWER FRAME. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-6. (M) 2 L 7 3 4F A3WE 1996121200720 19961212 00720 NM 1996 12 12 EISA96244 1 19960915 A 5712 RIB BOEING 727 72725 1384006 NM WS 656.5 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND LEFT WING RIB CRACKED AT WS 656.5, 2ND LOWER STRINGER FROM REAR SPAR. INSTALLED RIB REPAIR PER SRM 57-10-05. (M) 2 L 7 3 4F A3WE 1996121200721 19961212 00721 NM 1996 12 12 EISA96243 1 19960915 A 5320 WINDOW POST BOEING 727 72725 1384006 NM LT COCKPIT CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND CAPTAINS E-F WINDOW POST CRACKED. INSTALLED DOUBLER PER SB 53-0086. (M) 2 L 7 3 4F A3WE 1996121200722 19961212 00722 NM 1996 12 12 EISA96242 1 19960915 A 5320 INTERCOSTAL BOEING 727 72725 1384006 NM FS 804 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND CABIN LEFT FS 804, STRINGER 17 INTERCOSTAL WEB CRACKED. FABRICATED AND INSTALLED DOUBLER PER SRM 51-30-02. (M) 2 L 7 3 4F A3WE 1996121200723 19961212 00723 NM 1996 12 12 EISA96241 1 19960914 A 5315 FLOOR BEAM BOEING 727 72725 1384006 NM BS 940 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND CABIN FLOOR BEAM CRACKED FROM FASTENER HOLE TO AFT END FS 940 RBL 58. INSTALLED FLOOR BEAM REPAIR PER SB 727-53. (M) 2 L 7 3 4F A3WE 1996121200724 19961212 00724 NM 1996 12 12 EISA96240 1 19960914 A 5400 RIB BOEING 727 72725 1384006 NM NR 3 PYLON CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND NR 3 ENGINE PYLON RIB CRACKED, ACCESS THROUGH PANEL 5510. BLENDED DAMAGED AREA, FABRICATED AND INSTALLED PER SRM 54-20-03. (M) 2 L 7 3 4F A3WE 1996121200725 19961212 00725 NM 1996 12 12 EISA96239 1 19960914 A 5400 PYLON BOEING 727 72725 1384006 NM NR 1 ENGINE CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND NR 1 ENGINE PYLON TRAILING EDGE CRACKED JUST AFT OF BULB SEAL. FABRICATED NEW TRAILING EDGE ANGLES AND INSTALLED PER SRM 53-20-02. (M) 2 L 7 3 4F A3WE 1996121200726 19961212 00726 NM 1996 12 12 EISA96238 1 19960914 A 5754 RIB BOEING 727 72725 1384006 NM NR 5 LE SLAT BULGED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND NR 5 SLAT, OUTBOARD TRACK FITTING, INBOARD RIB WEB BULGING. INSTALLED NEW FITTING PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1996121200727 19961212 00727 NM 1996 12 12 EISA96237 1 19960914 A 5754 RIB BOEING 727 72725 1384006 NM NR 5 SLAT CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 NR 5 SLAT, INTERNAL OUTBOARD NOSE RIB CRACKED. REMOVED AND REPLACED RIB PER SRM 51-10-06. (M) 2 L 7 3 4F A3WE 1996121200728 19961212 00728 NM 1996 12 12 EISA96236 1 19960914 A 5522 SKIN BOEING 727 72725 1384006 NM ELEV SKIN CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND BONDED BEAD'S IN ELEVATOR SKIN, INTERNAL SURFACE ARE CRACKED IN THREE PLACES, INBOARD, END. STOP DRILLED CRACKS, FABRICATED AND INSTALLED DOUBLERS PER SRM 55-20-03. (M) 2 L 7 3 4F A3WE 1996121200729 19961212 00729 NM 1996 12 12 EISA96235 1 19960914 A 5241 DOOR BOEING 727 72725 1384006 NM GALLEY CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND GALLEY DOOR UPPER GATE DOOR IS CRACKED. REPLACED DOOR WITH SERVICEABLE UNIT. (M) 2 L 7 3 4F A3WE 1996121200730 19961212 00730 NM 1996 12 12 EISA96234 1 19960914 A 5712 RIB BOEING 727 72725 1384006 NM WS 546.5 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND RIGHT WING RIB CRACKED AT 3RD LOWER STRINGER FROM AFT SPAR, WS 546.5. FABRICATED AND INSTALLED REPAIR CHANNEL PER SRM 57-10-05. (M) 2 L 7 3 4F A3WE 1996121200731 19961212 00731 NM 1996 12 12 EISA96233 1 19960914 A 5730 SKIN BOEING 727 72725 1384006 NM LE WING CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND LE SKIN CRACKED AT CUTOUT FOR NR 4 SLAT INBOARD TRACK. FABRICATED AND INSTALLED DOUBLER PER SRM 51-30-02. (M) 2 L 7 3 4F A3WE 1996121200732 19961212 00732 NM 1996 12 12 EISA96232 1 19960914 A 5730 SKIN BOEING 727 72725 1384006 NM WING LE CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND LE SKIN CRACKED AT CUTOUT FOR NR 4 SLAT OUTBOARD TRACK. FABRICATED AND INSTALLED DOUBLER PER SRM 51-40-04. (M) 2 L 7 3 4F A3WE 1996121200733 19961212 00733 NM 1996 12 12 EISA96231 1 19960914 A 5753 SKIN BOEING 727 72725 1384006 NM RT TE FORE FLAP DENTED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND RIGHT WING, INBOARD FOREFLAP, INBOARD END UPPER SKIN DENTED. INSTALLED BONDED REPAIR PER SRM 51-40-02. (M) 2 L 7 3 4F A3WE 1996121200734 19961212 00734 NM 1996 12 12 EISA96230 1 19960914 A 5320 WEB BOEING 727 72725 1384006 NM NLG W/W CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND MAIN GEAR WHEEL WELL CEILING AT FS 274 ON LEFT SIDE IS CRACKED. FABRICATED AND INSTALLED DOUBLER PER SRM 51-40-02 . (M) 2 L 7 3 4F A3WE 1996121200735 19961212 00735 NM 1996 12 12 EISA96229 1 19960914 A 5230 FRAME BOEING 727 72725 1384006 NM CARGO DOOR TORN A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND MAIN CARGO DOOR FRAME AFT BOTTOM CORNER HAS TORN METAL. FABRICATED AND INSTALLED NEW WEB PER SRM 51-30-02. (M) 2 L 7 3 4F A3WE 1996121200736 19961212 00736 NM 1996 12 12 EISA96226 1 19960914 A 5754 ANGLE BOEING 727 72725 1384006 NM NR 2 LE FLAP CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND NR 2 LE FLAP ACTUATOR MOUNT, LOWER ANGLE CRACKED. FABRICATED AND INSTALLED NEW MOUNT ANGLE PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1996121200737 19961212 00737 NM 1996 12 12 EISA96225 1 19960914 A 5754 SKIN BOEING 727 72725 1384006 NM NR 3 LE FLAP CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND NR 3 LE FLAP INNER SKIN CRACKED. FABRICATED AND INSTALLED DOUBLER PER SRM 57-20-00 AND 57-20-04. (M) 2 L 7 3 4F A3WE 1996121200738 19961212 00738 NM 1996 12 12 EISA96224 1 19960914 A 5751 FITTING BOEING 727 72725 1384006 NM OUTBD AILERON CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND 1 INCH CRACK, OUTBOARD AILERON, 2ND FROM OUTBOARD ATTACHED FITTING. REPLACE FITTING WITH NEW PART PER SRM 51-40-0 1. (M) 2 L 7 3 4F A3WE 1996121200739 19961212 00739 NM 1996 12 12 EISA96223 1 19960914 A 5312 BULKHEAD WEB BOEING 727 72725 1384006 NM FS 870 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND 2 INCH CRACK AT FS 870 BULKHEAD, RIGHT WHEEL WELL, AT APU AIR DELIVERY VALVE CUT OUT. FABRICATED AND INSTALLED DO UBLER PER SRM 53-10-09. (M) 2 L 7 3 4F A3WE 1996121200740 19961212 00740 NM 1996 12 12 EISA96222 1 19960914 A 5730 SKIN BOEING 727 72725 1384006 NM LT WING CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND SKIN CRACKED FORWARD OF NR 2 SPOILER CENTER OUTBOARD HINGE CUT OUT. FABRICATED AND INSTALLED DOUBLER PER SRM 57-3 0-04. (M) 2 L 7 3 4F A3WE 1996121200741 19961212 00741 NM 1996 12 12 EISA96221 1 19960914 A 5730 SKIN BOEING 727 72725 1384006 NM LT WING CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND SKIN CRACKED FORWARD OF NR 2 SPOILER CENTER INBOARD HINGE CUT OUT. FABRICATED AND INSTALLED DOUBLER PER SRM 57-30 -04. (M) 2 L 7 3 4F A3WE 1996121200742 19961212 00742 NM 1996 12 12 EISA96220 1 19960914 A 5730 SKIN BOEING 727 72725 1384006 NM LT WING CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND SKIN CRACKED FORWARD OF NR 2 SPOILER AT INBOARD HINGE CUT OUT. FABRICATED AND INSTALLED DOUBLER PER SRM 57-30-04. (M) 2 L 7 3 4F A3WE 1996121200743 19961212 00743 NM 1996 12 12 EISA96219 1 19960914 A 5730 SKIN BOEING 727 72725 1384006 NM LT WING CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND SKIN CRACKED FORWARD OF NR 3 SPOILER AT INBOARD HINGE CUT OUT. FABRICATED AND INSTALLED DOUBLER PER SRM 57-30-03 AND 57-30-04. (M) 2 L 7 3 4F A3WE 1996121200744 19961212 00744 NM 1996 12 12 EISA96218 1 19960914 A 5730 SKIN BOEING 727 72725 1384006 NM LT WING CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND SKIN CRACKED FORWARD OF NR 4 SPOILER PANEL CENTER OUTBOARD HINGE CUT OUT. FABRICATED AND INSTALLED DOUBLER PER SR M 57-30-03 AND 57-30-04. (M) 2 L 7 3 4F A3WE 1996121200745 19961212 00745 NM 1996 12 12 EISA96217 1 19960914 A 5730 SKIN BOEING 727 72725 1384006 NM WING TE CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND SKIN CRACKED FORWARD OF NR 4 SPOILER AT CENTER INBOARD HINGE AREA. FABRICATED AND INSTALLED DOUBLER PER SRM 57-30 -03 AND 57-30-04. (M) 2 L 7 3 4F A3WE 1996121200746 19961212 00746 NM 1996 12 12 EISA96216 1 19960914 A 5720 ANGLE BOEING 727 72725 1384006 NM WS 130.7 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND RIGHT WING LE RIB LOWER ANGLE CRACKED AT WS 130.7. FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-30-02. (M) 2 L 7 3 4F A3WE 1996121200747 19961212 00747 NM 1996 12 12 EISA96215 1 19960914 A 5712 RIB BOEING 727 72725 1384006 NM WS 330 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND RIGHT WING LE NOSE RIB CRACKED BEYOND DOUBLER AT WS 330. FABRICATED AND INSTALLED LONGERON DOUBLER PER SRM 51-20- 6, 51-50-34 AND 51-30-02. (M) 2 L 7 3 4F A3WE 1996121200748 19961212 00748 NE 1996 12 12 EISA96280 2 19961119 A 7200 ENGINE BOEING 727 727223 1384074 NM PWA JT8 JT8D7B 52053 NE NR 3 FOD DAMAGED A EISA E A ENGINE SHUTDOWN UNSCHED LANDING C F.O.D. TO TAKEOFF 1 SW 07 311NE 61303 19703 648876 ON TAKEOFF, HAD COMPRESSOR STALL ON NR 3 ENGINE AND STARTED LOSING POWER ON CLIMB-OUT RETURNED TO SEA FOUND FOD DAMAGE T O NR 3 ENGINE. NO LIMITS WERE EXCEEDED. PERFORMED PRECAUTIONARY SHUT DOWN WITH CHECK LIST. REMOVED AND REPLACD NR 3 E NGINE. ENGINE RUN AND OPS CHECK GOOD. (M) 2 L 7 3 4F 4 F A3WE E2EA 1996121200749 19961212 00749 WP 1996 12 12 AALA961577 1 19961028 A 2910 7912643565 HYD LINE DOUG DC9 DC982 3022082 WP LT OUTBD SPOILER CRACKED A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 73444 49470 DFW - FLT 871 - AFTER TAKEOFF DFW DURING CLIMB-OUT, RIGHT HYDRAULIC SYSTEM PRESSURE WENT TO ZERO. ACCOMPLISHED MANUAL G EAR EXTENSION AND AIRCRAFT RETURNED TO DFW, LANDING WITHOUT INCIDENT. REPLACED LEFT OUTBOARD SPOILER LINE. REPLACED RI GHT ENGINE DRIVEN HYDRAULIC PUMP AND ALL SYSTEM FILTERS. ACCOMPLISHED SYSTEM LEAK AND GROUND CHECK WITH NO DEFECTS FOUN D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996121200750 19961212 00750 WP 1996 12 12 AALA961528 1 19961016 A 2131 60714622 CONTROLLER DOUG DC9 DC982 3022082 WP RIGHT DEFECTIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 234AA 49181 OMA - FLT 1587 - AFTER TAKEOFF OMA DURING CLIMB-OUT, SMOKE NOTED IN MAIN CABIN FOLLOWED BY CABIN SUPPLY TEMPERATURE NOTE D AT 150 DEGREES AND RIGHT PACK TRIP. SMOKE SUBSIDED AFTER PACK TRIP. AIRCRAFT RETURNED TO OMA AND LANDED WITHOUT INCI DENT. REPLACED CHECK VALVE AT PNEUMATIC CONNECTOR FOUND TO BE CAUSING DUCT LEAK. ACCOMPLISHED BURN OUT PROCEDURE OF HI GH PRESSURE DUCTING AND REPLACED BOTH AIR CYCLE MACHINE COALESCER BAGS. PLACARDED RIGHT PACK AUTO MODE AND ACCOMPLISHED GROUND ENGINE RUN WITH NO DEFECTS FOUND. RIGHT PACK SYSTEM GROUND CHECKED NORMAL OPERATION IN MANUAL MODE WITH NO SMOK E NOTED. SUBSEQUENTLY REPLACED RIGHT CABIN TEMP CONTROLLER. SYSTEM GROUD CHECKED NORMAL OPERATION AND PLACARD REMOVED. 2 L 7 2 4F A6WE 1996121200751 19961212 00751 WP 1996 12 12 AALA961571 1 19961027 A 2170 COALESCER BAG DOUG DC9 DC982 3022082 WP CABIN DIRTY A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 496AA 49734 ORD - FLT 435 - AFTER TAKEOFF ORD DURING CLIMB-OUT, FOUL ODOR ENTERED COCKPIT AND ODOR/SMOKE NOTED IN CABIN. AIRCRAFT R ETURNED TO ORD AND LANDED WITHOUT INCIDENT. CHECKED BOTH ENGINES AND NOTED POSSIBLE BIRD STRIKE TO RIGHT ENGINE. ACCOM PLISHED BORESCOPE OF RIGHT ENGINE WITH NO DEFECTS FOUND. REPLACED LEFT AND RIGHT COALESCER BAGS AND ACCOMPLISHED GRUOND RUN OF BOTH ENGINES, APUT AND BOTH PACKS WITH NO DEFECTS, SMOKE OR ODOR NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION AND AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1996121200752 19961212 00752 WP 1996 12 12 AALA961569 1 19961016 A 3222 SCHRADER VALVE DOUG DC9 DC982 3022082 WP NLG STRUT MALFUNCTION A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 7539A 49993 DFW - FLT 1718 - AFTER TAKEOFF DFW WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR DID NOT RETRACT. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. SERVICED NOSE LANDING GEAR STRUT AND REPLACED SCHRADER VALVE. ACCOMPLISHED NOSE LAND ING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996121200753 19961212 00753 EU 1996 12 12 AALA961551 1 19961024 A 3260 201251224 SENSOR FOKKER F28 F28MK0100 4990807 EU LT MLG DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 1466A 11498 ORD - FLT 1488 - AFTER TAKEOFF ORD WHEN LANDING GEAR RETRACTED, MFDU MESSAGE LEFT LANDING GEAR DOWN LOCK SWITCH ILLUMINA TED ALONG WITH LEFT MAIN LANDING GEAR GREEN LIGHT ILLUMINATED. EXTENDED LANDING GEAR AND ALL INDICATIONS RETURNED TO NO RMAL. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED LEFT MAIN LANDING GEAR DOWN LOCK SENSOR. ACCOMPL ISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1996121200754 19961212 00754 NM 1996 12 12 AALA961588 1 19961021 A 2131 10251831 CONTROLLER BOEING 727 727223 1384074 NM COCKPIT DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 870AA 46664 21382 TPA - FLT 1629 - AFTER TAKEOFF MIA DURING CLIMB-OUT, PASSING THRUOGH FL 290, CABIN ALTITUDE BEGAN TO CLIMB WITH ASSOCIAT ED WARNING HORN. CLOSED BOTH OUTFLOW VALVES AND ACCOMPLISHED EMERGENCY DESCENT. AIRCRAFT DIVERTED TO TPA LANDED WITHOU T INCIDENT. REPLACED AUTO AND MANUAL PRESSURIZATION CONTROLLERS AND BOTH OUTFLOW VALVES. ACCOMPLISHED GROUND ENGINE RU N AND PRESSURIZATION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1996121200755 19961212 00755 EU 1996 12 12 AALA961611 1 19961105 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 50051 459 JFK - DURING OVERNIGHT CHECK EMERGENCY FLOOR LIGHTS FROM PAX SEAT ROW 14 AB TO 19AB INOPERATIVE. REPLACED EMERGENCY FLO OR LIGHT STRIPS FROM PAX SEAT ROW 14AB TO 19AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996121200756 19961212 00756 WP 1996 12 12 AALA961585 1 19961030 A 5620 AAP3077 WINDOW DOUG DC10 DC1010 3022110 WP CABIN CRACKED A AALA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 132AA 47827 MIA - FLT 588 - EN ROUTE SDQ/JFK DURING CRUISE, CABIN WINDOW OUTER PANE AT PAX SEAT 12A CRACKED ALONG EDGE OF FRAME. AI RCRAFT DIVERTED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED OUTER WINDOW PANE AND SEAL AT PAX SEAT 12A. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A22WE 1996121200757 19961212 00757 WP 1996 12 12 AALA961621 1 19961107 A 3230 BYPASS LEVER DOUG DC9 DC983 3022083 WP LANDING GEAR NOT CLOSED A AALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 07 562AA 49344 DFW - FLT 2361- AFTER TAKEOFF DFW, WHEN LANDING GEAR LEVER SELECTED UP, LANDING GEAR DOORS WOULD NOT SEQUENCE AND LANDIN G GEAR DID NOT RETRACT. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. PLACED LANDING GEAR DOOR BYPASS HANDLE I N CLOSED POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 1996121200758 19961212 00758 WP 1996 12 12 AALA961587 1 19961029 A 3230 3914464503 DOWNLOCK LINK DOUG DC9 DC982 3022082 WP NLG BROKEN A AALA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SW 07 244AA 49256 JFK - FLT 346 - DURING APPROACH TO LGA WHEN LANDING GEAR SELECTED DOWN, NLG INDICATED UNSAFE. ACCOMPLISHED ABNORMAL PRO CEDURES WITH SAME RESULTS. A/C DIVERTED TO JFK AND LANDED WITH NLG UP AND LOCKED AND NOSE GEAR EXTENSION PIN ON INSTRUM ENT PANEL EXTENDED. A/C RECOVERED AND NLG EXTENDED. REPLACED BROKEN NLG UPPER DOWNLOCK LINK. ACCOMP L/G RETRACTION CH ECK AND ALTERNATE GEAR EXTENSION WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. A/C MX FERRY JFK/BNA/T UL FOR STRUCTURAL/SKIN REPAIR. (M) 2 L 7 2 4F A6WE 1996121200759 19961212 00759 EU 1996 12 12 AALA961533 1 19961021 A 3350 A3060698101 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 14065 508 MIA - DURNING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT CROSS AISLE BY PAX SEAT ROW 6 INOPERATIVE. RESECURED LOOSE EME RGENCY FLOOR LIGHT STRIP CONNECTOR BY PAX SEAT ROW 6. CROSS AISLE LIGHTS GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996121200760 19961212 00760 EU 1996 12 12 AALA961576 1 19961027 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 18066 509 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 21B AND 24B INOPERATIVE. REPLACED MISSING EM ERGENCY FLOOR LIGHT STRIP BETWEEN PAX SEAT ROWS 21B AND 24B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996121200761 19961212 00761 EU 1996 12 12 AALA961545 1 19961022 A 2424 M740120B GEN CONTL UNIT AIRBUS 300 A300B4605R 3930308 EU NR 2 DEFECTIVE A AALA A UNSCHED LANDING H B ELECT. POWER LOSS-50 PC SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 7062A 474 JFK - FLT 611 - AFTER TAKEOFF JFK DURING CLIMB-OUT, NR 2 ENGINE GENERATOR FAULT ACCOMPANIED BY REPORT OF BURNING ODOR IN CABIN. AIRCRAFT RETURNED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED NR 2 GENERATOR CONTROL UNIT. SYSTEM GROUND CHE CKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996121200762 19961212 00762 NM 1996 12 12 ASAA9640088 1 19961006 A 3350 P4010033210 BATTERY PACK BOEING 737 7374Q8 NM CABIN DISCHARGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 754AS 25095 PDX - DURING MAINTENANCE CHECK, THE R2 DOOR EVACUATION SLIDE BATTERY PACK ACTIVATION PIN WAS FOUND TO BE DISCONNECTED FR OM THE PACK. REMOVED AND REPLACED EVACUATION SLIDE. (M) 2 L 7 2 4F RT A16WE 1996121200763 19961212 00763 NM 1996 12 12 ASAA9610141 1 19961107 A 3350 90835A BATTERY PACK BOEING 737 737210C 1384459 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 744AS 21822 SEA - DURING MAINTENANCE CHECK, THE LEFT OVERWING EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AND LIG HT OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1996121200764 19961212 00764 NM 1996 12 12 ASAA9610140 1 19961104 A 2612 20035008300 FIRE MODULE BOEING 737 737290C 138448V NM WHEEL WELL INOPERATIVE A ASAA O OTHER N FALSE WARNING DE DESCENT 1 NM 01 742AS 23136 ANC - FLT 55 - UPON DESCENT INTO ANC, THE WHEEL WELL FIRE WARNING LIGHT ILLUMINATED INTERMITTENTLY. FIRE WARNING TEST N ORMAL AND AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED WHEEL WELL WIRING AND DETECTION LOOP, NO FAULTS FOUND. REPLACED WHEEL WELL FIRE DETECTION MODULE AND SYSTEM OPS CHECKS NORMAL. (M) 2 L 7 2 4F A16WE 1996121200765 19961212 00765 NM 1996 12 12 EIAA 1 19961104 A 5753 65B0190129 SKIN BOEING 747 747273C 1384896 NM LT TE FORE FLAP CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 JFK - NOTED DURING MAINTENANCE IN FLAP WELL AREA, OUTBOARD FLAP WAS DAMAGED FROM LEADING EDGE CAP. REPLACED FORE FLAP. FABRICATED AND INSTALLED NEW WEB AND UPPER CHORD PER SRM 51-10-01 AND 51-10-02 AND REPAIRED LOWER FIXED WING PANEL PER SRM 51-40-07 DUE TO RIB OUTBOARD OF LEFT FORE FLAP CRACKED 10.5 INCH THROUGH LIGHTENING HOLE AND 24 INCH HORIZONTAL CRAC K. (M) 2 L 7 4 4F A20WE 1996121200766 19961212 00766 NM 1996 12 12 EIAA9632 1 19960918 A 2612 WIRE BOEING 747 747121 1384871 NM APU CHAFED A EIAA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 NM 09 480EV 20348 RJNN - AT CRUISE ALTITUDE APU FIRE WARNING LIGHT CAME ON AND FIRE BELL SOUNDED. PULLED FIRE HANDLE, LIGHT STAYED ON. D ISCHARGED FIRE BOTTLE AND LIGHT IMMEDIATELY WENT OUT. INSPECTED APU COMPARTMENT. NO FIRE DAMAGE FOUND. FOUND CHAFED F IRE DETECTION WIRE RIGHT UPPER SIDE. REPAIRED WIRE, OPS CHECK GOOD PER MM 26-15-00. (M) 2 L 7 4 4F A20WE 1996121200767 19961212 00767 NM 1996 12 12 EIAA9613 1 19960512 A 8010 21SN4149 SWITCH BOEING 747 747212B 1384886 NM PWA JT9 JT9D7J 52054 NE NR 3 STARTER MALFUNCTIONED A EIAA E ENGINE SHUTDOWN O OTHER IN INSP/MAINT 1 NM 09 485EV 20712 662268 JFK - FL 310 - NR 3 START VLV OPEN LIGHT ILLUMINATED. ACCOMP ABNORMAL PROCEDURE, ENG SHUTDOWN. WHEN ENG WAS THROTTLED BACK, ENG STALLED. NO ABNORMAL EGT EXCURSIONS NOTED. OCCURRED ABOUT 1.20 EPR. REMOVED AND REPLACED ENG NR 3 START VLV AND PRESS SWITCH PER MM 80-11-80. OPS CHECK GOOD. PERFORMED ENG INSPECTION PER MM 71-00-43. PERFORMED BOROSCOPE INSP ECT PER 72-00-00. PERFORMED WINDMILLING INSPECT PER 72-00-00. ENG OPS CHECK GOOD PER 71-00-00. CHECKED MAIN OIL FILTE R AND CHIP DETECT, FOUND OK. REPLACED START VLV PRESS SWITCH PER MM 80-11-05. (M) 2 L 7 4 4F 4 F A20WE E20EA 1996121200768 19961212 00768 NE 1996 12 12 EIAA9682 2 19961102 A 7261 O-RING BOEING 747 747132 1384882 NM PWA JT9 JT9D7AH 52054 NE OIL FILL CAP CUT A EIAA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 09 479EV 19898 662553 SBGR - DURING CLIMB, NR 2 ENGINE OIL QTY SLOWLY DECREASED TO ZERO, ACCOMPANIED WITH FLUCTUATING OIL PRESSURE. IN FLIGHT ENGINE FAILURE AND SHUTDOWN CHECKLIST COMPLETED TOTAL WINDMILLING TIME 3 PLUS 10, MINIMUM OIL PRESSURE WAS 16 PSI STEAD Y. IN FLIGHT SHUTDOWN INSPECTION COMPLETED AS PER MM 77-00-00. DURING INSPECTION FOUND OIL CAP SEAL CUT. REMOVED AND REPLACED O-RING PER MM V12-13-03. ENGINE RUN COMPLETED, LEAK CHECK OK. (M) 2 L 7 4 4F 4 F A20WE E20EA 1996121200769 19961212 00769 NM 1996 12 12 EIAA9683 1 19961108 A 2810 AS11329015 SEAL BOEING 747 747132 1384882 NM CENTER WING LEAKING A EIAA O OTHER B K SMOKE/FUMES/ODORS/SPARKS FLUID LOSS CL CLIMB 1 NM 09 479EV 19898 JFK - AFTER TAKEOFF FROM LCK, A SMELL OF FUEL WAS EVIDENT IN COCKPIT DURING LANDING GEAR RETRACTION. SMELL DISSIPATED A FTER AIRCONDITIONING PACKAGE WAS TURNED ON. NO OTHER ABNORMAL INDICATIONS NOTED. FOUND RIGHT SUMP DRAIN SEEPING. RESE ATED DRAIN CHECKED OK. ON 11/7/96, LOG PAGE F08454, HAD A FUEL SMELL AGAIN. REPLACED BASE PLATE FOR CENTER WING TANK S TK NR 24 HOUSING, RESEALED PER MM 28-11-00 WITH PRC 1422B1/2. (M) 2 L 7 4 4F A20WE 1996121200770 19961212 00770 NM 1996 12 12 EIAA9685 1 19961115 A 5320 65B38096962V POST BOEING 747 747212B 1384886 NM BS 1920 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 485EV 20712 JFK - DURING ROUTINE SERVICE CHECK, SUPPORT POST IN THE LOWER REAR CARGO COMPARTMENT AT STATION 1920 RBL 61.25, WAS FOUN D SHEARED AND CRACKED ABOVE STABILIZATION STRAP. THE CAUSE OF THE DAMAGE IS UNKNOWN AT THIS TIME. REPLACED ALL DAMAGED PARTS AND NDI INSPECTION OF SURROUNDING STRUCTURES AND FASTENERS. (M) 2 L 7 4 4F A20WE 1996121200771 19961212 00771 SO 1996 12 12 WTAA960192 1 19961114 A 5270 MS250851 SWITCH EMB 120 EMB120RT SO SERVICE DOOR OUT OF ADJUST A WTAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 17 284UE 120145 LAX - SERVICE DOOR LIGHT ILLUMINATED ON TAKEOFF. TAKEOFF ABORTED. MAINTENANCE ADJUSTED SERVICE DOOR MICROSWITCH SCREW. DOOR LIGHT OUT ON GROUND. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996121200772 19961212 00772 NE 1996 12 12 WTAA960195 2 19961119 A 7261 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE LEFT LOW OIL QTY A WTAA O OTHER J WARNING INDICATION CL CLIMB 1 WP 17 271YV 120271 FAT - LOW OIL PRESS WARNING ON LEFT ENG ON CLIMB-OUT REPORTED. AIRCRAFT RETURNED TO STATION. MAINTENANCE ADDED FOUR QU ARTS OF OIL TO LEFT ENGINE. OIL PRESSURE INDICATION OPERATES NORMAL. INSPECTED ENGINE FOR LEAKS. NO LEAKS NOTED. AIR CRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1996121200773 19961212 00773 WP 1996 12 12 HALA96162 1 19961119 A 2170 P113 COALESCER BAG DOUG DC9 DC951 3022051 WP LT/RT DIRTY A HALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 13 679HA 47662 HNL - FLT 167 - SMOKE IN CABIN. EVACUATED SMOKE FROM CABIN, COCKPIT AND A/C DUCTING. REPLACED LEFT AND RIGHT WATER SEP S. RAN NR 1 AND NR 2 ENG AND A/C SYSTEM LEAK CHECK OK. OP CHECK NORMAL. (M) 2 L 7 2 4F A6WE 1996121200774 19961212 00774 NM 1996 12 12 MALA965203 1 19961115 A 2720 CONTROLS DHAV DHC8 DHC8102 2809003 NM RUDDER FROZEN A A MALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 15 824MA 327 FLT 3250 - ON CLIMB-OUT FROM MSP, THE CREW REPORTED THAT THE RUDDER PEDALS WERE FROZEN AFTER GEAR RETRACTION. THE AIRCR AFT RETURNED TO MSP. AFTER GEAR EXTENSION, THE RUDDER SYSTEM OPERATED NORMALLY. MAINTENANCE PERFORMED TROUBLESHOOTING AS PROVIDED BY DEHAVILLAND. ALL ASPECTS OF THE RUDDER SYSTEM OPERATED NORMALLY. THE RUDDER CONTROL SYSTEM OPERATED SAT ISFACTORILY DURING A TEST FLIGHT. (M) 2 H 7 2 4T RT A13NM 1996121200775 19961212 00775 EU 1996 12 12 SIMA963241 1 19961119 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72202 8680940 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 252AM 691 253 ORD - FLT 4389 - EMERGENCY FLOOR LIGHTING IN FORWARD CABIN INOP. REPLACED EMERGENCY POWER SUPPLY UNIT BATTERY PACK AND OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996121200776 19961212 00776 NM 1996 12 12 EISA96228 1 19960914 A 5542 SKIN BOEING 727 72725 1384006 NM RUDDER CORROSION A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 LOWER RUDDER HAS THREE SPOTS OF CORROSION BUILD-UP. CUT OUT DAMAGED AREA, FABRICATED FILLER AND DOUBLER INSTALLED REPAI R PER SRM 51-30-02. (M) 2 L 7 3 4F A3WE 1996121200777 19961212 00777 NM 1996 12 12 EISA96273 1 19961101 A 5312 BLKHD VERT BEAM BOEING 727 727223 1384074 NM BS 1183 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING A SCHEDULED D-CHECK, FOUND THE 1183 BLKHEAD VERTICAL BEAM CRACKED RBL 35. REPAIRED PER SRM 51-30-2 AND 51-40-4. (M) 2 L 7 3 4F A3WE 1996121200778 19961212 00778 NM 1996 12 12 EISA96272 1 19961101 A 5312 BLKHD VERT BEAM BOEING 727 727223 1384074 NM BS 1183 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING A SCHEDULED D-CHECK, FOUND THE 1183 BLKHEAD VERTICAL BEAM CRACKED LBL 35. REPAIRED PER SRM 51-40-4 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1996121200779 19961212 00779 NM 1996 12 12 EISA96211 1 19961101 A 5720 REPAIR DOUBLER BOEING 727 727223 1384074 NM WS 686.5 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING A SCHEDULED D-CHECK, FOUND THE LEFT WING STATION 686.5 FORWARD LOWER WEB REPAIR CRACKED IN THE RADIUS. REPAIRED PER SB 727-57-127. (M) 2 L 7 3 4F A3WE 1996121200780 19961212 00780 NM 1996 12 12 EISA96212 1 19961101 A 5720 DOUBLER BOEING 727 727223 1384074 NM WS 686.5 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING A SCHEDULED D-CHECK, FOUND THE LEFT WING STATION 686.5 AFT LOWER WEB REPAIR CRACKED IN THE RADIUS. REPAIRED PER SB 727-57-127. (M) 2 L 7 3 4F A3WE 1996121200781 19961212 00781 NM 1996 12 12 EISA96278 1 19961101 A 5320 TIE CLIPS BOEING 727 727223 1384074 NM BS 480-1070 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING A SCHEDULED D-CHECK, FOUND VARIOUS STRINGER TIE CLIPS CRACKED, FROM STATINS 480 TO 1070. REPLACED CLIPS PER SRM 51-10-1 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1996121200782 19961212 00782 NM 1996 12 12 EISA96277 1 19961101 A 5320 TIE CLIPS BOEING 727 727223 1384074 NM BS 580/590 MISSING A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING A SCHEDULED D-CHECK, FOUND STRINGER TIE CLIPS MISSING, STATIONS 580 AND 590 STRINGER 26 LEFT. INSTALLED CLIPS PE R SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1996121200783 19961212 00783 NM 1996 12 12 EISA96276 1 19961101 A 5320 TIE CLIP BOEING 727 727223 1384074 NM BS 720A MISMANUFACTURED A EISA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 314NE 19495 DURING A SCHEDULED D-CHECK, FOUND STRINGER TIE CLIP RADIUSED OUT TOO FAR, STATION 720A STRINGER 3 RIGHT. REPLACED TIE C LIP PER SRM 51-30-2 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1996121200784 19961212 00784 NM 1996 12 12 EISA96275 1 19961101 A 5311 FRAME BOEING 727 727223 1384074 NM BS 930 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING A SCHEDULED D-CHECK, FOUND FRAME CRACKED STATION 930 BETWEEN STRINGERS 12 AND 13 LEFT. REPAIRED PER SRM 51-30-2 AND 53-10-4. (M) 2 L 7 3 4F A3WE 1996121200785 19961212 00785 NM 1996 12 12 EISA96274 1 19961101 A 5312 BLKHD STIFFENER BOEING 727 727223 1384074 NM BS 1183 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING A SCHEDULED D-CHECK, FOUND A VERTICAL STIFFENER CRACKED IN OUTBOARD FLANGE STATION 1183 LBL 45. REPAIRED PER SRM 51-40-4. (M) 2 L 7 3 4F A3WE 1996121200786 19961212 00786 NM 1996 12 12 EISA96271 1 19961101 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 970 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING A SCHEDULED D-CHECK, FOUND STRINGER 22 LEFT CORRODED STATION 970. REPAIRED PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1996121200787 19961212 00787 NM 1996 12 12 EISA96270 1 19961101 A 5320 FITTING BOEING 727 727223 1384074 NM BS 740 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING A SCHEDULED D-CHECK, FOUND THE STATION 740 FITTING CRACKED AT STRINGER 23 LEFT EXTENDING 1.5 INCH BELOW STRINGER. REPAIRED PER S/B 727-53-0062 FIG 6 AND DWG NR 65C1534. (M) 2 L 7 3 4F A3WE 1996121200788 19961212 00788 NM 1996 12 12 EISA96269 1 19961101 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 640 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING A SCHEDULED D-CHECK, FOUND THE SEAT TRACK CORRODED STATION 560 RBL 45.5 TO STATION 640 RBL 45.5. REPLACED TRACK PER SRM 53-10-5 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1996121200789 19961212 00789 NM 1996 12 12 EISA96268 1 19961101 A 5713 STRINGER BOEING 727 727223 1384074 NM WS 560 BROKEN A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING A SCHEDULED D-CHECK, FOUND A LEFT WING STRINGER STATION 686 WITH A PIECE BROKE OFF THE AFT SIDE. REPAIRED PER SR M 57-10-4. (M) 2 L 7 3 4F A3WE 1996121200790 19961212 00790 NM 1996 12 12 EISA96267 1 19961101 A 5311 FRAME BOEING 727 727223 1384074 NM BS 560 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING A SCHEDULED D-CHECK, FOUND FRAME CRACKED STATION 560 STRINGER 6 LEFT. REPAIRED FRAME PER SRM 53-10-4 AND 51-30-2 . (M) 2 L 7 3 4F A3WE 1996121200791 19961212 00791 NM 1996 12 12 EISA96266 1 19961101 A 5330 SKIN BOEING 727 727223 1384074 NM BS 690 OIL CANNING A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING A SCHEDULED D-CHECK, FOUND FUSELAGE SKIN OIL CANNING STATION 690 BETWEEN STRINGER 25 AND 26 RIGHT. REPAIRED SKIN PER SRM 51-30-3 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1996121200792 19961212 00792 NM 1996 12 12 EISA96265 1 19961101 A 5311 BELT FRAME BOEING 727 727223 1384074 NM BS 629 DAMAGED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING A SCHEDULED D-CHECK, FOUND A HOLE IN THE BELT FRAME, STATION 700 STRINGER 16 LEFT. REPAIRED PER SRM 53-10-4. (M ) 2 L 7 3 4F A3WE 1996121200793 19961212 00793 NM 1996 12 12 EISA96264 1 19961101 A 5713 STRINGER BOEING 727 727223 1384074 NM WS 629 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING A SCHEDULED D-CHECK, FOUND A LEFT WING STRINGER CRACKED STATION 629, 11 INCHES FORWARD OF REAR SPAR. REPAIRED PE R SRM 57-10-4 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1996121200794 19961212 00794 NM 1996 12 12 EISA96213 1 19961101 A 5712 RIB BOEING 727 727223 1384074 NM WS 656 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING A SCHEDULED D-CHECK, FOUND IN THE RIB FLANGE LOWER RADIUS, LEFT WING STATION 656 ABOUT 12 INCHES FORWARD OF THE R EAR SPAR. REPAIRED PER SB 727-57-127. (M) 2 L 7 3 4F A3WE 1996121200795 19961212 00795 NM 1996 12 12 EISA96214 1 19960914 A 5720 ANGLE BOEING 727 72725 1384006 NM WS 300 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND RIGHT WING LE ANGLE CRACKED AT AFT END JUST INBOARD OF WS 330. FABRICATED AND INSTALLED DOUBLER PER SRM 51-20-2 A ND 51-30-2. (M) 2 L 7 3 4F A3WE 1996121200796 19961212 00796 NM 1996 12 12 EISA96210 1 19961101 A 5315 FLOOR BEAM BOEING 727 727223 1384074 NM BS 1050-1090 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING A SCHEDULED D-CHECK, FOUND A FLOOR BEAM CORRODED STATION 1050-1090 LBL 12. REPLACED FLOOR BEAM PER SRM 51-10-1 A ND 51-30-2. (M) 2 L 7 3 4F A3WE 1996121200797 19961212 00797 NM 1996 12 12 EISA96209 1 19961101 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 1110-1130 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING A SCHEDULED D-CHECK, FOUND A SEAT TRACK CORRODED STATION 1110-1130 RBL 24.75. REPLACED SEAT TRACK PER 53-10-5. ( M) 2 L 7 3 4F A3WE 1996121200798 19961212 00798 NM 1996 12 12 EISA96208 1 19961101 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 720 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING A SCHEDULED D-CHECK, FOUND A SEAT TRACK CORRODED STATION 720 LBL PLUS 10 LBL 24.75. REPLACED SEAT TRACK PER 53-1 0-5. (M) 2 L 7 3 4F A3WE 1996121200799 19961212 00799 NM 1996 12 12 EISA96207 1 19961101 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 720 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING A SCHEDULED D-CHECK, FOUND A SEAT TRACK CORRODED STATION 720 LBL 45.5. REPLACED SEAT TRACK PER 53-10-5. (M) 2 L 7 3 4F A3WE 1996121200800 19961212 00800 NM 1996 12 12 EISA96206 1 19961101 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 720 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING A SCHEDULED D-CHECK, FOUND A SEAT TRACK BROKEN STATION 610 LBL 62.5. REPLACED SEAT TRACK PER 53-10-5. (M) 2 L 7 3 4F A3WE 1996121200801 19961212 00801 NM 1996 12 12 EISA96205 1 19961101 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 600 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING A SCHEDULED D-CHECK, FOUND A SEAT TRACK CORRODED STATION 600 LBL L45.5. REPLACED SEAT TRACK PER 53-10-5. (M) 2 L 7 3 4F A3WE 1996121200802 19961212 00802 NM 1996 12 12 EISA96204 1 19961101 A 5712 RIB BOEING 727 727223 1384074 NM WS 629 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING A SCHEDULED D-CHECK, FOUND A CRACK IN A CRACK IN THE RIB FLANGE UPPER RADIUS, LEFT WING STATION 546.5 ABOUT 11.5 INCH FORWARD OF THE AFT SPAR. REPAIRED PER SB 727-57-127. (M) 2 L 7 3 4F A3WE 1996121200803 19961212 00803 NM 1996 12 12 EISA96203 1 19961101 A 5712 RIB BOEING 727 727223 1384074 NM WS 629 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURIGN A SCHEDULED D-CHECK, FUOND A CRACK IN A CRACK IN THE RIB FLANGE LOWER RADIUS, LEFT WING STATION 629 ABOUT 14 INCH ES AFT OF THE FRONT SPAR. REPAIRED PER SB 727-57-127. (M) 2 L 7 3 4F A3WE 1996121200804 19961212 00804 NM 1996 12 12 EISA96202 1 19961101 A 5712 RIB BOEING 727 727223 1384074 NM WS 629 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING A SCHEDULED D-CHECK, FOUND A CRACK IN A CRACK IN THE RIB FLANGE LOWER RADIUS, RIGHT WING STATION 629 ABOUT 13 INC HES FORWARD OF THE REAR SPAR. REPAIRED PER SB 727-57-127. (M) 2 L 7 3 4F A3WE 1996121200805 19961212 00805 NM 1996 12 12 EISA96201 1 19961101 A 5712 RIB BOEING 727 727223 1384074 NM WS 629 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING A SCHEDULED D-CHECK, FOUND A CRACK IN A CRACK IN THE RIB FLANGE LOWER RADIUS, RIGHT WING STATION 629 ABOUT 14 INC HES AFT OF THE FRONT SPAR. REPAIRED PER SB 727-57-127. (M) 2 L 7 3 4F A3WE 1996121200806 19961212 00806 NM 1996 12 12 EISA96200 1 19961101 A 5712 RIB BOEING 727 727223 1384074 NM WS 546.5 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING A SCHEDULED D-CHECK, FOUND A CRACK IN A CRACK IN THE RIB FLANGE LOWER RADIUS, LEFT WING STATION 546.5 ABOUT 18 IN CHES FORWARD OF THE AFT SPAR. REPAIRED PER SB 727-57-127. (M) 2 L 7 3 4F A3WE 1996121200807 19961212 00807 NM 1996 12 12 EISA96199 1 19961101 A 5712 RIB BOEING 727 727223 1384074 NM WS 601.5 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING A SCHEDULED D-CHECK, FOUND A CRACK IN A CRACK IN THE RIB FLANGE LOWER RADIUS, RIGHT WING STATION 601.50 ABOUT 14 INCHES FORWARD OF THE AFT SPAR. REPAIRED PER SB 727-57-127. (M) 2 L 7 3 4F A3WE 1996121200808 19961212 00808 NM 1996 12 12 EISA96198 1 19961101 A 5712 RIB BOEING 727 727223 1384074 NM WS 601.5 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING A SCHEDULED D-CHECK, FOUND A CRACK IN A RIB FLANGE LOWER RADIUS, LEFT WING STATION 601.5 ABOUT 14 INCHES FORWARD OF THE AFT SPAR. REPAIRED PER SB 727-57-127. (M) 2 L 7 3 4F A3WE 1996121200809 19961212 00809 NM 1996 12 12 EISA96197 1 19961101 A 5315 FLOOR BEAM BOEING 727 727223 1384074 NM BS 720 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING A SCHEDULED D-CHECK, FOUND A FLOOR BEAM CORRODED STATION 720 RBL 20. REPAIRED FLOOR BEAM PER SRM 51-40-6. (M) 2 L 7 3 4F A3WE 1996121200810 19961212 00810 NM 1996 12 12 EISA96263 1 19960915 A 5712 RIB BOEING 727 72725 1384006 NM WS 686.5 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND RIB CRACKED AT FORWARD SIDE OF UPPER VENT BOX AT WING STATION 686.5. INSTALLED REPAIR PER SRM 57-10-05. (M) 2 L 7 3 4F A3WE 1996121200811 19961212 00811 NM 1996 12 12 EISA96262 1 19960915 A 5712 RIB BOEING 727 72725 1384006 NM WS 70.5 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 300NE 18974 FOUND 2 CRACKS FROM FASTENER HOLES IN RIGHT WING RIB CHORD UPPER VERTICAL FLANGE WS 70.5 RT SIDE. INSTALLED REPAIR PER SB 727-57-0112. (M) 2 L 7 3 4F A3WE 1996121200812 19961212 00812 NM 1996 12 12 USAASB96231 1 19961030 A 3350 20121 POWER SUPPLY BOEING 737 737301 1384611 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 573US 23560 CLT - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT OVER THE MAIN ENTRY DOOR INOP DURING ROUTINE TEST. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY IN THE FORWARD OVERHEAD CABIN. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996121200813 19961212 00813 NM 1996 12 12 USAASB96237 1 19961118 A 3244 TIRE TREAD BOEING 737 737301 1384611 NM LT MLG SEPARATION A USAA O OTHER C W F.O.D. INADEQUATE Q C AP APPROACH 1 EA 19 591US 23936 BWI - FL 209 - AFTER T/O, INFORMED TIRE DEBRIS WAS ON RUNWAY AFTER T/O. DURING PREP FOR LANDING, THE LT MAIN GEAR RED U NSAFE LIGHT ILLUMINATED. AFTER TWO FLYBYS, TOWER DETERMINED GEAR DOWN WITH SOME DEBRIS BETWEEN LEFT MAIN TIRES. F/O MA DE VISUAL INSPECTION THRU MAIN GEAR VIEWER. CAPT DECLARED EMERGENCY AND THE FLT LANDED W/O INCIDENT. AFTER LANDING, MA IN GEAR WAS PINNED AND A/C TAXIED TO GATE. MX FOUND TREAD SEPARATED FROM THE LT MAIN GEAR INBD TIRE, CAUSING DAMAGE TO THE LT MAIN GEAR UPPER DOWNLOCK ASSY AND THE LT INBD T/E AFT FLAP. REPLACED DOWNLOCK ASSY, AFT FLAP AND WHEEL/TIRE ASSY (P/N 6558256275). GEAR TEST AND OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 1996121200814 19961212 00814 NM 1996 12 12 USAASB96229 1 19961118 A 5210 SEAL BOEING 737 7373B7 1384580 NM PAX DOOR ROLLED UNDER A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 373US 22952 CLT - FLT 489 - AFTER TAKEOFF, CREW WAS UNABLE TO PRESSURIZE AIRCRAFT DUE TO MAIN ENTRY DOOR SEAL BEING PARTIALLY ROLLED UNDER. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED MAIN ENTRY DOOR SEAL AND FO UND THE SEAL PARTIALLY ROLLED UNDER. OPERATED DOOR FOR PROPER SEAL, DOOR CHECKED NORMAL. (M) 2 L 7 2 4F RT A16WE 1996121200815 19961212 00815 NM 1996 12 12 USAASB96232 1 19961102 A 3350 AD20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 522AU 23857 PHL - MAINTENANCE FOUND THE EMERGENCY EXIT OVER THE AFT ENTRY DOOR INOP. MAINTENANCE REPLACED THE BATTERY PACK IN THE P OWER SUPPLY. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996121200816 19961212 00816 NM 1996 12 12 USAASB96235 1 19961116 A 3397 WIRE BOEING 737 7373B7 1384580 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 533AU 24515 CLT - MX FOUDN THE EXTERIOR LEFT LOWER MID FUSELAGE EMERGENCY EVACUATION LIGHT AND THE FORWARD SECTION OF INTERIOR FLOOR TRACK EMERGENCY EVACUATION LIGHTS INOP. MAINTENANCE RELAMPED AND CLEANED CONTACT OF EXTERIOR LEFT LOWER MID FUSELAGE E MERGENCY EVACUATION LIGHT AND REPAIRED BROKEN WIRES TO FORWARD SECTION OF FLOOR TRACK EMERGENCY EVACUATION LIGHTS. BOTH OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A16WE 1996121200817 19961212 00817 EU 1996 12 12 USAAF96118 1 19961116 A 3230 RETRACT MECH FOKKER F28 F28MK4000 4990810 EU LANDING GEAR MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 EA 19 494US 11167 FLT 873 - CLT-TYS - ON APPROACH TO TRI MAIN GEAR DOORS OPENED BUT GEAR DID NOT EXTEND. FLIGHT RETURNED TO CLT. CAPTAIN USED THE ALTERNATE EXTEND METHOD AND GEARS EXTENDED NORMALLY BY FREEFALL. AN EMERGENCY WAS DECLARED AS A PRECAUTION. F LIGHT LANDED NORMALLY WITHOUT FURTHER INCIDENT. (M) 2 L 7 2 4F RT A20EU 1996121200818 19961212 00818 EU 1996 12 12 USAAF96117 1 19961114 A 3260 UNSAFE LIGHT FOKKER F28 F28MK0100 4990807 EU LT MLG ILLLUMINATED A USAA O OTHER N FALSE WARNING CL CLIMB 1 EA 19 861US 11297 FLT 7900 - PIT - DLIGHT WAS A MAINTENANCE TEST FLIGHT. LEFT MAIN GEAR SHOWED AN UNSAFE CONDITION. RECYCLED GEAR AND AL L THREE INDICATIONS WERE NORMAL. CAPTAIN REQUESTED EMERGENCY EQUIPMENT AS A PRECAUTION. FLIGHT LANDED NORMALLY WITHOUT FURTHER INCIDENT. (M) 2 L 7 2 4F RT 1996121200819 19961212 00819 EU 1996 12 12 96ZZZM1556 1 19961114 A 3230 F28B410767M UPLOCK ASSY FOKKER F28 F28MK0100 4990807 EU RT MLG MALFUNCTIONED A USAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 19 861US 11297 FLT 7900 - PIT - FLIGHT WAS A MAINTENANCE TEST FLIGHT. LEFT MAIN GEAR SHOWED AN UNSAFE CONDITION. RECYCLED GEAR AND AL L THREE INDICATIONS WERE NORMAL. CAPTAIN REQUESTED EMERGENCY EQUIPMENT AS A PRECAUTION. FLIGHT LANDED NORMALLY WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED BOTH LEFT MAIN UPLOCK ASSEMBLIES, RIGHT MAIN FORWARD UPLOCK ASSEMBLY, AND LEFT MAIN OUTBOARD DOOR ASSEMBLY. GEAR SWING PERFORMED. ALL OPERATIONS NORMAL. REFERENCE USAAF96117 2 L 7 2 4F RT 1996121200820 19961212 00820 EU 1996 12 12 96ZZZM1557 1 19961114 A 3230 F28B410768M UPLOCK ASSY FOKKER F28 F28MK0100 4990807 EU RT MLG MALFUNCTIONED A USAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 19 861US 11297 FLT 7900 - PIT - FLIGHT WAS A MAINTENANCE TEST FLIGHT. LEFT MAIN GEAR SHOWED AN UNSAFE CONDITION. RECYCLED GEAR AND AL L THREE INDICATIONS WERE NORMAL. CAPTAIN REQUESTED EMERGENCY EQUIPMENT AS A PRECAUTION. FLIGHT LANDED NORMALLY WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED BOTH LEFT MAIN UPLOCK ASSEMBLIES, RIGHT MAIN FORWARD UPLOCK ASSEMBLY, AND LEFT MAIN OUTBOARD DOOR ASSEMBLY. GEAR SWING PERFORMED. ALL OPERATIONS NORMAL. (REFERENCE USAAF96117) 2 L 7 2 4F RT 1996121200821 19961212 00821 EU 1996 12 12 96ZZZM1558 1 19961114 A 5280 D13300405 DOOR ASSY FOKKER F28 F28MK0100 4990807 EU LT MLG DAMAGED A USAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 19 861US 11297 FLT 7900 - PIT - FLIGHT WAS A MAINTENANCE TEST FLIGHT. LEFT MAIN GEAR SHOWED AN UNSAFE CONDITION. RECYCLED GEAR AND AL L THREE INDICATIONS WERE NORMAL. CAPTAIN REQUESTED EMERGENCY EQUIPMENT AS A PRECAUTION. FLIGHT LANDED NORMALLY WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED BOTH LEFT MAIN UPLOCK ASSEMBLIES, RIGHT MAIN FORWARD UPLOCK ASSEMBLY, AND LEFT MAIN OUTBOARD DOOR ASSEMBLY. GEAR SWING PERFORMED. ALL OPERATIONS NORMAL. REFERENCE USAAF96117 2 L 7 2 4F RT 1996121200822 19961212 00822 NM 1996 12 12 USAABB96046 1 19961112 A 3350 86210066 BATTERY PACK BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 611AU 27123 LAX - FOUND SEAT MOUNTED EMERGENCY LIGHT EXIT BATTERIES BAD. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 1996121200823 19961212 00823 CE 1996 12 12 C2XA96CL038 1 19961107 A 5522 130610000613 SKIN BEECH 1900 1900D 1154162 CE LT ELEVATOR LIGHTNING STRIKE A C2XA K NONE C F.O.D. CR CRUISE 1 SW 09 16540 2414 487 UE172 CLE - FLT 3246 - THE CREW REPORTED A LIGHTNING STRIKE ON THE NOSE OF THE AIRCRAFT. MAINTENANCE ACCOMPLISHED A LIGHTNING STRIKE INSPECTION AND REMOVED AND REPLACED THE LEFT HAND ELEVATOR IAW B1900D MM 27-30-02, ALL OPERATIONAL CHECKS WERE G OOD. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A24CE 1996121200824 19961212 00824 CE 1996 12 12 C2XA96CL036 1 19961109 A 2435 23078019 START/GEN BEECH 1900 1900D 1154162 CE RT ENG FAILED A C2XA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. J WARNING INDICATION TX TAXI/GRND HDL 1 SW 09 38537 1332 UE158 FLT 3190 - CREW REPORTED THAT ON ATTEMPTED ENG START, THE RT STARTER/GEN CONTINUED TO RUN WITH THE ENG SHUT DOWN AND THE STARTER SW OFF. THE CREW RECEIVED A FIRE IND AND ACTIVATED THE FIRE EXTINGUISHER. MX INSPECTED THE A/C AND REMOVED AN D REPLACED THE RIGHT STARTER/GEN IAW B1900D MM 24-30-01, THE RIGHT ENG POWER SUPPLY AND THE BUS TIE CONTROL PC BOARD WER E ALSO REPLACED IAW B1900D MM 24-30-00. THE RIGHT FIRE BOTTLE WAS REPLACED IAW B1900 MM 24-30-00. AIRCRAFT RELEASED FO R SERVICE. (M) 2 L 7 2 4T RT A24CE 1996121200825 19961212 00825 SO 1996 12 12 C2XA96IA279 1 19961102 A 5713 12016085002 STRINGER EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16718 120136 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING STRINGER 10 WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE STRINGER USING A SPLICE. ALL WORK WAS ACCOMPLISHED IAW EMBRAER FAX EST 501/95. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SER VICE. (M) 2 L 7 2 4T RT A31SO 1996121200826 19961212 00826 SO 1996 12 12 C2XA96IA280 1 19961102 A 5347 12026864007 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16718 120136 IAH - DURING C-CHECK INSPECTION, THE AFT LEFT FLOOR NEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLAC ED THE AFFECTED PORTION OF SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996121200827 19961212 00827 SO 1996 12 12 C2XA96IA281 1 19961104 A 5713 12016085002 STRINGER EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 22727 120177 IAH - DURING EXTENDED RANGE MODIFICATION, THE RIGHT WING STRINGER 10 WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE STRINGER USING A SPLICE. ALL WORK WAS ACCOMPLISHED IAW EMBRAER FAX EST 501/95. THE AIRCRAFT WAS THEN APPROVED FOR RETU RN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996121200828 19961212 00828 EU 1996 12 12 C2XA96RT017 1 19961031 A 3234 1005383Y00 SELECTOR VLV AEROSP ATR42 ATR42320 8680930 EU LANDING GEAR FAILED A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 09 47801 60 ROD - FLT 3627 - AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO ROC UNEVENTFULLY. LANDING GAER MEL 'D. SUBSEQUENTLY FOUND LANDING GEAR SELECTOR VALVE INOPERATIVE. REMOVED AND REPLACED SELECTOR VALVE IAW ATR 42 MX MANU AL 32-31-51. OPS AND LEAK CHECK GOOD. AIRCRAFT REMOVED FROM MEL AND RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996121200829 19961212 00829 EU 1996 12 12 C2XA96IA278 1 19961024 A 3230 10GA CONNECTOR AEROSP ATR42 ATR42320 8680930 EU RT MLG LOOSE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 93840 271 LIT - FLT 3789 - PILOT REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE AIRCRAFT RETURNED TO THE FIE LD WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS THEN DISPATCHED UNDER MEL 32-31-3, CONTROL NR 895816. UPON CLEARING OF T HE MEL, MAINTENANCE CLEANED ALL CANNON PLUG CONNECTIONS, AND RESECURED THE RIGHT GEAR UPLOCK BOX CANNON PLUG. THE GEAR OPERATIONALLY CHECKED GOOD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996121200830 19961212 00830 NE 1996 12 12 C2XA96CL040 2 19961111 A 7260 3022375 GARLOCK SEAL EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE WORN A C2XA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SW 09 16702 120078 CLE - FLT 3121 - CREW REPORTED THAT THEY NOTICED A OIL LEAK ON THE RIGHT ENGINE IN FLIGHT. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED THE RIGHT ENGINE STARTER GENERATOR GARLOCK SEAL AND SHAFT O-RIN G IAW PW MM 72-01-50. OPERATIONAL AND LEAKS WERE GOOD, AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1996121200831 19961212 00831 CE 1996 12 12 C2XA96CL039 1 19961107 A 5320 129440061602 STRAKE BEECH 1900 1900D 1154162 CE RT FUSELAGE LIGHTNING STRIKE A C2XA K NONE C F.O.D. CR CRUISE 1 SW 09 16540 2414 UE172 CLE - FLT 3246 - THE CREW REPORTED A LIGHTNING STRIKE ON THE NOSE OF THE AIRCRAFT. MAINTENANCE ACCOMPLISHED A LIGHTNING STRIKE INSPECTION AND FOUND DAMAGE TO THE RIGHT AFT STRAKE. MAINTENANCE REMOVED AND REPLACED THE STRAKE IAW B1900D STR UCTURAL REPAIR MANUAL 51-40-00 AND 51-40-03. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A24CE 1996121200832 19961212 00832 NE 1996 12 12 EIAA9684 2 19961112 A 7260 MODUL04AG ANGLE GEARBOX BOEING 747 747212B 1384886 NM PWA JT9 JT9D7F 52054 NE NR 3 ENGINE LEAKING A EIAA E ENGINE SHUTDOWN J K WARNING INDICATION FLUID LOSS CR CRUISE 1 NM 09 485EV 272 20712 662479 LOG PAGE: F35815. JFK - 3 HOURS OUT OF EINN, NR 3 ENGINE OIL QUANTITY STARTED TO DECREASE FROM ONE-HALF TO 'E'. NR 3 OIL PRESSURE STARTED DROPPING INTO CAUTION RANGE, THE LOW OIL PRESSURE LIGHT ILLUMINATED. ENGINE WAS SHUT DOWN. N1 IND . 30.4 PERCENT AND N2 26.7 PERCENT AT PRESSURE ALT OF 260,000 FEET. OIL PRESSURE INDICATED 21 PSI FOR 3.5 HOURS OF WIND MILLING IN-FLIGHT. PERFORMED WINDMILLING AND CHIP DETECTOR CHECKS WITH NO DEFECTS NOTED. OIL LEAK WAS FOUND AT ANGLE D RIVE GEARBOX COVER PLATE. FOUND A HEILCOIL PULLED LOOSE FROM COVER AND REPAIRED PER ECRA 66-2479-72-015-1. (X) 2 L 7 4 4F 4 F A20WE E20EA 1996121200833 19961212 00833 NM 1996 12 12 USAASB96218 1 19961025 A 5240 STRAP BOEING 737 7373B7 1384580 NM SERVICE DOOR OUT OF POSITION A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 527AU 23862 CLT - FL 1635 - CAPTAIN CONTACTED DISPATCH AND INDICATED HE NEEDED TO DIVERT DUE TO AN AFT SERVICE DOOR RESTRAINING STRA P CAUGHT OUTSIDE THE DOOR AND BANGING AGAINST THE FUSELAGE. DECISION WAS MADE TO DIVERT TO CLT. FLGHT LANDED WITHOUT F URHTER INCIDENT. MAINTENANCE PROPERLY STOWED STRAP AND CHECKED THE AFT SERVICE DOOR FOR SIGNS OF DAMAGE. NO DAMAGE NOT ED. (M) 2 L 7 2 4F RT A16WE 1996121200834 19961212 00834 NM 1996 12 12 USAASB96219 1 19961026 A 2131 7638101 CONTROLLER BOEING 737 737301 1384611 NM E/E COMPT FAILED A USAA A B UNSCHED LANDING EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 19 576US 11466 23741 MCI - FLT 136 - CAPTAIN REPORTED PRESSURIZATION LOSS AND DESCENDED TO 10,000 FEET. CAPTAIN COULD NOT REGAIN CONTROL OF CABIN UNTIL LEVEL OFF AT 10,000 FEET. EMERGENCY WAS DECLARED FOR THE EMERGENCY DESCENT. THE OXYGEN MASKS WERE NOT DEP LOYED. FLIGHT DIVERTED TO MCI AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CABIN PRESSURE CONTROLLER. ACCOMPLISHED TEST PER MM 21-31-00. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 1996121200835 19961212 00835 NM 1996 12 12 TAOA119603 1 19961115 A 3350 900835A BATTERY PACK GRIMES BOEING 727 727225 1384077 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 923TS 11307 20441 ON THE OVERNIGHT CHECK, THE RIGHT OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED BATTERY PACK. OPERATIO NAL CHECKED OK. (M) 2 L 7 3 4F A3WE 1996121200836 19961212 00836 EU 1996 12 12 SIMA963201 1 19961115 A 3350 7012201 BULB AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 251AE 250 ORD - FLT 4235 - TWO FORWARD EMERGENCY LIGHTS WILL NOT TEST DURING TEST. RAI'D LAMP (BULB) IN THE LEFT AND RIGHT FORWAR D EXIT DOORS SIGN. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996121200837 19961212 00837 EU 1996 12 12 M3HA96033 1 19961115 A 3320 8ED00558800 POWER UNIT AEROSP ATR42 ATR42300 8680920 EU CABIN SHORTED A M3HA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 13 4206G 081 HNL - FLT 659 - ON RETURN FLIGHT FROM PASSENGER REPORTED SMOKE ROW 5 C/D, LATERAL LIGHTS AREA. MEL'D LATERAL LIGHTS. P OWER UNIT FOUND TO BE BURNED. (M) 2 H 7 2 4T RT A53EU 1996121200838 19961212 00838 EU 1996 12 12 M3HA96034 1 19961115 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A M3HA K NONE L NO TEST IN INSP/MAINT 1 WP 13 4204G 3070 061 HNL - DURING DAILY INSPECTION, FLOOR TRACK EMERGENCY LIGHTS, WERE FOUND TO BE OUT. REMOVED AND INSTALLED SERVICEABLE EM ERGENCY BATTERY PACK. (M) 2 H 7 2 4T RT A53EU 1996121200839 19961212 00839 NE 1996 12 12 ASOA96048 2 19961106 A 7200 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE LEFT FAILED A A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 11 232AS 16462 120036 DURING INITIAL APPROACH DHN-ATL, THE LEFT ENGINE FAILED WITHOUT WARNING. THE CREW ACCOMPLISHED THE 'ENGINE FAILURE IN F LIGHT' CHECKLIST, REQUESTED EMERGENCY CLEARANCE FOR IMMEDIATE LANDING, AND LANDED SAFELY AND WITHOUT INCIDENT IN ATL. R EMOVED AND REPLACED THE LEFT ENGINE. OPERATIONAL AND LEAK CHECKS WERE GOOD AND AIRCRAFT WAS RELEASED FOR FURTER SERVICE . (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1996121200840 19961212 00840 WP 1996 12 12 HALA96161 1 19961117 A 3350 LIGHT DOUG DC9 DC951 3022051 WP CABIN SHORTED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 669HA 47654 HNL - FLT 514 - EMERGENCY FLOOR LIGHTS FRONT HALF INOP. REMOVED AND REPLACED FORWARD EMERGENCY FLOOR LIGHT BATTERIES. C ONDITION SAME. REPAIRED SHORTED RIBBON. OPS CHECK OK. (M) 2 L 7 2 4F A6WE 1996121200841 19961212 00841 SW 1996 12 12 MALA965184 1 19961105 A 5311 2722102 FRAME SWRNGN SA227 SA227AC 8780603 SW BS 317 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 433MA AC714 DURING A BLOCK INSPECTION IN MSP, MAINTENANCE FOUND THE LEFT BELT FRAME P/N 27-22102 AT FS 317 AND WL 78 TO HAVE A .150 INCH CRACK IN THE RELIEF RADIUS. REPAIRED CRACK BY FABRICATING AND INSTALLING A REPAIR DOUBLER IAW AEROTECH DESIGNS EA0 1-96115, DATED NOV 5/96. (M) 2 L 7 2 4T RT A8SW 1996121200842 19961212 00842 SW 1996 12 12 MALA965181 1 19961107 A 5330 SKIN SWRNGN SA227 SA227AC 8780603 SW BS 594 DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 436MA AC719B DURING AN INSPECTION IN MSP, MAINTENANCE FOUND FUSELAGE SKIN DENTED AND OIL CANNING AT FS 594 AND RIGHT FUSELAGE STRINGE R NR 8. COMPLETED REPAIR TO FUSELAGE SKIN BY FABRICATING AND INSTALLING (4.25 BY 4.25) .040 INCH 2024-T3 EXTERNAL DOUBL ER IAW FAC SRM 53-90-20 REPAIR NR 14. (M) 2 L 7 2 4T RT A8SW 1996121200843 19961212 00843 SW 1996 12 12 MALA965187 1 19961105 A 5712 RIB SWRNGN SA227 SA227AC 8780603 SW WS 39 DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 433MA AC714 DURING A BLOCK INSPECTION IN MSP, MAINTENANCE FOUND THE RIGHT AFT FALSE WING RIB AT WS 39 DENTED AND CHAFED APPROX .025 IN FLANGE. COMPLETED REPAIR BY FABRICATING AND INSTALLING A REPAIR DOUBLER IAW AEROTECH DESIGNS EA01-96113 DATED NOV 4/ 96. (M) 2 L 7 2 4T RT A8SW 1996121200844 19961212 00844 SW 1996 12 12 MALA965186 1 19961105 A 5230 SKIN SWRNGN SA227 SA227AC 8780603 SW CARGO DOOR CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 433MA AC714 DURING A BLOCK INSPECTION IN MSP, MAINTENANCE FOUND THE CARGO DOOR SKIN AT BOTH FORWARD AND AFT ENDS OF CARGO DOOR HINGE CHAFED APPROXIMATLEY .015 INCH BY 1.25 INCH. COMPLETED REPAIR BY FABRICATING AND INSTALLING REPAIR DOUBLERS TO AFFECTE D AREAS IAW FAIRCHILD ARP 52-30-9130 DATED JUNE 20/91. (M) 2 L 7 2 4T RT A8SW 1996121200845 19961212 00845 SW 1996 12 12 MALA965185 1 19961105 A 5311 2722093 FRAME SWRNGN SA227 SA227AC 8780603 SW BS 332 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 433MA AC714 DURING A BLOCK INSPECTION IN MSP, MAINTENANCE FOUND THE LEFT BELT FRAME P/N 27-22093 AT FS 332 AND WL 78 TO HAVE A .25 I NCH CRACK IN THE RELIEF RADIUS. REPAIRED CRACK BY FABRICATING AND INSTALLING A REPAIR DOUBLER IAW AEROTECH DESIGNS EA01 -96115 DATED NOV 5/96. (M) 2 L 7 2 4T RT A8SW 1996121200846 19961212 00846 SW 1996 12 12 MALA965183 1 19961105 A 5311 2722100 FRAME SWRNGN SA227 SA227AC 8780603 SW BS 242 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 433MA AC714 DURING A BLOCK INSPECTION IN MSP, MAINTENANCE FOUND THE LEFT BELT FRAME P/N 27-22100 AT FS 242 AND WL 78 TO HAVE A .125 INCH CRACK IN THE RELIEF RADIUS. REPAIRED CRACK BY FABRICATING AND INSTALLING A REPAIR DOUBLER IAW AEROTECH DESIGNS EA 01-96115 DATED NOV 5/96. (M) 2 L 7 2 4T RT A8SW 1996121200847 19961212 00847 SW 1996 12 12 MALA965182 1 19961105 A 5311 2722093 FRAME SWRNGN SA227 SA227AC 8780603 SW BS 144 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 433MA AC714 DURING A BLOCK INSPECTION IN MSP, MAINTENANCE FOUND THE RIGHT BELT FRAME P/N 27-22093 AT FS 144 AND JUST ABOVE WL 70 TO HAVE A 1 INCH CRACK IN THE RELIEF RADIUS. REPAIRED AREA BY FABRICATING AND INSTALLING A REPAIR DOUBLER IAW FAIRCHILD SR M 53-90-20, REPAIR NR 20, PGS 87-90. (M) 2 L 7 2 4T RT A8SW 1996121200848 19961212 00848 NM 1996 12 12 MALA965204 1 19961116 A 3350 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 831MA 339 DURING MAINTENANCE INSPECTION IN DTW, AN EMERGENCY TRACK LIGHT WAS FOUND TO BE INOP AT SEAT 4D PLUS E. MAINTENANCE REPL ACED A DAMAGED LIGHT SOCKET. ALL CHECKS SATISFACTORY. (M) 2 H 7 2 4T RT A13NM 1996121200849 19961212 00849 1996 12 12 MALA965205 4 19961116 A 3417 7000700975 AIR DATA COMP DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 802MA 245 FLT 3281 - ON CLIMB-OUT FROM MSP, THE FLIGHT OFFICERS VSI SHOWED ZERO. DURING DESCENTS, THE SYSTEM OPERATED NORMALLY. T HE AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE NR 2 ADC. ALL CHECKS SATISFACTORY. (M) 2 H 7 2 4T RT A13NM 1996121200850 19961212 00850 NM 1996 12 12 TWRA96357 1 19961113 A 3350 S1356B37 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 620FF 471 21162 DURING DAILY CHECK, FOUND MID GALLEY EMERGENCY CEILING LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY. OPS CHECKED NORMAL PER 33-51-00. (M) 2 L 7 4 4F A20WE 1996121200851 19961212 00851 NM 1996 12 12 TWRA96363 1 19961121 A 3350 3004181A LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 619FF 1471 21316 DURING DAILY CHECK, FOUND 4L MED UPPER BUSTLE EMERGENCY LIGHT NOT ILLUMINATING. REMOVED AND REPLACED LIGHT ASSY PER MM 33-51-00. OPS CHECKED NORMAL. (M) 2 L 7 4 4F A20WE 1996121200852 19961212 00852 1996 12 12 TWRA95362 4 19961121 A 2565 7A14188 DOOR SLIDE BFGOODRICH BOEING 747 747238B 1384828 NM 3R DOOR ZERO PRESSURE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 607PE G318 20011 ROUTINE CHECK MAINTENANCE FOUND NR 3 MED SLIDE WITH ZERO PRESSURE. REMOVED AND REPLACED SLIDE AS PER MM 25-65-06 AND WI , TC 25-664-23R. OPERATIONAL CHECK OK. AIRCRAFT RETURN TO SERVICE. (M) 2 L 7 4 4F A20WE 1996121200853 19961212 00853 NM 1996 12 12 TWRA96364 1 19961121 A 3350 3004181A LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 6186 1380 21439 DURING DAILY CHECK, FOUND 1R MED UPPER BUSTLE EMERGENCY LIGHT DOES NOT ILLUMINATE. REMOVED AND REPLACED R1 LIGHT ASSY P ER MM 33-51-00. OPS CHECKED NORMAL. (M) 2 L 7 4 4F A20WE 1996121200854 19961212 00854 NE 1996 12 12 TWRA96327 2 19961005 A 7261 BEARING TUBE BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE NR 4 ENGINE CLOGGED A TWRA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 15 614FF 89566 20534 AFTER STARTING NR 4 ENGINE, FLIGHT ATTENDANT REPORTED SMOKE IN CABIN. FURTHER EVALUATION NEEDED ON THE ENGINE. MAINTEN ANCE FOUND NR 3 BEARING TUBE CLOGGED. RETRIEVED CARBON DEPOSIT ON NR 3 COMPARTMENT. REMOVED AND REPLACED EVC AS PER TC 75-361. RAN ENGINE PER MM 71-00-00 TEST 8, OPS CHECKED NORMAL. A/C RETURN TO LEASE COMPANY. (M) 2 L 7 4 4F 4 F A20WE E20EA 1996121200855 19961212 00855 NM 1996 12 12 TWRA96365 1 19961123 A 3350 S1356B37 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 616FF 00096A 21939 DURNG DAILY CHECK, FOUND CEILING EMEGENCY LIGHT AT 52 HJK INOP. REMOVED AND REPLACED CEILING LIGHT AS PER MM 33-51-07 P AGE 401. OPS CHECKED NORMAL. (M) 2 L 7 4 4F A20WE 1996121200856 19961212 00856 1996 12 12 TWRA96361 4 19961118 A 2565 7A14188 DOOR SLIDE BFGOODRICH BOEING 747 747238B 1384828 NM 3R DOOR LOW PRESSURE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 607PE G382 20011 DURING ROUTINE CHECK, MAINTENANCE FOUND NR 3MED SLIDE WITH LOW PRESSURE. REMOVED AND REPLACED SLIDE AS PER MM 25-65-01 PAGE 401. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 4 4F A20WE 1996121200857 19961212 00857 NM 1996 12 12 TWRA96359 1 19961119 A 5210 MS1656237 PIN BOEING 747 747121 1384871 NM 2R DOOR SHEARED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 609FF 20354 DURING TRAINING TEST 2R DOOR, DOOR ASSIST BOTTLE DID NOT DEPLOY OR DISCHARGE BOTTLE ON SLIDE DEPLOYMENT OPERATION, CABLE ATTACHMENT PIN SHEARED. RIGHT FUSELAGE TO WING PANEL 192RR SUSTAINED DAMAGE DUE TO SLIDE DEPLOYMENT. REPLACED TRIGGER RETAINING PIN AS PER MM 52-11-08. PERFORMED OPERATION CHECK NORMAL. REPAIRED PANEL AS PER SRM 51-40-15. (M) 2 L 7 4 4F A20WE 1996121200858 19961212 00858 NM 1996 12 12 TWRA96354 1 19961107 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE PUNCTURED A TWRA K NONE O OTHER IN INSP/MAINT 1 EA 15 617FF 19650 DURING WALKAROUND, FOUND SMALL HOLE ON FUSELAGE (APPROX .75 INCH BY .5 INCH) JUST FORWARD OF AFT CARGO DOOR, CAUSED BY C ARGO LOADING EQUIPMENT. REPAIRED SMALL HOLE ON FUSELAGE PER SRM 53-30-03 PAGE 2J FIG 1A. AIRCRAFT RETURN TO SERVICE. ( M) 2 L 7 4 4F A20WE 1996121200859 19961212 00859 NM 1996 12 12 AWXA9600665 1 19961109 A 5330 SKIN BOEING 737 737277 1384570 NM BS 747 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 184AW 22651 PHX - CRACK IN FUSELAGE AREA AFT OF WING TO BODY FAIRING, STATION 747 BETWEEN STRINGER 18R AND STRINGER 19R. STRINGER 19R AT DOME NUT PLATE CORRODED AT STATION 747. TERMINATED CRACK APPROXIMATELY 1 INCH BY STOP DRILL. VERIFIED BY HFEC. REPAIRED PER SRM 53-30-3, FIG 1. REMOVED CORRODED SECTION AT STRINGER. SPLICED NEW SECTION IN PER SRM 53-10-3, FIG 1, SHEET 8. (M) 2 L 7 2 4F RT A16WE 1996121200860 19961212 00860 NM 1996 12 12 AWXA9600649 1 19961103 A 3213 STRUT BOEING 737 737277 1384570 NM LT MLG FLUID LOW A AWXA K NONE F FLT CONT AFFECTED CL CLIMB 1 WP 28 180AW 22647 PHX - FLT 2887 - AIRPLANE ROLLS OFF TO RIGHT UPON LIFT OFF. FLIGHT CONTROLS ARE NORMAL. WIND CONDITIONS LIGHT. ROLL C ONTROL NORMAL AFTER TAKEOFF. CHECKED LEFT STRUT SERVICING AS CREW REQUESTED. FOUND FLUID VERY DIRTY AND QTY LOW. FLUS HED STRUT AND SERVICED PER BMM 12-51-31. NO LEAKS NOTED. (M) 2 L 7 2 4F RT A16WE 1996121200861 19961212 00861 NM 1996 12 12 AWXA9600661 1 19961109 A 3397 WIRE BOEING 757 757225 1384959 NM CABIN DISCONNECTED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 913AW 22207 PHX - FLT 2611 - EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 19. RESPLICED WIRING. OPERATIONS CHECK GOOD. (M) 2 L 7 2 4F RT A2NM 1996121200862 19961212 00862 EU 1996 12 12 AWXA9600651 1 19961103 A 3350 321430 BATTERY PACK AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 624AW 321430 55 PHX - FLT 2050 - AFT EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK ABOVE L-2 DOOR. OPERATIONS CHECK GOOD. (M) 2 L 7 2 4F RT A28NM 1996121200863 19961212 00863 NM 1996 12 12 AWXA9600659 1 19961109 A 3397 WIRE HARNESS BOEING 737 7373Y0 1384671 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 EICKV 23747 PHX - FLT 2541 - FOUND EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 20L. REPLACED WIRE HARNESS. OPERATIONS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996121200864 19961212 00864 NM 1996 12 12 AWXA9600660 1 19961109 A 3350 1060091101 LIGHT BOEING 737 737277 1384570 NM CABIN INOP A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 183AW 22650 PHX - FLT 2267 - FOUND EMERGENCY EXIT LIGHT ON SEAT AT OVERWING EMERGENCY EXIT IS INOPERATIVE. REMOVED AND REPLACED LIG HT ASSEMBLY. OPERATIONS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996121200865 19961212 00865 NM 1996 12 12 AWXA9600656 1 19961106 A 3350 PLUG BOEING 737 7372U9 1384498 NM CABIN DISCONNECTED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 149AW 22575 PHX - FLT 7705 - FOUND SEAT EMERGENCY LIGHT INOP AT ROW 17. RECONNECTED PLUG UNDE SEAT. OPERATIONS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996121200866 19961212 00866 NM 1996 12 12 AWXA9600657 1 19961106 A 3397 WIRE BOEING 737 7373G7 1384595 NM CABIN DISCONNECTED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 302AW 24009 PHX - FLT 2498 - FOUND EMERGENCY LIGHTS AT SEATS 8, 9, 10 AND 11 INOP. RECONNECTED WIRE AT ROW 10 A, B, C. OPERATIONS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996121200867 19961212 00867 NM 1996 12 12 AWXA9600655 1 19961105 A 3350 SOCKET BOEING 737 73733A 1384673 NM WING FAIRING DIRTY A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 174AW 23633 PHX - FLT 651 - FOUND EMERGENCY LIGHT LEFT SIDE AFT OF WING TO BODY FAIRING INOPERATIVE. CLEANED SOCKET. SYSTEM OPERAT IONS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996121200868 19961212 00868 NM 1996 12 12 AWXA960645 1 19961029 A 3350 LIGHT BOEING 737 7373Q8 1384670 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 327AW 23507 FLT 2598 - PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY LIGHT ROW 19 INOP. REPLACED LIGHT LENS FOR ROW 19 EXIT LIGHT. LIGHT FUNCTION CHECK OK. (M) 2 L 7 2 4F RT A16WE 1996121200869 19961212 00869 NM 1996 12 12 AWXA9600662 1 19961109 A 3350 20121 BATT CHARGER BOEING 737 73733A 1384673 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 164AW 9942 23625 PHX - FLT 2274 - FOUND EMERGENCY EXIT LIGHTS INOPERATIVE ROWS 19 TO 23. REMOVED AND REPLACED EMERGENCY BATTERY CHARGER ASSEMBLY. OPERATIONS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996121200870 19961212 00870 NM 1996 12 12 AWXA9600666 1 19961107 A 3350 900835A BATTERY PACK BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 189AW 21087 22656 PHX - FLT 2024 - FOUND LEFT OVERWING FLOOR PROXIMITY EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK, SEAT 20 OVERHEAD. SYSTEM OPERATES NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996121200871 19961212 00871 NM 1996 12 12 AWXA9600658 1 19961106 A 3350 900542 BATTERY BOEING 737 737275 1384485 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 CGCPW 20959 FOUND EMERGENCY EXIT SIGN ABOVE R-2 DOOR INOPERATIVE. REMOVED AND REPLACED BATTERY. OPERATIONS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1996121200872 19961212 00872 NM 1996 12 12 AWXA9600653 1 19961105 A 3350 900835A BATTERY PACK BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 187AW 23226 22654 FOUND L-2 AND R-2 VERTICAL EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. LIGHTS OPERATIONS CHEC K GOOD. (M) 2 L 7 2 4F RT A16WE 1996121200873 19961212 00873 NM 1996 12 12 AWXA9600654 1 19961105 A 3350 864705 POWER SUPPLY BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 187AW 3645 22654 CMH - FLT 400 - FOUND VERTICALLY MOUNTED EXIT SIGN AT LEFT OVERWING EXIT INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY . OPERATIONS CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 1996121200874 19961212 00874 NM 1996 12 12 AWXA9600650 1 19961104 A 3350 849029 BATTERY PACK BOEING 737 737301 1384611 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 324AW AWA102 23261 PHX - FLT 2541 - DURING EMERGENCY LIGHT TEST, R-2 DOOR AND LAST 6 ROWS EMERGENCY LIGHTS WOULD NOT ILLUMINATE. REPLACED BATTERY PACK, OPERATIONS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996121200875 19961212 00875 NM 1996 12 12 AWXA960646 1 19961031 A 3350 831862 BATTERY PACK BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 184AW 036 22651 CMH - FLT 400 - DURING ROUTINE MAINTENANCE CHECK, FOUND LEFT OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED LEFT OVERWING EMERGENCY LIGHT BATTERY PACK. OPERATIONS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996121200876 19961212 00876 NM 1996 12 12 AWXA960643 1 19961029 A 3350 415405 BATTERY PACK BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 189AW 9399 22656 PHX - FLT 2267 - DURING ROUTINE MAINTENANCE CHECK, FOUND VERTICAL EMERGENCY EXIT LIGHTS AT L-2 AND R-2 DOORS INOP. REMO VED AND REPLACED BATTERY PACK AT M1051. OPERATIONS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1996121200877 19961212 00877 WP 1996 12 12 ASAA9680262 1 19961125 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 965AS 53079 PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND DIM. REPLACED THE LIGHT ASSEMBLY AND OPE RATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996121200878 19961212 00878 WP 1996 12 12 ASAA9680261 1 19961124 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 941AS 17787 49925 PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996121200879 19961212 00879 WP 1996 12 12 ASAA9680260 1 19961122 A 3350 S103 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 947AS 53020 SAN - PRIOR TO DEPARTURE OF FLT 511, CREW REPORTED ALL EMERGENCY LIGHTS WERE FOUND INOPERATIVE. FOUND ALL EMERGENCY LIG HTS HAD BEEN LEFT IN OPERATION AND BATTERIES DISCHARGED. FERRIED AIRCRAFT TO SFO AND REPLACED THE BATTERIES FOR ALL INT ERIOR EMERGENCY LIGHTS AND REPLACED THE POWER SUPPLY FOR THE EXTERIOR OVERWING EMERGENCY LIGHTS AND ALL OPERATED NORMALL Y. (M) 2 L 7 2 4F RT A6WE 1996121200880 19961212 00880 WP 1996 12 12 96ZZZM1559 1 19961122 A 3350 6011779 POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 947AS 53020 SAN - PRIOR TO DEPARTURE OF FLT 511, CREW REPORTED ALL EMERGENCY LIGHTS WERE FOUND INOPERATIVE. FOUND ALL EMERGENCY LIG HTS HAD BEEN LEFT IN OPERATION AND BATTERIES DISCHARGED. FERRIED AIRCRAFT TO SFO AND REPLACED THE BATTERIES FOR ALL INT ERIOR EMERGENCY LIGHTS AND REPLACED THE POWER SUPPLY FOR THE EXTERIOR OVERWING EMERGENCY LIGHTS AND ALL OPERATED NORMALL Y. REFERENCE ASAA9680260. 2 L 7 2 4F RT A6WE 1996121200881 19961212 00881 WP 1996 12 12 ASAA9680258 1 19961117 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 962AS 14174 53076 PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT NEON LAMP WAS FOUND INOPERATIVE. REPLACED THE LIGH T ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996121200882 19961212 00882 WP 1996 12 12 ASAA9680256 1 19961115 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 934AS 49235 PDX - DURNG MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE TAIL CONE AREA WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996121200883 19961212 00883 NM 1996 12 12 ASAA9640099 1 19961122 A 3397 WIRE BOEING 737 7374S3 1384711 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 786AS 24795 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 14-17. RECON NECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996121200884 19961212 00884 WP 1996 12 12 ASAA9680253 1 19961112 A 3350 41B004AD07G3 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 967AS 49103 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 1 TO 7 WERE FOUND INOPERATIVE. REPLACED THE BAT TERIES AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1996121200885 19961212 00885 WP 1996 12 12 ASAA9680251 1 19961110 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 973AS 14612 53449 PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996121200886 19961212 00886 WP 1996 12 12 ASAA9680250 1 19961110 A 3350 014597101 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 944AS 53019 SEA - DURING MAINTENANCE CHECK, THE FORWARD OVERWING EMERGENCY EXIT LGHTS WERE FOUND INOPERATIVE. REPLACED THE BATTERIE S AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996121200887 19961212 00887 WP 1996 12 12 ASAA9680247 1 19961105 A 3350 0105601003PA54 LIGHT DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 53016 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. REPLACED SECTION OF FLOOR TRACK LIGHTS AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996121200888 19961212 00888 NM 1996 12 12 ASAA9640097 1 19961108 A 3397 WIRE BOEING 737 7374S3 1384711 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 786AS 24795 SEA - DURING MAINTENANE CHECK, THE EMERGNECY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE IN THE MID CABIN AND THE AF T TWO RED LIGHTS WERE FOUND INOPERATIVE. REPAIRED BROKEN WIRING AT ROW 15 SIDEWALL AND AT THE AFT SECTION OF TRACK. (M ) 2 L 7 2 4F RT A16WE 1996121200889 19961212 00889 NM 1996 12 12 ASAA9640096 1 19961106 A 3350 S417N50914 LIGHT BOEING 737 7374Q8 NM CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 773AS 25106 OAK - FLT 445 - CREW REPORTED THAT THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE KICKED OFF AT ROWS 15 AND 16. REPLACED LI GHT RECEPTACLE AND RECONNECTED WIRING AT ROW 15 AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996121200890 19961212 00890 NM 1996 12 12 ASAA9640095 1 19961106 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 772AS 25105 SEA - DURING MAINTENANCE CHECK, THE TWO FORWARD MOST EMERGNCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REC ONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996121200891 19961212 00891 NM 1996 12 12 ASAA9610142 1 19961110 A 3350 8821004 BATTERY PACK BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTING AT ROWS 10-11 WOULD NOT EXTINGUISH. REPLACED RE CEIVER AND BATTERY PACK, LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1996121200892 19961212 00892 NM 1996 12 12 96ZZZM1560 1 19961110 A 3350 883200312 RECEIVER BOEING 737 737290C 138448V NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTING AT ROWS 10-11 WOULD NOT EXTINGUISH. REPLACED RE CEIVER AND BATTERY PACK, LIGHTS OPERATED NORMALLY. REFERENCE ASAA9610142. 2 L 7 2 4F A16WE 1996121200893 19961212 00893 NM 1996 12 12 AWXA9600731 1 19961124 A 5320 WEB BOEING 737 7373G7 1384595 NM BS 1016-1032 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 DURING ROUTINE MAINTENANCE CHECK, FOUND PRESSURE WEB BS 1016 TO 1032, RBL O TO 38, WL 208 CORRODED OUT OF LIMITS. REMOV ED, FABRICATED AND INSTALLED WEB PER SRM 51-40-02, 51-70-13 AND PSR 009. 2 L 7 2 4F RT A16WE 1996121200894 19961212 00894 NM 1996 12 12 AWXA9600732 1 19961127 A 5320 69686602 SILL BOEING 737 7373G7 1384595 NM BS 913 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON MOPSILL BS 913 TO 1006, RBL 55, WL 208. REMOVED DISCREPENT MOPSILL AND INSTALLED REPLACEMENT MOPSILL (P/N 69-68660-2), TSW, SRM 51-30-01 AND 51-40-02. 2 L 7 2 4F RT A16WE 1996121200895 19961212 00895 NM 1996 12 12 AWXA9600733 1 19961125 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 967 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 DURING ROUTINE MAINTENANCE CHECK, FOUND FLOORBEAM BS 967, WL 208, LBL 44 TO 55 CORRODED. INSTALLED REPLACEMENT T-CAP ON FLOORBEAM AND FASTENERS FROM BS 967, WL 208, LBL 44 TO 55 PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 1996121200896 19961212 00896 NM 1996 12 12 AWXA9600734 1 19961125 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 986.5 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOORBEAM RBL 55 TO LBL 55, WL 208, BS 986.5. REMOVED, FABRICATED UPPER CHORD AND INSTALLED PER SRM 51-41-02 AND ER 3-53-16-15. 2 L 7 2 4F RT A16WE 1996121200897 19961212 00897 NM 1996 12 12 AWXA9600735 1 19961127 A 5320 WEB BOEING 737 7373G7 1384595 NM BS 520 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 308AW 24710 DURING ROUTINE MAINTENANCE CHECK, FOUND CRACK AT THE AFT SIDE OF THE VERTICAL WEB IN THE UPPER CHORD RADIUS ON BS 520, R BL 24.75, WL 207.5. REPAIRED PER RHD 4040, ER 3-53-14-06 AND 81103. 2 L 7 2 4F RT A16WE 1996121200898 19961212 00898 WP 1996 12 12 CALA9601777 1 19961124 A 5230 FITTING DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17531 45847 INSPECTION FOUND A .5 INCH CRACK IN AFT CARGO DOOR BEAM NR 3 FORWARD END FITTING. A NEW FITTING WAS INSTALLED IAW SRM 5 1-30-0. 2 L 7 2 4F A6WE 1996121200899 19961212 00899 WP 1996 12 12 CALA9601778 1 19961126 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 965 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17531 45847 INSPECTION FOUND A 1 INCH CRACK IN LONGERON 17L AT STA 965. A LONGERON REPAIR WAS INSTALLED IAW SRM 53-02, FIGURE 2A. 2 L 7 2 4F A6WE 1996121200900 19961212 00900 NM 1996 12 12 CALA9601779 1 19961123 A 5754 RIB BOEING 727 727224 1384076 NM NR 8 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79746 22449 INSPECTION FOUND A .5 INCH CRACK IN RT WING NR 8 SLAT RIB, JUST INBOARD OF ANTI-ICE DUCT. THE CRACK WAS ROUTED OUT AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-50-3, FIGURE 9. 2 L 7 3 4F A3WE 1996121200901 19961212 00901 NM 1996 12 12 CALA9601780 1 19961123 A 5720 WEB BOEING 727 727224 1384076 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79746 22449 INSPECTION FOUND A 1 INCH CRACK IN RT WING FALSE SPAR WEB LOWER AREA, JUST INBOARD OF NR 5 FLAP TRACK. THE CRACKED AREA OF WEB WAS CUT OUT, A WEB REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1996121200902 19961212 00902 NM 1996 12 12 CALA9601781 1 19961123 A 3350 900835A BATTERY PACK BOEING 727 727224 1384076 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 79746 22449 INSPECTION FOUND THE SECOND FROM FRONT AISLE CEILING EMERGENCY LIGHT INOPERATIVE. THE BATTERY PACK WAS REMOVED, SERVICED AND REINSTALLED. 2 L 7 3 4F A3WE 1996121200903 19961212 00903 NM 1996 12 12 CALA9601782 1 19961123 A 3350 BATTERY PACK BOEING 727 727224 1384076 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 79746 22449 INSPECTION FOUND THE AFT AISLE FLOOR EMERGENCY LIGHT BETWEEN REAR LAVATORIES INOPERATIVE. THE BATTERY PACK WAS REMOVED, SERVICED AND REINSTALLED. 2 L 7 3 4F A3WE 1996121200904 19961212 00904 WP 1996 12 12 CALA9601783 1 19961120 A 5542 SKIN DOUG DC9 DC932 3022066 WP RUDDER CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10556 47423 INSPECTION FOUND CORROSION BETWEEN RUDDER SKIN AND BONDED DOUBLERS ON LT SIDE AT STA ZR 111. THE SKIN WAS SPLICED TO PR ODUCTION SPLICE, A LOWER LEFT SKIN SECTION WAS FABRICATED AND INSTALLED IAW ECRA 5540-01070, SRM 55-03 FIGURE 12 AND SRM 55-40-1. 2 L 7 2 4F A6WE 1996121200905 19961212 00905 NM 1996 12 12 9626122297 1 19961208 A 3260 POSITION SWITCH BOEING 727 727251 138408H NM NLG MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 01 297US 21789 AFTER TAKEOFF, RECEIVED NOSE GEAR RED AND GREEN LIGHT INDICATION, FLICKERED SEVERAL TIMES AND THEN STAYED ON. AIRCRAFT WAS DIVERTED FOR MAINTENANCE TO MSP AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING POSITION SWITCH AND REPAIRED WIR E AT CONNECTOR. OPERATION AND INDICATION WERE NORMAL. 2 L 7 3 4F A3WE 1996121200906 19961212 00906 NM 1996 12 12 9626132706 1 19961207 A 3350 BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 815EA 22552 FORWARD EXIT SIGN EMERGENCY LIGHT FLASHES DURING TEST. REPLACED POWER SUPPLY AND BATTERY PACK. 2 L 7 3 4F A3WE 1996121200907 19961212 00907 1996 12 12 9626149981 4 19961207 A 2565 113317 SLIDE DOUG DC9 DC931 3022065 WP SERVICE DOOR LOW BATTERY A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 994Z 59918 814 47097 DURING PERIODIC CHECK, FORWARD SERVICE DOOR EVACUATION SLIDE FAILED BATTERY TEST. REPLACED SLIDE. 2 L 7 2 4F A6WE 1996121200908 19961212 00908 WP 1996 12 12 9626159966 1 19961210 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9330 47138 SEVERAL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE DURING FAA GROUND INSPECTION. REPLACED BATTERIES TO FORWARD CABIN OVERHEAD EMERGENCY LIGHTS, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996121200909 19961212 00909 WP 1996 12 12 9626169969 1 19961208 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9333 47246 DURING LINE MAINTENANCE INSPECTION, FOUND OVERWING EMERGENCY EXIT LIGHTS AT ROW 11 VERY WEAK. REPLACED BATTERIES, OPERA TIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996121200910 19961212 00910 WP 1996 12 12 9626179981 1 19961207 A 3350 6011779 BATTERY PACK DOUG DC9 DC931 3022065 WP RT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 994Z 47097 DURING PERIODIC CHECK, THE RIGHT NACELLE EMERGENCY LIGHT FAILED TEN MINUTE TEST. REPLACED BATTERY PACK, OPERATIONAL CHE CK NORMAL. 2 L 7 2 4F A6WE 1996121200911 19961212 00911 WP 1996 12 12 9626189990 1 19961208 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8950E 47186 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES. 2 L 7 2 4F A6WE 1996121200912 19961212 00912 WP 1996 12 12 9626199991 1 19961208 A 3320 SIDEWALL LIGHTS DOUG DC9 DC931 3022065 WP CABIN SMOKING A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 01 8957E 47215 EN ROUTE, PASSENGER REPORTED SMOKE COMING FROM SIDEWALL LIGHTS AT ROW 9 ON LEFT SIDE. FLIGHT CONTINUED TO DESTINATION A ND LANDED WITHOUT INCIDENT. MAINTENANCE DEFERRED SIDEWALL LIGHTS PER MEL 33-2. SUSPECT BAD BALLAST. 2 L 7 2 4F A6WE 1996121200913 19961212 00913 WP 1996 12 12 9626209975 1 19961209 A 2780 T-DUCT DOUG DC9 DC931 3022065 WP RT WING SLAT FAILED A A NWAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 01 9339 47382 DURING APPROACH, SLAT DISAGREEMENT LIGHT ILLUMINATED WITH NO BLUE SLAT EXTEND LIGHT. AIRCRAFT APPEARED TO ROLL SLIGHTLY TO THE LEFT. CREW EXECUTED GO-AROUND PROCEDURES, AN UNEVENTFUL LANDING WAS ACCOMPLISHED WITH FLAPS AT 40 DEGREES AND N O SLATS. MAINTENANCE REPLACED RIGHT WING SLAT T-DUCT AND INSTALLED MISSING BUSHINGS ON OUTBOARD SIDE OF FRONT SPAR WING SUPPORTS, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996121200914 19961212 00914 SO 1996 12 12 COMA9610358 1 19961209 A 5312 12002574001 BULKHEAD EMB 120 EMB120RT SO FWD FUSELAGE DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 168CA 120168 DETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: FWD PRESSURE BULKHEAD DAMGED. PERFORMED R EPAIR IAW COMAIR ENGINEERING 53-012. 2 L 7 2 4T RT A31SO 1996121200915 19961212 00915 SO 1996 12 12 COMA9610359 1 19961209 A 5330 12026335041 SKIN EMB 120 EMB120RT SO FWD FUSELAGE DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 168CA 120168 DETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: FWD LOWER SKIN PANEL JUST AFT OF THE NLG D AMGED. PERFORMED REPAIR IAW COMAIR ENGINEERING ORDER 53-012. 2 L 7 2 4T RT A31SO 1996121200916 19961212 00916 SO 1996 12 12 COMA9610360 1 19961209 A 5330 12019269001 SKIN EMB 120 EMB120RT SO BS 9964.5-13056 DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 168CA 120168 DETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: FUSELAGE CENTER SECTION II, LOWER SKIN PAN EL FROM FS 9964.5 TO FS 13056.0 DAMAGED. REMOVED AND REPLACED SKIN IAW ENGINEERING ORDER 53-012. 2 L 7 2 4T RT A31SO 1996121200917 19961212 00917 SO 1996 12 12 COMA9610361 1 19961209 A 5413 12041440002 STRINGER EMB 120 EMB120RT SO RT NACELLE DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 168CA 120168 DETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: RIGHT NACELLE INBD STRINGER NR 1 DAMAGED. REMOVED AND REPLACED STRINGER IAW EMBRAER DOCUMENTS EDU-014/96 AND EST-420-96. 2 L 7 2 4T RT A31SO 1996121200918 19961212 00918 SO 1996 12 12 COMA9610362 1 19961209 A 5414 12001400013 SKIN EMB 120 EMB120RT SO LT/RT NACELLE DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 168CA 120168 DETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: LEFT AND RIGHT NACELLE LOWER SKINS DAMAGED . REMOVED AND REPLACED LT AND RT NACELLE LOWER SKINS IAW COMAIR ENGINEERING ORDER 54-005. 2 L 7 2 4T RT A31SO 1996121200919 19961212 00919 SO 1996 12 12 COMA9610363 1 19961209 A 5411 12042266002 FRAME EMB 120 EMB120RT SO LT/RT NACELLE DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 168CA 120168 DETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: LEFT AND RIGHT NACELLE FRAME 10 WEB, INBD AND OUTBD SIDES DAMAGED. PERFORMED REPAIRS IAW COMAIR ENGINEERING ORDER 54-005. 2 L 7 2 4T RT A31SO 1996121200920 19961212 00920 SO 1996 12 12 COMA9610364 1 19961209 A 5720 12023738001 AUX SPAR WEB EMB 120 EMB120RT SO CTR WING DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 168CA 120168 DETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: WING AUXILIARY SPAR WEB LT AND RT DAMAGED. PERFORMED REPAIR IAW EMBRAER ENGINEERING DRAWING 120-44623. 2 L 7 2 4T RT A31SO 1996121200921 19961212 00921 SO 1996 12 12 COMA9610365 1 19961209 A 5720 12016045001 AUX SPAR CAP EMB 120 EMB120RT SO CTR WING DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 168CA 120168 DETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: WING AUXILIARY SPAR CAPS, LOWER LT AND RT DAMAGED. PERFORMED REPAIR IAW EMBRAER ENGINEERING DRAWING 120-44623. 2 L 7 2 4T RT A31SO 1996121200922 19961212 00922 SO 1996 12 12 COMA9610366 1 19961209 A 5711 12016812001 SPAR WEB EMB 120 EMB120RT SO CTR WING DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 168CA 120168 DETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: WING FRONT SPAR WEB LT AND RT DAMAGED. PE RFORMED REPAIRS IAW EMBRAER ENGINEERING DRAWING 120-44623. 2 L 7 2 4T RT A31SO 1996121200923 19961212 00923 SO 1996 12 12 COMA9610367 1 19961209 A 5711 12016806001 SPAR CAP EMB 120 EMB120RT SO CTR WING DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 168CA 120168 DETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: WING FRONT SPAR CAPS, LOWER LT AND RT DAMA GED. PERFORMED REPAIRS IAW EMBRAER ENGINEERING DRAWING 120-44623. 2 L 7 2 4T RT A31SO 1996121200924 19961212 00924 SO 1996 12 12 COMA9610368 1 19961209 A 5712 12017510003 RIB EMB 120 EMB120RT SO CENTER WING DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 168CA 120168 DETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: WING RIB NR 1, CL RIB DAMAGED. REMOVED AN D REPLACED IAW EMBRAER ENGINEERING DRAWING 120-44623. 2 L 7 2 4T RT A31SO 1996121200925 19961212 00925 SO 1996 12 12 COMA9610369 1 19961209 A 5730 12033270001 SKIN EMB 120 EMB120RT SO CTR WING DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 168CA 120168 DETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: WING LOWER SKIN NR 1 LEFT AND RIGHT DAMAGE D. PERFORMED REPAIRS IAW EMBRAER ENGINEERING DRAWING 120-44623. 2 L 7 2 4T RT A31SO 1996121200926 19961212 00926 SO 1996 12 12 COMA9610370 1 19961209 A 5730 12015668001 SKIN EMB 120 EMB120RT SO CTR WING DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 168CA 120168 DETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: WING LOWER SKIN NR 2 LEFT AND RIGHT DAMAGE D. PERFORMED REPAIRS IAW EMBRAER ENGINEERING DRAWING 120-44623. 2 L 7 2 4T RT A31SO 1996121200927 19961212 00927 SO 1996 12 12 COMA9610371 1 19961209 A 5220 12027451005 SUPPORT EMB 120 EMB120RT SO RT EMER EXIT LOOSE A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 168CA 120168 INSPECTION REVEALED THE AFT RIGHT EMERGENCY EXIT MECHANISM BELLCRANK SUPPORT MOUNTING RIVETS, THROUGH DOOR SKIN TO BE LO OSE CAUSING EXCESSIVE PLAY IN THE DOOR OPENING MECHANISM. THE RIVETS WERE REPLACED PER EMB120 SRM STANDARD PRACTICES, C HAPTER 51, NO OTHER DEFECTS FOUND. 2 L 7 2 4T RT A31SO 1996121200928 19961212 00928 SO 1996 12 12 COMA9610372 1 19961209 A 5320 12005805003 BUTT STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 168CA 120168 INSPECTION REVEALED THE FUSELAGE FWD FLOOR SUPPORT CENTER BUTT-STRAP CORRODED. THE BUTT STRAP WAS REPLACED WITH A NEW P ART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51. 2 L 7 2 4T RT A31SO 1996121200929 19961212 00929 SO 1996 12 12 COMA9610373 1 19961209 A 5320 12004149002 CROSSBEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 168CA 120168 INSPECTION REVEALED THE FUSELAGE FLOOR SUPPORT CROSSBEAM AT FRAME 16 CORRODED. THE CROSSBEAM WAS REPLACED WITH A NEW PA RT PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51. 2 L 7 2 4T RT A31SO 1996121200930 19961212 00930 SO 1996 12 12 COMA9610374 1 19961209 A 5320 12013138001 SUPPORT EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 168CA 120168 INSPECTION REVEALED THE FUSELAGE CENTER SECTION AFT LT SIDEWALL SEAT TRACK SUPPORT CORRODED. THE SUPPORT WAS REPLACED P ER EMB120 SRM STANDARD PRACTICES, CHAPTER 51. 2 L 7 2 4T RT A31SO 1996121200931 19961212 00931 SO 1996 12 12 COMA610375 1 19961209 A 5320 12013135001 SUPPORT EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 168CA 120168 INSPECTION REVEALED THE FUSELAGE CENTER SECTION RT SIDEWALL SEAT TRACK SUPPORT CORRODED. THE SUPPORT WAS REPLACED WITH A NEW PART PER EMB120SRM STANDARD PRACTICES, CHAPTER 51. 2 L 7 2 4T RT A31SO 1996121200932 19961212 00932 SO 1996 12 12 COMA9610376 1 19961209 A 5320 12013134001 SUPPORT EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 168CA 120168 INSPECTION REVEALED THE FUSELAGE CENTER SECTION LT SIDEWALL SEAT TRACK SUPPORT CORRODED. THE SUPPORT WAS REPLACED WITH A NEW PART PER EMB 120 SRM STANDARD PRACTICES, CHAPTER 51. 2 L 7 2 4T RT A31SO 1996121200933 19961212 00933 SO 1996 12 12 COMA9610377 1 19961209 A 5320 12013136001 SUPPORT EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 168CA 120168 INSPECTION REVEALED THE FUSELAGE FWD LT SIDEWALL SEAT TRACK SUPPORT CORRODED. THE SUPPORT WAS REPLACED WITH A NEW PART PER EMB 120 SRM PRACTICES, CHAPTER 51. 2 L 7 2 4T RT A31SO 1996121200934 19961212 00934 SO 1996 12 12 COMA9610378 1 19961209 A 5330 12027879001 SKIN EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 168CA 120168 INSPECTION REVEALED THE LOWER FUSELAGE SKIN CORRODED BENEATH THE NR 2 COM ANTENNA. THE SKIN WAS REPAIRED PER AERODESIGN REPORT NR 2089-1 REV IR, DATED 11-7-96. 2 L 7 2 4T RT A31SO 1996121200935 19961212 00935 SO 1996 12 12 COMA9610379 1 19961209 A 5313 12006173003 STRINGER EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 168CA 120168 INSPECTION REVEALED THE FUSELAGE FWD SECTION OF STRINGER 18L CORRODED. THE STRINGER WAS REPAIRED PER AERODESIGN REPORT NR 1990-A, REV IR, DATED 11-6-96. 2 L 7 2 4T RT A31SO 1996121200936 19961212 00936 SO 1996 12 12 COMA9610380 1 19961209 A 5320 12006962001 SUPPORT EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 168CA 120168 INSPECTION REVEALED THE FUSELAGE FWD FLOOR SUPPORT T-SECTION, AT FRAME 16 CORRODED. THE T-SECTION WAS REPLACED WITH A N EW PART PER EMB 120 SRM STANDARD PRACTICES, CHAPTER 51. 2 L 7 2 4T RT A31SO 1996121200937 19961212 00937 SO 1996 12 12 COMA9610381 1 19961209 A 5320 12005803001 SILL EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 168CA 120168 INSPECTION REVEALED THE FUSELAGE FWD FLOOR SUPPORT RT SILL CORRODED. THE RT SILL WAS REPLACED WITH A NEW PART PER EMB 1 20 SRM STANDARD PRACTICES, CHAPTER 51. 2 L 7 2 4T RT A31SO 1996121200938 19961212 00938 SO 1996 12 12 COMA9610382 1 19961209 A 5320 12005806003 BUTT STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 168CA 120168 INSPECTION REVEALED THE FUSELAGE FWD FLOOR SUPPORT RT BUTT STRAP CORRODED. THE BUTT STRAP WAS REPLACED WITH A NEW PART PER EMB 120 SRM STANDARD PRACTICES, CHAPTER 51. 2 L 7 2 4T RT A31SO 1996121200939 19961212 00939 SO 1996 12 12 COMA9610383 1 19961209 A 5320 12007089003 BUTT STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 168CA 120168 INSPECTION REVEALED THE FUSELAGE FWD FLOOR SUPPORT CENTER BUTT STRAP CORRODED. THE BUTT STRAP WAS REPLACED WITH A NEW P ART PER EMB 120 SRM STANDARD PRACTICES, CHAPTER 51. 2 L 7 2 4T RT A31SO 1996121200940 19961212 00940 SO 1996 12 12 COMA9610384 1 19961209 A 5320 12026671001 BUTT STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 168CA 120168 INSPECTION REVEALED THE FUSELAGE FWD FLOOR SUPPORT LT BUTT STRAP TO BE CORRODED. THE BUTT STRAP WAS REPLACED PER EMB 12 0 SRM STANDARD PRACTICES, CHAPTER 51. 2 L 7 2 4T RT A31SO 1996121200941 19961212 00941 SO 1996 12 12 COMA9610385 1 19961209 A 5320 12034416001 BRACKET EMB 120 EMB120RT SO FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 168CA 120168 INSPECTION REVEALED THE LEFT FWD FUSELAGE SKIN SUPPORT BRACKET, AT FRAME 9 TO BE CRACKED. THE BRACKET WAS REPLACED PER AERODESIGN REPORT 660-1. 2 L 7 2 4T RT A31SO 1996121200942 19961212 00942 SO 1996 12 12 COMA9610386 1 19961209 A 5730 12015354001 SKIN EMB 120 EMB120RT SO LT WING MISDRILLED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 168CA 120168 DURING COMPLIANCE OF S/B 120-57-0031, ONE FASTENER HOLE IN THE LEFT WING UPPER SKIN WAS MISDRILLED AT RIB 18. THE HOLE WAS REPAIRED PER EMBRAER DOCUMENT EST 430/96. 2 L 7 2 4T RT A31SO 1996121200943 19961212 00943 SO 1996 12 12 COMA9610387 1 19961209 A 5320 12039724001 SILL EMB 120 EMB120RT SO EMERGENCY EXIT CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 168CA 120168 INSPECTION REVEALED SEVERE CORROSION ON THE FUSELAGE RIGHT AFT EMERGENCY EXIT CUTOUT LOWER SILL. THE SILL WAS REPLACED WITH A NEW PART PER EMB 120 SRM STANDARD PRACTICES CHAPTER 51. 2 L 7 2 4T RT A31SO 1996121200944 19961212 00944 SO 1996 12 12 COMA9610388 1 19961209 A 5730 12015354001 SKIN EMB 120 EMB120RT SO LT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 168CA 120168 DURING 20K LANDING INSPECTION, FOUND ONE FASTENER HOLE CRACK INDICATION ON LEFT WING UPPER SKIN AT RIB NR 11. HOLE WAS REPAIRED PER EMBRAER DOCUMENT EST431/96. 2 L 7 2 4T RT A31SO 1996121200945 19961212 00945 NM 1996 12 12 96FDEA01700 1 19961211 A 5330 SKIN BOEING 727 72725C 138400H NM BS 870 OVERSIZED HOLE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 117FE 19299 NR 1653 STRINGER 9L FASTENER HOLE IN FUSELAGE SKIN IS OVERSIZED AT STA 870 WING TO FUSE TERMINAL PIN CASTING. INSTALLED FREEZE PLUG AND DOUBLER PER EA 7-5330-28947A. 2 L 7 3 4F A3WE 1996121200946 19961212 00946 NM 1996 12 12 96FDEA01701 1 19961211 A 5711 SPAR WEB BOEING 727 72725C 138400H NM RT WING MIS-MANUFACTURED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 117FE 19299 NR 1663 RT WING, FRONT SPAR WEB MILLED BEYOND DRAWING 65C29064 SPECIFICATIONS. FABRICATED NEW SPLICES AND INSTALLED SPI CES PER EA 7-5710-28952DATED 12/10/96 AND ACCOMPLISHED REMAINING EA 7-5710-28952 DTD 12/10/96 INSTRUCTIONS. 2 L 7 3 4F A3WE 1996121200947 19961212 00947 WP 1996 12 12 ABXA9600679 1 19961206 A 2761 MP701DC8 CIRCUIT BREAKER DOUG DC9 DC932 3022066 WP SPOILER DEFECTIVE A ABXA B A EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 23 984AX 47258 THERE WAS A STRONG SMELL IN THE COCKPIT, FOLLOWED BY SMOKE COMING FROM UNDERNEATH THE RADAR. AIRCRAFT MADE AN EMERGENCY LANDING AT MSY. FOUND THE AUTO SPOILER ACTUATOR OVERHEATED AND 115 VAC, 5 AMP CIRCUIT BREAKER DEFECTIVE. REPLACED THE DEFECTIVE CIRCUIT BREAKER AND REPAIRED A BROKEN WIRE G517A24N AT P1-127, PIN NR 2, OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996121200948 19961212 00948 NM 1996 12 12 SCNA96431 1 19961205 A 3260 SWITCH WIRE BOEING 727 7272A1 138407F NM NLG FAILED A SCNA K NONE N FALSE WARNING CL CLIMB 1 GL 15 286SC 21601 ON RETRACTION, NOSE GEAR DISAGREE LIGHT REMAINED ON WITH ALL OTHER INDICATIONS NORMAL. LIGHT EXTINGUISHED WHEN GEAR CYC LED DOWN. FOUND WIRE-C BROKEN AT S96 NOSE LANDING GEAR LOCK SWITCH. REPAIRED WIRE, OPS CHECKED GOOD IN ACCORDANCE WITH 32-60-2. 2 L 7 3 4F A3WE 1996121200949 19961212 00949 WP 1996 12 12 SCNA96432 1 19961206 A 2611 SMOKE DETECTOR DOUG DC10 DC1010 3022110 WP LAVATORY INOPERATIVE A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 LAV 7 SMOKE DETECTOR LIGHT INOP. RESECURED WIRES TO LIGHT SOCKET AND OPS TESTED NORMAL. 2 L 7 3 4F A22WE 1996121200950 19961212 00950 NM 1996 12 12 SCNA96433 1 19961208 A 5210 DOOR BOEING 727 727225 1384077 NM R1 DOOR NOT SECURED A SCNA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 GL 15 282SC 22558 R1 DOOR OPENED AFTER TAKEOFF. DUMPED APPROXIMATELY 4,000 POUNDS OF FUEL AND RETURNED, HAD SAFE AND NORMAL INDICATION ON TAXI. CHECKED DOOR OPERATION, ACTUATORS, LOCKS AND INDICATORS, ALL OK FOR SERVICE. 2 L 7 3 4F A3WE 1996121200951 19961212 00951 WP 1996 12 12 CKSA96325 1 19961208 A 5240 57641071 DOOR DOUG DC8 DC861 3021952 WP NR 1 NACELLE DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 DURING SEVERE TURBULENCE INSPECTION FOUND: NR 1 ENGINE LEFT UPPER NACELLE DOOR DAMAGED. INSTALLED NEW DOOR PER MM 71-1 0-0, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 81780. 2 L 7 4 4F 4A25 1996121200952 19961212 00952 WP 1996 12 12 CKSA96326 1 19961208 A 5240 57641072 DOOR DOUG DC8 DC861 3021952 WP NR 1 NACELLE CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 DURING SEVERE TURBULENCE INSPECTION FOUND: NR 1 ENGINE RIGHT UPPER NACELLE DOOR CRACKED AND DENTED. INSTALLED NEW DOOR PER MM 71-10-0, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 81784. 2 L 7 4 4F 4A25 1996121200953 19961212 00953 WP 1996 12 12 CKSA96327 1 19961208 A 5414 5765900515 SKIN DOUG DC8 DC861 3021952 WP NR 2 PYLON DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 DURING SEVERE TURBULENCE INSPECTION FOUND: HOLE IN NR 2 PYLON INBOARD SIDE ABOVE ENGINE EXHAUST. REPAIRED HOLE IAW DC- 8 SRM 54-2-1 FIGURE 7, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 81792. 2 L 7 4 4F 4A25 1996121200954 19961212 00954 WP 1996 12 12 CKSA96328 1 19961208 A 5414 5765900515 SKIN DOUG DC8 DC861 3021952 WP NR 2 PYLON DENTED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 DURING SEVERE TURBULENCE INSPECTION FOUND: DENT IN NR 2 PYLON INBOARD SIDE ABOVE ENGINE EXHAUST. REPAIRED DENT IAW DC- 8 SRM 54-2-1 FIGURE 7, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 81793. 2 L 7 4 4F 4A25 1996121200955 19961212 00955 WP 1996 12 12 CKSA96329 1 19961208 A 5751 5705321511 SKIN DOUG DC8 DC861 3021952 WP LT AILERON CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 DURING SEVERE TURBULENCE INSPECTION FOUND: LEFT INBOARD AILERON LOWER SURFACE CRACKED APPROXIMATELY .5 INCH LONG. REPA IRED PER DC-8 SRM 57-2-0 AND 57-2-1. TREATED AND PRIMED PER 51-1-8, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 818 16. 2 L 7 4 4F 4A25 1996121200956 19961212 00956 WP 1996 12 12 CKSA96330 1 19961208 A 5754 57699852 DOOR DOUG DC8 DC861 3021952 WP LT LE SLAT MISSING A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 DURING SEVERE TURBULENCE INSPECTION FOUND: LEFT HAND INBOARD SLOT DOOR LEADING EDGE MISSING. REPAIR DONE ON RO#230452 INSTALLED IAW DC-8 SRM 51-1-20D AND 51-3-0, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 81809. 2 L 7 4 4F 4A25 1996121200957 19961212 00957 WP 1996 12 12 CKSA96331 1 19961208 A 5414 SKIN DOUG DC8 DC861 3021952 WP NR 2 PYLON DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 DURING SEVERE TURBULENCE INSPECTION FOUND: NR 2 PYLON DAMAGED INBOARD SIDE UPPER STATION YIP.230 APPROXIMATELY 1 HOLE. REPAIRED INBOARD PYLON INBOARD SIDE SKIN IAW DC-8 SRM 54-2-1 FIGURE 7, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 81996. 2 L 7 4 4F 4A25 1996121200958 19961212 00958 WP 1996 12 12 CKSA96332 1 19961208 A 5754 57695871 DOOR DOUG DC8 DC861 3021952 WP LT LT SLAT DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 DURING SEVERE TURBULENCE INSPECTION FOUND: LEFT HAND OUTBOARD SLOT DOOR DAMAGED. REMOVED AND REPLACED LEFT HAND OUTBOA RD SLOT DOOR IAW DC-8 MM 27-41-2, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 81805. 2 L 7 4 4F 4A25 1996121200959 19961212 00959 WP 1996 12 12 CKSA96333 1 19961208 A 5753 5642970505 RIB DOUG DC8 DC861 3021952 WP LT TE FLAP DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 DURING SEVERE TURBULENCE INSPECTION FOUND: LEFT HAND OUTBOARD FLAP 2ND RIB OUTBOARD OF EXHAUST GATE DAMAGED. REMOVED A ND REPLACED RIB IAW DC-8 SRM 51-1-21, 57-2-5 AND 57-7-1, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 82005. 2 L 7 4 4F 4A25 1996121200960 19961212 00960 WP 1996 12 12 CKSA96334 1 19961208 A 5400 576951564 ANGLE DOUG DC8 DC861 3021952 WP NR 2 PYLON DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 DURING SEVERE TURBULENCE INSPECTION FOUND: NR 2 PYLON INBOARD FORWARD SIDE OF STUB WING HAS TEMPORARY REPAIR ANGLE INST ALLED AT STA YIP.230. REMOVED TEMPORARY ANGLE AND REPLACED ANGLE IAW DC-8 SRM 51-1-20, 51-3-0, 54-3-1 FIGURE 26, DC-8 M IP-1 SECTION 15, NON-ROUTINE TASK CARD NR 82017. 2 L 7 4 4F 4A25 1996121200961 19961212 00961 WP 1996 12 12 CKSA96335 1 19961208 A 5400 57652071 APRON DOUG DC8 DC861 3021952 WP NR 1 PYLON DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 DURING SEVERE TURBULENCE INSPECTION FOUND: NR 1 PYLON APRON FORWARD OUTBOARD SECTION DAMAGED APPROXIMATELY 24L BY 3W. R EPAIRED APRON PER SRM 54-2-1, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 81975. 2 L 7 4 4F 4A25 1996121200962 19961212 00962 WP 1996 12 12 CKSA96336 1 19961208 A 5730 561136017 SKIN DOUG DC8 DC861 3021952 WP WS 140-150 DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 DURING SEVERE TURBULENCE INSPECTION FOUND: LEFT WING UPPER SKIN DAMAGED AT STA 140 TO 150 JUST FORWARD OF CENTER SPAR D ENTS AND HOLE APPROXIMATELY 2 INCHES DIAMETER. REPAIRED LEFT WING UPPER SKIN IAW DC-8 SRM 57-2-1 FIGURE 39, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 81977. 2 L 7 4 4F 4A25 1996121200963 19961212 00963 WP 1996 12 12 CKSA96337 1 19961208 A 5400 5769523143 ANGLE DOUG DC8 DC861 3021952 WP NR 1 PYLON DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 DURING SEVERE TURBULENCE INSPECTION FOUND: NR 1 PYLON INBOARD SIDE AT STA YOP.270 HAS TEMPORARY REPAIR ANGLE INSTALLED. REMOVED AND REPLACED ANGLE IAW DC-8 SRM 51-1-20D, 51-3-0, 54-3-1 FIGURE 31A, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK C ARD NR 82013. 2 L 7 4 4F 4A25 1996121200964 19961212 00964 WP 1996 12 12 CKSA96338 1 19961208 A 5400 5765901501 ANGLE DOUG DC8 DC861 3021952 WP NR 1 PYLON CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 DURING SEVERE TURBULENCE INSPECTION FOUND: NR 1 PYLON INBOARD UPPER SPAR WEB CRACKED AT STA YOP.270 APPROXIMATELY 2 INC HES LONG. REPAIRED NR 1 PYLON UPPER SPAR WEB ANGLE IAW DC-8 SRM 51-1-20D, 51-1-21, 54-2-1 FIGURE 5, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 82011. 2 L 7 4 4F 4A25 1996121200965 19961212 00965 WP 1996 12 12 CKSA96339 1 19961208 A 5414 5765901501 SKIN DOUG DC8 DC861 3021952 WP NR 1 PYLON DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 DURING SEVERE TURBULENCE INSPECTION FOUND: NR 1 PYLON SKIN DAMAGED AT STA YOP.270 INBOARD SIDE, APPROXIMATELY 3 INCH LO NG HOLE. REPAIRED DAMAGED SKIN NR 1 PYLON IAW DC-8 SRM 54-2-1, 51-1-20D, 51-1-21, DC-8 MIP-1 SECTION 15, NON-ROUTINE TA SK CARD NR 82014. 2 L 7 4 4F 4A25 1996121200966 19961212 00966 WP 1996 12 12 CKSA96341 1 19961208 A 5730 57699481 SKIN DOUG DC8 DC861 3021952 WP WING LE CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 DURING SEVERE TURBULENCE INSPECTION FOUND: WING LEADING EDGE LOWER SURFACE AT WING PYLON INTERSECTION CRACKED NR 1. RE PAIRED WING LEADING EDGE SKIN CRACK IAW DC-8 SRM 54-2-1 FIGURE 21, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 82081 . 2 L 7 4 4F 4A25 1996121200967 19961212 00967 WP 1996 12 12 CKSA96342 1 19961208 A 5400 576951563 ANGLE DOUG DC8 DC861 3021952 WP NR 3 PYLON CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 DURING SEVERE TURBULENCE INSPECTION FOUND: NR 3 PYLON INBOARD STUB WING ATTACH ANGLE CRACKED. REPAIRED NR 3 PYLON STUB WING ANGLE IAW DC-8 SRM 54-2-1 FIGURE 19, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 84763. 2 L 7 4 4F 4A25 1996121200968 19961212 00968 WP 1996 12 12 CKSA96343 1 19961208 A 5754 57699331 SKIN DOUG DC8 DC861 3021952 WP LT LE FLAP DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 DURING SEVERE TURBULENCE INSPECTION FOUND: LEFT HAND OUTBOARD SLOT LEADING EDGE DAMAGED. REPAIRED PER SRM 57-2-1 FIGUR E 2H, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 82125. 2 L 7 4 4F 4A25 1996121200969 19961212 00969 WP 1996 12 12 CKSA96344 1 19961208 A 5753 56514111 EXHAUST GATE DOUG DC8 DC861 3021952 WP LT TE FLAP TORN A A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 DURING SEVERE TURBULENCE INSPECTION FOUND: LEFT OUTBOARD FLAP EXHAUST GATE TORN UPPER AND LOWER SURFACE APPROXIMATELY 1 2 INCHES BOTH SIDES. REINSTALLED EXHAUST GATE IAW DC-8 MM 27-51-5, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 8181 8. 2 L 7 4 4F 4A25 1996121200970 19961212 00970 WP 1996 12 12 CKSA96345 1 19961208 A 5754 5769545521 PLATING DOUG DC8 DC861 3021952 WP LE FLAP DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 DURING SEVERE TURBULENCE INSPECTION FOUND: SKIN UNDER OUTBOARD SLOT PANEL DAMAGED APPROXIMATELY 1 HOLE. REMOVED AND RE PLACED PLATING IAW DC-8 SRM 51-1-21, 51-1-20D, 51-3-0, 54-3-1 FIGURE 31A, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD N R 82012. 2 L 7 4 4F 4A25 1996121200971 19961212 00971 WP 1996 12 12 CKSA96346 1 19961208 A 5720 5616894 FITTING DOUG DC8 DC861 3021952 WP WS 98 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 DURING SEVERE TURBULENCE INSPECTION FOUND: LEFT WING TRAILING EDGE FITTING STA 98 CRACKED. REMOVED AND REPLACED LOWER WING TRAILING EDGE FITTING STA 98 IAW SRM 53-01-0, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 82112. 2 L 7 4 4F 4A25 1996121200972 19961212 00972 WP 1996 12 12 CKSA96347 1 19961208 A 5730 56110111 PANEL DOUG DC8 DC861 3021952 WP WS 106 DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 DURING SEVERE TURBULENCE INSPECTION FOUND: LEFT WING LOWER TRAILING EDGE PANEL AT STA 106 HAS HOLE IN IT. REMOVED AND REPLACED LOWER TRAILING EDGE PANEL AT STA 106 IAW SRM 53-01-0, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 82156. 2 L 7 4 4F 4A25 1996121200973 19961212 00973 WP 1996 12 12 CKSA96348 1 19961208 A 5753 5751631 FAIRING DOUG DC8 DC861 3021952 WP WS 98 DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 DURING SEVERE TURBULENCE INSPECTION FOUND: FLAP FAIRING TRAILING EDGE PANEL STA 98 LOWER LEFT WING DAMAGED. REMOVED AN D REPLACED FLAP FAIRING TRAILING EDGE PANEL STA 98 LOWER WING IAW SRM 51-1-21, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK C ARD NR 82111. 2 L 7 4 4F 4A25 1996121200974 19961212 00974 WP 1996 12 12 CKSA96349 1 19961208 A 5754 57695811 DOOR DOUG DC8 DC861 3021952 WP LT FLAP DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 DURING SEVERE TURBULENCE INSPECTION FOUND: LEFT HAND INBOARD SLOT DOOR DAMAGED. REMOVED AND REPLACED LEFT HAND WING IN BOARD SLOT DOOR IAW DMM 27-80-1 PAGE 201, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 81808. 2 L 7 4 4F 4A25 1996121200975 19961212 00975 WP 1996 12 12 CKSA96350 1 19961208 A 5240 57629751 DOOR DOUG DC8 DC861 3021952 WP NR 2 NACELLE DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 DURING SEVERE TURBULENCE INSPECTION FOUND: NR 2 ENGINE LEFT FORWARD COWL DOOR DENTED AND HAS SMALL HOLE. REPAIRED SMAL L HOLE AND REMOVED DENT IAW DC-8 SRM 78-2-0, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 81785. 2 L 7 4 4F 4A25 1996121200976 19961212 00976 WP 1996 12 12 CKSA96351 1 19961208 A 5240 57629802 DOOR DOUG DC8 DC861 3021952 WP NR 2 NACELLE DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 DURING SEVERE TURBULENCE INSPECTION FOUND: INBOARD AFT COWL DOOR NR 2 TRAILING EDGE DAMAGED APPROXIMATELY 24 INCHES LON G. PATCHED COWL DOOR TRAILING EDGE IAW DC-8 SRM 78-2-0, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 81974. 2 L 7 4 4F 4A25 1996121200977 19961212 00977 WP 1996 12 12 CKSA96352 1 19961208 A 5711 5597842 SPAR CAP DOUG DC8 DC861 3021952 WP RT WING CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 DURING SEVERE TURBULENCE INSPECTION FOUND: RIGHT WING AFT SPAR LOWER CAP CRACKED AT STA 408 SPLICE. REPAIRED IAW DRAWI NG AIA/E/2285, AIA/E/2342, AIA/E/2343 AND DAC DRAWING NR 5613922. REFERENCE REPORT 96AA-156, DC-8 MIP-1 SECTION 15, NON -ROUTINE TASK CARD NR 82070. 2 L 7 4 4F 4A25 1996121200978 19961212 00978 WP 1996 12 12 CKSA96353 1 19961208 A 5711 5597837 SPAR CAP DOUG DC8 DC861 3021952 WP FWD SPAR CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 DURING SEVERE TURBULENCE INSPECTION FOUND: FORWARD UPPER SPAR CAP CRACKED AT OUTBOARD SPLICE. REPAIRED UPPER SPAR CAP CRACK IAW AIA ENGINEERING SKETCH NR'S AIA/E/2234, AIA/E/2341, AIA/E/2336, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD N R 82126. 2 L 7 4 4F 4A25 1996121200979 19961212 00979 WP 1996 12 12 CKSA96354 1 19961208 A 5711 5597838 SPAR CAP DOUG DC8 DC861 3021952 WP FWD SPAR CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 DURING SEVERE TURBULENCE INSPECTION FOUND: FORWARD LOWER SPAR CAP CRACKED AT OUTBOARD SPLICE. REPAIRED LOWER SPAR CAP CRACK IAW AIA ENGINEERING SKETCH NR'S AIA/E/2335, AIA/E/2337, AIA/E/2340, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD N R 82127. 2 L 7 4 4F 4A25 1996121200980 19961212 00980 WP 1996 12 12 CKSA96355 1 19961208 A 5751 5705321504H SKIN DOUG DC8 DC861 3021952 WP RT AILERON CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 DURING SEVERE TURBULENCE INSPECTION FOUND: RIGHT INBOARD AILERON TRAILING EDGE DENTED AND CRACKED. REPAIRED AILERON TR AILING EDGE IAW DC-8 SRM 57-2-0, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 81824. 2 L 7 4 4F 4A25 1996121200981 19961212 00981 WP 1996 12 12 CKSA96356 1 19961208 A 5754 57707021 SLOT VANE DOUG DC8 DC861 3021952 WP LT LE FLAP DAMAGED A A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 DURING SEVERE TURBULENCE INSPECTION FOUND: LEFT HAND OUTBOARD SLOT VANE TRAILING EDGE DAMAGED. REMOVED AND REPLACED LE FT HAND OUTBOARD SLOT VANE TRAILING EDGE IAW DAC DRAWING NR 5769933, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 821 30. 2 L 7 4 4F 4A25 1996121200982 19961212 00982 WP 1996 12 12 CKSA96357 1 19961208 A 5400 3765200504 PYLON DOUG DC8 DC861 3021952 WP NR 4 DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 DURING SEVERE TURBULENCE INSPECTION FOUND: NR 4 PYLON TO BE REPLACED. INSTALLED NR 4 PYLON IAW DC-8 MM 54-40-0 AND SRM 51-1-20D, 51-3-0 AND DAC DRAWING NR 5765901, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 81964. 2 L 7 4 4F 4A25 1996121200983 19961212 00983 WP 1996 12 12 CKSA96358 1 19961208 A 5753 5642970505 SKIN DOUG DC8 DC861 3021952 WP LT TE FLAP CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 DURING SEVERE TURBULENCE INSPECTION FOUND: LEFT OUTBOARD FLAP UPPER AND LOWER SURFACE CRACKED AND TORN. REMOVED AND RE PLACED TORN SURFACE IAW DC-8 SRM 51-1-21, 57-2-5 AND 57-7-1, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 81817. 2 L 7 4 4F 4A25 1996121200984 19961212 00984 WP 1996 12 12 CKSA96359 1 19961208 A 5753 5642970505 TRAILING EDGE DOUG DC8 DC861 3021952 WP WS 340 DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 DURING SEVERE TURBULENCE INSPECTION FOUND: LEFT OUTBOARD FLAP TRAILING EDGE DAMAGED AT STA 340 APPROXIMATELY 12 INCHES LONG. REPLACED TRAILING EDGE IAW DC-8 SRM 51-1-0, 51-1-21A, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 82006. 2 L 7 4 4F 4A25 1996121200985 19961212 00985 WP 1996 12 12 CKSA96360 1 19961208 A 5753 5642970505 TRAILING EDGE DOUG DC8 DC861 3021952 WP LT TE FLAP DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 DURING SEVERE TURBULENCE INSPECTION FOUND: LEFT OUTBOARD FLAP TRAILING EDGE DAMAGED INBOARD OF EXHAUST GATE. REPAIRED LEFT HAND OUTBOARD TRAILING EDGE IAW DC-8 SRM 57-2-1 FIGURE 25S, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 82008. 2 L 7 4 4F 4A25 1996121200986 19961212 00986 SO 1996 12 12 SRAA961051 1 19961013 A 5320 SUPPORT LKHEED 382 382G 526414U SO BS 295 CORROSION A SRAA K NONE O OTHER IN INSP/MAINT 1 GL 23 905SJ 45318 4472 DURING C-CHECK, FOUND CARGO COMPARTMENT FLOOR PANEL SUPPORT BEAM AT FS 295, LBL 40 HAS CORROSION AT FORWARD SIDE BEYOND LIMITS. CUT OUT CORRODED SECTION, FABRICATED AND INSTALLED FLOORBEAM REPAIR AND 2 STRAPS LAC SRM CHAPTER 51-40-22. 2 H 7 4 4T A1SO 1996121800002 19961218 00002 NE 1996 12 18 P5CA9600969 2 19961124 A 7314 38690113 FUEL PUMP BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE NR 1 ENGINE FAILED A P5CA A E J UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL Y ENGINE STOPPAGE CR CRUISE 1 WP 23 920FT 28733 746 22237 702091 LOST POWER ON NR 1 ENGINE, OIL PRESSURE LIGHT CAME ON, SHUT DOWN ENGINE. FOUND FUEL PUMP FAILED, METAL IN FUEL CONTROL UNIT, NO CONTAMINATION IN ENGINE VANE AND BLEED CONTROL FILTER. REPLACED FUEL PUMP, FUEL CONTROL AND TT2 SENSOR PER BOE ING MAINTENANCE MANUAL 73-21-01, 73-11-01, 73-21-04 AND 71-00-00 TEST 09. 2 L 7 4 4F 4 F A20WE E3NE 1996121800003 19961218 00003 GL 1996 12 18 CA960604020 2 19960510 A 7250 23038160 TURBINE BELL 206 206L 1181522 SW ALLSN 250C 250C20 03013 GL POWER SECTION SEIZED W K NONE O OTHER IN INSP/MAINT 1 CA 3122 1 CAE295239 (CAN)INSTALLED TURBINE ON AIRCRAFT AND COMPLETED A GROUND RUN AND TEST FLIGHT. TURBINE CHECKED OK. A SECOND START WAS AT TEMPTED BUT THERE WAS NO NR UPON REACHING 30 PERCENT N1. ANOTHER START WAS ATTEMPTED,BUT AGAIN THE NR WOULD NOT ROTATE. TURBINE RETURNED TO SHOP. 1 G 7 1 3U 3 U H2SW E4CE 1996121800004 19961218 00004 WP 1996 12 18 HALA96152 1 19961102 A 3397 WIRE DOUG DC10 DC1010 3022110 WP HAMSTD 14SF 14SF23 NE CABIN DISCONNECTED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 148AA 46703 FLT 1038 - HNL - L-3 DOOR EMERGENCY LIGHT WILL NOT TEST. REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY AND RECONNECTED WIRES TO L-3 DOOR. THE OPERATIONAL CHECK WAS OK. (M) 2 L 7 3 4F A22WE 6 C P7NE 1996121800005 19961218 00005 SO 1996 12 18 COMA9610338 1 19961203 A 3010 DEICE BOOTS EMB 120 EMB120RT SO LT/RT WING WORN A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 205CA 120205 LT AND RT WING DEICE BOOTS AND LT AND RT ENGINE INLET DEICE BOOTS FAILED DURING FLIGHT. REPLACED WING AND ENGINE INLET DEICE BOOTS. 2 L 7 2 4T RT A31SO 1996121800007 19961218 00007 EU 1996 12 18 AALA961444 1 19961002 A 5330 SKIN FOKKER F28 F28MK0100 4990807 EU BS 4610-2411 DAMAGED A AALA K NONE C F.O.D. IN INSP/MAINT 1 SW 07 1470K 11506 LIGHTNING STRIKES IN CROWN SKIN OF FUSELAGE. LIGHT TO SEVERE CONDITION; 2 BURN HOLES AND 77 PLUS 'POCK' MARKS. REPAIRE D IAW AARD 53-00-01-2 AND ES0 51000 DTE 10-2-96 RFS 188032 ISSUED TO SCHEDULED INSPECTIONS AND PERMANENT REPAIR REQUIREM ENTS. TST: 6,428.13. CYCLES, 4,440. 2 L 7 2 4F RT 1996121800008 19961218 00008 1996 12 18 ORJA9662 4 19961003 A 2565 D29982107 SLIDE DOUG DC9 DC983 3022083 WP PASSENGER DOOR LOW PRESSURE A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 882RA 1352 49949 REMOVE AND REPLACE PASSENGER DOOR EVACUATION SLIDE DUE TO LOW BOTTLE PRESSURE. REMOVED AND REPLACED PASSENGER DOOR EVAC UATION SLIDE DUE TO LOW BOTTLE PRESSURE. (X) 2 L 7 2 4F RT A6WE 1996121800009 19961218 00009 CE 1996 12 18 NSVA96003 1 19961013 A 3260 727725 CIRCUIT BREAKER KLIXON BEECH 1900 1900C 1154161 CE LANDING GEAR FAILED A NSVA O OTHER P NO WARNING INDICATION LD LANDING 1 EA 27 129CJ 9147 UC129 LANDING GEAR GREEN DOWN AND LOCKED ANNUNCIATORS FAILED TO ILLUMINATE UPON LANDING GEAR EXTENSION. FLIGHT CREW VERIFIED GEAR IN DOWN AND LOCKED POSITION BY VISUAL AND MECHANICAL MEANS. AIRCRAFT SUCCESSFULLY COMPLETED EMERGENCY LANDING. IN SPECTION BY MAINTENANCE PERSONNEL REVEALED LANDING GEAR CIRCUIT BREAKER FAILED IN OPEN POSITION. CIRCUIT BREAKER WAS RE PLACED AND SYSTEM FUNCTIONS NORMAL. (X) 2 L 7 2 4T RT A24CE 1996121800010 19961218 00010 NE 1996 12 18 EIAA9616640 2 19961003 A 7260 MS9388153 SEAL BOEING 747 747SR46 NM PWA JT9 JT9D7F 52054 NE NR 4 ENGINE LEAKING A EIAA O OTHER E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 NM 09 689UP 6275 21033 662970 ANC - NR 4 ENGINE PRECAUTIONARY SHUT DOWN AT FL 331, MACH .84, DUE TO LOW OIL QTY AND FLUCTUATING PRESSURE (30 PSI). UP ON TROUBLESHOOTING, FOUND OIL COMING FROM THE GENERATOR PAD DRAIN LINE. REPLACED THE GENERATOR PAD DRIVE SEAL PER MM. L EAK CHECK AND OPS CHECK WERE OK. (X) 2 L 7 4 4F 4 F A20WE E20EA 1996121800011 19961218 00011 WP 1996 12 18 96ZZZX5944 1 19960927 A 3610 CLAMP DOUG DC9 DC983 3022083 WP TAIL COMPT LOOSE A TWAA K NONE J WARNING INDICATION TO TAKEOFF 1 CE 05 9407R 49400 MCI - FLT 229 - DURING TAKEOFF, THE TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. REPOSITIONED AND TIGHTENED CLA MP AT AUGMENTATION VALVE. HIGH POWER LEAK CHECK ACCOMPLISHED, NO LEAKS NOTED. CHECK C-2D - 6-27-96 - JFK. 2 L 7 2 4F RT A6WE 1996121800012 19961218 00012 EA 1996 12 18 CA960612022 1 19960602 A 6100 GUIDE PINS DHAV DHC6 DHC6300 EA PWA PT6 PT6A27 52043 EA HARTZL HCB3T HCB3TN3 GL BETA RING DRY & DIRTY W C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CA 1523 PCE42733 BU4024 (CAN)ON TAKEOFF, RIGHT HAND PROPELLER DID NOT REACH TAKEOFF RPM. TAKEOFF ABORTED. BETA RING GUIDE PINS FOUND DIRTY AND D RY, CLEANED AND LUBRICATED. 1 H 7 2 3T 4 T A9EA E4EA 6 C P15EA 1996121800014 19961218 00014 EA 1996 12 18 CA960703034 2 19960626 A 7414 1038256011 MAGNETO BENDIX 10385126105 CESSNA 182 R182 2072734 CE LYC O540 O540J3C5 41532 EA MCAULY 2D34C B2D34C214 GL ENGINE INTERNAL WEAR W O OTHER E VIBRATION/BUFFET CR CRUISE 1 CA 1153 L2027840A 790258 (CAN) ENGINE WAS RUNNING ROUGH WITH A LARGE MAG DROP. MAGNETO REPLACED. 1 H 7 1 3O 3 O RT 3A13 E295 5 C P7EA 1996121800015 19961218 00015 EA 1996 12 18 CA960715009 2 19960622 A 8530 E530786 VALVE CESSNA 182 R182 2072734 CE LYC O540 O540J3C5 41532 EA MCAULY 2D34C B2D34C214 GL #3 CYL EXH BURNT W A K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 804 804 L1966340A 7910432 (CAN) DURING INSPECTION IT WAS FOUND THAT THERE WAS NO COMPRESSION ON #3 & #4 CYLINDERS. AFTER DISASSEMBLY IT WAS FOUND THAT THE ROCKER ARMS OF THE EXHAUST AND INTAKE HAD BEEN MISINSTALLED AT OVERHAUL. THE ROCKER ARM FOR THE INTAKE WAS INST ALLED ON THE EXHAUST VALVE AND THE ROCKER ARM FOR THE EXHAUST WAS INSTALLED ON THE INTAKE VALVE. THIS RESULTED IN BURNT EXHAUST VALVES WHICH WERE STUCK IN THE OPEN POSITION. 1 H 7 1 3O 3 O RT 3A13 E295 5 C P7EA 1996121800019 19961218 00019 CE 1996 12 18 CA960212104 1 19960123 A 8011 534757 ENGINE CESSNA 185 A185E 2072818 CE CONT O520 IO520D 17032 SO MCAULY 2A34C D2A34C58 GL START ADAPTER FAILED W K NONE Y ENGINE STOPPAGE IN INSP/MAINT 1 CA 785 785 293138R 701131 (CAN) ENGINE KICKED BACK ON START UP BREAKING THE STARTER ADAPTER. UPON PUTTING THE NEW ADAPTER, THE ENGINE WOULD NOT ST ART. ENGINE REPLACED. 1 H 7 1 3O 3 O 3A24 E5CE 5 C P3EA 1996121800020 19961218 00020 NM 1996 12 18 DL757962662 1 19961207 A 3350 POWER SUPPLY BPS73 BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 681DA 28962 26957 P1326 ESCAPE PATH LIGHT INOP FROM MID GALLEY TO FWD GALLEY. REPLACED POWER SUPPLY. 2 L 7 2 4F 4 F RT A2NM E17NE 1996121800022 19961218 00022 CE 1996 12 18 GLBA96208 1 19961014 A 5320 FRAME BEECH 1900 1900C 1154161 CE CABIN DOORWAY CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 CE 01 141UE UC141 DEN - CABIN DOOR FRAME CRACKED. REPAIRED 1.75 INCH CRACK AT SNUBBER ATTACH POINT. (M) 2 L 7 2 4T RT A24CE 1996121800023 19961218 00023 NM 1996 12 18 EIAA9686 1 19961118 A 5210 65B100034 CRANK ROLLER BOEING 747 747273C 1384896 NM PAX DOOR BROKEN A EIAA O OTHER O OTHER CL CLIMB 1 NM 09 470EV 20653 ANC - CLIMBING THRU FL 10,000 FT A SOFT POPPING SOUND CAME FROM THE CARGO COMPT, A LOUD POPPING SOUND FOLLOWED. JARRIN G OF THE FLT DECK ACCOMP BY 'L ENTRY DOOR 1' LIGHT CAME ON. CABIN PRESS WAS NORM. VISUAL CHK'D, DOOR HANDLE IN LOCKED POSITION. NO AIR LEAKAGE NOTICED. FOUND L1 DOOR, AFT SIDE, UPPR AND LWR LATCH ROLLER CRANK BROKEN. REPLACED BOTH UPPR AND LWR LATCH ROLLER CRANK AND ASSOCIATED HARDWARE. UPPR AND LWR DOOR LATCH TORQUE TUBE HAD TO BE REMOVED AND REPLACED TO INSTALL LATCH ROLLER CRANK. SCRATCHES IND THE 2 ROLLERS WERE NOT PROPERLY ENGAGED AT TOP AFT CORNER. (M) 2 L 7 4 4F A20WE 1996121800024 19961218 00024 1996 12 18 WTAA960191 3 19961111 A 6140 8659566 BETA SWITCH BAG JETSTM JETSTM3101 1500215 EU LT ENGINE FAILED A WTAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 17 428UE 806 LAX - LEFT BETA LIGHT ILLUMINATED ON TAKEOFF. TAKEOFF ABORTED. MAINTENANCE REPLACED LEFT ENGINE BETA LIGHT PRESSURE SW ITCH. OPERATIONAL CHECK SATISFACTORY. (M) 2 L 7 2 4T RT A21EU 1996121800025 19961218 00025 WP 1996 12 18 CKSA96340 1 19961208 A 5400 5769545521 WEB DOUG DC8 DC861 3021952 WP NR 1 PYLON DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 DURING SEVERE TURBULENCE INSPECTION FOUND: NR 1 PYLON INBOARD STUB WING UPPER WEB DAMAGED APPROXIMATELY 2 INCH HOLE. R EMOVED AND REPLACED WEB PLATING IAW DC-8 SRM 51-1-21, 54-3-1 FIGURE 31A, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 82015. 2 L 7 4 4F 4A25 1996121900001 19961219 00001 NM 1996 12 19 TWRA96369 1 19961128 A 3350 58223 BATTERY PACK BOEING 747 747136 1384883 NM CABIN DISCHARGED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 606FF 20273 DURING DAILY CHECK, FOUND B-ZONE EGRESS LIGHT STRIP ON LEFT SIDE INOPERABLE. REPLACED BATTERY PACK PER MM 33-50-00. OP S CHECKED NORMAL. (X) 2 L 7 4 4F A20WE 1996121900002 19961219 00002 NM 1996 12 19 TWRA96368 1 19961128 A 3350 900835A BATTERY PACK BOEING 747 747136 1384883 NM CABIN DISCHARGED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 606FF 301 20273 DURING DAILY CHECK, FOUND U/D EXIT SIGN INOPERABLE. REPLACED BATTERY PACK AND BLOWN FUSE. OPS CHECKED NORMAL PER MM 33 -51-00. (X) 2 L 7 4 4F A20WE 1996121900003 19961219 00003 NM 1996 12 19 TWRA96367 1 19961128 A 3350 900835A BATTERY PACK BOEING 747 747136 1384883 NM CABIN DISCHARGED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 606FF 1910694 20273 DURING DAILY CHECK, FOUND EXIT SIGN BY L1 AND L2 MED INOPERABLE. REMOVED AND REPLACED BATTERY PACK AT L2 AND L2 MED. O PS CHECKED NORMAL PER MM 33-50-00. (X) 2 L 7 4 4F A20WE 1996121900004 19961219 00004 NM 1996 12 19 TWRA96372 1 19961202 A 3350 90083 BATTERY PACK BOEING 747 747282B 1384860 NM CABIN DISCHARGED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 611FF 12731 20502 DURING DAILY CHECK, FOUND EMERGENCY EXIT SIGN ADJACENT TO SEAT 65AC INOPERABLE. REPLACED EXIT SIGN BATTERY PACK. OPS C HECKED NORMAL PER MM 33-51-00. (X) 2 L 7 4 4F A20WE 1996121900005 19961219 00005 NM 1996 12 19 TWRA96373 1 19961129 A 3350 3004183 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 616FF 0592 21939 DURING DAILY CHECK, FOUND L1 MED EVAC BUSTLE LIGHT INOPERABLE. REMOVED AND REPLACED BUSTLE LIGHT PER MM 35-51-06. OPS CHECKED NORMAL. (X) 2 L 7 4 4F A20WE 1996121900006 19961219 00006 NM 1996 12 19 TWRA95370 1 19961129 A 3350 6012111 POWER SUPPLY BOEING 747 747212B 1384886 NM CABIN MALFUNCTION A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 619FF 270 21316 DURING DAILY CHECK, FOUND FORWARD 2 EACH OVERWING EMERGENCY EVAC LIGHTS ARE INOPERATIVE (LEFT BODY FAIRING). (X) 2 L 7 4 4F A20WE 1996121900007 19961219 00007 NM 1996 12 19 TWRA96371 1 19961201 A 3350 3004181A LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 620FF 232 21162 DURING DAILY CHECK, FOUND L1 MED BUSTLE EVAC LIGHT INOPERATIVE. REMOVED AND REPLACED L1 BUSTLE LIGHT PER MM 33-51-00. O PS CHECKED NORMAL. (X) 2 L 7 4 4F A20WE 1996121900008 19961219 00008 NM 1996 12 19 HNAA9693775 1 19961114 A 3230 XD4N RELAY DHAV DHC8 DHC8102 2809003 NM LANDING GEAR FAILED A HNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 07 937HA 20950 148 HPN/PHL - FLT 3158 - WHEN SELECTING GEAR UP, GEAR WOULD NOT RETRACT. RED, GREEN, AND HANDLE LIGHTS ON. GEAR CONFIRMED DOWN AND DOORS CLOSED. THE AIRCRAFT TURNED BACK TO HPN AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE 3261-K5 R ELAY. (X) 2 H 7 2 4T RT A13NM 1996121900009 19961219 00009 WP 1996 12 19 USAAD96172 1 19961126 A 5610 WINDSHIELD DOUG DC9 DC931 3022065 WP RT COCKPIT BIRD STRIKE A USAA A UNSCHED LANDING C F.O.D. CL CLIMB 1 EA 19 956VJ 47588 MYR/CLT - FLT 312 - ON ROTATION, FIRST OFFICER'S WINDSHIELD STRUCK A MEDIUM SIZE BIRD. RETURNED TO FIELD. PERFORMED BI RD STRIKE INSPECTION ON F/O'S WINDSHIELD, NR 2 ENGINE, AND RIGHT WING. NO DEFECTS NOTED. (X) 2 L 7 2 4F A6WE 1996121900010 19961219 00010 NM 1996 12 19 USAASB96243 1 19961018 A 3350 AD20131A BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 441US 24812 CLE - MAINTENANCE FOUND THE AFT RIGHT FUSELAGE, EXTERNAL EMERGENCY DOOR LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPL ACED THE BATTERY PACK. OPS CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1996121900011 19961219 00011 NE 1996 12 19 961128001 2 19961128 A 7261 693905 OIL CAP DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9A 52048 NE NR 1 ENGINE LOOSE A GTIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 23 12505 45788 665873 DTW - FLT 423 - IN CLIMB CONFIGURATION, FLIGHT CREW OBSERVED NR 1 ENGINE OIL QUANTITY DECREASE FROM 16 QUARTS TO 6 QUART S. RETURNED TO DTW WITHOUT INCIDENT. MAINTENANCE FOUND NR 1 ENGINE OIL TANK SERVICE CAP NOT SECURED. SERVICED ENGINE WITH OIL, SECURED OIL CAP. ENGINE RUN-UP CHECKED NORMAL IAW DC 9 MM, CHAPTER 79-11-0. ACCOMPLISHED AN OVERWEIGHT LANDI NG INSPECTION IAW DC 9 MM 5-51-0 AND NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F 4 F A6WE E2EA 1996121900012 19961219 00012 NM 1996 12 19 MALA965210 1 19961123 A 3060 7826893 BRUSH BLOCK DHAV DHC8 DHC8102 2809003 NM RIGHT ELEV WORN A MALA O OTHER O OTHER CL CLIMB 1 GL 15 824MA 327 FLT 3121 - ON CLIMB-OUT FROM MSP, THE RIGHT ELEVATOR HORN HEAT BECAME INOPERATIVE. THE AIRCRAFT RETURNED TO MSP. MAINT ENANCE REPLACED THE RIGHT BRUSH BLOCK, P/N 782689-3, WHICH WAS FOUND TO BE WORN, AND THE CURRENT LIMITERS, P/N MS28937-3 0, WHICH WAS FOUND TO PRODUCE LOW VOLTAGE. ALL CHECKS SATISFACTORY. REFERENCE: OPERATOR CONTROL NR 96ZZZX6039. (X) 2 H 7 2 4T RT A13NM 1996121900013 19961219 00013 NM 1996 12 19 96ZZZX6039 1 19961123 A 3060 MS2893730 LIMITERS DHAV DHC8 DHC8102 2809003 NM RIGHT ELEV FAILED A MALA O OTHER O OTHER CL CLIMB 1 GL 15 824MA 327 FLT 3121 - ON CLIMB-OUT FROM MSP, THE RIGHT ELEVATOR HORN HEAT BECAME INOPERATIVE. THE AIRCRAFT RETURNED TO MSP. MAINT ENANCE REPLACED THE RIGHT BRUSH BLOCK, P/N 782689-3, WHICH WAS FOUND TO BE WORN, AND THE CURRENT LIMITERS, P/N MS28937-3 0, WHICH WAS FOUND TO PRODUCE LOW VOLTAGE. ALL CHECKS SATISFACTORY. REFERENCE: OPERATOR CONTROL NR MALA965210. 2 H 7 2 4T RT A13NM 1996121900014 19961219 00014 SW 1996 12 19 MALA965209 1 19961121 A 3260 1EN516 SWITCH SWRNGN SA227 SA227AC 8780603 SW NLG FAILED A MALA O OTHER N FALSE WARNING AP APPROACH 1 GL 15 160MC AC733B FLT 3365 - ON APROACH TO DTW, THE GEAR HAD TO BE CYCLED TWO TIMES BEFORE A NOSE GEAR DOWN INDICATION WAS RECEIVED. MAIN TENANCE REPLACED THE DOWN AND LOCKED SWITCHES ON THE RIGHT SIDE OF THE NOSE GEAR. ALL CHECKS SATISFACTORY. (X) 2 L 7 2 4T RT A8SW 1996121900015 19961219 00015 EU 1996 12 19 MALA965207 1 19961120 A 3020 NY24668081 INLET ASSY SAAB SF340 SF340A 7850100 EU RT NACELLE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 112XJ 340A112 FLT 2915 - IN-FLIGHT, THE RIGHT INTAKE HEAT ANNUNCIATOR LIGHT ILLUMINATED DURING FLIGHT. THE CREW RECYCLED THE RIGHT EN GINE ANTI-ICE CIRCUIT BREAKER, BUT THE PROBLEM REMAINED. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE RIGHT FORWARD LOWER INLET ASSEMBLY. ALL CHECKS SATISFACTORY. (X) 2 L 7 2 4T RT A52EU 1996121900016 19961219 00016 WP 1996 12 19 ZIAA96073 1 19961112 A 5313 LONGERON CVAC 340 340D 242270H WP BS 526 CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 3417 58121 48 YIP - DURING BELT FRAME INSPECTION PER AD 74-16-01, LONGERON 25R WAS FOUND CRACKED. REFERENCE: OPERATOR CONTROL NRS 96 ZZZX6040, 96ZZZX6041, 96ZZZX6042, AND 96ZZZX6043. (X) 2 L 7 2 4R 6A6 1996121900017 19961219 00017 WP 1996 12 19 96ZZZX6040 1 19961112 A 5313 LONGERON CVAC 340 340D 242270H WP BS 565 CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 3417 58121 48 YIP - DURING BELT FRAME INSPECTION PER AD 74-16-01, LONGERON 12R WAS FOUND CRACKED. REFERENCE: OPERATOR CONTROL NRS ZI AA96073, 96ZZZX6041, 96ZZZX6042, AND 96ZZZX6043. 2 L 7 2 4R 6A6 1996121900018 19961219 00018 WP 1996 12 19 96ZZZX6041 1 19961112 A 5313 LONGERON CVAC 340 340D 242270H WP BS 565 CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 3417 58121 48 YIP - DURING BELT FRAME INSPECTION PER AD 74-16-01, LONGERON 30R WAS FOUND CRACKED. REFERENCE: OPERATOR CONTROL NRS ZI AA96073, 96ZZZX6040, 96ZZZX6042, AND 96ZZZX6043. (X) 2 L 7 2 4R 6A6 1996121900019 19961219 00019 WP 1996 12 19 96ZZZX6042 1 19961112 A 5313 LONGERON CVAC 340 340D 242270H WP BS 745 CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 3417 58121 48 YIP - DURING BELT FRAME INSPECTION PER AD 74-16-01, LONGERON 2L WAS FOUND CRACKED. REFERENCE: OPERATOR CONTROL NRS ZIA A96073, 96ZZZX6040, 96ZZZX6041, AND 96ZZZX6043. (X) 2 L 7 2 4R 6A6 1996121900020 19961219 00020 WP 1996 12 19 96ZZZX6043 1 19961112 A 5313 LONGERON CVAC 340 340D 242270H WP BS 798 CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 3417 58121 48 YIP - DURING BELT FRAME INSPECTION PER AD 74-16-01, LONGERON 25R WAS FOUND CRACKED. REFERENCE: OPERATOR CONTROL NRS ZI AA96073, 96ZZZX6040, 96ZZZX6041, AND 96ZZZX6042. (X) 2 L 7 2 4R 6A6 1996121900021 19961219 00021 SW 1996 12 19 MALA965208 1 19961121 A 3230 2752000191 UPLOCK SHAFT SWRNGN SA227 SA227AC 8780603 SW NLG LACK OF LUBE A MALA O OTHER J WARNING INDICATION CL CLIMB 1 GL 15 442MA AC725 FLT 3240 - ON CLIMB-OUT FROM GFK, THE NOSE GEAR CONTINUED TO CYCLE AFTER GEAR RETRACTION. THE CREW CYCLED THE GEAR FOUR TIMES, BUT THE PROBLEM CONTINUED. THE CREW LOWERED THE GEAR AND CONTINUED TO MSP WITH THE GEAR DOWN. MAINTENANCE FOUN D THE UPLOCK HOOK SHAFT TO BE SLIGHTLY STIFF. MAINTENANCE LUBED THE UPLOCK SHAFT. ALL CHECKS SATISFACTORY DURING GEAR SWINGS. (X) 2 L 7 2 4T RT A8SW 1996121900022 19961219 00022 WP 1996 12 19 96ZZZX6044 1 19961114 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 945 CRACKED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 AFT CARGO STA 945 HAS CIRCUMFERENTIAL FRAME WITH CRACK IN RADIUS AT STR 30. 2 L 7 2 4F A6WE 1996121900023 19961219 00023 WP 1996 12 19 96ZZZX6045 1 19961121 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 130/160 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEDULED INSPECTION AT AERO CORP, CORROSION WAS FOUND IN THE E/E COMPARTMENT FRAMES AT STA 130 AND STA 160 BET WEEN S28L TO S28R. REMOVED FRAME STA 130 AND SHEAR CLIP. CORROSION OUT OF LIMITS IAW DC9 SRM 53-01 FIG 1. FABBED NEW SHEAR CLIP IAW DC9 SRM 53-11-3, DIMENSIONS 53.5 INCHES BY 2.5 INCHES. MECHANICALLY REMOVED CORROSION FROM FRAME 130 AND FRAME 160, WITHIN LIMITS. SHEAR CLIP STA 160 OUT OF LIMITS IAW DC9 SRM 53-01 FIG 1. FABBED REPAIR IAW DC9 SRM 53-01 F IG 2. ALODINED AND PRIMED IAW DC9 SRM 51-10-3. INSTALLED FRAME AND SHEAR CLIP STA 130 AND STA 160 IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1996121900024 19961219 00024 WP 1996 12 19 96ZZZX6046 1 19961121 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 120/130 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEDULED INSPECTION AT AERO CORP, CORROSION WAS FOUND IN THE E/E COMPARTMENT, S28L, S29L, S30, S29R, AND S28R FROM STA 120 TO STA 130. REMOVED AND REPLACED LONGERONS 29L/R AND LONGERON 30 IAW DC9 SRM 53-02. REMOVED CORROSION, WI THIN LIMITS. ALODINED AND PRIMED LONGERON 28L/R IAW DC9 SRM 51-10-3. FABBED LONGERON 29L/R AND LONGERON 30. INSTALLED LONGERON IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1996121900025 19961219 00025 WP 1996 12 19 96ZZZX6047 1 19961129 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 930-935 CORROSION A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEDULED INSPECTION AT AERO CORP, CORROSION WAS FOUND IN THE RIGHT OUTBOARD SEAT TRACK FROM STA 930 TO STA 935 . DRILL OUT SEATED TRACK, BUT SEAT TRACK OUT. FAB NEW SEAT TRACK DRILL UP NEW, DEBURRED HOLES, INSTALLED SEAT TRACK AN D SPLICE PART, IAW DC9 SRM 5305 FIG 4. DRILLED AND DEBURRED SPLICE AND SPLICE PLATE IAW DC9 SRM'S 51-10-4, 53-05 FIG 4D . 2 L 7 2 4F A6WE 1996121900026 19961219 00026 WP 1996 12 19 96ZZZX6048 1 19961121 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 579-756 CORROSION A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEDULED INSPECTION AT AERO CORP, CORROSION WAS FOUND IN THE LEFT INBOARD SEAT TRACK BETWEEN STA 579 - STA 756 . REMOVED CORROSION IAW DC9 SRM 51-10-3. CORROSION OUT OF LIMITS IAW DC9 SRM 53-01 FIG 1, FABRICATED REPAIR SPLICE (70 75 T6 .160 INCH, .180 INCH, .125 INCH, .100 INCH) IAW DC9 SRM 53-05 FIG 40. DRILLED DEBURRED, TREATED AND PRIMED NEW SEAT TRACK IAW DC9 SRM 51-10-3, SRM 51-10-4. ALODINED AND PRIMED AND INSTALLED REPAIR PARTS IAW DC9 SRM 53-05 FIG 4B, SR M 51-10-3. 2 L 7 2 4F A6WE 1996121900027 19961219 00027 WP 1996 12 19 96ZZZX6049 1 19961121 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP CABIN CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEDULED INSPECTION AT AERO CORP, CORROSION WAS FOUND IN THE NR 1 SEAT TRACK LEFT FLANGE. 2 L 7 2 4F A6WE 1996121900028 19961219 00028 WP 1996 12 19 96ZZZX6050 1 19961121 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 180-218 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEDULED INSPECTION AT AERO CORP, CORROSION WAS FOUND IN THE NR 4 SEAT TRACK FS 180 TO FS 218, INBD AND OTBD F LANGES. (X) 2 L 7 2 4F A6WE 1996121900029 19961219 00029 WP 1996 12 19 96ZZZX6051 1 19961121 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 522 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEDULED INSPECTION AT AERO CORP, CORROSION WAS FOUND IN THE FWD CARGO PIT, FRAME STA 522 FROM S28R TO S29L. 2 L 7 2 4F A6WE 1996121900031 19961219 00031 WP 1996 12 19 96ZZZX6053 1 19961121 A 5313 STRINGER DOUG DC9 DC932 3022066 WP BS 756 CORROSION A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEDULED INSPECTION AT AERO CORP, CORROSION WAS FOUND IN THE AFT CARGO PIT AT STA 756 S30 AROUND FASTENERS. R EMOVED CORROSION, OUT OF LIMITS IAW DC9 SRM 53-01, WAS .180 INCH, NOW .130 INCH. NDT VERIFIED. REMOVED CORRODED END OF SPLICE IAW DC9 SRM 53-02 FIG 12. FABBED LONGERON 30 END SPLICE. INSTALLED LONGERON 30 END SPLICE, TORQUED BOLTS IAW D C9 SRM 51-30-2. INSTALLED END SPLICE IAW DC9 SRM 51-30-2 AND SRM 51-30-5. 2 L 7 2 4F A6WE 1996121900032 19961219 00032 WP 1996 12 19 96ZZZX6054 1 19961121 A 5315 FLOOR BEAM DOUG DC9 DC932 3022066 WP BS 996 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEUDLED INSPECTION AT AERO CORP, CORROSION WAS FOUND IN THE AFT CARGO PIT CABIN FLOOR BEAM AT STA 996 AT BL 3 4R. REMOVED CORROSION IAW DC9 SRM 51-10-2. FOUND TO BE OUT OF LIMITS AT LBL 31, 38, 40, 45, AT STA 980 IAW DC9 SRM 53- 05 FIG 20A, 50 PERCENT MATERIAL LOSS. FABBED FLOOR BEAM REPAIR ANGLE WITH 7075T6511. DIMENSIONS 26.50 INCHES BY 1 INCH BY 1 INCH, UPPER FLANGE .156 INCH, LOWER .125 INCH IAW DC9 SRM 53-05 PG 31. FABBED FILLER WITH 7075T6.100. DIMENSION S 17 INCHES BY .8750 INCH AND SHIM WITH 301.FH.025 INCH STAINLESS STEEL IAW DC9 SRM 53-05 PG 31. MACHINE TAPERED REPAIR ANGLE IAW DC9 SRM 53-05 FIG 20A. TREATED AND PRIMED REPAIR PARTS. 2 L 7 2 4F A6WE 1996121900033 19961219 00033 WP 1996 12 19 96ZZZX6055 1 19961121 A 5320 THRESHOLD DOUG DC9 DC932 3022066 WP CARGO COMPT CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEDULED INSPECTION AT AERO CORP, CORROSION WAS FOUND IN THE FWD PIT LOWER THRESHOLD PAN SECTION AND 1 EACH SP LICE. 2 L 7 2 4F A6WE 1996121900034 19961219 00034 WP 1996 12 19 96ZZZX6056 1 19961121 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 870/897 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEDULED INSPECTION AT AERO CORP, CORROSION FOUND IN THE AFT CARGO PIT, S29R FROM STA 870 - STA 897. S29R WAS NOT CORRODED, INTERCOSTAL ON TOP WAS CORRODED AND CRACKED. REMOVED CORROSION, CORROSION WAS OUT OF LIMITS IAW DC9 SRM 53-01 FIG 1, SRM 51-10-3. RECEIVED NEW INTERCOSTAL. DRILLED, DEBURRED, AND INSTALLED INTERCOSTAL IAW DC9 SRM'S 51-30-5 , 51-30-2, 51-20-3, 51-10-4. 2 L 7 2 4F A6WE 1996121900035 19961219 00035 WP 1996 12 19 96ZZZX6057 1 19961121 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 897 CRACKED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEDULED INSPECTION AT AERO CORP, A 1 INCH CRACK WAS FOUND IN THE AFT CARGO PIT FRAME AT STA 897 BETWEEN S28L AND S27L. REMOVED OLD REPAIR CRACKED DOUBLER IAW DC9 SRM 51-30-5. REMOVED CORROSION ON ANGLE FRAME, MATERIAL LOSS LESS THAN .002 INCH IAW DC9 SRM 51-10-3. TREATED AND PRIMED IAW DC9 SRM 51-10-3. FABBED DOUBLER 13.5 INCHES BY 2.750 INCHE S OUT OF 7075-T6 .063 INCH. TRIMMED, PRIMED, COUNTERSUNK, AND DEBURRED IAW DC9 SRM 53-01 PAGE 8 FIG 2. TREATED AND PRI MED IAW DC9 SRM 51-10-3. INSTALLED REPAIRS IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1996121900036 19961219 00036 WP 1996 12 19 96ZZZX6058 1 19961121 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 897/965 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEDULED INSPECTION AT AERO CORP, CORROSION WAS FOUND IN THE AFT CARGO PIT, STA S30 FROM STA 897 TO STA 965. M ECHANICALLY REMOVED CORROSION. CORROSION FOUND TO BE OUT OF LIMITS IAW DC9 SRM 51-01 FIG 1. REMOVED CORRODED AREA OF S TR 30 IAW DC9 SRM 51-01. CLEANED BLUE WATER FROM STA 897 TO STA 963 IAW DC9 SRM. TREATED AND PRIMED LONGERON FROM STA 897 TO STA 963 IAW DC9 SRM 51-10-3. INSTALLED LONGERON AND SPLICES AT STA 897 TO STA 963 IAW DC9 SRM'S 51-30-0 51-30-1, 51-30-2, 51-30-5. 2 L 7 2 4F A6WE 1996121900037 19961219 00037 WP 1996 12 19 96ZZZX6059 1 19961121 A 5313 STRINGER DOUG DC9 DC932 3022066 WP BS 389-408 CORROSION A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEDULED INSPECTION AT AERO CORP, CORROSION WAS FOUND IN THE FORWARD CARGO PIT, S29R BETWEEN STA 389 AND STA 4 08 AROUND NUTPLATES FOR RADIO ALTIMETER NR 1. 2 L 7 2 4F A6WE 1996121900038 19961219 00038 WP 1996 12 19 96ZZZX6060 1 19961114 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 830 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 AFT CARGO HAS HEAVY CORROSION ON CIRCUMFERENTIAL FRAME BETWEEN STRINGERS 29L-29R AT STA 830. 2 L 7 2 4F A6WE 1996121900039 19961219 00039 WP 1996 12 19 96ZZZX6061 1 19961114 A 5320 END CAP DOUG DC9 DC932 3022066 WP BS 750 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 AFT CARGO HAS HEAVY CORROSION NEAR FWD BULKHEAD AT STA 750 AT STRINGERS 29L-29R END CAP AT STR 30. 2 L 7 2 4F A6WE 1996121900040 19961219 00040 WP 1996 12 19 96ZZZX6062 1 19961114 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 770 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 AFT CARGO HAS CORROSION ON CIRCUMFERENTIAL FRAME BETWEEN STRINGERS 29L AND 29R, STA 770. 2 L 7 2 4F A6WE 1996121900041 19961219 00041 WP 1996 12 19 96ZZZX6063 1 19961114 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 790 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 AFT CARGO HAS CORROSION ON CIRCUMFERENTIAL FRAME BETWEEN STRINGERS 29L AND 29R AT STA 790. 2 L 7 2 4F A6WE 1996121900042 19961219 00042 WP 1996 12 19 96ZZZX6064 1 19961114 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 810 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 AFT CARGO HAS CORROSION ON CIRCUMFERENTIAL FRAME BETWEEN STRINGERS 29L AND 29R, STA 810. 2 L 7 2 4F A6WE 1996121900043 19961219 00043 WP 1996 12 19 96ZZZX6065 1 19961114 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 850 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 AFT CARGO HAS CORROSION ON CIRCUMFERENTIAL FRAME AT STA 850 BETWEEN STRINGERS 29L AND 29R. 2 L 7 2 4F A6WE 1996121900044 19961219 00044 WP 1996 12 19 96ZZZX6066 1 19961114 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 870 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 AFT CARGO HAS CORROSION ON CIRCUMFERENTIAL FRAME AT STA 870 BETWEEN STRINGERS 29L AND 29R. 2 L 7 2 4F A6WE 1996121900045 19961219 00045 WP 1996 12 19 96ZZZX6067 1 19961114 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 850-890 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 AFT CARGO HAS CORROSION ALONG INTERCOSTAL BETWEEN STA 850 - STA 890, STR 28. 2 L 7 2 4F A6WE 1996121900046 19961219 00046 WP 1996 12 19 96ZZZX6068 1 19961114 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 850-890 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 AFT CARGO HAS CORROSION ALONG INTERCOSTAL BETWEEN STATIONS 850-890, STRINGER 29. 2 L 7 2 4F A6WE 1996121900047 19961219 00047 WP 1996 12 19 96ZZZX6069 1 19961114 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 917 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 AFT CARGO HAS SEVERAL SPOTS OF CORROSION ON CIRCUMFERENTIAL FRAME AT STA 917, CORROSION EXTENDS UNDER FINGERS OF ATTACH ANGLE. 2 L 7 2 4F A6WE 1996121900048 19961219 00048 EU 1996 12 19 WTAA960196 1 19961120 A 5730 SKIN BAG JETSTM JETSTM3101 1500215 EU LT WING LE BIRD STRIKE A WTAA O OTHER C F.O.D. NR NOT REPORTED 1 WP 17 421UE 804 CIC - BIRD STRIKE ON LEFT WING LEADING EDGE REPORTED. MAINTENANCE C/W BIRD STRIKE INSPECTION. REPLACED LEFT INBOARD ST UB WING LEADING EDGE. DE-ICE SYSTEM OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A21EU 1996121900049 19961219 00049 NM 1996 12 19 ZZDA5722896 1 19961108 A 5755 654645151 SKIN BOEING 737 7372L9 1384497 NM NR 3 SPOILER DELAMINATION A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT MA4317 21278 NR 3 SPOILER - CUT OUT DELAMINATED AREA ON LOWER SKIN SURFACE 17.50 INCHES BY 7 INCHES. INSTALLED REPAIR IAW B-737 SRM 57-50-5. (X) 2 L 7 2 4F RT A16WE 1996121900050 19961219 00050 NM 1996 12 19 ZZDA7921296 1 19961020 A 7931 O-RING BOEING 737 737214 138446R NM NR 1 ENGINE LEAKING A ZZDA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 15 460AT 20158 MCO/OMA - FLT 800 - ON FLIGHT, NR 1 ENGINE OIL QUANTITY STARTED TO DECREASE ACCOMPANIED BY A DROP IN OIL PRESSURE (TO 30 PSI) FOLLOWED BY THE NR 1 ENGINE OIL PRESSURE LIGHT ON STEADY. POWER WAS REDUCED TO IDLE RPM ON NR 1 ENGINE AND AIRCRA FT WAS DIVERTED TO MCI WHERE A NORMAL LANDING WAS CONDUCTED. MECHANICS INSPECTED NR 1 ENGINE AND FOUND AN O-RING LEAKIN G AT THE OIL PRESSURE DIFFERENTIAL SWITCH. THE O-RING WAS REPLACED AND THE ENGINE WAS RUN FOR A LEAK CHECK. ALL CONDIT IONS CHECKED NORMAL. AIRCRAFT WAS RELEASED FOR FLIGHT. (X) 2 L 7 2 4F A16WE 1996121900051 19961219 00051 NM 1996 12 19 ZZDA7921396 1 19961022 A 7931 201575 ELBOW BOEING 737 737214 138446R NM NR 1 ENGINE LOOSE A ZZDA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 15 460AT 20158 MCI/MCO - FLT 823 - DURING CRUISE POWER, OIL QUANTITY ON NR 1 ENGINE DROPPED TO .6 GALLONS WITH PRESSURE AND TEMPERATURE NORMAL. REDUCED RPM TO IDLE AND DIVERTED TO BNA WHERE A NORMAL LANDING WAS MADE. MECHANICS INSPECTED NR 1 ENGINE AND FOUND DIFFERENTIAL OIL PRESSURE LINE LEAKING AT ACCESSORY GEARBOX. FURTHER INVESTIGATION REVEALED THE THREADED INSERT F OR THE PRESSURE LINE FITTING HAD BECOME LOOSE. REPLACED THREADED INSERT IN DIFFERENTIAL OIL PRESSURE LINE BOSS IAW PWJT 8D ENGINE MANUAL 72-61-01 (REPAIR NR 5 PAGES 902-908) AND STANDARD PRACTICES. SERVICED OIL. RAN ENGINE, FOUND NO LEAKS, RETURNED TO SERVICE. (X) 2 L 7 2 4F A16WE 1996121900052 19961219 00052 EU 1996 12 19 WTAA960197 1 19961117 A 3231 137254B7 ROD END BAG JETSTM JETSTM3101 1500215 EU RT MLG DOOR BROKEN A WTAA K NONE O OTHER UK UNKNOWN 1 WP 17 429UE 807 LAX - RIGHT MAIN GEAR DOOR ATTACHMENT ROD END BROKEN. MAINTENANCE INSPECTED RIGHT MAIN LANDING GEAR AND DOOR FOR DAMAGE . NO DAMAGE NOTED. REPLACED ROD END BUSHING AND NUT. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1996121900053 19961219 00053 SO 1996 12 19 96ZZZX6070 1 19961119 A 7931 3012517 PRESS RELIEF VLV GRUMAN G73 G73T SO NR 1 ENGINE WORN A FVYA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 17 130FB 9504 3018 J30 DURING STRAIGHT AND LEVEL CRUISE FLIGHT, FLIGHT CREW INITIATED A PRECAUTIONARY SHUT DOWN OF THE NR 1 ENGINE OF A G-73T S EAPLANE DUE TO DROPPING OIL PRESSURE. AFTER AN UNEVENTFUL LANDING INTO CHUB CAY, BAHAMAS, MAINTENANCE PERSONNEL FOUND T HE OIL PRESSURE RELIEF VALVE WAS DISLODGED FROM ITS SEAT. THE VALVE WAS REINSTALLED, OIL SERVICED, AND RUN UP PERFORMED . AIRCRAFT WAS RETURNED TO SERVICE. 1 H 7 2 3R A783 1996121900054 19961219 00054 WP 1996 12 19 96ZZZX6071 1 19961121 A 5711 SPAR DOUG DC9 DC932 3022066 WP WS 58.5-111.5 CORRODED B ZIAD K NONE O OTHER IN INSP/MAINT 1 SO 11 901VJ 47275 DURING C-CHECK, FOUND CORROSION IN NR 1 TANK ON AFT SPAR XW58.50 TO XRS111.5. 2 L 7 2 4F A6WE 1996121900055 19961219 00055 EU 1996 12 19 NVEA9600009 1 19961209 A 2424 10200311 GCU AEROSP ATR42 ATR42300 8680920 EU E/E COMPT INOPERATIVE A NVEA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 SO 03 249AT 249 CAPT REPORTED, RT GEN RELAY WAS CHATTERING. TOOK THE RT GEN OFF LINE AND THE BTC WOULD NOT COUPLE. DEPARATED DCA TO JF K AND DIVERTED TO BWI. NO EMERGENCY WAS DECLARED AND NO FURTHER INCIDENT. REMOVED AND REPLACED GENERATOR CONTROL UNIT, OPS CHECKS GOOD. 2 H 7 2 4T RT A53EU 1996121900056 19961219 00056 EU 1996 12 19 NVEA9600008 1 19961205 A 7110 COWLING SAAB SF340 340B 7860101 EU RT ENGINE SEPARATED A NVEA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 SO 03 219AE 340B219 CREW REPORTED ON CLIMBOUT AT APPROX 400 FEET, THE RT O/B COWL WAS UP. THE CREW TURNED THE A/C BACK TO MIA. AS THEY WER E COMING BACK JUST SHORT OF APPROACH, THE RT O/B COWL SEPARATED FROM THE NACELLE. 2 L 7 2 4T RT A52EU 1996121900057 19961219 00057 NM 1996 12 19 AWXA9600736 1 19961208 A 3350 BATTERY BOEING 737 73733A 1384673 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 174AW 23633 DURING ROUTINE MAINTENANCE CHECK, FOUND BULLNOSE EMERGENCY LIGHTS INOP AT 12 DEF, 13 ABC, 17 ABC AND 19 DEF. RECHARGED LIGHTING SYSTEM, OPS CHECK GOOD BOEING STANDARD. 2 L 7 2 4F RT A16WE 1996121900058 19961219 00058 EU 1996 12 19 AWXA9600737 1 19961209 A 3350 321430 BATTERY PACK AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 636AW 098 DURING ROUTINE MAINTENANCE CHECK, FOUND RT OVERWING EMERGENCY LIGHT POWER SUPPLY FAILS SELF TEST. REMOVED AND REPLACED RT OVERWING EMERGENCY LIGHT POWER SUPPLY SYSTEM. REMOVED AND REPLACED RT OVERWING BATTERY PACK, OPS CHECK GOOD. POWER SUPPLY 321454 0704 INOP RT OVERWING. 2 L 7 2 4F RT A28NM 1996121900059 19961219 00059 NM 1996 12 19 AWXA9600738 1 19961208 A 3230 CIRCUIT BREAKER BOEING 737 737277 1384570 NM LANDING GEAR TRIPPED A AWXA K NONE J WARNING INDICATION TO TAKEOFF 1 WP 28 189AW 22656 ON TAKEOFF, COULD NOT RETRACT LANDING GEAR, USED OVERRIDE TO RETACT GEAR. FOUND LANDING GEAR LEVER LATCH C/B POPPED. R ESET C/B AND SYSTEM OPS NORMAL. 2 L 7 2 4F RT A16WE 1996121900060 19961219 00060 NM 1996 12 19 AWXA9600739 1 19961208 A 7830 TR HINGE FITTING BOEING 757 757225 1384959 NM NR 2 ENGINE CRACKED A AWXA A UNSCHED LANDING E J M VIBRATION/BUFFET WARNING INDICATION OVER TEMP CL CLIMB 1 WP 28 913AW 22207 AIR TURNBACK CLIMBING THROUGH FL 13, RT ENG OVERHEAT MESSAGE ACCOMPANIED BY VIBRATION. ENG THRUST WAS REDUCED BUT NOT S HUTDOWN. PROBLEM NOT EVIDENT AT REDUCED THRUST. NO EVENT TAKEN AND NO AUTO EVENT ON EICAS. REMOVED AND REPLACED NR 2 ENG HP2 DUCT AT ENGINE TO PYLON, LEAK CHECKED GOOD. REMOVED AND REPLACED NR 2 ENG HP6 DUCT AT ENG TO PYLON, LEAK CHECK ED GOOD. BORESCOPED AREAS IAW I5B72607, NO FAULT FOUND. CHECKED PRESSURE AND SCAVENGE SCREENS FOR METAL, NO METAL FOUN D. PERFORMED ENG RUN, LEAK CHECK GOOD. VIBRATION CAUSED BY T/R HINGE FITTING CRACK. REMOVED AND REPLACED HINGE FITTIN G PER EO 545102. 2 L 7 2 4F RT A2NM 1996121900061 19961219 00061 WP 1996 12 19 9626219880 1 19961206 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 6575M 47651 DURING LINE CHECK, FOUND EMERGENCY LIGHTS IN TAILCONE AREA INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY PACKS, OPERAT IONAL CHECK OK. 2 L 7 2 4F RT A6WE 1996121900062 19961219 00062 NM 1996 12 19 9626286304 1 19961211 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 661US 23819 DURING LINE CHECK, FOUND LEFT AND RIGHT UPPER DECK EMERGENCY EXIT LIGHTS AND EMERGENCY FLOOR TRACK LIGHTS AT DOORS 3L AN D 4L INOPERATIVE. REPLACED BATTERY PACKS AND RELAMPED LIGHTS, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1996121900063 19961219 00063 WP 1996 12 19 9626229945 1 19961206 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 1038 ELONGATED HOLE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8925E 45840 DURING PERIODIC CHECK, FOUND FRAME AT FS 1038 BETWEEN LONGERONS 13L AND 14L WITH AN ELONGATED HOLE FROM BRACE ROD ATTACH FITTING. REPAIRED FRAME PER EA 99-111-14. 2 L 7 2 4F A6WE 1996121900064 19961219 00064 WP 1996 12 19 9626239952 1 19961207 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 609 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 916RW 47144 DURING PERIODIC CHECK, FOUND LONGERON 30 'T' CHORD CRACKED IN RADIUS AT FS 609, RIGHT KEEL AREA. REPAIRED PER EA 99-120 157. 2 L 7 2 4F A6WE 1996121900065 19961219 00065 WP 1996 12 19 9626249614 1 19961209 A 5713 LONGERON DOUG DC9 DC932 3022066 WP RT /LT WINGS CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 614NW 47128 DURING ACCEPTANCE CHECK, FOUND WING LONGERONS 17L AND 17R CORRODED. INSTALLED NEW LONGERONS PER EA 99-097708. 2 L 7 2 4F A6WE 1996121900066 19961219 00066 WP 1996 12 19 9626259614 1 19961209 A 5720 ACCESS PANEL DOUG DC9 DC932 3022066 WP RT WING CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 614NW 47128 DURING ACCEPTANCE CHECK, FOUND RIGHT WING LOWER LEADING EDGE ACCESS PANEL NR 1220A CORRODED AT INBOARD END. INSTALLED R EPAIR PER EA 99-099978. 2 L 7 2 4F A6WE 1996121900067 19961219 00067 WP 1996 12 19 9626269618 1 19961206 A 5540 ANGLE DOUG DC9 DC932 3022066 WP RUDDER CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 618NW 47433 DURING ACCEPTANCE CHECK, FOUND RIGHT ANGLE AT RUDDER FRONT SPAR CORRODED. REPAIRED PER EA 99-099971. 2 L 7 2 4F A6WE 1996121900068 19961219 00068 WP 1996 12 19 9626279618 1 19961209 A 5530 FITTING DOUG DC9 DC932 3022066 WP BS 1089 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 618NW 47433 DURING ACCEPTANCE CHECK, FOUND VERTICAL STABILIZER LOWER LEADING EDGE FORWARD LEFT ANCHOR WITH AN 8 INCH CRACK AT FS 108 9, LONGERON 2L. REPLACED FITTING PER EA 99-097758. 2 L 7 2 4F A6WE 1996121900069 19961219 00069 NM 1996 12 19 UPS96221741 1 19961210 A 3350 1000679 LIGHT BOEING 727 727247 138408F NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 212UP 21392 INSPECTION TYPE-N/A, FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY, OPS CK G OOD (P/N 10-0067-9) (S/N 19703) ON, S/N 18001) OFF. 2 L 7 3 4F A3WE 1996121900070 19961219 00070 NM 1996 12 19 UPS96221744 1 19961211 A 3260 DOWNLOCK SWITCH BOEING 727 72751C 1384015 NM RT MAIN GEAR INOPERATIVE A IPXA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 905UP 18947 INSPECTION TYPE-N/A, UNSAFE INDICATION RT MAIN GEAR. MANUAL GEAR EXTENSION CHKLIST ACCOMPLISHED, NO SAFE INDICATION. T OWER FLY-BY FOR POSSIBLE STATUS OF GEAR. DECLARED EMERGENCY REQUESTED CRASH CREWS. REMOVED AND REPLACED RT MAIN GEAR D OWNLOCK SWITCH IAW MM32-61-21, PERFORMED ADJ AND TEST IAW MM 32-61-21 AND OPS CHK GOOD. 2 L 7 3 4F A3WE 1996121900071 19961219 00071 WP 1996 12 19 UPS96821740 1 19961209 A 2822 PUMP SWTCH DOUG DC8 DC873F 302199F WP NR 3 ENG BOOST OUT OF POSITION A IPXA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 SO 01 806UP 46006 INSPECTION TYPE-N/A, DURING CLIMB THROUGH FL350 NR 3 ENG N1 BEGAN TO FLUCTUATE +/- 3 PERCENT THEN GOT WORSE. SHUT OFF P MC TO STABILIZE, NO EFFECT. LOST THROTTLE CONTROL OF NR 3 ENG. PERFORMED INFLIGHT SHUTDOWN AND TURNED BACK TO SDF. SE COND OFFICER NOTED NR 3 BOOST/FEED SWITCH WAS IN OFF POSITION. RESTART AT FL190 WAS SUCCESSFUL, OPERATED NORMALLY. INS PECTED ENGINE VISUALLY FOR DEFECTS, NONE FOUND. 2 L 7 4 4F RT 4A25 1996121900072 19961219 00072 EU 1996 12 19 QXEA9600486 1 19961209 A 3350 5515800104 CIRCUIT BOARD FOKKER FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 491US 11156 FRONT CENTER OVERHEAD EMERGENCY SIGNS ARE INOP. CIRCUIT BOARD REPLACED IN FRONT AND CENTER OVERHEAD SIGN, SIGN OPS CHEC KED GOOD. 2 L 7 2 4F RT A20EU 1996121900073 19961219 00073 EU 1996 12 19 QXEA9600487 1 19961210 A 3350 5515800104 CIRCUIT BOARD FOKKER FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 491US 11156 EMERGENCY EXIT SIGN OVER COCKPIT DOOR HAS NUMEROUS BULBS OUT. CIRCUIT BOARD REPLACED AND SIGN OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996121900074 19961219 00074 NM 1996 12 19 96UAL900805 1 19961014 A 3230 83517 DRIVER CARD BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE E/E COMPT FAILED A UALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 29 609UA 21870 ON GEAR RETRACTION RECEIVED GEAR DISAGREE EICAS MESSAGE AND GEAR DOORS LIGHT REMAINED ON. RECYCLED GEAR, RIGHT GEAR SLO W TO EXTEND AND RETRACT. DOOR LIGHT AND GEAR DISAGREE MESSAGE CLEARED. NO INDICATION OF HYDRAULIC LOW PRESSURE OR LOSS OF FLUID. *S/D* THE A5 DRIVER CARD FAULTED AND WAS REPLACED. THE S266 NOSE GEAR PROXIMITY SENSOR WAS ALSO ADJUSTED. RECYCLED GEAR, OPERATIONS CHECK NORMAL PER MM 32-61-00. 2 L 7 2 4F 4 F RT A1NM E3NE 1996121900075 19961219 00075 NE 1996 12 19 96UAL900910 2 19961127 A 7230 COMPRESSOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT ENGINE STALLED A UALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 641UA 25091 717541 AIRCRAFT RETURNED TO FIELD DUE TO RIGHT ENGINE COMPRESSOR STALL AND HIGH EGT. *S/D* COMPRESSOR STALL IS ATTRIBUTED TO THE N2 COMPRESSOR FAILURE. THE ENGINE WAS REMOVED FROM THE AIRCRAFT. THE ENGINE IS NOT YET DISASSEMBLED. 2 L 7 2 4F 4 F RT A1NM E24NE 1996121900076 19961219 00076 NM 1996 12 19 96UAL900911 1 19961127 A 2822 BOOST PUMPS BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE NR 1 FUEL TANK FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 990UA 21980 AFTER TAKEOFF, NUMBER ONE ENGINE FORWARD AND AFT LOW PRESSURE LIGHTS ILLUMINATED. CIRCUIT BREAKERS WERE FOUND POPPED, R ETURNED TO DEN. *S/D* REPLACED FWD AND AFT FUEL BOOST PUMPS, FUEL PANEL, FWD AND AFT CIRCUIT BREAKERS, BLED PUMP LOW P RESSURE SWITCHES, SUMPED NR 1 TANK AND FOUND NO CONTAMINATION, OPS CHECK GOOD. 2 L 7 2 4F 4 F A16WE E2EA 1996121900077 19961219 00077 NM 1996 12 19 96UAL900912 1 19961127 A 3234 65B8293116 GEAR HANDLE BOEING 757 757222 1384956 NM PWA JT9 JT9D7J 52054 NE COCKPIT DIRTY A UALA L ABORTED APPROACH J WARNING INDICATION LD LANDING 1 WP 29 161UA 21352 NOSE GEAR HAD TO BE EXTENDED BY ALTERNATE SYSTEM, HAD A RED GEAR LIGHT AND NO ALTERNATE NOSE GEAR OPEN LIGHT. GPWS SYST EM GAVE AN AURAL GEAR WARNING, CYCLED GEAR. *S/D* DETERMINED THAT GEAR HANDLE WAS NOT MOVING INTO FORWARD DETENT WHEN PUT IN DOWN POSITION. CLEANED SHAFT AND DEBRIS FROM GEAR HANDLE MODULE. CYCLED NOSE GEAR NUMEROUS TIMES, OPS CHECKS OK . 2 L 7 2 4F 4 F RT A2NM E20EA 1996121900078 19961219 00078 NM 1996 12 19 96UAL900913 1 19961127 A 3350 1317 LIGHT BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 908UA 25008 EMERGENCY AISLE LIGHT IN BULL NOSE ROW 18 INOP. REPLACED LAMP, CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1996121900080 19961219 00080 WP 1996 12 19 96UAL900916 1 19961204 A 2120 AIR DISTR GARRET 3810262MOD DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 1816U 90213700 46615 THERE WAS A STRONG ODOR LIKE GLYCOL THROUGHOUT CABIN DURING CLIMB AND EARLY PART OF CRUISE. *S/D* SUSPECTED OIL LEAK A T APU CASE COOLING FAN. APU WAS REPLACED, BUT SHOP COULD NOT CONFIRM LEAK. THERE HAS BEEN NO REOCCURANCE. 2 L 7 3 4F 4 F A22WE E23EA 1996121900081 19961219 00081 WP 1996 12 19 96UAL900917 1 19961127 A 3350 CONNECTOR DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1830U 46629 FIRST CLASS EMERGENCY EEL LIGHTS INOPERATIVE. LEFT AND RIGHT SIDES RESEATED CONNECTORS, CHECKS OK. 2 L 7 3 4F 4 F A22WE E23EA 1996121900082 19961219 00082 NM 1996 12 19 96UAL900918 1 19961128 A 2530 35200015 COFFEEMAKER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE AFT GALLEY OVERHEATED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 7277U 21424 ELECTRICAL BURNING SMELL IN AFT GALLEY. *S/D* BURNING SMELL ISOLATED TO AFT LOWER COFFEEMAKER. REPLACED COFFEEMAKER. 2 L 7 3 4F 4 F A3WE E2EA 1996121900083 19961219 00083 NM 1996 12 19 96UAL900919 1 19961127 A 3350 S106 BATTERIES BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7442U 21896 AFT AIRSTAIR OVERHEAD EMERGENCY LIGHT INOPERATIVE. *S/D* BATTERIES DISCHARGED. REPLACED BATTERIES. 2 L 7 3 4F 4 F A3WE E2EA 1996121900084 19961219 00084 NE 1996 12 19 96UAL900920 2 19961129 A 7260 564908600U GEARBOX BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE DAMAGED A UALA O OTHER K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 WP 29 7462U 21916 NR 3 MAIN OIL PUMP ASSEMBLY LEAKING OIL ON IDLE RUN. *S/D* OIL PUMP LINER DAMAGED DURING REPLACEMENT OF PUMP O-RINGS. REPLACED MAIN ACCESSORY GEARBOX. 2 L 7 3 4F 4 F A3WE E2EA 1996121900085 19961219 00085 1996 12 19 96UAL900921 4 19961206 A 2565 INFLATION TUBE AIR CRUISERS D28935103 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE DOOR SLIDE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7444U 179191078 21898 SLIDE REMOVED PER AIR CRUISERS SERVICE INFORMATION LETTER 25-98. DURING SHOP OVERHAUL A SEAM LEAK DEVELOPED ON THE INF LATION TUBE. SLIDE SCRAPPED. 2 L 7 3 4F 4 F A3WE E2EA 1996121900086 19961219 00086 NM 1996 12 19 96UAL900922 1 19961206 A 2497 W3666000410 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN LOOSE A UALA K NONE A FLAME/FIRE IN INSP/MAINT 1 WP 29 594UA 28145 REPEATED ELECTRICAL POWER AND SUPPLY PROBLEMS WITH THIS AIRCRAFT REVEALED A LOOSE GALLEY GROUND WIRE CONNECTION. FURTHE R INVESTIGATION FOUND INDICATIONS OF ARCING AND FIRE/SMOKE DAMAGE. *S/D* DISCOVERED WIRE W3666000410 WAS NOT CONNECTED SECURELY TO AIRCRAFT GROUND. WIRE WAS INSTALLED ON THE TERMINAL WITHOUT A RETAINING NUT. ALSO, A NEW DELIVERED AIRCR AFT WAS RECEIVED IN SIMILAR CONDITION. REPLACED WIRE AND CORRECTED DAMAGE, OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996121900087 19961219 00087 1996 12 19 96UAL900923 4 19961206 A 2565 INFLATION TUBE AIR CRUISERS D28935103 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE DOOR SLIDE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7455U 178671078 21909 SLIDE REMOVED PER AIR CRUISERS SERVICE INFORMATION LETTER 25-98. DURING SHOP OVERHAUL A SEAM LEAK DEVELOPED ON THE INFL ATION TUBE. SCRAPPED SLIDE. 2 L 7 3 4F 4 F A3WE E2EA 1996121900088 19961219 00088 WP 1996 12 19 MWEA96652 1 19961207 A 3830 59147921 SERVICE PANEL DOUG DC9 DC914 3022034 WP AFT FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 DURING ROUTINE INSPECTION, FOUND SMALL CRACK IN AFT LAV SERVICE PANEL. REPAIRED SERVICE PANEL IN ACCORDANCE WITH DC9 SR M 53-01 FIG 2 SHT 3. 2 L 7 2 4F A6WE 1996121900089 19961219 00089 WP 1996 12 19 MWEA96653 1 19961210 A 5330 59114051 SKIN DOUG DC9 DC914 3022034 WP BS 160-200 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 DURING ROUTINE INSPECTION, FOUND 3 LIGHTNING STRIKES ON TOP OF FUSELAGE RIGHT SIDE BETWEEN FS 160 AND FS 200 AT LONGERON 5 LOCATION. REPAIRED LIGHTNING STRIKE WITH INTERNAL DOUBLER REPAIR IAW DC9 SRM 53-04 FIG 38 VIEWS H, I, SRM 51-30-2. 2 L 7 2 4F A6WE 1996121900090 19961219 00090 WP 1996 12 19 MWEA96654 1 19961210 A 5330 SKIN DOUG DC9 DC914 3022034 WP BS 160-200 LIGHTNING STRIKE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 DURING INSPECTION, FOUND THREE LIGHTNING STRIKES ON TOP OF FUSELAGE RT SIDE BETWEEN STA 160 TO 200 AT LONGERON 5R. INST ALLED REPAIR IAW SRM 53-04 FIG 38 VIEW H AND VIEW I. 2 L 7 2 4F A6WE 1996121900091 19961219 00091 1996 12 19 DHL96708007 4 19961209 A 2210 25888801 YAW DAMPER BOEING 727 72725 1384006 NM RUDDER MALFUNCTIONED A A DHLA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 SO 01 708DH 18275 AT FL 310 AND MACH .80, RECEIVED SUDDEN UNCOMMANDED RUDDER INPUTS FROM LOWER YAW DAMPER. WHEN YAW DAMPER SWITCH TURNED OFF, THE UNCOMMANDED RUDDER INPUTS CEASED. CLEANED LOWER YAW DAMPER CONNECTOR AND RERACKED COUPLER, CYCLED RUDDER TO F ULL TRAVEL LEFT AND RIGHT SEVERAL TIMES, FOUND NO PROBLEM. OPS CHECK OK PER M/M 22-11-01. 2 L 7 3 4F A3WE 1996121900092 19961219 00092 WP 1996 12 19 DHL96807002 1 19961210 A 3270 TAIL SKID DOUG DC8 DC873F 302199F WP AFT FUSELAGE DAMAGED A DHLA A J UNSCHED LANDING DUMP FUEL O OTHER CL CLIMB 1 SO 01 807DH 45990 SUSPECTED TAIL STRIKE ON TAKE-OFF. INSPECTED TAIL SKID PER M/M 5-55-0, OK FOR SERVICE. 2 L 7 4 4F RT 4A25 1996121900093 19961219 00093 NE 1996 12 19 RRXA96169 2 19961210 A 7200 ENGINE DOUG DC8 DC8F54 3021926 WP PWA JT3D JT3D3B 52039 NE NR 1 FAILED A A RRXA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 WP 15 992CF 45884 669678 NR 1 ENGINE FAILURE RESULTING IN INFLIGHT SHUTDOWN. SHUTDOWN ENGINE IAW ENGINE FIRE OR DAMAGE CHECKLIST IN QRH. MAINTE NANCE REMOVED AND REPLACED NR 1 ENGINE AND PERFORMED GROUND RUN-UP PER EMERY PAPERWORK PACKAGE MEO77 AND DC-8 MM CHAPTER 71-00. 2 L 7 4 4F 4 F 4A25 1E8 1996121900094 19961219 00094 WP 1996 12 19 RRXA96170 1 19961209 A 2110 TURBTURBO COMP DOUG DC8 DC863F 302198F WP NR 1 ODOR A RRXA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 15 865F 46088 WITH NR 1 TURBINE OPERATING HAD A BAD BURNED OIL ODOR IN THE COCKPIT. MAINTENANCE TRANSFERED TO DMI LIST PER MEL 21-1-2 A CAT C DMI NR 612092 DUE 12/20/96, PLACARD INSTALLED. COULD NOT DUPLICATE PROBLEM ON FLIGHT FROM ALB TO ELP, THIS CLEA RS DMI NR 612092. 2 L 7 4 4F 4A25 1996121900095 19961219 00095 SO 1996 12 19 SRAA961060 1 19961013 A 5320 SUPPORT BEAM LKHEED 382 382G 526414U SO BS 697 CORROSION A SRAA K NONE O OTHER IN INSP/MAINT 1 GL 23 905SJ 45318 4472 DURING C-CHECK, FOUND CARGO COMPARTMENT FLOOR PANEL SUPPORT BEAM AT FS 697, LBL 40 HAS CORROSION AT FORWARD AND AFT SIDE BEYOND LIMITS. CUT OUT CORRODED SECTION, FABRICATED AND INSTALLED FILLER AND L-ANGLE, DOUBLER AND STRAP DOUBLER IAW LA C SRM CHAPTER 51-40-22. 2 H 7 4 4T A1SO 1996121900195 19961219 00195 EU 1996 12 19 AWXA9600740 1 19961210 A 3397 WIRE AIRBUS 320 A320231 3930325 EU CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 627AW 66 DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 26 A, B, C SEAT MOUNTED EMERGENCY LIGHT INOP. REPAIRED WIRING AS NEEDED, OP S CHECK GOOD. 2 L 7 2 4F RT A28NM 1996121900196 19961219 00196 NM 1996 12 19 AWXA9600741 1 19961212 A 3397 WIRE BOEING 737 73733A 1384673 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 169AW 23630 DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 3 EMERGENCY LIGHT INOP. FOUND BROKEN WIRE. REPLACED SPLICE, OPS CHECK GOOD . 2 L 7 2 4F RT A16WE 1996121900197 19961219 00197 NM 1996 12 19 AWXA9600742 1 19961212 A 3231 LINKAGE BOEING 737 737275 1384485 NM NLG DOOR BROKEN A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 CGBPW 20958 ON GEAR RETRACTION, BANG HEARD IN NOSE WHEEL WELL WITH VIBRATION. REPLACED BROKEN LT NOSE GEAR DOOR LINKAGE, CHECKED AN D ADJUSTED DOORS PER BMM 32-22-11, PAGE 407, STEP L. NOSE GEAR EXT/RET PER 32-33-0, PAGE 101. 2 L 7 2 4F A16WE 1996121900198 19961219 00198 NM 1996 12 19 AWXA9600743 1 19961211 A 3242 214747 BRAKE BOEING 737 7373B7 1384580 NM LT MLG LEAKING A AWXA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 28 328AW 9010 633 23377 LT MAIN BRAKE WAS REPORTED TO BE SMOKING BY GROUND CONTROL. EMERGENCY DECLARED. FOUND NR 1 BRAKE LEAKING. REMOVED AND REPLACED BRAKE PER AWM 353. 2 L 7 2 4F RT A16WE 1996121900199 19961219 00199 SO 1996 12 19 RAAA96E4024 1 19961213 A 3350 100055 LIGHT LKHEED 188 188C 5262604 SO CABIN FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 9744C 188C1140 RT AFT EMERGENCY EXIT PULLDOWN LIGHT FAILED SERVICE CHECK. CHANGED EMERGENCY LIGHT ASSY. 2 L 7 4 4T 4A22 1996121900200 19961219 00200 NE 1996 12 19 CALA9601784 2 19961211 A 7230 COMP BLADE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9 52048 NE NR 1 ENGINE FAILED A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 69523 47520 665871 THE NR 1 ENGINE FAILED AT ROTATION WITH NO WINDMILLING RPM OR OIL PRESSURE NOTED IN FLIGHT. THE AIRCRAFT WAS RETURNED T O RSW WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND METAL IN THE NR 1 ENGINE TAILPIPE. THE NR 1 ENGINE WAS REMOV ED AND REPLACED. *S/D* INVESTIGATION CONCLUDED THAT THE PRIMARY CAUSE OF ENGINE FAILURE WAS DUE TO AN 8TH STAGE COMPRE SSOR BLADE FAILING IN HIGH CYCLE FATIGUE. 2 L 7 2 4F 4 F A6WE E2EA 1996121900201 19961219 00201 WP 1996 12 19 9626299945 1 19961210 A 5350 TAILCONE DOUG DC9 DC931 3022065 WP AFT FUSELAGE OUT OF ADJUST A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8925E 45840 DURING PERIODIC CHECK, TAILCONE RELEASE FORCE EXCEEDED MAXIMUM LIMITS ON FUNCTION DROP CHECK. ADJUSTED PER CITEXT 09-53 50-1-0021, SECOND TEST WAS WITHIN LIMITS. 2 L 7 2 4F A6WE 1996121900203 19961219 00203 WP 1996 12 19 9626319903 1 19961212 A 3350 6011779 POWER SUPPLY DOUG DC9 DC931 3022065 WP NACELLE FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 953N 47083 DURING LINE MAINTENANCE INSPECTION, FOUND NACELLE EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY, OPER ATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996121900204 19961219 00204 WP 1996 12 19 9626329982 1 19961212 A 3350 60030451 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 982US 45790 DURING PERIODIC CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996121900205 19961219 00205 WP 1996 12 19 9626339969 1 19961210 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9333 47246 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS AT SEAT 17D INOPERATIVE. MAINTENANCE REPAIRE D BROKEN WIRE AT SEAT TRACK AREA, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996121900206 19961219 00206 WP 1996 12 19 9626349982 1 19961211 A 3397 WIRE DOUG DC9 DC932 3022066 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 982US 45790 DURING PERIODIC CHECK, FOUND FORWARD CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE INSI DE BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996121900207 19961219 00207 WP 1996 12 19 9626359601 1 19961211 A 3350 PLUG DOUG DC9 DC932 3022066 WP CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 601NW 47038 DURING LINE MAINTENANCE INSPECTION, FOUND RED EMERGENCY MARKER LIGHT FOR FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE AT ROW 11. MAINTENANCE SECURED LOOSE PLUG UNDER SEAT 11D, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996121900208 19961219 00208 WP 1996 12 19 9626369981 1 19961211 A 5531 RIB DOUG DC9 DC931 3022065 WP VERT STABILIZER CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 994Z 47097 DURING PERIODIC CHECK, FOUND MULTIPLE VERTICAL STABILIZER RIBS CRACKED AT AFT ATTACH POINTS. REPAIRED PER EA 99-111928. 2 L 7 2 4F A6WE 1996121900209 19961219 00209 WP 1996 12 19 9626379981 1 19961212 A 5312 BULKHEAD DOUG DC9 DC931 3022065 WP BS 110 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 994Z 47097 DURING PERIODIC CHECK, FOUND NOSE WHEEL WELL PRESSURE PANEL CRACKED AT FS 110 AT INBOARD VERTICAL BEAM ON RIGHT SIDE. F ABRICATED DOUBLER AND REPAIRED PER EA 99-111924. 2 L 7 2 4F A6WE 1996121900210 19961219 00210 SO 1996 12 19 COMA9610389 1 19961210 A 2750 3472001001 CONTROL UNIT EMB 120 EMB120RT SO E/E COMPT MALFUNCTION A COMA K NONE O OTHER AP APPROACH 1 SO 01 249CA 120230 FLAP CONTROL FAULT WARNING DURING APPROACH. REPLACED THE FLAP CONTROL UNIT. 2 L 7 2 4T RT A31SO 1996121900211 19961219 00211 NE 1996 12 19 COMA9610390 2 19961211 A 7200 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE LEFT FAILED A COMA E A ENGINE SHUTDOWN UNSCHED LANDING Y B ENGINE STOPPAGE SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 263CA 120255 115366 LEFT ENGINE FAILED AT 23,000 FT, SMOKE IN COCKPIT. CAGED ENGINE AND RETURNED TO FIELD. REPLACED LEFT ENGINE. 2 L 7 2 4T 4 T RT A31SO E20NE 1996121900212 19961219 00212 SO 1996 12 19 COMA9610391 1 19961211 A 3230 12038594001 CONTROL MODULE EMB 120 EMB120RT SO LANDING GEAR MALFUNCTION A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 267CA 11482 626 120259 LANDING GEAR CONTROL HAD TO BE CYCLED 3 TIMES BEFORE GEAR EXTENDED. REPLACED THE LANDING GEAR CONTROL MODULE. 2 L 7 2 4T RT A31SO 1996121900213 19961219 00213 SO 1996 12 19 COMA9610392 1 19961212 A 5270 SWITCHES EMB 120 EMB120RT SO CARGO DOOR OUT OF ADJUST A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 161CA 120143 CARGO DOOR WARNING DURING TAKEOFF. ADJUSTED DOOR MICRO SWITCHES. 2 L 7 2 4T RT A31SO 1996121900214 19961219 00214 SO 1996 12 19 COMA9610393 1 19961212 A 5246 12048166003 LATCH EMB 120 EMB120RT SO RT FUEL DOOR MISSING A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 463CA 120267 SERVICE DOOR WARNING DURING TAKEOFF. REPLACED MISSING FASTENER IN FUEL SERVICE DOOR. 2 L 7 2 4T RT A31SO 1996121900215 19961219 00215 SO 1996 12 19 COMA9610394 1 19961211 A 2751 3471001001 ANNUNCIATOR EMB 120 EMB120RT SO INST PANEL MALFUNCTIONED A COMA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 130G 7736 120130 REPEATED FLAP CONTROL FAULT WARNINGS DURING FLIGHT. REPLACED THE FLAP ANNUCIATOR UNIT. 2 L 7 2 4T RT A31SO 1996121900216 19961219 00216 SO 1996 12 19 COMA9610395 1 19961211 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST UK UNKNOWN 1 SO 01 1110J 10682 120110 EMERGENCY EXIT LIGHT AT ROW 5C IS INOP. REPLACED THE EMERGENCY BATTERY PACK. 2 L 7 2 4T RT A31SO 1996121900217 19961219 00217 EU 1996 12 19 COMA9630162 1 19961212 A 3020 ND00751940 LOAD MONITOR SAAB SF340 SF340A 7850100 EU LT NACELLE MALFUNCTION A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 359CA 14232 4785 340A053 LEFT ENGINE INTAKE ANTI-ICE INOP WARNING. REPLACED THE LOAD MONITOR. 2 L 7 2 4T RT A52EU 1996121900218 19961219 00218 EA 1996 12 19 COMA9660222 1 19961211 A 2912 NAS16124 PACKING CNDAIR CL600 CL6002B19 EA NR 2 HYD SYST DETERIORATED A COMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 949CA 7048 NR 2 HYDRAULIC SYSTEM LOW PRESSURE MESSAGE ON EICAS. SYSTEM QUANTITY INDICATES ZERO. REPLACED A DETERIORATED O-RING SE AL ON FILTER DRAIN PLUG. SYSTEM SERVICED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1996121900219 19961219 00219 EA 1996 12 19 COMA9660223 1 19961211 A 3230 4622 VALVE CNDAIR CL600 CL6002B19 EA NLG DEFECTIVE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 941CA 7050 NOSE LANDING GEAR DISAGREE WARNING WHEN LANDING GEAR RETRACTED. REPLACED THE NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 1996121900220 19961219 00220 EA 1996 12 19 COMA9660224 1 19961212 A 2742 83963 ACTUATOR CNDAIR CL600 CL6002B19 EA HORZ STAB TRIM MALFUNCTION A COMA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SO 01 964CA 7129 CONFIG WARNING DURING TAKEOFF. REPLACED THE HORIZONTAL STABILIZER TRIM ACTUATOR. 2 L 7 2 4F RT A21EA 1996121900221 19961219 00221 EA 1996 12 19 COMA9660225 1 19961205 A 5230 H2912A SPRING CNDAIR CL600 CL6002B19 EA CARGO DOOR BROKEN A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 916CA 7014 CARGO DOOR LATCH POPPED OPEN ON TAKEOFF, CABIN WOULD NOT PRESSURIZE. REPLACED CARGO DOOR HANDLE LATCH SPRING. 2 L 7 2 4F RT A21EA 1996121900222 19961219 00222 SO 1996 12 19 COMA9610396 1 19961212 A 7603 0881824 SOLENOID EMB 120 EMB120RT SO NACELLE FAILED A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 257CA 120248 FLIGHT IDLE STOP SOLENOID CIRCUIT BREAKER IS TRIPPED. REPLACED THE FLIGHT IDLE STOP SOLENOID. 2 L 7 2 4T RT A31SO 1996121900223 19961219 00223 NM 1996 12 19 SWAA961335 1 19961209 A 5330 SKIN BOEING 737 7372H4 138448C NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 53SW 21534 DURING SCHEDULED C1 CHECK, FOUND NOSE WHEEL WELL SKIN CRACKED, 4 INCHES BEHIND GEAR MANUAL EXTENSION RETURN SPRING BRACK ET. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996121900224 19961219 00224 NM 1996 12 19 SWAA961336 1 19961209 A 5330 SKIN BOEING 737 7372H4 138448C NM SERV DOOR CUTOUT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21722 DURING SCHEDULED B-CHECK, FOUND FWD SERVICE DOOR LOWER HINGE CUTOUT CRACKED .3125 INCH. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996121900225 19961219 00225 NM 1996 12 19 SWAA961337 1 19961209 A 5320 FRAME BOEING 737 7372H4 138448C NM CARGO DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21722 DURING SCHEDULED B-CHECK, FOUND A .75 INCH CRACK ON DOOR FRAME THROUGH 1ST FASTENER AFT OF LOWER FWD DOOR STOP MOUNT INS IDE DOOR. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996121900226 19961219 00226 NM 1996 12 19 SWAA961338 1 19961211 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 922 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED SERVICE CHECK, FOUND A 3 INCH SKIN CRACK AFT LOWER FUSELAGE AT BS 922. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996121900227 19961219 00227 1996 12 19 SWAA961339 4 19961208 A 2565 22D2290013 SLIDE BOEING 737 7372H4 138448C NM FWD RT DOOR LOW PRESS A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 62SW 22060 DURING WALKAROUND CHECK, FOUND FWD RT DOOR ESCAPE SLIDE PRESSURE BELOW SERVICABLE LIMITS. REPLACED PER BOEING M/M. 2 L 7 2 4F A16WE 1996121900228 19961219 00228 NM 1996 12 19 SWAA961340 1 19961209 A 3350 2330127 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 64SW 22062 DURING SCHEDULED TERMINAL CHECK, FOUND EMERGENCY EXIT LIGHT ASSEMBLY ABOVE FWD SERVICE DOOR INOP. REPLACED PER BOEING M /M. 2 L 7 2 4F A16WE 1996121900229 19961219 00229 NM 1996 12 19 SWAA961341 1 19961209 A 5330 SKIN BOEING 737 7372H4 138448C NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 80SW 22675 DURING SCHEDULED C1 CHECK, FOUND FWD SERVICE DOOR OUTER SKIN CRACKED THROUGH RIVET EXTENDING FWD .25 AND AFT .125. RIVE T LOCATED UPPER FWD ABOVE LOWER HINGE CUTOUT. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996121900230 19961219 00230 NM 1996 12 19 SWAA961342 1 19961209 A 3350 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 81SW 22730 DURING SCHEDULED TERMINAL CHECK, FOUND FWD SERVICE DOOR AND FWD ENTRY DOOR EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK AND OPS CHECKED PER BOEING M/M. 2 L 7 2 4F A16WE 1996121900231 19961219 00231 NM 1996 12 19 SWAA961343 1 19961120 A 5330 SKIN BOEING 737 7373A4 1384585 NM NOSE BIRD STRIKE A SWAA A UNSCHED LANDING C F.O.D. CL CLIMB 1 SW 07 673AA 23251 AFTER TAKEOFF, LARGE BIRD OR BIRDS HIT NEAR LEFT NOSE WHEEL WELL. AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDI NG. INSPECTED AND FOUND SLIGHT EVIDENCE OF STRIKE TO NOSE LEFT SIDE, WITHIN BOEING SRM AND NUMBER 1 ENGINE. BORESCOPED AND PERFORMED ENGINE RUN-UP, WITH NO DAMAGE NOTED. 2 L 7 2 4F RT A16WE 1996121900232 19961219 00232 NM 1996 12 19 SWAA961344 1 19961211 A 5230 SKIN BOEING 737 7372H4 138448C NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 96SW 23055 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACK AT AFT CARGO DOOR SPRING DOOR HANDLE CUTOUT. REPAIRED PER SWA RA 1 -A52-020. 2 L 7 2 4F A16WE 1996121900233 19961219 00233 NM 1996 12 19 SWAA961345 1 19961211 A 5312 BULKHEAD SUPPORT BOEING 737 7372H4 138448C NM BS 727B CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 96SW 23055 DURING SCHEDULED C2 CHECK, FOUND FWD BULKHEAD SUPPORT CRACKED 2.5 AT BS 727B. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996121900234 19961219 00234 NM 1996 12 19 SWAA961346 1 19961203 A 5330 SKIN BOEING 737 7372T4 1384492 NM BS 807 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 807, STRINGER 18L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996121900235 19961219 00235 NM 1996 12 19 SWAA961347 1 19961210 A 5320 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 1138 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE AT BS 1138 AT STRINGER 5R DAMAGED. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996121900236 19961219 00236 NM 1996 12 19 SWAA961348 1 19961210 A 5320 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 1138 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED D-CHECK, FOUND LOWER CHORD ON STRINGER 5T AT 1139 + 5 CRACKED. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996121900237 19961219 00237 NM 1996 12 19 SWAA961349 1 19961210 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 887 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED D-CHECK, FOUND PROTRUDING DENT AT BS 887 + 2, BETWEEN STRINGERS 18 AND 19L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996121900238 19961219 00238 NM 1996 12 19 SWAA961350 1 19961210 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 787 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED D-CHECK, FOUND SKIN DAMAGED AT BS 787 + 8, BETWEEN STRINGERS 18 AND 19L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996121900239 19961219 00239 NM 1996 12 19 SWAA961351 1 19961210 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 330 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED D-CHECK, FOUND SKIN DENTED AT BS 330, BETWEEN STRINGERS 25 AND 26. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996121900240 19961219 00240 NM 1996 12 19 SWAA961352 1 19961210 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 289 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED D-CHECK, FOUND SKIN DENTED AT BS 289, BETWEEN STRINGERS 21 AND 22. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996121900241 19961219 00241 NM 1996 12 19 SWAA961353 1 19961210 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 319 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED D-CHECK, FOUND SKIN DENTED AT BS 319, BETWEEN STRINGERS 20 AND 21. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996121900242 19961219 00242 NM 1996 12 19 SWAA961354 1 19961210 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 380 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED D-CHECK, FOUND SKIN DENTED AT BS 380, BETWEEN STRINGERS 23 AND 24. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996121900243 19961219 00243 NM 1996 12 19 SWAA961355 1 19961210 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 380+19 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED D-CHECK, FOUND SKIN DENTED AT BS 380 + 19, BETWEEN STRINGERS 24 AND 25R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996121900244 19961219 00244 NM 1996 12 19 SWAA961356 1 19961210 A 5320 T-ANGLE BOEING 737 7373H4 1384600 NM BS 727 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED D-CHECK, FOUND T-ANGLES DAMAGED AT BS 727, AT S20L AND S20R. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996121900245 19961219 00245 NM 1996 12 19 SWAA961357 1 19961210 A 5312 BULKHEAD WEB BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED D-CHECK, FOUND WEB AT BULKHEAD BS 178, BL 0, WL 187, CRACKED 1 INCH LONG. REPAIRED PER TRAMCO EWO 96-0 690. 2 L 7 2 4F RT A16WE 1996121900246 19961219 00246 NM 1996 12 19 SWAA961358 1 19961210 A 5312 BULKHEAD WEB BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED D-CHECK, FOUND PRESSURE WEB CRACKED AT BULKHEAD BS 178, LBL 6.7, WL 212.5. REPAIRED PER TRAMCO EWO 96- 0691. 2 L 7 2 4F RT A16WE 1996121900247 19961219 00247 NM 1996 12 19 SWAA961359 1 19961210 A 5312 BULKHEAD WEB BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED D-CHECK, FOUND PRESSURE WEB CRACKED AT BULKHEAD BS 178, LBL 4.7, WL 198. REPAIRED PER TRAMCO EWO 96-06 91. 2 L 7 2 4F RT A16WE 1996121900248 19961219 00248 NM 1996 12 19 SWAA961360 1 19961210 A 5312 BULKHEAD WEB BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED D-CHECK, FOUND PRESSURE WEB CRACKED AT BULKHEAD BS 178, RBL 4.7, WL 201. REPAIRED PER TRAMCO EWO 96-06 91. 2 L 7 2 4F RT A16WE 1996121900249 19961219 00249 NM 1996 12 19 SWAA961361 1 19961210 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 498 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED D-CHECK, FOUND STRINGER CRACKED AT BS 498, S23R. REPLACED DAMAGED SECTION PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996121900250 19961219 00250 NM 1996 12 19 SWAA961362 1 19961210 A 5320 CLIP BOEING 737 7373H4 1384600 NM BS 500 S19L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, S19L. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996121900251 19961219 00251 NM 1996 12 19 SWAA961363 1 19961210 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED D-CHECK, FOUND FWD CARGO BAY, FLOOR TO BULKHEAD SUPPORT ANGLE CORRODED AT BS 500D, LBL 24, RBL 24. WL 1 56. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996121900252 19961219 00252 NM 1996 12 19 SWAA961364 1 19961210 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 519 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM DENTED AT BS 519, LBL 8, WL 156. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996121900253 19961219 00253 NM 1996 12 19 SWAA961365 1 19961210 A 5312 BULKHEAD ANGLE BOEING 737 7373H4 1384600 NM BS 947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED D-CHECK, FOUND FLOOR TO BULKHEAD SUPPORT ANGLE CORRODED AT BS 947, LBL 21 TO RBL 21, WL 179. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996121900254 19961219 00254 NM 1996 12 19 SWAA961366 1 19961210 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 1020 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 1020, AT S14L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996121900255 19961219 00255 NM 1996 12 19 SWAA961367 1 19961210 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 384 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 384, AT S17L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996121900256 19961219 00256 NM 1996 12 19 SWAA961368 1 19961210 A 5320 CLIP BOEING 737 7373H4 1384600 NM BS 277/520/663.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, S15R, AT BS 663.5, S10R AND AT BS 520, S4R. REPLACED P ER BOEING SRM. 2 L 7 2 4F RT A16WE 1996121900257 19961219 00257 NM 1996 12 19 SWAA961369 1 19961210 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 455 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 455, 1 INCH BELOW S16L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996121900258 19961219 00258 NM 1996 12 19 SWAA961370 1 19961210 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 496 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 496, 1 INCH ABOVE S16R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996121900259 19961219 00259 NM 1996 12 19 SWAA961371 1 19961210 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED D-CHECK, FOUND DRAG ANGLE CRACKED IN RADIUS AT BS 540, RIGHT 2 INCHES ABOVE S22. REPLACED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1996121900260 19961219 00260 NM 1996 12 19 SWAA961372 1 19961210 A 5320 CHORD BOEING 737 7373H4 1384600 NM BS 1138 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED D-CHECK, FOUND LOWER CHORD ON STRINGER 5L, AT BS 1138 + 7 CRACKED. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996121900261 19961219 00261 NM 1996 12 19 SWAA961373 1 19961210 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 328 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOORWAY LOWER AFT SKIN CUTOUT CRACKED AT BS 328, RBL 65, WL 210. REPAIRED P ER BOEING SRM. 2 L 7 2 4F RT A16WE 1996121900262 19961219 00262 NM 1996 12 19 SWAA961374 1 19961210 A 5311 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 480, BS 887 S9L AND 9R, BS 907, S9L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996121900263 19961219 00263 NM 1996 12 19 SWAA961375 1 19961208 A 5330 SKIN BOEING 737 7373H4 1384600 NM SERV DR CUTOUT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 328SW 23692 DURING SCHEDULED C1 CHECK, FOUND FORWARD SERVICE DOOR UPPER CUTOUT LOWER CORNER CRACKED. REPAIRED PER SWA RA 1-352-0260 . 2 L 7 2 4F RT A16WE 1996121900264 19961219 00264 NM 1996 12 19 SWAA961376 1 19961208 A 5330 SKIN BOEING 737 7373H4 1384600 NM PAX DOOR CUTOUT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 328SW 23692 DURING SCHEDULED C1 CHECK, FOUND FORWARD ENTRY DOOR UPPER HINGE CUTOUT UPPER CORNER CRACKED. REPAIRED PER SWA RA 1-352- 0261. 2 L 7 2 4F RT A16WE 1996121900265 19961219 00265 NM 1996 12 19 SWAA961377 1 19961206 A 3350 20121 CHARGER BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 611SW 27697 DURING SCHEDULED C1 CHECK, FOUND CENTER CABIN FLOOR TRACK LIGHTING INOP. REPLACED BATTERY CHARGER PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996121900266 19961219 00266 1996 12 19 SWAA961378 4 19961211 A 2565 6121469 SLIDE BOEING 737 7373A4 1384585 NM SERVICE DOOR LOW PRESS A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677SW 23289 DURING SCHEDULED RON CHECK, FOUND AFT SERVICE DOOR SLIDE PRESSURE LOW. REPLACED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996121900267 19961219 00267 NM 1996 12 19 SWAA961379 1 19961210 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 294/328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 294 RBL 145, WL 208 AND AT BS 328 RBL 21.5 AND 35. REPAIRED P ER BOEING SRM. 2 L 7 2 4F RT A16WE 1996121900268 19961219 00268 NM 1996 12 19 SWAA961380 1 19961203 A 5320 CHORD BOEING 737 7372T4 1384492 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED SERVICE CHECK, FOUND BS 727 O/B CHORD AT S18A CRACKED AT FWD AND AFT HOLES. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1996121900269 19961219 00269 NM 1996 12 19 SWAA961381 1 19961210 A 5315 SUPPORT BOEING 737 7373H4 1384600 NM BS 998/1003 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 1003 AND 998. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996121900270 19961219 00270 NM 1996 12 19 SWAA961382 1 19961210 A 5315 SUPPORT BOEING 737 7373H4 1384600 NM BS 998/1003 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CRACKED AT BS 947 LBL 54 WL 208 AND AT RBL 4.5 AND 5.3, WL 207 AND 208. REPLA CED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1996121900271 19961219 00271 NE 1996 12 19 TC8A96070 2 19961211 A 7321 71128719 FUEL CONTROL DOUG DC8 DC8F55 3021928 WP PWA JT3D JT3D3B 52039 NE NR 2 ENGINE MALFUNCTIONED A A TC8A C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 23 808CK 45817 643799 NR 2 ENGINE COMPRESSOR STALLED AT HIGH ENGINE RPMS, HIGH FUEL FLOW NOTED. REMOVED AND REPLACED FUEL CONTROL, RAN ENGINE , TRIMMED IDLE AND PART POWER, OPS CHECKS GOOD IAW PWA 73-2-2. TRIM RUN IAW DAC MM 71-0, ALL PARAMETERS. 2 L 7 4 4F 4 F 4A25 1E8 1996121900309 19961219 00309 WP 1996 12 19 ZIAA96040 1 19961013 A 5730 SKIN DOUG DC8 DC862 3021970 WP LT WING LE CORROSION A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 DURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSI ON. LT WING LE EXT CORROSION. XFS 710-746. XW 761.695. XFS 817-820. REPAIRED IAW APPLICABLE SRM'S, DWG, ETC. (X) 2 L 7 4 4F 4A25 1996121900310 19961219 00310 WP 1996 12 19 ZIAA96041 1 19961013 A 5730 SKIN DOUG DC8 DC862 3021970 WP RT WING LE CORROSION A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 DURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSI ON. RT WING LE EXT CORROSION. XW 761.695-765. REPAIRED IAW APPLICABLE SRM'S, DWG, ETC. (X) 2 L 7 4 4F 4A25 1996121900311 19961219 00311 WP 1996 12 19 ZIAA96042 1 19961013 A 5730 SKIN DOUG DC8 DC862 3021970 WP LT WING LE CORROSION A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 DURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSI ON. LT WING LE EXT WS 575-599. XFS 566-603. REPAIRED IAW APPLICABLE SRM'S, DWG, ETC. (X) 2 L 7 4 4F 4A25 1996121900312 19961219 00312 WP 1996 12 19 ZIAA96043 1 19961013 A 5730 SKIN DOUG DC8 DC862 3021970 WP RT WING LE CORROSION A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 DURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSI ON. RT WING LE EXT. XIS 697 SEAM. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X) 2 L 7 4 4F 4A25 1996121900313 19961219 00313 WP 1996 12 19 ZIAA96044 1 19961013 A 5730 SKIN DOUG DC8 DC862 3021970 WP LT WING CORROSION A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 DURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSI ON. LT WING XW 408 EXT XRS 763. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X) 2 L 7 4 4F 4A25 1996121900314 19961219 00314 WP 1996 12 19 ZIAA96045 1 19961013 A 5751 SKIN DOUG DC8 DC862 3021970 WP RT AIL CORROSION A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 DURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSI ON. RT AIL INT XA 474-535. XA 646-678. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X) 2 L 7 4 4F 4A25 1996121900315 19961219 00315 WP 1996 12 19 ZIAA96046 1 19961013 A 5730 SKIN DOUG DC8 DC862 3021970 WP LT STUB LE CORROSION A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 64430 45922 DURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSI ON. LT STUB LE EXT. XFS 560-575. XFS 575. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X) 2 L 7 4 4F 4A25 1996121900316 19961219 00316 WP 1996 12 19 ZIAA96047 1 19961013 A 5730 SKIN DOUG DC8 DC862 3021970 WP RT WING LE CORROSION A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 DURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSI ON. RT WING LE EXT. XFS 422.750. MIDDLE PANEL. XFS 566.250. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X) 2 L 7 4 4F 4A25 1996121900317 19961219 00317 WP 1996 12 19 ZIAA96048 1 19961013 A 5730 SKIN DOUG DC8 DC862 3021970 WP LT WING CORROSION A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 DURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSI ON. LT WING XW 257-408. XFS 285-309. XFS 329. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X) 2 L 7 4 4F 4A25 1996121900318 19961219 00318 WP 1996 12 19 ZIAA96049 1 19961013 A 5711 SPAR DOUG DC8 DC862 3021970 WP LT WING LE CORROSION A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 DURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSI ON. LT WING LE SPAR XFS 500. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X) 2 L 7 4 4F 4A25 1996121900319 19961219 00319 WP 1996 12 19 ZIAA96050 1 19961013 A 5730 SKIN DOUG DC8 DC862 3021970 WP LT IB STUB CORROSION A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 DURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSI ON. LT INB STUB EXT XW 223-257. XW 246-251. XW 246.519. XW 246-519 AFT INB SLOT. REPAIRED IAW APPLICABLE SRM'S, DWG ., ETC. (X) 2 L 7 4 4F 4A25 1996121900320 19961219 00320 WP 1996 12 19 ZIAA96051 1 19961013 A 5730 SKIN DOUG DC8 DC862 3021970 WP LT INB STUB CORROSION A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 DURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSI ON. LT INB STUB INT. UPPER FLANGE. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X) 2 L 7 4 4F 4A25 1996121900321 19961219 00321 WP 1996 12 19 ZIAA96052 1 19961013 A 5730 SKIN DOUG DC8 DC862 3021970 WP RT INB STUB CORROSION A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 DURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSI ON. RT INB STUB EXT. WS 163.750. SLOT PANEL. UPPER SURFACE. XFS 291.500. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X) 2 L 7 4 4F 4A25 1996121900322 19961219 00322 WP 1996 12 19 ZIAA96053 1 19961013 A 5730 SKIN DOUG DC8 DC862 3021970 WP RT I/B LE CORROSION A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 DURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSI ON. RT WING I/B LE EXT. WFS 200. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X) 2 L 7 4 4F 4A25 1996121900323 19961219 00323 WP 1996 12 19 ZIAA96054 1 19961013 A 5512 SKIN DOUG DC8 DC862 3021970 WP LT HOR O/B CORROSION A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 DURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSI ON. LT HOR O/B EXT. XE 271-273. XE 310-312.5. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X) 2 L 7 4 4F 4A25 1996121900324 19961219 00324 WP 1996 12 19 ZIAA96055 1 19961013 A 5512 SKIN DOUG DC8 DC862 3021970 WP RT HOR O/B CORROSION A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 DURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSI ON. RT HOR O/B EXT. XE 290. XE 222. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X) 2 L 7 4 4F 4A25 1996121900325 19961219 00325 WP 1996 12 19 ZIAA96056 1 19961013 A 5330 SKIN DOUG DC8 DC862 3021970 WP FUSE UPPER FWD CORROSION A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 DURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSI ON. FUSE UPPER FWD EXT SKIN LONG 20-21R. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X) 2 L 7 4 4F 4A25 1996121900326 19961219 00326 WP 1996 12 19 ZIAA96057 1 19961013 A 5320 SKIN DOUG DC8 DC862 3021970 WP FS 400-420 CORROSION A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 DURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSI ON. FWD LWR RT TUNNEL INT FS 400-420. FS 300-320. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X) 2 L 7 4 4F 4A25 1996121900327 19961219 00327 WP 1996 12 19 ZIAA96058 1 19961013 A 5320 EXTRUSION DOUG DC8 DC862 3021970 WP FS 460-480 CORROSION A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 DURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSI ON. RT CUSP EXTRUSION. FS 460-480. FS 870-LONG 24R. FS 220-RT UPPER. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X) 2 L 7 4 4F 4A25 1996121900328 19961219 00328 WP 1996 12 19 ZIAA96059 1 19961013 A 5320 SKIN DOUG DC8 DC862 3021970 WP FS 1100 L 35L CORROSION A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 DURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSI ON. AFT LWR LT TUNNEL INT. FS 1100 LONG 35L. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X) 2 L 7 4 4F 4A25 1996121900329 19961219 00329 WP 1996 12 19 ZIAA96060 1 19961013 A 5320 SKIN DOUG DC8 DC862 3021970 WP FS 1060 L 27R CORROSION A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 DURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSI ON. AFT LWR RT TUNNEL INT FS 1060 LONG 27R. FS 1040 LONG 26L-27R. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X) 2 L 7 4 4F 4A25 1996121900330 19961219 00330 WP 1996 12 19 ZIAA96061 1 19961013 A 5320 SKIN DOUG DC8 DC862 3021970 WP FS 1190 CORROSION A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 DURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSI ON. AFT LOWER CARGO BILGE. FS 1190 LONG 35L. FS 1085-1090 SKIN. FS 1080 LONG 35R-36R. FS 1020-CIRCUM. FS 1020 LONG 35R-36R. FS 1100-CIRCUM. FS 1100 LONG 35R-36R. FS 980-1250 TRACK. FS 1120 LONG 35R-36R. REPAIRED IAW APPLICABLE SR M'S, DWG., ETC. (X) 2 L 7 4 4F 4A25 1996121900331 19961219 00331 WP 1996 12 19 ZIAA96062 1 19961013 A 5320 SKIN DOUG DC8 DC862 3021970 WP AFT ACCY COMPT CORROSION A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 DURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSI ON. AFT ACCY COMPT-FS 1440-1500. FS 1563 LONG 18-34R. FS 1563. FS 1563 LONG 34R. FS 1564 LONG 24L. FS 1563 LONG 18 L. FS 1560 LONG 18L ANGLES. FS 1440 LONG 34L-35R. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X) 2 L 7 4 4F 4A25 1996121900332 19961219 00332 WP 1996 12 19 ZIAA96063 1 19961013 A 5230 HINGE DOUG DC8 DC862 3021970 WP UPPER CARGO DOOR CORROSION A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 DURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSI ON. UPPER CARGO DOOR HINGE ABOVE FWD SWIVEL DOOR AFT END. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X) 2 L 7 4 4F 4A25 1996121900333 19961219 00333 WP 1996 12 19 ZIAA96064 1 19961013 A 5320 EXTRUSION DOUG DC8 DC862 3021970 WP FS 780 CORROSION A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 DURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSI ON. FS 780 AT FRAME. LT CUSP EXTRUSION. FS 520 AT FRAME. FS 1340 AT FRAME. FS 600 AT FRAME. FS 1020 AT FRAME. FS 1040 AT FRAME. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X) 2 L 7 4 4F 4A25 1996121900334 19961219 00334 WP 1996 12 19 ZIAA96065 1 19961013 A 5320 EXTRUSION DOUG DC8 DC862 3021970 WP FS 780 CORROSION A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 DURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSI ON. RT CUSP EXTRUSION: FS 600 AT FRAME. FS 1240-1260. FS 879.375 FITTING. FS 1400-AT FRAME. FS 1442-1450 WEB. REP AIRED IAW APPLICABLE SRM'S, DWG., ETC. (X) 2 L 7 4 4F 4A25 1996121900335 19961219 00335 WP 1996 12 19 ZIAA96066 1 19961013 A 5320 SKIN DOUG DC8 DC862 3021970 WP MAIN CABIN CORROSION A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 DURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSI ON. MAIN CABIN INTERIOR, FRAMES, LONGERONS, TRACK FROM FS 340 THROUGH FS 1590 BOTH LT AND RT. 54 AREAS NOTED ON TASK H 57300551. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X) 2 L 7 4 4F 4A25 1996121900336 19961219 00336 WP 1996 12 19 ZIAA96067 1 19961013 A 5314 KEEL BEAM DOUG DC8 DC862 3021970 WP LT W/W CORROSION A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 DURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSI ON. LT W/W KEEL BEAM. FS 944-980 TORQUE BOX. FS 947-974 WEB. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X) 2 L 7 4 4F 4A25 1996121900337 19961219 00337 WP 1996 12 19 ZIAA96068 1 19961013 A 5314 KEEL BEAM DOUG DC8 DC862 3021970 WP RT W/W CORROSION A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 DURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSI ON. RT W/W KEEL BEAM FS 902-940 WEB. FS 879-FITTING. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X) 2 L 7 4 4F 4A25 1996121900338 19961219 00338 WP 1996 12 19 ZIAA96069 1 19961013 A 5532 SKIN DOUG DC8 DC862 3021970 WP VERT STAB CORROSION A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 DURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSI ON. VERT STAB EXT LT SKIN, LT ATTACH ANGLE. RT SKIN ZR 225, RT SKIN ZR 270. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X) 2 L 7 4 4F 4A25 1996121900339 19961219 00339 WP 1996 12 19 ZIAA96070 1 19961013 A 5531 SPAR DOUG DC8 DC862 3021970 WP VERT STAB AFT CORROSION A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 DURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSI ON. VERT STAB AFT SPAR ZR 218-281. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (C) 2 L 7 4 4F 4A25 1996121900340 19961219 00340 WP 1996 12 19 ZIAA96071 1 19961013 A 5414 PANEL DOUG DC8 DC862 3021970 WP NR 1 PYLON CORROSION A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 799AL 64430 45922 DURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSI ON. NR 1 PYLON EXT PANEL, RT YN220. REPLACED. 2 L 7 4 4F 4A25 1996121900342 19961219 00342 1996 12 19 HEEA968617 4 19961209 A 2370 9806019001 CVR BELL 412 412 1182202 SW COCKPIT WONT TEST E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 2148K 3007 36001 CVR WILL NOT TEST. 1 G 7 2 4U H4SW 1996121900343 19961219 00343 1996 12 19 HEEA968618 4 19961209 A 3442 MI5852013 INDICATOR P4001 SKRSKY S76 S76A 8143006 NE COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 760035 P4001 INDICATOR WILL NOT POWER UP AND MOUNTING BRACKETS LOOSE. 1 G 7 2 3U H1NE 1996121900344 19961219 00344 1996 12 19 HEEA968619 4 19961209 A 3452 066106200 TRANSCEIVER KT76 BELL 206 206B3 1181506 SW COCKPIT ATC WEAK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107PH 2789 TRANSCEIVER WEAK RECEIVE. 1 G 7 1 3U H2SW 1996121900345 19961219 00345 NE 1996 12 19 HEEA968620 1 19961209 A 6210 7615009043050 TIP CAP SKRSKY S76 S76A 8143006 NE M/R DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545X 760050 TIP CAP HAS EXCESSIVE DAMAGE ON THE TRAILING EDGE NEAR THE INBOARD END. 1 G 7 2 3U H1NE 1996121900346 19961219 00346 NE 1996 12 19 HEEA968621 1 19961209 A 6410 7610105101041 BLADE SKRSKY S76 S76A 8143006 NE T/R DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 8962 760035 T/R BLADE PRIMARY POLYURETHANE STRIP TORN TO THE FIBERGLASS ON PADDLE "B". 1 G 7 2 3U H1NE 1996121900347 19961219 00347 NE 1996 12 19 HEEA968622 1 19961209 A 6410 7610105101041 BLADE SKRSKY S76 S76A 8143006 NE T/R SEPARATION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 8171 760035 SEPARATION OF THE TRAILING EDGE OF PADDLE "A". 1 G 7 2 3U H1NE 1996121900348 19961219 00348 NE 1996 12 19 HEEA968623 1 19961209 A 6210 7615009043051 TIP CAP SKRSKY S76 S76A 8143006 NE M/R SEPARATION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 15460 760223 SEPARATION ON THE TRAILING EDGE NEAR THE OUTBOARD END BEYOND THE MAX DEPTH ALLOWED. SENT TO COMPOSITE TECHNICS FOR INSPE CTION AND REPAIR. 1 G 7 2 3U H1NE 1996121900349 19961219 00349 SW 1996 12 19 HEEA968624 1 19961209 A 6210 412015300109 BLADE BELL 412 412 1182202 SW M/R SHIELD PEEL E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893P 7736 33012 EROSION SHIELD PEELING ON THE INBOARD END. THE OUTBOARD LEADING EDGE ABRASION STRIP HAS A COMPLETE CHORDWISE CRACK WITH SEPARATION NEAR THE INBOARD END OF THE STRIP. 1 G 7 2 4U H4SW 1996121900350 19961219 00350 1996 12 19 HEEA968625 4 19961209 A 3457 0110005400 GPS 150 BELL 206 206L3 1182108 SW COCKPIT INTERMITTENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 21497 51518 CURSOR AND ENTER BUTTON INTERMITTENT. 1 G 7 1 3U H2SW 1996121900351 19961219 00351 EU 1996 12 19 HEEA968626 1 19961209 A 6210 10515141 BLADE BOLKMS 105 BO105S 5626006 EU M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911FL 6058 S717 NOSE AND NECK SHELLS CRACKED IN THE ROOT AND CUFF AREA. 1 G 7 2 3U H3EU 1996121900352 19961219 00352 EU 1996 12 19 HEEA968627 1 19961209 A 6210 10515141 BLADE BOLKMS 105 BO105S 5626006 EU M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911FL 4774 S717 BLADE IS CRACKED. (NOSE AND NECK SHELLS CRACKED IN THE ROOT END AREAS) 1 G 7 2 3U H3EU 1996121900353 19961219 00353 EU 1996 12 19 HEEA968628 1 19961209 A 6210 10515141 BLADE BOLKMS 105 BO105S 5626006 EU M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911FL 6058 S717 BLADE IS CRACKED. (NOSE AND NECK SHELLS CRACKED IN THE ROOT AND CUFF AREAS) 1 G 7 2 3U H3EU 1996121900354 19961219 00354 EU 1996 12 19 HEEA968629 1 19961209 A 6210 10515141 BLADE BOLKMS 105 BO105S 5626006 EU M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911FL 4774 S717 BLADE IS CRACKED. (NOSE AND NECK SHELLS CRACKED IN THE ROOT END AREA) 1 G 7 2 3U H3EU 1996121900355 19961219 00355 SW 1996 12 19 HEEA968630 1 19961209 A 7810 212061201011 EJECTOR ASSY BELL 412 412 1182202 SW LT EXH CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893S 33022 EJECTOR IS CRACKED. (ROUND CRACK AND WORKING RIVETS) SENT TO ALPINE AEROTECH LTD. FOR INSPECTION AND REPAIR. 1 G 7 2 4U H4SW 1996121900356 19961219 00356 EU 1996 12 19 HEEA968631 1 19961209 A 7722 10590947 INDICATOR BOLKMS 105 BO105S 5626006 EU COCKPIT TOT ERROR E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3538T S350 INDICATOR HAS EXCESSIVE FRICTION ERROR THROUGHOUT SCALE. 1 G 7 2 3U H3EU 1996121900357 19961219 00357 EU 1996 12 19 HEEA968632 1 19961209 A 7722 50061036 INDICATOR BOLKMS 105 BO105S 5626006 EU EXH TEMP ERROR E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3538T S350 EXH TEMP HAS EXCESSIVE FRICTION ON HIGH END OF SCALE. 1 G 7 2 3U H3EU 1996121900358 19961219 00358 SW 1996 12 19 HEEA968633 1 19961209 A 6220 412010124109 BOLT BELL 412 412 1182202 SW M/R HEAD DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 23023 2585 33080 TUNGSTON COATING FLAKED OFF. SERIAL NUMBERS REMOVED ARE A28, A374, A395, AND A564. SEE MMIR# HEEA0008634 FOR ADDITION AL RETENTION BOLTS REPLACED. 1 G 7 2 4U H4SW 1996121900359 19961219 00359 SW 1996 12 19 HEEA968634 1 19961209 A 6220 412010124109 BOLT BELL 412 412 1182202 SW M/R DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 23023 2585 33080 TUNGSTON COATING FLAKED OFF. SERIAL NUMBERS REMOVED ARE A369, A863, A715, AND A27. SEE MMIR# HEEA0008633 FOR ADDITIONA L RETENTION BOLTS REPLACED. 1 G 7 2 4U H4SW 1996121900360 19961219 00360 SW 1996 12 19 HEEA968636 1 19961210 A 6230 214010500115 SWASHPLATE ASSY BELL 214 214ST 1182106 SW M/R OVERSPEED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 2471 28101 SWASHPLATE OVERSPEED INSPECTION. OVERSPEED TO 112%. (2500 HOUR OVERHAUL DUE) 2 G 7 2 4U H10SW 1996121900361 19961219 00361 SW 1996 12 19 HEEA968637 1 19961210 A 6220 204010937009 DAMPER ASSY BELL 212 212 1181420 SW M/R LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 1079U 31122 DAMPER LEAKING OIL. 1 G 7 1 4U H4SW 1996121900362 19961219 00362 EU 1996 12 19 HEEA968641 1 19961210 A 6420 350A33211905 BODY SNIAS 350 AS350B2 8680813 EU T/R WORN EXCESS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100R 1682 2862 BEARING BORE WORN BEYOND LIMITS AND BEARING SEPARATION. 1 G 7 1 3U H9EU 1996121900363 19961219 00363 SW 1996 12 19 HEEA968642 1 19961210 A 2800 222366621103 FUEL FILTER BELL 407 407 SW TEST BUTTON DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407PH 383 53003 FUEL FILTER TEST BUTTON WILL NOT MAKE LIGHT COME ON. 1 G 7 1 3U O H2SW 1996121900364 19961219 00364 SW 1996 12 19 HEEA968643 1 19961210 A 6400 206040344009 HANGER ASSY BELL 206 206L1 1182107 SW T/R OUT OF LIMITS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1072T 45385 SPRING I.D. OUT OF LIMITS AS PER ASB 206L-95-101 REV. A. 1 G 7 1 3U H2SW 1996121900365 19961219 00365 GL 1996 12 19 HEEA968648 2 19961210 A 7260 23055464 GEARBOX COVER 6894171 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ACCY DRIVE LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 137AE CAG33225 S851 CAE835356 ENGINE REMOVED DUE TO AFT TORQUE METER LEAK. UPON INSPECTION OF GEARBOX PARTS NOTED: TM BORE TO BUSHING HAS A LINE TO LINE FIT ON COVER ASSEMBLY. INSTALLED A PHI REWORKED GEARBOX COVER. 1 G 7 2 3U 3 U H3EU E4CE 1996121900366 19961219 00366 GL 1996 12 19 HEEA968649 2 19961210 A 7250 6851531 NOZZLE 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL NR 14 OUT OF LIMITS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 9190Y 258 CAT33140 S669 CAE834012 TURBINE REMOVED DUE TO 1750 HOUR INSPECTION. UPON INSPECTION OF TURBINE PARTS NOTED: GROOVED AND EXCESSIVE RUNOUT BEYO ND SERVICEABLE LIMITS ON #4 NOZZLE 3RD STAGE TIP PATH (T/R .0055) AND 4TH STAGE TIP PATH (T/R .005) MAX ALLOWABLE TIP P ATH RUNOUT.004. INSTALLED A DALLAS AIRMOTIVE OVERHAULED #4 NOZZLE. PART SENT TO DALLAS AIRMOTIVE, ATTN: EDITH WILLIAMS FOR 100% WARRANTY REPAIR PER GARY GENTZ INSTRUCTION. 1 G 7 2 3U 3 U H3EU E4CE 1996121900367 19961219 00367 SW 1996 12 19 HEEA968650 1 19961210 A 6500 212040506005 CASE ASSY BELL 412 412 1182202 SW T/R DEFECTIVE E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 SHIMS P/N 212-040-506-011 AND 212-040-506-013 IMPROPERLY GROUND. .000 BACKLASH UPON ASSEMBLY. 1 G 7 2 4U H4SW 1996121900368 19961219 00368 EU 1996 12 19 HEEA968651 1 19961210 A 6410 10531980 BLADE 10531713 BOLKMS 105 BO105S 5626006 EU T/R PAINT PEEL E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7136J 195 150 S830 ORIGINAL PAINTS PEELING AND RUBBER COATINGS DAMAGED ON BOTH BLADES. SEE MMIR# HEEA0008652 FOR ADDITIONAL T/R BLADE REPL ACED. 1 G 7 2 3U H3EU 1996121900369 19961219 00369 EU 1996 12 19 HEEA968652 1 19961210 A 6410 10531980 BLADE 10531713 BOLKMS 105 BO105S 5626006 EU T/R PAINT PEEL E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7136J 195 150 S830 ORIGINAL PAINTS PEELING AND RUBBER COATINGS DAMAGED ON BOTH BLADES. SEE MMIR# HEEA0008651 FOR ADDITIONAL T/R BLADE REPL ACED. 1 G 7 2 3U H3EU 1996121900370 19961219 00370 NE 1996 12 19 HEEA968653 1 19961210 A 6210 7615009100051A BLADE SKRSKY S76 S76A 8143006 NE M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 15460 7239 760223 TO COMPLY WITH 500 HOUR INSPECTION. BLADE HAS SEVERAL CRACKS ON THE TITANIUM STRIP WITH SEPARATION. THE CRACK AT STATI ON 123 HAS MULTIPLE BRANCHES. 1 G 7 2 3U H1NE 1996121900371 19961219 00371 EU 1996 12 19 HEEA968654 1 19961210 A 6320 4638201003 CENTER CASE BOLKMS 105 BO105S 5626006 EU M/R XMSN BORE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 54191 S804 CENTER CASE OUTPUT BORE WORN, CORROSION ON BASE FLANGE AND WEAR STEP ON SUPPORT PINS AND NOZZLE RING SURFACE. 1 G 7 2 3U H3EU 1996121900372 19961219 00372 NE 1996 12 19 HEEA968655 1 19961210 A 6220 7610608000050 DAMPER SKRSKY S76 S76A 8143006 NE M/R BUSHING DEFECT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1547D 760077 DAMPER INNER BUSHING OVERSIZED. 1 G 7 2 3U H1NE 1996121900373 19961219 00373 SW 1996 12 19 HEEA968656 1 19961210 A 7810 212061201012 EJECTOR ASSY BELL 412 412 1182202 SW RT EXH CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 EJECTOR IS CRACKED. 1 G 7 2 4U H4SW 1996121900374 19961219 00374 NE 1996 12 19 HEEA968657 1 19961210 A 6220 7610608000050 DAMPER SKRSKY S76 S76A 8143006 NE M/R BUSHING DEFECT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 792CH 760193 DAMPER INNER BUSHING OVERSIZED. 1 G 7 2 3U H1NE 1996121900375 19961219 00375 SW 1996 12 19 HEEA968658 1 19961210 A 7810 212061201012 EJECTOR ASSY BELL 412 412 1182202 SW RT EXH CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 RT EJECTOR ASSY IS CRACKED. 1 G 7 2 4U H4SW 1996121900376 19961219 00376 SW 1996 12 19 HEEA968659 1 19961210 A 7810 212061201011 EJECTOR ASSY BELL 412 412 1182202 SW LT EXH CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5759N 33002 LT EJECTOR ASSY IS CRACKED. 1 G 7 2 4U H4SW 1996121900377 19961219 00377 SW 1996 12 19 HEEA968660 1 19961210 A 3213 AB205050403031 CROSSTUBE BELL 412 412 1182202 SW GEAR ASSY DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 21498 36003 SCRIBE MARKS IN AREA OF CROSSTUBE NOT PERMITTED AS PER BHT412-CR&O. 1 G 7 2 4U H4SW 1996121900378 19961219 00378 SW 1996 12 19 HEEA968661 1 19961210 A 5330 212030101003 PANEL ASSY BELL 212 212 1181420 SW FUSELAGE MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 30888 PANEL EDGE IS TOO THICK. PANEL EDGE IS .150 ORIGINAL PANEL IS .090 #1 HANGER BEARING SUPPORT ON LEFT LEG WILL BE NEGATI VE SHIM BECAUSE PANEL IS TOO THICK. 1 G 7 1 4U H4SW 1996121900379 19961219 00379 SW 1996 12 19 HEEA968662 1 19961210 A 6210 206015001107 BLADE BELL 206 206L1 1182107 SW M/R DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 BLADE NOT ACCEPTABLE FOR PHI USE. BLADE RECEIVED WITH A DEPRESSION IN IT. 1 G 7 1 3U H2SW 1996121900380 19961219 00380 EU 1996 12 19 HEEA968663 2 19961210 A 7200 345437A23 ENGINE AEROSP SA316 SA315B 8680615 EU TMECA ARTST3 ARTOUSTE3B 60003 EU INTERNAL MAKING METAL E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3207T 1362 2441 ENGINE IS MAKING METAL. 1 G 7 1 4U 3 U H1IN E11N 1996121900381 19961219 00381 SW 1996 12 19 HEEA968664 1 19961210 A 5330 206033100261 SHELL ASSY BELL 206 206L1 1182107 SW FUSELAGE MIS MFG E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 TUB WEIGHT 72.054 LB. AVERAGE 55 LBS. INSERTS IMPROPERLY INSTALLED. SOME INSERTS CORRODED. FIBERGLASS ON FWD EDGE SA NDED THROUGH METAL. ANGLE FOR CONSOLE BROOM CLOSET INSTALLED TOO FAR RIGHT. AFT R/H CENTER FUEL CELL ANGLE TOO SHORT A T INBOARD.INSERTS MISSING FOR COVER OF FUEL LINERS ON PASSENGER FLOOR AREA. FUEL CELL SUMP RING CENTER TOO THICK. ORIN G WILL NOT SEAT PROPERLY. 1 G 7 1 3U H2SW 1996121900382 19961219 00382 NE 1996 12 19 HEEA968665 1 19961210 A 5321 7620402002050 PANEL SKRSKY S76 S76A 8143006 NE FUSELAGE FLOOR MIS REPAIRED E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 RECENTLY SENT TO DODS FOR REPAIR. EXISTING INSERTS IN FLOOR PANEL WERE LEFT INSIDE OLD CORE MATERIAL AND NEW TOP SKIN W ERE INSTALLED. THE OLD INSERTS INSIDE PANEL MAKE IT IMPOSSIBLE TO INSTALL NEW INSERTS THAT MUST GO THROUGH TOP AND BOTT OM SKINS. 1 G 7 2 3U H1NE 1996121900383 19961219 00383 SW 1996 12 19 HEEA968666 1 19961210 A 5321 206033103009 PANEL ASSY BELL 206 206L1 1182107 SW FUSELAGE MIS REPAIRED E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 3904L 45597 PANEL ASSY CORE TOO LONG AT CENTER OF PANEL WHERE FUEL LINE COVER NUT PLATES NEED TO BE INSTALLED. 1 G 7 1 3U H2SW 1996121900384 19961219 00384 NE 1996 12 19 HEEA968667 1 19961210 A 5321 7620402021041 FLOOR SKRSKY S76 S76A 8143006 NE LT OUTB MIS MFG E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 FLOOR DOESN'T HAVE PROPER JOGGLE ON INBOARD AND FWD. EDGE OF PANEL AS NEEDED TO GO BELOW (-051) LARGE FLOOR. 1 G 7 2 3U H1NE 1996121900385 19961219 00385 SW 1996 12 19 HEEA968668 1 19961210 A 2100 212030009097 DECK ASSY BELL 212 212 1181420 SW DROOP COMP HOLE MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 30888 DROOP COMPENSATOR THROUGH HOLE NOT DRILLED. 1 G 7 1 4U H4SW 1996121900386 19961219 00386 SW 1996 12 19 HEEA968669 1 19961210 A 5320 206033100261 SHELL ASSY BELL 206 206L1 1182107 SW LT FWD FUSELAGE MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 5742N 45477 INSERTS FOR L/H FORWARD FUSELAGE STEP INSTALLED TOO FAR FORWARD. "Z" ANGLE AT BASE OF AFT BOOM CLOSET ANGLES CRACKED ON UPPER R/H END IN RADIUS. INSERTS WERE NOT SENT WITH PANEL 1 G 7 1 3U H2SW 1996121900387 19961219 00387 EU 1996 12 19 HEEA968670 1 19961210 A 2435 150SG122Q STARTER SNIAS 350 AS350B2 8680813 EU START/GEN FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 350BZ 417 2653 HAS DEAD SPOT ON ARMATURE. STARTER WON'T TURN WHEN ENGAGED. 1 G 7 1 3U H9EU 1996121900389 19961219 00389 EU 1996 12 19 HEEA968672 1 19961211 A 2432 RG390E BATTERY BOLKMS 105 BO105S 5626006 EU CASE DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6607K 628 S841 BATTERY DEFECTIVE. EVALUATION OF CASE BULGE. 1 G 7 2 3U H3EU 1996121900390 19961219 00390 EU 1996 12 19 HEEA968673 1 19961211 A 2422 2A10001G INVERTER BOLKMS 117 BK117A4 5626017 EU AC GEN NOISEY E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911RZ 7092 INVERTER CAUSES NOISE INTERFERENCE IN #2 VHF AND NAV RADIOS. 1 G 7 2 3U H13EU 1996121900391 19961219 00391 EU 1996 12 19 HEEA968674 1 19961211 A 6520 4619002003 GEAR BOX BOLKMS 105 BO105S 5626006 EU INTERMED GRBOX MAKING METAL E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 54197 5776 S805 INTERMEDIATE GR BOX MAKING METAL, FRONT SEAL LEAKS. 1 G 7 2 3U H3EU 1996121900392 19961219 00392 NM 1996 12 19 HEEA968675 1 19961211 A 7110 900F2611400107 COWL ASSEMBLY DOUG MD900 MD900 3027375 NM LT ENG HOLES ELONGATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 9213P 385 90000013 LT COWL ASSY HOLES ELONGATED. 1 G 7 2 3U NC H19NM 1996121900393 19961219 00393 NM 1996 12 19 HEEA968676 1 19961211 A 7110 900F2611400108 COWL ASSEMBLY DOUG MD900 MD900 3027375 NM RT ENG HOLES ELONGATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 9213P 385 90000013 RT COWL ASSY HOLES ELONGATED. 1 G 7 2 3U NC H19NM 1996121900394 19961219 00394 GL 1996 12 19 HEEA968677 2 19961211 A 7313 6899001 NOZZLE BELL 230 230 1182149 SW ALLSN 250C 250C30G2 03013 GL ENG FUEL DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 236X 170 23015 FUEL NOZZLE NEEDS TO BE REPLACED, NOT ENOUGH THREADS TO ADD SHIMS. 1 G 7 2 3U 3 U NC H9SW E1GL 1996121900395 19961219 00395 EU 1996 12 19 HEEA968678 1 19961211 A 6220 350A31190703 STARFLEX SNIAS 350 AS350B2 8680813 EU M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100U 1619 2863 CRACK IN STARFLEX ARM LEADING EDGE. 1 G 7 1 3U H9EU 1996121900396 19961219 00396 EU 1996 12 19 HEEA968679 1 19961211 A 6520 350A33200403 SPIDER SNIAS 350 AS350B2 8680813 EU T/R SEALS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4000L 484 2873 SEALS BAD ON BOTH ENDS OF SPIDER. 1 G 7 1 3U H9EU 1996121900397 19961219 00397 EU 1996 12 19 HEEA968680 1 19961211 A 6520 350A33020005 GEAR BOX ASSY SNIAS 350 AS350B2 8680813 EU T/R MAKING METAL E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100U 537 2863 T/R GR BOX MAKING METAL. 1 G 7 1 3U H9EU 1996121900398 19961219 00398 EU 1996 12 19 HEEA968681 1 19961211 A 6220 117775P BALLJOINT SNIAS 350 AS350B2 8680813 EU STARFLEX WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100U 1084 2863 STARFLEX BALLJOINT WORN TO .015 MAXIMUM LIMIT. SCRAPPED LOCALLY. 1 G 7 1 3U H9EU 1996121900399 19961219 00399 SW 1996 12 19 HEEA968682 1 19961211 A 7931 407375004101 INDICATOR BELL 407 407 SW ENG OIL PRESS FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 141MA 28 53016 ENGINE OIL PRESSURE INDICATOR FAILED. 1 G 7 1 3U O H2SW 1996121900400 19961219 00400 SW 1996 12 19 HEEA968683 1 19961211 A 6220 407010111101 CONE SET BELL 407 407 SW M/R DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407PH 588 53003 COULD NOT TRACK AND BALANCE MAIN ROTOR SYSTEM. 1 G 7 1 3U O H2SW 1996121900401 19961219 00401 EU 1996 12 19 HEEA968684 1 19961211 A 6220 117775P STARFLEX SNIAS 350 AS350B2 8680813 EU FREQ ADAPTER WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100R 1778 2862 STARFLEX WORN FREQUENCY ADAPTER BEARINGS. 1 G 7 1 3U H9EU 1996121900402 19961219 00402 SW 1996 12 19 HEEA968685 2 19961211 A 7320 SYLC95481 LINEAR ACTUATOR DYLM735011 BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL ENGINE FAULTY E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 15909 INSPECTED BY ACCESSORY OVERHAUL SHOP AND FOUND ACTUATOR RETRACTED VERY SLOW AND INTERMITTENTLY. FOUND VENDOR REPAIRED M OTOR WAS DEFECTIVE. 1 G 7 1 3U 3 U H2SW E4CE 1996121900403 19961219 00403 SW 1996 12 19 HEEA968686 1 19961211 A 6730 214001970111 ACTUATOR ASSY BELL 214 214ST 1182106 SW M/R FROZEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 ACTUATOR FROZEN IN PLACE. 2 G 7 2 4U H10SW 1996121900404 19961219 00404 SW 1996 12 19 HEEA968687 1 19961211 A 6730 214001970111 ACTUATOR ASSY BELL 214 214ST 1182106 SW M/R DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 8045T 28101 KICKS OFF LINE AT 100-120 KNOTS. 2 G 7 2 4U H10SW 1996121900405 19961219 00405 SW 1996 12 19 HEEA968688 1 19961211 A 7810 212061202010 DUCT ASSY BELL 412 412 1182202 SW RT EXH CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 21498 36003 RT DUCT ASSY EXCESSIVE CRACKING. 1 G 7 2 4U H4SW 1996121900406 19961219 00406 SW 1996 12 19 HEEA968689 1 19961211 A 7810 212061202009 DUCT ASSY BELL 412 412 1182202 SW LT EXH CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 23023 33080 LT DUCT ASSY CRACKED SEVERAL PLACES AROUND MOUNT RING. 1 G 7 2 4U H4SW 1996121900407 19961219 00407 1996 12 19 HEEA968691 4 19961211 A 3421 102005403 GYRO BELL 206 206L3 1182108 SW COCKPIT HORIZ DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 363BH 51345 HORIZ GYRO UNRELIABLE. TIME SINCE REPAIR 0:00. 1 G 7 1 3U H2SW 1996121900408 19961219 00408 1996 12 19 HEEA968692 4 19961211 A 3416 10143501211 ALTIMETER BOLKMS 105 BO105S 5626006 EU COCKPIT ENCODER FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3533T S111 ENCODE ALTIMETER WILL NOT REPORT ALTITUDE ABOVE 2500 FEET. SENT TO THE RADIO SHOP FOR INSPECTION AND REPAIR. 1 G 7 2 3U H3EU 1996121900409 19961219 00409 1996 12 19 HEEA968693 4 19961211 A 2562 ELT910 ELT NARCO BOLKMS 105 BO105S 5626006 EU COCKPIT MALFUNCTION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 7136J S830 ELT COMES ON WITH EACH LIGHTNING BOLT. 1 G 7 2 3U H3EU 1996121900410 19961219 00410 SW 1996 12 19 HEEA968695 1 19961211 A 5510 206023119151 STABILIZER ASSY BELL 206 206L1 1182107 SW TAILBOOM MIS FIT E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 STABILIZER TOO THICK; WILL NOT ALIGN TO STABILIZER SUPPORTS THAT ATTACH TO TAILBOOM. REPAIRED BY DODS. 1 G 7 1 3U H2SW 1996121900411 19961219 00411 SW 1996 12 19 HEEA968696 1 19961211 A 5510 206023119151A STABILIZER ASSY BELL 206 206L1 1182107 SW TAILBOOM DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 DURING PAINT PREPARATION FOUND THAT EXISTING PRIMER COAT WAS PEELING OFF STABILIZER AND THAT PRIMER COAT WOULD NOT ADH ERE TO EXISTING PRIMER COAT. BLASTED ASSEMBLY TO REMOVE EXISTING PRIMER COAT. FOUND THAT STABILIZER SKIN HAD SEVERAL S MALLDENTS IN AREA WHERE SKIN WAS SANDED ON WITH HEAVY GRIT PAPER AND A DEEP SCRATCH COMING FROM AN INSERT FOR R/H LOWER SUPPORT PLATE. 1 G 7 1 3U H2SW 1996121900412 19961219 00412 SW 1996 12 19 HEEA968697 1 19961211 A 5510 206023119151 STABILIZER ASSY BELL 206 206L1 1182107 SW TAILBOOM MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 STABILIZER INSERTS FOR L/H AND R/H TAILBOOM ATTACHMENT SUPPORTS MISLOCATED. INSTALLED TOO FAR OFF. 1 G 7 1 3U H2SW 1996121900413 19961219 00413 SW 1996 12 19 HEEA968698 1 19961211 A 5210 206033600103 DOOR BELL 206 206L1 1182107 SW LT FWD DAMAGED E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 5007N 45184 DOOR HAS A FLAT AREA JUST BELOW WINDOW APPROXIMATELY 8" DOWN THE FULL WIDTH OF DOOR. 1 G 7 1 3U H2SW 1996121900414 19961219 00414 SW 1996 12 19 HEEA968699 1 19961211 A 5510 206023119151 STABILIZER ASSY BELL 206 206L1 1182107 SW TAILBOOM MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 2 INSERTS ON R/H FORWARD BOTTOM SIDE MISLOCATED. 4 INSERTS ON L/H AFT BOTTOM SIDE MISLOCATED. 1 G 7 1 3U H2SW 1996121900415 19961219 00415 NE 1996 12 19 HEEA968700 1 19961211 A 5321 7620402002049 PANEL SKRSKY S76 S76A 8143006 NE FLOOR MIS REPAIRED E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 EXISTING INSERTS FLOOR PANEL WERE LEFT INSIDE OLD CORE MATERIAL AND NEW SKINS WERE INSTALLED. OLD INSERTS INSIDE THE PA NEL MAKE IT IMPOSSIBLE TO INSTALL NEW STYLE INSERTS THAT MUST GO THROUGH TOP AND BOTTOM SKINS. 1 G 7 2 3U H1NE 1996121900416 19961219 00416 SW 1996 12 19 HEEA968701 1 19961211 A 6730 206076062003 CYLINDER BELL 206 206L1 1182107 SW SERVO SYS LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 5006F 17398 45181 BEARING UNSTAKED; LEAKING AT VALVE. 1 G 7 1 3U H2SW 1996121900417 19961219 00417 SW 1996 12 19 HEEA968702 1 19961211 A 6730 206076062003 CYLINDER (HR) BELL 206 206L1 1182107 SW SERVO SYS LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 3904L 18629 45597 OUTPUT SHAFT SEAL LEAKING AND TORN. 1 G 7 1 3U H2SW 1996121900418 19961219 00418 SW 1996 12 19 HEEA968703 1 19961211 A 5510 206023119151 STABILIZER ASSY BELL 206 206L1 1182107 SW TAILBOOM MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 BOTH ENDS OF STABILIZER ARE TOO THICK AND WON'T ALLOW WINGLET WITH ANGLES TO BE INSTALLED. 1 G 7 1 3U H2SW 1996121900419 19961219 00419 SW 1996 12 19 HEEA968704 1 19961211 A 3212 206050248107 FLOAT BAG ASSY BELL 206 206L1 1182107 SW INLET VALVE DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 FLOAT BAG ASSY UNBONDED INLET VALVE. 1 G 7 1 3U H2SW 1996121900420 19961219 00420 1996 12 19 HEEA968705 4 19961211 A 3422 206075606103 GYRO BELL 206 206L1 1182107 SW COCKPIT DG PRECESSES E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 83MT 45492 PRECESSES 20% EVERY 10 MINUTES. 1 G 7 1 3U H2SW 1996121900421 19961219 00421 SW 1996 12 19 HEEA968707 1 19961211 A 6730 214001970111 ACTUATOR ASSY BELL 214 214ST 1182106 SW ELEV FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 ELEVATOR ACTUATOR FAILED. 2 G 7 2 4U H10SW 1996121900423 19961219 00423 SW 1996 12 19 HEEA968710 1 19961213 A 2842 206063656001 TRANSMITTER BELL 206 206L1 1182107 SW FUEL PRESS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 27702 45300 FUEL PRESS TRANSMITTER WILL NOT INDICATE ABOVE ZERO. TIME SINCE REPAIR 0:00. 1 G 7 1 3U H2SW 1996121900424 19961219 00424 GL 1996 12 19 HEEA968711 2 19961213 A 7230 23038162 SHROUD HOUSING 23033193 BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL ENGINE OVER SPECS E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 8594X CAC91100 51531 CAE895162 RECEIVING INSPECTION REVEALED: AFT PILOT MEASURE .004 TO .006 OVERSPECS ON SHROUD HOUSING. (SPEC 10.199 - 10.200) 1 G 7 1 3U 3 U H2SW E1GL 1996121900425 19961219 00425 SW 1996 12 19 HEEA968712 1 19961213 A 6710 214001347005 ACTUATOR ROTARY BELL 412 412 1182202 SW M/R CONTROL BINDING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 293CA ROTARY ACTUATOR UNIT IS BINDING. 1 G 7 2 4U H4SW 1996121900426 19961219 00426 SW 1996 12 19 HEEA968713 1 19961213 A 6710 214001347005 ACTUATOR ROTARY BELL 412 412 1182202 SW CYCLIC FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 33008 36004 CYCLIC STICK DOES NOT MOVE ATT MODE. 1 G 7 2 4U H4SW 1996121900427 19961219 00427 NE 1996 12 19 HEEA968714 1 19961213 A 7600 7630103901102 ACUTATOR SKRSKY S76 S76A 8143006 NE ENGINE FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1545X 760050 ACTUATOR MOTOR TURNS -- SHAFT WILL NOT TURN. 1 G 7 2 3U H1NE 1996121900428 19961219 00428 SW 1996 12 19 HEEA968715 1 19961213 A 6330 206033554101 LINK ASSY BELL 206 206L3 1182108 SW M/R XMSN MOUNT SEPARATION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8591X 51495 LINK ASSY BEARING SEPARATION. 1 G 7 1 3U H2SW 1996121900429 19961219 00429 SW 1996 12 19 HEEA968716 1 19961213 A 6330 206033554101 LINK ASSY BELL 206 206L3 1182108 SW M/R XMSN MOUNT SEPARATION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8591X 51495 LINK ASSY BEARING SEPARATION. 1 G 7 1 3U H2SW 1996121900430 19961219 00430 SW 1996 12 19 HEEA968717 1 19961213 A 6330 206033554101 LINK ASSY BELL 206 206L3 1182108 SW M/R XMSN MOUNT SEPARATION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8591X 51495 LINK ASSY BEARING SEPARATION. 1 G 7 1 3U H2SW 1996121900431 19961219 00431 EU 1996 12 19 HEEA968718 1 19961213 A 6510 1053180301 SHAFT BOLKMS 105 BO105S 5626006 EU TAIL ROTOR PITTED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 91070 S145 T/R SHAFT PITTING PITTING AT INBOARD BEARING JOURNAL. 1 G 7 2 3U H3EU 1996121900432 19961219 00432 EU 1996 12 19 HEEA968719 1 19961213 A 6240 10594564 INDICATOR BOLKMS 105 BO105S 5626006 EU MAST MOMENT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 54197 S805 MAST MOMENT INDICATOR LIGHT COMES ON INTERMITTENTLY. OUT OF TOLERANCE. 1 G 7 2 3U H3EU 1996121900433 19961219 00433 EU 1996 12 19 HEEA968720 1 19961213 A 6240 10594575 TRANSMITTER BOLKMS 105 BO105S 5626006 EU MAST MOMENT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 54197 S805 TRANSMITTER LIGHT INTERMITTENTLY COMES ON. 1 G 7 2 3U H3EU 1996121900434 19961219 00434 EU 1996 12 19 HEEA968721 1 19961213 A 7714 DL40404 INDICATOR BOLKMS 105 BO105S 5626006 EU TRIPLE TACH WIRE BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7136J S830 TRIPLE TACH REAR CONNECTOR SEPARATED FROM CAN AND WIRE BROKEN. TIME SINCE REPAIR 0:00. 1 G 7 2 3U H3EU 1996121900435 19961219 00435 SW 1996 12 19 HEEA968722 1 19961213 A 7714 412075010109 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7128R 36007 #2 NEEDLE HAS NO INDICATION. TIME SINC E REPAIR 90:10. 1 G 7 2 4U H4SW 1996121900436 19961219 00436 1996 12 19 HEEA968723 4 19961213 A 3444 066106103 ALTIMETER BELL 206 206L3 1182108 SW RADAR ALT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3107N 51512 RADAR ALTIMETER INDICATOR PEGS OUT. 1 G 7 1 3U H2SW 1996121900437 19961219 00437 1996 12 19 HEEA968724 4 19961213 A 2210 2593996444 TARSYN BELL 412 412 1182202 SW AUTO FLIGHT INTERMITTENT E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3893N 33010 REPORTED #1 AFCS KICKS INTERMITTENTLY ON ROLL CHANNEL. TIME SINCE REPAIR 149:15. 1 G 7 2 4U H4SW 1996121900438 19961219 00438 1996 12 19 HEEA968725 4 19961213 A 3453 25410036 7000 RCU SKRSKY S76 S76A 8143006 NE COCKPIT LORAN DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1545K 760047 LORAN WILL NOT ACCEPT PROGRAMMING. DISPLAY FAILS CODE 4. 1 G 7 2 3U H1NE 1996121900439 19961219 00439 1996 12 19 HEEA968726 4 19961213 A 3442 MI5853011 INDICATOR P500 SKRSKY S76 S76A 8143006 NE RADAR MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 278X 760440 WHEN UNIT IS WX MODE AND VARIABLE GAIN IS TURNED OUT OF PRESET UNIT INTERMITTENTLY SHOWS CYCLE MODE WHEN IT SHOULD STILL SHOW WX AND UNIT ALSO INTERMITTENTLY GLITCHES PICTURE ON DISPLAY. TIME SINCE REPAIR 0:00. 1 G 7 2 3U H1NE 1996121900440 19961219 00440 EU 1996 12 19 HEEA968728 1 19961213 A 6240 10594575 TRANSMITTER BOLKMS 117 BK117A3 5626015 EU MAST MOMENT INTERMITTENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 401PH 7050 TORQUE TRANSMITTER INTERMITTENT. TIME SINCE REPAIR 31:25. 1 G 7 2 3U H13EU 1996121900441 19961219 00441 NM 1996 12 19 RAAA96B2046 1 19961216 A 3520 4566M37B042NM PBE BOEING 727 72722C 138400F NM CABIN FAILED A RAAA K NONE O OTHER CR CRUISE 1 AL 03 832RV 19098 FLIGHT ATTENDANT REPORTED ROW 22 PBE RED INDICATOR PIN PROTRUDING. CHANGED PBE DUE SEAL FAILURE. 2 L 7 3 4F A3WE 1996121900442 19961219 00442 WP 1996 12 19 CALA9601785 1 19961209 A 5320 JAMB DOUG DC9 DC932 3022066 WP BS 996 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12508 47797 INSPECTION FOUND THE FULL LENGTH OF LOWER AFT STAIRWELL DOOR JAMB CORRODED AT STA 996. A SPLICE REPAIR WAS PERFORMED IA W SRM 53-05, FIGURE 34, SECTIONS A-A AND D-D, ECRA 5310-03379. 2 L 7 2 4F A6WE 1996121900443 19961219 00443 NM 1996 12 19 CALA9601786 1 19961209 A 5713 STRINGER BOEING 737 737130 1384435 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16201 19018 INSPECTION FOUND A 1 INCH CRACK AT STRINGER 7R FASTENER ON RT WING UPPER SURFACE, WBL 200. A REPAIR STRAP WAS FABRICATE D AND INSTALLED IAW SRM 51-10-2 AND ECRA 5710-01765. 2 L 7 2 4F A16WE 1996121900444 19961219 00444 NM 1996 12 19 CALA9601787 1 19961211 A 5330 SKIN BOEING 737 737130 1384435 NM BS 240 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16201 19018 INSPECTION FOUND NLG WHEEL WELL UPPER SKIN CORRODED AFT OF ACCESS, STA 240. THE SKIN WAS REPAIRED IAW ECRA 5310-03378. 2 L 7 2 4F A16WE 1996121900445 19961219 00445 NM 1996 12 19 CALA9601788 1 19961211 A 5313 STRINGER BOEING 737 737130 1384435 NM BS 970-1000 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16201 19018 INSPECTION FOUND FUSELAGE STRINGER 24L CORRODED FROM FS 970 TO 1000. THE CORRODED SECTION OF STRINGER WAS REMOVED IAW S RM 51-10-6. STRINGER REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-3, 51-10-2 AND 51-30-2. 2 L 7 2 4F A16WE 1996121900446 19961219 00446 NM 1996 12 19 CALA9601789 1 19961211 A 5330 SKIN BOEING 737 737130 1384435 NM BS 380 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16201 19018 INSPECTION FOUND EXTERNAL FUSELAGE SKIN LAP BULGED AND ONE FASTENER SHEARED AT FS 380, STRINGER 26R. THE CORROSION WAS REMOVED IAW SRM 51-10-6. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-2, 51-10-2, 53-30-2 AND 51-30-2 . 2 L 7 2 4F A16WE 1996121900447 19961219 00447 NM 1996 12 19 CALA9601790 1 19961211 A 5330 SKIN BOEING 737 737130 1384435 NM BS 755 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16201 19018 INSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN AT BS 755, STRINGER 19R. THE CRACKED AREA WAS REMOVED IAW SRM 53-30-3. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, 51-10-2 AND 51-30-2. 2 L 7 2 4F A16WE 1996121900448 19961219 00448 NM 1996 12 19 CALA9601791 1 19961211 A 5315 FLOORBEAM BOEING 737 737130 1384435 NM BS 294.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16201 19018 INSPECTION FOUND CABIN FLOORBEAM CORRODED ON UPPER CHORD AT STA 294.5 FROM RBL 20 TO LBL 20. THE CORRODED SECTION OF FL OORBEAM WAS REMOVED, A NEW FLOORBEAM WAS FABRICATED AND INSTALLED IAW SRM 51-20-1, 51-10-2 AND 51-30-2. 2 L 7 2 4F A16WE 1996121900449 19961219 00449 WP 1996 12 19 CALA9601792 1 19961213 A 3260 802530 PROX UNIT DOUG DC10 DC1010 3022110 WP E/E COMPT INOPERATIVE A CALA O OTHER N FALSE WARNING CL CLIMB 1 SW 09 68043 46902 THE LEFT MAIN RED GEAR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION LEAVING BGR. THE INDICATION HAD A BRIEF PROBLEM HISTORY. THE FLIGHT WAS CONTINUED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PROXI MITY CONTROL UNIT AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 3 4F A22WE 1996121900450 19961219 00450 WP 1996 12 19 CALA9601793 1 19961215 A 2910 97608 HYD LINE DOUG DC10 DC1030 3023501 WP LT ENGINE RUPTURED A CALA A J UNSCHED LANDING DUMP FUEL K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 09 14062 47863 THE AIRCRAFT LOST NR 1 HYDRAULIC SYSTEM FLUID AFTER FLAP RETRACTION DEPARTING MAD. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO MAD WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE LT ENGINE DRIVEN PUMP PRESSURE LIN E TO MANIFOLD RUPTURED. THE PRESSURE LINE WAS REPLACED, THE NR 1 HYDRAULIC SYSTEM WAS SERVICED TO FULL. THE NR 1 ENGIN E WAS RUN AND NO LEAKS WERE NOTED. 2 L 7 3 4F A22WE 1996121900451 19961219 00451 NM 1996 12 19 CALA9601794 1 19961215 A 3350 1000677 LIGHT BOEING 727 727232 1384082 NM COCKPIT INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14788 20642 TWO CEILING EXIT LIGHTS BEHIND FIRST CLASS PARTITION WERE FOUND INOPERATIVE. MAINTENANCE FOUND THE 28V POWER FAIL CIRCU IT BREAKER NOT FULLY ENGAGED. THE CIRCUIT BREAKER WAS RESET AND OPERATION CHECKED GOOD. THE COCKPIT EMERGENCY EXIT LIG HT WAS ALSO FOUND INOPERATIVE. THE LIGHT WAS REMOVED AND REPLACED. 2 L 7 3 4F A3WE 1996121900452 19961219 00452 WP 1996 12 19 CALA9601795 1 19961215 A 3350 EMSE299A BATTERY DOUG DC10 DC1030 3023501 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14074 46911 THE EMERGENCY LIGHTS WOULD NOT TEST. CHANGING BATTERY CHARGER AT OVERWING POSITION DID NOT HELP. THE BATTERY AT DOOR 3 L WAS REPLACED AND THE EMERGENCY LIGHTS TESTED GOOD. 2 L 7 3 4F A22WE 1996121900453 19961219 00453 NM 1996 12 19 CALA9601796 1 19961211 A 5330 SKIN BOEING 737 737130 1384435 NM BS 188-251 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16201 19018 INSPECTION FOUND .5 INCH CRACKS IN LT FUSELAGE SKIN AT BS 188 TO 251, WL 207 TO 234. THE AREA WAS REPAIRED IAW SRM 51-3 0-2, BAC DRAWING NR 65-18420, AND EA 5310-01188. 2 L 7 2 4F A16WE 1996121900454 19961219 00454 NM 1996 12 19 CALA9601797 1 19961211 A 5320 WINDOW FRAME BOEING 737 737130 1384435 NM CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16201 19018 INSPECTION FOUND FORWARD LOWER CORNER OF NR 4 RT CABIN WINDOW FRAME CORRODED. THE WINDOW FRAME WAS REMOVED AND A NEW FR AME WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A16WE 1996121900455 19961219 00455 NE 1996 12 19 9626385517 2 19961215 A 7230 COMPRESSOR BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE NR 1 ENGINE FOD A NWAA O OTHER C F.O.D. IN INSP/MAINT 1 GL 01 517US 23205 716355 WHILE WAITING IN LINE TO DE-ICE, NR 1 ENGINE SHUT DOWN. A 727 IN FRONT HAD JUST THROTTLED UP AFTER BEING DE-ICED. MAIN TENANCE FOUND SNOW AND ICE PLUGGING INTERMEDIATE AREA OF COMPRESSOR. VISUAL AND BORESCOPE INSPECTION OF THE ENGINE WAS PERFORMED, NO DAMAGE WAS FOUND. ENGINE GROUND RUN AND ALL OPERATING PARAMETERS WERE NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996121900456 19961219 00456 NM 1996 12 19 9626396304 1 19961215 A 3350 LIGHT BOEING 747 747451 1384940 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 664US 23819 DURING LINE CHECK, FOUND LEFT 'E' ZONE EMERGENCY LIGHTS INOPERATIVE. RECONNECTED LIGHTS, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1996121900457 19961219 00457 NM 1996 12 19 9626406627 1 19961001 A 3230 69B803585 DOWNLOCK ACT BOEING 747 747251B 1384892 NM LT MLG FAILED A NWAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 01 627US 21709 DURING APPROACH, THE LEFT WING LANDING GEAR WOULD NOT EXTEND. AIRCRAFT EXECUTED A GO-AROUND AND ALTERNATELY EXTENDING T HE LANDING GEAR. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE LEFT WING LANDING GEAR DOWNLOCK ACTUATOR, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996121900458 19961219 00458 WP 1996 12 19 9626419607 1 19961214 A 3231 RETRACT MECH DOUG DC9 DC932 3022066 WP NLG DOOR OUT OF ADJUST A NWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 01 607NW 47232 VIBRATION FROM NOSE GEAR AREA AFTER TAKEOFF. FLIGHT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT FORWARD NOSE GEAR DOOR DOWN AND FORWARD LINK OUT OF ADJUSTMENT. ADJUSTED EYEBALL ON LINK, OPERATIONAL CHECK NORMA L. 2 L 7 2 4F A6WE 1996121900459 19961219 00459 NM 1996 12 19 UPS96221745 1 19961212 A 2782 14109592 SLAT ACTUATOR BOEING 727 72722C 138400F NM NR 2 SLAT INOPERATIVE A A IPXA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 SO 01 929UP 19092 INSPECTION TYPE-N/A, NR 2 SLAT WOULD NOT RETRACT AFTER T/O. COMPLETED AOM PROCEDURES, DUMPED FUEL AND RETURNED TO OAK. REPLACED NR 2 SLAT ACT AS PER MM 27-81-32, SLAT OPS CHKS NORMAL ON GROUND (P/N 141095-9-2) (S/N 3997L) OFF, (S/N 01405 BDJLMN) ON. 2 L 7 3 4F A3WE 1996121900460 19961219 00460 NM 1996 12 19 UPS96221746 1 19961122 A 5720 65217992 STRUT FITTING BOEING 727 72725C 138400H NM RT FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE-C, RT SIDE FUSELAGE TO WING STRUT FITTING, WBL 40 RT FWD LWR SPAR CHORD IS HEAVILY CORRODED. REMOVED, F ABRICATED AND INSTALLED STRUT FITTING IAW DWG 65-21799 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996121900461 19961219 00461 NM 1996 12 19 UPS96221747 1 19961122 A 5720 651628155 STIFFENER BOEING 727 72725C 138400H NM CTR WING SPAR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE-C, CENTER WING FRONT LWR SPAR STIFFENER LBL 42 HAS HEAVY CORROSION. REMOVED, FABRICATED AND INSTALLED R EPLACEMENT STIFFENER IAW DWG 65-16281 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1996121900462 19961219 00462 NM 1996 12 19 UPS96221748 1 19961119 A 5711 651850402 SPAR CHORD BOEING 727 72725C 138400H NM CTR WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE-C, CENTER WING TANK FWD LOWER SPAR CHORD SEVERELY CORRODED FROM LBL 26 TO LBL 40 REF N/R 588971. REMOVE D AND REPLACED SPAR CHORD IAW SRM 51-30-2, 51-30-10, 51-30-1. 2 L 7 3 4F A3WE 1996121900463 19961219 00463 NM 1996 12 19 UPS96221749 1 19961213 A 3350 BATTERIES BOEING 727 727108C 1384039 NM COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE-N/A, COCKPIT AND FOREWARD DOOR EMERGENCY EXIT LIGHTS INOP. INSTALLED NEW BATTERIES IN COCKPIT AND FOREW ARD DOOR EMERGENCY EXIT LIGHTS, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1996121900464 19961219 00464 WP 1996 12 19 UPS96821753 1 19961122 A 5711 SPAR DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE-C, CRACK INDICATIONS NOTED HOLE F IN SPAR, HOLES C AND D IN SKIN/SPAR INTERFACE OF RT WING C/W S/B 57 88 PER UPS EO DC8 5730. 2 L 7 4 4F RT 4A25 1996121900465 19961219 00465 WP 1996 12 19 UPS96821754 1 19961128 A 5711 SPAR CAP DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE-C, NR 2 TO NR 4 LEFT HAND LEADING EDGE SPAR ATTACHMENT HOLES HAVE CRACKS. REAMED HOLES 2 + 3 TO .500 R EAMED HOLE 4 TO .747 NO CRACKS NOTED. FABRICATED AND INSTALLED BUSHINGS ANGLE DOUBLERS, FILLERS AND STRESS COI NED ALL HOLES IAW DAC DWG J060232 AND REO 02487 ANAD DPS 3.67-56 2 L 7 4 4F RT 4A25 1996121900466 19961219 00466 WP 1996 12 19 UPS96821755 1 19961126 A 5330 ACCESS PLATE DOUG DC8 DC873F 302199F WP NR 2 FUEL TANK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE-C, NR 2 MAIN TANK ACCESS PLATE 505F LAND IS CRACKED AT FASTENERS LOCATION MARKED IN RED. REMOVED FASTE NERS, REMOVED DAMAGED AREA OF LAND, FABED DOUBLER AND FILLER IAW DC8 SRM 57-2-1. ALODINED AND PRIMED IAW DC8 SRM 51-1-8 , INSTALLED REPAIR IAW DC8 SRM 51-1-21 AND 57-2-1. 2 L 7 4 4F RT 4A25 1996121900467 19961219 00467 WP 1996 12 19 UPS96821756 1 19961127 A 5711 SPAR CAP DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE-C, NR 2 TO 5 HOLES HAVE CRACKS ON RT L/E SPAR ATTACHMENT HOLE INB OF NR 4 PYLON REAMED HOLES 2, 4, 5 TO .500 AND NR 3 HOLE TO .747, NO CRACKS NOTED. FABRICATED AND INSTALLED BUSHINGS, STRAPS, FILLERS AND ANGLES IAW DAC DW G J06032 AND DC8 SRM 51-9-0 AND REO 02493. 2 L 7 4 4F RT 4A25 1996121900468 19961219 00468 NE 1996 12 19 WWMA9500105 2 19961211 A 7261 5034T11PO5 PUMP SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT ENGINE DEFECTIVE A WWMA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 WP 15 280AE 340B280 LEFT ENGINE OIL TEMPERATURE EXCEEDED 122 DEGREES CELSIUS AND THE OIL PRESSURE DROPPED TO 35 PSI. MAINTENANCE FOUND EXCE SSIVE OIL IN THE TAILPIPE, REPLACED LEFT ENGINE OIL SCAVENGE PUMP, OIL PRESSURE TRANDUCER AND OIL TEMPERATURE SENSOR. P ERFORMED GROUND RUNS WITH NO PROBLEMS NOTED. 2 L 7 2 4T 4 T RT A52EU E8NE 1996121900492 19961219 00492 1996 12 19 SCNA96434 2 19961205 A 7261 OIL SYSTEM DOUG DC10 DC1030F 3023504 WP NR 2 ENGINE OVERSERVICED A SCNA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 601GC 47921 HAD SMOKE IN FLIGHT COMPARTMENT. TURNED OFF NUMBER 1 PACK AND PROBLEM STOPPED. WHILE TROUBLESHOOTING, DRAINED 1 GALLON FROM OVERSERVICED NUMBER 2 ENGINE, OPS CHECKED GOOD. 2 L 7 3 4F RT A22WE 1996121900493 19961219 00493 NM 1996 12 19 SCNA96435 1 19961207 A 3350 900835A BATTERY PACK BOEING 727 7272J4 1384006 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 288SC 20765 L2 DOOR EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY PACK FOR L2 DOOR EMERGENCY EXIT SIGN, OPS CHECK GOOD. 2 L 7 3 4F RT A3WE 1996121900494 19961219 00494 WP 1996 12 19 SCNA96436 1 19961211 A 3350 EMSE299 BATTERY PACK DOUG DC10 DC1010 3022110 WP CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 572SC 46977 FWD EMERGENCY BATTERY POWER SUPPLY FAILED EMERGENCY LIGHTING SELF TEST. REMOVED AND REPLACED FORWARD POWER SUPPLY BATTE RY PACK AND OPS CHECKED GOOD. 2 L 7 3 4F A22WE 1996121900495 19961219 00495 NM 1996 12 19 SCNA96437 1 19961211 A 3350 EXIT SIGN BOEING 727 727259 138408J NM CABIN MISSING A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 FOUND RIGHT FORWARD EMERGENCY EXIT LUMINESCENCE SIGN MISSING. REMOVED AND REPLACED RIGHT FORWARD EMERGENCY EXIT LUMINES CENT EXIT SIGN IN ACCORDANCE WITH MM 33-50-31. 2 L 7 3 4F A3WE 1996121900496 19961219 00496 NM 1996 12 19 DHL96701010 1 19961211 A 3260 327 BULB BOEING 727 72730C 1384009 NM NLG FAILED A DHLA O OTHER P NO WARNING INDICATION AP APPROACH 1 SO 01 701DH 19011 ON APPROACH, BROUGHT GEAR HANDLE TO DOWN POSITION, DID NOT GET GREEN NOSE GEAR INDICATION. WENT TO ALTERNATE PROCEDURE, PUT GEAR HANDLE BACK TO THE DOWN POSITION AND HAD NORMAL INDICATIONS, COMPLETED THE ALTERNATE PROCEDURE. CHECKED NOSE GEAR LOCK AND POSITION SWITCHES IAW MM 32-61, OPS CHECKS NORMAL. RELAMPED NOSE GEAR GREEN INDICATION LIGHT IAW MM 33-10 -41, OPS CHECKS GOOD. 2 L 7 3 4F A3WE 1996121900497 19961219 00497 WP 1996 12 19 RRXA96171 1 19961213 A 7830 O-RING DOUG DC8 DC862F 3021972 WP NR 2 ENG TR UNIT FAILED A RRXA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CL CLIMB 1 WP 15 996CF 46162 HYDRAULIC LOW LIGHT CAME ON AFTER TAKEOFF WITH A LOSS OF HYDRAULIC QUANTITY. REPLACED O-RING AT NR 2 ENGINE THRUST REVE RSER, CHECK VALVE IN PYLON AND LEAK CHECKS GOOD. 2 L 7 4 4F 4A25 1996121900498 19961219 00498 NE 1996 12 19 RRXA96172 2 19961213 A 7200 ENGINE DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C1 13802 NE NR 1 FLAMED OUT A RRXA E ENGINE SHUTDOWN X ENGINE FLAMEOUT DE DESCENT 1 WP 15 8079U 45947 NR 1 ENGINE FLAMED OUT DURING DESCENT THROUGH 15,000. CHECKED OIL FILTER CHIP DETECTORS, FUEL FILTER, IGNITION SYSTEM, FUEL TANK SELECTOR RIG, AND LEAK CHECK, NO DEFECTS NOTED. PERFORM CHECKS PER MM 71-00-46. FOUND VBV RIGGING TOO CLOSE, RE-RIGGED VBV PER MM. ENGINE RUN CHECKS OK. 2 L 7 4 4F 4 F RT 4A25 E2GL 1996121900499 19961219 00499 WP 1996 12 19 CKSA96361 1 19961213 A 5330 SKIN PATCH DOUG DC8 DC851 3021920 WP FWD FUSELAGE MISINSTALLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 804CK 45689 DURING A CHECK INSPECTION, FOUND FORWARD STATIC PORT SCAB PATCH TOO CLOSE. REMOVED SCAB PATCH AND INSTALLED REPAIR IAW EA 96-346 AIA SKETCH AIA/E/2442 AND 8110-3 DATED 12-11-96. FAA FINDING, NON-ROUTINE TASK CARD NR 91871. 2 L 7 4 4F 4A25 1996121900500 19961219 00500 SO 1996 12 19 SRAA961205 1 19961214 A 2120 DUCT LKHEED 382 382B 5264104 SO CARGO COMP DISCONNECTED A SRAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 907SJ 4248 ON CLIMBOUT AT FL 180, AIRCRAFT WOULD NOT PRESSURIZE. ACCOMPLISHED AIR TURNBACK TO CHS. FOUND CARGO COMPARTMENT AIR CO NDITIONING DUCT TO WATER SEPARATOR NOT ATTACHED. RECONNECTED DUCT, SYSTEM OPS CHECKED GOOD PER MM CH 21. 2 H 7 4 4T A1SO 1996121900501 19961219 00501 WP 1996 12 19 SRAA961207 1 19961215 A 3310 389598213 LIGHT PLATE DOUG DC8 DC873F 302199F WP COCKPIT SHORTED A SRAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 23 875SJ 46063 ON TAXI OUT, CREW REPORTED SMOKE IN COCKPIT COMING FROM LONGITUDINAL TRIM LIGHT PLATE, AIRCRAFT RETURNED TO BLOCK. FOUN D APPARENT INTERNAL SHORT IN LIGHT PLATE. DEFERRED LIGHT PLATE PER MEL 33-1, AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 1996121900502 19961219 00502 NM 1996 12 19 AWXA9600744 1 19961213 A 3350 BATTERY PACK BOEING 737 7373Y0 1384671 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 323AW 23684 DURING ROUTINE MAINTENANCE CHECK, FOUND R1 AND L1 DOOR EXTERIOR EMERGECNY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK ASSEMBLIES, SYSTEM OPS CK GOOD. 2 L 7 2 4F RT A16WE 1996121900503 19961219 00503 NM 1996 12 19 AWXA9600745 1 19961213 A 3397 WIRE BOEING 737 737277 1384570 NM CABIN DISCONNECTED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 185AW 22652 DURING ROUTINE MAINTENANCE CHECK, FOUND AFT SEAT LT SIDE EMERGENCY LIGHT INOP. RECONNECTED CONNECTOR, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 1996121900504 19961219 00504 NM 1996 12 19 AWXA9600746 1 19961214 A 3350 1060091101 LIGHT BOEING 737 737277 1384570 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 180AW 22647 DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 2 EMERGENCY EXIT SEAT LIGHT INOP. NEW LIGHT FIXTURE INSTALLED. 2 L 7 2 4F RT A16WE 1996121900505 19961219 00505 EU 1996 12 19 AWXA9600747 1 19961212 A 2150 761AO4AMDTB PACK INLET ACT AIRBUS 320 A320231 3930325 EU NR 2 PACK INOPERATIVE A AWXA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 28 624AW 16866 1700 55 STRONG SMELL OF SMOKE IN CABIN ASSOCIATED WITH NR 2 PACK FAILURE. REMOVED AND REPLACED NR 2 PACK INLET ACTUATOR PER AMM , OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 1996121900506 19961219 00506 EU 1996 12 19 AWXA9600748 1 19961214 A 2910 PACKING AIRBUS 320 A320231 3930325 EU GREEN HYD SYST LEAKING A AWXA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 WP 28 634AW 091 EMERGENCY DECLARED, HYDRAULIC GREEN RESERVOIR LOW LEVEL. FOUND PRIORITY VALVE LEAKING MAIN WHEEL WELL. REPLACED PACKIN GS PER 29-11-03, NO LEAKS FOUND. SERVICED HYDRAULIC SYSTEM, OK FOR SERVICE. 2 L 7 2 4F RT A28NM 1996121900507 19961219 00507 NM 1996 12 19 AWXA9600749 1 19961215 A 3350 831862 BATTERY PACK BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 188AW 22655 DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT ABOVE L-2 DOOR INOP. REMOVED AND REPLACED BATTERY PACK, STC - S A3432NM. 2 L 7 2 4F RT A16WE 1996121900508 19961219 00508 NM 1996 12 19 AWXA9600750 1 19961216 A 3350 1060091101 LIGHT BOEING 737 7373Q8 1384670 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 327AW 23507 DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT INOP AT ROW 21. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY, OPS CHECKS GOOD,STC - SA1889SO. 2 L 7 2 4F RT A16WE 1996121900509 19961219 00509 NM 1996 12 19 RAAA96B2047 1 19961217 A 3350 86210144 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 LT FWD OVERWING EMERGENCY EXIT EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE LOW CHARGE. 2 L 7 3 4F A3WE 1996121900510 19961219 00510 NM 1996 12 19 RAAA96B2048 1 19961217 A 3350 86210144 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 LT AFT OVERWING EMERGENCY EXIT EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE LOW CHARGE. 2 L 7 3 4F A3WE 1996121900511 19961219 00511 WP 1996 12 19 CALA9601798 1 19961010 A 5730 SKIN DOUG DC10 DC1030 3023501 WP WS 602 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 87070 48292 A-1 CRACK WAS FOUND IN THE RT WING LOWER LEADING EDGE SKIN AT XOS 602. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5730-014 21, REV A. 2 L 7 3 4F A22WE 1996121900512 19961219 00512 NM 1996 12 19 CALA9601799 1 19961010 A 3350 6012111RF POWER SUPPLY BOEING 747 747243B 1384830 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 33021 20520 INSPECTION FOUND OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. THE EMERGENCY EXIT LIGHT POWER SUPPLY WAS REMOVED AND REPLA CED. 2 L 7 4 4F A20WE 1996121900513 19961219 00513 NM 1996 12 19 CALA9601800 1 19961008 A 5730 SKIN BOEING 747 747243B 1384830 NM WS 400-420 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33021 20520 INSPECTION FOUND LT WING UPPER SURFACE OF SKIN CORRODED ABOVE REAR SPAR AT WS 400 TO 420, WBL 150. THE AREA WAS REPAIRE D IAW ECRA 5720-01553. 2 L 7 4 4F A20WE 1996121900514 19961219 00514 NM 1996 12 19 CALA9601801 1 19961008 A 5730 SKIN BOEING 747 747243B 1384830 NM WS 411-420 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33021 20520 INSPECTION FOUND RT WING UPPER SURFACE OF SKIN CORRODED ABOVE REAR SPAR AT WS 411 TO 420. THE AREA WAS REPAIRED IAW ECR A 5720-01551. 2 L 7 4 4F A20WE 1996121900515 19961219 00515 NM 1996 12 19 CALA9601802 1 19961017 A 5312 BULKHEAD BOEING 747 747243B 1384830 NM BS 400 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33021 20520 INSPECTION FOUND A .4375 INCH CRACK AT RT CORNER OF BULKHEAD BS 400. A CRACK OF UNIDENTIFIED LENGTH WAS FOUND AT LT COR NER OF BULKHEAD BS 400. THE AREAS WERE REPAIRED IAW ECRA 5310-03369. 2 L 7 4 4F A20WE 1996121900516 19961219 00516 NM 1996 12 19 CALA9601803 1 19961014 A 5711 SPAR BOEING 747 747243B 1384830 NM WS 405 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33021 20520 INSPECTION FOUND CORROSION ON REAR SPAR AFT FACE AT WS 405. THE AREA WAS REPAIRED IAW SRM 5720-01551. 2 L 7 4 4F A20WE 1996121900517 19961219 00517 NM 1996 12 19 CALA9601804 1 19961103 A 5320 ANGLE BOEING 747 747243B 1384830 NM BS 1940 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33021 20520 INSPECTION FOUND FLOOR ANGLE CORRODED AT STA 1940, RBL 10. THE CORROSION WAS REMOVED AND A REINFORCEMENT REPAIR WAS INS TALLED IAW SRM 53-10-07, 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1996121900518 19961219 00518 NM 1996 12 19 CALA9601805 1 19961030 A 5320 ANGLE BOEING 747 747243B 1384830 NM BS 1980 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33021 20520 INSPECTION FOUND FLOOR ANGLE CORRODED AT STA 1980, LBL 10. THE CORROSION WAS REMOVED, A REINFORCEMENT STIFFENER WAS FAB RICATED AND INSTALLED IAW SRM 53-10-07, 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1996121900519 19961219 00519 NM 1996 12 19 CALA9601806 1 19961030 A 5320 SPLICE BOEING 747 747243B 1384830 NM BS 1980 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33021 20520 INSPECTION FOUND CORROSION ON STRINGER SPLICE, STRINGER 50 AND ON FILLER UNDER SPLICE AT STA 1980 IN AFT CARGO COMPARTME NT. THE SPLICE AND CORROSION WERE REMOVED, A NEW DOUBLER WAS INSTALLED IAW SRM 51-10-01 AND 51-30-02. 2 L 7 4 4F A20WE 1996121900520 19961219 00520 NM 1996 12 19 CALA9601807 1 19961031 A 5320 FLOOR SUPPORT BOEING 747 747243B 1384830 NM BS 2350 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33021 20520 INSPECTION FOUND CORROSION ON FLOOR SUPPORT AT STA 2350, LBL 40. THE FLOOR SUPPORT WAS REMOVED AND A NEW PART WAS FABRI CATED AND INSTALLED IAW SRM 53-10-07. 2 L 7 4 4F A20WE 1996121900521 19961219 00521 NM 1996 12 19 CALA9601808 1 19961027 A 5320 ANGLE BOEING 747 747243B 1384830 NM BS 2280 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33021 20520 INSPECTION FOUND CORROSION ON FLOOR ANGLE AT STA 2280 NEAR DOOR R-5. THE ANGLE WAS REMOVED, A NEW PART WAS FABRICATED A ND INSTALLED IAW SRM 53-10-23 AND 51-10-02. 2 L 7 4 4F A20WE 1996121900522 19961219 00522 NM 1996 12 19 CALA9601809 1 19961113 A 5320 SUPPORT BOEING 747 747243B 1384830 NM BS 1300 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33021 20520 INSPECTION FOUND CORROSION ON GALLEY SUPPORT AT BS 1300 BETWEEN LBL 11 TO RBL 11. THE SUPPORT AND FILLER WERE REMOVED, A NEW SUPPORT AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-10-07, 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1996121900523 19961219 00523 NM 1996 12 19 CALA9601810 1 19961113 A 5320 SUPPORT BOEING 747 747243B 1384830 NM BS 1320 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33021 20520 INSPECTION FOUND CORROSION ON GALLEY SUPPORT AT STA 1320 BETWEEN RBL 11 TO 33. THE SUPPORT AND FILLER WERE REMOVED, A N EW SUPPORT AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-10-07. 2 L 7 4 4F A20WE 1996121900524 19961219 00524 NM 1996 12 19 CALA9601811 1 19961103 A 5315 FLOORBEAM BOEING 747 747243B 1384830 NM BS 480-500 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33021 20520 INSPECTION FOUND CORROSION ON FLOORBEAM AT STA 480 TO 500, RBL 40. THE CORROSION WAS REMOVED, A REINFORCEMENT ANGLE AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-10-01, 53-10-07 AND 51-10-02. 2 L 7 4 4F A20WE 1996121900525 19961219 00525 NM 1996 12 19 CALA9601812 1 19961119 A 5320 ANGLE BOEING 747 747243B 1384830 NM BS 1380 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33021 20520 INSPECTION FOUND CORROSION AT T-ANGLE, STA 1380 BETWEEN LBL 11 AND RBL 11. THE ANGLE AND FILLER WERE REMOVED, REPLACEME NT PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-07. 2 L 7 4 4F A20WE 1996121900526 19961219 00526 NM 1996 12 19 CALA9601813 1 19961119 A 5320 SUPPORT BOEING 747 747243B 1384830 NM BS 1350-1360 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33021 20520 INSPECTION FOUND CORROSION ON GALLEY SUPPORT BETWEEN STA 1350 AND 1360, LBL 11 TO 33. THE SUPPORT WAS REMOVED, A REPLAC EMENT SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-10-07. 2 L 7 4 4F A20WE 1996121900527 19961219 00527 NM 1996 12 19 CALA9601814 1 19961125 A 5313 STRINGER BOEING 747 747243B 1384830 NM BS 1700 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33021 20520 INSPECTION FOUND STRINGER 50L CORRODED AT STA 1700 IN AFT CARGO COMPARTMENT. THE CORRODED SECTION WAS REMOVED AND A NEW STRINGER SECTION AND TWO SUPPORTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-03, FIGURE 7. 2 L 7 4 4F A20WE 1996121900528 19961219 00528 NM 1996 12 19 CALA9601815 1 19961124 A 5313 STRINGER BOEING 747 747243B 1384830 NM BS 1700 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33021 20520 INSPECTION FOUND CORROSION AT STRINGER 51L, STA 1700 IN AFT CARGO COMPARTMENT. THE CORRODED SECTION WAS REMOVED, A NEW STRINGER SECTION AND TWO SUPPORTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-03, FIGURE 7. 2 L 7 4 4F A20WE 1996121900529 19961219 00529 NM 1996 12 19 CALA9601816 1 19961213 A 3246 654621520 AXLE BOEING 737 7373T0 1384582 NM NLG CRACKED A CALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 09 14342 23580 WHILE TURNING ONTO THE RUNWAY FOR TAKEOFF, THE CREW FELT THE NOSE STRUT BOTTOM OUT. THE CREW IN AIRCRAFT BEHIND THEM RE PORTED THAT THEY LOST A NOSE TIRE. THE AIRCRAFT WAS RETURNED TO THE GATE. MAINTENANCE FOUND THE NOSE STRUT AXLE CRACKE D. THE NOSE LOWER STRUT ASSEMBLY WAS REMOVED AND REPLACED IAW MM 32-21-11. A GEAR SWING WAS PERFORMED AND OPERATION CH ECKED GOOD. 2 L 7 2 4F RT A16WE 1996121900530 19961219 00530 WP 1996 12 19 CALA9601817 1 19961211 A 2752 59370525001 ACTUATOR DOUG DC9 DC981 3022081 WP LT TE FLAP LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 09 37882 48027 THE RT HYDRAULIC QUANTITY WAS LOST WHILE ON APPROACH. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND SEAL LEA KING AT LEFT INBOARD FLAP ACTUATOR. THE LT INBOARD FLAP ACTUATOR CYLINDER WAS REPLACED IAW MM 27-52-02. THE FLAPS AND ALL OTHER FLIGHT CONTROLS WERE OPERATED SEVERAL TIMES WITH NO DEFECTS OR LEAKS NOTED. THE HYDRAULIC SYSTEMS WERE SERVIC ED. 2 L 7 2 4F A6WE 1996121900531 19961219 00531 NM 1996 12 19 CALA9601818 1 19961024 A 5320 ANGLE BOEING 747 747243B 1384830 NM BS 835 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33021 20520 INSPECTION FOUND CORROSION ON FLOOR SUPPORT ANGLE AT STA 835 BETWEEN LBL 11 AND RBL 11. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-07. 2 L 7 4 4F A20WE 1996121900532 19961219 00532 NM 1996 12 19 CALA9601819 1 19961104 A 5320 SUPPORT BOEING 747 747243B 1384830 NM BS 540-560 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33021 20520 INSPECTION FOUND CORROSION ON FLOOR SUPPORT AT STA 540 TO 560 BETWEEN RBL 11.33 TO LBL 33.88. THE FLOOR SUPPORT WAS REM OVED AND A REPLACEMENT WAS FABRICATED AND INSTALLED IAW SRM 53-10-07 AND 51-30-02. 2 L 7 4 4F A20WE 1996121900533 19961219 00533 NM 1996 12 19 CALA9601820 1 19961022 A 5320 ANGLE BOEING 747 747243B 1384830 NM BS 2280 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33021 20520 INSPECTION FOUND CORROSION ON FLOOR ANGLE AT STA 2280, RBL 11. THE FLOOR ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICAT ED AND INSTALLED IAW SRM 53-10-07 AND 51-10-02. 2 L 7 4 4F A20WE 1996121900534 19961219 00534 NM 1996 12 19 CALA9601821 1 19961104 A 5320 SUPPORT BOEING 747 747243B 1384830 NM BS 520 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33021 20520 INSPECTION FOUND FLOOR SUPPORT CORRODED NEAR SEAT TRACK AT STA 520, LBL 11.33. A NEW FLOOR SUPPORT WAS FABRICATED AND I NSTALLED IAW SRM 53-10-07, 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1996121900535 19961219 00535 NM 1996 12 19 CALA9601822 1 19961024 A 5320 ANGLE BOEING 747 747243B 1384830 NM BS 2280-2340 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33021 20520 INSPECTION FOUND FLOOR ANGLE CORRODED BETWEEN STA 2280 AND 2340, LBL 40. A NEW FLOOR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996121900536 19961219 00536 NM 1996 12 19 CALA9601823 1 19961022 A 5320 ANGLE BOEING 747 747243B 1384830 NM BS 2350 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33021 20520 INSPECTION FOUND FLOOR ANGLE CORRODED AT STA 2350 BETWEEN BL 0 TO LBL 38. A NEW FLOOR ANGLE WAS FABRICATED AND INSTALLE D IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1996121900537 19961219 00537 NM 1996 12 19 CALA9601824 1 19961027 A 5320 ANGLE BOEING 747 747243B 1384830 NM BS 900 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33021 20520 INSPECTION FOUND FLOOR ANGLE CORRODED AT STA 900 BETWEEN LBL 11 AND RBL 11. THE FLOOR ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-07. 2 L 7 4 4F A20WE 1996121900538 19961219 00538 NM 1996 12 19 CALA9601825 1 19961027 A 5320 ANGLE BOEING 747 747243B 1384830 NM BS 2350 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33021 20520 INSPECTION FOUND FLOOR ANGLE CORRODED AT STA 2350, BL 0 TO RBL 38. THE ANGLE WAS REMOVED AND A NEW FLOOR ANGLE WAS FABR ICATED AND INSTALLED IAW SRM 53-10-07, 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1996121900539 19961219 00539 NM 1996 12 19 CALA9601826 1 19961017 A 5320 ANGLE BOEING 747 747243B 1384830 NM BS 870 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33021 20520 INSPECTION FOUND ANGLE CORRODED AT STA 870 BETWEEN RBL 11 AND LBL 11. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICA TED AND INSTALLED IAW SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900540 19961219 00540 NM 1996 12 19 QXEA9600488 1 19961211 A 3350 321430 BATTERY PACK DORNER DORNER DO32 DO328100 2996000 NM CABIN DISCHARGED A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 338PH 3029 FORWARD EMERGENCY LIGHT ABOVE FLIGHT ATTENDENT JUMP SEAT IS INOP. BATTERY PACK 5LK REPLACED AND LIGHT OPS CHECKED GOOD. 2 H 7 2 4T RT A45NM 1996121900541 19961219 00541 EU 1996 12 19 QXEA9600489 1 19961212 A 3397 WIRE FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN BROKEN A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 466US 11075 FLOOR PROXIMITY LIGHT ON SEAT 2AB IS INOP. WIRING FAULT REPAIRED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996121900542 19961219 00542 EU 1996 12 19 QXEA9600490 1 19961212 A 3350 1820 BULB FOKKER FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 491US 11156 EMERGENCY LIGHT IS INOP AT THE RIGHT HAND FORWARD EXIT. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996121900543 19961219 00543 NM 1996 12 19 QXEA9600491 1 19961212 A 2611 WIRE DHAV DHAV DHC8 DHC8102 2809003 NM NR 2 SMOKE DET BROKEN A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 818PH 58 CARGO SMOKE WARNING LIGHT ILLUMINATED DURING CLIMB. LIGHT REMAINED ON FOR 5 SECONDS THEN WENT OUT. LIGHT ILLUMINATED A GAIN THEN WENT OUT. AIRCRAFT RETURNED TO SEA AND LANDED WITHOUT FURTHER PROBLEMS. NO SIGNS OF SMOKE OR HEAT NOTED. BR OKEN WIRE AT NUMBER TWO SMOKE DETECTOR. CANNON PLUG REPAIRED, NUMBER ONE SMOKE DETECTOR REPLACED AS A PRECAUTIONARY MEA SURE, UNIT WAS SLOW TO TEST. SYSTEM OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 1996121900544 19961219 00544 SW 1996 12 19 QXEA9600492 1 19961213 A 2130 MS243312 SWITCH SWRNGN SA227 SA227AC 8780603 SW RT MLG MALFUNCTIONED A QXEA B EMER. DESCENT O OTHER CL CLIMB 1 NM 09 31168 AC599 LOSS OF CABIN PRESSURE AT 12,000 FT WITH +/- 2000 FT PER MINUTE FLUCTUATIONS. PROBLEM TRACED TO INTERMITTENT SQUAT SWIT CH ON RIGHT MAIN GEAR. SWITCH REPLACED AND ADJUSTED IAW MAINTENANCE MANUAL. SWITCH OPS CHECKED GOOD. 2 L 7 2 4T RT A8SW 1996121900545 19961219 00545 EU 1996 12 19 QXEA9600493 1 19961215 A 3350 6008905 POWER SUPPLY FOKKER FOKKER F28 F28MK1000 4990808 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 802PH 11017 EMERGENCY LIGHT BY SERVICE EMERGENCY DOOR IS INOP. POWER SUPPLY REPLACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996121900546 19961219 00546 NM 1996 12 19 QXEA9600494 1 19961216 A 3350 82410162007 CONTROL BOX DHAV DHAV DHC8 DHC8102 2809003 NM CABIN MALFUNCTIONED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 817PH 56 CABIN EMERGENCY LIGHTS WOULD NOT EXTINGUISH WHEN SELECTED OFF AT FIRST OFFICERS SWITCH. AIRCRAFT MUST BE POWERED DOWN A ND CYCLED OFF TO EXTINGUISH. EMERGENCY LIGHT CONTROL BOX REPLACED AND LIGHT OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 1996121900547 19961219 00547 EU 1996 12 19 QXEA9600495 1 19961216 A 3350 6008905 BATTERY PACK FOKKER FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 487US 11238 LEFT HAND AND RIGHT HAND AFT WING FAIRING EMERGENCY LIGHTS ARE DIM. AFT BATTERY PACK REPLACED AND LIGHTS OPS CHECKED GO OD. 2 L 7 2 4F RT A20EU 1996121900548 19961219 00548 NM 1996 12 19 96FDEA01702 1 19961215 A 2910 2249409521 TUBE DOUG MD11 MD11F 3023600 NM NR 3 HYD SYST BROKEN A FDEA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 611FE 48604 DURING CRUISE, NR 3 HYDRAULIC SYSTEM FAILED (LOSS OF FLUID). PUMPS WERE TURNED OFF WITH 2.4 GALLONS REMAINING. REPLACE D RT PUMP. CASE DRAIN REPLACED. P/N 224-9409-521. LEAK CHECKS GOOD, OK FOR SERVICE. 2 L 7 3 4F RT A22WE 1996121900549 19961219 00549 1996 12 19 SRAA961208 4 19961216 A 3422 25863331 DIR GYRO LKHEED 382 382E 526413U SO E/E COMP FAILED A SRAA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 GL 23 910SJ 4383 AFTER TAKEOFF, FOUND NR 1 COMPASS WOULD NOT TURN. DUMPED FUEL AND ACCOMPLISHED AIR TURNBACK TO CHS. FOUND NR 1 DIRECTI ONAL GYRO FAULTY. REMOVED AND REPLACED NR 1 DG, SYSTEM OPS CHECKED GOOD PER MM CH 34. 2 H 7 4 4T A1SO 1996121900550 19961219 00550 WP 1996 12 19 AALA961623 1 19961109 A 3520 44A35 SWITCH DOUG DC9 DC982 3022082 WP FLIGHT DECK DEFECTIVE A AALA G O2 MASK DEPLOYED N FALSE WARNING CL CLIMB 1 SW 07 403A 49314 DFW - FLT 1568 - EN ROUTE SJC/DFW - DURING CRUISE AT FL 370, CABIN OXYGEN LIGHT ILLUMINATED AND ALL PAX OXYGEN MASKS DRO PPED SUCCESSFULLY. CABIN ALTITUDE WAS 8000 FEET. AIRCRAFT PROCEEDED DFW AND LANDED WITHOUT INCIDENT. REPLACED OXYGEN PRESSURE CABIN AIRCONDITIONING ANEROID SWITCH. RESTOWED ALL PAX OXYGEN MASKS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996121900551 19961219 00551 WP 1996 12 19 AALA961586 1 19961030 A 3230 59650651 LOCK LINK DOUG DC9 DC982 3022082 WP NLG CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 410AA RM502 49321 BOS - DURING OVERNIGHT CHECK, NOSE LANDING GEAR UPPER LOCK LINK ASSEMBLY FOUND WITH LINK, P/N 3914464-11, CRACKED. REPL ACED NOSE LANDING GEAR UPPER LOCK LINK ASSEMBLY. PRECAUTIONARY REPLACED NOSE LANDING GEAR LOWER LOCK LINK ASSEMBLY. AC COMPLISHED NOSE LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996121900552 19961219 00552 EU 1996 12 19 AALA961618 1 19961107 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 8067A 510 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOR LIGHTS AT CROSS AISLE BETWEEN L4 AND R4 DOORS INOPERATIVE. REPLACED EMERGE NCY FLOOR LIGHT STRIPS AT CROSS AISLE BETWEEN L4 AND R4 DOORS. SYSTEM GROUND CHECKED NORMAL OPERATIONS. (M) 2 L 7 2 4F RT A35EU 1996121900553 19961219 00553 NM 1996 12 19 AALA961615 1 19961105 A 3350 A3060698101 CONNECTOR DOUG MD11 MD11 3023602 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1767A 48598 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT LEFT AISLE BETWEEN L3 AND L4 DOORS INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTOR AT LEFT AISLE BETWEEN L3 AND L4 DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. ( M) 2 L 7 3 4F RT A22WE 1996121900554 19961219 00554 WP 1996 12 19 AALA961640 1 19961113 A 3350 LIGHT DOUG DC10 DC1010 3022110 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 161AA 46942 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT LEFT AISLE BETWEEN PAX SEAT ROWS 32 AND 37 INOPERATIVE. REPLACE D EMERGENCY FLOOR LIGHT STRIP AT LEFT AISLE BETWEEN PAX SEAT ROWS 32 AND 37. SYSTEM GROUND CHECKED NORMAL OPERATION. ( M) 2 L 7 3 4F A22WE 1996121900555 19961219 00555 WP 1996 12 19 AALA961667 1 19961114 A 3350 A3060698101 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 491AA 49684 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS FROM FORWARD PART OF MAIN CABIN TO PAX SEAT ROW 21 INOPERATIVE. RE SECURRED EMERGENCY FLOOR LIGHT STRIP CONNECTOR AT PAX SEAT ROW 21. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996121900556 19961219 00556 EU 1996 12 19 AALA961501 1 19961010 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 80084 675 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY L4 DOOR INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BY L4 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996121900557 19961219 00557 EU 1996 12 19 AALA961498 1 19961009 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 80052 460 SJU - DURING OVERNIGHT CHECK, EMERGENCY POWER SUPPLY FOR EXIT LIGHTS AT L4 DOOR DID NOT TEST. RESEATED CANNON PLUG ON E MERGENCY POWER SUPPLY UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1996121900558 19961219 00558 WP 1996 12 19 AALA961570 1 19961028 A 3350 A3060698101 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 574AA 53151 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT IN FIRST CLASS CABIN INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR L IGHT STRIP CONNECTOR AT FORWARD PART OF FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996121900559 19961219 00559 WP 1996 12 19 AALA961549 1 19961024 A 3350 4TL1110B SWITCH HONEYWELL DOUG DC9 DC982 3022082 WP COCKPIT DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 560AA 53090 DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT OPERATION INTERMITTENT DURING TEST. REPLACED EMERGENCY FLOOR LIGHT COCKPI T OVERHEAD SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1996121900560 19961219 00560 NM 1996 12 19 AALA961520 1 19961016 A 5510 BEAM BOEING 727 727227 1384078 NM RT HORIZ STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 726AA 20733 TUL - FOUND CORROSION UPPER HORIZONTAL TE BEAM 2 PLACES BEYOND LIMITS. CUT OUT AND BLENDED AREAS. TREATED AND PRIMED, REPAIRED PER ESO 11697 AND SRM 55-10-6 FIG 1. (M) 2 L 7 3 4F A3WE 1996121900561 19961219 00561 NM 1996 12 19 AALA961519 1 19961016 A 5713 STRINGER BOEING 727 727227 1384078 NM BS 1166-1183 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 726AA 20733 TUL - FOUND STRINGER 22L HEAVILY CORRODED STATION 1166 TO 1183. REPAIRED STRINGER 22L, STATION 1166 TO 1183 PER SRM 53- 10-3 AND STATION 1183, STRINGER 22L AND FITTING REPLACED. (M) 2 L 7 3 4F A3WE 1996121900562 19961219 00562 NM 1996 12 19 AALA961515 1 19961016 A 5730 SKIN BOEING 727 727227 1384078 NM BS 839 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 726AA 20733 TUL - FOUND LOWER WING SKIN CORRODED ABOVE AFT HEAT EXCHANGER INBOARD DUCT MOUNT ANGLE. CORROSION ON BOTH SIDES OF ANGL E APPROX 3 INCH DIAMETER. REMOVED CORROSION AND REPAIRED PER ESO 11697, DATED 10-8-96. (M) 2 L 7 3 4F A3WE 1996121900563 19961219 00563 NM 1996 12 19 AALA961517 1 19961016 A 5330 SKIN BOEING 727 727227 1384078 NM BS 1166-1183 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 726AA 20733 TUL - FOUND SKIN BULGING AND FASTENER HEAD SHEAR BELOW AFT LAV SERVICE DOOR. REPAIRED AFFECTED AREA PER ESO 11697 DATED 2 OCT 1996. (M) 2 L 7 3 4F A3WE 1996121900564 19961219 00564 NM 1996 12 19 AALA961513 1 19961013 A 5730 65185443 SKIN BOEING 727 727227 1384078 NM BS 825 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 726AA 20733 TUL - FOUND LOWER WING SKIN CORRODED ABOVE THE AFT HEAT EXCHANGER INBOARD DUCT STATION 826. REMOVED AND BLENDED CORROSI ON PER SRM 51-10-6. PERFORMED THICKNESS CHECK RANGE FROM .209 TO .238, ORIGINAL THICKNESS .220-0226. (M) 2 L 7 3 4F A3WE 1996121900565 19961219 00565 NM 1996 12 19 AALA961511 1 19961016 A 5330 SKIN BOEING 727 727227 1384078 NM BS 680-700 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 726AA 20733 TUL - FOUND FUSELAGE SKIN LAP HAS 3 POPPED RIVETS AND BUBBLED SKIN STRINGER 26L. REMOVED DAMAGED SKIN AND INSTALLED DOU BLER REPAIR PER SRM 53-30-3 FIG 14 PAGE 80 A. (M) 2 L 7 3 4F A3WE 1996121900566 19961219 00566 WP 1996 12 19 AALA961550 1 19961023 A 5320 961224641 SHEAR TIE DOUG DC9 DC982 3022082 WP BS 1380 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 286AA 49298 FOUND SHEAR TIE CRACKED AT FUSELAGE FRAME 1380 BETWEEN LONGERON 13L AND 14L. REMOVED AND REPLACED SHEAR TIE. (M) 2 L 7 2 4F A6WE 1996121900567 19961219 00567 WP 1996 12 19 AALA961572 1 19961025 A 5320 CUSP DOUG DC9 DC982 3022082 WP BS 1148-1155 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 485AA 49678 TUL - FOUND HEAVY CORROSION ON RIGHT CUSP MEMBRANE APPROXIMATELY FROM STATION 1148 TO 1155. REMOVED DAMAGE AND INSTALLE D DOUBLER PER SRM 53-01, FIG 4 SHEET 3. (M) 2 L 7 2 4F A6WE 1996121900568 19961219 00568 WP 1996 12 19 AALA961554 1 19961024 A 5320 CUSP DOUG DC9 DC982 3022082 WP BS 674-712 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 485AA 49678 TUL - FOUND CORROSION ON CUSP MEMBRANE FROM FS 674 TO FS 712 RIGHT SIDE. REMOVED CORRODED CUSP. INSTALLED NEW CUSP MEM BRANE STATION 598-712 RIGHT. (M) 2 L 7 2 4F A6WE 1996121900569 19961219 00569 WP 1996 12 19 AALA961526 1 19961016 A 5320 CUSP DOUG DC9 DC982 3022082 WP BS 1231 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 216AA 49167 TUL - FOUND STATION 1231 LEFT CUSP HAS CORROSION AT LAP JOINT. REMOVED OLD CUSP AND INSTALLED NEW CUSP. (M) 2 L 7 2 4F A6WE 1996121900570 19961219 00570 WP 1996 12 19 AALA961530 1 19961018 A 5320 CUSP DOUG DC9 DC982 3022082 WP BS 228 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 216AA 49167 TUL - FOUND CUSP MEMBRANE CRACKED AT LIGHTENING HOLE, STATION 228, OUTBOARD OF NR 1 SEAT TRACK. REPLACED CUSP MEMBRANE. (M) 2 L 7 2 4F A6WE 1996121900571 19961219 00571 WP 1996 12 19 AALA961529 1 19961018 A 5320 CUSP DOUG DC9 DC982 3022082 WP BS 1287 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 216AA 49167 TUL - FOUND CUSP MEMBRANE CRACKED AT LIGHTENING HOLE, JUST FORWARD OF STATION 1287, OUTBOARD OF NR 1 SEAT TRACK. REPLAC ED CUSP MEMBRANE. (M) 2 L 7 2 4F A6WE 1996121900572 19961219 00572 WP 1996 12 19 AALA961505 1 19961009 A 5312 BULKHEAD DOUG DC9 DC982 3022082 WP BS 110 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 216AA 49167 TUL - FOUND CRACK IN PRESSURE BULKHEAD STATION 110 AFT OF LEFT TRUNNION. INSTALLED FIGURE DOUBLER PER SRM 53-04 FIG 38 SHEET 21. (M) 2 L 7 2 4F A6WE 1996121900573 19961219 00573 WP 1996 12 19 AALA961524 1 19961016 A 5320 CUSP DOUG DC9 DC982 3022082 WP BS 164-197 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 216AA 49167 TUL - FOUND CORROSION FORWARD ENTRY CUSP, STATION 164-197. REPLACED CUSP AND SUPPORT ANGLE. (M) 2 L 7 2 4F A6WE 1996121900574 19961219 00574 WP 1996 12 19 AALA961503 1 19961010 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 235 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 216AA 49167 TUL - FOUND NR 5 SEAT TRACK CORRODED AT STATION 235. ROUTED OUT DAMAGED AREA AND INSTALLED PLUG PER SRM 53-05 FIG 4A PA GE 8C. (M) 2 L 7 2 4F A6WE 1996121900575 19961219 00575 NM 1996 12 19 AALA961516 1 19961011 A 5320 NGLL6040175 ANGLE DOUG MD11 MD11 3023602 NM BS 2007 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1763 48553 TUL - FOUND CORROSION AT STATION 2007 NR 3 GALLEY SUPPORT CONNECTION TO T-ANGLE. INSTALLED REPAIR DOUBLER PER ESO 4100 DATED 10-10-96. (M) 2 L 7 3 4F RT A22WE 1996121900576 19961219 00576 NM 1996 12 19 AALA961514 1 19961010 A 5320 NLL6040175 ANGLE DOUG MD11 MD11 3023602 NM BS 2007 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1763 48553 TUL - FOUND CORROSION AT STATION 2007 NR 8 SEAT TRACK CONNECTION TO T-ANGLE. INSTALLED REPAIR PER ESO 4100, DATED 10-10 -96. (M) 2 L 7 3 4F RT A22WE 1996121900577 19961219 00577 NM 1996 12 19 AALA961512 1 19961011 A 5320 NLL6040175 ANGLE DOUG MD11 MD11 3023602 NM BS 2007 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1763 48553 TUL - FOUND CORROSION AT STATION 2007 NR 1 GALLEY SUPPORT CONNECTION TO T-ANGLE. FABRICATED T-ANGLE REPAIR INSTALLED FA STENERS PER ESO 4100, DATED 10-10-96. (M) 2 L 7 3 4F RT A22WE 1996121900578 19961219 00578 NM 1996 12 19 AALA961537 1 19961021 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 919 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1767A 48598 TUL - FOUND SEAT TRACK NR 5 HAS CORROSION JUST FORWARD OF STATION 919. PERFORMED SEAT TRACK PLUG REPAIR PER SRM 53-70-0 0 VOL 1 PAGE 8-9 FIG 4 SHEETS 1 AND 2. ALODINED, TREATED, PRIMED AND PAINTED BORE AREAS PER SRM 51-21-01 VOL 2. (M) 2 L 7 3 4F RT A22WE 1996121900579 19961219 00579 NM 1996 12 19 AALA961538 1 19961021 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 899-919 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1767A 48598 TUL - FOUND SEAT TRACK NR 8 HAS CORROSION BETWEEN STATION 899 AND 919. PERFORMED SEAT TRACK PLUG REPAIR PER SRM 53-70-0 0 VOL I, PAGE 8-9, FIG 4 SHEETS 1 AND 2 ALODINED, TREATED, PRIMED AND PAINTED PER SRM 51-21-01. (M) 2 L 7 3 4F RT A22WE 1996121900580 19961219 00580 NM 1996 12 19 AALA961536 1 19961021 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 919 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1767A 48598 TUL - FOUND SEAT TRACK NR 6 HAS CORROSION JUST FORWARD OF STATION 919. PERFORMED SEAT TRACK PLUG REPAIR PER SRM 53-70-0 0 VOL 1, PAGE 8-9, FIG 4 SHEETS 1 AND 2. ALODINED, TREATED, PRIMED AND PAINTED PER SRM 51-21-01, VOL 2. (M) 2 L 7 3 4F RT A22WE 1996121900581 19961219 00581 NM 1996 12 19 AALA961626 1 19961108 A 5312 BULKHEAD ANGLE DOUG MD11 MD11 3023602 NM BS 2007 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1762B 48552 TUL - FOUND CORROSION ON PRESSURE BULKHEAD T-ANGLE AT NR 3 GALLEY SUPPORT. REPAIRED ANGLE PER ESO 41000 DATED 11-27-96. INSTALLED ANGLE REPAIR 2 FASTENERS BEYOND DAMAGE. (M) 2 L 7 3 4F RT A22WE 1996121900582 19961219 00582 NM 1996 12 19 AALA961628 1 19961108 A 5312 BULKHEAD ANGLE DOUG MD11 MD11 3023602 NM BS 2007 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1762B 48552 TUL - FOUND CORROSION ON PRESSURE BULKHEAD T-ANGLE AT GALLEY NR 1 SUPPORT. REPAIRED PER ESO 41000 DATED 11/07/96. INST ALLED ANGLE REPAIR OVER DAMAGE 2 FASTENERS BEYOND. (M) 2 L 7 3 4F RT A22WE 1996121900583 19961219 00583 NM 1996 12 19 AALA961630 1 19961108 A 5312 BULKHEAD ANGLE DOUG MD11 MD11 3023602 NM BS 2007 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1762B 48552 TUL - FOUND CORROSION ON PRESSURE BULKHEAD T-ANGLE AT GALLEY SUPPORT NR 4. REPAIRED PER ESO NR 41000, DATED 11/07/96. I NSTALLED ANGLE REPAIR OVER DAMAGED AREA 2 FASTENERS BEYOND. (M) 2 L 7 3 4F RT A22WE 1996121900584 19961219 00584 NE 1996 12 19 AWXA960669 2 19961110 A 7200 ENGINE BOEING 737 7372E3 NM PWA JT8 JT8D15 52051 NE NR 2 FAILED A AWXA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 WP 28 138AW 44161 22792 AIR TURNBACK WHEN APPLYING TAKEOFF POWER 1 OR 2 MINOR COMPRESSOR STALLS WERE FELT WITH ALL ENGINE INSTRUMENTS INDICATING NORMAL SO TAKEOFF WAS CONTINUED. AT ABOUT 12,000 FEET, NR 2 ENGINE HAD RAPID COMPRESSOR STALLS AND EGT WAS RED. SHUTD OWN ENGINE. BORESCOPE PER P AND W TROUBLESHOOTING CHART 72-50. FOUND EVIDENCE OF FOD DAMAGE AT NGV AND MOLTEN METAL AT PLATFORM OF HPT TURBINE. REMOVED AND REPLACED NR 2 ENGINE IAW CARD R5M71005, R5M78002, R5M76001. TRIMMED ENGINE IAW R 5M71002. (M) 2 L 7 2 4F 4 F RT A16WE E2EA 1996121900585 19961219 00585 NE 1996 12 19 AWXA960578 2 19961010 A 7510 320115 ANTI-ICE VLV BOEING 737 737277 1384570 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE INOP A AWXA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 WP 28 184AW 11274 22651 PHX - FLT 2590 - ON TAKEOFF ROLL WHEN AUTO THROTTLE ADVANCES LEFT THROTTLE SPLIT WITH RIGHT THROTTLE LEAD EGT NR 1 EMG N EAR RED LINE DISCONNECT FOR AUTO THROTTLE TO BRING LEFT THROTTLE BUT NO HELP EGT STILL GOES TO MAX RED LINE. PERFORMED EPR LEAK TEST ENG NR 1 AND ENG NR 2. OPS NORMAL. REPLACED RIGHT ANTI-ICE VALVE. OPS CHECK GOOD. (M) 2 L 7 2 4F 4 F RT A16WE E2EA 1996121900586 19961219 00586 NE 1996 12 19 AWXA960577 2 19961010 A 7200 ENGINE BOEING 737 737277 1384570 NM PWA JT8 JT8D15 52051 NE NR 1 FOD A AWXA A E UNSCHED LANDING ENGINE SHUTDOWN O OTHER CL CLIMB 1 WP 28 189AW 22656 PHX - FLT 2545 - ON TAKEOFF CREW NOTED SPLIT BETWEEN NR 1 AND NR 2 POWER LEVERS. APPROACHING LEVEL OFF THE NR 1 POWER L EVER LOCKED AT MID POSITION. CREW ELECTED TO SHUT DOWN NR 1 ENGINE AND RETURN TO PHOENIX. PERFORMED LEAK CHECK PT6 AND PT7 ON BOTH ENGINES FOR THROTTLE SPLIT. COULD NOT DUPLICATE ON GROUND. FOREIGN OBJECT IN COWLING POSSIBLE INTERFERENC E. (M) 2 L 7 2 4F 4 F RT A16WE E2EA 1996121900587 19961219 00587 NM 1996 12 19 AWXA960641 1 19961022 A 5320 DOUBLER BOEING 737 7373G7 1384595 NM BS 370 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 PAE - FLT 7820 - DURING ROUTINE MAINTENANCE CHECK, FOUND BONDED DOUBLER TO BE CRACKED AT BS 370, BL0, WL 148. REPAIRED PER ER 3-53-33-18. TCO-PAN-96-151 RR 8110-3. (M) 2 L 7 2 4F RT A16WE 1996121900588 19961219 00588 NM 1996 12 19 AWXA960640 1 19961020 A 5753 SKIN BOEING 737 7373G7 1384595 NM RT TE FOREFLAP DELAMINATED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 PAE - FLT 7820 - DURING ROUTINE MAINTENANCE CHECK, FOUND RIGHT WING OUTBOARD FORE FLAP HAD DELAMINATED DENT ON UPPER SUR FACE 36 INCHES OUTBOARD OF INBOARD END. REPAIRED DAMAGED AREA, IAW SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 1996121900589 19961219 00589 NM 1996 12 19 AWXA960639 1 19961018 A 5315 BAC1505100617 FLOOR BEAM BOEING 737 7373G7 1384595 NM BS 294.5 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 PAE - FLT 7820 - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR BAM STATION 294.5 HAS CORROSION ON UPPER SURFACE AND AROU ND FASTENER HOLES, LBL 15 TO RBL 50, WL 208. REMOVED, FABRICATED AND INSTALLED TOP CHORD OF FLOOR BEAM AT BS 294.5, LBL 10 - RBL 65, WL 208 PER SRM 53-10-51, 51-40-02. (M) 2 L 7 2 4F RT A16WE 1996121900590 19961219 00590 NM 1996 12 19 AWXA960638 1 19961018 A 5315 BAC1505100617 FLOOR BEAM BOEING 737 7373G7 1384595 NM BS 312 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 PAE - FLT 7820 - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR BEAM STATION 312 HAS CORROSION ON UPPER SURFACE AND AROUN D FASTENER HOLES, RBL 12 TO LBL 17, WL 208. CUT OUT CORRODED AREA OF FLOOR BEAM AND REPAIRED PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1996121900591 19961219 00591 NM 1996 12 19 AWXA960637 1 19961018 A 5320 6517688125 MOPSILL BOEING 737 7373G7 1384595 NM BS 306-344 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 PAE - FLT 7820 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON UPPER SURFACE OF MOPSILL AT FORWARD DOR STATION 30 6 TO 344, LBL 55, WL 208. REMOVED CORRODED MOPSILL AND REPLACED WITH NEW IAW SRM 53-10-15. (M) 2 L 7 2 4F RT A16WE 1996121900592 19961219 00592 NM 1996 12 19 AWXA960636 1 19961019 A 5314 KEEL BEAM BOEING 737 7373G7 1384595 NM BS 500 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 PAE - FLT 7820 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON KEEL BEAM AT BS 5000 D PLUS 2, RBL 4, STRINGER 18, WL 148.5. REPAIRED PER ER 3-53-13-10. TCO-PAN-96-1502RR, FAA FORM 8110-3. (M) 2 L 7 2 4F RT A16WE 1996121900593 19961219 00593 NM 1996 12 19 AWXA960549 1 19960918 A 5311 FRAME BOEING 737 7373S3 1384711 NM BS 685 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 PAE - FLT 7806 - DURING ROUTINE SCHEDULED C-10 MAINTENANCE CHECK, FOUND LEFT MAIN LANDING GEAR FORWARD BOTTLE PIN BUSHIN G CORRODED. REPAIRED LEFT FRAME BS 685 PER ER 3-53-15-09, ENGINEERING REF, TCO-PAN-96-1300RR. (M) 2 L 7 2 4F RT A16WE 1996121900594 19961219 00594 NM 1996 12 19 AWXA960550 1 19960918 A 5311 FRAME BOEING 737 7373S3 1384711 NM BS 685 WORN A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 DURING ROUTINE SCHEDULED C-10 MAINTENANCE CHECK, FOUND RIGHT 685 FRAME BOTH BUSINGS FOR BOTTLE PIN ARE WORN AND MIGRATIN G. REPAIRED FRAME 685 RIGHT PER ER 3-53-15-09. ENGINEERING REF, TCO-PAN-96-1300RR. (M) 2 L 7 2 4F RT A16WE 1996121900595 19961219 00595 NM 1996 12 19 AWXA960548 1 19960916 A 5247 DOOR BOEING 737 7373S3 1384711 NM APU CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 PAE - FLT 7806 - DURING ROUTINE SCHEDULED C-10 MAINTENANCE CHECK, FOUND APU DOOR INNER SKIN CHAFED THROUGH 50 PERCENT. R EPAIRED DOOR IAW, SRM 52-00-01. (M) 2 L 7 2 4F RT A16WE 1996121900596 19961219 00596 NM 1996 12 19 AWXA960536 1 19960919 A 5320 MOPSILL BOEING 737 7373S3 1384711 NM BS 312-344 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 PAE - FLT 7806 - DURING ROUTINE SCHEDULED C-10 MAINTENANCE CHECK, FOUND CORROSION ON FORWARD ENTRY DOOR MOPSILL ON UNDER SIDE BS 312 TO 344, LBL 50, WL 208. REPAIRED IAW, SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1996121900597 19961219 00597 NM 1996 12 19 AWXA960535 1 19960913 A 5315 FLOOR BEAM BOEING 737 7373S3 1384711 NM BS 328 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 DURING ROUTINE SCHEDULED C-10 MAINTENANCE CHECK, FOUND CORROSION AROUND FLOOR BOARD HOLES ON FLOOR BEAM STATION 328, WL 208, LBL 51 AND LBL 28. REMOVED CORRODED TOP OF FLOOR BEAM AND REPAIRED IAW, SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1996121900598 19961219 00598 NM 1996 12 19 AWXA960534 1 19960919 A 5315 FLOOR BEAM BOEING 737 7373S3 1384711 NM BS 344 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 314AW 23733 PAE - FLT 7806 - DURING ROUTINE SCHEDULED C-10 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM AROUND FLOOR HOLES LBL 2 1 AND LBL 28, STATION 344, WL 208. REPAIRED FLOOR BEAM STATION 344, LB 21 - 31.5, WL 208 PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1996121900599 19961219 00599 NM 1996 12 19 AWXA960635 1 19961013 A 5320 65C807351 MOPSILL BOEING 737 7373G7 1384595 NM BS 967-991 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 PAE - FLT 7814 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON ASD MOPSILL FROM BS 967 TO 99, RBL 47, WL 208. RE MOVED AND REPLACED ASD MOPSILL, FROM BS 967 TO 991, RBL 47 IAW SRM 51-30-01 AND 51-40-02. (M) 2 L 7 2 4F RT A16WE 1996121900600 19961219 00600 NM 1996 12 19 AWXA960634 1 19961018 A 5315 BAC1505100617 FLOOR BEAM BOEING 737 7373G7 1384595 NM BS 98 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 PAE - FLT 7814 - DURING ROUTINE MAINTENANCE CEHCK, FOUND CORROSION ON FLOOR BEAM UPPER CHORD AT BS 98G5, LBL 21 THROUGH RBL 12, WL 208. REMOVED, FABRICATED AND INSTALLED NEW UPPER CHORD SECTION PER ER 3-53-1590. (M) 2 L 7 2 4F RT A16WE 1996121900601 19961219 00601 NM 1996 12 19 AWXA960633 1 19961013 A 5320 65C80735116 MOPSILL BOEING 737 7373G7 1384595 NM BS 957/988 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 157AW 23779 DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON AED MOPSILL AT BS 957 AND 988 LBL 50, WL 208. INSTALLED AFT ENTRY DOOR MOPSILL IAW SRM 51-40-02. REINSTALLED DRAIN AS PER 51-40-00, 51-30-01. (M) 2 L 7 2 4F RT A16WE 1996121900602 19961219 00602 NM 1996 12 19 96ZZZM1561 1 19961104 A 2751 10618411 TRANSMITTER BOEING 737 7372L9 1384497 NM RT TE FLAP MALFUNCTIONED A A ZZDA O OTHER N FALSE WARNING LD LANDING 1 SO 15 737Q 21279 FLT 822 - MCO-MCI - DURING FLAP EXTENSION THE RIGHT T/E FLAP STAYED AT 2 UNITS AND THE LEFT FLAP AT 1 UNIT CAUSING AN AS YMMETRIC SPLIT FLAP LOCKOUT CONDITION. THE MECHANIC IN MCI REMOVED AND REPLACED THE RIGHT FLAP POSITION TRANSMITTER PAR T NR 10-61841-1 PER BOEING 737 MAINTENANCE MANUAL 27-58-41 TO CORRECT THE DISCREPANCY AND RETURN THE AIRCRAFT TO SERVICE . REFERENCE AML-1 LOG PAGE 097-2459 FOR CORRECTIVE ACTION. (M) 2 L 7 2 4F RT A16WE 1996121900603 19961219 00603 WP 1996 12 19 USAAD96170 1 19961123 A 3350 AD20131A BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 985VJ 47208 DAY - FORWARD EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE. REPLACED FORWARD EMERGENCY LIGHT BATTERY PACK. (M) 2 L 7 2 4F A6WE 1996121900604 19961219 00604 NE 1996 12 19 USAAD96169 2 19961124 A 7261 OIL FILTER DOUG DC9 DC981 3022081 WP PWA JT8 JT8D217 52053 NE NR 2 ENGINE LOOSE A USAA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 828US 48028 FLT 1468 - FLL-DCA - TEN MILES NORTH OF MCO, RIGHT ENGINE LOW OIL PRESSURE WARNING CAME ON. GAUGES SHOWED PRESSURE DROP PING TO ZERO WHILE OIL QUANTITY ALREADY INDICATED ZERO. SHUT DOWN NR 2 ENGINE AND DIVERTED TO MCO. FOUND PULLED STUDS ON MAIN OIL FILTER. REPAIRED PER PRATT AND WHITNEY 72-61-01, REPAIR 38. (M) 2 L 7 2 4F 4 F A6WE E9NE 1996121900605 19961219 00605 WP 1996 12 19 USAAD96171 1 19961124 A 3350 AD20131A BATTERY PACK DOUG DC9 DC931 3022065 WP AFT LAV FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 939VJ 48120 FLOOR TRACK EMERGNCY LIGHTING INOPERATIVE AT SECTION 4, AFT CABIN. REPLACED POWER SUPPLY AND CHARGER, AFT LEFT LAV CEI LING. (M) 2 L 7 2 4F A6WE 1996121900606 19961219 00606 EU 1996 12 19 USAAF96123 1 19961124 A 3350 6008905 POWER SUPPLY FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 482US 11231 MAINTENANCE CHECK REVEALED AFT CABIN EMERGENCY LIGHTING INOP. MAINTENANCE REPLACED AFT RIGHT EMERGENCY LIGHTING POWER S UPPLY. (M) 2 L 7 2 4F RT A20EU 1996121900607 19961219 00607 EU 1996 12 19 USAAF96121 1 19961124 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 880US 11331 MAINTENANCE CHECK REVEALED LEFT FORWARD EMERGENCY LIGHT INOP. MAINTENANCE REPLACED THE BATTERY PACK. (M) 2 L 7 2 4F RT 1996121900608 19961219 00608 EU 1996 12 19 USAAF96122 1 19961124 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 866US 11310 MAINTENANCE CHECK REVEALED MID CABIN CEILING EXIT SIGN LIGHTS INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE ON LIGHT AS SEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT 1996121900609 19961219 00609 WP 1996 12 19 VJ960003R1 1 19961123 A 3397 L338D14 WIRE DOUG DC9 DC932 3022066 WP LT FLOOD LIGHT FAILED A VJ6A A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 11 933VV 47489 MCO-ATL - FLT 116 - A/C RETURNED TO MCO ON CLIMB-OUT, AS PRECAUTION DUE TO BURNING ODOR IN CABIN, REPORTED BY PAX. A F/ A REPORTED TO MX REP THAT A SMALL AMOUNT OF SMOKE WAS SEEN DURING LANDING. PRELIMINARY FINDINGS INDICATED LEFT GROUND P OWER WIRE AT FLOOR LIGHT ASSEMBLY WAS SHORTED. SUBSEQUENTLY, INSPECTED AND EVALUATED DAMAGE TO FORWARD CARGO COMPARTMEN T RELAY AND TRANSFORMER PANEL. AS A PRECAUTIONARY MEASURE, REPLACED VARIOUS RELAYS (R2-10, R2-11, R2-69, R1-134, R2-135 , R2-136, R2-155, AND TRANSFORMERS (T1-39, T1-7, T1-8, T1-9, T1-10, IN ADDITION TO THE DAMAGED WIRE AND ASSOCIATED HARDW ARE IAW DC9 MM. (M) 2 L 7 2 4F A6WE 1996121900610 19961219 00610 NM 1996 12 19 96ZZZM1562 1 19961121 A 5330 SKIN BOEING 737 737212 1384461 NM BS 727-907 CORRODED A RIVA K NONE O OTHER IN INSP/MAINT 1 SO 17 161FN 20521 EVALUATION OF A/C, FOR PROPOSAL OF BEING PLACED ON AN AIR CARRIER 121 CERTIFICATE. REVEALED THE FOLLOWING CONCERNS, DIS BONDING OF THE FUSELAGE SKIN FROM THE TEAR STRAPS DUE TO CORROSION FROM BS 727-907 AND STR 14R-21R. A/C REMAINING OUT O F SERVICE UNTIL A PERMANENT REPAIR CAN BE ACCOMPLISHED. (M) 2 L 7 2 4F A16WE 1996121900611 19961219 00611 1996 12 19 JBXA00031 4 19961125 A 2230 AUTO THROTTLE FOKKER F28 F28MK0100 4990807 EU NR 1/2 MALFUNCTIONED A JBXA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 05 104ML 11445 BOS - FLT 552 - DURING TAKEOFF ROLL, ABORTED TAKEOFF DUE TO AUTO THROTTLE FAULT 1 AND 2 THE AIRCRAFT RETURNED TO THE GAT E WHERE MAINTENANCE PERFORMED THRUST REVERSER TEST. T/R OPERATING NORMALLY. AFCAS FAULTED FAC MAINTENANCE PERFORMED AF ACS TEST OPS CHECK GOOD. (M) 2 L 7 2 4F RT 1996121900612 19961219 00612 EU 1996 12 19 VTZA97067 1 19961117 A 3080 3D314715 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU NR 2 ENGINE LOOSE A VTZA D RETURN TO BLOCK O N OTHER FALSE WARNING TX TAXI/GRND HDL 1 EA 27 309UE 41022 FLT 6531 - IAD-ORF - DURING TAXI, RETURNED TO GATE DUE TO CIRCUIT NR 2 LIGHT ILLUMINATED AND WOULD NOT GO OUT. MAINTENA NCE INSPECTED AND RESEATED CANNON ON CIRCUIT NR 2 PRESSURE SWITCH, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURNT TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996121900613 19961219 00613 1996 12 19 HALA96163 4 19961121 A 3417 CADC DOUG DC10 DC1010 3022110 WP E/E COMPT MALFUNCTIONED A HALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 13 119AA 46519 SEA - FLT 2025 - OVERSPEED WARNING ON TAKEOFF AT 90 KNOTS. ABORTED TAKEOFF. NO STICK SHAKER. PERFORMED AURAL WARNING CHECKS PER TAFI 31-51-00 PAGE 105. PERFORMED PITOT STATIC CHECKS. ALL SYSTEM CHECK NORMAL. REPLACED NR 1 CADC AS A PR ECAUTIONARY. (M) 2 L 7 3 4F A22WE 1996121900614 19961219 00614 WP 1996 12 19 USAAD96163 1 19961112 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN SHORTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 943VJ 47058 EMERGENCY LIGHTS CIRCUIT BREAKER POPS IN OFF POSITION. REPAIRED SHORTED WIRE IN AFT RIGHT LAV EMERGENCY LIGHT BATTERY P ACK. (M) 2 L 7 2 4F A6WE 1996121900615 19961219 00615 WP 1996 12 19 USAA960735 1 19961028 A 5320 T-CAP DOUG DC9 DC931 3022065 WP BS 996 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 958VJ 59849 47351 PIT - DURING Q-4/C-6 CHECK, FOUND LEVEL 1 CORROSION AT T-CAP AT FS 996 AFT T-CAP BETWEEN LONGERON L29 TO R29. SPLICE IN SECTION OF T-CAP PER SRM 53-03 FIG 37 AND EA 33802A. CORROSION LEVEL 1. (M) 2 L 7 2 4F A6WE 1996121900616 19961219 00616 WP 1996 12 19 USAAD96160 1 19961110 A 3350 60030451LB POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 824US 49143 FIRST CLASS OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. (M) 2 L 7 2 4F A6WE 1996121900617 19961219 00617 WP 1996 12 19 USAAD96161 1 19961109 A 2410 696233B CSD DOUG DC9 DC981 3022081 WP LEFT FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 811US 38963 48043 FLT 741 - BWI-CLT - DURING CLIMB, LT CSD LOW OIL PRESSURE LIGHT ILLUMINATED. CAPTAIN BELIEVED CSD DID NOT DISCONNECT. R ETURNED TO FIELD. MAINTENANCE FOUND THAT THE CSD FAILED, AND DID IN FACT DISCONNECT. A/C WAS RELEASED PER MEL 24-1A. THE CSD WAS LATER REPLACED. (M) 2 L 7 2 4F A6WE 1996121900618 19961219 00618 WP 1996 12 19 USAAD96162 1 19961110 A 3231 LATCH ROLLER DOUG DC9 DC931 3022065 WP LT MLG DOOR LOOSE A USAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 19 968VJ 47429 FLT 1188 - CLT-BHM- UPON GEAR EXTENSION AT BHM, THE GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED. A/C LANDED AFTER EMERGEN CY EXTENSION HANDLE WAS PULLED. MX FOUND THE LT MLG DOOR LATCH ROLLER ASSEMBLY LOOSE. TIGHTENED ASSEMBLY AND FERRIED T O PIT FOR FURTHER REPAIRS. RIGHT GEAR DOOR WAS REPLACED IN PIT. (M) 2 L 7 2 4F A6WE 1996121900619 19961219 00619 NE 1996 12 19 USAAD96159 2 19961107 A 7200 ENGINE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7B 52053 NE LEFT BIRDSTRIKE A USAA A UNSCHED LANDING C R E F.O.D. PARTIAL RPM/PWR LOSS VIBRATION/BUFFET CL CLIMB 1 EA 19 973VJ 47099 FLT 2123 - SYR-CLT - ON CLIMB-OUT AT 500 FEET AGL, INGESTED ONE OR MORE SEAGULLS INTO LEFT ENGINE. LEFT ENGINE EPR WENT FROM 1.95 TO 1.40 AND HAD LIGHT VIBRATION. RETURNED TO FIELD. REPLACED ENGINE. (M) 2 L 7 2 4F 4 F A6WE E2EA 1996121900620 19961219 00620 WP 1996 12 19 USAA960754 1 19961120 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 141 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 945VJ 72597 47066 PIT - DURING AGING/C-1 CHECK, FOUND CORROSION ON SKIN AT LONGERON 27L, FS 141 AREA. SPLICED IN NEW SECTION OF SKIN FROM FS 110 TO FS 178, 26L TO 26R PER EA 34046. (M) 2 L 7 2 4F A6WE 1996121900621 19961219 00621 NM 1996 12 19 USAASB96220 1 19961031 A 2613 20035008300 OVERHEAT MODULE BOEING 737 7372B7 1384560 NM E/E COMPT DEFECTIVE A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 270AU 16016 22882 MCO - FLT 1176 - DURING CLIMB-OUT, THE LT WING BODY O/H LIGHT ILLUMINATED AT FL 020. CREW ACCOMPLISHED NORMAL AND ABNOR MAL CHECKLIST. FLIGHT RETURNED TO FIELD AT MCO AS PRECAUTIONARY. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHO UT FURTHER INCIDENT. MAINTENANCE FOUND OVERHEAT CONTROL MODULE DEFECTIVE. REPLACED SAME. ALSO FOUND BARE WIRE ON SENS ING ELEMENT CANNON PLUG D864 IN AFT SECTION 56. REPLACED CANNON PLUG D864 (P/N 35303-10). OPS CHECK OF WING-BODY OVERH EAT SYSTEM NORMAL. (M) 2 L 7 2 4F A16WE 1996121900622 19961219 00622 NM 1996 12 19 USAA960732 1 19961105 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 950 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 37396 22885 ROA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK AFT ENTRY DOOR CUT OUT FORWARD LOWER CORNER FUSELAGE SKI N (STRINGER 17L BS 950). REMOVED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 24. (M) 2 L 7 2 4F A16WE 1996121900623 19961219 00623 NM 1996 12 19 USAA960734 1 19961105 A 5330 SKIN BOEING 737 737201 1384454 NM BS 950 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 223US 48416 21665 ROA - DURING CX-6 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 1.5 INCH CRACK AFT ENTRY DOOR CUT OUT FORWARD LOWER CORNER (STRINGER 17L, BS 950) FUSELAGE SKIN. REMOVED CRACK AND INSTALLED REPAIR, REPAIRED PER SRM 53-30-3, FIG 24. (M) 2 L 7 2 4F A16WE 1996121900624 19961219 00624 NM 1996 12 19 USAASB96226 1 19961109 A 5610 5893543109 WINDSHIELD BOEING 737 737201 1384454 NM LT COCKPIT CRACKED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 233US 952 22273 PIT - FL 820 - ON CLIMB-OUT, CAPTAINS FORWARD WINDSHIELD ARCED AND THEN CRACKED. FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE WINDSHIELD. (M) 2 L 7 2 4F A16WE 1996121900625 19961219 00625 NM 1996 12 19 USAASB96225 1 19961108 A 2612 876635 CONNECTOR BOEING 737 737201 1384454 NM RT ENGINE LOOSE A USAA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 EA 19 228US 21817 RSW - FL 1429 - ON APPROACH TO RSW, CREW RECEIVED THE FIRE WARNING FOR THE NR 2 ENGINE. CREW SHUT DOWN ENGINE AND FIRED BOTH BOTTLES. FLIGHT LANDED AT RSW WITH NO FURTHER INCIDENT. MAINTENANCE INSPECTED THE ENGINE AND FOUND NO EVIDENCE O F FIRE. THE D1096 CONNECTOR TO THE M337 DETECTOR WAS FOUND LOOSE. THE CONNECTOR WAS CLEANED AND SECURED, AND SUBSEQUEN TLY REPLACED. (M) 2 L 7 2 4F A16WE 1996121900626 19961219 00626 NM 1996 12 19 USAA960737 1 19961110 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 297 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 268AU 38828 22880 ROA - DURING CX-5 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 1 INCH CRACK FORWARD GALLEY DOOR CUT OUT AFT LOWER CORNER FUSELAGE SKIN (STRINGER 17 R BS 297). REMOVED CRACK AND INSTALLED DOUBLER, REPAIRED PER T/R 53-10-19 REV A. (M) 2 L 7 2 4F A16WE 1996121900627 19961219 00627 NM 1996 12 19 USAA960753 1 19961121 A 5320 DOUBLER BOEING 737 737201 1384454 NM BS 377.5-379 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 237US 41590 22353 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK SKIN DOUBLER BS 377.5 TO BS 379 LBL 3 WL 148.5. FABRICAT ED AND INSTALLED NEW DOUBLER, REPAIRED PER SRM 53-30-2 AND SRM 51-10-1. (M) 2 L 7 2 4F A16WE 1996121900628 19961219 00628 NM 1996 12 19 USAA960752 1 19961121 A 5330 SKIN BOEING 737 737201 1384454 NM BS 379 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 237US 41590 22353 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1.25 INCH CRACK WL 148.5 LBL 4, BS 279 SKIN. INSTALLED EXT DOUBELR WT A DDED 9.4 LBS AT BS 279, REPAIRED PER TR 53-30-4. (M) 2 L 7 2 4F A16WE 1996121900629 19961219 00629 NM 1996 12 19 USAA960751 1 19961121 A 5320 WEB BOEING 737 737201 1384454 NM BS 708 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 237US 41590 22353 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK BS 708 STRINGER 18R, SHEAR BEAM WEB. INSTALLED REPAIR KI T, REPAIRED PER EO NR 5393G256 AND BOEING DRAWING NR 65C29228. (M) 2 L 7 2 4F A16WE 1996121900630 19961219 00630 NM 1996 12 19 USAA960750 1 19961121 A 5320 CHORD BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 237US 41590 22353 INT - DURING Q-3 CHECK NDT INSPECTION, FOUND .25 INCH CRACK INBOARD AT FORWARD OUTBOARD HOE AT INTERSECTION OF STRINGER 18 A OUTBOARD STRAP AND BS 727 CHORD (RIGHT SIDE). INSTALLED REPAIR/MOD, REPAIRED PER EO 5394G068. (M) 2 L 7 2 4F A16WE 1996121900631 19961219 00631 NM 1996 12 19 USAA960749 1 19961121 A 5330 SKIN BOEING 737 737201 1384454 NM BS 1156 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 237US 41590 22353 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 4 INCH CRACK IN SKIN STATION 1156, LBL 12. INSTALLED DOUBLER (REPLACED DOUBLER), REPAIRED PER SRM 53-30-3, FIG 6. (M) 2 L 7 2 4F A16WE 1996121900632 19961219 00632 NM 1996 12 19 USAA960747 1 19961121 A 5312 BULKHEAD BOEING 737 737201 1384454 NM BS 1023 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 237US 41590 22353 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 2 INCH CORRODED AREA AT BULKHEAD BS 1023 RBL 1 INCH WL 195. I NSTALLED EXT REPAIR, REPAIRED PER SRM 53-10-4/53-10-3. CORROSION TASK NR C53-202-01, CORROSION LEVEL 1. (M) 2 L 7 2 4F A16WE 1996121900633 19961219 00633 NM 1996 12 19 USAA960746 1 19961121 A 5320 SPLICE BOEING 737 737201 1384454 NM BS 362-363 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 237US 41590 22353 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 2 INCH CORRODED AREA STRINGER SPLICE BS 362 TO 363, STRINGER 27L. INSTALLED NEW SPLICE WITH 2 ADDITIONAL FASTENER ROWS, REPAIRED PER EA NR 41756. CORROSION TASK NR C53-202-01, COR ROSION LEVEL 1. (M) 2 L 7 2 4F A16WE 1996121900634 19961219 00634 NM 1996 12 19 USAA960745 1 19961121 A 5320 CHORD BOEING 737 737201 1384454 NM BS 727 CRACK A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 237US 41590 22353 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK INDICATION INSIDE FORWARD UPPER FASTENER HOLE OUTSIDE CHO RD BS 727, STRINGER 18 A STRAP. INSTALLED REPAIR MOD, REPAIRED PER EO 5394G068. (M) 2 L 7 2 4F A16WE 1996121900635 19961219 00635 NM 1996 12 19 USAA960744 1 19961121 A 5311 FRAME BOEING 737 737201 1384454 NM BS 967 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 237US 41590 22353 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 2 INCH CORROSION AT FRAME, BS 967. INSTALLED REPAIR ANGLE, RE PAIRED PER SRM 53-10-4. CORROSION TASK NR C53-202-01, CORROSION LEVEL 1. (M) 2 L 7 2 4F A16WE 1996121900636 19961219 00636 NM 1996 12 19 USAA960743 1 19961121 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 373-378 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 237US 41590 22353 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 5 INCH CORRODED AREA STRINGER 27R, BS 373 TO BS 378 (STRINGER) . INSTALLED STRINGER REPAIR AND REPAIRED PER SRM 53-10-3, FIG 1. CORROSION LEVEL 1, CORROSION TASK NR C53-202-01. (M) 2 L 7 2 4F A16WE 1996121900637 19961219 00637 NE 1996 12 19 USAASB96241 2 19961120 A 7510 CONNECTOR BOEING 737 737201 1384454 NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE LOOSE A USAA A E UNSCHED LANDING ENGINE SHUTDOWN M OVER TEMP CL CLIMB 1 EA 19 223US 21665 JAX - FL 1420 - EN ROUTE FROM MCO-IAD - AT FL 290, THE NR 1 ENGINE OIL TEMPERATURE ROSE TO 140 DEGREES CELSIUS. CREW SH UT DOWN THE NR 1 ENGINE AND DIVERTED TO JAX. FLIGHT LANDED WITHOUT FURTHER INCIDENT. CAPTAINDID DECLARE AN EMERGENCY. TOTAL SINGLE ENGINE TIME WAS 10 MINUTES. MX FOUND THE CANNON PLUG LOOSE ON THE NR 1 ENGINE FUEL HEAT VALVE. RECONNECT ED CANNON PLUG. OPS CHECK NORMAL. DRAINED OIL FROM NR 1 ENGINE AND INSPECTED OIL SCREEN FOR FOREIGN MATTER. NONE FOUN D. RESERVICED ENGINE WITH OIL. RAN ENGINE, NO LEAKS OR DEFECTS NOTED. (M) 2 L 7 2 4F 4 F A16WE E2EA 1996121900638 19961219 00638 NM 1996 12 19 USAA960748 1 19961121 A 5330 SKIN BOEING 737 737201 1384454 NM BS 967 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 237US 41590 22353 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 3 INCH CORRODED AREA BS 967 BETWEEN STRINGER 27L AND STRINGER 27R SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. CORROSION TASK NR C53--202-01, CORROSION LEVEL 1. (M) 2 L 7 2 4F A16WE 1996121900639 19961219 00639 NM 1996 12 19 USAA960741 1 19961117 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 996-1016 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 239US 41484 22354 ROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 20 INCH CORROSION AT STRINGER 26 RIGHT BS 996 TO 1016. REMOV ED CORROSION AND INSTALLED NEW STRINGER AND SPLICE, REPAIRED PER SRM 53-10-3, FIG 1. (M) 2 L 7 2 4F A16WE 1996121900640 19961219 00640 NM 1996 12 19 USAA960740 1 19961117 A 5313 STRINGER BOEING 737 737201 1384454 NM 41484 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 239US 22354 ROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 68 INCH CORROSION AT STRINGER 27 LEFT BS 948 TO 1016. REMOVE D CORROSION AND INSTALLED NEW STRINGER AND SPLICE, REPAIRED PER SRM 53-10-3, FIG 1. (M) 2 L 7 2 4F A16WE 1996121900641 19961219 00641 NM 1996 12 19 USAA960733 1 19961105 A 5313 STRINGER BOEING 737 7372B7 1384560 NM BS 947-1006 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 37396 22885 ROA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 10 INCH CORROSION STRINGER 27 L, BS 947 TO 1006. REMOVED COR RODED STRINGER AND SPLICED IN NEW SECTION, REPAIRED PER SRM 53-10-3 DETAIL 6. (M) 2 L 7 2 4F A16WE 1996121900642 19961219 00642 NM 1996 12 19 USAA960736 1 19961110 A 5313 STRINGER BOEING 737 7372B7 1384560 NM BS 9865-1006 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 268AU 38828 22880 ROA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 8 INCH CORROSION STRINGER 27L, BS 9865 TO 1006. REMOVED CORR ODED STRINGER AND INSTALLED NEW STRINGER AND SPLICE, REPAIRED PER SRM 53-30-3 FIG 1. (M) 2 L 7 2 4F A16WE 1996121900643 19961219 00643 NM 1996 12 19 USAA960742 1 19961117 A 5330 SKIN BOEING 737 737201 1384454 NM BS 328 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 22756 ROA - DURING CX-1 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND .1.25 INCH CRACK FORWARD GALLEY DOOR CUT OUT AFT LOWER COR NER (STRINGER 17 R BS 328) FUSELAGE SKIN. REMOVED CRACK AND INSTALLED DOUBLER, REPAIRED PER T/R 53-10-19 REV A. (M) 2 L 7 2 4F A16WE 1996121900644 19961219 00644 NM 1996 12 19 USAASB96240 1 19961120 A 3260 BR9AXH5V3 RELAY BOEING 737 7373B7 1384580 NM NLG SHORTED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 505AU 23380 CLT - FL 1702- ON T/O, RED N/G UNSAFE LIGHT ILLUMINATED. ON T/O, GEAR HANDLE WOULD NOT RETRACT TO UP POS, ONLY TO OFF. PLACED GEAR HANDLE BACK TO DOWN POS AND INSTEAD OF GETTING DOWN AND LOCKED GREEN LIGHTS, GOT RED N/G AND RT MAIN UNSAFE LIGHTS. CREW CYCLED GEAR AGAIN TO DOWN POS AND OFF POS AND RECEIVED NO LIGHTS AT ALL. CAPT DECIDED TO RETURN TO FIELD AT CLT. CREW DID A FLYBY AND VERIFIED GEAR WAS DOWN AND LOCKED BY LOOKING THRU VIEWPORTS. NO EMERG WAS DECLARED AND T HE FLT LANDED W/O INCIDENT. MX FOUND THE R374 RELAY SHORTED IN THE L/G LOGIC SHELF E11. REPLACED SAME. JACKED A/C AND SWUNG GEAR. ALL IND NORMAL. (M) 2 L 7 2 4F RT A16WE 1996121900645 19961219 00645 NM 1996 12 19 USAABB96048 1 19961119 A 5230 S182349 DOOR SEAL BOEING 767 767201 1385125 NM CARGO DOOR DAMAGED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 646US 23898 PHL - FL 894 - ON CLIMB-OUT FROM PHL, CREW COULD NOT PRESSURIZE AIRCRAFT. FLIGHT RETURNED TO PHL AND LANDED WITH NO FUR THER INCIDENT. MAINTENANCE FOUND THE FORWARD CARGO DOOR SEAL DAMAGED AND REPLACED IT. (M) 2 L 7 2 4F RT A1NM 1996121900646 19961219 00646 NM 1996 12 19 USAASB96228 1 19961116 A 7931 SRL0C4N OIL GAUGE BOEING 737 737201 1384454 NM NR 2 ENG FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 235US 22275 BWI - FL 322 - AFTER TAKEOFF, THE NR 2 ENGINE OIL PRESSURE WENT FROM LOWER GREEN LINE TO MID YELLOW BAND. FLIGHT RETURN ED TO FIELD AT BWI AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MX REPLACED THE NR 2 ENGINE OIL PRE SSURE GAUGE AND TRANSMITTER AND CLEANED THE CANNON PLUG TO THE TRANSMITTER. RAN ENGINE. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1996121900647 19961219 00647 NM 1996 12 19 96ZZZM1563 1 19961116 A 7931 ST104Z OIL TRANSMITTER BOEING 737 737201 1384454 NM NR 2 ENG FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 235US 22275 BWI - FL 322 - AFTER TAKEOFF, THE NR 2 ENGINE OIL PRESSURE WENT FROM LOWER GREEN LINE TO MID YELLOW BAND. FLIGHT RETURN ED TO FIELD AT BWI AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MX REPLACED THE NR 2 ENGINE OIL PRE SSURE GAUGE AND TRANSMITTER AND CLEANED THE CANNON PLUG TO THE TRANSMITTER. RAN ENGINE. OPS CHECK GOOD. REFERENCE USA ASB96228. 2 L 7 2 4F A16WE 1996121900648 19961219 00648 WP 1996 12 19 USAAD96164 1 19961003 A 3350 60030451LB POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 939VJ 48120 PHL - AFT CABIN FLOOR LEVEL AND CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. (M) 2 L 7 2 4F A6WE 1996121900649 19961219 00649 WP 1996 12 19 USAAD96165 1 19961031 A 3350 14597101 BATTERIES DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 804US 48052 PHL - OVERHEAD EMERGENCY LIGHTS INOPERATIVE AT ROWS 9-11. REPLACED BATTERIES IN POWER SUPPLY. (M) 2 L 7 2 4F A6WE 1996121900650 19961219 00650 WP 1996 12 19 USAAD96166 1 19961116 A 2450 9008D092 RELAY DOUG DC9 DC931 3022065 WP LEFT FAILED A USAA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 EA 19 966VJ 47420 FLT 882 - PIT-YUL - AT CRUISE FL 330, LEFT AC BUS PHASE A CIRCUIT BREAKER POPPED. THEN PHASE A RIGHT FORWARD BOOST PUMP , PHASE A CENTER FORWARD AND PHASE 'A' LEFT AFT BOOST PUMPS, AND PHASE 'B' ON ALL THREE PUMPS POPPED. ALSO, PHASE 'A' A ND 'B' ON RADIO RACK POPPED. FIRST OFFICER RESET AC BUS CIRCUIT BREAKERS AND PULLED BREAKER ON RADIO RACK FAN. FLIGHT DIVERTED TO SYR. NO EMERGENCY WAS DECLARED. FLIGHT LANDED NORMALLY. MX REPLACED LEFT AUXILLARY BUS RELAY. ELECTRICAL SYSTEM CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 1996121900651 19961219 00651 WP 1996 12 19 USAAD96167 1 19961118 A 3246 WHEEL DOUG DC9 DC981 3022081 WP NLG SHIMMIED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 819US 48099 FLT 359 - CLT-GSP - AT TAKEOFF NOSE WHEEL SHIMMIED. AFTER GEAR RETRACTION THERE WAS A BURNED RUBBER SMELL IN THE COCKPI T. CREW LOWERED GEAR AND PERFORMED TOWER FLYBY. CONTROLLERS SAID GEAR LOOKED NORMAL. FLIGHT RETURNED TO FIELD. NO FU RTHER INCIDENTS. FLIGHT LANDED NORMALLY. MAINTENANCE INSPECTED AIRCRAFT AND FOUND NO PROBLEMS. THEY REPLACED BOTH NOS E TIRES AND LUBED NOSE GEAR STRUT AS A PRECAUTION. (M) 2 L 7 2 4F A6WE 1996121900652 19961219 00652 WP 1996 12 19 USAAD96168 1 19961120 A 3350 1315 BULB DOUG DC9 DC981 3022081 WP CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 809US 48041 ROX - MX CHECK FOUND CEILING EMERGENCY LIGHTS OUT FROM ROWS 10-14. MAINTENANCE RELAMPED LIGHT. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A6WE 1996121900653 19961219 00653 NM 1996 12 19 USAASB96238 1 19961119 A 2424 948F4581 GCU BOEING 737 7374B7 1384702 NM COCKPIT FAILED A A USAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 432US 26557 24554 PIT- FL 1082 - CAPT REPORTED THAT IT TOOK TWO ATTEMPTS TO GET THE NR 1 ENG GEN ON LINE AFTER ENG START. ON CLIMB-OUT, C REW DETECTED A BURNING PLASTIC LIKE SMELL IN THE COCKPIT. NO SMOKE WAS PRESENT. F/O FELT GEN CONTROL UNIT G3 AND OBSER VED THAT IT WAS HOT. AT THAT TIME THE APU WAS STARTED AND PUT ON LINE FOR THE NR 1 GEN. C/B FOR GEN CONTROL UNIT G3 WA S PULLED CAUSING UNIT TO COOL AND BURNING SMELL TO STOP. MX REMOVED AND REPLACED NR 1 GEN CONTROL UNIT. STARTED ENG. G EN COMES ON LINE AND OPERATES NORM. NO SMELL NOTED. (M) 2 L 7 2 4F RT A16WE 1996121900654 19961219 00654 EU 1996 12 19 USAAF96120 1 19961121 A 3231 RETRACT MECH FOKKER F28 F28MK4000 4990810 EU LT MLG DOOR OUT OF ADJUST A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 494US 11167 FLT 1297 - GSO-PIT - AFTER T/O AND GEAR RETRACTED, LEFT GEAR DOOR LIGHT STAYED ILLUMINATED. FLIGHT RETUREND TO GSO WITH OUT FURTHER INCIDENT. MAINTENANCE FOUND THE LEFT GEAR DOOR WOULD NOT LOCK. RIGGED LEFT INBOARD DOOR STOP ON MAIN LANDI NG GEAR. INSPECTION OF RIGGING WAS COMPLETED. OPERATIONAL CHECK WAS GOOD. (M) 2 L 7 2 4F RT A20EU 1996121900655 19961219 00655 EU 1996 12 19 VTZA97064 2 19961115 A 7320 21188407 IEC JETAIR JETSTM JETSTM4101 1500501 EU RIGHT MALFUNCTIONED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 27 325UE 41063 FLT 6198 - IAD-BDL - ABORTED TAKEOFF DUE TO RIGHT IEC FAILED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAIN TENANCE CLEARED IEC FAULT CODE 64. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996121900656 19961219 00656 EU 1996 12 19 VTZA97062 1 19961115 A 3310 LT52A DIMMER BAG JETSTM JETSTM3201 1500217 EU LT COCKPIT FAILED A VTZA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 27 493UE 805 FLT 6394 - HVN-IAD - DURING CRUISE FLIGHT, MADE A SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS ELECTRIC ODOR COMING FROM BASE OF CAPTAINS SEAT PEDESTAL, NO SMOKE SEEN. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MX INSPECTED AND R EMOVED AND REPLACED DIMMER. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996121900657 19961219 00657 EU 1996 12 19 VTZA97060 1 19961112 A 7714 AG34 TACH GENERATOR BAG JETSTM JETSTM3201 1500217 EU RIGHT FAILED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 497UE 904 FLT 6372 - IAD-AIB - DURING CRUISE, MADE AN UNSCHEDULED LANDING DUE TO RIGHT RPM FAILED IN FLIGHT. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED TACH GEN, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RET URNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996121900658 19961219 00658 1996 12 19 VTZA97059 4 19961108 A 3425 4020531574 ADI BAG JETSTM JETSTM3201 1500217 EU RT COCKPIT FAILED A VTZA K NONE J WARNING INDICATION CR CRUISE 1 EA 27 497UE 904 FLT 6381 - IAD-CMH - DURING CRUISE FLIGHT, MADE AN UNSCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS FLIGHT OFFICERS AD I GYRO FLAG ILLUMINATED. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED ADI, OPS CHE CK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996121900659 19961219 00659 EU 1996 12 19 VTZA97057 1 19961108 A 2433 LT52A CONVERTER UNIT BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A VTZA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 27 491UE 911 FLT 6316 - IAD-RIC - DURING TAXI TO RIC GATE SMOKE ODOR DETECTED IN COCKPIT. NO SMOKE SEEN. MAINTENANCE INSPECTED AND FOUND COCKPIT BACKLIGHTING TO BE SOURCE OF ODOR IN DIMMER CONTROL BOX. MAINTENANCE OPENED DMI 18306, MEL 33-1 ON DIMMER CONTROL BOX. MAINTENANCE CLOSED DMI ON 11-08-96 BY REMOVING AND REPLACING CONVERTER. AIRCRAFT WAS RELEASED AND RETURN ED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996121900660 19961219 00660 EU 1996 12 19 VTZA97070 1 19961118 A 2150 1718D0000 ACM JETAIR JETSTM JETSTM4101 1500501 EU CABIN STUCK A VTZA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 27 313UE 41026 FLT 6551 - IAD-CLE - DURING TAXI, RETURNED TO GATE DUE TO RIGHT DUCT OVERTEMP LIGHT ILLUMINATED. MAINTENANCE INSPECTION AND FREED STUCK ACM, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996121900661 19961219 00661 1996 12 19 VTZA97069 3 19961118 A 6140 31054294 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU NR 1 ENGINE FAILED A VTZA O OTHER N FALSE WARNING CR CRUISE 1 EA 27 436JX 41036 FLT 6214 - IAD-ORD - DURING CRUISE, MADE AN UNSCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS NR 1 ENG RED BETA LIGHT I LLUMINATED FOR TEN MINUTES IN FLIGHT. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED NR 1 BETA PRESSURE SWITCH. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1996121900662 19961219 00662 EU 1996 12 19 VTZA97068 1 19961118 A 5270 SWITCH BAG JETSTM JETSTM3201 1500217 EU PAX DOOR LACK OF LUBE A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 497UE 904 FLT 6343 - IAD-SYR - DURING CLIMB, MADE AN UNSCHEDULED LANDING DUE TO PAX DOOR LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE CLEANED AND LUBED HANDLE MICROSWITCH, OPS CHECK OK. AIRCRAFT WAS RELEASED A ND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996121900663 19961219 00663 1996 12 19 VTZA97066 4 19961113 A 3418 C771076 LIFT TRANSDUCER BAG JETSTM JETSTM3201 1500217 EU RT WING FAILED A VTZA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 EA 27 486UE 905 FLT 6575 - IAD-PHF - ABORTED TAKEOFF DUE TO RIGHT AMBER STALL CAP LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED STALL VANE LIFT TRANSDUCER. OPS CHECK OK. AIRCRAFT WAS RELEASED A ND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996121900664 19961219 00664 EU 1996 12 19 VTZA97065 1 19961114 A 2711 MECHANISM BAG JETSTM JETSTM3201 1500217 EU LT/RT AILERON LACK OF LUBE A VTZA K NONE F FLT CONT AFFECTED CR CRUISE 1 EA 27 472UE 823 FLT 6384 - ROC-IAD - DURING CRUISE, MADE AN UNSCHEDULED LANDING WITH ONE DISCREPANCY OF AILERON TRIM FREEZES IN FLIGHT. AIRCRAFT WENT TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE CLEANED AND LUBED AILERON TRIM JACK, OPS CHECK OK. AIRCR AFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1996121900665 19961219 00665 NM 1996 12 19 TSAA9653088 1 19961113 A 5330 SKIN BOEING 737 7372S2C 138448G NM BS 746 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 806AL 21927 DURING OVERNIGHT CHECK, DISCOVERED FUSELAGE SKIN CRACK 2.5 INCH AT BS 746, STRINGER 17R. REPAIRED PER SRM 53-30-3. AIR CRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1996121900666 19961219 00666 NM 1996 12 19 TSAA9627086 1 19961107 A 2750 BACN103C6CD NUT BOEING 737 7372T4 1384492 NM TE FLAPS LOOSE A A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 808AL 23445 DURING PREFLIGHT CHECK DISCOVERED, RIGHT AILERON AND TAB DAMAGED. SUBSEQUENT INSPECTION REVEALED NR 8 FLAP TRANSMISSION SPLINED COUPLING RETAINING NUT BACKING OFF CAUSING DAMAGES TO THE ABOVE. REPLACED NR 8 AND NR 7 FLAP TRANSMISSIONS FOR PRECAUTIONARY, TORQUE CHECK ACCOMPLISHED ON FLAP DRIVE COUPLING NUTS. REPLACED DAMAGED RIGHT T/E FLAP MID FLAP, AILERO N, AND TAB ASSY. PERFORMED TEST FLIGHT AND AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1996121900667 19961219 00667 NM 1996 12 19 TSAA9626085 1 19961104 A 2611 SMOKE DETECTOR BOEING 737 7372M6C 1384708 NM CARGO COMPT MALFUNCTIONED A TSAA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 WP 13 805AL 21809 ON 10-31-96, FLIGHT NR 934, PIREP NR 2, FORWARD CARGO SMOKE WENT OFF INFLIGHT. WENT OUT WHEN RETURNED TO FIELD AFTER LA NDING. INSPECTED CARGO COMPARTMENT, CHECK SMOKE DETECTORS. REPLACED DETECTOR BULBS IN A/B DETECTORS. SYSTEM CHECKED N ORMAL AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1996121900668 19961219 00668 NM 1996 12 19 TSAA9632087 1 19961108 A 3244 26015711 TIRE GOODYEAR 404F429 BOEING 737 737297 1384480 NM MLG FAILED A TSAA O OTHER E VIBRATION/BUFFET TO TAKEOFF 1 WP 13 725AL 61220560 22051 FLT 48 - PIREP NR 4, VIBRATION ON TAKEOFF AND ROTATION. SUSPECT BLOWN TIRE. REMOVED AND REPLACED NR 4 M/W ASSEMBLY, DU E TO BLOWN TIRE, AND M/W ASSEMBLY FOR PRECAUTIONARY. M122 TIRE TREAD LOSS/TIRE BURST INSPECTION AND ANTI-SKID TEST ACCO MPLISHED. REMOVED AND REPLACED RIGHT MLG INNER DOOR DUE TO DAMAGE. RETRACTION TEST OK. REPAIRED RIGHT INBOARD MID FLA P LOWER SKIN PER EA 737-57-009. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1996121900669 19961219 00669 NM 1996 12 19 TSAA9653090 1 19961119 A 5320 INTERCOSTAL BOEING 737 7372Q9 138448M NM BS 332 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 804AL 21719 DURING SCHEDULED INSPECTION OF FUSELAGE, FORWARD SERVICE DOORWAY AFT FRAME, DISCOVERED CRACK AT DOOR STOP SUPPORT INTERC OSTAL AT BS 332, STRINGER 8A (REF AD88-03-03 AMDT39-5832, AND AD 90-06-02 AMDT 39-6489). REPAIRED PER ECO 1475R4, PER D RAWING 65C33288, FIG 3, PT 2 AND 3. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1996121900670 19961219 00670 EU 1996 12 19 RAIA961116 1 19961114 A 7712 P323A701135SN1E CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU RIGHT ENG CONTAMINATED A RAIA B EMER. DESCENT O OTHER LD LANDING 1 CE 03 551HK 764 41040 LEX - FLT 7481- RIGHT POWER LEVER DOES NOT RESPOND TO POWER LEVER INPUTS. MAINTENANCE CLEANED OIL FROM THE RIGHT TORQUE RING CANNON PLUG. (M) 2 L 7 2 4T RT A41NM 1996121900671 19961219 00671 EU 1996 12 19 RAIA961115 1 19961114 A 2910 NTA152506 O-RING AEROSP ATR42 ATR42300 8680920 EU HYD BAY LEAKS A RAIA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 CE 03 EICBF 14729 176 STL - FLT 7406 - GREEN HYDRAULIC LOW PRESSURE AND LOW LEVEL LIGHT ILLUMINATED. MAINTENANCE REPLACED THE GREEN ACCUMULAT OR O-RING. (M) 2 H 7 2 4T RT A53EU 1996121900672 19961219 00672 EU 1996 12 19 RAIA961113 1 19961112 A 3222 STRUT BAG JETSTM JETSTM3201 1500217 EU NLG LEAKING A RAIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CE 03 432AM 883 STL - FLT 7378 - NOSE GEAR WOULD NOT RETRACT. MAINTENANCE REPACKED THE NOSE STRUT. (M) 2 L 7 2 4T RT A56EU 1996121900673 19961219 00673 EU 1996 12 19 RAIA961110 1 19961108 A 2170 8323715 WATER SOCK BAG JETSTM JETSTM3201 1500217 EU RIGHT DIRTY A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 03 859AE 859 SAN - FLT 4745 - RIGHT BLEED STARTED TO STINK DURING FLIGHT. AS A PRECAUTIONARY. THE CREW DIVERTED TO LAX. MAINTENANC E REPLACED THE RIGHT WATER SOCK. (M) 2 L 7 2 4T RT A56EU 1996121900674 19961219 00674 EU 1996 12 19 RAIA961106 1 19961106 A 2844 1103P0645 PRESS SWITCH BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 436AM 891 STL - FLT 7080 - LEFT FUEL CAP LIGHT ILLUMINATED DURING TAKEOFF. MAINTENANCE REPLACED THE LEFT FUEL LOW PRESSURE SWITCH . (M) 2 L 7 2 4T RT A56EU 1996121900675 19961219 00675 1996 12 19 RAIA961117 4 19961119 A 3425 7003360948 AHRS COMPUTER JETAIR JETSTM JETSTM4101 1500501 EU LEFT FLAGGED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 552HK 3710 41057 STL - FLT 7326 - CAPTAINS AHRS RECEIVED A COMPARATOR WARNING. MAINTENANCE REPLACED THE NR 1 AHRS COMPUTER. (M) 2 L 7 2 4T RT A41NM 1996121900676 19961219 00676 EU 1996 12 19 RAIA961111 1 19961111 A 5270 J4152007 SWITCH BRACKETS JETAIR JETSTM JETSTM4101 1500501 EU BAGG COMPT WEAK A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 561HK 1830 1830 41077 PIT - FLT 7796 - BAGGAGE DOOR CAPTION ILLUMINATED DURING TAKEOFF. MAINTENANCE PERFORMED SB J41-52-007, BY REPLACING THE SWITCH BRACKETS. (M) 2 L 7 2 4T RT A41NM 1996121900677 19961219 00677 WP 1996 12 19 RAIA961107 2 19961105 A 7320 8974764 APR COMPENSATOR BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT ENGINE ERRATIC A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 CE 03 435AM 11717 889 STL - FLT 7466 - LEFT EGT FLUCTUATED WITH SRL ON, NORMAL WITH WITH SRL OFF. MAINTENANCE REPLACED THE LEFT AUTO. POWER RESERVE COMPENSATOR. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996121900678 19961219 00678 EU 1996 12 19 RAIA961120 4 19961120 A 3160 7011672112 SYMBOL GENERATOR JETAIR JETSTM JETSTM4101 1500501 EU NR 2 FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 560HK 2147 2147 41076 BHM - FLT 7463 - NR 2 EADI AND EHSI FAILED IN FLIGHT. REMOVED AND REPLACED NR 2 SYMBOL GENERATOR. (M) 2 L 7 2 4T RT A41NM 1996121900679 19961219 00679 EU 1996 12 19 RAIA961119 1 19961118 A 6120 NAS1351CLL6 BOLT BAG JETSTM JETSTM3201 1500217 EU NR 1 ENGINE LOOSE A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 859AE 6685 859 LAX - FLT 4767 - LEFT ENGINE RPM FLUCTUATING ON TAKEOFF. SECURED UNDERSPEED GOVERNOR ROD BOLT. (M) 2 L 7 2 4T RT A56EU 1996121900680 19961219 00680 EU 1996 12 19 JBXA9600030 1 19961118 A 2420 GENERATOR FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAYMK65015 EU NR 1 FAULTED A JBXA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 05 108ML 11484 LGA - FLT 4 - GEN 1 FAULTS AFTER START, LGA, ABORTED TAKEOFF. ASSIGNED TO DMI NR 02447, MEL NR 24-21-3-1. STILL T/S SY STEM, ITEM STILL CURRENT. (M) 2 L 7 2 4F 4 F RT 1996121900681 19961219 00681 CE 1996 12 19 GLBA96219 1 19961110 A 2841 812081 INDICATOR BEECH 1900 1900C 1154161 CE LT/RT FUEL QTY MALFUNCTIONED A GLBA K NONE O OTHER IN INSP/MAINT 1 CE 01 98GL UC98 SPI - RIGHT FUEL GAUGE PEGS TO TOP OF SCALE ERRATICALLY. LEFT GAUGE FOLLOWS TO A LESSER DEGREE. MAINTENANCE REPLACED B OTH FUEL QUANTITY INDICATORS AND TEST FLIGHT WAS SATISFACTORY. (M) 2 L 7 2 4T RT A24CE 1996121900682 19961219 00682 SO 1996 12 19 GLBA96218 1 19961108 A 5753 TRACKS EMB 120 EMB120RT SO TE FLAPS DIRTY A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 281UE 120092 ORD - ON DEPARTURE INBOARD FLAPS FAILED TO RETRACT. MAINTENANCE FOUND FLAP TRACKS GUMMED UP AND STICKY. CLEANED AND LU BED TRACKS AND FLAPS OPERATE NORMALLY. (M) 2 L 7 2 4T RT A31SO 1996121900683 19961219 00683 CE 1996 12 19 GLBA96217 1 19961107 A 5270 SWITCH BEECH 1900 1900C 1154161 CE BAGGAGE DOOR DIRTY A GLBA O OTHER N FALSE WARNING CR CRUISE 1 CE 01 87GL UC87 HUF - NOSE BAGGAGE DOOR ANNUNCIATOR ILLUMINATES IN FLIGHT. MAINTENANCE CLEANED MICROSWITCH. (M) 2 L 7 2 4T RT A24CE 1996121900684 19961219 00684 SO 1996 12 19 GLBA96216 1 19961107 A 2910 HYD LINE EMB 120 EMB120RT SO RT ENGINE CHAFED A GLBA O OTHER K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 CE 01 452UE 120096 UIN - BLUE SYSTEM LOST ALL HYDRAULIC PRESSURE. MAINTENANCE FOUND CHAFED HIGH PRESSURE LINE IN RIGHT ENGINE NACELLE AREA . REPLACED DAMAGED LINE. (M) 2 L 7 2 4T RT A31SO 1996121900685 19961219 00685 SO 1996 12 19 GLBA96214 1 19961106 A 7712 30005000052 TSCU EMB 120 EMB120RT SO LT ENGINE FAILED A GLBA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 01 451UE 120108 ALO - AFTER START LEFT ENGINE REMAINED IN FEATHER UNTIL AUTOFEATHER SWITCHED OFF. CYCLING AUTOFEATHER SWITCH CAUSES EAC H PROP TO FEATHER ALTERNATELY. SMOKE FROM LEFT SIDE PANEL. MAINTENANCE REMOVED AND REPLACED RIGHT TORQUE SIGNAL CONDIT ION UNIT. NO SMOKE OR DAMAGE NOTED. (M) 2 L 7 2 4T RT A31SO 1996121900686 19961219 00686 CE 1996 12 19 GLBA96213 1 19961106 A 3230 CIRCUIT BREAKER BEECH 1900 1900C 1154161 CE LANDING GEAR TRIPPED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 96UE UC96 SPI - LANDING GEAR FAILED TO RETRACT. MAINTENANCE FOUND 60 AMP CIRCUIT BREAKER POPPED, RESET GEAR CIRCUIT BREAKER AND C YCLED GEAR. OPERATION NORMAL. (M) 2 L 7 2 4T RT A24CE 1996121900687 19961219 00687 CE 1996 12 19 GLBA96212 1 19961031 A 2434 23078019 STARTER/GEN BEECH 1900 1900C 1154161 CE RT ENGINE FAILED A GLBA O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 CE 01 167GL 1611 UC167 MYR - RIGHT GENERATOR FAILED INFLIGHT. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE STARTER/GEN. (M) 2 L 7 2 4T RT A24CE 1996121900688 19961219 00688 NE 1996 12 19 ASOA96051 2 19961118 A 7200 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE RIGHT FIRE A ASOA A E F UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. A FLAME/FIRE TO TAKEOFF 1 SO 11 247AS 120113 115450 ON TAKEOFF MCN-ATL, TOWER ADVISED CREW OF A FIRE AT THE RIGHT ENGINE, CLEARED THE AIRCRAFT FOR IMMEDIATE RETURN TO MCN, AND CALLED OUT FIRE EQUIPMENT TO MEET THE AIRCRAFT. LANDING WAS MADE SAFELY, ENGINE SHUT DOWN AND FIRE HANDLE PULLED. T HE CREW EXPERIENCED NO FIRE INDICATION UNTIL THE AIRCRAFT WAS STOPPED ON THE RUNWAY AT WHICH TIME A 'TAIL PIPE' FIRE IND ICATION OCCURRED. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1996121900689 19961219 00689 SO 1996 12 19 ASOA96050 1 19961115 A 2910 HYDRAULIC LINE EMB 120 EMB120RT SO LT ENGINE RUPTURED A ASOA O OTHER F J K FLT CONT AFFECTED WARNING INDICATION FLUID LOSS CR CRUISE 1 SO 11 229AS 120042 FLT 7070 - IN BOUND CRW-ATL - LOST HYDRAULIC PRESSURE OF THE GREEN SYSTEM, THEN LOST HYDRAULIC QUANTITY. CREW DECLARED AN EMERGENCY AND LANDED ZERO FLAPS, SAFELY AND WITHOUT FURTHER INCIDENT. SPLICED IN NR 6 STAINLESS STEEL HYDRAULIC LINE AND PERMASWEGED. ALSO REPLACED THE LEFT ENGINE DRIVEN HYDRAULIC PUMP. (M) 2 L 7 2 4T RT A31SO 1996121900690 19961219 00690 SW 1996 12 19 MALA965180 1 19961105 A 8200 SWITCH SWRNGN SA227 SA227AC 8780603 SW WATER METH SYS OUT OF POSITION A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 442MA AC725 FLT 3038 - ON CLIMB-OUT FROM MSP, THE CREW REPORTED THAT THERE WAS NO AIR FLOW FROM THE BLEED AIR SYSTEM AFTER IT WAS SE LECTED. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. UPON FURTHER INVESTIGATION , THE WATER METH QTY WAS AT ZERO. MAINTENANCE SUSPECTS THAT THE WATER METH SWITCH WAS ON, THUS CUTTING OUT THE BLEED AI R SYSTEM. ALL CHECKS SATISFACTORY. (M) 2 L 7 2 4T RT A8SW 1996121900691 19961219 00691 SW 1996 12 19 MALA965173 1 19961027 A 5412 FIREWALL DOUBLER SWRNGN SA227 SA227AC 8780603 SW RT NACELLE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 2692P AC658B DURING MAINTENANCE IN MSP, FOUND RIGHT FIREWALL DOUBLER CRACKED AT UPPER OUTBOARD SIDE ABOVE TOP ENGINE HARNESS CANNON P LUG CONNECTOR .375 INCH LONG. REPAIR COMPLETED PER EA 01-96110 DATED 10/27/96. (M) 2 L 7 2 4T RT A8SW 1996121900692 19961219 00692 SW 1996 12 19 MALA965174 1 19961031 A 5400 ANGLE SWRNGN SA227 SA227AC 8780603 SW NACELLE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 433MA AC714 DURING A BLOCK INSPECTION IN MSP, MAINTENANCE FOUND A CRACK IN RIGHT UPPER OUTBOARD WING TO NACELLE INTRANSIT ANGLE. ( M) 2 L 7 2 4T RT A8SW 1996121900693 19961219 00693 SW 1996 12 19 MALA965175 1 19961031 A 5311 FRAME SWRNGN SA227 SA227AC 8780603 SW BS 242 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 433MA AC714 DURING A BLOCK INSPECTION IN MSP, MAINTENANCE FOUND A CRACK IN LEFT SIDE OF BELT FRAME AT FUSELAGE STATION 242 BL 25 APP ROXIMATELY .25 INCH IN LENGTH. REPAIRED PER EA01-96115 BY FABRICATING AND INSTALLING A REPAIR DOUBLER. (M) 2 L 7 2 4T RT A8SW 1996121900694 19961219 00694 SW 1996 12 19 MALA965176 1 19961101 A 5230 2724010001 SPRING SWRNGN SA227 SA227AC 8780603 SW CARGO DOOR FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 426MA AC645 FLT 3430 - AFTER TAKEOFF FROM LSE, THE CARGO DOOR PRIMARY AND SECONDARY WARNING LIGHTS ILLUMINATED. THE AIRCRAFT RETURN ED TO LSE. MAINTENANCE REPLACED THE OVERCENTERING SPRING, P/N 27-24010-001, AND REPLACED A BENT ROD ASSEMBLY, P/N 27-24 133-155. ALL CHECKS SATISFACTORY. (M) 2 L 7 2 4T RT A8SW 1996121900695 19961219 00695 SW 1996 12 19 96ZZZM1564 1 19961101 A 5230 2724133155 ROD SWRNGN SA227 SA227AC 8780603 SW CARGO DOOR BENT A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 426MA AC645 FLT 3430 - AFTER TAKEOFF FROM LSE, THE CARGO DOOR PRIMARY AND SECONDARY WARNING LIGHTS ILLUMINATED. THE AIRCRAFT RETURN ED TO LSE. MAINTENANCE REPLACED THE OVERCENTERING SPRING, P/N 27-24010-001, AND REPLACED A BENT ROD ASSEMBLY, P/N 27-24 133-155. ALL CHECKS SATISFACTORY. REFERENCE MALA965176. 2 L 7 2 4T RT A8SW 1996121900696 19961219 00696 SW 1996 12 19 MALA965201 1 19961114 A 3260 1EN516 SWITCHES SWRNGN SA227 SA227AC 8780603 SW NLG DIRTY A MALA O OTHER N FALSE WARNING AP APPROACH 1 GL 15 422MA AC635 FLT 3226 - ON APPROACH TO YQT, THE NOSE GEAR DOOR LIGHT FAILED TO ILLUMINATE FTER GEAR EXTENSION. THE CREW CYCLED THE G EAR UNTIL ALL INDICATIONS WERE NORMAL. MAINTENANCE CLEANED AND LUBED THE SWITCHES AND PERFORMED GEAR SWINGS. ALL CHECK S NORMAL. (M) 2 L 7 2 4T RT A8SW 1996121900697 19961219 00697 SW 1996 12 19 MALA965197 1 19961113 A 5320 2722085 DOOR FRAME SWRNGN SA227 SA227AC 8780603 SW BS 438 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 426MA AC645 DURING A MAINTENANCE INSPECTION IN MSP, MAINTENANCE FOUND THE FORWARD CARGO DOOR FRAME AT FS 438 CRACKED AT GAS STRUT SU PPORT MOUNTING HOLE. COMPLETED REPAIR TO FUSELAGE FORWARD CARGO DOOR FRAME P/N 27-22085 AT FS 438 DUE TO REPAIR TO FUSE LAGE FORWARD CARGO DOOR FRAME P/N 27-22085 AT FS 438 DUE TO .25 INCH CRACK NOTED IN AREA OF THE DOOR GAS STRUT SUPPORT L OWER MOUNT HOLE. REMOVED CRACKED AREA AND INSTALLED REPAIR DOUBLERS IAW FAC ARP 53-20-9503. (M) 2 L 7 2 4T RT A8SW 1996121900698 19961219 00698 SW 1996 12 19 MALA965199 1 19961113 A 5753 2736015001 RIB SWRNGN SA227 SA227AC 8780603 SW TE FLAP CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 426MA AC645 DURING A BLOCK INSPECTION IN MSP, MAINTENANCE FOUND A CRACK IN THE LEFT OUTBOARD FLAP NOSE RIB. REMOVED AND REPLACED FL AP NOSE RIB P/N 27-36015-001 IAW FAC SRM 57-90-60 PAGES 43-46. (M) 2 L 7 2 4T RT A8SW 1996121900699 19961219 00699 SW 1996 12 19 MALA965198 1 19961113 A 5753 RIB RIB SWRNGN SA227 SA227AC 8780603 SW TE FLAP CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 426MA 2736004008 AC645 DURING BLOCK INSPECTION IN MSP, MAINTENANCE FOUND A CRACK IN RIGHT INBOARD FLAP NOSE RIB. REMOVED AND REPLACED FLAP NOS E RIB P/N 27-36004-008 IAW FAIRCHILD STRUCTURAL REPAIR MANUAL 51-00-00 PAGE 4 AND FAIRCHILD SB 227-27-023. (M) 2 L 7 2 4T RT A8SW 1996121900700 19961219 00700 SW 1996 12 19 MALA965200 1 19961103 A 3260 1EN516 SWITCH SWRNGN SA227 SA227AC 8780603 SW NLG DIRTY A MALA O OTHER N FALSE WARNING AP APPROACH 1 GL 15 422MA AC635 FLT 3342 - ON APPROACH TO DTW, THE GREEN DOWN AND LOCKED LIGHT FOR THE NOSE GEAR WASN'T RECEIVED UNTIL THE GEAR WAS CYCL ED THREE TIMES. MAINTENANCE CLEANED AND LUBED THE DOWN LOCK POSITION SWITCHES. ALL CHECKS SATISFACTORY DURING GEAR SWI NGS. (M) 2 L 7 2 4T RT A8SW 1996121900701 19961219 00701 SW 1996 12 19 MALA965196 1 19961112 A 3260 1EN516 SWITCH SWRNGN SA227 SA227AC 8780603 SW RT MLG DIRTY A MALA O OTHER J WARNING INDICATION AP APPROACH 1 GL 15 425MA AC640 FLIGHT 3085 - ON APPROACH TO MSP, THE RIGHT GEAR INTRANSIT LIGHT AS SLOW TO EXTINGUISH AFTER GEAR EXTENSION. MAINTENANC E CLEANED AND LUBED THE RIGHT INTRANSIT LIGHT SWITCHES. ALL CHECKS SATISFACTORY. (M) 2 L 7 2 4T RT A8SW 1996121900702 19961219 00702 SW 1996 12 19 MALA965195 1 19961111 A 3260 1EN516 SWITCH SWRNGN SA227 SA227AC 8780603 SW RT MLG DIRTY A MALA O OTHER N FALSE WARNING AP APPROACH 1 GL 15 425MA AC640 FLT 3355 - ON APPROACH TO DTW, THE RIGHT MAIN GEAR DIDN'T INDICATED DOWN AND LOCKED AFTER GEAR EXTENSION. THE CREW CYCL ED THE GEAR UNTIL A DOWN INDICATION WAS RECEIVED. MAINTENANCE CLEANED AND LUBED THE RIGHT GEAR POSITION SWITCHES. ALL CHECKS SATISFACTORY. (M) 2 L 7 2 4T RT A8SW 1996121900703 19961219 00703 NM 1996 12 19 MALA965202 1 19961114 A 2424 GCU DHAV DHC8 DHC8102 2809003 NM NR 1 MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 824MA 327 FLT 3370 - EN ROUTE, THE NR 1 AC GEN LIGHT ILLUNMINATED. THE CREW RESET THE GENERATOR AND THEN THE NR 2 AC BUS, RT HORN , AND RT STALL LIGHTS ILLUMINATED. A FEW MINUTES LATER THE LEFT AC BUS AND ASSOCIATED LIGHTS ILLUMINATED. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE CYCLED THE AC SWITCH AND ALL SYSTEMS OPERATED NORMALLY THROUGH SEVERAL FEATHERING AND UNF EATHERING CYCLES. THE AC GCU'S WERE REPLACED AS A PRECAUTION. (M) 2 H 7 2 4T RT A13NM 1996121900704 19961219 00704 SW 1996 12 19 MALA965191 1 19961110 A 5330 SKIN SWRNGN SA227 SA227AC 8780603 SW BS 392 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 426MA AC645 DURING A BLOCK INSPECTION IN MSP, MAINTENANCE FOUND A CRACK IN RIGHT SIDE OF LOWER CONSTANT SECTION AT FUSELAGE STATION 392. COMPLETED REPAIR TO CONSTANT SECTION IAW FAC SRM 53-90-20 REPAIR NR 20. (M) 2 L 7 2 4T RT A8SW 1996121900705 19961219 00705 SW 1996 12 19 MALA965193 1 19961109 A 5414 SKIN SWRNGN SA227 SA227AC 8780603 SW LT NACELLE DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 158MC AC726B DURING MAINTENANCE IN MSP, MAINTENANCE FOUND THE LEFT INBAORD NACELLE HAD SEVERAL RIVETS PULLING THROUGH. COMPLETED REP AIR TO LEFT INBOARD NACELLE SKIN JUST AHEAD OF THE INBOARD GEAR DOOR BY INSTALLING A REPAIR DOUBLER IAW FAC SRM 54-90-40 PAGES 35-37. (M) 2 L 7 2 4T RT A8SW 1996121900706 19961219 00706 SW 1996 12 19 MALA965192 1 19961109 A 5753 2736004007 RIB SWRNGN SA227 SA227AC 8780603 SW LT FLAP NOSE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 434MA AC717 DURING SCHEDULED MAINTENANCE IN MSP, THE LEFT FLAP NOSE RIB HAD A .5 INCH CRACK FROM THE RELIEF RADIUS. COMPLETED REPAI R TO LEFT FLAP BY REPLACING THE INBOARD NOSE RIB P/N 27-36004-007 IAW 51-00-00 PAGE 4 AND 51-40-02. (M) 2 L 7 2 4T RT A8SW 1996121900707 19961219 00707 SW 1996 12 19 MALA965190 1 19961110 A 5400 ANGLE SWRNGN SA227 SA227AC 8780603 SW RT NACELLE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 426MA AC645 DURING A BLOCK IINSPECTION IN MSP, FOUND A CRACK IN RIGHT LOWER INBOARD WING TO NACELLE INTRANSIT ANGLE. COMPLETED REPA IR TO WING TO NACELLE ANGLE IAW FAIRCHILD ARP 54-20-9101 REV B. (M) 2 L 7 2 4T RT A8SW 1996121900708 19961219 00708 SW 1996 12 19 MALA965177 1 19961103 A 5320 FRAME SWRNGN SA227 SA227AC 8780603 SW PAX DOORWAY CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 433MA AC714 DURING A BLOCK INSPECTION IN MSP, MAINTENANCE FUOND A CRACK IN THE AFT CORNER OF THE PASSENGER DOOR FRAME AT HINGE END O F DOOR. THE CRACK IS APPROX .5 INCH IN LENGTH AROUND THE AFT DOOR SNUBBER ATTACH BRACKET SCREW HOLE. COMPLETED REPAIR TO FRAME IAW FAIRCHILD LAR 96-MALA-174. (M) 2 L 7 2 4T RT A8SW 1996121900709 19961219 00709 SW 1996 12 19 MALA965178 1 19961102 A 5320 FRAME SWRNGN SA227 SA227AC 8780603 SW PAX DOOR WAY CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 433MA AC714 DURING A BLOCK INSPECTION IN MSP, MAINTENANCE FOUND A CRACK IN THE FORWARD CORNER OF THE PASSENGER DOOR FRAME AT HINGE E ND OF DOOR. THE CRACK IS APPROX .5 INCH IN LENGTH AROUND THE FORWARD DOOR SNUBBER ATTACH BRACKET SCREW HOLE. (M) 2 L 7 2 4T RT A8SW 1996121900710 19961219 00710 NM 1996 12 19 USAASB96236 1 19961117 A 3350 6013211 POWER SUPPLY BOEING 737 7372B7 1384560 NM CARGO INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 271AU 22883 ROA - MAINTENANCE FOUND THE AFT EXTERIOR DOOR ESCAPE SLIDE LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE POWER SUPP LY FOR THE AFT EXTERIOR ESCAPE SLIDE LIGHTS. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1996121900711 19961219 00711 NM 1996 12 19 USAASB96227 1 19961112 A 3350 500000043 POWER SUPPLY BOEING 737 7372B7 1384560 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 286AU 23133 FOUND FORWARD CEILING EMERGENCY EXIT SIGN LIGHT INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERY PACK. ( M) 2 L 7 2 4F A16WE 1996121900712 19961219 00712 1996 12 19 USAASB96230 4 19961118 A 3416 STATIC LINE BOEING 737 737201 1384454 NM LT/RT ALTIMETERS DISCONNECTED A A USAA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 EA 19 237US 22353 MYR - FL 8033 - ON T/O AT INT, BOTH THE CAPTAINS AND F/O ALTIMETERS FROZE AT 1,200 FT ANT TRIPPED TO STANDBY. TRIED BOT H STANDBY STATIC SOURCES WITH NO RECOVERY OF EITHER ALTIMETER. ALTIMETERS APPEARED TO OPERATE NORMALLY UPON PASSING THR OUGH 1,200 FT. FLIGHT DIVERTED TO MYR AND LANDED W/O FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. UPON LANDING AT MYR , BOTH ALTIMETERS RECOVERED, WORKING FROM 1,200 FT TO LANDING. BOTH RESET TO CADC. BOTH APPEAR NORMAL ON GROUND. MX R EMOVED BOTH ALTIMETERS AND FOUND BOTH STATIC LINES DISCONNECTED. RECONNECTED STATIC LINES AND REINSTALLED ALTIMETERS. ( M) 2 L 7 2 4F A16WE 1996121900713 19961219 00713 NM 1996 12 19 USAASB96234 1 19961115 A 3350 900835A BATTERY PACK BOEING 737 737201 1384454 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 260AU 22866 ALB, MAINTENANCE FOUND THE EMERGENCY EVACUATION LIGHTING ON SEATS 1-3 AB AND 4-6 ABC INOP. MAINTENANCE REPLACED THE BAT TERY PACK AT SEAT 5 ABC. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1996121900714 19961219 00714 NM 1996 12 19 USAASB96233 1 19961111 A 3350 1000679 LIGHT BOEING 737 737201 1384454 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 229US 21818 ROA - MAINTENANCE FOUND THE AFT SERVICE DOOR INTERIOR EMERGENCY EXIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE L IGHT ASSEMBLY AND INSTALLED NEW BATTERIES (P/N S106). OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1996121900715 19961219 00715 NM 1996 12 19 USAASB96239 1 19961113 A 3350 6104789 BATTERY PACK BOEING 737 737201 1384454 NM CARGO COMPT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 227AU 21816 ROA - MAINTENANCE FOUND THE RIGHT OVERWING EXTERIOR EMERGENCY EXIT LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BA TTERY PACK FOR THE RIGHT OVERWING EMERGENCY EXIT LIGHTS. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1996121900716 19961219 00716 NE 1996 12 19 SIMA963311 2 19961126 A 7320 311489201 SWITCHING VLV AEROSP ATR72 ATR72212 EU PWA PW120 PW127 NE RT ENGINE FAILED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 408AT 408 DFW - FLT 3864 - FLIGHT ATTENDANT REPORTED SMELLING SMOKE, LIKE BURNING RUBBER, AFTER LANDING. TURNED OFF PACKS AND THA T SEEMED TO CURE PROBLEM. RAI'D P2.5/P3 SWITCHING VALVE IAW JIC 72-30-00. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SE RVICE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1996121900717 19961219 00717 EU 1996 12 19 SIMA963331 1 19961128 A 3350 3011151 POWER SUPPLY AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 47AE 9317 047 SGF - FLT 3688 - FORWARD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED POWER SUPPLY UNIT 3WL. OPS CHECK SATISFACTOR Y. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996121900718 19961219 00718 NM 1996 12 19 96ZZZM1565 1 19961025 A 3397 WIRE BOEING 737 7372P6 1C84609 NM CABIN BROKEN A A6XA K NONE L NO TEST CR CRUISE 1 SO 13 EICLK EMERGENCY TRACK LIGHT FOUND INOPERATIVE. MAINTENANCE FOUND BROKEN WIRE, SOCKET AND LAMP. 2 L 7 2 4F RT A16WE 1996121900719 19961219 00719 NM 1996 12 19 96ZZZM1566 1 19961021 A 3350 08163023610 LIGHT BOEING 737 7372P6 NM CABIN SERVICEABLE A A6XA K NONE L NO TEST IN INSP/MAINT 1 SO 13 EICKL 21356 WIRE STICKING OUT OF EMERGENCY FLOOR TRACK LIGHTING. PASSENGER KICKED UP TRACK LIGHTING COVERING. WIRE RESECURED IN TR ACK COVER. 2 L 7 2 4F RT A16WE 1996121900720 19961219 00720 NM 1996 12 19 GAIA9635 1 19961123 A 2611 SMOKE DETECTOR BOEING 727 727251 138408H NM CARGO COMPT MALFUNCTIONED A GAIA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 279US 21158 FLT NR 279 - BRO-DFW - DURING CRUISE THE CARGO COMPARTMENT SMOKE DETECTOR ILLUMINATED. VISUALLY VERIFIED NO SMOKE PRESE NT IN CARGO CABIN. MAINTENANCE COULD NOT DUPLICATE INDICATION, SMOKE DETECTOR SYSTEM CHECKED PER MM 26-31. AIRCRAFT RE LEASED FOR FLIGHT. SUSPECT MOISTURE CONDENSATION ON THE SMOKE DETECTOR LENS. (M) 2 L 7 3 4F A3WE 1996121900721 19961219 00721 WP 1996 12 19 GAIA9636 1 19961126 A 5313 5916441 LONGERON DOUG DC9 DC915F 3022037 WP BS 360 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING C-CHECK INSPECTION, REVEALED TWO CRACKS ON LONGERON 30 BY THE PRODUCTION SPLICE AT FUSELAGE STATION 360. REPAIRE D LONGERON IAW KITTY HAWK EA D9-35-040. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1996121900722 19961219 00722 EU 1996 12 19 SIMA963271 1 19961122 A 3350 3011206 LIGHT AEROSP ATR72 ATR72202 8680940 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 252AM 573 253 ORD - DURING A-CHECK INSPECTION, FOUND LEFT EXTERIOR FORWARD FUSELAGE LIGHT 89WL INOP. RAI'D GROUND ILLUMINATION LIGHT PER JIC 33-51-24. PERFORMED GRUOND OPERATION CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996121900723 19961219 00723 NE 1996 12 19 SIMA963281 2 19961123 A 7320 310848501 VALVE AEROSP ATR72 ATR72212 EU PWA PW120 PW127 NE LT ENGINE FAILED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 288AM 288 DFW - FLT 3655 - PILOT SQUAWKED ELECTRICAL SMOKE INDICATION AFTER ENGINE START. MX REMOVED AND REPLACED P2.5 SWITCHING VALVE. GROUND RUN CHECKS WERE SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1996121900724 19961219 00724 NM 1996 12 19 TWRA96349 1 19961023 A 3350 276005 FUSE BOEING 747 747212B 1384886 NM CABIN BLOWN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 6186 21439 DURING SERVICE FOUND L2 DOOR ALL THREE EXIT SIGN OVERHEAD INOP. FOUND FUSES BURNED OUT AT BATTERY CHARGER. REPLACED TH E FUSES. SYSTEM OPS CHECKED NORMAL PER MM 33-51-00 PAGE 501. (M) 2 L 7 4 4F A20WE 1996121900725 19961219 00725 NM 1996 12 19 TWRA96345 1 19961025 A 3230 PIN BOEING 747 747212B 1384886 NM NLG INSTALLED A TWRA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 6186 21439 AFTER TAKEOFF NOSE GEAR AND DOORS WOULD NOT RETRACT. PRIMARY AND ALTERNATE NOSE DOWN AND NOSE DOOR OPEN LIGHT ILLUMINAT ED WITH LANDING GEAR HANDLE IN UP POSITION. FOUND NOSE GEAR PIN INSTALLED. REMOVED PIN. CHECKED NOSE GEAR. ALL NORMA L AS PER MM 32-21-00. (M) 2 L 7 4 4F A20WE 1996121900726 19961219 00726 NM 1996 12 19 TWRA96366 1 19961125 A 3350 3004181 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 620FF 235 21162 DURING DAILY CHECK, FOUND 2L MED UPPER BUSTLE EMERGENCY LIGHT INOP. REMOVED AND REPLACED 2L MED BUSTLE LIGHT PER MM 33- 51-00. OPS CHECKED NORMAL. (M) 2 L 7 4 4F A20WE 1996121900727 19961219 00727 EU 1996 12 19 AWXA9600663 1 19961109 A 3350 321454 BATTERY AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 641AW 453 PHX - FLT 7 - EMERGENCY EXIT LIGHT RIGHT OVERWING LIGHT BATTERY FAILED TEST. REMOVED AND REPLACED BATTERY. OPERATIONS CHECK GOOD. (M) 2 L 7 2 4F RT A28NM 1996121900728 19961219 00728 EU 1996 12 19 AWXA9600664 1 19961110 A 3350 CONNECTOR AIRBUS 320 A320231 3930325 EU CABIN LOOSE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 629AW 076 PHX - FLT 2050 - EMERGENCY LIGHT INOP AT ROW 26. RE-PINNED CANNON PLUG. OPERATIONS CHECK GOOD. (M) 2 L 7 2 4F RT A28NM 1996121900729 19961219 00729 EU 1996 12 19 SIMA963327 1 19961127 A 3213 D226850401310 TRUNNION LEG AEROSP ATR42 ATR42300 8680920 EU LEFT FAILED INSP A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 242AT 17591 17591 MN84 242 ORD - LEFT LANDING GEAR FAILED ULTRASOUND INSPECTION OF TRUNNION LEG AS PER MESSIER DOWTY TECHNIQUE A/VT NO 20317/96 (FC D E-9-32-002). REPLACED GEAR ASSEMBLY IAS ATR 42 JIC 32-11-00. OPS CHECK AND LEAK CHECK GOOD. AIRCRAFT WAS RETURNED T O SERVICE. (M) 2 H 7 2 4T RT A53EU 1996121900730 19961219 00730 EU 1996 12 19 SIMA963326 1 19961127 A 3213 D2268604068 TRUNNION LEG AEROSP ATR42 ATR42300 8680920 EU RIGHT FAILED INSP A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 242AT 11041 11041 MN233 242 ORD - RIGHT LANDING GEAR FAILED ULTRASOUND INSPECTION OF TRUNNION LEG AS PER MESSIER, DOWTY TECHNIQUE A/VT NR 20317/96 ( FCD E9-32-002). REPLACED GEAR ASSEMBLY IAW ATR 42 JIC 32-11-00. OPS CHECK AND LEAK CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996121900731 19961219 00731 EU 1996 12 19 SIMA963325 1 19961127 A 3213 D226860401 TRUNNION LEG AEROSP ATR42 ATR42300 8680920 EU RIGHT FAILED INSP A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 430MQ 10215 10215 MN110 0136 ORD - RIGHT LANDING GEAR FAILED ULTRASOUND INSPECTION OF TRUNNION LEG AS PER MESSIER DOWTY TECHNIQUE A/VT NR 20317/96 (F CD E9-32-002). REPLACED GEAR ASSEMBLY IAW ATR 42 JIC 32-11-00. OPS CHECK AND LEAK CHECK GOOD. AIRCRAFT WAS RETURNED T O SERVICE. (M) 2 H 7 2 4T RT A53EU 1996121900732 19961219 00732 EU 1996 12 19 SIMA963324 1 19961127 A 3213 D226860404 TRUNNION LEG AEROSP ATR42 ATR42300 8680920 EU RIGHT FAILED INSP A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 262AT 13808 13808 MN143 0262 ORD - RIGHT LANDING GEAR FAILED ULTRASOUND INSPECTION OF TRUNNION LEG AS PER MESSIER DOWTY TECHNIQUE A/VT NR 20317/96 (F CD E9-32-002). REPLACED GEAR ASSEMBLY IAW ATR 42 JIC 32-11-00. OPS CHECK AND LEAK CHECK GOOD. AIRCRAFT WAS RETURNED T O SERVICE. (M) 2 H 7 2 4T RT A53EU 1996121900733 19961219 00733 EU 1996 12 19 SIMA963322 1 19961127 A 3213 D226850401310 TRUNNION LEG AEROSP ATR42 ATR42300 8680920 EU LEFT FAILED INSP A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 135MQ MN23 135 LEFT LANDING GEAR FAILED ULTRASOUND INSPECTION OF TRUNNION LEG AS PER MESSIER DOWTY TECHNIQUE A/VT NR 20317/96 (FCD E9-3 2-002). REPLACED GEAR ASSEMBLY IAW ATR 42-JIC 32-11-00. OPS CHECK AND LEAK CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVI CE. (M) 2 H 7 2 4T RT A53EU 1996121900734 19961219 00734 EU 1996 12 19 SIMA963321 1 19961127 A 3213 D226850406 TRUNNION LEG AEROSP ATR42 ATR42300 8680920 EU LEFT FAILED INSP A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 430MQ 10215 10215 MV237 0136 ORD - LEFT LANDING GEAR FAILED ULTRASOUND INSPECTION OF TRUNNION LEG AS PER MESSIER DOWTY TECHNIQUE A/VT NR 20317/96 (FC D E9-32-002). REPLACED GEAR ASSEMBLY IAW ATR 42 JIC 32-11-00. OPS CHECK AND LEAK CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996121900735 19961219 00735 SO 1996 12 19 C2XA96CL042 1 19961118 A 3233 2060500005 ACTUATOR EMB 120 EMB120RT SO NLG FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 31711 12650 124 120107 SDF - FLT 4244 - CREW REPORTED THAT AFTER TAKEOFF, THE NOSE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT WAS FERRIED TO CLE, MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE NOSE LANDING GEAR ACTUATOR IAW EMB 120 MM 32-32-11 . ALL OPERATIONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1996121900736 19961219 00736 EU 1996 12 19 C2XA96BT018 1 19961116 A 3234 F96GA0102 CONTROL LEVER AEROSP ATR42 ATR42320 8680930 EU COCKPIT INTERMITTENT A C2XA O OTHER J WARNING INDICATION AP APPROACH 1 SW 09 86842 13002 361 286 EWR - FLT 3557 - INBOUND FOR NEWARK, CREW REPORTED LANDING GEAR HAD TO BE EMERGENCY EXTENDED. AIRCRAFT LANDED WITHOUT I NCIDENT. LANDING GEAR WAS MEL'D DOWN UNDER MEL 32-31-3 PLACARD NR 896997 AND RETURNED TO SERVICE. A/C RON'D IN BTV MAI NTENANCE. FOUND LANDING GEAR SELECTOR CONTROL LEVER TO BE INTERMITTENT, REMOVED AND REPLACED CONTROL LEVER IAW JIC 32-3 1-81. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996121900737 19961219 00737 EU 1996 12 19 C2XA96BT019 1 19961116 A 3350 3011180A POWER SUPPLY AEROSP ATR42 ATR42300 8680920 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16824 166 BTV - AIRCRAFT IN MAINTENANCE FOR 'A' CHECK FOUND UPPER AFT EMERGENCY EXIT SIGNS AND EVERY OTHER FLOOR TRACK LIGHT INOPE RATIVE. REMOVED AND REPLACED POWER SUPPLY AT STATION 15WL. SYSTEM OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A53EU 1996121900738 19961219 00738 SO 1996 12 19 C2XA96IA282 1 19961119 A 5347 12026865609 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 58733 120197 IAH - INSPECTION CHECK 1C, 2C, 4C - DURING A ROUTINE INSPECTION, THE AFT CABIN RIGHT FLOOR LEVEL SEAT TRACK WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE DAMAGED TRACK AND THE AIRCRFT WAS LATER APPROVED FOR R ETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996121900739 19961219 00739 SO 1996 12 19 C2XA96IA283 1 19961119 A 5347 12015994003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 58733 120197 IAH - INSPECTION CHECK 1X, 2C, 4C, - DURING A ROUTINE INSPECTION, THE FORWARD CABIN LEFT SIDEWALL SEAT TRACK WAS FOUND T O BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE DAMAGED TRACK AND THE AIRCRAFT WAS LATER APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996121900740 19961219 00740 SO 1996 12 19 C2XA96IA284 1 19961119 A 5347 12015997603 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 58733 120197 IAH - INSPECTION CHECK 1C, 2C, 4C - DURING A ROUTINE INSPECTION, THE FORWARD CABIN RIGHT SIDEWALL SEAT TRACK WAS FOUND T O BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE DAMAGED TRACK AND THE AIRCRAFT WAS LATER APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996121900741 19961219 00741 SO 1996 12 19 C2XA96IA285 1 19961119 A 5347 12015995003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 58733 120197 IAH - INSPECTION CHECK 1C, 2C, 4C - DURING A ROUTINE INSPECTION, THE FORWARD CABIN FLOOR LEVEL LEFT SEAT TRACK WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACD THE DAMAGED TRACK AND THE AIRCRAFT WAS LATER APPROVED FO R RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996121900742 19961219 00742 SO 1996 12 19 C2XA96IA286 1 19961119 A 5347 12016000603 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 58733 120197 IAH - INSPECTION CHECK 1C, 2C, 4C - DURING A ROUTINE INSPECTION, THE FORWARD CABIN FLOOR LEVEL RIGHT SEAT TRACK WAS FOUN D TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SEAT TRACK AND THE AIRCRAFT WAS LATER RETU RNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996121900743 19961219 00743 SO 1996 12 19 C2XA96IA287 1 19961119 A 5320 12027929001 BUTT STRAP EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 58733 120197 IAH - INSPECTION CHECK 1C, 2C, 4C - DURING A ROUTINE INSPECTION, THE AFT CABIN CENTER FLOOR BEAM BUTT STRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES NR 33-39. MAINTENANCE REMOVED AND REPLACED THE DAMAGED PORTION OF THE BUTT STRAP AND THE AI RCRAFT WAS LATER APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996121900751 19961219 00751 WP 1996 12 19 96ZZZX6117 1 19961203 A 5347 340302 SEAT TRACK CVAC 440 440 2422902 WP CABIN CORROSION A P21A K NONE O OTHER IN INSP/MAINT 1 WP 09 8042W 503 DURING B-1/B-2 INSPECTION, THE RT OUTBOARD FORWARD SEAT TRACK (MAIN CABIN) WAS FOUND TO HAVE INTERGRANULAR CORROSION ON THE TRACK. REMOVED AND REPLACED WITH NEW TRACK. AIRCRAFT WILL BE RETURNED TO SERVICE AFTER INSPECTION IS COMPLETED. 2 L 7 2 4R 6A6 1996121900762 19961219 00762 NM 1996 12 19 ANCF173C 1 19961114 A 5270 WARNING LIGHT BOEING 767 767259 1385136 NM EMERG DOOR ILLUMINATED W ANCF C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 23 985AN 28066 15376 24618 MAC/BOG - FLT 011 - EMERGENCY DOOR LIGHT ILLUMINATED STEADY EICAS MSG L EMER DOOR DISPLAYED STEADY. TAKEOFF WAS REJECTE D AT 129 KNOTS. PERFORMED PROCEDURE FOR F1M 52-71-00 FIG 105 THE OVERWING EMERG EXIT LT SIDE BITE CHECKED TO PROXIMITY SWITCH AND NO FAULT FOUND. DUE TAKEOFF REJECTED INSP WAS ACCOMPLISHED ACCORDING TO AMM 05-51-15. THE 8 BRAKES AND WHEE LS ASSY WERE CHANGED. BRAKES WERE BLED AND HYDRAULIC SYSTEM REFILLED TO CORRECT LEVEL. (X) 2 L 7 2 4F RT A1NM 1996121900770 19961219 00770 EU 1996 12 19 CA960415009 1 19960404 A 2435 03601018 BEARING LUCAS 23079009 BAG JETSTM JETSTM3212 1500217 EU STARTER DRV END FAILED W A K NONE O OTHER IN INSP/MAINT 1 CA 761 6139 (CAN)ANTI-DRIVE END BEARING FAILURE CAUSING EXTENSIVE DAMAGE TO ARMATURE AND STARTER ASSEMBLY. 2 L 7 2 4T RT BA15CAA 1996121900771 19961219 00771 EU 1996 12 19 CA960502018 1 19960228 A 2913 704A33690004 BELT SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1B 6OO30 NE HYD PUMP DRIVE BROKEN W A B UNSCHED LANDING EMER. DESCENT F FLT CONT AFFECTED CR CRUISE 1 CA 419 290 (CAN) HYDRAULIC BELT FAILED IN FLIGHT. 1 G 7 1 3U 3 U H9EU E19EU 1996121900773 19961219 00773 EU 1996 12 19 CA960502021 1 19960301 A 6320 350A32030004 BEVEL REDUCTION SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE INPUT QUILL EXCESS PLAY W K NONE E VIBRATION/BUFFET IN INSP/MAINT 1 CA 8691 2135 347 (CAN) RADIAL AND AXIAL PLAY OF INPUT QUILL. REPORTED VIBRATION DURING POWER REDUCTION. NUT ON QUILL DOES NOT APPEAR TO H AVE BACKED OFF BUT WASHER BEHIND NUT CAN BE MOVED FREELY. 1 G 7 1 3U 3 U H9EU E19EU 1996121900774 19961219 00774 GL 1996 12 19 CA960502025 2 19960415 A 7323 23057870 GOVERNOR HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL PT GOV LEAKING W K NONE O OTHER IN INSP/MAINT 1 CA 651 CAE832104 (CAN) LEAKING PURPLE GREASE FROM INPUT. 1 G 7 1 3U 3 U H3WE E4CE 1996121900775 19961219 00775 SW 1996 12 19 CA960502028 1 19960406 A 6520 206040400009 GEARBOX BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL T/R WEARING W K NONE O OTHER IN INSP/MAINT 1 CA 11110 1390 CAE821443 (CAN) OIL CONSTANTLY DARK AND PASTE FOUND ON CHIP DETECTOR REPEATEDLY. 1 G 7 1 3U 3 U H2SW E4CE 1996121900776 19961219 00776 WP 1996 12 19 CA960502030 1 19960408 A 6420 369D2172313 PITCH LINK HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL T/R LOOSE BEARING W K NONE O OTHER IN INSP/MAINT 1 CA CAE830926 (CAN) SPHERICAL BEARING ON ONE END WAS FOUND HALF WAY OUT OF PITCH LINK. 1 G 7 1 3U 3 U H3WE E4CE 1996121900778 19961219 00778 SW 1996 12 19 CA960502060 1 19960419 A 6220 206011100025 MAIN ROTOR ASSY BELL 206 206L 1181522 SW YOKE SEIZED W K NONE O OTHER IN INSP/MAINT 1 CA 7142 278 (CAN) DURING A 100 HOUR INSPECTION, IT WAS NOTICED THAT ONE OF THE GRIP GREASE SEALS ON THE M/R ASSEMBLY WAS FURTHER OUT BOARD ON ONE SIDE OF THE YOKE. UPON DISASSEMBLY OF THE ASSEMBLY ONE FITTING COULD NOT BE REMOVED WITH THE TOOLS AVAILABL E. 1 G 7 1 3U H2SW 1996121900779 19961219 00779 1996 12 19 CA960502063 4 19960417 A 2215 07101103 CONTROL CABLE KING KFC200 PIPER PA31 PA31 7103102 SO ELEVATOR SERVO FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA 9500 (CAN) AUTOPILOT INOPERATIVE. AUTOPILOT SERVO ACTUATOR CABLE TO ELEVATOR BELLCRANK FRAYED AND BROKEN AT THE BUILHEAD PULL EY. CABLE GUARD ON THE PULLEY ALSO BROKEN. 1 L 7 2 3O A20SO 1996121900780 19961219 00780 CE 1996 12 19 CA960507001 1 19960422 A 2140 A24A9238 BLOWER MOTOR JANITROL E10D40S100 BEECH 99 99 1154002 CE PWA PT6 PT6A20 52043 EA COMB HEATER SEIZED W C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 CA 385 5691067 PCE21541 (CAN) ON TAKEOFF ROLL, TOWER ADVISED THAT FLAME VISIBLE ON BOTTOM OF AIRCRAFT, TAKEOFF ABORTED. COMBUSTION BLOWER MOTOR FOUND INOPERATIVE, OTHER HEATER SYSTEM FUNCTIONS CHECKED OK AT THIS TIME. 1 L 7 2 3T 3 T A14CE E4EA 1996121900781 19961219 00781 CE 1996 12 19 CA960507005 1 19960421 A 3230 RETRACT MECH BEECH BEECH 100 A100 1152915 CE PWA PT6 PT6A27 52043 EA MAIN GEAR MALFUNCTION W A UNSCHED LANDING O OTHER CL CLIMB 1 CA PCE40865 (CAN) AFTER TAKEOFF, UNDERCARRIAGE REFUSED TO RETRACT. ELECTRICAL CIRCUIT INSPECTED, CONNECTIONS CHECKED AND SEVERAL RET RACTIONS PERFORMED ON JACKS WITHOUT THE FAULT RECURRING, UNABLE TO DETERMINE CAUSE. 1 L 7 2 3T 4 T A14CE E4EA 1996121900782 19961219 00782 CE 1996 12 19 CA960507008 1 19960318 A 3246 115800118 WHEEL HALF BFG 11580014 BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA NEAR BOLT HOLE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 441 D2273 PCE50228 (CAN) WHEEL LOSING AIR PRESSURE. WHEEL HALF CRACKED 1.5 INCH AROUND THE TIE BOLT HOLE. 1 L 7 2 3T 4 T A14CE E4EA 1996121900783 19961219 00783 CE 1996 12 19 CA960507009 1 19960320 A 3246 115800116 WHEEL HALF BFG 11580014 BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA BEAD RIM CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 19 KA0099 PCE50228 (CAN) WHEEL LOSING 70 PSI AIR PRESSURE IN 24 HOURS. 3 INCH CRACK AROUND WHEEL RIM IN THE BEAD AREA. 1 L 7 2 3T 4 T A14CE E4EA 1996121900784 19961219 00784 CE 1996 12 19 CA960507012 1 19960501 A 2913 98811411 MOTOR CESSNA 98811241 CESSNA 210 210R 2073458 CE CONT O520 IO520L 17032 SO MCAULY D3A34 D3A34C404 GL MLG PWR PAC OVERHEATED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA 6888 270293R 850299 (CAN) CREW REPORTED BURNT SMELL AND UNDERCARRIAGE CIRCUIT BREAKER POPPED. GEAR LOWERED BY HAND PUMP. HYDRAULIC POWERPACK MOTOR RUNNING SLOW AND OVERHEATING. MOTOR REPLACED. 1 H 7 1 3O 3 O RT 3A21 E5CE 5 C P47GL 1996121900785 19961219 00785 CE 1996 12 19 CA960507014 1 19960404 A 3213 07410018 GEAR LEG CESSNA 185 A185F 2072821 CE MCAULY D3A34 D3A34C403 GL AXLE BOLT HOLE BROKE W K NONE O OTHER LD LANDING 1 CA 7710576 (CAN) ON SLOWING DOWN AFTER LANDING ON SKIS, LEFT GEAR BROKE AT THE UPPER AXLE ATTACHMENT BOLT HOLES. THIS AIRCRAFT HAS HAD PREVIOUS REPAIRS DUE TO A HARD LANDING ON SKIS. 1 H 7 1 3O 3A24 5 C P47GL 1996121900786 19961219 00786 SO 1996 12 19 CA960507016 1 19960429 A 2140 A23D0475 REGULATOR JANITROL 650792 PIPER PA31 PA31350 7103110 SO HEATR FUEL PRESS LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 3 516881 (CAN) FUEL STAIN ON BELLY OF AIRCRAFT TRACED TO LEAKING HEATER FUEL PRESSURE REGULATOR. THIS IS THE THIRD SUCH OCCURRENC E IN THE LAST FEW HOURS OF OPERATION. 1 L 7 2 3O A20SO 1996121900787 19961219 00787 CE 1996 12 19 CA960507017 1 19960429 A 7120 50980089 ATTACHMENT ASSY BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA ENG MOUNT HOLES ELONGATED W K NONE O OTHER IN INSP/MAINT 1 CA 40000 50747 (CAN) ENGINE MOUNT STRUCTURE LOOSING INTEGRITY DUE TO SEVERAL LOOSE RIVETS AND ELONGATED RIVET HOLES. 1 L 7 2 3T 4 T A14CE E4EA 1996121900790 19961219 00790 SW 1996 12 19 CA960514103 1 19960508 A 2911 2120760073 ACCUMULATOR BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA HYD CYLINDER CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 9601 3872 CPPS61805 (CAN) FOUND CORROSION PITTING ON CYLINDER FROM OUTSIDE TO INSIDE. PITTING APPROXIMATELY 1/8" DIAMETER. 1 G 7 1 4U 4 U H4SW E22EA 1996121900791 19961219 00791 WP 1996 12 19 CA960514106 1 19960506 A 5610 369H202481 DOOR WINDOW HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL PILOTS DOOR FAILED W K NONE D INFLIGHT SEPARATION CR CRUISE 1 CA CAE831949 (CAN) HELICOPTER IN CRUISE, APPROXIMATELY 120 KNOTS, WHEN PILOTS WINDOW IMPLODED THEN EXITED AND SHATTERED. 1 G 7 1 3U 3 U H3WE E4CE 1996121900792 19961219 00792 CE 1996 12 19 CA960515002 1 19960507 A 3411 53335 STATIC SENSOR NARCO AR850 BEECH 95 E95 1153410 CE LYC O360 IO360B1B 41514 EA HOUSING LEAK W K NONE O OTHER IN INSP/MAINT 1 CA 53335 RL162451A (CAN) PIEZO STATIC SENSOR HOUSING LEAKING IN EXCESS OF LIMITS 1 L 7 2 3O 3 O 3A16 1E10 1996121900796 19961219 00796 1996 12 19 CA960515006 4 19960209 A 2210 100000901 TURN AND SLIP KING H14B274 BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA YAW RATE MALFUNCTION W H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED CR CRUISE 1 CA 236 PCE50280 (CAN) AUTOPILOT DOES NOT MAINTAIN BANK ANGLES IN RIGHT TURN ONLY, ROLLS 45 DEGREES, PITCHES DOWN. SYSTEM TROUBLESHOT AND EVENTUALLY TURN AND SLIP INDICATORS REPLACED AND AIRCRAFT RETUNED TO SERVICE. ADDITIONAL SDR 960222011 WITH SAME TROU BLE ON ANOTHER AIRCRAFT. 1 L 7 2 3T 4 T A14CE E4EA 1996121900797 19961219 00797 CE 1996 12 19 CA960515009 1 19960506 A 2434 C8FF10A396A TIE BOLT FORD C6115030104R CESSNA 210 210R 2073458 CE CONT O520 IO520L 17032 SO MCAULY D3A34 D3A34C404 GL ALTERNATOR CASE BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 541 A74402 294530 850299 (CAN) ALTERNATOR CASE TIE BOLT BROKEN IN THREADED AREA, 1/2 INCH FROM THE END OF THE BOLT. THIS IS THE 3RD SIMILAR OCCUR RENCE ON THIS AIRCRAFT. PREVIOUS CASES WERE ON DIFFERENT S/N ALTERNATORS. 1 H 7 1 3O 3 O RT 3A21 E5CE 5 C P47GL 1996121900798 19961219 00798 CE 1996 12 19 CA960517101 1 19960425 A 3230 1048200501 ARM BEECH 958100175 BEECH 95 95B55 1152729 CE CONT O470 IO470L 17026 SO NLG ACTUATOR BROKEN W A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 CA 3140 CS20170473L (CAN) ON GEAR EXTENSION, A SNAP SOUND WAS HEARD AND NO INDICATION OF GEAR DOWN. CONTROL TOWER REPORTED NOSE GEAR AT 45 D EGREES. NOSE GEAR COLLAPSED ON LANDING. ACTUATOR ARM BROKEN AT MID-LENGTH. 1 L 7 2 3O 3 O RT 3A16 3E1 1996121900800 19961219 00800 GL 1996 12 19 CA960522005 1 19960508 A 6410 281500021 BLADE ENSTRM F28 F28C 3300407 GL LYC O360 HIO360E1AD 41514 EA T/R DELAMINATION W K NONE O OTHER IN INSP/MAINT 1 CA 750 L2006851A (CAN) BLADE DELAMINATING IN MID PART OF BLADE TOWARDS LEADING EDGE. 1 G 7 1 3O 3 O H1CE 1E10 1996121900801 19961219 00801 SW 1996 12 19 CA960522006 1 19960501 A 6330 204031928009 MOUNT ASSEMBLY BELL 212 212 1181420 SW PWA PT6T PT6T3B 52045 NE XMSN MOUNT VIBRATION W K NONE O OTHER IN INSP/MAINT 1 CA CPPS62436 (CAN) AT 90 KNOTS INDICATED AND AT 11,200 GROSS WEIGHT HELICOPTER DEVELOPED AN AIRFRAME LATERAL VIBRATION. BELL HELICOPT ERS RECOMMENDED REMOVAL/REPLACEMENT OF MOUNT ASSEMBLY P/N 204-031-928-009, 5TH MOUNT ASSEMBLY P/N 204-031-927-005, BOLT ASSEMBLY P/N 204-031-244-005, LINK ASSEMBLY P/N 212-030-104-005 AND FRICTION DAMPER P/N 204-031-920-003. PARTS CHANGED, COULD NOT DUPLICATE PROBLEM. 1 G 7 1 4U 4 U H4SW E22EA 1996121900802 19961219 00802 SO 1996 12 19 CA960524026 1 19960501 A 7120 1235112 MOUNT PIPER PA18 PA18135 7101820 SO LYC O320 O320A2B 41508 EA ENGINE BROKEN TUBING W K NONE O OTHER IN INSP/MAINT 1 CA RC5032227A (CAN) CUSTOMER REPORTED THAT COWLING WAS RUBBING ON THE OIL COOLER. INSPECTION REVEALED THAT ENGINE WAS SAGGING TO THE R IGHT DUE TO A BROKEN ENGINE MOUNT. 1 H 7 1 3O 3 O 1A2 E274 1996121900803 19961219 00803 SW 1996 12 19 CA960524027 1 19960509 A 3212 212050207101 FLOAT BAG ASSY BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA AFT L/H OUTBOARD SEPARATION W K NONE O OTHER IN INSP/MAINT 1 CA 2691 CPPS61494 (CAN) DURING DEPLOYMENT AS PART OF PERIODIC INSPECTION 4TH AFT BAG LOST PRESSURE. LEAK DETECTED AROUND VALVE ASSEMBLY P/ N 492-8D1-2. 1 G 7 1 4U 4 U H4SW E22EA 1996121900804 19961219 00804 SO 1996 12 19 CA960527001 1 19960508 A 3244 TIRE CLEVELAND 40166 PIPER PA42 PA42 7104202 SO PWA PT6 PT6A41 52043 EA L.H. MAIN BURST W O OTHER O OTHER LD LANDING 1 CA PCE85163 (CAN) ON LANDING, LEFT MAIN TIRE BLEW UP. NO OTHER DAMAGE. 1 L 7 2 4T 4 T A23SO E4EA 1996121900805 19961219 00805 CE 1996 12 19 CA960527003 1 19960513 A 3231 11581006052 GEAR DOOR BEECH 99 99 1154002 CE PWA PT6 PT6A20 52043 EA L.H. INBOARD JAMMED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA PCE22549 (CAN) GEAR IN TRANSIT LIGHT STAYED ON AFTER GEAR RETRACTION. EMERGENCY GEAR EXTENSION RESULTED IN L.H. GEAR PARTIALLY EX TENDED. L.H. MAIN INBOARD GEAR DOOR JAMMED, PREVENTING GEAR EXTENSION. 1 L 7 2 3T 3 T A14CE E4EA 1996121900806 19961219 00806 CE 1996 12 19 CA960527004 1 19960515 A 2497 P100L8 WIRE BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA RT CB PANEL LOOSE W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA 36430 50587 (CAN) SMOKE IN COCKPIT. ARCING AND BURNING BEHIND RT CIRCUIT BREAKER PANEL. PO WER WIRE P100L8 WAS LOOSE. 1 L 7 2 3T 4 T A14CE E4EA 1996121900810 19961219 00810 NM 1996 12 19 CA960529001 1 19960515 A 2820 A72917 VENT LINE ROBSIN R22 R22BETA NM LYC O320 O320B2C 41508 EA AUX TANK KINKED W K NONE O OTHER IN INSP/MAINT 1 CA 1946 L1462339A (CAN) FUEL WAS VERY SLOW TO DRAIN FROM AUXILIARY TANK TO MAIN TANK AND SELECTOR VALVE. THE AUXILIARY TANK VENT LINE WAS FOUND KINKED OVER THUS BLOCKING ANY AIR FLOW INTO TANK. THE SUSPECTED CAUSE OF THIS CONDITION WAS THE ROTOR BRAKE ENGAGE MENT CHAIN WHICH APPEARS TO HAVE CAUGHT ON THE LOCK WIRE ATTACHING THE FLEXIBLE VENT TUBE TO THE SOLID VENT FLANGE ON TH E TANK. WHEN THE ROTOR BRAKE WAS ENGAGED THE TUBE WAS PULLED INTO THE KINKED POSITION. 1 G 7 1 3O 3 O H10WE E274 1996121900811 19961219 00811 CE 1996 12 19 CA960529005 1 19960513 A 3230 4027000 FILTER ELECTROMECH 1153800025 BEECH 99 B99 1154004 CE PWA PT6 PT6A27 52043 EA GEAR MOTOR MALFUNCTION W O OTHER J WARNING INDICATION AP APPROACH 1 CA 1189 PCE41224 (CAN) LANDING GEAR FAILED TO EXTEND, HAND PUMP WAS USED. LANDING GEAR MOTOR NOT RUNNING WHEN POWER APPLIED. RFI FILTER I NTERMITTENT, REPLACED. 1 L 7 2 3T 4 T A14CE E4EA 1996121900813 19961219 00813 CE 1996 12 19 CA960529011 1 19960514 A 3250 50420101 BELLCRANK CESSNA 5842000207 CESSNA 310 310R 2074245 CE CONT O520 IO520M 17032 SO MCAULY 3AF32C 3AF32C87 GL NLG STEERING CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 7259 270662R 696863 (CAN) NOSE WHEEL STEERING BELLCRANK CRACKED IN THE RADIUS OF THE MAIN ATTACH PIVOT POINT AT ALL FOUR CORNERS. 1 L 7 2 3O 3 O 3A10 E5CE 5 C P22EA 1996121900815 19961219 00815 SW 1996 12 19 CA960530003 1 19960415 A 6310 206040015103 DRIVESHAFT BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL MAIN DRIVE TORN BOOT W K NONE O OTHER IN INSP/MAINT 1 CA 3104 75 CAE832648 (CAN) RUBBER BOOT COMPLETELY TORN. 1 G 7 1 3U 3 U H2SW E4CE 1996121900816 19961219 00816 SW 1996 12 19 CA960530004 1 19960513 A 6220 471103781 TIE ROD BELL 47 47G3B1 1181028 SW ALLSN 250C 250C20 03013 GL M/R HEAD SHEARED W A UNSCHED LANDING D E INFLIGHT SEPARATION VIBRATION/BUFFET CR CRUISE 1 CA 663 CAE822192 (CAN) THE COUNTERWEIGHT ROD SHEARED AT THE BASE OF THE SPACER AND DRAG BRACE ATTACHMENT ON THE MAIN ROTOR HEAD. THE COUN TERWEIGHT, WASHERS AND SPACER LEFT THE AIRCRAFT CAUSING A VIBRATION IN THE AIRCRAFT AND FLIGHT CONTROLS. THE TIE ROD IS SUBJECT TO A 300 HOUR MAGNAFLUX INSPECTION (ASB 47-78-2) WHICH HAD BEEN CARRIED OUT 116.5 HOURS PREVIOUS TO FAILURE. 1 G 7 1 3O 3 U 2H3 E4CE 1996121900818 19961219 00818 EU 1996 12 19 CA960604009 1 19960522 A 6510 112131531 DISK ASSEMBLY BOLKMS 105 BO105C 5626005 EU ALLSN 250C 250C20B 03013 GL INPUT IGB DEFECTIVE W K NONE E VIBRATION/BUFFET TX TAXI/GRND HDL 1 CA 3427 CAE834769 (CAN) AFTER COMPLETING A 100 HOUR AND BALANCING THE TAIL ROTOR A VIBRATION WAS FELT THROUGH THE PEDALS. FURTHER TROUBLES HOOTING REVEALED THE DISK ASSEMBLY WAS NOT AS STIFF AS ON OTHER AIRCRAFT. DISK ASSEMBLY CHANGED, VIBRATION DISAPPEARED. 1 G 7 2 3U 3 U H3EU E4CE 1996121900819 19961219 00819 EU 1996 12 19 CA960604019 1 19960512 A 3020 1092T100 ACTUATOR BOLKMS 105 BO105C 5626005 EU ALLSN 250C 250C20B 03013 GL #1 ENG AI SHORTED W K NONE O OTHER IN INSP/MAINT 1 CA CAE835656 (CAN) AFTER INSTALLATION OF ACTUATOR THE INITIAL TEST RESULTED IN THE CIRCUIT BREAKER TRIPPING, DIODE 1N4007 SHORTED AND RELAY W25OD4A FAILED. 1 G 7 2 3U 3 U H3EU E4CE 1996121900820 19961219 00820 EU 1996 12 19 CA960605001 1 19960528 A 5600 M1052330113 WIND DEFLECTOR BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL PASSENGER DOOR DEBONDED W A UNSCHED LANDING D C INFLIGHT SEPARATION F.O.D. CR CRUISE 1 CA 5637 CAE835711 (CAN) WHILE SLIDING PASSENGER DOOR WINDOW TO THE CLOSED POSITION THE WIND DEFLECTOR DEBONDED AND CAME OFF THE AIRCRAFT S TRIKING THE HORIZONTAL STABILIZER. 1 G 7 2 3U 3 U H3EU E4CE 1996121900821 19961219 00821 SW 1996 12 19 CA960605006 1 19960517 A 5210 206033601140 DOOR BELL 206 206L4 1182110 SW STATION 116 CRACKED W K NONE O E OTHER VIBRATION/BUFFET CR CRUISE 1 CA 858 (CAN) DURING FLIGHT THE TWO REAR DOORS OPENED COMPLETELY. THE RIGHT REAR DOOR STARTED TO VIBRATE AND BROKE AT STATION 11 6 AT THE INTERIOR REINFORCEMENT. 1 G 7 1 3U NC H2SW 1996121900822 19961219 00822 SW 1996 12 19 CA960606006 1 19960525 A 2910 6000D4 HYD SOCKET BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL MAIN HYD LEAKING JOINT W K NONE K FLUID LOSS IN INSP/MAINT 1 CA CAE800419BA (CAN) SMALL LEAK AT JOINT CONNECTION. 1 G 7 1 3U 3 U H2SW E4CE 1996121900823 19961219 00823 SW 1996 12 19 CA960606007 1 19960524 A 6510 206040339009 BEARING BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL T/R DRIVE LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA 751 CAE800419BA (CAN) #1 HANGER BEARING LOOSE. EXCESSIVE PLAY BETWEEN INNER AND OUTER RACE. 1 G 7 1 3U 3 U H2SW E4CE 1996121900824 19961219 00824 SW 1996 12 19 CA960606008 1 19960525 A 6510 206040338009 HANGER BEARING BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL T/R DRIVE WORN W K NONE O OTHER IN INSP/MAINT 1 CA CAE800419BA (CAN) WEAR AT THE INSIDE OF SLEEVE AND #1 HANGER. 1 G 7 1 3U 3 U H2SW E4CE 1996121900825 19961219 00825 EU 1996 12 19 CA960606011 1 19960502 A 6210 BLC3LA12S LOCKING PIN BOLKMS 105 BO105C 5626005 EU ALLSN 250C 250C20B 03013 GL PIN END LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA CAE835628 (CAN) PIP PIN USED TO HOLD BLADE BOLT IN BLADE FOLDING SETUP, MISSING BALL BEARINGS. 1 G 7 2 3U 3 U H3EU E4CE 1996121900826 19961219 00826 EA 1996 12 19 CA960606101 2 19960531 A 7314 RG9080J4A FUEL PUMP LEARSIEGLER PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2B 41532 EA ENG DRIVEN LOW PRESSURE W A UNSCHED LANDING J R WARNING INDICATION PARTIAL RPM/PWR LOSS CR CRUISE 1 CA B4122019 L161761A (CAN) 5 MINUTES AFTER ESTABLISHING LEVEL CRUISE, LEFT ENGINE SLIGHT LOSS OF POWER. LOW FUEL PRESSURE RESTORED BY TURNING ELECTRICAL FUEL PUMP "ON". ENGINE DRIVEN FUEL PUMP REPLACED. 1 L 7 2 3O 3 O A20SO E14EA 1996121900828 19961219 00828 CE 1996 12 19 CA960610005 1 19960526 A 3230 26430621 SPRING CESSNA 26430621 CESSNA 208 208B 2073701 CE NOSE GEAR CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA 100 850702 (CAN) DURING ROUTINE MAINTENANCE IT WAS NOTICED THAT THE FIRST DZUS FASTENER ON THE LOWER NOSE GEAR FAIRING WAS CHAFING ON THE NOSE GEAR SPRING ONLY WHEN THE WHEEL WAS OFF THE GROUND. CORRECTIVE ACTION FINALLY HAD TO BE REPLACING THE FASTEN ER WITH A NUT PLATE AND SCREW. SUBMITTER NOTES A SIMILAR PROBLEM WITH OTHER CARAVANS IN THE FLEET. 1 H 7 1 3T A37CE 1996121900830 19961219 00830 SO 1996 12 19 CA960610013 1 19960531 A 2823 757257 O-RING PIPER 492111 PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2C 41532 EA FIREWALL SOV DAMAGED W O OTHER Y ENGINE STOPPAGE CR CRUISE 1 CA 11941 11941 L125561 (CAN) LEFT HAND ENGINE QUIT IN CRUISE FLIGHT WHEN THE ELECTRIC BOOST PUMPS WERE SELECTED OFF AND WOULD NOT RESTART. INVE STIGATION FOUND THE LEFT HAND FIREWALL SHUTOFF VALVE PARTIALLY OFF WITH THE CUT AND JAMMING O-RING STOPPING THE PROPER L EVER SELECTION. THIS CAUSED FUEL STARVATION TO THE ENGINE EVEN WITH THE ENGINE DRIVEN PUMPS FUNCTIONING. 1 L 7 2 3O 3 O A20SO E14EA 1996121900831 19961219 00831 CE 1996 12 19 CA960610014 1 19960603 A 3710 211CC PUMP SPLINE AIRBORNE 211CC CESSNA 182 R182 2072734 CE MCAULY 2D34C B2D34C214 GL REAR ACC.ENGINE SHEARED W H DEACTIVATE SYST/CIRCUITS I FLT. ATTITUDE INST. CR CRUISE 1 CA 1200 11AE9700 780298 (CAN) PILOT REPORTED LOST INDICATION OF VACUUM AND LOST VACUUM ACTIVATION FLIGHT INSTRUMENTS. MAINTENANCE FOUND PROBLEM TO BE THE SHEARED SHAFT OF THE VACUUM PUMP. SUBMITTER STATES THAT THE PUMP SHOWED SIGNS OF OVERHEATING. 1 H 7 1 3O RT 3A13 5 C P7EA 1996121900832 19961219 00832 CE 1996 12 19 CA960611008 1 19960524 A 3252 AN6227B10 O-RING CESSNA 22430013 CESSNA 182 R182 2072734 CE MCAULY 2D34C B2D34C214 GL PISTON HEAD CUT W C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CA 3947 3947 780298 (CAN) PILOT REPORTED NOSE WHEEL SHIMMY. MINOR LEAK ON SHIMMY DAMPER. PISTON HEAD "O" RING CUT. 1 H 7 1 3O RT 3A13 5 C P7EA 1996121900833 19961219 00833 CE 1996 12 19 CA960611010 1 19960524 A 3250 MS2878218 RETAINER CESSNA 22430013 CESSNA 182 R182 2072734 CE MCAULY 2D34C B2D34C214 GL SHIMMY DAMPENER MIS INSTALLED W C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CA 778345 (CAN) PILOT REPORTED A SHIMMY AT THE END OF THE TAKEOFF ROLE. INVESTIGATION FOUND THE RETAINER RING IN THE PISTON, INSTA LLED WITH A TWIST ALLOWING THE O-RING TO NOT SEAL PROPERLY. 1 H 7 1 3O RT 3A13 5 C P7EA 1996121900834 19961219 00834 CE 1996 12 19 CA960611011 1 19960604 A 3250 NAS464P23A3 BOLT CESSNA 2243001205 CESSNA 182 R182 2072734 CE MCAULY 2D34C B2D34C214 GL BELLCRANK COLLAR LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA 3562 778345 (CAN) ON PREFLIGHT, PILOT FOUND LOOSE BOLT ON TOP OF NOSE GEAR STRUT. BOLT ATTACHING STEERING BELLCRANK TO COLLAR LOOSE. 1 H 7 1 3O RT 3A13 5 C P7EA 1996121900835 19961219 00835 CE 1996 12 19 CA960611013 1 19960603 A 2750 151228041 CONTROL CABLE CESSNA 182 R182 2072734 CE MCAULY 2D34C B2D34C214 GL FLAP CONTROL BINDING W O OTHER W F INADEQUATE Q C FLT CONT AFFECTED CL CLIMB 1 CA 780298 (CAN) PILOT HAD TO RESELECT FLAPS UP SEVERAL TIMES BEFORE FLAPS WOULD RETRACT. WIRE BUNDLE FROM A GPS INSTALLATION WAS F OUND TIE WRAPPED TO THE FLAP SELECTOR ACTUATING CABLE AND PUTTING TENSION ON IT.INSTALLATION CLEANED UP. 1 H 7 1 3O RT 3A13 5 C P7EA 1996121900840 19961219 00840 EA 1996 12 19 CA960614004 1 19960512 A 6220 107R35581 BEARING BOEING 107 1072 9420604 EA GE CT58 CT581401 30011 NE M/R HEAD LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA 280239C (CAN) THE TEFLON LINING ON THE INNER RACE OF THE BEARING IS BREAKING OUT ALLOWING EXCESSIVE PLAY OF THE BEARING. 2 G 7 2 4U 4 U 1H16 1E3 1996121900841 19961219 00841 SO 1996 12 19 CA960614005 1 19960605 A 7810 124568 MANIFOLD TAB GRUMAN 124568 GRUMAV G21 G21A 3951204 SO PWA R985 R985AN14B 52008 NE RT ENG EXH BROKE W K NONE O OTHER IN INSP/MAINT 1 CA JP211111 (CAN) THE SINGLE TAB WHICH ATTACHES THE EXHAUST MANIFOLD TO THE EXHAUST COLLECTOR BROKE. THIS ALLOWED THE MANIFOLD TO RO TATE AND DIRECT ALL THE EXHAUST ON THE RIGHT HAND ENGINE ACCESSORY COWL. THIS DAMAGED THE REAR SECTION OF THE "HORSE COL LAR", RIGHT HAND GOVERNOR CABLE AND VARIOUS WIRES. 1 H 7 2 3R 3 R TC654 5E1 1996121900844 19961219 00844 SO 1996 12 19 CA960614012 1 19960605 A 3260 65430130 SWITCH GULSTM GA7 GA7 3960401 SO LYC O320 O320D1D 41508 EA NLG OVCENTER SHORTED W O OTHER N FALSE WARNING LD LANDING 1 CA 11004 L1727739A (CAN) NOSE GEAR UNSAFE ON GEAR EXTENSION. THE SWITCH ON THE NOSE GEAR OVERCENTER BRACE WAS SHORTED OUT. 1 L 7 2 3O 3 O A17SO E274 1996121900845 19961219 00845 CE 1996 12 19 CA960619002 1 19960613 A 3260 MS243311 SWITCH MTSBSI MU2 MU2B36 5780412 CE GARRTT TPE331 TPE3316 01514 WP LH NLG GEAR DOOR SHORTED W K NONE J WARNING INDICATION LD LANDING 1 CA P20057C (CAN) ON GEAR EXTENSION, 3 GREEN LIGHTS SHOWED MOMENTARILY THEN WENT OUT AS THE GEAR DOORS CLOSED. FORWARD LEFT GEAR DOO R SWITCH FAILED AND SHORTED TO GROUND INTERNALLY. 1 H 7 2 3T 4 T RT A10SW E4WE 1996121900846 19961219 00846 1996 12 19 CA960619004 4 19960617 A 2210 R1 RESISTOR PIPER PA31 PA31 7103102 SO HARTZL HCC4Y HCC4YR2 GL AUTO PILOT BURNT W B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA 2371 FH271 (CAN) RESISTOR OVERHEATED, LIKELY DUE TO HIGH CURRENT LOAD OR SHORT CIRCUIT. CIRCUIT BREAKERS TRIPPED AUTOMATICALLY, BUT NOT BEFORE SIGNIFICANT OVERHEATING OF THE MOTOR DRIVE RESISTOR HAD TAKEN PLACE. 1 L 7 2 3O A20SO 5 C P52GL 1996121900847 19961219 00847 EU 1996 12 19 CA960619009 1 19960415 A 2430 371GG01Y02 MASTER ELECT BOX SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE DC SYS SHORT W E ENGINE SHUTDOWN A P FLAME/FIRE NO WARNING INDICATION LD LANDING 1 CA 835 (CAN) STARTER GENERATOR FIRE OCCURRED ON SHUTDOWN. REVERSE CURRENT RELAY REPLACED DUE TO NOT OPENING ON SHUTDOWN CAUSING GENERATOR TO MOTOR WHEN BATTERY VOLTAGE HIGHER THAN GENERATOR OUTPUT. GENERATOR LIGHT STILL FLICKERED AND RELAY CLICKS. CHANGED MEB. 1 G 7 1 3U 3 U H9EU E19EU 1996121900848 19961219 00848 SW 1996 12 19 CA960619010 1 19960430 A 2842 EA470B3588 TRANSMITTER BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL FUEL QTY FLOAT JAMS W D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CA CAE831824 (CAN) FUEL QUANTITY INDICATION WOULD STICK AT APPROXIMATELY 60-65 GALLONS WHEN TANK IS FULL. REMOVAL OF THE LOWER QUANTI TY TRANSMITTER REVEALED A BROKEN SOLDER JOINT ALLOWING THE FLOAT TO TWIST APPROXIMATELY 45 DEGREES WHICH ALLOWED FLOAT T O JAM WHILE CONTACTING AN INTERNAL FUEL CELL LINE. 1 G 7 1 3U 3 U H2SW E4CE 1996121900849 19961219 00849 SW 1996 12 19 CA960619011 1 19960430 A 7120 2060611043 MOUNT FITTING BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA CAE820733 (CAN) FITTING WAS SHEARED AT MOUNT LOCATION ALONG WITH EXCESSIVE WEAR ON STUD. 1 G 7 1 3U 3 U H2SW E4CE 1996121900850 19961219 00850 EU 1996 12 19 CA960619012 1 19960501 A 2913 704A33690004 BELT SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1B 6OO30 NE HYD DRIVE SEPARATING W K NONE O OTHER IN INSP/MAINT 1 CA 107 290 (CAN) BELT SEPARATING AT JOINT. TOTAL TIME SINCE NEW 107.4 HOURS. 1 G 7 1 3U 3 U H9EU E19EU 1996121900851 19961219 00851 EU 1996 12 19 CA960619013 1 19960502 A 6220 704A3364029A FREQ ADAPTER SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE M/R SPLIT W K NONE O OTHER IN INSP/MAINT 1 CA 878 (CAN) 3/4" SPLIT DEVELOPED ON AFT SIDE OF FREQUENCY ADAPTER IN ELASTOMERICS. 1 G 7 1 3U 3 U H9EU E19EU 1996121900852 19961219 00852 GL 1996 12 19 CA960619014 2 19960509 A 7321 23034702 FCU BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE FAILED W O OTHER M OVER TEMP IN INSP/MAINT 1 CA 807 802694 (CAN) UNABLE TO ADJUST FCU FOR HOT STARTS. ALSO NO NOTCH IN T.O.T. DURING START. FCU REPLACED AND RETURNED TO SERVICE. T IME THIS INSTALLATION, 89.2 HOURS. CYCLES THIS INSTALLATION, 130 HOURS. 1 G 7 1 3U 3 U H2SW E4CE 1996121900853 19961219 00853 EU 1996 12 19 CA960619015 1 19960513 A 2550 140277 CARGO SLING SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE RELEASE CABLE MISRIGGED W K NONE O OTHER CL CLIMB 1 CA 52 836 (CAN) UNCOMMANDED SLINGLOAD RELEASE. MANUAL EMERGENCY RELEASE WAS IMPROPERLY RIGGED. 1 G 7 1 3U 3 U H9EU E19EU 1996121900855 19961219 00855 EU 1996 12 19 CA960619017 1 19960529 A 2842 647510032 TRANSMTTER SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE FUEL QTY INACCURATE W K NONE O OTHER IN INSP/MAINT 1 CA 386B (CAN) DURING A COMPANY SPECIAL INSPECTION TO TEST THE FUEL QUANTITY INDICATING SYSTEM, THE LOW FUEL INDICATION WAS READI NG INACCURATELY. 1 G 7 1 3U 3 U NC H9EU E19EU 1996121900856 19961219 00856 GL 1996 12 19 CA960619018 2 19960602 A 7323 23007506 GOVERNOR BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE FAULTY W K NONE O OTHER IN INSP/MAINT 1 CA 597 CAE802078BA (CAN)GOVERNOR WOULD NOT ALLOW ENGINE TO REACH 100 PERCENT NR. WITH RIGGING IN LIMITS AND ENGINE WARM 100 PERCENT BARELY ATTAINABLE. 1 G 7 1 3U 3 U H2SW E4CE 1996121900857 19961219 00857 GL 1996 12 19 CA960619019 2 19960602 A 7250 6898734 TURBINE ASSEMBLY BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE CRACKED W K NONE O E OTHER VIBRATION/BUFFET IN INSP/MAINT 1 CA 11626 1858 CAE802078BA (CAN) SUSPECT THIS WAS A VIBRATION SOURCE THAT CAUSED COMPRESSOR ANTI-ICE PORT TO CRACK AND OUTER COMBUSTION CAN TO CRAC K 2". THERE WERE ONLY 88.3 HOURS SINCE FIRST AND SECOND STAGE WHEELS WERE REPLACED. 1 G 7 1 3U 3 U H2SW E4CE 1996121900858 19961219 00858 GL 1996 12 19 CA960619020 2 19960602 A 7230 6853337 COMPRESSOR ASSY BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ANTI-ICE PORT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 13326 1195 CAE802078BA (CAN) DURING TROUBLESHOOTING OF LACK OF POWER PROBLEM, A CRACKED FORWARD SUPPORT FOR ANTI-ICE PORT WAS FOUND. THERE WERE 276.7 HOURS SINCE REPAIRED FOR VIBRATION PROBLEM. UNIT REPLACED AND RETURNED TO SERVICE. 1 G 7 1 3U 3 U H2SW E4CE 1996121900859 19961219 00859 GL 1996 12 19 CA960619022 2 19960604 A 7323 23007506 GOVERNOR BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE FLUCTUATING W K NONE O OTHER CR CRUISE 1 CA 844 CAE823426 (CAN) RPM FLUCTUATING AT TOP END. 1 G 7 1 3U 3 U H2SW E4CE 1996121900860 19961219 00860 GL 1996 12 19 CA960619023 2 19960604 A 7250 6898734 TURBINE ASSY BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL 1ST STAGE TURBIN CRACKED W K NONE O OTHER CL CLIMB 1 CA 6471 1471 CAE823426 (CAN) ENGINE FAILED POWER CHECK. TROUBLESHOOTING DISCOVERED FIRST STAGE STATOR VANES CRACKED, 5 IN TOTAL. TURBINE ASSEMB LY REPLACED, AND AIRCRAFT RETURNED TO SERVICE. 1 G 7 1 3U 3 U H2SW E4CE 1996121900861 19961219 00861 SW 1996 12 19 CA960619024 1 19960610 A 2550 206072902005 RELEASE CABLE BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL SLING BINDING W K NONE O OTHER CR CRUISE 1 CA CAE860407 (CAN) UNCOMMANDED SLING LOAD RELEASE. INVESTIGATION FOUND THAT MANUAL RELEASE CABLE WOULD NOT RETURN TO FULLY EXTENDED P OSITION. SUSPECT CABLE FRAYED AND BINDING INSIDE SHEATH. 1 G 7 1 3U 3 U H2SW E1GL 1996121900862 19961219 00862 SW 1996 12 19 CA960619025 1 19960610 A 6220 206011100021 TRUNNION BEARING BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL MAIN ROTOR HUB EXCESS PLAY W K NONE O OTHER IN INSP/MAINT 1 CA CAE821010 (CAN) PITCH HORN TRUNNION BEARING REPLACED DUE TO AXIAL PLAY IN THE PITCH LINK BOLT BEARING. 1 G 7 1 3U 3 U H2SW E4CE 1996121900863 19961219 00863 WP 1996 12 19 CA960619026 1 19960613 A 6320 MS29561437 O-RING HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL M/R TRANSMISSION LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA CAE830896 (CAN) UPPER MAIN ROTOR TRANSMISSION O-RING LEAKING. AS TRANSMISSION WARMED TO OPERATING TEMPERATURE THE NEW PAINT MELTED AND UNSEATED O-RING. 1 G 7 1 3U 3 U H3WE E4CE 1996121900864 19961219 00864 WP 1996 12 19 CA960619027 1 19960613 A 6310 369A535041 CLUTCH HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL HOUSING BEARING LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA 1469 1141 CAE830896 (CAN) STEADY BEARING HOUSING SPINNING IN OVERRUNNING CLUTCH HOUSING DUE TO BEARING VIBRATING. BEARING WAS SPINNING UNDER SNAP RING CAUSING ALUMINUM BEARING HOUSING TO WEAR AND CONTAMINATE BEARING WITH METAL SHAVINGS. 1 G 7 1 3U 3 U H3WE E4CE 1996121900866 19961219 00866 GL 1996 12 19 CA960619030 2 19960602 A 7240 6870992 COMBUSTION CAN BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL AFT END CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA CAE802078BA (CAN) A CRACK OVER 2" WAS FOUND WHILE TROUBLESHOOTING FOR LOW POWER. CRACK WAS IN THE AREA OF THE FUEL NOZZLE/IGNITOR PO RTS. CRACK DID NOT OCCUR ON A WELD LINE. APPEARED TO BE CAUSED BY VIBRATION. 1 G 7 1 3U 3 U H2SW E4CE 1996121900867 19961219 00867 EU 1996 12 19 CA960619032 2 19960602 A 7270 DUCT CROSSOVER FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU NR 1 ENG LIBERATED W C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CA 27531 9279 (CAN) REJECTED TAKEOFF DUE TO INSUFFICIENT POWER FROM #1 ENGINE. INSPECTION FOUND THE OUTER CROSSOVER DUCT ATTACH POINT HAD PULLED OUT OF THE BYPASS DUCT. REPLACEMENT ENGINE INSTALLED. ENGINE GROUND RUN SERVICEABLE AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A20EU E2EU 1996121900868 19961219 00868 EU 1996 12 19 CA960619038 1 19960424 A 2140 A35A8974 VENT BLOWER JANITROL H52C98M BRAERO 748 HS7482A 4231001 EU HEATER FAILED W F D ACTIVATE FIRE EXT. RETURN TO BLOCK J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA 130 2674 (CAN) 1.3 MINUTES INTO TAXI #2 JANITROL WAS LIT, FIRE INDICATION ON JANITROL. JANITROL SHUT DOWN EXTINGUISHER ACTIVATED. FIRE CONTAINED IN THE JANITROL. THE VENT BLOWER HAD FAILED AND THE VENT BLOWER PRESSURE SWITCH DID NOT ACTIVATE THE SAF ETY CIRCUIT TO SHUT DOWN THE FUEL SOLENOID AND IGNITION UNIT. THE SAFETY CIRCUIT WAS OPERATING PROPERLY. 2 L 7 2 3T A24EU 1996121900869 19961219 00869 NM 1996 12 19 AWXA9600751 1 19961216 A 3350 CONNECTOR BOEING 737 73733A 1384673 NM CABIN DISCONNECTED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 165AW 23626 DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 17. RECONNECTED AND SECURED EMERGENCY LIGHT CO NNECTOR, OPS TEST NORMAL BOEING STANDARD. 2 L 7 2 4F RT A16WE 1996121900870 19961219 00870 NM 1996 12 19 AWXA9600752 1 19961217 A 3397 WIRE BOEING 757 757225 1384959 NM CABIN DISCONNECTED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 913AW 22207 DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT WIRES RIPPED OUT AT ROW 7 LEFT. REPAIRED WIRES AS REQUIRED. 2 L 7 2 4F RT A2NM 1996121900871 19961219 00871 WP 1996 12 19 CALA9601827 1 19961114 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1887 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68065 46590 INSPECTION FOUND CORROSION ON FLOOR SUPPORTS AT STA 1887, LBL 30 TO LBL 50 AND RBL 33 TO RBL 53. NEW SUPPORTS WERE FABR ICATED AND INSTALLED USING FASTENERS IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1996121900872 19961219 00872 WP 1996 12 19 CALA9601828 1 19961114 A 5320 CHANNEL DOUG DC10 DC1030 3023501 WP BS 1871-1887 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68065 46590 INSPECTION FOUND CORROSION ON CHANNEL AT STA 1871 TO 1887, RBL 33 TO LBL 35. A NEW PARTS WERE FABRICATED AND INSTALLED USING FASTENERS IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1996121900873 19961219 00873 WP 1996 12 19 CALA9601829 1 19961114 A 5320 CHANNEL DOUG DC10 DC1030 3023501 WP BS 1887-2007 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68065 46590 INSPECTION FOUND CORROSION ON CHANNEL AT STA 1887 TO 2007, LBL 25 AND LBL 60. NEW PARTS WERE FABRICATED AND INSTALLED U SING FASTENERS IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1996121900874 19961219 00874 WP 1996 12 19 CALA9601830 1 19961114 A 5320 CHANNEL DOUG DC10 DC1030 3023501 WP BS 1887-1942 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68065 46590 INSPECTION FOUND CORROSION ON CHANNEL AT STA 1887 TO 1942, RBL 25. A NEW PART WAS FABRICATED AND INSTALLED USING FASTEN ERS IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1996121900875 19961219 00875 WP 1996 12 19 CALA9601831 1 19961114 A 5320 CHANNEL DOUG DC10 DC1030 3023501 WP BS 1820-1887 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68065 46590 INSPECTION FOUND CORROSION ON CHANNEL AT STA 1820 TO 1887, LBL 30. A NEW PART WAS FABRICATED AND INSTALLED USING FASTEN ERS IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1996121900876 19961219 00876 WP 1996 12 19 CALA9601832 1 19961114 A 5320 CHANNEL DOUG DC10 DC1030 3023501 WP BS 1910-2007 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68065 46590 INSPECTION FOUND CORROSION ON CHANNEL AT STA 1910 TO 2007, LBL 22 AND AT STA 1910 TO 1920, RBL 22. NEW PARTS WERE FABRI CATED AND INSTALLED USING FASTENERS IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1996121900877 19961219 00877 NM 1996 12 19 CALA9601833 1 19961203 A 5320 FITTINGS BOEING 747 747238B 1384828 NM BS 2360 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND STRINGER END FITTINGS CORRODED AT BS 2360, S49L, S50L, S51L, S48R AND S51R. THE STRINGER END FITTINGS WERE REPLACED IAW SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900878 19961219 00878 NM 1996 12 19 CALA9601834 1 19961122 A 5320 SUPPORT BOEING 747 747238B 1384828 NM BS 765-880 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND TWO FLOOR SUPPORTS CORRODED AT BS 765 TO 880, LBL 36. THE CORROSION WAS REMOVED AND TREATED, THE FLOOR SUPPORTS WERE REPLACED IAW SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1996121900879 19961219 00879 NM 1996 12 19 CALA9601835 1 19961129 A 5320 SUPPORT BOEING 747 747238B 1384828 NM BS 1259 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND TWO FLOOR SUPPORTS CORRODED AT BS 1259, LBL 33 TO RBL 11. THE FLOOR SUPPORTS WERE REPLACED IAW SRM 51- 10-01. 2 L 7 4 4F A20WE 1996121900880 19961219 00880 NM 1996 12 19 CALA9601836 1 19961129 A 5320 SUPPORT PLATE BOEING 747 747238B 1384828 NM BS 1259 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND FLOOR SUPPORT PLATE CORRODED AT BS 1259, RBL 11 TO 33. THE FLOOR SUPPORT PLATE WAS REPLACED IAW SRM 51 -10-01. 2 L 7 4 4F A20WE 1996121900881 19961219 00881 NM 1996 12 19 CALA9601837 1 19961204 A 5320 SUPPORT BOEING 747 747238B 1384828 NM BS 1300 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND LATERAL FLOOR SUPPORT CORRODED AT BS 1300, RBL 11 TO 33. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-10- 01. 2 L 7 4 4F A20WE 1996121900882 19961219 00882 NM 1996 12 19 CALA9601838 1 19961204 A 5320 ANGLE BOEING 747 747238B 1384828 NM BS 480 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND ANGLE CORRODED AT BS 480, LBL 89. THE ANGLE WAS REPLACED IAW SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900883 19961219 00883 NM 1996 12 19 CALA9601839 1 19961204 A 5320 SUPPORT BOEING 747 747238B 1384828 NM BS 1280 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 1280, LBL 11 TO RBL 11. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900884 19961219 00884 NM 1996 12 19 CALA9601840 1 19961204 A 5320 SUPPORT BOEING 747 747238B 1384828 NM BS 1367 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 1367, RBL 11 TO RBL 33. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900885 19961219 00885 NM 1996 12 19 CALA9601841 1 19961205 A 5320 WEB BOEING 747 747238B 1384828 NM BS 980 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND A 3.5 INCH CRACK IN BEAM WEB AT BS 980, STRINGER 5R. THE WEB WAS REPLACED IAW SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900886 19961219 00886 NM 1996 12 19 CALA9601842 1 19961125 A 5330 SKIN BOEING 737 737130 1384435 NM BS 964 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16201 19018 INSPECTION FOUND FUSELAGE SKIN CORRODED BETWEEN RIVETS AT BS 964, STRINGER 20L. THE CORRODED AREA OF SKIN WAS CUT OUT, DOUBLERS AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 53-30-3. 2 L 7 2 4F A16WE 1996121900887 19961219 00887 NM 1996 12 19 CALA9601843 1 19961116 A 5330 SKIN BOEING 737 737130 1384435 NM BS 775 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16201 19018 INSPECTION FOUND A 1.75 INCH CRACK IN FUSELAGE SKIN AT BS 775, STRINGER 19R. THE CRACKED AREA WAS CUT OUT, A REPAIR DOU BLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. 2 L 7 2 4F A16WE 1996121900888 19961219 00888 NM 1996 12 19 CALA9601844 1 19961207 A 5330 SKIN BOEING 737 737130 1384435 NM BS 540 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16201 19018 INSPECTION FOUND FUSELAGE EXTERIOR SKIN LAP CORRODED AT STA 540, STRINGER 26L. REPAIR FILLER AND DOUBLER WERE FABRICATE D AND INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A16WE 1996121900889 19961219 00889 NM 1996 12 19 CALA9601845 1 19961209 A 5330 SKIN BOEING 737 737130 1384435 NM BS 253-312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16201 19018 INSPECTION FOUND NOSE WHEEL WELL CUTOUT AFT RT CORNER HAD CORRODED SKIN AND STRESSED FASTENERS. LOWER LOBE SKINS WERE C UT AND REMOVED FROM STA 253 TO 312. THE LOWER CHORD AT STA 294.5 WAS REMOVED AND REPLACED IAW BAC DRAWING 65-45808. A SPLICE WAS FABRICATED IAW SRM 53-30-3, SKINS AND SPLICE DOUBLERS WERE INSTALLED IAW SRM 51-10-2 AND 51-30-2. 2 L 7 2 4F A16WE 1996121900890 19961219 00890 NM 1996 12 19 CALA9601846 1 19961209 A 5320 BEAR STRAP BOEING 737 737130 1384435 NM E/E DOOR CUTOUT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16201 19018 INSPECTION FOUND E AND E DOOR CUTOUT BEAR STRAP CORRODED AT FORWARD SIDE OF CUTOUT. STRINGER 29 WAS REMOVED AND CORROSI ON WAS REMOVED FROM SKIN AND BEAR STRAP IAW SRM 51-10-6. A REPAIR SECTION WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-30-2. 2 L 7 2 4F A16WE 1996121900891 19961219 00891 WP 1996 12 19 9626429762 1 19961214 A 3222 STRUT DOUG DC9 DC941 302207N WP NLG REQD SERVICE A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 762NW 47395 AFTER TAKEOF, NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. GEAR EXTENDED NORMALLY BUT GEAR HANDLE WOULD NOT GO UP AGAIN. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. AIRCRAFT JACKED AND NOSE STRUT WAS RESERVI CED, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1996121900892 19961219 00892 EU 1996 12 19 9626433213 1 19961212 A 5610 NP1653111 WINDOW AIRBUS 320 A320211 3930320 EU FLIGHT DECK SHATTERED A NWAA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 01 313US 11043 153 CAPTAIN'S WINDSHIELD OUTER PANE SHATTERED AT FL350. RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE WINDOW, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996121900893 19961219 00893 EU 1996 12 19 9626443240 1 19961213 A 3350 321454 EPSU AIRBUS 320 A320212 EU CABIN FAULTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 340NW 23254 9626 372 DURING LINE MAINTENANCE CHECK, THE FOLLOWING MESSAGES ILLUMINATED ON THE FLIGHT ATTENDANT PANEL: INT LOADS EMER L, BATT EMER L, UNIT EMER L. ALSO, THE CEILING MOUNT AND LEFT OVERWING EXIT SIGNS WERE INOPERATIVE. REPLACED EPSU 11WL, OPERAT IONAL CHECK OK. 2 L 7 2 4F RT A28NM 1996121900894 19961219 00894 WP 1996 12 19 9626459921 1 19961213 A 3350 6011779 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN MALFUNCTIONED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 943N 47647 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996121900895 19961219 00895 WP 1996 12 19 9626469926 1 19961214 A 3350 60030451 POWER SUPPLY DOUG DC9 DC932 3022066 WP TAILCONE MALFUNCTIONED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 926NW 47425 DURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES AND POWER SUPPLY, O PERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996121900896 19961219 00896 WP 1996 12 19 9626479937 1 19961214 A 3350 BATTERY PACKS DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 908H 47517 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS AT ROWS 5, 7 AND 9 INOPERATIVE DURING TEST. REPLACE D BATTERY PACK AND POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996121900897 19961219 00897 WP 1996 12 19 9626489933 1 19961214 A 3260 LOCK SWITCH DOUG DC9 DC931 3022065 WP NOSE GEAR FROZEN A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 1334U 47280 DURING APPROACH, NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. RECYCLED GEAR AND NORMAL INDICA TIONS WERE ACHIEVED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NOSE GEAR LOCK SWITCH COVERED WITH ICE. CLEA NED LOCK SWITCH, OPERATIONAL CHECK NORMAL ON GROUND. 2 L 7 2 4F A6WE 1996121900898 19961219 00898 WP 1996 12 19 9626499969 1 19961215 A 3610 DUCT DOUG DC9 DC931 3022065 WP RIGHT PACK BLOWN A NWAA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 GL 01 9333 47246 TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT RETURNED TO ATL AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BLOWN DUCT BETWEEN RIGHT PACK VALVE AND FLOW CONTROL VALVE. REPLACED DUCT, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996121900899 19961219 00899 WP 1996 12 19 9626509957 1 19961213 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP COCKPIT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 915RW 47139 DURING PREFLIGHT CHECK, FOUND COCKPIT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. RESEATED FORWARD POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996121900900 19961219 00900 WP 1996 12 19 9626519937 1 19961214 A 3350 6011779 BATTERY PACKS DOUG DC9 DC931 3022065 WP RT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 908H 47517 DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT ENGINE NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACKS, OPE RATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996121900901 19961219 00901 NM 1996 12 19 9626522717 1 19961204 A 5320 CHORD BOEING 727 7272S7 138407Z NM BS 950- 970 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 721RC 22442 AFT CARGO DOOR LOWER FRAME LOWER 'T' CHORD STR 27R OUTBOARD FLANGE IS EXFOLIATED AT BS 950E TO 970. REPAIRED (P/N 65-56 129-10) PER EA 27-120674. 2 L 7 3 4F A3WE 1996121900902 19961219 00902 NM 1996 12 19 9626536635 1 19961217 A 7722 CONNECTOR BOEING 747 747227B 1384888 NM PWA JT9 JT9D7Q 52054 NE NR 4 EGT IND LOOSE A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 635US 21682 02452 DURING TAKEOFF, THE NR 4 ENGINE EGT INDICATOR WAS ERRATIC. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GAT E. MAINTENANCE FOUND INDICATOR CANNON PLUG LOOSE. CLEANED AND TIGHTENED THE CANNON PLUG, RUN-UP WAS NORMAL AND THE AIRC RAFT RETURNED TO SERVICE. 2 L 7 4 4F 4 F A20WE E3NE 1996121900903 19961219 00903 NE 1996 12 19 9626546718 2 19961211 A 7200 ENGINE BOEING 747 747251F 1384898 NM PWA JT9 JT9D7F 52054 NE NR 1 BIRD STRIKE A NWAA E A ENGINE SHUTDOWN UNSCHED LANDING C F.O.D. TO TAKEOFF 1 GL 01 618US 21122 89565 DURING TAKEOFF, THE NR 1 ENGINE N1 WENT TO ZERO WITH VIBRATION NOTED. THE ENGINE WAS SHUT DOWN, DUMPED 55.000 LBS OF FU EL AND THE AIRCRAFT RETURNED TO SFO WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTION REVEALED A BIRD STRIKE. PERFORMED ENGINE RUN-UP AT TAKEOFF POWER AND NO VIBRATION WAS EXPERIENCED. 2 L 7 4 4F 4 F A20WE E20EA 1996121900904 19961219 00904 NM 1996 12 19 9626552709 1 19961213 A 2121 215201 GASPER FAN BOEING 727 727225 1384077 NM E/E COMPT FAILED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 818EA 11568 11568 22555 DURING TAKEOFF ROTATION, A STRONG SMELL OF ELECTRICAL FUMES WAS EVIDENT. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT IN CIDENT. REPLACED GASPER FAN MOTOR, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996121900905 19961219 00905 NM 1996 12 19 9626562287 1 19961215 A 3150 SWITCH BOEING 727 727251 138408H NM T/O WARNING FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 287US 21375 RECEIVED TAKEOFF WARNING HORN DURING TAKEOFF ROLL. ABORTED TAKEOFF WITHOUT INCIDENT AND RETURNED TO THE GATE. REPLACED THE WARNING SWITCH S532. PERFORMED TAKEOFF WARNING OPERATIONAL CHECK, SYSTEM CHECKED OK. 2 L 7 3 4F A3WE 1996121900906 19961219 00906 NM 1996 12 19 9626575645 1 19961211 A 3350 POWER SUPPLY BOEING 727 727251 138408H NM CABIN INOPERATIVE A NWAA K NONE O OTHER UK UNKNOWN 1 GL 01 545US 26492 AFTER PERFORMING EMERGENCY LIGHT CHECK, DOOR 2L WOULD NOT EXTINGUISH. REPLACED POWER SUPPLY AT DOOR 2L, EMERGENCY LIGHT OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996121900907 19961219 00907 NM 1996 12 19 9626582291 1 19961215 A 3350 POWER SUPPLY BOEING 727 727251 138408H NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 291US 21379 DURING PREFLIGHT, FOUND OUTSIDE EMERGENCY LIGHTS FORWARD RIGHT OVERWING INOPERATIVE. REPLACED POWER SUPPLY M665 AND BAT TERY PACK PRECAUTIONARY, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1996121900908 19961219 00908 NE 1996 12 19 COMA9610397 3 19961216 A 6111 8173861 BEARING RFC11AA16A EMB 120 EMB120RT SO PWA 118 PW118 NE HAMSTD 14RF 14RF9 NE PROP BLADE WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 1968 1968 886346 120264 115571 910337 PROPELLER ASSEMBLY WAS REMOVED FOR EXCESSIVE VIBRATION. DURING DISASSEMBLY AND INSPECTION, IT WAS DETERMINED THAT THE V IBRATION WAS DUE TO THE UNEVEN WEAR OF THE BEARING INSERT. INSERT HAD DETERIORATED FROM .100\ TO .0650\ AT THE THINEST WALL TO .095\ AT THE THICKEST WALL WEARING IN AN OVAL FASHION. BLADE PIN AND BEARING WERE REMOVED FROM SERVICE AND REPL ACED WITH SERVICEABLE UNITS. 2 L 7 2 4T 4 T RT A31SO E20NE 6 C P11NE 1996121900911 19961219 00911 NE 1996 12 19 COMA9610400 3 19961216 A 6111 8173861 BEARING RFC11AA16A EMB 120 EMB120RT SO PWA 118 PW118 NE HAMSTD 14RF 14RF9 NE PROP BLADE WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 1968 1968 886349 120264 115571 910337 PROPELLER ASSEMBLY WAS REMOVED FOR EXCESSIVE VIBRATION. DURING DISASSEMBLY AND INSPECTION, IT WAS DETERMINED THAT THE V IBRATION WAS DUE TO THE UNEVEN WEAR OF THE BEARING INSERT. INSERT HAD DETERIORATED FROM .100\ TO .0255\ AT THE THINEST WALL TO .092\ AT THE THICKEST WALL WEARNING IN AN OVAL FASHION. BLADE PIN AND BEARING WERE REMOVED FROM SERVICE AND REP LACED WITH SERVICABLE UNITS. 2 L 7 2 4T 4 T RT A31SO E20NE 6 C P11NE 1996121900912 19961219 00912 SO 1996 12 19 COMA9610401 1 19961215 A 2910 12035694005 TUBING EMB 120 EMB120RT SO LT NACELLE CHAFED A COMA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 247CA 120225 HYDRAULIC FLUID LEAKING FROM LT ENGINE NACELLE. REPLACED DAMAGED SECTION OF GREEN SYSTEM HYDRAULIC PRESSURE TUBING BETW EEN NACELLE 13 AND 14. 2 L 7 2 4T RT A31SO 1996121900913 19961219 00913 SO 1996 12 19 COMA9610402 1 19961216 A 2130 PRESS SYST EMB 120 EMB120RT SO CABIN MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 462CA 120264 AIRCRAFT PRESSURIZATION SYSTEM FAILED. TRANSFERRED DISCREPANCY TO DEFERRED MAINTENANCE LIST AND AIRCRAFT CONTINUED SERV ICE. 2 L 7 2 4T RT A31SO 1996121900914 19961219 00914 SO 1996 12 19 COMA9610403 1 19961216 A 3010 44E202A SEPARATOR EMB 120 EMB120RT SO WING CENTER CRACKED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 156CA 120156 WING AND STABILIZER INBD DE-ICE BOOTS ARE INOP. REPLACED A CRACKED BLEED AIR WATER SEPARATOR. 2 L 7 2 4T RT A31SO 1996121900915 19961219 00915 EA 1996 12 19 COMA610226 1 19961216 A 3010 124112450 TEMP SENSOR CNDAIR CL600 CL6002B19 EA LT WING DEFECTIVE A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 917CA 7017 LEFT WING ANTI-ICE DUCT WARNING MESSAGE ON EICAS. REPLACED DEFECTIVE TEMP SENSOR PROBE AT LT WING LEADING EDGE. 2 L 7 2 4F RT A21EA 1996121900916 19961219 00916 EA 1996 12 19 COMA9660227 1 19961214 A 3620 356024310 SENSOR LOOP CNDAIR CL600 CL6002B19 EA LT ENGINE FALSE WARN A COMA K NONE N FALSE WARNING CR CRUISE 1 SO 01 948CA 7079 LT 14TH STAGE BLEED AIR WARNING MESSAGE DURING FLIGHT. REPLACED THE LT ENGINE PYLON BLEED LEAK SENSOR LOOP. 2 L 7 2 4F RT A21EA 1996121900917 19961219 00917 NE 1996 12 19 SWAA961383 2 19961208 A 7200 ENGINE BOEING 737 7375H4 138449D NM GE CFM56 CFM563B1 13802 NE NR 2 FAILED A SWAA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SW 07 513SW 24190 721715 NUMBER 2 ENGINE OIL QUANTITY DROPPED. CREW PERFORMED ENGINE SHUTDOWN CHECKLIST. AIRCRAFT DIVERTED TO ONT AND MADE AN U NEVENTFUL LANDING. REPLACED NUMBER 2 ENGINE PER BOEING M/M. 2 L 7 2 4F 4 F RT A16WE E2GL 1996121900918 19961219 00918 1996 12 19 SWAA961384 4 19961209 A 3454 NAV CONTL PNL BOEING 737 7373H4 1384600 NM NR 1 INOPERATIVE A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 392SW 27379 NUMBER 1 VHF NAV SYSTEM BECAME INOPERATIVE, SWITCHING TO AUX, NO HELP. AIRCRAFT DIVERTED TO PHX AND MADE AN UNEVENTFUL LANDING. REPLACED BOTH NAV CONTROL PANELS AND NR 1 NAV RECEIVER PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996121900919 19961219 00919 NM 1996 12 19 SWAA961385 1 19961211 A 2130 711025 CONTROL PANEL BOEING 737 7372T4 1384492 NM CABIN MALFUNCTIONED A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 130SW 22699 CLIMBING THROUGH 25,000, CABIN ALTITUDE ALERT SOUNDED. ALL SWITCHES WERE IN NORM POSITIONS, CABIN PRESSURE READ 9,500 F T. AIRCRAFT RETURNED TO MDW AND MADE AN UNEVENTFUL LANDING. REPLACED CABIN PRESSURE CONTROL PANEL PER BOEING M/M. 2 L 7 2 4F A16WE 1996121900920 19961219 00920 NM 1996 12 19 96FDEA01703 1 19961218 A 3010 DUCT BOEING 727 727247 138408F NM NR 1 ENGINE LOOSE A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION UK UNKNOWN 1 SO 25 236FE 21330 ENGINE NR 1 STRUT OVERHEAT. 1ST LIGHT WENT OUT BEFORE CHECKLIST WAS RUN. 2ND LIGHT WENT OUT WHEN ENGINE NR 1 WING ANTI -ICE SWITCH TURNED OFF. AIRCRAFT DE-ICED AT IND ON THE GROUND PRIOR TO FLIGHT. RAN NR 1 ENGINE FOUND LEAKS IN STRUT AR EA. TIGHTENED FLANGES ON DUCT, OPERATIONAL CHECKED GOOD ON GROUND. 2 L 7 3 4F A3WE 1996121900921 19961219 00921 NM 1996 12 19 SCNA96438 1 19961211 A 2611 CONNECTOR BOEING 727 7272A1 138407F NM LAV SMOKE DET LOOSE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 286SC 21601 ALL THREE LAV SMOKE DETECTORS FAILED TO TEST. RECONNECTED CANNON PLUGS IN ACCORDANCE WITH 20-60-06, ALL OPS CHECKED GO OD. 2 L 7 3 4F A3WE 1996121900922 19961219 00922 WP 1996 12 19 SCNA96439 1 19961213 A 3350 EMBS1392 POWER SUPPLY DOUG DC10 DC1010 3022110 WP CABIN INOPERATIVE A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 46645 AFT EMERGENCY POWER SUPPLY FAILED SELF TEST. REMOVED AND REPLACED AFT EMERGENCY EXIT POWER SUPPLY AND OPS CHECKED GOOD. 2 L 7 3 4F A22WE 1996121900923 19961219 00923 WP 1996 12 19 SCNA96440 1 19961213 A 3350 EMBS1392 POWER SUPPLY DOUG DC10 DC1010 3022110 WP CABIN INOPERATIVE A SCNA K NONE L NO TEST NR NOT REPORTED 1 GL 15 572SC 46977 EMERGENCY LIGHTS CHARGE AND STANDBY CIRCUIT BREAKER POPPED IN FLIGHT. REMOVED AND REPLACED LEFT OVERWING BATTERY CHARGE R POWER SUPPLY AND OPS CHECKED GOOD IN ACCORDANCE WITH MM 33-50-11. 2 L 7 3 4F A22WE 1996121900924 19961219 00924 NM 1996 12 19 P5CA9601032 1 19960812 A 5320 HI-LOCK RIVET BOEING 747 747121 1384871 NM FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON HEAD OF HI-LOCK AND OPEN HOLE AT STA 1700 BETWEEN STRINGER 3 TO 5. CORROSION RIVETS TAKEN OUT AND OPEN HOL E AREA INSTALLED NEW HI-LOCKS PER SRM 51-30-02 OBTAINED FROM STA STOCK. 2 L 7 4 4F A20WE 1996121900925 19961219 00925 NM 1996 12 19 P5CA9601033 1 19960812 A 5720 RIVETS BOEING 747 747121 1384871 NM WS 480 SHEARED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 SHEARED RIVETS ON UPPER WING SKIN RT AT STA 480 IN FRONT SPAR AREA. INSTALLED NEW RIVETS .1875 PER SRM 51-30-02. 2 L 7 4 4F A20WE 1996121900926 19961219 00926 NM 1996 12 19 P5CA9601034 1 19960812 A 5720 RIVETS BOEING 747 747121 1384871 NM WS 565 SHEARED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 SHEARED RIVETS ON UPPER WING SKIN RT AT STA 565 FRONT SPAR. NEW RIVETS PER SRM 51-30-02. 2 L 7 4 4F A20WE 1996121900927 19961219 00927 NM 1996 12 19 P5CA9601035 1 19960812 A 5720 RIVETS BOEING 747 747121 1384871 NM WS 600 SHEARED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 SHEARED RIVETS ON UPPER WING SKIN RT AT STA 600 IN FRONT SPAR AREA. INSTALLED NEW RIVETS OBTAINED FROM STA STOCK BN 916 62-25. 2 L 7 4 4F A20WE 1996121900928 19961219 00928 NM 1996 12 19 P5CA9601036 1 19960812 A 5720 RIVETS BOEING 747 747121 1384871 NM WS 990 SHEARED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 SHEARED RIVETS ON UPPER WING SKIN RT AT STA WS 990 IN FRONT SPAR AREA. INSTALLED NEW RIVET .1875 PER SRM 51-30-02. 2 L 7 4 4F A20WE 1996121900929 19961219 00929 NM 1996 12 19 P5CA9601037 1 19960805 A 5210 DOOR BOEING 747 747121 1384871 NM NR 2R DOOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 NR 2R ENTRY DOOR SURFACE CORROSION ON DOOR STOPS. CORROSION REMOVED AND TREATED PER MM 51-21-03. 2 L 7 4 4F A20WE 1996121900930 19961219 00930 NM 1996 12 19 P5CA9601038 1 19960805 A 5210 DOOR BOEING 747 747121 1384871 NM NR 2L DOOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 NR 2L ENTRY DOOR 2 CORROSION SCREWS ON OUTER DOOR HANDLE. CORROSION REMOVED AND TREATED PER MM 51-21-03. 2 L 7 4 4F A20WE 1996121900931 19961219 00931 NM 1996 12 19 P5CA9601039 1 19960812 A 5330 SKIN BOEING 747 747121 1384871 NM BS 1420-1400 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON INTERNAL SKIN BETWEEN STA 1420 TO 1400 AND BETWEEN STRINGER 1 TO 4 LT. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900932 19961219 00932 NM 1996 12 19 P5CA9601040 1 19960812 A 5311 FRAME BOEING 747 747121 1384871 NM BS 1241 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON FRAME AT STA 1241 NEAR STRINGER 1 LT. CORROSION BLENDED OUT, SURFACE SMOOTHED PER SRM 51-10-01 AND 51-10-0 2. 2 L 7 4 4F A20WE 1996121900933 19961219 00933 NM 1996 12 19 P5CA9601041 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1260-1320 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STRINGER 1 BETWEEN STA 1260 TO 1320 LT. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900934 19961219 00934 NM 1996 12 19 P5CA9601042 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1440 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STRINGER 10 LT AND ON FRAME STA 1440. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900935 19961219 00935 NM 1996 12 19 P5CA9601043 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1420-1440 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STRINGER 7 LT AT STA 1420 TO 1440. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900936 19961219 00936 NM 1996 12 19 P5CA9601044 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1380-1400 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STRINGER 8, 9, 10 LT BETWEEN STA 1380 TO 1400. CORROSION BLENDED OUT SURFACE, SMOOTHED PER SRM 51-10-01 AN D 51-10-02. 2 L 7 4 4F A20WE 1996121900937 19961219 00937 NM 1996 12 19 P5CA9601045 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1420 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STRINGER 5 AT STA 1420. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900938 19961219 00938 NM 1996 12 19 P5CA9601046 1 19960812 A 5330 SKIN BOEING 747 747121 1384871 NM BS 2120-1960 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON THE SKIN UNDER SEALER AT STRINGER 12 LAP JOINT AREA BETWEEN STA 2120 TO 1960 RT SIDE. CORROSION REMOVED AN D TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900939 19961219 00939 NM 1996 12 19 P5CA9601047 1 19960812 A 5311 FRAME BOEING 747 747121 1384871 NM BS 1500 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON FRAME AT STA 1500 NEAR STRINGER 3 LT. CORROSION REMOVED AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900940 19961219 00940 NM 1996 12 19 P5CA9601048 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1520 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION TIE CLIP AT STA 1520 NEAR STRINGER 2 RT. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900941 19961219 00941 NM 1996 12 19 P5CA9601049 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1580-1600 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION STRINGER 2 RT BETWEEN STA 1580 TO 1600. CORROSION BLENDED OUT SURFACE, SMOOTHED PER SRM 51-10-01 AND 51-10-0 2. 2 L 7 4 4F A20WE 1996121900942 19961219 00942 NM 1996 12 19 P5CA9601050 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1580-1600 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION STRINGER 7 TO 9 BETWEEN STA 1580 TO 1600 LT. CORROSION REMOVED AND AREA TREATED PER 51-10-01. 2 L 7 4 4F A20WE 1996121900943 19961219 00943 NM 1996 12 19 P5CA9601051 1 19960812 A 5311 FRAME BOEING 747 747121 1384871 NM BS 1600 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION FRAME LWR CHORD AT STA 1600 ABOVE STR 11, 12. CORROSION BLENDED OUT PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1996121900944 19961219 00944 NM 1996 12 19 P5CA9601052 1 19960812 A 5314 KEEL BEEM BOEING 747 747121 1384871 NM BS 1000-1241 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION SHEET METAL COVER AND BRACKET SUPPORTS AROUND TO KEEL BEAM CUTOUTS AT CENTER LWR FUS BETWEEN STA 1000 TO 1241. CORROSION REMOVED, AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900945 19961219 00945 NM 1996 12 19 P5CA9601053 1 19960812 A 5320 INTERCOSTAL BOEING 747 747121 1384871 NM BS 1920-1940 DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 DENT ON INTERCOSTAL AT STRINGER 35 BETWEEN STA 1920 TO 1940 LT SIDE. STRAIGHTEN SRM 51-40-01 AND TREATED PER SRM 51-10- 01. VISUAL CHECK FOUND OK. 2 L 7 4 4F A20WE 1996121900946 19961219 00946 NM 1996 12 19 P5CA9601054 1 19960812 A 5343 BEAM BOEING 747 747121 1384871 NM RT MLG CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 RIGHT BODY LANDING GEAR WHEEL WELL AFTER REMOVAL OF SPLICE PLATES CORROSION FOUND ON L/G BEAM LWR CHORD HORIZ FLANGE. A LSO, SCRATCHES EXIST ON FLANGE AFT EDGE. CORROSION AND DAMAGE REMOVED PER SB53-2310. 2 L 7 4 4F A20WE 1996121900947 19961219 00947 NM 1996 12 19 P5CA9601055 1 19960812 A 5343 BEAM BOEING 747 747121 1384871 NM LT MLG CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 LEFT BODY LANDING GEAR WHEEL WELL AFTER REMOVAL OF SPLICE PLATES CORROSION FOUND IN LANDING GEAR BEAM LOWER CHORD HORIZO NTAL FLANGE. ALSO, ON VERTICAL FLANGE INBOARD AFT SIDE. CORROSION REMOVED SB53-2310. 2 L 7 4 4F A20WE 1996121900948 19961219 00948 NM 1996 12 19 P5CA9601056 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 460 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FOUND 2 CRACKS IN AFT ROW STA 460 BETWEEN STRINGER 14E AND 15 RT. REPAIRED IAW SB53-2289. 2 L 7 4 4F A20WE 1996121900949 19961219 00949 NM 1996 12 19 P5CA9601057 1 19960812 A 5320 CHORD BOEING 747 747121 1384871 NM BS 1580 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CRACK ON UPPER CHORD STA 1580 RT SIDE ABOVE STRINGER 39 TO 40. REPAIRED PER SRM 53-10-04. 2 L 7 4 4F A20WE 1996121900950 19961219 00950 NM 1996 12 19 P5CA9601058 1 19960812 A 5320 WEB BOEING 747 747121 1384871 NM BS 1880 TORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 TEAR ON THE WEB AT STA 1880 RT SIDE UNDER UPPER CHORD ABOVE STRINGER 48 TO 49. AREA REPAIRED PER SRM 51-40-02. 2 L 7 4 4F A20WE 1996121900951 19961219 00951 NM 1996 12 19 P5CA9601059 1 19960812 A 5330 SKIN BOEING 747 747121 1384871 NM BS 1372-1740 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 SURFACE CORROSION ON THE SKIN BETWEEN STA 1372 TO 1740 AND BETWEEN STRINGER 12 TO 18 LT SIDE. CORROSION REMOVED AND ARE A TREATED PER SRM 51-10-01, FOUND WITHIN THE LIMITS PER SRM 53-30-01. 2 L 7 4 4F A20WE 1996121900952 19961219 00952 NM 1996 12 19 P5CA9601060 1 19960812 A 5320 CHORD BOEING 747 747121 1384871 NM BS 1800 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CRACK WITH STOP HOLES ON UPPER CHORD STA 1800 LT SIDE ABOVE STRINGER 42. REPAIRED PER SRM 53-10-04 AND 51-30-02. 2 L 7 4 4F A20WE 1996121900953 19961219 00953 NM 1996 12 19 P5CA9601061 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1900 CRACK A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CRACK BEYOND EXISTING REPAIR ON STA 1900 LT SIDE ABOVE STRINGER 41 TO 42. REPAIRED PER SRM 53-10-04. 2 L 7 4 4F A20WE 1996121900954 19961219 00954 NM 1996 12 19 P5CA9601062 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1640 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STRINGER 4 RT AT STA 1640. CORROSION REMOVED AND TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900955 19961219 00955 NM 1996 12 19 P5CA9601063 1 19960812 A 5320 FAIRING BOEING 747 747121 1384871 NM BS 1120-1140 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION FAIRING SUPPORT LWR FUS BETWEEN AREA RBL TO LBL 58 AND BETWEEN STA 1120 TO 1140. CORROSION REMOVED AND AREA T REATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900956 19961219 00956 NM 1996 12 19 P5CA9601064 1 19960812 A 5320 SUPPORT BOEING 747 747121 1384871 NM BS 1160 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION FAIRING SUPPORT LWR FUS AT RBL 62 AREA STA 1160. CORROSION BLENDED OUT SURFACE, SMOOTH PER SRM 51-10-01 AND 5 1-40-03. 2 L 7 4 4F A20WE 1996121900957 19961219 00957 NM 1996 12 19 P5CA9601065 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1400-1420 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION STRINGER 5 LT BETWEEN STA 1400 TO 1420. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900958 19961219 00958 NM 1996 12 19 P5CA9601066 1 19960812 A 5210 DOME NUTS BOEING 747 747121 1384871 NM NR 3 PAX DOOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 NR 3L MAIN ENTRY DOOR CORROSION ON DOME NUTS AT UPPER FRAME INNER SURFACE. CORROSION REMOVED AND AREA TREATED PER SRM 5 1-10-01 AND 51-30-02. 2 L 7 4 4F A20WE 1996121900959 19961219 00959 NM 1996 12 19 P5CA9601067 1 19960812 A 5321 FLOOR BOEING 747 747121 1384871 NM BS 780 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CRACK ON FLOOR SHEET METAL AT STRINGER 26 AREA NEAR STA 780 RT SIDE. FAB NEW PART PER SRM 53-10-21 AND 51-30-02. 2 L 7 4 4F A20WE 1996121900960 19961219 00960 NM 1996 12 19 P5CA9601068 1 19960812 A 5330 SKIN BOEING 747 747121 1384871 NM BS 780-1000 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 SURFACE CORROSION ON THE SKIN BETWEEN STA 780 TO 1000 RT SIDE AND BETWEEN STRINGER 12 TO 18. CORROSION REMOVED AND TREA TED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900961 19961219 00961 NM 1996 12 19 P5CA9601069 1 19960812 A 5315 FLOORBEAM BOEING 747 747121 1384871 NM BS 2360 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION INBOARD CHORD STA 2360 BETWEEN STRINGER 45 RT TO 45 LT. CORROSION REMOVED AND TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900962 19961219 00962 NM 1996 12 19 P5CA9601070 1 19960812 A 5320 SUPPORT BOEING 747 747121 1384871 NM BS 1480 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CRACKS ON FAIRING SUPPORT ANGLES LWR FUS LT SIDE STA 1480. REPAIRED PER SRM 53-50-04. 2 L 7 4 4F A20WE 1996121900963 19961219 00963 NM 1996 12 19 P5CA9601071 1 19960812 A 5320 SUPPORT BOEING 747 747121 1384871 NM BS 1180 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION FAIRING SUPPORT LWR FUS STA 1180 BETWEEN AREA RBL TO LBL 58. REPAIRED PER SRM 53-50-04. 2 L 7 4 4F A20WE 1996121900964 19961219 00964 NM 1996 12 19 P5CA9601072 1 19960812 A 5320 ANGLE BOEING 747 747121 1384871 NM BS 2280-2360 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION AND LOOSE CLIPS ON FLOOR ANGLE BETWEEN STA 2280 TO 2360 LT SIDE. CLEANED CORROSION AND TREATED PER SRM 51-10- 01 AND 51-30-02. 2 L 7 4 4F A20WE 1996121900965 19961219 00965 NM 1996 12 19 P5CA9601073 1 19960812 A 5320 WINDOW FRAME BOEING 747 747121 1384871 NM BS 1940-1960 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION WINDOW FRAME UNDER SEALANT AT STRINGER 22 BETWEEN STA 1940 TO 1960 RT. CORROSION REMOVED AND TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900966 19961219 00966 NM 1996 12 19 P5CA9601074 1 19960812 A 5330 SKIN BOEING 747 747121 1384871 NM BS 1820-1840 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON THE SKIN BETWEEN STA 1820 TO 1840 RT SIDE AND BETWEEN STRINGER 45 TO 46. CORROSION REMOVED AND AREA TREATE D PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900967 19961219 00967 NM 1996 12 19 P5CA9601075 1 19960812 A 2550 RESTRAINT BOEING 747 747121 1384871 NM CARGO COMPT DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FWD CARGO COMPARTMENT FIXED RESTRAINT DAMAGED AT STA 780R. RESTRAINT REPLACED AS PER MM 25-50-00. 2 L 7 4 4F A20WE 1996121900968 19961219 00968 NM 1996 12 19 P5CA9601076 1 19960812 A 5751 STRIP BOEING 747 747121 1384871 NM LT AILERON TORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 LEFT OUTBOARD AILERON UPPER OUTBOARD STRIP IS TORN. TORN STRIP REPLACED PER MM 57-51-00. 2 L 7 4 4F A20WE 1996121900969 19961219 00969 NM 1996 12 19 P5CA9601077 1 19960812 A 2150 WATER DRAIN BOEING 747 747121 1384871 NM BS 1100 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 AIR COND BAY RT WATER DRAIN TUBE IS CRACKED ON TWO LOCATION AT B STA 1100R APPROX WATER DRAIN TUBE. REPLACED PER MM 21- 10-00. 2 L 7 4 4F A20WE 1996121900970 19961219 00970 NM 1996 12 19 P5CA9601078 1 19960812 A 5320 SUPPORT BOEING 747 747121 1384871 NM FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON BRACKETS ABOVE FAIRING SUPPORT LWR FUS LT SIDE AT AREA LBL 20 TO LBL 60. CORROSION REMOVED AND AREA TREATE D PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900971 19961219 00971 NM 1996 12 19 P5CA9601079 1 19960812 A 5320 SUPPORT BOEING 747 747121 1384871 NM BS 1540 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION AND BENT ON FAIRING SUPPORT AT LWR FUS STA 1540 BETWEEN AREA LBL 1000 TO RBL 100. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900972 19961219 00972 NM 1996 12 19 P5CA9601080 1 19960812 A 5330 SKIN BOEING 747 747121 1384871 NM BS 1520-1540 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 SURFACE CORROSION ON THE SKIN AND ON ANCHOR NUT BETWEEN STA 1520 TO 1540 LT SIDE AND BETWEEN STRINGER 24 TO 25. CORROSI ON REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900973 19961219 00973 NM 1996 12 19 P5CA9601081 1 19960812 A 5330 SKIN BOEING 747 747121 1384871 NM BS 580-600 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON THE SKIN UNDER SEALING AT STRINGER 23 BETWEEN STA 580 TO 600. CORROSION REMOVED AND AREA TREATED PER SRM 5 1-10-01. 2 L 7 4 4F A20WE 1996121900974 19961219 00974 NM 1996 12 19 P5CA9601082 1 19960812 A 5330 SKIN BOEING 747 747121 1384871 NM BS 2240-2280 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON REINFORCEMENT DOUBLER ON FUS SKIN ABOVE AND LWR PASSENGER DOOR 5 AT STA 2240 AND 2280. CORROSION REMOVED P ER SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900975 19961219 00975 NM 1996 12 19 P5CA9601083 1 19960812 A 5330 SKIN BOEING 747 747121 1384871 NM BS 2300-2320 DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 DENT ON FUS SKIN LT SIDE BETWEEN STA 2300 TO 2320 AND BETWEEN STRINGER 15 TO 16. REWORKED PER SRM 51-40-01 AND 53-30-01 . 2 L 7 4 4F A20WE 1996121900976 19961219 00976 NM 1996 12 19 P5CA9601084 1 19960812 A 5210 SKIN BOEING 747 747121 1384871 NM PAX DOOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION AND HOLE ON LWR SIDE OF PASSENGER DOOR LT BETWEEN STA 2260 TO 2280. HOLE RIVETED WITH NAS 78585-7 RIVET BN.08 729-96 PER SRM 51-30-02. REMOVED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900977 19961219 00977 NM 1996 12 19 P5CA9601085 1 19960812 A 5330 SKIN BOEING 747 747121 1384871 NM BS 260 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON NOSE SKIN UNDER FWD COCKPIT WINDOW AT STA 260 AREA. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900978 19961219 00978 NM 1996 12 19 P5CA9601086 1 19960812 A 5320 BRACKET BOEING 747 747121 1384871 NM BS 1940 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CRACKED AND CORROSION, MISSING RIVETS ON BRACKET AT STA 1940 RT SIDE ABOVE STRINGER 40 TO 43. AREA REPAIRED PER SRM 51- 40-02 AND 51-40-03. 2 L 7 4 4F A20WE 1996121900979 19961219 00979 NM 1996 12 19 P5CA9601087 1 19960812 A 5320 CHORD BOEING 747 747121 1384871 NM BS 1920 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON PROFILE TEE ABOVE UPPER CHORD STA 1920. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900980 19961219 00980 NM 1996 12 19 P5CA9601088 1 19960812 A 5330 SKIN BOEING 747 747121 1384871 NM BS 800 DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 HIT ON PANEL NEAR DOOR 2 UNDER COVER HINGE LWR BETWEEN STA 800 TO 820 LT. SMOOTHED AREA AND TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900981 19961219 00981 NM 1996 12 19 P5CA9601089 1 19960812 A 5330 SKIN BOEING 747 747121 1384871 NM BS 140-160 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON HEAD FASTENERS AT FUS SKIN ABOVE AND UNDER PASSENGER WINDOW LT BETWEEN STA 140 TO 160 AND RT SIDE. CORROSI ON REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900982 19961219 00982 NM 1996 12 19 P5CA9601090 1 19960812 A 5330 SKIN BOEING 747 747121 1384871 NM BS 1960 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 SURFACE CORROSION ON FUS SKIN RT SIDE STA 1960 AT STRINGER 12 AREA. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01 . 2 L 7 4 4F A20WE 1996121900983 19961219 00983 NM 1996 12 19 P5CA9601091 1 19960812 A 5330 SKIN BOEING 747 747121 1384871 NM BS 2040-2360 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 SURFACE CORROSION ON FUS SKIN RT SIDE BETWEEN STA 2040 TO 2360 AT STRINGER 12 AREA. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900984 19961219 00984 NM 1996 12 19 P5CA9601092 1 19960812 A 5320 CLIP BOEING 747 747121 1384871 NM BS 1820 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CRACK ON TIE CLIP AT STA 1820 IN STRINGER 4 LT AREA. INST NEW CLIP (P/N 65B38600-160) AND RIVETED OBTAINED FROM STA STO CK PER SRM 51-30-02. 2 L 7 4 4F A20WE 1996121900985 19961219 00985 NM 1996 12 19 P5CA9601093 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1080 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STRINGER 1 RT AT STA 1080. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900986 19961219 00986 NM 1996 12 19 P5CA9601094 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1080-1100 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STRINGER 7, 9 BETWEEN STA 1080 TO 1100. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900987 19961219 00987 NM 1996 12 19 P5CA9601095 1 19960812 A 5311 FRAME BOEING 747 747121 1384871 NM BS 1110 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON FRAME AT STA 1110 STRINGER 1 LT. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900988 19961219 00988 NM 1996 12 19 P5CA9601096 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1080-1100 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STRINGER 1, 4, 5, 6 LT BETWEEN STA 1080 TO 1100. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900989 19961219 00989 NM 1996 12 19 P5CA9601097 1 19960812 A 5330 SKIN BOEING 747 747121 1384871 NM BS 1372-1394 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON THE SKIN UNDER SEALING AT WINDOW FRAME AREA AT STRINGER 21 AND SHEARED RIVET ON ANCHOR NUT BETWEEN STRINGER 24 TO 25 AND BETW STA 1372 TO 1394 RT SIDE. CORROSION REMOVED AREA TREATED PER SRM 51-10-01 AND 51-30-02. 2 L 7 4 4F A20WE 1996121900990 19961219 00990 NM 1996 12 19 P5CA9601098 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1394-1416 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STRINGER 22 UNDER SEALING AT WINDOW FRAME AREA BETWEEN STA 1394 TO 1416 RT SIDE. CORROSION REMOVED AND ARE A TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900991 19961219 00991 NM 1996 12 19 P5CA9601099 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1660-1680 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STRINGER 15 AND 16 BETWEEN STA 1660 TO 1680 RT SIDE. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900992 19961219 00992 NM 1996 12 19 P5CA9601100 1 19960812 A 5330 SKIN BOEING 747 747121 1384871 NM BS 1740-1496 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 SURFACE CORROSION ON THE SKIN BETWEEN STA 1740 TO 1496 AND BETWEEN STRINGER 19 TO 12. CORROSION REMOVED AND AREA TREATE D PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900993 19961219 00993 NM 1996 12 19 P5CA9601101 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1740 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STRINGER 13 NEAR STA 1740 RT SIDE. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900994 19961219 00994 NM 1996 12 19 P5CA9601102 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1800-1820 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STRINGER 20 ABOVE PASSENGER WINDOW BETWEEN STA 1800 TO 1820 RT SIDE. CORROSION REMOVED AND AREA TREATED PE R SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900995 19961219 00995 NM 1996 12 19 P5CA9601103 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1880 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON DOUBLER AT STRINGER 19 AREA AND BENT ON BRACKET NEAR STRINGER 16 AT STA 1880 RT SIDE. CORROSION REMOVED AN D AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900996 19961219 00996 NM 1996 12 19 P5CA9601104 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1920-1940 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STRINGER 22 AT FRAME WINDOW AREA BETWEEN STA 1920 TO 1940. CORROSION REMOVED AND AREA TREATED PER SRM 51-1 0-01. 2 L 7 4 4F A20WE 1996121900997 19961219 00997 NM 1996 12 19 P5CA9601105 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1960 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STRINGER 12 NEAR STA 1960 RT SIDE. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900998 19961219 00998 NM 1996 12 19 P5CA9601106 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1960 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON REINFORCEMENT DBL AT STA 1960 RT SIDE BETW STRINGER 17 TO 18 INCLUDING CORRODED ON STRINGER 17. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1996121900999 19961219 00999 SO 1996 12 19 SRAA961209 1 19961216 A 5730 SKIN LKHEED 382 382G 526414U SO BS 36 CRACKED A SRAA K NONE O OTHER IN INSP/MAINT 1 GL 23 909SJ 4763 ON WALKAROUND INSPECTION, FOUND RIGHT WING LEADING EDGE HAS A 5 INCH CRACK IN LOWER SURFACE AT O/B WING STATION 36. REP AIRED LEADING EDGE PER SRM FIG 51-140-12. 2 H 7 4 4T A1SO 1996122300001 19961223 00001 NM 1996 12 23 TWRA96356 1 19961109 A 3350 900835A BATTERY PACK BOEING 747 747212B 1384886 NM CABIN DISCHARGED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 616FF 21939 DURING DAILY CHECK, RIGHT SIDE OVERWING EVAC LIGHTS, FORWARD ARE BLINKING. REPLACED BATTERY PACK, BATTERY CHARGER AND F USE. OPS CHECKED NORMAL AS PER MM 33-51-00 PAGE 501. (M) 2 L 7 4 4F A20WE 1996122300002 19961223 00002 NM 1996 12 23 EISA96284 1 19961101 A 5320 CLIP BOEING 727 727223 1384074 NM BS 560-1050 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 314NE 19495 DURING A SCHEDULED D-CHECK, FOUND STRINGER TIE CLIPS AT VARIOUS STATIONS CRACKED FROM BS 560 TO 1050. REPLACED CLIPS PE R SRM 51-10-1 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1996122300003 19961223 00003 SW 1996 12 23 MALA965251 1 19961108 A 3260 1EN516 SWITCH SWRNGN SA227 SA227AC 8780603 SW NLG DIRTY A MALA O OTHER N FALSE WARNING AP APPROACH 1 GL 15 422MA AC635 FLT 3342 - ON APPROACH TO DTW, THE NOSE GEAR DOWN AND LOCKED LIGHT FAILED TO ILLUMINATE AFTER GEAR EXTENSION. THE CREW CYCLED THE GEAR UNTIL THE LIGHT ILLUMINATED. MAINTENANCE CLEANED AND LUBRICATED THE DOWNLOCK SWITCHES. ALL CHECKS SATI SFACTORY. (M) 2 L 7 2 4T RT A8SW 1996122600012 19961226 00012 SO 1996 12 26 96ZZZX6146 2 19961204 A 8500 ENGINE PIPER PA34 PA34220T 7103420 SO CONT O360 TSIO360KB 17025 SO LT ENG MAKING METAL A MOGA K NONE O OTHER IN INSP/MAINT 1 GL 25 84643 972 348233033 268067R DURING 100 HR INSPECTION, THE LEFT ENGINE OIL FILTER WAS FOUND TO BE CONTAMINATED WITH METAL. REMOVAL OF PROPELLER REVE ALED METAL CONTAMINATION IN CRANKSHAFT. ENGINE WAS REMOVED FOR OVERHAUL. FURTHER DETAILS WILL BE PROVIDED UPON RECEIP T OF TEAR DOWN REPORT. 1 L 7 2 3O 3 O A7SO E9CE 1996122600013 19961226 00013 1996 12 26 MWEA96636 4 19961121 A 2565 11331DC EVAC SLIDE DOUG DC9 DC914 3022034 WP FWD ENTRY LOW PRESS A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 6361 45725 DURING SERVICE CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE BOTTLE PRESSURE LOW. MAINTENANCE REMOVED AND REPLACED FWD E NTRY EVACUATION SLIDE. RETURNED A/C TO SERVICE. (X) 2 L 7 2 4F A6WE 1996122600014 19961226 00014 WP 1996 12 26 GAIA9632 1 19961115 A 3234 GEAR HANDLE CVAC 340 34031 2422704 WP LANDING GEAR LACK OF LUBE A GAIA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 SW 07 3412 32 FLT 475 ON APPROACH INTO CLE, FLIGHT CREW NOTED WITH LANDING GEAR HANDLE DOWN THE GREEN DOWN SAFE LIGHTS DID NOT ILLUMIN ATE. ATC WAS NOTIFIED, FLIGHT CREW REQUESTED TO GO AROUND AND RECYCLE THE LANDING GEAR. AFTER RECYCLING THE GEAR, THE THREE GREEN DOWN SAFE LIGHTS CAME ON. AN UNEVENTFUL LANDING WAS MADE. THE FLIGHT CREW NOTED THE LANDING GEAR HANDLE (L ATCH) WAS STICKING. MAINTENANCE LUBED THE LATCH SYSTEM. LIGHTS OPERATED NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4R 6A6 1996122600015 19961226 00015 NE 1996 12 26 C2XA96CL037 3 19961107 A 6110 PROPELLER BEECH 1900 1900D 1154162 CE HARTZL HCE4A HCE4A3A NE RT ENGINE LIGHTNING STRIKE A C2XA K NONE C F.O.D. CR CRUISE 1 SW 09 16540 1530 UE172 HJ562 CLE - FLT 3246 - THE CREW REPORTED A LIGHTNING STRIKE ON THE NOSE OF THE AIRCRAFT. MAINTENANCE ACCOMPLISHED A LIGHTNING STRIKE INSPECTION AND REMOVED AND REPLACED THE RIGHT HAND PROPELLER ASSEMBLY IAW B1900D MM 61-10-00. ALL OPERATIONAL A ND LEAKS WERE GOOD. AIRCRAFT RELEASED FOR SERVICE. A/C TOTAL CYCLES, 2,995. (X) 2 L 7 2 4T RT A24CE 5 C P10NE 1996122600017 19961226 00017 NM 1996 12 26 96ZZZX6148 1 19961106 A 3260 H1015133 DOWNLOCK SWITCH 6516364 BOEING 727 7272J7 138400E NM NLG INOPERATIVE A C8GA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 15 128NA 8582 L347 20879 AFTER TAKEOFF FROM TPA WITH THE GEAR HANDLE IN THE GEAR UP POSITION, BOTH THE RED AND GREEN NOSE GEAR LIGHTS REMAINED IL LUMINATED. THE GEAR HANDLE WAS PLACED IN THE GEAR DOWN POSITION AND THE AIRCRAFT RETURNED TO TPA WITHOUT INCIDENT. TRO UBLESHOOTING OF THE NOSE GEAR INDICATING SYSTEM REVEALED A FAULTY DOWNLOCK SWITCH. THE SWITCH WAS REPLACED, A NOSE GEAR SWING WAS ACCOMPLISHED. THE SYSTEM CHECKED NORMAL IAW 727 MM 32-61-01 AND THE AIRCRAFT WAS RELEASED FOR FLIGHT. 2 L 7 3 4F A3WE 1996122600018 19961226 00018 NM 1996 12 26 HNAA9698974 1 19961101 A 7712 311555701 TORQUE SENSOR DHAV DHC8 DHC8201 2809001 NM NR 2 ENGINE FAILED A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 989HA 1761 MM0523 427 FLT 3180, TPA TO PBI - AFTER TAKEOFF, POWER UPTRIM LIGHT FLICKERED ON, NR 1 TQ FLUXED PLUS OR MINUS 5 PERCENT, SECONDS L ATER THE NR 2 PROP FEATHERED. NR 2 TQ WAS HIGH FOR TWO SECONDS BEFORE POWER WAS REDUCED. NR 2 ENGINE CONTINUED TO RUN WITH ALL OTHER INDICATIONS NORMAL. THE AIRCRAFT RETURNED TO TPA AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE NR 2 TORQUE SENSOR, NR 2 TORQUE SIGNAL CONDITIONING UNIT (TSCU), AND NR 2 PROP ASSEMBLY. INTERROGATED TORQUE INDICATOR. NO OVERTORQUE FAULTS FOUND. REFERENCE: OPERATOR CONTROL NRS: 96ZZZX6149 AND NR 96ZZZX6150. (X) 2 H 7 2 4T RT A13NM 1996122600019 19961226 00019 NM 1996 12 26 96ZZZX6149 1 19961101 A 7712 30005000051 TSCU DHAV DHC8 DHC8201 2809001 NM NR 2 ENGINE FAILED A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 989HA 1761 MM4643 427 FLT 3180, TPA TO PBI - AFTER TAKEOFF, POWER UPTRIM LIGHT FLICKERED ON, NR 1 TQ FLUXED PLUS OR MINUS 5 PERCENT, SECONDS L ATER THE NR 2 PROP FEATHERED. NR 2 TQ WAS HIGH FOR TWO SECONDS BEFORE POWER WAS REDUCED. NR 2 ENGINE CONTINUED TO RUN WITH ALL OTHER INDICATIONS NORMAL. THE AIRCRAFT RETURNED TO TPA AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE NR 2 TORQUE SENSOR, NR 2 TORQUE SIGNAL CONDITIONING UNIT (TSCU), AND NR 2 PROP ASSEMBLY. INTERROGATED TORQUE INDICATOR. NO OVERTORQUE FAULTS FOUND. REFERENCE: OPERATOR CONTROL NRS: HNAA9698974 AND NR 96ZZZX6150. 2 H 7 2 4T RT A13NM 1996122600020 19961226 00020 NE 1996 12 26 96ZZZX6150 3 19961101 A 6110 PROP ASSY DHAV DHC8 DHC8201 2809001 NM HAMSTD 14SF 14SF23 NE NR 2 ENGINE OVERTORQUE A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 989HA 1761 427 951123 FLT 3180, TPA TO PBI - AFTER TAKEOFF, POWER UPTRIM LIGHT FLICKERED ON, NR 1 TQ FLUXED PLUS OR MINUS 5 PERCENT, SECONDS L ATER THE NR 2 PROP FEATHERED. NR 2 TQ WAS HIGH FOR TWO SECONDS BEFORE POWER WAS REDUCED. NR 2 ENGINE CONTINUED TO RUN WITH ALL OTHER INDICATIONS NORMAL. THE AIRCRAFT RETURNED TO TPA AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE NR 2 TORQUE SENSOR, NR 2 TORQUE SIGNAL CONDITIONING UNIT (TSCU), AND NR 2 PROP ASSEMBLY. INTERROGATED TORQUE INDICATOR. NO OVERTORQUE FAULTS FOUND. REFERENCE: OPERATOR CONTROL NRS: HNAA9698974 AND NR 96ZZZX149. 2 H 7 2 4T RT A13NM 6 C P7NE 1996122600021 19961226 00021 CE 1996 12 26 MESA201666 1 19961015 A 3397 WIRE BEECH 1900 1900D 1154162 CE CTR CONSOLE SHORTED A MASA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 01 14YV 9542 UE14 FLT 5960 EN ROUTE TO PITTSBURGH - NOTICED SPARKS COMING FROM POST AND AREA AROUND PRESSURIZATION DUMP SWITCH ON CENTER C ONSOLE IN COCKPIT. MAINTENANCE INSPECTED AREA AND REPAIRED WIRE ON POST LIGHT ASSY, P/N A8970C1327. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1996122600022 19961226 00022 WP 1996 12 26 96NK213A 1 19961028 A 3610 CLAMP DOUG DC9 DC941 302207N WP PNEU DUCT LOOSE A GTIA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 23 130NK 47604 REF MRR NR 96NK213. LOG/ITEM NR 027691/M293. IN-FLIGHT, BOTH SMOKE DETECTORS WENT OFF. FINDINGS: AFTER INSP, TESTS, AND INVESTIGATION OF CAUSE, FOUND PNEUMATIC DUCTING CLAMP CAME LOOSE AND CAUSED INSTALLATION TO SEPARATE AND AIRBORNE DU ST ENTERED THE AIR CYCLE MACHINE, AND PARTICLES FORMED IN CABIN AREA, AND TAIL CONE AREA SETTING OFF SMOKE DETECTORS. F CD GENERATED TO CHECK FLEET FOR SIMILAR PROBLEM. PNEU DUCT CLAMP FAILURE. (X) 2 L 7 2 4F A6WE 1996122600023 19961226 00023 NM 1996 12 26 USAABB96041 1 19961028 A 3350 873100251 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 626AU 27303 SFO - THREE EXIT IDENTIFIERS FOUND INOPERATIVE. MAINTENANCE REPLACED THE EXIT IDENTIFIERS. (X) 2 L 7 2 4F RT A2NM 1996122600024 19961226 00024 1996 12 26 HEEA968727 4 19961213 A 2312 9210121 TRANSCEIVER TFM138 BELL 412 412 1182202 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2014K 33020 NO AUDIO. SENT TO DALLAS AVIONICS FOR WARRANTY REPAIR. RECEIVED IN JULY 95. 1 G 7 2 4U H4SW 1996122600025 19961226 00025 EU 1996 12 26 HEEA968729 1 19961213 A 6240 117945641 INDICATOR BOLKMS 117 BK117A3 5626015 EU MAST MOMENT INTERMITTENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 401PH 7050 INDICATOR INTERMITTENT. TIME SINCE REPAIR 31:25. 1 G 7 2 3U H13EU 1996122600026 19961226 00026 1996 12 26 HEEA968730 4 19961213 A 2312 6222078001 TRANSCEIVER VHF251 BOLKMS 105 BO105S 5626006 EU COCKPIT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3520T S539 TRANSCEIVER WEAK AND BROKEN UP SEVERAL TIMES DURING FLIGHT. 1 G 7 2 3U H3EU 1996122600027 19961226 00027 GL 1996 12 26 HEEA968731 2 19961213 A 7320 11320003A2 HMU BELL 407 407 SW ALLSN 250C 250C47B GL ENG SEAL LEAK E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 407PH 624 53003 HMU INPUT SHAFT SEAL LEAKING. 1 G 7 1 3U 3 U O H2SW E1GL 1996122600029 19961226 00029 EU 1996 12 26 HEEA968733 1 19961213 A 6520 7704411 SEAL AEROSP AS355 AS355F1 8680810 EU T/R GR BOX CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5791M 5116 MAGNETIC SEAL UNIT CRACKED. 1 G 7 2 3U H11EU 1996122600030 19961226 00030 1996 12 26 HEEA968734 4 19961213 A 3452 066106200 TRANSCEIVER KT76 BELL 206 206B3 1181506 SW COCKPIT ATC MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 39122 3312 LOCK BROKEN. REPLACED BROKEN LOCKING MECHANISM. ALSO REPLACED DEFECTIVE DIODE CR202 THAT CAUSED WEAK SENSITIVITY. ADJU STED PRESELECTOR FOR PROPER SENSITIVITY. UNIT BENCH CHECK GOOD. 1 G 7 1 3U H2SW 1996122600031 19961226 00031 1996 12 26 HEEA968735 4 19961213 A 3451 066106901 INDICATOR BELL 412 412 1182202 SW COCKPIT DME DIM E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 108X 33115 INDICATOR TOO DIM. PERFORMED PRELIMINARY INSPECTION. REPLACED V901 (PHOTOCELL) REPAIRED. BENCH CHECK GOOD. 1 G 7 2 4U H4SW 1996122600032 19961226 00032 1996 12 26 HEEA968736 4 19961213 A 3452 066106200 TRANSCEIVER KT76 BOLKMS 117 BK117A4 5626017 EU COCKPIT ATC DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911RZ 7092 FREQUENCY OUT OF TOLERANCE. PERFORMED PRELIMARY INSPECTION. ADJUSTED PULSE WIDTH AND FREQUENCY TO SPECS. FOUND RECEIVE R SENSITIVITY LOW. REPLACED CR202 MIXER DIODE. HEATED AND VIBRATED UNIT. BENCH CHECK GOOD. 1 G 7 2 3U H13EU 1996122600033 19961226 00033 1996 12 26 HEEA968737 4 19961213 A 3452 066106200 TRANSCEIVER KT76 BELL 206 206L1 1182107 SW COCKPIT ATC INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 16938 45157 REPORTED BY TOWER, INOPERATIVE. PERFORMED PRELIMINARY INSPECTION. FOUND SWITCH ASSY. INTERMITTENT. ALSO FOUND POWER OU T LOW AND PHOTOCELL (V301) PHOTOCELL. REPAIRED. ADJUSTED PULSE WIDTH AND FREQUENCY. BENCH CHECK GOOD. 1 G 7 1 3U H2SW 1996122600034 19961226 00034 EU 1996 12 26 HEEA968738 1 19961213 A 2842 647511011 TRANSMITTER AEROSP AS355 AS355F1 8680810 EU FUEL QTY MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5796S 5164 LOW FUEL LIGHT INOPERATIVE. TIME SINCE REPAIR 102:45. 1 G 7 2 3U H11EU 1996122600035 19961226 00035 1996 12 26 HEEA968739 4 19961213 A 3453 4530103 LORAN ARNAV21 AEROSP AS355 AS355F1 8680810 EU COCKPIT BATTERY WARN E HEEA K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 03 5796S 5164 INTERMITTENT LOW BATTERY WARNING. 1 G 7 2 3U H11EU 1996122600036 19961226 00036 SW 1996 12 26 HEEA968740 1 19961213 A 7712 412075008111 INDICATOR BELL 412 412 1182202 SW TORQUE SHORTED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D 33076 #1 NEEDLE SHORTED TO CASE. SENT TO MASCO FOR WARRANTY REPAIR. 1 G 7 2 4U H4SW 1996122600037 19961226 00037 1996 12 26 HEEA968741 4 19961213 A 3451 066106602 TRANSCEIVER BELL 214 214ST 1182106 SW COCKPIT DME WEAK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 TRANSCEIVER RECEIVE WEAK. 2 G 7 2 4U H10SW 1996122600038 19961226 00038 EU 1996 12 26 HEEA968742 1 19961213 A 2612 0301037070 HARNESS SNIAS 350 AS350B2 8680813 EU ENG FIRE DET PROBE BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 2771 ONE PROBE WAS FOUND BROKEN LOOSE FROM ENGINE AND HANGING FROM HARNESS. 1 G 7 1 3U H9EU 1996122600039 19961226 00039 EU 1996 12 26 HEEA968743 1 19961213 A 6220 10514101111 HEX.BOLT BOLKMS 105 BO105S 5626006 EU M/R DAMAGED E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 81992 1174 S827 HEAD OF BOLT IS CRACKED AT ONE CORNER OF WENCH FLATS. SEEMS TO BE CAUSED BY CORNER BEING HIT OR WRENCH SHIPPING. INSTAL LED SERVICEABLE BOLT. 1 G 7 2 3U H3EU 1996122600040 19961226 00040 EU 1996 12 26 HEEA968744 1 19961213 A 6220 10514101111 HEX.BOLT BOLKMS 105 BO105S 5626006 EU M/R DAMAGED E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 81982 710 S818 CORNER OF BOLT HEAD CRACKED. REPLACED WITH SERVICEABLE BOLT. 1 G 7 2 3U H3EU 1996122600041 19961226 00041 1996 12 26 HEEA968745 4 19961213 A 3453 25410036 7000 RCU SKRSKY S76 S76A 8143006 NE LORAN INOP E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545K 760047 LORAN INOPERATIVE. CDU DISPLAY REMAINS BLANK. TIME SINCE REPAIR 0:00. 1 G 7 2 3U H1NE 1996122600042 19961226 00042 1996 12 26 HEEA968746 4 19961213 A 3455 066107700 RECEIVER BELL 412 412 1182202 SW COCKPIT ADF MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22347 36005 ADF WON'T POINT TO STATION. 1 G 7 2 4U H4SW 1996122600043 19961226 00043 1996 12 26 HEEA968747 4 19961213 A 3453 27010045 ANTENNA SKRSKY S76 S76A 8143006 NE COCKPIT LORAN DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545K 760047 LORAN DOES NOT RECEIVE SIGNAL. 1 G 7 2 3U H1NE 1996122600044 19961226 00044 SW 1996 12 26 HEEA968748 1 19961213 A 5302 206032118123 PANEL ASSY BELL 206 206L1 1182107 SW FUSELAGE MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 3904L 45597 INSERTS DON'T LINE UP WITH ACCESS PANEL AS MARKED. 1 G 7 1 3U H2SW 1996122600045 19961226 00045 1996 12 26 HEEA968749 4 19961213 A 3442 MI585202 ANT PEDESTAL SKRSKY S76 S76A 8143006 NE RADAR MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1547D 760077 RADAR WILL NOT SCAN. 1 G 7 2 3U H1NE 1996122600046 19961226 00046 1996 12 26 HEEA968750 4 19961213 A 3453 453105004 LORAN ARNAV BELL 412 412 1182202 SW COCKPIT MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 108X 33115 ARNAV SYS ENTER BUTTON INOPERATIVE. 1 G 7 2 4U H4SW 1996122600047 19961226 00047 NE 1996 12 26 HEEA968751 1 19961213 A 6220 7610708006144 PIN 761070810012 SKRSKY S76 S76A 8143006 NE M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 1077 PHI1010 760035 M/R PIN WORN BEYOND LIMITS. REPLACED WITH SERVICEABLE PARTS. 1 G 7 2 3U H1NE 1996122600048 19961226 00048 NE 1996 12 26 HEEA968752 1 19961213 A 6220 7610708007103 TAPERED WASHERS 761070810012 SKRSKY S76 S76A 8143006 NE M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 1077 PHI1010 760035 TAPERED WASHER WORN BEYOND LIMITS. REPLACED WITH SERVICEABLE PARTS. 1 G 7 2 3U H1NE 1996122600049 19961226 00049 NE 1996 12 26 HEEA968753 1 19961213 A 6220 7610708002114 BUSHING 761070810012 SKRSKY S76 S76A 8143006 NE M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 1077 PHI1010 760035 BUSHING WORN BEYOND LIMITS. REPLACED WITH SERVICEABLE PARTS. 1 G 7 2 3U H1NE 1996122600050 19961226 00050 NE 1996 12 26 HEEA968754 1 19961213 A 6220 7610708002113 BUSHINGS 761070810012 SKRSKY S76 S76A 8143006 NE M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22342 797 PHI1004 760096 BUSHINGS WORN BEYOND LIMITS. REPLACED WITH SERVICEABLE PARTS. 1 G 7 2 3U H1NE 1996122600051 19961226 00051 NE 1996 12 26 HEEA968755 1 19961213 A 6220 7610708006144 PIN 761070810012 SKRSKY S76 S76A 8143006 NE M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22342 797 PHI1004 760096 PIN WORN BEYOND LIMITS. REPLACED WITH SERVICEABLE PARTS. 1 G 7 2 3U H1NE 1996122600052 19961226 00052 NE 1996 12 26 HEEA968756 1 19961213 A 6220 7610708007103 TAPERED WASHERS 761070810012 SKRSKY S76 S76A 8143006 NE M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22342 797 PHI1004 760096 TAPERED WASHER WORN BEYOND LIMITS. REPLACED WITH SERVICEABLE PARTS. 1 G 7 2 3U H1NE 1996122600053 19961226 00053 NE 1996 12 26 HEEA968757 1 19961213 A 6220 7610708002113 BUSHINGS 761070810012 SKRSKY S76 S76A 8143006 NE M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545K 1334 PHI1013 760047 BUSHING WORN BEYOND LIMITS. REPLACED WITH SERVICEABLE PARTS. 1 G 7 2 3U H1NE 1996122600054 19961226 00054 NE 1996 12 26 HEEA968758 1 19961213 A 6220 7610708002114 BUSHING 761070810012 SKRSKY S76 S76A 8143006 NE M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545K 1334 PHI1013 760047 BUSHING WORN BEYOND LIMITS. REPLACED WITH SERVICEABLE PARTS. 1 G 7 2 3U H1NE 1996122600055 19961226 00055 NE 1996 12 26 HEEA968759 1 19961213 A 6220 7610708006144 PIN 761070810012 SKRSKY S76 S76A 8143006 NE M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545K 762 PHI1013 760047 PIN WORN BEYOND LIMITS. REPLACED WITH SERVICEABLE PARTS. 1 G 7 2 3U H1NE 1996122600056 19961226 00056 NE 1996 12 26 HEEA968760 1 19961213 A 6220 7610708007103 TAPERED WASHERS 761070810012 SKRSKY S76 S76A 8143006 NE M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545K 762 PHI1013 760047 TAPERED WASHERWORN BEYOND LIMITS. REPLACED WITH SERVICEABLE PARTS. 1 G 7 2 3U H1NE 1996122600057 19961226 00057 NE 1996 12 26 HEEA968761 1 19961213 A 6220 7610708006143 PINS 761070810012 SKRSKY S76 S76A 8143006 NE M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545K 762 PHI1013 760047 PIN WORN BEYOND LIMITS. REPLACED WITH SERVICEABLE PARTS. 1 G 7 2 3U H1NE 1996122600058 19961226 00058 WP 1996 12 26 CALA9601848 1 19961021 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1882 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37077 46981 INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 1882, LBL 36. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-21-01 , 51-31-01 AND 53-60-01, FIGURE 1. 2 L 7 3 4F A22WE 1996122600059 19961226 00059 WP 1996 12 26 CALA9601849 1 19961010 A 5330 SKIN DOUG DC10 DC1030 3023501 WP BS 1049-1069 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37077 46981 INSPECTION FOUND CORROSION ON FUSELAGE SKIN AT BS 1049 TO 1069, STRINGER 52. THE CORRODED AREA WAS REMOVED. REPAIR DOU BLERS, FINGER DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-20-00, FIGURE 7. 2 L 7 3 4F A22WE 1996122600060 19961226 00060 WP 1996 12 26 CALA9601850 1 19961010 A 5330 SKIN DOUG DC10 DC1030 3023501 WP BS 1009-1029 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37077 46981 INSPECTION FOUND FUSELAGE SKIN CORRODED AT BS 1009 TO 1029, STRINGER 52. THE CORRODED AREA WAS CUT OUT. REPAIR DOUBLER S, FINGER DOUBLERS AND FILLER WERE INSTALLED IAW SRM 53-20-00, FIGURE 7. 2 L 7 3 4F A22WE 1996122600061 19961226 00061 WP 1996 12 26 CALA9601851 1 19961021 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1963 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37077 46981 INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 1963, LBL 27. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-21-01 , 51-31-01 AND 53-60-01, FIGURE 1. 2 L 7 3 4F A22WE 1996122600062 19961226 00062 WP 1996 12 26 CALA9601852 1 19961114 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1900 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37077 46981 INSPECTION FOUND THE UPPER HORIZONTAL SURFACE OF FORWARD END FLOOR SUPPORT CORRODED AT STA 1900, RBL 57. THE CORRODED S ECTION WAS REMOVED, A NEW SECTION WAS SPLICED IN IAW SRM 53-70-00, FIGURE 13. 2 L 7 3 4F A22WE 1996122600063 19961226 00063 WP 1996 12 26 CALA9601853 1 19961021 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1986-2007 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37077 46981 INSPECTION FOUND FLOOR SUPPORT CORRODED AROUND FLOOR PANEL ATTACH HOLES FROM BS 1986 TO 2007, RBL 27. A NEW FLOOR SUPPO RT WAS FABRICATED AND INSTALLED IAW SRM 53-60-01 FIGURE 1, 51-31-01 AND 51-20-01. 2 L 7 3 4F A22WE 1996122600064 19961226 00064 WP 1996 12 26 CALA9601854 1 19961021 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37077 46981 INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 1986, LBL 27. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-21-01 , 51-31-01 AND 53-60-01, FIGURE 1. 2 L 7 3 4F A22WE 1996122600065 19961226 00065 WP 1996 12 26 CALA9601855 1 19961015 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 472 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37077 46981 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 472, LBL 54. TWO ANGLES, FILLER AND A FLOOR SUPPORT WERE FABRICATED AND INSTALLED IAW SRM 51-31-01, 51-21-01, 51-35-01 AND 53-60-01 FIGURE 1. 2 L 7 3 4F A22WE 1996122600066 19961226 00066 WP 1996 12 26 CALA9601856 1 19961020 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 457 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37077 46981 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 457, RBL 29. A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-21-01 , 51-35-01 AND 53-11-01, FIGURE 1A. 2 L 7 3 4F A22WE 1996122600067 19961226 00067 WP 1996 12 26 9626599611 1 19961213 A 7711 LG80A2 TRANSMITTER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7 52053 NE RT ENGINE INOPERATIVE A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 611NA 38808 1640 47435 657515 WHEN APPLYING TAKEOFF POWER, THE RIGHT ENGINE EPR INDICATION DID NOT RESPOND. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE RIGHT ENGINE EPR TRANSMITTER, OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F A6WE E2EA 1996122600068 19961226 00068 NE 1996 12 26 9626609105 2 19961216 A 7200 751601 ENGINE DOUG DC9 DC915 3022036 WP PWA JT8 JT8D7 52053 NE LEFT FAILED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN E VIBRATION/BUFFET CL CLIMB 1 GL 01 95S 472055 649030 DURING CLIMB AT 1000 FEET AGL, A NOISE WAS HEARD FOLLOWED BY VIBRATIONS AND A CONTAINED FAILURE OF THE LEFT ENGINE. CRE W FOLLOWED COM EMERGENCY PROCEDURES. RETURNED TO MSP AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEF T ENGINE. 2 L 7 2 4F 4 F A6WE E2EA 1996122600069 19961226 00069 WP 1996 12 26 9626619912 1 19961218 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 962N 47406 EMERGENCY LIGHTS IN FORWARD CABIN AND AT GALLEY SERVICE DOOR EXIT REMAINED ON DURING FLIGHT. REPLACED BATTERIES IN MODU LE AT GALLEY SERVICE DOOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996122600070 19961226 00070 WP 1996 12 26 9626629909 1 19961217 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 959N 47255 DURING LINE MAINTENANCE INSPECTION, FOUND AFT OVERWING EMERGENCY LIGHTS ON LEFT AND RIGHT SIDES INOPERATIVE. REPLACED B ATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996122600071 19961226 00071 WP 1996 12 26 9626639967 1 19961217 A 3350 CONNECTOR DOUG DC9 DC931 3022065 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9331 47263 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS BETWEEN ROWS 14 THROUGH 17 INOPERATIVE. REPAIRED CONNECTOR I N CEILING AT ROW 17, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996122600072 19961226 00072 WP 1996 12 26 9626649995 1 19961216 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN MALFUNCTIONED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8978E 47327 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, OPERATI ONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996122600073 19961226 00073 WP 1996 12 26 9626659962 1 19961217 A 3260 DOWNLOCK IND DOUG DC9 DC931 3022065 WP LT MLG MALFUNCTIONED A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 914RW 47362 DURING APPROACH, LEFT MAIN LANDING GEAR GREEN DOWNLOCK LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. CREW RECYCLED GEA R AND VERIFIED VISUALLY THROUGH PERISCOPE THAT GEAR WAS DOWN AND LOCKED. GREEN LIGHT ILLUMINATED AFTER BULB REPLACEMENT . AIRCRAFT LANDED WITHOUT INCIDENT. DISCREPANCY COULD NOT BE DUPLICATED BY MAINTENANCE ON GROUND, OPERATIONAL CHECK NO RMAL. 2 L 7 2 4F A6WE 1996122600074 19961226 00074 WP 1996 12 26 9626669918 1 19961218 A 2780 RETRACT MECH DOUG DC9 DC932 3022066 WP LT LE FLAP MALFUNCTIONED A NWAA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 01 940N 47572 SLAT DISAGREEMENT LIGHT ILLUMINATED WITH NO SLAT EXTEND BLUE LIGHT ON APPROACH. RECYCLED SLATS TWICE WITH SAME RESULTS. AIRCRAFT LANDED WITHOUT INCIDENT WITH NO SLATS AND FLAPS AT 40 DEGREES. MAINTENANCE INSPECTED T-DUCTS, ACTUATOR AND B ELL CRANK MECHANISM. ALSO, PERFORMED SLAT ACTUATION SYSTEM TEST, ALL CHECKED NORMAL. DISCREPANCY COULD NOT BE DUPLICAT ED. 2 L 7 2 4F A6WE 1996122600075 19961226 00075 SO 1996 12 26 COMA9610404 1 19961218 A 6120 7845191 PITCHLOCK SCREW 7902015 EMB 120 EMB120RT SO PWA 118 PW118 NE HAMSTD 14RF 14RF9 NE PROP ACTUATOR FAILED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 1968 880601 120264 115571 910337 PROPELLER ASSEMBLY WAS ORIGINALLY REMOVED FOR EXCESSIVE VIBRATION. UPON DISASSEMBLY AND VISUAL INSPECTION, ACTUATOR (S/ N 880601) WAS FOUND UNSERVICEABLE DUE TO THE FEATHER STOP TAB ON THE PITCHLOCK SCREW BEING DISPLACED APPROXIMATELY .5 IN FROM ORIGINAL POSITION. 2 L 7 2 4T 4 T RT A31SO E20NE 6 C P11NE 1996122600076 19961226 00076 SO 1996 12 26 COMA9610405 1 19961217 A 2910 12040344005 HYDRAULIC HOSE EMB 120 EMB120RT SO LT MLG FAILED A COMA K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 SO 01 152CA 120152 HYDRAULIC FLUID LEAKING FROM LT LANDING GEAR AREA. REPLACED LEAKING LANDING GEAR ACTUATOR HYDRAULIC HOSE. 2 L 7 2 4T RT A31SO 1996122600077 19961226 00077 SO 1996 12 26 COMA9610406 1 19961217 A 3230 12038594001 CONTROL UNIT EMB 120 EMB120RT SO LANDING GEAR MALFUNCTION A COMA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 130G 11751 1088 120130 AFTER TAKEOFF, WHEN LANDING GEAR SELECTED UP, THE LT MLG INDICATED DOWN. CYCLED GEAR CONTROL WITH SAME RESULTS. ELECTR ICAL OVERRIDE PROCEDURE WAS USED TO EXTEND LANDING GEAR FOR LANDING. REPLACED THE LANDING GEAR CONTROL ASSY. 2 L 7 2 4T RT A31SO 1996122600078 19961226 00078 NE 1996 12 26 COMA9630163 2 19961218 A 7510 32899541 SHUTOFF VALVE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LT ENGINE MALFUNCTION A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 359CA 1853 5 340A053 WITH ENGINE ANIT-ICE OPERATING, THE LT AIR VALVE WARNING ILLUMINATED ON CWP. REPLACED THE BLEED AIR SHUT OFF VALVE. 2 L 7 2 4T 4 T RT A52EU E8NE6 1996122600079 19961226 00079 EA 1996 12 26 COMA9660228 1 19961217 A 5210 60031535 SEAL STRIKER CNDAIR CL600 CL6002B19 EA BS 349 DENTED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 952CA 7092 PASSENGER DOOR FRAME AFT SEAL STRIKE, ON FUSELAGE, DAMAGED IN TWO PLACES AT THE BOTTOM BY THE LOWER LATCH PIN AND AT THE TOP BY THE PULL-IN LEVER ROLLER. BOTH AREAS REPAIRED PER CANADAIR REO 601R-52-11-008, REPAIR B, PERMANENT REPAIR. 2 L 7 2 4F RT A21EA 1996122600080 19961226 00080 NE 1996 12 26 COMA9660229 2 19961211 A 7230 6018T30P06 FAN BLADE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RT ENGINE FOD A COMA O OTHER C E F.O.D. VIBRATION/BUFFET CL CLIMB 1 SO 01 963CA 7127 807402 AT 25,000 FT A BANG SOUND WAS HEARD FOLLOWED BY A 2.2 VIB ON RT ENGINE. MAINTENANCE REPLACED TWO SETS OF DAMAGED FAN BL ADES ON RT ENGINE. IT IS PROBABLE THAT THIS FOD WAS CAUSED BY ICE FROM THE GALLEY WATER DRAIN MAST. 2 L 7 2 4F 4 F RT A21EA E15NE 1996122600081 19961226 00081 NM 1996 12 26 UPS96221786 1 19961217 A 3350 LIGHTS BOEING 727 72725C 138400H NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHT IN COCKPIT INOP. REPLACED BATTERIES, OPS CHKS GOOD. 2 L 7 3 4F A3WE 1996122600082 19961226 00082 NM 1996 12 26 UPS96521785 1 19961216 A 3350 5283T0143 LIGHT BOEING 757 75724APF 1384969 NM CABIN INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 422UP 25324 INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHTS FAIL TO TEST ON PDC. EMERGENCY EXIT LIGHTS POWER SUPPLY AND BATTERY REMOVED AND REPLACED AS PER MM 33-51-07 AND OPS CHK GOOD, (P/N 33-50-190-320) ON, (P/N 5283T014-3) OFF, (S/N FTW Z42114) ON, (S/ N 39161). 2 L 7 2 4F RT A2NM 1996122600083 19961226 00083 WP 1996 12 26 UPS96821783 1 19961214 A 3350 6012235 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CK OK (P/N 60-1 223-5) (S/N 322) ON, (S/N 10) OFF. 2 L 7 4 4F RT 4A25 1996122600084 19961226 00084 WP 1996 12 26 UPS96821784 1 19961217 A 2170 COALESCER BAG DOUG DC8 DC871F 302199D WP RT PACK CONTAMINATED A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE-N/A, STRONG DIESEL FUEL SMELL COMING FROM RIGHT PACK. CREW FELT NAUSEA AND HEADACHES, ONE HAD TO USE OX YGEN. REPLACED RT A/C WATER COALESCER BAG. BOTH PACKS OP/C FOR SMELL, NO SMELL NOTED OP/CK GOOD. 2 L 7 4 4F RT 4A25 1996122600085 19961226 00085 WP 1996 12 26 ABXA9600683 1 19961213 A 3260 H146 UPLATCH SWITCH DOUG DC9 DC931 3022065 WP RT MLG DEFECTIVE A ABXA K NONE N FALSE WARNING TO TAKEOFF 1 GL 23 949AX 47325 RIGHT HAND MAIN GEAR UNSAFE LIGHT ON AFTER TAKEOFF. RECYCLED LANDING GEAR, LIGHT WENT OUT. PERFORMED GEAR UPLATCH CHEC K, ALL SYSTEMS NORMAL. REPLACED RIGHT MAIN LANDING GEAR UPLATCH SWITCH IAW DC-9 SUPP MM 32-60-01, OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996122600086 19961226 00086 WP 1996 12 26 ABXA9600684 1 19961214 A 3230 8756252 UPLATCH ASSY DOUG DC9 DC931 3022065 WP RT MLG OVERTORQUED A ABXA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 949AX 47325 RIGHT GEAR UNSAFE LIGHT ILLUMINATED ON GEAR RETRACTION. RECYCLED GEAR, NO HELP. ON UPLATCH CHECK, GEAR DOOR OPEN LIGHT ILLUMINATED. RAISED HANDLE, KEPT RIGHT HYDRAULIC PRESSURE AT 3,000 PSI. FOUND HARDWARE ON UPLATCH MECHANISM OVER TORQ UED NOT ALLOWING THE LATCH HOOK TO MOVE INTO POSITION. RETORQUED HARDWARE IAW DC-9 MM 32-31-4, OPS CHECK GOOD ON GEAR S WING. 2 L 7 2 4F A6WE 1996122600087 19961226 00087 WP 1996 12 26 MWEA96655 1 19961218 A 3231 3914985515 LATCH MECH DOUG DC9 DC932 3022066 WP NLG DOOR FROZEN A MWEA D RETURN TO BLOCK E VIBRATION/BUFFET TO TAKEOFF 1 GL 31 209ME 47730 PILOT REPORTS VIBRATION ON TAKEOFF DUE TO NOSE GEAR DOOR NOT CLOSING. RETURNED TO OMA. FOUND LT NOSE LANDING GEAR DOOR OPEN. REMOVED ICE FROM LATCH MECHANISM, CYCLED DOOR SEVERAL TIMES, OPS CHECK GOOD. 2 L 7 2 4F A6WE 1996122600088 19961226 00088 WP 1996 12 26 MWEA96656 1 19961218 A 2560 5917689103 SLIDE COVER DOUG DC9 DC914 3022034 WP GALLEY DOOR FELL OFF A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 CREW REPORTS, FWD ENTRANCE EVAC SLIDE COVER FELL OFF. REINSTALLED FWD ENTRY DOOR SLIDE COVER. RETURNED A/C TO SERVICE. 2 L 7 2 4F A6WE 1996122600089 19961226 00089 WP 1996 12 26 DLL13962670 1 19961209 A 3350 5165741 BATTERY PACK LKHEED 1011 10113851 5265010 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 783DL 193A1009 AIRCRAFT EMERGENCY LIGHTS AT L-1 AND R-1 DOORS INOP. REPLACED THE AIRCRAFT BATTERY PACKS AT L-1 AND R-1. 2 L 7 3 4F A23WE 1996122600090 19961226 00090 NM 1996 12 26 DL72W962672 1 19961209 A 3350 S106 BATTERY BOEING 727 727247 138408F NM AFT AIRSTAIR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 296WA 22533 AFT AIRSTAIR EMERGENCY LIGHT INOP. REPLACED BATTERIES, CHECKS NORMAL. 2 L 7 3 4F A3WE 1996122600091 19961226 00091 WP 1996 12 26 DLL10962686 1 19961212 A 3350 BATTERY 3125 LKHEED 1011 10113851 5265010 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 733DS 193C1224 F/A FLASHLIGHT AT DOOR 2R INOP. 2 L 7 3 4F A23WE 1996122600092 19961226 00092 NM 1996 12 26 DL733962688 1 19961212 A 3350 BATTERY PACK 20131A BOEING 737 737347 1384647 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 311WA 13957 23597 EMERGENCY EXIT LIGHT OVER F/C DIVIDER AND 3 BULL NOSE LIGHTS AT ROWS 12, 14, 16 INOP. REPLACED BATT PACK AT M1135, ALL EMERGENCY LIGHTS NOW OPS TEST OK. 2 L 7 2 4F RT A16WE 1996122600093 19961226 00093 NM 1996 12 26 DL72S962689 1 19961213 A 5320 ANGLE BOEING 727 727232 1384082 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 522DA 21582 FOUND DURING F-2 LETTER CHECK, CORROSION AT FUSELAGE BELLY PANEL 3348L FWD HINGE SUPPORT. REPAIRED PER M/M 53-30-01. 2 L 7 3 4F A3WE 1996122600094 19961226 00094 NM 1996 12 26 DL72S962690 1 19961213 A 5320 WEB BOEING 727 727232 1384082 NM BS 1219-1224 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 522DA 21582 FOUND DURING F-2 LETTER CHECK, 3 EA .5 INCH CRACKS LWR TORQUE BOX WEB STA 1219 TO 1224 LEFT SIDE. REPAIRED PER M/M 53-1 1-0. 2 L 7 3 4F A3WE 1996122600095 19961226 00095 NM 1996 12 26 DL72L962691 1 19961213 A 3350 BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 509DA 588 21311 EMERGENCY EXIT SIGN LIGHTS OVER RT OVERWING EXITS DID NOT TEST PROPERLY. REPLACED BATTERY PACK, OPN CKS OK. 2 L 7 3 4F A3WE 1996122600096 19961226 00096 1996 12 26 DLM88962692 4 19961214 A 2210 4034234902 PANEL DOUG MD88 MD88 3023688 NM COCKPIT SHORTED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 979DL 53266 AFTER LIGHT CHECK ON PREFLIGHT, F/O TRP PANEL UPPER RIGHT CORNER BEGAN TO SMOKE WITH ACRID ELECTRICAL ODOR. SECURED ALL ELECTRICS, REPLACED TRP PANEL, ALL CHECKS NORMAL. 2 L 7 2 4F RT A6WE 1996122600097 19961226 00097 NM 1996 12 26 DLM88962693 1 19961214 A 3350 LIGHTS DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 921DL 49645 THE FORWARD TRACK LIGHTS FWD THREE 2 RED AND ONE WHITE STRIP LIGHTS INOP. REPAIRED WIRE BETWEEN THE FORWARD THREE LIGHT S AND THE MAIN TRACK LIGHTS, OPS CHECKS GOOD ON EMERGENCY LIGHT TEST. 2 L 7 2 4F RT A6WE 1996122600098 19961226 00098 NM 1996 12 26 DLM88962694 1 19961214 A 2150 PACKS DOUG MD88 MD88 3023688 NM LT/RT FAILED A DALA B EMER. DESCENT G MULTIPLE FAILURE CL CLIMB 1 SO 27 972DL 53215 ON CLIMBOUT THROUGH 30,000 FT, RT PACK TRIPPED OFF, TEMP VALVE FULL HOT. CHECKLIST ACCOMPLISHED. WHILE ATTEMPTING TO R ESET THE RT PACK, THE LT PACK TRIPPED OFF. CABIN ALT BEGAN CLIMBING AT 1,500 FPM. CABIN EXEEDED 10K FT MASK DEPL OYED BY CREW. EMERGENCY DESCENT ACCOMPLISHED. 2 L 7 2 4F RT A6WE 1996122600099 19961226 00099 NM 1996 12 26 DLM88962695 1 19961214 A 3231 SPRING 4951635501 DOUG MD88 MD88 3023688 NM RT NLG DOOR BROKEN A DALA K NONE E VIBRATION/BUFFET TO TAKEOFF 1 SO 27 998DL 53370 EXCESSIVE AIR NOISE COMING FROM NOSE GEAR AREA AFTER DEPART. AIRCRAFT RETURNED TO LGA. FOUND RT UPPER LOCK LINK SPRIN G BROKEN. DAMAGED RT NOSE GEAR DOOR. 2 L 7 2 4F RT A6WE 1996122600100 19961226 00100 NM 1996 12 26 DLM88962696 1 19961214 A 2910 O-RING DOUG MD88 MD88 3023688 NM RT MLG WW LEAKING A DALA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 940DL 49813 EN ROUTE, RIGHT HD QTY IND DECREASED TO 4 QTS. FOUND O-RING ON SPOILER REDUCER LEAKING. REPLACED SAME. 2 L 7 2 4F RT A6WE 1996122600101 19961226 00101 NM 1996 12 26 DL72P962699 1 19961214 A 3350 LIGHT 1000677 BOEING 727 727225 1384077 NM L2 DOOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8873Z 20597 21291 L-2 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT/BATTERY ASSY, OPS OK. 2 L 7 3 4F A3WE 1996122600102 19961226 00102 1996 12 26 DHL96705001 4 19961217 A 3100 7225432002 INSTRUMENT AMP BOEING 727 72722C 138400F NM EQUIP BAY FAILED A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 705DH 19191 ON CLIMBOUT, CAPT ADI DISPLAYED GYRO AND STEER FLAGS. REMOVED AND REPLACED NR 1 INSTRUMENT AMP, OPS CHECK OK PER M/M 34 -62-61. 2 L 7 3 4F A3WE 1996122600103 19961226 00103 NE 1996 12 26 VNAA9612001 2 19961208 A 7322 311703603 HMU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE FAILED A VNAA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 07 437JS 3011 3055 PCE116112 AFTER 4 MINUTES OF FLIGHT, LEFT ENGINE TORQUE WENT TO ZERO AND LOST OIL PRESSURE. AIRCRAFT RETURNED TO FIELD ON RIGHT E NGINE ONLY WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LH HYDRO MECHANICAL UNIT, GROUND RUNS CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996122600104 19961226 00104 NM 1996 12 26 VNAA9612002 1 19961210 A 5270 869701 PROX SWITCH DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE BAGGAGE DOOR OUT OF ADJUST A VNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 461PS 899 3075 WHILE PASSING THROUGH 1700 FEET, THE BAGGAGE COMPARTMENT DOOR LIGHT CAME ON. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED THE BAGGAGE DOOR PROXIMITY SWITCH. OPERATIONAL CHECKED GOOD, AIRCRAFT APPROVED FOR RET URN TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996122600105 19961226 00105 NM 1996 12 26 VNAA9612003 1 19961216 A 3234 7178011 SELECTOR DORNER DO32 DO328100 2996000 NM COCKPIT SHORTED A VNAA O OTHER P NO WARNING INDICATION DE DESCENT 1 GL 07 461PS 947 134 3075 CLT - FLT 4008 - LANDING GEAR GREEN DOWN AND LOCKED LIGHTS DID NOT COME ON WHEN LANDING GEAR WAS SELECTED DOWN. TOWER O BSERVATIONS WERE THAT THE GEAR WAS EXTENDED. DECLARED EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOV ED AND REPLACED THE LANDING GEAR SELECTOR LEVER, AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. PART TOTAL CYCLES 828. ( X) 2 H 7 2 4T RT A45NM 1996122600106 19961226 00106 WP 1996 12 26 CKSA96362 1 19961215 A 5711 SPAR DOUG DC8 DC863F 302198F WP WS 295 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND LEFT WING UPPER REAR SPAR STA XRS295 HAS SEVERE CORROSION, WITH SEPARATION. REPAIRED IAW SKETCH NR AIA/E/2415. CORROSION CARD NR 117L-0551. NON-ROUTINE TASK CARD NR 88649, LEVEL 2. 2 L 7 4 4F 4A25 1996122600107 19961226 00107 WP 1996 12 26 CKSA96363 1 19961215 A 5313 2641455 LONGERON DOUG DC8 DC863F 302198F WP BS 1160-1180 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND FS 1160 TO 1180 LONGERON 32 LT LONGERON CORRODED. REMOVED CORROSION, OUT OF LIMITS, FABRICATED DOUBLER REPAIR AS PER AIA/E/2422. TREATED AND PRIMED IAW SRM 51-1-8 AND INSTALLED REPAIR AS PER SRM 51-1-20D . CORROSION CARD NR 5590-0551. NON-ROUTINE TASK NR 90855, LEVEL 2. 2 L 7 4 4F 4A25 1996122600108 19961226 00108 WP 1996 12 26 CKSA96364 1 19961215 A 5320 DOUBLER DOUG DC8 DC863F 302198F WP BS 1220 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND FS 1220 LONGERON 30 TO 31 LT INNER DOUBLER CORRODED. REMOVED CORROSION, OUT OF LIMIT S. REPAIRED, TREATED AND PRIMED IAW DC-8 SRM 51-1-8, 53-2-0 FIGURE 1F AND 53-2-0 FIGURE 1B. CORROSION CARD NR 5590-055 1. NON-ROUTINE TASK CARD NR 89605, LEVEL 2. 2 L 7 4 4F 4A25 1996122600109 19961226 00109 WP 1996 12 26 CKSA96365 1 19961215 A 5320 37558452 FITTING DOUG DC8 DC863F 302198F WP BS 1200 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND C-BAGGAGE COMPARTMENT FS 1200 LONGERON 34 LT TO LONGERON 35 LT, BATHTUB FITTING CORRO DED. REMOVED CORROSION AND TREATED IAW SRM 51-1-8 AND INSTALLED FITTING WITH HI-LOCKS IAW SRM 51-1-20D. CORROSION CARD NR 5590-0551. NON-ROUTINE TASK CARD NR 89597, LEVEL 2. 2 L 7 4 4F 4A25 1996122600110 19961226 00110 WP 1996 12 26 CKSA96366 1 19961215 A 5730 SKIN DOUG DC8 DC863F 302198F WP WS 693 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND LEFT HAND WING UPPER SURFACE STA XRS693 CORROSION LIMIT EXCEEDED, REFERENCE M-40 NBR. 88626. INSTALLED DOUBLER REPAIR IAW AIA ENGINEERING SKETCH NR 2423. CORROSION CARD NR 109L-0551. NON-ROUTINE TASK CA RD NR 90769, LEVEL 2. 2 L 7 4 4F 4A25 1996122600111 19961226 00111 WP 1996 12 26 CKSA96367 1 19961215 A 5720 36411253502F FITTING DOUG DC8 DC863F 302198F WP BS 759 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND UPPER WING CENTER SECTION STA 759 RBL 57 FRAME SUPPORT FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D. CORROSION CARD NR 2000-0551. NON-ROUTINE TASK CARD NR 90922, LEVEL 2. 2 L 7 4 4F 4A25 1996122600112 19961226 00112 WP 1996 12 26 CKSA96368 1 19961215 A 5753 SKIN DOUG DC8 DC863F 302198F WP TE FLAP GOUGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND OUTBOARD FLAP HAS BOLT GOUGE, INBOARD SIDE OF INBOARD ICE BREAKER MARKED H6. REPAIR OUTBOARD FLAP IAW DC8 SRM 57-2-5 FIGURE 1. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. C-1 CHECK CARD NR 1008. NON-ROUTIN E TASK CARD NR 89573. 2 L 7 4 4F 4A25 1996122600113 19961226 00113 WP 1996 12 26 CKSA96369 1 19961215 A 5320 DOUBLER DOUG DC8 DC863F 302198F WP BS 80 FLOOR CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND STA 80 AT STRINGER 22R PRESSURE FLOOR PANEL FINGER DOUBLERS SEPARATING AND FASTENERS SHEARED. REMOVED AND REPLACED FINGER DOUBLERS CLEANED CORROSION AND FOUND TO BE WITHIN LIMITS ON PRESSURE FLOOR PANEL. REPLACED DOUBLER AROUND POWER CABLES IAW DC-8 SRM 53-2-0, 51-1-21. C-1 CHECK WORK CARD NR 0065. NON-ROUTINE TASK CARD NR 91641. 2 L 7 4 4F 4A25 1996122600114 19961226 00114 WP 1996 12 26 CKSA96370 1 19961215 A 5320 3755843501 CASTING DOUG DC8 DC863F 302198F WP BS 1140 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND C-PIT CASTING CRACKED STA 1140 LONGERON 35R. REMOVED AND REPLACED CASTING IAW DC-8 S RM 51-1-20D AND 51-1-10, M-59 ATTACHED. CORROSION CARD NR 5590-0551. NON-ROUTINE TASK CARD NR 91658. 2 L 7 4 4F 4A25 1996122600115 19961226 00115 WP 1996 12 26 CKSA96371 1 19961215 A 5320 3754041501 FITTING DOUG DC8 DC863F 302198F WP BS 300 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND CRACK IN LOWER END OF FITTING STA 300 STRINGER 37L. REMOVED AND REPLACED LOWER END F ITTING IAW DC-8 SRM 51-1-0 AND 51-1-20D. CORROSION CARD NR 5570-0551. NON-ROUTINE TASK CARD NR 89615. 2 L 7 4 4F 4A25 1996122600116 19961226 00116 WP 1996 12 26 CKSA96372 1 19961215 A 5320 3754041501 FITTING DOUG DC8 DC863F 302198F WP BS 320 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND CRACK IN LOWER END OF FITTING STA 320 STRINGER 27L. REMOVED AND REPLACED LOWER END F ITTING IAW DC8 SRM 51-1-0 AND 51-1-20D. PARTS FABRICATION FORM M-59 ATTACHED. CORROSION CARD NR 5570-0551. NON-ROUTIN E TASK CARD NR 89616. 2 L 7 4 4F 4A25 1996122600117 19961226 00117 WP 1996 12 26 CKSA96373 1 19961215 A 5313 2645716 STRINGER DOUG DC8 DC863F 302198F WP BS 1690 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND STRINGER TIE FITTING CRACKED AFT SIDE OF PRODUCTION SPLICE AT STA 1690, STRINGER 25R MARKED H52. REMOVED AND REPLACED STRINGER IAW DOUGLAS SRM 51-01-20. PART FABRICATION FORM M-59 ATTACHED. CORROSION CA RD NR 5600-0551. NON-ROUTINE TASK CARD NR 91474. 2 L 7 4 4F 4A25 1996122600118 19961226 00118 WP 1996 12 26 CKSA96374 1 19961215 A 5313 4711722 FITTING DOUG DC8 DC863F 302198F WP BS 8 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND RIGHT HAND SKIN STRINGER 29R FITTING CORRODED AT STA 8. REMOVED AND REPLACED STRINGE R 29R END FITTING IAW DC-8 SRM 51-1-0. PART FABRICATION FORM M-59 ATTACHED. CORROSION CARD NR 5570-0551. NON-ROUTINE TASK CARD NR 8893, LEVEL 2. 2 L 7 4 4F 4A25 1996122600119 19961226 00119 WP 1996 12 26 CKSA96375 1 19961215 A 5230 47732951 FITTING DOUG DC8 DC863F 302198F WP BS 158-260 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND CARGO DOOR SPOOL BACK-UP FITTINGS CORRODED STA 158 TO 260. REMOVED AND REPLACED BACK -UP FITTINGS IAW DC8 SRM 51-1-21 AND 51-3-1. C-1 CHECK WORK CARD NR 0049. NON-ROUTINE TASK CARD NR 89537, LEVEL 2. 2 L 7 4 4F 4A25 1996122600120 19961226 00120 WP 1996 12 26 CKSA96376 1 19961215 A 5313 2610340 LONGERON DOUG DC8 DC863F 302198F WP BS 1610-1660 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND LONGERON 24L CORRODED THROUGH SEVERAL AREA'S BETWEEN STA 1610 THROUGH STA 1660. REPA IRED LONGERON 24L BETWEEN STA 1610 THROUGH STA 1660 IAW DC-8 SRM 53-2-2. CORROSION CARD NR 5590-0551. NON-ROUTINE TASK CARD NR 91560, LEVEL 2. 2 L 7 4 4F 4A25 1996122600121 19961226 00121 WP 1996 12 26 CKSA96377 1 19961215 A 5320 WEB DOUG DC8 DC863F 302198F WP BS 1220-1230 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND FS 1220 TO 1230 TORQUE BOX UPPER WEB CRACKED RIGHT SIDE. REPAIRED TORQUE BOX UPPER W EB IAW AIA SKETCH NR AIA/E/2421/2421815C DRAWING, EA 96-348 REPORT 96 AIA-197 DATED 12-12-96. CORROSION CARD NR 5590-05 51. NON-ROUTINE TASK CARD NR 90790. 2 L 7 4 4F 4A25 1996122600122 19961226 00122 WP 1996 12 26 CKSA96378 1 19961215 A 5730 SKIN DOUG DC8 DC863F 302198F WP WS 11.25-182.5 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND RIGHT WING LEADING EDGE FROM XFS 11.25 TO XFS 182.5 HAVE CORROSION AROUND ATTACH FAST ENERS AS MARKED. INSTALLED DOUBLER REPAIR IAW AIA SKETCH NR 2425, EA 96-348 REPORT NR 96-197 DATED 12-12-96. CORROSION CARD NR 121R-0552. NON-ROUTINE TASK CARD NR 91475, LEVEL 2. 2 L 7 4 4F 4A25 1996122600123 19961226 00123 WP 1996 12 26 CKSA96379 1 19961215 A 5730 SKIN DOUG DC8 DC863F 302198F WP WS 697-841.5 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND RIGHT WING OUTBOARD LEADING EDGE CORROSION AT UPPER LEADING EDGE FASTENERS, APPROXIMA TELY XFS697 TO XFS 841.5. INSTALLED REPAIR IAW AIA ENGINEERING SKETCH NR 2420, EA 96-348 REPORT 96 AIA-197 DATED 12-12- 96. CORROSION CARD NR 116R-0551. NON-ROUTINE TASK CARD NR 88948, LEVEL 2. 2 L 7 4 4F 4A25 1996122600124 19961226 00124 WP 1996 12 26 CKSA96380 1 19961215 A 5540 TIP DOUG DC8 DC863F 302198F WP RUDDER DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND TOP OF RUDDER TIP HAS HOLE IN IT. REPAIRED HOLE AT THE TOP OF RUDDER TIP IAW AIA DRA WING NR AIA/E/2439 REV ORIG AND DC-8 SRM 51-21-1A, EA 96-348, REPORT 96 AIA-197 DATED 12-12-96. C-1 CHECK WORK CARD NR 4001 1OF1. NON-ROUTINE TASK CARD NR 88993. 2 L 7 4 4F 4A25 1996122600125 19961226 00125 WP 1996 12 26 CKSA96381 1 19961215 A 5542 SKIN DOUG DC8 DC863F 302198F WP RUDDER CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND RUDDER LEFT SIDE SURFACE CORROSION AROUND STATIC WICK AT STA ZR293 AND TRAILING EDGE AT STA ZR284 AND ZR330. REPAIRED STATIC WICKS ON RUDDER LEFT HAND IAW AIA DRAWING AIA/E/2433 AND DC-8 SRM 51-1-21, 51-1 -21A AND EA 96-348 REPORT NR 96 AIA 197 DATED 12-12-96. CORROSION CARD NR 6000-0551. NON-ROUTINE TASK CARD NR. 88997, LEVEL 2. 2 L 7 4 4F 4A25 1996122600126 19961226 00126 WP 1996 12 26 CKSA96382 1 19961215 A 5542 SKIN DOUG DC8 DC863F 302198F WP RUDDER CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND RUDDER 4TH STATIC WICK FROM TOP CORRODED RIGHT SIDE. REPAIRED STATIC WICKS AT ZR293 AND ZR284 IAW AIA DRAWING AIA/E/2434 REV ORIG AND DC-8 SRM 51-1-21, AND 51-1-21A, EA 96-348 REPORT NR 96 AIA 197 DATED 1 2-12-96. CORROSION CARD NR 6000-0551. NON-ROUTINE TASK CARD NR 89041, LEVEL 2. 2 L 7 4 4F 4A25 1996122600127 19961226 00127 WP 1996 12 26 CKSA96383 1 19961215 A 5400 APRON DOUG DC8 DC863F 302198F WP LT WING WORN A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND COWLING APRON WORN THROUGH ON RIGHT HAND SIDE MARKED. REPAIRED APRON, RIGHT HAND SID E IAW SKETCH AIA/E/2436, EA 96-348 REPORT NR 96 AIA 197. C-1 CHECK WORK CARD NR 1006. NON-ROUTINE TASK CARD NR 89228. 2 L 7 4 4F 4A25 1996122600128 19961226 00128 WP 1996 12 26 CKSA96384 1 19961215 A 5730 SKIN DOUG DC8 DC863F 302198F WP WS 100-141 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND LEFT HAND WING LEADING EDGE UPPER SURFACE STA XFS100 TO XFS141. CORROSION REMOVAL EX CEEDED LIMITS. REPAIRED LEADING EDGE UPPER SURFACE STA XFS100 TO XFS141 IAW AIA SKETCH AIA/E/2419 REFERENCE M-40 NR 908 11. CORROSION CARD NR 116L-0551. NON-ROUTINE TASK CARD NR 90770, LEVEL 2. 2 L 7 4 4F 4A25 1996122600129 19961226 00129 WP 1996 12 26 CKSA96385 1 19961215 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1000 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND FS 1000 LONGERON 36 FRAME FORWARD SIDE LOWER LEG CORRODED. REPAIRED FRAME AS PER SKE TCH AIA/E/2435, EA 96-348, REPORT 96 AIA-197 DATED 12-12-96. CORROSION CARD NR 5590-0551. NON-ROUTINE TASK CARD NR 908 85, LEVEL 2. 2 L 7 4 4F 4A25 1996122600130 19961226 00130 WP 1996 12 26 CKSA96386 1 19961215 A 5320 WEB DOUG DC8 DC863F 302198F WP FUSELAGE CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND FORWARD DOOR TRACK WEB HAS INNER GRANULAR CORROSION ABOVE STRINGER 31 TO 33R. REMOVE D CORROSION, FOUND OUT OF LIMITS. INSTALLED DOUBLER IAW AIA SKETCH AIA/E/2414 DATED 11-21-96 EA 96-348 AND REPORT 96 AI A 197 DATED 12-12-96. CORROSION CARD NR 5590-0551. NON-ROUTINE TASK CARD NR 90935, LEVEL 2. 2 L 7 4 4F 4A25 1996122600131 19961226 00131 WP 1996 12 26 CKSA96387 1 19961215 A 5320 ANGLE DOUG DC8 DC863F 302198F WP BS 280/340 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND L-ANGLE AT LONGERON 27L IN A CARGO BIN IS CORRODED BETWEEN STA 280 AND STA 340 MARKED . REMOVED CORROSION, OUT OF LIMITS, INSTALLED REPAIR IAW AIA SKETCH AIA/E/2437 AND EA 96-348 REPORT NR 96 AIA 197 DATED 12-12-96. CORROSION CARD NR 5570-0551. NON-ROUTINE TASK CARD NR 90955, LEVEL 2. 2 L 7 4 4F 4A25 1996122600132 19961226 00132 WP 1996 12 26 CKSA96388 1 19961215 A 5312 BULKHEAD DOUG DC8 DC863F 302198F WP BS 8 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND FORWARD BULKHEAD STA 8 IS CORRODED BOTH SIDES OF STRINGER TIE AT STRINGER 35R AND STR INGER TIE FITTING ALSO CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. INSTALLED DOUBLER IAW AIA SKETCH AIA/E/ 2427 EA 96-348 REPORT NR 96 AIA 197. CORROSION CARD NR 5570-0551. NON-ROUTINE TASK CARD NR 91038. 2 L 7 4 4F 4A25 1996122600133 19961226 00133 WP 1996 12 26 CKSA96389 1 19961215 A 5711 SPAR WEB DOUG DC8 DC863F 302198F WP WS 6 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND RIGHT WING AFT UPPER SPAR WEB CORRODED AT STA XRS -6.0. REMOVED PARTS AND CORROSION IAW DRAWING AIA/E/2424, EA 96-348 REPORT 96 AIA-197 DATED 12-12-96. CORROSION CARD NR 124R-0551. NON-ROUTINE TASK CARD NR 91051, LEVEL 2. 2 L 7 4 4F 4A25 1996122600134 19961226 00134 WP 1996 12 26 CKSA96390 1 19961215 A 5320 FITTING DOUG DC8 DC863F 302198F WP BS 1560 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND LONGERON END FITTING CORRODED STA 1560 LONGERON 33R. REMOVED AND REPLACED LONGERON E ND FITTING STA 1560 IAW AIA SKETCH NR AIA/E/2432, EA 96-348 REPORT NR 96-AIA 197 DATED 12-12-96. CORROSION CARD NR 5600 -0551. NON-ROUTINE TASK CARD NR 91568, LEVEL 2. 2 L 7 4 4F 4A25 1996122600135 19961226 00135 WP 1996 12 26 CKSA96391 1 19961215 A 5730 SKIN DOUG DC8 DC863F 302198F WP WS 250 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND UPPER LEFT WING SKIN CORRODED AT XRS 250 AT WING STRINGER NR 7 AND 8. INSTALLED DOU BLER IAW AIA/E/DRAWING 2426 AND EA 96-348 REPORT NR 96 AIA 197 DATED 12-12-96. CORROSION CARD NR 117L-0551. NON-ROUTIN E TASK CARD NR 91640, LEVEL 2. 2 L 7 4 4F 4A25 1996122600136 19961226 00136 WP 1996 12 26 CKSA96392 1 19961215 A 5320 SHEAR TIE DOUG DC8 DC863F 302198F WP BS 1040 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND FS 1040 LONGERON 34R THROUGH 35 LT FRAME SHEAR TIES CORRODED BEYOND ALLOWABLE LIMITS. REPAIRED FRAME SHEAR TIES FS 1040 IAW AIA DRAWING NR AIA/E/2431, EA 96-348 REPORT NR 96 AIA 197 DATED 12-12-96. CORRO SION CARD NR 5590-0551. NON-ROUTINE TASK CARD NR 91667, LEVEL 2. 2 L 7 4 4F 4A25 1996122600137 19961226 00137 WP 1996 12 26 CKSA96393 1 19961215 A 5313 LONGERON DOUG DC8 DC863F 302198F WP BS 240-300 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND LONGERON 36 CRACKED AND CORRODED STA 240 TO STA 300. REPAIRED LONGERON 36 AT STA 240 THROUGH STA 300 IAW AIA SKETCH AIA/E/2438 DATED 12-09-96 EA 96-348 REPORT NR 96 AIA 197 DATED 12-12-96. CORROSION CARD NR 5590-0551. NON-ROUTINE TASK CARD NR 91679, LEVEL 2. 2 L 7 4 4F 4A25 1996122600138 19961226 00138 WP 1996 12 26 CKSA96394 1 19961215 A 5730 SKIN DOUG DC8 DC863F 302198F WP WS 302-424 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND LEFT HAND WING LEADING EDGE UPPER SURFACE FROM STA XFS302 TO XFS424 CORROSION EXCEEDE D ALLOWABLE LIMITS. REFERENCE M-40 NR 88619. REPAIRED LEFT HAND WING LEADING EDGE UPPER SURFACE IAW AIA/EA SKETCH NR 2 418 AND DC-8 SRM REPAIR CHAPTER 57-2-1 FIGURE 38, EA 96-348 REPORT 96 AIA 197 DATED 12-12-96. CORROSION CARD NR 115L-05 51. NON-ROUTINE TASK CARD NR 91670, LEVEL 2. 2 L 7 4 4F 4A25 1996122600139 19961226 00139 WP 1996 12 26 CKSA96395 1 19961215 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 680 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND CORROSION AT FS 680 BETWEEN STRINGER 33 AND 32R. CUT OUT CORRODED AREA, INSTALLED RE PAIR IAW AIA/E/2430 AND EA 96-348 REPORT 96 AIA 197 DATED 12-12-96. CORROSION CARD NR 5590-0551. NON-ROUTINE TASK CARD NR 91681, LEVEL 2. 2 L 7 4 4F 4A25 1996122600140 19961226 00140 WP 1996 12 26 CKSA96396 1 19961215 A 5312 BLKHD STIFFENER DOUG DC8 DC863F 302198F WP AFT PRESS BLKHD CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND AFT PRESSURE BULKHEAD, WEB AND VERTICAL STIFFENER HAS INNER GRANULAR CORROSION AT RBL 22 AT FLOOR LINE. REPAIRED VERTICAL STIFENER IN ACCORDANCE WITH AIA DRAWING AIA/E/2443 AND REPORT NR 96 AIA 197 DATED 12-12-96 EA 96-348. CORROSION CARD NR 5600-0551. NON-ROUTINE TASK CARD NR 9175, LEVEL 2. 2 L 7 4 4F 4A25 1996122600141 19961226 00141 WP 1996 12 26 CKSA96397 1 19961215 A 5320 SHEAR TIE DOUG DC8 DC863F 302198F WP BS 1700 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTIO, FOUND SHEAR TIE AT STA 1700 BETWEEN STRINGER 22L AND STRINGER 23L IS CORRODED. REMOVED CORR ODED SHEAR TIE FABRICATED SHEAR TIE IAW SRM 51-1-4. INSTALLED NEW SHEAR TIE IAW SRM 51-1-20D AND SRM 51-1-21. CORROSIO N CARD NR 5590-0551. NON-ROUTINE TASK CARD NR 91970, LEVEL 2. 2 L 7 4 4F 4A25 1996122600142 19961226 00142 WP 1996 12 26 CKSA96398 1 19961215 A 5320 WEB DOUG DC8 DC863F 302198F WP BS 120 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND INNER GRANULAR CORROSION ON FORMER WEB, FORWARD SIDE, BETWEEN STRINGER 32 AND STRINGE R 33R AT STA 120 MARKED H36. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. INSTALLED DOUBLER REPAIR IAW DC8 SRM 53-2-0 FIGURE 2. PART FABRICATION FORM M-59 ATTACHED. CORROSION CARD NR 5570-0551. NON-ROUTINE TASK CARD NR 90940, LEVEL 2. 2 L 7 4 4F 4A25 1996122600143 19961226 00143 WP 1996 12 26 CKSA96399 1 19961215 A 5320 37558452 FITTING DOUG DC8 DC863F 302198F WP BS 1230 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND FS 1230 LONGERON 35R THROUGH LONGERON 36 BATHTUB FITTING CRACKED. INSTALLED FITTING AND INSTALLED HI-LOCK IAW SRM 51-1-20D. CORROSION CARD NR 5590-0551. NON-ROUTINE TASK CARD NR 90967. 2 L 7 4 4F 4A25 1996122600144 19961226 00144 WP 1996 12 26 CKSA96400 1 19961215 A 5320 5646955501 FITTING DOUG DC8 DC863F 302198F WP BS 1160 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND FS 1160 LONGERON 31 LT THROUGH LONGERON 32 LT BATHTUB FITTING CORRODED. REMOVED CORR OSION, TREATED, PRIMED IAW SRM DC8 51-1-8. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D. CORROSION CARD NR 5590-0551. N ON-ROUTINE TASK CARD NR 90856, LEVEL 2. 2 L 7 4 4F 4A25 1996122600145 19961226 00145 WP 1996 12 26 CKSA96401 1 19961215 A 5720 1419056 ANGLE DOUG DC8 DC863F 302198F WP BS 781.5 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND LOWER WING CENTER SECTION STA 781.5 RBL 64 HAS CRACKED SUPPORT ANGLE MARKED M6. REPL ACED SUPPORT ANGLE IAW DC8 SRM 53-2-0. CORROSION CARD NR 2000 TO 0551. NON-ROUTINE TASK CARD NR 90982. 2 L 7 4 4F 4A25 1996122600146 19961226 00146 WP 1996 12 26 CKSA96402 1 19961215 A 5347 2772660 SEAT TRACK DOUG DC8 DC863F 302198F WP BS 980-1140 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND FS 980 TO 1140 LONGERON -3RT SEAT TRACK AND MOUNT CORRODED MARKED L-177. REMOVED AND REPLACED SEAT TRACK AND REPAIRED IAW DC8 SRM 53-2-3 FIGURE 14. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. CORROSION CARD NR 5590-0551. NON-ROUTINE TASK CARD NR 90844, LEVEL 2. 2 L 7 4 4F 4A25 1996122600147 19961226 00147 WP 1996 12 26 CKSA96403 1 19961215 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1600 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING C-1 CHECK INSPECTION, FOUND LOWER AREA OF FRAME STA 1600 CORRODED FROM LONGERON 35L TO LONGERON 34R. REMOVED COR RODED AREA AND INSTALLED ZEE FRAME REPAIR IAW DC8 SRM 53-2-0 FIGURE 2. INSTALLED FASTENER IAW DC8 SRM 51-1-20D AND 51-1 -21 ALODINED AND PRIME IAW DC8 SRM 51-1-8. CORROSION CARD NR 5600-0551. NON-ROUTINE TASK CARD NR 91562, LEVEL 2. 2 L 7 4 4F 4A25 1996122600148 19961226 00148 EU 1996 12 26 RAIA961130 1 19961125 A 5313 S53671400203 STRINGER AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 119 STL - CORROSION ON STRINGER 17R FROM FRAME 29 TO 41. MAINTENANCE TREATED CORROSION PER ATR SRM 51-21-42. (M) 2 H 7 2 4T RT A53EU 1996122600149 19961226 00149 EU 1996 12 26 RAIA961131 1 19961125 A 5313 S53671400203 STRINGER AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - FOUND CORROSION ON STRINGER 18R FROM FRAME 27-39. MAINTENANCE TREATED CORROSION PER ATR SRM 51-21-42. (M) 2 H 7 2 4T RT A53EU 1996122600150 19961226 00150 EU 1996 12 26 RAIA961132 1 19961125 A 5313 S53671400203 STRINGER AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - FOUND CORROSION ON STRINGER FROM FRAME 27-39. MAINTENANCE TREATED CORROSION PER ATR SRM 51-21-42. (M) 2 H 7 2 4T RT A53EU 1996122600151 19961226 00151 EU 1996 12 26 RAIA961133 1 19961125 A 5313 S53671400203 STRINGER AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - FOUND CORROSION ON STRINGER 20R FROM FRAME 27-30. MAINTENANCE TREATED CORROSION PER ATR SRM 51-21-42. (M) 2 H 7 2 4T RT A53EU 1996122600152 19961226 00152 EU 1996 12 26 RAIA961134 1 19961125 A 5313 S53671400203 STRINGER AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - FOUND CORROSION ON STRINGER 21L AFT OF FRAME 32. MAINTENANCE TREATED CORROSION PER ATR SRM 51-21-42. (M) 2 H 7 2 4T RT A53EU 1996122600153 19961226 00153 EU 1996 12 26 RAIA961135 1 19961125 A 5313 S53671400203 STRINGER AEROSP ATR42 ATR42300 8680920 EU STR 21R FR 29 CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 18155 119 STL - FOUND CORROSION ON STRINGER 21R AT FRAME 29. MAINTENANCE TREATED CORROSION PER ATR SRM 51-21-42. (M) 2 H 7 2 4T RT A53EU 1996122600154 19961226 00154 EU 1996 12 26 RAIA961136 1 19961125 A 5313 S53671400203 STRINGER AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - FOUND CORROSION ON STRINGER 20L AT FRAME 32. MAINTENANCE TREATED CORROSION PER ATR SRM 51-21-42. (M) 2 H 7 2 4T RT A53EU 1996122600155 19961226 00155 EU 1996 12 26 RAIA961137 1 19961125 A 5313 S53671400203 STRINGER AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - FOUND CORROSION ON STRINGER 17L FROM FRAME 34-39. MAINTENANCE TREATED CORROSION PER ATR SRM 51-21-42. (M) 2 H 7 2 4T RT A53EU 1996122600156 19961226 00156 EU 1996 12 26 RAIA961138 1 19961125 A 5711 SPAR AEROSP ATR42 ATR42300 8680920 EU RT WING AFT DAMAGED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - FOUDN RIGHT WING AFT SPAR IS DAMAGED, OUTBOARD OF RIB 28. REPAIRED DAMAGED AREA OF AFT SPAR PER ATR DRAWING ATR25 512/96. (M) 2 H 7 2 4T RT A53EU 1996122600157 19961226 00157 EU 1996 12 26 RAIA961139 1 19961125 A 5311 S536672408228 FRAME AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - FOUND CORROSION ON FRAME 37 FROM STRINGER 15R TO 17R. MAINTENANCE REPLACED FRAME 37 PER SRM 51-25-01. (M) 2 H 7 2 4T RT A53EU 1996122600158 19961226 00158 EU 1996 12 26 RAIA961140 1 19961125 A 5311 S53672408228 FRAME AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - FOUND CORROSION ON FRAME 36 FROM STRINGER 15R TO 17R. MAINTENANCE TREATED CORROSION PER ATR SRM 51-21-42. (M) 2 H 7 2 4T RT A53EU 1996122600159 19961226 00159 EU 1996 12 26 RAIA961141 1 19961125 A 5315 S53672406200 FLOOR BEAM AEROSP ATR42 ATR42300 8680920 EU CABIN CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 119 STL - FOUND CORROSION ON FLOOR BEAM 40 BEAM 40 FROM STRINGER 17L TO 17R. MAINTENANCE REPLACED FLOOR BEAM 40. (M) 2 H 7 2 4T RT A53EU 1996122600160 19961226 00160 EU 1996 12 26 RAIA961142 1 19961125 A 5315 S53672406200 FLOOR BEAM AEROSP ATR42 ATR42300 8680920 EU CABIN CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - FOUND CORROSION ON FLOOR BEAM 39 AT STRINGER 17L TO 17R. MX REPLACED FLOOR BEAM 39. (M) 2 H 7 2 4T RT A53EU 1996122600161 19961226 00161 EU 1996 12 26 RAIA961143 1 19961126 A 5315 S53672406200 FLOOR BEAM AEROSP ATR42 ATR42300 8680920 EU CABIN CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 MX - FOUND CORROSION ON FLOOR BEAM 38 AT STRINGER 17L AND 17R. MX REPLACED NOTED BEAM. (M) 2 H 7 2 4T RT A53EU 1996122600162 19961226 00162 EU 1996 12 26 RAIA961144 1 19961126 A 5315 S53672400000 FLOOR BEAM AEROSP ATR42 ATR42300 8680920 EU CABIN CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 119 STL - FOUND CORROSION ON FLOOR BEAM 36 AT STRINGER 17L AND 17R. MX REPLACED BEAM 36 WITH NEW OEM UNIT. (M) 2 H 7 2 4T RT A53EU 1996122600163 19961226 00163 EU 1996 12 26 RAIA961145 1 19961126 A 5347 S53375001 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - FOUND CORROSION ON RIGHT OUTBOARD SEAT TRACK AT FLOOR BEAM 36. MX TREATED MINOR CORROSION PER ATR SRM 51-21-42. ( M) 2 H 7 2 4T RT A53EU 1996122600164 19961226 00164 EU 1996 12 26 RAIA961146 1 19961126 A 5347 S53375001 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - MAINTENANCE FOUND CORROSION ON RIGHT INBOARD SEAT TRACK AT FLOOR BEAM 35 AND 36. MAINTENANCE TREATED MINOR CORROS ION PER ATR SRM 51-21-47. (M) 2 H 7 2 4T RT A53EU 1996122600165 19961226 00165 EU 1996 12 26 RAIA961147 1 19961126 A 5347 S53375001 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - MAINTENANCE FOUND CORROSION ON LEFT INBOARD SEAT TRACK AT FLOOR BEAM 36. MAINTENANCE SPLICED IN NEW SEAT TRACK. ( M) 2 H 7 2 4T RT A53EU 1996122600166 19961226 00166 EU 1996 12 26 RAIA961148 1 19961126 A 5347 S53375001 SEAT TRACKS AEROSP ATR42 ATR42300 8680920 EU CABIN CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - FOUND CORROSION ON BOTH F/A SEAT TRACKS. MAINTENANCE REPAIRED ADN REPLACED SEAT TRACKS. (M) 2 H 7 2 4T RT A53EU 1996122600167 19961226 00167 EU 1996 12 26 RAIA961149 1 19961126 A 5320 S5367241000662 SUPPORT BEAM AEROSP ATR42 ATR42300 8680920 EU CARGO COMPT CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - MX FOUND CORROSION ON LOWER CARGO SUPPORT BEAM AT FRAME 41 ABOVE STRINGER 19R AND 21R. TREATED CORROSION IAW SRM 51-21-42. (M) 2 H 7 2 4T RT A53EU 1996122600168 19961226 00168 EU 1996 12 26 RAIA961150 1 19961126 A 5330 S536720206200 SKIN AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - MAINTENANCE FOUND CORROSION ON SERVICE DOOR TORQUE BOX SKIN FROM FRAME 36 TO 39. MAINTENANCE REPLACED SKIN. (M) 2 H 7 2 4T RT A53EU 1996122600169 19961226 00169 EU 1996 12 26 RAIA961158 1 19961126 A 5320 S53672408228 CLIPS AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - MAINTENANCE FOUND CORROSION ON FRAME 38 SKIN CLIPS BETWEEN STRINGER 16L AND 15R. MAINTENANCE REPLACED NOTED CLIPS . (M) 2 H 7 2 4T RT A53EU 1996122600170 19961226 00170 EU 1996 12 26 RAIA961159 1 19961126 A 5320 S53672408228 CLIPS AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - MAINTENANCE FOUND CORROSION ON FRAME 36 SKIN CLIPS BETWEEN STRINGER 18L AND 14R. MAINTENANCE REPLACED NOTED CLIPS . (M) 2 H 7 2 4T RT A53EU 1996122600171 19961226 00171 EU 1996 12 26 RAIA961160 1 19961126 A 5320 S53672408228 CLIPS AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - MAINTENANCE FOUND CORROSION ON FRAME 35 SKIN CLIPS BETWEEN STRINGER 15L AND 15R. MAINTENANCE REMOVED CORROSION FR OM FRAME 35 AND FOUND TO BE WITHIN LIMITS. (M) 2 H 7 2 4T RT A53EU 1996122600172 19961226 00172 EU 1996 12 26 RAIA961161 1 19961126 A 5320 S53672408228 CLIPS AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - MAINTENANCE FOUND CORROSION ON FRAME 34 SKIN CLIPS BETWEEN STRINGER 18L AND 19R. MAINTENANCE REPAIRED FRAME 34 BE TWEEN STRINGER 18L AND 19R. (M) 2 H 7 2 4T RT A53EU 1996122600173 19961226 00173 EU 1996 12 26 RAIA961162 1 19961126 A 5320 S53672408228 CLIPS AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - MAINTENANCE FOUND CORROSION ON FRAME 30 SKIN CLIPS BETWEEN STRINGER 20L AND 20R. MAINTENANCE REPLACED NOTED CLIPS . (M) 2 H 7 2 4T RT A53EU 1996122600174 19961226 00174 EU 1996 12 26 RAIA961163 1 19961126 A 5320 S53672408228 CLIPS AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - MAINTENANCE FOUND CORROSION ON FRAME 29 SKIN CLIPS BETWEEN STRINGER 19L AND 20R. MAINTENANCE REPLACED NOTED SKIN CLIPS. (M) 2 H 7 2 4T RT A53EU 1996122600175 19961226 00175 EU 1996 12 26 RAIA961164 1 19961126 A 5320 S53672408228 CLIPS AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - MAINTENANCE FOUND CORROSION ON FRAME 28 SKIN CLIPS BETWEEN STRINGER 21L AND 21R. MAINTENANCE REPLACED NOTED SKIN CLIPS. (M) 2 H 7 2 4T RT A53EU 1996122600176 19961226 00176 EU 1996 12 26 RAIA961165 1 19961126 A 5320 NTA46356 CLIPS AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - FOUND CORROSION ON STRINGER 21L AND 21R SKIN CLIPS AT FRAME 33. MAINTENANCE REPLACED NOTED CLIPS. (M) 2 H 7 2 4T RT A53EU 1996122600177 19961226 00177 EU 1996 12 26 RAIA961166 1 19961126 A 5313 NTA46356 STRINGERS AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - FOUND CORROSION ON STRINGER 21L AND 21R BETWEEN FRAME 16 AND 18. MAINTENANCE TREATED MINOR CORROSION PER ATR SRM 51-21-42. (M) 2 H 7 2 4T RT A53EU 1996122600178 19961226 00178 EU 1996 12 26 RAIA961167 1 19961126 A 5313 NTA46356 STRINGERS AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - MAINTENANCE FOUND CORROSION ON STRINGERS 21R AND 21L BETWEEN FRAMES 23 AND 25. MAINTENANCE TREATED MINOR CORROSIO N. (M) 2 H 7 2 4T RT A53EU 1996122600179 19961226 00179 EU 1996 12 26 RAIA961168 1 19961126 A 5313 NTA46356 STRINGER AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 119 STL - FOUND CORROSION ON STRINGER 21L FROM 40 TO 41. MAINTENANCE TREATED MINOR CORROSION. (M) 2 H 7 2 4T RT A53EU 1996122600180 19961226 00180 EU 1996 12 26 RAIA961169 1 19961126 A 5330 S53672408228 SKIN AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - FOUND CORROSION ON SKIN AND DOUBLER BETWEEN FRAMES 18 AND 19 AND STRINGERS 21L AND 20R. MAINTENANCE TREATED MINOR CORROSION. (M) 2 H 7 2 4T RT A53EU 1996122600181 19961226 00181 EU 1996 12 26 RAIA961170 1 19961126 A 5320 S5367131828001 SHEER WEB AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - FOUND CORROSION ON SHEER WEB FORWARD OF FRAME 36. MAINTENANCE TREATED MINOR CORROSION. (M) 2 H 7 2 4T RT A53EU 1996122600182 19961226 00182 EU 1996 12 26 RAIA961171 1 19961126 A 5320 S53671318001 SHEER WEB AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - FOUND CORROSION ON 4H SHEER WEB BETWEEN FRAME 40 AND 41. MAINTENANCE TREATED MINOR CORROSION. (M) 2 H 7 2 4T RT A53EU 1996122600183 19961226 00183 EU 1996 12 26 RAIA961172 1 19961126 A 5311 S5367131828001 FRAME AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - MAINTENANCE FOUND CORROSION ON 'Z' SHEER FRAME FROM FRAME 39 TO 40. MAINTENANCE TREATED MINOR CORROSION. (M) 2 H 7 2 4T RT A53EU 1996122600184 19961226 00184 EU 1996 12 26 RAIA961173 1 19961126 A 5320 S53671257206 INTERCOSTAL AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - FOUND CORROSION INTERCOSTAL AT STRINGER 21L FROM FRAME 40 TO 41. MAINTENANCE TREATED MINOR CORROSION. (M) 2 H 7 2 4T RT A53EU 1996122600185 19961226 00185 EU 1996 12 26 RAIA961174 1 19961126 A 5320 S53671257206 INTERCOSTALS AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - MAINTENANCE FOUND CORROSION ON RIGHT INTERCOSTAL FROM FRAME 35 TO 40 ABOVE STRINGER 17R. REPLACED INTERCOSTALS IA W SRM. (M) 2 H 7 2 4T RT A53EU 1996122600186 19961226 00186 EU 1996 12 26 RAIA961175 1 19961126 A 5320 S53671257206 INTERCOSTALS AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - FOUND CORROSION ON 4A INTERCOSTALS FROM FRAME 35 TO 40 STRINGER 17L. MAINTENANCE TREATED NOTED INTERCOSTALS. (M) 2 H 7 2 4T RT A53EU 1996122600187 19961226 00187 1996 12 26 USAABB96049 4 19961121 A 3431 285T05534 CONTROL PANEL BOEING 757 757225 1384959 NM COCKPIT FAILED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 19 609AU 18567 22205 SFO - FLT 45 - ON FINAL INTO SFO, CREW NOTED LOSS OF ILS INDICATION. APPROXIMATELY TEN MINUTES LATER, CREW NOTED AN ELE CTRICAL FIRE TYPE ODOR. CREW SECURED THE UTILITY BUSS, COMPLETED THE ELECTRICAL SMOKE REMOVAL PROCEDURE AND DECLARED AN EMERGENCY. FLIGHT LANDED AT SFO WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE ILS CONTROL PANEL. (M) 2 L 7 2 4F RT A2NM 1996122600188 19961226 00188 NM 1996 12 26 USAABB96050 1 19961114 A 3350 8731002511 LIGHT BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 601AU 22193 LAX - FOUND LOWER EXIT IDENTIFIER ON L1 DOOR INOPERATIVE. MAINTENANCE REPLACED THE IDENTIFIER. (M) 2 L 7 2 4F RT A2NM 1996122600189 19961226 00189 NM 1996 12 26 MZZA96125 1 19961023 A 5313 STRINGER BOEING 727 727224 1384076 NM BS 950 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69742 22251 TNN - DURING 1/4D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT AT THE F OLLOWING AREAS; BS 950 BULKHEAD LOWER CHORD BETWEEN STRINGER 29R AND STRINGER 28R, STRINGER 29R KEEL BEAM OUTBOARD FLANG E AT BS 950A. THE CORRODED AREAS WAS CLEANED UP AND REPAIRED PER EC/RA 5310-03352. REF, HANGAR NON ROUTINE REPAIR ITEM CARDS NR 804010 AND 804032 (SEQ NR 01115 AND 01136). (M) 2 L 7 3 4F A3WE 1996122600190 19961226 00190 NM 1996 12 26 MZZA96124 1 19961023 A 5311 FRAME BOEING 727 727224 1384076 NM BS 950 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69742 22251 TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT BS 950F FRAME LOWER CHORD FLANGE BETWEEN STRINGER 29L AND STRINGER 28L. THE CORRODED FRAME WAS TRIMMED OUT AND REPAIRED PER B7 27 SRM 53-10-4 FIGURE 11. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 804037 (SEQ NR 01141). (M) 2 L 7 3 4F A3WE 1996122600191 19961226 00191 NM 1996 12 26 MZZA96123 1 19961023 A 5311 FRAME BOEING 727 727224 1384076 NM BS 950 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69742 22251 TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT BS 950F FRAME LOWER CHORD FLANGE BETWEEN STRINGER 27R AND STRINGER 28R. THE CORRODED FRAME LOWER CHORD WAS TRIMMED AND REPAIRE D PER B727 SRM 53-10-4 FIGURE 11. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 804041 (SEQ NR 01145). (M) 2 L 7 3 4F A3WE 1996122600192 19961226 00192 NM 1996 12 26 MZZA96122 1 19961023 A 5311 FRAME BOEING 727 727224 1384076 NM BS 970 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69742 22251 TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT BS 970 FRAME LOWER CHORD FLANGE BETWEEN STRINGER 27R AND STRINGER 28R. THE CORRODED FRAME LOWER CHORD WAS TRIMMED OUT AND REPA IRED PER B727 SRM 53-10-4 FIGURE 11. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 804047 (SEQ NR 01151) (M) 2 L 7 3 4F A3WE 1996122600193 19961226 00193 NM 1996 12 26 MZZA96121 1 19961023 A 5311 FRAME BOEING 727 727224 1384076 NM BS 720 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69742 22251 TNN - DURING 1/4D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FUOND ON FORWARD CARGO COMPARTMENT BS 7 20C FRAME LOWER CHORD FLANGE BETWEEN STRINGER 25R AND STRINGER 26R. THE CORRODED FRAME WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-3 FIGURE 1. REF HANGAR NON ROUTINE REPAIR ITEM CARD NR 816010 (SEQ NR 01165). (M) 2 L 7 3 4F A3WE 1996122600194 19961226 00194 NM 1996 12 26 MZZA96120 1 19961024 A 5347 SEAT TRACK BOEING 727 727224 1384076 NM BS 1030-1070 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69742 22251 TNN - DURING 1/4D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON PASSENGER CABIN SEAT TRACK FLA NGE AT RBL 45.5 BETWEEN BS 1040 AND BS 1070. THE CORRODED SEAT TRACK FROM BS 1030 TO BS 1070 WAS TRIMMED OUT AND REPAIR ED PER B727 SRM 53-10-3 FIGURE 7. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 814858 (SEQ NR 01186). 2 L 7 3 4F A3WE 1996122600195 19961226 00195 NM 1996 12 26 MZZA96118 1 19961025 A 5311 FRAME BOEING 727 727224 1384076 NM BS 1148 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69742 22251 TNN - DURING 1/4D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT BS 1148 FRAME LOWER CHORD FLANGE BETWEEN STRINGER 29L AND STRINGER 30. THE CORRODED FRAME WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-10-4 FIGURE 11. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 814900. (SEQ NR 01228). 2 L 7 3 4F A3WE 1996122600196 19961226 00196 NM 1996 12 26 MZZA96117 1 19961025 A 5311 FRAME BOEING 727 727224 1384076 NM BS 1148 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69742 22251 TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARG COMPARTMENT BS 1148 FRAME LOWER CHORD FLANGE BETWEEN STRINGER 29L AND STRINGER 28L. THE CORRODED FRAME WAS TRIMMED OUT AND REPAIRED PER B72 7 SRM 53-10-4 FIGURE 11. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 814901. (SEQ NR 01229). (M) 2 L 7 3 4F A3WE 1996122600197 19961226 00197 NM 1996 12 26 MZZA96116 1 19961028 A 5311 FRAME BOEING 727 727224 1384076 NM BS 480 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69742 22251 TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON FORWARD CARGO COMPARTMENT BS 480 FRAME LOWER CHORD FLANGE BETWEEN STRINGER 28R AND STRINGER 27L. THE CORRODED FRAME LOWER CHORD FROM STRINGER 28L TO STRINGER 28R WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-3 FIGURE 1. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 8 16024 (SEQ NR 01249) (M) 2 L 7 3 4F A3WE 1996122600198 19961226 00198 NM 1996 12 26 MZZA96115 1 19961028 A 5311 FRAME BOEING 727 727224 1384076 NM BS 1130 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69742 22251 TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT BS 1130 FRAME LOWER CHORD FLANGE BETWEEN STRINGER 27R AND STRINGER 28R. THE CORRODED FRAME WAS TRIMMED OUT AND REPAIRED PER B7 27 SRM 53-10-4 FIGURE 11. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 814923 (SEQ NR 01253). (M) 2 L 7 3 4F A3WE 1996122600199 19961226 00199 NM 1996 12 26 MZZA96114 1 19961028 A 5311 FRAME BOEING 727 727224 1384076 NM BS 1130 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69742 22251 TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT BS 1130 FRAME LOWER CHORD FLANGE BETWEEN STRINGER 28R AND STRINGER 29R. THE CORRODED FRAME WAS TRIMMED OUT AND REPAIRED PER B7 27 SRM 53-10-4 FIGURE 11. REF, HANGAR NON ROUTINE REPAIR ITME CARD NR 814924. (SEQ NR 01254) (M) 2 L 7 3 4F A3WE 1996122600200 19961226 00200 NM 1996 12 26 MZZA96113 1 19961028 A 5311 FRAME BOEING 727 727224 1384076 NM BS 1130 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69742 22251 TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT BS 1130 FRAME LOWER CHORD FLANGE BETWEEN STRINGER 29R AND STRINGER 30. THE CORRODED FRAME WAS TRIMMED OUT AND REPAIRED PER B72 7 SRM 53-10-4 FIGURE 11. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 814925. (SEQ NR 01255) (M) 2 L 7 3 4F A3WE 1996122600201 19961226 00201 NM 1996 12 26 MZZA96112 1 19961028 A 5311 FRAME BOEING 727 727224 1384076 NM BS 1130 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69742 22251 TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT BS 1130 FRAME LOWER CHORD FLANGE BETWEEN STRINGER 29L AND STRINGER 30. THE CORRODED FRAME WAS TRIMMED OUT AND REPAIRED PER B72 7 SRM 53-10-4 FIGURE 11. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 814926. (SEQ NR 01256) (M). 2 L 7 3 4F A3WE 1996122600202 19961226 00202 NM 1996 12 26 MZZA96111 1 19961023 A 5311 FRAME BOEING 727 727224 1384076 NM BS 1130 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69742 22251 TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT BS 1130 FRAME LOWER CHORD FLANGE BETWEEN STRINGER 29L AND STRINGER 28L. THE CORRODED FRAME WAS TRIMMED OUT AND REPAIRED PER B7 27 SRM 53-10-4 FIGURE 11. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 814927. (SEQ NR 01257). (M) 2 L 7 3 4F A3WE 1996122600203 19961226 00203 NM 1996 12 26 MZZA96109 1 19961021 A 3350 SIGN COVER BOEING 727 727224 1384076 NM CABIN BROKEN A MZZA K NONE L NO TEST IN INSP/MAINT 1 WP 13 69742 22251 TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, BROKEN COVER WAS FOUND ON FORWARD GALLEY AREA 'EXIT' SIGN C OVER. THE DAMAGED 'EXIT' SIGN ASSEMBLY WAS REMOVED AND REPLACED WITH P/N BR9279-103 PER B727 MM 33-50-11 AND OPERATIONA L CHECK FOUND SATISFACTORY. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 804675 (SEQ NR 02205) (M) 2 L 7 3 4F A3WE 1996122600204 19961226 00204 NM 1996 12 26 MZZA96108 1 19961021 A 3350 SIGN COVER BOEING 727 727224 1384076 NM CABIN BROKEN A MZZA K NONE L NO TEST IN INSP/MAINT 1 WP 13 69742 22251 TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, BROKEN COVER WAS FOUND ON R1 GALLEY SERVICE DOOR 'EXIT' SIG N COVER. THE DAMAGED 'EXIT' SIGN ASSEMBLY WAS REMOVED AND REPLACED WITH P/N BR9279-106 PER B727 MM 33-50-11 AND OPERATI ONAL CHECK FOUND SATISFACTORY. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 804676 (SEQ NR 02206) (M) 2 L 7 3 4F A3WE 1996122600205 19961226 00205 NM 1996 12 26 MZZA96107 1 19961021 A 3350 SIGN COVER BOEING 727 727224 1384076 NM CABIN BROKEN A MZZA K NONE L NO TEST IN INSP/MAINT 1 WP 13 69742 22251 TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, BROKEN COVER WAS FOUND ON L2 SERVICE DOOR 'EXIT' SIGN COVER . THE DAMAGED 'EXIT' SIGN ASSEMBLY WAS REMOVED AND REPLACED WITH P/N BR9279-105 PER B727 MM 33-50-11 AND OPERATIONAL CH ECK FOUND SATISFACTORY. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 804677 (SEQ NR 02207) (M) 2 L 7 3 4F A3WE 1996122600206 19961226 00206 NM 1996 12 26 MZZA96106 1 19961021 A 3350 S106 BATTERIES BOEING 727 727224 1384076 NM CABIN DISCHARGED A MZZA K NONE L NO TEST IN INSP/MAINT 1 WP 13 69742 22251 TNN - DURNIG 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, AFT AIRSTAIR CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPER ATIVE. THE BATTERIES, P/N S106, WERE REMOVED AND REPLACED PER B727 MM 33-50-0 AND OPERATIONAL CHECK FOUND SATISFACTORY. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 803974. (SEQ NR 02253) (M) 2 L 7 3 4F A3WE 1996122600207 19961226 00207 NM 1996 12 26 MZZA96104 1 19961027 A 5347 SEAT TRACK BOEING 727 727224 1384076 NM BS 1030-1070 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69742 22251 TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON PASSENGER CABIN SEAT TRACK AT RBL 24.75 BETWEEN BS 1030 AND BS 1070. THE CORRODED SEAT TRACK FROM BS 1030 TO BS 1070 WAS TRIMMED OUT AND REPAIRED PE R B727 SRM 53-10-5 FIGURE 7. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 804784 (SEQ NR 02334) (M) 2 L 7 3 4F A3WE 1996122600208 19961226 00208 SO 1996 12 26 C2XA96IA288 1 19961119 A 5320 12027929001 BUTT STRAP EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 58733 120197 IAH - DURING A ROUTINE INSPECTION, THE AFT CABIN RIGHT FLOOR BEAM BUTT STRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES NR 33-39. MAINTENANCE REMOVED AND REPLACED THE DAMAGED BUTT STRAP AND THE AIRCRAFT WAS LATER APPROVED FOR RETURN TO SERVIC E. (M) 2 L 7 2 4T RT A31SO 1996122600209 19961226 00209 SO 1996 12 26 C2XA96IA289 1 19961119 A 5320 12004149001 CROSSBEAM EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 58733 120197 IAH - DURING A ROUTINE INSPECTION, FRAME NR 36 FLOOR CROSSBEAM WAS FOUND TO BE CORRODED ON RIGHT SIDE OF CABIN. MAINTEN ANCE REMOVED AND REPLACED THE DAMAGED CROSSBEAM AND THE AIRCRAFT WAS LATER APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996122600210 19961226 00210 SO 1996 12 26 C2XA96IA290 1 19961119 A 5320 12004149002 CROSSBEAM EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 58733 120197 IAH - DURING A ROUTINE INSPECTION, FRAME NR 36 FLOOR CROSSBEAM WAS FOUND TO BE CORRODED ON LEFT SIDE OF CABIN. MAINTENA NCE REMOVED AND REPLACED THE DAMAGED CROSSBEAM AND THE AIRCRFT WAS LATER APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996122600211 19961226 00211 SO 1996 12 26 C2XA96IA291 1 19961119 A 5320 12004449001 CROSSBEAM EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 58733 120197 IAH - DURING A ROUTINE INSPECTION, FRAME NR 38 FLORO CROSSBEAM WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMO VED AND REPLACED THE DAMAGED CROSSBEAM AND THE AIRCRAFT WAS LATER APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1996122600212 19961226 00212 SO 1996 12 26 C2XA96IA292 1 19961202 A 5713 12016085002 STRINGER EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 47722 120166 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING STRINGER NR 10 WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE AFFECT ED PORTION OF STRINGER AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE STRINGER REPAIR WAS ACCOMPLISHED IAW CO NTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION NR EC5710-01010. (M) 2 L 7 2 4T RT A31SO 1996122600213 19961226 00213 NE 1996 12 26 96ZZZM1567 2 19961025 A 7250 311838301 BLADE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE POWER SECTION CRACKED A UUAA K NONE O OTHER IN INSP/MAINT 1 SO 17 45AR 2715 UE12 114122 FOUND POWER TURBINE BLADE HALF MISSING. 2 L 7 2 4T 4 T RT A24CE E26NE 1996122600214 19961226 00214 NM 1996 12 26 GAIA9633 1 19961120 A 3350 1000479 LIGHT BOEING 727 727223 1384074 NM BS 328 INTERMITTENT A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 6809 19484 DURING 'PS' CHECK INSPECTION, FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT TESTED INTERMITTENTLY. MAINTENANCE FOUND BATTERY PACK DISCHARGED. REPLACED EXIT LIGHT ASSEMBLY. CHECKED GOOD. (M) 2 L 7 3 4F A3WE 1996122600215 19961226 00215 WP 1996 12 26 TWAA9613504 1 19961023 A 5330 SKIN DOUG DC9 DC951 3022051 WP FWD FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 408EA 47693 STL - DURING OP-15, FOUND NOSE SKIN CRACKED ABOVE STRAKE, RIGHT SIDE. REPAIRED PER SRM 53-04, FIGURE 38, AND ARA 10575. AIRCRAFT TOTAL TIME: 46,296 HOURS; 43,121 CYCLES. (X) 2 L 7 2 4F RT A6WE 1996122600216 19961226 00216 WP 1996 12 26 TWAA9613505 1 19961031 A 5347 SEAT TRACK DOUG DC9 DC951 3022051 WP CABIN CORRODED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 408EA 47693 STL - DURING OP-15, FOUND CORROSION ON INBOARD RT SEAT TRACK, FORWARD OF AFT END. SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05. AIRCRAFT TOTAL TIME: 46,296 HOURS; 43,121 CYCLES. 2 L 7 2 4F RT A6WE 1996122600217 19961226 00217 WP 1996 12 26 TWAA9613503 1 19961020 A 5330 SKIN DOUG DC9 DC951 3022051 WP FWD FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 408EA 47693 STL - DURING OP-15, FOUND FUSELAGE NOSE SKIN CRACKED ABOVE STRAKES, LEFT SIDE. INSTALLED REPAIR DOUBLER PER ARA 10574. AIRCRAFT TOTAL TIME: 46,296 HOURS; 43,121 CYCLES. (X) 2 L 7 2 4F RT A6WE 1996122600218 19961226 00218 WP 1996 12 26 TWAA9613502 1 19961106 A 3350 58222 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN MALFUNCTIONED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 406EA 47686 STL - FLT 567 - DURING PREFLIGHT, EGRESS LIGHTS WERE SLOW TO ILLUMINATE. FOUND POWER SUPPLY, MFG PN 5822-2, WEAK. REPL ACED POWER SUPPLY. EGRESS LIGHT OPERATION CHECKED NORMAL. CHECK C - 9-17-95 - STL. (X) 2 L 7 2 4F RT A6WE 1996122600219 19961226 00219 NM 1996 12 26 TWAA9613501 1 19961105 A 3230 69153643 INNER ROD BOEING 727 727231 1384079 NM RT MLG BENT A TWAA O OTHER J WARNING INDICATION AP APPROACH 1 CE 05 54342 21629 ABQ - FLT 287 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, RIGHT MAIN LANDING GEAR DID NOT SHOW DOWN AND LOCKED. C YCLED LANDING GEAR. FOUND SIDE BRACE DOWNLOCK SPRING BUNGEE INNER ROD, MFG PN 69-15364-3, BENT. REPLACED DOWNLOCK BUNG EE ASSEMBLY. LANDING GEAR OPERATION AND INDICATION CHECKED NORMAL. CHECK C-2 - 3-15-96 - JFK. (X) 2 L 7 3 4F A3WE 1996122600220 19961226 00220 WP 1996 12 26 TWAA9613702 1 19961110 A 3260 H146 DOWNLOCK SWITCH DOUG DC9 DC931 3022065 WP RT MLG MALFUNCTIONED A TWAA O OTHER P NO WARNING INDICATION AP APPROACH 1 CE 05 979Z 47343 STL - FLT 631 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, RIGHT MAIN LANDING GEAR DID NOT INDICATE DOWN AND LOCKED . CYCLED LANDING GEAR. FOUND RIGHT MAIN LANDING GEAR DOWNLOCK SWITCH, MFG PN H14-6, MALFUNCTIONING. REPLACED RIGHT MAI N LANDING GEAR DOWNLOCK SWITCH. LANDING GEAR INDICATION SYSTEM OPERATIONS CHECKED NORMAL. CHECK C - 10-14-96 - STL. ( X) 2 L 7 2 4F A6WE 1996122600221 19961226 00221 NM 1996 12 26 TWAA9613701 1 19961107 A 8012 CONNECTOR BOEING 727 727231 1384079 NM NR 1 ENGINE LOOSE A TWAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 CE 05 54335 20462 STL - FLT 375 - DURING CRUISE, SHUT DOWN NR 1 ENGINE, SN 1541, DUE TO START VALVE LIGHT ILLUMINATION. FOUND DISCONNECT PLUG D374J, MFG PN CA3100KR28-11S727A, CONTAMINATED WITH MOISTURE. REPLACED THE D374J DISCONNECT PLUG. ENGINE START VA LVE AND ENGINE OPERATION CHECKED NORMAL. ENGINE TOTAL TIME: 36,913 HOURS; 23,850 CYCLES. CHECK C-3 - 8-9-96 - JFK. ( X) 2 L 7 3 4F A3WE 1996122600222 19961226 00222 NE 1996 12 26 TWAA9613801 2 19961109 A 7200 ENGINE BOEING 727 727231 1384079 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE FAILED A TWAA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CE 05 84355 21987 MIA - FLT 149 - DURING CLIMB, SHUT DOWN NR 3 ENGINE, SN 3940, DUE TO OIL LOSS. FOUND INTERNAL OIL LEAK WITH TURBINE AND TAILPIPE OIL COVERED. CHANGED ENGINE. ENGINE OPERATION THEN CHECKED NORMAL. ENGINE TOTAL TIME: 59,561 HOURS; 40,218 CYCLES. CHECK C-1 - 2-13-96 - JFK. (X) 2 L 7 3 4F 4 F A3WE E2EA 1996122600223 19961226 00223 WP 1996 12 26 TWAA9613508 1 19961102 A 5330 SKIN DOUG DC9 DC951 3022051 WP SERV DOORWAY TORN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 408EA 47693 STL - DURING OP-15, FOUND SKIN TORN AT FORWARD LOWER CORNER OF SERVICE DOOR OPENING. REPAIRED PER ARA 10588 AND SRO 953 0172. AIRCRAFT TOTAL TIME: 46,296 HOURS; 43,121 CYCLES. (X) 2 L 7 2 4F RT A6WE 1996122600224 19961226 00224 WP 1996 12 26 TWAA9613606 1 19961101 A 5315 FLOOR BEAM DOUG DC9 DC951 3022051 WP BS 370 WORN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 408EA 47693 STL - DURING OP-15, FOUND WORN SPOT ON FLOOR BEAM APPROXIMATELY FOUR INCHES LEFT OF CENTERLINE, STATION 370. REPAIRED F LOOR BEAM PER SRM 53-05, PAGE 31, FIGURE 20A. (M) 2 L 7 2 4F RT A6WE 1996122600225 19961226 00225 WP 1996 12 26 TWAA9613507 1 19961101 A 5312 BULKHEAD DOUG DC9 DC951 3022051 WP BS 1136 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 408EA 47693 STL - DURING OP-15, FOUND A FOUR INCH CRACK AT BOTTOM OUTBOARD CORNER OF FORWARD BULKHEAD OF RIGHT LAV, STA 1136. REPAI RED PER SRM 53-03, FIGURE 21, SHEETS 1 AND 2. AIRCRAFT TOTAL TIME: 46,296 HOURS; 43,121 CYCLES. (X) 2 L 7 2 4F RT A6WE 1996122600226 19961226 00226 NM 1996 12 26 TWAA9613601 1 19961107 A 7930 A008032 SWITCH BOEING 727 727231 1384079 NM NR 1 ENGINE MALFUNCTIONED A TWAA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 CE 05 54335 20462 STL - FLT 422 - DURING CLIMB, SHUT DOWN NR 1 ENGINE, SN 1541, DUE TO OIL FILTER BYPASS LIGHT ILLUMINATION. FOUND OIL FI LTER BYPASS LIGHT SWITCH MALFUNCTIONING. REPLACED BYPASS LIGHT SWITCH, MFG PN A00803-2. ENGINE OPERATION AND INDICATION OK. ENGINE TOTAL TIME: 36,904 HOURS; 23,844 CYCLES. CHECK C-3 - 8-9-96 - JFK. (X) 2 L 7 3 4F A3WE 1996122600227 19961226 00227 EU 1996 12 26 USAA960738 1 19961113 A 5312 BULKHEAD ANGLE FOKKER F28 F28MK0100 4990807 EU AFT PRESS BLKHD CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 861US 15734 11297 PIT - DURNIG Q-1 CHECK, FOUND TWO 3 INCH CRACKS IN ADDITION TWO NESTED ANGLES CRACKED .75 AFT CENTER PRESSURE BULKHEAD, CRACKS FOUND SUBJECT ANGLE ONE AT STRINGER NR 11 LHS AND ONE AT STRINGER NR 62RHS. INSTALLED DOUBLER REPAIR PER USAIR E A NR 33790. (M) 2 L 7 2 4F RT 1996122600228 19961226 00228 NM 1996 12 26 AWXA9600652 1 19961105 A 2720 65C370527 RUDDER PCU BOEING 737 7372U9 1384498 NM RUDDER CONTROL MALFUNCTIONED A A AWXA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 WP 28 149AW 1123A 22575 LAS - FLT 2606 - WHILE AT CRUISE AT 35,000 FT, 72M W/AUTOPILOT ENGAGED, THE A/C EXPERIENCED A SHARP LEFT YAW. DISENGAGE D THE AUTOPILOT. A/C DIVERTED TO LAS. INSPECTED A/C, FOUND TO BE SAFE FOR MX. FERRY TO PHX. R/R'D THE YAW DAMPER COU PLER, AUTOPILOT ACCESSORY UNIT, AND THE P5-3 CONTROL MODULE. THE P5-3 WAS CHANGED FOR THE EARLIER FINDINGS OF UNCOMMAND ED RUDDER INPUT, THAT BEING WHEN THE B-CHANNEL FLT CONTROL SW GUARD WAS RESET IT TRIPPED THE AUTOPILOT AND YAW DAMPER OF F. REPLACED RUDDER PWR CONTROL UNIT (PCU), PERFORMED ADJ TEST W/NO PROBLEMS. YAW TEST DAMPER TEST PERFORMED. THE PCU HAS BEEN PLACED UNDER QUAR FOR INVESTIGATION BY THE NTSB. (M) 2 L 7 2 4F RT A16WE 1996122600229 19961226 00229 NM 1996 12 26 GAIA9634 1 19961121 A 2611 SMOKE DET BOEING 727 727251 138408H NM CARGO COMPT MALFUNCTIONED A GAIA K NONE N FALSE WARNING CR CRUISE 1 SW 07 279US 21158 FLT 711 - SJC-TOL - DURING CRUISE, IN LAST HOUR OF FLT CARGO COMPARTMENT SMOKE DETECTOR ILLUMINATED. VISUALL VERIFIED N O SMOKE PRESENT IN CARGO. AGAIN DURING DESCENT, SMOKE DETECTOR ILLUMINATED. AGAIN VERIFIED VISUALL NO SMOKE. MX COULD NOT DUPLICATE INDICATION, SMOKE DETECTOR SYSTEM CHECKED PER MM 26-31. AIRCRAFT RELEASED FOR FLIGHT. MX DID NOTE INDIC ATIONS OF HIGH HUMIDITY IN CARGO ON AIRCRAFT ARRIVAL. SUBMITTER STATES, IT IS SUSPECTED THAT THE FALSE SMOKE INDICATION WS CAUSED BY FOGGING OF THE INDICATOR LENSES. (M) 2 L 7 3 4F A3WE 1996122600230 19961226 00230 SO 1996 12 26 96ZZZM1568 1 19961014 A 5610 1159SCB31024 WINDSHIELD GULSTM G1159 GIV 3980115 SO RT COCKPIT FAILED A YNOA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 11 917W 1158 EN ROUTE FROM NEWARK, DURING CRUISE AT FLT LEVEL 410, A LOUD REPORT WAS RECEIVED FROM THE FRONT RT WINDSHIELD. ELECTRIC AL ARCHING AND NUMEROURS CRACKS IN THE HEATED OUTER PLY WERE OBSERVED. THE A/C DIVERTED TO SAVANNAH. THE HEATING SYSTE M COMPONENTS WERE OP TESTED AND THE HEATER CONTROL UNIT AND THE EFFECTED WINDSHIELD WAS REPLACED. REPAIRS WERE FACILITA TED RETURNING THE AIRCRAFT TO SERVICE. REQUIRED INSPECTION WAS CONDUCTED. THE REPLACEMENT WINDSHIELD HAS INCORPORATED MODIFICATIONS WHICH SHOULD RESOLVE FUTURE OCCURRENCES OF THIS NATURE. 2 L 7 2 4F RT A12EA 1996122600231 19961226 00231 NM 1996 12 26 EIAA9687 1 19961122 A 2611 30231R7B SMOKE DETECTOR BOEING 747 747132 1384882 NM CARGO INOP A EIAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 481EV 85210 19896 LAX - ON CLIMB-OUT LWR AFT CARGO FIRE WARNING LIGHT CAME ON TWICE. NR 1 FIRE BOTTLE DID NOT DISCHARGE. NR 2 FIRE BOTTL E DISCHARGED NORMALLY. SMELL OF ELECT BURNING IN THE COCKPIT. RETURNED TO LAX. FOUND BOTH NR 1 AND NR 2 FIRE BOTTLES DISCHARGED. NR 1 BOTTLE AFT DISCHARGE PRESS SW INSTALLED IN NR 1 FWD POSITION. REPOSITIONED TO THE CORRECT POSITIONS. NO EVIDENCE OF FIRE SMOKE OR CHARRED WIRING FOUND. 4 HOUR OPS CHECK WAS OK. FOUND NR 3 AFT SMOKE DETECT LIGHT CAME ON AND STAYED ON DURING OPS CHECK. REPLACED NR 3 AFT SMOKE DETECTOR. (M) 2 L 7 4 4F A20WE 1996122600232 19961226 00232 EU 1996 12 26 REXA96071 1 19961108 A 3230 5EN16N95 SWITCH BAG JETSTM JETSTM3101 1500215 EU NLG OUT OF ADJUST A REXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 302PX 661 AFTER TAKEOFF, GEAR WOULDN'T RETRACT. ADJUSTED NLG OLEO MICROSWITCH. PERFORMED GEAR SWING 3 TIMES. A/C OK FOR SERVICE . (M) 2 L 7 2 4T RT A21EU 1996122600233 19961226 00233 EU 1996 12 26 REXA96070 1 19961104 A 3233 6158D ACTUATOR BAG JETSTM JETSTM3101 1500215 EU NLG FAILED A REXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 317PX LK8608336 688 NOSE GEAR LANDING INTRANSIT LIGHT WITH GEAR UP SELECTED. CLEANED UPLOCK MICROSWITCH. REMOVED AND REPLACED NLG RETRACT ACTUATOR. PERFORMED GEAR SWINGS. ALL SYSTEMS CHECK GOOD. AIRCRAFT OK FOR CONTINUED SERVICE. (M) 2 L 7 2 4T RT A21EU 1996122600234 19961226 00234 NE 1996 12 26 ORJA96107 2 19961119 A 7261 OIL FILTER DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE LT ENGINE CLOGGED A ORJA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 11 834RA 53124 DURING TAKEOFF ROLL LT OIL STRAINER CLOG WARN CAME ON. DISCONTINUED TAKEOFF. RETURNED TO GATE. REPLACED NR 1 ENGINE M AIN OIL FILTER. OPS CHECKED PER 72-00-00. OPS CHECKED NORMAL, NO LEAKS. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 1996122600235 19961226 00235 WP 1996 12 26 ORJA96104 1 19961122 A 3350 41B004AD073 BATTERY DOUG DC9 DC983 3022083 WP EMPENNAGE DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 833RA 53045 EMPENNAGE EMERGENCY LIGHTS INOP. REPLACED BATTERY PACKS, EMERGENCY LIGHTS OPS NORMAL. (M) 2 L 7 2 4F RT A6WE 1996122600236 19961226 00236 EU 1996 12 26 M3HA96035 1 19961125 A 3350 3011151 BATTERY AEROSP ATR42 ATR42300 8680920 EU CABIN BROKEN A M3HA K NONE L NO TEST IN INSP/MAINT 1 WP 13 4210G 10469 149 HNL - DURING DAILY INSPECTION, TAB ON EMERGENCY BATTERY PACK 3WL WAS FOUND TO BE BROKEN. REMOVED AND INSTALLED SERVICEA BLE EMERGENCY BATTERY PACK. (M) 2 H 7 2 4T RT A53EU 1996122600237 19961226 00237 EU 1996 12 26 M3HA96033A 1 19961125 A 3320 8ED00558800 POWER UNIT AEROSP ATR42 ATR42300 8680920 EU CABIN SHORTED A M3HA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 13 4206G 081 HNL - ON RETURN FLIGHT FROM OGG, PASSENGER REPORTED SMOKE, ROW 5 C/D, LATERAL LIGHTS AREA. REMOVED AND INSTALLED SERVIC EABLE POWER UNIT. (M) 2 H 7 2 4T RT A53EU 1996122600238 19961226 00238 EU 1996 12 26 M3HA96036 1 19961203 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A M3HA K NONE L NO TEST IN INSP/MAINT 1 WP 13 4206G 10472 081 HNL - DURING DAILY INSPECTION, EMERGENCY LIGHT (3WL) OUT. REMOVED AND INSTALLED SERVICEABLE POWER UNIT. (M) 2 H 7 2 4T RT A53EU 1996122600239 19961226 00239 EU 1996 12 26 SIMA963251 1 19961120 A 3211 D60259 TRUNNION MESSIER D226860405 AEROSP ATR42 ATR42300 8680920 EU RT MLG FAILED A A SIMA E ENGINE SHUTDOWN O OTHER TX TAXI/GRND HDL 1 SW 21 47AE N425R 047 CVG - FLT 4016 - ON TAXI OUT TO RUNWAY, AIRCRAFT RT MLG TRUNNION FAILED. CREW COMPLETED WITH ENGINE SHUTDOWN AND EMERGE NCY EVACUATION OF PASSENGERS. INVESTIGATION SHOWED THE GEAR BROKE AT THE TRAILING ARM CONNECTION TO THE LEFT ASSEMBLY. THIS WAS STRUCTURE FAILURE OF THE LEG. AFTER IN DEPTH INSPECTION, ANOTHER GEAR WAS INSTALLED, AND THE AIRCRAFT WAS FER RIED TO DFW FOR PANEL REPAIRS. THE AIRCRAFT HAS RETURNED TO SERVICE. DAMAGED GEAR COMPONENTS ARE BEING SENTO TO THE NT SB. (M) 2 H 7 2 4T RT A53EU 1996122600240 19961226 00240 EU 1996 12 26 SIMA963372 1 19961202 A 2120 CLAMP AEROSP ATR72 ATR72212 EU RIGHT LOOSE A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 447AM 447 DFW - FLT 3597 - SMOKE IN CABIN WITH RT BLEED IN X OVER, RT ENGINE RUNNING, LEFT ENGINE SHUT DOWN. PERFORMED RIGHT ENGI NE RUN FOUND AIR LEAKING AROUND GROUND COOLING FAN, TIGHTENED CLAMPS, NO ADDITIONAL LEAKS NOTICED. OPS CHECK GOOD IAW 7 2-00. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996122600241 19961226 00241 NM 1996 12 26 BJNA961100 1 19961121 A 3350 S106 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 456TM 61585 20336 AFT BULL NOSE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERYS IAW BMM 33-51-01. OPS CHECK OK. (M) 2 L 7 2 4F A16WE 1996122600242 19961226 00242 NM 1996 12 26 BJNA961108 1 19961121 A 3350 S106 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 456TM 61585 20336 L1 PORTABLE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERYS IAW BMM 33-51-101. OPS CHECK OK. (M) 2 L 7 2 4F A16WE 1996122600243 19961226 00243 NM 1996 12 26 BJNA961106 1 19961108 A 5753 6590737563 RIB BOEING 737 737214 138446R NM LT TE MID FLAP CRACKED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 457TM 20156 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE LEFT WING INBOARD MID FLAP SIXTH RIB FROM INBOARD END WAS FOUND WITH TWO CRACKS ON THE LOWER FLANGE. REMOVED THE NR 6 RIB, CUT OUT GOUGED AND CRACKED SECTION OF WEB. FA BRICATED AND INSTALLED TWO DOUBLERS AND FILLER. INSTALLED NEW RIB IAW B737 SRM 51-40-2, 51-30-02 PAGE 2,51-10-01, MM 51 -21-31 AND AERO CORP EO 96-391 REV 1 DATED 11-11-96. (M) 2 L 7 2 4F A16WE 1996122600244 19961226 00244 NM 1996 12 26 BJNA961107 1 19961108 A 5753 694066311 RIB BOEING 737 737214 138446R NM LT TE FLAP CRACKED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 457TM 52149 20156 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE LEFT WING INBOARD FLAP SECOND RIB FROM INBOARD END WAS FOUND WITH A CRACK AT THE LOWER AFT CORNER. GAINED ACCESS TO AREA. REMOVED CRACKED RIB. DRILLED AND INSTALLED NE W RIB AND KIT IAW 737-200 SRM 51-10-02 PAGE 1, 51-10-01, 51-30-02, MM 27-51-01 AND 27-62-91. (M) 2 L 7 2 4F A16WE 1996122600245 19961226 00245 NM 1996 12 26 BJNA961105 1 19961119 A 5753 SPAR BOEING 737 737214 138446R NM RT TE MID FLAP CRACKED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 457TM 52149 20156 UPON A SCHEDULED INSPECTION AT AERO CORP, THE LEFT INBOARD MID FLAP FRONT SPAR WAS FOUND WITH A GOUGE AND A 1.5 INCH CRA CK AT THE NR 7 RIB FROM THE INBOARD END. (M) 2 L 7 2 4F A16WE 1996122600246 19961226 00246 NM 1996 12 26 BJNA961101 1 19961119 A 5730 1A14174 SKIN BOEING 737 737214 138446R NM RT WING CRACKED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 457TM 52149 20156 RIGHT WING NR 5 SLAT DE-ICE DUCT CUTOUT HAS .25 INCH LONG CRACK TOP CENTER. REMOVED CRACK FABRICATED AND INSTALLED REPA IR DOUBLER IAW B737 SRM 57-30-4 ND 57-50-3 FIG. (M) 2 L 7 2 4F A16WE 1996122600247 19961226 00247 NM 1996 12 26 BJNA9611110 1 19961122 A 7120 MOUNT BOEING 737 737214 138446R NM NR 1 ENG CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 457TM 52148 20156 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND THE NR 1 ENGINE FORWARD MOUNTS MISSING SUPPAGE MARKS FO R ELASOMETRIC MATERIAL. REMOVED ISOLATORS, REMOVED CORROSION. SHOT PEENED AND REWORKED AREA. ULTRASONICALLY INSPECTED , APPLIED PRIMER, AND REINSTALLED ISOLATORS IAW B737 OHM 71-23-01 AND AERO CORP EO 96-396 REV IR DATED 11/19/96 WITH APP ROVAL BY FAA FORM 8110-3. (M) 2 L 7 2 4F A16WE 1996122600248 19961226 00248 NM 1996 12 26 BJNA961111 1 19961104 A 5315 1A19098 FLOOR BEAM BOEING 737 737214 138446R NM BS 269 CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 457TM 52148 20156 DURING A SCHEDULED INSPECTION AT AERO COPR IN LAKE CITY, FLORIDA, THE LATERAL FLOOR SUPPORT ANGLE AT BS 268 BL 11L WAS F OUND WITH EXFOLIATED CORROSION ON THE UNDERSIDE OF THE FLT DECK. REMOVED CORRODED FLOOR BEAM. FABRICATED AND INSTALLED NEW FLOOR BEAM IAW B737 SRM 53-10-01 PAGE 1, 51-10-2, 51-41-161 AND 51-40-4. (M) 2 L 7 2 4F A16WE 1996122600249 19961226 00249 NM 1996 12 26 BJNA961112 1 19961108 A 5753 6590737563 RIB BOEING 737 737214 138446R NM TE MID FLAP CRACKED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 457TM 52149 20156 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA THE LEFT WING INBOARD MID FLAP SEVENTH RIB FROM THE INB OARD END WAS FOUND WITH A CRACK ON THE LOWER FLANGE. REMOVED AND REPLACED WITH A NEW NR 7 RIB IAW B737 SRM 51-10-01, 51 -30-02 PAGE 1 AND AERO CORP EO 96-391 REV 1 DATED NOV 13, 1996. (M) 2 L 7 2 4F A16WE 1996122600250 19961226 00250 NE 1996 12 26 HALA96164 2 19961203 A 7200 ENGINE DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE NR 1 FAILED A HALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 699HA 47763 688712 HNL - FLT 529 - LEFT OIL STRAINER CLOGGING LIGHT ILLUMINATED DURING CLIMB-OUT, LT WOULD NOT EXTINGUISH W/THROTTLE BACK T O IDLE. ALL ENGINE INSTRUMENT READINGS NORMAL. AIR RETURN TO HNL. REMOVED NR 1 ENGINE MAIN OIL FILTER. FOUND EXCESSI VE AMT OF FERROUS MATERIAL IN FILTER AND CORRESPONDING DRAINED OIL. REMOVED AND REPLACED NR 1 ENGINE. (M) 2 L 7 2 4F 4 F RT A6WE E2EA 1996122600251 19961226 00251 1996 12 26 ASAA9680263 4 19961126 A 2565 D37013117 SLIDE BOTTLE D29984103 DOUG DC9 DC982 3022082 WP TAIL CONE LOW PRESSURE A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 01 940AS 49825 OAK - DURING C-CHECK, THE TAILCONE EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSUER WAS FOUND LOW. REPLACED THE TAI LCONE EMERGNCY EVACUATION SLIDE. (M) 2 L 7 2 4F A6WE 1996122600252 19961226 00252 WP 1996 12 26 ASAA9680257 1 19961111 A 5311 59135953 FRAME DOUG DC9 DC983 3022083 WP BS 1418 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 946AS 49658 OAK - DURING C-CHECK, A CRACK WAS FOUND IN FRAME AT LONGERON 2R AT Y1418. INSTALLED DOUBLER PER ASA EA 5310-01499. (M) 2 L 7 2 4F RT A6WE 1996122600253 19961226 00253 1996 12 26 ASAA9680254 4 19961112 A 2565 D29985107 SLIDE DOUG DC9 DC983 3022083 WP L2 DOOR OUT OF POSITION A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 939AS 49657 LAX - AFTER ARRIVAL OF FLT 255 - CREW REPORTED THE L2 DOOR DIFFICULT TO OPEN, APPEARS TO BE STICKING AT LOWER AFT CORNER . FOUND THE EMERGENCY EVACUATION SLIDE COVER HOLDING THE DOOR TRIM OUT OF POSITION AND INTERFERRING WITH DOOR FRAME. R EPLACED THE EMERGENCY EVACUATION SLIDE ASSEMBLY AND DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996122600254 19961226 00254 WP 1996 12 26 ASAA9680249 1 19961106 A 5210 4928806501 HOOK DOUG DC9 DC983 3022083 WP L-1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 972AS 53448 PDX - AFTER ARRIVAL OF FLT 383, CREW REPORTED THE L-1 DOOR STICKS IN THE OPEN POSITION. ADJUSTED THE HOLD OPEN HOOK AND DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996122600255 19961226 00255 WP 1996 12 26 ASAA9680255 1 19961112 A 5210 4928806501 HOOK DOUG DC9 DC983 3022083 WP L1 DOOR BENT A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 977AS 53453 PSP - PRIOR TO DEPARTURE OF FLT 481, CREW REPORTED THE L1 DOOR WOULD NOT LATCH IN OPEN POSITION. FOUND THE HOLD OPEN HO OK BENT. STRAIGHTENED AND INSPECTED THE HOOK AND DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996122600256 19961226 00256 WP 1996 12 26 ASAA9680252 1 19961110 A 5210 LATCH DOUG DC9 DC983 3022083 WP L1 DOOR MALFUNCTIONED A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 979AS 53471 SEA - AFTER ARRIVAL OF FLIGHT 333, CREW REPORTED THE L1 DOOR HOLD OPEN LOCK WOULD NOT RELEASE, HAD TO USE RELEASE BUTTON ON FUSELAGE TO RELEASE DOOR. LUBRICATED THE HOLD OPEN LATCH ASSEMBLY AND DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1996122600257 19961226 00257 NM 1996 12 26 USAA960760 1 19961127 A 5730 SKIN BOEING 737 737301 1384611 NM LT WING GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 26963 23559 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND GOUGED 3 INCH BY .5 INCH BY .027 INCH LEFT WING INBOARD LEADING EDGE OF OUTBOARD MIDFLAP SKIN. REMOVED EXISTING REPAIR, FABRICATED FILLER AND DOUBLER AND INSTALLED. REPAIRED PER EA 41753 AND SB 57-1236. (M) 2 L 7 2 4F RT A16WE 1996122600258 19961226 00258 NM 1996 12 26 USAA960761 1 19961127 A 5753 SKIN BOEING 737 737301 1384611 NM RT TE MID FLAP GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 26963 23559 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND GOUGED 4 INCH BY .75 INCH BY .037 INCH RIGHT WING INBOARD LEADING EDGE O F OUTBOARD MID FLAP SKIN OF FLAP. REMOVED EXISTING REPAIR, FABRICATED FILLER AND DOUBLER AND INSTALLED. REPAIRED PER E A 41754, SB 737-57-1236. (M) 2 L 7 2 4F RT A16WE 1996122600259 19961226 00259 NM 1996 12 26 USAA960762 1 19961127 A 5313 STRINGER BOEING 737 737301 1384611 NM BS 500D CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 26963 23559 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 3 INCH CORRODED AREA BS 500 D PLUS 2 INCHES STRINGER 28R. RE MOVED CORRODED AREA INSTALLED REPAIR PARTS COMPLETED REPAIR, REPAIRED PER SRM 53-30-12 FIG 202. (M) 2 L 7 2 4F RT A16WE 1996122600260 19961226 00260 NM 1996 12 26 USAA960763 1 19961127 A 5320 ANGLE BOEING 737 737301 1384611 NM BS 540 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 26963 23559 INT - DURING Q-3 CHECK VISUAL INSPECTION FOUND 1.5 INCH CRACK BS 540 ABOVE STRINGER 22R ATTACH ANGLE. INSTALLED DOUBLE R, REPAIRED PER TR 53-50-03. (M) 2 L 7 2 4F RT A16WE 1996122600261 19961226 00261 NM 1996 12 26 USAA960764 1 19961127 A 5330 SKIN BOEING 737 737301 1384611 NM BS 328 HOLE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 26963 23559 INT - DURING Q-3 CHECK CARRY OVER INSPECTION, FOUND 2 INCH BY 3 INCH HOLE BS 328, BETWEEN STRINGER 20R TO STRINGER 21R S KIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-00-01 FIG 202. (M) 2 L 7 2 4F RT A16WE 1996122600262 19961226 00262 NM 1996 12 26 USAA960765 1 19961127 A 5320 65C10592153 ANGLE BOEING 737 737301 1384611 NM BS 960 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 26963 23559 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCH BY 3 INCH BY .040 INCH, STATION 960 RBL 9 FLOOR SUPPORT ANGLE. REPLACED FLOOR ANGLE, REPAIRED PER MODIFIED PART NR 65-C10592-153. REPAIRED PER SRM 51-10-2 AND BOEING DRAWING NR 65-46812. (M) 2 L 7 2 4F RT A16WE 1996122600263 19961226 00263 NM 1996 12 26 USAA960766 1 19961127 A 5320 WEB BOEING 737 737301 1384611 NM BS 986-1006 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 26963 23559 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 4 INCH CORROSION STATION 986 TO 1006 LBL 38 WEB. FABRICATED W EB AND INSTALLED, REPAIRED PER BOEING DRAWING 65-C32677. CORROSION TASK NR C53-107-02. CORROSION LEVEL 1. (M) 2 L 7 2 4F RT A16WE 1996122600264 19961226 00264 NM 1996 12 26 USAA960767 1 19961127 A 5230 SKIN BOEING 737 737301 1384611 NM BS 450 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 26963 23559 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK INTERIOR NR 1 CARGO DOOR SKIN STATION 450. STOP DRILLED C RACK, FABRICATED DOUBLER AND INSTALLED. REPAIRED PER SRM 51-40-2, FIG 1. (M) 2 L 7 2 4F RT A16WE 1996122600265 19961226 00265 NM 1996 12 26 USAA960768 1 19961127 A 5312 BULKHEAD SKIN BOEING 737 737301 1384611 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 356US 26963 23559 INT - DURING Q-3 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND CRACK .25 INCH LONG AT STATION 178 BULKHEAD SKIN LBL 4 WL 1 99. STOP DRILLED CRACK AND FABRICATED DOUBLER AND INSTALLED. REPAIRED PER TR 53-10-07 STEP 2 AND 3. (M) 2 L 7 2 4F RT A16WE 1996122600266 19961226 00266 NM 1996 12 26 USAA960755 1 19961127 A 5315 FLOOR BEAM BOEING 737 7373B7 1384580 NM BS 328 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 521AU 30780 23856 CLT - INSPECTION VISUALLY FOUND LEVEL 2 CORROSION MEASURING 1 INCH BY 1 INCH LOCATED AT FLOOR BEAM FLANGE STATION 328, S TATION 528 LBL 13 AND AT LBL 49. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. APPLIED FILLER 'T' AND SPLICE ANGLE AS PER USAIR TYPICAL REPAIR 53-10-03. (M) 2 L 7 2 4F RT A16WE 1996122600267 19961226 00267 NM 1996 12 26 USAA960756 1 19961127 A 5315 FLOOR BEAM BOEING 737 7373B7 1384580 NM BS 312 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 518AU 29321 23704 CLT - INSPECTION VISUALLY FOUND LEVEL 2 CORROSION AROUND VARIOUS CLIPNUT HOLES UPPER 'T' CAP OF STATION 312, BL 0 TO RBL 40, STATION 312. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. INSTALLED NEW 'T' CAP REPAIR/REPLACEMENT AS PER USA IR TYPICAL REPAIR 53-10-03. (M) 2 L 7 2 4F RT A16WE 1996122600268 19961226 00268 EU 1996 12 26 USAASB96246 2 19961126 A 7200 ENGINE BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU NR 1 BIRD STRIKE A USAA A UNSCHED LANDING C E F.O.D. VIBRATION/BUFFET TO TAKEOFF 1 EA 19 394US 23316 DAB - FLT 282 - UPON ROTATION WITH THE NOSE JUST OFF THE RUNWAY, THE AIRCRAFT STRUCK A FLOCK OF BIRDS. SEVERE VIBRATION WAS FELT FROM THE NR 2 ENGINE. THE CAPTAIN DID NOT SHUT DOWN THE ENGINE BUT KEPT IT IN IDLE WHILE THEY RETURNED TO FIE LD AT DAB. NO EMERGENCY WAS DECLARED AND THE FLT LANDED W/OUT FURTHER INCIDENT. MX REPLACED THE NR 1 ENGINE ASSY, THE NR 2 ENG FAN ASSY, THE NR 2 ENG PRECOOLER, THE LEFT INBD T/E FLAPS AND THE RT INBD AFT FLAP. ALL OP CHECKS, LEAK CHECKS AND ENGINE RUN GOOD. (M) 2 L 7 2 4F 4 F RT A16WE E21EU 1996122600269 19961226 00269 1996 12 26 RAIA961122 4 19961124 A 3418 45150561 ALPHA PROBE AEROSP ATR72 ATR72202 8680940 EU LT FUSELAGE FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 721TE 9181 217 STL - FLT 7003 - CAPTAINS ALPHA PROBE HEAT C/B POPPED AND WON'T RESET. MAINTENNCE REPLACED THE CAPTAINS ALPHA PROBE. ( M) 2 H 7 2 4T RT A53EU 1996122600270 19961226 00270 1996 12 26 RAIA961125 4 19961125 A 3418 45150560 ALPHA PROBE AEROSP ATR42 ATR42300 8680920 EU LT FUSELAGE FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 423TE 7797 119 STL - FLT 7136 - CAPTAINS ALPHA PROBE C/B POPPED, AND WOULD NOT RESET. MAINTENANCE REPLACED THE CAPTAINS ALPHA PROBE. ( M) 2 H 7 2 4T RT A53EU 1996122600271 19961226 00271 EU 1996 12 26 RAIA961118 1 19961119 A 6120 1680640 MONOPOLE BAG JETSTM JETSTM3201 1500217 EU PROP GOVERNOR FAILED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 342TE 954 STL - FLT 7029 - RIGHT SRL CAPTION CAME ON AT 80 PERCENT TORQUE. MAINTENANCE REPLACED THE RIGHT ENGINE PROP GOVERNOR MO NOPOLE. (M) 2 L 7 2 4T RT A56EU 1996122600272 19961226 00272 EU 1996 12 26 RAIA961121 1 19961123 A 7722 8974696 EGT SHORTLEAD BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 427AM 9918 876 STL - FLT 7308 - RIGHT EGT WAS ERRATIC ON TAKEOFF ROLL. MAINTENANCE REPLACED THE RIGHT ENGINE EGT SHORT LEAD. (M) 2 L 7 2 4T RT A56EU 1996122600273 19961226 00273 1996 12 26 RAIA961123 4 19961124 A 3425 7003360948 AHRS COMPUTER JETAIR JETSTM JETSTM4101 1500501 EU LEFT FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 568HK 1117 41086 JFK - FLT 7789 - CAPTAINS AHRS FAILED. MAINTENANCE REPLACED THE CAPTAINS AHRS COMPUTER. (M) 2 L 7 2 4T RT A41NM 1996122600274 19961226 00274 1996 12 26 RAIA961126 4 19961125 A 3414 7002860909 AIR SPEED IND AEROSP ATR42 ATR42300 8680920 EU LT COCKPIT FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 423TE 15049 119 STL - FLT 7136 - NR 1 AIR DATA COMPUTER FAILED IN FLIGHT. MAINTENANCE REPLACED THE CAPTAINS AIRSPEED INDICATOR. (M) 2 H 7 2 4T RT A53EU 1996122600275 19961226 00275 EU 1996 12 26 RAIA961127 1 19961125 A 2430 PB20 WIRE JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE BROKEN A RAIA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 CE 03 562HK 1868 41078 JFK - FLT 7654 - LEFT GENERATOR FELL OFF LINE, AND WOULD NOT RESET. MAINTENANCE REPAIRED WIRE AT THE LEFT STARTER/GENER ATOR. (M) 2 L 7 2 4T RT A41NM 1996122600276 19961226 00276 EU 1996 12 26 RAIA961128 1 19961125 A 3350 311701 BATTERY PACKS BAG JETSTM JETSTM3201 1500217 EU BS 130/452 DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 866AE 866 FAT - CABIN EMERGENCY LIGHTS ARE INOP. MAINTENANCE REPLACED FOUR EMERGENCY LIGHT BATTERY PACKS AT STATION 130 AND STATI ON 452. (M) 2 L 7 2 4T RT A56EU 1996122600277 19961226 00277 EU 1996 12 26 RAIA961129 1 19961125 A 5313 S53671400203 STRINGER AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - FOUND CORROSION ON STRINGER 15R FROM FRAME 33 TO 39. MAINTENANCE TREATED CORROSION PER ATR SRM 51-21-42. (M) 2 H 7 2 4T RT A53EU 1996122600278 19961226 00278 EU 1996 12 26 RAIA961151 1 19961126 A 5320 S5367125720402 SPRING TQ BOX AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - MAINTENANCE FOUND CORROSION ON SPRING TORQUE BOX AFT OF FRAME 39. MAINTENANCE CLEANED CORROSION AS REQUIRED. (M) 2 H 7 2 4T RT A53EU 1996122600279 19961226 00279 EU 1996 12 26 RAIA961152 1 19961126 A 5320 S5367131828001 WEB AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - CORROSION FOUND ON RIGHT 'Z' SHEER WEB FROM FRAME 39 TO 41. MAINTENANCE TREATED MINOR CORROSION. (M) 2 H 7 2 4T RT A53EU 1996122600280 19961226 00280 EU 1996 12 26 RAIA961153 1 19961126 A 5320 S5367131828001 WEB AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - FOUND CORROSION ON RIGHT SHEER WEB AFT OF FRAME 39. MAINTENANCE TREATED MINOR CORROSION. (M) 2 H 7 2 4T RT A53EU 1996122600281 19961226 00281 EU 1996 12 26 RAIA961154 1 19961126 A 5320 S5367131828001 WEB AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - FOUND CORROSION ON RIGHT SHEER WEB FORWARD OF FRAME 36. MAINTENANCE TREATED MINOR CORROSION. (M) 2 H 7 2 4T RT A53EU 1996122600282 19961226 00282 EU 1996 12 26 RAIA961155 1 19961125 A 5330 S536770206200 SKIN AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - FOUND CORROSION ON PAX DOOR TORQUE BOX SKIN FROM FRAME 36 TO 39. MAINTENANCE REPLACED THE PAX DOOR TORQUE BOX SKI N. (M) 2 H 7 2 4T RT A53EU 1996122600283 19961226 00283 EU 1996 12 26 RAIA961156 1 19961126 A 5320 S53672408228 CLIPS AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - FOUND CORROSION ON FRAME NR 40 SKIN CLIPS BETWEEN STRINGER 17L AND 17R. MAINTENANCE REPLACED FRAME 40 FROM FACTOR Y SPLICES. (M) 2 H 7 2 4T RT A53EU 1996122600284 19961226 00284 EU 1996 12 26 RAIA961157 1 19961126 A 5320 S53672408228 CLIPS AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 18155 119 STL - MAINTENANCE FOUND CORROSION ON FRAME 39 SKIN CLIPS BETWEEN STRINGER 16L AND 19R. MAINTENANCE REPLACED FRAME 39 LO WER FROM FACTORY SPLICES. (M) 2 H 7 2 4T RT A53EU 1996122600285 19961226 00285 NM 1996 12 26 TAOA129604 1 19961208 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 924TS T3758 21041 FORWARD ENTRY AISLE EMERGENCY EXIT SIGN INOP. REPLACED BATTERY PACK, OPERATION CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1996122600286 19961226 00286 NM 1996 12 26 TAOA129606 1 19961206 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 925TS VA4695 21244 EMERGENCY EXIT SIGN AT AISLE ROW 3 INOP. REPLACED BATTERY PACK, OPERATION CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1996122600287 19961226 00287 NM 1996 12 26 TAOA129602 1 19961204 A 5315 FLOOR BEAM BOEING 727 727254 138408L NM BS 950 CRACKED A TAOA O OTHER O OTHER IN INSP/MAINT 1 EA 15 914TS 20251 C-2 CARGO DOOR BUNGEE TORQUE SHAFT ATTACHMENT BRACKET AT FLOOR BEAM FLANGE HAS 6.5 INCH CRACK AT STATION 950E. PERFORME D CABIN FLOOR BEAM REPAIR AT STATION 950E, REPAIRED LOWER FLANGE IAW STRUCTURAL REPAIR MANUAL CHAPTER 53-10-8. REPLACED AFT CARGO DOOR FORWARD BUNGEE CABLE, C-2 DOOR OPERATION CHECK NORMAL PER MM 52-35-31. (M) 2 L 7 3 4F A3WE 1996122600288 19961226 00288 NM 1996 12 26 TAOA129601 1 19961203 A 3350 7912 LENS GRIMES BOEING 727 727254 138408L NM CABIN MISSING A TAOA K NONE O OTHER IN INSP/MAINT 1 EA 15 915TS 20252 FLOOR PATH LIGHTING ROW 18 IS OUT, AND LENSE IS MISSING. ROW 27 LENS MISSING. INSTALLED LENS AT ROW 18 AND 27, ALL LIG HTS CHECK OK. (M) 2 L 7 3 4F A3WE 1996122600289 19961226 00289 NM 1996 12 26 TAOA119606 1 19961127 A 3350 1000679 LIGHT GRIMES BOEING 727 727225 1384077 NM COCKPIT BROKEN A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 919TS 4380 20447 EMERGENCY EXIT LIGHT IN COCKPIT INOP. REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK OK. (M) 2 L 7 3 4F A3WE 1996122600290 19961226 00290 NM 1996 12 26 TAOA119605 1 19961127 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 923TS 11306 20441 EMERGENCY EXIT CEILING LIGHT AT ROW 17 INOP. REPLACED BATTERY PACK OPERATION CHECK OK. (M) 2 L 7 3 4F A3WE 1996122600291 19961226 00291 NM 1996 12 26 TAOA119604 1 19961129 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 918TS T3921 20445 FORWARD ENTRY AISLE EMERGENCY EXIT SIGN INOP. REPLACED BATTERY PACK OPS OK. (M) 2 L 7 3 4F A3WE 1996122600292 19961226 00292 EU 1996 12 26 SIMA963431 1 19961208 A 3350 3011151 BATTERY PACKS AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 424MQ 045 ORD - FLT 4076 - THE FORWARD EMERGENCY EXIT LIGHT AT THE BOTTOM OF THE FORWARD EMERGENCY EXIT DOOR DOES NOT ILLUMINATE W ITH POWER OFF THE AIRCRAFT. RAI'D AND REAR EMERGENCY BATTERY POWER PACKS (S/N 4296 AND 3035). OPS CHECK GOOD. AIRCRAF T WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996122600293 19961226 00293 EU 1996 12 26 SIMA963442 1 19961209 A 3350 3011185 POWER SUPPLY AEROSP ATR42 ATR42300 8680920 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 216AT 155 216 ORD - FLT 4087 - FOUND EMERGENCY LIGHTS NOT COMPLETELY LIGHTING. REMOVED AND REPLACED POWER SUPPLY AT 18WL. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996122600294 19961226 00294 1996 12 26 SIMA963371 4 19961202 A 3425 7004544712 SGU HONEYWELL AEROSP ATR72 ATR72212 EU NR 2 EFIS FAILED A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 248AT 91081332 248 ORD - FLT 4051 - AFTER TAKEOFF ROTATION BOTH EFIS SCREENS ON FO'S SIDE WENT BLANK ACCOMPANIED BY GPWS, DON'T SINK, STICK PUSHER FAULT AND GEAR NOT DOWN WARNING. REPLACED NR 2 EFIS SGU IAW 34-71-10. OPS CHECK GOOD. AIRCRAFT WAS RETURNED T O SERVICE. (M) 2 H 7 2 4T RT A53EU 1996122600295 19961226 00295 EU 1996 12 26 SIMA963381 1 19961203 A 3350 E0062BCA4AC0A SWITCH AEROSP ATR72 ATR72212 EU COCKPIT FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 438AT 438 DFW - FLT 3745 - EMERGENCY LIGHT REMAIN ON IN ARMED POSITION, WHEN SELECTING DISARM THEY WILL GO OUT. RAI'D COCKPIT EME RGENCY LIGHT SWITCH 2WL. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996122600296 19961226 00296 EU 1996 12 26 SIMA963441 1 19961209 A 3233 NTA11555K18 BOLT AEROSP ATR42 ATR42300 8680920 EU LT MLG ACT BROKEN A A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 262AT 0262 MQT - MAINTENANCE PERFORMING AN IMBV INSPECTION, FOUND THE LEFT MAIN LANDING GEAR ACTUATOR BRACKET FORWARD LOWER BOLT BR OKEN OFF. MAINTENANCE REMOVED AND REPLACED BOLT IAW EO E15300-208. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1996122600297 19961226 00297 EU 1996 12 26 PLGA9611231 1 19961123 A 3230 4018401 HYD PUMP SAAB SF340 340B 7860101 EU LANDING GEAR FAILED A PLGA O OTHER J WARNING INDICATION AP APPROACH 1 NE 05 351BE DA46 340B237 ROC - FLT 4890 - WHEN SELECTING THE GEAR DOWN FOR LANDING, THE HYDRAULIC ANNUNCIATOR LIGHT ILLUMINATED AND THE GEAR FAIL ED TO EXTEND. THE CREW NOTED THAT THE HYDRAULIC PUMP FAILED TO OPERATE. THE CREW THEN PUMPED THE GEAR AND FLAPS DOWN, LANDING WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT AND REPLACED THE HYDRAULIC PUMP AND MOTOR ASSEMBLY RETURNING THE AIRCRAFT TO SERVICE (M) 2 L 7 2 4T RT A52EU 1996122600298 19961226 00298 1996 12 26 PLGA9611241 3 19961124 A 6140 4018401 PROP IND SAAB SF340 SF340A 7850100 EU LT PROP FAILED A PLGA A UNSCHED LANDING O OTHER CR CRUISE 1 NE 05 747BA DA46 340A148 BOS - FLT 4949 - TWENTY MINUTES AFTER DEPARTURE FROM BOS TO YQB, THE LEFT PROPELLER RPM INDICATION BEGAN TO FLUCTUATE 50 -100 RPM. THE AIRCRAFT RETURNED TO BOS, LANDING WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PROPELLER RPM I NDICATOR AND RETURNED TO AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1996122600299 19961226 00299 EU 1996 12 26 PLGA9611261 1 19961126 A 2420 WIRE SAAB SF340 SF340A 7850100 EU RT GENERATOR BROKEN A PLGA A UNSCHED LANDING O OTHER CL CLIMB 1 NE 05 344BE 340A104 BOS - FLT 4453 - DURING CLIMB-OUT FROM BOS, THE RIGHT AC GENERATOR FAIL LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO BOS , LANDING WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT AND REPAIRED AN OPEN WIRE BETWEEN THE AC GENERAT OR CONTROL UNIT AND THE WHEEL WELL CIRCUIT BREAKER TO RETURN THE AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1996122600300 19961226 00300 NM 1996 12 26 USAASB96251 1 19961203 A 3350 AD20131A BATTERY BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 435US 24557 ROC - FOUND MAIN ENTRANCE DOOR EMERGENCY LIGHT AND FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED THE AFT UPPER P OWER SUPPLY BATTERY. (M) 2 L 7 2 4F RT A16WE 1996122600301 19961226 00301 1996 12 26 USAASB96248 4 19961130 A 3425 7725005009 ADI BOEING 737 737401 1384701 NM COCKPIT FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 411US 23447 23880 PVD - FL 155, FIRST OFFICERS ADI FAILED. FLIGHT RETURNED TO PVD AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLA CED THE ADI. (M) 2 L 7 2 4F RT A16WE 1996122600302 19961226 00302 1996 12 26 USAAD96176 4 19961202 A 2312 COMM SYST DOUG DC9 DC931 3022065 WP NR 1/2 MALFUNCTIONED A USAA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 EA 19 963VJ 47508 FLT 2048 - SWF-CLT - LOST BOTH COMM'S ON TAKEOFF. RETURNED TO FIELD. EVENTUALLY WERE ABLE TO TRANSMIT ON NUMBER 2, AND RECIEVE ON NUMBER 1. RERACKED NUMBER 1 AND 2 COMMS. FOUND NUMBER 1 LOOSE. SECURED BOTH. ALL CHECKED GOOD. (M) 2 L 7 2 4F A6WE 1996122600303 19961226 00303 WP 1996 12 26 USAAD96175 1 19961203 A 3350 110049 CHARGER DOUG DC9 DC931 3022065 WP CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 976VJ 48147 MID CABIN FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE. FOUND FUSE IN CHARGER ASSEMBLY OPEN AND CORRODED. REPLACED CHARGER ASSEMBLY. (M) 2 L 7 2 4F A6WE 1996122600304 19961226 00304 WP 1996 12 26 USAAD96174 1 19961127 A 3350 60030451LB POWER SUPPLY DOUG DC9 DC981 3022081 WP CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 802US 48036 FORWARD AND MID CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN MID CABIN POWER SUPPLY. REPLACED PO WER SUPPLY AND BATTERIES IN FORWARD CABIN. (M) 2 L 7 2 4F A6WE 1996122600305 19961226 00305 WP 1996 12 26 USAAD96173 1 19961128 A 3350 14597101 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 829US 49429 FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE. REPLACED BATTERIES IN BATTERY PACK. (M) 2 L 7 2 4F A6WE 1996122600306 19961226 00306 EU 1996 12 26 USAAF96124 1 19961128 A 3350 CONNECTOR FOKKER F28 F28MK0100 4990807 EU CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 893US 11373 RIC - LEFT AFT UPPER EMERGENCY EVACUATION EXIT LIGHT IS INOP. MAINTENANCE REPAIRED BROKEN CONNECTOR ON BACK OF LIGHT FI XTURE, CONNECTOR 2801B01. (M) 2 L 7 2 4F RT 1996122600307 19961226 00307 EU 1996 12 26 USAAF96125 1 19961124 A 3350 6008905 POWER SUPPLY FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 482US 11231 ROA - AFT CABIN EMERGENCY LIGHTING INOPERATIVE. REPLACED AFT RIGHT EMERGENCY LIGHTING POWER SUPPLY. (M) 2 L 7 2 4F RT A20EU 1996122600308 19961226 00308 NM 1996 12 26 TWRA96376 1 19961210 A 3350 S1356B37 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY CHECK, FOUND B-ZONE RIGHT SIDE CEILING EMERGENCY LIGHT INOP. REMOVED AND REPLACED CEILING LIGHT PER MM 33- 51-00. OPS CHECKED NORMAL. (M) 2 L 7 4 4F A20WE 1996122600309 19961226 00309 NM 1996 12 26 TWRA96375 1 19961211 A 5610 60B100288 WINDSHIELD BOEING 747 747130 1384880 NM RT COCKPIT SHATTERED A TWRA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 15 603FF 7H0416P1772 19746 DURING CLIMB, R1 WINDSHIELD SHATTERED AND ARCED FLIGHT LEVEL 20. WITH WINDOW HEAT ON. DIFF PRESS 5.0 WINDSHIELD HAD A SEVERE AIR LEAK 5,500 TO 20,000 FT. REMOVED AND REPLACED WINDOW PER MM 56-11-01, WI 56-152. ALL CHECKS NORMAL. CHECKE D WIRING AT R1 WINDOW POINT TO POINT PER WDM 30-41-11 PAGE 4. WIRING CHECKED GOOD. REPLACED WINDOW HEAT CONTROLLER. O PS CHECKED GOOD. (M) 2 L 7 4 4F A20WE 1996122600310 19961226 00310 NM 1996 12 26 TWRA96374 1 19961203 A 3350 S1356B37 LIGHT BOEING 747 747282B 1384860 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 611FF 20502 DURING DAILY CHECK, FOUND CEILING LIGHT INOP AT R4 DOOR, B AND C ZONE RIGHT SIDE CEILING LIGHT INOP. REMOVED AND REPLA CED LIGHT ASSEMBLY. OPS CHECKED NORMAL PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996122600311 19961226 00311 NM 1996 12 26 TSAA9657091 1 19961126 A 5730 SKIN BOEING 737 7372Y5 1384554 NM WS 505-557 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 810AL 24031 DURING C-CHECK VISIT, NOTED EXFOLIATION CORROSION LOWER WING SKIN RIGHT, CORROSION AT INBOARD AILERON ATTACH POINT WING TO FITTING WS 505 - 557 REPAIRED PER ECO 1684 R7. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4U RT A16WE 1996122600312 19961226 00312 NM 1996 12 26 TSAA9655093 1 19961126 A 5532 SKIN BOEING 737 7372Y5 1384554 NM VERT STAB CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 810AL 24031 DURING C-CHECK VISIT, CORROSION NOTED ON VERTICAL STABILIZER LEFT SIDE BETWEEN FS 111 - FS 113. REPAIRED PER ECO 2509 R 2. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4U RT A16WE 1996122600313 19961226 00313 SW 1996 12 26 96ZZZM1569 1 19961126 A 2910 27810322684 TUBE FRCHLD SA227 SA227DC 3377521 SW RT NACELLE CRACKED A EQGA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 19 847LS DC847B EN ROUTE TO DFW, THE AIRCRAFT LOST ALL HYDRAULIC PRESSURE. CAPTAIN PUMPED GEAR DOWN USING THE EMERGENCY EXTENSION SYSTE M. AIRCRAFT LANDED AT DFW WITHOUT FURTHER INCIDENT. ON INSPECTION, A CRACKED HYDRAULIC LINE WAS FOUND TO BE THE PROBLE M. THE LINE WAS REPLACED AND THE AIRCRAFT WAS SERVICED WITH HYDRAULIC FLUID AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A18SW 1996122600314 19961226 00314 NM 1996 12 26 AWXA9600753 1 19961209 A 5347 BAC1520792 SEAT TRACK BOEING 737 73733A 1384673 NM BS 338 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 169AW 23630 DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON SEAT TRACK AT STA 338, RBL 25, WL 208. INSTALLED NEW SEAT TRACK AT BS 338, RBL 25, WL 208 IN ACCORDANCE WITH SRM 53-00-52. 2 L 7 2 4F RT A16WE 1996122600315 19961226 00315 NM 1996 12 26 AWXA9600754 1 19961204 A 5347 BAC1520792 SEAT TRACK BOEING 737 73733A 1384673 NM BS 338 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 169AW 23630 DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON SEAT TRACK AT STA 338, RBL 45, WL 208. INSTALLED NEW SEAT TRACK AT BS 338, RBL 45, WL 258 IN ACCORDANCE WITH SRM 53-00-52. 2 L 7 2 4F RT A16WE 1996122600316 19961226 00316 NM 1996 12 26 AWXA9600755 1 19961203 A 5320 654587545 MOPSILL BOEING 737 73733A 1384673 NM BS 284-332 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 169AW 23630 DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON RT MOPSILL AT BS 284 TO 332, RBL 62, WL 208. REMOVED AND REPLACED MOPSILL AT BS 284 TO 332, WL 208, RBL 62, IAW, SRM 51-40-2. 2 L 7 2 4F RT A16WE 1996122600317 19961226 00317 NM 1996 12 26 AWXA9600756 1 19961205 A 5753 654648106 CARRIAGE BOEING 737 73733A 1384673 NM RT TE MID FLAP CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 169AW 23630 DURING ROUTINE MAINTENANCE CHECK, FOUND R/W OUTBOARD MID FLAP INBOARD CARRIAGE SPINDAL CORRODED. REMOVED AND REPLACED R /W O/B MID FLAP I/B CARRIAGE PER MM 27-51-44. 2 L 7 2 4F RT A16WE 1996122600318 19961226 00318 NM 1996 12 26 AWXA9600757 1 19961203 A 5315 FLOORBEAM BOEING 737 73733A 1384673 NM BS 294.5 CORRODED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 169AW 23630 DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOORBEAM UPPER CHORD AT BS 294.5, WL 208, RBL 14 TO LBL 2. REPAIR ED FLOORBEAM UPPER CHORD IAW, SRM 53-10-51. 2 L 7 2 4F RT A16WE 1996122600319 19961226 00319 NM 1996 12 26 AWXA9600758 1 19961214 A 2497 WIRE HARNESS BOEING 737 737277 1384570 NM WS 213 CHAFED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 22646 DURING ROUTINE MAINTENANCE CHECK, FOUND LEFT WING LEADING EDGE WIRE BUNDLE LOCATED AT W142, LES 213, FS 205, SHORTED AND MELTED 15 OF 32 WIRES. CAUSE OF THE SHORT WAS DETERMINED TO BE CHAFING AS NOTED BY BOEING SERVICE LETTER 737-SL-24-27. REPAIR WAS ACCOMPLISHED PER SERVICE BULLETIN 24-10-53. ALL EFFECTED SYSTEMS OPERATIONALLY CHECKED. 2 L 7 2 4F RT A16WE 1996122600320 19961226 00320 NM 1996 12 26 AWXA9600759 1 19961210 A 5330 SKIN BOEING 737 737277 1384570 NM BS 727 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 22646 DURING ROUTINE MAINTENANCE CHECK, FOUND SKIN CRACKED AT BS 727 L/H, COMMON TO STR 18A AND 727 CHORD AFT HOLE. REPAIRED CRACK PER ER 2-53-15-54, TCO-PAN-96-1744RR, 8110-3. 2 L 7 2 4F RT A16WE 1996122600321 19961226 00321 NM 1996 12 26 AWXA9600760 1 19961211 A 5315 FLOORBEAM BOEING 737 737277 1384570 NM BS 947 CORROSION A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 22646 DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON BS 947 FLOORBEAM ON UPPER CHORD, LBL 13 TO RBL 53, WL 208. REPAIRE D BS 947 FLOORBEAM PER ER 2-53-16-45, TCO-PAN-96-1746RR 8110-3. 2 L 7 2 4F RT A16WE 1996122600322 19961226 00322 NM 1996 12 26 AWXA9600761 1 19961203 A 5315 FLOORBEAM BOEING 737 737277 1384570 NM BS 987 CORROSION A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 22646 DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOORBEAM BS 987, LBL 17 TO RBL 45, WL 208. REPAIRED FLOORBEAM BS 987, LBL 29 TO RBL 55, WL 208 PER EO 2-53-16-46. 2 L 7 2 4F RT A16WE 1996122600323 19961226 00323 NM 1996 12 26 AWXA9600762 1 19961207 A 5315 69779421 FLOORBEAM BOEING 737 737277 1384570 NM BS 520 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 22646 DURING ROUTINE MAINTENANCE CHECK, FOUND CRACK FROM STOP DRILL HOLE OUTBOARD BS 520, LBL 24.75, WL 208. STOP DRILLED CRA CK FROM HOLE WL 208, LBL 24.75. NDI VERIFICATION OF CRACK CONTAINMENT PER D6-37239.6. REPAIRED FLOORBEAM BS 520 PER EO 53-14-12 AND SB 737-53-1120R1. 2 L 7 2 4F RT A16WE 1996122600324 19961226 00324 NM 1996 12 26 AWXA9600763 1 19961207 A 5315 FLOORBEAM BOEING 737 737277 1384570 NM BS 1016 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 22646 DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON BS 1016 FLOORBEAM ON UPPER CHORD LBL 7 TO RBL 39, WL 208. REPAIRED BS 1016 FLOORBEAM UPPER CHORD PER ER 2-53-15-53. ER REF TCO-PAN-96-1738RR 8110-3. 2 L 7 2 4F RT A16WE 1996122600325 19961226 00325 NM 1996 12 26 AWXA9600764 1 19961206 A 5320 65C807351 MOPSILL BOEING 737 737277 1384570 NM BS 970-1000 CORROSION A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 179AW 22646 DURING ROUTINE MAINTENANCE CHECK, FOUND RT MOPSILL AT AFT SERVICE DOOR HAS CORROSION BS 970 TO 1000, WL 208. REMOVED AN D REPLACED MOPSILL FROM BS 914 TO 1006, RBL 55, WL 208, IAW SRM 51-10-04. 2 L 7 2 4F RT A16WE 1996122600326 19961226 00326 EU 1996 12 26 AWXA9600765 1 19961219 A 3350 321430 BATTERY PACK AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 622AW 054 DURING ROUTINE MAINTENANCE CHECK, FOUND RT MID EMERGENCY BATTERY PACK FAILED TEST. REMOVED AND REPLACED BATTERY PACK, O PS CHECK GOOD. 2 L 7 2 4F RT A28NM 1996122600327 19961226 00327 NM 1996 12 26 AWXA9600766 1 19961219 A 3350 1060091101 LIGHT BOEING 737 7373G7 1384595 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 160AW 23782 DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT 2B EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED SEAT 2B EMERGENCY LIGHT ASSEMBLY, OPS GOOD STC - SA3432NM. 2 L 7 2 4F RT A16WE 1996122600328 19961226 00328 NM 1996 12 26 AWXA9600767 1 19961219 A 3397 WIRE BOEING 737 7373Q8 1384670 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 327AW 23507 DURING ROUTINE MAINTENANCE CHECK, FOUND FWD HALF OF CABIN EMERGENCY LIGHTS WILL NOT ILLUMINATE. REPAIRED WIRES AS REQUI RED, OPS CHECKED GOOD ON GROUND AT THIS TIME, STC - SA1889SO. 2 L 7 2 4F RT A16WE 1996122600329 19961226 00329 NM 1996 12 26 AWXA9600768 1 19961218 A 7931 BYPASS SW LINE BOEING 737 7372E3 NM NR 2 ENGINE LEAKING A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 28 138AW 22792 CAPTAIN CALLED OUTSIDE OF LAS AND INFORMED MX. CONTROL THAT THE NR 2 ENGINE OIL QUANTITY WAS SLOWLY DROPPING AND OIL PRE SSURE/TEMPERATURE WERE NORMAL. AIRCRAFT DIVERTED TO LAS. REMOVED AND REPLACED FILTER BYPASS SWITCH LINE, ADDED 10 QTS OIL FOR LOSS, LEAK CHECK GOOD PER MM. 2 L 7 2 4F RT A16WE 1996122600330 19961226 00330 WP 1996 12 26 CALA9601857 1 19961219 A 2497 3917032513 WIRE DOUG DC9 DC982 3022082 WP ELEC EQ COMP FAILED A CALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 09 478AC 48063 THE CIRCUIT BREAKER FOR CENTER FUEL TANK AFT BOOST PUMP POPPED AND ALL FUEL QUANTITY GAUGES WENT BLANK AT TAKEOFF. BOTH A AND B CHANNELS WERE BLANK. THE CIRCUIT BREAKER WAS RESET, BUT IT POPPED AGAIN. THE CIRCUIT BREAKER FOR FUEL QUANTIT Y POWER TRANSFER WAS PULLED AND RESET. THE AIRCRAFT WAS RETURNED TO EWR. MAINTENANCE FOUND THE RT MAIN AC BUS CIRCUIT BREAKER (B1-739) BAD AND A BURNT BUSING CABLE B7-5. THE CABLE AND CIRCUIT BREAKER WERE REMOVED AND REPLACED. 2 L 7 2 4F A6WE 1996122600331 19961226 00331 WP 1996 12 26 CALA9601858 1 19961219 A 2780 APG70005503 CONTROL VALVE DOUG DC10 DC1010 3022110 WP LT LE FLAPS INOPERATIVE A A CALA A UNSCHED LANDING F FLT CONT AFFECTED TO TAKEOFF 1 SW 09 68043 46902 WHEN SLATS WERE SELECTED TO RETRACT AFTER TAKEOFF, THE AIRCRAFT ROLLED SLIGHTLY TO THE RIGHT AND THE SLAT DISAGREE LIGHT REMAINED ILLUMINATED. A VISUAL INSPECTION CONFIRMED SLAT EXTENDED. SLATS WERE SELECTED TO EXTEND POSITION AND THE DIS AGREE LIGHT WENT OUT AT 15 DEGREES. THE AIRCRAFT WAS RETURNED TO HNL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REM OVED AND REPLACED THE LT OUTBOARD SLAT CONTROL VALVE PER MM 27-82-02, PAGE 201 TO 204. LEAK AND OPERATIONAL CHECKS WER E GOOD WITH NO DISAGREE LIGHT NOTED AT ALL FLAP SETTINGS. 2 L 7 3 4F A22WE 1996122600332 19961226 00332 NE 1996 12 26 96UAL900775 2 19961007 A 7314 MR73150155 FUEL PUMP SUNDSTRANDEM MR73150155 BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE FAILED A A UALA E ENGINE SHUTDOWN X ENGINE FLAMEOUT AP APPROACH 1 WP 29 511UA 0785 24799 ON APPROACH, LEFT ENGINE FLAMED OUT. ENGINE SHUTDOWN. *S/D* IMPROPER LAPPING OF BEARINGS BY THE OEM CAUSED THE FUEL G EAR STAGE BEARINGS TO BIND WITH THE HOUSING. UAL OVERHAULED AND REPLACED BEARINGS ON FUEL PUMPS PRODUCED DURING THE SA ME TIME PERIOD, OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996122600333 19961226 00333 EU 1996 12 26 96UAL900816 1 19961017 A 3350 BATTERY PACK GENERIC 321454 AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 432UA 6230 587 EMERGENCY LIGHTS FAIL CABIN INTERCOMMUNICATION DATA SYSTEM TEST ON NR 2 SERVICE. *S/D* REPLACED 11WL POWER SUPPLY AND BATTERY PACK. ALSO, REPLACED BATTERY PACK OVER DOOR 2L, OPERATIONALLY CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 1996122600334 19961226 00334 EU 1996 12 26 96UAL900817 1 19961017 A 2611 SMOKE ALARM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT MALFUNCTIONED A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 411UA 464 CREW REPORTED, ELECTRONIC CENTRALIZED AIRCRAFT MONITORING MESSAGE CARGO SMOKE DISCHARGE AGENT 2. *S/D* RECYCLED AIRCRA FT POWER AND THE MESSAGE CLEARED. NO FURTHER MESSAGES ENCOUNTERED. 2 L 7 2 4F 4 F RT A28NM E40NE 1996122600335 19961226 00335 NM 1996 12 26 96UAL900914 1 19961210 A 2750 CONTROL MECH BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE TE FLAPS DAMAGED A UALA K NONE O OTHER LD LANDING 1 WP 29 163UA 21353 AIRCRAFT EXPERIENCED A HARDER THAN NORMAL LANDING AT NRT. THE LANDING DAMAGED THE RT INBOARD TRAILING EDGE FLAP INSTALL ATION, FAILING AFT FLAP CONTROL RODS AT FLAP POSITION NR 5 AND NR 6 AND THE NR 6 MOVABLE FAIRING ACTUATOR ROD ATTACH FIT TING. ADDITIONALLY, THE RT INBOARD AILERON EDGE WAS DAMAGED DURING TAXI AS THE TRAILING EDGE FLAPS WERE RETRACTED. CAU SE WAS HARD LANDING. DAMAGED AFT FLAP CONTROL RODS, RT INBOARD AILERON AND MOVABLE FLAP FAIRING ACTUATOR ROD ATTACH FIT TING WERE REPLACED. (P/N 65B15651-6) ROD, (P/N 65B39035-2) FITTING, (P/N 65B02200) AILERON, (P/N 65B15950-5) ROD. 2 L 7 4 4F 4 F A20WE E20EA 1996122600336 19961226 00336 NM 1996 12 26 96UAL900924 1 19961207 A 2150 940114 PACK BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LEFT MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 780UA 26944 ON CLIMBOUT, LEFT AIR CONDITIONING PACK TRIPPED AT FLIGHT LEVEL 050. RESET PACK BUT TRIPPED AGAIN AT FL 250. DIVERTED TO LHR. *S/D* AIRCRAFT DEPARTED CDG WITH RIGHT AIR CYCLE MACHINE INOPERATIVE. AFTER DEPARTURE THE LEFT PACK FAILED AN D THE AIRCRAFT DIVERTED TO LHR. FAILURE WAS ISOLATED TO THE LEFT PACK FLOW SENSOR, (P/N 810230-2), WHICH WAS REPLACED. 2 L 7 2 4F 4 F RT T0001SE E46NE 1996122600337 19961226 00337 1996 12 26 96UAL900925 4 19961207 A 2300 RADIO SYST BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 516UA 24860 FLIGHT OFFICER'S RADIO SYSTEM BLOCKING ALL TRANSMISSIONS AND RECEPTIONS WHEN ACTIVATED. 2 L 7 2 4F 4 F RT A2NM E17NE 1996122600338 19961226 00338 NM 1996 12 26 96UAL900926 1 19961205 A 2530 201042401 OVEN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE GALLEY DAMAGED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 7260U 21407 RETURNED TO BOS DUE TO SMOKE IN COCKPIT. *S/D* STRONG SMOKE ODOR AND ELECTRICAL SMELL CAME FROM FORWARD GALLEY AREA. S MOKE COMING FROM INSIDE OVEN. FOUND COOKIE CONTAINER LIDS CHARRED. REPLACED OVEN AND CONTROLLER, GALLEY MODULE OPERATI ON NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1996122600339 19961226 00339 NM 1996 12 26 96UAL900927 1 19961207 A 7312 129474 FUEL HEAT VALVE BOEING 737 737291 138448W NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 980UA 21545 AFTER TAKEOFF, WITH APPLICATION OF NR 1 FUEL HEAT, WARNING LIGHT CAME ON BRIGHT, THEN DIM AND THEN BRIGHT AGAIN. NR 1 O IL TEMPERATURE CONTINUED TO RISE TO 130 DEGREES. FLIGHT RETURNED TO DEN. *S/D* REPLACED NR 1 ENGINE ANTI-ICE HEAT VAL VE, OPS CHECK GOOD. 2 L 7 2 4F 4 F A16WE E2EA 1996122600341 19961226 00341 NM 1996 12 26 96UAL900929 1 19961206 A 3234 GEAR HANDLE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE COCKPIT MALFUNCTIONED A UALA L ABORTED APPROACH J WARNING INDICATION LD LANDING 1 WP 29 7251U 21398 ON LANDING, GEAR EXTENSION ALL GEAR UNSAFE LIGHTS REMAINED ON. HANDLE WOULD NOT GO TO DETENT, MUSHY HANDLE AND MISSED A PPROACH. *S/D* JACKED AIRCRAFT AND PERFORMED SEVERAL GEAR SWINGS, INCLUDING TEST OF MANUAL GEAR EXTENSION SYSTEM. NO ABNORMALITIES NOTED. NO ABNORMALITIES NOTED IN OVER 90 SUBSEQUENT FLIGHT HOURS. 2 L 7 3 4F 4 F A3WE E2EA 1996122600342 19961226 00342 NM 1996 12 26 96UAL900930 1 19961211 A 2421 736664D IDG BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE RT ENGINE FAILED A UALA K NONE H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 WP 29 608UA 21869 DURING CRUISE ALTITUDE, THE INTEGRATED DRIVE GENERATOR DISCONNECTED ON THE RIGHT ENGINE. THE FLIGHT CONTINUED TO MIA. * S/D* THE RIGHT INTEGRATED DRIVE GENERATOR FAILED. THE IDG WAS REPLACED, OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 1996122600343 19961226 00343 NM 1996 12 26 96UAL900931 1 19961211 A 2120 AIR DISTR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN ODOR A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 586UA 26710 ODOR NOTICED MAIN CABIN DURING POWER CHANGES. MOST NOTICEABLE DURING TRANSITION FROM CRUISE TO IDLE. 2 L 7 2 4F 4 F RT A2NM E17NE 1996122600344 19961226 00344 NE 1996 12 26 96UAL900932 2 19961213 A 7200 ENGINE BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE NR 4 FAILED A UALA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 WP 29 163UA 21353 685969 NUMBER 4 ENGINE SHUTDOWN INFLIGHT DUE OIL FILTER BYPASS LIGHT. *S/D* ENGINE REPLACED, UNABLE TO DETERMINE CAUSE AT TH IS POINT IN TIME. 2 L 7 4 4F 4 F A20WE E20EA 1996122600345 19961226 00345 1996 12 26 96UAL900933 4 19961213 A 3441 HG1050AD05 IRU BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE E/E BAY MISALIGNED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 644UA 25094 THE AIRCRAFT RETURNED, DUE TO A FLIGHT MANAGEMENT COMPUTER NAVIGATION DISCREPANCY. *S/D* FLIGHT RECORDER DATA INDICATE D THAT THE FMC POSITION WAS APPROXIMATELY 34 NM NORTHEAST OF THE ACTUAL POSITION AFTER PUSHBACK. THE IRU WAS MISALIGNED , OPERATIONS CHECKED NORMAL AFTER REALIGNMENT. 2 L 7 2 4F 4 F RT A1NM E24NE 1996122600346 19961226 00346 NM 1996 12 26 96UAL900934 1 19961213 A 2730 PCU 6419913 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LT ELEVATOR FAILED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 7261U 21408 CONTROL YOKE BINDS RIGHT BEFORE FULL TRAVEL STOP IN NOSE DOWN ATTITUDE. MORE PRONOUNCED WITH A-SYSTEM PRESSURIZED. *S/ D* FOUND LEFT ELEVATOR HAD ERRATIC MOVEMENT AT END OF NOSE DOWN TRAVEL. REPLACED ELEVATOR POWER CONTROL UNIT. 2 L 7 3 4F 4 F A3WE E2EA 1996122600347 19961226 00347 1996 12 26 96UAL900935 4 19961213 A 2565 INFLATION TUBE AIR CRUISERS D28935103 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE SLIDE LEAKS A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7450U 179451178 21904 SLIDE REMOVED FOR AIR CRUISER SERVICE INFORMATION LETTER. DURING SHOP OVERHAUL INFLATION TUBE DEVELOPED A SEAM LEAK. S CRAPPED SLIDE. 2 L 7 3 4F 4 F A3WE E2EA 1996122600348 19961226 00348 1996 12 26 96UAL900936 4 19961213 A 2565 INFLATION TUBE AIR CRUISERS D28935103 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE SLIDE LEAKS A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7276U 179231078 21423 SLIDE REMOVED FOR AIR CRUISERS SERVICE INFORMATION LETTER. DURING SHOP OVERHAUL INFLATION TUBE DEVELOPED A SEAM LEAK. SCRAPPED SLIDE. 2 L 7 3 4F 4 F A3WE E2EA 1996122600349 19961226 00349 1996 12 26 96UAL900937 4 19961214 A 2565 D228935103 INFLATION TUBE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE SLIDE LEAKS A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7277U 21424 SLIDE REMOVED FOR AIR CRUISERS SERVICE INFORMATION LETTER. DURING SHOP OVERHAUL INFLATION TUBE DEVELOPED A SEAM LEAK. S CRAPPED SLIDE. 2 L 7 3 4F 4 F A3WE E2EA 1996122600350 19961226 00350 1996 12 26 96UAL900938 4 19961214 A 2565 D28935103 INFLATION TUBE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE SLIDE LEAKS A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7255U 21402 SLIDE REMOVED FOR AIR CRUISES SERVICE INFORMATION LETTER SIL 25-98. DURING SHOP OVERHAUL INFLATION TUBE DEVELOPED A SEA M LEAK. SLIDE SCRAPPED. 2 L 7 3 4F 4 F A3WE E2EA 1996122600351 19961226 00351 1996 12 26 96UAL900939 4 19961214 A 2565 D28935103 INFLATION TUBE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE SLIDE LEAKS A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7272U 21419 SLIDE REMOVED FOR AIR CRUISERS SERVICE INFORMATION LETTER 25-98. DURING SHOP OVERHAUL INFLATION TUBE DEVELOPED A SEAM LEAK. SLIDE SCRAPPED. 2 L 7 3 4F 4 F A3WE E2EA 1996122600352 19961226 00352 1996 12 26 96UAL900940 4 19961214 A 2565 D28935103 INFLATION TUBE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE SLIDE LEAKS A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7271U 21418 SLIDE REMOVED FOR AIR CRUISERS SERVICE INFORMATION LETTER 28-98. DURING SHOP OVERHAUL INFLATION TUBE DEVELOPED A SEAM L EAK. SLIDE SCRAPPED. 2 L 7 3 4F 4 F A3WE E2EA 1996122600353 19961226 00353 NM 1996 12 26 DL72S962700 1 19961213 A 3350 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 539DA 22385 FOUND EMERGENCY FLASH LIGHT INOP DURING LAYOVER. REPLACED EMERGENCY FLASHLIGHT AND BATTERY. 2 L 7 3 4F A3WE 1996122600354 19961226 00354 NM 1996 12 26 DL76S962701 1 19961216 A 2150 460500 BY PASS VALVE BOEING 767 767332 1382001 NM RT PACK BROKEN A DALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 27 116DL 23275 ON CLIMBOUT, GOT A RT DUCT LEAK LIGHT AND ASSOCIATED EICAS MSG AFTER ISOLATION PROCEDURE WAS DONE, LIGHT REMAINED ON AND RT PACK STAYED ON. FOUND RT ISOLATION BYPASS VALVE BROKEN. REPLACED SAME. REPLACED SEALS ON SLIP JOINT OUTBOARD OF R T ISOLATION CHECK VALVE. 2 L 7 2 4F RT A1NM 1996122600355 19961226 00355 NM 1996 12 26 DLM88962702 1 19961217 A 2611 SMOKE DETECTOR DOUG MD88 MD88 3023688 NM AFT LAV MALFUNCTIONED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 998DL 53370 ON PUSH BACK, AFT LAV COPILOTS SIDE SMOKE ALARM WENT OFF. LIGHT SMOKE CAME INTO MID CABIN. APU HAD BEEN STARTED 11 MIN PRIOR TO PUSH BACK AND PACKS OPERATED 4 TO 5 MIN. BEFORE PUSH BACK PACK TEMP GAUGE AT 90 DEG. RETURNED TO GATE WITH P ACKS OFF, HAD PAX DEPLANE. RAN LEFT/RIGHT PKS WITH APU AIR, NO SMOKE NOTICED. REPLACED RT REAR LAV SMOKE DETECTOR RAN PACKS WITH ENGINES RUNNING, NO SMOKE. 2 L 7 2 4F RT A6WE 1996122600356 19961226 00356 NM 1996 12 26 DL72W962704 1 19961217 A 5720 STIFFENER BOEING 727 727247 138408F NM LT FRONT SPAR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2813W 20869 A 1.75 INCH CRACK AT FRONT SPAR VERTICAL STIFFENER NR 3 SLAT I/B TRACK. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1996122600357 19961226 00357 NM 1996 12 26 DL72W962705 1 19961217 A 2782 BRACKET BOEING 727 727247 138408F NM NR 1 LE FLAP ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2813W 20869 FOUND ON B1 LETTER CK, .5 INCH CRACK AT NR 1 L/E FLAP ACTUATOR MOUNT BRACKET UPPER INBD CORNER. REPAIRED PER MM 57-20-2 1. 2 L 7 3 4F A3WE 1996122600358 19961226 00358 WP 1996 12 26 DLL15962706 1 19961218 A 3350 337201959 SOCKET LKHEED 1011 10113853 5265020 WP CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 755DL 193Y1184 EMERGENCY PATH LIGHTS SOCKET BROKEN AT ROW 22G AND 27C. INSTALLED NEW LIGHT SOCKETS, OPS CHECK OK. 2 L 7 3 4F A23WE 1996122600359 19961226 00359 NM 1996 12 26 DL73K962707 1 19961211 A 5320 65479592 DOOR FRAME BOEING 737 737232 1384475 NM BS 794.3 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 322DL 23094 THE AFT CARGO DOOR OPENING FORWARD FRAME STA 794.3 WAS FOUND WITH A 1 INCH CRACK AT THE NR 5 STOP FITTING. THE FRAME IS MADE FROM A 0.071 7075-T6 CLAD MATERIAL. THIS ER/A WILL ALLOW THE USE OF THE SRM TYPICAL FORMED SECTION REPAIR ON A TIM E LIMITED BASIS. 2 L 7 2 4F RT A16WE 1996122600360 19961226 00360 NM 1996 12 26 DL73K962708 1 19961211 A 5312 651630084 BULKHEAD WEB BOEING 737 737232 1384475 NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 313DL 23085 SIX CRACKS WERE FOUND ON THE FWD FACE OF THE FS 178 BULKHEAD WEB. THREE INDEPENDENT CUTOUTS WERE REQUIRED TO REMOVE THE CRACKS. TWO CUTOUTS MEASURE 5.O VERTICALLY BY 1.0 INBOARD-OUTBOARD AT WL 197 TO WL 202 AND ARE AT THE LBL 5.7 AND RBL 5.7 VERTICAL STRAP POSITIONS. THE THIRD CUTOUT IS LOCATED AT THE BL 0 VERTICAL STRAP POSITION FROM WL 187 TO WL 190 AND MEASURES 2.5 VERTICALLY BY 2.75 INBOARD-OUTBOARD. 2 L 7 2 4F RT A16WE 1996122600361 19961226 00361 NM 1996 12 26 DL73K962709 1 19961215 A 5312 BULKHEAD WEB BOEING 737 737232 1384475 NM BS 178 FATIGUE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 322DL 23094 THE STATION 178 BULKHEAD WEB WAS FOUND CRACKED IN SEVERAL LOCATIONS. DAMAGE CUTOUT DIMENSIONS ARE: 1 BY 4 FOR RBL 5.7 A T WL 198 TO 201; 1 BY 4 FOR LBL 5.7 AT WL 198 TO 201; AND 2 BY 1 FOR RBL 1 AT WL 188. DIMENSIONS ARE I/B TO O/B VERTI CALLY RESPECTIVELY. THE BULKHEAD WEB IS MANUFACTURED FROM .032 CLAD 2024-T3. 2 L 7 2 4F RT A16WE 1996122600362 19961226 00362 NM 1996 12 26 DL72W962711 1 19961208 A 5330 65545662 SKIN BOEING 727 727247 138408F NM BS 486 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2821W 21059 FOUND CORROSION ON FUSELAGE SKIN AT STA 486. REPAIRED IN ACCORDANCE DAL ER/A 258313-14, REV A. 2 L 7 3 4F A3WE 1996122600363 19961226 00363 NM 1996 12 26 DL72W962712 1 19961203 A 5330 65545662 SKIN BOEING 727 727247 138408F NM BS 580 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2821W 21059 FOUND CORROSION ON THE LOWER EDGE OF THE C-1 DOOR CUTOUT AT STATION 580. REPAIRED PER DAL ER/A 304497-14, REV A. 2 L 7 3 4F A3WE 1996122600364 19961226 00364 NM 1996 12 26 DL76L962715 1 19961213 A 5414 311T3450 SKIN BOEING 767 767332 1382001 NM NR 2 ENG STRUT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 176DN 25061 A 2 INCH CRACK WAS FOUND IN THE NR 2 ENGINE PYLON O/B STRUT SKIN. THE CRACK EMANATES FROM THE FWD TORQUE BOX ACCESS HOL E. THE CRACK WAS REPAIRED PER A BAC MOD DWG. REV E TO ER/A PROVIDES BAC DER FAA APPROVAL. 2 L 7 2 4F RT A1NM 1996122600365 19961226 00365 NM 1996 12 26 DL76S962716 1 19961213 A 5754 114T4105 SKIN BOEING 767 767332 1382001 NM NR 8 LE FLAP DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 132DN 24981 THE NR 8 L/E SLAT T/E WEDGE WAS FOUND WITH UPPER SKIN DELAMINATION. THE DELAMINATED AREA WAS TRIMMED OUT AND REPAIRED P ER SRM 57-43-02, FIG 201. 2 L 7 2 4F RT A1NM 1996122600366 19961226 00366 NM 1996 12 26 DL76L962717 1 19961209 A 5414 311T3450 SKIN BOEING 767 767332 1382001 NM NR 1 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 176DN 25061 A CRACK WAS FOUND IN THE NR 1 PYLON I/B STRUT SKIN EMANTING FROM THE TORQUE BOX ACCESS HOLE. THE CRACK WAS REPAIRED PER BAC MOD DWG 311T3401. 2 L 7 2 4F RT A1NM 1996122600367 19961226 00367 WP 1996 12 26 DLL15962718 1 19961203 A 5330 1608987105 SKIN LKHEED 1011 10113853 5265020 WP BS 983 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 754DL 193Y1181 THE FUSELAGE SKIN WAS FOUND CRACKED UNDER THE RT EXTERNAL FUSELAGE TO WING BOX LONGERON. THE CRACK IS THROUGH TWO ATTAC HMENT HOLES COMMON TO THE STA 983 BULKHEAD CAP. THE CRACK WAS STOP DRILLED AND REPAIRED WITH DOUBLERS. 2 L 7 3 4F A23WE 1996122600368 19961226 00368 WP 1996 12 26 DLL15962719 1 19961211 A 5730 1605382101 SKIN LKHEED 1011 10113853 5265020 WP BS 1212 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 754DL 193Y1181 THE UPPER SURFACE OF THE CENTER WING SKIN BETWEEN RBL AND LBL 94.5 AND 115.8 WAS FOUND CORRODED FROM THE FRONT SPAR TO T HE REAR SPAR AT FS 1212. THE CORROSION WAS BLENDED OUT AND SHOWN GOOD. 2 L 7 3 4F A23WE 1996122600369 19961226 00369 WP 1996 12 26 DLL15962720 1 19961118 A 5312 1503621 FRAME LKHEED 1011 10113853 5265020 WP PRESS DOME CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 754DL 193Y1181 THE P-DOME ZEE FRAME BETWEEN S-29 AND S-37 WAS FOUND CORRODED AND IN NEED OF REPLACEMENT. A NEW SECTION WAS SPLICED IN. 2 L 7 3 4F A23WE 1996122600370 19961226 00370 WP 1996 12 26 DLL15962722 1 19961202 A 5711 1605415102 SPAR LKHEED 1011 10113853 5265020 WP WS 320 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 754DL 193Y1181 SEVERAL HOLES IN THE RT REAR SPAR, UPPER CAP AND UPPER WING SKIN WERE FOUND CRACKED FROM THE FASTENER HOLES. 2 L 7 3 4F A23WE 1996122600371 19961226 00371 WP 1996 12 26 DLL15962723 1 19961111 A 5312 LS13112 PRESS DECK LKHEED 1011 10113853 5265020 WP BS 378 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 754DL 193Y1181 THE FUSELAGE HORIZ PRESSURE DECK PANEL WAS FOUND WITH A 1 INCH LONG CRACK AT RBL 102, JUST AFT OF FS 378. THE CRACK WAS CUTOUT AND REINFORCED WITH DOUBLERS. 2 L 7 3 4F A23WE 1996122600372 19961226 00372 NE 1996 12 26 DL76L962726 2 19961218 A 7530 VANE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 171DN 24759 724149 FOUND ON GROUND INSP, EXIT VANES DAMAGED/MISSING AND INTERMED CASE FAIRING DAMAGE. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 1996122600373 19961226 00373 NE 1996 12 26 DLL10962727 2 19961218 A 7200 ENGINE LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B02 54555 NE NR 1 TAILPIPE FIRE A DALA D RETURN TO BLOCK A FLAME/FIRE TX TAXI/GRND HDL 1 SO 27 729DA 193C1180 10652 NR 1 ENG TAILPIPE FIRE ON START. GROUND CREW FIRED HALON INTO TAILPIPE. TAILPIPE FIRE/ENGINE RUNDOWN CHECKLIST COMPLIE D WITH. ENGINE WAS INSPECTED PER M/M AND RETURNED TO SERVICE. 2 L 7 3 4F 4 F A23WE E12EU 1996122600374 19961226 00374 NM 1996 12 26 DL72S962728 1 19961218 A 3310 BAC106075211 BALLAST BOEING 727 727232 1384082 NM COCKPIT MELTED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 494DA 21074 JUST AFTER LEVEL OFF AT FL230, NOTED SMOKE IN THE COCKPIT COMING FROM BEHIND S/O PANEL. SMOKE STOPPED AFTER 2 TO 3 MINU TES. AT THE GATE NOTICED PANEL FLOOR C/B POPPED. FOUND PANEL FLOOR BALLAST M354 MELTED AND CONTROL PANEL FLOOR C/B POPPED. REPLACED BALLAS, OPS CK GOOD. 2 L 7 3 4F A3WE 1996122600375 19961226 00375 NM 1996 12 26 DLM88962730 1 19961218 A 3222 STRUT 5952247504 DOUG MD88 MD88 3023688 NM NLG REQD SERVICE A DALA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 980DL 53267 10652 AFTER T/O, NOSE GEAR WOULD NOT RETRACT. CYCLED GEAR DOWN, ALL THREE GREEN, RAISED GEAR, MAINS UP AND LOCKED, NOSE GEAR UNSAFE RED. REPLACED RT NOSE GEAR SPRAY DEFLECTOR AND SERVICED NOSE GEAR STRUT. SWUNG NOSE GEAR, OPS CKS OK. 2 L 7 2 4F RT A6WE 1996122600376 19961226 00376 NM 1996 12 26 DL757962731 1 19961209 A 5415 310N302626 BUSHING BOEING 757 757232 1384965 NM NR 2 ENG PYLON WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 653DL 24393 10652 DURING ACCOMPLISHMENT OF INSPECTION PER OPN 8201, OUTBOARD MIDSPAR FITTING BUSHING ON THE NR 2 ENGINE WAS FOUND TO HAVE MIGRATED .150 AND WAS LOOSE. THIS ER/A AUTHORIZES REPLACEMENT OF THE BUSHING PER BACO S/B 757-54-0026. DIA OF OUTBOARD LUG PRIOR TO REWORK WAS 1.8420. AFTER REWORK, INSURANCE CUT AND HONGIN, DIA WAS 1.8520. THIS IS WITHIN LIMITS GIVEN I N BACO TWX DAL-ATL-96-1821RR, DATED 12-05-96. 2 L 7 2 4F RT A2NM 1996122600377 19961226 00377 NM 1996 12 26 DL767962732 1 19961217 A 5330 SKIN BOEING 767 767232 1385132 NM BS 1542 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 102DA 22214 10652 NR 95 CORROSION THROUGH FUSELAGE SKIN AT STA 1542 STR 35. NR 177 THROUGH 182 WRITTEN FOR STRINGER DAMAGE STR 34L THROUG H 39L WILL REPAIR PER ERA 360836-14 AS OF 12/19/96 ERA PENDING FAA APPROVAL. 2 L 7 2 4F RT A1NM 1996122600378 19961226 00378 NM 1996 12 26 DL767962733 1 19961218 A 2912 291001372 HYD FILTER 271T00424 BOEING 767 767232 1385132 NM RT MLG CRACKED A DALA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 SO 27 105DA 00605 22217 ON TAXI OUT, LOSS OF CENTER HYDR QTY WENT TO ZERO AND SYS PRESS LIGHT CAME ON. FOUND C-SYS HYD MODULE AFT BLEW ELEMENT CASE CAUSING HYD FAILURE OF C-SYS. REPLACED EDP FILTERS AND MODULE. 2 L 7 2 4F RT A1NM 1996122600380 19961226 00380 NM 1996 12 26 DL72W962735 1 19961218 A 5754 651622296 SKIN BOEING 727 727247 138408F NM NR 6 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2807W 20579 INNER SKIN CRACKED BETWEEN RIBS 10/11. REPAIRED PER M/M 57-54-0. 2 L 7 3 4F A3WE 1996122600381 19961226 00381 NM 1996 12 26 DL76L962736 1 19961218 A 4900 APU BOEING 767 767332 1382001 NM MLG WW FAILED A DALA F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 186DN 27962 36674 AT GATE, APU MADE EXPLOSION NOISE AND GEN DROPPED OFF LINE, AIRPLANE SHOOK AND EXHAUST SMOKE OBSERVED. PULLED APU FIRE HANDLE. MAINT DETERMINED APU TO BE AN INTERNAL FAILURE, REMOVED APU. 2 L 7 2 4F RT A1NM 1996122600382 19961226 00382 NM 1996 12 26 DL757962738 1 19961218 A 3350 POWER SUPPLY 20131A BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 669DN 948 25142 10652 LT EMERGENCY OVERWING INOP. REPLACED EMERGENCY POWER SUPPLY BATTERY PACK, OPS CHECKS GOOD PER MM. 2 L 7 2 4F RT A2NM 1996122600383 19961226 00383 NM 1996 12 26 DL72W962740 1 19961213 A 5210 SKIN BOEING 727 727247 138408F NM L1 DOOR BENT A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2817W 20873 36674 L-1 DOOR EXT SKIN UPPER AFT CORNER BENT. STRAIGHTENED METAL, DYE-CHECKED FOR CRACKS PER PS 400-6-3. REPAIRED PER M/M 5 2-10-01 FIGURE 804, PG 806. 2 L 7 3 4F A3WE 1996122600384 19961226 00384 NM 1996 12 26 DL72S962741 1 19961003 A 5753 652163262 SPAR BOEING 727 727232 1384082 NM RT TE FLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 404DA 21148 36674 FOUND DAMAGE ON RT FLAP. REPLACED AFT SPAR SECTION 0 TO 54 FROM I/B END OF FLAP PER M/M 57-52-0, TASK BN BO. 2 L 7 3 4F A3WE 1996122600385 19961226 00385 NM 1996 12 26 SCNA96441 1 19961217 A 3350 POWER STRIP BOEING 727 727259 138408J NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 AFT 10 FEET OF EMERGENCY FLOOR TRACK LIGHTING WAS FOUND VERY DIM. REMOVED AND REPLACED AFT POWER STRIP UNDERNEATH TRACK LIGHTS. ALSO, REPLACED ONE TRACK LIGHT STRIP JUST FORWARD OF THE L2 DOOR. SYSTEM OPS CHECKED NORMAL IN ACCORDANCE WIT H MM 33-50-00. 2 L 7 3 4F A3WE 1996122600386 19961226 00386 WP 1996 12 26 SCNA96442 1 19961206 A 5320 CLIP DOUG DC10 DC1015 3022118 WP BS 559-595 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING HEAVY MAINTENANCE, CORROSION WAS FOUND ON AN INTERCOSTAL AND CLIPS BETWEEN FS 559 AND 595, APPROXIMATELY LONGERON 44L. CLEANED CORROSION, FABRICATED AND INSTALLED A NEW CLIP IN ACCORDANCE WITH SRM 53-60-00. 2 L 7 3 4F A22WE 1996122600387 19961226 00387 WP 1996 12 26 SCNA96443 1 19961205 A 5712 RIB DOUG DC10 DC1015 3022118 WP LT WING TORN A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING HEAVY MAINTENANCE, FOUND TORN METAL ON THE LEFT HAND WING LEADING EDGE, INBOARD OF THE NUMBER 8 SLAT, INBOARD TRA CK. INNER RIB REMOVED AND A NEW RIB FABRICATED PER DC10 BLUEPRINT AND INSTALLED PER 51-31-01 AND 51-33-01. 2 L 7 3 4F A22WE 1996122600388 19961226 00388 WP 1996 12 26 SCNA96444 1 19961210 A 5320 SUPPORT DOUG DC10 DC1015 3022118 WP BS 824 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT FS 824, RBL 36 UNDER MID GALLEY. REMOVED FLOOR SUPPORT, F ABRICATED AND INSTALLED A NEW FLOOR SUPPORT IN ACCORDANCE WITH SRM 51-21-01 AND 51-33-01. 2 L 7 3 4F A22WE 1996122600389 19961226 00389 WP 1996 12 26 SCNA96445 1 19961210 A 5320 SUPPORT DOUG DC10 DC1015 3022118 WP BS 879 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING HEAVY MAINTENANCE, FOUND MID GALLEY FLOOR SUPPORT CORRODED AT FS 879 RBL 36. REMOVED AND REPLACED FLOOR SUPPORT IN ACCORDANCE WITH SRM 53-60-01 AND SRM 51-30-00. 2 L 7 3 4F A22WE 1996122600390 19961226 00390 WP 1996 12 26 SCNA96446 1 19961205 A 5320 SUPPORT DOUG DC10 DC1015 3022118 WP BS 807-897 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING HEAVY MAINTENANCE, FOUND MID GALLEY FLOOR SUPPORT AT FS 791 AND FS 814, RBL 38 CORRODED ON TOP SURFACE. REMOVED AND REPLACED FLOOR SUPPORT FROM FS 735 TO FS 1039 AND FABRICATED SPLICES AT FS 807 AND 897 IN ACCORDANCE WITH ENGINEERIN G AUTHORIZATION AND SRM 51-30-00. 2 L 7 3 4F A22WE 1996122600391 19961226 00391 NM 1996 12 26 DHL96741004 1 19961219 A 5280 6516306138 DOOR SEAL BOEING 727 7272Q9 138448M NM NLG WW FROZEN A DHLA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 741DH 21931 ON APPROACH, NOSE GEAR DOOR LIGHT ILLUMINATED WITH GEAR LOWERING AND WOULD NOT EXTINGUISH WHEN GEAR WAS DOWN AND LOCKED. ALSO, RED GEAR DOOR LIGHT ILLUMINATED. VISUALLY CHECKED GEAR DOWN AND LOCKED INDICATOR AFTER GO-AROUND. INDICATOR I NDICATED DOWN AND LOCKED. CLEANED ICE FROM SEAL, DRIED SEAL AND REINSTALLED PER M/M 20-80-0. DOOR WARNING SYSTEM CHECK S OK PER M/M 32-20-0. 2 L 7 3 4F RT A3WE 1996122600392 19961226 00392 1996 12 26 DHL96807003 4 19961003 A 2310 SA20535004 ARRESTOR DOUG DC8 DC873F 302199F WP NR 2 HF FAILED A DHLA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 807DH 45990 DURING CRUISE, NR 2 HF DOES NOT RECEIVE, TRANSMITS OK. REPLACED LIGHTNING ARRESTOR, OPS CHECK GOOD PER M/M 23-10. 2 L 7 4 4F RT 4A25 1996122600393 19961226 00393 SO 1996 12 26 SWIA95780 1 19961119 A 5246 FASTENERS EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE FUEL DOOR FAILED A SWIA D RETURN TO BLOCK O OTHER TO TAKEOFF 1 NM 07 194SW 120120 SERVICE DOOR LIGHT CAME ON SHORTLY AFTER DEPARTURE. RETURNED TO AIRPORT. CAMLOC POPPED. REPLACED BOTH RECEPTACLES FOR PRESSURE FUELING OUTBD DOOR, CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1996122600394 19961226 00394 SO 1996 12 26 SWIA95781 1 19961121 A 5246 LATCH EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE FUEL DOOR NOT LATCHED A SWIA D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 NM 07 194SW 120120 SERVICE DOOR LIGHT CAME ON DURING TAKEOFF. ABORTED TAKEOFF. LIGHT WENT OUT. FOUND LATCH ON FORWARD OUTBOARDD FUEL DOO R NOT LATCHED. INSPECTED DOOR AND LATCH RECEPTACLE. ADJUSTED AND OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1996122600395 19961226 00395 SO 1996 12 26 SWIA95782 1 19961122 A 3080 D55201001 DE-ICE MONITOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE E/E COMPT MALFUNCTIONED A SWIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 NM 07 232SW 120306 DURING TAKEOFF ROLL, PRIOR TO ROTATION MAP DE-ICE LIGHT ILLUMINATES AS WELL AS OVERHEAD BOOTS PROPELLER AND ENGINE AIR L IGHT REMAIN ON. REPLACED DE-ICE MONITOR PERFORM OPS CHECKS GOOD. ALL DE-ICE SYSTEMS WITH BOTH ENGINE RUNNING AT HIGH POWER SETTING, OPS CHECKS GOOD AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 1996122600396 19961226 00396 SO 1996 12 26 SWIA95784 1 19961128 A 3150 AURAL WARNING EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE COCKPIT SOUNDED A SWIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 NM 07 213SW 120277 ON TAKEOFF ROLL, TRIM AURAL WARNING SOUNDED, ABORTED TAKEOFF. RESET AURAL WARNING CIRCUIT BREAKER, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1996122600397 19961226 00397 SO 1996 12 26 SWIA95786 1 19961201 A 2910 HYDRAULIC SYS EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE GREEN HYD SYST REQD SERVICE A SWIA O OTHER J WARNING INDICATION TO TAKEOFF 1 NM 07 203SW 120240 ON TAKEOFF, GOT GREEN SYSTEM LOW LEVEL LIGHT, GAUGE SHOWED EMPTY BUT PRESSURE REMAINED NORMAL. SERVICED GREEN SYSTEM HY DRAULICS TO CORRECT LEVEL AND LOW LEVEL LIGHT WAS EXTINGUISHED. 2 L 7 2 4T 4 T RT A31SO E20NE 1996122600398 19961226 00398 EA 1996 12 26 SWIA95788 1 19961202 A 5210 LATCH MECH CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE PAX DOOR LACK OF LUBE A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 413SW 7102 ON DEPARTURE, PASSENGER DOOR STOW AMBER CAUTION LIGHT CAME ON. RETURNED FOR LANDING. MEL 52-70-1, LUBED PASSENGER DOOR INTERNAL LATCH MECHANISM. OPS AND INDICATION CHECKS GOOD PER MM 52-11-02. 2 L 7 2 4F 4 F RT A21EA E15NE 1996122600399 19961226 00399 SO 1996 12 26 SWIA95789 1 19961207 A 2751 DISAGREE LIGHT EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE TE FLAPS MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 215SW 120281 ON DEPARTURE AFTER SELECTING FLAPS UP, RECEIVED DISAGREEMENT LIGHT. PERFORMED ORH PROCEDURES, DISAGREEMENT DID NOT GO A WAY. UPON LANDING DISAGREEMENT WENT OUT. INSPECTED FLAP ROLLERS AND TRACKS OPS CHECKS IN MAINT MODE. NO FAULTS FOUND. CYCLED FLAPS NUMEROUS TIMES, OPS CHECKS PER MM 27-50-00. 2 L 7 2 4T 4 T RT A31SO E20NE 1996122600400 19961226 00400 NM 1996 12 26 P5CA9601250 1 19961218 A 5230 DOOR BOEING 747 747124 1384874 NM FWD CARGO BENT A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 GROUND DAMAGE FORWARD CARGO DOOR BENT UP BY CARGO LOADER AT LOWER AFT CORNER APPROXIMATELY 8 TO 10 INCH LENGTH. INSTALL ED OUTSIDE SKIN DOUBLER AS PER BOEING SRM 51-40-03 AND PRESS CHECKED PER BOEING M/M 21-00-00. 2 L 7 4 4F A20WE 1996122600401 19961226 00401 SO 1996 12 26 SRAA961211 1 19961219 A 6120 VALVE HOUSING LKHEED 382 382E 526413U SO NR 2 ENGINE FAILED A SRAA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 GL 23 908SJ 4300 ON CLIMBOUT, AT FL 175 NR 2 PROP RPM WENT TO 105 PERCENT. SHUT DOWN NR 2 ENGINE AND CONTINUED TO DESTINATION. AIRCRAFT LANDED AT TOL WITHOUT INCIDENT. REPLACED PROP VALVE HOUSING ASSY AND OPERATIONAL CHECKED PER MM CH 61. 2 H 7 4 4T A1SO 1996122600402 19961226 00402 EU 1996 12 26 96ZZZX6151 2 19961205 A 7250 ENGINE HWKSLY DH125 BH125600A 4210101 EU RROYCE VIPER VIPER60122 54551 EU RT ENG FAILED A B7PA A UNSCHED LANDING J Y WARNING INDICATION ENGINE STOPPAGE CR CRUISE 1 NE 05 523MA 256023 VL601184 PILOTS REPORT LOUD BANG FOLLOWED BY LOSS OF POWER ON RT ENGINE FAILURE AT 1843Z 12-05-96. AFTER A/C LANDED, PILOTS REPO RT TURBINE WHEEL DAMAGE. SUBMITTER STATED UNABLE AT THIS TIME TO DETERMINE WHAT CAUSED THE FAILURE. A/C LANDED AT MADI SON,WI WITHOUT INCIDENT. A FOLLOW-UP REPORT WILL BE MADE AS SOON AS INFO IS AVAILABLE. 2 L 7 2 4J 4 J A3EU E15EU 1996122600403 19961226 00403 EA 1996 12 26 96ZZZX6152 1 19961121 A 3231 MS141014 PUSH/PULL ROD CNDAIR CL600 CL6002B16 1900305 EA RT MLG DOOR BENT A J7SA O OTHER J WARNING INDICATION CL CLIMB 1 SW 21 306FX 750 5175 ON TAKEOFF FROM (APA) AIRCRAFT LANDING GEAR DISPLAYED A TRANSIT LIGHT IN GEAR HANDLE. AFTER AN UNEVENTFUL LANDING IN DE N, THE RIGHT GEAR DOOR LINKAGE WAS DETERMINED TO BE DAMAGED. 2 L 7 2 4F RT A21EA 1996122600419 19961226 00419 EU 1996 12 26 96ZZZX6167 1 19961206 A 3241 40921 TRANSDUCER ISRAEL 1124 1124 4500102 EU RT MLG ANTI SKID CONTAMINATED A W3NA O OTHER J WARNING INDICATION LD LANDING 1 GL 25 1124F 281 RIGHT ANTI-SKID FAILED ON LANDING. FOUND TRANSDUCER CONTAMINATED WITH METAL FILLINGS. FOUND THE SAFETY WIRE FROM THE A XLE NUT HAD SHIFTED AND RUBBED ON HUB CAP. CLEANED TRANSDUCER AND CANNON PLUG. RESAFTIED AXLE NUT. SYSTEM OPERATIONAL CHECKED SATISFACTORY. 2 M 7 2 4F A2SW 1996122600427 19961226 00427 EU 1996 12 26 HCMA9670 1 19961119 A 6520 350A33215300 LAMIFICATION SNIAS 350 AS350B2 8680813 EU REAR ROTOR TORN E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 992BH 71 2889 REAR ROTOR LAMIFICATION IS TORN BEYOND LIMITS. 1 G 7 1 3U H9EU 1996122600428 19961226 00428 GL 1996 12 26 HEEA968762 2 19961217 A 7230 23056634 GEARSHAFT 23033191 BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL SPUR ADAPTER STEP WEAR E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 27702 195 CAC70781 45300 CAE860520 ENGINE REMOVED DUE TO METAL IN OIL. UPON INSPECTION OF COMPRESSOR PARTS NOTED THE FOLLOWING: STEP WEAR BEYOND SERVICEA BLE LIMITS ON SHAFT AFT SPLINES. INSTALLED A USED SERVICEABLE PART. 1 G 7 1 3U 3 U H2SW E1GL 1996122600429 19961226 00429 GL 1996 12 26 HEEA968763 2 19961217 A 7230 23056634 GEARSHAFT 23051643 SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL SPUR ADAPTER STEP WEAR E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 706AE 646 CAC91649 760275 CAE890627S ENGINE REMOVED DUE TO CYCLED OUT 1ST AND 2ND STAGE WHEELS. UPON VISUAL INSPECTION OF COMPRESSOR NOTED THE FOLLOWING: S TEP WEAR BEYOND SERVICEABLE LIMITS ON SHAFT AFT SPLINES. INSTALLED A USED SERVICEABLE PART. 1 G 7 2 3U 3 U H1NE E1GL 1996122600430 19961226 00430 GL 1996 12 26 HEEA968764 2 19961217 A 7230 23056634 GEARSHAFT 23051643 SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL SPUR ADAPTER STEP WEAR E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545K 374 CAC90703 760047 CAE890555S ENGINE REMOVED DUE TO CRACKED SCROLL. UPON VISUAL INSPECTION OF COMPRESSOR NOTED THE FOLLOWING: STEP WEAR BEYOND SERVI CEABLE LIMITS ON SHAFT AFT SPLINES. INSTALLED A USED SERVICEABLE PART. 1 G 7 2 3U 3 U H1NE E1GL 1996122600431 19961226 00431 NM 1996 12 26 AWXA9600769 1 19961220 A 3397 WIRE BOEING 737 737297 1384480 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 147AW 22630 DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT MOUNTED EMERGENCY LIGHT AT ROW 13 INOPERATIVE. REPAIRED SEAT WIRING. OPS GOOD. STC - SA3432NM. 2 L 7 2 4F A16WE 1996122600432 19961226 00432 1996 12 26 CALA9601859 4 19961220 A 2320 RDAX5321 DECODER DOUG DC10 DC1030 3023501 WP CABIN FAILED A CALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 19072 46576 THE SECOND OFFICER WAS NOTIFIED THAT THE READING LIGHTS IN MIDDLE SECTION OF COACH WERE INOPERATIVE WHILE IN FLIGHT. TH E CIRCUIT BREAKER FOR THE READING LIGHTS WAS OUT. IT WAS RESET AND BEGAN FUNCTIONING. A BURNING SMELL AND SMOKE WERE THEN OBSERVED. THE FLIGHT ATTENDANT REPORTED HEARING AN ARCING NOISE, THE SECOND OFFICER REPULLED THE CIRCUIT BREAKER , THE SMELL AND SMOKE DISSIPATED. THE FLIGHT WAS CONTINUED TO LGW WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND TH E OVERHEAD DECODER AND THE PLUGS AND WIRING TO THE DECODER CHARED. THE OVERHEAD DECODER WAS REPLACED. THE OVERHEAD CAB LES WERE REPLACED. THE SEAT ENCODER WAS ALSO REPLACED. THE CIRCUIT BREAKER WAS RESET. OPERATIONAL CHECKS WERE GOOD. 2 L 7 3 4F A22WE 1996122600433 19961226 00433 NM 1996 12 26 CALA9601860 1 19961220 A 2782 1U1110 ACTUATOR BOEING 727 727224 1384076 NM NR 5 LE FLAP LEAKING A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 93738 45896 5602 20666 THE A-HYDRAULIC SYSTEM WAS LOST WHILE EN ROUTE FROM IAH TO AUS. THE LOSS WAS ACCOMPANIED BY ILLUMINATION OF PUMP LOW PRE SSURE LIGHTS 1 AND 2. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 5 L/ E FLAP ACTUATOR SEALS BLOWN. THE ACTUATOR WAS REMOVED AND REPLACED. THE HYDRAULIC SYSTEM WAS SERVICED TO FULL. LEAK A ND OPERATIONAL CHECKS WERE GOOD. PART TOTAL CYCLES, 31,400. 2 L 7 3 4F A3WE 1996122600434 19961226 00434 NM 1996 12 26 CALA9601861 2 19961222 A 7260 BACP11P216 SEAL BOEING 747 747230B 1384889 NM PWA JT9 JT9D7A 52054 NE NR 4 ENGINE LEAKING A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 78019 20527 662507 THE NR 4 ENGINE OIL PRESSURE BEGAN TO DROP WHILE EN ROUTE FROM HNL TO NRT. THE ENGINE OIL PRESSURE LIGHT WAS INTERMITTE NT WHILE OIL PRESSURE DECREASED INTO THE AMBER ZONE. THE LIGHT BECAME STEADY WHEN PRESSURE REACHED RED LINE. THE PRESS URE CONTINUED TO DECREASE AND THE OIL TEMP INCREASED FROM 99 TO 105 DEGREES DURING RETURN TO HNL. THE OIL QUANTITY REMA INED PEGGED FULL THROUGHOUT FLIGHT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 4 ENGINE STARTER DR IVE SEAL LEAKING. THE SEAL WAS FLAT AND CRACKED. THE SEAL WAS REPLACED. THE ENGINE WAS SERVICED WITH OIL. THE ENGINE WAS RUN AND LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 4 4F 4 F A20WE E20EA 1996122600435 19961226 00435 WP 1996 12 26 CALA9601862 1 19961221 A 7830 9007M60G50 TR COWL DOUG DC10 DC1010 3022110 WP NR 3 ENGINE FAILED A CALA O OTHER J D WARNING INDICATION INFLIGHT SEPARATION LD LANDING 1 SW 09 68046 21905 12923 47800 THE NR 3 ENGINE REVERSER UNLOCK LIGHT AND REVERSER 3 VALVE OPEN LIGHT ILLUMINATED DURING LANDING ROLL. MAINTENANCE FOUN D THE TRANSLATING COWL HAD SEPARATED FROM THE ENGINE AND FELL ON THE RUNWAY. THERE WAS DAMAGE TO THE COWL AND FAN REVER SER. THE NR 3 THRUST REVERSER RT HALF TRANSLATING COWL AND FAN REVERSER WERE REMOVED AND REPLACED. *S/D* INVESTIGATIV E FINDINGS REVEALED THAT THE PRIMARY CAUSE OF THE TRANSLATING COWL ASSEMBLY LOSS WAS DUE TO A SEPARATION OF THE FORWARD OUTER COWL TO THE AFT COWL, ALONG THE AFT COWL FORWARD CLOSE-OUT Z-CHANNEL BONDING ZONE. 2 L 7 3 4F A22WE 1996122600436 19961226 00436 WP 1996 12 26 9626679994 1 19961218 A 3260 DOWNLOCK SWITCH DOUG DC9 DC931 3022065 WP NLG FAILED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 8979E 47328 DURING APPROACH INTO MSO, NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. RECYCLED GEAR AND NORM AL INDICATIONS WERE ACHIEVED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NOSE GEAR LOCK SWITCH. OPERATION AL CHECK NORMAL ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1996122600437 19961226 00437 WP 1996 12 26 9626689968 1 19961219 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9332 47264 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 10 THROUGH 12 INOPERATIVE. REPLACED BA TTERIES IN POWER SUPPLY. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1996122600438 19961226 00438 WP 1996 12 26 9626699605 1 19961217 A 8011 STARTER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9 52048 NE RT ENGINE FAILED A A NWAA A E F UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. J WARNING INDICATION CL CLIMB 1 GL 01 605NW 47223 657761 DURING CLIMB, THE RIGHT ENGINE FIRE WARNING SYSTEM ILLUMINATED. CREW PULLED THE RIGHT ENGINE FIRE HANDLE AND FIRED ONE BOTTLE. THE A/C RETURNED TO AUS AND LANDED WITHOUT FURTHER INCIDENT. UPON INSPECTION, MAINTENANCE FOUND THE RIGHT ENGI NE STARTER HAD EXPERIENCED AN UNCONTAINED FAILURE. NO FIRE HAD OCCURRED. MAINTENANCE REPLACED THE RIGHT ENGINE. 2 L 7 2 4F 4 F A6WE E2EA 1996122600439 19961226 00439 NM 1996 12 26 9626706739 1 19961220 A 2910 PRESSURE TUBE BOEING 747 747251F 1384898 NM NR 1 HYD SYS LEAKING A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 639US 23887 DURING CLIMB, THE HYDRAULIC FLUID IN THE NR 1 HYDRAULIC SYSTEM DECREASED. AIRCRAFT RETURNED TO NRT AND LANDED WITHOUT I NCIDENT. REPLACED THE PRESSURE TUBE ON THE PRESSURE MODULE. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1996122600440 19961226 00440 NE 1996 12 26 9626719869 2 19961220 A 7320 PT 2 LINE DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE RT ENGINE LOOSE A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 778NC 48100 696732 DURING CLIMB, THE RIGHT ENGINE EPR INDICATION WAS ABNORMAL. A/C RETURNED TO ATL AND LANDED WITHOUT INCIDENT. MAINTENAN CE TIGHTENED THE RIGHT ENGINE PT-2 FLEX LINE. OPERATIONAL CHECK WAS OK. 2 L 7 2 4F 4 F RT A6WE E2EA 1996122600441 19961226 00441 1996 12 26 SWAA961386 4 19961217 A 3418 AOA VANE BOEING 737 7373H4 1384600 NM FUSE BROKEN A SWAA D RETURN TO BLOCK F FLT CONT AFFECTED CL CLIMB 1 SW 07 326SW 23690 IN FLIGHT, EXPERIENCED STALL WARNING IN FLIGHT, WITH STICK SHAKER, CREW LOWERED FLAPS AND EXTENDED SLATS TO FULL DOWN. AIRCRAFT RETURNED TO MDW AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND AOA VANE BROKEN OFF. REPLACED AOA VANE A ND OP CHECKED SYSTEM PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996122600442 19961226 00442 1996 12 26 SWAA961387 4 19961216 A 2565 D31355427 SLIDE BOEING 737 7372K6 NM PAX DOOR LOW PRESS A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22340 DURING SCHEDULED TERMINAL CHECK, FOUND FWD ENTRY DOOR SLIDE PRESSURE LOW. REPLACED SLIDE PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996122600443 19961226 00443 NM 1996 12 26 SWAA961388 1 19961216 A 3397 WIRE BOEING 737 7373H4 1384600 NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 639SW 27712 DURING SCHEDULED RON, FOUND EMERGENCY EXIT FLOOR TRACK LIGHTING INOPERATIVE AT ROW 21. RECONNECTED WIRES AND OP CHECKE D PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996122600444 19961226 00444 NM 1996 12 26 SWAA961389 1 19961216 A 3350 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 311SW 23333 DURING WALKAROUND CHECK, FOUND AFT CABIN UPPER FLASHLIGHT INOPERATIVE. REPLACED BATTERY PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996122600445 19961226 00445 NM 1996 12 26 SWAA961390 1 19961214 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 827/480 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 827, AT STRINGER 9, AND AT BS 480, S9L. REPAIRED PER BOEI NG SRM. 2 L 7 2 4F RT A16WE 1996122600446 19961226 00446 NM 1996 12 26 SWAA961391 1 19961213 A 3397 WIRE BOEING 737 7373H4 1384600 NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 390SW 26593 DURING SCHEDULED RON, FOUND EMERGENCY LIGHTING INOPERATIVE AT FORWARD EMERGENCY EXIT. REPAIRED WIRING PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996122600447 19961226 00447 NM 1996 12 26 SWAA961392 1 19961213 A 3350 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 390SW 26593 DURING SCHEDULED RON, FOUND AFT EMERGENCY FLASHLIGHT WEAK AT AFT CABIN. REPLACED BATTERY PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996122600448 19961226 00448 NM 1996 12 26 SWAA961393 1 19961213 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 808 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED 1/4 D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 808, BETWEEN STRINGERS 27R AND 27L. REPAIRED SKIN PER BO EING SRM. 2 L 7 2 4F RT A16WE 1996122600449 19961226 00449 NM 1996 12 26 SWAA961394 1 19961213 A 5330 SKIN BOEING 737 7375H4 138449D NM BS 970 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 511SW 24188 DURING SCHEDULED BC3 CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 970, AT STRINGER 19L. REPAIRED SKIN PER SWA RA 1-553-1566. 2 L 7 2 4F RT A16WE 1996122600450 19961226 00450 NM 1996 12 26 SWAA961395 1 19961213 A 3350 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 64SW 22062 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY LIGHTING INOPERATIVE OVER AFT LEFT AND RIGHT EXIT DOORS. REPLACED BATTE RY PER BOEING M/M. 2 L 7 2 4F A16WE 1996122600451 19961226 00451 NM 1996 12 26 SWAA961396 1 19961213 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 470/500/510 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 29SW 21340 DURING SCHEDULED TERMINAL CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510B, AT S10L, BS 470, AT S10L, AND AT BS 500-500A, AT S10L. REPAIRED SKIN PER BOEING SRM. 2 L 7 2 4F A16WE 1996122600452 19961226 00452 NM 1996 12 26 SWAA961397 1 19961217 A 3350 LIGHT BOEING 737 7372K6 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED C3 CHECK, FOUND AFT EMERGENCY EXIT LIGHT INOPERATIVE AT MID-CABIN. REPLACED LIGHT PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996122600453 19961226 00453 NM 1996 12 26 SWAA961398 1 19961217 A 3350 LIGHT BOEING 737 7372K6 NM CABIIN DIM A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED C3 CHECK, FOUND FORWARD ENTRY DOOR O/H EMERGENCY EXIT LIGHT DIM. REPLACED LIGHT ASSEMBLY PER BOEING M /M. 2 L 7 2 4F RT A16WE 1996122600454 19961226 00454 NM 1996 12 26 SWAA961399 1 19961217 A 3350 LIGHT BOEING 737 7372K6 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED C3 CHECK, FOUND FORWARD SERVICE DOOR O/H EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1996122600455 19961226 00455 NE 1996 12 26 SWAA961400 2 19961215 A 7200 ENGINE BOEING 737 7372H4 138448C NM GE CFM56 CFM563B1 13802 NE NR 2 BIRD STRIKE A SWAA A UNSCHED LANDING C E F.O.D. VIBRATION/BUFFET CL CLIMB 1 SW 07 71SW 22358 687812 AFTER TAKEOFF, AIRCRAFT EXPERIENCED MULTIPLE BIRD STRIKES TO RIGHT SIDE OF AIRCRAFT. ENGINE PARAMETERS REMAINED NORMAL EXCEPT FOR A SLIGHT VIBRATION IN NR 2 ENGINE START LEVER. AIRCRAFT RETURNED TO MCI AND MADE AN UNEVENTFUL LANDING. PE RFORMED BIRD STRIKE INSPECTION AND FOUND EVIDENCE OF MULTIPLE BIRD STRIKES AND DAMAGE TO NR 2 ENGINE. REPLACED ENGINE P ER BOEING M/M. 2 L 7 2 4F 4 F A16WE E2GL 1996122600456 19961226 00456 NM 1996 12 26 UPS96221787 1 19961221 A 3260 DOWNLOCK SWITCH BOEING 727 72725C 138400H NM NLG INOPERATIVE A IPXA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 951UP 19850 UNSAFE NOSE GEAR LIGHT INDICATION ON GEAR EXTENSION. STRIPS WERE ALIGNED IN NOSE WHEELWELL. NOSE GEAR MANUAL EXTENSION PERFORMED. EMERGENCY DECLARED AND NORMAL LANDING FOLLOWED. REMOVED AND REPLACED DOWNLOCK SWITCH PER 727 MM 32-61-21. PERFORMED NOSE GEAR SWING, OPS CK OK. 2 L 7 3 4F A3WE 1996122600457 19961226 00457 NM 1996 12 26 UPS96221788 1 19961221 A 3350 LIGHTS BOEING 727 7271A7C 13840X2 NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 935UP 20143 BOTH EMERGENCY LIGHTS DO NOT ILLUMINATE WITH SWITCH IN ON POSITION. RELAMPED BOTH EMERGENCY LIGHTS. OPS CHKS GOOD. 2 L 7 3 4F A3WE 1996122600458 19961226 00458 NM 1996 12 26 UPS96421789 1 19961218 A 3231 2670112 SAFETY VALVE BOEING 747 747121 1384871 NM RT MLG DOOR DEFECTIVE A IPXA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 682UP 20349 AFTER TAKEOFF, RED DOOR OPEN LIGHT FRONT PANEL ILLUMINATED WITH GEAR HANDLE OFF. ASSOCIATED PRIMARY AND ALTERNATE RT BO DY DOOR OPEN LIGHTS ILLUMINATED, SECOND OFFICER'S PANEL. REMOVED AND REPLACED BODY GEAR DOOR SAFETY VALVE. OPS CHECK A ND LEAK CHECK GOOD PER MM 32-33-09. P/N OFF 2670112, S/N OFF 879. P/N ON 2670112. S/N ON 4563. 2 L 7 4 4F A20WE 1996122600459 19961226 00459 NM 1996 12 26 UPS96421790 1 19961222 A 3350 LIGHT BOEING 747 747123 1384873 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 673UP 20325 EMERGENCY LIGHT UPPER DECK OUT. REPLACED. CHECKS GOOD. 2 L 7 4 4F A20WE 1996122600460 19961226 00460 WP 1996 12 26 MWEA96957 1 19961214 A 5330 SKIN DOUG DC9 DC914 3022034 WP BS 817 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 DURING INSPECTION, FOUND CRACK IN SKIN AT STA 817 ABOVE LONG 16L. INSTALLED REPAIR IAW SRM 53-04, FIG. 17A. RETURNED A /C TO SERVICE. 2 L 7 2 4F A6WE 1996122600461 19961226 00461 WP 1996 12 26 TC8A96071 1 19961219 A 3260 INDICATION DOUG DC8 DC862F 3021972 WP LANDING GEAR MALFUNCTIONED A TC8A O OTHER N FALSE WARNING AP APPROACH 1 GL 23 183SK 45904 KOAK TO KIND - FLT 35404 - DISCREPANCY: CYCLED LANDING GEAR IN-FLIGHT DUE TO UNSAFE WARNING, AFTER RECYCLED, ALL INDI CATIONS NORMAL. CORRECTIVE ACTION: INSPECTED DOWNLOCK WARNING TRIGGERING MECHANISM ON SWITCHES ASSY. FREED SPRING IA W MM 32-60-0, SYSTEM CHECKS NORMAL. GEAR SWING NOT REQUIRED IAW TCA MEL GMM CHAP II, P. 63. 2 L 7 4 4F 4A25 1996122600462 19961226 00462 WP 1996 12 26 TC8A96072 1 19961222 A 2926 RESERVOIR DOUG DC8 DC851 3021920 WP SPOILER SYST REQD SERVICE A TC8A D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 GL 23 805CK 45649 KIND TO KIND - FLT 35702 - DISCREPANCY: ON TAXI-OUT KIND, FLIGHT CONTROL CHECK SPOILER PRESSURE WENT TO ZERO, SPOILE R PUMP TURNED OFF. RETURNED TO RAMP. CORRECTIVE ACTION: SERVICED SPOILER RESERVOIR, GROUND CHECKS OK IAW MM 27-62-1. 2 L 7 4 4F 4A25 1996122600463 19961226 00463 SO 1996 12 26 SRAA961206 1 19961215 A 3244 9550616 TIRE LKHEED 382 382G 526414U SO RT MLG BLOWN A SRAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 921SJ 4586 ON TAXI OUT FOR FLIGHT 1008, RIGHT FORWARD MAIN WHEEL HAD A TIRE BLOWN OUT, SUSPECT RIM FAILURE, AIRCRAFT RETURNED TO BL OCK. VERIFIED RT FORWARD WHEEL ASSY HAD RIM FAILURE, REPLACED RT FORWARD AND AFT MAIN WHEELS, O/B MLG DOOR, SHEARED ACT UATOR ROD, 3 EACH DOOR HINGES, HINGE SUPPORT STIFFENER, AND FS 547 DIAGONAL STIFFENER. RIGGED GEAR DOOR AND ACCOMPLISHE D GEAR RETRACTION TEST PER M.M. CH 32-10, ALL STRUCTURAL REPAIR ACCOMPLISHED PER LOCKHEED SRM CH 51 AND 52. 2 H 7 4 4T A1SO 1996122600467 19961226 00467 WP 1996 12 26 CALA9601863 1 19961019 A 5330 SKIN DOUG DC10 DC1030 3023501 WP BS 1255 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37077 46981 INSPECTION FOUND A 1 INCH CRACK IN INNER SKIN AT RT DOOR CUT-OUT SURROUNDING FRAME STRUCTURE, STA 1255, AT CABIN FLOOR. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-00-01, FIGURE 4, SRM 51-21-01, AND 51-35 -01. 2 L 7 3 4F A22WE 1996122600468 19961226 00468 WP 1996 12 26 CALA9601864 1 19961019 A 5330 SKIN DOUG DC10 DC1030 3023501 WP BS 1308.5 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37077 46981 INSPECTION FOUND A 1 INCH CRACK IN INNER SKIN AT RT DOOR CUT-OUT SURROUNDING FRAME STRUCTURE, STA 1308.5, AT CABIN FLOOR . THE SKIN WAS REPAIRED BY FABRICATING AND INSTALLING A DOUBLER IAW SRM'S 51-21-01 AND 53-00-01, FIGURE 4. 2 L 7 3 4F A22WE 1996122600469 19961226 00469 WP 1996 12 26 CALA9601865 1 19961105 A 5330 SKIN DOUG DC10 DC1030 3023501 WP BS 1581/1585 GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37077 46981 INSPECTION FOUND FUSELAGE SKIN GOUGED IN TWO PLACES AT STRINGER 48R, B.S. 1581 AND 1585. THE GOUGES WERE REMOVED IAW SR M 53-00-01, FIGURE 1. TWO DOUBLERS, FILLER, AND A FINGER DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-20-00, FIGURE 6. 2 L 7 3 4F A22WE 1996122600470 19961226 00470 WP 1996 12 26 CALA9601866 1 19961105 A 5754 SKIN DOUG DC10 DC1030 3023501 WP NR 4 LE FLAP DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37077 46981 INSPECTION FOUND THE RT WING NR 4 SLAT DENTED AT XORS 480. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-10-00, FIG URE 12. 2 L 7 3 4F A22WE 1996122600471 19961226 00471 WP 1996 12 26 CALA9601867 1 19961010 A 5280 FRAME DOUG DC10 DC1030 3023501 WP CTR MLG DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37077 46981 THE RT CENTER MLG DOOR AFT FRAME WAS FOUND CORRODED. THE AFT FRAME WAS REMOVED AND REPLACED IAW SRM'S 51-35-01 AND 51- 35-02. 2 L 7 3 4F A22WE 1996122600472 19961226 00472 WP 1996 12 26 CALA9601868 1 19961129 A 5330 SKIN DOUG DC10 DC1030 3023501 WP BS 1509-1521 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37077 46981 INSPECTION FOUND FUSELAGE SKIN CORRODED STA 1509-1521, XCW 25 TO XCW -25. SKIN DOUBLERS WERE FABRICATED AND INSTALLED I AW ECRA 5330-02465 AND SRM 51-31-01. 2 L 7 3 4F A22WE 1996122600473 19961226 00473 WP 1996 12 26 CALA9601869 1 19961111 A 5414 SKIN DOUG DC10 DC1030 3023501 WP NR 3 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37077 46981 INSPECTION FOUND A .50 INCH CRACK ON LT AND RT CORNERS OF NR 3 ENGINE PYLON FORWARD END. THE CRACKED AREAS WERE CUT OUT . TWO EACH DOUBLERS, FILLERS, AND TRIPLERS WERE FABRICATED AND INSTALLED IAW SRM 54-00-01, FIGURE 2A. 2 L 7 3 4F A22WE 1996122600474 19961226 00474 WP 1996 12 26 CALA9601870 1 19961127 A 5400 DOUBLER DOUG DC10 DC1030 3023501 WP NR 3 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37077 46981 INSPECTION FOUND BOTH INBOARD AND OUTBOARD FORWARD UPPER ATTACH DOUBLERS OF NR 3 PYLON AFT FAIRING 489AL CRACKED THROUGH . THE CRACKED DOUBLERS WERE REMOVED IAW SRM 51-30-01. NEW DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM'S 51-21-01, 5 1-31-01, AND 53-00-01. 2 L 7 3 4F A22WE 1996122600475 19961226 00475 WP 1996 12 26 CALA9601871 1 19961013 A 5512 HINGED PANEL DOUG DC10 DC1030 3023501 WP LT HORIZ STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37077 46981 INSPECTION FOUND A .50 INCH CRACK AROUND FASTENER OF LT HORIZONTAL STABILIZER LOWER TRAILING EDGE HINGED PANEL AT STA XE 158. THE AREA WAS REPAIRED IAW SRM 51-70-00. 2 L 7 3 4F A22WE 1996122600476 19961226 00476 WP 1996 12 26 CALA9601872 1 19961012 A 5312 BLKHD STIFFENER DOUG DC10 DC1030 3023501 WP CTR MLG WW CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37077 46981 INSPECTION FOUND CORROSION AROUND LOWER BOLT HOLE OF T-SHAPED VERTICAL STIFFENER AT CENTER WHEELWELL AFT FACE OF FORWARD BULKHEAD, XCW -15.0. THE STIFFENER WAS REMOVED AND REPLACED IAW SRM'S 51-10-00, 51-21-01, AND 51-31-01. 2 L 7 3 4F A22WE 1996122600477 19961226 00477 WP 1996 12 26 CALA9601873 1 19961019 A 5754 SKIN DOUG DC10 DC1030 3023501 WP LT LE SLAT DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37077 46981 INSPECTION FOUND LT WING NR 1 LEADING EDGE SLAT DENTED ON LEADING EDGE NOSE STARTING 30 INCHES OUTBOARD OF XFS 145. THE DENTED AREA WAS CUT OUT AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 57-10-00, FIGURE 43. 2 L 7 3 4F A22WE 1996122600478 19961226 00478 WP 1996 12 26 CALA9601874 1 19961019 A 5730 SKIN DOUG DC10 DC1030 3023501 WP WS 810 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37077 46981 THE LT WING FIXED LEADING EDGE SKIN HAD A 2.5 INCH CRACK FROM LOWER EDGE RUNNING FORWARD AT APPROXIMATELY XORS 810. THE CRACKED AREA WAS REMOVED. DOUBLER, FILLERS, AND FASTENERS WERE INSTALLED IAW SRM 57-00-01. 2 L 7 3 4F A22WE 1996122600479 19961226 00479 NE 1996 12 26 COMA9610399 3 19961216 A 6110 8173861 INSERT RFC11AA16A EMB 120 EMB120RT SO PWA 118 PW118 NE HAMSTD 14RF 14RF9 NE PROP BEARING WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 1968 1968 886347 120264 115571 910337 PROPELLER ASSEMBLY WAS REMOVED FOR EXCESSIVE VIBRATION DURING DISASSEMBLY AND INSPECTION, IT WAS DETERMINED THAT THE VIB RATION WAS DUE TO THE UNEVEN WEAR OF THE BEARING INSERT. INSERT HAD DETERIORATED FROM .100 INCH TO .0840 INCH AT THE TH INEST WALL TO .098 INCH AT THE THICKEST WALL WEARING IN AN OVAL FASHION. BLADE PIN AND BEARING WERE REMOVED FROM SERVIC E AND REPLACED WITH SERVICABLE UNITS. PART TOTAL CYCLES, 2,044. 2 L 7 2 4T 4 T RT A31SO E20NE 6 C P11NE 1996122600480 19961226 00480 SO 1996 12 26 COMA9610408 1 19961219 A 2910 12040350001 HYDRAULIC HOSE EMB 120 EMB120RT SO LT ENGINE LOOSE A COMA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 263CA 120255 LT HYDRAULIC SYSTEM QUANTITY INDICATED ZERO DURING FLIGHT. EMERGENCY FREE FALL SYSTEM WAS USED TO EXTEND LANDING GEAR. TIGHTENED LOOSE HYDRAULIC PUMP HOSE FITTING AT LT NACELLE FIRE DECK. 2 L 7 2 4T RT A31SO 1996122600481 19961226 00481 SO 1996 12 26 COMA9610407 1 19961221 A 6120 78249012 PCU EMB 120 EMB120RT SO RT ENGINE MALFUNCTION A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 269CA 11663 1229 120263 AFTER TAKEOFF, THE RT PROPELLER RPM INCREASED TO 102 PERCENT. WHEN POWER REDUCED, THE RPM DROPPED TO 96 PERCENT AND THE N INCREASED AGAIN TO 102 PERCENT. REPLACED THE RT PROPELLER CONTROL UNIT. PART TOTAL CYCLES, 11,585. 2 L 7 2 4T RT A31SO 1996122600482 19961226 00482 SO 1996 12 26 COMA9610409 1 19961223 A 6100 7845191 PITCHLOCK SCREW 790201 EMB 120 EMB120RT SO PWA 118 PW118 NE HAMSTD 14RF 14RF9 NE PROP ACTUATOR FAILED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 265CA 3614 910102 120257 115300 9012222 PROPELLER ASSEMBLY WAS ORIGINALLY REMOVED FROM AIRCRAFT FOR ENGINE RELATED MAINTENANCE. ONCE REMOVED, IT WAS DISCOVERED THAT THE ACTUATOR FEATHER STOP TAB HAD BEEN DISPLACED APPROXIMATELY .25 INCH. PITCH LOCK SCREW WAS REMOVED FROM SERVIC E AND RETURNED TO MANUFACTURER. 2 L 7 2 4T 4 T RT A31SO E20NE 6 C P11NE 1996122600483 19961226 00483 NE 1996 12 26 COMA9610410 3 19961223 A 6110 7845191 PITCHLOCK SCREW 7902015 EMB 120 EMB120RT SO PWA 118 PW118 NE HAMSTD 14RF 14RF9 NE PROP ACTUATOR FAILED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 179CA 3617 910310 120179 115519 910123 PROPELLER ASSEMBLY WAS ORIGINALLY REMOVED FOR ENGINE RELATED MAINTENANCE. ONCE REMOVED, THE ACTUATOR PITCHLOCK SCREW FE ATHER STOP TAB WAS FOUND TO BE DISPLACED APPROXIMATELY .125 INCH. PITCHLOCK SCREW WAS REMOVED FROM SERVICE AND RETURNED TO MANUFACTURER. 2 L 7 2 4T 4 T RT A31SO E20NE 6 C P11NE 1996122600484 19961226 00484 SO 1996 12 26 COMA9610411 1 19961223 A 5313 12006173003 STRINGER EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 152CA 18383 120152 DURING 2C CHECK INSPECTION FOUND CORROSION ON FUSELAGE STRINGER 19L BETWEEN FRAMES 19 AND 20. STRINGER 19L WAS REPAIRED PER AERODESIGN REPORT NR 1990-2, REV.IR DATED 9-15-96. 2 L 7 2 4T RT A31SO 1996122600485 19961226 00485 SO 1996 12 26 COMA9610412 1 19961223 A 5320 12005802001 SILL EMB 120 EMB120RT SO LT PAX DOOR CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 152CA 18383 120152 DURING 2C CHECK FUSELAGE FWD CABIN FLOOR SUPPORT STRUCTURE LT SILL FOUND CORRODED. SILL WAS REPLACED WITH NEW PART PER SRM 51-40, STANDARD PRACTICES. AIRCRAFT TOTAL CYCLES, 20,051. 2 L 7 2 4T RT A31SO 1996122600486 19961226 00486 SO 1996 12 26 COMA9610413 1 19961223 A 5320 12026671001 BUTT STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 152CA 18383 120152 DURING 2C CHECK FUSELAGE FWD FLOOR SUPPORT STRUCTURE LT BUTT STRAP FOUND CORRODED. BUTT STRAP WAS REPLACED WITH NEW PAR T PER SRM CHAPT 51, STANDARD PRACTICES. AIRCRAFT TOTAL CYCLES, 20,051. 2 L 7 2 4T RT A31SO 1996122600487 19961226 00487 SO 1996 12 26 COMA9610414 1 19961223 A 5320 12007089003 BUTT STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 152CA 18383 120152 DURING 2C CHECK FWD FUSELAGE FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP FOUND CORRODED. BUTT STRAP REPLACED WITH NEW PAR T PER SRM CHAPT. 51, STANDARD PRACTICES. AIRCRAFT TOTAL CYCLES, 20,051. 2 L 7 2 4T RT A31SO 1996122600488 19961226 00488 SO 1996 12 26 COMA9610415 1 19961223 A 5320 12005805003 BUTT STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 152CA 18383 120152 DURING 2C CHECK FUSELAGE FWD FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP FOUND CORRODED. REPLACED BUTT STRAP WITH NEW PAR T PER SRM CHAPT. 51, STANDARD PRACTICES. AIRCRAFT TOTAL CYCLES, 20,051. 2 L 7 2 4T RT A31SO 1996122600489 19961226 00489 SO 1996 12 26 COMA9610416 1 19961223 A 5320 1200508 SILL EMB 120 EMB120RT SO PAX DOOR CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 152CA 18383 120152 DURING 2C CHECK FUSELAGE FWD FLOOR SUPPORT STRUCTURE RT SILL FOUND CORRODED. REPLACED SILL WITH NEW PART PER SRM CHAPT. 51, STANDARD PRACTICES. AIRCRAFT TOTAL CYCLES, 20,051. 2 L 7 2 4T RT A31SO 1996122600490 19961226 00490 SO 1996 12 26 COMA9610417 1 19961223 A 5320 12006664004 SILL EMB 120 EMB120RT SO PAX DOOR CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 152CA 20051 120152 DURING 2C CHECK FUSELAGE CENTER SECTION FLOOR SUPPORT STRUCTURE RT SILL FOUND CORRODED. SILL WAS REPLACED WITH NEW PART PER SRM CHAPT. 51, STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1996122600491 19961226 00491 SO 1996 12 26 COMA9610418 1 19961223 A 5320 12006664003 SILL EMB 120 EMB120RT SO PAX DOOR CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 152CA 18383 120152 DURING 2C CHECK FUSELAGE CENTER SECTION FLOOR SUPPORT STRUCTURE LT SILL CORRODED. SILL WAS REPAIRED PER AERODESIGN REPO RT NR 2140-1, REV IR, DATED 12-22-96. AIRCRAFT TOTAL CYCLES, 20,051. 2 L 7 2 4T RT A31SO 1996122600492 19961226 00492 SO 1996 12 26 COMA9610419 1 19961223 A 5320 12006664001 SILL EMB 120 EMB120RT SO PAX DOOR CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 152CA 18383 120152 DURING 2C CHECK FUSELAGE CENTER SECTION FLOOR SUPPORT STRUCTURE LT SILL FOUND CORRODED. SILL REPLACED WITH NEW PART PER SRM CHAPT. 51 STANDARD PRACTICES. AIRCRAFT TOTAL CYCLES, 20,051. 2 L 7 2 4T RT A31SO 1996122600493 19961226 00493 SO 1996 12 26 COMA9610420 1 19961223 A 5320 12027929003 BUTT STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 152CA 18383 120152 DURING 2C CHECK FUSELAGE CENTER SECTION FLOOR SUPPORT RT BUTT STRAP FOUND CORRODED. BUTT STRAP REPLACED WITH NEW PART P ER SRM CHAPT. 51, STANDARD PRACTICES. AIRCRAFT TOTAL CYCLES, 20,051. 2 L 7 2 4T RT A31SO 1996122600494 19961226 00494 SO 1996 12 26 COMA9610421 1 19961223 A 5720 12029798001 JOINT SHEET EMB 120 EMB120RT SO WING AUX SPAR GOUGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 152CA 18383 120152 DURING 2C CHECK, INSPECTION REVEALED THE WING AUX SPAR CENTER SECTION JOINT SHEET DAMAGED BY SCREWS THAT ATTACH THE LOWE R FAIRING. THE DAMAGE CONSISTS OF A SMALL GOUGE ALONG THE BOTTOM EDGE, ONE ON THE LEFT SIDE AND ONE ON THE RIGHT SIDE O F THE SHEET. THE SHEET WAS REPAIRED PER AERODESIGN REPORT NR 2138-1, REV A., DATED 12-22-96. AIRCRAFT TOTAL CYCLES, 20 ,051. 2 L 7 2 4T RT A31SO 1996122600495 19961226 00495 SO 1996 12 26 COMA9610422 1 19961223 A 5320 12037024001 BUTT STRAP EMB 120 EMB120RT SO FUSELAGE MISDRILLED A COMA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 152CA 18383 120152 DURING 2C CHECK THE FUSELAGE AFT FLOOR SUPPORT STRUCTURE BUTT STRAP AT CARGO DOOR OPENING WAS FOUND TO HAVE MISDRILLED H OLES. THE BUTT STRAP WAS REPAIRED PER AERODESIGN REPORT NR 2139-1, REV IR, DATED 12-22-96. AIRCRAFT TOTAL CYCLES, 20,0 51. 2 L 7 2 4T RT A31SO 1996122600496 19961226 00496 NE 1996 12 26 COMA9630164 2 19961220 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RIGHT FAILED A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 356CA 943 340A034 367159 UNUSUAL ROARING SOUND COMING FROM RT ENGINE WHEN POWER IS ADVANCED ABOVE 75 PERCENT N.G. REPLACED THE RT ENGINE 2 L 7 2 4T 4 T RT A52EU E8NE6 1996122600497 19961226 00497 EA 1996 12 26 COMA9660230 1 19961222 A 3010 124112450 HEAT PROBES CNDAIR CL600 CL6002B19 EA RT WING DEFECTIVE A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 976CA 24 7151 ANTI-ICE DUCT WARNING MESSAGE ON EICAS WHEN WING DEICE SELECTED ON. REPLACED 6 DEFECTIVE HEAT PROBES IN RT WING LEADING EDGE. 2 L 7 2 4F RT A21EA 1996122600498 19961226 00498 EA 1996 12 26 COMA9660231 1 19961219 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA LT TE FLAP MALFUNCTION A COMA K NONE O OTHER AP APPROACH 1 SO 01 969CA 409 7141 FLAPS FAIL CAUTION MESSAGE WHEN FLAPS SELECTED FOR LANDING. REPLACED THE LEFT FLAP BRAKE AND POSITION SENSOR UNIT. 2 L 7 2 4F RT A21EA 1996122600499 19961226 00499 NM 1996 12 26 QXEA9600496 1 19961222 A 3350 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 822PH 106 EMERGENCY LIGHT AT CABIN DOOR ENTRY BROKEN, REATTACHED COVER . LIGHT OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SE RVICE. 2 H 7 2 4T RT A13NM 1996122600500 19961226 00500 SW 1996 12 26 QXEA9600497 1 19961220 A 2120 AIR DISTR SWRNGN SA227 SA227AC 8780603 SW CABIN SMOKE A QXEA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 27442 AC750 ON BOTH ENGINE STARTS, CABIN FILLED WITH SMOKE. STARTED ENGINES I.A.W. MM 71-00-30 WITH BLEEDS ON SMALL AMOUNT OF SMOKE IN CABIN, CONTINUED ENGINE OPERATION UNTIL THE SMELL CLEARED. SUSPECT DEICING FLUID HAD ENTERED THE ENGINES. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A8SW 1996122600501 19961226 00501 EU 1996 12 26 QXEA9600498 1 19961221 A 3350 6008905 BATTERY PACK FOKKER F28 F28MK1000 4990808 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 454US 5709 319 11107 SEAT 7AB EMERGENCY LIGHT INOPERATIVE AND LT EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED FWD LT OVERHEAD BIN BATTERY POWER SUPPLY I.A.W. M.M. 33-50-01. AIRCRAFT RETURNED TO SERVICE. AIRCRAFT TOTAL CYCLES, 6,977. 2 L 7 2 4F RT A20EU 1996122600502 19961226 00502 NM 1996 12 26 96UAL900941 1 19961216 A 2133 PRESS REG VALVE ABLE CORP 1060704 BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE CABIN FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 9016U 435 19054 CREW REPORTS, UNABLE TO PRESSURIZE AIRCRAFT WITH RIGHT PACK, OUTFLOW VALVE FULLY CLOSED. TRIED OTHER PACK, NO HELP. TR IED MANUAL AND AUTO, NO HELP. *S/D* REPAIRED DOOR 2L LEAK AND REPLACED PRESSURE REGULATOR VALVE, OPS CHECK GOOD. 2 L 7 2 4F 4 F A16WE E2EA 1996122600503 19961226 00503 NM 1996 12 26 96UAL900942 1 19961216 A 2133 OUT FLOW VALVE HAMILTON STA 711003 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LEFT FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 323UA 200 23955 UNABLE TO PRESSURIZE CABIN IN ANY MODE. OUTFLOW VALVE SHOWS FULL CLOSED, LOUD AIR NOISE COMING FROM DOOR ONE LEFT. *S/ D* FOUND OUTFLOW VALVE NOT CLOSING. AC MOTOR CLOSE LIMIT SWITCH NOT OPERATING. REPLACED AFT OUTFLOW VALVE, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 1996122600504 19961226 00504 NM 1996 12 26 96UAL900943 1 19961216 A 3350 M983 BATTERY PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7466U 21920 LEFT AFT SLIDE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK 2 L 7 3 4F 4 F A3WE E2EA 1996122600505 19961226 00505 NM 1996 12 26 96UAL900944 1 19961217 A 2750 126344151U1 DRIVE UNIT ALLIED SIGNA BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 2 LE FLAP FAILED A UALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 WP 29 4724U 19875 LEFT NR 2 LEADING EDGE FLAP WOULD NOT RETRACT. RETURNED TO FIELD. *S/D* NR 2 LEFT HAND LEADING EDGE FLAP DRIVE UNIT W AS REPLACED. REMOVED UNIT WAS DISASSEMBLED IN THE SHOP WITH NO DEFECTS NOTED. 2 L 7 4 4F 4 F A20WE E20EA 1996122600506 19961226 00506 WP 1996 12 26 96UAL900945 1 19961217 A 3397 WIRE DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1847U 48263 B-ZONE AFT LEFT EEL LIGHT DOES NOT TEST. REPAIRED BROKEN CABLE. SYSTEM CHECKS OKAY. 2 L 7 3 4F 4 F A22WE E23EA 1996122600507 19961226 00507 NM 1996 12 26 96UAL900946 1 19961217 A 2120 AIR DISTR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN SMOKE A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 7266U 21413 APU SMOKING EXCESSIVELY AND FLUID DRIPPING FROM EXHAUST AND INSULATION BLANKET. SMOKE GETTING INTO CABIN. ORD 12/17/9 7 RAN APU AND PACKS. FOUND NO SMOKE OR FLUID DRIPPING FROM EXHAUST DUCT. SUSPECT DEICER FLUID IN EXHAUST. AIRPLANE PR EVIOUSLY IN DEN. 2 L 7 3 4F 4 F A3WE E2EA 1996122600508 19961226 00508 WP 1996 12 26 96UAL900947 1 19961217 A 2121 FAN DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL APU OIL LEAK A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 1816U 46615 STRONG ACRID ODOR NOTED IN COCKPIT AND AFT CABIN DURING CLIMB. *S/D* MAINTENANCE FOUND THE APU COOLING FAN LEAKING OIL . REMOVED AND REPLACED APU. SHOP COULD NOT DUPLICATE COOLING FAN LEAK. APU OPERATED NORMALLY WITH NO EXTERNAL LEAKS. SUSPECT GLYCOL INGESTION DURING DE-ICING PROCEDURE. 2 L 7 3 4F 4 F A22WE E23EA 1996122600509 19961226 00509 EU 1996 12 26 96UAL900948 1 19961217 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN MALFUNCTIONED A UALA K NONE L NO TEST CR CRUISE 1 WP 29 416UA 479 RIGHT REAR OVER WING EMERGENCY EXIT LIGHT CAME ON IN LIGHT TURBULENCE. PROBLEM COULD NOT BE DUPLICATED AND CAUSE COULD NOT BE DETERMINED. UPON SUBSEQUENT REINSPECTIONS, NO PROBLEM COULD BE FOUND. 2 L 7 2 4F 4 F RT A28NM E40NE 1996122600510 19961226 00510 NM 1996 12 26 96UAL900949 1 19961218 A 2421 IDG BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ENGINE FAILED A UALA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 WP 29 532UA 25072 RIGHT GENERATOR DRIVE LIGHT ILLUMINATED. AIRCRAFT RETURNED TO FIELD. *S/D* RIGHT INTEGRATED DRIVE GENERATOR WAS REMOV ED AND SENT TO SHOP. INTEGRATED DRIVE GENERATOR HAD BROKEN PISTON SLIPPERS. NEW INTEGRATED DRIVE INSTALLED, OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996122600511 19961226 00511 NM 1996 12 26 96UAL900950 1 19961219 A 2740 69B834131 COVER BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE STAB TRIM WHEEL BROKEN A UALA K NONE O OTHER TX TAXI/GRND HDL 1 WP 29 163UA 21353 DURING OP CHECK OF STABILIZER TRIM CONTROL SYSTEM, FLIGHT CREW NOTICED THE STABILIZER DID NOT APPEAR TO TRIM USING EITHE R THE SWITCHES ON THE CONTROL YOKE OR MANUAL CONTROL LEVERS. 1ST OFFICER'S STABILIZER POSITION TRIM INDICATOR WHEEL OUT ER COVER HAD BROKEN AND WAS JAMMING THE STAB TRIM POSITION INDICATORS, PREVENTING THEM FROM MOVING. THE JAMMING SUBSEQU ENTLY LED TO THE FAILURE OF THE STAB INDICATOR AFT CABLE QUADRANT SHEAR RIVETS AS THE STABILIZER WAS MOVED. STAB TRIM I NDICATOR WHEEL OUTER COVER WAS REPLACED, THE STAB INDICATOR AFT CABLE QUADRANT WAS REPAIRED . 2 L 7 4 4F 4 F A20WE E20EA 1996122600512 19961226 00512 NM 1996 12 26 96UAL900951 1 19961219 A 2130 PRESSURE SYST BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 952UA 26699 UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF. AIRCRAFT RETURNED TO FIELD. *S/D* ACCOMPLISHED CHECK OF BOTH PACKS AND E NGINE PRESSURE BLEEDS. PRESSURIZED ACFT TO 6 PSID OFF ONE PACK. CHECKED OUTFLOW VALVE HEATER GASKET RESISTANCE. ALL S YSTEMS PERFORMED NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 1996122600513 19961226 00513 NM 1996 12 26 96UAL900953 1 19961219 A 2782 ACTUATOR 2145014 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE SPEED BRAKES MALFUNCTIONED A UALA O OTHER F FLT CONT AFFECTED DE DESCENT 1 WP 29 7272U 21419 WHEN SPEED BRAKES ARE EXTENDED, WITH TRIM AT ZERO, THE AIRCRAFT ROLLS TO THE RIGHT. *S/D* THE INBOARD LT FLIGHT SPOILE R (A5) WAS NOT DEPLOYING FULLY BECAUSE OF A FAULTY ACTUATOR. ASYMMETRIC SPOILER DEPLOYMENT DURING SPEED BRAKE EXTENSION CAUSED THE ROLL. NR 5 FLIGHT SPOILER ACTUATOR REPLACED, SYSTEM OPERATES NORMALLY. 2 L 7 3 4F 4 F A3WE E2EA 1996122600514 19961226 00514 NM 1996 12 26 96UAL900954 1 19961220 A 5330 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE BS 1030 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7462U 21916 AFT LOWER RT FUSELAGE OUTBOARD OF AFT VHF ANTENNA HAS A ONE INCH CRACK IN SKIN AND EVIDENCE OF CORROSION. *S/D* SKIN R EPAIRED PER SRM 53-30-03. 2 L 7 3 4F 4 F A3WE E2EA 1996122600515 19961226 00515 WP 1996 12 26 96UAL900955 1 19961220 A 2121 FAN ALLIED SIGNA 6054578 DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 1847U 344983 48263 RETURNED TO BLOCKS BECAUSE OF STRANGE SMELL IN THE CABIN. *S/D* THE SMELL WAS ISOLATED TO THE NR 1 RECIRCULATION FAN. REPLACED FAN. THE SHOP FOUND NO FAULT WITH THE FAN, NO REOCCURANCE. 2 L 7 3 4F 4 F A22WE E23EA 1996122600516 19961226 00516 NM 1996 12 26 96UAL900956 1 19961220 A 5412 BULKHEAD FITTING BOEING 65B903351 BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 4 PYLON LOOSE FASTENERS A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 4719U 19880 DURING ROUTINE ENGINE CHANGE ON NR 4 ENGINE FOUND 4 LOOSE FASTENERS ON THE PYLON FWD ENGINE MOUNT FITTING INBOARD SIDE C OMMON TO THE BULKHEAD. INSTALLED NEW FASTENERS. ADJACENT FASTENERS WERE INSPECTED WITH NO DEFECTS NOTED. BOEING S/B 7 47-54A2069 WAS PREVIOUSLY ACCOMPLISHED. 2 L 7 4 4F 4 F A20WE E20EA 1996122600517 19961226 00517 WP 1996 12 26 MWEA96657 1 19961220 A 2560 3952273501 GIRT BAR LATCH DOUG DC9 DC932 3022066 WP GALLEY DOOR DIRTY A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 302ME 47102 CREW REPORTS GALLEY SERVICE DOOR EVACUATION SLIDE GIRT BAR DIFFICULT TO ARM AND DISARM. -- MAINTENANCE CLEANED AND LUB ED GIRT BAR LATCHES. OPS CHECK GOOD. RETURNED A/C TO SERVICE. 2 L 7 2 4F A6WE 1996122600518 19961226 00518 NM 1996 12 26 MWEA96658 1 19961222 A 2560 D29988107 EVAC SLIDE DOUG MD88 MD88 3023688 NM GALLEY DOOR FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 701ME 48760 CREW REPORTS AFT GALLEY SERVICE DOOR SLIDE FELL OFF WHEN CATERERS OPENED DOOR. -- RESECURED AFT GALLEY DOOR EVACUATION SLIDE. RETURNED A/C TO SERVICE. 2 L 7 2 4F RT A6WE 1996122600519 19961226 00519 WP 1996 12 26 MWEA96659 1 19961222 A 2560 5917689103 SLIDE COVER DOUG DC9 DC932 3022066 WP GALLEY DOOR FELL OFF A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 602ME 48133 CREW REPORTS WHILE PARKING AT GATE THE GALLEY SERVICE DOOR SLIDE COVER FELL OFF. -- REINSTALLED GALLEY SERVICE DOOR SL IDE COVER. RETURNED A/C TO SERVICE. 2 L 7 2 4F A6WE 1996122600520 19961226 00520 WP 1996 12 26 SCNA96447 1 19961218 A 3350 14111101 BATTERY DOUG DC10 DC1015 3022118 WP L2 DOOR DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 152SY 48289 FOUND L2 DOOR ESCAPE SLIDE PRESS TO TEST LIGHT INOP. RELAMPED AND REPLACED BATTERIES AND OPS CHECKED GOOD IN ACCORDANCE WITH MM 25-61-01. 2 L 7 3 4F A22WE 1996122600521 19961226 00521 NE 1996 12 26 SCNA96448 2 19961220 A 7200 ENGINE BOEING 727 727225 1384077 NM PWA JT8 JT8D17R 52049 NE NR 3 FAILED A SCNA E ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 GL 15 282SC 22558 700823 IN FLIGHT, NR 3 ENGINE LOW OIL/FILTER BYPASS LIGHT ILLUMINATED IN-FLIGHT. OIL PRESSURE, TEMPERATURE AND QUANTITY INDIC ATED NORMAL. SHUT DOWN ENGINE IN ACCORDANCE WITH COM PROCEDURES. REMOVED AND REPLACED OIL FILTER AND INSPECTION FOUND SMALL METAL CONTAMINATION IN FILTER. REMOVED AND REPLACED ENGINE. 2 L 7 3 4F 4 F A3WE E2EA 1996122600522 19961226 00522 SO 1996 12 26 BIER960039 1 19961224 A 5513 63586800 TRIM TAB PIPER PA32 PA32300 7103212 SO HORIZ STAB CRACKED B BIEA K NONE O OTHER IN INSP/MAINT 1 EA 21 3073W 250 327940081 DURING REMOVAL OF HORIZONTAL STABILATOR TRIM TAB HINGES FOR REPLACEMENT, FOUND BOTH TRIM TABS CRACKED UNDER CONTROL HORN ATTACHMENT. CRACKS NOT VISIBLE WITH TABS ATTACHED. SUBMITTER SUGGEST REMOVAL OF HORN AT ANNUAL INSPECTION FOR ROUTINE INSPECTION. 1 L 7 1 3O A3SO 1996122600523 19961226 00523 1996 12 26 P5CA9601251 4 19961220 A 3414 A4321710103 AIRSPEED IND BOEING 747 747122 1384872 NM RT COCKPIT INOPERATIVE A P5CA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 WP 23 851FT 19756 FIRST OFFICER'S AIRSPEED INDICATOR READ ZERO WHILE CAPTAIN'S ASI INDICATED 100 KNOTS. PERFORMED HIGH ENERGY STOP INSPEC TION PER BAC MM 05-51-10 AND REPLACED FIRST OFFICER'S AIR SPEED INDICATOR PER BAC MM 34-13-05. 2 L 7 4 4F A20WE 1996122600524 19961226 00524 1996 12 26 P5CA9601252 4 19961219 A 3442 MI585285 RADAR SCOPE BOEING 747 747122 1384872 NM NR 1 INOPERATIVE A P5CA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 23 854FT 19754 CAPTAIN'S WEATHER RADAR INDICATOR WENT BLANK WITH SMELL OF SMOKE IN COCKPIT - PULLED CIRCUIT BREAKER. REPLACED RADAR IN DICATOR PER BAC MM 34-43-05 AND TESTED PER MM 34-43-00. 2 L 7 4 4F A20WE 1996122600525 19961226 00525 NE 1996 12 26 P5CA9601253 2 19961223 A 7261 DRAIN CAP BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 4 ENGINE BAD SEAL A P5CA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 WP 23 853FT 19753 LOSS OF OIL QUANTITY NR 4 ENGINE ON TAXI OUT. FOUND DRAIN CAP SEAL LEAKING ON KIT INSTALLED FOR ENGINE DRIVEN HYDRAULIC PUMP DEACTIVATION PER MEL 29-01 PER MAINTENANCE MANUAL 29-11-05. REPLACED CAP LEAK CHECK OK. 2 L 7 4 4F 4 F A20WE E20EA 1996122600535 19961226 00535 1996 12 26 CA960619041 4 19960514 A 3413 1003840541 INDICATOR AEROSONIC 1003840541 BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA COCKPIT VERT SPD SLOW REACTING W K NONE O OTHER CL CLIMB 1 CA 531 W2275G PCE81939 (CAN) THE VERTICAL SPEED INDICATOR HAD BEEN INDICATING SLOW, ERRATIC AND SOMETIMES INCORRECTLY. THE UNIT HAS A HISTORY OF ERRATIC BEHAVIOUR EVEN AFTER SUCCESSIVE OVERHAULS. 1 L 7 2 4T 4 T A24CE E4EA 1996122600536 19961226 00536 CE 1996 12 26 CA960619042 1 19960514 A 2931 P50018LMBE INDICATOR STCSA4378WP BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA HYD SYS READS INCORRECT W K NONE O OTHER IN INSP/MAINT 1 CA 1539 ADI1203 PCE81939 (CAN) LANDING GEAR HYDRAULIC PRESSURE GAUGE READS INCORRECTLY. THE GAUGE IS RATED FOR 2000 PSI, AND THE SYSTEM OPERATES AT 2000 PSI. SUBMITTER STATES THAT THE RELIEF VALVE FUNCTIONS AT 2200 PSI AND THIS PUTS UNDO STRAIN ON THE GAUGE DURING HOT WEATHER RELATED THERMAL RELIEF, HENCE THE GAUGE BEGINS TO READ INCORRECTLY. SUBMITTER SUGGESTS REPLACING THE GAUGE W ITH A HIGHER RATED ONE. 1 L 7 2 4T 4 T A24CE E4EA 1996122600538 19961226 00538 CE 1996 12 26 CA960620006 1 19960523 A 7830 553832816 JUNCTION BOX CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE THRUST REV MIS WIRED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 71721 (CAN) WHILE PERFORMING A ROUTINE PHASE 5 INSPECTION, THE TECHNICIAN FOUND THAT IMPROPER WIRING PROCEDURES WERE FOLLOWED DURING MANUFACTURE OF THE THRUST REVERSER JUNCTION BOX P/N 5538328-16 REF. IPC 78-30-03. IT WAS NOTED THAT SEVERAL WIRES WERE INCORRECTLY ROUTED AND SUPPORTED. WIRES WERE RUNNING AGAINST OR THROUGH THE HEAT SINK ASSEMBLY. THIS IS CONTRARY T O STANDARD PRACTICES AC 43.13.1A, PAR 447 & 448. SOME WIRE TENSIONS WERE TOO TIGHT, CAUSING COMPONENTS TO FRACTURE. DIOD E D171 CATHODE LEAD FRACTURED DUE TO STRESS AND VIBRATION BY A TY-WRAP. DEFECTIVE COMPONENTS WERE REPLACED AND REPAIRED IN ACCORDANCE WITH STANDARD PRACTICES. 1 L 7 2 4F 4 F A22CE E1NE 1996122600539 19961226 00539 SW 1996 12 26 CA960620007 1 19960521 A 2121 CM3505C BLOWER ASSEMBLY BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL LOCK SCREWS SHORTING W K NONE O OTHER IN INSP/MAINT 1 CA CAE800093BA (CAN) BLOWER ASSEMBLY WAS REMOVED FOR ROUTINE 600 HOUR BENCH CHECK. BEFORE DISASSEMBLY IT WAS NOTED THAT THE LOCKWIRE SE CURING THE ASSEMBLY BOLTS WERE HEAT DISCOLOURED. THE BLOWER ONLY USES 28 VDC, IT WAS THOUGHT THAT THE GROUND CONNECTION VIA AIRCRAFT WIRING MIGHT BE OPEN AND THE UNIT WAS GROUNDING THROUGH ITS CHASSIS. AS POWER WAS APPLIED TO PIN A AND GROU ND TO CHASSIS THE LOCKWIRE BEGAN TO GLOW. IT WOULD APPEAR THAT SOME OF THE BOLTS HAD A BUILT UP RESISTANCE AND AT LEAST ONE OF THE THREE BOLT CLUSTERS HAD LOW RESISTANCE WHICH SET UP A CURRENT PATH DUE TO BAD GROUNDING AT PIN B. THE LOCKWIR E UNDER THIS CIRCUMSTANCE ACTED LIKE A FUSE WITH A VIRTUAL STRAIGHT ELECTRICAL SHORT. 1 G 7 1 3U 3 U H2SW E4CE 1996122600541 19961226 00541 EA 1996 12 26 CA960620010 1 19960527 A 2421 731633 IDG CNDAIR CL600 CL6002A12 1900304 EA GE CF34 CF341A NE ENGINE OIL LOSS W K NONE J K WARNING INDICATION FLUID LOSS CR CRUISE 1 CA 8618 350143 (CAN) OIL LOSS RESULTED IN FAILURE OF CONSTANT SPEED DRIVE PORTION OF INTEGRATED DRIVE GENERATOR. 2 L 7 2 4F 4 F RT A21EA E15NE 1996122600542 19961226 00542 CE 1996 12 26 CA960620011 1 19960522 A 7830 QUADRANT SWITCH CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE THROTTLE BROKEN WIRING W K NONE O OTHER IN INSP/MAINT 1 CA 71714 (CAN) ON THIS AIRCRAFT AND 4 OTHERS, THROTTLE QUADRANT SWITCHES S153, S161, S154 AND S162 WHICH CAUSE THRUST REVERSER TO STOW OR DEPLOY, HAVE FAILED. CAUSE WAS FOUND TO BE BECAUSE THE SWITCHES ARE MOUNTED ON THE MOVING THROTTLE WHERE THE WI RING IS CONTINUOUSLY BEING FLEXED DUE TO THE TIGHTNESS OF THE INSTALLATION. THE SWITCHES ARE POTTED AND THE WIRING IS EN CASED IN HEAT SHRINK UP TO THE POTTING. IT IS AT THIS POINT THE WIRING BREAKS. IT MAY BE THE HEAT SHRINK IS MAKING THE W IRING TOO RIGID AND NOT ALLOWING ENOUGH FLEXABILITY AT THIS AREA. THE SUBMITTER HAS SUGGESTED MOUNTING A STRIKER PLATE O N THE MOVING THROTTLE AND MOUNTING THE SWITCH RIGIDLY ON THE AIRFRAME. THIS WAY THERE WOULD BE NO MOVEMENT OF THE WIRING 1 L 7 2 4F 4 F A22CE E1NE 1996122600543 19961226 00543 NM 1996 12 26 CA960620012 1 19960529 A 5713 STRINGER BOEING 757 75723A 1384967 NM RROYCE RB211 RB211535E4 54555 NE WS 1060 CORROSION W K NONE O OTHER IN INSP/MAINT 1 CA 30655 (CAN) LIGHT SURFACE CORROSION AT STN 1060 AT REAR FACE OF STRINGER, REMOVED AND REFINISHED. 2 L 7 2 4F 4 F RT A2NM E12EU 1996122600544 19961226 00544 NM 1996 12 26 CA960620013 1 19960529 A 5330 SKIN BOEING 757 75723A 1384967 NM RROYCE RB211 RB211535E4 54555 NE BS 1020 STR 17 CORROSION W K NONE O OTHER IN INSP/MAINT 1 CA 30655 (CAN) LIGHT SURFACE CORROSION AT BODY STATION 1020 RH FRAME AT STRINGER 17 CREASE BEAM. REMOVED AND REFINISHED. 2 L 7 2 4F 4 F RT A2NM E12EU 1996122600545 19961226 00545 NM 1996 12 26 CA960620014 1 19960529 A 5315 FLOOR BEAM BOEING 757 75723A 1384967 NM RROYCE RB211 RB211535E4 54555 NE BS 1681 CORROSION W K NONE O OTHER IN INSP/MAINT 1 CA 30655 (CAN) MODERATE CORROSION FOUND AT FLOOR BEAM STA 1681 4 INCHES + 8 INCHES + 4 INCHES LEFT OF CENTER OF BEAM ON FORWARD F ACE OF UPPER FLANGE, 12 INCHES LEFT OF CENTER ON AFT UPPER FLANGE, 30 INCHES RIGHT OF CENTER ON LOWER FACE OF UPPER FLA NGE. REPAIRED. 2 L 7 2 4F 4 F RT A2NM E12EU 1996122600546 19961226 00546 NM 1996 12 26 CA960620015 1 19960529 A 2510 3A090015011 TORQUE TUBE 3A0900015 BOEING 757 75723A 1384967 NM RROYCE RB211 RB211535E4 54555 NE CAPT SEAT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 30655 (CAN) CAPTAINS SEAT TORQUE TUBE CRACKED. REPLACED WORN ADJUSTMENT CABLE AND TUBE. 2 L 7 2 4F 4 F RT A2NM E12EU 1996122600547 19961226 00547 EA 1996 12 26 CA960620016 2 19960606 A 7310 S123630190 FUEL HOSE CESSNA S123630190 CESSNA 182 R182 2072734 CE LYC O540 O540L3C5 41532 EA MCAULY 2D34C B2D34C214 GL CARB DETERIORATION W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 3504 778345 (CAN) A BRAIDED FUEL LINE BETWEEN THE CARBURETOR AND 90 DEGREE ELBOW ON THE LEFT SIDE OF THE FIREWALL WAS FOUND SATURATE D WITH FUEL AND STAINED. IT WAS FOUND THAT THE INTERIOR OF THE LINE WAS BEGINNING TO BREAK DOWN. LINE CHANGED. 1 H 7 1 3O 3 O RT 3A13 E295 5 C P7EA 1996122600548 19961226 00548 CE 1996 12 26 CA960620019 1 19960611 A 3230 2243001205 BELLCRANK CESSNA 2243001205 CESSNA 182 R182 2072734 CE MCAULY 2D34C B2D34C214 GL MLG LOOSE BOLT W K NONE O OTHER IN INSP/MAINT 1 CA 4033 4033 780298 (CAN) LOOSE BOLT FOUND DURING 100 HOUR INSPECTION DURING THE GEAR RETRACTION TESTS. SUBMITTER NOTES THIS IS THE SECOND OCCURENCE. SUBMITTER RECOMMENDS REPLACING THE BOLT WITH A DRILLED HEAD VERSION FOR LOCKWIRE SAFETY PURPOSE. BOLT P/N N AS464P3A3. 1 H 7 1 3O RT 3A13 5 C P7EA 1996122600549 19961226 00549 NM 1996 12 26 CA960620021 1 19960611 A 3610 321N53217 DUCT ASSEMBLY BOEING 757 757236 NM RROYCE RB211 RB211535E4 54555 NE ENG BLEED SEAL DAMAGE W K NONE M OVER TEMP IN INSP/MAINT 1 CA 30739 (CAN) SIGN OF OVERHEAT DETECTED AT ENGINE OUTBOARD 'C' DUCT ACCESS PANEL, TOP. AIR OFF TAKE DUCT ASSEMBLY FROM HP6 STAGE WAS LEAKING HOT AIR. DUCT REMOVED AND DETERIORATED EXPANSION JOINT SEAL WAS FOUND. OTHER SIGNS OF OVERHEAT DETECTED, TH RUST REVERSER HYDRAULIC HOSES REPLACED AS PRECAUTION. 2 L 7 2 4F 4 F RT A2NM E12EU 1996122600550 19961226 00550 EU 1996 12 26 CA960620025 1 19960603 A 2910 T2C5000605500 LINE BRAERO 748 HS7482A 4231001 EU HYD SYS BROKEN W O OTHER K FLUID LOSS DE DESCENT 1 CA (CAN) LOSS OF HYDRAULIC PRESSURE, ACHIEVED 3 GREEN/DOWN LOCKED. LANDED WITHOUT INCIDENT. LINE REPLACED. 2 L 7 2 3T A24EU 1996122600552 19961226 00552 NM 1996 12 26 CA960624002 1 19960612 A 2420 WIRE BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE AC GEN SYS MISINSTALLED W K NONE H J W ELECT. POWER LOSS-50 PC WARNING INDICATION INADEQUATE Q C DE DESCENT 1 CA 687714 (CAN) ON GROUND AND BOTH GENERATORS TRIPPED OFF WITH STANDBY POWER AS WELL, THEN ALL RETURNED TO NORMAL. ON TAXI SAME T HING HAPPENED. ON DESCENT NEXT FLIGHT SAME, LOSS POWER BETWEEN 500' AND 200' BEFORE ALL POWER RETURNED TO NROMAL. REPLAC ED GENERATOR POWER CONTROL RELAY. TWO DAYS LATER SAME, VOLTAGE SENSOR CARD REPLACED. ON TAXI IN SHUT DOWN #2 ENGINE, LOS T STANDBY POWER. FOUND CONTROL WIRES TO R3 CROSSED. REPAIRED. 2 L 7 2 4F 4 F A16WE E2EA 1996122600553 19961226 00553 SO 1996 12 26 CA960624003 1 19960617 A 2910 HOSE PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2C 41532 EA NLG ACTUATOR LEAKING W A UNSCHED LANDING P K NO WARNING INDICATION FLUID LOSS CL CLIMB 1 CA RL348661A (CAN) NO GREEN LIGHT ON GEAR RETRACTION. ON GEAR EXTENSION, NOSE GEAR REMAINED PARTIALLY EXTENDED. ON LANDING, NOSE GEAR FOLDED. HYDRAULIC HOSE LEAKING ON THE DOWN SIDE OF THE NOSE GEAR ACTUATOR WHICH DEPLETED BOTH THE MAIN AND EMERGENCY HY DRAULIC SYSTEMS. 1 L 7 2 3O 3 O A20SO E14EA 1996122600554 19961226 00554 NM 1996 12 26 CA960625001 1 19960619 A 2910 NAS161210 SEAL ESSEX 90115201001 BOEING 737 7372T7 NM PWA JT8 JT8D17 52049 NE HYD SYS LEAKING W A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 CA 708808 (CAN) AIRCRAFT DIVERTED DUE TO LOSS OF HYDRAULIC FLUID. ATTENUATOR SEAL REPLACED. 2 L 7 2 4F 4 F RT A16WE E2EA 1996122600555 19961226 00555 CE 1996 12 26 CA960625011 1 19960605 A 2910 1145800501 PIPE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3A NE RESERVOIR CRACKED W O OTHER J K WARNING INDICATION FLUID LOSS DE DESCENT 1 CA 2406 PCE114293 HJ339 (CAN) HYDRAULIC FLUID LOW LIGHT ON DESCENT. SOLID LINE FROM THE FILLER POINT TO THE RESERVOIR CRACKED AT THE FLARE. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 1996122600557 19961226 00557 NM 1996 12 26 CA960626102 1 19960613 A 2750 285T00495 ELECTRONIC UNIT BOEING 285T004953 BOEING 767 767375 NM FLAP CONTROL FAILED W A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CA 32394 30631 D00284 (CAN) AFTER TAKEOFF FLAPS WOULD NOT RETRACT FROM 1 TO UP. TRIED UNSUCCESSFULLY SEVERAL TIMES, ALSO ALT FLAP, NO CHANGE. REPLACED FLAP/SLAT ELECTRONIC UNIT. 2 L 7 2 4F RT A1NM 1996122600559 19961226 00559 NM 1996 12 26 CA960627102 1 19960611 A 2761 DREM10122 ROD END BOEING 727 72722 1384002 NM PWA JT8 JT8D7B 52053 NE NR 11 SPOILER BROKEN W K NONE F FLT CONT AFFECTED CR CRUISE 1 CA 655353 (CAN) AIRCRAFT REQUIRES 3 UNITS OF LEFT ROLL TRIM IN ALL PHASES OF FLIGHT. BROKEN ROD END ON #11 SPOILER ACTUATOR. ACTUA TOR REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 1996122600560 19961226 00560 NE 1996 12 26 CA960703002 1 19960623 A 6210 7610208000061 BLADE SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL M/R BLD LE SP CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA CAE890865S (CAN) A BORESCOPE INSPECTION OF BLADE ROOT END REVEALED A CRACK ON LEADING EDGE OF SPAR APPROXIMATELY 2" FROM ROOT END A ND APPROXIMATELY 1" IN LENGTH. EXACT LENGTH UNKNOWN AS CRACK PROCEEDS UNDER A PHENOLIC BLOCK. 1 G 7 2 3U 3 U H1NE E1GL 1996122600562 19961226 00562 CE 1996 12 26 CA960703004 1 19960618 A 5730 5012006897 SKIN BEECH BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA UPPER FWD FITTIN CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 9858 PCE50218 (CAN) SKIN CRACKS FOUND FROM THREE (3) FASTNER LOCATIONS AT THE UPPER INBOARD BATHTUB FITTING. BEECH CONTACTED AND REPLI ED WITH A 25 HOUR INSPECITON AS PER BEECH MESSAGE 52-5870. 1 L 7 2 3T 4 T A14CE E4EA 1996122600563 19961226 00563 EU 1996 12 26 CA960703005 1 19960609 A 3213 200633202 TORQUE LINKS DOWTY 200427010 FOKKER F28 F28MK1000 4990808 EU RTMLG LEG BROKEN W O OTHER O OTHER LD LANDING 1 CA DRG108372 (CAN) IMMEDIATELY AFTER A SMOOTH LANDING, A VERY STRONG VIBRATION STARTED IN THE MAIN LANDING GEAR. HEAVY BRAKE APPLICAT ION MOMENTARILY STOPPED THE VIBRATION, THEN IT STARTED AGAIN, FOLLOWED BY YAWING TO THE RIGHT, AND THE AIRCRAFT APPEARED TO LOWER ON THE RIGHT SIDE ONTO THE GEAR LEG. FURTHER YAWING WAS CONTROLLED BY ASYMMETRIC BRAKING AND STEERING. THE SEP ARATED R/H MAIN WHEELS CAUGHT UP WITH THE AIRCRAFT WHICH FINALLY STOPPED. AIRCRAFT EVACUATED ON RUNWAY. 2 L 7 2 4F RT A20EU 1996122600565 19961226 00565 SO 1996 12 26 CA960703008 1 19960626 A 2720 8DJ49GAY4 INDICATOR GE 8DJ49GAY2 LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL HAMSTD 54H 54H60117 NE RUD TRIM MALFUNCTION W K NONE O OTHER DE DESCENT 1 CA 11793 11793 K0360 500859 235867 (CAN) ON DESCENT WITH RUDDER TRIM AT ZERO IT WAS NOTED THAT THE TRIM INDICATOR HAD DRIFTED TO 10 DEGREES RIGHT. A FEW MI NUTES LATER INDICATION RETURNED TO ZERO WITH NO EFFECT TO FLIGHT CONTROL IN EITHER INSTANCE. INDICATOR REPLACED. 2 H 7 4 4T 4 T A1SO E282 6 C P906 1996122600567 19961226 00567 CE 1996 12 26 CA960703021 1 19960621 A 5541 0433010C SPAR CESSNA CESSNA 150 150M 2071830 CE CONT O200 O200A 17020 SO RUD UPPER HINGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 90101450 (CAN) DURING A 200 HOUR INSPECTION THE RUDDER SPAR WAS FOUND CRACKED. INSPECTED IN ACCORDANCE WITH SB 94.03. RUDDER SPAR WAS REPLACED. 1 H 7 1 3O 3 O 3A19 E252 1996122600569 19961226 00569 CE 1996 12 26 CA960703025 1 19960614 A 3210 NAS464P3A3 BOLT CESSNA 2243001205 CESSNA 182 R182 2072734 CE MCAULY 2D34C B2D34C214 GL MLG ASSY CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 4532 4532 778345 (CAN) BOLT CAME LOOSE. INVESTIGATION FOUND IT TO BE CORRODED AND BROKEN. SUBMITTER NOTED THAT THE AIRCRAFT IS OPERATED F ROM A GRAVEL STRIP. 1 H 7 1 3O RT 3A13 5 C P7EA 1996122600570 19961226 00570 1996 12 26 CA960703026 4 19960618 A 2330 48725009 VIDEO CONTROL LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB21122B02 54555 NE AFT STORAGE SHORTED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA 10171 (CAN) WHILE ENROUTE VIDEO CONTROL UNIT IN AFT STORAGE COMPARTMENT SMOKING BADLY. ALL CBS PULLED AND SYSTEM DEACTIVATED. FLIGHT CONTINUED. UNIT REPLACED. 2 L 7 3 4F 4 F A23WE E12EU 1996122600571 19961226 00571 CE 1996 12 26 CA960703028 1 19960613 A 2440 C5930050101 MONITOR CESSNA C5930050101 CESSNA 208 208B 2073701 CE PWA PT6 PT6A114 52043 NE GROUND PWR OVER VOLT COND W O OTHER H ELECT. POWER LOSS-50 PC IN INSP/MAINT 1 CA 0115362 PCE17268 (CAN) THE AIRCRAFT APPEARS TO HAVE SUSTAINED AN OVERVOLTAGE CONDITION DURING THE COURSE OF MAINTENANCE WITH THE GROUND P OWER APPLIED. THE AIRCRAFT HAS A GROUND POWER MONITOR FOR OVERVOLTAGE PROTECTION. 1 H 7 1 3T 3 T A37CE E4EA 1996122600573 19961226 00573 SW 1996 12 26 CA960704002 1 19960624 A 5320 206031106017 STIFFENER BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL VERTICAL TUNNEL CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 12517 CAE821934 (CAN) STIFFENER FOUND CRACKED. CRACK ORIGINATING FROM LOWER ONE OF FOUR HUCK RIVETS AT UPPER END OF STIFFENER. 1 G 7 1 3U 3 U H2SW E4CE 1996122600574 19961226 00574 CE 1996 12 26 CA960704003 1 19960624 A 2750 1005240741 GEARBOX RAYTHN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FLAP MOTOR DAMAGED GEARS W A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CA 1391 PCE114357 (CAN) THE FLAP MOTOR TRIPPED THE CIRCUIT BREAKER AND DAMAGED THE GEARBOX DRIVE GEAR. THE RIGHT HAND SPLIT SAFETY SWITCH FOUND STICKING AND THE SWITCH ACTUATOR ROD END WAS FOUND STIFF. 2 L 7 2 4T 4 T RT A24CE E26NE 1996122600576 19961226 00576 NM 1996 12 26 CA960708005 1 19960701 A 2761 106051511 ACTUATOR BORGWARNER 106051511 BOEING 727 727212 138407G NM PWA JT8 JT8D7B 52053 NE NR 14 SPOILER BINDING W D RETURN TO BLOCK E VIBRATION/BUFFET TX TAXI/GRND HDL 1 CA 399734 654890 (CAN) DURING PRE-TAKEOFF CHECKS A VIBRATION WAS GENERATED WHEN RIGHT AILERON WAS COMMANDED. AIRCRAFT RETURNED TO BLOCKS. #14 SPOILER ACTUATOR WAS BINDING, REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 1996122600578 19961226 00578 CE 1996 12 26 CA960709003 1 19960626 A 3213 3581524613 BUSHING BEECH 95810002756 BEECH 95 E95 1153410 CE LYC O360 IO360B1B 41514 EA RT MLG OVERSIZED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA L496351A (CAN) RIGHT HAND MAIN LANDING GEAR BUSHING PURCHASED NEW FROM BEECHCRAFT FOUND TO BE OUTSIDE THE TOLERANCE OF THE MAINTE NANCE MANUAL. THE BUSHING WAS RETURNED FOR A CREDIT. 1 L 7 2 3O 3 O 3A16 1E10 1996122600580 19961226 00580 1996 12 26 CA960711007 4 19960710 A 3418 10615 TRANSFORMER OECO 10615 BOEING 747 747475 NM AOA SENSOR BURNT W K NONE M OVER TEMP TX TAXI/GRND HDL 1 CA 3598 (CAN) LH ANGLE OF ATTACK SENSOR FAILED. ON INSTALL ANGLE OF ATTACK SENSOR TRANSFORMER OVERHEATED AND CAUSED BURNING SMEL L IN COCKPIT. TRANSFORMER SELF DESTRUCTED. REPLACED. 2 L 7 4 4F RT A20WE 1996122600581 19961226 00581 NM 1996 12 26 CA960711008 1 19960710 A 2420 941D3352 BREAKER SUNDSTRAND 941D3352 BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE NR 1 GEN BURNT W D RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 CA RA3850 667246 (CAN) AIRCRAFT RETURNED AFTER ENGINE START DUE #1 GENERATOR WOULD NOT GO ON LINE. REPLACED BUS TIE BREAKER. 2 L 7 2 4F 4 F A16WE E2EA 1996122600582 19961226 00582 EU 1996 12 26 CA960711010 1 19960621 A 2750 A83021407 DRIVE SHAFT FOKKER F28 F28MK1000 4990808 EU FLAPS WORN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) FLAP DRIVE ASSEMBLY WORN BETWEEN FLAP MOTOR AND SELECTOR, COTTER PIN MISSING AT FLAP DRIVE. REPLACED FLAP DRIVE, T HREE U-JOINTS. 2 L 7 2 4F RT A20EU 1996122600586 19961226 00586 CE 1996 12 26 CA960711017 1 19960708 A 7160 265805713 ACTUATOR ARM CESSNA 265805713 CESSNA 208 208B 2073701 CE PWA PT6 PT6A114 52043 NE INERTIAL SEP CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 12707 12707 17280 (CAN) THE INERTIAL SEPARATOR ACTUATOR ARM CRACKED AT THE ATTACH POINT FOR THE CONTROL ROD EYE BOLT. THE ACTUATOR ARM WAS REPLACED. SUBMITTER STATES THAT THIS IS THE SECOND OCCURRENCE IN THE PAST 4 YEARS. 1 H 7 1 3T 3 T A37CE E4EA 1996122600588 19961226 00588 EA 1996 12 26 CA960712105 1 19960619 A 6710 107D31544 ADAPTER BOEING 107 1072 9420604 EA GE CT58 CT581401 30011 NE SYNCH SHAFT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 755 292 280224A (CAN) DURING EDDY CURRENT INSPECTION (MIZ-20A) OF #5 SYNCH SHAFT ADAPTER AS PER BV AD82-11-05, A CRACK IN THE KEY SLOT W AS DETECTED. A SUBSEQUENT DYE PENETRANT INSPECTION REVEALED NO FURTHER CONFIRMATION OF SUSPECTED CRACK. COMPONENT WAS RE MOVED FROM AIRCRAFT AND SUSPECTED AREA WAS INSPECTED UNDER MAGNIFICATION, STILL WITH NO POSITIVE EVIDENCE OF THE CRACK. THE ADAPTER WAS REMOVED & REPLACED WITH NEW. THE FEEDBACK REPORT INDICATED THE SUSPECT ADAPTER WAS INSPECTED USING MAGNE TIC PARTICLE METHOD. A SMALL CRACK WAS FOUND IN SPLINE WHICH WAS TOO SMALL TO BE DETECTED BY EDDY CURRENT SIGNAL. IT IS FELT THAT PLATING FRETTING EDGE CAUSED THE REJECT EDDY CURRENT SIGNAL & THE SHOP OVERHAULING THESE ADAPTERS HAVE BEEN AD 2 G 7 2 4U 4 U 1H16 1E3 1996122600589 19961226 00589 WP 1996 12 26 CA960712106 1 19960611 A 6220 369H120331 LEAD LAG LINK HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL M/R LINK EAR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 2764 2764 CAE832839 (CAN) CRACK FOUND ON EAR OF LEAD - LAG LINK. FROM BOLT HOLE TO EDGE. 1 G 7 1 3U 3 U H3WE E4CE 1996122600590 19961226 00590 WP 1996 12 26 CA960712107 1 19960611 A 5210 369H202471 WINDOW HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL PILOTS DOOR DEPARTED W A UNSCHED LANDING D INFLIGHT SEPARATION CR CRUISE 1 CA CAE830150 (CAN) PILOT NOTICED INCREASED NOISE FOLLOWED BY WINDOW AND SEAL DEPARTING AIRCRAFT. IT IS BELIEVED THAT WINDOW WAS PROBA BLY INSTALLED FROM OUTSIDE OF DOOR INSTEAD OF FROM INSIDE DOOR FRAME. 1 G 7 1 3U 3 U H3WE E4CE 1996122600591 19961226 00591 SO 1996 12 26 CA960712108 1 19960702 A 3234 487155 SOLENOID PIPER PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2B 41532 EA GEAR SELECTOR INTERMITENT W K NONE O OTHER IN INSP/MAINT 1 CA 8266 L735161 (CAN) THE SOLENOID WAS FUNCTIONING ON AN INTERMITTENT BASIS. THE PROBLEM WAS TRACED TO A GUMMY DEPOSIT FOUND IN THE TIGH T TOLERANCE AREA OF THE SLIDING PARTS. IT LEAD TO A BENDING OF THE SOLENOID PLUNGER. THE PART WAS REPLACED AND THE AIRCR AFT RETURNED TO SERVICE. 1 L 7 2 3O 3 O A20SO E14EA 1996122600592 19961226 00592 CE 1996 12 26 CA960715001 1 19960630 A 3230 105962 MOTOR PRESTOLITE 105932 BEECH 100 100BEECH 1152916 CE PWA PT6 PT6A28 EA MLG FAILED W L O ABORTED APPROACH OTHER P NO WARNING INDICATION LD LANDING 1 CA 4798 AH1840 PCE50123 (CAN) THE GEAR DOWN LIGHTS WERE NOT ILLUMINATED. BOTH GEAR MOTOR AND INDICATOR BREAKERS WERE RESET AND THE GEAR CYCLED A GAIN. NO RESULTS. THE EMERGENCY GEAR DOWN PROCEDURES FOLLOWED AND THE AIRCRAFT LANDED SAFELY. INSPECTION FOUND THE HYDRA ULIC GEAR MOTOR HAD FAILED INTERNALLY. A NEW MOTOR WAS INSTALLED AND THE AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 3T 4 T A14CE E4EA 1996122600593 19961226 00593 EA 1996 12 26 CA960715005 1 19960708 A 7120 ENGINE MOUNT DHAV DHAV DHC6 DHC6300 EA PWA PT6 PT6A27 52043 EA #2 ENGINE BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA PCE40583 (CAN) INSPECITON FOR HEAVY LANDING FOUND #2 PROPELLER SPINNER NOT CENTRED IN REFERENCE TO COWLING. INVESTIGATION SHOWED #2 INBOARD LOWER ENGINE MOUNT BROKEN. 1 H 7 2 3T 4 T A9EA E4EA 1996122600594 19961226 00594 NM 1996 12 26 CA960715006 1 19960705 A 3231 1V10851 SEQUENCE VALVE BOEING 727 727277 138408S NM PWA JT8 JT8D15 52051 NE LT MLG DOOR CRACKED W A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 CA 695337 (CAN) ON DEPARTURE A SYSTEM HYDRAULIC FLUID LOST. LH MLG DOOR LOCK OPERATED SEQUENCE VALVE HOUSING CRACKED. REPLACED. 2 L 7 3 4F 4 F RT A3WE E2EA 1996122600595 19961226 00595 GL 1996 12 26 CA960715008 1 19960704 A 6220 28142649 DAMPER ENSTRM F28 280C 3300505 GL LYC O360 HIO360E1AD 41514 EA M/R HUB ATTACH SHEARED BOLT W K NONE O OTHER IN INSP/MAINT 1 CA L1911151A (CAN) BOLT FOUND SHEARED IN TWO AT THE ATTACHMENT TO THE MAIN ROTOR HUB. 1 G 7 1 3O 3 O H1CE 1E10 1996122600597 19961226 00597 NM 1996 12 26 CA960716001 1 19960705 A 3230 82970010173 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 SEQ VALVE CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 120832 (CAN) CONSIDERABLE AMOUNT OF FLUID COMING FROM #1 GEAR WELL. FOUND CRACKED HYDRAULIC LINE TO SEQUENCING VALVE. 2 H 7 2 4T 4 T RT A13NM E20NE 1996122600598 19961226 00598 EU 1996 12 26 CA960716002 1 19960711 A 5753 BOLTS BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE AFT FLAP TRACK LOOSE W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 18163 18163 LF05567A (CAN) FUEL DRIPPING FROM #1 PYLON. LEAK FOUND TO BE RESULT OF TWO LOOSE HIGHLOCK BOLTS AT DOUBLER AT REAR FLAP TRACKS. B OLTS TORQUE TIGHTENED AND RESEALED. 2 H 7 4 4F 4 F RT A49EU E6NE 1996122600599 19961226 00599 EA 1996 12 26 CA960716003 1 19960711 A 3221 85310339009 TRUNNION DHAV DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE NOSE GEAR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 123136 (CAN) BOTH NOSE LANDING GEAR TRUNNIONS FOUND CRACKED THE WEB AREA. MOD 8/1880 (SB 8-53-45) P/N 85310339.011 TRUNNION INS TALLED. 2 H 7 2 4T 4 T RT A13NM E20NE 1996122600600 19961226 00600 EA 1996 12 26 CA960716005 2 19960711 A 8520 LW12372 CRACKCASE CESSNA 177 177B 2073708 CE LYC O360 O360A1F6 41514 EA AREA #2 CYLINDER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1028 L2330036A (CAN) CRACK DETECTED VISUALLY ON CRANKCASE AT UPPER LEFT HAND FORWARD OF #2 CYLINDER MOUNT STUD. NO OIL LEAK WAS EVIDENT , HOWEVER THE CRACK APPEARED TO ORIGINATE IN THE AREA OF A PREVIOUS WELDED REPAIR. 1 H 7 1 3O 3 O A13CE E286 1996122600602 19961226 00602 SW 1996 12 26 CA960716007 1 19960701 A 6210 K911001009 BLADE KAMAN K1200 K1200 05625F6 SW LYC T53 T5317A 41549 NE M/R LT HAND CRACKED W A UNSCHED LANDING F FLT CONT AFFECTED HO HOVERING 1 CA 388 LE81024 (CAN) DURING HELI LOGGING OPERATION THE PILOT NOTICED INCREASED RIGHT PEDAL REQUIRED TO MAINTAIN POSITION. WHEN IT BECAM E OBVIOUS THAT WIND CONDITIONS WERE NOT RESPONSIBLE THE HELICOPTER LANDED WHERE IT WAS FOUND THAT THE BLADE HAD A 10" CR ACK CHORDWISE ACROSS THE TOP OF THE BLADE APPROXIMATELY 1.5" INTO ABRASION STRIP AND WITHIN 1.5" OF TRAILING EDGE AT STN .162. 1 G 7 1 4F 4 U NT TR7BO E17EA 1996122600604 19961226 00604 EA 1996 12 26 CA960716010 1 19960705 A 2910 DSC252B40124 LINE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE NLG ACTUATOR FAILED W K NONE K FLUID LOSS CL CLIMB 1 CA 123018 (CAN) FLIGHT CREW REPORTED #2 HYDRAULIC FLUID LOST ENROUTE STARTING AFTER INITIAL GEAR RETRACTION. FLEX LINE ON NOSE LAN DING GEAR ACTUATOR LEAKING. LINE FAILED AT SWAGE. 2 H 7 2 4T 4 T RT A13NM E20NE 1996122600605 19961226 00605 SO 1996 12 26 CA960716011 1 19960627 A 3240 492152 VALVE PIPER PA31 PA31350 7103110 SO PARK BRAKE BROKEN CABLE W O OTHER O OTHER CL CLIMB 1 CA 14987 (CAN) PARK BRAKE FOUND BROKEN. SUSPECT THAT DURING CLIMB THE PILOTS APPLIED BRAKE PRESSURE PRIOR TO GEAR RETRACTION AND PRESSURE RELIEF ALLOWED THE ACTUATOR ARM TO MOVE TO THE ON POSITION. THE AIRCRAFT LANDED AND THE BRAKES OVERHEATED AND C AUSED THE BRAKE CABLE TO STRETCH AND BREAK. 1 L 7 2 3O A20SO 1996122600606 19961226 00606 EU 1996 12 26 CA960716012 1 19960709 A 3240 190287 CONTROL CABLE 251130 BAG JETSTM JETSTM4112 EU PARKING BRAKE BROKEN W O OTHER O OTHER NR NOT REPORTED 1 CA 3280 (CAN) EMERGENCY PARK BRAKE CABLE FOUND BROKEN NEAR THE FORK END FITTING. 1 L 7 2 4T RT A196 1996122600607 19961226 00607 NM 1996 12 26 CA960717002 1 19960709 A 2710 82710097101 SPRING DHAV DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE CLUTCH MALFUNCTION W O OTHER F FLT CONT AFFECTED LD LANDING 1 CA 123046 (CAN) AIRCRAFT EXPERIENCED AN UNCOMMANDED ROLL DISCONNECT ON LANDING. ROLL DISCONNECT SYSTEM INSPECTED AND NO FAULT FOUN D. MANUFACTURER NOTIFIED. AWAITING APPROVAL OF DEHAVILLAND SB 8-27-79 REINSTALLATION AND REPOSITION OF MODIFIED DISCONNE CT SPRING. 2 H 7 2 4T 4 T RT A13NM E20NE 1996122600608 19961226 00608 NM 1996 12 26 CA960717003 1 19960605 A 3210 HANDLE DHAV DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE RT WHEEL WELL FOULING W O OTHER C F.O.D. CL CLIMB 1 CA 120543 (CAN) STARBOARD MAIN GEAR DID NOT LOCK UP. INSPECTION REVEALED THAT HANDPUMP HANDLE WAS FOULING GEAR IN RH NACELLE. BRAC KETS TO HOLD HANDLE IN NACELLE WERE REMOVED BY COMPANY AND IT WILL BE KEPT ONBOARD ONLY. 2 H 7 2 4T 4 T RT A13NM E20NE 1996122600609 19961226 00609 SW 1996 12 26 CA960717004 1 19960710 A 6220 212010300001 STABILIZER BAR BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA M/R PITCH LINK WORN BEARING W K NONE O OTHER IN INSP/MAINT 1 CA CPPS61494 (CAN) EXCESSIVE PLAY DISCOVERED IN BEARING ALSO ON BOLT. 1 G 7 1 4U 4 U H4SW E22EA 1996122600610 19961226 00610 SW 1996 12 26 CA960719001 1 19960711 A 3250 2781032682 LINE SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP NOSE WHEE WELL CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 15868 P54202 (CAN) CAPTAIN REPORTED A SMALL HYDRAULIC LEAK IN AREA OF HYDRAULIC FILTER IN NOSE WHEEL WELL. INSPECTION FOUND SHORT HIG H PRESSURE LINE ATTACHED TO NOSE STEERING FILTER CRACKED AND LEAKING. HYDRAULIC ACCUMULATOR WAS FLAT. A FLAT ACCUMULATOR CAN CAUSE A 'BUZZ' AND CAN LEAD TO HYDRAULIC LINE FAILURE. SUBMITTER NOTES THAT SERVICING OF ACCUMULATOR IS COVERED BY A PHASE INSPECTION AT EVERY 300 HOURS, THIS IS CONSIDERED ADEQUATE. SUBMITTER ALSO USES A FORM TO INDICATE LOSS OF HYDRA ULIC PRESSURE AND WHAT WAS DONE TO CORRECT. 2 L 7 2 4T 4 T RT A8SW E4WE 1996122600611 19961226 00611 NE 1996 12 26 CA960719002 2 19960711 A 7270 D361100260200 FAN AIR DUCT AIRBUS 320 A320212 EU CFMINT CFM56 CFM565A1 NE ENGINE DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ON INSPECTION, FAN AIR VALVE P/N 6730B01, FAN AIR DUCT AND FAN AIR OUTLET P/N D361100300200 FOUND DAMAGED. ALSO FO UND CHAFED MANIFOLD OUTER P/N 144M50 G12. ALL DAMAGED PARTS REPLACED. SUSPECT DAMAGED WAS CAUSED BY LOOSE CLAMP. 2 L 7 2 4F 4 F RT A28NM E29NE 1996122600612 19961226 00612 NM 1996 12 26 CA960719101 1 19960709 A 2432 24M220 CELLS MARATHON 255823 BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE BATTERY MELTED W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA 10779 1106 0355 674513 (CAN) ON WALKAROUND CREW REPORTED HOT PLASTIC BURNING SMELL IN CABIN. FOUND BATTERY OVERHEATED. REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1996122600613 19961226 00613 EU 1996 12 26 CA960719102 1 19960712 A 3231 D3221007100000 BELL CRANK PIN AIRBUS 320 A320211 3930320 EU NLG DOOR SHEARED W A UNSCHED LANDING D E J INFLIGHT SEPARATION VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 CA (CAN) IMMEDIATELY AFTER ROTATION A LOUD NOISE AND VIBRATION OCCURRED DURING LANDING GEAR RETRACTION. GEAR INDICATED GREE N AND RED IN TRANSIT. MAINTENANCE INVESTIGATION REVEALED THE PIN WHICH ATTACHES THE NOSE GEAR DOOR HYDRAULIC ACTUATOR TO THE BELLCRANK HAD SHEARED. BUSHING AND PIN REPLACED AND GEAR SWUNG. 2 L 7 2 4F RT A28NM 1996122600615 19961226 00615 SW 1996 12 26 CA960722006 1 19960709 A 2710 PANEL SWRNGN SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP BELLY JAMS AILERON W A C ABORTED TAKEOFF F FLT CONT AFFECTED TX TAXI/GRND HDL 1 CA 22820 P54259 (CAN) ON PREFLIGHT CREW FOUND AILERONS JAMMED. INVESTIGATION FOUND THAT THE RIGHT HAND BELLY PANEL (PANEL 612) THAT COVE RS THE AILERON PUSH PULL RODS AND THE FLAP INTERCONNECT WAS BULGED INWARDS AND WAS FOULING THE AILERON SWING LINK. A HOL E HAD DEVELOPED IN THE PANEL ALLOWING THE AILERON PUSH PULL ROD END BOLT TO CATCH THE HOLE AND JAM THE AILERON. (SEE IPC 27-10-03, FIG.1, ITEM 18, SWING LINK, P/N 27-71004-035). SWING LINK CAN BE INSTALLED IN TWO WAYS. (1) ANGLED UP IT VERY CLOSE TO FLAP INTERCONNECT BEAM. (2) ANGLED DOWN (CONDITION FOUND) WITH PUSH ROD END BOLTS INSTALLED HEAD ON TOP, THE B OLT ENDS ARE CLOSE TO THE PANEL. SUBMITTER SAYS THEY INSTALLED THE BOLTS WITH THE NUT AND COTTER KEY ON TOP, GIVING MAX. 2 L 7 2 4T 4 T RT A8SW E4WE 1996122600616 19961226 00616 NM 1996 12 26 CA960722007 1 19960715 A 2760 82970010217 LINE DHAV DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE DUMP VALVE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 120817 (CAN) HYDRAULIC FLUID LEAKING FROM #1 WHEEL WELL. INVESTIGATION FOUND HYDRAULIC LINE LEAKING FROM THE FORWARD LIFT DUMP VALVE FOR THE FLIGHT SPOILERS. 2 H 7 2 4T 4 T RT A13NM E20NE 1996122600618 19961226 00618 EA 1996 12 26 CA960722009 1 19960524 A 2720 C2CF741AND CONTROL CABLE DHAV DHC2 DHC2MK1 2800102 EA PWA R985 R985AN14B 52008 NE RUDDER FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA 210 JP210653 (CAN) ON 100 HOUR INSPECTION BOTH RELATIVELY NEW RUDDER CABLES WERE FOUND FRAYED AT FIRST PULLEY AFT OF RUDDER PEDAL CON NECTIONS. THE CABLES WERE STAINLESS AND ARE SUPPOSED TO BE GOOD FOR 1000 HOURS PLUS. 1 H 7 1 3R 3 R A806 5E1 1996122600619 19961226 00619 EU 1996 12 26 CA960722011 1 19960712 A 2731 AS104 BEARING BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE ELEVATOR TRIM SEIZED W K NONE O OTHER IN INSP/MAINT 1 CA LF05784A (CAN) DURING MAINTENANCE OF ELEVATOR TRIM SYSTEM THE TRIM SEEMED VERY STIFF AND JUMPY. FOUND HORIZONTAL STAB CENTRE REAR SPAR PULLEY SEIZED. 2 H 7 4 4F 4 F RT A49EU E6NE 1996122600620 19961226 00620 WP 1996 12 26 CA960723001 1 19960702 A 7810 369A287007 CLAMP HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL EXHAUST PIPE LOOSE W A UNSCHED LANDING D INFLIGHT SEPARATION DE DESCENT 1 CA CAE834289 (CAN) PILOT EXPERIENCED A MOMENTARY JAMMED T/R PEDAL. INSPECTION FOUND THE CLAMP AT THE AFT SECTION OF THE EXHAUST STACK HAD DEPARTED CAUSING DAMAGE TO THE TAILBOOM, T/R ASSEMBLY, T/R SWASHPLATE AND T/R CONTROL ROD. 1 G 7 1 3U 3 U H3WE E4CE 1996122600621 19961226 00621 NM 1996 12 26 CA960723003 1 19960718 A 5101 STRUCTURE BOEING 737 7372T7 NM PWA JT8 JT8D17 52049 NE AIRFRAME DAMAGED W A UNSCHED LANDING C F.O.D. CR CRUISE 1 CA 708808 (CAN) AIRCRAFT DECLARED AN EMERGENCY AND DIVERTED. EXTENSIVE DAMAGE TO LEADING EDGES, HORIZONTAL STAB, VERTICAL STAB, RA DOME, #1 WINDSHIELD CRACKED. ALL SLATS REPAIRED OR REPLACED. UPPER ANTI COLLISION LIGHT DAMAGED. 2 L 7 2 4F 4 F RT A16WE E2EA 1996122600622 19961226 00622 EA 1996 12 26 CA960723009 2 19960705 A 7414 10357584 DISTRIBUTOR GEAR BENDIX 101630052 BEECH 95 D95A 1153408 CE LYC O360 IO360B1B 41514 EA GEAR/SHAFT HUB LOOSE ELECTRODE W K NONE O OTHER IN INSP/MAINT 1 CA 651 K249202ER L285951A (CAN) THE MAGNETO WAS SENT IN FOR WARRANTY REPAIR. A TEST FOUND THAT THE UNIT WAS FIRING ON ONE CYLINDER. INSPECTION FOU ND THAT THE ELECTRODE HAD BROKEN FREE OF ITS MOUNTING. THE UNIT WAS GIVEN A 500 HOUR SERVICE AND THE DEFECTIVE PART REPL ACED AND THE UNIT RETURNED TO SERVICE. 1 L 7 2 3O 3 O 3A16 1E10 1996122600623 19961226 00623 EU 1996 12 26 CA960723010 1 19960628 A 2822 SPE19841 ARMATURE PLESSEY BP1RSMK6 BRAERO 748 HS7482A 4231001 EU BOOST PUMP WRONG PART W A K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 41352R (CAN) BOOST PUMP RECEIVED FOR OVERHAUL. INSPECTION DISCOVERED THAT THE ARMATURE HAD BEEN MODIFIED TO ACCEPT A DIFFERENT TYPE (SIZE) OF BEARING. THE ARMATURE SHOULD HAVE MEASURED .236" FOR THE COMMUTATOR END BEARING JOURNAL. THE JOURNAL HAD BEEN REWORKED TO .296". THE PROPER BEARING P/N IS SPE 100020 OR 515-4-13303, THE BEARING THAT WAS INSTALLED WAS MRC, P/N 35ZZ. ARMATURE REPLACED. 2 L 7 2 3T A24EU 1996122600624 19961226 00624 SW 1996 12 26 CA960723013 1 19960712 A 5280 DOOR SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP RH MLG BENT W O OTHER G MULTIPLE FAILURE AP APPROACH 1 CA 21631 P54174 (CAN) CREW HAD TROUBLE GETTING RIGHT MLG TO EXTEND USING EITHER NORMAL OR EMERGENCY SYSTEM. AFTER RESETTING THEY GOT IT TO EXTEND WITH NORMAL SYSTEM. INVESTIGATION FOUND THAT THE RIGHT HAND OUTBOARD GEAR DOOR WOULD HANG UP ON THE NACELLE. T HE GEAR DOOR WAS REWORKED TO PROVIDE THE NECESSARY CLEARANCE. IN ADDITION, A CRACKED DOOR ACTUATING SHAFT P/N 2755001009 , WAS REPLACED. AIRCRAFT RECENTLY IMPORTED. AD 90-05-06R1 WAS APPARENTLY COMPLETED. SUBMITTER BELIEVES DOOR MAY HAVE BEE N BENT BY GROUND HANDLING ACCIDENT. 2 L 7 2 4T 4 T RT A8SW E4WE 1996122600625 19961226 00625 NE 1996 12 26 CA960723015 2 19960710 A 7310 3038454 FUEL FILTER PWA 3035817 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE #2 ENG LP WRONG FILTER W O OTHER W INADEQUATE Q C NR NOT REPORTED 1 CA 789 120176 (CAN) #2 ENGINE FUEL FILTER BYPASS CAUTION LIGHT ILLUMINATES AT POWER SETTINGS ABOVE 45 PERCENT. INVESTIGATION FOUND A S HORTER TYPE OF FUEL FILTER (P/N 3038454) WAS INSTALLED INSTEAD OF THE LONGER TYPE (P/N 3035729). DUE TO THE INSUFFICIENT LENGTH OF THE FILTER IT HAD BEEN LOOSE IN THE FILTER BOWL AND HAD CAUSED WEAR TO BOTH THE FILTER AND THE FILTER BOWL. I N THIS CONDITION THE FUEL WAS NOT BEING FILTERED. NB P/N 3038454 FUEL FILTER IS TO BE USED IN CONJUNCTION WITH A SPRING ASSEMBLY. 2 H 7 2 4T 4 T RT A13NM E20NE 1996122600626 19961226 00626 EA 1996 12 26 CA960723501 1 19960412 A 3231 LINKAGE CNDAIR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE NLG DOOR OUT OF ADJUST W A UNSCHED LANDING O OTHER CL CLIMB 1 CA 2872 2872 807181 (CAN) AFTER TAKEOFF AND GEAR RETRACTION, NOSE GEAR BEGAN MAKING CLUNKING NOISE. FOUND NOSE GEAR DOOR LINKAGE OUT OF ADJU STMENT. ACTUATING RODS ADJUSTED. 2 L 7 2 4F 4 F RT A21EA E15NE 1996122600627 19961226 00627 EA 1996 12 26 CA960723502 1 19960413 A 2752 ACTUATOR CNDAIR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE RIGHT OUTB FLAP FAILED W O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 CA 2875 807181 (CAN) AFTER LANDING FLAP RETRACTION FAILED AT 14 DEGREES. CHANGED RIGHT WING OUTBAORD FLAP INBOARD SCREW JACK ACTUATOR D UE TO HIGH FRICTION. ALSO CHANGED FLAP P.D.U. 2 L 7 2 4F 4 F RT A21EA E15NE 1996122600628 19961226 00628 EU 1996 12 26 CA960723503 1 19960414 A 2720 TRIM ACTUATOR AIRBUS 320 A320211 3930320 EU RUD AUTO FLT FAILED W O OTHER F FLT CONT AFFECTED CR CRUISE 1 CA (CAN) "AUTO FLIGHT" RUDDER TRIM 1 FAULT. FLIGHT AUGMENTATION COMPUTER 1, RUDDER TRIM ACTUATOR 10CC. RUDDER TRIM ACTUATOR 10CC AND RELAY 7CC1 REPLACED. 2 L 7 2 4F RT A28NM 1996122600629 19961226 00629 WP 1996 12 26 CA960723504 1 19960414 A 2150 21700031 COOLING TURBINE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE LT AIR COND LEAKING W O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA P657518D (CAN) SMOKE IN CABIN WHILE USING LEFT AIR CONDITIONING PACK AND A.P.U.MAINTENANCE INVESTIGATION REVEALED LEFT AIR CONDIT IONING PACK LEAKING AT REAR OF HEAT EXCHANGER FLEX COUPLING. NEW COOLING TURBINE INSTALLED AND OPERATIONALLY CHECKED. 2 L 7 2 4F 4 F A6WE E2EA 1996122600630 19961226 00630 NM 1996 12 26 CA960723505 1 19960414 A 7920 LINE BOEING 747 747133 138448B NM PWA JT9 JT9D7 52054 NE NR 3 ENG OIL LEAKING W E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA P685933 (CAN) DURING CRUISE #3 ENGINE OIL PRESSURE WENT INTO AMBER BAND, WITH OIL PRESSURE LIGHT ON, OIL QUANTITY INDICATING BEL OW 2 GALLONS. AFTER FEW MINUTES OIL PRESSURE OCCASIONALLY WENT INTO RED BAND. #3 ENGINE SHUTDOWN AIRCRAFT DIVERTED. OIL LINE REPLACED. 2 L 7 4 4F 4 F A20WE E20EA 1997010200001 19970102 00001 NE 1997 1 2 96ZZZX6181 2 19961119 A 7321 7436024 FUEL CONTROL BOEING 727 7272J7 138400E NM PWA JT8 JT8D15A 52051 NE NT 1 ENGINE FAILED A A C8GA E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CL CLIMB 1 SO 15 128NA 82971 20879 709209 FLT PT 301 DEPARTED MIAMI, FL FOR CUARAZAO (CUR) ON THIS DATE. TAKEOFF WAS NORMAL UP TO THE TIME OF THE FIRST POWER RED UCTION. POWER REDUCTION WAS NORMAL FOR NR 2 AND NR 3 ENGINES; BUT, NR 1 ENGINE REMAINED AT HI POWER WITH NO RESPONSE TO THROTTLE MOVEMENT. ENGINE NR 1 WAS SHUT DOWN AND AIRCRAFT RETURNED TO MIA. ENGINE PARAMETERS WERE HIGH AT TIME OF SHU T DOWN. EVENT RECORDED IN A/C LOG BOOK. 2 L 7 3 4F 4 F A3WE E2EA 1997010200002 19970102 00002 WP 1997 1 2 GAIA9639 1 19961126 A 5311 9922042 FITTING DOUG DC9 DC915F 3022037 WP FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 44572 47062 DURING C-CHECK, INSPECTION REVEALED SEVENTEEN CRACKED STRUT FRAME ATTACH FITTINGS IN THE LOWER FUSELAGE CARGO COMPARTMEN TS. CLOSER INSPECTION REVEALED THE CRACKS TO BE STRESS CORROSION CRACKS ALONG GRAIN LINES. EIGHT FRAMES WERE REPLACED IAW DOUGLAS SRM AND NINE OF THE FRAMES WERE REPAIRED IAW KITTY HAWK E.A. D9-53-042. THE AIRCRAFT WAS RETURNED TO SERVIC E. STA 275, 294, 351, 370, 389, 408, 427, 661, 680, 699, 718, 737, BETWEEN L22L AND L25L. STA 237, 256, 294, 389, 661, BETWEEN L22R AND L25R. (X) 2 L 7 2 4F A6WE 1997010200003 19970102 00003 WP 1997 1 2 GAIA9638 1 19961126 A 5315 FLOOR BEAM DOUG DC9 DC915F 3022037 WP BS 642 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 50880 47062 DURING C-CHECK, INSPECTION REVEALED CORROSION ON FUSELAGE FLOOR BEAM AT STA 642. REPAIRED FLOOR BEAM IAW KITTY HAWK EA D9-53-037. THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4F A6WE 1997010200004 19970102 00004 WP 1997 1 2 GAIA9637 1 19961126 A 5347 3922277 SPLICE DOUG DC9 DC915F 3022037 WP BS 474 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 50880 50880 47062 DURING C-CHECK, INSPECTION REVEALED A CRACKED SEAT TRACK SPLICE AT STA 474. REPLACED SPLICE IAW DOUGLAS SRM. THE AIRCR AFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4F A6WE 1997010200005 19970102 00005 WP 1997 1 2 TWAA9614008 1 19961112 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 200-237 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 956U 49701 MCI - DURING OP-16, FOUND CORROSION ON SEAT TRACK NR 6, FS 200 TO FS 237. CUT OUT AND REPLACED CORRODED SECTION PER SRM 53-05, FIGURE 4F. AIRCRAFT TOTAL TIME: 26,489 HOURS; 13,301 CYCLES. (X) 2 L 7 2 4F A6WE 1997010200006 19970102 00006 WP 1997 1 2 TWAA9614001 1 19961117 A 3260 MS25231313 LAMP DOUG DC9 DC915 3022036 WP LANDING GEAR FAILED A TWAA O OTHER P NO WARNING INDICATION AP APPROACH 1 CE 05 490SA 45798 STL - FLT 483 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, LANDING GEAR DID NOT SHOW DOWN AND LOCKED. FOUND LANDIN G GEAR INDICATOR LAMP, MFG PN MS25231-313, SHORTING OUT INDICATOR SOCKET, MFG PN 035-1881-007. RELAMPED INDICATOR AND R ESET P26 CIRCUIT BREAKER. LANDING GEAR INDICATION THEN CHECKED NORMAL. CHECK C - 7-11-96 - STL. (X) 2 L 7 2 4F A6WE 1997010200007 19970102 00007 WP 1997 1 2 TWAA9614002 1 19961117 A 3260 DOOR SWITCH DOUG DC9 DC932 3022066 WP LANDING GEAR DR OUT OF ADJUST A TWAA O OTHER N FALSE WARNING CL CLIMB 1 CE 05 995Z 47027 STL - FLT 543 - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, DOOR OPEN LIGHT REMAINED ILLUMINATED. CYCLED LANDING GEA R. FOUND DOOR SWITCH, MFG PN H14-6, OUT OF ADJUSTMENT. REPLACED DOOR SWITCH. LANDING GEAR DOOR INDICATION THEN CHECKE D NORMAL. CHECK C - 9-5-96 - STL. (X) 2 L 7 2 4F A6WE 1997010200008 19970102 00008 WP 1997 1 2 TWAA9614003 1 19961112 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP BS 1307-1320 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 MCI - DURING OP-16, FOUND CORROSION ON TOP OF INTERCOSTAL BETWEEN STR 27L AND STR 28L, BS 1307 TO BS 1320. REPAIRED PER SRM 51-10-1 AND TWA STANDARD PRACTICES. AIRCRAFT TOTAL TIME: 42,221 HOURS; 22,107 CYCLES. (X) 2 L 7 2 4F A6WE 1997010200009 19970102 00009 WP 1997 1 2 TWAA9614004 1 19961112 A 5313 STRINGER DOUG DC9 DC982 3022082 WP BS 808 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 956U 49701 MCI - DURING OP-16, FOUND CORROSION AT STR 29R, STA 808. REPAIRED PER SRM 51-04, PAGE 525 AND TWA STANDARD PRACTICES. A IRCRAFT TOTAL TIME: 26,489 HOURS; 13,301 CYCLES. (X) 2 L 7 2 4F A6WE 1997010200010 19970102 00010 WP 1997 1 2 TWAA9614005 1 19961112 A 5320 FORMER RING DOUG DC9 DC982 3022082 WP BS 1271 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 956U 49701 MCI - DURING OP-16, FOUND CORROSION ON AFT CARGO FORMER RING, LONGERON 29R TO LONGERON 28L, STA 1271. REMOVED CORROSION PER SRM 51-3 AND REPAIRED PER SRM 53-03, PAGE 4E. AIRCRAFT TOTAL TIME: 26,489 HOURS; 13,301 CYCLES. (X) 2 L 7 2 4F A6WE 1997010200011 19970102 00011 WP 1997 1 2 TWAA9614006 1 19961112 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 522 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 956U 49701 MCI - DURING OP-16, FOUND CORROSION ON FLOOR SUPPORT, LONGERON 28L TO LONGERON 28R, STA 522. REPLACED FLOOR SUPPORT PER SRM 51-01 AND TWA STANDARD PRACTICES. AIRCRAFT TOTAL TIME: 26,489 HOURS; 13,301 CYCLES. (X) 2 L 7 2 4F A6WE 1997010200012 19970102 00012 WP 1997 1 2 TWAA9614007 1 19961112 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP BS 1307-1320 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 956U 49701 MCI - DURING OP-16, FOUND CORROSION ON TOP OF INTERCOSTAL BETWEEN STR 27L AND STR 28L, BS 1307 TO BS 1320. REPAIRED PER SRM 51-10-1 AND TWA STANDARD PRACTICES. AIRCRAFT TOTAL TIME: 26,489 HOURS; 13,301 CYCLES. (X) 2 L 7 2 4F A6WE 1997010200013 19970102 00013 WP 1997 1 2 TWAA9613506 1 19961101 A 5315 FLOOR BEAM DOUG DC9 DC951 3022051 WP BS 370 WORN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 408EA 47693 STL - DURING OP-15, FOUND WORN SPOT ON FLOOR BEAM APPROXIMATELY FOUR INCHES LEFT OF CENTERLINE, STA 370. REPAIRED FLOOR BEAM PER SRM 53-05, PAGE 31, FIGURE 20A. AIRCRAFT TOTAL TIME: 46,296 HOURS; 43,121 CYCLES. (X) 2 L 7 2 4F RT A6WE 1997010200014 19970102 00014 WP 1997 1 2 TWAA9613901 1 19961114 A 3350 20131A BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 406EA 47686 STL - FLT 593 - DURING CRUISE, EGRESS L IGHTS AT WING EXITS ILLUMINATED. CYCLED LIGHT SWITCH. FOUND BATTERY PACK, MFG PN 2013-1A, WEAK. REPLACED BATTERY PACK. EGRESS LIGHT OPERATION THEN CHECKED NORMAL. CHECK C - 9-17-95 STL. (X) 2 L 7 2 4F RT A6WE 1997010200015 19970102 00015 WP 1997 1 2 TWAA9613902 1 19961111 A 5320 FORMER RING DOUG DC9 DC982 3022082 WP BS 1320 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 MCI - DURING OP-16, FOUND CORROSION ON FORMER RING, LONGERON 29R TO LONGERON 29L, FS 1320. REPAIRED PER SRM 53-03, FIGU RE 2A AND TWA STANDARD PRACTICES. AIRCRAFT TOTAL TIME: 42,221 HOURS; 22,017 CYCLES. (X) 2 L 7 2 4F A6WE 1997010200016 19970102 00016 WP 1997 1 2 TWAA9613903 1 19961112 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1241-1307 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 DURING OP-16, FOUND CORROSION ON NR 2 CABIN CHAIR TRACK, BETWEEN STA 1241 AND STA 1307. CUT OUT CORRODED TRACK; INSTALL ED NEW SECTION OF TRACK AND SPLICED PER SRM 53-05, FIGURE 4F. AIRCRAFT TOTAL TIME: 42,221 HOURS; 22,017 CYCLES. (X) 2 L 7 2 4F A6WE 1997010200017 19970102 00017 WP 1997 1 2 TWAA9613904 1 19961112 A 5347 TIEDOWN TRACK DOUG DC9 DC982 3022082 WP BS 1174-1307 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 MCI - DURING OP-16, FOUND CORROSION ON NR 1 TIE-DOWN TRACK, STA 1174 TO STA 1307. INSTALLED NEW NR 1 TIE-DOWN TRACK PER SRM 51-01, ITEM C. AIRCRAFT TOTAL TIME: 42,221 HOURS; 22,107 CYCLES. (X) 2 L 7 2 4F A6WE 1997010200018 19970102 00018 WP 1997 1 2 TWAA9613905 1 19961112 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1307 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 903TW 49154 MCI - DURING OP-16, FOUND CORROSION ON FORMER FRAME, STR 29R TO STR 25L, BS 1307. REPAIRED PER SRM 53-03, FIGURE 1A AND TWA STANDARD PRACTICES. AIRCRAFT TOTAL TIME: 42,221 HOURS; 22,107 CYCLES. (X) 2 L 7 2 4F A6WE 1997010200019 19970102 00019 WP 1997 1 2 TWAA9614101 1 19961107 A 5313 LONGERON DOUG DC9 DC951 3022051 WP BS 1151 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 408EA 47693 STL - DURING OP-15, FOUND A ONE INCH CRACK IN RIGHT LAV, UPPER FLANGE OF LONGERON 17R, STA 1151. REPLACED LONGERON PER MDC DRAWING C03607 AND SRM'S 51-30-2, 51-30-5, AND 51-10-3. AIRCRAFT TOTAL TIME: 46,296 HOURS; 43,121 CYCLES. (X) 2 L 7 2 4F RT A6WE 1997010200118 19970102 00118 EU 1997 1 2 AWXA9600770 1 19961222 A 2121 EVT3454G COOLNG FAN AIRBUS 320 A320231 3930325 EU AVIONICS BAY FAILED A AWXA K NONE J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 WP 28 620AW 11831 2532 052 ECAM MESSAGE VENT EXTRACT FAULT, ELECTRIC SMELL PRESENT. REMOVED AND REPLACED AVIONIC EXTRACT FAN PER MM 21-26-51. TES T OK. 2 L 7 2 4F RT A28NM 1997010200119 19970102 00119 NM 1997 1 2 AWXA9600771 1 19961223 A 3350 900835A BATTERY PACK BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 187AW 22654 DURING ROUTINE MAINTENANCE CHECK, FOUND EXIT LIGHT ON R-2 DOOR INOP. REMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD . STC - SA3432NM 2 L 7 2 4F RT A16WE 1997010200120 19970102 00120 NM 1997 1 2 AWXA9600772 1 19961224 A 3350 LIGHT BOEING 757 75723A 1384967 NM CABIN LOOSE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 916AW 24291 DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT AT 16-L INOP. ATTACHED LIGHT TO SEAT. OPS CHECK GOOD. 2 L 7 2 4F RT A2NM 1997010200121 19970102 00121 NM 1997 1 2 AWXA9600773 1 19961224 A 3350 831862 BATTERY BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 180AW 22647 DURING ROUTINE MAINTENANCE CHECK, FOUND L/H OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED L/H OVERWING EMERGENCY BATTERY. OPS CHECK OK. STC - SA3432NM 2 L 7 2 4F RT A16WE 1997010200122 19970102 00122 EU 1997 1 2 AWXA9600774 1 19961225 A 3350 FUSE AIRBUS 320 A320231 3930325 EU CABIN MISSING A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 624AW 55 DURING ROUTINE MAINTENANCE CHECK, FOUND BOTH RIGHT EMERGENCY OVERWING EXIT HANDLE COVER LIGHTS INOP. FOUND MISSING FUSE ON BATTERY PACK AND INSTALLED NEW ONE. OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 1997010200123 19970102 00123 NM 1997 1 2 AWXA9600775 1 19961224 A 3397 WIRE BOEING 737 7373G7 1384595 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 309AW 24711 DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT PROBLEM. REPAIRED BROKEN WIRE. OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 1997010200124 19970102 00124 WP 1997 1 2 CALA9601875 1 19961224 A 2913 6506606 HYD PUMP DOUG DC10 DC1030 3023501 WP NR 2 ENGINE CRACKED A CALA A J UNSCHED LANDING DUMP FUEL K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 19072 46576 THE A/C LOST NR 2 SYSTEM HYDRAULIC FLUID WHILE ENROUTE FROM HNL TO GUM. THE FLUID LOSS WAS ACCOMPANIED BY ILLUMINATION O F BOTH LT AND RT PUMP PRESSURE LOW LIGHTS. THE NR 2 HYD QTY LOSS CHECKLIST WAS PERFORMED, FUEL WAS DUMPED, AND THE A/C W AS RETURNED TO HNL WHERE IT LANDED WITHOUT INCIDENT. MX FOUND THE NR 2 ENG RT ENG DRIVEN HYDRAULIC PUMP CASE CRACKED. B OTH THE RT AND LT NR 2 ENG DRIVEN HYDRAULIC PUMPS WERE REMOVED AND REPLACED. IN ADDITION, THE RT HYDRAULIC PUMP PRESSUR E LINE WAS REPLACED DUE TO LEAKAGE. THE HYDRAULIC SYS WAS SERVICED. THE NR 2 ENGINE WAS RUN AND LEAK AND OPERATIONAL C HECKS WERE GOOD. 2 L 7 3 4F A22WE 1997010200125 19970102 00125 NM 1997 1 2 CALA9601876 1 19961224 A 2910 65445101708 HYD LINE BOEING 737 737130 1384435 NM NR 2 ENGINE LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SW 09 44214 19031 THE A HYDRAULIC SYSTEM QUANTITY AND PRESSURE DROPPED TO ZERO ON DESCENT INTO EWR. THE A SYSTEM PUMPS WERE TURNED OFF AN D THE HYDRAULIC LOSS CHECKLIST WAS ACCOMPLISHED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT ENGINE A SYSTEM PRESSURE LINE LEAKING. THE LINE WAS REPLACED USING FLEX LINE. A DIP WAS ISSUED TO REPLACE THE FLEX LINE WITHI N 500 FLIGHTS OR 1200 FLIGHT HOURS, WHICHEVER COMES FIRST. 2 L 7 2 4F A16WE 1997010200126 19970102 00126 NM 1997 1 2 9626726302 1 19961222 A 7930 OIL FILTER LIGHT BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE NR 4 ENGINE ILLUMINATED A NWAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 01 622US 23720 17637 DURING CRUISE AT FL290, THE NR 4 ENGINE OIL FILTER ADVISORY MESSAGE CAME ON AND WOULD NOT EXTINGUISH AT IDLE THRUST. CR EW ELECTED TO SHUTDOWN THE ENGINE AND RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED VISUAL INSPECTION OF THE OIL FILTER BYPASS SWITCH, RESEATED PINS AND RUNUP ENGINE. RUNUP WAS NORMAL AND A/C RETURNED TO SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 1997010200127 19970102 00127 NM 1997 1 2 9626735637 1 19961222 A 2421 GENERATOR BOEING 757 757251 1384970 NM LEFT FAILED A NWAA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 GL 01 537US 26484 DURING CRUISE, THE LEFT GENERATOR DISCONNECTED AND WOULD NOT RESET, APU WOULD NOT START FOR SECOND POWER SOURCE. AIRCR AFT DIVERTED TO DEN AND LANDED WITHOUT INCIDENT. MAINTENANCE PLACED LEFT GENERATOR ON MEL AND PERFORMED APU CHECK OUT, SYSTEM CHECKED OK. 2 L 7 2 4F RT A2NM 1997010200128 19970102 00128 WP 1997 1 2 9626741150 1 19961218 A 2751 96010206 TRANSMITTER DOUG DC10 DC1040 3023508 WP LT TE FLAP INTERMITTENT A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 150US 61176 61176 46759 DURING POWER APPLICATION FOR TAKEOFF, THE TAKEOFF WARNING HORN SOUNDED. TAXIED OFF THE RUNWAY AND RETURNED TO GATE. MA INTENANCE FOUND THE FLAP TRANSMITTER INTERMITTENT, AND REPLACED. 2 L 7 3 4F A22WE 1997010200129 19970102 00129 WP 1997 1 2 9626759307 1 19961221 A 3260 UPLOCK SENSOR DOUG DC9 DC982 3022082 WP LT MLG MALFUNCTIONED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 309RC 48088 AFTER TAKEOFF, ON GEAR RETRACTION, LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURE. RECYCLED GEAR ONE TIME. FLIGHT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEFT MAIN GEAR UPLOCK SENSOR. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F A6WE 1997010200130 19970102 00130 WP 1997 1 2 9626769607 1 19961221 A 3231 LATCH ARM DOUG DC9 DC932 3022066 WP RT NLG DOOR FROZEN A NWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 01 607NW 47232 EXCESSIVE VIBRATION FROM NOSE GEAR AREA OCCURRED AFTER GEAR RETRACTION. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCID ENT. MAINTENANCE FOUND RIGHT NOSE GEAR DOOR UNLATCHED. CLEANED ICE AND SAND FROM ACTUATOR LATCHING ARM. OPERATIONAL C HECK NORMAL ON SEVERAL DOOR CYCLES. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1997010200131 19970102 00131 WP 1997 1 2 9626779302 1 19961218 A 2741 CAWS WARNING DOUG DC9 DC982 3022082 WP STAB TRIM ACTIVATED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 302RC 48055 REJECTED TAKEOFF AT APPROX 90 KTS DUE TO STAB CAWS WARNING. FLIGHT RETURNED TO GATE. MAINTENANCE CYCLED STAB TRIM AND CHECKED STAB TAKEOFF WARNING SWITCH. NO DISCREPANCIES FOUND. AIRCRAFT APPROVED FOR FURTHER SERVICE. 2 L 7 2 4F A6WE 1997010200132 19970102 00132 WP 1997 1 2 9626789869 1 19961220 A 2781 DISAGREE LIGHT DOUG DC9 DC951 3022051 WP LE FLAPS ILLUMINATED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 778NC 48100 ON CLIMB-OUT OF ATL, SLAT DISAGREEMENT LIGHT ILLUMINATED. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURE. FLIGHT RETURNED TO ATL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED SLAT SWITCHES AND SLAT OPERATION. OPERATION CHECKS GOOD. 2 L 7 2 4F RT A6WE 1997010200133 19970102 00133 WP 1997 1 2 9626799990 1 19961222 A 7711 EPR LINES DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9 52048 NE RT ENGINE FROZEN A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 8950E 47186 657252 AS THROTTLES WERE ADVANCED FOR TAKEOFF, THE RIGHT ENGINE EPR INDICATION WAS INOPERATIVE. CREW ABORTED TAKEOFF AND RETUR NED TO GATE. MAINTENANCE APPLIED HEAT TO ASSOCIATED EPR LINES AND RAN ENGINE. INDICATIONS WERE OK, SUSPECT ICING OF EP R RELATED LINES. 2 L 7 2 4F 4 F A6WE E2EA 1997010200134 19970102 00134 1997 1 2 9626809986 4 19961220 A 2565 113317 EVAC SLIDE DOUG DC9 DC932 3022066 WP SERVICE DOOR LOW BATTERY A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 986US 5285 1697 47480 DURING PERIODIC CHECK, FOUND FORWARD SERVICE DOOR EVACUATION SLIDE WITH LOW BATTERY. REPLACED SLIDE. 2 L 7 2 4F A6WE 1997010200135 19970102 00135 1997 1 2 9626819920 4 19961222 A 2565 13621228 EVAC SLIDE DOUG DC9 DC932 3022066 WP TAILCONE LOW PRESSURE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 942N 2646 1402 47459 DURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE EVACUATION SLIDE LOW ON PRESSURE. REPLACED SLIDE. 2 L 7 2 4F A6WE 1997010200136 19970102 00136 WP 1997 1 2 9626829912 1 19961220 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN BROKEN A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 962N 47406 FORWARD CABIN EMERGENCY FLOOR PROXIMITY LIGHTS ILLUMINATED DURING FLIGHT. MAINTENANCE REPAIRED BROKEN WIRE UNDER SEATS 2C AND 2D. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1997010200137 19970102 00137 1997 1 2 9626839911 4 19961222 A 2565 113317 EVAC SLIDE DOUG DC9 DC931 3022065 WP PAX DOOR LOW BATTERY A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 961N 18718 5180 47405 DURING PERIODIC CHECK, MAIN CABIN DOOR EVACUATION SLIDE FAILED EMERGENCY BATTERY TEST. REPLACED SLIDE. 2 L 7 2 4F A6WE 1997010200138 19970102 00138 WP 1997 1 2 9626849937 1 19961223 A 3350 6011779 BATTERY PACK DOUG DC9 DC931 3022065 WP LT NACELLE MALFUNCTIONED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 908H 47517 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK. 2 L 7 2 4F A6WE 1997010200139 19970102 00139 WP 1997 1 2 9626859763 1 19961216 A 3350 BATTERY PACK DOUG DC9 DC941 302207N WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 763NW 47396 DURING LINE CHECK, FOUND MID SECTION EMERGENCY LIGHTS BY EMERGENCY EXIT DOORS INOPERATIVE. REPLACED 05-903 BATTERY PACK AND CHARGER. OPERATION CHECKS GOOD. 2 L 7 2 4F A6WE 1997010200140 19970102 00140 WP 1997 1 2 9626869852 1 19961219 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 761NC 47709 DURING LINE CHECK, FOUND TAIL COMPARTMENT EMERGENCY ESCAPE/CATWALK LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND OPERAT ION CHECKS GOOD. 2 L 7 2 4F RT A6WE 1997010200141 19970102 00141 WP 1997 1 2 9626879307 1 19961221 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 309RC 48088 DURING LINE CHECK, FOUND TAIL COMPARTMENT OVERHEAD LIGHT INOPERATIVE. REPLACED BATTERIES. OPERATION CHECKS GOOD. 2 L 7 2 4F A6WE 1997010200142 19970102 00142 WP 1997 1 2 9626889307 1 19961221 A 3350 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 309RC 48088 DURING LINE CHECK, FOUND TAILCONE SLIDE EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY AND OPERATION CHECKS GOOD. 2 L 7 2 4F A6WE 1997010200143 19970102 00143 WP 1997 1 2 9626899964 1 19961224 A 7711 EPR LINE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9 52048 NE RT ENGINE FROZEN A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 912RW 47150 666315 AS TAKEOFF POWER WAS APPLIED, THE RIGHT ENGINE EPR INDICATION DID NOT RESPOND. CREW ABORTED TAKEOFF AND RETURNED TO GAT E. MAINTENANCE REPLACED THE RIGHT ENGINE EPR INDICATOR, EPR TRANSMITTER AND THE PROBLEM CONTINUED. MAINTENANCE THEN AP PLIED HEAT TO PT7 LINES AND DRAINED THE MOISTURE. OPERATIONAL CHECK OK. SUSPECT ICING OF THE PT7 LINES. 2 L 7 2 4F 4 F A6WE E2EA 1997010200144 19970102 00144 WP 1997 1 2 9626909853 1 19961223 A 7714 8DJ81LVB4 N1 INDICATOR DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE RT ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 762NC 34787 20345 47110 707924 DURING TAKEOFF ROLL, THE RIGHT ENGINE N1 INDICATION WAS ABNORMALLY LOW. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE N1 INDICATORS FOR BOTH ENGINES, OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F RT A6WE E2EA 1997010200145 19970102 00145 WP 1997 1 2 9626919301 1 19961225 A 7711 2047021 EPR INDICATOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE NR 1 ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 301RC 23548 19725 48054 708402 AS TAKEOFF POWER WAS APPLIED, THE NR 1 ENGINE EPR INDICATION DID NOT RESPOND. CREW ABORTED TAKEOFF AND EPR SYSTEM WAS P LACED ON MEL. MAINTENANCE LATER REPLACED THE LEFT ENGINE EPR INDICATOR, OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F A6WE E9NE 1997010200146 19970102 00146 EU 1997 1 2 WWMA100106 1 19961217 A 3260 249412001 CONTROL UNIT SAAB SF340 340B 7860101 EU LANDING GEAR DEFECTIVE A WWMA K NONE N FALSE WARNING CL CLIMB 1 WP 15 254AE 340B254 LANDING GEAR UNSAFE LIGHT INDICATION FAILS TO EXTINGUISH AFTER GEAR RETRACTION. REPLACED THE LANDING GEAR CONTROL UNIT AND PERFORMED GEAR SWINGS. 2 L 7 2 4T RT A52EU 1997010200147 19970102 00147 EU 1997 1 2 WWMA9600108 1 19961222 A 2530 MS3476W145BN PLUG SAAB SF340 340B 7860101 EU GALLEY ARCED A WWMA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 WP 15 286AE 340B286 CREW REPORTED AN UNUSUAL ODOR EMMITTING FROM THE HOT WATER JUGS. MAINTENANCE FOUND THE NR 1 HOT JUG ELECTRICAL PLUG ARC ED, SYSTEM WAS DEACTIVATED AND DEFERRED DUE TO TIME TO REPLACE THE PLUG. 2 L 7 2 4T RT A52EU 1997010200148 19970102 00148 EU 1997 1 2 96FDEA01704 1 19961218 A 7830 PILOT VALVE AIRBUS 300 A300* EU NR 1 TR UNIT MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 668FE 772 ON POWER APPLICATION, NR 1 REV PRESS LIGHT CAME ON AND THEN WENT OUT, ON THE ECAM AT APPROX 200-300 FT AGL WARNING CAME BACK ON. REMOVED AND REPLACED NR 1 THRUST REVERSER DIRECTIONAL PILOT VALVE. OPS CHECK GOOD. 2 L 7 2 4F RT A35EU 1997010200149 19970102 00149 NM 1997 1 2 96FDEA01707 1 19961224 A 2612 FIRE LIGHT BOEING 727 72725 1384006 NM WHEEL WELL ILLUMINATED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 120FE 19356 WHEEL WELL FIRE LIGHT CAME ON INTERMITTENTLY DURING TAKEOFF. GROUND RACK HOLD DOWN BROKEN. REMOVED AND REPLACED HOLD D OWN. OPERATIONAL CHECK GOOD. 2 L 7 3 4F A3WE 1997010200150 19970102 00150 NM 1997 1 2 96FDEA01708 1 19961225 A 2782 ACTUATORS BOEING 727 727232 1384082 NM NR 3/4 LE FLAPS ICED UP A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 497FE 20866 N 3 AND NR 4 LEADING EDGE FLAPS FAILED TO RETRACT FROM 2 DEGREES TO UP ON TAKEOFF. EXTENDED TO 5 DEGREES OK. LATER RET RACTION TO UP OK, THEN WENT INTERMITTENT WITH AIR SPEED INCREASE. DE-ICED LEADING EDGE ACTUATORS. OPERATIONAL CHECK O K. 2 L 7 3 4F A3WE 1997010200151 19970102 00151 WP 1997 1 2 ABXA9600685 1 19961219 A 3310 9958267501 LIGHT PLATE DOUG DC9 DC941 302207N WP LEFT DEFECTIVE A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 990AX 47493 SMOKE APPEARED AT COMPARATOR RESET BUTTON, LEFT AC ISOLATED AND OPERATIONS WERE NORMAL. REPLACED COMPARATOR TEST LIGHT PANEL IAW DC-9 M.M. 33-10. 2 L 7 2 4F A6WE 1997010200152 19970102 00152 NE 1997 1 2 ABXA9600686 2 19961223 A 7200 ENGINE DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 4 FAILED A ABXA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 23 814AX 46041 671344 NR 4 ENGINE OIL PRESSURE LIGHT ILLUMINATED AT CRUISE, FL 330. QUANTITY WENT TO ZERO, TEMPERATURE WENT OFF SCALE HIGH. P ERFORMED ENGINE SECURING. REPLACED NR 4 ENGINE IAW J CARD 7002. 2 L 7 4 4F 4 F 4A25 1E8 1997010200153 19970102 00153 NM 1997 1 2 DLM88962737 1 19961219 A 2130 PRESSURE SYST DOUG MD88 MD88 3023688 NM CABIN MALFUNCTIONED A DALA O OTHER J WARNING INDICATION DE DESCENT 1 SO 27 953DL 49884 LOST BOTH AUTO PRESS DESCENDING THROUGH FLT 230. UNABLE TO CONTROL CABIN ALT, CABIN O2 MASK DEPLOYED. 2 L 7 2 4F RT A6WE 1997010200154 19970102 00154 WP 1997 1 2 DLL10962739 1 19961219 A 2170 COALESCER BAGS 217103262 LKHEED 1011 10113851 5265010 WP CABIN DIRTY A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 712DA NONE 193C1088 ALL AFT CABIN LAV SMOKE DETECTORS WENT OFF AND A STRONG SMELL ENTERED CABIN AFTER TAKE OFF. ALL ENG INSTRUMENTS WERE NO RMAL. ALL PACK INDICATIONS WERE NORMAL. RETURNED TO SFO. OVERWEIGHT LANDING PERFORMED BRAKES APPLIED AT 90 KTS TIME 1 820Z. A/C WEIGHT 415,000 LBS. PERFORMED VISUAL INSP ALL 3 PACK AREAS, DUCTS IN HYD BAY, APU COMPT, NR 2 ENG AREA. NO D ISCREPANCIES FOUND. REPLACED COALESCER BAGS ALL 3 PACKS AS PRECAUTIONARY. RAN ALL ENGS AT IDLE AND MAX PWR PER PFHB, N O ODOR DETECTED IN CABIN. ALL LAV SMOKE DET CHK'D NORMAL DURING ENG RUN. PERFORMED OVERWEIGHT INSP PER MM 5-50-01. 2 L 7 3 4F A23WE 1997010200155 19970102 00155 NM 1997 1 2 DL76S962753 1 19961221 A 2910 LINE 340545 BOEING 767 767332 1382001 NM LT HYD SYST CRACKED A DALA K NONE K J FLUID LOSS WARNING INDICATION LD LANDING 1 SO 27 136DL 4803 23146 LT HYD PRESS CAUTION WITH LT HYD QTY AND RUDDER RATIO ADVISORY MESSAGES ILLUMINATED. LT HYD QTY READS ZERO. 2 L 7 2 4F RT A1NM 1997010200157 19970102 00157 NM 1997 1 2 DLM88962759 1 19961223 A 3320 LIGHT ASSY UNK DOUG MD88 MD88 3023688 NM PWA JT8 JT8D15 52051 NE CABIN FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 942DL UNK 49815 685565 F/A'S AND PAX REPORT SMELL OF BURNING RUBBER OR ELECTRICAL SMELL IN REAR OF A/C, SMELL PRESENT IN ALL PHASES OF FLT. NO SMOKE PRESENT. C/A FOUND CEILING LIGHT FIXTURE AT SEAT ROW 36AB SMOLDERING. REMOVED LAMP AND DISCONNECTED BALLAST FWD TO MCO/PLAC MEL 33-00-2. LIGHT ASSY WILL BE REPLACED. 2 L 7 2 4F 4 F RT A6WE E2EA 1997010200158 19970102 00158 NE 1997 1 2 DL76S962760 2 19961223 A 7200 ENGINE BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 2 MALFUNCTIONED A A DALA D RETURN TO BLOCK A FLAME/FIRE TX TAXI/GRND HDL 1 SO 27 134DL 29528 25123 580317 AFTER BEGINING TAXI OUT BOSTON, TOWER RADIOED TO COCKPIT THAT FLAMES WERE VISIBLE IN VICINITY OF RT ENG/WING. NO INDICA TIONS FROM COCKPIT, ENGINE WAS SHUTDOWN AS A PRECAUTION FOR LOCAL AUTHORITIES AND MX PERFORMED CKS ON ENG. CHECKED INLE T AND EXHAUST OF RT ENG, ALSO CHECKED DRAINS FOR FLUID LEAKS. NONE FOUND, CHECKED WING AREA FOR LEAKS OR DAMAGE, NONE FOUND. STARTED ENG ALL NORM. 2 L 7 2 4F 4 F RT A1NM E13NE 1997010200159 19970102 00159 NM 1997 1 2 DLM11962761 1 19961218 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1771-1861 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 803DE 48474 SEAT TRACK CORRODED IN SEVERAL PLACES BETWEEN FS 1771 AND 1861 RBL 27. REPAIRED PER SRM 53-70-00 MAJOR REPAIR. 2 L 7 3 4F RT A22WE 1997010200160 19970102 00160 NM 1997 1 2 DLM11962762 1 19961218 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1781-1841 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 803DE 48474 SEAT TRACK CORRODED IN SEVERAL PLACES BETWEEN FS 1781 AND 1841 LBL 27. REPAIRED PER SRM 53-70-00 MAJOR REPAIR. 2 L 7 3 4F RT A22WE 1997010200161 19970102 00161 NM 1997 1 2 DLM11962763 1 19961218 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1305-1361 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 803DE 48474 SEAT TRACK CORRODED IN SEVERAL PLACES BETWEEN FS 1305 AND 1361 RBL 75. REPAIRED PER SRM 53-70-00 MAJOR REPAIR. 2 L 7 3 4F RT A22WE 1997010200162 19970102 00162 NM 1997 1 2 DL72S962764 1 19961224 A 3350 334102486 BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 409DA 21153 CABIN EMERGENCY LIGHTS INOP. 2 L 7 3 4F A3WE 1997010200163 19970102 00163 NE 1997 1 2 DLM88962765 2 19961224 A 7321 76960613 FUEL CONTROL DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE MALFUNCTIONED A A DALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 27 978DL 15957 F12472 53259 725815 AFTER ATTAINING T/O PWR, NR 1 ENGINE ROLLED BACK, PRESSURIZATION WAS LOST. NR 1 ENGINE DID COME BACK WITH NORMAL OPS DU RING CLIMB. MX IN PROGRESS REPLACING FUEL PUMP AND FUEL CONTROL. 2 L 7 2 4F 4 F RT A6WE E9NE 1997010200164 19970102 00164 NE 1997 1 2 DL72L962767 2 19961224 A 7230 COMPRESSOR BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE STALLED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 27 512DA 42743 21314 700436 REJECTED TAKOFF DUE TO NOISE OF COMPRESSOR STALL, FOLLOWED BY ENG FAIL LIGHTS. STRONG CROSS WIND AT 70 DEGS OF 19 KNTS OCCURED PRIOR TO TAKE OFF AIRSPEED INDICATION. INSPECTED 1, 2, AND 3 ENGINE INTAKE AND EXHAUSTS, RAN ENGINES PER P.F.H. B. 4-0-7-7 ALL PARAMETERS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1997010200165 19970102 00165 NM 1997 1 2 DL72W962768 1 19961216 A 5530 STRINGER BOEING 727 727247 138408F NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2817W 20873 FOUND DURING MV2, JUST INSIDE ACCESS 9504 ON RT SIDE 2ND FROM TOP STRINGER, CRACK AT RIB ATTACH BOLT. FABRICATED AND D RILLED REPAIR PARTS PER M/M 55-30-0 PG. 803. INSTALLED REPAIR PER M/M 55-30-0. 2 L 7 3 4F A3WE 1997010200166 19970102 00166 EA 1997 1 2 SWIA95790 1 19961208 A 7714 5071T98P02 N1 CONTL AMP CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RT ENGINE FAILED A SWIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 07 411SW 7067 RIGHT ENGINE N1 AND N/FF FLUCTUATING AT CRUISE N1 96-88 PERCENT, NORMAL OPERATION AFTER RT ENGINE SPEED SWITCH TURNED OF F PER A/C ORH MANUAL MEL 26-11-1. RIGHT ENGINE SPEED SWITCH. RETURNED TO FIELD. REPLACED RT ENGINE N1, CONTROL AMP I AW MM 73-21-03. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 1997010200167 19970102 00167 EA 1997 1 2 SWIA95791 1 19961209 A 2750 B55D1007 BPSU CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE TE FLAPS MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 413SW 7102 FLAPS FAIL MESSAGE. RETURNED TO FIELD. REPLACED FECU. PROBLEM STILL THERE. REPLACED LEFT BPSU. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 1997010200168 19970102 00168 SO 1997 1 2 SWIA95793 1 19961217 A 2750 12042642507 COMPUTER EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE TE FLAPS MALFUNCTIONED A SWIA L A ABORTED APPROACH UNSCHED LANDING N FALSE WARNING AP APPROACH 1 NM 07 213SW 120277 FLAP CONTROL FAULT OUTBOARD FLAPS 15 DEG INBD AND NACELLE FLAPS 25 DEG. UNABLE TO LAND SBP DIVERTED TO SMX.REPLACED FL AP COMPUTER, CLEANED TRACKS, RAN FLAPS. SYSTEM OPS CHECKS GOOD AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 1997010200169 19970102 00169 1997 1 2 SWIA95794 4 19961218 A 2216 6225734002 SERVO EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE AUTO PILOT TRIM FAILED A A SWIA K NONE F FLT CONT AFFECTED LD LANDING 1 NM 07 205SW 120260 DURING LANDING FLARE, AILERONS BECAME EXTREMELY STIFF ALMOST AS THOUGH AUTO PILOT WAS STILL ENGAGED. PRESSING CAPTS A/P TRIM DISC HAD NO EFFECT. STIFFNESS CAUSED ROLL OSCILLATION. STIFFNESS BROKE LOOSE BY MOVING AILERONS AFTER LANDING AND FELT LIKE A/P DISCONNECTED. REPLACED AUTO PILOT AILERON SERVO. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1997010200171 19970102 00171 WP 1997 1 2 CA960723507 1 19960416 A 2120 AC PACK DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE AIR COND CABIN SMOKE W O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA P657270D (CAN) SMOKE IN CABIN WHILE USING APU AND AIR CONDITIONING. MAINTENANCE CHECKED COOLING FAN. AIR CONDITIONING, A.P.U. AND ENGINES RUN. UNABLE TO DUPLICATE FAULT. 2 L 7 2 4F 4 F A6WE E2EA 1997010200172 19970102 00172 EA 1997 1 2 CA960723508 1 19960416 A 3260 PSEU CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE GEAR EXTENSION FAILED W O OTHER J WARNING INDICATION DE DESCENT 1 CA 1692 807267 (CAN) PROXIMITY SYSTEM FAULT ON DESCENT. HAD TO CARRY OUT MANUAL LANDING GEAR EXTENSION. STEERING INOPERATIVE AFTER LAND ING. CHANGED PROXIMITY SENSOR ELECTRONIC UNIT (PSEU). 2 L 7 2 4F 4 F RT A21EA E15NE 1997010200173 19970102 00173 EU 1997 1 2 CA960723510 1 19960418 A 2750 FLAP AIRBUS 320 A320211 3930320 EU FLT CONTROL ALIGNMENT FAULT W A O OTHER J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 CA (CAN) FLIGHT CONTROL, FLAP LOCKED ALIGNMENT FAULT OCCURRED WHEN FLAP 2 SELECTED ON APPROACH. FLAP SYSTEM CHECKED, UNABLE TO DUPLICATE FAULT. 2 L 7 2 4F RT A28NM 1997010200174 19970102 00174 EA 1997 1 2 CA960723511 1 19960420 A 2750 855D1005 BPSU CNDAIR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE FLAPS FAILED W D RETURN TO BLOCK F FLT CONT AFFECTED CL CLIMB 1 CA 2544 807211 (CAN) FLAPS FAIL MESSAGE WITH FLAPS LOCKED AT 8 DEGREES. CHANGED LEFT B.P.S.U. 2 L 7 2 4F 4 F RT A21EA E15NE 1997010200175 19970102 00175 NE 1997 1 2 CA960723512 2 19960425 A 7230 BLADE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE LT ENG NICKED W C D ABORTED TAKEOFF RETURN TO BLOCK J X WARNING INDICATION ENGINE FLAMEOUT TO TAKEOFF 1 CA P657518D (CAN) PRIOR TO TAKEOFF, ENGINE RUN-UP COMPLETED TO 1.4 EPR, ALL INDICATIONS NORMAL. DURING TAKEOFF ROLL TWO COMPRESSOR S TALLS OCCURRED BEFORE 100 KNOTS. TAKEOFF ABORTED. MAINTENANCE INVESTIGATION REVEALED 3 ENGINE FAN BLADES NICKED ON LEFT ENGINE FROM ICE INGESTION. FAN BLADES DRESSED AS PER M.M. 72-00.ENGINE GROUND RUN. 2 L 7 2 4F 4 F A6WE E2EA 1997010200176 19970102 00176 EA 1997 1 2 CA960723513 1 19960427 A 5280 60033043100707 DOOR CNDAIR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LEFT NOSE DAMAGED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 588 807343 (CAN) DURING CLIMB PASSING THROUGH 230 KNOTS, THE NOSE LANDING GEAR DOOR OPENED WITH AURAL WARNING, EICAS MESSAGE AND TH E SOUND OF RUSHING AIR. FOUND LEFT NOSE GEAR DOOR HAD BEEN DAMAGED BY RAMP EQUIPMENT. DOOR REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 1997010200178 19970102 00178 NE 1997 1 2 CA960723515 2 19960504 A 7230 BLADE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7 52053 NE #2 ENGINE FAN DAMAGED W A O OTHER O OTHER TX TAXI/GRND HDL 1 CA 56476 P657309D (CAN) DURING AIRCRAFT WALK AROUND SEVERE DAMAGE TO THE RIGHT ENGINE FAN BLADES WAS OBSERVED. DAMAGE WAS TO EVERY FIRST S TAGE FAN ROTOR BLADES AND TO MOST SECOND STAGE FAN ROTOR AND STATOR BLADES. PRELIMINARY REPORT. 2 L 7 2 4F 4 F A6WE E2EA 1997010200179 19970102 00179 WP 1997 1 2 CA960723516 1 19960505 A 2530 ELECTRICAL PANEL DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE GALLEY LOOSE SCREWS W O H OTHER DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 CA P657757D (CAN) ON ARRIVAL, GALLEY EQUIPMENT TURNED OFF DUE TO ELECTRICAL BURNING SMELL. MAINTENANCE CHECKED FOUND 3 LOOSE SCREWS BEHIND ELECTRICAL CONTROL PANEL. SCREWS TIGHTENED AND GALLEY ELECTRICAL POWER TESTED. 2 L 7 2 4F 4 F A6WE E2EA 1997010200180 19970102 00180 NE 1997 1 2 CA960723517 2 19960508 A 7322 HYDRO MECH UNIT AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE #1 ENGINE BLOWN GASKET W A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CR CRUISE 1 CA 731668 (CAN) DURING FLIGHT FUEL QUANTITY SHOWED A CONSTANT LOSS OF FUEL. AIRCRAFT DIVERTED. POST FLIGHT INSPECTION CONFIRMED A FUEL LEAK ON #1 ENGINE. FUEL LEAK STOPPED WHEN ENGINE WAS SHUTDOWN. INSPECITON FOUND BLOWN GASKET AT I.D.G. INLET LINE O N HYDRO MECHANICAL UNIT. GASKET REPLACED AND AFTER SERVICEABLE ENGINE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A28NM E29NE 1997010200182 19970102 00182 EA 1997 1 2 CA960723519 1 19960509 A 3232 10811005 ACTUATOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE NOSE GEAR DOOR FAILED W O OTHER J WARNING INDICATION AP APPROACH 1 CA 2856 807213 (CAN) ON APPROACH, NOSE LANDING GEAR WOULD NOT EXTEND ON FIRST SELECTION, RECYCLED AND THEN OK. FOUND NOSE LANDING GEAR DOOR ACTUATOR BY PASSING AND 3A HYDRAULIC PUMP DELIVERING LOW PRESSURE. BOTH ACTUATOR AND PUMP P/N 848847 REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 1997010200183 19970102 00183 NE 1997 1 2 CA960723520 2 19960511 A 7261 GEARBOX FITTING DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE LEFT ENGINE LOOSE W A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CR CRUISE 1 CA P657222D (CAN) LEFT ENGINE OIL QUANTITY DROPPED FROM 9 LITERS TO 3 LITERS IN APPROXIMATELY 30 MINUTES. MAINTENANCE CHECK FOUND LE FT GEARBOX FITTING TO OIL PRESSURE SWITCH LOOSE AND GEARBOX THREADS STRIPPED. RECTIFICATION INVOLVED INSTALLING A HELICO IL AS PER PRODUCTION PERMIT APPROVED BY POWERPLANT ENGINEERING. GROUND RUN AND LEAK CHECK CARRIED OUT. 2 L 7 2 4F 4 F A6WE E2EA 1997010200184 19970102 00184 WP 1997 1 2 CA960723521 1 19960515 A 2530 CA167072 ELECT RECEPTACLE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE GALLEY OVEN BURNT W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA P657361D (CAN) ELECTRICAL BURNING SMELL DETECTED IN OVEN GALLEY AREA. MAINTENANCE CHECK FOUND OVEN #2, POSITION 16 ELECTRICAL REC EPTACLE BURNT. RECEPTACLE CHANGED. 2 L 7 2 4F 4 F A6WE E2EA 1997010200185 19970102 00185 EU 1997 1 2 CA960723522 1 19960517 A 2780 SLAT AIRBUS 320 A320211 3930320 EU NR 1 & NR 2 INOPERATIVE W A O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 CA (CAN) PRIOR TO ARRIVAL AND ON SELECTION OF FLAPS 1, ECAM MESSAGE DISPLAYED FLAP/SLATS LOCKED. CFDS FAULTS SLATS #1 & #2 SYSTEM JAM CHECK SET MECHANICAL DRIVE FOUND TORQUE LIMITERS POPPED ON #2 RIGHT SLAT DRIVES. MAINTENANCE CARRIED OUT DETA ILED INSPECTION ON TRANSMISSION, TRACK ROLLER, PINIONS AND RACK GEARS. ALSO RIGHT WING SLAT SYSTEM LUBRICATED AND OPERAT IONAL CHECK CARRIED OUT. 2 L 7 2 4F RT A28NM 1997010200187 19970102 00187 NM 1997 1 2 CA960723525 1 19960519 A 2612 K1536335D FIRE LOOP K1536335D BOEING 747 747238B 1384828 NM PWA JT9 JT9D7F 52054 NE NR 4 ENG INTERMITTENT W C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CA P685656 (CAN) #4 FIRE DETECTION LIGHT ON CAPTAIN'S ANNUNCIATOR PANEL. #4B NACELLE TEMPERATURE INDICATOR NEEDLE SHOWED 5-6 UNITS, AS POWER WAS ADVANCED ON TAKEOFF ROLL. REJECTED. #4 NACELLE TEMPERATURE INDICATOR REMAINED AT 3 UNITS EVEN AFTER SHUTDO WN. NO OTHER ABNORMAL INDICATIONS. CHANGED #4 ENGINE LOOP B. TESTED DETECTION CARD. 2 L 7 4 4F 4 F A20WE E20EA 1997010200188 19970102 00188 EA 1997 1 2 CA960723526 1 19960523 A 2721 601R512261 SWITCH CNDAIR CL600 CL6002B19 EA RUDDER TRIM LOOSE W O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 CA 2579 (CAN) RUDDER TRIM WOULD NOT TRIM LEFT AND TRIMMED ONLY 1/3 RIGHT. RUDDER TRIM SWITCH FOUND LOOSE. 2 L 7 2 4F RT A21EA 1997010200189 19970102 00189 WP 1997 1 2 CA960723527 1 19960525 A 2422 26440005 INVERTER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE EMERG ELECT BURNT W O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA P656825D (CAN) PRIOR TO DEPARTURE, A BURNING SMELL WAS DETECTED IN THE CABIN AND AT THE SAME TIME THE RAMP PERSONNEL REPORTED A E LECT BURNING SMELL IN THE FORWARD CARGO AREA. MAINTENANCE INVESTIGATION FOUND THE EMERGENCY INVERTER BURNT. SERVICEABLE INVERTER INSTALLED. 2 L 7 2 4F 4 F A6WE E2EA 1997010200190 19970102 00190 EA 1997 1 2 CA960723528 1 19960526 A 2920 AE409660060000 LINE CNDAIR CL600 CL6002B19 EA #3 HYD.PRESSURE LEAKING W O OTHER J K WARNING INDICATION FLUID LOSS CR CRUISE 1 CA 1689 (CAN) EICAS MESSAGE, 'HYDRAULIC 3 LOW PRESSURE' WITH LOSS OF #3 SYSTEM QUANTITY. MANUAL LANDING GEAR EXTENSION CARRIED O UT. #3 HYDRAULIC PRESSURE LINE LEAKING. 2 L 7 2 4F RT A21EA 1997010200191 19970102 00191 EU 1997 1 2 CA960723529 1 19960526 A 3230 664700500A4B SENSOR AIRBUS 320 A320211 3930320 EU MLG NR 6 FAILED W O OTHER J WARNING INDICATION AP APPROACH 1 CA (CAN) ON APPROACH WHEN LANDING GEAR SELECTED DOWN, GEAR DOORS PARTIALLY UNLOCKED AND GEAR DID NOT LOWER, RECYCLED GEAR O KAY WITH THREE GREEN LIGHTS. MAINTENANCE ACTION INVOLVED REPLACING RIGHT N6 SENSOR 36A OF THE LANDING GEAR CONTROL INTER FACE UNIT #2. OPERATIONAL TEST OF LANDING GEAR CARRIED OUT. 2 L 7 2 4F RT A28NM 1997010200192 19970102 00192 WP 1997 1 2 CA960723530 1 19960528 A 2170 1808491 COALESCER BAGS DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE AIR COND CONTAMINATED W O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA P657413D (CAN) PRIOR TO DEPARTURE, A.P.U. SUPPLYING AIR PRESSURE TO AIR CONDITIONING PACKS ENABLED SMOKE AND ODOUR TO ENTER THE C ABIN. MAINTENANCE ACTION INVOLVED CHANGING BOTH COALESCER BAGS. 2 L 7 2 4F 4 F A6WE E2EA 1997010200193 19970102 00193 WP 1997 1 2 CA960723531 1 19960528 A 3233 39140165501 ACTUATOR DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE RT MLG FAILED W O OTHER O K OTHER FLUID LOSS TX TAXI/GRND HDL 1 CA P657442D (CAN) SHORTLY AFTER LANDING GEAR RETRACTION, LOUD BANG HEARD ACCOMPANIED WITH VIBRATION AND RIGHT GEAR UNSAFE LIGHT ILLU MINATED WITH LOSS OF RIGHT HYDRAULIC QUANTITY. MAINTENANCE CHECK FOUND RIGHT MAIN GEAR RETRACT ACTUATOR SPLIT AND AUXILI ARY HYDRAULIC PUMP LEAKING. MAINTENANCE ACTION INVOLVED CHANGING RIGHT GEAR RETRACT ACTUATOR, CHECKING AND CHANGING ALL HYDRAULIC FILTERS. ALSO AUXILIARY HYDRAULIC PUMP AND BUNGEE CYLINDER REPLACED. GEAR OPERATIONALLY CHECKED. 2 L 7 2 4F 4 F A6WE E2EA 1997010200194 19970102 00194 EU 1997 1 2 CA960723532 1 19960528 A 2530 OVEN AIRBUS 320 A320211 3930320 EU GALLEY SMOKING W O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 CA (CAN) BOTH CLASS GALLEY OVENS SMOKING ON TAKEOFF. SMOKE CAUSE BY SPILLED FOOD ON OVEN ELEMENTS. OVENS CLEANED. 2 L 7 2 4F RT A28NM 1997010200195 19970102 00195 WP 1997 1 2 CA960723533 1 19960531 A 3320 ELECT RHEOSTAT DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE ATTENDANT PANEL ELECT SHORT W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA P657270D (CAN) SMOKE IN AFT CABIN BEHIND FLIGHT ATTENDANT PANEL. MAINTENANCE CHECK FOUND TWO BURNT WIRES. LIGHT RHEOSTAT AND TWO BURNT WIRES REPLACED. 2 L 7 2 4F 4 F A6WE E2EA 1997010200196 19970102 00196 EU 1997 1 2 CA960723534 1 19960602 A 2752 831202 SENSOR AIRBUS 320 A320211 3930320 EU RT FLAP 40 CV FAILED W A O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA (CAN) FLAPLOCK OCCURRED BETWEEN POSITON 1 & 2 ON APPROACH. MAINTENANCE ACTION INVOLVED REPLACING INTERCONNECT SENSOR 40 CV AND R.M.A. 27-50-867 CARRIED OUT. ALSO #1 RIGHT FLAP ACTUATOR ADJUSTED AND TESTED. 2 L 7 2 4F RT A28NM 1997010200198 19970102 00198 NM 1997 1 2 CA960723536 1 19960604 A 2710 60B800506 ACTUATOR BOEING 767 767209 NM PWA JT9 JT9D7R4D 52054 NE AILERON MALFUNCTION W O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 CA P707529 (CAN) DURING FLIGHT AILERON LOCKOUT MESAGE ON EICAS. RH AILERON LOCKOUT ACTUATOR REPLACED. 2 L 7 2 4F 4 F RT A1NM E3NE 1997010200199 19970102 00199 NM 1997 1 2 CA960723537 1 19960608 A 2421 SHAFT BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE NR 2 ENG IDG SHEARED W E ENGINE SHUTDOWN J K WARNING INDICATION FLUID LOSS CL CLIMB 1 CA P709691 (CAN) ONE-HALF HOUR INTO FLIGHT THE #2 ENGINE OIL QUANTITY DROPPED TO ZERO, WITH OIL PRESSURE FLICKERING AND OIL PRESSUR E DROPPING TO AMBER BAND. #2 ENGINE SHUTDOWN. POST FLIGHT INSPECTION FOUND INTEGRATED DRIVE GENERATOR (I.D.G.) QUADRANT RING SCREW SHEARED AND I.D.G. SHAFT SHEARED. REPLACED I.D.G. AND QUADRANT RING ASSEMBLY. GEARBOX INSPECTED AND ENGINE GR OUND RUN SERVICEABLE. 2 L 7 2 4F 4 F RT A1NM E3NE 1997010200200 19970102 00200 NM 1997 1 2 CA960723538 1 19960608 A 3230 SOLENOID BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE MLG FAILED W O OTHER J WARNING INDICATION AP APPROACH 1 CA P709691 (CAN) PRIOR TO ARRIVAL CREW WERE UNABLE TO RAISE LANDING GEAR, HAD TO PUSH OVERRIDE BUTTON. SOLENOID REPLACED. 2 L 7 2 4F 4 F RT A1NM E3NE 1997010200202 19970102 00202 NM 1997 1 2 CA960723540 1 19960609 A 5730 P113T1663912 PANEL BOEING 767 767209 NM PWA JT9 JT9D7R4D 52054 NE RT WING TE MISSING W A K NONE O OTHER IN INSP/MAINT 1 CA P707529 (CAN) ON WALKAROUND FOUND RH WING TRAILING EDGE FALSEWORK PANEL MISSING, 9 FEET BY 1 FOOT. 2 L 7 2 4F 4 F RT A1NM E3NE 1997010200203 19970102 00203 WP 1997 1 2 CA960723541 1 19960609 A 2170 COALESCER BAG DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE CABIN AIR COND CONTAMINATED W O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 CA P657763D (CAN) AT APPROXIMATELY V1 ON TAKEOFF CREW NOTICED BURNING RUBBER SMELL. FLY BY TOWER REVEALED NORMAL EXTENDED GEAR. MAI NTENANCE ACTION INVOLVED CHECKING NOSE LANDING GEAR FORWARD ACCESSORY AND E/E COMPARTMENTS. A STRONG ODOUR WAS DETECTED IN AREA OF LEFT HAND AIR CONDITIONING PACK. COALESCER BAGS REPLACED AND PNEUMATIC PILOT PRESSURE REGULATOR AND AIR CONDI TIONING PILOT PRESSURE REGULATOR CHANGED. 2 L 7 2 4F 4 F A6WE E2EA 1997010200204 19970102 00204 EA 1997 1 2 CA960723542 1 19960609 A 5210 RODS CNDAIR CNDAIR CL600 CL6002B19 EA DOOR LATCH OUT OF ADJUST W O OTHER J WARNING INDICATION CL CLIMB 1 CA 222 (CAN) MAIN CABIN DOOR RED WARNING LIGHT AND DOOR AUDIO WARNING MESSAGE ON EICAS. FOUND PASSENGER DOOR UPPER LATCH MISALI GNED IN CLOSED POSITION. DOOR LATCH CONTROL ROD ADJUSTED. 2 L 7 2 4F RT A21EA 1997010200205 19970102 00205 WP 1997 1 2 CA960723543 1 19960610 A 3610 LINE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE PRESS REG VALVE LOOSE W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA P657506D (CAN) DURING INITIAL CLIMB, TAIL COMPARTMENT HIGH HEAT LIGHT ILLUMINATED. AIR FOIL ICE PROTECTION NOT SELECTED. AIR COND ITIONING SELECTED TO HP PRESSURE BLEED OFF, LIGHT WENT OUT. MAINTENANCE CHECK REVEALED A LOOSE LINE BELOW LEFT HAND PRES SURE REGULATOR VALVE. ALSO DUCT AND TOP CLAMP LOOSE ON LH PRESSURE REGULATOR VALVE CAUSING HOT AIR TO LEAK OUT. 2 L 7 2 4F 4 F A6WE E2EA 1997010200206 19970102 00206 NM 1997 1 2 CA960723544 1 19960613 A 2780 5T004953 ELECTRONIC UNIT BOEING 767 767209 NM PWA JT9 JT9D7R4D 52054 NE LE FLAPS MALFUNCTION W A O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 CA P709637 (CAN) ON APPROACH LEADING EDGE FLAPS DISAGREE LIGHT ON. FLAP ZERO DEGREE LANDING. REPLACED FLAP SLAT ELECTRONIC UNIT. 2 L 7 2 4F 4 F RT A1NM E3NE 1997010200207 19970102 00207 EU 1997 1 2 CA960723545 1 19960615 A 2530 TIMER SEIZED AIRBUS 320 A320211 3930320 EU GALLEY HOT CUP BURNING SMELL W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA (CAN) AFTER TAKEOFF, ELECTRICAL BURNING SMELL DETECTED IN FORWARD GALLEY. MAINTENANCE CHECK REVEALED HOT CUP TIMER WAS T EMPORARILY SEIZED. ELECTRICAL POWER AT HOT CUP AND TIMER OUTLET OPERATIONALLY CHECKED. 2 L 7 2 4F RT A28NM 1997010200208 19970102 00208 WP 1997 1 2 CA960723546 1 19960615 A 2530 ELECT RECEPTACLE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE GALLEY MALFUNCTION W O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA P657518D (CAN) PRIOR TO DEPARTURE, BURNING SMELL DETECTED IN GALLEY AREA. OVENS AND ELECTRICAL OUTLET CHECKED. 2 L 7 2 4F 4 F A6WE E2EA 1997010200209 19970102 00209 WP 1997 1 2 CA960723547 1 19960617 A 4930 26011931 FUEL ATOMIZER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE AUX POWER UNIT LEAKING W O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA P657518D (CAN) PRIOR TO DEPARTURE AND WITH AIR CONDITIONING PACKS ON, THERE WAS A PRESENCE OF OILY SMOKE IN THE CABIN. MAINTENANC E CHECK FOUND FUEL LEAKING AT AUXILIARY POWER UNIT FUEL ATOMIZER. THE FUEL ATOMIZER ASSEMBLY AND SEAL WERE CHANGED AND L EAK CHECK CARRIED OUT. 2 L 7 2 4F 4 F A6WE E2EA 1997010200210 19970102 00210 WP 1997 1 2 CA960723548 1 19960617 A 2131 21011404 CONTROLLER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE CABIN PRESS INOPERATIVE W B G O EMER. DESCENT O2 MASK DEPLOYED OTHER J WARNING INDICATION CR CRUISE 1 CA P657442D (CAN) AT FLIGHT LEVEL 330, FLOW LIGHT CAME ON, CABIN 1000 FT/MINUTE. COMPLETED DRILL, CABIN UNCONTROLLABLE, OXYGEN MASKS DEPLOYED WHEN CABIN THRU FLIGHT LEVEL 10,000 FT., RECOVERED CABIN PRESSURE AT FLIGHT LEVEL 220. MAINTENANCE ACTION INVO LVED CHANGING #1 CABIN CONTROLLER. 2 L 7 2 4F 4 F A6WE E2EA 1997010200211 19970102 00211 EU 1997 1 2 CA960723549 1 19960618 A 2841 SIC5059040107 INDICATOR AIRBUS 320 A320211 3930320 EU FUEL QTY INOPERATIVE W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) ON CLIMB OUT, FUEL QUANTITY READING 10,400 KGS AND DID NOT DECREASE. AIRCRAFT RETURNED TO DEPARTURE BASE. MAINTENA NCE ACTION INVOLVED CHANGING THE FUEL QUANTITY INDICATOR COMPUTER (F.Q.I.C.). FUEL SYSTEM CHECKED. 2 L 7 2 4F RT A28NM 1997010200212 19970102 00212 WP 1997 1 2 CA960723550 1 19960618 A 2131 21011404 CONTROLLER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE CABIN PRESS INOPERATIVE W O B OTHER EMER. DESCENT J WARNING INDICATION CR CRUISE 1 CA P657222D (CAN) AT FLIGHT LEVEL 350 FLOW LIGHT CAME ON. DESCENT INITIATED, LIGHT WOULD GO OFF AND ON. AT FLIGHT LEVEL 290 LIGHT CA ME ON AND CABIN STARTED TO CLIMB AT MAX RATE. EMERGENCY DESCENT INITIATED AND CABIN CONTROL REGAINED JUST BELOW 20,000 F EET. MAINTENANCE CARRIED OUT BITE TEST ON #1 CONTROLLER. #1 CABIN PRESSURE CONTROLLER CHANGED. 2 L 7 2 4F 4 F A6WE E2EA 1997010200213 19970102 00213 EA 1997 1 2 CA960723551 1 19960618 A 3230 864806 PSEU CNDAIR CL600 CL6002B19 EA MLG RETRACT FAILED W O OTHER J WARNING INDICATION CL CLIMB 1 CA 1835 (CAN) UNABLE TO RETRACT LANDING GEAR AFTER TAKEOFF. PROXIMITY SWITCH ELECTRONIC UNIT (PSEU) AND LANDING GEAR SELECTOR HA NDLE (P/N 717901-5) REPLACED. 2 L 7 2 4F RT A21EA 1997010200214 19970102 00214 EA 1997 1 2 CA960723552 1 19960618 A 2760 54C54677E01 MANIFOLD CNDAIR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE GROUND SPOILER FAILED W O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 CA 3688 807199 (CAN) PRIOR TO ARRIVAL, OUTBOARD GROUND SPOILER FAULT. OUTBOARD GROUND SPOILER PAIR INOPERATIVE AND #2 SECU BITE TEST SH OWED GROUND SPOILER MANIFOLD FAILURE. 2 L 7 2 4F 4 F RT A21EA E15NE 1997010200215 19970102 00215 EU 1997 1 2 CA960723553 1 19960619 A 2750 SENSOR AIRBUS 320 A320211 3930320 EU FLAP 40CV FAILED W A O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA (CAN) DURING APPROACH WHEN FLAP 2 SELECTED FLAP LOCKOUT OCCURRED. PERFORMED QUICK REFERENCE HANDBOOK (QRH) LANDING. REQU IRED MAINTENANCE ACTION (R.M.A.) 27-50-867 COMPLETED. INTERCONNECT SENSOR 40 CV REPLACED. FLAP OPERATION CARRIED OUT. 2 L 7 2 4F RT A28NM 1997010200216 19970102 00216 EA 1997 1 2 CA960723554 1 19960620 A 3234 7179015 SELECTOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE LANDING GEAR FAILED W O OTHER J WARNING INDICATION AP APPROACH 1 CA 4035 807157 (CAN) PRIOR TO ARRIVAL COULD NOT LOWER LANDING GEAR. AFTER THREE ATEMPTS IT LOWERED NORMALLY. LANDING GEAR SELECTOR CHAN GED. 2 L 7 2 4F 4 F RT A21EA E15NE 1997010200217 19970102 00217 WP 1997 1 2 CA960723555 1 19960520 A 2530 ELECT RECEPTACLE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE GALLEY OVEN CABIN ELECT ODOR W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA P657270D (CAN) ACUTE ACCRID ELECTRICAL ODOUR COMING FROM THE GALLEY, OVENS SWITCHED OFF. OVEN RECEPTACLES CHECKED AND GALLEY POWE R AND EQUIPMENT CHECK CARRIED OUT. 2 L 7 2 4F 4 F A6WE E2EA 1997010200218 19970102 00218 WP 1997 1 2 CA960723556 1 19960623 A 2131 1304081 CONTROLLER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE CABIN PRESS FAILED W A G UNSCHED LANDING O2 MASK DEPLOYED J WARNING INDICATION CL CLIMB 1 CA P657518D (CAN) AIRCRAFT RETURNED FROM FLIGHT DUE TO ONE PRESSURE CONTROLLER ON DEVIATION AND A SECOND CONTROLLER FAILED DURING CL IMB. PASSENGER OXYGEN MASKS DEPLOYED. MAINTENANCE ACTION INVOLVED CHANGING #1 AND #2 PRESSURE CONTROLLERS AND #1 CABIN P RESSURE SELECTOR. CABIN PRESSURIZATION CHECKS CARRIED OUT. 2 L 7 2 4F 4 F A6WE E2EA 1997010200220 19970102 00220 EU 1997 1 2 CA960724001 1 19960702 A 2910 SD3731235 LINE STBROS SD3 SD360 8100606 EU PWA PT6 PT6A65AR 52043 NE NOSE AREA CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA PCE97047 (CAN) ON WALKAROUND, FLIGHT CREW NOTICED HYDRAULIC FLUID DRIPPING FROM NOSE LANDING GEAR AREA. TWO HYDRAULIC LINES FOUND WITH CRACKED COUPLING NUTS. 2 H 7 2 4T 4 T A41EU E4EA 1997010200221 19970102 00221 EU 1997 1 2 CA960724002 1 19960716 A 7603 SD3476160 CABLE STBROS SD3 SD360 8100606 EU PWA PT6 PT6A65AR 52043 NE STA 75.45 FRAYED W K NONE O OTHER LD LANDING 1 CA PCE97047 (CAN) CABLE FRAYED AT PULLEY LOCATION STA 75.45 FOR LEFT ENGINE POWER CONTROL. CABLE WAS LAST INSPECTED PER SD360-76-08R 1, 414 HOURS PREVIOUSLY. COULD NOT ACHIEVE REVERSE THRUST. IN ADDITION A CHANGE WAS NOTED IN N1 SPEEDS AT WHICH AUTOFEAT HER AND RTOP ARMING LIGHTS CAME ON DUE TO OUT OF RIG POWER LEVERS. 2 H 7 2 4T 4 T A41EU E4EA 1997010200222 19970102 00222 NM 1997 1 2 CA960724004 1 19960713 A 2120 32167441 PACK VALVE BOEING 727 727217 NM PWA JT8 JT8D17 52049 NE LT SIDE PACK INOPERATIVE W A G I UNSCHED LANDING O2 MASK DEPLOYED CABIN DEPRESSURIZATION J WARNING INDICATION CL CLIMB 1 CA 688240 (CAN) PRESSURIZATION LOST ON CLIMB AT 25,000 FEET. LH SIDE PACK VALVE REPLACED. 2 L 7 3 4F 4 F RT A3WE E2EA 1997010200223 19970102 00223 NM 1997 1 2 CA960724401 1 19960620 A 3150 MODULE BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE AURAL WARN MALFUNCTION W C D ABORTED TAKEOFF RETURN TO BLOCK J O WARNING INDICATION OTHER TO TAKEOFF 1 CA 30692 (CAN) AUTO PILOT DISCONNECTED PLUS AURAL WARNING AT 90 KNOTS. FMC DUMP OF ALL PERFORMANCE AND NAVIGATION INFORMATION. AU RAL WARNING MODULE REPLACED, FDR REPLACED. 2 L 7 2 4F 4 F RT A2NM E12EU 1997010200225 19970102 00225 EU 1997 1 2 CA960725101 1 19960716 A 5753 D5754054420200 BOLT AIRBUS D57540510007 AIRBUS 320 A320211 3930320 EU #2 RH FAIRING MISSING W A K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING WALK AROUND FOUND SIDE STAY ROD PROTRUDING THROUGH A 9 INCH BY 3 INCH HOLE IN THE #2 RH FLAP FAIRING. FURTH ER MAINTENANCE CHECK FOUND THE BOLT WHICH ATTACHES THE DRIVE ROD TO THE FAIRING WAS FOUND INSIDE THE FAIRING, THE CASTEL LATED NUT, WASHER AND COTTER PIN WERE MISSING. FAIRING WAS REMOVED FOR REPAIRS AND AIRCRAFT DISPATCHED AS PER CDL 27-01. 2 L 7 2 4F RT A28NM 1997010200226 19970102 00226 NM 1997 1 2 CA960725102 1 19960717 A 3040 1483 CAPACITOR PACIFICELECT 2312 BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE WINDOW HEAT BURNT W A K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA 1483 707313 (CAN) DURING FLIGHT CREW REPORTED LEFT SIDE WINDOW HEATER DID NOT WORK . WORKED AFTER CB RESETTHIRTY MINUTES AFTER ARRI VAL CREW REPORTED ELECTRICAL SMOKE AND SMELLL ON THE FLIGHT DECK LH SIDE WINDOW HEATER WIRE BROKEN AT THE LOWER WINDOW T ERMINAL STRIP. LH SIDE CONTROLLER BURNED INSIDE. REPAIRED OR REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1997010200227 19970102 00227 NM 1997 1 2 CA960725103 1 19960722 A 3242 2611723 PRESSURE PLATE BENDIX 26088126 BOEING 767 767375 NM NR 5 BRAKE MISSING W D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 CA 23493 8918 B1774G (CAN) AIRCRAFT RETURNED TO GATE DUE TO MASSIVE HYDRAULIC LEAK #5 BRAKE DISINTEGRATED. PRESSURE PLATE MISSING, #1 STATOR HAD DISINTEGRATED. ALL PISTONS HAD HYPER EXTENDED. ONE PISTON BROKEN OUT OF BACK PLATE. REPLACED. 2 L 7 2 4F RT A1NM 1997010200228 19970102 00228 SW 1997 1 2 CA960729002 1 19960621 A 6520 212040365019 BEARING BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA T/R QUILL ASSY BROKEN CAGE W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 6662 CPPS60190 (CAN) WHILE INVESTIGATING AN OIL LEAK IN THE AREA OF THE TAIL ROTOR DRIVE QUILL AT THE REAR OF THE MAIN GEARBOX, THE AME REMOVED THE SUSPECTED LEAKING SEAL. IT WAS FOUND THAT THE INNER CAGE OF THE BEARING HAD BROKEN AND THE BALL BEARINGS WH ERE LOOSE IN WHAT REMAINED OF THE BEARING. 1 G 7 1 4U 4 U H4SW E22EA 1997010200229 19970102 00229 NM 1997 1 2 CA960729003 1 19960718 A 5344 HINGE BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE GALLEY CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 687746 (CAN) ON COMPLIANCE WITH AD 96-10-06, A 12 INCH CRACK WAS DETECTED ON THE FORWARD LOWER GALLEY LOWER HINGE. REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1997010200231 19970102 00231 EU 1997 1 2 CA960729005 1 19960724 A 2110 139312 SUPERCHARGER BRAERO 748 HS7482A 4231001 EU CABIN PRESS FAILED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA 1950 (CAN) ROTOR OF LH CABIN SUPERCHARGER FAILED, HOWEVER DID NOT SEIZE, QUILL SHAFT FAILED INTERNALLY CAUSING CABIN TO FILL WITH OIL MIST. VIBRATION ALSO CAUSED HYDRAULIC FITTING P/N ISS5757 (ATTACHED TO HYDRAULIC PUMP) TO CRACK, RESULTING IN LOSS OF HYDRAULIC FLUID. 2 L 7 2 3T A24EU 1997010200232 19970102 00232 EU 1997 1 2 CA960729009 1 19960717 A 3222 1800163 STRUT MENASCO STBROS SD3 SD330 8100602 EU PWA PT6 PT6A45R 52043 EA NOSE OVER INFLATED W A O UNSCHED LANDING OTHER G J MULTIPLE FAILURE WARNING INDICATION TO TAKEOFF 1 CA MC022 PCE84133 (CAN) ON TAKEOFF AND WHEN GEAR WAS SELECTED UP, NEAR THE END OF THE CYCLE A LARGE THUD WAS HEARD AND SIMULTANEOUSLY THE NOSE GEAR STEERING WENT HARD RIGHT. CREW DID SEVERAL FLY BYS AND GEAR CONFIRMED OFF TO RIGHT. LANDING OK. DISASSEMBLY SH OWED EXTENSIVE DAMAGE TO INTERNAL COMPONENTS OF NOSE STRUT. DAMAGE LIKELY A RESULT OF PREVIOUS OWNER OVER-INFLATING STRU T TO ENSURE TAIL OF AIRCRAFT WOULD CLEAR HANGAR ROOF. SUBMITTER NOTES THAT THIS IS NOT AN ACCEPTABLE PRACTICE AS THE CEN TERING CAMS ARE IN HARD CONTACT WITH EACH OTHER AND ROTATING THE NOSE GEAR DURING TOWING CAN CAUSE DAMAGE. 2 H 7 2 4T 4 T A41EU E4EA 1997010200234 19970102 00234 EU 1997 1 2 CA960729011 1 19960722 A 6410 355A12005004 BLADE AEROSP AS355 AS355F2 8680812 EU INTERNAL SPAR DEBONDED W K NONE O OTHER IN INSP/MAINT 1 CA 2629 (CAN) NOISE HEARD FROM BLADE WHILE PERFORMING DAILY INSPECTION. FOUND BLADE DELAMINATED AT SPAR. 1 G 7 2 3U H11EU 1997010200235 19970102 00235 SW 1997 1 2 CA960729013 1 19960716 A 2720 27420511 TUBE SWRNGN 2742001123 SWRNGN SA227 SA227AC 8780603 SW ROTOL R321 R321482F8 GL RUDDER CRACKED W A K NONE O OTHER IN INSP/MAINT 1 CA 23674 33183 (CAN) RUDDER TORQUE TUBE CRACKED WHERE LOWER FLANGE IS WELDED TO TUBE. CRACK EXTENDS APPROXIMATELY 20 PERCENT OF THE CIR CUMFERENCE. AT REMOVAL IT WAS DISCOVERED THAT A GROOVE WAS WORN BY THE PHENOLIC TORQUE TUBE SEAL OF UP TO 30 PERCENT OF THE TUBE WALL THICKNESS. FOUND DURING UNRELATED MAINTENANCE. 2 L 7 2 4T RT A8SW 6 C P61GL 1997010200236 19970102 00236 EU 1997 1 2 CA960729015 1 19960624 A 7120 350A21106605 MOUNT SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE INBOARD LT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 257 (CAN) L/H SHOCK MOUNT ASSEMBLY CRACKED. 1 G 7 1 3U 3 U H9EU E19EU 1997010200238 19970102 00238 EU 1997 1 2 CA960730502 1 19960630 A 7933 Z430440 TEMP SWITCH AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE #2 ENGINE OIL FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 731707 (CAN) AFTER THRUST REDUCTION ECAM WARNING #2 ENGINE OIL TEMPERATURE HIGH ILLUMINATED, OIL TEMPERATURE WAS BOXED AND FLAS HING AND INDICATED 700 DEGREES. ENGINE SHUT DOWN. MAINTENANCE ACTION INVOLVED CHANGING BOTH OIL TEMPERATURE SWITCHES. EN GINE GROUND RUN AND LEAK CHECK CARRIED OUT. 2 L 7 2 4F 4 F RT A28NM E29NE 1997010200239 19970102 00239 EU 1997 1 2 CA960730503 1 19960630 A 2612 FIRE WARN DET AIRBUS 320 A320211 3930320 EU NR 2 ENG CHAFED WIRE W C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CA (CAN) ON DEPARTURE FROM GATE, #2 ENGINE FIRE LOOP "B" FAULT LIGHT CAME ON INTERMITTENTLY. ON TAKEOFF ROLL ENGINE FIRE WA RNING CAME ON AT 120 KNOTS. TAKEOFF REJECTED. FIRE WARNING CEASED WHEN IDLE SELECTED AFTER REJECT. FLIGHT ATTENDANT REPO RTED WHITE SMOKE COMING OUT OF EXHAUST. MAINTENANCE CHECK FOUND CHAFED WIRE #2612-219 AT JUNCTION BOX FORWARD OF PLUG 47 0 VC RIGHT HAND ENGINE PYLON. WIRE REPAIRED AND RECLAMPED. FIRE DETECTION OPERATION TESTED SERVICEABLE. 2 L 7 2 4F RT A28NM 1997010200240 19970102 00240 EU 1997 1 2 CA960730505 1 19960711 A 5610 STA320141 WINDSHIELD AIRBUS 320 A320211 3930320 EU CAPTAINS SHATTERED W A O OTHER O OTHER CR CRUISE 1 CA (CAN) IN CRUISE AT FLIGHT LEVEL 370 CAPTAIN'S WINDSHIELD SHATTERED. WINDSHIELD AND HEAT CONTROLLER REPLACED. 2 L 7 2 4F RT A28NM 1997010200241 19970102 00241 WP 1997 1 2 CA960730506 1 19960711 A 2131 21011403 CONTROLLER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE CABIN PRESS INOPERATIVE W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA P657216D (CAN) UNABLE TO PRESSURIZE AIRCRAFT ON CLIMB OUT, STANDBY INOPERATIVE, ONLY MANUAL PRESSURIZATION AVAILABLE. BOTH CABIN PRESSURE CONTROLLERS REPLACED. 2 L 7 2 4F 4 F A6WE E2EA 1997010200242 19970102 00242 1997 1 2 CA960730507 4 19960714 A 2350 200461 HEADSET BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE FLIGHT OFFICER MALFUNCTION W A UNSCHED LANDING O OTHER TX TAXI/GRND HDL 1 CA P709662 (CAN) ON TAXI CAPTAIN AND FLIGHT OFFICER LOST VHF COMMUNICATIONS. FLIGHT OFFICERS HEADSET REPLACED. 2 L 7 2 4F 4 F RT A1NM E3NE 1997010200243 19970102 00243 NM 1997 1 2 CA960731002 1 19960720 A 2731 SERVO TABS DHAV DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE ELEVATOR OUT OF BALANCE W A K O NONE OTHER E F VIBRATION/BUFFET FLT CONT AFFECTED DE DESCENT 1 CA 15011 120339 (CAN) ELEVATOR FLUTTER OCCURRED WHEN AUTO PILOT WAS 'ON' AND AIRCRAFT IN DESCENT. INSPECTION OF PITCH CONTROL SURFACES R EVEALED THAT BOTH ELEVATOR SERVO TABS WERE 'OUT OF BALANCE' DUE TO A POOR PAINT JOB. HEAVY RUNS IN PAINT AT TRAILING EDG E. IT IS SUSPECTED THAT THIS OUT OF BALANCE CONDITION CAUSED THE FLUTTER WHICH IN TURN CAUSED THE CRANK P/N 82760119101, TO WORK LOOSE ON THE ELEVATOR CONTROL CRANK TUBE. ALUMINUM WASHERS USED IN ATTACHING HARDWARE FOR THE CRANK WERE HEAVIL Y WORN. A SMALL AMOUNT OF CHAFING WAS FOUND ON THE MATING SURFACES BETWEEN THE CRANK AND CRANK TUBE. 2 H 7 2 4T 4 T RT A13NM E20NE 1997010200244 19970102 00244 NM 1997 1 2 CA960731003 1 19960713 A 2910 65404012 SWIVEL BOEING 727 72790C 1384030 NM PWA JT8 JT8D7B 52053 NE NLG AREA CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 653646 (CAN) ON PUSH BACK A HYDRAULIC LEAK WAS NOTICED AT THE NOSE LANDING GEAR AREA, LEAKING SEALS AT SWIVEL JOINT. IN REPLACI NG SEALS A CRACK WAS DISCOVERED IN THE MANIFOLD. REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 1997010200246 19970102 00246 NM 1997 1 2 CA960801002 1 19960724 A 5230 1177261 EYE END DOWTY 1U11772 BOEING 737 737275 1384485 NM PWA JT8 JT8D17 52049 NE CARGO DOOR SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA 43052 19482 0118 702735 (CAN) EYE END OF MAIN GARGO DOOR ACTUATOR FAILED WHILE CLOSING DOOR FROM FULLY OPEN. DOOR CLOSED CAUSING DAMAGE TO ONE L OCK ASSEMBLY. 2 L 7 2 4F 4 F A16WE E2EA 1997010200247 19970102 00247 NM 1997 1 2 CA960801003 1 19960730 A 5350 RADOME BOEING 767 767375 NM NOSE HAIL DAMAGE W A UNSCHED LANDING C F.O.D. CL CLIMB 1 CA (CAN) BIRD STRIKE AND HAIL DAMAGE TO RADOME, WINDSHIELD REPLACED TEMPORARY REPAIR TO RADOME. 2 L 7 2 4F RT A1NM 1997010200248 19970102 00248 NM 1997 1 2 CA960801004 1 19960730 A 5350 RADOME BOEING 767 767375 NM NOSE HAIL DAMAGE W K NONE C F.O.D. CL CLIMB 1 CA (CAN) HAIL DAMAGE TO RADOME AND LH AND RH LEADING EDGE DEVICES. 2 L 7 2 4F RT A1NM 1997010200249 19970102 00249 NM 1997 1 2 CA960801005 1 19960731 A 3020 655812313 DUCT BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE NOSE COWL CRACKED W A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 CA 702660 (CAN) OVERHEAT LIGHT AND LOW PNEUMATIC PRESSURE INDICATION. NOSE COWL ANTI-ICE DUCT FOUND CRACKED AT FORWARD WELD FORWAR D OF BELLOWS. REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1997010200251 19970102 00251 NM 1997 1 2 CA960801007 1 19960726 A 2913 55097 PUMP ABEX 55097 BOEING 737 737210C 1384459 NM PWA JT8 JT8D9A 52048 NE HYD SYS LEAKING W O OTHER K FLUID LOSS CL CLIMB 1 CA 3053 101343H P678085 (CAN) DURING CLIMB A SYSTEM HYDRAULIC PRESSURE DROPPED TO ZERO. AIRCRAFT LANDED USING B SYSTEM. FLUID FROM #2 ENGINE HYD RAULIC PUMP REPALCED. #1 PUMP REPLACED AS PRECAUTION. 2 L 7 2 4F 4 F A16WE E2EA 1997010200259 19970102 00259 EA 1997 1 2 CA960801018 2 19960725 A 7314 90207801A GEARSET SUNDSTRAND 0253233003 BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA #2 ENG PUMP WORN SPLINES W K NONE X ENGINE FLAMEOUT AP APPROACH 1 CA 2722 8949 PCE80636 (CAN) ON FINAL APPROACH THE #2 ENGINE FLAMED OUT AND AUTO FEATHERED. THE LANDING WAS UNEVENTFUL AND MAINTENANCE WAS NOTI FIED. INSPECTION FOUND THE #2 ENGINE DRIVEN HP FUEL PUMP SPLINES WERE WORN OFF AND THE PUMP WAS SEIZED. THE #2 ENGINE HP FUEL PUMP WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. STRIP REPORT FROM THE OVERHAUL FACILITY STATES THAT "G EARSET DRIVE SPLINES WORN OFF COMPLETELY, ATTRIBUTED TO LACK OF LUBRICATION, DRIVE COUPLING WORN INTERNALLY, ONE DRIVE B EARING DIMENSIONALLY WORN". THE WORN PARTS WERE REPLACED AND THE UNIT OVERHAULED. 1 L 7 2 4T 4 T A24CE E4EA 1997010200260 19970102 00260 EU 1997 1 2 CA960801019 1 19960724 A 2621 FIRE BOTTLE AIRBUS 320 A320212 EU NR 1 CHAFED WIRE W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) #1 FIRE BOTTLE CIRCUIT TRIPS CB "2WEI" WHEN JOB TASK 262100-720-001 INITIATED. FURTHER CHECK REVEALED WIRE #CF20 C HAFED ON STEEL PIPE 1.5 FEET BACK FROM BOTTLE #1 SQUIB CONNECTION "5W32A" REF. WIRE MANUAL 26-21-03. CHAFED WIRE REPAIRE D IN ACCORDANCE WITH STANDARD MAINTENANCE MANUAL PRACTICES AND SYSTEM CHECKED SERVICEABLE. 2 L 7 2 4F RT A28NM 1997010200261 19970102 00261 SW 1997 1 2 CA960801501 1 19960502 A 7120 206031629103 MOUNT BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL ATTACHMENT POINT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 8568 CAE833907 (CAN) DURING AN ANNUAL INSPECTION, CRACKS WERE FOUND AT THE ATTACHMENT POINTS OF THE ENGINE FORWARD SUPPORTS. FORWARD EN GINE LEG SUPPORTS FITTINGS AND STIFFENERS 206-031-629-103 AND 206-031-201-291 REPLACED. ENGINE MOUNT SUPPORT CHANNEL AND FRAME 206-031-302-257 REPLACED. 1 G 7 1 3U 3 U H2SW E4CE 1997010200262 19970102 00262 NM 1997 1 2 CA960801502 1 19960709 A 5347 CO3600420750 SPRING DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE LH SEAT TRACK FOULED W O OTHER O OTHER TO TAKEOFF 1 CA 120543 (CAN) CAPTAINS SEAT SHIFTED AFT ON TAKEOFF. SEAT TRACK WAS FOUND DIRTY AND THE SPRING WAS FOULED. THIS INCIDENT WAS SUBJ ECT OF BRAD SERVICE ADVISORY #96 03 15006 WHICH COINCIDENTALLY WAS RECEIVED SAME DAY INCIDENT HAPPENED. 2 H 7 2 4T 4 T RT A13NM E20NE 1997010200263 19970102 00263 1997 1 2 CA960802001 4 19960724 A 2210 SP50 CONTROL SPERRY SP50 BOEING 727 72725 1384006 NM PWA JT8 JT8D7 52053 NE AP SYS CONTL BOX PLATE SHORTED W B O EMER. DESCENT OTHER A FLAME/FIRE CR CRUISE 1 CA 0791347 657356 (CAN) A/P SYSTEM CONTROL BOX HAD BACK PLATE LIGHTING SHORT. 2 L 7 3 4F 4 F A3WE E2EA 1997010200264 19970102 00264 NM 1997 1 2 CA960802005 1 19960512 A 5754 114N207517 SUPPORT FITTING BOEING 757 75723A 1384967 NM RROYCE RB211 RB211535E4 54555 NE INB AUX TRACK CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 30828 (CAN) #8 INBOARD AUXILIARY TRACK SUPPORT CASTING FOUND CRACKED. ALL DAMAGED ITEMS REPLACED. 2 L 7 2 4F 4 F RT A2NM E12EU 1997010200265 19970102 00265 EU 1997 1 2 CA960807001 1 19960702 A 2910 SD3730916 LINE STBROS SD3 SD360 8100606 EU PWA PT6 PT6A65AR 52043 NE NLG AREA CRACKED COUPLING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA PCE97047 (CAN) ON WALKAROUND FLIGHT CREW NOTED HYDRAULIC FLUID LEAKING FROM NOSE LANDING GEAR AREA. MAINTENANCE FOUND 2 HYDRAULIC LINES WITH CRACKED COUPLING NUTS. 2 H 7 2 4T 4 T A41EU E4EA 1997010200266 19970102 00266 SO 1997 1 2 CA960807010 2 19960726 A 8530 PISTON RING CONT CESSNA 206 U206G 2073356 CE CONT O520 IO520F 17032 SO MCAULY D3A34 D3A34C404 GL #3 PISTON BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 765 169393H 797644 (CAN) INSPECTION FOUND THE TOP RING ON THE #3 CYLINDER BROKEN INTO SEVEN PIECES. THE COMPRESSION CHECK FOUND COMPRESSION AT 12 PSI. 1 H 7 1 3O 3 O A4CE E5CE 5 C P47GL 1997010200267 19970102 00267 SO 1997 1 2 CA960807011 2 19960726 A 8530 VALVE CONT CESSNA 206 U206G 2073356 CE CONT O520 IO520F 17032 SO MCAULY D3A34 D3A34C404 GL #1 CYL EXH BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 765 169393H 797644 (CAN) DURING INSPECTION THE EXHAUST VALVE ON #1 CYLINDER WAS FOUND BROKEN. COMPRESSION TEST INDICATED "0" COMPRESSION. 1 H 7 1 3O 3 O A4CE E5CE 5 C P47GL 1997010200268 19970102 00268 SO 1997 1 2 CA960808006 2 19960708 A 8540 642083A7 ADAPTER CESSNA 310 310R 2074245 CE CONT O520 IO520M 17032 SO MCAULY 3AF32C 3AF32C87 GL STARTER BINDING W K NONE O OTHER IN INSP/MAINT 1 CA 277455R 892023 (CAN) THE STARTER ADATPER WAS STARTING TO SLIP SO A NEW STARTER ADAPTER (P/N 642083A7) WAS INSTALLED. AFTER THE FIRST FL IGHT THE ENGINE WAS STIFF AND THE STARTER WAS LABORING TO TURN OVER THE ENGINE. THE NEWLY INSTALLED STARTER ADAPTER WAS REMOVED AND FOUND ALMOST SEIZED WITH TRACES OF BRASS IN THE OIL FITLER. THE OIL SYSTEM WAS FLUSHED AND REPLENISHED AND A N OVERHAULED UNIT IN STOCK WAS INSTALLED WITHOUT FURTHER PROBLEMS. 1 L 7 2 3O 3 O 3A10 E5CE 5 C P22EA 1997010200269 19970102 00269 EA 1997 1 2 CA960808007 1 19960801 A 7120 87110016009 STRUT DHAV DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE RT ENG VERT BROKEN W K NONE E VIBRATION/BUFFET TX TAXI/GRND HDL 1 CA 123152 (CAN) PILOT NOTED PROP VIBRATION. INSPECTION FOUND RIGHT HAND ENGINE, OUTBOARD REAR ENGINE MOUNT, VERTICAL STRUT BROKEN. BOTH REAR ENGINE MOUNTS STRUTS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1997010200270 19970102 00270 NM 1997 1 2 CA960808008 1 19960801 A 2497 WIRE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE PLUG 9811-P159 MISINSTALLED W A K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 22744 120360 (CAN) WIRING AT CROSS-OVER DISCONNECT CONNECTOR 9811-P159 FOUND INCORRECTLY TERMINATED DURING MAINTENANCE TASK 7320/02. WIRE 7611-10036C20 FOUND TERMINATED AT PIN T OF CONNECTOR AND WIRE 7611-20036B20 FOUND TERMINATED AT PIN U OF SAME CONNE CTOR. THIS EFFECTIVELY TIED THE LEFT AND RIGHT ESSENTIAL BUSSES TOGETHER THROUGH THE 2.5 AMP BREAKER FOR ECU 1 AND ECU 2 . THE BACKUP POWER FROM THE CROSS-SIDE ESSENTIAL BUS DID NOT EXIST. 2 H 7 2 4T 4 T RT A13NM E20NE 1997010200271 19970102 00271 WP 1997 1 2 CA960808010 1 19960729 A 3610 1568537113 DUCT LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE PNEU BLEED SYS BLOWN OPEN W C F D ABORTED TAKEOFF ACTIVATE FIRE EXT. RETURN TO BLOCK B J M SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION OVER TEMP TO TAKEOFF 1 CA 52048 10443 (CAN) TAKEOFF REJECTED DUE TO AFT FUSELAGE SECTION OVERHEAT AND UNSAFE TAKEOFF WARNING ON FLIGHT ENGINEER ANNUNCIATOR PA NEL. CONTROL TOWER ADVISED OF SMOKE/FUMES COMING FROM AIRCRAFT AFT SECTION. BOTH #2 ENGINE FIRE BOTTLES DISCHARGED AND T AKEOFF REJECTED. FOUND PNEUMATIC BLEED AIR DUCT BLOWN. REPLACED. 2 L 7 3 4F 4 F A23WE E12EU 1997010200275 19970102 00275 SO 1997 1 2 CA960808101 2 19960802 A 7322 173159 METERING PIN FACET MA45105284 CESSNA 182 182Q 2072732 CE CONT O470 O470U 17026 SO MCAULY 2A34C C2A34C204 GL ACCEL PUMP LEVER WORN W A O OTHER O OTHER CR CRUISE 1 CA GL48601 249977R 766089 (CAN) PILOT HAD PROBLEM WITH THROTTLE STICKING. CARBURETOR HEAT WAS APPLIED AND THE PROBLEM WAS RECTIFIED. AS CARBURET OR ICING WAS SUSPECTED THE PROBLEM WAS NOT REPORTED. ON THE RETURN FLIGHT THE THROTTLE STUCK AGAIN, AND COULD NOT BE FR EED. POST FLIGHT INSPECTION FOUND THE THROTTLE ARM SEIZED. THE CARB WAS REMOVED & SENT FOR INSPECTION. REPORT STATES "THE THROTTLE SHAFT RUNS THROUGH AN OPENING IN THE ACCELERATOR PUMP LEVER ASSEMBLY & IS FIXED TO THE SHAFT BY MEANS OF A SET SCREW. PROTRUDING FROM THE LEVER IS AN AIR METERING PIN ACTUATOR. AFTER A TIME THIS CONTACTING SURFACE MANAGED TO WEAR PAST THE EDGE OF THE AIR METERING PIN & BECAME LOCKED ON THE PIN PREVENTING THE SHAFT FROM CLOSING. 1 H 7 1 3O 3 O NT 3A13 E273 5 C P3EA 1997010200276 19970102 00276 NE 1997 1 2 CA960808103 2 19960714 A 7210 GEARBOX SNIAS 350 AS350D 8680803 EU LYC LTS101 LTS101600A3 41560 NE #4 & #5 BEARING BROKEN BEARING W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 8040 43064C (CAN) AIRCRAFT HAD CHIP DETECTOR LIGHT IN CRUISE AND RETURNED TO BASE. POST FLIGHT INSPECTION FOUND METAL IN THE OIL TAN K. FURTHER INSPECTION REVEALED THE #4 AND #5 BEARINGS HAD FAILED. THE COMPLETE GEARBOX WAS REPLACED. 1 G 7 1 3U 3 U H9EU E5NE 1997010200277 19970102 00277 EU 1997 1 2 CA960808105 1 19960716 A 2435 150G1061 TERMINAL BLOCK 150SG122Q SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE START/GEN BURNT W K NONE O OTHER IN INSP/MAINT 1 CA 1136 4496 (CAN) THE THIRD TERMINAL BLOCK (LOOKING FROM REAR, LEFT TO RIGHT) BURNT OUT. 1 G 7 1 3U 3 U NC H9EU E19EU 1997010200278 19970102 00278 NE 1997 1 2 CA960808106 2 19960801 A 7322 7436024 FUEL CONTROL HAMSTD BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE #2 ENGINE FAULTY W A D C RETURN TO BLOCK ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CA 40705 13854 94469 674465 (CAN) ON TAKEOFF, ADVANCED THRUST LEVERS TO NORMAL SPOOL UP POSITION, ENGINE ACCELERATION NORMAL, CONTINUED TO ADVANCE T HRUST LEVERS, #2 ENGINE ACCELERATION WAS A LITTLE SLOWER THAN #1 ENGINE, THEN AS THRUST LEVERS ADVANCED, #2 ENGINE ASSUM ED CONTINUOUS POWER ON ITS OWN UP TO 2.1 EPR (12 SECONDS). EGT WAS ALMOST ALWAYS IN THE GREEN BAND. TAKEOFF WAS REJECTED AT 70 KNOTS. #2 ENGINE DID NOT RESPOND TO THRUST LEVER POSITION. THE #2 ENGINE FUEL CONTROL UNIT AND THE HIGH PRESSURE FUEL PUMP WERE REPLACED. THE #2 ENGINE WAS RUN UP SERVICEABLE. CERTAIN INTERNAL FAILURES OF THE FCU WILL, AS A FAIL SAFE FEATURE, DRIVE THE SYSTEM TO A "MAXIMUM CONTINUOUS" POWER SETTING. 2 L 7 2 4F 4 F A16WE E2EA 1997010200280 19970102 00280 NM 1997 1 2 CA960809001 1 19960716 A 2431 5224871 BATTERY MONITOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE MAIN & AUXILIARY SMOKING W K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CA 760 08850047B 120063 (CAN) ON APPLYING BATTERY POWER TO AIRCRAFT THE MAIN AND AUXILIARY BATTERY TEMPERATURE MONITORS INDICATED HOT AND SMOKE STARTED TO POUR FROM THE MONITOR. THIS UNIT WAS MODIFIED IN AUGUST 1994 TO DASH 1 MOD. B STATUS, PER AMETEK SB 522487-24 -01 AND AD 96-03-09 AND DEHAVILLAND SB 8-24-53. IT HAD NOT BEEN MODIFIED TO AMETEK SB 522487-24-02 STATUS. 2 H 7 2 4T 4 T RT A13NM E20NE 1997010200281 19970102 00281 NM 1997 1 2 CA960812001 1 19960809 A 3242 SEAL DUNLOP 214664 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE RIGHT SIDE MLG LEAKING W O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA 17607 120305 (CAN) AFTER LANDING CREW ADVISED THAT RIGHT HAND WHEELS WERE SMOKING. PROBLEM FOUND TO BE FLUID ON BRAKES FROM LEAKING P ISTON SEAL. BRAKE ASSEMBLY REPLACED. PROBLEM KNOWN TO MANUFACTURER. 2 H 7 2 4T 4 T RT A13NM E20NE 1997010200282 19970102 00282 NM 1997 1 2 CA960812002 1 19960809 A 2910 82970010337 LINE DHAV DHC8 DHC8101 2809002 NM PWA PW120 PW123 NE #1 NACELLE CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 123138 (CAN) HYDRAULIC LEAK FROM #1 NACELLE. CRACKED HYDRAULIC LINE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1997010200284 19970102 00284 NE 1997 1 2 CA960812005 2 19960812 A 7530 3033716 CARBON SEAL DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE #2 ENGINE LEAKING OIL W O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA 123133 (CAN) CREW REPORTED SMOKE IN CABIN AFTER START. INSPECTION FOUND #2 ENGINE P2.5/P3 SWITCHING VALVE CARBON SEAL LEAKING O IL. P2.5/P3 SWITCHING VALVE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1997010200286 19970102 00286 SO 1997 1 2 CA960812009 1 19960802 A 6120 582855 VALVE HOUSING HAMSTD LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL HAMSTD 54H 54H60117 NE #3 PROPELLER COVER CRACKED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA 1190 500859 117226 (CAN) DURING CRUISE SMOKE BEGAN FILLING THE CABIN. FLIGHT CONTINUED AND LANDED WITHOUT INCIDENT. MAINTENANCE INVESTIGATI ON FOUND #3 PROPELLER VALVE HOUSING COVER WAS CRACKED AND LEAKING OIL. FRICTION ON SLIP RINGS GENERATED SMOKE WHICH WAS INGESTED BY THE PRESSURIZATION SYSTEM. VALVE HOUSING COVER, SLIP RING AND BRUSH BLOCK REPLACED. AIRCRAFT RETURNED TO SER VICE. 2 H 7 4 4T 4 T A1SO E282 6 C P906 1997010200287 19970102 00287 EU 1997 1 2 CA960812010 2 19960524 A 7310 451801 SWITCH SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE FUEL FILTER LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 386B (CAN) SWITCH IS LEAKING FUEL UP TO THE CANNON PLUG FOR THE BYPASS LIGHT. 1 G 7 1 3U 3 U NC H9EU E19EU 1997010200288 19970102 00288 SW 1997 1 2 CA960812011 1 19960617 A 6230 206010450113 SWASHPLATE BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL UNIBALL INCORRECT ASSY W E ENGINE SHUTDOWN F FLT CONT AFFECTED IN INSP/MAINT 1 CA 11260 3017 CAE823426 (CAN) SWASHPLATE WAS REPLACED AND TILT FRICTION CHECKED, FOUND TO BE WITHIN LIMITS. AFTER A GROUND RUN THE PILOT COMPLAI NED OF THE CYCLIC BEING EXTREMELY HARD TO MOVE WITH HYDRAULICS ON AND ALMOST IMPOSSIBLE WITH HYDRAULIC OFF. INVESTIGATIO N REVEALED THAT THE SWASHPLATE WAS INCORRECTLY SHIMMED, WITH AN UNEVEN AMOUNT OF SHIMS ON EACH SIDE CAUSING THE SWASHPLA TE TO BIND. MANUAL CALLS FOR SHIMS TO BE OF EQUAL THICKNESS ON BOTH SIDES OF UNIBALL. 1 G 7 1 3U 3 U H2SW E4CE 1997010200289 19970102 00289 SW 1997 1 2 CA960812012 1 19960611 A 6320 206040002025 TRANSMISSION BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL SEAL LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 1859 CAE821569 (CAN) AFTER A SHORT FLIGHT PILOT NOTICED MAJOR AMOUNT OF OIL COMING FROM TRANSMISSION AREA. ENGINEER DISCOVERED MAGNETIC SEAL.LEAKING. 1 G 7 1 3U 3 U H2SW E4CE 1997010200290 19970102 00290 EU 1997 1 2 CA960812013 1 19960623 A 2822 BOOST PUMP SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE GROUNDING POINT INCORRECT ATTACH W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA 836 (CAN) FUEL PRESSURE AND FUEL QUANTITY FLUCTUATIONS. PUMP WAS FOUND NOT RUNNING AND WAS SPARKING AT REMOTE FUEL DRAIN SPR ING. GROUND FOR BOOST PUMP AND FUEL QUANTITY TRANSMITTER WAS HOOKED UP CORRECTLY BUT WAS GROUNDING THROUGH MANUAL SUMP D RAIN CABLE. 1 G 7 1 3U 3 U H9EU E19EU 1997010200291 19970102 00291 SW 1997 1 2 CA960812014 1 19960626 A 2822 23003114 FUEL PUMP BELL 206 206L 1181522 SW INPUT DRIVE SEAL LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) INPUT DRIVE SEAL LEAKING BADLY. UNIT 0.3 HOURS OUT OF OVERHAUL. 1 G 7 1 3U H2SW 1997010200292 19970102 00292 SW 1997 1 2 CA960812015 1 19960717 A 6320 206040002025 TRANSMISSION BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL M/R MAKING METAL W K NONE O OTHER IN INSP/MAINT 1 CA 10898 2015 CAE821569 (CAN) TRANSMISSION MAKING METAL. 155.9 HOURS OUT OF OVERHAUL. 1 G 7 1 3U 3 U H2SW E4CE 1997010200293 19970102 00293 SW 1997 1 2 CA960812016 1 19960719 A 6420 206011810013 HUB BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL T/R ASSY UNBALANCED W K NONE O OTHER IN INSP/MAINT 1 CA 8564 1384 800631F (CAN) TAIL ROTOR INSTALLED AFTER OVERHAUL. UNABLE TO BALANCE TAIL ROTOR ASSEMBLY AFTER SEVERAL RUNS. UNIT REMOVED AND RE PLACED. 1 G 7 1 3U 3 U H2SW E4CE 1997010200294 19970102 00294 CE 1997 1 2 CA960812022 1 19960805 A 3250 07430118 STEERING ARM CESSNA 0543062206 CESSNA 172 172P 2072436 CE MCAULY 1C160 1C160DTM GL LUBE FITTING CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 7147 83617 (CAN) THE PILOT REPORTED STEERING DIFFICULTY. MAINTENANCE FOUND THE STEERING ARM ASSEMBLY CRACKED AT THE LUBRICATION FIT TING. 1 H 7 1 3O NT 3A12 5 N P910 1997010200295 19970102 00295 NE 1997 1 2 CA960826012 2 19960809 A 7200 ENGINE BOEING 727 727227 1384078 NM PWA JT8 JT8D9A 52048 NE #3 ENGINE FAILED W E A ENGINE SHUTDOWN UNSCHED LANDING O G OTHER MULTIPLE FAILURE CL CLIMB 1 CA 666191B (CAN) DURING CLIMBOUT, THE START VALVE OPEN LIGHT ILLUMINATED, #3 ENGINE OIL PRESSURE LIGHT ILLUMINATED, OIL PRESSURE ST ARTED TO DROP, FOLLOWED BY A DECAY IN N1 AND N2 WITH AN INCREASE IN EGT. ENGINE FAILURE AND SHUTDOWN DRILL AND CHECKLIST ACCOMPLISHED. AIRCRAFT RETURNED TO ITS POINT OF DEPARTURE. 2 L 7 3 4F 4 F A3WE E2EA 1997010200296 19970102 00296 EU 1997 1 2 CA960826016 1 19960727 A 2150 COCKPIT PACK FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU AIR COND CABIN SMOKE W A D UNSCHED LANDING RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 CA 9516 (CAN) ONE MINUTE AFTER TAKEOFF FLIGHT ATTENDANT INFORMED CREW OF SMOKE IN CABIN, AND LAVATORY SMOKE DETECTOR HAD SOUNDED . AIRCRAFT RETURNED TO GATE. FLIGHT TEST CONFIRMED COCKPIT PACK EMITTING SMOKE. OPERATED ON MEL. 2 L 7 2 4F 4 F RT A20EU E2EU 1997010200297 19970102 00297 EU 1997 1 2 CA960826025 1 19960731 A 4910 APU FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU AIR DIST CABIN SMOKE W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 CA 14 9516 (CAN) ON DEPARTURE SMOKE IN CABIN AND COCKPIT AND SMOKE DETECTOR IN LAVATORY WAS ACTIVATED. AIRCRAFT COMPLETED OVERWEIGH T WITHOUT INCIDENT. SECOND OCCURRENCE OF SAME PROBLEM. OVERWEIGHT LANDING CHECK REVEALED CRACK AT RETENTION ACTUATOR AND LEG. GEAR REPLACED. MAINTENANCE REPLACED COOLING TURBINE, HEAT EXCHANGER AND REFRIGERATION BYPASS UNIT. STILL SMOKE AND OIL SMELL PRESENT IN CABIN. APU REPLACED. NO MORE SMOKE IN CABIN. 2 L 7 2 4F 4 F RT A20EU E2EU 1997010200298 19970102 00298 NE 1997 1 2 CA960826032 2 19960815 A 8500 ENGINE CURTIS C46 C46DAIRLIFT SO PWA R2800 R280075M1 52026 NE HAMSTD 23E 23E50 NE #2 POSITION FAILED W A E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CL CLIMB 1 CA 95 FP043144 MM76883 (CAN) THE AIRCRAFT WAS CLIMBING THROUGH 1900 FEET WHEN THE #2 ENGINE OIL PRESSURE BEGAN A RAPID DECREASE, ACCOMPANIED BY AN EQUALLY RAPID INCREASE IN OIL TEMPERATURE. THE ENGINE WAS SHUTDOWN AND THE AIRCRAFT RETURNED TO ITS POINT OF DEPARTU RE. THE #2 ENGINE WAS REPLACED AND IS BEING PREPARED FOR RETURN FOR OVERHAUL. 2 L 7 2 4R 4 R 3A2 5E8 6 C P603 1997010200299 19970102 00299 EA 1997 1 2 CA960826064 2 19960808 A 7200 ENGINE DHAV DHC6 DHC6300 EA PWA PT6 PT6A27 52043 EA #1 POSITION OVER TEMPERATURE W E ENGINE SHUTDOWN E M VIBRATION/BUFFET OVER TEMP AP APPROACH 1 CA 3245 PCE42455 (CAN) #1 ENGINE GAVE A COUPLE OF "POPS" FOLLOWED BY A LOSS OF TORQUE AND THE ITT ROSE TO BETWEEN 950 AND 1000 DEGREES FO R 25-30 SECONDS. THE #1 ENGINE WAS SHUTDOWN FOLLOWED BY A SAFE LANDING. 1 H 7 2 3T 4 T A9EA E4EA 1997010200301 19970102 00301 NM 1997 1 2 CA960826071 1 19960810 A 7120 8DK1763001 STRUT ASSEMBLY DHAV 87110028005 DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE R/H ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 16789 8169 055AO 123045 (CAN) INBOARD REAR MOUNT STRUT ON RIGHT HAND ENGINE FOUND CRACKED. CRACK IS APPROXIMATELY 1 INCH LONG AND LOCATED AT CEN TRE INBOARD WELD SPOT. STRUT ASSEMBLY REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1997010200302 19970102 00302 NE 1997 1 2 CA960826102 1 19960814 A 6320 AN104149 BOLT SKRSKY S16352000002 SKRSKY S58T S58ET 8141803 NE PWA PT6T PT6T3 52045 EA M/R GR BOX CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 848 848 S58E20582137 CPPS60754 (CAN) WHILE COMPLYING WITH AD 95-26-08, MPI INSPECTION OF THE MAIN ROTOR SHAFT, THESE BOLTS WERE ALSO MPI'D REVEALING CR ACKS UNDER THE HEAD IN 4 OUT OF 5 BOLTS. SUGGEST MPI INSPECTION OF THE BOLTS BE DONE TO COINCIDE WITH THE SHAFT INSPECIT ON. 2 G 7 2 4U 4 U 1H11 E22EA 1997010200304 19970102 00304 NE 1997 1 2 CA960827006 2 19960630 A 8520 32154A ROD PIN DHAV DHC3 DHC3 2800202 EA PWA R1340 R1340AN2 52016 NE #1 CYLINDER BROKEN LOCKS W A K NONE O OTHER IN INSP/MAINT 1 CA 980 24826 (CAN) AFTER ENGINE WARM-UP PRIOR TO COMPRESSION CHECK, WITH THE FRONT SPARK PLUGS REMOVED, THE PROP WAS SPUN TO LOCATE T OP DEAD CENTRE (TDC) ON #1 CYLINDER. THE PROP SUDDENLY STOPPED. REMOVAL OF THE #1 CYLINDER REVEALED THE CONNECTING ROD P IN HAD SLID OUT ALLOWING THE CONNECTING ROD TO SLIDE FREELY FROM THE CRANKSHAFT. THE LINK PIN WOULD JAM IN THE CRANKSHAF T JOURNAL WITH 90 DEGREE MOVEMENT EITHER WAY. THE LOCK BOLT PIN P/N 280, AND LOCK P/N 11919 WERE MISSING FROM NOS.1, 2 & 9 CYLINDERS. 1 H 7 1 3R 3 R A815 5E2 1997010200305 19970102 00305 NE 1997 1 2 CA960910004 2 19960829 A 8500 ACCESSORY GEARBX DOUG DC3 DC3CS1C3G 3021458 WP PWA R1830 R183092 52020 NE #1 ENGINE DECOUPLED W E ENGINE SHUTDOWN Y ENGINE STOPPAGE CR CRUISE 1 CA 1250 11593 (CAN) #1 ENGINE SUFFERED COMPLETE POWER LOSS WITHOUT WARNING. PROPELLER WAS FEATHERED AND AIRCRAFT RETURNED TO BASE. INV ESTIGATION REVEALED THE ENGINE ACCESSORY CASE HAD DECOUPLED FROM THE POWER SECTION DRIVE. MAGNETOS AND GENERATOR REMAIN STATIONARY WHEN THE ENGINE IS MANUALLY ROTATED. 2 L 7 2 4R 4 R A669 5E4 1997010200306 19970102 00306 NE 1997 1 2 CA960910016 2 19960730 A 7230 ENGINE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE L/H ENGINE STALLED W A D E RETURN TO BLOCK ENGINE SHUTDOWN M R OVER TEMP PARTIAL RPM/PWR LOSS CL CLIMB 1 CA 807184 (CAN) AFTER DOING A REDUCED THRUST TAKEOFF, THE CREW SELECTED CLIMB POWER. THERE WAS AN ABRUPT LOSS OF THRUST AND A LOUD COMPRESSOR STALL AT ABOUT 2500 FEET. LEFT ENGINE TEMPERATURE EXCEEDED RED LINE FOR 30 TO 40 SECONDS AND ENGINE WAS SHUT DOWN. LEFT HAND ENGINE WAS CHANGED DUE TO COMPRESSOR STALL. 2 L 7 2 4F 4 F RT A21EA E15NE 1997010200308 19970102 00308 NM 1997 1 2 CA960916021 1 19960829 A 5315 85311176 WEB DHAV DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE FLIGHT DECK CRACKED W K NONE O OTHER LD LANDING 1 CA 20298 120786 (CAN) FLIGHT DECK WEB BRACKET CRACKED. WEB AND SKIN REPLACED IN SAME AREA. RH 8-53-2273 APPLIES. SUBMITTER SUGGESTS THAT AIRCRAFT IN THIS AREA IS OF POOR DESIGN AS THERE HAVE BEEN MANY RD'S DONE IN THE PAST. 2 H 7 2 4T 4 T RT A13NM E20NE 1997010200309 19970102 00309 NE 1997 1 2 CA960919006 2 19960906 A 7200 ENGINE BELL 205 205A1 1181414 SW LYC T53 T5313B 41549 NE TURBINE FAILED W O OTHER O OTHER IN INSP/MAINT 1 CA LEO7186X (CAN) THE HELICOPTER WAS ON THE INITIAL GROUND RUN AFTER A 1000 HOUR INSPECTION. THE AIRCRAFT WAS RUNNING IN FLIGHT IDLE FOR APPROXIMATELY 10 MINUTES AND ALL PARAMETERS WERE NORMAL. THE PILOT ACCELERATED THE ENGINE TO MAX POWER TURBINE (N2) SPEED TO ESTABLISH THE MAX N2 SPEED AVAILABLE IN ORDER TO ADJUST THE UPPER GOVERNOR LIMIT. BETWEEN 100-101 PERCENT THE FOLLOWING OCCURRED: AN AUDIBLE "CLANK" FOLLOWED BY A "WHOOSH"; SEVERAL ENGINE RELATED FRAGMENTS EXITED AFT THROUGH THE T AILPIPE; THE PILOT OBSERVED THE N2 SPEED INDICTION DROP OFF RAPIDLY (NEEDLE SPLIT) AND IMMEDIATELY ROLLED THE THROTTLE O FF; THE ENGINE SPOOLED DOWN AND STOPPED. 1 G 7 1 4U 4 U H1SW E17EA 1997010200310 19970102 00310 NE 1997 1 2 CA960923008 2 19960828 A 7210 TOWER SHAFT DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE #1 ENGINE FAILED W A D UNSCHED LANDING RETURN TO BLOCK E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 CA 12526 123052 (CAN) AFTER TAKEOFF #1 ENGINE TORQUE STARTED TO CLIMB EXCEEDING 130 PERCENT. POWER RETARDED AND TORQUED FLUCTUATED FROM 40-100 PERCENT. ENGINE SELECTED TO MANUAL AND TORQUE DECREASED BUT DID NOT CEASE. AIRCRAFT RETURNED TO BASE. POST FLIGHT INSPECTION FOUND ENGINE NH WOULD JUMP TO 44 PERCENT WHEN A START WAS ATTEMPTED AND THE PT SHAFT WOULD NOT ROTATE WHEN T HE STARTER WAS SPINNING. SUSPECT TOWER SHAFT OR TORQUE SHAFT SHEARED OR DAMAGED. ENGINE REPLACED. STRIP REPORT TO FOLLOW . 2 H 7 2 4T 4 T RT A13NM E20NE 1997010200311 19970102 00311 EA 1997 1 2 CA960924029 1 19960915 A 5740 85320053 FITTINGS DHAV DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE WING TO FUSELAGE CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA 11887 123018 (CAN) DURING REMOVAL OF CENTRE SECONDARY FLAP DRIVE FLEX SHAFT, FOUND CHAFING DAMAGE TO THE TOP EXTERNAL SURFACE OF BOTH AFT STRINGER #3 BATHTUB FITTINGS (WING TO FUSELAGE), AFT OF REAR SPAR. THE DAMAGE WAS BLENDED OUT AS PER TEMPORARY REPA IR RD. 2 H 7 2 4T 4 T RT A13NM E20NE 1997010200312 19970102 00312 EA 1997 1 2 CA960927001 2 19960810 A 7322 105253 CARBURETOR MARVELSCHEB 4A6 CESSNA 172 172RG 2072438 CE LYC O360 O360F1A6 41514 EA MCAULY 2D34C B2D34C220 GL FLOAT ASSEMBLY ABNORMAL WEAR W A K NONE E VIBRATION/BUFFET IN INSP/MAINT 1 CA 595 DL41197 E2991136A 805428 (CAN) PILOT EXPERIENCED STARTING PROBLEMS. INVESTIGATION OF SNAG WAS INCONCLUSIVE. INSPECTION OF CARBURETOR INDICATED WE AR ON THE FLOAT ASSEMBLY, WHICH IS UNCOMMON WITH THE AMOUNT OF TIME AND USAGE OF THIS UNIT. FURTHER INVESTIGATION IS UND ERWAY. 1 H 7 1 3O 3 O 3A17 E286 5 C P7EA 1997010200313 19970102 00313 WP 1997 1 2 CA961001006 2 19960911 A 7250 TURBINE SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE3313UW 01514 WP L/H ENGINE DAMAGED W A E ENGINE SHUTDOWN Y ENGINE STOPPAGE CR CRUISE 1 CA 14343 03453 (CAN) ON APPROACH, ENGINE SHUT DOWN AND THE PROPELLER FEATHERED. THE LANDING WAS ACCOMPLISHED WITHOUT INCIDENT. THE FLIG HT CREW CHECKED THE L/H ENGINE AND FOUND THAT THE PROPELLER COULD NOT BE TURNED BY HAND. MAINTENANCE DISPATCHED AND ENGI NE REPLACED. FIELD REPRESENTATIVE SUPERVISED TEAR DOWN AND THE FOLLOWING WAS FOUND; FOD AND HEAT DAMAGE TO #1 STATOR, #1 T WHEEL SEVERE BLADE DAMAGE, FIRST STAGE T WHEEL SHROUD DAMAGED AND TWO SEGMENTS BROKEN, #2 AND #3 T WHEELS SEVERE FOD DAMAGE. DETAILED ANALYSIS REPORT TO FOLLOW. 2 L 7 2 4T 4 T RT A8SW E4WE 1997010200314 19970102 00314 SO 1997 1 2 CA961003001 1 19960628 A 3220 BRACKET PIPER PIPER PA34 PA34200 7103405 SO LYC O360 LIO360C1E6 41515 EA OVER CENTRE BRKT TORN W K NONE O OTHER LD LANDING 1 CA 99 99 L91467A (CAN) NOSE GEAR RETRACTED ON LANDING. AWAITING FURTHER INFO FROM FIELD. 1 L 7 2 3O 3 O A7SO 1E10 1997010200317 19970102 00317 EU 1997 1 2 CA961021008 1 19961007 A 3220 200429005 GEAR ASSY FOKKER F28 F28MK1000 4990808 EU NLG MALFUNCTION W K NONE J WARNING INDICATION AP APPROACH 1 CA (CAN) NOSE LANDING GEAR REPLACED DUE TO INTERNAL LEAK INTO STEERING RACK FROM #1 SYSTEM. RETURNED TO SERVICE. ON NEXT FL IGHT NOSE GEAR WOULD NOT LOCK DOWN, NOSE LANDING GEAR PRESSURE REDUCING VALVE REPLACED. ON FOURTH FLIGHT, SAME SNAG. TWO WAY RESTRICTOR VALVE REPLACED IN ACTUATOR LINE. NEXT DAY, ON APPROACH GEAR SELECTED DOWN NO NOSE LANDING GEAR GREEN LIG HT, NLG RECYCLED OK. MAINTENANCE REPLACED NOSE LANDING GEAR AND TORQUE LINKS AND PINS, GREASED. SERVICEABLE. 2 L 7 2 4F RT A20EU 1997010200318 19970102 00318 WP 1997 1 2 TWAA9614102 1 19961110 A 5330 SKIN DOUG DC9 DC951 3022051 WP BS 670 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 408EA 47693 STL - DURING OP-15, FOUND PULLED RIVET HEAD AND SKIN PILLOWED, LONGERONS 29L, 30, AND 29R, STA 670. REPLACED SKIN AND I NNER DOUBLER PER SRM 53-04, FIGURE 43, SHEET 4; SRM 51-00, AND TWA STANDARD PRACTICES. AIRCRAFT TOTAL TIME: 46,296 HOU RS; 43,121 CYCLES. (X) 2 L 7 2 4F RT A6WE 1997010200319 19970102 00319 WP 1997 1 2 TWAA9614103 1 19961112 A 5320 DOUBLER DOUG DC9 DC982 3022082 WP BS 678 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 956U 49701 MCI - DURING OP-16, FOUND CORROSION ON ANTENNA MOUNT DOUBLER FORWARD SIDE BETWEEN LONGERON 20L AND LONGERON 29L, FS 2678 . REMOVED AND REPLACED DOUBLER PER SRM 51-01 AND TWA STANDARD PRACTICES. AIRCRAFT TOTAL TIME: 26,489 HOURS; 13,301 CY CLES. (X) 2 L 7 2 4F A6WE 1997010200320 19970102 00320 WP 1997 1 2 TWAA9614104 1 19961112 A 5320 ANGLE DOUG DC9 DC982 3022082 WP PAX DOORWAY BENT A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 956U 49701 MCI - DURING OP-16, FOUND FORWARD DOORWAY LOWER MOUNT ANGLE BENT AND CORRODED. REPAIRED PER SRM 51-10-3, AND TWA STANDA RD PRACTICES. AIRCRAFT TOTAL TIME: 26,489 HOURS: 13,301 CYCLES. (X) 2 L 7 2 4F A6WE 1997010200321 19970102 00321 WP 1997 1 2 TWAA9614105 1 19961112 A 5347 SEAT TRACKS DOUG DC9 DC982 3022082 WP BS 1121 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 956U 49701 MCI - DURING OP-16, FOUND CORROSION ON SHORT SEAT TRACK, FS 1121 FORWARD. REMOVED CORROSION PER SRM 51-10-3. AIRCRAFT TOTAL TIME: 26,489 HOURS; 13,301 CYCLES. (X) 2 L 7 2 4F A6WE 1997010200322 19970102 00322 WP 1997 1 2 TWAA9614106 1 19961112 A 5320 FORMER DOUG DC9 DC982 3022082 WP BS 1271 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 956U 49701 MCI - DURING OP-16, FOUND CORROSION ON AFT CARGO FORMER RING, LONGERON 29R TO LONGERON 28L, STA 1271. REMOVED CORROSION PER SRM 51-3, AND REPAIRED FORMER PER SRM 53-03, PAGE 4E. AIRCRAFT TOTAL TIME: 26,489 HOURS; 13,301 CYCLES. (X) 2 L 7 2 4F A6WE 1997010200323 19970102 00323 NM 1997 1 2 TWAA9614201 1 19961119 A 3310 65B4752230 TEST BOX BOEING 747 747257B 1384853 NM COCKPIT FAILED A TWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 303TW 20116 JFK - FLT 885 - DURING CRUISE, HAD SMOKE AND ELECTRICAL ODOR FROM ENGINEER PANEL. TURNED OFF WINDOW HEAT. FOUND OVERHE AT INDICATION IN MASTER DIM AND TEST BOX, MFG P/N 65B47522-30. REPLACED MASTER DIM AND TEST BOX, CHECKED WINDOW HEAT WI RING. MASTER DIM AND TEST BOX AND WINDOW HEAT OPERATION CHECKED NORMAL. CHECK C - 4-16-96 - MCI. (X) 2 L 7 4 4F A20WE 1997010200324 19970102 00324 WP 1997 1 2 TWAA9614202 1 19961014 A 5753 HINGE DOUG DC9 DC951 3022051 WP TE FLAPS CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 405EA 47688 STL - DURING OP-15, FOUND .3750 INCH CRACK AT FIRST HOLE OF INBOARD FLAP HINGE AT AFT EDGE OF LOWER CAP. INSTALLED REPA IR PER SB A57-146 AND ARA 10569. AIRCRAFT TOTAL TIME: 45,363 HOURS; 42,011 CYCLES. (X) 2 L 7 2 4F RT A6WE 1997010200325 19970102 00325 NM 1997 1 2 TWAA9614301 1 19961120 A 3350 363673 LIGHT BOEING 747 747156 1384884 NM CABIN MOISTURE CONTAM A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 133TW 19957 STL - FLT 1 - DURING PRE-FLIGHT, FOUND EGRESS LIGHTS INOPERATIVE BETWEEN 'B' AND 'C' GALLEYS. FOUND MOISTURE IN EGRESS LIGHT TRACK, MFG PN 36367-3. CLEANED MOISTURE FROM LIGHT TRACK. EGRESS LIGHT OPERATION THEN CHECKED NORMAL. CHECK C-2 - 2-5-96 - JFK. (X) 2 L 7 4 4F A20WE 1997010200326 19970102 00326 NM 1997 1 2 TWAA9614303 1 19961120 A 7931 21SN04149 OIL PRESS SW BOEING 747 747156 1384884 NM NR 1 ENGINE LEAKING A TWAA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 05 134TW 19958 STL - FLT 845 - DURING CRUISE, SHUT DOWN NR 1 ENGINE, SN 4183, DUE TO DECREASING OIL QUANTITY. FOUND OIL PRESSURE DIFFE RENTIAL SWITCH, MFG PN 21SN04-149, CAP LEAKING. RE-TORQUED DIFFERENTIAL PRESSURE SWITCH CAP. SERVICED ENGINE OIL SYSTE M. ENGINE OPERATION AND OIL QUANTITY SYSTEM OPERATION CHECKED NORMAL. ENGINE TOTAL TIME: 79,296 HOURS; 13,809 CYCLES. CHECK C - 2-5-96 - JFK. (X) 2 L 7 4 4F A20WE 1997010200327 19970102 00327 WP 1997 1 2 TWAA9614302 1 19961120 A 3350 601179LB BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 932L 47669 STL - FLT 567 - DURING PRE-FLIGHT, FOUND EGRESS LIGHTS INOPERATIVE. FOUND BATTERY PACK, MFG PN 60-117-9LB, WITH LOW VOL TAGE. REPLACED BATTERY PACK AND POWER SUPPLY. EGRESS LIGHT SYSTEM OPERATION THEN CHECKED NORMAL. CHECK C - 9-3-95 - S TL. (X) 2 L 7 2 4F A6WE 1997010200328 19970102 00328 WP 1997 1 2 TWAA9614304 1 19961120 A 3350 58223 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 931L 47173 STL - FLT 608 - DURING PRE-FLIGHT, FOUND EGRESS LIGHTS IN FIRST CLASS INOPERATIVE. FOUND POWER SUPPLY, MFG PN 5822-3, M ALFUNCTIONING. REPLACED POWER SUPPLY AND EGRESS LIGHT SYSTEM OPERATION CHECKED NORMAL. CHECK C - 7-25-96 - STL. (X) 2 L 7 2 4F A6WE 1997010200329 19970102 00329 WP 1997 1 2 TWAA9614401 1 19961121 A 3350 58222 POWER SUPPLY DOUG DC9 DC934 302207E WP CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 936L 47711 STL - FLT 459 - DURING PRE-FLIGHT, FOUND EGRESS LIGHTS INOPERATIVE AT SEAT ROWS 10 TO 15. FOUND MALFUNCTIONING POWER SU PPLY, MFG PN 5822-2. REPLACED POWER SUPPLY. EGRESS LIGHTS OPERATION THEN CHECKED NORMAL. CHECK C - 4-10-96 - STL. (X ) 2 L 7 2 4F RT A6WE 1997010200330 19970102 00330 NE 1997 1 2 TWAA9614402 2 19961122 A 7230 BLADE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE NR 1 ENGINE DAMAGED A TWAA O OTHER R PARTIAL RPM/PWR LOSS CL CLIMB 1 CE 05 EICIW 49785 STL - FLT 341 - DURING CLIMB, SHUT DOWN NR 1 ENGINE, SN 1421, DUE TO COMPRESSOR STALL AND OIL QUANTITY WENT TO ZERO. FO UND TURBINE DAMAGE. REPLACED NR 1 ENGINE. ENGINE OPERATION THEN CHECKED NORMAL. ENGINE TOTAL TIME: 13,723 HOURS; 11, 055 CYCLES. INVESTIGATION OF NR 1 ENGINE, SN 1421, COMPRESSOR STALL AND OIL QUANTITY DROP TO ZERO, FOUND THAT AN LPT 3 VANE WAS FITTED WITH INSUFFICIENT TILT AND CHAFED THROUGH THE REAR WALL OF THE INNER AIRSEAL AND RUBBED ON THE STAGE 3 B LADE. ENGINE S/N 1421 WAS REPAIRED AND RETURNED TO SERVICE. (X) 2 L 7 2 4F 4 F RT A6WE E9NE 1997010200331 19970102 00331 WP 1997 1 2 TWAA9614501 1 19961125 A 3230 BOLT DOUG DC9 DC982 3022082 WP GROUND SHIFT ROD MISSING A TWAA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 903TW 49154 STL - FLT 482 - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, LANDING GEAR HANDLE WOULD NOT MOVE. USED HANDBOOK PROCED URES TO RETRACT LANDING GEAR. FOUND BOLT MISSING IN GROUND SHIFT ROD TO QUADRANT. INSTALLED NEW BOLT IN GROUND SHIFT R OD. LANDING GEAR OPERATION THEN CHECKED NORMAL. CHECK C - 9-21-96 - MCI. (X) 2 L 7 2 4F A6WE 1997010200332 19970102 00332 WP 1997 1 2 TWAA9614601 1 19961126 A 3350 58222 POWER SUPPLY DOUG DC9 DC915 3022036 WP CABIN INOPERATIVE A TWAA K NONE O OTHER CR CRUISE 1 CE 05 970Z 45772 STL - FLT 209 - DURING CRUISE, EGRESS LIGHTS AT SEAT ROWS 10 TO 14 ILLUMINATED. FOUND MALFUNCTIONING POWER SUPPLY, MFG PN 5822-2. REPLACED POWER SUPPLY. EGRESS L IGHT SYSTEM OPERATION CHECKED NORMAL. CHECK C- 6-2-96 - STL. (X) 2 L 7 2 4F A6WE 1997010200333 19970102 00333 NM 1997 1 2 TWAA9614602 1 19961126 A 2530 916583 CONTROLLER BOEING 767 767231 1385131 NM GALLEY FAILED A TWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 601TW 22564 STL - FLT 104 - DURING CRUISE, AISLE WARMER CART EMITTED ELECTRICAL ODOR AND SMOKE. FOUND FAULTY POWER CONTROLLER, MFG PN 91658-3. REPLACED WARMER CART CONTROLLER. WARMER CART OPERATION THEN CHECKED NORMAL. CHECK C-1C - 10-2-96 - LAX. ( X) 2 L 7 2 4F RT A1NM 1997010200334 19970102 00334 WP 1997 1 2 TWAA9614701 1 19961127 A 3350 32890 STRIP DOUG DC9 DC982 3022082 WP CABIN BROKEN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 915TW 49186 STL - FLT 469 - DURING PRE-FLIGHT, FOUND SECTION OF FIRST CLASS EGRESS LIGHTS INOPERATIVE. FOUND BROKEN FLOOR STRIP, MF G PN 32890. REPLACED FLOOR STRIP. EGRESS LIGHT OPERATION THEN CHECKED NORMAL. CHECK C - 4-23-96 - MCI. (X) 2 L 7 2 4F A6WE 1997010200335 19970102 00335 WP 1997 1 2 TWAA9614801 1 19961129 A 3231 39265281 CONTROL CABLE DOUG DC9 DC951 3022051 WP NLG DOOR BROKEN A TWAA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 411EA 47732 STL - FLT 627 - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, HAD LOUD NOISE FROM NOSE LANDING GEAR AND UNSAFE LIGHT RE MAINED ILLUMINATED. FOUND RIGHT NOSE LANDING GEAR DOOR STOP CABLE BROKEN, MFG PN 3926528-1. REPLACED RIGHT NOSE LANDIN G GEAR DOOR STOP CABLE. NOSE LANDING GEAR AND DOOR OPERATION THEN CHECKED NORMAL. CHECK C - 6-2-96 - STL. (X) 2 L 7 2 4F RT A6WE 1997010200336 19970102 00336 NE 1997 1 2 TWAA9614802 2 19961129 A 7260 746450001 GEARBOX BOEING 747 747131 1384881 NM PWA JT9 JT9D7A 52054 NE NR 2 ENGINE CRACKED A TWAA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 05 93108 19674 JFK - FLT 6751 - DURING CRUISE, SHUT DOWN NR 2 ENGINE, SN 4199, DUE TO LOSS OF OIL. FOUND ACCESSORY GEARBOX, MFG PN 746 450-001, CRACKED AT HYDRAULIC PUMP DRIVE. REPLACED ACCESSORY GEARBOX THEN ENGINE OPERATION AND LEAK CHECKS NORMAL. ENG INE TOTAL TIME: 72,518 HOURS; 14,326 CYCLES. CHECK C - 1-15-96 - MCI. (X) 2 L 7 4 4F 4 F A20WE E20EA 1997010200337 19970102 00337 WP 1997 1 2 TWAA9614803 1 19961129 A 3230 RETRACT MECH DOUG DC9 DC931 3022065 WP LANDING GEAR LACK OF LUBE A TWAA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 985Z 47491 JFK - FLT 214 - AFTER TAKEOFF, LANDING GEAR SELECTOR WAS CYCLED TO GET LANDING GEAR RETRACTED AND ON LANDING GEAR EXTENS ION DURING APPROACH, LANDING GEAR WAS SLOW TO EXTEND AND LOCK IN DOWN POSITION. LUBRICATED ALL LANDING GEARS. LANDING GEAR OPERATION THEN CHECKED NORMAL. CHECK C - 6-14-96 - STL. (X) 2 L 7 2 4F A6WE 1997010200338 19970102 00338 WP 1997 1 2 TWAA9614901 1 19961130 A 3230 LINKAGE DOUG DC9 DC931 3022065 WP LT MLG LACK OF LUBE A TWAA O OTHER O OTHER AP APPROACH 1 CE 05 983Z 47411 STL - FLT 212 - DURING APROACH WHEN LANDING GEAR WAS EXTENDED, LEFT MLG DOWN AND LOCKED LIGHT WAS SLOW TO ILLUMINATE. L UBRICATED SWITCH AND LINKAGE. LANDING GEAR INDICATION THEN CHECKED NORMAL. CHECK C - 8-1-96 - STL. (X) 2 L 7 2 4F A6WE 1997010200339 19970102 00339 NM 1997 1 2 TWAA9614902 1 19961130 A 2410 652673831 CSD DUCT BOEING 727 727231 1384079 NM NR 2 ENGINE RUPTURED A TWAA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 54353 21985 CUN - FLT 68 - DURING CLIMB NR 2 ENGINE, SN 3984, FIREWARNING ILLUMINATED. REDUCED POWER. FOUND CSD EJECTOR DUCT, MFG PN 65-26738-31, RUPTURED. REPLACED CSD EJECTOR DUCT. ENGINE OPERATION AND LEAK CHECKS NORMAL. CHECK C-1 - 5-20-96 - J FK. (X) 2 L 7 3 4F A3WE 1997010200340 19970102 00340 NM 1997 1 2 TWAA9614903 1 19961130 A 3230 RETRACT MECH BOEING 727 727231 1384079 NM RT MLG LACK OF LUBE A TWAA O OTHER P NO WARNING INDICATION AP APPROACH 1 CE 05 54342 21629 PHX - FLT 169 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, RT MLG DOWN AND LOCKED LIGHT DID NOT ILLUMINATE. PERFOR MED MANUAL EXTENSION OF RT MLG. LUBRICATED LANDING GEAR, DOWNLOCK, AND TRUNNION BEARINGS. LANDING GEAR OPERATION CHECK ED NORMAL. CHECK C-2 - 3-15-96 - JFK. (X) 2 L 7 3 4F A3WE 1997010200341 19970102 00341 NM 1997 1 2 TWAA9614904 1 19961201 A 3610 652244419 DUCT BOEING 727 727231 1384079 NM NR 1 ENGINE RUPTURED A TWAA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 52312 19831 STL - FLT 123 - DURING CLIMB NR 1 ENGINE, SN 4001, FIREWARNING ILLLUMINATED. REDUCED POWER. FOUND 8TH STAGE DUCT, MFG PN 65-22444-19, RUPTURED. REPLACED 8TH STAGE DUCT. ENGINE OPERATION AND LEAK CHECKS NORMAL. CHECK C-4 - 3-29-96 - JFK. (X) 2 L 7 3 4F A3WE 1997010200342 19970102 00342 WP 1997 1 2 TWAA9614905 1 19961202 A 3350 58222 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN FAILED A TWAA K NONE O OTHER CR CRUISE 1 CE 05 915TW 49186 STL - FLT 263 - DURING CRUISE EGRESS LIGHTS FLASHED ON AND OFF. FOUND FAULTY FIRST CLASS POWER SUPPLY, MFG PN 5822-2. R EPLACED POWER SUPPLY. EGRESS LIGHT SYSTEM OPERATION THEN CHECKED NORMAL. CHECK C - 4-23-96 - MCI. (X) 2 L 7 2 4F A6WE 1997010200348 19970102 00348 SW 1997 1 2 96ZZZX6187 1 19961125 A 6310 206040204001 PLATE 206040270177 BELL 206 206L 1181522 SW FREEWHEEL MAKING METAL A NYBA K NONE O OTHER IN INSP/MAINT 1 EA 11 122NH 1628 1043 45101 DURING NORMAL OPERATION IT WAS NOTED THAT THE FREE WHEELING UNIT WAS DETERMINED TO BE GENERATING METAL. THIS UNIT WAS M ODIFIED FROM A -3 TO -117 BY TB206L-95-177 DURING LAST OVERHAUL. DURING TEAR DOWN INSPECTION IT WAS NOTED THAT PLATE W AS FOUND LOOSE AND WAS SPINNING, WHICH CAUSED THE METAL GENERATION. REPLACED FREE WHEELING UNIT IAW BELL 206L MM PAR 66 -159-66-163A. 1 G 7 1 3U H2SW 1997010200349 19970102 00349 NM 1997 1 2 TWAA9614502 1 19961125 A 2170 22D10 COALESCER BAG BOEING 727 727231 1384079 NM RIGHT DIRTY A TWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 05 54329 20307 STL - FLT 169 - AFTER TAKEOFF, HAD STRONG ODOR IN CABIN. TURNED OFF RIGHT AIR CONDITIONING PACK AND ODOR SUBSIDED. FOUN D COALESCER, MFG PN 22D10, CONTAMINATED WITH DEICER FLUID. REPLACED BOTH COALESCER ELEMENTS. AIR CONDITIONING SYSTEM O PERATION THEN CHECKED NORMAL. CHECK C-4 - 5-2-96 - MCI. (X) 2 L 7 3 4F A3WE 1997010200350 19970102 00350 NM 1997 1 2 CALA9601877 1 19961224 A 3320 7157 BALLAST BOEING 737 7373T0 1384582 NM CABIN BURNT A CALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 09 69311 23362 SMOKE WAS SEEN COMING FROM LIGHT AREA OF FIRST CLASS CLOSET WHILE AIRCRAFT WAS AT GATE AFTER PASSENGERS WERE DEPLANED. T HE SMOKE STOPPED AFTER EXTERNAL POWER WAS REMOVED FROM BUS AND BATTERY WAS TURNED OFF. MAINTENANCE FOUND THE FORWARD GA LLEY WORK LIGHT BALLAST INSIDE COAT CLOSET AT FAULT. THE BALLAST WAS REMOVED AND REPLACED, NO OTHER DISCREPANCIES WERE NOTED. 2 L 7 2 4F RT A16WE 1997010200351 19970102 00351 WP 1997 1 2 CALA9601878 1 19961226 A 3350 EMBS1392 CHARGER DOUG DC10 DC1030 3023501 WP CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 68060 39937 4770 47850 THE EMERGENCY LIGHT SYSTEM FAILED TO TEST PROPERLY. THE MID-SECTION POWER SUPPLY AND BATTERY WERE REMOVED AND REPLACED. 2 L 7 3 4F A22WE 1997010200352 19970102 00352 WP 1997 1 2 CALA9601879 1 19961126 A 5320 ANGLE DOUG DC9 DC932 3022066 WP E/E COMPT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17531 45847 INSPECTION FOUND A 1.75 INCH CRACK IN FORWARD E AND E COMPARTMENT ATTACH ANGLE. THE ANGLE WAS REMOVED AND A NEW ANGLE W AS FABRICATED AND INSTALLED IAW SRM 51-30-02. 2 L 7 2 4F A6WE 1997010200353 19970102 00353 WP 1997 1 2 CALA9601880 1 19961124 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BAGGAGE COMPT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17531 45847 INSPECTION FOUND A .25 INCH CRACK IN RADIUS OF ANGLE IN FORWARD BAGGAGE BIN AT DOOR UPPER AFT CORNER. THE ANGLE WAS REM OVED AND REPLACED IAW SRM 51-30-3. 2 L 7 2 4F A6WE 1997010200354 19970102 00354 WP 1997 1 2 CALA9601881 1 19961124 A 5230 FITTINGS DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17531 45847 INSPECTION FOUND A .5 INCH CRACK IN EACH OF THREE END FITTINGS AT AFT CARGO DOOR BEAM NR 1, NR 2 AND NR 4. THE FITTINGS WERE REMOVED AND REPLACED IAW SRM 51-30-00. 2 L 7 2 4F A6WE 1997010200355 19970102 00355 WP 1997 1 2 CALA9601882 1 19961206 A 5712 RIB DOUG DC9 DC932 3022066 WP RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17531 45847 INSPECTION FOUND A .5 INCH CRACK AT LOWER ATTACH BOLT HOLE IN INBOARD RIB OF RT WING NR 2 SLAT DRIVE TRACK. THE RIB WAS REPLACED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 1997010200356 19970102 00356 WP 1997 1 2 9626929952 1 19961225 A 3231 CONTROL CABLE DOUG DC9 DC931 3022065 WP LT MLG DOOR BROKEN A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 916RW 47144 LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER RETRACTION. FLIGHT RETURNED TO MSP, LANDED WITHOUT INCIDENT. MAI NTENANCE REPLACED SHEARED RIVETS ON LEFT MAIN GEAR DOOR LATCH MECHANISM AND BROKEN DOOR SEQUENCE CABLE, OPERATIONAL CHEC K NORMAL. 2 L 7 2 4F A6WE 1997010200357 19970102 00357 WP 1997 1 2 9626939941 1 19961223 A 3233 ACTUATOR DOUG DC9 DC932 3022066 WP NLG MALFUNCTIONED A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 3324L 47103 DURING APPROACH, NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. RECYCLED GEAR SIX TIMES BEFORE NORMAL INDICATIONS WERE ACHIEVED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NOSE GEAR ACTUATING CYLINDER AND DOWNLOCK SWITCH, OPERATIONAL CHECK NORMAL ON GEAR SWING. 2 L 7 2 4F A6WE 1997010200358 19970102 00358 WP 1997 1 2 9626949865 1 19961225 A 3230 RETRACT MECH DOUG DC9 DC951 3022051 WP NLG MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 774NC 47776 AFTER TAKEOFF, NOSE GEAR WOULD NOT RETRACT, GROUND SHIFT DID OCCUR. PERFORMED COCKPIT OPERATING MANUAL PROCEDURE AND RE TURNED TO MSP. GEAR EXTENDED NORMALLY, FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE CYCLED GEAR THREE TIMES WITH NO PRO BLEM. SERVICED GEAR AND RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 1997010200359 19970102 00359 WP 1997 1 2 9626959995 1 19961225 A 3350 60030451 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8978E 47327 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATI ONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1997010200360 19970102 00360 WP 1997 1 2 9626969969 1 19961225 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9333 47246 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN PACK, OPERA TIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1997010200361 19970102 00361 WP 1997 1 2 9626979968 1 19961224 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9332 47264 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS AT ROWS 5, 7 AND 9 INOPERATIVE. REPLACED BATTERIES IN PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1997010200362 19970102 00362 WP 1997 1 2 9626989938 1 19961224 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN MALFUNCTIONED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 1798U 47369 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1997010200363 19970102 00363 WP 1997 1 2 9626999140 1 19961224 A 3260 INDICATION DOUG DC9 DC914 3022034 WP NLG MALFUNCTIONED A NWAA O OTHER J WARNING INDICATION DE DESCENT 1 GL 01 930RC 45729 DURING DESCENT UPON GEAR EXTENSION, NOSE WHEEL GREEN LIGHT WOULD NOT ILLUMINATE. PERFORMED COCKPIT OPERATING MANUAL PRO CEDURE. RECYCLED GEAR AND GREEN ILLUMINATED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE CYCLED GEAR SEVERAL TIMES WITH ALL OPERATIONS AND INDICATIONS NORMAL. LUBRICATED NOSE GEAR AND APPROVED FOR SERVICE. 2 L 7 2 4F A6WE 1997010200364 19970102 00364 NE 1997 1 2 9627002707 2 19961221 A 7230 COMPRESSOR BOEING 727 727225 1384077 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE STALLED A NWAA A UNSCHED LANDING C F.O.D. CL CLIMB 1 GL 01 816EA 22553 696471 DURING CLIMB, THE NUMBER ONE ENGINE EXPERIENCED MULTIPLE COMPRESSOR STALLS. CREW REDUCED POWER ON THE NUMBER ONE ENGINE , DIVERTED TO LAS AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NUMBER ONE ENGINE DUE TO FOD. 2 L 7 3 4F 4 F A3WE E2EA 1997010200365 19970102 00365 WP 1997 1 2 9627019918 1 19961226 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 940N 47572 DURING LINE MAINTENANCE INSPECTION, FOUND OVERWING EXIT EMERGENCY LIGHTS AT ROW 11 INOPERATIVE. REPLACED BATTERIES, OPE RATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1997010200366 19970102 00366 WP 1997 1 2 9627021229 1 19961224 A 3350 POWER SUPPLY DOUG DC10 DC1030 3023501 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 229NW 46551 DURING LINE CHECK, THE AFT EMERGENCY LIGHT POWER SUPPLY FAILED TEST. REPLACED AFT EMERGENCY LIGHT POWER SUPPLY (EMBS139 -2) AND THE BATTERY (EMSE299). 2 L 7 3 4F A22WE 1997010200367 19970102 00367 WP 1997 1 2 9627039981 1 19961226 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 362-435 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 994Z 47097 DURING PERIODIC CHECK, FOUND DOUBLER AT FORWARD BAG BIN DOOR JAMB WITH SEVERAL AREAS OF CORROSION FROM FS 362 TO FS 435, INSIDE AND OUTSIDE SKIN AT BOTTOM SIDE OF DOOR OPENING. CUT LOWER SECTION OF DOOR DOUBLER AT FORWARD AND AFT SIDE. IN STALLED REPAIR DOUBLER PER EA 99-111941, L/P 0907623. 2 L 7 2 4F A6WE 1997010200368 19970102 00368 SW 1997 1 2 QXEA9600499 1 19961225 A 2621 30300020 FIRE BOTTLE SWRNGN SWRNGN SA227 SA227AC 8780603 SW LT NACELLE DISCHARGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 2697V AC663 DURING MAINTENANCE, FOUND NR 1 ENGINE FIRE BOTTLE DISCHARGED. REPLACED BOTTLE AND TESTED SYSTEM, RETURNED AIRCRAFT TO S ERVICE. 2 L 7 2 4T RT A8SW 1997010200369 19970102 00369 WP 1997 1 2 MWEA96660 1 19961225 A 3397 WIRE DOUG DC9 DC932 3022066 WP CABIN LOOSE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 209ME 47730 DURING ROUTINE MAINTENANCE, FOUND OVERHEAD EMERGENCY LIGHT DIM BETWEEN NR 2 GALLEY AND COAT CLOSET. SECURED EMERGENCY L IGHT GROUND SOURCE AS REQUIRED, OPERATES NORMAL. 2 L 7 2 4F A6WE 1997010200370 19970102 00370 NM 1997 1 2 SCNA96449 1 19961221 A 3350 900835A BATTERY BOEING 727 727225 1384077 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 283SC 22559 FOUND AFT AIRSTAIR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES AND CLEANED CONTACTS. EMERGENCY LIGHT OPS CHECKS GOOD IN ACCORDANCE WITH MM 33-50-01. 2 L 7 3 4F A3WE 1997010200371 19970102 00371 WP 1997 1 2 SCNA96450 1 19961222 A 3350 P4010049 BATTERY PACK DOUG DC10 DC1010 3022110 WP CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 573SC 46905 FOUND EMERGENCY FLOOR TRACK LIGHT IN MID CABIN RIGHT SIDE INOP. REMOVED AND REPLACED BATTERY PACK AND OPS CHECKED GOOD. 2 L 7 3 4F A22WE 1997010200372 19970102 00372 NM 1997 1 2 SCNA96451 1 19961226 A 3350 900542 POWER SUPPLY BOEING 727 727227 1384078 NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 275AF 22092 FOUND FORWARD AISLE BULLNOSE EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK AND POWER SUPPLY, OPS CHECKED GOOD . 2 L 7 3 4F A3WE 1997010200373 19970102 00373 NM 1997 1 2 SCNA96452 1 19961226 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 275AF 22092 FOUND AFT AIRSTAIR OVERHEAD EMERGENCY LIGHTS DIM. REMOVED AND REPLACED BATTERIES AND OPS CHECKED GOOD. 2 L 7 3 4F A3WE 1997010200374 19970102 00374 NM 1997 1 2 SCNA96453 1 19961226 A 3350 90052 POWER SUPPLY BOEING 727 7272J4 1384006 NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 285SC 21676 FOUND L2 OVER DOOR EMERGENCY EXIT LIGHT WILL NOT TEST. REMOVED AND REPLACED POWER SUPPLY AND OPS CHECKED GOOD IN ACCORD ANCE WITH MM 33-50-71. 2 L 7 3 4F RT A3WE 1997010200375 19970102 00375 NM 1997 1 2 DHL96705002 1 19961223 A 2782 10605595 ACTUATOR BOEING 727 72722C 138400F NM NR 3 LE SLAT CRACKED A DHLA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 705DH 19191 SYSTEM-A HYDRAULICS SYSTEM FAILED ON DEPARTURE, QUANTITY WAS ZERO. FOUND NR 3 L/E SLAT ACTUATOR HOUSING CRACKED. REPLA CED SAME. 2 L 7 3 4F A3WE 1997010200376 19970102 00376 1997 1 2 DHL96720004 4 19961226 A 3418 10608783 STALL WARN VANE BOEING 727 727228 NM RIGHT BROKEN A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 720DH 19544 BIRD STRIKE ON DEPARTURE, STALL WARNING STICKSHAKER ACTIVATED CONTINUOUSLY UNTIL TOUCHDOWN. BIRD PARTS ON CAPT WINSHIEL D, SAW AT LEAST 5 BIG BIRDS BEFORE IMPACT. CLEANED WINDOW AND NOSE AREA INSPECTED, NO DAMAGE. EVALUATED DENT PER SRM, COMPLIED WITH BIRD STRIKE INSP PER MM 5-51-41. REMOVED AND REPLACED STALL WARNING VANE AND OPS CHECKED PER MM. 2 L 7 3 4F A3WE 1997010200377 19970102 00377 SO 1997 1 2 SWIA95795 1 19961219 A 2613 WIRE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT ENGINE OUT OF POSITION A SWIA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 187SW 120037 ON CLIMBOUT, DUCT LEAK LIGHT FOR RIGHT ENGINE ILLUMINATED, IT STAYED ON FOR MORE THAN 3 MINUTES. SHUT DOWN RIGHT ENGINE PER QRH AND RETURNED TO RNO. INSPECTED A/C RIGHT ENGINE BLEED AIR SYSTEM, FOUND SUSPECT TEMP SENSOR WIRE TO BE IN CLOS E PROXIMITY TO BLEED AIR LINE. SECURED WIRE WITH A/C WIRE BUNDLE, RAN A/C 10 MIN USING BLEED AIR SYSTEM, COULD NOT DUPL ICATE. CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1997010200379 19970102 00379 SO 1997 1 2 SWIA95797 1 19961221 A 2752 3472001001 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT TE FLAP FAILED A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 203SW 120240 DURING CRUISE FLIGHT REPEATED FLAP CONTROL FAULTS. EACH FAULT INCLUDED ASSOCIATED LIGHTS ANNUNCIATED AND FLAP GAUGE IND ICATED 45 DEGREES. ATTEMPTED SEVERAL TIMES TO CLEAR FAULTS WITH SUCCESS. HOWEVER, DURING LANDING UNABLE TO SET LANDING FLAPS AND UNABLE TO CLEAR FAULT ON THE FLAP CONTROL PANEL. REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATOR IAW MM 27-5 0-00. 2 L 7 2 4T 4 T RT A31SO E20NE 1997010200380 19970102 00380 SO 1997 1 2 SWIA95798 1 19961221 A 7712 311694201 TORQUE MONITOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT ENGINE MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 223SW 120291 LEFT ENGINE FAILED AFTER TAKEOFF AT 600 FT. RETURNED TO FIELD. DETERMINED LEFT ENGINE HAD AN AUTO FEATHER WITHOUT ENGI NE SHUT DOWN. REPLACED LEFT ENGINE TORQUE PROBE WITH SERVICEABLE UNIT. ALL GROUND CHECKS GOOD IAW MM 73. 2 L 7 2 4T 4 T RT A31SO E20NE 1997010200381 19970102 00381 WP 1997 1 2 TC8A96073 1 19961223 A 3510 OXYGEN LINE DOUG DC8 DC851 3021920 WP COCKPIT LOOSE A TC8A A UNSCHED LANDING O OTHER CR CRUISE 1 GL 23 805CK 45649 WHILE EN ROUTE, THE CREW OXYGEN DEPLETED TO 200 PSI. SERVICED CREW OXYGEN TO 1850 PSI, TIGHTENED LEAKING LINE AT 2ND OB SERVERS REGULATOR AND LEAK CHECKS GOOD. 2 L 7 4 4F 4A25 1997010200382 19970102 00382 NM 1997 1 2 AALA961521 1 19961012 A 5330 141N3312 SKIN BOEING 757 757223 1384957 NM BS 350 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 695AN 26975 AFW - REPAIR USED FASTENERS BACR15CE4D FOR DAMAGED SKIN. REPAIRED PER MRB 757-990. (M) 2 L 7 2 4F RT A2NM 1997010200383 19970102 00383 NM 1997 1 2 AALA961525 1 19961012 A 5210 146N62016 PAN BOEING 757 757223 1384957 NM R4 DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 695AN 26975 AFW - DOOR PAN AFTER BLENDING CORROSION, REMAINING MATERIAL IS BEYOND SRM LIMITS. REPAIRED PER MRB 757-977. (M) 2 L 7 2 4F RT A2NM 1997010200384 19970102 00384 NM 1997 1 2 AALA961527 1 19961012 A 5751 113N7108 FRAME BOEING 757 757223 1384957 NM LT AILERON DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 695AN 26975 AFW - LEFT AILERON LOWER CONDUCTIVE FRAME HAS SMALL BURN HOLE FROM STATIC DISCHARGE. REPAIRED PER MRB 757-984. (M) 2 L 7 2 4F RT A2NM 1997010200385 19970102 00385 NM 1997 1 2 AALA9641 1 19961101 A 5315 141N5113 FLOOR BEAM BOEING 757 757223 1384957 NM BS 377 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 660AM 25294 AFW - FLOOR BEAM HAS CORROSION REMOVAL MATERIAL, REMAINING IS BEYOND SRM ALLOWABLE LIMITS. REPAIRED PER MRB 757-1000. ( M) 2 L 7 2 4F RT A2NM 1997010200386 19970102 00386 NM 1997 1 2 AALA961644 1 19961101 A 5320 141N5160 SUPPORT BOEING 757 757223 1384957 NM BS 403 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 660AM 25294 AFW - FLOOR SUPPORTS IN SECTION 41 HAVE CORROSION REMOVAL, MATERIAL REMAINING IS BEYOND SRM ALLOWABLE LIMITS. REPAIRED PER MRB 757-994. (M) 2 L 7 2 4F RT A2NM 1997010200387 19970102 00387 NM 1997 1 2 AALA961648 1 19961101 A 5320 141N8322 ANGLE BOEING 757 757223 1384957 NM BS 360 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 660AM 25294 AFW - ANGLE HAS CORROSION REMOVAL ON UPPER SURFACE, MATERIAL REMAINING IS BEYOND SRM LIMITS. REPAIRED PER MRB 757-995. (M) 2 L 7 2 4F RT A2NM 1997010200388 19970102 00388 NM 1997 1 2 AALA961652 1 19961101 A 5315 141N5801 FLOOR BEAM BOEING 757 757223 1384957 NM BS 310 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 660AM 25294 AFW - FLOOR BEAM HAS CORROSION REMOVAL, MATERIAL REMAINING IS BEYOND SRM ALLOWABLE LIMITS. REPAIRED PER MRB 757-996. ( M) 2 L 7 2 4F RT A2NM 1997010200389 19970102 00389 NM 1997 1 2 AALA961656 1 19961101 A 5315 141N2032 FLOOR BEAM BOEING 757 757223 1384957 NM BS 324 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 660AM 25294 AFW - FLOOR BEAM HAS CORROSION REMOVAL, MATERIAL REMAINING IS BEYOND ALLOWABLE SRM LIMITS. REPAIRED PER MRB 757-997. ( M) 2 L 7 2 4F RT A2NM 1997010200390 19970102 00390 NM 1997 1 2 AALA961659 1 19961101 A 5315 146N5089 FLOOR BEAM BOEING 757 757223 1384957 NM BS 1640 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 660AM 25294 AFW - FLOOR BEAM HAD 2 AREAS OF CORROSION BLENDED BEYOND SRM LIMITS. REPAIRED PER MRB 757-998. (M) 2 L 7 2 4F RT A2NM 1997010200391 19970102 00391 NM 1997 1 2 AALA961663 1 19961101 A 5320 146N8522 SILL BOEING 757 757223 1384957 NM CARGO DOORWAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 660AM 25294 AFW - AFT CARGO DOOR SURROUND STRUCTURE LOWER SILL HAD CORROSION BLEND BEYOND SRM LIMITS. REPAIRED PER MRB 757-999. (M ) 2 L 7 2 4F RT A2NM 1997010200392 19970102 00392 NM 1997 1 2 AALA961539 1 19961018 A 5315 146N5089 FLOOR BEAM BOEING 757 757223 1384957 NM BS 1640 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 665AA 25299 AFW - FLOOR BEAM AT STATION 1640 HAS CORROSION REMOVAL, REMAINING MATERIAL IS BEYOND SRM ALLOWABLE LIMITS. REPAIR PER M RB 757-982. (M) 2 L 7 2 4F RT A2NM 1997010200393 19970102 00393 NM 1997 1 2 AALA961544 1 19961018 A 5315 141N5113 FLOOR BEAM BOEING 757 757223 1384957 NM BS 377 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 665AA 25299 AFW - FLOOR BEAM AT STATION 377 HAS CORROSION, REMOVAL ON UPPER SURFACE MATERIAL REMAINING IS BEYOND SRM LIMITS. REPAIR PER MRB 980. (M) 2 L 7 2 4F RT A2NM 1997010200394 19970102 00394 NM 1997 1 2 AALA961543 1 19961018 A 5315 141N5112 FLOOR BEAM BOEING 757 757223 1384957 NM BS 365 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 665AA 25299 AFW - FLOOR BEAM AT STATION 365 HAS DRILL MARK BLENDOUT, MATERIAL REMAINING IS BEYOND SRM ALLOWABLE LIMITS. REPAIR PER MRB 757-981. (M) 2 L 7 2 4F RT A2NM 1997010200395 19970102 00395 NM 1997 1 2 AALA961542 1 19961018 A 5210 146N62016 PAN BOEING 757 757223 1384957 NM R4 DOOR GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 665AA 25299 AFW - R-4 DOOR HANDLE PAN HAS GOUGE BEYOND SRM LIMITS. GOUGE WAS BLENDED. REPAIRED PER MRB 757-983. (M) 2 L 7 2 4F RT A2NM 1997010200396 19970102 00396 NM 1997 1 2 AALA961540 1 19961018 A 5320 141N516154 INTERCOSTAL BOEING 757 757223 1384957 NM BS 395-418 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 665AA 25299 AFW - INTERCOSTAL BETWEEN STATION 395 AND 418 HAS CORROSION REMOVAL, REMAINING MATERIAL IS BEYOND ALLOWABLE SRM LIMITS. REPAIR PER MRB 757-979. (M) 2 L 7 2 4F RT A2NM 1997010200397 19970102 00397 WP 1997 1 2 AALA961672 1 19961111 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 160-205 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 205AA 49155 TUL - CUSP T-ANGLE AND CUSP MEMBRANE CORRODED STATION 160-205, JUST INBOARD OF FORWARD SERVICE DOOR. INSTALLED NEW SECT ION OF CUSP ANGLE STATION 165-205 PER SRM 53-05 FIG 55, INSTALLED NEW SECTION OF CUSP STATION 175-200 PER SRM 53-01 FIG 2. TREATED AND PRIMED BARE METAL PER SRM 51-10-3. (M) 2 L 7 2 4F A6WE 1997010200398 19970102 00398 WP 1997 1 2 AALA961673 1 19961108 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 1060 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 205AA 49155 TUL - CORROSION INSIDE GOUGE L-28 RIGHT BLENDED BEYOND LIMITS. REPAIRED PER ESO 80559, DATED 11-7-96. INSTALLED STRAP DOUBLER INSIDE LONGERON CHANNEL. (M) 2 L 7 2 4F A6WE 1997010200399 19970102 00399 WP 1997 1 2 AALA961674 1 19961108 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 1078 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 205AA 49155 TUL - FOUND CORROSION INSIDE GOUGE L-27 RIGHT BLENDED TO BEYOND LIMITS. REPAIRED PER ESO 80559, DATED 11-7-96. INSTALL ED STRAP DOUBLER INSIDE LONGERON CHANNEL. (M) 2 L 7 2 4F A6WE 1997010200400 19970102 00400 NM 1997 1 2 AALA961598 1 19961103 A 5730 SKIN BOEING 727 727223 1384074 NM BS 760 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND CORROSION ABOVE RIGHT PRIMARY HEAT EXCHANGER ON CENTER WING SKIN. REMOVED CORROSION AND INSTALLED DOUBLER P ER ESO 11697, DATED 10-30-96. (M) 2 L 7 3 4F A3WE 1997010200401 19970102 00401 NM 1997 1 2 AALA961596 1 19961103 A 5720 WEB BOEING 727 727223 1384074 NM RT WING CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - WEB CRACKED INBOARD OF AILERON QUAD CASTING. INSTALLED DOUBLER PER SRM 51-40-2. (M) 2 L 7 3 4F A3WE 1997010200402 19970102 00402 NM 1997 1 2 AALA961602 1 19961103 A 5320 WINDOW FRAME BOEING 727 727223 1384074 NM BS 219 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - CAPTAINS NR 1 WINDOW FRAME CRACKED. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 8. (M) 2 L 7 3 4F A3WE 1997010200403 19970102 00403 NM 1997 1 2 AALA961600 1 19961103 A 3231 BRACKET BOEING 727 727223 1384074 NM BS 950 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - MOUNT BRACKET FOR AFT UPSTOP BOLT INBOARD GEAR DOOR CRACKED. REMOVED AND REPLACED CRACKED BRACKETS. (M) 2 L 7 3 4F A3WE 1997010200404 19970102 00404 WP 1997 1 2 AALA961597 1 19961101 A 5320 59108284298 BRACKET DOUG DC9 DC982 3022082 WP BS 1309 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 205AA 49155 TUL - CORROSION ON PULLEY BRACKET. BRACKET REPLACED. (M) 2 L 7 2 4F A6WE 1997010200405 19970102 00405 WP 1997 1 2 AALA961599 1 19961101 A 5320 3648583503 BRACKET DOUG DC9 DC982 3022082 WP BS 1309 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 205AA 49155 TUL - CORROSION ON PULLEY BRACKET. BRACKET REPLACED. (M) 2 L 7 2 4F A6WE 1997010200406 19970102 00406 WP 1997 1 2 AALA961664 1 19961115 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 207-218 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 205AA 49155 TUL - CORROSION ON CUSP ANGLE LONGERON 18L. INSTALLED DOUBLER PER ESO 80559, DATE 11-14-96. (M) 2 L 7 2 4F A6WE 1997010200407 19970102 00407 WP 1997 1 2 AALA961601 1 19961103 A 5314 KEEL BEAM DOUG DC9 DC982 3022082 WP BS 927 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 505AA 49799 TUL - FORWARD END OF KEEL BEAM CRACKED. REPAIRED IAW SRM AARD 53-10-00-6, AARD 53-10-00-1. (M) 2 L 7 2 4F A6WE 1997010200408 19970102 00408 WP 1997 1 2 AALA961609 1 19961103 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1322 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 234AA 49181 TUL - HEAVY CORROSION, VERTICAL LEG AT LONGERON 30, FORWARD FACE. REPAIRED IAW 53-03 PAGE 46 AND 53-10-00-17 PAGE 21. ( M) 2 L 7 2 4F A6WE 1997010200409 19970102 00409 WP 1997 1 2 AALA961604 1 19961104 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1198-1220 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 70401 49312 TUL - CORROSION ON NR 3 SEAT TRACK, STATION 1098 TO 1220. REMOVED AND REPLACED NR 3 SEAT TRACK STATION 1098 TO 1220. ( M) 2 L 7 2 4F A6WE 1997010200410 19970102 00410 WP 1997 1 2 AALA961607 1 19961104 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1198-1220 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 70401 49312 TUL - CORROSION ON NR 3 SEAT TRACK STATION 1098 TO 1220. REMOVED AND REPLACED NR 3 SEAT TRACK STATION 1098 TO 1220. (M ) 2 L 7 2 4F A6WE 1997010200411 19970102 00411 WP 1997 1 2 AALA961691 1 19961118 A 5320 CUSP DOUG DC9 DC982 3022082 WP BS 1170 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 493AA 49731 TUL - CORROSION ON CUSP MEMBRANE ABOVE AFT CX DOOR FORWARD HINGE. INSTALLED DOUBLER WITH SEALANT PER SRM 53-01, PAGE 4 SHEET 3 PAGE 17. (M) 2 L 7 2 4F A6WE 1997010200412 19970102 00412 EU 1997 1 2 VTZA96422 1 19961205 A 5230 DOOR JETAIR JETSTM JETSTM4101 1500501 EU CARGO COMPT NOT LATCHED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 312UE 41025 FLT 6355 - IAD-TYS - ABORTED TAKEOFF DUE TO BAGGAGE DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO F URTHER PROBLEMS. MAINTENANCE INSPECTED AND FOUND DOOR NOT CLOSED PROPERLY AND SECURED DOOR, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1997010200413 19970102 00413 EU 1997 1 2 VTZA96425 1 19961204 A 2770 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU GUST LOCK OUT OF ADJUST A VTZA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 325UE 41063 FLT 6185 - IAD-RDU - ABORTED TAKEOFF DUE TO CONFIGURATION WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURHTER PROBLEMS. MAINTENANCE INSPECTED AND ADJUSTED GUST LOCK MICROSWITCH, OPS CHECK OK. AIRCRAFT WAS RELEASED AND AP PROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1997010200414 19970102 00414 1997 1 2 VTZA96423 3 19961204 A 6140 BETA LIGHT JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE ILLUMINATED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 327UE 41080 FLT 6531 - IAD-ORF - ABORTED TAKEOFF DUE TO LEFT ENGINE RED BETA LIGHT ILLUMINATED WITH TORQUE ROLLED BACK TO 24 PERCENT . AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED BETA SYSTEM AND COULD NOT DUPLICATE, OPS C HECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1997010200415 19970102 00415 EU 1997 1 2 VTZA96404 1 19961120 A 3260 9005EN38 SWITCH BAG JETSTM JETSTM3201 1500217 EU LT MLG FAILED A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 484UE 899 FLT 6173 - IAD-HVN - MADE AN UNSCHEDULED LANDING DUE TO LEFT RED INTRANSIT LIGHT REMAINED ON FOLLOWING GEAR UP. AIRCRAF T RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED UPLOCK MICROSWITCH, OPS CHECK OK. AIRCR AFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1997010200416 19970102 00416 1997 1 2 VTZA96405 4 19961121 A 3416 066306202 ALTIMETER BAG JETSTM JETSTM3201 1500217 EU LT COCKPIT FAILURE A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 482UE 897 FLT 6155 - IAD-ALB - MADE AN UNSCHEDULED LANDING DUE TO CAPTAINS ALTIMETER FAILED. AIRCRAFT RETURNED TO GATE WITH NO FU RTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED CAPTAINS ALTIMETER, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1997010200417 19970102 00417 EU 1997 1 2 VTZA96408 1 19961126 A 2432 BTCA520 BATTERY BAG JETSTM JETSTM3201 1500217 EU NR 1 OVERTEMP A VTZA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CR CRUISE 1 EA 27 470UE 814 FLT 941 - SWF-IAD - MADE AN UNSCHEDULED LANDING DUE TO NR 1 BATTERY OVERTEMP. AIRCRAFT RETURNED TO GATE WITH NO FURTHE R INCIDENTS. MAINTENANCE FERRIED AIRCRAFT TO IAD AND REMOVED AND REPLACED BATTERY, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1997010200418 19970102 00418 1997 1 2 VTZA96407 4 19961126 A 3413 066500012704 VSI BAG JETSTM JETSTM3201 1500217 EU LEFT FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 482UE 897 FLT 6328 - PIT-IAD - MADE AN UNSCHEDULED LANDING DUE TO CAPTAINS VSI FAILED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED CAPTAINS VSI, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1997010200419 19970102 00419 1997 1 2 VTZA96406 4 19961126 A 3454 KNOB BAG JETSTM JETSTM3201 1500217 EU NAV SYSTEM LOOSE A VTZA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 27 488UE 907 FLT 6523 - JFK-ROC - RETURNED TO GATE DUE TO NAV SELECT KNOB FELL OFF CONTROL HEAD, AND WITH NO FURTHER PROBLEMS. MAINT ENANCE RESECURED NAV SELECT KNOB, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1997010200420 19970102 00420 EU 1997 1 2 VTZA96411 1 19961201 A 2150 ACM JETAIR JETSTM JETSTM4101 1500501 EU RIGHT REQ'D SERVICE A VTZA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 27 313UE 41026 FLT 6429 - IAD-JFK - RETURNED TO GATE DUE TO RIGHT DUCT O-TEMP LIGHT ILLUMINATED. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND FREED ACM, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE . (M) 2 L 7 2 4T RT A41NM 1997010200421 19970102 00421 1997 1 2 VTZA96410 4 19961201 A 3442 CONNECTORS BAG JETSTM JETSTM3201 1500217 EU RADAR SYSTEM WATER CONTAM A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 488UE 907 FLT 6247 - IAD-BGM - MADE AN UNSCHEDULED LANDING DUE TO WX RADAR INOP. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLE MS. MAINTENANCE CLEANED WATER FROM RIGHT CONNECTORS, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1997010200422 19970102 00422 EU 1997 1 2 VTZA96409 1 19961201 A 3610 8659567 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE FAILED A VTZA D RETURN TO BLOCK N O FALSE WARNING OTHER TX TAXI/GRND HDL 1 EA 27 324UE 41017 FLT 6502 - JFK-IAD - DURING TAXI, RETURNED TO GATE DUE TO LEFT AIR OFF LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WIT H NO FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED LEFT FLOW HIGH PRESSURE SWITCH, OPS CHECK OK. AIRCRAFT WAS REL EASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1997010200423 19970102 00423 EU 1997 1 2 VTZA96419 1 19961124 A 5270 SWITCH BRACKET JETAIR JETSTM JETSTM4101 1500501 EU BAGG DOOR FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 306UE 41020 FLT 6292 - IAD-DAY - ABORTED TAKEOFF DUE TO BAGGAGE DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO F URTHER PROBLEMS. MAINTENANCE OPENED DMI 53138, MEL 52-3. MAINTENANCE CLOSED DMI 53138 BY REMOVING AND REPLACING MICROS WITCH BRACKET, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1997010200424 19970102 00424 EU 1997 1 2 VTZA96418 1 19961116 A 5270 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGG DOOR OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 324UE 41017 FLT 6235 - JFK-IAD - TAKEOFF DUE TO MAIN BAGGAGE DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURT HER PROBLEMS. MAINTENANCE OPENED DMI 57953, MEL 52-3. MAINTENANCE CLOSED DMI 57953 BY ADJUSTING AFT DOOR MICROSWITCH, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1997010200425 19970102 00425 EU 1997 1 2 VTZA96417 1 19961113 A 5270 SWITCH WIRE BAG JETSTM JETSTM3201 1500217 EU BAGG DOOR BROKEN A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 497UE 904 FLT 6401 - IAD-SWF - ABORTED TAKEOFF DUE TO POD DOOR LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBL EMS. MAINTENANCE OPENED DMI 55139, MEL 52-1. MAINTENANCE CLOSED DMI 55139 BY REPAIRING BROKEN WIRE TO MICROSWITCH, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1997010200426 19970102 00426 EU 1997 1 2 VTZA96416 1 19961112 A 2133 OUTFLOW VLV BAG JETSTM JETSTM3201 1500217 EU CABIN LOOSE LINES A VTZA O OTHER O OTHER DE DESCENT 1 EA 27 487UE 906 FLT 6194 - IAD-EVR - MADE AN SCHEDULED LANDING AT EVR WITH ONE DISCREPANCY WHICH WAS UNABLE TO CONTROL FLOWS. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI 55980, MEL 21-14. MAINTENANCE CLOSED DMI 55980 BY C LEANING AND RESECURING LINES TO OUTFLOW VALVE, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1997010200427 19970102 00427 1997 1 2 VTZA96415 4 19961108 A 2213 CIRCUIT BREAKER JETAIR JETSTM JETSTM4101 1500501 EU FCC PANEL TRIPPED A VTZA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 EA 27 313UE 41026 FLT 6222 - JFK-IAD - DURING APPROACH, MADE AN SCHEDULED LANDING WITH ONE DISCREPANCY DUE TO PITCH WENT TO FULL UP. AIRC RAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE OPEN DMI 07424, MEL 22-1. MAINTENANCE CLOSED DMI 07424 BY CYCL ING FCC CIRCUIT BREAKER, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1997010200428 19970102 00428 EU 1997 1 2 VTZA96414 1 19961106 A 5270 SWITCH BAG JETSTM JETSTM3201 1500217 EU CARGO DOOR OUT OF ADJUST A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 493UE 805 FLT 6332 - IAD-PIT - DURING CLIMB, MADE AN UNSCHEDULED LANDING DUE TO POD DOOR LIGHT ILLUMINATED AND ATC SAID POD DOOR O PENED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED DOOR AND FOUND SECURED ALSO INSPECTED HINGES AND SHOOT BOLTS. MAINTENANCE OPENED DMI 05774 BY ADJUSTING HANDLE MICROSWITCH, OPS CHECK OK. AIRCRAFT WAS RELE ASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1997010200429 19970102 00429 EU 1997 1 2 VTZA96413 1 19961113 A 3310 2TW11 SWITCH BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A VTZA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 27 491UE 911 FLT 6372 - IAD-AIB - DURING CRUISE, MADE AN SCHEDULED FLIGHT WITH ONE DISCREPANCY WHICH WAS THE SMELL OF SMOKE AND THE O VERHEAD PANEL LIGHTS WENT OUT. MAINTENANCE INSPECTED AND FOUND COCKPIT CONVERTER SOURCE OF PROBLEM. MAINTENANCE OPENED DMI 18309 , MEL 33-1 ON CONVERTER. MAINTENANCE CLOSED DMI 18309 BY REMOVING AND REPLACING DIMMER SWITCH, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1997010200430 19970102 00430 EU 1997 1 2 VTZA96403 1 19961120 A 5240 14153133271 DOOR JETAIR JETSTM JETSTM4101 1500501 EU LAV LOOSE A VTZA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 27 319UE 41042 FLT 6203 - IAD-MHT - DURING CLIMB, AN UNSCHEDULED LANDING DUE TO BAD VIBRATION COMING FROM AFT AREA. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND OPENED DMI 41443, MEL 52-4, ON LAV DOOR. MAINTENANCE REMO VED AND REPLACED LAV DOOR AND CLOSED DMI 41443. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE . (M) 2 L 7 2 4T RT A41NM 1997010200431 19970102 00431 EU 1997 1 2 VTZA96412 1 19961106 A 5270 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGGAGE DOOR DIRTY A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 324UE 41017 FLT 6186 - LYH-IAD - ABORTED TAKEOFF DUE TO MAIN BAGGAGE DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE OPENED DMI 57952, MEL 52-3. MAINTENANCE CLOSED DMI 57952 BY CLEANING MICROSWITCH, OP S CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1997010200432 19970102 00432 NE 1997 1 2 VTZA96421 2 19961202 A 7200 310349015 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE LEFT BIRD STRIKE A VTZA A UNSCHED LANDING C F.O.D. CL CLIMB 1 EA 27 315UE 41033 P75011 FLT 6154 - IAD-BOS - AN UNSCHEDULED LANDING DUE TO LEFT ENGINE BIRD STRIKE INGESTION. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED REMOVED AND REPLACED ENGINE, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 4 T RT A41NM E18NE 1997010200433 19970102 00433 EU 1997 1 2 VTZA96379 1 19960919 A 3260 622800200 UPLOCK SWITCH BAG JETSTM JETSTM3201 1500217 EU LT MLG FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 474UE 849 FLT 6442 - IAD-HVN - DURING CRUISE, EXPERIENCED A LEFT GEAR INTRANSIT LIGHT AFTER SELECTING THE GEAR UP FUNCTION. AIRCR AFT RETURNED TO IAD WHERE THE MAINTENANCE PERSONNEL TROUBLESHOT THE DISCREPANCY AND FOUND THAT THE LEFT GEAR UPLOCK MICR OSWITH HAD FAILED. THE MICROSWITCH WAS REPLACED AND THE SYSTEM WAS FUNCTIONALLY CHECKED. THE AIRCRAFT WAS THEN RELEASE D FOR SERVICE. (M) 2 L 7 2 4T RT A56EU 1997010200434 19970102 00434 EU 1997 1 2 WTAA960203 1 19961123 A 3230 6158D RETRACTION JACK BAG JETSTM JETSTM3101 1500215 EU NLG FAILED A WTAA K NONE O OTHER NR NOT REPORTED 1 WP 17 419UE 779 LAX - NOSE LANDING GEAR WOULD NOT RETRACT. AIRCRAFT FERRIED TO FAT. MAINTENANCE REPLACED NOSE GEAR RETRACTION JACK. O PERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1997010200435 19970102 00435 SO 1997 1 2 WTAA960202 1 19961122 A 5101 STRUCTURE EMB 120 EMB120RT SO AIRFRAME BIRD STRIKE A WTAA O OTHER C F.O.D. LD LANDING 1 WP 17 275UE 120058 SNA - BIRD STRIKE REPORTED. AIRCRAFT FERRIED TO LAX. MAINTENANCE INSPECTED AIRCRAFT FOR DAMAGE, NO DAMAGE NOTED. AIRC RAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1997010200436 19970102 00436 NE 1997 1 2 WTAA960207 2 19961127 A 7261 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE LEFT LOW OIL A WTAA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 17 271YV 120271 SFO - LEFT ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED AFTER TAKEOFF. CREW SECURED LEFT ENGINE AND LANDED WITHOUT INCIDEN T. MAINTENANCE SERVICED LEFT ENGINE WITH FOUR QUARTS OIL. LEAK AND OPERATIONAL CHECKS SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1997010200437 19970102 00437 1997 1 2 WTAA960200 4 19961121 A 3442 6222504001 RADAR ANTENNA EMB 120 EMB120RT SO RADOME FAILED A WTAA K NONE O OTHER NR NOT REPORTED 1 WP 17 275UE 120058 MRY - WEATHER RADAR WILL NOT PAINT GROUND. AIRCRAFT FERRIED TO FAT. MAINTENANCE REPLACED RADAR ANTENNA AND RADOME. RA DAR OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1997010200438 19970102 00438 EU 1997 1 2 WTAA960201 1 19961121 A 3260 62280020 SWITCH BAG JETSTM JETSTM3101 1500215 EU NLG BROKEN WIRES A WTAA K NONE N FALSE WARNING LD LANDING 1 WP 17 424UE 796 LAX - NOSE GEAR DOWN AND LOCKED INDICATION REPORTED ON LANDING. MAINTENANCE REPAIRED BROKEN WIRE TO NOSE LANDING GEAR D OWNLOCK MICROSWITCH. MICROSWITCH AND OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1997010200439 19970102 00439 WP 1997 1 2 ORJA96100 1 19961108 A 5320 JAMB DOUG DC9 DC983 3022083 WP CARGO DOOR CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 879RA 53185 NUMEROUS AREAS OF CORROSION AT AFT CARGO LOWER DOOR JAMB. AREAS OF CORROSION WERE REMOVED. AREAS OUT OF LIMITS WERE RE PAIRED BY FABRICATING DOUBLER AND STRAP. PARTS WERE INSTALLED. ALL WORK PERFORMED IAW SRM 53-05, PAGES 173-174. (M) 2 L 7 2 4F RT A6WE 1997010200440 19970102 00440 NM 1997 1 2 ASAA9610144 1 19961202 A 4920 380428115 APU BOEING 737 7372X6C 1384552 NM AFT FUSELAGE MALFUNCTIONED A ASAA F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 NM 01 746AS 23123 ANC - FLT 113 - DURING APU START ATTEMPT, GROUND PERSONNEL REPORTED THAT FLAMES WERE EVIDENT FROM THE APU EXHAUST. CREW DISCONTINUED START ATTEMPT AND DISCHARGED APU FIRE BOTTLE. REPLACD APU AND APU FIRE BOTTLE. ALLIED SIGNAL CONCLUDED T HAT THE TURBINE SEALS WERE LEAKING AND THE TURBINE BEARING WAS GALLED. IT APPEARED THAT THE ROTATING GROUP HAD AN UNBAL ANCE THAT WAS CAUSING VIBRATION. NO APPARENT REASON OR INDICATION FOR THE EXHAUST FLAMES COULD BE FOUND. THE APU WAS D ISASSEMBLED, INSPECTED AND REPAIRED BY ALLIED SIGNAL. (M) 2 L 7 2 4F RT A16WE 1997010200441 19970102 00441 WP 1997 1 2 ASAA9680267 1 19961209 A 3350 41B004AD07G3 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 966AS 49104 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 24 TO 27 WERE FOUND INOPERATIVE. REPLACED THE B ATTERIES AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1997010200442 19970102 00442 WP 1997 1 2 ASAA9680266 1 19961208 A 3350 41B004AD07G3 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 943AS 53018 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 9 TO 12 WERE FOUND INOPERATIVE. REPLACED THE BA TTERIES AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1997010200443 19970102 00443 1997 1 2 ASAA9680265 4 19961208 A 2565 D29984103 SLIDE DOUG DC9 DC983 3022083 WP TAIL CONE FAILED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 939AS 49657 OAK - DURING C-CHECK, THE TAILCONE EMERGENCY EVACUATION SLIDE EMERGENCY LIGHTS FAILED TEST. REPLACED THE TAILCONE EMERG ENCY EVACUATION SLIDE. (M) 2 L 7 2 4F RT A6WE 1997010200444 19970102 00444 WP 1997 1 2 ASAA9680264 1 19961128 A 3350 TERMINAL DOUG DC9 DC983 3022083 WP TAILCONE LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 945AS 49643 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD TAILCONE EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. SECURED LOOSE TERMINA L ON LIGHT ASSEMBLY AND LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1997010200445 19970102 00445 WP 1997 1 2 ASAA9680259 1 19961121 A 3350 6011779 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 931AS 49232 SEA - DURING MAINTENANCE CHECK, THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPL Y AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1997010200446 19970102 00446 NM 1997 1 2 ASAA9640098 1 19961116 A 3397 WIRE BOEING 737 7374S3 1384711 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 786AS 24795 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROW 14. RECONNECT ED WIRING TO LIGHT ASSEMBLY AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1997010200447 19970102 00447 NM 1997 1 2 ASAA9610145 1 19961205 A 3350 RPS1B BATTERY PACK BOEING 737 737298C 1384490 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROW 16. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1997010200448 19970102 00448 NM 1997 1 2 ASAA9610143 1 19961127 A 3350 20131A BATTERY BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACKS LIGHTS WERE FOUND TO BE INOPERATIVE AT ROW 18. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1997010200449 19970102 00449 1997 1 2 ASAA9680268 4 19961209 A 2565 D37013111 INFLATION BOTTLE DOUG DC9 DC983 3022083 WP L2 DOOR LOW PRESSURE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 939AS 49657 OAK - DURING C-CHECK, THE L2 DOOR EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. REPLACED THE EMER GENCY EVACUATION SLIDE. (M) 2 L 7 2 4F RT A6WE 1997010200450 19970102 00450 WP 1997 1 2 AALA961713 1 19961121 A 3350 0200335001 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 07 7517A 49894 IAH - FLT 1107 - AT THE GATE AFTER ARRIVAL, EMERGENCY FLOOR LIGHT STRIPS ILLUMINATED AT ALL TIMES WITH THE EMERGENCY EXI T LIGHT SWITCH IN OFF POSITION. FOUND EMERGENCY EXIT LIGHT ASSEMBLY SHORTED TO GROUND IN AFT AIR STAIR. REPLACED EMERG ENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1997010200451 19970102 00451 WP 1997 1 2 AALA961714 1 19961121 A 3350 LIGHTS DOUG DC9 DC982 3022082 WP CABIN MALFUNCTIONED A AALA K NONE L NO TEST TO TAKEOFF 1 SW 07 7517A 49894 MIA - FLT 1460 - DURING TAKEOFF IAH, EMERGENCY FLOOR LIGHTS AFT OF PAX SEAT ROW 18 ILLUMINATED. DURING CRUISE EMERGENCY FLOOR LIGHTS AFT OF PAX SEAT ROW 18 EXTINGUISHED. AIRCRAFT PROCEEDED TO MIA. DURING LANDING ROLL OUT, EMERGENCY FLOOR LIGHTS AFT OF PAX SEAT ROW 18 WERE FLASHING ON AND OFF. ACCOMPLISHED TEST OF EMERGENCY FLOOR LIGHTS PER MAINTENANCE MA NUAL. COULD NOT DUPLICATE ON GROUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1997010200452 19970102 00452 EU 1997 1 2 AALA961715 1 19961120 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 80058 466 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT PAX SEAT ROW 19AB TO 20AB INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP AT PAX SEAT ROW 19AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1997010200453 19970102 00453 NM 1997 1 2 AALA961738 1 19961201 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 896AA 22012 DFW - DURING OVERNIGHT CHECK, AFT THREE FOOT SECTION OF EMERGENCY FLOOR LIGHTS IN COACH INOPERATIVE. REPLACED AFT THREE FOOT SECTION OF EMERGENCY FLOOR LIGHT STRIP IN COACH. SYSTEM GROUND CHECK NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1997010200454 19970102 00454 NM 1997 1 2 AALA961724 1 19961121 A 3350 STB1304 LIGHT BOEING 727 727227 1384078 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 718AA 20611 DFW - DURING OVERNIGHT CHECK, OVERHEAD EMERGENCY EXIT SIGN AT FORWARD GALLEY DOOR INOPERATIVE. REPLACED OVERHEAD EMERGE NCY EXIT SIGN LIGHT ASSEMBLY AT FORWARD GALLEY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1997010200455 19970102 00455 NM 1997 1 2 AALA961741 1 19961130 A 3350 BPS73 POWER SUPPLY BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 649AA 24607 SFO - DURING OVERNIGHT CHECK, FORWARD EMERGENCY FLOOR LIGHTS REMAINED ON WHEN TURNED OFF. RECONNECTED FORWARD EMERGENCY FLOOR LIGHT POWER SUPPLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1997010200456 19970102 00456 NM 1997 1 2 AALA961709 1 19961120 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 863AA 21090 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AFT OF EMERGENCY EXITS INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIPS AFT OF EMERGENCY EXITS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1997010200457 19970102 00457 NM 1997 1 2 AALA961737 1 19961201 A 3350 1000679 LIGHT BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 869AA 21374 JFK - DURING OVERNIGHT CHECK, EMERGENCY EXIT SIGN OVER AFT GALLEY DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEM BLY OVER AFT GALLEY DOOR. SYSETM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1997010200458 19970102 00458 NM 1997 1 2 AALA961740 1 19961201 A 2910 HYD SYSTEM BOEING 767 767223 1385123 NM CENTER HYD SYS REQ SERVICE A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 302AA 1111111111 22308 ORD - FLT 177 - EN ROUTE JFK-ORD, DURING CRUISE, CENTER HYDRAULIC SYSTEM LOW QTY MESSAGE. ACCOMPLISHED ALTERNATE LANDIN G GEAR AND ALTERNATE FLAP PROCEDURES AND AIRCRAFT LANDED ORD WITHOUT INCIDENT. SERVICED CENTER HYDRAULIC SYSTEM. ACCOM PLISHED LEAK AND GROUND CHECKED WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NROMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1997010200526 19970102 00526 NE 1997 1 2 96ZZZX6188 2 19961117 A 7200 ENGINE CNDAIR CL600 CL6002B16 1900305 EA GE CF34 CF343A1 30015 NE LT ENG FAILED A A AMPA K NONE J WARNING INDICATION LD LANDING 1 WP 09 48FU 5021 FLT 5270 - AFTER A NORMAL APPROACH AND LANDING TO EXETER, UNITED KINGDOM, AT 90 KNOTS WITH THRUST REVERSERS DEPLOYED AND A POWER SETTING OF ABOUT 40 PERCENT N1, THE LEFT ENGINE FAILED. NO ADVERSE INDICATIONS OR EFFECTS WERE NOTED EITHER DU RING CRUISE OR DURING THE LANDING UP TO THE POINT OF THE FAILURE. MAINTENANCE VISUALLY INSPECTED ENGINE EXTERNALLY; NO DEFECTS NOTED. BORESCOPED COMPRESSOR AND TURBINE SECTION, NO DEFECTS NOTED. INSTALLED LOANER FUEL CONTROL AND FUEL PUM P, CONDITION STILL EXISTED. REMOVED ENGINE AND INSTALLED LOANER ENGINE ASSEMBLY RECEIVED FROM GENERAL ELECTRIC. REMOVE D ENGINE SHIPPED TO GENERAL ELECTRIC STRUTHERS, WICHITA KS FOR TEAR DOWN AND INSPECTION. ADDITIONAL REPORTS TO FOLLOW. 2 L 7 2 4F 4 F RT A21EA E15NE 1997010200527 19970102 00527 WP 1997 1 2 TWAA9615001 1 19961204 A 3350 58222 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 982PS 47251 STL - FLT 517 - DURING CRUISE, EGRESS LIGHTS ILLUMINATED AT SEAT ROWS 1 TO 7. FOUND FAULTY POWER SUPPLY, MFG PN 5822-2. REPLACED POWER SUPPLY. EGRESS LIGHT OPERATION THEN CHECKED NORMAL. CHECK C - 11-13-95 - STL. 2 L 7 2 4F A6WE 1997010200528 19970102 00528 NM 1997 1 2 TWAA9615002 1 19961204 A 3232 731414 ACTUATOR BOEING 727 727231 1384079 NM RT MLG DOOR LEAKING A TWAA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CE 05 54345 21632 MIA - FLT 4 - DURING CLIMB, A-HYDRAULIC SYSTEM QUANTITY DECREASED. SHUT DOWN A-HYDRAULIC SYSTEM. FOUND RT MLG DOOR AC TUATOR, MFG PN 7-3141-4, LEAKING. REPLACED RT MLG DOOR ACTUATOR. HYDRAULIC SYSTEM AND RT MLG DOOR OPERATION THEN CHECK ED NORMAL. CHECK C-2 - 6-21-96 - JFK. (X) 2 L 7 3 4F A3WE 1997010200529 19970102 00529 WP 1997 1 2 TWAA9615101 1 19961205 A 3350 2150005061 POWER PACK DOUG DC9 DC982 3022082 WP CABIN WEAK A TWAA K NONE O OTHER AP APPROACH 1 CE 05 915TW 49186 STL - FLT 159 - DURING APPROACH, EGRESS LIGHTING ILLUMINATED. FOUND POWER PACK, MFG PN 2150-0050-61, WEAK. REPLACED PO WER PACK AND EGRESS LIGHT SYSTEM, OPERATION CHECKED NORMAL. CHECK C - 4-23-96 - MCI. (X) 2 L 7 2 4F A6WE 1997010200530 19970102 00530 WP 1997 1 2 TWAA9615102 1 19961205 A 2530 5038 OVEN DOUG DC9 DC982 3022082 WP GALLEY FAILED A A TWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 CE 05 953U 49267 STL - FLT 222 - DURING DESCENT, HAD ELECTRICAL ODOR IN AFT CABIN. PULLED CIRCUIT BREAKER FOR AFT GALLEY OVENS. FOUND O VEN, MFG PN 50381, WITH INTERNAL MALFUNCTION. REPLACED OVEN. OVEN OPERATION THEN CHECKED NORMAL. CHECK C-1D - 5-28-96 - JFK. (X) 2 L 7 2 4F A6WE 1997010200531 19970102 00531 WP 1997 1 2 TWAA9615201 1 19961206 A 3260 0351881007 SOCKET DOUG DC9 DC915 3022036 WP LT MLG FAILED A TWAA O OTHER N FALSE WARNING CL CLIMB 1 CE 05 973Z 47033 STL - FLT 692 - DURING CLIMB-OUT, THE LT MLG UNSAFE RED LIGHT ILLUMINATED. REMOVED AND REPLACED RED LIGHT SOCKET, MFG P N 0351881007. OPERATIONAL CHECK NORMAL. CHECK C - 2-6-96 - STL. (X) 2 L 7 2 4F A6WE 1997010200532 19970102 00532 SO 1997 1 2 WTAA960208 1 19961202 A 2751 MS3126P1210S CONNECTOR EMB 120 EMB120RT SO TE FLAP ACTUATOR WATER CONTAM A WTAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 17 120AM 120012 ACV - FLAP DISAGREEMENT ON CLIMB-OUT. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE CLEANED MOISTURE FROM CANNON PLUG ON OUTBOARD FLAP ACTUATOR AND RERACKED COMPUTER. OPERATIONAL CHECKS SATISFACTORY. AIRCRAFT RETURNED TO SE RVICE. (X) 2 L 7 2 4T RT A31SO 1997010200533 19970102 00533 SO 1997 1 2 WTAA960209 1 19961203 A 3150 MS33202 CIRCUIT BREAKER EMB 120 EMB120RT SO COCKPIT TRIPPED A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 17 120AM 120012 SFO - TRIM WARNING ON TAKEOFF REPORTED. TAKEOFF ABORTED. MAINTENANCE RESET AURAL WARNING CIRCUIT BREAKER. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1997010200534 19970102 00534 SO 1997 1 2 WTAA960198 1 19961121 A 2751 30690001005 ANNUNCIATOR EMB 120 EMB120RT SO COCKPIT FAILED A WTAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 17 120AM 120012 SBA - FLAP DISAGREEMENT REPORTED DURING DEPARTURE. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. AIRCRAFT FERRIED TO FAT FOR REPAIR. MAINTENANCE REPLACED FLAP ANNUNCIATOR. FLAPS OPERATIONAL CHECK SATISFACTORY ON GROUND AND DURING SUBSE QUENT TEST FLIGHT. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1997010200535 19970102 00535 1997 1 2 WTAA960199 4 19961121 A 3444 AM275C ALTITUDE ALERTER BAG JETSTM JETSTM3101 1500215 EU COCKPIT FAILED A WTAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 17 419UE 779 LAX - ALTITUDE ALERTER FAILURE CAUSING SMOKE AND ELECTRICAL ODOR REPORTED. AIRCRAFT RETURNED TO GATE. MAINTENANCE REPL ACED ALTITUDE ALTERTER. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A21EU 1997010200536 19970102 00536 EU 1997 1 2 WTAA960204 1 19961121 A 3260 622800200 SWITCH BAG JETSTM JETSTM3101 1500215 EU NLG BROKEN WIRES A WTAA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 WP 17 424UE 796 SNA - NOSE GEAR INTRANSIENT LIGHT FAILED TO ILLUMINATE DURING GEAR EXTENSION. MAINTENANCE REPAIRED BROKEN WIRES TO NOSE LANDING GEAR DOWNLOCK MICROSWITCH. SYSTEMS OPERATIONAL CHECK AND GEAR SWING CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A21EU 1997010200537 19970102 00537 NM 1997 1 2 PCAA9600320 1 19961108 A 5542 85540001003 SKIN DHAV DHC8 DHC8102 2809003 NM RUDDER CRACKED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 805EX 8049 CAP3353 228 FORWARD RUDDER SKIN FOUND CRACKED AT TOP RIGHT SIDE. REPAIRED CRACK IN FORWARD RUDDER IAW RD 8-55-335. A/C RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A13NM 1997010200538 19970102 00538 NM 1997 1 2 PCAA9600323 1 19961106 A 5311 FRAME DHAV DHC8 DHC8102 2809003 NM AFT FUSELAGE CRACKED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 806EX 263 DURING A SCHEDULED C-CHECK, FRAME 4 IN TAIL SECTION, AT STR 4S, WAS FOUND CRACKED. REPAIRED CRACK AT FRAME 4, STR 4S, I AW DHC RD 8-55-199. A/C RETURNED TO SERVICE. ACTT: 13,718. AIRCRAFT TOTAL CYCLES, 15,540. (X) 2 H 7 2 4T RT A13NM 1997010200539 19970102 00539 NM 1997 1 2 PCAA9600319 1 19961105 A 5610 NP1579017 WINDSHIELD DHAV DHC8 DHC8102 2809003 NM LT COCKPIT SHATTERED A PCAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 13 818EX 13658 7H8138 235 EN ROUTE FROM LGA TO MHT, CAPTAIN'S WINDSHIELD SHATTERED DURING CRUISE FLIGHT. A/C DIVERTED TO BDL. REMOVED AND REPLAC ED CAPTAIN'S WINDSHIELD, REPLACED HEAT CONTROLLER AS PRECAUTIONARY MEASURE. WORK PERFORMED IAW DHC MM. A/C RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A13NM 1997010200540 19970102 00540 NM 1997 1 2 PCAA9600321 1 19961109 A 5610 17180003 WINDOW DHAV DHC8 DHC8102 2809003 NM LT COCKPIT CRACKED A PCAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 13 805EX 8193 000123 228 DURING CRUISE FLIGHT, CAPTAIN'S SIDE WINDOW CRACKED NEAR HEATING ELEMENT. A/C DIVERTED INTO MDT. REMOVED AND REPLACED CAPTAIN'S SIDE WINDOW IAW DHC MM. A/C RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A13NM 1997010200541 19970102 00541 NE 1997 1 2 PCAA9600324 2 19961115 A 7200 ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE LEFT FAILED A PCAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 13 809EX 8762 302 120969 DURING CRUISE FLIGHT, THE CREW NOTICED A STRONG ODOR OF SMOKE OR OIL COMING FROM THE BLEED SYSTEM. A/C MADE AN EMERGENC Y LANDING IN BOS. MAINTENANCE PERFORMED AN INSPECTION AND RELEASED THE A/C FOR A FERRY FLIGHT TO MDT. (NOTE: ODOR/SMO KE DISSIPATED WHEN THE ENGINE BLEEDS WERE SELECTED OFF). MDT MAINTENANCE TROUBLESHOT THE BLEED SYSTEM AND DETERMINED TH E LEFT ENGINE WAS AT FAULT. REMOVED AND REPLACED THE LEFT ENGINE IAW MM. A/C RETURNED TO SERVICE. (X) 2 H 7 2 4T 4 T RT A13NM E20NE 1997010200542 19970102 00542 NM 1997 1 2 PCAA9600325 1 19961117 A 2910 82970010141 HYD LINE DHAV DHC8 DHC8102 2809003 NM LT MLG FAILED A PCAA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 EA 13 819EX 016 EN ROUTE TO SYR FROM LGA, A/C LOST NR 1 HYDRAULIC CONTENTS. TROUBLESHOT AND FOUND THE LEFT ANTI-SKID HYDRAULIC LINE DEF ECTIVE. REMOVED AND REPLACED LINE IAW DHC MM. LEFT ENGINE DRIVEN HYDRAULIC PUMP ALSO REPLACED DUE TO OPERATING WITHOUT FLUID. A/C RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A13NM 1997010200543 19970102 00543 1997 1 2 GLBA96224 4 19961119 A 3425 6229682002 DPU BEECH 1900 1900D 1154162 CE NR 1 INTERMITTENT A GLBA O OTHER O OTHER TO TAKEOFF 1 CE 01 96UX UE96 ISN - CAPTAIN'S DPU FAILED ON TAKEOFF. MAINTENANCE RERACKED DISPLAY PROCESSOR UNIT AND EVENTUALLY REPLACED THE UNIT. ( X) 2 L 7 2 4T RT A24CE 1997010200544 19970102 00544 CE 1997 1 2 GLBA96221 1 19961111 A 3260 UPLIMIT SWITCH BEECH 1900 1900C 1154161 CE LANDING GEAR DIRTY A GLBA O OTHER N FALSE WARNING CL CLIMB 1 CE 01 87GL UC87 BMG - GEAR UNSAFE LIGHT ILLUMINATED AFTER GEAR SELECTED UP ON TAKEOFF. MAINTENANCE CLEANED UPLIMIT SWITCH. (X) 2 L 7 2 4T RT A24CE 1997010200545 19970102 00545 CE 1997 1 2 GLBA96222 1 19961111 A 3230 MS2417101 RELAY BEECH 1900 1900C 1154161 CE LANDING GEAR FAILED A GLBA O OTHER J WARNING INDICATION CL CLIMB 1 CE 01 45GL UC45 ORD - GEAR DID NOT EXTEND. EXTENDED GEAR MANUALLY. REMOVED AND REPLACED LANDING GEAR RELAY. OPS CHECKS GOOD. (X) 2 L 7 2 4T RT A24CE 1997010200546 19970102 00546 CE 1997 1 2 GLBA96223 1 19961118 A 2120 1143800401 THROUGH-VALVE BEECH 1900 1900C 1154161 CE RIGHT SEIZED A GLBA O OTHER O OTHER CR CRUISE 1 CE 01 145GL UC145 TUS - LEFT ENVIRONMENTAL FAIL IN-FLIGHT. MAINTENANCE REPLACED RIGHT THROUGH-VALVE AND SYSTEM OPS NORMALLY. (X) 2 L 7 2 4T RT A24CE 1997010200547 19970102 00547 CE 1997 1 2 GLBA96225 1 19961119 A 3260 UPLOCK SWITCH BEECH 1900 1900C 1154161 CE LT MLG FAILED A GLBA O OTHER N FALSE WARNING CL CLIMB 1 CE 01 101UE UC101 DVL - AFTER GEAR RETRACTION, GEAR UNSAFE LIGHTS REMAINED ILLUMINATED. MAINTENANCE ADJUSTED PEDESTAL SWITCH TO OBTAIN LO WER N1 SETTING FOR GEAR UNSAFE LIGHT. TEST FLIGHT NORMAL. LEFT UPLOCK SWITCH WAS LATER REPLACED. (X) 2 L 7 2 4T RT A24CE 1997010200548 19970102 00548 CE 1997 1 2 GLBA96226 1 19961119 A 3246 114800821 WHEEL BEECH 1900 1900C 1154161 CE NLG DEFECTIVE A GLBA O OTHER E VIBRATION/BUFFET TO TAKEOFF 1 CE 01 168GL UC168 RDU - LOUD GRINDING SOUND ON ACCELERATION FOR TAKEOFF WITH EXCESSIVE VIBRATION. MAINTENANCE REMOVED AND REPLACED NOSE W HEEL. (X) 2 L 7 2 4T RT A24CE 1997010200549 19970102 00549 CE 1997 1 2 GLBA96227 1 19961122 A 3234 10138413737 GEAR HANDLE BEECH 1900 1900C 1154161 CE COCKPIT INTERMITTENT A GLBA O OTHER N FALSE WARNING CL CLIMB 1 CE 01 101UE 320 UC101 DVL - RED LIGHTS REMAIN ILLUMINATED WHEN GEAR IS UP. MAINTENANCE REMOVED AND REPLACED LANDING GEAR HANDLE AND PC RELAY BOARD. TEST FLIGHT NORMAL. (X) 2 L 7 2 4T RT A24CE 1997010200550 19970102 00550 SO 1997 1 2 GLBA96229 1 19961125 A 2751 WARNING LIGHT EMB 120 EMB120RT SO TE FLAPS ILLUMINATED A GLBA O OTHER N FALSE WARNING TO TAKEOFF 1 CE 01 129AM 120119 DEN - FLAP DISAGREEMENT ON DEPARTURE. MAINTENANCE COULD NOT DUPLICATE. (X) 2 L 7 2 4T RT A31SO 1997010200551 19970102 00551 SO 1997 1 2 GLBA96230 1 19961126 A 7931 OIL PRESS IND EMB 120 EMB120RT SO LT ENGINE MALFUNCTIONED A GLBA O OTHER O OTHER CR CRUISE 1 CE 01 281UE 120092 LAN - LEFT ENGINE OIL PRESSURE INDICATOR UNRELIABLE. MAINTENANCE CHECKED OIL QUANTITY, CONNECTIONS, INDICATORS. TEST F LIGHT NORMAL. (X) 2 L 7 2 4T RT A31SO 1997010200552 19970102 00552 CE 1997 1 2 GLBA96232 1 19961121 A 2731 CONTROL CABLE BEECH 1900 1900D 1154162 CE ELEVATOR TRIM OUT OF ADJ A A GLBA O OTHER F FLT CONT AFFECTED CR CRUISE 1 CE 01 170GL UE170 RDU - ELEVATOR TRIM JAMMED DURING FLIGHT, WOULD NOT MOVE MANUALLY OR ELECTRICALLY. MAINTENANCE FOUND LOOSE RUDDER SADDL E CABLE INTERFERRING WITH ELEVATOR TRIM CABLE. SADDLE CABLE WAS TIGHTENED AND TRIM OPERATION WAS NORMAL. (X) 2 L 7 2 4T RT A24CE 1997010200553 19970102 00553 CE 1997 1 2 GLBA96233 1 19961126 A 3260 H111541 UPLOCK SWITCH BEECH 1900 1900C 1154161 CE LT MLG FAILED A GLBA O OTHER N FALSE WARNING CL CLIMB 1 CE 01 122GL UC122 SPI - AFTER RETRACTION, RED INTRANSIT LIGHT STAYED ON. MAINTENANCE REMOVED AND REPLACED LEFT UPLOCK SWITCH. ALL SWITCH ES WERE LATER ADJUSTED. TEST FLIGHT SATISFACTORY. (X) 2 L 7 2 4T RT A24CE 1997010200554 19970102 00554 CE 1997 1 2 GLBA96234 1 19961127 A 3240 BRAKE SYSTEM BEECH 1900 1900C 1154161 CE LT MLG REQ'D SERVICE A GLBA O OTHER O OTHER LD LANDING 1 CE 01 84GL UC84 ORD - PARTIAL LOSS OF LEFT MAIN BRAKE. MAINTENANCE BLED BRAKES AND OPERATION WAS NORMAL. (X) 2 L 7 2 4T RT A24CE 1997010200555 19970102 00555 CE 1997 1 2 GLBA96235 1 19961129 A 3260 WARNING HORN BEECH 1900 1900C 1154161 CE LANDING GEAR SOUNDED A GLBA O OTHER N FALSE WARNING CL CLIMB 1 CE 01 98GL UC98 GFK - GEAR UNSAFE HORN SOUNDS AFTER GEAR RETRACTION. MAINTENANCE COULD NOT DUPLICATE IN HANGAR OR ON TEST FLIGHT. (X) 2 L 7 2 4T RT A24CE 1997010200556 19970102 00556 NM 1997 1 2 AWXA9600777 1 19961229 A 3397 WIRE BOEING 737 737301 1384611 NM CABIN DISCONNECTED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 326AW 23258 DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 19 FLOOR PROXIMITY LIGHTS INOP. RESPLICED WIRE, OPS NORMAL, STC - SA3140NM. 2 L 7 2 4F RT A16WE 1997010200557 19970102 00557 NM 1997 1 2 AWXA9600778 1 19961228 A 3350 1060091101 LIGHT BOEING 737 737277 1384570 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 178AW 22645 DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT ON SEAT 5-L INOP. NEW LIGHT WIRED IN, INSTALLED RIVETS AND REPLACED LAMPS, OPS CHECK NORMAL, STC - SA3432NM. 2 L 7 2 4F RT A16WE 1997010200558 19970102 00558 NM 1997 1 2 AWXA9600779 1 19961227 A 3397 WIRE BOEING 737 7373G7 1384595 NM CABIN DISCONNECTED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 151AW 23219 DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT EMERGENCY LIGHT INOP. REPAIRED BROKEN WIRE, CHECKS GOOD, STC - SA3432NM. 2 L 7 2 4F RT A16WE 1997010200559 19970102 00559 NM 1997 1 2 AWXA9600780 1 19961229 A 3350 1060091101 LIGHT BOEING 737 7372A6 138448B NM CABIN DAMAGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 145AW 20194 DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT AT DOOR L-2 DAMAGED. REPLACED EMERGENCY LIGHT ASSEMBLY, OP S CHECK GOOD, STC - SA3432NM. 2 L 7 2 4F A16WE 1997010200560 19970102 00560 WP 1997 1 2 CALA9601883 1 19961227 A 2822 7934123525 CONDUIT DOUG DC9 DC981 3022081 WP RT WING DAMAGED A A CALA O OTHER O OTHER TO TAKEOFF 1 SW 09 16883 48073 THE RT WING FORWARD FUEL TANK BOOST PUMP CIRCUIT BREAKERS POPPED AFTER TAKEOFF. THE CIRCUIT BREAKERS WERE RESET AND THE REAR FUEL TANK BOOST PUMP CIRCUIT BREAKER POPPED IMMEDIATELY. THE FORWARD BOOST PUMP CIRCUIT BREAKER POPPED SHORTLY AF TERWARD. THE FLIGHT CONTINUED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE A AND C PHASE CIRCUIT BRE AKERS POPPED ON FORWARD PUMP AND THE B-PHASE CIRCUIT BREAKER POPPED ON AFT PUMP. THE ELECTRICAL CONNECTORS FOR BOTH RT WING BOOST PUMPS SHOWED EVIDENCE OF ARCING AND INSULATION DAMAGE. THE ELECTRICAL CONDUITS FOR BOTH BOOST PUMPS WERE REM OVED AND REPLACED. IN ADDITION, BOTH BOOST PUMPS WERE REMOVED AND REPLACED, LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F A6WE 1997010200561 19970102 00561 NM 1997 1 2 CALA9601884 1 19961228 A 2910 651784938 HYD LINE BOEING 727 727232 1384082 NM B-HYD SYST LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 14788 20642 BOTH B-SYSTEM LOW PRESSURE LIGHTS ILLUMINATED WITH B-SYSTEM SHOWING ONE GALLON IN RESERVOIR DURING CRUISE PORTION OF FLI GHT. THE A-SYSTEM SHOWED 3 GALLONS AND WENT TO 2.25 GALLONS OVER THE NEXT 1.5 HOURS. THE FLIGHT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND HYDRAULIC RETURN LINE IN HYDRAULIC BAY LEAKING. THE HYDRAULIC RETURN LINE WAS REMOVED AND REPLACED. IN ADDITION, BOTH THE NR 1 AND NR 2 ELECTRIC B-PUMPS WERE REMOVED AND REPLACED. THE HYDRAULIC SYSTEM WAS SER VICED TO FULL, LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 3 4F A3WE 1997010200562 19970102 00562 WP 1997 1 2 CALA9601885 1 19961209 A 5712 RIB DOUG DC9 DC932 3022066 WP WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17531 45847 INSPECTION FOUND OUTBOARD WING TRAILING EDGE RIB, NR 3 FROM INBOARD END CRACKED .5 INCH AT FORWARD END UPPER SKIN. A RE PAIR DOUBLER WAS INSTALLED IAW SRM 57-01, FIGURE 2. 2 L 7 2 4F A6WE 1997010200563 19970102 00563 WP 1997 1 2 CALA9601886 1 19961213 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 948 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17531 45847 INSPECTION FOUND RIVETS POPPED AND FUSELAGE SKIN CORRODED AT STA 948. THE LAST THREE INCHES OF L22R WAS CORRODED THROUG H. THE LONGERON WAS REMOVED AND REPLACED AND THE SKIN WAS REPAIRED IAW SRM 53-02, FIGURE 2A. 2 L 7 2 4F A6WE 1997010200564 19970102 00564 WP 1997 1 2 CALA9601887 1 19961211 A 5753 CHORD DOUG DC9 DC932 3022066 WP LT TE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17531 45847 INSPECTION FOUND A 3 INCH CRACK IN RADIUS OF LT FLAP TRAILING EDGE UPPER CHORD NEAR INBOARD EDGE OF FLAP. THE AREA WAS REPAIRED IAW ECRA 5710-01768. 2 L 7 2 4F A6WE 1997010200565 19970102 00565 WP 1997 1 2 CALA9601888 1 19961127 A 5711 SPAR WEB DOUG DC9 DC932 3022066 WP WS 58 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17531 45847 INSPECTION FOUND A 2 INCH CRACK IN OUTBOARD RADIUS OF RT WING TRAILING EDGE REAR SPAR WEB AT STA XCW 58. THE AREA WAS R EPAIRED IAW DOUGLAS DRAWING 593528. 2 L 7 2 4F A6WE 1997010200566 19970102 00566 WP 1997 1 2 CALA9601889 1 19961206 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 980 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17531 45847 INSPECTION FOUND A 4 INCH CRACK IN INBOARD RADIUS AT STA 980, LONGERON 17L. A REPAIR WAS INSTALLED IAW SRM 53-03. 2 L 7 2 4F A6WE 1997010200567 19970102 00567 WP 1997 1 2 CALA9601890 1 19961204 A 5312 BULKHEAD CAP DOUG DC9 DC932 3022066 WP BS 996 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17531 45847 INSPECTION FOUND T-CAP CORRODED AFT OF AFT PRESSURE BULKHEAD AT STA 996, LONGERON 28R. A NEW T-CAP SECTION WAS INSTALLE D IAW SRM 53-03, FIGURE 37. 2 L 7 2 4F A6WE 1997010200568 19970102 00568 WP 1997 1 2 CALA9601891 1 19961203 A 5312 BULKHEAD CAP DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17531 45847 INSPECTION FOUND A .5 INCH CRACK IN AFT PRESSURE BULKHEAD T-CAP AT RT LAV NEAR STRINGER 34 AND A .5 INCH CRACK IN T-CAP AT RT LAV NEAR STRINGER 14. A REPLACEMENT SECTION OF T-CAP WAS SPLICED IN AT EACH LOCATION IAW SRM 53-03, FIGURE 37 AND ECRA 5310-03392. 2 L 7 2 4F A6WE 1997010200569 19970102 00569 WP 1997 1 2 CALA9601892 1 19961225 A 3246 LM328448 BEARING DOUG DC10 DC1010 3022110 WP RT MLG FAILED A CALA O OTHER O OTHER LD LANDING 1 SW 09 68047 47801 THE AIRCRAFT LANDED AT NRT WITH THE RT MLG NR 4 WHEEL/TIRE ASSEMBLY MISSING. THE AIRCRAFT LANDED SAFELY. THE RT MLG TR UCK ASSEMBLY WAS REPLACED DUE TO NR 4 AXLE DAMAGE. THE NR 4 BRAKE ASSEMBLY WAS REPLACED DUE TO DAMAGE CAUSED BY DEPARTU RE OF NR 4 WHEEL ASSEMBLY. A TIRE AND WHEEL ASSEMBLY WAS INSTALLED IN THE NR 4 POSITION. IN ADDITION, THE NR 3, 7 AND 8 WHEEL ASSEMBLIES WERE REPLACED DUE TO OVERLOAD. *S/D* ENGINEERING CONCLUDED THAT THE LOSS OF THE RT MLG NR 4 WHEEL/ TIRE ASSEMBLY WAS DUE TO BEARING FAILURE. 2 L 7 3 4F A22WE 1997010200570 19970102 00570 WP 1997 1 2 9627049301 1 19961225 A 7711 EPR TRANSMITTER DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE NR 1 ENGINE FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 301RC 48054 708402 AS TAKEOFF POWER WAS APPLIED, THE NR 1 ENGINE EPR INDICATION WAS LOW. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. M AINTENANCE REPLACED THE RIGHT ENGINE EPR TRANSMITTER AND PROBLEMS CONTINUED. THE AIRCRAFT WAS BROUGHT TO THE HANGAR. T HE PT7 LINES WERE FOUND TO HAVE CONTAINED WATER. THE WATER WAS DRAINED AND ENGINE OPERATIONAL CHECK WAS OK. SUSPECT IC ING OF THE PT7 LINES. 2 L 7 2 4F 4 F A6WE E9NE 1997010200571 19970102 00571 NM 1997 1 2 9627052716 1 19961222 A 2710 65217097 CASTING BOEING 727 7272S7 138407Z NM LT AILERON FAILED A A NWAA A J UNSCHED LANDING DUMP FUEL F FLT CONT AFFECTED CL CLIMB 1 GL 01 720RC 22491 DURING CLIMB AIRFRAME STARTED TO BUFFET. A VISUAL INSPECTION OF THE WINGS SHOWED THE INBOARD AILERONS FLUTTERING ABOUT TWO INCHES IN MOVEMENT ON BOTH WINGS. AIRCRAFT DUMPED FUEL AND RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED L EFT HAND AILERON BELL CRANK HINGE TRUNNION CASTING AND QUADRANT BRACKET, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1997010200572 19970102 00572 NE 1997 1 2 9627062288 2 19961226 A 7230 COMPRESSOR BOEING 727 727251 138408H NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE FOD A NWAA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 01 288US 21376 695252 DURING CRUISE AT FLIGHT LEVEL 31, THE NUMBER TWO ENGINE EXPERIENCED COMPRESSOR STALLS. CREW REDUCED THE NUMBER TWO ENGI NE POWER TO IDLE, RETURNED TO MSP AND LANDED WITHOUT FURTHER INCIDENT. THE ENGINE WAS SHUTDOWN AFTER LANDING. MAINTENA NCE FOUND A PIECE OF DELAMINATED FIBERGLASS FROM THE UPPER VHF ANTENNA LOGGED ACROSS THE NUMBER TWO ENGINE STATOR VANES. ENGINE DEBRIS WAS REMOVED, THE PS3 FILTER AND 8TH, 13TH STAGE END CAPS WERE CHECKED FOR DEBRIS. THE ENGINE WAS RUN AT TAKEOFF POWER AND ALL PARAMETERS WERE NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1997010200573 19970102 00573 NM 1997 1 2 9627072768 1 19961218 A 3350 LIGHT BOEING 727 7272M7 138407S NM CABIN INOPERATIVE A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 728RW 21741 DURING PREFLIGHT, FOUND OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1997010200574 19970102 00574 NM 1997 1 2 9627082298 1 19961218 A 3350 BATTERY BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 298US 22152 DURING PREFLIGHT, FOUND EMERGENCY LIGHT BOTTOM OF AFT AIR STAIRS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1997010200575 19970102 00575 WP 1997 1 2 9627099911 1 19961228 A 3350 CONNECTOR DOUG DC9 DC931 3022065 WP CABIN DAMAGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 961N 47405 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, NO HELP. R EPAIRED BAD CONNECTOR BEHIND SIDEWALL, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1997010200576 19970102 00576 WP 1997 1 2 9627109940 1 19961228 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 3322L 47031 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERA TIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1997010200577 19970102 00577 1997 1 2 9627119950 4 19961228 A 2565 13621224 SLIDE DOUG DC9 DC932 3022066 WP TAILCONE LOW PRESSURE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9346 21766 2433 47376 DURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE EVACUATION SLIDE PRESSURE LOW. REPLACED SLIDE. 2 L 7 2 4F A6WE 1997010200578 19970102 00578 WP 1997 1 2 9627129970 1 19961229 A 3350 60030451 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9334 47247 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS AT ROW 12 AND 14 INOPERATIVE. REPLACED BATTERY PACK , OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1997010200579 19970102 00579 WP 1997 1 2 9627139992 1 19961228 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8960E 45869 DURING PERIODIC CHECK, TAIL COMPARTMENT OVERHEAD AND BOTH NACELLE EMERGENCY LIGHTS FAILED TEN MINUTE TEST. REPLACED BAT TERIES IN TAIL COMPARTMENT PACKS AND REPLACED BATTERY PACKS FOR NACELLE LIGHTS, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1997010200580 19970102 00580 NM 1997 1 2 9627146308 1 19961225 A 3350 CONNECTOR BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 668US 24223 DURING LINE CHECK, FOUND FLOOR EMERGENCY LIGHTS INOPERATIVE FROM ROWS 12AB TO 14AB. RECONNECTED PIN AT CONNECTOR, OPERA TIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1997010200581 19970102 00581 WP 1997 1 2 9627159992 1 19961228 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8960E 45869 DURING PERIODIC CHECK, OVERWING EXIT EMERGENCY LIGHTS AT ROW 11 FAILED TEN MINUTE TEST. REPLACED BATTERIES IN PACK, OPE RATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1997010200582 19970102 00582 NE 1997 1 2 9627169989 2 19961228 A 7320 FUEL CONTROL DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7 52053 NE NR 1 ENGINE OUT OF TRIM A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 01 8945E 47181 654682 AS TAKEOFF POWER WAS APPLIED THE NUMBER ONE ENGINE EPR INDICATION WOULD NOT REACH TARGET EPR SETTING. CREW ABORTED TAKE OFF AND RETURNED TO GATE. MAINTENANCE TRIMMED THE NUMBER ONE ENGINE FUEL CONTROL AND DRAINED THE MOISTURE TRAP, OPERATI ONAL CHECK WAS OK. 2 L 7 2 4F 4 F A6WE E2EA 1997010200583 19970102 00583 NE 1997 1 2 9627179989 2 19961229 A 7261 FILTER DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7 52053 NE LT ENGINE CLOGGED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 8945E 47181 654682 DURING TAKEOFF ROLL, THE LEFT ENGINE OIL STRAINER LIGHT ILLUMINATED. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINTE NANCE REPLACED LEFT ENGINE OIL FILTER, OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F A6WE E2EA 1997010200584 19970102 00584 NE 1997 1 2 9627189989 2 19961229 A 7261 FILTER DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7 52053 NE RT ENGINE CLOGGED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 8945E 47181 655196 DURING TAKEOFF ROLL, THE RIGHT ENGINE OIL STRAINER LIGHT ILLUMINATED. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINT ENANCE REPLACED RIGHT ENGINE OIL FILTER, OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F A6WE E2EA 1997010200585 19970102 00585 NM 1997 1 2 9627196730 1 19961228 A 7830 POWER DRIVE UNIT BOEING 747 7472J9F 1384806 NM NR 3 ENGINE FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 630US 21668 DURING TAKEOFF ROLL, ENGINE NR 3 REVERSER UNLOCK LIGHT ILLUMINATED. TAKEOFF ABORTED AT 80 KNOTS. GROUND MAINTENANCE FO UND POWER DRIVE UNIT INOPERATIVE, SYSTEM PLACED ON MEL. 2 L 7 4 4F RT A20WE 1997010200586 19970102 00586 WP 1997 1 2 9627201153 1 19961228 A 7830 REVERSER SYSTEM DOUG DC10 DC1040 3023508 WP NR 2 ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 153US 46762 DURING TAKEOFF ROLL, ENGINE NR 2 AMBER REVERSE UNLOCK LIGHT ANNUNCIATED. TAKEOFF ABORTED AT 120 KNOTS. MAINTENANCE PER FORMED REJECTED TAKEOFF INSPECTION, NO DAMAGE FOUND. REVERSER ON MEL. 2 L 7 3 4F A22WE 1997010200587 19970102 00587 NM 1997 1 2 9627216716 1 19961228 A 3510 831SG25020R TRANSDUCER BOEING 747 747251F 1384898 NM CREW OXY SYST MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 01 616US 16772 5327 21120 DURING CRUISE, THE FLIGHT CREW OXYGEN GAUGE INDICATED ZERO. AIRCRAFT RETURNED TO SFO AND LANDED WITHOUT INCIDENT. REPL ACED THE OXYGEN PRESSURE TRANSDUCER, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1997010200588 19970102 00588 WP 1997 1 2 9627229935 1 19961227 A 3610 CLAMPS DOUG DC9 DC931 3022065 WP TAIL COMPARTMENT LOOSE A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 1332U 47404 TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED APPROXIMATELY TEN MINUTES AFTER TAKEOFF. LIGHT EXTINGUISHED AFTER B LEEDS WERE TURNED OFF. FLIGHT RETURNED TO ATL AND LANDED WITHOUT INCIDENT. MAINTENANCE TIGHTENED CLAMPS TO LEFT AUGMEN TATION VALVE AND REPLACED CLAMP AT TURBINE OUTLET, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1997010200589 19970102 00589 WP 1997 1 2 9627239933 1 19961228 A 3260 DOWNLOCK DOUG DC9 DC931 3022065 WP NLG MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 GL 01 1334U 47280 DURING APPROACH, NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. RED UNSAFE LIGHT WAS OUT. RECY CLED GEAR AND NORMAL INDICATIONS WERE ACHIEVED. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE REPAIR ED BROKEN WIRE G200L24 AT SPLICE IN NOSE WHEEL WELL. ALSO, REPLACED NOSE GEAR UPLIMIT SWITCH AND DIMMING BOX, OPERATIO NAL CHECK NORMAL ON GEAR SWING. 2 L 7 2 4F A6WE 1997010200590 19970102 00590 SO 1997 1 2 COMA9610423 1 19961220 A 2430 SM600BA60N1 RCCB EMB 120 EMB120RT SO COCKPIT OVERHEATED A COMA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SO 01 267CA 120259 BURNING ODOR COMING FROM PILOTS SIDE PANEL. REPLACED RCCB0217. 2 L 7 2 4T RT A31SO 1997010200591 19970102 00591 SO 1997 1 2 COMA9610424 1 19961224 A 5270 WARNING EMB 120 EMB120RT SO CARGO DOOR ACTIVATED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 161CA 120143 CARGO DOOR WARNING DURING TAKEOFF. FOUND TO BE FALSE WARNING. WARNING SYSTEM PLACED ON DEFERRED MAINTENANCE LIST. 2 L 7 2 4T RT A31SO 1997010200592 19970102 00592 SO 1997 1 2 COMA9610425 1 19961224 A 3150 ATG120TR SENSOR EMB 120 EMB120RT SO ELEVATOR DEFECTIVE A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 249CA 120239 TAKEOFF TRIM CONFIG WARNING DURING TAKEOFF. REPLACED THE ELEVATOR TRIM PROXIMITY SENSORS. 2 L 7 2 4T RT A31SO 1997010200593 19970102 00593 SO 1997 1 2 COMA9610426 1 19961225 A 5246 12047700001 DOOR EMB 120 EMB120RT SO RT WING NOT CLOSED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 249CA 120230 SERVICE DOOR WARNING DURING TAKEOFF. FOUND FUEL SERVICE DOOR OPEN. SECURED FUEL SERVICE DOOR. 2 L 7 2 4T RT A31SO 1997010200594 19970102 00594 SO 1997 1 2 COMA9610427 1 19961225 A 2916 RESERVOIR EMB 120 EMB120RT SO RT HYD SYST ICED UP A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 189CA 120189 RT HYDRAULIC RESERVOIR LOW PRESSURE WARNING LIGHT ON. THAWED ICE FROM RESERVOIR PRESSURIZATION SYSTEM. 2 L 7 2 4T RT A31SO 1997010200595 19970102 00595 NE 1997 1 2 COMA9610428 3 19961226 A 6110 8173861 BEARING RFC11AA16A EMB 120 EMB120RT SO PWA 118 PW118 NE HAMSTD 14RF 14RF9 NE PROPELLER WORN A A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 179CA 1611 1611 887215 120179 115519 910123 PROPELLER ASSEMBLY WAS ORIGINALLY REMOVED FOR ENGINE RELATED MAINTENANCE. INSPECTION REVEALED UNEVEN WEAR ON THE BLADE BEARING INSERT. WEAR HAD OCCURED IN AN OVAL FASHION AND INSERT WALL THICKNESS HAD DETERIORATED FROM ORIGINAL .100\ WITH THICKNESS RANGING FROM .069\ TO .090\. BEARINGS WERE REMOVED FROM SERVICE AND REPLACED WITH SERVICEABLE UNITS. 2 L 7 2 4T 4 T RT A31SO E20NE 6 C P11NE 1997010200596 19970102 00596 NE 1997 1 2 COMA9610429 3 19961226 A 6110 8173861 BEARING RFC11AA16A EMB 120 EMB120RT SO PWA 118 PW118 NE HAMSTD 14RF 14RF9 NE PROPELLER WORN A A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 179CA 1611 1611 887163 120179 115519 910123 PROPELLER ASSEMBLY WAS ORIGINALLY REMOVED FOR ENGINE RELATED MAINTENANCE. INSPECTION REVEALED UNEVEN WEAR ON THE BLADE BEARING INSERT. WEAR HAD OCCURED IN AN OVAL FASHIION AND INSERT WALL THICKNESS HAD DETERIORATED FROM ORIGINAL .100\ WIT H THE THICKNESSES RANGING FROM .076\ TO .088\. BEARINGS WERE REMOVED FROM SERVICE AND REPLACED WITH SERVICEABLE UNITS. 2 L 7 2 4T 4 T RT A31SO E20NE 6 C P11NE 1997010200597 19970102 00597 NE 1997 1 2 COMA9610430 3 19961226 A 6110 8173861 BEARING RFC11AA16A EMB 120 EMB120RT SO PWA 118 PW118 NE HAMSTD 14RF 14RF9 NE PROPELLER WORN A A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 179CA 1611 1611 887208 120179 115519 910123 PROPELLER ASSEMBLY WAS ORIGINALLY REMOVED FOR ENGINE RELATED MAINTENANCE. INSPECTION REVEALED UNEVEN WEAR ON THE BLADE BEARING INSERT. WEAR HAD OCCURED IN AN OVAL FASHION AND INSERT WALL THICKNESS HAD DETEIORATED FROM ORIGINAL .100\ WITH THE THICKNESSES RANGING FROM .073\ TO .086\. BEARINGS WERE REMOVED FROM SERVICE AND REPLACED WITH SERVICEABLE UNITS. 2 L 7 2 4T 4 T RT A31SO E20NE 6 C P11NE 1997010200598 19970102 00598 EU 1997 1 2 COMA9630165 1 19961224 A 3020 CONNECTOR SAAB SF340 SF340A 7850100 EU RT ENGINE LOOSE A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 356CA 340A034 RT ENGINE INLET ANTI-ICE WARNING ILLUMINATED. SECURED LOOSE WIRING CONNECTOR AT ENGINE INLET. 2 L 7 2 4T RT A52EU 1997010200599 19970102 00599 NE 1997 1 2 COMA9630166 3 19961226 A 6111 6607132886 BLADE R3894123F25 SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE ROTOL R389 R3894123F25 NE PROPELLER CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 359CA 18623 3553 DRG277184 340A053 367181 DRG277184 PROPELLER ASSEMBLY ORIGINALLY REMOVED FOR EXCESSIVE GREASE LEAK. UPON DISASSEMBLY AND INSPECTION A CRACK WAS OBSERVED I N THE BLADE ROOT OUTER SLEEVE. CRACK IS APPROXIMATELY 6 INCHES IN LENGTH AND HAS BEEN CONFIRMED BY DYE PENETRANT INSPEC TION. BLADE HAS BEEN REMOVED FROM SERVICE AT THIS TIME. 2 L 7 2 4T 4 T RT A52EU E8NE6 6 C P30NE 1997010200600 19970102 00600 EA 1997 1 2 COMA9660232 1 19961224 A 2760 ECU CNDAIR CL600 CL6002B19 EA FLIGHT SPOILERS TRIPPED A COMA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 01 927CA 7031 FLIGHT SPOILERS CAUTION MESSAGE ON EICAS. RESET THE SPOILER ELECTRONIC CONTROL UNITS. COULD NOT DUPLICATE, SYSTEM FUNC TION TEST SATISFACTORY. 2 L 7 2 4F RT A21EA 1997010200601 19970102 00601 EA 1997 1 2 COMA9660233 1 19961224 A 3010 DE-ICE FLUID CNDAIR CL600 CL6002B19 EA WINGS SMOKING A COMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 963CA 7127 PASSENGER REPORTED SMOKE COMING FROM WINGS. SMOKE FOUND TO BE DE-ICING FLUID EVAPORTING. 2 L 7 2 4F RT A21EA 1997010200602 19970102 00602 EA 1997 1 2 COMA9660234 1 19961221 A 3220 16400103 DRAG BRACE CNDAIR CL600 CL6002B19 EA NLG FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 941CA 7050 WHEN LANDING GEAR SELECTED UP, THE NLG DID NOT RETRACT. REPLACED THE NLG DRAG BRACE. 2 L 7 2 4F RT A21EA 1997010200603 19970102 00603 EA 1997 1 2 COMA9660235 1 19961225 A 2760 ECU CNDAIR CL600 CL6002B19 EA SPOILERS TRIPPED A COMA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 01 951CA 7091 SPOILERS CAUTION MESSAGE DURING TAXI. RESET THE SPOILER ELECTRONIC CONTROL UNITS. COULD NOT DUPLICATE DISCREPANCY. 2 L 7 2 4F RT A21EA 1997010200604 19970102 00604 1997 1 2 COMA9660236 4 19961222 A 3417 8220372115 ADC CNDAIR CL600 CL6002B19 EA NR 1 MALFUNCTION A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 916CA 7589 4016 7014 ALTITUDE ALERT AURAL WARNING ON DURING FLIGHT, WILL NOT TURN OFF. REPLACED THE NR 1 ADC. 2 L 7 2 4F RT A21EA 1997010200605 19970102 00605 EA 1997 1 2 COMA9660237 1 19961226 A 2840 7366437 FUEL COMPUTER CNDAIR CL600 CL6002B19 EA E/E COMPT INOPERATIVE A COMA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 916CA 7738 7014 AFTER TAKEOFF, FUEL IMBALANCE MESSAGE CAME ON. REPLACED FUEL COMPUTER, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 1997010200606 19970102 00606 NM 1997 1 2 SWAA961401 1 19961222 A 3234 189929 PROX SWITCH BOEING 737 7373A4 1384585 NM LANDING GEAR FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 07 678AA 23290 AFTER TAKEOFF, LANDING GEAR HANDLE WOULD NOT RISE PAST THE OFF POSITION. CREW USED OVERRIDE TO RAISE GEAR. WARNING HOR N SOUNDED WITH FLAPS UP, PRESSURIZATION AND ALL OTHER INDICATIONS NORMAL. DIVERTED TO PHX AND MADE AN UNEVENTFUL LANDIN G. FOUND DEFECTIVE AIR/GROUND SENSING PROXIMITY SWITCH. REPLACED SWITCH AND PERFORMED GEAR RETRACTION TEST PER BOEING M/M. 2 L 7 2 4F RT A16WE 1997010200607 19970102 00607 NM 1997 1 2 SWAA961402 1 19961220 A 3350 P4010021 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 20SW 21337 DURING SCHEDULED SERVICE CHECK, FOUND FWD F/A STATION EMERGENCY FLASHLIGHT NOT TESTING. REPLACED BATTERY PER BOEING M/M . 2 L 7 2 4F A16WE 1997010200608 19970102 00608 NM 1997 1 2 SWAA961403 1 19961220 A 5312 BULKHEAD SKIN BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 23SW 21339 DURING SCHEDULED 1/2 D-CHECK, FOUND BS 178 BULKHEAD WEB SKIN CRACKED UNDERNEATH REINFORCEMENT CHANNEL. INSTALLED REPAIR DOULBER PER BOEING SRM. 2 L 7 2 4F A16WE 1997010200609 19970102 00609 NM 1997 1 2 SWAA961404 1 19961223 A 5330 SKIN BOEING 737 7372T4 1384492 NM SERV DR CUTOUT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR CRACKED AT LOWER HINGE CUTOUT. INSTALLED REPAIR PER BOEING SRM. 2 L 7 2 4F A16WE 1997010200610 19970102 00610 NM 1997 1 2 SWAA961405 1 19961220 A 3241 340565 VALVE BOEING 737 7373H4 1384600 NM MLG WW MALFUNCTIONED A SWAA O OTHER J WARNING INDICATION DE DESCENT 1 SW 07 314SW 23336 ON GEAR EXTENSION, ANTI-SKID INOP LIGHT ILLUMINATED. AIRCRAFT RETURNED TO STL AND MADE AN UNEVENTFUL LANDING. REMOVED PARKING BRAKE VALVE AND OP CHECKED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1997010200611 19970102 00611 NM 1997 1 2 SWAA961406 1 19961223 A 5320 DOOR FRAME BOEING 737 7373H4 1384600 NM BS 440 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED D-CHECK, FOUND DOOR FRAME CRACKED AT BS 440, RBL 38, WL 159. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1997010200612 19970102 00612 NM 1997 1 2 SWAA961407 1 19961223 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 440 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED D-CHECK, FOUND FUSELAGE WEB GOUGED AND DENTED AT BS 440, RBL 26, WL 156. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1997010200613 19970102 00613 NM 1997 1 2 SWAA961408 1 19961223 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 500-515 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 500 PLUS 15, BELOW STRINGER 16L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1997010200614 19970102 00614 NM 1997 1 2 SWAA961409 1 19961223 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 211 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 211, 6 INCHES FROM NOSE GEAR DOOR CUTOUT. REPAIRED PER BOEIN G SRM. 2 L 7 2 4F RT A16WE 1997010200615 19970102 00615 NM 1997 1 2 SWAA961410 1 19961223 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 420 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 420 PLUS 1, BELOW STRINGER 20R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1997010200616 19970102 00616 NM 1997 1 2 SWAA961411 1 19961223 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 344 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 344, 5 INCHES FROM E AND E COMPT DOOR, BELOW S26L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1997010200617 19970102 00617 NM 1997 1 2 SWAA961412 1 19961223 A 5314 KEEL BEAM BOEING 737 7373H4 1384600 NM BS 724/721/713 CRACK/CORR A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED D-CHECK, FOUND CRACKING AND CORROSION ON CORRUGATED PLATES, ON TOP OF KEEL BEAM AT BS 724, 721, AND 713 , BL 0, WL 155. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1997010200618 19970102 00618 NM 1997 1 2 SWAA961413 1 19961223 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 500 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 500B PLUS 6, BELOW S16R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1997010200619 19970102 00619 NM 1997 1 2 SWAA961414 1 19961223 A 5320 STRAP BOEING 737 7373H4 1384600 NM BS 774-858 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED D-CHECK, FOUND AFT CARGO BAY DOOR CUTOUT LOWER BEAM STRAP CORRODED AT BS 774 TO 858, WL 162 TO 157. RE PLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1997010200620 19970102 00620 NM 1997 1 2 SWAA961415 1 19961223 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED D-CHECK, FOUND BS 178 PRESSURE WEBS CRACKED AT WL 198, LBL 4.7, AND AT WL 212.5, LBL 4 AND 7. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1997010200621 19970102 00621 NM 1997 1 2 SWAA961416 1 19961225 A 2150 6937319148 AC MODULE BOEING 737 7373H4 1384600 NM COCKPIT MALFUNCTIONED A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 368SW 26579 DIVERTED TO OAK DUE TO ELECTRICAL SMELL, NO SMOKE NOTED, EMITTING FROM F/O OVERHEAD AREA. LANDED WITHOUT INCIDENT. INS PECTED P5 OVERHEAD PANEL AREA. REPLACED AC MODULE PER BOEING M/M. 2 L 7 2 4F RT A16WE 1997010200622 19970102 00622 1997 1 2 SWAA961417 4 19961225 A 3414 208311 INDICATOR BOEING 737 7373H4 1384600 NM LT COCKPIT FAILED A SWAA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 634SW 27939 DIVERTED TO PHX DUE TO CAPT AIRSPEED INDICATOR FAILURE. REPLACED INDICATOR PER BOEING M/M. 2 L 7 2 4F RT A16WE 1997010200623 19970102 00623 NM 1997 1 2 SWAA961418 1 19961224 A 3350 CONNECTORS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 635SW 23938 ON ARRIVAL, FOUND 5 ROWS OF EMERGENCY EXIT LIGHT INOP AND WIRES DISCONNECTED. RECONNECTED EMERGENCY LIGHT SEGMENT CONNE CTOR PINS AND OP CHECKED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1997010200624 19970102 00624 NM 1997 1 2 SWAA961419 1 19961221 A 2450 912522C7C4001 RELAY BOEING 737 7373H4 1384600 NM E/E COMPT FAILED A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 673AA 23251 RETURNED TO MCI DUE TO NUMBER 1 TRANSFER C/B TRIPPING IN FLIGHT. REPLACED R3 RELAY AND OP CHECKED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1997010200625 19970102 00625 NM 1997 1 2 SWAA961420 1 19961219 A 2150 PACK BOEING 737 7373G7 1384595 NM RIGHT FAILED A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 360SW 24008 INFLIGHT, RT PACK TRIPPED OFF, ATTEMPTED TO RESET, NO HELP. TRIPPED AGAIN AND NOTED LIGHT SMOKE. AIRCRAFT RETURNED TO LAS AND MADE AN UNEVENTFUL LANDING. CHECKED SYSTEM FOR LEAKS, RT AIR CYCLE MACHINE, TURBO FAN AND ALL RELATED PACK COMP ONENTS AND OPERATED PACK NORMALLY PER BOEING M/M. 2 L 7 2 4F RT A16WE 1997010200626 19970102 00626 NM 1997 1 2 SWAA961421 1 19961222 A 2150 PACK BOEING 737 7373G7 1384595 NM RIGHT FAILED A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 683SW 24008 INFLIGHT, RT PACK TRIPPED OFF ALONG WITH A SMOKE SMELL. ISOLATED TO RIGHT PACK, LEFT PACK CLEARED SMELL. AIRCRAFT RETU RNED TO BNA AND MADE AN UNEVENTFUL LANDING. REPLACED COMPRESSOR DISCHARGE, TURBINE INLET AND DUCT OVERHEAT SENSORS PER BOEING M/M. 2 L 7 2 4F RT A16WE 1997010200627 19970102 00627 NM 1997 1 2 SWAA961422 1 19961220 A 5315 FLOORBEAM BOEING 737 7373T5 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED C1 CHECK, FOUND FLOORBEAM STRAP CRACKED UNDERNEATH FWD ENTRY DOOR. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1997010200628 19970102 00628 NM 1997 1 2 SWAA961423 1 19961220 A 5315 FLOORBEAM BOEING 737 7373T5 NM BS 312 BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED C1 CHECK, FOUND FLOORBEAM STRAPS BROKEN AND CRACKED ABOVE AIRSTAIR SHROUD AT BS 312, BL 0 AND BL 12. R EPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1997010200629 19970102 00629 NM 1997 1 2 SWAA961424 1 19961220 A 5315 FLOORBEAM BOEING 737 7373T5 NM BS 328 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED C1 CHECK, FOUND FLOORBEAM STRAP CRACKED ABOVE AIRSTAIR SHROUD AT BS 328, LBL 12 AND 33. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1997010200630 19970102 00630 NM 1997 1 2 SWAA961425 1 19961226 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 423 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 342SW 24133 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 423, AT S18R. REPAIRED PER SWA RA 1-353-1575. 2 L 7 2 4F RT A16WE 1997010200631 19970102 00631 NM 1997 1 2 SWAA961426 1 19961226 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 920 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 920, AT S23R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1997010200632 19970102 00632 EU 1997 1 2 WWMA9600109 1 19961226 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT DEFECTIVE A WWMA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 WP 15 261AE 340B261 WHILE GETTING READY TO TAXI, THE CARGO SMOKE LIGHT ILLUMINATED FOR A SECOND. THE SMOKE TEST FUNCTION CHECKED GOOD. MAI NTENANCE REPLACED BOTH CARGO SMOKE DETECTORS. 2 L 7 2 4T RT A52EU 1997010200633 19970102 00633 EU 1997 1 2 QXEA9600500 1 19961226 A 3350 6008905 BATTERY PACK FOKKER FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 484US 11234 CABIN EMERGENCY LIGHTS FROM ROW 11 AFT ARE INOP. POWER SUPPLY REPLACED AND LIGHTS OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1997010200634 19970102 00634 EU 1997 1 2 QXEA9600501 1 19961229 A 4920 APU FOKKER F28 F28MK1000 4990808 EU APU COMPT MALFUNCTIONED A QXEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 09 457US 11036 CABIN FILLED WITH SMOKE AFTER DEPARTURE. AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT FURTHER PROBLEM. PROBLEM TRACED TO OIL IN THE CABIN PACK FROM THE APU. PACK AND APU PLACED ON MEL 21-1 AND 49-1. 2 L 7 2 4F RT A20EU 1997010200635 19970102 00635 NM 1997 1 2 96FDEA01710 1 19961227 A 3260 GEAR LIGHT BOEING 727 727116 1384043 NM RT MLG FAILED A FDEA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 SO 25 115FE 19814 ON APPROACH, THE RIGHT MAIN GEAR GREEN LIGHT FAILED TO ILLUMINATE. MISSED APPROACH CALLED OUT AND MANUAL GEAR EXTENSION WITH NO RIGHT GREEN LIGHT STILL A FLY-BY WAS DONE AND THE RIGHT GEAR DID APPEAR TO BE DOWN. ON THE MISSED APPROACH THE GEAR WAS RETRACTED AND A SECOND MANUAL EXTENSION DONE WITH A GREEN DOWN LIGHT ILLUMINATING THIS TIME FOLLOWED BY A NORM AL LANDING AND ROLL OUT. INSPECTED DOWN AND LOCK SWITCH, SPRAYED CANNON PLUG WITH CONTACT CLEANER, CHECKED SERVICEABLE. 2 L 7 3 4F A3WE 1997010200636 19970102 00636 NM 1997 1 2 96FDEA01711 1 19961226 A 5610 PPG5893543095 WINDSHIELD BOEING 727 727227 1384078 NM LT COCKPIT CRACKED A FDEA A I UNSCHED LANDING CABIN DEPRESSURIZATION O OTHER CR CRUISE 1 SO 25 490FE 21493 AT FLIGHT LEVEL 330, CAPTAIN'S OUTER WINDSHIELD L1 CRACKED ABRUPTLY. FOLLOWED RED TAB PROCEDURES, DESCENDED TO FLIGHT L EVEL 240 AND REDUCED CABIN PRESSURE. REMOVED AND REPLACED L1 WINDSHIELD PER MAINTENANCE MANUAL 56-11-11. ALSO, REMOVED AND REPLACED HEAT CONTROLLER. REINSTALLED ALL MOLDING AND OK FOR SERVICE. 2 L 7 3 4F A3WE 1997010200637 19970102 00637 NM 1997 1 2 96FDEA01709 1 19961227 A 5312 AYG72341 BULKHEAD FITTING DOUG MD11 MD11F 3023600 NM BS 1453 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 611FE 48604 THE CENTER LANDING GEAR WHEEL WELL AREA HAS A CRACK AT THE RT BULKHEAD AND DRAG LINK VERTICAL SUPPORT FITTING AT STA 145 3 AT X = - 31.50 CRACK MEASURES 13 AT LOWER END OF FITTING. ADDITIONALLY, VERTICAL STIFFENERS AND DIAGONAL STIFFENER HA VE DEEP GOUGES AT STA 1461 AND 1469 RESPECTFULLY. DAMAGE APPEARS TO BE CAUSED DUE TO A BENT RT FWD DOOR ACTUATING CRANK AT DRAG LINK TUBE (P/N AYG 7234-1). *S/D* VERTICAL STIFFENER STA 1461 AND 1469 GOUGES ARE BLENDED PER SRM 53-00-01. P ERFORMED HFED INSP ON MEASURED REMAINING THICKNESS AND NO DEFECTS INDICATED. REF SRM NR 00143 AND 00141 TRIMMED CRACKED SECTION AT LOWER END. COMPLIED WITH EA 1531031789. 2 L 7 3 4F RT A22WE 1997010200638 19970102 00638 NM 1997 1 2 SCNA96454 1 19961226 A 5210 DOOR SEAL BOEING 727 7272J4 1384006 NM L2 DOOR NOT SEATED A SCNA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 285SC 21676 UNABLE TO MAINTAIN PRESSURIZATION IN AUTO, STANDBY, OR MANUAL MODE. PERFORMED ALL APPROPRIATE CHECKLISTS IN COM AND RET URNED TO SLC. CHECKED AND RESEATED L-2 DOOR, RAN ENGINE AND PRESSURIZED TO 4 PSI DIFFERENTIAL AND NO LEAKS NOTED. 2 L 7 3 4F RT A3WE 1997010200639 19970102 00639 NM 1997 1 2 SCNA96455 1 19961226 A 5610 WINDOW SEAL BOEING 727 7272J4 1384006 NM L1 WINDOW NOT SEATED A SCNA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 288SC 20765 COULD NOT HOLD PRESSURIZATION IN CABIN AT 25,000 FT, NOISE WAS HEARD AT L1 AND L2 AREA DURING CLIMBOUT. RETURNED TO LAS . RESEATED AND RETORQUED L1 WINDOW, PRESSURIZED AIRCRAFT TO 6.5 PSI IN ACCORDANCE WITH MM 21-31-0 AND NO LEAKS WERE NOT ED. 2 L 7 3 4F RT A3WE 1997010200640 19970102 00640 WP 1997 1 2 SCNA96456 1 19961226 A 5320 SCUFF PLATE DOUG DC10 DC1010 3022110 WP L2 DOOR DAMAGED A SCNA K NONE O OTHER UK UNKNOWN 1 GL 15 572SC 46977 JET BRIDGE CONTACTED AIRCRAFT ON PUSHBACK. INSTALLED TEMPORARY REPAIR ON L2 DOOR SCUFF PLATE. FERRIED TO PHX. REMOVED AND REPLACED L2 FORWARD SCUFF PLATE IN ACCORDANCE WITH MM 53-30-1. 2 L 7 3 4F A22WE 1997010300001 19970103 00001 WP 1997 1 3 CKSA96404 1 19961218 A 5230 LS154713096 SEAL LKHEED 1011 1011385115 5265015 WP CARGO DOOR DAMAGED A CKSA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 105CK 193N1178 C-4 CARGO DOOR SEAL FAILED DURING CLIMBOUT, NO FIRM CODE. RESECURED DOOR SEAL, DEFERRED PRESSURE CONTROL SYSTEM PER L-1 011 MEL 21-31-00. COMPLIED WITH SP 21-31-00. DMI NR 140. REMOVED AND REPLACED SEAL IAW L1011 MM 52-30-05 PRESSURIZATIO N CHECKS GOOD IAW L1011 MM 21-31-00. THIS CLEARS DMI NR 140. 2 L 7 3 4F A23WE 1997010300002 19970103 00002 NM 1997 1 3 CKSA96405 1 19961220 A 3232 NAS13037 BOLT BOEING 727 727251 138408H NM LT MLG WORN A CKSA O OTHER J WARNING INDICATION TO TAKEOFF 1 GL 23 255US 19974 ON TAKEOFF, LEFT MAIN GEAR SHOWED LEFT GEAR RED LIGHT AND LEFT GEAR GREEN LIGHT. CYCLED GEAR, NO HELP. ON LANDING 3 GR EEN, NO RED LIGHTS FORWARD PANEL SECONDARY GEAR INDICATION, NO GREEN ON LEFT MAIN GEAR OPERATED NORMALLY THROUGH FLIGHT. FOUND LEFT HAND MAIN LANDING GEAR DOWNLOCK SENSOR CONTROL ROD TO SENSOR ACTUATOR BOLT BACKED OFF. REPLACED HARDWARE A S REQUIRED. HARDWARE REPLACED: NAS1303-7 BOLT, NAS679A3 NUT. JACKED AIRCRAFT IAW MM 7-11, SWUNG GEAR SIX TIMES IAW MM 32-32-0, NO DEFECTS NOTED. 2 L 7 3 4F A3WE 1997010700001 19970107 00001 NM 1997 1 7 AALA961541 1 19961018 A 5311 146N1015 FRAME BOEING 757 757223 1384957 NM BS 1480 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 665AA 25299 AFW - FUSELAGE FRAME AT STATION 1480 HAS CORROSION REMOVED, REMAINING MATERIAL IS BEYOND ALLOWABLE SRM LIMITS. REPAIR P ER MRB 757-986. (M) 2 L 7 2 4F RT A2NM 1997010800001 19970108 00001 EU 1997 1 8 USAA960739 1 19961113 A 5330 SKIN FOKKER F28 F28MK0100 4990807 EU BS 24011 DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 861US 15734 11297 PIT - DURING Q-1 CHECK, FOUND SKIN DISBONDED/DELAMINATION AT STATION 24011, STRINGER RT 51. INSTALLED FASTENERS LEFT SI DE AND SKIN REPAIR RIGHT SIDE PER USAIR EA NR 33782. (M) 2 L 7 2 4F RT 1997010800004 19970108 00004 SO 1997 1 8 SWIA95792 1 19961210 A 3260 12041127001 PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO LT MLG MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 293SW 120320 LEFT MAIN GREEN 'A' LIGHT WILL NOT EXTINGUISH WITH LANDING GEAR UP. RETURNED TO FIELD. INSTALLED NEW LEFT MAIN A DOWN PROX SENSOR, SWUNG GEAR. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 1997010800005 19970108 00005 NM 1997 1 8 VNAA9612004 1 19961222 A 3231 LATCH MECH DORNER DO32 DO328100 2996000 NM HARTZL HDE6C HDE6C3B NE NLG DOOR MALFUNCTIONED A VNAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 426JS 3038 AFTER TAKEOFF, HEARD A BANGING NOISE FROM THE NOSE GEAR AREA. RETURNED TO THE FIELD WITHOUT INCIDENT. MAINTENANCE FOUND THE RT NOSE LANDING GEAR DOOR UNLATCHED. INSPECTED THE DOOR AND THE LATCHING MECHANISM AND FOUND NO DEFECTS. THE DOOR WAS SECURED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A45NM 6 C P34NE 1997010800006 19970108 00006 NE 1997 1 8 CA960729008 2 19960709 A 7532 310334701 DIAPHRAGM PWA 312124803 CESSNA 208 208B 2073701 CE PWA PT6 PT6A114 52043 NE COMP BLEED VALVE RUPTURED W A O OTHER E VIBRATION/BUFFET CR CRUISE 1 CA 499 21A026 PCE19368 (CAN) AIRCRAFT WAS BEING TROUBLESHOT FOR POOR ENGINE PERFORMANCE AND WAS BEING FERIED BACK TO MAINTENANCE BASE. DURING C RUISE THE PILOT AND ENGINEER FELT A SUDDEN SURGE AT A CONSTANT POWER SETTING. POWER WAS REDUCED AND ALL ENGINE INDICATIO NS WERE NORMAL.POST FLIGHT INSPECTION SHOWED UNUSUAL WEAR ON THE COMPRESSOR BLEED VALVE AND FOUND THE DIAPHRAGM WAS RUPT URED. 1 H 7 1 3T 3 T A37CE E4EA 1997010800008 19970108 00008 NE 1997 1 8 CA960808009 2 19960724 A 7250 BLADES CESSNA 501 501 2076603 CE PWA JT15 JT15D1 52060 NE HP TURBINE DAMAGED W A O OTHER O R OTHER PARTIAL RPM/PWR LOSS CR CRUISE 1 CA 3287 PCE76873 (CAN) PILOT REPORTED MAXIMUM POWER COULD NOT BE ACHIEVED ON #1 ENGINE AT FL330, UNLESS IGNITERS WERE TURNED ON. HOT SECT ION INSPECTION REVEALED ALL HIGH PRESSURE TURBINE BLADES WERE DAMAGED WITH SEVERAL BLADES MISSING LARGE PIECES. CAUSE AT THIS TIME IS NOT KNOWN. 1 L 7 2 4F 4 F A27CE E1NE 1997010800009 19970108 00009 EU 1997 1 8 CA960812004 1 19960809 A 2150 4754C000 HEAT EXCHANGER BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE NR 1 AIR COND CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA B5922563 LF05627A (CAN) #1 AIR CONDITIONING PACK HEAT EXCHANGER FOUND WITH 1/2 INCH CRACK IN FORWARD RIGHT HAND CORNER AND IS LEAKING AIR. 2 H 7 4 4F 4 F RT A49EU E6NE 1997010800010 19970108 00010 SO 1997 1 8 SWIA95799 1 19961223 A 2750 CONNECTOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT TE FLAP FAILED A SWIA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 NM 07 215SW 120281 FLAP DISAGREEMENT ON TAKEOFF. RETURNED TO FIELD. REPLACED CONNECTOR FOR LEFT INBOARD FLAP ACTUATOR, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1997010900001 19970109 00001 NE 1997 1 9 961209001 2 19961207 A 7200 ENGINE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9A 52048 NE NR 2 FAILED A GTIA O OTHER J WARNING INDICATION CR CRUISE 1 GL 23 12505 34443 45788 665847 DTW - FLT 626 - IN CRUISE CONFIGURATION, NR 2 THROTTLE SPLIT 3.50 INCHES WITH NR 1 THROTTLE. NR 2 EGT AND FUEL FLOW HIG H, DURING ENGINE ACCELERATION COMPRESSOR STALLS WERE EXPERIENCED ON NR 2 ENGINE. CORRECTIVE ACTION: MAINTENANCE INSPEC TED NR 2 ENGINE AND DECLARED AN ENGINE CHANGE. ENGINE REMOVED AND REPLACED WITH A SERVICEABLE ENGINE. MRR TO REMAIN OP EN UNTIL A TEAR DOWN REPORT IS RECEIVED FROM ENGINE REPAIR FACILITY. PART TOTAL CYCLES, 36,637. (X) 2 L 7 2 4F 4 F A6WE E2EA 1997010900002 19970109 00002 WP 1997 1 9 961209002 1 19961207 A 3231 RETRACT MECH DOUG DC9 DC931 3022065 WP NLG DOOR LACK OF LUBE A GTIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 934ML 47526 BUF - FLT 856 - IN CLIMB CONFIGURATION WHEN LANDING GEAR RETRACTED, A LOUD FLUCTUATING SOUND WAS PRODUCED. SOUNDED LIKE NOSE LANDING GEAR DOORS. CORRECTIVE ACTION: MAINTENANCE INSPECTED NOSE LANDING GEAR DOORS, FOUND NOT TO BE SECURED. L UBRICATED NOSE GEAR DOOR LINKAGE, AND SECURED DOORS. OPERATIONAL CHECKED GOOD IAW DC 9 MM, CHAPTER 32. (X) 2 L 7 2 4F A6WE 1997010900003 19970109 00003 WP 1997 1 9 961211001 1 19961209 A 5610 5912290501 WINDSHIELD DOUG DC9 DC931 3022065 WP LT COCKPIT FAILED A GTIA O OTHER O OTHER CR CRUISE 1 GL 23 969ML 1491 47268 DTW - FLT 634 - IN CRUISE CONFIGURATION, OBSERVED ARCING FOLLOWED BY A LARGE FLASH IN THE CAPTAIN'S WINDSHIELD. CAPTAIN 'S WINDSHIELD CIRCUIT BREAKER'S TRIPPED. CORRECTIVE ACTION: MAINTENANCE REMOVED AND REPLACED THE CAPTAIN'S WINDSHIELD AND WINDSHIELD TEMP CONTROLLER. SYSTEM OPERATIONAL CHECKED IAW DC 9 MM, CHAPTERS 56-10, 30, 40. AIRCRAFT RETURNED TO S ERVICE. (X) 2 L 7 2 4F A6WE 1997010900004 19970109 00004 NM 1997 1 9 GAIA9641 1 19961212 A 2611 SMOKE DETECTOR BOEING 727 727251 138408H NM CARGO COMPT MALFUNCTIONED A GAIA O OTHER N FALSE WARNING DE DESCENT 1 SW 07 279US 21158 STL/SJC - FLT 712 - DURING DESCENT INTO SJC; CARGO COMPARTMENT SMOKE DETECTOR ILLUMINATED. VISUALLY VERIFIED NO SMOKE P RESENT IN CARGO CABIN. LIGHT WENT OUT AFTER 10 MINUTES. AGAIN DURING SHORT FINAL APPROACH SMOKE DETECTOR ILLUMINATED. AGAIN VERIFIED VISUALLY NO SMOKE IN CARGO CABIN. (X) 2 L 7 3 4F A3WE 1997010900005 19970109 00005 NM 1997 1 9 GAIA9642 1 19961211 A 2611 302842 SMOKE DETECTOR BOEING 727 727251 138408H NM CABIN INTERMITTENT A GAIA O OTHER N FALSE WARNING DE DESCENT 1 SW 07 279US 1200 21158 SJC/TOL - FLT 711 - CARGO COMPARTMENT SMOKE DETECTOR ILLUMINATED. MAINTENANCE REPLACED NR 5 SMOKE DETECTOR. SYSTEM OPS CK NORMAL. (X) 2 L 7 3 4F A3WE 1997010900006 19970109 00006 NM 1997 1 9 GAIA9643 1 19961212 A 2611 30303A SMOKE DET AMP BOEING 727 727251 138408H NM E/E COMPT FAILED A GAIA O OTHER N FALSE WARNING DE DESCENT 1 SW 07 279US 21158 CARGO SMOKE LIGHT ILLUMINATED IN-FLIGHT. CHANGED SMOKE DETECTOR CONTROL AMP AND NRS 1, 2, 3, 4, AND 6 SMOKE DETECTORS. (X) 2 L 7 3 4F A3WE 1997010900007 19970109 00007 1997 1 9 EISA96283 4 19961213 A 3417 ABB43211 ADC BOEING 727 727223 1384074 NM E/E COMPT INOPERATIVE A EISA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 314NE 19495 F/O'S AIRSPEED AND ALTIMETER INTERMITTENTLY INOP. REMOVED AND REPLACED NR 2 AIR DATA COMPUTER. OPS CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1997010900008 19970109 00008 SO 1997 1 9 ASOA96054 1 19961122 A 3234 12038594001 CONTROL HANDLE EMB 120 EMB120RT SO COCKPIT DEFECTIVE A ASOA O OTHER P NO WARNING INDICATION AP APPROACH 1 SO 11 266AS 23393 1726 120188 FLT 7995 - UPON GEAR EXTENSION ON APPROACH LFT/DFW, RECEIVED NO INDICATION ON LEFT MAIN (EITHER SYSTEM) OR RIGHT MAIN (A ) SYSTEM. CREW DECLARED AN EMERGENCY AND LANDED SAFELY AT DFW WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED LANDING G EAR CONTROL HANDLE IAW MM. OPERATONAL CHECKS WERE GOOD AND AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (X) 2 L 7 2 4T RT A31SO 1997010900009 19970109 00009 SO 1997 1 9 ASOA96053 1 19961121 A 2120 AIR DISTR EMB 120 EMB120RT SO COCKPIT SMOKE A ASOA K NONE B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 11 502AS 120274 ON TAKEOFF MCN-ATL, SMOKE AND FUMES (OIL SMELL) BEGAN COMING INTO THE COCKPIT. NO PACK FAIL OVERHEAT OR BLEED LEAK NOTE D ON OVERHEAD PANEL. SMOKE EVACUATED NORMALLY AND FLIGHT CONTINUED TO ATL WHERE LANDING WAS MADE SAFELY AND WITHOUT FUR THER INCIDENT. INSPECTED AND OPERATIONALLY CHECKED PACKS IAW MM, NO DEFECTS WERE NOTED. SUSPECT SLIGHT OIL RESIDUE THA T DISSIPATED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1997010900010 19970109 00010 EU 1997 1 9 M3HA96037 1 19961204 A 3350 3011151 BATTERY AEROSP ATR42 ATR42300 8680920 EU CABIN MALFUNCTIONED A M3HA K NONE L NO TEST IN INSP/MAINT 1 WP 13 4204G 10464 061 HNL - DURING DAILY INSPECTION, EMERGENCY LIGHTS UNABLE TO TEST. REMOVED AND INSTALLED SERVICEABLE EMERGENCY BATTERY PAC K. (X) 2 H 7 2 4T RT A53EU 1997010900011 19970109 00011 NM 1997 1 9 USAA960784 1 19961207 A 5313 STRINGER BOEING 737 7372B7 1384560 NM BS 967 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 267AU 38932 22879 ROA - DURING CX-4 CHECK, VISUAL INSPECTION FOUND 2 INCH BY 12 INCH CORROSION, STR 27L, BS 967. REMOVED CORROSION AND IN STALLED DOUBLER AND SPLICED, REPAIRED PER SRM 53-10-3, FIG 1. (X) 2 L 7 2 4F A16WE 1997010900012 19970109 00012 NM 1997 1 9 USAA960769 1 19961203 A 5320 ANGLE BOEING 737 737201 1384454 NM BS 767-795 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 262AU 35743 22868 INT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND CORROSION .50 INCH BY .24 INCH CHORD ANGLE, STA 767 TO STA 795, STR 25R. INSTALLED REPAIR ANGLE, REPAIRED PER SRM 51-40-4 AND EA 41801. CORROSION TASK NR: C53-202-01. CORROSION LEVEL: 2. (X) 2 L 7 2 4F A16WE 1997010900013 19970109 00013 NM 1997 1 9 USAA960774 1 19961203 A 5320 STRAP BOEING 737 737201 1384454 NM BS 907 TORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 262AU 35743 22868 INT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND .50 INCH GOUGE AND TORN AT REINFORCEMENT STRAP STA 907, STR 20R. REPAIRE D DOUBLER, REPAIRED PER SRM 53-10-4 AND EA 41803. (X) 2 L 7 2 4F A16WE 1997010900014 19970109 00014 NM 1997 1 9 USAA960773 1 19961203 A 5330 SKIN BOEING 737 737201 1384454 NM BS 767-787 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 262AU 35743 22868 INT - DURING Q-4 CHECK, VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORROSION STA 767 TO STA 787, BL ZERO 'O' BRACKET AND SKIN. INSTALLED SKIN DOUBLER AND REPLACED BRACKET. REPAIRED PER SRM 53-30-3. (X) 2 L 7 2 4F A16WE 1997010900015 19970109 00015 NM 1997 1 9 USAA960772 1 19961203 A 5312 BULKHEAD WEB BOEING 737 737201 1384454 NM BS 1016 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 262AU 35743 22868 INT - DURING Q-4 CHECK, VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORROSION REAR PRESSURE BULKHEAD WEB LOWER EDGE BS 101 6, S23R. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-3. (X) 2 L 7 2 4F A16WE 1997010900016 19970109 00016 NM 1997 1 9 USAA960771 1 19961203 A 5320 ANGLE BOEING 737 737201 1384454 NM BS 947-986 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 262AU 35743 22868 INT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND CORROSION 1 INCH BY 40 INCH Z-ANGLE LEFT SIDE STA 947 TO STA 986. INSTA LLED REPAIR AT FORWARD SECTION OF UPPER FLANGE. REMAINDER OF CORROSION WAS MINOR, REPAIRED PER SRM 53-40-3. CORROSION TASK NR: C53-107-02. CORROSION LEVEL: 2. (X) 2 L 7 2 4F A16WE 1997010900017 19970109 00017 NM 1997 1 9 USAA960770 1 19961203 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 525 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 262AU 35743 22868 INT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND 4 INCH BY 2 INCH CORRODED STRINGER AT S28L BS 525. INSTALLED DOUBLER, R EPAIRED PER EA 41784. CORROSION TASK NR: C53-208-01. CORROSION LEVEL: 2. (X) 2 L 7 2 4F A16WE 1997010900018 19970109 00018 NM 1997 1 9 USAA960775 1 19961203 A 5311 FRAME BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 262AU 35743 22868 INT - DURING Q-4 CHECK, EDDY CURRENT INSPECTION FOUND .1250 INCH LONG CRACK FRAME CHORD STA 727 STR 18A LEFT SIDE. REPL ACED FRAME CHORD, REPAIRED PER EO 5394G068. (X) 2 L 7 2 4F A16WE 1997010900019 19970109 00019 NM 1997 1 9 USAA960783 1 19961208 A 5330 1716823 SKIN BOEING 737 737201 1384454 NM BS 767 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 244US 38924 22752 ROA - DURING A-CHECK, VISUAL INSPECTION FOUND .75 INCH CRACK LOCATED AT STA 767 AT S20R SKIN. INSTALLED DOUBLER PER SRM 53-30-3 FIG 6 PAGES 11 THROUGH 12B. (X) 2 L 7 2 4F A16WE 1997010900020 19970109 00020 NM 1997 1 9 USAA960757 1 19961127 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 302 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 37595 22886 ROA - DURING CX-3 CHECK, EDDY CURRENT INSPECTION FOUND .25 INCH CRACK IN A/C SKIN AT LOWER HINGE CUT OUT FORWARD ENTRY D OOR. BODY STA 302 - JUST ABOVE STR 13L. REMOVED CRACK AND INSTALLED DOUBLER, REPAIRED PER T/R 53-30-11. (X) 2 L 7 2 4F A16WE 1997010900021 19970109 00021 NM 1997 1 9 USAASB96221 1 19961031 A 2133 322684003 OUTFLOW VALVE BOEING 737 7372B7 1384560 NM E/E COMPT INTERMITTENT A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 270AU 16466 22882 MCO - FLT 1176 - CREW REPORTED A PRESSURIZATION PROBLEM OVER JAX. NEITHER AUTO STANDBY OR MANUAL WOULD STOP CABIN FROM CLIMBING. FLIGHT RETURNED TO FIELD AT MCO AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT SYSTEM AND FOUN D THE FORWARD OUTFLOW VALVE WORKS INTERMITTENTLY. REMOVED AND REPLACED FORWARD OUTFLOW VALVE. SYSTEM OPS CHECK GOOD. ( X) 2 L 7 2 4F A16WE 1997010900022 19970109 00022 NM 1997 1 9 USAASB96242 1 19961109 A 3230 654610912 BEAM BOEING 737 737201 1384454 NM RT MLG FRACTURED A USAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 19 264AU 34975 22961 CLT - FL 693 - CAPTAIN REPORTED THE RIGHT MAIN LANDING GEAR UPLOCK DOES NOT ENGAGE. WITH GEAR LEVER UP, RIGHT MAIN GEAR RED LIGHT IS ILLUMINATED. MOVE GEAR LEVER TO OFF, THE RIGHT MAIN GEAR COMES DOWN. FLIGHT LANDED AT CLT. MAINTENANCE FOUND THE RIGHT MAIN LANDING GEAR ACTUATOR BEAM ARM ASSEMBLY HAD FRACTURED AT THE FORWARD LUG CAUSING THE AFT LUG TO FAI L. REMOVED AND REPLACED THE ACTUATOR BEAM ARM ASSEMBLY. (M) 2 L 7 2 4F A16WE 1997010900023 19970109 00023 NM 1997 1 9 USAASB96250 1 19961202 A 2150 20405010 AIR CYCLE MACH BOEING 737 737201 1384454 NM RIGHT FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 243US 32973 22445 ORF - FLT 916 - AFTER TAKEOFF, CREW NOTED ACRID SMELL IN COCKPIT FOLLOWED BY BOTH SMOKE DETECTORS ACTIVATING. FLIGHT RE TURNED TO ORF AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE RT AIR CYCLE MACHINE. (X) 2 L 7 2 4F A16WE 1997010900024 19970109 00024 NM 1997 1 9 USAASB96244 1 19961111 A 3350 6104789 BATTERY PACK BOEING 737 7372B7 1384560 NM AFT CARGO COMPT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 278AU 22890 CLE - MAINTENANCE FOUND THE LEFT OVERWING EXTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK FOR THE LEFT OVERWING EMERGENCY EXIT LIGHTS. OPS CHECK GOOD. (X) 2 L 7 2 4F A16WE 1997010900025 19970109 00025 NM 1997 1 9 USAASB96245 1 19961125 A 7331 8DJ88LWX INDICATOR BOEING 737 7372B7 1384560 NM NR 2 ENGINE FAILED A USAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 266AU 22878 DCA - FLT 1503 - CREW REPORTED THEY OBSERVED GREEN SMOKE INSIDE THE FUEL FLOW INDICATOR GAUGE FOR THE NR 2 ENGINE FOLLOW ED BY A HEAVY ELECTRICAL SMELL. CIRCUIT BREAKER WAS PULLED AND ISOLATED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAIN TENANCE REMOVED AND REPLACED THE NR 2 ENGINE FUEL FLOW INDICATOR GAUGE AND THE TRANSMITTER. SYSTEM OPS CHECK AND LEAK C HECK GOOD. FUEL FLOW INDICATOR - PN 8DJ33LWX. FUEL FLOW TRANSMITTER - PN 85J50GBZ. REFERENCE: OPERATOR CONTROL NR 96 ZZZX6222. (X) 2 L 7 2 4F A16WE 1997010900026 19970109 00026 NM 1997 1 9 97ZZZX6222 1 19961125 A 7331 8TJ50GBZ TRANSMITTER BOEING 737 7372B7 1384560 NM NR 2 ENGINE FAILED A USAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 266AU 22878 DCA - FLT 1503 - CREW REPORTED THEY OBSERVED GREEN SMOKE INSIDE THE FUEL FLOW INDICATOR GAUGE FOR THE NR 2 ENGINE FOLLOW ED BY A HEAVY ELECTRICAL SMELL. CIRCUIT BREAKER WAS PULLED AND ISOLATED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAIN TENANCE REMOVED AND REPLACED THE NR 2 ENGINE FUEL FLOW INDICATOR GAUGE AND THE TRANSMITTER. SYSTEM OPS CHECK AND LEAK C HECK GOOD. FUEL FLOW INDICATOR - PN 8DJ33LWX. FUEL FLOW TRANSMITTER - PN 85J50GBZ. REFERENCE: OPERATOR CONTROL NR US AASB96245. 2 L 7 2 4F A16WE 1997010900027 19970109 00027 NM 1997 1 9 USAASB96247 1 19961130 A 3397 WIRE BOEING 737 737201 1384454 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 247US 22754 PHL - CABIN EMERGENCY LIGHTS ILLUMINATED AND WOULD ONLY EXTINGUISH WHEN TURNED OFF FROM THE COCKPIT. MAINTENANCE REPAIR ED WIRING AT ROW 13 LEFT. (X) 2 L 7 2 4F A16WE 1997010900028 19970109 00028 NE 1997 1 9 WRLA96053 2 19961210 A 7310 1604220001 CONTROL CABLE DOUG MD11 MD11F 3023600 NM PWA 4460 PW4460 NE NR 3 ENGINE BINDING A WRLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 274WA 48633 DURING TAXI-OUT, FLIGHT CREW RECEIVED A NR 3 ENGINE FADEC MAINTENANCE ALERT. FLIGHT CREW ELECTED TO RETURN TO DEPARTURE GATE FOR CORRECTIVE ACTION. AIRCRAFT RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE PERSONNEL FOUND TURBINE CASE COOL ING (TCC) CONTROL VALVE ACTUATING CABLE BINDING. CABLE WAS REPLACED. ENGINE GROUND RUNS PERFORMED WITH NO MALFUNCITON NOTED. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 3 4F 4 F RT A22WE E24NE 1997010900029 19970109 00029 NE 1997 1 9 ORJA9699 2 19961111 A 7230 500091601 LOCK RING DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE C1 BLADE CRACKED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 822RA DGVPWA608 49932 718262 FOUND C-1 BLADE LOCK RING BROKEN AT PULL HOLE APPROXIMATELY 2 INCHES FROM END. REPLACED C-1 BLADE LOCK RING. PART TOTA L CYCLES, 11,904. (X) 2 L 7 2 4F 4 F A6WE E9NE 1997010900030 19970109 00030 WP 1997 1 9 ORJA96101 1 19961115 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN BROKEN A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 832RA 53044 EMERGENCY FLOOR-TRACK LIGHTING IN FIRST CLASS INOPERABLE. REPAIRED BROKEN WIRE AND RELAMPED. OPS CHECK NORMAL. (X) 2 L 7 2 4F RT A6WE 1997010900031 19970109 00031 WP 1997 1 9 ORJA96102 1 19961115 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN BROKEN A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 872RA 49793 EMERGENCY LIGHT OUT AT 31. FOUND BROKEN WIRE; REPAIRED PER MM. OPS CHECK GOOD. (X) 2 L 7 2 4F RT A6WE 1997010900032 19970109 00032 EA 1997 1 9 97ZZZX6223 2 19961108 A 7532 310092208 LP BLEED VALVE STBROS SD3 SD330 8100602 EU PWA PT6 PT6A45R 52043 EA COMPRESSOR WORN A DATA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 13 938MA 1638 467 SH3046 PCE84003 MKE - ON TAKEOFF, COMPRESSOR STALLED ON START AND TAKEOFF POWER. PILOT ABORTED TAKEOFF AND RETURNED TO BASE. MAINTENAN CE REMOVED AND REPLACED LOW PRESSURE BLEED VALVE. RAN ENGINE, OPERATIONAL CHECK FOUND NORMAL. 2 H 7 2 4T 4 T A41EU E4EA 1997010900033 19970109 00033 NE 1997 1 9 97ZZZX6224 2 19961106 A 7260 313594 CASE BUSHING BOEING 727 727214 138407R NM PWA JT8 JT8D15 52051 NE NR 3 ACCESS GB PULLED THREADS A C8GA E ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 SO 15 227JL 50684 12076 20875 687468 AIRCRAFT DEPARTED DAY AT 1011Z FOR TPA, FL. AT 1115Z, NR 3 ENGINE WAS SHUT DOWN DUE TO LOSS OF OIL QUANTITY AND OIL PRE SSURE. UPON LANDING IN TAMPA, FL, THE CAUSE OF THE SHUT DOWN WAS DETERMINED TO BE A LOOSE BUSHING IN THE ACCESSORY DRIV E CASE. A REPAIR WAS EFFECTED IAW PWA JT8D MM 72-61-01, REPAIR 05. THE ENGINE WAS INSPECTED IAW PWA JT8D MM 72-00, PAR A J, AND RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 1997010900034 19970109 00034 EU 1997 1 9 RAIA961102 1 19961102 A 7603 14176007175 FRICTION KNOB JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT OUT OF ADJUST A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 03 570HK 933 41089 JFK - FLT 7706 - CONFIGURATION WARNING SOUNDED ON TAKEOFF. ADJUSTED FRICTION KNOB. 2 L 7 2 4T RT A41NM 1997010900035 19970109 00035 EU 1997 1 9 RAIA961105 1 19961104 A 7603 S2700004 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT OUT OF ADJUST A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 570HK 947 41089 JFK - FLT 7743 - TAKEOFF CONFIG WARNING SOUNDED ON TAKEOFF. MAINTENANCE ADJUSTED THE LEFT CONDITION LEVER MICROSWITCH. (X) 2 L 7 2 4T RT A41NM 1997010900036 19970109 00036 WP 1997 1 9 97ZZZX6225 1 19961119 A 5730 SKIN DOUG DC9 DC932 3022066 WP LT WING CRACKED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 910VJ 47277 DURING A SCHEDULED INSPECTION AT AERO CORP., THE LEFT WING UPPER SKIN PANEL WAS FOUND CRACKED (LENGTH OF CRACK .4375 INC H) FROM EDGE TO FASTENER HOLE OF ACCESS PANEL NR 1307A LANDING AT AFT OUTBOARD QUADRANT OF ACCESS OPENING. STOP DRILLED CRACK, FABRICATED DOUBLER 7075T6 .0375 15 .75 INCH BY 29 INCHES IAW DC9 SRM 57-03, FIG 23. DRILLED DOUBLER, COUNTERSUN K AND DEBURRED IAW DC9 SRM 51-10-4. ALODINED AND PRIMED IAW DC9 SRM 50-10-3, INSTALLED DOUBLER IAW DC9 SRM 51-10-3, FIG 23. NON-ROUTINE REF NR 027N1-0059. 2 L 7 2 4F A6WE 1997010900037 19970109 00037 CE 1997 1 9 97ZZZX6226 1 19960716 A 2750 DT2R17 LIMIT SWITCH 1015210839 BEECH 200 B200 1152922 CE RT TE FLAPS OUT OF ADJUST A FUBA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 NE 03 508MV BB877 FLAPS WERE OBSERVED NOT TO BE OPERATING ON THE VOR RWY 15 @ ASE. FLAP HANDLE WAS PLACED IN THE UP POSITION ON THE LANDI NG ROLL OUT. SMOKE BEGAN TO ENTER CABIN. PROBLEM WAS DUE TO FLAP LIMIT SWITCH OUT OF ADJUSTMENT CAUSED FLAPS TO BIND I N THE UP POSITION, WHILE TRYING TO ACTUATE FLAPS, THE FLAPS MOTOR BEGAN TO SMOKE. 1 L 7 2 4T A24CE 1997010900038 19970109 00038 EU 1997 1 9 97ZZZX6227 1 19961108 A 3260 SWITCHES STBROS SD3 SD360 8100606 EU LANDING GEAR LACK OF LUBE A GUUA O OTHER N FALSE WARNING IN INSP/MAINT 1 SO 19 261GA SH3745 TPA/MIA - FLT 408 - PILOT REPORT: GEAR WARNING HORN SOUNDS ON GROUND IN RESPONSE TO THROTTLE POSITION AND FLAP HANDLE. CORRECTIVE: CLEARED AND LUBRICATED THROTTLE MICROSWITCHES. 2 H 7 2 4T A41EU 1997010900039 19970109 00039 EU 1997 1 9 97ZZZX6228 1 19961111 A 3260 SWITCH STBROS SD3 SD360 8100606 EU LANDING GEAR OUT OF ADJUST A GUUA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 19 261GA SH3745 NAS/MIA - FLT 3430 - PILOT REPORT: LANDING GEAR WARNING HORN DID NOT SOUND AT FLIGHT IDLE WITH GEAR UP. CORRECTIVE: A DJUSTED WARNING HORN MICROSWITCH AT THROTTLE QUADRANT. 2 H 7 2 4T A41EU 1997010900040 19970109 00040 EU 1997 1 9 97ZZZX6229 1 19961115 A 3260 21HE252 DOWNLOCK SWITCH STBROS SD3 SD360 8100606 EU NLG CRACKED A GUUA O OTHER P NO WARNING INDICATION LD LANDING 1 SO 19 264GA SH3756 MCO/MIA - FLT 3406 - PILOT REPORT: NOSE GEAR DOWN LIGHT DID NOT ILLUMINATE AT LANDING. CORRECTIVE: REMOVED AND REPLAC ED DOWNLOCK MICROSWITCH. EXTENSION/RETRACTION TESTS OK. 2 H 7 2 4T A41EU 1997010900041 19970109 00041 NM 1997 1 9 PCAA9600317 1 19961009 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM COCKPIT DIRTY A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 830EX 060081 155 COCKPIT EMERGENCY LIGHT, PN 10005511, STAYS ON WITH SWITCH IN ARMED POSITION. TIGHTENED CONTACTS AT LIGHT MOUNT. OPER ATIONALLY CHECK GOOD. A/C RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A13NM 1997010900042 19970109 00042 NE 1997 1 9 GLBA96204 2 19961017 A 7530 EVA SYSTEM BEECH 1900 1900D 1154162 CE PWA 118 PW118 NE RIGHT LEAKING A GLBA O OTHER J WARNING INDICATION TO TAKEOFF 1 CE 01 210UX UE210 MSP - RIGHT BLEED AIR FAIL ANNUNCIATOR ILLUMINATED. MAINTENANCE REPAIRED LEAK IN EVA SYSTEM. OPS CHECKED GOOD. (X) 2 L 7 2 4T 4 T RT A24CE E20NE 1997010900043 19970109 00043 WP 1997 1 9 AALA961532 1 19961019 A 3350 A3060698101 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 569AA 49351 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AFT OF PASSENGER SEAT ROW 21D FOUND INOPERATIVE. REPLACED BROKEN E MERGENCY FLOOR LIGHT STRIP CONNECTOR BY LAST ROW OF PASSENGER SEATS. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2 L 7 2 4F RT A6WE 1997010900044 19970109 00044 EA 1997 1 9 97ZZZX6230 2 19961028 A 7260 GARLOCK SEAL PIPER PA31T PA31T 7103124 SO PWA PT6 PT6A28 EA GEARBOX UNSEATED A GRMA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 19 30DU 52 31T7720054 PCE51403 ENGINE WAS SHUT DOWN IN-FLIGHT DUE TO DIMINISHING AND FLUCTUATING OIL PRESSURE. INSPECTED ENGINE IAW PWC MM. NO SIGNIF ICANT METAL FOUND IN FILTERS OR CHIP DETECTOR. FOUND GARLOCK SEAL ON AFT SCAVENGE PUMP UNSEATED FROM CARRIER. REPLACED GARLOCK SEAL AND RAN ENGINE AT POWER FOR ONE HOUR. RECHECKED FILTERS AND CHIP DETECTOR, NO METAL FOUND. LEAK CHECKS G OOD. 1 L 7 2 3T 4 T A8EA E4EA 1997010900045 19970109 00045 SO 1997 1 9 97ZZZX6231 1 19961115 A 5310 STRUCTURE GULSTM G1159 GIV 3980115 SO BS 539.75 CORRODED A WJCA K NONE O OTHER IN INSP/MAINT 1 EA 11 226G 2875 1122 DURING SCHEDULED C/W BAG COMPT BEHIND PANEL INSP PER CMP CODE 532045, CORROSION WAS NOTED WHERE STR 2L PASSED THROUGH BU LKHEAD 539.75. INVESTIGATION REVEALED THAT POTABLE WATER HOSE ASSY LOCATED ABOVE HEADLINER IN LAVATORY AREA HAD OVERHEA TED WHICH LED TO CONDENSATION FORMATION IN THE AREAS ADJACENT TO THE HOSE. DAMAGE WAS EVIDENT ON STRINGERS, CLIPS, BRAC KETS, AND THE VERTICAL STRUCTURE OF THE DOOR POST BETWEEN THE LAVATORY AND BAG COMPT. PRESSURE TESTING AND ELECTRICAL T ESTING OF THE HOSE ASSY REVEALED NO DEFECTS. THE CLOSE CONFINES OF THE AREA WHERE THE HOSE IS INSTALLED MAY HAVE BEEN A CONTRIBUTING FACTOR. CYCLES, 1,534. 2 L 7 2 4F RT A12EA 1997010900046 19970109 00046 NM 1997 1 9 HNAA9698676 1 19961120 A 7712 30005000056 TSCU DHAV DHC8 DHC8201 2809001 NM NR 2 ENGINE FAILED A HNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 07 986HA 714 MM4832 421 TLH/TPA - FLT 3240 - ON CLIMB-OUT AT 300 FEET, AUTOFEATHER SELECTED ON, NR 1 ENGINE UP-TRIM LIGHT FLICKERED, AND ENGINE ATTEMPTED TO UP-TRIM. THE AIRCRAFT TURNED BACK TO TLH AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 TORQUE SI GNAL CONDITIONING UNIT (TSCU) AND TIGHTENED NR 2 TORQUE PROBE CANNON PLUG. (X) 2 H 7 2 4T RT A13NM 1997010900047 19970109 00047 1997 1 9 G60A96323 4 19961118 A 2565 SLIDE DOUG DC10 DC1030 3023501 WP PASSENGER DOOR MALFUNCTIONED A G6OA K NONE O OTHER TX TAXI/GRND HDL 1 EA 27 604GC 47924 WHEN AIRCRAFT BLOCKED IN AT PHF FOR UNLOAD OF TRAINING CREW, THE DOOR WAS OPENED WITHOUT DISARMING EVACUATION SLIDE BY M EMBER OF FLIGHT CREW. THE SLIDE FAILED TO DEPLOY TO THE FULLY DEPLOYED POSITION. (X) 2 L 7 3 4F A22WE 1997010900048 19970109 00048 EU 1997 1 9 MALA965206 1 19961118 A 3297 WIRE SAAB SF340 SF340A 7850100 EU LT MLG LOOSE A MALA A UNSCHED LANDING P NO WARNING INDICATION AP APPROACH 1 GL 15 89XJ 340A089 TOL - FLT 3378 - ON APROACH TO TOL, THE LEFT GREEN DOWNLOCK LIGHT FAILED TO ILLUMINATE AFTER GEAR EXTENSION. THE TRANSI TION LIGHT WAS EXTINGUISHED. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPAIRED A WIRE AT CANNON PLUG P1. ALL CHECKS SATISFACTORY. (X) 2 L 7 2 4T RT A52EU 1997010900049 19970109 00049 EU 1997 1 9 REXA96065 1 19961027 A 2612 1734362450 FIRE DETECTORS FENWAL SAAB SF340 SF340A 7850100 EU RT ENGINE CONTAMINATED A REXA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SO 25 107PX 340A010 RECEIVED TAILPIPE HOT LIGHT IN-FLIGHT ON RT ENGINE. CLEANED AND APPLIED RTV TO TAILPIPE FIRE SENSORS. GROUND RUN. OPS CHECK NORMAL. (X) 2 L 7 2 4T RT A52EU 1997010900050 19970109 00050 SW 1997 1 9 HEEA968772 1 19961227 A 6220 206011111001 BEARING ASSY BELL 206 206L1 1182107 SW M/R FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 11 EACH ROLLERS MISSING FROM M/R TRUNNION BEARING. 1 G 7 1 3U H2SW 1997010900051 19970109 00051 GL 1997 1 9 HEEA968773 2 19961227 A 7250 23034775 SUPPORT 23035128 BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL NR 2 NOZZLE MISMANUFACTURED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8594X CAT90616 51531 CAE895162 RECEIVING INSPECTION REVEALED: I.D. MEASURED .049-.071 BELOW SPECS ON G.P. SUPPORT AT #2 NOZZLE TANG SLOTS. SPECS (7.6 3) #2 NOZZLE WILL NOT FIT INTO SUPPORT. INSTALLED DALLAS AIRMOTIVE OVERHAULED G.P. SUPPORT. 1 G 7 1 3U 3 U H2SW E1GL 1997010900052 19970109 00052 GL 1997 1 9 HEEA968774 2 19961227 A 7250 6886407 WHEEL 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL NR 1 STAGE BLADES ERRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81982 1614 CAT37905 S818 CAE823458F ENGINE REMOVED DUE TO CYCLED #1 AND #2 WHEELS. UPON INSPECTION OF TURBINE PARTS NOTED: (1) ERODED ALL LEADING EDGE AND SULPHIDATION ON 17 OF THE #1 WHEEL BLADES (2) ERODED LEADING EDGE 11 AND BURNT TRAILING EDGE ON 7 OF THE #1 NOZZLE V ANES. PARTS SENT TO ALLISON ENGINE ON AFA#29359A FOR EVALUATION. (RFSE 250-93-2) 1 G 7 2 3U 3 U H3EU E4CE 1997010900053 19970109 00053 GL 1997 1 9 HEEA968775 2 19961227 A 7250 23060403 NOZZLE VAMES 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL NR 1 BURNT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81982 1614 CAT37905 S818 CAE823458F ENGINE REMOVED DUE TO CYCLED NR 1 AND NR 2 WHEELS. UPON INSPECTION OF TURBINE PARTS NOTED: (1) ERODED ALL LEADING EDGE AND SULPHIDATION ON 17 OF THE NR 1 WHEEL BLADES. (2) ERODED LEADING EDGE 11 AND BURNT TRAILING EDGE ON 7 OF THE NR 1 NO ZZLE VANES. PARTS SENT TO ALLISON ENGINE ON AFA NR 29359A FOR EVALUATION. (RFSE 250-93-2) 1 G 7 2 3U 3 U H3EU E4CE 1997010900054 19970109 00054 SW 1997 1 9 HEEA968776 1 19961227 A 6230 204011430001 BEARING 412010402105 BELL 412 412 1182202 SW M/R MAST ROUGH E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911PB RE304 33186 BEARING WORN AND ROUGH. SCRAPPED AT PHI. 1 G 7 2 4U H4SW 1997010900055 19970109 00055 SW 1997 1 9 HEEA968777 1 19961227 A 6230 204011451001 TRUNNION ASSY 412010402105 BELL 412 412 1182202 SW M/R MAST WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911PB RE304 33186 TRUNNION ASSY WORN AND ROUGH. SCRAPPED AT PHI. 1 G 7 2 4U H4SW 1997010900056 19970109 00056 SW 1997 1 9 HEEA968778 1 19961227 A 6230 412310400107 BEARING 412010402105 BELL 412 412 1182202 SW M/R MAST WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911PB RE304 33186 BEARING WORN AND ROUGH. SCRAPPED AT PHI. 1 G 7 2 4U H4SW 1997010900057 19970109 00057 SW 1997 1 9 HEEA968779 1 19961227 A 6230 412010427101 BEARING 412010402105 BELL 412 412 1182202 SW M/R MAST WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911PB RE304 33186 BEARING WORN AND ROUGH. SCRAPPED AT PHI. 1 G 7 2 4U H4SW 1997010900058 19970109 00058 SW 1997 1 9 HEEA968780 1 19961227 A 6230 MS2764110 BEARING 412010402105 BELL 412 412 1182202 SW M/R MAST WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911PB RE304 33186 BEARING WORN AND ROUGH. SCRAPPED AT PHI. 1 G 7 2 4U H4SW 1997010900059 19970109 00059 SW 1997 1 9 HEEA968781 1 19961227 A 6230 412010421101 BUSHING 412010402105 BELL 412 412 1182202 SW M/R MAST WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911PB RE304 33186 BUSHING WORN AND ROUGH. SCRAPPED AT PHI. 1 G 7 2 4U H4SW 1997010900060 19970109 00060 SW 1997 1 9 HEEA968782 1 19961227 A 6230 412010416101 SPACER 412010402105 BELL 412 412 1182202 SW M/R MAST WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911PB RE304 33186 SPACER WORN AND ROUGH. SCRAPPED AT PHI. 1 G 7 2 4U H4SW 1997010900061 19970109 00061 EU 1997 1 9 HEEA968783 1 19961227 A 6520 350A33200403 SPIDER SNIAS 350 AS350B2 8680813 EU T/R BEARING LOOSE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100R 1099 2862 T/R SPIDER LOOSE BEARING-SLINGING GREASE. 1 G 7 1 3U H9EU 1997010900062 19970109 00062 EU 1997 1 9 HEEA968784 1 19961227 A 6520 350A33200401 SPIDER SNIAS 350 AS350B2 8680813 EU T/R BUSHING BINDING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6097Z 2151 2820 T/R SPIDER INBOARD SPLIT BUSHINGS BINDING UP ON SHAFT. 1 G 7 1 3U H9EU 1997010900063 19970109 00063 EU 1997 1 9 HEEA968785 1 19961227 A 6720 350A33214501 ROD SNIAS 350 AS350B2 8680813 EU PITCH CONTROL WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 350BZ 1307 2653 PITCH CONTROL ROD WORN BEARING. 1 G 7 1 3U H9EU 1997010900064 19970109 00064 EU 1997 1 9 HEEA968786 1 19961227 A 6520 350A33215300 BEARING SNIAS 350 AS350B2 8680813 EU T/R HEAD WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6097Z 1943 2820 WORN RUBBER BEARINGS. 1 G 7 1 3U H9EU 1997010900065 19970109 00065 EU 1997 1 9 HEEA968787 1 19961227 A 6520 350A33215300 BEARING SNIAS 350 AS350B2 8680813 EU T/R HEAD CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 350BZ 1881 2653 RUBBER CRACKED. 1 G 7 1 3U H9EU 1997010900066 19970109 00066 EU 1997 1 9 HEEA968788 1 19961227 A 6520 350A33215300 BEARING SNIAS 350 AS350B2 8680813 EU T/R HEAD CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6095S 1562 2777 RUBBER CRACKED. 1 G 7 1 3U H9EU 1997010900067 19970109 00067 EU 1997 1 9 HEEA968789 1 19961227 A 6520 350A33215300 BEARING SNIAS 350 AS350B2 8680813 EU T/R HEAD SEPARATION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100U 429 2863 BEARING SEPARATION . 1 G 7 1 3U H9EU 1997010900068 19970109 00068 EU 1997 1 9 HEEA968790 1 19961227 A 6520 350A33215300 BEARING SNIAS 350 AS350B2 8680813 EU T/R HEAD SEPARATION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100R 254 2862 BEARING SEPARATION. 1 G 7 1 3U H9EU 1997010900069 19970109 00069 1997 1 9 HEEA968791 4 19961230 A 3442 MI585200 RADAR RT BELL 212 212 1181420 SW COCKPIT MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 27805 31106 NO PICTURE ON SCREEN, INCOMPLETE TEST PATTERN. SPIDER WEB PATTERN IN MAP/WX. 1 G 7 1 4U H4SW 1997010900071 19970109 00071 1997 1 9 HEEA968793 4 19961230 A 3453 25410038 7000 CDU BELL 412 412 1182202 SW COCKPIT LORAN KNOB BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D 33076 CONTROL KNOB BROKEN. 1 G 7 2 4U H4SW 1997010900072 19970109 00072 SW 1997 1 9 HEEA968794 1 19961230 A 6210 214015300107 BLADE BELL 214 214ST 1182106 SW M/R SKIN VOID E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 1986 28101 SKIN VOID ON UPPER AND LOWER SURFACES NEAR BLADE STATION 43.5" APPROXIMATELY 2.5" FROM TRAILING EDGE. EACH VOID IS APPR OXIMATELY 4" IN DIAMETER. 2 G 7 2 4U H10SW 1997010900073 19970109 00073 NM 1997 1 9 HEEA968795 1 19961230 A 6210 900R1150001115 BLADE DOUG MD900 MD900 3027375 NM M/R DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 9214U 446 90000014 HOLE IN THE LEADING EDGE AT ROOT SECTION. PAINT PEELING. 1 G 7 2 3U NC H19NM 1997010900074 19970109 00074 NM 1997 1 9 HEEA968796 1 19961230 A 6210 900R1150001115 BLADE DOUG MD900 MD900 3027375 NM M/R PAINT PEEL E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 9214U 446 90000014 M/R BLADE PAINT PEELING. 1 G 7 2 3U NC H19NM 1997010900075 19970109 00075 NM 1997 1 9 HEEA968797 1 19961230 A 6210 900R1150001115 BLADE DOUG MD900 MD900 3027375 NM M/R PAINT PEEL E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 9214U 446 90000014 M/R BLADE PAINT PEELING. 1 G 7 2 3U NC H19NM 1997010900076 19970109 00076 NM 1997 1 9 HEEA968798 1 19961230 A 6210 900R1150001115 BLADE DOUG MD900 MD900 3027375 NM M/R DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 9214U 446 90000014 HOLES IN THE LEADING EDGE ROOT SECTION. PAINT PEELING. 1 G 7 2 3U NC H19NM 1997010900077 19970109 00077 NM 1997 1 9 HEEA968799 1 19961230 A 6210 900R1150001111 BLADE DOUG MD900 MD900 3027375 NM M/R DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 9214U 68 90000014 HOLES IN THE LEADING EDGE ROOT SECTION. PAINT PEELING. SENT TO MCDONNELL DOUGLAS FOR INSPECTION. 1 G 7 2 3U NC H19NM 1997010900078 19970109 00078 SW 1997 1 9 HEEA968800 1 19961230 A 5610 M2052122851 WINDOW BELL 412 412 1182202 SW LT SIDE MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 23023 33080 PLEXIGLASS DOES NOT FIT IN NEEDED AREA. MARKED IN BLUE INK. 1 G 7 2 4U H4SW 1997010900079 19970109 00079 NE 1997 1 9 HEEA968801 1 19961230 A 7810 7630507003044 EJECTOR SKRSKY S76 S76A 8143006 NE EXHAUST CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5128 760181 EJECTOR IS CRACKED. 1 G 7 2 3U H1NE 1997010900080 19970109 00080 NE 1997 1 9 HEEA968802 1 19961230 A 7810 7630507003044 EJECTOR SKRSKY S76 S76A 8143006 NE EXHAUST CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5128 760181 EJECTOR HAS NUMEROUS CRACKS. 1 G 7 2 3U H1NE 1997010900081 19970109 00081 SW 1997 1 9 HEEA968803 1 19961230 A 5320 212030101003A PANEL ASSY BELL 212 212 1181420 SW COCKPIT DEFECTIVE E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 30888 HANGER BEARING BUSHING LOCATED TOO FAR AFT AND WILL NOT ALLOW FOR PROPER EDGE DISTANCE ON FWD AND AFT TRANSISTOR AREA AN D RIVET HOLES. 1 G 7 1 4U H4SW 1997010900082 19970109 00082 1997 1 9 HEEA968804 4 19961230 A 3416 212070238003 INDICATOR SKRSKY S76 S76A 8143006 NE COCKPIT ALT STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545K 760047 INDICATOR INTERMITTENTLY STICKS THROUGHOUT SCALE. 1 G 7 2 3U H1NE 1997010900083 19970109 00083 EU 1997 1 9 HEEA968805 1 19961230 A 7722 50061036 INDICATOR BOLKMS 105 BO105S 5626006 EU EXH TEMP EXCESS ERROR E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3538T S350 EXH TEMP INDICATOR EXCESSIVE FRICITON ERROR. 1 G 7 2 3U H3EU 1997010900084 19970109 00084 EU 1997 1 9 HEEA968806 1 19961230 A 7722 TM42739 INDICATOR BOLKMS 105 BO105S 5626006 EU EXH TEMP EXCESS ERROR E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81832 S828 EXH TEMP INDICATOR EXCESSIVE FRICITON ERROR. 1 G 7 2 3U H3EU 1997010900085 19970109 00085 GL 1997 1 9 HEEA968807 2 19961230 A 7311 50C00072 HEAT EXCHANGER SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL B NUT LINE WELD LEAKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2743E 760155 HEAT EXCHANGER LEAKS AT WELD ALONG OUTER B-NUTLINE. 1 G 7 2 3U 3 U H1NE E1GL 1997010900086 19970109 00086 1997 1 9 HEEA968808 4 19961230 A 2312 40001278500 TRANSCEIVER RT406 BOLKMS 105 BO105S 5626006 EU COCKPIT VHF FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911HM S683 TRANSCEIVER DOESN'T RECEIVE. 1 G 7 2 3U H3EU 1997010900087 19970109 00087 1997 1 9 HEEA968809 4 19961230 A 3444 071111400 ANTENNA BOLKMS 105 BO105S 5626006 EU RADAR ALTIMETER DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911FL 9 S717 RADAR ALTIMETER UNRELIABLE. 1 G 7 2 3U H3EU 1997010900088 19970109 00088 EU 1997 1 9 HEEA968810 1 19961230 A 6310 4638202007 CLUTCH 4638001004 BOLKMS 105 BO105S 5626006 EU FREEWHEEL FAIL INSP E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 724MB 3505 1291 S756 FAILED 600 HOUR INSPECTION. INNER CAGE WORN BEYOND LIMITS. REPLACED WITH SERVICEABLE CLUTCH. 1 G 7 2 3U H3EU 1997010900089 19970109 00089 EU 1997 1 9 HEEA968811 1 19961230 A 7120 1176272101 MOUNT BOLKMS 117 BK117A3 5626015 EU ENG CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911NC 7026 ONE LEG OF ENGINE MOUNT CRACKED IN HALF. 1 G 7 2 3U H13EU 1997010900090 19970109 00090 SW 1997 1 9 HEEA968812 1 19961231 A 6710 214001347005 ACTUATOR ROTARY BELL 412 412 1182202 SW FLT CONTROL INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 33008 36004 ACTUATOR ROTARY INOPERATIVE. CYCLIC LATERAL FORCE TRIM DOESN'T HOLD WHEN FORCE TRIM IS ON. 1 G 7 2 4U H4SW 1997010900091 19970109 00091 SW 1997 1 9 HEEA968814 1 19961231 A 2844 BSE20630G TRANSDUCER BELL 206 206L3 1182108 SW FUEL PRESS DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 42EA 51542 TRANSMITS LOW OUT OF TOLERANCE. 1 G 7 1 3U H2SW 1997010900092 19970109 00092 1997 1 9 HEEA968815 4 19961231 A 2562 ELT910 ELT BELL 206 206L3 1182108 SW COCKPIT MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3107N 51512 TRANSMITTER ACTIVATED; WOULD NOT SHUT OFF. SENT TO NARCO AVIONICS FOR WARRANTY REPAIR. TIME SINCE REPAIR 68:10. 1 G 7 1 3U H2SW 1997010900093 19970109 00093 1997 1 9 HEEA968816 4 19961231 A 3453 066401018 RNAV BELL 214 214ST 1182106 SW COCKPIT MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5748M 28102 REMOTE ARNAV LIGHT ALWAYS ILLUMINATED WHEN UNIT IS TURNED ON. SENT TO THE RADIO SHOP FOR REPAIR. 2 G 7 2 4U H10SW 1997010900124 19970109 00124 CE 1997 1 9 97ZZZX31 1 19961220 A 2436 51539012 GCU 200SGL119Q CESSNA 208 208B 2073701 CE START/GEN FAILED A AWHA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CR CRUISE 1 WP 17 872FE 455 9377 208B0200 PILOT REPORTED WHILE EN ROUTE FROM ONT TO SBA, THE RED GENERATOR OFF LIGHT ILLUMINATED. THE STAND-BY ALTERNATOR DID NOT COME ON LINE. THE STAND-BY ELECTRICAL POWER ON LIGHT NOR THE STAND-BY ELECTRICAL POWER OFF LIGHT ILLUMINATED. THE AIR CRAFT WAS OPERATING ON BATTERY POWER ONLY. THE PILOT ELECTED TO PERFORM A PRECAUTIONARY LANDING IN OXR. MAINTENANCE WA S DISPATCHED TO THE AIRCRAFT AND CONFIRMED A GCU FAILURE. THE GCU WAS REPLACED, ADJUSTED AND OPERATIONALLY CHECK GOOD. THE STAND-BY ALTERNATOR SYSTEM WAS FUNCTIONALLY CHECKED AND NO DISCREPANCIES WERE FOUND. THE AIRCRAFT WAS RETURNED TO SERVICE AND FLOWN TO FAT WITH NO DEVIATIONS. 1 H 7 1 3T A37CE 1997010900125 19970109 00125 CE 1997 1 9 97ZZZX32 1 19961114 A 2422 INVERTER CESSNA 500 560CESSNA 2076750 CE NR 1 SYS MALFUNCTION A DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 336QS 5600336 ALTITUDE AND HEADING FAIL ON PILOT AND COPILOT PFD DISPLAYS. FOUND NR 1 INVERTER MALFUNCTIONING. 2 L 7 2 4F RT A22CE 1997010900126 19970109 00126 CE 1997 1 9 97ZZZX33 1 19961112 A 5210 SEAL CESSNA 500 560CESSNA 2076750 CE DOOR MALFUNCTION A DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 375QS 5600375 DOOR SEAL LIGHT CAME ON AT ALTITUDE. FOUND FROZEN MOISTURE IN SEAL. 2 L 7 2 4F RT A22CE 1997010900127 19970109 00127 1997 1 9 97ZZZX34 4 19961107 A 3424 GYRO CESSNA 500 560CESSNA 2076750 CE RATE GYRO MALFUNCTION A DXTA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 07 336QS 5600336 AUTOPILOT INOPERATIVE. RATE GYRO CIRCUIT BREAKER POPPED. FOUND RATE GYRO MALFUNCTIONING. 2 L 7 2 4F RT A22CE 1997010900128 19970109 00128 EU 1997 1 9 97ZZZX35 1 19961111 A 2130 AUX VALVE BRAERO 1000 BAE1251000 1500287 EU CABIN PRESS MALFUNCTION A DXTA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 07 520QS NA1008 AUX VALVE WILL NOT STAY OPEN. FOUND MALFUNCTIONING AUX VALVE. 2 L 7 2 4F RT A3EU 1997010900129 19970109 00129 CE 1997 1 9 97ZZZX36 1 19961107 A 5210 SEAL CESSNA 500 S550 2076607 CE DOOR LEAKING A DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 93QS S5500093 ENTRANCE DOOR SEAL LEAKING AT ALTITUDE. FOUND BAD CABIN DOOR SEAL. 1 L 7 2 4F RT A22CE 1997010900130 19970109 00130 WP 1997 1 9 CALA9601893 1 19961230 A 3222 5910448561 STRUT DOUG DC9 DC982 3022082 WP NLG LOW PRESSURE A CALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 09 937MC 49450 THE NOSE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR WAS RETRACTED. CYCLING THE GEAR DID NOT HELP. THE AIRCR AFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NLG SHOCK STRUT PRESSURE LOW. A FULL S TRUT SERVICE WAS PERFORMED IAW MM 32-21-02. THE NOSE GEAR WAS SWUNG WITH OPERATION AND INDICATIONS CHECKING NORMAL. 2 L 7 2 4F A6WE 1997010900131 19970109 00131 WP 1997 1 9 CALA9601894 1 19961126 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 965 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17531 45847 INSPECTION FOUND A .75 INCH CRACK IN LONGERON 12L, 12R, AND 13R AT STA 965. SPLICE REPAIRS WERE INSTALLED IAW SRM 53-02 , FIGURE 2A. 2 L 7 2 4F A6WE 1997010900132 19970109 00132 WP 1997 1 9 CALA9601895 1 19961126 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 965 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17531 45847 INSPECTION FOUND A 1 INCH CRACK IN LONGERON 16L AT STA 965. THE LONGERON WAS REPLACED IAW SRM 53-02. 2 L 7 2 4F A6WE 1997010900133 19970109 00133 WP 1997 1 9 CALA9601896 1 19961112 A 5320 CHORD DOUG DC10 DC1010 3022110 WP BS 1997 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68047 47801 INSPECTION FOUND CORROSION ON LOWER CHORD AT STA 1997 BETWEEN STRINGER 52R AND 48R. A NEW PART WAS FABRICATED AND INSTA LLED IAW SRM 51-21-01 AND 53-30-00. 2 L 7 3 4F A22WE 1997010900134 19970109 00134 WP 1997 1 9 CALA9601897 1 19961110 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1119-1139 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68047 47801 INSPECTION FOUND OUTER FUSELAGE SKIN CORRODED AT STRINGER 46R, STA 1119 TO 1139. THE CORROSION WAS REMOVED IAW SRM 53-0 0-01. A REPAIR WAS INSTALLED IAW SRM 53-20-00, FIGURE 13. 2 L 7 3 4F A22WE 1997010900135 19970109 00135 NM 1997 1 9 CALA9601898 1 19961023 A 5320 ANGLE BOEING 747 747243B 1384830 NM BS 1540 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33021 20520 INSPECTION FOUND A 1 INCH CRACK ON SUPPORT ANGLE ATTACHED TO FRAME AT BS 1540 BETWEEN STRINGER 37 TO 38L. A NEW ANGLE W AS FABRICATED AND INSTALLED IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1997010900136 19970109 00136 NM 1997 1 9 CALA9601899 1 19961211 A 5320 ANGLE BOEING 737 7373T0 1384582 NM AFT CARGO CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12327 23457 INSPECTION FOUND ATTACH ANGLE CORRODED AROUND NUT PLATES IN AFT CARGO AREA ON RT SIDE. THE ANGLE WAS REMOVED AND REPLAC ED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 1997010900137 19970109 00137 NM 1997 1 9 CALA9601900 1 19961211 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM BS 767-787 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12327 23457 INSPECTION FOUND CENTER CARGO FLOOR SUPPORT CORRODED AT STA 767 TO 787. THE CORRODED SECTION OF FLOOR SUPPORT WAS REPLA CED IAW SRM 53-00-53. 2 L 7 2 4F RT A16WE 1997010900138 19970109 00138 NM 1997 1 9 CALA9601901 1 19961211 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM BS 787 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12327 23457 INSPECTION FOUND A 2 INCH CRACK IN CENTER CARGO FLOOR SUPPORT AT STA 787. A NEW SECTION OF FLOOR SUPPORT WAS INSTALLED IAW SRM 53-00-53, FIGURE 202. 2 L 7 2 4F RT A16WE 1997010900139 19970109 00139 NM 1997 1 9 CALA9601902 1 19961223 A 5754 SKIN BOEING 737 7373T0 1384582 NM NR 6 SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12327 23457 INSPECTION FOUND A .5 INCH CRACK AT RIVET IN LOWER SKIN OF NR 6 SLAT AT ACTUATOR. THE SKIN WAS REPAIRED IAW ECRA 5750-0 1159. 2 L 7 2 4F RT A16WE 1997010900140 19970109 00140 NM 1997 1 9 CALA9601903 1 19961212 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 947 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12327 23457 INSPECTION FOUND FLOORBEAM CORRODED AT STA 947, RBL 5 AND LBL 5. A REPAIR WAS INSTALLED IAW SRM 53-50-01. 2 L 7 2 4F RT A16WE 1997010900141 19970109 00141 NM 1997 1 9 CALA9601904 1 19961211 A 5320 ANGLE BOEING 737 7373T0 1384582 NM BS 727-767 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12327 23457 INSPECTION FOUND LEFT CENTER FLOOR ATTACH ANGLE CORRODED AROUND NUT PLATES AT STA 727 TO 767. A DOUBLER WAS INSTALLED I AW SRM 53-60-53. 2 L 7 2 4F RT A16WE 1997010900142 19970109 00142 NM 1997 1 9 CALA9601905 1 19961210 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12327 23457 INSPECTION FOUND FLOORBEAM CORRODED AT FORWARD ENTRY BS 344 AND CORROSION WAS FOUND ON FLOORBEAM AT BS 344 FROM CENTERLI NE TO LT SIDE WALL. THE FLOORBEAMS WERE REMOVED AND REPLACED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 1997010900143 19970109 00143 NM 1997 1 9 CALA9601906 1 19961211 A 5320 ANGLE BOEING 737 7373T0 1384582 NM BS 940-997 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12327 23457 INSPECTION FOUND Z-ANGLE AT SIDE WALL OF R-2 DOOR FLOOR AREA CORRODED FROM STA 940 TO 997. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 1997010900144 19970109 00144 NM 1997 1 9 CALA9601907 1 19961209 A 5350 FORMER BOEING 737 7373T0 1384582 NM BS 540 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12327 23457 INSPECTION FOUND A 1 INCH AND 3 INCH CRACK IN FUSELAGE WING TO BODY FAIRING SUPPORT FORMER AT STA 540R. A DOUBLER WAS I NSTALLED IAW ECRA 5350-01227. 2 L 7 2 4F RT A16WE 1997010900145 19970109 00145 NM 1997 1 9 CALA9601908 1 19961211 A 5320 CHANNEL BOEING 737 7373T0 1384582 NM BS 767-787 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12327 23457 INSPECTION FOUND AFT CARGO PIT FLOOR SUPPORT CHANNEL NR 1, NR 2 AND NR 3 CORRODED AT STA 767 TO 787. THE CORRODED SECTI ONS WERE REMOVED AND REPLACED IAW ECRA 5310-03396. 2 L 7 2 4F RT A16WE 1997010900146 19970109 00146 NM 1997 1 9 CALA9601909 1 19961209 A 5320 ANGLE BOEING 737 7373T0 1384582 NM FWD CARGO CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12327 23457 INSPECTION FOUND FORWARD CARGO COMPARTMENT RIGHT SIDE CENTER FLOOR SUPPORT ANGLE CORRODED. A NEW ANGLE WAS INSTALLED IA W SRM 51-10-2. 2 L 7 2 4F RT A16WE 1997010900147 19970109 00147 WP 1997 1 9 CALA9601910 1 19961229 A 4930 8762962 FUEL CONTL UNIT DOUG DC9 DC982 3022082 WP APU MALFUNCTIONED A CALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 09 14814 49112 THE APU AUTO SHUT DOWN INFLIGHT AND THE HIGH OIL TEMP LIGHT ILLUMINATED. ALSO, THE NR 2 FIRE BOTTLE LOW AGENT LIGHT ILL UMINATED. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND NR 2 FIRE BOTTLE APU SQUIB BLOWN. THE APU WA S PLACARDED INOPERATIVE. THE NR 2 FIRE BOTTLE WAS REMOVED AND REPLACED. THE NR 2 FIRE BOTTLE APU SQUIB WAS REMOVED AND REPLACED. THE APU PLACARD WAS REMOVED, A TEST OF THE FIRE DETECTION SYSTEM WAS PERFORMED AND OPERATION CHECKED GOOD. * S/D* THE APU CONTINUED TO HAVE A HISTORY OF THE OIL TEMP HIGH LIGHT ILLUMINATING. THE APU FUEL CONTROL UNIT AND TEMP S ENSOR WERE REPLACED. THE APU WAS RUN AND OPERATION CHECKED GOOD. 2 L 7 2 4F A6WE 1997010900148 19970109 00148 NM 1997 1 9 CALA9601911 1 19961230 A 2910 65445101708 HYDRAULIC LINE BOEING 737 737130 1384435 NM RT ENG PYLON LEAKING A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 09 44214 19031 THE A-SYSTEM HYDRAULIC QUANTITY BEGAN TO DROP DURING CLIMBOUT. THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND HYDRAULIC SUPPLY FLEX LINE IN RIGHT ENGINE PYLON AREA LEAKING. THE LINE WAS REMOVED AND R EPLACED AND LEAK CHECKS WERE GOOD. 2 L 7 2 4F A16WE 1997010900149 19970109 00149 NM 1997 1 9 CALA9601912 1 19961211 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM BS 951 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12327 23457 INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 951 APPROXIMATELY 6 INCHES FROM LEFT SIDEWALL. REPAIRED IAW SRM 51 -10-02. 2 L 7 2 4F RT A16WE 1997010900150 19970109 00150 NM 1997 1 9 CALA9601913 1 19961211 A 5320 ANGLE BOEING 737 7373T0 1384582 NM BS 945-1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12327 23457 INSPECTION FOUND CABIN FLOOR Z-ANGLE CORRODED AT C-2 DOOR FROM STA 945 TO 1016. THE ANGLE WAS REPLACED IAW SRM 51-40-02 . 2 L 7 2 4F RT A16WE 1997010900151 19970109 00151 NM 1997 1 9 CALA9601914 1 19961211 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM BS 986-1006 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12327 23457 INSPECTION FOUND LEFT AFT LAV FLOOR ANGLE SUPPORT CORRODED FROM STA 986 TO 1006. A NEW SUPPORT WAS INSTALLED IAW SRM 51 -40-2. 2 L 7 2 4F RT A16WE 1997010900152 19970109 00152 NM 1997 1 9 CALA9601915 1 19961211 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM BS 986-1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12327 23457 INSPECTION FOUND RT AFT LAV FLOOR SUPPORT CORRODED FROM STA 986 TO 1016, 12 INCHES RIGHT OF CENTER AND THE LEFT AFT LAV FLOOR SUPPORT WAS CORRODED FROM STA 1006 TO 1016, 8 INCHES LEFT OF CENTER. NEW FLOOR SUPPORTS WERE INSTALLED IAW SRM 51 -10-2. 2 L 7 2 4F RT A16WE 1997010900153 19970109 00153 NM 1997 1 9 CALA9601916 1 19961211 A 5320 ANGLE BOEING 737 7373T0 1384582 NM BS 994 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12327 23457 INSPECTION FOUND RT AFT LAV FLOOR SUPPORT AND ATTACH ANGLE FOR FORWARD WALL CORRODED AT STA 994. A FLOOR SUPPORT AND AT TACH ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 1997010900154 19970109 00154 NM 1997 1 9 CALA9601917 1 19961211 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 967 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12327 23457 INSPECTION FOUND MAIN CABIN FLOORBEAM CORRODED AT STA 967. A FLOORBEAM UPPER CHORD REPAIR WAS INSTALLED IAW ECRA 5310-0 3385 AND SRM 53-00-51. 2 L 7 2 4F RT A16WE 1997010900155 19970109 00155 NM 1997 1 9 CALA9601918 1 19961219 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12327 23457 INSPECTION FOUND FLOORBEAM CORRODED AT STA 986, R-2 DOOR TO L-2 DOOR. A FLOORBEAM UPPER CHORD REPAIR WAS INSTALLED IAW ECRA 5310-03385. 2 L 7 2 4F RT A16WE 1997010900156 19970109 00156 NM 1997 1 9 CALA9601919 1 19961211 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM BS 1006-1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12327 23457 INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT AIRCRAFT CENTERLINE BETWEEN STA 1006 AND 1016. THE AREA WAS REPAIRED I AW ECRA 5310-03381. 2 L 7 2 4F RT A16WE 1997010900157 19970109 00157 NM 1997 1 9 CALA9601920 1 19961211 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM BS 947-986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12327 23457 INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED FROM STA 947.5 TO 967, 18 INCHES RIGHT OF CENTER AND CABIN FLOOR SUPPORT C ORRODED FROM 967 TO 986.5, 18 INCHES LEFT OF CENTER. REPAIRS WERE FABRICATED AND INSTALLED IAW ECRA 5310-03381. 2 L 7 2 4F RT A16WE 1997010900158 19970109 00158 NM 1997 1 9 CALA9601921 1 19961211 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM BS 951 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12327 23457 INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 951, 12 INCHES RIGHT OF CENTER AND CABIN FLOOR SUPPORT CORRODED AT STA 951, 20 INCHES FROM RIGHT SIDEWALL. REPAIRS WERE FABRICATED AND INSTALLED IAW ECRA 5310-03381. 2 L 7 2 4F RT A16WE 1997010900159 19970109 00159 NE 1997 1 9 CALA9601922 2 19961231 A 7250 SEAL BOEING 737 737291 138448W NM PWA JT8 JT8D9 52048 NE NR 6 BEARING LEAKING A CALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 10251 20361 667085 THE NR 1 ENGINE WAS SHUTDOWN DUE TO LOSS OF OIL WHILE EN ROUTE. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENAN CE FOUND OIL LEAKING FROM NR 1 ENGINE NR 6 BEARING GIT SEAL. THE NR 6 BEARING GIT SEAL WAS REMOVED AND REPLACED. THE E NGINE WAS SERVICED WITH OIL AND NO LEAKS WERE NOTED DURING AN ENGINE RUN. 2 L 7 2 4F 4 F A16WE E2EA 1997010900160 19970109 00160 WP 1997 1 9 9627249905 1 19961228 A 5330 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 955N 47160 DURING PERIODIC CHECK, FOUND CORROSION ON BELLY OF AIRCRAFT, ELEVEN INCHES AFT OF E/E COMPARTMENT OPENING BETWEEN LONGER ONS 29L AND 30L. INSTALLED TEMPORARY REPAIR PER EA 99-110796, L/P 6377247. 2 L 7 2 4F A6WE 1997010900161 19970109 00161 WP 1997 1 9 9627259926 1 19961227 A 2810 PANEL DOUG DC9 DC932 3022066 WP WS 250 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 926NW 47425 DURING PERIODIC CHECK, FOUND RIGHT WING INBOARD FUEL PANEL CRACKED EXTENDING BEYOND DOUBLER AND CRACKED AT TRACK OPENING AT WS 250, LEADING EDGE. INSTALLED REPAIR DOUBLER PER EA 99-120700, L/P 0907644. 2 L 7 2 4F A6WE 1997010900162 19970109 00162 WP 1997 1 9 9627269982 1 19961230 A 5320 PANEL DOUG DC9 DC932 3022066 WP BS 83 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 982US 45790 DURING PERIODIC CHECK, FOUND PRESSURE PANEL CRACKED IN NOSE WHEEL WELL AT FS83. REPAIRED PER EA 99-111957, L/P 0908794. 2 L 7 2 4F A6WE 1997010900163 19970109 00163 NM 1997 1 9 9627272717 1 19961217 A 5311 658261519 FRAME BOEING 727 7272S7 138407Z NM BS 950 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 721RC 22492 DURING 'H' CHECK, THE BS 950E FRAME INNER CHORD AT STR 24L WAS FOUND CRACKED. DAMAGED AREA CUTOUT AND REPAIR INSTALLED PER EA 27-120691. 2 L 7 3 4F A3WE 1997010900164 19970109 00164 NM 1997 1 9 9627285509 1 19961224 A 5315 146V5091 FLOORBEAM BOEING 757 757251 1384970 NM BS 1681 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 509 23198 DURING C-CHECK INSPECTION, FLOORBEAM UPPER CHORD AND DECK PLATE WERE FOUND CORRODED AT BS 1681. THE DECK PLATE WAS REMO VED AND ADDITIONAL CORROSION WAS FOUND ON THE FLOORBEAM. THE DECK PLATE IS ORIGINALLY 0.071 INCH THICK 2024-T3 CLAD ALU MINUM. THE FLOORBEAM IS MADE FROM BAC1518-827 7075T6511 ALUMINUM EXTENSION. REPAIRED PER IAW EA 55-120079. 2 L 7 2 4F RT A2NM 1997010900165 19970109 00165 WP 1997 1 9 9627299867 1 19961229 A 2410 CSD DOUG DC9 DC951 3022051 WP LT ENGINE LEAKING A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 776NC 47786 AFTER TAKEOFF, LEFT CSD OIL PRESSURE LOW LIGHT ILLUMINATED. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. FOUND CSD OIL COOLER LEAKING. REPLACED LEFT CSD OIL COOLER AND LEAK CHECKED GOOD. 2 L 7 2 4F RT A6WE 1997010900166 19970109 00166 WP 1997 1 9 9627319160 1 19961229 A 5248 LATCH MECH DOUG DC9 DC914 3022034 WP TAIL CONE DOOR OUT OF ADJUST A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 8903E 45744 AFTER TAKEOFF, FLIGHT ATTENDANT IN AFT FLIGHT ATTENDANT SEAT HEARD A NOISE AND FELT PRESSURE ON THE SEAT. ALL COCKPIT I NDICATIONS NORMAL. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED DOOR AND ADJUSTED LATCH M ECHANISM, NO DAMAGE FOUND. CABIN PRESSURIZED WITH NO ABNORMAL SOUNDS NOTED. 2 L 7 2 4F A6WE 1997010900167 19970109 00167 NM 1997 1 9 9627326627 1 19961230 A 7830 TR UNIT BOEING 747 747251B 1384892 NM PWA JT9 JT9D7Q 52054 NE NR 1 ENGINE MALFUNCTIONED A NWAA O OTHER R X PARTIAL RPM/PWR LOSS ENGINE FLAMEOUT LD LANDING 1 GL 01 627US 21709 702055 DURING LANDING, ENGINE NR 1 REVERSER WOULD NOT STOW. DURING SECOND STOW ATTEMPT ENGINE NR 1 EXPERIENCED A COMPRESSOR ST ALL AND AUTO SHUTDOWN. MAINTENANCE INSPECTED ENGINE NR 1, OPS CHECK OF ENGINE AND REVERSER WAS PERFORMED. NO DISCREPAN CIES NOTED. 2 L 7 4 4F 4 F A20WE E3NE 1997010900168 19970109 00168 WP 1997 1 9 9627339960 1 19961230 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP COCKPIT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 920RW 47163 DURING LINE MAINTENANCE INSPECTION, FOUND COCKPIT AND RIGHT NACELLE EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLI ES AND BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1997010900169 19970109 00169 WP 1997 1 9 9627349992 1 19961230 A 3350 11331DGDME BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8960E 4247 4244 45869 DURING PERIODIC CHECK, FOUND MAIN CABIN DOOR EVACUATION SLIDE WITH LOW BATTERY. REPLACED SLIDE. 2 L 7 2 4F A6WE 1997010900170 19970109 00170 WP 1997 1 9 9627359851 1 19961227 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 760NC 47708 DURING LINE CHECK, FOUND OVERHEAD EMERGENCY LIGHTS OUT. REPLACED BATTERY PACK FOR ROWS 16 AFT, OPERATION CHECKS GOOD. 2 L 7 2 4F RT A6WE 1997010900171 19970109 00171 WP 1997 1 9 9627369856 1 19961228 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 765NC 47718 DURING LINE CHECK, FOUND AFT OVERWING EMERGENCY EXIT LIGHTS ABOVE DOOR DO NOT LIGHT. REPLACED BATTERIES IN PACK 85-25, OPERATION CHECKS GOOD. 2 L 7 2 4F RT A6WE 1997010900172 19970109 00172 EU 1997 1 9 9627373206 1 19961230 A 3350 BATTERY AIRBUS 320 A320211 3930320 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 306US 60 DURING LINE CHECK, EMERGENCY LIGHTS FAILED CIDS PANEL CHECK. REPLACED BATTERIES AND POWER SUPPLY BETWEEN RIGHT OVERWING EXITS, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A28NM 1997010900173 19970109 00173 NE 1997 1 9 9627385640 2 19961230 A 7230 BLADE BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE NR 1 ENG COMP BENT A A NWAA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 01 540US 26487 727170 DURING CLIMB AT 7,000 FT, NR 1 ENGINE EXPERIENCED TWO COMPRESSOR STALLS. AIRCRAFT RETURNED TO MSP. GROUND MAINTENANCE FOUND TWO BENT FAN BLADES. REPLACED BLADES, PMA STATOR AND PROBE CURRENT SENSE RELAY. ENGINE OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F RT A2NM E17NE 1997010900174 19970109 00174 WP 1997 1 9 9627399163 1 19961230 A 8012 39279621 START VALVE DOUG DC9 DC914 3022034 WP PWA JT8 JT8D7 52053 NE RT ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 8906E 38440 4572 45747 657287 AS TAKEOFF POWER WAS APPLIED, THE RIGHT ENGINE START VALVE LIGHT ILLUMINATED. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE RIGHT ENGINE STARTER AND START VALVE, OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F A6WE E2EA 1997010900176 19970109 00176 WP 1997 1 9 9627401162 1 19961230 A 7711 8DJ184LWG1 EPR INDICATOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 3 ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 162US 27415 892 46771 86151 DURING TAKEOFF, THE NR 3 ENGINE EPR INDICATION WAS LOW. TAKEOFF WAS ABORTED. MAINTENANCE REPLACED THE EPR INDICATOR. E NGINE GROUND RUN CHECKED GOOD. 2 L 7 3 4F 4 F A22WE E20EA 1997010900177 19970109 00177 EU 1997 1 9 9627413237 1 19961231 A 2421 740119E IDG AIRBUS 320 A320212 EU RT ENGINE OVERHEATED A NWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 01 337NW 10534 1707 358 DURING CRUISE AT FL310, THE RIGHT ENGINE INTEGRATED DRIVE GENERATOR TEMPERATURE BEGAN CLIMBING WHILE THE INDICATION FLAS HED GREEN. CREW STARTED THE APU AND UNLOADED THE RIGHT GENERATOR WITH NO HELP. DISCONNECTED IDG AT 192 DEGREES CELSIUS . FOLLOWING IDG DISCONNECT, RECEIVED APU LOW FUEL PRESSURE WARNING, DESCENDED TO FL280 WITH NO HELP. AIRCRAFT DIVERTED TO PHX AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE IDG AND IDG OIL COOLER, LEAK AND OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1997010900178 19970109 00178 EU 1997 1 9 9627423223 1 19961230 A 3350 321430 BATTERY AIRBUS 320 A320211 3930320 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 323US 272 DURING LINE MAINTENANCE, THE LEFT FORWARD EPSU DID NOT TEST. REPLACED BATTERY PACK, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1997010900181 19970109 00181 NM 1997 1 9 9627436608 1 19961206 A 5712 RIB BOEING 747 747151 1384891 NM WS 766 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 608US 19785 DURING PERIODIC CHECK, FOUND SEVERAL CRACKS ON THE LEFT WING LEADING EDGE RIB. STOP DRILLED CRACKS, INSTALLED .100 REPA IR ANGLES, AND .160 REPAIR STRAP MADE FROM 7075-T6. REPAIR DONE PER EA 66-120602, SEC 1, MFG PART NUMBER 65B10151-601. 2 L 7 4 4F A20WE 1997010900182 19970109 00182 SO 1997 1 9 COMA9710001 1 19961227 A 5210 12026749003 BOLT EMB 120 EMB120RT SO PAX DOOR CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 259CA 120252 DURING 2C INSPECTION, FOUND PAX DOOR ROTATING ARM ATTACH BOLTS TO BE HEAVILY CORRODED. FORWARD AND AFT PASSENGER DOOR R OTATING ARM ATTACH BOLTS REPLACED WITH SERVICEABLE BOLTS AS PER EMB120 MAINTENANCE MANUAL 52-10-00 PG 401 TO 403. 2 L 7 2 4T RT A31SO 1997010900194 19970109 00194 SO 1997 1 9 COMA9710013 1 19961230 A 3350 RELAY EMB 120 EMB120RT SO CABIN FAILED A COMA K NONE L NO TEST CR CRUISE 1 SO 01 247CA 120225 EMERGENCY LIGHTING NOT ARMED WARNING ON MAP, CIRCUIT BREAKER TRIPPED. COULD NOT DUPLCIATE DISCREPANCY. REPLACED RELAY K201 FOR TROUBLESHOOTING. 2 L 7 2 4T RT A31SO 1997010900195 19970109 00195 SO 1997 1 9 COMA9710014 1 19961223 A 3240 214791 BRAKE EMB 120 EMB120RT SO LT MLG LOCKED UP A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 267CA 15154 2195 120259 THE LT MLG INBD BRAKE LOCKED UP DURING TAXI. REPLACED THE LT INBD BRAKE ASSY. 2 L 7 2 4T RT A31SO 1997010900197 19970109 00197 EU 1997 1 9 COMA9730001 1 19961223 A 3350 6104781 BATTERIES SAAB SF340 SF340A 7850100 EU CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 361CA 340056 EMERGENCY LIGHTING SYSTEM IS INOP. REPLACED THE EMERGENCY LIGHTING BATTERIES. 2 L 7 2 4T RT A52EU 1997010900198 19970109 00198 1997 1 9 COMA9760001 4 19961223 A 3418 3995100207A COMPUTER CNDAIR CL600 CL6002B19 EA E/E COMPT MALFUNCTION A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 966CA 8135 400 7132 STALL FAIL MESSAGE ON EICAS. REPLACED THE STALL COMPUTER. 2 L 7 2 4F RT A21EA 1997010900199 19970109 00199 EA 1997 1 9 COMA9760002 1 19961230 A 3250 16900105 ECU CNDAIR CL600 CL6002B19 EA NLG STEERING FAILED A COMA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 918CA 5525 858 7018 STEERING FAIL MESSAGE DURING CRUISE FLIGHT. REPLACED THE NWS ELECTRONIC CONTROL UNIT. 2 L 7 2 4F RT A21EA 1997010900201 19970109 00201 NM 1997 1 9 SWAA961427 1 19961229 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 28SW 21339 DURING SCHEDULED 1/2 D-CHECK, FOUND FUSELAGE SKIN LAP CRACKED IN LOWER SKIN AT LOWER ROW OF FASTENERS AT BS 500, S10R. R EPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1997010900202 19970109 00202 NM 1997 1 9 SWAA961428 1 19961229 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 765 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 28SW 21339 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORRODED AROUND NUTPLATE HOLES, AFT OF BS 765, LBL 7.5. REPAIRED PER BOEI NG SRM. 2 L 7 2 4F A16WE 1997010900203 19970109 00203 1997 1 9 SWAA961429 2 19961230 A 7220 658536911 DOME BOEING 737 7372H4 138448C NM NR 1 ENGINE MISSING A SWAA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 SW 07 59SW 21811 AFTER TAKEOFF AT 1500 FT, HEARD A VERY LOUD BANG, ENGINE PARAMETERS WERE NORMAL. RETURNED TO MDW AND MADE AN UNEVENTFUL LANDING. DURING INSPECTION, FOUND NR 1 ENGINE NOSE DOME MISSING. REPLACED FRONT ACCESSORY DRIVE SUPPORT AND NOSE DOME PER BOEING M/M. 2 L 7 2 4F A16WE 1997010900204 19970109 00204 NM 1997 1 9 SWAA961430 1 19961228 A 3350 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 87SW 22903 DURING SCHEDULED SERVICE CHECK, FOUND AFT RIGHT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER BOEI NG M/M. 2 L 7 2 4F A16WE 1997010900205 19970109 00205 NM 1997 1 9 SWAA961431 1 19961227 A 3350 6104781 BATTERY BOEING 737 7372K6 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED SERVICE CHECK, FOUND LEFT OVERWING EXIT LIGHT AND LEFT ESCAPE LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1997010900206 19970109 00206 NM 1997 1 9 SWAA961432 1 19961227 A 3350 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK AND HOUSING PER BOEING M/M. 2 L 7 2 4F RT A16WE 1997010900207 19970109 00207 NM 1997 1 9 SWAA961433 1 19961230 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 721/386 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 721, AT S2L, AND AT BS 386 ABOVE S17L. REPAIRED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1997010900208 19970109 00208 NM 1997 1 9 SWAA961434 1 19961230 A 5330 SKIN BOEING 737 7373H4 1384600 NM SERV DOORWAY CRACK A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED D-CHECK, FOUND CRACK IN FUSELAGE SKIN AT BOTTOM LT CORNER OF FORWARD SERVICE DOOR OPENING. REPAIRED PE R BOEING SRM. 2 L 7 2 4F RT A16WE 1997010900209 19970109 00209 NM 1997 1 9 SWAA961435 1 19961230 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED D-CHECK, FOUND MECHANICAL DAMAGE TO FUSELAGE SKIN AT BS 312 S4L, AT BS 990 TO 1011 BETWEEN S13 AND 16L, AT BS 860 TO 886 BETWEEN S2L AND S2R, AND AT BS 363 TO 374 S4L TO 6L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1997010900210 19970109 00210 NM 1997 1 9 SWAA961436 1 19961230 A 5320 CLIPS BOEING 737 7373H4 1384600 NM FUSELAGE DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED D-CHECK, FOUND MECHANICAL DAMAGE TO STRINGER CLIPS, AT BS 344 S8R AND 11R, AND A CRACKED CLIPS AT BS 36 0 S10R, AT BS 787 S4R, AT BS 827 S13R AND AT BS 807 S4R. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1997010900211 19970109 00211 NM 1997 1 9 SWAA961437 1 19961230 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 344 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM DAMAGE AT BS 344, RBL 1 AND 8, WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1997010900212 19970109 00212 NM 1997 1 9 SWAA961438 1 19961230 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 303 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED D-CHECK, FOUND L-ANGLE CRACK AT FWD ENTRY DOOR CUTOUT AT BS 303, LBL 60. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1997010900213 19970109 00213 NM 1997 1 9 SWAA961439 1 19961230 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 987 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 987, WL 208, RBL 5, 15, 19, 28, 43, AND LBL 4, 5, 19, 40, AND 43. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1997010900214 19970109 00214 NM 1997 1 9 SWAA961440 1 19961230 A 5312 BULKHEAD WEB BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED D-CHECK, FOUND BS 178 PRESSURE BULKHEAD WEB CRACKED AT WL 218, RBL 9.5 AND AT WL 202, RBL 5. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1997010900215 19970109 00215 NM 1997 1 9 SWAA961441 1 19961230 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 1008 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED D-CHECK, FOUND SKIN BULGE AT BS 1008, AT S13L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1997010900216 19970109 00216 1997 1 9 SWAA961442 4 19961230 A 2565 D31354433 SLIDE BOEING 737 7373T5 NM PAX DOOR LOW PRESS A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 694SW 23061 DURING WALKAROUND INSPECTION, FOUND LEFT AFT ENTRY DOOR ESCAPE SLIDE PRESSURE BELOW SERVICEABLE LIMITS. REPLACED SLIDE ASSEMBLY PER BOEING M/M. 2 L 7 2 4F RT A16WE 1997010900217 19970109 00217 NM 1997 1 9 SWAA961443 1 19961230 A 2170 COALESCER BAG BOEING 737 7373G7 1384595 NM RIGHT DIRTY A SWAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 683SW 24008 INFLIGHT, RIGHT PACK TRIPPED OFF. RESET AND IT TRIPPED AGAIN, REPORTED LIGHT SMOKE. RETURNED TO LAS AND MADE AN UNEVEN TFUL LANDING. CHECKED SYSTEM AND AIR CYCLE MACHINE FOR LEAKS, NONE FOUND. REPLACED COALESCER BAGS AND OP CHECKED PER B OEING M/M. 2 L 7 2 4F RT A16WE 1997010900218 19970109 00218 NM 1997 1 9 SWAA961444 1 19961228 A 5330 SKIN BOEING 737 7373H4 1384600 NM R2 DOORWAY DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED CHECK, FOUND FUSELAGE SKIN DENTED ABOVE AND SLIGHTLY AFT OF R2 DOOR CUTOUT. REPAIRED PER SWA RA 1-353- 1576. 2 L 7 2 4F RT A16WE 1997010900219 19970109 00219 NM 1997 1 9 SWAA961445 1 19961229 A 5313 STRINGER WEB BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 690SW 23783 DURING SCHEDULED SERVICE CHECK, FOUND LT STRINGER 18A SHEAR BEAM WEB CRACKED, ORIGINATING FROM AFT END OF WEB TO THE MOS T I/B AFT FASTENER HOLE. REPAIRED PER SWA ACO 6580-53. 2 L 7 2 4F RT A16WE 1997010900220 19970109 00220 1997 1 9 SWAA961446 4 19961228 A 2565 D32354433 SLIDE BOEING 737 7375H4 138449D NM AFT ENTRY LOW PRESS A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 510SW 24187 DURING SCHEDULED RON CHECK, FOUND AFT ENTRY DOOR SLIDE PRESSURE LOW. REPLACED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1997010900221 19970109 00221 NM 1997 1 9 SWAA961447 1 19961227 A 3350 P4010021 BATTERY BOEING 737 7375H4 138449D NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 528SW 26570 DURING WALKAROUND INSPECTION, FOUND FWD RIGHT FLASHLIGHT NOT TESTING. REPLACED BATTERY PER BOEING M/M. 2 L 7 2 4F RT A16WE 1997010900222 19970109 00222 1997 1 9 SWAA961448 2 19961226 A 7230 BLADES BOEING 737 7373H4 1384600 NM NR 2 ENGINE BENT A SWAA A UNSCHED LANDING C F.O.D. CL CLIMB 1 SW 07 361SW 26572 EXPERIENCED NUMEROUS BIRD STRIKES AFTER TAKEOFF. ALL ENGINE PARAMETERS REMAINED NORMAL. RETURNED TO SDF AND MADE AN UN EVENTFUL LANDING. PERFORMED BIRD STRIKE INSPECTION. FOUND 2 BENT FAN BLADES ON NR 2 ENGINE, BUT WITHIN M/M LIMITS. OK FOR SERVICE, BORESCOPE SCHEDULED WITHIN 10 CYCLES. 2 L 7 2 4F RT A16WE 1997010900223 19970109 00223 WP 1997 1 9 UPS96821794 1 19961229 A 2750 57726913 ACTUATOR DOUG DC8 DC871F 302199D WP RT TE FLAPS FAILED A IPXA K NONE K J FLUID LOSS WARNING INDICATION LD LANDING 1 SO 01 703UP 45939 INSPECTION TYPE-N/A, AFTER LANDING ROLLOUT WHEN RETRACTING FLAPS, RES LOW LIGHT CAME ON FLAPS WOULD NOT RETRACT, HYD QTY FALLING RAPIDLY, SYS PRS WENT TO 0 PSI. FOUND RT W/FLAP ACT CYL BROKE AT COMPENSATING LINK, AND UP-HYD PRS LINE CRACKE D AT FITTING. REPLACED SAME CYL, PER 27-51-09. SERVICED LOCK-OUT PER 27-51-01, OPS CKD AND LEAK CKD NORMAL PER 27-51-0 9. 2 L 7 4 4F RT 4A25 1997010900224 19970109 00224 SW 1997 1 9 QXEA9600503 1 19961224 A 2721 2742004003 ACTUATOR SWRNGN SWRNGN SA227 SA227AC 8780603 SW RUDDER WORN A QXEA K NONE E VIBRATION/BUFFET CR CRUISE 1 NM 09 27186 1669 AC707 RUDDER VIBRATES WITH TRIM IN NEUTRAL POSITION. TRIMMING AWAY FROM NEUTRAL STOPS THE VIBRATION. RUDDER TRIM ACTUATOR RE PLACED IAW MAINT MANUAL. RUDDER TRIM ACTUATOR PUSH-PULL ROD REPLACED AS A PRECAUTIONARY MEASURE. TRIM RIGGED IAW MAINT MANUAL. TRIM OPS CHECKED GOOD IAW MAINT MANUAL. 2 L 7 2 4T RT A8SW 1997010900225 19970109 00225 SW 1997 1 9 QXEA9600504 1 19961230 A 3310 PS401 POWER SUPPLY SWRNGN SWRNGN SA227 SA227AC 8780603 SW COCKPIT SHORTED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 26861 8977 AC649 CAPTAINS FORWARD CONSOLE AND ROCKER SWITCH PANEL LIGHTS ARE INOP. ELECTRICAL FUMES APPEAR TO COME FROM THE CONSOLE PANE L. POWER SUPPLY REPLACED AND LIGHTS OPS CHECKED GOOD. NO ELECTRICAL FUMES NOTED AFTER THE REPLACEMENT OF THE POWER SUP PLY. 2 L 7 2 4T RT A8SW 1997010900226 19970109 00226 EU 1997 1 9 QXEA9600505 1 19961231 A 3350 1820 BULB FOKKER FOKKER F28 F28MK4000 4990810 EU GALLEY FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 491US 11156 GALLEY SERVICE/EMERGENCY DOOR UPPER EMERGENCY LIGHT IS INOP. BULB WAS RELACED AND LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1997010900231 19970109 00231 NM 1997 1 9 96FDEA01712 1 19961231 A 2910 2249409501 DRAIN LINE DOUG MD11 MD11F 3023600 NM NR 3 ENGINE BROKEN A FDEA O OTHER F K J FLT CONT AFFECTED FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 586FE 48487 HYDRAULIC SYSTEM NR 3 OFF ALERT, HYDRAULIC PRESSURE WENT TO ZERO, SYSTEM QUANTITY WAS AT 3.2 GALLONS AND OTHER WARNINGS WERE PRESENT BECAUSE OF HYDRAULIC LOSS. FABRICATED NEW LINE PER EA 1-2910-31452, INSTALLED AND LEAK CHECKED, OPS CHECKE D GOOD. NEW LINE TO BE REPLACED AT NEXT B-CHECK PER EA 1-2910-31452. 2 L 7 3 4F RT A22WE 1997010900233 19970109 00233 NM 1997 1 9 97FDEA00002 1 19961223 A 5312 65C232311 BULKHEAD FORGING BOEING 727 72725 1384006 NM BS 870 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 117FE 19299 LT FUSE 870 BULKHEAD FORGING. CRACKED BEYOND LIMITS OF SB 727-53-116, REF NR S001. INSTALLED NEW LT 870 FORGING PER FE D EX EA 7-5310-28935, SB 727-53-116, SRM 51-30-2. 2 L 7 3 4F A3WE 1997010900234 19970109 00234 NM 1997 1 9 97FDEA00003 1 19961223 A 5330 SKIN BOEING 727 72725 1384006 NM BS 863-875 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 117FE 19299 CORROSION ON INNER FUSE SKIN STR 10 L STA 863 TO 875, FOUND DURING REPLACEMENT OF 870 CASTING. REMOVED CORROSION AND IN ST DOUBLER AND FILLER ON OUTSIDE OF FUSE PER EA 7-5330-28946 DOUBLER 2024 T 3.071. 2 L 7 3 4F A3WE 1997010900240 19970109 00240 NM 1997 1 9 97FDEA00009 1 19961223 A 5341 FITTING BOEING 727 72725 1384006 NM FS 740 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 117FE 19299 FUSE STA 740 LT WING ATTACH FWD FITTING CORRODED, FOR LT FWD BOTTLE BOLT. REMOVED CORROSION BY REAMING BORE PER BOEING SRM 57-10-7 FIG 2, SHEET 1. FABRICATED AND INSTALLED SLEEVE PER SRM 57-10-7, FIG 2 SHEET 5. 2 L 7 3 4F A3WE 1997010900241 19970109 00241 1997 1 9 MWEA96661 4 19961227 A 3416 28007204 ALTIMETER DOUG DC9 DC914 3022034 WP RT COCKPIT MALFUNCTIONED A MWEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 31 800ME 45842 F/O'S ALTIMETER FLAGGED DURING LEVEL OFF. RETURNED TO MKE. REMOVED AND REPLACED F/O'S PRIMARY ALTIMETER, LEAK CHECK IA W FAR 91.411. ALTIMETER ENCODING NOT C/W AT THIS TIME, NR 2 ALTITUDE ENCODING DEFERRED. 2 L 7 2 4F A6WE 1997010900242 19970109 00242 WP 1997 1 9 MWEA96662 1 19961225 A 2910 O-RING DOUG DC9 DC914 3022034 WP RT MLG WW DAMAGED A MWEA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 31 600ME 45725 PILOT REPORTS, RIGHT HYDRAULIC SYSTEM PRESSURE AND QUANTITY DROPPED TO ZERO. MAINTENANCE REPLACED O-RING ON HYDRAULIC U NION AFT RIGHT MAIN GEAR DOOR ACTUATOR. RESERVICED HYDRAULIC SYSTEM, OPS AND LEAK CHECKED SYSTEM. 2 L 7 2 4F A6WE 1997010900243 19970109 00243 1997 1 9 MWEA96663 4 19961227 A 3416 28007204 ALTIMETER DOUG DC9 DC914 3022034 WP RT COCKPIT MALFUNCTIONED A MWEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 31 800ME 45842 PILOT REPORTS, FIRST ALTIMETER FLAGGED DURING LEVEL OFF. RETURNED TO MKE. MAINTENANCE REMOVED AND REPLACED FIRST OFFIC ERS ALTIMETER, OPS CHECK GOOD. 2 L 7 2 4F A6WE 1997010900246 19970109 00246 NE 1997 1 9 DL72L962769 2 19961225 A 7314 FUEL PUMP 37820113 BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE SHEARED SHAFT A DALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 27 504DA 5443 21306 687376 NR 1 ENG FAILED ON T/O, ALL INDICATIONS NORMAL. FOUND FUEL PUMP SHAFT SHEARED. REPLACED PUMP, CHECKS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1997010900247 19970109 00247 NM 1997 1 9 DL757962771 1 19961225 A 3350 POWER SUPPLY 333780100 BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 613DL 18448 22820 REPLACED OVERWING EMERGENCY LIGHT POWER SUPPLY, CHKS GOOD. 2 L 7 2 4F RT A2NM 1997010900248 19970109 00248 NM 1997 1 9 DL72S962773 1 19960919 A 5753 652163261 SPAR BOEING 727 727232 1384082 NM NR 2 TE MID FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 403DA 21147 NR 2 MID FLAP AFT LOWER SPAR RAIL WAS FOUND CRACKED DURING INSPECTION. REPAIRED PER MM 57-52-0, PAGE 807. 2 L 7 3 4F A3WE 1997010900249 19970109 00249 NM 1997 1 9 DL72S962774 1 19960919 A 5753 652163261 SPAR BOEING 727 727232 1384082 NM NR 2 TE MID FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 403DA 21147 DURING INSPECTION, FOUND NR 2 MID FLAP AFT SPAR RAIL CRACKED. THE RAIL WAS REPAIRED PER MM 57-52-0, PG 807. 2 L 7 3 4F A3WE 1997010900250 19970109 00250 WP 1997 1 9 DLL10962775 1 19961226 A 2560 MEGAPHONE MV10 LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 714DA NA 193C1090 FC MEGAPHONE INOP. REPLACED SAME. 2 L 7 3 4F A23WE 1997010900251 19970109 00251 NM 1997 1 9 DL73K962776 1 19961226 A 7312 MANIFOLD 577957 BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE NR 2 FUEL HEAT RUPTURED A DALA A UNSCHED LANDING M OVER TEMP TO TAKEOFF 1 SO 27 322DL NONE 23094 717148 RIGHT ENGINE OVERHEAT LIGHT ON T/O. FOUND RT ENGINE FUEL HEAT MANIFOLD RUPTURED. REPLACED MANIFOLD. 2 L 7 2 4F 4 F RT A16WE E2EA 1997010900252 19970109 00252 WP 1997 1 9 DLL17962777 1 19961227 A 3520 PBE 4566M37B046N LKHEED 1011 10113853 5265020 WP 3 R DOOR FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 768DL E9342103 193H1216 FLIGHT ATTENDANT REPORTED THAT THE PBE AT 3R HAD IT'S RED INDICATOR EXPOSED OUTSIDE OF CASE. THE PBE WAS REPLACED. 2 L 7 3 4F A23WE 1997010900253 19970109 00253 WP 1997 1 9 DLL10962778 1 19961227 A 3350 LENS 079123 LKHEED 1011 10113851 5265010 WP CABIN MISSING A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 723DA NONE 193C1150 WORKING MCO FLOOR TRACK LIGHTING AT 4C INOP. REPLACED RED LENS, CKS OK. REMOVED MCO/PLAC. 2 L 7 3 4F A23WE 1997010900254 19970109 00254 NM 1997 1 9 DL72S962779 1 19961227 A 3350 BATTERY PACK 900542 BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 496DA VA6447 21076 RIGHT AFT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK AND BATTERY RACK FOR RIGHT AFT OVERWING EMERGENCY E XIT LIGHT, LIGHT OPERATES NORMALLY. 2 L 7 3 4F A3WE 1997010900255 19970109 00255 1997 1 9 DLL14962780 2 19961229 A 7260 GEARBOX LKHEED 1011 1011385115 5265015 WP NR 1 ENGINE OIL LEAK A DALA E A ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SO 27 1738D 17418 14781 193C1234 14781 AFTER T/O, NR 1 ENG LOST ALL OIL QUANTITY. ENGINE WAS SHUTDOWN IAW POM AND RETURNED TO MCO WITHOUT FURTHER INCIDENT. E NGINE INFLIGHT SHUTDOWN REPORT COMPLETED AND PLACED IN LOGBOOK. ALSO, REPORT FAX TO ENGINE ANALYST. REPLACED 06 HIGH S PEED GEARBOX ON ROUTINE CARD DECK. PERFORMED PFHB TEST 1, 3, 9, 16, 20 AND 13, ALL CHECKS NORMAL. 2 L 7 3 4F A23WE 1997010900256 19970109 00256 NM 1997 1 9 DL72L962781 1 19961229 A 2710 CONTROL MODULE 65178234 BOEING 727 727232 1384082 NM LT AILERON LEAKING A DALA O OTHER K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SO 27 513DA 8380 21315 SHORTLY AFTER T/O, AILERON SYS-A LIGHT ACCOMPANIED BY A LOSS OF SY-A HYD FLUID, APPROX 2 MIN AFTER. FOUND AILERON FLIGH T CONTROL MODULE LEAKING. REPLACED SAME, CHECKS NORMAL. 2 L 7 3 4F A3WE 1997010900257 19970109 00257 WP 1997 1 9 DLL13962783 1 19961230 A 3350 POWER SUPPLY 5165741 LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 786DL 37610 193A1123 14781 EMERGENCY LIGHTS INOP. REPLACED PWR SUPPLY, OPS GOOD. 2 L 7 3 4F A23WE 1997010900258 19970109 00258 NM 1997 1 9 DL72S962784 1 19961229 A 3350 BATTERY S106 BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 492DA 21061 AIRSTAIRS EMER LIGHTS INOP. REPLACED BATT, OPS CK GOOD. 2 L 7 3 4F A3WE 1997010900259 19970109 00259 NM 1997 1 9 DLM88962785 1 19961230 A 2560 AL1600 MEDICAL KIT DOUG MD88 MD88 3023688 NM CABIN DEFECTIVE A DALA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 912DL 49543 14781 EMERGENCY MEDICAL KIT USED. REPLACED EMERGENCY MEDICAL KIT. 2 L 7 2 4F RT A6WE 1997010900260 19970109 00260 NE 1997 1 9 DL76P962786 2 19961228 A 7200 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 FAILED A DALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 SO 27 140LL 14389 25988 724691 ON TAKEOFF PASSING 400 FT, AGL LEFT ENG COMPRESSOR STALLED. THROTTLE REDUCED TO IDLE AND RETURN FOR LANDING, MAX EGT 69 7 DEGREE. FOUND ENG AT FAULT. REPLACED NR 1 ENGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 1997010900261 19970109 00261 NM 1997 1 9 DL73E962787 1 19961230 A 3350 RPS1 PWR SUPPLY BOEING 737 7372S3 NM BS 920 INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 367DL 21774 BOTH LT AND RT LOWER EMERG DOOR EXIT IDENTIFIERS INOP. REPLACED EMERG LIGHT PWR SUPPLY PACK M9027, OPS GOOD PER MM. 2 L 7 2 4F RT A16WE 1997010900262 19970109 00262 NM 1997 1 9 DL73E962788 1 19961230 A 2150 DUCT 65544728 BOEING 737 737247 138448D NM RT PACK COLLAPSED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 239WA NONE 23187 ON TAKEOFF AFTER RETRACTING L/GEAR, LOUD BANG FOLLOWED BY SMOKE IN CABIN. A/C RETURNED TO GATE. FOUND DUCT FROM RT PAC K HOT AIR SIDE OF MIX VALVE DISCONNECTED AND COLLAPSED (P/N 65-54474-1). MUFFLER 21-20-0-46A REF G COLLAPSED(P/N 65 -78947-10) AND MIX CHAMBER REF 360 (P/N 65-54472-8) PARTIALLY COLLAPSED. DUCTS REPLACED AND SYS CHKS OK. 2 L 7 2 4F A16WE 1997010900263 19970109 00263 NM 1997 1 9 DLM90962789 1 19961231 A 3244 M90M TIRE DOUG MD90 MD9030 3023690 NM RT MLG FAILED A DALA K NONE O OTHER LD LANDING 1 SO 27 911DA 53391 14781 ON LANDING, NR 4 TIRE BLEW, RIGHT GEAR FLYING DOOR SEPARATED FROM AIRCRAFT. REPLACED NR 3 AND NR 4 WHEEL ASSYS AND FLYI NG DOOR. 2 L 7 2 4F RT A6WE 1997010900264 19970109 00264 NM 1997 1 9 DL757962790 1 19961230 A 2530 FOOD CARRIER NONUMBER BOEING 757 757232 1384965 NM GALLEY DIRTY A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 619DL NA 22909 14781 RETURNED AFTER TAKEOFF WITH SMOKE SMELL IN CABIN. FOUND PROBLEM TO BE MASKING TAPE LEFT ON FOOD CARRIER BY CATERER. TA PE GAVE OFF ODOR WHEN MEALS HEATED. NO MAINTENANCE ACTION NECESSARY. 2 L 7 2 4F RT A2NM 1997010900265 19970109 00265 NM 1997 1 9 DL73K962792 1 19961231 A 2420 P6 PANEL 915F2134 BOEING 737 737232 1384475 NM E/E COMPT TRIPPED A DALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 SO 27 319DL 23091 BOTH GENRATORS WERE LOST AT FL310. ACCOMPLISHED LOSS OF BOTH GENERATORS CHECKLIST PER AOM. DIVERTED TO JFK, STIMATED LANDING WT 103,500 AND LANDING NORMAL. REPLACED G7 BUS PROTECTION PANEL AND R3 RELAY. RUN UP AND FUNCTIONAL CHECK GOOD . 2 L 7 2 4F RT A16WE 1997010900266 19970109 00266 NM 1997 1 9 DL72S962794 1 19961229 A 3350 BATTERY PACK 900835A BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 418DA 3943 21271 LEFT AND RIGHT EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED RACK AND BATTERY PACK, CHECKS NORMAL. 2 L 7 3 4F A3WE 1997010900267 19970109 00267 NM 1997 1 9 DL76L970001 1 19961231 A 3350 LIGHT UNKNOWN BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST CR CRUISE 1 SO 27 174DN NA 24802 EMERGENCY TRACK LIGHT AT 2 LEFT INOPERATIVE AND LIFTED FROM THE FLOORING. RESECURED EMERGENCY TRACK LIGHT, OPERATION NO W NORMAL. 2 L 7 2 4F RT A1NM 1997010900268 19970109 00268 NM 1997 1 9 SCNA96457 1 19961228 A 3350 S106 BATTERY PACK BOEING 727 727225 1384077 NM FWD GALLEY OUT OF POSITION A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 283SC 22559 FOUND FORWARD GALLEY EMERGENCY EXIT LIGHTS EXCESSIVELY DIM. REPOSITIONED BATTERY PACK AND OPS CHECKED GOOD. 2 L 7 3 4F A3WE 1997010900269 19970109 00269 NM 1997 1 9 SCNA96458 1 19961230 A 3350 S106 BATTERY PACK BOEING 727 727225 1384077 NM FWD GALLEY OUT OF POSITION A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 283SC 22559 FOUND FORWARD GALLEY EMERGENCY EXIT LIGHTS EXCESSIVELY DIM. SECURED BATTERY PACK AND OPS CHECKED GOOD. 2 L 7 3 4F A3WE 1997010900270 19970109 00270 SO 1997 1 9 SWIA95801 1 19961225 A 2910 CONNECTOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE GREEN HYD SYST LOOSE A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 205SW 120260 AFTER TAKEOFF, NOISE CAME FROM FO SIDE, SIDE CONSOLE MUCH LIKE RELAY CHATTER WHICH INTENSIFIED. UPON RETURN TO LAND THE RELAY CHATTER QUIT AS REDUCED POWER FOR DESCENT, WINDSHIELD HEAT APPEARED TO WORK NORMALLY WITH CORRECT INDICATION WITH SWITCH POSITION. TROUBLESHOT SYSTEM, FOUND LOOSE CANNON PLUG ON GREEN SYSTEM HYDRAULIC PRESSURE SWITCH, WAS ABLE TO DU PLICATE PROBLEM. TIGHTENED AND CLEANED CANNON PLUG, OPS CHECKS GOOD AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 1997010900271 19970109 00271 SO 1997 1 9 SWIA95802 1 19961225 A 2751 CONNECTOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE TE FLAPS LOOSE A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 215SW 120281 RETURNED TO SLC AFTER FLAP FAULT INDICATION. REMOVED OUTBOARD CANNON PLUGS FOR ACTUATORS AND FOUND SOME MOISTURE. CLEA NED CANNON PLUGS AND CONNECTORS ACCOMPLISHED BIT TEST IAW MM 27-50-00. NO FAULT FOUND AT THIS TIME, OPS CHECKS GOOD. A LSO, INSPECTED ALL ROLLERS AND TRACKS. 2 L 7 2 4T 4 T RT A31SO E20NE 1997010900272 19970109 00272 SO 1997 1 9 SWIA95803 1 19961222 A 2751 3472001001 ANNUNICATOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE TE FLAPS MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 203SW 120240 ON CLIMBOUT, RECEIVED CONTROL FAULT WITH ASSOCIATED MAP LIGHTS. RESET SYSTEM AND RECEIVED ANOTHER CONTROL FLAP FAULT. R EPLACED FLAP ANNUNICATOR AND TESTED IAW MM 27-30-03, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1997010900273 19970109 00273 1997 1 9 SWIA95804 4 19961227 A 3418 3995100207A STALL COMPUTER CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE E/E COMPT MALFUNCTIONED A SWIA O OTHER N FALSE WARNING CL CLIMB 1 NM 07 408SW 7055 STALL FAIL MESSAGE CAUTION CAME ON DURING DEPARTURE AND STAYED ON. REMOVED AND REPLACED STALL COMPUTER, OPS CHECKS GOOD . 2 L 7 2 4F 4 F RT A21EA E15NE 1997010900274 19970109 00274 NM 1997 1 9 P5CA9601254 1 19961228 A 3030 856CC12 PITOT PROBE BOEING 747 747122 1384872 NM FUSELAGE MALFUNCTIONED A P5CA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 23 854FT 19754 RIGHT MAIN PITOT PROBE HEATER LIGHT ILLUMINATED IN CRUISE. DUE TO WEATHER EN ROUTE THE DECISION WAS MADE TO RETURN TO M ELBORNE. REPLACED THE RIGHT MAIN PITOT PROBE, FUNCTIONAL AND LEAK CHECKED PER MAINTENANCE MANUAL 34-11-01. 2 L 7 4 4F A20WE 1997010900275 19970109 00275 NM 1997 1 9 P5CA9601255 1 19961229 A 2710 65B821062 SPRING BOEING 747 747123 1384873 NM AILERON CONTL CRACKED A P5CA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 WP 23 858FT 20109 ON TAXI IN, FIRST OFFICERS CONTROLS STIFF. FOUND AILERON LOAD LIMITER SPRING BROKEN. REPLACED AILERON LOAD LIMITER AND OPERATIONAL CHECKED PER BOEING MAINTENANCE MANUAL 27-11-05. 2 L 7 4 4F A20WE 1997010900276 19970109 00276 WP 1997 1 9 RRXA96176 1 19961224 A 5512 56407991 PANELS DOUG DC8 DC863F 302198F WP HORIZ STAB CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 959R 46143 FERRY FLIGHT, DUE TO HORIZONAL STABILIZER DAMAGE. FOUND 2 EACH HORIZONAL STABILIZER LOWER PANELS DAMAGED AT STA XE160 A ND XE171. CUT OUT DAMAGED PANEL AND STRINGER, FABRICATED NEW PANEL SECTIONS AND SPLICED IN IAW DOUGLAS DWG SRO8550001-7 041. 2 L 7 4 4F 4A25 1997010900277 19970109 00277 WP 1997 1 9 RRXA96178 1 19961227 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 1240 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 500MH 45812 DURING INSPECTION, FOUND 5 INCH CRACK IN LOWER FUSELAGE SKIN AT STA 1240. REPAIRED DAMAGED SKIN TO STA 1240 BY TEMPORAR Y REPAIR IAW ENGINEER DRAWING B87-R01. 2 L 7 4 4F RT 4A25 1997010900278 19970109 00278 WP 1997 1 9 RRXA96175 1 19961228 A 3233 57714071 ATTACH LUGS DOUG DC8 DC873F 302199F WP NLG ACTUATOR BROKEN A RRXA K NONE O OTHER AP APPROACH 1 WP 15 2674U 46062 LOUD NOISE WAS HEARD WHEN GEAR EXTENDED. MAINTENANCE FOUND NLG RETRACT CYLINDER ATTACH LUGS BROKEN ON TOP LEFT SIDE OF NLG. CAPPED AND PLUGGED PRESSURE LINES, SECURED NLG DOWNLOCK PIN TO GEAR, SECURED DISCONNECTED HYDRAULIC LINE AND PREPA RED AIRCRAFT FOR ONE TIME FERRY FLIGHT TO ELLX TO FACILITATE REPAIRS. 2 L 7 4 4F RT 4A25 1997010900281 19970109 00281 WP 1997 1 9 ARWA9612002 1 19961230 A 3350 5708458503 BATTERY PACK DOUG DC8 DC863F 302198F WP CABIN DISCHARGED A ARWA K NONE L NO TEST CR CRUISE 1 SO 19 441J 45988 EMERGENCY LIGHTS DISARM SWITCH WILL NOT DISARM. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, SYSTEM OPS CHECKED N ORMAL IAW 33-50-00. 2 L 7 4 4F 4A25 1997010900282 19970109 00282 1997 1 9 VNAA9612005 4 19961223 A 3442 7008470922 RADAR UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FWD FUSELAGE FAILED A VNAA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 07 424JS 2614 3033 RADAR FAILED AT 22,000 FT, RETURNED TO FIELD WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RADAR UNIT, OPERATI ONAL CHECKED GOOD. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1997010900284 19970109 00284 NM 1997 1 9 VNAA9612009 1 19961229 A 2822 177310 BOOST PUMP DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT WING FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 328JS 3030 ON TAKEOFF ROLL, RECEIVED A EL PUMP FAIL CAS MESSAGE ON LT SIDE. ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT FURTH ER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LT ELECTRIC BOOST PUMP, OPERATIONAL CHECKED GOOD. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1997010900286 19970109 00286 NM 1997 1 9 CKSA96406 1 19961218 A 2150 BACC10DU600 COUPLING BOEING 727 727223 1384074 NM RT PACK DISCONNECTED A CKSA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 23 6806 19481 HEARD LOUD NOISE FROM CABIN, LOST PRESSURIZATION, UNABLE TO CONTROL. DESCENDED TO 10,000 AT 10,000 MAX CABIN DIFFERENT IAL PRESSURE WAS 0.8, CABIN ALTITUDE 8,000. FOUND DUCT AT RIGHT HAND PACK WATER SEPARATOR DISCONNECTED. RESECURED DUCT , LEAK CHECKED GOOD. PRESSURIZED AIRCRAFT CHECKED GOOD AS PER B727 MM 21-10-0. 2 L 7 3 4F A3WE 1997010900287 19970109 00287 WP 1997 1 9 TC8A96074 1 19961231 A 2710 POWER BYPASS DOUG DC8 DC8F55 3021928 WP AILERON OUT OF ADJUST A TC8A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 808CK 45817 ON TAXI DURING CONTROL CHECK, AILERONS WENT INTO MANUAL REVERSION AND SYSTEM PRESS 800 PSI. ADJUSTED LT AND RT AILERON POWER BYPASS IAW DACO MM 27-5-2, OPS CHECKS GOOD. 2 L 7 4 4F 4A25 1997010900288 19970109 00288 SO 1997 1 9 SRAA961213 1 19961224 A 6120 582855 VALVE HOUSING LKHEED 382 382E 526413U SO NR 4 ENGINE DEFECTIVE A SRAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 23 910SJ 4383 DURING FLIGHT, NR 4 ENGINE WENT TO 103 PERCENT RPM, AT THE SAME TIME ENGINE TORQUE, TIT AND FUEL FLOW READINGS WERE DECR EASING. SHUT DOWN NR 4 ENGINE AND LANDED WITHOUT INCIDENT. FOUND NR 4 VALVE HOUSING DEFECTIVE. REPLACED NR 4 VALVE HO USING, OPS CHECKED IAW J/C 7101 AND 7101-2. 2 H 7 4 4T A1SO 1997010900289 19970109 00289 WP 1997 1 9 SRAA961214 1 19961225 A 2612 FIRE LOOP DOUG DC8 DC871F 302199D WP NR 1 ENG OUT OF POSITION A SRAA O OTHER N FALSE WARNING DE DESCENT 1 GL 23 872SJ 46040 DURING DESCENT, FIRE BELL RANG ONCE AND NR 1 SHORT CIRCUIT TEST LIGHT FLICKERED ON BRIEFLY THEN STOPPED. AIRCRAFT LANDE D WITHOUT INCIDENT. INSPECTED NR 1 ENGINE, FOUND FIRE LOOP OUT OF POSITION, REPOSITIONED FIRE LOOP, PERFORMED FUNCTIONA L CHECK AND ENGINE RUN-UP CHECK. FIRE WARNING OPERATED NORMALLY PER MM CH 26-00-00. 2 L 7 4 4F RT 4A25 1997010900290 19970109 00290 SO 1997 1 9 SRAA961215 1 19961228 A 3350 LIGHT LKHEED 382 382E 526413U SO CABIN MISINSTALLED A SRAA K NONE L NO TEST CR CRUISE 1 GL 23 910SJ 4383 DURING FLIGHT, FOUND THE EMERGENCY EXIT LIGHT WOULD NOT FUNCTION PROPERLY IN THE ARMED OR ON POSITIONS. FOUND LIGHT ASS EMBLY MOUNTED BACKWARDS. REMOVED LIGHT, CLEANED ALL CONNECTIONS AND REINSTALLED EMERGENCY LIGHT, SYSTEM OPS CHECKED IAW MM CH 23. 2 H 7 4 4T A1SO 1997010900292 19970109 00292 GL 1997 1 9 97ZZZX37 2 19960807 A 7200 ENGINE CESSNA 525 525 2076601 CE WILINT FJ44 FJ44 66000 GL RIGHT FAILED A L A FUBA E ENGINE SHUTDOWN M OVER TEMP TX TAXI/GRND HDL 1 NE 03 525AL 525011 1010 AFTER SEVERAL ENGINE START ATTEMPTS, INSPECTION REVEALED THE ENGINE COWLING WAS BURNED AND THE TAILPIPE WAS DISTORTED DU E TO HEAT DAMAGE. THE RIGHT ENGINE WAS REPLACED. 1 L 7 2 4F 4 F RT A1WI E3GL 1997010900293 19970109 00293 GL 1997 1 9 97ZZZX38 2 19961015 A 7200 ENGINE CESSNA 525 525 2076601 CE WILINT FJ44 FJ44 66000 GL LEFT FAILED A A FUBA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 NE 03 525AL 525011 1011 DURING A ROUTINE FLIGHT ON SECOND LEG FROM PHU TO BRD ABOUT 3 HOURS INTO THE FLIGHT, THE CREW MEMBERS HEARD A POP FROM T HE LEFT ENGINE. AT THE SAME TIME, THE OIL PRESSURE DECREASED TO 15 PSI IN THE LEFT ENGINE. THE PILOT SHUT DOWN ENGINE AND DIVERTED TO CLOSEST AIRPORT AND LANDED IN DLH. AFTER LANDING, THE ENGINE BLADES WOULD NOT ROTATE AND THERE ARE META L CHIPS ON THE CHIP DETECTORS. THE CAUSE OF THE PROBLEM IS UNKNOWN AT THIS TIME. 1 L 7 2 4F 4 F RT A1WI E3GL 1997010900294 19970109 00294 NE 1997 1 9 USAABB96047 2 19961117 A 7200 ENGINE BOEING 757 757225 1384959 NM RROYCE RB211 RB211535E4 54555 NE NR 1 BIRD STRIKE A USAA A UNSCHED LANDING B C SMOKE/FUMES/ODORS/SPARKS F.O.D. CL CLIMB 1 EA 19 607AU 22203 BOS - FLT 29 - CREW NOTED BIRD STRIKE IN NR 1 ENGINE SHORTLY AFTER TAKEOFF. BURNING SMELL WAS NOTED COMING FROM THE AIR CONDITIONING SYSTEM. LEFT FUEL FLOW INDICATION JUMPED HIGHER THAN RIGHT, THEN BECAME INOPERATIVE. FLIGHT RETURNED TO BOS AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE CARRIED OUT EXTERIOR AND BORESCOPE INSPECTIONS OF THE ENGINE. NO DEFECTS WERE FOUND. FUEL FLOW INDICATION RETURNED TO NORMAL AT THE GATE. RUN UP OF ENGINE WAS PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE. (X) 2 L 7 2 4F 4 F RT A2NM E12EU 1997010900295 19970109 00295 WP 1997 1 9 97ZZZX39 1 19961119 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 580 L30 CORROSION A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 910VJ 47277 DURING A SCHEDULED INSPECTION AT AERO CORP, CORROSION WAS FOUND IN THE SKIN AT STA 580, LONGERON 30. 2 L 7 2 4F A6WE 1997010900296 19970109 00296 SO 1997 1 9 ASOA96052 1 19961117 A 2752 3203001001 ACTUATOR EMB 120 EMB120RT SO LT TE FLAP DEFECTIVE A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 11 131AM 120158 DFW/AEX - FLT 9131 - ON APPROACH, CREW EXPERIENCED A FLAP CONTROL FAULT. RESET INITIALLY, BUT CONTINUED TO FAULT ON THE GROUND. THE AIRCRAFT WAS FOUND SAFE FOR A ZERO-FLAP FERRY FLIGHT TO DFW. INBOUND DFW, THE CAPTAIN DECLARED AN EMERGEN CY. LANDING WAS MADE UNEVENTFULLY. REMOVED AND REPLACED THE LEFT INBOARD FLAP ACTUATOR. AS PREVENTIVE MAINTENANCE, AL SO REPLACED THE FLAP CONTROL HANDLE. OPERATIONAL CHECKS WERE NORMAL, AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (X) 2 L 7 2 4T RT A31SO 1997010900297 19970109 00297 SO 1997 1 9 ASOA96049 1 19961113 A 7931 CONNECTOR EMB 120 EMB120RT SO LT ENGINE DIRTY A ASOA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 11 265AS 16462 5520 120170 UPON DEPARTURE CSG/ATL - RECEIVED RED MAP LIGHT 'OIL', AWU 'OIL', AND NOTED OIL PRESSURE GAUGE FLUCTUATING, THE WARNING S SELF-EXTINGUISHED THEN RECURRED TWO MORE TIMES. THE CREW PROCEEDED WITH THE CLIMB-OUT AND NOTIFIED THE TOWER OF THE N EED TO RETURN. THE WARNINGS EXTINGUISHED WITH THE ENGINE POWER BELOW 100 PERCENT AND THE CREW ELECTED TO KEEP THE ENGIN E RUNNING. LANDING WAS MADE SAFELY AND WITHOUT INCIDENT. LOCAL MECHANIC ADDED 1 QUART OF OIL TO THE LEFT ENGINE AND CL EANED THE CANNON PLUG AT THE TRANSDUCER. PERFORMED GROUND RUN-UP, NO LEAKS NOTED. ATL MTC INSPECTED OIL PRESSURE TRANS MITTER AND GROUND RAN THE ENGINE. OPERATIONAL AND LEAK CHECKS WERE GOOD, AIRCRAFT RELEASED FOR SERVICE. (X) 2 L 7 2 4T RT A31SO 1997010900298 19970109 00298 EU 1997 1 9 MALA965188 1 19961107 A 2432 501122804 POWER SUPPLY SAAB SF340 SF340A 7850100 EU COCKPIT EMERG FAILED A MALA K NONE L NO TEST AP APPROACH 1 GL 15 114XJ 340A114 FLT 3113 - ON APROACH TO DTW - THE EMER PWR LIGHT ILLUMINATED 5 TO 6 TIMES. MAINTENANCE REPLACED THE EMERGENCY POWER SU PPLY. (X) 2 L 7 2 4T RT A52EU 1997010900299 19970109 00299 EU 1997 1 9 MALA965189 1 19961108 A 7931 CONNECTOR SAAB SF340 SF340A 7850100 EU RT PROP DIRTY A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 114XJ 340A114 FLT 3030 - EN ROUTE TO DTW, THE RIGHT PROP OIL PRESSURE BEGAN TO FLUCTUATE FULL SCALE. ALL OTHER ENGINE PARAMETERS WERE NORMAL. THE AIRCRAFT DIVERTED TO TVC. MAINTENANCE CLEANED THE CANNON PLUG AT THE RIGHT PGB OIL TRANSDUCER. ALL CHECK S SATISFACTORY DURING GROUND RUNS. (X) 2 L 7 2 4T RT A52EU 1997010900300 19970109 00300 EU 1997 1 9 MALA965194 1 19961110 A 3020 447301 CONTROL BOX SAAB SF340 SF340A 7850100 EU RT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 89XJ 340A089 FLT 3384 - DURING CLIMB-OUT FROM DTW, THE RIGHT INTAKE LIGHT ILLUMINATED WHEN THE ICE PROTECTION WAS TURNED OFF. THE AI RCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE RIGHT ENGINE ANTI-ICE CONTROL BOX. ALL CHECKS SATISFACTORY. 2 L 7 2 4T RT A52EU 1997010900301 19970109 00301 EU 1997 1 9 MALA965179 1 19961103 A 3350 CONNECTOR SAAB SF340 340B 7860101 EU CABIN LOOSE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 403XJ 340B403 FLT 3311 - DURING THE PRE-FLIGHT INSPECTION IN DTW, THE EMERGENCY EXIT LIGHT ABOVE THE FLIGHT ATTENDANT'S SEAT WAS FOUND INOPERATIVE. MAINTENANCE RESECURED LOOSE PLUG WIRES AT PLUG 465VP. ALL CHECKS SATISFACTORY. (X) 2 L 7 2 4T RT A52EU 1997010900302 19970109 00302 NM 1997 1 9 USAABB96051 1 19961115 A 3350 9221009 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 625VJ 27246 LAX - FOUND R1 DOOR EXIT LIGHT BATTERY DEAD. REPLACED BATTERY. (X) 2 L 7 2 4F RT A2NM 1997010900303 19970109 00303 EU 1997 1 9 97ZZZX40 1 19961117 A 3260 WARNING HORN STBROS SD3 SD360 8100606 EU LANDING GEAR OUT OF ADJUST A GUUA O OTHER N FALSE WARNING UK UNKNOWN 1 SO 19 261GA SH3745 MCO/MIA - FLT 396 - PILOT REPORT: GEAR WARNING HORN GOES OFF 13-1400 TQ. CORRECTIVE: ADJUSTED GEAR WARNING HORN. OPS CHK GOOD ON GROUND AND ON TEST FLIGHT. 2 H 7 2 4T A41EU 1997010900304 19970109 00304 NM 1997 1 9 97ZZZX41 1 19961122 A 4950 490400 PERI SEALS GTCP85129 BOEING 737 737291 138448W NM APU DUCT WORN A RYNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 07 730TJ P35402 20364 PROBLEM: APU FIRE WARNING INFLIGHT. CORRECTIVE ACTION: REMOVED AND REPLACED 6 EACH PERI SEALS ON APU BLEED AIR DUCT. 2 L 7 2 4F A16WE 1997010900305 19970109 00305 CE 1997 1 9 GLBA96215 1 19961106 A 2460 1293800161 DC PWR PANEL BEECH 1900 1900D 1154162 CE COCKPIT FAILED A GLBA O OTHER H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 CE 01 208GL 0532 UE208 FAR - RIGHT GENERATOR WILL NOT COME ON LINE. MAINTENANCE REPLACED THE RIGHT DC POWER PANEL. (X) 2 L 7 2 4T RT A24CE 1997010900306 19970109 00306 1997 1 9 JBXA00029 4 19961118 A 2230 AUTOTHROTTLE FOKKER F28 F28MK0100 4990807 EU LT/RT ENGINES MALFUNCTIONED A JBXA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 05 110ML 11486 RDU - FLT 771 - BOTH AUTOTHROTTLES FAULTED PRIOR TO 80 KNOTS, ABORTED TAKEOFF. CORRECTIVE ACTION: PERFORMED AFCAS MAIN TENANCE, SHOWED TOGA SWITCH, FCC1, FCC2. RESET TOGA SWITCH, PERFORMED FCC1, FCC2 TEST AND FAC1, 2 TEST ON AFCAS. MAIN TENANCE TEST DONE IAW F-100 MM 22-11-00. VERIFIED SECONDARY LOCK ACTUATORS ON BOTH T/R'S ARE WORKING. SYSTEM OPS CHECK NORMAL. OK FOR SERVICE AT THIS TIME. (X) 2 L 7 2 4F RT 1997010900307 19970109 00307 EU 1997 1 9 RAIA961112 1 19961112 A 2912 QA03043 FILTER JETAIR JETSTM JETSTM4101 1500501 EU HYD BAY DIRTY A RAIA O OTHER O OTHER AP APPROACH 1 CE 03 571HK 1043 41090 MEM - FLT 7149 - NOSE GEAR TOOK TOO LONG TO EXTEND. MAINTENANCE REPLACED THE HYDRAULIC PRESSURE FILTER AND RETURN FILTE R. (X) 2 L 7 2 4T RT A41NM 1997010900308 19970109 00308 NM 1997 1 9 ZZDA2721696 1 19961109 A 2751 1817381 TRANSMITTER BOEING 737 7372P6 NM TE FLAPS MALFUNCTIONED A A ZZDA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 SO 15 1PC 50016 21613 CAK - FLT 720 - ON APROACH INTO CAK, THE AIRCRAFT EXPERIENCED A FLAP ASSEMETRY TRIP. CAPTAIN ELECTED TO DIVERT INTO CVG WHERE A NORMAL LANDING WAS MADE. MECHANICS TROUBLESHOT SYSTEM AND FOUND THE RIGHT FLAP POSITION/STALL WARNING TRANSMIT TER AND THE TRAILING EDGE FLAP POSITION INDICATOR WERE INOPERATIVE. REMOVED AND REPLACED THE FLAP TRANSMITTER AND POSIT ION INDICATOR IAW BOEING MM 27-58. OPERATIONALLY CHECKED NORMAL. RELEASED AIRCRAFT FOR FLIGHT. INDICATOR PN 18-1299-6 , SN 02746. PART CONDITION: SERVICEABLE. (X) 2 L 7 2 4F RT A16WE 1997010900309 19970109 00309 NM 1997 1 9 ZZDA2121596 1 19961031 A 2150 SENSE LINE 106070710 BOEING 737 7372L9 1384497 NM LT ENGINE MALFUNCTIONED A ZZDA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 15 465AT 5887 21528 MCO - FLT 822 - FLIGHT DEPARTED MCO 10-31-96 WITH THE LEFT AIR CONDITIONING PACK TRIPPING AFTER TAKEOFF. RESET PACK. L OST CONTROL OF LEFT PACK MIX VALVE. ABLE TO CONTROL MIX VALVE AFTER LANDING. TROUBLESHOT SYSTEM PER 737 MM, CHAPTER 21 -11-0, AND FOUND LOOSE SENSE LINE FROM THE PRESSURE REGULATOR TO THE FLOW CONTORL VALVE BLEEDING AIR. TIGHTENED LOOSE S ENSE LINE AND LT PACK OPS CHECKED NORMAL. REFERENCE AML-1 LOG SHEETS 097-2394, 2395, 2396, AND 2431. (X) 2 L 7 2 4F RT A16WE 1997010900310 19970109 00310 WP 1997 1 9 TWAA9615601 1 19961216 A 3350 58222 BATTERY PACK DOUG DC9 DC941 302207N WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 933L 47617 STL - DURING CRUISE AISLE EGRESS LIGHTS ILLUMINATED AT SEAT ROWS 14 THROUGH 18. FOUND BATTERY PACK, MFG P/N 5822-2, WEA K. REPLACED BATTERY PACK. EGRESS LIGHTING SYSTEM OPERATION THEN CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 1997010900311 19970109 00311 WP 1997 1 9 TWAA9615202 1 19961208 A 3350 LIGHTS DOUG DC9 DC941 302207N WP COCKPIT INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 933L 47617 STL - FLT 550 - DURING PRE-FLIGHT, CABIN EGRESS LIGHTS WERE INOPERATIVE. RESET ARM AND CHANGE CIRCUIT BREAKER. OPERATI ON CHECK NORMAL. OP-15 - 11-15-96 - STL. (X) 2 L 7 2 4F A6WE 1997010900312 19970109 00312 NM 1997 1 9 PCAA9600322 1 19961111 A 5311 FRAME DHAV DHC8 DHC8102 2809003 NM AFT FUSELAGE CRACKED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 832EX 280 DURING A C-CHECK INSPECTION, FRAME NR 4 IN THE TAIL SECTION AT STR 4S WAS FOUND CRACKED. FRAME NR 4 WAS REPAIRED IAW DH C RD 8-55-199. A/C RETURNED TO SERVICE. ACTT: 13,173. ACTC: 15,058. (X) 2 H 7 2 4T RT A13NM 1997010900313 19970109 00313 NM 1997 1 9 PCAA9600318 1 19961102 A 5610 07803 WINDSHIELD DHAV DHC8 DHC8102 2809003 NM RT COCKPIT SHATTERED A PCAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 13 832EX 995 TH2106 280 FIRST OFFICER'S WINDSHIELD SHATTERED IN CRUISE FLIGHT AT 21,000 FEET. A/C DIVERTED INTO SCE. REMOVED AND REPLACED F/O' S WINDSHIELD IAW DHC MM. A/C RETURNED TO SERVICE. ACTT: 13,105 ACTC: 14,988. (X) 2 H 7 2 4T RT A13NM 1997010900314 19970109 00314 CE 1997 1 9 GLBA96228 1 19961122 A 7110 COWLING BEECH 1900 1900D 1154162 CE LT ENGINE CAME LOOSE A GLBA O OTHER O OTHER NR NOT REPORTED 1 CE 01 202ZK UE202 MAX - LEFT ENGINE COWLING POPPED IN-FLIGHT. MAINTENANCE INSPECTED AND RESECURED INBOARD COWL. OPS CHECKS GOOD. (X) 2 L 7 2 4T RT A24CE 1997010900315 19970109 00315 CE 1997 1 9 GLBA96220 1 19961108 A 3230 RETRACT MECH BEECH 1900 1900D 1154162 CE RT MLG OUT OF ADJUST A GLBA O OTHER J WARNING INDICATION CL CLIMB 1 CE 01 202ZK UE202 RDU - GROUND LOCK J-HOOK ON LANDING GEAR HANDLE WOULD NOT CLEAR HANDLE UNTIL 10 SECONDS AFTER TAKEOFF. MAINTENANCE ADJU STED ROD-END ON RIGHT GEAR SAFETY SWITCH, CLEANED SAFETY SWITCH CANNON PLUGS, OPS CHECKS GOOD. (X) 2 L 7 2 4T RT A24CE 1997010900316 19970109 00316 NE 1997 1 9 97ZZZX42 2 19960718 A 7260 430124102 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE ACCESSORY DRV LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 10UM 482 7231 LE45522EF SEALS LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH 3 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997010900317 19970109 00317 NE 1997 1 9 97ZZZX43 2 19960718 A 7260 430101501 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE ACCESSORY DRV LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 10UM 482 7231 LE45522EF SEALS LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW 3 EACH UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997010900318 19970109 00318 NE 1997 1 9 97ZZZX44 2 19960718 A 7260 430101301 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE ALTERNATOR AFT LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 10UM 482 7231 LE45522EF SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997010900319 19970109 00319 NE 1997 1 9 97ZZZX45 2 19960916 A 7260 230307203 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE CSD LIP LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 10UM 245 7231 LE45807F SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997010900320 19970109 00320 NE 1997 1 9 97ZZZX46 2 19960916 A 7250 410106701 SEAL RING BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE TURB SHROUD WORN A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 10UM 245 7231 LE45807F SEAL RING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997010900322 19970109 00322 NE 1997 1 9 97ZZZX48 2 19960916 A 7260 430101201 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE ALTERNATOR FWD LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 10UM 245 7231 LE45807F SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997010900323 19970109 00323 NE 1997 1 9 97ZZZX49 2 19960916 A 7260 430101301 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE ALTERNATOR AFT LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 10UM 245 7231 LE45807F SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997010900324 19970109 00324 NE 1997 1 9 97ZZZX50 2 19960916 A 7230 430150601 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE NR 2 BEARING LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 10UM 245 1544 7231 LE45807F NR 2 BEARING SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997010900325 19970109 00325 NE 1997 1 9 97ZZZX51 2 19960916 A 7260 430124102 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE ACCESSORY DRV LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 10UM 245 7231 LE45807F SEALS LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997010900326 19970109 00326 NE 1997 1 9 97ZZZX52 2 19960718 A 7260 430101201 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE ALTERNATOR FWD LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 10UM 482 7231 LE45522EF SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997010900327 19970109 00327 NE 1997 1 9 97ZZZX53 2 19960718 A 7260 230307203 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE CSD LIP LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 10UM 482 7231 LE45522EF CSD LIP SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997010900328 19970109 00328 NE 1997 1 9 97ZZZX54 2 19960816 A 7230 430151101 BEARING BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE NR 2 DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 10UM 597 43556 7231 LE45514EF REMOVED DEFECTIVE NR 2 BEARING TO C/W SB LT101-72-10-0151. REPLACEMENT PART FROM KIT PN T054K21717. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997010900329 19970109 00329 NE 1997 1 9 97ZZZX55 2 19960816 A 7230 430150601 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE NR 2 BEARING LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 10UM 597 1324 7231 LE45514EF SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997010900330 19970109 00330 NE 1997 1 9 97ZZZX56 2 19960816 A 7260 430124102 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE ACCESSORY DRV LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 10UM 597 7231 LE45514EF SEALS LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH 3 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997010900331 19970109 00331 NE 1997 1 9 97ZZZX57 2 19960816 A 7260 430101301 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE ALTERNATOR AFT LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 10UM 597 7231 LE45514EF SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997010900332 19970109 00332 NE 1997 1 9 97ZZZX58 2 19960816 A 7260 430101201 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE ALTERNATOR FWD LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 10UM 597 7231 LE45514EF SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997010900333 19970109 00333 NE 1997 1 9 97ZZZX59 2 19960816 A 7250 410106802 SPRING BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE SEAL RING WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 10UM 597 7231 LE45514EF SEAL RING SPRING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997010900334 19970109 00334 NE 1997 1 9 97ZZZX60 2 19960816 A 7250 410106701 SEAL RING BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE TURB SHROUD WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 10UM 597 7231 LE45514EF SEAL RING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH UNIT UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997010900335 19970109 00335 NE 1997 1 9 97ZZZX61 2 19960816 A 7260 230307203 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE CSD LIP LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 10UM 597 7231 LE45514EF CSD LIP SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997010900336 19970109 00336 NE 1997 1 9 97ZZZX62 2 19960723 A 7250 430144801 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE NR 3 BEARING LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 420MB 560 38945 7077 LE45207E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1997010900337 19970109 00337 NE 1997 1 9 97ZZZX63 2 19960723 A 7260 430101501 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE ACCESSORY DRV LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 420MB 560 7077 LE45207E SEALS LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH 3 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1997010900338 19970109 00338 NE 1997 1 9 97ZZZX64 2 19960723 A 7260 430101301 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE ALTERNATOR AFT LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 420MB 460 7077 LE45207E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1997010900339 19970109 00339 NE 1997 1 9 97ZZZX65 2 19960723 A 7260 430101201 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE ALTERNATOR FWD LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 420MB 560 7077 LE45207E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1997010900340 19970109 00340 NE 1997 1 9 97ZZZX66 2 19960723 A 7250 410106701 SEAL RING BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE TURB SHROUD WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 420MB 560 7077 LE45207E SEAL RING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1997010900341 19970109 00341 NE 1997 1 9 97ZZZX67 2 19960723 A 7260 230307203 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE CSD LIP LEAKING A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 420MB 560 7077 LE45207E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1997010900342 19970109 00342 NE 1997 1 9 97ZZZX68 2 19960606 A 7260 430124102 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101650B1 41560 NE ACCESSORY DRV LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 5188B 129 7163 LE45757EF SEALS LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH 3 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1997010900343 19970109 00343 NE 1997 1 9 97ZZZX69 2 19960606 A 7260 430101301 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE ALTERNATOR AFT LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 5188B 129 7163 LE45757EF SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997010900344 19970109 00344 NE 1997 1 9 97ZZZX70 2 19960606 A 7260 430101201 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE ATLERNATOR FWD LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 5188B 129 7163 LE45757EF SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997010900345 19970109 00345 NE 1997 1 9 97ZZZX71 2 19960606 A 7260 230307203 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE CSD LIP LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 5188B 129 7163 LE45757EF SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997010900346 19970109 00346 NE 1997 1 9 97ZZZX72 2 19960703 A 7260 430124102 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE ACCESSORY DRV LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 7059N 400 7154 LE45755E SEALS LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH 3 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997010900347 19970109 00347 NE 1997 1 9 97ZZZX73 2 19960703 A 7260 430101201 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE ALTERNATOR FWD LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 7059N 400 7154 LE45755E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997010900348 19970109 00348 NE 1997 1 9 97ZZZX74 2 19960703 A 7230 430124202 BEARING BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE NR 1 WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 7059N 961 3214 7154 LE45755E BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997010900349 19970109 00349 NE 1997 1 9 97ZZZX75 2 19960703 A 7250 410106802 SPRING BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE SEAL RING WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 7059N 961 7154 LE45755E SEAL RING SPRING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997010900350 19970109 00350 NE 1997 1 9 97ZZZX76 2 19960703 A 7250 410106701 SEAL RING BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE TURB SHROUD WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 7059N 961 7154 LE45755E SEAL RING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997010900351 19970109 00351 NE 1997 1 9 97ZZZX77 2 19960703 A 7260 230307203 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE CSD LIP LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 7059N 400 7154 LE45755E CSD LIP SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997010900352 19970109 00352 EU 1997 1 9 97ZZZX78 1 19961121 A 2913 704A34310006 PUMP SNIAS 350 AS350B2 8680813 EU HYD SYS DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 96LG 933 50337442 2817 HYDRAULIC PUMP LOW PRESSURE OUTPUT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1997010900353 19970109 00353 EU 1997 1 9 97ZZZX79 1 19961121 A 2912 BFS155 REGULATOR SNIAS 350 AS350B2 8680813 EU FILTER LOW PRESSURE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 96LG 933 61 2817 FILTER REGULATION UNIT LOW PRESSURE READING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1997010900354 19970109 00354 NE 1997 1 9 97ZZZX80 2 19960719 A 7260 430101801 BEARING BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE ACCESSORY DRV ROUGH A R7MA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 11 951AM 7017 LE45291E NEW BEARING ROUGH OUT-OF-BOX. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1997010900355 19970109 00355 CE 1997 1 9 12196825AA 1 19961202 A 3260 1EN18 SWITCH LEAR 24 24 5170302 CE LT MLG DOWN MALFUNCTION A KKFA K NONE N FALSE WARNING NR NOT REPORTED 1 GL 23 825AA 147 LEFT LANDING GEAR DOWN LIGHT INTERMITTENT. COULD NOT DUPLICATE DISCREPANCY. REPLACED LEFT MAIN GEAR DOWN AND LOCK WITH NEW AS A PRECAUTIONARY MEASURE. ADJUSTED AND SWUNG GEAR. CHECKED GOOD. ALL WORK DONE IAW LEAR 24 MM. (X) 2 L 7 2 4J A10CE 1997010900356 19970109 00356 WP 1997 1 9 97ZZZX81 1 19961119 A 5730 SKIN DOUG DC9 DC932 3022066 WP RT WING CRACKED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 910VJ 47277 DURING A SCHEDULED INSPECTION AT AERO CORP., A 1 INCH CRACK WAS FOUND ON THE RIGHT WING UPPER SKIN PANEL FROM EDGE OF AC CESS PANEL NR 1410 A LANDING, THROUGH FASTENER HOLE AT AFT OUTBOARD QUADRANT OF ACCESS OPENING. STOP DRILLED CRACK, FAB RICATED DOUBLER 7075T6 .0375 15 .75 INCH BY 29 INCHES IAW DC9 SRM 57-03, FIG 23. DRILLED DOUBLER, COUNTERSUNK AND DEBUR RED IAW DC9 SRM 51-10-4. ALODINED AND PRIMED IAW DC9 SRM 51-10-3, INSTALLED DOUBLER IAW DC9 SRM 57-03, FIG 23. NON-ROU TINE REF NR 027N1-0058. 2 L 7 2 4F A6WE 1997010900357 19970109 00357 1997 1 9 AWXA9600781 4 19961230 A 2565 D31591459AW SLIDE BOEING 737 7373G7 1384595 NM L1 DOOR MALFUNCTIONED A AWXA K NONE O OTHER TX TAXI/GRND HDL 1 WP 28 150AW 23218 L-1 DOOR SLIDE BLEW ON OPENING OF DOOR. REMOVED AND REPLACED L-1 DOOR SLIDE PER MM 25-00. 2 L 7 2 4F RT A16WE 1997010900361 19970109 00361 NM 1997 1 9 AWXA9600782 1 19961220 A 5320 65176884165 SILL BOEING 737 7373Y0 1384671 NM PAX DOOR CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 DURING ROUTINE MAINTENANCE CHECK, FOUND BS 338 FWD ENTRY DOOR MOPSILL CORRODED. REPLACED MOPSILL IAW SRM 51-40-02, SRM 53-10-15. 2 L 7 2 4F RT A16WE 1997010900362 19970109 00362 NM 1997 1 9 AWXA9600783 1 19961219 A 5315 FLOORBEAM BOEING 737 7373Y0 1384671 NM BS 312 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 DURING ROUTINE MAINTENANCE CHECK, FOUND BS 312 LBL 1 WL 208 FLOORBEAM UPPER CHORD HAS CORROSION. REMOVED UPPER CHORD FR OM BS 312 FLOORBEAM FROM RBL 20 TO LBL 20 AND REPAIRED IT IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 1997010900363 19970109 00363 NM 1997 1 9 AWXA9600784 1 19961220 A 5347 SEAT TRACK BOEING 737 7373Y0 1384671 NM BS 348 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 DURING ROUTINE MAINTENANCE CHECK, FOUND BS 348 RBL 45 WL 208 SEAT TRACK CORRODED. REMOVED, FABRICATED AND INSTALLED SEA T TRACK IAW SRM 53-00-52, 51-40-02. 2 L 7 2 4F RT A16WE 1997010900364 19970109 00364 NM 1997 1 9 AWXA9600785 1 19961220 A 5347 CARGO TRACK BOEING 737 7373Y0 1384671 NM BS 500 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 DURING ROUTINE MAINTENANCE CHECK, FOUND RT CARGO TRACK CORRODED FWD CARGO BAY BS 500A TO 500B. REMOVED CORRODED TRACK, FABRICATED AND DRILLED NEW TRACK PER SRM 51-40-01, INSTALLED TRACK PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 1997010900365 19970109 00365 NM 1997 1 9 AWXA9600786 1 19961220 A 5347 SEAT TRACK BOEING 737 7373Y0 1384671 NM BS 342 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 323AW 23684 DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON SEAT TRACK STA 342 RBL 53 WL 208. REMOVED, FABRICATED AND INSTALLE D SEAT TRACK IAW SRM 53-00-52, 51-40-02. 2 L 7 2 4F RT A16WE 1997010900366 19970109 00366 NM 1997 1 9 AWXA9600787 1 19961231 A 5230 SKIN BOEING 737 7373G7 1384595 NM CARGO DOOR DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 304AW 24011 DURING ROUTINE MAINTENANCE CHECK, FOUND C-2 DOOR AFT CARGO OUTER SKIN DENTED AND CREASED IN SEVERAL PLACES. REMOVED AND REPLACED C-2 DOOR OUTER SKIN IAW B737, SRM 52-30-01 AND 51-40-02. MAT ID 2024-T3 .071. FABRICATED NEW DOOR SKIN IAW B 737 SRM 52-30-01. 2 L 7 2 4F RT A16WE 1997010900367 19970109 00367 SW 1997 1 9 PNSA961201 1 19961207 A 2130 PRESSURE LINE SWRNGN SA227 SA227AC 8780603 SW CABIN FROZEN A PNSA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 640PA AC759B AIRCRAFT WOULD NOT PRESSURIZE, THAWED LINE TO OUTFLOW VALVE, PURGED WATER, OPS CK OK. 2 L 7 2 4T RT A8SW 1997010900368 19970109 00368 SW 1997 1 9 PNSA961202 1 19961211 A 3260 1CH16 SWITCH SWRNGN SA227 SA227AC 8780603 SW RT MLG INTERMITTANT A PNSA O OTHER N FALSE WARNING LD LANDING 1 AL 03 2708D AC713B RT MAIN DOWN LIGHT EXTINGUISHED INTERMITTANTLY DURING ROLL OUT. REPLACED SWITCH, OPS CHECK OK. 2 L 7 2 4T RT A8SW 1997010900369 19970109 00369 GL 1997 1 9 PNSA961203 3 19961221 A 6110 1641 GREASE ZERK PIPER PA32 PA32300 7103212 SO HARTZL HCC2Y HCC2YK1 GL PROPELLER FAILED A PNSA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 AL 03 8677N 327240021 CH31710A PROP LEAKING GREASE INFLIGHT. REPLACED GREASE ZERK, CHECKS OK. 1 L 7 1 3O A3SO 5 C P920 1997010900370 19970109 00370 SW 1997 1 9 PNSA961204 1 19961216 A 2910 2787003239 HYDRAULIC LINE SWRNGN SA227 SA227AC 8780603 SW LT NACELLE SPLIT A PNSA O OTHER K FLUID LOSS IN INSP/MAINT 1 AL 03 41NE AC741B DURING PREFLIGHT, FOUND HYDRAULIC PUDDLE UNDER LT NACELLE. 2 L 7 2 4T RT A8SW 1997010900371 19970109 00371 SW 1997 1 9 PNSA961205 1 19961221 A 2130 PRESSURE LINE SWRNGN SA227 SA227AC 8780603 SW CABIN WATER CONTAM A PNSA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 2708D AC713B AIRCRAFT WOULD NOT PRESSURIZE, PURGED MOISTURE FROM LINE TO OUTFLOW VALVE. 2 L 7 2 4T RT A8SW 1997010900372 19970109 00372 CE 1997 1 9 PNSA961206 1 19961227 A 2436 51539012M GCU CESSNA 208 208 2073702 CE ENGINE MALFUNCTIONED A PNSA O OTHER O OTHER TX TAXI/GRND HDL 1 AL 03 9602F 20800103 ENGINE WOULD NOT CRANK. REPLACED GCU, OPS CK OK. 1 H 7 1 3T NT A37CE 1997010900374 19970109 00374 NM 1997 1 9 CALA9700001 1 19961107 A 5311 FRAME BOEING 747 747238B 1384828 NM BS 220 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND A 1.75 INCH CRACK IN RT FRAME AT BS 220, STRINGER 32A. THE FRAME WAS REPAIRED IAW ECRA 5310-03374. 2 L 7 4 4F A20WE 1997010900375 19970109 00375 NM 1997 1 9 CALA9700002 1 19961107 A 5753 LUG BOEING 747 747238B 1384828 NM NR 4 TE FLAP WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND LT WING NR 4 MOVEABLE FLAP TRACK FAIRING DRIVE ARM LOWER OUTBOARD HINGE OUTBOARD LUG WORN. THE WORN AR EA WAS REPAIRED IAW ECRA 5750-02580. 2 L 7 4 4F A20WE 1997010900376 19970109 00376 NM 1997 1 9 CALA9700003 1 19961107 A 5753 DOUBLER BOEING 747 747238B 1384828 NM LT TE MID FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND CORROSION ON LT WING OUTBOARD TRAILING EDGE MID FLAP OUTBOARD DOUBLER. THE DOUBLER WAS REPAIRED IAW EC RA 5750-02581. 2 L 7 4 4F A20WE 1997010900377 19970109 00377 NM 1997 1 9 CALA9700004 1 19961101 A 5320 SPLICE BOEING 747 747238B 1384828 NM BS 1480 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND STRINGER SPLICE CORRODED WITH A 1.8 INCH CRACK ALONG FLANGE AT BS 1480, STRINGER 1L. THE STRINGER SPLI CE WAS REPLACED IAW ECRA 5310-03380. 2 L 7 4 4F A20WE 1997010900378 19970109 00378 NM 1997 1 9 CALA9700005 1 19961106 A 5313 STRINGER BOEING 747 747238B 1384828 NM BS 1740 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND A 0.87 INCH CRACK AT INBOARD VERTICAL FLANGE FASTENER HOLE OF STRINGER 9R AT THE MANUFACTURING SPLICE L OCATION, BS 1740. THE STRINGER WAS REPAIRED IAW ECRA 5310-03373. 2 L 7 4 4F A20WE 1997010900379 19970109 00379 NM 1997 1 9 CALA9700006 1 19961109 A 5313 STRINGER BOEING 747 747238B 1384828 NM BS 741 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND CRACKS IN STRINGER 2R AND 2AR AT BS 741. THERE WERE A TOTAL OF FOUR CRACKS MEASURING 2.5, 1.18, 1.38, AND 0.62 LONG. THE STRINGERS WERE REPAIRED IAW ECRA 5310-03383. 2 L 7 4 4F A20WE 1997010900380 19970109 00380 NM 1997 1 9 CALA9700007 1 19961108 A 5330 SKIN BOEING 747 747238B 1384828 NM BS 520-741 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND CORROSION IN SKIN LAP SPLICE AT SEVERAL LOCATIONS FROM BS 520 TO 741, STRINGER 6L. THE SKIN WAS REPAIR ED IAW ECRA 5330-02472. 2 L 7 4 4F A20WE 1997010900381 19970109 00381 WP 1997 1 9 9627449140 1 19961226 A 3230 BUNGEE CYLINDER DOUG DC9 DC914 3022034 WP NLG FAILED A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 930RC 45729 DURING CLIMBOUT, THE NOSE GEAR HAD TO BE RECYCLED TO GET GREEN INDICATION. FLIGHT CONTINUED TO DTW AND LANDED WITHOUT I NCIDENT. REPLACED NOSE GEAR BUNGEE CYLINDER, LEAK AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1997010900386 19970109 00386 EU 1997 1 9 9627453240 1 19961206 A 5320 D54380034205 SILL AIRBUS 320 A320212 EU BS 32571 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 340NW 372 DURING C-CHECK, CORROSION WAS FOUND ON THE INBOARD FLANGE OF THE RIGHT AFT DOOR LOWER SILL. REPAIRED PER EA 32-120564. 2 L 7 2 4F RT A28NM 1997010900387 19970109 00387 EU 1997 1 9 9627463240 1 19961206 A 5320 D53480043204 SILL AIRBUS 320 A320212 EU BS 32571 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 340NW 372 DURING C-CHECK, CORROSION WAS FOUND ON THE INBOARD FLANGE OF THE LEFT AFT DOOR LOWER SILL. REPAIRED PER EA 32-120566. 2 L 7 2 4F RT A28NM 1997010900388 19970109 00388 EU 1997 1 9 9627473204 1 19961213 A 5320 D54380034205 SILL AIRBUS 320 A320211 3930320 EU BS 32571 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 304US 40 DURING C-CHECK, CORROSION WAS FOUND ON THE INBOARD FLANGE OF THE RIGHT AFT DOOR SILL. REPAIRED PER EA 32-120550. 2 L 7 2 4F RT A28NM 1997010900389 19970109 00389 EU 1997 1 9 9627483215 1 19961206 A 5320 D53480043 SILL AIRBUS 320 A320211 3930320 EU BS 32571 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 315US 171 DURING C-CHECK, FOUND CORROSION DAMAGE TO THE UMBRAIL SILL AT FRAME 68, Y+1292. REPAIRED PER EA 32-120561. 2 L 7 2 4F RT A28NM 1997010900390 19970109 00390 EU 1997 1 9 9627493202 1 19961126 A 5313 LONGERON AIRBUS 320 A320211 3930320 EU BS 32571 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 302US 32 DURING C-CHECK, THE FLOOR STRINGER AT FRAME 68, Y 1270 LEFT SIDE WAS FOUND WITH AREAS OF CORROSION. REPAIRED PER EA 32- 106173. 2 L 7 2 4F RT A28NM 1997010900395 19970109 00395 NM 1997 1 9 UPS97421795 1 19961231 A 3350 POWER SUPPLY BOEING 747 747121 1384871 NM UPPER DECK INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE-N/A, EXIT SIGN UPPER DECK INOP. REMOVED AND REPLACED POWER SUPPLY MODULE BATT, OPS CHECKS OK. 2 L 7 4 4F A20WE 1997010900404 19970109 00404 NM 1997 1 9 97FDEA00016 1 19961223 A 5720 PIN CASTING BOEING 727 72725C 138400H NM WS 740 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 117FE 19299 RT WING, THE FWD TERMINAL PIN CASTING AT STA 740 IS CRACKED IN INSIDE BORE ON I/B LWR SIDE OF BORE. REMOVED AND REPLACE D THE RT WING FWD WING TO FUSE TERMINAL PIN CASTING AT STA 740 IAW EA 7-5710-28934, EA 7-5710-28952, BOEING DWG NR 62C29 064, BOEING DEG 65-16200, AND SRM 51-30-2. 2 L 7 3 4F A3WE 1997010900405 19970109 00405 NM 1997 1 9 97FDEA00017 1 19961223 A 3220 DRAGE BRACE BOEING 727 72725C 138400H NM NLG CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 117FE 19299 NOSE GEAR DRAG BRACE SHELF CRACKED LT AFT LOWER CORNER. REMOVED AND REPLACED NLG DRAG BRACE SHELF PER S/B 727-53-108 AN D SRM 51-10-1. 2 L 7 3 4F A3WE 1997010900407 19970109 00407 WP 1997 1 9 SCNA96459 1 19961230 A 3350 110049 BATTERY CHARGER DOUG DC10 DC1010 3022110 WP CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 152SY 48289 FOUND FORWARD CABIN EMERGENCY FLOOR LIGHTS INOP. REMOVED AND REPLACED FORWARD CABIN EMERGENCY LIGHT LOWER BATTERY CHARG ER AND ALL LIGHTS OPS CHECKED GOOD. 2 L 7 3 4F A22WE 1997010900408 19970109 00408 WP 1997 1 9 SCNA96460 1 19961230 A 3350 EMBS1392 POWER SUPPLY DOUG DC10 DC1010 3022110 WP CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 152SY 48289 EMERGENCY LIGHTS FAILED SELF TEST FROM COCKPIT. REMOVED AND REPLACED FORWARD CABIN UPPER BATTERY POWER SUPPLY AND OPS C HECKED GOOD. 2 L 7 3 4F A22WE 1997010900409 19970109 00409 NM 1997 1 9 SCNA96461 1 19961231 A 3350 S106 BATTERY PACK BOEING 727 7272J4 1384006 NM COCKPIT DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 284SC 21438 FOUND COCKPIT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERIES AND OPS CHECKED GOOD. 2 L 7 3 4F RT A3WE 1997010900410 19970109 00410 NM 1997 1 9 SCNA96462 1 19961231 A 3350 LAMP BOEING 727 7272J4 1384006 NM COCKPIT INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 284SC 21438 COCKPIT EMERGENCY LIGHT UNARMED LIGHT WAS FOUND INOP. RELAMPED FIXTURE AND OPS CHECKED GOOD. 2 L 7 3 4F RT A3WE 1997010900414 19970109 00414 SO 1997 1 9 SWIA95808 1 19961230 A 5230 CLOSING MECH EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE CARGO DOOR OUT OF ADJUST A SWIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 NM 07 235SW 120310 DURING TAKEOFF ROLL, CARGO DOOR LIGHT CAME ON. ABORTED TAKEOFF AND RETURNED TO GATE. EXERCISED DOOR HANDLE, LIGHT WENT OUT AND STAYED OUT AFTER REPEATED TRIES, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1997010900425 19970109 00425 GL 1997 1 9 97ZZZX90 2 19961115 A 7250 TURBINE WHEEL BOLKMS 105 BO105CB* SW ALLSN 250C 250C20B 03013 GL NR 2 ENGINE FAILURE A L A HEEA K NONE T ENGINE CASE PENETRATION IN INSP/MAINT 1 SW 03 911FL S717 CAE831144 ROTORCRAFT SUFFERED AN UNCONTAINED TURBINE FAILURE CAUSING DAMAGE TO AIRCRAFT. NR 2 ENG FAILED AND TURBINE WHEEL ENTERE D TAILBOOM TUNNEL CAUSING A 9 INCH TEAR IN CENTER OF FIRE WALL. HIT NR 1 T/R DRIVESHAFT HANGER BEARING SUPPORT, RIPPED MOUNTING. WHEEL THEN HIT NR 1 ENG AIR DISCHARGE TUBES. AIRCRAFT WAS ON HELIPAD READYING FOR TAKEOFF. 1 G 7 2 4U 3 U H3EU E4CE 1997010900429 19970109 00429 NE 1997 1 9 97ZZZX94 2 19960907 A 7261 BEARING SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE ENG OIL PORT BLOCKED A A R7MA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 11 93LG 2217 2654 9234 IN-FLIGHT OIL PRESSURE FLUCTUATED UP TO 8 BARS, PILOT LANDED AND MAINT CALLED, PERFORMED OIL FLOW CHECK. RESULT, 18 CC. REMOVED ENG AND DISASSEMBLED, FOUND REAR BEARING OIL DELIVERY PORT IN BEARING CAGE COMPLETELY BLOCKED BY COKING. SUBM ITTER RECOMMENDS ENLARGMENT OF JETS TO REAR BEARING. 1 G 7 1 3U 3 U H9EU E19EU 1997010900432 19970109 00432 GL 1997 1 9 97ZZZX97 2 19961107 A 7250 6892828 NOZZLE SHIELD SKRSKY S76 S76 8143010 NE ALLSN 250C 250C30 03013 GL 1ST STG TURBINE DAMAGED A A AC2A K NONE O OTHER IN INSP/MAINT 1 SW 03 5447C 760180 CAE890873 THE NR 2 ENGINE FIRST STAGE TURBINE NOZZLE SHIELD WAS FOUND TO HAVE AN .8750 INCH BY 1.75 INCH SECTION MISSING AT THE 6 O'CLOCK POSITION. THIS DEFECT WAS FOUND DURING A ROUTINE INSPECTION. IT WAS SEEN THROUGH THE FUEL NOZZLE MOUNTING HOL E. AFTER REMOVAL OF PART, ALLISON CEB 72-3208 WAS PERFORMED ON THE PART. THE NOZZLE SHIELD PASSED THE TEST WHICH IS US ED TO DETERMINE IF THE NOZZLE WAS MADE OF THE PROPER MATERIAL. 1 G 7 2 3U 3 U H1NE E1GL 1997010900452 19970109 00452 CE 1997 1 9 12196900WA 1 19961202 A 3260 1EN18 SWITCH LEAR 25 25D 5170514 CE MLG MALFUNCTIONED A KKFA K NONE N FALSE WARNING NR NOT REPORTED 1 GL 23 900WA 248 RIGHT LANDING GEAR DOWN LIGHT INTERMITTENT. REPLACED RIGHT MAIN GEAR DOWN AND LOCK MICROSWITCH WITH NEW. ADJUSTED AND SWUNG GEAR. CHECKED GOOD. ALL WORK DONE IAW LEAR 25D MM. (X) 2 L 7 2 4J A10CE 1997010900458 19970109 00458 NE 1997 1 9 97ZZZX121 2 19960816 A 7230 70BM035400 MODULE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE MO 2-3 BEARING ROUGH A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 96LG 762 9437 2817 9362 DURING ENG COAST DOWN, UNUSUAL NOISE WAS HEARD. ROTATION OF FREE TURBINE WAS NORMAL, COMPRESSOR ROTATION WAS ROUGH. SU SPECTED REAR BEARING, BUT DID A BORESCOPE TO CHECK TURBINE WHEELS AND NOZZLES. FOUND CRACK IN 2ND STAGE GAS GEN STATOR/ NOZZLE OUTER RING. REMOVED ENGINE. REMOVED NRS 2 AND 3. REMOVED REAR BEARING HOUSING AND ROTATED COMPRESSOR. ROUGHNE SS WAS GONE. REINSTALLED REAR BEARING AND ROUGHNESS CAME BACK. FOUND SEVERAL MORE CRACKS ON TURBINE NOZZLE. REPLACED 2, 3 MODULES. NG CYCLES 3040. PT CYCLES 3526. 1 G 7 1 3U 3 U H9EU E19EU 1997010900459 19970109 00459 NM 1997 1 9 AWXA9600776 1 19961225 A 2720 65C370527 RUDDER PCU BOEING 737 7373G7 1384595 NM RUDDER CONTROL MALFUNCTIONED A AWXA K NONE F FLT CONT AFFECTED CR CRUISE 1 WP 28 150AW 32216 2521 23218 YAW DAMPER IS INTERMITTANT. AIRCRAFT EXPERIENCES NEARLY CONSTANT SLIGHT DUTCH ROLL WITH EXCURIOUS TO MODERATE DUTCH ROL L. REMOVED AND REPLACED RUDDER PCU. 2 L 7 2 4F RT A16WE 1997010900460 19970109 00460 SO 1997 1 9 PNSA1207 1 19961226 A 8010 103572001 SWITCH PIPER PA32 PA32301 7103207 SO STARTER MALFUNCTIONED A PNSA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 AL 03 8305H 328106017 STARTER WAS INTERMITTANT, RETURNED TO BASE. 1 L 7 1 3O A3SO 1997010900464 19970109 00464 NM 1997 1 9 CALA9700011 1 19961028 A 5311 FRAME BOEING 747 747238B 1384828 NM BS 380 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND A .75 INCH CRACK IN FRAME AT BS 380, STRINGER 23R. THE FRAME WAS REPAIRED IAW ECRA 5310-03367. 2 L 7 4 4F A20WE 1997010900465 19970109 00465 NM 1997 1 9 CALA9700012 1 19961104 A 5311 FRAME BOEING 747 747238B 1384828 NM BS 360 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND A .75 INCH CRACK IN FRAME AT BS 360 ON RT SIDE, STRINGER 14E. THE FRAME WAS REPAIRED IAW ECRA 5310-033 75. 2 L 7 4 4F A20WE 1997010900466 19970109 00466 NM 1997 1 9 CALA9700013 1 19961028 A 5311 FRAME BOEING 747 747238B 1384828 NM BS 280 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND A 2 INCH CRACK IN FRAME AT THE OUTBOARD FRAME WEB BETWEEN STRINGER 26R AND 27AR, BS 280. THE FRAME WAS REPAIRED IAW ECRA 5310-03370. 2 L 7 4 4F A20WE 1997010900467 19970109 00467 NM 1997 1 9 CALA9700014 1 19961104 A 5311 FRAME BOEING 747 747238B 1384828 NM BS 360 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND A .5 INCH CRACK IN FRAME AT MAIN DECK BS 360, LT SIDE, BETWEEN STRINGER 15 AND 16. THE FRAME WAS REPAI RED IAW ECRA 5310-03376. 2 L 7 4 4F A20WE 1997010900468 19970109 00468 NM 1997 1 9 CALA9700015 1 19961107 A 5711 FITTING BOEING 747 747238B 1384828 NM LT REAR SPAR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND SPLICE FITTING AND UPPER SPLICE PLATE CRACKED AT LT WING REAR SPAR. THE CRACKS WERE 0.040 AND .25 INCH LONG. THE SPLICE PLATE AND SPLICE FITTING WERE REPLACED IAW EA 5710-01199 AND BOEING SB 57-2110. 2 L 7 4 4F A20WE 1997010900469 19970109 00469 NM 1997 1 9 CALA9700016 1 19961106 A 5730 SKIN BOEING 747 747238B 1384828 NM WING CTR SEC CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND A 0.040 CRACK AT THE RT WING EXTERNAL SPLICE FITTING AND A .1875 INCH CRACK AT THE MATING STRUCTURE WIN G CENTER SECTION UPPER SKIN PANEL. THE SPLICE FITTING WAS REPLACED IAW EA 5710-01199. THE SKIN PANEL WAS REPAIRED IAW ECRA 5710-01769. 2 L 7 4 4F A20WE 1997010900470 19970109 00470 NM 1997 1 9 CALA9700017 1 19961106 A 5313 STRINGER BOEING 747 747238B 1384828 NM BS 990 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND A 1 INCH CRACK IN STRINGER 9R AT BS 990 MANUFACTURING SPLICE LOCATION. THE STRINGER WAS REPAIRED IAW E CRA 5310-03384. 2 L 7 4 4F A20WE 1997010900471 19970109 00471 NM 1997 1 9 CALA9700018 1 19961028 A 5712 RIB BOEING 747 747238B 1384828 NM WS 670 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND A 1 INCH CRACK IN FORWARD SHEAR TIE AT LT WING NR 2 MAIN TANK WS 670, UPPER STRINGER 27 AND A .5 INCH C RACK WAS FOUND AT SHEAR TIE OF RIB CHORD, LOWER STRINGER 19. THE RIB CHORD AT UPPER STRINGER 27 WAS REPAIRED IAW SB 57- 2273. THE RIB CHORD AT LOWER STRINGER 19 WAS REPLACED IAW SRM 51-10-01. 2 L 7 4 4F A20WE 1997010900472 19970109 00472 NM 1997 1 9 CALA9700019 1 19961026 A 5412 BULKHEAD BOEING 747 747238B 1384828 NM NR 4 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND A 2 INCH CRACK AT UPPER POSITION OF NR 4 PYLON AFT BULKHEAD INBOARD CHORD. THE CHORD AND AFT BULKHEAD ASSEMBLY WERE REPLACED IAW SRM 57-10-01 AND SB 747-54A2159. 2 L 7 4 4F A20WE 1997010900473 19970109 00473 NM 1997 1 9 CALA9700020 1 19961026 A 5412 BULKHEAD BOEING 747 747238B 1384828 NM NR 3 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND A .125 INCH CRACK AT NR 3 PYLON FASTENER HOLE COMMON TO THE AFT BULKHEAD VERTICAL CHORD LT FITTING. TH E NR 3 PYLON LT BULKHEAD ASSEMBLY WAS REPLACED IAW SRM 51-10-01 AND BOEING DRAWING 65B90413. 2 L 7 4 4F A20WE 1997010900474 19970109 00474 EU 1997 1 9 9627503218 1 19961225 A 3260 PROX SENSOR AIRBUS 320 A320211 3930320 EU LANDING GEAR MALFUNCTIONED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 318US 206 AFTER LANDING GEAR EXTENSION, THE LANDING GEAR DOOR INDICATED OPEN. CYCLED LANDING GEAR HANDLE AND ALL INDICATIONS WERE NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE BRAKE STEERING CONTROL UNIT AND TESTED THE NOSE LA NDING GEAR PROXIMITY SENSORS, 18GA AND 19GA, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1997010900475 19970109 00475 NM 1997 1 9 9627516730 1 19961111 A 3230 6988035828 ACTUATOR BOEING 747 7472J9F 1384806 NM RT MLG DOWNLOCK LEAKING A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 630US 21668 DURING APPROACH, THE RIGHT WING LANDING GEAR WOULD NOT EXTEND. RECYCLED LANDING GEAR AND RIGHT WING LANDING GEAR STILL WOULD NOT EXTEND. ALTERNATELY EXTENDED LANDING GEAR AND RIGHT WING LANDING GEAR EXTENDED. AIRCRAFT LANDED WITHOUT INCI DENT. REPLACED THE RIGHT WING LANDING GEAR DOWNLOCK ACTUATOR, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1997010900486 19970109 00486 NM 1997 1 9 97FDEA00020 1 19961231 A 5315 6520827154 FLOORBEAM BOEING 727 727233 138408A NM BS 620 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 282FE 22349 NR 0435 CORROSION (C53-224-01,1) ON BS 620 BEAM, LBL 45 TO RBL 25, WL 208.1. *S/D* REMOVED AND REPLACED TOP CHORD OF F LOORBEAM AT BS 620, RBL 35 TO LBL 35, WL 208 PER FED-EX SRM 53-10-8, FIG 3. 2 L 7 3 4F RT A3WE 1997010900562 19970109 00562 EA 1997 1 9 SWIA95805 1 19961221 A 2740 STAB TRIM CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE HORIZ STAB MALFUNCTIONED A SWIA K NONE N FALSE WARNING CR CRUISE 1 NM 07 409SW 7056 STABILIZER TRIM FAILURE BOTH CHANNELS INFLIGHT. STABILIZER TRIM WOULD NOT RESET IN FLIGHT. PERFORMED SYSTEM TEST AT AS TCU, NO FAULTS SHOWN. RESET ASTCU, CHECKED MDC AND FOUND NO HSTCU LOADS. OPERATED STABILIZER TRIM WITH BOTH CHANNELS AND NO PROBLEMS. INSPECTED STABILIZER VISUALLY, FOUND OK. 2 L 7 2 4F 4 F RT A21EA E15NE 1997010900563 19970109 00563 NE 1997 1 9 ARWA9701001 2 19960103 A 7260 730374 SEAL DOUG DC8 DC862 3021970 WP PWA JT3D JT3D7 52039 NE NR 1 ENGINE LEAKING A ARWA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 19 810BN 45905 AFTER DEPARTURE, SHUT DOWN NR 1 ENGINE DUE TO HIGH OIL CONSUMPTION. FOUND ENGINE FUEL PUMP AND NASH PUMP GARLOC SEALS L EAKING. REMOVED AND REPLACED GARLOC SEALS, NO LEAK NOTED. 2 L 7 4 4F 4 F 4A25 1E8 1997010900571 19970109 00571 NE 1997 1 9 AALA961725 2 19961122 A 7230 COMP BLADE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE NR 2 ENG BROKEN A AALA E A ENGINE SHUTDOWN UNSCHED LANDING C E F.O.D. VIBRATION/BUFFET CL CLIMB 1 SW 07 413AA 49324 SMF - FLT 1842 - AFTER T/O SMF, DURING INITIAL CLIMB, NR 2 ENG INGESTED SEVERAL BIRDS FOLLOWED BY ENG VIBRATION. ACCOMP PROCEDURES AND SHUTDOWN NR 2 ENG. A/C RETURNED TO SMF AND LANDED O/W WITHOUT INCIDENT. REPLACED NR 2 ENG. ACCOMP LEA K CHECKS AND GROUND ENG RUN WITH NO DEFECTS FOUND. ACCOMP O/W LANDING AND BIRDSTRIKE INSPECTIONS WITH NO DEFECTS FOUND. SYS GROUND CHECKED NORMAL OP. SIGNIFICANT DAMAGE WAS DONE TO FAN BLADES. TWO FAN BLADES BROKEN OFF APPROX 3 INCHES F ROM TIP. SOME DAMAGE WAS EVIDENT THROUGH OUT THE LOW AND HIGH PRESS COMPRESSORS. ENG PROCESSED THROUGH SHOP FOR REPAIR AND RETURN TO SERV. (M) 2 L 7 2 4F 4 F A6WE E9NE 1997010900572 19970109 00572 WP 1997 1 9 AALA961723 1 19961123 A 4900 5940405503 APU DOUG DC9 DC982 3022082 WP APU BAY DEFECTIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 513AA 49890 SJC - FLT 1156 - AFTER TAKEOFF SJC DURING CLIMB-OUT, SMOKE NOTED IN COCKPIT AND CABIN. AIRCRAFT RETURNED TO SJC AND LAN DED OVERWEIGHT WITHOUT INCIDENT. ACCOMPLISHED PACK BURNOUT PROCEDURES AND OVERWEIGHT LANDING INSPECTION WITH NO DEFECTS FOUND. REPLACED APU ASSEMBLY AND LEFT AND RIGHT AIR CONDITIONING COALESCER BAGS. ACCOMPLISHED GROUND ENGINE RUN AND O PERATED APU WITH NO DEFECTS OR SMOKE NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1997010900573 19970109 00573 WP 1997 1 9 AALA961749 1 19961203 A 3260 SWITCH DOUG DC9 DC982 3022082 WP CENTER PEDESTAL DIRTY A AALA K NONE O OTHER TO TAKEOFF 1 SW 07 7530 49922 DFW - FLT 237 - AFTER TAKEOFF ATL, ALL THREE LANDING GEAR RED LIGHTS REMAINED ILLUMINATED WITH LANDING GEAR HANDLE IN TH E UP POSITION. LANDING GEAR ARMING HORN SOUNDED SEVERAL TIMES. CYCLED LANDING GEAR WITH NO CHANGE IN INDICATION. AIRC RAFT PROCEEDED TO DFW AND LANDED WITHOUT FURTHER INCIDENT. COULD NOT DUPLICATE ON GROUND. PRECAUTIONARY CLEANED LEFT A ND RIGHT THROTTLE SWITCHES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1997010900574 19970109 00574 WP 1997 1 9 AALA961734 1 19961125 A 2150 O-RING DOUG DC9 DC982 3022082 WP A/C BAY DEFECTIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 7514A 49891 LAX - FLT 1234 - AFTER TAKEOFF LAX, SMOKE NOTED IN CABIN. AIRCRAFT RETURNED TO LAX AND LANDED WITHOUT INCIDENT. REPLAC ED APU OIL COOLER O-RINGS AND ALL COALESCER BAGS. ACCOMPLISHED LEAK CHECK AND PACK BURNOUT PROCEDURE WITH NO SMOKE NOTE D. SYSTEM GROUND CHECKED NORMAL OPERATIONS. (M) 2 L 7 2 4F A6WE 1997010900575 19970109 00575 WP 1997 1 9 AALA961736 1 19961201 A 3350 A3030398101 CONNECTOR DOUG DC10 DC1010 3022110 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 133AA 47828 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PAX SEAT ROW 6H INOPERATIVE. REINSERTED PIN INTO EMERGENCY FLOO R LIGHT CONNECTOR BY PAX SEAT ROW 6H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A22WE 1997010900576 19970109 00576 WP 1997 1 9 AALA961595 1 19961102 A 2170 COALESCER BAG DOUG DC9 DC982 3022082 WP CABIN DIRTY A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 07 216AA 49167 DFW - DURING TAXI OUT AT SJC, SLIGHT SMOKE NOTED IN CABIN WHEN APU STARTED. SMOKE DISSIPATED BEFORE TAKEOFF BUT RETURNE D BRIEFLY AFTER TAKEOFF WITH NO OTHER ABNORMAL INDICATIONS. AIRCRAFT PROCEEDED TO DFW AND LANDED WITHOUT INCIDENT. REM OVED OILY RAG FROM INSIDE THE APU RAM AIR DOOR SURROUNDING APU INLET SHROUD/SCREEN. REPLACED BOTH COALESCER BAGS. OPER ATED APU AND BOTH PACKS WITH NO SMOKE OR ODOR NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1997010900577 19970109 00577 WP 1997 1 9 AALA961668 1 19961114 A 3222 2C9294 SCHRADER VLV DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 07 513AA 49890 BOS - FLT 487 - AFTER TAKEOFF BOS, WHEN LANDING GEAR LEVER SELECTED UP, NOSE LANDING GEAR DID NOT RETRACT. AIRCRAFT RET URNED TO BOS AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR STRUT SHRAEDER VALVE AND SERVICED STRUT. ACCOMPLI SHED NOSE LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1997010900578 19970109 00578 NM 1997 1 9 AALA961624 1 19961112 A 3350 1722331 CONNECTOR BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 39356 24037 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 21A/B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECT OR AND CONTACTS AT PAX SEAT 21 A/B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1997010900579 19970109 00579 WP 1997 1 9 AALA961675 1 19961117 A 3350 A3060698101 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 291AA 49303 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN HALF OF MAIN CABIN INOPERATIVE. REPAIRED EMERGENCY FLOOR LIGHT CONNECTORS AT PAX SEAT ROWS 10 AND 24. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1997010900580 19970109 00580 WP 1997 1 9 AALA961637 1 19961111 A 3233 39281375001 CYLINDER DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 455AA 49560 PDX - FLT 1394 - AFTER TAKEOFF PDX, WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR RED LIGHT REMAINED ILLUMINATED. ACCO MPLISHED ABNORMAL PROCEDURES WITH SAME RESULTS. AIRCRAFT RETURNED TO PDX AND LANDED WITHOUT INCIDENT. REPLACED NOSE LA NDING GEAR RETRACTION CYLINDER. ACCOMPLISHED LEAK CHECK AND NOSE LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1997010900581 19970109 00581 NM 1997 1 9 AALA961548 1 19961022 A 3230 A42006028305 SOLENOID BOEING 727 727223 1384074 NM LANDING GEAR DEFECTIVE A AALA K NONE O OTHER CL CLIMB 1 SW 07 862AA 21089 SJU - FLT 706 - AFTER TAKEOFF STX, LANDING GEAR LEVER LATCH C/B TRIPPED WHEN GEAR HANDLE SELECTED UP. C/B WOULD NOT RES ET AND OVERRIDE TRIGGER WAS USED TO RAISE GEAR HANDLE. NO OTHER ABNORMAL INDICATIONS AND AIRCRAFT PROCEEDED TO SJU, LAN DING WITHOUT INCIDENT. REPLACED LANDING GEAR LEVER LATCH SOLENOID. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1997010900582 19970109 00582 NM 1997 1 9 AALA961546 1 19961022 A 2810 106003162 PANEL BOEING 727 727223 1384074 NM RT WING SEAL LEAK A AALA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SW 07 708AA 22465 IAH - FLT 423 - AFTER TAKEOFF IAH DURING CLIMB-OUT, FUEL LEAK NOTED FROM RIGHT WING. AIRCRAFT RETURNED TO IAH AND LANDE D WITHOUT INCIDENT. REPLACED RIGHT WING FUEL TANK PANELS 15, 16 AND 17 DUE TO SEALS LEAKING. SYSTEM LEAK AND GROUND CH ECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1997010900583 19970109 00583 NM 1997 1 9 AALA961307 1 19960902 A 3350 A3060698101 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 601AN 27052 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PAX SEAT 3E INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT STRIP CONNECTOR BY PAX SEAT 3E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1997010900584 19970109 00584 NM 1997 1 9 AALA961303 1 19960831 A 3350 210013 SWITCH BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA K NONE L NO TEST CL CLIMB 1 SW 07 357AA 24038 DFW - FLT 79 - AFTER TAKEOFF LGW DURING CLIMB TO CRUISE ALTITUDE, EMERGENCY EXIT AND PATH LIGHTING BEGAN OPERATING INTER MITTENTLY. AFTER 20 MINUTES OF INTERMITTENT OPERATION, LIGHTS EXITNGUISHED AND COULD NOT BE ILLUMINATED WITH EITHER COC KPIT SWITCH OR AT F/A STATION. AIRCRAFT PROCEEDED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED EMERGENCY LIGHT TEST SW ITCH AT AFT RIGHT SIDE FLIGHT ATTENDANTS PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1997010900585 19970109 00585 NM 1997 1 9 AALA961281 1 19960828 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 338AA 22335 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 31H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 31H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1997010900586 19970109 00586 NM 1997 1 9 AALA961329 1 19960907 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 338AA 22335 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 31HJ INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT C ONNECTOR AT PAX SEAT 31HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1997010900587 19970109 00587 NM 1997 1 9 AALA961325 1 19960906 A 3350 A3060698101 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 649AA 24607 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PAX SEAT ROW 18F INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR L IGHT STRIP CONNECTOR BY PAX SEAT ROW 18F. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1997010900588 19970109 00588 NM 1997 1 9 AALA961639 1 19961113 A 3350 AC4G3002 SIGN BOEING 727 727227 1384078 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 718AA 20611 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT SIGN AT FIRST CLASS GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT SIGN AT FI RST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1997010900589 19970109 00589 NM 1997 1 9 AALA961636 1 19961112 A 3397 WIRE BOEING 727 727223 1384074 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 707AA 22464 IAH - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR LIGHTS AT FIRST CLASS DIVIDER INOPERATIVE. REPAIRED EMERGENCY EXIT F LOOR LIGHT WIRE AT FIRST CLASS DIVIDER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1997010900590 19970109 00590 NM 1997 1 9 AALA961635 1 19961112 A 3397 WIRE BOEING 727 727223 1384074 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 884AA 21523 BWI - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR LIGHT STRIP BY FORWARD GALLEY INOPERATIVE. REPAIRED EMERGENCY EXIT F LOOR LIGHT STRIP WIRE SPLICE BY FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1997010900591 19970109 00591 EU 1997 1 9 AALA961592 1 19961031 A 3230 715441 SELECTOR VALVE FOKKER F28 F28MK0100 4990807 EU LANDING GEAR DEFECTIVE A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 07 1452B 11464 ORD - FLT 1488 - DURING APPROACH TO ORD WHEN LANDING GEAR EXTENDED, NOSE LANDING GEAR GREEN LIGHT ILLUMINATED BUT LEFT A ND RIGHT MAIN LANDING GEAR GREEN LIGHTS FAILED TO ILLUMINATE. ACCOMPLISHED ALTERNATE GEAR EXTENSION AND AIRCRAFT LANDED ORD WITHOUT INCIDENT. REPLACED MAIN LANDING GEAR SELECTOR VALVE. ACCOMPLISHED LEAK CHECK WITH NO DEFECTS FOUND. ACCO MPLISHED LANDING GEAR RETRACTIN CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1997010900592 19970109 00592 EU 1997 1 9 AALA961620 1 19961106 A 3260 INDICATION FOKKER F28 F28MK0100 4990807 EU NLG MALFUNCTIONED A AALA K NONE N FALSE WARNING CR CRUISE 1 SW 07 1409B 11367 MSP - FLT 2068 - EN ROUTE DFW/MSP, DURING CRUISE, NOSE LANDING GEAR GREEN LIGHT ILLUMINATED. AIRCRAFT PROCEEDED TO MSP AND WHEN LANDING GEAR CYCLED, ALL INDICATIONS RETURNED TO NORMAL. AIRCRAFT LANDED MSP WITHOUT INCIDENT. CHECKED NOSE L ANDING GEAR SENSORS, WITH NO DEFECTS FOUND. ACCOMPLISHED NOSE LANDING GEAR RETRACTION CHECK, WITH NO DEFECTS FOUND. AC COMPLISHED PSEU BITE CHECK, WITH NO DEFECTS FOUND. SYSTEM GROUND CHECK NORMAL OPERATION. UNABLE TO DUPLICATE DISCREPAN CY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT 1997010900593 19970109 00593 EU 1997 1 9 AALA961671 1 19961116 A 3350 STRIP AIRBUS 300 A300B4605R 3930308 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 8067A 510 MIA - DURING OVERNIGHT CHECK, FIRST CLASS EMERGENCY FLOOR LIGHTS INOPERATIVE. RESECURED EMERGENCY FLOOR LIGHT STRIP IN FIRST CLASS SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1997010900594 19970109 00594 NM 1997 1 9 AALA961669 1 19961114 A 2150 68064043 ACM BOEING 767 767223 1385123 NM AFT FUSELAGE DEFECTIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 323AA 22324 RDU - FLT 174 - AFTER TAKEOFF RDU, FUMES SIMILAR TO ELECTRICAL OVERHEATING ODOR NOTED THROUGHOUT AIRCRAFT. ODOR BEGAN D ISSIPATING ON CLIMB-OUT, BUT INCREASED DURING DESCENT TO RDU. AIRCRAFT LANDED RDU WITHOUT FURTHER INCIDENT. ACCOMPLISH ED ENGINE RUN-UP AND NOTED FUMES COMING FROM RIGHT PACK. RIGHT PACK PLACARDED 'DO NOT OPERATE'. AIRCRAFT MAINTENANCE F ERRY RDU/AFW LANDED WITHOUT INCIDENT. REPLACED ACM, BOTH HEAT EXCHANGERS, CATALYTIC CONVERTER AND REMOVED, CLEANED, AND REINSTALLED PNEUMATIC DUCTS IN RIGHT PACK BAY. ACCOMPLISHED LEAK CHECK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1997010900595 19970109 00595 NM 1997 1 9 AALA961578 1 19961030 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 328 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 846AA 20987 TUL - FOUND CRACK ON FRAME ATTACH ANGLE. DAMAGED AREA REMOVED, INSTALLED NEW ANGLE IAW SRM 53-10-4 PG 58-60. (M) 2 L 7 3 4F A3WE 1997010900596 19970109 00596 NM 1997 1 9 AALA961579 1 19961030 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 318 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 846AA 20987 TUL - FOUND CRACK ON FRAME ATTACH ANGLE. DAMAGED AREA REMOVED, INSTALLED NEW ANGLE IAW SRM 53-10-4 PG 58-60. (M) 2 L 7 3 4F A3WE 1997010900597 19970109 00597 NM 1997 1 9 AALA961580 1 19961030 A 5330 SKIN BOEING 727 727223 1384074 NM BS 486 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 846AA 20987 TUL - FOUND SKIN CORRODED THROUGH AT STRINGER 27L, STATION 486. REMOVED SECTION OF CORRODED SKIN AND INSTALLED REPAIR D OUBLER PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 1997010900598 19970109 00598 NM 1997 1 9 AALA961581 1 19961030 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 846AA 20987 TUL - FOUND STRINGER CRACKED AT END, FORWARD OF STATION 720C. REPAIRED STRINGER PER SRM 53-10-3 PAGE 413. (M) 2 L 7 3 4F A3WE 1997010900599 19970109 00599 NM 1997 1 9 AALA961582 1 19961030 A 5311 FRAME BOEING 727 727223 1384074 NM BS 970 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 846AA 20987 TUL - FOUND BELL FRAME AT STATION 970 CRACKED AT SIDE PANEL ATTACH HOLE BETWEEN STRINGER 26 AND 27 LEFT (HFEC). STOPPED DRILLED CRACK AND INSTALLED DOUBLER PER SRM 51-40-3 PAGE 3. (M) 2 L 7 3 4F A3WE 1997010900600 19970109 00600 NM 1997 1 9 AALA961583 1 19961030 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1130 MIS-DRILLED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 846AA 20987 TUL - MIS-DRILLED HOLE IN BELT FRAME. REPAIRED BELT FRAME PER SRM 53-10-4 PAGE 1. (M) 2 L 7 3 4F A3WE 1997010900601 19970109 00601 NM 1997 1 9 AALA961523 1 19961012 A 5210 141N63023 PAN BOEING 757 757223 1384957 NM L1 DOOR GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 695AN 26975 AFW - AFTER BLENDING GOUGE REMAINING MATERIAL IS BEYOND SRM LIMITS. REPAIRED PER MRB 757-978. (M) 2 L 7 2 4F RT A2NM 1997010900602 19970109 00602 NM 1997 1 9 AALA961522 1 19961012 A 5210 141N63022 PAN BOEING 757 757223 1384957 NM R1 DOOR GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 695AN 26975 AFW - AFTER BLENDING GOUGE, REMAINING MATERIAL IS BEYOND SRM LIMITS. REPAIRED PER MRB 757-976. (M) 2 L 7 2 4F RT A2NM 1997010900603 19970109 00603 EU 1997 1 9 PLGA9611221 1 19961122 A 3230 PINS SAAB SF340 SF340A 7850100 EU MLG NOT REMOVED A PLGA A UNSCHED LANDING O OTHER CL CLIMB 1 NE 05 749BA 340A152 BOS - FLT 4377 - DEPARTING BOS, THE LANDING GEAR FAILED TO RETRACT. THE AIRCRAFT RETURNED TO BOS, LANDING WITHOUT INCID ENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT FINDING THE MAIN GEAR GROUND PINS INSTALLED. MAINTENANCE REMOVED THE P INS AND RETURNED THE AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1997010900604 19970109 00604 EU 1997 1 9 PLGA9611211 1 19961121 A 7110 COWL SAAB SF340 340B 7860101 EU LT ENGINE NOT LATCHED A PLGA A UNSCHED LANDING O OTHER CL CLIMB 1 NE 05 350BE 340B197 BWI - FLT 4858 - TEN MINUTES AFTER DEPARTURE THE FLIGHT ATTENDANT NOTED THAT THE LEFT ENGINE INBOARD FORWARD COWL DOOR L ATCH WAS OPEN. THE AIRCRAFT RETURNED TO BWI LANDING WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT TO IN SPECT THE COWL AND LATCH. NO DEFECTS WERE FOUND. MAINTENANCE RESECURED THE LATCH AND RETURNED THE AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1997010900605 19970109 00605 SW 1997 1 9 MALA965231 1 19961204 A 3260 1EN516 SWITCH SWRNGN SA227 SA227AC 8780603 SW NLG FAILED A MALA K NONE N FALSE WARNING AP APPROACH 1 GL 15 425MA AC640 FLT 3016 - ON APPROACH TO CWA, THE NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR EXTENSION AND NO DOWN AND LOCK ED LIGHT WAS RECEIVED. THE CREW CYCLED THE GEAR TWICE, WITH NO CHANGE IN INDICATIONS. MAINTENANCE REPLACED THE LEFT NO SE GEAR DOWN AND LOCKED SWITCH. ALL CHECKS SATISFACTORY. (M) 2 L 7 2 4T RT A8SW 1997010900606 19970109 00606 CE 1997 1 9 97ZZZM1 1 19961117 A 2612 CONNECTOR BEECH 1900 1900 1154160 CE RT ENGINE DIRTY A GUUA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 19 194GA UB8 FLT 4171 - FLL-MIA - RIGHT ENGINE FIRE INDICATOR 'D' FLICKERED IN FLIGHT. TROUBLE SHOT SYSTEM, CLEANED CONNECTOR, COULD NOT DUPLICATE. (M) 2 L 7 2 4T RT A24CE 1997010900607 19970109 00607 CE 1997 1 9 97ZZZM2 1 19961130 A 2140 CLAMP BEECH 1900 1900C 1154161 CE HEATER LOOSE A GUUA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 19 195GA UB65 FLT 162 - MIA-TCB - RIGHT 'T' HANDLE ILLUMINATED FOR 2 SECONDS WHEN MAX TAKEOFF POWER WAS APPLIED. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO GATE. RESECURED CLAMP ON HEATER TUBE INLET. (M) 2 L 7 2 4T RT A24CE 1997010900608 19970109 00608 CE 1997 1 9 97ZZZM3 1 19961202 A 2612 WIRE BEECH 1900 1900C 1154161 CE LT ENGINE CHAFED A GUUA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 SO 19 187GA UC31 FLT 4193 - FLL-MIA - LEFT FIRE LIGHT ILLUMINATED ON TAXI INTO RAMP. REPAIRED CHAFED WIRE. (M) 2 L 7 2 4T RT A24CE 1997010900609 19970109 00609 WP 1997 1 9 97ZZZM4 1 19961127 A 5270 SWITCH DOUG DC9 DC932 3022066 WP TAIL CONE OUT OF ADJUST A GTIA O OTHER N FALSE WARNING LD LANDING 1 GL 23 942ML 47478 DTW - FLT 927 - TAIL CONE WARNING LIGHT FLICKERED ON LANDING ROLL. CHECKED SECURITY OF TAILCONE AND TAILCONE ATTACH HAN DLES, ALL CHECKED NORMAL. FOUND TAIL CONE MICROSWITCH TO BE OUT OF ADJUSTMENT, ADJUSTED MICROSWITCH AND ACCOMPLISHED TA IL CONE DROP CHECK, SYSTEM CHECKED IAW DC0 MM CHAPTER 53-50. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1997010900610 19970109 00610 WP 1997 1 9 97ZZZM5 1 19961203 A 5297 WIRE DOUG DC9 DC932 3022066 WP TAILCONE LOOSE A GTIA O OTHER N FALSE WARNING LD LANDING 1 GL 23 942ML 47478 FLT 841 - ACY - DURING LANDING ROLL, TAILCONE WARNING LIGHT FLASHED ON AND OFF SEVERAL TIMES. MAINTENANCE FOUND AND SEC URED LOOSE WIRE ON TAILCONE MICROSWITCH. OPERATIONAL CHECKED NORMAL IAW DC9 MM 53-5-3. (M) 2 L 7 2 4F A6WE 1997010900611 19970109 00611 WP 1997 1 9 97ZZZM6 1 19961121 A 3350 CM3071BPGPL LIGHT DOUG DC9 DC932 3022066 WP CABIN DAMAGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 942ML 47478 DTW - FORWARD WHITE EMERGENCY FLOOR EVACUATION LIGHT CRUSHED. REPLACED BULB AND LENS. OPERATIONAL CHECKED NORMAL IAW M M 33-50-0. (M) 2 L 7 2 4F A6WE 1997010900612 19970109 00612 NM 1997 1 9 GAIA9640 1 19961206 A 2611 SMOKE LIGHT BOEING 727 727251 138408H NM CARGO COMPT ILLUMINATED A GAIA O OTHER N FALSE WARNING DE DESCENT 1 SW 07 279US 21158 CARGO SMOKE LIGHT ILLUMINATED DURING DESCENT, VERIFIED NO SMOKE OR FIRE AS PER EMERGENCY CHECK LIST. COULD NOT DUPLICAT E. OPERATES NORMALLY ON GROUND IAW B 727 MM 26-31. (M) 2 L 7 3 4F A3WE 1997010900613 19970109 00613 NM 1997 1 9 F3LA96063 1 19961127 A 5311 6545801 FRAME BOEING 737 737201 1384454 NM BS 277.8 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 212US 20212 PAE - FOUND CORROSION ON FORWARD SIDE OF FUSELAGE FRAME VERTICAL FLANGE, STATION 227.8 RBL 19, WL 168. REMOVED CORROSIO N AND FOUND OUT OF LIMITS PER SRM. FLAP PEENED REWORKED AREA AND TREATED. FABRICATED STRAP, ALODINED AND PRIMED REPAIR PARTS AND INSTALLED ALL WORK DONE IAW SRM 51-10-2, 51-30-2 AND EWO 96-0780. WORK ACCOMPLISHED ON TRAMCO MWO FUSELAGE 2 07. (M) 2 L 7 2 4F A16WE 1997010900614 19970109 00614 NM 1997 1 9 EISA96281 1 19961201 A 3020 DUCT BOEING 727 727223 1384074 NM NR 3 ENGINE LOOSE A EISA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. J WARNING INDICATION CR CRUISE 1 SW 07 313NE 19702 NR 3 ENGINE FIRE INDICATION, SHUT DOWN ENGINE AND DISCHARGE BOTTLES. REMOVED AND REPLACED LEFT AND RIGHT ENGINE FIRE BO TTLES IAW MM 26-21-7. DURING ENGINE INSPECTION FOUND NOSE COWL ANTI-ICE DUCT LOOSE AT NOSE COWL, RESECURED DUCT. FOUND ENGINE LOOP CANNON PLUG WIRES CHAFING. REPAIRED WIRES, OPS CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1997010900615 19970109 00615 NM 1997 1 9 EISA96282 1 19961201 A 2133 7110033 OUTFLOW VLV BOEING 727 727221 1384071 NM STA 1183 INOPERATIVE A EISA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 368PA 155465 22540 CABIN PRESSURE CONTROL SYSTEM MALFUNCTIONED IN CLIMB. FAILED IN STANDBY MODE TO FULL CABIN DESCENT, SWITCHED TO MANUAL DC FAILED OPS PER AOM VOL 1. REMOVED AND REPLACED OUTFLOW VALVE PER MM. OPS CHECK GOOD PER GROUND OPS PROCEDURE. (M) 2 L 7 3 4F A3WE 1997010900616 19970109 00616 NM 1997 1 9 USAA960758 1 19961126 A 5321 FLOOR PAN BOEING 737 7374B7 1384702 NM BS 1016 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 439US 18642 24781 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 3 INCH CORRODED AREA BS 1016 LBL 30 FLOOR PAN. INSTALLED FILL ER AND DOUBLER, REPAIRED PER SRM 51-70-13, FIG 1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 1. (M) 2 L 7 2 4F RT A16WE 1997010900617 19970109 00617 NM 1997 1 9 USAA960759 1 19961126 A 5311 FRAME BOEING 737 7374B7 1384702 NM BS 993 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 439US 18642 24781 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 3 INCH CORROSION STATION 993, JUST ABOVE STRINGER 17 R FRAME. INSTALLED REPAIR ANGLE, REPAIRED PER SRM 51-70-11. CORROSION TASK NR C53-107-02, CORROSION LEVEL 1. (M) 2 L 7 2 4F RT A16WE 1997010900618 19970109 00618 WP 1997 1 9 97ZZZM7 1 19961206 A 5711 SPAR CAP DOUG DC9 DC932 3022066 WP WS 58.768 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE LEFT MAIN TANK XW 58.768 REAR SPAR LOWER CAP TO STRI NGER 11 WAS CORRODED. 2 L 7 2 4F A6WE 1997010900619 19970109 00619 WP 1997 1 9 97ZZZM8 1 19961206 A 5711 SPAR DOUG DC9 DC932 3022066 WP WS 109 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE LEFT MAIN TANK XRS 109 LOWER AUX SPAR UPPER FLANGE I S CORRODED. 2 L 7 2 4F A6WE 1997010900620 19970109 00620 WP 1997 1 9 97ZZZM9 1 19961206 A 5720 CLIP DOUG DC9 DC932 3022066 WP WS 111.5 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND RIGHT WING TANK STRINGER CLIP XRS 111.5 STRINGER 12-13 H AS HEAVY CORROSION. 2 L 7 2 4F A6WE 1997010900621 19970109 00621 WP 1997 1 9 97ZZZM10 1 19961206 A 5720 CLIP DOUG DC9 DC932 3022066 WP WS 111.5 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND RIGHT WING TANK STRINGER CLIP AT XRS 111.5, STRINGER 13- 14 HAS HEAVY CORROSION. 2 L 7 2 4F A6WE 1997010900622 19970109 00622 WP 1997 1 9 97ZZZM11 1 19961206 A 5720 CLIP DOUG DC9 DC932 3022066 WP WS 111.5 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND RIGHT WING TANK STRINGER CLIP AT XRS 111.5 STRINGER 11-1 2 HAS HEAVY CORROSION. 2 L 7 2 4F A6WE 1997010900623 19970109 00623 WP 1997 1 9 97ZZZM12 1 19961206 A 5720 CLIP DOUG DC9 DC932 3022066 WP WS 109 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURIGN SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND LEFT MAIN TANK XRS 109 STRINGER CLIP, STRINGER 13-14 IS CORRODED. 2 L 7 2 4F A6WE 1997010900624 19970109 00624 WP 1997 1 9 97ZZZM13 1 19961206 A 5720 CLIP DOUG DC9 DC932 3022066 WP WS 109 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND LEFT MAIN TANK XRS 109 STRINGER CLIP, STRINGER 12-13 IS CORRODED. 2 L 7 2 4F A6WE 1997010900625 19970109 00625 WP 1997 1 9 97ZZZM14 1 19961206 A 5711 SPAR DOUG DC9 DC932 3022066 WP WS 88 CRACKED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND RIGHT WING TANK STATION 88 REAR SPAR HAS .5 INCH CRACK E MANATING FROM FASTENER. 2 L 7 2 4F A6WE 1997010900626 19970109 00626 WP 1997 1 9 97ZZZM15 1 19961206 A 5711 SPAR CAP DOUG DC9 DC932 3022066 WP WS 69-91 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FUOND RIGHT WING TANK REAR SPAR CAP XRS 69-91 LOWER CAP HAS CO RROSION ON LOWER FLANGE AND LOWER FLANGE TO WEB SHELF. 2 L 7 2 4F A6WE 1997010900627 19970109 00627 WP 1997 1 9 97ZZZM16 1 19961206 A 5720 CLIP DOUG DC9 DC932 3022066 WP WS 109 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND RIGHT WING TANK STRINGER CLIP XRS 109, STRINGER 13-14 IS CORRODED. 2 L 7 2 4F A6WE 1997010900628 19970109 00628 WP 1997 1 9 97ZZZM17 1 19961206 A 5720 CLIP DOUG DC9 DC932 3022066 WP WS 109 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND RIGHT WING TANK STRINGER CLIP XRS 109, STRINGER 14-15 IS CORRODED. 2 L 7 2 4F A6WE 1997010900629 19970109 00629 WP 1997 1 9 97ZZZM18 1 19961206 A 5720 CLIP DOUG DC9 DC932 3022066 WP WS 109 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND RIGHT WING TANK STRINGER CLIP XRS 109, STRINGER 15-16 IS CORRODED. 2 L 7 2 4F A6WE 1997010900630 19970109 00630 WP 1997 1 9 97ZZZM19 1 19961206 A 5720 CLIP DOUG DC9 DC932 3022066 WP WS 109 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND RIGHT WING TANK STRINGER CLIP XRS 109, STRINGER 16-17 IS CORRODED. 2 L 7 2 4F A6WE 1997010900631 19970109 00631 WP 1997 1 9 97ZZZM20 1 19961206 A 5711 SPAR CAP DOUG DC9 DC932 3022066 WP WS 92-97 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND RIGHT WING TANK REAR SPAR CAP LOWER FLANGE XRS 92-97 IS CORRODED. 2 L 7 2 4F A6WE 1997010900632 19970109 00632 WP 1997 1 9 97ZZZM21 1 19961206 A 5713 STRINGER DOUG DC9 DC932 3022066 WP WS 109 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND RIGHT WING TANK STRINGER CLIP XRS 109, STRINGER 12-13 IS CORRODED. 2 L 7 2 4F A6WE 1997010900633 19970109 00633 WP 1997 1 9 97ZZZM22 1 19961206 A 5720 CLIP DOUG DC9 DC932 3022066 WP WS 111.5 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND RIGHT WING TANK STRINGER CLIP AT XRS 111.5, STRINGER 15- 16 HAS HEAVY CORROSION. 2 L 7 2 4F A6WE 1997010900634 19970109 00634 NM 1997 1 9 W8PA960183 1 19961111 A 5315 BAC1505100246 FLOOR BEAM BOEING 737 7373L9 1384470 NM BS 312 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 961WP 23332 DURING C-CHECK, FOUND FLOOR BEAM UPPER CHORD, BS 312, LBL 1, WL 208 CORRODED AROUND FASTENER HOLE. CORROSION REMOVAL BE YOND LIMITS. REMOVED DAMAGED CHORD, INSTALLED NEW. (M) 2 L 7 2 4F RT A16WE 1997010900635 19970109 00635 NM 1997 1 9 W8PA960184 1 19961107 A 5320 6545834524 INTERCOSTAL BOEING 737 7373L9 1384470 NM BS 306 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 961WP 23332 DURING C-CHECK, FOUND CORROSION UNDER INTERCOSTAL, BS 306, LBL 27, WL 208. CORROSION REMOVAL BEYOND LIMITS. REMOVED AN D REPLACED INTERCOSTAL. (M) 2 L 7 2 4F RT A16WE 1997010900636 19970109 00636 NM 1997 1 9 W8PA960185 1 19961118 A 5315 FLOOR BEAM BOEING 737 7373L9 1384470 NM BS 328 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 961WP 23332 DURING C-CHECK, FOUND THE UPPER CHORD OF THE BS 328 FLOOR BEAM CORRODED AROUND FASTENER HOLES AND ON TOP FLANGE. REMOVE D UPPER CHORD, FOUND CORROSION OUT OF LIMITS. FABRICATED AND INSTALLED NEW FLOOR BEAM. (M) 2 L 7 2 4F RT A16WE 1997010900637 19970109 00637 NM 1997 1 9 W8PA960186 1 19961118 A 5320 654583446T6 SUPPORT BOEING 737 7373L9 1384470 NM BS 328-344 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 961WP 23332 DURING C-CHECK, FOUND THE FLOOR SUPPORT AT BS 328-344, RBL 10, WL 208 CORRODED. FOUND THE CORROSION TO BE OUT OF LIMITS . REMOVED AND REPLACED FLOOR SUPPORT. (M) 2 L 7 2 4F RT A16WE 1997010900638 19970109 00638 NM 1997 1 9 W8PA960188 1 19961111 A 5347 BAC15207927178 SEAT TRACK BOEING 737 7373L9 1384470 NM BS 328-344 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 961WP 23332 DURING C-CHECK, FOUND SEAT TRAC, RBL 22, CORRODED AT BS 330, 333, 338 AND 342. FOUND THE CORROSION TO BE OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK FROM BS 328-344. (M) 2 L 7 2 4F RT A16WE 1997010900639 19970109 00639 NM 1997 1 9 W8PA961089 1 19961111 A 5347 BAC15207927178 SEAT TRACK BOEING 737 7373L9 1384470 NM BS 331 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 961WP 23332 DURING C-CHECK, FOUND SEAT TRACK, RBL 43, CORRODED AT BS 331. FOUND THE CORROSION TO BE OUT OF LIMITS. FABRICATED AND INSTALLED SEAT TRACK. (M) 2 L 7 2 4F RT A16WE 1997010900640 19970109 00640 NM 1997 1 9 W8PA960190 1 19961111 A 5347 BAC15207927178 SEAT TRACK BOEING 737 7373L9 1384470 NM BS 344-360 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 961WP 23332 DURING C-CHECK, FOUND SEAT TRACK, LBL 54, BS 344-360, CORRODED ON THE FLANGE AT BS 344. FOUND THE CORROSION TO BE OUT O F LIMITS. FABRICATED AND INSTALLED SEAT TRACK. (M) 2 L 7 2 4F RT A16WE 1997010900641 19970109 00641 NM 1997 1 9 W8PA960191 1 19961117 A 5347 7178T6511 SEAT TRACK BOEING 737 7373L9 1384470 NM BS 344 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 961WP 23332 DURING C-CHECK, FOUND THE END OF THE SEAT TRACK, LBL 17, BS 344, CORRODED. FOUND THE CORROSION TO BE OUT OF LIMITS. FA BRICATED AND INSTALLED SEAT TRACK. (M) 2 L 7 2 4F RT A16WE 1997010900642 19970109 00642 NM 1997 1 9 W8PA960192 1 19961113 A 5320 BAC15061702 SUPPORT BOEING 737 7373L9 1384470 NM BS 927-947.5 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 961WP 23332 DURNG C-CHECK, FOUND THE SEAT TRACK SUPPORT, RBL 18, TO BE CORRODED FROM BS 927-947.5. FOUND THE CORROSION TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW SUPPORT. (M) 2 L 7 2 4F RT A16WE 1997010900643 19970109 00643 NM 1997 1 9 W8PA960193 1 19961111 A 5320 6517688125 SILL BOEING 737 7373L9 1384470 NM BS 294-344 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 961WP 23332 DURING C-CHECK, FOUND THE FORWARD ENTRY MOP SILL, LBL 58, BS 294-344, TO BE CORRODED. FOUND THE CORROSION TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW MOP SILL. (M) 2 L 7 2 4F RT A16WE 1997010900644 19970109 00644 NM 1997 1 9 W8PA960194 1 19961111 A 5320 7075T6040 WEB BOEING 737 7373L9 1384470 NM BS 305-353 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 961WP 23332 DURING C-CHECK, FUOND THE L-1 DOORWAY THRESHOLD WEB, LBL 58, BS 305-353, TO BE CORRODED IN SEVERAL AREAS. CORROSION REW ORK DEEMED TO BE OUT OF LIMITS AT STATION 315-316. REPAIRED THRESHOLD WEB IAW SRM. (M) 2 L 7 2 4F RT A16WE 1997010900645 19970109 00645 NM 1997 1 9 W8PA960195 1 19961111 A 5320 654587545 SILL BOEING 737 7373L9 1384470 NM BS 294-328 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 961WP 23332 DURING C-CHECK, FOUND THE R-1 DOORWAY MOP SILL, RBL 57, BS 294-328, TO BE CORRODED. CORROSION REWORK DEEMED TO BE OUT O F LIMITS. REMOVED AND INSTALLED NEW MOP SILL. (M) 2 L 7 2 4F RT A16WE 1997010900646 19970109 00646 NM 1997 1 9 W8PA960196 1 19961118 A 5320 7075T6 WEB BOEING 737 7373L9 1384470 NM BS 294-328 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 961WP 23332 DURING C-CHECK, FOUND BOTTOM SIDE OF THRESHOLD WEB, R-1 DOORWAY, BS 294-328, TO BE CORRODED. CORROSION REWORK DEEMED TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW WEB. (M) 2 L 7 2 4F RT A16WE 1997010900647 19970109 00647 NM 1997 1 9 W8PA960198 1 19961107 A 5320 6545834283 CHANNEL BOEING 737 7373L9 1384470 NM BS 281.5 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 961WP 23332 DURING C-CHECK, FOUND CORROSION ON SIDE OF LAV WALL SUPPORT AT BS 281.5, LBL 11.5, WL 208.5. LAV WALL SUPPORT FOUND TO BE CORRODED BEYOND LIMITS. REMOVED AND INSTALLED NEW LAV WALL SUPPORT. (M) 2 L 7 2 4F RT A16WE 1997010900648 19970109 00648 NM 1997 1 9 W8PA960200 1 19961213 A 2120 BACC45FT10A5S6 CONNECTOR BOEING 737 7373Y0 1384671 NM BS 213 FAILED A W8PA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 03 962WP 23748 WITH NORMAL EQUIPMENT COOLING FAN ON MEL, AND ALTERNATE FAN IN USE, 'FAN OFF' LIGHT CAME ON IN FLIGHT. WITH NO EQUIPMEN T COOLING AVAILABLE, AIRCRAFT RETURNED TO BASE. REPAIRED WIRE AT LOW FLOW SENSOR, AND SUBSEQUENTLY REPLACED SENSORS CAN NON PLUG. (M) 2 L 7 2 4F RT A16WE 1997010900649 19970109 00649 NM 1997 1 9 W8PA960175 1 19961130 A 3397 WIRE BOEING 737 7373Q8 1384670 NM CABIN LOOSE A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 956WP 24299 FOUND EMERGENCY FLOOR TRACK LIGHTING INOP AT ROWS 4, 5, AND 6. RECONNECTED LOOSE WIRE TO LIGHT SOCKETS. (M) 2 L 7 2 4F RT A16WE 1997010900650 19970109 00650 NM 1997 1 9 W8PA960176 1 19961127 A 3350 COVER BOEING 737 7373Y0 1384671 NM CABIN LOOSE A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 955WP 24463 FOUND EMERGENCY FLOOR TRACK LIGHTING COVERS HAVE TOO LARGE A GAP AT ROWS 2, 3, AND 5. INSTALLED NEW FLOOR TRACK LIGHTIN G COVERS. (M) 2 L 7 2 4F RT A16WE 1997010900651 19970109 00651 NM 1997 1 9 W8PA960177 1 19961122 A 3350 WIRING BOEING 737 7373Q8 1384670 NM CABIN LOOSE A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 956WP 24299 FOUND EMERGENCY FLOOR TRACK LIGHTING INOP AT ROW 22. RESECURED LOOSE WIRE CONNECTION. (M) 2 L 7 2 4F RT A16WE 1997010900652 19970109 00652 NM 1997 1 9 W8PA960178 1 19961122 A 3350 LAMP BOEING 737 7373Q8 1384670 NM CARGO DOOR FAILED A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 956WP 24299 FOUND EXTERIOR EMERGENCY LIGHT INOP ADJACENT TO FORWARD CARGO DOOR. REPLACED LAMP. (M) 2 L 7 2 4F RT A16WE 1997010900653 19970109 00653 NM 1997 1 9 W8PA960179 1 19961126 A 3397 WIRE BOEING 737 7373Q8 1384670 NM CABIN LOOSE A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 956WP 24299 FOUND EMERGENCY TRACK LIGH TINOP AT ROW 19. RESECURED LOOSE WIRE CONNECTION. (M) 2 L 7 2 4F RT A16WE 1997010900654 19970109 00654 NM 1997 1 9 W8PA960171 1 19961208 A 3350 BULB BOEING 737 7373B7 1384580 NM CABIN LOOSE A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 509AU 23384 FOUND EMERGENCY FLOOR TRACK LIGHTING INOP AT ROWS 1, 2, 7, 22 AND AFT GALLEY AREA. RESEAT LAMPS. (M) 2 L 7 2 4F RT A16WE 1997010900655 19970109 00655 NM 1997 1 9 W8PA960172 1 19961208 A 3397 WIRE BOEING 737 7373Q8 1384670 NM CABIN LOOSE A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 956WP 24299 FOUND EMERGENCY FLOOR TRACK LIGHTING INOP AT ROWS 1 AND 2, FIRST THREE LIGHTS. RECONNECTED PINS TO LIGHT SOCKETS. REPL ACED BROKEN WIRE. (M) 2 L 7 2 4F RT A16WE 1997010900656 19970109 00656 NM 1997 1 9 W8PA960199 1 19961211 A 3350 BULB BOEING 737 7373B7 1384580 NM CABIN FAILED A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 509AU 23384 FOUND EMERGENCY FLOOR TRACK LIGHTING INOP AT ROWS 18 AND 23. REPLACED BULBS. (M) 2 L 7 2 4F RT A16WE 1997010900657 19970109 00657 NM 1997 1 9 W8PA960187 1 19961212 A 3350 BPS73 BATTERY CHARGER BOEING 737 7373S3 1384711 NM BS 987 FAILED A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 375TA 36492 23787 EMERGENCY LIGHTS WILL NOT ILLUMINATE, ROWS 19 THROUGH 22. REPLACED BATTERY CHARGER. (M) 2 L 7 2 4F RT A16WE 1997010900658 19970109 00658 NM 1997 1 9 W8PA960174 1 19961129 A 3350 LAMP BOEING 737 7373L9 1384470 NM CABIN FAILED A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 961WP 23332 FOUND EMERGENCY FLOOR TRACK LIGHTING INOP AT ROW 9. REPLACED FLEX LAMP. (M) 2 L 7 2 4F RT A16WE 1997010900659 19970109 00659 NM 1997 1 9 W8PA960182 1 19961117 A 5320 6545834132 SUPPORT BOEING 737 7373L9 1384470 NM BS 294-312 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 961WP 23332 DURING C-CHECK, FOUND FLOOR SUPPORT, BS 294-312, LBL 42, WL 208 CORRODED. CORROSION REMOVAL BEYOND LIMITS. REMOVED DAM AGED AREA, FABRICATED REPAIR PARTS AND INSTALLED. (M) 2 L 7 2 4F RT A16WE 1997010900660 19970109 00660 NM 1997 1 9 W8PA960181 1 19961111 A 5315 AND101362404 FLOOR BEAM BOEING 737 7373L9 1384470 NM BS 294.5 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 961WP 23332 DURING C-CHECK, FUOND UPPER CHORD OF THE FLOOR BEAM AT BS 294.5 CORRODED AROUND MOST OF THE FASTENER HOLES, LBL 53-RBL 5 3, WL 208. CORROSION REMOVAL BEYOND LIMITS. REPLACED UPPER CHORD. (M) 2 L 7 2 4F RT A16WE 1997010900661 19970109 00661 NM 1997 1 9 W8PA960180 1 19961119 A 5347 BAC1522792 SEAT TRACK BOEING 737 7373L9 1384470 NM BS 270-294 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 961WP 23332 DURIGN C-CHECK, FOUND SEAT TRACK CORRODED AROUND FASTENER HOLES. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK. (M) 2 L 7 2 4F RT A16WE 1997010900662 19970109 00662 NM 1997 1 9 W8PA960201 1 19961215 A 3397 WIRE BOEING 737 7373B7 1384580 NM CABIN EEL LOOSE A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 952WP 23378 EMERGENCY LIGHTS WILL NOT ILLUMINATE, ROWS 15 THROUGH 18. FOUND WIRE DISCONNECTED UNDER SEAT TRACK COVER. RECONNECTED WIRE. (M) 2 L 7 2 4F RT A16WE 1997010900663 19970109 00663 EU 1997 1 9 RAIA961201 1 19961201 A 3350 ML44 BULB AEROSP ATR72 ATR72202 8680940 EU COCKPIT FAILED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 722TE 220 STL - THE AFT LEFT EXTERIOR EMERGENCY LIGHT INOP. MAINTENANCE REPLACED THE BULB. (M) 2 H 7 2 4T RT A53EU 1997010900664 19970109 00664 EU 1997 1 9 RAIA961176 1 19961129 A 3150 350A23008314 CCAS COMPUTER AEROSP ATR42 ATR42300 8680920 EU COCKPIT FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 03 423TE 11423 119 STL - FLT 7114 - TAKEOFF CONFIGURATION WARNING DURING TAKEOFF ROLL. MAINTENANCE REPLACED THE CCAS COMPUTER. (M) 2 H 7 2 4T RT A53EU 1997010900665 19970109 00665 EU 1997 1 9 RAIA961177 1 19961127 A 3350 167006 BULB AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 EICBK 14805 199 STL - FLT 7139 - EMERGENCY FLOOR PATH LIGHT AT ROW 2 IS INOP. MAINTENANCE REPLACED THE FLOOR PATH LIGHT BULB AT ROW 2. (M) 2 H 7 2 4T RT A53EU 1997010900666 19970109 00666 EU 1997 1 9 RAIA961124 1 19961124 A 2930 1173T0319 SWITCH AEROSP ATR42 ATR42300 8680920 EU HYD BAY FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 424TE 7948 124 STL - GREEN HYDRAULIC PUMP OVERHEAT WARNING ILLUMINATED. MAINTENANCE REPLACED THE HYDRAULIC OVERHEAT SWITCH. (M) 2 H 7 2 4T RT A53EU 1997010900667 19970109 00667 EU 1997 1 9 RAIA961204 1 19961203 A 3010 30351906 EJECTOR VALVE JETAIR JETSTM JETSTM4101 1500501 EU AIR FRAME DIRTY CONN A RAIA A UNSCHED LANDING N FALSE WARNING DE DESCENT 1 CE 03 558HK 2344 41071 EVV - FLT 7409 - AIRFRAME DE-ICE CIRCUIT 2 AUTO AND MANUAL INOP. CLEANED ELECTRICAL CONNECTION ON DE-ICE EJECTOR VALVE. (M) 2 L 7 2 4T RT A41NM 1997010900668 19970109 00668 EU 1997 1 9 RAIA961203 1 19961203 A 3240 AC63742 CONTROL VALVE BAG JETSTM JETSTM3201 1500217 EU LT MLG FAILED A RAIA K NONE O OTHER TX TAXI/GRND HDL 1 CE 03 429AM 7690 879 LEFT BRAKE NOT FUNCTIONING PROPERLY. REPLACED BRAKE CONTROL VALVE. (M) 2 L 7 2 4T RT A56EU 1997010900669 19970109 00669 EU 1997 1 9 RAIA961202 1 19961202 A 3350 BATTERY AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A RAIA K NONE L NO TEST TX TAXI/GRND HDL 1 CE 03 EICBF 14844 176 PORTION OF EMERGENCY LIGHTS INOP. REPLACED LIGHT BATTERY. (M) 2 H 7 2 4T RT A53EU 1997010900670 19970109 00670 EU 1997 1 9 WTAA960206 1 19961125 A 2430 A7036 CONTACTOR BAG JETSTM JETSTM3101 1500215 EU AVIONICS BAY FAILED A WTAA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 WP 17 422UE 782 MCE - LEFT GENERATOR FAILED IN FLIGHT, EN ROUTE FAT TO MCE. AIRCRAFT DIVERTED TO SFO FOR REPAIRS. MAINTENANCE REPLACED LEFT STARTER GENERATOR. PROBLEMS CONTINUES. AIRCRAFT FERRIED TO FAT FOR ADDITIONAL REPAIRS. FAT MAINTENANCE REPLACED LEFT GENERATOR CONTACTOR. GENERATOR SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1997010900671 19970109 00671 EU 1997 1 9 WTAA960211 1 19961203 A 3230 7445B RELEASE VALVE BAG JETSTM JETSTM3101 1500215 EU LANDING GEAR POPPED PIN A WTAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 17 430UE 784 LAX - LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE RESET L ANDING GEAR RELEASE VALVE ASSEMBLY BYPASS PIN. LANDING GEAR RETRACTION SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETUR NED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1997010900672 19970109 00672 EU 1997 1 9 USAA960781 1 19961206 A 5320 A3215013 FITTING FOKKER F28 F28MK4000 4990810 EU LT REAR SPAR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 475AU 24638 11222 PIT - DURING FC-1 CHECK, FOUND .5 INCH CRACK AT LEFT REAR SPAR FITTING (INBD PLATE). ACCOMPLISHED EO NR 5393J006B FOR R EPAIR. (M) 2 L 7 2 4F RT A20EU 1997010900673 19970109 00673 EU 1997 1 9 USAA960780 1 19961206 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 5305 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 475AU 24638 11222 PIT - DURING FC-1 CHECK,FOUND 3 INCH BY 1 INCH AREA OF CORROSION AT FWD CARGO FRAME 5305 AT STRINGER NR 74. CUT OUT COR RODED AREA AND INSTALLED A FILLER AND A REPAIR ANGLE PER SRM 53-02-12 PAGE 9. CORROSION LEVEL 1, CORROSION TASK NR C250 -00. (M) 2 L 7 2 4F RT A20EU 1997010900674 19970109 00674 EU 1997 1 9 USAA960779 1 19961206 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 8805 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 475AU 24638 11222 PIT - DURING FC-1 CHECK, FOUND 8 INCH BY 1 INCH AREA OF CORROSION AT FWD CARGO FRAME 8805 ABOVE STRINGER NR 1. CUT OUT CORRODED AREA AND INSTALLED A FILLER AND A REPAIR ANGLE PER SRM 53-02-12 PAGE 9. CORROSION LEVEL 1, CORROSION TASK NR C 250-00. (M) 2 L 7 2 4F RT A20EU 1997010900675 19970109 00675 EU 1997 1 9 USAA960778 1 19961206 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 475AU 24638 11222 PIT - DURING FC-1 CHECK, FOUND 4 INCH BY 1 INCH AREA OF CORROSION AT FORWARD CARGO FRAME 9305 BETWEEN STRINGERS NR 74 AN D NR 1. CUT OUT DAMAGED AREA AND INSTALLED A FILLER AND A DOUBLER (REPAIR ANGLE) PER SRM 53-02-12 PAGE 9. CORROSION LE VEL 1, CORROSION TASK NR C250-00. (M) 2 L 7 2 4F RT A20EU 1997010900676 19970109 00676 NM 1997 1 9 97ZZZM23 1 19961205 A 2612 42839KS145 CONNECTOR BOEING 737 7372H5 138448E NM FIREWALL SHORTED A E9WA E ENGINE SHUTDOWN N FALSE WARNING LD LANDING 1 SO 05 220US 20453 NR 1 ENGINE FIRE WARNING CAME ON INTERMITTENTLY ON LANDING. FOUND DEFECTIVE CANNON PLUG, MANUFACTURERS PART NR 42839 KS 14S-5SX SHORTED. 2 L 7 2 4F A16WE 1997010900677 19970109 00677 WP 1997 1 9 97ZZZM24 1 19961126 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 522 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND CORROSION TO BE BEYOND LIMITS AT THE FORWARD CARGO PIT F RAME STATION 522 FROM STRINGER 28R TO STRINGER 29L. (M) 2 L 7 2 4F A6WE 1997010900678 19970109 00678 WP 1997 1 9 97ZZZM25 1 19961202 A 5315 FLOOR BEAM DOUG DC9 DC932 3022066 WP BS 965 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND CORROSION ON THE UPPER CAP OF THE FLOOR BEAM STA 965, L BL 48. RECEIVED FROM AERO SUPPLY L-ANGLE NR 635060. FIT, TRIMMED, DRILLED UP, DEBURRED ANGLE IAW DC9 SRM 53-11-3 FIG 1 1A, SRM 51-10-4. TREATED AND PRIMED IAW DC9 SRM 51-10-3. INSTALLATION TO BE COMPLETED ON W/O NR 59881. (X) 2 L 7 2 4F A6WE 1997010900679 19970109 00679 WP 1997 1 9 97ZZZM26 1 19961202 A 5320 SPLICE DOUG DC9 DC932 3022066 WP BS 424 CRACKED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND A 5 INCH CRACK ON THE INBOARD FLANGE AT STA 424 L30 SPL ICE. FABRICATED 1 EACH LONGERON 30 IAW DRAWING 5920319. (X) 2 L 7 2 4F A6WE 1997010900680 19970109 00680 WP 1997 1 9 97ZZZM27 1 19961202 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 180/218 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND THE NR 4 SEAT TRACK STA 180 - STA 218 INBOARD AND OUTBO ARD FLANGES WERE CORRODED. REMOVED CORROSION IAW SRM 51-10-3. FOUND TO BE OUT OF LIMITS IAW SRM 53-05 FIG 4B. REMOVED , DRILLED AND DEBURRED NEW SEAT TRACK IAW DC9 SRM 51-10-4 AND SRM 53-05 FIG 4F. INSTALLED NEW SEAT TRACK IAW DC9 SRM 53 -05 FIG 4F AND SRM 51-10-3. (X) 2 L 7 2 4F A6WE 1997010900681 19970109 00681 WP 1997 1 9 97ZZZM28 1 19961202 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 522 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE FORWARD CARGO PIT FRAME AT STATION 522 WAS CORRODED BEYOND LIMITS, STRINGER 28R TO STRINGER 29L. (M) 2 L 7 2 4F A6WE 1997010900682 19970109 00682 WP 1997 1 9 97ZZZM29 1 19961202 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 140 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND THE PILOT'S INBOARD SEAT TRACK CORRODED ON OUTBOARD FLA NGE, STA 140. REMOVED FLOOR PANELS PER DC9 SRM 51-30-1. REMOVED SEAT TRACK PER DC9 SRM 51-30-1. LOCATED AND DRILLED N EW SEAT TRACK PER DC9 SRM 51-10-4. INSTALLED NEW SEAT TRACK PER DC9 SRM 51-30-1. INSTALLED FLOOR PANELS PER DC9 SRM 51 -30-1. GAUGE A-0299 USED TO DETERMINE OLD TRACK OUT OF LIMITS PER DC9, SRM 53-5 FIG 92. (X) 2 L 7 2 4F A6WE 1997010900683 19970109 00683 WP 1997 1 9 97ZZZM30 1 19961202 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 140 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND THE COPILOT'S OUTBOARD SEAT TRACK CORRODED ON OUTBOARD FLANGE, STA 140. REMOVED FLOOR PANELS PER DC9 SRM 51-30-1. REMOVED SEAT TRACK PER DC9 SRM 51-30-1. LOCATED AND DRILLE D NEW SEAT TRACK PER DC9 SRM 51-10-4. INSTALLED NEW SEAT TRACK PER DC9 SRM 51-30-1. INSTALLED FLOOR PANELS PER DC9 SRM 51-30-1. GAUGE A-0299 USED TO DETERMINE THAT OLD TRACK OUT OF LIMITS PER DC9 SRM 53-5 FIG 92. (X) 2 L 7 2 4F A6WE 1997010900684 19970109 00684 WP 1997 1 9 97ZZZM31 1 19961202 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 140 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND THE PILOT'S OUTBOARD SEAT TRACK CORRODED ON THE INBOARD FLANGE, STA 140. REMOVED FLOOR PANELS PER DC9 SRM 51-30-1. REMOVED SEAT TRACK PER DC9 SRM 51-30-1. LOCATED AND DRILL ED NEW SEAT TRACK PER DC9 SRM 51-10-4. INSTALLED NEW SEAT TRACK PER DC9 SRM 51-30-1. INSTALLED FLOOR PANELS PER DC9 SRM 51-30-1. GAUGE A-0299 USED TO DETERMINE THAT OLD TRACK IS OUT OF LIMITS PER DC9 SRM 53-5 FIG 92. (X) 2 L 7 2 4F A6WE 1997010900685 19970109 00685 WP 1997 1 9 97ZZZM32 1 19961202 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 209 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND THE NR 1 SEAT TRACK FLANGE AT STA 209 CORRODED. REMOVE D SEAT TRACK FLOOR BOARDS FROM STA 203 TO STA 230 IAW DC9 SRM 53-05, 4F. FABBED NEW SEAT TRACK IAW DC9 SRM 51-10-03. D RILLED UP SPLICE AND PLACED IAW DC9 SRM 51-10-04. INSTALLED SEAT TRACK, SPLICE, AND PLATE IAW DC9 SRM 53-05 FIG 4. CLE ANED VACUUMED AREA. INSTALLED FLOOR BOARDS, STA 237 - STA 313 IAW DC9 SRM 51-30-1 AND SRM 51-30-2. SPLICE AND PLATE WA S TREATED, ALODINED, AND PRIMED IAW DC9 SRM 51-10-3. (X) 2 L 7 2 4F A6WE 1997010900686 19970109 00686 WP 1997 1 9 97ZZZM33 1 19961202 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 920-935 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING SCHEUDLED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND THE LT OUTBOARD SEAT TRACKS AT STA 920 - STA 935 CORROD ED. REMOVED CORRODED SECTION OF SEAT TRACK, FABBED NEW SECTION, DRILLED AND DEBURRED, ALODINED AND PRIMED, AND INSTALLE D. DRILLED AND DEBURRED COUNTERSUNK, ALODINED, PRIMED AND INSTALLED SPLICE AND PLATE IAW DC9 SRM 53-05 FIG 4. (X) 2 L 7 2 4F A6WE 1997010900687 19970109 00687 WP 1997 1 9 97ZZZM34 1 19961202 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 996 CRACKED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE JACK POINT SUPPORT FITTING CRACKED 2 INCHES. (M) 2 L 7 2 4F A6WE 1997010900688 19970109 00688 WP 1997 1 9 97ZZZM35 1 19961202 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 135 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND THE CO-PILOT'S SEAT TRACK INBOARD SIDE AT STA 135 CORRO DED. REMOVED FLOOR PANELS PER DC9 SRM 51-30-1. REMOVED SEAT TRACK PER DC9 SRM 51-30-1. LOCATED AND DRILLED NEW SEAT T RACK PER DC9 SRM 51-10-4. INSTALLED NEW SEAT TRACK PER DC9 SRM 51-30-1. INSTALLED FLOOR PANELS PER DC9 SRM 51-30-1. G AUGE A-0299 USED TO DETERMINE THAT OLD TRACK IS OUT OF LIMITS PER DC9 SRM 53-5 FIG 92. (X) 2 L 7 2 4F A6WE 1997010900689 19970109 00689 WP 1997 1 9 VJ6A960005 1 19961207 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 1121.225 PUNCTURE A VJ6A K NONE O OTHER TX TAXI/GRND HDL 1 SO 11 938VV 47442 TWO BAG CARTS FROM ANOTHER CARRIER CAME LOOSE FROM TOW TUG AND STRUCK AIRCRAFT PARKED AT GATE C20 CAUSING DAMAGE AAT FUS ELAGE STATION 1121.225, STRINGER NR 21, RESULTING IN DAMAGE TO TAIL SECTION, ABOVE RIGHT SIDE OF AIR STAIRS. INCURRED A PUNCTURE OF 1.5 INCHES DIAMETER TO SKIN WITH CRACKS 6 INCHES WIDE AND 8 INCHES HIGH EMANATING FROM HOLE. FERRIED A/C F ROM ATL TO MACON FOR REPAIRS. REPLACED DAMAGED STRINGER END FITTING AND FRAME TEE CLIP. REPAIRED DAMAGED SKIN PER SRM 53-01 AND 51-10-5. (M) 2 L 7 2 4F A6WE 1997010900690 19970109 00690 WP 1997 1 9 VJ6A960006 1 19961209 A 2420 905D9881 CURRENT X-FORMER DOUG DC9 DC932 3022066 WP RIGHT ENG FAILED A VJ6A A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 11 945VV 47238 EN ROUTE FROM ATL-CMH, AIR INTERRUPTED AND RETURNED TO ATL AS A PRECAUTIONARY MEASURE BECAUSE CROSS TIE FAILED AND RIGHT GENERATOR CAME OFF LINE. RESET GENERATOR. REMOVED AND REPLACED RIGHT GENERATOR CONTROL PANEL, P/N 976J2544, S/N Y0206 7ABD, AND CURRENT TRANSFORMER, P/N 905D988-1, S/N SM5871. LATTER PART ATTRIBUTED TO CROSS TIE FAILURE. OPS CHECKED NOR MAL IAW MM 24-20-0. (M) 2 L 7 2 4F A6WE 1997010900691 19970109 00691 WP 1997 1 9 97ZZZM36 1 19961211 A 5713 STRINGER DOUG DC9 DC932 3022066 WP CENTER WING CRACKED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 910VJ 47277 DURING SCHEUDLED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND CENTER WING FUEL TANK NR 1 STRINGER IS CRACKED .75 INCH AT RT END RUNNING THROUGH BOTH BOLT HOLES. REMOVED CRACKED NR 1 STRINGER AND FORMED NEW NR 1 STRINGER FROM 7075T6. DIM ENSIONS ARE 4 FEET BY 8 FEET IAW DC9 DOUGLAS DRAWING NR 5919240. INSTALLED NEW STRINGER IAW DC9 SRM 51-30-1 AND SRM 51- 30-5. N/R REF NR 027N1-0201. (X) 2 L 7 2 4F A6WE 1997010900692 19970109 00692 WP 1997 1 9 97ZZZM37 1 19961206 A 5711 SPAR DOUG DC9 DC932 3022066 WP WS 68 AFT DAMAGED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE RIGHT WING AFT SPAR LOWER SPAR CAP FS 699 XRS 86 HAS A .375 INCH HOLE .090 DEEP WITH A AREA 1.25 INCH BLEND OUT .060 DEEP. 2 L 7 2 4F A6WE 1997010900693 19970109 00693 WP 1997 1 9 97ZZZM38 1 19961206 A 5720 CLIP DOUG DC9 DC932 3022066 WP WS 111.5 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE LEFT MAIN TANK STRINGER CLIP AT XRS 111.5 STRINGER 1 1-12 IS CORRODED. 2 L 7 2 4F A6WE 1997010900694 19970109 00694 WP 1997 1 9 97ZZZM39 1 19961206 A 5720 CLIP DOUG DC9 DC932 3022066 WP WS 111.5 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE LEFT MAIN TANK STRINGER CLIP AT XRS 111.5 REAR STRAP LOWER CAP TO STRINGER 11 IS CORRODED. 2 L 7 2 4F A6WE 1997010900695 19970109 00695 WP 1997 1 9 97ZZZM40 1 19961206 A 5720 CLIP DOUG DC9 DC932 3022066 WP WS 111.5 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE LEFT MAIN TANK STRINGER CLIP AT XRS 111.5, STRINGER 12-13 IS CORRODED. 2 L 7 2 4F A6WE 1997010900696 19970109 00696 WP 1997 1 9 97ZZZM41 1 19961206 A 5720 CLIP DOUG DC9 DC932 3022066 WP WS 111.5 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE LEFT MAIN TANK STRINGER CLIP XRS 111.5, STRINGER 13- 14 IS CORRODED. 2 L 7 2 4F A6WE 1997010900697 19970109 00697 WP 1997 1 9 97ZZZM42 1 19961206 A 5720 CLIP DOUG DC9 DC932 3022066 WP WS 111.5 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE LEFT WING TANK STRINGER CLIP AT XRS 111.5, STRINGER 14-15 IS CORRODED. 2 L 7 2 4F A6WE 1997010900698 19970109 00698 WP 1997 1 9 97ZZZM43 1 19961206 A 5720 CLIP DOUG DC9 DC932 3022066 WP WS 111.5 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE LEFT WING TANK STRINGER CLIP 111.5 STRINGER 15-16 IS CORRODED. 2 L 7 2 4F A6WE 1997010900699 19970109 00699 WP 1997 1 9 97ZZZM44 1 19961206 A 5711 SPAR CAP DOUG DC9 DC932 3022066 WP WS 115 CORRODED A VJ6A K NONE O OTHER NR NOT REPORTED 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE LEFT WING TANK FORWARD SPAR LOWER CAP XRS 115 IS COR RODED. 2 L 7 2 4F A6WE 1997010900700 19970109 00700 WP 1997 1 9 97ZZZM45 1 19961206 A 5720 BLOCKS DOUG DC9 DC932 3022066 WP WS 58.768 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE LEFT WING TANK AFT SPAR XW 58.768, TWO EACH RADIUS B LOCKS WERE CORRODED. 2 L 7 2 4F A6WE 1997010900701 19970109 00701 WP 1997 1 9 97ZZZM46 1 19961206 A 5711 SPAR CAP DOUG DC9 DC932 3022066 WP WS 67-89 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURNIG SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE LEFT WING TANK AFT SPAR LOWER CAP SHELF IS CORRODED XRS 67-89. 2 L 7 2 4F A6WE 1997010900702 19970109 00702 WP 1997 1 9 97ZZZM47 1 19961206 A 5720 CLIP DOUG DC9 DC932 3022066 WP WS 109 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE LEFT WING TANK XRS 109 STRINGER CLIP STRINGER 11 TO REAR SPAR CAP IS CORRODED. 2 L 7 2 4F A6WE 1997010900703 19970109 00703 WP 1997 1 9 97ZZZM48 1 19961206 A 5720 CLIP DOUG DC9 DC932 3022066 WP WS 109 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE LEFT WING TANK STRINGER CLIP XRS 109, STRINGER 11-12 IS CORRODED. 2 L 7 2 4F A6WE 1997010900704 19970109 00704 WP 1997 1 9 97ZZZM49 1 19961206 A 5720 CLIP DOUG DC9 DC932 3022066 WP WS 109 CORRODED A VJ6A K NONE O OTHER NR NOT REPORTED 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE LT WING TANK STRINGER CLIP XRS 109, STRINGER 15-16 I S CORRODED. 2 L 7 2 4F A6WE 1997010900705 19970109 00705 WP 1997 1 9 97ZZZM50 1 19961206 A 5720 TEE CAP DOUG DC9 DC932 3022066 WP WS 58.768 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE LEFT WING TANK XW 58.768 BETWEEN STRINGER 11-12 TEE CAP IS CORRODED. 2 L 7 2 4F A6WE 1997010900706 19970109 00706 WP 1997 1 9 97ZZZM51 1 19961206 A 5720 TEE CAP DOUG DC9 DC932 3022066 WP WS 58.768 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE LEFT WING TANK XW 58.768 BETWEEN STRINGER 12-13 TEE CAP IS CORRODED. 2 L 7 2 4F A6WE 1997010900707 19970109 00707 WP 1997 1 9 97ZZZM52 1 19961206 A 5720 TEE CAP DOUG DC9 DC932 3022066 WP WS 58.768 A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV CORRODED 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE XW 58.768 BETWEEN STRINGER 13-14 TEE CAP IS CORRODED . 2 L 7 2 4F A6WE 1997010900708 19970109 00708 WP 1997 1 9 97ZZZM53 1 19961206 A 5720 TEE CAP DOUG DC9 DC932 3022066 WP WS 58.768 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE LEFT MAIN TANK XW 58.768 BETWEEN STRINGER 14-15 TEE CAP IS CORRODED. 2 L 7 2 4F A6WE 1997010900709 19970109 00709 WP 1997 1 9 97ZZZM54 1 19961206 A 5720 TEE CAP DOUG DC9 DC932 3022066 WP WS 58.768 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE LEFT MAIN TANK XW 58.76B BETWEEN STRINGER 15-16 TEE CAP IS CORRODED. 2 L 7 2 4F A6WE 1997010900710 19970109 00710 WP 1997 1 9 97ZZZM55 1 19961206 A 5720 TEE CAP DOUG DC9 DC932 3022066 WP WS 58.768 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE LT MAIN TANK XW 58.768 BETWEEN STRINGER 16-17 TEE CA P IS CORRODED. 2 L 7 2 4F A6WE 1997010900711 19970109 00711 WP 1997 1 9 97ZZZM56 1 19961206 A 5713 STRINGER DOUG DC9 DC932 3022066 WP WS 58-69 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SHCEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE LEFT MAIN TANK XRS 58-69 STRINGER 17 LOWER CAP IS CO RRODED ON LOWER STRINGER. 2 L 7 2 4F A6WE 1997010900712 19970109 00712 WP 1997 1 9 97ZZZM57 1 19961206 A 5713 STRINGER DOUG DC9 DC932 3022066 WP WS 58-69 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE LEFT MAIN TANK XRS 58-69, STRINGER 16 UPPER CAP IS C ORRODED ON LOWER STRINGER. 2 L 7 2 4F A6WE 1997010900713 19970109 00713 WP 1997 1 9 97ZZZM58 1 19961206 A 5713 STRINGER DOUG DC9 DC932 3022066 WP WS 58-69 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE LEFT MAIN TANK XRS 58-69 STRINGER 14 UPPER CAP IS CO RRODED OF LOWER STRINGER. 2 L 7 2 4F A6WE 1997010900714 19970109 00714 WP 1997 1 9 97ZZZM59 1 19961206 A 5713 STRINGER DOUG DC9 DC932 3022066 WP WS 58-69 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE LEFT MAIN TANK XRS 58-69, STRINGER 13 TOP CAP IS COR RODED OF LOWER STRINGER. 2 L 7 2 4F A6WE 1997010900715 19970109 00715 WP 1997 1 9 97ZZZM60 1 19961206 A 5713 STRINGER DOUG DC9 DC932 3022066 WP WS 58-69 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE LEFT MAIN TANK XRS 58-69, STRINGER 12 TOP CAP IS COR RODED OF LOWER STRINGER. 2 L 7 2 4F A6WE 1997010900716 19970109 00716 WP 1997 1 9 97ZZZM61 1 19961206 A 5713 STRINGER DOUG DC9 DC932 3022066 WP WS 58-69 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE LEFT MAIN TANK XRS 58-69, STRINGER 15 UPPR AND LOWER CAP IS CORRODED ON LOWER STRINGER. 2 L 7 2 4F A6WE 1997010900717 19970109 00717 WP 1997 1 9 97ZZZM62 1 19961206 A 5312 BULKHEAD FRAME DOUG DC9 DC932 3022066 WP BS 996 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND AFT PRESSURE BULKHEAD MAIN FRAME STATION 996, RBL 56 COR RODED AT FASTENER HOLE. 2 L 7 2 4F A6WE 1997010900718 19970109 00718 WP 1997 1 9 97ZZZM63 1 19961206 A 5713 STRINGER DOUG DC9 DC932 3022066 WP WS 58-69 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE LEFT MAIN TANK XRS 58-69, STRINGER 16 UPPER AND LOWE R CAP CORRODED ON LOWER STRINGER. 2 L 7 2 4F A6WE 1997010900719 19970109 00719 WP 1997 1 9 97ZZZM64 1 19961206 A 5711 SPAR DOUG DC9 DC932 3022066 WP WS 70 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE LEFT MAIN TANK REAR SPAR LOWER CAP XRS 70 HAS CORROS ION AROUND 1 FASTENER. 2 L 7 2 4F A6WE 1997010900720 19970109 00720 SW 1997 1 9 MALA965222 1 19961127 A 2700 FLIGHT CONTROLS SWRNGN SA227 SA227AC 8780603 SW AIR FRAME BUFFETING A MALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 15 438MA AC721B FLT 3090 - ON CLIMB-OUT FROM MSP, THE CREW NOTED AN AERODYNAMIC BUFFETING EVERY 5 SECONDS IN AIRSPEED RANGES BETWEEN 160 -230 KNOTS. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE PERFORMED TROUBLESHOOTING TO THE HYDRAULIC SYSTEM, FLIGHT CONTRO L CABLE TENSION. ALL CHECKS GOOD. THE HYDRAULIC ACCUMULATRO PRESSURE WAS SERVICED AFTER IT WAS FOUND TO BE LOW. ENGIN E AND DE-ICE SYSTEM CHECKS WERE ALSO PERFORMED. ALL CHECKS SATISFACTORY. (M) 2 L 7 2 4T RT A8SW 1997010900721 19970109 00721 WP 1997 1 9 TWAA9615710 1 19961216 A 5320 INTERCOSTAL DOUG DC9 DC983 3022083 WP BS 1183 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9307R 49663 MCI - DURING OP-16, FOUND CORROSION ON CORNER CLIP BETWEEN FS 1183 FORMER AND INTERCOSTAL. REMOVED CORROSION PER SRM 51 -10-03, INSTALLED FASTENERS PER SRM 51-30-0. (M) 2 L 7 2 4F RT A6WE 1997010900722 19970109 00722 WP 1997 1 9 TWAA9615711 1 19961216 A 5320 FORMER DOUG DC9 DC983 3022083 WP BS 1183 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9307R 49663 MCI - DURING OP-16, FOUND CORROSION ON BOTTOM FLANGE AFT SIDE OF FS 1183 FORMER, BETWEEN LONGERON 29L TO 29R. REMOVED C ORROSION PER SRM 51-10-3, PARAGRAPH 31-48, INSTALLED FASTENERS PER SRM 51-30-0. (M) 2 L 7 2 4F RT A6WE 1997010900723 19970109 00723 NM 1997 1 9 97ZZZM65 1 19961214 A 2613 894120 SENSING ELEMENT BOEING 727 727231 1384079 NM NR 2 ENGINE FAILED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 52311 19830 STL - DURING CRUISE SHUT DOWN NR 2 ENGINE, S/N 3953, DUE TO OVERHEAT WARNING. FOUND LOW RESISTANCE IN SENSING ELEMENT, MFG P/N 894120. REPLACED SENSING ELEMENT. ENGINE OVERHEAT WARNING SYSTEM OPERATION THEN CHECKED NORMAL. (M) 2 L 7 3 4F A3WE 1997010900724 19970109 00724 WP 1997 1 9 TWAA9615712 1 19961216 A 5320 SUPPORT DOUG DC9 DC983 3022083 WP BS 1155 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9307R 49663 MCI - DURING OP-16, FOUND CORROSION IN AFT CARGO AREA FLOOR SUPPORT BEAM, RBL 12 TO LBL 12, FS 1155. REPLACED FLOOR SUP PORT BEAM PER SRM 51-01, PAGE 1, ITEM C. (M) 2 L 7 2 4F RT A6WE 1997010900725 19970109 00725 WP 1997 1 9 97ZZZM66 1 19961216 A 5320 ANGLE DOUG DC9 DC983 3022083 WP BS 1174-1212 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9307R 49663 MCI - DURING OP-16, FOUND CORROSION ON AFT CARGO FLOOR SUPPORT T-ANGLE, AND AROUND SCREW HOLES, FS 1174 TO FS 1212, RBL 14. REPLACED T-ANGLE PER SRM 51-01. (M) 2 L 7 2 4F RT A6WE 1997010900726 19970109 00726 NM 1997 1 9 TWAA9615502 1 19961214 A 2530 88011 SERVING CART BOEING 747 747131 1384881 NM GALLEY FAILED A TWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 93108 19674 STL - FLT 2 - DURING CRUISE, HAD A BURNING ODOR FROM AISLE SERVING CART, POSITION 1 IN 'B' GALLEY. FOUND DEFECTIVE AISL E SERVING CART, MFG P/N 8801-1. REPLACED AISLE SERVING CART. GALLEY AND SERVING CART OPERATION THEN CHECKED NORMAL. ( M) 2 L 7 4 4F A20WE 1997010900727 19970109 00727 WP 1997 1 9 TWAA9615714 1 19961216 A 3222 STRUT DOUG DC9 DC983 3022083 WP NLG CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9307R 49663 MCI - DURING OP-16, FOUND CORROSION ON NOSE GEAR UPPER STRUT HOUSING LOWER BEARING FLANGE. REMOVED CORROSION PER EMLR 6 70. (M) 2 L 7 2 4F RT A6WE 1997010900728 19970109 00728 WP 1997 1 9 TWAA9615715 1 19961216 A 5347 FLOOR TRACK DOUG DC9 DC983 3022083 WP BS 1211 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9307R 49663 MCI - DURING OP-16, FOUND CORROSION ON TOP OF FLOOR TRACK, LBL 56, STATION 1211. REMOVED CORROSION PER SRM 51-10-3, REP AIRED GALLEY TIE DOWN HOLE PER ARA 10750. (M) 2 L 7 2 4F RT A6WE 1997010900729 19970109 00729 WP 1997 1 9 TWAA9615716 1 19961216 A 5347 FLOOR TRACK DOUG DC9 DC983 3022083 WP BS 1211-3122 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9307R 49663 MCI - DURING OP-16, FOUND CORROSION ON AFT CARGO BIN RT AFT FLOOR TRACK, FS 1211 TO FS 3122. REPLACED TRACK PER SRM 51- 5-00, PATE 1, ITEM C AND STANDARD PRACTICES. (M) 2 L 7 2 4F RT A6WE 1997010900730 19970109 00730 WP 1997 1 9 TWAA9615301 1 19961211 A 3350 LIGHTS DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 110HM 49787 STL - FLT 640 - EGRESS LIGHTS INOPERATIVE AT ROW 16D THROUGH 21D. REMOVED AND REPLACED EGRESS LIGHTS, MFG P/N ML7732. O PERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 1997010900731 19970109 00731 NM 1997 1 9 TWAA9615701 1 19961217 A 3211 TRUNNION BOEING 727 727231 1384079 NM NLG LACK OF LUBE A TWAA O OTHER J WARNING INDICATION AP APPROACH 1 CE 05 54340 20845 MIA - FLT 5 - DURING APPROACH WHEN LANDING GEAR WS EXTENDED, THE NOSE LANDING GEAR DID NOT INDICATE DOWN AND LOCKED. CY CLED LANDING GEAR. FOUND NOSE LANDING GEAR TRUNNIONS DRY. LUBRICATED NOSE LANDING GEAR. LANDING GEAR OPERATION AND IN DICATION THEN CHECKED NORMAL. (M) 2 L 7 3 4F A3WE 1997010900732 19970109 00732 WP 1997 1 9 TWAA9615702 1 19961216 A 5320 ANGLE DOUG DC9 DC983 3022083 WP BS 1190 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9307R 49663 MCI - DURING OP-16, FOUND CORROSION AROUND STRINGER 29R LOWER ANGLE AT ONE HI-LOCK, FS 1190. REMOVED CORROSION PER SRM 51-10-34 AND STANDARD PRACTICES, THEN REPAIRED PER ARA 10751 AND STANDARD PRACTICES. (M) 2 L 7 2 4F RT A6WE 1997010900733 19970109 00733 WP 1997 1 9 97ZZZM67 1 19961216 A 5330 SKIN DOUG DC9 DC983 3022083 WP NLG DOORWAY CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9307R 49663 MCI - DURING OP-16, FOUND CRACK IN SKIN AFT LEFT HINGE CUTOUT NLG DOOR. INSTALLED DOUBLER REPAIR PER SRM 53-05, PAGE 16 9, FIGURE 62. (M) 2 L 7 2 4F RT A6WE 1997010900734 19970109 00734 WP 1997 1 9 TWAA9615705 1 19961216 A 5320 ANGLE DOUG DC9 DC983 3022083 WP BS 1212 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9307R 49663 MCI - DURING OP-16, FOUND CORROSION ON SMALL FLOOR TIE CLIP ANGLE BETWEEN LONGERON 27R AND 28R, FS 1212. REMOVED CORROS ION PER SRM 51-10-3, PARAGRAPH 31-48. REPLACED FASTENERS PER SRM 51-30-0. (M) 2 L 7 2 4F RT A6WE 1997010900735 19970109 00735 WP 1997 1 9 TWAA9615704 1 19961216 A 5320 FORMER DOUG DC9 DC983 3022083 WP BS 1193 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9307R 49663 MCI - DURING OP-16, FOUND CORROSION ON FORMER FOOT BETWEEN LONGERONS 29L AND 30L, FS 1193. REMOVED CORROSION PER SRM 51 -10-3, PARAGRAPH 31-48, REPLACED FASTENERS PER SRM 51-30-0. (M) 2 L 7 2 4F RT A6WE 1997010900736 19970109 00736 WP 1997 1 9 TWAA9615706 1 19961216 A 5320 FORMER DOUG DC9 DC983 3022083 WP BS 1212 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9307R 49663 MCI - DURING OP-16, FOUND CORROSION ON FORMER FOOT, FS 1212, BETWEEN STRINGER 29R TO 30R. REMOVED CORROSION PER SRM 51- 10-3, PARAGRAPH 31-48, REPLACED FASTENERS PER SRM 51-10-3. (M) 2 L 7 2 4F RT A6WE 1997010900737 19970109 00737 WP 1997 1 9 TWAA9615707 1 19961216 A 5320 FORMER DOUG DC9 DC983 3022083 WP BS 1212 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9307R 49663 MCI - DURING OP-16, FOUND CORROSION ON FORMER, LONGERON 27L TO LONGERON 29R, ON FORWARD AFT AND TOP OF FS 1212. REMOVED CORROSION PER SRM 51-10-3, REPLACED FASTENERS PER SRM 53-30-0. (M) 2 L 7 2 4F RT A6WE 1997010900738 19970109 00738 WP 1997 1 9 TWAA9615708 1 19961216 A 5320 ANGLE DOUG DC9 DC983 3022083 WP BS 1212 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9307R 49663 MCI - DURING OP-16, FOUND CORROSION AROUND SCREW HOLES TOP AND BOTTOM OF FLOOR SUPPORT UPPER ANGLE, LBL 25 TO RBL 6, FS 1212. REPLACED PART PER SRM 51-01. (M) 2 L 7 2 4F RT A6WE 1997010900739 19970109 00739 WP 1997 1 9 TWAA9615709 1 19961216 A 5320 FORMER DOUG DC9 DC983 3022083 WP BS 1993 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9307R 49663 MCI - DURING OP-16, FOUND CORROSION ON FORMER FOOT, BETWEEN LONGERON 29R AND 30R, FS 1993. REMOVED CORROSION PER SRM 51 -10-03, PARAGRAPH 31-48. REPLACED FASTENERS PER SRM 51-30-0. (M) 2 L 7 2 4F RT A6WE 1997010900740 19970109 00740 SW 1997 1 9 MALA965232 1 19961205 A 5753 RIB SWRNGN SA227 SA227AC 8780603 SW RT TE FLAP CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 425MA AC640 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND A .5 INCH CRACK ON THE RIGHT FLAP OUTBOARD NOSE RIB. (M) 2 L 7 2 4T RT A8SW 1997010900741 19970109 00741 SW 1997 1 9 MALA965221 1 19961127 A 5270 DOOR SWITCH SWRNGN SA227 SA227AC 8780603 SW CARGO DOOR OUT OF ADJUST A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 60NE AC760B FLT 3192 - CLIMBING THROUGH 11,000 FEET, THE CARGO DOOR WARNING LIGHTS ILLUMINATED. THE CREW PERFORMED QRH PROCEDURES A ND THE CABIN WAS DEPRESSURIZED. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE ADJUSTED THE CARGO DOOR HANDLE POSTION SWITC H. ALL CHECKS SATISFACTORY. (M) 2 L 7 2 4T RT A8SW 1997010900742 19970109 00742 SW 1997 1 9 MALA965223 1 19961128 A 3230 1EN516 UPLIMIT SWITCH SWRNGN SA227 SA227AC 8780603 SW NLG OUT OF ADJUST A MALA O OTHER J WARNING INDICATION CL CLIMB 1 GL 15 438MA AC721B FLT 3491 - ON CLIMB-OUT FROM MSP, THE NOSE GEAR CYCLED IN FLIGHT AFTER GEAR RETRACTION. THE AIRCRAFT CONTINUED TO STC W ITHOUT INCIDENT. MAINTENANCE RERIGGED THE NOSE GEAR UPLIMIT SWITCH. (M) 2 L 7 2 4T RT A8SW 1997010900743 19970109 00743 SW 1997 1 9 MALA965219 1 19961126 A 3230 1EN516 UPLIMIT SWITCH SWRNGN SA227 SA227AC 8780603 SW NLG OUT OF ADJUST A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 438MA AC721B FLT 3416 - ON CLIMB-OUT FROM DTW, THE NOSE GEAR CONTINUED TO CYCLED IN THE GEAR WELL AFTER GEAR RETRACTION. THE AIRCRAF T RETURNED TO DTW. MAINTENANCE CLEANED AND ADJUSTED THE UPLIMIT SWITCHES. ALL CHECKS SATISFACTORY. (M) 2 L 7 2 4T RT A8SW 1997010900744 19970109 00744 SW 1997 1 9 MALA965214 1 19961121 A 5753 2736015001 RIB SWRNGN SA227 SA227AC 8780603 SW LT TE FLAP CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 430MA AC710 DURING A BLOCK INSPECTION IN MSP, MAINTENANCE FOUND TWO CRACKS IN LEFT FLAP SN C-134 OUTBOARD FLAP NOSE RIB. REMOVED AN D REPLACED FLAP NOSE RIB P/N 27-36015-001 IAW FAIRCHILD STRUCTURAL REPAIR MANUAL 57-90-60 PAGES 43-46. (M) 2 L 7 2 4T RT A8SW 1997010900745 19970109 00745 SW 1997 1 9 MALA965215 1 19961121 A 5753 2736015002 RIB SWRNGN SA227 SA227AC 8780603 SW RT TE FLAP CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 430MA AC710 DURING A BLOCK INSPECTION IN MSP, MAINTENANCE FOUND A CRACK APPROX .75 INCH LONG IN RIGHT INBOARD FLAP NOSE RIB. REMOVE D AND REPLACED FLAP NOSE RIB P/N 27-36015-002 IAW FAIRCHILD STRUCTURAL REPAIR MANUAL 52-00-00 PAGE 4 AND 51-40-02. (M) 2 L 7 2 4T RT A8SW 1997010900746 19970109 00746 SW 1997 1 9 MALA965216 1 19961123 A 3230 1EN516 SWITCH SWRNGN SA227 SA227AC 8780603 SW NLG OUT OF ADJUST A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 424MA AC639 FLT 3429 - ON CLIMB-OUT FROM MSP, THE NOSE GEAR WOULD NOT REMAIN UP AND LOCKED AFTER GEAR RETRACTION. THE AIRCRAFT RETU RNED TO MSP. MAINTENANCE ADJUSTED THE NLG UPLIMIT SWITCH. ALL CHECKS SATISFACTORY. (M) 2 L 7 2 4T RT A8SW 1997010900747 19970109 00747 SW 1997 1 9 MALA965211 1 19961120 A 5400 ANGLE SWRNGN SA227 SA227AC 8780603 SW WING/NACELLE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 430MA AC710 DURING A BLOCK INSPECTION IN MSP, MAINTENANCE FOUD THE RIGHT INBOARD LOWER NACELLE TO WING TRANSIT ANGLE CRACKED AT THE FORWARD EDGE. REPAIR WAS COMPLETED BY INSTALLING A REPAIR DOUBLER IAW ARP 54-20-9101 REV B AND FAIRCHILD SRM 51-30-02, 51-40 AND 51-30-03. (M) 2 L 7 2 4T RT A8SW 1997010900748 19970109 00748 SW 1997 1 9 MALA965212 1 19961120 A 5400 ANGLE SWRNGN SA227 SA227AC 8780603 SW WING/NACELLE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 430MA AC710 DURING A BLOCK INSPECTION IN MSP, MAINTENANCE FUOND LEFT INBOARD LOWER NACELLE TO WING TRANSIT ANGLE CRACKED AT FORWARD EDGE. COMPLETED REPAIR BY REMOVING EXISTING REPAIR, FABRICATING AND WET INSTALLING NEW DOUBLER IAW ARP 54-20-9101 REV B DATED MAY 12, 1993, AND FAIRCHILD SRM CHAPTERS 51-30-02, 51-40 AND 51-30-03. (M) 2 L 7 2 4T RT A8SW 1997010900749 19970109 00749 SW 1997 1 9 MALA965213 1 19961120 A 5400 ANGLE SWRNGN SA227 SA227AC 8780603 SW WING/NACELLE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 430MA AC710 DURING A BLOCK INSPECTION IN MSP, MAINTENANCE FOUND THE LEFT INBOARD UPPER NACELLE TO WING TRANSIT ANGLE CRACKED AT THE FORWARD EDGE. REPAIR WAS COMPLETED BY INSTALLING A REPAIR DOUBLER IAW ARP 54-20-9101 REV B AND FAIRCHILD SRM 51-30-02, 51-40 AND 51-30-03. (M) 2 L 7 2 4T RT A8SW 1997010900750 19970109 00750 SW 1997 1 9 MALA965229 1 19961127 A 5753 2736015 RIB SWRNGN SA227 SA227AC 8780603 SW TE FLAP CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 434MA AC717 DURING A SCHEDULED INSPECTION IN MSP, MAINTENACNE FOUND A CRACK IN THE LEFT FLAP S/N RPL10-88 OUTBOARD FLAP NOSE RIB. R EMOVED AND REPLACED IAW FAC SRM 57-90-60. (M) 2 L 7 2 4T RT A8SW 1997010900751 19970109 00751 SW 1997 1 9 MALA965228 1 19961127 A 5400 ANGLE SWRNGN SA227 SA227AC 8780603 SW WING/NACELLE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 434MA AC717 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND A CRACK IN THE RIGHT FORWARD LOWER INBOARD WING TO NACELLE INTRA NSIT ANGLE. (M) 2 L 7 2 4T RT A8SW 1997010900752 19970109 00752 SW 1997 1 9 MALA965227 1 19961126 A 5320 2722093 INTERCOSTAL SWRNGN SA227 SA227AC 8780603 SW BS 377 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 434MA AC717 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND A .25 INCH CRACK IN LT INTERCOSTAL RELIEF RADIUS AT FUSELAGE STA TION 377. REPAIRED PER FAC MM 53-90-20 REPAIR NR 20. (M) 2 L 7 2 4T RT A8SW 1997010900753 19970109 00753 SW 1997 1 9 MALA965226 1 19961128 A 2720 27420518037 TORQUE TUBE SWRNGN SA227 SA227AC 8780603 SW RUDDER WORN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 434MA AC717 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE RUDDER TORQUE TUBE WORN BEYOND ALLOWABLE LIMITS OF .003 FROM PHENOLIC SEAL. REPAIRED RUDDER TORQUE TUBE BY REMOVING AND REPLACING WITH A NEW RUDDER TORQUE TUBE, P/N 27-42051-8037, IAW FAIRCHILD MM 27-20-20, PAGE 201-202 AND FAIRCHILD SRM 51-00-00 PAGE 04, PART FOR PART REPLACEMENT. (M) 2 L 7 2 4T RT A8SW 1997010900754 19970109 00754 SW 1997 1 9 MALA965230 1 19961128 A 5330 SKIN SWRNGN SA227 SA227AC 8780603 SW BS 241 CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 434MA AC717 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND SKIN CHAFE DAMAGE AT FS 241 AND ON BOTH SIDES OF BL 0.00. CHAF DAMAGE IS APPROX .025 INCH DEEP AND .125 INCH IN DIAMETER. FABRICATED AND INSTALLED EXTERNAL REPAIR DOUBLER (.050 BY 4 BY 5 INCH) IAW FAC SRM 51-90-04 PG 7-8 REV JUN 1/93. (M) 2 L 7 2 4T RT A8SW 1997010900755 19970109 00755 NM 1997 1 9 MALA965224 1 19961129 A 2910 HYD LINE DHAV DHC8 DHC8102 2809003 NM NR 2 ENGINE FAILED A MALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 15 824MA 327 FLT NR 3421 - ON CLIMB-OUT, WHEN GEAR WAS SELECTED UP, THE MASTER CAUTION LIGHT, NR 2 ENGINE HYDRAULIC PUMP, OUTBOARD RO LL SPOILER, RUD PRESS NR 2 AND RUD FULL PRESS LIGHTS ILLUMINATED. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED A RUPTURED HYDRAULIC LINE ON THE NLG ACTUATOR. ALL CHECKS SATISFACTORY. (M) 2 H 7 2 4T RT A13NM 1997010900756 19970109 00756 SW 1997 1 9 MALA965218 1 19961126 A 3260 1EN516 SWITCH SWRNGN SA227 SA227AC 8780603 SW NLG DIRTY A MALA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 15 63NE AC763B FLT 2931 - ON APPROACH TO GPZ, THE NOSE GEAR GREEN LGIHT FAILED TO ILLUMINATE AFTER GEAR EXTENSION. THE CREW CYCLED THE GEAR UNTIL THE LIGHT ILLUMINATED. MAINTENANCE CLEANED, DRIED AND LUBED THE DOWN POSITION SWITCHES. ALL CHECKS SATISFA CTORY. (M) 2 L 7 2 4T RT A8SW 1997010900757 19970109 00757 NM 1997 1 9 USAASB96257 1 19961212 A 5270 189929 PROX SENSOR BOEING 737 7373B7 1384580 NM AFT ENTRY DOOR LOOSE A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 397US 23319 CLT - FLT 489 - ON CLIMB-OUT FROM CLT, THE AFT ENTRY DOOR WARNING LIGHT ILLUMINATED AND THE FLIGHT ATTENDANT NOTED A LOU D AIR NOISE. CAPTAIN DECIDED TO RETURN TO FIELD AT CLT ALTHOUGH PRESSURIZATION WAS NORMAL. FLIGHT LANDED WITHOUT FURTH ER INCIDENT. MAINTENANCE FOUND THE AFT ENTRY DOOR PROXIMITY SENSOR LOOSE. SECURED AND ADJUSTED SENSOR. OPS CHECK GOOD . (M) 2 L 7 2 4F RT A16WE 1997010900758 19970109 00758 EU 1997 1 9 USAAF96126 2 19961212 A 7320 CASC509 FUEL FLOW FOKKER F28 F28MK0100 4990807 EU RROYCE SPEY SPEY55515 54521 EU NR 1 ENGINE FAILED A USAA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 EA 19 888AU 10733 11357 017450 FLT 284 - BWI-IND - WHILE EN ROUTE OVER PIT, CAPT REPORTED LT ENG DID NOT RESPOND. UPON DESCENT NR 1 EPR WOULD NT GO TO IDLE, 85 PERCENT N2. TRIED TO ADVANCE THROTTLES SEVERAL TIMES. FLIGHT DIVERTED TO PIT AND AN EMERGENCY WAS DECLARED. ENGINE WAS DOWN TO 1.2 EPR DURING APPROACH AND FINALLY CAME TO IDLE AT TOUCHDOWN WHEN THROTTLES WERE RETARDED FOR LANDI NG. MX REPLACED NR 1 FUEL FLOW REGULATOR. TRIMMED AND LEAK CHECKED SATISFACTORY. (M) 2 L 7 2 4F 4 F RT E2EU 1997010900759 19970109 00759 NM 1997 1 9 USAASB96249 1 19961202 A 7930 21SN04226A OIL BYPASS SW BOEING 737 737301 1384611 NM LT ENGINE FAILED A USAA A E UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 EA 19 338US 13003 23234 PIT - FLT 1594 - AFTER LEVEL OFF AT FL 250, CREW RECEIVED THE LEFT OIL FILTER BYPASS INDICATION. LIGHT REMAINED ON WHEN THRUST WAS REDUCED. CREW SHUT DOWN LEFT ENGINE. FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT. MAINTENA NCE CHECKED THE OIL FILTERS AND FOUND NO CLOGGING MATERIAL. FOUND THE LEFT ENGINE OIL FILTER BYPASS SWITCH BAD AND REPL ACED IT. (M) 2 L 7 2 4F RT A16WE 1997010900760 19970109 00760 NM 1997 1 9 USAABB96058 1 19961201 A 7714 3301KGAMS1 N3 TACH BOEING 757 757225 1384959 NM RT ENGINE FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 618AU 11906 22210 BWI - FLT 1441 - EN ROUTE BWI-SXM, CREW NOTED THE RIGHT DUCT PRESSURE LOW, THE RIGHT ENGINE N3 INDICATION AT ZERO, AND T HE RIGHT ENGINE OIL PRESSURE IN THE AMBER BAND. FLIGHT RETURNED TO BWI AND LANDED WITH NO FURTHER INCIDENT. MAINTENANC E FOUND AND SECURED A LOOSE SENSE LINE AT THE 490 DEGREE SWITCH, AND REPLACED THE RIGHT N3 TACHOMETER GENERATOR. (M) 2 L 7 2 4F RT A2NM 1997010900761 19970109 00761 NE 1997 1 9 USAABB96057 2 19961201 A 7200 ENGINE BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211535E4 54555 NE LEFT FAILED A A USAA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 EA 19 622AU 27201 31217 CLT - FLT 60 - ON CLIMB-OUT FROM CLT, CREW NOTED HIGH VIBRATION (4.6) FROM LEFT ENGINE. CREW RETARDED LEFT THRUST LEVER . FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 1997010900762 19970109 00762 EU 1997 1 9 SIMA963522 1 19961217 A 3350 E0062B1A4ACOR SWITCH AEROSP ATR42 ATR42300 8680920 EU COCKPIT FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 135MQ 135 ORD - FLT 4162 - EMERGENCY LIGHTS COME ON WITH SWITCH SELECTED TO DISARM WHEN BATTERY SWITCH SELECTED OFF. RAI'D SWITCH 2WL ON OVERHEAD PANEL. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1997010900763 19970109 00763 WP 1997 1 9 USAAD96177 1 19961205 A 3350 110049 CHARGER DOUG DC9 DC931 3022065 WP CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 943VJ 47058 IND - AFTER EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE. REPLACED BATTERY PACK AND CHARGER, REPAIRED WIRING IN SECTIONS 3 AND 4. (M) 2 L 7 2 4F A6WE 1997010900764 19970109 00764 NE 1997 1 9 USAAD96178 2 19961208 A 7200 ENGINE DOUG DC9 DC981 3022081 WP PWA JT8 JT8D217C 52053 NE RT FAILED A A USAA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 EA 19 806US 36330 48038 708459 FLT 532 - CLT-BDL - AFTER TAKEOFF, CREW HEARD A LOUD BANG, AND NR 2 ENGINE EPR WAS DROPPING. RETURNED TO CLT. A/C WAS FERRIED TO PIT, WHERE NR 2 ENGINE WAS CHANGED. (M) 2 L 7 2 4F 4 F A6WE E9NE 1997010900765 19970109 00765 NE 1997 1 9 USAAD96179 2 19961209 A 7200 ENGINE DOUG DC9 DC981 3022081 WP PWA JT8 JT8D217C 52053 NE RIGHT FAILED A A USAA E A ENGINE SHUTDOWN UNSCHED LANDING E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CR CRUISE 1 EA 19 828US 36119 48028 696422 FLT 878 - MCI-LGA - OVER CLE AT FL 250, THE AIRCRAFT EXPERIENCED A SHUDDER, THEN RIGHT ENGINE EPR BEGAN TO DROP. SHUT D OWN RIGHT ENGINE, AND DIVERTED TO CLE. FOUND DAMAGE TO 6TH, 7TH, 12TH, AND 13TH STAGE COMPRESSOR BLADES. REPLACED ENGI NE. (M) 2 L 7 2 4F 4 F A6WE E9NE 1997010900766 19970109 00766 WP 1997 1 9 USAA960777 1 19961206 A 5320 2777976 ANGLE DOUG DC9 DC931 3022065 WP BS 996 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 933VJ 74251 47216 PIT - DURING Q-1, C-2 CHECK, FOUND SKIN BULGE AT CUSP ANGLE AT STATION 996, LONGERON 18R. SPLICED IN NEW SECTION OF CUS P ANGLE PER SRM 53-05 FIG 25. CORROSION TASK NR C50-53300, CORROSION LEVEL 1. (M) 2 L 7 2 4F A6WE 1997010900822 19970109 00822 CE 1997 1 9 97ZZZX178 1 19960901 A 3230 08421022 BELLCRANK IDLER CESSNA 320 320B 2074508 CE MLG FAILED A A EWPA O OTHER O OTHER AP APPROACH 1 SO 07 99004 320B0013 UPON LOWERING LANDING GEAR, BELLCRANK IDLER FAILED NOT ALLOWING NOSE GEAR TO EXTEND FULLY AND LOCK IN POSITION. SUSPECT CAUSE DUE TO METAL FATIGUE. 1 L 7 2 3O 3A25 1997010900828 19970109 00828 CE 1997 1 9 11159616SL 1 19961129 A 3260 BZ2R0T3 SWITCH 3342 BEECH 18 E18S 1151006 CE LT MLG MALFUNCTION A KKFA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 GL 23 16SL BA65 ON APPROACH TO LANDING AT LOUISVILLE LEFT MAIN GEAR WOULD NOT INDICATE DOWN AND LOCKED. REPEATED CYCLES DID NOT HELP. A IRCRAFT RETURNED TO HOME BASE AND LANDING GEAR EXTENDED NORMALLY. AIRCRAFT WAS PLACED ON JACKS, GEAR FUNCTIONED NORMALL Y. LEFT MAIN SWITCH WAS REPLACED. AIRCRAFT WAS RETURNED TO SERVICE. RECOMMEND REPLACING GEAR SWITCHES WHEN IRREGULAR INDICATION IS NOTED. (X) 1 L 7 2 3R A765 1997010900831 19970109 00831 EA 1997 1 9 97ZZZX186 2 19961218 A 7414 10400320 IMPULSE COUPLING PIPER PA32 PA32300 7103212 SO LYC O540 IO540K1A5 41532 EA ENG MAG SPRING BROKE A AVSA K NONE O OTHER NR NOT REPORTED 1 WP 13 4168R 300 K029 3240484 IMPULSE COUPLING SPRING BROKE IN COUPLING THEREFORE RETARDING TIMING. ALL OTHER PIECES LOOK OK. SPRING APPEARS TO BE O F POOR QUALITY. IT BROKE CLEAN - NO WEAR OR SCRATCHES. 1 L 7 1 3O 3 O A3SO 1E4 1997010900832 19970109 00832 EA 1997 1 9 97ZZZX187 2 19961218 A 7414 10400320 IMPULSE COUPLING PIPER PA32 PA32300 7103212 SO LYC O540 IO540K1A5 41532 EA ENG MAG SPRING BROKEN A AVSA K NONE O OTHER NR NOT REPORTED 1 WP 13 4171R K01J 3240504 IMPULSE COUPLING SPRING BROKE IN COUPLING, THEREFORE RETARDING TIMING. ALL OTHER PIECES LOOK OK. SPRING APPEARS TO BE OF POOR QUALITY. IT BROKE CLEAN, NO WEAR OR SCRATCHES. 1 L 7 1 3O 3 O A3SO 1E4 1997010900836 19970109 00836 CE 1997 1 9 97ZZZX191 1 19961218 A 5312 12124096 BULKHEAD 12128581 CESSNA 207 T207 2073612 CE TAIL CONE CRACKED A OEZA K NONE O OTHER IN INSP/MAINT 1 WP 19 775EA 11000 20700162 INSPECTION FOUND 3 CRACKS IN BULKHEAD AND 4 IN BULKHEAD DOUBLER. INSPECTION AND REPLACEMENT OF PARTS DONE IAW AD 72-07- 09 AND CESSNA SE 72-3 AND SE 72-29. 1 H 7 1 3O A16CE 1997010900857 19970109 00857 NE 1997 1 9 97ZZZX212 2 19961202 A 7200 ENGINE AIRBUS 320 A320232 3930326 EU IAE V2500 V2500A1 NE NR 2 FAILED A SOKF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 23 941LF 461 V10039 ON TAXI OUT OF SFO, PILOT REPORTED ENG NR 2 FAILED. A/C RETURNED TO GATE AND AFTER INSPECTION (DELAY OF 2 HRS, 23 MIN) A/C CONTINUED TO MEX. AND TO SFO W/O PROBLEM. PFR GAVE ECAM MSE 'ENG 1 VANE COMPRESSOR' WITH CFDS MESSAGE 'VSV MECH/HYD VALVE, ENG INSP'. MAX EGT WAS C36 DEGREES FOR 2 SEC. VSV ACTUATOR WAS CHANGED AND THE LINKING MECHANISM INSP FOR RIGG ING. THE 7TH AND 10TH STAGE BLEED VALVES WERE CHECKED TO ENSURE THEY WERE WORKING, AND THE ENGINE WAS AGAIN INSPECTED F OR HIGH TEMP. 2 L 7 2 4F 4 F RT A28NM E311NE 1997010900860 19970109 00860 NM 1997 1 9 CALA9700021 1 19961101 A 5711 SPAR WEB BOEING 747 747238B 1384828 NM WS 688 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND A .1875 INCH CRACK AT FASTENER HOLE OF NR 2 PYLON WING FRONT SPAR VERTICAL WEB AT INBOARD NACELLE RIB P OST ATTACH AREA, WS 688. THE FRONT SPAR VERTICAL WEB WAS REPAIRED PER BOEING DRAWING 112U8040, FCD 5710-01758 AND SRM 5 1-10-01. 2 L 7 4 4F A20WE 1997010900861 19970109 00861 NM 1997 1 9 CALA9700022 1 19961106 A 5313 STRINGER BOEING 747 747238B 1384828 NM BS 2180-2190 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND A .125 INCH CRACK IN STRINGER 3R AT MAIN DECK BS 2180 TO 2190. THE STRINGER WAS REPAIRED IAW SRM 53-10 -03, FIGURE 6. 2 L 7 4 4F A20WE 1997010900862 19970109 00862 NM 1997 1 9 CALA9700023 1 19961026 A 5412 BULKHEAD CHORD BOEING 747 747238B 1384828 NM NR 2 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND A .125 INCH CRACK AT FASTENER HOLE COMMON TO THE AFT BULKHEAD VERTICAL CHORD LT FITTING OF NR 2 PYLON. THE CHORD ASSEMBLY WAS REPLACED IAW BOEING DRAWING 65B90413 AND SRM 51-10-01. 2 L 7 4 4F A20WE 1997010900863 19970109 00863 NM 1997 1 9 CALA9700024 1 19961105 A 5753 SKIN BOEING 747 747238B 1384828 NM LT TE MID FLAP DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND LT WING INBOARD MID FLAP PANEL NR 577KT SKIN DELAMINATED. A HOT BOND REPAIR WAS ACCOMPLISHED IAW SRM 5 1-40-06, FIGURE 15. 2 L 7 4 4F A20WE 1997010900864 19970109 00864 NM 1997 1 9 CALA9700025 1 19961101 A 5741 FITTING BOEING 747 747238B 1384828 NM LT/RT WING CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND LT AND RT WING TO BODY KICK FITTINGS CORRODED. THE BODY KICK FITTINGS WERE REPAIRED IAW ECRA 5340-0128 3. 2 L 7 4 4F A20WE 1997010900865 19970109 00865 NM 1997 1 9 CALA9700026 1 19961031 A 5730 SKIN BOEING 747 747238B 1384828 NM WS 1454-1548 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND CORROSION AT RT WING LOWER SKIN FORWARD OF FRONT SPAR LOWER CHORD AND EXTENDING AFT OF FRONT SPAR BETWE EN WS 1454 AND WS 1548. THE AREA WAS REPAIRED IAW ECRA 5710-01766. 2 L 7 4 4F A20WE 1997010900866 19970109 00866 NM 1997 1 9 CALA9700027 1 19961222 A 5753 CHORD BOEING 747 747238B 1384828 NM LT TE MID FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND AN 8 INCH CRACK IN UPPER CHORD OF LT WING OUTBOARD MID FLAP OUTBOARD REAR SPAR. THE CHORD WAS REPAIRED IAW SRM 51-40-02. 2 L 7 4 4F A20WE 1997010900867 19970109 00867 NM 1997 1 9 CALA9700028 1 19961222 A 5720 STIFFENER BOEING 747 747238B 1384828 NM WS 636.72 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND A 1.5 INCH CRACK IN FORWARD VERTICAL STIFFENER AT LT WING LEADING EDGE RIB, INBOARD LEADING EDGE STA 63 6.72. THE STIFFENER WAS REPLACED IAW SRM 51-10-01. 2 L 7 4 4F A20WE 1997010900868 19970109 00868 NM 1997 1 9 CALA9700029 1 19961212 A 5712 RIB BOEING 747 747238B 1384828 NM WS 628 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND A .5 INCH CRACK IN RIB TOP AREA OF LT WING INBOARD LEADING EDGE STA 628. THE RIB WAS REPAIRED IAW SRM 51-40-02. 2 L 7 4 4F A20WE 1997010900869 19970109 00869 NM 1997 1 9 CALA9700030 1 19961222 A 5753 WEB BOEING 747 747238B 1384828 NM RT TE FOREFLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND A .5 INCH CRACK IN THREE LOCATIONS OF MOST INBOARD WEB OF RT WING INBOARD FOREFLAP. THE WEB WAS REPLAC ED IAW SRM 51-10-01, PAGE 18. 2 L 7 4 4F A20WE 1997010900870 19970109 00870 NM 1997 1 9 CALA9700031 1 19961222 A 5711 WEB BOEING 747 747238B 1384828 NM WS 780 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND A 2 INCH CRACK IN FORWARD SPAR WEB OF LT WING AT WS 780. THE WEB WAS REPAIRED IAW SRM 51-40-02, FIGURE 1. 2 L 7 4 4F A20WE 1997010900871 19970109 00871 NM 1997 1 9 CALA9700032 1 19961222 A 5753 CHORD BOEING 747 747238B 1384828 NM RT TE MID FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND A 6 INCH CRACK IN UPPER CHORD OF RT WING OUTBOARD MID FLAP OUTBOARD REAR SPAR. THE CHORD WAS REPAIRED IAW SRM 51-40-02. 2 L 7 4 4F A20WE 1997010900872 19970109 00872 NM 1997 1 9 CALA9700033 1 19961222 A 5720 ANGLE BOEING 747 747238B 1384828 NM WS 631 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND A .5 INCH CRACK IN VERTICAL SUPPORT ANGLE OF RT WING LEADING EDGE NOSE STRUCTURE BACKING WEB AT INBOARD LEADING EDGE STA 631. THE ANGLE WAS REPLACED IAW SRM 51-10-01. 2 L 7 4 4F A20WE 1997010900873 19970109 00873 NM 1997 1 9 CALA9700034 1 19961219 A 5210 DOOR FRAME BOEING 747 747238B 1384828 NM BS 440 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND A 1 INCH CRACK IN DOOR FRAME AT BS 440, STRINGER 26R. THE DOOR FRAME WAS REPAIRED IAW SRM 52-10-02, FI GURE 2. 2 L 7 4 4F A20WE 1997010900874 19970109 00874 NM 1997 1 9 CALA9700035 1 19961216 A 5320 WEB BOEING 747 747238B 1384828 NM BS 1650 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND A .75 INCH CRACK IN WEB AT BS 1650, STRINGER 24L. THE WEB WAS REPAIRED IAW SRM 53-10-04, FIGURE 84. 2 L 7 4 4F A20WE 1997010900875 19970109 00875 NM 1997 1 9 CALA9700036 1 19961216 A 5311 FRAME BOEING 747 747238B 1384828 NM BS 800 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND A .75 INCH CRACK IN FRAME WEB AT STRINGER 24R AND A .75 INCH CRACK WAS FOUND IN FRAME WEB AT STRINGER 2 4L, BS 800. THE WEBS WERE REPAIRED IAW SRM 53-10-04, FIGURE 84. 2 L 7 4 4F A20WE 1997010900876 19970109 00876 NM 1997 1 9 CALA9700037 1 19961216 A 5712 RIB BOEING 747 747238B 1384828 NM WS 670 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND A 1.5 INCH CRACK IN RIB CHORD AT RT WING NR 3 MAIN TANK, WS 670. THE RIB CHORD WAS REPAIRED IAW SB 57- 2273. 2 L 7 4 4F A20WE 1997010900877 19970109 00877 NM 1997 1 9 CALA9700038 1 19961222 A 5712 RIB BOEING 747 747238B 1384828 NM WS 614 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND TOP RIB CHORD CORRODED AT LT WING LEADING EDGE, WS 614. THE RIB CHORD WAS REPAIRED IAW SRM 51-40-02, F IGURE 1. 2 L 7 4 4F A20WE 1997010900878 19970109 00878 NM 1997 1 9 CALA9700039 1 19961211 A 5320 DOUBLER BOEING 747 747238B 1384828 NM BS 400 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND A .25 INCH CRACK IN DOUBLER AT BS 400 BULKHEAD AFT FACE, WL 120, RBL 40. A REPAIR WAS ACCOMPLISHED IAW SRM 53-10-04, FIGURE 37. 2 L 7 4 4F A20WE 1997010900879 19970109 00879 NM 1997 1 9 CALA9700040 1 19961222 A 5754 CHANNEL BOEING 747 747238B 1384828 NM NR 4 LE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17025 20535 INSPECTION FOUND A .125 INCH CRACK IN AFT SUPPORT CHANNEL AT LT WING NR 4 LEADING EDGE FLAP. THE CHANNEL WAS REPAIRED I AW SRM 51-40-03, FIGURE 2. 2 L 7 4 4F A20WE 1997010900880 19970109 00880 WP 1997 1 9 9627309874 1 19961231 A 3350 POWER PACK DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 783NC 48108 DURING LINE CHECK, FOUND TAIL COMPARTMENT EMERGENCY LIGHT INOPERATIVE. REPLACED AFT POWERPACK IN RIGHT LAV CEILING, OPE RATIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1997010900883 19970109 00883 WP 1997 1 9 9627529911 1 19961231 A 3350 CONNECTOR DOUG DC9 DC931 3022065 WP CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 961N 47405 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS BETWEEN ROWS 1 THROUGH 4 INOPERATIVE. MAINT ENANCE RESEATED SPLICE CONNECTOR IN OVERHEAD, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1997010900884 19970109 00884 WP 1997 1 9 9627539972 1 19961231 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9336 47338 DURING PERIODIC CHECK, FOUND FORWARD OVERWING UPPER EMERGENCY LIGHTS ON BOTH LEFT AND RIGHT SIDES INOPERATIVE. REPLACED BATTERIES IN POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1997010900899 19970109 00899 NM 1997 1 9 DL733970009 1 19960103 A 2612 FIRE DETECTOR 72130001008 BOEING 737 737347 1384647 NM FWD LAV SHORTED A DALA K NONE N FALSE WARNING CR CRUISE 1 SO 27 309WA 2829 23442 LAV FIRE WARNING LIGHT AND CHIME CAME ON TWICE DURING FLIGHT WITHOUT CAUSE. REPLACED FORWARD LAV DETECTOR UNIT, OPERATI ONAL TEST NORMAL. 2 L 7 2 4F RT A16WE 1997010900903 19970109 00903 NM 1997 1 9 DL72W970015 1 19960105 A 3350 BATTERY PACK 900835A BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2810W UA4645 20648 LT OVERWING EMERGENCY LIGHTS WILL NOT TEST. REPLACED BATTERY PACK, CHECKS NORMAL. 2 L 7 3 4F A3WE 1997010900904 19970109 00904 NM 1997 1 9 DL72S970016 1 19960106 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 522DA 21582 EXIT LIGHT SIGN NEXT TO FWD COAT CLOSET DOES NOT WORK WHEN EMERGENCY EXIT LIGHTS ARE TURNED ON. REPLACED BATTERY PACK A ND CKS NORMAL. 2 L 7 3 4F A3WE 1997010900905 19970109 00905 NM 1997 1 9 DL73E970018 1 19961228 A 5312 BULKHEAD WEB BOEING 737 737247 138448D NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 376DL 23603 DURING INSPECTIONS PER SI 3-69482-12, THE STATION 178 BULKHEAD WAS FOUND CRACKED IN ONE LOCATION APPROXIMATELY AT RBL 4 AND WL 200. THE RESULTING DAMAGE CUTOUT IS 1 WIDE AND 4.75 LONG. THE BULKHEAD WEB IS FABRICATED FROM 0.032 CLAD 2024-T 3. 2 L 7 2 4F A16WE 1997010900926 19970109 00926 SO 1997 1 9 SRAA960102 1 19960106 A 5320 VERT BEAM WEB LKHEED 382 382E 526413U SO LT MLG WW CRACKED A SRAA K NONE O OTHER IN INSP/MAINT 1 GL 23 908SJ 4300 DURING ROUTINE INSPECTION, FOUND LEFT FORWARD MLG WHEEL WELL HAS 2 CRACKS ON VERTICAL BEAM WEB, APPROX WL 175. ONE CRAC K IS APPROX 2 INCHES AND THE OTHER APPROX 1 INCH. AIRCRAFT IS BEING PREPARED FOR A MAINTENANCE FERRY TO 31J TO FACILITA TE REPAIR. 2 H 7 4 4T A1SO 1997011400001 19970114 00001 EU 1997 1 14 97DXTA087 1 19961101 A 2131 CONTROL VALVE BRAERO 1000 BAE1251000 1500287 EU CABIN PRESSURE WRONG POSITION A DXTA K NONE W INADEQUATE Q C CR CRUISE 1 GL 07 540QS 259040 AIRCRAFT WILL NOT PRESSURIZE IN FLIGHT. FOUND MANUAL CONTROL VALVE 'OPEN' DURING GROUND CHECK. REPOSITIONED VALVE TO ' CLOSED'. (X) 2 L 7 2 4F RT A3EU 1997011400002 19970114 00002 EU 1997 1 14 97DXTA088 1 19961105 A 2120 DUCT BRAERO 1000 BAE1251000 1500287 EU CABIN PRESSURE LEAKING A DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 525QS 259025 FLT 68798 - AIRCRAFT WILL NOT PRESSURIZE IN FLIGHT WITH MAIN AIR VALVE, BUT WILL WITH AUX VALVE. FOUND CABIN AIR FLOW D UCT LEAKING. REMOVED AND REPLACED DUCT. (X) 2 L 7 2 4F RT A3EU 1997011400003 19970114 00003 CE 1997 1 14 97DXTA091 1 19961108 A 2422 INVERTER CESSNA 500 560CESSNA 2076750 CE NR 2 FAILED A DXTA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 GL 07 330QS 5600329 FLT 72905 - NR 2 INVERTER INOPERATIVE. (X) 2 L 7 2 4F RT A22CE 1997011400004 19970114 00004 EU 1997 1 14 HEEA968813 1 19961231 A 2844 APT10010002030SG TRANSDUCER BOLKMS 117 BK117B1 5626012 EU FUEL PRESS DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911TL 7198 FUEL PRESS READING IS HIGH. 1 G 7 2 3U H13EU 1997011400005 19970114 00005 WP 1997 1 14 RRXA96177 1 19961224 A 5711 SPAR CAP DOUG DC8 DC8F54 3021926 WP WS 420 DAMAGE A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 991CF 45801 DURING INSPECTION, FOUND RIGHT WING STA 420 SPAR CAP DAMAGED DUE TO CUTTING TOOL. RELEASED FOR FLIGHT FOR 6 CYCLES PER LETTER FROM COTNEY CO DER DERRRICK. 2 L 7 4 4F 4A25 1997011400006 19970114 00006 NM 1997 1 14 VNAA9612008 1 19961228 A 2752 1048A000002 ACTUATOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT TE FLAP FAILED A A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 438JS 3056 PASSING THROUGH 13,000 FT, HAD A FLAP ASSYM AND FLAP CONTROL FAIL CAS MESSAGE. RETURNED TO FIELD WITHOUT FURTHER INCIDE NT. MAINTENANCE REMOVED AND REPLACED THE LT FLAP ACTUATOR, OPERATIONAL CHECK GOOD. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1997011400009 19970114 00009 WP 1997 1 14 AALA961678 1 19961018 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 505AA 49799 SFO - DURING OVERNIGHT CHECK, LOWER EMERGENCY EXIT SIGN AT RIGHT ENTRY DOOR INOPERATIVE. REPAIRED BROKEN WIRE BEHIND WA LL TO RIGHT ENTRY DOOR LOWER EMERGENCY EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1997011400010 19970114 00010 NM 1997 1 14 AALA961547 1 19961022 A 3230 AAP2448A ACCESSORY UNIT BOEING 727 727223 1384074 NM LANDING GEAR DEFECTIVE A AALA K NONE J WARNING INDICATION CL CLIMB 1 SW 07 862AA 21089 STX - FLT 695 - EN ROUTE MIA-STX - DURING CRUISE, EXPERIENCED NUISANCE WARNING HORN DUE TO A TRIPPED LEVER LATCH CIRCUIT BREAKER. RESET CIRCUIT BREAKER AND WARNING HORN CEASED FOLLOWED BY ELECTRICAL ODOR IN COCKPIT. LEVER LATCH C/B TRIPPE D AGAIN AND WAS NOT RESET. AIRCRAFT PROCEEDED TO STX AND LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR ACCESSORY UNIT AND RESET C/B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1997011400013 19970114 00013 GL 1997 1 14 UPS96821743 2 19961211 A 7261 DRAIN CAP DOUG DC8 DC873F 302199F WP GE CFM CFM562 GL NR 4 ENGINE LOOSE A IPXA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 874UP 46074 692251 INSPECTION TYPE-N/A, DURING 2.5 HR FLIGHT MONITORED NR 4 OIL QTY DROP TO JUST OVER 2 QTS. PERFORMED INFLIGHT ENGINE SHU TDOWN IAW QRH, AIR DIVERT TO BOS. FOUND NR 4 ENG QAD PAD DRAIN FITTING CAP BACKED OFF, TORQUES CAP AND RAN ENG, NO FURT HER LEAKS NOTED 80-10-01 IAW. 2 L 7 4 4F 4 F RT 4A25 E2GL 1997011400014 19970114 00014 SW 1997 1 14 HEEA968706 1 19961211 A 7933 206075187001 INDICATOR BELL 206 206L1 1182107 SW OIL TEMP READS HIGH E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 10814 45415 DUAL INDICATOR TEMP SIDE READS HIGH, OUT OF TOLERANCE OVER 100 DEGREES. 1 G 7 1 3U H2SW 1997011400015 19970114 00015 WP 1997 1 14 UPS96821750 1 19961214 A 2822 BOOST PUMP SW DOUG DC8 DC873F 302199F WP GE CFM CFM562 GL NR 3 ENGINE OUT OF POSITION A IPXA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SO 01 806UP 46006 692619 INSPECTION TYPE-N/A, NR 3 ENGINE FLAMED OUT AT 35,000 FT. BOOST PUMP SWITCH WAS OFF, RESTARTED AT 15,000 FT. PERFORMED NEG PRESS TEST ON NR 3 ENG FEED LINE PER MM 28-22-12. APPLIED NEG PRESS OF -5 PSI FOR 2 MINS, OBSERVED PRES HELD TO -4 .6 PSI. FEED LINE CK FROM BOOST PUMP TO NASH PUMP, NO LK NOTED PER MM 28-22-12. ACCOMPLISHED FCD DC8-7200-0064A AND DC 8-CFM56-2 MIN FUEL PRESS 18 PSI NO DISCREPANCY NOTED. 2 L 7 4 4F 4 F RT 4A25 E2GL 1997011400016 19970114 00016 EU 1997 1 14 SIMA963323 1 19961127 A 3213 D22686050 LANDING GEAR AEROSP ATR42 ATR42300 8680920 EU RIGHT FAILED INSP A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 351AT 11134 11134 MN211 354 ORD - RIGHT LANDING GEAR FAILED ULTRASOUND INSPECTION OF TRUNNION LEG AS PER MESSIER DOWTY TECHNIQUE A/VT NR 20317/96 (F CD E9-32-002). REPLACED GEAR ASSEMBLY IAW ATR 42 JIC 32-11-00. OPS CHECK AND LEAK CHECK GOOD. AIRCRAFT WAS RETURNED T O SERVICE. (M) 2 H 7 2 4T RT A53EU 1997011400018 19970114 00018 NM 1997 1 14 P5CA9601218 1 19960805 A 5400 SKIRT BOEING 747 747121 1384871 NM NR 1 PYLON CHAFED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 SKIRT NR 1 FWD BRIDGE ABOVE PRESS MODULE CHAFED. SMOOTHED CHAFED AND AREA TREATED PER SRM 51-40-03. 2 L 7 4 4F A20WE 1997011400019 19970114 00019 NM 1997 1 14 CALA9601847 1 19961218 A 2910 FILTER BOEING 737 7373T0 1384582 NM A-HYD SYST LEAKING A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 17326 23456 THE A-SYSTEM ENGINE DRIVEN HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATED WHILE EN ROUTE. THE A-HYDRAULIC SYSTEM WAS SHU T OFF AND THE QUANTITY DROPPED TO ZERO. THE AIRCRAFT WAS DIVERTED TO DEN WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE O-RING ON A SYSTEM ELECTRIC PUMP ACOUSTIC FILTER ASSEMBLY LEAKING. THE FILTER WAS REMOVED AND REPLACED. IN ADDITION, THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP WAS REPLACED, LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 1997011400020 19970114 00020 NM 1997 1 14 UPS96421763 1 19960910 A 5320 654U60751694 WEB FITTING BOEING 747 747212B 1384886 NM BS 1420 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE-C, CRACK IN WEB FITTING RBL 10 STA 1420. NEW WEB FITTING INSTALLED IAW SRM 51-30-02, (P/N 654U6075-169) . 2 L 7 4 4F A20WE 1997011400021 19970114 00021 NM 1997 1 14 UPS96421764 1 19961004 A 5313 STRINGER BOEING 747 747212B 1384886 NM BS 2100-2140 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE-C, DEEP CORROSION ON STR 2 LT BETWEEN STA 2100 TO 2140. TYPICAL SPLICE REPAIR CARRIED OUT AS PER SRM 53 -10-03 FIG 5 MATERIAL OBTAINED FROM STA STOCK. 2 L 7 4 4F A20WE 1997011400022 19970114 00022 NM 1997 1 14 UPS96421765 1 19961004 A 5313 STRINGER BOEING 747 747212B 1384886 NM BS 2120-2140 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE-C, CORROSION ON STR 3 LT BETWEEN STA 2120 TO 2140. DAMAGED SECTION OF STRINGER REMOVED. AREA CHECKED A ND CLEANED. TYPICAL SPLICE REPAIR DONE IAW SRM 53-10-03 FIG 5 ANF FIG 6. FASTENERS OBTAINED FROM STA STOCK. 2 L 7 4 4F A20WE 1997011400023 19970114 00023 NM 1997 1 14 UPS96421766 1 19961004 A 5320 TIE CLIP BOEING 747 747212B 1384886 NM BS 2100 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE-C, DEEP CORROSION ON TIE CLIP STA 2100 STR 2, 3 LT CORRODED TIE CLIP REMOVED. NEW TIE CLIP (P/N 65B3860 0-160) PER SRM 51-30-02, OBTAINED FROM STA STOCK. 2 L 7 4 4F A20WE 1997011400024 19970114 00024 NM 1997 1 14 UPS96421767 1 19960929 A 5313 65B04368129 STRINGER BOEING 747 747212B 1384886 NM BS 1680-1740 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE-C, CORROSION ON STR 3 LT BETWEEN STA 1680 TO 1740. INSTALLED NEW PORTION OF STRINGER (P/N 65B04368-129) AND TYPICAL SPLICE REPAIR CARRIED OUT IAW SRM 53-10-03 FIG 5, FASTENERS OBTAINED FROM STA STOCK. 2 L 7 4 4F A20WE 1997011400025 19970114 00025 NM 1997 1 14 UPS96421768 1 19960930 A 5313 65B043368129 STRINGER BOEING 747 747212B 1384886 NM BS 1720-1760 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE-C, DEEP CORROSION ON STR 3 LT INSTALLED NEW PORTION OF STRINGER (P/N 65B04368-129) AND TYPICAL SPLIC E REPAIR CARRIED OUT IAW SRM 53-10-03 FIG 5, FASTENERS OBTAINED FROM STA STOCK. 2 L 7 4 4F A20WE 1997011400026 19970114 00026 NM 1997 1 14 UPS96421769 1 19960829 A 5330 SKIN BOEING 747 747212B 1384886 NM BS 1060 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE-C, CORROSION ON C/S UPPER SKIN STA 1060 UNDER RT STUB FRAME RBL 106 APPROX STUB FRAME. REMOVED CORR OSION AND AREA ANTI-CORROSION TREATMENT. INSTALLED O/S HI-LOCKS BN R3836/96 WORK ACCOMPLISHED PER IAI EO MF-MAN-B747-57 -14-84866 AND SRM 51-30-02. 2 L 7 4 4F A20WE 1997011400027 19970114 00027 NM 1997 1 14 UPS96421770 1 19960912 A 5311 FRAME BOEING 747 747212B 1384886 NM BS 1920 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE-C, S/M DEEP CORROSION ON UPPER CHORD FRAME STA 1920 RT SIDE BETWEEN STR 42 TO 43. UPPER CHORD REMOVED, FABRICATED NEW CHORD PER SRM 53-10-23, CHORD INSTALLED PER SRM 51-30-02, OBTAINED FROM STA STOCK. 2 L 7 4 4F A20WE 1997011400028 19970114 00028 NM 1997 1 14 UPS96421771 1 19960925 A 5313 STRINGER BOEING 747 747212B 1384886 NM BS 2160 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE-C, WEB OF STA 2160 BETWEEN STR 27L TO 27R IS DAMAGED. FABRICATED NEW WEB PER SRM 53-10-23 FIG 9, INSTAL LED PER SRM 51-30-02, OBTAINED FROM STA STOCK. 2 L 7 4 4F A20WE 1997011400029 19970114 00029 NM 1997 1 14 UPS96421772 1 19961009 A 5320 65B38600160 CLIP BOEING 747 747212B 1384886 NM BS 1540 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE-C, CORROSION ON TIE CLIP IN STA 1540 AT STR 3 RT AREA. CORRODED TIE CLIP REMOVED, INSTALLED NEW TIE CLI P (P/N 65B38600-160) PER SRM 51-30-02, OBTAINED FROM STA STOCK. 2 L 7 4 4F A20WE 1997011400030 19970114 00030 NM 1997 1 14 UPS96421773 1 19961009 A 5320 65B38600160 CLIP BOEING 747 747212B 1384886 NM BS 1640 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE-C, CORROSION ON TIE CLIP IN STA 1640 AT STR 3 RT AREA. CORRODED TIE CLIP REMOVED, NEW TIE CLIP (P/N 65B 38600-160) INSTALLED PER SRM 51-30-02, OBTAINED FROM STA STOCK. 2 L 7 4 4F A20WE 1997011400031 19970114 00031 NM 1997 1 14 UPS96421774 1 19961009 A 5320 65B38600160 CLIP BOEING 747 747212B 1384886 NM BS 1680 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE-C, CORROSION ON TIE CLIP IN STA 1680 AT STR 1 RT AREA. CORRODED TIE CLIP REMOVED, NEW TIE CLIP (P/N 65B 38600-160) INSTALLED PER SRM 51-30-02, OBTAINED FROM STA STOCK. 2 L 7 4 4F A20WE 1997011400032 19970114 00032 NM 1997 1 14 UPS96421775 1 19960930 A 5320 WEB BOEING 747 747212B 1384886 NM BS 2240 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE-C, CRACK ON WEB AT STA 2240 BETWEEN STR 16 TO 17, NR 5 PAX RT PAX DOOR AREA. CRACKED WEB REMOVED A NEW WEB MADE IAW SRM 53-10-23 FIG 1. 2 L 7 4 4F A20WE 1997011400033 19970114 00033 NM 1997 1 14 UPS96421776 1 19961004 A 5320 CLIP BOEING 747 747212B 1384886 NM BS 400 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE-C, CRACK ON CLIP IN FLOORBEAM AT STA 400 LBL 20 AREA. CRACKED CLIP REMOVED, FABRICATED NEW CLIP IAW SRM 53-10-20 FIG 12 AND INSTALLED IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1997011400034 19970114 00034 NM 1997 1 14 UPS96421777 1 19960930 A 5330 SKIN BOEING 747 747212B 1384886 NM BS 440 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE-C, CRACK AT 1 LT DOOR ON STA 440 AT STR 26 AREA. CRACKED ANGLE REMOVED, FABRICATED NEW ANGLE SAME AS OR IGINAL PER SRM 53-10-21, NEW ANGLE INSTALLED PER SRM 51-30-02, OBTAINED FROM STA STOCK. 2 L 7 4 4F A20WE 1997011400035 19970114 00035 NM 1997 1 14 UPS96421778 1 19961013 A 5320 SUPPORT BOEING 747 747212B 1384886 NM BS 2260-2300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE-C, CORROSION ON SUPPORT FLOOR BETWEEN STA 2260 TO 2300 RBL 90 AT 5 RT DOOR AREA. TYPICAL SPLICE REPAIR CARRIED OUT IAW SRM 51-40-03. 2 L 7 4 4F A20WE 1997011400036 19970114 00036 NM 1997 1 14 UPS96421780 1 19961111 A 5312 BULKHEAD CLIPS BOEING 747 747212B 1384886 NM BS 340 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE-C, FOUND CRACK ON BULKHEAD ATTACH CLIPS AT STA 340 LT (3) MARKED ATTACHED TO NWW SIDE PANEL. CRACKED CL IPS REMOVED AND NEW CLIPS FABRICATED AS PER SRM 51-40-03 AND INSTALLED AS PER SRM 51-30-02, OBTAINED FROM STA STOCK. 2 L 7 4 4F A20WE 1997011400037 19970114 00037 NM 1997 1 14 UPS96421781 1 19961111 A 5312 BULKHEAD CLIP BOEING 747 747212B 1384886 NM BS 340 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE-C, FOUND CRACK ON BULKHEAD ATTACH CLIP AT STA 340 RT (2) MARKED. CRACKED CLIPS REMOVED AND NEW CLIPS FA BRICATED AS PER SRM 51-40-03 AND INSTALLED AS PER 51-30-02. 2 L 7 4 4F A20WE 1997011400038 19970114 00038 NM 1997 1 14 UPS96421782 1 19961105 A 5313 STRINGER BOEING 747 747212B 1384886 NM BS 1744 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE-C, AFTER SPLICE REMOVED (NR 469307) CRACK FOUND ON STRINGER 10 RT AT STA 1744 APPROX 1 INCH LENGTH. TYP ICAL SPLICE REPAIR CARRIED OUT IAW SRM 53-10-03 FIG 5, NEW PORTION REPLACED. 2 L 7 4 4F A20WE 1997011400039 19970114 00039 SO 1997 1 14 SWIA95783 1 19961122 A 6120 78249046 PCU EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT ENGINE MALFUNCTIONED A A SWIA O OTHER O OTHER CL CLIMB 1 NM 07 236SW 120312 ON CLIMBOUT, RT TORQUE GAUGE FLUCTUATES 80 PERCENT TO 105 PERCENT BOTH IN DIGITAL AND ANALOG WITH EEC'S IN MANUAL. REMO VED AND REPLACED RT ENGINE PCU. ALL GROUND RUNS AND LEAKS CHECKS IAW MM 61-00-00. 2 L 7 2 4T 4 T RT A31SO E20NE 1997011400040 19970114 00040 SO 1997 1 14 SWIA95785 1 19961201 A 5230 DOOR SEAL EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE CARGO COMPT LOOSE A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 229SW 120305 CABIN WOULD NOT PRESSURIZE AND CABIN ALT REMAINED AT 10,000 THROUGH OUT CLIMB. RESECURED ELECTRO PNEUMATIC VALVE CLOSED AS PER MEL 21-30-01, GROUND RUN SHOWS MANUAL CHECKS GOOD. FOUND LOOSE SECTION OF CARGO DOOR SEAL. PRESSURIZED ACFT TO 5.0 PSID IN AUTO AND MANUAL, OPS CHECKS GOOD. RESTORED ELECTRO PNEUMATIC VALVE TO NORMAL. 2 L 7 2 4T 4 T RT A31SO E20NE 1997011400041 19970114 00041 SO 1997 1 14 SWIA95787 1 19961202 A 3232 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT MLG OUT OF ADJUST A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 292SW 120319 RIGHT MAIN GEAR DOORS WOULD NOT CLOSE, CYCLED SEVERAL TIMES. ADJUSTED RIGHT MAIN LANDING GEAR ACTUATOR HALF TURN IAW MM 32-32-10, OPS CKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1997011400042 19970114 00042 NE 1997 1 14 P5CA9601249 2 19961218 A 7200 ENGINE BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE NR 1 LOW POWER A P5CA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 23 920FT 44908 3087 22237 702091 REJECTED TAKEOFF, NR 1 ENGINE UNABLE TO REACH TAKEOFF POWER, CHARTED 1.58 COULD ONLY ACHIEVE 1.47 ALL OTHER PARAMETERS N ORMAL, EXCEPT FOR N1 NR 1 ENGINE 94 PERCENT NR 4 ENGINE 99 PERCENT. REMOVED AND REPLACED NR 1 ENGINE FUEL FILTER, NO DE FECTS NOTED PER M/M 73-11-01, PERFORMED FUEL PUMP HYDRAULIC STAGE (FD12) 800 PSI WITHIN LIMITS, PERFORMED POWER CONFIDEN CE RUN PER M/M 71-00-01 ACCEPTED BY POLAR AIR CARGO ENGINEERING. FULL POWER TAKEOFF COMPLETED AT HNL. 2 L 7 4 4F 4 F A20WE E3NE 1997011600001 19970116 00001 NM 1997 1 16 TAOA129605 1 19961208 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 926TS J1756 20774 RIGHT FORWARD EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATION CHECK NORMAL. (X) 2 L 7 3 4F A3WE 1997011600002 19970116 00002 EU 1997 1 16 JBXA00028 1 19961115 A 2741 WARNING LIGHT FOKKER F28 F28MK0100 4990807 EU STAB CONTROL ILLUMINATED A JBXA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 05 107ML 11450 BDL - FLT 373 - AIRCRAFT STARTED TAKEOFF ROLL, HAD A STAB NR 1 AND NR 2 FAULT. PLANE RETURNED TO GATE. MAINTENANCE PER FORMED AFCAS TEST. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT 1997011600003 19970116 00003 NM 1997 1 16 IXKA9600083 1 19961107 A 3610 BACC10DU350 GASKET GARRTT 12355814 BOEING 727 727225 1384077 NM 8TH STAGE CKVLV LEAKING A IXKA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 25 8883Z 21580 DURING CLIMB-OUT, NR 3 STRUT OVERHEAT LIGHT CAME ON. FOLLOWED AFM PROCEDURES AND RETURNED TO ATL. INSTALLED NEW CLAMP AND GASKET ON 8TH STAGE CHECK VALVE. (X) 2 L 7 3 4F A3WE 1997011600004 19970116 00004 WP 1997 1 16 ZIAA96074 1 19961204 A 2612 CONNECTOR DOUG DC8 DC8F54 3021926 WP NR 3 ENG LOOP DIRTY A ZIAA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 8041U 45675 MHR - DURING CLIMB-OUT, NR 3 ENGINE FIRE WARNING CAME ON. SHUT DOWN THE ENGINE, DISCHARGED BOTH RIGHT WING FIRE BOTLES. RETURNED TO MHR. INSPECTED ENGINE, FOUND NO EVIDENCE OF FIRE. INSPECTED FIRE DETECTION SYSTEM AND CLEANED CONNECTOR ON LOWER LOOP. RESISTANCE AND OPERATION CHECK WERE NORMAL. REPLACED BOTH RIGHT WING FIRE BOTTLES. (X) 2 L 7 4 4F 4A25 1997011600005 19970116 00005 NM 1997 1 16 97ZZZX214 1 19961112 A 3350 987190 SOCKET AMPHENOL 487191 BOEING 727 727251 138408H NM CABIN INOPERATIVE A SQ7A K NONE L NO TEST IN INSP/MAINT 1 SO 01 282US 21161 ONE EACH TRACK LIGHT INOPERATIVE, ROW 18. CORRECTIVE ACTION: REMOVED AND REPLACED LIGHT SOCKET. 2 L 7 3 4F A3WE 1997011600006 19970116 00006 NM 1997 1 16 97ZZZX215 1 19961112 A 3350 900835A BATTERY PACK 900835A BOEING 727 727251 138408H NM CABIN DISCHARGED A SQ7A K NONE L NO TEST IN INSP/MAINT 1 SO 01 282US 10642 21161 EMERGENCY EXIT LIGHT ON FORWARD LIFE RAFT COMPARTMENT INOPERATIVE. CORRECTIVE ACTION: REMOVED AND REPLACED BATTERY PAC K. 2 L 7 3 4F A3WE 1997011600007 19970116 00007 WP 1997 1 16 SABA9600022 2 19961120 A 7321 807432 FUEL CONTROL BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110U 01514 WP LT ENGINE FAILED A A SABA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 SO 33 157PC 3620 2123743 737 SHD - FLT 5116 - LOST POWER LEVER CONTROL ON LEFT ENGINE. SHUT DOWN ENGINE, DECLARED AN EMERGENCY, MADE AN UNEVENTFUL L ANDING IN SHD. MAINTENANCE PERSONNEL PERFORMED GROUND RUN AND VERIFIED CONTROL PROBLEM. FUEL CONTROL UNIT WAS REMOVED AND REPLACED AND AIRCRAFT WAS THEN RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A21EU E4WE 1997011600008 19970116 00008 CE 1997 1 16 97ZZZX216 1 19961018 A 3240 V332 SWITCH CESSNA 500 550 2076604 CE BRAKE SYSTEM INOPERATIVE A NADA O OTHER O OTHER AP APPROACH 1 NE 05 217FS 5500273 LOSS OF HYDRAULIC POWER BRAKE SYSTEM. MICROSWITCH FAILED. AIRCRAFT LANDED SAFELY WITHOUT POWER BRAKE SYSTEM. 1 L 7 2 4F A22CE 1997011600009 19970116 00009 EU 1997 1 16 JBXA00027 1 19961115 A 2920 D9347025400600 FITTING AIRBUS 320 A320231 3930325 EU YELLOW HYD SYST LOOSE A JBXA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SO 05 304ML 373 RDU - FLT 32 - AIRCRAFT DEPARTED RDU FOR LAX. EN ROUTE, CREW HAD YELLOW SYSTEM LOW PRESSURE WARNING ON ECAM AND RETURNE D TO RDU. UPON SHORT FINAL HAD YELLOW RESERVOIR LOW LEVEL. MAINTENANCE FOUND LOOSE B-NUT FITTING ON YELLOW SYSTEM ACCU MULATOR BOTTLE. TIGHTENED B-NUT. OPS CHECK AND LEAK CHECK GOOD IAW A320 MM 29-13. (X) 2 L 7 2 4F RT A28NM 1997011600010 19970116 00010 NE 1997 1 16 C2XA96CL041 2 19961118 A 7230 COMP BLADES BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT ENGINE DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 48544 2216 114405 UE183 114405 CLE - DURING A SCHEDULED OVERNIGHT INSPECTION, MAINTENANCE FOUND THE RT HAND ENGINE TO HAVE DAMAGED COMPRESSOR BLADES. T HE COMPRESSOR BLADES WERE DETERMINED TO BE OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED THE RT HAND ENGINE IAW BEECH CRAFT 1900D MM 71-00-00, OPERATIONAL AND LEAKS CHECKS WERE GOOD IAW BEECHCRAFT 1900D MM 76-10-00. AIRCRAFT RELEASED FOR SERVICE. (X) 2 L 7 2 4T 4 T RT A24CE E26NE 1997011600011 19970116 00011 EU 1997 1 16 97ZZZX217 1 19960917 A 2612 B232M DETECTOR BOLKMS 105 BO105S 5626006 EU NR 2 ENGINE LEAD LOOSE A ALGA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 03 107AL S772 IN CRUISE FLIGHT, THE NR 2 ENGINE FIRE LIGHT FLASHED ON AND OFF CONTINUOUSLY. DESCENDED TO 300 FEET, CHECKED SHADOW FOR SMOKE, NONE SEEN, RETURNED TO BASE. ALL ENGINE INSTRUMENTS NORMAL. REMOVED NR 2 ENGINE COWL, INSPECTED LOWER DETECTOR , INSPECTED UPPER DETECTOR, FOUND LEAD LOOSE ON UPPER DETECTOR. INSTALLED NEW LOCK WASHER AND NUT. OPS CHECK OK. 1 G 7 2 3U H3EU 1997011600022 19970116 00022 SW 1997 1 16 97ZZZX228 1 19960828 A 6210 206010200133 BLADE BELL 206 206B 1181511 SW M/R CORRODED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 117AL 2740 A885 2391 DURING DAILY INSPECTION FOUND TIP WEIGHTS AND TIP BLOCK CORRODED CAUSING SPAR/SKIN DEBOND. 1 G 7 1 3U H2SW 1997011600028 19970116 00028 SW 1997 1 16 97ZZZX234 1 19960828 A 6210 206015001107 BLADE BELL 206 206L4 1182110 SW M/R CORRODED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 174AL 2617 A1198 52067 DURING DAILY INSPECTION FOUND BLADE SKIN CORROSION AND DELAMINATION AT BLADE TIP. 1 G 7 1 3U NC H2SW 1997011600031 19970116 00031 SW 1997 1 16 97ZZZX237 1 19960828 A 6210 206015001107 BLADE BELL 206 206L1 1182107 SW M/R CORRODED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 2092U 2611 A1097 45697 DURING DAILY INSPECTION FOUND BLADE SKIN CORRODED AND DELAMINATED AT TIP. 1 G 7 1 3U H2SW 1997011600033 19970116 00033 SW 1997 1 16 97ZZZX239 1 19960828 A 6210 206015001107 BLADE BELL 206 206L1 1182107 SW M/R CORRODED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 2755N 2542 A1333 45243 DURING DAILY INSPECTION, FOUND BLADE SKIN CORRODED AND SEPARATED AT TIP. 1 G 7 1 3U H2SW 1997011600034 19970116 00034 SW 1997 1 16 97ZZZX240 1 19960828 A 6210 206015001107 BLADE BELL 206 206L1 1182107 SW M/R CORRODED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 2755N 2542 A1326 45243 DURING DAILY INSPECTION FOUND BLADE SKIN CORRODED AND SEPARATED AT BLADE TIP. 1 G 7 1 3U H2SW 1997011600039 19970116 00039 SW 1997 1 16 97ZZZX245 1 19960828 A 6210 206015001107 BLADE BELL 206 206L3 1182108 SW M/R CORRODED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 343AL 2443 A717 51372 DURING DAILY INSPECTION FOUND BLADE SKIN CORRODED AND SEPARATED FROM SPAR AT BLADE TIP. 1 G 7 1 3U H2SW 1997011600043 19970116 00043 SW 1997 1 16 97ZZZX249 1 19960828 A 6210 206015001107 BLADE BELL 206 206L3 1182108 SW M/R CORRODED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 366AL 2638 A1437 51470 DURING DAILY INPSECCTION FOUND BLADE SKIN CORRODED AND SEPARATED AT BLADE TIP. CORROSION INSIDE OF SPAR AT TIP. 1 G 7 1 3U H2SW 1997011600044 19970116 00044 SW 1997 1 16 97ZZZX250 1 19960828 A 6210 206010200133 BLADE BELL 206 206B 1181511 SW M/R DELAMINATED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 42AL 2827 A954 918 DURING DAILY INPSECTION, FOUND LOWER SKIN DELAMINATED AND CORRODED AT OUTBOARD END OF GRIP FINGER DOUBLERS. STA 58 - ST A 60. 1 G 7 1 3U H2SW 1997011600046 19970116 00046 SW 1997 1 16 97ZZZX252 1 19960927 A 6300 206040106001 SPRING 206040015015 BELL 206 206L1 1182107 SW M/R DRIVE BROKEN A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 5734M A2328 45449 FOUND FORWARD COUPLING WOULD NOT STAY STRAIGHT. (POSSIBLY FOUND DURING OTHER MAINTENANCE). SPRING INSIDE OF OUTER COUP LING. SNAPPED AND BROKE IN HALF. 1 G 7 1 3U H2SW 1997011600047 19970116 00047 SW 1997 1 16 97ZZZX253 1 19960828 A 6210 206015001107 BLADE BELL 206 206L1 1182107 SW M/R CORRODED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 5734M 2303 A1651 45449 DURING DAILY INPSECTION FOUND BLADE SKIN CORRODED AND SEPARATED FROM SPAR AT BLADE TIP. 1 G 7 1 3U H2SW 1997011600056 19970116 00056 NE 1997 1 16 MALA965220 2 19961127 A 7510 6058T80P03 ANTIICE VALVE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE RT ENGINE FAILED A MALA O OTHER J WARNING INDICATION CR CRUISE 1 GL 15 99XJ 340A099 FLT 3485 - IN CRUISE FLIGHT, THE RT AIR VALVE LIGHT ILLUMINATED WHEN THE RIGHT ENGINE HEAT WAS SELECTED TO 'ON'. MAINTE NANCE REPLACED THE ANTI-ICE VALVE, PN 6058T80P03 AND THE BLEED VALVE, PN 5056T88P01. ALL CHECKS SATISFACTORY. REFERENC E: OPERATOR CONTROL NR 97ZZZX262. (X) 2 L 7 2 4T 4 T RT A52EU E8NE 1997011600057 19970116 00057 NE 1997 1 16 97ZZZX262 2 19961127 A 7532 5056T88P01 BLEED VALVE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE RT ENGINE FAILED A MALA O OTHER J WARNING INDICATION CR CRUISE 1 GL 15 99XJ 340A099 FLT 3485 - IN CRUISE FLIGHT, THE RT AIR VALVE LIGHT ILLUMINATED WHEN THE RIGHT ENGINE HEAT WAS SELECTED TO 'ON'. MAINTE NANCE REPLACED THE ANTI-ICE VALVE, PN 6058T80P03 AND THE BLEED VALVE, PN 5056T88P01. ALL CHECKS SATISFACTORY. REFERENC E: OPERATOR CONTROL NR MALA965220. (X) 2 L 7 2 4T 4 T RT A52EU E8NE 1997011600058 19970116 00058 EU 1997 1 16 MALA965217 1 19961124 A 3020 NY24668161 DUCT SAAB SF340 SF340A 7850100 EU LT ENGINE COWL FAILED A MALA K NONE O OTHER AP APPROACH 1 GL 15 99XJ 340A099 TOL - FLT 3352 - ON APPROACH TO TOL, THE LEFT ENGINE INTAKE HEAT SHORTED OUT AND BURNED A HOLE IN THE INTAKE LIP. MAINT ENANCE REPLACED THE LEFT AIR INTAKE LOWER DUCT ASSEMBLY. ALL CHECKS SATISFACTORY. (X) 2 L 7 2 4T RT A52EU 1997011600059 19970116 00059 NM 1997 1 16 TWAA9615401 1 19961212 A 2410 2138V088475 CSD SEAL BOEING 747 747206B 1384856 NM NR 3 ENG LEAKING A TWAA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 05 306TW 20398 CDG - DURING CRUISE SHUT DOWN NR 3 ENGINE, S/N 4299, DUE TO LOSS OF OIL. FOUND CSD DRIVE SEAL, MFG P/N 2-138V0884-75, L EAKING. REPLACED CSD DRIVE SEAL, ENGINE OPERATION AND LEAK CHECKS NORMAL. (M) 2 L 7 4 4F RT A20WE 1997011600060 19970116 00060 WP 1997 1 16 97ZZZX263 1 19961202 A 5743 MLG FITTING DOUG DC9 DC932 3022066 WP WS 115 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE RIGHT WING STATION 115 AT REAR SPAR STATION 719 MLG FITTING WAS FOUND TO BE CORRODED. UPON FURTHER EVALUATION, THIS REPAIR WAS FOUND TO BE WITHIN SRM AND DAC TRANSMITTAL L ETTER D035-0035. 2 L 7 2 4F A6WE 1997011600061 19970116 00061 NM 1997 1 16 97ZZZX264 1 19960329 A 3246 BEARING BOEING 737 737201 1384454 NM RT MLG FAILED A L A F3LA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 03 214AU 1243 20214 ABQ - FLT 322 - BLOCK TURN BACK. CREW REPORTED APPARENT RT MLG DAMAGE. MAINT FOUND THE NR 4 MAIN WHEEL, BRAKE AND AXLE ASSEMBLY DAMAGED. REPLACED THE LOWER STRUT ASSEMBLY, THE NR 4 BRAKE ASSEMBLY, THE NR 3 AND NR 4 TIRE ASSEMBLIES, WHEEL BEARING, WHEEL BEARING THRUST WASHER AND NUT, AND AXLE NUT, AND REPAIRED THE WIRING HARNESS AND CANNON PLUG. THE FAILU RE OF THE OUTB WHEEL BEARING PRECIPITATED FRACTURE. FRICTIONAL HEATING CAUSED THE LOCKING TAB ON THE WHEEL LOCK WASHER TO SHEAR OFF. WITH THE LOCK TAB SHEARED OFF, THE WASHER WAS FREE TO ROTATE WITH THE WHEEL IN THE CLOCKWISE DIRECTION. T HE TORQUE LOAD WAS THEN APPLIED TO THE AXLE NUT CAUSING IT TO TIGHTEN. 2 L 7 2 4F A16WE 1997011600062 19970116 00062 SW 1997 1 16 MALA965225 1 19961202 A 5753 2736000 SKIN SWRNGN SA227 SA227AC 8780603 SW RT TE FLAP CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 27465 AC755B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THREE CRACKS ON RT FLAP UPPER SKIN SURFACE P/N 27-36000. TWO AT WS 39.134, BOTH 1 INCH LONG AND 1 AT WS 51.167, .50 INCH LONG. INSTALLED PERMANENT REPAIR DOUBLER PER FAC SRM 57-90-60 , FIGU 10, PAGES 19-21. (X) 2 L 7 2 4T RT A8SW 1997011600063 19970116 00063 SO 1997 1 16 WTAA960210 1 19961205 A 2910 12035805009 HYDRAULIC LINE EMB 120 EMB120RT SO RT MLG WW BROKEN A WTAA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 17 284UE 120145 FAT - GREEN HYDRAULIC LOW PRESSURE AND LOW LEVEL LIGHTS ILLUMINATED. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MA INTENANCE REPLACED RIGHT OUTBOARD SEQUENCE VALVE HYDRAULIC PRESSURE LINE LEAK AND OPERATIONAL CHECK SATISFACTORY. AIRCR AFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1997011600065 19970116 00065 SO 1997 1 16 CA960131009 2 19960118 A 7322 666942 NOZZLE ASSEMBLY CESSNA 150 150M 2071830 CE CONT O200 O200A 17020 SO MCAULY 1A102 1A102OCM GL CARBURETOR MALFUNCTIONING W K NONE O OTHER IN INSP/MAINT 1 CA 437 1527 670607A G15894 (CAN) AT GROUND RUN-UP AT 15 DEGREES C AT 1700 RPM, SAME PROBLEM AS SDR 960131010. THE NOZZLE HAD BEEN CHANGED ON 3 APRI L 1995. THE AIRCRAFT WAS FLOWN FOR 436.9 HOURS WITHOUT A SIMILAR PROBLEM - HAVE CHANGED THE CARBURETOR, INSTALLED MA-3SP A P/N 10-4894V, S/N 1410624. BEFORE THIS PROBLEM SHOWING UP, CAUSED BY COMPLYING WITH SB MSA-7, WHICH HAD BEEN INTRODUCE D TO CORRECT VAPORIZATION AND TOO RICH MIXTURE DURING HOT WEATHER. SUBMITTER BELIEVES THAT PROBLEM WAS WITH COMPLYING WI TH SEB 92-3 AND TO THE WRONG CONFIGURATION OF VENTURIES P/N 46F123. 1 H 7 1 3O 3 O 3A19 E252 5 N P918 1997011600066 19970116 00066 SO 1997 1 16 CA960131010 2 19960116 A 7322 666942 NOZZLE ASSEMBLY CESSNA 150 150L 2071826 CE CONT O200 O200A 17020 SO MCAULY 1A102 1A102OCM GL CARBURETOR POOR OPERATION W K NONE O OTHER IN INSP/MAINT 1 CA 100 100 680397A K20691 (CAN) ON GROUND RUNUP AT -15 DEGREES C AT 1700 RPM, A DROP OF 300-400 RPM WITH FLAME THROWBACK AND GREAT HESITATION. WIT H ENGINE HEAT, INCREASED RPM TO 2000. AFTER 15 MINUTES OF GROUND RUNNING THE DROP WAS WITHIN ACCEPTABLE LIMITS. WHEN THE AIRCRAFT WAS ON FINAL, THE ENGINE COOLED AND THE PROBLEM RETURNED. DURING THE MIXTURE TEST ON THE GROUND RUNUP THE SYMP TOMS REAPPEARED ALMOST IMMEDIATELY WHILE THE FOLLOWING DAYS WITH WARMER WEATHER THERE WAS NO PROBLEM. SUBMITTER CONSIDER S THAT SB MSA-7 APPLIES TO HOT WEATHER ONLY AND NOT WITH COLD TEMPERATURE, THE EFFECT IS LACK OF FUEL TO THE CARBURETOR. OLD NOZZLE P/N 47-799 INSTALLED. 1 H 7 1 3O 3 O 3A19 E252 5 N P918 1997011600069 19970116 00069 NM 1997 1 16 CA960215103 1 19960212 A 2410 CSD BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE #2 ENGINE LOW OIL PRESSURE W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 28184 20166 702782 (CAN) AFTER TAKEOFF, #2 ENGINE CONSTANT SPEED DRIVE LOW OIL PRESSURE LIGHT ILLUMINATED AND #2 GENERATOR DISCONNECTED. LA NDED AIRCRAFT SAFELY AND REPLACED #2 CONSTANT SPEED DRIVE AND #2 OIL COOLER. #2 GENERATOR ALSO REPLACED DUE TO DAMAGE IN CURRED WHILE CHANGING CSD. 2 L 7 2 4F 4 F A16WE E2EA 1997011600070 19970116 00070 NE 1997 1 16 CA960222002 3 19960214 A 6111 SFA13M1OA BLADE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE #2 PROP FAILED TEST W K NONE O OTHER IN INSP/MAINT 1 CA 8815 120305 890915 (CAN) #2 PROP #2 BLADE FAILED WAVE SHEAR TEST AS PER SB 14SF-61-A95. BLADE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1997011600071 19970116 00071 NE 1997 1 16 CA960222003 3 19960214 A 6111 SFA13G1 BLADE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE PROP FAILED TEST W K NONE O OTHER IN INSP/MAINT 1 CA 6587 120657 841104 (CAN) BLADE FAILED SHEAR WAVE TEST AS PER SB 14SF-61-A95. BLADE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1997011600072 19970116 00072 NE 1997 1 16 CA960222006 3 19960219 A 6111 518373 SEAL LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL HAMSTD 54H 54H60117 NE #2 BLADE CUT W E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION DE DESCENT 1 CA 566 566 500859 235867 (CAN) AT TOP OF DESCENT, #4 PROP LOW OIL LIGHT ILLUMINATED. THE ENGINE WAS SHUT DOWN IN FLIGHT AND THE AIRCRAFT LANDED W ITHOUT INCIDENT. MAINTENANCE INVESTIGATION REVEALED A LEAKING BLADE ROOT SEAL. THE PROPELLER ASSEMBLY WAS REPLACED FOR C OMPANY CONVENIENCE. 2 H 7 4 4T 4 T A1SO E282 6 C P906 1997011600073 19970116 00073 EA 1997 1 16 CA960222007 2 19960207 A 8550 MS208234D ELBOW CESSNA 177 177RG 2073709 CE LYC O360 IO360A1B 41514 EA MCAULY 2D34C B2D34C207 GL #1 CYL OIL CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA L1764851A 774491 (CAN) SLIGHT OIL LEAK NOTED AT #1 CYLINDER. FOUND OIL RETURN FITTING ON CYLINDER HEAD CRACKED AROUND 90 PERCENT OF THE C IRCUMFERENCE AT PIPE THREADS FLUSH WITH BOSS. 1 H 7 1 3O 3 O A20CE 1E10 5 C P7EA 1997011600074 19970116 00074 EA 1997 1 16 CA960222008 2 19960207 A 7321 25244405 BEARING BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA FCU HOUSING FAILED W K NONE O OTHER DE DESCENT 1 CA 675 PCE50944 (CAN) ON DESCENT, ENGINE WENT TO IDLE AND WOULD NOT RESPOND TO FURTHER INPUTS. REMOVED FCU - FOUND DRIVE SHAFT FLOPPING AROUND INSIDE HOUSING. 1 L 7 2 3T 4 T A14CE E4EA 1997011600076 19970116 00076 EA 1997 1 16 CA960222024 2 19960201 A 7414 102093502 MAGNETO GULSTM 680 680F 0141606 SW LYC O540 IGSO540B1A 41532 EA L/H AND R/H FAULTY W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA L15450 (CAN) WHILE COMPLYING WITH SB 643 AT FOUR YEAR INTERVAL OR ONE TIME ENGINE, IT WAS DISCOVERED BOTH MAGNETOS WERE IN NEED OF REPLACEMENT. THERE WERE NO RECORDS SHOWING WHEN RIGHT MAGNETO WAS INSTALLED AND THE LEFT ONE WAS FOUND WITH MISSING BEARING BALLS, CASE SEAL WAS BROKEN, AND BREAKER POINTS WERE BURNT. THIS CASE PRESENTS AN EXCELLENT EXAMPLE OF WHY IT I S IMPORTANT TO CARRY OUT SBS AND MANUFACTURER'S RECOMMENDATIONS. BOTH MAGNETO WERE REPLACED AND LOG BOOK ENTRIES MADE. 1 H 7 2 3O 3 O 2A4 1E7 1997011600078 19970116 00078 EU 1997 1 16 CA960223007 2 19960213 A 7200 ENGINE AEROSP SA316 SA315B 8680615 EU TMECA ARTST3 ARTOUSTE3B 60003 EU TURB OIL LEAK W K NONE J K WARNING INDICATION FLUID LOSS LD LANDING 1 CA 2097 (CAN) UPON LANDING, AME NOTICED LARGE AMOUNT OF OIL ON ENGINE DECK AND WITH FURTHER INVESTIGATION, FOUND EXCESSIVE AMOUN T OF OIL IN TAIL PIPE. ENGINE REMOVED AND SENT TO REPAIR FACILITY. 1 G 7 1 4U 3 U H1IN E11N 1997011600082 19970116 00082 NE 1997 1 16 CA960227001 3 19960222 A 6111 SFA13M1OA BLADE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE #1 PROP FAILED TEST W K NONE O OTHER IN INSP/MAINT 1 CA 2750 PCE120056 890915 (CAN) #1 PROP #3 BLADE FAILED TEST AS PER SB 14SF-61-A95. BLADE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1997011600083 19970116 00083 NE 1997 1 16 CA960227002 3 19960222 A 6111 SFA13M1OA BLADE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE #1 PROP FAILED TEST W K NONE O OTHER IN INSP/MAINT 1 CA 2753 PCE120056 890915 (CAN) #1 PROP #1 BLADE FAILED SHEAR WAVE TEST AS PER SB 14SF-61-A95. BLADE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1997011600084 19970116 00084 NE 1997 1 16 CA960227003 3 19960222 A 6111 SFA13M1OA BLADE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE #2 PROP FAILED TEST W K NONE O OTHER IN INSP/MAINT 1 CA 13972 5426 120840 890709 (CAN) #2 PROP BLADE FAILED SHEAR WAVE TEST AS PER SB 14SF-61-A95. BLADE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1997011600085 19970116 00085 NE 1997 1 16 CA960227005 3 19960223 A 6111 SFA13N1OA BLADE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE PROP FAILED TEST W K NONE O OTHER IN INSP/MAINT 1 CA 8000 123136 901117 (CAN) 5 BLADES FAILED SHEAR WAVE TEST AS PER SB 14SF-61-A95. ALL BLADES REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1997011600086 19970116 00086 EA 1997 1 16 CA960227007 2 19960222 A 8520 5015 STUDS PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2B 41532 EA NR 5 CYL BROKEN W A E O A ENGINE SHUTDOWN OTHER UNSCHED LANDING E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CR CRUISE 1 CA L803061A (CAN) DURING CRUISE FLIGHT, THE RIGHT ENGINE BEGAN TO RUN ROUGH, AND LOST SOME POWER. THE CREW WAS UNABLE TO IMPROVE THE SITUATION WITH MAGS/MIXTURE AND ELECTED TO DO A PRECAUTIONARY ENGINE SHUT DOWN. AIRCRAFT LANDED WITHOUT INCIDENT. INVES TIGATION REVEALED 4 BROKEN STUDS; 1 P/N 50-15, 2 P/N 38-13, 1 P/N 69679 ON THE BOTTOM OF #5 CYLINDER. MOVEMENT OF THE CY LINDER CAUSED THE INDUCTION PIPE SEAL P/N 72711 TO DISLOCATE, CAUSING A LARGE INDUCTION AIR LEAK, RESULTING IN THE REPOR TED ROUGH ENGINE AND PARTIAL POWER LOSS. ENGINE WAS REMOVED FOR REPAIR. 1 L 7 2 3O 3 O A20SO E14EA 1997011600088 19970116 00088 SO 1997 1 16 CA960227010 2 19960213 A 8520 646277 LIFTER CESSNA 180 180A 2072604 CE CONT O470 O470K 17026 SO MCAULY 2A34C D2A34C58 GL #3 CYL EXHAUST GALLED W K NONE O OTHER IN INSP/MAINT 1 CA 830 830 845183R 842777 (CAN) #3 CYLINDER EXHAUST HYDRAULIC LIFTER GALLED (DISINTEGRATED). 1 H 7 1 3O 3 O 5A6 E273 5 C P3EA 1997011600090 19970116 00090 SO 1997 1 16 CA960227013 2 19960218 A 8520 632043 CONNECTING ROD CESSNA 404 404CESSNA 2075901 CE CONT O520 GTSIO520M 17032 SO MCAULY 3FF32 3FF32C501 GL #5 CYLINDER BROKEN W E ENGINE SHUTDOWN Y ENGINE STOPPAGE CR CRUISE 1 CA 1045 231539H 790858 (CAN) #5 CONNECTING ROD FAILED AND FRACTURED R/H HALF OF CRANKCASE AND CAMSHAFT BROKE. SUBMITTER SUSPECTS THAT ENGINE HA D BEEN OVERPRIMED PREVIOUSLY AND HAD CAUSED A HYDRAULIC LOCK ON THE CYLINDER BENDING THE CONNECTING ROD CAUSING IT TO FA IL SOMETIME LATER. #5 CYLINDER IS LOWEST POINT ON INBOARD SIDE OF THE LEFT HAND ENGINE. THERE IS ALSO NO INTAKE MANIFOLD DRAIN PROVIDED AT THIS LOCATION. THIS IS A FAULT WITH CESSNA 300 AND 400 SERIES ENGINES. 1 L 7 2 3O 3 O A25CE E7CE 5 C P45GL 1997011600092 19970116 00092 NE 1997 1 16 CA960227018 2 19960219 A 7230 COMPRESSOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 ENG OIL LEAKAGE W K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 CA 2965 120548 (CAN) ON DESCENT, OIL SMELL AND HAZE NOTICED IN THE CABIN IN A NOSE DOWN ATTITUDE. #1 ENGINE REPLACED DUE TO OIL LEAKAGE IN COMPRESSOR. 2 H 7 2 4T 4 T RT A13NM E20NE 1997011600096 19970116 00096 EU 1997 1 16 CA960229005 1 19960228 A 4990 SEALS BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE APU OIL LEAK W D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA LF05539A (CAN) AFTER ENGINE START WITH BLEEDS OFF AND APU AIR ON, CABIN FILLED WITH SMOKE. AIRCRAFT RETURNED TO RAMP AND APU REPL ACED. IT IS SUSPECTED THAT RECENT RASH OF OIL LEAKS IS DUE TO COMPANY CAMPAIGN TO REPLACE EXXON 2380 OIL WITH CASTROL 50 00. 2 H 7 4 4F 4 F RT A49EU E6NE 1997011600099 19970116 00099 CE 1997 1 16 CA960304003 1 19960108 A 3340 30317211RX FLASH TUBE CESSNA 441 441 2076020 CE GARRTT TPE331 TPE3318 01514 WP STROBE LIGHT SHORTED W K NONE O OTHER IN INSP/MAINT 1 CA 7 P31002C (CAN) STROBE LIGHT FLASH TUBE INSTALLED, OVERHAULED AND FAILED WITHIN 7 HOURS OF USE. A SECOND FLASH TUBE ALSO FAILED WI THIN 39 HOURS OF USE. 1 L 7 2 3T 4 T RT A28CE E4WE 1997011600101 19970116 00101 EA 1997 1 16 CA960304007 2 19960221 A 7324 25920 FUEL DIVIDER BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA ENGINE STICKING W A C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CA 7500 PCE32636P (CAN) DURING TAKEOFF ROLL, ENGINE WOULD NOT DEVELOP TAKEOFF POWER. ONLY PRODUCED 2000 LBS TORQUE INSTEAD OF 3400 LBS. FO UND SECONDARY FUEL NOZZLES NOT COMING ON LINE. CHANGED FLOW DIVIDER-PURGE VALVE. TEST RUN & TEST FLOWN SATISFACTORY. VAL VE HAD JUST HAD NEW 'O' RINGS INSTALLED AND HAD CHECKED OUT DURING FUEL MANIFOLD CLEANING. 2 L 7 2 4T 4 T RT A24CE E4EA 1997011600102 19970116 00102 CE 1997 1 16 CA960304008 1 19960208 A 7603 C805973 CABLE CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE THROTTLE DEFECTIVE W E ENGINE SHUTDOWN O OTHER TX TAXI/GRND HDL 1 CA 2169 2169 71714 (CAN) BOTH FORWARD THROTTLE CABLE ASSEMBLIES FOUND TO BE RETAINING MOISTURE. IN EXTREME COLD CONDITIONS, BOTH ASSEMBLIES PROGRESSIVELY STIFFENED, RESTRICTING THROTTLE MOVEMENT. WHEN CABLES WERE COLD SOAKED, THEY WOULD EVENTUALLY SEIZE CABLE S TO THE POINT WHERE FORCE WAS REQUIRED TO BREAK THROTTLE FREE. THIS REQUIRED CABLE REPLACEMENT. 1 L 7 2 4F 4 F A22CE E1NE 1997011600103 19970116 00103 EA 1997 1 16 CA960304009 1 19960208 A 7830 12675862 PNEUMATIC DRIVE CNDAIR CL600 CL6002A12 1900304 EA GE CF34 CF341A NE THRUST REV FAILURE W O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 CA 4512 4512 350143 (CAN) FAILURE OF INTERNAL LOCK MECHANISM OF THE FLEX SHAFT LOCK ON PNEUMATIC DRIVE UNIT. FAILURE OCCURRED DURING THRUST REVERSER STOW CYCLE. THRUST REVERSER ANNUNCIATOR REMAINED ON. FURTHER INVESTIGATION REVEALED THE PDU FLEX SHAFT LOCK FAU LTY WITHIN THE UNIT. 2 L 7 2 4F 4 F RT A21EA E15NE 1997011600106 19970116 00106 NM 1997 1 16 CA960306002 1 19960211 A 2913 O-RING DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE #2 EDP FITTING RUPTURED W L O ABORTED APPROACH OTHER K FLUID LOSS AP APPROACH 1 CA 123037 (CAN) ON APPROACH, THE CREW EXPERIENCED COMPLETE LOSS OF HYDRAULIC FLUID ON THE NUMBER TWO SYSTEM. THE CREW CARRIED OUT AN ALTERNATE GEAR EXTENSION. MAINTENANCE DISCOVERED THE PROBLEM TO BE CAUSED BY A RUPTURED 'O' RING ON A FITTING LEADING TO THE #2 ENGINE DRIVEN HYDRAULIC PUMP. 'O' RING REPLACED, ENGINE GROUND RUN COMPLETELY AND LEAK CHECKED SERVICEABLE. 2 H 7 2 4T 4 T RT A13NM E20NE 1997011600107 19970116 00107 SW 1997 1 16 CA960306003 1 19960222 A 2820 8945681 TUBE ASSEMBLY SWRNGN SA227 SA227AC 8780603 SW ROTOL R321 R321482F8 GL FUEL DIST CRACKED W A O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 CA DRG135484 (CAN) TUBE CRACKED AT 120 DEGREES BEND. TUBE SUPPORTS FUEL FLOW TRANSMITTER WHICH IS OTHERWISE UNSUPPORTED. 2 L 7 2 4T RT A8SW 6 C P61GL 1997011600109 19970116 00109 GL 1997 1 16 CA960306017 3 19960224 A 6114 757583 FLANGE PIPER PA31 PA31350 7103110 SO HARTZL HCE3Y HCE3YR2 GL PROP BASE OVERTORQUED W A K NONE O W OTHER INADEQUATE Q C IN INSP/MAINT 1 CA 1223 DJ308 (CAN) WHILE AME WAS PERFORMING DESLUDGING OF PROPELLER AND ENGINE SHAFT, THREE SEPARATE LARGE TOOLS WERE BROKEN BY THE F ORCE REQUIRED TO REMOVE THE PROPELLER BASE RETAINING NUTS. THE NUTS WERE OVERTORQUED AND THE LOCKWIRE JOB WAS POOR. ALL PARTS INSPECTED FOR CONDITION AND PROPS RE-INSTALLED. NUTS TORQUED TO 60 FT LBS AS PER ASM. 1 L 7 2 3O A20SO 5 C P33EA 1997011600111 19970116 00111 EA 1997 1 16 CA960311002 2 19960304 A 8520 LW17071 CRANKSHAFT CESSNA 172 172P 2072436 CE LYC O320 O320D2J 41508 EA MCAULY 1C160 1C160DTM GL #1 BORE OFF CENTRE W K NONE O OTHER IN INSP/MAINT 1 CA 6725 532 L1227939A BF039 (CAN) THE CRANKSHAFT WAS REMOVED FOR REPAIR OF CORROSION IN ACCORDANCE WITH LYCOMING MSB 505A. THE CENTRE-BORE IN THE FR ONT MAIN BEARING AREA WAS FOUND TO BE OFF CENTRE BY APPROXIMATELY 0.050 INCHES. THE AMO RECEIVED APPROVAL TO REPAIR THE CORROSION BY GRINDING THE CENTRE BORE CONCENTRIC WITH THE OFF CENTRE INSIDE DIAMETER. THIS IS THE THIRD CRANKSHAFT IN TH IS FLEET OF FIVE TO BE OFF CENTRE IN THIS AREA. TWO OF THE CRANKSHAFTS WERE TOO FAR OFF CENTRE TO BE REPAIRED AND WERE S CRAPPED. 1 H 7 1 3O 3 O NT 3A12 E274 5 N P910 1997011600114 19970116 00114 CE 1997 1 16 CA960311005 1 19960229 A 2910 572710024 LINE CESSNA 404 404CESSNA 2075901 CE MCAULY 3FF32 3FF32C501 GL RT WING CRACKED W K O NONE OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 CA 9827 779458 (CAN) ON GEAR LET DOWN, PILOT EXPERIENCED HYDRAULIC SYSTEM FLOW PROBLEMS INDICATED BY HYDRAULIC FLOW LIGHTS IN THE ANNUN CIATOR PANEL. THE UNDER CARRIAGE WAS LOWERED WITHOUT TROUBLE. MAINTENANCE FOUND A CRACKED HYDRAULIC PRESSURE LINE BETWEE N THE RIGHT WING HYDRAULIC FILTER AND THE FUSELAGE BULKHEAD FITTING. A NEW LINE ASSEMBLY WAS INSTALLED. THE SYSTEM WAS F UNCTIONALLY TESTED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1 L 7 2 3O A25CE 5 C P45GL 1997011600115 19970116 00115 EA 1997 1 16 CA960311007 2 19960220 A 7250 BLADES STBROS SD3 SD360 8100606 EU PWA PT6 PT6A65R 52043 EA PT DISC NR 2 ENG FAILED W A C D E ABORTED TAKEOFF RETURN TO BLOCK ENGINE SHUTDOWN E VIBRATION/BUFFET TO TAKEOFF 1 CA 12076 6481 97191 (CAN) ON TAKEOFF ROLL AT 2000 LBS TORQUE, A LARGE POPPING SOUND CAME FROM THE #2 ENGINE, FOLLOWED BY VIBRATION. TAKEOFF ABORTED AND ENGINE SHUT DOWN ON TAXI IN. INSPECTION FOUND DAMAGE TO #1 AND #2 POWER TURBINE DISCS AND IMPACT DAMAGE TO T HE EXHAUST PENUM PLENUM ASSEMBLY. ENGINE CHANGED AND AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T A41EU E4EA 1997011600116 19970116 00116 NE 1997 1 16 CA960311015 2 19960227 A 8520 6515 GEAR BEECH 18 3NM 1151044 CE PWA R985 R985AN14B 52008 NE INTERMED BLOWER CHIPPED W K NONE O OTHER IN INSP/MAINT 1 CA 72 13149 (CAN) DURING INSPECTION, METAL CHIPS FOUND IN ENGINE PORTION OF OIL SUMP. DETERMINED TO BE PART OF UNKNOWN GEAR TOOTH. M ETAL IDENTIFIED TO BE BLOWER INTERMEDIATE GEAR. BLOWER SECTION REMOVED TO CONFIRM FINDING. 1 L 7 2 3R 3 R A765 5E1 1997011600117 19970116 00117 NE 1997 1 16 CA960311023 2 19960302 A 7200 ENGINE BOEING 727 72727C 138400J NM PWA JT8 JT8D7B 52053 NE #2 ENGINE VIBRATION W A UNSCHED LANDING E VIBRATION/BUFFET TO TAKEOFF 1 CA 649507 (CAN) ON TAKEOFF, THE CREW CARRIED OUT A PRECAUTIONARY ENGINE SHUT DOWN DUE TO VIBRATION. 2 L 7 3 4F 4 F A3WE E2EA 1997011600118 19970116 00118 NE 1997 1 16 CA960311026 2 19960228 A 7230 BLADES BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE R/H ENGINE FOD W K NONE C F.O.D. TX TAXI/GRND HDL 1 CA 30819 (CAN) R/H ENGINE FAN BLADES (6) FOUND DAMAGED BY FOD. ALSO INLET NOSE COWL ACCOUSTIC PANEL DAMAGED. BLADE #6 REPLACED AN D THE FIVE OTHERS REPAIRED AS PER MM AND THE NOSE COWL REPAIRED AS PER SRM. 2 L 7 2 4F 4 F RT A2NM E12EU 1997011600119 19970116 00119 NE 1997 1 16 CA960311030 2 19960302 A 7200 ENGINE BOEING 727 727217 NM PWA JT8 JT8D17 52049 NE NR 3 FAILED W E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 CA 688372 (CAN) #3 ENGINE OIL PRESSURE BYPASS LIGHT ILLUMINATED WHILE ALL OTHER ENGINE INDICATIONS WERE NORMAL. THRUST REDUCED TO IDLE. OIL PRESSURE BYPASS LIGHT REMAINED ILLUMINATED AND ALL OTHER ENGINE INDICATIONS CONTINUED TO BE NORMAL. THUST WAS RESTORED TO CRUISE POWER AND ALMOST IMMEDIATELY FUEL FLOW, N2 AND OIL PRESSURE DROPPED TO ZERO. ENGINE REPLACED AND CHEC KED AS PER MM. 2 L 7 3 4F 4 F RT A3WE E2EA 1997011600123 19970116 00123 GL 1997 1 16 CA960312006 2 19960112 A 7261 SCAVENGE PUMP BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL GEARBOX FAILED W A C D E UNSCHED LANDING ABORTED TAKEOFF RETURN TO BLOCK ENGINE SHUTDOWN J WARNING INDICATION TO TAKEOFF 1 CA 9337 5777 CAE821397F (CAN) TIME THIS INSTALLATION - 1163.3 HOURS. NORMAL START UP AND TAKEOFF UNTIL TRANSLATION WHEN TORQUE AND OIL PRESSURE GAUGES STARTED TO FLUCTUATE. IMMEDIATE LANDING AND SHUT DOWN BY PILOT. ENGINE OIL LEVEL CHECKED, NO OIL FOUND IN ENGINE OIL RESERVOIR. NO EXTERNAL LEAKAGE WAS FOUND. INSPECTION BY AME FOUND GEARBOX TO BE FULL OF OIL AND NOTHING IN ENGINE RE SERVOIR. SUBMITTER SUSPECTS SCAVENGE OIL PUMP FAILURE. GEARBOX ASSEMBLY REPLACED AND HELICOPTER RETURNED TO SERVICE. 1 G 7 1 3U 3 U H2SW E4CE 1997011600124 19970116 00124 GL 1997 1 16 CA960312008 2 19960202 A 7200 ENGINE BELL 206 206L 1181522 SW ALLSN 250C 250C20B 03013 GL OIL SYS MAKING METAL W K NONE O OTHER IN INSP/MAINT 1 CA 7368 830805 (CAN) METAL CONTAMINATION FOUND IN OIL TANK AND ON ENGINE CHIP DETECTORS. ENGINE ASSEMBLY AND OIL COOLER REPLACED. HELIC OPTER RETURNED TO SERVICE. 1 G 7 1 3U 3 U H2SW E4CE 1997011600125 19970116 00125 GL 1997 1 16 CA960312015 2 19960131 A 7240 23056130 LINER BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENG COMB CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 509 CAE802078BA (CAN) CRACKS FOUND IN DOUBLER LIP AREA ON PREVIOUS REPAIR WELDS. UNIT REPLACED, AIRCRAFT RETURNED TO SERVICE. 1 G 7 1 3U 3 U H2SW E4CE 1997011600127 19970116 00127 NE 1997 1 16 CA960312022 2 19960221 A 7321 0164448330 FCU SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE INTERNAL FAILURE W A UNSCHED LANDING O OTHER CR CRUISE 1 CA 1260 451 (CAN) ENGINE DECELLERATED IN CRUISE TO 345 NR RPM. FCU REPLACED AND HELICOPTER RETURNED TO SERVICE. 1 G 7 1 3U 3 U H9EU E19EU 1997011600128 19970116 00128 NE 1997 1 16 CA960312028 2 19960223 A 7230 70BMO21060 COMPRESSOR SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE FAILURE W A E UNSCHED LANDING ENGINE SHUTDOWN O OTHER CR CRUISE 1 CA 4872 3025 834 (CAN) COMPRESSOR STALLED IN FLIGHT AT 60 PERCENT Q. COMPRESSOR WAS ON A 50 HOUR TBO EXTENSION. COMPRESSOR WAS REPLACED, AND HELICOPTER RETURNED TO SERVICE. 1 G 7 1 3U 3 U H9EU E19EU 1997011600129 19970116 00129 GL 1997 1 16 CA960312030 2 19960201 A 7321 23034702 FCU BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE FAILURE W K NONE O OTHER IN INSP/MAINT 1 CA 3216 802694 (CAN) TIME THIS INSTALLATION 1001.1 HOURS. UNABLE TO ADJUST FOR SLOW COLD STARTS. ALSO CAUSING A BURBLING SOUND NEAR TOP END OF START - SUSPECT COMPRESSOR STALL DUE TO FCU. FCU REPLACED, HELICOPTER RETURNED TO SERVICE. 1 G 7 1 3U 3 U H2SW E4CE 1997011600130 19970116 00130 GL 1997 1 16 CA960312032 2 19960225 A 7321 23057344 FCU BELL 206 206L 1181522 SW ALLSN 250C 250C20B 03013 GL ENGINE FAILURE W K NONE E O X VIBRATION/BUFFET OTHER ENGINE FLAMEOUT CR CRUISE 1 CA 426 CAE830144 (CAN) TIME THIS INSTALLATION SINCE LAST REPAIR 189.3 HOURS. IN FLIGHT EXPERIENCED A TEMPORARY FLAMEOUT. AFTER 3-4 SECO NDS, ENGINE AND ROTOR SPEEDS BACK UP TO NORMAL. FLIGHT RESUMED TO BASE WITHOUT FURTHER INCIDENT. PAST HISTORY OF THIS FCU IS ONE OF MANY PREMATURE REMOVALS CAUSING SIMILAR PROBLEMS AND ERRATIC STARTS, AND FIELD ADJUSTMENTS ARE NOT WORKING . FCU REMOVED FOR REPAIR. 1 G 7 1 3U 3 U H2SW E4CE 1997011600131 19970116 00131 NE 1997 1 16 CA960315011 2 19960311 A 7200 ENGINE BOEING 727 72727C 138400J NM PWA JT8 JT8D7B 52053 NE COMB CAN FAILURE W A K NONE O OTHER IN INSP/MAINT 1 CA 649507 (CAN) BOROSCOPE EXAMINATION OF ENGINE WAS INCONCLUSIVE BUT APPARENT DAMAGE SUGGESTS A COMBUSTION CAN FAILURE OF SOME DES CRIPTION MAY HAVE INDUCED THE NOZZLE AND T1 DAMAGE OR THE POSSIBILITY OF T1 BLADE FAILURE AS THE SECOND OPTION. AN ENGIN E CORE STRIP REPORT HAS BEEN REQUESTED, FINAL ANALYSIS TO FOLLOW. 2 L 7 3 4F 4 F A3WE E2EA 1997011600132 19970116 00132 NE 1997 1 16 CA960318005 3 19960315 A 6111 SFA13M1OA BLADE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE #1 PROP FAILED TEST W K NONE O OTHER IN INSP/MAINT 1 CA 8970 PCE120832 871022 (CAN) #1 BLADE ON #1 PROP FAILED SHEAR WAVE TEST AS PER SB 14SF-61-A95. BLADE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1997011600134 19970116 00134 NE 1997 1 16 CA960320541 2 19960207 A 7532 3017808040 BLEED VALVE AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE #1 ENGINE FAULTY W A UNSCHED LANDING O OTHER CL CLIMB 1 CA 731668 (CAN) AIRCRAFT RETURNED TO ORIGIN AFTER TAKEOFF DUE TO #1 ENGINE SURGING. EGT EXCEEDENCE. FOUND ENGINE COMPRESSOR BLEED VALVE AT FAULT. CHANGED #1 ENGINE VARIABLE BLEED VALVE SENSOR. FADEC TEST CARRIED OUT ON BOTH CHANNELS. 2 L 7 2 4F 4 F RT A28NM E29NE 1997011600135 19970116 00135 NE 1997 1 16 CA960320542 2 19960208 A 7200 ENGINE BOEING 747 747133 138448B NM PWA JT9 JT9D7 52054 NE #1 ENGINE VIBRATION W E F A ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 CA 46599 P685933 (CAN) #1 ENGINE VIBRATION, LOW AND HIGH SPEED ROTOR INDICATION STAYED AT 3.0 UNITS FROM BEGINNING OF FLIGHT. LOOP B ON D EVIATION AND LOOP A FULL RED, ENGINE SHUT DOWN. DISCHARGED BOTH FIRE EXTINGUISHER BOTTLES, AND AIRCRAFT RETURNED TO LAND SAFELY. 2 L 7 4 4F 4 F A20WE E20EA 1997011600138 19970116 00138 GL 1997 1 16 CA960325011 2 19960313 A 7260 23035176 BEARING BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL GR BOX NR 3 - 4 SPUN W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 4453 4453 CAE860547 (CAN) ENGINE CHIP LIGHT CAME ON IN CRUISE FLIGHT AND AIRCRAFT LANDED. 2 CHIP PLUGS AND OIL FILTER INSPECTED AS PER ALLIS ON MM REQUIREMENTS FOR CHIP LIGHT INDICATION. VERY FINE BRONZE COLOURED MATERIAL AND TWO MAGNETIC SLIVERS NOTED. PLUGS A ND FILTER CLEANED AND AIRCRAFT RETURNED TO SERVICE. SECOND CHIP LIGHT WARNING AFTER APPROXIMATELY 1 HOUR OF FLIGHT. VERY FINE PARTICLES NOTED AGAIN AND DECISION MADE TO REMOVE ENGINE FOR INSPECTION AND REPAIR. SUBMITTER SUSPECTS THAT THE #3 AND #4 GEARBOX BEARING OUTER RACE WAS BEGINNING TO SPIN. THERE IS AN ALLISON BULLETIN TO PIN THIS RACE AT THE GEARBOX/E NGINE OVERHAUL. 1 G 7 1 3U 3 U H2SW E1GL 1997011600140 19970116 00140 CE 1997 1 16 CA960401002 1 19960315 A 2130 V31001 SWITCH CESSNA 500 500CESSNA 2076602 CE TERMINALS SHORTED W A D UNSCHED LANDING RETURN TO BLOCK O OTHER CR CRUISE 1 CA (CAN) AIRCRAFT DEPRESSURIZED IN FLIGHT, RETURNED TO BASE. 85 PERCENT SWITCH TERMINAL FOUND LOOSE, SHORT CIRCUITED CAUSI NG PRESSURIZATION SYSTEM TO SENSE ON GROUND CONDITION OPENING OUTFLOW VALVE. S149 SWITCH REPLACED AND SYSTEM FUNCTION T ESTED. 1 L 7 2 4F A22CE 1997011600141 19970116 00141 WP 1997 1 16 CA960429010 2 19960217 A 7250 30727322 BLADE LEAR 35 35A 5170602 CE GARRTT TFE731 TFE7312 01518 WP HP TURBINE SEPARATED W A E ENGINE SHUTDOWN X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 CA 4066 P74369 (CAN) CRUISING AT 35,000 FEET AND ALL SYSTEMS NORMAL. THERE WAS A LOUD BANG, TIT WENT TO MAX., AND ENGINE FLAMED OUT. AI RCRAFT TURNED AROUND AND RETURNED TO ORIGIN. AFTER TEARDOWN, HP TURBINE BLADE SEPARATION WAS FOUND TO BE THE CAUSE OF TH E FAILURE. 2 L 7 2 4F 4 F A10CE E6WE 1997011600142 19970116 00142 NM 1997 1 16 CA960809003 1 19960802 A 5610 NP15790210 WINDOW PPG DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE TOP CORNER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 9401 933 91284H9292 120358 (CAN) DURING TASK 5310/07C (SIDE WINDOW TRANSPARENCY) FOUND A CRACK ON THE SIDE WINDOW3. CRACK LOCATED AROUND A SCREW HO LE IN THE TOP FORWARD CORNER. WINDOW PREVIOUSLY REPAIRED. THREE UNITS FROM STOCK FOUND CRACKED. 2 H 7 2 4T 4 T RT A13NM E20NE 1997011600143 19970116 00143 EU 1997 1 16 CA960812017 1 19960715 A 2822 P94B12203C PUMP SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE FUEL BOOST FAILED W C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CA 2 879 (CAN) PUMP FAILED AFTER 2 HOURS IN SERVICE (5 STARTS). 1 G 7 1 3U 3 U NC H9EU E19EU 1997011600144 19970116 00144 EU 1997 1 16 CA960812018 1 19960712 A 6220 350A31190703 STARFLEX SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE BLUE ARM DEBONDED W A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 CA 345 4431 (CAN) VIBRATION LEVEL INCREASED DURING FLIGHT, AND GROUND RESONANCE EXPERIENCED DURING LANDING. INSPECTION SHOWED THAT T HE BLUE POSITION STAR ARM END BUSHING HAD DEBONDED IN FLIGHT AND HAD CAUSED EXCESSIVE DAMAGE IN COMPOSITE. 1 G 7 1 3U 3 U NC H9EU E19EU 1997011600145 19970116 00145 EU 1997 1 16 CA960812019 2 19960806 A 7321 500104447002 FUEL TRIMMER PLESSEY 500104447002 BRAERO 748 HS7482B 1500248 EU RROYCE DART DART5342 EU NR 2 ENG FAILURE W A UNSCHED LANDING O OTHER CR CRUISE 1 CA 1459K 13568 (CAN) IN CRUISE #2 ENGINE FUEL TRIM FAILED. AIRCRAFT RETURNED TO BLOCKS. FUEL TRIM REPLACED. 2 L 7 2 3T 4 T A24EU A196 1997011600146 19970116 00146 NM 1997 1 16 CA960812020 1 19960804 A 2920 82970010591 LINE DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE SPOILER CHAFED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 123046 (CAN) HYDRAULIC LINE FOR FLIGHT SPOILER IN SYSTEM #2 IN THE WHEEL WELL FOUND CHAFED. LINE CHAFED AGAINST THE EXHAUST SHR OUD COOLING PIPE. THE STEEL WIRE THAT STRENGTHENS THE FLEX PIPE CAUSED THE CHAFE. 2 H 7 2 4T 4 T RT A13NM E20NE 1997011600147 19970116 00147 NE 1997 1 16 CA960813002 2 19960804 A 8550 125754 GASKET CNDAIR CL215 CL2151A10 EA PWA R2800 CA3 52026 NE OIL FILTER TORN W A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 CA P32474 (CAN) SHORTLY AFTER TAKEOFF THE PILOT NOTICED THE #1 ENGINE OIL QUANTITY GAUGE WAS DROPPING. THE AIRCRAFT RETURNED TO IT S POINT OF DEPARTURE. POST FLIGHT INSPECTION REVEALED THE PRESSURE OIL FILTER GASKET WAS MISSING A SECTION. THE GASKET W AS REPLACED AND THE OIL FILTER COVER NUTS (P/N AN3850) WERE REPLACED AND TORQUED. ENGINE WAS GROUND RUN SERVICEABLE AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4R 4 R A14EA E231 1997011600148 19970116 00148 SW 1997 1 16 CA960814201 1 19960804 A 6230 204011402009 INNER RING BELL 2040114009 BELL 204 204B 1181404 SW LYC T53 T5311B 41549 NE TRUNNION MOUNT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1877 172 J19903 LE08152A (CAN) ON DAILY INSPECTION, CRACK FOUND IN L.H. TRUNNION MOUNTING EAR OF THE SWASHPLATE INNER RING. 1 G 7 1 4U 4 U H1SW E1EA 1997011600149 19970116 00149 SO 1997 1 16 CA960819201 2 19960807 A 8530 630393 PUSHROD CESSNA 337 337A 2075704 CE CONT O360 IO360C 17025 SO MCAULY 2AF34C D2AF34C301 GL #3 CYLINDER SHEARED W O OTHER O OTHER TX TAXI/GRND HDL 1 CA 30 554316D 722892 (CAN) PILOT REPORTED BACKFIRE DURING GROUND RUN-UP. INVESTIGATION FOUND REAR ENGINE #3 CYLINDER EXHAUST PUSHROD SNAPPED APPROXIMATELY 1" FROM THE TIP. RETAINER P/N 628059 WAS ALSO FOUND FAILED. ENGINE WAS RETURNED TO OVERHAUL SHOP. 1 H 7 2 3O 3 O A6CE E1CE 5 C P5EA 1997011600150 19970116 00150 NE 1997 1 16 CA960826001 2 19960815 A 7260 313594 BOSS NUT BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE ACCESSORY GEARBX LOOSE W A E UNSCHED LANDING ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA P707369B (CAN) ENGINE OIL PRESSURE LOSS IN FLIGHT. ENGINE SHUTDOWN AND AIRCRAFT DIVERTED. POST FLIGHT INSPECITON FOUND BANJO BOLT LOOSE ON THE OIL BYPASS BOSS. BANJO BOLT TIGHTENED AND ENGINE GROUND RUN SERVICEABLE. 2 L 7 2 4F 4 F A16WE E2EA 1997011600151 19970116 00151 NM 1997 1 16 CA960826003 1 19960809 A 3233 65358492 BEARING BOEING 737 737242C 1384478 NM PWA JT8 JT8D9A 52048 NE NLG RETRACT CYL CORRODED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 707397 (CAN) NOSE GEAR WOULD NOT LOCK IN THE UP POSITION. RETRACT CYLINDER UPPER ATTACH CASTING OUTER RACE DEFORMED AND CORRODE D. CORROSION REMOVED AND BEARING REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1997011600152 19970116 00152 SW 1997 1 16 CA960826005 1 19960808 A 7922 8A575000 VERNATHERM VALVE SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110 01514 WP ENG OIL FAILED W A A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CR CRUISE 1 CA P54232 (CAN) DURING CRUISE, THE CREW NOTICED HIGH OIL TEMP ON THE RIGHT ENGINE. INVESTIGATION REVEALED HIGH OIL TEMP IN THE TAN K AND COLD OIL IN THE COOLER. THE VERNATHERM VALVE P/N 8A575-000 S/N 000123 WAS REPLACED WITH A SERVICEABLE ONE AND ENGI NE GROUND RUN. THE OIL TEMP QUICKLY REDUCED TO NORMAL CRUISE TEMPERATURE, AND THE COOLER BECAME HOT (INDICATING CORRECT OIL FLOW). 2 L 7 2 4T 4 T RT A8SW E4WE 1997011600153 19970116 00153 NE 1997 1 16 CA960826006 2 19960809 A 7530 3033716 CARBON SEAL DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE P2.5/P3 VALVE LEAKING OIL W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA 123133 (CAN) CREW REPORTED SMOKE IN CABIN AFTER START. INSPECTION FOUND P2.5/P3 SWITCHING VALVE CARBON SEAL LEAKING OIL. SWITCH ING VALVE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1997011600154 19970116 00154 EU 1997 1 16 CA960826007 1 19960809 A 2150 4754C000 HEAT EXCHANGER BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE #1 AC PAC CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 19162 3261 B5922563 LF05627A (CAN) #1 AIR CONDITIONING PACK HEAT EXCHANGER FOUND WITH 1/2 INCH CRACK IN FORWARD BOTTOM CORNER AND IS LEAKING AIR. 2 H 7 4 4F 4 F RT A49EU E6NE 1997011600156 19970116 00156 NM 1997 1 16 CA960826009 1 19960809 A 2910 82970010337 LINE DHAV DHC8 DHC8101 2809002 NM PWA PW120 PW123 NE #1 NACELLE CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 123138 (CAN) HYDRAULIC LEAK NOTED FROM #1 NACELLE. CRACKED HYDRAULIC LINE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1997011600157 19970116 00157 NM 1997 1 16 CA960826010 1 19960809 A 3242 0232 SEAL DUNLOP 214664 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE RT BRAKE ASSY LEAKING W O OTHER B K SMOKE/FUMES/ODORS/SPARKS FLUID LOSS TX TAXI/GRND HDL 1 CA 607 0232 120305 (CAN) AFTER LANDING, GROUND CONTROL ADVISED SMOKE WAS COMING FROM RIGHT WHEELS. PROBLEM FOUND TO BE FLUID ON BRAKES FRO M LEAKING PISTON SEAL. BRAKE ASSEMBLY REPLACED. PROBLEM KNOWN TO BRAKE MANUFACTURER 2 H 7 2 4T 4 T RT A13NM E20NE 1997011600158 19970116 00158 NE 1997 1 16 CA960826011 2 19960725 A 7322 A178097 CARBURETOR DHAV DHC2 DHC2MK1 2800102 EA PWA R985 R985AN14B 52008 NE ENGINE FAULTY W E B A ENGINE SHUTDOWN EMER. DESCENT UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 CA 77 JP211135 (CAN) ENGINE BEGAN TO RUN OVER RICH AND THEN FLOODED. THE PILOT ADDED CARBURETOR HEAT WHICH ONLY ENRICHED IT MORE. A SUC CESSFUL FORCED LANDING WAS CARRIED OUT AND THE CARBURETOR WAS REPLACED. 1 H 7 1 3R 3 R A806 5E1 1997011600159 19970116 00159 WP 1997 1 16 CA960826013 1 19960816 A 3233 71658 ATACH BOLT DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE MLG ACTUATOR SHEARED W L ABORTED APPROACH O OTHER LD LANDING 1 CA 517409 (CAN) MAIN LANDING GEAR RETRACT ACTUATOR SUPPORT FITTING ATTACHMENT BOLTS SHEARED AND ACTUATOR FELL OVER AND DOWN WHEN G EAR WAS EXTENDED. FREE FALL EXTENSION INITIATED, NO PROBLEMS. MAINTENANCE CHECK REVEALED ACTUATOR SUPPORT FITTING BOLTS SHEARED. BOLTS, NUTS AND ACTUATOR FITTING REPLACED. 2 L 7 3 4F 4 F A22WE E23EA 1997011600160 19970116 00160 NM 1997 1 16 CA960826014 1 19960822 A 7312 320115 VALVE ALLIED SIGNA 320115 BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE FUEL HEAT OPEN W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 646 674513 (CAN) AIRCRAFT RETURNED TO GATE AFTER OIL TEMPERATURE INDICATION IN CLIMB OUT. FOUND FUEL HEAT VALVE PARTIALLY OPEN. REP LACED. 2 L 7 2 4F 4 F A16WE E2EA 1997011600167 19970116 00167 SO 1997 1 16 97ZZZX271 2 19961223 A 8550 642336 PLUNGER 642224 CESSNA 402 402C 207590R CE CONT O520 TSIO520UB 17040 SO OIL PRESS RELIEF FOD MALFUNCTION A OEZA K NONE O OTHER IN INSP/MAINT 1 WP 19 26150 402C0111 278444R MECHANIC NOTICED THAT OIL PRESSURE DROPPED TO ZERO WHEN THROTTLE WAS RETARDED. FOUND 3 PIECES OF SAFETY WIRE STUCK UNDE R OIL PRESSURE RELIEF VALVE. REMOVED THE WIRE AND OPS CHECKED GOOD. 1 L 7 2 3O 3 O A7CE E8CE 1997011600169 19970116 00169 SO 1997 1 16 97ZZZX273 2 19961223 A 8550 631056A1 COVER ASSY 632970 CESSNA 402 402C 207590R CE CONT O520 TSIO520UB 17040 SO OIL PUMP LEAKING A OEZA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 19 26150 402C0111 278444R OIL PUMP COVER IMPROPERLY INSTALLED BY OVERHAULER CAUSING A SERIOUS LEAK. RE-SEALED COVER PER TCM O/H MANUAL. FIXED TH E PROBLEM. 1 L 7 2 3O 3 O A7CE E8CE 1997011600171 19970116 00171 CE 1997 1 16 97ZZZX275 1 19961224 A 5312 12124096 BULKHEAD CESSNA 207 T207 2073612 CE AFT CRACKED A OEZA K NONE O OTHER IN INSP/MAINT 1 WP 19 775EA 20700162 DURING C/W OF AD 72 07-09, FOUND 4 CRACKS IN BULKHEAD P/N 1212859-1 AND 3 CRACKS IN BULKHEAD P/N 1212409-6. THE REST OF THE FIN STRUCTURE WAS DYE CHCKED AND INSPECTED AND NO FURTHER CRACKS WERE FOUND. ONE FORWARD VERTICAL FIN BOLT HAD SHO WN SIGNS OF LOOSENING. THIS AIRPLANE HAD INSPECTION 1,000 HRS PREVIOUSLY. 1 H 7 1 3O A16CE 1997011600172 19970116 00172 CE 1997 1 16 97ZZZX276 1 19961224 A 5312 12128591 BULKHEAD CESSNA 207 T207 2073612 CE AFT CRACKED A OEZA K NONE O OTHER IN INSP/MAINT 1 WP 19 775EA 20700162 DURING C/W OF AD 72 07-09, FOUND 4 CRACKS IN BULKHEAD P/N 1212859-1 AND 3 CRACKS IN BULKHEAD P/N 1212409-6. THE REST OF THE FIN STRUCTURE WAS DYE CHCKED AND INSPECTED AND NO FURTHER CRACKS WERE FOUND. ONE FORWARD VERTICAL FIN BOLT HAD SHO WN SIGNS OF LOOSENING. THIS AIRPLANE HAD INSPECTION 1,000 HRS PREVIOUSLY. 1 H 7 1 3O A16CE 1997011600176 19970116 00176 NM 1997 1 16 CALA9700041 1 19961123 A 5313 STRINGER BOEING 727 727224 1384076 NM BS 520 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND STRINGER 28L CORRODED AT BS 520. A STRINGER AND SPLICE REPAIR WAS INSTALLED IAW SRM 53-10-3, FIGURE 1. 2 L 7 3 4F A3WE 1997011600177 19970116 00177 NM 1997 1 16 CALA9700042 1 19961129 A 5320 CHANNEL BOEING 727 727224 1384076 NM BS 540 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND FORWARD CARGO BAY SIDEWALL FLOOR SUPPORT CHANNEL CORRODED AT BS 540, STRINGER 27R. A FLOOR SUPPORT CHA NNEL WAS FABRICATED AND INSTALLED IAW SRM 51-30-1 AND 53-10-8. 2 L 7 3 4F A3WE 1997011600178 19970116 00178 NM 1997 1 16 CALA9700043 1 19961129 A 5320 SUPPORT BOEING 727 727224 1384076 NM BS 640 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND FORWARD CARGO BAY FLOOR SUPPORT TRACK CORRODED AT BS 640, STRINGER 28L. A FLOOR SUPPORT TRACK WAS FABR ICATED AND INSTALLED IAW SRM 53-10-2, FIGURE 8, SRM 51-10-6, AND 51-30-2. 2 L 7 3 4F A3WE 1997011600179 19970116 00179 NM 1997 1 16 CALA9700044 1 19961122 A 5321 FLOOR BOEING 727 727224 1384076 NM NR 2 GALLEY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND NR 2 GALLEY UPPER COMPARTMENT FLOOR CORRODED. THE CORROSION WAS REMOVED, TWO DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-10-1. 2 L 7 3 4F A3WE 1997011600180 19970116 00180 NM 1997 1 16 CALA9700045 1 19961130 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 511PE 20634 THE AFT CEILING AISLE EXIT LIGHT AT NR 3 GALLEY WAS INTERMITTENT DURING EMERGENCY LIGHT TEST. THE BATTERY PACK WAS REMO VED AND REPLACED. 2 L 7 3 4F A3WE 1997011600181 19970116 00181 NM 1997 1 16 CALA9700046 1 19961231 A 5720 STIFFENER BOEING 737 737130 1384435 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77204 19021 INSPECTION FOUND A 2 INCH CRACK IN RT WING VERTICAL STIFFENER AT STRINGER 13R. THE STIFFENER WAS REPAIRED IAW ECRA 5710 -01773 AND IN REFERENCE TO BOEING DRAWING 65C34533. 2 L 7 2 4F A16WE 1997011600182 19970116 00182 NM 1997 1 16 CALA9700047 1 19961217 A 5315 FLOORBEAM BOEING 737 737130 1384435 NM BS 328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77204 19021 INSPECTION FOUND FLOORBEAM CORRODED AT STA 328, BL 0 TO RBL 55. A FLOORBEAM WAS FABRICATED AND INSTALLED IAW SRM 51-10- 3. 2 L 7 2 4F A16WE 1997011600183 19970116 00183 NM 1997 1 16 CALA9700048 1 19961210 A 5330 SKIN BOEING 737 737130 1384435 NM BS 745 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77204 19021 INSPECTION FOUND A 2.25 INCH CRACK IN RT FUSELAGE SKIN AT STA 745 BETWEEN STRINGERS 15R AND 16R. THE CRACKED AREA WAS R EMOVED AND A DOUBLER WAS INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A16WE 1997011600184 19970116 00184 NM 1997 1 16 CALA9700049 1 19961217 A 5511 SPAR BOEING 737 737130 1384435 NM LT HORIZ STAB TORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77204 19021 INSPECTION FOUND A 3 BY .375 INCH TEAR IN LOWER FLANGE OF LT HORIZONTAL STABILIZER FORWARD LEADING EDGE SPAR. THE TEAR WAS LOCATED THREE FEET FROM OUTBOARD EDGE. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-10-5, FI GURE 1. 2 L 7 2 4F A16WE 1997011600185 19970116 00185 NM 1997 1 16 CALA9700050 1 19961210 A 5320 SUPPORT BOEING 737 737130 1384435 NM BS 312-328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77204 19021 INSPECTION FOUND CENTER FLOORBEAM SUPPORT CORRODED UNDER PANEL NR 8 BETWEEN STA 312 AND 328. A NEW SUPPORT WAS FABRICAT ED AND INSTALLED IAW SRM 53-10-2. 2 L 7 2 4F A16WE 1997011600186 19970116 00186 NM 1997 1 16 CALA9700051 1 19961207 A 5730 SKIN BOEING 737 737130 1384435 NM LT WING CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77204 19021 INSPECTION FOUND LT WING ROOT LOWER SKIN PANEL CORRODED. THE SKIN WAS REPAIRED IAW ECRA 5730-01471. 2 L 7 2 4F A16WE 1997011600188 19970116 00188 WP 1997 1 16 9627549950 1 19961203 A 2710 CONTROL MECH DOUG DC9 DC932 3022066 WP AILERONS LACK OF LUBE A NWAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 01 9346 47376 CONTROL WHEEL REQUIRED ABOVE NORMAL FORCE TO BANK AIRCRAFT TO THE LEFT. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCID ENT. MAINTENANCE LUBED ALL PULLEYS, FAIRLEADS, AND AILERON SECTORS. NO BINDING OR FLAT SPOTS WERE NOTED. ALSO, CLEANE D GRIT FROM RIGHT WHEEL WELL PULLEYS, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1997011600203 19970116 00203 WP 1997 1 16 9627551153 1 19961219 A 5320 DOUBLER DOUG DC10 DC1040 3023508 WP BS 911.97 GOUGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 153US 46762 DURING PERIODIC CHECK, GOUGES WERE FOUND ON THE FORWARD CARGO LOWER JAMB SKIN DOUBLER AT FS 911.97. BLENDED OUT GOUGES AND INSTALLED REPAIR DOUBLER PER EA 11-120623. 2 L 7 3 4F A22WE 1997011600204 19970116 00204 WP 1997 1 16 9627561153 1 19961218 A 5320 ANGLE DOUG DC10 DC1040 3023508 WP BS 1002 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 153US 46762 DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE FORWARD CARGO JAMB ANGLE AT FS 1002, LONGERON 43R. REMOVED CORROSION AND INSTALLED REPAIR ANGLE PER EA 11-120622 (P/N ADA0233-7). 2 L 7 3 4F A22WE 1997011600205 19970116 00205 WP 1997 1 16 9627571153 1 19961216 A 5320 DOORFRAME DOUG DC10 DC1040 3023508 WP BS 1787 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 153US 46762 DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE CENTER CARGO DOOR JAMB FRAME AT FS 1787, LONGERON 43R. REMOVED CORROS ION AND INSTALLED REPAIR DOUBLERS AND SHIMS PER EA 11-120612(PN AFA3876-3). 2 L 7 3 4F A22WE 1997011600206 19970116 00206 WP 1997 1 16 9627581153 1 19961212 A 5320 MOUNTING RINGS DOUG DC10 DC1040 3023508 WP RADIO ALT ANT CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 153US 46762 DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE RADIO ALTIMETER ANTENNA MOUNTING RINGS. REMOVED CORROSION AND INSTALL ED REPAIR DOUBLER PER EA 11-120609 (P/N AYB7053-1). 2 L 7 3 4F A22WE 1997011600207 19970116 00207 WP 1997 1 16 9627591223 1 19961219 A 5400 DOUBLER DOUG DC10 DC1030 3023501 WP NR 1 PYLON CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 223NW 46580 DURING MAINTENANCE INSPECTION, A CRACK WAS FOUND IN THE NR 1 PYLON UPPER SPAR DOUBLER AT STA YN=367. REMOVED DAMAGED AR EA PER EA 12-120123 (P/N AUB7366-501). 2 L 7 3 4F A22WE 1997011600208 19970116 00208 WP 1997 1 16 9627601153 1 19961204 A 5320 SUPPORT DOUG DC10 DC1040 3023508 WP BS 475 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 153US 46762 DURING PERIODIC CHECK, THE FLOOR PANEL ATTACH TAB WAS FOUND CRACKED AT FS 475, LBL 36 FLOOR SUPPORT RAIL. REMOVED DAMAG ED AREA AND INSTALLED REPAIR CHANNEL AND FILLERS PER EA 11-105163 (P/N NCA6042-33). 2 L 7 3 4F A22WE 1997011600209 19970116 00209 WP 1997 1 16 9627621153 1 19961223 A 5532 SKIN DOUG DC10 DC1040 3023508 WP VERT STAB DELAMINATED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 153US 46762 DURING PERIODIC CHECK, DELAMINATION OF THE VERTICAL STABILIZER SKIN AT STR 375 TO 405 RIGHT SIDE. REPAIRED PER EA 11-12 0122 (P/N ANC7047-2). 2 L 7 3 4F A22WE 1997011600210 19970116 00210 WP 1997 1 16 9627631153 1 19961223 A 5330 SKIN DOUG DC10 DC1040 3023508 WP BS 1509-1531 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 153US 46762 DURING TRANSITION CHECK, CORROSION WAS FOUND ON THE UNDERWING BARREL SKIN AT FS 1509 TO 1531, LBL 49 TO RBL 49. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLERS PER EA 11-120126 (P/N AYB7065-1). 2 L 7 3 4F A22WE 1997011600211 19970116 00211 WP 1997 1 16 9627641153 1 19961220 A 5510 SUPPORT DOUG DC10 DC1040 3023508 WP LT HORIZ STAB CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 153US 46762 DURING PERIODIC CHECK, A CRACK WAS FOUND ON THE LEFT HORIZONTAL STABILIZER SECONDARY PIVOT SUPPORT. REMOVED AND REPLACE D PIVOT SUPPORT PER EA 11-120135 (P/N AJC7230-1). 2 L 7 3 4F A22WE 1997011600220 19970116 00220 WP 1997 1 16 9627611153 1 19961216 A 5313 LONGERON DOUG DC10 DC1040 3023508 WP BS 1404-1515 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 153US 46762 DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE FUSELAGE OVERWING EXTERNAL LONGERONS AT FS 1404 TO 1515. BLENDED OUT CORROSION AND INSTALLED DOUBLERS PER EA 11-120121. 2 L 7 3 4F A22WE 1997011600223 19970116 00223 WP 1997 1 16 9627651221 1 19961101 A 5730 SKIN DOUG DC10 DC1030 3023501 WP RT WING CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 221NW 46579 DURING TRANSITION CHECK, A CRACK WAS FOUND ON THE RIGHT WING FIXED LEADING EDGE SKIN AT STA XOS 610. REMOVED DAMAGED AR EA AND INSTALLED REPAIR PER EA 12-110292 (P/N ARB2887-501). 2 L 7 3 4F A22WE 1997011600224 19970116 00224 WP 1997 1 16 9627661221 1 19961105 A 5330 SKIN DOUG DC10 DC1030 3023501 WP BS 1254 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 221NW 46579 DURING PERIODIC CHECK, A CRACK WAS FOUND ON THE INNER SKIN OF THE NR 3L DOOR JAMB AT FS 1254. REMOVED DAMAGE AND INSTAL LED DOUBLER PER EA 12-120108, (P/N AEA0115-503). 2 L 7 3 4F A22WE 1997011600225 19970116 00225 WP 1997 1 16 9627671220 1 19961204 A 5751 SKIN DOUG DC10 DC1030 3023501 WP RT AILERON DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 220NW 46577 DURING LINE CHECK, DAMAGE WAS FOUND ON THE UPPER SKIN OF THE RIGHT INBOARD AILERON AT STA XIA=300. REMOVED DAMAGE AND I NSTALLED DOUBLER PER EA 12-120115, (P/N NRC6043-502). 2 L 7 3 4F A22WE 1997011600226 19970116 00226 WP 1997 1 16 9627681155 1 19961127 A 5311 FRAME DOUG DC10 DC1040 3023508 WP BS 459 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 155US 46764 DURING L-CHECK, A CRACK WAS FOUND ON THE LOWER NOSE FUSELAGE FRAME AT STA 459 AND X=61. REPAIRED PER EA 11-12013, (P/N ABA7348-3). 2 L 7 3 4F A22WE 1997011600285 19970116 00285 NM 1997 1 16 96UAL900957 1 19961223 A 2820 2790482102 FLOAT VALVE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUEL TANK FAILED A UALA K NONE J WARNING INDICATION CL CLIMB 1 WP 29 602UA 21863 DURING TAKEOFF AND CLIMB, APPROXIMATELY 800 POUNDS OF FUEL TRANSFERRED INTO THE CENTER TANK. THE INBOARD FLOAT VENT VAL VE HINGE FAILED. REPLACED THE FUEL VENT FLOAT VALVE. OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 1997011600286 19970116 00286 NM 1997 1 16 96UAL900958 1 19961223 A 2932 32143341 PRSOV BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE AIR SPLY DUCT CLOGGED A UALA K NONE J WARNING INDICATION NR NOT REPORTED 1 WP 29 607UA 72787 21868 PER CREW, UNABLE TO RAISE FLAPS WITH THE AIR DRIVEN PUMP. *S/D* THE PRESSURE REGULATOR SHUT OFF VALVE FILTER CLOGGED. REPLACED PRESSURE REGULATOR SHUT OFF VALVE AND INSTALLED A NEW NON-CLOGGING FILTER. 2 L 7 2 4F 4 F RT A1NM E3NE 1997011600287 19970116 00287 WP 1997 1 16 96UAL900959 1 19961223 A 2782 NAS13514LB8P BOLT PARKER HANNI 26280215M4 DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL SPOILER ACT SHEARED A UALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 1844U 0704 48260 HYDRAULIC FLUID STREAMING FROM NR 5 SPOILER ACTUATOR. IT APPEARS THAT ONE OF THREE BOLTS HAS SHEARED FROM THE ACTUATOR CONTROL VALVE COVER ON THE LOWER AFT PART OF THE ACTUATOR. *S/D* BOLT FAILURE AT CONTROL VALVE COVER RESULTED IN SEAL DAMAGE AND LEAKAGE. ACTUATOR REPLACED. 2 L 7 3 4F 4 F A22WE E23EA 1997011600289 19970116 00289 NM 1997 1 16 96UAL900961 1 19961223 A 3350 S106 BATTERY PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7259U 21406 RT EMERGENCY LIGHT CONTROL CIRCUIT BREAKER POPPING AND UNABLE TO RESET. *S/D* REPLACED DISCHARGED BATTERY PACK AT AFT RT SERVICE DOOR. 2 L 7 3 4F 4 F A3WE E2EA 1997011600290 19970116 00290 1997 1 16 96UAL900962 4 19961223 A 2210 YAW DAMPER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE E/E COMPT MALFUNCTIONED A A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 587UA 26713 TUNING NR 1 HF CAUSES RIGHT YAW DAMPER INOP, ACCOMPANIED WITH EICAS MESSAGE. 2 L 7 2 4F 4 F RT A2NM E17NE 1997011600291 19970116 00291 NM 1997 1 16 96UAL900963 1 19961223 A 3350 CONTACTS BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DIRTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7253U 21400 EMERGENCY LIGHT ABOVE FWD GALLEY DOOR INOPERATIVE. CLEANED DISCONNECT CONTACTS, LIGHT CHECKS OK. 2 L 7 3 4F 4 F A3WE E2EA 1997011600292 19970116 00292 NM 1997 1 16 96UAL900964 1 19961223 A 3350 LIGHT LOCTITE LUMI BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 357UA 24378 EMERGENCY EXIT LIGHTS FLOOR LIGHT DAMAGED AT 12C. REPLACED EEL LIGHT STRIP, OPS CK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 1997011600293 19970116 00293 NM 1997 1 16 96UAL900965 1 19961223 A 3350 BATTERY PACK BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 399UA 24674 EEL EMERGENCY LIGHTS ROW 3 TO 10 AND LEFT OVERWING DOOR EEL LIGHT AND SLIDE LIGHT INOP. REPLACED EEL BATTERY PACK AT LE FT OVERWING EXIT, OPS CHECK OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1997011600294 19970116 00294 1997 1 16 96UAL900966 4 19961223 A 2565 SLIDE AIR CRUISERS D28935103 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7282U 17861078 21560 SLIDE REMOVED FOR AIR CRUISERS SERVICE INFORMATION LETTER DEVELOPED AN INFLATION TUBE SEAM LEAK DURING SHOP TEST. SLIDE SCRAPPED DUE TO INFLATION TUBE SEAM LEAK. 2 L 7 3 4F 4 F A3WE E2EA 1997011600295 19970116 00295 NM 1997 1 16 96UAL900967 1 19961223 A 3350 BULB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 562UA 26664 LEFT OVERHEAD OVERWING SLIDE EMERGENCY LIGHT INOP. RELAMPED LEFT OVERWING SLIDE EMERGENCY LIGHT, OPERATION CHECKS NORMA L. 2 L 7 2 4F 4 F RT A2NM E17NE 1997011600296 19970116 00296 NM 1997 1 16 96UAL900968 1 19961224 A 3350 POWER SUPPLY BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 4735U 19928 EXIT EMERGENCY LIGHT ABOVE UPPER DECK CREW EXIT DOOR IS INOP. REPLACED BATTERY POWER SUPPLY OVER UPPER DECK EMERGENCY E XIT. 2 L 7 4 4F 4 F A20WE E20EA 1997011600297 19970116 00297 NM 1997 1 16 96UAL900969 1 19961224 A 3350 CONNECTOR LOCTITE LUMI BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 912UA 25290 FLOOR EEL STRIP NEXT TO FWD GALLEY INOP. SECURED LIGHT CONNECTION, OPS CHECK OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1997011600298 19970116 00298 NM 1997 1 16 96UAL900970 1 19961224 A 3350 LIGHT LOCTITE LUMI BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 928UA 26651 EEL STRIP AT FWD GALLEY INOP ON TEST. REPLACED LIGHT STRIP, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 1997011600300 19970116 00300 NM 1997 1 16 96UAL900972 1 19961224 A 7830 AIR GROUND SEN BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE NLG MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 9011U 19049 REVERSER ARMED LIGHT ILLUMINATED INFLIGHT WITH LANDING GEAR UP. *S/D* REPLACED EAU AND ADJUSTED NOSE AIR-GROUND SENSOR RAMP. NOSE AIR-GROUND SWITCH ADJUSTMENT CORRECTED THE PROBLEM. NO DISCREPANCY NOTED DURING EAU OPERATIONAL CHECK AT H OME SHOP. 2 L 7 2 4F 4 F A16WE E2EA 1997011600301 19970116 00301 NM 1997 1 16 96UAL900973 1 19961226 A 2120 AIR DISTR BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN ODOR A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 607UA 21868 SHORTLY AFTER TAKEOFF 3 TO 5 MINUTES, NOTICED STRONG ELECTRICAL ODORS THROUGHOUT MAIN CABIN AND COCKPIT. *S/D* INSPECT ED SEVERAL AIR CONDITIONING AND INTERIOR CABIN RELATED COMPONENTS, NO SPECIFIC DEFECTS WERE FOUND OR ABNORMAL ODORS DETE CTED. NO PRIOR HISTORY NOTED, AND NO SUBSEQUENT DISCREPANCIES HAVE OCCURRED. 2 L 7 2 4F 4 F RT A1NM E3NE 1997011600302 19970116 00302 NM 1997 1 16 96UAL900974 1 19961226 A 3250 366103 SELECTOR VALVE BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NLG STEERING CRACKED A UALA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 WP 29 4732U 19927 ON LANDING HYDRAULIC SYSTEM NR 1 QUANTITY WENT TO ZERO. PRESSURE LIGHT CAME ON FOR AIR PUMP AND ENGINE PUMP. TAXIED O FF RUNWAY AND WAS TOWED TO THE GATE DUE TO LOSS OF BODY AND NOSE LANDING GEAR STEERING. *S/D* LOSS OF HYDRAULIC FLUID WAS DUE TO CRACKED BODY/NOSE LANDING GEAR SELECTOR VALVE WHICH CAUSED THE ENGINE DRIVEN PUMP TO FAIL. REPLACED VALVE, E NGINE DRIVEN PUMP AND CASE DRAIN FILTER. 2 L 7 4 4F 4 F A20WE E20EA 1997011600303 19970116 00303 EU 1997 1 16 96UAL900975 1 19961226 A 3350 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 420UA 489 EMERGENCY LIGHTS FAILED TEST ON PTP PANEL. *S/D* RESEATED POWER SUPPLY BATTERY AND OPERATIONALLY CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 1997011600304 19970116 00304 NE 1997 1 16 96UAL900976 2 19961226 A 7532 BLEED VALVE JANITROL 04P235 BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT ENGINE CORRODED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 29 659UA 27114 727461 ABORTED TAKEOFF DUE TO LEFT ENGINE OVERTEMP. *S/D* THE 2.95 BLEED SOLENOID VALVES REMAINED OPEN AT HIGH POWER DUE TO I NTERNAL CORROSION IN THE 2.95 BLEED VALVES. THIS LED TO THE LEFT ENGINE OVER TEMP CONDITION. THESE VALVES ARE CURRENTL Y UNDERGOING AN UPGRADE TO NON-CORROSIVE MATERIAL. 2 L 7 2 4F 4 F RT A1NM E24NE 1997011600305 19970116 00305 EU 1997 1 16 96UAL900977 1 19961226 A 3350 321430 BATTERY GENERIC 321430 AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 433UA 589 EMERGENCY LIGHTS FAIL TEST. *S/D* REPLACED BATTERY IN POWER SUPPLY 10WL. 2 L 7 2 4F 4 F RT A28NM E40NE 1997011600306 19970116 00306 NM 1997 1 16 96UAL900978 1 19961226 A 2120 AIR DISTR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN SMOKE A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 341UA 24245 AFTER SHUT DOWN, FOUND SMOKE IN CABIN. RAN APU AND BOTH PACKS FOR SEVERAL HOURS. NO SMELL NOTED. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 1997011600307 19970116 00307 NM 1997 1 16 96UAL900979 1 19961226 A 2120 AIR DISTR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT SMOKING A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 341UA 24245 SMOKE IN COCKPIT USING APU. 2 L 7 2 4F 4 F RT A16WE E2GL 1997011600308 19970116 00308 NM 1997 1 16 96UAL900980 1 19961227 A 2421 GENERATOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RT ENGINE FAILED A UALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION NR NOT REPORTED 1 WP 29 767UA 26918 EN ROUTE, LOST RIGHT ENGINE DRIVEN GENERATOR. RETURNED TO MIA. 2 L 7 2 4F 4 F RT T0001SE E46NE 1997011600309 19970116 00309 NM 1997 1 16 96UAL900981 1 19961227 A 2780 SPOILERS BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LT WING OUT OF ADJUST A UALA O OTHER F FLT CONT AFFECTED DE DESCENT 1 WP 29 7272U 21419 AIRPLANE ROLLS OFF TO RIGHT EXCESSIVELY WHEN SPEED BRAKES ARE EXTENDED. *S/D* INSPECTED AIRCRAFT AND RERIGGED LEFT WIN G SPOILERS. 2 L 7 3 4F 4 F A3WE E2EA 1997011600310 19970116 00310 NM 1997 1 16 96UAL900982 1 19961227 A 2121 FAN AIRESEARCH 2075621 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LT PACK FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 7451U 21905 CREW REPORTS, SMOKE SMELL IN AIRCRAFT WITH LEFT PACK RUNNING. *S/D* REPLACED FROZEN LT PACK COOLING FAN. 2 L 7 3 4F 4 F A3WE E2EA 1997011600311 19970116 00311 NM 1997 1 16 96UAL900983 1 19961227 A 3397 58782 WIRE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7291U 21569 FAA INSPECTOR FOUND AFT EEL INDICATOR LIGHT INOPERATIVE. *S/D* REPLACED DAMAGED EEL POWER STRIP FOR AFT CABIN. 2 L 7 3 4F 4 F A3WE E2EA 1997011600312 19970116 00312 NM 1997 1 16 96UAL900984 1 19961227 A 3350 5106 BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7466U 21920 AFT GALLEY EMERGENCY LIGHT IS ON AND GETTING DIMMER. *S/D* REPLACED DISCHARGED BATTERY AND EMERGENCY LIGHT ASSEMBLY. 2 L 7 3 4F 4 F A3WE E2EA 1997011600313 19970116 00313 NM 1997 1 16 96UAL900985 1 19961227 A 3350 900835A BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7459U 21913 CEILING EMERGENCY EXIT LIGHT AT OVERWING DOOR INOPERATIVE. *S/D* REPLACED DISCHARGED BATTERY PACK. 2 L 7 3 4F 4 F A3WE E2EA 1997011600314 19970116 00314 NM 1997 1 16 96UAL900986 1 19961227 A 3510 SST2S CLAMP BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE F/O SEAT LOOSE A UALA K NONE O OTHER NR NOT REPORTED 1 WP 29 7466U 21920 FIRST OFFICER'S OXYGEN DOES NOT STOP OR SHUTOFF IN EMERGENCY. AIRCRAFT TO BE FERRIED TO ORD FOR REPAIR. *S/D* RESECUR ED CLAMP ON F/O OXYGEN HOSE AT CREW DEMAND REGULATOR. 2 L 7 3 4F 4 F A3WE E2EA 1997011600315 19970116 00315 NM 1997 1 16 96UAL900987 1 19961227 A 5754 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 5 LE FLAP CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7450U 21904 NR 5 LEADING EDGE SLAT LOWER SKIN CRACK. *S/D* INSPECTED SLAT AND FOUND THREE ADDITIONAL CRACKS ON LOWER SKIN ATTACH A NGLE. STOP DRILLED ALL CRACKS AND SECURED AREA. 2 L 7 3 4F 4 F A3WE E2EA 1997011600316 19970116 00316 WP 1997 1 16 96UAL900988 1 19961227 A 2910 AYK7002582 TUBE ASSY DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL RT MLG WW CRACKED A UALA O OTHER K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 WP 29 1814U 46613 HYDRAULIC FLUID SPRAYING FROM LINE IN RIGHT WHEEL WELL WITH NR 3 SYSTEM PRESSURIZED. *S/D* BRAKE RETURN LINE CRACKED. SPLICED IN A NEW SECTION OF LINE USING RYNGLOK METHOD. 2 L 7 3 4F 4 F A22WE E23EA 1997011600317 19970116 00317 WP 1997 1 16 96UAL900989 1 19961227 A 2910 29169071 SEAL DOUGLAS AIRC AGY79155001 DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL HYD SYSTEM TORN A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 1847U AOR027 48263 LOST NR 2 HYDRAULIC QUANTITY. RETURNED TO ORD. *S/D* POPPET VALVE O-RING ON RESERVOIR RELIEF AND SAMPLING VALVE FAILE D RELEASING HYDRAULIC FLUID OVERBOARD. REPLACED VALVE. 2 L 7 3 4F 4 F A22WE E23EA 1997011600318 19970116 00318 NM 1997 1 16 96UAL900990 1 19961227 A 2121 FAN JOY 5007024620 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN FAILED A UALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 7297U AA77773 21892 ODOR LIKE SMOKE REPORTED IN MID-CABIN BY FLIGHT ATTENDANTS DURING PUSH BACK. ODOR DISSAPATED BUT REOCURRED DURING TAXI OUT. RETURNED TO GATE. *S/D* UPSTREAM INLET CHECK VALVE DESTROYED CAUSING GASPER FAN TO INGEST PARTS. REPLACED GASPE R FAN AND CHECK VALVE. 2 L 7 3 4F 4 F A3WE E2EA 1997011600319 19970116 00319 NM 1997 1 16 96UAL900991 1 19961227 A 3350 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 387UA 24662 EMERGENCY LIGHT IS INOPERATIVE ABOVE ROW 9C. 2 L 7 2 4F 4 F RT A16WE E2GL 1997011600320 19970116 00320 NM 1997 1 16 96UAL900992 1 19961230 A 2510 S906709037 TRANSFORMER BOEING 285W00122 BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE COCKPIT FAILED A UALA F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 773UA D00029 26929 CABIN CONTROL PANEL 4R SMOKING. USED TWO HALON BOTTLES TO EXTINGUISH SMOKE. *S/D* MULTIPLE COMPONENT FAILURES WITHIN THE CACP TXFMR T961, BACKLIGHT NR 2 BOTH FILAMENTS OPEN, POWER SUPPLY HEATER RESISTORS R995, R996, R997 AND R998 AND ASS OCIATED CIRCUIT TRACES BURNED. PREVIOUS HISTORY ON CACP UNITS INDICATED OVERHEAT COULD RESULT ONLY IF BOTH BACKLIGHTS F AILED OPENED. THIS UNIT FAILED WITH ONLY ONE LIGHT OUT. MAINTENANCE TIP PUBLISHED TO PULL AND COLLAR THE CACP CIRCUIT BREAKER WHEN A BACKLIGHT FAILS AND REPLACEMENT NOT AVAILABLE. BOEING STILL INVESTIGATING. 2 L 7 2 4F 4 F RT T0001SE E46NE 1997011600321 19970116 00321 WP 1997 1 16 96UAL900993 1 19961230 A 2910 APK7002532 TUBE ASSY DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL LT MLG WW CRACKED A UALA O OTHER K FLUID LOSS IN INSP/MAINT 1 WP 29 1817U 46616 LT WHEEL WELL OUTBOARD FORWARD SIDE HYDRAULIC LINE LT BRAKE RETURN LINE SYSTEM 3 CRACKED WHERE LINE GOES INTO WING ROOT. *S/D* CRACK IN TUBE ASSEMBLY. SPLICED IN NEW SECTION OF TUBE USING RYNGLOK SPLICE METHOD. 2 L 7 3 4F 4 F A22WE E23EA 1997011600323 19970116 00323 NM 1997 1 16 96UAL900995 1 19961230 A 2710 CONTROL WHEEL BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LT/RT COCKPIT LACK OF LUBE A UALA O OTHER F FLT CONT AFFECTED TO TAKEOFF 1 WP 29 7292U 21570 TAKEOFF WITH 5 DEGREE FLAPS AILERON CONTROL VERY STIFF TO THE RIGHT WITH 'A' SYSTEM PRESSURE, NORMAL TO THE LEFT. *S/D* LUBED CAPTAINS AND FIRST OFFICERS CONTROL WHEEL YOKE SPADES. CYCLED CONTROL WHEEL TO WORK IN LUBRICANT. CONTROL WHEE L OPERATES SMOOTHLY. 2 L 7 3 4F 4 F A3WE E2EA 1997011600324 19970116 00324 NM 1997 1 16 96UAL900996 1 19961230 A 5320 STRIP BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CARGO COMPT BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7254U 21401 AFT CARGO PIT FLOOR PANEL JOINING METAL STRIP IS BROKEN AND CORRODED. *S/D* FLOOR PANEL REMOVED AND STRUCTURE BELOW IN SPECTED FOR CORROSION, NONE FOUND. FLOOR PANEL REINSTALLED AND METAL STRIP REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 1997011600325 19970116 00325 NM 1997 1 16 96UAL900997 1 19961230 A 3350 BATTERY PACK BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE RT WING TE DISCHARGED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 974UA 21597 EMERGENCY LIGHT AT THE TRAILING EDGE OF THE RT WING IS INOP. RELAMPED AND REPLACED BATTERY, OPS CHECK OK. 2 L 7 2 4F 4 F A16WE E2EA 1997011600326 19970116 00326 NM 1997 1 16 96UAL900998 1 19961230 A 3350 LENS BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE DOOR 2L EEL LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 9051U 19932 EMERGENCY EXIT LIGHT LENS COVER LOOSE DOOR 2L. SECURED EMERGENCY EXIT LIGHT LENS COVER. 2 L 7 2 4F 4 F A16WE E2EA 1997011600327 19970116 00327 NM 1997 1 16 96UAL900999 1 19961230 A 3350 BULB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 591UA 28142 RIGHT EXTERIOR OVERWING EMERGENCY EGRESS LIGHT INOP. RELAMPED RIGHT OVERWING EMERGENCY EGRESS LIGHT, OPERATION CHECKS N ORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1997011600328 19970116 00328 NM 1997 1 16 96UAL901000 1 19961230 A 3350 BATTERY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 575UA 26689 CEILING EMERGENCY EGRESS LIGHTING AT OVERWING POSITION INOP. REPLACED BATTERY PACK, OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1997011600329 19970116 00329 WP 1997 1 16 96UAL901001 1 19961230 A 5720 ARB2363501 FAIRING DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL RT WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 1849U 46939 FAIRING ON THE RIGHT WING LOWER SURFACE INBOARD OF NR 3 PYLON BETWEEN WING STATION XORS-270 AND XORS-305 FORWARD OF THE FRONT SPAR, OUTBOARD OF ACCESS OPENING NR 616GB HAS A 12 INCH CRACK. IT BEGINS APPROXIMATELY 6 AFT OF LEADING EDGE OF U NFASTENED SIDE OF FAIRING AND RUNS ACROSS TO THE FASTENERS. IT THEN TRAVELS THROUGH 6 FASTENER HOLES AFT, FAIRING DIMEN SION 24 BY 4. REPLACED FAIRING PANEL. 2 L 7 3 4F 4 F A22WE E23EA 1997011600330 19970116 00330 NM 1997 1 16 96UAL901002 1 19961231 A 2560 11611 EVACUATION SLIDE BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE DOOR 1L LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 9075U 19956 THE NR 1 LEFT DOOR SLIDE PRESSURE READS AT THE BOTTOM OF THE GREEN BAND. *S/D* BOTTLE WAS COLD SOAKED CAUSING A FALSE LOW PRESSURE INDICATION. 2 L 7 2 4F 4 F A16WE E2EA 1997011600331 19970116 00331 WP 1997 1 16 96UAL901003 1 19961231 A 3397 S9191 WIRE DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1845U 48261 SECTION OF EEL INOPERATIVE AT ROWS 19 AND 20. *S/D* FLEX JUMPER OPEN. REPLACED JUMPER. 2 L 7 3 4F 4 F A22WE E23EA 1997011600332 19970116 00332 NM 1997 1 16 96UAL901004 1 19961231 A 3610 BLEED AIR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LEFT MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 361UA 24454 AFTER TAKEOFF, LEFT BLEED TRIPPED OFF. 2 L 7 2 4F 4 F RT A16WE E2GL 1997011600333 19970116 00333 NM 1997 1 16 96UAL901005 1 19961231 A 2613 OVERHEAT LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RT WING ILLUMINATED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 366UA 24535 RIGHT WING-BODY OVER HEAT LIGHT ILLUMINATED. ACCOMPLISHED DUCT LEAK CHECK IN RIGHT WING-BODY AREA. OPS CHECK NORMAL. N O SUBSEQUENT OCCURRENCES. 2 L 7 2 4F 4 F RT A16WE E2GL 1997011600346 19970116 00346 SO 1997 1 16 SRAA960103 1 19960106 A 5230 SKIN LKHEED 382 382E 526413U SO CARGO DOOR PUNCTURED A SRAA O OTHER O OTHER IN INSP/MAINT 1 GL 23 923SJ 4301 DURING ROUTINE MAINTENANCE, FOUND 2 HOLES PUNCTURED THROUGH CARGO DOOR SKIN AT APPROX FS STA 920. HOLES MEASURED APPROX 2 WIDE, ACCOMPLISHED REPAIR IAW LOCKHEED SRM 51-140-12. 2 H 7 4 4T A1SO 1997011600347 19970116 00347 EU 1997 1 16 97ZZZX280 1 19960516 A 5400 RIB BAG BAE146 BAE146200A 1500266 EU NR 2 PYLON CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 293UE E2097 ATW - NR 2 PYLON CENTER BOX BETWEEN RIBS 3 AND 4 HAS A CRACK ON THE LOWER FLANGE OF RIB NR 4 THAT IS APPROXIMATELY .4375 INCH LONG. CORRECTIVE ACTION: NR 2 PYLON RIB NR 4 CRACK HAS BEEN REPORTED TO AVRO RDO AND IS ACCEPTABLE FOR SERVICE P ER RIL HC546H9018. GENERATED W/C FOR REINSP. 2 H 7 4 4F RT A49EU 1997011600348 19970116 00348 EU 1997 1 16 97ZZZX281 1 19960514 A 5320 ANGLE BAG BAE146 BAE146200A 1500266 EU CARGO COMPT CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 293UE E2097 ATW - FREIGHT ANGLE AT FRAME 36 REAR CARGO BAY IS CRACKED AND CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED CRACKE D AND CORRODED FREIGHT ANGLE LOCATED AT FRAME 36 IN REAR CARGO BAY. 2 H 7 4 4F RT A49EU 1997011600349 19970116 00349 EU 1997 1 16 97ZZZX282 1 19960516 A 5400 RIB BAG BAE146 BAE146200A 1500266 EU NR 4 PYLON CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 293UE E2097 ATW - NR 4 PYLON CENTERBOX BETWEEN RIBS 3 AND 4 HAS A CRACK IN LOWER FLANGE OF RIB 4 THAT IS APPROXIMATELY .3125 INCH LO NG HAS BEEN REPORTED TO AVRO BAE RDO AND IS ACCEPTABLE FOR SERVICE PER RIL HC546H9018. GENERATED W/C FOR REINSP. 2 H 7 4 4F RT A49EU 1997011600350 19970116 00350 EU 1997 1 16 97ZZZX283 1 19960521 A 5330 SKIN BAG BAE146 BAE146200A 1500266 EU FUSELAGE DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 293UE E2097 ATW - C/W A PERMANENT REPAIR TO DENT IN RT FUSELAGE LOCATED 6 INCHES FORWARD OF FRAME 21 AND 51 INCHES BELOW SKIN LAP JO INT. REPORTED CLASS 'A' DAMAGE X=1.812 INCH, D=.032 INCH. CORRECTIVE ACTION: REPAIRED IAW SRM 53-00-12, PAGES 206-208 , AND AVRO FAX REF JM/RJ606-96. SCANNED AREA AFTER DAMAGE WAS REMOVED USING ET PER AWAC NDT SPEC TO ASSURE IT IS CRACK FREE. NO INDICATIONS NOTED AT THIS TIME, 5-20-96. 2 H 7 4 4F RT A49EU 1997011600351 19970116 00351 EU 1997 1 16 97ZZZX284 1 19960523 A 2710 CABLES BAG BAE146 BAE146200A 1500266 EU AILERON OUT OF ADJUST A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 293UE E2097 ATW - AILERON INTERCONNECT CABLES WORN AT THE RIGHT SIDE FUSELAGE PRESSURE SEALS. CORRECTIVE ACTION: REMOVED AND REPLA CED AND ADJUSTED INTERCONNECT CABLES IAW BAE MM 27-11-44 AND 00. GENERATED W/C TO C/W AILERON CONTROLS CK. 2 H 7 4 4F RT A49EU 1997011600352 19970116 00352 EU 1997 1 16 97ZZZX285 1 19960524 A 5330 SKIN BAG BAE146 BAE146200A 1500266 EU LT MLG DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 293UE E2097 ATW - PERMANENT REPAIR TO BE C/W ON LT FORWARD MLG FAIRING ZONE 725 AND DIAPHRAM DUE IN 1800 CYCLES AT 16005 CYC PER AW FAX'S LM/100-95, LM/101-95, LM/102-95 AND BAE FAX JM/RJ1321-95 =1=HC535H0040-200U, SKIN. CORRECTIVE ACTION: REPLACE LT FORWARD MLG FAIRING SKIN PANEL, DIAPHRAM AND CAMLOC ATTACH BRACKET JUST FORWARD OF PANEL 725BB. 2 H 7 4 4F RT A49EU 1997011600353 19970116 00353 1997 1 16 97ZZZX286 4 19960930 A 2565 D31050103 SLIDE BAG BAE146 BAE146200A 1500266 EU PAX DOOR NOT CHARGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 608AW 15551 0397 E2049 ATW - FLT 514 - FA REPORTS THAT THE RIGHT FORWARD PASSENGER DOOR EVACUATION SLIDE CHARGE IS IN THE RED. CORRECTIVE ACTI ON: REMOVED AND REPLACED EVAC SLIDE, CHECKS BAD, GENERATED W/C FOR CONTINUATION OF MAINTENANCE. S/N OFF: 0397. S/N O N: 0627. 2 H 7 4 4F RT A49EU 1997011600354 19970116 00354 EU 1997 1 16 97ZZZX287 1 19960813 A 5530 BOLTS BAG BAE146 BAE146300A 1500267 EU VERT STAB CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 VERTICAL STABILIZER TRAILING EDGE; TOP AND CENTER HINGE BOLTS HAVE INDICATIONS OF CORROSION. REMOVED FOR DV. CORRECTIV E ACTION: REMOVED, CLEANED, AND INSTALLED VERTICAL STABILIZER TO RUDDER, TOP, AND CENTER HINGE BOLTS. NO CORROSION NOT ED ON BOLTS. 2 H 7 4 4F RT A49EU 1997011600355 19970116 00355 EU 1997 1 16 97ZZZX288 1 19960809 A 5320 GUSSET BAG BAE146 BAE146300A 1500267 EU FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 CENTER GUSSET PLATES ON INTERCOSTALS IN FORWARD VEST AREA ARE CORRODED. NEED REPLACEMENT. CORRECTIVE ACTION: REMOVED AND REPLACED GUSSET PLATES ON CENTER INTERCOSTALS CENTER PLATES IN FORWARD VEST AREA. 2 H 7 4 4F RT A49EU 1997011600356 19970116 00356 EU 1997 1 16 97ZZZX289 1 19960809 A 5320 GUSSET BAG BAE146 BAE146300A 1500267 EU FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 GUSSET PLATE ON FRAME 15 AFT OF GALLEY IS CORRODED TO LIMITS. NEEDS TO BE REPLACED. CORRECTIVE ACTION: REMOVED AND RE PLACED GUSSET PLATE ON FRAME 15 AFT OF GALLEY. 2 H 7 4 4F RT A49EU 1997011600357 19970116 00357 EU 1997 1 16 97ZZZX290 1 19960809 A 5320 GUSSET BAG BAE146 BAE146300A 1500267 EU FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 GUSSET PLATE ON FRAME 18 IS CORRODED TO LIMITS. NEEDS TO BE REPLACED. CORRECTIVE ACTION: REMOVED AND REPLACED GUSSET PLATE ON FRAME 18. 2 H 7 4 4F RT A49EU 1997011600358 19970116 00358 EU 1997 1 16 97ZZZX291 1 19960809 A 5210 SUPPORT PLATES BAG BAE146 BAE146300A 1500267 EU AIRSTAIR CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 FORWARD AIRSTAIR AFT SUPPORT PLATES BEHIND AIRSTAIR RAILS ARE CORRODED, NEED REPLACEMENT. CORRECTIVE ACTION: DOWTY MAD E PART. REMOVED AND REPLACED FORWARD AIRSTAIR AFT SUPPORT PLATES. 2 H 7 4 4F RT A49EU 1997011600359 19970116 00359 EU 1997 1 16 97ZZZX292 1 19960808 A 2760 BOLT BAG BAE146 BAE146300A 1500267 EU RT SPOILER NOT PLATED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 RIGHT INBD LIFT SPOILER AFT JACK ATTACHMENT BOLT, PLATING MISSING. CORRECTIVE ACTION: INSTALLED NEW JACK ATTACHMENT BO LT. 2 H 7 4 4F RT A49EU 1997011600360 19970116 00360 EU 1997 1 16 97ZZZX293 1 19961026 A 3530 4566M37B PBE BAG BAE146 BAE146300A 1500267 EU CABIN MALFUNCTIONED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 616AW E9445482 E3145 DEN - FLT 580 - PLEASE INSPECT TOP FORWARD CABIN PBE FOR SERVICEABILITY. CORRECTIVE ACTION: REMOVED AND REPLACED PBE T OP FORWARD CABIN. S/N OFF E9445482. S/N ON V8916022. 2 H 7 4 4F RT A49EU 1997011600361 19970116 00361 EU 1997 1 16 97ZZZX294 1 19961014 A 2760 3799H1 SERVO VALVE BAG BAE146 BAE146200A 1500266 EU AIR BRAKES MALFUNCTIONED A A6WA O OTHER J WARNING INDICATION CR CRUISE 1 GL 31 609AW 12180 FYH165948 E2070 ATW - FLT 509 - AIR BRAKE OPENED DURING CRUISE WITHOUT BEING SELECTED. CORRECTIVE ACITON: REMOVED AND REPLACED AIRBRAK E SERVO VALVE, OPS TEST GOOD, LEAK CHECKS GOOD. S/N OFF: FYH165948. S/N ON FHY144505. 2 H 7 4 4F RT A49EU 1997011600362 19970116 00362 EU 1997 1 16 97ZZZX295 1 19961018 A 2750 RETRACT MECH BAG BAE146 BAE146300A 1500267 EU TE FLAPS MALFUNCTIONED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 616AW E3145 ORD - FLT 528 - AFTER TAKEOFF DURING CLIMB-OUT OF ORD, FLAPS WOULD NOT RETRACT FROM 18 DEGREES. FLAP FAULT AND INOP CAP TIONS ILLUMINATED. AIRCRAFT RETURNED TO ORD. CORROECTIVE ACTION: PERFORMED CLEARING PROCEDURE AND SAFETY LANE 2 CHECK S. OPS CHECKS NORMAL. 2 H 7 4 4F RT A49EU 1997011600363 19970116 00363 EU 1997 1 16 97ZZZX296 1 19960808 A 2760 BOLT BAG BAE146 BAE146300A 1500267 EU SPOILER CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 RT OTBD LIFT SPOILER INBD HINGE BOLT SCRAPED DUE TO CORROSION AROUND THREADS 2 H 7 4 4F RT A49EU 1997011600364 19970116 00364 EU 1997 1 16 97ZZZX297 1 19961028 A 2760 806002 CIRCUIT BOARD BAG BAE146 BAE146200A 1500266 EU E/E BAY FAILED A A6WA O OTHER N FALSE WARNING LD LANDING 1 GL 31 607AW 19054 91136 E2052 DEN - FLT 584 - ON LANDING ROLL-OUT, MAN. SPLR. FAULT AND GREEN FAIL LIGHTS ILLUM. YEL SPLR DEPLOYED. CORRECTIVE ACTIO N: REF W.C. NR 10 FOR WORK PERFORMED. OHMED WIRES FROM GA42 AND GA43 TO AND THROUGH SQUAT SWTICHES. CYCLED GEAR DURIN G OHM CHECK. TESTED SYS FOR PROPER OPS AND NO FAULT FOUND. RMEOVED AND RPELACED PCB GA42 AND GA43 AND RELAY GA19 FOR P RECAUTION TIS. SYS TESTED GOOD. S/N OFF: 119488/91136. S/N ON: 109661/117011. 2 H 7 4 4F RT A49EU 1997011600365 19970116 00365 EU 1997 1 16 97ZZZX298 1 19961028 A 2760 806002 CIRCUIT BOARD BAG BAE146 BAE146200A 1500266 EU E/E/ BAY FAILED A A6WA O OTHER N FALSE WARNING LD LANDING 1 GL 31 607AW 12818 119488 E2052 DEN - FLT 584 - ON LANDING ROLL-OUT, MAN. SPLR. FAULT AND GREEN FAIL LIGHTS ILUM. YEL SPLR DEPLOYED. CORRECTIVE ACTION : REF W.C. NR 10 FOR WORK PERFORMED. OHMED WIRES FROM GA42 AND GA43 TO AND THROUGH SQUAT SWITCHES. CYCLED GEAR DURING OHM CHECK. TESTED SYS FOR PROPER OPS AND NO FAULT FOUND. REMOVED AND REPLACED PCB GA42 AND GA43 AND RELAY GA19 FOR PR ECAUTION TIS. SYS TESTED GOOD. S/N OFF: 119433/91136. S/N ON: 109661/117011. 2 H 7 4 4F RT A49EU 1997011600366 19970116 00366 EU 1997 1 16 97ZZZX299 1 19961002 A 2150 PACK BAG BAE146 BAE146200A 1500266 EU NR 1 ODOR A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 31 610AW E2082 NR 1 PACK SMELLS 'OILY' AND CAUSES A HAZE IN CABIN, IF ALLOWED TO REACH 40 DEGREES CELSIUS. CORRECTIVE ACTION: RAN NR 1 PACK PER DUCT CLEARING PROCEDURE MM, REF 49-50-00. NO 'OIL' SMELL OR HAZE NOTED DURING PROCEDURE. 2 H 7 4 4F RT A49EU 1997011600367 19970116 00367 EU 1997 1 16 AALA961744 1 19961130 A 3260 201251225 SENSOR FOKKER F28 F28MK0100 4990807 EU LT MLG DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 1450A 11459 MSP - FLT T0787 - AFTER TAKEOFF MSP, UNABLE TO RETRACT LANDING GEAR. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDE NT. REPLACED LT NR 3 GROUND/FLIGHT SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2 L 7 2 4F RT 1997011600368 19970116 00368 EU 1997 1 16 AALA961745 1 19961129 A 3260 CONTROL UNIT FOKKER F28 F28MK0100 4990807 EU E/E BAY TRIPPED A AALA O OTHER O OTHER CL CLIMB 1 SW 07 1450A 11459 MSP - FLT T1140 - AFTER TAKEOFF ORD, GROUND/FLIGHT CONTROL DID NOT SWITCH TO FLIGHT. GEAR OVERRIDE BUTTON REQUIRED TO R AISE LANDING GEAR. AIRCRAFT PROCEEDED TO MSP AND LANDED WITHOUT INCIDENT. RERACKED LANDING GEAR PROXIMITY SWITCH CONTR OL UNIT. CHECKED AND CLEANED LANDING GEAR PROXIMITY CONTROL UNIT SENSORS AND SENSOR WIRING. ACCOMPLISHED BITE CHECK OF LANDING GEAR PROXIMITY SWITCH CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2 L 7 2 4F RT 1997011600369 19970116 00369 NM 1997 1 16 AALA961492 1 19961007 A 3350 A3060698101 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 685AA 25342 DFW - DURING OVERNIGHT CHECK, FOUND EMERGENCY FLOOR LIGHTS BY AFT RT LAVATORY INOPERATIVE. RESECURED LOOSE EMERGENCY FL OOR LIGHT STRIP CONNECTOR BY AFT RT LAVATORY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1997011600370 19970116 00370 EU 1997 1 16 97ZZZX300 1 19961120 A 3260 SWITCH STBROS SD3 SD360 8100606 EU NLG OUT OF ADJUST A GUUA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 SO 19 264GA SH3756 TPA/MIA - FLT 3408A - PILOT REPORT: NOSE GEAR RED INTRANSIT. LIGHT DOES NOT ILLUMINATE. CORRECTIVE: ADJUSTED NOSE GE AR DOWNLOCK MICROSWITCH. OPS CHECK GOOD ON RETRACTION AND EXTENSION. (X) 2 H 7 2 4T A41EU 1997011600371 19970116 00371 EU 1997 1 16 97ZZZX301 1 19961125 A 3260 UNSAFE IND STBROS SD3 SD360 8100606 EU NLG INOPERATIVE A GUUA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 SO 19 264GA SH3756 TPA/MIA - FLT 437A - PILOT REPORT: NOSE WHEEL UNSAFE INDICATOR INOPERATIVE. CORRECTIVE: REMOVED AND REPLACED NOSE GEA R INDICATOR LAMPS. (X) 2 H 7 2 4T A41EU 1997011600372 19970116 00372 EU 1997 1 16 97ZZZX302 1 19961126 A 3260 GEAR LIGHT STBROS SD3 SD360 8100606 EU NLG FLICKERS A GUUA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 19 264GA SH3756 MCO/MIA - FLT 3396 - PILOT REPORT: NOSE GEAR GREEN LIGHT FLICKERS ON AND OFF WITH GEAR DOWN. CORRECTIVE: COULD NOT DU PLICATE ON GROUND. 2 H 7 2 4T A41EU 1997011600373 19970116 00373 EU 1997 1 16 97ZZZX303 1 19961127 A 3260 WIRE STBROS SD3 SD360 8100606 EU NLG BROKEN A GUUA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 SO 19 264GA SH3756 TPA/MIA - FLT 3408A - PILOT REPORT: NOSE GEAR RED INTRANSIT, INOPERATIVE. LIGHT BULB TEST OK. CORRECTIVE: REPAIRED B ROKEN TERMINAL AT UPLOCK TERMINAL BOARD. 2 H 7 2 4T A41EU 1997011600374 19970116 00374 CE 1997 1 16 97ZZZX304 1 19961202 A 3297 WIRE BEECH 1900 1900C 1154161 CE LANDING GEAR SHORTED A GUUA O OTHER J WARNING INDICATION AP APPROACH 1 SO 19 154GA UB25 MIA/MCO - FLT 487 - PILOT REPORT: LANDING GEAR RELAY CIRCUIT BREAKER TRIPPED. GEAR HAD TO BE MANUALLY EXTENDED. CORRE CTIVE: REPAIRED SHORTED WIRING. 2 L 7 2 4T RT A24CE 1997011600375 19970116 00375 NM 1997 1 16 97ZZZX305 1 19961213 A 3350 900542 BATTERY PACK BOEING 727 727251 138408H NM CABIN DISCHARGED A SQ7A K NONE L NO TEST IN INSP/MAINT 1 SO 01 282US 630 21161 FORWARD EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK (CHARGER RACK). CHECKED GOOD 33-50. 2 L 7 3 4F A3WE 1997011600376 19970116 00376 NM 1997 1 16 W8PA960173 1 19961202 A 3397 WIRE BOEING 737 737317 138447P NM CABIN LOOSE A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 946WP 23173 FOUND EMERGENCY FLOOR TRACK LIGHTING ONLY PARTIALLY ILLUMINATED. ROWS 1 TO 10 INOPERATIVE. REPLACED BATTERY PACK. (X) 2 L 7 2 4F RT A16WE 1997011600377 19970116 00377 CE 1997 1 16 NSVA96005 1 19961127 A 3260 404EN16 DOWNLOCK SWITCH 1148100231 BEECH 1900 1900C 1154161 CE RT MLG FAILED A NSVA L ABORTED APPROACH N FALSE WARNING LD LANDING 1 EA 27 550CJ EAS1451 UC50 RIGHT MAIN GEAR GREEN DOWN AND LOCK ANNUNCIATOR WILL NOT ILLUMINATE. SELF-TEST FUNCTION GOOD. TROUBLESHOT POSITION AND WARNING SYSTEM, REPLACED OPEN DRAG BRACE DOWN AND LOCK SWITCH. CYCLED GEAR SEVERAL TIMES, SYSTEM CHECK GOOD. (X) 2 L 7 2 4T RT A24CE 1997011600378 19970116 00378 EU 1997 1 16 SIMA963521 1 19961217 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 282AE 17158 340B282 ORD - FLT 4255 - REPLACED TWO EMERGENCY POWER SUPPLIES, ONE IN FRONT OF SEAT 1, AND BETWEEN SEATS 2 AND 3 IN CENTER ISLE . AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1997011600379 19970116 00379 WP 1997 1 16 97ZZZX306 1 19961213 A 6210 369D21100 BLADE HUGHES 369 369E 4470707 WP M/R CRACKED A MLTA K NONE O OTHER IN INSP/MAINT 1 NM 09 161W 763 009999H994 0319E PILOT NOTICED A STRANGE NOISE DURING SHUT DOWN. UPON INSPECTION OF THE AIRCRAFT, HE FOUND THAT M/R BLADE S/N 009999-H99 4 HAD A CRACK ON BOTH THE TOP AND BOTTOM SKINS 15.75 INCH FROM THE DAMPER BRG CASTING. THE AIRCRAFT HAD BEEN IN 18 HRS B EFORE WITH A VERTICAL PROBLEM, BUT WE WERE ABLE TO CHANGE A COUPLE OF BELLCRANKS AND TRACK THE MAIN ROTOR AND MAKE THE A IRCRAFT SMOOTH AGAIN. AIRCRAFT HAS BEEN DOING XMAS TREES FOR JUST UNDER 300 HRS. 1 G 7 1 3U H3WE 1997011600390 19970116 00390 NM 1997 1 16 9627692768 1 19961230 A 3320 LIGHT BOEING 727 7272M7 138407S NM CABIN LOOSE A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 729RW 21741 DURING CLIMB, A LOUD CRACKING NOISE WAS HEARD BY THE FLIGHT ATTENDANT IN THE AFT CABIN BETWEEN THE RIGHT AND LEFT LAVATO RIES, AFT GALLEY FLOOR BECAME WARM IN SPOTS. AIRCRAFT DIVERTED TO MSP AND LANDED WITHOUT INCIDENT. PRESSURIZED AIRCRAF T WITH ALL BLEED SOURCES, NO TROUBLE FOUND. INSPECTED INLET/EXHAUST, ALL THREE ENGINES, NO TROUBLE FOUND. INSPECTED CE ILING BETWEEN REAR LAVATORIES, FOUND LIGHT ASSEMBLY LOOSE. SECURED AND CHECKED CARGO HEAT DUCTING SYSTEM. 2 L 7 3 4F A3WE 1997011600417 19970116 00417 NM 1997 1 16 DL733970036 1 19961210 A 5755 65C2524216A FITTING BOEING 737 737347 1384647 NM GROUND SPOILER CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 305WA 23346 THE INBOARD ACTUATOR FITTING HAS FAILED ON THE INBOARD GROUND SPOILER. THE SPOILER ACTUATOR FITTING WILL BE REPAIRED PE R S/B 737-57-1207. 2 L 7 2 4F RT A16WE 1997011600418 19970116 00418 NM 1997 1 16 DL72S970037 1 19961212 A 5330 65545906 SKIN BOEING 727 727232 1384082 NM RAM AIR DOOR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 532DA 22045 CORROSION WAS FOUND IN THREE AREAS AROUND THE RAM AIR ACTUATOR ACCESS DOOR. THE DAMAGED AREAS MEASURE 3.5 BY 4.375 IN T HE AFT RT CORNER, 7.375 BY 3.625 ON THE FWD LT SIDE AND 3.5 BY 4.75 ON THE AFT LT SIDE. THE DAMAGE WAS REPAIRED WITH TI TANIUM DOUBLERS AND APPROVED BY FAA FORM 8110-3 DER DESIGNATION SO-831, DTD 19, DEC 1996. 2 L 7 3 4F A3WE 1997011600419 19970116 00419 NM 1997 1 16 DL72W970038 1 19961214 A 5312 6516350 BLKHD STIFFENER BOEING 727 727247 138408F NM BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2817W 20873 A CRACK WAS FOUND IN THE VERTICAL STIFFENER AT LBL 36.83 ON THE FWD SIDE OF THE BS 1183 BULKHEAD. THE CRACK WAS APPROX 1.75 LONG AT WL 237. THE STIFFENER WAS REPAIRED PER BOEING S/B 727-53-0192. 2 L 7 3 4F A3WE 1997011600420 19970116 00420 NM 1997 1 16 DL72W970039 1 19961218 A 5320 BOLT BOEING 727 727247 138408F NM STRIINGER 3A SHEARED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2813W 20869 THE INBOARD TENSION TIE BOLT AT LT S-3A WAS FOUND SHEARED. THE BOLT WAS REPLACED AND THE TENSION TIE FITTING INSPECTED IN ACCORDANCE WITH S/B 727-53-0178, REV 2. 2 L 7 3 4F A3WE 1997011600421 19970116 00421 NM 1997 1 16 DL73E970040 1 19961216 A 5320 INTERCOSTAL BOEING 737 737247 138448D NM BS 328 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 376DL 23603 FOUND CRACK IN THE R1 DOOR FRAME INTERCOSTAL AT STR 8A. REPAIRED IN ACCORDANCE WITH S/B 737-53A1108 AND AD 88-03-03. 2 L 7 2 4F A16WE 1997011600424 19970116 00424 NM 1997 1 16 DL72S970043 1 19961224 A 5400 ANGLE BOEING 727 727232 1384082 NM NR 2 ENGINE WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 406DA 21150 FOUND THE LWR LIP OF FWD COWL SUPPORT ANGLE WORN AT THE NR 2 ENG FIREWALL. THE DAMAGE WAS REMOVED AND A NEW FRAME DRILL ED AND INSTALLED PER SRM 53-11-0, PG 801. 2 L 7 3 4F A3WE 1997011600433 19970116 00433 WP 1997 1 16 SRAA970106 1 19961209 A 3350 5165741 BATTERY PACK LKHEED 1011 10113851 5265010 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 783DL 193A1009 AIRCRAFT EMERGENCY LIGHTS AT L-1 AND R-1 DOORS INOP. REPLACED THE AIRCRAFT BATTERY PACKS AT L-1 AND R-1. 2 L 7 3 4F A23WE 1997011600520 19970116 00520 NE 1997 1 16 PLGA9612201 2 19961220 A 7260 CHIP LIGHT SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT ENGINE ILLUMINATED A PLGA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NE 05 356BE 340B275 BOS - FLT 4524 - EN ROUTE TO LEB FROM BOS, THE LT ENGINE CHIP LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO BOS LANDING W ITHOUT INCIDENT. MAINTENANCE INSPECTED THE OIL FILTER, SCAVENGE SCREENS AND CHIP DETECTOR AND DETERMINED THAT THE MATER IAL FOUND WAS WITHIN ALLOWABLE LIMITS. MAINTENANCE PERFORMED A SUCCESSFUL PENALTY RUN AND RETURNED THE AIRCRAFT TO SERV ICE. (X) 2 L 7 2 4T 4 T RT A52EU E8NE 1997011600521 19970116 00521 NE 1997 1 16 97ZZZX312 2 19961204 A 7250 311269601 BEARING BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ENGINE FAILED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 833CA 6794 UE24 114044 DURING POST FLIGHT WALK AROUND WHEN LEFT PROP WAS MOVED, A GRINDING NOISE WAS HEARD COMING FROM ENGINE POWER SECTION. M AIN OIL SCREEN WAS INSPECTED AND FOUND CONTAMINATED WITH METAL. ENGINE WAS REPLACED AND SENT TO PRATT AND WHITNEY CANAD A FOR REPAIR. 2 L 7 2 4T 4 T RT A24CE E26NE 1997011600526 19970116 00526 1997 1 16 97ZZZX314 4 19960526 A 2565 D31050103 SLIDE BAG BAE146 BAE146300A 1500267 EU CABIN FAILED TEST A A6WA K NONE L NO TEST IN INSP/MAINT 1 GL 31 611AW 0154 E3120 ATW - RIGHT AFT ESCAPE SLIDE ESCAPE PATH LIGHTS FALED TO ILLUMINATE DURING A SCHEDULED SLIDE DEPLOYMENT. REPLACED SLIDE ASSY. 2 H 7 4 4F RT A49EU 1997011600527 19970116 00527 1997 1 16 97ZZZX315 4 19960506 A 2565 D31050103 SLIDE BAG BAE146 BAE146200A 1500266 EU NR 3 FAILED TEST A A6WA K NONE L NO TEST IN INSP/MAINT 1 GL 31 294UE 23630 2363 0340 E2107 ATW - NR 3 POSITION ESCAPE SLIDE FAILED A SCHEDULED BATTERY PACK VOLTAGE EFFICIENCY CHECK. REPLACED SLIDE ASSY. 2 H 7 4 4F RT A49EU 1997011600528 19970116 00528 EU 1997 1 16 97ZZZX316 1 19960715 A 7722 CONNECTOR BAG BAE146 BAE146200A 1500266 EU NR 2 ENG TGT DIRTY A A6WA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 294UE E2107 ATW - FLT 581 - NR 2 ENGINE TGT WENT TO ZERO AFTER TAKEOFF. ACFT RETURNED TO ATW. GAUGE STARTED READING NORMALLY JUST BEFORE LANDING. CLEANED CONNECTION AT AN UNDERFLOOR CONNECTION. IT IS A TGT INPUT TO THE TMS SYSTEM. 2 H 7 4 4F RT A49EU 1997011600529 19970116 00529 EU 1997 1 16 97ZZZX317 1 19960719 A 2710 CABLES BAG BAE146 BAE146200A 1500266 EU RT AILERON CONTL RUSTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 609AW E2070 BOTH UPPER AND LOWER AILERON CONTROL CABLES RT WING ROOT ARE RUSTED AND NEED REPLACED. CORRECTIVE ACTION: REMOVED AND REPLACED UPPER AND LOWER RT AILERON CONTROL CABLES IAW A.M.M. SEE WORK CARD NR 2069 FOR FUNCTION CHECKS. 2 H 7 4 4F RT A49EU 1997011600530 19970116 00530 EU 1997 1 16 97ZZZX318 1 19960628 A 5720 JO BOLT BAG BAE146 BAE146200A 1500266 EU LT/RT WING LOOSE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 607AW E2052 ATW - REPLACED JO BOLT AT RIB 2 AND RIB ZERO PER BAE REPAIR INSTRUCTIONS HC571H9033. CORRECTIVE ACTION: REMOVED AND RE PLACED ALL JO BOLTS AT RIB 2 (LT AND RT) STRINGER CROWNS AND RIB ZERO STRINGER CROWNS. ALL WORK PERFORMED PER BAE 146 R EPAIR INSTRUCTIONS HC571H9033. SEE ADDITIONAL WC'S FOR OPS CHECK AND FUEL PIPE REINSTALLATION. 2 H 7 4 4F RT A49EU 1997011600531 19970116 00531 EU 1997 1 16 97ZZZX319 1 19960628 A 5720 BOLTS BAG BAE146 BAE146200A 1500266 EU LT WING DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 607AW E2052 ATW - INSPECT ATTACHMENT BOLTS AND NUTS OF THE REAR SPAR ROOT JOINT ATTACHMENT FITTINGS AT RIB 2 IAW EO E92/083/657C. C ORRECTIVE ACTION: C/W EO E92/083/657 REV C AND REPLACED BOLT WASHER AND NUT IN POSITION E, LT REAR WING SPAR. GENERATE D CARD FOR LEAK CHECK. SEALED INSIDE OF TANK IN POSITION E. 2 H 7 4 4F RT A49EU 1997011600532 19970116 00532 EU 1997 1 16 97ZZZX320 1 19960701 A 5712 RIB BAG BAE146 BAE146200A 1500266 EU LT WING MISDRILLED A A6WA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 607AW E2052 ATW - REF RIL HC571H9033 AT POSITIONS LT WING RIB 2 OTBD HOLE 'A' AT STRS 2 AND 5 AND RT WING RIB 2 INBD STR 2 HOLE 'E' AND RT WING RIB 2 OTBD STR 5 HOLE 'A' HAVE BEEN OVERSIZED TO .3750 INCH TO ACCEPT A MRL3210-12 FASTENER. REF 9002. COR RECTIVE ACTION: INSTALLED OVERSIZED MRL3210-12 FASTENER IN FUEL TANK WING STRINGERS. RT WING 2E, RT CTR 5A BOTH AT RIB 2, LT WING 2A AND 5A, BOTH AT RIB 2. 2 H 7 4 4F RT A49EU 1997011600533 19970116 00533 EU 1997 1 16 97ZZZX321 1 19960701 A 5210 RAIL BAG BAE146 BAE146200A 1500266 EU AIRSTAIRS CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 607AW E2052 ATW - PER AVRO FAX JM/RJ0562-96 DATE 5-13-96, FORWARD AIRSTAIR RAIL (FLOOR RAIL) CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED INBD AND OTBD FWD AIRSTAIR RAILS. 2 H 7 4 4F RT A49EU 1997011600534 19970116 00534 EU 1997 1 16 97ZZZX322 1 19960703 A 5230 SKIN BAG BAE146 BAE146200A 1500266 EU CARGO DOOR DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 607AW E2052 ATW - FORWARD CARGO DOOR HAS DENT CHAFE ON INNER LINER SKIN FROM TRIM SCREW ADJACENT TO PANEL I802. C/A: INSTALLED PAT CH PER 146 SRM 51-71-11, PAGE 4. 2 H 7 4 4F RT A49EU 1997011600535 19970116 00535 EU 1997 1 16 97ZZZX323 1 19960704 A 5313 LONGERON BAG BAE146 BAE146200A 1500266 EU FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 607AW E2052 ATW - RT STRUCTURE AFT OF FRAME 50, THERE IS A DIAPHRAGM BETWEEN THE UPPER AND LOWER SPEED BRAKE LOWER HINGE LONGERONS T HAT HAS A CRACK IN THE LIP OF ITS LIGHTNING HOLE, APPROXIMATELY .3750 INCH LONG. CORRECTIVE ACTION: STOP DRILLED CRACK END PER AVRO FAX. NO CRACKS. GEN WC FOR 2000 CYC REINSP. PERF'D ET AND LOCATED END OF CRACK. 2 H 7 4 4F RT A49EU 1997011600536 19970116 00536 EU 1997 1 16 97ZZZX324 1 19960705 A 5530 RIVETS BAG BAE146 BAE146200A 1500266 EU VERT STAB LOOSE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 607AW E2052 ATW - LAST 3 RIVETS ON THE VERTICAL STABILIZER TO FUSELAGE CLOSING ANGLE ARE SMOKING (RT). CORRECTIVE ACTION: REMOVED AND REPLACED RIVETS. ON LAST RIVET (MOST AFT) INSTALLED HI LOC BOLT. HLT900-6. GENERATED W/C FOR REINSP PER FAX DJH/R J0768-96. 2 H 7 4 4F RT A49EU 1997011600537 19970116 00537 EU 1997 1 16 97ZZZX325 1 19960705 A 5620 WINDOWS BAG BAE146 BAE146200A 1500266 EU CABIN SCRATCHED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 607AW E2052 ATW - ALL CABIN WINDOWS ARE CRAZED OR SCRATCHED. CORRECTIVE ACTION: REMOVED CABIN WINDOW CRAZING AND SCRATCHES BY POLI SHING AND SANDING. SEVEN WINDOWS WERE REPLACED DUE TO BEING OUT OF LIMITS AFTER REMOVAL OF SCRATCHES. UT INSP CABIN WI NDOWS WITHIN LIMITS MM. RETURN TO SERVICE 7-5-96. 2 H 7 4 4F RT A49EU 1997011600538 19970116 00538 EU 1997 1 16 97ZZZX326 1 19960706 A 5311 FRAME BAG BAE146 BAE146200A 1500266 EU FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 607AW E2052 ATW - UPPER FRAME STRUCTURE AFT OF FRAME NR 50 HAS AN APPROXIMATE 2 INCH LONG CRACK IN FLANGE RADIUS ON LT CORNER. CORR ECTIVE ACTION: FABRICATED PARTS FOR REPAIR ON AUXILIARY UPPER FRAME STRUCTURE LT SIDE PER FAX DJH/RJ0749-96. INSTALLED REPAIR PER FAX DJH/RJ0749-96. 2 H 7 4 4F RT A49EU 1997011600539 19970116 00539 EU 1997 1 16 97ZZZX327 1 19960710 A 2560 SLIDE BAG BAE146 BAE146100A 1500260 EU PAX DOOR LOOSE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 246SS E1003 CRW - FLT 605 - LEFT FORWARD PASSENGER DOOR EVACUATION SLIDE WILL NOT DISARM, BUT MOVED APPROXIMATELY 1 INCH. CORRECTIV E ACTION: REMOVED AND REPLACED LOWER HINGE ROD END. 2 H 7 4 4F RT A49EU 1997011600540 19970116 00540 EU 1997 1 16 97ZZZX328 1 19960625 A 5320 RIVETS BAG BAE146 BAE146200A 1500266 EU FUSELAGE LOOSE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 607AW E2052 ATW - BOTH ANGLE BRACKETS OR CLEATS BOTTOM OF FR 50 LOOSE. CORRECTIVE ACTION: REPLACED RIVETS. 2 H 7 4 4F RT A49EU 1997011600541 19970116 00541 EU 1997 1 16 97ZZZX329 1 19960617 A 5330 SKIN BAG BAE146 BAE146200A 1500266 EU FUSELAGE DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 607AW E2052 ATW - REF TASK NR 920003151 ZONAL INSP OF LT AIRBRAKE FOUND NUMEROUS DENTS IN OUTER SKIN. CORRECTIVE ACTION: TRANSFERR ED TO W/O BU5057. SEE LOG PAGE 30183 FOR ROB TRANSACTION. 2 H 7 4 4F RT A49EU 1997011600542 19970116 00542 EU 1997 1 16 97ZZZX330 1 19960814 A 5320 BRACKETS BAG BAE146 BAE146200A 1500266 EU FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 LOW FREQUENCY RUMBLE ON A/C AIR FRAME BETWEEN 270-285 KTS. CAN BE BOTH FELT AND HEARD. FLIGHT CONTROLS NORMAL. CORREC TIVE ACTION: FOUND FIVE CRACKED BRACKETS ON PANEL 281CT, REM AND REP ALL 5 BRACKETS. 2 H 7 4 4F RT A49EU 1997011600543 19970116 00543 EU 1997 1 16 97ZZZX331 1 19960827 A 7920 OIL LINE BAG BAE146 BAE146100A 1500260 EU NR 4 ENGINE LEAKING A A6WA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 31 463AP E1063 ORD - FLT 505 - NR 4 ENGINE SECURED DUE TO DECREASING OIL QUANTITY AND OIL PRESSURE. CORRECTIVE ACTION: TIGHTENED AFT OIL LINE TO THE FUEL/OIL HEAT EXCHANGER. 2 H 7 4 4F RT A49EU 1997011600544 19970116 00544 EU 1997 1 16 97ZZZX332 1 19960916 A 2621 FIRE BOTTLE BAG BAE146 BAE146100A 1500260 EU NR 1 ENGINE CHAFED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 246SS 12302 5108 CN1662M E1003 ATW - FOUND NR 1 ENGINE OTBD FIRE BOTTLE DISCHARGED DUE TO CHAFING OF BOTTLE ON COWLING BOLTS (REF W/C NR 2 THIS WORK PU RCHASE). CORRECTIVE ACTION: REPLACE NR 1 ENGINE OUTBOARD FIRE BOTTLE, OPS CHECK OK, S/N OFF CN1662M. S/N ON CL9784M. 2 H 7 4 4F RT A49EU 1997011600545 19970116 00545 EU 1997 1 16 97ZZZX333 1 19960530 A 5320 ANGLE BAG BAE146 BAE146200A 1500266 EU CARGO COMPT CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 293UE E2097 ATW - FORWARD CARGO BAY; FLOOR SUPPORT ANGLE CRACKED NEAR TIE-DOWN RING (OTBD). MARKED. CORRECTIVE ACTION: REPALCED A NGLE. 2 H 7 4 4F RT A49EU 1997011600546 19970116 00546 EU 1997 1 16 97ZZZX334 1 19960530 A 5320 ANGLE BAG BAE146 BAE146200A 1500266 EU CARGO COMPT CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 293UE E2097 ATW - FORWARD CARGO BAY SUPPORT FOR FORWARD OTBD TIE-DOWN CRACKED AT BOTH ENDS. REF IPC 53-21-05-30T (MARKED). CORRECT IVE ACTION: REPLACED ANGLE. 2 H 7 4 4F RT A49EU 1997011600547 19970116 00547 EU 1997 1 16 97ZZZX335 1 19960529 A 5753 BOLT BAG BAE146 BAE146200A 1500266 EU NR 6 TE FLAP FAILED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 293UE E2097 ATW - RT FLAP TAB HINGE NR 6 BOLT/PIN FAILED NDT. CORRECTIVE ACTION: REMOVED AND REPLACED NR 6 RT FLAP TAB HINGE BOLT. 2 H 7 4 4F RT A49EU 1997011600548 19970116 00548 EU 1997 1 16 97ZZZX336 1 19960529 A 5753 BOLT BAG BAE146 BAE146200A 1500266 EU NR 3 TE FLAP FAILED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 293UE E2097 LT FLAP TAB HINGE NR 3 BOLT/PIN FAILED NDT. CORRECTIVE ACTION: REPLACED NR 3 HINGE BOLT. 2 H 7 4 4F RT A49EU 1997011600549 19970116 00549 EU 1997 1 16 97ZZZX337 1 19960531 A 5320 BRACKET BAG BAE146 BAE146200A 1500266 EU FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 293UE E2097 ATW - BRACKET ATTACHED TO THE FRAME CAP OF FRAME 45 AT 12 O'CLOCK POSITION THAT HAS THE LT PACK VALVE DUCTING ATTACHED H AS A RIVET ALMOST SHEARED OFF AND CRACKED. CORRECTIVE ACTION: REPLACED BRACKET IAW AVRO FAX REF DJR/RJ0630-96 AND DRAW ING HC361J0137. 2 H 7 4 4F RT A49EU 1997011600550 19970116 00550 EU 1997 1 16 97ZZZX338 1 19960607 A 5210 CHANNELS BAG BAE146 BAE146200A 1500266 EU PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 293UE E2097 ATW - FORWARD PASSENGER LT DOOR HAS 2 L-CHANNELS CRACKED AT BOTTOM OF THE DOOR HANDLE BOX STRUCTURE. CRACKS WERE CONFIR MED WITH EDDY CURRENT INSP. CORRECTIVE ACTION: REMOVED BOTH ANGLE BRACKETS. BENT NEW ANGLES AND INSTALLED IAW BAE 146 SRM CHAPTERS 51 AND 52 ON FORWARD PASSENGER DOOR JUST BELOW DOOR HANDLE BOX 52-11-11 DETAIL (E). SEE ADDITIONAL WC'S N R 2280 AND 2281. 2 H 7 4 4F RT A49EU 1997011600551 19970116 00551 EU 1997 1 16 97ZZZX339 1 19960606 A 5320 GUSSET BAG BAE146 BAE146200A 1500266 EU FUSELAGE BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 293UE E2097 ATW - GUSSET PLATE FOR RT AIRBRAKE TOP HINGE LONGERON TO AFT WEB BROKE AFT AT LONGERON. CORRECTIVE ACTION: FABRICATED GUSSET IAW ASSY ON BAE R.I.L. NR HC539H0229 AND INSTALLED PER 51-00-00 OF THE SRM. 2 H 7 4 4F RT A49EU 1997011600552 19970116 00552 EU 1997 1 16 97ZZZX340 1 19960531 A 5313 LONGERON BAG BAE146 BAE146200A 1500266 EU FUSELAGE DAMAGED A A6WA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 293UE E2097 ATW - FORWARD PASSENGER DOOR FUSELAGE UPPER LONGERON AFT OF FUSELAGE FR NR 14 HAS DRILL MARK BOTTOM SURFACE APPROXIMATEL Y .018 INCH DEEP. PART NEEDS TO BE MADE, CHECKED, ALODINED, NOTED FOR CRACKS. CORRECTIVE ACTION: REC'D FAX JM/RJ0624- 96 DAI/1011/55 ALLOWING REPAIR PIECE MADE/INSTALLED. MADE REPAIR PER FAX. PART HEAT TREATED AND CHECKED FOR T-81 CONDI TION. ALODINED AND PAINTED PART. DRESSED AREA. NDT'D, NO CRACKS. 2 H 7 4 4F RT A49EU 1997011600553 19970116 00553 EU 1997 1 16 97ZZZX341 1 19960606 A 5313 LONGERON BAG BAE146 BAE146200A 1500266 EU FUSELAGE CHAFED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 293UE E2097 ATW - RT MOST UPPER AIRBRAKE HINGE MOUNTING LONGERON ASSY HAS BEEN CHAFED BY THE AIRBRAKE ACTUATOR TO A DEPTH OF .040 IN CH. CORRECTIVE ACTION: REPAIRED CHAFED AREA IAW BAE FAX DJR/RJ063096 AND BAE SRM CHAPTER 51-00-00 STANDARD PRACTICES A ND PROCEDURES. 2 H 7 4 4F RT A49EU 1997011600554 19970116 00554 EU 1997 1 16 97ZZZX342 1 19960530 A 5320 SUPPORT BAG BAE146 BAE146200A 1500266 EU CARGO COMPT CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 293UE E2097 ATW - FORWARD CARGO BAY; FLOOR SUPPORT CRACKED FORWARD END. MARKED. NEAR TIE-DOWN RING. REF IPC 53-21-05-30T. CORREC TIVE ACTION: REPAIRED INTERCOSTAL. 2 H 7 4 4F RT A49EU 1997011600555 19970116 00555 EU 1997 1 16 97ZZZX343 1 19960516 A 5400 RIB BAG BAE146 BAE146200A 1500266 EU NR 3 PYLON CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 293UE E2097 NR 3 PYLON CENTER BOX BETWEEN RIBS 3 AND 4 HAS A CRACK IN LOWER FLANGE OF RIB 4 THAT IS APPROXIMATELY .25 INCH LONG. CO RRECTIVE ACTION: NR 3 PYLON RIB 4 LOWER FLANGE APPROXIMATELY .25 INCH CRACK HAS BEEN REPORTED TO AVRO/RDO AND IS ACCEPT ABLE FOR SERVICE PER RIL HC54R6H9018. GENERATED W/C FOR REINSP. 2 H 7 4 4F RT A49EU 1997011600556 19970116 00556 EU 1997 1 16 97ZZZX344 1 19960518 A 5400 RIB BAG BAE146 BAE146200A 1500266 EU NR 2 PYLON CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 293UE E2097 ATW - NR 2 PYLON CENTER BOX BETWEEN RIBS 4 AND 5 HAS A CRACK ON THE LOWER FLANGE OF RIB NR 5 THAT IS APPROXIMATELY .4375 INCH LONG. CORRECTIVE ACTION: NR 2 PYLON RIB NR 5 CRACK HAS BEEN REPORTED TO AVRO RDO AND IS ACCEPTABLE FOR SERVICE P ER RIL HC546H9018. GENERATED W/C FOR REINSP. 2 H 7 4 4F RT A49EU 1997011600557 19970116 00557 EU 1997 1 16 97ZZZX345 1 19960517 A 5320 STIFFENERS BAG BAE146 BAE146200A 1500266 EU BS 25.94 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 293UE E2097 ATW - REF EO E95/003/653 ORIG ITEM 3 . TWO CRACKED STIFFENERS FOUND AT POSITIONS 25.94 ON RT SIDE AND AT POSITION 25.94 ON LT SIDE. C/W EO E95/005/653 ORIG FOR REPAIR. CORRECTIVE ACTION: C/W EO E95/005/653, 2/6/95. INSTALLATION OF REP AIR STIFFENERS, POSITIONS 25.94 LT AND RT SIDES. PERFORMED ET AND POSITIONS 25.94 LT AND RT AROUND CUTLINE AFT. DAMAGE REMOVED PER NOTE '1' OF DRAWING AW-53-20-9506-06. 2 H 7 4 4F RT A49EU 1997011600587 19970116 00587 NM 1997 1 16 AWXA9700033 1 19960106 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 328 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOORBEAM BS 328 RBL 21.5 AND 29, WL 208. REMOVED DAMAGE, FABRICAT ED NEW PART AND INSTALLED PER SRM 53-10-51. 2 L 7 2 4F RT A16WE 1997011600588 19970116 00588 NM 1997 1 16 AWXA9700034 1 19960104 A 5320 654587545 MOPSILL BOEING 737 7373G7 1384595 NM BS 290-294 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FWD SERVICE DOOR MOPSILL AT BS 290 TO 294 RBL 50 WL 208. REMOVED A ND REPLACED MOPSILL PER SRM 51-40-02, 51-40-05. 2 L 7 2 4F RT A16WE 1997011600595 19970116 00595 WP 1997 1 16 9627701147 1 19961231 A 5730 SKIN DOUG DC10 DC1040 3023508 WP WS 610 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 147US 46756 DURING LINE CHECK, A CRACK WAS FOUND ON THE LEFT WING FIXED LEADING EDGE SKIN AT XOS=610. REMOVED DAMAGED AREA AND INST ALLED REPAIR DOUBLERS PER EA 11-120641 (P/N ARB2887-501). 2 L 7 3 4F A22WE 1997011600610 19970116 00610 NM 1997 1 16 UPS97221812 1 19960114 A 3350 BATTERY PACK BOEING 727 72727C 138400J NM COCKPIT DISCHARGED A IPXA K NONE L NO TEST UK UNKNOWN 1 SO 01 908UP 19114 INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHT INOP AT CREW ENTRY DOOR AND EMERGENCY LIGHT INOP AT COCKPIT DOOR. REMOVED AND REPLACED BATTERY PACKS. 2 L 7 3 4F A3WE 1997011600635 19970116 00635 WP 1997 1 16 USAA960776 1 19961206 A 5330 SKIN DOUG DC9 DC981 3022081 WP BS 1437 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 810US 41567 48042 PIT - DURING C-2 CHECK, FOUND 1 INCH CRACK IN SKIN AT STATION 1437, 3RT. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 5 3-04 FIG 27. (M) 2 L 7 2 4F A6WE 1997011600636 19970116 00636 NM 1997 1 16 USAASB96254 1 19961130 A 3350 AD20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 504AU 23379 ALB - MAINTENANCE FOUND THE EMERGENCY EVACUATION LIGHTS LOCATED IN THE BULLNOSE FROM ROWS 16 TO 22, LEFT SIDE INOP. MAI NTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1997011600637 19970116 00637 EU 1997 1 16 USAA960782 1 19961206 A 5313 STRINGERS FOKKER F28 F28MK4000 4990810 EU FRAME 22293 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 475AU 24638 11222 PIT - DURING FC-1 CHECK, FOUND .5 INCH CRACK AND 1.625 INCH CRACK IN FRAME 22293 AT STRINGER NR 54 AND AT STRINGER NR 56 . STOP DRILLED AND INSTALLED REPAIR ANGLES PER EA 34103. (M) 2 L 7 2 4F RT A20EU 1997011600638 19970116 00638 NM 1997 1 16 EIAA9689 1 19961128 A 3350 S1356B37 LIGHT BOEING 747 747273C 1384896 NM CABIN INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 471EV 20651 JFK - DURING SERVICE CHECK, FOUND TWO UPPER DECK EMERGENCY LIGHTS, RIGHT CENTER AND ABOVE LADDER, INOPERATIVE. REPLACED BOTH UPPER DECK EMERGENCY LIGHTS. (M) 2 L 7 4 4F A20WE 1997011600639 19970116 00639 NM 1997 1 16 EIAA9688 1 19961126 A 2611 30231R7 SMOKE DETECTOR BOEING 747 747132 1384882 NM CARGO COMPT BAD BULBS A EIAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 481EV 19896 SYD - DURING DESCENT, MASTER FIRE WARNING LIGHTS CAME ON FOR TWO SECONDS, TWO DIFFERENT TIMES. NO OTHER INDICATIONS. D UE TO RECENT HISTORY, LOWER CARGO HOLDS WERE CHECKED. SHAKE CHECKS OF EXPOSED WIRING IN FORWARD AND AFT HOLDS CARRIED O UT. UNABLE TO FAULT DETECTOR LAMPS, CHECKED NR 3 AND BULK 'A', HAD INCORRECT LAMPS. RELAMPED SMOKE DETECTOR WITH BUILT IN SPARE LAMPS. CARD A8 INTERCHANGED WITH APU LOOP 2. SYSTEM TEST CARRIED OUT FROM P4 SATISFACTORY. (M) 2 L 7 4 4F A20WE 1997011600640 19970116 00640 NM 1997 1 16 97ZZZM68 1 19961118 A 5210 BACB10AF510H ROLLER BOEING 747 747273C 1384896 NM PAX DOOR DAMAGED A A EIAA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 470EV 20653 ANC - CLIMBING THRU FL 10,000 FT A SOFT POPPING SOUND CAME FROM THE CARGO COMPT, A LOUD POPPING SOUND FOLLOWED. JARRIN G OF THE FLT DECK ACCOMP BY 'L ENTRY DOOR 1' LIGHT CAME ON. CABIN PRESS WAS NORM. VISUAL CHK'D, DOOR HANDLE IN LOCKED POSITION. NO AIR LEAKAGE NOTICED. FOUND L1 DOOR, AFT SIDE, UPPR AND LWR LATCH ROLLER CRANK BROKEN. REPLACED BOTH UPPR AND LWR LATCH ROLLER CRANK AND ASSOCIATED HARDWARE. UPPR AND LWR DOOR LATCH TORQUE TUBE HAD TO BE REMOVED AND REPLACED TO INSTALL LATCH ROLLER CRANK. SCRATCHES IND THE 2 ROLLERS WERE NOT PROPERLY ENGAGED AT TOP AFT CORNER. (M) 2 L 7 4 4F A20WE 1997011600641 19970116 00641 NM 1997 1 16 WRLA96052 1 19961201 A 2810 NAS7604U9 BOLT DOUG MD11 MD11 3023602 NM NR 3 FUEL TANK LEAKING A A WRLA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 EA 27 272WA 48437 DURING TAXI-OUT, PASSENGER REPORTED FUEL SEEPING FROM TOP OF RIGHT WING. FLIGHT CREW ELECTED TO RETURN TO GATE FOR MAIN TENANCE. AIRCRAFT RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE PERSONNEL FOUND BOLT TO NR 3 FUEL TANK MULTI-JUNCTION PROBE WAS SEEPING. MAINTENANCE PERSONNEL REMOVED BOLTS AND INSPECTED FOR DAMAGE.(NONE NOTED) RE-INSTALLED AND RE-TORQU ED PROBE BOLTS, STOPPING SEEP. AIRCR AFT RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A22WE 1997011600642 19970116 00642 EU 1997 1 16 REXA96075 1 19961123 A 2612 FIRE WARNING FENWAL 72111211000 SAAB SF340 340B 7860101 EU CARGO COMPT ACTIVATED A REXA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 SO 25 366PX A3769 340B267 CARGO SMOKE IN CWP. CAPTAIN BLEW FIRE BOTTLE AND RETURNED TO LITTLE ROCK. NO EVIDENCE OF FIRE. REMOVED AND REPLACED S MOKE DETECTOR AND FIRE EXTINGUISHER CONTAINER BOTTLE. (M) 2 L 7 2 4T RT A52EU 1997011600643 19970116 00643 WP 1997 1 16 REXA96074 2 19961117 A 7310 FUEL LINE AEROQUIP 1379305A73 BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110U 01514 WP LT ENGINE FAILED A REXA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 25 304PX 663 P63029 ON TAKEOFF ROLL, LEFT FUEL CAP LIGHT ILLUMINATED AND FUEL PRESSURE DROPPED BELOW GREEN ARC. REMOVED AND REPLACED LEFT E NGINE MAIN FUEL SUPPLY LINE. (M) 2 L 7 2 4T 4 T RT A21EU E4WE 1997011600644 19970116 00644 EU 1997 1 16 REXA96073 1 19961118 A 7603 C821466 CONTROL CABLE TELEFLEX C821466 SAAB SF340 340B 7860101 EU RT PWR LEVER BROKEN A A REXA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 25 364PX 184 340B262 ON TAKEOFF RIGHT PROP OVERSPED TO APPROXIMATELY 1460 BEFORE RETURNING TO 1380, JUST SPIKED, BEFORE RETURNING TO NORMAL O PERATION. REMOVED AND REPLACED POWER LEVER CABLE FROM HMU TO PCU. GROUND RUN OPS CHECK NORMAL. (M) 2 L 7 2 4T RT A52EU 1997011600645 19970116 00645 WP 1997 1 16 REXA96072 2 19961116 A 7314 FUEL PUMP BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110U 01514 WP LT ENGINE FAILED A REXA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 25 304PX 663 P63029 LEFT ENGINE HAS LOW FUEL PRESSURE ON TAKEOFF. REMOVED AND REPLACED LEFT ENGINE FUEL PUMP. (M) 2 L 7 2 4T 4 T RT A21EU E4WE 1997011600646 19970116 00646 EU 1997 1 16 REXA96069 1 19961104 A 3350 LIGHT 311701 BAG JETSTM JETSTM3101 1500215 EU CABIN SHORTED A REXA K NONE L NO TEST IN INSP/MAINT 1 SO 25 301PX 654 EMERGENCY LIGHTS CIRCUIT BREAKER WILL POP WHEN POSITIONING SEAT BELT SIGN TO UTILITY. CB WILL NOT RESET. EXIT LIGHT IN OP WITH EMERGENCY LIGHT OR SEAT BELT SIGN. REPAIRED SHORTED LAMPS IN REAR EXIT LGHT. REMVOED AND REPLACED FORWARD EMER GENCY LIGHT BATTERIES, S/N 5294 AND 5458. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A21EU 1997011600647 19970116 00647 EU 1997 1 16 REXA96068 1 19961103 A 7110 COWLING SAAB SF340 SF340A 7850100 EU RT ENGINE NOT LATCHED A REXA A UNSCHED LANDING D INFLIGHT SEPARATION CR CRUISE 1 SO 25 106PX 340A106 RIGHT ENGINE COWLING BLEW OPEN IN FLIGHT. REMOVED AND REPLACED ENGINE COWLING. A/C OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1997011600648 19970116 00648 EU 1997 1 16 REXA96067 1 19961031 A 2450 PDU HARTMAN A2042C SAAB SF340 340B 7860101 EU LEFT FAILED A REXA C ABORTED TAKEOFF H ELECT. POWER LOSS-50 PC TO TAKEOFF 1 SO 25 370PX CG31299 340B300 LEFT MAIN AND ESS BUS BREAKER POPS INTERMITTENTLY. REMOVED AND REPLACED LEFT PDU. OPS CHECK GOOD. AC OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1997011600649 19970116 00649 NM 1997 1 16 USAABB96056 1 19961128 A 3610 S210U1222 OVERPRESSURE SW BOEING 767 767201 1385125 NM RT ENGINE FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 649US 23901 PHL - FL 3 - WITH LEFT PACK ON MEL, AIRCRAFT DEPARTED PHL FOR LAX. PASSING THROUGHT 10,000 FT THE CREW RECEIVED THE EIC AS MESSAGE 'R ENG PRV' AND SECURED THE RIGHT BLEED SYSTEM. FLIGHT RETURNED TO PHL AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT OVERPRESSURE SWITCH FOR THE BLEED PROBLEM, AND THE LEFT FLOW CONTROL VALVE FOR THE LEFT AIR CONDITIONING PACK PROBLEM. (M) 2 L 7 2 4F RT A1NM 1997011600650 19970116 00650 1997 1 16 USAABB96061 4 19961211 A 2397 11426513 WIRE BOEING 757 757225 1384959 NM ROW 25 LEFT BURNED A USAA A B F UNSCHED LANDING EMER. DESCENT ACTIVATE FIRE EXT. A FLAME/FIRE CR CRUISE 1 EA 19 603AU 22198 HUF - FL 158 - AFTER TAKEOFF FROM PHX. FLT ATTENDANT NOTED SLIGHT ODOR (THOUGHT TO BE FROM AIR CONDITIONING SYSTEM). CA PTAIN INVESTIGATED AND COULD NOT CONFIRM. SUBSEQUENTLY, FLIGHT ATTENDANT NOTED SMOKE AND SPARKS COMING FROM VENT BETWEE N ROWS 26 AND 30. THE VENTS WERE CLOSED AND HALON DISCHARGED INTO THE VENT. CAPTAIN DECLARED AN EMERGENCY AND INITIATE D AND EMERGENCY DESCENT. FLIGHT DIVERTED TO HUF AND LANDED WITH NO FURTHER INCIDENT. MX FOUND THE AUDIO WALL DISCONNEC T CABLE PINCHED NEAR SEAT 25A. THE CIRCUIT BREAKER FOR THE SYSTEM HAD OPENED. THE CABLE WAS REPLACED. USAIR ENGINEERI NG ISSUED A FLEET CAMPAIGN TO CHECK ALL SIMILAR WIRING ON THE 757 FLEET. (M) 2 L 7 2 4F RT A2NM 1997011600651 19970116 00651 NM 1997 1 16 USAA960787 1 19961213 A 5330 SKIN BOEING 737 737201 1384454 NM BS 500 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 227AU 46147 21816 GSO - DURING TRANSIT CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH SQUARE AT 6 INCH AFT OF 500 A, 2 INCH SQUARE AT STA TION 500 AT STRINGER 28 R STATION 500 A 6 INCH AFT BELLY AND 500 STATION SKIN, STRINGER. INSTALLED DOUBLER, REPAIRED PE R EA 41878. (M) 2 L 7 2 4F A16WE 1997011600652 19970116 00652 NM 1997 1 16 USAA960785 1 19961212 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 328 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 275AU 37282 22887 ROA - DURING CX-1 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND .75 INCH CRACK FORWARD GALLEY DOOR CUT OUT AFT LOWER CORNE R FUSELAGE SKIN (STRINGER 17 R BS 328). REMOVED CRACK AND INSTALLED DOUBLER, REPAIRED PER TR 53-10-19 REV A. (M) 2 L 7 2 4F A16WE 1997011600653 19970116 00653 NM 1997 1 16 USAA960786 1 19961214 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 957-962 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 255AU 37283 22797 ROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 5 INCH CORROSION STRINGER 27L BS 957 TO 962. REMOVED CORROSI ON AND INSTALLED STRINGER SPLICE. REPAIRED PER SRM 53-10-3 FIG 1. (M) 2 L 7 2 4F A16WE 1997011600654 19970116 00654 NM 1997 1 16 USAASB96252 1 19961213 A 3350 20121 POWER SUPPLY BOEING 737 737401 1384701 NM CABIN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 413US INOPERATIVE 23882 CLE - MAINTENANCE FOUND THE FORWARD RIGHT BULLNOSE EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE POWER SUP PLY IN THE FORWARD OVERHEAD CABIN. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1997011600655 19970116 00655 NM 1997 1 16 USAASB96258 1 19961215 A 5210 DOOR BOEING 737 7374B7 1384702 NM CABIN NOT CLOSED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 448US 24892 ATL - FLT 2346 - ON CLIMB-OUT OF ATL, CREW WAS UNABLE TO PRESSURIZE AIRCRAFT. FLIGHT RETURNED TO FIELD AT ATL. NO EMER GENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE MAIN ENTRY DOOR WAS NOT CLOSIN G AND SEALING PROPERLY. LUBRICATED MAN ENTRY DOOR AND SUBSEQUENTLY ADJUSTED THE UPPER TELESCOPING ASSEMBLY (PROGRAMMING ARM). OPENED AND CLOSED DOOR SEVERAL TIMES. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1997011600656 19970116 00656 NM 1997 1 16 USAASB96261 1 19961217 A 3350 6104789 BATTERY PACK BOEING 737 737201 1384454 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 249US 22756 CLE - MAINTENANCE FOUND THE FORWARD SERVICE DOOR AND THE MAIN ENTRANCE DOOR EMERGENCY EXIT LIGHTS INOP. MAINTENANCE REM OVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1997011600657 19970116 00657 NM 1997 1 16 USAASB96255 1 19961207 A 3350 1012623 LIGHT BOEING 737 737201 1384454 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 259AU 22806 BWI - FLT 404 - CREW REPORTED THE EMERGENCY EXIT LIGHT ABOVE SEAT 9C IS INOP. MAINTENANCE REMOVED AND REPLACED THE LIGH T ASSEMBLY. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1997011600658 19970116 00658 NM 1997 1 16 USAASB96256 1 19961209 A 3350 900835A BATTERY PACK BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 269AU 22881 ALB - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT SIGNS OVER THE WINDOW EXITS FLASHING OFF AND ON. MAINTENANCE REMOVED A ND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1997011600659 19970116 00659 NM 1997 1 16 USAASB96259 1 19961214 A 3350 6104789 BATTERY PACK BOEING 737 7372B7 1384560 NM LT/RT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 268AU 22880 ROA - MAINTENANCE FOUND THE AFT LEFT AND RIGHT EXTERIOR EMERGENCY EXIT LGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE LEFT AND RIGHT BATTERY PACKS LOCATED IN THE AFT CARGO COMPT. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1997011600660 19970116 00660 NM 1997 1 16 USAASB96260 1 19961216 A 3350 6104789 BATTERY PACK BOEING 737 737201 1384454 NM GALLEY DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 262AU 22868 ALB - MAINTENANCE FOUND THE EMERGENCY EVACUATION LIGHTS AT THE AFT GALLEY SERVICE DOORS INOP. MAINTENANCE REMOVED AND R EPLACED THE BATTERY PACK IN THE AFT RIGHT SIDE OF THE AFT CARGO COMPARTMENT. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1997011600661 19970116 00661 EU 1997 1 16 USAAF96127 1 19961217 A 3260 D07308001 LOCK PLATE FOKKER F28 F28MK0100 4990807 EU RT MLG DOOR BROKEN A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 860US 11295 PIT - FL 1193 - CREW RECIEVED BLUE LIGHT IN GEAR HANDLE AND MFDU MESSAGE 'R MLG' AFTER TAKEOFF. CREW CYCLED THE GEAR AN D RECEIVED NORMAL INDICATIONS. CREW DECIDED TO DIVERT TO PIT FOR MAINTENANCE AND LANDED WITH NO FURTHER INCIDENT. MAIN TENANCE FOUND THE LOCK TAB ON THE RIGHT MAIN LANDING GEAR DOOR UPSTOP BROKEN AND REPLACED IT. (M) 2 L 7 2 4F RT 1997011600662 19970116 00662 EU 1997 1 16 USAAF96128 1 19961218 A 3350 59177 LIGHT FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 476US 11224 CLT - THE FORWARD EXIT IDENTIFIER WAS INOPERATIVE. MAINTENANCE REPLACED THE EXIT LIGHT. (M) 2 L 7 2 4F RT A20EU 1997011600663 19970116 00663 NM 1997 1 16 USAABB96060 1 19961207 A 2910 271N61192 HOSE BOEING 757 757225 1384959 NM LT HYD SYSTEM LEAKING A USAA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CL CLIMB 1 EA 19 604AU 22199 PHL - FL 1963 - SHORTLY AFTER TAKEOFF, CREW RECEIVED LEFT HYDRAULIC SYSTEM LOW QUANTITY LEVEL MESSAGE. CREW SHUT DOWN T HE HYDRAULIC PUMP WHEN THE QTY REACHED 50 PERCENT. QTY CONTINUED TO DROP. FLIGHT RETURNED TO PHL AND LANDED WITH NO FU RTHER INCIDENT. MAINTENANCE FOUND THE LINE TO THE LEFT MAIN GEAR OVERCENTER ACTUATOR LEAKING AND REPLACED IT. (M) 2 L 7 2 4F RT A2NM 1997011600664 19970116 00664 NM 1997 1 16 USAASB96263 1 19961217 A 2613 355574255 DETECTION LOOP BOEING 737 7372B7 1384560 NM RT ENGINE FAILED A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 272AU 22884 PIT - FLT 1212 - FLIGHT DIVERTED TO PIT DUE TO A RIGHT WING BODY OVERHEAT LIGHT. NO EMERGENCY WAS DECLARED AND THE FLIG HT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE STRUT CAVITY OVERHEAT DETECTION L OOP. RAN ENGINE. ALL PARAMETERS, PRESSURES AND TEMPERATURES NORMAL. NO LEAKS NOTED ON DUCTING. (M) 2 L 7 2 4F A16WE 1997011600665 19970116 00665 NM 1997 1 16 USAABB96055 1 19961122 A 3350 86210066 BATTERIES BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 615AU 27146 LAX - MAINTENANCE FOUND THE SEAT EMERGENCY LIGHT BATTERIES AT POSITIONS 1 AND 10 INOPERATIVE AND REPLACED THEM. (M) 2 L 7 2 4F RT A2NM 1997011600666 19970116 00666 NM 1997 1 16 USAABB96053 1 19961121 A 3350 8731002511 LIGHT BOEING 757 757225 1384959 NM R-4 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 605AU 22201 LAX - MAINTENANCE FOUND THE R-4 DOOR EXIT IDENTIFIER INOPERATIVE AND REPLACED IT. (M) 2 L 7 2 4F RT A2NM 1997011600667 19970116 00667 NM 1997 1 16 USAABB96054 1 19961122 A 3350 8731002511 LIGHT BOEING 757 7572B7 1384964 NM R-4 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 615AU 27146 LAX - THE R-4 DOOR EXIT IDENTIFIER DID NOT TEST PROPERLY AND WAS REPLACED. (M) 2 L 7 2 4F RT A2NM 1997011600668 19970116 00668 NM 1997 1 16 USAABB96052 1 19961121 A 3350 86210066 BATTERIES BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 605AU 22201 LAX - MAINTENANCE FOUND EIGHT SEAT MOUNTED EMERGENCY LIGHT BATTERIES BAD AND REPLACED THEM. LOCATED IN POSITIONS 1 AND 4 THROUGH 10. (M) 2 L 7 2 4F RT A2NM 1997011600669 19970116 00669 NE 1997 1 16 USAASB96262 2 19961216 A 7200 ENGINE BOEING 737 7372B7 1384560 NM PWA JT8 JT8D15A 52051 NE RIGHT FAILED A A USAA A E UNSCHED LANDING ENGINE SHUTDOWN E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CR CRUISE 1 EA 19 273AU 31090 22885 709110 RIC - FL 2316 - DURING CRUISE, THE CREW HEARD A LOUD BANG. THE NR 2 ENGINE THEN SHOWED INDICATIONS OF LOW POWER. THE N R 2 ENGINE WAS SHUT DOWN AND THE FLIGHT DIVERTED TO RIC. CAPTAIN DID DECLARE AN EMERGENCY. FLIGHT LANDED SAFELY WITHOU T FURTHER INCIDENT. TOTAL SINGLE ENGINE TIME WAS 20 MINUTES. MX REMOVED AND REPLACED THE NR 2 ENGINE ASSY. OPS CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F 4 F A16WE E2EA 1997011600670 19970116 00670 WP 1997 1 16 VJ960004 1 19961223 A 3230 39569641 BUMPER PAD DOUG DC9 DC932 3022066 WP RT MLG OUT OF POSITION A VJ6A O OTHER J WARNING INDICATION CL CLIMB 1 SO 11 945VV 47238 ON CLIMB-OUT FROM ATL-PHL, FLIGHT NR 42, AIRCRAFT RETURNED TO ATL BECAUSE RIGHT GEAR UPLATCH CHECK UNSATISFACTORY. REMO VED AND REPLACED RIGHT BUMPER PAD. PERFORMED GEAR RETRACTION AND OPERATIONAL CHECK PER MM. OPS CHECKED GOOD. (M) 2 L 7 2 4F A6WE 1997011600671 19970116 00671 NM 1997 1 16 WRLA96054 1 19961222 A 5610 NBA6045502 WINDSHIELD DOUG MD11 MD11 3023602 NM RT COCKPIT CRACKED A WRLA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 278WA 48746 DURING INITIAL CLIMB-OUT 13,000 FEET AT APPROX 250 KTS, FIRST OFFICERS WINDSHIELD CRACKED. FLIGHT CREW ELECTED TO RETUR N TO POINT OF DEPARTURE. AIRCRAFT RETURNED TO CZVR WITHOUT FURTHER INCIDENT. REPLACED WINDSHIELD AND AS A PRECAUTION, REPLACED WINDSHIELD ANTI-ICE CONTROLLER. GROUND CHECKS COMPLETED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A22WE 1997011600672 19970116 00672 NM 1997 1 16 WRLA96055 1 19961222 A 7830 CONNECTOR DOUG MD11 MD11 3023602 NM NR 3 ENGINE TR LOOSE A WRLA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 273WA 48519 UPON POWER FOR T/O, NR 3 ENG REVERSER UNLOCK LIGHT ILLUMINATED. ABORTED T/O AND RETURNED TO GATE FOR MX. THRUST REVERS ER WAS DEFERRED PER MEL PROCEDURES. DEFERRAL WAS CLEARED ON 1/2/97. REMOVED AND CLEANED NR 3 ENG'S THRUST REVERSER STO W/DEPLOY SWITCHES. REINSTALL CANNON PLUGS, GROUND TEST THRUST REVERSER (NO FAULTS NOTED). A/C RETURNED TO SERV. A/C E XPERIENCED AN ADDITIONAL FAULT (UNLOCK LIGHT ILLUMINATED DURING T/O ROLL) ON 2/16/97. MALFUNCTION IDENTIFIED AS 'BLACK SHELL' TO CANNON PLUG ON LWR, RT LOCK ACT STOW SWITCH WAS LOOSE. SHIELD WAS CONTACTING ACT BODY. CANNON PLUG WAS CORRE CTED, GROUND TESTS WERE PERFORMED. A/C WAS RETURNED TO SERV. (M) 2 L 7 3 4F RT A22WE 1997011600673 19970116 00673 WP 1997 1 16 WTAA960219 2 19961218 A 7210 31011607 CARBON SEAL BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110U 01514 WP RED GEAR BOX LEAKING A WTAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 17 429UE 807 LAX - SMOKE REPORTED IN CABIN FROM RIGHT AIR CONDITIONING PACK ON DEPARTURE. AIRCRAFT RETURNED TO STATION WITHOUT INCID ENT. AIRCRAFT FERRIED TO FAT. MAINTENANCE REPLACED RIGHT ENGINE CARBON SEAL. GROUND AND LEAK CEHCK SATISFACTORY. AIR CRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A21EU E4WE 1997011600674 19970116 00674 EU 1997 1 16 WTAA960220 1 19961218 A 5330 SKIN BAG JETSTM JETSTM3101 1500215 EU FUSELAGE BIRD STRIKE A WTAA K NONE C F.O.D. LD LANDING 1 WP 17 425UE 798 BFL - BIRD STRIKE TO FUSELAGE ON LANDING REPORTED. MAINTENANCE INSPECTED AIRCRAFT FOR DAMAGE. NO DAMAGE NOTED. AIRCRA FT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1997011600675 19970116 00675 EU 1997 1 16 WTAA960217 1 19961213 A 3240 AC66867 BRAKE CNTL VLV BAG JETSTM JETSTM3101 1500215 EU HYD BAY FAILED A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 WP 17 426UE 774 SFO - AIRCRAFT VEERS TO RIGHT WHEN POWER APPLIED FOR TAKEOFF. TAKEOFF ABORTED. MAINTENANCE REPLACED THE BRAKE CONTROL VALVE. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1997011600677 19970116 00677 EU 1997 1 16 WTAA960215 1 19961213 A 5730 SKIN BAG JETSTM JETSTM3101 1500215 EU RT WING BIRD STRIKE A WTAA K NONE C F.O.D. NR NOT REPORTED 1 WP 17 423UE 799 STS - BIRD STRIKE TO RIGHT WING OUTBOARD LEADING EDGE SURFACE AREA. MAINTENANCE REPLACED RIGHT OUTBOARD LEADING EDGE. S TALL PROTECTION SYSTEM FUNCTIONAL CHECKS WITHIN LIMITS. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1997011600678 19970116 00678 NM 1997 1 16 BJNA961113 1 19961105 A 5753 1A16531 SPAR BOEING 737 737214 138446R NM LT TE MID FLAP CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 457TM 20156 DURIGN A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL THE LEFT WING INBD MID FLAP TRAILING EDGE WAS FOUND WITH DEL AMINATION IN TWO PLACES 16 INCHES AT THE OUTBOARD EDGE AND 6 INCHES AT PREVIOUS REPAIR AT INBOARD EDGE. CUT OUT CORRODE D HONEY COMB COMPOSITE AND REPLACED WITH NEW. CUT OUT CORRODED SECTION OF SPAR CHORD. FABRICATED AND INSTALLED REPAIR SECTION IAW AERO CORP FO 96-395 REV IR DATED 11/18/96. (M) 2 L 7 2 4F A16WE 1997011600679 19970116 00679 NM 1997 1 16 BJNA961103 1 19961115 A 5347 65554845 SEAT TRACK BOEING 737 737214 138446R NM BS 500-520 CORRODED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 457TM 52148 20156 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL CORROSION WAS FOUND IN THE FORWARD CARGO COMPARTMENT AROUND FASTENER HOLES AND THE TIE DOWN PAD ON THE FLOR TRACKS AT FS 500B TO FS 520 STRINGER 27L. CUT OUT CORRODED SECTION OF T RACK. FABRICATED AND INSTALLED NEW SPLICE IAW B737 SRM 53-10-5 FIG 11, 51-10-1, 51-30-8, 51-20-4 AND 51-30-2. (M) 2 L 7 2 4F A16WE 1997011600680 19970116 00680 WP 1997 1 16 97ZZZM69 1 19961204 A 2612 141211 GROMMET DOUG DC8 DC851 3021920 WP NR 4 ENGINE BROKEN A FXLA O OTHER N FALSE WARNING CR CRUISE 1 SO 19 507DC 45855 EXPERIENCED INTERMITTENT FIRE WARNING ON NR 4 ENGINE IN CRUISE UIO TO MIA AND NO OTHER INDICATION OF FIRE. INSPECTION R EVEALED BROKEN GROMMETS ON FIRE WARNING LOOP AT LEFT AND RIGHT AFT COWLING, CAUSING INTERMITTENT GROUNDING. REPLACED FI RE LOOP GROMMETS. SYSTEM CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 4 4F 4A25 1997011600681 19970116 00681 NM 1997 1 16 F3LA96066 1 19961221 A 5330 SKIN BOEING 737 737201 1384454 NM BS 784-786 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 205AU 19421 FLT 93 - DEN - DURING WALK AROUND, MAINTENANCE REPORTED A 2 INCH CRACK IN THE FUSELAGE SKIN AT STATION 784 TO 786, .5 IN CH ABOVE STRINGER 24L. MAINTENANCE STOP DRILLED CRACK AND INSTALLED TYPICAL REPAIR PER BOEING SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1997011600682 19970116 00682 EU 1997 1 16 97ZZZM70 1 19961126 A 3260 CONNECTOR SAAB SF340 340B 7860101 EU RT MLG LOOSE A NVEA A L UNSCHED LANDING ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 03 210AE 340210 FLT 4826 - JFK - RIGHT MAIN GEAR SHOWING UNSAFE FOR LANDING. LOWER LAMPS TEST INDICATES NO RIGHT INDICATION, BUT LDG TE ST SWITCH TEST NEAR GEAR HANDLE INDICATES GOOD INDICATION. (M) 2 L 7 2 4T RT A52EU 1997011600683 19970116 00683 NM 1997 1 16 NOCA0996 1 19961209 A 3350 BPS73 BATTERY PACK BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE CABIN DISCHARGED A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 750NA 26277 DURING INSPECTION OF E-PATH SYSTEM, BATTERY PACK M730 FAILED TO TEST. REPLACED BATTERY PACK, OPS CHECK NORMAL. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 1997011600684 19970116 00684 NE 1997 1 16 M3HA96038 2 19961206 A 7240 GAS GEN CASE AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE NR 1 ENGINE CRACKED A S M3HA K NONE O OTHER IN INSP/MAINT 1 WP 13 4202G 14687 6529 050 120481 HNL - DURING THE INVESIGATION OF HIGH OIL CONSUMPTION, HIGH ITT, AND FUEL FLOW, A 4 INCH LONG CRACK ABOUT .0625 INCH TO .1250 INCH WIDE WAS DETECTED ON GAS GENERATOR CASE NUMBER, ONE ENGINE SERIAL NUMBER 120481. REMOVED AIRCRAFT FROM SERVI CE AND REMOVED ENGINE. DISCREPANCY STILL OPEN AT THIS TIME. PART TOTAL CYCLES, 16,340. (X) 2 H 7 2 4T 4 T RT A53EU E20NE 1997011600685 19970116 00685 NM 1997 1 16 TAOA129608 1 19961216 A 2150 39608831 VALVE BOEING 727 727254 138408L NM RIGHT PACK LOOSE A TAOA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 EA 15 915TS P1989 20252 RIGHT PACK VALVE STUCK OPEN. SMOKE REPORTED IN CABIN, FOUND CONTROL AIR 'B' NUT ON RIGHT FLOW CONTROL AND MODULATING SH UT OFF VALVE LOOSE. SECURED 'B' NUT AND PERFORMED OPERATIONAL CHECK AND LEAK CHECK PER MM 36-12-01. (M) 2 L 7 3 4F A3WE 1997011600686 19970116 00686 NM 1997 1 16 TSAA9626096 1 19961217 A 2612 CONNECTOR BOEING 737 737297 1384480 NM NR 2 ENGINE DIRTY A TSAA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 13 725AL 22051 FLT NR 71 - OGG-HNL - NR 2 ENGINE FIRE WARNING CAME ON. ACCOMPLISHED ENGINE FIRE PROCEDURES AND SHUTDOWN. LIGHT WENT O UT AFTER 5 SEC. CAME ON AGAIN JUST PRIOR TO LANDING AND DISCHARGED RIGHT BOTTLE AND THEN LEFT BOTTLE. LIGHT CONTINUED TO GO ON AND OFF. MX CLEANED ALL LOOP CONNECTORS OF OIL. SYSTEM CHECKS GOOD. REPLACED BOTH NR 1 AND NR 2 FIRE BOTTLES . GROUND OPS AND SQUIB CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1997011600687 19970116 00687 EU 1997 1 16 SIMA963511 1 19961216 A 3610 1158200 PRESS SWITCH AEROSP ATR42 ATR42300 8680920 EU BLEED AIR SYST FAILED A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 262AT 491 0262 ORD - FLT 4171 - CREW REPORTED AN AIRFRAME/AIRBLEED FAULT FOLLOWED BY A HYDRAULIC LOW PRESSURE AND AN ACRIC SMELL IN THE COCKPIT. RAI'D AIRFRAME AIRBLEED PRESSURE SWITCH AND RESET CB FOR HYD SYSTEM. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1997011600688 19970116 00688 NM 1997 1 16 BJNA961201 1 19961214 A 2731 657379945 TRIM TAB BOEING 737 737214 138446R NM RT ELEV TRIM TAB LOOSE SCREWS A A BJNA A UNSCHED LANDING E VIBRATION/BUFFET NR NOT REPORTED 1 WP 11 457TM 20156 PRECAUTIONARY LANDING AT OMA FOR IN FLIGHT VIBRATION. FOUND LOOSE SCREWS RIGHT ELEVATOR TRIM TAB P/N 657379945 SECURED SCREWS PER CASINO EXPRESS MM REFERENCE 27-31-31. AIRCRAFT RELEASED BACK TO SERVICE. INSPECTED WORK IN EKO OF LOOSE SCR EWS, INSTALLATION CHECKS GOOD, PER BMM 27-31-31 ON ELEVATOR TRIM TAB. (M) 2 L 7 2 4F A16WE 1997011600689 19970116 00689 EU 1997 1 16 97ZZZM71 1 19961212 A 2160 2TP131 SWITCH BAG JETSTM JETSTM3101 1500215 EU COCKPIT SHORTED A CX7A H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 03 462CE 684 FLT 177 - DAY TO MDW - SMOKE EMANATED FROM AUXILIARY HEAT SWITCH. CREW PULLED CONTROL CIRCUIT BREAKER AND PERFORMED 'SM OKE IN COCKPIT OR CABIN CHECKLIST'. AIRCRAFT LANDED IN MDW UNEVENTFUL. MAINTENANCE INSPECTED SYSTEM AND FOUND THE CONT ROL SWITCH INTERNALLY SHORTED. REPLACED SWITCH AND OPERATIONAL CHECK WAS SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVIC E. 2 L 7 2 4T RT A21EU 1997011600690 19970116 00690 WP 1997 1 16 ASAA9680273 1 19961214 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 10 TO 12 WERE FOUND INOPERATIVE. RECONNECTED WIRING AT LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1997011600691 19970116 00691 WP 1997 1 16 ASAA9680272 1 19961214 A 3350 014597101 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 953AS 49386 SEA - DURING MAINTENANCE CHECK, THE FORWARD OVERWING EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. REPLACED THE BATTERI ES AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1997011600692 19970116 00692 WP 1997 1 16 ASAA9680270 1 19961212 A 3350 6011777 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 966AS 49104 SEA - DURING MAINTENANCE CHECK, THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPL Y AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1997011600693 19970116 00693 WP 1997 1 16 ASAA9680269 1 19961211 A 3350 41B004AD07G3 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 941AS 49925 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1997011600694 19970116 00694 WP 1997 1 16 ASAA9680274 1 19961216 A 5210 DOOR DOUG DC9 DC982 3022082 WP L1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 933AS 49234 SFO - AFTER ARRIVAL OF FLIGHT 496 - CREW REPORTED THE L1 DOOR HANDLE WAS DIFFICULT TO UNLOCK. ADJUSTED L1 DOOR AND OPER ATED NORMALLY. (M) 2 L 7 2 4F A6WE 1997011600695 19970116 00695 WP 1997 1 16 ASAA9680271 1 19961214 A 5210 SKIN DOUG DC9 DC982 3022082 WP L1 DOOR OVERSIZED A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 935AS 49236 PDX - AFTER ARRIVAL OF FLT 482 - CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN. FOUND L1 DOOR OUTER SKIN CONTACTING D OOR FRAME. TRIMMED DOOR SKIN AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1997011600697 19970116 00697 EU 1997 1 16 VTZA96471 1 19961231 A 5753 1415761623 HINGE BRACKET JETAIR JETSTM JETSTM4101 1500501 EU RT TE FLAP BROKEN A VTZA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 EA 27 318UE 41041 FLT 6370 - IAD-HPN - DURING CRUISE, AN UNSCHEDULED LANDING DUE TO VIBRATION IN FLIGHT. AIRCRAFT RETURNED TO GATE WITH N O FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED FLAP HINGE BRACKET. OPS CHECK OK. AIRCRAFT WAS REL EASED AND APPROVED FOR RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1997011600698 19970116 00698 1997 1 16 VTZA96470 4 19961231 A 6113 SPINNER JETAIR JETSTM JETSTM4101 1500501 EU RT PROP OUT OF ADJUST A VTZA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 27 318UE 41041 FLT 6203 - IAD-MHT - DURING CLIMB, MADE AN UNSCHEDULED LANDING DUE TO RIGHT PROP VIBRATION. AIRCRAFT RETURNED TO GATE W ITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED INSTALLED 3 SHIMS TO RIGHT SPINNER, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1997011600699 19970116 00699 EU 1997 1 16 VTZA96469 2 19961231 A 7320 8974575 BYPASS VALVE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT ENG ENG FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 370MT 800 FLT 6296 - IAD-ROC - ABORTED TAKEOFF DUE TO LEFT ENGINE WOULD ONLY MAKE 90 PERCENT TORQUE. THE AIRCRAFT RETURNED TO GAT E WITH NO FURTHER PROBLEM. MAINTENANCE INSPECTED AND REMOVED AND REPLACED LEFT TTL BYPASS VALVE, OPS CHECK OK. AIRCRAF T WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1997011600700 19970116 00700 EU 1997 1 16 VTZA96420 1 19961202 A 5270 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGG DOOR OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 306UE 41020 FLT 6432 - IAD-ORF - ABORTED TAKEOFF DUE TO BAGGAGE DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT WENT TO GATE WITH NO FURTH ER PROBLEMS. MAINTENANCE INSPECTED AND OPENED DMI 53141, MEL 52-3. MX CLOSED DMI 53141, BY ADJUSTING MICROSWITCH. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1997011600701 19970116 00701 EU 1997 1 16 VTZA96467 1 19961220 A 5270 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGG DOOR LACK OF LUBE A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 309UE 41022 FLT 6511 - JFK-IAD - ABORTED TAKEOFF DUE TO MAIN BAGGAGE DOOR WARNING LIGHT ILLUMINATED. MAINTENANCE OPEN DMI 52741, ME L 52-3. MAINTENANCE CLOSED DMI 52741 ON 12-30-96 BY INSPECTING AND LUBING FORWARD MICROSWITCH LEVER PLATE, OPS CHECK OK . AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1997011600702 19970116 00702 EU 1997 1 16 VTZA96466 1 19961227 A 7714 A634 TACH GEN BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 497UE 904 FLT 6319 - IAD-CLE - DURING CLIMB, MADE AN UNSCHEDULED LANDING DUE TO RIGHT RPM INDICATION DROPPED TO ZERO. AIRCRAFT RE TURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED TACH GEN, OPS CHECK OK. AIRCRAFT WAS RELEASE D AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1997011600703 19970116 00703 1997 1 16 VTZA96465 4 19961227 A 3416 066306202 ALTIMETER BAG JETSTM JETSTM3201 1500217 EU LT COCKPIT FAILED A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 482UE 897 FLT 6187 - IAD-SCE - DURING CLIMB, MADE AN UNSCHEDULED LANDING DUE TO CAPTAINS ALTIMETER FLAGGED ON CLIMB-OUT. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED ALTIMETER, OPS CHECK OK. AIRCRAFT WAS REL EASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1997011600704 19970116 00704 EU 1997 1 16 VTZA96464 1 19961229 A 2424 51539019 GCU JETAIR JETSTM JETSTM4101 1500501 EU RIGHT FAILED A VTZA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 EA 27 302UE 41013 FLT 6454 - IAD-CLE - DURING CLIMB, AN UNSCHEDULED LANDING DUE TO RIGHT GEN, RIGHT GCU, AND RIGHT PDU FAILED. AIRCRAFT R ETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED GCU, OPS CHECK OK. AIRCRAFT W AS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1997011600705 19970116 00705 1997 1 16 VTZA96463 4 19961228 A 2312 7510700807 COMM UNIT JETAIR JETSTM JETSTM4101 1500501 EU NR 2 FAILED A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 320UE 41043 FLT 6506 - IAD-BOS - DURING CLIMB, AN UNSCHEDULED LANDING DUE TO NR 2 COMM UNIT INOP. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED REMOVED AND REPLACED NR 2 COMM UNIT, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1997011600706 19970116 00706 EU 1997 1 16 VTZA96462 1 19961228 A 5270 DOOR WARNING JETAIR JETSTM JETSTM4101 1500501 EU BAGG COMPT ACTIVATED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 324UE 41017 FLT 900 - LYH-ROA - ABORTED TAKEOFF DUE TO MAIN BAGGAGE DOOR WARNING ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FUR THER PROBLEMS. MAINTENANCE INSPECTED AND RESET BAGGAGE DOOR VENT PANEL. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1997011600707 19970116 00707 EU 1997 1 16 VTZA96459 1 19961226 A 5270 WARNING LIGHT JETAIR JETSTM JETSTM4101 1500501 EU BAGGAGE DOOR ILLUMINATED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 312UE 41025 FLT 6454 - IAD-DTW - ABORTED TAKEOFF DUE TO BAGGAGE DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO F URTHER PROBLEMS. MAINTENANCE INSP AND OPEN DMI 57584, MEL 52-3. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVI CE. (M) 2 L 7 2 4T RT A41NM 1997011600708 19970116 00708 EU 1997 1 16 VTZA96460 1 19961226 A 5270 WARNING LIGHT JETAIR JETSTM JETSTM4101 1500501 EU BAGG DOOR ILLUMINATED A VTZA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 27 324UE 41017 FLT 6264 - BTV-IAD - ABORTED TAKEOFF DUE TO MAIN BAGGAGE DOOR WARNING ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FU RTHER PROBLEMS. MAINTENANCE INSPECTED AND OPEN DMI 57957, MEL 52-3. AIRCRAFT WAS RLEASED AND APPROVED FOR RETURN TO SE RVICE. (M) 2 L 7 2 4T RT A41NM 1997011600709 19970116 00709 NM 1997 1 16 TWRA96378 1 19961210 A 2120 2124B1283 DUCT BOEING 747 747212B 1384886 NM AIR COND BAY LEAKS A TWRA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 15 619FF 21316 IN CLIMB, ALL PACKS ON PACK NR 1 /2 TRIPPED. DUCT PRESS DOWN TO 16 PSI. CLOSED LT ISOLATION VLV AND NR 1/ 2 BLEED VLVS . LT WING PRESS ZERO. RT SIDE NORM 26 PSI WITH ONLY NR 3 BLEED OPEN. OPENED NR 1 BLEED EGT RISE. OPENED NR 2 BLEED EGT RISE. PAX AND CABIN CREW SAID SMOKE COMING OUT OF GASPER AND SIDE VENTS. DISAPPEARED AFTER WING ISOLATION. FOUND LT WING PNEUMATIC SUPPLY DUCT FLANGE SEPARATED UNDER FUSELAGE ELBOW DUCT TO WING SUPPLY. REPLACED DUCT, LK CHK OK. REP LACED NR 1 PACK ACCESS PNL. REPLACED BODY FAIRING 191EEL. REPLACED DUCT SUPPORT ROD. SYS DECAY OK. ALL CKD GOOD PER MM 36-11-12. A/C RETURN TO SERV. (M) 2 L 7 4 4F A20WE 1997011600710 19970116 00710 NM 1997 1 16 TWRA96381 1 19961222 A 3350 3004181A LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 619FF 975 21316 DURING DAILY CHECK, FOUND 5R MED UPPER BUSTLE EMERGENCY LIGHT INOP. REMOVED AND REPLACED UPPER BUSTLE LIGHT ASSEMBLY AS PER MM 33-56-00 PAGE 501. OPS CHECK OK. (M) 2 L 7 4 4F A20WE 1997011600711 19970116 00711 NM 1997 1 16 97ZZZM72 1 19961216 A 2560 80330034 ASSIST BOTTLE BOEING 747 747212B 1384886 NM 5L DOOR DEPLOYED A TWRA K NONE O OTHER TX TAXI/GRND HDL 1 EA 15 616FF 1331 21939 AFTER ARRIVAL 5L DOOR WAS INADVERTENTLY DEPLOYED. REMOVED AND REPLACED SLIDE AND DOOR ASSIST BOTTLE AS PER MM 25-65-01. OPS CHECKED NORMAL. A/C RETURN TO SERVICE. (M) 2 L 7 4 4F A20WE 1997011600712 19970116 00712 NM 1997 1 16 TWRA96382 1 19961225 A 2612 472925 FIRE LOOP BOEING 747 747121 1384871 NM NR 2 ENG FAULTY A TWRA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING TO TAKEOFF 1 EA 15 609FF 5004 20354 DURING TAXI, NR 2 ENG 'A' FIRE LOOP WENT TO FAULT. FULL SCALE 'B' LOOP TESTED OK WITH ALL OTHER IND NORM. JUST AFTER V 1 NR 2 ENGINE 'B' LOOP WENT TO FULL SCALE FAULT. NR 2 ENG WAS SHUT DOWN AND NR 1 FIRE BOTTLE DISCHARGED. C/B WERE RESE T AND ENG FIRE WARNING RETESTED. NR 2 FAILED TO TEST. NR 2 EDP WAS DEPRESSURIZED ONLY. FOUND BROKEN BRACKET ON FIRE L OOP ELEMENTS. INSTALLED NEW LOWER FWD LOOP AS PER MM 26-12-01 PAGE 501 CHECKED OPS OF NR 2 ENG FIRE LOOP A/B CHECK NORM PER MM 26-11-00 PG 501. R/R NR 1 FIRE BOTTLE ON ENG NR 2 PER WIC 26-259. A/C RETURN TO SERVICE. (M) 2 L 7 4 4F A20WE 1997011600713 19970116 00713 CE 1997 1 16 S2YA960040 1 19961210 A 3230 623372 SOLENOID VALVE BEECH 1900 1900D 1154162 CE WS 79.65 STUCK A S2YA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 13 79SK 3039 3039 UE79 FLT 1164 - FLT CREW MKE-SBN - LIFTED THE L/G HANDLE TO RETRACT THE L/G AFTER ROTATION. THE RT MAIN GEAR ANNUNCIATOR EXT INGUISHED, THE RED UNSAFE LIGHTS ILLUMINATED IN GEAR HANDLE, AND THE GEAR FAILED TO RETRACT. BEFORE LANDING BACK AT MKE THE L/G HANDLE WAS SELECTED DOWN, THE RT GEAR DOWN AND LOCKED ANNUNCIATOR ILLUMINATED, AND THE RED UNSAFE LIGHTS EXTING UISHED. MX FOUND THE GEAR EXTEND RETRACT SOLENOID INOP. THE SOLENOID VLV WAS REMOVED AND REPLACED. THE GEAR OP CHECKE D GOOD UP AND DOWN, AND MANUAL RETRACTION CHECKED GOOD. (M) 2 L 7 2 4T RT A24CE 1997011600714 19970116 00714 CE 1997 1 16 S2YA960037 1 19961127 A 2731 TRIM TAB BEECH 1900 1900D 1154162 CE HORIZ STAB FROZEN A A S2YA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 13 118SK UE108 THE FLT CREW, FOUND THE ELEVATOR AND RUDDER TRIM TABS FROZEN WHEN THEY LEVELED OFF AT CRUSING ALTITUDE, WHEN THE AIRCRAF T LANDED THE FREEZING ELEVATOR AND RUDDER TRIM TABS WERE WRITTEN UP. MAINTENANCE LUBED THE ELEVATOR AND RUDDER TRIM TAB ACTUATORS, OPS CHECKED GOOD MANUALLY AND ELECTRICALLY. AFTER SUBSEQUENT FLIGHTS NO OTHER PROBLEMS WERE NOTED. (M) 2 L 7 2 4T RT A24CE 1997011600715 19970116 00715 CE 1997 1 16 S2YA960038 1 19961213 A 3260 BULB BEECH 1900 1900D 1154162 CE RT MLG FAILED A S2YA O OTHER N FALSE WARNING AP APPROACH 1 GL 13 901SK UE90 FLT 1120 - GRR-YYZ - SELECTED THE LANDING GEAR DOWN ON FINAL APPROACH INTO YYZ. THE GEAR EXTENDED NORMALLY BUT THE RIGH T MAIN DOWN AND LOCKED ANNUNICATOR FAILED TO ILLUMINATE, THE GEAR UNSAFE LIGHTS IN THE GEAR HANDLE ALSO WERE NOT ILLUMIN ATED. THE FLIGHT CREW NOTIFIED THE AIRPORT. THE AIRCRAFT LANDED WITHOUT INCIDENT, AFTER TOUCHDOWN THE FLIGHT CREW TURN ED ONTO THE TAXIWAY, SHUT THE ENGINES DOWN, AND GEAR DOWN LOCKS WERE INSTALLED. MAINTENANCE CHNAGED THE RIGHT MAN GEAR BULBS, OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A24CE 1997011600716 19970116 00716 CE 1997 1 16 S2YA960039 1 19961209 A 2434 GENERATOR BEECH 1900 1900D 1154162 CE LEFT MALFUNCTIONED A S2YA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CL CLIMB 1 GL 13 841SK UE84 FLT 1042 - MKE-IND - 15 MINUTES INTO FLT, THE LT DC GENERATOR FELL OFF LINE, THE FLIGHT CREW ATTEMPTED TO RESET IT, BUT IT FAILED TO COME BACK ON LINE. THE FLIGHT RETURNED BACK TO MKE AND LANDED WITHOUT INCIDENT, ONCE ON THE GROUND THE FLI GHT CREW ATTEMPTED TO RESET THE LT DC GEN AGAIN, THIS TIME IT CAME BACK ON LINE. MAINTENANCE INSPECTED THE DC GENERATOR , GENERATOR CONTROL UNIT, DC POWER PANEL, AND ALL ASSOCIATED WIRING WITH NO PROBLEMS FOUND. THEY DECIDED TO SWAP THE GC U'S AND PARALLEL THEM, ALL OPS CHECKED GOOD ON THE GROUND, AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1997011600717 19970116 00717 CE 1997 1 16 S2YA960036 1 19961127 A 2731 TRIM TAB BEECH 1900 1900D 1154162 CE HORIZ STAB FROZEN A A S2YA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 13 148SK UE148 THE FLT CREW, FOUND THE ELEVATOR TRIM TABS FROZEN WHEN THEY LEVELED OFF AT CRUISING ALTITUDE. WHEN THE AIRCRAFT LANDED, THE FREEZING ELEVATOR TRIM TABS WERE WRITTEN UP. MAINTENANCE LUBED THE ELEVATOR TRIM TAB ACTUATORS. OPS CHECKED GOOD MANUALLY AND ELECTRICALLY. AFTER SUBSEQUENT FLIGHTS NO OTHER PROBLEMS WERE NOTED. (M) 2 L 7 2 4T RT A24CE 1997011600718 19970116 00718 CE 1997 1 16 S2YA960035 1 19961119 A 5270 DOOR WARNING BEECH 1900 1900D 1154162 CE CABIN DOOR ILLUMINATED A S2YA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 13 148SK UE148 FLT 1263 - DAY-BNA - AFTER TAKEOFF THE CABIN DOOR ANNUNCIATOR ILLUMINATED IN FLT. THE CO-PILOT INSPECTED THE DOOR LOCK CAMS IN FLIGHT TO CHECK FOR AN UNSAFE CONDITION, NONE WERE FOUND TO BE OUT OF ALIGNMENT. THE CREW MADE A SAFE LANDING IN DAY. MAINTENANCE INSPECTED THE DOOR LOCK SYSTEM AND FOUND NO DISCREPANCIES, THE ANNUNCIATOR WAS MEL'D UNDER 52.01. (M ) 2 L 7 2 4T RT A24CE 1997011600719 19970116 00719 CE 1997 1 16 S2YA960034 1 19961117 A 5610 10138402518 WINDSHIELD BEECH 1900 1900D 1154162 CE LT COCKPIT BURNT TERMINAL A S2YA A G UNSCHED LANDING O2 MASK DEPLOYED B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 13 841SK 494 UE84 FLT 1267 - MKE-BNA - TURNED ON THE WINDSHIELD ANTI-ICE DUE TO APPROACHING ICING CONDITIONS. WHEN THE CO-PILOTS WINDSHIE LD ANTI-ICE WAS SELECTED ON, THE CREW SMELLED SOMETHING ACRID AND NOTICED SMOKE STARTING TO COME OUT FROM BEHIND THE GLA RESHIELD. THE WINDSHIELD HEAT WAS TURNED OFF AND THE CREW OXYGEN MASKS WERE PUT ON. THE CREW PROCEEDED TO MAKE A SAFE EMERGENCY LANDING AT HOP. UPON INSPECTION MX FOUND THE LP TERMINAL BLOCK ON THE WINDOW TO BE BURNT. THE WINDOW WAS REP LACED AND OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A24CE 1997011600720 19970116 00720 CE 1997 1 16 S2YA960033 1 19961114 A 3230 CONNECTOR BEECH 1900 1900D 1154162 CE LANDING GEAR DIRTY A S2YA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 13 901SK UE90 FLT 1162 - MKE-SBN - CYCLED THE LANDING GEAR HANDLE, THE LANDING GEAR DID NOT RETRACT. THE CREW ATTEMPTED TO CYCLE THE LANDING GEAR A SECOND TIME, WITH NO RETRACTION OR ANNUNCIATION SHOWING GEAR RETRACTION THE CREW RETURNED TO MKE. UPON I NSPECTION MAINTENANCE FOUND THE CONNECTOR CONTACTS AT THE GROUND SERVICE VALVE DIRTY. CLEANED AND LUBED THE CONTACTS, R ETRACTION CHECKED GOOD ON JACKS. (M) 2 L 7 2 4T RT A24CE 1997011600721 19970116 00721 CE 1997 1 16 S2YA960032 1 19961114 A 2120 ACM DUCT BEECH 1900 1900D 1154162 CE LT ENGINE LOOSE A S2YA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 GL 13 81SK UE81 FLT 1120 - GRB-MKE - AFTER T/O TURNED ON THE RT AND LT BLEED VLVS, THE RT BLEED AIR FAIL ANNUNCIATOR ILLUMINATED AND ALL CABIN HEAT AND PRESSURIZATION CEASED. UPON RETURN TO GRB MX INSPECTED EVA TUBING, RT L/E AND CTR SECTION, BLEED AIR OV ERPRESSURE SWITCHES, AND PERFORMED BLEED AIR PRESSURE CHECK. CHANGED THE LT PRSOV DUE TO WEAK AIRFLOW. OPS CHECKED ON GROUND. ON FLT 1123, SAME PROBLEM OCCURED AGAIN, UPON LANDING IN MKE. MX INSPECTED AND FOUND LT ACM DUCT WHERE IT ATTA CHES TO THE MUFFLER ASSY, DETACHED AND CLAMP LOOSE. THE MELTED THE EVA TUBING ALONG SIDE DUCT CAUSING A BLEED AIR FAIL, EVA TUBING WAS REPLACED AND THE DUCT RE-ATTACHED. OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A24CE 1997011600722 19970116 00722 CE 1997 1 16 S2YA960028 1 19961021 A 3260 SWITCH BEECH 1900 1900D 1154162 CE LANDING GEAR OUT OF ADJUST A S2YA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 13 891SK UE89 FLT 1265 - AFTER TAKEOFF, THE CREW NOTICED THE GEAR HANDLE UNSAFE LIGHTS REMAINED ILLUMINATED AND THE WARNING HORN SOUND ED CONTINUOUSLY WHEN LANDING GEAR HANDLE WAS RAISED TO THE RETRACT POSITION. MAINTENANCE ADJUSTED FLAP LIMIT SWITCH S4 AND ADJUSTED FLAP SYSTEM AS REQUIRED, OPERATIONAL CHECKED GOOD. (M) 2 L 7 2 4T RT A24CE 1997011600723 19970116 00723 CE 1997 1 16 S2YA960027 1 19961016 A 2752 100384040 FLAP MOTOR BEECH 1900 1900D 1154162 CE TE FLAPS OVERHEATED A A S2YA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 13 891SK 669 UE89 DURING RUNUP BEFORE FIRST FLIGHT OF THE DAY, THE CREW NOTICED SMOKE IN THE CABIN, MAINTENANCE FOUND THE FLAP MOTOR WINDI NGS HAD OVERHEATED INTERNALLY. IT WAS REPLACED BUT THE FLAP SYSTEM WAS DEFERRED DUE TO RIGGING REQUIRED. (M) 2 L 7 2 4T RT A24CE 1997011600724 19970116 00724 NM 1997 1 16 W8PA960210 1 19961206 A 5320 69434961 SUPPORT BOEING 737 7373Y0 1384671 NM BS 847-867 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 962WP 23748 DURING C-CHECK, FOUND CORROSION ON BOTH TOP AND BOTTOM SIDE OF FLOOR TO SIDEWALL SUPPORT AROUND NUTPLATES AT BS 847-867, RBL 19.5, WL 157. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT. (M) 2 L 7 2 4F RT A16WE 1997011600725 19970116 00725 NM 1997 1 16 W8PA960209 1 19961206 A 5320 69434772 SUPPORT BOEING 737 7373Y0 1384671 NM BS 769-779 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 962WP 23748 DURING C-CHECK, FOUND CORROSION ON BOTH TOP AND BOTTOM SIDE OF FLOOR TO SIDEWALL SUPPORT AT BS 769-779, RBL 21.5, WL 157 . REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT. (M) 2 L 7 2 4F RT A16WE 1997011600726 19970116 00726 NM 1997 1 16 W8PA960208 1 19961206 A 5320 BAC1505100551 STRAP BOEING 737 7373Y0 1384671 NM BS 772 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 962WP 23748 DURING C-CHECK, FOUND CORROSION ON BOTH TOP AND BOTTOM OF FLOOR SUPPORT STRAP AROUND NUTPLATES AT BS 772, LBL 21 TO RBL 21, WL 156. REMOVED AND REPLACED FLOOR SUPPORT STRAP. (M) 2 L 7 2 4F RT A16WE 1997011600727 19970116 00727 NM 1997 1 16 W8PA960207 1 19961208 A 5320 HFAB53FB011 SUPPORT BOEING 737 7373Y0 1384671 NM BS 727-947 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 962WP 23748 DURING C-CHECK, FOUND CORROSION ON BOTH TOP AND BOTTOM OF FLOOR SUPPORT AROUND NUTPLATES AT BS 727D PLUS 5 TO BS 947, R BL 3 AND RBL 7.5, WL 155.5. REMOVED AND REPLACED FLOOR SUPPORT. (M) 2 L 7 2 4F RT A16WE 1997011600728 19970116 00728 NM 1997 1 16 W8PA960206 1 19961206 A 5320 BAC14902770 SUPPORT BOEING 737 7373Y0 1384671 NM BS 727-947 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 962WP 23748 DURING C-CHECK, FOUND CORROSION ON BOTH TOP AND BOTTOM OF FLOOR SUPPORT AROUND NUTPLATES AT BS 727D PLUS 5 TO BS 947, LB L 12, WL 155.5. REMOVED AND REPLACED SECTION OF FLOOR SUPPORT. (M) 2 L 7 2 4F RT A16WE 1997011600729 19970116 00729 NM 1997 1 16 W8PA960205 1 19961206 A 5320 HFAB53FB011 SUPPORT BOEING 737 7373Y0 1384671 NM BS 727-947 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 962WP 23748 DURING C-CHECK, FOUND CORROSION AROUND NUTPLATES ON FLOOR SUPPORT AT BS 727B PLUS 3 TO BS 947, LBL 3, WL 155.5. REMOVED AND REPLACED FLOOR SUPPORT. (M) 2 L 7 2 4F RT A16WE 1997011600730 19970116 00730 NM 1997 1 16 W8PA960213 1 19961229 A 3350 LIGHT BOEING 737 7373K9 138447L NM CABIN INOP A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 945WP 24212 FOUND EMERGENCY EXIT AISLE LIGHT IN OVERHEAD BIN AT ROW 11 PARTIALLY UNATTACHED. REATTACHED LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A16WE 1997011600731 19970116 00731 NM 1997 1 16 W8PA960212 1 19961229 A 3350 BPS73 BATTERY BOEING 737 7373K9 138447L NM CABIN DISCHARGED A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 945WP 26796 24212 FOUND CENTER AFT AND R-2 DOOR EMERGENCY EXIT SIGNS INOP. REPLACED BATTERY PACK. (M) 2 L 7 2 4F RT A16WE 1997011600732 19970116 00732 NM 1997 1 16 W8PA960211 1 19961206 A 5320 BAC1505100551 STRAP BOEING 737 7373Y0 1384671 NM BS 860 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 962WP 23748 DURING C-CHECK, FOUND CORROSION ON FLOOR SUPPORT STRAP AT BS 860, LBL 21.5 - RBL 18.5, WL 158. REMOVED AND REPLACED STR AP. (M) 2 L 7 2 4F RT A16WE 1997011600733 19970116 00733 1997 1 16 JBXA00033 4 19961206 A 2230 AUTO THROTTLE FOKKER F28 F28MK0100 4990807 EU E/E COMPT MALFUNCTIONED A JBXA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 05 104ML 11445 BDL - FLT 222 - NO AUTO THROTTLE ON FMA, ABORTED TAKEOFF AT BDL. PERFORMED AUTO THROTTLE SERVO TEST PER MM 22-31-01 AND AFCAS PANEL PROCEDURES PER MM 22-41-00. ALL CHECKS NORMAL. OPS CHECK OK. (M) 2 L 7 2 4F RT 1997011600734 19970116 00734 1997 1 16 JBXA00032 4 19961204 A 2213 FCC 6227476411 FOKKER F28 F28MK0100 4990807 EU NR 3 FAILED A A JBXA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 05 131ML 514 11323 RDU - FLT 552 - DURING TAKEOFF ROLL, ABORTED TAKEOFF DUE TO FLAP DISARMED MESSAGE. AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE PERFORMED AFCAS MAINTENANCE TEST, FCC NR 3 FAILED REMOVED AND REPLACED THE NR 3 FCC. NO PRESENT FAULTS REPO RTED. OPS CHECK GOOD IAW AMM 22-11-01. (M) 2 L 7 2 4F RT 1997011600735 19970116 00735 WP 1997 1 16 97ZZZM73 1 19961221 A 3350 LIGHT DOUG DC9 DC931 3022065 WP CABIN BROKEN A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 934ML 47526 DTW - FLT 1130 - RIGHT FORWARD EMERGNCY LIGHT TRACK BROKEN (LIGHTS WILL NOT STAY IN TRACK). MAINTENANCE REMOVED AND REP LACED PLASTIC RETAINER FOR FORWARD EMERGENCY PATH LIGHTING, OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1997011600736 19970116 00736 WP 1997 1 16 97ZZZM74 1 19961217 A 7931 CONNECTOR DOUG DC9 DC931 3022065 WP RT ENGINE LOOSE A GTIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 934ML 47526 ACY - FLT 511 - DURING CLIMB CONFIGURATION RIGHT ENGINE OIL PRESSURE DECREASE TO 42 PSI, AND BEGAN FLUCTUATING BETWEEN 4 2 AND 40 PSI. OIL TEMPERATURE AND QUANTITY NORMAL. MAINTENANCE FOUND OIL PRESSURE TRANSMITTER CANNON PLUG LOOSE AND SO AKED WITH OIL. CLEANED AND SECURED CANNON PLUG. PERFORMED AN ENGINE RUN UP AND OIL PRESSURE NORMAL IAW DC9 MM CHAPTER 79-32-00. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1997011600737 19970116 00737 WP 1997 1 16 97ZZZM75 1 19961218 A 3260 DOWNLOCK SW DOUG DC9 DC931 3022065 WP RT MLG FAILED A GTIA O OTHER N FALSE WARNING AP APPROACH 1 GL 23 934ML 47526 DTW - FLT 626 - DURING LANDING GEAR EXTENSION EXPERIENCED A UNSAFE INDICATION ON RIGHT MAIN LANDING GEAR. RECYCLED LAND ING GEAR, RIGHT MAIN GEAR REMAINED UNSAFE. LANDED DTW WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAI N GEAR DOWN LOCK POSITION SWITCH. OPERATIONAL CHECK GOOD IAW DC9 MM CHAPTER 32-60-1. AIRCRAFT RETURNED TO SERVICE. (M ) 2 L 7 2 4F A6WE 1997011600738 19970116 00738 NM 1997 1 16 HNAA9690878 1 19961205 A 7931 310614301 ADAPTOR PLATE DHAV DHC8 DHC8102 2809003 NM NR 1 ENGINE FAILED A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 908HA 30232 015 FLT 3255 - HVN-DCA - ON CLIMB-OUT AT 3000 FEET, THE MASTER WARNING LGIHT ILLUMINATED, THE NR 1 OIL PRESSURE LIGHT WAS ON , AND THE NR 1 OIL PRESSURE WAS FALLING. THE CREW SHUTDOWN NR 1 ENGINE AND RETURNED TO HVN WITHOUT INCIDENT. THE AIRCR AFT WAS FERRIED TO SBY FOR REPAIR. REPLACED ADAPTOR PLATE AND INSTALLED A NEW AC GENERATOR. (M) 2 H 7 2 4T RT A13NM 1997011600739 19970116 00739 NM 1997 1 16 97ZZZM76 1 19961205 A 7931 31708001A GENERATOR LUCAS DHAV DHC8 DHC8102 2809003 NM NR 1 ENGINE FAILED A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 908HA 12133 015 FLT 3255 - HVN-DCA - ON CLIMB-OUT AT 3000 FEET, THE MASTER WARNING LGIHT ILLUMINATED, THE NR 1 OIL PRESSURE LIGHT WAS ON , AND THE NR 1 OIL PRESSURE WAS FALLING. THE CREW SHUTDOWN NR 1 ENGINE AND RETURNED TO HVN WITHOUT INCIDENT. THE AIRCR AFT WAS FERRIED TO SBY FOR REPAIR. REPLACED ADAPTOR PLATE AND INSTALLED A NEW AC GENERATOR. (M) 2 H 7 2 4T RT A13NM 1997011600740 19970116 00740 WP 1997 1 16 97ZZZM77 1 19961217 A 5230 LS6868 DOOR SEAL DOUG DC8 DC851 3021920 WP CARGO DOOR PLUGGED A FXLA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 SO 19 508DC 45935 EN ROUTE ALB TO SDF, LOST CABIN PRESSURIZATION DURING CLIMB. INITIATED EMERGENCY DESCENT TO 10,000 FEET AND CONTINUED F LIGHT TO SDF. GROUND INSPECTION REVEALED MAIN CARGO DOOR SEAL VENT HOLES PARTIALLY PLUGGED AND NOTED RIGHT OVERWING DOO R AJAR. CLEARED SEAL VENT HOLES. RESECURED OVERWING DOOR. PRESSURIZED AIRCRAFT ON GROUND AND NO LEAKS WERE NOTED. RE TURNED AIRCRAFT TO SERVICE. (M) 2 L 7 4 4F 4A25 1997011600741 19970116 00741 WP 1997 1 16 97ZZZM78 1 19961213 A 3244 TIRES DOUG DC8 DC851 3021920 WP MLG BLOW OUT A FXLA O OTHER O OTHER LD LANDING 1 SO 19 508DC 62682 45935 PILOT REPORTED THAT DURING LANDING IN MIA, THREE TIRES WERE BLOWN DUE TO RUNWAY CONDITIONS (WET). GROUND INSPECTION OF AIRCRAFT REVEALED NO DISCREPANCIES PER SECTION 'A' OF THE DACO SPECIAL INSPECTINO HARD LANDING FORM. INSPECTION AND CHE CK OF THE ANTI-SKID AND SPOILER SYSTEM WAS ACCOMPLISHED AND FOUND TO OPERATE NORMAL. REPLACED 6 MAIN TIRES AND 2 NOSE T IRES AND RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 4 4F 4A25 1997011600742 19970116 00742 WP 1997 1 16 97ZZZM79 1 19961226 A 3310 BA170 BALLAST DOUG DC8 DC8F55 3021928 WP RT COCKPIT BURNED A FXLA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 19 55FB 45678 AFTER TAKEOFF MIA, EXPERIENCED SMOKE IN COCKPIT. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED A DE FECTIVE BALLAST AT THE FIRST OFFICERS FLUORESCENT LIGHT. REPLACED BALLAST AND RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 4 4F 4A25 1997011600743 19970116 00743 EU 1997 1 16 REXA96080 1 19961227 A 2611 SMOKE DETECTOR SAAB SF340 SF340A 7850100 EU LAVATORY FAILED A REXA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 25 325PX A1398 340A051 LAVATORY SMOKE LIGHT ON DURING TAXI OUT. REMOVED AND REPLACED LAVATORY SMOKE DETECTOR. (M) 2 L 7 2 4T RT A52EU 1997011600744 19970116 00744 EU 1997 1 16 REXA96078 1 19961220 A 6120 SENSOR 5035T27G04 SAAB SF340 SF340A 7850100 EU RT ENGINE FAILED A REXA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 25 346AM 340A032 CTOT WON'T HOLD LEFT ENGINE, AUTOCOARSEN LIGHT FLICKERS. REMOVED AND REPLACED NP SENSOR. (M) 2 L 7 2 4T RT A52EU 1997011600745 19970116 00745 EU 1997 1 16 REXA96077 1 19961220 A 2913 PUMP 4018501 SAAB SF340 SF340A 7850100 EU HYD SYSTEM FAILED A REXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 935MA 340A073 HYD PRESSURE DROPPED TO A 1000 PSI AFTER GEAR RETRACTION AND INTRANSIT LIGHT STAYED ILLUMINATED. REOVED AND REPLACED H YD PUMP. (M) 2 L 7 2 4T RT A52EU 1997011600746 19970116 00746 EU 1997 1 16 REXA96076 1 19961220 A 7722 CONNECTOR 897469621888 BAG JETSTM JETSTM3101 1500215 EU RT EGT LOOSE A REXA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 318PX 689 ON CLIMB, RIGHT EGT FAILURE. RESET PIN ON EGT HARNESS. (M) 2 L 7 2 4T RT A21EU 1997011600747 19970116 00747 EU 1997 1 16 SIMA963611 1 19961225 A 3350 3012001 BATTERY PACK SAFT AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 425MJ 0670 425 ORD - FLT 4321 - FORWARD EMERGENCY FLOOR LIGHTS WILL NOT RESET OR GO OUT WHEN SWITCH IS IN DISARM. RAI BATTERY PACK ASS EMBLYS. (M) 2 H 7 2 4T RT A53EU 1997011600748 19970116 00748 EU 1997 1 16 SIMA963631 1 19961228 A 3350 3011210 LIGHT AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 427MQ 330 091 ORD - FLT 4341 - EMERGENCY LIGHT ON STAIR AND CABIN EMERGENCY LIGHTS INOP. RAI'D EMERGENCY LIGHT ASSEMBLY FOR AIRSTAIR LIGHT AND BATTERY PACKS 10WL, 15WL AND 18WL. OPERATIONAL CHECK SATISFACTORY AIRCRAFT RTS. AIRCRAFT WAS RETURNED TO SER VICE. (M) 2 H 7 2 4T RT A53EU 1997011600749 19970116 00749 EU 1997 1 16 97ZZZM80 1 19961228 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 427MQ 330 091 ORD - FLT 4341 - EMERGENCY LIGHT ON STAIR AND CABIN EMERGENCY LIGHTS INOP. RAI'D EMERGENCY LIGHT ASSEMBLY FOR AIRSTAIR LIGHT AND BATTERY PACKS 10WL, 15WL AND 18WL. OPERATIONAL CHECK SATISFACTORY AIRCRAFT RTS. AIRCRAFT WAS RETURNED TO SER VICE. (M) 2 H 7 2 4T RT A53EU 1997011600750 19970116 00750 EU 1997 1 16 SIMA963612 1 19961226 A 3350 3011151 POWER SUPPLY AEROSP ATR42 ATR42300 8680920 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 971NA 4043 017 ORD - FLT 4340 - EMERGENCY LIGHTS INOP AT ROW 1. REPLACED EMERGENCY LIGHT POWER SUPPLY IAW ATR JOB CARD 33-51-21. AIRC RAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1997011600751 19970116 00751 NE 1997 1 16 Y2PA96007 2 19961218 A 7200 ENGINE AMD FALC20 FALCON 2720302 EU GE CF700 CF7002D2 30010 NE LEFT FLAMED OUT A A Y2PA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 GL 23 814AA 31 245U139 YIP - LT ENG FLAMED OUT DURING STEADY STATE CLIMB AT 36,000 FT. A/C DESCENDED AND THE ENG WAS AIRSTARTED PER THE CHECKL IST. A/C RETURNED, AND MADE A NORMAL TWO ENG LANDING. PRIOR TO THIS TEST FLT THE ENG UNDERWENT A HOT SECTION INSPECTIO N, INCLUDING REPLACEMENT OF THE STAGE 1 AND 2 TURBINE AIR NOZZLES AND COMBUSTION LINER. THE TURBINE ROTOR WAS DYNAMICAL LY BALANCED AND TURBINE CASINGS WERE MATCH GROUND TO THE ROTOR. THE FAN NOZZLE AND FAN EXIT GUIDE VANE WERE ALSO REPLAC ED. THE ENG SUCCESSFULLY PASSED THE MAX ALT ACCELERATION TEST AT 31,OOO FT BUT FAILED THE TEST AT 35,000 FT, PER THE GE MM THE A/C CEILING WILL BE RESTRICTED TO 31,000 FT FOR THE NEXT 836 HRS, AT WHICH TIME THE ENG WILL BE OVERHAULED. (M) 2 L 7 2 4F 4 F A7EU E7EA 1997011600752 19970116 00752 WP 1997 1 16 Y2PA96104 1 19961218 A 3230 RETRACT MECH DOUG DC9 DC915F 3022037 WP LT/RT MLG FROZE UP A Y2PA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 23 196US 47155 YIP - LANDING GEAR HANDLE FROZEN IN THE 'UP' POSITION. AFTER MISSED APPROACH, GEAR HANDLE OPERATED NORMALLY. INSPECTED AND FOUND ICE AND STANDING WATER IN BOTH MAIN GEAR WHEEL WELLS AND GEAR CONTROL VALVE AREA. REMOVED WATER AND ICE FROM BOTH WHEEL WELL AREAS. (M) 2 L 7 2 4F A6WE 1997011600753 19970116 00753 GL 1997 1 16 ZIAA96075 2 19961211 A 7230 6897606 BEARING SUPPORT LKHEED 188 188A 5262602 WP ALLSN 501D 501D13 03004 GL NR 2 ENGINE SEPARATED A A ZIAA E F A ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 5522 188A1033 501354 FWA - NR 2 ENGINE FIRE WARNING ILLUMINATED ON CLIMB-OUT. PULLED EMERGENCY SHUT DOWN HANDLE AND DISCHARGED FIRE BOTTLE. RETURNED TO FWA. FOUND REAR TURBINE BEARING SUPPORT SEPARATED AT MOUNT POINT. NO FIRE PRESENT BUT HOT EXHAUST GASES S ET OFF THE FIRE WARNING. A/C PREPARED FOR THREE ENGINE FERRY FLIGHT TO YIP WHERE THE ENGINE WLL BE REPLACED. A/C PRESE NTLY ON HOLD AT FWA FOR WEATHER. (M) 2 L 7 4 4T 4 T RT 4A22 E282 1997011600754 19970116 00754 NM 1997 1 16 TAOA129612 1 19961221 A 2781 WARNING LIGHTS BOEING 727 727225 1384077 NM LE FLAPS ILLUMINATED A TAOA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 15 923TS 20441 AFTER TAKEOFF LEADING EDGE AMBER LIGHTS WOULD NOT EXTINGUISH, RETURNED TO LGA AND LANDED FOR REPAIRS. INSPECTED ALL LEA DING EDGE DEVICES AND SWITCHES, ALL CHECK OK. OPERATED FLAPS SEVERAL TIMES AND COULD NOT DUPLICATE PROBLEM, FLAPS AND L EADING EDGE DEVICES OPERATES NORMAL PER MM 27-82-00. (M) 2 L 7 3 4F A3WE 1997011600755 19970116 00755 NM 1997 1 16 TAOA129610 1 19961220 A 5610 5717623112 WINDOW BOEING 727 727227 1384078 NM RT COCKPIT CRACKED A TAOA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 15 925TS 21244 IMMEDIATELY AFTER TAKEOFF R2 WINDOW CRACKED AND ARCED. PERFORMED ABNORMAL PROCEDURE AND RETURNED FOR LANDING. REPLACED R2 WINDOW PER MM 56-12-0. REPLACE R2 WINDOW HEAT CONTROLLER PER MM CHAPTER 30-41-12. (M) 2 L 7 3 4F A3WE 1997011600756 19970116 00756 NM 1997 1 16 TAOA129609 1 19961220 A 3220 65348784 APEX PIN BOEING 727 727225 1384077 NM NLG FAILED A TAOA O OTHER E VIBRATION/BUFFET LD LANDING 1 EA 15 919TS 24876 20447 DURING LANDING ROLL, AIRCRAFT BEGAN TO SHIMMY WILDLY. FOUND NOSE LANDING GEAR TORQUE LINK APEX DISCONNECTED. LOCKING M ECHANISM DEFECTIVE, INSPECTED TORQUE LINKS AND GEAR ASSEMBLY, NO DAMAGE FOUND. REPLACED TORQUE LINKS APEX PIN PER MM CH APTER 32-21-21. (M) 2 L 7 3 4F A3WE 1997011600757 19970116 00757 EA 1997 1 16 COEA9622202 1 19961211 A 2420 7930040041 TRANSFORMER FRCHLD F27 F27F 3373008 EA RIGHT FAILED A COEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 13 222DG 442 31 WHILE EN ROUTE FROM YVR-OAK, CO-PILOT'S DME INDICATOR DISPLAY WENT BLANK. LATER THE NR 1 DE-ICING GENERATOR FAILURE LIG HT ILLUMINATED ACCOMPANIED BY A SLIGHT SMELL OF SMOKE. CREW MADE A PRECAUTIONARY LANDING IN PDX. THE AIRCRAFT LANDED W ITHOUT INCIDENT. REMOVED AND REPLACED NR 2 DME AND NR 1 ISOLATION TRANSFORMER. DURING OPS CHECK WINDSHIELD HEAT C/B PO PPED WHEN SELECTED ON HIGH. FOUND NR 2 WINDSHIELD HEAT HI/LOW RELAY SHORTED TO GROUND CAUSING SEVERAL WIRES TO BURN. M AINTENANCE REPAIRED AND REPLACED BURNED WIRING. REMOVED AND REPLACED HI/LOW RELAY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T 7A1 1997011600758 19970116 00758 EA 1997 1 16 97ZZZM81 1 19961211 A 3040 9565H51 RELAY FRCHLD F27 F27F 3373008 EA RIGHT FAILED A COEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 13 222DG 442 31 WHILE EN ROUTE FROM YVR-OAK, CO-PILOT'S DME INDICATOR DISPLAY WENT BLANK. LATER THE NR 1 DE-ICING GENERATOR FAILURE LIG HT ILLUMINATED ACCOMPANIED BY A SLIGHT SMELL OF SMOKE. CREW MADE A PRECAUTIONARY LANDING IN PDX. THE AIRCRAFT LANDED W ITHOUT INCIDENT. REMOVED AND REPLACED NR 2 DME AND NR 1 ISOLATION TRANSFORMER. DURING OPS CHECK WINDSHIELD HEAT C/B PO PPED WHEN SELECTED ON HIGH. FOUND NR 2 WINDSHIELD HEAT HI/LOW RELAY SHORTED TO GROUND CAUSING SEVERAL WIRES TO BURN. M AINTENANCE REPAIRED AND REPLACED BURNED WIRING. REMOVED AND REPLACED HI/LOW RELAY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T 7A1 1997011600759 19970116 00759 NM 1997 1 16 TSAA9653096 1 19961221 A 5320 WEB BOEING 737 7372Q9 138448M NM BS 706-714 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 809AL 21720 DURING SCHEDULED INSPECTION OF FUSELAGE DETECTED MULTIPLE CRACKS ON BL 24.5R WEBBING BETWEEN BS 706 AND 714, CRACKS ORIG INATE FROM RIVET HOLES. REPAIRED PER ECO 2763. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1997011600760 19970116 00760 WP 1997 1 16 HAL960110 1 19961111 A 5320 INTERCOSTAL DOUG DC10 DC1010 3022110 WP BS 464 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 116AA 75043 46516 DURING C-CHECK, FOUND CORROSION ON INTERCOSTAL BETWEEN VERTICAL FRAMES ABOVE THE ACCESS DOOR 115AZ AT STATION 464. INST ALLED ANGLE DOUBLER PER SRM 53-00-01 VOL 1. (M) 2 L 7 3 4F A22WE 1997011600761 19970116 00761 WP 1997 1 16 HAL960109 1 19961111 A 5720 FALSE SPAR DOUG DC10 DC1010 3022110 WP WS 164 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 116AA 75043 75043 46516 DURING C-CHECK, FOUND CORROSION ON THE FALSE SPAR AFT INBOARD SIDE AT STATION XORS 164 TO STATION XORS 197. INSTALLED ' L' ANGLE DOUBLERS ON UPPER AND LOWER FALSE SPAR PER ESO 7349, DATED 11-8-96. (M) 2 L 7 3 4F A22WE 1997011600762 19970116 00762 WP 1997 1 16 HAL960107 1 19961108 A 5320 CHANNEL DOUG DC10 DC1010 3022110 WP BS 1139 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 116AA 46516 DURING C-CHECK, FOUND THE 'U' CHANNEL SUPPORT HAS CORROSION FROM LONGERON 51L TO 51R ON THE BELL FRAME AT STATION 1139. SPLICED IN NEW SECTION OF 'U' CHANNEL PER SRM 53-30-00. (M) 2 L 7 3 4F A22WE 1997011600763 19970116 00763 WP 1997 1 16 HAL960105 1 19961111 A 5320 CABLE TRACK DOUG DC10 DC1010 3022110 WP BS 1099 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 116AA 75043 46516 DURING C-CHECK, FOUND CORROSION AT AFT END OF RIGHT CABLE TRACK. INSTALLED NEW TRACK PER SRM 51-01-00-05. (M) 2 L 7 3 4F A22WE 1997011600764 19970116 00764 WP 1997 1 16 HAL960104 1 19961111 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP E/E COMPT CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 116AA 75043 46516 DURING C-CHECK, FOUND CORROSION ON LONGERON 48R AND INTERCOSTAL AT LONGERON 48R. INSTALLED NEW INTERCOSTAL AND LONGERON 48R PER AARD 51-01-00. (M) 2 L 7 3 4F A22WE 1997011600765 19970116 00765 WP 1997 1 16 HAL960103 1 19961109 A 5751 ARC03291 CASTING DOUG DC10 DC1010 3022110 WP LT INBD AILERON CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 116AA 46516 DURING C-CHECK, FOUND LEFT INBOARD AILERON ACTUATOR CASTING CRACKED AT THE LOWER AFT INBOARD END. REPAIRED PER ESO 7349 DATED 11-1-96. (M) 2 L 7 3 4F A22WE 1997011600766 19970116 00766 WP 1997 1 16 HAL960102 1 19961108 A 5320 SHEAR TIE DOUG DC10 DC1010 3022110 WP FWD CARGO PIT CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 116AA 75043 46516 DURING C-CHECK, FOUND CORROSION ON SHEAR TIE BELOW FRAME 979 ON AFT SIDE. REMOVED AND REPLACED SHEAR TIE PER SRM 51-01- 00-5. (M) 2 L 7 3 4F A22WE 1997011600767 19970116 00767 WP 1997 1 16 HAL960101 1 19961108 A 5720 TRAP PANEL DOUG DC10 DC1010 3022110 WP RT MLG CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 116AA 75043 46516 DURING C-CHECK, FOUND CORROSION IN THE AREA FOR BARREL NUTS OF THE TRAPEZOIDAL PANEL RIGHT MLG. INSTALLED INBOARD AND O UTBOARD BARREL NUT BUSHINGS PER SRM 57-20-00. BLENDED AREAS PER ESO 7349 DATED 11/1/96. (M) 2 L 7 3 4F A22WE 1997011600768 19970116 00768 WP 1997 1 16 HAL960097 1 19961104 A 5320 SHEAR TIE DOUG DC10 DC1010 3022110 WP BS 939 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 116AA 75043 46516 DURING C-CHECK, FOUND CORROSION ON AFT SIDE OF SHEAR TIE BELOW FRAME AT STATION 939, LONGERON 49 RIGHT TO 49 LEFT. REMO VED CORRODED SECTION OF SHEAR TIE AND INSTALLED NEW SECTION PER SRM 53-30-00. (M) 2 L 7 3 4F A22WE 1997011600769 19970116 00769 WP 1997 1 16 HAL960132 1 19961209 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 862/864 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 122AA 73433 46522 DURING C-CHECK, FOUND FUSELAGE SKIN BULGED AND FASTENERS PULLED THROUGH SHOWING CORROSION UNDER SKIN AT LONGERON 43R AT FORWARD END OF FORWARD CARGO DOOR STATION 462 TO 474. REMOVED CORROSION AND INSTALLED CLASS 1 DOUBLER PER ESO 7349, DAT ED 12/5/96. (M) 2 L 7 3 4F A22WE 1997011600770 19970116 00770 WP 1997 1 16 HAL960130 1 19961209 A 5711 SPAR DOUG DC10 DC1010 3022110 WP WS 376 CORROSION A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 122AA 73433 46522 DURING C-CHECK, FOUND CORROSION AROUND HI LOCK FASTENERS AT FRONT SPAR LOCATION LOWER SKIN AT RIGHT WING AT STATION XORS 376. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER ESO 7349, DATED 12/5/96. (M) 2 L 7 3 4F A22WE 1997011600771 19970116 00771 WP 1997 1 16 HAL960129 1 19961209 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 1330-1340 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 122AA 73433 46522 DURING C-CHECK, FOUND CORROSION ON THE LONGERON OUTBOARD OF THE LOWER LEG OF 51L AT STATION 1330 TO 1340. REPAIRED LONG ERON PER SRM 53-10-00. TREATED AND PRIMED PER SRM 51-21-01. (M) 2 L 7 3 4F A22WE 1997011600772 19970116 00772 WP 1997 1 16 HAL960128 1 19961209 A 5320 SHEAR TIE DOUG DC10 DC1010 3022110 WP BS 1206 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 122AA 73433 46522 DURING C-CHECK, FOUND CORROSION ON THE FORWARD SIDE OF THE SHEAR TIE AT STATION 1207, STRINGER 51 AND 52L. REPAIRED SHE AR TIE PER SRM 53-30-00. TREATED AND PRIMED AREA PER SRM 51-21-01. (M) 2 L 7 3 4F A22WE 1997011600773 19970116 00773 WP 1997 1 16 HAL960127 1 19961205 A 5720 ANGLE DOUG DC10 DC1010 3022110 WP WS 164/171 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 122AA 73433 46522 DURING C-CHECK, FOUND CORROSION ON THE FORWARD INBOARD SIDE OF THE FALSE SPAR ON THE LEFT WING AT STATION XORS 164 TO 17 1. INSTALL NEW REPAIR ANGLE WET, ALODINED AND PRIMED PARTS AND INSTALLED HI LOCKS PER ESO 7349, DATED 12/5/96. (M) 2 L 7 3 4F A22WE 1997011600774 19970116 00774 WP 1997 1 16 HAL960125 1 19961204 A 5320 PANEL DOUG DC10 DC1010 3022110 WP BS 1370 CORROSION A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 122AA 73433 46522 DURING C-CHECK, FOUND HEAVY INTERGRANNULAR CORROSION ON THE LOWER OUTBOARD CORNER OF THE LEFT MAIN GEAR WHEEL WELL SLANT PANEL. REPAIRED PER ENGINEERING INSTRUCTIONS ON ESO 7349, DATED 12/4/96. (M) 2 L 7 3 4F A22WE 1997011600775 19970116 00775 WP 1997 1 16 HAL960124 1 19961204 A 5720 SPLICE DOUG DC10 DC1010 3022110 WP WS 264 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 122AA 73433 46522 SPLICE PLATE HAS CORROSION DAMAGE ON THE FALSE SPAR FORWARD SIDE JUST OUTBOARD OF NR 1 SPOILER ACTUATOR ON THE RIGHT WIN G TE AT STATION XORS 264. REPAIRED CORROSION DAMAGE RED SRM VOL 1, CHAPTER 51 STR GENERAL AND ESO 7349, REF DATED 12/3/ 96. (M) 2 L 7 3 4F A22WE 1997011600776 19970116 00776 WP 1997 1 16 HAL960123 1 19961204 A 5720 CLIP DOUG DC10 DC1010 3022110 WP WS 356 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 122AA 73433 46522 DURING C-CHECK, FOUND THE PICK UP CLIP AT THE FALSE SPAR FORWARD OF THE INBOARD EDGE OF THE AILERON CLIP ON THE FORWARD SIDE OF THE FALSE SPAR ON TEH RIGHT WING TRAILING EDGE HAS CORROSION DAMAGE. REPAIRED THE CORRODED AREA PER SRM VOL 1, CHAPTER 57-00-01, FIG 3 SHEET 2 AND ESO 7349 REF DATED 12/3/96. (M) 2 L 7 3 4F A22WE 1997011600777 19970116 00777 WP 1997 1 16 HAL960122 1 19961204 A 5311 BELTFRAME DOUG DC10 DC1010 3022110 WP BS 939 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 122AA 73433 46522 DURING C-CHECK, FOUND CORROSION UNDER A PREVIOUSLY INSTALLED DOUBLER AT FORWARD CARGO COMPARTMENT FUSE STATION 939, STRI NGER 51 LEFT AND RIGHT. REMOVED DAMAGED SECTION OF BELT FRAME AND SPLICED IN NEW SECTION PER SRM 53-30-00, PAGE 15. (M ) 2 L 7 3 4F A22WE 1997011600778 19970116 00778 WP 1997 1 16 HAL960121 1 19961204 A 5313 STRINGER DOUG DC10 DC1010 3022110 WP BS 814-820 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 122AA 73433 46522 DURING C-CHECK, FOUND CORROSIONI ON STRINGER 52 FROM STATION 814 TO 820 IN THE FORWARD CARGO COMPARTMENT. REMOVED CORRO DED STRINGER AND REPLACED WITH ATTACHED SPLICES PER AARD 51-01-00. (M) 2 L 7 3 4F A22WE 1997011600779 19970116 00779 WP 1997 1 16 HAL960119 1 19961203 A 2550 CHAIN DRV TRACK DOUG DC10 DC1010 3022110 WP BS 879 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 122AA 73433 46522 DURING C-CHECK, FOUND THE INBOARD CHAIN DRIVE TRACK TRAY IN THE FORWARD CARGO COMPARTMENT CORRODED AT THE FORWARD END ON THE UNDERSIDE. REPLACED THE CHAIN DRIVE TRACK PER AARD 53-10-00-1. (M) 2 L 7 3 4F A22WE 1997011600780 19970116 00780 WP 1997 1 16 HAL960118 1 19961203 A 5320 ANGLE DOUG DC10 DC1010 3022110 WP BS 1968-1970 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 122AA 73433 46522 DURING C-CHECK, FOUND THE AFT CARGO WALL AND CEILING SUPPORT ANGLE HAS CORROSION AROUND SCREW HOLES. INSTALLED NEW ANGL E PER ESO 7349 AND AARD 53-01-00-05. (M) 2 L 7 3 4F A22WE 1997011600781 19970116 00781 WP 1997 1 16 HAL960117 1 19961127 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 1964/1965 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 122AA 73433 46522 DURNG C-CHECK, FOUND CORROSION ON LONGERON 51R BETWEEN STATION 1964 AND STATION 1975. INSTALLED LONGERON SPLICE REF SRM 53-10-00. ALL PARTS ALODINED, PRIMED AND SEALED PER SRM 51-21-01. (M) 2 L 7 3 4F A22WE 1997011600782 19970116 00782 WP 1997 1 16 HAL960116 1 19961126 A 5320 ANGLE DOUG DC10 DC1010 3022110 WP BS 1701 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 122AA 73433 46522 DURING C-CHECK, FOUND THE CENTER CARGO FLOORBOARD SUPPORT WITH DEEP CORROSION ON THE AFT SIDE BETWEEN THE RIGHT TRAY AND THE RT FORWARD DRIVE CHAIN CHANNEL. INSTALLED NEW FLOORBOARD SUPPORT ANGLE PER AARD 51-01-00-05. ALODINED AND PRIMED PER SRM 51-21-00-VOL 1 STATION 1701. (M) 2 L 7 3 4F A22WE 1997011600783 19970116 00783 WP 1997 1 16 HAL960115 1 19961125 A 5320 ROLLER TRAY DOUG DC10 DC1010 3022110 WP BS 1701/1781 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 122AA 73433 46522 DURING C-CHECK, FOUND THE LEFT TRAY IN THE CENTER CARGO FLOOR HAS CORROSION INSIDE AT SEVERAL AREAS. REMOVED DAMAGED TR AY AND INSTALLED NEW LEFT TRAY PER AARD 51-01-00-05. (M) 2 L 7 3 4F A22WE 1997011600784 19970116 00784 WP 1997 1 16 HAL960114 1 19961125 A 5320 LONGERON DOUG DC10 DC1010 3022110 WP BS 937/959 CORROSION A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 122AA 73433 46522 DURING C-CHECK, FOUND CORROSION INSIDE AND ON TOP OF LONGERON 52 AND ON SPLICE PLATES AT FUSE STATION 937 AND 959. REMO VED DAMAGED LONGERON. SPLICE NEW SECTION IN PER MM REF SRM 53-10-00. (M) 2 L 7 3 4F A22WE 1997011600785 19970116 00785 WP 1997 1 16 HAL960113 1 19961122 A 5720 ANGLE DOUG DC10 DC1010 3022110 WP WS 336 CORROSION A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 122AA 73433 46522 DURING C-CHECK, FOUND THE PICK UP ANGLE ON THE FORWARD SIDE OF THE FALSE SPAR AT THE OUTSIDE OF NR 1 SPOILER HINGE HAS A BRACKET WITH CORROSION DAMAGE, RT WING. INSTALLED NEW PICK UP ANGLE PER SRM 51-10-00-01. (M) 2 L 7 3 4F A22WE 1997011600786 19970116 00786 WP 1997 1 16 HAL960112 1 19961120 A 5320 FLOOR BEAM DOUG DC10 DC1010 3022110 WP BS 1841 CORRODED ANGLE A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 122AA 73433 73433 46522 DURING C-CHECK, FOUND CORROSION ON FLOOR BEAM ANGLE TOP FLANGE AT FUSE STATION 1841 BETWEEN LONGERON 46R AND LONGERON 45 R. REPAIRED FRAME CAP ANGLE AT STATION 1841 BETWEEN LONGERON 46R AND 45R REF SRM 53-30-00 FIG 8. ALODINED AND PRIMED R ED SRM 51-21-01. (M) 2 L 7 3 4F A22WE 1997011600787 19970116 00787 WP 1997 1 16 HAL960111 1 19961118 A 5320 DOUBLER DOUG DC10 DC1010 3022110 WP BS 1851.85/1868 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 122AA 46522 DURING C-CHECK, FOUND CORROSION ON SKIN DOUBLER BETWEEN FUSELAGE STATION 1851.85 AND 1868 AT LONGERON 52 LEFT. REMOVED CORRODED DOUBLER, FABRICATED AND INSTALLED NEW DOUBLER PER SRM 51-10-00-01. (M) 2 L 7 3 4F A22WE 1997011600788 19970116 00788 WP 1997 1 16 HAL960131 1 19961209 A 5320 CHANNEL DOUG DC10 DC1010 3022110 WP BS 879 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 122AA 73433 46522 DURING C-CHECK, FOUND CORROSION ON SUPPORT CHANNEL UNDERNEATH NR 2 ROLLER TRAY AFT END IN THE LOWER GALLEY. INSTALLED N EW SUPPORT CHANNEL UNDER NR 2 ROLLER TRAY PER SRM 51-20-00. (M) 2 L 7 3 4F A22WE 1997011600789 19970116 00789 WP 1997 1 16 EIAA9690 1 19960426 A 5320 INTERCOSTAL DOUG DC9 DC932F 3022067 WP BS 256-945 DAMAGE A EIAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 932F 47355 DURING C-CHECK INSPECTION, DISCOVERED DAMAGE ON NUMEROUS INTERCOSTALS LOCATED BETWEEN STATIONS 256 AND 945. LEFT AND RI GHT SIDES, CAUSED BY PERSONNEL ERROR (WORKMANSHIP). INTERCOSTALS WERE REMOVED AND REPLACED WITH FABRICATED INTERCOSTALS . REFERENCE EVERGREEN INTERNATIONAL AIRLINE ENGINEERING CHANGE/REPAIR AUTHORIZATION NR ECRA 932-53-029-2. (M) 2 L 7 2 4F A6WE 1997011600790 19970116 00790 WP 1997 1 16 EIAA9692 1 19960426 A 5320 59266417 STRAP DOUG DC9 DC932F 3022067 WP BS 218 DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47355 MZJ - DURING C-CHECK INSPECTION, DISCOVERED DRILL BIT DAMAGE TO BOTH THE PRIMARY AND SECONDARY 9G NET BRACE AT RIGHT STA TION 218 AND LEFT AND RIGHT STATION 256. DAMAGE WAS REPAIRED PER EVERGREEN INTERNATIONAL AIRLINES ENGINEERING CHANGE, R EPAIR AUTHORIZATION NR ECRA 932-53-031-2. (M) 2 L 7 2 4F A6WE 1997011600791 19970116 00791 WP 1997 1 16 97ZZZM82 1 19960426 A 5320 592377111 STRAP DOUG DC9 DC932F 3022067 WP BS 256 DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47355 MZJ - DURING C-CHECK INSPECTION, DISCOVERED DRILL BIT DAMAGE TO BOTH THE PRIMARY AND SECONDARY 9G NET BRACE AT RIGHT STA TION 218 AND LEFT AND RIGHT STATION 256. DAMAGE WAS REPAIRED PER EVERGREEN INTERNATIONAL AIRLINES ENGINEERING CHANGE, R EPAIR AUTHORIZATION NR ECRA 932-53-031-2. (M) 2 L 7 2 4F A6WE 1997011600792 19970116 00792 WP 1997 1 16 EIAA9693 1 19960429 A 5311 FRAME DOUG DC9 DC932F 3022067 WP FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47355 MZJ - DURING MAINTENANCE AT EVERGREEN AIR CENTER, NUMEROUS LOCATIONS IN THE OVERWING FRAMES WERE FOUND TO HAVE DRILL BIT DAMAGE, PRIMARILY TO THE INBOARD CHORDS. LOCATIONS ARE LEFT AND RIGHT STATIONS 598-737. DAMAGE WAS REPAIRED PER EVERG REEN INTERNATIONAL AIRLINES ENGINEERING CHANGE. REPAIR AUTHORIZATION NR ECRA 932-53-028-2. (M) 2 L 7 2 4F A6WE 1997011600793 19970116 00793 NM 1997 1 16 EIAA9697 1 19961212 A 3020 65B901821 DUCT BOEING 747 747132 1384882 NM NR 1 PYLON CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 DURING PART ROB ACTION INSPECTION, FOUND NR 1 PYLON ANTI-ICE DUCT CRACKED NEAR PICKUP FOR DUCT OVERPRESSURE SWITCH. REP LACED DUCT ASSEMBLY. (M) 2 L 7 4 4F A20WE 1997011600794 19970116 00794 NM 1997 1 16 EIAA9696 1 19961211 A 3020 65B901821 DUCT BOEING 747 747273C 1384896 NM NR 1 PYLON CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 DURING SERVICE CHECK INSPECTION, FOUND NR 1 PYLON ANTI-ICE DUCT SPLIT OPEN NEAR PICKUP FOR DUCT OVERPRESSURE SWITCH. RE PLACED DUCT ASSEMBLY. (M) 2 L 7 4 4F A20WE 1997011600795 19970116 00795 NM 1997 1 16 EIAA9695 1 19961210 A 5743 65B0189712 SUPPORT FITTING BOEING 747 747121 1384871 NM RT MLG CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 480EV 20348 SAT - DURING MAINTENANCE OF LANDING GEAR, THE RIGHT WING GEAR SIDE SUPPORT STRUT ATTACHMENT FITTING, AT RBS 1350, RBL 98 WL 195, A 3.5 INCH CRACK WAS DETECTED. STOP DRILLED CRACK PER BOEING FAX DES-SAT-96-0006RE OF 11 DEC 96. HIGH FREQ ED DY CURRENT TO VERIFY CRACK END WAS REMOVER. CUT .01325 INCH INSURANCE CUT OF STOP DRILL PER SRM 51-70-1. VERIFIED INTE GRITY OF ADJACENT BOLT BY PERFORMING A TORQUE CHECK AS PER THE DRAWING AND SRM GUIDE LINES. WILL REINSPECTOR FOR CRACK PROGRESSION EVER TEN FLIGHT CYCLES. (M) 2 L 7 4 4F A20WE 1997011600796 19970116 00796 NM 1997 1 16 EIAA9694 1 19961208 A 2782 1789002 ACTUATOR BOEING 747 747212B 1384886 NM LE FLAP SEIZED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 485EV 20712 JFK - DURING MAINTENANCE OPERATIONAL CHECKS OF THE LEADING EDGE DEVICES, NR 16 RIGHT WING LEADING EDGE FLAP LOCKED UP CA USING EXTENSIVE DAMAGE TO LEADING EDGE FLAP. FOUND OUTBOARD ACTUATOR SEIZED, NEXT INBOARD ACTUATOR BINDING, NR 16 TORQU E TUBE SHEARED AND SYSTEM DIODES X111 AND X112 BAD APPLYING BRAKE POWER AT ALL TIMES. REPLACED PNEUMATIC DRIVE ASSEMBLY , 2 FLAP ROTARY ACTUATOR. LEADING EDGE FLAP ASSEMBLY, TORQUE DRIVE SHAFT AND 2 DIODES. (M) 2 L 7 4 4F A20WE 1997011600797 19970116 00797 SO 1997 1 16 C2XA96CL044 1 19961203 A 2751 3069001017L ANNUNCIATOR EMB 120 EMB120RT SO E/E BAY FAILED A C2XA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SW 09 58733 13575 13575 68 120197 CLE - FLT 4244 - THE CREW REPORTED THAT AFTER TAKEOFF THEY RECEIVED A FLAP CONTROL FAULT WHICH WOULD NOT RESET. THE AIR CRAFT RETURNED TO BASE. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE FLAP ANNUNCIATOR ASSEMBLY. OPE RATIONAL CHECKS WERE GOOD IAW EMB120 MM 27-50-00. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1997011600798 19970116 00798 EU 1997 1 16 C2XA96IA295 1 19961206 A 5347 S5367800123802 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 97841 280 IAH - DURING C-CHECK INSPECTION, THE RIGHT OUTBOARD SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLAC ED THE AFFECTED PORTION OF SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1997011600799 19970116 00799 EU 1997 1 16 C2XA96IA296 1 19961206 A 5315 S53672406208 FLOOR BEAM AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 97841 280 IAH - DURING C-CHECK INSPECTION, FRAME 36 FLOOR BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REPAIRED THE FLORO BEAM USIN G A SPLICE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1997011600800 19970116 00800 SO 1997 1 16 C2XA96IA297 1 19961213 A 5347 12026864007 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17720 120142 IAH - DURING C-CHECK INSPECTION, THE LEFT FLOOR AFT SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLAC ED THE AFFECTED PORTION OF SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1997011600801 19970116 00801 SO 1997 1 16 C2XA96CL045 1 19961216 A 3010 29S7D513525 DE-ICE BOOT EMB 120 EMB120RT SO LT WING TORN A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 59708 4479 125CD 120098 CLE - FLT 3176 - CREW REPORTED THAT AFTER TAKEOFF ALL AIRCRAFT DE-ICE BOOTS FAILED. AIRCRAFT RETURN TO STATION. MAINTE NANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE LEFT INBOARD WING DE-ICE BOOT IAW EMB-120 MM 30-10-01. OPERAT IONAL CHECKS WERE GOOD, AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1997011600802 19970116 00802 SO 1997 1 16 C2XA96CL047 1 19961219 A 3230 12032770002 ROLLER ASSEMBLY EMB 120 EMB120RT SO NLG LACK OF LUBE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 15725 120173 CLE - FLT 3199 - CREW REPORTED THAT AFTER TAKEOFF AND GEAR RETRACTION THE NOSE GEAR A/B RED LIGHTS STAYED ILLUMINATED AS SOCIATED WITH A AIRCRAFT VIBRATION. AIRCRAFT RETURNED TO BASE. MAINTENANCE INSPECTED AIRCRAFT AND CLEANED AND LUBRICAT ED THE UPLOCK HOOK ROLLER ASSEMBLY, ALL OPERATIONAL CHECKS WERE GOOD IAW EMB 120MM 32-30-00. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 2 4T RT A31SO 1997011600803 19970116 00803 SO 1997 1 16 C2XA96CL046 1 19961219 A 3260 922FS2A6NZ735 PROX SWITCH EMB 120 EMB120RT SO NLG DIRTY A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 15725 120173 CLE - FLT 3283 - CREW REPORTED THAT AFTER TAKEOFF AND GEAR RETRACTION, THE NOSE LANDING GEAR A/B RED LIGHTS STAYED ILLUM INATED ASSOCIATED WITH A AIRCRAFT VIBRATION. AIRCRAFT RETURNED TO BASE. MAINTENANCE INSPECTED AIRCRAFT AND CLEANED THE NOSE LANDING GEAR PROXIMITY SWITCHES, ALL OPERATIONAL CHECKS WERE GOOD IAW EMB 120 MM 32-30-00. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1997011600804 19970116 00804 EU 1997 1 16 C2XA96IA298 1 19961219 A 5315 S53672408202800 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15823 165 IAH - DURING C-CHECK INSPECTION, FRAME 39 FLOOR BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFF ECTED FLOOR BEAM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1997011600805 19970116 00805 EU 1997 1 16 C2XA96IA299 1 19961219 A 5315 S5367240720202 FLOOR BEAM AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15823 165 IAH - DURING C-CHECK INSPECTION, THE FLOOR BEAM AT FRAME 38 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOOR BEAM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1997011600806 19970116 00806 EU 1997 1 16 C2XA96IA300 1 19961219 A 5315 S5367240620802 FLOOR BEAM AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15823 165 IAH - DURING C-CHECK INSPECTION, FRAME 36 FLOOR BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFF ECTED FLOOR BEAM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1997011600807 19970116 00807 EU 1997 1 16 C2XA96IA302 1 19961219 A 5315 S536724082021300 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15823 165 IAH - DURING C-CHECK INSPECTION, THE FLOOR BEAM AT FRAME 36 (CENTER) WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOOR BEAM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1997011600808 19970116 00808 EU 1997 1 16 C2XA96IA301 1 19961219 A 5230 S52376114205 SUPPORT AEROSP ATR42 ATR42320 8680930 EU CARGO DOOR CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15823 165 IAH - DURING C-CHECK INSPECTION, THE CARGO DOOR ACTUATOR SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLA CED THE AFFECTED SUPPORT AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1997011600809 19970116 00809 NE 1997 1 16 ORJA96113 2 19961203 A 7230 500091601 LOCK RING DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE C1 BLADE CRACKED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 871RA 12011 49788 725441 FOUND C-1 BLADE LOCK RING CRACKED AT PULL HOLE APPROXIMATELY TWO INCHES FROM END. REPLACED C-1 BLADE LOCK RING. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 1997011600810 19970116 00810 WP 1997 1 16 ORJA96105 1 19961122 A 3260 SENSORS DOUG DC9 DC982 3022082 WP NLG REQ AJUST A ORJA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 11 841RA 49421 NOSE GEAR UNSAFE INDICATION ON GROUND AND AFTER RETRACTION. ADJUSTED DOWN AND UPLOCK SENSORS ON NOSE GEAR AND SWUNG A T OTAL OF SIX TIMES. OPS NORMAL. (M) 2 L 7 2 4F A6WE 1997011600811 19970116 00811 WP 1997 1 16 ORJA96106 1 19961124 A 3260 PROX SENSOR DOUG DC9 DC982 3022082 WP NLG OUT OF ADJUST A ORJA O OTHER N FALSE WARNING CL CLIMB 1 WP 11 841RA 49421 AFTER TAKEOFF AT SJC, NOSE GEAR UNSAFE LIGHT REMAINED ON. AFTER PERFORMING ABNORMALS CHECKLIST LIGHT REMAINED ON. AFTE R LEVELING AT FL 330 FEET LIGHT WENT OUT. ADJUSTED PROX SENSOR D1-32 AND PERFORMED GEAR SWING TEST IAW MM 32-60-00. OP S CHECKS GOOD. (M) 2 L 7 2 4F A6WE 1997011600812 19970116 00812 WP 1997 1 16 ORJA96108 1 19961128 A 3350 41B004AD073 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 872RA 49793 CEILING PANEL EMERGENCY LIGHTS INOP AT 11 - 17 SECTIONS. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY FOR SECTION 11 - 17. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1997011600813 19970116 00813 WP 1997 1 16 ORJA96109 1 19961130 A 3350 41B004AD073 BATTERY EA1D13D3 DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 875RA 53182 GROUP OF EMERGENCY OVERHEAD LIGHTS NEAR AISLE 20 WILL NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1997011600814 19970116 00814 WP 1997 1 16 ORJA96110 1 19961203 A 3350 60030451 BATTERY PACK GRIMES 60030451 DOUG DC9 DC987 3022087 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 751RA 49779 EMERGENCY AISLE LIGHTS WILL NOT LIGHT WITH SWITCH IN 'ON' POSITION. REMOVED AND REPLACED AFT EMERGENCY LIGHT POWER SUPP LY. AISLE LIGHTS OPS NORMAL. (M) 2 L 7 2 4F RT A6WE 1997011600815 19970116 00815 WP 1997 1 16 ORJA96111 1 19961203 A 3397 WIRE DOUG DC9 DC987 3022087 WP CABIN BROKEN A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 EMERGENCY LIGHTS INOP AT ROW 26 DEF AND AT ROW 20 DEF. REATTACHED BROKEN WIRE AT LOWER FLOOR/SEAT ATTACH POINT. OPS CH ECK NORMAL. (M) 2 L 7 2 4F RT A6WE 1997011600816 19970116 00816 WP 1997 1 16 ORJA96112 1 19961202 A 3350 FUSE DOUG DC9 DC983 3022083 WP CABIN FAILED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 EMERGENCY LIGHTS IN EMPENNAGE INOP. FOUND FUSE BLOWN. REMOVED AND REPLACED SAME, OPS NORMAL. (M) 2 L 7 2 4F RT A6WE 1997011600817 19970116 00817 WP 1997 1 16 ORJA96115 1 19961206 A 3246 26088911 WHEEL ASSY DOUG DC9 DC983 3022083 WP NR 3 MLG FAILED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 880RA 38076 53186 NR 3 MAIN WHEEL THROUGH-BOLT SHEARED OFF. REPLACED TIRE AND WHEEL ASSEMBLY, WITH TWA BORROWED PART. (M) 2 L 7 2 4F RT A6WE 1997011600818 19970116 00818 NE 1997 1 16 VTZA96445 2 19961217 A 7260 CHIP LIGHT JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE LT ENGINE ILLUMINATED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 313UE 41026 FLT 6371 - EWR-IAD - ABORTED TAKEOFF DUE LEFT ENGINE OIL CONTAMINATION CAPTION LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND FOUND ONE SMALL SLIVER ON CHIP DETECTOR, SLIVER WITHIN LIMITS, GROUND RAN AND OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 4 T RT A41NM E18NE 1997011600819 19970116 00819 EU 1997 1 16 VTZA96443 1 19961216 A 2422 PC125123B INVERTER JETAIR JETSTM JETSTM4101 1500501 EU RIGHT FAILURE A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 317UE 41031 FLT 6266 - IAD-BTV - DURING CRUISE, AN UNSCHEDULED LANDING DUE TO RIGHT IVERTER FAILURE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED, REMOVED AND REPLACED RIGHT INVERTER, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1997011600820 19970116 00820 EU 1997 1 16 VTZA96442 1 19961214 A 7712 8972605M AP/P BOX JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE FAILED A VTZA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 27 310UE 41028 FLT 6418 - IAD-BOS - DURING TAXI, RETURNED TO GATE DUE TO RIGHT IEC WARNING LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED AP/P BOX, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1997011600821 19970116 00821 1997 1 16 VTZA96441 4 19961214 A 3414 39948B2236 AIRSPEED IND BAG JETSTM JETSTM3201 1500217 EU NR 1 STUCK A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 480UE 894 FLT 6193 - IAD-JFK - DURING CLIMB, MADE AN UNSCHEDULED LANDING DUE NR 1 AIRSPEED INDICATOR STUCK AT 220 KTS. AIRCRAFT R ETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED AIRSPEED INDICATOR, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1997011600822 19970116 00822 EU 1997 1 16 VTZA96440 1 19961213 A 7712 TQ SIG COND JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE MALFUNCTIONED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 325UE 41063 FLT 6337 - IAD-EWR - ABORTED TAKEOFF DUE TO LEFT ENGINE WOULD ONLY MAKE 87 PERCENT TORQUE. AIRCRAFT RETURNED TO GATE WI TH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND SWAPPED BRIDGES ON BOTH ENGINES SIGNAL CONDITIONERS THREW IEC, OPS CH ECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1997011600823 19970116 00823 EU 1997 1 16 VTZA96461 4 19961226 A 3160 A2104F PDU JETAIR JETSTM JETSTM4101 1500501 EU LT ENG REQUIRED RESET A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 325UE 41063 FLT 6280 - ORF-IAD - DURING CLIMB, AN UNSCHEDULED LANDING DUE TO LEFT ENGINE START CAPTION LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND RESET LT PDU, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1997011600824 19970116 00824 EU 1997 1 16 VTZA96449 1 19961218 A 3010 29S7D524501 DE-ICE BOOT JETAIR JETSTM JETSTM4101 1500501 EU LT WING BLOWN A VTZA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 EA 27 303UE 41015 FLT 6501 - IAD-JFK - DURING TAXI, RETURNED TO GATE DUE TO CCT-1 FAULT ON AUTO AND MANUAL MODES. MAINTENANCE INSPECTION AND FOUND LEFT INBOARD DE-ICE BOOT BLOWN. MAINTENANCE REMOVED AND REPLACED DE-ICE BOOT, OPS CHECK OK. AIRCRAFT WAS REL EASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1997011600825 19970116 00825 1997 1 16 VTZA96448 3 19961218 A 6140 31056294 PRESS SWITCH JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE FAILURE A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 327UE 41080 FLT 6531 - LGA-IAD - ABORTED TAKEOFF DUE TO LEFT ENGINE RED BETA WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE W ITH NO FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED PRESSURE SWITCH, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APP ROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1997011600826 19970116 00826 NE 1997 1 16 VTZA96447 2 19961219 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE NR 1 LOW TORQUE A A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 EA 27 325UE 41063 IAD-JFK - FLT 6577 - ABORTED TAKEOFF DUE TO NR 1 ENGINE WOULD ONLY MAKE 85 PERCENT TORQUE ON TAKEOFF ROLL. AIRCRAFT RET URNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND ADJUSTED EGT RESERVE AND MAX POWER, OPS CHECK OK. AI RCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 4 T RT A41NM E18NE 1997011600827 19970116 00827 EU 1997 1 16 VTZA96446 1 19961219 A 7697 WIRE JETAIR JETSTM JETSTM4101 1500501 EU RT IEC BROKEN A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 321UE 41045 FLT NR 6295 - IAD-EWR DURING CRUISE, MADE AN UNSCHEDULED LANDING DUE TO RIGHT ENGINE IEC FAILURE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND FOUND BROKEN WIRE IN ZONE 2 CANNON PLUG AND REPAIRED WIRE, OP S CHECK OK. AIRCRAFT WAS RELEASED ADN APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1997011600828 19970116 00828 EU 1997 1 16 VTZA96455 1 19961222 A 2150 ACM JETAIR JETSTM JETSTM4101 1500501 EU LEFT STUCK A VTZA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 303UE 41015 FLT 6479 - IAD-EWR - DURING TAXI, RETURNED TO GATE DUE TO LEFT DUCT OVER TEMP WARNING LIGHT ILLUMINATED. MAINTENANCE IN SPECTED AND FOUND ACM STUCK. MAINTENANCE FREED STUCK ACM. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1997011600829 19970116 00829 EU 1997 1 16 VTZA96454 1 19961221 A 2435 23079009 STARTER GEN BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A VTZA O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION AP APPROACH 1 EA 27 488UE 907 FLT 6363 - LYH - IAD - DURING APPROACH, MADE AN SCHEDULED LANDING WITH ONE DISCREPANCY, RIGHT STARTER GENERATOR FAILED O N APPROACH. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED STARTER/GENERATOR, OPS CH ECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1997011600831 19970116 00831 EU 1997 1 16 VTZA96452 1 19961220 A 7600 IEC JETAIR JETSTM JETSTM4101 1500501 EU LT/RT ENGINE MALFUNCTIONED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 318UE 41041 FLT 6577 - IAD-JFK - AIRCRAFT ABORTED TAKEOFF DUE TO LEFT AND RIGHT ENGINE IEC FAILED ON TAKEOFF. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED, CLEARED ALL FAULTS AND REPROGRAMMED IEC'S. OPS CHECK OK. AIRCRA FT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1997011600832 19970116 00832 EU 1997 1 16 VTZA96451 1 19961221 A 3150 TO WARNING JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT ACTIVATED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 310UE 41028 FLT 6353 - IAD-TYS - ABORTED TAKEOFF DUE TO TAKEOFF CONFIGURATION WARNING LIGHT ILLUMINATED. MAINTENANCE INSPECTED AND CREW RESET ALL FLIGHT CONTROLS, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1997011600833 19970116 00833 EU 1997 1 16 VTZA96457 1 19961224 A 5240 DOOR BAG JETSTM JETSTM3201 1500217 EU GPU COMPT NOT SECURED A VTZA A UNSCHED LANDING O OTHER TO TAKEOFF 1 EA 27 474UE 849 FLT 6253 - IAD-ABE - DURING TAKEOFF, MADE A UNSCHEDULED LANDING DUE GPU DOOR WARNING LIGHT. AIRCRAFT RETURNED TO GATE W ITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND SECURED GPU ACCESS DOOR. AIRCRAFT WAS RELEASED AND RETURNED TO SERV ICE. (M) 2 L 7 2 4T RT A56EU 1997011600834 19970116 00834 WP 1997 1 16 VTZA96456 2 19961223 A 7310 8975131 FUEL FILTER JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33110U 01514 WP RT ENGINE CONTAMINATED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 319UE 41042 FLT 6234 - IAD-RIC - DURING CLIMB, AN UNSCHEDULED LANDING DUE TO RIGHT ENGINE FUEL FILTER CAUTION LIGHT ILLUMINATED. AI RCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED FUEL FILTER, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 4 T RT A41NM E4WE 1997011600835 19970116 00835 EU 1997 1 16 VTZA96458 1 19961226 A 2710 YOKE CABLE JETAIR JETSTM JETSTM4101 1500501 EU AILERON CONTL OUT OF ADJUST A VTZA K NONE F FLT CONT AFFECTED CR CRUISE 1 EA 27 301UE 41012 FLT 6150 - IAD-EWR - DURING CRUISE, MADE A SCHEDULED FLIGHT WITH ONE DISCREPANCY WHICH WAS ONE INCH PLAY TO THE LEFT AND RIGHT IN YOKE CONTROLS WITH NO AILERON RESPONSE. AIRCRAFT WETN TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTI ON AND ADJUSTED YOKE CABLE TENSION. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1997011600836 19970116 00836 EU 1997 1 16 VTZA96450 1 19961220 A 5270 WARNING LIGHT JETAIR JETSTM JETSTM4101 1500501 EU BAGG DOOR ILLUMINATED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 309UE 41022 FLT 6418 - IAD-BOS - ABORTED TAKEOFF DUE TO MAIN BAGGAGE DOOR WARNING LIGHT ILLUMINATED. MAINTENANCE OPEN DMI 52737, ME L 52-3. MAINTENANCE CLOSED DMI 52737 ON 12-21-96 BY INSPECTING MAIN BAGGAGE DOOR. COULD NOT DUPLICATE, OPS CHECK OK. A IRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1997011600837 19970116 00837 WP 1997 1 16 VTZA96444 2 19961216 A 7200 ENGINE BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE3311 01514 WP RIGHT MALFUNCTIONED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 473UE 828 FLT 6528 - BUF-IAD - ABORTED TAKEOFF DUE TO RIGHT ENGINE TORQUE FLUX. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEM S. MAINTENANCE OPEN DMI 52079, MEL 77-1 ON RT SRL. MAINTENANCE CLOSED DMI 52079 ON 12-17-96 BY INSPECTION AND RUN UP N O DEFECTS NOTED AND COULD NOT DUPLICATE. OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T 3 T RT A21EU E3WE 1997011600838 19970116 00838 EU 1997 1 16 VTZA96427 1 19961206 A 2710 TRIM JACK BAG JETSTM JETSTM3201 1500217 EU RT AILERON LACK OF LUBE A VTZA O OTHER F FLT CONT AFFECTED CR CRUISE 1 EA 27 370MT 800 FLT 6561 - GSO-IAD DURING CRUISE CRUISE, EXPERIENCED SLIGHT RESISTANCE TO AILERON TRIM PILOT INPUTS. AIRCRAFT LANDED AT IAD WHERE THE MAINTENANCE TECHNICIANS TROUBLESHOT THE DISCREPANCY AND FOUND THAT THE AILERON TRIM JACK NEEDED TO BE LUB RICATED. LUBRICATED THE TRIM JACK ON THE RT AILERON IAW THE J3200 MX PROCEDURES. AIRCRAFT WAS THEN RELEASED AND APPROV ED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1997011600900 19970116 00900 SO 1997 1 16 SWIA97812 1 19961227 A 3246 118120 HUB CAP EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE NR 3 MLG MISSING A SWIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 NM 07 194SW 120120 ON TAKEOFF ROLL AT 80 KNOTS, RIGHT ANTI-SKID LIGHT ILLUMINATED FOLLOWED BY BRAKES LIGHT ON MAP AND CAUTION WARNING LIGHT S. ABORTED TAKEOFF. FOUND NR 3 MAIN TIRE/WHEEL ASSEMBLY HUB CAP MISSING. INSTALLED SERVICEABLE HUB CAP, TAXIED AIRCRA FT. ANTI-SKID OPERATED NORMAL AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 1997011600915 19970116 00915 NM 1997 1 16 CA960826015 1 19960822 A 5313 Z MEMBER DHAV DHAV DHC8 DHC8101 2809002 NM PWA STA.X97.0 CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 24500 123138 (CAN) LH VERTICAL Z MEMBER AT STA.X97.0 FOUND CRACKED. HORIZONTAL BEAM AT STA.X97.0 ALSO CRACKED. RH VERTICAL Z MEMBER AT SAME STA. MISSING RIVETS. CRACKS REPAIRED AS PER DEHAVILLAND SUPPLIED DRAWINGS. 2 H 7 2 4T RT A13NM 1997011600916 19970116 00916 NE 1997 1 16 CA960826017 2 19960728 A 7310 5905587 HP FUEL FILTER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE #2 ENGINE PARTLY BLOCKED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 81 120244 (CAN) ENROUTE #2 ENGINE FUEL FILTER BY-PASS CAUTION LIGHT ILLUMINATED. THE AIRCRAFT CONTINUED TO DESTINATION WITHOUT INC IDENT. POST FLIGHT INVESTIGATION REVEALED SOME MINOR CONTAMINATION OF THE #2 ENGINE HIGH PRESSURE FUEL PUMP FILTER. FILT ER ELEMENT REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. THE SUBMITER STATES THAT THIS OCCURRENCE IS FREQUENT AND I S THE SUBJECT OF ANALYSIS WITH THE OPERATORS RELIABILITY DEPARTMENT AND PRATT & WHITNEY. THERE ARE 13 SIMILAR OCCURRENCE S ON THE SDR DATA BASE. 2 H 7 2 4T 4 T RT A13NM E20NE 1997011600917 19970116 00917 NM 1997 1 16 CA960826019 1 19960724 A 5270 841005 PSEU DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE PAX DOOR WARN FAILED W C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA 120342 (CAN) ON TAKEOFF ROLL, RED WARNING LIGHT FOR PASSENGER DOOR AND CARGO DOOR ON. TAKEOFF REJECTED. DOOR CONFIRMED OK. ON 2 3 JULY 96, CREW HAD REPORTED THAT DOOR LIGHT HAD COME ON TWICE IN FLIGHT, NO FAULT FOUND. ON 24 JULY 96 INCIDENT RE-OCCU RRED. MAINTENANCE REPLACED PSEU AND EVERYTHING OK. 2 H 7 2 4T 4 T RT A13NM E20NE 1997011600918 19970116 00918 EU 1997 1 16 CA960826020 1 19960803 A 3232 ACTUATOR FOKKER F28 F28MK1000 4990808 EU RT AFT GEAR DOOR SPLIT W A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CL CLIMB 1 CA (CAN) LOST UTILITIES SYSTEM HYDRAULIC FLUIDS AFTER TAKEOFF, FLIGHT RETURNED, EMERGENCY DECLARED. CFR CALLED OUT, ALTERNA TE GEAR LOWERING, LANDED OK. ON RUNWAY HAD TO BE TOWED DUE TO LOSS OF HYDRAULICS. RH AFT GEAR DOOR ACTUATOR SPLIT, REPLA CED. 2 L 7 2 4F RT A20EU 1997011600919 19970116 00919 SO 1997 1 16 CA960826022 2 19960808 A 7414 6310 MAGNETO SLICK CESSNA 206 U206F 2073333 CE CONT O520 IO520F 17032 SO MCAULY 2A34C D2A34C58 GL MT FLANGE HOUSING BROKE W O OTHER O OTHER TX TAXI/GRND HDL 1 CA 1229 93020098 286399R 757515 (CAN) MAGNETO HOUSING BROKE AT MOUNTING FLANGE. COUPLING WAS ALSO DAMAGED. 1 H 7 1 3O 3 O A4CE E5CE 5 C P3EA 1997011600920 19970116 00920 NM 1997 1 16 CA960826023 1 19960731 A 2435 STARTER LUCAS DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE #2 ENGINE RELAY STUCK W E ENGINE SHUTDOWN B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 CA 120279 (CAN) AFTER #2 ENGINE START THE #2 STARTER GENERATOR CAUTION LIGHT ILLUMINATED AS WELL AS THE D.C. BUS FAULT. CREW TRIED TO RESET BUT TO NO AVAIL. #2 ENGINE WAS SHUTDOWN. GROUND CREW APPLIED EXTERNAL POWER AND SMOKE BEGAN COMING FROM #2 ENG INE. #2 ENGINE STARTER CONTACT RELAY REPLACED DUE TO BEING ARCHED IN THE CLOSED POSITION. ALSO #2 ENGINE STARTER GENERAT OR REPLACED DUE TO 2431-K2 RELAY BEING STUCK IN THE "START" POSITION CAUSING THE STARTER TO OVERHEAT. ENGINE GROUND RUN SERVICEABLE AND AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 1997011600921 19970116 00921 NM 1997 1 16 CA960826024 1 19960726 A 7312 10718K HEATER STWARNER DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE FUEL/OIL FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 1440 123030 (CAN) DURING CLIMB, THE #2 OIL TEMPERATURE INCREASED INTO YELLOW (115 DEGREES). CREW LEVELLED AT 20,000 FT., BUT OIL TEM PERATURE DID NOT DECREASE. REDUCED POWER TO 4O PERCENT TORQUE AND OIL TEMPERATURE DROPPED INTO GREEN (100 DEGREES). MAIN TENANCE FOUND FUEL OIL HEATER UNSERVICEABLE. 2 H 7 2 4T 4 T RT A13NM E20NE 1997011600922 19970116 00922 SW 1997 1 16 CA960826026 1 19960812 A 6230 206010443001 BEARING BELL 20601045011 BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL SWASHPLATE OVERHEATED W K NONE F FLT CONT AFFECTED CR CRUISE 1 CA 3280 JILG09472 CAE822919 (CAN) PILOT REPORTED STIFFNESS OF CYCLIC CONTROL. AFTER SHUTDOWN, CYCLIC WAS VERY DIFFICULT TO MOVE AND SWASHPLATE WAS H OT. CONTROLS DISCONNECTED AT SWASHPLATE AND BEARING ROUGHNESS NOTED. GREASE PURGED BUT BEARING STILL ROUGH. 1 G 7 1 3U 3 U H2SW E4CE 1997011600923 19970116 00923 EU 1997 1 16 CA960826027 1 19960729 A 2410 695379F CSD UNITEDTECH 695379F FOKKER F28 F28MK1000 4990808 EU RROYCE NR 2 FAILED W O OTHER P NO WARNING INDICATION CR CRUISE 1 CA 613 (CAN) DURING FLIGHT PILOTS REPORTED NOSE LANDING GEAR INDICATORS DID NOT ILLUMINATE UPON RETRACTION SELECTION. NO GREEN OR RED LIGHT INDICATION. THIS ALL OCCURRED WHEN THE #2 CONSTANT SPEED DRIVE AND GENERATOR FELL OFFLINE. CSD CAUTION LIGH T ON. THE #3 GENERATOR WAS BROUGHT ON LINE BUT BURNT OUT THE NOSE GEAR INDICATION BULBS. REPLACED #2 CSD. 2 L 7 2 4F RT A20EU 1997011600924 19970116 00924 EU 1997 1 16 CA960826029 1 19960731 A 3222 200429003 STRUT ASSEMBLY FOKKER F28 F28MK1000 4990808 EU RROYCE ACTUATOR ATTACH CRACKED W A D UNSCHED LANDING RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA 32934 (CAN) AIRCRAFT LANDED OVERWEIGHT. NDT INSPECTION REVEALED CRACK IN ACTUATOR ATTACHMENT LUG AREA. STRUT REPLACED. 2 L 7 2 4F RT A20EU 1997011600925 19970116 00925 EU 1997 1 16 CA960826030 1 19960804 A 2432 23765 BATTERY SAFT 23765 FOKKER F28 F28MK1000 4990808 EU DC SYS OVERHEATED W A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 CA 35116 (CAN) AFTER DEPARTURE BATTERY OVERTEMPERATURE LIGHT ON. AN UNEVENTFUL LANDING, CFR CALLED OUT. BATTERY CHECKED ON RUNWAY , RETURNED TO GATE, BATTERY REPLACED. 2 L 7 2 4F RT A20EU 1997011600926 19970116 00926 NE 1997 1 16 CA960826033 2 19960524 A 7310 451801 SWITCH SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE BYPASS LIGHT LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 4294 (CAN) SWITCH LEAKING FUEL UP TO THE CANNON PLUG FOR THE BYPASS LIGHT. 1 G 7 1 3U 3 U NC H9EU E19EU 1997011600927 19970116 00927 SW 1997 1 16 CA960826034 1 19960611 A 6320 206040156101 SEAL BELL 206040002025 BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL TRANSMISSION LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 1859 B122394 CAE821569 (CAN) DURING PREFLIGHT INSPECTION, PILOT NOTICE A SIGNIFICANT AMOUNT OF OIL IN THE TRANSMISSION AREA. MAGNETIC SEAL LEAK ING, REPLACED. 1 G 7 1 3U 3 U H2SW E4CE 1997011600928 19970116 00928 SW 1997 1 16 CA960826035 1 19960617 A 6230 DP361 SHIM BELL 206010450113 BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL SWASHPLATE UNIBALL BIND W K NONE O OTHER IN INSP/MAINT 1 CA 11260 3017 DP361 CAE823426 (CAN) ON INSTALLATION AFTER REPAIR BY OVERHAUL FACILITY, SWASHPLATE TILT FRICTION CHECKED AND FOUND WITHIN LIMITS AFTER GROUND RUN, PILOT REPORTED CYCLIC HARD TO MOVE WITH HYDRAULICS ON, ALMOST IMPOSSIBLE TO MOVE WITH HYDRAULICS OFF. SWASH PLATE HAD BEEN SHIMMED INCORRECTLY WITH AN UNEVEN AMOUNT OF SHIMS ON EACH SIDE CAUSING THE UNIBALL TO BIND. SHIMMING WAS CORRECTED AND RETURNED TO SERVICE. 1 G 7 1 3U 3 U H2SW E4CE 1997011600929 19970116 00929 EU 1997 1 16 CA960826036 1 19960623 A 2822 GROUND WIRE SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE FUEL QTY/PRESS BAD GROUND W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 836 (CAN) IN CRUISE, FUEL PRESSURE FLUCTUATIONS AND FUEL QUANTITY FLUCTUATIONS. PUMP NOT RUNNING AND SPARKING AT REMOTE FUEL DRAIN SPRING. GROUND WIRE FOR BOOST PUMP AND FUEL QUANTITY TRANSMITTER WAS HOOKED UP CORRECTLY, BUT IN FACT GROUNDING T HROUGH THE MANUAL SUMP DRAIN CABLE. POSSIBLE FIRE HAZARD. GROUND WIRE RELOCATED TO THE AIRFRAME. 1 G 7 1 3U 3 U H9EU E19EU 1997011600930 19970116 00930 EU 1997 1 16 CA960826037 1 19960712 A 6220 M3041 STAR ARM AEROSP 350A31190703 SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE END BUSHING DEBONDED W A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 CA 345 M3041 4431 (CAN) IN FLIGHT, VIBRATION LEVEL INCREASING AND GROUND RESONANCE ENCOUNTERED DURING LANDING STAR ARM - BLUE POSITION - END BUSHING SLEEVE DEBONDED CAUSING IT TO WEAR INTO STAR ARM COMPOSITE MATERIAL NO EVIDENCE OF DEBOND WAS FOUND AT LAST 100 HOUR INSPECTION. 1 G 7 1 3U 3 U NC H9EU E19EU 1997011600931 19970116 00931 EU 1997 1 16 CA960826038 1 19960715 A 2822 21860 PUMP P94B12203C SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE FUEL BOOST FAILED W C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CA 2 21860 879 (CAN) PUMP FAILED INTERNALLY AFTER ONLY 2 HOURS AND 5 ENGINE STARTS SINCE INSTALLED 1 G 7 1 3U 3 U NC H9EU E19EU 1997011600932 19970116 00932 SW 1997 1 16 CA960826039 1 19960719 A 6400 GDLG09647 ROTOR ASSEMBLY BELL 206011810013 BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL T/R OUT OF BALANCE W K NONE O OTHER IN INSP/MAINT 1 CA 8564 1384 GDLG09647 800631F (CAN) ON INSTALLATION AFTER REPAIR, UNABLE TO BALANCE TAIL ROTOR ASSEMBLY AFTER SEVERAL RUNS, UNIT REJECTED 1 G 7 1 3U 3 U H2SW E4CE 1997011600933 19970116 00933 SW 1997 1 16 CA960826040 1 19960717 A 6320 B121294 TRANSMISSION BELL 206040002025 BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL M/R GR BOX FAILURE W K NONE O OTHER IN INSP/MAINT 1 CA 10898 2015 B121294 CAE821569 (CAN) METAL ON CHIP DETECTOR INDICATING INTERNAL FAILURETRANSMISSION REPLACED 1 G 7 1 3U 3 U H2SW E4CE 1997011600934 19970116 00934 SO 1997 1 16 CA960826042 1 19960802 A 6120 582855 VALVE HOUSING HAMSTD LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL HAMSTD 54H 54H60117 NE #3 PROPELLER COVER CRACKED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA 1190 0 500859 226247 (CAN) DURING FLIGHT SMOKE BEGAN TO FILL THE CABIN. THE AIR CONDITIONING SYSTEM AND RH AC BUS WERE ISOLATED. FLIGHT CONTI NUED TO DESTINATION. POST FLIGHT INSPECTION FOUND #3 PROPELLER VALVE HOUSING COVER WAS CRACKED AND LEAKING OIL. FRICTION ON SLIP RING GENERATED SMOKE WHICH WAS INJESTED BY THE PRESSURIZATION SYSTEM. VALVE HOUSING COVER, SLIP RING AND BRUSH BLOCK WERE REPLACED AND AIRCRAFT RETURNED TO SERVICE. 2 H 7 4 4T 4 T A1SO E282 6 C P906 1997011600935 19970116 00935 EA 1997 1 16 CA960826044 2 19960731 A 8520 CRANKCASE BEECH 95 E95 1153410 CE LYC O360 IO360B1B 41514 EA CYLINDER FLANGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 904 L389151AA (CAN) DURING A SCHEDULED INSPECTION A CRACK WAS FOUND ON THE RH ENGINE BETWEEN #2 AND #4 CYLINDERS, APPROXIMATELY 4" LON G PROPAGATING FROM THE #4 CYLINDER FLANGE. THE ENGINE WAS REPLACED. 1 L 7 2 3O 3 O 3A16 1E10 1997011600936 19970116 00936 EU 1997 1 16 CA960826045 1 19960725 A 2611 4724161 SMOKE DETECTOR AIRBUS 310 A310324 3930206 EU PWA 4152 PW4152 NE FORWARD CARGO FALSE WARNING W F ACTIVATE FIRE EXT. J N WARNING INDICATION FALSE WARNING DE DESCENT 1 CA P717703 (CAN) ECAM WARNING OF SMOKE IN THE FORWARD CARGO AREA. SMOKE LIGHT ILLUMINATED. EMERGENCY PROCEDURES INITIATED AND #1 FI RE BOTTLE DISCHARGED. SMOKE LIGHT WENT OUT AND AIRCRAFT LANDED SAFELY. MAINTENANCE INSPECTION OF FORWARD CARGO AREA CARR IED OUT AND EVERYTHING FOUND NORMAL. BOTH FORWARD AND AFT SMOKE DETECTORS REPLACED IN FORWARD CARGO AREA AND #2 BOTTLE P OSITIONED IN #1 POSITION. 2 L 7 2 4F RT A35EU E24NE 1997011600937 19970116 00937 CE 1997 1 16 CA960826062 1 19960619 A 2750 50000084 CONTROL CABLE CESSNA 401 401A 207590D CE MCAULY 3AF32C 3AF32C87 GL FLAP EXTEND SEPARATED W K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 CA 8456 760771 (CAN) THE AREA WHERE THIS FAILURE OCCURRED IS LOCATED BEHIND A PULLEY AND IS NOT EASILY INSPECTED WITHOUT THE USE OF A M IRROR LOOKING INBOARD. SOME WEAR AND FRAYING WAS ALSO NOTICED JUST OUTBOARD OF THE PULLEY. THERE WAS SOME CORROSION ON T HE CABLE BUT NOT IN THE AREA OF THE FAILURE. THE PULLEYS WERE NOT SEIZED AND THE CABLE WAS NOT RUBBING ON ANYTHING. THE TENSION WAS CHECKED 114 HOURS PREVIOUSLY. 1 L 7 2 3O A7CE 5 C P22EA 1997011600938 19970116 00938 SW 1997 1 16 CA960826066 1 19960720 A 2913 0016 PUMP BODY K974120101 KAMAN K1200 K1200 05625F6 SW LYC T53 T5317A 41549 NE MOUNTING FLANGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 518 0016 LR81008 (CAN) PUMP WAS REMOVED TO FACILITATE TRANSMISSION REPLACEMENT WHEN PUMP MOUNTING FLANGE WAS FOUND CRACKED APPROXIMATELY 1 INCH ACROSS THE THINNEST PORTION OF THE FLANGE ADJACENT TO THE 1 O'CLOCK MOUNT HOLE 1 G 7 1 4F 4 U NT TR7BO E17EA 1997011600939 19970116 00939 SO 1997 1 16 CA960826069 1 19960729 A 3230 SHUTTLE VALVE GULSTM G159 G159 3952202 SO EMERGENCY SYSTEM STUCK W O OTHER O OTHER AP APPROACH 1 CA (CAN) GEAR FAILED TO EXTEND DURING APPROACH. EMERGENCY EXTENSION SYSTEM WAS USED TO EXTEND THE GEAR AND AIRCRAFT LANDED SAFELY. RETRACTIONS CARRIED OUT AND IT WAS DISCOVERED THAT SHUTTLE VALVE WAS NOT REPOSITIONING PROPERLY. SHUTTLE VALVE W AS REPOSITIONED USING APPROVED MM PROCEDURE. FURTHER RETRACTIONS WERE CARRIED OUT AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 1A17 1997011600941 19970116 00941 NM 1997 1 16 CA960826072 1 19960807 A 2913 NAS1602908 O-RING VICKERS 570347 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE #2 SYS PUMP DETERIORATED W K NONE K FLUID LOSS CR CRUISE 1 CA 3410 3410 MX449127C 120584 (CAN) #2 HYDRAULIC SYSTEM LOST ALL HYDRAULIC FLUID DURING FLIGHT. POST FLIGHT INVESTIGATION FOUND "O" RING AT #2 ENGINE DRIVEN HYDRAULIC PUMP DETERIORATED CAUSING LEAK OF ALL FLUID. 2 H 7 2 4T 4 T RT A13NM E20NE 1997011600942 19970116 00942 EA 1997 1 16 CA960826073 1 19960813 A 2421 720845 GENERATOR SUNDSTRAND 731579 CNDAIR CL600 CL6002A12 1900304 EA GE CF34 CF341A NE IDG FAILED W E ENGINE SHUTDOWN J WARNING INDICATION TX TAXI/GRND HDL 1 CA 567 350143 (CAN) AFTER ENGINE START, GENERATOR ON LINE AND THEN FAILED. IDG (INTEGRATED DRIVE GENERATOR) REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 1997011600945 19970116 00945 EU 1997 1 16 CA960826079 1 19960720 A 3250 CA248003 SELECTOR VALVE CASA C212 C212CC 2410204 EU STEERING WORN W K NONE K FLUID LOSS LD LANDING 1 CA 4920 4920 (CAN) UPON LANDING, A NOSE WHEEL SHIMMY DEVELOPED ALLOWING THE NOSE GEAR TO MAKE A SHARP RIGHT TURN BEYOND NORMAL STEERI NG LIMITS. THIS IN TURN ALLOWED THE STEERING RAM TO EXTEND TO THE END OF THE ACTUATOR, BREAKING OFF THE END OF THE ACTUA TOR RESULTING IN HYDRAULIC POWER LOSS TO STEERING SYSTEM. THE PRESELECTOR VALVE, ACTUATOR, AND STEERING CABLES WERE REPL ACED. SYSTEM THEN FUNCTIONED NORMALLY. 2 H 7 2 4T A43EU 1997011600946 19970116 00946 SW 1997 1 16 CA960826083 1 19960725 A 6310 A2000758 OUTER COUPLING BELL 212040005103 BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA DRIVE SHAFT CHAFED-OVERHEAT W K NONE J WARNING INDICATION IN INSP/MAINT 1 CA A2000758 CPPS61494 (CAN) TEMPERATURE INDICATING PAINT STRIPS ON THE ENGINE/TRANSMISSION DRIVESHAFT TURNED BLACK INDICTING OVERHEAT CHAFING ON THE OUTER COUPLING CAUSED BY AN EXTERNAL SOURCE 1 G 7 1 4U 4 U H4SW E22EA 1997011600947 19970116 00947 EU 1997 1 16 CA960826085 2 19960724 A 8510 996879R GEARBOX DIAMON DA20A1 DA20A1 05626UX GL ROTAX 912 ROTAX912 55555 EU PROP SHAFT LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 702 119 4076102 (CAN) LEAK FOUND ON PROP SHAFT TO GEARBOX SEAL. GEARBOX REPLACED. 1 L 7 1 3O 3 I NT TA4CH EXPE3I 1997011600948 19970116 00948 1997 1 16 CA960826088 4 19960810 A 3417 HG480813 CADC BOEING 727 7272J4 1384006 NM PWA JT8 JT8D17 52049 NE CAPT ASI/ALT INTERMITTENT W C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CA 688133 (CAN) TAKEOFF REJECTED DUE TO FAILURE OF CAPTAINS ASI AND ALTIMETER. CADC REPLACED. 2 L 7 3 4F 4 F RT A3WE E2EA 1997011600949 19970116 00949 WP 1997 1 16 CA960826090 1 19960818 A 2150 PACK LKHEED 1011 1011385115 5265015 WP AIR COND FAILED CONTROL W D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA (CAN) AIRCONDITIONING PACK FAILED IN AUTO, MANUAL OPERATION MODE WENT UNSERVICEABLE. OVERHEAT CONDITION CAUSING SMOKE IN CABIN. REPLACED. 2 L 7 3 4F A23WE 1997011600950 19970116 00950 EA 1997 1 16 CA960826093 2 19960814 A 7414 M3548 ROTOR SLICK 4370 BEECH 23 C23 1151242 CE LYC O360 O360A4K 41514 EA MAGNETO BROKEN SHAFT W O OTHER O OTHER TX TAXI/GRND HDL 1 CA 69 96010253 L2472236A (CAN) THE MAGNETO DID NOT FUNCTION DURING GROUND RUN. THE MAGNETO WAS REPLACED. INSPECTION OF THE FAULTY MAGNETO REVEALE D THE SLOTTED END OF THE ROTOR SHAFT BROKE NEAR THE SHOULDER. 1 L 7 1 3O 3 O A1CE E286 1997011600951 19970116 00951 NE 1997 1 16 CA960826094 2 19960803 A 8530 114651 VALVE CVAC PBY5 PBY5A 2421208 WP PWA R1830 R183092 52020 NE #5 CYLINDER BROKEN W A UNSCHED LANDING B E R SMOKE/FUMES/ODORS/SPARKS VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CR CRUISE 1 CA 820 BP488687 (CAN) BROKEN EXHAUST VALVE ON #5 CYLINDER. CYLINDER REPLACED, ENGINE GROUND RUN SERVICEABLE AND AIRCRAFT RETURNED TO SER VICE. 2 H 7 2 4R 4 R 2548 5E4 1997011600952 19970116 00952 NE 1997 1 16 CA960826095 2 19960807 A 7300 CG14552 ACCUMULATOR BELL 212 212 1181420 SW PWA PT6T PT6T3B 52045 NE FUEL CRACKED BELLOWS W K NONE O OTHER IN INSP/MAINT 1 CA 2803 40454046 62055 (CAN) WHILE COMPLYING WITH PRATT & WHITNEY SERVICE BULLETIN #5379, PARAGRAPH 3(A)(1), ALL FUEL COULD NOT BE DRAINED FROM THE ACCUMULATOR. WEIGHT OF THE ACCUMULATORS IN ACCORDANCE WITH SUB-PARAGRAPH (D) OF THE A.M. REFERENCE ACCUMULATORS WER E NOTED AS WEIGHING 156 AND 158 GRAMS. COMPONENTS REJECTED AS HAVING EXCEEDED THE WEIGHT RESTRICTION OF 154 GRAMS. 1 G 7 1 4U 4 U H4SW E22EA 1997011600953 19970116 00953 EU 1997 1 16 CA960826096 1 19960806 A 2822 216079008 PUMP LYC BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE FUEL BOOST WORN SHAFT W K NONE O OTHER IN INSP/MAINT 1 CA 6519 0772 LF05784A (CAN) WHEN FUEL BOOST PUMP REMOVED, IT WAS NOTED THAT THE SPLINE TEETH OF THE SHAFT HAD SEVERE WEAR. 2 H 7 4 4F 4 F RT A49EU E6NE 1997011600954 19970116 00954 EA 1997 1 16 CA960826097 2 19960807 A 8530 STUD CESSNA 172 172N 2072434 CE LYC O320 O320H2AD 41508 EA #4 CYL RKR ARM BROKEN W E A ENGINE SHUTDOWN UNSCHED LANDING E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS DE DESCENT 1 CA 1779 RL622276T (CAN) DURING FLIGHT ENGINE STARTED TO RUN ROUGH. ENGINE POWER REDUCED AND AIRCRAFT LANDED ON HIGHWAY. GROUND INSPECTION FOUND #4 CYLINDER EXHAUST ROCKER STUD BROKE ALLOWING THE ROCKER ARM AND STUD TO FALL INTO THE BOTTOM OF THE ROCKER COVER . THIS RESTRICTED THE VALVE OPENING WHICH CAUSED THE PUSH ROD TO BEND. STUD, PUSH ROD AND PUSH ROD TUBE REPLACED. VALVE CLEARANCES CHECKED OK AND ENGINE GROUND RUN SERVICEABLE. 1 H 7 1 3O 3 O NT 3A12 E274 1997011600955 19970116 00955 WP 1997 1 16 CA960826101 1 19960808 A 5248 AKC733223 DOOR DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE TAIL CONE DEPARTED W K NONE D INFLIGHT SEPARATION CR CRUISE 1 CA 517762 (CAN) ON DEPARTURE, LOWER TAIL CONE ACCESS DOOR AT STA 2184 SEPARATED FROM TAIL CONE OF AIRCRAFT. AS THE DOOR OPENED IN TO THE SLIP STRESAM WIND, THE HINGE POINTS WERE TORN FROM THE STRUCTURE. THE SEPARATED DOOR STRUCK THE UNDERSIDE OF THE TAIL CONE RESULTING IN MINOR BUCKLING TO THE SKIN AND SUPPORTING FORMERS DIRECTLY AFT OF THE DOOR. MAINTENANCE INVEWTIGA TION OF BOTH DOOR LATCH FITTINGS REVEALED THAT THE HOLES SHOWED APPROXIMATELY 5 PERCENT ELONGATION. THE FITTING BRACKETS WERE REPLACED AS A PRECAUTIONARY MEASURE. 2 L 7 3 4F 4 F A22WE E23EA 1997011600956 19970116 00956 WP 1997 1 16 CA960826103 1 19960720 A 6320 369D25132BSC OUTPUT SHAFT HUGHES 369D25100501 HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL XMSN UPPER DISC BULGED W K NONE O OTHER IN INSP/MAINT 1 CA 2030 1297 CAE830950 (CAN) WHILE ACCOMPLISHING CF-88-09 PER DN 148.1, BULGE OR DEFORMATION FOUND ON THE UPPER DISC.TIME SINCE LAST INSPECTION , 293 HOURS. 1 G 7 1 3U 3 U H3WE E4CE 1997011600957 19970116 00957 NE 1997 1 16 CA960826105 1 19960703 A 6320 S58592363 TRANSMISSION SKRSKY S16352000001 SKRSKY S58T S58ET 8141803 NE PWA PT6T PT6T6 52045 EA M/R GR BOX MAKING METAL W K NONE O OTHER IN INSP/MAINT 1 CA 6344 692 S58592363 CPPS72089 (CAN) MAIN GEARBOX REMOVED DUE TO METAL FOUND IN OIL FILTER 2 G 7 2 4U 4 U 1H11 E22EA 1997011600958 19970116 00958 EA 1997 1 16 CA960826106 1 19960701 A 2750 C3CF4011 BELLCRANK DHAV C3CF577 DHAV DHC3 DHC3 2800202 EA LH AND RH CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 18014 0 (CAN) BOTH LEFT AND RIGHT BELLCRANKS IN THE FLAP ACTUATOR WERE FOUND CRACKED AND/OR CORRODED. THE RIGHT ONE WAS CORRODED IN THE CORNERS OF THE FORK, WHILE THE LEFT ONE WAS CRACKED IN THE UPPER SECTION OF THE FORK. 1 H 7 1 3R A815 1997011600959 19970116 00959 NM 1997 1 16 CA960826107 1 19960719 A 6310 CLUTCH ROBSIN R22 R22BETA NM LYC ROTOR SEIZED W A B UNSCHED LANDING EMER. DESCENT J WARNING INDICATION CR CRUISE 1 CA L158133914 (CAN) HELICOPTER CRASH LANDED AT 5000 FEET. PILOT REPORTED LOW ROTOR WARNING AND INTERMITTENT CLUTCH LIGHT. INVESTIGATIO N REPORT TO FOLLOW. 1 G 7 1 3O H10WE 1997011600960 19970116 00960 NM 1997 1 16 CA960827001 1 19960823 A 2422 DH103024600CS1 INVERTER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE AC SYS BURNED W H DEACTIVATE SYST/CIRCUITS B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 CA 19087 120832 (CAN) STRONG ELECTRICAL BURN ODOUR IN COCKPIT AND CABIN ON APPROACH. PRIMARY INVERTER WARNING LIGHT ON AND BREAKER POPPE D. INVERTER REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1997011600961 19970116 00961 EU 1997 1 16 CA960827002 1 19960823 A 3242 HW026 ROTOR DUNLOP AHA1412 BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE BRAKE ASSY DISINTEGRATED W O OTHER O OTHER LD LANDING 1 CA HW026 LF05539A (CAN) THE ROTOR APPERARS TO HAVE FAILED AS IT WAS COMPLETELY DESTROYED. PRESSURE STATOR REMAINED WITH THE BRAKE ASSEMBL Y, BUT WAS BADLY DELAMINATED 2 H 7 4 4F 4 F RT A49EU E6NE 1997011700001 19970117 00001 1997 1 17 TWRA96377 4 19961216 A 2565 7A123929 SLIDE BOEING 747 747212B 1384886 NM 5L DOOR DEPLOYED A TWRA K NONE O OTHER TX TAXI/GRND HDL 1 EA 15 616FF 1331 21939 AFTER ARRIVAL 5L DOOR WAS INADVERTENTLY DEPLOYED. REMOVED AND REPLACED SLIDE AND DOOR ASSIST BOTTLE AS PER MM 25-65-01. OPS CHECKED NORMAL. A/C RETURN TO SERVICE. (M) 2 L 7 4 4F A20WE 1997012200005 19970122 00005 GL 1997 1 22 CA960826041 2 19960626 A 7314 PE7667 DRIVE SEAL SUNDSTRANDEM 23003114 BELL 206 206L 1181522 SW ALLSN 250C 250C20R2 GL INPUT SHAFT LEAKING W O OTHER K FLUID LOSS TO TAKEOFF 1 CA 1 PE7667 CAE832536 (CAN) INPUT DRIVE SEAL LEAKING BADLY AFTER ONLY 0 3 HOURS SINCE OVERHAUL 1 G 7 1 3U 3 U H2SW E4CE 1997012200006 19970122 00006 GL 1997 1 22 CA960826077 1 19960812 A 7810 938795 SPRING DIAMON DA20A1 DA20A1 05626UX GL ROTAX 912 ROTAX912 55555 EU ENG EXH MISSING W K NONE O OTHER IN INSP/MAINT 1 CA 4412574 (CAN) THE EXHAUST SPRING WAS MISSING. SUSPECT THE SPRING WAS NOT INSTALLED AT THE FACTORY. 1 L 7 1 3O 3 I NT TA4CH EXPE3I 1997012300006 19970123 00006 NM 1997 1 23 9627716611 1 19961013 A 5330 SKIN BOEING 747 747251B 1384892 NM BS 1920 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 611US 20356 DURING CHECK, FOUND CORROSION ON SKIN INTERNAL DOUBLER. REPLACED DOUBLER PER EA 66-120221. 2 L 7 4 4F A20WE 1997012300007 19970123 00007 NM 1997 1 23 9627726611 1 19961028 A 5320 WEB BOEING 747 747251B 1384892 NM BS 1470 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 611US 20356 DURING CHECK, FOUND CORROSION ON THE MAIN DECK PRESSURE WEB INTERIOR SURFACE. REPAIRED PER EA 66-120205. 2 L 7 4 4F A20WE 1997012300008 19970123 00008 NM 1997 1 23 9627736613 1 19961221 A 5412 BULKHEAD CHORD BOEING 747 747251B 1384892 NM AFT BULKHEAD CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 613US 20358 DURING CHECK, FOUND NR 4 STRUT AFT BULKHEAD VERTICAL T-CHORD CRACKED VERTICALLY TWO INCHES FROM TOP RIGHT SIDE. REPLACE D VERTICAL T-CHORD PER EA 66-120269 AND EA 66-120281. 2 L 7 4 4F A20WE 1997012300009 19970123 00009 NM 1997 1 23 9627746637 1 19961221 A 5400 FITTING BOEING 747 747251B 1384892 NM MID SPAR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 637US 23548 DURING PERIODIC CHECK, FOUND THE FORWARD LOWER INBOARD MIDSPAR FITTING CRACKED AT SECOND FROM AFT INBOARD FASTENER HOLE TO INBOARD EDGE OF FITTING. REPLACED FITTING. WORK COMPLETED ON CITEXT 66-5441-1-0088, FM 65 THROUGH FM 72 REPLACEMENT PROCEDURE, DRAWING NR SA5441-01048-7 AND SB 5441-01048-9. 2 L 7 4 4F A20WE 1997012300010 19970123 00010 NM 1997 1 23 9627756636 1 19961212 A 5400 FITTING BOEING 747 747251B 1384892 NM NR 3 PYLON CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 636US 23547 DURING PERIODIC CHECK, FOUND THE NR 3 PYLON INBOARD MIDSPAR FITTING CRACKED. REPLACED FITTING. WORK COMPLETED ON CITEX T JOB NBR 222, EM 5441-01016. 2 L 7 4 4F A20WE 1997012300029 19970123 00029 WP 1997 1 23 UPS97821822 1 19961230 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 6.225 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE: C. RT WING L/E RIB AT STA. XOLDI 6.225 CRACKED APPROX. 2.8 INCHES. REMOVED DAMAGED AREA PER SRM 57-2 -0. FABRICATED FILLER, DOUBLER, AND INTERCOSTAL PER SRM 57-2-0 AND INSTALLED PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1997012300030 19970123 00030 WP 1997 1 23 UPS97821823 1 19961230 A 5744 CASTING DOUG DC8 DC871F 302199D WP WS 98 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE: C. RT WING T/E, OUTBOARD OF MLG TRUNNION AND FWD OF AUXILIARY SPAR, THE STA 98 FLAP HINGE LWR ATTACH CASTING CRACKED. REMOVED CRACKED CASTING, FABRICATED REPLACMENT CASTING INSTALLED CASTING PER SRM 51-1-20D, AND SRM 51- 3-1. 2 L 7 4 4F RT 4A25 1997012300039 19970123 00039 WP 1997 1 23 ABXA9700003 1 19961230 A 5330 CLAD2014T6 SKIN DOUG DC8 DC863 302198A WP BS 28 DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 823AX 46122 DURING SORT OPERATIONS, A CARGO LOADER WAS DRIVEN INTO THE AIRCRAFT PUTTING A HOLE IN THE FUSELAGE SKIN AT STATION 28 L EFT. REPAIRED IAW ABX REA D853-17575. 2 L 7 4 4F 4A25 1997012300042 19970123 00042 NE 1997 1 23 SWIA97820 2 19961231 A 7321 EEC EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT ENGINE MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 NM 07 234SW 120308 RIGHT TORQUE WENT TO 137 PERCENT ON TAKEOFF WITH THE EEC ON. TURNED OFF EEC AND EVERYTHING WENT BACK TO NORMAL. RETUR NED TO SGU. MEL THE EEC 73-21-1. COMPLIED WITH OVER TORQUE INSPECTION PROCEDURES PER PWC MM 05-50-00. RIGHT EEC IS STILL DEFERRED. 2 L 7 2 4T 4 T RT A31SO E20NE 1997012300097 19970123 00097 WP 1997 1 23 9627769609 1 19961127 A 3010 THERMOSTAT DOUG DC9 DC932 3022066 WP WING DE-ICE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 609NW 47234 LEFT ICE PROTECTION TEMPERATURE HIGH LIGHT ILLUMINATED AS TAKEOFF THRUST WAS APPLIED. ABORTED TAKEOFF AT 50 KNOTS AND R ETURNED TO THE GATE. MAINTENANCE REPLACED THE LEFT ANTICIPATOR AND THERMOSTAT, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1997012300118 19970123 00118 WP 1997 1 23 UPS97821824 1 19961230 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 316.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-C, RT WING L/E RIB AT STA XFS 316.5 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED PE R SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1997012300119 19970123 00119 WP 1997 1 23 UPS97821825 1 19961230 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 329 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-C, RT WING L/E RIB AT STA XFS 329 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACKED AND REPAIRED PE R SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1997012300120 19970123 00120 WP 1997 1 23 UPS97821826 1 19961230 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 366. CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-C, RT WING L/E RIB AT STA XFS 366.5 IS CRACKED AT THE AFT UPPER EDGE. STOP DRILLED CRACK AND REPAIRED P ER SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1997012300121 19970123 00121 WP 1997 1 23 UPS97821827 1 19961230 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 360.2 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-C, RT WING L/E RIB AT STA XFS 360.25 IS CRACKED AT THE AFT UPPER EDGE. STOP DRILLED CRACK AND REPAIRED PER SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1997012300128 19970123 00128 NM 1997 1 23 DHL9774001C 1 19961230 A 5311 FRAME BOEING 727 7272Q9 138448M NM BS 203.8 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C-CHECK, CRACK IN FRAME AT STA 203.8, APPROX RBL 18. ACCOMPLISHED HFEC, NO NEW CRACKS, CRACK FROM PREVIOUS STOP DRIL L. INSTALLED ANGLE DOUBLER PER SRM 51-40-4, 16 INCHES LONG. 2 L 7 3 4F RT A3WE 1997012300131 19970123 00131 NM 1997 1 23 DHL9774004C 1 19961230 A 5330 SKIN BOEING 727 7272Q9 138448M NM BS 450 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C-CHECK, FOUND SKIN OIL CANNING AND HAS BULGE AT BS 450 BELOW STR 17R. CUT OUT DAMAGED AREAS AND INSTALLED DOUBLER R EPAIR PER SRM 53-30-3, DOUBLER 9 BY 6.5, FILLER 2.5 BY 1.5. 2 L 7 3 4F RT A3WE 1997012300132 19970123 00132 NM 1997 1 23 DHL9774005C 1 19961230 A 5240 SKIN BOEING 727 7272Q9 138448M NM FWD SERV DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C-CHECK, FWD SERVICE DOOR SKIN CRACKED FROM THE RIVET AT UPPER CORNER OF LOWER HINGE CUTOUT. STOP DRILLED PER SRM 51 -10-1, HFEC INSP, INSTALLED DOUBLER PER SRM 52-00-3, 5 BY 5. 2 L 7 3 4F RT A3WE 1997012300133 19970123 00133 NM 1997 1 23 DHL9774006C 1 19961231 A 2782 ACTUATOR MOUNT BOEING 727 7272Q9 138448M NM NR 5 LE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C-CHECK, NR 5 LEADING EDGE FLAP ACTUATOR MOUNT IS CRACKED AT INBOARD CORNERS. REMOVED AND REPLACED ACTUATOR MOUNT AT L/E FLAP PER SRM 51-10-1, REPAIR 6.5 BY 8. 2 L 7 3 4F RT A3WE 1997012300135 19970123 00135 NM 1997 1 23 DHL9774008C 1 19961230 A 5400 DUCT BOEING 727 7272Q9 138448M NM NR 2 ENGINE MISSING A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C-CHECK, NR 2 ENGINE INLET SHORT METAL CONNECTOR DUCT BETWEEN S-DUCT AND FWD FLANGE HAS APPROX 6 INCH SECTION OF FWD EDGE MISSING. REMOVED AND REPLACED INLET DUCT PER M/M 71-00-21. 2 L 7 3 4F RT A3WE 1997012300136 19970123 00136 NM 1997 1 23 DHL9774009C 1 19961231 A 7810 TAIL PIPE BOEING 727 7272Q9 138448M NM PWA JT8 JT8D7B 52053 NE NR 1 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 688155 AT C-CHECK, NR 1 ENGINE EXHAUST PIPE ACCOUSTIC LINER HAS APPROX 18 INCH CRACK AT 12 O'CLOCK. WELDED CRACK PER AVIATION EQUIPMENT OHM 727-23-5. 2 L 7 3 4F 4 F RT A3WE E2EA 1997012300145 19970123 00145 NM 1997 1 23 DHL9774018C 1 19961231 A 5320 ANGLE BOEING 727 7272Q9 138448M NM BS 1275 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C-CHECK, AFT AIRSTAIRS RT TORQUE BOX FS 1275 RBL 21 TO 28 WEB ATTACH ANGLE PREVIOUS REPAIR CRACKED UNDER AIRSTAIRS OPERATING MECHANISM FWD SIDE OF WEB. REPLACED DAMAGED ATTACH WEB ANGLES PER SRM 51-10-1, 7.5 BY 2 BY 1. 2 L 7 3 4F RT A3WE 1997012300146 19970123 00146 NM 1997 1 23 DHL9774019C 1 19961231 A 5312 BULKHEAD ANGLE BOEING 727 7272Q9 138448M NM BS 1263 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C-CHECK, AFT AIRSTAIRS RT TORQUE BOX FS 1263 RBL 23 AIRSTAIRS OPERATING MECHANISM SUPPORT STRUCTURE ATTACH ANGLES UND ER SHELF CRACKED FWD AND AFT SIDE OF BULKHEAD FS 1263. REPLACED DAMAGE ATTACH ANGLES PER SRM 51-10-1, 2.25 BY 7.5 BY 1 . 2 L 7 3 4F RT A3WE 1997012300147 19970123 00147 NM 1997 1 23 DHL9774020C 1 19961231 A 5320 ANGLE BOEING 727 7272Q9 138448M NM BS 1265 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 AT C-CHECK, AFT AIRSTAIRS TORQUE BOX SIDEWALL TO SHELF UPPER CHORD AND REPLACEMENT CHORD CRACKED FROM FS 1265 TO 1275 R BL 21. REMOVED AFT AIRSTAIR ACTUATOR AND SPRING, REPLACED CHORD ANGLE PER SRM 51-10-1, 22 BY 1.5 BY 1. INSTALLED ACTU ATOR AND SPRING. 2 L 7 3 4F RT A3WE 1997012300148 19970123 00148 NM 1997 1 23 DHL9774021C 1 19961231 A 5330 SKIN BOEING 727 7272Q9 138448M NM BS 228.8 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 740DH 21930 CORROSION ON INTERCOSTAL AND WATER DRAIN VALVE AREA STA 228, LBL 4. REMOVED DRAIN VALVE, INTERCOSTAL AND NOSE W/W SEAL. CUT OUT DAMAGED AREA, REMOVED CORROSION ON AJOINING AREA, INSTALLED REPAIR PER SRM 51-40-4, 2 BY 2. REINSTALLED SEAL, DRAIN VALVE AND INTERCOSTAL. 2 L 7 3 4F RT A3WE 1997012300236 19970123 00236 NM 1997 1 23 96UAL901006 1 19961215 A 5320 6550781 PRESSURE WEB BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE MLG WW CRACKED A UALA O OTHER O OTHER UK UNKNOWN 1 WP 29 9011U 19049 FUSELAGE COULD NOT BE PRESSURIZED. GLASS FABRIC/PLASTIC/PHENOLIC RESIN PRESSURE WEB CRACKED APPROXIMATELY 16 INCHES. W EB IS LOCATED IN THE MLG CEILING FWD LT O/B CORNER BETWEEN BS 664 AND 684. REPLACED WEB. 2 L 7 2 4F 4 F A16WE E2EA 1997012300237 19970123 00237 NM 1997 1 23 96UAL901007 1 19961231 A 3350 BATTERY PACK BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 4714U 19876 FOUND DOOR 1L, 5L AND 5R SLIDE EMERGENCY LIGHTS STAYED ON. UNABLE TO TURN OFF. REPLACED BATTERY PACK. 2 L 7 4 4F 4 F A20WE E20EA 1997012300238 19970123 00238 NM 1997 1 23 96UAL901008 1 19961231 A 2780 285T004953 FSEU BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE E/E BAY FAILED A UALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 WP 29 607UA 72794 21868 DURING CLIMB RECEIVED MASTER CAUTION AND LEADING EDGE AMBER LIGHT. THE AIRCRAFT RETURNED TO IAD. *S/D* THE FLAP SLAT ELECTRONIC UNIT INDICATED A NON-SUBSTANTIATED SLAT ASYMMETRY CONDITION. REPLACED FSEU, OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 1997012300240 19970123 00240 NM 1997 1 23 96UAL901010 1 19961231 A 2810 2670054 CHECK VALVE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE RT WING BROKEN A UALA O OTHER K FLUID LOSS IN INSP/MAINT 1 WP 29 7444U 21898 CREW REPORTED FUEL ALL OVER THE RAMP AFTER HOSE DISCONNECTED FROM AIRCRAFT. *S/D* MAINTENANCE FOUND FILL CONNECTION CH ECK VALVE MISSING. REMOVED ELBOW, BROKEN PIECES AND INSTALLED POPPET VALVE. 2 L 7 3 4F 4 F A3WE E2EA 1997012300241 19970123 00241 NM 1997 1 23 96UAL901011 1 19960305 A 2720 MKP4A BEARING PARKER 654486111 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RUDDER CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 2060A 24539 RUDDER PCU WAS REMOVED FROM AIRCRAFT TO ACCOMPLISH AD94-01-07. THE SUMMING LEVER BEARING WAS FOUND CRACKED AT THE INNER RACE. DURING SHOP OVERHAUL OF THE PCU THE PRIMARY SUMMING LEVER WAS REPLACED. AN ALTERNATE CONFIGURATION BOLT WAS USE D IN PLACE OF THE BOEING SPECIFIED SUMMING LEVER BOLT. THE BOLT HEAD-TO-SHANK RADIUS HAS AN UNFAVORABLE RELATIONSHIP WI TH THE BEARING INNER RACE ID CHAMFER, POSSIBLY CONTRIBUTING TO THE FAILURE OF THE BEARINGS INNER RACE. RUDDER OPS CHECK GOOD. NOW ACTIVELY REPLACING OLD BOLTS AND INSPECTING SUMMING LEVER BEARING INNER RACE TO VERIFY INTEGRITY ON ALL UNIT S. 2 L 7 2 4F 4 F RT A16WE E2GL 1997012300242 19970123 00242 NM 1997 1 23 96UAL901012 1 19961230 A 3350 BATTERY PACK BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 301UA 23642 EEL LIGHT INOP, ROW 3 THROUGH 9. REPLACED BATTERY PACK M1134, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 1997012300243 19970123 00243 NM 1997 1 23 96UAL901013 1 19961231 A 3350 LIGHT BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 938UA 26671 EEL LIGHT IS INOP FROM ROW 16 TO 20. REPLACED M1137 AND FLOOR TRACK CONNECTION EEL STRIP, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 1997012300244 19970123 00244 NM 1997 1 23 96UAL901014 1 19961221 A 2420 286W7860002 CONNECTOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE APU GENERATOR DAMAGED A UALA O OTHER H ELECT. POWER LOSS-50 PC NR NOT REPORTED 1 WP 29 776UA 26937 APU GENERATOR DROPS OFF LINE AFTER FOUR OR FIVE MINUTES OF OPERATION. FOUND OVERHEAT CONDITION FOR GENERATOR FEEDERS CA BLES. *S/D* AREA OF OVERHEAT WAS AT THE CABLE APU GENERATOR POWER PHASE LEAD TERMINAL INTERFACE. SUFFICIENT RESISTANC E WAS PRESENT TO CAUSE HEATING AND EVENTUAL FAILURE OF THE ELECTRICAL/MECHANICAL CONNECTION. LIKELY CAUSES CONTRIBUTING TO THE HIGH RESISTANCE INCLUDE THE HARDWARE ON THE POWER FEEDER CABLE PHASE TERMINATION AND/OR TORQUE VALUE ON THE NUT SECURING POWER FEEDER CABLE. PROCEDURES/IPC UNDER REVIEW BY UA/BOEING. ALERTS ISSUED BY UA. 2 L 7 2 4F 4 F RT T0001SE E46NE 1997012300331 19970123 00331 SW 1997 1 23 97ZZZX403 1 19961204 A 3231 222031194101 DOOR LINK 222031194101 BELL 222 222 1182122 SW NLG DOOR AFT FAILED A EGUA O OTHER O OTHER LD LANDING 1 GL 23 40EA 1487 47061 NOSE GEAR AFT DOOR LINK THAT CONNECTS DOOR TO NOSE GEAR STRUT FAILED WHERE ROD END ATTACHES LINK TO STRUT ALLOWING DOOR TO HANG DOWN FREELY. WHEN AIRCRAFT LANDED, DOOR WAS CAUGHT BETWEEN TIRE AND AIRFRAME AND BROKE OFF AT HINGE. NO OTHER DAMAGE RESULTED. DOOR IS FIBERGLASS COMPOSITE AND LINK IS PLASTIC. 1 G 7 2 3U H9SW 1997012300333 19970123 00333 SW 1997 1 23 97ZZZX405 1 19961210 A 6720 206030113 SUPPORT BELL 206 206B 1181511 SW NOSE TUNNEL CORRODED A A NYBA K NONE O OTHER IN INSP/MAINT 1 EA 11 83086 12551 914 DURING REPAIR IN LANDING LIGHT BAY AREA, MECHANIC NOTED BELLCRANK SUPPORT P/N 206-030-111-3 EXCESSIVELY CORRODED. REPLA CED BELLCRANK AND SUPPORT P/N 206-030-111-003. 1 G 7 1 3U H2SW 1997012300336 19970123 00336 CE 1997 1 23 S2YA960030 1 19961001 A 2840 10138901821 PRESSURE SWITCH BEECH 1900 1900D 1154162 CE AUX FUEL SYST FAILED A A S2YA K NONE O OTHER IN INSP/MAINT 1 GL 13 2324 DURING THE MONTH OF OCTOBER THERE WERE TWO FUEL PRESSURE SWITCH (P/N 101-389018-21) FAILURES. AIRCRAFT N NR 901SK PRESS URE SWITCH S/N NR 2895 FAILED AT 1316.4 HOURS. AIRCRAFT N NR 148SK PRESSURE SWITCH S/N NR 2050 FAILED AT 3320.0 HOURS. THE PRESSURE SWITCHES WERE FROM THE AUX FUEL TRANSFER SYSTEM, PRESSURE SWITCH S/N NR 2895 FAILED TO GIVE AN 'RT NO AUX XFR' ANNUNCIATOR IN THE 'ON' MODE AND PRESSURE SWITCH S/N NR 2050 FAILED TO GIVE AN 'LT NO AUX XFR' ANNUNCIATOR IN THE ' AUTO' MODE. THE MEAN TIME BETWEEN FAILURE WAS 2324.2 HOURS. (X) 2 L 7 2 4T RT A24CE 1997012300337 19970123 00337 CE 1997 1 23 S2YA960029 1 19960901 A 7714 1143800365 TACH INDICATOR BEECH 1900 1900D 1154162 CE INSTRUMENT PANEL INOPERATIVE A A S2YA K NONE O OTHER IN INSP/MAINT 1 GL 13 6088 DURING THE MONTH OF SEPTEMBER THERE WERE THREE TURBINE TACH INDICATORS, P/N 114-380036-5, THAT HAD PART OF THEIR LIGHTED DIGITAL READOUT BURN OUT, THE ANALOG PORTION OF THE INDICATOR REMAINED OPERATIVE. THE PARTS' TOTAL TIMES WERE 6105 HOU RS FROM A/C N NR 801SK, 6166.1 HOURS FROM A/C N NR 85SK, AND 5993 HOURS FROM A/C N NR 87SK. WHEN SENT OUT FOR REPAIR, INDICATORS' LIGHT BARS WERE REPLACED AND RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1997012300339 19970123 00339 NM 1997 1 23 MZZA96140 1 19961128 A 3397 WIRE BOEING 727 727224 1384076 NM CABIN CHAFED A MZZA K NONE L NO TEST IN INSP/MAINT 1 WP 13 69742 22251 GUM - DURING SERVICE CHECK, EMERGENCY AISLE PATH LIGHTS WOULD NOT TEST AT ROWS 17 TO 23, TROUBLESHOT AND FOUND FORWARD A ND AFT BATTERY CHARGERS BLOWING FUSES. FOUND SHORTED WIRE AT SEAT 22B CHAFFING ON SEAT ASSEMBLY. REPAIRED WIRE AND RER OUTED WIRE. REPLACED FUSES AND EMERGENCY LIGHT OPERATION RESTORED TO NORMAL. (M) 2 L 7 3 4F A3WE 1997012300340 19970123 00340 NM 1997 1 23 MZZA96141 1 19961206 A 7930 STB390 BYPASS LIGHT BOEING 727 727227 1384078 NM COCKPIT WIRE LOOSE A MZZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 13 89427 21365 FLT 951 - GUM - DURING CLIMB, ALL THREE ENGINE LOW PRESSURE FILTER BYPASS LIGHTS CAME ON. FOUND WIRE L26 AT FAULT. PER MM REF 33-19-02 CORRECTED FAULT. PERFORMED OPERATIONAL CHECK AND ALL INDICATIONS WERE NORMAL. AIRCRAFT RELEASED FOR S ERVICE. (M) 2 L 7 3 4F A3WE 1997012300341 19970123 00341 NM 1997 1 23 MZZA96142 1 19961122 A 5313 STRINGER BOEING 727 727224 1384076 NM BS 950 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT STRINGE R S-30 ROOT OF OUTER FLANGE AT BS 950A. THE CORRODED STRINGER WAS CLEANUP AND REPAIRED PER B 727 SRM 53-10-3 FIGURE 2. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 809746 (SEQ NR 01071) (M) 2 L 7 3 4F A3WE 1997012300342 19970123 00342 NM 1997 1 23 MZZA96143 1 19961122 A 5320 CORRODED TIE CHANNEL BOEING 727 727224 1384076 NM BS 950 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING 1/4 D-CHECK INSPECTION AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT STRINGER STRINGER 3 0 TIE CHANNEL AT BS 950 BULKHEAD. THE CORRODED STRINGER TIE CHANNEL WAS REMOVED AND REPLACED WITH NEW STRINGER TIE CHAN NEL PER B 727 SRM 51-30-2. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 809747 (SEQ NR 01072). (M) 2 L 7 3 4F A3WE 1997012300343 19970123 00343 NM 1997 1 23 MZZA96144 1 19961125 A 5320 SHEART TIE BOEING 727 727224 1384076 NM BS 1166 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING 1/4 D-CHECK INSPECTION ON A/C AT AIR ASIA, SEVERE CORROSION WAS FOUND ON BS 1166 FRAME SHEAR TIE BETWEEN ST RINGER 29R AND STRINGER 28L. THE CORRODED SHEAR TIE FROM STRINGER 29R TO STRINGER 28L WAS REMOVED AND REPLACED WITH NEW SHEAR TIE PER B727 SRM 53-10-4. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 809768 (SEQ NR 01143). (M) 2 L 7 3 4F A3WE 1997012300344 19970123 00344 NM 1997 1 23 MZZA96145 1 19961125 A 5311 FRAME BOEING 727 727224 1384076 NM BS 1166 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 DURING 1/4 D-CHECK INSPECTION ON A/C AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT BS 1166 FRAME LOWE R FLANGE BETWEEN STRINGER 30 AND STRINGER 29R. THE DAMAGED PART OF FRAME WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-1 0-4 FIGURE 11. REF - HANGAR NON ROUTINE REPAIR ITEM CARD NR 809769 (SEQ NR 01144). (M) 2 L 7 3 4F A3WE 1997012300345 19970123 00345 NM 1997 1 23 MZZA96146 1 19961125 A 5320 SHEAR TIE BOEING 727 727224 1384076 NM BS 1148 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING 1/4 D-CHECK INSPECTION ON A/C AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT BS 1148 FRAM E SHEAR TIE BETWEEN STRINGER 27R AND STRINGER 28R. THE CORRODED SHEAR TIE WAS REMOVED AND REPLACED WITH NEW SHEAR TIE P ER B727 SRM 53-10-4. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 809770 (SEQ NR 01145). (M) 2 L 7 3 4F A3WE 1997012300346 19970123 00346 NM 1997 1 23 MZZA96147 1 19961125 A 5320 SHEAR TIE BOEING 727 727224 1384076 NM BS 1130 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING 1/4 D-CHECK INSPECTION ON A/C AT AIR ASIIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT BS 1130 FR AME SHEAR TIE BETWEEN STRINGER 27R AND STRINGER 29R. THE CORRODED SHEAR TIE WAS REMOVED AND REPLACES WITH NEW SHEAR TIE PER B727 SRM 53-10-4. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 809772 (SEQ NR 01147). (M) 2 L 7 3 4F A3WE 1997012300347 19970123 00347 NM 1997 1 23 MZZA96148 1 19961125 A 5320 SHEAR TIE BOEING 727 727224 1384076 NM BS 1130 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING 1/4 D-CHECK INSPECTION ON A/C AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT BS 1130 FRAM E SHEAR TO BETWEEN STRINGER 29L AND STRINGER 30. THE CORRODED SHEAR TIE WAS REMOVED AND REPLACED WITH NEW SHEAR TIE PER B 727 SRM 53-10-4. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 809773 (SEQ NR 01148) 2 L 7 3 4F A3WE 1997012300348 19970123 00348 NM 1997 1 23 MZZA96149 1 19961125 A 5320 SHEAR TIE BOEING 727 727224 1384076 NM BS 1130 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT BS 1130 FRAME SHEAR TIE BETWEEN STRINGER 27L AND STRINGER 28L. THE CORRODED SHEAR TIE WAS REMOVED AND REPLACED WITH NEW SHEAR TIE PER B727 SRM 53-10-4. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 809774 (SEQ NR 01149). (M) 2 L 7 3 4F A3WE 1997012300349 19970123 00349 NM 1997 1 23 MZZA96150 1 19961125 A 5320 69455802 FITTING BOEING 727 727224 1384076 NM C2 CARGO DOOR BROKEN A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING 1/4 D-CHECK INSPECTION ON A/C AT AIR ASIA, C2 CARGO DOOR UPPER STOP FITTING WAS FOUND TO BE BROKEN AT BS 95 0F. THE DAMAGED STOP FITTING, P/N 69-45580-2 WAS REMOVED AND REPLACED PER B727 SRM 51-30-2 AND DOOR OPERATIONAL CHECK F OUND SATISFACTORY. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 809795 (SEQ NR 01170). ( M) 2 L 7 3 4F A3WE 1997012300350 19970123 00350 NM 1997 1 23 MZZA96151 1 19961127 A 5313 STRINGER BOEING 727 727224 1384076 NM BS 710 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON FORWARD CARGO COMPARTMENT STR INGER 26L BETWEEN BS 706 AND BS 710. THE CORRODED STRINGER FROM BS 704 TO BS 712 WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-10-3 FIGURE 1. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 809909 (SEQ NR 01244). (M) 2 L 7 3 4F A3WE 1997012300351 19970123 00351 NM 1997 1 23 MZZA96152 1 19961122 A 3350 EXIT SIGN BOEING 727 727224 1384076 NM CABIN BROKEN A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, BROKEN "EXIT' SIGN COVERS WERE FOUND PASSENGER CABIN AT THE FOLLOWING POSTION, LEFT FORWARD EMERGENCY EXIT DOOR, RIGHT FORWARD EMERGENCY EXIT DOOR. THE DAMAGED 'EXIT' SIGN ASSEMB LIES WERE REMOVED AND REPLACED WITH P/N 9003-27 PER B727 MM 33-50-11 AND OPERATIONAL CHECK FOUND SATISFACTORY. REF, HAN GAR NON ROUTINE REPAIR ITEM CARDS NR 808953 AND 808954 (SEQ NR 02133 AND 02134). (M) 2 L 7 3 4F A3WE 1997012300352 19970123 00352 NM 1997 1 23 MZZA96153 1 19961121 A 3350 EXIT SIGN BOEING 727 727224 1384076 NM CABIN BROKEN A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING 1/4 D-CHECK INSPECTION ON A/C AT AIR ASIA, BROKEN 'EXIT' SIGN COVER WAS FOUND ON R1 GALLEY SERVICE DOOR. T HE DAMAGED 'EXIT' SIGN ASSEMBLY WAS REMOVED AND REPLACED WITH P/N BR9279-106 PER B727 MM 33-50-11 AND OPERATIONAL CHECK FOUND SATISFACTORY. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 808955 (SEQ NR 02135). (M) 2 L 7 3 4F A3WE 1997012300353 19970123 00353 NM 1997 1 23 MZZA96154 1 19961122 A 3350 10617891007 EMERGENCY SIGN BOEING 727 727224 1384076 NM CABIN FAILED TEST A MZZA K NONE L NO TEST IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING SELF ILLUMINATION SIGN BRIGHTNESS TEST PER 1/4 D-CHECK, WORK CARD 07-1130-1-7301 ON A/C AT AIR ASIA, EMERGE NCY EXIT DOOR 'EMERGENCY' SIGN BRIGHTNESS MEASUREMENT WERE FOUND BELOW THE SPECIFIED LIMIT (100 MICROLAMBERTS) AT THE FO LLOWING POSITION; RIGHT FORWARD EMERGENCY EXIT DOOR, RIGHT AFT EMERGENCY EXIT DOOR, LEFT FORWARD EMERGENCY EXIT DOOR, LE FT AFT EMERGENCY EXIT DOOR. THE 'EMERGENCY SIGNS WERE REMOVED AND REPLACED PER B727 MM 33-50-31. (M) 2 L 7 3 4F A3WE 1997012300354 19970123 00354 NM 1997 1 23 MZZA96155 1 19961121 A 5330 SKIN BOEING 727 727224 1384076 NM BS 1218 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING 1/4 D-CHECK INSPECTION ON A/C AT AIR ASIA, 1 INCH LONG CRACK WAS FOUND ON LEFT SIDE VENTRAL STAIRWALL TORQU E BOX LIGHTENING HOLE CUTOUT AT BS 1218. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM 51-40-2 FIGURE 1. REF, H ANGAR NON ROUTINE REPAIR ITEM CARD NR 809714 (SEQ 02156). (M) 2 L 7 3 4F A3WE 1997012300355 19970123 00355 NM 1997 1 23 MZZA96156 1 19961121 A 5330 SKIN BOEING 727 727224 1384076 NM BS 1238 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING 1/4D-CHECK INSPECTION ON A/C AT AIR ASIA, .5 INCH LONG CRACK WAS FOUND ON LEFT SIDE VENTRAL STAIRWALL TORQU E BOX LIGHTENING HOLE CUT OUT AT BS 1238. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM 51-40-2 FIGURE 1. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 809715 9SEQ NR 02157). (M) 2 L 7 3 4F A3WE 1997012300356 19970123 00356 NM 1997 1 23 MZZA96157 1 19961112 A 5330 SKIN BOEING 727 727224 1384076 NM BS 1235 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING 1/4 D-CHECK INSPECTION ON A/C AT AIR ASIA, .5 INCH LONG CRACK WAS FOUND ON LEFT SIDE VENTRAL STAIRWALL TORQ UE BOX LIGHTENING HOLE CUTOUT AT BS 1235. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM 51-40-2 FIGURE 1. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 809716 (SEQ NR 02158). (M) 2 L 7 3 4F A3WE 1997012300357 19970123 00357 NM 1997 1 23 MZZA96158 1 19961121 A 5330 SKIN BOEING 727 727224 1384076 NM BS 1235 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, .5 INCH LONG CRACK WAS FOUND ON RIGHT SIDE VENTRAL STAIRWAL L TORQUE BOX LIGHTENING HOLE CUTOUT AT BS 1235. THE CRACK WAS STOP DRILLED AND REPAIRED PER B 727 SRM 51-40-2 FIGURE 1. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 809717 (SEQ NR 02159). (M) 2 L 7 3 4F A3WE 1997012300358 19970123 00358 NM 1997 1 23 MZZA96159 1 19961123 A 5543 SKIN BOEING 727 727224 1384076 NM RUDDER TAB CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING 1/4 D-CHECK INSPECTION ON A/C AT AIR ASIA, SEVERE CORROSION WAS FOUND ON UPPER RUDDER TAB L/E NOSE SKIN AT RUDDER STATION 175 AND 196. THE CORRODED NOSE SKINS, P/N 65-62445-6 AND 65-65445-7 WERE REMOVED AND REPLACED PER B727 SRM 55-40-1 IN CONJUNCTION WITH BOEING PARTS LIST NR PL65-62445. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 809755 (SE Q NR 03005). (M) 2 L 7 3 4F A3WE 1997012300359 19970123 00359 NM 1997 1 23 MZZA96160 1 19961123 A 5543 SKIN BOEING 727 727224 1384076 NM RUDDER TAB CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING 1/4D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON LOWER RUDDER TAB L/E NOSE SKIN AT RUDDER STATION 159, 136 AND 83. THE CORRODED NOSE SKINS, P/N 65-62444-2, 65-62444-3 AND 65-62444-6 AND WERE REMOVED AND REPLACED PER B 727 SRM 55-40-1 IN CONJUNTION WITH BOEING PARTS LIST NR PL65-62444. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 809757 (SEQ NR 03007). (M) 2 L 7 3 4F A3WE 1997012300360 19970123 00360 NM 1997 1 23 MZZA96161 1 19961126 A 5520 ELEV TABS BOEING 727 727224 1384076 NM LT/RT ELEV REQ'D REPAINT A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, PER CUSTOMER REQUEST ITEMS TO REPAINT LT/RT ELEVATORS AND T ABS. THE LT/RT ELEVATORS AND TABS WERE REPAINTED AND REBALANCED PER CONTINENTAL DRAWING NR 5100D8465 ADN B727 SRM 51-80 -7 AND -9 RESPECTIVE. REF, HANGAR NON ROUTINE REPAIR ITEM CARDS NR 815477 AND 815478 (SEQ NR 03036 AND 03037) (M) 2 L 7 3 4F A3WE 1997012300361 19970123 00361 NM 1997 1 23 MZZA96162 1 19961120 A 5755 SKIN BOEING 727 727224 1384076 NM NR 2 SPOILER DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING 1/4 D-CHECK INSPECTION ON A/C AT AIR ASIA, DELAMINATION WAS FOUND ON LT WING NR 2 SPOILER UPPER SKIN NEAR O UTBOARD EDGE. THE DAMAGED SKIN 4 INCH BY 3 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. REF, HANGAR NON-ROUTINE REPAIR ITEM CARD NR 809194 (SEQ NR 05024) (M) 2 L 7 3 4F A3WE 1997012300362 19970123 00362 NM 1997 1 23 MZZA96163 1 19961125 A 5753 SKIN BOEING 727 727224 1384076 NM NR 1 AFT FLAP DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON LT WING T/E NR 1 AFT FLAP LOWER S KIN AT WBL 467. THE DAMAGED SKIN 6 INCH BY 4 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M) 2 L 7 3 4F A3WE 1997012300363 19970123 00363 NM 1997 1 23 MZZA96164 1 19961125 A 5753 SKIN BOEING 727 727224 1384076 NM NR 2 FORE FLAP DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING Q/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON LEFT WING NR 2 FORE FLAP T/E LOWE R SKIN BETWEEN WBL 127 AND WBL 140. THE DAMAGED SKIN 13 INCH BY 8.5 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 809245 (SEQ NR 05045). (M) 2 L 7 3 4F A3WE 1997012300364 19970123 00364 NM 1997 1 23 MZZA96165 1 19961127 A 5754 SKIN BOEING 727 727224 1384076 NM NR 1 LE FLAP CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURNIG 1/4 D-CHECK INSPECTION ON A/C AT AIR ASIA, SEVERE CORROSION WAS FOUND ON LT WING NR 1 L/E FLAP SKIN INTERIO R SURFACE AT LES 306. THE CORRODED SKIN WAS CLEAN UP AND REPAIRED PER B727 SRM 57-50-3, FIG 2. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 809302 (SEQ NR 05052). (M) 2 L 7 3 4F A3WE 1997012300365 19970123 00365 NM 1997 1 23 MZZA96166 1 19961120 A 5755 SKIN BOEING 727 727224 1384076 NM NR 9 SPOILER DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON RT WING NR 9 SPOILER T/E UPPER SKIN. THE DAMAGED SKIN 16 INCH BY 6 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 809215 (SEQ NR 06015). (M) 2 L 7 3 4F A3WE 1997012300366 19970123 00366 NM 1997 1 23 MZZA96167 1 19961120 A 5755 SKIN BOEING 727 727224 1384076 NM NR 12 SPOILER DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON RT WING NR 12 SPOILER UPPER SKIN. THE DAMAGED SKIN 7 INCH BY 6 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 809216 (SEQ NR 06016). (M) 2 L 7 3 4F A3WE 1997012300367 19970123 00367 NM 1997 1 23 MZZA96168 1 19961209 A 7931 ST1042 TRANSMITTER BOEING 727 727232 1384082 NM NR 2 ENGINE FAILED A MZZA O OTHER N FALSE WARNING CL CLIMB 1 WP 13 15790 20644 FLT 951 - GUM - AFTER TAKEOFF, NR 2 OIL PRESSURE WENT TO ZERO. SHORTLY THEREAFTER PRESSURE RETURNED TO NORMAL. GUM MAI NTENANCE ADVISED FLIGHT CREW TO RETURN TO GUM DUE TO NO MAINTENANCE IN ROR AND YAP. REMOVED AND REPLACED NR 2 OIL PRESS URE TRANSMITTER PER MM 79-32-1. ALSO, REPLACED NR 2 QIL PRESSURE TRANSMITTER PER MM 79-32-1. ALSO, REPLACED NR 2 QIL P RESSURE GAUGE AS PRECAUTIONARY. LEAK CHECK AND OPERATIONAL CHECK NORMAL ON ENGINE RUN. (M) 2 L 7 3 4F A3WE 1997012300368 19970123 00368 NM 1997 1 23 MZZA96172 1 19961206 A 5313 655612910 STRINGER BOEING 727 727224 1384076 NM BS 950 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, INTERGRANNULAR CORROSION WAS FOUND ON AFT CARGO COMPARTMENT AT STRINGER 27R OUTBOARD CHORD BETWEEN BS 950E AND 950E PLUS 5. THE CORRODED STRINGER 27R OUTBOARD CHORD WAS CLEAN UP AND REPAIRED PER EC/RA 5330-02473. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 810119 (SEQ NR 01075) (M) 2 L 7 3 4F A3WE 1997012300369 19970123 00369 NM 1997 1 23 MZZA96173 1 19961207 A 5330 SKIN BOEING 727 727224 1384076 NM BS 720 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON FUSELAGE BELLY SKIN BETWEEN BS 700 AND BS 720 AT STRINGER 28R AND STRINGER 28L. THE CORRODED SKIN 4 INCH BY 21 INCH IN SIZE ON STRINGER 28L AND 5 INCH BY 21 INCH IN SIZE ON STRINGER 28R, WERE TRIMMED OUT AND REPAIRED PER B727 SRM 53-30-3 FIGURE 1. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 809958 (SEQ NR 01082). (M) 2 L 7 3 4F A3WE 1997012300370 19970123 00370 NM 1997 1 23 MZZA96174 1 19961207 A 5311 FRAME BOEING 727 727224 1384076 NM BS 720 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON FORWARD CARGO COMPARTMENT BS 720 FRAME LOWER FLANGE AT STRINGER 28R. THE CORRODED FRAME LOWER FLANGE WAS TRIMMED OUT AND REPIRED PER B727 SRM 51-40- 3 FIGURE 1. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 809961 (SEQ NR 01085). (M) 2 L 7 3 4F A3WE 1997012300371 19970123 00371 NM 1997 1 23 MZZA96175 1 19961207 A 5311 FRAME BOEING 727 727224 1384076 NM BS 950 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT BS 950F FRAME LOWER FORWARD FLANGE AT STRINGER 29R. THE CORRODED FRAME FLANGE WAS TRIMMED AND REPAIRED PER B727 SRM 51-40-2 FI GURE 1. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 810143 (SEQ NR 01103). (M) 2 L 7 3 4F A3WE 1997012300372 19970123 00372 NM 1997 1 23 MZZA96176 1 19961207 A 5311 FRAME BOEING 727 727224 1384076 NM BS 970 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURNIG 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT BS 970 FRAME LOWER FORWARD FLANGE. THE CORRODED FRAME FLANGE WAS TRIMMED AND REPAIRED PER B727 SRM 51-40-2, FIGURE 1. REF, HA NGAR NON ROUTINE REPAIR ITEM CARD NR 810147, (SEQ NR 01107). (M) 2 L 7 3 4F A3WE 1997012300373 19970123 00373 NM 1997 1 23 MZZA96177 1 19961207 A 5311 FRAME BOEING 727 727224 1384076 NM BS 970 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT BS 970 FRAME AFT LOWER CHORD BETWEEN STRINGER 29R AND STRINGER 28R. THE CORRODED FRAME LOWER CHORD WAS TRIMMED OUT AND REPAIRE D PER B727 SRM 51-40-3 FIGURE 1. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 810149 (SEQ NR 01109). (M) 2 L 7 3 4F A3WE 1997012300374 19970123 00374 NM 1997 1 23 MZZA96178 1 19961207 A 5311 FRAME BOEING 727 727224 1384076 NM BS 970 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING 1/4 D-CHECK INSPECTION ON A/C AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT BS 970 FRAME AFT LOWER CHORD BETWEEN STRINGER 28R AND STRINGER 27R. THE CORRODED FRAME LOWER CHORD WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-3 FIGURE. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 810150 (SEQ NR 01110). (M) 2 L 7 3 4F A3WE 1997012300375 19970123 00375 NM 1997 1 23 MZZA96179 1 19961207 A 5311 FRAME BOEING 727 727224 1384076 NM BS 1130 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING 1/4 D-CHECK INSPECTION ON A/C AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT BS 1130 FRAM E SHEAR TIE AT STRINGER 29L. THE CORRODED SHEAR TIE WAS REMOVED AND REPLACED WITH NEW SHEAR TIE PER B727 SRM 53-10-4 FI GURE 15. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 810163 (SEQ NR 01123). (M) 2 L 7 3 4F A3WE 1997012300376 19970123 00376 NM 1997 1 23 MZZA96180 1 19961207 A 5311 FRAME BOEING 727 727224 1384076 NM BS 700 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING 1/4 D-CHECK INSPECTION ON A/C AT AIR ASIA, SEVERE CORROSION WAS FOUND ON FORWARD CARGO COMPARTMENT BS 700 F RAME SHEAR TIE BETWEEN STRINGER 27R AND STRINGER 28R. THE CORRODED SHEAR TIE WAS REMOVED AND REPLACED WITH NEW SHEAR TI E PER B727 SRM 53-10-4 FIGURE 15. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 809962 (SEQ NR 01139). (M) 2 L 7 3 4F A3WE 1997012300377 19970123 00377 NM 1997 1 23 MZZA96181 1 19961207 A 5313 STRINGER BOEING 727 727224 1384076 NM BS 720 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING 1/4 D-CHECK INSPECTION ON A/C AT AIR ASIA, SEVERE CORROSION WAS FOUND ON FORWARD CARGO COMPARTMENT STRINGER 28R BETWEEN BS 700 AND BS 720. THE CORRODED STRINGER FROM BS 684 TO BS 725 WAS TRIMMED OUT AND REPLACED WITH NEW HAT S ECTION STRINGER PER B727 SRM 53-10-3 FIGURE 1. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 809963 (SEQ NR 01140). (M) 2 L 7 3 4F A3WE 1997012300378 19970123 00378 NM 1997 1 23 MZZA96182 1 19961209 A 5320 6518915286 CHANNEL BOEING 727 727224 1384076 NM NLG W/W CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING 1/4 D-CHECK INSPECTION ON A/C AT AIR ASIA, SEVERE CORROSION WAS FOUND ON NLG LEFT TRUNNING SUPPORT FITTING FORWARD LEG ATTACHED EXTRUDED 'U' CHANNEL AT BS 303.9. THE CORRODED 'U' CHANNEL WAS CLEANUP AND REPAIRED PER EC/RA 5340 -01286. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 809989 (SEQ NR 01167). (M) 2 L 7 3 4F A3WE 1997012300379 19970123 00379 NM 1997 1 23 MZZA96183 1 19961205 A 5320 WEB BOEING 727 727224 1384076 NM BS 1238 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, .75 INCH LONG CRACK WAS FOUND ON RT SIDE VENTRAL STAIRWALL TORQUE BOX WEB AT BS 1238. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM 51-40-2 FIGURE 1. REF, HANGAR NON RUOT INE REPAIR ITME CARD NR 810097 (SEQ NR 02125). (M) 2 L 7 3 4F A3WE 1997012300380 19970123 00380 NM 1997 1 23 MZZA96184 1 19961205 A 5330 WEB BOEING 727 727224 1384076 NM BS 1225 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, .5 INCH LONG CRACK WAS FOUND ON LEFT SIDE VENTRAL STAIRWALL TORQUE BOX WEB AT BS 1225. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM 51-40-2 FIGURE 1. REF, HANGAR NON ROU TINE REPAIR ITEM CARD NR 810098 (SEQ NR 02126) (M) 2 L 7 3 4F A3WE 1997012300381 19970123 00381 NM 1997 1 23 MZZA96185 1 19961205 A 5320 WEB BOEING 727 727224 1384076 NM BS 1213-1303 OIL CANNING A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING 1/4 D-CHECK INSPECTION ON A/R AT AIR ASIA, OIL CANNING WERE FOUND ON RT SIDE VENTRAL STAIRWALL TORQUE BOX W EB AT THE FOLLOWING AREAS; BETWEEN BS 1213 AND BS 1223, BETWEEN BS 1223 AND 1233, BETWEEN BS 1233 AND BS 1243, AND BETWE EN BS 1293 AND BS 1303. THE DAMAGED WEBS WERE REPAIRED PER B727 SRM 51-40-2 FIGURE 1. REF, HANGAR NON ROUTINE REPAIR I TEM CARDS NR 810099, 810100, 810101 AND 810102 (SEQ NR 02127, 02128, 02129 AND 02130). (M) 2 L 7 3 4F A3WE 1997012300382 19970123 00382 NM 1997 1 23 MZZA96186 1 19961205 A 5320 WEB BOEING 727 727224 1384076 NM BS 1243-1323 OIL CANNING A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING 1/4 D-CHECK INSPECTION ON A/C AT AIR ASIA, OIL CANNING WERE FOUND ON LT SIDE VENTRAL STAIRWALL TORQUE BOX W EB AT THE FOLLOWING AREA; BETWEEN BS 1243 AND BS1253, BETWEEN BS 1283 AND BS 1293, BETWEEN BS 1313 AND BS 1323. THE DAM AGED WEBS WERE REPAIRED PER B 727 SRM 51-40-2 FIGURE 1. REF HANGAR NON ROUTINE REPAIR ITEM CARDS NR 810103, 810104 AND 810105 (SEQ NR 02138, 02139 AND 02140). (M) 2 L 7 3 4F A3WE 1997012300383 19970123 00383 NM 1997 1 23 MZZA96187 1 19961206 A 3350 10617891008 SIGN BOEING 727 727224 1384076 NM EXIT DOOR INOPERATIVE A MZZA K NONE L NO TEST IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING SELF ILLUMINATION SIGN BRIGHTNESS TEST PER 1/4 D-CHECK WORK CARD 07-1130-1-7301 ON A/C AT AIR ASIA, EMERGNE CY EXIT DOOR 'PULL' SIGN BRIGHTNESS MEASUREMENT WERE FOUND BELOW THE SPECIFIED LIMIT (100 MICROLAMBERTS) AT THE FOLLOWIN G POSITION; RT FORWARD EMERGENCY EXIT DOOR, RT AFT EMERGENCY EXIT DOOR, LT FORWARD EMERGENCY EXIT DOOR, LT AFT EMERGENCY EXIT DOOR. THE 'PULL' SIGNS WERE REMOVED AND REPLACED PER B727 MM 33-50-31. REF, HANGAR NON ROUTINE REPAIR ITEM CARDS NR 809936, 809937, 809938 AND 809939 (SEQ NR 02141, 02142, 02143 AND 02144). (M) 2 L 7 3 4F A3WE 1997012300384 19970123 00384 NM 1997 1 23 MZZA96188 1 19961206 A 3350 10617891007 SIGN BOEING 727 727224 1384076 NM EXIT DOOR INOPERATIVE A MZZA K NONE L NO TEST IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING SELF ILLUMINATION SIGN BRIGHTNESS TEST PER 1/4 D-CHECK WORK CARD 07-1130-1-7301 ON A/C AT AIR ASIA, EMERGEN CY EXIT DOOR 'EMERGENCY' SIGN BRIGHTNESS MEASUREMENT WRE FOUND BELOW THE SPECIFIED LIMIT (100 MIRCROLAMBERTS) AT THE FOL LOWING POSITION; RT FORWARD EMERGENCY EXIT DOOR, RT AFT EMERGENCY EXIT DOOR, LT FORWARD EMERGENCY EXIT DOOR, LT AFT EMER GENCY EXIT DOOR. THE 'EMERGENCY' SIGNS WERE REMOVED AND REPLACED PER B727 MM 33-50-31. REF, HANGAR NON ROUTINE REPAIR ITEM CARDS NR 809936, 809937, 809938 AND 809939 (SEQ NR 02141, 02142, 02143 AND 02144). (M) 2 L 7 3 4F A3WE 1997012300385 19970123 00385 NM 1997 1 23 MZZA96189 1 19961210 A 3350 SIGN COVER BOEING 727 727224 1384076 NM CABIN BROKEN A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING 1/4 D-CHECK INSPECTION ON A/C AT AIR ASIA, BROKEN 'EXIT' SIGN BASE WAS FOUND ON RT AFTER EMERGENCY EXIT DOO R. THE DAMAGED 'EXIT' SIGN ASSEMBLY WAS REMOVED AND REPLACED WITH P/N BR9279-106 PER B727 MM 33-50-11 AND OPERATIONAL C HECK FOUND SATISFACTORY. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 814530 (SEQ NR 02313). (M) 2 L 7 3 4F A3WE 1997012300386 19970123 00386 NM 1997 1 23 MZZA96190 1 19961207 A 5543 SKIN BOEING 727 727224 1384076 NM RUDDER DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING 1/4 D-CHECK INSPECTION ON A/C AT AIR ASIA, DELAMINATION WAS FOUND ON UPPER RUDDER TAB RT L/E SKIN AT RUDDER STATION 270. THE DAMAGED SKIN 3 INCH BY 15 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. REF, HANGA R NON ROUTINE REPAIR ITEM CARD NR 815494 (SEQ 03012). (M) 2 L 7 3 4F A3WE 1997012300387 19970123 00387 NM 1997 1 23 MZZA96191 1 19961206 A 5543 65624444 SKIN BOEING 727 727224 1384076 NM RUDDER CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING 1/4 D-CHECK INSPECTION ON A/C AT AIR ASIA, EXFOLIATION CORROSIO WAS FOUND ON LOWER RUDDER TAB NOSE SKIN AT RUDDER STATION 130. THE CORRODED NOSE SKIN, P/N 65-62444-4 WAS REMOVED AND REPLACED PER B727 SRM 55-40-1 IN CONJUNCTION WITH BOEING PARTS LIST NR PL65-62444. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 815495 (SEQ NR 03015). (M) 2 L 7 3 4F A3WE 1997012300388 19970123 00388 NM 1997 1 23 MZZA96192 1 19961207 A 5543 SKIN BOEING 727 727224 1384076 NM RUDDER CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING 1/4 D-CHECK INSPECTION ON A/C AT AIR ASIA, SEVERE CORROSION WAS FOUND ON UPPER RUDDER TAB LT L/E SKIN AT RU DDER STATION 185. THE CORRODED SKIN 6 INCH BY 6 INCH WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. REF, HANGAR NO N ROUTINE REPAIR ITEM CARD NR 815508 (SEQ NR 03028). (M) 2 L 7 3 4F A3WE 1997012300389 19970123 00389 NM 1997 1 23 MZZA96193 1 19961205 A 5753 SKIN BOEING 727 727224 1384076 NM NR 1 MID FLAP CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING 1/4 D-CHECK INSPECTION ON A/C AT AIR ASIA, SEVERE CORROSION WAS FOUND ON LT WING OUTBOARD T/E MID FLAP LOWR SKIN AT WBL 444. THE CORRODED SKIN WAS CLEANUP AND REPAIRED PER B727 SRM 57-50-4 FIGURE 3. REF, HANGAR NON ROUTINE RE PAIR ITEM CARD NR 809349 (SEQ NR 05009). (M) 2 L 7 3 4F A3WE 1997012300390 19970123 00390 NM 1997 1 23 MZZA96194 1 19961215 A 5753 SKIN BOEING 727 727224 1384076 NM NR 1 MID FLAP CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING 1/4 D-CHECK INSPECTION ON A/C AT AIR ASIA, SEVERE CORROSION WAS FOUND ON LT WING OUTBOARD T/E MID FLAP LOWE R SKIN AT WBL 350. THE CORRODED SKIN 2 INCH BY 2 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 57-50-4 FIGURE 3. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 809350 (SEQ NR 05010). (M) 2 L 7 3 4F A3WE 1997012300391 19970123 00391 NM 1997 1 23 MZZA96195 1 19961206 A 5754 SKIN BOEING 727 727224 1384076 NM NR 1 LE SLAT CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON LT WING L/E NR 1 SLAT LOWER S KIN AROUND SCREW HEADS AT BS 421. THE CORRODED SKIN WAS CLEANED AND REPAIRED PER B727 SRM 57-50-3 FIGURE 1. REF, HANGA R NON ROUTINE REPAIR ITEM CARD NR 809362 (SEQ NR 05022) (M) 2 L 7 3 4F A3WE 1997012300392 19970123 00392 NM 1997 1 23 MZZA96196 1 19961209 A 5753 SKIN BOEING 727 727224 1384076 NM NR 1 FORE FLAP DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON LT WING OUTBOARD T/E FORE FLAP UP PER SKIN AT WBL 420. THE DAMAGED SKIN 2 INCH BY 3 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 810207 (SEQ NR 05057). (M) 2 L 7 3 4F A3WE 1997012300393 19970123 00393 NM 1997 1 23 MZZA96197 1 19961209 A 5753 SKIN BOEING 727 727224 1384076 NM NR 2 TE MID FLAP DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING 1/4 D-CHECK INSPECTION ON A/C AT AIR ASIA, DELAMINATION WAS FOUND ON LT WING INBOARD T/E MID FLAP T/E LOWER SKIN AT WBL 92. THE DAMAGED SKIN 3.75 INCH BY 11 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 810222 (SEQ NR 05072). (M) 2 L 7 3 4F A3WE 1997012300394 19970123 00394 NM 1997 1 23 MZZA96198 1 19961209 A 5753 SKIN BOEING 727 727224 1384076 NM NR2 TE FORE FLAP DISBONDED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING 1/4 D-CHECK INSPECTION ON A/C AT AIR ASIA, DISBONDED WAS FOUND ON LT WING INBOARD T/E FORE FLAP UPPER SKIN AT INBOARD AFT CORNER. THE DAMAGED SKIN 2 INCH BY 8 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. RE F, HANGAR NON ROUTINE REPAIR ITEM CARD NR 810223 (SEQ NR 05073). (M) 2 L 7 3 4F A3WE 1997012300395 19970123 00395 NM 1997 1 23 MZZA96199 1 19961212 A 5753 SKIN BOEING 727 727224 1384076 NM NR2 TE MID FLAP DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING 1/4 D-CHECK INSPECTION ON A/C AT AIR ASIA, DELAMINATION WAS FOUND ON LT WING INBOARD T/E MID FLAP T/E UPPER SKIN AT WBL 129. THE DAMAGED SKIN 4 INCH BY 6.5 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 810287 (SEQ NR 05087). (M) 2 L 7 3 4F A3WE 1997012300396 19970123 00396 NM 1997 1 23 MZZA96200 1 19961212 A 5753 SKIN BOEING 727 727224 1384076 NM NR2 AFT TE FLAP SEPARATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING 1/4 D-CHECK INSPECTION ON A/C AT AIR ASIA, DELAMINATION WAS FOUND ON LT WING INBOARD T/E AFT FLAP T/E UPPER SKIN BETWEEN WBL 78 AND WBL 86. THE DAMAGED SKIN 4 INCH BY 8 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51 -40-6. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 810288 (SEQ NR05088). (M) 2 L 7 3 4F A3WE 1997012300397 19970123 00397 NM 1997 1 23 MZZA96201 1 19961205 A 5755 SKIN BOEING 727 727224 1384076 NM NR 11 SPOILER DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON RT WING NR 11 SPOILER UPPER SKIN NEAR OUTBOARD. THE DAMAGED SKIN 9 INCH BY 12 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. REF, HANG AR NON ROUTINE REPAIR ITEM CARD NR 809391 (SEQ NR 06011). (M) 2 L 7 3 4F A3WE 1997012300398 19970123 00398 NM 1997 1 23 MZZA96202 1 19961209 A 5753 SKIN BOEING 727 727224 1384076 NM NR3 FORE FLAP DISBONDED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURNG 1/4 D-CHECK INSPECTION ON A/C AT AIR ASIA, DISBONDED WAS FOUND ON RT WING INBOARD T/E FORE FLAP LOWER SKIN E XISTING REPAIR DOUBLER AT WBL 236. THE DAMAGED EXISTING REPAIR DUOBLER WAS REMOVED AND REPAIRED PER B727 SRM 51-40-6. R EF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 810264 (SEQ NR 06064). (M) 2 L 7 3 4F A3WE 1997012300399 19970123 00399 NM 1997 1 23 MZZA96204 1 19961222 A 5320 SHEAR TIE BOEING 727 727224 1384076 NM BS 1166 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69741 22250 TNN - DURING S-CHECK INSPECTION ON A/C AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMEN BS 1166 FRAME SHE AR TIE BETWEEN STRINGER 28L AND STRINGER 29L. THE CORRODED SHEAR TIE WAS REMOVED AND REPLACED WITH NEW SHEAR TIE PER B7 27 SRM 53-10-4. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 810591 (SEQ NR 01074). (M) 2 L 7 3 4F A3WE 1997012300400 19970123 00400 NM 1997 1 23 MZZA96205 1 19961222 A 5320 SHEAR TIE BOEING 727 727224 1384076 NM BS 1166 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69741 22250 TNN - DURING S-CHECK INSPECTION ON A/C AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT BS 1166 FRAME SH EAR TIE BETWEEN STRINGER 29L AND STRINGER 30. THE CORRODED SHEAR TIE WAS REMOVED AND REPLACED WITH NEW SHEAR TIE PER B 727 SRM 53-10-4. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 810592 (SEQ NR 01075) (M) 2 L 7 3 4F A3WE 1997012300401 19970123 00401 NM 1997 1 23 MZZA96206 1 19961222 A 5320 SHEAR TIE BOEING 727 727224 1384076 NM BS 1166 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69741 22250 TNN - DURING S-CHECK INSPECTION ON A/C AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT BS 1166 FRAME SH EAR TIE AT RT SIDE OF STRINGER 29R. THE CORRODED SHEAR TIE FROM STRINGER 28R AND STRINGER 29R WAS REMOVED AND REPLACED WITH NEW SHEAR TIE PER B727 SRM 53-10-4. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 810593 9SEQ NR 01076). (M) 2 L 7 3 4F A3WE 1997012300402 19970123 00402 NM 1997 1 23 MZZA96207 1 19961222 A 5312 69162692 BULKHEAD WEB BOEING 727 727224 1384076 NM BS 950 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69741 22250 TNN - DURING S-CHECK INSPECTION ON A/C AT AIR ASIA, 4.5 INCH LONG CRACK WAS FOUND ON BS 950 PLUS 5.13 PRESSURE BULKHEAD WEB TO RT BULKHEAD FITTING SPLICE ANGLE (69-16269-2) AT WL 174.80. THE DAMAGED SPLICE ANGLE, P/N 69-16269-2 WAS REMOVED AND REPLACED PER B727 SRM 51-30-2. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 810600 (SEQ NR 01033)(M) 2 L 7 3 4F A3WE 1997012300403 19970123 00403 NM 1997 1 23 MZZA96208 1 19961222 A 5313 STRINGER BOEING 727 727224 1384076 NM BS 720 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69741 22250 TNN - DURING S-CHECK INSPECTION ON A/C AT AIR ASIA, SEVERE CORROSION WAS FOUND ON FORWARD CARGO COMPARTMENT, STRINGER 27 R BETWEEN BS 720F PLUS 15 AND BS 740. THE CORRODED STRINGER FROM BS 720F PLUS 12 TO BS 740 WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-10-3 FIGURE 1. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 839915 (SEQ NR 01100). (M) 2 L 7 3 4F A3WE 1997012300404 19970123 00404 NM 1997 1 23 MZZA96209 1 19961222 A 5320 ANGLE BOEING 727 727224 1384076 NM BS 740 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69741 22250 TNN - DURING S-CHECK INSPECTION ON A/C AT AIR ASIA, INTERGRANNULAR CORROSION WAS FOUND ON FORWARD CARGO COMPARTMENT STRI NGER 27R END TIE ANGLE AT BS 740. THE DAMAGED TIE ANGLE WAS REMOVED AND REPLACED WITH NEW TIE ANGLE PER B727 SRM 51-30- 2. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 839916 9SEQ NR 01101). (M) 2 L 7 3 4F A3WE 1997012300405 19970123 00405 EU 1997 1 23 RAIA961248 1 19961220 A 5311 S5367240600860 FRAME AEROSP ATR42 ATR42300 8680920 EU AFT FUS CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON WEB OF FRAME 37. MAINTENANCE REPAIRED AND REPLACED FRAME 37 IAW ATR 42 SRM 53. (M) 2 H 7 2 4T RT A53EU 1997012300406 19970123 00406 EU 1997 1 23 RAIA961247 1 19961220 A 5311 S5367131828001 FRAME AEROSP ATR42 ATR42300 8680920 EU AFT FUS CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON WEB OF FRAME 36. MAINTENANCE REPLACED LOWER FRAME 36 IAW ATR 42 SRM 53-00-00. (M) 2 H 7 2 4T RT A53EU 1997012300407 19970123 00407 SW 1997 1 23 MALA965236 1 19961207 A 5753 SKIN SWRNGN SA227 SA227AC 8780603 SW RT FLAP CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 159MC AC728B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND A CRACK IN RT FLAP SKIN S/N RPL 1688. CRACK IS APPROXIMATELY 1 INCH IN LENGTH. COMPLETED REPAIR TO FLAP IAW FAIRCHILD SRM 57-90-60 PAGES 19-21. (M) 2 L 7 2 4T RT A8SW 1997012300408 19970123 00408 SW 1997 1 23 MALA965235 1 19961207 A 5753 2736015002 RIB SWRNGN SA227 SA227AC 8780603 SW RT TE FLAP CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 159MC AC728B MALA - DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND A CRACK IN RT FLAP, S/N RPL1688, OUTBOARD FLAP NOSE RIB. REMOVED AND REPLACED FLAP NOSE RIB, P/N 27-36015-002 IAW FAIRCHILD SRM 57-90-60 PAGES 43-46. (M) 2 L 7 2 4T RT A8SW 1997012300409 19970123 00409 NM 1997 1 23 MALA965234 1 19961209 A 5411 FRAME DHAV DHC8 DHC8102 2809003 NM NS 176 CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 816MA 231 DURING A SCHEDULED INSPECTION IN CWA, MAINTENANCE FOUND LT FORWARD MAIN LANDING GEAR DOOR AFT HINGE ARM BOLT CHAFING ON NACELLE FRAME AT NS 176. CHAF IS WORN THROUGH THE FRAME AT OUTBOARD EDGE F FRAME. (M) 2 H 7 2 4T RT A13NM 1997012300410 19970123 00410 1997 1 23 MALA965238 4 19961210 A 3414 2114011342 AIRSPEED IND DHAV DHC8 DHC8102 2809003 NM RT COCKPIT FAILED A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 819MA 251 FLT 3189 - AFTER DEPARTING DTW, THE FIRST OFFICERES AIRSPEED, ALTIMETER, AND IVSI WERE GIVING ERRONEOUS INDICATIONS. TH E AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE AIRSPEED INDICATOR. ALL CHECKS GOOD. (M) 2 H 7 2 4T RT A13NM 1997012300411 19970123 00411 SW 1997 1 23 MALA965246 1 19961217 A 3230 RETRACT MECH SWRNGN SA227 SA227AC 8780603 SW LANDING GEAR LACK OF LUBE A MALA O OTHER J WARNING INDICATION CL CLIMB 1 GL 15 426MA AC645 FLT 3492 - ON CLIMB-OUT FROM STC, THE LANDING GEAR DIDN'T REMAIN UP AND LOCKED AFTER GEAR RETRACTION. THE CREW CYCLED T HE GEAR AND THE GEAR REMAINED UP AND LOCKED. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. MAINTENANCE LUBED TH E GEARS AND CHANGED THE MAIN HYDRAULIC FILTER AS A PRECAUTION. (M) 2 L 7 2 4T RT A8SW 1997012300412 19970123 00412 NM 1997 1 23 MALA965247 1 19961217 A 3231 AR2674 LATCH DHAV DHC8 DHC8102 2809003 NM NLG DOOR BROKEN A MALA K NONE O OTHER CL CLIMB 1 GL 15 831MA 339 FLT NR 3478 - ON CLIMB-OUT FROM MSP, THE MAIN GEAR DIDN'T UP AND LOCK AFTER GEAR RETRACTION AND THE NOSE GEAR YELLOW AMB ER LIGHT REMAINED ILLUMINATED. MAINTENANCE REPLACED A BROKEN LATCH ON THE NOSE GEAR DOOR, P/N AR 2674. ALL CHECKS SATI SFACTORY. (M) 2 H 7 2 4T RT A13NM 1997012300413 19970123 00413 NM 1997 1 23 USAA960805 1 19961224 A 5330 SKIN BOEING 737 737201 1384454 NM BS 760 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 232US 44487 22018 ROA - DURING CX-3 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 2.1250 INCH CRACK STRINGER 17 L, BS 760 FUSELAGE SKIN. RE MOVED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 1. (M) 2 L 7 2 4F A16WE 1997012300414 19970123 00414 NM 1997 1 23 USAA960804 1 19961224 A 5330 SKIN BOEING 737 737201 1384454 NM BS 740 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 232US 44487 22018 ROA - DURING CX-3 CHECK VISUAL/EDDY CURRENT, INSPECTION FOUND .75 INCH CRACK AT FUSELAGE SKIN STRINGER 17L, BS 740. REM OVED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 1. (M) 2 L 7 2 4F A16WE 1997012300415 19970123 00415 NM 1997 1 23 USAA960803 1 19961224 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 1000-1016 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 232US 44487 22018 ROA - DURING CX-3 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 10 INCH CORROSION STRINGER 27L, BS 1000 TO 1016. SPLICED IN STRINGER, REPAIRED PER CD 25G00984A, SRM 53-10-3 FIG 1. (M) 2 L 7 2 4F A16WE 1997012300416 19970123 00416 NM 1997 1 23 USAA960802 1 19961224 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 232US 44487 22018 ROA - DURING CX-3 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 3 INCH CRACK STRINGER 16 BS 727A PLUS 8 L FUSELAGE SKIN. I NSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1997012300417 19970123 00417 NM 1997 1 23 USAA960801 1 19961224 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 232US 44487 22018 ROA - DURING CX-3 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 1.75 INCH CRACK STRINGER 18A, SHEAR BEAM BS 727 LEFT. INS TALLED REPAIR KIT 65C29228-3, REPAIRED PER EO 5393G256/EA 59193. (M) 2 L 7 2 4F A16WE 1997012300418 19970123 00418 NM 1997 1 23 USAA960800 1 19961224 A 5330 SKIN BOEING 737 737201 1384454 NM PAX DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 232US 44487 22018 ROA - DURING CX-3 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND .3125 INCH CRACK FORWARD ENTRY DOOR CUT OUT FORWARD UPPER HINGE CUT OUT FUSELAGE SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 1 AND TR 53-30-11. (M) 2 L 7 2 4F A16WE 1997012300419 19970123 00419 NM 1997 1 23 USAA960799 1 19961224 A 5330 SKIN BOEING 737 737201 1384454 NM BS 328 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 232US 44487 22018 ROA - DURING CX-3 CHECK VISUAL/EDDY CURRENT, FOUND 2.5 INCH CRACK FORWARD GALLEY DOOR CUT OUT AFT LOWER CORNER (STRINGER 17 R BS 328) FUSELAGE SKIN, TEAR STRAP AND BEAR STRAP. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1997012300420 19970123 00420 NM 1997 1 23 USAA960798 1 19961221 A 5330 SKIN BOEING 737 737201 1384454 NM BS 440 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 248US 38686 22755 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO CRACKS .175 INCH LONG BS 440, BETWEEN STRINGER 23R AND STRINGER 24R SKIN. TRIMMED OUT DAMAGE, INSTALLED FILLERS AND REPAIRED DOUBLER, REPAIRED PER EA NR 41810. (M) 2 L 7 2 4F A16WE 1997012300421 19970123 00421 NM 1997 1 23 USAA960797 1 19961221 A 5330 SKIN BOEING 737 737201 1384454 NM SERV DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 248US 38686 22755 INT - DURIGN Q-6 CHECK EDDY CURRENT INSPECTION, FOUND 1.75 INCH CRACK LOWER AFT CORNER RT FORWARD SERVICE DOOR CUTOUT SK IN. INSTALLED TRIPLER REPAIR PLUS 3.7 LB WEIGHT CHANGE. REPAIRED PER SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1997012300422 19970123 00422 NM 1997 1 23 USAA960796 1 19961221 A 5311 737201 FRAME BOEING 737 737201 1384454 NM BS 296 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 248US 38686 22755 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 296, RBL 55 WL 208 FRAME. STOP DRILLED AND INSTALLED DO UBLER, REPAIRED PER SRM 51-40-3 FIG 1. (M) 2 L 7 2 4F A16WE 1997012300423 19970123 00423 NM 1997 1 23 USAA960795 1 19961221 A 5330 SKIN BOEING 737 737201 1384454 NM SERVICE DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 248US 38686 22755 INT - DURING Q-6 CHECK EDDY CURRENT INSPECTION, FOUND .125 INCH CRACK AFT SERVICE DOOR CUTOUT AT UPPER HINGE CUTOUT FORW ARD END SKIN. INSTALLED EXT SKIN DOUBLER, REPAIRED PER SRM 53-30-3 FIG 21A. (M) 2 L 7 2 4F A16WE 1997012300424 19970123 00424 NM 1997 1 23 USAA960794 1 19961221 A 5314 KEEL BEAM BOEING 737 737201 1384454 NM BS 670-767 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 248US 38686 22755 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION .25 INCH DIAMETER SEVERAL AREAS BS 670 TO 727 LEFT SIDE KEEL B EAM W/W LEFT OUTBOARD FLANGE. INSTALLED REPAIR STRAP AND CHAFING STRIP, REPAIRED PER EA 41879. CORROSION TASK NR C53-2 12-01, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1997012300425 19970123 00425 NM 1997 1 23 USAA960793 1 19961221 A 5312 BULKHEAD BOEING 737 737201 1384454 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 248US 38686 22755 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK BS 178 BULKHEAD LBL 5.7 WL 184 BEAM CHORD. STOP DRILLED AN D INSTALLED REPAIR ANGLE, REPAIRED PER TR 53-10-17. (M) 2 L 7 2 4F A16WE 1997012300426 19970123 00426 NM 1997 1 23 USAA960788 1 19961218 A 5315 FLOOR BEAM BOEING 737 7373B7 1384580 NM BS 312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 521AU 30780 23856 CLT - INSPECTION VISUALLY FOUND LEVEL 2 CORROSION 3 EACH MEASURING 1 INCH BY 1 INCH AREAS LOCATED AT STATION 312 BL 0, L BL 26, LBL 37 FLOORBEAM. INSTALLED NEW 'T' REPAIR ANGLES AND STRAPS AS PER USAIR TYPICAL REPAIR MANUAL 53-10-03. (M) 2 L 7 2 4F RT A16WE 1997012300427 19970123 00427 NM 1997 1 23 USAABB96062 1 19961218 A 3260 849704 PSEU BOEING 767 7672B7 1385107 NM E/E COMPT FAULTY A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 652US 593 24765 FRA - FLT 893 - CREW RECEIVED AN AIR/GROUND DISAGREE INDICATION SHORTLY AFTER TAKEOFF. FLIGHT RETURNED TO FRA AND LANDE D WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE PROXIMITY SWITCH ELECTRONIC UNIT. (M) 2 L 7 2 4F RT A1NM 1997012300428 19970123 00428 NM 1997 1 23 USAASB96269 1 19961225 A 5730 9001105 FUEL DOOR BOEING 737 737401 1384701 NM RT WING LEAKING A A USAA A UNSCHED LANDING K W FLUID LOSS INADEQUATE Q C CR CRUISE 1 EA 19 422US 23989 CLT - FL 1034 - CAPTAIN REPORTED FUEL LEAK AND HAD LOST APPROXIMATELY 450 POUNDS OF FUEL. FUEL WAS VISIBLE LEAKING OUT OF THE TOP OF RIGHT WING. FLIGHT DIVERTED INTO CLT AS A PRECAUTIONARY MEASURE. NO EMERGENCY WAS DECLARED AND THE FLIGH T LANDED WITHOUT INCIDENT. MAINTENANCE FOUND AN UPPER WING ACCESS PANEL, BEHIND THE STRUT, ON THE RIGHT WING LEAKING FU EL. REPLACED THREE DEFECTIVE DOME NUTS, ACCESS PANEL AND HARDWARE. FILLED RIGHT WING TANK TO FULL. NO LEAKS NOTED. ( M) 2 L 7 2 4F RT A16WE 1997012300429 19970123 00429 SW 1997 1 23 MALA965249 1 19961219 A 5712 2731080 RIB SWRNGN SA227 SA227AC 8780603 SW WS 27 CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 421MA AC634 DURING A SCHEDULED INSPECTION IN MSP, THE LEFT WS 27 AFT FLAP WELL RIB P/N 27-31080 WAS FOUND CHAFFED BY THE FLAP SWING LINK. BLENDED OUT CHAF DAMAGE AND INSTALLED A REPAIR DOUBLER AS PER EA 01-96132, AND LAR 92-MALA-107. (M) 2 L 7 2 4T RT A8SW 1997012300430 19970123 00430 SW 1997 1 23 MALA965252 1 19961220 A 3230 246006 VALVE SWRNGN SA227 SA227AC 8780603 SW LANDING GEAR FAILED A MALA O OTHER N FALSE WARNING CL CLIMB 1 GL 15 426MA AC645 FLIGHT 3330 - ON CLIMB-OUT FROM LSE, ALL THREE RED INTRANSIT LIGHTS REMAINED ILLUMINATED AFTER GEAR RETRACTION. AFTER A N EXTENDED PERIOD OF TIME, ALL GEARS SHOWED GREEN UP AND LOCKED. MAINTENANCE REPLACED THE LANDING GEAR VALVE, P/N 24600 -6. ALL CHECKS SATISFACTORY. (M) 2 L 7 2 4T RT A8SW 1997012300431 19970123 00431 NM 1997 1 23 MALA965254 1 19961219 A 3260 841005 PSEU DHAV DHC8 DHC8102 2809003 NM NLG FAILED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 824MA 327 FLT 3319 - ON CLIMB-OUT FROM DTW, THE NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE AIRCRAFT RET URNED TO DTW. MAINTENANCE REPLACED THE PSEU. ALL CHECKS SATISFACTORY. (M) 2 H 7 2 4T RT A13NM 1997012300432 19970123 00432 SW 1997 1 23 MALA965255 1 19961221 A 5230 DOOR MECH SWRNGN SA227 SA227AC 8780603 SW CARGO COMPT OUT OF ADJUST A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 60NE AC760B FLT 3016 - ON CLIMB-OUT FROM DTW, THE CARGO DOOR WARNING LIGHTS ILLUMINATED. THE AIRCRAFT RETURNED TO DTW. THE LIGHT E XTINGUISHED ON TOUCHDOWN. MAINTENANCE ADJUSTED THE CARGO DOOR CLICK-CLACKS. ALL CHECKS SATISFACTORY. (M) 2 L 7 2 4T RT A8SW 1997012300433 19970123 00433 NE 1997 1 23 MALA965256 2 19961222 A 7200 ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 SURGE A A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 852MA 349 FLT 3250 - ON CLIMB-OUT FROM GFK, THE NR 1 ENGINE EXPERIENCED A POWER SURGE. THE AIRCRAFT RETURNED TO GFK. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY THROUGH DIAGNOSTIC AND OPERATIONAL CHECKS. AS PART OF THE INSPECTION, MAINTENA NCE CLEANED TWO CANNON PLUGS INCLUDED IN THE WIRING HARNESS. (M) 2 H 7 2 4T 4 T RT A13NM E20NE 1997012300434 19970123 00434 SW 1997 1 23 MALA965257 1 19961222 A 3260 1EN516 POSITION SWITCH SWRNGN SA227 SA227AC 8780603 SW RT MLG FAILED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 426MA AC645 FLT 3038 - ON CLIMB-OUT FROM MSP, THE RIGHT GEAR INTRANSIT LIGHT WAS SLOW TO EXTINGUISH AFTER GEAR RETRACTION. THE AIRC RAFT RETURNED TO MSP. MAINTENANCE REPLACED THE RIGHT OUTBOARD GEAR POSITION SWITCH. ALL CHECKS SATISFACTORY. (M) 2 L 7 2 4T RT A8SW 1997012300435 19970123 00435 SW 1997 1 23 MALA965250 1 19961219 A 5712 2731023 RIB SWRNGN SA227 SA227AC 8780603 SW WS 81 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 433MA AC714 DURING AN INSPECTION IN MSP, MAINTENANCE FOUND A 3.5 INCH CRACK IN THE RADIUS OF THE RT WING RIB LOWER ATTACH FLANGE P/N 27-31023. APPROXIMATE LOCATION IS WS 81 AND BETWEEN NS 130 AND 141. STOP DRILLED CRACK, FABRICATED AND INSTALLED A 6. 5 INCH BY 3 INCH BY 1 INCH BY .05 INCH 2024-T3 REPAIR DOUBLER AND APPLICABLE FILLER PLATES WHERE NEEDED. ALL WORK COMPL ETED IAW AEROTECH DESIGNS EA 01-96125. (M) 2 L 7 2 4T RT A8SW 1997012300436 19970123 00436 SW 1997 1 23 MALA965245 1 19961218 A 5712 2731023 RIB SWRNGN SA227 SA227AC 8780603 SW WS 81 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 434MA AC717 DURING AN INSPECTION IN MSP, MAINTENANCE FOUND TWO CRACKS 1INCH BY 1 INCH IN THE RADIUS OF THE LT WING RIB LOWER ATTACH FLANGE (P/N 27-31023). APPROXIMATE LOCATION IS WS 81 AND BETWEEN NS 130 AND 141. STOP DRILLED CRACK, FABRICATED AND IN STALLED A 6.5 INCH, 3 INCH BY 1 INCH BY .050 INCH 2024-T3 REPAIR DOUBLER AND APPLICABLE FILLER PLATES WHERE NEEDED. ALL WORK COMPLETED IAW AEROTECH DESIGNS EA01-96125. (M) 2 L 7 2 4T RT A8SW 1997012300437 19970123 00437 SW 1997 1 23 MALA965244 1 19961218 A 5712 2731023 RIB SWRNGN SA227 SA227AC 8780603 SW WS 81 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 434MA AC717 DURING AN INSPECTION IN MSP, MAINTENANCE FOUND TWO CRACKS 2 INCH BY 1 INCH IN THE RADIUS OF THE RIGHT WING RIB LOWR ATTA CH FLANGE (P/N 27-31023). APPROXIMATE LOCATION IS WS 81 BETWEEN NS 130 AND 141. STOP DRILLED CRACK, FABRICATED AND INS TALLED A 6.5 INCH, 3 INCH BY 1 INCH BY .050 INCH 2024-T3 REPAIR DOUBLER AND APPLICABLE FILLER PLATES WHERE NEEDED. ALL WORK COMPLETED IAW AERO TECH DESIGNS EA01-96125. (M) 2 L 7 2 4T RT A8SW 1997012300438 19970123 00438 SW 1997 1 23 MALA965240 1 19961218 A 5712 2731023 RIB SWRNGN SA227 SA227AC 8780603 SW WS 81 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 430MA AC710 DURING AN INSPECTION IN MSP, MAINTENANCE FOUND TWO CRACKS 1 INCH BY 1 INCH IN THE RADIUS OF THE LT WING RIB LOWER ATTACH FLANGE (P/N 27-31023). APPROXIMATE LOCATION IS WS 81 AND BETWEEN NS 130 AND 141. STOP DRILLED CRACK, FABRICATED AND I NSTALLED AN APPROPRIATE SIZED 3 INCH BY 1 INCH BY .050 INCH 2024-T3 REPAIR DOUBLER AND APPLICABLE FILLER PLATES WHERE NE EDED. ALL WORK DONE IAW AEROTECH DESIGNS EA01-96125. (M) 2 L 7 2 4T RT A8SW 1997012300439 19970123 00439 SW 1997 1 23 MALA965239 1 19961218 A 5712 2731023 RIB SWRNGN SA227 SA227AC 8780603 SW WS 81 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 434MA AC717 DURING AN INSPECTION IN MSP, MAINTENANCE FOUND A 5 INCH CRACK IN THE RADIUS OF THE WING RIB LOWER ATTACH FLANGE (P/N 27- 31023). APPROXIMATE LOCATION IS WS 81 AND BETWEEN NS 130 AND 141. STOP DRILLED CRACK, FABRICATED AND INSTALLED A 8.25 INCH BY 3 INCH BY 1 INCH BY .050 REPAIR DOUBLER AND APPLICABLE FILLER PLATES WHERE NEEDED. ALL WORK IAW AERO TECH DESIG NS EA01-96125. (M) 2 L 7 2 4T RT A8SW 1997012300440 19970123 00440 SW 1997 1 23 MALA965243 1 19961218 A 5712 2731023 RIB SWRNGN SA227 SA227AC 8780603 SW WS 81 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 433MA AC714 DURING AN INSPECTION IN MSP, MAINTENANCE FOUND A 'X.0' CRACK IN THE RADIUS OF THE LT WING RIB LOWER ATTACH FLANGE (P/N 2 7-31023). APPROXIMATE LOCATION IS WS 81 AND BETWEEN NS 130 AND 141. STOP DRILLED CRACK, FABRICATED ADN INSTALLED A 'X. 00' BY 3 INCH BY 1 INCH BY .050 2024-T3 REPAIR DOUBLER AND APPLICABLE FILLER PLATES WHERE NEEDED. ALL WORK COMPLETED IA W AEROTECH DESIGNS EA01-96125. (M) 2 L 7 2 4T RT A8SW 1997012300441 19970123 00441 SW 1997 1 23 MALA965242 1 19961218 A 5712 2731023 RIB SWRNGN SA227 SA227AC 8780603 SW WS 81 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 433MA AC714 DURING AN INSPECTION IN MSP, MAINTENANCE FOUND A 'X.0' CRACK IN THE RADIUS OF THE RT WING RIB LOWER ATTACH FLANGE (P/N 2 7-31023). APPROXIMATE LOCATIONIS WS 81 AND BETWEEN NS 130 AND 141. STOP DRILLED CRACK, FABRICATED AND INSTALLED A 'X.0 BY 3 INCH BY 1 INCH BY .050 2024-T3 REPAIR DOUBLER APPLICABLE FILLER PLATES WHERE NEEDED. ALL WORK COMPLETED IAW AEROT ECH DESIGNS EA01-96125. (M) 2 L 7 2 4T RT A8SW 1997012300442 19970123 00442 NE 1997 1 23 97ZZZM83 2 19961013 A 7230 804061 BEARING DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7A 52053 NE NR 2 ENG NR 3 FAILED A TWAA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 984Z 47412 IAD - DURING CLIMB NR 2 ENGINE, S/N 2153, OIL FILTER BYPASS LIGHT ILLUMINATED. REDUCED POWER TO IDLE. FOUND METAL PART ICLES IN OIL FILTER. REPLACED NR 2 ENGINE. ENGINE OPERATION THEN CHECKED NORMAL. INVESTIGATION OF NR 2 ENGINE REVEALE D NR 3 BEARING, MFG P/N 804061, FRACTURED LIBERATING PARTICLES INTO OIL SYSTEM. NR 3 BEARING REPLACED AND ENGINE REPAIR ED. ENGINE RETURNED TO SERVICE. (M) 2 L 7 2 4F 4 F A6WE E2EA 1997012300443 19970123 00443 NE 1997 1 23 97ZZZM84 2 19960722 A 7230 COMPRESSOR BOEING 767 767231 1385131 NM PWA JT9 JT9D7R4D 52054 NE NR 2 ENGINE DAMAGED A A TWAA O OTHER R PARTIAL RPM/PWR LOSS CL CLIMB 1 CE 05 609TW 22572 JFK - DURING CLIMB NR 2 ENGINE, S/N 4619, EXPERIENCED A POWER SURGE. ENGINE PARAMETERS REMAINED WITHIN LIMITS. FOUND 9 TH STAGE COMPRESSOR BLADE DAMAGE. REPLACED ENGINE AND THEN ENGINE OPERATION CHECKED NORMAL. INVESTIGATION REVEALED THE HIGH PRESSURE COMPRESSOR HAD SEVERE RUB OF THE INNER AIRSEALS AND TO THE OUTER RUBSTRIPS AND BLADE TIPS. THE HIGH PRES SURE COMPRESSOR MODULE WAS REPLACED AND ENGINE S/N 4619 WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F 4 F RT A1NM E3NE 1997012300446 19970123 00446 NM 1997 1 23 USAASB96265 1 19961221 A 2170 1830104 WATER SEPARATOR BOEING 737 7373B7 1384580 NM RT PACK COLLAPSED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 528AU 24410 CLT - FL 645 - ON CLIMB-OUT FROM CLT, CREW WAS UNABLE TO PRESSURIZE A/C. AFTER PERFORMING CHECKLIST AND CLIMBING TO 7,0 00 FT, CREW ELECTED TO RETURN TO FIELD AT CLT. NO EMERGENCY WAS DECLARED AND THE FIGHT LANDED W/O FURTHER INCIDENT. MX FOUND THE RT PACK WATER SEPARATOR ASSY COLLAPSED AND THE GROUND AIR CHECK VLV LEAKING. REPLACED WATER SEPARATOR ASSY ( P/N 183010-4) AND REMOVED DEBRIS FROM MIX MANIFOLD AND CHECK VLV. FOUND HOLE IN RT PACK TURBO FAN DUCT AND LT RECIRULAT ION FAN FODDED. REPLACED DUCT (P/N 69-49792-5) AND FAN (P/N 645405-1). ALSO, FOUND RT 35 DEGREE CONTROL VLV STICKING A ND 35 DEGREE CONTROL BOX DEFECTIVE. REPLACED VLV (P/N 321942-1) AND CONTROL BOX (P/N 607510-3). ACCOMP PRESS SYS OP CH 2 L 7 2 4F RT A16WE 1997012300447 19970123 00447 NM 1997 1 23 USAASB96267 1 19961224 A 3230 MFGSPEC0023270 UPLOCK ACTUATOR BOEING 737 7373B7 1384580 NM LT MLG FAILED A USAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 19 532AU 23683 24479 PIT - FL 185 - AFTER DEPARTURE FROM LGA, LEFT GEAR RED LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. RECYCLED GEAR SEVERAL TIMES. LIGHT WENT OUT WHEN GEAR HANDLE WAS PLACED IN DOWN POSITION AND ILLUMINATED WHEN GEAR HANDLE WAS PLACED TO THE UP OR OFF POSITION. ALL LIGHTS OPERATED NORMALLY WHEN GEAR WAS PLACED DOWN FOR LANDING. NO EMERGENCY WAS DECLAR ED AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT INBOARD MAIN LANDING GEAR UPLOCK ACTUATOR PER MM 32-32-41. GEAR RETRACTION AND EXTENSION CHECKS GOOD. (M) 2 L 7 2 4F RT A16WE 1997012300448 19970123 00448 NM 1997 1 23 USAASB96270 1 19961116 A 3350 AD20131A BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 432US 24554 SYR - MAINTENANCE FOUND THE FORWARD ENTRYWAY EVACUATION LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE FORWARD ENTRYWAY CEILING. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1997012300449 19970123 00449 NM 1997 1 23 USAASB96266 1 19961224 A 3350 20121 POWER SUPPLY BOEING 737 737401 1384701 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 417US 23984 CLE - MAINTENANCE FOUND THE RIGHT AFT SERVICE DOOR EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE POWER SUP PLY IN THE AFT OVERHEAD CABIN. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1997012300450 19970123 00450 NM 1997 1 23 USAASB96268 1 19961225 A 3350 BATTERY PACK BOEING 737 737201 1384454 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 232US 22018 CLE - MAINTENANCE FOUND THE FORWARD SERVICE DOOR AND THE MAIN ENTRANCE DOOR INTERIOR AND EXTERIOR EXIT LIGHTS INOP. ALS O, THE MAIN ENTRANCE DOOR UPPER EMERGENCY LIGHT WAS FOUND TO BE VERY DIM. MAINTENANCE REMOVED AND REPLACED THE MAIN ENT RANCE DOOR UPPER EMERGENCY LIGHT BATTERY PACK (P/N S106) AND THE FORWARD SERVICE DOOR AND MAIN ENTRANCE DOOR INTERIOR AN D EXTERIOR EXIT LIGHT BATTERY PACK (P/N 61-0478-9). OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1997012300451 19970123 00451 NM 1997 1 23 USAASB96271 1 19961210 A 3350 6104789 BATTERY PACK BOEING 737 7372B7 1384560 NM CARGO COMPT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 278AU 22890 CLT - MAINTENANCE FOUND THE EMERGENCY ESCAPE SLIDE LIGHTS FOR THE FORWARD ENTRY DOOR AND FORWARD SERVICE DOOR BLINKING O N AND OFF. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE FORWARD CARGO COMPARTMENT FOR THE FORWARD DOOR ESCA PE SLIDE LIGHTS. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1997012300452 19970123 00452 EU 1997 1 23 USAASB96264 2 19961220 A 7320 3205004030 PMC HARNESS BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU NR 1 ENGINE MALFUNCTIONED A USAA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 EA 19 428US 24550 CLT - FLT 276 - CLIMBING THROUGH 12,000 FEET, THE NR 1 ENGINE SURGED, PLUS OR MINUS 7 TO 8 PERCENT N1. CAPTAIN PULLED B ACK NR 1 ENGINE TO IDLE, DECLARED AND EMERGENCY AND RETURNED TO FIELD AT CLT. ALL INDICATIONS FOLLOWED N1 AND THE ENGIN E SURGED WITH AND WITHOUT AUTO-THROTTLE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE PMC BLUE HARNESS ASSEMBLY AND LEAD. OPS CHECKED PMC AT PART POWER PER MM 71-00-01. OPS CHECK GOOD. (M) 2 L 7 2 4F 4 F RT A16WE E21EU 1997012300453 19970123 00453 SW 1997 1 23 MALA965233 1 19961209 A 5720 2735112 ANGLE SWRNGN SA227 SA227AC 8780603 SW RT WING/NAC WORN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 63NE AC763B DURING A BLOCK INSPECTION IN MSP, MAINTENANCE FOUND THE RT INBOARD UPPER WING SKIN TO NACELLE ATTACH ANGLE REPAIR DOUBLE R WORN. REMOVED EXISTING REPAIR AND FOUND ANGLE P/N 27-35112 WORN ALSO. REMOVED AND REPLACED ANGLE WITH NEWLY FABRICAT ED FROM SAME MATERIAL AND INSTALLED A 6 INCH REPAIR DOUBLER OVER AREA OF NACELLE SKIN, IAW FAIRCHILD SRM 51-00-00 PAGE 4 PART FOR PART REPLACEMENT AND FAC SRM 51-90-02, 51-40-02 REV JUNE 93. (M) 2 L 7 2 4T RT A8SW 1997012300454 19970123 00454 EU 1997 1 23 RAIA961232 1 19961220 A 5320 S5367800821602 ANGLE AEROSP ATR42 ATR42300 8680920 EU AFT FUS CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON FRAME 38 FAIL/SAFE ANGLE FROM STRINGER 20L TO 20R. MAINTENANCE REMOVED CORROSION IAW ATR 42 SR M 51-21-42. (M) 2 H 7 2 4T RT A53EU 1997012300455 19970123 00455 EU 1997 1 23 RAIA961231 1 19961220 A 5320 S536780082102 ANGLE AEROSP ATR42 ATR42300 8680920 EU AFT FUS CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION UNDER FRAME 36 FAIL/SAFE ANGLE FROM STRINGER 21L TO 21R. MAINTENANCE REMOVED CORROSION IAW ATR 42 SRM 51-21-42. (M) 2 H 7 2 4T RT A53EU 1997012300456 19970123 00456 EU 1997 1 23 RAIA961230 1 19961220 A 5320 S5367800821602 ANGLE AEROSP ATR42 ATR42300 8680920 EU AFT FUS CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON FRAME 28 FAIL/SAFE ANGLE FROM STRINGER 21L TO 21R. MAINTENANCE REMOVED CORROSION IAW ATR 42 SR M 51-21-42. (M) 2 H 7 2 4T RT A53EU 1997012300457 19970123 00457 EU 1997 1 23 RAIA961229 1 19961220 A 5320 S53672408228 CLIPS AEROSP ATR42 ATR42300 8680920 EU AFT FUS CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON FRAME 40 SKIN CLIPS FROM STRINGER 18L TO 21L. MAINTENANCE REMOVED CORROSION IAW ATR 42 SRM 51- 21-42. (M) 2 H 7 2 4T RT A53EU 1997012300458 19970123 00458 EU 1997 1 23 RAIA961228 1 19961220 A 5315 S53672400000 FLOOR BEAM AEROSP ATR42 ATR42300 8680920 EU AFT FUS CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON FRAME 39 SKIN CLIPS FROM STRINGER 16L TO 15R. MAINTENANCE REPLACED FRAME 39 IAW ATR 42 SRM 53- 00-00. (M) 2 H 7 2 4T RT A53EU 1997012300460 19970123 00460 EU 1997 1 23 RAIA961226 1 19961220 A 5320 S53672408228 CLIPS AEROSP ATR42 ATR42300 8680920 EU AFT FUS CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON FRAME 35 SKIN CLIPS FROM STRINGER 20L TO 20R. MAINTENANCE REPAIRED FRAME IAW ATR 42 SRM 53-00- 00. (M) 2 H 7 2 4T RT A53EU 1997012300461 19970123 00461 EU 1997 1 23 RAIA961225 1 19961220 A 5320 S53672408228 CLIPS AEROSP ATR42 ATR42300 8680920 EU AFT FUS CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON FRAME 34 SKIN CLIPS FROM STRINGER 19L TO 19R. MAINTENANCE REPAIRED FRAME IAW ATR42 SRM 53-00-0 0. (M) 2 H 7 2 4T RT A53EU 1997012300462 19970123 00462 EU 1997 1 23 RAIA961224 1 19961220 A 5320 S53672408228 CLIPS AEROSP ATR42 ATR42300 8680920 EU AFT FUS CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - MAINTENANCE FOUND CORROSION ON FRAME 33 SKIN CLIPS FROM STRINGER 19L TO 20R. MAINTENANCE REMOVED CORROSION IAW AT R 42 SRM 51-21-42. (M) 2 H 7 2 4T RT A53EU 1997012300463 19970123 00463 EU 1997 1 23 RAIA961223 1 19961220 A 5320 S53672408228 CLIPS AEROSP ATR42 ATR42300 8680920 EU AFT FUS CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 124 STL - FOUND CORROSION ON FRAME 32 SKIN CLIPS FROM STRINGER 19L TO 21L. MAINTENANCE REMOVED CORROSION IAW ATR 42 SRM 51- 21-42. (M) 2 H 7 2 4T RT A53EU 1997012300464 19970123 00464 EU 1997 1 23 RAIA961222 1 19961220 A 5320 S53672408228 CLIPS AEROSP ATR42 ATR42300 8680920 EU AFT FUS CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 124 STL - MAINTENANCE FOUND CORROSION ON FRAME 32 SKIN CLIP FROM STRINGER 20R TO 21R. MAINTENANCE REMOVED CORROSION IAW ATR 42 SRM 51-21-42. (M) 2 H 7 2 4T RT A53EU 1997012300465 19970123 00465 EU 1997 1 23 RAIA961221 1 19961220 A 5320 S53672408228 CLIPS AEROSP ATR42 ATR42300 8680920 EU AFT FUS CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 124 STL - FOUND CORROSION ON FRAME 31 SKIN CLIPS FROM STRINGER 20R TO 21R. MAINTENANCE REMOVED CORROSION IAW ATR 42 SRM 51- 21-42. (M) 2 H 7 2 4T RT A53EU 1997012300466 19970123 00466 EU 1997 1 23 RAIA961220 1 19961220 A 5320 S53672408228 CLIPS AEROSP ATR42 ATR42300 8680920 EU AFT FUS CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON FRAME 30 SKIN CLIPS FROM STRINGER 21L TO 21R. MAINTENANCE REPAIRED FRAME IAW ATR 42 SRM 5300. (M) 2 H 7 2 4T RT A53EU 1997012300467 19970123 00467 EU 1997 1 23 RAIA961219 1 19961220 A 5320 S53672408228 CLIPS AEROSP ATR42 ATR42300 8680920 EU AFT FUS CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON FRAME 30 SKIN CLIPS FROM STRINGER 21L TO 21R. MAINTENANCE REPAIRED FRAME IAW ATR 42 SRM 5300. (M) 2 H 7 2 4T RT A53EU 1997012300468 19970123 00468 EU 1997 1 23 RAIA961218 1 19961220 A 5320 S53672408228 CLIPS AEROSP ATR42 ATR42300 8680920 EU AFT FUS CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON FRAME 29 SKIN CLIPS FROM STRINGER 20L TO 20R. MAINTENANCE REMOVED CORROSION IAW ATR 42 SRM 51- 21-42. (M) 2 H 7 2 4T RT A53EU 1997012300469 19970123 00469 EU 1997 1 23 RAIA961217 1 19961219 A 5320 S53672408228 CLIPS AEROSP ATR42 ATR42300 8680920 EU AFT FUS CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON FRAME 28 SKIN CLIPS FROM STRINGER 21L TO 21R. MAINTENANCE REMOVED CORROSION PER SRM 51-21-00. (M) 2 H 7 2 4T RT A53EU 1997012300470 19970123 00470 1997 1 23 RAIA961215 4 19961219 A 3414 39948B2236 AIRSPEED IND BAG JETSTM JETSTM3201 1500217 EU LT COCKPIT STUCK A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 337TE 9436 9436 929 ALO - FLT 7455 - CAPTAINS AIRSPEED INDICATOR STUCK AT ZERO. MAINTENANCE REPLACED THE CAPTAINS AIRSPEED INDICATOR. (M) 2 L 7 2 4T RT A56EU 1997012300471 19970123 00471 EU 1997 1 23 RAIA961212 1 19961219 A 3246 AH52688 WHEEL JETAIR JETSTM JETSTM4101 1500501 EU NOSE GEAR OUT OF BALANCE A RAIA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 CE 03 556HK 41073 JFK - FLT 7654 - NOSE GEAR VIBRATION DURING RETRACTION. MAINTENANCE REPLACED BOTH NOSE WHEEL ASSEMBLIES. (M) 2 L 7 2 4T RT A41NM 1997012300472 19970123 00472 1997 1 23 RAIA961213 3 19961219 A 6140 31056294 BETA SWITCH JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 03 558HK 2449 41071 STL - FLT 7506 - LEFT BETA CAPTION ILLUMINATED DURING TAKEOFF. MAINTENANCE REPLACED THE LEFT BETA SWITCH. (M) 2 L 7 2 4T RT A41NM 1997012300473 19970123 00473 1997 1 23 RAIA961211 4 19961218 A 3414 39948B2236 AIRSPEED IND BAG JETSTM JETSTM3201 1500217 EU LT COCKPIT STUCK A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 435AM 4587 889 STL - FLT 7466 - CAPTAINS AIRSPEED INDICATOR STUCK AT 50 KNOTS. MAINTENANCE REPLACED THE CAPTAINS AIRSPEED INDICATOR. ( M) 2 L 7 2 4T RT A56EU 1997012300474 19970123 00474 EU 1997 1 23 RAIA961210 1 19961218 A 2422 559012A INVERTER AEROSP ATR42 ATR42300 8680920 EU NR 1 FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 421TE 102 STL - FLT 7116 - NR 1 INVERTER FAULTED AND WOULD NOT RESET. MAINTENANCE REPLACED THE NR 1 INVERTER. (M) 2 H 7 2 4T RT A53EU 1997012300475 19970123 00475 EU 1997 1 23 RAIA961209 4 19961218 A 6122 8975481 PROP GOVERNOR BAG JETSTM JETSTM3201 1500217 EU RT ENGINE OUT OF ADJUST A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 343TE 10406 10406 955 STL - FLT 7344 - RIGHT ENGINE TAKEOFF RPM 99 PERCENT. MAINTENANCE ADJUSTED PROP GOVERNOR HIGH STOP. (M) 2 L 7 2 4T RT A56EU 1997012300476 19970123 00476 EU 1997 1 23 RAIA961208 1 19961213 A 3234 1379098D401 SELECTOR VALVE JETAIR JETSTM JETSTM4101 1500501 EU LANDING GEAR FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION LD LANDING 1 CE 03 558HK 2420 2420 41071 BMI - FLT 7545 - DURING GEAR EXTENSION, THE LANDING GEAR CONTROL CIRCUIT BREAKER POPPED, AND WOULD NOT RESET. MAINTENAN CE REPLACED THE LANDING GEAR SELECTOR VALVE. (M) 2 L 7 2 4T RT A41NM 1997012300477 19970123 00477 EU 1997 1 23 RAIA961207 4 19961217 A 6122 8975481 PROP GOVERNOR BAG JETSTM JETSTM3201 1500217 EU LT ENGINE OUT OF ADJUST A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 423AM 11075 11075 858 JLN - FLT 7060 - LEFT ENGINE RPM DROPPED TO ZERO DURING TAKEOFF. MAINTENANCE ADJUSTED PROP GOVERNOR HIGH STOP. (M) 2 L 7 2 4T RT A56EU 1997012300478 19970123 00478 EU 1997 1 23 RAIA961206 1 19961210 A 7712 31024766 TQ SIGNAL COND BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 422AM 10620 10620 856 STL - FLT 7316 - LEFT ENGINE WILL NOT MAKE TORQUE. REMOVED AND REPLACED TORQUE SIGNAL CONDITIONER. (M) 2 L 7 2 4T RT A56EU 1997012300479 19970123 00479 EU 1997 1 23 RAIA961205 1 19961211 A 3060 7826894 BRUSH BLOCK AEROSP ATR42 ATR42300 8680920 EU NR 2 PROP INOP A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 426TE 13649 228 STL - FLT 7134 - NR 2 PROP DE-ICE FAULTED AND WOULD NOT RESET. REMOVED AND REPLACED DE-ICE BRUSH BLOCK. (M) 2 H 7 2 4T RT A53EU 1997012300480 19970123 00480 1997 1 23 RAIA961283 3 19961225 A 6140 8659566 BETA SWITCH BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 432AM 7955 883 DEC - FLT 7305 - LEFT BETA WARNING ILLUMINATED DURING TAKEOFF. MAINTENANCE REPLACED THE LEFT BETA SWITCH. (M) 2 L 7 2 4T RT A56EU 1997012300481 19970123 00481 EU 1997 1 23 RAIA961282 1 19961225 A 2435 23079009 STARTER/GEN BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TO TAKEOFF 1 CE 03 424AM 7841 865 STL - FLT 7466 - RIGHT GENERATOR WARNING ILLUMINATED DURING TAKEOFF. MAINTENANCE REPLACED THE RIGHT STARTER/GENERATOR. (M) 2 L 7 2 4T RT A56EU 1997012300482 19970123 00482 1997 1 23 RAIA961281 3 19961224 A 6140 8659566 BETA SWITCH BAG JETSTM JETSTM3201 1500217 EU LT ENGINE CONTAM A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 432AM 883 STL - FLT 7512 - LEFT BETA LIGHT ILLUMINATED DURING TAKEOFF. MAINTENANCE CLEANED THE BETA SWITCH SNUBBER. (M) 2 L 7 2 4T RT A56EU 1997012300483 19970123 00483 EU 1997 1 23 RAIA961279 1 19961220 A 3411 PH11001BJ PITOT TUBE BAG JETSTM JETSTM3201 1500217 EU LEFT CONTAMINATED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 425AM 6850 6850 870 ALO - FLT 7455 - CAPTAINS AIR SPEED INDICATOR STICKS. MAINTENANCE CLEANED ICE FROM CAPTAINS PITOT TUBE. (M) 2 L 7 2 4T RT A56EU 1997012300484 19970123 00484 EU 1997 1 23 RAIA961275 1 19961218 A 3350 6047051 POWER SUPPLY JETAIR JETSTM JETSTM4101 1500501 EU CABIN FAILED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 564HK 2120 41081 STL - AFT EMERGENCY LIGHTS INOP. MAINTENANCE REPLACED THE AFT EMERGENCY POWER SUPPLY (M) 2 L 7 2 4T RT A41NM 1997012300485 19970123 00485 EU 1997 1 23 RAIA961276 1 19961220 A 3350 ML44 BULB AEROSP ATR72 ATR72202 8680940 EU CABIN FAILED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 722TE 220 STL - FLT 7019 - RIGHT AFT EXTERIOR EMERGENCY LIGHT INOP. MAINTENANCE REPLACED THE BULB. (M) 2 H 7 2 4T RT A53EU 1997012300486 19970123 00486 EU 1997 1 23 RAIA961277 1 19961220 A 3350 ML44 BULB AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 424TE 124 STL - FLT 7134 - EMERGENCY LIGHT AT CARGO DOOR INOP. MAINTENANCE REPLACED THE BULB. (M) 2 H 7 2 4T RT A53EU 1997012300487 19970123 00487 EU 1997 1 23 RAIA961278 1 19961220 A 3350 7622210 BULB BAG JETSTM JETSTM3201 1500217 EU CABIN FAILED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 426AM 874 STL - FLT 7054 - RIGHT CENTER EMERGENCY EXIT LIGHT INOP. MAINTENANCE REPLACED THE BULB. (M) 2 L 7 2 4T RT A56EU 1997012300488 19970123 00488 EU 1997 1 23 RAIA961274 1 19961220 A 5320 S53672408228 DOUBLER AEROSP ATR42 ATR42300 8680920 EU AFT FUS CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - DENT IN RIGHT AFT FUSELAGE SKIN AFT OF FRAME 40 BETWEEN STRINGER 12R AND 13R. MAINTENANCE REPAIRED DENT BY INSTAL LATION OF FLUSH REPAIR AND DOUBLER IAW ATR 42 SRM 53-00-00. (M) 2 H 7 2 4T RT A53EU 1997012300489 19970123 00489 EU 1997 1 23 RAIA961273 1 19961220 A 5320 S53672408228 DOUBLER AEROSP ATR42 ATR42300 8680920 EU AFT FUS CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON DOUBLER PLATES AROUND LAV PAN. MAINTENANCE REMOVED CORROSION FROM AROUND LAV PAN IAW ATR 42 SR M 51-21-43. (M) 2 H 7 2 4T RT A53EU 1997012300490 19970123 00490 EU 1997 1 23 RAIA961272 1 19961220 A 5320 S5367131828001 'Z' WEB AEROSP ATR42 ATR42300 8680920 EU AFT FUS CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON RIGHT 'Z' WEB FROM FRAME 39 TO 41. MAINTENANCE REPLACED RIGHT 'Z' WEB FROM FRAME 39 TO 41 IAW ATR 42 SRM 51-20-00. (M) 2 H 7 2 4T RT A53EU 1997012300491 19970123 00491 EU 1997 1 23 RAIA961271 1 19961220 A 5320 S5367131828001 WEB AEROSP ATR42 ATR42300 8680920 EU AFT FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON LEFT 'Z' WEB FROM FRAME 39 TO 40. MAINTENANCE REPLACED LEFT 'Z' WEB FROM FRAME 39 TO 40 IAW AT R 42. (M) 2 H 7 2 4T RT A53EU 1997012300492 19970123 00492 EU 1997 1 23 RAIA961270 1 19961220 A 5320 S5367125720402 TORQUE BOX AEROSP ATR42 ATR42300 8680920 EU AFT FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON LEFT SPRING TORQUE BOX AFT OF FRAME 39. MAINTENANCE REPLACED DECK OF LEFT SPRING TORQUE BOX IA W ATR 42 SRM 51-20-00. (M) 2 H 7 2 4T RT A53EU 1997012300493 19970123 00493 EU 1997 1 23 RAIA961269 1 19961220 A 5320 S5367131828001 WEB AEROSP ATR42 ATR42300 8680920 EU AFT FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 124 STL - MAINTENANCE FOUND CORROSION ON LEFT SHEAR WEB FORWARD OF FRAME 36. MAINTENANCE REPLACED LEFT SHEAR WEB FORWARD OF FRAME 36 IAW ATR 42 SRM 51-20-00. (M) 2 H 7 2 4T RT A53EU 1997012300494 19970123 00494 EU 1997 1 23 RAIA961268 1 19961220 A 5320 S5367131828001 WEB AEROSP ATR42 ATR42300 8680920 EU AFT FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON RIGHT SHEAR WEB FORWARD OF FRAME 36. MAINTENANCE REPLACED RIGHT SHEAR WEB FORWARD OF FRAME 36 IAW ATR 42 SRM 51-20-00. (M) 2 H 7 2 4T RT A53EU 1997012300495 19970123 00495 EU 1997 1 23 RAIA961267 1 19961220 A 5320 S5367131828001 WEB AEROSP ATR42 ATR42300 8680920 EU AFT FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 124 STL - FOUND CORROSION ON RIGHT SHEER WEB AFT OF FRAME 39. MAINTENANCE REPLACED SHEER WEB ON RIGHT SIDE AFT OF FRAME 39 IAW ATR 42 SRM 51-20-00. (M) 2 H 7 2 4T RT A53EU 1997012300496 19970123 00496 EU 1997 1 23 RAIA961266 1 19961220 A 5320 S536720206200 TORQUE BOX AEROSP ATR42 ATR42300 8680920 EU AFT FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON LEFT TORQUE BOX BETWEEN FRAME 36 TO 39. MAINTENANCE REPLACED SILL PLATE ON LEFT TORQUE BOX BET WEEN FRAME 36 T0 39 IAW ATR 42 SRM 51-20-00. (M) 2 H 7 2 4T RT A53EU 1997012300497 19970123 00497 EU 1997 1 23 RAIA961265 1 19961220 A 5320 S536720206200 TORQUE BOX AEROSP ATR42 ATR42300 8680920 EU AFT FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON RIGHT TORQUE BOX BETWEEN FRAME 36 TO 39. MAINTENANCE REPLACED SILL PLATE ON RIGHT TORQUE BOX B ETWEEN FRAME 36 T0 39 IAW ATR 42 SRM 51-20-00. (M) 2 H 7 2 4T RT A53EU 1997012300498 19970123 00498 EU 1997 1 23 RAIA961264 1 19961220 A 5347 S53375001 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU AFT FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON FLIGHT ATTEND SEAT TRACK LEFT SIDE FROM FRAME 36 TO 38. MAINTENANCE REPLACED LEFT FLIGHT ATTEN D SEAT TRACK FROM FRAME 36 YO 38 IAW ATR 42 SRM 53-53-00. (M) 2 H 7 2 4T RT A53EU 1997012300499 19970123 00499 EU 1997 1 23 RAIA961263 1 19961220 A 5347 S53375001 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU AFT FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON FLIGHT ATTENDANT SEAT TRACK RIGHT SIDE FROM FRAME 36 TO 38. MAINTENANCE REPLACED RIGHT FLIGHT ATTEND SEAT TRACK FROM FRAME 36 TO 38 IAW ATR 42 SRM 53-53-00. (M) 2 H 7 2 4T RT A53EU 1997012300500 19970123 00500 EU 1997 1 23 RAIA961262 1 19961220 A 5347 S53375001 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU AFT FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON RIGHT OUTBOARD SEAT TRACK FLOOR BEAM 35 AND 36. MAINTENANCE REPLACED AFT SECTION OF RIGHT OUTB OARD SEAT TRACK FROM FLOOR BEAM 36 FORWARD IAW ATR 42 SRM 53-53-00. (M) 2 H 7 2 4T RT A53EU 1997012300501 19970123 00501 EU 1997 1 23 RAIA961261 1 19961220 A 5347 S53375001 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU AFT FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 124 STL - FOUND CORROSION ON RIGHT INBOARD SEAT TRACK AT FLOOR BEAM. MAINTENANCE REPLACED AFT SECTION OF RIGHT INBOARD SEAT TRACK FROM FLOOR BEAM 36 FORWARD IAW ATR 42 SRM 53-53-00. (M) 2 H 7 2 4T RT A53EU 1997012300502 19970123 00502 EU 1997 1 23 RAIA961260 1 19961220 A 5320 S53671257206 INTERCOSTALS AEROSP ATR42 ATR42300 8680920 EU AFT FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON INTERCOSTALS AT STRINGER 17R FROM FRAME 35 TO FRAME 40. MAINTENANCE REPLACED INTERCOSTALS AT S TRINGER 17R FROM FRAME 35 TO 40 IAW ATR 42 SRM 53-00-00. (M) 2 H 7 2 4T RT A53EU 1997012300503 19970123 00503 EU 1997 1 23 RAIA961259 1 19961220 A 5313 S53671407210218 STRINGER AEROSP ATR42 ATR42300 8680920 EU AFT FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 124 STL - FOUND CORROSION ON STRINGER 21R FROM FRAME 28 TO 29. MAINTENANCE REMOVED CORROSION IAW ATR 42 SRM 51-21-42. (M) 2 H 7 2 4T RT A53EU 1997012300504 19970123 00504 EU 1997 1 23 RAIA961258 1 19961220 A 5313 S53671407210218 STRINGER AEROSP ATR42 ATR42300 8680920 EU AFT FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON STRINGER 20R FROM FRAME 28 TO 30. MAINTENANCE REMOVED CORROSION IAW ATR 42 SRM 51-21-42. (M) 2 H 7 2 4T RT A53EU 1997012300505 19970123 00505 EU 1997 1 23 RAIA961257 1 19961220 A 5320 S53672408228 DOUBLER AEROSP ATR42 ATR42300 8680920 EU AFT FUSELAGE CLOSED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND DOUBLER CORRODED ON FRAME 39 ABOVE STRINGER 15R. MAINTENANCE REPLACED DOUBLER ON FRAME 39 ABOVE STRINGER 15 R IAW ATR42 SRM 53-00-00. (M) 2 H 7 2 4T RT A53EU 1997012300506 19970123 00506 EU 1997 1 23 RAIA961255 1 19961220 A 5320 S53672408228 DOUBLER AEROSP ATR42 ATR42300 8680920 EU AFT FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 124 STL - FOUND CORROSION ON ANTENNA DOUBLER BETWEEN FRAME 32 AND 33. MAINTENANCE REPLACED ANTENNA DOUBLER IAW ATR 42 SRM 5 3-00-00. (M) 2 H 7 2 4T RT A53EU 1997012300507 19970123 00507 EU 1997 1 23 RAIA961254 1 19961220 A 5313 S53671407210218 STRINGER AEROSP ATR42 ATR42300 8680920 EU AFT FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON STRINGER 15R FROM FRAME 38 TO FRAME 41. MAINTENANCE REPAIRED STRINGER 15R FROM FRAME 38 TO 41 IAW ATR 42 SRM 53-00-00. (M) 2 H 7 2 4T RT A53EU 1997012300508 19970123 00508 EU 1997 1 23 RAIA961253 1 19961220 A 5313 S53671407210218 STRINGER AEROSP ATR42 ATR42300 8680920 EU AFT FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON STRINGER 17L FROM FRAME 34 TO FRAME 41. MAINTENANCE REPLACED STRINGER 17L FROM FRAME 34 TO 41 IAW ATR 42 SRM 53-00-00. (M) 2 H 7 2 4T RT A53EU 1997012300509 19970123 00509 EU 1997 1 23 RAIA961252 1 19961220 A 5315 S5367240820201 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU AFT FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON FLOOR BEAM 39. MAINTENANCE REPLACED FLOOR BEAM 39 IAW ATR SRM 53-00-00. (M) 2 H 7 2 4T RT A53EU 1997012300510 19970123 00510 EU 1997 1 23 RAIA961251 1 19961220 A 5315 S5367240820201 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU AFT FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 124 STL - FOUND CORROSION ON FLOOR BEAM 38. MAINTENANCE REPLACED FLOOR BEAM 38 IAW ATR 42 SRM 53. (M) 2 H 7 2 4T RT A53EU 1997012300511 19970123 00511 EU 1997 1 23 RAIA961250 1 19961220 A 5315 S5367240820201 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU AFT FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON FLOOR BEAM 36. MAINTENANCE REPLACED FLOOR BEAM 36 IAW ATR 42 SRM 53-00-00. (M) 2 H 7 2 4T RT A53EU 1997012300512 19970123 00512 EU 1997 1 23 RAIA961249 1 19961220 A 5311 S5367131828001 FRAME AEROSP ATR42 ATR42300 8680920 EU AFT FUSELAGE CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON FRAME 38, WEB. MAINTENANCE REPLACED LOWER FRAME 38 IAW ATR 42 SRM 53-00-00. (M) 2 H 7 2 4T RT A53EU 1997012300513 19970123 00513 NM 1997 1 23 TWRA96383 1 19961226 A 3350 S1356A36 LIGHT BOEING 747 747238B 1384828 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 607PE 20011 DURING DAILY CHECK, FOUND CEILING LIGHT INOP AT SEAT 45 AND 52. REMOVED AND REPLACED CEILING LIGHT ASSEMBLY. OPS CHECK ED NORMAL AS PER MM 33-51-07. (M) 2 L 7 4 4F A20WE 1997012300514 19970123 00514 NM 1997 1 23 TWRA96384 1 19961226 A 3350 3004185 LIGHT BOEING 747 747238B 1384828 NM R2 DOOR INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 607PE 2002 20011 DURING DAILY CHECK, FOUND R2 BUSTLE LIGHT INOP. REMOVED AND REPLACED R2 BUSTLE LIGHT AS PER MM 33-51-07. OPS CHECKED N ORMAL. (M) 2 L 7 4 4F A20WE 1997012300515 19970123 00515 NM 1997 1 23 TWRA96385 1 19961226 A 3350 69B4601017 LIGHT MODULE BOEING 747 747124 1384874 NM L1 DOOR INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 602FF 1165 19734 DURING DAILY CHECK, FOUND AIRCRAFT EVAC LIGHT WOULD NOT SHUT OFF AT 1L DOOR. (SHUTOFF AT FLIGHT DECK ONLY). CLEANED SW ITCH AT L1 DOOR. OPS CHECK OK PER MM 33-51-00. REPLACED EMERGENCY MODULE ASSEMBY ON P5 PANEL. EMERGENCY LIGHTS CHECK NORMAL PER MM 33-51-00 PAGE 501. (M) 2 L 7 4 4F A20WE 1997012300516 19970123 00516 NM 1997 1 23 TWRA96386 1 19961220 A 3350 S1356B37 LIGHT ASSEMBLY BOEING 747 747121 1384871 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 609FF 20354 DURING B-CHECK, FOUND CEILING LIGHT INOP AT 'A' ZONE LEFT SIDE, B-ZONE RIGHT SIDE AND LEFT SIDE FORWARD, R1 DOOR AND L1 DOOR. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM 33-51-00. OPS CHECKED NORMAL. (M) 2 L 7 4 4F A20WE 1997012300517 19970123 00517 NM 1997 1 23 TWRA96387 1 19961220 A 3350 900835A BATTERY PACK BOEING 747 747121 1384871 NM CABIN DISCHARGED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 609FF 20354 DURING B-CHECK, FOUND EXIT SIGN INOP AT R2 DOOR, L2 DOOR, L3 DOOR. REMOVED AND REPLACED BATTERY PACK. OPS CHECKED NORM AL PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1997012300518 19970123 00518 NM 1997 1 23 TWRA96388 1 19961220 A 3350 20131A BATTERY PACK BOEING 747 747121 1384871 NM CABIN DISCHARGED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 609FF 17153 20354 DURING 'B' SERVICE, FOUND 'C' ZONE LEFT AND RIGHT SIDE EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM 3 3-51-00. OPS CHECKED NORMAL. (M) 2 L 7 4 4F A20WE 1997012300519 19970123 00519 WP 1997 1 23 USAAD96184 1 19961222 A 3231 59151695511 LATCH DOUG DC9 DC931 3022065 WP LT MLG DOOR WORN A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 912VJ 47020 FLT 1035 - CLT-SAV - ON GEAR RETRACTION, LEFT GEAR UNSAFE LIGHT REMAINED ON. RETURNED TO CLT. FOUND LEFT MAIN STRIKER WORN ON DOOR LATCH MECHANISM. REPLACED DOOR LATCH ASSEMBLY. (M) 2 L 7 2 4F A6WE 1997012300520 19970123 00520 1997 1 23 USAAD96183 4 19961220 A 3414 B020081104 AIRSPEED IND DOUG DC9 DC931 3022065 WP LEFT STUCK A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 980VJ 33797 48156 FLT 528 - LGA-ROC - ON ROTATION, CAPTAINS AIRSPEED INDICATION FROZE. RETURNED TO FIELD. REPLACED CAPTAINS AIRSPEED IND ICATOR. (M) 2 L 7 2 4F A6WE 1997012300521 19970123 00521 NM 1997 1 23 USAABB96063 1 19961205 A 3350 86210066 BATTERIES BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 619AU 27198 LAX - FOUND EMERGENCY LIGHT BATTERIES DEAD. REPLACED BATTERIES AT ROWS 1, 2, 3, 9 AND 18. (M) 2 L 7 2 4F RT A2NM 1997012300522 19970123 00522 EU 1997 1 23 USAAF96130 1 19961221 A 3230 RETRACT MECH FOKKER F28 F28MK0100 4990807 EU LANDING GEAR LACK OF LUBE A USAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 19 887US 11349 FLT 1475 - PHL-DTW - ON DESCENT INTO DTW RECEIVED AN UNSAFE GEAR INDICATION WARNING AT FL 010. NOSE GEAR DID NOT COME D OWN. CREW DID A GO AROUND AND RECYCLED THE GEAR. LANDING GEAR OPERATED NORMALLY AFTER RECYCLE. NO EMERGENCY DECLARED AND FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE LUBED NOSE GEAR ASSEMBLY, CLEANED SENSORS AND CHECKED TARGET GA PS. PERFORMED SEVERAL GEAR SWINGS. ALL OPERATIONS CHECKED NORMAL. (M) 2 L 7 2 4F RT 1997012300523 19970123 00523 EU 1997 1 23 USAAF96132 1 19961229 A 5270 CONNECTOR FOKKER F28 F28MK0100 4990807 EU CARGO DOOR LOOSE A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 860US 11295 FLT 946 - MEM-PIT - ON CLIMB-OUT, THE MID CARGO DORO UNSAFE LIGHT ILLUMINATED. THE FLIGHT RETURNED TO MEM WITHOUT FURTH ER INCIDENT. MAINTENANCE FOUND THE MID CARGO DOOR WIRING HARNESS CONNECTOR LOOSE. MAINTENANCE SECURED CONNECTOR. DOOR OPERATES NORMALLY. (M) 2 L 7 2 4F RT 1997012300524 19970123 00524 EU 1997 1 23 USAAF96129 1 19961220 A 3260 602HE16 SWITCH FOKKER F28 F28MK4000 4990810 EU RT MLG FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 476US 11224 FLT 519 - PIT-GSO - AFTER TAKEOFF FROM PIT, WHEN CREW RAISED THE GEAR THE GEAR UNSAFE LIGHT ILLUMINATED. RECYCLED GEAR, NO HELP. NO EMERGENCY WAS DECLARED. FLIGHT RETURNED TO PIT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED RIGHT MAIN DOOR SAFE SWITCH AS PER MM 32-61-7. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A20EU 1997012300525 19970123 00525 EU 1997 1 23 USAAF96131 1 19961229 A 2130 SHUTOFF VLV FOKKER F28 F28MK4000 4990810 EU CABIN MALFUNCTIONED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 483US 11233 FLT 577 - PIT-CRW - AIRCRAFT WOULD NOT PRESSURIZE. SELECTED CONTROLLER TO HIGHER BUT NO EFFECT. SHUT OFF PACKS. RETUR NED TO PIT. NO OTHER PROBLEMS FOR DURATION OF FLIGHT. MAINTENANCE RESET THE MANUAL PRESSURIZATION SHUTOFF VALVE AND SE CURED IT. PRESSURIZATION CHECK NORMAL. (M) 2 L 7 2 4F RT A20EU 1997012300526 19970123 00526 EU 1997 1 23 USAA960792 1 19961223 A 5532 SKIN FOKKER F28 F28MK0100 4990807 EU VERT STAB GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 862US 15933 11300 PIT - DURING Q-1 CHECK, FOUND 1.125 INCH LONG, .1875 INCH WIDE (AT TOP) .09375 INCH WIDE (AT BOTTOM) .029 INCH DEEP GOUG ES AT LEFT SIDE OF THE VERTICAL STAB SKIN AT RIB 5.0 AND RIB 3.6. BURNISHED GOUGE AREAS AND INSTALLED AN EXTERNAL DOUBL ER PER EA 34175. (M) 2 L 7 2 4F RT 1997012300527 19970123 00527 EU 1997 1 23 USAA960791 1 19961223 A 5312 D31108001 BULKHEAD FOKKER F28 F28MK0100 4990807 EU BS 14911 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 862US 15933 11300 PIT - DURING Q-1 CHECK, FOUND TWO 3 INCH CRACKS AND 2 .75 INCH CRACKS (LT AND RT SIDES) CENTER PRESSURE BULKHEAD STATION 14911 AT STATION NR 11 (LHS) AND AT STATION NR 64 (RHS). ROUTED OUT CRACKS IN THE FRAME AND INSTALLED SHIMS AND NEW FA BRICATED ANGLES PER EA NR 34172. (M) 2 L 7 2 4F RT 1997012300528 19970123 00528 EU 1997 1 23 USAA960790 1 19961223 A 5330 SKIN FOKKER F28 F28MK0100 4990807 EU FS 23011-24611 DISBONDED A A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 862US 15933 11300 PIT - DURING Q-1 CHECK, FOUND 20 INCH BY 20 INCH DISBONDED SKIN AND HEAT DAMAGE IN FUSELAGE SKIN RIGHT SIDE AND SEAM BET WEEN FRAME 23011 AND 24611. CUT OUT DAMAGED AREA AND INSTALLED AN EXTERNAL DOUBLER PER EA NR 29573B. (M) 2 L 7 2 4F RT 1997012300529 19970123 00529 EU 1997 1 23 USAA960789 1 19961223 A 5311 FRAME FOKKER F28 F28MK0100 4990807 EU FRAME 8805 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 862US 15933 11300 PIT - DURING Q-1 CHECK FOUND .5 INCH BY .5 INCH BY .042 INCH MAX DEPTH TWO AREAS CORRODED AT AFT FRAME OF THE FORWARD CA RGO DOOR OPENING AT FRAME 8805 AND BL 300R. REMOVED CORROSION, BLENDED TO A SMOOTH CONTOUR AND INSTALLED A REPAIR ANGLE PER EA NR 34177. CORROSION LEVEL 1. (M) 2 L 7 2 4F RT 1997012300644 19970123 00644 NM 1997 1 23 9627776608 1 19961127 A 5315 FLOORBEAM BOEING 747 747151 1384891 NM BS 2280 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 608US 19785 DURING PERIODIC CHECK, FOUND CORROSION ON FLOORBEAM AND RIGHT OUTBOARD SUPPORT ANGLE. REMOVED CORROSION, FABRICATED AND INSTALLED .071 FILLER AND .063 7075-T6 STRAP DOUBLER PER EA 66-120474. 2 L 7 4 4F A20WE 1997012300645 19970123 00645 NM 1997 1 23 9627786608 1 19961127 A 5347 SEAT TRACK BOEING 747 747151 1384891 NM BS 452-458 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 608US 19785 DURING PERIODIC CHECK, FOUND CORROSION ON SEAT TRACK FLANGE 28 INBOARD AND 13 TO 18 AFT OF 1L ENTRYWAY FORWARD LOWER COR NER. REPAIRED PER EA 66-120462. 2 L 7 4 4F A20WE 1997012300646 19970123 00646 NM 1997 1 23 9627796608 1 19961209 A 5740 BULKHEAD FITTING BOEING 747 747151 1384891 NM BS 1241 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 608US 19785 DURING PERIODIC CHECK, FOUND CORROSION ON LEFT WING LANDING GEAR WHEEL WELL BULKHEAD FITTING. REPAIRED PER EA 66-120423 . 2 L 7 4 4F A20WE 1997012300647 19970123 00647 NM 1997 1 23 9627806613 1 19961211 A 5315 FLOORBEAM BOEING 747 747251B 1384892 NM BS 460-461 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 613US 20358 DURING CHECK, FOUND CRACK ON UPPER DECK FLOOR BEAM WEB. REPAIRED PER EA 66-120233. 2 L 7 4 4F A20WE 1997012300648 19970123 00648 NM 1997 1 23 9627816636 1 19961213 A 5315 FLOORBEAM BOEING 747 747251B 1384892 NM BS 1300 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 636US 23547 DURING PERIODIC CHECK, FOUND CORROSION ON TOP CHORD OF FLOORBEAM. REPAIRED PER EA 66-120596. 2 L 7 4 4F A20WE 1997012300649 19970123 00649 NM 1997 1 23 9627826636 1 19961213 A 5347 SEAT TRACK BOEING 747 747251B 1384892 NM BS 1318 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 636US 23547 DURING PERIODIC CHECK, FOUND CORROSION ON SEAT TRACK FLANGE. REPAIRED PER EA 66-120596. 2 L 7 4 4F A20WE 1997012300692 19970123 00692 EU 1997 1 23 97ZZZX409 1 19960917 A 3397 WIRE BAG BAE146 BAE146200A 1500266 EU CABIN LOOSE A A6WA K NONE L NO TEST IN INSP/MAINT 1 GL 31 179US E2041 EMERGENCY EXIT LIGHT OVER AISLE IS INOPERATIVE IN BACK. CORRECTIVE ACTION: FOUND LOOSE WIRE, REPAIRED. 2 H 7 4 4F RT A49EU 1997012300693 19970123 00693 NM 1997 1 23 AWXA960436 1 19960820 A 3350 900835A SIGN BOEING 737 737275 1384485 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 CGBPW 21577 20958 PHX - FLT 2081 - DURING ROUTINE MAINTENANCE CHECK, FOUND CENTER AISLE EMERGENCY LIGHT SIGN INOPERATIVE AT ROW 2. REPLAC ED CARTRIDGE ASSEMBLY. OPS CHECK GOOD. (X) 2 L 7 2 4F A16WE 1997012300694 19970123 00694 WP 1997 1 23 97ZZZX410 1 19961203 A 5347 340302 SEAT TRACK CVAC 440 440 2422902 WP CABIN CORROSION A P21A K NONE O OTHER IN INSP/MAINT 1 WP 09 8042W 503 DURING B-1/B-2 INSPECTION, THE RT OUTBOARD FORWARD SEAT TRACK (MAIN CABIN) WAS FOUND TO HAVE INTERGRANULAR CORROSION ON THE TRACK. REMOVED AND REPLACED WITH NEW TRACK. AIRCRAFT WILL BE RETURNED TO SERVICE AFTER INSPECTION IS COMPLETED. 2 L 7 2 4R 6A6 1997012300695 19970123 00695 NM 1997 1 23 USAASB96253 1 19961205 A 3350 AD20131A BATTERY PACK BOEING 737 737301 1384611 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 591US 23936 ALB MAINTENANCE FOUND THE BULLNOSE EMERGENCY EVACUATION LIGHTS INOPERATIVE AT ROWS 12, 16, 18, AND 20. MAINTENANCE REMO VED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1997012300696 19970123 00696 SO 1997 1 23 97ZZZX411 1 19961125 A 3230 454682 CIRCUIT BREAKER PIPER PA31T PA31T3 7103128 SO CB PANEL BROKEN A SOCA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 304SC 31T8275017 AFTER TAKEOFF, PILOT ATTEMPTED TO SELECT THE MAIN LANDING GEAR TO THE UP POSITION. THE GEAR HANDLE WOULD NOT SELECT UP. PILOT RETURNED TO KENAI WITHOUT INCIDENT. AFTER INSPECTING THE AIRCRAFT, MAINTENANCE PERSONNEL FOUND THAT THE CIRCUIT BREAKER FOR THE LANDING GEAR SOLENOID HAD FAILED. THIS SOLENOID PREVENTS THE RETRACTION OF THE MAIN LANDING GEAR WHEN THE AIRCRAFT IS ON THE GROUND. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE CIRCUIT BREAKER PER MM AND OPS CHECKED LA NDING GEAR SYSTEM. RETURNED AIRCRAFT TO SERVICE. 1 L 7 2 3T A8EA 1997012300697 19970123 00697 EU 1997 1 23 829111496 1 19961114 A 2150 PACK BAG JETSTM JETSTM3101 1500215 EU LEFT MALFUNCTIONED A CX7A O E A OTHER ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 03 829JS 713 DSM/MDW - FLT 145 - THE LEFT 'DUCT' WARNING LIGHT ILLUMINATED, PILOT PERFORMED ABNORMAL CHECK LIST AND THEN SHUT DOWN LE FT ENGINE. LANDED IN MCI. AIRCRAFT WAS INSPECTED AND FERRIED TO MDW. LEFT AIR CONDITIONING GROUP DEFERRED PER MEL 21- 1- AND AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A21EU 1997012300698 19970123 00698 EU 1997 1 23 VTZA96468 1 19961228 A 3320 0800634001 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU CABIN SHORTED A VTZA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 27 328UE 41083 EWR/IAD - FLT 6457 - DURING TAXI AT 1730 HRS ON 12-28-96, RETURNED TO GATE DUE TO SMOKE AND ARCING COMING FROM LT CABIN OVERHEAD LIGHT. MAINTENANCE INSPECTED AND PULLED CIRCUIT BREAKER AND FERRIED AIRCRAFT TO IAD. MAINTENANCE REMOVED AND REPLACED OVERHEAD LIGHT SOCKET AND INSPECTED WIRING. MAINTENANCE ALSO FOUND CHAFED WIRE CAUSED BY RUBBING ON RIVET AND REPAIRED WIRE, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1997012300699 19970123 00699 CE 1997 1 23 S2YA960031 1 19961108 A 3010 1293840091 PRESSURE SWITCH BEECH 1900 1900D 1154162 CE BS 570.107 FAILED A A S2YA A UNSCHED LANDING O P OTHER NO WARNING INDICATION CR CRUISE 1 GL 13 881SK 2590 2590 UE88 THE CREW OF FLT 1052, MKE TO IND, CYCLED THE SURFACE DEICE SYSTEM BEFORE ENTERING ICING CONDITIONS USING AUTOMODE. THE TAIL DEICE ANNUNCIATOR FAILED TO ILLUMINATE. THE CREW TURNED BACK FOR MKE DUE TO HEAVY ICING CONDITONS IN IND. MAINTEN ANCE FOUND WATER IN AIR LINE TO THE SWITCH. THEY DRAINED THE LINE AND INSTALLED SERVICEABLE PRESSURE SWITCH, OPS CHECKE D GOOD. (X) 2 L 7 2 4T RT A24CE 1997012300700 19970123 00700 NM 1997 1 23 97ZZZX412 1 19961119 A 3260 631352 BUSHING BOEING 727 727224 1384076 NM NLG POSITION SW WORN A PCSA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 17 895AJ 20660 AFTER DEPARTURE FROM FLL, MLG WAS RETRACTED. GEAR HANDLE WAS THEN MOVED FROM 'UP' TO 'OFF'. GEAR EXTENDED. GEAR WAS S ELECTED DOWN, GEAR INDICATED DOWN AND LOCKED. GEAR WAS RETRACTED AGAIN RESULTING IN NLG UNSAFE INDICATION, AND F.E. PAN EL NLG DOOR LIGHT ILLUMINATED. GEAR SELECTED DOWN, GEAR EXTENDED AND LOCKED NORMALLY. ACFT RETURNED TO FLL. CORRECTIV E ACTION CONSISTED OF REPLACING THE NLG POSITION SWITCH ACTUATOR ARM BUSHING, P/N 63-1352, DUE TO WEAR. 2 L 7 3 4F A3WE 1997012300701 19970123 00701 NM 1997 1 23 W8PA960214 1 19961230 A 3350 BULB BOEING 737 7373B7 1384580 NM CABIN FAILED A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 953WP 23384 FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE AT ROWS 2, 3, 9, 17, AND 22. REPLACED BULBS. (X) 2 L 7 2 4F RT A16WE 1997012300702 19970123 00702 1997 1 23 REXA96079 4 19961223 A 3425 6226190113 AHRS COMPUTER COLLINS 6226190113 CESSNA 340 340A 2076405 CE AVIONICS BAY FAILED A REXA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 111PX 340A024 HEADING SPLIT, HSI WOULD NOT SLAVE. REMOVED AND REPLACED AHRS AND REPAIRED WIRE ON SLAVE BUTTON. (X) 1 L 7 2 3O 3A25 1997012300703 19970123 00703 NM 1997 1 23 M8XA961205 1 19961224 A 2430 1030200 HALL EFFECT SENS DORNER DO32 DO328100 2996000 NM RT ENGINE DEFECTIVE A M8XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 331MX 94 1571 3074 FLT 3535 - AIRCRAFT RETURNED FROM FLIGHT. CREW WAS ALERTED BY A RT GENERATOR FAILURE INDICATION. AIRCRAFT LANDED COS W ITHOUT FURTHER INCIDENT. COS - MX REPLACED HALL EFFECT SENSOR IAW AMM 24-30-00. GROUND CHECKED GOOD. AIRCRAFT RETURNE D TO SERVICE. (X) 2 H 7 2 4T RT A45NM 1997012300704 19970123 00704 NM 1997 1 23 M8XA961206 1 19961227 A 3020 851003A FLOW CNTRL VALVE DORNER DO32 DO328100 2996000 NM LT ENGINE DEFECTIVE A M8XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 03 330MX 1762 0553A 3067 FLT 3005 - AIRCRAFT RETURNED FROM FLIGHT WHEN CREW WAS ALERTED TO LT ENGINE INLET DEICE FAILURE INDICATION. AIRCRAFT LA NDED COS WITHOUT FURTHER INCIDENT. COS - MX REPLACED LT ENGINE INLET EJECTOR FLOW CONTROL VALVE IAW AMM 30-22-03. GROU ND CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A45NM 1997012800002 19970128 00002 SW 1997 1 28 MALA965241 1 19961217 A 5712 2731023 RIB SWRNGN SA227 SA227AC 8780603 SW WS 81 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 430MA AC710 DURING AN INSPECTION IN MSP, FOUND TWO CRACKS IN THE RADIUS OF THE RT WING RIB LOWER ATTACH FLANGE (P/N 27-31023). APPR OXIMATE LOCATION IS WS 81 AND BETWEEN NS 130 AND 141. STOP DRILLED CRACK, FABRICATED AND INSTALLED AN APPROPRIATE SIZED 3 INCH BY 1 INCH BY .050 INCH 2024-T3 REPAIR DOUBLER AND APPLICABLE FILLER PLATES WHERE NEEDED. ALL WORK DONE IAW AERO TECH DESIGNS EA01-96125. (M) 2 L 7 2 4T RT A8SW 1997013000008 19970130 00008 CE 1997 1 30 121696404CK 1 19961217 A 2840 LINE BEECH 18 C45H 1151018 CE FUEL PRESS GAUGE CHAFED A A KKFA A UNSCHED LANDING K FLUID LOSS NR NOT REPORTED 1 GL 23 404CK AF297 FUEL WAS NOTED ON FLOOR OF COCKPIT. PILOT ELECTED TO MAKE A PRECAUTIONARY LANDING. INSPECTION REVEALED THE ALUMINUM FU EL LINE TO THE FUEL PRESSURE GAUGE HAD CHAFED THROUGH ITSELF AGAINST A STRINGER. LINE WAS REPLACED AND LEAK CHECKED. R ECOMMEND THAT ROUTING AND INSPECTION OF ALUMINUM FUEL LINES BE CLOSELY SCRUTINIZED. (X) 1 L 7 2 3R A765 1997013000048 19970130 00048 WP 1997 1 30 9627839614 1 19961218 A 5713 LONGERON DOUG DC9 DC932 3022066 WP WS 58-137 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 614NW 47128 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON LEFT WING STR 19L FROM WS 58 WEB TO WS 137 WEB. REPAIR ED PER EA 99-97708. 2 L 7 2 4F A6WE 1997013000049 19970130 00049 WP 1997 1 30 9627849614 1 19961120 A 5713 LONGERON DOUG DC9 DC932 3022066 WP WS 58-137 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 614NW 47128 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE RIGHT WING STR 16R WS 58 WEB TO WS 137 WEB. REPAIR ED PER EA 99-97708. 2 L 7 2 4F A6WE 1997013000050 19970130 00050 WP 1997 1 30 9627859614 1 19961120 A 5713 LONGERON DOUG DC9 DC932 3022066 WP WS 58 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 614NW 47128 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LEFT WING STR 20L, WS 58 WEB. REPAIRED PER EA 99-9 7708. 2 L 7 2 4F A6WE 1997013000051 19970130 00051 WP 1997 1 30 9627869614 1 19961209 A 5713 LONGERON DOUG DC9 DC932 3022066 WP WS 58-137 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 614NW 47128 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE RIGHT WING STR 17R FROM WS 58 WEB TO OUTBOARD OF WS 137 WEB. REPAIRED PER EA 99-97708. 2 L 7 2 4F A6WE 1997013000052 19970130 00052 WP 1997 1 30 9627879614 1 19961120 A 5713 LONGERON DOUG DC9 DC932 3022066 WP WS 58-137 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 614NW 47128 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE RIGHT WING STR 20R FROM WS 58 WEB TO WS 137 WEB. R EPAIRED PER EA 99-97708. 2 L 7 2 4F A6WE 1997013000053 19970130 00053 WP 1997 1 30 9627889618 1 19961121 A 5713 LONGERON DOUG DC9 DC932 3022066 WP WS 58-69 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 618NW 47433 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE RIGHT WING STR 13R FROM WS 58 TO WS 69. REPAIRED P ER EA 99-97715. 2 L 7 2 4F A6WE 1997013000054 19970130 00054 WP 1997 1 30 9627899618 1 19961121 A 5713 LONGERON DOUG DC9 DC932 3022066 WP WS 58-95 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 618NW 47433 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LEFT WING STR 11L FROM WS 58 TO 4 OUTBOARD OF WS 91 WEB. REPAIRED PER EA 99-97715. 2 L 7 2 4F A6WE 1997013000069 19970130 00069 WP 1997 1 30 UPS97821832 1 19961230 A 5751 DOUBLER DOUG DC8 DC871F 302199D WP LT AILERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-C, LT O/B AILERON AT CENTER HINGE CUTOUT, SKIN DOUBLER IS CRACKED 2 PLACES. REMOVED DAMAGED DOUBLER, FA BRICATED AND INSTALLED DOUBLER PER SRM 57-8-01 FIG 4 AND 51-1-20. 2 L 7 4 4F RT 4A25 1997013000071 19970130 00071 WP 1997 1 30 UPS97821843 1 19961231 A 5751 HINGE DOUG DC8 DC871F 302199D WP LT REAR SPAR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C/CK, LOWER REAR SPAR O/B AILERON O/B HINGE CRACKED. REMOVED LT O/B AILERON, REMOVED AND REPLACED SUPP ORT ASSY IAW DC8 SRM 51-3-1 AND REINSTALLED LT O/B AILERON IAW DC8 MM 27-11-02. 2 L 7 4 4F RT 4A25 1997013000099 19970130 00099 NM 1997 1 30 DL767970117 1 19961223 A 5330 146T02005 SKIN BOEING 767 767232 1385132 NM BS 1540 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 102DA 22214 SKIN AND STRINGERS WERE FOUND CORRODED AT FS 1540 BETWEEN STR 34L AND 39L. A 3.75 BY 2.25 CUTOUT WAS MADE. STRS 34L TO 39L REQUIRED NEW SECTIONS TO BE SPLICED IN. ADDITIONAL DAMAGE WAS FOUND AFTER INITIAL RELEASE OF ER/A. A SECOND 2 BY 3 CUTOUT WAS MADE BETWEEN STR 37L TO 38L. 2 L 7 2 4F RT A1NM 1997013000100 19970130 00100 WP 1997 1 30 DLL13970118 1 19961220 A 5711 1503232129 SPAR WEB LKHEED 1011 10113851 5265010 WP CENTER WING FATIGUE A A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 790DL 193A1143 DURING INSP OF CENTER WING TANK, FS 1043, 1103, 1163 SPAR WEBS WERE FOUND WITH A MISSING ROW OF FASTENERS AT LBL AND RBL 116 END RIBS. THIS WAS A MANUFACTURE DEFECT. NUMEROUS CRACKS WERE FOUND EMANATING FROM THE HOLES. 2 L 7 3 4F A23WE 1997013000144 19970130 00144 SO 1997 1 30 97ZZZX439 1 19961218 A 3260 DOWNLOCK SWITCH PIPER PA31 PA31350 7103110 SO RT MLG REQ LUBE A BSYA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 07 35551 6496 318052063 NO RT GEAR DOWN AND LOCK INDICATION. CLEANED AND LUBED DOWN AND LOCK MECHANISMS AND DOWN AND LOCK SWITCH. CYCLED GEAR. OPS CHECKED GOOD. 1 L 7 2 3O A20SO 1997013000150 19970130 00150 CE 1997 1 30 97ZZZX445 1 19961008 A 3230 HCA3 MOTOR BEECH 18 E18S 1151006 CE MLG MALFUNCTION A GGPA O OTHER P NO WARNING INDICATION AP APPROACH 1 NM 01 42D BA117 PILOT SELECTED GEAR DOWN, GREEN LIGHT DID NOT ILLUMINATE. PILOT THEN CYCLED GEAR AGAIN AND GEAR GREEN LIGHT ILLUMINATED . A/C LANDED WITH NO PROBLEM. AIRCRAFT JACKED AND GEAR RETRACTION PERFORMED SEVERAL TIMES. LANDING GEAR MOTOR WAS CHA NGED FOR PRECAUTION. 1 L 7 2 3R A765 1997013000153 19970130 00153 CE 1997 1 30 97ZZZX448 1 19961217 A 2121 19A3022 FAN MOTOR CESSNA 310 310R 2074245 CE RADIO COOLING FAILED A BSYA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 07 5338C 13493 310R1544 BAD ELECTRICAL SMELL FROM COPILOT'S INST PANEL. FOUND RADIO COOLING FAN MOTOR BAD. REMOVED AND REPLACED COOLING FAN MO TOR AND CIRCUIT BREAKER. OPS CHECKED GOOD. 1 L 7 2 3O 3A10 1997013000218 19970130 00218 CE 1997 1 30 97ZZZX467 1 19961201 A 5713 262200064 STRINGER CESSNA 208 208B 2073701 CE RT WING CRACKED A A HSYA K NONE O OTHER IN INSP/MAINT 1 NM 05 716FX 592 208B0442 WING STRINGER WAS FOUND CRACKED DURING A ROUTINE INSPECTION. CAUSE OF STRINGER FAILURE UNKNOWN. TWELVE OTHER, P/N 2622 000-64, STRINGERS HAVE BEEN FOUND CRACKED ON 208 AND 208B AIRCRAFT WITH PART TT RANGING FROM 596 TO 6511 HOURS. 1 H 7 1 3T A37CE 1997013000219 19970130 00219 SW 1997 1 30 97ZZZX468 1 19961201 A 5713 262200064 STRINGER CESSNA 208 208B 2073701 CE RT WING CRACKED A A HSYA K NONE O OTHER IN INSP/MAINT 1 NM 05 710FX 208B0431 WING STRINGER WAS FOUND CRACKED DURING A ROUTINE INSPECTION. CAUSE OF STRINGER FAILURE UNKNOWN. TWELVE OTHER, P/N 2622 000-64, STRINGERS HAVE BEEN FOUND CRACKED ON 208 AND 208B AIRCRAFT WITH PART TT RANGING FROM 596 TO 6511 HOURS. 1 H 7 1 3T A37CE 1997013000220 19970130 00220 CE 1997 1 30 97ZZZX469 1 19961201 A 5713 262200064 STRINGER CESSNA 208 208B 2073701 CE RT WING CRACKED A HSYA K NONE O OTHER IN INSP/MAINT 1 NM 05 794FE 208B0292 WING STRINGER WAS FOUND CRACKED DURING A ROUTINE INSPECTION. CAUSE OF STRINGER FAILURE UNKNOWN. TWELVE OTHER, P/N 2622 000-64, STRINGERS HAVE BEEN FOUND CRACKED ON 208 AND 208B AIRCRAFT WITH PART TT RANGING FROM 596 TO 6511 HOURS. 1 H 7 1 3T A37CE 1997013000221 19970130 00221 CE 1997 1 30 97ZZZX470 1 19961201 A 5713 262200064 STRINGER CESSNA 208 208B 2073701 CE RT WING CRACKED A HSYA K NONE O OTHER IN INSP/MAINT 1 NM 05 766FE 208B0260 WING STRINGER WAS FOUND CRACKED DURING A ROUTINE INSPECTION. CAUSE OF STRINGER FAILURE UNKNOWN. TWELVE OTHER, P/N 2622 000-64, STRINGERS HAVE BEEN FOUND CRACKED ON 208 AND 208B AIRCRAFT WITH PART TT RANGING FROM 596 TO 6511 HOURS. 1 H 7 1 3T A37CE 1997013000222 19970130 00222 CE 1997 1 30 97ZZZX471 1 19961201 A 5713 262200064 STRINGER CESSNA 208 208B 2073701 CE RT WING CRACKED A HSYA K NONE O OTHER IN INSP/MAINT 1 NM 05 751FE 208B0245 WING STRINGER WAS FOUND CRACKED DURING A ROUTINE INSPECTION. CAUSE OF STRINGER FAILURE UNKNOWN. TWELVE OTHER, P/N 2622 000-64, STRINGERS HAVE BEEN FOUND CRACKED ON 208 AND 208B AIRCRAFT WITH PART TT RANGING FROM 596 TO 6511 HOURS. 1 H 7 1 3T A37CE 1997013000223 19970130 00223 CE 1997 1 30 97ZZZX472 1 19961201 A 5713 262200064 STRINGER CESSNA 208 208B 2073701 CE RT WING CRACKED A HSYA K NONE O OTHER IN INSP/MAINT 1 NM 05 877FE 208B0232 WING STRINGER WAS FOUND CRACKED DURING A ROUTINE INSPECTION. CAUSE OF STRINGER FAILURE UNKNOWN. TWELVE OTHER, P/N 2622 000-64, STRINGERS HAVE BEEN FOUND CRACKED ON 208 AND 208B AIRCRAFT WITH PART TT RANGING FROM 596 TO 6511 HOURS. 1 H 7 1 3T A37CE 1997013000224 19970130 00224 CE 1997 1 30 97ZZZX473 1 19961201 A 5713 262200064 STRINGER CESSNA 208 208B 2073701 CE RT WING CRACKED A HSYA K NONE O OTHER IN INSP/MAINT 1 NM 05 796FE 208B0212 WING STRINGER WAS FOUND CRACKED DURING A ROUTINE INSPECTION. CAUSE OF STRINGER FAILURE UNKNOWN. TWELVE OTHER, P/N 2622 000-64, STRINGERS HAVE BEEN FOUND CRACKED ON 208 AND 208B AIRCRAFT WITH PART TT RANGING FROM 596 TO 6511 HOURS. 1 H 7 1 3T A37CE 1997013000225 19970130 00225 CE 1997 1 30 97ZZZX474 1 19961201 A 5713 262200064 STRINGER CESSNA 208 208B 2073701 CE RT WING CRACKED A HSYA K NONE O OTHER IN INSP/MAINT 1 NM 05 868FE 208B0193 WING STRINGER WAS FOUND CRACKED DURING A ROUTINE INSPECTION. CAUSE OF STRINGER FAILURE UNKNOWN. TWELVE OTHER, P/N 2622 000-64, STRINGERS HAVE BEEN FOUND CRACKED ON 208 AND 208B AIRCRAFT WITH PART TT RANGING FROM 596 TO 6511 HOURS. 1 H 7 1 3T A37CE 1997013000226 19970130 00226 CE 1997 1 30 97ZZZX475 1 19961201 A 5713 262200064 STRINGER CESSNA 208 208B 2073701 CE RT WING CRACKED A A HSYA K NONE O OTHER IN INSP/MAINT 1 NM 05 798FE 208B0174 WING STRINGER WAS FOUND CRACKED DURING A ROUTINE INSPECTION. CAUSE OF STRINGER FAILURE UNKNOWN. TWELVE OTHER, P/N 2622 000-64, STRINGERS HAVE BEEN FOUND CRACKED ON 208 AND 208B AIRCRAFT WITH PART TT RANGING FROM 596 TO 6511 HOURS. 1 H 7 1 3T A37CE 1997013000227 19970130 00227 CE 1997 1 30 97ZZZX476 1 19961201 A 5713 262200064 STRINGER CESSNA 208 208B 2073701 CE RT WING CRACKED A HSYA K NONE O OTHER IN INSP/MAINT 1 NM 05 851FE 208B0166 WING STRINGER WAS FOUND CRACKED DURING A ROUTINE INSPECTION. CAUSE OF STRINGER FAILURE UNKNOWN. TWELVE OTHER, P/N 2622 000-64, STRINGERS HAVE BEEN FOUND CRACKED ON 208 AND 208B AIRCRAFT WITH PART TT RANGING FROM 596 TO 6511 HOURS. 1 H 7 1 3T A37CE 1997013000228 19970130 00228 CE 1997 1 30 97ZZZX477 1 19961201 A 5713 262200064 STRINGER CESSNA 208 208B 2073701 CE RT WING CRACKED A HSYA K NONE O OTHER IN INSP/MAINT 1 NM 05 797FE 208B0042 WING STRINGER WAS FOUND CRACKED DURING A ROUTINE INSPECTION. CAUSE OF STRINGER FAILURE UNKNOWN. TWELVE OTHER, P/N 2622 000-64, STRINGERS HAVE BEEN FOUND CRACKED ON 208 AND 208B AIRCRAFT WITH PART TT RANGING FROM 596 TO 6511 HOURS. 1 H 7 1 3T A37CE 1997013000229 19970130 00229 CE 1997 1 30 97ZZZX478 1 19961201 A 5713 262200064 STRINGER CESSNA 208 208B 2073701 CE RT WING CRACKED A HSYA K NONE O OTHER IN INSP/MAINT 1 NM 05 933FE 208B0033 WING STRINGER WAS FOUND CRACKED DURING A ROUTINE INSPECTION. CAUSE OF STRINGER FAILURE UNKNOWN. TWELVE OTHER, P/N 2622 000-64, STRINGERS HAVE BEEN FOUND CRACKED ON 208 AND 208B AIRCRAFT WITH PART TT RANGING FROM 596 TO 6511 HOURS. 1 H 7 1 3T A37CE 1997013000230 19970130 00230 CE 1997 1 30 97ZZZX479 1 19961201 A 5713 262200064 STRINGER CESSNA 208 208B 2073701 CE RT WING CRACKED A HSYA K NONE O OTHER IN INSP/MAINT 1 NM 05 9454B 208B0072 WING STRINGER WAS FOUND CRACKED DURING A ROUTINE INSPECTION. CAUSE OF STRINGER FAILURE UNKNOWN. TWELVE OTHER, P/N 2622 000-64, STRINGERS HAVE BEEN FOUND CRACKED ON 208 AND 208B AIRCRAFT WITH PART TT RANGING FROM 596 TO 6511 HOURS. 1 H 7 1 3T A37CE 1997013000234 19970130 00234 WP 1997 1 30 Y2PA96102 1 19961215 A 5610 5912290502 WINDOW DOUG DC9 DC915F 3022037 WP RT COCKPIT FAILED A Y2PA O OTHER O OTHER CR CRUISE 1 GL 23 193US FGP494 45828 IND - FLT 23340 - DURING CRUISE, FL 350, THE OUTER PANE OF THE FLIGHT DECK FIRST OFFICER'S MAIN WINDOW CRACKED. THE COM PANY OPERATION MANUAL PROCEDURES WERE FOLLOWED AND THE AIRCRAFT LANDED AT ITS ARRIVAL LOCATION (IND) WITHOUT INCIDENT. A MECHANIC WAS SENT FROM YIP TO IND TO INSPECT THE WINDOW. IT WAS INSPECTED AND FOUND SAFE FOR A FERRY FLIGHT FROM IND T O YIP (UNPRESSURIZED, BELOW FL 100), WHERE THE WINDOW WAS REPLACED. (X) 2 L 7 2 4F A6WE 1997013000235 19970130 00235 EU 1997 1 30 C2XA96IA294 1 19961203 A 3260 140FL01D3Y1 SWITCH AEROSP ATR42 ATR42500 EU RT MLG FAILED A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 14451 512 IAH - FLT 3861 - PILOT REPORTED THAT THE RIGHT GEAR UNLOCK LIGHT REMAINED ILLUMINATED AFTER GEAR WAS UP. THE AIRCRAFT R ETURNED TO THE FIELD WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT GEAR LIMIT SWITCH, AND THE AIRCRAFT W AS APPROVED FOR RETURN TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1997013000236 19970130 00236 EU 1997 1 30 C2XA96IA293 1 19961203 A 3230 C24589000 UPLOCK AEROSP ATR42 ATR42500 EU LT MLG FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 19446 1493 504 IAH - FLT 3939 - PILOT REPORTED THAT THE LT MAIN GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT INC IDENT. MAINTENANCE REMOVED AND REPLACED THE LT GEAR UPLOCK, THE GEAR SYSTEM OPERATIONALLY CHECKED GOOD AND WAS RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1997013000237 19970130 00237 EU 1997 1 30 97ZZZX483 1 19961031 A 2133 143312C OUTFLOW VALVE AMD FALC20 FALCON20C5 2730107 EU CABIN MALFUNCTIONED A DKAA A B UNSCHED LANDING EMER. DESCENT F G FLT CONT AFFECTED MULTIPLE FAILURE CL CLIMB 1 GL 23 810RA 1537 1576 81 AIRCRAFT WILL NOT HOLD CABIN PRESSURE IN EITHER MANUAL OR NORMAL PRESSURIZATION. REPLACED CABIN OUTFLOW VALVE AND CABIN PRESSURE CONTROLLER. OPERATIONAL CHECKS GOOD IAW WITH AMD MM CHAPTER 21. (MCO) 2 L 7 2 4F RT A7EU 1997013000238 19970130 00238 EU 1997 1 30 97ZZZX484 1 19961031 A 2131 133007 CONTROLLER AMD FALC20 FALCON20C5 2730107 EU CABIN MALFUNCTIONED A DKAA A B UNSCHED LANDING EMER. DESCENT O OTHER CL CLIMB 1 GL 23 810RA 1537 538 81 AIRCRAFT WILL NOT HOLD CABIN PRESSURE IN EITHER MANUAL OR NORMAL PRESSURIZATION . REPLACED CABIN OUTFLOW VALVE AND CABI N PRESSURE CONTROLLER. OPERATIONAL CHECKS GOOD IAW WITH AMD MM CHAPTER 21. (MCO) 2 L 7 2 4F RT A7EU 1997013000239 19970130 00239 EU 1997 1 30 97ZZZX485 1 19961213 A 7931 MS3126F106S CONNECTOR AMD FALC20 FALCON20C5 2730107 EU LT ENGINE FAILED A DKAA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 23 301R 3 LEFT OIL PRESSURE LIGHT CAME ON AND LT OIL PRESSURE GAUGE INDICATED ZERO. PROCEEDED WITH PRECAUTIONARY ENGINE SHUT DOWN . REPLACED NR 1 OIL PRESSURE TRANSMITTER CANNON PLUG. SYSTEM OPERATIONAL CHECKS GOOD ON GROUND RUN (MDT). AIRCRAFT RE TURNED TO SERVICE. 2 L 7 2 4F RT A7EU 1997013000240 19970130 00240 NM 1997 1 30 WRLA96056 1 19961223 A 2710 AILERON CONTROLS DOUG MD11 MD11 3023602 NM RIGHT FAILED TEST A WRLA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 EA 27 277WA 48743 DURING TAXIING OUT, FLIGHT CREW NOTED RIGHT OUTBOARD AILERON FAILED CONTROL TEST. FLIGHT CREW ELECTED TO RETURN TO GATE . AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE CREW PERFORMED AILERON TEST SEVERAL TIMES, EACH TIME SYSTEM PASSED WITH NO FAULTS NOTED. MAINTENANCE COULD NOT IDENTIFY ANY FAULT WITH FLIGHT CONTROL SYSTEM. AIRCRAFT RET URNED TO SERVICE. (X) 2 L 7 3 4F RT A22WE 1997013000296 19970130 00296 NE 1997 1 30 97ZZZX488 2 19960112 A 7230 COMPRESSOR BOEING 767 767205 1385121 NM PWA JT9 JT9D7R4D 52054 NE NR 1 ENGINE FAILED A TWAA O OTHER R PARTIAL RPM/PWR LOSS CL CLIMB 1 CE 05 650TW 23057 SEA - FLT 740 - DURING CLIMB, NR 1 ENGINE, SN 4603, SURGED. POWER WAS REDUCED TO IDLE. CHANGED NR 1 ENGINE. ENGINE TO TAL TIME: 29,752 HOURS; 8,040 CYCLES. INVESTIGATION REVEALED THE HIGH PRESSURE COMPRESSOR HAD NON-CONCENTRIC RUBBING O F RUBSTRIPS ON THE 11TH THROUGH 15TH STAGES. THE HIGH PRESSURE COMPRESSOR 'B' MODULE WAS REPLACED AND ENGINE, SN 4603, W AS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A1NM E3NE 1997013000297 19970130 00297 NM 1997 1 30 AALA961590 1 19961031 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1310 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1762B 48552 TUL - CORROSION AT LAVATORY 'M' FORWARD INBOARD TIE DOWN LUG. INSTALLED PLUG REPAIR PER SRM 53-70-00. TST 16,115.02 HO URS. CYCLES, 2,121. (X) 2 L 7 3 4F RT A22WE 1997013000298 19970130 00298 WP 1997 1 30 AALA961591 1 19961031 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1129 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 162AA 46943 TUL - DURING SPECIAL VISIT TO TUL, FOUND FUSELAGE SKIN BULGED AND CRACKED AT STA 1129 BETWEEN LONGERONS 47L AND 48L. CU T OUT SKIN TO REMOVE CORROSION AND CRACK AND INSTALLED REPAIR DOUBLER PER SRM 53-20-00, VOL I, PAGES 75 AND 76. TST: 6 4,427:38 HOURS. CYCLES, 24,723. (X) 2 L 7 3 4F A22WE 1997013000299 19970130 00299 NM 1997 1 30 AALA961605 1 19961030 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 493-495 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1762B 48552 TUL - CORROSION AT NR 7 RT FLOOR SEAT TRACK, AFT, INBOARD ANCHOR POINT FOR LAVATORY 'B'. INSTALLED CHANNEL PLUG PER SRM 53-70-00-0, VOL 1, FIG 4. TST: 16,115.02 HOURS. CYCLES, 2,121. (X) 2 L 7 3 4F RT A22WE 1997013000300 19970130 00300 NM 1997 1 30 AALA961682 1 19961114 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 459 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1764B 48554 TUL - CORROSION ON NR 1 SEAT TRACK ON FLOOR, LT SIDE, OF A-ZONE. INSTALLED FLOOR SEAT TRACK REPAIR PLUG PER SRM 53-70-0 0-0, VOL I, PAGE 8, FIGURE 4, SHEETS 1 AND 2. TST: 16,324 HOURS. CYCLES, 2,103. (X) 2 L 7 3 4F RT A22WE 1997013000301 19970130 00301 NM 1997 1 30 AALA961679 1 19961114 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1346-1348 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1764B 48554 TUL - DURING C-CHECK, FOUND CORROSION ON NR 2 SEAT TRACK UNDER LAVATORY 'L' BETWEEN STA 1346 AND STA 1348 IN MID-CABIN. CUT OUT CORROSION AND INSTALLED SEAT TRACK PLUG REPAIR PER SRM 53-70-00, VOL I, PAGES 8-9, FIG 4. TST: 16,324.30 HOUR S. CYCLES, 2,103. (X) 2 L 7 3 4F RT A22WE 1997013000302 19970130 00302 NM 1997 1 30 AALA961683 1 19961114 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 496 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1764B 48554 TUL - CORROSION ON NR 2 SEAT TRACK ON FLOOR, LT SIDE OF A-ZONE. INSTALLED FLOOR SEAT TRACK REPAIR PLUG IAW SRM CH 53-70 -00-0, VOL 1, PAGE 8, FIGURE 4, SHEETS 1 AND 2. TST: 16,324. CYCLES, 2,103. (X) 2 L 7 3 4F RT A22WE 1997013000303 19970130 00303 NM 1997 1 30 AALA961684 1 19961114 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1312-1315 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1764B 48554 TUL - DURING C-CHECK, FOUND CORROSION ON NR 2 SEAT TRACK UNDER LAVATORY 'L' IN MID-CABIN BETWEEN STA 1312 AND STA 1315. CUT OUT CORROSION AND INSTALLED SEAT TRACK PLUG REPAIR PER SRM 53-70-00, VOL I, PAGES 8-9, FIGURE 4. TST: 16,324.30 H OURS. CYCLES, 2,103. (X) 2 L 7 3 4F RT A22WE 1997013000305 19970130 00305 NM 1997 1 30 AALA961686 1 19961115 A 5320 SUPPORT DOUG MD11 MD11 3023602 NM BS 392 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1764B 48554 TUL - FLOOR BOARD SUPPORT IS CORRODED AT BS 392. FABRICATED NEW FLOOR BOARD SUPPORT PER SRM 53-0, VOL I, PAGE 1 AT STA 392 TO STA 467. PRIMED AND PAINTED. TST: 16,324.30 HOURS. CYCLES, 2,103. (X) 2 L 7 3 4F RT A22WE 1997013000306 19970130 00306 NM 1997 1 30 AALA961688 1 19961115 A 5320 SUPPORT DOUG MD11 MD11 3023602 NM BS 467 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1764B 48554 TUL - FLOOR BOARD SUPPORT AT STA 467 BETWEEN SEAT TRACKS 3 AND 4 HAS CORROSION AROUND ALL SCREW HOLES. INSTALLED A NEW FLOOR BOARD SUPPORT PER SRM 53-00-01, PAGE 1, VOL I. TST: 16,324 HOURS. CYCLES, 2,103. (X) 2 L 7 3 4F RT A22WE 1997013000307 19970130 00307 NM 1997 1 30 AALA961689 1 19961115 A 5320 SUPPORT DOUG MD11 MD11 3023602 NM BS 467 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1764B 48554 TUL - FLOOR BOARD SUPPORT BETWEEN SEAT TRACKS 5 AN 6 HAS CORROSION AROUND SCREW HOLES. INSTALLED A NEW FLOOR BOARD SUPP ORT PER SRM 53-00-01, PAGE 1, VOL I AND PAINTED. TST: 16,324.30 HOURS. CYCLES, 2,103. (X) 2 L 7 3 4F RT A22WE 1997013000308 19970130 00308 NM 1997 1 30 AALA961690 1 19961115 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 459 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1764B 48554 TUL - CORROSION ON NR 8 SEAT TRACK ON FLOOR, RT SIDE OF A-ZONE. PERFORMED STANDARD SEAT TRACK REPAIR. PLUG INSTALLATIO N IAW SRM 53-70-00-0, VOL I, PAGES 8 AND 9, FIG 4, SHEETS 1 AND 2. TST: 16,324.30 HOURS. CYCLES, 2,103. (X) 2 L 7 3 4F RT A22WE 1997013000309 19970130 00309 NM 1997 1 30 AALA961697 1 19961118 A 5320 SUPPORT DOUG MD11 MD11 3023602 NM BS 392 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1764B 48554 TUL - NR 2 GALLEY INBOARD SUPPORT HAS CORROSION AROUND AFT INBOARD EDGES. INSTALLED NEW NR 2 GALLEY FLOOR SUPPORT PER S RM 53-00-01. TST: 16,324.30 HOURS. CYCLES, 2,103. 9X) 2 L 7 3 4F RT A22WE 1997013000310 19970130 00310 NM 1997 1 30 AALA961698 1 19961118 A 5347 TIE DOWN DOUG MD11 MD11 3023602 NM BS 428 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1764B 48554 TUL - NR 2 GALLEY CENTER SUPPORT TIE DOWN HAD CORROSION AROUND AFT END. INSTALLED A NEW NR 2 GALLEY CENTER SUPPORT TIE DOWN PER SRM 53-00-01. TST: 16,324.30 HOURS. CYCLES, 2,103. (X) 2 L 7 3 4F RT A22WE 1997013000311 19970130 00311 NM 1997 1 30 AALA961699 1 19961118 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1961-1964 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1764B 48554 TUL - DURING C-CHECK, FOUND CORROSION ON NR 1 SEAT TRACK UNDER LAVATORY 'H' IN AFT CABIN BETWEEN STA 1961 AND STA 1964. CUT OUT CORROSION AND INSTALLED SEAT TRACK REPAIR PER SRM 53-70-00, PAGES 8 AND 9, AND ESO 41000 DATED 11-18-96. TST: 16,324.30 HOURS. CYCLES, 2,103. (X) 2 L 7 3 4F RT A22WE 1997013000312 19970130 00312 NM 1997 1 30 AALA961702 1 19961111 A 5210 146N6201 PAN BOEING 757 757223 1384957 NM R4 DOOR GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 668AA 25333 AFW - R-4 DOOR HANDLE PAN HAS A SMALL GOUGE. AFTER BLENDING, IS BEYOND SRM LIMITS. REFINISH THE BLEND OUT PER REF 'C', SRM SECTION. TST: 14,753.23 HOURS. CYCLES, 5,396. (X) 2 L 7 2 4F RT A2NM 1997013000313 19970130 00313 NM 1997 1 30 AALA961703 1 19961106 A 5315 141N5113 FLOOR BEAM BOEING 757 757223 1384957 NM BS 377 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 668AA 25333 AFW - FLOOR BEAM AT STA 377 HAS CORROSION. ALODINE BLENDED AREAS, FABRICATE STRAPS .050 INCH 301 1/2 HARD STAINLESS STE EL. APPLY TWO COATS PRIMER TO STRAP AND FLOOR BEAM. FILL BLENDED AREA WITH BMS 5-92. INSTALL STRAP USING BACB 30NW6 H ILOCKS. TST: 14,753.23 HOURS. CYCLES, 5,396. (X) 2 L 7 2 4F RT A2NM 1997013000314 19970130 00314 NM 1997 1 30 AALA961704 1 19961106 A 5320 141N5100 SUPPORT BOEING 757 757223 1384957 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 668AA 25333 AFW - FLOOR SUPPORT STRUCTURE IN SEC 41 HAS CORROSION. MATERIAL REMAINING IS BEYOND SRM ALLOWABLE LIMITS. BLENDED OUT CORROSION AT ALL LOCATIONS. ALODINED, APPLY TWO COATS PRIMER AND FILL WITH BMS5-92. TST: 14,753.23 HOURS. CYCLES, 5, 396. (X) 2 L 7 2 4F RT A2NM 1997013000315 19970130 00315 NM 1997 1 30 AALA961705 1 19961106 A 5315 141N5089 FLOOR BEAM BOEING 757 757223 1384957 NM BS 1640 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 668AA 25333 AFW - FLOOR BEAM AT STA 1640 HAS CORROSION ON UPPER SURFACE. MATERIAL REMAINING IS BEYOND SRM ALLOWABLE LIMITS. ALODIN E ALL BLENDED AREAS. FABRICATE STRAPS FROM .050 INCH 301 1/2 HARD STAINLESS STEEL. APPLY TWO COATS PRIMER TO STRAPS A ND FLOOR BEAM. FILL ALL BLENDED AREAS WITH MS5-92 TYPE 10R3. INSTALL STRAPS USING BACB30NW6 HILOCKS. TST: 14,753.23 HOURS. CYCLES, 5,396. (X) 2 L 7 2 4F RT A2NM 1997013000316 19970130 00316 NM 1997 1 30 AALA961706 1 19961106 A 5315 141N2932 FLOOR BEAM BOEING 757 757223 1384957 NM BS 324 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 668AA 25333 AFW - FLOOR BEAM AT STA 324 HAS CORROSION ON UPPER SURFACE. MATERIAL REMAINING IS BEYOND SRM ALLOWABLE LIMITS. BLEND O UT CORROSION. ALODINE, APPLY TWO COATS PRIMER AND FILL WITH BMS5-92. TST: 14,753.23 HOURS. CYCLES, 5,396. (X) 2 L 7 2 4F RT A2NM 1997013000317 19970130 00317 NM 1997 1 30 AALA961707 1 19961111 A 5320 146N8522 SILL BOEING 757 757223 1384957 NM CARGO DOORWAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 668AA 25333 AFW - AFT CARGO DOOR LOWER SILL INNER CHORD HAD CORROSION. BLENDED BEYOND SRM LIMITS. BLEND OUT IAW 757 SRM 5-10-00. A LODINE AND APPLY TWO COATS OF PRIMER. FILL BLENDED AREA WITH BMS5-92 TYPE 10R3. APPLY DINOL OVER AREA. REINSTALL SAME TYPE FASTENER AS REMOVED. TST: 14,753.23 HOURS. CYCLES, 5,396. (X) 2 L 7 2 4F RT A2NM 1997013000318 19970130 00318 NM 1997 1 30 AALA961753 1 19961202 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1351 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1765B 48596 TUL - NR 7 SEAT TRACK CORRODED AT STA 1351. REMOVED CORROSION, INSTALLED SEAT TRACK PLUG PER SRM 53-70-00. TST: 16,38 5. CYCLES, 2,173. (X) 2 L 7 3 4F RT A22WE 1997013000319 19970130 00319 NM 1997 1 30 AALA961754 1 19961202 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1315 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1765B 48596 TUL - NR 8 SEAT TRACK CORRODED AT STA 1315. REMOVED CORROSION, INSTALLED SEAT TRACK PLUG PER SRM 53-70-00, VOL I. TST: 16,385. CYCLES, 2,173. (X) 2 L 7 3 4F RT A22WE 1997013000320 19970130 00320 WP 1997 1 30 AALA961758 1 19961101 A 5320 CUSP DOUG DC9 DC982 3022082 WP BS 685 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 483A 49676 TUL - CORORSION AT CUSP STA 685, RT. CUT OUT CORROSION, INSTALLED DOUBLER PER SRM 53-01, FIG 4, SHEET 3. TST: 23,817. 05 HOURS. CYCLES, 13,327. (X) 2 L 7 2 4F A6WE 1997013000321 19970130 00321 NM 1997 1 30 AALA961761 1 19961204 A 5320 SUPPORT DOUG MD11 MD11 3023602 NM BS 1887-2007 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1765B 48596 TUL - FLOOR BOARD SUPPORT INBOARD OF NR 2 GALLEY SUPPORT HAS CORRODED. INSTALLED A NEWLY MANUFACTURED FLOOR BOARD SUPPO RT JUST INBOARD OF THE NR 2 GALLEY SUPPORT. DATE, 12-4-96, PER SRM 53-00-01-0, VOL I. TST: 16,385 HOURS. CYCLES, 2,1 73. (X) 2 L 7 3 4F RT A22WE 1997013000322 19970130 00322 NM 1997 1 30 AALA961762 1 19961204 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1351 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1765B 48596 TUL - NR 2 SEAT TRACK CORRODED AT STA 1351. REMOVED DAMAGED SECTION OF SEAT TRACK AND INSTALLED NEW SECTION OF TRACK AN D SPLICES PER SRM 53-70-00, FIG 1, VOL I. TST: 16,385 HOURS. CYCLES, 2,173. (X) 2 L 7 3 4F RT A22WE 1997013000323 19970130 00323 NM 1997 1 30 AALA961763 1 19961204 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1315 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1765B 48596 TUL - NR 2 SEAT TRACK CORRODED AT STA 1315. REMOVED DAMAGED SECTION OF SEAT TRACK AND INSTALLED NEW SECTION OF SEAT TRA CK WITH SPLICES PER SRM 53-70-00, FIG 1, VOLT I. TST: 16,385. CYCLES, 2,173. (X) 2 L 7 3 4F RT A22WE 1997013000324 19970130 00324 NM 1997 1 30 AALA961766 1 19961204 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1351 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1765B 48596 TUL - NR 1 SEAT TRACK CORRODED AT STA 1351. REMOVED 40 INCHES OF TRACK FROM STA 1331 TO STA 1371. INSTALLED NEW SECTIO N OF TRACK AND TWO SPLICES 17 INCHES EACH LONG. TREATED/PRIMED AND PAINTED PER SRM 57-70-00, VOL I. TST: 16,385 HOURS . CYCLES, 2,173. (X) 2 L 7 3 4F RT A22WE 1997013000325 19970130 00325 NM 1997 1 30 AALA961767 1 19961205 A 5347 GALLEY TRACK DOUG MD11 MD11 3023602 NM BS 1887-2007 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1765B 48596 TUL - GALLEY SUPPORT NR 4 HAS CORROSION ALONG TRACK. NEW SUPPORT MADE PER SRM 51-00-00-1, AND INSTALLED ON AIRCRAFT. T ST: 16,385 HOURS. CYCLES, 2,173. (X) 2 L 7 3 4F RT A22WE 1997013000326 19970130 00326 NM 1997 1 30 AALA961792 1 19961120 A 5315 141N5111 FLOOR BEAM BOEING 757 757223 1384957 NM BS 345 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 661AA 25295 AFW - FLOOR BEAM STA 345 HAS CORROSION REMOVAL ON UPPER SURFACE. MATERIAL REMAINING IS BEYOND SRM LIMITS. REF E58 AND NR 1830905. ALODINE BLENDED AREA. FABRICATE STRAP USING .050 INCH 301 1/2 HARD SS. APPLY 2 COATS PRIMER TO STRAP AND FLOOR BEAM. FILL ALL BLENDED AREAS USING BMS5-92, TYPE 10R3. INSTALL STRAP WET WITH BMS 5-95 SEALANT USING BACB30NW6 H ILOCKS. TST: 15,026.39 HOURS. CYCLES, 5,412. (X) 2 L 7 2 4F RT A2NM 1997013000327 19970130 00327 NM 1997 1 30 AALA961793 1 19961120 A 5315 141N5114 FLOOR BEAM BOEING 757 757223 1384957 NM BS 395 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 661AA 25295 AFW - FLOOR BEAM STA 395 HAS CORROSION REMOVAL. ALODINE BLENDED AREA, FABRICATE STRAP USING .050 301 1/2 HARD SS. APPL Y 2 COATS PRIMER TO STRAP AND FLOOR BEAM. FILL BLENDED AREA WITH BMS5-92 TYPE 10R3. INSTALL STRAP WET USING BMS5-95 SE ALANT USING BACB30NW6 HILOCKS. TST: 15,026.39 HOURS. CYCLES, 5,412. (X) 2 L 7 2 4F RT A2NM 1997013000328 19970130 00328 NM 1997 1 30 AALA961794 1 19961209 A 5320 ANGLE DOUG MD11 MD11 3023602 NM NR 4 GALLEY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1765B 48596 TUL - T-ANGLE CORRODED AT NR 4 GALLEY SUPPORT HOOK-UP POINT. INSTALLED T-ANGLE DOUBLER REPAIR AT NR 4 GALLEY SUPPORT PE R ESO 41000 DATED 12-6-96. TST: 16,385 HOURS. CYCLES, 2,173. (X) 2 L 7 3 4F RT A22WE 1997013000329 19970130 00329 NM 1997 1 30 AALA961795 1 19961119 A 5315 146N5089 FLOOR BEAM BOEING 757 757223 1384957 NM BS 1640 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 661AA 25295 AFW - FLOOR BEAM AT STA 1640 HAS CORROSION REMOVAL ON UPPER SURFACE. MATERIAL REMOVED IS BEYOND SRM ALLOWABLE LIMITS. R EF: E58 1830949 AND 1830950. ALODINE ALL BLENDED AREAS. FABRICATE STRAPS USING .050 INCH 301 1/2 HARD SS. APPLY 2 CO ATS PRIMER TO STRAPS AND FLOOR BEAM. FILL BLENDED AREA WITH BMS95-2, TYPE 10R3. INSTALL WET USING BMS5-95 SEALANT AND BAC30NW36. TST: 150,026.39 HOURS. CYCLES, 5,412. (X) 2 L 7 2 4F RT A2NM 1997013000330 19970130 00330 NM 1997 1 30 AALA961796 1 19961120 A 5311 141N8312 FRAME BOEING 757 757223 1384957 NM BS 377.7 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 661AA 25295 AFW - FUSELAGE FRAME AT 377.7 HAS CORROSION REMOVAL ON WEB ON FORWARD SIDE. MATERIAL REMAINING IS BEYOND SRM ALLOWABLE LIMITS. REPAIR PER MRB 757-1020. TST: 15,026.39 HOURS. CYCLES, 5,412. (X) 2 L 7 2 4F RT A2NM 1997013000331 19970130 00331 NM 1997 1 30 AALA961798 1 19961126 A 5315 141N5131 FLOOR BEAM BOEING 757 757223 1384957 NM BS 412-419 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 661AA 25295 AFW - FLOOR BEAM AT STA 412 TO STA 419 AT RBL 45 HAS GOUGE BLENDED. MATERIAL REMAINING IS BEYOND SRM ALLOWABLE LIMITS. REPAIR PER MRB 757-1025. TST: 15,026.39 HOURS. CYCLES, 5,412. (X) 2 L 7 2 4F RT A2NM 1997013000332 19970130 00332 NM 1997 1 30 AALA961799 1 19961120 A 5315 141N5113 FLOOR BEAM BOEING 757 757223 1384957 NM BS 377 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 661AA 25295 AFW - FLOOR BEAM AT STA 3877 HAS CORROSION REMOVAL ON UPPER SURFACE. MATERIAL REMAINING IS BEYOND SRM LIMITS. REPAIR P ER MRB 757-1014. TST: 15,056.39 HOURS. CYCLES, 5,412. (X) 2 L 7 2 4F RT A2NM 1997013000333 19970130 00333 NM 1997 1 30 AALA961801 1 19961121 A 5320 146N8522 SILL BOEING 757 757223 1384957 NM CARGO DOORWAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 661AA 25295 AFW - LOWER SILL INNER CHORD HAS CORROSION REMOVAL ON UPPER AND LOWER SURFACES. MATERIAL REMAINING IS BEYOND ALLOWABLE SRM LIMITS. REPAIR PER MRB 757-1023. TST: 15,026.39 HOURS. CYCLES, 5,412. (X) 2 L 7 2 4F RT A2NM 1997013000334 19970130 00334 NM 1997 1 30 AALA961802 1 19961122 A 5330 144N3100 SKIN BOEING 757 757223 1384957 NM BS 1162 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 661AA 25295 AFW - CORROSION BLENDED FROM CROWN SKIN AT 2 AFT MOUNT HOLES FOR THE ADF ANTENNA. MATERIAL REMAINING IS BEYOND ALLOWABL E SRM LIMITS. REPAIR PER MRB 1022. TST: 15,026.39 HOURS. CYCLES, 5,412. (X) 2 L 7 2 4F RT A2NM 1997013000335 19970130 00335 NM 1997 1 30 AALA961803 1 19961120 A 5315 141N5810 FLOOR BEAM BOEING 757 757223 1384957 NM BS 310 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 661AA 25295 AFW - FLOOR BEAM AT STA 310 HAS CORROSION REMOVAL ON UPPER SURFACE. MATERIAL REMAINING IS BEYOND SRM LIMITS. REPAIR PE R MRB 757-1019. TST: 15,026.39 HOURS. CYCLES, 5,412. (X) 2 L 7 2 4F RT A2NM 1997013000337 19970130 00337 CE 1997 1 30 97ZZZX490 1 19961201 A 3260 62083162 DIODE CESSNA 525 525 2076601 CE GEAR IND FAILED A FUBA K NONE O OTHER NR NOT REPORTED 1 NE 03 472SW 5250033 DIODE DRO26 FAILED TO A SHORT. WITH LANDING RECOGNITION LIGHT IN 'LANDING' POSITION, CURRENT (20 AMPS) PASSED THROUGH DIODE DRO28 SWITCH S1066, CONNECTOR JI015/PI015 TO GROUND AT PB015. DAMAGE FOUND ON ALL WIRING AND DRO28. REPLACED DAM AGED PARTS AND WIRING. SUBMITTER RECOMMENDS INSTALLING FUSEABLE LINK RATED AT 5 AMPS ACROSS (A2) TO (X1) JUMPER OF RELA YS RELATED TO LANDING AND RECOGNITION SYSTEM. 1 L 7 2 4F RT A1WI 1997013000350 19970130 00350 WP 1997 1 30 IXXA9700006 1 19961110 A 5313 56153282 LONGERON DOUG DC8 DC862 3021970 WP RT MLG WW CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 21CX 11474 45955 DURING ROUTINE C-CHECK INSPECTION, LONGERON 24 RIGHT WAS FOUND TO BE CRACKED IN TWO PLACES ADJACENT TO THE BATHTUB FITTI NG AT FUSELAGE STATION 870. THE CRACKS WERE STOP DRILLED, REPAIR DOUBLERS FABRICATED AND INSTALLED IN ACCORDANCE WITH D OUGLAS STRUCTURAL REPAIR MANUAL 53-2-2 AND 51-1-20D. 2 L 7 4 4F 4A25 1997013000351 19970130 00351 WP 1997 1 30 IXXA9700007 1 19961122 A 5315 2614462 FLOORBEAM DOUG DC8 DC862 3021970 WP BS 226-270 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 21CX 11474 45955 DURING ROUTINE C-CHECK INSPECTION, FLOORBEAM BETWEEN FUSELAGE STATION 226 AND 270 WAS FOUND TO BE CRACKED. REPAIR OF TH E FLOORBEAM WAS ACCOMPLISHED BY FABRICATING AND INSTALLING REPAIR DOUBLERS IN ACCORDANCE WITH FAA DER APPROVED SKETCH B6 8-R29 AND THE DOUGLAS STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F 4A25 1997013000352 19970130 00352 WP 1997 1 30 IXXA9700008 1 19961110 A 5743 5611425503 FITTING DOUG DC8 DC862 3021970 WP LT MLG CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 21CX 3273 45955 DURING ROUTINE C-CHECK INSPECTION, THE LEFT MAIN LANDING GEAR ATTACH FITTING WAS FOUND TO BE CRACKED. THE ATTACH FITTIN G WAS REPLACED IN ACCORDANCE WITH THE DOUGLAS REPLACEMENT GUIDE AND SRM 51-1-21. 2 L 7 4 4F 4A25 1997013000353 19970130 00353 WP 1997 1 30 IXXA9700009 1 19961110 A 5743 5611425504 FITTING DOUG DC8 DC862 3021970 WP RT MLG CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 21CX 3273 45955 DURING ROUTINE C-CHECK INSPECTION, THE RIGHT MAIN LANDING GEAR ATTACH FITTING WAS FOUND TO BE CRACKED. THE ATTACH FITTI NG WAS REPLACED IN ACCORDANCE WITH THE DOUGLAS REPLACEMENT GUIDE AND SRM 51-1-21. 2 L 7 4 4F 4A25 1997013000365 19970130 00365 WP 1997 1 30 CALA9700097 1 19961203 A 5541 RIBS DOUG DC9 DC932 3022066 WP RUDDER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17531 45847 INSPECTION FOUND TWO RUDDER RIBS CRACKED. THE CRACKS WERE .25 INCH LONG. THE RIBS WERE REMOVED AND REPLACED IAW EA 554 0-01019 AND SRM 55-40-0 AND 55-40-1. 2 L 7 2 4F A6WE 1997013000454 19970130 00454 SW 1997 1 30 97ZZZX526 1 19960928 A 7712 31010612 SENSOR BODY ALIDSIGNAL MTSBSI MU2 MU2B30 5780410 SW ENG GR BOX BROKEN A H2OA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 GL 05 618BB 533 DURING THE AFTER TAKEOFF CLIMB, AND IMMEDIATELY AFTER GEAR RETRACTION THE ENGINE FLAMED OUT. THE TORQUE SENSOR BODY FAI LED AROUND THE DRIVE GEAR FOR THE FUEL CONTROL UNIT AND AROUND THE RETAINING BOLTS. ONE TORQUE SENSOR RETAINING BOLT WA S FOUND AT THE BOTTOM OF THE GEARBOX CASE. S.O.A.P. RECEIVED 2 DAYS PRIOR TO ACCIDENT INDICATED MAGNESIUM FLAKES AND RE QUESTED RESAMPLE IN 25 HRS. 1 H 7 2 3T A2PC 1997013000455 19970130 00455 EA 1997 1 30 CA960827004 2 19960617 A 7260 3011405 SHAFT INPUT DHAV DHC6 DHC6200 EA PWA PT6 PT6A20 52043 EA ACCESSORY GEARBX DECOUPLED W A E A ENGINE SHUTDOWN UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 CA PCE21116 (CAN) DURING CLIMBOUT AFTER TAKEOFF THE #2 ENGINE STOPPED WITHOUT WARNING. ENGINE FAILURE DRILLS WERE CARRIED OUT & AIRC RAFT RETURNED TO POINT OF DEPARTURE. POST FLIGHT INSPECTION REVEALED METAL FLAKES IN THE OIL FILTER & A GRATINGSOUND FRO M THE ACCESSORY GEARBOX (AGB). THE AGB WAS REMOVED & THE INPUT COUPLING SHAFT WHICH COUPLES THE COMPRESSOR TO THE ACCESS ORY GEARBOX WAS FOUND TO BE DECOUPLED CAUSING SEVERE DAMAGE TO THE INPUT GEARSHAFT & ITS SUPPORT BEARING IN THE AGB HOUS ING. THE DECOUPLING WAS A RESULT OF THE BALL LOCK FEATURE BEING NOT PROPERLY LCOKED AT A PREVIOUS SHOP VISIT FOR REPLACE MENT OF THE STARTER GENERATOR GEARSHAFT. 1 H 7 2 3T 3 T A9EA E4EA 1997013000456 19970130 00456 NM 1997 1 30 CA960827007 1 19960813 A 5270 BULB BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE EE DOOR WARN BURNT W A UNSCHED LANDING O OTHER CL CLIMB 1 CA 667246 (CAN) AIRCRAFT WOULD NOT PRESSURIZE ON TAKEOFF. FOUND E & E DOOR OPEN, DOOR CLOSED. FOUND DOOR INDICATION LIGHT ON FLIGH T DECK BRUNED OUT. REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1997013000457 19970130 00457 NM 1997 1 30 CA960827008 1 19960813 A 2613 WIRE BOEING 737 7372A9C 1384495 NM PWA JT8 JT8D9A 52048 NE OVERHEAT DETECT SHORTED W A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CA P674318B (CAN) LH WING BODY OVERHEAT LIGHT STARTED TO FLICKER, AIRCRAFT DIVERTED. WIRE HAD CHAFED THROUGH AND WAS SHORTING OUT IN TERMITTENTLY. WIRE CONNECTED TO D866 OF SENSING ELEMENT M276 "OVHT DET SECTION 58" AT THE APU SHROUD AREA. REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1997013000458 19970130 00458 EA 1997 1 30 CA960827009 1 19960820 A 2820 82821015003 TUBE ASSEMBLY DHAV 82821001001 DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE SPOT WELD CRACKED W A K NONE K FLUID LOSS IN INSP/MAINT 1 CA 11720 0 123018 (CAN) FUEL LEAK NOTED FROM REFUEL/DEFUEL LINE SHROUD DRAIN IN RIGHT HAND NACELLE. PRESSURE DEFUEL TUBE ASSEMBLY LOCATED BELOW R/H EXHAUST SHROUD FOUND LEAKING BETWEEN INNER AND OUTER TUBE. OUTER TUBE IS WELDED TO INNER TUBE WHICH CONTAINS F UEL. OUTER TUBE IS INTENDED TO DRAIN LEAKAGE OVERBOARD. FUEL LEAKED INTO OUTER TUBE FROM A CRACKED INNER TUBE SPOT WELD AND INTO A FLEX. FUEL SHROUD P/N ASC427-2, WHICH IS ATTACHED TO OUTER TUBE. FLEX TUBE WAS DETERIORATED AND FUEL LEAKED B ELOW R/H EXHAUST SHROUD. TUBE ASSEMBLY, AND FLEX SHROUD REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1997013000459 19970130 00459 EA 1997 1 30 CA960827010 1 19960825 A 7830 1267586 PDU CNDAIR CL600 CL6002A12 1900304 EA GE CF34 CF341A NE INTERNAL FAILED W O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 CA 350139 (CAN) PDU WOULD NOT MAINTAIN INITIAL RIGGING AS PER MM 1 1/3 TURNS ON DIRECTIONAL CONTROL VALVE GAP (0.315 +/- 0.015). F AILED RESET OF DIRECTIONAL CONTROL VALVE (SHOP AIR). 2 L 7 2 4F 4 F RT A21EA E15NE 1997013000460 19970130 00460 SW 1997 1 30 CA960827011 1 19960827 A 6210 206010200133 BLADE BELL 206010200133 BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL M/R TIP TE BULGED W K NONE O OTHER IN INSP/MAINT 1 CA 127 A2923 820928CAE (CAN) ON INSPECTION, BULGE FOUND IN BLADE SKIN APPROXIMATELY 12 INCHES LONG X 2.5 INCHES WIDE X 0.5 INCH HIGH NEAR TRAIL ING EDGE OF BLADE AT THE TIP. 1 G 7 1 3U 3 U H2SW E4CE 1997013000461 19970130 00461 SW 1997 1 30 CA960827012 1 19960827 A 6210 206010200133 BLADE BELL 206010200133 BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL M/R PEELING PAINT W K NONE O OTHER IN INSP/MAINT 1 CA 127 A2618 820928CAE (CAN) EXCESSIVE PEELING OF PAINT ON THE UNDERSIDE OF THIS BLADE NEAR THE TIP. THIS BLADE ALSO PRODUCES WHISTLING NOISES THAT CAN BE HEARD FROM INSIDE THE CABIN DURING ROTOR RUNDOWN AFTER THE ENGINE IS STOPPED. 1 G 7 1 3U 3 U H2SW E4CE 1997013000463 19970130 00463 EA 1997 1 30 CA960827015 2 19960726 A 7322 60260 BUSHING MARVELSCHEB MA3PA10526 CESSNA 150 152 2071835 CE LYC O235 O235L2C 41505 EA MCAULY 1A103 1A103TCM GL CARB THROT SHAFT LOOSE W K NONE R PARTIAL RPM/PWR LOSS IN INSP/MAINT 1 CA 1619 OT31722MFV L1524715 776458 (CAN) HESITANT ACCELERATION OF THE ENGINE CAUSED BY THE PLAY IN THE BUSHING ALLOWING FUEL LEAKAGE WHEN FULL POWER WAS AP PLIED FROM IDLE. THIS CONDITIONN WAS NOTICED DURING INSPECTION OF THE OPERATION OF THE THROTTLE, THE LOSS OF FUEL WAS TH ROUGH THE THROTTLE BUSHING. THE CARBURETOR WAS SENT FOR REPAIR. 1 H 7 1 3O 3 O NT 3A19 E223 5 N P50GL 1997013000464 19970130 00464 EA 1997 1 30 CA960827016 2 19960809 A 8530 E5307A7 VALVE CESSNA 182 R182 2072734 CE LYC O540 O540J3C5 41532 EA MCAULY 2D34C B2D34C214 GL #4 CYL EXH STEM STICKING W K NONE O OTHER IN INSP/MAINT 1 CA 1292 L1959240A 786158 (CAN) ON INSPECTION THERE WAS NO COMPRESSION ON #4 CYLINDER. THE CYLINDER WAS REMOVED AND THE EXHAUST VALVE GUIDE WAS ST UCK AND THE VALVE WAS IN THE FULL OPEN POSITION. THE CYLINDER WAS REPLACED. 1 H 7 1 3O 3 O RT 3A13 E295 5 C P7EA 1997013000465 19970130 00465 EA 1997 1 30 CA960827017 2 19960808 A 8530 E5307A7 VALVE CESSNA 182 R182 2072734 CE LYC O540 O540J3C5 41532 EA MCAULY 2D34C B2D34C214 GL #3 CYL EXH WARPED SEAT W K NONE O OTHER IN INSP/MAINT 1 CA 1976 1976 L1990440A 880728 (CAN) ON A 200 HOUR INSPECTION #3 AND #4 CYLINDERS HAD NO COMPRESSION. THE VALVES WERE NOT SEATING PROPERLY. DUE TO THE HIGH TIME OF THE ENGINE THE ENGINE WAS REPLACED. 1 H 7 1 3O 3 O RT 3A13 E295 5 C P7EA 1997013000466 19970130 00466 EA 1997 1 30 CA960827018 2 19960811 A 7322 3024973 COUPLING DRIVE BEECH 90 65A90 1152908 CE PWA PT6 PT6A20 52043 EA FUEL CONTROL SHEARED W A E UNSCHED LANDING ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 CA (CAN) THE PILOT WAS FORCED TO SHUT THE ENGINE DOWN BECAUSE HE WAS UNABLE TO CONTROL IT. THE DEFECT WAS CAUSED BY THE BRE AKING OF THE FUEL CONTROL AND FUEL PUMP COUPLING. 1 L 7 2 3T 3 T 3A20 E4EA 1997013000468 19970130 00468 1997 1 30 CA960827101 4 19960525 A 2210 2588880901 CARD HONEYWELL 2588880901 BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE YAW DAMPER CORRODED W H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED AP APPROACH 1 CA 21739 1280838 702782 (CAN) DURING APPROACH WITH FLAPS AT 40, AIRCRAFT YAWED UNTIL YAW DAMPER TURNED OFF. AUTOPILOT WAS OFF, ALTITUDE 1200 AGL , WIND 10 MPH, TEMP 18C, REPLACED COUPLER. EXTENSIVE CORROSION ON ANODE CONNECTOR LUG FOR CR3 ON A1A1 CARD. 2 L 7 2 4F 4 F A16WE E2EA 1997013000469 19970130 00469 1997 1 30 CA960827102 4 19960512 A 2210 2588880901 CARD HONEYWELL 2588880901 BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE YAW DAMPER CORRODED W C D ABORTED TAKEOFF RETURN TO BLOCK F FLT CONT AFFECTED TO TAKEOFF 1 CA 53598 0831500 702782 (CAN) TAKEOFF REJECTED DUE TO VIOLENT LATERAL MOVEMENT. YAW DAMPER REPLACED. VISUAL INSPECTION OF A1A1 YAW INTERLOCK CAR D REVEALED EXTENSIVE CORROSION ON ANODE CONNECTOR LUG FOR CR3. REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1997013000476 19970130 00476 NE 1997 1 30 CA960828005 2 19960605 A 7314 FUEL PUMP DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE #2 ENGINE LOOSE GEARS W E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 CA 20289 2680 120396 (CAN) DURING CRUISE THE #2 ENGINE FUEL PRESSURE LIGHT AND ENGINE MANUAL LIGHT CAME ON. THIS WAS FOLLOWED BY A POWER ROLL BACK AND AN IN FLIGHT SHUTDOWN. POST FLIGHT INSPECTION REVEALED THE FUEL PUMP INTERNAL GEARS WERE LOOSE WHICH CAUSED TH E ROUGH RUNNING. THE PUMP HAS BEEN RETURNED TO THE VENDOR. 2 H 7 2 4T 4 T RT A13NM E20NE 1997013000481 19970130 00481 CE 1997 1 30 CA960909001 1 19960905 A 2750 JAELEACH RELAY MTSBSI MU2 MU2B35 5780411 CE GARRTT TPE331 TPE3316252M 01514 NE FLAP CONTROL BURNT CONTACTS W A UNSCHED LANDING F O FLT CONT AFFECTED OTHER TO TAKEOFF 1 CA 8492 549 P20148C (CAN) THE CREW SELECTED 20 DEGREES FOR FLAPS AND NOTED THE SETTING GOING TO 40 DEGREES. A CIRCUIT WAS CARRIED OUT AND TH E AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. INSPECTION FOUND THE CONTACTS OF THE FLAP MOTOR WERE STUCK CLOSED, WHICH DRO VE THE FLAPS TO 40 DEGREES AND WOULD NOT RESPOND TO THE UP COMMAND. THE RELAY WAS REPLACED AND SERVICE CHECKS OF THE FLA P SYSTEM CARRIED OUT AND THE AIRCRAFT RETURNED TO SERVICE. 1 H 7 2 3T RT A10SW E2WE 1997013000482 19970130 00482 SW 1997 1 30 CA960909002 1 19960822 A 6210 A10231 BLADE BELL 204011250001 BELL 205 205A1 1181414 SW LYC T53 T5313B 41549 NE STA 203.5 CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 2338 A10231 LEO7506 (CAN) BLADE TOP SKIN CRACKED AT STATION 203 5 CRACKED APPROXIMATELY 6 INCHES FROM SPAR REARWARD 1 G 7 1 4U 4 U H1SW E17EA 1997013000483 19970130 00483 SO 1997 1 30 CA960909003 1 19960828 A 2120 2859702 AIR DIST BOX PIPER 2859702 PIPER PA23 PA23250 7102308 SO LYC O540 IO540C4B5 41532 EA AFT BOTTOM GROOVED W K NONE O OTHER IN INSP/MAINT 1 CA 4414 4414 L1240040A (CAN) ELEVATOR CABLES GROOVED THE AIR DISTRIBUTION BOX. THE CONTROL CABLES WERE INSTALLED CORRECTLY AS PER PIPER PARTS B OOK. THE CORRECTIVE ACTION WAS TO CUT BACK THE BOX AS REQUIRED FOR CLEARANCE AND WELD IN A NEW BOTTOM FOR THE AIR BOX. 1 L 7 2 3O 3 O 1A10 1E4 1997013000486 19970130 00486 SW 1997 1 30 CA960909008 1 19960824 A 2436 REGULATOR BELL BELL 204 204B 1181404 SW LYC T53 T5313B 41549 NE DC SYS MALFUNCTION W K NONE O OTHER IN INSP/MAINT 1 CA LE07531 (CAN) ON STARTUP, LOADMETER SPIKES WHEN GENERATOR TURNED ON, THEN LOAD STAYS HIGHER THAN NORMAL FOR A LONG TIME. VOLTAGE REGULATOR REPLACED. 1 G 7 1 4U 4 U H1SW E17EA 1997013000487 19970130 00487 EA 1997 1 30 CA960909009 2 19960823 A 8550 LW11847 TUBE DRAIN CESSNA 177 177RG 2073709 CE LYC O360 IO360A1B6 41514 EA MCAULY 2D34C B2D34C207 GL #2 CYLINDER CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 1868 L1764851A 774491 (CAN) OIL LEAK WAS NOTED ON #2 CYLINDER ON INSPECTION. FLARE ON OIL RETURN TUBE FOUND TO BE CRACKED APPROXIMATELY 2/3 AR OUND ITS CIRCUMFERENCE. 1 H 7 1 3O 3 O A20CE 1E10 5 C P7EA 1997013000488 19970130 00488 GL 1997 1 30 CA960909010 3 19960822 A 6111 F847SR BLADE PIPER PA36 PA36300 7103612 SO LYC O540 IO540K1G5 41532 EA HARTZL HCC2Y HCC2YK1 GL 32" STATION TIP SEPARATED W A A UNSCHED LANDING D E INFLIGHT SEPARATION VIBRATION/BUFFET CR CRUISE 1 CA 565 L1741948A CH6831 (CAN) BLADE TIP SEPARATED AT THE 32" STATION DURING FLIGHT. 1 L 7 1 3O 3 O A10SO 1E4 5 C P920 1997013000489 19970130 00489 SO 1997 1 30 CA960909011 1 19960813 A 2434 30E2041A GENERATOR GULSTM G159 G159 3952202 SO RROYCE DART DART5298X 54507 EU R/H DC SYS HOT W H E A DEACTIVATE SYST/CIRCUITS ENGINE SHUTDOWN UNSCHED LANDING J M WARNING INDICATION OVER TEMP CR CRUISE 1 CA 796 16272 (CAN) WHILE IN CRUISE FLIGHT, THE RIGHT HAND GENERATOR LIGHT CAME ON, FOLLOWED BY RIGHT HAND GENERATOR HOT LIGHT. THE EN GINE WAS SECURED AND THE AIRCRAFT RETURNED TO THE AIRPORT FOR AN UNEVENTFUL LANDING. THE GENERATOR WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T 1A17 E297 1997013000492 19970130 00492 EU 1997 1 30 CA960909015 1 19960806 A 2432 23531 BATTERY SAFT 23531 FOKKER F28 F28MK1000 4990808 EU NR 1 OVERHEAT W A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 CA 0533 (CAN) ON DEPARTURE AIRCRAFT EXPERIENCED #1 BATTERY OVERHEAT INDICATION. REPLACED. 2 L 7 2 4F RT A20EU 1997013000493 19970130 00493 EU 1997 1 30 CA960909016 1 19960805 A 2131 10264411 CONTROLLER AIRESEARCH 10264411 FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU CABIN PRESS FAILURE W O OTHER O OTHER CR CRUISE 1 CA 39125 9077 (CAN) AIRCRAFT ENCOUNTERED PRESSURIZATION PROBLEMS SPIKING UP TO 2000 FEET MIN. IN ASSOCIATION WITH POWER LEVER MOVEMENT . HIGH BLEED CYCLING ON AND OFF. TURNING RATE KNOB TO MINIMUM HAD NO EFFECT. PRESSURE CONTROLLER REPLACED. 2 L 7 2 4F 4 F RT A20EU E2EU 1997013000495 19970130 00495 NM 1997 1 30 CA960909018 1 19960815 A 3230 DSCZ52B40124 LINE DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE DRAG STRUT CRACKED W A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CL CLIMB 1 CA 17765 17765 123073 (CAN) AFTER TAKEOFF, WHEN GEAR SELECTED UP IT DID NOT FULLY RETRACT AND THE GEAR DOORS REMAINED OPEN. THEN ALL LIGHTS AS SOCIATED WITH #2 HYDRAULIC SYSTEM FAILURE CAME ON, AND #2 HYDRAULIC INDICATOR DROPPED TO ZERO. AIRCRAFT RETURNED HOME AN D LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A CRACKED HYDRAULIC LINE AT NOSE DRAG STRUT ACTUATOR. 2 H 7 2 4T 4 T RT A13NM E20NE 1997013000496 19970130 00496 NM 1997 1 30 CA960909019 1 19960817 A 7603 SWITCH ARM DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE CONDITION LEVER BROKEN W C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CA 120467 (CAN) ON TAKEOFF ROLL, WHEN POWER APPLIED THE TAKEOFF WARNING HORN SOUNDED. TAKEOFF WAS ABORTED. MAINTENANCE FOUND THE # 2 CONDITION LEVER ANGLE MICRO SWITCH ARM BROKEN. SWITCH REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1997013000497 19970130 00497 EU 1997 1 30 CA960909020 1 19960809 A 2150 6837204 ACM FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU NR 1 CABIN SMOKE W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA 9516 (CAN) ON CLIMB OUT CREW REPORTED SMOKE IN CABIN. FOUND OIL AT #1 AIR CYCLE MACHINE. REPLACED. 2 L 7 2 4F 4 F RT A20EU E2EU 1997013000499 19970130 00499 SO 1997 1 30 CA960909022 1 19960822 A 7810 LW16620 EXHAUST PIPE PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA #2 ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1369 L288461A (CAN) DURING INSPECTION THE LEFT ENGINE INBOARD EXHAUST PIPE WAS FOUND CRACKED AT THE RADIUS ATTACHMENT FLANGE. THE "V" BAND COUPLING HAD TO BE REMOVED TO SEE THE CRACK. THE CRACK WAS APPROXIMATELY 1.5 INCHES LONG. 1 L 7 2 3O 3 O A20SO E14EA 1997013000500 19970130 00500 SW 1997 1 30 CA960909023 1 19960824 A 5320 205031025001 FITTING 205030845131 BELL 205 205A1 1181414 SW LYC T53 T5313B 41549 NE AFT HOLE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA LE07641 (CAN) LIFT BEAM ASSEMBLY FITTING CRACKED AT THE HOLE ON THE AFT EAR. 1 G 7 1 4U 4 U H1SW E17EA 1997013000501 19970130 00501 EU 1997 1 30 CA960909024 1 19960826 A 2612 D891N FIRE WIRE BRAERO 748 HS7482A 4231001 EU #1 ENGINE SHORTED W A E F UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 CA (CAN) ON CLIMB OUT THE PILOT RECEIVED A FIRE INDICATION ON #2 ENGINE. THE ENGINE WAS SECURED AND BOTH FIRE BOTTLES WERE ACTIVATED. THE AIRCRAFT RETURNED TO BASE. POST FLIGHT INSPECTION FOUND NO EVIDENCE OF FIRE, BUT FOUND A SHORTED FIRE DET ECTION WIRE ABOVE THE REAR TURBINE. THE FIRE DETECTION WIRE AND BOTH FIRE BOTTLES WERE REPLACED AND THE AIRCRAFT RETURNE D TO SERVICE. 2 L 7 2 3T A24EU 1997013000503 19970130 00503 NM 1997 1 30 CA960909028 1 19960829 A 2612 87823802 CONNECTOR BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE NR 1 FIRE WIRE BROKEN W B E F EMER. DESCENT ENGINE SHUTDOWN ACTIVATE FIRE EXT. J WARNING INDICATION DE DESCENT 1 CA 700329 (CAN) ENROUTE TOP OF DESCENT #1 ENGINE FIRE WARNING SOUNDED. FIRE DRILL COMPLETED, BOTTLES FIRED, LIGHT ON. BELL AND LIG HT INITIALLED CANCELLED WHEN FLIGHT IGNITION WAS SELECTED. EMERGENCY LANDING. #1 FIRE WIRE HARNES FAULTY. 2 L 7 3 4F 4 F RT A3WE E2EA 1997013000510 19970130 00510 WP 1997 1 30 WTAA960223 2 19961227 A 7200 ENGINE BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110U 01514 WP RIGHT FAILED A WTAA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 17 423UE 799 P63299 IYK - RIGHT ENGINE LOST POWER ON CLIMB-OUT. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT ENGINE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A21EU E4WE 1997013000511 19970130 00511 EU 1997 1 30 WTAA960222 1 19961227 A 5280 GEAR DOOR BAG JETSTM JETSTM3101 1500215 EU RT MLG BIRD STRIKE A WTAA O OTHER C F.O.D. LD LANDING 1 WP 17 420UE 788 VIS - BIRD STRIKE TO RIGHT MAIN GEAR DOOR ON LANDING. AIRCRAFT FERRIED TO FAT. MAINTENANCE INSPECTED RIGHT MAIN GEAR D OOR FOR DAMAGE. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1997013000512 19970130 00512 EU 1997 1 30 WTAA960218 1 19961213 A 3350 D46301001 CAP PANEL BAG JETSTM JETSTM3101 1500215 EU COCKPIT FAILED A WTAA K NONE L NO TEST NR NOT REPORTED 1 WP 17 429UE 807 SNA - EMERGENCY LIGHTS REPORTED INOPERATIONAL. AIRCRAFT FERRIED TO LAX. MAINTENANCE REPLACED CAP PANEL. OPERATIONAL C HECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1997013000513 19970130 00513 EU 1997 1 30 WTAA960216 1 19961213 A 3350 311701 BATTERY PACK BAG JETSTM JETSTM3101 1500215 EU CABIN DISCHARGED A WTAA K NONE L NO TEST IN INSP/MAINT 1 WP 17 429UE 807 LAX - EMERGENCY LIGHTS REPORTED INOPERATIONAL. MAINTENANCE REPLACED FOUR EMERGENCY LIGHT BATTERY PACKS. EMERGENCY LIGH TS OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1997013000514 19970130 00514 SO 1997 1 30 WTAA960213 1 19961211 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A WTAA K NONE L NO TEST IN INSP/MAINT 1 WP 17 216YV 120216 LAX - AFT EMERGENCY LIGHTS REPORTED INOPERATIONAL. MAINTENANCE REPLACED AFT EMERGENCY BATTERY PACK. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1997013000515 19970130 00515 SO 1997 1 30 WTAA960214 1 19961212 A 5270 MS250851 SWITCH EMB 120 EMB120RT SO PAX DOOR OUT OF ADJUST A WTAA K NONE N FALSE WARNING CR CRUISE 1 WP 17 453UE 120148 SFO - FORWARD DOOR LIGHT INTERMITTENTLY ON IN FLIGHT. MAINTENANCE ADJUSTED MICROSWITCH ON DOOR. OPERATIONAL CHECK SATI SFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1997013000517 19970130 00517 1997 1 30 WRLA96057 4 19961226 A 2230 AUTO THROTTLE DOUG MD11 MD11 3023602 NM E/E COMPT MALFUNCTIONED A WRLA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 275WA 48631 DURING TAKEOFF ROLL, AT APPROX 35-40 KNOTS, FLIGHT CREW NOTED AUTO THROTTLE 'FAIL' ALERT FLASHED. FLIGHT CREW ELECTED T O TERMINATE TAKEOFF. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REP PERFORM RETURN TO SERVICE TES T ON AUTO THROTTLE SEVERAL TIMES, NO FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A22WE 1997013000518 19970130 00518 SO 1997 1 30 ASOA96055 1 19961224 A 3260 2050500101 PROX SWITCH EMB 120 EMB120RT SO NLG FAILED A ASOA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION LD LANDING 1 SO 11 243AS 120072 ABI-DFW - UPON LANDING IN DFW, NOSE WHEEL STEERING FAILED. SHORTLY AFTER, CABIN FILLED WITH SMOKE. CAPTAIN STOPPED A/C ON THE TAXIWAY AND EVACUTATED THE PASSENGERS. THE PASSENGERS WERE BUSSED TO THE GATE. UPON INSPECTION, FOUND THAT THE RIGHT AIR-GROUND PROX SWITCH HAD FAILED. THE CAPT SHUT OFF THE PACKS AND TAXIED THE A/C TO THE GATE. REMOVED AND REPLA CED RT MLG PROXIMITY SWITCH. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1997013000519 19970130 00519 WP 1997 1 30 97ZZZM87 1 19961230 A 2410 6882286 CSD DISCONNECT DOUG DC8 DC8F54 3021926 WP NR 3 ENG LEAKING A FXLA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 19 44UA 45932 45800 IN CLIMB-OUT OF MIA, EXPERIENCED OIL QTY LOSS ON NR 3 ENGINE. MADE PRECAUTIONARY SHUTDOWN. RETURNED AND LANDED MIA WIT HOUT INCIDENT. INSPECTION REVEALED NR 3 CSD CLUTCH LEAKING AT BASE. REPLACED CSD CLUTCH DISCONNECT ASSEMBLY AND RETURN ED AIRCRAFT TO SERVICE. (M) 2 L 7 4 4F 4A25 1997013000520 19970130 00520 NE 1997 1 30 EIAA96100 2 19961222 A 7261 704835 OIL LINE BOEING 747 747SR46 NM PWA JT9 JT9D7A 52054 NE NR 1 ENGINE CHAFFED A EIAA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 09 478EV 21033 JFK - DURING CRUISE FLT, NR 1 ENG OIL QTY DECREASED 3-4 QUARTS PER HOUR. SIX HOURS INTO FLIGHT AT PRECAUTIONARY SHUT DO WN OF ENGINE WAS PERFORMED. WINDMILLING OIL PRESSURE WAS 17-20 PSI WITH QTY READING 2 QUARTS. FOUND NR 1 ENGINE, NR 4 BEARING OIL SCAVANGER LINE CHAFFED. REPLACED OIL SCAVANGE LINE. (M) 2 L 7 4 4F 4 F A20WE E20EA 1997013000521 19970130 00521 WP 1997 1 30 EIAA96101 1 19961222 A 3222 59104475503 STRUT DOUG DC9 DC932F 3022067 WP NLG REQ'D SERVICE A EIAA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 935F 48710 47220 AFTER TAKEOFF, AIRCRAFT WOULD NOT SHIFT INTO FLIGHT MODE. LANDING GEAR DID RETRACT. SERVICED NOSE LANDING GEAR. (M) 2 L 7 2 4F A6WE 1997013000522 19970130 00522 WP 1997 1 30 EIAA96102 1 19961219 A 3230 RETRACT MECH DOUG DC9 DC933F 302207A WP LANDING GEAR LACK OF LUBE A EIAA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 945F 45479 47279 AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT DUE TO GROUND SHIFT. AFTER 5 MINUTES, GROUND SHIFT WORKED AND GEAR RETRAC TED NORMALLY. INSPECTED GROUDN SHIFT MECH AND CABLES, LANDING GEAR CONTROL VALVE AND CABLES. CLEANED AND LUBED CABLES SYSTEMS. (M) 2 L 7 2 4F A6WE 1997013000523 19970130 00523 WP 1997 1 30 EIAA96103 1 19961208 A 5330 SKIN DOUG DC9 DC915F 3022037 WP BS 642 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 916F 49919 47044 DURING C-CHECK INSPECTION, DISCOVERED EXFOLIATION CORROSION ON THE LOWER FUSELAGE SKIN AT BS 642, LONGERON 30, BL 0.0. A FFECTED AREA WAS TRIMMED TO REMOVE CORROSION. INSTALLED INTERNAL FINGER DOUBLERS AND EXTERNAL REPAIR DOUBLERS WET WITH SEALANT AND TOP COATED AS REQUIRED. ACCOMPLISHED IAW EIAA, ENGINEERING CHANGE/REPAIR AUTHORIZATION NR 916-53-016-2. (M ) 2 L 7 2 4F A6WE 1997013000524 19970130 00524 WP 1997 1 30 GAIA9644 1 19961210 A 5411 FRAME CVAC 440 440 2422902 WP LT NACELLE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 587CA 463 DURING C-CHECK INSPECTION, FOUND CORROSION ON THE INBOARD LEFT NACELLE FRAME AT STATION 150. THE ABOVE DAMAGE WAS REPAI RED IAW KHA. EA NR CV-54-31. BY SPLICING IN A NEW SECTION OF NACELLE FRAME. THE ABOVE EA NR CV-54-31 WAS (DER) APPROVE D ON FAA FORM 8110-3. (M) 2 L 7 2 4R 6A6 1997013000525 19970130 00525 WP 1997 1 30 GAIA9648 1 19961221 A 3260 H146 DOOR SWITCH DOUG DC9 DC915F 3022037 WP RT MLG FAILED A GAIA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 562PC 46092 47012 KHA - FLT 490 - CVG-ROC - WHILE IN CRUISE THE 'GEAR DOOR OPEN' LIGHT ILLUMINATED CREW PROCEEDED TO ROC AND USED ALTERNAT E GEAR EXTENSION PROCEDURES. DUE TO THE USEOF ALTERNATE GEAR EXTENSION PROCEDURES THE MAIN GEAR DOORS DRAGGED ON THE GR UOND CAUSING MINOR DAMAGE DURING LANDING. SPECIAL GEAR DOWN FERRIED TO YIP. INSPECTION REVEALED A FAULTY RT MLG DOOR S WITCH. REMOVED AND REPLACED DOOR SWITCH. REPAIRED DOOR MINOR DAMAGE PER SRM. AIRCRAFT RELEASED FOR FLIGHT. (M) 2 L 7 2 4F A6WE 1997013000526 19970130 00526 EU 1997 1 30 JBXA00035 1 19961224 A 2421 IDG FOKKER F28 F28MK0100 4990807 EU NR 2 INOPERATIVE A JBXA C D ABORTED TAKEOFF RETURN TO BLOCK G H J MULTIPLE FAILURE ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 SO 05 131ML 11323 RDU - FLT 005 - NR 1 FOUND AND NR 2 IDG FAULTED ON TAKEOFF OUT OF RDU. REMOVED AND REPLACED GPCU IAW AMM 24-41-01. OPS CHECK OF NR 1 IDG SYSTEM GOOD. NR 2 IDG INOP PLACED ON DMI PER MEL 24-21-3-2. (M) 2 L 7 2 4F RT 1997013000527 19970130 00527 NM 1997 1 30 HNAA9693380 1 19961213 A 5210 BOLT DHAV DHC8 DHC8102 2809003 NM AIRSTAIR OUT OF POSITION A HNAA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 EA 07 933HA 134 FLT 3147 - DCA-BWI - UPON LANDING IN BWI, THE AIRSTAIR DOOR WOULD NOT OPEN FROM THE INSIDE. FOUND BOLT FELL FROM AIRSTA IR HANDRAIL. SECURED HARDWARE FOR FORWARD DOOR SUPPORT. (M) 2 H 7 2 4T RT A13NM 1997013000528 19970130 00528 EA 1997 1 30 HNAA9690582 1 19961219 A 3260 UNSAFE LIGHT DHAV DHC7 DHC7102 2802708 EA NLG ILLUMINATED A HNAA O OTHER N FALSE WARNING CR CRUISE 1 EA 07 905HA 070 FLT 3281 - BWI-DCA - THE NOSE GEAR UNSAFE LIGHT ILLUMINATED IN FLIGHT. SELECTED GEAR DOWN AND GOT THREE GREEN DOWN AND LOCKED INDICATION. THE AIRCRAFT CONTINUED ON TO DCA AND LANDED WITHOUT INCIDENT. EVALUATION FLIGHT WAS SATISFACTORY. A T RON, INSPECTED NOSE LANDING GEAR FOR CONDITION AND NO DEFECTS NOTED. PERFORMED GEAR SWING OF NOSE LANDING GEAR SEVERA L TIMES, INDICATION NORMAL. (M) 2 H 7 4 4T A20EA 1997013000529 19970130 00529 NE 1997 1 30 HNAA9690683 2 19961222 A 7260 3037223 CARBON SEAL DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 ENGINE DAMAGED A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 906HA 31691 009 FLT 3221 - PHL-SBY - AT 1000 FEET ON CLIMB-OUT, THE NR 1 ENGINE OIL PRESSURE WARNING LIGHT CAME ON, OIL PRESSURE AT 20 P SI ON GAUGE. THE CREW SHUTDOWN THE NR 1 ENGINE AND RETURNED TO PHL AND LANDED WITHOUT INCIDENT. INSPECTED THE NR 1 ENG INE, NO METAL CONTAMINATION FOUND IN MAIN OR RGB FILTERS AND CHIP DETECTORS. SERVICED WITH 7 QUARTS OF OIL. LATER AT R ON MAINTENANCE, PERFORMED ENGINE OIL FILTER REMOVED AND REPLACED AND REPLACED FORWARD CENTRIFUGAL CARBON SEAL AS A PRECA UTION. (M) 2 H 7 2 4T 4 T RT A13NM E20NE 1997013000530 19970130 00530 1997 1 30 VTZA96426 3 19961205 A 6140 BETA LIGHT JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE ILLUMINATED A VTZA C E D ABORTED TAKEOFF ENGINE SHUTDOWN RETURN TO BLOCK G J X MULTIPLE FAILURE WARNING INDICATION ENGINE FLAMEOUT TO TAKEOFF 1 EA 27 324UE 41017 FLT 6267 - IAD-BTV - ABORTED TAKEOFF DUE TO LEFT AND RIGHT RED BETA LIGHT ILLUMINATED AND RIGHT OIL PRESSURE LIGHT ILLUM INATED. ENGINE SHUT DOWN AS A PRECAUTIONARY MEASURE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND RAN ENGINE AND INSPECTED BETA SYSTEM AND FOUND NO DEFECTS AND COULD NOT DUPLICATE. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1997013000531 19970130 00531 EU 1997 1 30 VTZA96424 1 19961205 A 5270 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGGAGE DOOR LACK OF LUBE A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 314UE 41027 FLT 6318 - ROA-IAD - ABORTED TAKEOFF DUE TO MAIN BAGGAGE DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE OPENED DMI 03841, MEL 52-3. MAINTENANCE CLOSED DMI 03841 BY CLEANING AND LUBING SWIT CHES AND ACTUATOR ARM. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1997013000532 19970130 00532 EU 1997 1 30 VTZA96439 1 19961213 A 2611 72111211000 SMOKE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU CARGO COMPT MALFUNCTIONED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 307UE 41021 FLT 6483 - IAD-CHS - DURING CLIMB, AN UNSCHEDULED LANDING DUE TO MAIN CARGO SMOKE WARNING LIGHT ILLUMINATED. AIRCRAFT R ETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED SMOKE DETECTOR, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1997013000533 19970130 00533 EU 1997 1 30 VTZA96438 1 19961214 A 2150 1718D000 ACM VLV JETAIR JETSTM JETSTM4101 1500501 EU RIGHT STUCK A VTZA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 306UE 41020 FLT 6297 - ORF-IAD - DURING TAXI, RETURNED TO GATE DUE TO RT DUCT O-TEMP WARNING LIGHT ILLUMINATED. MAINTENANCE INSPECT ED AND FREED STUCK ACM VALVE, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1997013000534 19970130 00534 1997 1 30 VTZA96437 4 19961213 A 6122 PROP GOV JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 306UE 41020 FLT 6508 - IAD-BOS - ABORTED TAKEOFF DUE TO LEFT ENGINE SLOW TO MAKE 100 PERCENT TORQUE AT 90 KNOTS, ONLY REACHED 91 PER CENT TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND ADJUSTED PROP GOV, OPS CHEC K OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1997013000535 19970130 00535 EU 1997 1 30 VTZA96436 1 19961210 A 2750 5148YMK83NP FLAP HANDLE BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILURE A A VTZA K NONE F FLT CONT AFFECTED AP APPROACH 1 EA 27 494UE 810 FLT 6224 - PHL-IAD - DURING APPROACH, EXPERIENCED A DISCREPANCY WITH THE FLAP SELECTOR SYSTEMS. FLAPS SELECTED NOT LOCK ING AT FLAPS 35 DEGREES. SELECTED 35 DEGREES, SELECTOR WENT FROM 35 DEGREES TO 20 DEGREES. AIRCRAFT LANDED AT IAD WITH NO INCIDENT REPORTED. MAINTENANCE TROUBLESHOT DISCREPANCY AND REMOVED AND REPLACED FAULTY FLAP HANDLE AND FUNCTIONALLY CHECKED SYSTEM IAW MX PROCEDURES. A/C WAS THEN RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1997013000536 19970130 00536 EU 1997 1 30 VTZA96435 1 19961209 A 3246 1855222 LOCKING PLATE BAG JETSTM JETSTM3201 1500217 EU NLG CRACKED A A VTZA K NONE O OTHER TX TAXI/GRND HDL 1 EA 27 485UE 901 FLT 6419 - BOS-JFK - AFTER LANDING, NOTIFIED BY RAMP PERSONNEL THAT THE LT NOSE WHEEL WAS MISSING FROM THE A/C. IAD MX WAS NOTIFIED, VIA MX CONTROL, AND THE REQUIRED MX TECHS AND MATERIAL WAS REPOSITIONED TO JFK TO INSPECT AND REPAIR THE A /C. AT JFK, BOTH NOSE TIRES AND AXLE WERE REPLACED. ALSO, A DETAILED INSPECTION OF THE SURROUNDING AREA AND THE PROPE R OP CHECK OF THE NLG RETRACTION SYSTEM WAS PERFORMED. A/C WAS THEN RELEASED FOR SERV. DURING THE INSPECT OF THE NOSE WHEEL, THAT WAS RECOVERED, IT WAS NOTICED THAT THE LOCKING PLATE FOR THE LT NOSE WHEEL WAS CRACKED WHICH WOULD HAVE CAUS ED THE WHEEL TO SEPARATE FROM THE A/C. (M) 2 L 7 2 4T RT A56EU 1997013000537 19970130 00537 EU 1997 1 30 VTZA96434 1 19961208 A 2435 23095002 STARTER JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE FAILED A VTZA D RETURN TO BLOCK M J OVER TEMP WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 308UE 41023 FLT 6490 - BOS-JFK - DURING TAXI OUT, EXPERIENCED A RT ENGINE HOT START. A/C RETURNED TO THE GATE WHERE THE MX TECHS TR OUBLESHOT THE DISCREPANCY AND FOUND THAT THE RT STARTER GEN HAD FAILED. MAINTENANCE REPLACED THE RT STARTER GENERATOR I AW ALL MAINTENANCE PROCEDURES. PERFORMED ENGINE STARTS WITH NO FURTHER PROBLEMS. A/C WAS THEN RELEASED AND APPROVED FO R RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1997013000538 19970130 00538 1997 1 30 VTZA96429 4 19961206 A 3418 C771076 LIFT TRANSDUCER BAG JETSTM JETSTM3201 1500217 EU LT WING FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 474UE 849 FLT 6196 - MDT-IAD - DURING FLIGHT, EXPERIENCED A LT STALL WARN AND STICK SHAKER ACTIVATION, A/C RETURNED. A/C WAS THEN FERRIED TO IAD, AFTER INSPECTED BY CONTRACT MX AND DETERMINATION THAT THE LT LIFT TRANSDUCER HAD FAILED. UPON ARRIVAL AT IAD, MX TECHNICIANS VERIFIED THAT THE LT LIFT TRANSDUCER WAS THE FAULT AND REMOVED, REPLACED AND TESTED THE TRANSDUCE R AND SYSTEM IAW THE J3200 MX PROCEDURES. A/C WAS THEN RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1997013000539 19970130 00539 1997 1 30 VTZA96428 4 19961206 A 3418 C771076 LIFT TRANSDUCER BAG JETSTM JETSTM3201 1500217 EU LT WING FAILED A VTZA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 492UE 790 FLT 6423 - IAD-ROC - DURING TAXI, EXPERIENCED A LT STALL SYSTEM THAT WOULD NOT TEST ON THE GROUND. A/C RETURNED TO THE GATE WHERE THE MX TECHS FOUND THE LT LIFT TRANSDUCER TO BE INOPERATIVE. REPLACED AND TESTED THE LT LIFT TRANSDUCER IAW MX PROCEDURES. A/C WAS THEN RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1997013000540 19970130 00540 EU 1997 1 30 VTZA96433 1 19961207 A 2150 ACM JETAIR JETSTM JETSTM4101 1500501 EU RIGHT STUCK A VTZA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 313UE 1718D000 41026 FLT 6538 - IAD-RIC - DURING TAXI OUT, EXPERIENCED A RT DUCT OVERTEMP LIGHT ILLUMINATION. AIRCRAFT RETURNED TO THE GATE WHERE THE MAINTENANCE TECHNICIANS TROUBLESHOT THE DISCREPANCY AND FOUND THAT THE RT AIR CYCLE MACHINE HAD BECOME STUCK. MAINTENANCE FREED THE AIR CYCLE MACHINE IAW WITH ALL MAINTENANCE PROCEDURES. AIRCRAFT WAS THEN RELEASED AND APPROVED F OR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1997013000541 19970130 00541 WP 1997 1 30 VTZA96432 2 19961206 A 7321 31059005 FUEL CONTROL JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE3311 01514 WP NR 1/NR 2 ENGINE OUT OF ADJUST A VTZA O OTHER J WARNING INDICATION LD LANDING 1 EA 27 324UE 41017 FLT 6426 - IAD-DTW - DURING LANDING, EXPERIENCED A NR 1 AND NR 2 RED BETA LIGHT DURING LANDING FLARE AT IAD. UPON FINAL ARRIVAL AT IAD, MX TECHNICIANS TROUBLESHOT THE DISCREPANCY AND FOUND THAT THE LT AND RT ENGINE FLIGHT IDLE FUEL FLOW SY STEM OF THE FUEL CONTROL UNITS NEEDED TO BE ADJUSTED. ADJUSTMENTS WERE MADE IAW WITH GARRETT AND JETSTREAM MAINTENANCE PROCEDURES. AIRCRAFT WAS THEN RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 3 T RT A41NM E3WE 1997013000542 19970130 00542 EU 1997 1 30 VTZA96431 1 19961207 A 5270 AIR132256 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGGAGE DOOR FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 317UE 41031 FLT 6532 - IAD-ORF - ABORTED TAKEOFF DUE TO A BAGGAGE DOOR LIGHT ILLUMINATION. AIRCRAFT RETURNED TO THE GATE WHERE THE MAINTENANCE TECHNICIANS TROUBLESHOT THE DISCREPANCY AND FOUND THAT THE BAGGAGE BAY DOOR MICROSWITCH HAD FAILED. OPENED A DEFERRED MAINTENANCE ITEM UNDER 52-3 IAW WITH DEFERRED MX PROCEDURES. MAINTENANCE CLOSED DMI 40824, BY INSPECTING BAG GAGE BAY DOOR, COULD NOT DUPLICATE FAULT. AIRCRAFT WAS THEN RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1997013000543 19970130 00543 NM 1997 1 30 TWRA96380 1 19961219 A 3350 3004181 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 267 21937 DURING DAILY CHECK, FOUND 4L MED UPPER BUSTLE EMERGENCY EVAC LIGHT INOP. REMOVED AND REPLACED BUSTLE LIGHT ASSEMBLY. O PS CHECK NORMAL PER MM 33-51-00 PAGE 501. (M) 2 L 7 4 4F A20WE 1997013000544 19970130 00544 NM 1997 1 30 TWRA96379 1 19961212 A 3350 S1356B37 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 13334 21937 DURING DAILY CHECK, FOUND CEILING EVAC LIGHT INOP AT ROW 30 ABC. REMOVED AND REPLACED LIGHT ASSEMBLY. OPS CHECK NORMAL PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1997013000545 19970130 00545 NM 1997 1 30 TWRA96337 1 19961017 A 5400 63B100471280 FITTING BOEING 747 747130 1384880 NM NR 3 PYLON CRACKED A TWRA K NONE O OTHER IN INSP/MAINT 1 EA 15 603FF 19746 NR 3 ENGINE LOWER FORWARD DIAGONAL BRACE FITTING, CRACKED AT REAR VERTICAL FLANGE. REPLACED DIAGONAL BRACE FITTING IAW SB 747-54-2062, SRM 51-30-02 AND EA 54-044-3. A/C RETURN TO SERVICE. (M) 2 L 7 4 4F A20WE 1997013000546 19970130 00546 NM 1997 1 30 TWRA96338 1 19961017 A 5412 65B904138 BULKHEAD BOEING 747 747130 1384880 NM NR 3 PYLON CRACKED A TWRA K NONE O OTHER IN INSP/MAINT 1 EA 15 603FF 19746 NR 3 ENGNIE PYLON REAR TORQUE BULKHEAD T-CHORD CRACKED THROUGH ON LEFT AND RIGHT SIDES APPROXIMATELY 60 TO 8 INCHES LONG IN RADIUS. REPLACED T-CHORD ASSEMBLY ON LEFT AND RIGHT SIDES, IAW SRM 51-10-01/51-30-02. (M) 2 L 7 4 4F A20WE 1997013000547 19970130 00547 NM 1997 1 30 97ZZZM88 1 19961017 A 5412 65B9041345 CHORD BOEING 747 747130 1384880 NM NR 3 PYLON CRACKED A TWRA K NONE O OTHER IN INSP/MAINT 1 EA 15 603FF 19746 NR 3 ENGNIE PYLON REAR TORQUE BULKHEAD T-CHORD CRACKED THROUGH ON LEFT AND RIGHT SIDES APPROXIMATELY 60 TO 8 INCHES LONG IN RADIUS. REPLACED T-CHORD ASSEMBLY ON LEFT AND RIGHT SIDES, IAW SRM 51-10-01/51-30-02. REFERENCE TWRA96338. 2 L 7 4 4F A20WE 1997013000553 19970130 00553 EU 1997 1 30 WTAA970003 1 19961230 A 2612 FIRE LIGHT BAG JETSTM JETSTM3101 1500215 EU RT ENGINE ILLUMINATED A WTAA K NONE N FALSE WARNING CR CRUISE 1 WP 17 401UE 729 SFO - RIGHT ENGINE FIRE DETECTION LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE TESTED RIGHT ENGINE FIRE DETECTION SYSTEM. S YSTEMS OPERATIONAL CHECK SATISFACTORY. COULD NOT DUPLICATE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1997013000554 19970130 00554 EU 1997 1 30 WTAA960221 1 19961218 A 3260 622800200 SWITCH BAG JETSTM JETSTM3101 1500215 EU RT MLG FAILED A WTAA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 WP 17 428UE 806 LAX - RIGHT MAIN GEAR RED INTRANSIT LIGHT INOPERATIONAL. MAINTENANCE REPLACED RIGHT MAIN UPLOCK TERMINAL ON MICROSWITCH . OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1997013000556 19970130 00556 SO 1997 1 30 WTAA970002 1 19961231 A 5101 STRUCTURE EMB 120 EMB120RT SO AIRFRAME BIRDSTRIKE A WTAA O OTHER C F.O.D. CL CLIMB 1 WP 17 251YV 120251 SMF - BIRD STRIKE AFTER TAKEOFF REPORTED. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAF T FOR DAMAGE, NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1997013000557 19970130 00557 SO 1997 1 30 WTAA970001 1 19961227 A 5246 12042953603 FUEL DOOR EMB 120 EMB120RT SO WING NOT LATCHED A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 17 216YV 120216 FAT - SERVICE LIGHT CAME ON DURING TAKEOFF. TAKEOFF ABORTED. MAINTENANCE FOUND OUTBOARD FUEL DOOR OPEN. INSPECTED AND RESECURED DOOR. GROUND CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1997013000558 19970130 00558 1997 1 30 USAASB96272 4 19961229 A 3417 HG480B42 AIR DATA COMP BOEING 737 7373B7 1384580 NM E/E COMP FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 516AU 31379 23702 TPA - FLT 1425 - DURING CLIMB, THE FIRST OFFICERS AIRSPEED INDICATION FAILED AND THE FIRST OFFICERS ALTIMETER READING WA S VERY LOW. FLIGHT RETURNED TO FIELD AT TPA. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT INCIDENT. MAINTE NANCE REMOVED AND REPLACED THE NR 2 AIR DATA COMPUTER PE MM 34-12-11. FUNCTIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1997013000559 19970130 00559 WP 1997 1 30 97ZZZM89 1 19961201 A 5330 SKIN DOUG DC6 DC6A 3021706 WP BS 843 CORRODED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 870TA 25799 45518 SKIN AT FORWARD EDGE OF FIRST EMERGENCY EXIT RIGHT SIDE F/S 843. REWORK, CORRODED AREA AND REPAIRED PER SRM 12-21. (M) 2 L 7 4 4R 6A3 1997013000560 19970130 00560 WP 1997 1 30 97ZZZM90 1 19961201 A 5330 SKIN DOUG DC6 DC6A 3021706 WP BS 640 CORROSION A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 870TA 25799 45518 FOUND CORROSION AT SKIN LAP AT FORWARD UPPER CORNER OF AFT ENTRY DOOR F/S 640. REWORKED CORRODED AREA. REPAIRED PER SR M 12-21. (M) 2 L 7 4 4R 6A3 1997013000561 19970130 00561 WP 1997 1 30 97ZZZM91 1 19961201 A 5330 SKIN DOUG DC6 DC6A 3021706 WP BS 6 CORROSION A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 870TA 25799 45518 FOUND CORROSION BETWEEN SKIN LAP FORWARD OF RIGHT WINDSHIELD STATION 6. REWORKED, IAW SRM 12-21. (M) 2 L 7 4 4R 6A3 1997013000562 19970130 00562 WP 1997 1 30 97ZZZM92 1 19961201 A 5330 SKIN DOUG DC6 DC6A 3021706 WP BS 66 CRACKED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 870TA 25799 45518 FOUND SKIN CRACKED, F/S 66 UPPER AFT EDGE OF RIGHT COCKPIT SLIDING WINDOW. REWORKED, IAW SRM 12-19. (M) 2 L 7 4 4R 6A3 1997013000563 19970130 00563 WP 1997 1 30 97ZZZM93 1 19961201 A 5330 SKIN DOUG DC6 DC6A 3021706 WP BS 58 CRACKED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 870TA 25799 45518 FOUND SKIN CRACKED, ABOVE RIGHT COCKPIT SLIDING WINDOW STATION 58. REWORKED, IAW SRM 12-21. (M) 2 L 7 4 4R 6A3 1997013000564 19970130 00564 WP 1997 1 30 97ZZZM94 1 19961201 A 5320 FITTING DOUG DC6 DC6A 3021706 WP BS 49 CORROSION A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 870TA 25799 45518 FOUND CORROSION AROUND FORWARD ENTRY DOOR HOLD OPEN FITTING F/S 49. REWORKED, REMOVED CORROSION, REPAIRED PER SRM 12-21 . (M) 2 L 7 4 4R 6A3 1997013000565 19970130 00565 WP 1997 1 30 97ZZZM95 1 19961201 A 5330 SKIN DOUG DC6 DC6A 3021706 WP BS 600-621 CORRODED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 870TA 25799 45518 FOUND CORRODED AROUND WINDOW PLUG LEFT SIDE FORWARD OF AFT ENTRY DOOR STATION 600-621. REWORKED, CORRODED AREA REPAIRED PER SRM 12-21. (M) 2 L 7 4 4R 6A3 1997013000566 19970130 00566 WP 1997 1 30 97ZZZM96 1 19961201 A 5330 SKIN DOUG DC6 DC6A 3021706 WP BS 780 CRACKED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 870TA 25799 45518 FOUND CRACKED SKIN AT MIDDLE FORWARD EDGE OF 2ND FROM LAST EMERGENCY EXIT, RIGHT SIDE STATION 780. REWORKED, CORRODED A REA REPAIRED PER SRM 12-19. (M) 2 L 7 4 4R 6A3 1997013000567 19970130 00567 WP 1997 1 30 97ZZZM97 1 19961201 A 5330 SKIN DOUG DC6 DC6A 3021706 WP BS 701 CORRODED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 870TA 25799 45518 FOUND CORROSION AT SKIN LAP ABOVE WINDOW RIGHT SIDE F/S 701. REWORKED, REPAIRED AREA PER SRM 12-21. (M) 2 L 7 4 4R 6A3 1997013000568 19970130 00568 WP 1997 1 30 97ZZZM98 1 19961201 A 5330 SKIN DOUG DC6 DC6A 3021706 WP BS 680 CORRODED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 870TA 45518 FOUND CORRODED AT LOWER FORWARD CORNER OF WINDOW PLUG RIGHT SIDE F/S 680. REWORKED, REPAIRED AREA PER SRM 12-21. (M) 2 L 7 4 4R 6A3 1997013000569 19970130 00569 WP 1997 1 30 97ZZZM99 1 19961201 A 5330 SKIN DOUG DC6 DC6A 3021706 WP BS 926 CORRODED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 870TA 25799 45518 FOUND CORRODED SKIN ABOVE LAP SEAM, ABOVE WINDOW LINE LEFT SIDE F/S 926. REWORKED, AREA REPAIRED PER SRM 12-21. (M) 2 L 7 4 4R 6A3 1997013000573 19970130 00573 NM 1997 1 30 MALA965260 1 19961224 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN LOOSE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 826MA 330 DURING A MAINTENANCE WALKAROUND IN CWA, MAINTENANCE FOUND THE AFT THREE FLOOR TRACK EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE RESECURED A LOOSE ELECTRICAL CONNECTOR UNDER THE FLOOR. ALL CHECKS SATISFACTORY. (M) 2 H 7 2 4T RT A13NM 1997013000574 19970130 00574 SW 1997 1 30 MALA965262 1 19961224 A 2431 CONNECTOR SWRNGN SA227 SA227AC 8780603 SW RT BATT TEMP DIRTY A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 436MA AC719B FLT 3302 - ON CLIMB-OUT FROM MSP, THE HOT BATTERY WARNING LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE CLEANED THE CONNECTOR AT THE RIGHT BATTERY TEMP SENSOR. ALL CHECKS GOOD. (M) 2 L 7 2 4T RT A8SW 1997013000575 19970130 00575 SW 1997 1 30 MALA965267 1 19961226 A 5311 FRAME SWRNGN SA227 SA227AC 8780603 SW BS 197 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 442MA AC725 DURING A BLOCK INSPECTION IN MSP, MAINTENANCE FOUND A CRACK IN RT SIDE OF LOWER CONSTANT SECTION FRAME FLANGE AT FUSELAG E STATION 197. COMPLETED REPAIR TO CONSTANT SECTION IAW FAIRCHILD STRUCTURAL REPAIR MANUAL 53-90-20 PAGES 87-90. (M) 2 L 7 2 4T RT A8SW 1997013000576 19970130 00576 NM 1997 1 30 MALA965266 1 19961228 A 7540 CAUTION LIGHT DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 BLEED AIR ILLUMINATED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 852MA 349 FLT 3223 - ON CLIMB-OUT FROM LNK, THE NR 2 BLEED AIR HOT CAUTION LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO LNK. MAIN TENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. (M) 2 H 7 2 4T 4 T RT A13NM E20NE 1997013000577 19970130 00577 SW 1997 1 30 MALA965268 1 19961228 A 3260 POSITION SWITCH SWRNGN SA227 SA227AC 8780603 SW RT MLG DIRTY A MALA O OTHER J WARNING INDICATION AP APPROACH 1 GL 15 425MA AC640 FLT 2999 - ON APPROACH TO MSP, THE CREW HAD TO CYCLE THE GEAR TWO TIMES BEFORE THE RIGHT GEAR DOWN/LOCKED LIGHT WAS RECE IVED. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. AS A PRECAUTION, THE POSITION SWITCHES WERE CLEANED AND LUB ED. (M) 2 L 7 2 4T RT A8SW 1997013000578 19970130 00578 NM 1997 1 30 P9IA96033 1 19961113 A 2560 290036 MEGAPHONE BOEING 727 727231 1384079 NM CABIN INTERMITTENT A P9IA K NONE O OTHER IN INSP/MAINT 1 SO 03 74318 63180 487 20051 ON PREFLIGHT, FOUND FORWARD MEGAPHONE INTERMITTENT. REMOVED AND REPLACED FORWARD MEGAPHONE. OPS CHECK OK IAW MM 25-60- 0. (M) 2 L 7 3 4F A3WE 1997013000579 19970130 00579 NM 1997 1 30 P9IA96031 1 19961028 A 3350 58225 BATTERY GRIMES BOEING 727 727231 1384079 NM CABIN DISCHARGED A P9IA K NONE L NO TEST IN INSP/MAINT 1 SO 03 74318 2918043 20051 EMERGENCY PATH LIGHTING DIM AT STATION 1030-1183. REMOVED AND REPLACED BATTERY POWER CENTER CEILING STATION 1090. OPS CHECKS NORMAL IAW MM 33-50-71. (M) 2 L 7 3 4F A3WE 1997013000580 19970130 00580 NM 1997 1 30 P9IA96034 1 19961223 A 3350 P4010021 BATTERY BOEING 727 727231 1384079 NM CABIN DISCHARGED A P9IA K NONE L NO TEST IN INSP/MAINT 1 SO 03 12305 64899 19562 ON PREFLIGHT, FOUND FORWARD RIGHT EMERGENCY FLASH LIGHT INOP. REMOVED AND REPLACED BATTERY. OPS CHECKS GOOD IAW MM 33- 50-00. (M) 2 L 7 3 4F A3WE 1997013000581 19970130 00581 NM 1997 1 30 MZZA96170 1 19961219 A 2782 07278690001 ACTUATOR BOEING 727 727232 1384082 NM NR 4 LE SLAT LEAKING A MZZA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 WP 13 15790 20644 FLT 959 - GUM - LOST SYSTEM 'A' HYDRAULIC PRESSURE WHILE LOWERING FLAPS, NR 4 LE SLAT DID NOT DEPLOY. COMPLIED WITH EME RGENCY PROCEDURES AS PER FLIGHT MANUAL. REMOVED AND REPLACED NR 4 LE SLAT ACTUATOR. CHECKED BOTH ENGINE CASE DRAIN FIL TER MAGNETIC PLUGS, FOUND METAL PARTICLES. REPLACED NR 1 AND NR 2 ENGINE DRIVEN HYDRAULIC PUMPS DUE TO SUSPECTED FAILUR E. PERFORMED LEAK AND OPERATIONAL CHECK ON ENGINE RUN AND ALL INDICATIONS NORMAL. (M) 2 L 7 3 4F A3WE 1997013000583 19970130 00583 NE 1997 1 30 M3HA96040 2 19961225 A 7310 3035681 FUEL FILTER AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE NR 2 ENGINE CLOGGED A M3HA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 13 4211G MASC142 178 HNL - FLT 702 - FUEL CLOG LIGHT CAME ON AFTER TAKEOFF, WHILE AT 100NP, UPON RETURN, LIGHT WENT OUT WHEN CL PLACED AT 100 PERCENT NP. AIRCRAFT WAS DIVERTED BACK TO HNL, AND UNEVENTFUL LANDING WAS MADE. REMOVED AND INSTALLED SERVICEABLE NR 2 ENGINE FUEL PUMP FILTER ELEMENT (OUTLET). (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1997013000584 19970130 00584 NM 1997 1 30 M2EA96008 1 19961006 A 2131 CONTROLLER BOEING 737 7373Y0 1384671 NM CABIN DIRTY A P2EA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 05 303AL 23499 FLT 307 - MCI - NO EMERGENCY DECLARED. RETURNED TO MCI. AUTO PRESSURE FAILED. STANDBY NOT WORKING EITHER. REMOVED CA BIN PRESSURE CONTROLLER, CLEANED CPC CONNECTORS AND RE-INSTALLED CPC. CABIN PRESSURE CONTROLLER AND CABIN PRESSURIZATIO N SYSTEM OPERATIONAL CHECKS NORMAL PER MM 21-31-00. (M) 2 L 7 2 4F RT A16WE 1997013000585 19970130 00585 1997 1 30 P2EA96007 4 19960913 A 3414 WL113AMAJA5 AIRSPEED IND BOEING 737 737281 138448P NM RT INST PANEL FAILED A P2EA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 05 219US 20414 FLT 130 - MCI - ABORTED T/O, NO AIRSPEED F/O SIDE. REJECTED T/O AT 100 KTS. NR 2 AIRSPEED IND REMAINED AT 0 WITH NO MO VEMENT. CHECKED QUICK DISCONNECT SECURITY AT IND'S, CHECKED PITOT DRAIN CAPS FOR SECURITY, CHECKED PITOT HEAD FOR OBSTR UCTIONS. PERFORMED TEST F/O'S PITOT SYS AT 50, 100, 150, 200, 250 AND 300 KNOTS FOR IND AND ACCURACY. LEAK TESTED AT 3 00 KNOTS FOR 5 MINUTES, NO LEAKS NOTED. NO LINES DISCONNECTED. SYS OP CHECKS IAW MM 34-11-0. ATTEMPT 2ND T/O, REJECTE D AT 80 KNOTS. NR 2 AIRSPEED IND REMAINED AT 0 KNOTS AGAIN, NO MOVEMENT. REPLACED F/O'S AIRSPEED IND, OPS CHECK AND LE AK CHECK IAW MM 34-12-0. RII ACCOMPLISHED. (M) 2 L 7 2 4F A16WE 1997013000588 19970130 00588 NM 1997 1 30 EISA96286 1 19961223 A 7931 RELIEF VALVE BOEING 727 727221 1384071 NM PWA JT8 JT8D17R 52049 NE NR 2 ENG OUT OF ADJUST A EISA K NONE N FALSE WARNING TO TAKEOFF 1 SW 07 368PA 22540 700503 DURING TAKEOFF, NR 2 OIL PRESSURE ROSE ABOVE RED LINE (APPROX 80 PSPSI). TROUBLESHOT ENGINE OIL PRESSURE RELIEF VALVE A ND ADJUSTED PER MM, LEAK AND OPS CHECK GOOD. (M) 2 L 7 3 4F 4 F A3WE E2EA 1997013000589 19970130 00589 1997 1 30 EISA96285 4 19961227 A 3425 2590281905 ADI BOEING 727 727221 1384071 NM RIGHT INOP A EISA K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 07 367PA 791061121 22539 F/O'S ADI GYRO FLAG IN VIEW IN BOTH NORMAL AND ALTERNATE. REMOVED AND REPLACED F/O'S ADI. OPS CHECK GOOD IAW MM 34-23- 11. (M) 2 L 7 3 4F A3WE 1997013000591 19970130 00591 WP 1997 1 30 ASAA9680280 1 19961224 A 5210 DOOR DOUG DC9 DC982 3022082 WP CABIN MISADJUSTED A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 933AS 49234 SEA - FLT 425 - CREW REPORTED FORWARD ENTRY DOOR DIFFICULT TO OPEN. PRESSURIZED AIRCRAFT TO 7.5 PSI. FOUND DOOR DIFFIC ULT TO OPEN ON FIRST ATTEMPT, BUT OPERATED NORMALLY AFTER BEING OPENED ONCE. ADJUSTED DOOR PER THE MM, PRESSURIZED AIRC RAFT TO 7.5 PSI AND DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1997013000592 19970130 00592 WP 1997 1 30 ASAA9680284 1 19961230 A 2150 ACM DOUG DC9 DC982 3022082 WP LEFT/RIGHT OVERSERVICED A ASAA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 01 955AS 48080 PDX - FLT 343 - ON ARRIVAL, CREW REPORTED SMOKE ALARM ACTIVATED AND SMOKE ODOR DETECTED WITH AIR CONDITIONING PACKS ON D URING TAKEOFF. SELECTED WARMER AIR ON PACKS AND ALARMS SILENCED AND ODOR SUBSIDED. FOUND LEFT AND RIGHT ACM'S OVERSERV ICED. DRAINED OIL TO PROPER LEVEL, RAN PACKS AT SEVERAL TEMPERATURES AND NO ODORS OR SMOKE DETECTED. (M) 2 L 7 2 4F A6WE 1997013000594 19970130 00594 WP 1997 1 30 ASAA9680281 1 19961226 A 5210 4928806501 HOLD OPEN HOOK DOUG DC9 DC983 3022083 WP L-1 DOOR BENT A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 942AS 53052 LAX - FLT 477 - CREW REPORTED, FORWARD ENTRY DOOR DIFFICULT TO LOCK IN THE OPEN POSITION. FOUND HOLD OPEN HOOK BENT. A DJUSTED HOOK AND DOOR LOCKED OPEN NORMALLY. (M) 2 L 7 2 4F RT A6WE 1997013000595 19970130 00595 WP 1997 1 30 ASAA9680275 1 19961217 A 5210 MECHANISM DOUG DC9 DC982 3022082 WP L1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 933AS 49234 LAX - AFTER ARRIVAL OF FLT 291 - CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN. ADJUSTED L1 DOOR AND LUBED LINKAGES A ND DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1997013000596 19970130 00596 WP 1997 1 30 ASAA9680282 1 19961227 A 5210 MECHANISM DOUG DC9 DC982 3022082 WP L-1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 933AS 49234 SEA - FLT 325 - CREW REPORTED FORWARD ENTRY DOOR DIFFICULT TO OPEN. RECYCLED DOOR AND OPENED EASIER. ADJUSTED DOOR PER THE MM, PRESSURIZED AIRCRAFT TO 7.5 PSI AND DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1997013000597 19970130 00597 EU 1997 1 30 97ZZZM100 1 19960819 A 5530 STRUCTURE BAG BAE146 BAE146300A 1500267 EU VERT STAB WORN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 VERTICAL STABILIZER LEADING EDGE, BOTH LEFT AND RIGHT DE-ICE SUPPLY DUCT WEARING INTO AUXILLIARY STRUCTURE. REMOVED DUC TS AND REPAIRED AUX STRUCTURE AT VERTICLE STAB RIB 1 AREA IAW AVRO FAX DJR/RJ0930-96. NEW W/C GENERATED FOR DUCT INSTAL LATION. 2 H 7 4 4F RT A49EU 1997013000598 19970130 00598 EU 1997 1 30 97ZZZM101 1 19960816 A 5347 SEAT RAIL BAG BAE146 BAE146300A 1500267 EU CABIN CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 FORWARD LEFT SEAT RAIL IS CORRODED OUTBOARD SIDE FRAME 18 TO FRAME 19A, REPLACEMENT REQUIRED. REMOVED AND REPLACED FORW ARD LEFT OUTBOARD SEAT RAIL PER A/C SRM STANDARD PRACTICES. 2 H 7 4 4F RT A49EU 1997013000599 19970130 00599 EU 1997 1 30 97ZZZM102 1 19960812 A 5753 BOLT BAG BAE146 BAE146300A 1500267 EU NR 2 TE FLAP TAB CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 LEFT NR 2 FLAP TAB CROSSHEAD BOLT HAS CRACK INDS IN UNDER CUT OF BOLT. INSTALLED NEW CROSSHEAD BOLT. 2 H 7 4 4F RT A49EU 1997013000600 19970130 00600 EU 1997 1 30 97ZZZM103 1 19960812 A 5753 PIN BAG BAE146 BAE146300A 1500267 EU NR 2 TE FLAP CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 LEFT NR 2 FLAP TRACK CROSSHEAD PIN IS CRACKED INBOARD SIDE. INSTALLED A NEW CROSSHEAD PIN. 2 H 7 4 4F RT A49EU 1997013000601 19970130 00601 EU 1997 1 30 UF6A960605 1 19960619 A 2750 3F12844 CONTROL CABLE BAG ATP ATP EU TE FLAPS FAILED A UF6A O OTHER O OTHER AP APPROACH 1 GL 31 856AW 9342 2032 AZO - FLT 5705 - FLAP 'CWP' ILLUMINATED IN FLIGHT. MAINTENANCE REMOVED AND REPLACED INNER MOST UPPER FLAP CABLE. (M) 2 L 7 2 4T RT A27NM 1997013000602 19970130 00602 EU 1997 1 30 UF6A961102 1 19961110 A 3350 6013211 POWER SUPPLY GRIMES BAG ATP ATP EU CABIN INOPERATIVE A UF6A K NONE L NO TEST TX TAXI/GRND HDL 1 GL 31 856AW 8290 17248 2032 FWA - FLT 5722 - FORWARD SET OF FLOOR PROXIMITY EMERGENCY ESCAPE PATH LIGHTS WILL NOT TEST. MAINTENANCE REMOVED AND REP LACED NR 1 EMERGENCY LIGHT POWER PACK. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1997013000603 19970130 00603 EU 1997 1 30 UF6A960907 1 19960921 A 2750 152645 TERMINAL BAG ATP ATP EU TE FLAPS LOOSE A UF6A A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 GL 31 859AW 2036 GRB - FLT 5764 - FLAPS WILL NOT DEPLOY TO 20 DEGREES IN FLIGHT. MAINTENANCE FOUND LOOSE TERMINAL, SECURED SAME. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1997013000604 19970130 00604 EU 1997 1 30 UF6A960803 1 19960806 A 6120 7863366 PCU HAMSTD BAG ATP ATP EU NR 1 ENGINE FAULTY A UF6A K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 858AW 4637 ATPCO111 2035 ORD - FLT 5702 - NR 1 PROP DID NOT FEATHER ON SHUTDOWN. MAINTENANCE PERFORMED OPERATIONAL TEST OF NR 1 PROP, SYSTEM CHE CK GOOD. (M) 2 L 7 2 4T RT A27NM 1997013000605 19970130 00605 EU 1997 1 30 UF6A960804 1 19960807 A 6120 7863366 PCU HAMSTD BAG ATP ATP EU NR 1 ENGINE FAULTY A UF6A K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 858AW 4642 ATPC0111 2035 ORD - FLT 5734 - NR 1 PROP DID NOT FEATHER ON SHUTDOWN. MAINTENANCE PERFORMED OPERATIONAL TEST OF NR 1 PROP, SYSTEM CHE CK GOOD. (M) 2 L 7 2 4T RT A27NM 1997013000606 19970130 00606 EU 1997 1 30 UF6A960807 1 19960808 A 6120 7863366 PCU HAMSTD BAG ATP ATP EU NR 1 ENGINE FAULTY A UF6A K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 853AW 9456 ATPC0043 2022 ORD - FLT 5733 - NR 1 PROP DOES NOT FEATHER ON SHUTDOWN. MAINTENANCE PERFORMED OPERATIONAL TEST OF NR 1 PROP, SYSTEM CH ECK GOOD. (M) 2 L 7 2 4T RT A27NM 1997013000607 19970130 00607 EU 1997 1 30 UF6A960810 1 19960814 A 6120 30048000014 AUTOFEATHER UNIT HAMSTD BAG ATP ATP EU NR 1 ENGINE FAULTY A UF6A C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 31 852AW 7106 566 2021 SBN - FLT 5760 - ON TAKEOFF, LEFT ENGINE UPPER FEATHER LIGHT DID NOT ARM. MAINTENANCE REMOVED AND REPLACED NR 1 AUTOFEA THER UNIT, SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1997013000608 19970130 00608 EU 1997 1 30 UF6A960811 1 19960815 A 6120 AUTOFEATHER BAG ATP ATP EU NR 1 ENGINE MALFUNCTIONED A UF6A O OTHER J WARNING INDICATION LD LANDING 1 GL 31 854AW 2028 YNG - 5709 - NR 2 PROP FEATHERED ON LANDING ROLL. UP TRIM OCCURRED. MAINTENANCE PERFORMED AUTOFEATHER TEST. SYSTEM O PS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1997013000609 19970130 00609 1997 1 30 UF6A960815 4 19960822 A 3442 36141655518 RADAR BAG ATP ATP EU FWD FUSELAGE FAILED A UF6A O OTHER O OTHER CL CLIMB 1 GL 31 857AW 9004 K1268 2034 ORD - FLT 5762 - WEATHER RADAR MALFUNCTION. MAINTENANCE REMOVED AND REPLACED RADAR SENSOR. SYSTEM OPS CHECKED GOOD. ( M) 2 L 7 2 4T RT A27NM 1997013000610 19970130 00610 EU 1997 1 30 UF6A960901 1 19960831 A 6120 7863366 PCU HAMSTD BAG ATP ATP EU NR 1 ENGINE FAULTY A UF6A K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 858AW 4637 ATPC0111 2035 ORD - FLT 5700 - ON SHUTDOWN, NR 1 ENGINE WILL NOT FEATHER. MAINTENANCE PERFORMED OPERATIONAL TEST OF NR 1 PROP. SYSTE M OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1997013000611 19970130 00611 EU 1997 1 30 UF6A960902 1 19960831 A 6120 7863366 PCU HAMSTD BAG ATP ATP EU NR 1 ENGINE FAULTY A UF6A K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 GL 31 858AW 4637 ATPCO111 2035 SBN - FLT 5752 - ON SHUTDOWN, NR 1 ENGINE WILL NOT FEATHER. MAINTENANCE PERFORMED OPERATIONAL TEST OF NR 1 PROP. SYSTE M OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1997013000612 19970130 00612 EU 1997 1 30 UF6A960903 1 19960831 A 6120 7863366 PCU HAMSTD BAG ATP ATP EU NR 1 ENGINE FAULTY A UF6A K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 GL 31 858AW ATPC0111 2035 ORD - FLT 5755 - ON SHUTDOWN, NR 1 ENGINE WILL NOT FEATHER. MAINTENANCE PERFORMED OPERATIONAL TEST OF NR 1 PROP. SYSTE M OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1997013000613 19970130 00613 EU 1997 1 30 UF6A960906 1 19960909 A 3412 E22226 OAT SENSOR BAG ATP ATP EU NR 1 FAILED A UF6A C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 31 859AW 1601 332 2036 CAK - FLT 5712 - DE-ICE CWP ILLUMINATED ON TAKEOFF BELOW 80 KNOTS, LEFT TORQUE FAILED 25 PERCENT, DE-ICE CWP WOULD NOT C LEAR. MAINTENANCE REMOVED AND REPLACED NR 1 OAT SENSOR. OPS CHECK OF ENGINE DE-ICE AND TORQUE BUG WAS GOOD. (M) 2 L 7 2 4T RT A27NM 1997013000614 19970130 00614 EU 1997 1 30 UF6A960802 1 19960805 A 6120 7863366 PCU HAMSTD BAG ATP ATP EU NR 1 ENG FAULTY A UF6A K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 858AW 4632 ATPC0111 2035 ORD - FLT 5749 - NR 1 PROP DID NOT FEATHER ON SHUTDOWN. MAINTENANCE PERFORMED OPERATIONAL TEST OF NR 1 PROP. SYSTEM CH ECK GOOD. (M) 2 L 7 2 4T RT A27NM 1997013000615 19970130 00615 EU 1997 1 30 UF6A960814 1 19960824 A 3350 6013211 POWER SUPPLY GRIMES BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 856AW 8660 16934 2032 ORD - EMERGENCY LIGHTS ABOVE ROW 12, 14 AND 16 INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY. (M ) 2 L 7 2 4T RT A27NM 1997013000616 19970130 00616 EU 1997 1 30 UF6A960904 1 19960904 A 3350 6013211 POWER SUPPLY GRIMES BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 854AW 7856 17370 2028 ORD - FLT 5722 - EMERGENCY LIGHTS ROWS 5, 6, 7 INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY. SY STEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1997013000617 19970130 00617 EU 1997 1 30 UF6A960908 1 19960924 A 2751 750SUE68 SYMBOL GENERATOR BAG ATP ATP EU NR 1 POSITION FAILED A UF6A O OTHER N FALSE WARNING CL CLIMB 1 GL 31 856AW 7004 C111J 2032 ORD - FLT 5744 - NR 1 PFD AND ND COMPLETE FAILURE AFTER TAKEOFF. MAINTENANCE REMOVED AND REPLACED NR SYMBOL GENERATOR. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1997013000618 19970130 00618 NE 1997 1 30 UF6A960602 3 19960615 A 6111 7863504 BLADE HAMSTD BAG ATP ATP EU HAMSTD 5500 65500F1 NE NR 2 PROP FAULTY A UF6A O OTHER E VIBRATION/BUFFET CR CRUISE 1 GL 31 852AW 3674 854322 2021 4A424883 ORD - FLT 5733 - PROP VIBRATION IN FLIGHT, AMPLIFIED AT HIGHER TORQUES. MAINTENANCE REMOVED AND REPLACED NR 1 BLADE ON NR 2 PROP. BALANCED ASSEMBLIES, SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4T RT A27NM 6 C P13NE 1997013000619 19970130 00619 EU 1997 1 30 UF6A960607 1 19960628 A 6123 30048000013 AUTOFEATHER UNIT SIMMONDS BAG ATP ATP EU NR 1 ENGINE FAILED A UF6A C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 31 852AW 9339 407 2021 AZO - FLT 5704 - LEFT AUTOFEATHER DID NOT ARM ON TAKEOFF ROLL. MAINTENANCE REMOVED AND REPLACED NR 1 AUTOFEATHER UNIT. (M) 2 L 7 2 4T RT A27NM 1997013000620 19970130 00620 NE 1997 1 30 UF6A960711 2 19960724 A 7260 303821417 CHIP DETECTOR BAG ATP ATP EU PWA PW120 PW126A NE NR 2 ENGINE FAULTY A UF6A O OTHER N FALSE WARNING CL CLIMB 1 GL 31 852AW 7610 2021 124403 SBN - FLT 5761 - RIGHT CHIP DETECTOR ILLUMINATED IMMEDIATELY AFTER TAKEOFF. MAINTENANCE REMOVED CHIP DETECTOR AND FOUND NO DEBRIS. CLEANED AND REINSTALLED CHIP DETECTOR, SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T 4 T RT A27NM E2ONE 1997013000621 19970130 00621 EU 1997 1 30 UF6A960703 1 19960712 A 7921 3036064 OIL COOLER BAG ATP ATP EU NR 1 ENGINE FAILED A UF6A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 859AW 8841 668 2036 ORD - FLT 5717 - NR 1 OIL PRESSURE CWP ILLUMINATED IN FLIGHT ALONG WITH NR 1 OIL PRESSURE GAUGE SHOWING BELOW 40 PSI. M AINTENANCE REMOVED AND REPLACED NR 1 ENGINE OIL COOLER, AND PERFORMED HIGH POWER RUN. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4T RT A27NM 1997013000622 19970130 00622 EU 1997 1 30 UF6A960710 1 19960723 A 6120 7863364 PCU HAMSTD BAG ATP ATP EU NR 1 ENGINE FAULTY A UF6A K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 852AW 9303 ATPC009 2021 ORD - FLT 5710 - NR 1 PROP DID NOT FULLY FEATHER ON ENGINE SHUTDOWN. MAINTENANCE PERFORMED OPERATIONAL CHECK, OPS CHECK ED GOOD. (M) 2 L 7 2 4T RT A27NM 1997013000623 19970130 00623 EU 1997 1 30 UF6A960712 1 19960726 A 6120 7863364 PCU HAMSTD BAG ATP ATP EU NR 1 ENGINE FAULTY A UF6A K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 852AW 9316 ATPC0099 2021 ORD - FLT 5710 - NR 1 PROP DID NOT FULLY FEATHER ON ENGINE SHUTDOWN. MAINTENANCE PERFORMED OPERATIONAL CHECK. SYSTEM O PS CHECK GOOD. (M) 2 L 7 2 4T RT A27NM 1997013000624 19970130 00624 EU 1997 1 30 UF6A960702 1 19960702 A 3350 60132111 POWER SUPPLY GRIMES BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 859AW 6182 17371 2036 FWA - FLT 5722 - EMERGENCY LIGHTS FORWARD FLOOR STRIP, DIRECTIONAL SIGNS, EXIT SIGNS INOP. MAINTENANCE REMOVED AND REPL ACED FORWARD POWER SUPPLY UNIT. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4T RT A27NM 1997013000625 19970130 00625 EU 1997 1 30 UF6A960706 1 19960714 A 2121 7846281 FAN BAG ATP ATP EU NR 1 FAILED A UF6A K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 31 855AW 7197 881067 2029 ORD - FLT 5716 - PLASTIC BURNING SMELL IN THE COCKPIT. NR 1 RECIRC FAN 'OFF' ILLUMINATED. CHECK LIST COMPLETED. MAINT ENANCE OPS CHECKED NR 1 RECIRC FAN FOR TWO HOURS. NO BURNING SMELL NOTICED. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4T RT A27NM 1997013000626 19970130 00626 1997 1 30 UF6A960705 4 19960715 A 3425 4608001311 AHRU LITTON BAG ATP ATP EU NR 1 DIRTY A UF6A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 852AW 6640 1316 2021 FWA - FLT 5728 - AFTER TAKEOFF 'EFIS' CWP ILLUMINATED WITH FAILURE OF NR 1 FFD AND ND. MAINTENANCE REMOVED NR 1 AHRU'S, CLEANED CONNECTIONS AND REINSTALLED. CLEANED AOG SWITCHES, SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4T RT A27NM 1997013000627 19970130 00627 EU 1997 1 30 UF6A960701 1 19960702 A 2121 75MA157I FAN BAG ATP ATP EU AVIONICS BAY FAILED A UF6A O OTHER J WARNING INDICATION TO TAKEOFF 1 GL 31 853AW 5489 4385915 2022 SBN - FLT 5764 - NR 1 AVIONICS FAN AND CWP ILLUMINATED JUST PRIOR TO ROTATION. MAINTENANCE REMOVED AND REPLACED NR 1 AV IONICS COOLING FAN. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4T RT A27NM 1997013000628 19970130 00628 EU 1997 1 30 UF6A960601 1 19960609 A 3350 6013211 POWER SUPPLY GRIMES BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 857AW 3860 15889 2034 ORD - FORWARD EMERGENCY FLOOR LIGHTING STRIP INOP. MAINTENANCE REMOVED AND REPLACED NR 1 POWER SUPPLY. SYSTEM OPS CHEC K GOOD. (M) 2 L 7 2 4T RT A27NM 1997013000629 19970130 00629 EU 1997 1 30 UF6A960603 1 19960617 A 3350 6013211 POWER SUPPLY GRIMES BAG ATP ATP EU GALLEY FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 857AW 3802 16108 2034 SBN - FLT 5753 - GALLEY EMERGENCY LIGHTS WERE INOP. MAINTENANCE REMOVED AND REPLACED AFT GALLEY POWER SUPPLY. SYSTEM O PS CHECK GOOD. (M) 2 L 7 2 4T RT A27NM 1997013000630 19970130 00630 EU 1997 1 30 UF6A960606 1 19960621 A 2421 BA03304 AC GENERATOR LUCAS BAG ATP ATP EU NR 1 FAILED A UF6A O OTHER H ELECT. POWER LOSS-50 PC CL CLIMB 1 GL 31 852AW 7053 2026CA 2021 ORD - FLT 5705 - NR 1 GENERATOR FAILED IN FLIGHT. COMPLIED WITH CHECK LIST GENERATOR CAME ON FOR APPROXIMATELY 1 MINUTE THEN FAILED. MAINTENANCE REMOVED AND REPLACED NR 1 GENERTOR, SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4T RT A27NM 1997013000631 19970130 00631 EU 1997 1 30 UF6A960405 1 19960421 A 3350 6013211 POWER SUPPLY GRIMES BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 858AW 3419 16357 2035 ORD - EMERGENCY EXIT LIGHTS AT ROW 8 ARE INOP. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY. (M) 2 L 7 2 4T RT A27NM 1997013000632 19970130 00632 EU 1997 1 30 UF6A960709 1 19960719 A 3350 6013211 POWER SUPPLY GRIMES BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 855AW 9364 17200 2029 CWA - FLT 5722 - ROW 15 AND AFT EMERGENCY FLOOR LIGHTING STRIP INOP ALONG WITH ALL GALLEY EMERGENCY EXIT SIGNS. MAINTEN ANCE REMOVED AND REPLACED AFT POWER SUPPLY. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4T RT A27NM 1997013000633 19970130 00633 EU 1997 1 30 UF6A960805 1 19960807 A 3350 6013211 POWER SUPPLY GRIMES BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 857AW 7474 17451 2034 ORD - EXIT LOCATOR SIGN SYSTEM INOPEATIVE AT 'B' FLIGHT ATTENDANT POSITION. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SYSTEM. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4T RT A27NM 1997013000634 19970130 00634 EU 1997 1 30 UF6A960715 1 19960730 A 3350 6013211 POWER SUPPLY GRIMES BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 854AW 9725 16857 2028 ORD - EMERGENCY LIGHTS INOP AT SEAT 12CD THROUGH 14CD. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT SEAT 12CD A ND 14CD. (M) 2 L 7 2 4T RT A27NM 1997013000635 19970130 00635 EU 1997 1 30 UF6A960713 1 19960728 A 6123 30048000014 AUTOFEATHER UNIT HAMSTD BAG ATP ATP EU NR 1 ENGINE FAILED A UF6A C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 31 852AW 7059 566 2021 ORD - FLT 5707 - LEFT AUTOFEATHER UNIT DID NOT ARM ON TAKEOFF. MAINTENANCE CLEANED THE CANNON PLUG ON THE NR 1 AFU. SY STEM CHECK GOOD. (M) 2 L 7 2 4T RT A27NM 1997013000636 19970130 00636 EU 1997 1 30 UF6A960707 1 19960717 A 2422 ASH6641PB INVERTER LELAND BAG ATP ATP EU NR 1 FAILED A UF6A O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 31 859AW 7278 KL577 2036 FWA - FLT 5758 - CAPTAINS EFIS INOP. NR 1 INVERTER WAS FLUCTUATING 100V TO 150V. SMELL OF SMOKE IN COCKPIT. MAINTENAN CE REMOVED AND REPLACED NR 1 INVERTER. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4T RT A27NM 1997013000637 19970130 00637 EU 1997 1 30 UF6A960714 1 19960730 A 2751 2S0030501 PROX SWITCH BAG ATP ATP EU NR 2 OUTOBARD FAILED A UF6A A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 31 858AW 8786 2035 SBN - FLT 5767 - IN CRUISE, AT 8000 FEET, AND 5 DEGREES CELSIUS, FLAP CWP CAME ON. THEN AT 2000 FEET AND 23 DEGREES, 14 0 KTS THE FLAP CWP WENT OFF. ON FINAL AT 120 KNOTS THE FLAP CWP CAME ON. MAINTENANCE REMOVED AND REPLACED NR 2 OUTBOAR D PROXIMITY SWITCH. PERFORMED OPS CHECK OF FLAP SYSTEM. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4T RT A27NM 1997013000638 19970130 00638 1997 1 30 UF6A961101 4 19961104 A 2565 2077001 ESCAPE SLIDE BAG ATP ATP EU CABIN FAILED TO DEPLOY A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 853AW 9920 111 2022 SBN - PERFORMED FUNCTIONAL TEST OF FORWARD ESCAPE SLIDE. SLIDE FAILED TO DEPLOY, PIN STAYED IN BOTTLE. MAINTENANCE DEP LOYED MANUALLY. (M) 2 L 7 2 4T RT A27NM 1997013000639 19970130 00639 EU 1997 1 30 UF6A961103 1 19961110 A 6123 30048000014 AUTOFEATHER UNIT HAMSTD BAG ATP ATP EU NR 1 ENGINE FAILED A UF6A K NONE O OTHER LD LANDING 1 GL 31 855AW 7846 583 2029 FWA - FLT 5730 - LEFT ENGINE AUTOFEATHERED ON LANDING WHEN PULLED INTO REVERSE. MAINTENANCE REMOVED AND REPLACED NR 1 A UTOFEATHER UNIT. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1997013000640 19970130 00640 EU 1997 1 30 RAIA961246 1 19961220 A 5313 S53671407210218 STRINGER AEROSP ATR42 ATR42300 8680920 EU AFT FUS CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON STRINGER 19R FROM FRAME 28 TO FRAME 30. MAINTENANCE REMOVED CORROSION FROM STRINGER 19R FROM F RAME 28 TO FRAME 30, FOUND TO BE WITHIN LIMITS IAW ATR 42 SRM 53-61-26. (M) 2 H 7 2 4T RT A53EU 1997013000641 19970130 00641 EU 1997 1 30 RAIA961245 1 19961220 A 5313 S53671407210218 STRINGER AEROSP ATR42 ATR42300 8680920 EU AFT FUS CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION STRINGER 18R FROM FRAME 28 TO FRAME 30. MAINTENANCE REMOVED CORROSION FROM STRINGER 18R FROM FRAM E 28 TO FRAME 30, FOUND TO BE WITHIN LIMITS IAW ATR 42 SRM 53-61-26. (M) 2 H 7 2 4T RT A53EU 1997013000642 19970130 00642 EU 1997 1 30 RAIA961244 1 19961220 A 5313 S53671407210218 STRINGER AEROSP ATR42 ATR42300 8680920 EU AFT FUS CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON STRINGER 17R FROM FRAME 28 TO FRAME 41. MAINTENANCE REMOVED CORROSION ON STRINGER 17R FROM FR AME 28 TO FRAME 34, FOUND TO BE WITHIN LIMITS IAW ATR 42 SRM 53-21-26. (M) 2 H 7 2 4T RT A53EU 1997013000643 19970130 00643 EU 1997 1 30 RAIA961243 1 19961220 A 5313 S53671407210218 STRINGER AEROSP ATR42 ATR42300 8680920 EU AFT FUS CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON STRINGER 16R FROM FRAME 29 TO FRAME 40. MAINTENANCE REMOVED CORROSION IAW ATR 42 SRM 51-21-42. (M) 2 H 7 2 4T RT A53EU 1997013000644 19970130 00644 EU 1997 1 30 RAIA961242 1 19961220 A 5320 S53671407210218 SPLICE AEROSP ATR42 ATR42300 8680920 EU AFT FUS CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 124 STL - FOUND CORROSION ON STRINGER 17R SPLICE AT FRAME 29. MAINTENANCE REMOVED CORROSION FROM SPLICE ON STRINGER 17R AT FRAME 29, FOUND TO BE WITHIN LIMITS IAW SRM 53-61-26. (M) 2 H 7 2 4T RT A53EU 1997013000645 19970130 00645 EU 1997 1 30 RAIA961241 1 19961220 A 5320 S53681407210218 SPLICE AEROSP ATR42 ATR42300 8680920 EU AFT FUS CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON STRINGER 16R SPLICE AT FRAME 29. MAINTENANCE REMOVED CORROSION FROM SPLICE ON STRINGER 16 AT F RAME 29, FOUND TO BE WITHIN LIMITS IAW ATR 42 SRM 52-61-26. (M) 2 H 7 2 4T RT A53EU 1997013000646 19970130 00646 EU 1997 1 30 RAIA961240 1 19961220 A 5313 S53671407210218 STRINGER AEROSP ATR42 ATR42300 8680920 EU STR 15R FR 33 CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 18174 124 STL - FOUND CORROSION ON STRINGER 15R FROM FRAME 33 TO FRAME 34. MAINTENANCE REPAIRED STRINGER 15R FROM FRAME 33 TO FRA ME 34 IAW ATR 42 SRM 53-00-00. (M) 2 H 7 2 4T RT A53EU 1997013000647 19970130 00647 EU 1997 1 30 RAIA961239 1 19961220 A 5313 S53671407210218 STRINGER AEROSP ATR42 ATR42300 8680920 EU AFT FUS CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 124 STL - FOUND CORROSION ON STRINGER TO FRAME CLIPS AT STRINGER 21L, 21R AND FRAME 34. MAINTENANCE REMOVED CORROSION IAW A TR 42 SRM 51-21-42. (M) 2 H 7 2 4T RT A53EU 1997013000648 19970130 00648 EU 1997 1 30 RAIA961238 1 19961220 A 5313 S53671407210218 STRINGER AEROSP ATR42 ATR42300 8680920 EU AFT FUS CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON STRINGER TO FRAME CLIPS AT STRINGER 21L AND FRAME 33. MAINTENANCE REMOVED CORROSION IAW ATR 42 SRM 51-21-42. (M) 2 H 7 2 4T RT A53EU 1997013000649 19970130 00649 EU 1997 1 30 RAIA961237 1 19961220 A 5313 S53671407210218 STRINGER AEROSP ATR42 ATR42300 8680920 EU AFT FUS CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON STRINGER TO FRAME CLIPS AT STRINGER 20L, 21L, 21R, AND FRAME 30. MAINTENANCE REMOVED CORROSION IAW ATR 42SRM 51-21-42. (M) 2 H 7 2 4T RT A53EU 1997013000650 19970130 00650 EU 1997 1 30 RAIA961236 1 19961220 A 5313 S53671407210218 STRINGER AEROSP ATR42 ATR42300 8680920 EU AFT FUS CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON STRINGER TO FRAME CLIPS AT STRINGER 21L, 20L, 21R AND FRAME 29. MAINTENANCE REMOVED CORROSION IAW ATR 42 SRM 51-21-42. (M) 2 H 7 2 4T RT A53EU 1997013000651 19970130 00651 EU 1997 1 30 RAIA961235 1 19961220 A 5313 S53671407210218 STRINGER AEROSP ATR42 ATR42300 8680920 EU AFT FUS CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON STRINGER TO FRAME CLIPS AT STRINGER 21L AND FRAME 28. MAINTENANCE REMOVED CORROSION IAW ATR 42 SRM 51-21-42. (M) 2 H 7 2 4T RT A53EU 1997013000652 19970130 00652 EU 1997 1 30 RAIA961234 1 19961220 A 5320 S5367800821602 ANGLE AEROSP ATR42 ATR42300 8680920 EU AFT FUS CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON FRAME 40 FAIL/SAFE ANGLE FROM STRINGER 21L TO 21R. MAINTENANCE REMOVED CORROSION IAW ATR 42 SR M 51-21-42. (M) 2 H 7 2 4T RT A53EU 1997013000653 19970130 00653 EU 1997 1 30 RAIA961233 1 19961220 A 5320 S5367800821602 ANGLE AEROSP ATR42 ATR42300 8680920 EU AFT FUS CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON FRAME 39 FAIL/SAFE ANGLE FROM STRINGER 19L TO 20R. MAINTENANCE REMOVED CORROSION IAW ATR42 SRM 51-21-42. (M) 2 H 7 2 4T RT A53EU 1997013000654 19970130 00654 WP 1997 1 30 TWAA9615805 1 19961212 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP BS 1231 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 MCI - DURING OP-16, FOUND CORROSION ON INTERCOSTAL AFT OF STATION 1231 FRAME AT LONGERON 25L. REMOVED CORROSION PER SRM 51-10-3 AND STANDARD PRACTICES. (M) 2 L 7 2 4F A6WE 1997013000655 19970130 00655 WP 1997 1 30 TWAA9615807 1 19961212 A 5320 PAN DOUG DC9 DC982 3022082 WP BS 1287-1307 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 MCI - DURING OP-16, FOND DIAPHRAM PAN CRACKED 12 INCHES OUTBOARD OF NR 6 CHAIR TRACK, LONGERON 18R, STATION 1287-1307. S TOP DRILLED CRACK PER SRM 51-10-00 AND REPAIRED PER SRM 53-00-09, PAGE 347. (M) 2 L 7 2 4F A6WE 1997013000656 19970130 00656 WP 1997 1 30 TWAA9615804 1 19961212 A 5320 FITTING DOUG DC9 DC982 3022082 WP BS 1338 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 MCI - DURING OP-16, FOUND CORROSION ON CORNER FITTING AT LEFT STATION 1338. REPLACED GUSSET PER SRM 51-1, PAGE 1. (M) 2 L 7 2 4F A6WE 1997013000657 19970130 00657 WP 1997 1 30 TWAA9615806 1 19961212 A 5320 PAN DOUG DC9 DC982 3022082 WP BS 1271-1287 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 MCI - DURING OP-16, FOUND DIAPHRAM PAN CRACKED 2.5 INCHES OUTBOARD OF NR 6 CHAIR TRACK, LONGERON 18R, STATION 1271-1287. STOP DRILLED CRACK PER SRM 51-10-00 AND REPAIRED PER SRM 53-00-09, PGE 347. (M) 2 L 7 2 4F A6WE 1997013000658 19970130 00658 WP 1997 1 30 TWAA9615803 1 19961212 A 5347 FLOOR TRACK DOUG DC9 DC982 3022082 WP BS 1126-1222 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 MCI - DURING OP-16, FOUND CORROSION ON NR 2 FLOOR TRACK AT LEFT AFT SERVICE DOOR, LBL 44. INSTALLED NEW FLOOR TRACK FS 1126 TO 1222, PER SRM 53-05, PAGE 10G. (M) 2 L 7 2 4F A6WE 1997013000659 19970130 00659 WP 1997 1 30 TWAA9615801 1 19961218 A 3297 WIRE DOUG DC9 DC931 3022065 WP LANDING GEAR BROKEN A TWAA O OTHER N FALSE WARNING CL CLIMB 1 CE 05 977Z 47249 STL - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, RIGHT MAIN LANDING GEAR DID NOT INDICATE UP AND LOCKED. CYCLED LAN DING GEAR. FOUND WIRE 2G204E24 AND 2G206E24, BROKEN. REPAIRED WIRES AND REPLACED SWITCH, MFG P/N H14-6. LANDING GEAR INDICATION AND OPERATION CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 1997013000660 19970130 00660 WP 1997 1 30 TWAA9615802 1 19961212 A 5320 FORMER DOUG DC9 DC982 3022082 WP BS 1271 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 MCI - DURING OP-16, FOUND CORROSION ON FORMER, STATION 1271 AT LONGERONS 28L AND 29R. REMOVED CORROSION PER SRM 51-10-0 1 AND REPAIRED PER SRM 53-03, FIGURE 2A. (M) 2 L 7 2 4F A6WE 1997013000661 19970130 00661 WP 1997 1 30 TWAA9615703 1 19961216 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9307R 49663 MCI - DURING OP-16, FOUND CRACK IN SKIN AFT LEFT HINGE CUTOUT NLG DOOR. INSTALLED DOUBLER REPAIR PER SRM 53-05, PAGE 16 9, FIGURE 62. (M) 2 L 7 2 4F RT A6WE 1997013000662 19970130 00662 WP 1997 1 30 TWAA9615811 1 19961212 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP CABIN FLOOR CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 MCI - DURING OP-16, FOUND CORROSION ON CABIN FLOOR SUPPORT INBOARD OF FORWARD GALLEY DOOR. REPLACED PART PER SRM 51-10- 3. (M) 2 L 7 2 4F A6WE 1997013000663 19970130 00663 WP 1997 1 30 TWAA9615812 1 19961212 A 5347 FLOOR TRACK DOUG DC9 DC982 3022082 WP BS 1022-1155 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 MCI - DURING OP-16, FOUND CORROSION ON CARGO FLOOR TRACK, LONGERON 27R-28R, FS 1022-1155. REPLACED PART PER SRM 51-01. (M) 2 L 7 2 4F A6WE 1997013000664 19970130 00664 WP 1997 1 30 TWAA9615808 1 19961212 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 MCI - DURING OP-16, FOUND INTERCOSTAL CORROSION. REPLACED PART PER SRM 51-00 AND STANDARD PRACTICES. (M) 2 L 7 2 4F A6WE 1997013000665 19970130 00665 WP 1997 1 30 TWAA9615809 1 19961212 A 5347 GALLEY TRACK DOUG DC9 DC982 3022082 WP BS 1174-1322 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 MCI - DURING OP-16, FOUND CORROSION AROUND TIE HOLES OF OUTBOARD GALLEY TIE TRACK, LBL 54, FS 1174, 1210, 1238, 1295. R EPLACED TRACK FROM 1174 TO 1322 PER MM 53-10-01. (M) 2 L 7 2 4F A6WE 1997013000666 19970130 00666 WP 1997 1 30 TWAA9615810 1 19961212 A 5320 FORMER DOUG DC9 DC982 3022082 WP BS 1309 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 MCI - DURING OP-16, FOUND FORMER CORROSION, LONGERON 20L TO 20R, FS 1309. REPLACED PART PER SRM 53-10-01. (M) 2 L 7 2 4F A6WE 1997013000667 19970130 00667 WP 1997 1 30 TWAA9615813 1 19961212 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 1320 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 MCI - DURING OP-16, FOUND CORROSION ON FLOOR SUPPORT, LONGERON 26L TO 26R, STATION 1320. REPAIRED PER SRM 53-01, FIGURE 1. (M) 2 L 7 2 4F A6WE 1997013000668 19970130 00668 WP 1997 1 30 TWAA9615815 1 19961212 A 5320 RUB STRIP DOUG DC9 DC982 3022082 WP BS 769-788 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 MCI - DURING OP-16, FOUND CORROSION IN THE FAIRING RUB STRIP AREA OF RT FORWARD FILLET, BETWEEN FS 769 TO FS 788, AND FR OM LONGERON 28R TO 29R. REPAIRED PER SRM 53-04, FIGURE 53. (M) 2 L 7 2 4F A6WE 1997013000669 19970130 00669 WP 1997 1 30 TWAA9615814 1 19961212 A 5320 RUB STRIP DOUG DC9 DC982 3022082 WP BS 788-807 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 MCI - DURING OP-16, FOUND CORROSION UNDER FAIRING RUB STRIP OF RT FORWARD FILLET AREA, BETWEEN FS 788-807, LONGERON 28R AND 29R. REMOVED CORROSION AND REPAIRED PER SRM 53-04, FIG 53. (M) 2 L 7 2 4F A6WE 1997013000670 19970130 00670 WP 1997 1 30 TWAA9615816 1 19961212 A 5320 RUB STRIP DOUG DC9 DC982 3022082 WP BS 807-826 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 MCI - DURING OP-16, FOUND CORROSION UNDER FAIRING RUB STRIP OF RT FORWARD FILLET AREA, LOONGEON 29L TO LONGERON 29R, BET WEEN FS 807 AND 826. REPAIRED PER ATA 10902. (M) 2 L 7 2 4F A6WE 1997013000671 19970130 00671 WP 1997 1 30 TWAA9615817 1 19961212 A 5320 RUB STRIP DOUG DC9 DC982 3022082 WP BS 750-769 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 905TW 49157 MCI - DURING OP-16, FOUND CORROSION IN THE FAIRING RUB STRIP AREA OF RT FORWARD FILLET, LONGERON 26R TO LONGERON 28R, BE TWEEN FS 750 TO FS 769. REPAIRED PER SRM 53-04, FIGURE 53. (M) 2 L 7 2 4F A6WE 1997013000672 19970130 00672 WP 1997 1 30 TWAA9615818 1 19961212 A 5347 FLOOR TRACK DOUG DC9 DC983 3022083 WP BS 1155-1079 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9307R 49663 MCI - DURING OP-16, FOUND CORROSION ON RT FLOOR TRACK, FS 1155-1079. REPLACED TRACK PER SRM 53-5, PAGE 10 AND STANDARD PRACTICES. (M) 2 L 7 2 4F RT A6WE 1997013000673 19970130 00673 WP 1997 1 30 TWAA9615819 1 19961212 A 5320 FORMER DOUG DC9 DC983 3022083 WP BS 1307 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9307R 49663 MCI - DURIGN OP-16, FOUND CORROSION AT STRINGER 28R AND 27L, FORMER FRAME LOWER FLANGE, FS 1307. REMOVED CORROSION PER SRM 51-10-03 AND REPAIRED PER SRM 53-03, PAGE 40. (M) 2 L 7 2 4F RT A6WE 1997013000679 19970130 00679 WP 1997 1 30 TWAA9615903 1 19961223 A 2530 953008119 SERVING CART LKHEED 1011 10113851 5265010 WP GALLEY FAILED A TWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 31013 193B1035 JFK - FLT 782 - DURING CRUISE, AISLE SERVING CART OVERHEATED AND EMITTED SMOKE. DISCONNECTED SERVING CART. FOUND SHORT ED HEATING ELEMENTS. REPLACED SERVING CART, MFG P/N 953008-119. SERVING CART OPERATION THEN CHECKED NORMAL. (M) 2 L 7 3 4F A23WE 1997013000681 19970130 00681 WP 1997 1 30 TWAA9616103 1 19961229 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 412EA 47733 STL - FLT 445 - DURING CRUISE, EGRESS LIGHTS ILLUMINATED. CYCLED SWITCH. FOUND BATTERY PACK, MFG P/N 2013-1, WEAK. RE PLACED BATTERY PACK. EGRESS LIGHT OPERATION THEN CHECKED NORMAL. (M) 2 L 7 2 4F RT A6WE 1997013000682 19970130 00682 NE 1997 1 30 TWAA9616105 2 19961227 A 7200 ENGINE BOEING 747 747131 1384881 NM PWA JT9 JT9D7A 52054 NE NR 2 FAILED A TWAA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 CE 05 53110 19676 STL - FLT 105 - DURING CLIMB, SHUT DOWN NR 2 ENGINE, S/N 4134, DUE TO ENGINE SURGE WITH HIGH EGT AND FUEL FLOW. FOUND M ETAL PARTICLES IN TAILPIPE. CHANGED ENGINE. ENGINE OPERATIONS AND INDICATION THEN CHECKED NORMAL. (M) 2 L 7 4 4F 4 F A20WE E20EA 1997013000683 19970130 00683 NM 1997 1 30 TWAA9616102 1 19961229 A 7930 A008032 BYPASS SWITCH BOEING 727 727231 1384079 NM NR 2 ENGINE FAILED A TWAA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 CE 05 54338 20843 STL - FLT 105 - DURING CRUISE, SHUT DOWN NR 2 ENGINE, S/N 3989, DUE TO OIL FILTER BYPASS LIGHT ILLUMINATION. FOUND MALF UNCTIONING OIL FILTER BYPASS SWITCH, MFG P/N A00803-2. REPLACED OIL FILTER BYPASS SWITCH. ENGINE INDICATION AND OPERAT ION THEN CHECKED NORMAL. (M) 2 L 7 3 4F A3WE 1997013000684 19970130 00684 NE 1997 1 30 TWAA9616002 2 19960804 A 7200 ENGINE LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B NE NR 3 MALFUNCTIONED A A TWAA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 15017 193B1063 LAX - DURING CLIMB, NR 3 ENGINE, S/N 4456 EXPERIENCED HIGH AVM. ENGINE WAS SHUT DOWN. INLET AND EXHAUST WERE CHECKED, CHIP DETECTORS CHECKED, AND GEARBOX WAS DRAINED AND SERVICED. NO DEFECTS WERE NOTED. ACCOMPLISHED TRIM BALANCED. (M) 2 L 7 3 4F 4 F A23WE E12EU 1997013000685 19970130 00685 NM 1997 1 30 TWAA9616101 1 19961227 A 8012 1774451 START VALVE BOEING 727 727231 1384079 NM NR 2 ENGINE FAILED A TWAA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 CE 05 54344 21631 STL - FLT 520 - DURING CLIMB, SHUT DOWN NR 2 ENGINE, S/N 1535, DUE TO START VALVE LIGHT ILLUMINATION. FOUND MALFUNCTION ED START VALVE, MFG P/N 1-77445-1. REPLACED START VALVE. START VALVE AND LIGHT OPERATION THEN CHECKED NORMAL. (M) 2 L 7 3 4F A3WE 1997013000686 19970130 00686 WP 1997 1 30 TWAA9616001 1 19961223 A 7930 42D1091A BYPASS SWITCH DOUG DC9 DC915 3022036 WP NR 2 ENGINE LEAKING A TWAA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 05 490SA 45798 STL - DURING CRUISE, SHUT DOWN NR 2 ENGINE, S/N 3811, DUE TO LOSS OF OIL QTY. FOUND OIL FILTER BYPASS SWITCH, MFG P/N 4 2D109-1A, LEAKING. REPLACED OIL FILTER BYPASS SWITCH. ENGINE OPERATION AND LEAKS CHECKS NORMAL. (M) 2 L 7 2 4F A6WE 1997013000687 19970130 00687 NM 1997 1 30 TWAA9615501 1 19961214 A 2613 894120 ELEMENT BOEING 727 727231 1384079 NM NR 2 ENGINE FAILED A TWAA O OTHER N FALSE WARNING CR CRUISE 1 CE 05 52311 19830 STL - FLT 475 - DURING CRUISE, SHUT DOWN NR 2 ENGINE, S/N 3953, DUE TO OVERHEAT WARNING. FOUND LOW RESISTANCE IN SENSIN G ELEMENT, MFG P/N 894120. REPLACED SENSING ELEMENT. ENGINE OVERHEAT WARNING SYSTEM OPERATION THEN CHECKED NORMAL. (M ) 2 L 7 3 4F A3WE 1997013000688 19970130 00688 WP 1997 1 30 TWAA9615901 1 19961221 A 3260 833703 PROX SENSOR DOUG DC9 DC982 3022082 WP LT MLG FAILED A TWAA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 912TW 49183 STL - FLT 29 - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED. CYCLED LA NDING GEAR. FOUND LEFT MAIN LANDING GEAR PROXIMITY SENSOR. LANDING GEAR INDICATION AND OPERATION THEN CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 1997013000689 19970130 00689 NM 1997 1 30 TWAA9615902 1 19961221 A 2121 6054571 GASPER FAN BOEING 747 747257B 1384853 NM CABIN FAILED A TWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 303TW 20116 LAX - FLT 849 - DURING CRUISE, GASPER FAN BECAME NOISY AND STARTED EMITTING BURNING ODOR INTO CABIN. TURNED OFF GASPER FAN. FOUND GASPER FAN HAD OVERHEATED. REPLACED GASPER FAN, MFG P/N 6054577. GASPER FAN OPERATION THEN CHECKED NORMAL. (M) 2 L 7 4 4F A20WE 1997013000690 19970130 00690 WP 1997 1 30 TWAA9616104 1 19961229 A 3222 STRUT DOUG DC9 DC931 3022065 WP NLG REQ'D SERVICE A TWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 05 983Z 47411 DSM - DSM - FLT 539 - AFTER TAKEOFF, LANDING GEAR SELECTOR HANDLE WAS LOCKED IN THE DOWN POSITION. RETURNED TO DSM. FO UND NOSE LANDING GEAR STRUT AIR PRESSURE LOW. SERVICED NOSE LANDING GEAR STRUT WITH NITROGEN. LANDING GEAR OPERATION T HEN CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 1997013000691 19970130 00691 WP 1997 1 30 97ZZZM104 1 19960927 A 3350 BATTERY PACK DOUG DC9 DC941 302207N WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 935L 47603 STL - FLT 541 - DURING CRUISE, EMERGENCY ESCAPE PATH LIGHTING ILLUMINATED AT ROWS 8 THROUGH 12. REMOVED AND REPLACED BA TTERY PACK, MFG P/N 2013-1A. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F A6WE 1997013000692 19970130 00692 NE 1997 1 30 97ZZZM105 2 19960927 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 1 FAILED A TWAA O OTHER Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 CE 05 953U 49267 1407 FLT 224 - GJT - DURING CRUISE, NR 1 ENGINE SPOOLED DOWN. AIRCRAFT DIVERTED TO GJT FOR AN ENGINE CHANGE. (M) 2 L 7 2 4F 4 F A6WE E9NE 1997013000694 19970130 00694 WP 1997 1 30 TWAA9615713 1 19961216 A 5320 ANGLE DOUG DC9 DC983 3022083 WP BS 1174-1212 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9307R 49663 MCI - DURING OP-16, FOUND CORROSION ON AFT CARGO FLOOR SUPPORT T-ANGLE, AND AROUND SCREW HOLES, FS 1174 TO FS 1212, RBL 14. REPLACED T-ANGLE PER SRM 51-01. (M) 2 L 7 2 4F RT A6WE 1997013000700 19970130 00700 WP 1997 1 30 USAAD97001 1 19960102 A 3260 LAMP DOUG DC9 DC931 3022065 WP LT MLG FAILED A USAA A UNSCHED LANDING P NO WARNING INDICATION AP APPROACH 1 EA 19 945VJ 47066 FLIGHT 1473 - PHL-DCA - ON APPROACH INTO DCA, LEFT MAIN GEAR DOWN AND LOCKED LIGHT DID NOT ILLUMINATE. DIVERTED TO BWI. RELAMPED LMG INDICATION LIGHT. (M) 2 L 7 2 4F A6WE 1997013000702 19970130 00702 WP 1997 1 30 USAAD96185 1 19961229 A 3150 WARNING LIGHT DOUG DC9 DC931 3022065 WP COCKPIT ILLUMINATED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 967VJ 47375 FLT 597 - SWF-PIT - MASTER WARNING LIGHT CAME ON SHORTLY AFTER TAKEOFF. THERE WERE NO OTHER RED WARNING OR ANNUNCIATOR LIGHTS. A TEST WAS DONE ON THE ANNUNCIATOR LIGHTS. ALL TESTED OK. AIRCRAFT WAS LEVELED AT 3000 FEET FOR RETURN TO FIE LD. AT FIRST POWER REDUCTION, THE MASTER WARNING DIMMED AND THEN WENT OUT. CHECKED MASTER CAUTION AND WARNING SYSTEM. RAN ENGINES AT HIGH POWER. CHECKED TAIL COMPARTMENT FOR LEAKS, NONE FOUND. UNABLE TO DUPLICATE. RETURNED A/C TO SERV ICE. (M) 2 L 7 2 4F A6WE 1997013000703 19970130 00703 WP 1997 1 30 USAAD96186 1 19961216 A 3350 60030451LB POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 981VJ 48157 CVG - FORWARD ENTRY, GALLEY SERVICE DOORS, AND COCKPIT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERIES. (M) 2 L 7 2 4F A6WE 1997013000704 19970130 00704 WP 1997 1 30 USAAD96180 1 19961213 A 3350 BULBS DOUG DC9 DC931 3022065 WP TAIL COMPT FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 939VJ 48120 SECTION 4 FLOOR TRACK LIGHTING, AFT F/A PANEL EXIT IDENTIFIER, CATWALK LOW LEVEL, AND TAILCONE RELEASE HANDLE EMERGENCY LIGHT INOPERATIVE. FOUND TWO LIGHT BULBS ON TAIL COMPARTMENT CATWALK SHORTED. REPLACED BULBS, CHECKS GOOD. (M) 2 L 7 2 4F A6WE 1997013000705 19970130 00705 WP 1997 1 30 USAAD96181 1 19961215 A 5244 LATCH DOUG DC9 DC981 3022081 WP ACCESS DOOR LOOSE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 803US 48035 FLT 1090 - BOS-CLT - AFTER TAKEOFF, ACCESS DOOR LIGHT CAME ON. RETURNED TO FIELD. RESECURED LOOSE LATCH. CHECKS GOOD. (M) 2 L 7 2 4F A6WE 1997013000706 19970130 00706 WP 1997 1 30 USAAD96182 1 19961213 A 3350 110049 CHARGER DOUG DC9 DC931 3022065 WP CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 943VJ 47058 DAY - AFT SECTION OF FLOOR TRACK EMERGENCY LIGHTING INOPERATIVE. REPLACED EMERGENCY LIGHT CHARGER AND BATTERY PACK. (M ) 2 L 7 2 4F A6WE 1997013000711 19970130 00711 WP 1997 1 30 HALA96191 1 19961228 A 3260 PROX SENSOR DOUG DC10 DC1010 3022110 WP LT MLG FAILED A HALA K NONE N FALSE WARNING CL CLIMB 1 WP 13 152AA 46707 HNL - FLT 11 - RIGHT MLG RED WARNING LIGHT CAME ON AFTER TAKEOFF AND REMAINED ON FOR MOST OF CLIMB-OUT. LIGHT THEN WENT OUT. THE GEAR AND DOOR WERE VISUALLY CHECKED AND FOUND TO BE UP. REMOVED AND REPLACED THE RIGHT MLG UPLOCK PROXIMITY SENSOR. THE GEAR SWING CHECKED OK. THE A/C WAS RELEASED FOR SERVICE (M) 2 L 7 3 4F A22WE 1997013000712 19970130 00712 GL 1997 1 30 HALA96192 2 19961228 A 7200 ENGINE DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 2 DAMAGED A A HALA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 WP 13 153AA 61556 46708 451296 LAX - FLT 921 - AIRCRAFT 153 DIVERTED TO LAX NR 2 ENGINE VIBRATION FELT IN THE RUDDER PEDALS AND IN THE AFT CABIN AT POW ER SETTINGS ABOVE 95 PERCENT N2. WHEN POWER WAS REDUCED BELOW 95 PERCENT, THE VIBRATION WENT AWAY. THE HIGHER THE POWE R SETTING, THE GREATER THE VIBRATION. DURING TROUBLESHOT LAX REPORTED OIL IN THE ENGINE SPINNER AND FOD DAMAGE TO THE 1 ST STAGE FAN. AIRCRAFT WAS SWAPPED AND ENGINE CHANGE PLANNED FOR POSITION TWO. (M) 2 L 7 3 4F 4 F A22WE E23EA 1997013000714 19970130 00714 WP 1997 1 30 97ZZZM106 1 19961212 A 5711 SPAR DOUG DC9 DC932 3022066 WP WS 58.458 CRACKED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND LEFT WING MAIN TANK REAR SPAR LOWER FLANGE XW 58.458 HAS A .125 CRACK FROM RADIUS TO A FASTENER HOLE. (M) 2 L 7 2 4F A6WE 1997013000733 19970130 00733 WP 1997 1 30 97ZZZM126 1 19960103 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 996 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THAT STRINGER NR 29 LEFT END FITTING STATION 996 WAS EXF OLIATED BEYOND LIMITS. REMOVED STRINGER 29 END CAP IAW DC9 SRM 53-11-3, INSTALLED NEW END CAP IAW DC-9 SRM 53-11-3 AND 51-30-1 INSTALLED BOOMERANG PANEL IAW DC-9 SRM 51-30-1. (M) 2 L 7 2 4F A6WE 1997013000734 19970130 00734 WP 1997 1 30 97ZZZM127 1 19961206 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 996 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND AFT PRESSURE BULKHEAD MAIN FRAME STATION 996 RBL 56 CORR ODED AT FASTENER HOLE. DC9 SRM 53-01 FIG 1 REVEALED CORROSION LIMITS (MICROMETER A-1729). CUT OUT CORRODED FRAME IAW D C9 SRM 51-10-2. FABRICATED 1 CHIP SPLICE (7075T6) AND 1 EACH FRAME SECTION (7075T6). ANNEALED AND FORMED PARTS IAW DC9 SRM 51-10-2 AND 51-10-2A. HEAT TREATED PARTS IAW DC9 SRM 51-10-2A. DRILLED, DEBURRED, FIT AND TRIMMED PARTS IAW DC9 S RM 51-10-4, 51-10-2. ALODINED AND PRIMED PARTS IAW DC9 SRM 51-10-3. INSTALLED PARTS IAW DC9 SRM 51-30-2, 51-30-1. INS TALLED ISOLATORS IAW RES 1 02780. 2 L 7 2 4F A6WE 1997013000739 19970130 00739 WP 1997 1 30 VJ96006 1 19961209 A 2430 905D9881 CURRENT TRANS DOUG DC9 DC932 3022066 WP RT ENGINE FAILED A VJ6A A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 11 945VV 47238 EN ROUTE ATL-CMH - AIR INTERRUPTED AND RETURNED TO ATL AS A PRECAUTIONARY MEASURE BECAUSE CROSS TIE FAILED AND RIGHT GEN ERATOR CAME OFF LINE. RESET GENERATOR. REMOVED AND REPLACED RT GENERATOR CONTROL PANEL, P/N 976J254-4, S/N Y020667ABD, AND CURRENT TRANSFORMER, P/N 905D988-1, S/N SM5871. LATTER PART ATTRIBUTED TO CROSS TIE FAILURE. OPS CHECKED NORMAL I AW MM 24-20-0. (M) 2 L 7 2 4F A6WE 1997013000740 19970130 00740 EA 1997 1 30 97ZZZM132 1 19961025 A 6120 3032970C CABLE DHAV DHC7 DHC7102 2802708 EA NR 4 ENG SEPARATED A L CICA E ENGINE SHUTDOWN A X FLAME/FIRE ENGINE FLAMEOUT TX TAXI/GRND HDL 1 SO 17 703MG 103 FLT 4908 - PID-MIA - AN ATTEMPT TO FEATHER, NR 4 ENG FAILED. FUEL SHUTOFF HANDLE WAS PULLED AND THE T5 TEMP INCREASED T O 1000 DEG. 'T' HANDLE WAS RESET AND TEMP DROPPED AND ENG CONTINUED TO RUN. MX PULLED 'T' HANDLE AND THE T5 WENT TO 60 0 DEG. START BUTTON WAS PUSHED AND THE TEMP BEGAN TO INCREASE PAST 1000 DEG. FLAMES WERE COMING OUT OF EXHAUST. FIRE EXTING BOTTLES WERE FIRED AND FLAMES OUT. A/C WAS INSPECTED AND FOUND TO BE SAFE FOR 3 ENG FERRY FLT TO FLL. ENG WAS R /R. PROP GOV PUSH PULL SEPARATION CAUSED THE COND LVR NOT TO GO TO SHUTOFF. THE ENG WAS INSPECTED FOR OVERTEMP COND. 2 H 7 4 4T A20EA 1997013000741 19970130 00741 NM 1997 1 30 MZZA96210 1 19961222 A 5320 WEB BOEING 727 727224 1384076 NM BS 1213 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69741 22250 TNN - DURING S-CHECK INSPECTION ON A/C AT AIR ASIA, ONE INCH LONG CRACK WAS FOUND ON LT SIDE LOWER VENTRAL STAIRWALL TOR QUE BOX WEB AT BS 1213 LIGHTENING HOLE CUTOUT. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM 51-40-2 FIGURE 1. R EF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 810531 (SEQ NR 02143). (M) 2 L 7 3 4F A3WE 1997013000742 19970130 00742 NM 1997 1 30 MZZA96211 1 19961222 A 5320 WEB BOEING 727 727224 1384076 NM BS 1225 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69741 22250 TNN - DURING S-CHECK INSPECTION ON A/C AT AIR ASIA, .5 INCH LONG CRACK WAS FOUND ON LT SIDE LOWER VENTRAL STAIRWALL TORQ UE BOX WEB AT BS 1225 LIGHTENING HOLE CUTOUT. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM 51-40-2 FIGURE 1. R EF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 810532 (SEQ NR 02144). (M) 2 L 7 3 4F A3WE 1997013000743 19970130 00743 NM 1997 1 30 MZZA96212 1 19961222 A 5320 WEB BOEING 727 727224 1384076 NM BS 1220 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69741 22250 TNN - DURING S-CHECK INSPECTION ON A/C AT AIR ASIA, .5 INCH LONG CRACK WAS FOUND ON LEFT SIDE LOWER VENTRAL STAIRWALL TO RQUE BOX WEB AT BS 1220 LIGHTENING HOLE CUTOUT. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM 51-40-2 FIGURE 1. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 810533 (SEQ NR 02145). (M) 2 L 7 3 4F A3WE 1997013000744 19970130 00744 NM 1997 1 30 MZZA96213 1 19961222 A 5320 WEB BOEING 727 727224 1384076 NM BS 1225-1303 OIL CANNING A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69741 22250 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING WAS FOUND ON LOWER VENTRAL STAIRWALL TORQUE BOX AT THE FOLLOWING AREAS, RT SIDE BETWEEN BS 1283 AND BS 1303, LEFT SIDE BETWEEN BS 1243 AND BS 1283, LT SIDE AT BS 1225. TH E DAMAGED WEB WERE REPAIRED PER B727 SRM 51-40-2 FIGURE 1. REF, HANGAR NON ROUTINE REPAIR ITEM CARDS NR 810539, 810540 AND 810541 (SEQ NR 02151, 02152 AND 02153). (M) 2 L 7 3 4F A3WE 1997013000745 19970130 00745 NM 1997 1 30 MZZA96214 1 19961223 A 5330 SKIN BOEING 727 727224 1384076 NM BS 1140 DENTED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69741 22250 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DENT WAS FOUND ON FUSELAGE SKIN AT BS 1140 BETWEEN STRINGER 20L AND STRINGER 21L AND THE DENT DEPTH BEYOND THE SPECIFIED LIMIT. THE DAMAGED SKIN WAS REPAIRED PER B727 SRM 53-30-3 FIG URE 1. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 810625 (SEQ NR 02201). (M) 2 L 7 3 4F A3WE 1997013000746 19970130 00746 NM 1997 1 30 MZZA96215 1 19961224 A 3350 SIGN COVER BOEING 727 727224 1384076 NM CABIN BROKEN A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69741 22250 TNN - DURING S-CHECK INSPECTION ON A/C AT AIR ASIA, BROKEN 'EXIT' SIGN COVERS WERE FOUND ON PASSENGER CABIN COMPARTMENT AT THE FOLLOWING POSITIONS; SIDE OF R1 GALLEY DOOR, SIDE OF R2 GALLEY DOOR, SIDE OF RT FORWARD EMERGENCY EXIT DOOR. THE DAMAGED 'EXIT' SIGN ASSEMBLIES WERE REMOVED AND REPLACED WITH P/N BR9279-16 PER B727 MM 3350-11 AND OPERATIONAL CHECK F OUND SATISFACTORY. REF, HANGAR NON ROUTINE REPAIR ITEM CARDS NR 814753, 814754 AND 814755 (SEQ NR 02239, 02240 AND 0224 1). (M) 2 L 7 3 4F A3WE 1997013000747 19970130 00747 NM 1997 1 30 MZZA96216 1 19961224 A 3350 SIGN COVER BOEING 727 727224 1384076 NM CABIN BROKEN A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69741 22250 TNN - DURING S-CHECK INSPECTION ON A/C AT AIR ASIA, BROKEN 'EXIT' SIGN COVER WAS FOUND ON LEFT AFT EMERGENCY EXIT DOOR. THE DAMAGED 'EXIT' SIGN ASSEMBLY WAS REMOVED AND REPLACED WITH P/N BR9279-105 PER B727 MM 33-50-11 AND OPERATIONAL CHEC K FOUND SATISFACTORY. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 814756 (SEQ NR 02242) (M) 2 L 7 3 4F A3WE 1997013000748 19970130 00748 NM 1997 1 30 MZZA96217 1 19961221 A 5755 SKIN BOEING 727 727224 1384076 NM NR 3 SPOILER DISBONDED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69741 22250 TNN - DURING S-CHECK INSPECTION ON A/C AT AIR ASIA, DISBONDED WERE FOND ON LEFT WING NR 3 SPOILER T/E UPPER SKIN EXISTIN G REPAIR DOUBLER AT OUTBOARD AND INBOARD CORNERS. THE EXISTING REPAIR DOUBLERS (2.5 INCH BY 6 INCH ON OUTBOARD CORNER, 6.2 INCH BY 8 INCH ON INBOARD CORNER) WERE REMOVED AND REPAIRED PER B727 SRM 51-40-6. REF, HANGAR NON ROUTINE REPAIR IT EM CARD NR 810307 (SEQ NR 05007) (M) 2 L 7 3 4F A3WE 1997013000749 19970130 00749 NM 1997 1 30 MZZA96218 1 19961221 A 5755 SKIN BOEING 727 727224 1384076 NM NR 4 SPOILER DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69741 22250 TNN - DURING S-CHECK INSPECTION ON A/C AT AIR ASIA, DELAMINATION WERE FOUND ON LT WING NR 4 SPOILER T/E UPPER SKIN AT OU TBOARD AND INBOARD CORNERS. THE DAMAGED SKIN 2.5 INCH BY 6.4 INCH IN SIZE (ON OUTBOARD CORNER) AND 2.5 INCH BY 12.5 INC H IN SIZE (ON INBOARD CORNER) WERE TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. REF, HANGAR NON ROUTINE REPAIR ITEM C ARD 810308 (SEQ NR 05008). (M) 2 L 7 3 4F A3WE 1997013000750 19970130 00750 NM 1997 1 30 MZZA96219 1 19961222 A 5753 SKIN BOEING 727 727224 1384076 NM LT TE AFT FLAP DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69741 22250 TNN - DURING S-CHECK INSPECTION ON A/C AT AIR ASIA, DELAMINATION WAS FOUND ON LT WING INBOARD T/E AFT FLAP T/E UPPER SKI N AT WBL 100. THE DAMAGED SKIN 1.75 INCH BY 8.5 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. REF, H ANGAR NON ROUTINE REPAIR ITEM CARD NR 810396 (SEQ NR 05046). (M) 2 L 7 3 4F A3WE 1997013000751 19970130 00751 NM 1997 1 30 MZZA96220 1 19961222 A 5753 SKIN BOEING 727 727224 1384076 NM LT AFT TE FLAP DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69741 22250 TNN - DURING S-CHECK INSPECTION ON A/C AT AIR ASIA, DELAMINATION WAS FOUND ON LT WING INBOARD T/E AFT FLAP T/E UPPER SKI N AT WBL 77. THE DAMAGED SKIN 2.2 INBY BY 7.8 INCH SIZE WAS TRIMED OUT AND REPAIRED PER B727 SRM 51-40-6. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 810397 9SEQ NR 05047). (M) 2 L 7 3 4F A3WE 1997013000752 19970130 00752 NM 1997 1 30 MZZA96221 1 19961220 A 5755 SKIN BOEING 727 727224 1384076 NM NR 14 SPOILER DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69741 22250 TNN - DURING S-CHECK INSPECTION ON A/C AT AIR ASIA, DELAMINATION WAS FOUND RT WING NR 14 SPOILER T/E UPPER SKIN AT OUTBO ARD AFT CORNER. THE DAMAGED SKIN 2.75 INCH BY 10.5 INCH WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 810342 (SEQ NR 06012) (M) 2 L 7 3 4F A3WE 1997013000753 19970130 00753 NM 1997 1 30 MZZA96222 1 19961220 A 5755 SKIN BOEING 727 727224 1384076 NM NR 8 SPOILER DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69741 22250 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION DISBONDED WAS FOUND ON RT WING NR 8 SPOILER UPPER SKIN AND SKIN EXISTING REPAIR DOUBLER. THE DAMAGED SKIN AND EXISTING REPAIR DOUBLER 4 INCH BY 27 INCH WAS TRIMMED OUT A ND REPAIRED PER B727 SRM 51-40-6. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 810343 (SEQ NR 06013). (M) 2 L 7 3 4F A3WE 1997013000754 19970130 00754 NM 1997 1 30 MZZA96223 1 19961222 A 5751 SKIN BOEING 727 727224 1384076 NM OUTBOARD AILERON TORN A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69741 22250 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, RT WING OUTBOARD AILERON T/E HONEYCOMB LOWER SKIN WAS FOUND TO BE TORN AT AFT EDGE. THE DAMAGED SKIN .375 INCH BY 1 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. R EF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 810413 (SEQ NR 06043). (M) 2 L 7 3 4F A3WE 1997013000755 19970130 00755 NM 1997 1 30 MZZA96224 1 19961222 A 5753 SKIN BOEING 727 727224 1384076 NM NR 4 FORE FLAP DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69741 22250 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON RT WING OUTBOARD T/E FORE FLAP L/E UP PER SKIN AT WBL 417. THE DAMAGED SKIN 2.2 INCH BY 3.2 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. R EF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 810414 (SEQ NR 06044). (M) 2 L 7 3 4F A3WE 1997013000756 19970130 00756 NM 1997 1 30 MZZA96225 1 19961224 A 5320 WEB BOEING 727 727224 1384076 NM TAIL SKIN COMP CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69741 22250 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON TAIL SKIN COMPARTMENT RT SIDE OF WEB AT AFT LOWER POSITION. THE CORRODED WEB WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-2 FIGURE 1. REF, HANGAR NO N ROUTINE REPAIR ITEM CARD NR 840802 (SEQ NR 01150). (M) 2 L 7 3 4F A3WE 1997013000757 19970130 00757 NM 1997 1 30 MZZA96226 1 19961224 A 5320 ANGLE BOEING 727 727224 1384076 NM TAIL SKID CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 69741 22250 TNN - DURING S-CHECK INSPECTION ON A/C AT AIR ASIA, BULGE WAS FOUND ON TAIL SKID COMPARTMENT CUTOUT AT REAR POSITION. T HE CORRODED ANGLE WAS REMOVED REPAIRED PER B727 SRM 51-40-3 FIG 1. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 840803 9 SEQ NR 01151). (M) 2 L 7 3 4F A3WE 1997013000758 19970130 00758 EA 1997 1 30 97ZZZM133 2 19961127 A 7310 MS28882A6 CHECK VALVE DHAV DHC7 DHC7102 2802708 EA PWA PT6 PT6A50 52043 EA NR 1 ENGINE LEAKING A CICA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 17 4860J 19 PCE86022 FLT NR 783 - FLL-PBI - PILOT REPORTED SMOKE COMING OUT OF NR 1 ENGINE INTAKE AFTER SHUTDOWN. THE AIRCRAFT WAS INSPECTED AND FOUND SAFE FOR 3 ENGINE FERRY FLIGHT TO FLL. EMERGENCY FUEL SHUTOFF T-HANDLE WAS PULLED. UPON ARRIVAL AT FLL, INS PECTION FOUND FUEL DUMP CHECK VALVE LEAKING. REPLACED FUEL DUMP CHECK VALVE AND LEAK CHECKED GOOD. AIRCRAFT RELEASED F OR FLIGHT. (M) 2 H 7 4 4T 4 T A20EA E4EA 1997013000759 19970130 00759 EA 1997 1 30 97ZZZM134 2 19961104 A 7220 3027707 COMP INLET CASE DHAV DHC7 DHC7102 2802708 EA PWA PT6 PT6A50 52043 EA NR 4 ENGINE CRACKED A CICA E ENGINE SHUTDOWN M Y OVER TEMP ENGINE STOPPAGE DE DESCENT 1 SO 17 234SL 19612 24 FLT 4909 - MIA-PID - PILOT REPORTED, NR 4 ENGINE FAILED IN FLIGHT (TORQUE OFF, T5 RISE) AND PROP LOCKED UP. ENGINE SHUT DOWN. THE AIRCRAFT WAS INSPECTED AND FOUND SAFE FOR 3 ENGNIE FERRY TO FLL. THE NR 4 T-HANDLE WAS SECURED. UPON RETURN TO FLL, INSPECTION INDICATED NR 4 ENGINE COMPRESSOR INLET CASE HAS MULTIPLE FRACTURES. ENGINE WAS REMOVED AND WILL BE SHIPPED TO REPAIR FACILITY FOR DETERMINATION OF CAUSE AND REPAIR. (M) 2 H 7 4 4T 4 T A20EA E4EA 1997013000760 19970130 00760 NE 1997 1 30 P2EA96009 2 19961012 A 7261 659030527 FILTER BOEING 737 737247 138448D NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE CLOGGED A P2EA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 05 204AU 19603 FLT 160 MDW - NR 2 ENGINE 'OIL FILTER BYPASS' ILLUMINATED AFTER TAKEOFF. POWER WAS BROUGHT BACK AND LIGHT EXTINGUISHED MOMENTARILY, THEN CAME BACK ON. PRECAUTIONARY LANDING AT MDW. REMOVED THE NR 2 ENGINE OIL FILTER AND FOUND CONTAMINATI ON, REPLACED OIL FILTER PER PWA JT8D MM 72-61-0. RAN ENGINE AND PERFORMED LEAK CHECK. NO LEAKS NOTED. (M) 2 L 7 2 4F 4 F A16WE E2EA 1997013000765 19970130 00765 WP 1997 1 30 CALA9700102 1 19961204 A 5754 SKIN DOUG DC10 DC1030 3023501 WP NR 3 SLAT DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37078 46926 INSPECTION FOUND A 5 INCH DIAMETER BY 0.060 DEEP DENT IN OUTBOARD RT WING NR 3 SLAT. A SKIN AND DOUBLER REPAIR WAS INST ALLED IAW SRM 57-10-00, FIGURE 11. 2 L 7 3 4F A22WE 1997013000766 19970130 00766 WP 1997 1 30 CALA9700103 1 19961203 A 5720 WING TIP DOUG DC10 DC1030 3023501 WP WS 988 CREASED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37078 46926 INSPECTION FOUND A 3L BY .5W BY 0.080D CREASE IN RT WING TIP AT XW 988, BETWEEN TIP LEADING EDGE AND TRAILING EDGE. A F ILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-00-01, FIGURE 4 AND SRM 57-31-01 FIGURE 3. 2 L 7 3 4F A22WE 1997013000769 19970130 00769 WP 1997 1 30 CALA9700106 1 19961218 A 5754 SLAT DOUG DC10 DC1030 3023501 WP NR 6 LE SLAT GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37077 46981 INSPECTION FOUND RT NR 6 SLAT CHAFED AND GOUGED AT INBOARD END, 12 INCHES UP FROM L/E TIP. THE SLAT WAS REPAIRED IAW EC RA 5750-02573. 2 L 7 3 4F A22WE 1997013000770 19970130 00770 WP 1997 1 30 CALA9700107 1 19961208 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 472 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37077 46981 INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 472 LBL 54. A FLOOR SUPPORT REPAIR WAS FABRICATED AND INSTALLED IA W SRM 53-00-01, 51-21-01, 51-31-01, 51-35-01 AND 53-60-01 FIGURE 1. 2 L 7 3 4F A22WE 1997013100003 19970131 00003 1997 1 31 RAIA961214 4 19961219 A 3414 39948B2236 AIRSPEED IND BAG JETSTM JETSTM3201 1500217 EU RT COCKPIT STUCK A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 424AM 9016 865 PAH - FLT 7367 - FIRST OFFICERS AIRSPEED INDICATOR STAYED AT ZERO. MAINTENANCE REPLACED THE FLIGHT OFFICERS AIRSPEED IN DICATOR. (M) 2 L 7 2 4T RT A56EU 1997020600072 19970206 00072 EA 1997 2 6 CA960909033 2 19960826 A 7414 1068256011 MAGNETO BENDIX CESSNA 182 R182 2072734 CE LYC O540 O540J3C5 41532 EA MCAULY 2D34C B2D34C214 GL INTERNAL FAULTY W C D ABORTED TAKEOFF RETURN TO BLOCK E Y VIBRATION/BUFFET ENGINE STOPPAGE TO TAKEOFF 1 CA 1542 R22698K L2027840A 790258 (CAN) MAGNETO CUT OUT AT ACCELERATION ON TAKEOFF. 1 H 7 1 3O 3 O RT 3A13 E295 5 C P7EA 1997020600073 19970206 00073 EU 1997 2 6 CA960909034 2 19960729 A 7322 CCU515106AS FUEL CONTROL LUCAS BRAERO 748 HS7482A 4231001 EU RROYCE DART DART5342 EU #2 ENGINE FAULTY W K NONE Y ENGINE STOPPAGE DE DESCENT 1 CA B10752 18129 (CAN) IN DESCENT FROM 13,000 FEET WITH RPM AT 13,500, FUEL TRIM AT 20 PERCENT & FUEL HEAT IN MANUAL, AT 3,000 FEET #2 EN GINE STARTED TO AUTOFEATHER. THE PILOT TRIMMED UP 80 PERCENT & APPLIED FULL POWER, ENGINE WAS SLOW TO SPOOL UP. #2 ENGIN E FUEL CONTROL WAS REPLACED, & THE AIRCRAFT RETURNED TO SERVICE. THIS IS THE THIRD INSTANCE OF POWER FLUCTUATION WITH FU EL HEAT ON. THE AIRLINE IS TREATING THIS AS A RECURRING DEFECT. JETSTREAM HAS BEEN CONTACTED FOR INPUT. AIRLINE SUSPECTS OVERHEATING OF FUEL IN WARM OUTSIDE AIR TEMPERATURE (OAT), ALTHOUGH FLIGHT MANUAL DOES NOT SUPPLY A WARNING IN THIS REG ARD, IT DOES NOTE THAT "WHEN OAT HAS NOT BEEN BELOW 5 DEGREES C THROUGHOUT THE FLIGHT, IT IS NOT NECESSARY TO CARRY OUT 2 L 7 2 3T 4 T A24EU A196 1997020600074 19970206 00074 NE 1997 2 6 CA960909035 2 19960824 A 8530 CYLINDER DHAV DHC3 DHC3 2800202 EA PWA R1340 R134059 52016 NE #1 & #2 POSITION CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 3264212 (CAN) #1 AND #2 CYLINDERS WERE FOUND CRACKED ON THE CENTRE OF THE HEAD. 1 H 7 1 3R 3 R A815 5E2 1997020600075 19970206 00075 WP 1997 2 6 CA960909036 1 19960814 A 2820 1515816147 FUEL LINE LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE FS 1975 PUNCTURED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 10242 (CAN) FUEL LEAK AT #2 ENGINE. RIGID FUEL TUBE PUNCTURED BEHIND CLAMP AT REAR SECTION BETWEEN FS 1975 AND 1860 OVER WL200 . LINE REPLACED. 2 L 7 3 4F 4 F A23WE E12EU 1997020600077 19970206 00077 NM 1997 2 6 CA960909038 1 19960808 A 3242 26011825 BRAKE BENDIX 26011825 BOEING 727 727217 NM PWA JT8 JT8D17 52049 NE NR 2 WORN W K NONE O OTHER IN INSP/MAINT 1 CA 2549 688128 (CAN) DURING WALKAROUND #2 BRAKE SHOWED SIGNS OF METAL SHAVINGS. ALL BRAKE PADS WERE SHEARED OFF AND THE BRAKE SEIZED. S OLID RIVETS WERE USED. TIRE HAD FLAT SPOTS. BRAKE REPLACED. 2 L 7 3 4F 4 F RT A3WE E2EA 1997020600078 19970206 00078 CE 1997 2 6 CA960909039 1 19960812 A 2810 TANK BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE TOP OF WING TANK LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA PCE114459 (CAN) FUEL LEAK FOUND ON THE TOP RIGHT FUEL TANK (WING) STA. 117.0 TO 159.0. THE FUEL WAS LEAKING FROM A LOOSE RIVET. RE PAIR WAS CARRIED OUT AS PER RAYTHEON REPAIR DRAWING KIT 129-4017-1. 2 L 7 2 4T 4 T RT A24CE E26NE 1997020600079 19970206 00079 WP 1997 2 6 CA960909040 1 19960828 A 2760 1529417113 FITTING LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE NR 2 LT SPOILER BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 10471 (CAN) #2 LH SPOILER ATTACH FITTING BROKEN IN HALF, REPLACED. 2 L 7 3 4F 4 F A23WE E12EU 1997020600080 19970206 00080 EA 1997 2 6 CA960909041 1 19960813 A 2430 MS24171D1 RELAY DHAV DHC6 DHC6300 EA PWA PT6 PT6A27 52043 EA BATTERY STUCK CLOSED W K NONE O OTHER TX TAXI/GRND HDL 1 CA 24 PCE41911 (CAN) AFTER ENGINE SHUTDOWN, BATTERY SWITCH AND MASTER OFF, BUT DID NOT DISCONNECT BATTERY. BATTERY CONNECTOR HAD TO BE DISCONNECTED TO REMOVE BATTERY POWER. BATTERY RELAY WAS TAPPED AND THIS OPENED RELAY. RELAY REPLACED. 1 H 7 2 3T 4 T A9EA E4EA 1997020600086 19970206 00086 NE 1997 2 6 CA960910001 2 19960724 A 8530 STUD DHAV DHC2 DHC2EVANS 2801832 EA PWA R985 R985AN14B 52008 NE #1 CYLINDER BROKEN W A UNSCHED LANDING K E FLUID LOSS VIBRATION/BUFFET CR CRUISE 1 CA 901 JP208136 (CAN) PILOT LANDED AFTER IN FLIGHT ENGINE VIBRATION. THERE WAS OIL ON THE WIND SCREEN. INSPECTION REVEALED THE #1 CYLIND ER WAS LOOSE ON THE CRANKCASE, EIGHT CYLINDER HOLDDOWN STUDS WERE FOUND SHEARED FLUSH WITH THE FLANGE THE REMAINING TWO STUDS WERE FOUND LOOSE. 1 H 7 1 3O 3 R A806 5E1 1997020600087 19970206 00087 SO 1997 2 6 CA960910003 2 19960814 A 8530 SA629404 VALVE CONT C61AIR CESSNA 150 150M 2071830 CE CONT O200 O200A 17020 SO MCAULY 1A102 1A102OCM GL EXH VALVE GUIDE STUCK OPEN W A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 CA 773 252634A48 G15741 (CAN) WHILE IN CRUISE AN ENGINE CYLINDER EXHAUST VALVE STUCK OPEN. THE SUBMITTER STATES THAT THIS ENGINE WAS OPERATED WI TH MOGAS, WHICH HE SAYS IS HARD ON THE VALVES AND SUGGESTS THAT 80/87 OR 100 LOW LEAD GASOLINE SHOULD BE USED. 1 H 7 1 3O 3 O 3A19 E252 5 N P918 1997020600088 19970206 00088 SW 1997 2 6 CA960910005 1 19960609 A 2742 M0915 LOCK PIN SIMMONDS DL5040M5 SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP STAB ACTUATOR SHEARED W A K NONE O OTHER IN INSP/MAINT 1 CA 2999 M0915 P54183 (CAN) ACTUATOR HAD REFURBISHED NUTS AND SHAFTS INSTALLED AT PREVIOUS OVERHAUL INSPECTION AT 3000 HOURS FOUND RH SHAFT F REE END PLAY AT MID POINT OF TRAVEL WAS APPROXIMATELY 0 010, LEFT SHAFT FREE END PLAY NEGLIGIBLE, LEFT ROD END ASSEMBLY INNER SHAFT COULD BE ROTATED INSIDE THE SECOND SHAFT DUE TO RESPECTIVE SHAFT LOCK PIN BEING SHEARED. THIS LOOSE SHAFT RE SULTED IN THE LOAD BEING CARRIED BY THAT SHAFT BEING REDUCED. FAA AD 93-15-02R1 DOES NOT ADDRESS THIS ISSUE. 2 L 7 2 4T 4 T RT A8SW E4WE 1997020600089 19970206 00089 EA 1997 2 6 CA960910006 2 19960822 A 8520 3813 STUD PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2B 41532 EA #2 CYLINDER BROKEN W A E ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 CA 383 L27861 (CAN) DURING CRUISE A SLIGHT OIL LEAK WAS NOTICED ON THE #2 ENGINE COWLING, A LOSS OF 3 TO 4 INCHES OF MANIFOLD PRESSURE AND A DROP IN OIL PRESSURE. THE ENGINE WAS SHUTDOWN. POST FLIGHT INSPECTION FOUND THE #2 CYLINDER HAD SEPARATED FROM TH E CRANKCASE, DUE TO THREE BROKEN STUDS. THE CYLINDER BASE FLANGE WAS BROKEN WHERE IT ATTACHES TO THE THROUGH BOLT. ALL T HECYLINDER BASE STUDS AND THROUGH BOLTS WERE REPLACED. A CERTIFIED CYLINDER AND PISTON WERE REINSTALLED AND THE AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 3O 3 O A20SO E14EA 1997020600090 19970206 00090 SO 1997 2 6 CA960910007 1 19960828 A 3230 762554 ROD END PIPER PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2B 41532 EA MLG ACTUATOR CRACKED W A K NONE O OTHER IN INSP/MAINT 1 CA 5275 RL56461 (CAN) DURING MAIN LANDING GEAR MAINTENANCE THE RIGHT HAND MLG ROD END WAS FOUND CRACKED. FURTHER INSPECTION FOUND THE LE FT HAND ROD END WAS ALSO CRACKED. BOTH ROD ENDS WERE CRACKED IN THE THREADED PORTION. THE SUBMITTER STATES THAT THIS ITE M IS DIFFICULT TO INSPECT WHILE ON THE AIRCRAFT. A SEARCH OF THE SDR DATABASE FOUND FOUR (4) SIMILAR OCCURRENCES. 1 L 7 2 3O 3 O A20SO E14EA 1997020600091 19970206 00091 SO 1997 2 6 CA960910008 2 19960831 A 8530 646612 VALVE CESSNA 150 150M 2071830 CE CONT O200 O200A 17020 SO MCAULY 1A102 1A102OCM GL #2 CYL EXH STUCK OPEN W A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 CA 636 636 242508H K20043 (CAN) EXHAUST VALVE STUCK IN OPEN POSITION ON #2 CYLINDER. 1 H 7 1 3O 3 O 3A19 E252 5 N P918 1997020600092 19970206 00092 NM 1997 2 6 CA960910009 1 19960608 A 5210 H22581 PIN BOEING 747 747133 138448B NM PWA JT9 JT9D7 52054 NE OVERHEAD HATCH BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA P685933 (CAN) CREW COMPARTMENT OVERHEAD HATCH JAMMED. PIN BROKEN, REPLACED. 2 L 7 4 4F 4 F A20WE E20EA 1997020600094 19970206 00094 EU 1997 2 6 CA960910011 1 19960718 A 2750 FLAP AIRBUS 320 A320211 3930320 EU FLAP 2 MALFUNCTION W A K NONE O OTHER DE DESCENT 1 CA (CAN) FLAPS LOCKED ON SELECTION TO FLAP 2. #1 AND #2 SFCC (SLAT/FLAT CONTROL CO MPUTER) TESTED. ALL ROTARY ACTUATORS C HECKED. NO FAULT FOUND. FLAT/SLAT OPERATI ON CARRIED OUT SEVERAL TIMES. UNABLE TO DUPLICATE FAULT. 2 L 7 2 4F RT A28NM 1997020600095 19970206 00095 EA 1997 2 6 CA960910012 1 19960720 A 3230 7179015 SELECTOR EATON CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE LANDING GEAR FAILED W O OTHER J WARNING INDICATION CL CLIMB 1 CA 1539 808307 (CAN) LANDING GEAR DID NOT RETRACT ON FIRST ATTEMPT. OK ON RESELECTION. BOTH LANDING GEAR SELECTOR AND PSEU (P/N 8-648-0 6) REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 1997020600096 19970206 00096 NM 1997 2 6 CA960910013 1 19960725 A 2420 LUG BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE APU C PHASE BROKEN W K NONE O B OTHER SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA P707535 (CAN) PRIOR TO DEPARTURE APU (AUXILIARY POWER UNIT) GENERATOR FIELD TRIPPED AND ELECTRICAL SWEET SMELL IN CABIN. C-PHASE LUG BROKEN. LUG AND GENERATOR REPLACED. 2 L 7 2 4F 4 F RT A1NM E3NE 1997020600097 19970206 00097 EU 1997 2 6 CA960910015 1 19960730 A 2421 740119D GENERATOR AIRBUS 320 A320211 3930320 EU #1 IDG FAILED W O OTHER O OTHER CR CRUISE 1 CA (CAN) FLIGHT DISPATCHED UNDER M.E.L. #2 INTEGRATED DRIVE GENERATOR (IDG) DISCONNECTED. APPROXIMATELY 1 HOUR INTO FLIGHT, #1 IDG DISCONNECTED DUE TO LOW OIL PRESSURE. FLIGHT OPERATED WITH APU GENERATOR. MAINTENANCE CHANGED #1 IDG CHECKED SER VICEABLE. 2 L 7 2 4F RT A28NM 1997020600098 19970206 00098 WP 1997 2 6 CA960910017 1 19960805 A 5240 591479237 SERVICE PANEL DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE LAVATORY SERVICE MISSING W K NONE D INFLIGHT SEPARATION IN INSP/MAINT 1 CA P656973D (CAN) ON ARRIVAL AT DESTINATION, AFT LAVATORY SERVICE PANEL FOUND MISSING. HINGE ASSEMBLY REMOVED FOR INSPECTION FOUND T O BE SERVICEABLE. NEW PANEL ASSEMBLY INSTALLED. 2 L 7 2 4F 4 F A6WE E2EA 1997020600099 19970206 00099 1997 2 6 CA960910018 4 19960806 A 2211 25866873 ROLL COMPUTER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE AUTO PILOT ERRATIC W A O OTHER F FLT CONT AFFECTED CR CRUISE 1 CA P657759D (CAN) WHEN AUTO PILOT ENGAGED AT FL 290 AIRCRAFT TURNED RIGHT SEVERELY AND AUTO PILOT DISCONNECTED IMMEDIATELY. AILERON SHOWING MORE THAN 1 NEEDLE TURN. ONE FLIGHT ATTENDANT SLIGHTLY INJURED. 2 L 7 2 4F 4 F A6WE E2EA 1997020600100 19970206 00100 NE 1997 2 6 CA960910020 2 19960807 A 7322 6078T55P05 FUEL CONTROL CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE #2 ENGINE FAULTY W E ENGINE SHUTDOWN X ENGINE FLAMEOUT DE DESCENT 1 CA (CAN) ON DESCENT #2 ENGINE SHUTDOWN. MAIN FUEL CONTROL AND MAIN FUEL PUMP ON #2 ENGINE REPLACED. THROTTLE AND FUEL SHUT OFF SYSTEM RIGGED AND GROUND RUN CARRIED OUT SERVICEABLE. 2 L 7 2 4F 4 F RT A21EA E15NE 1997020600101 19970206 00101 EA 1997 2 6 CA960910021 1 19960809 A 5210 DOOR CNDAIR CNDAIR CL600 CL6002B19 EA PASSENGER DOOR MALFUNCTION W K NONE O OTHER NR NOT REPORTED 1 CA 3125 (CAN) UNABLE TO OPEN MAIN PASSENGER DOOR FROM INSIDE AT DEPLANING. DOOR LUBRICATION ADJUSTED, NO OTHER FAULTS FOUND. 2 L 7 2 4F RT A21EA 1997020600102 19970206 00102 WP 1997 2 6 CA960910022 1 19960809 A 2131 21011403 CONTROLLER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE CABIN PRESSURE INOPERATIVE W A UNSCHED LANDING O OTHER CR CRUISE 1 CA P657361D (CAN) AIRCRAFT RETURNED FROM FLIGHT WITH DOUBLE PRESSURIZATION FAILURE. MAINTENANCE ACTION INVOLVED REPLACING #1 AND OUT FLOW VALVE ACTUATOR (P/N 20219741) AND #1 AND #2 OUTFLOW VALVE MOTOR (P/N 20220141). ALSO #2 PRESSURE CONTROLLER RPLACED . PRESSURIZATION SYSTEM CHECKED SERVICEABLE. 2 L 7 2 4F 4 F A6WE E2EA 1997020600103 19970206 00103 1997 2 6 CA960910023 4 19960811 A 2211 6224591512 COMPUTER BOEING 767 767275 NM PWA JT9 JT9D7R4D 52054 NE AUTO FLIGHT INTERNAL FAILURE W O OTHER J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA 709633 (CAN) AUTOPILOT LIGHT ON LINE THROUGH VNAV ON ATTITUDE DIRECTION INDICATOR AND EICAS MESSAGE (AUTOPILOT) WITH RIGHT AUTO PILOT ENGAGED. AUTOPILOT LIGHT REMAINED OUT. ALSO DISTINCT SMELL OF BURNING. ALSO (FD) FLAG ON CAPTAINS ATTITUDE DIRECTI ON INDICATOR AND AUTOLAND STATUS ANNUNCIATOR (NO LAND 3). PIN 2 OF CONNECTOR D4207J PUSHED BACK, PIN LOCKED AND SECURED. 2 L 7 2 RT 4 F RT A1NM E3NE 1997020600104 19970206 00104 EA 1997 2 6 CA960910024 1 19960811 A 3242 C2029334B4B4B BRAKE ASSEMBLY MESSIER CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE #1 SMOKING W K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 CA 4050 807199 (CAN) SMOKE FROM BRAKES ON LANDING AND DURING TAXI. #1 BRAKE ASSEMBLY CHANGED DUE TO LEAK. 2 L 7 2 4F 4 F RT A21EA E15NE 1997020600105 19970206 00105 EU 1997 2 6 CA960910025 1 19960811 A 3244 3008050T3 TIRE AIRBUS 320 A320211 3930320 EU LT MLG FAILURE W C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CA (CAN) TAKEOFF ABORTED DUE TO MAIN WHEEL TIRE FAILURE AT 90 KNOTS. ALSO LANDING GEAR ECAM MESSAGE SHOWN. THERE WAS A LOSS OF RUBBER ON INSIDE LEFT MAIN WHEEL ASSEMBLY,FOLLOWED BY GEAR UNSAFE INDICATION. MAINTENANCE FOUND CIRCULAR PUNCTURE ON LEFT MAIN OUTBOARD TIRE. MAIN LANDING GEAR WHEEL ASSEMBLY #1 AND #2 CHANGED AND #1 SYSTEM #15 GO AROUND SENSOR CHANGED (P/N ABS0121-10). 2 L 7 2 4F RT A28NM 1997020600106 19970206 00106 NM 1997 2 6 CA960910026 1 19960813 A 2611 DETECTOR BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE FWD WASHROOM INOPERATIVE W K NONE O OTHER CR CRUISE 1 CA P709614 (CAN) ON DESCENT FIRE IN FORWARD WASHROOM WASTE BIN, EXTINGUISHED WITH WATER. SMOKE ALARM DID NOT ACTIVATE. BATTERIES RE PLACED. TEMPERATURE INDICATOR ON WASTE BIN FIRE EXTINGUISHER CHECKED FOUND NOT ACTIVATED. SMOKE DETECTOR TESTED. REPLACE D. 2 L 7 2 4F 4 F RT A1NM E3NE 1997020600107 19970206 00107 1997 2 6 CA960910027 4 19960813 A 2310 6225272001 TRANSCEIVER BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE COCKPIT HF INTERMITTENT W K NONE O OTHER CR CRUISE 1 CA P709691 (CAN) HF #1 WOULD OPERATE FOR FOUR HOURS IN FLIGHT AND QUIT ALSO WHEN KEYING HF #1 AIRCRAFT PITCH WOULD CHANGE AND THROT TLES WOULD ROLL BACK. LH TRANSCIEVER, CONTROL PANEL AND COUPLER REPLACED. 2 L 7 2 4F 4 F RT A1NM E3NE 1997020600108 19970206 00108 WP 1997 2 6 CA960910028 1 19960813 A 3340 44040 LIGHT ASSEMBLY DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE LH LANDING LIGHT MISSING W K NONE O OTHER TX TAXI/GRND HDL 1 CA P657216D (CAN) LEFT LANDING LIGHT FOUND MISSING ON ARRIVAL AT DESTINATION. MISSING LIGHT ASSEMBLY REPLACED. 2 L 7 2 4F 4 F A6WE E2EA 1997020600109 19970206 00109 WP 1997 2 6 CA960910029 1 19960814 A 2160 60714621 TEMP CONTROLLER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE CABIN INOPERATIVE W A UNSCHED LANDING O OTHER CR CRUISE 1 CA P656873D (CAN) UNABLE TO CONTROL PRESSURIZATION OR TEMPERATURE, RETURNED TO DEPARTURE BASE. MAINTENANCE FOUND BOTH AUTO TEMPERATU RE CONTROLLER INOPERATIVE. ALSO PNEUMATIC DUCT OFF RIGHT AIR CYCLING MACHINE ON TURBINE SIDE. LEFT AND RIGHT TEMPERATURE CONTROLLER REPLACED AND DUCT REINSTALLED. SYSTEM GROUND RUN AND CHECKED SERVICEABLE. 2 L 7 2 4F 4 F A6WE E2EA 1997020600110 19970206 00110 WP 1997 2 6 CA960910030 1 19960816 A 2130 DUCTING DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE LH AIR COND PACK DISCONNECTED W K NONE J WARNING INDICATION CR CRUISE 1 CA P654059D (CAN) DURING CRUISE CABIN PRESSURIZATIN CLIMB 1000 FEET PER MINUTE AT 25,000 FEET AND FLOW LIGHT CAME ON. MAINTENANCE CH ECK REVEALED LEFT HAND AIR CONDITIONING PACK DUCT HAD BECOME DISCONNECTED BETWEEN AIR CYCLING MACHINE AND HEAT EXCHANGER . DUCT REINSTALLED. 2 L 7 2 4F 4 F A6WE E2EA 1997020600111 19970206 00111 WP 1997 2 6 CA960910031 1 19960816 A 2530 CA167072 RECEPTACLE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE GALLEY OVEN SHORTED W H DEACTIVATE SYST/CIRCUITS O B OTHER SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA P657222D (CAN) ELECTRICAL BURNING SMELL DETECTED IN GALLEY AREA. ODOUR DISSIPATED AFTER GALLEY CB PULLED. CHECK OF EQUIPMENT REVE ALED OVEN RECEPTACLE #18 WAS SHORTED. OVEN RECEPTACLE CHANGED. 2 L 7 2 4F 4 F A6WE E2EA 1997020600112 19970206 00112 NM 1997 2 6 CA960910034 1 19960819 A 3232 257T120016 ACTUATOR BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE RT MLG DOOR INTERMITTENT W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA P707531 (CAN) UNABLE TO RAISE RH MAIN LANDING GEAR ON TAKEOFF, RETURNED TO BLOCKS. RH MAIN LANDING GEAR DOOR ACTUATOR REPLACED, ADJUSTED LH MAIN LANDING GEAR SEQUENCE. 2 L 7 2 4F 4 F RT A1NM E3NE 1997020600113 19970206 00113 WP 1997 2 6 CA960910035 1 19960819 A 2130 BUTTERFLY VALVE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE CABIN PRESS STICKING W O OTHER O OTHER CR CRUISE 1 CA P657442D (CAN) AT FL350, CABIN COMMENCED CLIMB OF A 1,000 FEET PER MINUTE CONTROL LOCKED FORWARD DESCENDED TO FL250 MAINTAINED 1. 8 E.P.R. (ENGINE PRESSURE RATIO). REGAINED CONTROL AND LOCKOUT LIGHT ON, CABIN WAS DESCENDING AT 2,000 FEET PER MINUTE. CONTROL SELECTED TO AUTO, PRESSURE NORMAL. MAINTENANCE CHECK REVEALED PRESSURIZATION BUTTERFLY VALVE STICKING. THE VALVE WAS REMOVED, CLEANED AND REINSTALLED. OPERATIONAL CHECK CARRIED OUT SERVICEABLE. 2 L 7 2 4F 4 F A6WE E2EA 1997020600114 19970206 00114 EU 1997 2 6 CA960910036 1 19960820 A 2121 F4957 COOLING FAN AIRBUS 320 A320211 3930320 EU FLIGHT DECK BURNING ODOUR W K NONE O B OTHER SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA (CAN) BURNING ELECTRICAL SMELL DETECTED IN FLIGHT DECK. MAINTENANCE CHECK FOUND PROBLEM CAUSED BY AVIONICS FAN MOTOR. TH E COOLING FAN WAS REPLACED. 2 L 7 2 4F RT A28NM 1997020600115 19970206 00115 EU 1997 2 6 CA960910040 1 19960903 A 5711 SPAR CAP BNORM BN2 BN2B21 7080221 EU LYC O540 IO540K1B5 41532 EA UPPER CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 2514 913648A (CAN) DURING CORROSION INSPECTION PER SB 190 (CAA AD 020-02-90) CORROSION WAS DETECTED ON FACE OF SPAR CAP LAMINATE. REP AIR SCHEME GIVEN BY FACTORY REP. DURING REPAIR, CORROSION FOUND BETWEEN LAMINATES EXTENDING PAST REPAIR SCHEME LIMITS. F INAL REPAIR ENTAILS REPLACING UPPER REAR SPAR CAP, FROM LEFT INBOARD FUEL TANK RIB TO RIGHT INBOARD FUEL TANK RIB. 1 H 7 2 3O 3 O A17EU 1E4 1997020600118 19970206 00118 WP 1997 2 6 CA960916001 1 19960908 A 7810 501D13D CLAMP CVAC 340 340CVAC 242270A WP ALLSN 501D 501D13D 03004 GL EXHAUST SHEARED W E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 CA 501793 (CAN) DURING FLIGHT, ZONE #1 FIRE WARNING ON #1 ENGINE ILLUMINATED, ENGINE SHUT DOWN AND AIRCRAFT LANDED WITHOUT INCIDEN T. INVESTIGATION FOUND TAILPIPE CLAMP BROKEN. 2 L 7 2 4R 4 T 6A6 E282 1997020600247 19970206 00247 EU 1997 2 6 MALA965237 1 19961211 A 2613 CONNECTOR SAAB SF340 SF340A 7850100 EU LT ENGINE LOOSE A MALA O OTHER N FALSE WARNING CR CRUISE 1 GL 15 103XJ 340A103 DTW - FLT 3150 - IN CRUISE FLIGHT TO DTW WITH THE ENGINE ANTI-ICE ON, THE LEFT TAIL PIPE HOT LIGHT ILLUMINATED. THE CRE W REDUCED POWER AND THE WARNING LIGHT EXTINGUISHED. MAINTENANCE SECURED A LOOSE CANNON PLUG TO THE HOT SENSOR. ALL CHE CKS GOOD. (X) 2 L 7 2 4T RT A52EU 1997020600248 19970206 00248 EU 1997 2 6 MALA965248 1 19961219 A 7540 BLEED LIGHTS SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE LT/RT ILLUMINATED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 109XJ 340A109 DTW - FLT 3032 - AFTER TAKEOFF FROM DTW, THE LT AND RT BLEED CLOSED LIGHTS ILLUMINATED. THE CREW TRIED TO RESET THE BLE EDS WITHOUT POSITIVE RESULTS. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. (X) 2 L 7 2 4T 4 T RT A52EU E8NE 1997020600249 19970206 00249 EU 1997 2 6 MALA965253 1 19961220 A 2421 31342001 AC GENERATOR SAAB SF340 SF340A 7850100 EU NR 2 FAILED A MALA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CL CLIMB 1 GL 15 107XJ 340A107 DTW - FLT 3032 - CLIMB-OUT FROM DTW, THE RIGHT AC GENERATOR BECAME INOPERATIVE. THE AIRCRAFT RETURNED TO DTW. MAINTENA NCE REPLACED THE NR 2 AC GENERATOR. ALL CHECKS SATISFACTORY. (X) 2 L 7 2 4T RT A52EU 1997020600250 19970206 00250 1997 2 6 MALA965258 4 19961223 A 3425 DCP SAAB SF340 340B 7860101 EU NR 1 MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 402XJ 340B402 FLT 2924 - IN CRUISE FLIGHT, THE CREW RECEIVED LRN1 FLAG. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE WAS UNABLE TO DUPL ICATE THE DISCREPANCY. THE NR 1 DCP WAS REPLACED AS A PRECAUTION. (X) 2 L 7 2 4T RT A52EU 1997020600251 19970206 00251 1997 2 6 MALA965259 4 19961223 A 3442 6227337001 RT UNIT SAAB SF340 340B 7860101 EU FWD FUSELAGE FAILED A MALA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 403XJ 340B403 FLT 2907 - EN ROUTE, THE WEATHER RADAR SYSTEM STOPPED WORKING. THE CREW RESET THE CIRCUIT BREAKER AND IT BEGAN TO WORK INTERMITTENTLY. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE WEATHER RADAR R/T. ALL CHECKS SATISFACTORY. ( X) 2 L 7 2 4T RT A52EU 1997020600252 19970206 00252 NM 1997 2 6 USAABB96065 1 19961223 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 631AU 27809 LAX - BATTERY VOLTAGE LOW ON AISLE EMERGENCY LIGHTS. MAINTENANCE REPLACED THE BATTERIES AT ROWS 1, 4, 6, 9, AND 13. (X ) 2 L 7 2 4F RT A2NM 1997020600253 19970206 00253 WP 1997 2 6 AALA961789 1 19961209 A 5320 SUBFLOOR DOUG DC9 DC982 3022082 WP BS 161 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 400AA 49311 TUL - SUBFLOOR CORRODED AT INBOARD MOUNT FOR NR 1 GALLEY BOTTOM SIDE. REMOVED CORROSION ON BOTTOM OF SUBFLOOR. DIGITAL THICK CHECKED. INSTALLED REPAIR DOUBLER PER SRM 53-01, FIG 2 (SHT 3) PAGE 8. (X) 2 L 7 2 4F A6WE 1997020600254 19970206 00254 WP 1997 2 6 AALA961760 1 19961204 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1309 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 400AA 49311 TUL - CORROSION INSIDE J-CHANNEL ON AFT SIDE OF STA 1309 FRAME FROM LONGERON 30 TO 23L. INSTALLED DOUBLER PER AARD 53-1 0-00-14 AT STA 1309 L23 - L25 LEFT SIDE. (X) 2 L 7 2 4F A6WE 1997020600313 19970206 00313 WP 1997 2 6 DLL10970168 1 19961218 A 5312 BULKHEAD CAP LKHEED 1011 10113851 5265010 WP BS 449 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 721DA 193C1139 FS 449 BULKHEAD FOUND CRACKED IN HORIZONTAL FLANGE OF THE CAP. THE LOCATION IS FBL 19 AND EXTENDS FROM THE FORWARD EDGE , THROUGH AN EXISTING SEAL RETAINER HOLE, AND TOWARD THE CAP RADIUS. THE REPAIR WILL BE ACCOMPLISHED BY SB 093-53-233,2 .A PAGES 7-9. 2 L 7 3 4F A23WE 1997020600314 19970206 00314 WP 1997 2 6 DLL10970169 1 19961223 A 5312 BULKHEAD WEB LKHEED 1011 10113851 5265010 WP BS 1212 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 720DA 193C1136 BS 1212 BULKHEAD WEB FOUND CRACKED AT RBL 6. CRACK IS 2 INCHES. THE RBL 6 LOCATION REQUIRES A CHANGE TO THE DOUBLER PRO FILE TO ACCOMMODATE A CABLE PASS-THROUGH. 2 L 7 3 4F A23WE 1997020600320 19970206 00320 NM 1997 2 6 DL73K970175 1 19960815 A 5241 6552855502 GATE HINGE BOEING 737 737232 1384475 NM R1 DOOR LOWER CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 305DL 23077 THE R-1 DOOR LOWER GATE HINGE WAS FOUND CRACKED. THE CRACK WAS TYPICAL TO THOSE DISCUSSED IN AND REPAIRED BY BACO S/B 7 37-52A1124. THE SUBJECT HINGE WAS REMOVED AND REPLACED WITH A SERVICEABLE PART. 2 L 7 2 4F RT A16WE 1997020600328 19970206 00328 NM 1997 2 6 DL72W970183 1 19960726 A 5754 651622172 RIB BOEING 727 727247 138408F NM NR 5 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2817W 20873 DURING INITIAL INSPECTION, RIB NR 4 AND RIB NR 5 WERE FOUND CRACKED. THEY WERE REPAIRED PER SRM 57-50-3. 2 L 7 3 4F A3WE 1997020600426 19970206 00426 WP 1997 2 6 ABXA9700025 1 19961211 A 5753 3651366505 DRIVE LINK DOUG DC8 DC861 3021952 WP TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 847AX 46031 ULTRASONIC INSPECTION, SHOWS CRACK INDICATION ON LEFT FLAP INBOARD DRIVE LINK ON INBOARD LUG AT POINT J. REPLACED FLAP DRIVE LINK IAW DC-8 MM 27-51-4. 2 L 7 4 4F 4A25 1997020600614 19970206 00614 WP 1997 2 6 97ZZZM135 1 19961126 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 408 CRACKED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 DURNING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND A CRACK IN THE FORWARD PIT FRAME AT FS 408 AND LONGERON 30. (M) 2 L 7 2 4F A6WE 1997020600615 19970206 00615 WP 1997 2 6 97ZZZM136 1 19961205 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 370 DAMAGED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE FORWARD CARGO COMPARTMENT STATION 370, HAS INTERCOST AL WITH DRILL MARK AT LONGERON 28R. (M) 2 L 7 2 4F A6WE 1997020600616 19970206 00616 WP 1997 2 6 97ZZZM137 1 19961205 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 218/237 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE FORWARD PIT LONGERON 29R HAS CORROSION UNDER LONGERO N AT SPLICE BETWEEN STATION 218 BULKHEAD AND STATION 237. (M) 2 L 7 2 4F A6WE 1997020600617 19970206 00617 WP 1997 2 6 97ZZZM138 1 19961205 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 580 CRACKED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND FORWARD CARGO COMP LONGERON 29R END FITTING CAP CRACKED AT STATION 580 APPROX 2 INCHES LONG. (M) 2 L 7 2 4F A6WE 1997020600618 19970206 00618 WP 1997 2 6 97ZZZM139 1 19961205 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 218-237 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND FORWARD CARGO PIT CORRODED AND BLOWN OUT SPLICE AT BULKH EAD STATION 218 TO STATION 237 LONGERON 29R. (M) 2 L 7 2 4F A6WE 1997020600619 19970206 00619 WP 1997 2 6 97ZZZM140 1 19961205 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 120 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND E/E BAY LONGERON 29L AND 29R CORRODED BEYOND LIMITS FS 1 20 AND L30. 2 L 7 2 4F A6WE 1997020600620 19970206 00620 WP 1997 2 6 97ZZZM141 1 19961126 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 408 CRACKED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 DURING A SCHEDULED INSPECTION AT AERO CORP, A CRACK WAS FOUND IN THE FORWARD PIT FRAME AT FS 408 AND LONGERON 30. 2 L 7 2 4F A6WE 1997020600621 19970206 00621 WP 1997 2 6 97ZZZM142 1 19961205 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 580 CORROSION A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND CORROSION IN THE SKIN AT STATION 580 LONGERON 30, LEVEL 2. (M) 2 L 7 2 4F A6WE 1997020600622 19970206 00622 WP 1997 2 6 97ZZZM143 1 19961202 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 389 CRACKED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE FORWARD PIT FRAME AT FS 408 AND LONGERON 30 FRAME WA S CRACKED AT THE BOTTOM, THREE 1 INCH CRACKS. (M) 2 L 7 2 4F A6WE 1997020600623 19970206 00623 WP 1997 2 6 97ZZZM144 1 19961202 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 408 CRACKED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE FORWARD PIT FRAME AT FS 389 AND LONGERON 30 FRAME CR ACKED AT BOTTOM, CRACK LENGTH 3, 1 INCH. (M) 2 L 7 2 4F A6WE 1997020600624 19970206 00624 WP 1997 2 6 97ZZZM145 1 19961202 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 750 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND CORROSION AT LONGERON 30 END FITTING AT STATION 750. (M ) 2 L 7 2 4F A6WE 1997020600625 19970206 00625 EU 1997 2 6 SABA9600023 1 19961227 A 2910 1379305A77 HYD LINE BAG JETSTM JETSTM3101 1500215 EU RIGHT RUPTURED A SABA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 33 157PC 737 CLT - FLT 5182 - JUST AFTER T/O WHILE RETRACTING THE L/G THE A/C LOST PRESS ON LT HYD PUMP THE CAPT CALLED ATC AND REQUE STED TO RETURN TO CLT FOR LANDING. THE A/C THEN LOST PRESS ON RT HYD PUMP. THE CAPT DECLARED AN EMERGENCY AND REQUESTE D TO LAND ON THE LONGEST RUNWAY. WHEN THE L/G WAS SELECTED DOWN THE N/G CAME DOWN AND LOCKED THE MAIN GEAR LIGHTS STAYE D RED. THE CAPT SELECTED EMERG GEAR DOWN AND THE MAINS LOCKED W/O HAVING TO BE PUMPED. THE FLAPS CAME DOWN NORM WHEN S ELECTED TO 10 DEGREES. UPON LANDING NO NOSE STEERING WAS AVAILABLE, BUT BRAKING ACTION WAS NORM. THE A/C WAS T/S AND A RUPTURED RT HYD PUMP OUTPUT LINE. THE LINE WAS REPLACED, THE HYD SYS SERVICED AND BLEED, AND THE A/C RETURNED TO SERV. 2 L 7 2 4T RT A21EU 1997020600626 19970206 00626 NM 1997 2 6 97ZZZM146 1 19961121 A 2130 M390295205 CONNECTOR 39608831 BOEING 727 727214 138407R NM E/E COMPT WORN A C8GA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 15 227JL P670 20875 KTPA - DURING CLIMB-OUT THE CABIN CLIMBE TO 10,000 FEET AT FL 180, CLOSED CARGO HEAR OUT FLOW VALVE, NO HELP. SWITCHED TO MANUAL MODE, NO HELP. INITIATED DESCENT TO 10,000 FEET AND RETURNED TO THE RAMP. TROUBLESHOT PROBLEM TO TWO BAD WIR ES ON V23 OF RIGHT FLOW CONTROL SHUTOFF AND MODULATING VALVE. PINS 1 AND 5 WERE NOT MAKING CONTACT. REPINNED C/P, RAN ENGINES 1 AND 3, PRESSURIZED A/C TO 6 PSI FLOW CONTROL SHUT OFF AND MODULATING VALVE CHECKED OK IAW MM 36-12-61. (M) 2 L 7 3 4F A3WE 1997020600628 19970206 00628 EU 1997 2 6 MALA965264 1 19961225 A 3411 PITOT TRAP SAAB SF340 SF340A 7850100 EU NR 1 WATER CONTAM A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 103XJ 340A103 FLT 2971 - AFTER TAKEOFF, THE CAPTAINS AIRSPEED INDICATOR GAVE AN ERRONEOUS INDICATION. THE AIRCRAFT RETURNED TO DTW. M AINTENANCE PURGED WATER FROM THE NR 1 PITOT TRAP. AS A PRECAUTION, THE ADC AND ASI WERE REPLACED. (M) 2 L 7 2 4T RT A52EU 1997020600629 19970206 00629 EU 1997 2 6 97ZZZM147 1 19961225 A 3350 20VO3KHB BATTERY STBROS SD3 SD360 8100606 EU CABIN DISCHARGED A GUUA K NONE L NO TEST IN INSP/MAINT 1 SO 19 264GA 8909044 SH3756 AT SCHEDULED POS/FLT SERVICE DESK CHECK DETERMINED EMERGENCY LIGHTS TO BE INOPERATIVE. REMOVED AND REPLACED TAIL BATTER Y. (M) 2 H 7 2 4T A41EU 1997020600630 19970206 00630 CE 1997 2 6 97ZZZM148 1 19961222 A 3230 MS24171D1 RELAY BEECH 1900 1900C 1154161 CE LANDING GEAR FAILED A GUUA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 19 154GA UB25 FLT 398 - TCB-MIA - LANDING GEAR WILL NOT RETRACT. REMOVED AND REPLACED LANDING GEAR MOTOR RELAY AND HANDLE ASSEMBLY. O PERATIONAL CHECK SATISFACTORY. (M) 2 L 7 2 4T RT A24CE 1997020600631 19970206 00631 CE 1997 2 6 97ZZZM149 1 19961220 A 5330 SKIN BEECH 1900 1900C 1154161 CE BS 288 CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 181GA UB24 AT SCHEDULED INSPECTION, DISCOVERED CORROSION ON BELLY SKIN AND STRINGER DOUBLER AT FUSELAGE STATION 288 AND STRINGER 14 LEFT. REPLACED CORRODED STRINGER AND SKIN PER THE STRUCTURAL REPAIR MANUAL. 337 FORM SUBMITTED. 2 L 7 2 4T RT A24CE 1997020600632 19970206 00632 CE 1997 2 6 97ZZZM150 1 19961225 A 3240 BRAKES BEECH 1900 1900C 1154161 CE RIGHT INOPERATIVE A GUUA K NONE O OTHER NR NOT REPORTED 1 SO 19 153GA UB34 FLT 437 - TPA-MIA - RIGHT BRAKE INOP, SLIPS. CLEANED AND SERVICED BRAKES. OK FOR SERVICE. (M) 2 L 7 2 4T RT A24CE 1997020600633 19970206 00633 WP 1997 2 6 97ZZZM151 1 19960927 A 3610 CLAMP DOUG DC9 DC983 3022083 WP TAIL COMPT LOOSE A TWAA O OTHER J WARNING INDICATION TO TAKEOFF 1 CE 05 9407R 49400 MCI - FLT 229 - DURING TAKEOFF THE TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. REPOSITIONED AND TIGHTENED CLAM P AT AUGMENTATION VALVE. HIGH POWER LEAK CHECK ACCOMPLISHED, NO LEAKS NOTED. (M) 2 L 7 2 4F RT A6WE 1997020600639 19970206 00639 NE 1997 2 6 97ZZZM156 2 19961121 A 7230 3024711 COMPRESSOR BLADE DHAV DHC7 DHC7102 2802708 EA PWA PT6 PT6A65AG 52043 NE NR 1 ENGINE SPLIT A L CICA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 SO 17 8041D 026 86155 FLT - 759 - MIA-PID - PILOT REPORTED NR 1 TORQUE 3000 AT 11,000 FEET AND T5 AT 770 DEG, NG 93 PERCENT. OTHER ENGINES RU NNING NORMAL WITH 3700 TORQUE. A/C RETURNED TO MIA. THE A/C WAS INSPECTED AND FOUND TO BE SAFE FOR 3 ENGINE FERRY TO F LL. MAINTENANCE REPLACED NR 1 ENGINE. ENGINE S/N 86155 WAS SPLIT AT 'C' FLANGE AND FOUND CT DISK BLADES HAVE NICKS. A HOT SECTION AND REPAIR IS BEING PERFORMED. 2 H 7 4 4T 4 T A20EA E4EA 1997020600640 19970206 00640 1997 2 6 P2EA96011 4 19961112 A 3420 CIRCUIT BREAKER BOEING 737 7373Y0 1384671 NM IRS SYSTEM TRIPPED A P2EA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 05 303AL 23499 MSP - FLT 401 - AIR RETURN, NO EMERGENCY DECLARED, LANDING UNEVENTFUL. ATTITUDE AND HEADING FLAGS ON CAPTAIN'S AND F/O' S ADI'S, HSI'S AND RMI'S ONE MINUTES AFTER TAKEOFF. RESET NR 1 IRS AC CIRCUIT BREAKER, REALIGNED IRS SYSTEM, PERFORMED BITE TEST PER 22-05-00. SYSTEM PASSES. RECHECKED SYSTEM UPON ARRIVAL MCI, NO DISCREPANCIES NOTED. NO FURTHER FLIGHT R EMARKS. (M) 2 L 7 2 4F RT A16WE 1997020600641 19970206 00641 NM 1997 2 6 P2EA96012 1 19961106 A 3230 65446915 RETRACT MODULAR BOEING 737 737247 138448D NM NLG FAILED A P2EA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 204AU 1877 19603 FLT 107 - DFW - NOSE GEAR DID NOT RETRACT ON TAKEOFF, BOTH RED UNLOCKED AND GREEN DOWN AND LOCKED LIGHTS WERE ON, MAIN G EAR RETRACT NORMAL. LUBED NOSE GEAR PER MM 12-8-21 AND REPLACED NOSE GEAR MODULAR PACKAGE PER MM 32-38-31. PERFORMED N OSE GEAR SWING AND ALL ACTIONS AND INDICATIONS NORMAL. OK FOR SERVICE. (M) 2 L 7 2 4F A16WE 1997020600642 19970206 00642 NM 1997 2 6 P2EA96013 1 19961113 A 5313 STRINGER BOEING 737 737281 138448P NM BS 664 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 DURING C-CHECK, PERFORMED INSPECTION IAW AD95-12-17, FINDINGS RESULTED IN THE FOLLOWNG REPAIR; PERFORMED MAJOR REPAIR IA W SB737-53-1066R1, PERTINENT DETAILS UNDER WO NR 0003-02-F055 AND 0003-02-F056. INSPECTION AND REPAIRS COMPLETED DURING C-CHECK BY SABRE TECH, 9809 TRADEORT DR, ORLANDO, FLORIDA 32827. (M) 2 L 7 2 4F A16WE 1997020600643 19970206 00643 NM 1997 2 6 P2EA96014 1 19961129 A 2761 6544561K ACTUATOR BOEING 737 737222 1384473 NM NR 6 SPOILER FAILED A A P2EA O OTHER F FLT CONT AFFECTED AP APPROACH 1 CE 05 209US 409022 19548 MCI - FLT 8067 - ON FINAL APPROACH WITH A/P ON APP MODE, AIRCRAFT MADE SUDDEN TURN AND ROLL TO THE RIGHT REQUIRING AILER ON AND RUDDER TO CORRECT. POST FLIGHT INSPECTION FOUND NR 6 SPOILER STILL EXTENDED. REPLACED NR 6 SPOILER ACTUATOR PER MM 27-61-51, GROUND OPS CHECKS OK. PER TELEPHONE CONVERSATION BOEING RECOMMENDED AND MAINTENACNE CONTROL REQUEST, REPL ACED RN 7 SPOILER ACTUATOR (PRECAUTIONARY) PER MM 27-61-51, GROUND OPS CHECK OK. ALSO, PERFORMED VISUAL INSPECTION OF R IGHT WING SPOILER CABLE RUN. ALL CABLE RUNS, AND PULLEYS CHECKED OK. NO CABLE KINKS OR FRAYS NOTED. PERFORMED EVALUAT ION FLIGHT, SYSTEM CHECKED OK. (M) 2 L 7 2 4F A16WE 1997020600644 19970206 00644 WP 1997 2 6 ORJA96119 1 19961221 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN LOOSE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 876RA 53183 EMERGENCY FLOOR LIGHTS INOP AT 4/5 D-SECTION. REPAIRED LOOSE WIRE AT FLOOR TRACK FOR 4/5-D. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1997020600645 19970206 00645 WP 1997 2 6 ORJA96118 1 19961224 A 3260 LOCK SENSOR DOUG DC9 DC982 3022082 WP NLG OUT OF ADJUST A ORJA O OTHER N FALSE WARNING CL CLIMB 1 WP 11 841RA 49421 NOSE GEAR RED UNSAFE LIGHT ILLUMINATES INTERMITTENTLY WITH GEAR HANDLE UP. FOUND NOSE GEAR LOCK SENSOR OUT OF ADJUSTMEN T. ADJUSTED AS PER MM 32-60-05. TESTED SENSORS WITH 'GO NO-GO GAUGE', ALL CHECKS GOOD. (M) 2 L 7 2 4F A6WE 1997020600646 19970206 00646 WP 1997 2 6 ORJA96120 1 19961225 A 3260 PROX SENSOR DOUG DC9 DC982 3022082 WP NLG OUT OF ADJUST A ORJA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 11 841RA 49421 RED NOSE UNSAFE LIGHT COMES ON IN FLIGHT. ADJUSTED NOSE GEAR UPLOCK PROX SENSOR IAW MM 32-60-05. (M) 2 L 7 2 4F A6WE 1997020600648 19970206 00648 WP 1997 2 6 ORJA96123 1 19961229 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN BROKEN A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 836RA 53046 EMERGENCY LIGHTS AT ROWS 7-8-9 INOP (WIRE BROKEN AND BULB MISSING). REPAIRED WIRING AND RELAMPED. ALL FLOOR EMERGENCY PROXIMITY LIGHTING OPERATIONAL CHECKS OK. (M) 2 L 7 2 4F RT A6WE 1997020600649 19970206 00649 WP 1997 2 6 ORJA96122 1 19961230 A 3260 UPLOCK SENSOR DOUG DC9 DC982 3022082 WP NLG INOPERATIVE A ORJA O OTHER N FALSE WARNING CL CLIMB 1 WP 11 842RA 49604 NOSE GEAR UNSAFE LIGHT CAME ON INTERMITTENTLY AFTER TAKEOFF. NOSE LANDING GEAR INDICATOR INDICATED UP AND LOCKED. NO B UFFET OR NOISE. STEADY GREEN WITH GEAR DOWN. REPLACED UPLOCK PROXIMTITY SENSOR AND OPS CHECKED GOOD IAW MM 32-60-05. ( M) 2 L 7 2 4F A6WE 1997020600650 19970206 00650 WP 1997 2 6 ORJA96121 1 19961230 A 3260 PROX SENSOR DOUG DC9 DC982 3022082 WP NLG INOPERATIVE A ORJA O OTHER N FALSE WARNING CL CLIMB 1 WP 11 842RA 49604 NOSE GEAR RED LIGHT ILLUMINATES INTERMITTENTLY IN CLIMB AND CRUISE LAX-SJC. REMOVED AND REPLACED NOSE GEAR UP/DOWN AND LOCKED PROXIMITY SENSOR IAW AMM 32-60-05. OPS CHECK OK. (M) 2 L 7 2 4F A6WE 1997020600655 19970206 00655 NM 1997 2 6 TAOA129614 1 19961230 A 3350 20131A BATTERY PACK BOEING 727 727254 138408L NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 913TS 13887 20250 ON OVERNIGHT CHECK, FOUND FORWARD SECTION OF ESCAPE PATH LIGHTS INOP. REPLACED BATTERY PACK. OPERATION CHECKED OK. (M ) 2 L 7 3 4F A3WE 1997020600656 19970206 00656 NM 1997 2 6 TAOA129615 1 19961230 A 3350 S106 BATTERIES BOEING 727 727225 1384077 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 919TS 20447 ON OVERNIGHT CHECK, THE FORWARD R1 DOOR EMERGENCY LIGHT WAS FOUND INOP. REPLACED FORWARD EMERGENCY EXIT LIGHT BATTERIES . OPERATIONAL CHECKED OK. (M) 2 L 7 3 4F A3WE 1997020600657 19970206 00657 NM 1997 2 6 TAOA129613 1 19961228 A 2410 MS832481014 O-RING 700842A BOEING 727 727225 1384077 NM NR 1 CSD LEAKING A TAOA C D ABORTED TAKEOFF RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TO TAKEOFF 1 EA 15 919TS 14315 20447 ON FLT 6121 - NR 1 ENGINE WAS MOVED TO TAKEOFF POWER. NR 1 CSD LOW OIL PRESSURE LIGHT FLICKERED AND NR 1 GENERATOR BREA KER TRIPPED. AIRCRAFT ABORTED TAKEOFF. FOUND THE INTEGRAL OIL FILTER HOUSING LEAKING. REPLACED O-RINGS FOR SAME AND S ERVICED CSD. OPERATIONAL CHECKED THE CSD AND THE NR 1 GENERATOR MM 24-10-00. (M) 2 L 7 3 4F A3WE 1997020600664 19970206 00664 WP 1997 2 6 ASAA9680283 1 19961228 A 3350 6011779 POWER SUPPLY DOUG DC9 DC982 3022082 WP EXTERIOR INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 966AS 49104 SFO - DURING MAINTENANCE CHECK, THE EXTERIOR EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. REPLACED BATTERY PACK POWER SUPPLY AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1997020600665 19970206 00665 WP 1997 2 6 ASAA9680279 1 19961222 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 962AS 53076 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 1 TO 3 WERE FOUND INOPERATIVE. REPAIRED BROK EN WIRE AT ROW 3 AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1997020600666 19970206 00666 WP 1997 2 6 ASAA9680278 1 19961219 A 3350 D29984103 SLIDE LIGHT DOUG DC9 DC983 3022083 WP TAILCONE FAILED TEST A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 943AS 53018 OAK - DURING C-CHECK, THE TAILCONE EMERGENCY EVACUATION SLIDE EMERGENCY LIGHTS FAILED TEST. REPLACED THE TAILCONE EMERG ENCY EVACUATION SLIDE. (M) 2 L 7 2 4F RT A6WE 1997020600667 19970206 00667 WP 1997 2 6 ASAA9680277 1 19961219 A 3350 D29985107 SLIDE LIGHT DOUG DC9 DC983 3022083 WP L2 DOOR FAILED TEST A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 943AS 53018 OAK - DURING C-CHECK, THE L2 DOOR EMERGENCY EVACUATION SLIDE EMERGENCY LIGHT FAILED TEST. REPLACED THE L2 DOOR EMERGENC Y EVACUATION SLIDE. (M) 2 L 7 2 4F RT A6WE 1997020600668 19970206 00668 WP 1997 2 6 ASAA9680276 1 19961219 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 939AS 49657 PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 1 TO 6 WERE FOUND INOPERATIVE. REPLACED BATT ERY PACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1997020600673 19970206 00673 NM 1997 2 6 ASAA9610148 1 19961230 A 3350 8821004 BATTERY PACK BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 18 AND 19. R EPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1997020600674 19970206 00674 NM 1997 2 6 ASAA9610147 1 19961223 A 3350 8821004 BATTERY BOEING 737 737210C 1384459 NM CARGO COMPT DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 744AS 21822 SEA - DURING MAINTENANCE CHECK, THE NR 3 PALLET EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY AN D LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1997020600676 19970206 00676 NM 1997 2 6 ASAA9640101 1 19961222 A 5315 65468101 FLOOR BEAM BOEING 737 7374Q8 NM BS 967 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 762AS 25099 SEA - DURING C-CHECK, THE UPPER AFT FLANGE OF THE FLOOR BEAM AT STATION 967 WAS FOUND TO BE CORRODED. REPAIRED PER EA 5 310-01502 AND BOEING TELEX ASA-SEA-96-0584RR. (M) 2 L 7 2 4F RT A16WE 1997020600681 19970206 00681 1997 2 6 PCAA9600334 4 19961221 A 3442 071131313 RADAR DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A PCAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 13 977HA 1311 220 FLT 3825 - DURING CLIMB, SMOKE NOTICED IN COCKPIT, SUSPECT RADAR GRAPHICS UNIT. INSPECTED, PULLED AND BANDED CIRCUIT BR EAKER K4 (RADAR GRAPHICS) RAN ALL ELECTRICAL SYSTEMS. SMOKE DISIPATED, NO OTHER DEFECTS FOUND. AIRCRAFT DISPATCHED UND ER MEL. SUBSEQUENTLY REPLACED RADAR GRAPHICS CONTROL HEAD. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (M ) 2 H 7 2 4T RT A13NM 1997020600682 19970206 00682 NM 1997 2 6 PCAA9600332 1 19961217 A 3234 574205 SELECTOR VALVE DHAV DHC8 DHC8102 2809003 NM LANDING GEAR FAILED A PCAA O OTHER J WARNING INDICATION DE DESCENT 1 EA 13 977HA 446 220 UPON DESCENT INTO ITH, LANDING GEAR DID NOT EXTEND WHEN SELECTED DOWN. CREW PERFORMED EXTENSION PER EMERGENCY CHECKLIST . A/C LANDED WITHOUT INCIDENT. A/C FERRIED TO BGM FOR REPAIR. TROUBLESHOT SYSTEM, REMOVED AND REPLACED LANDING GEAR S ELECTOR VALVE IAW DHC MM, LEAK AND OPERATIONAL CHECKED GOOD. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1997020600683 19970206 00683 NM 1997 2 6 PCAA9600330 1 19961212 A 3230 DSC252B40124 HYD HOSE DHAV DHC8 DHC8102 2809003 NM NLG FAILED A PCAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 13 821EX 173 UPON TAKEOFF OUT OF MHT, WHEN LANDING GEAR WAS SELECTED UP, THE NR 2 HYDRAULIC CONTENTS FELL TO ZERO. CREW PERFORMED A MANUAL EXTENSION OF GEAR . THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. INSPECTED AND FOUND THE NOS E LANDING GEAR DRAG STRUT RETRACTION HOSE FAILED. REMOVED AND REPLACED, AND SY STEM INSPECTED IAW DHC MM. AIRCRAFT RET URNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1997020600684 19970206 00684 NM 1997 2 6 PCAA9600326 1 19961202 A 2120 AIR DISTR DHAV DHC8 DHC8102 2809003 NM CABIN ODOR A PCAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 13 817EX 14691 191 EN ROUTE FROM ABE TO BOS, AIRCRAFT DIVERTED INTO MHT DUE TO A STRONG ODOR OF FUEL EVIDENT IN PASSENGER COMPARTMENT AFT O F ROW 7. INSPECTED BOTH ENGINES FOR FUEL LEAKS, INSPECTED FUEL LINES, APU, AND BLEEDS. DRAINED EPA TANKS. NO LEAKS NO TED. GROUND RAN AIRCRAFT WITH BLEEDS ON, COULD NOT DUPLICATE ODOR. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1997020600685 19970206 00685 NM 1997 2 6 PCAA9600329 1 19961209 A 5520 85510031 PLATE DHAV DHC8 DHC8102 2809003 NM HORIZ STAB LOOSE A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 EICBJ 15269 15269 215 ELEVATOR GUST LOCK PLATE HAS SEVERAL WORKING JO-BOLTS. REPAIRED GUST LOCK PLATES IAW DHC REPAIR DRAWING 8-55-099. AIRC RAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1997020600686 19970206 00686 NE 1997 2 6 PCAA9600333 2 19961212 A 7320 MS3476L2255P CONNECTOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 ENGINE FAILED A PCAA O OTHER O OTHER NR NOT REPORTED 1 EA 13 809EX 302 120966 NR 1 ENGINE FAILED WHEN ECU SELECTED TO MANUAL. FOUND LEFT ECU WING ROOT CANNON PLUG 9811-P13 WET, BACK SHEEL FULL OF W ATER AND DE-ICE FLUID. CLEANED, DRIED AND RECONNECTED CONNECTOR. UPON ENGINE RUN, CIRCUIT BREAKER L6 POPPED AND WOULD NOT RESET. REMOVED AND REPLACED ELECTRICAL CONNECTOR 9811-P13. OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVI CE. (M) 2 H 7 2 4T 4 T RT A13NM E20NE 1997020600716 19970206 00716 1997 2 6 USAABB96059 4 19961206 A 2397 114265011 WIRE BOEING 757 7572B7 1384964 NM CABIN CHAFED A USAA O OTHER A FLAME/FIRE CR CRUISE 1 EA 19 616AU 27147 PIT - FL 27 - EN ROUTE BOS-PIT, A PASSENGER REPORTED SPARKS AND SMOKE COMING FROM JUST AFT OF THE L-2 DOOR WHILE THE PLA NE WAS ENCOUNTERING MODERATE TURBULENCE. MAINTENANCE FOUND THE WIRE FROM THE AFT WALL DISCONNECT BADLY CHAFED. THE LEF T WALL DISCONNECT BOXES POWER SUPPLY CIRCUIT BREAKER WAS POPPED. MAINTENANCE REPLACED THE CABLE. (M) 2 L 7 2 4F RT A2NM 1997020600717 19970206 00717 NM 1997 2 6 USAABB96066 1 19961211 A 3350 86210066 BATTERIES BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 632AU 27810 LAX - ON CHECK, FOUND EMERGENCY AISLE LIGHT BATTERIES AT ROWS 4, 9, 13, 18, 23 AND 26 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 1997020600726 19970206 00726 NM 1997 2 6 USAA960806 1 19961230 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 1003-1016 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 265AU 35100 22962 ROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND 13 INCHES OF CORROSION, STRINGER 27 LEFT, BETWEEN STATION 1003 AND 101 6. INSTALLED STRINGER SPLICE AND REPAIRED PER SRM 53-10-3 FIG 1. (M) 2 L 7 2 4F A16WE 1997020600727 19970206 00727 NM 1997 2 6 USAASB97008 1 19961230 A 3350 BATTERY PACK BOEING 737 737401 1384701 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 417US 23984 PIT - MAINTENANCE FOUND THE AFT EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER AND THE BAT TERY PACK. BATTERY CHARGER P/N 2012-1, BATTERY PACK P/N 2013-1. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1997020600728 19970206 00728 NM 1997 2 6 USAASB97007 1 19961226 A 3350 20121 POWER SUPPLY BOEING 737 737401 1384701 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 417US 23984 PHL - MAINTENANCE FOUND THE LEFT AFT ENTRY DOOR EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPL Y IN THE AFT OVERHEAD CABIN. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1997020600740 19970206 00740 NM 1997 2 6 UIEA9613 1 19961225 A 8012 3978921 START VALVE BOEING 747 747230B 1384889 NM NR 4 ENGINE LEAKING A UIEA E A ENGINE SHUTDOWN UNSCHED LANDING J M WARNING INDICATION OVER TEMP CR CRUISE 1 EA 15 508MC 21644 FLT CI314 - 7PE-ANG - NR 4 ENGINE SHUTDOWN AND AIR TURN BACK TO TAIPEI, DUE TO HIGH NACELLE TEMP. FOUND START VALVE DIA PHRAGM LEAK AND 'A' LOOP WIRE RUBBING HORIZONTAL FIREWALL. REPLACED VALVE AND PERFORMED HIGH POWR RUN OPS OK. (M) 2 L 7 4 4F A20WE 1997020600749 19970206 00749 NM 1997 2 6 97ZZZM167 1 19961224 A 5311 65465931 FRAME BOEING 737 737247 138448D NM BS 500 CRACKED A A6XA K NONE O OTHER IN INSP/MAINT 1 SO 13 4515W 40897 19612 FUSELAGE FRAME AT STATION 500A HAS TWO .5 INCH CRACKS BETWEEN STRINGERS 20L AND 21L. (M) 2 L 7 2 4F A16WE 1997020600750 19970206 00750 NM 1997 2 6 97ZZZM168 1 19961224 A 5311 65465331 FRAME BOEING 737 737247 138448D NM BS 500 CRACKED A A6XA K NONE O OTHER IN INSP/MAINT 1 SO 13 4515W 40897 19612 FUSELAGE FRAME AT STATION 500 HAS A 1 INCH CRACK AT BL 0. (M) 2 L 7 2 4F A16WE 1997020600751 19970206 00751 NM 1997 2 6 97ZZZM169 1 19961224 A 5311 65465931 FRAME BOEING 737 737247 138448D NM BS 500 CRACKED A A6XA K NONE O OTHER IN INSP/MAINT 1 SO 13 4515W 40897 19612 FUSELAGE FRAME AT STATION 500A HAS A 2 INCH CRACK AT BL 0. (M) 2 L 7 2 4F A16WE 1997020600752 19970206 00752 NM 1997 2 6 97ZZZM170 1 19961224 A 5313 BAC149896 STRINGER BOEING 737 737247 138448D NM BS 500 CRACKED A A6XA K NONE O OTHER IN INSP/MAINT 1 SO 13 4515W 40897 19612 FUSELAGE STRINGER 25L HAS TWO 1 INCH LONG CRACKS AT STATION 500. 2 L 7 2 4F A16WE 1997020600753 19970206 00753 NM 1997 2 6 97ZZZM171 1 19961224 A 5311 65465661 FRAME BOEING 737 737247 138448D NM BS 767 CRACKED A A6XA K NONE O OTHER IN INSP/MAINT 1 SO 13 4515W 40897 19612 FUSELAGE FRAME AT STATION 767 HAS A .5 INCH CRACK ABOVE STRINGER 25R. 2 L 7 2 4F A16WE 1997020600754 19970206 00754 NM 1997 2 6 97ZZZM172 1 19961224 A 5311 65465661 FRAME BOEING 737 737247 138448D NM BS 987 CRACKED A A6XA K NONE O OTHER IN INSP/MAINT 1 SO 13 4515W 40897 19612 FUSELAGE FRAME AT STATION 987 HAS A 4 INCH CRACK BETWEEN STRINGERS 20L AND 21L. 2 L 7 2 4F A16WE 1997020600755 19970206 00755 NM 1997 2 6 97ZZZM173 1 19961224 A 5320 65465941 CHANNEL BOEING 737 737247 138448D NM BS 500 BENT A A6XA K NONE O OTHER IN INSP/MAINT 1 SO 13 4515W 40897 19612 FUSELAGE CHANNEL AT STATION 500B AT STRINGER 20R IS BENT OUT OF LIMITS. 2 L 7 2 4F A16WE 1997020600756 19970206 00756 NM 1997 2 6 97ZZZM174 1 19961224 A 5315 65468111 FLOOR BEAM BOEING 737 737247 138448D NM BS 986.5 CORRODED A A6XA K NONE O OTHER IN INSP/MAINT 1 SO 13 4515W 40897 19612 FLOOR BEAM AT STATION 986.6 LBL 29 HAS CORROSION AT THE NUT PLATE HOLES 5 SQUARE INCHES TOTAL. 2 L 7 2 4F A16WE 1997020600757 19970206 00757 NM 1997 2 6 97ZZZM175 1 19961224 A 5311 65465941 FRAME BOEING 737 737247 138448D NM BS 500 GOUGED A A6XA K NONE O OTHER IN INSP/MAINT 1 SO 13 4515W 40897 19612 FRAME AT STATION 500B HAS GOUGES AROUND THE ANCHOR NUT AT STRINGER 20L. 2 L 7 2 4F A16WE 1997020600758 19970206 00758 WP 1997 2 6 97ZZZM176 2 19961231 A 7200 ENGINE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP RIGHT FAILED A A SWHA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 17 718C 20309 AC572 P44300C FLT 4060 - ON TRAINING FLIGHT, THE PILOT REPORTED A LOSS OF OIL PRESSURE ON THE RIGHT ENGINE. THE RIGHT ENGINE WAS SHUT DOWN AND SECURED IN FLIGHT. THE FLIGHT RETURNED TO AUS AND LANDED WITHOUT INCIDENT. THE ENGINE WAS REPLACED AND OPERA TIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. THE ENGINE REMOVED WILL BE SENT OUT FOR REPAIR TO DETERMI NE THE NATURE OF FAILURE. (M) 2 L 7 2 4T 4 T RT A8SW E4WE 1997020600769 19970206 00769 WP 1997 2 6 97ZZZM179 1 19961208 A 5330 SKIN DOUG DC9 DC915F 3022037 WP BS 642 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 916F 49919 47044 DURING C-CHECK INSPECTION DISCOVERED EXFOLIATION CORROSION ON THE LOWER FUSELAGE EXTERNAL SKIN AT BS 642, LONGERON 30, B L 0. THE CORRODED AREA MEASURED 5.25 INCH IN LENGTH AND 4.9 INCH IN WIDTH. AFFECTED AREA WS TRIMMED TO REMOVE CORROSIO N. INSTALLED INTERNAL FINGER DOUBLERS AND EXTERNAL REPAIR DOUBLERS WET WITH SEALANT AND TOP COATED AS REQUIRED. ACCOMP IAW EIAA, ENGINEERING CHANGE/REPAIR AUTHORIZATION NR 916-53-016-2. (M) 2 L 7 2 4F A6WE 1997020600770 19970206 00770 WP 1997 2 6 97ZZZM180 1 19961208 A 5330 SKIN DOUG DC9 DC915F 3022037 WP BS 642 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 916F 49919 47044 DURNG C-CHECK INSPECTION DISCOVERED EXFOLIATION CORROSION ON THE LOWER FUSELAGE EXTERNAL SKIN AT BS 642, LONGERON 30, BL 0. THE CORRODED AREA MEASURED 5.25 INCH IN LENGTH AND 4.9 IN WIDTH. AFFECTED AREA WAS TRIMMED TO REMOVE CORROSION. I NSTALLED INTERNAL FINGER DOUBLERS AND EXTERNAL REPAIR DOUBLERS WET WITH SEALANT AND TOP COATED AS REQUIRED. ACCOMP IAW EIAA ENGINEERING CHANGE/REPAIR AUTHORIZATION NR 916-53-016-2. (M) 2 L 7 2 4F A6WE 1997020600775 19970206 00775 NM 1997 2 6 F3LA96072 1 19961230 A 5320 69389331 FORGING BOEING 737 737201 1384454 NM BS 727 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 PAE - FOUND CRACK IN FORGING AT BS 727 BL 0, WL 208, 1.5 INCH LONG. REMOVED AND REPLACED FORGING AT BS 727 BL 0, WL 208 IAW SRM 51-10-1 AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1997020600776 19970206 00776 NM 1997 2 6 F3LA96071 1 19961230 A 5241 6545871140 FRAME BOEING 737 737201 1384454 NM GALLEY DOOR CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 PAE - FORWARD GALLEY DOOR AFT SIDE FRAME IS CRCKED, 3 INCHES TO 5 INCH CRACKS FOUND. REMOVED AND REPLACED FORWARD GALLE Y DOOR AFT SIDE FRAME PER SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1997020600777 19970206 00777 NM 1997 2 6 F3LA96070 1 19961230 A 5720 65634619 ANGLE BOEING 737 737201 1384454 NM LT WING CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 PAE - INBOARD LOWER RIB ANGLE CRACKED ON AFT END AT L/W AILERON NR 3 HINGE FITTING. REMOVED AND REPLACED INBOARD AND OU TBOARD LOWER RIB ANGLE ON L/W AILERON NR 3 HINGE FITTING IAW OHM 20-50-1. (M) 2 L 7 2 4F A16WE 1997020600778 19970206 00778 NM 1997 2 6 F3LA96069 1 19961226 A 5315 6545812 FLOORBEAM BOEING 737 737201 1384454 NM BS 967 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 PAE - FOUND CORROSION (C53-107-02) ON TOP OF FLOORBEAM BS 967 RBL 50, LBL 25, WL 208. FOUND CORROSION ON FLOORBEAM TO B E OUT OF LIMITS. REPLACED FLOORBEAM PER EWO 96-0930 AND SRM 53-10-9. (M) 2 L 7 2 4F A16WE 1997020600779 19970206 00779 NM 1997 2 6 F3LA96068 1 19961223 A 5315 6545834 FLOORBEAM BOEING 737 737201 1384454 NM BS 312 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 PAE - FOUND CORROSION (C53-107-02) ON FLOORBEAM, BS 312, RBL 10 TO RBL 12, WL 208. REMOVED CORROSION ON TOP CHORD OF FL OORBEAM, BS 312, RBL 10 TO RBL 12, WL 208. REMOVED 3 INCH BY 3 INCH BY .024 INCH ORIGINAL THICKNESS .080 INCH. FOUND T O BE OUT OF LIMITS IAW SRM 53-10-01. REMOVED DAMAGED AREA AND REPAIRED IAW SRM 53-10-9. (M) 2 L 7 2 4F A16WE 1997020600780 19970206 00780 NM 1997 2 6 F3LA96067 1 19961223 A 5315 6545812 FLOORBEAM BOEING 737 737201 1384454 NM BS 328 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 PAE - FOUND CORROSION (C53-107-02) ON FLOORBEAM BS 328, RBL 10 TO RBL 41, WL 208. REMOVED CORROSION IN AN AREA OF 3 INC H BY 18 INCH WITH A DEPTH OF .028 INCH AND AN ORIGINAL THICKNESS OF .080 INCH, FOUND TO BE OUT OF LIMITS PER SRM 53-10-0 1. REMOVED AND REPLACED UPPER T-CHORD. ALL WORK DONE IAW SRM 53-10-01, 53-10-02, AND 53-10-9. (M) 2 L 7 2 4F A16WE 1997020600781 19970206 00781 NM 1997 2 6 F3LA96065 1 19961216 A 5320 69353521 CLIP BOEING 737 737201 1384454 NM BS 727 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 PAE - FOUND CRACKED STRINGER CLIP BS 727A STRINGER 21R. REMOVED STRINGER CLIP BS 727A STRINGER 21R. FABRICATED STRINGE R CLIP, ALODINED AND PRIMED. INSTALLED STRINGER CLIP IAW SRM 51-20-1 AND SRM 51-30-02. (M) 2 L 7 2 4F A16WE 1997020600782 19970206 00782 NM 1997 2 6 F3LA96064 1 19961216 A 5320 65C807351 SILL BOEING 737 737201 1384454 NM BS 920-960 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 FOUND CORROSION 9C53-107-02) THROUGH R/T MOP SILL, BS 920-960, RBL 60, WL 208. FOUND R/T MOP SILL (CREASE BEAM) CORRODE D OUT OF LIMITS PER SRM 53-10-3. REMOVED AND REPLACED MOP SILL AT BS 920-960, RBL 60, WL 208 PER SRM 51-30-02. (M) 2 L 7 2 4F A16WE 1997020600783 19970206 00783 NM 1997 2 6 F3LA96061 1 19961126 A 5210 SKIN BOEING 737 737201 1384454 NM AIRSTAIR DOOR DENTED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 212US 20212 FOUND DENT ON AFT AIRSTAIR DOOR APPROXIMATELY 16 INCHES FROM TOP OF DOOR. REMOVED DAMAGE ON AFT ENTRY DOOR OUTER SKIN 1 .75 INCH BY 1.75 INCH APPROX 16 INCHES FROM TOP OF DOOR AND 16 INCHES FROM FORWARD SIDE. INSTALLED REPAIR DOUBLER IAW S RM 52-00-3, 52-10-1, 51-10-1, 51-20-4 AND 51-30-0. (M) 2 L 7 2 4F A16WE 1997020600784 19970206 00784 NM 1997 2 6 F3LA96060 1 19961121 A 5330 BAC1518399 SKIN BOEING 737 737201 1384454 NM BS 977 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 212US 20212 PAE - FOUND CRACK IN SKIN AT THE TOP EDGE OF LOWER DOOR CUTOUT AT BS 977 WL 208. CRACK IS APPROXIMATE 1.5 INCH LONG, TR AVELING FROM EDGE INTO HOLE AND BEYOND. CRACK IS IN QUADRUPLER. REMOVED CRACKED QUADRUPLER, AND TRIPLER AT BS 947-1016 WL 218-190 AND FABRICATED A NEW QUADRUPLER. REINSTALLED TRIPLER AND QUADRUPLER PER EWO 96-0767 AND B737-200 SRM 51-10- 2. (M) 2 L 7 2 4F A16WE 1997020600785 19970206 00785 NM 1997 2 6 F3LA96059 1 19961120 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM BS 947 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 212US 20212 PAE - FOUND CORROSION ON FLOORBEAM AROUND NUTCLIP HOLE AT BS 947, RBL 50, WL 208. BLENDED DAMAGED AREA PER SRM 51-10-02 , DAMAGED AREA WAS FOUND TO BE OUT OF LIMITS. FABRICATED A REPAIR STRAP AND TREATED PER SRM 51-20-01. INSTALLED STRAP, ALL WORK ACCOMPLISHED ON MWO 96-0746 AND B737-200 SRM 53-10-9. (M) 2 L 7 2 4F A16WE 1997020600786 19970206 00786 NM 1997 2 6 F3LA96058 1 19961119 A 5320 651360086 CHORD BOEING 737 737201 1384454 NM BS 178 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 212US 20212 PAE - CRACK INDICATIONS NOTED (3), RIGHT CHORD BS 178, BETWEEN WL 195 AND WL 204. REMOVED 178 RT WEB FOR ACCESS. REMOV ED CRACKED CHORD, FABRICATED NEW CHORD AND INSTALLED CHORD AND RT WEB IAW SRM 53-10-11, SRM 51-30-2, CUS NR 0000899 FUSE NR 00292. (M) 2 L 7 2 4F A16WE 1997020600787 19970206 00787 NM 1997 2 6 F3LA96057 1 19961118 A 5320 BAC14902808 CHORD BOEING 737 737201 1384454 NM BS 440 PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 212US 20212 PAE - FOUND PUNCTURE IN FAIL/SAFE CHORD BS 440 BETWEEN STRINGER 27 AND 28 RT. PUNCTURE IS BELIEVED TO HAVE BEEN CAUSED BY CORROSION. REMOVED AND REPLACED ENTIRE CHORD, REF SRM 51-30-2, SRM 53-10-2. WORK ACCOMPLISHED ON TRAMCO MWO NR FUSE LAGE 214. (M) 2 L 7 2 4F A16WE 1997020600788 19970206 00788 NM 1997 2 6 F3LA96056 1 19961118 A 5320 6546547 CHORD BOEING 737 737201 1384454 NM BS 727 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 212US 20212 PAE - FOUND CRACK INDICATION NOTED AT BS 727 OUTBOARD CHORD AT LEFT STRINGER 18A UPPER AFT FASTENER HOLE. ACCESSED AREA , INSTALLED TEMPORARY REPAIR PER SB 73753A1166. REINSTALLED ALL ITEMS REMOVED FOR ACCESS. ALL WORK DOCUMENTED ON TRAMC O MWO NR FUSELAGE 269. (M) 2 L 7 2 4F A16WE 1997020600789 19970206 00789 NM 1997 2 6 F3LA96055 1 19961118 A 5320 6546547 CHORD BOEING 737 737201 1384454 NM BS 727 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 212US 20212 PAE - FOUND CRACK INDICATIONS NOTED IN BS 727 OUTBOARD CHORD AT RT STRINGER 18A BETWEEN FORWARD AD AFT FASTENERS, UPPER AND LOWER. ACCESSED AREA. INSTALLED TEMPORARY REPAIR PER SB 737-53A1166. REINSTALLED ALL ITEMS REMOVED FOR ACCESS. W ORK DOCUMENTED ON TRAMCO MWO NR FUSELAGE 268. (M) 2 L 7 2 4F A16WE 1997020600790 19970206 00790 NM 1997 2 6 F3LA96054 1 19961113 A 5311 6546811 FRAME BOEING 737 737201 1384454 NM BS 987 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 212US 20212 PAE - WHILE WORKING FLOOR WEB AT BS 987, FOUND CORROSION AND MECHANICAL DAMAGE ON FRAME AT BS 993, RBL 49, WL 210-206. B LENDED OUT CORROSION ON FRAME. FOUND OUT OF LIMITS. CUT OUT DAMAGED AREA OF FRAME. MECHANICAL DAMAGE WAS LOCATED ON W EB AREA OF FRAME. CUTOUT DAMAGED AREA. FAIL/SAFE CHORD ON FRAME WAS ALSO DAMAGED. CUT OUT DAMAGED AREA. FABRICATED R EPAIR PARTS FOR FRAME FLANGE, FRAME WEB, AND FAIL/SAFE CHORD. TREATED ALL REPAIR PARTS AND INSTALLED WET WITH SEALANT. REF SRM 51-40-2, SRM 51-40-3, SRM 51-40-4. WORK ACCOMPLISHED ON TRAMCO MWO NR INTERIOR 230. (M) 2 L 7 2 4F A16WE 1997020600791 19970206 00791 NM 1997 2 6 F3LA96053 1 19961114 A 5315 6546811 FLOORBEAM BOEING 737 737201 1384454 NM BS 986.5 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 212US 20212 PAE - FOUND CORROSION (C53-107-02) ON FLOORBEAM AT NUTCLIP HOLE BS 986.5 RBL 18 UNDER SIDE OF UPPER CHORD. REPAIRED FLO OR BEAM AT BS 986.5, RLB 18, WL 208 IAW EWO NR 96-0742, SRM 53-10-0 AND SRM 51-20-01 CUST NR 0000844 INT NR 224. (M) 2 L 7 2 4F A16WE 1997020600792 19970206 00792 NM 1997 2 6 F3LA96052 1 19961115 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 260-266 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 212US 20212 PAE - FOUND CORROSION ON FORWARD END OF STRINGER BS 260-266 STRINGER 22L. FOUND CORROSION OUT OF LIMITS. CUT OUT DAMAG ED SECTION OF STRINGER AND REPAIRED PER SRM 53-10-03. WORK ACCOMPLISHED ON TRAMCO MWO FUSELAGE 289. (M) 2 L 7 2 4F A16WE 1997020600793 19970206 00793 NM 1997 2 6 F3LA96051 1 19961021 A 5313 655162812 STRINGER BOEING 737 737201 1384454 NM BS 947-967 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 214AU 20214 PAE - FOUND CORROSION AROUND FASTENERS IN STRINGER 27R, BS 947-967 WL 173. REMOVED DAMAGED SECTION OF STRINGER 27R, FAB RICATED REPAIR PARTS AND INSTALLED IAW SRM 51-40-3. (M) 2 L 7 2 4F A16WE 1997020600794 19970206 00794 NM 1997 2 6 F3LA96050 1 19961018 A 5312 6516300970 BULKHEAD WEB BOEING 737 737201 1384454 NM BS 178 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 214AU 20214 PAE - FOUND NUMEROUS PREVIOUS REPAIRS AND MORE CRACKS DURING INSPECTION ON BS 178 CENTER WEB BULKHEAD. CENTER WEB WS RE PLACED IAW BOEING SRM AND BOEING DRAWING NR 65-16300. REPLACEMENT ACCOMPLISHED ON TRAMCO MWO FUSELAGE 212. (M) 2 L 7 2 4F A16WE 1997020600795 19970206 00795 NM 1997 2 6 F3LA96049 1 19961018 A 5312 654540969 BULKHEAD WEB BOEING 737 737201 1384454 NM BS 663.75 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 214AU 20214 PAE - FOUND 1 INCH LONG CRACK IN BS 663.75 BULKHEAD WEB, RBL 48, 8.5 INCHES BELOW THE PRESSURE DECK. REPAIRED CRACK IN BULKHEAD WEB BS 663.75, RBL 48 8.5 INCHES BELOW PRESSURE DECK IAW EWO 96-0606. LEAK CHECKED ALL ITEMS. REMOVED FOR ACC ESS, NO LEAKS FOUND. REF TRAMCO WORK ORDER FUSELGE 175. (M) 2 L 7 2 4F A16WE 1997020600796 19970206 00796 NM 1997 2 6 F3LA96048 1 19961017 A 5320 CHORD BOEING 737 737201 1384454 NM BS 727 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 214AU 20214 PAE - FOUND CRACK INDICATIONS IN LT BS 727, STRINGER 18A OUTBOARD CHORD FORWARD AND AFT OF BOTH FASTENER HOLES. ACCESSE D REPAIR AREA. FOUND CRACKS CONTAINED IN FASTENER HOLES. FABRICATED AND INSTALLED REPAIR PARTS FOR INTERIM REPAIR PER SB 737-53A1166. RE-INSTALLED ALL ITEMS REMOVED FOR ACCESS. WORK DOCUMENTED ON TRAMCO MWO FUSELAGE 289. (M) 2 L 7 2 4F A16WE 1997020600797 19970206 00797 NM 1997 2 6 F3LA96047 1 19961015 A 5320 STIFFENER BOEING 737 737201 1384454 NM BS 203.5 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 214AU 20214 PAE - FOUND CRACK EMANATING FROM FASTENER HOLE AT BS 540, WL 203.5, LBL 26 ON VERTICAL STIFFENER. REMOVED DAMAGED STIFF ENER. FABRICATED NEW STIFFENER AND INSTALLED PER SRM 57-10-02, SRM 51-30-02. WORK DOCUMENTED ON TRAMCO MWO INTERIOR 17 4. (M) 2 L 7 2 4F A16WE 1997020600798 19970206 00798 NM 1997 2 6 F3LA96046 1 19961017 A 5315 65468032 FLOORBEAM BOEING 737 737201 1384454 NM BS 520 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 214AU 20214 PAE - FOUND FLOORBEAM CRACKED IN UPPER RADIUS BS 520 WL 207.75, RBL 25 AND RBL 46. REPAIRED FLOORBEAM CRACK AT BS 520, WL 207.75, RBL 25 AND RBL 46 IAW EWO 396-0643. (M) 2 L 7 2 4F A16WE 1997020600799 19970206 00799 NM 1997 2 6 F3LA96045 1 19961017 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM BS 520 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 214AU 20214 PAE - FOUND FLOORBEAM CRACKED IN UPPER RADIUS AT BS 520, WL 207.75, LBL 25 - LBL 47. REPAIRED CRACKS IN FLOORBEAM AT BS 520, WL 207.75, LBL 25, LBL 45 AND LBL 47 PER EWO NR 96-0643. (M) 2 L 7 2 4F A16WE 1997020600800 19970206 00800 NM 1997 2 6 F3LA96044 1 19961016 A 5320 651360086 CHORD BOEING 737 737201 1384454 NM BS 178 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 214AU 20214 PAE - HFEC INSPECTION OF THE BS 178 LT SIDE CHORD AT WL 194-196 SHOWS A CRACK INDICATION. CUT OUT DAMAGED AREA OF CHORD . FABRICATED REPAIR PARTS AND INSTALLED REPAIR PER TRAMCO EWO NR 96-0619. WORK DOCUMENTED ON TRAMCO MWO FUSELAGE 276. (M) 2 L 7 2 4F A16WE 1997020600801 19970206 00801 NM 1997 2 6 F3LA96042 1 19961015 A 5320 65353022 CHORD BOEING 737 737201 1384454 NM BS 540 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 214AU 20214 HFEC INSPECTION EXHIBITS CRACK APPROX 1.5 INCH LONG IN RADIUS OF BS 540 CHORD BETWEEN STRINGER 21R AND STRINGER 22R, CRA CK IS ON SPLICE PLATE. ACCESSED AREA, REMOVED DAMAGED SPLICE PLATE. FABRICATED NEW SPLICE PLATE PER TRAMCO EO NR 96-06 29. INSTALLED NEW SPLICE PLATE AND ALL ITEMS REMOVED FOR ACCESS. WORK DOCUMENTED ON TRAMCO MWO FUSELAGE 284. (M) 2 L 7 2 4F A16WE 1997020600802 19970206 00802 NM 1997 2 6 F3LA96041 1 19961015 A 5320 6573743 DOOR FRAME BOEING 737 737201 1384454 NM CARGO DOOR CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 214AU 20214 PAE - HFEC INSPECTION OF THE FORWARD CARGO DOOR FRAME, REVEALED A CRACK INDICATION AT STRINGER 23R ON THE FORWARD SIDE O F THE FRAME AT THE LOWEST OUTBOARD CORNER OF THE DOOR STOP FITTING. ACCESSED INDICATED AREA AND FOUND NUMEROUS GOUGES L OCATED BENEATH DOOR STOP FITTING. BLENDED GOUGES AND OVERSIZED FASTENER HOLES FOR STOP FITTING. RE-INSTALLED ALL ITEMS REMOVED FOR ACCESS REF TRAMCO EWO NR 96-0655. WORK DOCUMENTED ON TRAMCO MWO FUSELAGE 277. (M) 2 L 7 2 4F A16WE 1997020600803 19970206 00803 NM 1997 2 6 F3LA96040 1 19961016 A 5314 6747693 KEELBEAM BOEING 737 737201 1384454 NM BS 814-818 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 214AU 20214 PAE - FOUND CRACK IN THE AFT END OF RT KEELBEAM BS 814-818, STRINGER 27 RT. REPAIRED CRACK IAW TRAMCO EWO 96-0613. WOR K DOCUMENTED ON TRAMCO MWO FUSELAGE 255. (M) 2 L 7 2 4F A16WE 1997020600804 19970206 00804 NM 1997 2 6 F3LA96039 1 19961014 A 5311 6573741 FRAME BOEING 737 737201 1384454 NM BS 294.5 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 214AU 20214 PAE - FOUND CRACK IN FRAME WEB AT UPPER CORNER OF STRINGER CUTOUT BS 294.5, STRINGER 18R. FOUND CRACK CONTAINED IN FAST ENER HOLE. REPAIRED PER SRM 51-40-02 AND TRAMCO ER100396MW3. WORK DOCUMENTED ON TRAMCO MWO FUSELAGE 233. (M) 2 L 7 2 4F A16WE 1997020600805 19970206 00805 NM 1997 2 6 F3LA96038 1 19961015 A 5311 6573743 FRAME BOEING 737 737201 1384454 NM BS 520 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 214AU 20214 PAE - FOUND CORROSION (C53-208-01) ON AFT SIDE OF FRAME BS 520 RBL 7, WL 150. CORROSION FOUND TO BE OUT OF LIMITS. REP AIRED FRAME PER SRM 51-40-3. (M) 2 L 7 2 4F A16WE 1997020600806 19970206 00806 NM 1997 2 6 F3LA96037 1 19961014 A 5320 SHEAR TIE BOEING 737 737201 1384454 NM BS 360 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 214AU 20214 PAE - FOUND CORROSION ON SHEAR TIE AT BS 360, BETWEEN STRINGERS 27 LEFT AND 27 RIGHT. FOUND CORROSION OUT OF LIMITS. C UT OUT DAMAGE AND REPAIRED PER SRM 53-10-4, FIG 8. DURING REPAIR, FOUND DAMAGE TO BONDED DOUBLER BENEATH SHEAR TIE. CU T OUT DAMAGED DOUBLER AND REPAIRED PER SRM 53-30-3, FIG 17. REF WORK ORDER FUSELAGE 292. (M) 2 L 7 2 4F A16WE 1997020600807 19970206 00807 NM 1997 2 6 F3LA96036 1 19961012 A 5315 BAC15051238 FLOORBEAM BOEING 737 737201 1384454 NM BS 500 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 214AU 20214 PAE - FOUND CORROSION ON UNDERSIDE OF CARGO FLOORBEAM BS 500, RBL 18, WL 156. REMOVED CORROSION ON UNDERSIDE OF FLOORBE AM AND REPAIRED IAW SRM 53-10-1, 51-40-3 REF WORK ORDER FUSELAGE 262. (M) 2 L 7 2 4F A16WE 1997020600808 19970206 00808 NM 1997 2 6 F3LA96035 1 19961012 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 296 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 214AU 20214 PAE - FOUND CRACK IN STRINGER 10 LEFT, BS 296, WL 256. REMOVED DAMAGED SECTION OF STRINGER 10L BS 296, WL 256. REPAIRE D STRINGER IAW SRM 53-10-3 FIGURE 3 RED WORK ORDER INTERIOR 154. (M) 2 L 7 2 4F A16WE 1997020600809 19970206 00809 NM 1997 2 6 F3LA96034 1 19961012 A 5230 65C8073589 INTERCOSTAL BOEING 737 737201 1384454 NM CARGO DOOR CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 214AU 20214 PAE - FORWARD CARGO DOOR FORWARD AND AFT HINGE ARM MOUNT FORGED INTERCOSTALS ARE CRACKED ON THE AFT OTBOARD FLANGE. REM OVED AND REPLACED FORWARD CARGO DOOR FORWARD AND AFT HINGE ARM MOUNT FORGED INTERCOSTALS IAW SRM 51-10-1, 51-10-2, 51-30 -2, REF WORK ORDER DOORS 93. (M) 2 L 7 2 4F A16WE 1997020600810 19970206 00810 NM 1997 2 6 F3LA96033 1 19961012 A 5313 BAC1493659 STRINGER BOEING 737 737201 1384454 NM BS 277 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 214AU 20214 FOUND CRACK IN STRINGER 14R AT BS 277. STOP DRILLED CRACK AND INSTALLED REPAIR PER SRM 53-10-3, FIG 1. WORK DOCUMENTED ON TRAMCO NRC INTERIOR 178. (M) 2 L 7 2 4F A16WE 1997020600811 19970206 00811 NM 1997 2 6 F3LA96032 1 19961012 A 5311 FRAME BOEING 737 737201 1384454 NM BS 807 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 214AU 20214 PAE - FOUND CORROSION ON FORWARD AND AFT SIDE OF FRAME AND CORRODED AND CRACKED SHEAR TIE BS 807, LBL 25 - RBL 25, WL 14 8-153. REMOVED CORROSION FROM FRAME AND FOUND WITHIN LIMITS OF SRM. CUTOUT DAMAGED SHEAR TIES BETWEEN STRINGER 26-27L AND STRINGER 27L-27R AND REPAIRED PER SRM 53-10-04, FIG 10. DURING REPAIR FOUND CORROSION ON SKIN INNER SURFACE BENEATH SHEAR TIE BETWEEN STRINGER 27L-27R WITH EVIDENCE OF PREVIOUS REWORK. AFTER CORROSION REMOVAL FOUND SKIN OUT OF LIMITS PER SRM. CUTOUT DAMAGED SKIN AND REPAIRED PER SRM 53-30-3, FIG 1. WORK DOCUMENTED ON TRAMCO NRC FUSELAGE 252. (M) 2 L 7 2 4F A16WE 1997020600813 19970206 00813 NM 1997 2 6 F3LA96026 1 19960930 A 5330 6546570 SKIN BOEING 737 737301 1384611 NM BS 1032-1050 GOUGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 FOUND SKIN GOUGED AND DENTED FROM 1032-1050, BETWEEN STRINGERS 23R AND 24R. REMOVED DAMAGED SKIN AND EXISTING DOUBLER, FABRICATED AND INSTALLED NEW DOUBLER AND FILLER AT BS 1032-1050 BETWEEN STRINGERS 23R AND 24R PER SRM 53-80-01. (M) 2 L 7 2 4F RT A16WE 1997020600814 19970206 00814 NM 1997 2 6 F3LA96025 1 19960930 A 5230 6546921168 DOOR FRAME BOEING 737 737301 1384611 NM CARGO DOOR CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 PAE - FORWARD CARGO DOOR AFT LOWER CORNER FRAME IS CRACKED AT OUTBOARD RADIUS AT NR 5 STOP FITTING (2.5 INCH LONG). REM OVED FORWARD CARGO DOOR AND DAMAGED AREA OF AFT LOWER CORNER FRAME, INSTALLED NEW AFT LOWER CORNER FRAME ON FORWARD CARG O DOOR, INSTALLED FORWARD CARGO DOOR PER MM 52-31-00, SRM 51-40-02 AND SRM 51-70-13. (M) 2 L 7 2 4F RT A16WE 1997020600815 19970206 00815 NM 1997 2 6 F3LA96024 1 19960927 A 5754 65C266011 SKIN BOEING 737 737301 1384611 NM NR 1 SLAT CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 PAE - NR 1 SLAT LOWER SKIN CRACKED IN SEVERAL AREAS AT FASTENERS AT ACTUATOR. REPAIRED NR 1 SLAT LOWER SKIN AT T/E JUST AFT OF ACTUATOR ROD END IAW 737 DRAWING 65C30133. (M) 2 L 7 2 4F RT A16WE 1997020600820 19970206 00820 NM 1997 2 6 F3LA96022 1 19960919 A 5314 65621258 KEEL BEAM BOEING 737 737317 138447P NM BS 546-549 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 23177 PAE - FOUND CORROSION ON RT KEEL BEAM HORIZONTAL FLANGE AT BS 546-549, RBL 6.5, WL 148. REMOVED CORROSION AND FOUND OUT OF LIMITS PER SRM. FABRICATED AND INSTALLED REPAIR STRAPS PER EO NR 96-0582. ALL WORK ACCOMPLISHED ON NRC FUSELAGE 55 , UNDER WORK ORDER NR 214912. (M) 2 L 7 2 4F RT A16WE 1997020600821 19970206 00821 NM 1997 2 6 F3LA96023 1 19960930 A 5230 6546921169 DOOR FRAME BOEING 737 737301 1384611 NM CARGO DOOR CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 PAE - FOUND FORWARD CARGO DOOR FORWARD LOWER FRAME IS CRACKED AT INBOARD RADIUS BENEATH UPLOCK HOOK. ALSO, CRACKED AT O UTBOARD LOCATION BETWEEN NR 4 AND NR 5 STOP FITTING. ACCESSED INNER SKIN. REMOVED FORWARD LOWER CORNER FRAME. INSTALL ED NEW FORWARD LOWER CORNER FRAME. REINSTALLED INNER SKIN AND ALL OTHER ITEMS ACCESSED PER SRM 51-40-02 AND 51-70-13. ( M) 2 L 7 2 4F RT A16WE 1997020600822 19970206 00822 NM 1997 2 6 USAASB96273 1 19961229 A 2913 5718607 HYDRAULIC PUMP BOEING 737 737401 1384701 NM LT MLG WW FAILED A USAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 19 413US 24246 23882 BWI - FL 1282 - THE 'A' HYDRAULIC SYSTEM OVERHEAT LIGHT ILLUMINATED DURING FLIGHT. CREW TURNED PUMP OFF AND AFTER FIVE MINUTES, LIGHT WENT OUT. HYDRAULIC QTY AND PRESSURE WERE NORMAL. FLIGHT DIVERTED TO BWI AND LANDED WITHOUT FURTHER INC IDENT. MAINTENANCE REMOVED AND REPLACED THE 'A' SYSTEM ELECTRIC HYDRAULIC PUMP AND CASE DRAIN FILTER. SERVICED 'A' HYD RAULIC SYSTEM RESERVOIR. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1997020600829 19970206 00829 EA 1997 2 6 97ZZZM184 2 19961202 A 7310 1143890327 FUEL FILTER BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA LEFT ENGINE CONTAMINATED A YADA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 AL 01 1563C UC20 PCE32436 APPROX 30 MINUTES OUT, INBOUND TO ANC, LEFT ENGINE FUEL FLOW, ITT, TORQUE AND N1 RPM DECREASED. PILOT ALSO REPORTED COM PRESSOR STALL. LEFT ENGINE SHUT DOWN. AIRCRAFT LANDED AT ANC WITHOUT INCIDENT. MAINTENANCE FOUND LEFT AIRFRAME FUEL F ILTER CLOGGED WITH RUST AND OTHER DEBRIS. REPLACED AIRFRAME FUEL FILTER ELEMENTS AND ENGINE DRIVEN FUEL PUMP FILTER. A IRCRAFT GROUND RUN AND TEST FLOWN WITH NO PROBLEMS. AIRCRAFT RETURNED TO SERVICE. CONTINUING INVESTIGATION AS TO SOURC E OF FUEL CONTAMINATION. (M) 2 L 7 2 4T 4 T RT A24CE E4EA 1997020600830 19970206 00830 CE 1997 2 6 97ZZZM185 1 19961211 A 7931 1013890235 TRANSMITTER BEECH 1900 1900C 1154161 CE RT ENGINE FAILED A YADA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 AL 01 5632C UC81 DURING CLIMB FROM ANC, RIGHT ENGINE OIL PRESSURE DROPPED TO 30 PSI, LOW PRESSURE WARNING LIGHT DID NOT ILLUMINATE, AIRCR AFT RETURNED TO ANC. RESET CANNON PLUG ON OIL PRESSURE TRANSMITTER. GROUND RAN ENGINE, OIL PRESSURE INDICATION NORMAL. AIRCRAFT RETURNED TO SERVICE. 12 MINUTES AFTER TAKEOFF FROM ANC, RIGHT ENGINE OIL PRESSURE DROPPED TO 30 PSI, LOW OIL PRESSURE LIGHT DID NOT COME ON. MAINTENANCE REPLACED OIL PRESSURE TRANSMITTER. OPS CHECKED NORMAL, AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1997020600832 19970206 00832 NM 1997 2 6 AALA961727 1 19961126 A 3350 1721651 CONNECTOR BOEING 767 767223 1385123 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 321AA 22322 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT PAX SEATS 25B AND 27B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AND CONTACT AT PAX SEAT 27B AND RESECURRED EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 25B. SYSTEM GROUND CHE CKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1997020600833 19970206 00833 NM 1997 2 6 AALA961531 1 19961018 A 3397 WIRE BOEING 767 767223 1385123 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 336AA 22334 SFO - DURING OVENIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 24B INOPERATIVE. REPAIRED BROKEN EMERGENCY EXIT LIGHT WIR E AT PAX SEAT 24B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1997020600834 19970206 00834 NM 1997 2 6 AALA961509 1 19961016 A 3350 1703663 CONNECTOR BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 371AA 25198 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 35H INOPERATIVE. REPLACED BROKEN EMERGENCY EXIT LIGHT CO NNECTOR AT PAX SEAT 35H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1997020600835 19970206 00835 NM 1997 2 6 AALA961677 1 19961118 A 3350 A3030398101 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 614AA 24490 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 4E THROUGH 6E INOPERATIVE. RESECURED LOOSE E MERGENCY FLOOR LIGHT CONNECTOR BY PAX SEAT ROW 4E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1997020600836 19970206 00836 NM 1997 2 6 AALA961676 1 19961117 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 306AA 22312 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 29B INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT CANNON PLUG AT PAX SEAT 29B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1997020600837 19970206 00837 NM 1997 2 6 AALA961593 1 19961103 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 324AA 22325 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 29H INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CO NNECTOR AT PAX SEAT 29H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1997020600839 19970206 00839 NM 1997 2 6 AALA961619 1 19961108 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 376AN 25445 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 32H INOPERATIVE. REPAIRED BROKEN EMERGENCY EXIT LIGHT WI RE AT PAX SEAT 32H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1997020600840 19970206 00840 NM 1997 2 6 AALA961634 1 19961112 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 661AA 25295 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR LIGHTING AT AFT CABIN INOPERATIVE. REPAIRED BROKEN EMERGENCY EXIT FL OOR LIGHT WIRE AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1997020600841 19970206 00841 NM 1997 2 6 AALA961613 1 19961105 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 322AA 22323 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 24H INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CO NNECTOR AT PAX SEAT 24H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1997020600842 19970206 00842 WP 1997 2 6 AALA961722 1 19961122 A 2150 NH105523110 CLAMPS DOUG DC9 DC982 3022082 WP LT PACK LOOSE A AALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 SW 07 294AA 49306 BNA - FLT 1573 - EN ROUTE BNA-DFW - DURING CRUISE, THE TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. LIGHT EXTIN GUISHED WITH POWER REDUCTION. AIR INTERRUPTED AND LANDED BNA WITHOUT FURTHER INCIDENT. RESECURRED LEFT PACK WATER SEPA RATOR CLAMPS. ACCOMPLISHED DUCT LEAK CHECK DURING ENGINE RUN UP AT HIGH POWER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1997020600875 19970206 00875 NM 1997 2 6 F3LA97005 1 19961220 A 5330 SKIN BOEING 737 737201 1384454 NM BS 791 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 PAE - FOUND CRACK IN EXTERNAL SKIN AT BS 797, STRINGER 24 LEFT, CRACK WAS APPROXIMATELY 4 INCHES LONG. STOP DRILLED CRA CK. FABRICATED REPAIR DOUBLER AND INSTALLED PER SRM 53-30-3. WORK WAS DOCUMENTED ON TRAMCO CARD NR FUSELAGE 240, CUST ID NR 0732. (M) 2 L 7 2 4F A16WE 1997020600879 19970206 00879 NM 1997 2 6 F3LA96075 1 19961231 A 5312 65465622 DOME BOEING 737 737201 1384454 NM DOME BS 1016 MIS REPAIRED A F3LA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 03 207AU 19423 PAE - REPAIR ON BS 1016 PRESSURE DOME DOES NOT CONFORM TO THE SRM. REMOVED OLD REPAIR AND INSTALLED NEW REPAIR ON PRESS URE DOME BS 1016, LBL 19, WL 244 PER SRM 53-10-4 FIGURE 3. (M) 2 L 7 2 4F A16WE 1997020600880 19970206 00880 NM 1997 2 6 F3LA96074 1 19961230 A 5315 6545812 FLOORBEAM BOEING 737 737201 1384454 NM BS 1006 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 PAE - FOUND CORROSION (C53-107-02) ON FLOORBEAM BS 1006 LBL 10 TO LBL 36 WL 208. CORROSION DAMAGE FOUND TO BE OUT OF LI MITS. REMOVED DAMAGED AREA AND INSTALLED REPAIR PART IAW SRM 53-10-1, 53-10-6 AND 53-10-9 AT BS 1006 LBL 10 TO LBL 36 W L 208. (M) 2 L 7 2 4F A16WE 1997020600881 19970206 00881 NM 1997 2 6 F3LA96073 1 19961230 A 5315 609247 FLOORBEAM BOEING 737 737201 1384454 NM BS 947 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 PAE - FOUND CORROSION (C53-107-02) ON TOP OF FLOORBEAM BS 947 RBL 40-47 WL 208 AND RBL 5-15. FOUND TO BE OUT OF LIMITS. REPLACED TOP CHORD AT STATION 947 LBL 35 TO RBL 61 WL 208 IAW SRM 53-10-9 AND EWO 96-0931. (M) 2 L 7 2 4F A16WE 1997021100001 19970211 00001 GL 1997 2 11 COEA9674601 3 19961118 A 6110 PROPELLER CESSNA 208 208B 2073701 CE MCAULY 3G34C7 3GFR34C701 GL ENGINE DAMAGED A COEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 13 746FX 306 952161 208B0498 952161 ON TAXI OUT OF ANC, DEICING CONDENSATION BEGAN TO BUILD ON THE INSIDE OF THE WINDSHIELD. PILOT ATTEMPTED TO USE BLEED A IR TO DEFROST THE WINDSHIELD. VISABILITY WAS DENSE FOG AND THE RAMP WAS COVERED WITH ICE AND SNOW. THE PILOT WAS IN TH E PROCESS OF STOPPING THE ACFT TO WAIT FOR THE WINDSHIELD TO DEFROST WHEN HE HEARD A CLUNK. PILOT IMMEDIATELY SHUT DOWN THE AIRCRAFT. VISUAL INSPECTION DISCOVERED ACFT HAD STRUCK AN OBSCURED TAXIWAY LIGHT. REPLACEMENT PROPELLER EN ROUTE. TURBINE SECTIONS INSPECTED IAW P & W MM. NO DEFECTS NOTED. PROPELLER REMOVED AND REPLACED IAW MANUFACTURE INSTRUCTIO NS. ENGINE GROUND RUN AND FUNCTION CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE 11-21-96. (X) 1 H 7 1 3T A37CE 5 C P60GL 1997021100002 19970211 00002 WP 1997 2 11 IXXA9700010 1 19961118 A 5320 GUSSET DOUG DC8 DC862 3021970 WP BS 128 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 21CX 11474 45955 DURING ROUTINE C-CHECK INSPECTION, A CORRODED GUSSET AT FUSELAGE STATION 128 AND LONGERON 22 LEFT WAS FOUND. THE GUSSET WAS REMOVED, FABRICATED AND INSTALLED IN ACCORDNACE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL 53-1-0, AND FAA DER APPRO VED SKETCH B68-R16. 2 L 7 4 4F 4A25 1997021100004 19970211 00004 NM 1997 2 11 MALA965265 1 19961225 A 3010 BOOT DHAV DHC8 DHC8102 2809003 NM RT WING PUNCTURED A MALA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 819MA 251 FLT 3183 - EN ROUTE TO TVC, THE NR 2 INBOARD BOOT SECTION FROM THE WING TIP ON THE RIGHT SIDE DIDN'T INFLATE. THE AIRCR AFT RETURNED TO DTW. MAINTENANCE PATCHED A SMALL HOLE IN THE NR 2 BOOT AND REMOVED MOISTURE. ALL CHECKS SATISFACTORY. (M) 2 H 7 2 4T RT A13NM 1997021300065 19970213 00065 CE 1997 2 13 97ZZZX618 1 19960108 A 2612 DETECTOR LOOP CESSNA 208 208 2073702 CE ENG CASE CHAFED A A BAJA E ENGINE SHUTDOWN N FALSE WARNING TX TAXI/GRND HDL 1 AL 01 9642F 20800110 WHILE BACK TAXIING PRIOR TO TAKEOFF, THE PILOT WAS ALERTED OF AN 'ENGINE FIRE' ANNUNCIATOR ALARM. THE ENGINE WAS IMMEDI ATELY SHUT DOWN AND ALL PASSENGERS EVACUATED SAFELY. MAINTENANCE PERSONNEL FOUND NO EVIDENCE INDICATING THERE WAS A FIR E PRESENT. THE AIRCRAFT RETURNED TO THE MAINTENANCE BASE FOR A DETAILED INSPECTION OF THE DETECTION SYSTEM. IT WAS DISC OVERED THAT PORTION OF THE FIRE DETECTION LOOP WAS CHAFED AGAINST THE ACCESSORY CASE ALLOWING IT TO TOUCH GROUND AND GIV ING A FALSE INDICATION OF ENGINE FIRE. 1 H 7 1 3T NT A37CE 1997021300080 19970213 00080 SO 1997 2 13 97ZZZX634 1 19961220 A 2913 31800002 POWER PACK PIPER PA23 PA23250 7102308 SO NLG MALFUNCTION A L BRDA O OTHER P NO WARNING INDICATION AP APPROACH 1 NE 05 40571 6206 277405313 AIRCRAFT WAS ON A PART 91 TRAINING FLIGHT. ON APPROACH TO AIRPORT, PILOT PUT THE LANDING GEAR LEVER DOWN. LANDING GEAR WENT DOWN, BUT DID NOT GET A GREEN (NOSE DOWN AND LOCKED LIGHT). THE PILOT RECYCLED THE LANDING GEAR. THE LANDING GEA R CAME DOWN, BUT, AGAIN, NO NOSE GEAR GREEN LIGHT. THE PILOT VERIFIED THAT THE NOSE GEAR WAS DOWN WITH (GEAR VERIFICATI ON MIRROR). HE LANDED NORMALLY, ON LANDING THE NOSE GREEN LIGHT CAME ON. POWER PACK BYPASSING INTERNALLY. 1 L 7 2 3O 1A10 1997021300229 19970213 00229 EU 1997 2 13 97ZZZX636 1 19961107 A 6210 117150081 BLADE BOLKMS 117 BK117A3 5626015 EU M/R CRACKED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 528SF 6407 2856 123 7104 M/R BLADE CRACKS AND SKIN BULGING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1997021300230 19970213 00230 EU 1997 2 13 97ZZZX637 1 19961107 A 6210 117150081 BLADE BOLKMS 117 BK117A3 5626015 EU M/R CRACKED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 528SF 6407 2856 223 7104 M/R BLADE CRACKS AND SKIN BULGING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1997021300231 19970213 00231 CE 1997 2 13 97ZZZX638 1 19961215 A 7930 991028716 SWITCH 2456 CESSNA 441 441 2076020 CE OIL SYS STICKS A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 8970N 570 4410092 SWITCH STICKS IN OPEN POSITION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 L 7 2 3T RT A28CE 1997021300232 19970213 00232 NM 1997 2 13 97ZZZX639 1 19960803 A 6220 900R32101004101 SEAL DOUG MD900 MD900 3027375 NM M/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 789 90000012 M/R HEAD SEAL WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997021300233 19970213 00233 NM 1997 2 13 97ZZZX640 1 19961125 A 6320 900D3409526105 HOSE DOUG MD900 MD900 3027375 NM M/R XMSN LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 901CF 453 453 90000012 HOSE LEAKING BEYOND SERVICEABLE LIMITS. SMALL PINHOLE 3 INCHES FROM OIL PUMP OUTLET. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997021300234 19970213 00234 NM 1997 2 13 97ZZZX641 1 19960924 A 7110 900F3611805101 LATCH DOUG MD900 MD900 3027375 NM COWL WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 936 90000012 COWL LATCH WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997021300235 19970213 00235 NM 1997 2 13 97ZZZX642 1 19961007 A 6310 900D1400528101 INPUT PINION DOUG MD900 MD900 3027375 NM XMSN LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 901CF 2062190054 90000012 INPUT PINION UPON INSTALLATION UNIT BEGAN LEAKING OIL BEYOND SERVICEABLE LIMITS. THIS REPORT FOR INFORMATION ONLY. REP LACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997021300236 19970213 00236 NM 1997 2 13 97ZZZX643 1 19961110 A 2140 900P2250229103 COVER PLATE DOUG MD900 MD900 3027375 NM CABIN HEAT WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 90000012 COVER PLATE WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997021300237 19970213 00237 NM 1997 2 13 97ZZZX644 1 19961110 A 5210 900F2305225103 ROLLER DOUG MD900 MD900 3027375 NM DOOR TRACK WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 1030 90000012 CABIN DOOR ROLLER TRACK WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW 5 EACH UNITS, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997021300238 19970213 00238 NM 1997 2 13 97ZZZX645 1 19960926 A 6220 900R3101004101 SEAL DOUG MD900 MD900 3027375 NM M/R LEAK A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 901CF 48 90000012 M/R HEAD SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997021300239 19970213 00239 NM 1997 2 13 97ZZZX646 1 19960611 A 6220 900R3101001107 BEARING DOUG MD900 MD900 3027375 NM M/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 635 0206040359 90000012 M/R CENTERING BEARING ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. DEBONDING. REPLACED WITH NEW UNIT, CORRECTED PROBLE M. 1 G 7 2 3U NC H19NM 1997021300240 19970213 00240 NM 1997 2 13 97ZZZX647 1 19960611 A 6220 900R3101001107 BEARING DOUG MD900 MD900 3027375 NM M/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 635 0206040358 90000012 M/R CENTERING BEARING ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. DEBONDING. REPLACED WWITH NEW UNIT, CORRECTED PROBL EM. 1 G 7 2 3U NC H19NM 1997021300241 19970213 00241 NM 1997 2 13 97ZZZX648 1 19960611 A 6220 900R3101001107 BEARING DOUG MD900 MD900 3027375 NM M/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 635 0206040357 90000012 M/R CENTERING BEARING ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. DEBONDING. REPLACED WTIH NEW UNIT, CORRECTED PROBLE M. 1 G 7 2 3U NC H19NM 1997021300242 19970213 00242 NM 1997 2 13 97ZZZX649 1 19960611 A 6220 900R3101001107 BEARING DOUG MD900 MD900 3027375 NM M/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 635 0206040356 90000012 M/R CENTERING BEARING ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997021300243 19970213 00243 NM 1997 2 13 97ZZZX650 1 19960529 A 6220 900R3101001107 BEARING DOUG MD900 MD900 3027375 NM M/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 601 90000012 M/R CENTERING BEARING ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. DEBONDING. REPLACED WITH NEW UNIT, CORRECTED PROBLE M. 1 G 7 2 3U NC H19NM 1997021300244 19970213 00244 NM 1997 2 13 97ZZZX651 1 19960926 A 6210 900R3100001101 RETAIN BOLT DOUG MD900 MD900 3027375 NM BLADE GROOVED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 936 0098840213 90000012 BLADE RETAIN BOLT UNIT EXCESSIVELY GROOVED. REPLACED WITH NEW UNIT, CORRECTED PROBLEM 1 G 7 2 3U NC H19NM 1997021300245 19970213 00245 NM 1997 2 13 97ZZZX652 1 19960926 A 6210 900R3100001101 RETAIN BOLT DOUG MD900 MD900 3027375 NM BLADE GROOVED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 936 0098840332 90000012 BLADE RETAIN BOLT UNIT EXCESSIVELY GROOVED. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997021300246 19970213 00246 NM 1997 2 13 97ZZZX653 1 19960611 A 6200 900R1103001111 FLEX BEAM DOUG MD900 MD900 3027375 NM M/R BUMPER DELAMINATED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 190 099990302 90000012 FLEX BEAM BUMPER EXCESSIVE DELAMINATION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997021300247 19970213 00247 NM 1997 2 13 97ZZZX654 1 19960611 A 6200 900R1103001111 FLEX BEAM DOUG MD900 MD900 3027375 NM M/R BUMPER DELAMINATED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 190 099990301 90000012 FLEX BEAM BUMPER EXCESSIVE DELAMINATION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997021300248 19970213 00248 NM 1997 2 13 97ZZZX655 1 19960611 A 6200 900R1103001111 FLEX BEAM DOUG MD900 MD900 3027375 NM M/R BUMPER DELAMINATD A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 190 099990313 90000012 FLEX BEAM BUMPER EXCESSIVE DELAMINATION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997021300249 19970213 00249 NM 1997 2 13 97ZZZX656 1 19960926 A 3610 900P3250257101 VALVE DOUG MD900 MD900 3027375 NM BLEED CHECK STUCK A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 936 90000012 BLEED AIR CHECK VALVE STUCK CLOSED. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997021300250 19970213 00250 NM 1997 2 13 97ZZZX657 1 19961215 A 2140 900P2250229103 COVER PLATE DOUG MD900 MD900 3027375 NM HEAT CONTROL WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 56 90000012 HEAT CONTROL COVER WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997021300251 19970213 00251 NM 1997 2 13 97ZZZX658 1 19961215 A 2913 900H3821501103 PUMP DOUG MD900 MD900 3027375 NM NR 2 SYS MALFUNCTION A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 430 MX568401 90000012 HYDRAULIC PUMP, NR 2 SYSTEM PRESSURE TOO HIGH, 860 PSI. REPLACED WITH NEW UNIT, CORRECTED PROBLEM 1 G 7 2 3U NC H19NM 1997021300252 19970213 00252 NM 1997 2 13 97ZZZX659 1 19960531 A 7110 900F3611806101 LATCH DOUG MD900 MD900 3027375 NM COWLING SEIZED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 606 90000012 LOW PROFILE COWL LATCH SEIZED. WILL NOT MOVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997021300253 19970213 00253 NM 1997 2 13 97ZZZX660 1 19960615 A 7110 900F3611805101 LATCH DOUG MD900 MD900 3027375 NM COWLING WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 651 90000012 HIGH PROFILE COWL LATCH WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997021300254 19970213 00254 NM 1997 2 13 97ZZZX661 1 19961015 A 5610 900F3305405101 WINDSCREEN DOUG MD900 MD900 3027375 NM COCKPIT DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 988 90000012 THE TINTED SMOKE COLOR OF THE WINDSCREEN GLASS CREATED VISIBILITY PROBLEMS DURING NIGHT-TIME FLIGHTS, ESPECIALLY WHILE R UNNING THE UV FILTERED SX5 NIGHT SUN. PILOTS REPORTED SEVERAL INADVERTENT IFR PROBLEMS BECAUSE OF THE TINTED COLOR. TH E TINTED GLASS IS A FACTORY OPTION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997021300255 19970213 00255 NM 1997 2 13 97ZZZX662 1 19961015 A 5610 900F3305405102 WINDSCREEN DOUG MD900 MD900 3027375 NM COCKPIT DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 988 90000012 THE TINTED SMOKE COLOR OF THE WINDSCREEN GLASS CREATED VISIBILITY PROBLEMS DURING NIGHT-TIME FLIGHTS, ESPECIALLY WHILE R UNNING THE UV FILTERED SX5 NIGHT SUN. PILOTS REPORTED SEVERAL INADVERTENT IFR PROBLEMS BECAUSE OF THE TINTED COLOR. TH E TINTED GLASS IS A FACTORY OPTION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997021300256 19970213 00256 NM 1997 2 13 97ZZZX663 1 19960525 A 3210 900F2361408103 COMPRESSION PAD DOUG MD900 MD900 3027375 NM MLG WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 591 90000012 COMPRESSION PAD WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997021300257 19970213 00257 NM 1997 2 13 97ZZZX664 1 19961015 A 5610 900F2305607102 WINDSCREEN DOUG MD900 MD900 3027375 NM CHIN ASSY DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 988 90000012 THE TINTED SMOKE COLOR OF THE WINDSCREEN GLASS CREATED VISIBILITY PROBLEMS DURING NIGHT-TIME FLIGHTS, ESPECIALLY WHILE R UNNING THE UV FILTERED SX5 NIGHT SUN. PILOTS REPORTED SEVERAL INADVERTENT IFR PROBLEMS BECAUSE OF THE TINTED COLOR. TH E TINTED GLASS IS A FACTORY OPTION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997021300258 19970213 00258 NM 1997 2 13 97ZZZX665 1 19961015 A 5610 900F2305607101 WINDSCREEN DOUG MD900 MD900 3027375 NM CHIN ASSY DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 988 90000012 THE TINTED SMOKE COLOR OF THE WINDSCREEN GLASS CREATED VISIBILITY PROBLEMS DURING NIGHT-TIME FLIGHTS, ESPECIALLY WHILE R UNNING THE UV FILTERED SX5 NIGHT SUN. PILOTS REPORTED SEVERAL INADVERTENT IFR PROBLEMS BECAUSE OF THE TINTED COLOR. TH E TINTED GLASS IS A FACTORY OPTION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997021300259 19970213 00259 NM 1997 2 13 97ZZZX666 1 19960926 A 6230 900C2010511101 BUSHING DOUG MD900 MD900 3027375 NM SWASHPLATE WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 936 90000012 SWASHPLATE BUSHING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW 5 EACH UNITS, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997021300260 19970213 00260 NM 1997 2 13 97ZZZX667 1 19960525 A 6230 900C2010184103 SCISSORS DOUG MD900 MD900 3027375 NM M/R MAST WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 298 90000012 DRIVE SCISSORS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997021300261 19970213 00261 NM 1997 2 13 97ZZZX668 1 19961125 A 6320 900D3409526105 HOSE DOUG MD900 MD900 3027375 NM GR BOX LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 901CF 1059 90000012 HOSE LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997021300262 19970213 00262 NM 1997 2 13 97ZZZX669 1 19961224 A 6320 900D3409526105 HOSE DOUG MD900 MD900 3027375 NM GR BOX LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 901CF 33 90000012 HOSE LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997021300263 19970213 00263 NM 1997 2 13 97ZZZX670 1 19960803 A 6720 CEKP3AR112 BEARING DOUG MD900 MD900 3027375 NM T/R CONTROL WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 789 90000012 THRUST BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 3 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997021300264 19970213 00264 NM 1997 2 13 97ZZZX671 1 19960701 A 6720 CEKP3AR112 BEARING DOUG MD900 MD900 3027375 NM T/R CONTROL WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 691 90000012 THRUST BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 4 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997021300265 19970213 00265 NM 1997 2 13 97ZZZX672 1 19961110 A 5302 900F2306788103 HINGE DOUG MD900 MD900 3027375 NM T/B SPOILER WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 1030 90000012 SPOILER HINGE WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997021300266 19970213 00266 NM 1997 2 13 97ZZZX673 1 19960827 A 7920 900F5331230111 TUBE DOUG MD900 MD900 3027375 NM ENG OIL LEAK A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 873 90000012 TUBE REPLACED PER SL 900-016. CORRECTION OF ENGINE OIL LEAK. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997021300267 19970213 00267 NM 1997 2 13 97ZZZX674 1 19960525 A 7110 900F3611805101 LATCH DOUG MD900 MD900 3027375 NM COWLING WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 591 90000012 HIGH PROFILE COWL LATCH WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 3 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997021300268 19970213 00268 NM 1997 2 13 97ZZZX675 1 19960926 A 6210 900R3100001101 RETAIN NUT DOUG MD900 MD900 3027375 NM BLADE GROOVED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 48 0098840367 90000012 BLADE RETAIN BOLT UNIT EXCESSIVELY GROOVED. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997021300275 19970213 00275 WP 1997 2 13 CALA9700163 1 19961018 A 5320 CLIP DOUG DC10 DC1030 3023501 WP BS 1501 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37077 46981 INSPECTION FOUND CLIP FROM RT WHEEL WELL PRESSURE PANEL TO FRAME CORRODED ON UPPER FORWARD FACE OF FLANGE AT STA 1501, S IX INCHES BELOW CABIN FLOOR. A NEW CLIP WAS FABRICATED AND INSTALLED IAW SRM 51-21-01, 51-31-01, 53-00-01, FIGURE 1 AND 53-14-01, FIGURE 11. 2 L 7 3 4F A22WE 1997021300415 19970213 00415 NM 1997 2 13 UPS97221984 1 19961227 A 5311 69154054 FRAME BOEING 727 727185C 138406N NM BS 1342 RUSTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE: C B.S. 1342 RT HD FRAME CHORD RBL 20 P/N 69-15405 IS SEVERELY RUSTED. REMOVED AND REPLACED CHORD IAW UPS E.O. B727-5530-4601-B. 2 L 7 3 4F A3WE 1997021300417 19970213 00417 NM 1997 2 13 UPS97221986 1 19961227 A 5311 65175086 FRAME BOEING 727 727185C 138406N NM BS 1342 RUSTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE: C. B.S. 1342 RT HD LOWER FRAME CHORD RBL 24 P/N 65-17508-6 IS SEVERELY RUSTED. REMOVED AND REPLACED LOWER FRAME CHORD IAW UPS EO B727-5530-4601-B. 2 L 7 3 4F A3WE 1997021300418 19970213 00418 NM 1997 2 13 UPS97221987 1 19961227 A 5320 65195322 CHORD BOEING 727 727185C 138406N NM BS 1342 RUSTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE: C. B/S 1342 RT HD OUTBOARD CHORD RBL 30 WL 250 P/N 19532-2 IS SEVERELY RUSTED. REMOVED AND REPLACED O UTBOARD CHORD IAW UPS EO B727-5530-4601-B. 2 L 7 3 4F A3WE 1997021300419 19970213 00419 NM 1997 2 13 UPS97221988 1 19961231 A 5320 651250678 SHEAR TIE BOEING 727 727185C 138406N NM BS 1303 MIS LOCATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE: C. SHEAR TIE BS 1303 BETWEEN STRS 13R AND 14R HAS FASTENER HOLES WITH IMPROPER PITCH AND SHORTED. RE MOVED SHEAR TIE, FABRICATED AND INSTALLED PER SRM 53-10-2, 51-10-1, AND 51-10-2. 2 L 7 3 4F A3WE 1997021300502 19970213 00502 EU 1997 2 13 CA960916006 1 19960815 A 2750 14116 U-JOINT FOKKER 14116 FOKKER F28 F28MK1000 4990808 EU LT FLAP DRIVE WORN W K NONE O OTHER IN INSP/MAINT 1 CA 37778 (CAN) WEAR ON FLAP DRIVESHAFT U-JOINT, L/H SIDE OF THE FEEDBACK ASSEMBLY WHICH GOES INTO THE L/H WHEELBAY. REPLACED. 2 L 7 2 4F RT A20EU 1997021300503 19970213 00503 SW 1997 2 13 CA960916007 1 19960909 A 6210 3115 SKIN BELL 212015501115 BELL 205 205A1 1181414 SW LYC T53 T5313B 41549 NE M/R BLADE DEBONDED W K NONE O OTHER IN INSP/MAINT 1 CA 3115 LE18135A (CAN) MAIN ROTOR BLADE UPPER AND LOWER SKINS DEBONDED FROM TRAILING EDGE EXTRUSION FOR 66 INCHES FROM THE TIP INBOARD 1 G 7 1 4U 4 U H1SW E17EA 1997021300504 19970213 00504 SW 1997 2 13 CA960916009 1 19960812 A 5751 1041 BALANCE WEIGHT SWRNGN 2734000002 SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP RIGHT HAND AIL LOOSE W A K NONE O OTHER IN INSP/MAINT 1 CA 24213 1041 P54143 (CAN) DURING DAILY INSPECTION THE RIGHT HAND AILERON BALANCE WEIGHT WAS FOUND LOOSE, BENT AND HANGING BY THE OUTBOARD BO LTWEIGHT HAD BEEN LOOSE FOR SOME TIME TWO HOLES HAD BEEN SWAGED COMPLETELY THROUGH AND THE LAST HOLE WAS 1/2 WAY THROUG H. WEIGHT WAS BENT AT CENTRE AND APPEARS TO HAVE JAMMED THE CONTROL AT SOME TIME PREVIOUS. ALL THREE HOLES OXIDIZED IN O RIGINAL AREAS OF CONTACT. ALL OTHER FLEET AIRCRAFT CHECKED AND FOUND OK. 2 L 7 2 4T 4 T RT A8SW E4WE 1997021300507 19970213 00507 EU 1997 2 13 CA960916012 1 19960905 A 3246 LM1148484629 BEARING BRAERO 748 HS7482B 1500248 EU LH MLG FAILED W K NONE O OTHER LD LANDING 1 CA (CAN) ON ROLL OUT AIRCRAFT WAS PULLING TO THE LEFT AND DIFFICULT TO STEER. LH OUTER WHEEL BEARING HAD DISINTEGRATED CAUS ING INNER RACE TO SEIZE TO SPACER AND AXLE. REPLACED. 2 L 7 2 3T A24EU 1997021300508 19970213 00508 EU 1997 2 13 CA960916013 1 19960907 A 2612 D890N FIRE WIRE BRAERO 748 HS7482B 1500248 EU NR 1 ENGINE SHORTED W E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. J WARNING INDICATION DE DESCENT 1 CA (CAN) ON DESCENT FIRE INDICATION ON #1 ENGINE BOTTLES DISCHARGED AND ENGINE SHUT DOWN. INTERNALLY SHORTED FIRE WIRE. BOT TLES AND WIRE REPLACED. 2 L 7 2 3T A24EU 1997021300509 19970213 00509 NM 1997 2 13 CA960916014 1 19960831 A 2750 5906989102 CASING ASSEMBLY SUNDSTRAND 745581A DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE TE FLAP CONTROL BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA E0063 120323 (CAN) ON REMOVAL OF FLEX SHAFT COUPLING FOR INSPECTION, THE ALUMINUM END FITTING CAME OUT OF THE CASING ASSEMBLY OF THE RIGHT HAND INBOARD FLEX SHAFT ASSEMBLY. 2 H 7 2 4T 4 T RT A13NM E20NE 1997021300510 19970213 00510 CE 1997 2 13 CA960916017 1 19960814 A 2797 WIRE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE PITCH TRIM LIGHT MISSING W K NONE P W NO WARNING INDICATION INADEQUATE Q C IN INSP/MAINT 1 CA PCE114459 (CAN) THE PITCH TRIM CAUTION LIGHT WAS REPORTED NOT WORKING. INSPECTION FOUND A WIRE MISSING. 2 L 7 2 4T 4 T RT A24CE E26NE 1997021300515 19970213 00515 SW 1997 2 13 CA960919001 1 19960801 A 6320 20604000225 TRANSMISSION BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL M/R GR BOX BROKEN PIN W K NONE O OTHER IN INSP/MAINT 1 CA 11920 CAE832639 (CAN) CHECK OF THE MAST MOVEMENT ON THE GROUND WAS EXCESSIVE AS IF THE ISOLATION MOUNT WAS NOT WORKING. A CLOSER INSPECT ION SHOWED THE PIN ASSEMBLY TO BE BROKEN. 1 G 7 1 3U 3 U H2SW E4CE 1997021300516 19970213 00516 NM 1997 2 13 CA960919002 1 19960910 A 2910 651784417 LINE BOEING 727 727227 1384078 NM PWA JT8 JT8D9A 52048 NE A HYD SYS LEAKS W A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 CA 666282 (CAN) "A" SYSTEM HYDRAULIC FLUID LOSS AIRCRAFT RETURNED, LEAK AT AFT STAIRWELL AREA RH SIDE, #2 HYDRAULIC PUMP PRESSURE LINE WAS TEMPORARY FIX, REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 1997021300517 19970213 00517 CE 1997 2 13 CA960919003 1 19960910 A 3244 1690 TIRE PARKERHANFIN 40135 CESSNA 402 402B 207590P CE MCAULY 3AF32C 3AF32C87 GL RIGHT MAIN GEAR BLOWN W O OTHER O OTHER LD LANDING 1 CA 1690 861168 (CAN) ON LANDING THE RIGHT HAND MAIN TIRE BLEW. CAUSE OF THE BLOWN TIRE COULD NOT BE DETERMINED NEW WHEEL INSTALLED AN D THE AIRCRAFT RETURNED TO SERVICE 1 L 7 2 3O A7CE 5 C P22EA 1997021300518 19970213 00518 NM 1997 2 13 CA960919004 1 19960828 A 7933 PROBE BOEING 727 727227 1384078 NM PWA JT8 JT8D9A 52048 NE NR 2 ENG OIL TEM BROKEN WIRE W A E UNSCHED LANDING ENGINE SHUTDOWN J M WARNING INDICATION OVER TEMP CL CLIMB 1 CA 666295 (CAN) #2 ENGINE SHUT DOWN IN CLIMB DUE TO OIL TEMPERATURE AT ALLOWABLE MAXIMUM. BROKEN GROUND WIRE AT PROBE. 2 L 7 3 4F 4 F A3WE E2EA 1997021300519 19970213 00519 SW 1997 2 13 CA960919005 1 19960907 A 2740 C0402 CONNECTOR SWRNGN DL5040M5 SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP PITCH TRIM FAULTY W O OTHER L NO TEST CR CRUISE 1 CA 20 C0402 P54183 (CAN) CREW REPORTED THAT THE PITCH TRIM ACTUATOR WAS FAULTY AS THE CAPTAINS PITCH TRIM COULD BE ACTIVATED USING ONLY ONE SWITCH SWITCH IS A SPLIT SWITCH THAT NORMALLY REQUIRES BOTH SWITCHES TO BE ACTIVATED TO OPERATE PITCH TRIM. SUBSEQUENT INVESTIGATION FOUND LEFT ACTUATOR CANNON CONNECTOR WITH SHORTED PIN TO CASE. 2 L 7 2 4T 4 T RT A8SW E4WE 1997021300520 19970213 00520 EA 1997 2 13 CA960919007 2 19960908 A 8530 CYLINDER PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA #2 CYLINDER SEPARATED W O OTHER O R OTHER PARTIAL RPM/PWR LOSS CL CLIMB 1 CA 461 L171568A (CAN) PILOT REPORTED LOSS OF POWER ON TAKEOFF ON #2 ENGINE. POST FLIGHT INSPECTION FOUND #2 CYLINDER HAD SEPARATED AT TH E HEAD. THE #2 CYLINDER WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 3O 3 O A20SO E14EA 1997021300521 19970213 00521 NM 1997 2 13 CA960919009 1 19960910 A 3213 DCL24887 SHOCK STRUT ROTOL 10100117 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE TORQUE LINK DAMAGED W K NONE J WARNING INDICATION LD LANDING 1 CA 17999 DCL24887 120584 (CAN) AFTER AIRCRAFT LANDED THE MAIN LANDING GEAR TORQUE LINKS FOLDED IN TOWARD THE OLEO INSTEAD OF AWAY FROM THE OLEO. THIS CAUSED THE WEIGHT ON THE WHEELS, LACK OF BRAKING AND NOSEWHEEL STEERING. THE CAUSE OF TORQUE LINKS SCISSORING THE WRONG WAY IN THE SHOCK STRUT IS INTERNAL TO THE STRUT. 2 H 7 2 4T 4 T RT A13NM E20NE 1997021300522 19970213 00522 EU 1997 2 13 CA960919012 1 19960818 A 5210 14152016429 DOOR BRAERO BAG JETSTM JETSTM4112 EU GARRTT TPE331 TPE33114 01514 NE AIRSTAIR MALFUNCTION W K NONE O OTHER IN INSP/MAINT 1 CA 3593 3593 WIPLSD0056 P75067 (CAN) AIRSTAIR DOOR DIFFICULT TO OPEN AND CLOSE. WOULD NOT OPEN WITH EXTERNAL HANDLE. DOOR REPLACED. 1 L 7 2 4T 4 T RT A196 E18NE 1997021300523 19970213 00523 WP 1997 2 13 CA960923005 1 19960905 A 2910 22305668 CHECK VALVE DOUG DC4 C54A 3021512 WP PWA R2000 R20007M2 52023 NE NR 3 ENG NAC DISCONNECTED W O OTHER G K MULTIPLE FAILURE FLUID LOSS DE DESCENT 1 CA P107846 (CAN) LOSS OF MAIN HYDRAULIC FLUID DURING FLIGHT DUE TO GROUND HYDRAULIC TEST CONNECTION (P/N 230566-8) COMING LOOSE AND SEPARATING FROM ADAPTER FITTING (P/N 22336699) THAT IS ATTACHED TO PIPE ASSEMBLY (P/N 5321900-26) HYDRAULIC PRESSURE LI NE IN #3 ENGINE NACELLE. SUSPECT CAUSE ATTRIBUTED TO DETERIORATION OF THE "O" RING RESULTING IN THE LOSS OF TORQUE FRICT ION ALLOWING THE CHECK VALVE TO WORK LOOSE UNDER VIBRATING CONDITIONS. 2 L 7 4 4R 4 R A762 5E5 1997021300524 19970213 00524 EU 1997 2 13 CA960923006 1 19960910 A 2170 DUCT FOKKER F28 F28MK1000 4990808 EU WATER SEPARATOR BLOWN W C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CA (CAN) WHEN TAKEOFF POWER APPLIED A LOUD POP AND THE RUSH OF AIR WAS HEARD. TAKEOFF WAS REJECTED. DUCT WAS BLOWN OFF WATE R SEPARATOR TO THE #1 PACK. REPAIRED. 2 L 7 2 4F RT A20EU 1997021300525 19970213 00525 NE 1997 2 13 CA960923011 2 19960916 A 7311 447883 CONNECTOR BOEING 727 727212 138407G NM PWA JT8 JT8D7B 52053 NE FUEL OIL COOLER CRACKED W K NONE O X OTHER ENGINE FLAMEOUT AP APPROACH 1 CA 654890 (CAN) ON APPROACH #2 ENGINE FLAMED OUT. DURING CRUISE PORTION OF THE FLIGHT AN INITIAL 15 PERCENT DROP IN EPR WAS OBSERV ED, NO OTHER ENGINE PARAMETERS WERE AFFECTED. THE DROP IN RPM INCREASED TO APPROXIMATELY 50 PERCENT PRIOR TO FLAME OUT. POST FLIGHT INSPECTION DETERMINDED THE OIL COOLER FUEL INLET TUBE CONNECTOR HAD CRACKED AND ALLOWED THE ENGINE FUEL SUPP LY TO BE INTERRUPTED CAUSING THE ENGINE TO FLAME OUT. THE CONNECTOR WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 1997021300527 19970213 00527 EU 1997 2 13 CA960923013 1 19960918 A 6410 355A12004008 BLADE SNIAS 350 AS350B2 8680813 EU T/R DEBONDED W K NONE O OTHER IN INSP/MAINT 1 CA 1899 (CAN) DURING PILOT DI AN ABNORMAL NOISE WAS HEARD WHILE FLEXING T/R BLADE. INSPECTION OF BLADE FOUND DEBONDING BETWEEN S EAL JUNCTION AND BLADE CUFF. DEPTH OF DEBONDING WAS BETWEEN 28.58 MM TO 31.76 MM. 1 G 7 1 3U H9EU 1997021300528 19970213 00528 EA 1997 2 13 CA960923014 2 19960912 A 7414 S6LN204 MAGNETO BENDIX PIPER PA23 PA23250 7102308 SO LYC O540 IO540C4B5 41532 EA #1 ENGINE FAULTY W K NONE O OTHER IN INSP/MAINT 1 CA 1047 898693 L1337648 (CAN) ON INSPECTION THE MAGNETO DISTRIBUTOR TEETH WERE FOUND MISSING. 1 L 7 2 3O 3 O 1A10 1E4 1997021300529 19970213 00529 EU 1997 2 13 CA960923015 1 19960916 A 2916 19702398 RESERVOIR BRAERO 748 HS7482A 4231001 EU HYD SYS CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) 1 INCH CRACK FOUND IN RESERVOIR DURING INVESTIGATION OF A REPORTED HYDRAULIC LEAK. REPLACED. 2 L 7 2 3T A24EU 1997021300530 19970213 00530 NM 1997 2 13 CA960923016 1 19960916 A 2782 1439 SEAL DECOTO 269002913 BOEING 727 72744C 1384100 NM PWA JT8 JT8D7B 52053 NE NR 6 LE SLAT WORN W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 11592 1439 655457 (CAN) DURING WALKAROUND OBSERVED SEAPAGE AT #6 LEADING EDGE SLAT, BEYOND LIMITS ACTUATOR REPLACED 2 L 7 3 4F 4 F A3WE E2EA 1997021300531 19970213 00531 1997 2 13 CA960923018 4 19960828 A 2350 A930 RESISTOR BENDIX M151A CVAC 440 440 2422902 WP COCKPIT SPEAKER SHORTED W A A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 CA A930 (CAN) AFTER TAKEOFF, A WISP OF SMOKE AND A BURNING SMELL WAS DETECTED IN THE COCKPIT BY THE CREW. PRECAUTIONARY LANDING WAS CARRIED OUT SUBSEQUENT MAINTENANCE TROUBLE SHOOTING REVEALED THE PROBLEM WAS LOCATED IN THE RIGHT HAND SPEAKER AND WAS DUE TO A PARTIALLY SHORTED TRANSFORMER OVERLOADING A RESISTOR. 2 L 7 2 4R 6A6 1997021300532 19970213 00532 1997 2 13 CA960923019 4 19960913 A 3418 P004 STALL WARN SYS DIAMON DIAMON DA20A1 DA20A1 05626UX GL TUBE LOW POINT CONTAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) WATER FOUND IN THE STALL WARNING TUBING WHERE IT REACHES ITS LOWEST POINT UNDER THE PILOTS SEAT. THE AMOUNT OF WAT ER FOUND WAS BLOCKING THE TUBING. SUBMITTER STATES THAT THERE IS NO WAY OF VISUALLY INSPECTING THIS AREA DURING A PRE-FL IGHT (D.I.) AND BELIEVES IT WOULD AFFECT THE STALL WARNING SYSTEM. REFERENCE SDR 960923020. 1 L 7 1 3O NT TA4CH 1997021300533 19970213 00533 1997 2 13 CA960923020 4 19960913 A 3418 S004 STALL WARN SYS DIAMON DIAMON DA20A1 DA20A1 05626UX GL TUBE LOW POINT CONTAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) STALL WARNING SYSTEM, WATER FOUND IN THE TUBING WHERE THE TUBING IS AT ITS LOWEST POINT UNDER THE PILOTS SEAT. THE AMOUNT OF WATER FOUND WAS BLOCKING THE TUBING. SUBMITTER STATES THAT THERE IS NO WAY TO VISUALLY INSPECT THIS AREA DURI NG A PRE-FLIGHT (D.I.) AND BELIEVES IT WOULD AFFECT THE STALL WARNING SYSTEM. REFERENCE SDR 96092319. 1 L 7 1 3O NT TA4CH 1997021300534 19970213 00534 NM 1997 2 13 CA960923022 1 19960825 A 2932 7G772 SWITCH DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE #1 HYDRAULIC LEAKING W K NONE K FLUID LOSS AP APPROACH 1 CA 120323 (CAN) ON APPROACH #1 HYDRAULIC QUANTITY DROPPING. INSPECTION FOUND HYDRAULIC QUANTITY PRESSURE SWITCH HAD A SMALL HOLE O N ITS SIDE AND IT WAS LEAKING. 2 H 7 2 4T 4 T RT A13NM E20NE 1997021300535 19970213 00535 NM 1997 2 13 CA960923024 1 19960911 A 3610 12355814 CLAMP BOEING 727 7272J4 1384006 NM PWA JT8 JT8D17 52049 NE 8TH STG CK VALVE LOOSE W A J UNSCHED LANDING DUMP FUEL J M WARNING INDICATION OVER TEMP TO TAKEOFF 1 CA 700814 (CAN) DURING TAKEOFF #3 ENGINE FIRE WARNING CAME ON, FUEL DUMPED. INVESTIGATION REVEALED DUCT SEPARATED UP STREAM OF #8 STAGE CHECK VALVE. CLAMPS AND VALVE REPLACED. 2 L 7 3 4F 4 F RT A3WE E2EA 1997021300538 19970213 00538 NM 1997 2 13 CA960924003 1 19960912 A 3241 82970010415 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE ANTI SKID CRACKED W O OTHER K FLUID LOSS AP APPROACH 1 CA 120056 (CAN) ON LET DOWN #2 HYDRAULIC SYSTEM LOST FLUID. ON LANDING ROLL AT 60 KTS BRAKE PEDALS WENT TO THE FLOOR DUE TO FLUID LOSS. BOTH QUANTITY GAUGES SHOWED EMPTY. LINE FROM ANTI-SKID VALVE TO QLV ON #1 SYSTEM FOUND CRACKED. #2 SYSTEM GROUND S POILER BLANKING CAP FITTING FOUND LOOSE AND O-RING DAMAGED. 2 H 7 2 4T 4 T RT A13NM E20NE 1997021300539 19970213 00539 1997 2 13 CA960924004 4 19960920 A 3422 83423051003 CONTROLLER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE COCKPIT DG BURNED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA 120056 (CAN) BURNT ELECTRICAL SMELL IN COCKPIT. STANDBY DIRECTIONAL GYRO CONTROL FOUND TO BE SOURCE OF SMELL. 2 H 7 2 4T 4 T RT A13NM E20NE 1997021300540 19970213 00540 NM 1997 2 13 CA960924005 1 19960912 A 3230 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NOSE GEAR CRACKED W K NONE B K SMOKE/FUMES/ODORS/SPARKS FLUID LOSS LD LANDING 1 CA 120832 (CAN) BURNING ACIDIC SMELL IN COCKPIT ON TAKEOFF AND RIGHT AFTER SHUTDOWN. VISIBLE SMOKE IN THE COCKPIT AFTER SHUTDOWN. SMOKE CONFIRMED TO BE SKYDROL MIST. NOSE GEAR DOWN LINE FOUND CRACKED 5 INCHES FORWARD OF COCKPIT BULKHEAD. 2 H 7 2 4T 4 T RT A13NM E20NE 1997021300541 19970213 00541 NM 1997 2 13 CA960924006 1 19960912 A 2910 82950010137 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE #1 NACELLE CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 120305 (CAN) HYDRAULIC LINE AFT AREA OF #1 NACELLE FOUND CRACKED. 2 H 7 2 4T 4 T RT A13NM E20NE 1997021300542 19970213 00542 NM 1997 2 13 CA960924007 1 19960918 A 8010 AJA4N176 RELAY DHAV DHC8 DHC8301 NM PWA 120 PW120A NE STARTER FAILED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA 121164 (CAN) #1 STARTER DID NOT CUT OUT ON STARTUP. STARTER WAS SMOKING. ENGINE SHUT DOWN AND FIRE BOTTLES FIRED. RELAY 2431-K1 AT FAULT. 2 H 7 2 4T 4 T RT A13NM E20NE 1997021300543 19970213 00543 EA 1997 2 13 CA960924008 1 19960912 A 3231 82910010175 LINE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE NOSE GEAR DOOR CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 123151 (CAN) NOSE GEAR DOOR CLOSE LINE FOUND LEAKING. 2 H 7 2 4T 4 T RT A13NM E20NE 1997021300544 19970213 00544 NM 1997 2 13 CA960924010 1 19960911 A 2910 BACH8B04NN02 LINE BOEING BACH8B04NN02 BOEING 737 737275 1384485 NM PWA JT8 JT8D17 52049 NE NLG ACTUATOR SPLIT W A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS TO TAKEOFF 1 CA 702661 (CAN) NOSE GEAR UNSAFE LIGHT ON WITH GEAR SELECTED UP. HYDRAULIC LINE TO UPLOCK ACTUATOR SPLIT, REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1997021300545 19970213 00545 1997 2 13 CA960924011 4 19960911 A 3442 20709620102 INDICATOR 20709620102 BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE COCKPIT RADAR NO PICTURE W A UNSCHED LANDING L NO TEST CL CLIMB 1 CA 1830 707313 (CAN) AIRCRAT HAD NO PICTURE ON WEATHER PPI. REPLACED PPI AND TRANSCEIVER. PPI REPLACED SECOND TIME. 2 L 7 2 4F 4 F A16WE E2EA 1997021300546 19970213 00546 NM 1997 2 13 CA960924012 1 19960911 A 2740 2588810901 COMPUTER HONEYWELL 2588810901 BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE STAB TRIM INTERMITTENT W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 1040665 708827 (CAN) ABORTED TAKEOFF ROLL AT 70 KTS DUE STAB OUT OF TRIM LGIHT ON. PITCH CHANNEL COMPUTER REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1997021300554 19970213 00554 1997 2 13 97ZZZM193 4 19961225 A 3421 258733513 VERT GYRO DOUG DC9 DC931 3022065 WP NR 2 MALFUNCTIONED A GTIA O OTHER O OTHER CL CLIMB 1 GL 23 969ML 47268 FLT 1421 - DTW - DURING CLIMB CONFIGURATION WITH THE AUTO PILOT ENGAGED EXPERIENCED A VIOLENT PITCH DOWN CONDITION, AUTO PILOT DISENGAGED. REMOVED AND REPLACED NR 2 VERTICAL GYRO. SYSTEM OP CHECK GOOD ON GROUND IAW DC-9 MM 34-27-0 AND 22- 10-0. (M) 2 L 7 2 4F A6WE 1997021300558 19970213 00558 NM 1997 2 13 97ZZZM194 1 19961221 A 5240 HANDLE BOEING 737 7372P6 NM SERVICE DOOR OUT OF ADJUST A ZZDA O OTHER J WARNING INDICATION DE DESCENT 1 SO 15 1PC 21613 DESCENDING THROUGH 23,000 FEET 'AFT SERVICE' DOOR LIGHT ILLUMINATED. FLIGHT ATTENDANT MOVED DOOR HANDLE, LIGHT WENT OUT . FLIGHT ATTENDANT REPORTED APPROXIMATELY 2 INCH PLAY IN HANDLE. NO EMERGENCY PROCEDURES WERE NECESSARY. MAINTENANCE ACCOMPLISHED ADJUSTMENT FOR 'SOFT UNLATCHING' IAW B737 MM 52-41-0. REQUIRED INSPECTION ITEM COMPLIED WITH. NO AD'S, SB 'S, STC'S OR PMA'S APPLICABLE AT THIS TIME. (M) 2 L 7 2 4F RT A16WE 1997021300561 19970213 00561 NM 1997 2 13 97ZZZM197 1 19961219 A 5530 BEAM BOEING 737 7372L9 1384497 NM VERT STAB CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT 21278 FOUND CORROSION ON TRAILING EDGE BEAM ON VERTICAL FIN 4H SIDE ATT FIN STATION 127.10 RUD STATION 60.15 (MARKED). REPAIR ED TRAILING EDGE BEAM PER TRAMCO EWO 96-09-29. (M) 2 L 7 2 4F RT A16WE 1997021300562 19970213 00562 NM 1997 2 13 97ZZZM198 1 19961211 A 2425 693731543 PANEL BOEING 737 737214 138446R NM NR 1 ENG CSD MALFUNCTIONED A ZZDA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 SO 15 460AT 20158 FLT 570 - MCO-ROC - NR 1 CSD LOW OIL PRESS LIGHT INTERMITTENT AND DRIVE TEMP FLUCTUATES INTO THE CAUTION RANGE, DISCONNE CTED THE CSD. REPLACED P-5 CONTROL PANEL AS WELL AS NR 1 CSD OIL IN TEMP BULB IAW WITH B737 MM 24-11-0. OPERATIONAL CH ECK ACCOMPLISHED SATISFACTORILY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1997021300576 19970213 00576 EU 1997 2 13 97ZZZM201 1 19961206 A 3244 301408870 TIRE GOODYEAR BRAERO DH125 HS125700A 4230170 EU RT MLG FAILED A KKYA A UNSCHED LANDING O OTHER TO TAKEOFF 1 NE 03 270KA 5363 NA0307 ON TAKEOFF, NR 3 MAIN GEAR TIRE FAILED. PROCEEDED TO ALTERNATE, AIRPORT WITH LONGER RUNWAY AND BETTER EQUIPMENT, AND TO BURN FUEL TO REDUCE WEIGHT. UPON LANDING TIRE CAME APART CAUSING DAMAGE TO RT FLAP. MAIN GEAR LEG ALSO SUSTAINED DAMA GE FROM WHEEL/AXEL VIBRATION. CAUSE OF TIRE FAILURE IS UNKNOWN AND IS UNDER INVESTIGATION. (M) 2 L 7 2 4F A3EU 1997021300577 19970213 00577 SO 1997 2 13 97ZZZM202 1 19961224 A 3230 1159LM203081 STRIKER ARM GULSTM G1159 G1159A 3970109 SO LT MLG CRACKED A KKYA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NE 03 165G 5350 414 THE A/C DEPARTED SFA EN ROUTE TO LGA, WHEN THE LANDING GEAR WAS SELECTED UP THE LEFT MLG DID NOT RETRACT. THE A/C RETUR NED TO SFA AND LANDED WITHOUT INCIDENT. AN EXAMINATION OF THE AFT TIMING VALVE REVEALED A SMALL CRACK IN THE STRIKER AR M, THIS ALLOWED THE LEFT MLG DOOR AFT TIMING VALVE TO GO OUT OF RIG. THE AIRCRAFT WAS FERRIED WITH THE GEAR DOWN TO A B ASE WHERE THE ARM WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. THE CRACK STARTED IN A HOLE DRILLED FOR SAFTY WIRE. THE CRACK IS ONLY .25 INCH LONG AND IS DIFFICULT TO SEE. (M) 2 L 7 2 4F A12EA 1997021300582 19970213 00582 NE 1997 2 13 EIAA9698 2 19961216 A 7200 ENGINE BOEING 747 747212B 1384886 NM PWA JT9 JT9D70 52054 NE NR 2 SURGED A A EIAA E ENGINE SHUTDOWN O OTHER CL CLIMB 1 NM 09 482EV 42058 20713 662354 AFTER TAKEOFF, WHEN POWER WAS REDUCED FOR CRUISE SETTING, NR 2 ENGINE SURGED WITH INCREASING EGT ENGINE WAS SHUT DOWN AN D RESTARTED WITH ABNORMALLY HIGH EGT (720) FOR IDLE THRUST POWER SETTING AT FL 350. WITH ENGINE RESTARTED N2 AT IDLE WA S 50 PERCENT. NO LIMITATIONS EXCEEDED. ENGINE WAS SHUTDOWN AGAIN FOR HIGH EGT. PERFORMED ENGINE WINDMILLING CHECK, IN SPECTION OF ALL VISIBLE VANES, BLEED AND FUEL CONTROL UNIT PLUMBING WITH NO DEFECTS EVIDENT. FULE PUMP PRESSURE CHECKED AT 600 PSI. ENGINE IDLE RUN CARRIED OUT AND ALL PARAMETERS WITHIN LIMITS. SUBSEQUENT FLT WAS NORMAL. (M) 2 L 7 4 4F 4 F A20WE E3NE 1997021300583 19970213 00583 WP 1997 2 13 EIAA9699 1 19961216 A 5720 WING TIP DOUG DC9 DC933F 302207A WP LEFT GOUGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 50151 47191 SEA - WHILE A/C WAS TAXIING IN TO PARKING POSITION THE TOP OF THE LEFT WING TIP MADE CONTACT WITH A 'K' LOADER THAT WAS PARKED TO SERVICE AIRCRAFT. RESULTANT DAMAGE WAS TWO GOUGES TO THE TOP OF THE LEFT WING TIP, 3.75 ICNH AND 12.5 INCH LO NG AND 3-4 INCHES WIDE, .5 INCH TO .75 INCH DEEP. REPLACED LEFT WING TIP PER ECRA 933-57-035-1 AND MAINTENANCE MANUAL. (M) 2 L 7 2 4F A6WE 1997021300584 19970213 00584 NM 1997 2 13 97ZZZM204 1 19961114 A 5313 STRINGER BOEING 737 7372P6 NM BS 787 CRACKED A A6XA K NONE O OTHER IN INSP/MAINT 1 SO 13 EICKW 21677 FOUND 5 INCH FATIGUE CRACK AT STATION 787 STRINGER ISL. REPAIR COMPLETED BY INSTALLING A DOUBLER PER STRUCTURAL REPAIR MANUAL 53-30-3 FIGURE 6. (M) 2 L 7 2 4F RT A16WE 1997021300585 19970213 00585 NM 1997 2 13 97ZZZM205 1 19961121 A 2621 FIRE BOTTLE BOEING 737 7372P6 NM APU COMPT DISCHARGED A A6XA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SO 13 EICKL 21356 WHILE ATTEMPTING START AT 33,000 FEET, APU FIRE WARNING INDICATION, BOTTLE DISCHARGED. MADE VISUAL INSPECTION OF APU FO R EVIDENCE OF FIRE, NONE NOTED. REPLACED APU FIRE BOTTLE AND SQUIB. MADE OPERATIONAL TEST OF APU AND FIRE WARNING SYST EM, ALL CHECKED OK. (M) 2 L 7 2 4F RT A16WE 1997021300590 19970213 00590 NM 1997 2 13 97ZZZM208 1 19961128 A 2910 65445534 HYDRAULIC LINE BOEING 737 7372L9 1384497 NM LT LE FLAP ACT PIN HOLE A ZZDA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 15 465AT 21528 FLT 532 - MCO-SWF - A/C 485 RETURNED TO MCD DUE TO A TOTAL LOSS OF HYDRAULIC FLUID IN 'A' SYSTEM. AFTER LANDING AT MCO THE A/C HAD NO NOSE WHEEL STEERING. THE A/C HAD TO BE TOWED FROM RUNWAY TO THE GATE AREA. PASSENGERS WERE TRANSFERRED TO A/C 737Q TO COMPLETE FLT. 2 L 7 2 4F RT A16WE 1997021300610 19970213 00610 EU 1997 2 13 USAA970023 1 19960120 A 5312 BULKHEAD FOKKER F28 F28MK0100 4990807 EU BS 64 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 863US 15724 11303 PIT - DURING Q-1 CHECK, FOUND 3 INCH CRACK (RT SIDE) OF CENTER FUEL TANK PRESSURE BULKHEAD AT FRAME 14911 AND STATION 64 . STOP DRILLED AND CUT OUT CRACKED AREA. INSTALLED FILLER AND NEW ANGLES PER EA NR 34272. (M) 2 L 7 2 4F RT 1997021300611 19970213 00611 EU 1997 2 13 USAA970022 1 19960120 A 5320 D28858005 BEAM FOKKER F28 F28MK0100 4990807 EU BS 11333-12791 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 863US 11303 PIT - DURING Q-1 CHECK, FOUND 2 INCH BY 2 INCH AREA OF CORROSION (.068 INCH DEEP) IN MID CARGO DOOR LATCH BEAM TOP SURFA CE BETWEEN STATION 11333-12791, STATION 72. CUT OUT CORRODED AREA AND INSTALLED A BATH TUP REPAIR FITTING PER EA NR 460 74. CORROSION LEVEL 1. (M) 2 L 7 2 4F RT 1997021300612 19970213 00612 EU 1997 2 13 USAA970025 1 19960120 A 5330 SKIN FOKKER F28 F28MK0100 4990807 EU FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 863US 15724 11303 PIT - DURING Q-1 CHECK, FOUND 18 INCH BY 24 INCH AREA OF DISBONDED AND HEAT DAMAGED SKIN AT LT STUBWING FUSELAGE SKIN BE TWEEN FRAMES 24011 AND 24611 AND BETWEEN STRINGER 21A AND UPPER CONTACT ANGLE. CUT OUT DAMAGED AREA OF SKIN AND INSTALL ED AN EXTERNAL DOUBLER PER EA NR 29374A. (M) 2 L 7 2 4F RT 1997021300613 19970213 00613 EU 1997 2 13 USAA970024 1 19960120 A 5312 BULKHEAD FOKKER F28 F28MK0100 4990807 EU BS 11 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 863US 15724 11303 PIT - DURING Q-1 CHECK, FOUND TWO .5 INCH CRACK (LT SIDE) OF CENTER FUEL TANK PRESSURE BULKHEAD AT FRAME 14911 AND STATI ON 11. STOP DRILLED AND CUT OUT CRACKED AREA. INSTALLED FILLER AND NEW ANGLES PER EA NR 34272. (M) 2 L 7 2 4F RT 1997021300614 19970213 00614 EU 1997 2 13 USAA970026 1 19960120 A 5330 SKIN FOKKER F28 F28MK0100 4990807 EU FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 863US 15724 11303 PIT - DURING Q-1 CHECK, FOUND 18 INCH BY 20 INCH AREA OF DISBONDED AND HEAT DAMAGED SKIN AT RT STUBWING FUSELAGE SKIN BE TWEEN FRAMES 24011 AND 24611 AND BETWEEN STRINGER 21A AND UPPER CONTACT ANGLE. CUT OUT DAMAGED AREA OF SKIN AND INSTALL ED AN EXTERNAL DOUBLER PER EA NR 29374A. (M) 2 L 7 2 4F RT 1997021300625 19970213 00625 NM 1997 2 13 TWRA9704 1 19961211 A 3530 5500CIABF20B OXYGEN BOTTLE BOEING 747 747259B NM CABIN CONTAMINATED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 EICEO 937401 21730 DURING 'C' SERVICE, FOUND PORTABLE OXYGEN BOTTLE, S/N 937401 4/R POSITION CONTAMINATED WITH A JELLY LIKE SUBSTANCE AND W ATER CONTAMINATION. REPLACED PORTABLE OXYGEN BOTTLE ON 4/R POSITION. (M) 2 L 7 4 4F RT A20WE 1997021300628 19970213 00628 NE 1997 2 13 N3VR96157 2 19961202 A 7230 537131 IGV CASE BOEING 727 727231 1384079 NM PWA JT8 JT8D9 52048 NE ENGINE CRACKED A P9IA K NONE O OTHER IN INSP/MAINT 1 SO 03 590CA 20098 INLET GUIDE VANE CASE WAS CRACKED AT A PREVIOUS WELD REPAIR. THE INLET GUIDE VALVE (I/G/V) CASE WAS REPLACED IAW MM 72- 00 AND THE NR 1 BEARING WAS REPLACED IAW MM 72-00-23. (M) 2 L 7 3 4F 4 F A3WE E2EA 1997021300629 19970213 00629 NM 1997 2 13 N3VR96154 1 19961204 A 5320 65198615 T-CHORD BOEING 727 727231 1384079 NM BS 227/280 CORRODED A P9IA K NONE O OTHER IN INSP/MAINT 1 SO 03 590CA 20098 LEFT NOSE WHEEL WELL T-CHORD CORRODED BEYOND LIMITS. CUT OUT SKIN APPROX 14 INCHES AT STATION 280 LEFT FOR REPLACEMENT OF LT NOSE WHEEL WELL T-CHORD. REPLACED T-CHORD AND SPLICED NEW SKIN IAW DWG 96-0804 DATED AUGUST 19, 1996. REF SRM 51 -10-6, 51-10-2 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1997021300630 19970213 00630 NM 1997 2 13 N3VR96153 1 19961204 A 5510 RETAINER BOEING 727 727231 1384079 NM LT H STAB SEAL CRACKED A P9IA K NONE O OTHER IN INSP/MAINT 1 SO 03 590CA 20098 LEFT HORIZ STABILIZER LOWR T/E SEAL RETAINER HAS SEAL RIVETS LOOSE AND LIGHT SURFACE CORROSION BETWEEN ELEVATOR HINGES N R 3 THROUGH NR 6 POSITION. CRACKS FOUND RUNNING FROM LOOSE RIVET HOLES. BLENDED OUT DAMAGED AREA, REMOVED CORROSION, R ELOCATED FASTENERS IAW EO 96-1031 DATED 10/31/96. REF SRM 51-10-2, 51-30-2 AND 51-10-6. (M) 2 L 7 3 4F A3WE 1997021300631 19970213 00631 NM 1997 2 13 N3VR96152 1 19960913 A 5510 RETAINER BOEING 727 727231 1384079 NM HOR STAB SEAL CORRODED A P9IA K NONE O OTHER IN INSP/MAINT 1 SO 03 590CA 20098 RIGHT HORIZ STAB T/E SEAL RETAINER, SEAL LOOSE AT ELEVATOR HINGES NR 2, NR 5 AND NR 7 POSITIONS, CRACKS FOUND RUNNING FR OM LOOSE RIVET HEADS. BLENDED OUT DAMAGED AREAS, REMOVED CORROSION, RELOCATED FASTENERS IAW EO 96-1031, REF SRM 51-10-2 , 51-30-2 AND 51-10-6. (M) 2 L 7 3 4F A3WE 1997021300635 19970213 00635 NM 1997 2 13 AALA961700 1 19961106 A 5315 141N2932 FLOORBEAM BOEING 757 757223 1384957 NM BS 324 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 668AA 25333 AFW - FOUND FLOOR BEAM AT STATION 324 HAS CORROSION BEYOND SRM LIMITS. ALODINED ALL BLENDED AREAS. FABRICATE STRAPS FR OM .050 301.5 HARD STAINLESS STEEL. APPLY TWO COATS PRIMER TO STRAPS AND BEAM FILL BLEND AREA WITH AMS 5092. INSTALL S TRAP WITH BACB30NN6 HI-LOKS. (M) 2 L 7 2 4F RT A2NM 1997021300636 19970213 00636 NM 1997 2 13 AALA961701 1 19961106 A 5315 FLOORBEAM BOEING 757 757223 1384957 NM BS 365 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 668AA 25333 AFW - FOUND FLOORBEAM AT STATION 365 HAD 2 AREAS OF CORROSION BEYOND SRM LIMITS. ALODINED ALL BLENDED AREAS. FABRICATE STRAPS USING .050 301.5 HARD STAINLESS STEEL. APPLY 2 COATS PRIMER TO STRAPS AND BEAM. FILL ALL BLEND AREAS WITH BMS5 -92. INSTALL STRAPS USING BACBACRN616 HI-LOCKS. (M) 2 L 7 2 4F RT A2NM 1997021300637 19970213 00637 NM 1997 2 13 AALA961881 1 19961219 A 5320 SUPPORT DOUG MD11 MD11 3023602 NM BS 480 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1766A 48597 TUL - FOUND CORRODED FLOOR (GALLEY) SUPPORT, AROUND FASTENERS HOLES AND FORWARD MOUNTING BLOCK. FABRICATED RIGHT NR 3 GALLEY SUPPORT PER SRM 53-00-01 PAGE 1 AND INSTALLED. (M) 2 L 7 3 4F RT A22WE 1997021300638 19970213 00638 NM 1997 2 13 AALA961877 1 19961219 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1321 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1766A 48597 TUL - CORROSION BEYOND LIMITS. SPLICED IN NEW SECTIONS OF SEAT TRACK PER SRM 53-70-00. (M) 2 L 7 3 4F RT A22WE 1997021300639 19970213 00639 NM 1997 2 13 AALA961876 1 19961219 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1308-1361 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1766A 48597 TUL - CORROSION IN THREE AREAS. SPLICED IN NEW SECTION OF TRACK PER SRM 53-70-00. (M) 2 L 7 3 4F RT A22WE 1997021300640 19970213 00640 NM 1997 2 13 AALA961875 1 19961217 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 776 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1766A 48597 TUL - FOUND CORRODED SEAT TRACK. REPAIR TO SPECS PER SRM 53-70-00-0 VOL I PAGE 8 AND 9. (M) 2 L 7 3 4F RT A22WE 1997021300641 19970213 00641 WP 1997 2 13 AALA961835 1 19961210 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1309 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 219AA 49171 TUL - FOUND FRAME CORRODED BEYOND LIMITS. REPAIRED IAW SRM 53-10-00-14 NR 1 PAGE 2. (M) 2 L 7 2 4F A6WE 1997021300642 19970213 00642 WP 1997 2 13 AALA961834 1 19961212 A 5320 CUSP DOUG DC9 DC982 3022082 WP BS 1309 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 219AA 49171 TUL - FOUND CORROSION TWO AREAS ON BOTTOM SURFACE OF CUSP. REPAIRED PER ESO 80559, DATED 12-12-96. (M) 2 L 7 2 4F A6WE 1997021300643 19970213 00643 NM 1997 2 13 AALA961831 1 19961216 A 5320 WEB BOEING 727 727223 1384074 NM BS 740 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 6818 19493 TUL - NR 2 CENTER WING TANK, SEVERAL BULGES AND CRACKS AT STATION 740 LOWER CHORD, WEB FROM RBL 14 TO RBL 27. INSTALLED DOUBLER REPAIR PER ESO 11782. (M) 2 L 7 3 4F A3WE 1997021300644 19970213 00644 NM 1997 2 13 AALA961832 1 19961216 A 5320 RIVET BOEING 727 727223 1384074 NM BS 740 POPPED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 6818 19493 TUL - POPPED RIVET TAIL STATION 740 RBL 3, INSIDE NR 2 TANK CENTER LOWER CHORD AREA. INSTALLED REPAIR DOUBLER PER ESO 1 1782. (M) 2 L 7 3 4F A3WE 1997021300645 19970213 00645 NM 1997 2 13 AALA961830 1 19961120 A 5321 FLOOR SKIN BOEING 727 727223 1384074 NM BS 1176 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 6818 19493 TUL - CORROSION ON CHORD AND RT AFT LAV FLOOR SKIN, BS 1176.9 RBL 29-32 WL 208.1. REMOVED CORROSION TREATED AND PRIMED AREA PER MM 51-20-0. INSTALLED DOUBLER ON LAV FLOOR SKIN. (M) 2 L 7 3 4F A3WE 1997021300646 19970213 00646 NM 1997 2 13 AALA961828 1 19961120 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 1070 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 6818 19493 TUL - BS 1070 RBL 45.5 HEAVY CORROSION ON TOP LEG OF FLOORBEAM. REMOVED CORRODED PORTION OF FLOORBEAM. INSTALLED NEW P ORTION PER SRM 53-10-8. (M) 2 L 7 3 4F A3WE 1997021300648 19970213 00648 NM 1997 2 13 AALA961850 1 19961219 A 3240 26094724 BRAKE DOUG MD11 MD11 3023602 NM NR 1 MLG DEFECTIVE A AALA K NONE A FLAME/FIRE TX TAXI/GRND HDL 1 SW 07 1750B 0914 48419 MIA - FLT 901 - AFTER LANDING MIA, THE NR 1 MLG BRAKE CAUGHT FIRE. FIRE TRUCKS CALLED, FIRE WAS EXTINGUISHED BY RAMP PE RSONNEL. INSPECTED WHEEL AXLE PER MM AND REPLACED BRAKE ASSEMBLY AND WHEEL ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPER ATION. (M) 2 L 7 3 4F RT A22WE 1997021300649 19970213 00649 WP 1997 2 13 AALA961785 1 19961207 A 3610 BLEED DUCT DOUG DC10 DC1030 3023501 WP NR 3 ENGINE LOOSE A AALA A F UNSCHED LANDING ACTIVATE FIRE EXT. J WARNING INDICATION CR CRUISE 1 SW 07 164AA 46950 LAX - FLT 123 - EN ROUTE DFW/HNL, DURING CRUISE, FIRE WARNING ON NR 3 ENGINE. ACCOMPLISHED SHUTDOWN OF NR 3 ENGINE AND DISCHARGED BOTH FIRE BOTTLES. AIRCRAFT DIVERTED TO LAX AND LANDED WITHOUT INCIDENT. REPLACED BOTH FIRE EXTINGUISHER BO TTLES ON NR 3 ENGINE. RESECURED HIGH STAGE BLEED DUCT ON RT SIDE OF ENGINE AT Y DUCT. REPLACED PNEUMATIC DUCT UNDER ENG INE STANDOFF BRACKET AND STANDOFF BRACKET ROD END. REPLACED HEAT SHIELDS FROM B SUMP VENT LINE. REPLACED FAN AIR WIRES . REPLACED NR 3 ENGINE FIRE DETECTOR LOOPS A AND B FOR FAN AND PYLON. ACCOMPLISHED LEAK CHECK AND GROUND ENGINE RUN WI TH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A22WE 1997021300650 19970213 00650 WP 1997 2 13 AALA961872 1 19961228 A 2170 21D101 COALESCER DOUG DC9 DC982 3022082 WP ACM BAYS CONTAMINATED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 490AA 49683 AMA - FLT 1677 - EN ROUTE DFW/OAK - DURING CRUISE, ELECTRICAL TYPE ODOR NOTED IN CABIN. AIRCRAFT DIVERTED TO AMA AND LA NDED OVERWEIGHT WITHOUT INCIDENT. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION WITH NO DEFECTS FOUND. REPLACED ALL COALE SCER BAGS. ACCOMPLISHED GROUND ENGINE RUN, OPERATING ALL PACKS WITH NO ODOR NOTED. AIRCRAFT FCF/MAINTENANCE FERRY AMA/ DFW WITH NO DEFECTS OR ODOR NOTED. (M) 2 L 7 2 4F A6WE 1997021300651 19970213 00651 WP 1997 2 13 AALA961871 1 19961228 A 3222 STRUT DOUG DC9 DC983 3022083 WP NLG REQ'D SERVICE A AALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 07 594AA 53284 LAX - FLT 2098 - AFTER TAKEOFF LAX, WHEN LANDING GEAR RETRACTED, RED NOSE LANDING GEAR LIGHT REMAINED ILLUMINATED WITH A SSOCIATED WIND NOISE GEAR AREA. EXTENDED LANDING GEAR AND AIRCRAFT RETURNED TO LAX, LANDING OVERWEIGHT WITHOUT INCIDENT . ACCOMPLISHED OIL AND NITROGEN SERVICING TO NOSE GEAR STRUT. ACCOMPLISHED NOSE LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION WITH NO DEFECTS FOUN D. (M) 2 L 7 2 4F RT A6WE 1997021300652 19970213 00652 WP 1997 2 13 AALA961853 1 19961220 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 70524 49916 SFO - DURING OVERNIGHT CHECK, FOUND THE CEILING EMERGENCY LIGHTS BETWEEN ROWS 24-28 ARE INOPERATIVE. REPAIRED TERMINAL WIRE AT BATTERY CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1997021300653 19970213 00653 NM 1997 2 13 AALA961862 1 19961224 A 3350 653954819 HARNESS BOEING 727 727223 1384074 NM AFT CARGO DOOR DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 709AA 22466 DFW - DURING OVERNIGHT MAINTENANCE, FOUND AFT CARGO EMERGENCY LIGHT INOPERATIVE. REPLACED AFT CARGO DOOR HARNESS. SYST EM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1997021300654 19970213 00654 NM 1997 2 13 AALA961863 1 19961225 A 3350 1000679 LIGHT BOEING 727 727227 1384078 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 717AA 20610 DFW - DURING OVERNIGHT CHECK, FOUND OVERHEAD EMERGENCY LIGHT AT ROW 25 INOPERATIVE. REPLACED LIGHT ASSEMBLY AT ROW 25. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1997021300656 19970213 00656 EU 1997 2 13 AALA961845 1 19961218 A 3350 A3060698101 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 59081 639 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PAX SEAT ROW 20AB INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT STRIP CONNECTOR BY PAX SEAT ROW 20AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1997021300657 19970213 00657 EU 1997 2 13 AALA961861 1 19961223 A 3350 STRIP AIRBUS 300 A300B4605R 3930308 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 18066 509 BDL - DURING OVERNIGHT CHECK, FUOND EMERGENCY EXIT FLOOR PATH LIGHTING AT ROW 21 A/B BROKEN. REPAIRED EMERGENCY EXIT FL OOR PATH LIGHT STRIP AT ROW 21 A/B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1997021300658 19970213 00658 NM 1997 2 13 AALA961849 1 19961218 A 3397 WIRE DOUG MD11 MD11 3023602 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1756 48491 DFW - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTING AT L2 DOOR INOPERATIVE. REPAIRED WIRE AT THE L2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1997021300659 19970213 00659 NM 1997 2 13 AALA961846 1 19961217 A 3397 WIRE DOUG MD11 MD11 3023602 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1750B 48419 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 7G AND 18G INOPERATIVE. REPAIRED BROKEN AND CORRODED EMERGENCY FLOOR LIGHT CONNECTION IN AREA OF R2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1997021300660 19970213 00660 NM 1997 2 13 AALA961827 1 19961213 A 2560 D31038201 SLIDE BOEING 757 757223 1384957 NM L1 DOOR LOOSE A AALA K NONE O OTHER CR CRUISE 1 SW 07 690AA 25696 ORD - FLT 1700 - DURING CRUISE L1 DOOR EMERGENCY ESCAPE SLIDE IS LOOSE FROM DOOR AND SLIDE PACKAGE COVER. CAPTAIN DECLA RED AN EMERGENCY AND LANDED ORD AND WITHOUT FURTHER INCIDENT. INSPECTED L1 DOOR SLIDE ASSEMBLY AND SECURED SLIDE AND CO VER. (M) 2 L 7 2 4F RT A2NM 1997021300661 19970213 00661 NM 1997 2 13 AALA961750 1 19961203 A 2750 251N405039 INDICATOR BOEING 757 757223 1384957 NM LT TE FLAPS REQ RESET A A AALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 SW 07 625AA 24583 LAX - FLT 649 - DURING DESCENT INTO SNA, FLAP ASYMMETRY WARNING CAME ON AFTER SELECTING 1 DEGREE FLAP. ACCOMPLISHED EME RGENCY CHECKLIST AND LOWERED FLAPS BY ALTERNATE METHOD TO 20 DEGREES. AIRCRAFT DIVERTED TO LAX AND LANDED WITHOUT FURTH ER INCIDENT. RESET LEFT INBOARD FLAP TRANSMISSION OVER TORQUE INDICATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1997021300662 19970213 00662 NM 1997 2 13 AALA961726 1 19961124 A 2121 731376 FAN BOEING 757 757223 1384957 NM E/E COMPT DEFECTIVE A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 645AA 24603 MIA - FLT 2142 - EN ROUTE CCS/MIA - DURING CRUISE, FUMES NOTED COMING FROM COCKPIT INSTRUMENT PANEL. AIRCRAFT PROCEEDED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED NR 1 EQUIPMENT SUPPLY FAN AND FILTER. SYSTEM GROUND CHECKED NORMAL OPERA TION. (M) 2 L 7 2 4F RT A2NM 1997021300663 19970213 00663 WP 1997 2 13 AALA961866 1 19961226 A 3350 A3060698101 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 554AA 53084 DFW - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTING IN FIRST CLASS SECTION INOPERATIVE. RECONNECTED EMERGENCY EXIT FLOOR PATH LIGHT STRIP IN FIRST CLASS SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1997021300664 19970213 00664 WP 1997 2 13 AALA961865 1 19961226 A 3350 STRIP DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 285AA 49297 DFW - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTING AT AFT OF PLANE INOPERATIVE. REPLACE EMERGENCY E XIT FLOOR PATH LIGHT STRIP AT AFT OF PLANE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1997021300665 19970213 00665 WP 1997 2 13 AALA961860 1 19961223 A 3350 L201011 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7528A 49920 DFW - DURING OVERNIGHT CHECK, FOUND THE FORWARD RIGHT SIDE EMERGENCY EXIT LIGHT AT OVERWING EXIT DOOR INOPERATIVE. REPL ACED EMERGENCY EXIT LIGHT ASSEMBLY FOR FORWARD RIGHT OVERWING EMERGENCY EXIT SIDEWALL LIGHT. SYSTEM GROUND CHECKED NORM AL OPERATION. (M) 2 L 7 2 4F A6WE 1997021300666 19970213 00666 WP 1997 2 13 AALA961859 1 19961223 A 3350 STRIP DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 453AA 49558 DFW - DURING OVERNIGHT MAINTENANCE, FOUND TWO FEET OF EMERGENCY EXIT FLOOR PATH LIGHTING IN AFT CABIN INOPERATIVE. REPL ACED SECTION OF EMERGENCY EXIT FLOOR PATH LIGHT STRIP IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1997021300667 19970213 00667 NM 1997 2 13 AALA961868 1 19961227 A 2121 732591E FAN BOEING 767 767223 1385123 NM E/E COMPT DEFECTIVE A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 329AA 564 22329 LHR - FLT 108 - EN ROUTE BOS-LHR - THE FORWARD EQUIPMENT EXHAUST FAN CIRCUIT BREAKER (20H) POPPED. CREW NOTED ELECTRICA L BURNING, NO SMOKE. AFTER 10 MINUTES SMELL WENT AWAY. LANDED LHR WITHOUT FURTHER INCIDENT. REPLACED FORWARD EQUIPMEN T EXHAUST FAN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1997021300668 19970213 00668 NM 1997 2 13 AALA961852 1 19961220 A 2780 834503 SWITCH BOEING 767 767323 1385205 NM LT LE SLAT DEFECTIVE A AALA B EMER. DESCENT J WARNING INDICATION AP APPROACH 1 SW 07 363AA 24044 DFW - FLT 1998 - DURING APPROACH DFW, WHILE EXTENDING FLAPS TO 5 DEGREES A EICAS LEADING EDGE SLAT ASYMMETRIC AND LEADIN G EDGE LIGHT CAME ON. DECLARED EMERGENCY, ACCOMPLISHED PCDR AND LANDED DFW WITHOUT INCIDENT. REPLACED LEFT OUTBOARD SL AT NR 2 INBOARD PROX SWITCH. ACCOMPLISHED SENSOR TARGET TEST, SENSOR TEST NORMAL. SYSTEM GROUND CHECKED NORMAL OPERATI ON. (M) 2 L 7 2 4F RT A1NM 1997021300669 19970213 00669 WP 1997 2 13 AALA961857 1 19961218 A 5280 ANB7216503 DOOR DOUG DC10 DC1030 3023501 WP LT MLG MISSING A AALA K NONE O OTHER UK UNKNOWN 1 SW 07 137AA 47847 HNL - FLT 73 - ON ARRIVAL HNL, DURING MAINTENANCE WALK AROUND FOUND LEFT MAIN LANDING GEAR DOOR OUTER DOOR PANEL MISSING . DEFERRED DUE TO NO PARTS AVAILABLE, INSPECTED AIRCRAFT FOR AIRWORTHINESS OF FLIGHT. NO OTHER DISCREPANCIES NOTED. A IRCRAFT RELEASE FOR MAINTENANCE FERRY FLIGHT TO TUL ACCOMPLISHED FERRY FLIGHT TO TUL. REPLACED MAIN LANDING GEAR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A22WE 1997021300670 19970213 00670 WP 1997 2 13 AALA961833 1 19961207 A 5280 ANB7216503 DOOR DOUG DC10 DC1030 3023501 WP LT MLG MISSING A AALA K NONE O OTHER UK UNKNOWN 1 SW 07 137AA 47847 HNL - FLT 73 - AFTER GATE ARRIVAL DURING WALK AROUND, LT MAIN LANDING GEAR DOOR OUTER DOOR PANEL DISCOVERED MISSING WITH SLIGHT DAMAGE TO LEFT INBOARD FLAP ACCESS PANEL. ACCOMPLISHED TEMPORARY REPAIR TO FLAP ACCESS PANEL AND AIRCRAFT MAINT ENANCE FERRY HNL/TUL. REPLACED LEFT MAIN LANDING GEAR DOOR OUTER DOOR PANEL. ACCOMPLISHED LANDING GEAR RETRACTION CHEC K WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A22WE 1997021300672 19970213 00672 WP 1997 2 13 AALA961854 1 19961221 A 2520 5762451 SEAT BELT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 07 557AN 53087 SNA - FLT 1820 - DURING TAKEOFF ROLL AT SNA, THE LAND LIGHT ILLUMINATED AND CREW ABORTED TAKEOFF. DURING ABORTED TAKEOF F SEAT BELT 25F CAME APART. AIRCRAFT CAME TO A HALT WITHOUT FURTHER INCIDENT. REPLACED SEAT BELT 25F AND ROUTED OLD BE LT TO TUL. (M) 2 L 7 2 4F A6WE 1997021300673 19970213 00673 WP 1997 2 13 AALA961856 1 19961218 A 3260 H14000 ROLLER DOUG DC9 DC982 3022082 WP NOSE GEAR BROKEN A AALA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 215AA 49163 ORD - FLT 2225 - DURING CRUISE EN ROUTE SYR-ORD, NOSE GEAR RED LIGHT REMAINED ON. NO AIR NOISE OR YAW ASSOCIATED WITH L IGHT. NOSE WHEEL STEERING TURNS NOSE WHEEL TO THE POINT NOSE DOORS OPEN. AUXILIARY PUMP, TRANS PUMP, AND ENGINE PUMPS ON HIGH DOES NOT EXTINGUISH LIGHT. LANDED ORD WITHOUT FURTHER INCIDENT. REPLACED GROUND SENSE CONTROL MECHANISM ROLLER . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1997021300674 19970213 00674 NE 1997 2 13 AALA961843 2 19961216 A 7200 ENGINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE RIGHT LEAKING OIL A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 564AA 49346 MIA - FLT 1989 - AFTER T/O MIA, DURING INITIAL CLIMB-OUT, SMOKE NOTED IN COCKPIT AND CABIN. AIRCRAFT RETURNED TO MIA AN D LANDED OVERWEIGHT WITHOUT INCIDENT. REPLACED RT ENGINE DUE TO OIL LEAK AT NR 3 BEARING DRAIN BREATHER. ACCOMPLISHED LEAK CHECK AND GROUND ENGINE RUN WITH NO DEFECTS FOUND. REPLACED ALL COALESCER BAGS AND ACCOMPLISHED PACK BURNOUT PROCE DURE. SYSTEM GROUND CHECKED NORMAL OPERATION. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION WITH NO DEFECTS FOUND. ACCO MPLISHED FUNCTIONAL CHECK FLIGHT WITH NO SMOKE NOTED. SYSTEM OPERATIONAL CHECKED NORMAL. (M0 2 L 7 2 4F 4 F RT A6WE E9NE 1997021300675 19970213 00675 WP 1997 2 13 AALA961818 1 19961213 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 505AA 49799 SFO - DURING OVERNIGHT MAINTENANCE, FOUND THE EMERGENCY EXIT FLOOR PATH LGHTS BETWEEN ROW 16 AND 20 IS INTERMITTENT. SE CURED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR AT SEAT ROW 15D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1997021300676 19970213 00676 EU 1997 2 13 AALA961791 1 19961210 A 3350 STRIP AIRBUS 300 A300B4605R 3930308 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 19059 469 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN AFT SECTION OF MAIN CABIN INOPERATIVE. REPLACED TWO SECTIONS OF EMERGENCY FLOOR LIGHT STRIP IN AFT SECTION OF MAIN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1997021300677 19970213 00677 EU 1997 2 13 AALA961764 1 19961204 A 3350 A3030398101 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7076A 610 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY 4L DOR INOPERATIVE. RESECURED EMERGENCY FLOOR LIGHT CONNECTOR B Y 4L DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1997021300678 19970213 00678 EU 1997 2 13 AALA961769 1 19961208 A 3350 A3030398101 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7055A 462 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT PAX SEATS 8A AND 8B INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT CONNECTORS AT DOOR 2L. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1997021300679 19970213 00679 EU 1997 2 13 AALA961768 1 19961208 A 3350 A3030398101 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 14061 471 MIA - DURING OVERNIGHT CHECK, RIGHT AISLE EMERGENCY FLOOR LIGHTS INOPERATIVE. RESECURED RIGHT AISLE EMERGENCY FLOOR LIG HT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1997021300680 19970213 00680 EU 1997 2 13 AALA961821 1 19961214 A 3350 STRIP AIRBUS 300 A300B4605R 3930308 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 70072 515 JFK - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY EXIT FLOOR PATH LIGHTS AT 12HJ TO 14HJ INOPERATIVE. REPLACED EMERGE NCY EXIT FLOOR PATH LIGHT ASSEMBLY BETWEEN 12HJ AND 14HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1997021300681 19970213 00681 WP 1997 2 13 AALA961817 1 19961213 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG OVER SERVICED A AALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 07 429AA 49341 LAX - FLT 1508 - AFTER TAKEOFF LAX, THE NOSE GEAR WOULD NOT RETRACT. RETURNED AND LANDED LAX WITHOUT FURTHER INCIDENT. RESERVICED OVER SERVICED NOSE GEAR PER MM. ACCOMPLISHED NOSE GEAR RETRACTION. GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1997021300682 19970213 00682 WP 1997 2 13 AALA961824 1 19961215 A 3260 833703 SENSOR DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA K NONE N FALSE WARNING CL CLIMB 1 SW 07 462AA 49592 ORD - FLT 1059 - DURING CLIMB-OUT BOS, THE RED NOSE GEAR UNSAFE LIGHT ILLUMINATED FOR APPROXIMATELY ONE MINUTE THEN EXTI NGUISHED. LANDED ORD WITHOUT FURTHER INCIDENT. REPLACED NLG UP SENSOR AND PROX ELECTRONIC BOX. ACCOMPLISHED GEAR SWIN G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1997021300683 19970213 00683 EU 1997 2 13 AALA961773 1 19961206 A 3230 715391 SELECTOR VALVE FOKKER F28 F28MK0100 4990807 EU NLG DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 1455K 11467 SAT FLT 1488 - AFTER TAKEOFF UNABLE TO RETRACT NOSE LANDING GEAR. RECYCLED LANDING GEAR WITH SAME RESULT. AIRCRAFT RET URNED TO SAT AND LANDED WITHOUT FURTHER INCIDENT. INSPECTED NOSE LANDING GEAR AND FOUND NO VISIBLE DEFECTS. AIRCRAFT R ELEASED FOR GEAR DOWN MAINTENANCE FERRY SAT/DFW. REPLACED NOSE GEAR DOOR SELECTOR VALVE AT DFW. ACCOMPLISHED RETRACTIO N CHECK AND LEAK CHECK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1997021300684 19970213 00684 NM 1997 2 13 AALA961772 1 19961206 A 3350 STRIP DOUG MD11 MD11 3023602 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1755 48490 DFW - DURING OVERNIGHT CHECK, TWO EMERGENCY FLOOR LIGHT STRIP BULBS INOPERATIVE AT PAX SEAT 38C. REPLACED EMERGENCY FLO OR LIGHT STRIP AT PAX SEAT 38C. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1997021300685 19970213 00685 WP 1997 2 13 AALA961822 1 19961214 A 3350 P4010051127 CONTROL MODULE DOUG DC10 DC1010 3022110 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 168AA 46938 JFK - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS AND BUSINESS CLASS RIGHT SIDE IN OPERATIVE. REPLACED CONTROL MODULE AND BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A22WE 1997021300686 19970213 00686 NM 1997 2 13 AALA961771 1 19961207 A 3350 0201820001 LIGHT BOEING 767 767223 1385123 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 338AA 22335 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT AT LEFT FORWARD CROSS AISLE INOPERATIVE. REPLACED EMERGENCY FLOOR L IGHT ASSEMBLY AT LEFT FORWARD CROSS AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1997021300687 19970213 00687 NM 1997 2 13 AALA961584 1 19961029 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 330AA 22330 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT PAX SEAT 2H INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT SI DEWALL CONNECTOR AT PAX SEAT 2H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1997021300688 19970213 00688 NM 1997 2 13 AALA961808 1 19961211 A 3350 FCC4007 RELAY BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SW 07 6823 19701 DFW - FLT 548 - AFTER GATE DEPARTURE DURING TAXI-OUT, EMERGENCY EXIT LIGHTS ILLUMINATED INTERMITTENTLY WITH SWITCH IN AR MED POSITION. AIRCRAFT RETURNED TO GATE. REPLACED EMERGENCY EXIT LIGHT RELAY R-70. SYSTEM GROUND CHECKED NORMAL OPERA TION. (M) 2 L 7 3 4F A3WE 1997021300689 19970213 00689 NM 1997 2 13 USAABB96068 1 19961226 A 3350 873100151 LIGHT BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 618AU 22210 LAX - FOUND SEAT EMERGENCY ASSEMBLY INOPERATIVE. MAINTENANCE REPLACED THE ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 1997021300690 19970213 00690 NM 1997 2 13 USAABB96067 1 19961223 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 631AU 27809 LAX - FOUND PASSENGER SEAT EMERGENCY LIGHT BATTERIES DEAD IN ROWS 1, 4, 6, 9 AND 13. MAINTENANCE REPLACED THE BATTERIES . (M) 2 L 7 2 4F RT A2NM 1997021300707 19970213 00707 NM 1997 2 13 USAA970017 1 19960117 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 986 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 376US 35405 22955 CLT - INSPECTION VISUALLY FOUND MULTIPLE LEVEL 2 CORROSION MEASURING 1 INCH BY 1 INCH LOCATED AT FLOORBEAM STATION 986, B10 BL 46 L PLUS R. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. REPAIRED FLOORBEAM PER SRM 53-60-51 AND TYPICAL R EPAIR MANUAL 53-15-01A. (M) 2 L 7 2 4F RT A16WE 1997021300712 19970213 00712 NM 1997 2 13 AALA961804 1 19961120 A 5330 148N3611 SKIN BOEING 757 757223 1384957 NM BS 1862.7 WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 661AA 25295 AFW - FOUND FUSELAGE SKIN AT STATION 1862.7 (LT) LOWER HAS WEAR FROM HORIZONTAL STAB SEAL. MATERIAL REMAINING IS BEYOND SRM LIMITS. REPAIR PER MRB 757-1013. (M) 2 L 7 2 4F RT A2NM 1997021300713 19970213 00713 NM 1997 2 13 AALA961805 1 19961120 A 5315 141N5111 FLOORBEAM BOEING 757 757223 1384957 NM BS 345 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 661AA 25295 AFW - FOUND FLOORBEAM AT STATION 345 HAS GOUGE/CORROSION REMOVED ON UPPER SURFACE. MATERIAL REMAINING IS BEYOND SRM ALL OWABLE LIMITS. REPAIRED PER MRB 757-1024. (M) 2 L 7 2 4F RT A2NM 1997021300714 19970213 00714 NM 1997 2 13 AALA961806 1 19961120 A 5320 141N5100 FLOOR SUPPORT BOEING 757 757223 1384957 NM BS 400 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 661AA 25295 AFW - FLOOR SUPPORT STRUCTURE HAS CORROSION REMOVAL ON UPPER SURFACE. MATERIAL REMAINING IS BEYOND SRM ALLOWABLE LIMITS . REF E58 NR 1830913. ALODINE ALL BLENDED AREAS. FABRICATE STRAPS USING .050 301.5 HARD STAINLESS STEEL. APPLY 2 COA TS PRIMER TO STRAP AND FLOORBEAM. FILL ALL BLENDED AREA WITH AM 55-92 TYPE 1023 INSTALL STRAP WET WITH BM55-95 SEALANT USING BACB30NWG, HI-LOCKS. (M) 2 L 7 2 4F RT A2NM 1997021300715 19970213 00715 NM 1997 2 13 AALA961807 1 19961120 A 5315 141N5112 FLOORBEAM BOEING 757 757223 1384957 NM BS 365 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 661AA 25295 AFW - FLOORBEAM AT STATION 365 HAS CORROSION REMOVAL ON UPPER SURFACE. MATERIAL REMAINING IS BEYOND ALLOWABLE SRM LIMIT S. REPAIRED PER MRB 757-1016. (M) 2 L 7 2 4F RT A2NM 1997021300716 19970213 00716 NM 1997 2 13 AALA961893 1 19961219 A 5330 148N3611 SKIN BOEING 757 757223 1384957 NM BS 1862.7 WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 662AA 25296 AFW - FOUND STATION 1862.7 HAS SMALL AREA OF WEAR, BEYOND SRM LIMITS. REPAIR PER MRB 757-1038. (M) 2 L 7 2 4F RT A2NM 1997021300717 19970213 00717 NM 1997 2 13 AALA961894 1 19961219 A 5315 141N5112 FLOORBEAM BOEING 757 757223 1384957 NM BS 365 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 662AA 25296 AFW - FOUND FLOORBEAM AT STATION 365 RBL 61 HAD CORROSION BLENDED BEYOND ALLOWABLE SRM LIMITS. REPAIRED PER MRB 757-102 8. (M) 2 L 7 2 4F RT A2NM 1997021300718 19970213 00718 NM 1997 2 13 AALA961895 1 19961219 A 5320 146N8522 SILL BOEING 757 757223 1384957 NM CARGO DOORWAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 662AA 25296 AFW - AFT CARGO DOOR LOWER SILL INNER CHORD HAD CORROSION BLENDED BEYOND ALLOWABLE SRM LIMITS. REPAIR PER MRB 757-1037. (M) 2 L 7 2 4F RT A2NM 1997021300719 19970213 00719 NM 1997 2 13 AALA961896 1 19961219 A 5320 141N516151 FLOOR SUPPORT BOEING 757 757223 1384957 NM BS 372 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 662AA 25296 AFW - FLOOR STRUCTURE AT STATION 372 RBL 62 HAD CORROSION BLENDED BEYOND ALLOWABLE SRM LIMITS. REPAIR PER MRB 757-1027. (M) 2 L 7 2 4F RT A2NM 1997021300720 19970213 00720 NM 1997 2 13 AALA961897 1 19961219 A 5320 141N5160 FLOOR SUPPORT BOEING 757 757223 1384957 NM BS 357 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 662AA 25296 AFW - FOUND FLOOR STRUCTURE AT STATION 357 RBL 62 HAD CORROSION BLENDED BEYOND SRM LIMITS. REPAIR PER MRB 757-1029. (M ) 2 L 7 2 4F RT A2NM 1997021300721 19970213 00721 NM 1997 2 13 AALA961898 1 19961219 A 5320 141N516255 FLOOR SUPPORT BOEING 757 757223 1384957 NM BS 408 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 662AA 25296 AFW - FLOOR STRUCTURE AT STATION 408 RBL 57 HAD CORROSION BLENDED BEYOND SRM LIMITS. REPAIR PER MRB 757-1030. (M) 2 L 7 2 4F RT A2NM 1997021300722 19970213 00722 NM 1997 2 13 AALA961899 1 19961219 A 5320 141N5160 FLOOR SUPPORT BOEING 757 757223 1384957 NM BS 331 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 662AA 25296 AFW - FLOOR STRUCTURE AT STATION 331 RBL 3 HAD CORROSION BLENDED BEYOND SRM LIMITS. REPAIR PER MRB 757-1031. (M) 2 L 7 2 4F RT A2NM 1997021300723 19970213 00723 NM 1997 2 13 AALA961900 1 19961219 A 5315 141N5810 FLOORBEAM BOEING 757 757223 1384957 NM BS 310 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 662AA 25296 AFW - FLOORBEAM AT STATION 310 RBL 3 HAD CORROSION BLENDED BEYOND SRM LIMITS. REPAIR PER MRB 757-1032. (M) 2 L 7 2 4F RT A2NM 1997021300724 19970213 00724 NM 1997 2 13 AALA961901 1 19961219 A 5320 141N5161 FLOOR SUPPORT BOEING 757 757223 1384957 NM BS 403 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 662AA 25296 AFW - FLOOR STRUCTURE AT STATION 403 RBL 59 HAD CORROSION BLENDED BEYOND SRM LIMITS. REPAIR PER MRB 757-1034. (M) 2 L 7 2 4F RT A2NM 1997021300725 19970213 00725 NM 1997 2 13 AALA961902 1 19961219 A 5315 141N5113 FLOOR BEAM BOEING 757 757223 1384957 NM BS 377 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 662AA 25296 AFW - FLOOR BEAM AT STATION 377 RBL 11 HAD CORROSION BLENDED BEYOND SRM LIMITS. REPAIR PER MRB 757-1035. (M) 2 L 7 2 4F RT A2NM 1997021300726 19970213 00726 NM 1997 2 13 AALA961903 1 19961219 A 5210 146N62015 DOOR PAN BOEING 757 757223 1384957 NM L4 DOOR GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 662AA 25296 AFW - L-4 DOOR HANDLE PAN HAS GOUGE BEYOND SRM LIMITS. REPAIR PER MRB 757-1040. (M) 2 L 7 2 4F RT A2NM 1997021300727 19970213 00727 NM 1997 2 13 AALA961904 1 19961219 A 5315 146N5089 FLOORBEAM BOEING 757 757223 1384957 NM BS 1640 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 662AA 25296 AFW - FLOOR BEAM AT STATION 1640 HAS CORROSION REMOVAL ON UPPER SURFACE. MATERIAL REMAINING IS BEYOND SRM ALLOWABLE LIM ITS. REPAIR PER MRB 757-1036. (M) 2 L 7 2 4F RT A2NM 1997021300728 19970213 00728 NM 1997 2 13 AALA961687 1 19961115 A 5320 SUPPORT DOUG MD11 MD11 3023602 NM BS 467 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1764B 48554 TUL - FLOOR BOARD SUPPORT HAS CORROSION AROUND ALL SCREW HOLES. INSTALLED A NEW FLOORBOARD SUPPORT PER SRM 53-00-01 PAG E 2 VOL I AND PAINTED. (M) 2 L 7 3 4F RT A22WE 1997021300729 19970213 00729 NM 1997 2 13 AALA961782 1 19961209 A 5320 WEB BOEING 727 727223 1384074 NM BS 950-930 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 864AA 21369 TUL - MLG W/W PRESSURE DECK WEB CRACKED, STATION 950 AND 930. REMOVED DAMAGED AREA AND REPAIRED PER ESO 11677 DATE 11-6 -96. (M) 2 L 7 3 4F A3WE 1997021300730 19970213 00730 NM 1997 2 13 AALA961786 1 19961206 A 5400 S-DUCT BOEING 727 727227 1384078 NM BS 1210 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 730AA 20737 TUL - FOUND CORROSION AT LOWER SIDE OF MATE POINTS FOR UPPER AND LOWER S-DUCTS (WORN DUCTS) 6 O'CLOCK ON DUCT OUTSIDE DI AMETER. REMOVED CORROSION AND INSTALLED DOUBLER PER ESO 11697, DATED 11-26-96. (M) 2 L 7 3 4F A3WE 1997021300731 19970213 00731 NM 1997 2 13 AALA961733 1 19961113 A 5330 SKIN BOEING 727 727223 1384074 NM BS 410 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 6813 19488 TUL - FOUND SKIN CRACKED AT 4 RIVITS HEADS, STATION 410. CUT OUT CRACKS IN SKIN INSTALLED REPAIR PER SRM 53-30-3 . (M) 2 L 7 3 4F A3WE 1997021300732 19970213 00732 NM 1997 2 13 AALA961784 1 19961209 A 5311 FRAME BOEING 727 727223 1384074 NM BS 540 WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 844AA 20985 TUL - FOUND OBLONG HOLE IN FRAME STATION 540, STRINGER 28R. INSTALLED 063 30155 DOUBLER ON FRAME PER SRM 51-40-3. (M) 2 L 7 3 4F A3WE 1997021300733 19970213 00733 NM 1997 2 13 AALA961779 1 19961209 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 450-480 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 844AA 20985 TUL - FOUND STRINGER 28L DEEP GOUGES AND DENTED STATION 450-480. INSTALLED STRINGER SPLICE ON STRINGER 28L, STATION 450 -480 PER SRM 51-10-1 PAGE 4. (M) 2 L 7 3 4F A3WE 1997021300734 19970213 00734 NM 1997 2 13 AALA961780 1 19961209 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 844AA 20985 TUL - FOUND STATION 720B STRINGER 15L CRACKED AT END. REMOVED STRINGER, MADE FILLER, REPLACED AND REPAIRED WITH U-CHANN EL AND SPLICE REPAIR PER SRM 51-10-3. (M) 2 L 7 3 4F A3WE 1997021300735 19970213 00735 NM 1997 2 13 AALA961781 1 19961209 A 5314 KEEL BEAM BOEING 727 727223 1384074 NM BS 874 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 844AA 20985 TUL - FOUND 1 INCH CRACK LEFT LOWER CHORD KEEL BEAM AT UPPER FLANGE STATION 874. 5 INCH CRACK LT SIDEWALL WEB OF KEEL B EAM LOWER CORNER STATION 874. BOEING MANUFACTURE SPECIAL BULLETIN S/B 53-0208 REPAIR (A) BOTH CRACKS. (M) 2 L 7 3 4F A3WE 1997021300736 19970213 00736 NM 1997 2 13 AALA961775 1 19961209 A 5730 SKIN BOEING 727 727223 1384074 NM BS 830 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 844AA 20985 TUL - FOUND LOWER WING SKIN CORRODED INSIDE PLENUM AT FS 830 LBL 36. REMOVED CORROSION AT FS 830 LBL 36 TREATED AND PAI NTED AND INSTALLED REPAIR PER SRM 5730-36 SEALED DOUBLER REPAIR AND FASTENERS. (M) 2 L 7 3 4F A3WE 1997021300737 19970213 00737 NM 1997 2 13 AALA961778 1 19961209 A 5330 SKIN BOEING 727 727223 1384074 NM BS 660 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 844AA 20985 TUL - FOUND SKIN CORRODED AND BULGED OUT STRINGER 25L-26L. CUT OUT DAMAGED SKIN AND INSTALLED FLUSH DOUBLER REPAIR PER SRM 53-30-3 FIG 6. (M) 2 L 7 3 4F A3WE 1997021300738 19970213 00738 NM 1997 2 13 AALA961777 1 19961209 A 5320 SPLICE BOEING 727 727223 1384074 NM BS 1010-1030 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 844AA 20985 TUL - BOTTOM ENTIRE LENGTH OF SPLICE CHANNEL CORRODED. INSTALLED NEW STRINGER SPLICE STATION 1010. (M) 2 L 7 3 4F A3WE 1997021300739 19970213 00739 NM 1997 2 13 AALA961776 1 19961209 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1096 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 844AA 20985 TUL - FUSELAGE SKIN HAS .75 INCH CRACK ALONG STRINGER 1 AT FS 1096. CUT OUT CRACKED AREA OF FUSELAGE SKIN AND INSTALLED DOUBLER PER SB 727-53 A0204 FIG 1 AND 2. (M) 2 L 7 3 4F A3WE 1997021300740 19970213 00740 WP 1997 2 13 AALA961829 1 19961213 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 180-200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 488AA 49681 TUL - FOUND CORROSION ON CUSP ANGLE STATION 180 TO 200 AT FORWARD SERVICE DOOR LOWER JAMB. INSTALLED DOUBLER PER ESO 80 559, DATED 7-23-96. (M) 2 L 7 2 4F A6WE 1997021300741 19970213 00741 WP 1997 2 13 AALA961816 1 19961211 A 5320 FRAME DOUG DC9 DC982 3022082 WP CARGO DOORWAY BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 577AA 53154 TUL - FOUND ON THE AFT CARGO DOOR APPROX 7 O'CLOCK POSITION FUSELAGE SKIN OUTER FRAME BENT. INSTALLED DOUBLER PER SRM 5 3-05 AND ESO80559. (M) 2 L 7 2 4F A6WE 1997021300742 19970213 00742 NM 1997 2 13 AALA961606 1 19961030 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 460-465 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1762B 48552 TUL - FOUND CORROSION AT NR 1 LEFT FLOOR SEAT TRACK FORWARD OUTBOARD CORNER ANCHOR POINT FOR LAV A. REPLACED CORRODED S ECTION WITH SEAT TRACK PLUG AS PER SRM 53-70-00 VOL I FIG 102. (M) 2 L 7 3 4F RT A22WE 1997021300743 19970213 00743 NM 1997 2 13 AALA961608 1 19961030 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 460-465 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1762B 48552 TUL - FOUND CORROSION AT NR 8 RIGHT FLOOR SEAT TRACK FORWARD OUTBOARD CORNER ANCHOR POINT FOR LAV B. INSTALLED CHANNEL PLUG PER SRM 53-70-00-0 VOL 1 FIG 4. (M) 2 L 7 3 4F RT A22WE 1997021300744 19970213 00744 NM 1997 2 13 AALA961589 1 19961031 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1351 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1762B 48552 TUL - FOUND CORROSION AT LAV 'M' AFT INBOARD TIE DOWN LUG. INSTALLED PLUG REPAIR PER SRM 53-70-00. (M) 2 L 7 3 4F RT A22WE 1997021300763 19970213 00763 CE 1997 2 13 C2XA96CL048 1 19961223 A 5210 129400034605 DOOR BEECH 1900 1900D 1154162 CE PAX DOOR DAMAGED A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 09 16540 2712 UE172 CLE - FLT 3021 - CREW REPORTED THAT DURING CLIMB THE PASSENGER AIRSTAIR DOOR FLEW OPEN, AIRCRAFT RETURNED TO FIELD AND D AMAGE TO THE DOOR OCCURRED UPON LANDING. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED THE PASSENGER DOOR IAW B1900 MM 52-10-00. INVESTIGATION PENDING AS TO CAUSE FO THE DOOR OPENING IN FLIGHT. (M) 2 L 7 2 4T RT A24CE 1997021900001 19970219 00001 NM 1997 2 19 F3LA96076 1 19961005 A 2730 CONTROL SYSTEM BOEING 737 737201 1384454 NM ELEVATOR STIFF A F3LA O OTHER O OTHER AP APPROACH 1 NM 03 205AU 19421 UPON ARRIVAL, FLIGHT CREW REPORTED ELEVATOR STIFF, ESPECIALLY DURING FLARE. MAINTENANCE CHECKED ALL FLIGHT CONTROLS FOR MOVEMENT AND POSITION PER MM AND FOUND OK. PERFORMED TEST FLIGHT AND CHECK OK. (M) 2 L 7 2 4F A16WE 1997021900002 19970219 00002 NM 1997 2 19 F3LA96030 1 19961009 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 380 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 214AU 20214 PAE - FOUND CRACK IN STRINGER 27 LEFT AT BS 380 PLUS 12. CUTOUT DAMAGED AREA OF STRINGER AND REPAIRED PER SRM 53-10-03. WORK DOCUMENTED ON NRC FUSELAGE 291. (M) 2 L 7 2 4F A16WE 1997022000005 19970220 00005 NM 1997 2 20 CAL960450 1 19960409 A 5753 PIN BOEING 737 7373T0 1384582 NM TE FLAP FAIRING FAILED A CALA O OTHER D E INFLIGHT SEPARATION VIBRATION/BUFFET CL CLIMB 1 SW 09 14342 23580 THE FLIGHT CREW REPORTED AIRFRAME VIBRATION AFTER TAKEOFF FROM PHX. THE FLIGHT CONTINUED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT INBOARD FLAP FAIRING HAD DEPARTED THE AIRCRAFT. THE FAIRING WAS RECOVERED ON OR NE AR THE RUNWAY AT PHX. A NEW FAIRING WAS INSTALLED. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION . INVESTIGATION REVEALED THAT ONE OF THE FAIRING GUIDE PINS HAD BROKEN OFF RESULTING IN EVENTUAL SEPARATION OF THE FAIR ING FROM THE AIRCRAFT. 2 L 7 2 4F RT A16WE 1997022000051 19970220 00051 WP 1997 2 20 97ZZZX714 1 19961207 A 5743 5893930 FITTING DOUG DC8 DC8F54 3021926 WP RT MLG CRACKED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 7046H 38071 16336 46011 DURING ROUTINE INSPECTION, FOUND RIGHT MLG FITTING CRACKED BEYOND FLYABLE LIMITS. AIRCRAFT PLACED ON INACTIVE STATUS PE NDING REPLACEMENT OF FITTING. 2 L 7 4 4F 4A25 1997022000052 19970220 00052 EU 1997 2 20 97ZZZX715 1 19961230 A 6340 6607A2114 SWITCH BOLKMS 105 BO105LSA3 5626020 EU OIL PRESS WARN INOPERATIVE A R7MA K NONE P NO WARNING INDICATION NR NOT REPORTED 1 NM 11 202LF 592 T18147 2014 OIL PRESS WARN SWITCH INOPERATIVE. LIGHT CAME ON DURING FLIGHT THEN WENT OUT. REPLACED WITH NEW UNIT, CORRECTED PROBLE M. 1 G 7 2 3U H3AU 1997022000054 19970220 00054 1997 2 20 97ZZZX717 4 19961223 A 3452 066011410101 TRANSPONDER KING KT70 BOLKMS 117 BK117B1 5626012 EU COCKPIT INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 7059N 7154 TRANSPONDER INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1997022000055 19970220 00055 NM 1997 2 20 97ZZZX718 1 19961124 A 6220 900R210123101 SNUBBER BOLT DOUG MD900 MD900 3027375 NM M/R HEAD WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 1057 90000012 M/R HEAD SNUBBER BOLT WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW 5 EACH UNITS, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997022000056 19970220 00056 NM 1997 2 20 97ZZZX719 1 19961029 A 6220 900R3101001107 BEARING DOUG MD900 MD900 3027375 NM M/R CENTERING WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 121 0206040396 90000012 M/R CENTERING BEARING ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. DEBONDING FROM BALL. REPLACED WITH NEW UNIT, CORREC TED PROBLEM. 1 G 7 2 3U NC H19NM 1997022000057 19970220 00057 NM 1997 2 20 97ZZZX720 1 19961029 A 6200 9003101001107 BEARING DOUG MD900 MD900 3027375 NM M/R CENTERING WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 121 0206040408 90000012 M/R CENTERING BEARING ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. DEBONDING FROM BALL. REPLACED WITH NEW UNIT, CORREC TED PROBLEM. 1 G 7 2 3U NC H19NM 1997022000058 19970220 00058 NM 1997 2 20 97ZZZX721 1 19961125 A 6220 900R3101001107 BEARING DOUG MD900 MD900 3027375 NM M/R CENTERING WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 48 0206040526 90000012 CENTERING BEARING ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. DEBONDING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997022000059 19970220 00059 NM 1997 2 20 97ZZZX722 1 19961125 A 6220 900R3101001107 BEARING DOUG MD900 MD900 3027375 NM M/R CENTERING WORN A R7MA D RETURN TO BLOCK O OTHER IN INSP/MAINT 1 NM 11 901CF 168 0206040402 90000012 M/R CENTERING BEARING ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. DEBONDING. REPLACED WITH NEW UNIT, CORRECTED PROBLE M. 1 G 7 2 3U NC H19NM 1997022000060 19970220 00060 NM 1997 2 20 97ZZZX723 1 19961125 A 6220 900R3101001107 BEARING DOUG MD900 MD900 3027375 NM M/R CENTERING WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 48 0206040509 90000012 M/R CENTERING BEARING ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. DEBONDING. REPLACED WITH NEW UNIT, CORRECTED PROBLE M. 1 G 7 2 3U NC H19NM 1997022000062 19970220 00062 NM 1997 2 20 97ZZZX725 1 19961022 A 6720 CEKP3AR112 THRUST BEARING DOUG MD900 MD900 3027375 NM T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 100 90000012 THRUST BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 3 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997022000063 19970220 00063 NM 1997 2 20 97ZZZX726 1 19961125 A 6220 900R3101001107 BEARING DOUG MD900 MD900 3027375 NM M/R CENTERING WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 168 0206040431 90000012 M/R CENTERING BEARING ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. DEBONDING. REPLACED WITH NEW UNIT, CORRECTED PROBLE M. 1 G 7 2 3U NC H19NM 1997022000064 19970220 00064 NM 1997 2 20 97ZZZX727 1 19961206 A 5210 51237 DOOR LATCH DOUG MD900 MD900 3027375 NM COCKPIT DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 90000012 DOOR LATCH DEFECT. (SB900-040.) REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997022000065 19970220 00065 NM 1997 2 20 97ZZZX728 1 19961206 A 5210 51238 DOOR LATCH DOUG MD900 MD900 3027375 NM COCKPIT DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 90000012 DOOR LATCH DEFECT. (SB 900-040). REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997022000066 19970220 00066 NM 1997 2 20 97ZZZX729 1 19961020 A 3213 900F2361105103 ABRASION STRIP DOUG MD900 MD900 3027375 NM SKID TUBE LT FWD WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 988 90000012 SKID ABRASION STRIP WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997022000067 19970220 00067 NM 1997 2 20 97ZZZX730 1 19961020 A 3213 900F2361105104 ABRASION STRIP DOUG MD900 MD900 3027375 NM SKID TUBE RT FWD WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 90000012 SKID ABRASION STRIP WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997022000068 19970220 00068 NM 1997 2 20 97ZZZX731 1 19961215 A 6230 900C1010004125 SWASHPLATE DOUG MD900 MD900 3027375 NM SPLIT LINE MISALIGNED A R7MA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 11 901CF 90000012 SWASHPLATE RECEIVED FROM MDHS WITH IMPROPER SPLIT LINE ALIGNMENT. SWASHPLATE SHOULD HAVE BEEN ALIGNED WITH THE AIRCRAFT CENTERLINE PER SB 900-032, BUT INSTEAD, THE TECHNICIAN ALIGNED THE SWASHPLATE WITH THE LATERIAL PITCH EAR IN ERROR. RM H PERSONNEL CORRECTED THE ALIGNMENT AND INSTALLED THE SWASHPLATE. 1 G 7 2 3U NC H19NM 1997022000069 19970220 00069 1997 2 20 97ZZZX732 4 19961224 A 3160 900A3720002107 DISPLAY SYS DOUG MD900 MD900 3027375 NM COCKPIT LIGHTS FLUCTUATE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 50 50 008251001 90000012 DISPLAY DIMMER AND LIGHTS FLUCTUATE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997022000070 19970220 00070 NM 1997 2 20 97ZZZX733 1 19961015 A 6720 16549011 ACTUATOR DOUG MD900 MD900 3027375 NM DAMPNER VSCS FAULTY A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 988 0089831014 90000012 DAMPNER ACTUATOR FAILED BREAKAWAY TORQUE TOLERANCE INSPECTION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997022000071 19970220 00071 NM 1997 2 20 97ZZZX734 1 19961015 A 6720 16549011 ACTUATOR DOUG MD900 MD900 3027375 NM DAMPNER VSCS DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 008931016 90000012 DAMPNER ACTUATOR INSPECT FOR BREAKAWAY TORQUE TOLERANCE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997022000072 19970220 00072 NM 1997 2 20 97ZZZX735 1 19961005 A 5302 900F2318401103 BUMPER DOUG MD900 MD900 3027375 NM TAILBOOM BENT A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 953 90000012 TAILBOOM BUMPER BENT BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997022000073 19970220 00073 NM 1997 2 20 97ZZZX736 1 19961023 A 5210 900F3305187102 DOOR LATCH DOUG MD900 MD900 3027375 NM COCKPIT DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 989 90000012 DOOR LATCH DEFECT. COCKPIT FWD (SL 900-011.) REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997022000074 19970220 00074 NM 1997 2 20 97ZZZX737 1 19961001 A 3213 900F2361106101 ABRASION STRIP DOUG MD900 MD900 3027375 NM SKID TUBE AFT WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 90000012 SKID ABRASION STRIP WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997022000078 19970220 00078 NM 1997 2 20 97ZZZX741 1 19961224 A 5315 65468111 FLOORBEAM BOEING 737 737247 138448D NM STA 986.5 CORRODED A A6XA K NONE O OTHER IN INSP/MAINT 1 SO 13 4515W 40897 19612 FLOORBEAM AT STATION 986.5 LBL 29 HAS CORROSION AT THE NUTPLATE HOLES 5 SQUARE INCHES TOTAL. MAINT BY USAIR RPR STA. 2 L 7 2 4F A16WE 1997022000079 19970220 00079 NM 1997 2 20 97ZZZX742 1 19961224 A 5320 65465941 CHANNEL BOEING 737 737247 138448D NM FS 500B BENT A A6XA K NONE O OTHER IN INSP/MAINT 1 SO 13 4515W 40897 19612 FUSELAGE CHANNEL AT STA 500B AT STRINGER 20R IS BENT OUT OF LIMITS. MAINT BY USAIR RPR STA. 2 L 7 2 4F A16WE 1997022000080 19970220 00080 NM 1997 2 20 97ZZZX743 1 19961224 A 5311 65465661 FRAME BOEING 737 737247 138448D NM FS 987 CRACKED A A6XA K NONE O OTHER IN INSP/MAINT 1 SO 13 4515W 40897 19612 FUSELAGE FRAME AT STATION 987 HAS A 4 INCH CRACK BETWEEN STRINGERS 20L AND 21L. MAINT BY USAIR RPR STA. 2 L 7 2 4F A16WE 1997022000081 19970220 00081 NM 1997 2 20 97ZZZX744 1 19961224 A 5311 65465661 FRAME BOEING 737 737247 138448D NM FS 767 CRACKED A A6XA K NONE O OTHER IN INSP/MAINT 1 SO 13 4515W 40897 19612 FUSELAGE FRAME AT STATION 767 HAS A .50 INCH CRACK ABOVE STRINGER 25R. MAINT BY USAIR RPR STA. 2 L 7 2 4F A16WE 1997022000082 19970220 00082 NM 1997 2 20 97ZZZX745 1 19961224 A 5313 BAC149896 STRINGER BOEING 737 737247 138448D NM FS 500 CRACKED A A6XA K NONE O OTHER IN INSP/MAINT 1 SO 13 4515W 40897 19612 FUSELAGE STRINGER 25L HAS 2 EACH 1 INCH LONG CRACKS AT STATION 500. MAINT BY USAIR RPR STA. 2 L 7 2 4F A16WE 1997022000083 19970220 00083 NM 1997 2 20 97ZZZX746 1 19961224 A 5311 65465931 FRAME BOEING 737 737247 138448D NM FS 500A CRACKED A A6XA K NONE O OTHER IN INSP/MAINT 1 SO 13 4515W 40897 19612 FUSELAGE FRAME AT STATION 500A HAS A 2 INCH CRACK AT BL ZERO. MAINT BY USAIR RPR STA. 2 L 7 2 4F A16WE 1997022000084 19970220 00084 NM 1997 2 20 97ZZZX747 1 19961224 A 5311 65465331 FRAME BOEING 737 737247 138448D NM FS 500B CRACKED A A6XA K NONE O OTHER IN INSP/MAINT 1 SO 13 4515W 40897 19612 FUSELAGE FRAME AT STATION 500 HAS A 1 INCH CRACK AT BL ZERO. MAINT BY USAIR RPR STA. 2 L 7 2 4F A16WE 1997022000085 19970220 00085 NM 1997 2 20 97ZZZX748 1 19961224 A 5311 65465931 RIB BOEING 737 737247 138448D NM FS 500 CRACKED A A6XA K NONE O OTHER IN INSP/MAINT 1 SO 13 4515W 40897 19612 FUSELAGE RIB AT STATION 500A HAS TWO .5 INCH CRACKS BETWEEN STRINGERS 20L AND 21L. MAINT BY USAIR RPR STA. 2 L 7 2 4F A16WE 1997022000086 19970220 00086 NM 1997 2 20 97ZZZX749 1 19961224 A 5311 65465941 FRAME BOEING 737 737247 138448D NM BS 500B GOUGED A A6XA K NONE O OTHER IN INSP/MAINT 1 SO 13 4515W 40897 19612 FRAME AT STATION 500B HAS GOUGES AROUND THE ANCHOR NUT AT STRINGER 20L. MAINT BY USAIR RPR STA. 2 L 7 2 4F A16WE 1997022000087 19970220 00087 NM 1997 2 20 97ZZZX750 1 19961023 A 5210 900F3305187101 DOOR LATCH DOUG MD900 MD900 3027375 NM COCKPIT DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 989 90000012 DOOR LATCH DEFECT. COCKPIT FWD (SL 900-011.) REPLACED WITH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997022000088 19970220 00088 EU 1997 2 20 CA960924013 1 19960911 A 3231 836804 TARGET AIRBUS 320 A320211 3930320 EU MLG UPLOCK BROKEN W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) ON TAKEOFF, LEFT MAIN LANDING GEAR DOOR INDICATED NOT CLOSED ON ECAM. SUBSEQUENT MAINTENANCE CHECK REVEALED SHIM P /N 201061607 WAS MISSING AND TARGET BROKEN. MAIN LANDING GEAR UPLOCK REPLACED. 2 L 7 2 4F RT A28NM 1997022000089 19970220 00089 EA 1997 2 20 CA960924020 1 19960823 A 2435 230321910 BACK PLATE LEARSIEGLER 23048004 DHAV DHC6 DHC6100 EA PWA PT6 PT6A20 52043 EA START/ GEN WORN OUT W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 2928 PCE22330 (CAN) DURING OVERHAUL A PIECE OF BRASS WAS NOTED PROTRUDING BETWEEN THE BACK PLATE AND THE ARMATURE SHAFT. BRASS TURNED OUT TO BE A BRASS SHIM. INSERTED BETWEEN THE ARMATURE AND THE BACK PLATE SEAT. BACK PLATE FOUND WORN WELL BEYOND TOLERAN CES AND THE BRASS HAD BEEN USED TO TAKE UP THE EXTRA PLAY. AS A RESULT THE DAMPER BACK PLATE AND FRICTION DISK WERE ALLO WED TO WOBBLE ON THE ARMATURE SHAFT. UNIT ALSO CONTAINED PMA PARTS. 1 H 7 2 3T 3 T A9EA E4EA 1997022000091 19970220 00091 SW 1997 2 20 CA960924022 1 19960916 A 6410 2060162021131 BLADE BELL 206 206L4 1182110 SW ALLSN 250C 250C30P 03013 GL T/R SEPARATION W K NONE O OTHER IN INSP/MAINT 1 CA 699 CAE895715 (CAN) SKIN SEPARATION FROM LEADING EDGE OF BOTH BLADES. 1 G 7 1 3U 3 U NC H2SW E1GL 1997022000092 19970220 00092 EA 1997 2 20 CA960924025 2 19960905 A 7414 S4LN204 MAGNETO BEECH 95 D95A 1153408 CE LYC O360 IO360B1B 41514 EA #2 ENGINE SHAFT SHEARED W A K NONE O OTHER IN INSP/MAINT 1 CA 1004 1038458 L389151A (CAN) THE RIGHT ENGINE WOULD NOT START. INSPECTION REVEALED THE #2 ENGINE LEFT HAND MAGNETO HAD SEPARATED FROM THE CASE BREAKING THE MAG CASTING AT THE MOUNTING FLANGES & THE MAGNETO SHAFT WAS BENT. FURTHER INVESTIGATION FOUND THE FUEL PUMP , CAMSHAFT, VACUUM PUMP & LEFT HAND MAGNETO WERE NOT TURNING. THE ENGINE WAS REPLACED & THE AIRCRAFT RETURNED TO SERVICE . SUBSEQUENT INSPECTION REVEALED THE CRANKSHAFT IDLER GEAR HAD SHEARED WHICH DRIVES THE L/H MAG, FUEL PUMP, VACUUM PUMP, TACH DRIVE & CAMSHAFT WAS MISSING TWO TEETH THUS THE GEAR WAS NOT ENGAGED. INSPECTION OF THE MAG REVEALED THE SHAFT HAD SHEARED ALLOWING THE MAGNETO TO JAM THE HOUSING CAUSING THE DAMAGE TO THE CRANKSHAFT IDLER GEAR. 1 L 7 2 3O 3 O 3A16 1E10 1997022000093 19970220 00093 NE 1997 2 20 CA960924030 2 19960914 A 8530 234221 PISTON PIN PWA DHAV DHC2 DHC2MK1 2800102 EA PWA R985 R985AN14B 52008 NE NR 2 CYLINDER SHEARED W A A UNSCHED LANDING E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CR CRUISE 1 CA 700 19458 (CAN) PILOT HEARD BANG BUT ENGINE CONTINUED TO PERFORM NORMALLY. APPROXIMATELY 2 MINUTES LATER THE ENGINE BEGAN TO SHAKE VIOLENTLY WITH NOTICEABLE POWER LOSS. AIRCRAFT LANDED AND ENGINE WAS SHUTDOWN. POST FLIGHT INSPECTION FOUND #2 CYLINDER PISTON PIN BROKEN, PISTON PIN BOSSES BROKEN OFF BOTH SIDES, SEVERAL SECTIONS OF THE PISTON BROKE AT THE BOTTOM. 1 H 7 1 3R 3 R A806 5E1 1997022000094 19970220 00094 SW 1997 2 20 CA960924032 1 19960502 A 3213 206031302269 CROSSTUBE BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL AFT SUPPORT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 8568 CAE833907 (CAN) DURING ANNUAL INSPECTION AFT CROSSTUBE SUPPORT STRUCTURE FOUND CRACKED AND CORRODED. 1 G 7 1 3U 3 U H2SW E4CE 1997022000096 19970220 00096 SW 1997 2 20 CA960924035 1 19960731 A 2840 7G547 SWITCH BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL FUEL PRESS INOPERATIVE W K NONE O OTHER IN INSP/MAINT 1 CA CAE800419BA (CAN) WITH PRESSURE FROM BOOST PUMP ON, SWITCH WOULD NOT OPEN CIRCUIT AND PANEL LIGHT WOULD STAY ON. 1 G 7 1 3U 3 U H2SW E4CE 1997022000097 19970220 00097 EU 1997 2 20 CA960924038 1 19960830 A 6310 350A103021 BOLT SNIAS 350 AS350B2 8680813 EU OUTPUT FLANGE LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA 469 (CAN) DURING THE 100 HOUR INSPECTION THE BOLT HOLDING THE ENGINE TO THE TAIL ROTOR DRIVE FLANGE HAD LOOSENED OFF AND THE FLANGE HAD MOVED AFT AND RUBBED AGAINST THE FIBREGLASS FIREWALL AND BRACKETS. THIS WAS FOUND AGAIN ON THE 500 HOUR. EUR OCOPTER HAVE SINCE ISSUED AN ALERT SERVICE INFORMATION LETTER REGARDING THIS PROBLEM. 1 G 7 1 3U H9EU 1997022000098 19970220 00098 SW 1997 2 20 CA960924039 1 19960916 A 6320 212040001059 TRANSMISSION BELL 212 212 1181420 SW PWA PT6T PT6T3B 52045 NE LIFT LINK CRACKED W K NONE O K OTHER FLUID LOSS IN INSP/MAINT 1 CA 11457 4630 CPPS62436 (CAN) INSPECTION OF TRANSMISSION REVEALED A CRACK AT THE LIFT LINK FITTING ATTACHMENT. ALSO APPEARS AS IF THE GEARBOX WA S WEEPING OIL FROM CRACK. 1 G 7 1 4U 4 U H4SW E22EA 1997022000102 19970220 00102 WP 1997 2 20 CA960925002 1 19960920 A 6320 369D25146 BEARING HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL M/R GR BOX CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA CAE830895 (CAN) INVESTIGATION REVEALED THAT THE BEARING P/N 369D25146 HAD A LONGITUDINAL CRACK ENTIRELY THROUGH THE INNER RACE. TH E BEARING INNER RACE IS MOUNTED ON A PINION P/N 369D25125-13. THE RETAINING RING P/N RSN-118 CAME OFF ALLOWING THE INNER RACE TO MOVE PARTIALLY OFF THE PINION THUS CONTACTING THE BACK OF THE BEARING HOUSING AND MILLING ITS WAY INTO THE TOP CASE. 1 G 7 1 3U 3 U H3WE E4CE 1997022000103 19970220 00103 WP 1997 2 20 CA960925003 1 19960831 A 6210 369D21100505M BLADE HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL ABRASION STRIP DELAMINATION W K NONE O OTHER IN INSP/MAINT 1 CA 2778 CAE830588 (CAN) 7"X14" DELAMINATION OF ABRASION STRIP ON UPPER SURFACE OF MAIN ROTOR BLADE. 1 G 7 1 3U 3 U H3WE E4CE 1997022000104 19970220 00104 NM 1997 2 20 CA960925004 1 19960825 A 2432 23180 BATTERY MARATHON 23180 BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE ACFT MAIN DC OVERHEAT W O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA 3134 1445 9402056 674646 (CAN) APU START UP MAIN AIRCRAFT BATTERY OVERTEMP/THERMAL RUNAWAY. SMOKE IN PASSENGER CABIN. CFR CALLED. REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1997022000105 19970220 00105 1997 2 20 CA960925005 4 19960913 A 3421 7725005005 GYRO BOEING 737 7372T7 NM PWA JT8 JT8D17 52049 NE FO VG JAMMING W A UNSCHED LANDING I FLT. ATTITUDE INST. CL CLIMB 1 CA 708808 (CAN) F/OS A.D.I. HORIZON CARD KEEPS JAMMING. VG CHANGED AND RESET OF C/B HAD NO EFFECT. F/OS A.D.I. AND GYRO REPLACED. #2 VG TRANSFER RELAY REPLACED AS PER MAINTENANCE REQUEST. 2 L 7 2 4F 4 F RT A16WE E2EA 1997022000106 19970220 00106 NE 1997 2 20 CA960925006 2 19960822 A 7311 320115 VALVE WHITTAKER 320115 BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE NR 1 ANTI ICE STICKING W A UNSCHED LANDING M OVER TEMP CL CLIMB 1 CA 23621 4155 646M 674513 (CAN) ON CLIMB #1 ENGINE OIL TEMPERATURE INCREASED TO 126 DEGREES CELSIUS. BY INCREASING POWER TO MAX CONTINUOUS IT CAME TO 120 DEGREES CELSIUS. DURING DESCENT FUEL FLOW AT 7500 PPH TEMPERATURE REMAINED AT 120 DEGREES CELSIUS. OIL TEMPERATU RE BULB AND PLUG CHECKED AND CLEANED. #1 FUEL VALVE REPLACED. SUSPECT ANTI-ICE VALVE. REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1997022000108 19970220 00108 EU 1997 2 20 CA960927003 1 19960906 A 2435 1260 DRIVE SHAFT LUCAS BC0908 STBROS SD3 SD330 8100602 EU PWA PT6 PT6A45R 52043 EA START/GEN SHEARED W K NONE H J ELECT. POWER LOSS-50 PC WARNING INDICATION AP APPROACH 1 CA 1260 PCE84133 (CAN) ON APPROACH A GENERATOR FAULT WARNING WAS NOTED COULD NOT RESET. AFTER LANDING CREW TRIED TO MOTOR ENGINE BUT WO ULD NOT START. STARTER GENERATOR FOUND SEVERELY OVERHEATED AND SOME SMOKE AND HEAT DAMAGE FOUND. DRIVE SHAFT HAD SHEARE D. 2 H 7 2 4T 4 T A41EU E4EA 1997022000109 19970220 00109 NE 1997 2 20 CA961011005 2 19961002 A 7200 ENGINE DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE #1 POSITION POWER LOSS W C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CA 9123 123039 (CAN) DURING TAKEOFF #1 ENGINE ROLLED BACK APPROXIMATELY 30 PERCENT. THE PROBLEM COULD NOT BE DUPLICATED ON RUN-UP. THE PRATT & WHITNEY ENGINE HARNESS, MFC AND ECU WERE REPLACED AFTER THE ROLL BACK. AN INVESTIGATION BY PRATT & WHITNEY HAS B EEN REQUESTED. 2 H 7 2 4T 4 T RT A13NM E20NE 1997022000110 19970220 00110 NE 1997 2 20 CA961018013 2 19961002 A 7200 ENGINE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE NR 1 POSITION FAILED W E ENGINE SHUTDOWN K FLUID LOSS NR NOT REPORTED 1 CA P657413D (CAN) INFLIGHT SHUTDOWN OF #1 ENGINE DUE TO TOTAL LOSS OF OIL QUANTITY. POST FLIGHT INSPECTION FOUND NO OIL IN #1 ENGINE RESERVOIR. FOUND OIL COMING FROM TURBINE EXHAUST. #1 ENGINE REPLACED. 2 L 7 2 4F 4 F A6WE E2EA 1997022000111 19970220 00111 EA 1997 2 20 CA961104017 1 19961028 A 5610 601R330332 WINDSHIELD PPG CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE RIGHT HAND SHATTERED W B EMER. DESCENT O OTHER CR CRUISE 1 CA 4882 0 807157 (CAN) AT 350 FLIGHT LEVEL IN CRUISE, THE FIRST OFFICERS FRONT WINDSHIELD SHATTERED. AIRCRAFT DESCENDED TO REDUCE DIFFERE NTIAL CABIN PRESSURE. 2 L 7 2 4F 4 F RT A21EA E15NE 1997022000112 19970220 00112 GL 1997 2 20 CA961112006 2 19961029 A 7323 6875630 RIGID LINE BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL GOVERNOR FITTING BROKEN W A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 CA 10000 CAE822151 (CAN) THE PILOT WAS AT LOW ALTITUDE WHEN THE ENGINE FLAMED OUT. HELICOPTER WAS SUBSTANTIALLY DAMAGED. INVESTIGATION FOUN D RIGID LINE BROKE OFF THE END OF FERRULE ON LINE CAUSING THE N1 TO COME DOWN TO 35 PERCENT N1. RIGID LINE SENT FOR TEST ING BUT SUBMITTER SUGGESTS POSSIBLE CAUSE TO BE INCORRECT CLAMPING AS PER ALLISON IPC. 1 G 7 1 3U 3 U H2SW E4CE 1997022000113 19970220 00113 SW 1997 2 20 CA961115001 1 19961107 A 3297 WIRE SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE3313 01514 WP LANDING GEAR SHORTED W D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CA 25559 P54214 (CAN) SHORTLY AFTER TOUCHDOWN, ALL THREE GEAR COLLAPSED. THREE AREAS BEING CHECKED. 1) GEAR SELECTOR VALVE FAILURE; 2) G EAR SELECTOR WIRING FAILURE. 3) GEAR SELECTOR FAILURE. OPERATOR CONFIDENT THAT GEAR WAS SELECTED DOWN AS EVIDENCED BY NI L DAMAGE TO THE GEAR ACTUATORS. LH GEAR FOUND IN UP AND LOCKED POSITION, THUS OPERATOR BELIEVES THAT HYDRAULIC POWER WAS APPLIED TO DRIVE THE GEAR UP DESPITE THE GEAR BEING SELECTED DOWN. IT IS POSSIBLE THAT THE DOWN POWER WIRE SHORTED TO T HE UP POWER WIRE RESULTING IN UN-COMMANDED GEAR UP SELECTION. 2 L 7 2 4T 4 T RT A8SW E4WE 1997022000114 19970220 00114 1997 2 20 CA961115003 4 19960914 A 3418 P004 STALL WARNING DIAMON DA20A1 DA20A1 05626UX GL UNDER PILOT SEAT CONTAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) WATER FOUND IN STALL WARNING TUBING UNDER THE PILOTS SEAT. WATRE FOUND TO BE BLOCKING THE SYSTEM FROM OPERATING PR OPERLY. 1 L 7 1 3O NT TA4CH 1997022000115 19970220 00115 1997 2 20 CA961115004 4 19961003 A 3418 P004 STALL WARNING DIAMON DA20A1 DA20A1 05626UX GL UNDER PILOT SEAT CONTAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) WATER FOUND IN STALL WARNING TUBE UNDER THE PILOT SEAT. 1 L 7 1 3O NT TA4CH 1997022000116 19970220 00116 1997 2 20 CA961115008 4 19961106 A 3418 P004 STALL WARNING DIAMON DA20A1 DA20A1 05626UX GL UNDER PILOT SEAT CONTAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) WATER FOUND IN STALL WARNING SYSTEM TUBING UNDER THE PILOTS SEAT. WATER BLOCKED TUBE. 1 L 7 1 3O NT TA4CH 1997022000117 19970220 00117 1997 2 20 CA961115011 4 19961109 A 3418 P004 STALL WARNING DIAMON DA20A1 DA20A1 05626UX GL UNDER PILOT SEAT CONTAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) WATER FOUND IN TUBING UNDER THE PILOTS SEAT AND FORMED A BLOCK. 1 L 7 1 3O NT TA4CH 1997022000118 19970220 00118 1997 2 20 CA961118005 4 19961113 A 3418 P004 STALL WARNING DIAMON DA20A1 DA20A1 05626UX GL UNDER PILOT SEAT CONTAMINATED W A UNSCHED LANDING O OTHER CR CRUISE 1 CA (CAN) NO STALL INDICATION. WATER FOUND IN THE STALL WARNING TUBE UNDER THE PILOTS SEAT WHICH IS THE LOWEST POINT IN THE SYSTEM. 1 L 7 1 3O NT TA4CH 1997022000119 19970220 00119 NM 1997 2 20 CA961120003 1 19961111 A 3320 BA080061 BALLAST BRUCE DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE CABIN BURNT W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA 6590 123046 (CAN) BURNING SMELL NOTED AT REAR OF CABIN. LIGHT BALLAST SMELLED BURNT ON INSIDE OF BALLAST. 2 H 7 2 4T 4 T RT A13NM E20NE 1997022000120 19970220 00120 SW 1997 2 20 CA961126005 1 19961126 A 3260 1EN516 SWITCH SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP DOWN AND LOCKED INTERMITTENT W K NONE O OTHER IN INSP/MAINT 1 CA P54082 (CAN) REFERENCE SB 226-32-025, ACCOMPLISHED IN JULY 1995. AN UPGRADE TO A 'MORE RELIABLE SWITCH'. AFTER UPGRADE OPERATOR HAD PROBLEMS WITH ONGOING GEAR INDICATION PROBLEMS. EVERYTHING CHECKED. SWITCHES REMOVED AND TESTED. INTERNAL RESISTANC E FOUND TO VARY FROM 25 TO 1000 OHMS. IF SWITCH COOLED TO 0 DEGREE CELSIUS THE SWITCH FAILED MORE OFTEN WITH NEAR INFINI TE RESISTANCE. ON SOME OCCASIONS RESISTANCE WOULD SLOWLY DECREASE WITH CONTINUITY BEING ESTABLISHED AFTER SEVERAL SECOND S. SWITCHES REPLACED. 2 L 7 2 4T 4 T RT A8SW E4WE 1997022000121 19970220 00121 NM 1997 2 20 CA961128007 1 19961123 A 2770 NAS130431 BOLT DHAV DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE GUST LOCK CORRODED W K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 CA 21290 0 120657 (CAN) ON REMOVAL OF THE BOLT THAT HOLDS THE RUBBER BUMPERS ON THE GUST LOCK ASSEMBLY, THE BOLT WAS FOUND CORRODED ALMOST 1/2 WAY THROUGH. FAILURE OF THIS BOLT CAN CAUSE THE SPRINGLOADED PLUNGER TO EXTEND OUTWARDS LOCKING UP THE ELEVATOR AS WAS THE CASE WHEN THIS BOLT WAS REMOVED. THE ASSEMBLY, IS CONSTRUCTED IN SUCH A WAY THAT WATER SITS IN THE RECESS FOR TH E BOLT THEREBY CAUSING THE CORROSION. THRE ARE NO INSPECTION TASKS TO COVER THIS ITEM. REF. IPC 55-20-00 FIG. 35, ITEM 6 0. 2 H 7 2 4T 4 T RT A13NM E20NE 1997022000122 19970220 00122 EU 1997 2 20 CA961205013 1 19961125 A 2612 FIRE WARN SYS AIRBUS 320 A320211 3930320 EU CABIN WARNING W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA (CAN) CREW REPORTED SMOKE IN CABIN. AREAS OF AIRCRAFT INSPECTED AND FOUND NO EVIDENCE RELATED TO THE WARNING. AIRCRAFT R ETURNED TO DEPARTURE BASE. 2 L 7 2 4F RT A28NM 1997022000123 19970220 00123 EA 1997 2 20 CA961216008 1 19961031 A 5343 85411782003 FITTING DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE ACTUATOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 4605 123125 (CAN) BOTH LANDING GEAR ACTUATOR SUPPORT FITTINGS FOUND CRACKED. BOTH FITTINGS ARE POST-MOD 8/1830 AND 8/2049 IN ACCORDA NCE WITH BRAD SB 8-54-27 AND 8-54-34 RESPECTIVELY AS MANDATED BY AIRWORTHINESS DIRECTIVE CF-91-25. CRACKS FOUND IN SAME AREA AS PER THE PRE-AD CRACKING. CRACKS WERE ONLY DETECTED BY MAGNETIC PARTICLE INSPECTION WHICH WAS CARRIED OUT ONLY AS A PRECAUTION. IT HAS BEEN NOTED THAT A NEW FITTING OF IMPROVED MANUFACTURE PER MOD 8/2075 IS AVAILABLE, ALTHOUGH IT IS NOT BEING INTRODUCED IN THE FIELD PER THE SB. 2 H 7 2 4T 4 T RT A13NM E20NE 1997022000154 19970220 00154 NE 1997 2 20 97ZZZX781 2 19961129 A 7261 5004T01P01 OIL TUBE LEAR 25 25D 5170514 CE GE CJ610 CJ6106 30006 NE FRONT FRAME CRACKED A A JKIA K NONE O OTHER IN INSP/MAINT 1 SO 17 99NJ 16414 4918 220 251194A A SMALL HAIRLINE CRACK AT THE SWEDGED 90 DEGREE ELBOW WHERE IT ATTACHES TO THE FRONT FRAME OIL FITTING. OIL PRESSURE FL UCTUATION OCCURRED DURING 2ND LEG OF A SCHEDULED TRIP. 2 L 7 2 4J 4 J A10CE 1E16 1997022000203 19970220 00203 WP 1997 2 20 9627909869 1 19961216 A 5350 LATCH MECHANISM DOUG DC9 DC951 3022051 WP TAILCONE OUT OF ADJUST A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 778NC 48100 DURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE TAILCONE. RIGGED TAILCONE LATCHING MECHANISM. 2 L 7 2 4F RT A6WE 1997022000204 19970220 00204 WP 1997 2 20 9627919981 1 19961219 A 5350 RELEASE MECH DOUG DC9 DC931 3022065 WP TAILCONE MALFUNCTIONED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 994Z 47097 DURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE TAILCONE. ADJUSTED TAILCONE RELEASE MECHANISM, F UNCTIONAL TEST OK. 2 L 7 2 4F A6WE 1997022000205 19970220 00205 WP 1997 2 20 9627929873 1 19961217 A 5350 PIN PLATES DOUG DC9 DC951 3022051 WP TAILECONE WORN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 782NC 48107 DURING LINE CHECK, FOUND INADEQUATE FORCE WAS REQUIRED TO PULL THE EXTERIOR TAILCONE HANDLE FROM THE CLIPS. ALSO, FOUND EIGHT TAILCONE GUIDE PINS WORN, UPPER LEFT LATCH WORN AND TWO ALIGNMENT PIN PLATES WORN. REPLACED CLIPS, GUIDE PINS, L ATCH AND PIN PLATES. 2 L 7 2 4F RT A6WE 1997022000263 19970220 00263 NE 1997 2 20 96UAL900952 2 19961219 A 7230 6A3322 LEVER ARM 6A3322 AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ENGINE FAILED A A UALA E ENGINE SHUTDOWN E VIBRATION/BUFFET CL CLIMB 1 WP 29 424UA 6742 506 ON CLIMBOUT PASSING APPROXIMATELY 6,000 FEET A LOUD BANG WAS HEARD AND THE NR 2 ENGINE ROLLED BACK. ALL INDICATIONS LOO KED GOOD FOR A RELIGHT. WHEN RELIGHT WAS ATTEMPTED VIBRATION WAS HIGH AND THE RESTART WAS ABORTED. *S/D* 3 HIGH PRESS URE COMPRESSOR VARIABLE STATOR LEVER ARMS IN THE THIRD STAGE WERE FOUND BROKEN AT THE 3 O'CLOCK LOCATION ALLOWING INDIVI DUAL VANES TO OBSTRUCT THE AIRFLOW THROUGH THE COMPRESSOR CAUSING SEVERE STAGE 4 BLADE FAILURES. THE LEVER ARM FAILURE IS STILL UNDER INVESTIGATION BY UAL AND THE MANUFACTURER. 2 L 7 2 4F 4 F RT A28NM E40NE 1997022000308 19970220 00308 NE 1997 2 20 GLBA96238 2 19961208 A 7530 19357222 PACKINGS BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT BLEED LINE DETERIORATED A GLBA O OTHER O OTHER CR CRUISE 1 CE 01 210UX UE210 DEN - RIGHT BLEED AIR FAIL INFLIGHT. MAINTENANCE REPAIRED EVA TUBING AND REPLACED O-RINGS IN RIGHT BLEED AIR LINE. OPE RATES NORMALLY ON GROUND. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 1997022000309 19970220 00309 SO 1997 2 20 GLBA96237 1 19961208 A 3234 GEAR HANDLE EMB 120 EMB120RT SO COCKPIT FAILED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 129AM 120119 FSD - GEAR WOULD NOT COME UP. MAINTENANCE REMOVED AND REPLACED GEAR HANDLE. OPERATIONAL CHECKS GOOD. (M) 2 L 7 2 4T RT A31SO 1997022000310 19970220 00310 1997 2 20 GLBA96236 4 19961208 A 3431 RECEIVER BEECH 1900 1900C 1154161 CE NR 1 NAV INOPERATIVE A GLBA K NONE O OTHER IN INSP/MAINT 1 CE 01 145GL UC145 PHX - NR 1 NAV INOP. MAINTENANCE SWAPPED NAV CONTROL HEADS FOR TROUBLESHOOTING. FLAGS PULLED AND OPS CHECKS GOOD. (M) 2 L 7 2 4T RT A24CE 1997022000311 19970220 00311 CE 1997 2 20 GLBA96231 1 19961205 A 2121 1143800281 VENT BLOWER BEECH 1900 1900C 1154161 CE CABIN OVERHEATED A GLBA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 01 130UE 10500 10500 82 UC130 FLO - WHITE SMOKE FILLED COCKPIT AND CABIN. TURNED OFF ENVIRONMENTAL VALVES. MAINTENANCE FOUND AFT VENT BLOWER INOPERA TIVE. RAN AIRCRAFT WITH BLEEDS OPEN AND COULD NOT DUPLICATE AT THIS TIME. MEL'D BLOWERS AND LATER REPLACED AFT VENT BL OWER. (M) 2 L 7 2 4T RT A24CE 1997022000346 19970220 00346 EU 1997 2 20 RAIA970108 1 19961206 A 7712 310703411 TORQUE RING BAG JETSTM JETSTM3201 1500217 EU NR 2 ENGINE BAD BRIDGE A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 422AM 10416 856 CGI - FLT 7393 - NR 2 ENGINE INDICATES ZERO TORQUE. SWITCHED BRIDGES ON TORQUE RING. (M) 2 L 7 2 4T RT A56EU 1997022000351 19970220 00351 EU 1997 2 20 RAIA961280 1 19961221 A 7722 CA3108R12S3F80 CONNECTOR BAG JETSTM JETSTM3201 1500217 EU NR 2 ENGINE LOOSE A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 875JX 10497 875 FAT - FLT 4734 - RIGHT SRL CAPTION LIGHT CAME ON. MAINTENANCE RESECURED T2 SENSOR CANNON PLUG. (M) 2 L 7 2 4T RT A56EU 1997022000352 19970220 00352 EU 1997 2 20 RAIA961284 1 19961230 A 7332 1103P0645 PRESSURE SWITCH BAG JETSTM JETSTM3201 1500217 EU LT ENGINE INOP A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 871JX 11123 871 SBA - FLT 4703 - LEFT FUEL LOW PRESSURE CAP LIGHT ILLUMINATED ON TAKEOFF ROLL. FUEL PRESSURE INDICATOR INDICATES PRESSU RE NORMAL. REMOVED AND REPLACED FUEL LOW PRESSURE SWITCH. (M) 2 L 7 2 4T RT A56EU 1997022000361 19970220 00361 1997 2 20 97ZZZM225 4 19961228 A 2210 AUTO PILOT DOUG DC9 DC932 3022066 WP E/E COMPT MALFUNCTIONED A GTIA O OTHER F FLT CONT AFFECTED CL CLIMB 1 GL 23 942ML 47478 ACY - FLT 256 - DURING CLIMB CONFIGURATION THE AUTO PILOT DIS-ENGAGED EXPERIENCED A VERY BRISK PITCH DOWN CONDITION. MA INTENANCE COULD NOT DUPLICATE MALFUNCTION. RAN FULL SYSTEM SELF TEST, FOR HALF HOUR OPERATIONAL CHECKS GOOD IAW DC-9 MM , CHAPTER 22-10-01. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1997022000396 19970220 00396 WP 1997 2 20 VJ970023 1 19960103 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 996 EXFOLIATED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THAT STRINGER NR 29 LEFT END FITTING STATION 996 WAS EXF OLIATED BEYOND LIMITS. REMOVED STRINGER 29 END CAP IAW DC9 SRM 53-11-3, INSTALLED NEW END CAP IAW DC-9 SRM 53-11-3 AND 51-30-1 INSTALLED BOOMERANG PANEL IAW DC-9 SRM 51-30-1. (M) 2 L 7 2 4F A6WE 1997022000461 19970220 00461 1997 2 20 TWRA96360 4 19961119 A 2565 14070101L SLIDE BFGOODRICH BOEING 747 747121 1384871 NM 4L DOOR FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 609FF 654 20354 DURING TRAINING TEST, 4L MAIN ENTRY DOOR SLIDE FAILED TO DEPLOY CORRECTLY DUE TO ASPIRATOR HOSE 'B' FITTING FAILURE, SLI DE P/N D30440105 S/N 0817. REMOVED AND REPLACED 4L MAIN ENTRY DOOR SLIDE PER MM 25-69-00. OPS CHECK NORMAL. (M) 2 L 7 4 4F A20WE 1997022000494 19970220 00494 NM 1997 2 20 97ZZZX807 1 19960525 A 5500 900F3341237101 BEARING DOUG MD900 MD900 3027375 NM EMPENNAGE WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 55 90000012 BEARING JOURNAL WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 4 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997022000701 19970220 00701 NM 1997 2 20 LR00696 1 19961229 A 2910 BACH8A04NN0264T HOSE ASSY BOEING 737 7372L9 1384497 NM MLG WW DAMAGED A SOKF O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SO 23 281LF 22701 BAQ/SJO - FLT 610 - HYDRAULIC SYSTEM 'A' HAD A TOTAL LOSS OF HYDRAULIC OIL DUE TO FLEX HOSE ASSY, P/N BACH8A04NN0264T, S PRUNG LEAK AT WHEELWELL AND CREW DECLARED EMERGENCY LANDING. AIRCRAFT LANDED WITH NO INCIDENTS AT SJO. HOSE WAS REPLAC ED AND TEST WAS ACCOMPLISHED PER MM-29-10-29 SERVICE SYSTEM PER 20-10-52. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1997022000702 19970220 00702 NM 1997 2 20 PCAA9600331 1 19961214 A 2910 82970010477 HYD LINE DHAV DHC8 DHC8102 2809003 NM NR 2 HYD SYST FAILED A PCAA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 EA 13 824EX 387 PHL - EN ROUTE, NR 2 HYDRAULIC SYSTEM QUANTITY WENT TO ZERO. INSPECTED AND FOUND HYDRAULIC LINE FROM NR 2 ENGINE DRIVEN PUMP BROKEN. REMOVED AND REPLACED HYDRAULIC LINE, ENGINE DRIVEN PUMP, AND CASE DRAIN FILTER IAW DHC MM REQUIREMENTS. S YSTEM OPERATIONALLY CHECKED GOOD. A/C RETURNED TO SERVICE. ACTC: 6,717. (X) 2 H 7 2 4T RT A13NM 1997022000705 19970220 00705 EU 1997 2 20 97ZZZX810 2 19961205 A 7250 TURBINE HWKSLY DH125 BH125600A 4210101 EU RROYCE VIPER VIPER60122 54551 EU NR 2 ENGINE FAILED A A B7PA A E UNSCHED LANDING ENGINE SHUTDOWN T Y ENGINE CASE PENETRATION ENGINE STOPPAGE CR CRUISE 1 NE 05 523MA 805 256023 601184 MKE/MKC - CHARTER FLIGHT. PILOT REPORT CARD NR 96-8, ITEMS 1-2, ENGINE NR 2 FAILURE, LOUD BANG FOLLOWED BY A RAPID AND COMPLETE LOSS OF POWER. FAILURE AT 1843Z WITH 3 PASSENGERS ON BOARD. AIRFRAME TIME APPROX 7,083.2 HOURS, END OF PILOT REPORT. FLIGHT DIVERTED TO MADISON MSN. PILOTS REPORT REAR TURBINE WHEEL FAILURE. ENGINE TO BE SHIPPED TO ROLLS ROYCE FOR TEAR DOWN AND INSPECTION TO DETERMINE CAUSE OF MALFUNCTION. TOTAL CYCLES, 808. 2 L 7 2 4J 4 J A3EU E15EU 1997022000764 19970220 00764 WP 1997 2 20 ABXA9700031 1 19961008 A 2760 3654073 LINK DOUG DC8 DC861 3021952 WP NR 4 SPOILER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 852AX 46016 BOTH THE INBOARD AND OUTBOARD OVERCENTER LINKS CRACKED ON THE RIGHT WING NR 4 SPOILER. REPLACED NR 4 SPOILER OVERCENTER LINKS AND OPS CHECKED SPOILER IAW DC-8 MM 27-61. 2 L 7 4 4F 4A25 1997022000765 19970220 00765 WP 1997 2 20 ABXA9700032 1 19961111 A 5320 5700921 TRAPEZOIDAL FTG DOUG DC8 DC861 3021952 WP LEFT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 853AX 46037 FOUND CRACK 1.46 INCHES IN LENGTH ON THE FORWARD END OF TRAPEZOIDAL FITTING, LEFT SIDE. REMOVED TRAPEZOIDAL FITTING, CL EANED AREA AND ANTI-CORROSION TREATED IAW SRM 51-1-8. INSTALLED NEW TRAPEZOIDAL FITTING. 2 L 7 4 4F 4A25 1997022500002 19970225 00002 WP 1997 2 25 CALA9700162 1 19961218 A 5753 HINGE ANGLE DOUG DC10 DC1030 3023501 WP LT TE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37077 46981 INSPECTION FOUND A 5.5 INCH CRACK IN UPPER RADIUS OF LOWER AFT FAIRING 535JL INBOARD HINGE AT OUTBOARD LT FLAP INBOARD F ACE. THE FAIRING WAS REMOVED AND THE CORRODED AREA OF SKIN WAS CUT OUT, FILLER AND DOUBLER WERE FABRICATED AND INSTALLE D IAW DRAWING SKB 020118N00677 AND ECRA 5720-01558. THE CORRODED HINGE ANGLE WAS CUT OUT, A SPLICE AND DOUBLER WERE FAB RICATED AND INSTALLED IAW DRAWING SKB 020118N00677. THE FAIRING WAS REINSTALLED IAW SRM 51-31-1. 2 L 7 3 4F A22WE 1997022500004 19970225 00004 EA 1997 2 25 CA960916016 2 19960911 A 7414 1068256011 MAGNETO BENDIX D6LN3000 CESSNA 182 R182 2072734 CE LYC O540 O540J3C5 41532 EA MCAULY 2D34C B2D34C214 GL INTERNAL COIL FAULTY W A UNSCHED LANDING E Y VIBRATION/BUFFET ENGINE STOPPAGE CR CRUISE 1 CA 12 6011980 L2281840A 778345 (CAN) MAGNETO, WITH NEW CAPACITORS, INSTALLED ON AIRCRAFT AND FAILED WITHIN 12 HOURS. UNIT RETURNED FOR WARRANTY RECOVER Y. 1 H 7 1 3O 3 O RT 3A13 E295 5 C P7EA 1997022500005 19970225 00005 EU 1997 2 25 CA960923004 1 19960909 A 3246 AH43207 WHEEL HALF DUNLOP AH52689 BAG JETSTM JETSTM4112 EU ROTOL R333 R333482F12 GL INBOARD FLANGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA RX079 DRG728187 (CAN) DURING WALKAROUND CREW NOTICED APPROXIMATELY 12 INCH PIECE OF RH MAIN WHEEL INBOARD FLANGE CRACKED AWAY FROM WHEEL . 1 L 7 2 4T RT A196 6 C P61GL 1997022500006 19970225 00006 EU 1997 2 25 CA960924002 1 19960918 A 3260 SENSOR BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE LEFT MLG IND FAILED W O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 CA LF05627A (CAN) LEFT LANDING GEAR UNSAFE LIGHT REMAINED ON AT POWER UP. CONFIRMED AS INDICATION ONLY. LEFT MAIN GEAR DOWN LOCK PRO XIMITY SWITCH SENSOR FOUND FAILED. 2 H 7 4 4F 4 F RT A49EU E6NE 1997022700019 19970227 00019 NM 1997 2 27 UPS97222078 1 19961227 A 5320 65225511 CHANNEL BOEING 727 727185C 138406N NM BS 1342 RUSTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE: C. B.S. 1342 LT SIDE AT LBL 18 WL 247 CHANNEL P/N 65-22551-1 IS SEVERELY RUSTED. REMOVED AND REPLACE D CHANNEL WITH P/N 65-93155-567 IAW UPS E.O. B727-5530-4601-B, AND SRM 51-10-1, AND 51-30-2. 2 L 7 3 4F A3WE 1997022700020 19970227 00020 NM 1997 2 27 UPS97222079 1 19961227 A 5311 65175085 FRAME BOEING 727 727185C 138406N NM BS 1342 RUSTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE: C. BS 1342 LT LOWER FRAME CHORD AT LBL 24 P/N 65-17508-5 IS SEVERELY RUSTED. REMOVED AND REPLACED FR AME CHORD WITH P/N 65-17508-223 IAW SRM 51-10-1, 51-30-2, AND UPS E.O. B727-5530-4601-B. 2 L 7 3 4F A3WE 1997022700021 19970227 00021 NM 1997 2 27 UPS97222080 1 19961227 A 5400 652368723 CHORD BOEING 727 727185C 138406N NM NR 2 ENGINE WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE: C. NR 2 ENGINE RING CHORD IS SEVERLY WORN AND CHAFED. REMOVED NR 2 ENGINE'S OLD CHORD AND INSTALLED A NEW CHORD PER SRM 51-30-2. 2 L 7 3 4F A3WE 1997022700023 19970227 00023 NM 1997 2 27 UPS97222082 1 19961227 A 5320 65225517 CHANNEL BOEING 727 727185C 138406N NM BS 1342 RUSTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE: C. BS 1342 AFT CENTER CHANNEL W.L. 250 P/N 65-22551-7 IS SEVERELY RUSTED. REMOVED AND REPLACED CHAN NEL IAW SRM 51-10-1, 51-30-2, AND UPS E.O. B727-5530-4601-B. 2 L 7 3 4F A3WE 1997022700062 19970227 00062 SO 1997 2 27 97ZZZX815 1 19961004 A 5610 1159SCB31024 WINDSHIELD GULSTM G1159 GIV 3980115 SO COPILOT CRACKED A N9WA K NONE O OTHER TX TAXI/GRND HDL 1 EA 11 226G 2909 1122 WHILE TAXIING FOLLOWING LANDING AT (TEB) DESTINATION, COPILOT'S WINDSHIELD OUTER HEATING LAYER WAS FOUND CRACKED IN SEVE RAL PLACES. DEFERRED ITEM PER GULFSTREAM FLIGHT MANUAL CDL APPENDIX B, 56-1 AND FLEW TO GULFSTREAM, SAVANNAH, GA FOR RE PAIRS. WINDSHIELD WAS REPLACED, CHECKED, AND RETURNED TO SERVICE. NO PASSENGERS ON AIRCRAFT. TOTAL TIME, 2,908.9 HOUR S. CYCLES, 1,561. 2 L 7 2 4F RT A12EA 1997022700172 19970227 00172 NM 1997 2 27 DHL97724002 1 19960218 A 3240 MS288892 HYD PRESS TRANS ST7R BOEING 727 727228 NM RT MLG LEAKING A DHLA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 724DH 4891 19862 HYD BRAKE PRESSURE GAUGE INDICATES 1,500 LBS, 'A' AND 'B' HYD PRESSURE AND QUANTITY IS NORMAL. BRAKES WORKED NORMALLY O N LANDING. FOUND BRAKE ACC SHRADER VALVE LEAKING IN RT W/W. REPLACED VALVE, LEAK CHECKS GOOD. ALSO, FOUND BRAKE ACC P RESS TRANSMITTER LEAKING FROM UNION ON BOTTOM OF TRANSMITTER. REPLACED BRAKE ACC PRESS TRANSMITTER, LEAK CHECK GOOD. S ERVICED BRAKE HYD ACCUMULATOR MM 29-30. 2 L 7 3 4F A3WE 1997022700173 19970227 00173 1997 2 27 DHL97807001 4 19960219 A 3417 2587400436 ADC DOUG DC8 DC873F 302199F WP E/E COMPT FAILED A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 807DH 45990 ON CLIMB AIR DATA COMPUTER INOP. REMOVED AND REPLACED AIR DATA COMPUTER PER MM 34-11-0, OPS CHECKS NORMAL. PERFORMED P ITOT STATIC CHECK PER 34-11-0, ALL CHECKS GOOD. ALL TEST EQUIPMENT REMOVED. 2 L 7 4 4F RT 4A25 1997022700231 19970227 00231 NE 1997 2 27 97ZZZX857 2 19960724 A 7230 430109102 BEARING BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE ENGINE NR 2 FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 532KH 1677 C516 7069 LE45068 NR 2 BEARING FAILED. NO REPLACEMENT BEARING AT TIME OF THIS REPORT. 1 G 7 2 3U 3 U H13EU E5NE 1997022700232 19970227 00232 NE 1997 2 27 97ZZZX858 2 19960724 A 7250 414105201 BEARING BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE ENGINE NR 2 FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 532KH 2457 H420 7069 LE45068 NR 2 BEARING FAILED. NO REPLACEMENT BEARING AT TIME OF THIS REPORT. 1 G 7 2 3U 3 U H13EU E5NE 1997022700233 19970227 00233 NE 1997 2 27 97ZZZX859 2 19960704 A 7250 430124202 BEARING BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE NR 3 FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 532KH 1677 11870 7069 LE45068 TURBINE NR 3 BEARING FAILED. NO REPLACEMENT BEARING AT TIME OF THIS REPORT. 1 G 7 2 3U 3 U H13EU E5NE 1997022700236 19970227 00236 WP 1997 2 27 USAA970028 1 19960122 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 936 DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 932VJ 71625 47189 PIT - DURING Q-1 CHECK, FOUND 2 INCH LONG GOUGE 0.035 INCH DEEP AND 3 INCH CHAFE 0.009 INCH DEEP IN SKIN JUST ABOVE AND BELOW LONGERON 15R STA 936 AND JUST AFT OF STA 936 LONGERON 15R. REPAIRED WITH TITANIUM DOUBLER AND FINGER DOUBLER PER SRM 53-04, FIGURE 3A AND SRM 53-04, FIGURE 12B. (X) 2 L 7 2 4F A6WE 1997022700237 19970227 00237 WP 1997 2 27 USAA970027 1 19960122 A 5311 BELT FRAME DOUG DC9 DC931 3022065 WP BS 1076 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 932VJ 71625 47189 PIT - DURING Q-1 CHECK, FOUND .3750 INCH CRACK AT FASTENER STA 1076, LONGERON 15RT BELT FRAME. INSTALLED DOUBLER PER EA 29699. (X) 2 L 7 2 4F A6WE 1997022700281 19970227 00281 EU 1997 2 27 PLGA9612203 1 19961220 A 2432 501122804 POWER SUPPLY SAAB SF340 SF340A 7850100 EU AVIONICS RACK LOW VOLTAGE A PLGA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 NE 05 744BA 5379 340A105 BOS - FLT 4406 - DURING FLIGHT, CREW REPORTED THE EMERGENCY BUSS WENT INOPERATIVE. AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND JET PACK POWER SUPPLY AT FAULT. POWER PACK WAS REPLACED AND SYSTEM CHECKED NORMAL. (M) 2 L 7 2 4T RT A52EU 1997022700304 19970227 00304 NM 1997 2 27 ASAA9610149 1 19961229 A 3350 1102833 LIGHT BOEING 737 737298C 1384490 NM R1 DOOR INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 ANC - DURING MAINTENANCE CHECK, THE R1 DOOR OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE CAUSING SEVERAL OT HER EMERGENCY EXIT LIGHTS TO ILLUMINATE WITH THE EMERGENCY EXIT LIGHT SWITCH IN THE ARMED POSITION. DISCONNECTED AND SE CURED WIRING FROM THE R1 EMERGENCY EXIT LIGHT. REMAINING EMERGENCY EXIT LIGHTS OPERATED NORMALLY. RELEASED R1 DOOR OVE RHEAD EMERGENCY EXIT LIGHT INOPERATIVE PER MEL 33-15. SUBSEQUENTLY REPLACED R1 DOOR OVERHEAD EMERGENCY EXIT LIGHT ASSEM BLY TO CLEAR MEL. (M) 2 L 7 2 4F RT A16WE 1997022700305 19970227 00305 NM 1997 2 27 ASAA9610146 1 19961214 A 3350 86210151 BATTERY BOEING 737 737298C 1384490 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 SEA - FLT 54 - PRIOR TO DEPARTURE CREW REPORTED, THE EXIT LIGHT ON THE SMOKE BARRIER WAS FLASHING. REPLACED BATTERY AND LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1997022700319 19970227 00319 NM 1997 2 27 97ZZZM258 1 19961229 A 2910 BACH8A04NN0264T HOSE BOEING 737 7372L9 1384497 NM MLG WHEEL WELL DAMAGED A SOKF A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SO 23 281LF 22701 FLT 610 - BAQ-SJO - HYDRAULIC SYSTEM 'A' HAD A TOTAL LOSS OF HYDRAULIC OIL DUE FLEX HOSE ASSEMBLY, P/N BACH8A04NN0264T S PRUNG A LEAK AT WHEEL WELL AND CREW DECLARED EMERGENCY LANDING. AIRCRAFT LANDED WITH NO INCIDENTS AT SJO. HOSE WAS REP LACED AND TEST WAS ACCOMPLISHED AS PER MM 29-10-29 SERVICE SYSTEM AS PER 20-10-52. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1997022700344 19970227 00344 CE 1997 2 27 GLBA96255 1 19961230 A 2130 11438004221 PRSOV BEECH 1900 1900C 1154161 CE LT ENGINE MALFUNCTIONS A GLBA O OTHER O OTHER CR CRUISE 1 CE 01 141UE UC141 CIU - LEFT AND RIGHT ENVIRONMENTAL FAIL ANNUNCIATOR IN FLIGHT. MAINTENANCE SWAPPED PRSOV VALVES FOR TROUBLESHOOTING. R IGHT SIDE OPERATES NORMALLY. DEFERRED LEFT SIDE AND LATER REPLACED LEFT PRSOV. (M) 2 L 7 2 4T RT A24CE 1997022700345 19970227 00345 NE 1997 2 27 GLBA96254 2 19961222 A 7510 3D237606 VALVE EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE RT ENGINE STICKY A GLBA O OTHER O OTHER CR CRUISE 1 CE 01 299UX 120299 MQT - RIGHT ENGINE AIR INLET DE-ICE FAILS CONTINUOUSLY. MAINTENANCE REPLACED RIGHT ENGINE EJECTOR CONTROL VALVE. OPS C HECKS GOOD. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1997022700346 19970227 00346 CE 1997 2 27 GLBA96252 1 19961202 A 2750 SWITCHES BEECH 1900 1900C 1154161 CE TE FLAPS DIRTY A GLBA O OTHER J WARNING INDICATION TO TAKEOFF 1 CE 01 84GL UC84 SPI - FLAPS DID NOT COME UP AFTER DEPARTURE. MAINTENANCE CLEANED LIMIT SWITCHES. (M) 2 L 7 2 4T RT A24CE 1997022700347 19970227 00347 SO 1997 2 27 GLBA96251 1 19961213 A 3250 STEERING HANDLE EMB 120 EMB120RT SO NLG STEERING OUT OF ADJUST A GLBA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 01 279UE 120085 DLH - AIRCRAFT PULLS HARD RIGHT ON TOUCHDOWN AND ALSO WHEN TILLER IS RELEASED AIRCRAFT PULLS RIGHT. MAINTENANCE RIGGED STEERING HANDLE POTENTIOMETER. OPERATIONAL CHECKS GOOD. (M) 2 L 7 2 4T RT A31SO 1997022700348 19970227 00348 SO 1997 2 27 GLBA96250 1 19961228 A 3260 32138 SWITCH EMB 120 EMB120RT SO LANDING GEAR FAILED A GLBA O OTHER N FALSE WARNING CL CLIMB 1 CE 01 281UE 120092 DLH - LANDING GEAR ALARM ON MAP ILLUMINATES BETWEEN 2,500 FEET AND 4,000 FEET AGL. AURAL WARNING CALLS OUT 'LANDING GEA R'. MAINTENANCE REPLACED BOTH AIRSPEED SWITCHES, PERFORMED PITOT-STATIC TEST AND OPERATIONAL CHECKS GOOD. (M) 2 L 7 2 4T RT A31SO 1997022700349 19970227 00349 SO 1997 2 27 GLBA96249 1 19961229 A 5753 FLAP TRACKS EMB 120 EMB120ER 3260203 SO TE FLAPS DIRTY A GLBA O OTHER J WARNING INDICATION TO TAKEOFF 1 CE 01 297UX 120297 OSH - AFTER TAKEOFF, OUTBOARD PAIR OF FLAPS RETRACTED ONLY 10 DEGREES RESULTING IN A FLAP DISAGREEMENT WARNING. MAINTEN ANCE CLEANED OUTBOARD FLAP TRACKS AND COULD NOT DUPLICATE PROBLEM. (M) 2 L 7 2 4T RT A31SO 1997022700350 19970227 00350 CE 1997 2 27 GLBA96248 1 19961227 A 3240 BRAKE BEECH 1900 1900C 1154161 CE LEFT REQUIRED SERVICE A GLBA K NONE O OTHER TX TAXI/GRND HDL 1 CE 01 98GL UC98 SPW - LEFT BRAKE ON CAPTAINS SIDE DOES NOT HOLD PRESSURE. MAINTENANCE BLED BRAKES AND OPERATION WAS NORMAL. (M) 2 L 7 2 4T RT A24CE 1997022700351 19970227 00351 SO 1997 2 27 GLBA96247 1 19961225 A 2751 CONNECTOR EMB 120 EMB120RT SO TE FLAPS LOOSE A GLBA O OTHER N FALSE WARNING TO TAKEOFF 1 CE 01 267UE 120071 DLH - FLAP DISAGREEMENT AFTER TAKEOFF ON FLAP RETRACTION. MAINTENANCE RESECURED LOOSE CONNECTION AT RIGHT OUTBOARD CANN ON PLUG ON FLAP ACTUATOR. CLEANED ALL CANNON PLUGS AND OPS CHECK IS NORMAL ON GROUND AND IN FLIGHT. (M) 2 L 7 2 4T RT A31SO 1997022700352 19970227 00352 CE 1997 2 27 GLBA96246 1 19961224 A 3010 727725 CIRCUIT BREAKER BEECH 1900 1900D 1154162 CE WING DE-ICE FAILED A GLBA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 CE 01 97UX UE97 DIK - ON DESCENT, THE 'WING ICE' CIRCUIT BREAKER STARTED TO SMOKE. PULLED BREAKER AND SMOKE STOPPED. (M) 2 L 7 2 4T RT A24CE 1997022700353 19970227 00353 SO 1997 2 27 GLBA96245 1 19961225 A 5753 FLAP TRACKS EMB 120 EMB120RT SO TE FLAPS DIRTY A GLBA O OTHER J WARNING INDICATION TO TAKEOFF 1 CE 01 279UE 120085 SPW - FLAP DISAGREEMENT AFTER TAKEOFF. MAINTENANCE CLEANED FLAP TRACKS AND COULD NOT DUPLICATE PROBLEM. (M) 2 L 7 2 4T RT A31SO 1997022700354 19970227 00354 SO 1997 2 27 GLBA96244 1 19961223 A 3260 922AA24A6P PROX SENSOR EMB 120 EMB120RT SO LT MLG FAILED A GLBA O OTHER J WARNING INDICATION LD LANDING 1 CE 01 267UE 120071 MQT - LANDING GEAR WOULD NOT EXTEND BY NORMAL EXTENSION. GEAR EXTENDED BY ELECTRIC OVERRIDE. MAINTENANCE RECONFIGURED DOWNLOCK SENSORS AND REPLACED LEFT GEAR 'B' SYSTEM PROXIMITY SENSOR. (M) 2 L 7 2 4T RT A31SO 1997022700355 19970227 00355 SO 1997 2 27 GLBA96243 1 19961222 A 3233 ACTUATOR EMB 120 EMB120RT SO RT MLG FAILED A GLBA O OTHER J WARNING INDICATION LD LANDING 1 CE 01 129AM 120119 OSH - RIGHT MAIN LANDING GEAR FAILED TO EXTEND NORMALLY. MAINTENANCE REPLACED RIGHT MAIN LANDING GEAR ACTUATOR. (M) 2 L 7 2 4T RT A31SO 1997022700356 19970227 00356 SO 1997 2 27 GLBA96242 1 19961220 A 5753 FLAP TRACKS EMB 120 EMB120RT SO TE FLAPS DIRTY A GLBA O OTHER J WARNING INDICATION LD LANDING 1 CE 01 267UE 120071 MQT - OUTBOARD FLAP DISAGREEMENT. MAINTENANCE CLEANED FLAP TRACKS AND ROLLERS. TEST FLIGHT NORMAL. (M) 2 L 7 2 4T RT A31SO 1997022700357 19970227 00357 SO 1997 2 27 GLBA96241 1 19961218 A 2150 PACK EMB 120 EMB120RT SO RIGHT FAILED A GLBA O OTHER J WARNING INDICATION CR CRUISE 1 CE 01 451UE 120108 DEN - RIGHT AIR CONDITIONING PACK FAILED IN FLIGHT ON HIGH AND COULD NOT KEEP CABIN COMFORTABLE. MAINTENANCE REPLACED C ABIN TEMP CONTROL VALVE. (M) 2 L 7 2 4T RT A31SO 1997022700358 19970227 00358 SO 1997 2 27 GLBA96240 1 19961217 A 3250 SWITCH EMB 120 EMB120ER 3260203 SO NLG STEERING DIRTY A GLBA O OTHER O OTHER LD LANDING 1 CE 01 295UX 120295 FSD - AFTER LANDING, UNABLE TO STEER NOSEWHEEL BY TILLER OR RUDDER PEDALS. MAINTENANCE FOUND PROXIMITY SWITCHES STICKIN G. CLEANED AND OPERATES NORMALLY. (M) 2 L 7 2 4T RT A31SO 1997022700359 19970227 00359 CE 1997 2 27 GLBA96239 1 19961213 A 2720 RUDDER BOOST BEECH 1900 1900D 1154162 CE EMPENNAGE ACTIVATED A GLBA O OTHER F FLT CONT AFFECTED CR CRUISE 1 CE 01 169GL UE169 RDU - UNSCHEDULED RUDDER BOOST ACTIVATION. MAINTENANCE COULD NOT DUPLICATE. (M) 2 L 7 2 4T RT A24CE 1997022700381 19970227 00381 NM 1997 2 27 USAA970042 1 19960128 A 5315 FLOOR BEAM BOEING 737 7373B7 1384580 NM BS 986 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 376US 35405 22955 CLT - INSPECTION VISUALLY FOUND LEVEL 2 MULTIPLE CORROSION MEASURING 1 INCH BY 1 INCH LOCATED AT FLOOR BEAM AT STATION 9 06, BL0 BL46 L/R. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. REPAIRED FLOOR BEAM PER SRM 53-60-51 AND TRM 53-15- 01A. (M) 2 L 7 2 4F RT A16WE 1997022700384 19970227 00384 NM 1997 2 27 USAASB97031 1 19961227 A 3350 6104789 BATTERY PACK BOEING 737 737201 1384454 NM CARGO COMPART DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 264AU 22961 BWI - MAINTENANCE FOUND THE LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BAT TERY PACK IN THE AFT CARGO COMPARTMENT. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1997022700394 19970227 00394 WP 1997 2 27 USAA970010 1 19960109 A 5312 BULKHEAD DOUBLER DOUG DC9 DC931 3022065 WP BS 996 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 946VJ 74632 47026 PIT - DURING AGING VISIT 89K, FOUND 1.125 INCH CRACK IN 591013-13 BULKHEAD DOUBLER, 1.25 INCH CRACK IN 5910130-22 DOUBLE R, .25 INCH CRACK IN 5910130-13 DOUBLER, 4.25 INCH CRACK IN THE RADIUS OF 5910130-13 DOUBLER. (M) 2 L 7 2 4F A6WE 1997022700401 19970227 00401 WP 1997 2 27 USAAD97020 1 19960122 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 936VJ 48116 PIT - LOW LEVEL EMERGENCY LIGHTS INOPERATIVE AT SEAT ROWS 3 AND 4. REPAIRED BROKEN WIRE IN FLOOR TRACK. (M) 2 L 7 2 4F A6WE 1997022700413 19970227 00413 NM 1997 2 27 USAABB97014 1 19960201 A 3350 873203193 CONTROL MODULE BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 626AU 27303 LAX - EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE REPLACED THE CONTROL MODULE ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 1997022700414 19970227 00414 NM 1997 2 27 USAABB97013 1 19960116 A 3350 86210066 BATTERIES BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 624AU 27245 LAX - FOUND EMERGENCY FLOOR LIGHT BATTERIES INOPERATIVE AT ROWS 1, 4, 13, 19 AND 23. REPLACED BATTERIES. (M) 2 L 7 2 4F RT A2NM 1997022700437 19970227 00437 NM 1997 2 27 97ZZZX861 1 19961229 A 2750 65222347 DRIVE MOTOR BOEING 727 727251 138408H NM RT TE FLAP LEAKING A PCSA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 17 296AJ 21156 CUR - AIRCRAFT DEPARTED, LOST A-SYSTEM PRESSURE SHORTLY AFTER TAKEOFF. AIRCRAFT RETURNED TO CUR AND MADE AN UNEVENTFUL LANDING. AFTER BLOCK IN, THE HYDRAULIC INTERCONNECT WAS OPENED. B-SYSTEM DUMPED INTO A-SYSTEM DEPLETING BOTH SYSTEMS. TROUBLESHOOTING FOUND THE RT OUTBOARD FLAP DRIVE MOTOR LEAKING FROM THE CASE AND THE DRAIN LINE. REMOVED AND REPLACED FLAP DRIVE MOTOR IAW MM 27-50, SERVICED BOTH 'A' AND 'B' SYSTEMS TO CAPACITY, ACCOMPLISHED OPS CHECK IAW MM 27-51. OPS CHECKED GOOD, NO LEAKS NOTED, AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A3WE 1997022700439 19970227 00439 WP 1997 2 27 TWAA9615821 1 19961218 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1106-1109 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 MCI - DURING CHECK C, FOUND CORROSION ON MAIN CABIN SEAT TRACK SURFACE, LBL 45 TO LBL 22, STA 1106 - STA 1109. REMOVED CORRODED SEAT TRACK PER SRM 51-30-1, FABRICATED SPLICES PER SRM 53-05, FIGURE 4D; ALODINED AND PRIMED PER SRM 51-10-31 AND INSTALLED SEAT TRACK PER SRM 51-30-1. AIRCRAFT TOTAL TIME: 19,271 HOURS; 15,596 CYCLES. (X) 2 L 7 2 4F A6WE 1997022700440 19970227 00440 WP 1997 2 27 TWAA9615820 1 19961218 A 5312 BULKHEAD FITTING DOUG DC9 DC982 3022082 WP AFT PRESS BLKHD CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 MCI - DURING CHECK C, FOUND CORROSION ON AFT PRESSURE BULKHEAD FITTING, SEVERAL SPOTS. REMOVED AND REPLACED LONGERON FI TTING PER SRM 51-00 AND INSTALLED FASTENERS PER SRM 51-30-2. AIRCRAFT TOTAL TIME: 19,271 HOURS; 15,596 CYCLES. (X) 2 L 7 2 4F A6WE 1997022700441 19970227 00441 WP 1997 2 27 TWAA9615822 1 19961218 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9420D 49824 MCI - DURING CHECK C, FOUND CORROSION UNDER CLIP NUTS OF MAIN CABIN SEAT TRACK, LBL 45. REMOVED AND REPLACED SEAT TRACK PER SRM 51-30-2; SPLICED NEW SECTION PER SRM 53-05, FIGURE 4L. AIRCRAFT TOTAL TIME: 19,271 HOURS; 15,596 CYCLES. (X) 2 L 7 2 4F A6WE 1997022700442 19970227 00442 EU 1997 2 27 97ZZZX862 1 19961217 A 2910 HYDRAULIC SYSTEM STBROS SD3 SD360 8100606 EU RIGHT REQ'D SERVICE A GUUA O OTHER J WARNING INDICATION CL CLIMB 1 SO 19 265GA SH3757 MIA/TPA - FLT 445 - PILOT REPORT: HYDRAULIC RIGHT LIGHT AFTER ROTATION. GEAR UP SLOWLY, TOO SLOW. GEAR DOWN - 3 GREEN . RT HYD LT OUT. NOW LT HYD LT ON. R AND B. NO ADVERSE INDICATIONS ON HYD PANEL EXCEPT HIGH RESERVOIR CONTENTS, MAIN SYSTEM PRESSURE FLUCTUATES 500-1,000 DURING GEAR TRANSIT. CHECK LIST ACCOMPLISHED IAW SOP. SERVICED HYD SYSTEM AND PE RFORMED GEAR RETRACTION. OPS CHECK GOOD. LEAK CHECK GOOD. 2 H 7 2 4T A41EU 1997022700443 19970227 00443 NE 1997 2 27 USAABB96064 2 19961221 A 7200 ENGINE BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211535E4 54555 NE RIGHT FAILED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 627AU 27805 31324 PIT - FLT 9 - STRONG ODOR OF OIL FUMES IN CABIN. CREW TURNED RIGHT ENGINE BLEED AIR AND RECIRCULATION AND FANS OFF. TH IS WAS THE SECOND OCCURRENCE OF THIS SITUATION IN AS MANY FLIGHTS. MAINTENANCE REPLACED THE RIGHT ENGINE. (X) 2 L 7 2 4F 4 F RT A2NM E12EU 1997022700444 19970227 00444 EU 1997 2 27 MALA965263 1 19961225 A 5270 SWITCH SAAB SF340 SF340A 7850100 EU CABIN DOOR OUT OF ADJUST A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 991XJ 340A091 ATW - FLT 2973 - ON CLIMB-OUT, THE MAIN DOOR HANDLE ANNUNCIATOR LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO ATW. MAINT ENANCE ADJUSTED THE MAIN DOOR MICROSWITCH. ALL CHECKS GOOD. (X) 2 L 7 2 4T RT A52EU 1997022700445 19970227 00445 WP 1997 2 27 G60A004 1 19961224 A 7830 TR MOUNT DOUG DC10 DC1030 3023501 WP NR 3 ENGINE BROKE A G6OA O OTHER J WARNING INDICATION LD LANDING 1 EA 27 605GC 47925 NR 3 ENGINE THRUST REVERSER RHS CENTER BALL ACTUATOR ASSEMBLY FAILED TO RETRACT AFTER LANDING. THE BALL SCREW ACTUATOR M OUNT BRACKET BROKE OFF AND DAMAGED THE LEADING EDGE OF TRANSLATING COWL. (X) 2 L 7 3 4F A22WE 1997022700447 19970227 00447 NE 1997 2 27 97ZZZX864 2 19961220 A 7310 50389110 FUEL FILTER BEECH 200 B200 1152922 CE PWA PT6 PT6A42 52043 NE RT ENGINE FROZE UP A FFSA K NONE O OTHER IN INSP/MAINT 1 AL 01 4277C BB1309 PCE94304 PRECAUTIONARY SHUT DOWN FOR FLUCTUATING TORQUE AND WP. UPON INSPECTION, DETERMINED THE RIGHT FUEL SEDIMENT BOWL (FIREWA LL FILTER) CONTAINED A SUFFICIENT AMOUNT OF ICE CRYSTALS TO RESTRICT FUEL FLOW. DISASSEMBLED, CLEANED, AND REINSTALLED FILTER ELEMENTS/ASSEMBLY. PERFORMED A COMPLETE MAINTENANCE 'POWER ASSURANCE CHECK' AND FOUND THE AIRCRAFT AND POWERPLAN TS ACCEPTABLE FOR CONTINUED OPERATION. 1 L 7 2 4T 4 T A24CE E4EA 1997022700449 19970227 00449 EU 1997 2 27 MALA965261 1 19961224 A 3260 UPLOCK HOOK SAAB SF340 340B 7860101 EU LANDING GEAR ICED UP A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 402XJ 340B402 DTW - FLT 3431 - ON CLIMB-OUT, THE GEAR INTRANSIT LIGHT REMAINED ON AFTER GEAR EXTENSION. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REMOVED ICE FROM THE UPLOCK HOOK AND MICROSWITCH. ALL CHECKS SATISFACTORY. (X) 2 L 7 2 4T RT A52EU 1997022700493 19970227 00493 NM 1997 2 27 UPS97222085 1 19961226 A 5320 65225512 CHANNEL BOEING 727 727185C 138406N NM BS 1342 RUSTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 954UP 19827 BS 1342 RT HD CHANNEL RBL 18 WL 247, P/N 65-22551-2, IS SEVERELY RUSTED. REMOVED AND REPLACED CHANNEL WITH P/N 65-93155 -67 IAW SRM 51-30-2, AND UPS EO B727-5530-4601-B. 2 L 7 3 4F A3WE 1997022700551 19970227 00551 NM 1997 2 27 DL72K970310 1 19960926 A 5730 651622295 SKIN BOEING 727 727232 1384082 NM WING LE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 471DA 20748 A CRACK WAS FOUND IN THE TIA DUCT CUTOUT AREA. INSTALLED A DOUBLER PER MM 57-54-00, PG 814. 2 L 7 3 4F A3WE 1997022700667 19970227 00667 NM 1997 2 27 UPS97222152 1 19961227 A 5320 CHANNEL BOEING 727 727185C 138406N NM CARGO DOORWAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE-C, FWD LWR CARGO DOOR FRAME IS CRACKED AT AFT HINGE ARM FWD OF UPPER AFT STOP. REMOVED AND REPLACED CHA NNEL (P/N 65-18620-7) PER SRM 51-30-2. 2 L 7 3 4F A3WE 1997030600031 19970306 00031 WP 1997 3 6 IXXA9700023 1 19961230 A 5320 57799282 FITTING DOUG DC8 DC871F 302199D WP BS 220/240 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825BX 74553 5912 45978 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND ON A LONGERON SPLICE FITTING BETWEEN FUSELAGE STATION 220 AND 240 AT LONGERON 29 RT. REPAIR ACCOMPLISHED BY REMOVAL OF SPLICE FITTING, FABRICATION AND INSTALLATION OF A NEW FITTING IN AC CORDANCE WITH ENGINEERING ORDER 53-DC8-432 AND SRM 53-1-0 AND FAA DER APPROVED DRAWING 853-08-97. 2 L 7 4 4F RT 4A25 1997030600180 19970306 00180 NM 1997 3 6 UPS97222171 1 19961228 A 5754 65185328 FITTING BOEING 727 727185C 138406N NM NR 5 LE FLAP CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE-C, RT WING L/E NR 5 K-FLAP ACTUATOR HINGE SUPPORT CASTING HAS HEAVY CORROSION. REMOVED AND REPLACED HIN GE FITTING (P/N 65-18532-8) PER DWG NR 65-18532 AND SRM 51-30-2 AND DWG NR 65-16269. 2 L 7 3 4F A3WE 1997030600496 19970306 00496 NM 1997 3 6 AALA970032 1 19961221 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 495 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1766A 48597 TUL - FOUND CORROSION IN NR 8 SEAT TRACK AT LAV B OUTBOARD AFT TIEDOWN. ACCOMPLISHED A STANDARD SEAT TRACK REPAIR PER S RM 53-70-00-0 VOL 1 PAGE 3 AND 4. (M) 2 L 7 3 4F RT A22WE 1997030600514 19970306 00514 NM 1997 3 6 AALA970126 1 19961231 A 5210 146N6201 PAN BOEING 757 757223 1384957 NM R1 DOOR GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 670AA 25335 AFW - R-1 DOOR HANDLE PAN HAS GOUGE BEYOND SRM LIMITS, REF E58 1814484. REF MRB NR 757-1050. (M) 2 L 7 2 4F RT A2NM 1997030600625 19970306 00625 WP 1997 3 6 AALA970028 1 19961230 A 2840 ANN01001 BRACKET DOUG DC10 DC1010 3022110 WP WS 538 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 130AA 46989 TUL - FUEL QUANTITY ASSEMBLY HAS HEAVY CORROSION ON BRACKETS. FUEL QUANTITY GAUGE ASSEMBLY REMOVED AND REPLACED WITH SE RVICEABLE UNIT AND 8130 PARTS TAG. (M) 2 L 7 3 4F A22WE 1997030600626 19970306 00626 WP 1997 3 6 AALA970030 1 19961219 A 5320 SUPPORT TRACK DOUG DC10 DC1010 3022110 WP BS 778-779 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 130AA 46989 TUL - CENTER SERVICE CART STOWAGE SUPPROT TRACKS HAVE CORROSION DAMAGE. FABRICATED TWO NEW SUPPORTS AND INSTALLED PER A ARD 51-10-00-1. (M) 2 L 7 3 4F A22WE 1997030600627 19970306 00627 WP 1997 3 6 AALA970034 1 19961223 A 5320 SUPPORT TRACK DOUG DC10 DC1010 3022110 WP BS 862 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 130AA 46989 TUL - GALLEY SUPPORT TRACK HAS CORROSION DAMAGE AT AFT ATTACH POINT LEFT SIDE OF CART LIFT. REMOVED CORRODED TRACK AND REPLACED WITH NEW TRACK PER SRM 51-10-00. (M) 2 L 7 3 4F A22WE 1997030600650 19970306 00650 EU 1997 3 6 CA960418009 1 19960326 A 6730 SC5082 SERVO SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE R/H SERVO LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 3076 2601 866 (CAN) AFTER A VERY SHORT FLIGHT AND SHUTDOWN, A TURN AROUND CHECK WAS CARRIED OUT AND IT WAS NOTED THAT THE AREAS AROUND THE R/H SERVO WERE WET WITH HYDRAULIC FLUID. AIRCRAFT TOPPED UP WITH 0.5 LITRES OF HYDRAULIC FLUID. SUBSEQUENT RUN UP F OUND NO LEAKAGE. SIMILAR OCCURRENCE ON PREVIOUS OCCASION. 1 G 7 1 3U 3 U H9EU E19EU 1997030600652 19970306 00652 CE 1997 3 6 CA960502005 1 19960501 A 2910 AE1003957G HOSE CESSNA 414 414A 2075907 CE CONT O520 TSIO520NB 17040 SO MCAULY 3AF32C 3AF32C93 GL HYD SYS LOOSE FITTINGS W K NONE J K WARNING INDICATION FLUID LOSS AP APPROACH 1 CA 244951R 792838 (CAN) HYDRAULIC HOSE FITTINGS FOUND LOOSE ON INLET AND DISCHARGE PORTS. NO APPARENT REASON COULD BE FOUND FOR THIS CONDI TION, HOWEVER LOSS OF HYDRAULIC FLUID RESULTED. 1 L 7 2 3O 3 O A7CE E8CE 5 C P22EA 1997030600653 19970306 00653 GL 1997 3 6 CA960502008 2 19960226 A 7321 23057344 FCU BELL 206 206L 1181522 SW ALLSN 250C 250C20B 03013 GL ENGINE FAILURE W B EMER. DESCENT X R ENGINE FLAMEOUT PARTIAL RPM/PWR LOSS CR CRUISE 1 CA 426 CAE830144 (CAN) DURING CRUISE FLIGHT, A TEMPORARY FLAMEOUT OCCURRED. AFTER 3-4 SECONDS, ENGINE CAME BACK ON LINE. FCU WAS REPLACED . TIME SINCE LAST REPAIR IS 189.3 HOURS. THE SUBMITTER STATES THAT THIS PARTICULAR FCU HAS A HISTORY OF PREMATURE REMOVA LS. 1 G 7 1 3U 3 U H2SW E4CE 1997030600654 19970306 00654 GL 1997 3 6 CA960502010 2 19960222 A 7250 6898734 TURBINE ASSY BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE FAILURE W K NONE O R M OTHER PARTIAL RPM/PWR LOSS OVER TEMP IN INSP/MAINT 1 CA 10267 2846 CAE820758 (CAN) ENGINE DEVELOPING LOW POWER AND HIGH TOT, POWER ASSURANCE CHECK FAILED. TURBINE ASSEMBLY REPLACED, AIRCRAFT RETURN ED TO SERVICE. 1 G 7 1 3U 3 U H2SW E4CE 1997030600655 19970306 00655 GL 1997 3 6 CA960502011 2 19960222 A 7313 6890917 NOZZLE BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 1416 CAE820758 (CAN) SUSPECTED OF CAUSING SEVERE CARBON BUILD UP INSIDE COMBUSTION LINER DOME. NO VISIBLE DAMAGE WAS NOTED. NOZZLE REPL ACED, AIRCRAFT RETURNED TO SERVICE. 1 G 7 1 3U 3 U H2SW E4CE 1997030600656 19970306 00656 EU 1997 3 6 CA960502013 1 19960223 A 7170 0174126090 VALVE SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENG DRAIN DEFECTIVE W K NONE E W VIBRATION/BUFFET INADEQUATE Q C TX TAXI/GRND HDL 1 CA 31 956 (CAN) ENGINE MAKING A POPPING NOISE ON SHUT DOWN. TROUBLESHOOTING DETERMINED THAT THE DRAIN VALVE RECENTLY INSTALLED HAD BEEN ASSEMBLED MISSING AN ORIFICE IN THE TEE FITTING. 1 G 7 1 3U 3 U H9EU E19EU 1997030600657 19970306 00657 NE 1997 3 6 CA960502017 2 19960223 A 7230 COMPRESSOR SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE FAILED W A E UNSCHED LANDING ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 CA 3025 834 (CAN) COMPRESSOR STALL IN FLIGHT AT 60 PERCENT Q. BOTH UNITS WERE ON A 50 HOUR TBO EXTENSION FOR OVERHAUL. MO2 AND MO3 R EPLACED, AIRCRAFT RETURNED TO SERVICE. 1 G 7 1 3U 3 U H9EU E19EU 1997030600659 19970306 00659 EU 1997 3 6 CA960502022 1 19960308 A 2842 647510032A TRANSMITTER SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE FUEL QTY FAILED W K NONE J L P WARNING INDICATION NO TEST NO WARNING INDICATION IN INSP/MAINT 1 CA 416 (CAN) LOW FUEL WARNING IS WAY OUT OF LIMITS. GAUGE READS 20 PERCENT, LIGHT ON, AND ONLY 30 LITRES OF FUEL ACTUALLY ON BO ARD. THERE IS SUPPOSED TO BE 60 LITRES OF FUEL ON BOARD WHEN LIGHT COMES ON. FUEL QUANTITY TRANSMITTER REPLACED AND AIRC RAFT RETURNED TO SERVICE. 1 G 7 1 3U 3 U H9EU E19EU 1997030600660 19970306 00660 GL 1997 3 6 CA960502026 2 19960415 A 7321 252464429 FCU HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL ENGINE FAILURE W K NONE O OTHER IN INSP/MAINT 1 CA 214 CAE832104 (CAN) FCU WILL NOT HOLD GROUND IDLE. LEAKING PURPLE GREASE FROM INPUT. FCU REPLACED AND AIRCRAFT RETURNED TO SERVICE. 1 G 7 1 3U 3 U H3WE E4CE 1997030600661 19970306 00661 GL 1997 3 6 CA960502027 2 19960327 A 7321 23057344 FCU HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL ENGINE FAILURE W K NONE O OTHER IN INSP/MAINT 1 CA 246 CAE832056 (CAN) TIME THIS INSTALLATION 144.5 HOURS. BLUE GREASE LEAKING FROM BEARING. STAGNATED STARTS WHICH COULD NOT BE ADJUSTED USING FCU ADJUSTMENTS (ALREADY AT THE LIMITS). THIS FCU HAS PREVIOUS HISTORY FOR REMOVAL FOR SIMILAR REASON. FCU REPLAC ED AND AIRCRAFT RETUNED TO SERVICE. 1 G 7 1 3U 3 U H3WE E4CE 1997030600662 19970306 00662 GL 1997 3 6 CA960502029 2 19960320 A 7321 23034702 FCU BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE FAILURE W K NONE O OTHER IN INSP/MAINT 1 CA 1593 CAE820758 (CAN) ENGINE STARTING TEMPS WERE TOO HIGH IN 35 PERCENT TO 50 PERCENT NG RANGE. START DERICH ADJUSTED TO FULL DECREASE. FCU REPLACED, AIRCRAFT RETURNED TO SERVICE. 1 G 7 1 3U 3 U H2SW E4CE 1997030600663 19970306 00663 CE 1997 3 6 CA960502050 1 19960422 A 3221 WEBS CESSNA 404 404CESSNA 2075901 CE MCAULY 3FF32 3FF32C501 GL NOSE WELL CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 11492 803645 (CAN) CRACKS FOUND IN ACCORDANCE WITH CESSNA CONTINUED AIRWORTHINESS PROGRAM 32-20-01. DOUBLERS AND WEBS WERE FOUND CRAC KED AT FS 71.00. THE FOLLOWING P/NS WERE FOUND CRACKED AS WELL; DOUBLER P/N 5213045-2, WEB P/N 58130841-2, LEFT AND RIGH T SIDE WEBS P/N 5213040-9 AND 5213040-10. NEW PARTS FABRICATED IN ACCORDANCE WITH MAINTENANCE MANUAL. GEAR SWINGS CARRIE D OUT AFTER REPAIR AND CHECKED SERVICEABLE. 1 L 7 2 3O A25CE 5 C P45GL 1997030600664 19970306 00664 WP 1997 3 6 CA960502056 1 19960419 A 2612 35590055 SENSE LOOP CVAC 340 340CVAC 242270A WP ALLSN 501D 501D13 03004 GL NR 2 ENG ZONE 2 CHAFED W E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING DE DESCENT 1 CA 500963 (CAN) ON DESCENT THERE WAS A ZONE 2 FIRE INDICATION ON NUMBER TWO ENGINE. THE FIRE EXTINGUISHER WAS DISCHARGED AND THE E NGINE WAS SHUT DOWN. THE FIRE WARNING BELL DID NOT GO OUT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REVEALED TH AT THE FIRE SENSE LOOP WAS CHAFED THROUGH IN ONE PLACE WHICH SHORTED THE LOOP, GIVING A FALSE WARNING. FIRE SENSE LOOP R EPLACED. 2 L 7 2 4R 4 T 6A6 E282 1997030600667 19970306 00667 CE 1997 3 6 CA960813003 1 19960807 A 3244 301393190 TIRE GOODYEAR 22X67510 BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA INBOARD SIDEWALL BULGED W K NONE O OTHER IN INSP/MAINT 1 CA 382 31262159 PCE81195 (CAN) DURING DAILY INSPECTION THE SIDEWALL TREAD OF THE MAIN WHEEL WAS FOUND BULGING ON SOME PORTIONS OF THE INBOARD TRE AD AREA. THE TREAD WAS SOFT WHEN DEPRESSED. 1 L 7 2 4T 4 T A24CE E4EA 1997030600668 19970306 00668 SO 1997 3 6 CA960813004 1 19960726 A 8120 LW12452 TURBOCHARGER PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA RH TUBE GUSSET SUPPORT CRACKED W A K NONE O OTHER IN INSP/MAINT 1 CA L457361A (CAN) DURING A 100 HOUR INSPECTION THE R/H ENGINE TURBOCHARGER SUPPORT WAS FOUND BROKEN AT THE UPPER R/H TUBE GUSSET. SU BMITTER STATES THAT THIS SAME PART HAD BEEN REPLACED DURING THE PREVIOUS 100 HOUR INSPECITON. 1 L 7 2 3O 3 O A20SO E14EA 1997030600670 19970306 00670 CE 1997 3 6 CA960826021 1 19960808 A 5510 12326232 REINFORCEMENT CESSNA 210 T210L 2073449 CE CONT O520 TSIO520H 17040 SO MCAULY 3A32C D3A32C88 GL HORIZ STAB CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 2513 506710 771086 (CAN) HORIZONTAL STAB REINFORCEMENT BRACKET REPLACED WITH HEAVIER REPLACEMENT PART SUPPLIED THROUGH CESSNA. 1 H 7 1 3O 3 O 3A21 E8CE 5 C P21EA 1997030600671 19970306 00671 CE 1997 3 6 CA960826028 1 19960812 A 3411 503242699 TUBE BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA STATIC SYS NO FLARE W K NONE O OTHER IN INSP/MAINT 1 CA PCE50944 (CAN) WHILE PERFORMING A STATIC SYSTEM LEAK CHECK IT WAS FOUND THAT THE TUBE DID NOT HAVE A FLARE ON THE END. 1 L 7 2 3T 4 T A14CE E4EA 1997030600673 19970306 00673 SO 1997 3 6 CA960826063 1 19960620 A 3260 4793802 SWITCH PIPER PA31T PA31T 7103124 SO PWA PT6 PT6A28 EA NLG UPLOCK FAULTY W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA PCE50170 (CAN) LANDING GEAR WOULD NOT COMPLETE THE RETRACT CYCLE. TROUBLESHOOTING FOUND THE NOSE GEAR UPLOCK LIMIT SWITCH TO BE A T FAULT. FAULT CORRECTED. 1 L 7 2 3T 4 T A8EA E4EA 1997030600677 19970306 00677 EU 1997 3 6 CA960826080 1 19960806 A 2434 ALU8421LS BEARINGS PRESTOLITE ALU8421LS ZLIN 242 Z242L 9970204 EU GENERATOR SEIZED W A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CR CRUISE 1 CA 511 5012841 (CAN) GENERATOR LIGHT ILLUMINATED IN FLIGHT. AIRCRAFT LANDED AND MAINTENANCE FOUND THE BEARINGS SEIZED. ALTERNATOR REPLA CED AND AIRCRAFT RETURNED TO SERVICE. 1 L 7 1 3O 0 A76EU 1997030600678 19970306 00678 GL 1997 3 6 CA960826084 1 19960807 A 2460 W23X1A1G3 CIRCUIT BREAKER DIAMON DA20A1 DA20A1 05626UX GL DC DIST FAILED W O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 CA 460 460 (CAN) CIRCUIT BREAKER WILL NOT RESET. 1 L 7 1 3O NT TA4CH 1997030600679 19970306 00679 EU 1997 3 6 CA960826086 2 19960724 A 8550 911674 HOUSING DIAMON DA20A1 DA20A1 05626UX GL ROTAX 912 ROTAX912 55555 EU OIL PUMP STRIPPED W A UNSCHED LANDING O K M OTHER FLUID LOSS OVER TEMP CR CRUISE 1 CA 727 (CAN) PILOT NOTED THE OIL TEMPERATURE HIGH AND ELECTED TO LAND. MAINTENANCE FOUND AN OIL LEAK AT THE "BANJO" FITTING AND TRIED TO VERIFY THE TORQUE BUT FOUND THE THREADS WERE STRIPPED. 1 L 7 1 3O 3 I NT TA4CH EXPE3I 1997030600680 19970306 00680 1997 3 6 CA960826089 4 19960812 A 3418 P004 STALL WARNING DIAMON DIAMON DA20A1 DA20A1 05626UX GL UNDER PILOT SEAT WATER IN TUBE W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) STALL WARNING SYSTEM. WATER FOUND IN THE TUBING. WARNING SYSTEM INOPERATIVE DUE TO WATER IN THE TUBE. NO WAY TO VI SUALLY INSPECT PRIOR TO FLIGHT. TUBING THAT COLLECTED WATER WAS AS DESIGNED UNDER THE PILOTS SEAT. 1 L 7 1 3O NT TA4CH 1997030600681 19970306 00681 CE 1997 3 6 CA960826091 1 19960813 A 7603 16938008413 CABLE BEECH 23 C23 1151242 CE LYC O360 O360A4K 41514 EA THROTTLE INNER BROKEN W D RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 CA L2239036A (CAN) AT RUN-UP THE PILOT NOTED THAT THE ENGINE DID NOT RESPOND TO THROTTLE INPUT. THE ENGINE WAS SHUTDOWN BY THE MIXTUR E CONTROL AND THE AIRCRAFT TOWED TO THE HANGAR. MAINTENANCE FOUND THE INNER CABLE OF THE THROTTLE CABLE BROKEN. 1 L 7 1 3O 3 O A1CE E286 1997030600682 19970306 00682 CE 1997 3 6 CA960826092 1 19960809 A 5511 053200123 SPAR CESSNA 172 172N 2072434 CE LYC O320 O320H2AD 41508 EA MCAULY 1C160 1C160DTM GL HORIZ STAB CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 5063 L341576 734345 (CAN) DURING INSPECTION A CRACK WAS DETECTED IN THE CENTRE OF THE SPAR. SPAR WAS REPLACED. CRACKED DETECTED WAS APPROXIM ATELY 1 INCH LONG. 1 H 7 1 3O 3 O NT 3A12 E274 5 N P910 1997030600684 19970306 00684 EA 1997 3 6 CA960927004 2 19960527 A 7261 MS9388115 O-RING BEECH 5038912115 BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA CHIP DET UNDERSIZED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA PCE81939 (CAN) WHILE CARRYING OUT MAINTENANCE ON AN ENGINE THE INSPECTION OF THE REDUCTION GEARBOX CHIP DETECTOR REQUIRED THE REP LACEMENT OF AN O-RING. IN DRAWING THE O-RING FROM STORES THE AME NOTED THE SIZE OF THE NEW O-RING WAS NOT THE SAME AS TH AT OF THE ONE REMOVED. AS OTHER O-RINGS WERE INSPECTED IT APPEARS THAT THIS IS AN ISOLATED CASE. 1 L 7 2 4T 4 T A24CE E4EA 1997030600685 19970306 00685 GL 1997 3 6 CA960927005 1 19960922 A 3243 MC4D CYLINDER DIAMON MC4D DIAMON DA20A1 DA20A1 05626UX GL COPILOT BRAKE LOW PRESSURE W K NONE K O FLUID LOSS OTHER LD LANDING 1 CA (CAN) BOTH LEFT AND RIGHT MASTER CYLINDERS ON THE CO-PILOTS SIDE FAIL TO PRODUCE ADEQUATE PRESSURE FOR BRAKING. PILOT'S CYLINDERS SEEM TO WORK WELL. THE SUBMITTER STATES THAT THE FLUID IN THE CYLINDERS APPEARS DIRTY AND SPECULATES THAT THER E COULD BE SOME O-RING DETERIORATION. 1 L 7 1 3O NT TA4CH 1997030600686 19970306 00686 GL 1997 3 6 CA960927006 1 19960918 A 2701 CONTROL COLUMN DIAMON DIAMON DA20A1 DA20A1 05626UX GL COCKPIT JAMMED W O OTHER F FLT CONT AFFECTED CR CRUISE 1 CA (CAN) AFTER PERFORMING SPINS AND STALLS, THE PILOT NOTED THAT HE COULD NO LONGER MOVE THE STICK FORWARD FROM THE NEUTRA L POSITION. THE TRIM WAS ALSO INEFFECTIVE. AFT MOVEMENT OF THE STICK AND TRIM WERE POSSIBLE. MAINTENANCE FOUND THAT THE RUDDER PEDAL ADJUSTMENT CABLE 'T' HANDLE WAS JAMMED BETWEEN THE STICK AND THE SEAT PAN. THE LEATHER CONTROL STICK SHROU D WAS IN PLACE. THE 'T' HANDLE WAS ON TOP OF THIS LEATHER SHROUD. 1 L 7 1 3O NT TA4CH 1997030600687 19970306 00687 CE 1997 3 6 CA960927007 1 19960918 A 2434 C6115020204 ALTERNATOR CESSNA 337 337G 2075730 CE CONT O360 IO360G 17025 SO MCAULY 2AF34C D2AF34C306 GL DC SYS BROKEN DRIVE W K NONE H ELECT. POWER LOSS-50 PC CR CRUISE 1 CA 493 352436 754603 (CAN) THE ALTERNATOR FAILED IN FLIGHT AND GROUND INSPECTION REVEALED THE DRIVE SHAFT HAD SHEARED. 1 H 7 2 3O 3 O A6CE E1CE 5 C P5EA 1997030600688 19970306 00688 SO 1997 3 6 CA960930001 2 19960906 A 8550 639388 SCAVENGE PUMP CESSNA 340 340A 2076405 CE CONT O520 TSIO520N 17040 SO MCAULY 3AF32C 3AF32C93 GL #2 ENGINE CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 1637 1089 R509130N 760963 (CAN) AFTER LANDING THE PILOT NOTICED A LARGE OIL LEAK ON #2 ENGINE. FURTHER INSPECTION REVEALED THE SCAVENGE PUMP HOUSI NG WAS CRACKED. A NEW PUMP WAS INSTALLED AND THE AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 3O 3 O 3A25 E8CE 5 C P22EA 1997030600689 19970306 00689 CE 1997 3 6 CA960930002 1 19960514 A 3250 50420101 BELLCRANK CESSNA 5842000207 CESSNA 310 310R 2074245 CE CONT O520 IO520M 17032 SO MCAULY 3AF32C 3AF32C87 GL NLG STEERING CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA L565389 745544 (CAN) NOSE WHEEL STEERING BELLCRANK CRACKED IN THE RADIUS OF THE MAIN ATTACH PIVOT POINT AT ALL FOUR CORNERS. 1 L 7 2 3O 3 O 3A10 E5CE 5 C P22EA 1997030600690 19970306 00690 NE 1997 3 6 CA960930004 2 19960919 A 7320 310102101 LP COMPRESSOR CESSNA 500 500CESSNA 2076602 CE PWA JT15 JT15D1 52060 NE #1 ENGINE FOD DAMAGE W K NONE C F.O.D. TO TAKEOFF 1 CA 7041 772 PCE76308 (CAN) ON DEPARTURE, A SCREECHING SOUND WAS HEARD FROM #1 ENGINE, SINCE ALL ENGINE PARAMETERS WERE NORMAL THE FLIGHT CONT INUED. AFTER LANDING AND ENGINE SHUTDOWN SUBSTANTIAL DAMAGE WAS OBSERVED TO THE FAN. FURTHER INSPECTION REVEALED DAMAGE ALSO TO THE STATOR AND THE T1 SENSOR. THE #1 ENGINE WAS REMOVED FOR REPAIR. THE CAUSE OF THE FOD WAS NOT DETERMINED. IT WAS NOT A BIRD STRIKE AND ALL THE FASTENERS WERE ACCOUNTED FOR. 1 L 7 2 4F 4 F A22CE E1NE 1997030600691 19970306 00691 EU 1997 3 6 CA961001002 1 19960914 A 5280 A11320448 DOOR FOKKER A11320448 FOKKER F28 F28MK1000 4990808 EU RT MLG CRACKED W O OTHER J WARNING INDICATION CR CRUISE 1 CA SH151 (CAN) INBOUND R/H MAIN LANDING GEAR INDICATION UNSAFE ON GEAR DOWN SELECTION - 3 GREEN AND R/H RED - GEAR RECYCLED LANDI NG OK. AIRCRAFT SAFE FOR FERRY FLIGHT TO TORONTO (YYZ). R/H DOOR REPLACED DUE TO ONE FOOT CRACK FROM THE ACTUATOR INBOAR D. DOOR REPLACED. NEXT FLIGHT PASSING THROUGH FL210 R/H MLG WARNING LIGHT CAME ON, GEAR RECYCLED OK. DOORS RERIGGED AND GROUND SWING CARRIED OUT SERVICEABLE. 2 L 7 2 4F RT A20EU 1997030600692 19970306 00692 NM 1997 3 6 CA961001004 1 19960823 A 3260 BULBS DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE GEAR POSITION BURNT W L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 CA 123071 (CAN) ON APPROACH AFTER GEAR SELECTED DOWN, GEAR POSITION LIGHTS NOT ON. CREW DID GO AROUND, AND BULBS REPLACED IN SIDE INDICATORS. 2 H 7 2 4T 4 T RT A13NM E20NE 1997030600708 19970306 00708 NE 1997 3 6 97ZZZX931 2 19960725 A 7250 411105064 ROTOR ASSY BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE GAS PRODUCER DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 117CW 2265 4326 7125 LE45295E GAS PRODUCER ROTOR ASSY DUE SB LT101-72-10-0150. REQUIRES DISASSEMBLY AND INSPECTION OF THE ROTOR BROACH SLOTS FOR POSS IBLE CRACKS IN THE DISC/TENON AREA. REPLACED WITH NEW UNIT CORRECT PROBLEM. PART TOTAL CYCLES 3.701.7. 1 G 7 2 3U 3 U H13EU E5NE 1997030600709 19970306 00709 NE 1997 3 6 97ZZZX932 2 19961125 A 7250 411105064 ROTOR ASSY BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE GAS PRODUCER DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 586BH 2192 4243 7129 LE45144 GAS PRODUCER ROTOR ASSY DUE SB LT101-72-10-0150. REQUIRES DISASSEMBLY AND INSPECTION OF THE ROTOR BROACH SLOTS FOR POSS IBLE CRACKS IN THE DISC/TENON AREA. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. PART TOTAL CYCLES, 4,271.2. 1 G 7 2 3U 3 U H13EU E5NE 1997030600713 19970306 00713 GL 1997 3 6 97ZZZX936 2 19961216 A 7322 23059933 FUEL CONTROL BELL 206 206L4 1182110 SW ALLSN 250C 250C30P 03013 GL ENGINE LEAK A ALGA K NONE O B OTHER SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 03 173AL 5980 20 BR52265 52066 EN ROUTE, STRONG SMELL OF FUEL WAS NOTICED IN THE COCKPIT. INITIALLY SUSPECTED ONE OF THE PASSENGERS WHO HAD PREVIOUSLY REFUELED AIRCRAFT HAD GOTTEN FUEL ON HIS CLOTHING. AFTER LANDING, FUEL WAS OBSERVED COMING FROM FUEL CONTROL UNIT. FO UND FUEL CONTROL LEAKING AT METERING VALVE. REMOVED AND REPLACED FUEL CONTROL. PERFORMED REQUIRED MAINTENANCE PROCEDUR ES. AIRCRAFT RETURNED TO SERVICE. 1 G 7 1 3U 3 U NC H2SW E1GL 1997031100006 19970311 00006 SO 1997 3 11 CA960418004 1 19960402 A 8120 LW12778 WASTE GATE PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA LIP TORN SEAL W E A ENGINE SHUTDOWN UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CL CLIMB 1 CA 1 L165968A (CAN) WASTE GATE LIP SEAL TORN AND ENGINE OIL PUMPED OUT THROUGH CASE DRAIN CAUSING DROP IN OIL PRESSURE AND FORCED SHUT DOWN OF ENGINE. THIS WAS A NEWLY OVERHAULED ENGINE WITH 1.3 HOURS OF OPERATING TIME. 1 L 7 2 3O 3 O A20SO E14EA 1997031100008 19970311 00008 GL 1997 3 11 CA960826082 1 19960716 A 7910 MA2210164 CHECK VALVE DIAMON DA20A1 DA20A1 05626UX GL ROTAX 912 ROTAX912 55555 EU ENG OIL LEAKING W K NONE O OTHER IN INSP/MAINT 1 CA 425 4380734 (CAN) CHECK VALVE FAILED INTERNAL LEAK TEST. 1 L 7 1 3O 3 I NT TA4CH EXPE3I 1997031100009 19970311 00009 CE 1997 3 11 CA960927008 1 19960830 A 6120 3011213 CLAMP CESSNA 208 208 2073702 CE MCAULY 3G34C7 3GFR34C701 GL PROP LINKAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 96 960697 (CAN) PILOT REPORTED A SLIGHT FLUCTUATION OF TORQUE AND FUEL FLOW. DURING TROUBLESHOOTING A PIECE OF A SPECIAL BOLT WAS FOUND IN THE LOWER COWLING. FURTHER INVESTIGATION REVEALED THIS PIECE WAS PART OF A CLAMP FROM THE PROPELLER REVERSING I NTERCONNECT LINKAGE (REAR) USED TO CLAMP THE WIRE ROPE INSIDE THE TERMINAL. THE FAILURE MAY HAVE BEEN DUE TO OVERTORQUIN G. 1 H 7 1 3T NT A37CE 5 C P60GL 1997031300058 19970313 00058 NE 1997 3 13 97ZZZX989 2 19961222 A 7230 UL25713 RUB STRIP BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE C1 COMPRESSOR DISBONDED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 518AT 123 42 27974 31451 DURING PRE-FLIGHT PIC NOTED THE NR 2 ENGINE C1 COMPRESSOR WOULD NOT TURN. FURTHER INSPECTION REVEALED THE SEGMENTED LIN ING ASSY (RUB STRIP) WAS DISBONDED IN THE UPPER SECTION OF THE ENGINE (FROM 4 O'CLOCK TO 10 O'CLOCK POSITION). THE NR 2 ENGINE WAS REMOVED AND REPLACED IAW MM, ALL CHECKS WERE SATISFACTORY, NO LEAKS NOTED. (X) 2 L 7 2 4F 4 F RT A2NM E12EU 1997031300059 19970313 00059 NM 1997 3 13 USAABB97012 1 19960115 A 3350 86210066 BATTERIES BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 628AU 27806 LAX - FOUND EMERGENCY FLOOR LIGHT BATTERIES INOPERATIVE AT ROWS 1, 9, AND 23. REPLACED BATTERIES. (X) 2 L 7 2 4F RT A2NM 1997031300064 19970313 00064 WP 1997 3 13 AALA961879 1 19961218 A 5320 SHIM DOUG DC10 DC1010 3022110 WP BS 1761 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 130AA 46989 TUL - SHIM CORRODED BETWEEN SKIN AND CASTING. MANUFACTURED AND INSTALLED NEW SHIM. TST: 57,695. CYCLES, 19,464. (X) 2 L 7 3 4F A22WE 1997031300065 19970313 00065 WP 1997 3 13 AALA961880 1 19961218 A 5320 PAN DOUG DC10 DC1010 3022110 WP LAV SERV PNL CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 130AA 46989 TUL - CORROSION AROUND FLANGE OF PAN ON SIDE IN CONTACT WITH SKIN. REPLACED PAN WITH NEW. TST: 57,695 HOURS. CYCL ES, 19,464. (X) 2 L 7 3 4F A22WE 1997031300066 19970313 00066 WP 1997 3 13 AALA961842 1 19961218 A 5320 CUSP DOUG DC9 DC982 3022082 WP BS 1149-1174 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 489AA 49682 TUL - CUSP MEMBRANE CORRODED RIGHT SIDE. REMOVED CORRODED AREA BY CUTTING OUT A PORTION OF CUSP MEMBRANE FROM STA 1145 TO STA 1174 RT. FABRICATED DOUBLER FROM .31 INCH 7075-T6 AND INSTALLED WET WITH SEALANT PER SRM 53-0, PAGE 17, FIGURE 4 , SHEET 3. TST: 23,581 HOURS. CYCLES, 13,157. (X) 2 L 7 2 4F A6WE 1997031300067 19970313 00067 WP 1997 3 13 AALA961883 1 19961218 A 5347 TIE DOWN TRACK DOUG DC9 DC982 3022082 WP BS 1155-1300 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 489AA 49682 TUL - LEFT CARGO TIE-DOWN TRACK CORRODED FROM STA 1155 - STA 1300 AROUND CENTER FASTENERS AND HOLES. TREATED, PRIMED TI E-DOWN TRACK FROM STA 1155 TO STA 1222. REMOVED OUT OF LIMITS TRACK FROM STA 1222 TO STA 1322. INSTALLED NEW TIE-DOWN T RACK, LT CARGO FROM STA 1222 TO STA 1322. INSTALLED PER SRM 53-05, FIGURE 45. TST: 23,581 HOURS. CYCLES, 13,157. (X ) 2 L 7 2 4F A6WE 1997031300068 19970313 00068 WP 1997 3 13 AALA961884 1 19961218 A 5320 MEMBRANE DOUG DC9 DC982 3022082 WP BS 1022-1095 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 489AA 49682 TUL - CUSP MEMBRANE CORRODED FROM STA 1022 TO STA 1098, LT SIDE. REPLACED CUSP MEMBRANE FROM STA 1022 TO STA 1098 PER S RM 53-01, FIGURE 4, SHEET 3. (X) 2 L 7 2 4F A6WE 1997031300082 19970313 00082 CE 1997 3 13 MASA97004 1 19961126 A 2612 24409015 FIRE LOOP BEECH 1900 1900D 1154162 CE LT ENGINE BROKEN A MASA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 01 144ZV UE144 HVN - FLT 5362 - A FALSE FIRE WARNING FLICKERED IN-FLIGHT. PILOT VERIFIED ENGINE WAS NOT ON FIRE AND OPTED TO DIVERT TO ISP. FERRY PERMIT WAS ISSUED ISP/RDG. FOUND FAULT TO BE AFT FIRE LOOP. REMOVED AND REPLACED AFT FIRE LOOP. (X) 2 L 7 2 4T RT A24CE 1997031300085 19970313 00085 NM 1997 3 13 97ZZZX1001 1 19961228 A 3320 1011801 LIGHTS DHAV DHC8 DHC8202 2809007 NM AIRSTAIR DOOR FAILED A MASA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 01 449YV 449 AIRCRAFT TAXIED FROM GATE IN DENVER WHEN FLIGHT ATTENDANT INFORMED CREW THERE WAS ELECTRICAL SMOKE AROUND THE AIRSTAIR D OOR. AIRCRAFT RETURNED TO GATE. AIRCRAFT WAS INSPECTED BY MAINTENANCE AND SMOKE WAS DETERMINED TO HAVE COME FROM THE A IRSTAIR DOOR LIGHTS. AIRSTAIR DOOR LIGHTS WERE DEFERRED AND CIRCUIT BREAKER WAS TIE-WRAPPED. AIRCRAFT RETURNED TO SERV ICE. (X) 2 H 7 2 4T RT A13NM 1997031300088 19970313 00088 EU 1997 3 13 RAIA961285 1 19961230 A 7332 1103P0645 PRESSURE SWITCH BAG JETSTM JETSTM3201 1500217 EU GARRTT LT ENGINE INOPERATIVE A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 864AE 490 864 FAT - FLT 4734 - LEFT FUEL LOW PRESSURE CAP LIGHT ILLUMINATED ON TAKEOFF ROLL. REPLACED FUEL LOW PRESSURE SWITCH. (X) 2 L 7 2 4T RT A56EU 1997031300089 19970313 00089 EU 1997 3 13 97ZZZX1002 1 19961228 A 2121 EVT3454G FAN TECHNOFAN AIRBUS 320 A320231 3930325 EU E/E COMPT FAILED A P9RA O OTHER J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 09 302ML 3612 379 338 ECAM MESSAGE 'EXTRACT FAULT'. CREW REPORTED GRINDING NOISE AND ODOR OF BURNED ELECTRICAL EQUIPMENT. REPLACED AVIONICS COOLING FAN. 2 L 7 2 4F RT A28NM 1997031300226 19970313 00226 CE 1997 3 13 97ZZZX1046 1 19960508 A 7120 56541095 MOUNT BEAM CESSNA 402 402C 207590R CE FWD MT PAD CRACKED A S A HYIA K NONE O OTHER IN INSP/MAINT 1 NE 01 1376G 13382 402C0271 ESTIMATED CYCLES = 28,000. ESTIMATED ENGINE CHANGES = 70. LEFT ENGINE OUTBOARD BEAM FOUND CRACKED AT FORWARD MOUNT LO CATION BETWEEN NUTPLATE HOLES. 1 L 7 2 3O A7CE 1997031300249 19970313 00249 NE 1997 3 13 CA961001005 2 19960917 A 7414 C28406 LEAD TITEFLEX D25388 DOUG DC4 C54A 3021512 WP PWA R2000 R20007M2 52023 NE #3 ENG HI TENSIO FAULTY W E ENGINE SHUTDOWN E VIBRATION/BUFFET CR CRUISE 1 CA 969 BP701790 (CAN) #3 ENGINE BEGAN RUNNING ROUGH IN CRUISE. PRECAUTIONARY SHUT DOWN WAS CARRIED OUT. POST FLIGHT INSPECTION FOUND A S HORT TO GROUND HIGH TENSION LEAD FROM THE LEFT MAGNETO TO THE DISTRIBUTOR BLOCK. LEFT HIGH TENSION LEAD AND FRON TSPARK PLUG REPALCED. ENGINE GROUND CHECKED SERVICEABLE. 2 L 7 4 4R 4 R A762 5E5 1997031300250 19970313 00250 GL 1997 3 13 CA961001007 3 19960723 A 6110 PROPELLER DHAV DHC6 DHC6300 EA PWA PT6 PT6A27 52043 EA HARTZL HCB3T HCB3TN3 GL #2 ENGINE SURGING W K NONE O OTHER AP APPROACH 1 CA 23147 160 PCE41402 BU2864 (CAN) ON APPROACH WITH THE POWER LEVERS AT 10 PSI TORQUE AND THE PROPELLER LEVERS FULL FORWARD. THE POWER LEVERS WERE BR OUGHT UP TO 20 PSI TORQUE. THE PROPELLER RPM ON THE RIGHT HAND PROPELLER WOULD DROP OFF FROM 94 PERCENT TO 84 PERCENT AN D THEN GO BACK TO 94 PERCENT. THE R/H PROPELLER KEPT SURGING/SEEKING UNTIL THE POWER WAS INCREASED OR THE PROPELLER LEVE RS WERE BROUGHT BACK TO MINIMUM GOVERNING. THE PROBLEM COULD NOT BE DUPLICATED ON THE GROUND. REPLACEMENT OF THE R/H PRO PELLER RECTIFIED THE PROBLEM. 1 H 7 2 3T 4 T A9EA E4EA 6 C P15EA 1997031300251 19970313 00251 WP 1997 3 13 CA961001010 1 19960904 A 2530 OVEN DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE GALLEY ACRID ODOUR W K NONE O B OTHER SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA P656873D (CAN) PRIOR TO DEPARTURE, BURNING ODOUR PRESENT IN GALLEY. ELECTRICAL RECEPTACLES CHECKS OK. OVEN REPLACED. 2 L 7 2 4F 4 F A6WE E2EA 1997031300252 19970313 00252 EU 1997 3 13 CA961001011 1 19960908 A 2130 87292325V04 EXTRACT VALVE AIRBUS 320 A320211 3930320 EU SKIN AIR INOPERATIVE W A UNSCHED LANDING O OTHER CL CLIMB 1 CA (CAN) UNABLE TO PRESSURIZE AIRCRAFT ON DEPARTURE. AIRCRAFT RETURNED TO DEPARTURE POINT. MAINTENANCE CHECK FOUND SKIN AI R EXTRACT VALVE INOPERATIVE. VALVE DID NOT CLOSE CAUSING PRESSURIZATION PORBLEM. AVIONICS EXTRACT VALVE COMPUTER REPLACE D. 2 L 7 2 4F RT A28NM 1997031300254 19970313 00254 EA 1997 3 13 CA961002001 1 19960926 A 2612 3039875 FIRE DETECT LINE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE B-LOOP NR 1 ENG BROKEN W D RETURN TO BLOCK J N WARNING INDICATION FALSE WARNING TX TAXI/GRND HDL 1 CA 123151 (CAN) #1 ENGINE 'FAULT B' FIRE DETECT ON DURING TAXI. B LOOP FOUND BROKEN AT SENSOR BODY ON P2.5 LINE. 2 H 7 2 4T 4 T RT A13NM E20NE 1997031300255 19970313 00255 NM 1997 3 13 CA961002002 1 19960926 A 3244 265X813 TIRE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE MLG BLOWN W O OTHER O OTHER LD LANDING 1 CA 120226 (CAN) TIRE BLEW ON LANDING. A 4" RADIAL SPLIT. 2 H 7 2 4T 4 T RT A13NM E20NE 1997031300256 19970313 00256 EA 1997 3 13 CA961002003 1 19960818 A 3233 6227B15 O-RING WIPLINEINC 6A0500006 DHAV DHC2 DHC2MK3 2800107 EA PWA PT6 PT6A27 52043 EA LT MLG ACTUATOR FAILED W K NONE K FLUID LOSS LD LANDING 1 CA PCE52332 (CAN) LANDING GEAR FAILED TO OPERATE DUE TO LOSS OF ALL HYDRAULIC FLUID BECAUSE OF A FAILED O-RING IN THE LEFT MAIN GEAR ACTUATOR. THIS RESULTED IN A GEAR UP LANDING WITH NOSE GEAR DOWN AND MAIN GEAR UP. MAJOR KEEL DAMAGE TO BOTTOM OF BOTH FLOATS. SUBMITTER SUGGESTS THAT WIPLINE SL #28 BE MANDATORY. 1 H 7 1 3T 4 T A806 E4EA 1997031300257 19970313 00257 EA 1997 3 13 CA961002004 2 19960820 A 7322 252414511 FUEL CONTROL BENDIX PIPER PA30 PA30 7103002 SO LYC O320 IO320B1A 41508 EA ENGINE FAULTY W E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CR CRUISE 1 CA 870 L484355A (CAN) FUEL CONTROL UNIT FAILED. 1 L 7 2 3O 3 O A1EA 1E12 1997031300258 19970313 00258 SW 1997 3 13 CA961002005 1 19960828 A 2720 705241 CONTROL CABLE AIRTRC AT802 AT802 0390305 SW RUD FAIR LEADS DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA 97 (CAN) DURING INSPECTION IT WAS NOTED THAT THE RUDDER CONTROL CABLES WERE BLENDED AT THE FAIRLEADS WHERE THE CABLES EXIT THE FUSELAGE IN THE TAIL SECTION. SUBMITTER STATES THAT AIR TRACTOR SERVICE LETTER #77 ADDRESSES THIS ISSUE AND ADDS THE BLENDING IS WITHIN SPECIFIED LIMITS. 1 L 7 1 3T NC A19SW 1997031300262 19970313 00262 NE 1997 3 13 CA961002010 2 19960918 A 8530 446888 CYLINDER DOUG DC4 C54A 3021512 WP PWA R2000 R20007M2 52023 NE NR 6 RKR BOX BROKEN W A E A ENGINE SHUTDOWN UNSCHED LANDING E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CL CLIMB 1 CA 965 P106106 (CAN) #2 ENGINE BEGAN TO RUN ROUGH AND BACKFIRE IN CLIMB. ENGINE WAS SHUTDOWN AND AIRCRAFT RETURNED TO BASE. POST FLIGHT INSPECTION FOUND THE #6 CYLINDER EXHAUST ROCKER BOX SECTION BROKEN LOOSE FROM THE CYLINDER CAUSING THE EXHAUST VALVE TO REMAIN CLOSED. #6 CYLINDER REPLACED, ENGINE OIL SCREENS INSPECTED, ENGINE GROUND RUN SERVICEABLE AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4R 4 R A762 5E5 1997031300263 19970313 00263 CE 1997 3 13 CA961002011 1 19960920 A 3260 95361015601 SWITCH BEECH BEECH 95 95B55 1152729 CE CONT O470 IO470L 17026 SO MLG SAFETY BROKEN WIRE W K NONE O OTHER CL CLIMB 1 CA CS192942R (CAN) AFTER A MISSED APPROACH THE GEAR FAILED TO RETRACT. INSPECTION REVEALED THAT A WIRE HAD BROKEN IN THE LANDING GEAR SAFETY SWITCH BUNDLE AT THE LOCATION WHERE THE BUNDLE FLEXES DURING GEAR CYCLING. 1 L 7 2 3O 3 O RT 3A16 3E1 1997031300264 19970313 00264 NM 1997 3 13 CA961002013 1 19960921 A 3233 AC252B40124 HOSE AEROQUIP DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE NLG DRAG STRUT RUPTURED W A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 CA 15575 123141 (CAN) DURING GEAR RETRACTION ALL APPROPRIATE CAUTION LIGHTS INDICATING FAILURE OF #2 HYDRAULIC SYSTEM CAME ON. THE NOSE LANDING GEAR DRAG STRUT ACTUATOR FLEX UP LINE WAS FOUND RUPTURED, CAUSING A LOSS OF FLUID IN #2 SYSTEM. 2 H 7 2 4T 4 T RT A13NM E20NE 1997031300265 19970313 00265 EA 1997 3 13 CA961002014 1 19960924 A 7712 30005000046 TQ SIGNAL COND SIMMONDS DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE #2 ENGINE FAULTY W A A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 CA 11715 11715 1871 123142 (CAN) JUST AFTER TAKEOFF, DURING CLIMB OUT AT APPROXIMATELY 600 FEET WITH BOTH ENGINES AT 90 PERCENT TORQUE, THE #2 ENGI NE HAD A UNCONTROLLABLE AUTOFEATHER WITH AN UPTRIM TO 105 PERCENT ON #1 ENGINE, #2 ENGINE OVERTORQUED TO 125 PERCENT FOR APPROXIMATELY 20 SECONDS. #1 TORQUE SIGNAL CONDITIONING UNIT (TSCU) FOUND TO BE AT FAULT AND REPLACED. #2 TSCU REPLACED AS A PRECAUTIONARY MEASURE. #2 PROPELLER WAS REPLACED DUE TO OVERTORQUE. 2 H 7 2 4T 4 T RT A13NM E20NE 1997031300266 19970313 00266 CE 1997 3 13 CA961002015 1 19960731 A 7120 05131323 MOUNT CESSNA 05131323 CESSNA 172 R172K 2072431 CE CONT O360 IO360KB 17025 SO MCAULY 2A34C 2A34C203 GL LT TOP STRINGER CRACKED W A K NONE O OTHER IN INSP/MAINT 1 CA 4483 256240H 799461 (CAN) DURING ROUTINE INSPECTION THE AME NOTICED UNUSUAL MOVEMENT IN THE ENGINE COWLING. INVESTIGATION FOUND THE STEEL EN D FITTING ON THE LEFT HAND UPPER ENGINE MOUNT STRINGER ON THE AFT FACE OF THE FIREWALL TO BE SEVERELY CRACKED. THE ENGIN E MOUNT WAS FOUND PULLED AWAY FROM THE FIREWALL STRUCTURE. 1 H 7 1 3O 3 O 3A17 E1CE 5 C P3EA 1997031300268 19970313 00268 CE 1997 3 13 CA961003002 1 19960813 A 2434 DOFF10300J ALTERNATOR FORD DUFF10300J CESSNA 172 172N 2072434 CE LYC O320 O320H2AD 41508 EA MCAULY 1C160 1C160DTM GL DC SYS FAILED W A UNSCHED LANDING H ELECT. POWER LOSS-50 PC NR NOT REPORTED 1 CA 2000 2000 RL295376A 733664 (CAN) THE AIRCRAFT RETURNED WITH A DEAD BATTERY. THE ALTERNATOR WAS FOUND TO HAVE NO OUTPUT. ALTERNATOR REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 1 H 7 1 3O 3 O NT 3A12 E274 5 N P910 1997031300269 19970313 00269 SW 1997 3 13 CA961003004 1 19960918 A 5751 27340001 BALANCE WEIGHT SWRNGN SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE3313UW 01514 WP LEFT HAND AIL BROKEN W A K NONE O OTHER IN INSP/MAINT 1 CA 25878 03453 (CAN) LEFT AILERON INBOARD BALANCE WEIGHT FOUND BROKEN AT CENTRE ATTACH BOLT. WEIGHT HAD BEEN CRACKED FOR SOME TIME. RES T OF FLEET OF 12 AIRCRAFT CHECKED AND 6 OTHERS FOUND WITH BROKEN BALANCE WEIGHTS AT SAME PLACE. ALL CRACKED BALANCE WEIG HTS FOLLOWED A SIMILAR PATTERN, THEY WERE ATTACHED WITH 3 BOLTS AND WERE CRACKED AND OR BROKEN AT ONE OR MORE HOLES. CRA CKS IN LEAD WEIGHTS DIFFICULT TO DETECT AS THE OXIDIZED SURFACE OF THE WEIGHT AND THE OXIDIZED SURFACE OF THE CRACK ARE VERY SIMILAR IN COLOUR. DETAILS FORWARDED TO MANUFACTURER. 2 L 7 2 4T 4 T RT A8SW E4WE 1997031300270 19970313 00270 SW 1997 3 13 CA961003005 1 19960918 A 5751 27340001 BALANCE WEIGHT SWRNGN SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP LT AILERON CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 27267 P54183 (CAN) LEFT AILERON 2ND FROM INBOARD BALANCE WEIGHT FOUND BROKEN AT 2 ATTACH HOLES. 6 OTHER AIRCRAFT SIMILAR IN FLEET OF 12. 2 L 7 2 4T 4 T RT A8SW E4WE 1997031300271 19970313 00271 SW 1997 3 13 CA961003006 1 19960918 A 5751 27340002 BALANCE WEIGHT SWRNGN SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP RT AILERON BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 24268 24268 P54143 (CAN) RIGHT AILERON BALANCE WEIGHT FOUND BROKEN AT CENTRE ATTACH HOLE. 6 OTHERS OF 12 AIRCRAFT FOUND WITH SAME PROBLEM. 2 L 7 2 4T 4 T RT A8SW E4WE 1997031300272 19970313 00272 SW 1997 3 13 CA961003007 1 19960918 A 5751 27340001 BALANCE WEIGHT SWRNGN SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP LT AILERON CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 23157 P54259 (CAN) LEFT AILERON ALL 3 BALANCE WEIGHTS FOUND CRACKED AT CENTRE HOLE. 6 OTHERS OF 12 AIRCRAFT FOUND WITH SAME PROBLEM. 2 L 7 2 4T 4 T RT A8SW E4WE 1997031300273 19970313 00273 SW 1997 3 13 CA961003008 1 19960918 A 5751 27340001 BALANCE WEIGHT SWRNGN SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP RT AIL INBD CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 21885 P54174 (CAN) RIGHT AILERON INBOARD BALANCE WEIGHT FOUND CRACKED AT CENTRE AND OUTBOARD ATTACH HOLES. 6 OF 12 OTHER AIRCRAFT FOU ND WITH SAME PROBLEM. 2 L 7 2 4T 4 T RT A8SW E4WE 1997031300274 19970313 00274 SW 1997 3 13 CA961003009 1 19960918 A 5751 27340002 BALANCE WEIGHT SWRNGN SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP RT AIL INBD CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 31819 P54082 (CAN) RIGHT AILERON INBOARD BALANCE WEIGHT FOUND CRACKED AT ATTACH HOLE. 6 OF 12 OTHER AIRCRAFT FOUND WITH SAME PROBLEM. 2 L 7 2 4T 4 T RT A8SW E4WE 1997031300275 19970313 00275 SW 1997 3 13 CA961003010 1 19960918 A 5751 27340001 BALANCE WEIGHT SWRNGN SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE3313UW 01514 WP LT AIL OUTBD CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 6564 P03551C (CAN) LEFT AILERON OUTBOARD BALANCE WEIGHT FOUND CRACKED AT CENTRE HOLE. 6 OF 12 OTHER AIRCRAFT FOUND WITH SIMILAR PROBL EM. 2 L 7 2 4T 4 T RT A8SW E4WE 1997031300276 19970313 00276 EA 1997 3 13 CA961007001 1 19960923 A 5740 MS90354 BOLT DHAV C2W11151 DHAV DHC2 DHC2MK1 2800102 EA PWA R985 R985AN14B 52008 NE UPPER STRUT LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA 54008 901 17954 (CAN) DURING 100 HOUR INSPECTION WING SHAKEN TO CHECK UPPER STRUT FITTING BOLT. MOVEMENT NOTICED IN THE RIVETS HOLDING S TRUT UPPER FITTING. THIS MOVEMENT FOUND IN BOTH STRUT UPPER FITTINGS. RH STRUT P/N C2W115-2. 1 H 7 1 3R 3 R A806 5E1 1997031300277 19970313 00277 NM 1997 3 13 CA961007002 1 19960924 A 2910 LINE BOEING 727 727172C 1384058 NM PWA JT8 JT8D7B 52053 NE NR 2 A PUMP LEAKING W A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CL CLIMB 1 CA 657595 (CAN) AFTER TAKEOFF "A" HYDRAULIC SYSTEM PRESSURE AND FLUID LOST. PRESSURE FLEX LINE FROM #2 "A" PUMP TO FIREWALLL LEAKI NG. REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 1997031300278 19970313 00278 NM 1997 3 13 CA961007003 1 19960925 A 2910 LINE BOEING 727 727172C 1384058 NM PWA JT8 JT8D7B 52053 NE A SYS HYD LEAKING W K NONE J K WARNING INDICATION FLUID LOSS CR CRUISE 1 CA 657595 (CAN) ENROUTE AIRCRAFT BEGAN TO LOSE "A" SYSTEM FLUID. UPON ARRIVAL #2 ENGINE PRESSURE QUICK DISCONNECT FOUND LEAKING AT "B" NUT. REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 1997031300280 19970313 00280 WP 1997 3 13 CA961007006 1 19960922 A 7810 C20055336 EXHAUST SEGMENT SOLAR DOUG DC4 C54EDC 3021528 WP PWA R2000 R20004 52023 NE #1 CYLINDER BLOWN OPEN W A E A ENGINE SHUTDOWN UNSCHED LANDING J M WARNING INDICATION OVER TEMP TO TAKEOFF 1 CA P107335 (CAN) #3 ENGINE FIRE WARNING LIGHT ILLUMINATED SHORTLY AFTER LIFTOFF. #3 ENGINE SHUTDOWN AND AIRCRAFT RETURNED TO POINT OF DEPARTURE. POST FLIGHT INSPECTION FOUND THE EXHAUST RING SEGMENT FROM #1 CYLINDER HAD OPENED UP AT THE TOP AREA AND A CTIVATED FIRE WARNING. METAL AT THE FAILED AREA OF THE EXHAUST RING SEGMENT IS MALLEABLE, WITH LITTLE OR NO SIGN OF BRIT TLEMENT. 2 L 7 4 4R 4 R A762 5E5 1997031300281 19970313 00281 NM 1997 3 13 CA961007007 1 19960927 A 3010 153212A DEICEVALVE DRAIN BENDIX DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE DIST VALVE PLUGGED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA RF4028 120657 (CAN) DRAIN HOLE OF DEICE DISTRIBUTION VALVE COMPLETELY PLUGGED BY POTTING COMPOUND CAUSING MALFUNCTION DUE TO EXCESSIVE ACCUMULATION OF MOISTURE. THE POTTING IS USED FOR INSTALLATION OF INTERNAL ELECTRIC HEATERS. 2 H 7 2 4T 4 T RT A13NM E20NE 1997031300282 19970313 00282 EA 1997 3 13 CA961007008 2 19960721 A 8550 A4427 CHIP DETECTOR DHAV DHC6 DHC6100 EA PWA PT6 PT6A20 52043 EA NOSE CASE GB BROKEN W E A ENGINE SHUTDOWN UNSCHED LANDING J K WARNING INDICATION FLUID LOSS TO TAKEOFF 1 CA 21565 PCE22424 (CAN) ON TAKEOFF OIL PRESSURE ON LEFT ENGINE STARTED DROPPING AND VISUAL INSPECTION NOTED OIL POURING FROM ENGINE COWLIN G. ENGINE SHUTDOWN AND AIRCRAFT RETURNED. CANNON PLUG ON CHIP DETECTOR WAS INSTALLED 180 DEGREES OUT AND WAS HITTING ON LOWER COWLING RIB. 1 H 7 2 3T 3 T A9EA E4EA 1997031300283 19970313 00283 NM 1997 3 13 CA961007017 1 19961001 A 7603 8760052001 CABLE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE RH COND LEVER FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA 18070 120443 (CAN) DURING 400 HOUR INSPECTION ON RIGHT HAND ENGINE, THE LOWER CONDITION CABLE WAS FOUND FRAYED WITH STRANDS BROKEN AP PROXIMATELY 24 INCHES AFT OF ENGINE CONTROL QUADRANT. 2 H 7 2 4T 4 T RT A13NM E20NE 1997031300284 19970313 00284 NM 1997 3 13 CA961007019 1 19960911 A 6120 7901802 PROP ACTUATOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE #2 ENGINE LEAKING OIL W E A ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CR CRUISE 1 CA 3835 120544 880923 (CAN) THIRTY MINUTES AFTER TAKEOFF THE FLIGHT CREW NOTICED LOW OIL PRESSURE CAUTION LIGHT ON #2 ENGINE. A PRECAUTIONARY SHUTDOWN WAS CARRIED OUT. FLUID LOSS WAS EVIDENT ON THE STARBOARD NACELLE. POST FLIGHT INVESTIGATION DETERMINED THE #2 P ROPELLER ACTUATOR WAS LEAKING. THE ACTUATOR WAS REPLACED AND THE AIRCRAFT WAS TEST FLOWN SERVICEABLE AND RETURNED TO SER VICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1997031300285 19970313 00285 WP 1997 3 13 CA961007021 1 19960919 A 7830 672772129 CLAMP LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB21122B02 54555 NE HP SOV BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 10285 (CAN) ON WALKAROUND FOUND 2 GAS GENERATOR FAIRINGS MISSING FROM #3 ENGINE. HP SHUT-OFF VALVE LOWER CLAMP BROKEN IN TWO P IECES AND HP PNEUMATIC PRESSURE FORCED TWO FAIRINGS TO SEPARATE. REPLACED. 2 L 7 3 4F 4 F A23WE E12EU 1997031300286 19970313 00286 EA 1997 3 13 CA961007022 1 19960927 A 2920 MS21908D4 ELBOW FITTING CNDAIR CL600 CL6002A12 1900304 EA GE CF34 CF341A NE NR 3 HYD SYS CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 4648 350157 (CAN) #3 SYSTEM HYDRAULIC BULKHEAD FITTING REAR OF VERTICAL STABILIZER REAR SPAR, BOTTOM PCV FOUND CRACKED ELBOW FITTING . REPLACED WITH STAINLESS FITTING. 2 L 7 2 4F 4 F RT A21EA E15NE 1997031300292 19970313 00292 EA 1997 3 13 CA961007031 2 19960912 A 7414 S6LN200 MAGNETO BENDIX PIPER PA23 PA23250 7102308 SO LYC O540 IO540C4B5 41532 EA #1 ENGINE FAULTY W K NONE O OTHER IN INSP/MAINT 1 CA 1047 32038 L1337648 (CAN) DURING INSPECTION OF THE #1 ENGINE, THE MAGNETO INPUT SHAFT NUT WAS FOUND SEPARATED FROM THE SHAFT. 1 L 7 2 3O 3 O 1A10 1E4 1997031300293 19970313 00293 EA 1997 3 13 CA961007032 2 19960912 A 7414 S6LN204 MAGNETO BENDIX PIPER PA23 PA23250 7102308 SO LYC O540 IO540C4B5 41532 EA #2 ENGINE CRACKED COIL W K NONE O OTHER IN INSP/MAINT 1 CA 542 C299304ER L937348 (CAN) DURING INSPECTION THE #2 ENGINE MAGNETO HAD A CRACKED COIL. 1 L 7 2 3O 3 O 1A10 1E4 1997031300294 19970313 00294 SO 1997 3 13 CA961009001 2 19961003 A 7322 6252192A21 FUEL CONTROL CESSNA 185 A185E 2072818 CE CONT O520 IO520D 17032 SO MCAULY 2A34C D2A34C58 GL MIXTURE CONTROL MISSING STOP PIN W A K NONE O OTHER IN INSP/MAINT 1 CA 570 570 293093R 712533 (CAN) PILOT REPORTED LOSS OF SPRING BACK IN MEXTURE FULL RICH POSITION AND REPORTED SOME RISE IN FUEL FLOW AS MIXTURE CO NTROL INITIALLY PULLED BACK FROM FULL RICH POSITION. INSPECTION FOUND FULL RICH STOP PIN MISSING. 1 H 7 1 3O 3 O 3A24 E5CE 5 C P3EA 1997031300299 19970313 00299 EU 1997 3 13 97ZZZX1068 1 19961227 A 3250 ES129707 BRACKET ISRAEL 1124 1124 4500102 EU NLG CRACKED A A ECAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 11 801SM 297 FLT 2 - NOSE WHEEL STEERING BINDING WHILE TAXIING FROM TERMINAL TO ACTIVE TAXIWAY. FOUND UPPER AND LOWER NOSE GEAR STEE RING ACTUATOR BRACKETS CRACKED. INSTALLED NEW BRACKETS. 2 M 7 2 4F A2SW 1997031300307 19970313 00307 NM 1997 3 13 AALA961751 1 19961202 A 2121 731378 EXHAUST FAN BOEING 757 757223 1384957 NM E/E COMPT DEFECTIVE A AALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 07 622AA 1466 24580 SJU - FLT T0672 - EN ROUTE STT/MIA DURING CRUISE, CABIN CREW REPORTED ELECTRICAL FUME SMELL IN CABIN. SMOKE DETECTORS I N FORWARD, MID, AND AFT CABIN LAVATORIES SOUNDED. AIRCRAFT DIVERTED TO SJU AND LANDED WITHOUT FURTHER INCIDENT. REPLAC ED NR 1 AFT EQUIPMENT VENTILATION FAN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1997031300308 19970313 00308 NM 1997 3 13 AALA961790 1 19961210 A 3350 21007 SWITCH BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST CR CRUISE 1 SW 07 631AA 24589 DFW - FLT T0600 - EN ROUTE SNA/DFW DURING CRUISE, EMERGENCY EXIT LIGHTS ILLUMINATED SEVERAL TIMES AND THEN EXTINGUISHED. AIRCRAFT PROCEEDED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED AFT CABIN EMERGENCY LIGHT TEST SWITCH. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1997031300442 19970313 00442 CE 1997 3 13 BSAA112096 1 19961120 A 8120 47090813 CONTROLLER CESSNA 402 402C 207590R CE RIGHT STICKING A BSAA O OTHER J WARNING INDICATION CL CLIMB 1 NM 05 2718Y 402C0232 BIL - RIGHT FUEL FLOW LAGGED AND THEN MANIFOLD PRESSURE SPIKED. STICKING WASTEGATE CONTROLLER. WASTEGATE CONTROLLER DI SASSEMBLED, CLEANED, INSPECTED, AND REASSEMBLED WITH NEW SEALS. THE OLD SEALS SHOWED SIGNS OF WEAR IN SOME AREAS. GROU ND RUN AND LEAK CHECKED OK. (M) 1 L 7 2 3O A7CE 1997031300443 19970313 00443 SW 1997 3 13 BSAA122396 1 19961223 A 3260 602EN6026 SWITCH SWRNGN SA226 SA226TC 8780404 SW HYD PACK INTERMITTENT A BSAA O OTHER N FALSE WARNING CL CLIMB 1 NM 05 116BS TC311 NOSE GEAR WOULD NOT UP AND LOCK. HYDRAULIC PACK CONTROL SWITCH INTERMITTENT. REPLACED UPLOCK HYDRAULIC PACK CONTROL SW ITCH. PERFORMED SEVERAL GEAR RETRACTION CHECKS TO VERIFY PROPER OPERATION. (M) 2 L 7 2 4T RT A8SW 1997031300444 19970313 00444 SW 1997 3 13 BSAA121196 1 19961211 A 3260 602EN6026 SWITCH SWRNGN SA226 SA226TC 8780404 SW HYD PACK INTERMITTENT A BSAA O OTHER N FALSE WARNING CL CLIMB 1 NM 05 115BS TC324 BIL - RIGHT GEAR WOULD NOT UP AND LOCK WHEN RETRACTION ATTEMPTED. SELECTED GEAR DOWN AND THREE GREEN LIGHTS ILLUMINATED AND LANDED WITHOUT INCIDENT. FOUND HYDRAULIC PACK CONTROL SWITCH INTERMITTENT. REPLACED HYDRAULIC PACK CONTROL SWITCH (PART NR 602EN602-6 BY MICROSWITCH). GEAR RETRACTION CHECKED OK. (M) 2 L 7 2 4T RT A8SW 1997031300445 19970313 00445 SO 1997 3 13 BSAAA111396 2 19961115 A 7313 6462108A1 FUEL PUMP CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO NR 2 ENGINE OUT OF ADJUST A BSAA O OTHER R PARTIAL RPM/PWR LOSS CL CLIMB 1 NM 05 2718Y 402C0232 BIL - RIGHT ENGINE SURGING. FUEL FLOW WAS GOING OVER RED LINE AND CAUSED THE ENGINE TO FLOOD OUT. ADJUSTED ENGINE DRIV EN FUEL PUMP TO SPECS/GROUND RUN OK. (M) 1 L 7 2 3O 3 O A7CE E8CE 1997031300565 19970313 00565 NM 1997 3 13 TWRA9709 1 19960916 A 5312 BULKHEAD WEB BOEING 747 747131 1384881 NM BS 2360 CRACKED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 608FF 19672 DURING D-SERVICE, FOUND FOLLOWING DISCREPANCIES, AFT PRESSURE BULKHEAD AT BS 2360, LOWER WEB AT LBL 15 TO RBL 15 ADJACEN T TO 'Y' CHORD CORRODED, CRACKED, AND PREVIOUS REPAIR INTERFERES WITH APU CUTOUT DOUBLER INSTALLATION (S/B 747-53-2275). REMOVED CENTER LOWER SECTION AROUND APU CUTOUT DUE TO CORROSION AND REPAIR DOUBLER. INSTALLED NEW WEB PER SRM 51-30-0 2, EA 53-114, SB 747-53-2275. (M) 2 L 7 4 4F A20WE 1997031300566 19970313 00566 NM 1997 3 13 TWRA9710 1 19960916 A 5312 BULKHEAD WEB BOEING 747 747131 1384881 NM BS 2360 CRACKED A TWRA K NONE O OTHER IN INSP/MAINT 1 EA 15 608FF 19672 DURING D-SERVICE, FOUND FOLLOWING DISCREPANCIES, AFT PRESSURE BULKHEAD AT BS 2360, AFT DOUBLER AT REAR OF LOWER WEB IS C HAFED, CRACKED AND CORRODED. REMOVED AND REPLACED WEB AND DOUBLER PER SRM 51-30-02. (M) 2 L 7 4 4F A20WE 1997031300567 19970313 00567 NM 1997 3 13 TWRA9711 1 19960916 A 5312 BULKHEAD FILLER BOEING 747 747131 1384881 NM BS 2360 CRACKED A TWRA K NONE O OTHER IN INSP/MAINT 1 EA 15 608FF 19672 DURING D-SERVICE, FOUND FOLLOWING DISCREPANCIES, AFT PRESSURE BULKHEAD AT BS 2360, AFT FILLER AT REAR OF LOWER WEB IS CH AFFED AND CRACKED BELOW APU DUCT CUTOUT. REMOVED AND REPLACED AFT FILLER PER SRM 51-30-02. (M) 2 L 7 4 4F A20WE 1997031300568 19970313 00568 NM 1997 3 13 TSAA9732006 1 19960130 A 3221 6545827501 TRUNNION BOEING 737 7372X6C 1384552 NM NLG CORROSION A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 816AL 23122 DURING C-CHECK VISIT, FOUND CORROSION ON NLG TRUNNION BOSS HOLE BORE. REPAIRED PER ECO 2383 R2. AIRCRAFT RETURNED TO S ERVICE. (M) 2 L 7 2 4F RT A16WE 1997031300569 19970313 00569 NM 1997 3 13 TWRA9708 1 19960916 A 5312 BULKHEAD CHORD BOEING 747 747131 1384881 NM BS 2360 MIS MANUFACTURED A TWRA K NONE O OTHER IN INSP/MAINT 1 EA 15 608FF 19672 DURING D-SERVICE, FOUND FOLLOWING DISCREPANCIES, AFT PRESSURE BULKHEAD AT BS 2360, LOWER 'Y' CHORD AT 0 BL TO RBL 10 HAS SHORT EDGE DISTANCE AT FASTENER HOLES . REPAIRED AS PER EA 47-5383-12-A0119, S/B 747-53-2275 REV 4. (M) 2 L 7 4 4F A20WE 1997031300570 19970313 00570 NM 1997 3 13 TWRA96318 1 19960916 A 5312 BULKHEAD WEB BOEING 747 747131 1384881 NM BS 2360 CORRODED A TWRA K NONE O OTHER IN INSP/MAINT 1 EA 15 608FF 19672 DURING D-SERVICE, FOUND FOLLOWING DISCREPANCIES, AFT PRESSURE BULKHEAD AT BS 2360, LOWER WEB AT RBL 15 TO RBL 30 ADJACEN T TO 'Y' CHORD IS CORRODED. REMOVED LOWER WEB DUE TO CORROSION AND REPLACED WEB PER SRM 51-30-02, EA 47-5383-12. (M) 2 L 7 4 4F A20WE 1997031300571 19970313 00571 NM 1997 3 13 TWRA9707 1 19960916 A 5312 BULKHEAD WEB BOEING 747 747131 1384881 NM BS 2360 CRACKED A TWRA K NONE O OTHER IN INSP/MAINT 1 EA 15 608FF 19672 DURING D-SERVICE, FOUND FOLLOWING DISCREPANCIES, AFT PRESSURE BULKHEAD AT BS 2360, LOWER WEB AT LBL 25 ADJACENT TO 'Y' C HORD IS CRACKED. REMOVED AND REPLACED WEB AS PER SRM 51-30-02 S/B 747-53-2275 REV 4. (M) 2 L 7 4 4F A20WE 1997031300577 19970313 00577 NM 1997 3 13 97ZZZM270 1 19961227 A 7830 311N51061 FITTING BOEING 757 75723APF 1384966 NM NR 1 TR UNIT CRACKED A CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 571CA 24456 DURING C-CHECK, NR 1 ENGINE OUTBOARD THRUST REVERSER HINGE FLANGE WAS FOUND CRACKED. REMOVED AND REPLACED FITTING IAW S /B 757-54-0015. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A2NM 1997031300600 19970313 00600 WP 1997 3 13 97ZZZM276 1 19961202 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 389 CRACKED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE FORWARD PIT FRAME AT FS 389 AND LONGERON 30 FRAME CRACKED AT BOTTOM, CRACK LENGTH 3, 1 INCH. CUT OUT CRACKED SEGMENT OF FRAME AND FORMED NEW SEGMENT AND SPLICE IAW DC 9 SRM 53-03 FIG 2A. HEAT TREATED SEGMENT AND SPLICE PARTS IAW DC-9 SRM 51-10-2A. TREATED AND PRIMED SEGMENT AND SPLICE I AW DC-9 SRM 51-10-3. INSTALLED REPAIR SPLICE AND SEGMENT IAW DC-9 SRM 51-30-5. (M) 2 L 7 2 4F A6WE 1997031300601 19970313 00601 WP 1997 3 13 97ZZZM277 1 19961126 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 408 CRACKED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND A CRACK IN THE FORWARD PIT FRAME AT FS 408 AND LONGERON 30, FRAME CRACKED AT BOTTOM. CUT OUT CRACKED SEGMENT OF FRAME AND FORWARD NEW SEGMENT AND SPLICE IAW DC-9 SRM 53-03 FIG 2A HEAT TREATED SEGMENT AND SPLICE PARTS IAW DC-9 SRM 51-10-2A. TREATED AND PRIMED SEGMENT AND SPLICE IAW DC-9 SRM 51- 10-3, INSTALLED REPAIR SPLICE AND SEGMENT IAW DC-9 SRM 51-30-5. (M) 2 L 7 2 4F A6WE 1997031300602 19970313 00602 WP 1997 3 13 97ZZZM278 1 19961205 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 580 CRACKED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND FORWARD CARGO COMP LONGERON 29R END FITTING CAP CRACKED AT STATION 580 APPROXIMATELY 2 INCHES LONG. REMOVED FASTENERS, REMOVED CRACKED END CAP FITTING, DRILLED NEW FITTING, TR EATED AND INSTALLED IAW DC-9 SRM 51-10-4, 51-30-0, 51-10-3. (M) 2 L 7 2 4F A6WE 1997031300603 19970313 00603 WP 1997 3 13 97ZZZM279 1 19961205 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 370 DAMAGED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE FORWARD CARGO COMP STATION 370 HAS INTERCOSTAL WITH DRILL MARK AT LONGERON 28R. REMOVED INTERCOSTAL, FABRICATED NEW INTERCOSTAL IAW DC-9 SRM CH 53-11-2 FROM 2024-T3, .090 INBH BY 1 INCH BY 3 INCH BY 6.9 INCH, DRILLED DEBURRED, TRIMMED ALODINED AND PRIMED AND INSTALLED IAW DC-9 SRM CH 51-10- 4, 51-10-2, 51-30-5, 51-30-2. (M) 2 L 7 2 4F A6WE 1997031300604 19970313 00604 WP 1997 3 13 97ZZZM280 1 19961205 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 120 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND E/E BAY LONGERON 29L AND 29R CORRODED BEYOND LIMITS FUSE LAGE STATION 120, AND L30. CORRODED LONGERONS 29L, 29R AND 30 REMOVED 3 NEW LONGERONS FABRICATED IAW DC-9 SRM 53-11-1. LONGERONS TREATED AND PRIMED IAW DC-9 SRM 51-10-3 AND INSTALLED IAW DC-9 51-30, 2.125 INCH BY 19.125 INCH, 7075-T6. (M ) 2 L 7 2 4F A6WE 1997031300605 19970313 00605 WP 1997 3 13 97ZZZM281 1 19961126 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 160-218 CORROSION A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND CORROSION IN THE E/E COMP AT L30 FROM STATION 160 TO 218 . LONGERON 30 CORRODED BEYOND LIMITS IAW DC-9 SRM 53-01. LONGERON REMOVED BETWEEN STATION 160 AND STATION 229. NEW LO NGERON FABRICATED IAW DC-9 SRM 53-11-1 FIG 3. TREATED AND PRIMED IAW DC-9 SRM 51-10-3 AND INSTALLED IAW DC-9 SRM 51-30- 2 AND 51-30-3. (M) 2 L 7 2 4F A6WE 1997031300606 19970313 00606 WP 1997 3 13 97ZZZM282 1 19961114 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 945 CRACKED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 AFT CARGO STATION 945 HAS CIRCUMFERENTIAL FRAME WITH CRACK IN RADIUS AT STRINGER 30. DISASSEMBLED CIRCUMFERENTIAL TO AC CESS WELD IAW DC-9 SRM 51-30-2, WELDED REPAIR IAW EA 12-5321-29-C1056 USING 4951 OPT ROD, DYE PENETRATED INSPECTION PERF ORMED, NO CRACKS FOUND, PRIMED IAW DC-9 SRM 51-10-3. FINAL INSTALLATION IAW DC-9 SRM 51-30-5. (M) 2 L 7 2 4F A6WE 1997031300607 19970313 00607 WP 1997 3 13 97ZZZM283 1 19961205 A 5320 SPLICE DOUG DC9 DC932 3022066 WP BS 400 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND LONGERON 30 AND 29L WERE CORRODED AT STATION 400 AT SPLI CES. FABRICATED 2 SPLICES IAW DC-9 SRM 53-02, FIG 14. (M) 2 L 7 2 4F A6WE 1997031300608 19970313 00608 WP 1997 3 13 97ZZZM284 1 19961205 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 389 CRACKED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE FORWARD CARGO COMP, FRAME AT STATION 389 LONGERON 29 R IS CRACKED APPROXIMATELY .5 LONG. REMOVED CRACKED FRAME STATION 389 AND L29R APPROX 5 INCH, FABRICATED FRAME AND REPA IR SPLICES AND REPAIR PLATES AND INSTALLED IAW DC-9 SRM 53-03 FIG 24 SHEET 1 AND 51-30-2. (M) 2 L 7 2 4F A6WE 1997031300609 19970313 00609 WP 1997 3 13 97ZZZM285 1 19961202 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 750 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL THE FOLLOWING WAS FOUND CORROSION AT LONGERON 30 END FITTING AT STATION 750. REMOVED CORRODED SECTION OF LONGERON 30 FABRICATED, INSTALLED LONGERON END SPLICE, P/N 1A-16536-1 IAW DC0 SRM 53-02 FIG 12, 51-10-3, 51-10-2, 51-10-4. (M) 2 L 7 2 4F A6WE 1997031300610 19970313 00610 WP 1997 3 13 97ZZZM286 1 19961114 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 770 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 AFT CARGO HAS CORROSION ON CIRCUMFERENTIAL FRAME BETWEEN STRINGERS 29L AND 29R, STATION 770. CORROSION OUT OF LIMITS IA W DC-9 SRM 53-01 FIG 1, PREPARED REPAIR AREA AND FABRICATED REPAIR SPLICE, FILLER AND REPAIR PLATES IAW DC-9 SRM 53-03 F IG 2. TREATED AND PRIMED ALL BARE SURFACES IAW DC9 SRM 51-10-3. INSTALLED REPAIR PARTS IAW DC-9 SRM 53-03 FIG 2, ONE P ART 1 INCH BY 6 INCH, ONE 1.5 INCH BY 18 INCHES AND TWO 2.5 BY 16 INCHES. (M) 2 L 7 2 4F A6WE 1997031300611 19970313 00611 WP 1997 3 13 97ZZZM287 1 19961114 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 790 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 AFT CARGO HAS CORROSION ON CIRCUMFERENTIAL FRAME BETWEEN STRINGERS 29L AND 29R AT STATION 790. MECHANICALLY REMOVED COR ROSION MATERIAL LOSS LESS THAN .003 WITHIN LIMITS IAW DC-9 SRM 51-10-3. REMOVED FASTENERS AND STIFFENERS, ANGLES TWO TO FORM. TREATED AND PRIMED IAW DC-9 SRM 51-10-3 INSTALLED FASTENERS IAW DC-9 SRM 51-30-2, AFT CARGO STATION 790, BETWEEN STRINGER 29L AND STRINGER 29R. (M) 2 L 7 2 4F A6WE 1997031300612 19970313 00612 WP 1997 3 13 97ZZZM288 1 19961114 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 810 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 AFT CARGO HAS CORROSION ON CIRCUMFERENTIAL FRAME BETWEEN STRINGERS 29L AND 29R STATION 810. REMOVED FASTENERS IAW DC-9 SRM 51-30-1, 51-30-1, 51-30-1, 51-30-5. MECHANICALLY REMOVED CORROSION MATERIAL LOSS LESS THAN .005 IAW DC-9 SRM 51-10- 3. TREATED AND PRIMED IAW DC-9 SRM 51-10-3. INSTALLED FASTENER IAW DC-9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 1997031300613 19970313 00613 WP 1997 3 13 97ZZZM289 1 19961114 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 850 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 AFT CARGO HAS CORROSION ON CIRCUMFERENTIAL FRAME AT STATION 850 BETWEEN STRINGERS 29L AND 29R. MECHANICALLY REMOVED COR ROSION IAW DC-9 SRM 51-10-3 MATERIAL LOSS .005 WITHIN LIMITS IAW DC-9 SRM 53-04 FIG 38 TREAT AND PRIME IAW DC-9 SRM 51-1 0-3. (M) 2 L 7 2 4F A6WE 1997031300614 19970313 00614 WP 1997 3 13 97ZZZM290 1 19961114 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 870 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 DURING A SCHEDULED INSPECTION AT AERO CORP IN THE AFT CARGO AREA CORROSION WAS FOUND ON CIRCUMFERENTIAL FRAME AT STATION 870 BETWEEN STRINGER 29L AND 29R. REMOVED FASTENERS TO FOM, MECHANICALLY REMOVED CORROSION MATERIAL LOSS LESS THAN .00 3 WITHIN LIMITS TREATED AND PRIMED ALL BARE SURFACES AND REINSTALLED FASTENERS IAW DC-9 SRM 53-01 FIG 1, 51-10-30, 51-30 -2. (M) 2 L 7 2 4F A6WE 1997031300615 19970313 00615 WP 1997 3 13 97ZZZM291 1 19961114 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 850-890 CORROSION A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 DURING A SCHEDULED INSPECTION AT AERO CORP IN THE AFT CARGO AREA, CORROSION ALONG THE INTERCOSTAL BETWEEN STATION 850-89 0, STRINGER 29R. MECHANICALLY REMOVED CORROSION IAW DC-9 SRM 51-10-3 .003 MATERIAL, CHECKED WITH DME A1244, WITHIN LIMI TS IAW DC-9 SRM 53-04 FIG 38 TREATED AND PRIMED IAW DC-9 SRM 51-10-3 AT AFT CARGO COMP ALONG INTERCOSTAL BETWEEN STATION 850 AND 890 AT STRINGER 28R. (M) 2 L 7 2 4F A6WE 1997031300616 19970313 00616 WP 1997 3 13 97ZZZM292 1 19961114 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 850-890 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 AFT CARGO HAS CORROSION ALONG INTERCOSTAL BETWEEN STATION 850-890. MECHANICALLY REMOVED CORROSION IAW DC-9 SRM 51-10-3, .003 MATERIAL LOSS CHECKED WITH DME A1244, WITHIN LIMITS IAW DC-9 SRM 53-04 FIG 38 TREATED AND PRIMED IAW DC-9 SRM 51-1 0-3 AT AFT CARGO ALONG INTERCOSTAL STATION 850 TO 890 AT STRINGER 29R. (M) 2 L 7 2 4F A6WE 1997031300617 19970313 00617 WP 1997 3 13 97ZZZM293 1 19961114 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 830 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 AFT CARGO HAS HEAVY CORROSION ON CIRCUMFERENTIAL FRAME BETWEEN STRINGERS 29L-29R AT STATION 830. CUT OUT CORRODED SECTI ON OF FRAME IAE DC-9 SRM 53-03 FIG 2A. FABRICATED 1 FILLER 7075-0-071, 4 SPLICE ANGLES 7075-0-.080, HEAT TREAT TO T6 IA E DC-9 SRM 51-10-2A, 4 SPLICE PLATES 7075-T6-.080. ALODINED AND PRIMED IAW DC-9 SRM 51-10-3. INSTALLED 1 FILLER 4 ANGL ES AND 4 SPLICE PLATES IAW DC-9 SRM 51-30-5. (M) 2 L 7 2 4F A6WE 1997031300623 19970313 00623 WP 1997 3 13 97ZZZM294 1 19961126 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 389 CRACKED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND A 2 INCH CRACK IN THE FORWARD PIT AT FS 389 LONGERON 30. REMOVED CORROSION MATERIAL LOSS .001 TO .002 WITHIN LIMITS TREATED AND PRIMED IAW DC-9 SRM 51-10-3, 51-30-3. (M) 2 L 7 2 4F A6WE 1997031300624 19970313 00624 WP 1997 3 13 97ZZZM295 1 19961114 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 917 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 AFT CARGO HAS SEVERAL SPOTS OF CORROSION ON CIRCUMFERENTIAL FRAME AT STATION 917, CORROSION EXTENDS UNDER FINGERS OF ATT ACH ANGLE. CUT OUT CORRODED AREA BETWEEN STRINGER 27 AND 28-29 BEYOND LIMITS .020. ROLLED 2 FRAME REPAIR SPLICE IAW DC -9 SRM 53-05 PAGE 4G. DIMENSIONS 20 INCH BY 3 INCH 15 INCH BY 3 INCH, 6.8 INCH BY 1.90 INCH 7075-0-.063. HEATED TO 707 5 T6 IAW DC-9 SRM 51-10-2A AND 7075-0-.066 TREATED AND PRIMED IAW DC-9 SRM 51-10-3 PAGE 18 AND 46. INSTALLED PARTS AND FASTENERS IAW DC-9 SRM 51-30-3, 51-30-5. (M) 2 L 7 2 4F A6WE 1997031300625 19970313 00625 WP 1997 3 13 97ZZZM296 1 19961205 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 218/237 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE FORWARD PIT LONGERON 29R HAS CORROSION UNDER LONGERO N, AT SPLICE BETWEEN STATION 218 BULKHEAD AND STATION 237. REMOVED SPLICE IAW DC-9 SRM 51-30-2, CORROSION ON SPLICE FOU ND TO BE OUT OF LIMITS IAW DC-9 SRM 53-01 FIG 1. CORROSION ON LONGERON FOUND TO BE OUT LIMITS IAW DC-9 SRM 53-01 FIG 1. MECHANICALLY REMOVED CORROSION ON SKIN LESS THAN .005 REMOVED FOUND WITHIN LIMITS IAW DC-9 SRM 53-01 FIG 1, TREATED AN D PRIMED SKIN IAW DC-9 SRM 51-10-3. (M) 2 L 7 2 4F A6WE 1997031300626 19970313 00626 WP 1997 3 13 97ZZZM297 1 19961205 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 218-237 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND FORWARD CARGO PIT CORRODED AND BLOWN OUT SPLICE, AT BUL KHEAD STATION 218 TO STATION 237 LONGERON 29R. REMOVED CORROSION AND SPLICE FOUND TO BE OUT OF LIMITS, IAW DC-9 SRM 53- 01 FIG 1. REMOVED LONGERON CORROSION FOUND TO BE OUT OF LIMITS IAW DC-9 SRM 53-01 FIG 1. FABRICATED REPAIR SPLICED TWO AND LONGERON 11 INCH BY 2.5 INCH, 10.25 INCH BY 2.5 INCH, 11 FEET BY 2 FEET P/N 2777922-3, 063 INCH THICKNESS 7075 T6, CLAD IAW DC-9 SRM 53-2 FIG 2. (M) 2 L 7 2 4F A6WE 1997031800004 19970318 00004 SW 1997 3 18 CA961002008 1 19960920 A 7603 111B0100 BALL JOINT 154203 SWRNGN SA226 SA226AT 8780405 SW GARRTT TPE331 TPE3311151A 01514 WP POWER LEVER BENT W A E ENGINE SHUTDOWN O OTHER DE DESCENT 1 CA P91132 (CAN) ON DESCENT THE PILOT TRIED TO REDUCE POWER ON LEFT ENGINE, BUT LEVER WAS FROZEN, IN THE PROCESS THE BALL JOINT ON THE END OF THE CABLE WAS BENT 60 DEGREES UP WHICH WOULD NOT LET THE POWER BE REDUCED TO THE REQUIRED RPM. ENGINE SHUT DO WN. A NEW BALL JOINT OF NEW DESIGN P/N 85043-1 WAS INSTALLED. 2 L 7 2 4T 4 T RT A5SW E3WE 1997031800005 19970318 00005 GL 1997 3 18 CA961002012 3 19960926 A 6110 PROPELLER BEECH 95 95B55 1152729 CE CONT O470 IO470L 17026 SO HARTZL HCC2Y BHCC2YF2 GL R/H PROP FAULTY W K NONE O OTHER AP APPROACH 1 CA 1530 237685R AN6600 (CAN) ON APPROACH THE R/H RPM DROPPED TO 1500 WHEN THE POWER WAS REDUCED, THE AIRCRAFT LANDED WITHOUT INCIDENT BUT THE P ROPELLER FEATHERED ON SHUTDOWN. THE PROPELLER WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 3O 3 O RT 3A16 3E1 5 C P920 1997032000001 19970320 00001 NM 1997 3 20 CA961009006 1 19960911 A 2612 655280915 DETECTOR UNIT BOEING 737 7372A3 138448A NM PWA JT8 JT8D9A 52048 NE NR 2 ENG FIRE INTERMITTENT W E ENGINE SHUTDOWN N FALSE WARNING AP APPROACH 1 CA 665233 (CAN) ON APPROACH MASTER CAUTION LIGHT AND #2 ENGINE OVERHEATING LIGHT ON. THE ENGINE OVERHEAT AND FIRE CHECKLIST WAS CO MPLETED. SINGLE ENGINE APPROACH CARRIED OUT, NORMAL LANDING. REPLACED FIRE DETECTION UNIT. 2 L 7 2 4F 4 F A16WE E2EA 1997032000007 19970320 00007 NM 1997 3 20 CA961011004 1 19961006 A 2731 82760174005 TRIM JACK DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE ELEVATOR FROZEN W O OTHER F FLT CONT AFFECTED CR CRUISE 1 CA 17655 120384 (CAN) IN CRUISE, ELEVATOR TRIM FROZE. AT WARMER ALTITUDE SYSTEM OK. SCREW JACK ASSEMBLIES PURGE OF WATER AND GREASE AS P ER TASK 2730/04. 2 H 7 2 4T 4 T RT A13NM E20NE 1997032000009 19970320 00009 SO 1997 3 20 CA961016003 2 19960917 A 8530 SA628488 HYDRAULIC LIFTER CESSNA 180 180J 2072622 CE CONT O470 O470R 17026 SO MCAULY 2A34C 2A34C203 GL PUSH ROD SLEEVE SEIZED W K NONE O OTHER IN INSP/MAINT 1 CA 1000 462647 950479 (CAN) DURING A CYLINDER CHANGE A FAULTY HYDRAULIC LIFTER WAS NOTED AND FURTHER INSPECTION FOUND THE INTERNAL SLEEVE (PIS TON) WAS SEIZED. 1 H 7 1 3O 3 O 5A6 E273 5 C P3EA 1997032000010 19970320 00010 EA 1997 3 20 CA961016006 1 19961011 A 7160 3023608 INLET SCREEN DHAV DHC6 DHC6300 EA PWA PT6 PT6A27 52043 EA AIR INLET BROKEN WIRES W K NONE C F.O.D. IN INSP/MAINT 1 CA 2916 PCE40609 (CAN) ON INSPECTION THE COMPRESSOR INLET SCREEN WIRES WERE FOUND BROKEN IN SEVERAL LOCATIONS WITH PIECES MISSING UNDER T HE AIR FRAME BLEED AIR DUCTS AND FCU P3 LINE. FIRST STAGE COMPRESSOR BLADES WERE FOUND NICKED BEYOND MAINTENANCE MANUAL MINIMUM LIMITS. THE ENGINE WAS REPLACED. 1 H 7 2 3T 4 T A9EA E4EA 1997032000011 19970320 00011 NM 1997 3 20 CA961016008 1 19961005 A 8012 START VALVE BOEING 727 727212 138407G NM PWA JT8 JT8D17 52049 NE NR 3 ENG CHAFED WIRE W A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 CA 688149 (CAN) #3 ENGINE START VALVE LIGHT ON IN FLIGHT. ENGINE SHUT DOWN AND AIRCRAFT RETURNED TO BLOCKS. WIRE CHAFED APPROZIMAT ELY 10 INCHES FROM MAIN PYLON ELECTRICAL CONNECTION. REPAIRED. 2 L 7 3 4F 4 F A3WE E2EA 1997032000012 19970320 00012 NM 1997 3 20 CA961016009 1 19961005 A 2840 LG1136AA01 DENTIOMETER BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE FUEL QTY CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 30734 (CAN) FUEL QUANTITY INDICATION FLUCTUATING. FUEL DENTIOMETER WITH CORRODED CANNON PLUG. UNABLE TO REMOVE CANNON PLUG, WI RES CUT AND NEW UNIT INSTALLED. 2 L 7 2 4F 4 F RT A2NM E12EU 1997032000018 19970320 00018 SO 1997 3 20 CA961018002 2 19960913 A 8530 649166C CYLINDER CESSNA 210 2105 2073404 CE CONT O470 IO470S 17026 SO MCAULY 2A34C D2A34C58 GL ENGINE HEAD SEPARATED W D RETURN TO BLOCK E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CL CLIMB 1 CA 661 0320097 CS1025202S 692238 (CAN) HEAD BLOWN OFF CYLINDER. 1 H 7 1 3O 3 O 3A21 3E1 5 C P3EA 1997032000019 19970320 00019 EU 1997 3 20 CA961018010 1 19960912 A 5510 355A1305200302 STABILIZER SNIAS 350 AS350B2 8680813 EU HORIZ STAB OUT OF BAL W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) TAIL ROTOR ASSEMBLY HAS ALWAYS BEEN DIFFICULT TO DYNAMICALLY BALANCE USING THE CHADWICK 8500 SERIES STOBEX. OVER T HE LIFE OF THE TAIL ROTOR SEVERAL SETS OF EXPENSIVE BEARINGS HAVE BEEN CHANGED. WHILE THIS PARTIALLY RESOLVED THE PROBLE M, IT STILL TOOK MANY HOURS TO BRING THE BALANCE TO AN ACCEPTABLE LEVEL. AT THE LAST OCCURRENCE THE CHADWICK REP WAS CAL LED IN AND AT HER SUGGESTION WE PLACED SMALL SANDBAGS ON THE HORIZONTAL STABILIZER DURING GROUND BALANCING. THIS IMMEDIA TELY HALVED THE OUT OF BALANCE CONDITION AND THE TAIL ROTOR WAS BALANCED TO THE REQUIRED LEVEL IN 3 MINOR ADJUSTMENTS. T HE HORIZONTAL STABILIZER WAS REPLACED & THE TAIL ROTOR WAS BALANCED AGAIN WITHIN 3 RUNS WITHOUT THE SANDBAGS. THE STABIL 1 G 7 1 3U H9EU 1997032000020 19970320 00020 EU 1997 3 20 CA961018015 1 19960917 A 5610 STA320271 WINDSHIELD AIRBUS 320 A320211 3930320 EU L1 & R1 PITTED W K NONE O OTHER CR CRUISE 1 CA (CAN) AIRCRAFT FLEW IN VOLCANIC ASH FOR 3 TO 5 MINUTES. SMOKE ENTERED COCKPIT AND CABIN A FEW SECONDS LATER. NO INSTRUME NT INDICATION OR MALFUNCTION. AIRCRAFT LANDED WITHOUT INCIDENT. PRELIMINARY MAINTENANCE CHECK REVEALED WINDSHIELDS PITTE D, LH ENGINE STATOR VANE PITTED AND WING LEADING EDGE PAINT ERRODED. WINDSHIELDS REPLACED, BOROSCOPE CHECK CARRIED OUT O N #1 AND #2 ENGINES AND HIGH PRESSURE VANES FOUND OK. 2 L 7 2 4F RT A28NM 1997032000021 19970320 00021 WP 1997 3 20 CA961018017 1 19960919 A 2120 20495021 TURBINE COOLING DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE LT AIR COND FAILED W K NONE O B OTHER SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA P654059D (CAN) LEFT HAND AIR CONDITIONING PACK INDUCED SMOKE IN THE CABIN. MAINTENANCE ACTION INVOLVED REPLACING AIR CYCLE MACHIN E, LH AND RH COALESCER BAGS. SYSTEM TST CARRIED OUT SERVICEABLE. 2 L 7 2 4F 4 F A6WE E2EA 1997032000022 19970320 00022 WP 1997 3 20 CA961018019 1 19960922 A 2170 1808491 COALESCER BAG DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE AIR COND SATURATED W K NONE O OTHER TX TAXI/GRND HDL 1 CA P654059D (CAN) ON RAMP WITH APU AIR ON LH PACK HP BLEED OFF, FUMES PRESENT IN CABIN. WHEN ENGINES RUNNING PACK OPERATION NORMAL. MAINTENANCE ACTION INVOLVED CHANGING COALESCER BAGS AND SYSTEM CHECKED. 2 L 7 2 4F 4 F A6WE E2EA 1997032000023 19970320 00023 EU 1997 3 20 CA961018021 1 19960913 A 2750 FLAP AIRBUS 320 A320211 3930320 EU FLT CONTROL LOCKED W K NONE F FLT CONT AFFECTED AP APPROACH 1 CA (CAN) ON APPROACH WITH FLAP SELECTION 2, FLAP CONTROL LOCKED. MAINTENANCE INSPECTED FLAP/SLAT AND UNABLE TO DUPLICATE FA ULT. ALL HYDRAULIC SYSTEMS PRESSURIZED AND FLAP SYSTEM RECYCLED SERVICEABLE. 2 L 7 2 4F RT A28NM 1997032000024 19970320 00024 WP 1997 3 20 CA961018022 1 19960925 A 7910 OIL TANK DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE RT ENG OIL MISSING CAP W K NONE K FLUID LOSS IN INSP/MAINT 1 CA P654059D (CAN) RH ENGINE OIL QUANTITY LOW. FOUND ACCESS PANEL OPEN AND OIL TANK CAP MISSING. CAP REPLACED AND SYSTEM REPLENISHED. 2 L 7 2 4F 4 F A6WE E2EA 1997032000025 19970320 00025 EU 1997 3 20 CA961018024 1 19960918 A 6320 350A32010004 BEARING SNIAS 350 AS350D 8680803 EU TMECA ARRIEL ARRIEL1B 6OO30 NE PLANETARY GEAR PITTED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 4120 (CAN) M/R TRANSMISSION EPICYCLIC REDUCTION GEARS REMOVED DUE TO UPPER ROLLER BEARING IN ONE OF THE PLANETARY GEARS BREAK ING DOWN AND MAKING METAL. 1 G 7 1 3U 3 U H9EU E19EU 1997032000026 19970320 00026 NM 1997 3 20 CA961018025 1 19961003 A 5220 85220160103 CABLE DHAV DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE PAX EMERG DOOR CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 120304 (CAN) DURING INSPECTION AS PER TASK CARD 5220/51 THE CABLE AND PULLEY ASSEMBLY ON THE PASSENGER EMERGENCY DOOR (R/H) REL EASE, BOTH THE CABLE AND PULLEY WERE FOUND CORRODED, AND THE PULLEY WAS SEIZED. 2 H 7 2 4T 4 T RT A13NM E20NE 1997032000028 19970320 00028 NM 1997 3 20 CA961021003 1 19960924 A 2910 KFAE246051 LINE BOEING 727 727172C 1384058 NM PWA JT8 JT8D7B 52053 NE NR 2 HYD SYS CRACKED W A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS K FLUID LOSS CR CRUISE 1 CA 657595 (CAN) LOST 'A' SYSTEM HYDRAULIC PRESSURE. #2 ENGINE HYDRAULIC PUMP PRESSURE LINE BETWEEN PUMP AND BULKHEAD RUPTURED. #1 AND #2 CASE DRAIN FILTERS INSPECTED OK. LINE INSTALLED SYSTEM SERVICED. 2 L 7 3 4F 4 F A3WE E2EA 1997032000029 19970320 00029 NM 1997 3 20 CA961021004 1 19960924 A 2910 KFAE2460510J0480 HOSE BOEING 727 727172C 1384058 NM PWA JT8 JT8D7B 52053 NE A SYS HYD LOOSE W H DEACTIVATE SYST/CIRCUITS K FLUID LOSS CR CRUISE 1 CA 657595 (CAN) LOST 'A' SYSTEM HYDRAULIC PRESSURE. AIRCRAFT TOWED FROM TAXIWAY. CONNECTION LOOSE AT QUICK DISCONNECT ATTACHMENT. REPAIRED. 2 L 7 3 4F 4 F A3WE E2EA 1997032000030 19970320 00030 SW 1997 3 20 CA961021006 1 19961003 A 3310 1300071 TRANSISTOR BELL 222 222U 1182140 SW LYC LTS101 LTS101750C1 41560 NE PEDESTAL BURNT OUT W O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 CA 1585 LE47220AE (CAN) PEDESTAL LIGHT FAILED, INSTRUMENT LIGHTING WAS FUNCTIONING. 1 G 7 2 3U 3 U H9SW E5NE 1997032000031 19970320 00031 EU 1997 3 20 CA961021009 1 19961002 A 3230 200498005 ACTUATOR FOKKER F28 F28MK1000 4990808 EU MLG INTERMITTENT W O OTHER J WARNING INDICATION AP APPROACH 1 CA 7198 7198 (CAN) MAIN LANDING GEAR WILL NOT LOCK DOWN WHEN SELECTED. CYCLED SEVERAL TIMES, ALTERNATE MEANS ATTEMPTED, FLY BY CARRIE D OUT TO VERIFY GEAR DOWN AND LANDED WITHOUT INCIDENT. GEAR WAS NOT LOCKED DOWN AND PIN WAS HALFWAY OBSTRUCTED. PULLED S IDE STAYS DOWN INTO LOCKED POSITION AND INSERTED PIN. AIRCRAFT RETURNED WITH GEAR PINNED DOWN. DOWNLOCK ACTUATOR REPLACE D. 2 L 7 2 4F RT A20EU 1997032000032 19970320 00032 SW 1997 3 20 CA961021010 1 19961012 A 3222 54510051 YOKE SWRNGN SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP NOSE GEAR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 27360 PAL32205 P54183 (CAN) ULTRASONIC INSPECTION OF LANDING GEAR YOKES AS PER AD 96-19-05. OF 41 YOKES INSPECTED 12 HAD CRACKS. ALL 12 HAD BE EN FOUND OK ONE YEAR PREVIOUS. ALL ARE FAIRLY HIGH TIME. SUBMITTER SUGGESTS THAT CRACKING NOT ENTIRELY RELATED TO FATIGU E AS SOME NEW YOKES THEY HAVE RECEIVED HAVE BEEN CRACKED. 2 L 7 2 4T 4 T RT A8SW E4WE 1997032000033 19970320 00033 NM 1997 3 20 CA961021011 1 19961010 A 2910 651784981 LINE BOEING 727 72790C 1384030 NM PWA JT8 JT8D7B 52053 NE B HYD SYS BROKEN W H DEACTIVATE SYST/CIRCUITS J K WARNING INDICATION FLUID LOSS DE DESCENT 1 CA 653646 (CAN) ON APPROACH 'B' HYDRAULIC SYSTEM FAILURE. SYSTEM DEACTIVATED AND AIRCRAFT LANDED WITHOUT INCIDENT. #1 'B' PUMP TO MODULE RIGID LINE BROKEN AT FERRULE. REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 1997032000034 19970320 00034 EU 1997 3 20 CA961021013 1 19961010 A 2130 VFT300A11 SKIN VALVE AIRBUS 320 A320211 3930320 EU CABIN CONTROL FAILED W A UNSCHED LANDING O OTHER CR CRUISE 1 CA (CAN) ENROUTE FLIGHT DIVERTED DUE TO ECAM MESSAGE VENT AVIONICS SYSTEM FAULT. VENT AND EXTRACT VALVES POSITION AMBER ON CABIN PRESSURE PAGE AND UNABLE TO PRESSURIZE CABIN. MAINTENANCE ACTION INVOLVED REPLACING SKIN AIR EXHAUST VALVE. EXTRAC T VALVE SEQUENCED AND AEVC (AVIONICS EQUIPMENT VENTILATION COMPUTER) RESET. 2 L 7 2 4F RT A28NM 1997032000035 19970320 00035 WP 1997 3 20 CA961021015 1 19961011 A 5220 1522310101 HINGES LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE FLT DECK HATCH CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 10535 (CAN) FLIGHT DECK ESCAPE HATCH HINGES CRACKED, REPLACED. 2 L 7 3 4F 4 F A23WE E12EU 1997032000036 19970320 00036 NM 1997 3 20 CA961022001 1 19961007 A 3260 CONNECTOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE WOW SENSOR CONTAMINATED W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA 120134 (CAN) ON CLIMB THROUGH, FL180K, WEIGHT ON WHEELS LIGHT ON INTERMITTENTLY. AIRCRFT RETURNED AND LANDED OK. MAINTENANCE DI D BITE TEST FOUND WOW SENSOR, RIGHT HAND CANNON PLUG CONTAMINATED. 2 H 7 2 4T 4 T RT A13NM E20NE 1997032000037 19970320 00037 EA 1997 3 20 CA961022002 2 19961015 A 7200 ENGINE BEECH 99 B99 1154004 CE PWA PT6 PT6A28 EA NR 2 ENG MAKING METAL W O OTHER O OTHER CR CRUISE 1 CA 40252 (CAN) #2 ENGINE OIL PRESSURE AND TORQUE FLUCTUATIONS ENROUTE. POWER REDUCED AND AIRCRAFT LANDED WITHOUT INCIDENT. POST F LIGHT INSPECTION FOUND METAL IN THE OIL SYSTEM. ENGINE REMOVED AND SHIPPED TO R&O. 1 L 7 2 3T 4 T A14CE E4EA 1997032000038 19970320 00038 SW 1997 3 20 CA961022003 1 19961012 A 3213 54530051 YOKE SWRNGN SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP LH MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 31904 PAL32324 P54082 (CAN) ULTRASONIC INSPECTION OF LANDING GEAR YOKES AS PER AD 96-19-05. OF 41 YOKES INSPECTED 12 HAD CRACKS. ALL 12 HAD BE EN FOUND OK ONE YEAR PREVIOUS. ALL ARE FAIRLY HIGH TIME. SUBMITTER SUGGESTS THAT CRACKING NOT ENTIRELY RELATED TO FATIGU E AS SOME NEW YOKES HAVE BEEN RECEIVED WITH CRACKS. 2 L 7 2 4T 4 T RT A8SW E4WE 1997032000039 19970320 00039 SW 1997 3 20 CA961022004 1 19961012 A 3222 54510051 YOKE SWRNGN SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP NOSE GEAR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 28585 PAL32204 P54019 (CAN) ULTRASONIC INSPECTION OF LANDING GEAR YOKES AS PER AD 96-19-05. OF 41 YOKES INSPECTED 12 HAD CRACKS. ALL 12 HAD BE EN FOUND OK ONE YEAR PREVIOUS. ALL ARE FAIRLY HIGH TIME. SUBMITTER SUGGESTS THAT CRACKING NOT ENTIRELY RELATED TO FATIGU E AS THEY HAVE RECEIVED SOME NEW YOKES THAT HAVE BEEN CRACKED. 2 L 7 2 4T 4 T RT A8SW E4WE 1997032000040 19970320 00040 SW 1997 3 20 CA961022005 1 19961012 A 3222 54510051 YOKE SWRNGN SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP NOSE GEAR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 16233 PAL32413 P54202 (CAN) ULTRASONIC INSPECTION OF LANDING GEAR YOKES AS PER AD 96-19-05. OF 41 YOKES INSPECTED 12 HAD CRACKS. ALL 12 HAD BE EN FOUND OK ONE YEAR PREVIOUS. ALL ARE FAIRLY HIGH TIME. SUBMITTER SUGGESTS THAT CRACKING NOT ENTIRELY RELATED TO FATIGU E AS SOME NEW YOKES THEY HAVE RECEIVED HAVE BEEN CRACKED. 2 L 7 2 4T 4 T RT A8SW E4WE 1997032000041 19970320 00041 SW 1997 3 20 CA961022006 1 19961012 A 3213 54530051 YOKE SWRNGN SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE3313UW 01514 WP R/H MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 6564 PAL32116 P03551C (CAN) ULTRASONIC INSPECTION OF LANDING GEAR YOKES AS PER AD 96-19-05. OF 41 YOKES INSPECTED 12 HAD CRACKS. ALL 12 HAD BE EN FOUND OK ONE YEAR PREVIOUS. ALL ARE FAIRLY HIGH TIME. SUBMITTER SUGGESTS THAT CRACKING NOT ENTIRELY RELATED TO FATIGU E AS SOME NEW YOKES THEY HAVE RECEIVED HAVE BEEN CRACKED. 2 L 7 2 4T 4 T RT A8SW E4WE 1997032000042 19970320 00042 SW 1997 3 20 CA961022007 1 19961012 A 3213 54530051 YOKE SWRNGN SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP L/H MAIN CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 27970 PAL32110 P54158 (CAN) ULTRASONIC INSPECTION OF LANDING GEAR YOKES AS PER AD 96-19-05. OF 41 YOKES INSPECTED 12 HAD CRACKS. ALL 12 HAD BE EN FOUND OK ONE YEAR PREVIOUS. ALL ARE FAIRLY HIGH TIME. SUBMITTER SUGGESTS THAT CRACKING NOT ENTIRELY RELATED TO FATIGU E AS SOME NEW YOKES HAD BEEN RECEIVED WITH CRACKS. 2 L 7 2 4T 4 T RT A8SW E4WE 1997032000043 19970320 00043 SW 1997 3 20 CA961022008 1 19961012 A 3222 54510051 YOKE SWRNGN SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP NOSE GEAR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 27970 PAL32207 P54158 (CAN) ULTRASONIC INSPECTION OF LANDING GEAR YOKES AS PER AD 96-19-05. OF 41 YOKES INSPECTED 12 HAD CRACKS. ALL 12 HAD BE EN FOUND OK ONE YEAR PREVIOUS. ALL ARE FAIRLY HIGH TIME. SUBMITTER SUGGESTS THAT CRACKING NOT ENTIRELY RELATED TO FATIGU E AS SOME NEW YOKES HAD BEEN RECEIVED WITH CRACKS. 2 L 7 2 4T 4 T RT A8SW E4WE 1997032000044 19970320 00044 SW 1997 3 20 CA961022009 1 19961012 A 3213 54530051 YOKE SWRNGN SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP R/H MAIN CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 24268 PAL32100 P54143 (CAN) ULTRASONIC INSPECTION OF LANDING GEAR YOKES AS PER AD 96-19-05. OF 41 YOKES INSPECTED 12 HAD CRACKS. ALL 12 HAD BE EN FOUND OK ONE YEAR PREVIOUS. ALL ARE FAIRLY HIGH TIME. SUGGESTS THAT CRACKING NOT ENTIRELY RELATED TO FATIGUE AS SOME NEW YOKES HAVE BEEN RECEIVED WITH CRACKS. 2 L 7 2 4T 4 T RT A8SW E4WE 1997032000045 19970320 00045 SW 1997 3 20 CA961022010 1 19961012 A 3222 54510051 YOKE SWRNGN SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP NOSE GEAR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 24268 PAL32213 P54143 (CAN) ULTRASONIC INSPECITON OF LANDING GEAR YOKES AS PER AD 96-19-05. OF 41 YOKES INSPECTED 12 HAD CRACKS. ALL 12 HAD BE EN FOUND OK ONE YEAR PREVIOUS. ALL ARE FAIRLY HIGH TIME. SUBMITTER SUGGESTS THAT CRACKING NOT ENTIRELY RELATED TO FATIGU E AS SOME NEW YOKES HAD BEEN RECEIVED WITH CRACKS. 2 L 7 2 4T 4 T RT A8SW E4WE 1997032000046 19970320 00046 SW 1997 3 20 CA961022011 1 19961012 A 3213 54530051 YOKE SWRNGN SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE3313UW 01514 WP L/H MAIN CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 25932 PAL32114 03453 (CAN) ULTRASONIC INSPECTION OF LANDING GEAR YOKES AS PER AD 96-19-05. OF 41 YOKES INSPECTED 12 HAD CRACKS. ALL 12 HAD BE EN FOUND OK ONE YEAR PREVIOUS. ALL ARE FAIRLY HIGH TIME. SUBMITTER SUGGESTS THAT CRACKING NOT ENTIRELY RELATED TO FATIGU E AS SOME NEW YOKES HAD BEEN RECEIVED WITH CRACKS. 2 L 7 2 4T 4 T RT A8SW E4WE 1997032000118 19970320 00118 SW 1997 3 20 CA961022012 1 19961012 A 3222 54510051 YOKE SWRNGN SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE3313UW 01514 WP NOSE GEAR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 25932 PAL32209 03453 (CAN) ULTRASONIC INSPECTION OF LANDING GEAR YOKES AS PER AD 96-19-05. OF 41 YOKES INSPECTED 12 HAD CRACKS. ALL 12 HAD BE EN FOUND OK ONE YEAR PREVIOUS. ALL ARE FAIRLY HIGH TIME. SUBMITTER SUGGESTS THAT CRACKING NOT ENTIRELY RELATED TO FATIGU E AS SOME NEW YOKES HAVE BEEN RECEIVED WITH CRACKS. 2 L 7 2 4T 4 T RT A8SW E4WE 1997032000120 19970320 00120 NE 1997 3 20 CA961022014 2 19961010 A 7530 451077 PSU LINE BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE #2 ENGINE LOOSE W O OTHER R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CA 700329 (CAN) ON TAKEOFF ROLL, #2 ENGINE INDICATED UNDER POWER AND HIGH EGT CONDITION. ENGINE INSPECTED FOR PNEUMATIC LEAKS, NON E FOUND. INSPECTED PRBC PSU LINE AND FOUND LOWER FITTING BACKED OFF ALLOWING PSU PRESSURE LEAK WHICH IN TURN ALTERED THE BLEED SCHEDULING RESULTING IN A LOW POWER HIGH EGT CONDITION. LINE RETIGHTENED AND ENGINE GROUND RUN SERVICEABLE. 2 L 7 3 4F 4 F RT A3WE E2EA 1997032000121 19970320 00121 NM 1997 3 20 CA961023002 1 19961012 A 5210 SEAL BOEING 737 737275C NM PWA JT8 JT8D9A 52048 NE L1 DOOR LOOSE W A UNSCHED LANDING O OTHER CL CLIMB 1 CA P665497B (CAN) ON TAKEOFF AND WHEN STARTED TO PRESSURIZE LOUD NOISE COMING FROM L1 FORWARD L/H MAIN ENTRY DOOR AIRCRAFT RETURNED. LOWER HINGE CAME ADRIFT, SEAL REINSTALLED. 2 L 7 2 4F 4 F A16WE E2EA 1997032000123 19970320 00123 WP 1997 3 20 CA961023004 1 19961014 A 3060 9565H13A RELAY CVAC 440 440 2422902 WP LH PROP ANTI ICE INOPERATIVE W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) AFTER TAKEOFF, NO INDICATION OF PROP ANTI-ICE ON LEFT ENGINE. AIRCRAFT RETURNED TO DEPARTURE BASE. MAINTENANCE ACT ION INVOLVED CHANGING UNSERVICEABLE ANTI-ICE RELAY. 2 L 7 2 4R 6A6 1997032000124 19970320 00124 SO 1997 3 20 CA961023005 2 19961001 A 8520 CRANKCASE CESSNA 207 207A 2073604 CE CONT O520 IO520F 17032 SO TOP LEFT SIDE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 280238R (CAN) THE CRANKCASE WAS FOUND CRACKED ON THE TOP LEFT SIDE BEHIND THE LEFT MAGNETO, THE CRACK WAS APPROXIMATELY 6" LONG. 1 H 7 1 3O 3 O A16CE E5CE 1997032000125 19970320 00125 NM 1997 3 20 CA961023006 1 19961008 A 2750 5906989101 CORE ASSEMBLY SUNDSTRAND 745581 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE FLAP DRIVE BROKEN W K NONE J WARNING INDICATION AP APPROACH 1 CA 0658 120323 (CAN) DURING APPROACH THE FLAP DRIVE CAUTION LIGHT CAME ON. INSPECTION FOUND THAT THE CORE ASSEMBLY WAS BROKEN AT THE EN D FITTING. NEW FLEX SHAFT ASSEMBLY INSTALLED. 2 H 7 2 4T 4 T RT A13NM E20NE 1997032000126 19970320 00126 NM 1997 3 20 CA961024001 1 19961008 A 2920 SM601BA20A1 CIRCUIT BREAKER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HYD SYS NR 2 FAILED W H DEACTIVATE SYST/CIRCUITS J O WARNING INDICATION OTHER CR CRUISE 1 CA 120144 (CAN) NO INDICATION OF STANDBY HYDRAULIC PRESSURE SYSTEM #2. STANDBY PUMP REPLACED. PROBLEM REOCCURRED. RCCB CHECKED AND FOUND WEAK. CB REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1997032000127 19970320 00127 NM 1997 3 20 CA961024002 1 19961009 A 5610 8SC0043003 WINDSHIELD DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE LEFT HAND CRACKED W A UNSCHED LANDING O OTHER CR CRUISE 1 CA 84H219236 120083 (CAN) LEFT HAND WINDSHIELD CRACKED IN FLIGHT. APPEARS TO BE THERMAL SHOCK. 2 H 7 2 4T 4 T RT A13NM E20NE 1997032000128 19970320 00128 NM 1997 3 20 CA961024003 1 19961009 A 2910 82970010217 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE SPOILER SYSTEM PIN HOLE W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 120226 (CAN) HYDRAULIC LEAK FROM #1 NACELLE. LINE BETWEEN #2 HYDRAULIC SYSTEMS SPOILER LIFT DUMP VALVES FOUND LEAKING AT 3000 P SI. BENCH CHECK FOUND LINE START TO WEEP AT 400 PSI AND JUST STARTS TO DIP AT 1000 PSI. STEADY STREAM AT 3000 PSI. LINE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1997032000130 19970320 00130 EU 1997 3 20 CA961024006 1 19961002 A 3230 GA40 CIRCUIT BOARD ELDEC 806002 BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE GEAR SWITCH DEFECTIVE W O OTHER J WARNING INDICATION LD LANDING 1 CA 119489 LF05627A (CAN) ON GEAR DOWN SELECTION, FOLLOWING LIGHTS ON: LIFT SPOILERS; MANUAL SPOILER FAULT; Q POT FEEL HEATER FAULT. LANDING GEAR SWITCH CARD FOUND SLOW TO REACT. CIRCUIT BOARD GA40 REPLACED. 2 H 7 4 4F 4 F RT A49EU E6NE 1997032000131 19970320 00131 SW 1997 3 20 CA961024016 1 19961017 A 7603 C8102421 CABLE SWRNGN SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE3313UW 01514 WP RT ENG BROKEN W A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CA 154 03453 (CAN) AFTER START UP THE RIGHT HAND ENGINE DID NOT RESPOND TO SPEED LEVER INPUT. AIRCRAFT RETURNED TO TERMINAL. INSPECTI ON FOUND THAT THE INNER RIBBON OF THE 'COCKPIT TO WING ROOT ASSEMBLY' HAD FAILED AT THE QUADRANT. ACCORDING TO SUBMITTER THIS CABLE HAD BEEN POORLY INSTALLED WITH THE CABLE MAKING A SHARP TURN AT THE POINT OF FAILURE. 2 L 7 2 4T 4 T RT A8SW E4WE 1997032000132 19970320 00132 EA 1997 3 20 CA961024017 1 19961022 A 3240 C6SF13463 PUSH ROD TUBE C6SF13001 DHAV DHC6 DHC6300 EA PWA PT6 PT6A27 52043 EA BRAKE SYS LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA 7274 PCE40147 (CAN) ON LOWER END OF BRAKE PUSH ROD THE MAGNEFORMED THREAD INSERT WAS FOUND LOOSE INSIDE THE MAGNEFORMED END. 1 H 7 2 3T 4 T A9EA E4EA 1997032000133 19970320 00133 SW 1997 3 20 CA961024018 1 19960904 A 6320 7G1981 SWITCH BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL M/R TRANSMISSION MALFUNCTION W K NONE N FALSE WARNING IN INSP/MAINT 1 CA CAE800419BA (CAN) MAIN ROTOR TRANSMISSION PRESSURE LIGHT ON ALL THE TIME. CHANGED PRESSURE SWITCH. 1 G 7 1 3U 3 U H2SW E4CE 1997032000134 19970320 00134 EU 1997 3 20 CA961024019 1 19961018 A 3231 1413200355 ROD END 162631 BAG JETSTM JETSTM4112 EU LT MLG DOOR SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA 3992 (CAN) LEFT HAND MAIN LANDING GEAR DOOR ACTUATING ROD FOUND WITH ROD-END SHEARED OFF. MAINTENANCE DETERMINED THAT THE SWI VEL THAT THE ROD END ATTACHED TO, HAD SEIZED CAUSING THE ROD END TO BREAK. REST OF FLEET INSPECTED. NO OTHERS FOUND. 1 L 7 2 4T RT A196 1997032000135 19970320 00135 EU 1997 3 20 CA961025001 1 19961023 A 2820 HTE7300F1 SEAL BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE FUEL FEED PIPE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA LF05539A (CAN) FUEL NOTED LEAKING FROM #3 PYLON. FOUND TO BE LEAKING FROM SEAL OF FUEL FEED PIPE. SEALS REPLACED. 2 H 7 4 4F 4 F RT A49EU E6NE 1997032000137 19970320 00137 NM 1997 3 20 CA961025003 1 19961024 A 2760 SWITCH DHAV DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE SPOILER CLUTCH BROKEN WIRE W K NONE J WARNING INDICATION IN INSP/MAINT 1 CA 120657 (CAN) RECURRING DEFECTS FOUND OF BROKEN SPOILER CLUTCH WIRES. IN THIS CASE THE LEFT UPPER WIRE AT THE SWITCH. 2 H 7 2 4T 4 T RT A13NM E20NE 1997032000139 19970320 00139 WP 1997 3 20 CA961025005 1 19961023 A 3250 ACG70111 STEERING COLLAR DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NOSE LDG GEAR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 517177 (CAN) NOSE WHEEL LANDING GEAR STEERING COLLAR FOUND CRACKED AT RH STEERING CYLINDER UPPER ATTACHMENT LUG. COLLAR REPLACE D. 2 L 7 3 4F 4 F A22WE E23EA 1997032000140 19970320 00140 SO 1997 3 20 CA961025010 2 19961004 A 8530 CYLINDER SUPAIRPART CESSNA 185 A185F 2072821 CE CONT O520 IO520D 17032 SO MCAULY 2A34C D2A34C58 GL #3 CYLINDER SEPARATION W K NONE O OTHER NR NOT REPORTED 1 CA 145 552397 820420 (CAN) SEPARATION OF #3 CYLINDER. SUSPECT VALVE KEEPERS LET LOOSE. 1 H 7 1 3O 3 O 3A24 E5CE 5 C P3EA 1997032000141 19970320 00141 CE 1997 3 20 CA961025011 1 19961011 A 2612 24409015 FIRE DETECTOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE #1 ENGINE BROKEN W A E UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 CA 2120 PCE114351 (CAN) #1 ENGINE FIRE WARNING LIGHT FLICKERED IN FLIGHT, BUT NO OTHER INDICATIONS. PRECAUTIONARY ENGINE SHUTDOWN WAS CARR IED OTU. POST FLIGHT INSPECTION OF THE ENGINE FOUND THE FIRE LOOP BROKEN UNDER THE REAR OF THE ENGINE. A NEW FIRE LOOP W AS INSTALLED. 2 L 7 2 4T 4 T RT A24CE E26NE 1997032000143 19970320 00143 NM 1997 3 20 CA961025014 1 19961024 A 2760 SWITCH DHAV DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE LT SPOILER BROKEN WIRE W O OTHER J WARNING INDICATION IN INSP/MAINT 1 CA 120854 (CAN) RECURRING DEFECT FOUND OF BORKEN SPOILER CLUTCH WIRES. IN THIS CASE THE LEFT HAND AT THE SWITCH. 2 H 7 2 4T 4 T RT A13NM E20NE 1997032000144 19970320 00144 EA 1997 3 20 CA961025015 1 19961024 A 2760 SWITCH DHAV DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE LT SPOILER BROKEN WIRE W K NONE J WARNING INDICATION NR NOT REPORTED 1 CA 123138 (CAN) RECURRING DEFECTS FOUND OF BROKEN SPOILER CLUTCH WIRES. IN THIS CASE THE LEFT HAND AT THE SWITCH. 2 H 7 2 4T 4 T RT A13NM E20NE 1997032000145 19970320 00145 EA 1997 3 20 CA961025016 1 19961024 A 2760 SWITCH DHAV DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE LT SPOILER BROKEN WIRE W K NONE J WARNING INDICATION NR NOT REPORTED 1 CA 123138 (CAN) RECURRING DEFECTS FOUND OF BROKEN SPOILER CLUTCH WIRES. IN THIS CASE THE LEFT UPPER WIRE AT THE SWITCH. 2 H 7 2 4T 4 T RT A13NM E20NE 1997032000146 19970320 00146 EA 1997 3 20 CA961025017 1 19961024 A 2760 SWITCH DHAV DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE RT SPOILER BROKEN WIRE W K NONE J WARNING INDICATION NR NOT REPORTED 1 CA 123132 (CAN) RECURRING DEFECTS FOUND OF BROKEN SPOILER CLUTCH WIRES. IN THIS CASE THE RIGHT HAND WIRE AT THE SWITCH. 2 H 7 2 4T 4 T RT A13NM E20NE 1997032000392 19970320 00392 NM 1997 3 20 97ZZZX1122 1 19961218 A 2150 HEAT EXCHANGER BOEING 727 727214 138407R NM CABIN MALFUNCTIONED A AMTA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 11 785AT 21691 MDW-SRQ - FLT 563 - DURING CLIMB, AIRCRAFT PRESSURIZATION CANNOT BE HELD WITH SINGLE PACK OPERATION WITH CARGO HEAT OUTF LOW VALVE CLOSED. AIRCRAFT WAS DIVERTED TO INDIANAPOLIS, INDIANA. REMOVED AND REPLACED THE HEAT EXCHANGERS, THE FLOW M ULTIPLIER AND SHUT-OF VALVE, AND THE WATER SEPARATOR BAGS. CABIN DECAY TESTED AND THE APU/ECS CONDITION MONITORING C/W PER BOELING MM. 2 L 7 3 4F A3WE 1997032000483 19970320 00483 EU 1997 3 20 UF6A961204 1 19961225 A 2720 WATER TRAPS BAG ATP ATP EU RUDDER BOOST REQ'D SERVICE A UF6A O OTHER O OTHER CL CLIMB 1 GL 31 852AW 2021 ORD - FLT 5729 - UPON TAKEOFF AND CLIMB, REQUIRED EXCESSIVE RUDDER PRESSURE TO MAINTAIN DIRECTIONAL CONTROL. MAINTENANC E DRAINED WATER FROM RUDDER BOOST WATER TRAPS. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1997032000484 19970320 00484 EU 1997 3 20 UF6A961201 1 19961217 A 2611 CG7PT2 SMOKE DETECTOR BAG ATP ATP EU LAVATORY FAILED A UF6A O OTHER N FALSE WARNING CL CLIMB 1 GL 31 851AW 2020 SBN - FLT 5764 - SMOKE IN LAVATORY LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED LAVATORY SMOKE DETECTOR. (M) 2 L 7 2 4T RT A27NM 1997032000487 19970320 00487 EU 1997 3 20 UF6A961203 1 19961224 A 3350 6013211 POWER SUPPLY GRIMES BAG ATP ATP EU CABIN INOPERATIVE A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 858AW 8936 17404 2035 ORD - FLT 5729 - FORWARD EMERGENCY LIGHT STRIP INOP. MAINTENANCE REMOVED AND REPLACED FORWARD BATTERY PACK. (M) 2 L 7 2 4T RT A27NM 1997032000488 19970320 00488 EU 1997 3 20 UF6A961205 1 19961229 A 5270 WARNING LIGHT BAG ATP ATP EU PAX DOOR ILLUMINATED A UF6A C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 31 855AW 2029 FWA - FLT 5722 - EXIT CWP ILLUMINATED ON TAKEOFF WITH LEFT FRONT DOOR INDICATING OPEN. FLIGHT ATTENDANT REPORTED DOOR W AS CLOSED. MAINTENANCE INSPECTED AND PERFORMED OPS CHECK OF ALL DOOR WARNING INDICATORS. ALL SYSTEMS CHECKED GOOD. (M ) 2 L 7 2 4T RT A27NM 1997032000574 19970320 00574 EU 1997 3 20 AALA961770 1 19961207 A 2163 6177862 TEMP SENSOR AIRBUS 300 A300B4605R 3930308 EU RIGHT DEFECTIVE A AALA B EMER. DESCENT J WARNING INDICATION DE DESCENT 1 SW 07 14077 050C11762 612 MIA - FLT 1315 - DURING DESCENT INTO MIA AT APPROXIMATELY FL 250, RIGHT BLEED VALVE FAILED. CABIN PRESSURE STARTED TO C LIMB RAPIDLY. FLIGHT CREW DECLARED EMERGENCY, STARTED RAPID DESCENT AND RESET BOTH BLEED VALVES. BLEED VALVES WORKED F OR SHORT TIME. STARTED APU TO CONTROL CABIN PRESSURE. AIRCRAFT LANDED MIA WITHOUT FURTHER INCIDENT. REPLACED NR 2 ENG INE TEMPERATURE CONTROL SENSOR AND NR 1 PNEUMATIC CONTROLLER. ACCOMPLISHED HIGH POWER ENGINE RUN. SYSTEM GROUND CHECKE D NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1997032000575 19970320 00575 EU 1997 3 20 AALA961844 1 19961217 A 4990 RETURN LINE AIRBUS 300 A300B4605R 3930308 EU APU COMPT LOOSE A AALA A UNSCHED LANDING J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 7062A 474 SJU - FLT 1014 - AFTER TAEKOFF SJU DURING CLIMB-OUT, ACRID ODOR NOTE IN CONDITIONED AIR AND MINIMUM EQUIPMENT BAY SMOKE WARNING ACTUATED FOLLOWED BY LAVATORY SMOKE DETECTORS. AIRCRAFT RETURNED TO SJU AND LANDED WITHOUT INCIDENT. PLACARDED APU DUE TO EXTERNAL OIL LEAK AND REPLACED ALL COALESCER BAGS. ACCOMPLISHED FUNCTIONAL CHECK FLIGHT WITH NO ODOR NOTED. SYSTEM OPERATIONAL CHECKED NORMAL SUBSEQUENTLY RESECURED APU OIL COOLER LINE AT MIA. REMOVED APU PLACARD AND SYSTEM G ROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1997032000576 19970320 00576 1997 3 20 AALA961851 4 19961219 A 2565 D31021107 SLIDE AIRBUS 300 A300B4605R 3930308 EU L3 DOOR LOW PRESSURE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 91050 423 JFK - DURING OVERNIGHT CHECK, FOUND THE LEFT EMERGENCY EVACUATION SLIDE BOTTLE PRESSURE LOW. INSTALLED NEW SLIDE. SYST EM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1997032000603 19970320 00603 NM 1997 3 20 97ZZZM307 1 19961226 A 3350 3315048 BATTERY PACK BOEING 727 7272B7 138407L NM CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 762AT 22162 DURING PREFLIGHT, FOUND AFT LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LEFT AFT OVERWING EMERGENCY E XIT LIGHT BATTERY PACK, OPS CHECK GOOD. (M) 2 L 7 3 4F A3WE 1997032000604 19970320 00604 NM 1997 3 20 97ZZZM308 1 19961221 A 3350 3315048 BATTERY BOEING 727 727227 1384078 NM CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 768AT 21996 DURING PREFLIGHT, FOUND LEFT FORWARD FORWARD EXIT LEFT INOP, EGRESS TRACK LIGHT INOP. REMOVED AND REPLACED BATTERY PACK . REPLACED PIGTAIL AND LAMP EGRESS LIGHT AT 16D. OPS CHECK GOOD. (M) 2 L 7 3 4F A3WE 1997032000605 19970320 00605 NM 1997 3 20 97ZZZM309 1 19961211 A 3350 3314024 BATTERY BOEING 727 727227 1384078 NM CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 772AT 22003 DURING PREFLIGHT, FOUND CEILING EMERGENCY LIGHT INOP AT ROW 24. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY ASSEMBLY, OPS CHECK GOOD. (M) 2 L 7 3 4F A3WE 1997032000606 19970320 00606 NM 1997 3 20 97ZZZM310 1 19961130 A 3350 3315235 BATTERY BOEING 727 7272Q8 138407W NM CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 776AT 21608 DURING PREFLIGHT, FOUND EMERGENCY OVERHEAD AISLE LIGHT AT SEAT ROW 11 IS INOP. REMOVED AND REPLACED LIGHT BATTERIES, OP S CK NORMAL. (M) 2 L 7 3 4F A3WE 1997032000608 19970320 00608 NM 1997 3 20 97ZZZM312 1 19961116 A 3350 2410070 BATTERY BOEING 727 7272Q8 138407W NM CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 776AT 21608 DURING PREFLIGHT, FOUND BATTERY PACK INOP. EXIT OVERHEAD ABOVE SEATS 4ABC-DEF. INSTALLED BATTERY PACK (CHARGER). OPS CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1997032000609 19970320 00609 NM 1997 3 20 97ZZZM313 1 19961112 A 3350 3322037 LIGHT BOEING 727 727227 1384078 NM CABIN INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 779AT 22091 DURING PREFLIGHT, FOUND FORWARD SECTION OF EGRESS TRACK LIGHTS, INOP. REMOVED AND REPLACED THE FORWARD FLOOR PATH LIGHT S. BATTERY PACK CHECKS OK. (M) 2 L 7 3 4F A3WE 1997032000610 19970320 00610 NM 1997 3 20 97ZZZM314 1 19961111 A 3350 LIGHTS BOEING 727 7272B7 138407L NM CABIN BROKEN A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 762AT 22162 DURNG PREFLIGHT, FOUND EMERGENCY FLOOR LGIHTING IS BROKEN AND NOT SECURED TO FLOOR. FORWARD MOST PART OF TRACK, WIRES L OOSE AND BROKEN. SECURED FLOOR LIGHTING AS REQUIRED. OPS CHECKED NORMAL. (M) 2 L 7 3 4F A3WE 1997032000611 19970320 00611 NM 1997 3 20 97ZZZM315 1 19961105 A 3350 SOCKET BOEING 727 727227 1384078 NM EXTERIOR FAILED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 779AT 22091 DURING PREFLIGHT, FOUND L1 EMERGENCY LIGHT INOP, OUTSIDE LIGHT. REPLACED L1 EMERGENCY LIGHT SOCKET, OPS CHECKED GOOD. ( M) 2 L 7 3 4F A3WE 1997032000612 19970320 00612 NM 1997 3 20 97ZZZM316 1 19961116 A 3350 3315048 BATTERY BOEING 727 7272B7 138407L NM CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 770AT 21953 ON PREFLIGHT, FOUND EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK. OPS CHECKED NORMAL. (M) 2 L 7 3 4F A3WE 1997032700082 19970327 00082 EA 1997 3 27 CA961025018 1 19961024 A 2760 SPOILER CLUTCH DHAV DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE LH AT SWITCH BROKEN WIRE W O OTHER J WARNING INDICATION NR NOT REPORTED 1 CA 123151 (CAN) RECURRING DEFECTS FOUND OF BROKEN SPOILER CLUTCH WIRES. IN THIS CASE THE LEFT HAND WIRE AT THE SWITCH. 2 H 7 2 4T 4 T RT A13NM E20NE 1997032700083 19970327 00083 EA 1997 3 27 CA961025019 1 19961024 A 2760 SPOILER CLUTCH DHAV DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE RIGHT AT SWITCH BROKEN WIRE W O OTHER J WARNING INDICATION NR NOT REPORTED 1 CA 123126 (CAN) RECURRING DEFECTS FOUND OF BROKEN SPOILER CLUTCH WIRES. IN THIS CASE THE LEFT UPPER WIRE AT THE SWITCH. 2 H 7 2 4T 4 T RT A13NM E20NE 1997032700085 19970327 00085 1997 3 27 CA961028004 4 19961021 A 2350 506111 SELECTOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE COPILOT AUDIO BURNT W K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 CA 313 120443 (CAN) CREW COULD SMELL ELECTRICAL BURNING ON FINAL. INSPECTION FOUND CO-PILOTS AUDIO PANEL OVERHEATED. 2 H 7 2 4T 4 T RT A13NM E20NE 1997032700087 19970327 00087 NM 1997 3 27 CA961028006 1 19961021 A 3310 7107135 INTERFACE UNIT GRIMES 7002537 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE AFCS BURNT W K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 CA 0025 120360 (CAN) DURING DESCENT THE ADVISORY LIGHTS CAME ON BRIGHT WITH AN ASSOCIATED BURNING SMELL. 2 H 7 2 4T 4 T RT A13NM E20NE 1997032700089 19970327 00089 EA 1997 3 27 CA961029001 1 19961022 A 3246 VALTBS12451 WIRE DHAV DHC2 DHC2MK3 2800107 EA PWA PT6 PT6A20 52043 EA CLEVIS LEFT HAND BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 803 PCE21710 (CAN) ON PREFLIGHT PILOT NOTICED FLOAT BRACE WIRE END FORWARD LEFT HAND BROKEN AT BRACE WIRE CLEVIS ATTACH. PART SENT TO MANUFACTURER FOR INVESTIGATION. 1 H 7 1 3T 3 T A806 E4EA 1997032700090 19970327 00090 NE 1997 3 27 CA961029003 2 19961018 A 7510 577957 MANIFOLD DUCT BOEING 737 737275C NM PWA JT8 JT8D9A 52048 NE 13TH STAGE BLEED SEPARATED W A E ENGINE SHUTDOWN J K WARNING INDICATION FLUID LOSS CL CLIMB 1 CA P665497B (CAN) THROUGH FL240 #1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. ENGINE SHUTDOWN WAS CARRIED OUT. POST FLIGHT INSPECTI ON FOUND THE 13TH STAGE BLEED AIR DUCT HAD SEPARATED AT THE FORWARD MOUNTING POSITION. FURTHER INSPECTION FOUND THE HOT BLEED AIR RELEASED CAUSED THE MELTING OF THE ENGINE ISOLATOR MOUNTS; THE SOLDER ON THE OIL PRESSURE TRANSMITTER AND THE OIL PRESSURE SWITCH; DAMAGE TO THE FUEL HEAT VALVE AND FUEL FLOW TRANSMITTER; OTHER COMPONENTS IN THE AREA ALSO SUFFERED HEAT DAMAGE. THE #1 ENGINE WAS REMOVED AND THE DAMAGED ITEMS REPLACED. THE ENGINE WAS REINSTALLED AND GROUND RUN SERVIC EABLE. 2 L 7 2 4F 4 F A16WE E2EA 1997032700091 19970327 00091 EU 1997 3 27 CA961029010 1 19961016 A 2750 FLAP AIRBUS 320 A320211 3930320 EU NR 2 DRIVE LOCKED UP W O OTHER O OTHER AP APPROACH 1 CA (CAN) ON APPROACH AFTER SELECTING FLAP 2, ECAM WARNING, FLAP FAULT, GROUND APPROACH INITIATED AND LANDING MADE WITH FLAP S LOCKED UP. WING TIP BRAKE/PRESSURE OFF BRAKE TEST COMPUTER RESELECTED, FLAP/SLAT ALL POSITIOIN CHECKED SERVICEABLE. RE D TRIP INDICATOR FOUND POPPED ON LEFT HAND #2 FLAP DRIVE AND ON RIGHT HAND #3 FLAP DRIVE. RESET, SYSTEM CHECK SERVICEABL E. 2 L 7 2 4F RT A28NM 1997032700092 19970327 00092 EU 1997 3 27 CA961029013 1 19960923 A 2750 ACTUATOR BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE FLAP BALL SCREW CONTAMINATED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA 5843A (CAN) AIRCRAFT CARRIED OUT A ZERO DEGREE 'FLAPLESS' LANDING DUE TO FLAPS BEING STUCK IN THE ZERO DEGREE POSITION. MAINTE NANCE SUSPECTED MOISTURE IN THE FLAP BALL SCREW ACTUATORS. 2 H 7 4 4F 4 F RT A49EU E6NE 1997032700094 19970327 00094 EU 1997 3 27 CA961104002 1 19961030 A 2810 FUEL TANK BRAERO BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE LT WING LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA LF05567A (CAN) FUEL LEAK NOTED AT LEFT WING UPPER CORNER. STEADY WEEP FROM AREA OF HI-LOK FASTENER. FASTENERS TORQUE TIGHTENED AN D AREA SEALED. 2 H 7 4 4F 4 F RT A49EU E6NE 1997032700095 19970327 00095 EA 1997 3 27 CA961104009 1 19961022 A 3242 C6SF13463 PUSH ROD INSERT DHAV C6SF13001 DHAV DHC6 DHC6300 EA PWA PT6 PT6A27 52043 EA BRAKE CONTROL LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA 7274 PCE40147 (CAN) ON LOWER END OF THE BRAKE CONTROL PUSH ROD THE MAGNEFORMED THREADED INSERT WAS FOUND LOOSE INSIDE THE MAGNEFORMED END. 1 H 7 2 3T 4 T A9EA E4EA 1997032700096 19970327 00096 WP 1997 3 27 CA961104013 1 19961017 A 2530 CA167072 OVEN PLUG DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE GALLEY BURNT W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA P656825D (CAN) DURING CRUISE AN ELECTRICAL BURNING SMELL WAS NOTICED COMING FROM THE FRONT AREA OF THE AIRCRAFT NEAR THE FLIGHT D ECK. INVESTIGATION REVEALED PLUG OF GALLEY OVEN #4 BURNT. PLUG REPLACED. 2 L 7 2 4F 4 F A6WE E2EA 1997032700097 19970327 00097 EU 1997 3 27 CA961104014 1 19961016 A 2530 25806531 HOT CUP AIRBUS 320 A320211 3930320 EU GALLEY ELECT SHORT W A O OTHER O OTHER CR CRUISE 1 CA (CAN) FLIGHT ATTENDANT RECEIVED ELECTRICAL SHOCK FROM THE HOT CUP IN AFT GALLEY. LARGE SPARK SEEN IN GALLEY AREA. INVEST IGATION REVEALED HOT CUP RECEPTACLE DEFECTIVE. RECEPTACLE REPLACED. 2 L 7 2 4F RT A28NM 1997032700098 19970327 00098 NE 1997 3 27 CA961104015 2 19961020 A 7230 601R5520052 OVERHEAT SENSOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE 14TH STAGE FAULTY W E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 CA 807181 (CAN) INFLIGHT SHUTDOWN #2 ENGINE. MASTER WARNING LIGHT #2 ENGINE 14TH STAGE DUCT. RIGHT DUCT FAIL LIGHT ON OVERHEAD PAN EL. WARNING LIGHT AND AURAL WAS INTERMITTENT. POST FLIGHT INSPECITON FOUND 14TH STAGE OVERHEAT SENSOR FAULTY. SENSOR WAS REPLACED. ENGINE RUN CARRIED OUT SERVICEABLE. 2 L 7 2 4F 4 F RT A21EA E15NE 1997032700099 19970327 00099 EU 1997 3 27 CA961104016 1 19961028 A 2750 COMPUTER AIRBUS 320 A320211 3930320 EU FLAP ALIGNMENT FAULT W K NONE O OTHER AP APPROACH 1 CA (CAN) ON APPROACH, FLIGHT CONTROL FLAPS LOCKED ALIGNMENT FAULT APPEARED ON E.C.A.M. WHEN FLAP MOVED TO #2 POSITION. CORR ECTIVE ACTION INVOLVED RESETING SLAT/FLAP COMPUTER #1 AND #2. ALSO FLAP WING TIP BRAKE RESET AND TEST CARRIED OUT. FLAP OPERATION AND INDICATION CHECKED SERVICEABLE. 2 L 7 2 4F RT A28NM 1997032700100 19970327 00100 NM 1997 3 27 CA961105006 1 19960923 A 3213 DCL3589 BUSH DOWTY 10100117 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE MLG STRUT CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 22038 DCL3589 120251 (CAN) MAIN LANDING GEAR STRUT BUSH CHECKED FOR REWORK AND FOUND CORRODED. SEVERAL OTHER LANDING GEAR FOUND WITH SAME PR OBLEM 2 H 7 2 4T 4 T RT A13NM E20NE 1997032700101 19970327 00101 SW 1997 3 27 CA961105501 1 19960923 A 7120 206064105102 LEG ASSEMBLY BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL ENG R/H STRUT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA CAE860057 (CAN) WHILE REMOVING TURBINE FROM AIRFRAME, THE STRUT CRACKED IN TWO. THE CRACK OCCURRED UNDER THE HOSE CLAMP. THE CLAMP HAD PROBABLY NEVER BEEN REMOVED AND THE AREA UNDERNEATH CLEANED. THIS LED TO A BUILD UP OF DIRT WHICH EVENTUALLY CORROD ED THE STRUT TO THE POINT OF FAILURE. 1 G 7 1 3U 3 U H2SW E1GL 1997032700102 19970327 00102 EU 1997 3 27 CA961112001 1 19961101 A 3320 82806101 SOCKET BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE AFT LAV BURNT W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA LF05539A (CAN) DURING MAINTENANCE SMOKE AND ELECTRICAL BURNING ODOUR NOTED IN THE REAR LAVATORY. FLUORESCENT LIGHT SOCKET FOUND B ADLY BURNED. 2 H 7 4 4F 4 F RT A49EU E6NE 1997032700103 19970327 00103 EA 1997 3 27 CA961112003 2 19960805 A 7520 D1742LOT4A FAN WHEEL ROBSIN R44 R44 7640120 WP LYC O540 O540F1B5 41532 EA COOLING FAN MISALIGNMENT W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 50 L2497240A (CAN) WITNESS MARKS MISALIGNED ON COOLING FAN. 1 G 7 1 3O 3 O H11NM E295 1997032700105 19970327 00105 NM 1997 3 27 CA961112018 1 19961023 A 3000 153212A VALVE BENDIX DHAV DHC8 DHC8101 2809002 NM PWA PW120 PW123 NE DE ICE DIST FAILED W K NONE O OTHER IN INSP/MAINT 1 CA RF3909 123138 (CAN) FAILURE OF THE DEICE DISTRIBUTION VALVE BECAUSE OF ACCUMULATION OF MOISTURE DUE TO ABSENCE OF A DRAIN HOLE. DRAIN HOLE PLUGGED BY POTTING COMPOUND. 2 H 7 2 4T 4 T RT A13NM E20NE 1997032700106 19970327 00106 NM 1997 3 27 CA961112022 1 19961022 A 6123 83910321017 CONTROLLER DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE PROP FEATHER MALFUNCTION W C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CA 10757 123073 890933 (CAN) PILOT REPORTED THAT AUTOFEATHER WOULD NOT DISARM IN FLIGHT UNTIL POWER LEVERS WERE BROUGHT BACK TO BELOW 64 PERCEN T TORQUE. AIRCRAFT THEN TO OPERATE AS PER MEL 61-3. NEXT FLIGHT ABORTED DUE TO AN UNCOMMANDED AUTOFEATHER. AIRCRAFT RETU RNED TO GATE. NEW AUTOFEATHER CONTROLLER INSTALLED. BUT SYSTEM WORKED OK EXCEPT WHEN THE A/FX TEST TOGGLE LEVERS WERE SE LECTED TO TEST. WIRING AT THE SELECTSWITCH FOUND IN BAD SHAPE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1997032700107 19970327 00107 SW 1997 3 27 CA961112027 1 19961029 A 2742 AA56142 NUT TUBES SIMMONDS DL5040M5 SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP ACTUATOR FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 773 G0612 P54158 (CAN) DURING PERIODIC INSPECTION, PITCH TRIM NOTED MAKING LOUD GRINDING NOISES. ACTUATOR REPLACED. TEAR DOWN INDICATED T HAT THE NUT TUBES WERE REPLACED AT OVERHAUL. AD 93-15-02R2 REQUIRES THAT THE OPERATOR DETERMINE IF THE NUT TUBE ASSEMBLY WAS REPLACED AND IF SO WAS IT NEW OR REWORKED. THIS INFO WAS NOT SUPPLIED BY THE OVERHAUL AGENT. THUS THE STATUS OF THE NUT TUBE COULD NOT BE DETERMINED, WHICH COULD LEAD TO THE BEING INSPECTED AT AN INCORRECT TIME. 2 L 7 2 4T 4 T RT A8SW E4WE 1997032700108 19970327 00108 EU 1997 3 27 CA961112033 1 19961029 A 2750 012130 SENSOR AIRBUS 320 A320211 3930320 EU LH FLAP FAILED W K NONE F FLT CONT AFFECTED AP APPROACH 1 CA (CAN) ON APPROACH FLIGHT CONTROL FLAPS LOCKED ALIGNMENT FAULT APPEARED ON ECAM WHEN FLAP MOVED TO 2 POSITION. LH FLAP AT TACHMENT FAILURE DETECTION SENSOR 37 CV REPLACED. SYSTEM TEST SERVICEABLE. 2 L 7 2 4F RT A28NM 1997032700109 19970327 00109 WP 1997 3 27 CA961112034 1 19961030 A 2170 1808491 COALESCER BAG DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE LT AIR COND SATURATED W K NONE O OTHER TX TAXI/GRND HDL 1 CA P654059D (CAN) DURIG DEPARTURE CHECK WITH APU RUNNING SUPPLYING PRESSURE ON LEFT HAND AIR CONDITIONING PACK A STRONG ODOUR WITH L IGHT SMOKE WAS NOTED IN THE CABIN AND DUCT TEMPERATURE AROUND 70 DEGREES. LEFT HAND COALESCER BAG CHANGED. ALSO CHECKED AIR CYLING MACHINE FOR LEAKS AND OIL LEVEL. 2 L 7 2 4F 4 F A6WE E2EA 1997032700110 19970327 00110 NE 1997 3 27 CA961112037 2 19961002 A 7250 BEARING DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE #1 ENG NR 6 LEAKING OIL W E ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 CA P657413D (CAN) INFLIGHT SHUTDOWN CARRIED OUT ON #1 ENGINE DUE TO LOSS OF OIL QUANTITY. POST FLIGHT INSPECTION FOUND NO OIL IN #1 ENGINE OIL RESERVOIR. OIL WAS COMING FROM THE ENGINE EXHAUST. #1 ENGINE CHANGED. THE OIL LOSS WAS DUE TO #6 BEARING FAIL URE AND THE OIL WAS LOST THROUGH THE #6 CARBON SEAL. 2 L 7 2 4F 4 F A6WE E2EA 1997032700111 19970327 00111 EA 1997 3 27 CA961112038 1 19961021 A 2150 T-FITTING CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE LT AIR COND LEAKING W D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA 4491 807199 (CAN) DURING DEPARTURE CABIN FILLED WITH SMOKE. FOUND LEFT HAND AIR CONDITIONING PACK OVERHEATING. LEAK FOUND AT 'T' FIT TING IN SENSE LINE. 2 L 7 2 4F 4 F RT A21EA E15NE 1997032700114 19970327 00114 NE 1997 3 27 CA970114002 2 19961227 A 7250 GP SECTION BELL 205 205A1 1181414 SW LYC T53 T5313B 41549 NE ENGINE DAMAGED W E ENGINE SHUTDOWN B E M SMOKE/FUMES/ODORS/SPARKS VIBRATION/BUFFET OVER TEMP TX TAXI/GRND HDL 1 CA LEO07611 (CAN) AIRCRAFT LANDED AND ENGINE WAS SHUTDOWN. ON THE NEXT START THE ENGINE WAS GOING TO A HOT START, SO THE START WAS A BORTED. ON THE SECOND START ATTEMPT AN ENGINE VIBRATION WAS FELT AND THE EGT BEGAN TO RISE RAPIDLY AND COULD NOT BE CONT AINED BY CUTTING OFF THE FUEL AND CLOSING THE THROTTLE. THE EGT REACHED 750 DEGREES C. THE ENGINE WAS REMOVED AND INITIA L INSPECTION REVEALED THE GAS PRODUCER SECTION HAD BURNED OFF ALL THE BLADES ON THE #2 STAGE TURBINE WHEEL, GP NOZZLES W ERE BURNT, PT SECTION, NOZZLES WERE BURNT, BLADES DAMAGED, BROKEN AND BURNT. THERE WAS NO EVIDENCE OF F.O.D. REPORT TO F OLLOW. 1 G 7 1 4U 4 U H1SW E17EA 1997032700117 19970327 00117 NE 1997 3 27 CA970129010 2 19961130 A 7230 COMPRESSOR DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE #2 ENGINE DAMAGED W A E UNSCHED LANDING ENGINE SHUTDOWN M OVER TEMP TO TAKEOFF 1 CA P657506D (CAN) SHORTLY AFTER TAKEOFF AT APPROXIMATELY 500 FEET THE CREW HEARD A LOUD BANG COMPRESSOR STALL, THEN A SECOND ONE. TH E RIGHT ENGINE EGT WENT TO THE HIGH ZONE. THE #2 ENGINE WAS SHUTDOWN AND THE AIRCRAFT RETURNED TO POINT OF DEPARTURE. PO ST FLIGHT INSPECTION FOUND METAL PARTICLES IN THE EXHAUST PIPE AND SIGNS OF COMPRESSOR FAILURE. FINAL REPORT TO FOLLOW. 2 L 7 2 4F 4 F A6WE E2EA 1997032700264 19970327 00264 GL 1997 3 27 ERAA96362 2 19961210 A 7250 23007202 BEARING BOLKMS 105 BO105A EU ALLSN 250C 250C20B 03013 GL NR 7 GALLED A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 291EH 1742 S842 ROLLERS ARE GALLED & GROOVED. 1 G 7 2 3U 3 U H3EU E4CE 1997032700265 19970327 00265 GL 1997 3 27 ERAA96365 2 19961212 A 7323 252466714 GOVERNOR BOLKMS 105 BO105A EU ALLSN 250C 250C20B 03013 GL ENGINE STIFF A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 296EH 6852 S849 GOVERNOR REM'D FROM 296EH 10/28/96 AND SENT FOR REPAIR; REC'D BACK AT ERA 12-12-96 AND WAS REJECTED BECAUSE OF GOVERNOR ARM BEING STIFF. 1 G 7 2 3U 3 U H3EU E4CE 1997032700318 19970327 00318 WP 1997 3 27 CALA9700385 1 19961211 A 5313 LONGERON DOUG DC10 DC1030 3023501 WP BS 1119-1139 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37078 46926 INSPECTION FOUND LONGERON 4L CORRODED BETWEEN BS 1119 TO 1139. THE CORRODED SPLICE WAS REMOVED AND A NEW ONE WAS FABRIC ATED AND INSTALLED IAW SRM 53-10-00 FIGURE 3, 53-13-01 FIGURE 33 AND 51-21-01. 2 L 7 3 4F A22WE 1997032700319 19970327 00319 WP 1997 3 27 CALA9700386 1 19961209 A 5320 CASTING DOUG DC10 DC1030 3023501 WP BS 1321-1341 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37078 46926 INSPECTION FOUND STRINGER 24R CASTING CORRODED BETWEEN STA 1321 AND 1341. THE CASTING WAS REMOVED AND REPLACED IAW SRM 51-33-01. 2 L 7 3 4F A22WE 1997032700320 19970327 00320 WP 1997 3 27 CALA9700387 1 19961217 A 5414 PANEL DOUG DC10 DC1030 3023501 WP NR 1 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37078 46926 INSPECTION FOUND A 1 INCH CRACK AT CUTOUT OF NR 1 ENGINE PYLON PANEL NR 437DR. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-00-01, FIGURE 1 AND 2. 2 L 7 3 4F A22WE 1997032700321 19970327 00321 WP 1997 3 27 CALA9700388 1 19961206 A 5312 BULKHEAD ANGLE DOUG DC10 DC1030 3023501 WP BS 1521 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37078 46926 INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT L-ANGLE AT CENTER CARGO FORWARD BULKHEAD FS 1521, RBL 19. THE CRACK WA S STOP DRILLED, AN L-ANGLE AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-00-01, FIGURE 2 AND 51-31-01. 2 L 7 3 4F A22WE 1997032700322 19970327 00322 WP 1997 3 27 CALA9700389 1 19961207 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 420 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37078 46926 INSPECTION FOUND FLOORBOARD SUPPORT CRACKED IN THREE PLACES AT STA 420, X-13 TO X-22. THE CRACKS WERE .125 INCH LONG. T HE FLOOR SUPPORT WAS REMOVED, A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-31-01, 51-21-01 AND 51-35-01. 2 L 7 3 4F A22WE 1997032700323 19970327 00323 WP 1997 3 27 CALA9700390 1 19961211 A 5320 ANGLE DOUG DC10 DC1030 3023501 WP BS 1341 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37078 46926 INSPECTION FOUND A 1.5 INCH CRACK ON SUPPORT ANGLE UNDER BODY FILLET JUST ABOVE WING AT FS 1341R. THE CRACKED AREA WAS REMOVED AND A NEW PART WAS FABRICATED AND INSTALLED IAW SRM 51-31-01, 51-21-01 AND 53-53-01. 2 L 7 3 4F A22WE 1997032700324 19970327 00324 WP 1997 3 27 CALA9700391 1 19961210 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 2004 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37078 46926 INSPECTION FOUND CORROSION ON LAV TIE DOWN FLOOR SUPPORT AT STA 2004, X-55. THE FLOOR SUPPORT WAS REPAIRED IAW SRM 53-7 0-01, FIGURE 13. 2 L 7 3 4F A22WE 1997032700325 19970327 00325 WP 1997 3 27 CALA9700392 1 19961228 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 497 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37078 46926 INSPECTION FOUND CORROSION ON FLOOR SUPPORT AROUND GALLEY FLOOR SPACER AT STA 497, X+22. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-21-01 AND 51-31-01. TWO EACH BOSSES WERE REMOVED AND RE PLACED IAW SRM 51-31-01. THE DOME NUTS WERE REPLACED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1997032700326 19970327 00326 WP 1997 3 27 CALA9700393 1 19961106 A 5311 FRAME DOUG DC10 DC1030 3023501 WP BS 1781 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37078 46926 INSPECTION FOUND FORWARD SIDE OF FRAME CORRODED IN AFT CARGO BILGE AREA AT STA 1781 FROM LONGERON 50L TO 50R. THE CORRO DED SECTION WAS CUT OUT, AN L-ANGLE DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-00, FIGURE 8, 51-21-0 1 AND 53-30-01 FIGURE 8. 2 L 7 3 4F A22WE 1997032700327 19970327 00327 WP 1997 3 27 CALA9700394 1 19961210 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1915/2004 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37078 46926 INSPECTION FOUND LAV TIE DOWN FLOOR SUPPORT CORRODED AT STA 1915 AND 2004, LBL X+55. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 53-70-00. 2 L 7 3 4F A22WE 1997032700328 19970327 00328 WP 1997 3 27 CALA9700395 1 19961221 A 5532 PANEL DOUG DC10 DC1030 3023501 WP VERT STAB GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37078 46926 INSPECTION FOUND A GOUGE AT CORNER EDGE OF VERTICAL STABILIZER ACCESS PANEL NR 373EL. A DOUBLER WAS FABRICATED AND INST ALLED IAW SRM 55-00-01, FIGURE 3 AND 51-21-01. 2 L 7 3 4F A22WE 1997032700329 19970327 00329 WP 1997 3 27 CALA9700396 1 19961127 A 5320 ANGLE DOUG DC10 DC1030 3023501 WP ADF ANTENNA CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37078 46926 INSPECTION FOUND L-ANGLE CORRODED AT FORWARD ADF LOOP ANTENNA. AN L-ANGLE WAS FABRICATED AND INSTALLED WITH NUT PLATES IAW SRM 53-00-01, FIGURE 2, SHEET 2, 51-11-01, 51-31-01, 51-21-01 AND 51-30-00. 2 L 7 3 4F A22WE 1997032700330 19970327 00330 WP 1997 3 27 CALA9700397 1 19961130 A 5730 PANEL DOUG DC10 DC1030 3023501 WP RT WING DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37078 46926 INSPECTION FOUND FOUR DENTS ON UPPER SURFACE OF RT WING TRAILING EDGE PANEL 641HB. A DOUBLER AND FOUR FILLERS WERE FABR ICATED AND INSTALLED IAW SRM 51-71-00, FIGURE 33. 2 L 7 3 4F A22WE 1997032700331 19970327 00331 WP 1997 3 27 CALA9700398 1 19961205 A 5754 SKIN DOUG DC10 DC1030 3023501 WP NR 1 LE SLAT RIPPLED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37078 46926 INSPECTION FOUND RIPPLING ONE FOOT IN DIAMETER IN RT WING NR 1 SLAT AT INBOARD END. THE RIPPLED AREA WAS CUT OUT, A SKI N INSERT, SPLICE STRAPS, DOUBLERS AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 51-10-00, FIGURE 43 AND 51-31-01. 2 L 7 3 4F A22WE 1997032700332 19970327 00332 WP 1997 3 27 CALA9700399 1 19961127 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 879/899 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37078 46926 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 879 AND 899, Y= -44. CHANNEL FLOOR SUPPORT ANGLES AND BOSSES WERE FABRIC ATED AND INSTALLED IAW SRM 51-31-01, 51-21-01 AND 53-70-00. 2 L 7 3 4F A22WE 1997032700333 19970327 00333 WP 1997 3 27 CALA9700400 1 19961228 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1887 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37078 46926 INSPECTION FOUND FLOORBOARD SUPPORT CRACKED IN SIX PLACES AT STA 1887, X = 38-57. THE CRACKS WERE 1 OR LESS IN LENGTH. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-31-01 AND 51-21-01. 2 L 7 3 4F A22WE 1997032700337 19970327 00337 WP 1997 3 27 CALA9700404 1 19961210 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1986 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37078 46926 INSPECTION FOUND TWO CRACKS APPROXIMATELY .5 INCH LONG IN FLOORBOARD SUPPORT AT STA 1986, X + 1 TO 16. A NEW SUPPORT WA S FABRICATED AND INSTALLED IAW SRM 51-21-01 AND 51-31-01. 2 L 7 3 4F A22WE 1997032700338 19970327 00338 WP 1997 3 27 CALA9700405 1 19961210 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1943 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37078 46926 INSPECTION FOUND A .35 INCH CRACK IN FLOORBOARD SUPPORT AT STA 1943, X-1 TO 16. A NEW SUPPORT WAS FABRICATED AND INSTAL LED IAW SRM 51-21-01 AND 51-31-01. 2 L 7 3 4F A22WE 1997032700339 19970327 00339 WP 1997 3 27 CALA9700406 1 19961210 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1943 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37078 46926 INSPECTION FOUND THREE CRACKS UP TO .30 INCH LONG IN FLOORBOARD SUPPORT AT STA 1943, X - 11 TO 16. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-21-01 AND 51-31-01. 2 L 7 3 4F A22WE 1997032700340 19970327 00340 WP 1997 3 27 CALA9700407 1 19961210 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1921 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37078 46926 INSPECTION FOUND A .20 INCH CRACK IN FLOORBOARD SUPPORT AT STA 1921, X + 1 TO 16. TWO CRACKS UP TO .30 INCH LONG WERE F OUND IN FLOORBOARD SUPPORT AT STA 1921, X - 1 TO 16. NEW FLOOR SUPPORTS WERE FABRICATED AND INSTALLED IAW SRM 51-21-01 AND 51-31-01. 2 L 7 3 4F A22WE 1997032700341 19970327 00341 WP 1997 3 27 CALA9700408 1 19961210 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1965 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37078 46926 INSPECTION FOUND TWO CRACKS UP TO .35 LONG IN FLOORBOARD SUPPORT AT STA 1965, X -1 TO 16. ALSO, TWO CRACKS UP TO .20 IN CH LONG WERE FOUND IN FLOORBOARD SUPPORT AT STA 1965, X + 1 TO 16. NEW FLOOR SUPPORTS WERE FABRICATED AND INSTALLED IAW SRM 51-21-01 AND 51-31-01. 2 L 7 3 4F A22WE 1997032700386 19970327 00386 WP 1997 3 27 ABXA9700076 1 19960531 A 3231 3923167501 ROD ASSY DOUG DC9 DC941 302207N WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 DURING ACCEPTANCE INSPECTION, WHILE ACCOMPLISHING AD 91-22-07, THE LEFT MAIN LANDING GEAR FLYING DOOR LINKAGE WAS FOUND WORN AT THE LOWER ATTACH POINT. THE LINKAGE WAS REPAIRED IAW DC 9 OHM 32-10-6. 2 L 7 2 4F A6WE 1997032700387 19970327 00387 WP 1997 3 27 ABXA9700077 1 19960625 A 5720 99193574 FITTING DOUG DC9 DC932 3022066 WP WS 267 MISDRILLED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 DURING C-CHECK, FOUND A .1875 INCH HOLE DRILLED THROUGH THE UPPER SURFACE OF THE WING INBOARD FLAP ATTACH FITTING. REPA IRED IAW ABX REA D957-15559-MR. 2 L 7 2 4F A6WE 1997032700388 19970327 00388 WP 1997 3 27 ABXA970078 1 19960711 A 3231 S24312157A016 BUSHING DOUG DC9 DC941 302207N WP RT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 957AX 47759 DURING C-CHECK AND COMPLIANCE WITH AD 91-22-07, FOUND RIGHT DOOR LINK TO DOUBLE ROD LINK HAS EXESSIVE PLAY. REPLACED BU SHING IAW DC-9 OHM 32-10-06. 2 L 7 2 4F A6WE 1997032700389 19970327 00389 WP 1997 3 27 ABXA9700079 1 19960726 A 3231 2245042 HINGE PIN DOUG DC9 DC931 3022065 WP LT MLG DOOR CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 929AX 47148 WHILE COMPLYING WITH N-CARD 3219 AND AD 91-22-07, FOUND HINGE PINS ON LEFT MAIN LANDING GEAR OUTBOARD DOORS ARTICULATING SECTION RUSTED. REPLACED 3 ARTICULATING DOOR HINGE PINS IAW DC-9 OHM 32-10-6. 2 L 7 2 4F A6WE 1997032700390 19970327 00390 WP 1997 3 27 ABXA9700082 1 19960813 A 5312 5910163184 BULKHEAD WEB DOUG DC9 DC931 3022065 WP BS 996 DRILL MARKS A ABXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK, FOUND DRILL STARTS IN APB WEB. REPAIRED IAW ABX REA D953-15885-MR. 2 L 7 2 4F A6WE 1997032700391 19970327 00391 WP 1997 3 27 ABXA9700083 1 19960905 A 3231 3923159505 CONTROL LINKAGE DOUG DC9 DC931 3022065 WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, WHILE ACCOMPLISHING AD 91-22-07, THE LEFT MAIN LANDING GEAR OUTBOARD DOOR CONTROL LINKAGE WAS FOUND WORN . THE CONTROL LINKAGE WAS REPLACED IAW DC-9 M/M 32-12-1. 2 L 7 2 4F A6WE 1997032700392 19970327 00392 WP 1997 3 27 ABXA9700084 1 19960826 A 5521 5910412515 SPAR DOUG DC9 DC931 3022065 WP LT ELEVATOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 907AX 47203 DURING COMPLIANCE OF AD 79-19-02, SB 55-28 FOUND LT ELEVATOR REAR SPAR CRACKED. REPLACED LT ELEVATOR IAW DC-9 MAINTANC E MANUAL TEMPORY REVISION 27-30-2. 2 L 7 2 4F A6WE 1997032700393 19970327 00393 WP 1997 3 27 ABXA9700080 1 19960806 A 5280 HB218600 BUSHING DOUG DC9 DC932 3022066 WP RT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 985AX 47522 DURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND RIGHT MAIN LANDING GEAR DOOR HINGE WORN. REPLACED ALL BUSHINGS IAW DC-9 SRM 32-12-1. 2 L 7 2 4F A6WE 1997032700394 19970327 00394 WP 1997 3 27 ABXA9700085 1 19960824 A 3231 NAS130418 BOLT DOUG DC9 DC941 302207N WP RT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47494 DURING COMPLIANCE OF AD 91-22-07, ASB 32-244 FOUND RT MAIN LANDING GEAR OUTBOARD DOOR LINK LOOSE. REPLACED BOLT IAW DC- 9 OVERHAUL MANUAL. 2 L 7 2 4F A6WE 1997032700395 19970327 00395 WP 1997 3 27 ABXA9700081 1 19960812 A 3231 S2210370P4109 BUSHING DOUG DC9 DC932 3022066 WP RT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 989AX 47314 DURING COMPLIANCE OF AD 91-22-07, ASB 32-244 FOUND RT MAIN LANDING GEAR OUTBOARD DOOR LINKAGE ARM WORN. REPLACED RT MAI N LANDING GEAR OUTBOARD DOOR LINKAGE ARM BUSHING IAW DC-9 OVERHAUL MANUAL CHAPTER 32. 2 L 7 2 4F A6WE 1997032700396 19970327 00396 WP 1997 3 27 ABXA9700086 1 19960919 A 5320 CR3212 RIVETS DOUG DC9 DC932 3022066 WP BS 256-313 MISINSTALLED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 DURING C-CHECK AND COMPLIANCE WITH AD 96-07-51, FOUND CHERRY RIVETS INSTALLED IN FUSELAGE SKIN REPAIRS FROM STA 256 TO 3 13. REMOVED CHERRY LOCK RIVETS AND INSTALLED SOLID FASTENERS IAW DC-9 SRM 51-30-2, 53-30-5, 51-30-1. 2 L 7 2 4F A6WE 1997032700397 19970327 00397 WP 1997 3 27 ABXA9700087 1 19960521 A 5312 9915558 BULKHEAD CLIPS DOUG DC9 DC941 302207N WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 DURING ACCEPTANCE INSPECTION, WHILE ACCOMPLISHING AD 92-22-08, SEVERAL RADIUS CLIPS WERE FOUND CRACKED ON THE FORWARD F ACE OF THE AFT PRESURE BULKHEAD. THESE CLIPS ARE COMMON DEFECTS FOUND IN SERVICE BULLETIN 53-166. THE CLIPS WERE REPAI RED IAW DC-9 SRM 51-30-5 AND DRAWING K05159. 2 L 7 2 4F A6WE 1997032700398 19970327 00398 WP 1997 3 27 ABXA9700088 1 19960611 A 5320 591015873 JAMB DOUG DC9 DC941 302207N WP BS 1012 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 DURING ACCEPTANCE INSPECTION, WHILE ACCOMPLISHING AD 92-22-08, THE AFT LOWER CARGO DOOR JAMB WAS FOUND CRACKED AT STATIO N 1012 BETWEEN LONGERONS 26 AND 27 RIGHT. THE DOOR JAMB WAS REPAIRED IAW DC-9 SRM 53-05 FIG 44. 2 L 7 2 4F A6WE 1997032700399 19970327 00399 WP 1997 3 27 ABXA9700089 1 19960417 A 5313 591140887 LONGERON DOUG DC9 DC941 302207N WP BS 446 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 DURING ACCEPTANCE INSPECTION, WHILE ACCOMPLISHING AD 92-22-08, A LONGERON AT 5 LEFT WAS FOUND CRACKED AT STATION 446. T HE LONGERON WAS REPLACED BETWEEN STATIONS 420 AND 454 IAW THE DC-9 SRM 53-02 FIG 2. 2 L 7 2 4F A6WE 1997032700400 19970327 00400 WP 1997 3 27 ABXA9700090 1 19960522 A 5320 391617450IN FITTING DOUG DC9 DC941 302207N WP BS 645 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 DURING ACCEPTANCE INSPECTION, WHILE ACCOMPLISHING AD 92-22-08, A LONGERON END FITTING WAS FOUND CRACKED AT STATION 645 L ONGERON 29 RIGHT. THE LONGERON WAS REPLACED BETWEEN STATIONS 420 AND 454 IAW THE DC-9 SRM 53-30-5. 2 L 7 2 4F A6WE 1997032700401 19970327 00401 WP 1997 3 27 ABXA9700091 1 19960606 A 5312 591142717 BULKHEAD TEE DOUG DC9 DC941 302207N WP AFT PRESS BLKHD DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 DURING ACCEPTANCE INSPECTION, THE AFT PRESSURE BULKHEAD LOWER TEE WAS FOUND TO BE GOUGED AND HAVE A HOLE DRILLED THROUGH THE TEE AT LONGERON 30. THE TEE SECTION WAS REPLACED AND TRIMMED FOR EASE OF INSTALLATION IAW REA D953-15368-MR, DC-9 SRM 51-30-5 AND 51-30-2. 2 L 7 2 4F A6WE 1997032700402 19970327 00402 WP 1997 3 27 ABXA9700092 1 19960608 A 5330 59114063 SKIN DOUG DC9 DC941 302207N WP FUSELAGE GOUGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 DURING ACCEPTANCE INSPECTION, THE FUSELAGE SKIN WAS FOUND GOUGED FOWARD OF THE MAIN ENTRY DOOR AT LONGERON 16 LEFT. THE SKIN WAS REPAIRED IAW REA D953-15392-MR. 2 L 7 2 4F A6WE 1997032700403 19970327 00403 WP 1997 3 27 ABXA9700093 1 19960613 A 5315 99115957 FLOORBEAM DOUG DC9 DC941 302207N WP BS 160 DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 DURING ACCEPTANCE INSPECTION, THE FLOORBEAM AT STATION 160 WAS FOUND TO HAVE SEVERAL DOUBLE DRILLED AND CLOSELY SPACED H OLES. THE FLOORBEAM WAS REPAIRED IAW REA D953-15436-MR. 2 L 7 2 4F A6WE 1997032700404 19970327 00404 WP 1997 3 27 ABXA9700094 1 19960516 A 5743 59248419 TRUNNION DOUG DC9 DC941 302207N WP LT MLG CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 DURING ACCEPTANCE INSPECTION, THE LEFT MAIN LANDING GEAR TRUNNION WAS FOUND GOUGED AND CORRODED. THE TRUNNION WAS REPAI RED IAW REA D957-15353-MR AND DC-9 DRAWING K05177. 2 L 7 2 4F A6WE 1997032700405 19970327 00405 WP 1997 3 27 ABXA9700095 1 19960613 A 5315 99115445 FLOORBEAM DOUG DC9 DC941 302207N WP BS 237 DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 DURING ACCEPTANCE INSPECTION, THE FLOORBEAM AT STATION 237 WAS FOUND TO HAVE TWO GOUGES IN THE UPPER FOWARD FLANGE AT LB L 6. THE FLOORBEAM WAS REPAIRED IAW REA D953-15500-MR. 2 L 7 2 4F A6WE 1997032700406 19970327 00406 WP 1997 3 27 ABXA9700096 1 19960514 A 5311 39248361 FRAME DOUG DC9 DC941 302207N WP BS 870 DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 DURING D-CHECK, THE FUSELAGE FRAME AT STATION 870 AT LONGERON 5 RT HAD MISSING FASTENERS AND DOUBLE DRILLED HOLES. THE FRAME WAS REPAIRED IAW REA D953-15220-MR. 2 L 7 2 4F A6WE 1997032700407 19970327 00407 WP 1997 3 27 ABXA9700097 1 19960514 A 5311 39259821 FRAME DOUG DC9 DC941 302207N WP BS 889 DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 DURING ACCEPTANCE INSPECTION, THE FUSELAGE AT STATION 889 AT LONGERON 5 RT HAD MISSING FASTENERS AND DOUBLE DRILLED HOLE S. THE FRAME WAS REPAIRED IAW REA D953-15220-MR. 2 L 7 2 4F A6WE 1997032700408 19970327 00408 WP 1997 3 27 ABXA9700098 1 19960514 A 5311 39259831 FRAME DOUG DC9 DC941 302207N WP BS 946 DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 DURING ACCEPTANCE INSPECTION, THE FUSELAGE FRAME AT STATION 946 AT LONGERON 5 RT HAD MISSING FASTENERS AND DOUBLE DRILLE D HOLES. THE FRAME WAS REPAIRED IAW REA D953-15220-MR. 2 L 7 2 4F A6WE 1997032700409 19970327 00409 WP 1997 3 27 ABXA9700099 1 19960514 A 5311 99196031 FRAME DOUG DC9 DC941 302207N WP BS 1005 DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 DURING ACCEPTANCE INSPECTION, THE FUSELAGE FRAME AT STATION 1005 AT LONGERON 5 RT HAD MISSING FASTENERS AND DOUBLE DRILL ED HOLES. THE FRAME WAS REPAIRED IAW REA D953-15220-MR. 2 L 7 2 4F A6WE 1997032700410 19970327 00410 WP 1997 3 27 ABXA9700100 1 19960514 A 5311 9957739507 FRAME DOUG DC9 DC941 302207N WP BS 1012 DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 DURING ACCEPTANCE INSPECTION, THE FUSELAGE FRAME AT STATION 1012 AT LONGERON 5 RT HAD MISSING FASTENERS AND DOUBLE DRILL ED HOLES. THE FRAME WAS REPAIRED IAW REA D953-15220-MR. 2 L 7 2 4F A6WE 1997032700411 19970327 00411 WP 1997 3 27 ABXA9700101 1 19960530 A 5311 5920337 FRAME DOUG DC9 DC941 302207N WP FUSELAGE DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 DURING ACCEPTANCE INSPECTION, DOUBLE DRILLED HOLES WERE FOUND ON FRAMES AT FUSELAGE STATIONS 655, 617 AND 718 AT LONGERO NS 4 LEFT AND RIGHT AND 737 AT LONGERON 5 LEFT. THE FRAMES WERE REPAIRED IAW REA D953-15501-MR. 2 L 7 2 4F A6WE 1997032700412 19970327 00412 WP 1997 3 27 ABXA9700102 1 19960418 A 5744 5912596501 FITTING DOUG DC9 DC941 302207N WP LT WING WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 DURING ACCEPTANCE INSPECTION, THE LEFT WING OUTBOARD FLAP HINGE FITTING PIVOT POINT BUSHINGS WERE FOUND WORN AND GOUGED. THE HINGE FITTING WAS REPAIRED IAW REA D927-15041-MR. 2 L 7 2 4F A6WE 1997032700413 19970327 00413 WP 1997 3 27 ABXA9700103 1 19960409 A 5312 591757321 BULKHEAD DOUG DC9 DC941 302207N WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 DURING ACCEPTANCE INSPECTION, CRACKS WERE FOUND IN THE AFT PRESSURE BULKHEAD DOOR JAMB AT THE UPPER FOWARD RIGHT CORNER. THE FRAME WAS REPLACED AND THE SKIN WAS REPAIRED IAW THE DC-9 SRM 53-05 FIG 76. 2 L 7 2 4F A6WE 1997032700414 19970327 00414 WP 1997 3 27 ABXA9700104 1 19960515 A 5330 59208022 SKIN DOUG DC9 DC941 302207N WP BS 440-495 DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 DURING ACCEPTANCE INSPECTION, THE FUSELAGE SKIN AND FUSELAGE FRAME SPLICE HAD AN EXISTING REPAIR WHICH DID NOT CONFORM T O THE DC-9 SRM, STATION 440 TO 495 AT LONGERON 15 TO 18 RIGHT. THE SKIN WAS REPAIRED IAW REA D953-15228-MR. 2 L 7 2 4F A6WE 1997032700415 19970327 00415 WP 1997 3 27 ABXA9700105 1 19960606 A 5330 591993121 SKIN DOUG DC9 DC941 302207N WP FUSELAGE DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 DURING ACCEPTANCE INSPECTION, THE WATER SUPPLY PANEL WAS DEACTIVATED PER ABX EA FS-38-AA04. THE EXISTING SERVICE PANEL DOOR WAS DAMAGED BEYOND REPAIR AND REQUIRES AN ALTERNATIVE METHOD FOR PLUGGING THE PANEL ASSY OPENING. THE SKIN WAS REP AIRED IAW REA D938-15221-MR. 2 L 7 2 4F A6WE 1997032700416 19970327 00416 WP 1997 3 27 ABXA9700106 1 19960424 A 5320 5913055504 FITTING DOUG DC9 DC941 302207N WP BS 636 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 DURING ACCEPTANCE INSPECTION, WHILE ACCOMPLISHING AD 92-22-08, THE RIGHT PORK CHOP FITTING FOR THE CENTER TANK AT STATIO N 636 WAS FOUND CORRODED. THE FITTING WAS REPLACED IAW DC-9 SRM 51-30-5 AND 51-30-2. 2 L 7 2 4F A6WE 1997032700417 19970327 00417 WP 1997 3 27 ABXA9700107 1 19960522 A 5313 591140617N LONGERON DOUG DC9 DC941 302207N WP BS 200 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 DURING ACCEPTANCE INSPECTION, WHILE ACCOMPLISHING AD 92-22-08, A LONGERON WAS FOUND CRACKED AT 4 LEFT STATION 200. THE LONGERON WAS REPLACED IAW DC-9 STM 51-30-5 AND 51-30-2. 2 L 7 2 4F A6WE 1997032700418 19970327 00418 WP 1997 3 27 ABXA9700108 1 19960730 A 7830 5958782501 LINK DOUG DC9 DC931 3022065 WP NR 2 TR UNIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK AND COMPLIANCE WITH AD 75-14-06, 90-18-03, FOUND NR 2 ENGINE UPPER OUTBOARD THRUST REVERSER DRIVER LINK C RACKED. REPLACED IAW DC-9 M/M 78-31-5. 2 L 7 2 4F A6WE 1997032700419 19970327 00419 WP 1997 3 27 ABXA9700109 1 19960725 A 5321 9910078871 FLOOR PANEL DOUG DC9 DC931 3022065 WP BS 160 PUNCTURED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND HOLE IN SUBFLOOR STA 160. 2 L 7 2 4F A6WE 1997032700420 19970327 00420 WP 1997 3 27 ABXA9700110 1 19960724 A 5320 CHANNEL DOUG DC9 DC931 3022065 WP BS 200 BENT A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND H-CHANNEL BENT APPROXIMATELY STA 200. 2 L 7 2 4F A6WE 1997032700421 19970327 00421 WP 1997 3 27 ABXA9700111 1 19960812 A 5320 99101515 CUSP WEB DOUG DC9 DC931 3022065 WP BS 639-658 TORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK, FOUND CUSP WEB DAMAGED AT STA 639 LEFT SIDE. REPAIRED IAW ABX REA D953-15889-MR. 2 L 7 2 4F A6WE 1997032700422 19970327 00422 WP 1997 3 27 ABXA9700112 1 19960813 A 5712 99193466 RIB DOUG DC9 DC931 3022065 WP WS 20 DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK, FOUND RIGHT WING RIB LOWER T-CAP WITH A .50 DIAMETER HOLE DRILLED IN IT. REPAIRED IAW ABX REA D957-1586 4-MR. 2 L 7 2 4F A6WE 1997032700423 19970327 00423 WP 1997 3 27 ABXA9700113 1 19960821 A 5720 2913254 SPLICE DOUG DC9 DC931 3022065 WP STRINGER DRILLED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK, FOUND 2 HOLES DRILLED IN RADIUS OF SPLICE ANGLES ON STRINGER NR 17. REPAIRED IAW ABX REA D957-15944-MR. 2 L 7 2 4F A6WE 1997032700424 19970327 00424 WP 1997 3 27 ABXA9700114 1 19960821 A 5311 991960317 FRAME DOUG DC9 DC931 3022065 WP BS 889 DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK, FOUND FRAME 899 DAMAGED. 2 L 7 2 4F A6WE 1997032700425 19970327 00425 WP 1997 3 27 ABXA9700115 1 19960805 A 5330 9911535503 WINDOW BELT DOUG DC9 DC931 3022065 WP BS 737 DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK, FOUND PREVIOUS FLUSH BUSHING REPAIR IN WINDOW BELT PANEL AT STATION 737L WHICH WAS REMOVED TO FACILITATE FRAME 737L REPLACEMENT. REPAIRED IAW ABX REA D953-15820-MR. 2 L 7 2 4F A6WE 1997032700426 19970327 00426 WP 1997 3 27 ABXA9700116 1 19960804 A 5330 591142125 SKIN DOUG DC9 DC931 3022065 WP BS 760 DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK, FOUND CLASS 3 REPAIR AT STATION 760 AT LONGERON 30. REPAIRED IAW ABX REA D953-15793-MR. 2 L 7 2 4F A6WE 1997032700427 19970327 00427 WP 1997 3 27 ABXA9700117 1 19960802 A 5320 9910079871 DIAPHRAM DOUG DC9 DC931 3022065 WP BS 200 CUT A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK AND ACCOMPLISHMENT OF EA NR FS-53-3815, IT WAS NECESSARY TO CUT THE FOWARD DIAPHRAM TO FACILITATE SEAT TR ACK REMOVAL/REINSTALLATION. REPAIRED IAW ABX REA D953-15866-MR. 2 L 7 2 4F A6WE 1997032700428 19970327 00428 WP 1997 3 27 ABXA9700118 1 19960809 A 5312 5910163260 BULKHEAD TEE DOUG DC9 DC931 3022065 WP BS 996 DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK, FOUND BUCKING BAR MARKS ON APB UPPER T-CAP. REPAIRED IAW ABX REA D953-15875-MR. 2 L 7 2 4F A6WE 1997032700429 19970327 00429 WP 1997 3 27 ABXA9700119 1 19960731 A 5713 3911238504 STRINGER DOUG DC9 DC931 3022065 WP BS 58 GOUGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND STRINGER NR 22 GOUGED BELOW AFT TENSION BOLT AT BULKHEAD 58 RIGHT. REPAIRED IAW DC-9 SRM 57-03. 2 L 7 2 4F A6WE 1997032700430 19970327 00430 WP 1997 3 27 ABXA9700120 1 19960825 A 5347 593008413 SEAT TRACK DOUG DC9 DC931 3022065 WP BS 160-218 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND SEAT EXFOLIATED STATION 160 TO 218. REPLACED TRACK IAW DC-9 SRM 5 1-30-1, DRAWING K05406. 2 L 7 2 4F A6WE 1997032700431 19970327 00431 WP 1997 3 27 ABXA9700121 1 19960723 A 5347 59300845 SEAT TRACK DOUG DC9 DC931 3022065 WP BS 216-235 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND SEAT TRACK EXFOLIATED STATION 216 TO 235. BLENDED IAW DC-9 SRM 51 -10-3. 2 L 7 2 4F A6WE 1997032700432 19970327 00432 WP 1997 3 27 ABXA9700122 1 19960823 A 5320 3916209502 FITTING DOUG DC9 DC931 3022065 WP BS 680 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND FITTING CRACKED AT STATION 680. REPLACED FITTING IAW DC-9 SRM 51- 30-2, 51-30-5. 2 L 7 2 4F A6WE 1997032700433 19970327 00433 WP 1997 3 27 ABXA9700123 1 19960808 A 5320 3916208501 FITTING DOUG DC9 DC931 3022065 WP BS 680 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND FITTING CRACKED AT STATION 680. REPLACED FITTING IAW DC-9 SRM 51- 30-5. 2 L 7 2 4F A6WE 1997032700434 19970327 00434 WP 1997 3 27 ABXA9700124 1 19960830 A 5320 3916212502 FITTING DOUG DC9 DC931 3022065 WP BS 617 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND CRACKED FITTING AT STATION 617. REPLACED FITTING IAW DC-9 SRM 51- 10-4, 51-30-5, 51-30-1. 2 L 7 2 4F A6WE 1997032700435 19970327 00435 WP 1997 3 27 ABXA9700125 1 19960723 A 5320 991968914 ANGLE DOUG DC9 DC931 3022065 WP BS 658 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK AND COMPLIANCE AD 92-22-08, FOUND CRACKED ANGLE AT STATION 658. REPLACED ANGLE IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 1997032700436 19970327 00436 WP 1997 3 27 ABXA9700126 1 19960808 A 5320 5910148435 WEB DOUG DC9 DC931 3022065 WP BS 658 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERITCAL WEB CRACKED AT STATION 658. REPAIRED IAW DC-9 SRM 53-01 FIG 2 SHEET 3. 2 L 7 2 4F A6WE 1997032700437 19970327 00437 WP 1997 3 27 ABXA9700127 1 19960801 A 5311 991150391 FRAME DOUG DC9 DC931 3022065 WP BS 69 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND FRAME STATION 69 CRACKED. REPAIRED IAW SUPPLEMENTAL SRM DRAWING N R K05159. 2 L 7 2 4F A6WE 1997032700438 19970327 00438 WP 1997 3 27 ABXA9700128 1 19960730 A 5240 5921550501 PAN DOUG DC9 DC931 3022065 WP SERVICE DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08 FOUND SERVICE DOOR PAN CRACKED ABOVE UPPER HINGE. FOUND PAN TO BE PREVIO USLY REPAIRED. 2 L 7 2 4F A6WE 1997032700439 19970327 00439 WP 1997 3 27 ABXA9700129 1 19960812 A 5320 995772615 ANGLE DOUG DC9 DC931 3022065 WP BS 669 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND ANGLE CRACKED AT STATION 699. REPLACED IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 1997032700440 19970327 00440 WP 1997 3 27 ABXA9700130 1 19960821 A 5712 4917790502 RIB CLIP DOUG DC9 DC931 3022065 WP WS 20 GOUGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND LOWER CLIP GOUGED AT BULKHEAD 20 RIGHT BETWEEN STRINGERS 14 TO 15. BLENDED GOUGED IAW DC-9 SRM 57-03, 51-10-3B. 2 L 7 2 4F A6WE 1997032700441 19970327 00441 WP 1997 3 27 ABXA9700131 1 19960816 A 5330 59197073 SKIN DOUG DC9 DC931 3022065 WP BS 861 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK, CORROSION WAS FOUND BETWEEN ALC DOOR JAMB DOUBLER AND SKIN. REPAIRED IAW ABX REA D953-15860-MR. 2 L 7 2 4F A6WE 1997032700442 19970327 00442 WP 1997 3 27 ABXA9700132 1 19960816 A 5330 591142485 SKIN DOUG DC9 DC931 3022065 WP BS 897-937 DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK, FOUND TWO REPAIRS ON SKIN AROUND ALC DOOR CUTOUT. REPAIRED IAW ABX REA D953-15910-MR. 2 L 7 2 4F A6WE 1997032700443 19970327 00443 WP 1997 3 27 ABXA9700133 1 19960816 A 5330 591142485 SKIN DOUG DC9 DC931 3022065 WP BS 945 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK, FOUND FUSELAGE SKIN CORRODED AT STATION 945. REPAIRED IAW ABX REA D953-15870-MR. 2 L 7 2 4F A6WE 1997032700444 19970327 00444 WP 1997 3 27 ABXA9700134 1 19960814 A 5330 5911412185 SKIN DOUG DC9 DC931 3022065 WP BS 383 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK, FOUND SKIN CORRODED AT STATION 383, WHEN A PREVIOUS REPAIR WAS REMOVED. REPAIRED IAW ABX REA D953-15936 -MR. 2 L 7 2 4F A6WE 1997032700445 19970327 00445 WP 1997 3 27 ABXA9700135 1 19960819 A 5712 99193469 RIB TEE CAP DOUG DC9 DC931 3022065 WP WS 20 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK, FOUND CORROSION ON RIGHT WING RIB UPPER CAP. REPAIRED IAW ABX REA D95-15855-MR. 2 L 7 2 4F A6WE 1997032700446 19970327 00446 WP 1997 3 27 ABXA9700136 1 19960809 A 5312 991150985 BULKHEAD TEE DOUG DC9 DC931 3022065 WP BS 110 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK, FOUND STATION 110 BULKHEAD T-CAP CORRODED BETWEEN L26R TO L27R. REPAIRED IAW ABX REA D953-15846-MR. 2 L 7 2 4F A6WE 1997032700447 19970327 00447 WP 1997 3 27 ABXA9700137 1 19960731 A 5311 9919617502 FRAME DOUG DC9 DC931 3022065 WP BS 699 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK AND COMPLIANCE WITH AD 78-07-05, FOUND FUSELAGE MAIN FRAME AT STATION 699R CRACKED. REPAIRED IAW ABX REA D953-15805-MR. 2 L 7 2 4F A6WE 1997032700448 19970327 00448 WP 1997 3 27 ABXA9700138 1 19960802 A 5311 9919617501 FRAME DOUG DC9 DC931 3022065 WP BS 718 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK AND COMPLIANCE WITH AD 78-07-05, FOUND FUSELAGE MAIN FRAME AT STATION 718L CRACKED. REPAIRED IAW ABX REA D953-15805-MR. 2 L 7 2 4F A6WE 1997032700449 19970327 00449 WP 1997 3 27 ABXA9700139 1 19960805 A 5311 9919619503 FRAME DOUG DC9 DC931 3022065 WP BS 737 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK AND COMPLIANCE WITH AD 78-07-05, FOUND FUSELAGE MAIN FRAME AT STATION 737L CRACKED. REPAIRED IAW ABX RE A D953-15805-MR. 2 L 7 2 4F A6WE 1997032700450 19970327 00450 WP 1997 3 27 ABXA9700140 1 19960724 A 5311 99196182 FRAME DOUG DC9 DC931 3022065 WP BS 718 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK AND COMPLIANCE WITH AD 78-07-05, FOUND FUSELAGE MAIN FRAME AT STATION 718R CRACKED. REPAIRED IAW ABX REA D953-15805-MR. 2 L 7 2 4F A6WE 1997032700451 19970327 00451 WP 1997 3 27 ABXA9700141 1 19960731 A 5311 9919619504 FRAME DOUG DC9 DC931 3022065 WP BS 737 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK AND COMPLIANCE WITH AD 78-07-05, FOUND FUSELAGE MAIN FRAME AT STATION 737R CRACKED. REPAIRED IAW ABX REA D953-15805-MR. 2 L 7 2 4F A6WE 1997032700452 19970327 00452 WP 1997 3 27 ABXA9700142 1 19960905 A 3231 3923161503 CONTROL ARM DOUG DC9 DC931 3022065 WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, WHILE ACCOMPLISHING AD 91-22-07, THE LEFT MAIN LANDING GEAR OUTBOARD CONTROL LINKAGE WAS FOUND WORN. TH E CONTROL ARM WAS REPLACED IAW DC-9 M/M 32-12-1. 2 L 7 2 4F A6WE 1997032700535 19970327 00535 1997 3 27 97ZZZM324 4 19961210 A 3425 ADI WIRE BUNDLE BOEING 737 7372P6 NM E/E COMPT WATER CONTAM A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 DURING MX FOR F/O'S ADI INDICATOR MALFUNCTIONS, ELECTRONIC RACKS E-1 AND E-2 WERE REMOVED. THE REMOVAL OF THE RACKS WAS NESSITATED BY THE DISCOVERY OF 'BLUE WATER' INTRUSSION INTO THE WIRE BUNDLES FEEDING THE E-1 AND E-2 RACK CONNECTORS, W HILE THE LEAKAGE CAUSING THE INTRUSION HAD APPARENTLY BEEN RECTIFIED. THE RESIDUE HAD NOT BEEN COMPLETELY ELMINATED FRO M THE AREA. AS STATED ABOVE, THE E-1 AND E-2 RACKS WERE REMOVED FROM THE A/C AND THE WIRE BUNDLES WERE THOROUGHLY CLEAN ED AND TREATED. THE LOWER LOBE AREA WAS FULLY INSPECTED FOR FURTHER EVIDENCE OF FLUID DAMAGE. NONE NOTED. THE A/C WAS SUBSEQUENTLY RETURNED TO SERVICE WITH NO NEGATIVE FINDINGS. (M) 2 L 7 2 4F RT A16WE 1997032700536 19970327 00536 NM 1997 3 27 97ZZZM325 1 19961129 A 3411 PITOT LINE BOEING 737 7372P6 NM RIGHT LEAKING A ZZDA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 15 1PC 21613 FLT 822 - MCO-MCI - AIRCRAFT ABORTED TAKEOFF AS A RESULT OF A 20 KNOT DIFFERENTIAL REFERENCE BETWEEN CAPTAIN'S AND FIRST OFFICERS AIR SPEED INDICATORS. PERFORMED LEAK CHECK OF THE PITOT STATIC SYSTEM PER B737 MM 34-12-01. FOUND LEAK IN FI RST OFFICERS STATIC SOURCE. RE-TORQUED LINE CONNECTORS AND PERFORMED RE-CHECK OF SYSTEM. NO FURTHER LEAKAGE NOTED. RI I ACCOMPLISHED AS REQUIRED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1997032700573 19970327 00573 WP 1997 3 27 USAA970081 1 19960307 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 980 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 959VJ 59980 47352 PIT - DURING A-4 CHECK, FOUND .3125 INCH CRACK IN BELTFRAME AT STATION 980, LONGERON 14R. SPLICED IN NEW SECTION OF BEL TFRAME AT STATION 980 BETWEEN LONGERONS 10R AND 18R PER SRM 53-03 FIG 32.. (M) 2 L 7 2 4F A6WE 1997032700574 19970327 00574 WP 1997 3 27 USAA970082 1 19960307 A 5320 ANGLE DOUG DC9 DC931 3022065 WP BS 996 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 959VJ 59980 47352 PIT - DURING A-4 CHECK, FOUND 3.5 INCH CRACK AT STATION 996 LONGERON 16L LOWER PYLON DRAG ANGLE. INSTALLED NEW SECTION OF DRAG ANGLE 31 INCH BY 3.5 INCH PER SRM 54-04 FIG 10. (M) 2 L 7 2 4F A6WE 1997032700575 19970327 00575 WP 1997 3 27 USAA970079 1 19960307 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 1076 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 959VJ 59980 47352 PIT - DURING A-4 CHECK, FOUND .75 INCH CRACK AT AFT END OF LONGERON 2L, STATION 1076. REPLACED SECTION OF LONGERON PER SRM 53-02 FIG 8. (M) 2 L 7 2 4F A6WE 1997032700708 19970327 00708 EU 1997 3 27 97ZZZM374 1 19961011 A 5320 RIVETS BAG BAE146 BAE146200A 1500266 EU DOOR SILL CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 RIGHT FORWARD SILL PLATE AFT INBOARD ATTACHMENT HOLES HAVE CORRODED RIVETS THAT NEED TO BE REPLACED. REPLACED RIVETS. ( M) 2 H 7 4 4F RT A49EU 1997032700709 19970327 00709 EU 1997 3 27 97ZZZM375 1 19961014 A 5311 FRAME BAG BAE146 BAE146200A 1500266 EU E/E COMPT CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 LIGHT SURFACE CORROSION ON FRAME 15 FLOOR SUPPORT BEAM BY LEFT AFT CORNER OF AVIONICS BAY ACCESS OPENING. REMOVED MINOR SURFACE CORROSION, CLEANED, TREATED AND REPAINTED. (M) 2 H 7 4 4F RT A49EU 1997032700710 19970327 00710 EU 1997 3 27 97ZZZM376 1 19961014 A 5753 BOLT BAG BAE146 BAE146200A 1500266 EU NR 2 TE FLAP DAMAGED A A6WA K NONE C F.O.D. IN INSP/MAINT 1 GL 31 606AW E2033 RIGHT NR 2 FLAP TRACK FLAP TO CARRIAGE, BOLT APPEARS TO HAVE RECEIVED A LIGHTENING STRIKE,DUE TO PITS NEAR THREADED AREA . INSTALLED NEW BOLT IN NR 2, RIGHT FLAP TO CARRIAGE HOUSING. (M) 2 H 7 4 4F RT A49EU 1997032700711 19970327 00711 EU 1997 3 27 97ZZZM377 1 19961022 A 5320 HI-LOK BAG BAE146 BAE146200A 1500266 EU FUSELAGE SHEARED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 SIGHTING ATTACHMENT ON (BELLY) LONGERON FITTING OF FRAME NR 29 HAS HI-LOK SHEARED. REPLACED BROKEN HI-LOK IAW BAE 146MM (SAME PART AS ORIGINAL). (M) 2 H 7 4 4F RT A49EU 1997032700712 19970327 00712 EU 1997 3 27 97ZZZM378 1 19961021 A 5210 RAIL BAG BAE146 BAE146200A 1500266 EU REAR AIRSTAIR CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 REAR AIRSTAIR, INBOARD RAIL CORRODED NEEDS TO BE REPLACED. REMOVED AND REPLACED AFT INBOARD AIRSTAIR RAIL. (M) 2 H 7 4 4F RT A49EU 1997032700713 19970327 00713 EU 1997 3 27 97ZZZM379 1 19961018 A 2710 CABLES BAG BAE146 BAE146200A 1500266 EU RIGHT AILERON RUSTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 RIGHT AILERON CONTROL CABLES ARE RUSTED AT WING ROOT CABLE PULLEYS. INSTALLED RIGHT AILERON CONTROL CABLES IAW AMM W/C GENERATED FOR REQUIRED CHECKS AND SAFTIES. 2 H 7 4 4F RT A49EU 1997032700714 19970327 00714 EU 1997 3 27 97ZZZM380 1 19961017 A 5755 BOLT BAG BAE146 BAE146200A 1500266 EU CTR SPOILER FAILED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 FORWARD BOLT OF JACK ON MIDDLE LIFT SPOILER FAIL NDT LEFT WING. REMOVED AND REPLACED FORWARD BOLT OF JACK ON MIDDLE LIF T SPOILER LEFT WING. (M) 2 H 7 4 4F RT A49EU 1997032700715 19970327 00715 EU 1997 3 27 97ZZZM381 1 19961018 A 5210 ANGLE BAG BAE146 BAE146200A 1500266 EU PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 FORWARD PASSENGER DOOR HAS TWO CRACKED ANGLE BRACKETS AT THE BOTTOM OF BOX STRUCTURE FOR DOOR MECHANISM. REPLACED CRACK ED AREAS PER SRM. ANGLES MADE PER SRM. REMOVED STRUCTURE INSPECTED AND NO OTHER DAMAGE NOTED. 2 H 7 4 4F RT A49EU 1997032700716 19970327 00716 EU 1997 3 27 97ZZZM382 1 19961015 A 2510 BOLT BAG BAE146 BAE146200A 1500266 EU COCKPIT BAD A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 RIGHT FORWARD RESTRAINT LINK BOLT FOUND TO BE BAD ON MAG PART INSPECTION. DRILLED NEW BOLT FOR COTTER PIN AND INSTALLED IN RIGHT FORWARD RESTRAINT LINK. (M) 2 H 7 4 4F RT A49EU 1997032700717 19970327 00717 EU 1997 3 27 97ZZZM383 1 19961015 A 5210 STEP BAG BAE146 BAE146200A 1500266 EU FWD AIRSTAIR CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 FORWARD AIR STAIR ASSEMBLY NR 2 STEP CORRODED. REPLACED STEP ASSEMBLY. 2 H 7 4 4F RT A49EU 1997032700718 19970327 00718 EU 1997 3 27 97ZZZM384 1 19961029 A 5753 FLAP TRACKS BAG BAE146 BAE146200A 1500266 EU LT TE FLAPS WORN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 LEFT WING NR 2 FLAPTRACK WEARMARKS LOWER RAIL OUTBOARD EDGE FRM SLIP P/PLATE. WEARMARKS 94) BOTH SIDES TOP OF LOWER RAI L FROM ROLLERS AND 1, UPPER RAIL OUTBOARD EDGE FROM SIDE ROLL. COMPLIED WITH BLENDING OF WEARMARKS ON UPPER OUTBOARD RA IL AND BOTH SIDES ON TOP OF LOWER RAIL IAW SRM 57-20-41. BLENDED LOWER RAIL EDGES AND SHIMMED THE RUB PADS OF THE LOWER CARRIAGE PER FAX DJR/1200-96. 2 H 7 4 4F RT A49EU 1997032700719 19970327 00719 EU 1997 3 27 97ZZZM385 1 19961029 A 2710 CABLES BAG BAE146 BAE146200A 1500266 EU LT/RT AILERONS CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 LEFT AND RIGHT AILERON INTERCONNECT CABLES COVER SLEEVES ARE WORN IN TWO AT CABLE GUIDES. REMOVED AND REPLACED LEFT AND RIGHT AILERON INTERCONNECT CABLES IAW AMM W/C GENERATED FOR FUNCTIONAL CHECKS. REF W/C 2365. (M) 2 H 7 4 4F RT A49EU 1997032700720 19970327 00720 EU 1997 3 27 97ZZZM386 1 19961029 A 2710 CABLES BAG BAE146 BAE146200A 1500266 EU AILERONS CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 PERFORMED AILERON INTERCONNECT CABLE CHECK. FOUND AILERON INTERCONNECT CABLES CORRODED AT WING ROOT PULLEYS. REMOVED A ND REPLACED IAW AMM GENERATED W/C FOR FUNCTIONAL CHECK. 2 H 7 4 4F RT A49EU 1997032700721 19970327 00721 EU 1997 3 27 97ZZZM387 1 19961011 A 7120 BOLT BAG BAE146 BAE146200A 1500266 EU NR 4 ENGINE CRACKED A A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 NR 4 ENGINE YOKE TO PYLON, DURING UT INSPECTION OF TOP LEFT BOLT P/N HC712H0041-000 CRACK INDICATION. REMOVED BOLT FOR MT, VERIFICATION REQUIRED. REMOVED BOLT, BOLT FAILED MAGNETIC PARTICLE INSPECTION. REPLACED AND INSTALLED IAW BAE 146 MM. 2 H 7 4 4F RT A49EU 1997032700723 19970327 00723 EU 1997 3 27 97ZZZM389 1 19961008 A 5320 SILL BAG BAE146 BAE146200A 1500266 EU PAX DOOR CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 LEFT REAR PASS DOOR SILL PLATE CORRODED THROUGH. REMOVED OLD SILL PLATE AND INSTALLED NEW SILL PLATE FROM STOCK, FORWAR D HALF ONLY. REINSTALLED FORWARD GIRT BAR BRACKET. (M) 2 H 7 4 4F RT A49EU 1997032700724 19970327 00724 EU 1997 3 27 97ZZZM390 1 19961009 A 5312 BULKHEAD RIVETS BAG BAE146 BAE146200A 1500266 EU REAR PRESS DOME MIS INSTALLED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 FORWARD SIDE OF REAR PRESSURE DOME , 2 RIVETS NEED SHIMS AT HORIZONTAL STIFFENERS TO CENTER RING AS MARKED. DRILLED OUT 2 RIVETS MADE SHIM FROM SHEET METAL, INSTALLED SHIM AND 2 RIVETS. (M) 2 H 7 4 4F RT A49EU 1997032700725 19970327 00725 EU 1997 3 27 97ZZZM391 1 19961010 A 5753 BOLT BAG BAE146 BAE146200A 1500266 EU NR 3 TE FLAP OUT OF POSITION A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 LEFT WING NR 3 FLAP TRACK CARRIAGE TO FLAP BOLT, MAGNEFLUXED OK, BUT INNER BOLT HAS SLID OUT OF POSITION AND FIRST THREA DS NEED DRESSED-OUT. RESEALED AND RESE CURED INNER FAIL/SAFE BOLT. DRESSED-OUT OUT THREADS AS REQUIRED. 2 H 7 4 4F RT A49EU 1997032700726 19970327 00726 EU 1997 3 27 97ZZZM392 1 19961015 A 5755 BOLT BAG BAE146 BAE146200A 1500266 EU RT SPOILER CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 RIGHT WING OUTBOARD LIFT SPOILER MIDDLE HINGE BOLT HAS CORROSION AND CRACK INDICATION. REMOVED AND REPLACED BOLT, RIGHT WING OUTBOARD LIFT SPOILER MIDDLE HINGE. (M) 2 H 7 4 4F RT A49EU 1997032700727 19970327 00727 EU 1997 3 27 97ZZZM393 1 19961201 A 3297 WIRE HARNESS BAG BAE146 BAE146200A 1500266 EU LT MLG FAILED A A6WA O OTHER N FALSE WARNING CL CLIMB 1 GL 31 179US E2041 AFTER GEAR RETRACTION, LEFT MAINTENANCE GEAR INTRANSIT LIGHT REMAINED ILLUMINATED. CYCLED GEAR DOWN AND UP, LIGHT STILL ILLUMINATED. NO UNUSUAL YAW FELT OR UNUSUAL NOISE TO INDICATE GEAR NOT UP AND LOCKED. FOUND LEFT GEAR UPLOCK SWITCH H ARNESS INOP. REMOVED AND REPLACED HARNESS PER BAE, OPS CHECKS GOOD. (M) 2 H 7 4 4F RT A49EU 1997032700728 19970327 00728 NE 1997 3 27 97ZZZM394 2 19961130 A 7310 MANIFOLD BAG BAE146 BAE146300A 1500267 EU LYC ALF502 ALF502R5 41580 NE NR 3 ENGINE DEFECTIVE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 NR 3 ENGINE OUTBOARD FUEL MANIFOLD SHOWED DEFECTS DURING THE ET CHECK WITH SLIGHT SOOTING INSIDE THE COWL. REPLACED MAN IFOLD ASSEMBLY. (M) 2 H 7 4 4F 4 F RT A49EU E6NE 1997032700729 19970327 00729 EU 1997 3 27 97ZZZM395 1 19961121 A 3230 RELAY BAG BAE146 BAE146200A 1500266 EU LANDING GEAR FAILED A A6WA O OTHER J WARNING INDICATION CL CLIMB 1 GL 31 606AW E2033 UNABLE TO RAISE GEAR UNLESS OVERRIDE IS SELECTED. GEAR SELECTED DOWN NORMAL EXTENSION. REMOVED AND REPLACED RELAY GF4 SYSTEM CHECKS GOOD. (M) 2 H 7 4 4F RT A49EU 1997032700730 19970327 00730 EU 1997 3 27 97ZZZM396 1 19961110 A 5320 ANGLE BAG BAE146 BAE146200A 1500266 EU CABIN CRACKED A A6WA K NONE L NO TEST IN INSP/MAINT 1 GL 31 606AW E2033 MACHINED ANGLE ATTACHED TO SEAT RAIL 5 INCHES AFT OF FRAME 28 TO 6 INCHES AFT OF FRAME 29 LEFT OUTBOARD CRACKED. REPLAC ED ANGLE, REF FAX FOR HI-LOKS IN LIEU OF SP157 FAX NR DJR/RJ1282-96. (M) 2 H 7 4 4F RT A49EU 1997032700731 19970327 00731 1997 3 27 97ZZZM397 4 19961223 A 2565 D31050103 SLIDE BAG BAE146 BAE146200A 1500266 EU CABIN LIGHT FAILED A A6WA K NONE L NO TEST IN INSP/MAINT 1 GL 31 156TR E2156 NR 1 EVAC SLIDE LIGHTS BURNED OUT, SLIDE P/N D31050-103 S/N 0832. REMOVED AND REPLACED SLIDE ASSEMBLY. (M) 2 H 7 4 4F RT A49EU 1997032700733 19970327 00733 EU 1997 3 27 97ZZZM399 1 19961229 A 2751 CONNECTORS BAG BAE146 BAE146100A 1500260 EU TE FLAPS DIRTY A A6WA O OTHER N FALSE WARNING AP APPROACH 1 GL 31 246SS E1003 ON APPROACH TO ASE, UPON SELECTING FLAPS 24, BOTH FLAP INOP AND FLAP FAULT LIGH TS ILLUMINATED. FLAPS LOCKED AT 18 DEGR EES. RETURNED TO DEN. CLEANED ALL RESOLVER CANNON PLUGS AND OPERATED FLAPS NUMEROUS TIMES. NO MORE FAULTS NOTED. 2 H 7 4 4F RT A49EU 1997032700734 19970327 00734 1997 3 27 97ZZZM400 4 19961220 A 3431 NAV SYSTEM BAG BAE146 BAE146100A 1500260 EU NR 1 MALFUNCTIONED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 NR 1 NAV AND TACAN INOP, NR 2 OK. RE-RACKED NR 1 LEDEX RELAY, COMPLIED WITH 4OIL RAMP TEST OF NR 1 NAV SYSTEM. NO DEFE CTS NOTED. COMPLIED WITH SELF TEST OF NR 1 TACAN SYSTEM. NO DEFECTS NOTED. (M) 2 H 7 4 4F RT A49EU 1997032700735 19970327 00735 EU 1997 3 27 97ZZZM401 1 19961206 A 5753 FAIRING BAG BAE146 BAE146300A 1500267 EU LT TE FLAP CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 614AW E3132 LEFT INBOARD FLAP TRACK AFT FAIRING HAS DAMAGE ON THE INBOARD SIDE. REMOVED AND REPLACED LEFT INBOARD FLAP TRACK AFT FA IRING. (M) 2 H 7 4 4F RT A49EU 1997032700736 19970327 00736 EU 1997 3 27 97ZZZM402 1 19961205 A 5320 DOUBLER BAG BAE146 BAE146200A 1500266 EU BS 47.2 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 609AW E2070 RIGHT STIFFENER (STATION 47.20) AT FRAME 29 IN HYDRAULIC BAY HAS CRACKED DOUBLER PLATE AT BOTTOM END OF STIFFENER. REPL ACED RIGHT STIFFENER (STATION 47.20) AT FRAME 29 IAW BAE DRAWING NR HC536H0090 AND AIR FAX NR DS/W/TS/25913/96. 2 H 7 4 4F RT A49EU 1997032700737 19970327 00737 EU 1997 3 27 97ZZZM403 1 19961203 A 2710 TRIM CHAIN BAG BAE146 BAE146200A 1500266 EU LT AILERON CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 609AW E2070 LEFT AILERON TRIM SCREWJACK CHAIN APPEARS TO BE CORRODED. LEFT TRIM CABLE TURNBUCKLES LOOSE. REMOVED AND REPLACED LEFT AILERON TRIM CHAIN IAW 27-12-17. A DJUSTED CABLES AND COMPLIED WITH FUNCTION TEST IAW 27-12-00. CHECKS OK. (M) 2 H 7 4 4F RT A49EU 1997032700738 19970327 00738 EU 1997 3 27 97ZZZM404 1 19961202 A 5315 FLOORBEAM BAG BAE146 BAE146200A 1500266 EU CABIN CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 609AW E2070 THREE FLOORBEAMS ARE CRACKED AT FRAME 29 BEAM 3, 13 AND 19. REPAIRED CRACKS IAW BAE DRAWING HC536H9211 AND FAX AIRAMS/T /BAE/25858/96. 2 H 7 4 4F RT A49EU 1997032700739 19970327 00739 1997 3 27 97ZZZM405 4 19961130 A 2565 D31050103 SLIDE BAG BAE146 BAE146300A 1500267 EU PAX DOOR BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 LEFT FORWARD PAX DOOR EVAC SLIDE BACKBOARD IS BROKEN. REPLACED THE SLIDE. 2 H 7 4 4F RT A49EU 1997032700748 19970327 00748 NM 1997 3 27 97ZZZX1214 1 19961107 A 3350 3315235 BATTERY BOEING 727 7272B7 138407L NM CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 760AT 21954 KMCO - DURING PRE-FLIGHT, FOUND AFT EMERGENCY LIGHT OVER AFT ENTRY DOOR INOPERABLE. REPLACED BATTERIES FOR AFT EMERGENC IES, OPS CHECKED IAW MM 33-50-101. 2 L 7 3 4F A3WE 1997032700749 19970327 00749 NM 1997 3 27 97ZZZX1215 1 19961104 A 3350 3315235 BATTERY BOEING 727 727247 138408F NM CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 784AT 21393 KIND - DURING PRE-FLIGHT, FOUND 2L EMERGENCY EXIT LIGHT INOPERATIVE. INSTALLED SERVICEABLE BATTERY, CHECKS GOOD. 2 L 7 3 4F A3WE 1997032700750 19970327 00750 NM 1997 3 27 97ZZZX1216 1 19961207 A 3350 2410070 CHARGER BOEING 727 727247 138408F NM CABIN INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 784AT 21393 KIND - DURING PRE-FLIGHT, FOUND CEILING EGRESS LIGHT OVERHEAD FOR OVERWING EXITS IS INOPERABLE. REMOVED AND REPLACED CH ARGER (M1094) LIGHTS, OPS CHECK NORMAL. 2 L 7 3 4F A3WE 1997032700790 19970327 00790 WP 1997 3 27 ABXA9700143 1 19960822 A 5280 29242891 HINGE DOUG DC9 DC931 3022065 WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 57550 DURING C-CHECK , WHILE ACCOMPLISHING AD 91-22-07, THE LEFT MAIN LANDING GEAR OUTBOARD DOOR HINGE WAS FOUND WORN. THE HI NGE WAS REPLACED IAW DC-9 ONM 32-10-6. 2 L 7 2 4F A6WE 1997032700791 19970327 00791 WP 1997 3 27 ABXA9700144 1 19960904 A 5320 WEB DOUG DC9 DC931 3022065 WP BS 256-275 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, WHILE ACCOMPLISHING AD 91-22-07, THE LEFT MAIN CUSP WEB WAS FOUND CRACKED BETWEEN STATIONS 256 AND 275. THE CUSP WAS REPAIRED IAW REA D953-16190-MR. 2 L 7 2 4F A6WE 1997032700792 19970327 00792 WP 1997 3 27 ABXA9700145 1 19960826 A 5320 99101555 PRESSURE WEB DOUG DC9 DC931 3022065 WP LT MLG WW CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, THE LEFT WHEEL WELL PRESSURE PANEL WAS FOUND CORRODED AT STATION 718. THE PRESSUERE PANEL WAS REPAIRED IAW REA D953-16133-MR. 2 L 7 2 4F A6WE 1997032700793 19970327 00793 WP 1997 3 27 ABXA9700146 1 19960903 A 5330 591970713 SKIN DOUG DC9 DC931 3022065 WP BS 996 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, THE FUSELAGE SKIN WAS FOUND CORRODED BETWEEN LONGERONS 28 LT AND 28RT STATION 996. THE SKIN WAS REPAIRE D IAW REA D953-16200-MR. 2 L 7 2 4F A6WE 1997032700794 19970327 00794 WP 1997 3 27 ABXA9700147 1 19960905 A 5320 591746311 JAMB DOUG DC9 DC931 3022065 WP VENTRAL DOOR CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, THE LOWER SECTION OF THE VENTRAL DOOR JAMB WAS FOUIND CORRODED AND BOTH LOWER CORNERS WERE FOUND CRACKED . THE JAMB WAS REPAIRED IAW REA D953-16134-MR. 2 L 7 2 4F A6WE 1997032700795 19970327 00795 WP 1997 3 27 ABXA9700148 1 19960829 A 5711 5911300501 SPAR CAP DOUG DC9 DC931 3022065 WP LT/RT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, THE LEFT AND RIGHT WINGS REAR SPAR UPPER CAPS AT STATION XRS267 WERE FOUND CORRODED AT THE FLAP HINGE FI TTING HOLES. THE SPAR CAPS WERE REPAIRED IAW REA D957-16147-MR. 2 L 7 2 4F A6WE 1997032700796 19970327 00796 WP 1997 3 27 ABXA9700149 1 19960923 A 5230 5912494501 PAN DOUG DC9 DC941 302207N WP BS 380 GOUGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 990 47493 WHILE COMPLYING WITH C INSPECTION, FOUND THE FORWARD LOWER CARGO COMPARTMENT DOOR JAMB GOUGED AT FS 380. REPAIRED DOOR JAMB IAW REA D95516447-MR. 2 L 7 2 4F A6WE 1997032700797 19970327 00797 WP 1997 3 27 ABXA9700150 1 19960823 A 5280 5910557110 DOOR DOUG DC9 DC941 302207N WP RT MLG DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 990AX 47493 WHILE COMPLYING WITH C INSPECTION, FOUND THE RIGHT MAIN LANDING GEAR WING MOUNTED DOOR DISBONDED AROUND THE CRANK ARM AT TACH FITTING. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR DOOR IAW DC-9 MAINTENANCE MANUAL CHAPTER 32-12-1. 2 L 7 2 4F A6WE 1997032700798 19970327 00798 WP 1997 3 27 ABXA9700151 1 19960925 A 5753 59134505 TRACK DOUG DC9 DC941 302207N WP LT TE FLAP CHAFED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 990AX 47493 WHILE COMPLYING WITH C INSPECTION, FOUND THE LEFT FLAP TRACK AND BUS CABLE CHAFED THROUGH, APPROXIMATELY 2 FEET FROM CAB LE BALL END. REMOVED AND REPLACED LEFT HAND FLAP TRACK, CARRIAGE AND BUS CABLE IAW DC-9 MAINTENANCE MANUALS CHAPTERS 27 -50-0 AND 27-50-1. 2 L 7 2 4F A6WE 1997032700799 19970327 00799 WP 1997 3 27 ABXA9700152 1 19960920 A 5753 5910070518 VANE DOUG DC9 DC941 302207N WP RT TE FLAP DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 990AX 47493 WHILE COMPLYING WITH A C INSPECTION, FOUND THE RIGHT FLAP AFT MOVEABLE VANE DELAMINATED. REMOVED AND REPLACED AFT MOVEA BLE VANE IAW DC-9 MAINTENANCE MANUAL CHAPTER 27-51-02 2 L 7 2 4F A6WE 1997032700800 19970327 00800 WP 1997 3 27 ABXA9700153 1 19961203 A 5530 5912175502 FAIRING DOUG DC9 DC933F 302207A WP VERTICAL STAB DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 WHILE COMPLYING WITH A C INSPECTON, FOUND THE RIGHT UPPER HORIZONTAL TO VERTICAL STABLIZER FAIRING DELAMINATED. REPLACE D THE RIGHT UPPER HORIZONTAL TO VERTICAL STABLIZER FAIRING IAW ABX JOB CARD NR 40232. 2 L 7 2 4F A6WE 1997032700801 19970327 00801 WP 1997 3 27 ABXA9700154 1 19961203 A 5347 S2955978 TRACK DOUG DC9 DC933F 302207A WP BS 897-965 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 WHILE COMPLYING WITH A C INSPECTION, FOUND THE LEFT CARGO TIE DOWN TRACK IN THE AFT LOWER CARGO COMPARTMENT HAS EXFOLIAT ED CORROSION FROM FS 897 TO FS 965. REPLACED LEFT TRACK SECTION IAW DC-9 SRM CHAPTER 51-30-1. 2 L 7 2 4F A6WE 1997032700802 19970327 00802 WP 1997 3 27 ABXA9700155 1 19961206 A 5320 5912494501 PAN DOUG DC9 DC933F 302207A WP BS 370- 427 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 WHILE COMPLYING WITH A C INSPECTION, FOUND THE FORWARD LOWER CARGO COMPARTMENT DOOR JAMB CORRODED AND BULGED BETWEEN FS 370 AND 427. REPAIRED DOOR JAMB IAW DC-9 SRM CHAPTER 53-05 FIG 44 SHEET 2. 2 L 7 2 4F A6WE 1997032700803 19970327 00803 WP 1997 3 27 ABXA9700156 1 19961210 A 5347 99578551 TRACK DOUG DC9 DC933F 302207A WP BS 120 WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 WHILE COMPLYING WITH A C INSPECTION, FOUND THE CAPTAINS FOWARD SEAT TRACK WORN. REPLACED CAPTAINS FOWARD SEAT TRACKS IA W DC-9 SRM CHAPTER 51-30-1 AND MAINTENANCE MANUAL CHAPTER 25-13-1. 2 L 7 2 4F A6WE 1997032700804 19970327 00804 WP 1997 3 27 ABXA9700157 1 19961207 A 5320 5912492 PAN DOUG DC9 DC933F 302207A WP BS 200 DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 WHILE COMPLYING WITH A C INSPECTION, FOUND THE FORWARD SERVICE DOOR JAMB DAMAGED AT BAYONET ROLLERS. REPAIRED DOOR JAMB IAW DC-9 SRM CHAPTER 53-05 FIGURE 42. 2 L 7 2 4F A6WE 1997032700805 19970327 00805 WP 1997 3 27 ABXA9700158 1 19961207 A 5530 5912175501 FAIRING DOUG DC9 DC933F 302207A WP VERTICAL STAB DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 WHILE COMPLYING WITH A C INSPECTION, FOUND THE LEFT UPPER HORIZONTAL TO VERTICAL STABILIZER FAIRING DELAMINATED. REPLAC ED LEFT HAND UPPER HORIZONTAL TO VERTICAL STABILIZER FAIRING IAW ABD JOB CARD NR 40232. 2 L 7 2 4F A6WE 1997032700806 19970327 00806 WP 1997 3 27 ABXA9700159 1 19961205 A 5521 99115125 RIB DOUG DC9 DC933F 302207A WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 WHILE COMPLYING WITH A C INSPECTION, FOUND THE ANGLED RIB IN THE VERTICAL STABILIZER REMOVEABLE LEADING EDGE SECTION CRA CKED IN TWO PLACES. REPAIRED CRACKED RIB IAW SUP SRM DRAWING K05159. 2 L 7 2 4F A6WE 1997032700807 19970327 00807 WP 1997 3 27 ABXA9700160 1 19961205 A 5531 NAS12038 SCREW DOUG DC9 DC933F 302207A WP VERTICAL STAB RUSTED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 WHILE COMPLYING WITH A C INSPECTION, FOUND THE VERTICAL STABILIZER CENTER ATTACH FITTINGS HAVE HEAVY RUST ON EIGHT EACH FASTENERS, AT FUSELAGE FRAME AT STATION 1104. REPLACED RUSTED FASTENERS IAW DC-9 SRM CHAPTER 51-30-1. 2 L 7 2 4F A6WE 1997032700808 19970327 00808 WP 1997 3 27 ABXA9700161 1 19961210 A 5720 5919572501 BUTE DOOR DOUG DC9 DC933F 302207A WP WS 240 DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 WHILE COMPLYING WITH A C INSPECTON, FOUND THE LEFT WING BUTE DOOR NR 1502A DELAMINATED. REPLACED LEFT WING BUTE DOOR NR 1502A IAW DC-9 MAINTENANCE MANUAL CHAPTER 57-20-3. 2 L 7 2 4F A6WE 1997032700809 19970327 00809 WP 1997 3 27 ABXA9700162 1 19961210 A 7110 808009 FAN CASE DOUG DC9 DC933F 302207A WP PWA JT8 JT8D9A 52048 NE NR 1 ENGINE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 665693 WHILE COMPLYING WITH A C-INSPECTION, FOUND THE NR 1 ENGINE FORWARD FAN CASE MISSING MATERIAL AT THE 3, 5 AND 6 O'CLOCK P OSITIONS. REPLACED THE NR 1 ENGINE FAN CASE IAW ABX JOB CARD BS 846A AND BS 8235 AND THE DC-9 MAINTENANCE MANUAL CHAPTE RS 71-10-01 AND 71-10-02. 2 L 7 2 4F 4 F A6WE E2EA 1997032700811 19970327 00811 WP 1997 3 27 ABXA9700164 1 19961206 A 5730 59127372 PANEL DOUG DC9 DC933F 302207A WP WS 383-445 DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 WHILE COMPLYING WITH A C INSPECTION, FOUND THE RIGHT WING TRAILING EDGE PANEL JUST OUTBOARD OF THE SPOILER DELAMINATED. REPLACED BONDED PANEL IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 1997032700812 19970327 00812 WP 1997 3 27 ABXA9700165 1 19961203 A 5720 5919571502 BUTE DOOR DOUG DC9 DC933F 302207A WP WS 137 DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 WHILE COMPLYING WITH A C INSPECTION, FOUND THE RIGHT WING BUTE DOOR NR 1601A DELAMINATED . REPLACED RIGHT WING BUTE DOO R NR 1601 IAW DC-9 MAINTENANCE MANUAL CHAPTER 57-20-3. 2 L 7 2 4F A6WE 1997032700813 19970327 00813 WP 1997 3 27 ABXA9700166 1 19961205 A 5313 5911408153 LONGERON DOUG DC9 DC933F 302207A WP BS 446 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 WHILE COMPLYING WITH A C INSPECTION, FOUND LONGERON 4 LEFT CRACKED AT FS 446. REPAIRED LONGERON 4 LEFT IAW ABX REA D953 -17397-MR. 2 L 7 2 4F A6WE 1997032700814 19970327 00814 WP 1997 3 27 ABXA9700167 1 19961206 A 5330 5911401165 SKIN DOUG DC9 DC933F 302207A WP BS 160 DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 WHILE COMPLYING WITH A C INSPECTION, FOUND THAT AIRCRAFT HAS AN INTERIM REPAIR INSTALLED AT FS 160, BELOW MAIN ENTRY THA T REQUIRES CLASS I REPAIR INSTALLED PROIR TO 12-17-96. REPAIRED IAW ABX REA D953-17390-MR. 2 L 7 2 4F A6WE 1997032700815 19970327 00815 WP 1997 3 27 ABXA9700168 1 19961130 A 3231 S2210370P4109 BUSHING DOUG DC9 DC941 302207N WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 965AX 47498 DURING COMPLIANCE OF AD 91-22-07, ASB 32-244 R2, FOUND LEFT OUTBOARD MAIN LANDING GEAR DOOR ARTICULATING CRANK PIVOT POI NT WORN. REPLACED BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1997032700816 19970327 00816 WP 1997 3 27 ABXA9700169 1 19961130 A 3231 3923158501 LINK ASSY DOUG DC9 DC941 302207N WP RT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 965AX 47498 DURING COMPLIANCE OF AD 91-22-07; ASB 32-224 R2, FOUND LINK ASSEMBLY FOR RIGHT MAIN LANDING GEAR ARTICULATING DOOR WORN. REPLACED LINK ASSEMBLY IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1997032700817 19970327 00817 WP 1997 3 27 ABXA9700170 1 19961130 A 3231 AN960716L WASHER DOUG DC9 DC941 302207N WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 965AX 47498 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244 R2, FOUND LEFT OUTBOARD MAIN LANDING GEAR ARTICULATING CRANK PIVOT POINT WO RN. REPLACED WASHER IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1997032700818 19970327 00818 WP 1997 3 27 ABXA9700171 1 19961130 A 3231 NAS130425D BOLT DOUG DC9 DC941 302207N WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 965AX 47498 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244 R2, FOUND LEFT OUTBOARD MAIN LANDING GEAR ARTICULATING CRANK PIVOT POINT WO RN. REPLACED BOLT IAW DC-9 OVERHAUL MANUAL 32-10-06. 2 L 7 2 4F A6WE 1997032700819 19970327 00819 WP 1997 3 27 ABXA9700172 1 19961207 A 5720 59124371 DOUBLER DOUG DC9 DC941 302207N WP LT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47497 DURING C-CHECK, FOUND LEVEL 2 CORRSION ON LEFT MAIN LANDING GEAR DOUBLER. REPAIRED IAW DC-9 SRM 51-10-3, FIGURE 6. 2 L 7 2 4F A6WE 1997032700820 19970327 00820 WP 1997 3 27 ABXA9700173 1 19961203 A 5400 5913262 ANGLE DOUG DC9 DC941 302207N WP LT PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47497 DURING C-CHECK, FOUND REPAIR ON UPPER PYLON ATTACH ANGLE CRACKED ON LEFT PYLON. REPAIRED IAW DC-9 SRM 54-04, FIGURE 10. 2 L 7 2 4F A6WE 1997032700821 19970327 00821 WP 1997 3 27 ABXA9700174 1 19961202 A 5320 9911516 CLIP DOUG DC9 DC941 302207N WP BS 168 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47497 DURING C-CHECK, FOUND LEVEL 2 CORROSION ON CLIP AT BASE OF FRAME 168. FABRICATED CLIP IAW DAC DRAWING 9911516, INSTALLE D IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 1997032700822 19970327 00822 WP 1997 3 27 ABXA9700175 1 19961127 A 5320 59560805 SUPPORT DOUG DC9 DC941 302207N WP BS 215 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47497 DURING C-CHECK, FOUND LEVEL 2 CORROSION ON FLOOR SUPPORT STATION 215, AT LONGERON 28L-28R. REPLACED SUPPORT IAW DC-9 SR M, 51-30-2, 51-30-5. 2 L 7 2 4F A6WE 1997032700823 19970327 00823 WP 1997 3 27 ABXA9700176 1 19961127 A 5730 59127351 PANEL DOUG DC9 DC941 302207N WP LT WING DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47497 DURING C-CHECK, FOUND LEFT WING OUTBOARD PANEL DELAMINATED AND CORRODED. REPLACED LEFT WING OUTBOARD PANEL IAW DC-9 SRM 51-30-1. 2 L 7 2 4F A6WE 1997032700824 19970327 00824 WP 1997 3 27 ABXA9700177 1 19961203 A 5311 99234091 FRAME DOUG DC9 DC941 302207N WP BS 737 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47497 DURING C-CHECK, FOUND FS 737 LEFT MAIN FRAME CRACKED. REPAIRED LEFT MAIN FRAME AT FS 737 IAW ABX REA D953-17381. 2 L 7 2 4F A6WE 1997032700825 19970327 00825 WP 1997 3 27 ABXA9700178 1 19961202 A 5312 995821210 BLKHD STIFFENER DOUG DC9 DC941 302207N WP BS 794 GOUGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47497 DURING C-CHECK, FOUND VERTICAL STIFFENER GOUGED ON FORWARD BULKHEAD IN ALC COMPARTMENT. REPAIRED VERTICAL STIFFENER IAW ABX REA D953-17379-MR. 2 L 7 2 4F A6WE 1997032700826 19970327 00826 WP 1997 3 27 ABXA9700179 1 19961201 A 5320 5912285505 WINDOW FRAME DOUG DC9 DC941 302207N WP BS 718-737 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47497 DURING C-CHECK, FOUND WINDOW FRAME CRACKED BETWEEN STATION 718-737. REPAIRED THE WINDOW FRAME IAW ABX REA D953-17384. 2 L 7 2 4F A6WE 1997032700827 19970327 00827 WP 1997 3 27 ABXA9700180 1 19961204 A 5744 59260599 FITTING DOUG DC9 DC941 302207N WP LT WING GOUGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47497 DURING C-CHECK, FOUND LEFT WING INBOARD SPOILER FITTING GOUGED. REPAIRED THE LEFT WING INBOARD FITTING IAW ABX REA D957 -17399-MR. 2 L 7 2 4F A6WE 1997032700828 19970327 00828 WP 1997 3 27 ABXA9700181 1 19961127 A 5320 49559471 HOLD OPEN CUP DOUG DC9 DC941 302207N WP BS 130 GOUGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47497 DURING C-CHECK, FOUND GOUGES AROUND HOLD OPEN LATCH CUP ON LEFT SIDE OF FUSELAGE. REPAIRED IAW DC-9 SRM 53-04, FIG. 24, SHEET 2. REPLACED CUP IAW DC-9 SRM 51-30-2, 51-30-5. 2 L 7 2 4F A6WE 1997032700829 19970327 00829 WP 1997 3 27 ABXA9700182 1 19961127 A 5320 992345925 FITTING DOUG DC9 DC941 302207N WP BS 737 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47497 DURING C-CHECK, FOUND CRACK IN KEEL WEB FLANGE ABOVE FORWARD DOOR JAMB FRAME OF LEFT WHEEL WELL. REPLACED FITTING AT KE EL WEB FLANGE ABOVE FORWARD DOOR JAMB IN LEFT WHEEL WELL IAW DC-9 SRM 51-30-2, 51-30-5. 2 L 7 2 4F A6WE 1997032700830 19970327 00830 WP 1997 3 27 ABXA9700183 1 19961125 A 5210 3916139501 WEB DOUG DC9 DC941 302207N WP ENTRY DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47497 DURING C-CHECK, FOUND WEB CRACKED ON ENTRY DOOR. REPAIRED WEB ON ENTRY DOOR IAW DC-9 SRM 52-05, FIG.7. 2 L 7 2 4F A6WE 1997032700831 19970327 00831 WP 1997 3 27 ABXA9700184 1 19961201 A 5320 5912285509 WINDOW FRAME DOUG DC9 DC941 302207N WP BS 617 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47497 DURING C-CHECK, FOUND WINDOW FRAME CRACKED AT STATION 617 RIGHT. REPAIRED WINDOW FRAME AT STATION 617 RIGHT IAW ABX REA D953-17346. 2 L 7 2 4F A6WE 1997032700832 19970327 00832 WP 1997 3 27 ABXA9700185 1 19961127 A 5320 5912285509 WINDOW FRAME DOUG DC9 DC941 302207N WP BS 617-636 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47497 DURING C-CHECK, FOUND WINDOW FRAME CRACKED BETWEEN STATION 617-636 LEFT. REPAIRED WINDOW FRAME BETWEEN STATION 617-636 LEFT, IAW ABX REA D953-17346. 2 L 7 2 4F A6WE 1997032700833 19970327 00833 WP 1997 3 27 ABXA9700186 1 19961127 A 5320 5912285513 WINDOW FRAME DOUG DC9 DC941 302207N WP FS 636-655 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47497 DURING C-CHECK, FOUND WINDOW FRAME CRACKED BETWEEN STATION 636-655 LEFT. REPAIRED WINDOW FRAME BETWEEN STATION 636-655 LEFT, IAW ABX REA D953-17346. 2 L 7 2 4F A6WE 1997032700834 19970327 00834 WP 1997 3 27 ABXA9700187 1 19961127 A 5320 59912285515 WINDOW FRAME DOUG DC9 DC941 302207N WP BS 677-696 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47497 DURING C-CHECK, FOUND WINDOW FRAME BETWEEN STATION 677-696 RIGHT. REPAIRED WINDOW FRAME BETWEEN STATION 677-696 RIGHT, IAW ABX REA D842-17346. 2 L 7 2 4F A6WE 1997032700835 19970327 00835 WP 1997 3 27 ABXA9700188 1 19961201 A 5320 5912285515 WINDOW FRAME DOUG DC9 DC941 302207N WP BS 677-697 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47497 DURING C-CHECK, FOUND WINDOW FRAME BETWEEN STATION 677-697 LEFT. REPAIRED WINDOW FRAME BETWEEN STATION 677-697 LEFT, IA W ABX REA D953-17346. 2 L 7 2 4F A6WE 1997032700836 19970327 00836 WP 1997 3 27 ABXA9700189 1 19961130 A 5320 5912285509 WINDOW FRAME DOUG DC9 DC941 302207N WP BS 737-756 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47497 DURING C-CHECK, FOUND WINDOW FRAME BETWEEN STATION 737-756 LEFT. REPAIRED WINDOW FRAME BETWEEN STATION 737-756 LEFT, IA W ABX REA D953-17346. 2 L 7 2 4F A6WE 1997032700837 19970327 00837 WP 1997 3 27 ABXA9700190 1 19961211 A 5720 5919573502 DOOR DOUG DC9 DC941 302207N WP RT WING DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 966AX 47510 DURING C-CHECK , THE RIGHT WING BUTE DOOR NR 1603 WAS FOUND DELAMINATED, NR UD-004. REPLACED THE RIGHT WING BUTE DOOR N R 1603 IAW DC-9 M.M 57-20-3. 2 L 7 2 4F A6WE 1997032700838 19970327 00838 WP 1997 3 27 ABXA9700191 1 19961211 A 3231 3923159505 LINKAGE DOUG DC9 DC941 302207N WP RT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 966AX 47510 DURING C-CHECK, THE RIGHT LANDING GEAR OUTBOARD DOOR LINKAGE ASSEMBLY WAS FOUND WORN, NR CF-769. REPLACED THE LINKAGE A SSEMBLY IAW OHM 32-10-6. 2 L 7 2 4F A6WE 1997032700839 19970327 00839 WP 1997 3 27 ABXA9700192 1 19961211 A 3231 3923166501 LINKAGE DOUG DC9 DC941 302207N WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 966AX 47510 DURING C-CHECK, THE LEFT LANDING GEAR OUTBOARD DOOR HINGE AND LINKAGE ASSEMBLY WERE FOUND WORN. REPLACED THE LINKAGE AS SEMBLY IAW DC-9 MM 32-12-1. 2 L 7 2 4F A6WE 1997032700840 19970327 00840 WP 1997 3 27 ABXA9700193 1 19961211 A 5532 59189601 PANEL DOUG DC9 DC941 302207N WP VERTICAL STAB CHAFED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 966AX 47510 DURING C-CHECK, VERTICAL STABILIZER SKIN PANEL WAS FOUND CHAFED NEXT TO HORIZONTAL STABILIZER, NR CF-818. REPLACED THE SKIN PANEL IAW DC-9 SRM 51-10-4. 2 L 7 2 4F A6WE 1997032700841 19970327 00841 WP 1997 3 27 ABXA9700194 1 19961211 A 5512 591217148 PANEL DOUG DC9 DC941 302207N WP HORIZ STAB DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 966AX 47510 DURING C-CHECK, HORIZONTAL STABILIZER PANEL NR 3806 WAS FOUND DELAMINATED, NR CF-808. REPLACED THE PANEL IAW DC-9 SRM 5 1-10-4. 2 L 7 2 4F A6WE 1997032700842 19970327 00842 WP 1997 3 27 ABXA9700195 1 19961208 A 5311 99118595 CANTED FRAME DOUG DC9 DC941 302207N WP BS 1180 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 966AX 47510 DURING C-CHECK, FOUND THAT CANTED FRAME AT STATION 1180 LONGERON 4 RIGHT WAS FOUND CRACKED, NR CF-976. THE FRAME WAS RE PLACED IAW DC-9 SRM 51-10-4. 2 L 7 2 4F A6WE 1997032700843 19970327 00843 WP 1997 3 27 ABXA9700196 1 19961208 A 5320 991770 INTERCOSTAL DOUG DC9 DC941 302207N WP BS 1244 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 966AX 47510 DURING C-CHECK, THE LEFT INTERCOSTAL AT CANTED FRAME STATION 1244 WAS FOUND CRACKED, NR, CF-982. REPLACED INTERCOSTAL I AW DC-9 SRM 51-30-1. 2 L 7 2 4F A6WE 1997032700844 19970327 00844 WP 1997 3 27 ABXA9700197 1 19961207 A 5755 5910055513 PANEL DOUG DC9 DC941 302207N WP LT WING SPOILER DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 966AX 47510 DURING C-CHECK, THE OUTBOARD SPOILER PANEL WAS FOUND DELAMINATED, NR CF-751. REPLACED SPOILER IAW DC-9 MM 27-61-1. 2 L 7 2 4F A6WE 1997032700845 19970327 00845 WP 1997 3 27 ABXA9700198 1 19961208 A 5753 5910041504 VANE DOUG DC9 DC941 302207N WP RT TE FLAP DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 966AX 47510 DURING C-CHECK, THE INBOARD FLAP FIXED VANE WAS FOUND DELAMINATED, NR CF-880. THE INBOARD FLAP FIXED VANE REPLACED IAW DC-9 MM 27-51-3. 2 L 7 2 4F A6WE 1997032700846 19970327 00846 WP 1997 3 27 ABXA9700199 1 19961208 A 5730 5912161148 PANEL DOUG DC9 DC941 302207N WP RT WING DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 966AX 47510 DURING C-CHECK, THE RIGHT WING INBOARD UPPER AFT BONDED PANEL WAS FOUND DELAMINATED, NR CF-908. REPLACED THE RIGHT WING INBOARD UPPER AFT BONDED PANEL IAW DC-9 SRM 51-10-4. 2 L 7 2 4F A6WE 1997032700847 19970327 00847 WP 1997 3 27 ABXA9700200 1 19961207 A 5280 5910557110 DOOR DOUG DC9 DC941 302207N WP RT MLG DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 966AX 47510 DURING C-CHECK, THE RIGHT LANDING GEAR OUTBOARD DOOR WAS FOUND DELAMINATED, NR CF-772. REPLACED THE RIGHT LANDING GEAR OUTBOARD DOOR IAW DC-9 MM 32-12-1. 2 L 7 2 4F A6WE 1997032700848 19970327 00848 WP 1997 3 27 ABXA9700201 1 19961212 A 5280 5910557110 DOOR DOUG DC9 DC933F 302207A WP RT MLG DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 DURING COMPLIANCE WITH AD 91-22-07, ASB 32-244 FOUND RIGHT FLYING DOOR DELAMINATED. REPAIRED THE RIGHT FLYING DOOR IAW DC-9 SRM 52-02 PAGE 1. 2 L 7 2 4F A6WE 1997032700849 19970327 00849 WP 1997 3 27 ABXA9700202 1 19961212 A 3231 S2210370P4101 BUSHING DOUG DC9 DC933F 302207A WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 930AX 47363 DURING COMPLIANCE WITH AD 91-22-07, ASB 32-244 FOUND LEFT FLYING DOOR LINKAGE WORN. REPLACED THE BUSHING TO THE LEFT FL YING DOOR LINKAGE IAW DC-9 M/M 20-10-1. 2 L 7 2 4F A6WE 1997032700850 19970327 00850 WP 1997 3 27 ABXA9700203 1 19960905 A 3231 3923184 LINK DOUG DC9 DC931 3022065 WP RT MLG WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, WHILE ACCOMPLISHING AD 91-22-07, THE RIGHT MAIN LANDING GEAR OUTBOARD DOOR CONTROL LINKAGE WAS FOUND WOR N. THE CONTROL LINK WAS REPLACED IAW DC-9 M/M 32-12-1. 2 L 7 2 4F A6WE 1997040200002 19970402 00002 EU 1997 4 2 CA961018004 1 19960924 A 3260 90015EN38 SWITCH BAG JETSTM JETSTM3212 1500217 EU ROTOL R333 R333482F12 GL LT MLG FAILED W O OTHER N FALSE WARNING AP APPROACH 1 CA DRG471088 (CAN) PILOT REPORTED AFTER SELECTING GEAR DOWN AND INDICATING LOCKED WITH THREE GREEN LIGHTS, LH MAIN GEAR UNSAFE LIGHT CAME ON AND WARNING HORN SOUNDED. AIRCRAFT LANDED OK. BOTH UPLOCK AND DOWNLOCK SWITCHES REPLACED, SUSPECTED MOISTURE. 2 L 7 2 4T RT BA15CAA 6 C P61GL 1997040200003 19970402 00003 NM 1997 4 2 CA961018012 1 19961001 A 5246 65B9064510 DOOR ASSEMBLY BOEING 747 747233B NM PWA JT9 JT9D7 52054 NE NR 3 ENG CSD MISSING W K NONE O OTHER TX TAXI/GRND HDL 1 CA P686008 (CAN) PRIOR TO DEPARTURE #3 ENGINE CSD ACCESS PANEL MISSING, REPLACED. 2 L 7 4 4F 4 F RT A20WE E20EA 1997040200005 19970402 00005 NM 1997 4 2 CA961021014 1 19961006 A 2530 03910808P4 SOCKET BOEING 747 747233B NM PWA JT9 JT9D7 52054 NE GALLEY HOT CUP BURNT W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA P695768 (CAN) BIG SPARK FROM ORANGE LIGHT ON LEFT HOT CUP IN GALLEY #3 AREA AROUND BLACKENED AND HALF GALLEY SHUT DOWN, EXTINGUI SHER USED, FULL INFLIGHT FIRE DRILL. HOT CUP LIGHT SOCKET BURNT, REPLACED. 2 L 7 4 4F 4 F RT A20WE E20EA 1997040200007 19970402 00007 SW 1997 4 2 CA961023001 1 19961016 A 3233 50810165 PINION BEECH 265106503 SWRNGN SA226 SA226AT 8780405 SW MLG ACTUATOR DISENGAGED W K NONE J WARNING INDICATION LD LANDING 1 CA 309 7060 (CAN) ON LANDING LEFT HAND GEAR INDICATOR SHOWED UNSAFE. INSPECTION FOUND THAT THE LEFT HAND GEAR DID NOT HAVE THE REQUI RED SPRING TENSION ON THE DOWN LOCK. LEFT GEAR ACTUATOR HAD SLIPPED. ACTUATOR REMOVED AND OUTBOARD SUPPORT BEARING WAS F OUND PROTRUDING ABOUT 1/8 INCH FROM HOUSING WHICH MAY HAVE LET PINION GEARS SLIP. 2 L 7 2 4T RT A5SW 1997040200014 19970402 00014 GL 1997 4 2 CA961029009 4 19961011 A 6113 C5046 ATTACH PLATE CESSNA 182 R182 2072734 CE MCAULY 2D34C B2D34C218 GL PROP BOLT AREA CRACKED W K NONE E VIBRATION/BUFFET IN INSP/MAINT 1 CA 150 150 801468 (CAN) DURING INSPECTION THE PROPELLER BACK PLATE WAS FOUND CRACKED IN THE ATTACHMENT BOLT AREA. 1 H 7 1 3O RT 3A13 5 C P7EA 1997040300100 19970403 00100 WP 1997 4 3 ABXA9700205 1 19960812 A 3231 NAS110420D BOLT DOUG DC9 DC932 3022066 WP RT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 989AX 47314 DURING COMPLIANCE OF AD 91-22-07, ASB 32-244 FOUND RIGHT HAND MAIN LANDING GEAR OUTBOARD DOOR LINKAGE WORN AT PIVOT POIN T OF LINKAGE RODS. REPLACED RIGHT HAND MAIN LANDING GEAR OUTBOARD DOOR LINKAGE BOLT IAW DC-9 OVERHAUL MANUAL CHAPTER 32 . 2 L 7 2 4F A6WE 1997040300101 19970403 00101 WP 1997 4 3 ABXA9700206 1 19960824 A 3231 NAS130425D BOLT DOUG DC9 DC941 302207N WP RT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47494 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244 FOUND RIGHT HAND MAIN LANDING GEAR OUTBOARD DOOR LINKAGE ARM LOOSE. REPLAC ED BOLT IN RIGHT HAND MAIN LANDING GEAR OUTBOARD LINKAGE ARM IAW DC-9 OVERHAUL MANUAL. 2 L 7 2 4F A6WE 1997040300102 19970403 00102 WP 1997 4 3 ABXA9700207 1 19960824 A 3231 NAS130412 BOLT DOUG DC9 DC941 302207N WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47494 DURING COMPLIANCE OF AD 91-22-07, ASB 32-244 LEFT HAND MAIN LANDING GEAR LINKAGE ROD END WORN. REPLACED LOOSE AND WORN BOLT. 2 L 7 2 4F A6WE 1997040300103 19970403 00103 WP 1997 4 3 ABXA9700208 1 19960824 A 3231 3923159505 ARM DOUG DC9 DC941 302207N WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47494 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244 FOUND LEFT HAND MAIN LANDING GEAR OUTBOARD DOOR LINKAGE ARM LOOSE/WORN. RE PLACED ARTICULATING ARM AND HARDWARE IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1997040300104 19970403 00104 WP 1997 4 3 ABXA9700209 1 19960824 A 3231 S2210370P4101 BUSHING DOUG DC9 DC941 302207N WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47494 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244 FOUND LEFT HAND MAIN LANDING GEAR OUTBOARD DOOR LINKAGE LOOSE/WORN AT PIVOT OF LINKAGE RODS. REPLACED BUSHING AND HARDWARE IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1997040300105 19970403 00105 WP 1997 4 3 ABXA9700210 1 19960806 A 3231 2923166502 BRACKET DOUG DC9 DC932 3022066 WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 985AX 47522 DURING COMPLIANCE OF AD 91-22-07, ASB 32-244 FOUND RIGHT HAND MAIN LANDING GEAR OUTBOARD DOOR ARM WORN/LOOSE. REPLACED RIGHT HAND MAIN LANDING GEAR OUTBOARD DOOR ARM BRACKET IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1997040300106 19970403 00106 WP 1997 4 3 ABXA9700211 1 19960806 A 3231 29244721 PIN DOUG DC9 DC932 3022066 WP RT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 985AX 47522 DURING COMPLIANCE OF AD 91-22-07, ASB 32-244 FOUND RIGHT MAIN LANDING GEAR DOOR HINGE WORN. REPLACED HINGE PIN IAW DC-9 SRM 32-12-1. 2 L 7 2 4F A6WE 1997040300107 19970403 00107 WP 1997 4 3 ABXA9700212 1 19960621 A 7830 5958775186N FAIRING DOUG DC9 DC932 3022066 WP NR 2 TR UNIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND NR 2 REVERSER UPPER DOOR OUTBOARD FAIRING CRACKED. REPLACED IAW D C-9 SRM 51-30-2, 51-30-8. 2 L 7 2 4F A6WE 1997040300108 19970403 00108 WP 1997 4 3 ABXA9700213 1 19960619 A 5753 995760015 BRACKET DOUG DC9 DC932 3022066 WP LT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND LEFT FLAP ATTACH BRACKET CRACKED AT STATION 353. REPLACED IAW DC- 9 SRM 51-30-4, 51-30-1, 51-30-2. 2 L 7 2 4F A6WE 1997040300109 19970403 00109 WP 1997 4 3 ABXA9700214 1 19960619 A 5753 99576004 FORMER DOUG DC9 DC932 3022066 WP RT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND RIGHT FLAP OUTBOARD FLAP ATTACH FITTING CRACKED. REPLACED IAW DC- 9 SRM 51-30-1, 51-30-2. 2 L 7 2 4F A6WE 1997040300110 19970403 00110 WP 1997 4 3 ABXA9700215 1 19960628 A 7830 5958775185 FAIRING DOUG DC9 DC932 3022066 WP NR 1 TR UNIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-07, FOUND NR 1 REVERSER UPPER DOOR INBOARD FAIRING CRACKED. REPLACED IAW DC -9 SRM 51-30-2, 51-30-8. 2 L 7 2 4F A6WE 1997040300111 19970403 00111 WP 1997 4 3 ABXA9700216 1 19960530 A 5347 6013506 SEAT TRACK DOUG DC9 DC941 302207N WP CARGO COMPT CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 DURING ACCEPTANCE INSPECTION WHILE ACCOMPLISHING AD 92-22-08, LEVEL TWO CORROSION WAS FOUND ON A SEAT TRACK AT STATION 3 70 LONGERON 28 RIGHT. THE TRACK WAS REPLACED IAW DC-9 SRM 51-30-5 AND 51-30-2. 2 L 7 2 4F A6WE 1997040300112 19970403 00112 WP 1997 4 3 ABXA9700217 1 19960509 A 5280 591055725 SEAL DOUG DC9 DC941 302207N WP LT MLG DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 DURING ACCEPTANCE INSPECTION WHILE ACCOMPLISHING AD 92-22-08, THE METAL SEAL ON THE LEFT MAIN LANDING GEAR OUTBOARD DOOR WAS FOUND CRACKED ON THE TRAILING EDGE BY THE HINGE POINT. THE SEAL WAS REPLACED IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 1997040300113 19970403 00113 WP 1997 4 3 ABXA9700218 1 19960613 A 5315 99115957 FLOORBEAM DOUG DC9 DC941 302207N WP BS 200 DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 DURING ACCEPTANCE INSPECTION, THE FLOORBEAM AT STATION 200 WAS FOUND TO HAVE SEVERAL DOUBLE DRILLED AND CLOSELY SPACED H OLES. THE FLOORBEAM WAS REPAIRED IAW REA D953-15436-MR. 2 L 7 2 4F A6WE 1997040300114 19970403 00114 WP 1997 4 3 ABXA9700219 1 19961006 A 5280 29242891 BUSHINGS DOUG DC9 DC941 302207N WP RT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 955AX 47619 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND RIGHT MAIN LANDING GEAR OUTBOARD DOOR HAS PLAY AT HINGE. REPLACED R IGHT MAIN LANDING GEAR OUTBOARD DOOR HINGE BUSHINGS IAW DC-9 OVERHAUL MANUAL 32-10-10. BUSHINGS MANUFACTURED ON SHOP TR AVELER NR 43224. 2 L 7 2 4F A6WE 1997040300115 19970403 00115 WP 1997 4 3 ABXA9700220 1 19961122 A 5280 S2210370P4109 BUSHING DOUG DC9 DC941 302207N WP RT MLG WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 WHILE COMPLYING WITH AD 91-22-07, FOUND EXCESSIVE PLAY AT RIGHT MAIN LANDING GEAR OUTBOARD DOOR LINKAGE TO DOOR ATTACH L INK. REPLACED BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1997040300116 19970403 00116 WP 1997 4 3 ABXA9700221 1 19961122 A 5280 5910557109 SKIN DOUG DC9 DC941 302207N WP LT MLG DOOR DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 WHILE COMPLYING WITH AD 91-22-07, FOUND LEFT OUTBOARD MAIN LANDING GEAR DOOR DELAMINATED. REMOVED AND REPLACED LEFT MAI N LANDING GEAR ARTICULATING DOOR IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1997040300117 19970403 00117 WP 1997 4 3 ABXA9700222 1 19961122 A 5280 3923166501 FITTING DOUG DC9 DC941 302207N WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 WHILE COMPLYING WITH AD 91-22-07, FOUND EXCESSIVE PLAY AT LINKAGE TO DOOR ATTACH LINK ON LEFT MAIN LANDING GEAR OUTBAORD DOOR. REMOVED AND REPLACED FITTING IAW DC-9 OVERHAUL MANUAL 32-10-6 ON LEFT MAIN LANDING GEAR OUTBOARD DOOR. 2 L 7 2 4F A6WE 1997040300118 19970403 00118 WP 1997 4 3 ABXA9700223 1 19961122 A 5280 2210370P4109 BUSHINGS DOUG DC9 DC941 302207N WP RT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 WHILE COMPLYING WITH AD 91-22-0, FOUND EXCESSIVE PLAY AT RIGHT MAIN LANDING GEAR OUTBOARD DOOR TO WING HINGE. FABRICAT ED AND INSTALLED BUSHINGS ON RIGHT ARTICULATING DOOR FOWARD 4 HOLES IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1997040300119 19970403 00119 WP 1997 4 3 ABXA9700224 1 19961117 A 5280 BEARING DOUG DC9 DC931 3022065 WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 907AX 47203 WHILE COMPLYING WITH AD 91-22-07, FOUND LEFT HAND MAIN LANDING GEAR OUTBOARD DOOR LINKAGE TO HAVE EXCESSIVE PLAY AT LINK AGE ROD PIVOT POINT. REPLACED BEARING IAW SB 32-244. 2 L 7 2 4F A6WE 1997040300120 19970403 00120 WP 1997 4 3 ABXA9700225 1 19961106 A 3231 39231597 ARM DOUG DC9 DC932 3022066 WP LT MLG DOOR LOOSE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 984AX 47258 DURING COMPLIANCE WITH AD 91-22-07; ASB 32-244, FOUND LEFT HAND MAIN LANDING GEAR OUTBOARD DOOR ARTICULATING DOOR TO HA VE EXCESSIVE PLAY. REMOVED AND REPLACED BOLT AND SHIMMED LINKAGE ARM IAW DC-9 M/M 20-16-0. 2 L 7 2 4F A6WE 1997040300121 19970403 00121 WP 1997 4 3 ABXA9700226 1 19960928 A 3231 VTA00070 ROD END DOUG DC9 DC941 302207N WP RT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX 47615 DURING COMPLIANE WITH AD 92-22-07, ASB 32-244, FOUND RIGHT MAIN LANDING GEAR ARTICULATING DOOR LINK BEARING WORN ON OUTB OARD MAIN LANDING GEAR DOOR FOR ROD ASSEMBLY. REPLACED ROD END AND SHIMMED BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1997040300122 19970403 00122 WP 1997 4 3 ABXA9700227 1 19961106 A 5280 39231597 ARM DOUG DC9 DC932 3022066 WP RT MLG DOOR LOOSE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 984AX 47258 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND RIGHT HAND MAIN LANDING GEAR OUTBOARD DOOR LINKAGE ARM LOOSE/WORN. R EMOVED AND REPLACED BOLT AND SHIMMED LINKAGE ARM IAW DC-9 M/M 20-16-0. 2 L 7 2 4F A6WE 1997040300123 19970403 00123 WP 1997 4 3 ABXA9700228 1 19961109 A 2720 4616066 HUB DOUG DC9 DC931 3022065 WP RUDDER PEDALS CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 946AX 47003 DURING COMPLIANCE OF N 2757, AD 96-02-05, ASB A 27-325 REV NR 3 THE PEDAL ADJUST HUB ASSEMBLY HAD CRACK INDICATIONS. *S /D* CHANGED HUB ASSEMBLY IAW ABX EA AD 27-03967-MA. 2 L 7 2 4F A6WE 1997040300124 19970403 00124 WP 1997 4 3 ABXA9700229 1 19960924 A 5320 99155781 INTERCOSTAL DOUG DC9 DC933F 302207A WP BS 897-889 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 934AX 47462 DURING C-CHECK, AN INTERCOSTAL WAS FOUND CRACKED BETWEEN STATION 897 TO 889 LONGERONS 30 AND 29 RIGHT. REPLACED IAW DC- 9 SRM 53-30-2. 2 L 7 2 4F A6WE 1997040300125 19970403 00125 WP 1997 4 3 ABXA9700230 1 19961120 A 5320 5913055504 FITTING DOUG DC9 DC933F 302207A WP BS 598 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, THE CENTER FUEL TANK UPPER OUTBOARD ATTACH FITTING WAS FOUND CORRODED AT STATION 598 RIGHT, NR BF-399. T HE FITTING WAS REPLACED IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997040300126 19970403 00126 WP 1997 4 3 ABXA9700231 1 19961120 A 5320 992341014 ANGLE DOUG DC9 DC933F 302207A WP BS 655 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, THE CENTER FUEL TANK UPPER ATTACH ANGLE WAS FOUND CRACKED AT STATION 655 LBL, NR BF-422. THE ANGLE WAS REPLACED IAW DC-9 SRM AND REA D957-17305-MR. 2 L 7 2 4F A6WE 1997040300127 19970403 00127 WP 1997 4 3 ABXA9700232 1 19961120 A 5313 592480245 LONGERON DOUG DC9 DC933F 302207A WP BS 408 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, LONGERON 17 RIGHT AT STATION 408 WAS FOUND CRACKED, NR BF-378. THE LONGERON WAS REPLACED IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997040300128 19970403 00128 WP 1997 4 3 ABXA9700233 1 19961120 A 5313 592480245 LONGERON DOUG DC9 DC933F 302207A WP BS 389 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, LONGERON 17 RIGHT AT STATION 389 WAS FOUND CRACKED, NR BF-377. THE LONGERON WAS REPLACED IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997040300129 19970403 00129 WP 1997 4 3 ABXA9700234 1 19961120 A 5313 592480219 LONGERON DOUG DC9 DC933F 302207A WP BS 294 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, LONGERON 17 RIGHT AT STATON 294 WAS FOUND CRACKED, NR BF-375. THE LONGERON WAS REPLACED IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997040300130 19970403 00130 WP 1997 4 3 ABXA9700235 1 19961120 A 5313 592480219 LONGERON DOUG DC9 DC933F 302207A WP BS 313 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, LONGERON 17 RIGHT AT STATION 313 WAS FOUND CRACKED, NR BF-376. THE LONGERON WAS REPLACED IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997040300131 19970403 00131 WP 1997 4 3 ABXA9700236 1 19961120 A 5347 60219627075T6511 SEAT TRACK DOUG DC9 DC933F 302207A WP BS 957-965 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, THE SEAT TRACK FROM STATION 957 TO 965 WAS FOUND EXFOLIATED AT LBL 44, NR BF-543. THE SEAT TRACK WAS RE PLACED IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997040300132 19970403 00132 WP 1997 4 3 ABXA9700237 1 19961125 A 5330 59114273 SKIN DOUG DC9 DC933F 302207A WP BS 960 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, THE FUSELAGE SKIN WAS FOUND CRACKED AT STATION 960 BELOW LONGERON 16 RIGHT, NR BF-665. THE SKIN WAS REP AIRED IAW REA D953-17291-MR. 2 L 7 2 4F A6WE 1997040300133 19970403 00133 WP 1997 4 3 ABXA9700238 1 19961120 A 5313 5911479 LONGERON DOUG DC9 DC933F 302207A WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, LONGERON 17 LEFT AT STATION 980 WAS FOUND CRACKED, NR BF-599. THE LONGERON WAS REPLACED IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997040300134 19970403 00134 WP 1997 4 3 ABXA9700239 1 19961120 A 5313 59114279 LONGERON DOUG DC9 DC933F 302207A WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, LONGERON 17 RIGHT AT STATION 980 WAS FOUND CRACKED, NR BF-622. THE LONGERON WAS REPLACED IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997040300135 19970403 00135 WP 1997 4 3 ABXA9700240 1 19961120 A 5320 D0489832 WEB DOUG DC9 DC933F 302207A WP BS 775-794 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, THE RIGHT CUSP WEB AT STATION 775 TO 794 WAS FOUND CORRODED, NR BF-495. THE WEB WAS REPAIRED IAW DC-9 S RM. 2 L 7 2 4F A6WE 1997040300136 19970403 00136 WP 1997 4 3 ABXA9700241 1 19961120 A 5720 S095700036 FITTING DOUG DC9 DC933F 302207A WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, THE NR 2 SLAT TRACK INBOARD SUPPORT FITTING WAS FOUND CRACKED, NR BF-259. THE FITTING WAS REPLACED IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997040300137 19970403 00137 WP 1997 4 3 ABXA9700242 1 19961120 A 5315 99581881 FLOORBEAM DOUG DC9 DC933F 302207A WP BS 980 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, A FLOORBEAM AT STATION 980 RBL 22.0 WAS FOUND CORRODED, NR BF-692. THE FLOORBEAM WAS REPAIRED IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997040300138 19970403 00138 WP 1997 4 3 ABXA9700243 1 19961125 A 5320 4911383501 FITTING DOUG DC9 DC933F 302207A WP BS 980 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, A FRAME FITTING AT STATION 980, RIGHT CUSP WAS FOUND CORRODED, NR BF-598. THE FITTING WAS REPLACED IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997040300139 19970403 00139 WP 1997 4 3 ABXA9700244 1 19961203 A 5320 D0498935 CUSP WEB DOUG DC9 DC933F 302207A WP BS 960 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, A CUSP WEB AT STATION 960 WAS FOUND CRACKED, NR BF-698. THE CUSP WEB WAS REPAIRED IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997040300140 19970403 00140 WP 1997 4 3 ABXA9700245 1 19961125 A 5311 99582387 FRAME DOUG DC9 DC933F 302207A WP BS 980 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, A FRAME AT STATION 980 LONGERON 18 RIGHT WAS FOUND CORRODED, NR BF-596. THE FRAME WAS REPAIRED IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997040300141 19970403 00141 WP 1997 4 3 ABXA9700246 1 19961125 A 5320 9958238 FORMER DOUG DC9 DC933F 302207A WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, A FORMER AT STATION 980 LONGERON 16 RIGHT WAS FOUND CRACKED, NR BF-597. THE FORMER WAS REPLACED IAW DC- 9 SRM. 2 L 7 2 4F A6WE 1997040300142 19970403 00142 WP 1997 4 3 ABXA9700247 1 19961123 A 5320 99577375 INTERCOSTAL DOUG DC9 DC933F 302207A WP BS 980-996 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, AN INTERCOSTAL AT STATION 980 TO 996 WAS FOUND CORRODED AT LONGERON 14 LT, NR BF-602. THE INTERCOSTAL W AS REPLACED IAW DC9 SRM. 2 L 7 2 4F A6WE 1997040300143 19970403 00143 WP 1997 4 3 ABXA9700248 1 19961126 A 5320 9958238 FORMER DOUG DC9 DC933F 302207A WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, A FORMER AT STA 980 LONGERON 14 LT WAS FOUND CRACKED, NR BF-60. THE FORMER WAS REPLACED IAW DC9 SRM. 2 L 7 2 4F A6WE 1997040300144 19970403 00144 WP 1997 4 3 ABXA9700249 1 19961125 A 5412 9912243 BULKHEAD CLIP DOUG DC9 DC933F 302207A WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, A CLIP WAS FOUND CRACKED AT THE PYLON BULKHEAD STATION 965 LONGERON 17 RT, NR BF-600. THE CLIP WAS REPL ACED IAW DC9 SRM. 2 L 7 2 4F A6WE 1997040300145 19970403 00145 WP 1997 4 3 ABXA9700250 1 19961120 A 5313 9921594 LONGERON DOUG DC9 DC933F 302207A WP BS 443 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, A WEB AT STATION 443 LONGERON 14 LT WAS FOUND CORRODED, NB BF-637. THE WEB WAS REPLACED IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997040300146 19970403 00146 WP 1997 4 3 ABXA9700251 1 19961120 A 5320 991075521 WEB DOUG DC9 DC933F 302207A WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, THE RIGHT CUSP WEB WAS FOUND CRACKED AT STATION 965, NR BF-631. THE WEB WAS REPLACED IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997040300147 19970403 00147 WP 1997 4 3 ABXA9700252 1 19961122 A 5312 SB09530166295 BULKHEAD CLIP DOUG DC9 DC933F 302207A WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, A CLIP WAS FOUND CRACKED AT THE AFT PRESSURE BULKHEAD LONGERON 15 LEFT, NR BF-626. THE CLIP WAS REPAIRE D IAW DC9 SRM. 2 L 7 2 4F A6WE 1997040300148 19970403 00148 WP 1997 4 3 ABXA9700253 1 19961122 A 5312 SB09530166284 BULKHEAD CLIP DOUG DC9 DC933F 302207A WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, A CLIP WAS FOUND CRACKED AT THE AFT PRESSURE BULKHEAD LONGERON 12 RIGHT, NR BF-625. THE CLIP WAS REPAIR ED IAW DC9 SRM. 2 L 7 2 4F A6WE 1997040300149 19970403 00149 WP 1997 4 3 ABXA9700254 1 19961125 A 5312 SB09530166300 BULKHEAD CLIP DOUG DC9 DC933F 302207A WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, A CLIP WAS FOUND CRACKED AT THE AFT PRESSURE BULKHEAD LONGERON 17 RIGHT, NR BF-624. THE CLIP WAS REPAIR ED IAW DC9 SRM. 2 L 7 2 4F A6WE 1997040300150 19970403 00150 WP 1997 4 3 ABXA9700255 1 19961122 A 5312 SB09530166285 BULKHEAD CLIP DOUG DC9 DC933F 302207A WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, A CLIP WAS FOUND CRACKED AT THE AFT PRESSURE BULKHEAD LONGERON 14 LEFT, NR BF-627. THE CLIP WAS REPAIRE D IAW DC9 SRM. 2 L 7 2 4F A6WE 1997040300151 19970403 00151 WP 1997 4 3 ABXA9700256 1 19961119 A 5280 3923211 HINGE DOUG DC9 DC933F 302207A WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, THE LEFT MAIN LANDING GEAR OUTBOARD DOOR HINGE WAS FOUND WORN, NR AF-843. THE HINGE WAS REPLACED IAW DC -9 SRM. 2 L 7 2 4F A6WE 1997040300152 19970403 00152 WP 1997 4 3 ABXA9700257 1 19961118 A 5720 9919376503 SPLICE DOUG DC9 DC933F 302207A WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, THE WING LEADING EDGE SKIN SPLICE WAS FOUND CRACKED JUST OUTBOARD OF NR 6 SLAT TRACK, NR AF-796. THE CR ACK WAS REPAIRED IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997040300153 19970403 00153 WP 1997 4 3 ABXA9700258 1 19961203 A 5753 59121252 SPAR CAP DOUG DC9 DC933F 302207A WP RT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, THE FLAP LOWER SPAR CAP WAS FOUND CRACKED AT STATION 295, NR BF-667. THE FLAP WAS REPAIRED IAW REA D957 -17300-MR. 2 L 7 2 4F A6WE 1997040300154 19970403 00154 WP 1997 4 3 ABXA9700259 1 19961127 A 5753 99576001617 BRACKETS DOUG DC9 DC933F 302207A WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, THE RIGHT WING INBOARD AND OUTBOARD HINGE ATTACH BRACKETS WERE FOUND CRACKED AT STATION 353, NR AF-904. THE BRACKETS WERE REPLACED IAW DC9 SRM. 2 L 7 2 4F A6WE 1997040300155 19970403 00155 WP 1997 4 3 ABXA9700260 1 19961123 A 5720 4913567 ANGLE DOUG DC9 DC933F 302207A WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, THE RIGHT WING LOWER ATTACH OF OUTBOARD EXPANSION JOINT WAS FOUND CRACKED, NR AF-905. THE ANGLE WAS REP LACED IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997040300156 19970403 00156 WP 1997 4 3 ABXA9700261 1 19961120 A 3231 991932115 LINKAGE DOUG DC9 DC933F 302207A WP RT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, THE LEFT WING LEADING EDGE RIB WAS FOUND CRACKED INBOARD OF ANTI-ICE DUCT, NR AF-798. THE RIB WAS REPAI RED IAW DC9 SRM. 2 L 7 2 4F A6WE 1997040300157 19970403 00157 WP 1997 4 3 ABXA9700262 1 19961127 A 5753 59121681 VANE DOUG DC9 DC933F 302207A WP LT TE FLAP DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, THE LEFT WING FORWARD MOVEABLE VANE WAS FOUND DELAMINATED, NR AF-850. THE VANE WAS REPLACED IAW DC9 MM. 2 L 7 2 4F A6WE 1997040300158 19970403 00158 WP 1997 4 3 ABXA9700263 1 19961127 A 5753 5910041501 VANE DOUG DC9 DC933F 302207A WP LT TE FLAP CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, THE LEFT WING INBOARD FIXED VANE WAS FOUND CORRODED, NR AF-851. THE VANE WAS REPLACED IAW DC-9 MM. 2 L 7 2 4F A6WE 1997040300159 19970403 00159 WP 1997 4 3 ABXA9700265 1 19961127 A 5753 995760019 RIB DOUG DC9 DC933F 302207A WP LT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, THE LEFT WING FLAP RIB AT THE OUTBOARD HINGE WAS FOUND CRACKED, NR AF-937. THE RIB WAS REPAIRED IAW DC9 SRM. 2 L 7 2 4F A6WE 1997040300160 19970403 00160 WP 1997 4 3 ABXA9700266 1 19961118 A 5280 59203711 ANGLE DOUG DC9 DC933F 302207A WP MLG DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, THE LANDING GEAR INBOARD DOOR UPPER ATTACH ANGLE WAS FOUND CRACKED, NR BF-859. THE ANGLE WAS REPAIRED I AW ABX DRAWING K05818. 2 L 7 2 4F A6WE 1997040300161 19970403 00161 WP 1997 4 3 ABXA9700267 1 19961122 A 5753 99115244 LEADING EDGE DOUG DC9 DC933F 302207A WP RT TE FLAP CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, THE FLAP LEADING EDGE SECTION INTERIOR BONDED DOUBLER WAS FOUND CORRODED, NR BF-564. THE LEADING EDGE W AS REPLACED IAW DC9 SRM. 2 L 7 2 4F A6WE 1997040300162 19970403 00162 WP 1997 4 3 ABXA9700268 1 19961127 A 5730 9919385502 PANEL DOUG DC9 DC933F 302207A WP RT WING DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, BONDED PANEL 1249 WAS FOUND DELAMINATED, NR BF-421. THE PANEL WAS REPLACED IAW DC9 SRM. 2 L 7 2 4F A6WE 1997040300163 19970403 00163 WP 1997 4 3 ABXA9700269 1 19961127 A 5730 9919371502 PANEL DOUG DC9 DC933F 302207A WP RT WING DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, BONDED PANEL 1246 WAS FOUND DELAMINATED, NR BF-419. THE PANEL WAS REPLACED IAW DC9 SRM. 2 L 7 2 4F A6WE 1997040300164 19970403 00164 WP 1997 4 3 ABXA9700270 1 19961123 A 5753 491356716 BRACKET DOUG DC9 DC933F 302207A WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, THE FLAP OUTBOARD EXPANSION JOINT BRACKET WAS FOUND CRACKED, NR AF-905. THE BRACKETS WERE REPLACED IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997040300165 19970403 00165 WP 1997 4 3 ABXA9700271 1 19961119 A 5753 995760016 BRACKET DOUG DC9 DC933F 302207A WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, THE FLAP OUTBOARD HINGE ATTACH BRACKET WAS FOUND CRACKED, NR AF-904. THE BRACKETS WERE REPLACED IAW DC- 9 SRM. 2 L 7 2 4F A6WE 1997040300166 19970403 00166 WP 1997 4 3 ABXA9700272 1 19961123 A 5753 9958000 SPAR DOUG DC9 DC933F 302207A WP RT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, THE FLAP SPAR CAP AT STATION XFLS 298 WAS FOUND CRACKED, NR BF-667. THE SPAR WAS REPAIRED IAW REA DC957 -17300-MR. 2 L 7 2 4F A6WE 1997040300167 19970403 00167 WP 1997 4 3 ABXA9700273 1 19961127 A 5753 59121681 VANE DOUG DC9 DC933F 302207A WP LT TE FLAP DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, THE FORWARD MOVEABLE VANE UPPER SURFACE WAS FOUND DELAMINATED, NR AF-850. THE VANE WAS REPLACED IAW DC9 MM. 2 L 7 2 4F A6WE 1997040300168 19970403 00168 WP 1997 4 3 ABXA9700274 1 19961127 A 5753 5910041501 VANE DOUG DC9 DC933F 302207A WP LT TE FLAP DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, THE INBOARD FIXED VANE UPPER SURFACE WAS FOUND DELAMINATED, NR AF-851. THE VANE WAS REPLACED IAW DC9 MM . 2 L 7 2 4F A6WE 1997040300169 19970403 00169 WP 1997 4 3 ABXA9700275 1 19961120 A 5712 RIB DOUG DC9 DC933F 302207A WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, THE LEADING EDGE RIB INBOARD OF DE-ICE DUCT WAS FOUND CRACKED, NR AF-793. THE RIB WAS REPAIRED IAW DC9 SRM. 2 L 7 2 4F A6WE 1997040300170 19970403 00170 WP 1997 4 3 ABXA9700276 1 19961118 A 5720 SPLICE DOUG DC9 DC933F 302207A WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 41666 DURING C-CHECK, THE LEADING EDGE SKIN SPLICE OUTBOARD OF NR 6 TRACK WAS FOUND CRACKED, NR AF-796. THE RIB WAS REPAIRED IAW DC9 SRM. 2 L 7 2 4F A6WE 1997040300171 19970403 00171 WP 1997 4 3 ABXA9700277 1 19961125 A 5313 59114279 LONGERON DOUG DC9 DC933F 302207A WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, THE LONGERON AT STATION 980 AND 17 RIGHT WERE FOUND CRACKED, NR BF-622. THE LONGERON WAS REPLACED IAW D C-9 SRM. 2 L 7 2 4F A6WE 1997040300172 19970403 00172 WP 1997 4 3 ABXA9700278 1 19961203 A 5320 5913005504 FITTING DOUG DC9 DC933F 302207A WP CENTER FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, THE CENTER FUEL TANK OUTBOARD ATTACH FITTING WAS FOUND CORRODED, NR BF-399. THE FITTING WAS REPLACED IA W DC9 SRM. 2 L 7 2 4F A6WE 1997040300173 19970403 00173 WP 1997 4 3 ABXA9700279 1 19961203 A 5320 D04898 CUSP WEB DOUG DC9 DC933F 302207A WP BS 960 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, THE RIGHT CUSP WEB AT STATION 960 WAS FOUND CRACKED, NR BF-698. THE WEB REPLACED IAW DC9 SRM. 2 L 7 2 4F A6WE 1997040300174 19970403 00174 WP 1997 4 3 ABXA9700280 1 19961120 A 5320 D04989 CUSP WEB DOUG DC9 DC933F 302207A WP BS 775-794 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, THE RIGHT CUSP WEB FROM STATION 775 TO 794 WAS FOUND CORRODED, NR BF-495. THE WEB WAS REPAIRED IAW DC9 SRM. 2 L 7 2 4F A6WE 1997040300175 19970403 00175 WP 1997 4 3 ABXA9700281 1 19961203 A 5320 D04989 CUSP WEB DOUG DC9 DC933F 302207A WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, THE RIGHT CUSP WEB AT STATION 965 WAS FOUND CRACKED, NR BF-631. THE WEB WAS REPLACED IAW DC9 SRM. 2 L 7 2 4F A6WE 1997040300176 19970403 00176 WP 1997 4 3 ABXA9700282 1 19961125 A 5330 59114273 SKIN DOUG DC9 DC933F 302207A WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, FUSELAGE SKIN AT STATION 965 BELOW LONGERON 16 RIGHT WAS FOUND CRACKED, NR BF-665. THE SKIN WAS REPAIRE D IAW REA DC953-17291. 2 L 7 2 4F A6WE 1997040300177 19970403 00177 WP 1997 4 3 ABXA9700283 1 19961125 A 5330 59114273 SKIN DOUG DC9 DC933F 302207A WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, FUSELAGE SKIN AT STATION 965 BELOW LONGERON 16 RIGHT WAS FOUND CRACKED, NR BF-495. THE SKIN WAS REPAIRE D IAW REA DC953-17291. 2 L 7 2 4F A6WE 1997040300178 19970403 00178 WP 1997 4 3 ABXA9700284 1 19961125 A 5320 4911383501 FITTING DOUG DC9 DC933F 302207A WP BS 980 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, A FRAME FITTING AT STATION 980 RIGHT CUSP WAS FOUND CORRODED, NR BF-598. THE FITTING WAS REPLACED IAW D C9 SRM. 2 L 7 2 4F A6WE 1997040300179 19970403 00179 WP 1997 4 3 ABXA9700285 1 19961202 A 5320 99581881 SUPPORT DOUG DC9 DC933F 302207A WP BS 980 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 48291 DURING C-CHECK, A FLOOR SUPPORT AT STATION 980 RBL 22 WAS FOUND CORRODED, NR BF-692. THE SUPPORT WAS REPAIRED IAW DC9 S RM. 2 L 7 2 4F A6WE 1997040300180 19970403 00180 WP 1997 4 3 ABXA9700286 1 19961126 A 5320 9958238671 FORMER DOUG DC9 DC933F 302207A WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, A FORMER AT STATION 980 BELOW LONGERON 14 RIGHT WAS FOUND CRACKED, NR BF-601. THE FORMER WAS REPLACED I AW DC9 SRM. 2 L 7 2 4F A6WE 1997040300429 19970403 00429 WP 1997 4 3 ABXA9700287 1 19960810 A 5755 5910055516 SPOILER DOUG DC9 DC941 302207N WP RT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 RIGHT SPOILER LOWER SURFACE CORRODED. REPLACED HONEYCOMB CORE DOUBLERS AND SKIN. 2 L 7 2 4F A6WE 1997040300430 19970403 00430 WP 1997 4 3 ABXA9700288 1 19960810 A 5755 5910055516 SPOILER DOUG DC9 DC941 302207N WP LT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 LEFT WING SPOILER LOWER SURFACE CORRODED. REPLACED HONEYCOMB CORE, DOUBLERS AND SKIN. 2 L 7 2 4F A6WE 1997040300432 19970403 00432 WP 1997 4 3 ABXA9700291 1 19961123 A 5320 99577375 INTERCOSTAL DOUG DC9 DC933F 302207A WP BS 980-996 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, AN INTERCOSTAL STA 980 TO 996 BELOW LONG 124RT WAS FOUND CORRODED. THE INTERCOSTAL WAS REPLACED IAW DC SRM. 2 L 7 2 4F A6WE 1997040300433 19970403 00433 WP 1997 4 3 ABXA9700292 1 19961125 A 5412 9912243 BULKHEAD CLIP DOUG DC9 DC933F 302207A WP LT PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, A CLIP ON THE LT PYLON BULKHEAD STA 965, WAS FOUND CRACKED. THE CLIP WAS REPLACED IAW DC SRM. 2 L 7 2 4F A6WE 1997040300434 19970403 00434 WP 1997 4 3 ABXA9700293 1 19961120 A 5320 WEB DOUG DC9 DC933F 302207A WP BS 443 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, THE WEB AT STA 443 AT LONG 14LT WAS FOUND CORRODED. THE WEB WAS REPAIRED IAW DC SRM. 2 L 7 2 4F A6WE 1997040300435 19970403 00435 WP 1997 4 3 ABXA9700294 1 19961125 A 5320 995823870 FORMER DOUG DC9 DC933F 302207A WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, THE FORMER AT STA 980 AT LONG 16LT WAS FOUND CRACKED. THE FORMER WAS REPLACED IAW DC SRM. 2 L 7 2 4F A6WE 1997040300436 19970403 00436 WP 1997 4 3 ABXA9700295 1 19961125 A 5311 FRAME DOUG DC9 DC933F 302207A WP BS 980 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, THE FRAME AT STA 980 LONG 18RT TO 6RT WAS FOUND CORRODED. THE FRAME WAS REPLACED IAW DC9 SRM. 2 L 7 2 4F A6WE 1997040300437 19970403 00437 WP 1997 4 3 ABXA9700296 1 19961125 A 5313 2777922 LONGERON DOUG DC9 DC933F 302207A WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, THE LONGERON AT STA 980 LONG 17LT, WAS FOUND CRACKED. THE LONGERON WAS REPLACED IAW DC9 SRM. 2 L 7 2 4F A6WE 1997040300438 19970403 00438 WP 1997 4 3 ABXA9700297 1 19961120 A 5313 2777922 LONGERON DOUG DC9 DC933F 302207A WP BS 294 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, THE LONGERON AT STA 294 LONG 17RT, WAS FOUND CRACKED. THE LONGERON WAS REPLACED IAW DC9 SRM. 2 L 7 2 4F A6WE 1997040300439 19970403 00439 WP 1997 4 3 ABXA9700298 1 19961120 A 5313 2777922 LONGERON DOUG DC9 DC933F 302207A WP BS 313 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, THE LONGERON AT STA 313 LONG 17RT WAS FOUND CRACKED. THE LONGERON WAS REPLACED IAW DC9 SRM. 2 L 7 2 4F A6WE 1997040300440 19970403 00440 WP 1997 4 3 ABXA9700299 1 19961119 A 5313 2777922 LONGERON DOUG DC9 DC933F 302207A WP BS 408 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, THE LONGERON AT STA 408 LONG 17RT, WAS FOUND CRACKED. THE LONGERON WAS REPLACED IAW DC9 SRM. 2 L 7 2 4F A6WE 1997040300441 19970403 00441 WP 1997 4 3 ABXA9700300 1 19961119 A 5313 2777922 LONGERON DOUG DC9 DC933F 302207A WP BS 389 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, THE LONGERON AT STA 389 LONG 17RT, WAS FOUND CRACKED. THE LONGERON WAS REPLACED IAW DC9 SRM. 2 L 7 2 4F A6WE 1997040300442 19970403 00442 WP 1997 4 3 ABXA9700303 1 19961114 A 5320 99101401 CUSP DOUG DC9 DC915 3022036 WP BS 218 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 927AX 45717 DURING C-CHECK, FOUND LEFT CUSP WEB, CRACKED AT STA 218 (AD 92-22-08). REPLACED CUSP WEB IAW DC 9 SRM 51-30-2, 51-30-5, ABX REA D953-17208-MR. 2 L 7 2 4F A6WE 1997040300443 19970403 00443 WP 1997 4 3 ABXA9700304 1 19961114 A 5320 99101401 WEB DOUG DC9 DC915F 3022037 WP BS 237-256 CUT OUT A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 927AX 45717 DURING C-CHECK, FOUND A CUTOUT ON LEFT CUSP WEB BETWEEN STA 237-256. REPAIRED IAW ABX READ953-17208-MR. 2 L 7 2 4F A6WE 1997040300444 19970403 00444 WP 1997 4 3 ABXA9700305 1 19961112 A 5311 99582101 FRAME DOUG DC9 DC915 3022036 WP BS 642 MISDRILLED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 927AX 45717 DURING C-CHECK, FOUND FRAME STA 642 HAD A MISDRILLED HOLE. REPAIRED IAW REA D953-17177-MR. 2 L 7 2 4F A6WE 1997040300445 19970403 00445 WP 1997 4 3 ABXA9700306 1 19961106 A 5321 99100787 SUBFLOOR DOUG DC9 DC915 3022036 WP BS 208 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 927AX 45717 DURING C-CHECK, FOUND SUBFLOOR CRACKED AT STA 208 (AD 92-22-08). REPAIRED IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 1997040300446 19970403 00446 WP 1997 4 3 ABXA9700307 1 19961107 A 5752 59100512 TAB DOUG DC9 DC915 3022036 WP RT AILERON DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 927AX 45717 DURING C-CHECK, FOUND RIGHT AILERON TRIM TAB DELAMINATED AND DENTED (AD 92-22-08). REPLACED IAW DC-9 M/M 27-10-5. 2 L 7 2 4F A6WE 1997040300447 19970403 00447 WP 1997 4 3 ABXA9700309 1 19961106 A 5311 99582101 FRAME DOUG DC9 DC915F 3022037 WP BS 642 MISDRILLED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 927AX 45717 DURING C-CHECK, FOUND FRAME STA 642 HAD A MISDRILLED HOLE. REPAIRED IAW REA D953-17177-MR. 2 L 7 2 4F A6WE 1997040300448 19970403 00448 WP 1997 4 3 ABXA9700310 1 19961106 A 5320 99101401 WEB DOUG DC9 DC915 3022036 WP BS 237-256 CUT A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 927AX 45717 DURING C-CHECK, FOUND A CUTOUT ON LEFT CUSP WEB, BETWEEN STA 237-256. REPAIRED IAW ABX REA D953-17208-MR. 2 L 7 2 4F A6WE 1997040300449 19970403 00449 WP 1997 4 3 ABXA9700311 1 19961104 A 5312 59174637 BLKHD DOOR JAMB DOUG DC9 DC941 302207N WP AFT FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 970AX 47494 DURING C-CHECK, THE AFT PRESSURE BULKHEAD LT VENTRAL DOOR JAMB CORNER WAS FOUND CRACKED BEYOND A PREVIOUS STOP DRILL. R EPAIRED IAW REA D953-17172SB. 2 L 7 2 4F A6WE 1997040300450 19970403 00450 WP 1997 4 3 ABXA9700312 1 19961101 A 5753 5910043507 VANE DOUG DC9 DC941 302207N WP LT TE FLAP DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 970AX 47494 DURING C-CHECK, THE LEFT FLAP OUTBOARD FIXED VANE WAS FOUND DELAMINATED. REPLACED OUTBOARD FIXED VANE IAW DC-9 MM 27-51 -3. 2 L 7 2 4F A6WE 1997040300451 19970403 00451 WP 1997 4 3 ABXA9700313 1 19961101 A 5752 5910047501 TAB DOUG DC9 DC941 302207N WP LT AILERON DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 970AX 47494 DURING C-CHECK, THE LEFT AILERON CONTROL TAB WAS FOUND DELAMINATED. REPLACED AILERON CONTROL TAB IAW DC-9 M.M 27-10-2. 2 L 7 2 4F A6WE 1997040300452 19970403 00452 WP 1997 4 3 ABXA9700314 1 19961104 A 5320 991150985 TEE CAP DOUG DC9 DC941 302207N WP BS 110 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 970AX 47494 DURING C-CHECK, THE STA 110 TEE CAP WAS FOUND CORRODED AT LONGERON 25RT. REPAIRED IAW REA D953-17189. 2 L 7 2 4F A6WE 1997040300453 19970403 00453 WP 1997 4 3 ABXA9700315 1 19961104 A 5311 99118778 FRAME DOUG DC9 DC941 302207N WP BS 1231 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 970AX 47494 DURING C-CHECK, THE STA 1231 FRAME WAS FOUND CRACKED AT LONGERON 2 RT. REPAIRED IAW DC-9 SRM 51-10-2 AND 51-10-5. 2 L 7 2 4F A6WE 1997040300454 19970403 00454 WP 1997 4 3 ABXA9700316 1 19961104 A 5311 99118603 FRAME DOUG DC9 DC941 302207N WP BS 1185 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 970AX 47494 DURING C-CHECK, THE STA 1185 FRAME WAS FOUND CRACKED AT LONGERON 6RT. REPAIRED IAW SRM DWG NR K051-59. 2 L 7 2 4F A6WE 1997040300455 19970403 00455 WP 1997 4 3 ABXA9700317 1 19961104 A 5311 99118603 FRAME DOUG DC9 DC941 302207N WP BS 1185 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 970AX 47494 DURING C-CHECK, THE STA 1185 FRAME WAS FOUND CRACKED AT LONGERON 3 RT. REPAIRED IAW SSRM DWG NR K05159. 2 L 7 2 4F A6WE 1997040300456 19970403 00456 WP 1997 4 3 ABXA9700318 1 19961104 A 5312 99100733 BULKHEAD DOUG DC9 DC941 302207N WP BS 76 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 970AX 47494 DURING C-CHECK, THE BULKHEAD AT STA 76 WAS FOUND CRACKED NEXT TO RT CUSP. REPAIRED IAW REA D953-17160. 2 L 7 2 4F A6WE 1997040300457 19970403 00457 WP 1997 4 3 ABXA9700319 1 19961104 A 5312 5910130273 BULKHEAD DOUG DC9 DC941 302207N WP BS 1072 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 970AX 47494 DURING C-CHECK, THE BULKHEAD AT STA 1072 WAS FOUND CRACKED ON THE RT SIDE OF THE DOOR JAMB 24 FROM FLOOR. REPAIRED IAW REA D953-17165MR. 2 L 7 2 4F A6WE 1997040300458 19970403 00458 WP 1997 4 3 ABXA9700320 1 19961104 A 5312 9912243813 BULKHEAD DOUG DC9 DC941 302207N WP BS 1041 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 970AX 47494 DURING C-CHECK, THE BULKHEAD AT STA 1041 WAS FOUND CRACKED ON THE RT SIDE AT ENGINE MOUNT SPAR. REPAIRED IAW DC-9 SRM 5 1-30-1, 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1997040300459 19970403 00459 WP 1997 4 3 ABXA9700321 1 19961104 A 5400 59132628 ANGLE DOUG DC9 DC941 302207N WP BS 1056 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 970AX DURING C-CHECK, THE RT PYLON LOWER ATTACH ANGLE WAS FOUND CRACKED AT STA 1056. REPAIRED IAW DC-9 SRM 54-04. 2 L 7 2 4F A6WE 1997040300460 19970403 00460 WP 1997 4 3 ABXA9700322 1 19961104 A 7830 5958782503 DRIVER LINK DOUG DC9 DC941 302207N WP RT ENGINE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 970AX 47494 DURING C-CHECK, THE RT ENGINE THRUST REVERSER UPPER OUTBOARD DRIVER LINK WAS FOUND CRACKED. REPLACED DRIVER LINK IAW DC -9 M.M. 78-31-5. 2 L 7 2 4F A6WE 1997040300461 19970403 00461 WP 1997 4 3 ABXA9700323 1 19961104 A 5312 5910130279 BULKHEAD WEB DOUG DC9 DC941 302207N WP AFT FUSELAGE DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 970AX 47494 DURING C-CHECK, THE AFT PRESSURE BULKHEAD WEB WAS FOUND DAMAGED AT LONGERON 271LT. REPAIRED IAW REA D953-17185-MR. 2 L 7 2 4F A6WE 1997040300462 19970403 00462 WP 1997 4 3 ABXA9700324 1 19961016 A 5320 5912995503 DOOR JAMB DOUG DC9 DC931 3022065 WP EMERGENCY EXIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 929AX 45874 DURING C-CHECK, THE RIGHT FORWARD OVERWING EXIT DOOR JAMB PAN WAS FOUND CRACKED AT THE UPPER STOP. REPAIRED IAW DC9 SRM . 2 L 7 2 4F A6WE 1997040300464 19970403 00464 WP 1997 4 3 ABXA9700325 1 19961016 A 5312 591016331 BULKHEAD FTG DOUG DC9 DC931 3022065 WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 929AX 45874 DURING C-CHECK, THE AFT PRESSURE BULKHEAD AFT RADICAL 16 WAS FOUND CRACKED ON THE INBOARD END. REPLACED IAW DC9 SRM. 2 L 7 2 4F A6WE 1997040300465 19970403 00465 WP 1997 4 3 ABXA9700326 1 19961016 A 5320 39147241 FITTING DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 929AX 45874 DURING C-CHECK, THE LEFT INBOARD BONDED PANEL TO FUSELAGE ATTACH FITTING, WAS FOUND CRACKED. REPLACED IAW DC9 SRM. 2 L 7 2 4F A6WE 1997040300466 19970403 00466 WP 1997 4 3 ABXA9700327 1 19961016 A 5347 S29149137075 SEAT TRACK DOUG DC9 DC931 3022065 WP BS 163-167 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 929AX 45874 DURING C-CHECK, THE SEAT TRACK AT LBL 22.0 STA 163 TO 167 WAS FOUND CRACKED. REPLACED IAW DC9 SRM. 2 L 7 2 4F A6WE 1997040300467 19970403 00467 WP 1997 4 3 ABXA9700328 1 19961016 A 5313 4912261501 LONGERON DOUG DC9 DC931 3022065 WP BS 937 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 929AX 45874 DURING C-CHECK, LONGERON 17 LT AT FUS STA 937, WAS FOUND CRACKED. REPAIRED IAW DC9 SRM. 2 L 7 2 4F A6WE 1997040300468 19970403 00468 WP 1997 4 3 ABXA9700329 1 19961016 A 5320 991967315 CLIP DOUG DC9 DC931 3022065 WP BS 718 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 929AX 45874 DURING C-CHECK, THE FUSELAGE FRAME TO LONGERON ATTACH CLIP WAS CRACKED AT STA 718 LONGERON 15RT. REPLACED IAW DC9 SRM. 2 L 7 2 4F A6WE 1997040300469 19970403 00469 WP 1997 4 3 ABXA9700330 1 19961016 A 5311 991185812 FRAME DOUG DC9 DC931 3022065 WP BS 1074 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 929AX 45874 DURING C-CHECK, THE FUSELAGE FRAME WAS FOUND CRACKED AT STA 1074 LONGERON 13RT. REPAIRED IAW DC9 SRM. 2 L 7 2 4F A6WE 1997040300470 19970403 00470 WP 1997 4 3 ABXA9700331 1 19961016 A 5320 99100733 PRESSURE PANEL DOUG DC9 DC931 3022065 WP BS 81 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 929AX 45874 DURING C-CHECK, THE UPPER PRESSURE PANEL IN THE NOSE WHEEL WELL WAS FOUND CRACKED AT STA 81. REPAIRED IAW REA D953-1685 6. 2 L 7 2 4F A6WE 1997040300471 19970403 00471 WP 1997 4 3 ABXA9700332 1 19961016 A 5330 5910228212 SKIN DOUG DC9 DC931 3022065 WP BS 1132 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 929AX 45874 DURING C-CHECK, THE FUSELAGE SKIN WAS FOUND CRACKED AT STA 1132 LONGERON 17RT. REPAIRED IAW DC9 SRM. 2 L 7 2 4F A6WE 1997040300472 19970403 00472 WP 1997 4 3 ABXA9700333 1 19961016 A 5400 99122461 CLIP DOUG DC9 DC931 3022065 WP RT PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 929AX 45874 DURING C-CHECK, THE RIGHT PYLON UPPER SPAR TO WEB ATTACH CLIP WAS CRACKED AT STA 1038. REPAIRED IAW DC9 SRM. 2 L 7 2 4F A6WE 1997040300473 19970403 00473 WP 1997 4 3 ABXA9700334 1 19961016 A 5400 591771736 ANGLE DOUG DC9 DC931 3022065 WP RT PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 929AX 45874 DURING C-CHECK, THE RT UPPER PYLON SPAR CAP TO FRAME ATTACH ANGLE WAS FOUND CRACKED, AT STA 1038. REPAIRED IAW DC9 SRM. 2 L 7 2 4F A6WE 1997040300474 19970403 00474 WP 1997 4 3 ABXA9700335 1 19961016 A 5320 6025767075 SUPPORT DOUG DC9 DC931 3022065 WP BS 205 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 929AX 45874 DURING C-CHECK, A FLOOR SUPPORT WAS FOUND CRACKED RBL 14 STA 205. REPAIRED IAW DC9 SRM. 2 L 7 2 4F A6WE 1997040300493 19970403 00493 WP 1997 4 3 ABXA9700354 1 19961218 A 5400 59132626 ANGLE DOUG DC9 DC941 302207N WP PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 DURING C CHECK, THE LOWER PYLON TO FUSELAGE ATTACH ANGLE WAS FOUND CRACKED. THE ANGLE WAS REPAIRED IAW DC9 SRM 54-04, F IG.10. 2 L 7 2 4F A6WE 1997040300494 19970403 00494 WP 1997 4 3 ABXA9700355 1 19961218 A 5311 99234091 FRAME DOUG DC9 DC941 302207N WP BS 737 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 DURING C-CHECK, WHILE ACCOMPLISHING AD 78-07-05, THE MAIN FRAME AT STA 737 LT WAS FOUND CRACKED. THE FRAME WAS REPAIRED IAW REA DC953-17522-MR. 2 L 7 2 4F A6WE 1997040300495 19970403 00495 WP 1997 4 3 ABXA9700356 1 19961218 A 5311 99234091 FRAME DOUG DC9 DC941 302207N WP BS 737 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 DURING C-CHECK, WHILE ACCOMPLISHING AD 78-07-05, THE MAIN FRAME AT STA 737 RT, WAS FOUND CRACKED. THE FRAME WAS REPAIR ED IAW REA DC953-17522-MR. 2 L 7 2 4F A6WE 1997040300496 19970403 00496 WP 1997 4 3 ABXA9700357 1 19961219 A 5347 53AA17STC SEAT TRACK DOUG DC9 DC941 302207N WP BS 195 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 DURING C-CHECK, THE SEAT TRACK AT STA 195RBL 44, WAS FOUND CORRODED. THE SEAT TRACK WAS REPAIRED IAW REA D953-17543-DE AND THE DC9 SRM. 51-30-1. 2 L 7 2 4F A6WE 1997040300497 19970403 00497 WP 1997 4 3 ABXA9700358 1 19961217 A 5320 49241802 ANGLE DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 DURING C-CHECK, THE VENTRAL STAIR RIGHT HINGE ATTACH ANGLE WAS FOUND CRACKED. THE ANGLE WAS REPLACED IAW DC9 SRM 51-10- 4. 2 L 7 2 4F A6WE 1997040300498 19970403 00498 WP 1997 4 3 ABXA9700359 1 19961219 A 5311 99234091 FRAME DOUG DC9 DC941 302207N WP BS 737 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 DURING C-CHECK, WHILE ACCOMPLISHING AD 78-07-05, THE MAIN FRAME AT STA 737 LEFT WAS FOUND CRACKED. THE FRAME WAS REPAIR ED IAW S/B 53-131 AND REA D953-17522-MR. 2 L 7 2 4F A6WE 1997040300499 19970403 00499 WP 1997 4 3 ABXA9700360 1 19961218 A 5400 9915595 DOUBLER DOUG DC9 DC941 302207N WP PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 DURING C-CHECK, THE ENGINE PYLON BULKHEAD DOUBLER WAS FOUND CRACKED. THE DOUBLER WAS REPLACED IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 1997040300500 19970403 00500 WP 1997 4 3 ABXA9700361 1 19961218 A 5753 5912168506 VANE DOUG DC9 DC941 302207N WP RT TE FLAP CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 DURING C-CHECK, THE FLAP FORWARD MOVEABLE VANE WAS FOUND CORRODED. THE VANE WAS REPLACED IAW DC-9 MM 27-51-1. 2 L 7 2 4F A6WE 1997040300501 19970403 00501 WP 1997 4 3 ABXA9700362 1 19961215 A 5347 S29149137075 SEAT TRACK DOUG DC9 DC941 302207N WP BS 190 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 4751 DURING C CHECK, THE SEAT TRACK AT STA 190 RBL 22 WAS FOUND CORRODED. THE TRACK WAS REPAIRED IAW DC-9 SRM 53-05, FIG. 4A . 2 L 7 2 4F A6WE 1997040300502 19970403 00502 WP 1997 4 3 ABXA9700363 1 19961219 A 5320 59174971 FITTING DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 DURING C-CHECK, THE AFT JACK PAD ATTACH FITTING WAS FOUND CORRODED. THE FITTING WAS REPLACED IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 1997040300503 19970403 00503 WP 1997 4 3 ABXA9700364 1 19961218 A 5753 5910040504 VANE DOUG DC9 DC941 302207N WP RT TE FLAP DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 DURING C-CHECK, THE FLAP AFT MOVEABLE VANE WAS FOUND DELAMINATED. THE VANE WAS REPLACED IAW DC-9 MM 27-51-2. 2 L 7 2 4F A6WE 1997040300504 19970403 00504 WP 1997 4 3 ABXA9700365 1 19961218 A 2710 5918125501 DAMPER CRANK DOUG DC9 DC941 302207N WP RT AILERON CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 DURING C-CHECK, THE AILERON DAMPER CRANK WAS FOUND CORRODED. THE DAMPER WAS REPLACED IAW DC-9 MM 27-10-4. 2 L 7 2 4F A6WE 1997040300505 19970403 00505 WP 1997 4 3 ABXA9700366 1 19961216 A 5752 5910051502 TAB DOUG DC9 DC941 302207N WP RT AILERON WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 DURING C-CHECK, THE AILERON TRIM TAB INBOARD HINGE WAS FOUND WORN. THE TRIM TAB WAS REPLACED IAW DC-9 MM 27-10-5. 2 L 7 2 4F A6WE 1997040300506 19970403 00506 WP 1997 4 3 ABXA9700367 1 19961214 A 5280 591055726 DEPRESSOR DOUG DC9 DC941 302207N WP RT MLG DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 DURING C-CHECK, THE MAIN LANDING GEAR OUTBOARD DOOR SEAL DEPRESSOR WAS FOUND CRACKED. THE DEPRESSOR WAS REPLACED IAW DC -9 SRM 51-30-2. 2 L 7 2 4F A6WE 1997040300507 19970403 00507 WP 1997 4 3 ABXA9700368 1 19961218 A 5320 536002 DOUBLER DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 DURING C-CHECK, THE FUSELAGE SKIN DOUBLER AT THE MAIN ENTRY DOOR WAS FOUND CRACKED. THE DOUBLER WAS REPLACED IAW DC-9 S RM 51-30-5. 2 L 7 2 4F A6WE 1997040300508 19970403 00508 WP 1997 4 3 ABXA9700369 1 19961216 A 5347 1989OE308 GUIDE RAIL DOUG DC9 DC941 302207N WP BS 218 GOUGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 DURING C-CHECK, THE GUIDE RAIL AT STA 218 LBL 45, WAS FOUND GOUGED. THE GUIDE RAIL WAS REPLACED IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997040300509 19970403 00509 WP 1997 4 3 ABXA9700370 1 19961217 A 5320 5956034507 ANGLE DOUG DC9 DC941 302207N WP BS 1041 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 DURING C CHECK, THE SEAT TRACK ATTACH ANGLE AT STA 1041 LONG 27 LT, WAS FOUND CRACKED. THE ANGLE WAS REPLACED IAW DC-9 SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 1997040300510 19970403 00510 WP 1997 4 3 ABXA9700371 1 19961216 A 5753 39208191 CARRIAGE DOUG DC9 DC941 302207N WP LT TE FLAP WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 DURING C-CHECK, THE FLAP CARRIAGE ASSEMBLY WAS FOUND WORN. THE CARRIAGE ASSEMBLY WAS REPLACED IAW DC-9 SUP MM 27-51-5. 2 L 7 2 4F A6WE 1997040300511 19970403 00511 WP 1997 4 3 ABXA9700372 1 19961216 A 7830 5958775185 TR FAIRING DOUG DC9 DC941 302207N WP NR 1 ENGINE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 DURING C-CHECK, THE UPPER THRUST REVERSER BUCKET FAIRING WAS FOUND CRACKED. THE FAIRING WAS REPLACED IAW DC-9 SRM 51-30 -2. 2 L 7 2 4F A6WE 1997040300512 19970403 00512 WP 1997 4 3 ABXA9700373 1 19961217 A 5400 99577487 ANGLE DOUG DC9 DC941 302207N WP NR 1 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 DURING C-CHECK, THE PYLON UPPER SPAR CAP ANGLE AT THE OUTBOARD END WAS FOUND CRACKED. THE ANGLE WAS REPLACED IAW REA D9 54-17521. 2 L 7 2 4F A6WE 1997040300513 19970403 00513 WP 1997 4 3 ABXA9700374 1 19961217 A 7830 99577487 TR FAIRING DOUG DC9 DC941 302207N WP NR 1 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 DURING C-CHECK, THE LOWER THRUST REVERSER BUCKET FAIRING WAS FOUND CRACKED. THE FAIRING WAS REPLACED IAW DC-9 SRM 51-30 -2. 2 L 7 2 4F A6WE 1997040300514 19970403 00514 WP 1997 4 3 ABXA9700375 1 19961217 A 5400 59132624 ANGLE DOUG DC9 DC941 302207N WP NR 2 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 DURING C-CHECK, THE PYLON UPPER FUSELAGE ATTACH ANGLE AT STA 1072, WAS FOUND CRACKED. THE ANGLE WAS REPAIRED IAW DC-9 S RM 54-04, FIG.10. 2 L 7 2 4F A6WE 1997040300515 19970403 00515 WP 1997 4 3 ABXA9700376 1 19961219 A 5330 591140659 SKIN DOUG DC9 DC941 302207N WP PAX DOORWAY DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47541 DURING C-CHECK, THE FUSELAGE SKIN ON THE AFT SIDE OF THE FWD ENTRY DOOR LOWER CORNER WAS FOUND DAMAGED. THE SKIN WAS RE PAIRED IAW REA D953-17518. 2 L 7 2 4F A6WE 1997040300516 19970403 00516 WP 1997 4 3 ABXA9700377 1 19961218 A 5400 995815961 ANGLE DOUG DC9 DC941 302207N WP NR 1 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 DURING C CHECK, THE LOWER PYLON TO FUSELAGE ATTACH ANGLE WAS FOUND CRACKED. THE ANGLE WAS REPAIRED IAW DC-9 SSRM DRAWIN G NR K-05683. 2 L 7 2 4F A6WE 1997040300517 19970403 00517 WP 1997 4 3 ABXA9700378 1 19961217 A 7110 5910306 COWL FRAME DOUG DC9 DC941 302207N WP NR 1 ENGINE GOUGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 DURING C-CHECK, THE UPPER COWL INBOARD LONGERON FRAME WAS FOUND GOUGED. THE COWL WAS REPAIRED IAW ABX DWG K05013. 2 L 7 2 4F A6WE 1997040300518 19970403 00518 WP 1997 4 3 ABXA9700379 1 19961219 A 7830 5958775505 TR BUCKET DOUG DC9 DC941 302207N WP NR 2 ENGINE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 DURING C-CHECK, THE LOWER THRUST REVERSER BUCKET WAS FOUND CRACKED. THE BUCKET WAS REPLACED IAW DC9 MM 78-30-2. 2 L 7 2 4F A6WE 1997040300519 19970403 00519 WP 1997 4 3 ABXA9700380 1 19961218 A 5400 59131626 ANGLE DOUG DC9 DC941 302207N WP NR 2 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 DURING C-CHECK, THE LOWER PYLON TO FUSELAGE ATTACH ANGLE WAS FOUND CRACKED. THE ANGLE WAS REPAIRED IAW DC9 SRM 54-04, F IG.10. 2 L 7 2 4F A6WE 1997040300520 19970403 00520 WP 1997 4 3 ABXA9700381 1 19961218 A 5311 99234091 FRAME DOUG DC9 DC941 302207N WP BS 737 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 DURING C-CHECK, WHILE ACCOMPLISHING AD 78-07-05, THE FUSELAGE MAIN FRAME AT STA 737LT WAS FOUND CRACKED. THE FRAME WAS REPAIRED IAW REA D953-17522-MR AND S/B 53-131. 2 L 7 2 4F A6WE 1997040300524 19970403 00524 WP 1997 4 3 ABXA9700386 1 19961022 A 5530 01249011 FITTING NIHON YS11 YS11A500 6310416 WP VERT STAB CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 915AX 2062 DURING C-CHECK INSPECTION, FOUND VERTICAL STABILIZER LEFT FORWARD ATTACH FITTING CORRODED. REMOVED FITTING, REPLACED BU SHING IAW YS-11 OHM 53-40-3, CLEANED CORROSION IAW YS-11 CCM 20-40-0, REINSTALLED FITTING IAW YS-11 M.M. 55-30-0. 2 L 7 2 4T A1PC 1997040300525 19970403 00525 WP 1997 4 3 ABXA9700388 1 19961017 A 5720 20012 BOLT NIHON YS11 YS11A500 6310416 WP RT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 915AX 2062 DURING C-CHECK INSPECTION, FOUND CORRODED BOLT AT RIGHT WING UPPER FUSELAGE TO WING ATTACH FITTING. REPLACED BOLT IAW Y S-11 M.M. 57-41-1. 2 L 7 2 4T A1PC 1997040300526 19970403 00526 WP 1997 4 3 ABXA9700389 1 19961017 A 5720 20012 BOLT NIHON YS11 YS11A500 6310416 WP LT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 915AX 2062 DURING C-CHECK INSPECTION, FOUND CORRODED BOLT AT LEFT WING UPPER FUSELAGE TO WING ATTACH FITTING. REPLACED BOLT IAW YS -11 M.M. 57-41-1. 2 L 7 2 4T A1PC 1997040300527 19970403 00527 WP 1997 4 3 ABXA9700390 1 19961101 A 5330 SKIN NIHON YS11 YS11A500 6310416 WP BS 9900 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 915AX 2062 DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN CRACKED AT FS 9900. REPAIRED IAW YS-11 SRM 53-2-2, IB, FIG. 2. 2 L 7 2 4T A1PC 1997040300528 19970403 00528 WP 1997 4 3 ABXA9700391 1 19961024 A 5315 FLOORBEAM NIHON YS11 YS11A500 6310416 WP BS 4200 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 915AX 2062 DURING C-CHECK INSPECTION, FOUND CORRODED FLOORBEAM AT STATION 4200. REPAIRED IAW ABX REA Y153-16864-MR. 2 L 7 2 4T A1PC 1997040300529 19970403 00529 WP 1997 4 3 ABXA9700392 1 19961025 A 5315 FLOORBEAM NIHON YS11 YS11 6310406 WP BS 5160 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 915AX 2062 DURING C-CHECK INSPECTION, FOUND CORRODED FLOORBEAM AT STATION 5160, LBL 11. REPAIRED IAW ABX REA Y153-16864-MR. 2 L 7 2 4T A1PC 1997040300530 19970403 00530 WP 1997 4 3 ABXA9700394 1 19961025 A 5315 FLOORBEAM NIHON YS11 YS11A500 6310416 WP BS 6120 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 915AX 2062 DURING C-CHECK INSPECTION, FOUND CORRODED FLOORBEAM AT STATION 6120, RBL 12 TO 25. REPAIRED IAW ABX REA Y153-16864-MR. 2 L 7 2 4T A1PC 1997040300531 19970403 00531 WP 1997 4 3 ABXA9700395 1 19961025 A 5315 FLOORBEAM NIHON YS11 YS11A500 6310416 WP BS 7080 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 915AX 2062 DURING C-CHECK INSPECTION, FOUND FLOORBEAM AT STATION 7080. REPAIRED IAW ABX REA Y153-16864-MR. 2 L 7 2 4T A1PC 1997040300532 19970403 00532 WP 1997 4 3 ABXA9700396 1 19961029 A 5315 FLOORBEAM NIHON YS11 YS11A500 6310416 WP BS 600 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 915AX 2062 DURING C-CHECK INSPECTION, FOUND CORRODED FLOORBEAM AT STATION 600, RBL 18 TO RBL 25. REPAIRED IAW ABX REA Y153-16864-M R. 2 L 7 2 4T A1PC 1997040300533 19970403 00533 WP 1997 4 3 ABXA9700397 1 19961029 A 5315 FLOORBEAM NIHON YS11 YS11A500 6310416 WP BS 600 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 915AX 2062 DURING C-CHECK INSPECTION, FOUND CORRODED FLOORBEAM AT STATION 600. REPAIRED IAW ABX REA Y153-16864-MR. 2 L 7 2 4T A1PC 1997040300534 19970403 00534 WP 1997 4 3 ABXA9700398 1 19961030 A 5315 FLOORBEAM NIHON YS11 YS11A500 6310416 WP BS 9180 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 915AX 2062 DURING C-CHECK INSPECTION, FOUND CORRODED FLOORBEAM AT STATION 9180, RBL 12 TO RBL 45. REPAIRED IAW ABX REA Y153-16864- MR. 2 L 7 2 4T A1PC 1997040300535 19970403 00535 WP 1997 4 3 ABXA9700399 1 19961030 A 5315 FLOORBEAM NIHON YS11 YS11A500 6310416 WP BS 5160 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 915AX 2062 DURING C-CHECK INSPECTION, FOUND CORRODED FLOORBEAM AT STATION +5160, RBL 22. REPAIRED IAW ABX REA Y153-16864-MR. 2 L 7 2 4T A1PC 1997040300536 19970403 00536 WP 1997 4 3 ABXA9700400 1 19961020 A 5315 FLOORBEAM NIHON YS11 YS11 6310406 WP BS 3720 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 915AX 2062 DURING C-CHECK INSPECTION, FOUND CORRODED FLOORBEAM, AT STATION 3720. REPAIRED IAW ABX REA Y153-16865-MR. 2 L 7 2 4T A1PC 1997040300537 19970403 00537 WP 1997 4 3 ABXA9700401 1 19961027 A 5315 FLOORBEAM NIHON YS11 YS11 6310406 WP BS 6600 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 915AX 2062 DURING C-CHECK INSPECTION, FOUND CORRODED FLOORBEAM, AT STATION 6600. REPAIRED IAW ABX REA Y153-16865-MR. 2 L 7 2 4T A1PC 1997040300538 19970403 00538 WP 1997 4 3 ABXA9700402 1 19961029 A 5315 FLOORBEAM NIHON YS11 YS11A500 6310416 WP BS 5640 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 915AX 2062 DURING C-CHECK INSPECTION, FOUND CORRODED FLOORBEAM, AT STATION 5640. REPAIRED IAW ABX REA Y153-16865-MR. 2 L 7 2 4T A1PC 1997040300539 19970403 00539 WP 1997 4 3 ABXA9700403 1 19961025 A 5315 FLOORBEAM NIHON YS11 YS11A500 6310416 WP BS 6120 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 915AX 2062 DURING C-CHECK INSPECTION, FOUND CORRODED FLOORBEAM AT STATION 6120, RBL 12 TO 25. REPAIRED IAW ABX REA Y153-16865-MR. 2 L 7 2 4T A1PC 1997040300540 19970403 00540 WP 1997 4 3 ABXA9700404 1 19961025 A 5315 FLOORBEAM NIHON YS11 YS11A500 6310416 WP BS 8280 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 915AX 2062 DURING C-CHECK INSPECTION, FOUND CORRODED FLOORBEAM, AT STATION -8280, RBL 37. REPAIRED IAW ABX REA Y153-16865-MR. 2 L 7 2 4T A1PC 1997040300541 19970403 00541 WP 1997 4 3 ABXA9700405 1 19961025 A 5315 FLOORBEAM NIHON YS11 YS11A500 6310416 WP BS 7080 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 915AX 2062 DURING C-CHECK INSPECTION, FOUND CORRODED FLOORBEAM, AT STATION 7080. REPAIRED IAW ABX REA Y153-16865-MR. 2 L 7 2 4T A1PC 1997040300542 19970403 00542 WP 1997 4 3 ABXA9700406 1 19961030 A 5315 FLOORBEAM NIHON YS11 YS11A500 6310416 WP BS 9180 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 915AX 2062 DURING C-CHECK INSPECTION, FOUND CORRODED FLOORBEAM AT STATION -9180, RBL 12 TO RBL. REPAIRED IAW ABX REA Y153-16865-MR . 2 L 7 2 4T A1PC 1997040300543 19970403 00543 WP 1997 4 3 ABXA9700407 1 19961024 A 5347 SEAT TRACK NIHON YS11 YS11A500 6310416 WP BS 3240-3720 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 915AX 2062 DURING C-CHECK INSPECTION, FOUND CORROSION ON LEFT SEAT TRACK STANDS BETWEEN STA 3240 AND 3720. REPAIRED IAW ABX REA Y1 53-16883-MR. 2 L 7 2 4T A1PC 1997040300544 19970403 00544 WP 1997 4 3 ABXA9700408 1 19961025 A 5347 SEAT TRACK NIHON YS11 YS11A500 6310416 WP BS 600-1080 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 915AX 2062 DURING C-CHECK INSPECTION, FOUND CORROSION ON LEFT SEAT TRACK STANDS BETWEEN STA -600 TO -1080. REPAIRED IAW ABX REA Y1 53-16883-MR. 2 L 7 2 4T A1PC 1997040300545 19970403 00545 WP 1997 4 3 ABXA9700409 1 19961024 A 5347 SEAT TRACK NIHON YS11 YS11A500 6310416 WP BS 1800-1320 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 915AX 2062 DURING C-CHECK INSPECTION, FOUND CORROSION ON RIGHT SEAT TRACK STANDS. REPAIRED IAW ABX REA Y153-16883-MR. 2 L 7 2 4T A1PC 1997040300546 19970403 00546 WP 1997 4 3 ABXA9700410 1 19961024 A 5347 SEAT TRACK NIHON YS11 YS11A500 6310416 WP BS 1800-2280 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 915AX 2062 DURING C-CHECK INSPECTION, FOUND CORROSION ON RIGHT SEAT TRACK STANDS BETWEEN STA 1800 TO 2280. REPAIRED IAW ABX REA Y1 53-16883-MR. 2 L 7 2 4T A1PC 1997040300547 19970403 00547 WP 1997 4 3 ABXA9700411 1 19961023 A 5347 SEAT TRACK NIHON YS11 YS11A500 6310416 WP BS 1320-1800 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 915AX 2062 DURING C-CHECK INSPECTION, FOUND CORROSION ON LEFT SEAT TRACK STANDS BETWEEN STA 1320 TO 1800. REPAIRED IAW ABX REA Y15 3-16883-MR. 2 L 7 2 4T A1PC 1997040300548 19970403 00548 WP 1997 4 3 ABXA9700412 1 19961023 A 5210 01357101 FRAME NIHON YS11 YS11A500 6310416 WP ENTRY DOOR DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 915AX 2062 DURING C-CHECK INSPECTION, FOUND ENTRY DOOR FORWARD LOWER CORNER DAMAGED. REPAIRED IAW ABX REA Y152-16886-MR. 2 L 7 2 4T A1PC 1997040300549 19970403 00549 WP 1997 4 3 ABXA9700413 1 19961025 A 3213 41200211 STRUT NIHON YS11 YS11A500 6310416 WP RT MLG CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 915AX 2062 DURING C-CHECK, FOUND RIGHT MAIN LANDING GEAR SHOCK STRUT CORRODED UNDER THE SERVICING PLACARD. REPAIRED IAW ABX REA Y1 32-16914-MR. 2 L 7 2 4T A1PC 1997040300550 19970403 00550 WP 1997 4 3 ABXA9700414 1 19961029 A 5320 JAMB NIHON YS11 YS11A500 6310416 WP PAX DOOR CUT A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 915AX 2062 DURING C-CHECK INSPECTION, FOUND A CUTOUT IN THE FORWARD ENTRY DOOR LOWER JAMB AND JAMB DOUBLER. REPAIRED IAW ABX REA Y 153-16926-MR. 2 L 7 2 4T A1PC 1997040300551 19970403 00551 WP 1997 4 3 ABXA9700415 1 19961029 A 5320 JAMB NIHON YS11 YS11A500 6310416 WP PAX DOOR CUT A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 915AX 2062 DURING C-CHECK INSPECTION, FOUND A CUTOUT IN THE FORWARD ENTRY DOOR LOWER JAMB AND JAMB DOUBLER. REPAIRED IAW ABX REA Y 153-16926-MR. 2 L 7 2 4T A1PC 1997040300552 19970403 00552 WP 1997 4 3 ABXA9700416 1 19961029 A 5320 JAMB NIHON YS11 YS11A500 6310416 WP PAX DOOR CUT A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 915AX 2062 DURING C-CHECK INSPECTION, FOUND A CUTOUT IN THE FORWARD ENTRY DOOR LOWER JAMB AND JAMB DOUBLER. REPAIRED IAW ABX REA Y 153-16926-MR. 2 L 7 2 4T A1PC 1997040300553 19970403 00553 WP 1997 4 3 ABXA9700417 1 19961009 A 7120 0118212911 MOUNT NIHON YS11 YS11A500 6310416 WP LT ENGINE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 914AX 2056 DURING B-CHECK, THE LEFT ENGINE INBOARD LOWER SUB MOUNT WAS FOUND CORRODED. THE MOUNT WAS REPLACED IAW YS-11 SRM. 2 L 7 2 4T A1PC 1997040300554 19970403 00554 WP 1997 4 3 ABXA9700418 1 19961009 A 7120 0118211901 MOUNT NIHON YS11 YS11A500 6310416 WP LT ENGINE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 914AX 2056 DURING B-CHECK, THE LEFT ENGINE OUTBOARD LOWER SUB MOUNT WAS FOUND CORRODED. THE MOUNT WAS REPLACED IAW YS-11 SRM. 2 L 7 2 4T A1PC 1997040300555 19970403 00555 WP 1997 4 3 ABXA9700419 1 19961023 A 5752 5642831502 TAB DOUG DC8 DC861 3021952 WP RT AILERON DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 851AX 45940 DURING OFF WING INSPECTION, FOUND TAB DELAMINATED. OVERHAULED AILERON CONTROL TAB IAW T.P.S. 1001, REV.E, AND DAC D.W.G . 5642831. PERFORMED WEIGHT AND BALANCE IAW DC-8 SRM 51-4-2. 2 L 7 4 4F 4A25 1997040300557 19970403 00557 WP 1997 4 3 ABXA9700421 1 19961211 A 2750 57511521 DRIVE LINK DOUG DC8 DC861 3021952 WP LT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 847AX 46031 DURING COMPLIANCE OF A.D.88-10-07, FOUND LEFT INBOARD FLAP DRIVE LINK CRACKED AT POINT J. REPLACED LEFT INBOARD FLAP DR IVE LINK IAW DC-8 M.M. 27-51-4. 2 L 7 4 4F 4A25 1997040300558 19970403 00558 WP 1997 4 3 ABXA9700422 1 19961218 A 5753 39208192 CARRIAGE DOUG DC9 DC941 302207N WP RT TE FLAP WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 DURING C-CHECK, THE FLAP CARRIAGE ROLLERS WERE FOUND WORN. THE CARRIAGE WAS REPLACED IAW DC9 SUP MM 27-51-5. 2 L 7 2 4F A6WE 1997040300559 19970403 00559 WP 1997 4 3 ABXA9700423 1 19960716 A 5312 591013013 BULKHEAD DR JAMB DOUG DC9 DC941 302207N WP BS 1072 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 957AX 47759 DURING C-CHECK, FOUND A RADIAL CRACK IN RIGHT UPPER CORNER OF APB VENTRAL DOOR JAMB. REPAIRED IAW ABX REA D953-15626-MR . 2 L 7 2 4F A6WE 1997040300560 19970403 00560 WP 1997 4 3 ABXA9700424 1 19960716 A 5512 39180041 SKIN DOUG DC9 DC941 302207N WP LT HORIZ STAB CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 957AX 47759 DURING C-CHECK, FOUND CORROSION ON LEFT HORIZONTAL STABILIZER UPPER SKIN ABOVE THE REAR SPAR. REPAIRED IAW ABX REA D955 -15636-MR. 2 L 7 2 4F A6WE 1997040300561 19970403 00561 WP 1997 4 3 ABXA9700425 1 19960712 A 5320 5956030 SUPPORT DOUG DC9 DC941 302207N WP BS 351 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 957AX 47759 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND FLOOR SUPPORT CRACKED AT STA 351. REPAIRED IAW ABX DRAWING K-0501 8. 2 L 7 2 4F A6WE 1997040300861 19970403 00861 WP 1997 4 3 TWAA9730001 1 19961206 A 5312 BULKHEAD CAP LKHEED 1011 10113851 5265010 WP BS 229 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 31023 193B1080 LAX - DURING C-CHECK, FOUND .4375 INCH CRACK IN BULKHEAD LOWER CAP THROUGH HORIZONTAL FLANGE AND UP VERTICAL FLANGE, FS 229, RBL 42. STOP DRILLED CRACK AND INSTALLED DOUBLER PER LOCKHEED DWG NR 1642621. 2 L 7 3 4F A23WE 1997040300862 19970403 00862 WP 1997 4 3 TWAA9730002 1 19961213 A 5312 BULKHEAD LKHEED 1011 10113851 5265010 WP CANTED BLKHD CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 11006 193B1018 LAX - DURING C-CHECK, FOUND A FOUR INCH CRACK IN CANTED PRESSURE BULKHEAD HYDRAULIC COMPARTMENT, LBL 10.0. REPAIRED CAN TED PRESSURE BULKHEAD PER LOCKHEED DRAWING NR 7622-385. (M) 2 L 7 3 4F A23WE 1997040700003 19970407 00003 WP 1997 4 7 ABXA9700308 1 19961106 A 5753 5910041504 VANE DOUG DC9 DC915F 3022037 WP RT TE FLAP DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 927AX 45717 DURING C-CHECK, FOUND RIGHT FLAP INBOARD FIXED VANE DELAMINATED (AD 92-22-08). REPLACED IAW DC-9 M/M 27-51-3. 2 L 7 2 4F A6WE 1997041000110 19970410 00110 EU 1997 4 10 97ZZZX1401 1 19961221 A 2760 CONNECTOR BAG BAE146 BAE146200A 1500266 EU RT SPOILER DIRTY A A6WA O OTHER P NO WARNING INDICATION TX TAXI/GRND HDL 1 GL 31 183US E2043 LAX - FLT 676 - RT ROLL SPOILER DOES NOT INDICATE ROLL. VISUAL CHECK INDICATES NORMAL SPOILER OPERATION. CLEANED RT RO LL SPOILER POTENTIOMETER CANNON PLUG, OP CKS GOOD. 2 H 7 4 4F RT A49EU 1997041000121 19970410 00121 WP 1997 4 10 IXXA9700032 1 19960319 A 5320 9751649 PRESSURE PANEL DOUG DC8 DC863 302198A WP MLG WW CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 869BX 2249 46035 DURING UNSCHEDULED MAINTENANCE VISIT, BOTH PRESSURE PANELS AT FUSELAGE STATION 680, LEFT AND RIGHT, WERE FOUND CRACKED. BOTH PRESSURE PANELS WERE REPLACED WITH NEW PANELS IN ACCORDANCE WITH THE DOUGLAS SRM, 51-1-12, 51-1-8, 51-1-16, 51-3-0 , 51-1-21 AND 51-1-20D. 2 L 7 4 4F 4A25 1997041000202 19970410 00202 WP 1997 4 10 ABXA9700472 1 19960924 A 5320 5917579237 DOOR JAMB DOUG DC9 DC932 3022066 WP BS 996 NOT TRIMMED A ABXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 902AX 47426 DURING C-CHECK, AFT VENTRAL DOOR LOWER JAMB WEBS WERE FOUND TO HAVE A PRIOR TRIM OUT ALONG AFT EDGE. ALSO, DURING COMPL IANCE WITH AD 85-01-02. REPAIRED IAW ABX REA D953-16420-MR. 2 L 7 2 4F A6WE 1997041000203 19970410 00203 WP 1997 4 10 ABXA9700473 1 19960916 A 5320 995823851 FORMER DOUG DC9 DC932 3022066 WP BS 980 DEFECTIVE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 DURING C-CHECK, THE FOOT OF THE FORMER AT STA 980 WAS REMOVED. REPAIRED IAW ABX REA D953-16348-MR. 2 L 7 2 4F A6WE 1997041000204 19970410 00204 WP 1997 4 10 ABXA9700474 1 19960916 A 5315 991224259 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 965 DRILLED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 DURING C-CHECK, FOUND A MISDRILLED HOLE IN UPPER CAP OF FLOORBEAM AT STA 965. REPAIRED IAW ABX REA D953-16391-MR. 2 L 7 2 4F A6WE 1997041000205 19970410 00205 WP 1997 4 10 ABXA9700457 1 19961016 A 5753 49165571 FITTING DOUG DC9 DC931 3022065 WP LT TE FLAP VANE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 929AX 45874 DURING C-CHECK, THE LEFT WING MOVEABLE VANE AFT ATTACH FITTING WAS FOUND CRACKED, NR WC-800. REPLACED ATTACH FITTING IA W DC9 OHM 27-50-2. 2 L 7 2 4F A6WE 1997041000206 19970410 00206 WP 1997 4 10 ABXA9700458 1 19961016 A 5400 59132627 ANGLE DOUG DC9 DC931 3022065 WP LT PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 929AX 45874 DURING C-CHECK, THE LEFT UPPER AFT PYLON ATTACH ANGLE WAS FOUND CRACKED NR WC-855. REPAIRED ATTACH ANGLE IAW DC9 SRM 51 -30-1. 2 L 7 2 4F A6WE 1997041000207 19970410 00207 WP 1997 4 10 ABXA9700459 1 19961121 A 5522 5910411544 SKIN DOUG DC9 DC941 302207N WP RT ELEVATOR DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 960AX 47762 RIGHT ELEVATOR UPPER SKIN DELAMINATED. REPLACED AND BONDED SKINS. 2 L 7 2 4F A6WE 1997041000208 19970410 00208 WP 1997 4 10 ABXA9700460 1 19960812 A 3231 NAS130425D BOLT DOUG DC9 DC932 3022066 WP RT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 989AX 47314 DURING COMPLIANCE OF AD 91-22-07, ASB 32-244 FOUND RIGHT MLG OUTBOARD DOOR LINKAGE ARM WORN. REPLACED RIGHT MLG OUTBOAR D DOOR LINKAGE ARM BOLT IAW DC-9 O/H MANUAL CHAPTER 32. 2 L 7 2 4F A6WE 1997041000209 19970410 00209 WP 1997 4 10 ABXA9700461 1 19961005 A 3231 NAS10420 BOLT DOUG DC9 DC941 302207N WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 955AX 47619 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244 FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR LINKAGE LOOSE/WORN AT LINKAGE RO DS PIVOT POINT. REPLACED WORN BOLT IAW DC-9 MM CHAPTER 20. 2 L 7 2 4F A6WE 1997041000210 19970410 00210 WP 1997 4 10 ABXA9700462 1 19960923 A 5523 5910413503 TAB DOUG DC9 DC933F 302207A WP ELEVATOR DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 934AX 47462 DURING C-CHECK, AN ELEVATOR CONTROL TAB WAS FOUND DELAMINATED. REPLACED IAW DC-9 MM 27-30-3. 2 L 7 2 4F A6WE 1997041000211 19970410 00211 WP 1997 4 10 ABXA9700463 1 19960916 A 5752 5910051501 TAB DOUG DC9 DC933F 302207A WP LT AILERON DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 934AX 47462 DURING C-CHECK, AN AILERON TRIM TAB WAS FOUND DELAMINATED. REPLACED IAW DC-9 MM 27-10-5. 2 L 7 2 4F A6WE 1997041000212 19970410 00212 WP 1997 4 10 ABXA9700464 1 19960920 A 5320 59258781 FITTING DOUG DC9 DC933F 302207A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 934AX 47462 DURING C-CHECK, AN END FITTING WAS FOUND TO BE ELONGATED AND CORRODED. REPAIRED IAW REA D953-16455-MR. 2 L 7 2 4F A6WE 1997041000213 19970410 00213 WP 1997 4 10 ABXA9700465 1 19960920 A 5311 9921189501 FRAME DOUG DC9 DC933F 302207A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 934AX 47462 DURING C-CHECK, CORROSION WAS FOUND ON FUSELAGE FRAME 351 UPPER CAP AT LONGERON 24 LEFT. REPAIRED IAW REA D953-16412-MR . 2 L 7 2 4F A6WE 1997041000214 19970410 00214 WP 1997 4 10 ABXA9700466 1 19960921 A 7120 5923937501 ENGINE MOUNT DOUG DC9 DC933F 302207A WP RT ENGINE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 934AX 47462 DURING C-CHECK, THE RIGHT HAND FORWARD ENGINE MOUNTS, BEAVERTAIL, WERE FOUND TO BE CORRODED. REPAIRED IAW REA D953-1645 4-MR. 2 L 7 2 4F A6WE 1997041000215 19970410 00215 WP 1997 4 10 ABXA9700467 1 19960927 A 5315 99223971 FLOORBEAM DOUG DC9 DC933F 302207A WP BS 917 DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 934AX 47462 DURING C-CHECK, THE AFT FLANGE OF THE FLOORBEAM AT STA 917 WAS FOUND TO BE GOUGED AND WORN. REPAIRED IAW REA D953-16470 -MR. 2 L 7 2 4F A6WE 1997041000216 19970410 00216 WP 1997 4 10 ABXA9700468 1 19960924 A 5330 59259913 SKIN DOUG DC9 DC933F 302207A WP BS 975 DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 934AX 47462 DURING C-CHECK, AN EXISTING CLASS TWO REPAIR WAS REMOVED FROM THE FUSELAGE SKIN AT STA 975 LONG 20 AND 21 RIGHT. REPAIR ED IAW REA D953-16442-MR. 2 L 7 2 4F A6WE 1997041000218 19970410 00218 WP 1997 4 10 ABXA9700470 1 19960712 A 5320 5956030 FLOOR SUPPORT DOUG DC9 DC941 302207N WP BS 408 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 957AX 47759 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND FLOOR SUPPORT CRACKED AT STA 408. REPAIRED IAW ABX DRAWING K-0501 8. 2 L 7 2 4F A6WE 1997041000219 19970410 00219 WP 1997 4 10 ABXA9700471 1 19960711 A 3231 S24312157A016 BUSHING DOUG DC9 DC941 302207N WP LT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 957AX 47759 DURING C-CHECK AND COMPLIANCE WITH AD 91-22-07, FOUND LEFT FLYING DOOR TO DOUBLE ROD ATTACH LINK HAS EXCESSIVE PLAY. RE PLACED BUSHING IAW DC-9 OHM 32-10-6. 2 L 7 2 4F A6WE 1997041000336 19970410 00336 NM 1997 4 10 97ZZZX1428 1 19961009 A 5320 LAP SEAM BOEING 727 727251 138408H NM BS 1170 S20L CORRODED B KT3R K NONE O OTHER IN INSP/MAINT 1 WP 07 259US 19978 DURING VISUAL INSPECTION OF SB 727-53-0072 R5, LAP SEAM 520L AT STA 1170 WAS FOUND BULGING WITH POPPED RIVET HEADS IN TH E LAP. LEVEL 2 CORROSION WAS NOTED BEHIND THE LAP SEAM WHEN OPENED UP FOR REPAIR. 2 L 7 3 4F A3WE 1997041000414 19970410 00414 WP 1997 4 10 ABXA9700482 1 19961101 A 2710 57077553 OVERRIDE MECH DOUG DC8 DC862 3021970 WP LT AILERON FAILED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 802AX 46134 OVERRIDE MECHANISM SHAFT AND BEARING FAILED DAMAGING LOWER SKIN, GUSSETT AND HINGE WEB FITTING. REPAIRED PER DC8 MM. 2 L 7 4 4F 4A25 1997041000584 19970410 00584 EU 1997 4 10 97ZZZM452 1 19961029 A 5320 ANGLES BAG BAE146 BAE146200A 1500266 EU FUSELAGE BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 AFT CARGO BAY AT FRAME NR 35, RT BELLY TIE DOWN AREA, SURROUND PLATE BENT AND ANGLES TO FRAME BROKEN. ALSO, MISSING RIV ETS IN FRAME. STRAIGHTEN PLATE AND REPLACED ANGLE AND REPLACED RIVETS. 2 H 7 4 4F RT A49EU 1997041000585 19970410 00585 EU 1997 4 10 97ZZZM453 1 19961101 A 5753 FLAP TRACK BAG BAE146 BAE146200A 1500266 EU LT TE FLAP WORN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 NR 1 FLAP TRACK LEFT SIDE HAS .020 INCH WEAR ON SIDE OF LOWER AND UPPER RAILS, FROM SLIPPER PLATES. BLENDED THE OUTBOAR D SIDE OF THE LEFT NR 1 FLAP TRACK UPPER AND LOWER RAILS PER FAX DJR/RJ1243-96, DATED OCT 31, 1996. 2 H 7 4 4F RT A49EU 1997041000586 19970410 00586 EU 1997 4 10 97ZZZM454 1 19961101 A 5712 RIB BAG BAE146 BAE146200A 1500266 EU NR 1 FLAP TRACK CHAFED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 RIB ABOVE LEFT NR 1 FLAP TRACK IS CHAFED WHERE IT CONTACTS ACCESS PANEL 285FT. BLENDED AND REPROTECTED THE CHAFE MARK O N THE SIDE OF RIB 2 TRAILING EDGE EXTENSION PER FAX DJR/RJ1243-96 DATED OCT 31, 1996 AND SRM 51-20-11. GENERATED W/C TO C/W A DV INSPECTION IN 4000 FLTS. 2 H 7 4 4F RT A49EU 1997041000587 19970410 00587 EU 1997 4 10 97ZZZM455 1 19961015 A 5755 BOLTS BAG BAE146 BAE146200A 1500266 EU RT SPOILER CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 RIGHT WING OUTBOARD LIFT SPOILER INBOARD HINGE BOLT SHOWS CRACK INDICATION. RIGHT WING, REMOVED AND REPLACED BOLT TO LI FT SPOILER INBOARD HINGE OF OUTBOARD SPOILER. 2 H 7 4 4F RT A49EU 1997041000588 19970410 00588 EU 1997 4 10 97ZZZM456 1 19961023 A 5320 SUPPORT BAG BAE146 BAE146200A 1500266 EU FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 FRAME 20 LEFT SIDE FLOOR SUPPORT BEAM HAS CORROSION WHERE BOTH FORWARD AIRSTAIR RAILS ATTACH. NEEDS TO BE CLEANED AND M EASURED FOR DEPTH. REPAIR OR REPAINT AS NECESSARY (ONLY ONE SIGNIFICANT SPOT W/A DEPTH MAX AT .029 INCH). REPAIRED IAW FAX DJR/RJ1197-96. 2 H 7 4 4F RT A49EU 1997041000589 19970410 00589 EU 1997 4 10 97ZZZM457 1 19961023 A 5312 BLKHD STIFFENERS BAG BAE146 BAE146200A 1500266 EU FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 PERFORMED ET AT FRAME 29 BULKHEAD TO C/W EO E95/003/653 ITEM NR 3. FOUND CRACKS AT STIFFENER STATION 36.62, 31.13, 25.9 4 LEFT AND 36.62, 31.13, 25.94 RT. REPAIR STIFFENERS IAW EO E95/005/654. END OF CRACKS MARKED WITH GREASE PENCIL. REP AIRED FRAME 29 STIFFENERS AT LT AND RT STATIONS 25.94, 31.13, 36.62 IAW EO E95/005/653 ORIG ISSUE AND AVRO FAXES DJR/RJ1 199-96 AND DJ/RJ059. 2 H 7 4 4F RT A49EU 1997041000590 19970410 00590 EU 1997 4 10 97ZZZM458 1 19961023 A 5312 BLKHD DOUBLER BAG BAE146 BAE146200A 1500266 EU BS 47.2 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 IN HYD BAY AT FRAME 29 BULKHEAD, THE TWO MOST OUTBOARD STIFFENERS LEFT AND RIGHT WERE FOUND TO HAVE CRACKED DOUBLERS AT BOTTOM BOLT HOLE. THESE STIFFENERS ARE NOT COVERED IN EO E95/003/653, STATION 47.20 LT/RT, END OF CRACKS MARKED WITH GR EASE PENCIL. REPLACED LT AND RT FRAME 29 DOUBLERS AT STIFFENER STATION 47.20 IAW BAE STRUCTURAL REPAIR MANUAL AND AVRO FAX NR DJR/RJ1201-96. 2 H 7 4 4F RT A49EU 1997041000591 19970410 00591 EU 1997 4 10 97ZZZM459 1 19961023 A 5755 BOLTS BAG BAE146 BAE146200A 1500266 EU LT SPOILER FAILED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 LEFT WING INBOARD LIFT SPOILER JACK BOLTS, FORWARD AND AFT, FAILED NDT. INSTALLED NEW FORWARD AND AFT JACK BOLTS ON LEF T INBOARD LIFT SPOILER. 2 H 7 4 4F RT A49EU 1997041000594 19970410 00594 EU 1997 4 10 97ZZZM461 1 19961023 A 5210 RAIL BAG BAE146 BAE146200A 1500266 EU AIRSTAIR CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 FORWARD VESTIBULE INBOARD AIRSTAIR RAIL NEEDS TO BE REPLACED DUE TO CORROSION. RAIL IS REMOVED. REPLACED FORWARD INBOA RD AIRSTAIR RAIL. 2 H 7 4 4F RT A49EU 1997041000595 19970410 00595 EU 1997 4 10 97ZZZM462 1 19961107 A 5753 SKIN BAG BAE146 BAE146200A 1500266 EU LT TE FLAP CHAFED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 REF FAX JM/RJ0927-6 DATED 8/14/96, LT FLAP TAB UPPER SKIN CHAFES AT RIBS 19 AND 21, FORWARD OF THE SPOILER RIB STRIP. R EQUIRE REPAIR BY 34682 TCA. AWAC FAX LM185-96 REFERS. REPAIRED IAW AVRO REPAIR DRAWING HC579H9080, HC579H9074 AND FAX REP NR JM/RJ1109-96. 2 H 7 4 4F RT A49EU 1997041000596 19970410 00596 EU 1997 4 10 97ZZZM463 1 19961107 A 5320 SUPPORT BAG BAE146 BAE146200A 1500266 EU CABIN CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 CABIN FLOOR SUPPORT AT FRAME 20A CRACKED AT CENTER GUSSET PLATE. REPAIRED FRAME 20A FLOOR SUPPORT IAW AVRO FAX REF NR D JR/R J1269-96. 2 H 7 4 4F RT A49EU 1997041000597 19970410 00597 EU 1997 4 10 97ZZZM464 1 19961106 A 5347 SEAT RAIL BAG BAE146 BAE146200A 1500266 EU CABIN CORRODED A A6WA K NONE L NO TEST IN INSP/MAINT 1 GL 31 606AW E2033 FORWARD VESTIBULE FRAME 18 RIGHT INBOARD SEAT RAIL CORRODED IN SEVERAL SPOTS, REF SRM 53-00-32 PAGE 203 AND 51-31-11 PAG E 22. REPAIRED FORWARD VESTIBLE RT INBOARD SEAT RAIL BY SPLICING NEW RAIL IN PLACE PER SRM 53-00-32 PAGES 202, 203, 204 . SPLICED PLACE WAS 20.75 INCH LONG AND SPLICED AT FORWARD END OF RAIL. 2 H 7 4 4F RT A49EU 1997041000598 19970410 00598 EU 1997 4 10 97ZZZM465 1 19961105 A 5315 FLOORBEAM BAG BAE146 BAE146200A 1500266 EU FRAME 29 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 ELEVEN CRACK INDICATIONS ON FORWARD END OF PRESSURE FLOORBEAMS AT FRAME 29. CRACKED BEAMS ARE NR 2, 3, 4, 5, 6, 7, 9, 1 3, 15, 19 AND 20 NUMBERED L TO RT. REPAIRED 11 CRACKS AT FRAME 29 IAW AVRO REPAIR DRAWING HC536H9211 AND FAX REP NR DJR /RJ1228-96 AND DJR/RJ1209-96. 2 H 7 4 4F RT A49EU 1997041000599 19970410 00599 EU 1997 4 10 97ZZZM466 1 19961105 A 5315 FLOORBEAM BAG BAE146 BAE146200A 1500266 EU CABIN CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 CRACK INDICATIONS FOUND ON THREE PRESSURE FLOORBEAMS OVER FRAME NR 32 LEFT SIDE. VERIFIED WITH ET INSPECTION. REPAIRED 3 CRACKS AT FRAME 32 IAW AVRO REPAIR DRAWING HC536H9211 AND FAX REF NR DJR/RJ1228-96 AND DJR/RJ1209-96. 2 H 7 4 4F RT A49EU 1997041000600 19970410 00600 EU 1997 4 10 97ZZZM467 1 19961011 A 7120 BOLT BAG BAE146 BAE146200A 1500266 EU NR 1 ENGINE FAILED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 NR 1 ENGINE YOKE TO PYLON. DURING INSPECTION OF BOLTS FOUND CRACK INDICATIONS ON BOTTOM RT IN THREAD RUNOUT AREA. REMO VED BOTTOM RT BOLT FOR MAGNETIC PARTICLE VERIFICATION SSI 54-00-123. REMOVED ABOVE BOLT, BOLT FAILED MAGNECTIC PARTICLE INSPECTION REPLACED AND INSTALLED IAW BAE 146 MM. 2 H 7 4 4F RT A49EU 1997041000652 19970410 00652 NM 1997 4 10 USAA970095 1 19960307 A 5312 BULKHEAD BOEING 737 7373B7 1384580 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 519AU 29982 23705 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO .5 INCH CRACKS BS 178 RBL 4.75 WL 198 WL 201 BULKHEAD. STOP DRILLED AND INSTALLED DOUBLER, REPAIRED PER TR 53-10-07 REV A. (M) 2 L 7 2 4F RT A16WE 1997041000809 19970410 00809 WP 1997 4 10 ABXA9700503 1 19960831 A 5753 5910041508 VANE DOUG DC9 DC932 3022066 WP RT TE FLAP GOUGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 RIGHT HAND INBOARD FLAP VANE HAS GOUGED SKINS. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN. 2 L 7 2 4F A6WE 1997041000811 19970410 00811 WP 1997 4 10 ABXA9700505 1 19961119 A 5753 5910041501 VANE DOUG DC9 DC933F 302207A WP LT TE FLAP DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 LEFT WING FIXED VANE DELAMINATED. REPLACED ALL HONEYCOMB CORE DOUBLERS AND SKIN. 2 L 7 2 4F A6WE 1997041000812 19970410 00812 WP 1997 4 10 ABXA9700506 1 19961119 A 5751 59100452 SKIN DOUG DC9 DC941 302207N WP RT AILERON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 960AX 47762 LEADING EDGE NEEDS TO BE WELDED. WELDED LEADING EDGE PER ABX REA D957-18214. 2 L 7 2 4F A6WE 1997041500004 19970415 00004 NM 1997 4 15 CA960809002 1 19960719 A 5610 NP15790110 WINDSHIELD PPG DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE COCKPIT SHORTED W K NONE O B OTHER SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA 8926 91322H2482 120329 (CAN) AFTER INSTALATION OF THE WINDSHIELD A GROUND TEST WAS PERFORMED IN WHICH THE WINDSHIELD SPARKED AND SMOKED AT THE TERMINAL BOARD. THE WINDSHIELD HAD BEEN RPEVIOUSLY REPAIRED FOR THE SAME PROBLEM. 2 H 7 2 4T 4 T RT A13NM E20NE 1997041500005 19970415 00005 CE 1997 4 15 CA960924009 1 19960918 A 6123 W103U6 UNFEATHER SWITCH MTSBSI MU2 MU2B35 5780411 CE GARRTT TPE331 TPE3316252M 01514 NE HARTZL HCB3T HCB3TN5 GL LT ENG PROP STUCK ON W C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CA 7450 P20317C BV1094 (CAN) DURING TAKEOFF ROLL, CREW NOTED THE LEFT ENGINE BETA LIGHT DID NOT EXTINGUISH WHEN THE RIGHT WENT OUT. WHEN THE EN GINES ENTERED PROPELLER GOVERNING MODE INDICATING A PROBLEM THE CREW ABORTED THE TAKEOFF. INVESTIGATION FOUND THE UNFEAT HER BUTTON HAD STUCK IN THE ON POSITION. THE SWITCH WAS LUBRICATED AND ACTIVATED AND SUBSEQUENTLY TESTED OK. 1 H 7 2 3T RT A10SW E2WE 6 C P15EA 1997041500006 19970415 00006 SO 1997 4 15 CA960924023 1 19960918 A 3220 AN17532 SCISSORS BOLT PIPER 4531800 PIPER PA31 PA31350 7103110 SO NOSE SCISSORS BENT W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) BOTH BOLTS SECURING THE NOSE SCISSORS TO THE GEAR WERE FOUND BENT. SUBMITTER BELIEVES SHEAR FORCES CAUSED THE BOLT TO DEFORM. DETAILED INSPECTION OF CASTINGS REVEALED NO FURTHER DEFECTS. 1 L 7 2 3O A20SO 1997041500009 19970415 00009 SO 1997 4 15 CA960925001 1 19960811 A 3230 MS28775113 O-RING WIEBEL 551968 PIPER PA42 PA42 7104202 SO PWA PT6 PT6A41 52043 EA ACTUATOR SHAFT WORN FLAT W H DEACTIVATE SYST/CIRCUITS K FLUID LOSS IN INSP/MAINT 1 CA 6067 WTC1363 PCE80905 (CAN) WITH SYSTEM PRESSURE ON, EMERGENCY UPLOCK ACTUATOR O-RINGS LEAK FLUID INTO THE RIGHT HAND GEAR WELL. WITH NO SYSTE M PRESSURE THERE IS NO LEAK. 1 L 7 2 4T 4 T A23SO E4EA 1997041500011 19970415 00011 CE 1997 4 15 CA960930003 1 19960923 A 2612 302158 FIRE SENSOR BEECH BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA LT ENGINE FAULTY INTERNAL W E ENGINE SHUTDOWN J WARNING INDICATION LD LANDING 1 CA S4505 50587 (CAN) LEFT HAND ENGINE SHUTDOWN DUE TO FALSE FIRE INDICATION. AIRCRAFT LANDED SAFELY AND THE FAULTY SENSOR WAS REPLACED. SUBMITTER STATES THAT WHITE LIGHT WAS SETTING IT OFF. 1 L 7 2 3T 4 T A14CE E4EA 1997041500012 19970415 00012 EA 1997 4 15 CA961028001 2 19961015 A 7414 10349234 GEAR ASSEMBLY BENDIX 103493659 PIPER PA34 PA34200 7103405 SO LYC O360 IO360C1E6 41514 EA MAGNETO BROKEN TEETH W K NONE O OTHER IN INSP/MAINT 1 CA 243 943641 L1215951A (CAN) DURING A MAGNETO INSEPCTION FOR ENGINE TIMING CHECK, MAINTENANCE FOUND TWO MISSING TEETH ON THE DISTRIBUTOR GEAR. NO REPORTS OF ENGINE RUNNING IRREGULAR. THE MAGNETO WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 3O 3 O A7SO 1E10 1997041500013 19970415 00013 1997 4 15 CA961029011 4 19961020 A 6122 8210004 PROP GOVERNOR DHAV DHC6 DHC6300 EA PWA PT6 PT6A27 52043 EA HARTZL HCB3T HCB3TN3 GL #2 ENGINE FAULTY W E A ENGINE SHUTDOWN UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CR CRUISE 1 CA 2451 1049 PCE41909 BU11842 (CAN) DURING FLIGHT WITH POWER SETTINGS IN CRUISE THE CREW NOTICED A CHANGE IN THE SOUND FROM THE #2 ENGINE, IT WAS ALSO NOTED THE BETA LIGHT WAS ON. THE PROP RPM WAS INCREASING AND THE TORQUE WAS DECREASING AND THE AIRCRAFT BEGAN TO YAW. T HE YAW HAD TO BE CORRECTED BY THE RUDDER PEDALS, SO THE #2 ENGINE WAS SHUTDOWN. POST FLIGHT INSPECTION, GROUND RUN AND F LIGHT TEST COULD NOT DUPLICATE THE FAULT. SUSPECT INTERMITTENT PROPELLER GOVERNOR FAULT. PROPELLER GOVERNOR SENT FOR TES TING. 1 H 7 2 3T 4 T A9EA E4EA 6 C P15EA 1997041500014 19970415 00014 NE 1997 4 15 CA961104004 2 19961029 A 7250 TURBINE SECTION BOEING 737 737275 1384485 NM PWA JT8 JT8D17 52049 NE NR 2 ENGINE FAILURE W C D ABORTED TAKEOFF RETURN TO BLOCK E VIBRATION/BUFFET TO TAKEOFF 1 CA 702601B (CAN) NR 2 ENGINE COMPRESSOR STALLED FOLLOWED BY VIBRATION WHEN APPLYING TAKEOF F POWER. TAKEOFF WAS REJECTED AND THE A IRCRAFT RETURNED TO THE RAMP. INSPECTION FOUND A MAJOR FAILURE OF THE TURBINE SECTION. THE NR 2 ENGINE WAS REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1997041500015 19970415 00015 NE 1997 4 15 CA961105001 2 19961026 A 7322 32448536 FUEL CONTRL DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE #2 ENGINE FAULTY W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 2056 124482 (CAN) DURING CLIMB THE #2 ENGINE TORQUE STARTED TO CYCLE UP AND DOWN 10-24 PERCENT - FUEL FLOW AND NL ALSO CYCLED UP AND DOWN. PILOTS SELECTED E.C.U. TO MANUAL, TURNED OFF PROP SYNC. AND BLEED AIR BUT FLUCTUATIONS STILL OCCURRED. AIRCRAFT R ETURNED TO POINT OF DEPARTURE. MAIN FUEL CONTROL WAS REPLACED AND THE ENGINE GROUND RUN SERVICEABLE. AIRCRAFT RETURNED T O SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 1997041500017 19970415 00017 GL 1997 4 15 CA961112026 3 19960926 A 6110 15701595 SHOULDER SCREW 57B1593 BEECH 95 95B55 1152729 CE CONT O470 IO470L 17026 SO HARTZL HCC2Y BHCC2YF2 GL NR 1 PROP BACKED OUT W O OTHER R PARTIAL RPM/PWR LOSS DE DESCENT 1 CA 1530 237685R AN6600 (CAN) ON APPROACH THE #1 PROPELLER RPM DROPPED WHEN THE POWER WAS REDUCED. THE AIRCRAFT LANDED WITHOUT INCIDENT, BUT THE PROPELLER FEATHERED ON SHUTDOWN. THE PROP WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. DISASSEMBLY OF THE FAULTY PROPELLER FOUND THE SHOULDER SCREW HAD BACKED OUT OF BRACKET P/N 57B1593, THIS SCREW IS HELD IN BY LOCTITE. THE SCREW AN D BRACKET WERE REPLACED AND THE PROPELLER RETURNED TO SERVICE. 1 L 7 2 3O 3 O RT 3A16 3E1 5 C P920 1997041500019 19970415 00019 NM 1997 4 15 CA961112044 1 19961024 A 3244 H31X975X14 TIRES DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE LEFT MAIN BLOWN W O OTHER O OTHER TX TAXI/GRND HDL 1 CA 123030 (CAN) PILOT REPORTED LOUD BANG AFTER LEAVING GATE. A CUT FOUND IN THE SIDEWALL OF THE INNER TIRE WHICH CAUSED THE BEAD O F THE OUTER TIRE TO FAIL. BOTH WHEEL ASSEMBLIES REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1997041500022 19970415 00022 SW 1997 4 15 CA961112049 1 19961025 A 5311 K931460039 FRAME KAMAN K1200 K1200 05625F6 SW LYC T53 T5317A 41549 NE STA 115.0 CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1868 LR81008 (CAN) DURING A ROUTINE INSPECTION THE AME DISCOVERED 2 HORIZONTAL CRACKS AT STA.115.0, WL 85.0, LBL 15 INCHES. BOTH CRAC KS ORIGINATE AT BOLT HOLE AND PROPAGATE OUTBOARD IN A HORIZONTAL DIRECTION LATERALLY ACROSS THE BULKHEAD. MANUFACTURER I NDICATED THAT THIS DEFECT IS TYPICAL ON AIRCRAFT NOT MODIFIED IN ACCORDANCE WITH KAMAN SB 025. 1 G 7 1 4F 4 U NT TR7BO E17EA 1997041500023 19970415 00023 SW 1997 4 15 CA961112050 1 19961028 A 6410 206016201125 BLADE BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL T/R LE PUNCTURED W A UNSCHED LANDING E C VIBRATION/BUFFET F.O.D. CR CRUISE 1 CA 970 CAE801318BA (CAN) DURING A SLOW LOW LEVEL TURN THE PILOT EXPERIENCED AN ABRUPT VIBRATION IN THE TAIL ROTOR PEDALS. UPON INVESTIGATIO N AN AN3-3A BOLT WAS FOUND EMBEDDED IN THE LEADING EDGE OF THE TAIL ROTOR BLADE. THE BOLT HAD COME LOOSE FROM THE TAIL R OTOR GEARBOX FAIRING. 1 G 7 1 3U 3 U H2SW E4CE 1997041500025 19970415 00025 EU 1997 4 15 CA961113001 1 19961108 A 3260 SENSORS BAG BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE DOOR AND UPLOCK DIRTY W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA LF05627A (CAN) LEFT HAND GEAR UNSAFE LIGHT ON AFTER GEAR RETRACTION. AIRCRAFT RETURNED TO AIRPORT. DIRT FOUND IN GEAR UPLOCK AND DOOR SENSORS. CLEANED AND GEAR SWUNG. 2 H 7 4 4F 4 F RT A49EU E6NE 1997041500026 19970415 00026 NE 1997 4 15 CA961113007 2 19961105 A 7200 ENGINE LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB21122B02 54555 NE #2 POSITION FAILED W E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. E Y VIBRATION/BUFFET ENGINE STOPPAGE AP APPROACH 1 CA 33463 10410 (CAN) ON APPROACH AT 700 FEET THE #2 ENGINE FAILED. AIRCRAFT LANDED AND PASSENGERS DEPLANED SAFELY. ENGINE FIRE BOTTLES FIRED AS A PRECAUTIONARY MEASURE. INVESTIGATION REVEALED METAL IN THE TAILPIPE. MAGNETIC CHIP DETECTOR VERIFIED NO METAL FLAKES. 2 L 7 3 4F 4 F A23WE E12EU 1997041500027 19970415 00027 NM 1997 4 15 CA961114001 1 19961023 A 7931 42D107A1 SWITCH BOEING 727 727227 1384078 NM PWA JT8 JT8D9A 52048 NE #2 ENG OIL PRESS FAULTY W E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 CA 666281 (CAN) ON DESCENT #2 ENGINE LOW OIL PRESSURE/FILTER BYPASS LIGHT ILLUMINATED. OIL TEMPERATURE, OIL QUANTITY AND OIL PRESS URE ALL INDICATED NORMAL. POWER WAS REDUCED, LIGHT WOULD NOT EXTINGUISH, #2 ENGINE WAS SHUTDOWN. POST FLIGHT INSPECTION AND ENGINE GROUND RUN COULD NOT DUPLICATE THE FAULT. OIL BYPASS SWITCH WAS DISCONNECTED AND DEFERRED FOR THE NEXT DAYS F LIGHT TO CHECK THE INTEGRITY OF THE ENGINE OIL PRESSURE SWITCH, WHICH CHECKED OK AT THE DAYS END. PRECAUTIONARY REPLACEM ENT OF THE #2 ENGINE OIL PRESSURE SWITCH WAS CARRIED OUT. 2 L 7 3 4F 4 F A3WE E2EA 1997041500028 19970415 00028 WP 1997 4 15 CA961114002 1 19961030 A 3297 WIRE CVAC 340 340CVAC 242270A WP ALLSN 501D 501D13 03004 GL NLG SWITCH BROKEN W O OTHER J WARNING INDICATION AP APPROACH 1 CA 501421 (CAN) ON APPROACH, NO DOWN LOCK INDICATION ON NOSE LANDING GEAR. EMERGENCY LANDING SAFELY CARRIED OUT. MAINTENANCE ACTIO N DISCOVERED BROKEN WIRE IN NLG CONDUIT BETWEEN SWITCH AND JUNCTION BOX. BROKEN WIRE REPAIRED AND LANDING OPERATION CHEC KED SERVICEABLE. 2 L 7 2 4R 4 T 6A6 E282 1997041500029 19970415 00029 WP 1997 4 15 CA961114003 1 19961031 A 3260 SWITCH CVAC 340 340CVAC 242270A WP ALLSN 501D 501D13 03004 GL R/H MLG DWN LOCK FAILED W O OTHER J WARNING INDICATION AP APPROACH 1 CA 501658 (CAN) ON APPROACH RH MAIN LANDING GEAR DID NOT INDICATE DOWN AND LOCKED. EMERGENCY PROCEDURE LANDING CARRIED OUT. MAINTE NANCE CHECK REVEALED DOWN LOCK SWITCH FAILED IN OPEN POSITION. WIRES ON DOWN LOCK SWITCH CONNECTED TO SPARE CONTACTS AND LANDING GEAR OPERATION CHECKED SERVICEABLE. SWITCH TO BE REPLACED WHEN PART AVAILABLE. 2 L 7 2 4R 4 T 6A6 E282 1997041500031 19970415 00031 GL 1997 4 15 CA961115005 1 19961003 A 2824 M72210164 CHECK VALVE DIAMON DA20A1 DA20A1 05626UX GL FUEL FAIL TEST W K NONE O OTHER IN INSP/MAINT 1 CA 1235 (CAN) CHECK VALVE FAILS PRESSURE TEST AS PER MAINTENANCE MANUAL. 1 L 7 1 3O NT TA4CH 1997041500032 19970415 00032 EU 1997 4 15 CA961115006 2 19961106 A 8500 2072000002 RADIATOR PIPE DIAMON DA20A1 DA20A1 05626UX GL ROTAX 912 ROTAX912 55555 EU COOLANT LINE GOUGED W K NONE O OTHER IN INSP/MAINT 1 CA 888 305 4076102 (CAN) DURING INSPECTION IT WAS DISCOVERED THE EXHAUST SPRING HAD GOUGED MORE THAN 60 PERCENT FROM THE WALL OF THE COOLAN T LINE. THE LINE WAS REPLACED AND THE LINE WAS PROTECTED TO PREVENT FURTHER DAMAGE. 1 L 7 1 3O 3 I NT TA4CH EXPE3I 1997041500033 19970415 00033 EU 1997 4 15 CA961115007 2 19961106 A 8500 850940 SEAL DIAMON DA20A1 DA20A1 05626UX GL ROTAX 912 ROTAX912 55555 EU WATER PUMP LEAKING W D E RETURN TO BLOCK ENGINE SHUTDOWN B K M SMOKE/FUMES/ODORS/SPARKS FLUID LOSS OVER TEMP TX TAXI/GRND HDL 1 CA 888 305 4076102 (CAN) ENGINE WATER SYSTEM INDICATING MAXIMUM DEFLECTION. INSPECTION FOUND ONLY WATER IN THE SYSTEM WAS IN THE RESERVOIR. THE SEAL WAS REPLACED ON THE WATER PUMP AND THE AIRCRAFT RETURNED TO SERVICE. 1 L 7 1 3O 3 I NT TA4CH EXPE3I 1997041500034 19970415 00034 GL 1997 4 15 CA961115010 1 19961106 A 2752 2027500500 FLAP ACTUATOR DIAMON DA20A1 DA20A1 05626UX GL PLASTIC COLLAR OUT OF POSITION W K NONE O OTHER IN INSP/MAINT 1 CA 633 (CAN) PLASTIC COLLAR FOUND OUT OF POSITION IN THE FLAP ASSMEBLY. SUBMITTER BELIEVES IT VIBRATED OUT OF ITS SECURE LOCATI ON AND WAS MOVING ALONG THE SHAFT. SUBMITTER IS CONCERNED THAT IT COULD POSSIBLY JAM THE FLAP. 1 L 7 1 3O NT TA4CH 1997041500035 19970415 00035 CE 1997 4 15 CA961115012 1 19961104 A 5753 5016000354 FLAP SPARS BEECH 90 B90 1152912 CE PWA PT6 PT6A20 52043 EA SLOT TRACK CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA PCE21010 (CAN) BOTH LEFT AND RIGHT HAND INBOARD FLAPS WERE FOUND TO HAVE CRACKS IN THEIR SPARS. THE CRACKS, APPROXIMATELY 1 INCH IN LENGTH ARE LOCATED AT THE SLOT IN THE SPAR THAT ALLOWS THE INBOARD FLAP TRACK TO PASS THROUGH. THE CRACKS RADIATE IN BOTH DIRECTIONS AWAY FROM THE TOP CORNERS OF THE SLOT AND RUN PARALLEL TO THE LENGTH OF THE SPAR. 1 L 7 2 3T 3 T 3A20 E4EA 1997041500036 19970415 00036 EA 1997 4 15 CA961118001 2 19961014 A 7230 3015956 SPACER BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA 2ND & 3RD STAGE FAULTY W O OTHER O OTHER TX TAXI/GRND HDL 1 CA CPPS60514 (CAN) AFTER A REFUELING STOP THE PILOT TRIED WITHOUT SUCCESS TO START THE AIRCRAFT. THE ENGINEER DID A VISUAL INSPECTION OF THE ENGINE AND NO FAULT WAS FOUND. DURING A SECOND START ATTEMPT AN AUDIBLE "CLUNK" WAS HEARD AND NO ROTATION OCCURR ED. THE STARTER WAS REMOVED AND AN ATTEMPT TO ROTATE THE STARTER DRIVE WAS UNSUCCESSFUL. THE INTAKE WAS CHECKED FOR F.O. D., THE COMPRESSOR WAS CLEAN. AN ATTEMPT TO TURN THE COMPRESSOR BY HAND WAS ALSO UNSUCCESSFUL. THE ENGINE WAS REMOVED AN D TEARDOWN REVEALED A DAMAGED 2ND STAGE SPACER BETWEEN THE 2ND AND 3RD STAGES OF COMPRESSION. 1 G 7 1 4U 4 U H4SW E22EA 1997041500037 19970415 00037 EA 1997 4 15 CA961118002 1 19961104 A 2730 C6CFM114027 TORQUE TUBE DHAV C6CF11371 DHAV DHC6 DHC6200 EA PWA PT6 PT6A20 52043 EA HARTZL HCB3T HCB3TN3 GL ELEVATOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA PCE20443 BU8721 (CAN) DURING EMMA #27 INSPECTION LIGHT RUB ON TOP STARBOARD SIDE OF CABLE BELLCRANK QUADRANT WHERE THE QUADRANT GOES THR OUGH THE BULKHEAD. FURTHER CHECK NOTED THAT THE TORQUE TUBE THAT JOINS THE ELEVATOR CONTROL ROD LEVER TO THE CABLE QUADR ANT HAD A DARK LINE RUNNING CIRCUMFERENTIALLY AROUND IT AT ABOUT THE MID POINT. TUBE REPLACED. 1 H 7 2 3T 3 T A9EA E4EA 6 C P15EA 1997041500038 19970415 00038 EU 1997 4 15 CA961118003 1 19960912 A 2140 350A72100509 PIPE SNIAS 350 AS350B2 8680813 EU P2 AIR LINE CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 2647 (CAN) ALUMINUM HEATER LINE UNDER CABIN FLOOR CORRODED AT STEEL FITTINGS, CAUSING P2 AIR LEAK. 1 G 7 1 3U H9EU 1997041500039 19970415 00039 EU 1997 4 15 CA961118004 1 19961002 A 2140 350A72100509 PIPE SNIAS 350 AS350B2 8680813 EU P2 AIR LINE CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 3048 (CAN) ALUMINUM HEATER LINE UNDER CABIN FLOOR CORRODED AT STEEL FITTINGS, CAUSING P2 AIR LEAK. 1 G 7 1 3U H9EU 1997041500040 19970415 00040 NE 1997 4 15 CA961118006 2 19961114 A 7250 310438901 LOCKING BOLT PWA 3024932 CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE LP TURBINE LOW TORQUE W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 1785 71752 (CAN) DURING DISASSEMBLY FOR HSI ABOUT 1/4 CUP OF CARBON GRANUALS WERE REMOVED FROM THE LP TURBINE SHAFT INCLUDING A RIN G OF CARBON AROUND THE INTERSHAFT OIL TRANSFER TUBE. THE SECURING BOLT WAS UNSTAKED AND WHEN A SOCKET WAS APPLIED TO REM OVE THE BOLT, A TORQUE OF ABOUT ONLY 50 IN. LBS WAS REQUIRED. THE TORQUE ON THE PULLER TO REMOVE THE LP TURBINE BALANCE ASSEMBLY WAS ALSO VERY LOW. THIS IS THE FIRST TIME THIS ENGINE HAS BEEN OPENED. 1 L 7 2 4F 4 F A22CE E1NE 1997041500041 19970415 00041 EU 1997 4 15 CA961118008 1 19961103 A 2530 25806531 ELECT RECEPTACLE AIRBUS 320 A320211 3930320 EU GALLEY SHORTED W K NONE O OTHER CR CRUISE 1 CA (CAN) FLIGHT ATTENDANT FELT ELECTRICAL SHOCK IN REAR GALLEY POSITION #527. HOT CUP RECEPTACLE REPLACED. 2 L 7 2 4F RT A28NM 1997041500042 19970415 00042 WP 1997 4 15 CA961118009 1 19961103 A 3222 STRUT DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE NLG COLLAPSED W K NONE O OTHER TO TAKEOFF 1 CA P657374D (CAN) AFTER GEAR SELECTED UP NOSE GEAR UNSAFE LIGHT ILLUMINATED AND LOUD NOISE HEARD COMING FROM VICINITY OF NOSE GEAR A REA. GEAR RECYCLED TWICE, NO CHANGE. MAINTENANCE CHECK REVEALED NOSE GEAR OLEO COLLAPSED. NOSE GEAR OLEO SERVICED AND SY STEM CHECKED SERVICEABLE. 2 L 7 2 4F 4 F A6WE E2EA 1997041500043 19970415 00043 WP 1997 4 15 CA961118010 1 19961103 A 3233 39208025505 ACTUATOR DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE RH MAIN LDG FAILED W A UNSCHED LANDING K FLUID LOSS AP APPROACH 1 CA P656991D (CAN) ON APPROACH LOST RIGHT HYDRAULIC SYSTEM (QUANTITY AND PRESSURE). MANUAL GEAR EXTENSION CARRIED OUT AND AIRCRAFT LA NDED SAFELY. MAINTENANCE ACTION INVOLVED REPLACING RH MAIN LANDING GEAR RETRACT ACTUATOR, ENGINE DRIVEN HYDRAULIC PUMP P /N 314195, CASE DRAIN FILTERS P/N 7506004 AND RH MAIN LANDING GEAR BUNGEE CYLINDER P/N 5914016-5503H. LADNING GEAR OPEAT IONAL CHECKED SERVICEABLE. 2 L 7 2 4F 4 F A6WE E2EA 1997041500044 19970415 00044 EU 1997 4 15 CA961118011 1 19961108 A 2610 73040102 FIRE DETECTION AIRBUS 320 A320211 3930320 EU ERRATIC W K NONE N FALSE WARNING CR CRUISE 1 CA (CAN) DURING FLIGHT TWO WARNING LIGHT CAME ON IN FIRE P/B SWITCH AND FIRE WARNING LIGHT CAME ON THE CENTRE CONSOLE. NO M ASTER WARNING LIGHTS OR BELL OR ECAM MESSAGE OR FAULT. FLIGHT PROCEEDED TO DESTINATION. MAINTENANCE ACTION INVOLVED CHAN GING FIRE DETECTION UNIT. SYSTEM TESTED SERVICEABLE. 2 L 7 2 4F RT A28NM 1997041500045 19970415 00045 1997 4 15 CA961118014 4 19961111 A 3433 6227194101 COUPLERS COLLINS CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE ILS SYS FAILED W K NONE O OTHER NR NOT REPORTED 1 CA 1832 807343 (CAN) BOTH CAPTAINS AND FIRST OFFICERS INSTRUMENT LANDING SYSTEM INOPERATIVE. ANTENNA COUPLERS REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 1997041500047 19970415 00047 SW 1997 4 15 CA961120001 1 19961003 A 2710 KP16B BEARING SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP ROTOL R321 R321482F8 GL AILERON ROUGH W A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CA P44121 DRIDRG160180 (CAN) DURING CLIMB AILERON SEIZED. AIRCRAFT RETURNED NO INCIDENT. BEARINGS IN ROLLER FOUND ROUGH AND REPLACED. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C P61GL 1997041500049 19970415 00049 NM 1997 4 15 CA961120004 1 19961110 A 3310 8006221 CONTROL DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE COCKPIT BURNT W K NONE J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA 0134 120581 (CAN) DURING ENGINE START THE WARNING LIGHTS CAME ON BRIGHT THEN A BURNING SMELL WAS NOTICED IN THE COCKPIT. 2 H 7 2 4T 4 T RT A13NM E20NE 1997041500050 19970415 00050 NE 1997 4 15 CA961120005 2 19961114 A 7321 JCT200 AMPLIFIER LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE FUEL CONT NR 3 FAULTY W C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CA BX32748 10482 (CAN) TAKEOFF REJECTED DUE TO LOW EPR ON #3 ENGINE. THE FUEL CONTROL AMPLIFIER SWITCH OVERRODE TO RESTORE POWER. THE FUE L CONTROL AMPLIFIER WAS REPLACED WHEN THE AIRCRAFT RETURNED TO BASE. 2 L 7 3 4F 4 F A23WE E12EU 1997041500051 19970415 00051 EU 1997 4 15 CA961120007 1 19960913 A 2821 206005 FUEL FILTER SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE BYPASS VALVE ERRATIC W K NONE O OTHER IN INSP/MAINT 1 CA 484 866 (CAN) BYPASS FUEL FLOW WAS FOUND TO BE ERRATIC. BYPASS VALVE CHANGED. 1 G 7 1 3U 3 U H9EU E19EU 1997041500052 19970415 00052 EA 1997 4 15 CA961120008 2 19960809 A 7260 MS124735 REG VALVE ASSY PWA 3017470 BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA ACCY GR BOX WORN W K NONE O OTHER IN INSP/MAINT 1 CA 14268 10 CPPS60095 (CAN) ON A POST FLIGHT INSPECTION THE CHECK AND PRESSURE REGULATING VALVE WAS FOUND TO HAVE DROPPED APPROXIMATELY 1/4 IN CH AWAY FROM ACCESSORY GEARBOX WITH INTERNAL OIL TRANSFER TUBES VISIBLE. THE ATTACHEMENT BOLT WAS FOUND TO HAVE FALLEN O UT OF ACCESSORY GEARBOX WITH LOCKWIRE STILL ATTACHED. THE POWER SECTION WAS REMOVED FROM AIRCRAFT. UPON REMOVAL OF CHECK AND PRESSURE REGULATING VALVE TO GAIN ACCESS TO BOLTHOLES IT WAS FOUND THAT OF THE THREE THREADED INSERTS ONE "TWINSTER " HAD BEEN TAPPED FOR A SINGLE HELICOIL, ONE WAS SO WORN IT WOULD NOT ALLOW THE BOLT TO TIGHTEN UP. THE THIRD WAS REJECT ED FOR EXCESSIVE WEAR. THE POWER SECTION WAS OVERHAULED 10.2 HOURS PREVIOUSLY. 1 G 7 1 4U 4 U H4SW E22EA 1997041500053 19970415 00053 NE 1997 4 15 CA961120009 2 19961025 A 7220 43011029 AIRFLOW MODULATO SNIAS 350 AS350D 8680803 EU LYC LTS101 LTS101600A3 41560 NE FLOW FENCE FAILED W A UNSCHED LANDING E F VIBRATION/BUFFET FLT CONT AFFECTED CL CLIMB 1 CA 1768 LE43438CE (CAN) DURING TAKEOFF AND CLIMB HELICOPTER STARTED TO YAW CAUSED BY ENGINE SURGING WITH FLUCTUATING NG TORQUE TOT CAUSED BY FAILURE OF AIRFLOW MODULATOR. 1 G 7 1 3U 3 U H9EU E5NE 1997041600003 19970416 00003 NM 1997 4 16 ANCF9600003 1 19961114 A 5270 WARNING LIGHT BOEING 767 767259 1385136 NM EMERG DOOR ILLUMINATED W ANCF C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 23 985AN 28066 15376 24618 MAC/BOG - FLT 011 - EMERGENCY DOOR LIGHT ILLUMINATED STEADY EICAS MSG L EMER DOOR DISPLAYED STEADY. TAKEOFF WAS REJECTE D AT 129 KNOTS. PERFORMED PROCEDURE FOR F1M 52-71-00 FIG 105 THE OVERWING EMERG EXIT LT SIDE BITE CHECKED TO PROXIMITY SWITCH AND NO FAULT FOUND. DUE TAKEOFF REJECTED INSP WAS ACCOMPLISHED ACCORDING TO AMM 05-51-15. THE 8 BRAKES AND WHEE LS ASSY WERE CHANGED. BRAKES WERE BLED AND HYDRAULIC SYSTEM REFILLED TO CORRECT LEVEL. (X) 2 L 7 2 4F RT A1NM 1997041700305 19970417 00305 WP 1997 4 17 ABXA9700527 1 19961116 A 5280 2210370P4101 BUSHING DOUG DC9 DC941 302207N WP RT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 956AX 47620 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244 FOUND RIGHT HAND MAIN LANDING GEAR OUTBOARD LINKAGE TO HAVE EXCESSIVE PLAY AT LINKAGE ROD PIVOT POINT. REPLACED LINKAGE ROD BUSHING IAW DC9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1997041700306 19970417 00306 WP 1997 4 17 ABXA9700528 1 19961116 A 3231 NAS110420D BOLT DOUG DC9 DC941 302207N WP RT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 956AX 47620 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND RIGHT HAND MAIN LANDING GEAR OUTBOARD DOOR LINKAGE TO HAVE EXCESSIVE PLAY AT LINKAGE ROD PIVOT POINT. REPLACED ATTACH BOLT IAW DC9 OVERHAUL MANUAL 32-10-6. 2 L 7 2 4F A6WE 1997041700339 19970417 00339 WP 1997 4 17 ABXA9700550 1 19961205 A 5751 5705321509 AILERON DOUG DC8 DC863 302198A WP LEFT BROKEN A A ABXA O OTHER O OTHER CR CRUISE 1 GL 23 813AX 46136 DURING LEVEL FLIGHT, BALL CENTERED, BOTH CONTROL WHEELS WERE COCKED APPPROXIMATELY 30 DEGREES TO THE RIGHT AND THERE WAS 30 DEGREES OF AILERON TRIM NEEDED. AS AIRCRAFT WAS SLOWED DOWN MORE AILERON TRIM WAS NEEDED TO KEEP AIRCRAFT LEVEL. R EPLACED LEFT INBOARD AILERON IAW DC-8 MM 27-11-1, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1997041700647 19970417 00647 WP 1997 4 17 ABXA9700608 1 19961007 A 5280 5910634ABX1 DOOR DOUG DC9 DC931 3022065 WP LT MLG CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK AND COMPLIANCE WITH AD 88-24-08, FOUND LEFT MLG INBOARD DOOR CRACKED AT FORWARD UPPER CORNER. REPLACED D OOR IAW DC-9 SUPPLEMENTAL M/M 32-12-01. 2 L 7 2 4F A6WE 1997041700648 19970417 00648 WP 1997 4 17 ABXA9700609 1 19961007 A 5210 49559483 LATCH CUP DOUG DC9 DC931 3022065 WP PAX DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK, FOUND ENTRY DOOR HOLD OPEN LATCH CUP CRACKED. REPAIRED IAW ABX REA D952-16507. 2 L 7 2 4F A6WE 1997041700649 19970417 00649 WP 1997 4 17 ABXA9700610 1 19961005 A 5347 59300845 SEAT TRACK DOUG DC9 DC931 3022065 WP BS 220-275 WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND RBL 22 SEAT TRACK WORN STA 220, 275. REPAIRED IAW ABX EA NR FS-53 -04023-MA. 2 L 7 2 4F A6WE 1997041700650 19970417 00650 WP 1997 4 17 ABXA9700611 1 19961001 A 5347 59300845 SEAT TRACK DOUG DC9 DC931 3022065 WP BS 313-522 WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND SEAT TRACK WORN AT STA 313 TO STA 522, RBL 22. BLENDED IAW DC-9 S RM 53-05, AG 4B. 2 L 7 2 4F A6WE 1997041700651 19970417 00651 WP 1997 4 17 ABXA9700612 1 19961001 A 5347 593008413 SEAT TRACK DOUG DC9 DC931 3022065 WP BS 605-630 WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND SEAT TRACK BL 0 WORN FROM STA 605 TO 630. BLENDED IAW DC-9 SRM 53 -05, FIGURE 4B. 2 L 7 2 4F A6WE 1997041700652 19970417 00652 WP 1997 4 17 ABXA9700613 1 19961005 A 5347 59300845 SEAT TRACK DOUG DC9 DC931 3022065 WP BS 690 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND SEAT TRACK CRACKED AT RBL 22 AT STA 690. REPAIRED IAW ABX EA NR F S-53-04023-MA. 2 L 7 2 4F A6WE 1997041700653 19970417 00653 WP 1997 4 17 ABXA9700614 1 19961001 A 5313 27779223 LONGERON DOUG DC9 DC931 3022065 WP BS 718 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK AND COMPLIANCE WITH AD 88-24-08, FOUND LONGERON 5L CRACKED AT FRAME 718. REPAIRED IAW DC-9 SRM 53-02, FI GURE 2. 2 L 7 2 4F A6WE 1997041700656 19970417 00656 WP 1997 4 17 ABXA9700615 1 19960515 A 5753 5910043503 FLAP VANE DOUG DC9 DC933F 302207A WP LT TE FLAP GOUGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 THE LEFT OUTBOARD FLAP VANE HAS TWO GOUGES THROUGH THE SKIN ON THE INBOARD LEADING EDGE. REPLACED ALL HONEYCOMB CORE, D OUBLERS AND SKINS IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997041700657 19970417 00657 WP 1997 4 17 ABXA9700616 1 19960924 A 5752 5910051502 TAB DOUG DC9 DC941 302207N WP RT AILERON DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 THE RIGHT AILERON TAB HAD 3 AREAS OF DELAMINATION BOTH UPPER AND LOWER, 20 PERCENT OVERALL. REPLACED ALL HONEYCOMB CORE , DOUBLERS AND SKINS IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997041700658 19970417 00658 WP 1997 4 17 ABXA9700617 1 19961004 A 5753 5912168505 VANE DOUG DC9 DC941 302207N WP LT TE FLAP CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 THE LEFT FORWARD FLAP VANE HAS WIDE SPREAD CORROSION AND PITTING ALONG THE TRAILING EDGE. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997041700659 19970417 00659 WP 1997 4 17 ABXA9700618 1 19960613 A 5753 5910041503 FLAP VANE DOUG DC9 DC931 3022065 WP LT TE FLAP DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 THE LEFT INBOARD FLAP VANE HAD 4 AREAS OF DELAMINATION OF THE UPPER INBOARD MIDDLE. REPLACED ALL HONEYCOMB CORE, DOUBLE RS AND SKINS IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997041700660 19970417 00660 WP 1997 4 17 ABXA9700619 1 19960813 A 5753 59121681 FLAP VANE DOUG DC9 DC931 3022065 WP LT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 924AX 47403 THE LEFT FORWARD FLAP VANE HAD THE INBOARD STOP SUPPORT CRACKED AND INDICATIONS OF CORROSION. REPLACED ALL HONEYCOMB CO RE, DOUBLERS AND SKINS IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997041700661 19970417 00661 WP 1997 4 17 ABXA9700620 1 19960719 A 5523 5910413510 TAB DOUG DC9 DC941 302207N WP RT ELEVATOR DELAMINATION A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 958AX 47760 THE RIGHT ELEVATOR TAB HAD 20 PERCENT DELAMINATION WITH POSSIBLE MOISTURE ENTRAPMENT. REPLACED ALL HONEYCOMB CORE, DOUB LERS AND SKIN IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997041700662 19970417 00662 WP 1997 4 17 ABXA9700621 1 19960710 A 5542 M07024507 SKIN DOUG DC9 DC941 302207N WP RUDDER DENTED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 958AX 47760 THE RUDDER ASSEMBLY HAD DENTS ON THE OUTER SKIN AND BAD RIVETS. REPAIRED IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997041700663 19970417 00663 WP 1997 4 17 ABXA9700622 1 19960514 A 5755 5910055515 SPOILER DOUG DC9 DC933F 302207A WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 THE LEFT OUTBOARD SPOILER WAS CRACKED AT THE CENTER HINGE CUP. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997041700665 19970417 00665 WP 1997 4 17 ABXA9700623 1 19961007 A 5320 99582423 INTERCOSTAL DOUG DC9 DC931 3022065 WP BS 699-718 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK AND COMPLIANCE WITH AD 88-24-08, FOUND CRACKED INTERCOSTAL BETWEEN FRAMES 699 TO 718 AT LONGERON 6L. FAB RICATED NEW INTERCOSTAL IAW DC-9 DWG 9958242-3, INSTALLED IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 1997041700666 19970417 00666 WP 1997 4 17 ABXA9700624 1 19961001 A 5313 27779221 LONGERON DOUG DC9 DC931 3022065 WP BS 756 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK AND COMPLIANCE WITH AD 88-24-08, FOUND LONGERON 4L CRACKED AT FRAME 756. REPAIRED IAW DC-9 SRM 53-02, FI GURE 2. 2 L 7 2 4F A6WE 1997041700667 19970417 00667 WP 1997 4 17 ABXA9700625 1 19960927 A 5320 9910073273 PRESSURE PANEL DOUG DC9 DC931 3022065 WP NLG WW CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK, FOUND PRESSURE PANEL CRACKED IN LEFT TUNNEL AREA OF NOSE WHEEL WELL. REPAIRED IAW DC-9 S/B 53-187. 2 L 7 2 4F A6WE 1997041700668 19970417 00668 WP 1997 4 17 ABXA9700626 1 19961007 A 5330 5956879501 SKIN DOUG DC9 DC931 3022065 WP BS 200 TORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK FOUND ENTRY DOOR AFT JAMB INNER SKIN TORN AT FS 200. REPAIRED IAW ABX REA D953-16621-MR. 2 L 7 2 4F A6WE 1997041700669 19970417 00669 WP 1997 4 17 ABXA9700627 1 19961008 A 5330 5911401117 SKIN DOUG DC9 DC931 3022065 WP BS 110-229 GOUGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK, FOUND FUSELAGE SKIN GOUGED FROM STATION 208 TO 223, BETWEEN LONGERON 24R TO 25R. REPAIRED IAW ABX REA D 953-16659-MR. 2 L 7 2 4F A6WE 1997041700670 19970417 00670 WP 1997 4 17 ABXA9700628 1 19961006 A 5320 99107349 WEB DOUG DC9 DC931 3022065 WP BS 237-317 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK, FOUND CUSP WEB BETWEEN FS 237 TO 317 CRACKED AND CORRODED. REPAIRED IAW ABX REA D953-16630-MR. 2 L 7 2 4F A6WE 1997041700671 19970417 00671 WP 1997 4 17 ABXA9700629 1 19961005 A 5312 5910130275 BULKHEAD WEB DOUG DC9 DC931 3022065 WP BS 996 GOUGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK, FOUND GOUGES ON APB WEB AT LONGERON 28L AT TEE CAP. REPAIRED IAW ABX REA D953-16658-MR. 2 L 7 2 4F A6WE 1997041700672 19970417 00672 WP 1997 4 17 ABXA9700630 1 19961004 A 5320 9957739117 SHEAR TIE DOUG DC9 DC931 3022065 WP BS 945 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND SHEAR TIE CRACKED AT FS 945. INSTALLED NEW SHEAR TIE IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 1997041700673 19970417 00673 WP 1997 4 17 ABXA9700631 1 19961008 A 5330 591140940 SKIN DOUG DC9 DC931 3022065 WP BS 334 DENTED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK, FOUND 2 DENTS IN FUSELAGE SKIN AND WINDOW BELT DOUBLER AT FS 334. REPAIRED IAW ABX REA D953-16639-MR. 2 L 7 2 4F A6WE 1997041700674 19970417 00674 WP 1997 4 17 ABXA9700632 1 19961012 A 5330 592032339 SKIN DOUG DC9 DC931 3022065 WP BS 427-475 GOUGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK, FOUND SKIN GOUGED AFT OF FLC DOOR. REPAIRED IAW ABX REA D953-16631-MR. 2 L 7 2 4F A6WE 1997041700675 19970417 00675 WP 1997 4 17 ABXA9700633 1 19961009 A 5311 9911841103 FRAME DOUG DC9 DC931 3022065 WP BS 1089 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK, CANTED FRAME WEB AT FS 1089 CORRODED. REPAIRED IAW ABX REA D953-16618-MR. 2 L 7 2 4F A6WE 1997041700676 19970417 00676 WP 1997 4 17 ABXA9700634 1 19961003 A 5531 99118225 RIB DOUG DC9 DC931 3022065 WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER REMOVABLE LEADING EDGE RIB CRACKED, SECOND FRO M BOTTOM LEFT. REPAIRED IAW SUPPLEMENTAL SRM DWG K05159. 2 L 7 2 4F A6WE 1997041700677 19970417 00677 WP 1997 4 17 ABXA9700635 1 19961003 A 5531 99118215 RIB DOUG DC9 DC931 3022065 WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER REMOVABLE LEADING EDGE RIB CRACKED, LOWER LEFT . REPAIRED IAW SUPPLEMENTAL SRM DWG K05159. 2 L 7 2 4F A6WE 1997041700678 19970417 00678 WP 1997 4 17 ABXA9700636 1 19961003 A 5531 99118246 RIB DOUG DC9 DC931 3022065 WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER REMOVABLE LEADING EDGE RIB CRACKED, FIFTH FROM BOTTOM RIGHT. \N\N\N\N\N REPAIRED IAW SUPPLEMENTAL SRM DWG K05159. 2 L 7 2 4F A6WE 1997041700679 19970417 00679 WP 1997 4 17 ABXA9700637 1 19961003 A 5531 99118246 RIB DOUG DC9 DC931 3022065 WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER REMOVABLE LEADING EDGE RIB CRACKED, FOURTH FRO M BOTTOM RIGHT. REPAIRED IAW SUPPLEMENTAL SRM DWG K05159. 2 L 7 2 4F A6WE 1997041700680 19970417 00680 WP 1997 4 17 ABXA9700638 1 19961003 A 5531 99118226 RIB DOUG DC9 DC931 3022065 WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER REMOVABLE LEADING EDGE RIB CRACKED, SECOND FRO M BOTTOM RIGHT. REPAIRED IAW SUPPLEMENTAL SRM DWG K05159. 2 L 7 2 4F A6WE 1997041700681 19970417 00681 WP 1997 4 17 ABXA9700639 1 19961003 A 5531 99118216 RIB DOUG DC9 DC931 3022065 WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER REMOVABLE LEADING EDGE RIB CRACKED, LOWER RIG HT. REPAIRED IAW SUPPLEMENTAL SRM DWG K05159. 2 L 7 2 4F A6WE 1997041700682 19970417 00682 WP 1997 4 17 ABXA9700640 1 19961003 A 5531 991182312 RIB DOUG DC9 DC931 3022065 WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER REMOVABLE LEADING EDGE RIB CRACKED, CANTED RIB RIGHT SIDE. REPAIRED IAW SUPPLEMENTAL SRM DWG K05159. 2 L 7 2 4F A6WE 1997041700683 19970417 00683 WP 1997 4 17 ABXA9700641 1 19961003 A 5531 99118127 RIB DOUG DC9 DC931 3022065 WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER REMOVABLE LEADING EDGE RIB CRACKED, UPPER RIGH T. REPAIRED IAW SUPPLEMENTAL SRM DWG K05159. 2 L 7 2 4F A6WE 1997041700684 19970417 00684 WP 1997 4 17 ABXA9700642 1 19961001 A 5531 991188210 RIB DOUG DC9 DC931 3022065 WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER LEADING EDGE RIB CRACKED, SEVENTH FROM BOTTOM RIGHT. REPAIRED IAW SUPPLEMENTAL SRM DWG K05159. 2 L 7 2 4F A6WE 1997041700685 19970417 00685 WP 1997 4 17 ABXA9700643 1 19961001 A 5531 99118819 RIB DOUG DC9 DC931 3022065 WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER LEADING EDGE RIB CRACKED, EIGHTH FROM BOTTOM L EFT. REPAIRED IAW SUPPLEMENTAL SRM DWG K05159. 2 L 7 2 4F A6WE 1997041700686 19970417 00686 WP 1997 4 17 ABXA9700644 1 19961002 A 5531 99118829 RIB DOUG DC9 DC931 3022065 WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER LEADING EDGE RIB CRACKED, SEVENTH FROM BOTTOM LEFT. REPAIRED IAW SUPPLEMENTAL SRM DWG K05159. 2 L 7 2 4F A6WE 1997041700688 19970417 00688 WP 1997 4 17 ABXA9700646 1 19961004 A 5511 59225802 SPAR CAP DOUG DC9 DC931 3022065 WP RT HORIZ STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK FOUND RIGHT HORIZONTAL STABILIZER FRONT SPAR LOWER CAP CRACKED, AT XFS 180. REPAIRED IAW ABX REA D955-15 489-MR. 2 L 7 2 4F A6WE 1997041700689 19970417 00689 WP 1997 4 17 ABXA9700647 1 19961008 A 2760 3923255504 FITTING DOUG DC9 DC931 3022065 WP RT SPOILER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK, FOUND RIGHT WING INBOARD SPOILER TORQUE TUBE CENTER SUPPORT FITTING CRACKED. REPLACED IAW DC-9 SRM 51-3 0-1, 51-30-2, 51-30-5. 2 L 7 2 4F A6WE 1997041700690 19970417 00690 WP 1997 4 17 ABXA9700475 1 19960909 A 5720 59209083 VORTILON DOUG DC9 DC932 3022066 WP LT WING DENTED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND LEFT WING VORTILON LEADING EDGE WITH PIN HOLES AND DENTS. REPAIRE D IAW ABX REA 953-16330. 2 L 7 2 4F A6WE 1997041700693 19970417 00693 WP 1997 4 17 ABXA9700651 1 19961002 A 5313 27779223 LONGERON DOUG DC9 DC931 3022065 WP BS 756 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK AND COMPLIANCE WITH AD 88-24-08, FOUND LONGERON 5R CRACKED AT FRAME 756. REPAIRED IAW DC-9 SRM 53-02, FI GURE 2. 2 L 7 2 4F A6WE 1997041700694 19970417 00694 WP 1997 4 17 ABXA9700652 1 19960906 A 5330 591140733 SKIN DOUG DC9 DC932 3022066 WP BS 229 DENTED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 DURING C-CHECK, FUSELAGE SKIN AT 229 WAS FOUND DENTED AND CRACKED. REPAIRED IAW ABX REA D953-16209-MR. 2 L 7 2 4F A6WE 1997041700695 19970417 00695 WP 1997 4 17 ABXA9700653 1 19960906 A 5330 5911401117 SKIN DOUG DC9 DC932 3022066 WP BS 180 DENTED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 DURING C-CHECK, DENTS WERE FOUND ON FUSELAGE SKIN AT FS 180 BETWEEN LONGERONS 20R TO 23R. REPAIRED IAW ABX REA D953-161 60-MR. 2 L 7 2 4F A6WE 1997041700696 19970417 00696 WP 1997 4 17 ABXA9700655 1 19960911 A 5313 27779221 LONGERON DOUG DC9 DC932 3022066 WP BS 256 DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 DURING C-CHECK AND COMPLIANCE WITH AD 96-07-51, FOUND LONGERON 2L DAMAGED AT STA 256. REPAIRED IAW DC-9 SRM 53-02, FIGU RE 2. 2 L 7 2 4F A6WE 1997041700697 19970417 00697 WP 1997 4 17 ABXA9700656 1 19960911 A 5240 9911579501 BEAM DOUG DC9 DC932 3022066 WP SERVICE DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND TOP HORIZONTAL BEAM CRACKED ON SERVICE DOOR. REPLACED IAW DC-9 SR M 51-30-2, 51-30-5. 2 L 7 2 4F A6WE 1997041700698 19970417 00698 WP 1997 4 17 ABXA9700657 1 19960918 A 5320 59103435 DOUBLER DOUG DC9 DC932 3022066 WP BS 160-218 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND LEVEL 2 CORROSION ON LONGERONS, SKIN AND FRAMES AT STA 160 TO 200 . REPLACED DOUBLER IAW DC-9 51-30-2, 51-30-5. 2 L 7 2 4F A6WE 1997041700699 19970417 00699 WP 1997 4 17 ABXA9700658 1 19960918 A 5313 27779223 LONGERON DOUG DC9 DC932 3022066 WP BS 160-218 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND LEVEL 2 CORROSION ON LONGERONS 30R, SKIN AND FRAMES AT STA 160 TO 200. REPLACED IAW DC-9 SRM 51-30-2, 51-30-5. 2 L 7 2 4F A6WE 1997041700700 19970417 00700 WP 1997 4 17 ABXA9700659 1 19960918 A 5313 27779223 LONGERON DOUG DC9 DC932 3022066 WP BS 160-218 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND LEVEL 2 CORROSION ON LONGERONS 29L, SKIN AND FRAMES AT STA 160 TO 200. REPLACED IAW DC-9 SRM 51-30-2, 51-30-5. 2 L 7 2 4F A6WE 1997041700701 19970417 00701 WP 1997 4 17 ABXA9700660 1 19960918 A 5313 27779223 LONGERON DOUG DC9 DC932 3022066 WP BS 160-218 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND LEVEL 2 CORROSION ON LONGERONS 29R, SKIN AND FRAMES AT STA 160 TO 200. REPLACED IAW DC-9 SRM 51-30-2, 51-30-5. 2 L 7 2 4F A6WE 1997041700702 19970417 00702 WP 1997 4 17 ABXA9700661 1 19960918 A 5313 27779224 LONGERON DOUG DC9 DC932 3022066 WP BS 160 218 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND LEVEL 2 CORROSION ON LONGERONS 28R, SKIN AND FRAMES AT STA 160 TO 200. REPLACED IAW DC-9 SRM 51-30-2, 51-30-5. 2 L 7 2 4F A6WE 1997041700703 19970417 00703 WP 1997 4 17 ABXA9700662 1 19960918 A 5313 27779223 LONGERON DOUG DC9 DC931 3022065 WP BS 160-218 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND LEVEL 2 CORROSION ON LONGERONS 27R, SKIN AND FRAMES AT STA 160 TO 200. REPLACED IAW DC-9 SRM 51-30-2, 51-30-5. 2 L 7 2 4F A6WE 1997041700704 19970417 00704 WP 1997 4 17 ABXA9700663 1 19960916 A 5311 9912243105 FRAME DOUG DC9 DC932 3022066 WP BS 180 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND LEVEL 2 CORROSION ON LONGERONS 30R, SKIN, FRAMES AT STA 160 TO 218 . REPAIRED FRAME IAW DC-9 SRM 53-04, FIGURE 2A. 2 L 7 2 4F A6WE 1997041700705 19970417 00705 WP 1997 4 17 ABXA9700664 1 19960831 A 5315 99115957 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 200 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 DURING C-CHECK, FOUND STA 200 FLOORBEAM UPPER CAP CORRODED AND WAS BLENDED OUT OF LIMITS. REPAIRED IAW ABX REA D953-163 29-MR. 2 L 7 2 4F A6WE 1997041700706 19970417 00706 WP 1997 4 17 ABXA9700665 1 19961002 A 5311 991187829 FRAME DOUG DC9 DC932 3022066 WP BS 1155 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47176 DURING C-CHECK, THE CANTED FRAME AT STA 1155 WAS FOUND CRACKED AT LONGERON 4 RT. REPAIRED IAW REA D953-16713-MR. 2 L 7 2 4F A6WE 1997041700707 19970417 00707 WP 1997 4 17 ABXA9700666 1 19961002 A 5311 991187829 FRAME DOUG DC9 DC932 3022066 WP BS 1155 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47176 DURING C-CHECK, THE CANTED FRAME AT STA 1155 WAS FOUND CRACKED AT LONGERON 4 LT. REPAIRED IAW REA D953-16713-MR. 2 L 7 2 4F A6WE 1997041700708 19970417 00708 WP 1997 4 17 ABXA9700667 1 19961002 A 5311 9911859501 FRAME DOUG DC9 DC932 3022066 WP BS 1104 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47176 DURING C-CHECK, THE CANTED FRAME AT STA 1104 WAS FOUND CRACKED AT LONGERON 4 LT. REPAIRED IAW REA D953-16685-MR. 2 L 7 2 4F A6WE 1997041700709 19970417 00709 WP 1997 4 17 ABXA9700668 1 19961002 A 5311 9911839515 FRAME DOUG DC9 DC932 3022066 WP BS 1121 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47176 DURING C-CHECK, THE CANTED FRAME AT STA 1121 WAS FOUND CORRODED AND CRACKED AT LONGERON 5 LT. REPAIRED IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997041700710 19970417 00710 WP 1997 4 17 ABXA9700669 1 19961002 A 5311 99118589 FRAME DOUG DC9 DC932 3022066 WP BS 1074 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47176 DURING C-CHECK, THE CANTED FRAME AT STA 1074 WAS FOUND CRACKED AT LONGERON 4 LT. REPAIRED IAW REA D953-16684-MR. 2 L 7 2 4F A6WE 1997041700711 19970417 00711 WP 1997 4 17 ABXA9700670 1 19961002 A 5530 99118335 ANGLE DOUG DC9 DC932 3022066 WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47176 DURING C-CHECK, THE VERTICAL STABILIZER INTER SPAR BOX FORWARD LOWER ATTACH ANGLE WAS FOUND CRACKED. REPAIRED IAW REA D 955-16656-MR. 2 L 7 2 4F A6WE 1997041700712 19970417 00712 WP 1997 4 17 ABXA9700671 1 19961001 A 5313 27779224 LONGERON DOUG DC9 DC932 3022066 WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47176 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND LONGERON 17L CRACKED AT FRAME 980. REPLACED IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997041700713 19970417 00713 WP 1997 4 17 ABXA9700672 1 19961001 A 5313 27779224 LONGERON DOUG DC9 DC932 3022066 WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47176 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND LONGERON 17R CRACKED AT FRAME 980. REPLACED IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997041700714 19970417 00714 WP 1997 4 17 ABXA9700674 1 19961217 A 5753 5910040504 VANE DOUG DC9 DC941 302207N WP RT TE FLAP DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 THE RIGHT AFT FLAP VANE HAD LARGE AREA'S OF DELAMINATION ON BOTH THE UPPER AND LOWER TRAILING EDGE. REPLACED ALL HONEYC OMB CORE, DOUBLERS AND SKINS IAW DC9 SRM. 2 L 7 2 4F A6WE 1997041700715 19970417 00715 WP 1997 4 17 ABXA9700675 1 19961109 A 5753 59100412 VANE DOUG DC9 DC932 3022066 WP RT TE FLAP DENTED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 939AX 47201 THE RIGHT INBOARD FLAP VANE WAS DEEPLY DENTED AND DELAMINATED ON THE UPPER SIDE AT THE CENTER RUBSTRIPS. REPLACED ALL H ONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997041700716 19970417 00716 WP 1997 4 17 ABXA9700676 1 19961217 A 5753 59121682 VANE DOUG DC9 DC941 302207N WP RT TE FLAP CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 THE RIGHT WING FORWARD FLAP VANE WAS CORRODED ALONG THE TRAILING EDGE. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997041700717 19970417 00717 WP 1997 4 17 ABXA9700677 1 19961211 A 5753 5910041504 VANE DOUG DC9 DC941 302207N WP RT TE FLAP DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 966AX 47510 THE RIGHT WING INBOARD FLAP VANE HAD DELAMINATION BETWEEN THE CENTER RUBSTRIPS. REPLACED ALL HONEYCOMB CORE, DOUBLERS A ND SKINS IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997041700718 19970417 00718 WP 1997 4 17 ABXA9700678 1 19961106 A 5753 5910041504 VANE DOUG DC9 DC915 3022036 WP RT TE FLAP DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 927AX 45717 THE LEFT WING INBOARD FIXED FLAP VANE HAD A AREA OF DELAMINATION BETWEEN MID RUBSTRIPS. REPLACED ALL HONEYCOMB CORE, DO UBLERS AND SKINS IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997041700719 19970417 00719 WP 1997 4 17 ABXA9700679 1 19961120 A 5753 59121681 VANE DOUG DC9 DC933F 302207A WP RT TE FLAP DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 THE RIGHT WING FORWARD FLAP VANE UPPER SURFACE WAS DELAMINATED. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC- 9 SRM. 2 L 7 2 4F A6WE 1997041700720 19970417 00720 WP 1997 4 17 ABXA9700680 1 19961111 A 5753 5912168506 VANE DOUG DC9 DC915 3022036 WP RT TE FLAP DENTED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 927AX 45717 THE RIGHT WING FORWARD FLAP VANE HAD NUMEROUS DENTS ON LOWER SURFACE. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS I AW DC-9 SRM. 2 L 7 2 4F A6WE 1997041700721 19970417 00721 WP 1997 4 17 ABXA9700681 1 19961001 A 5313 27779224 LONGERON DOUG DC9 DC932 3022066 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47176 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND LONGERON 17L CRACKED AT FRAME 965. REPLACED IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997041700722 19970417 00722 WP 1997 4 17 ABXA9700682 1 19960930 A 5720 9919376501 SPLICE DOUG DC9 DC932 3022066 WP WS 267 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47176 DURING C-CHECK, THE LEFT WING LEADING EDGE SPLICE WAS FOUND CRACKED AT STA 267. REPLACED SPLICE IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997041700723 19970417 00723 WP 1997 4 17 ABXA9700683 1 19960930 A 5720 9919376501 SPLICE DOUG DC9 DC932 3022066 WP WS 111 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47176 DURING C-CHECK, THE LEFT WING LEADING EDGE SPLICE WAS FOUND CRACKED AT STA 111. REPLACED SPLICE IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997041700724 19970417 00724 WP 1997 4 17 ABXA9700684 1 19961001 A 5311 99196181 FRAME DOUG DC9 DC932 3022066 WP BS 718 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47176 DURING C-CHECK, THE FUSELAGE MAIN FRAME AT STA 718 RT WAS FOUND CRACKED BEYOND A PREVIOUS REPAIR. REPAIRED IAW REA D953 -16620. 2 L 7 2 4F A6WE 1997041700725 19970417 00725 WP 1997 4 17 ABXA9700685 1 19961001 A 5320 59132624 ANGLE DOUG DC9 DC932 3022066 WP NR 2 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47176 DURING C-CHECK, A CRACK WAS FOUND IN THE UPPER PYLON TO FUSELAGE ATTACH ANGLE. REPLACED ANGLE IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997041700726 19970417 00726 WP 1997 4 17 ABXA9700686 1 19961228 A 5312 591013013 BULKHEAD DOOR DOUG DC9 DC941 302207N WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 DURING C-CHECK, WHILE ACCOMPLISHING S/B 53-137 A CRACK WAS FOUND IN THE UPPER RT DOOR CORNER OF THE AFT PRESSURE BULKHEA D. THE BULKHEAD WAS REPAIRED IAW REA D953-17604-MR. 2 L 7 2 4F A6WE 1997041700727 19970417 00727 WP 1997 4 17 ABXA9700687 1 19961228 A 5540 59131211 BEARING CUP DOUG DC9 DC941 302207N WP RUDDER CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 DURING C-CHECK, THE RUDDER BEARING SUPPORT CUP WAS FOUND CORRODED. THE CUP WAS REPLACED IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 1997041700728 19970417 00728 WP 1997 4 17 ABXA9700688 1 19960103 A 5312 9915558263 BLKHD STIFFENER DOUG DC9 DC941 302207N WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 DURING C-CHECK, WHILE ACCOMPLISHING AD 85-01-02 A STIFFENER ON THE AFT PRESSURE BULKHEAD, UPPER LEFT CORNER WAS FOUND CR ACKED. THE STIFFENER WAS REPLACED IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 1997041700729 19970417 00729 WP 1997 4 17 ABXA9700689 1 19960104 A 5311 FRAME DOUG DC9 DC941 302207N WP BS 200 DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 DURING C-CHECK, THE FRAME AT STA 200 OUTBOARD OF SERVICE DOOR BAYONET ROLLERS WAS FOUND DENTED AND BULGED. THE FRAME WA S REPAIRED IAW DC-9 SRM 51-30-1. 2 L 7 2 4F A6WE 1997041700730 19970417 00730 WP 1997 4 17 ABXA9700690 1 19960108 A 5320 49125401 FITTING DOUG DC9 DC941 302207N WP BS 1041 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 DURING C-CHECK, THE UPPER CARGO FLOOR STRUT ATTACH FITTING WAS FOUND CRACKED AT STA 1041. THE STRUT WAS REPLACED IAW DC 9 SRM 51-30-1. 2 L 7 2 4F A6WE 1997041700731 19970417 00731 WP 1997 4 17 ABXA9700691 1 19960107 A 5312 BULKHEAD SKIN DOUG DC9 DC941 302207N WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 DURING C-CHECK, WHILE ACCOMPLISHING AD 85-01-02 THE AFT PRESSURE BULKHEAD WAS FOUND CRACKED AT THE RT DOOR JAMB 2 INCHES ABOVE THE FLOOR LINE. THE SKIN WAS REPAIRED IAW DC9 SRM 53-05, FIGURE 76. 2 L 7 2 4F A6WE 1997041700732 19970417 00732 WP 1997 4 17 ABXA9700692 1 19960107 A 5311 9923409501 FRAME DOUG DC9 DC941 302207N WP BS 737 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 DURING C-CHECK, WHILE ACCOMPLISHING AD 78-07-05, THE MAIN FRAME AT STA 737 LT WAS CRACKED AT THE FORWARD AND AFT FLANGES . THE FRAME WAS REPLACED IAW REA D953-17588-MR. 2 L 7 2 4F A6WE 1997041700733 19970417 00733 WP 1997 4 17 ABXA9700693 1 19960106 A 5400 5923937502 FITTING DOUG DC9 DC941 302207N WP NR 1 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 DURING C-CHECK, THE PYLON FRONT SPAR UPPER BEAVER TAIL FITTING WAS CRACKED. THE FITTING WAS REPLACED IAW DC9 SRM 51-30- 1. 2 L 7 2 4F A6WE 1997041700734 19970417 00734 WP 1997 4 17 ABXA9700694 1 19961230 A 5712 9919329 RIB DOUG DC9 DC941 302207N WP WS 418/430 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 DURING C-CHECK, THE WING LEADING EDGE RIBS AT STA 418 AND 430 WERE FOUND CRACKED. THE RIBS WERE REPAIRED IAW DC9 SRM 51 -30-5. 2 L 7 2 4F A6WE 1997041700735 19970417 00735 WP 1997 4 17 ABXA9700695 1 19961016 A 5312 9915558235 BULKHEAD CLIP DOUG DC9 DC941 302207N WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 DURING ACCEPTANCE INSPECTION, FOUND THE AFT PRESSURE BULKHEAD LATERAL STIFFENER CRACKED AT LONGERON 15L. REPLACED END C LIP AT LONGERON 15L IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 1997041700736 19970417 00736 WP 1997 4 17 ABXA9700696 1 19961029 A 5312 991558147149 BULKHEAD CLIP DOUG DC9 DC941 302207N WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 DURING ACCEPTANCE INSPECTION FOUND THE AFT PRESSURE BULKHEAD LATERAL STIFFENER CRACKED AT LONGERON 16L. REMOVED AND REP LACED END CLIPS AT LONGERON 16L IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 1997041700737 19970417 00737 WP 1997 4 17 ABXA9700697 1 19961004 A 5312 9915558159243 CLIP DOUG DC9 DC941 302207N WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 DURING ACCEPTANCE INSPECTION, FOUND THE AFT PRESSURE BULKHEAD LATERAL STIFFENER CRACKED AT LONGERON 17L. REMOVED AND RE PLACED END CLIPS AT LONGERON 17L IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 1997041700738 19970417 00738 WP 1997 4 17 ABXA9700698 1 19960918 A 5313 S27779221 LONGERON DOUG DC9 DC941 302207N WP BS 237 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 DURING ACCEPTANCE INSPECTION FOUND LONGERON 17 RIGHT CRACKED AT FS 237. REMOVED AND REPLACED LONGERON AND SPLICE SECTIO N IAW DC-9 SRM CHAPTER 53-02, FIGURE 2. 2 L 7 2 4F A6WE 1997041700739 19970417 00739 WP 1997 4 17 ABXA9700699 1 19961022 A 5400 591326230 ANGLE DOUG DC9 DC941 302207N WP RT PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 DURING ACCEPTANCE INSPECTION, FOUND THE RIGHT ENGINE PYLON UPPER FUSELAGE ATTACH ANGLE CRACKED. REPLACED THE RT UPPER P YLON TO FUSELAGE ATTACH ANGLE IAW DC-9 SRM CHAPTER 51-30-2 AND 51-30-5 AND REPAIRED ONE CRACK IAW ABX REA D954-16695-MR. 2 L 7 2 4F A6WE 1997041700740 19970417 00740 WP 1997 4 17 ABXA9700700 1 19961017 A 5400 591326229 ANGLE DOUG DC9 DC941 302207N WP RT PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 DURING ACCEPTANCE INSPECTION, FOUND THE RIGHT ENGINE PYLON UPPER FUSELAGE ATTACH ANGLE CRACKED AT FS 1095. REPAIRED THE RIGHT PYLON UPPER ATTACH ANGLE IAW ABX REA NR D954-16695-MR. 2 L 7 2 4F A6WE 1997041700741 19970417 00741 WP 1997 4 17 ABXA9700701 1 19961029 A 5400 591326229 ANGLE DOUG DC9 DC941 302207N WP LT PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 DURING ACCEPTANCE INSPECTION FOUND THE LEFT ENGINE PYLON TO FUSELAGE ATTACH ANGLE CRACKED IN TWO PLACES. REPAIRED LEFT PYLON ATTACH ANGLE IAW ABX REA D954-16868-MR. 2 L 7 2 4F A6WE 1997041700742 19970417 00742 WP 1997 4 17 ABXA9700702 1 19961014 A 5730 591343840 PANEL DOUG DC9 DC941 302207N WP WS 690 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 DURING ACCEPTANCE INSPECTION, FOUND THE RIGHT WING LOWER TRAILING EDGE BONDED PANEL JUST INBOARD OF MLG CORRODED. REPLA CED RIGHT WING LOWER INBOARD TRAILING EDGE PANEL IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 1997041700751 19970417 00751 WP 1997 4 17 GTIA9700018 1 19961122 A 5321 FLOOR PANEL DOUG DC9 DC931 3022065 WP BS 200-237 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FORWARD LAVATORY FLOOR PANEL FS 200 TO 237 HAS SEVERAL FASTENER HOLES WITH CRACKS AND SURFACE CORROSION AROUND SCR EW HOLES. REMOVED AND REPLACED SKIN AND DOUBLERS IAW 51-10-0, 51-10-2, 51-10-3, 51-10-4 AND 51-30-3. (M) 2 L 7 2 4F A6WE 1997041700752 19970417 00752 WP 1997 4 17 GTIA9700019 1 19961123 A 5315 FLOORBEAM DOUG DC9 DC931 3022065 WP BS 389/408 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FORWARD CARGO COMPARTMENT FLOORBEAM LOWER LIP BL0 BROKEN OFF AT FS 389 AND FLOORBEAM LOWER LIP AT FS 408 IS CHAFED . REMOVED DAMAGED AREA, FABRICATED FLAT DOUBLERS AND ANGLE DOUBLERS AND INSTALLED IAW 53-10-8. (M) 2 L 7 2 4F A6WE 1997041700753 19970417 00753 WP 1997 4 17 GTIA9700020 1 19961124 A 5321 FLOOR DOUG DC9 DC931 3022065 WP COCKPIT CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - COCKPIT FLOOR AREA LEFT STORAGE AREA HAS A CRACK DEVELOPING IN FORWARD TOP EDGE OF RETAINER. FABRICATED AND INSTA LLED DOUBLER, CRACK STOP DRILLED IAW 52-01, 51-01, 51-10-03. (M) 2 L 7 2 4F A6WE 1997041700754 19970417 00754 WP 1997 4 17 GTIA9700000 1 19961125 A 5320 TRAP PANEL DOUG DC9 DC931 3022065 WP BS 697 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - LEFT TRAPEZOIDAL PANEL UPPER ATTACH LEG LOCATED AT PREVIOUS REPAIR CUT OUT C/T WING ATTACH ANGLE STATION 697 LBL 5 92 F-12 CRACK .80 INCH LONG. REMOVED NOTED CRACK TO THE FOURTH HOLE IAW SRM 57-9, FIG 6, NOTES 1 AND 2 AND 51-10-3. (M ) 2 L 7 2 4F A6WE 1997041700755 19970417 00755 WP 1997 4 17 GTIA9700021 1 19961125 A 5321 CHANNELS DOUG DC9 DC931 3022065 WP COCKPIT CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FLOOR PANEL RIGHT COCKPIT HAS CHANNELS DEFORMED, CRACKED AND WITH RIVETS PULLING THROUGH. REMOVED AND REPLACED CR ACKED HAT CHANNEL PER SRM 53-05, FIG 1. FABRICATED REPLACEMENT HAT SECTION. ALODINED AND PRIMED PER SRM 51-10-3. REPL ACED FASTENERS PER SRM 51-30-2 AND 51-30-8. (M) 2 L 7 2 4F A6WE 1997041700756 19970417 00756 WP 1997 4 17 GTIA9700022 1 19961125 A 5321 FLOOR BOARD DOUG DC9 DC931 3022065 WP CABIN CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - CABIN FLOOR BOARD HAS A CRACK IN UPPER SKIN. REPAIRED PER SRM 53-05, FIG 1. CUT OUT CRACKED AREA AND FABRICATED FILLER AND DOUBLER. ALODINED AND PRIMED PER SRM 51-10-3. INSTALLED FASTENERS PER SRM 51-30-2. (M) 2 L 7 2 4F A6WE 1997041700757 19970417 00757 WP 1997 4 17 GTIA9700023 1 19961126 A 5321 FLOOR DOUG DC9 DC931 3022065 WP BS 218 WORN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FLOOR WEB HAS TWO WEAR AREAS 1 INCH LONG OVER 50 PERCENT OF MATERIAL THICKNESS AT STATION 218 LBL 4 AND 7 ZF1. CU T OUT DAMAGE AREA FABRICATED FILLERS AND DOUBLER INSTALLED IAW 53-01, 51-30-2. (M) 2 L 7 2 4F A6WE 1997041700758 19970417 00758 WP 1997 4 17 GT9A9700024 1 19961126 A 5320 CHANNEL DOUG DC9 DC931 3022065 WP BS 1601 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FORWARD CABIN RIGHT FS 1601 CHANNEL HAS A HOLE IN IT WITH A CRACK EMANATING OUTBOARD .5 INCH. REMOVED DAMAGED ARE A, FABRICATED AND INSTALLED NEW DOUBLER PER SRM 53-01, 51-10-03. (M) 2 L 7 2 4F A6WE 1997041700759 19970417 00759 WP 1997 4 17 GTIA9700025 1 19961126 A 5321 FLOOR BOARD DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FLOOR BOARD, WING BOX AREA, THREE CRACKS IN TOP SKIN AREA, INSULATION TAPE IS LOOSE. CUT OUT CRACKED AREA ON FLOO R BOARD, FABRICATED FILLER AND DOUBLER AND REPAIRED PER SRM 53-05, FIG 1. ALODINED AND PRIMED PER SRM 51-10-3. INSTALL ED RIVETS PER SRM 51-30-2. RETAPED INSULATION PER MM 25-22-0. (M) 2 L 7 2 4F A6WE 1997041700760 19970417 00760 WP 1997 4 17 GTIA9700026 1 19961127 A 5321 FLOOR DOUG DC9 DC931 3022065 WP CABIN MISINSTALLED A GTIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 928ML 47326 MHV - PASSENGER CABIN FLOOR MEMBRANE REQUIRES MODIFICATION PER DOUGLAS REWORK DRAWING SR09530002. MODIFIED FLOOR MEMBRA NE PER DOUGLAS DRAWING SR09530002 FS 718-737 AND 737-756 LT AND RIGHT SIDES INBOARD OF FUSELAGE SKIN. (M) 2 L 7 2 4F A6WE 1997041700761 19970417 00761 WP 1997 4 17 GTIA9700027 1 19961127 A 5321 FLOOR DOUG DC9 DC931 3022065 WP BS 970 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FLOOR WEB HAS A 4 INCH CRACK BETWEEN 2 CUTOUTS AT STATION 970 LBL 50. FABRICATED DOUBLERS PER SRM 53-01, FIG 7. I NSTALLED IAW SRM 51-10-3. (M) 2 L 7 2 4F A6WE 1997041700763 19970417 00763 WP 1997 4 17 GTIA9700029 1 19961201 A 5320 JAMB DOUBLER DOUG DC9 DC931 3022065 WP CARGO DOOR MISSING A GTIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FORWARD CARGO DOOR JAMB FORWARD SIDE REPAIR IS NOT PER DOUGLAS DRAWING SR09530117. FINGER DOUBLER MISSING. FABRI CATED FILLERS AND DOUBLERS PER 51-10-2 AND EA 5330-96-001 REWORK DONE IAW EA 5330-96-001 AND SRM 51-30, 51-10-3. (M) 2 L 7 2 4F A6WE 1997041700764 19970417 00764 WP 1997 4 17 GTIA9700031 1 19961202 A 5320 TIE CLIP DOUG DC9 DC931 3022065 WP BS 965 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - PYLON SHEAR WEB TO LONGERON 17R, TIE CLIP IS CRACKED IN TWO, STATION 965. REPLACED TIE CLIP PER SRM 51-10-1, 51-1 0-3, 51-30-2. (M) 2 L 7 2 4F A6WE 1997041700765 19970417 00765 WP 1997 4 17 GTIA9700032 1 19961202 A 5320 MEMBRANE DOUG DC9 DC931 3022065 WP BS 950 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - CRACK IN MEMBRANE AT FS 950 48 INCHES LEFT OF A/C C/T. FABRICATED AND INSTALLED DOUBLERS IAW 53-01, PAGE 17, 51-1 0-3. (M) 2 L 7 2 4F A6WE 1997041700766 19970417 00766 WP 1997 4 17 GTIA9700033 1 19961202 A 5720 BRACKETS DOUG DC9 DC931 3022065 WP WS 250/256 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - RIGHT WING LEADING EDGE WING STATION XRS 250 AND XRS 256 HAVE CRACKED MOUNTS. REMOVED OLD BRACKETS, FABRICATED IA W 51-10-2 AND INSTALLED IAW 51-10-1/3. (M) 2 L 7 2 4F A6WE 1997041700767 19970417 00767 WP 1997 4 17 GTIA9700034 1 19961203 A 5280 CHANNEL DOUG DC9 DC931 3022065 WP LT MLG DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - LEFT OUTBOARD GEAR DOOR U-CHANNEL AT AFT SURFACE OF DOOR IS CRACKED. REMOVED OLD PART FABRICATED AND INSTALLED NE W PART IAW 52-10-2, 52-80-0. (M) 2 L 7 2 4F A6WE 1997041700768 19970417 00768 WP 1997 4 17 GTIA9700030 1 19961202 A 5312 BULKHEAD FRAME DOUG DC9 DC931 3022065 WP AFT PRESS BLKHD CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - AFT PRESS BULKHEAD FORWARD SIDE LEFT CANTED FRAME ABOVE BULKHEAD DOOR HAS A CRACKED ATTACH CLIP AT UPPER END WHERE BULKHEAD MEETS THE FUSELAGE SKIN. REMOVED AND FABRICATED NEW CLIP, INSTALLED IAW 51-10-2, 51-10-3, 53-01. (M) 2 L 7 2 4F A6WE 1997041700769 19970417 00769 WP 1997 4 17 GTIA9700035 1 19961203 A 5312 BULKHEAD FRAME DOUG DC9 DC931 3022065 WP AFT PRESS BLKHD CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - AFT PRESSURE BULKHEAD DOOR CANTED FRAME ON RT SIDE OF DOOR FRAME IS CRACKED AT UPPER END WHERE THE BULKHEAD MEETS THE FUSELAGE SKIN. REMOVED FRAME, TRIM CRACK AREA PER SRM 51-01, DYE PEN, NO CRACKS FOUND. REINSTALLED FRAME IAW SRM 5 1-10-3, 53-11-3 PAGE 16D. (M) 2 L 7 2 4F A6WE 1997041700770 19970417 00770 WP 1997 4 17 GTIA9700036 1 19961203 A 5320 JAMB DOUG DC9 DC931 3022065 WP CARGO COMPT DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - AFT CARGO PIT, LOWER FORWARD CORNER OF DOOR JAMB HAS DAMAGE ON EDGE OF DOUBLER AND IS DELAMINATING AND HAS NUMEROU S DAMAGED FASTENERS. FABRICATED DOUBLER AND INSTALLED WITH SRM 51-10-2 AND 51-10-3. (M) 2 L 7 2 4F A6WE 1997041700771 19970417 00771 WP 1997 4 17 GTIA9700037 1 19961203 A 5321 FLOOR PANEL DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FLOOR PANEL AFT CABIN HAS TWO CRACKS IN AFT AREA OF SKIN. CUT OUT CRACKS AND FABRICATED FILLER AND DOUBLER PER SR M 51-10-2. ALODINED PER SRM 51-10-3. DRILLED AND COUNTERSUNK PER SRM 51-10-4. INSTALLED FASTENERS PER SRM 51-30-2. F LOOR PANEL REPAIR COMPLETED PER SRM 53-21-0. (M) 2 L 7 2 4F A6WE 1997041700772 19970417 00772 WP 1997 4 17 GTIA9700038 1 19961204 A 5310 STRUCTURE DOUG DC9 DC931 3022065 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FLOORBOARD 27, 3 HAT SECTIONS CRACKED AT ONE END AND 2 SECTIONS CRACKED AT OTHER END. INSULATION BATTING MISSING ON ONE END, FALLING APART ON THE OTHER, AND UNBONDED AND FALLING APART AT A FEW AREAS IN THE CENTER SECTION. REMOVED 5 CRACKED HAT SECTIONS, DURING REWORK FOUND 4 SKIN CRACKS. FABRICATED 5 HAT SECTIONS, 5 HAT SECTION DOUBLERS, 2 FILLERS A ND 3 DOUBLERS. ALODINED AND PRIMED PER SRM 51-10-3. REPAIRED PER SRM 53-05, FIG 1. INSTALLED FASTENERS PER SRM 51-30- 2 AND 51-30-8. REBONDED BATTING PER MM 25-22-0. (M) 2 L 7 2 4F A6WE 1997041700773 19970417 00773 WP 1997 4 17 GTIA9700039 1 19961206 A 5321 FLOOR DOUG DC9 DC931 3022065 WP BS 931-948 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FLOOR WEB HAS CORROSION ON STATION 931-948 RBL 59 ZF1. REMOVED DAMAGE, FABRICATED NEW WEB AND INSTALLED IAW 51-10 -2, 51-10-3, 51-30-0. (M) 2 L 7 2 4F A6WE 1997041700774 19970417 00774 WP 1997 4 17 GTIA9700040 1 19961206 A 5321 FLOOR PANEL DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FLOOR PANEL NR 2A HAS SEVERAL SMALL CRACKS AT THE END ROW OF RIVET HOLES. STOP DRILLED HOLE AND ADDED DOUBLER IAW 51-10-3, SRM 51-10-4. (M) 2 L 7 2 4F A6WE 1997041700775 19970417 00775 WP 1997 4 17 GTIA970041 1 19961206 A 5321 FLOOR PANEL DOUG DC9 DC931 3022065 WP BS 117 DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - COCKPIT FLOOR AT STATION 117 RBL 3 INCH FROM CENTER LINE EXISTS DENTS AND A CRACK .823 INCH LONG THROUGH SUB STRUC TURE BARRIER FLOOR AND PLASTIC CABLE SHROUD. REMOVED DAMAGED AREA, FABRICATED AND INSTALL DOUBLERS PER SRM 53-01 FIG 2, 51-10-03, 51-30-02, 51-20-0. (M) 2 L 7 2 4F A6WE 1997041700776 19970417 00776 WP 1997 4 17 GTIA9700042 1 19961206 A 5321 FLOOR PANEL DOUG DC9 DC931 3022065 WP BS 142 DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - COCKPIT FLOOR AT STATION 142 RBL 17 INCH FROM CENTERLINE EXISTS A HOLE .275 INCH DIAMETER THROUGH SUB STRUCTURE BA RRIER FLOOR. REMOVED DAMAGE AREA AND FABRICATED AND INSTALLED NEW PARTS IAW SRM 53-01 FIG 2, 51-30-02. (M) 2 L 7 2 4F A6WE 1997041700777 19970417 00777 WP 1997 4 17 GTIA9700043 1 19961206 A 5321 FLOOR PANEL DOUG DC9 DC931 3022065 WP CABIN DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 NR 30 FLOOR PANEL HAS 3 CRACKS. REMOVED DAMAGED MATERIAL, DOT LOCATION 24, 25, 26 AND FABRICATED FILLERS AND DOUBLERS. ALODINED AND PRIMED PER SRM 51-10-3. DRILLED AND COUNTERSUNK PER SRM 51-10-4. INSTALLED RIVETS PER SRM 51-30-3. REPA IRED PER SRM 53-05, PAGE3. (M) 2 L 7 2 4F A6WE 1997041700778 19970417 00778 WP 1997 4 17 GTIA9700044 1 19961209 A 5210 DOOR DOUG DC9 DC931 3022065 WP PAX COMPT CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - PASSENGER ENTRY DOOR NUMEROUS CRACKS. REPAIR DOOR IAW 52-05, 51-30-2, 51-30-5. (M) 2 L 7 2 4F A6WE 1997041700779 19970417 00779 WP 1997 4 17 GTIA9700045 1 19961209 A 5321 FLOOR PANEL DOUG DC9 DC931 3022065 WP CABIN CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FLOOR PANEL NR 10 FORWARD HAS 3 HAT SECTIONS WITH CRACKS IN CORNERS (2 AT 1 END AND ONE AT THE OTHER END). ALSO, INSULATION BATTING FALLING APART. REPAIRED HAT SECTIONS IAW SRM 53-05, ALODINED AND PRIMED PER SRM 51-10-3. REPAIRED I NSULATION PER MM 25-22-0. (M) 2 L 7 2 4F A6WE 1997041700780 19970417 00780 WP 1997 4 17 GTIA9700046 1 19961210 A 5321 FLOOR PANEL DOUG DC9 DC931 3022065 WP CABIN CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FLOOR PANEL NR 15 HAS NUMEROUS CRACKS AND DELAMINATION. REMOVED DAMAGED AREA, FABRICATED NEW HAT CHANNELS PER SRM 53-05 FIG 1, INSTALLED IAW 51-30-2, 51-30-7. (M) 2 L 7 2 4F A6WE 1997041700781 19970417 00781 WP 1997 4 17 GTIA9700047 1 19961210 A 5321 FLOOR PANEL DOUG DC9 DC931 3022065 WP CABIN DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - AFT FLOOR PANEL HAS DELAMINATING DOUBLERS RIVETS PULLED OUT OF HAT CHANNELS AND TEARS IN TOP SKIN OF PANEL. REPAI RED FLOOR BOARD PER SRM 53-05. FABRICATED SKIN REPAIR DOUBLERS PER SRM 53-05. ALODINED AND PRIMED PER SRM 51-10-3. ST OP DRILLED TEAR IN TOP SKIN PER SRM 53-01. REPAIRED GRILLINER DOUBLERS PER MM 53-20-1. ALSO, REPLACED SPACER FOR FASTE NER INSTALLATION PER SRM 53-05. (M) 2 L 7 2 4F A6WE 1997041700782 19970417 00782 WP 1997 4 17 GTIA9700048 1 19961211 A 5321 FLOOR BOARD DOUG DC9 DC931 3022065 WP BS 218-237 TORN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - LEFT FUSELAGE FLOOR MEMBRANE THAT ATTACHES TO OUTBOARD SEAT TRACK AT STATION 218-237 LBL 44 IS TORN ON FORWARD SID E. REMOVED OLD MEMBRANE, FABRICATED NEW MEMBRANE AND INSTALLED PER SRM 51-30-01, 51-10-3. (M) 2 L 7 2 4F A6WE 1997041700783 19970417 00783 WP 1997 4 17 GTIA9700049 1 19961211 A 5321 FLOOR BOARD DOUG DC9 DC931 3022065 WP BS 237 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - LEFT FS 237 LBL 44, FLOOR MEMBRANE HAS A CRACK FORWARD OUTBOARD EDGE CORROSION AROUND FITTING AT STATION 237 THAT ATTACHES TO MEMBRANE. CLEANED CORROSION FROM FITTING, REMOVED DAMAGED AREA FABRICATED DOUBLER AND INSTALLED IAW 51-10-3 , 51-01-01, 51-10-2, 53-10-2. (M) 2 L 7 2 4F A6WE 1997041700784 19970417 00784 WP 1997 4 17 GTIA9700050 1 19961211 A 5321 FLOOR PANEL DOUG DC9 DC931 3022065 WP CABIN CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - NR 19 FLOOR PANEL, CORNER DELAMINATING, INSULATION MISSING CENTER AREAS OF HAT CHANNELS DELAMINATING, SKIN TORN AT CORNER. REPAIRED FLOORBOARD PER SRM 53-05. FABRICATED REPAIR DOUBLER PER SRM 53-5. ALODINED AND PRIMED PER 51-10-3. INSTALLED REPAIR DOUBLER PER SRM 53-05. STOP DRILLED TEAR IN TOP OF SKIN PER SRM 53-01. REPAIRED HAT CHANNELS PER SRM 53-05. (M) 2 L 7 2 4F A6WE 1997041700785 19970417 00785 WP 1997 4 17 GTIA9700051 1 19961212 A 5730 PANEL DOUG DC9 DC931 3022065 WP LT WING CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - LEFT WING UNDER AILERON CAM-LOCK RECEPTACLE AT INBOARD END OF PANEL 1509 EXISTS A CRACK FORWARD AND AFT OF FASTENE R HOLE. REMOVED CRACK, FABRICATED NEW ANGLE PER SRM 57-22-3 INSTALLED IAW 51-30-0. (M) 2 L 7 2 4F A6WE 1997041700786 19970417 00786 WP 1997 4 17 GTIA9700052 1 19961212 A 5730 PANEL DOUG DC9 DC931 3022065 WP LT WING CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - LEFT WING PANEL 1508 HAS A CRACK THAT EXISTS FROM RIVET HOLE TO CAM-LOCK HOLE. REMOVED CRACK, FABRICATED ANGLE, I NSTALLED IAW SRM 57-22-3, 51-30-0. (M) 2 L 7 2 4F A6WE 1997041700787 19970417 00787 WP 1997 4 17 GTIA9700053 1 19961212 A 5312 BULKHEAD DOUG DC9 DC931 3022065 WP BS 218 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - ON BULKHEAD BETWEEN FORWARD CARGO BAY AND FORWARD ACCESSORY COMPARTMENT AT STATION 218 EXISTS SEVERAL CRACK REPAIR S THAT ARE NOT PER SRM. REMOVED EXISTING REPAIRS, FABRICATED NEW PATCHES PER SRM 53-10-1 FIG 7B, 53-01 FIG 2, 51-10-3. INSTALLED IAW 53-01 FIG 2. (M) 2 L 7 2 4F A6WE 1997041700788 19970417 00788 WP 1997 4 17 GTIA9700054 1 19961212 A 5321 FLOOR PANEL DOUG DC9 DC931 3022065 WP CABIN DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - NR 23B FLOOR PANEL IS DELAMINATING AT CORNERS. INSULATION TAPE IS LOOSE. REBONDED FLOOR PANELS AT CORNERS WITH S COTCH GRIP ADHESIVE PER MM 53-20-1 AND RETAPED INSULATION PER MM 25-22-0. (M) 2 L 7 2 4F A6WE 1997041700789 19970417 00789 WP 1997 4 17 GTIA9700055 1 19961213 A 5260 STEP DOUG DC9 DC931 3022065 WP VENTRAL STAIR CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - AFT VENTRAL STAIR. RETRACTABLE STEP HAS CORROSION. REMOVED AND REPLACED STEP IAW 51-30-8. (M) 2 L 7 2 4F A6WE 1997041700790 19970417 00790 WP 1997 4 17 GTIA9700056 1 19961213 A 5321 FLOORBOARD DOUG DC9 DC931 3022065 WP WING BOX AREA BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FLOORBOARD WING BOX AREA, ON CORNER, METAL SECTION BROKEN OUT, INSULATION BATTING MISSING ALONG BOTH LONG EDGES, O NE SHORT EDGE HAS UNBONDING, AND OTHER SECTIONS OF SEAL MISSING. REMOVED BROKE SECTION FROM CORNER OF FLOORBOARD FABRIC ATED FILLER AND DOUBLER ALODINED AND PRIMED PER SRM 51-10-3. REPAIRED FLOORBOARD PER SRM 53-05, FIG 1. INSTALLED FASTE NERS PER SRM 57-30-2. INSTALLED INSULATION PER MM 25-22-0. REBONDED GILLINER PER MM 53-20-1. (M) 2 L 7 2 4F A6WE 1997041700791 19970417 00791 WP 1997 4 17 GTIA9700057 1 19961213 A 5321 FLOOR PANEL DOUG DC9 DC931 3022065 WP CABIN DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - NR 4 FLOOR PANEL HAS DELAMINATING DOUBLER AND SOME AREAS MISSING, ONE CRACKED SCREW HOLE, INSULATION MISSING AND M YLAR BROKEN. REPAIRED DELAMINATING DOUBLER AND INSTALLED MISSING DOUBLERS PER MM 53-20-1. REPAIRED CRACKED SCREW HOLE PER SRM 53-05 AND 53-01. FABRICATED REPAIR DOUBLER AND INSTALLED PER 53-05. INSTALLED MISSING INSULATION AND REPAIRED BROKEN MYLAR PER MM 25-22-0. ALODINED AND PRIMED PER SRM 51-10-3. (M) 2 L 7 2 4F A6WE 1997041700792 19970417 00792 WP 1997 4 17 GTIA9700058 1 19961213 A 5321 FLOOR PANEL DOUG DC9 DC931 3022065 WP CABIN DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FLOOR PANEL, AFT CABIN, UPPER SURFACE HAS HOLES, RIVETS PULLED THROUGH AND CRACKS, LOWER SURFACE HAS CRACKS TO FAS TENERS, PROTRUDING UPSET HEADS SHOULD BE FLUSH AND INSULATION TAPE IS LOOSE. REPAIRED HOLE PER SRM 53-05 BY INSTALLING DOUBLER. ALODINED AND PRIMED PER SRM 51-10-3. REPAIRED RIVET BY REMOVING AND REPLACING RIVETS PER SRM 51-30-2. REPAIR ED CRACK TO FASTENERS BY INSTALLING DOUBLER PER SRM 53-05, DRILLED AND COUNTERSUNK HOLES PER SRM 51-10-4 AND INSTALLED P ER SRM 51-30-2. REMOVED RIVET UPSET AND TOUCH COUNTERSUNK AND REINSTALLED RIVETS DOUBLER FLUSH PER SRM 51-30-2. REPAIR ED INSULATION AND LOOSE TAPE PER MM 25-22-0. (M) 2 L 7 2 4F A6WE 1997041700793 19970417 00793 WP 1997 4 17 GTIA9700059 1 19961213 A 5321 FLOOR PANEL DOUG DC9 DC931 3022065 WP CABIN BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FLOOR PANEL 12 HAT CHANNEL SECTION AT ONE END HAS BROKEN OUT ABOUT 1 INCH LONG. OTHER SECTION HAS DEEP GOUGE. RE PAIRED PER 53-21-0. INSTALLED RIVETS PER 51-30-2. BLENDED GOUGE EPR 53-01, REMOVED .008 FROM .040 MATERIAL, WITHIN LIM ITS PER SRM 53-01, TREATED AND PRIMED PER 51-10-3. (M) 2 L 7 2 4F A6WE 1997041700794 19970417 00794 WP 1997 4 17 GTIA9700060 1 19961213 A 5321 FLOOR PANEL DOUG DC9 DC931 3022065 WP CABIN DEFORMED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FLOOR PANEL NR 13, FORWARD END OF PANEL IS DEFORMED, RT HAT CHANNEL IS DELAMINATED AT CTR OF PANEL AND DEFORMED AT AFT END. FOUR CORNERS ARE DELAMINATED AND INSULATION IS MISSING. REPAIR HAT CHANNEL DELAMINATION PER SRM 51-30-3. ST RAIGHTEN PANEL DAMAGE PER SRM 53-01. REPAIR DOUBLERS ON FOUR CORNERS PER MM 53-20-1 (INSULATION IS NOT REQUIRED IN ELEC TRICAL POWER CABLE PANELS REF MM 25-27-0). (M) 2 L 7 2 4F A6WE 1997041700795 19970417 00795 WP 1997 4 17 GTIA9700061 1 19961213 A 5321 FLOOR PANEL DOUG DC9 DC931 3022065 WP CABIN DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - AFT FLOOR PANEL, 1 CORNER IS DELAMINATING AND INSULATION IS MISSING. THERE IS A HOLE IN THE SKIN. FABRICATED A P ATCH FOR THE DAMAGE. ALODINED AND PRIMED PATCH IAW SRM 51-10-3. INSTALLED PATCH IAW SRM 51-30-2. INSTALLED RIVETS IN DELAMINATING CORNER IAW SRM 51-30-2. INSTALLED INSULATION IAW MM 25-22-0, PAGE 201. (M) 2 L 7 2 4F A6WE 1997041700796 19970417 00796 WP 1997 4 17 GTIA9700062 1 19961213 A 5321 FLOOR PANEL DOUG DC9 DC931 3022065 WP CABIN CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FLOOR PANEL 14 FORWARD, ONE CORNER IS CRACKED ABOUT 2 INCHES LONG AND INSULATION BATTING MISSING ALONG ONE EDGE AN D OPPOSITE BATTING IS COMING APART. REPAIRED CORNER PER SRM 55-01, FIG 2. TREATED AND PRIMED PER 51-10-3. INSTALLED F ASTENERS PER 51-30-2. INSTALLED INSULATION PER MM 25-22-0. (M) 2 L 7 2 4F A6WE 1997041700797 19970417 00797 WP 1997 4 17 GTIA9700063 1 19961213 A 5321 FLOOR PANEL DOUG DC9 DC931 3022065 WP CABIN CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FLOOR PANEL NR 16 FORWARD HAS LIGHT CORROSION BETWEEN DOUBLER AND FORWARD END OF PANEL, ALSO, CRACK FROM FASTENER TO OUTSIDE OF PANEL. INSIDE IS MISSING INSULATION AND HAS LOOSE TAPE. BLENDED CORROSION (.002 REMOVED PER 51-10-3, WIT HIN LIMITS PER 51-10-1). FABRICATED AND INSTALLED DOUBLER PER 55-01, FIGURE 2. INSTALLED INSULATION (3 EACH) PER MM 25 -22-0. (M) 2 L 7 2 4F A6WE 1997041700798 19970417 00798 WP 1997 4 17 GTIA9700064 1 19961213 A 5320 FLOOR PANEL DOUG DC9 DC931 3022065 WP CABIN MISSING A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - LEFT OUTBOARD FLOOR PANEL HAS DOUBLER MISSING SOME AREAS DELAMINATING, TWO EACH, SPACER MISSING AT END OF U-CHANNE L. REPLACED MISSING SPACERS AT END OF U-CHANNEL. REBOND DOUBLER PER MM 53-20-1. FABRICATE AND INSTALL NEW DOUBLER PER SRM 53-20-0, FIG 3C SPACERS CEMENTED PER MM 20-20-0. (M) 2 L 7 2 4F A6WE 1997041700799 19970417 00799 WP 1997 4 17 GTIA9700065 1 19961213 A 5321 FLOOR PANEL DOUG DC9 DC931 3022065 WP FUSELAGE DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - RIGHT FORWARD OUTBOARD WING BOX FLOOR PANEL HAS DELAMINATING DOUBLERS, TWO SECTION DOUBLERS MISSING (TWO EACH) SPA CERS MISSING AT END OF U-CHANNEL. REPLACE MISSING SPACERS AT END OF U-CHANNEL. REBOND DOUBLER PER MM 53-20-1. FABRICA TED AND INSTALLED NEW DOUBLERS PER SRM 53-20-0 FIG 3C. SPACERS CEMENTED PER MM 20-20-0. (M) 2 L 7 2 4F A6WE 1997041700800 19970417 00800 WP 1997 4 17 GTIA9700066 1 19961214 A 5321 FLOOR PANEL DOUG DC9 DC931 3022065 WP CABIN CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FLOOR PANEL NR 13, LEFT FORWARD CORNER HAS CRACK. STOP DRILLED CRACK AND BONDED DOUBLER IAW 53-20-1. (M) 2 L 7 2 4F A6WE 1997041700801 19970417 00801 WP 1997 4 17 GTIA9700067 1 19961216 A 5321 FLOOR PANEL DOUG DC9 DC931 3022065 WP LAVATORY CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - LAVATORY FLOOR PANEL NR 8 HAS A CRACK ON RIGHT AFT CORNER, FORWARD SIDE HAS 4 FASTENER HEAD BROKEN. STOP DRILLED CRACK, FABRICATED DOUBLER, INSTALLED DOUBLER IAW 53-01, 53-05, 51-10-3, 51-30-3. (M) 2 L 7 2 4F A6WE 1997041700802 19970417 00802 WP 1997 4 17 GTIA9700068 1 19961216 A 2520 SPRING DOUG DC9 DC931 3022065 WP ATTEND SEAT BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FLIGHT ATTENDANT SEAT, AFT CABIN, RETURN SPRING RIGHT SEAT HINGE IS BROKEN. LUBRICATED HINGE SPRING, INSTALLED RE TURN SPRING SENT FULLY RETRACTS IAW 25-23-21. (M) 2 L 7 2 4F A6WE 1997041700803 19970417 00803 WP 1997 4 17 GTIA9700069 1 19961216 A 5321 FLOOR PANEL DOUG DC9 DC931 3022065 WP CABIN CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FLOOR PANEL NR 17 HAS CRACK AT FORWARD SIDE CENTER BESIDES SCREW HOLES. INSTALLED SKIN DOUBLER IAW 55-01 FIG 2. ( M) 2 L 7 2 4F A6WE 1997041700804 19970417 00804 WP 1997 4 17 GTIA9700070 1 19961216 A 5321 FLOOR PANEL DOUG DC9 DC931 3022065 WP CABIN TORN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FLOOR PANEL AFT CABIN FASTENER HOLE IS TORN OUT AT CORNER. REPAIRED BY FABRICATING RD DOUBLER. ALODINE AND PRIME D PER SRM 51-10-3 AND DRILLED AND COUNTERSUNK PER SRM 51-10-4 AND INSTALLED RIVETS PER SRM 51-30-2. REPAIRED PER SRM 53 -05. (M) 2 L 7 2 4F A6WE 1997041700805 19970417 00805 WP 1997 4 17 GTIA9700071 1 19961216 A 5321 FLOOR PANEL DOUG DC9 DC931 3022065 WP CABIN DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FLOOR PANEL NR 1 HAS DOUBLER DELAMINATION ON SOME AREAS, MYLAR CRACK ON 3 AREAS, DELAMINATED HAT SECTION, NUMEROUS CRACKS IN HAT SECTIONS AND CORROSION. REBONDED PER 53-20-21. DRILLED TACK RIVETS PER 51-10-4. INSTALLED RIVETS PER 5 1-30-3. TREATED CORROSION PER SRM 51-10-3. ALODINED AND PRIMED PER SRM 51-10-3. REPAIRED HAT SECTIONS PER SRM 53-05 F IG 1. (M) 2 L 7 2 4F A6WE 1997041700806 19970417 00806 WP 1997 4 17 GTIA9700072 1 19961216 A 5321 FLOOR PANEL DOUG DC9 DC931 3022065 WP CABIN CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FLOOR PANEL AFT CABIN 15A IS CRACKED ON TOP SURFACE AND ONE HAT CHANNEL IS CRACKED ALONG SAME EDGE. ALSO, AT OPPO SITE END OF WHERE CRACKS ARE INSULATION BATTING UNBONDING AND PROTRUDING BEYOND EDGE. FABRICATED AND INSTALLED HAT CHAN NEL REPAIRS (2) PER SRM 53-05 FIG 1. REPAIR SKIN CRACKS BY STOP DRILLING. FABRICATE AND INSTALL PATCH REPAIR PER SRM 5 5-01 PAGE 7. REPAIR INSULATION BATTING PER MM 25-22-0. (M) 2 L 7 2 4F A6WE 1997041700807 19970417 00807 WP 1997 4 17 GTIA9700073 1 19961217 A 5210 PAN DOUG DC9 DC931 3022065 WP PAX DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - PASSENGER ENTRY DOOR PAN FORWARD LOWER CORNER ON FORWARD SIDE IN CRACK JUST BELOW LOWER HINGE. REMOVED AND REPLAC ED DOOR PAN SEGMENT PER SRM 52-05, 51-10-3, 51-10-4, 51-30-2, 51-30-5, 51-30-7. (M) 2 L 7 2 4F A6WE 1997041700808 19970417 00808 WP 1997 4 17 GTIA9700074 1 19961217 A 5321 FLOOR PANEL DOUG DC9 DC931 3022065 WP CABIN CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FLOOR PANEL HAS BREAK OUT FROM ONE FASTENER HOLE ALONG EDGE AND TWO EACH EDGE STRIPS MISSING. FABRICATED PATCH IA W SRM 55-01. TREATED AND PRIMED PATCH IAW SRM 51-10-03. INSTALLED PATCH WITH RIVETS IAW SRM 51-30-2. FABRICATED EDGE STRIPS IAW MM 53-20-1. INSTALLED AND BONDED WITH SCOTCH GRIP IAW MM 20-20-0. (M) 2 L 7 2 4F A6WE 1997041700809 19970417 00809 WP 1997 4 17 GTIA9700075 1 19961217 A 5310 STRUCTURE DOUG DC9 DC931 3022065 WP FUSELAGE DAMAGED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FLOOR BOARD, WINGS BOX AREA, UPPER AREA HAS SEVERAL CRACKS AND TORN OUT HOLES. HAT CHANNELS HAVE CRACKS AT THE FO RWARD ENDS, INSULATION TAPE IS LOOSE. FLOOR SKIN DAMAGED BEYOND REPAIR. REMOVED FLOORBOARD PANEL SKIN AND FABRICATED N EW PANEL SKIN. REMOVED DAMAGED HAT SECTIONS. FABRICATED 3 HAT SECTIONS AND 3 HAT SECTION DOUBLERS. ALODINED AND PRIME D HAT SECTIONS AND SKIN PANEL PER SRM 51-10-3 REPAIRED FLOORBOARD IAW 53-05 FIG 1. INSTALLED FASTENERS PER SRM 51-30-2 AND 51-30-8. INSTALLED NEW INSULATION PER MM 25-22-0. (M) 2 L 7 2 4F A6WE 1997041700810 19970417 00810 WP 1997 4 17 GTIA9700076 1 19961218 A 5321 FLOORBOARD DOUG DC9 DC931 3022065 WP CABIN CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FLOORBOARD NR 21 HAT SECTIONS CHAFED, CRACKED AND BROKEN OUT. REPAIRED FLOORBOARD IAW 53-05, INSTALLED IAW 51-30- 2. (M) 2 L 7 2 4F A6WE 1997041700811 19970417 00811 WP 1997 4 17 GTIA9700077 1 19961218 A 5321 FLOOR PANEL DOUG DC9 DC931 3022065 WP CABIN CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FLOOR PANEL NR 21 HAS 6 CRACKS IN HAT CHANNELS. REMOVED DAMAGED AREAS, FABRICATED DOUBLERS AND INSTALLED IAW SRM 53-05, 51-10-3, 51-10-4, 53-30-2. (M) 2 L 7 2 4F A6WE 1997041700812 19970417 00812 WP 1997 4 17 GTIA9700078 1 19961218 A 5321 FLOOR PANEL DOUG DC9 DC931 3022065 WP CABIN DELAMINATED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 928ML 47326 MHV - AFT FLOOR PANEL S/N 2686 AND END DELAMINATED ALONG EDGE AND CRACKED IN LOWER ANGLE ALONG DELAMINATION. REPAIRED D ELAMINATION PER SRM 53-05. STOP DRILLED CRACK PER SRM 53-01 AND REPAIRED PER SRM 53-05. FABRICATED REPAIR DOUBLERS PER SRM 53-05. ALODINED AND PRIMED PER SRM 51-10-3. INSTALLED REPAIR DOUBLERS PER SRM 53-05. (M) 2 L 7 2 4F A6WE 1997041700813 19970417 00813 WP 1997 4 17 GTIA9700079 1 19961219 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 69.55 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - DURING NDT INSPECTION OF AIRCRAFT PER SID 53.09.029 CRACKS WERE INDICATED IN THE FUSELAGE SKIN AT 5 RIVETS AT FS 6 9.550 APPROXIMATELY 15 INCH LEFT OF CENTERLINE OF THE AIRCRAFT. INSPECTED FOUND INITIAL REPAIR PER DRAWING SR09530239 W AS IMPROPERLY INSTALLED. RE-REPAIR ACCOMPLISHED PER SRM 53-04 FIG 12B. (M) 2 L 7 2 4F A6WE 1997041700814 19970417 00814 WP 1997 4 17 GTIA9700080 1 19961219 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 929 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FRAME HAS CORROSION AT STATION 929 RBL 62 ZF 6-15. REMOVED CORRODED AREA, FABRICATED NEW SUPPORT BRACKET PER SRM 53-11-3. INSTALLED IAW 51-30-1. (M) 2 L 7 2 4F A6WE 1997041700815 19970417 00815 WP 1997 4 17 GTIA9700081 1 19961219 A 5320 ANGLE DOUG DC9 DC931 3022065 WP BS 180 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FORWARD ACCESSORY COMP AT STATION 180 AT CENTER LINE ABOVE LONGERON 30 ATTACH ANGLE FOR FLOOR SUPPORT IS CRACKED, ALSO ATTACH ANGLE ABOVE 29L IS ALSO CRACKED. FABRICATED ANGLES. REMOVED AND REPLACED ANGLES PER SRM 51-10-02, 51-10-3, AND 51-30-02. (M) 2 L 7 2 4F A6WE 1997041700816 19970417 00816 WP 1997 4 17 GTIA9700082 1 19961219 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 389 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FORWARD CARGO UPPER FLOORBEAM TO SKIN FORWARD SUPPORT IS CRACKED AT STATION 389 RBL 60 2F-6. INSTALLED NEW BRACKE T PER SRM 51-30-3. (M) 2 L 7 2 4F A6WE 1997041700817 19970417 00817 WP 1997 4 17 GTIA9700083 1 19961219 A 5321 FLOOR PANEL DOUG DC9 DC931 3022065 WP CABIN PEELING A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FLOOR PANEL NR 5 MYLAR PEEING, DOUBLER MISSING ON BOTH SIDES AND HAS SOME AREA DELAMINATING. FABRICATED AND INSTA LLED (3) NEW DOUBLERS. REBOND DOUBLERS PER MM 20-20-0. (M) 2 L 7 2 4F A6WE 1997041700818 19970417 00818 WP 1997 4 17 GTIA9700084 1 19961220 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 148-168 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 FLOOR SUPPORT ANGLE RT SIDE STATION 148-168 HAS EXFOLIATION CORROSION OUT OF LIMITS. REMOVED DAMAGED AREA FLOOR SUPPORT ANGLES, FABRICATE DOUBLERS AND FILLERS IAW SRM 53-01 FIG 2. INSTALLED IAW 51-30-2. (M) 2 L 7 2 4F A6WE 1997041700819 19970417 00819 WP 1997 4 17 GTIA9700085 1 19961220 A 7120 MOUNT DOUG DC9 DC931 3022065 WP NR 1 ENGINE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - NR 1 ENGINE AFT MOUNT FILLING HAS SURFACE CORROSION. REMOVED AND REPLACED NR 1 AFT VIBRATION ISOLATOR IAW 71-20-2 . (M) 2 L 7 2 4F A6WE 1997041700820 19970417 00820 WP 1997 4 17 GTIA9700086 1 19961220 A 5753 PANEL DOUG DC9 DC931 3022065 WP LT TE FLAP CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - LEFT WING LOWER FLAP AREA NR L-2 BUTTE PANEL HAS A LARGE CRACK. REPAIRED HONEY COMB PANEL PER SRM 57-04, DOUBLER INSTALLED PER SRM 57-04 AND 57-30. (M) 2 L 7 2 4F A6WE 1997041700821 19970417 00821 WP 1997 4 17 GTIA9700087 1 19961220 A 5531 RIB DOUG DC9 DC931 3022065 WP VERT STAB CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - VERTICAL STABILIZER LE PANEL RT SIDE HAS 5 RIBS CRACKED THROUGH FASTENER HOLES AT EDGE OF PANEL. LEFT SIDE HAS 3 RIBS CRACKED THROUGH FASTENER HOLES AT EDGE OF PANEL. FABRICATED AND INSTALLED PARTS IAW 55-02 FIG 14, 51-10-3, 51-20- 0, 51-30-0. ALL CRACKS STOP DRILLED. (M) 2 L 7 2 4F A6WE 1997041700822 19970417 00822 WP 1997 4 17 GTIA9700088 1 19961220 A 5320 ANGLE DOUG DC9 DC931 3022065 WP BS 150 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - COCKPIT OVERHEAD, FORWARD TOP MOUNT OF EPC LBL 12.5 ANGLE IS CRACKED FS 150. REPLACED NEW BRACKET IAW 53-01-0, 20 -16-0. (M) 2 L 7 2 4F A6WE 1997041700867 19970417 00867 EU 1997 4 17 REXA96037 1 19960828 A 3350 6104781 BATTERY GRIMES SAAB SF340 340B 7860101 EU CABIN DISCHARGED A REXA A UNSCHED LANDING L NO TEST IN INSP/MAINT 1 SO 25 370PX 340B300 EMERGENCY LIGHTS 58 LN, 59 LN, 60 LN, 41 LN, AND 39 LN ARE OUT. REMOVED AND REPLACED LIGHT BATTERIES AT LOCATIONS, 23LN , AND 24LN, S/N ELB071, ELB092. OPERATIONAL CHECKED GOOD. AIRCRAFT OK FOR CONTINUED SERVICE. (M) 2 L 7 2 4T RT A52EU 1997041700868 19970417 00868 EU 1997 4 17 REXA96051 1 19961016 A 3310 BACKLIGHTING BAG JETSTM JETSTM3101 1500215 EU RT GLARESHIELD SMOKING A REXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 25 330PX 698 FIRST OFFICERS BACKLIGHTING FLICKERED. THEN SMOKE BEGAN TO EMANATE FROM THE FIRST OFFICERS SKIRT PANEL AND GLARESHIELD. EMERGENCY WAS DECLARED, LANDED WITHOUT INCIDENT. DRIED DASH AND REPAIRED WIRING UNDER DASH. (M) 2 L 7 2 4T RT A21EU 1997041700869 19970417 00869 EU 1997 4 17 REXA96050 1 19961014 A 2150 AIR CONDITIONING SAAB SF340 SF340A 7850100 EU CABIN MALFUNCTIONED A REXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 25 321PX 340A031 SMOKE IN CABIN. AFT FREON A/C FOUND AT FAULT. DEFERRED (DMI16716) PER MEL 25-60-05. (M) 2 L 7 2 4T RT A52EU 1997041700870 19970417 00870 EU 1997 4 17 REXA96049 1 19961014 A 3350 BATTERIES BAG JETSTM JETSTM3101 1500215 EU CABIN DISCHARGED A REXA K NONE L NO TEST IN INSP/MAINT 1 SO 25 333PX 704 FORWARD TWO OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED FORWARD EMERGENCY BATTERIES. F/C IS GOOD (DS01 78033). (M) 2 L 7 2 4T RT A21EU 1997041700871 19970417 00871 WP 1997 4 17 REXA96059 2 19961023 A 7510 31998061 SHUTOFF VALVE BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110U 01514 WP LT ANTI-ICE FAILED A REXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 311PX 679 LEFT ANTI-ICE STOPPED WORKING AFTER TAKEOFF. REMOVED AND REPLACED LEFT ANTI-ICE SOLENOID SHUTOFF VALVE. OPS CHECK GOOD . (M) 2 L 7 2 4T 4 T RT A21EU E4WE 1997041700933 19970417 00933 WP 1997 4 17 GTIA9700089 1 19961220 A 5320 DOOR BEAM DOUG DC9 DC931 3022065 WP CARGO DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - AFT CARGO DOOR BEAM NR 1 AFT ATTACH ANGLE CRACKED. REPAIR PER SRM 51-10-4, 51-30-5, 51-30-1 (NEW PART INSTALLED). (M) 2 L 7 2 4F A6WE 1997041700934 19970417 00934 WP 1997 4 17 GTIA9700090 1 19961224 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 600 MIS INSTALLED A GTIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 928ML 47326 MHV - STATION 600 LONGERON 30 SKIN REPAIR NOT PER SRM 53-04 FIG 12B. FINGER DOUBLERS NOT INSTALLED. INSTALLED FINGER D OUBLERS AS PER SRM 53-04 PAGE 35 FIG 12B. (M) 2 L 7 2 4F A6WE 1997041700936 19970417 00936 WP 1997 4 17 GTIA9700092 1 19961227 A 5347 SEAT TRACK DOUG DC9 DC931 3022065 WP BS 200-230 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FORWARD CABIN SEAT TRACK AT RBL 22 FS 200 THROUGH 230 AT STATION 200 HAS CRACKS, DRILL START AND CORROSION. REMOV ED OLD SENT TRACK, FABRICATED AND INSTALLED NEW SEAT TRACK IAW 51-10-3, 51-10-2 AND 53-05. (M) 2 L 7 2 4F A6WE 1997041700937 19970417 00937 WP 1997 4 17 GTIA9700093 1 19961230 A 5310 STRUCTURE DOUG DC9 DC931 3022065 WP BS 598-550 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FWD CARGO COMPT FROM FS 598 TO FS 550 LONGERONS 28 LT, 29 LT, 30 CENTER, AND 29 RT, ATTACH ANGLES, SPLICE PLATE, A ND INTERIOR SKIN CORRODED. REMOVED SURFACE CORROSION (IN LIMITS). ALODINE AND PRIMED AREA IAW SRM 51-10-3. LONGERON A ND SPLICE INSULATION TRANS TO JOB C00029. REINSTALLED AIR DUCT AND RESAFETIED WIRE PER MM 28-189-0. CORROSION ON SKIN OF .065, REMOVED .002 MATERIAL IN LIMITS PER 53-01. CORROSION ON STRUCTURE OF .175, REMOVED .002 MATERIAL IN LIMITS PER 53-01. NEW REPAIR COMPLETED WITH EXTERNAL DOUBLER AND INTERNAL FINGER DOUBLER AS PER SRM 53-04 PAGE 35 FIG 12B. (M) 2 L 7 2 4F A6WE 1997042200008 19970422 00008 EA 1997 4 22 CA961120011 2 19961107 A 7322 25244405 FUEL CONTRL UNIT DHAV DHC6 DHC6300 EA PWA PT6 PT6A27 52043 EA #2 ENGINE FAULTY W O OTHER O OTHER AP APPROACH 1 CA 5503 PCE40068 (CAN) ON APPROACH IT WAS NOTICED THE FUEL FLOW FLUCTUATED WHEN THE POWER WAS RETARDED ON THE #2 ENGINE. ALL OTHER #2 ENG INE PARAMETERS WERE NORMAL. AFTER LANDING AND PASSENGERS DEPLANING AN ENGINE GROUND RUN WAS CARRIED OUT. WHEN THE POWER LEVER WAS ADVANCED BEYOND FLIGHT IDLE THE FUEL FLOW WOULD FLUCTUATE AND A POPPING SOUND COULD BE HEARD FROM THE #2 ENGIN E. THE #2 ENGINE FUEL CONTROL UNIT AND THE ENGINE FUEL PUMP WERE REPLACED AND THE ENGINE GROUND RUN SERVICEABLE. THE FCU AND FUEL PUMP WERE SENT FOR INSPECTION AND INVESTIGATION. 1 H 7 2 3T 4 T A9EA E4EA 1997042200010 19970422 00010 EA 1997 4 22 CA961125003 1 19961114 A 2730 MS2104205 BOLT DHAV 82710306101 DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE TORQUE TUBE LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA 12294 123144 (CAN) BOLTS AND NUTS FOUND LOOSE ON DISCONNECT ASSEMBLY CLUTCH. SEE IPC 27-34-00, FIG.10 ITEM #80, 90, 100, 110, 120, 13 0. NUTS AND BOLTS TIGHTENED. FLEET CHECK BEING CARRIED OUT. 2 H 7 2 4T 4 T RT A13NM E20NE 1997042200011 19970422 00011 NM 1997 4 22 CA961125004 1 19961114 A 3320 BA080061 BALLAST BRUCE DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE CABIN ROW 9 SHORTED W K NONE B M SMOKE/FUMES/ODORS/SPARKS OVER TEMP IN INSP/MAINT 1 CA 6863 123039 (CAN) MAINTENANCE PERSONNEL NOTICED A STRONG BURNING ELECTRICAL SMELL ON ENTERING AIRCRAFT CABIN. SMELL TRACED TO ROW 9, OVERHEAD LEFT HAND CABIN LIGHT BALLAST. 2 H 7 2 4T 4 T RT A13NM E20NE 1997042200013 19970422 00013 WP 1997 4 22 CA961125006 1 19961113 A 3260 0331881001 LIGHT BASE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE GEAR LIGHTS SHORTED W K NONE O OTHER CR CRUISE 1 CA P657314D (CAN) SHORTLY AFTER SELECTING GEAR UP, RIGHT MAIN LANDING GEAR LIGHT CAME ON. (GEAR UNSAFE LIGHT OUT) LANDING RECYCLED L IGHT WENT OUT. AFTER ANOTHER SHORT PERIOD LEFT GEAR LIGHT CAME ON AND THEN WENT OUT. NORMAL LANDING CARRIED OUT. MAINTEN ANCE CHECK REVEALED NOSE GEAR LIGHT AND RH GEAR LIGHT RECEPTACLE BASES FAULTY. BOTH LIGHT BASES REPLACED. RETRACTION TES T CARRIED OUT SERVICEABLE. 2 L 7 2 4F 4 F A6WE E2EA 1997042200014 19970422 00014 WP 1997 4 22 CA961125007 1 19961116 A 3260 SWITCH DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE RT MLG DOWNLOCK BROKEN WIRE W O OTHER P NO WARNING INDICATION AP APPROACH 1 CA P657239D (CAN) RIGHT LANDING GREEN LIGHT DID NOT ILLUMINATE ON APPROACH. MAINTENANCE CHECK FOUND BROKEN WIRE AT RH MAIN LANDING D OWN LOCK SWITCH. BROKEN WIRE REPAIRED. 2 L 7 2 4F 4 F A6WE E2EA 1997042200015 19970422 00015 WP 1997 4 22 CA961125008 1 19961116 A 7830 THRUST REVERSER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE LT ENG INTERMITTENT W K NONE O OTHER LD LANDING 1 CA P657053D (CAN) LEFT ENGINE REVERSE UNLOCK LIGHT REMAINS ON AFTER DEPLOYMENT. RECYCLED REVERSER SEVERAL TIMES WITH NO CHANGE. MAIN TENANCE ACTION INVOLVED ADJUSTING LH THRUST REVERSER LATCH AND SYSTEM CHECKED SERVICEABLE. 2 L 7 2 4F 4 F A6WE E2EA 1997042400131 19970424 00131 WP 1997 4 24 ABXA9700703 1 19961010 A 5730 59127372 PANEL DOUG DC9 DC941 302207N WP WS 509 DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 WHILE COMPLYING WITH ACCEPTANCE INSPECTION, FOUND THE RIGHT WING UPPER TRAILING EDGE BONDED PANEL FORWARD OF AILERON DEL AMINATED AND CORRODED. REMOVED AND REPLACED RIGHT WING TRAILING EDGE PANEL IAW DC-9 CHAPTERS 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 1997042400132 19970424 00132 WP 1997 4 24 ABXA9700704 1 19961010 A 5730 59127352 PANEL DOUG DC9 DC941 302207N WP WS 531 DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 DURING ACCEPTANCE INSPECTION, FOUND THE RIGHT WING OUTBOARD TRAILING EDGE PANEL FORWARD OF AILERON DELAMINATED AND CORRO DED. REPLACED RIGHT WING OUTBOARD TRAILING EDGE PANEL IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 1997042400133 19970424 00133 WP 1997 4 24 ABXA9700705 1 19961011 A 5320 59107842 JAMB DOUG DC9 DC941 302207N WP BS 756 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 DURING ACCEPTANCE INSPECTION, FOUND THE RIGHT MLG WHEEL WELL DOOR JAMB CRACKED INBOARD OF HYDRAULIC SUMP JAR. REPAIRED RIGHT MLG DOOR JAMB IAW ABX REA D953-16723. 2 L 7 2 4F A6WE 1997042400134 19970424 00134 WP 1997 4 24 ABXA9700706 1 19960920 A 5730 59127371 PANEL DOUG DC9 DC941 302207N WP WS 509 DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 DURING ACCEPTANCE INSPECTION, FOUND THE LEFT WING UPPER TRAILING EDGE BONDED PANEL OUTBOARD OF SPOILER DELAMINATED. REP LACED TRAILING EDGE PANEL IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 1997042400135 19970424 00135 WP 1997 4 24 ABXA9700707 1 19961008 A 5711 5911300501 SPAR CAP DOUG DC9 DC941 302207N WP WS 137 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 DURING ACCEPTANCE INSPECTION FOUND THE LEFT WING UPPER SPAR CAPS CORRODED ON THE AFT TANG AT WS XRS 137. REPAIRED IAW A BX REA D957-16496-MR. 2 L 7 2 4F A6WE 1997042400136 19970424 00136 WP 1997 4 24 ABXA9700708 1 19961008 A 5711 5911300501 SPAR CAP DOUG DC9 DC941 302207N WP WS 137 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 DURING ACCEPTANCE INSPECTION, FOUND THE RIGHT WING UPPER SPAR CAPS CORRODED ON THE AFT TANG AT WS XRS 137. REPAIRED IAW ABX REA 957-16496-MR. 2 L 7 2 4F A6WE 1997042400137 19970424 00137 WP 1997 4 24 ABXA9700709 1 19961009 A 5711 59113581 SPAR CAR DOUG DC9 DC941 302207N WP WS 137.5 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 DURING ACCEPTANCE INSPECTION, FOUND THE LEFT WING REAR TEE CAP DOUBLER CORRODED. REPAIRED LEFT WING REAR SPAR CAP IAW A BX REA D957-16504-MR. 2 L 7 2 4F A6WE 1997042400138 19970424 00138 WP 1997 4 24 ABXA9700710 1 19961015 A 5314 991073735 KEEL BEAM DOUG DC9 DC941 302207N WP BS 660 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 DURING ACCEPTANCE INSPECTION, FOUND THE BUTT LINE O KEEL BEAM UPPER CAP SEVERELY CORRODED AT FS 660. REPAIRED KEEL BEAM UPPER CAP IAW ABX REA D953-16673-MR. 2 L 7 2 4F A6WE 1997042400139 19970424 00139 WP 1997 4 24 ABXA9700711 1 19961022 A 5531 591138456 SPAR CAP DOUG DC9 DC941 302207N WP VERT STAB CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 DURING ACCEPTANCE INSPECTION, FOUND THE VERTICAL STABILIZER REAR SPAR CAPS CORRODED AT STATIONS ZRS 4, 8 AND 10. REPAIR ED VERTICAL STAB REAR SPAR CAPS IAW ABX REA D957-16873-MR. 2 L 7 2 4F A6WE 1997042400140 19970424 00140 WP 1997 4 24 ABXA9700712 1 19961018 A 5512 591062579 SKIN DOUG DC9 DC941 302207N WP HORIZ STAB ERODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 DURING ACCEPTANCE INSPECTION, FOUND THE LEFT HORIZONTAL STABILIZER LEADING EDGE SKINS ERODED. REPAIRED LEFT HORIZONTAL STAB LEADING EDGE SKINS IAW ABX REA D955-16859-MR. 2 L 7 2 4F A6WE 1997042400141 19970424 00141 WP 1997 4 24 ABXA9700713 1 19961014 A 5712 SS0957000321 RIB DOUG DC9 DC941 302207N WP WS 509.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 DURING ACCEPTANCE INSPECTION, FOUND THE OUTBOARD LEFT WING LEADING EDGE RIB AT SLAT TRACK NR 10 CRACKED. REMOVED AND RE PLACED LEADING EDGE RIB IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1997042400142 19970424 00142 WP 1997 4 24 ABXA9700714 1 19961008 A 5712 SS095700035 RIB DOUG DC9 DC941 302207N WP WS 111.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 DURING ACCEPTANCE INSPECTION, FOUND THE LEFT WING LEADING EDGE RIB AT SLAT TRACK NR 2 CRACKED. REMOVED AND REPLACED RIB IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1997042400144 19970424 00144 WP 1997 4 24 ABXA9700716 1 19961226 A 2760 3923250503 DRIVE LINK DOUG DC9 DC932 3022066 WP RT SPOILER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 DURING C-CHECK, FOUND RIGHT WING OUTBOARD SPOILER DRIVE LINK CRACKED, (AD 85-01-03, 90-18-03). REPLACED DRIVE LINK IAW DC-9 MAINTENANCE MANUAL CHAPTERS 27-61-1 AND 27-61-2. 2 L 7 2 4F A6WE 1997042400145 19970424 00145 WP 1997 4 24 ABXA9700717 1 19961227 A 5280 5933787505 HINGE DOUG DC9 DC932 3022066 WP RT MLG DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 DURING C-CHECK, FOUND RIGHT FLYING DOOR HINGE LOBE CRACKED FOR ARTICULATING DOOR, (AD 91-22-07). REPLACED WING MOUNTED GEAR DOOR, AND ATTACH FITTING IAW DC-9 SRM CHAPTERS 51-30-1. 2 L 7 2 4F A6WE 1997042400147 19970424 00147 WP 1997 4 24 ABXA9700719 1 19961229 A 5320 3916217501 FITTING DOUG DC9 DC932 3022066 WP BS 699 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 DURING C-CHECK, FOUND CRACKED FITTING AT STA 699 IN LEFT WHEEL WELL, (AD 92-22-08). REPLACED FITTING IAW DC-9 SRM CHAPT ER 51-30-5. 2 L 7 2 4F A6WE 1997042400255 19970424 00255 WP 1997 4 24 ABXA9700802 1 19961211 A 5755 5910055513 SPOILER DOUG DC9 DC941 302207N WP LT WING DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 966AX 47510 DURING C-CHECK, THE INBOARD SPOILER PANEL AT THE CENTER HINGE WAS FOUND DELAMINATED. THE SPOILER WAS REPLACED IAW DC9 M M. 2 L 7 2 4F A6WE 1997042400256 19970424 00256 WP 1997 4 24 ABXA9700803 1 19961211 A 5320 9917701 INTERCOSTAL DOUG DC9 DC941 302207N WP BS 1244 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 966AX 47510 DURING C-CHECK, THE LT INTERCOSTAL AT CANTED FRAME STA 1244 WAS FOUND CRACKED. THE INTERCOSTAL WAS REPLACED IAW DC9 SRM . 2 L 7 2 4F A6WE 1997042400304 19970424 00304 WP 1997 4 24 97ZZZX1761 1 19961111 A 5315 FLOOR BEAM DOUG DC9 DC932 3022066 WP BS 980 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEDULED INSPECTION AT AERO CORP., THE AFT CARGO PIT CABIN FLOOR BEAM AT STA 980 WAS FOUND CORRODED AT BL 34R. MECHANICALLY REMOVED CORROSION TO .075 INCH, FOUND TO BE OUT OF LIMITS IAW DC9 SRM 53-05 FIG 20A. CUT OUT CORRODED AR EA FROM RBL 18 TO RBL 43 IAW DC9 SRM 53-05 FIG 20A. FABBED REPAIR ANGLE FROM 7075T6511 EXTRUSION .156 INCH BY .125 INCH BY 34.5 INCHES IAW DC9 53-05, FIG 20A VIEW A-A. FABBED FILLER FROM 7075T6 .100 INCH BY 1 INCH BY 25.3750 INCHES AND WE AR STRIP FROM FULL HARD .025 INCH BY 1 INCH BY 25.3750 INCHES IAW DC9 SRM 53-05, FIGURE 20A. ALODINED AND PRIMED PARTS IAW DC9 SRM 51-10-2. INSTALLED REPAIR IAW DC9 SRM 53-05, FIG 20A. 2 L 7 2 4F A6WE 1997042400305 19970424 00305 WP 1997 4 24 97ZZZX1762 1 19961111 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 110/160 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEDULED INSPECTION AT AERO CORP., LONGERON 27R WAS FOUND CORRODED FROM STA 110 TO STA 160. BLENDED OUT CHAFE MARKS IAW DC9 SRM 53-01, FIG 2. MATERIAL OUT OF LIMITS IAW DC9 SRM 53-01, FIG 2. PERFORMED FIBERGLASS REPAIR OF INTER IOR MOLDING PANELS IAW DC9 SRM 53-01, FIG 3. FABRICATED NEW SEAL DEPRESSOR AND FRAME DOUBLER IAW DC-9 SRM 52-10-2. TRE ATED AND PRIMED IAW DC9 SRM 51-10-3. INSTALLED DOOR STOPS IAW DC9 SRM 52-11-00. 2 L 7 2 4F A6WE 1997042400306 19970424 00306 WP 1997 4 24 97ZZZX1763 1 19961204 A 5400 1A194251 WEB DOUG DC9 DC932 3022066 WP NR 2 PYLON CRACKED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND NR 2 PYLON CRACK ON DOUBLER JUST FORWARD OF AFT ENGIN E MOUNT. REMOVED DOUBLER AND WEB. FABBED AND INSTALLED NEW WEB IAW DC9 SRM'S 51-10-2, 54-10-0, AND 51-30-2. 2 L 7 2 4F A6WE 1997042400307 19970424 00307 WP 1997 4 24 97ZZZX1764 1 19961208 A 5532 SKIN DOUG DC9 DC932 3022066 WP VERT STAB CHAFED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND LT VERTICAL SKIN CHAFED AT BANNANA FAIRING. BLENDED OUT CHAFE MARKS IAW DC9 SRM 51-10-3. VERIFIED OUT OF LIMITS PER DC9 SRM 55-01 FIG 1. REMOVED PANEL IAW DC9 SRM 51-30-2 . FABBED NEW SKIN (2024-0.050) IAW DC9 SRM 51-10-2. HEAT TREATED PART IAW DC9 SRM 51-10 FIG 2A. FABBED NEW DOUBLER (2 014-T6.025 25 INCHES BY 11.50 INCHES) IAW DC9 SRM 51-10-2. TRIMMED, DRILLED, AND DEBURRED NEW PARTS IAW DC9 SRM 51-10-4 . BONDED DOUBLER TO SKIN PER SRM 51-20-3. ALODINED AND PRIMED PARTS IAW DC9 SRM 5T1-10-3. INSTALLED PANEL PER SRM 51- 30-2. 2 L 7 2 4F A6WE 1997042400308 19970424 00308 WP 1997 4 24 97ZZZX1765 1 19961127 A 5347 S291491313500N SEAT TRACK DOUG DC9 DC932 3022066 WP BS 200-240 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL,THE LT SEAT TRACK INBOARD, STA 200 - STA 240, WAS FOUND CORR ODED BEYOND LIMITS. REMOVED CORRODED SECTION OF TRACK, FABBED AND INSTALLED NEW SECTION AND SPLICE IAW DC9 SRM'S 51-30- 1, 51-30-2, 51-10-3, AND 53-05, FIG 10G. 2 L 7 2 4F A6WE 1997042400309 19970424 00309 WP 1997 4 24 97ZZZX1766 1 19961122 A 5315 S291275812006 FLOOR BEAM DOUG DC9 DC932 3022066 WP BS 996 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, STA 997 FL6OR BEAM CHAFED AND CORRODED FROM RBL 48 TO LBL 4 8. REMOVED FLOOR BEAM ANGLE, INSTALLED NEW ANGLE IAW DC9 SRM'S 53-11-3 FIG 11, 51-10-4, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1997042400310 19970424 00310 WP 1997 4 24 97ZZZX1767 1 19961122 A 5313 1A4150 LONGERON DOUG DC9 DC932 3022066 WP BS 645 CRACKED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND .75 INCH CRACK AT FASTENER HOLE LONGERON 12R STA 645. REMOVED CRACKED AREA. FABBED AND INSTALLED 2 EACH STACKED ANGLE REPAIRS IAW DC9 SRM'S 53-01 FIG 2 AND 51-10-3. 2 L 7 2 4F A6WE 1997042400311 19970424 00311 WP 1997 4 24 97ZZZX1768 1 19961203 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 645 CRACKED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND .75 INCH CRACK AT FASTENER HOLE LONGERON 12L STA 645. REMOVED CRACKED AREA, FABRICATED 2 EACH STACKED ANGLE REPAIRS IA-4150-2 2024-T3 .040 INCH 5 INCHES BY 2 INCHES IAW DC 9 SRM 53-01 FIG 2. TREATED AND PRIMED IAW DC9 SRM 51-10-3. INSTALLED ANGLE REPAIRS IAW DC9 SRM 530-01 FIG 2. 2 L 7 2 4F A6WE 1997042400312 19970424 00312 WP 1997 4 24 97ZZZX1769 1 19961114 A 5312 991556531 DOOR FRAME DOUG DC9 DC932 3022066 WP AFT ENTRY APB CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, AFT ENTRY DOOR HAS CORROSION ON BOTTOM FRAME. REMOVED CORR ODED CHANNEL. INSTALLED NEW CHANNEL IAW DC9 SRM'S 51-30-5, 51-10-4, AND 51-10-3. 2 L 7 2 4F A6WE 1997042400313 19970424 00313 WP 1997 4 24 97ZZZX1770 1 19961115 A 5320 HAT SECTION DOUG DC9 DC932 3022066 WP BS 965 CRACKED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND AFT CABIN FLOOR AREA HAS HAT SECTION FLOOR SUPPORT CR ACKED AND CORRODED AT STA 965 BL ZERO TO RT BL 24. FABBED NEW ANGLE SPLICE PER DC9 SRM 53-11-3, PAGE 3. ALODINED AND T REATED AREA. INSTALLED ANGLE SPLICE IAW DC9 SRM 51-30-3. NEW ANGLE SPLICE 7075-T6, .040 INCH. 2 L 7 2 4F A6WE 1997042400314 19970424 00314 WP 1997 4 24 97ZZZX1771 1 19961111 A 5321 FLOOR PANEL DOUG DC9 DC932 3022066 WP COCKPIT CORROSION A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEDULED INSPECTION AT AERO CORP, CORROSION FOUND ON THE COCKPIT FLOOR CENTER PANEL. REMOVED CENTER COCKPIT F LOOR IAW DC9 SRM 51-30-1, MECHANICALLY REMOVED CORROSION FROM HAT SECTIONS. LESS THAN .001 INCH REMOVED, FOUND WITHIN L IMITS IAW DC9 SRM 51-10-3. ALODINED AND PRIMED HAT SECTIONS IAW DC9 SRM 51-10-3. FABBED FLOOR PANEL OF 7075T-6 .040 IN CH 30 INCHES BY 20 INCHES BY 39 INCHES IAW DC9 SRM 51-10-2. ALODINED AND PRIMED FLOOR PANEL IAW DC9 SRM 51-10-3. ASSEM BLED FLOOR PANEL AND HAT SECTIONS IAW DC9 SRM 51-30-1. INSTALLED IN A/C IAW DC9 SRM 51-30-10. 2 L 7 2 4F A6WE 1997042400315 19970424 00315 WP 1997 4 24 97ZZZX1772 1 19961111 A 5320 SUBFLOOR DOUG DC9 DC932 3022066 WP BS 130/140 CORROSION A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEDULED INSPECTION AT AERO CORP, CORROSION WAS FOUND ON THE SUB-FLOOR BETWEEN STA 130 AND STA 140 BL 13R. RE MOVED CORRODED AREA, FABBED UP DOUBLER AND FILLER IAW DC9 SRM 51-10-4. ALODINED AND PRIMED IAW DC9 SRM 51-10-3. INSTAL LED DOUBLER AND FILLER IAW DC9 SRM 51-30-2. (MATERIAL DIMENSIONS 28.75 INCHES BY 2.75 INCHES, 2 EACH.) 2 L 7 2 4F A6WE 1997042400316 19970424 00316 WP 1997 4 24 97ZZZX1773 1 19961111 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 160/180 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEDULED INSPECTION AT AERO CORP, FOUND LONGERON 28L AND INTERCOSTAL CORRODED BETWEEN STA 160 AND STA 180. RE MOVED INTERCOSTAL IAW DC9 SRM 51-30-2, MECHANICALLY REMOVED CORROSION IAW DC9 SRM 51-10-3. MATERIAL LOSS LESS THAN .005 INCH (DEPTH GAUGE NR A-0358) WITHIN LIMITS IAW DC9 SRM 53-1 FIG 1. ALODINED AND PRIMED IAW DC9 SRM 51-10-3. REINSTALL ED INTERCOSTAL IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1997042400317 19970424 00317 WP 1997 4 24 97ZZZX1774 1 19961111 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 180/200 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEDULED INSPECTION AT AERO CORP, FOUND LONGERON 28L CORRODED STA 180 - STA 200. MECHANICALLY REMOVED CORROSI ON IAW DC9 SRM 51-10-3. MATERIAL LOSS LESS THAN .002 INCH (DEPTH GAUGE NR A-0299) WITHIN LIMITS IAW DC9 SRM 53-01 FIG 1 , ALODINED AND PRIMED IAW DC9 SRM 51-10-3. 2 L 7 2 4F A6WE 1997042400319 19970424 00319 WP 1997 4 24 97ZZZX1776 1 19961111 A 5320 VERTICAL BEAM DOUG DC9 DC932 3022066 WP BS 218 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEDULED INSPECTION AT AERO CORP, FOUND VERTICAL BEAM AT STA 218 LONGERON 30 CORRODED. MECHANICALLY REMOVED C ORROSION IAW DC9 SRM 51-10-3, MATERIAL LOSS LESS THAN .003 INCH (DEPTH GAUGE NR A-0299) WITHIN LIMITS IAW DC9 SRM 53-01 FIG 1, ALODINED AND PRIMED IAW DC9 SRM 51-10-3. 2 L 7 2 4F A6WE 1997042400320 19970424 00320 WP 1997 4 24 97ZZZX1777 1 19961111 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 120 CORROSION A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEDULED INSPECTION AT AERO CORP, CORROSION WAS FOUND ON THE FRAME AT STA 120 AT 28L TO LONGERON 28R. REMOVED CORROSION, ALODINED AND PRIMED IAW DC9 SRM 51-10-3 AND SRM 53-02 FIG 1. MATERIAL LOSS LESS THAN .005 INCH, NDT METHOD DME NR A-1244. 2 L 7 2 4F A6WE 1997042400321 19970424 00321 WP 1997 4 24 97ZZZX1778 1 19961111 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 130/160 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEDULED INSPECTION AT AERO CORP, FOUND FRAMES STA 130 AND STA 160 CORRODED BETWEEN LONGERON 28L AND LONGERON 28R. MECHANICALLY REMOVED CORROSION IAW DC9 SRM 51-10-3, MATERIAL LOSS LESS THAN .003 INCH (DEPTH GAUGE NR A-0299) WITH IN LIMITS IAW DC9 SRM 53-01 FIG 1. ALODINED AND PRIMED IAW DC9 SRM 51-10-3. 2 L 7 2 4F A6WE 1997042400322 19970424 00322 WP 1997 4 24 97ZZZX1779 1 19961111 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 996 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEDULED INSPECTION AT AERO CORP, THE AFT CARGO PIT, SUPPORT FRAME ABOVE LONGERON 30 AT STA 996 IS CORRODED. M ECHANICALLY REMOVED CORROSION FROM STR 23R TO STR 23L. LESS THAN .002 INCH MATERIAL LOSS. WITHIN LIMITS IAW DC9 SRM 51 -10-3 AND SRM 53-01 FIG 1. TREATED AND PRIMED IAW DC9 SRM 51-10-3. 2 L 7 2 4F A6WE 1997042400323 19970424 00323 WP 1997 4 24 97ZZZX1780 1 19961107 A 5313 STRINGER DOUG DC9 DC932 3022066 WP BS 945/965 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEDULED INSPECTION AT AERO CORP, FOUND STR 29R CORRODED, STA 945 TO STA 965. MECHANICALLY REMOVED CORROSION FROM STRINGER AND INTERCOSTAL, P/N 99582339. STRINGER WITHIN LIMITS, INTERCOSTAL REPLACED IAW DC9 SRM'S 51-10-3, 51-10 -4, AND 51-30-5. 2 L 7 2 4F A6WE 1997042400324 19970424 00324 WP 1997 4 24 97ZZZX1781 1 19961106 A 5313 591141253N LONGERON DOUG DC9 DC932 3022066 WP BS 400 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEDULED INSPECTION AT AERO CORP, FOUND LONGERON 29L CORRODED BETWEEN STA 389 - STA 408 AROUND NUTPLATES FOR R ADIO ALTIMETER NR 1. REMOVED LONGERON 29L AND 30 FOR ACCESS TO CORROSION. UPON REMOVAL OF LONGERON 30, A 5 INCH CRACK WAS FOUND IN THE FACTORY SPLICE. FABBED AND INSTALLED LONGERON 30, LONGERON SPLICES 29L AND 30, AND INSTALLED NEW ALTIM ETER DOUBLER IAW DC9 SRM'S 51-10-3, 53-01 FIG 1, AND DOUGLAS DWG NR 5911412. 2 L 7 2 4F A6WE 1997042400325 19970424 00325 WP 1997 4 24 97ZZZX1782 1 19961106 A 5315 FLOOR BEAM DOUG DC9 DC932 3022066 WP BS 218 AND 237 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEDULED INSPECTION AT AERO CORP, AT FS 218 TO FS 237 BL ZERO THE FLOOR BEAM WAS FOUND WITH CORROSION. REMOVE D CORRODED T-CAP, FABBED AND INSTALLED H-CHANNEL, L-ANGLE, 2 EACH IAW DC9 SRM'S 53-01 FIG 2, 51-30-2 AND 51-10-3. 2 L 7 2 4F A6WE 1997042400326 19970424 00326 WP 1997 4 24 97ZZZX1783 1 19961111 A 5310 STRUCTURE DOUG DC9 DC932 3022066 WP BS 590 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEDULED INSPECTION AT AERO CORP, CORROSION FOUND AROUND NUTPLATES ON LT AND RT KIDNEY PANELS (AFT OF AUXILIAR Y FUEL TANK). REMOVED STR'S 30, 29R, 29L, 28R, 28L, 27R, 27L, 26R, 26L, INTERCOSTALS 26L AND 27L, AND 26R AND 27R, FRAM ES 580, 585, 600, AND CAPS 27L, 27R, 28L, 28R, AND DOUBLER. UPON CLEANING, FOUND CRACKS. FABBED FRAME CLIP AND HEAT T REATED IAW 51-10-2A. FABBED NEW SKIN DOUBLER AND FILLER IAW SRM 51-10-2 AND EO 96-397. ALODINED AND PRIMED DOUBLER, TR IPLER, FILLER, AND SKIN FILLER. TREATED AND PRIMED FRAME SPLICE. INSTALLED STR'S 27L/R, 28L/R IAW DC-9 SRM 51-30-2 AND SRM 51-30-5 AND EO 96-397. INSTALLED LONGERONS 29L/R, 28L/R, 27L/R, AND 26L/R IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1997042400327 19970424 00327 WP 1997 4 24 97ZZZX1784 1 19961207 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 583 CRACKED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND THE LONGERON 24L END FITTING SPLICE HAD A 6 INCH CRAC K AT STA 583. REMOVED END FITTING SPLICE L24L IAW DC9 SRM 51-30-2. INSTALLED NEW END FITTING IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1997042400328 19970424 00328 WP 1997 4 24 97ZZZX1785 1 19961202 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 522 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND THE FORWARD CARGO PIT FRAME AT STA 522 CORRODED BEYON D LIMITS, FRAMES S28R TO S29L. FABBED REPAIR FILLER 7075-0 .071 INCH, AND REPAIRED DOUBLER 7075-0 .071 INCH. APPROXIMA TE DIMENSIONS OF DOUBLER 2 INCHES BY 34 INCHES, FILLER 1 INCH BY 20 INCHES. HEAT TREATED AND ROCKWELL TESTED 51-10-2A. DRILLED UP, DOUBLER AND FILLER IAW DC9 SRM 51-10-1. ALODINED AND PRIMED IAW DC9 SRM 51-10-3. INSTALLED FILLER AND DOU BLER IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1997042400477 19970424 00477 WP 1997 4 24 ABXA9700874 1 19961216 A 5753 5910041503 VANE DOUG DC9 DC941 302207N WP LT TE FLAP DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 960AX 47762 THE LEFT INBOARD FIXED FLAP VANE WAS DELAMINATED IN THE UPPER MID-AREA. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997042400478 19970424 00478 WP 1997 4 24 ABXA9700875 1 19961121 A 5752 59100511 TAB DOUG DC9 DC933F 302207A WP LT AILERON DENTED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 THE LEFT AILERON TAB HAD NUMEROUS DENTS ON BOTH THE UPPER AND LOWER SURFACES. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997042400480 19970424 00480 WP 1997 4 24 ABXA9700877 1 19961008 A 5755 5910055516 SPOILER DOUG DC9 DC941 302207N WP RT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 THE RIGHT OUTBOARD SPOILER HAD WIDESPREAD CORROSION. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997042400481 19970424 00481 WP 1997 4 24 ABXA9700878 1 19961218 A 5755 5910055515 SPOILER DOUG DC9 DC941 302207N WP LT WING DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 960AX 47762 THE LEFT INBOARD SPOILER HAD SEVERAL AREAS OF DELAMINATION. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SR M. 2 L 7 2 4F A6WE 1997042400487 19970424 00487 WP 1997 4 24 ABXA9700884 1 19961009 A 5755 5910055516 SPOILER DOUG DC9 DC941 302207N WP RT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 THE RIGHT WING OUTBOARD SPOILER HAD SEVERAL AREAS OF CORROSION. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC- 9 SRM. 2 L 7 2 4F A6WE 1997042400488 19970424 00488 WP 1997 4 24 ABXA9700885 1 19961127 A 5753 5910040510 VANE DOUG DC9 DC941 302207N WP RT TE FLAP CRACK A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 960AX 47762 THE RIGHT WING AFT FLAP VANE HAD CRACK AT THE INBOARD RIB. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM . 2 L 7 2 4F A6WE 1997042400489 19970424 00489 WP 1997 4 24 ABXA9700886 1 19960912 A 5543 5910257501 TAB DOUG DC9 DC933F 302207A WP RUDDER DENTED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 934AX 47462 THE RUDDER TAB HAD 2 LARGE DENTS TO THE OUTER SURFACE. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997042400490 19970424 00490 WP 1997 4 24 ABXA9700887 1 19960818 A 5753 59121681 VANE DOUG DC9 DC931 3022065 WP RT TE FLAP DENTED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 THE RIGHT WING FORWARD FLAP VANE HAD LARGE DENTS TO THE UPPER SURFACE. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997042400491 19970424 00491 WP 1997 4 24 ABXA9700888 1 19960826 A 5755 5910055515 SPOILER DOUG DC9 DC931 3022065 WP LT WING DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 THE LEFT WING SPOILER WAS DELAMINATED ALONG THE ENTIRE TRAILING EDGE. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS I AW DC-9 SRM. 2 L 7 2 4F A6WE 1997042400492 19970424 00492 WP 1997 4 24 ABXA9700889 1 19960827 A 5543 5910257501 TAB DOUG DC9 DC931 3022065 WP RUDDER CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 THE RUDDER TAB HAD HEAVY CORROSION ON THE LEADING EDGE. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997042400493 19970424 00493 WP 1997 4 24 ABXA9700890 1 19960914 A 5523 5910413503 TAB DOUG DC9 DC933F 302207A WP LT ELEVATOR DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 934AX 47462 THE LEFT ELEVATOR TAB WAS DELAMINATED ON THE INBOARD TRAILING EDGE. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997042400494 19970424 00494 WP 1997 4 24 ABXA9700891 1 19960919 A 5753 5910040518 VANE DOUG DC9 DC941 302207N WP RT TE FLAP DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 990AX 47493 THE RIGHT WING AFT FLAP VANE WAS DELAMINATED ON INBOARD TRAILING EDGE. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997042400495 19970424 00495 WP 1997 4 24 ABXA9700892 1 19960904 A 5753 5910042504 VANE DOUG DC9 DC931 3022065 WP RT TE FLAP DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 THE RIGHT WING CENTER FIXED FLAP VANE WAS DELAMINATED 75 PERCENT OVERALL. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKI NS IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997042400496 19970424 00496 WP 1997 4 24 ABXA9700893 1 19960815 A 5753 59100401 VANE DOUG DC9 DC931 3022065 WP LT TE FLAP DENTED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 THE LEFT WING AFT MOVEABLE VANE HAD A LARGE AREA OF THE UPPER SURFACE DENTED. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997042400497 19970424 00497 WP 1997 4 24 ABXA9700894 1 19961107 A 5752 59100512 TAB DOUG DC9 DC915 3022036 WP RT AILERON DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 927AX 45717 THE RIGHT AILERON TAB INBOARD TRAILING EDGE CORNER WAS DELAMINATED. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997042400498 19970424 00498 WP 1997 4 24 ABXA9700895 1 19960920 A 5753 5910041501 VANE DOUG DC9 DC941 302207N WP LT TE FLAP CHAFED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 990AX 47493 THE LEFT WING INBOARD FIXED FLAP VANE WAS HEAVILY CHAFFED AND DAMAGED ON BOTH THE UPPER AND LOWER INBOARD EDGE. REPLACE D ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997042400499 19970424 00499 WP 1997 4 24 ABXA9700896 1 19961125 A 5752 59100471 TAB DOUG DC9 DC933F 302207A WP LT AILERON DENTED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 THE LEFT WING AILERON CONTROL TAB HAD SEVERAL DENTS ON THE UPPER SURFACE. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKI NS IAW DC-9 SRM. 2 L 7 2 4F A6WE 1997042400503 19970424 00503 WP 1997 4 24 ABXA9700901 1 19961201 A 5230 591014119 DOOR DOUG DC9 DC933F 302207A WP CARGO COMPT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 WHILE COMPLYING WITH C INSPECTION, FOUND THE FORWARD LOWER CARGO DOOR INNER SKIN CRACKED AND BENT AT FORWARD HINGE. REM OVED AND REPLACED FORWARD BAG BIN DOOR IAW ABX JOB CARD C-3088. 2 L 7 2 4F A6WE 1997042400504 19970424 00504 WP 1997 4 24 ABXA9700902 1 19961202 A 5230 591014119 DOOR DOUG DC9 DC933F 302207A WP CARGO COMPT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 WHILE COMPLYING WITH C INSPECTION, FOUND A CRACKED FITTING INSIDE THE FORWARD LOWER CARGO DOOR NEAR FORWARD HINGE. REMO VED AND REPLACED FORWARD BAG BIN DOOR IAW ABX JOB CARD C-3088. 2 L 7 2 4F A6WE 1997042400505 19970424 00505 WP 1997 4 24 ABXA9700903 1 19961202 A 5230 591014119 DOOR DOUG DC9 DC933F 302207A WP CARGO COMPT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 WHILE COMPLYING WITH C INSPECTION, FOUND THE FORWARD LOWER CARGO COMPARTMENT DOOR PAN CRACKED AT THE UPPER FORWARD STOP. REPLACED FORWARD LOWER CARGO COMPARTMENT DOOR IAW ABX JOB CARD C-3088. 2 L 7 2 4F A6WE 1997042400515 19970424 00515 WP 1997 4 24 ABXA9700915 1 19960807 A 5753 5910041501 VANE DOUG DC9 DC931 3022065 WP LT TE FLAP CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 LEFT INBOARD FIXED VANE SKIN WORN AND CORRODED. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN. 2 L 7 2 4F A6WE 1997042400566 19970424 00566 WP 1997 4 24 GTIA9700113 1 19961206 A 5320 ANGLE DOUG DC9 DC931 3022065 WP BS 217 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FORWARD ACC COMP, FLOOR SUPPORT ANGLE AT FS STATION 217 HAS SEVERAL CORRODED CLIPNUTS AND LIGHT CORROSION ON BOTTO M SIDE. REMOVED AND REPLACED ANGLE AND CLIPNUTS IAW SRM 51-30-2, 51-30-8. (M) 2 L 7 2 4F A6WE 1997042400569 19970424 00569 WP 1997 4 24 GTIA9700116 1 19961205 A 5320 ANGLE DOUG DC9 DC931 3022065 WP BS 237 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FLOOR SUPPORT REPAIR HAS CORROSION AT STATION 218 BL 0 ZF-1 AND STATION 237 BL 0 ZF-1. REMOVED AND REPLACED CORR ODED ANGLES, NEW ANGLES WERE FABRICATED AND INSTALLED IAW 51-30-2, 51-10-3, 51-10-4, 51-30-0, AND 53-03 FIG 3. (M) 2 L 7 2 4F A6WE 1997042400577 19970424 00577 WP 1997 4 24 GTIA9700117 1 19961104 A 5320 JAMB DOUG DC9 DC931 3022065 WP SERVICE DOOR CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FORWARD CABIN R-1 SERVICE DOOR LOWER THRESHOLD HAS EXFOLIATION CORROSION INSIDE. REMOVED SURFACE CORROSION. FOUN D TO BE WITHIN LIMITS PER SRM 51-10-3 (FS 150-FS 237). (M) 2 L 7 2 4F A6WE 1997042400578 19970424 00578 WP 1997 4 24 GTIA9700118 1 19961206 A 5321 FLOOR DOUG DC9 DC931 3022065 WP BS 902/908 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FLOOR WEB HAS CORROSION AT STATION 902 RBL 59 ZF1 AND STATION 908 RBL 59 HAS EVIDENCE OF CORROSION BETWEEN WEBS. F ABRICATED AND REPLACED CORRODED WEB IAW 51-10-3/51-30-0. (M) 2 L 7 2 4F A6WE 1997042400579 19970424 00579 WP 1997 4 24 GTIA9700119 1 19961206 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 945 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FRAME HAS CORROSION AT STATION 945 RBL 61 AND 63 AF1 AND 3. FABRICATED AND INSTALLED NEW WEB IAW 51-10-2 AND 51-3 0-0. (M) 2 L 7 2 4F A6WE 1997042400581 19970424 00581 WP 1997 4 24 GTIA9700121 1 19961119 A 5321 FLOOR PANEL DOUG DC9 DC931 3022065 WP LAVATORY CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FORWARD LAV FLOOR PANEL HAS SURFACE CORROSION AND NUMEROUS RIVET HEADS. REMOVED DAMAGED AREA, FABRICATED FILLER A ND DOUBLER INSTALLED IAW 51-10-3, 53-05 FIG 1, 51-30-2. (M) 2 L 7 2 4F A6WE 1997042400582 19970424 00582 WP 1997 4 24 GTIA9700122 1 19961216 A 7120 ENGINE MOUNT DOUG DC9 DC931 3022065 WP NR 2 ENGINE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - NR 2 ENGINE PYLON AFT MOUNT HAS SURFACE CORROSION ON OUTER SURFACE. REMOVED AND REPLACED NR 2 ENGINE AFT VIBRATIO N ISOLATER AND LINK IAW 71-20-2. (M) 2 L 7 2 4F A6WE 1997042400583 19970424 00583 WP 1997 4 24 GTIA9700123 1 19961126 A 5313 LONGERON DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - LONGERON IN 3RD LEFT SIDE BAY FOR AFT BULKHEAD OF AFT PIT IS CORRODED HAS ABOUT 8 INCHES SECTION OF EXFOLIATION. F ABRICATED, TREATED, FINISHED, AND INSTALLED A NEW STIFFENER PER THE FOLLOWING SRM'S 51-10-0, 51-10-3, AND 51-30-4. (M) 2 L 7 2 4F A6WE 1997042400584 19970424 00584 WP 1997 4 24 GTIA9700124 1 19961206 A 5260 AIR STAIR DOUG DC9 DC931 3022065 WP AFT FUSELAGE MIS REPAIRED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - PERFORM REPAIR PER DOUGLAS SERVICE REWORK DRAWING SR09530219 (STAIR DOOR AREA). REMOVED TEMP REPAIR, FABRICATED N EW DOUBLERS AND FILLER IAW SRM 53-05-17A. INSTALLED PER DRAWINGS SR09530031 AND SR09530219. (M) 2 L 7 2 4F A6WE 1997042400585 19970424 00585 WP 1997 4 24 GTIA9700125 1 19961207 A 5313 STRINGER DOUG DC9 DC931 3022065 WP CARGO DOOR CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - NUMEROUS PATCHES OF SURFACE CORROSION ALONG TOP OF RIGHT STRINGER FORWARD OF AFT CARGO DOOR TO FORWARD BULKHEAD OF AFT PIT. SECTION CLOSEST TO CARGO DOR IS DELAMINATING. REMOVED BOTH ENDS, FABRICATED AND INSTALLED (2) SPLICES AND (2 ) ENDS IAW SRM 53-02. REMOVED CORROSION FROM CHANNEL IAW SRM 51-10-3 (.0005 REMOVED WITHIN LIMITS). ALODINED AND PRIME D AREAS IAW SRM 51-10-3. INSTALLED CHANNEL COMPLETE IAW SRM 51-30-2. (M) 2 L 7 2 4F A6WE 1997042400586 19970424 00586 WP 1997 4 24 GTIA9700126 1 19961208 A 5311 FRAME DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - SURFACE CORROSION ON FORWARD SIDE OF FRAME 1ST IN FRONT OF AFT PIT AFT BULKHEAD BETWEEN LONGERON 30 AND 29. FABRI CATED NEW SECTION OF RIB AND FILLER. REMOVED CORROSION OFF OF FRAME THAT WAS WITHIN LIMITS. REMOVED 2.70 BY 80 SECTION OF FRAME THAT WAS OUT OF LIMITS. ALODINED AND PRIMED FRAME AND FABRICATED PARTS. INSTALLED FABRICATED PARTS PER SRM 5 3-01 FIG 1, 51-10-3, 53-04 PAG 191, 51-30-2, AND 51-30-5. (M) 2 L 7 2 4F A6WE 1997042400587 19970424 00587 WP 1997 4 24 GTIA9700127 1 19961209 A 5312 BULKHEAD FRAME DOUG DC9 DC931 3022065 WP AFT PRESS BLKHD CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - AFT PRESSURE BULKHEAD RT SIDE 4TH HORIZONTAL BULKHEAD FRAME UP FROM CABIN FLOOR PANEL IS CRACKED AT OUTBOARD END. STOP DRILLED CRACK, FABRICATED DOUBLERS AND INSTALLED IAW 51-10-2, 51-10-3, 53-01 FIG 2. (M) 2 L 7 2 4F A6WE 1997042400588 19970424 00588 WP 1997 4 24 GTIA9700128 1 19961209 A 5312 BULKHEAD FRAME DOUG DC9 DC931 3022065 WP AFT PRESS BLKHD CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - AFT PRESSURE BULKHEAD RIGHT SIDE, 1ST 2ND, 3RD HORIZONTAL BULKHEAD FRAMES UP FROM CABIN FLOOR LEVEL ARE CRACKED. S TOP DRILLED CRACKS, FABRICATED DOUBLERS AND INSTALL IAW 53-01 FIG 2. (M) 2 L 7 2 4F A6WE 1997042400589 19970424 00589 WP 1997 4 24 GTIA9700129 1 19961209 A 5313 LONGERON DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - SURFACE CORROSION WITH EXFOLIATION ON LONGERON DIRECTLY BENEATH OUTFLOW VALVE IN AFT PIT, RIB ANGLE IN FRONT OF OU TFLOW VALVE HAS SURFACE CORROSION DOWN AND TO RT OF VALVE. REMOVED CORRODED STRAP, FABRICATED NEW PART ALODINED, PRIMED , AND INSTALLED IAW SRM 51-10-1, 51-10-3, 51-30-4. REMOVED CORROSION PER SRM 51-10-3 (WAS .040, IS .039, WITHIN LIMITS PER SRM 53-01 FIG 1. ALODINED AND PRIMED PER SRM 51-10-3. (M) 2 L 7 2 4F A6WE 1997042400590 19970424 00590 WP 1997 4 24 GTIA9700130 1 19961213 A 5320 HAT CHANNEL DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - PANEL NR 24, HAT CHANNEL AT AFT END OF PANEL HAS CRACKED OUT FASTENER HOLE. REPAIRED HAT CHANNEL IAW SRM 53-05, 5 1-10-3. (M) 2 L 7 2 4F A6WE 1997042400591 19970424 00591 WP 1997 4 24 GTIA9700131 1 19961216 A 5312 BULKHEAD FRAME DOUG DC9 DC931 3022065 WP AFT PRESS BLKHD CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - AFT PRESS BULKHEAD LEFT SIDE, THE 1ST AND 2ND HORIZONTAL FRAMES UP FROM CABIN FLOOR LEVEL ARE CRACKED. STOP DRILL ED CRACKS. FABRICATED DOUBLER AND CLIPS PER SRM 51-01. INSTALLED PER 53-01 FIG 2, 51-10-3. (M) 2 L 7 2 4F A6WE 1997042400592 19970424 00592 WP 1997 4 24 GTIA9700132 1 19961223 A 5230 FITTING DOUG DC9 DC931 3022065 WP CARGO DOOR CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - AFT CARGO DOOR AFT EDGE GUIDE FITTINGS AND FASTENERS CORRODED. AFT DOOR EDGE SPACER CORRODED. BEAM 5 UPPER FORWA RD ATTACH ANGLE, 1 FASTENER CORRODED. REMOVED AND REPLACED GUIDE FITTINGS PER SRM'S 52-30-4 AND 20-31. REMOVED CORROSI ON WITHIN LIMITS PER SRM 52-01 PAGE 5 (.002 MATERIAL REMOVED). REMOVED AND REPLACED FASTENER PER SRM 51-30-5. (M) 2 L 7 2 4F A6WE 1997042400593 19970424 00593 WP 1997 4 24 GTIA9700133 1 19961230 A 5240 DOOR DOUG DC9 DC931 3022065 WP LAV SERVICE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - AFT LAVATORY SERVICE PANEL, LEFT SIDE OF A/C, HAS EXFOLIATION CORROSION. REMOVED AND REPLACED AFT LAVATORY SERVIC E DOOR IAW MM 38-30-0. INSTALLED COMPLETE, TRIMMED TO FIT ALODINED, AND PRIMED IAW SRM 51-10-3. (M) 2 L 7 2 4F A6WE 1997042400609 19970424 00609 WP 1997 4 24 GTIA970008 1 19961114 A 5242 DOUBLER DOUG DC9 DC931 3022065 WP E/E DOOR NOT INSTALLED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - REPAIR AFT OF E/E DOOR AT STATION 257 NOT IN COMPLIANCE WITH SRM 53-04, FIG 12B. NO FINGER DOUBLER INSTALLED. IN STALLED NEW FINGER DOUBLER PER SRM 53-04, FIG 12B. (M) 2 L 7 2 4F A6WE 1997042400610 19970424 00610 WP 1997 4 24 GTIA9700009 1 19961114 A 5321 FLOOR PANEL DOUG DC9 DC931 3022065 WP BS 160-198 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FORWARD CABIN FLOOR PANEL INBOARD OF L1 DOOR FS 160 TO 198 HAS A HOLE WITH A CRACK NEXT TO COCKPIT DOOR CUTOUT, LI GHT CORROSION LEVEL 1. FABRICATED REPAIR IAW SRM 51-21-0, FIG 1. REPAIRED PANEL IAW SRM 53-05, 51-10-3. (M) 2 L 7 2 4F A6WE 1997042400611 19970424 00611 WP 1997 4 24 GTIA9700010 1 19961114 A 5320 DOUBLERS DOUG DC9 DC931 3022065 WP BS 332 NOT INSTALLED A GTIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 928ML 47326 MHV - STATION 332 LONGERON 30 REPAIR ON ANTENNA IS MISSING FINGER DOUBLERS BOTH SIDES. REMOVED OLD DOUBLER, FABRICATED INTERNAL DOUBLER AND EXTERNAL DOUBLER IAW SRM 53-04, INSTALLED PARTS SRM 51-30-2, 51-30-5, 53-04. (M) 2 L 7 2 4F A6WE 1997042400612 19970424 00612 WP 1997 4 24 GTIA9700011 1 19961115 A 5321 FLOOR PANEL DOUG DC9 DC931 3022065 WP BS 200-237 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FORWARD CABIN FLOOR PANEL RBL 20 TO 43 FS 200 TO 237 HAS DENT WITH CRACKS AND UNDER SIDE HAS A CRACK ON PANEL STRI NGER. REPAIRED FLOOR PANEL IAW SRM 53-01, FIG 2 SRM 53-05 FIG 1, 51-10-03. (M) 2 L 7 2 4F A6WE 1997042400613 19970424 00613 WP 1997 4 24 GTIA9700012 1 19961115 A 7110 STIFFENER DOUG DC9 DC931 3022065 WP NR 1 ENGINE COWL CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - NR 1 ENGINE NOSE COWL HAS A STIFFENER WITH A DAMAGED AND CRACKED FLANGE AT AFT EDGE OF COWL. REMOVED OLD STIFFENE R AND FABRICATED AND INSTALLED NEW STIFFENER IAW 51-01-01 AND 51-02-01. (M) 2 L 7 2 4F A6WE 1997042400614 19970424 00614 WP 1997 4 24 GTIA9700013 1 19961118 A 5280 DOUBLER DOUG DC9 DC931 3022065 WP NLG DOOR CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - REPAIR ON NOSE GEAR LT HINGED DOOR EXTERNAL REPAIR NEEDS INSPECTION TO VERIFY COMPLIANCE WITH SRM 53-05 FIG 62. S TOP DRILLED CRACK, FABRICATED NEW DOUBLER, INSTALLED IAW 53-05 FIG 62. (M) 2 L 7 2 4F A6WE 1997042400615 19970424 00615 WP 1997 4 24 GTIA9700014 1 19961118 A 5320 ANGLE DOUG DC9 DC931 3022065 WP BS 598 LOOSE RIVETS A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - RIGHT WING FUSELAGE STATION 598, UPPER WING ATTACH ANGLE HAS LOOSE RIVETS C/T NUTPLATE. FORMED AND INSTALLED NEW DOUBLER IAW 53-01, FIGURE 2. (M) 2 L 7 2 4F A6WE 1997042400616 19970424 00616 WP 1997 4 24 GTIA9700015 1 19961121 A 5320 STIFFENER DOUG DC9 DC931 3022065 WP CABIN CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - FLOORBOARD NR 6 FOR FORWARD CABIN HAS A STIFFENER CRACKED. REPAIRED HAT SECTION IAW 53-05 FIG 1, 51-10-3, 51-30-2 , 51-30-8. (M) 2 L 7 2 4F A6WE 1997042400617 19970424 00617 WP 1997 4 24 GTIA9700016 1 19961121 A 5321 FLOOR DOUG DC9 DC931 3022065 WP BS 820-830 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - SURFACE CORROSION ON FLOOR WEB AT STATION 820-830 RBL 59 ZF1. REMOVED DAMAGE AREA, FABRICATED NEW WEB. INSTALLED IAW 53-05, 51-10-3. (M) 2 L 7 2 4F A6WE 1997042400618 19970424 00618 WP 1997 4 24 GTIA9700017 1 19961121 A 5321 FLOOR PANEL DOUG DC9 DC931 3022065 WP BS 699-737 DELAMINATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MHV - RIGHT FLOOR PANEL STATION 699-737 DOUBLER DELAMINATION ON SOME AREA. REATTACHED PER MM 53-20-1. REBONDED FIBERGL ASS PER MM 53-20-1. (M) 2 L 7 2 4F A6WE 1997042400660 19970424 00660 NM 1997 4 24 97ZZZM503 1 19960913 A 5711 SPAR CAP BOEING 727 7272J7 138400E NM WS 738.5 CORRODED A ULHF K NONE O OTHER IN INSP/MAINT 1 SO 23 553NA 20707 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND RT WING STATION 738.5 LEFT FORWARD LOWER SPAR CAP CORROD ED. FOUND TO BE IN LIMIT. 2 L 7 3 4F A3WE 1997042400661 19970424 00661 NM 1997 4 24 97ZZZM504 1 19960906 A 7110 COWL BOEING 727 7272J7 138400E NM NR 3 ENGINE CRACKED A ULHF K NONE O OTHER IN INSP/MAINT 1 SO 23 553NA 20707 NR 3 ENGINE FIXED COWL FORWARD UPPER OUTER SKIN IS CRACKED 3 INCHES IN LENGTH 3H. REMOVED SECTION OF UPPER FORWARD OUTE R SKIN 21 INCHES BY 1.3125 INCHES BY 11.25 INCHES FROM NR 3 ENGINE FIXED COWLING. FABRICATED NEW SECTION OF SKIN OUT OF 2024-T3 .032. DRILLED NEW SECTION OF SKIN AND COUNTERSUNK AND DEBURRED. TREATED AND PRIMED, INSTALLED REPAIR IAW SRM 51-10-1, 51-10-2, 51-10-6 AND FED EX DRAWING IM-72753HW. 2 L 7 3 4F A3WE 1997042400662 19970424 00662 NM 1997 4 24 97ZZZM505 1 19960913 A 3233 FITTING BOEING 727 7272J7 138400E NM NLG CORRODED A ULHF K NONE O OTHER IN INSP/MAINT 1 SO 23 553NA 20707 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND NLG ACTUATOR ATTACH FITTING (AIRFRAME) CORRODED LT SIDE OUTBOARD. REMOVED NLG ATTACH FITTING FROM 2.799 TO 2.845. FABRICATED BUSHINGS TO 2.84700 (.002 INTERFENCE FIT). INSTA LLED BUSHING WET WITH PRIMER IAW B727 SRM 53-40-1. 2 L 7 3 4F A3WE 1997042400663 19970424 00663 NM 1997 4 24 97ZZZM506 1 19960904 A 5730 SKIN BOEING 727 7272J7 138400E NM WS 170-760 CORRODED A ULHF K NONE O OTHER IN INSP/MAINT 1 SO 23 553NA 20707 RIGHT WING UPPER LEFT END SKIN CORRODED AT MOUNT SCREWS FROM WS 170-760 FORWARD AND AFT CHORD. ACCOMPLISHED CORROSION R EMOVAL ON RIGHT WING UPPER LT SPAR IAW SRM 51-10-6. INSTALLED TWO REPAIRS AT W/S NR 3 AND NR 4, 16 AND 18 BETWEEN W/S 1 90 AND 332. REPAIR PARTS 2 1.2 INCH BY 4 INCH, 2 - 3 INCH BY 10 INCH, 2 - 2.3 INCH BY 2.8 INCH, 2 - 4.5 INCH BY 8 INCH , 2 - 4.2 INCH BY 3.2 INCH. FABRICATED 2 T-CLIPS IAW RES1 NR 0345. ALODINED AND PRIMED IAW SRM 51-10-2 AND MM 51-20-11 . INSTALLED REPAIR IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1997042400664 19970424 00664 NM 1997 4 24 97ZZZM507 1 19960913 A 5711 SPAR BOEING 727 7272J7 138400E NM WS 629 CORRODED A ULHF K NONE O OTHER IN INSP/MAINT 1 SO 23 553NA 20707 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND RT WING STATION 629, L/E SPAR CORRODED AT ACTUATOR ARM N R 7. FOUND TO BE IN LIMITS. 2 L 7 3 4F A3WE 1997042400665 19970424 00665 NM 1997 4 24 97ZZZM508 1 19960913 A 5711 SPAR BOEING 727 7272J7 138400E NM WS 546.5 CORRODED A ULHF K NONE O OTHER IN INSP/MAINT 1 SO 23 553NA 20707 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND RIGHT WING STATION 546.5 L/E SPAR CORRODED FORWARD OF NR 4 SLAT ACTUATOR ARM. FOUND TO BE IN LIMITS. 2 L 7 3 4F A3WE 1997042400666 19970424 00666 NM 1997 4 24 97ZZZM509 1 19960904 A 5711 SPAR BOEING 727 7272J7 138400E NM WS 616.5 CORRODED A ULHF K NONE O OTHER IN INSP/MAINT 1 SO 23 553NA 20707 WING STATION LEADING EDGE SPAR JUST FORWARD OF NR 2 SLAT ACT ROD HAS CORROSION AT 3 INCHES LONGERON. MECH REMOVED CORRO SION AT WING STATION 616.5 LE SPAR IAW SRM 51-10-6. REMOVED AT .024 METAL 6 INCHES LONG ORIGINAL THICKNESS .225 MAX OUT ALLOWABLE .012 OUT OF LIMITS IAW SRM 57-10-1. NO DEFECTS NOTED PER EDDY CURRENT. FLAP PEENED IAW SRM SOP 20-10-3. TR EATED AND PRIMED IAW SRM 51-10-2 AND MM 51-20-11. 2 L 7 3 4F A3WE 1997042400667 19970424 00667 NM 1997 4 24 97ZZZM510 1 19960913 A 5311 SPAR BOEING 727 7272J7 138400E NM WS 383 CORRODED A ULHF K NONE O OTHER IN INSP/MAINT 1 SO 23 553NA 20707 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND LT WING STATION 383 L/E SPAR AT NR 4 SLAT FORWARD OF ACT UATOR ROD CORRODED APPROXIMATELY 18 INCHES IN LENGTH. MECH REMOVED CORROSION AT LEFT WING L/E SPAR IAW SRM 51-10-6. RE MOVED AT .058 18 INCHES LONG ORIGINAL THICKNESS .0240 MAX ALLOWABLE .012 OUT OF LIMITS IAW SRM 57-10-1. FLAP PEENED ARE AS IAW B727 SOP 20-10-3. TREATED AND PRIMED IAW SRM 51-10-2 AND MM 51-20-11. 2 L 7 3 4F A3WE 1997042400668 19970424 00668 NM 1997 4 24 97ZZZM511 1 19960913 A 5711 SPAR BOEING 727 7272J7 138400E NM WS 491.5 CORRODED A ULHF K NONE O OTHER IN INSP/MAINT 1 SO 23 553NA 20707 DURING SCHEDULED INSPECTION AT AERO COP IN LAKE CITY, FL, FOUND LT WING STATION 491.5 L/E SPAR AFT OF NR 4 SLAT ACTUATOR CORRODED APPROX 6 INCHES IN LENGTH. MECH REMOVED CORROSION AT WS 491.5 L/E SPAR IAW B727-SRM 51-10-6. REMOVED AT .091 METAL 14 INCHES ORIGINAL THICKNESS .024 MAX ALLOWABLE LIMIT .012 OUT OF LIMITS IAW SRM 57-10-2. FLAP PEENED AREAS IAW B727 SOP 20-10-3. TREATED AND PRIMED IAW SRM 51-10-2. 2 L 7 3 4F A3WE 1997042400669 19970424 00669 NM 1997 4 24 97ZZZM512 1 19960904 A 5753 SKIN BOEING 727 7272J7 138400E NM LT TE MIDFLAP DELAMINATED A ULHF K NONE O OTHER IN INSP/MAINT 1 SO 23 553NA 20707 ON THE UPPER SURFACE T/E OF THE INBD MID-FLAP ON ITS OUTBD T/E THE FLAP HAS BECOME DELAMINATED. ALSO, AT TWO OTHER SMAL LER SPOTS ON ITS MIDDLE T/E OF THE SAME FLAP. REMOVED LT INBD FLAP IAW MM 27-51-31. REMOVED DELAMINATED SKIN AND CRUSH ED HONEYCOMB IAW SRM 51-40-9. FABRICATED AND INSTALLED HONEYCOMB REPLACEMENTS IAW SRM 51-40-6. FABRICATED AND INSTALLE D SKIN REPLACEMENTS IAW SRM 51-40-6. REMOVED, FABRICATED AND INSTALLED 2 CHAF STRIPS IAW SRM 51-20-1 AND 51-40-6. REMO VED AND REPLACED 8 BEARINGS IAW MM 20-40-1. REINSTALLED FLAP, RIGGED FLAPS, CHECKED GOOD. 2 L 7 3 4F A3WE 1997042400670 19970424 00670 NM 1997 4 24 97ZZZM513 1 19960904 A 5754 SKIN BOEING 727 7272J7 138400E NM NR 5 LE SLAT CORRODED A ULHF K NONE O OTHER IN INSP/MAINT 1 SO 23 553NA 20707 RIGHT WING LEADING EDGE 5 SLAT HAS CORROSION UNDER PANEL SS128. MECH REMOVED CORROSION AND TR WING LEADING EDGE SPAR IA W SRM 51-10-6. REMOVED AT .088 METAL ORIGINAL THICKNESS .360 MATERIAL ALLOWABLE .012 OUT OF LIMIT IAW SRM 57-10-1. NO CRACKS NOTED BY EDDY CURRENT. FLAP PEENED AREAS IAW B727 SOP 20-10-3. TREATED ADN PRIMED IAW SRM 51-10-2 AND MM 51-10- 11. 2 L 7 3 4F A3WE 1997042400671 19970424 00671 NM 1997 4 24 97ZZZM514 1 19960913 A 5712 RIB BOEING 727 7272J7 138400E NM WS 738.5 CRACKED A ULHF K NONE O OTHER IN INSP/MAINT 1 SO 23 553NA 20707 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND RT WING STATION 738.5 LOWER RIB FLANGE IS CRACKED AT ST RINGER NR 8 ATTACH POINT. STOP DRILLED CRACK IAW B 727 SRM 51-10-1. FABRICATED CHANNEL FROM 7075-0 .080 4 INCH BY 15 I NCH IAW B727 SRM 57-10-5. HEAT TREATED TO 7075-T6. DRILLED AND TRIMMED TO FIT AND DEBURRED IAW 51-10-5. TREATED AND P RIMED IAW SRM 51-10-2. INSTALLED REPAIR CHANNEL IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1997042400672 19970424 00672 NM 1997 4 24 97ZZZM515 1 19960917 A 8012 CONTROL VALVE BOEING 727 7272J7 138400E NM NR 1 ENG STARTER CHAFED A ULHF K NONE O OTHER IN INSP/MAINT 1 SO 23 553NA 20707 NR 1 ENGINE STARTER CONTROL VALVE CHAFED AND COVER BROKE AT CORNERS. REMOVED AND REPLACED STARTER CONTROL VALVE IAW B72 7 80-11-11. LEAK CHECKED OK. LOG PAGE 6465. 2 L 7 3 4F A3WE 1997042400673 19970424 00673 NM 1997 4 24 97ZZZM516 1 19960913 A 5755 FITTING BOEING 727 7272J7 138400E NM NR 5 SPOILER CRACKED A ULHF K NONE O OTHER IN INSP/MAINT 1 SO 23 553NA 20707 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND LT WING NR 5 SPOILER ACTUATOR FITTING IS CRACKED 2 PLAC ES. REMOVED AND REPLACED FITTING IAW SRM 51-30-2 AND 51-10-1. REMOVED AND REINSTALLED SPOILER PANEL TO FOM IAW MM 27-1 0-2. OPS CHECKED GOOD. 2 L 7 3 4F A3WE 1997042400674 19970424 00674 NM 1997 4 24 97ZZZM517 1 19960903 A 5753 SKIN BOEING 727 7272J7 138400E NM RT TE FLAP CORRODED A ULHF K NONE O OTHER IN INSP/MAINT 1 SO 23 553NA 20707 RIGHT WING OUTBOARD FLAP, THE AFT FLAP HAS A CORRODED AREA AT 9 FEET FROM THE OUTBOARD END. REMOVED CORROSION, REVEALED PUNCTURE HOLE IN FLAP FULL OF FILLER. CUT OUT CORRODED AREA. REQUIRES COMPOSITE REPAIR. CLEANED OUT OLD POTTING MATE RIAL. PRIMED AREA IAW 51-10-2 AND MM 51-20-2. POTTED REPAIR SANDED SMOOTH IAW SRM 51-40-6. PRIMED REPAIR AREA IAW SRM AND MM 51-10-2, 51-20-2. COMPLETE REPAIR DONE IAW SRM 51-40-6. (M) 2 L 7 3 4F A3WE 1997042400675 19970424 00675 NM 1997 4 24 97ZZZM518 1 19960830 A 5343 FITTING BOEING 727 7272J7 138400E NM NLG DAMAGED A ULHF K NONE O OTHER IN INSP/MAINT 1 SO 23 553NA 20707 REMOVED AND REPLACED LT NOSE GEAR FITTING PER B727 MM 32 AND S/B 727-53-0119R2 PART 3. REMOVED AND REPLACED LT NOSE GEA R FITTING PER B727 M32 AND SB 727-53. (M) 2 L 7 3 4F A3WE 1997042400714 19970424 00714 NM 1997 4 24 AALA961823 1 19961214 A 3222 STRUT SEAL BOEING 727 727223 1384074 NM NLG LEAKING A AALA A D UNSCHED LANDING RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SW 07 861AA 21088 TPA - FLT 0861 - DURING GEAR RETRACTION HAD A NOTICEABLE SHUTTER VIBRATION FROM THE NOSE GEAR AREA. RED NOSE GEAR DOOR WARNING LIGHT ILLUMINATED. RECYCLED GEAR TO NO AVAIL. LANDED TPA WITHOUT FURTHER INCIDENT. REPLACED STRUT SEALS AND S ERVICED NOSE GEAR PER MM. LEAK AND TAXI CHECKED NORMAL PERFORMED GEAR SWING. SYSTEM GROUND CHECKED NORMAL OPERATION. ( M) 2 L 7 3 4F A3WE 1997042400715 19970424 00715 NM 1997 4 24 AALA961752 1 19961202 A 3610 69179693 CLAMP BOEING 727 727223 1384074 NM NR 3 ENGINE LOOSE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 874AA 21386 MIA - FLT 1137 - AFTER TAKEOFF MIA DURING CLIMB, NR 3 ENGINE STRUT OVERHEAT LIGHT CAME ON. RETARDED THROTTLE AND STRUT OVERHEAT INDICATION EXTINGUISHED. AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT FURTHER INCIDENT. RESECURED LOOSE 13TH S TAGE MODULATING VALVE DUCT CLAMP AND REPLACED SEALS. ACCOMPLISHED LEAK CHECK WITH NO LEAKS FOUND. SYSTEM GROUND CHECKE D NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1997042400716 19970424 00716 NM 1997 4 24 AALA961765 1 19961205 A 3230 RETRACT MECH BOEING 727 727227 1384078 NM NLG LACK OF LUBE A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 07 723AA 20731 DFW - FLT 1356 - DURING APPROACH TO DFW WHEN LANDING GEAR EXTENDED, NOSE LANDING GEAR DID NOT EXTEND. RECYCLED LANDING GEAR AND NOSE LANDING GEAR EXTENDED. AIRCRAFT LANDED DFW WITHOUT INCIDENT. LUBRICATED NOSE LANDING GEAR. ACCOMPLISHED NOSE LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1997042400717 19970424 00717 NM 1997 4 24 AALA961728 1 19961125 A 3260 AAP2448A ACCESSORY UNIT BOEING 727 727223 1384074 NM E/E COMPT DEFECTIVE A AALA O OTHER N FALSE WARNING CL CLIMB 1 SW 07 846AA 20987 DFW - FLT 1187 - AFTER TAKEOFF BWI WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR RED LIGHT REMAINED ILLUMINATED WITH N O OTHER ABNORMAL INDICATIONS. AIRCRAFT PROCEEDED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR ACCESSORY U NIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1997042400718 19970424 00718 NM 1997 4 24 AALA961739 1 19961128 A 3260 AAP2448A ACCESSORY UNIT BOEING 727 727223 1384074 NM E/E COMPT DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 706AA 22463 MIA - FLT 63 - AFTER TAKEOFF MIA WHEN LANDING GEAR RETRACTED, LEFT MAIN LANDING GEAR RED AND GREEN LIGHTS REMAINED ILLUM INATED. AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT FURTHER INCIDENT. CHECKED WIRING FOR LANDING GEAR DOWNLOCK SWITCH AND CHECKED LANDING GEAR INDICATION SYSTEM. COULD NOT DUPLICATE ON GROUND. PRECAUTIONARY REPLACED LANDING GEAR ACCESSO RY BOX AND CHECKED ALL ASSOCIATED SWITCHES. ACCOMP LANDING GAR RETRACTION CHECK. SYSTEM GROUND CHECKED NORMAL OPS. (M ) 2 L 7 3 4F A3WE 1997042400760 19970424 00760 1997 4 24 S2YA960043 4 19961101 A 3420 6226135014 COMP CONTL UNIT CCU65 BEECH 1900 1900D 1154162 CE INSTRUMENT PANEL INOPERATIVE A S2YA K NONE O OTHER IN INSP/MAINT 1 GL 13 118SK 6806 UE108 DURING THE MONTH OF NOVEMBER, THERE WERE SEVEN CCU-65 COMPENSATION CONTROL UNITS, P/N 622-6135-014, REMOVED DUE TO PART OR ALL OF BACKLIGHTING BEING INOPERATIVE. THE PARTS TIME SINCE OVERHAUL WERE 6,805.5 HRS FROM N NR 118SK; 6,526.6 HRS FROM N NR 831SK; 6,825.1 HRS FROM N NR 801SK; 5,065.7 HRS FROM N NR 87SK; AND 5,947.8 HRS FROM N NR 91SK. WHEN SENT OUT FOR REPAIR, LAMPS WERE REPLACED AND THE UNITS RETURNED TO SERVICE. THIS GIVES MTBUR OF 6,234.0 HRS. REF: OPERATOR C ONTROL NRS 97ZZZX1787 THROUGH 97ZZZX1790. (X) 2 L 7 2 4T RT A24CE 1997042400761 19970424 00761 1997 4 24 97ZZZX1787 4 19961101 A 3420 6226135014 COMP CONTL UNIT CCU65 BEECH 1900 1900D 1154162 CE INSTRUMENT PANEL INOPERATIVE A S2YA K NONE O OTHER IN INSP/MAINT 1 GL 13 831SK 6527 UE83 DURING THE MONTH OF NOVEMBER, THERE WERE SEVEN CCU-65 COMPENSATION CONTROL UNITS, P/N 622-6135-014, REMOVED DUE TO PART OR ALL OF BACKLIGHTING BEING INOPERATIVE. THE PARTS TIME SINCE OVERHAUL WERE 6,805.5 HRS FROM N NR 118SK; 6,526.6 HRS FROM N NR 831SK; 6,825.1 HRS FROM N NR 801SK; 5,065.7 HRS FROM N NR 87SK; AND 5,947.8 HRS FROM N NR 91SK. WHEN SENT OUT FOR REPAIR, LAMPS WERE REPLACED AND THE UNITS RETURNED TO SERVICE. THIS GIVES MTBUR OF 6,234.0 HRS. REF: OPERAT OR CONTROL NRS S2YA960043, AND 97ZZZX1788 THROUGH 97ZZZX1790. 2 L 7 2 4T RT A24CE 1997042400762 19970424 00762 1997 4 24 97ZZZX1788 4 19961101 A 3420 6226135014 COMP CONTL UNIT CCU65 BEECH 1900 1900D 1154162 CE INSTRUMENT PANEL INOPERATIVE A S2YA K NONE O OTHER IN INSP/MAINT 1 GL 13 801SK 6825 UE80 DURING THE MONTH OF NOVEMBER, THERE WERE SEVEN CCU-65 COMPENSATION CONTROL UNITS, P/N 622-6135-014, REMOVED DUE TO PART OR ALL OF BACKLIGHTING BEING INOPERATIVE. THE PARTS TIME SINCE OVERHAUL WERE 6,805.5 HRS FROM N NR 118SK; 6,526.6 HRS FROM N NR 831SK; 6,825.1 HRS FROM N NR 801SK; 5,065.7 HRS FROM N NR 87SK; AND 5,947.8 HRS FROM N NR 91SK. WHEN SENT OUT FOR REPAIR, LAMPS WERE REPLACED AND THE UNITS RETURNED TO SERVICE. THIS GIVES MTBUR OF 6,234.0 HRS. REF: OPERAT OR CONTROL NRS S2YA960043, AND 97ZZZX1787 AND 97ZZZX1789, 97ZZZX1790. 2 L 7 2 4T RT A24CE 1997042400763 19970424 00763 1997 4 24 97ZZZX1789 4 19961101 A 3420 6226135014 COMP CONTL UNIT CCU65 BEECH 1900 1900D 1154162 CE INSTRUMENT PANEL INOPERATIVE A S2YA K NONE O OTHER IN INSP/MAINT 1 GL 13 87SK 5066 UE87 DURING THE MONTH OF NOVEMBER, THERE WERE SEVEN CCU-65 COMPENSATION CONTROL UNITS, P/N 622-6135-014, REMOVED DUE TO PART OR ALL OF BACKLIGHTING BEING INOPERATIVE. THE PARTS TIME SINCE OVERHAUL WERE 6,805.5 HRS FROM N NR 118SK; 6,526.6 HRS FROM N NR 831SK; 6,825.1 HRS FROM N NR 801SK; 5,065.7 HRS FROM N NR 87SK; AND 5,947.8 HRS FROM N NR 91SK. WHEN SENT OUT FOR REPAIR, LAMPS WERE REPLACED AND THE UNITS RETURNED TO SERVICE. THIS GIVES MTBUR OF 6,234.0 HRS. REF: OPERAT OR CONTROL NRS S2YA960043, AND 97ZZZX1787, 7ZZZX1788, 97ZZZX1790. 2 L 7 2 4T RT A24CE 1997042400764 19970424 00764 1997 4 24 97ZZZX1790 4 19961101 A 3420 6226135014 COMP CONTL UNIT CCU65 BEECH 1900 1900D 1154162 CE INSTRUMENT PANEL INOPERATIVE A S2YA K NONE O OTHER IN INSP/MAINT 1 GL 13 91SK 5948 UE91 DURING THE MONTH OF NOVEMBER, THERE WERE SEVEN CCU-65 COMPENSATION CONTROL UNITS, P/N 622-6135-014, REMOVED DUE TO PART OR ALL OF BACKLIGHTING BEING INOPERATIVE. THE PARTS TIME SINCE OVERHAUL WERE 6,805.5 HRS FROM ACFT 118SK; 6,526.6 HRS FROM N NR 831SK; 6,825.1 HRS FROM N NR 801SK; 5,065.7 HRS FROM N NR 87SK;, AND 5,947.8 HRS FROM N NR 91SK. WHEN SEN T OUT FOR REPAIR, LAMPS WERE REPLACED AND THE UNITS RETURNED TO SERVICE. THIS GIVES MTBUR OF 6,234.0 HRS. REF: OPERA TOR CONTROL NRS S2YA960043, AND 97ZZZX1787, 97ZZZX1788, 97ZZZX1789. 2 L 7 2 4T RT A24CE 1997042400778 19970424 00778 1997 4 24 S2YA960044 4 19961101 A 2312 6226520008 COMP CONTL HEAD CTL22 BEECH 1900 1900D 1154162 CE INSTRUMENT PANEL INOPERATIVE A S2YA K NONE O OTHER IN INSP/MAINT 1 GL 13 831SK 5448 UE83 DURING THE MONTH OF NOVEMBER, THERE WERE FOUR CTL-22 COMPENSATION CONTROL HEADS, P/N 622-6520-008, THAT WERE REMOVED DUE TO PART OR ALL OF BACKLIGHTING BEING INOPERATIVE. THE PARTS TIME SINCE OVERHAUL WERE 5,447.8 FROM N NR 831SK NR 1 SIDE ; 6,578.5 HRS FROM N NR 831SK NR 2 SIDE; 4,860.2 HRS FROM N NR 841SK; AND 6,538.1 HRS FROM N NR 85SK. WHEN SENT OUT FOR REPAIR, LAMPS WERE REPLACED BEFORE THE UNITS WERE RETURNED TO SERVICE. THIS GIVES A MTBUR OF 5,865.2 HOURS. REF: OP ERATOR CONTROL NRS 97ZZZX1802 THROUGH 97ZZZX1804. (X) 2 L 7 2 4T RT A24CE 1997042400779 19970424 00779 1997 4 24 97ZZZX1802 4 19961101 A 2312 6226520008 COMP CONTL HEAD CTL22 BEECH 1900 1900D 1154162 CE INSTRUMENT PANEL INOPERATIVE A S2YA K NONE O OTHER IN INSP/MAINT 1 GL 13 831SK 6579 UE83 DURING THE MONTH OF NOVEMBER, THERE WERE FOUR CTL-22 COMPENSATION CONTROL HEADS, P/N 622-6520-008, THAT WERE REMOVED DUE TO PART OR ALL OF BACKLIGHTING BEING INOPERATIVE. THE PARTS TIME SINCE OVERHAUL WERE 5,447.8 FROM N NR 831SK NR 1 SIDE ; 6,578.5 HRS FROM N NR 831SK NR 2 SIDE; 4,860.2 HRS FROM N NR 841SK; AND 6,538.1 HRS FROM N NR 85SK. WHEN SENT OUT FOR REPAIR, LAMPS WERE REPLACED BEFORE THE UNITS WERE RETURNED TO SERVICE. THIS GIVES A MTBUR OF 5,865.2 HOURS. REF: OP ERATOR CONTROL NRS S2YA960044 AND 97ZZZX1803, 97ZZZX1804. 2 L 7 2 4T RT A24CE 1997042400780 19970424 00780 1997 4 24 97ZZZX1803 4 19961101 A 2312 6226520008 COMP CONTL HEAD CTL22 BEECH 1900 1900D 1154162 CE INSTRUMENT PANEL INOPERATIVE A S2YA K NONE O OTHER IN INSP/MAINT 1 GL 13 841SK 4860 UE84 DURING THE MONTH OF NOVEMBER, THERE WERE FOUR CTL-22 COMPENSATION CONTROL HEADS, P/N 622-6520-008, THAT WERE REMOVED DUE TO PART OR ALL OF BACKLIGHTING BEING INOPERATIVE. THE PARTS TIME SINCE OVERHAUL WERE 5,447.8 FROM N NR 831SK NR 1 SIDE ; 6,578.5 HRS FROM N NR 831SK NR 2 SIDE; 4,860.2 HRS FROM N NR 841SK; AND 6,538.1 HRS FROM N NR 85SK. WHEN SENT OUT FOR REPAIR, LAMPS WERE REPLACED BEFORE THE UNITS WERE RETURNED TO SERVICE. THIS GIVES A MTBUR OF 5,865.2 HOURS. REF: OP ERATOR CONTROL NRS S2YA960044 AND 97ZZZX1802, 97ZZZX1804. 2 L 7 2 4T RT A24CE 1997042400781 19970424 00781 1997 4 24 97ZZZX1804 4 19961101 A 2312 6226520008 COMP CONTL HEAD CTL22 BEECH 1900 1900D 1154162 CE INSTRUMENT PANEL INOPERATIVE A S2YA K NONE O OTHER IN INSP/MAINT 1 GL 13 85SK 6538 UE85 DURING THE MONTH OF NOVEMBER, THERE WERE FOUR CTL-22 COMPENSATION CONTROL HEADS, P/N 622-6520-008, THAT WERE REMOVED DUE TO PART OR ALL OF BACKLIGHTING BEING INOPERATIVE. THE PARTS TIME SINCE OVERHAUL WERE 5,447.8 FROM N NR 831SK NR 1 SIDE ; 6,578.5 HRS FROM N NR 831SK NR 2 SIDE; 4,860.2 HRS FROM N NR 841SK; AND 6,538.1 HRS FROM N NR 85SK. WHEN SENT OUT FOR REPAIR, LAMPS WERE REPLACED BEFORE THE UNITS WERE RETURNED TO SERVICE. THIS GIVES A MTBUR OF 5,865.2 HOURS. REF: OP ERATOR CONTROL NRS S2YA960044 AND 97ZZZX1802, 97ZZZX1803. 2 L 7 2 4T RT A24CE 1997042400782 19970424 00782 1997 4 24 S2YA960042 4 19961101 A 3454 6226521016 NAV CONTL HEAD CTL32 BEECH 1900 1900D 1154162 CE INSTRUMENT PANEL INOPERATIVE A S2YA K NONE O OTHER IN INSP/MAINT 1 GL 13 79SK 6794 UE79 DURING THE MONTH OF NOVEMBER, THERE WERE SEVEN CTL-32 NAV CONTROL HEADS, P/N 622-6521-016, THAT WERE REMOVED DUE TO PART OR ALL OF BACKLIGHTING BEING INOPERATIVE. THE PARTS TIME SINCE OVERHAUL WERE 6,794.4 HRS FROM N NR 79SK NR 1 SIDE; 6,7 94.4 HRS FROM N NR 79SK NR 2 SIDE; 6,692.1 HRS FROM N NR 81SK; 5,952.7 HRS FROM N NR 831SK; 6,499.9 HRS FROM N NR 841SK; 5,741.2 HRS FROM N NR 85SK; AND 6,440.0 HRS FROM N NR 881SK. WHEN SENT OUT FOR REPAIR, LAMPS WERE REPLACED, AND THE UN ITS WERE RETURNED TO SERVICE. THIS GIVES AN MTBUR OF 6,416.7 HOURS. REF: OPERATOR CONTROL NRS 97ZZZX1805 THROUGH 97ZZ ZX1810. (X) 2 L 7 2 4T RT A24CE 1997042400783 19970424 00783 1997 4 24 97ZZZX1805 4 19961101 A 3454 6226521016 NAV CONTL HEAD CTL32 BEECH 1900 1900D 1154162 CE INSTRUMENT PANEL INOPERATIVE A S2YA K NONE O OTHER IN INSP/MAINT 1 GL 13 79SK 6794 UE79 DURING THE MONTH OF NOVEMBER, THERE WERE SEVEN CTL-32 NAV CONTROL HEADS, P/N 622-6521-016, THAT WERE REMOVED DUE TO PART OR ALL OF BACKLIGHTING BEING INOPERATIVE. THE PARTS TIME SINCE OVERHAUL WERE 6,794.4 HRS FROM N NR 79SK NR 1 SIDE; 6,7 94.4 HRS FROM N NR 79SK NR 2 SIDE; 6,692.1 HRS FROM N NR 81SK; 5,952.7 HRS FROM N NR 831SK; 6,499.9 HRS FROM N NR 841SK; 5,741.2 HRS FROM N NR 85SK; AND 6,440.0 HRS FROM N NR 881SK. WHEN SENT OUT FOR REPAIR, LAMPS WERE REPLACED, AND THE UN ITS WERE RETURNED TO SERVICE. THIS GIVES AN MTBUR OF 6,416.7 HOURS. REF: OPERATOR CONTROL NRS S2YA960042 AND 97ZZZX18 06 THROUGH 97ZZZX1810. 2 L 7 2 4T RT A24CE 1997042400784 19970424 00784 1997 4 24 97ZZZX1806 4 19961101 A 3454 6226521016 NAV CONTL HEAD CTL32 BEECH 1900 1900D 1154162 CE INSTRUMENT PANEL INOPERATIVE A S2YA K NONE O OTHER IN INSP/MAINT 1 GL 13 81SK 6692 UE81 DURING THE MONTH OF NOVEMBER, THERE WERE SEVEN CTL-32 NAV CONTROL HEADS, P/N 622-6521-016, THAT WERE REMOVED DUE TO PART OR ALL OF BACKLIGHTING BEING INOPERATIVE. THE PARTS TIME SINCE OVERHAUL WERE 6,794.4 HRS FROM N NR 79SK NR 1 SIDE; 6,7 94.4 HRS FROM N NR 79SK NR 2 SIDE; 6,692.1 HRS FROM N NR 81SK; 5,952.7 HRS FROM N NR 831SK; 6,499.9 HRS FROM N NR 841SK; 5,741.2 HRS FROM N NR 85SK; AND 6,440.0 HRS FROM N NR 881SK. WHEN SENT OUT FOR REPAIR, LAMPS WERE REPLACED, AND THE UN ITS WERE RETURNED TO SERVICE. THIS GIVES AN MTBUR OF 6,416.7 HOURS. REF: OPERATOR CONTROL NRS S2YA960042 AND 97ZZZX18 05, 97ZZZX1807 THROUGH 97ZZZX1810. 2 L 7 2 4T RT A24CE 1997042400785 19970424 00785 1997 4 24 97ZZZX1807 4 19961101 A 3454 6226521016 NAV CONTL HEAD CTL32 BEECH 1900 1900D 1154162 CE INSTRUMENT PANEL INOPERATIVE A S2YA K NONE O OTHER IN INSP/MAINT 1 GL 13 831SK 5953 UE83 DURING THE MONTH OF NOVEMBER, THERE WERE SEVEN CTL-32 NAV CONTROL HEADS, P/N 622-6521-016, THAT WERE REMOVED DUE TO PART OR ALL OF BACKLIGHTING BEING INOPERATIVE. THE PARTS TIME SINCE OVERHAUL WERE 6,794.4 HRS FROM N NR 79SK NR 1 SIDE; 6,7 94.4 HRS FROM N NR 79SK NR 2 SIDE; 6,692.1 HRS FROM N NR 81SK; 5,952.7 HRS FROM N NR 831SK; 6,499.9 HRS FROM N NR 841SK; 5,741.2 HRS FROM N NR 85SK; AND 6,440.0 HRS FROM N NR 881SK. WHEN SENT OUT FOR REPAIR, LAMPS WERE REPLACED, AND THE UN ITS WERE RETURNED TO SERVICE. THIS GIVES AN MTBUR OF 6,416.7 HOURS. REF: OPERATOR CONTROL NRS S2YA960042 AND 97ZZZX18 05, 97ZZZX1806, 97ZZZX1808 THROUGH 97ZZZX1810. 2 L 7 2 4T RT A24CE 1997042400786 19970424 00786 1997 4 24 97ZZZX1808 4 19961101 A 3454 6226521016 NAV CONTL HEAD CTL32 BEECH 1900 1900D 1154162 CE INSTRUMENT PANEL INOPERATIVE A S2YA K NONE O OTHER IN INSP/MAINT 1 GL 13 841SK 6500 UE84 DURING THE MONTH OF NOVEMBER, THERE WERE SEVEN CTL-32 NAV CONTROL HEADS, P/N 622-6521-016, THAT WERE REMOVED DUE TO PART OR ALL OF BACKLIGHTING BEING INOPERATIVE. THE PARTS TIME SINCE OVERHAUL WERE 6,794.4 HRS FROM N NR 79SK NR 1 SIDE; 6,7 94.4 HRS FROM N NR 79SK NR 2 SIDE; 6,692.1 HRS FROM N NR 81SK; 5,952.7 HRS FROM N NR 831SK; 6,499.9 HRS FROM N NR 841SK; 5,741.2 HRS FROM N NR 85SK; AND 6,440.0 HRS FROM N NR 881SK. WHEN SENT OUT FOR REPAIR, LAMPS WERE REPLACED, AND THE UN ITS WERE RETURNED TO SERVICE. THIS GIVES AN MTBUR OF 6,416.7 HOURS. REF: OPERATOR CONTROL NRS S2YA960042 AND 97ZZZX18 05 THROUGH 97ZZZX1807, 97ZZZX1809, 97ZZZX1810. 2 L 7 2 4T RT A24CE 1997042400787 19970424 00787 1997 4 24 97ZZZX1809 4 19961101 A 3454 6226521016 NAV CONTL HEAD CTL32 BEECH 1900 1900D 1154162 CE INSTRUMENT PANEL INOPERATIVE A S2YA K NONE O OTHER IN INSP/MAINT 1 GL 13 85SK 5741 UE85 DURING THE MONTH OF NOVEMBER, THERE WERE SEVEN CTL-32 NAV CONTROL HEADS, P/N 622-6521-016, THAT WERE REMOVED DUE TO PART OR ALL OF BACKLIGHTING BEING INOPERATIVE. THE PARTS TIME SINCE OVERHAUL WERE 6,794.4 HRS FROM N NR 79SK NR 1 SIDE; 6,7 94.4 HRS FROM N NR 79SK NR 2 SIDE; 6,692.1 HRS FROM N NR 81SK; 5,952.7 HRS FROM N NR 831SK; 6,499.9 HRS FROM N NR 841SK; 5,741.2 HRS FROM N NR 85SK; AND 6,440.0 HRS FROM N NR 881SK. WHEN SENT OUT FOR REPAIR, LAMPS WERE REPLACED, AND THE UN ITS WERE RETURNED TO SERVICE. THIS GIVES AN MTBUR OF 6,416.7 HOURS. REF: OPERATOR CONTROL NRS S2YA960042 AND 97ZZZX18 05 THROUGH 97ZZZX1808, 97ZZZX1810. 2 L 7 2 4T RT A24CE 1997042400788 19970424 00788 1997 4 24 97ZZZX1810 4 19961101 A 3454 6226521016 NAV CONTL HEAD CTL32 BEECH 1900 1900D 1154162 CE INSTRUMENT PANEL INOPERATIVE A S2YA K NONE O OTHER IN INSP/MAINT 1 GL 13 881SK 6440 UE88 DURING THE MONTH OF NOVEMBER, THERE WERE SEVEN CTL-32 NAV CONTROL HEADS, P/N 622-6521-016, THAT WERE REMOVED DUE TO PART OR ALL OF BACKLIGHTING BEING INOPERATIVE. THE PARTS TIME SINCE OVERHAUL WERE 6,794.4 HRS FROM N NR 79SK NR 1 SIDE; 6,7 94.4 HRS FROM N NR 79SK NR 2 SIDE; 6,692.1 HRS FROM N NR 81SK; 5,952.7 HRS FROM N NR 831SK; 6,499.9 HRS FROM N NR 841SK; 5,741.2 HRS FROM N NR 85SK; AND 6,440.0 HRS FROM N NR 881SK. WHEN SENT OUT FOR REPAIR, LAMPS WERE REPLACED, AND THE UN ITS WERE RETURNED TO SERVICE. THIS GIVES AN MTBUR OF 6,416.7 HOURS. REF: OPERATOR CONTROL NRS S2YA960042 AND 97ZZZX18 05 THROUGH 97ZZZX1809. 2 L 7 2 4T RT A24CE 1997042500003 19970425 00003 WP 1997 4 25 ABXA9700928 1 19960910 A 5240 39536851 BEAM DOUG DC9 DC932 3022066 WP SERVICE DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND SECOND FROM TOP HORIZONTAL BEAM CRACKED ON SERVICE DOOR. REPLACED IAW DC-9 SRM 51-30-2, 51-30-5. 2 L 7 2 4F A6WE 1997050100556 19970501 00556 WP 1997 5 1 96FDEA01124 1 19960613 A 5720 BEAM DOUG DC10 DC1010F 3022111 WP LT WING CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68058 46705 SNRM 5046 LT WING - AFT I BEAM, DIRECTLY BELOW AND 20 I/B OF NR 1 SPOILER, EXHIBITS HEAVY INTERGRANULAR CORROSION. *S/ D* REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 57-00-1, CLOSED 6/16/96. 2 L 7 3 4F A22WE 1997050100557 19970501 00557 WP 1997 5 1 97FDEA01207 1 19960708 A 7110 STIFFENER DOUG DC10 DC1010CF 3023502 WP NR 2 ENGINE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 056FE 47810 SNRM NR 4225 NR 2 ENGINE NOSE COWL BLKHD STIFFENER ON D-DUCT WEB CRACKED 10:00 POS AS SEEN THROUGH PANEL 361 KL. REMOVE D STIFFENER, WELDED CRACK AND REINSTALLED STIFFENER PER SRM 57-00-00, CLOSED 7/11/96. 2 L 7 3 4F RT A22WE 1997050100578 19970501 00578 NM 1997 5 1 AALA961882 1 19961230 A 3610 65234941 DUCT BOEING 727 727223 1384074 NM NR 3 ENGINE BLOWN A AALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 07 710AA 22467 DTW - FLT 1885 - DURING TAKEOFF DTW EN ROUTE DFW, A LOUD BANG WAS REPORTED BY THE AFT FLT ATTENDANT. THR NR 2 EPR GAUGE WENT TO 1.6 EPR AND THE LOWER AFT BODY LIGHT ILLUMINATED. THE LOWER AFT BODY EMERGENCY CHECKLIST WAS ACCOMPLISHED. TH E LIGHT EXTINGUISHED WHEN THE ENGINE WING AND NR 2 ANTI-ICE WAS COMMANDED OFF. RETURNED AND LANDED DTW WITHOUT INCIDENT . REPLACED RIGHT WING ANTI-ICE DUCTING AND HARDWARE FOR NR 3 ENGINE. ACCOMPLISHED LEAK CHECK AND OPERATIONS CHECK OF A IR CONDITIONING, PNEUMATICS, WING ANTI-ICE AND EPR SYSTEMS. SAFETY WIRED FUEL DUMP PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1997050100579 19970501 00579 NM 1997 5 1 AALA961905 1 19961226 A 3246 WHE5207 WHEEL BOEING 727 727223 1384074 NM RT MLG FAILED A AALA O OTHER E VIBRATION/BUFFET LD LANDING 1 SW 07 873AA 21385 SAP - FLT 941 - AFTER LANDING DURING INITIAL ROLLOUT, A/C BEGAN SHAKING VIOLENTLY AND RT MAIN LANDING GEAR RED LIGHT ILL UMINATED. A/C STOPPED W/O INCIDENT. DURING POST-FLIGHT CHECK, DISCOVERED NR 3 MAIN TIRE FAILED AND RT MAIN LANDING GEA R SIDE STRUT LOWER CLEVIS FAILED. REPLACED RT MAIN LANDING GEAR SIDE STRUT. REPLACED NR 2, 3 AND 4 MAIN WHEEL/TIRE ASS EMBLIES AND A/C MAINTENANCE FERRY SAP/IAH/TUL. ACCOMPLISHED GEAR SIDELOAD INSPECTION WITH NO DEFECTS FOUND. REPLACED R T TRAILING EDGE CENTER FLAP DUE TO FOD DAMAGE. SYSTEMS GROUND CHECKED NORMAL OPERATION. STOPPED ON TAXIWAY AND DEPLANE D PAX. AALA INITIATED FLEET CAMPAIGN TO MAG PARTICLE INSPECT ALL MLG SIDE STRUT LOWER CLEVIS FITTINGS. (M) 2 L 7 3 4F A3WE 1997050100580 19970501 00580 NM 1997 5 1 AALA961670 1 19961116 A 3020 65222723 ANTI-ICE DUCT BOEING 727 727223 1384074 NM NR 2 ENGINE DEFECTIVE A AALA K NONE J WARNING INDICATION CL CLIMB 1 SW 07 863AA 21090 MIA - FLT 706 - AFTER TAKEOFF STX, NR 2 ENGINE FIRE WARNING CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER AND IT POPPED AGAIN. AIRCRAFT PROCEEDED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED NR 2 ENGINE 6TH STAGE ANTI-ICE DUCT AND ACCOMP LISHED REPAIRS TO NR 2 ENGINE FIRE DETECTION WIRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1997050100591 19970501 00591 NM 1997 5 1 97ZZZM519 1 19960914 A 5531 RIB BOEING 727 7272J7 138400E NM VERT STAB CRACKED A ULHF K NONE O OTHER IN INSP/MAINT 1 SO 23 553NA 20707 FIN STATION 35, STRINGER NR 4 SECOND BAY UP FROM THE BOTTOM, RIB CRACKED WITH PREVIOUS ANGLE REPAIR, STOP DRILL IS NET . 25 INCH AND CRACKED ON FORWARD SIDE OF RIB RUNS TO THE SIDE OF STOP DRILL. CRACK RUNS PAST ANGLE DOUBLER RT SIDE OF VER TICAL STABILIZER. REMOVED EXISTING 'L' ANGLE REPAIR. REMOVED DEFECTIVE SECTION IAW SRM 55-30-4. NO CRACKS NOTED DURIN G HFEC INSPECTION. MANUFACTURED 2 'L ANGLE', 2 SHIMS AND OPTION 2 FILLER IAW SRM 55-30-4. TREATED AND PRIMED IAW MM 51 -20-11. INSTALLED REPAIR ANGLE IAW 55-30-060N1-0223. 2 L 7 3 4F A3WE 1997050100592 19970501 00592 NM 1997 5 1 97ZZZM520 1 19960918 A 7110 COWL BOEING 727 7272J7 138400E NM NR 1 ENGINE CORRODED A ULHF K NONE O OTHER IN INSP/MAINT 1 SO 23 553NA 20707 EXFOLIATED CORROSION ON NR 1 ENGINE FIXED COWL FORWARD SKIN. CORROSION BETWEEN HEAT SHILL AND SKIN. REMOVED FASTENERS AND SKIN. FABRICATED NEW SKIN FROM 2024-T3 .032 INCH 21.75 INCH BY 30.5 INCH. DRILLED, COUNTERSUNK AND DEBURRED. ALOD INED AND PRIMED NEW SKIN AND INSTALLED IAW SRM 51-30-2, 54-10-0, 51-10-2, 54-30-0 AND MM 51-20-11. 2 L 7 3 4F A3WE 1997050100593 19970501 00593 NM 1997 5 1 97ZZZM521 1 19960913 A 5711 SPAR CAP BOEING 727 7272J7 138400E NM WS 410 CORRODED A ULHF K NONE O OTHER IN INSP/MAINT 1 SO 23 553NA 20707 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND RIGHT WING STATION 410.0 L/E FORWARD LOWER SPAR CAP COR RODED. MECH REMOVED CORROSION BOTTOM OF FORWARD CHORD AT RIGHT WING STATION 410 IAW B727 SRM 51-10-6. CORROSION REMOVA L WENT OUT OF LIMITS IAW SRM 57-10-1. MATERIAL LOSS IS .127 .097 .133 (LESS THAN 20 PERCENT MATERIAL LOSS). TREATED AN D PRIMED IAW SRM 51-10-2 AND MM 51-20-11. WORK ACCOMPLISHED IAW EO 02545. (M) 2 L 7 3 4F A3WE 1997050100594 19970501 00594 NM 1997 5 1 97ZZZM522 1 19960913 A 5711 SPAR CAP BOEING 727 7272J7 138400E NM WS 420 CORRODED A ULHF K NONE O OTHER IN INSP/MAINT 1 SO 23 553NA 20707 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND RT WING STATION 420 L/E FORWARD LOWER SPAR CAP CORRODED . FOUND TO BE IN LIMITS. 2 L 7 3 4F A3WE 1997050100595 19970501 00595 NM 1997 5 1 97ZZZM523 1 19960913 A 5711 SPAR CAP BOEING 727 7272J7 138400E NM WS 520 CORRODED A ULHF K NONE O OTHER IN INSP/MAINT 1 SO 23 553NA 20707 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND RIGHT WING STATION 520 L/E FORWARD LOWER SPAR CAP CORRO DED. FOUND TO BE IN LIMITS. 2 L 7 3 4F A3WE 1997050100626 19970501 00626 EU 1997 5 1 RAIA961288 1 19961219 A 3233 D226860408 ACTUATOR AEROSP ATR42 ATR42300 8680920 EU RT MLG GOUGED A RAIA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 CE 03 423TE 18302 119 STL - FLT 7126 - BOTH MAIN GEARS WOULD NOT RETRACT. MAINTENANCE REPLACED THE RIGHT MAIN GEAR DUE TO GOUGE IN CYLINDER. (M) 2 H 7 2 4T RT A53EU 1997050100649 19970501 00649 NM 1997 5 1 P2EA97022 1 19961206 A 5320 CREASE BEAM BOEING 737 737205 NM BS 287-291 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 PAE - FOUND DURING INSPECTION, 40 INCHES LONG BY 1 INCHES WIDE BY .010 INCH DEEP OF CORROSION ON CREASE BEAM AT BS 287-2 91, RBL 51, WL 208. FABRICATED NEW PART AND DOUBLERS AND INSTALLED PER SRM 51-40-03, 53-10-01. (M) 2 L 7 2 4F A16WE 1997050100650 19970501 00650 NM 1997 5 1 P2EA97021 1 19961207 A 5320 WEB BOEING 737 737205 NM BS 328 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 PAE - FOUND DURING VISUAL INSPECTION, CORROSION ON NUMEROUS AREAS ON WEB. REMOVED AND REPAIRED DAMAGED SECTION OF WEB A T BS 328 LBL 56-61 PER SRM 51-40-02. MODIFIED PART NR INSTALLED 7075-T6 .040 (WEB). (M) 2 L 7 2 4F A16WE 1997050100651 19970501 00651 NM 1997 5 1 P2EA97020 1 19961207 A 5320 65458753 WEB BOEING 737 737205 NM BS 292-294 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 PAE - FOUND DURING VISUAL INSPECTION, 10 INCHES BY 2 INCHES OF CORROSION ON WEB AT BS 292-294. FABRICATED NEW LENGTH OF WEB AND INSTALLED AT BS 292-300 WITH REPAIR AT 300 PER SRM 51-40-2 DWG NR 65-45875. (M) 2 L 7 2 4F A16WE 1997050100652 19970501 00652 NM 1997 5 1 P2EA97019 1 19961208 A 5315 BAC1505100246 FLOORBEAM BOEING 737 737205 NM BS 328 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 PAE - FOUND DURING VISUAL INSPECTION, 105 INCHES BY 2 INCHES OF CORROSION ON FLOORBEAM AT BS 328. AREA PREVIOUSLY REWOR KED. REMOVED, FABRICATED, AND INSTALLED NEW FLOORBEAM PER SRM 53-10-09. (M) 2 L 7 2 4F A16WE 1997050100653 19970501 00653 NM 1997 5 1 P2EA97018 1 19961208 A 5315 FLOORBEAM BOEING 737 737205 NM BS 294 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 PAE - FOUND DURING VISUAL INSPECTION, 81 INCHES BY 2 INCHES OF CORROSION ON FLOORBEAM AT BS 294. AREA PREVIOUSLY REWORK ED. REMOVED DAMAGED UPPER CHORD OF BS 294 FLOORBEAM AND INSTALLED EXTRUSION AN 101362404. (M) 2 L 7 2 4F A16WE 1997050100654 19970501 00654 NM 1997 5 1 P2EA97017 1 19961208 A 5315 6545810523 FLOORBEAM BOEING 737 737205 NM BS 312 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 PAE - FOUND DURING VISUAL INSPECTION, 85 INCHES BY 2 INCHES OF CORROSION ON FLOORBEAM AT BS 312. AREA PREVIOUSLY REWORK ED. REPAIRED UPPER FLOORBEAM CHORD BY REMOVING UPPER CHORD AND REPLACING WITH EXTRUSION REPAIR PER SRM 53-10-9 FIG 5. M ODIFIED PART INSTALLED BAC 1505-100246. (M) 2 L 7 2 4F A16WE 1997050100655 19970501 00655 NM 1997 5 1 P2EA97016 1 19961208 A 5315 6545808535 FLOORBEAM BOEING 737 737205 NM BS 294 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 PAE - FOUND DURING VISUAL INSPECTION, 81 INCHES BY 2 INCHES OF CORROSION ON FLOORBEAM AT BS 294 LBL 32 TO RBL 49 WL 608. AREA PREVIOUSLY REWORKED. REMOVED DAMAGED SECTION OF CHORD, FABRICATED AND INSTALLED NEW CHORD PER SRM 53-10-9 FIG 5. (M) 2 L 7 2 4F A16WE 1997050100656 19970501 00656 NM 1997 5 1 P2EA97014 1 19961207 A 5320 CREASE BEAM BOEING 737 737205 NM BS 344-312 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 PAE - DURING C-CHECK, FOUND CORROSION .017 INCH DEEP BY .5 INCH DEEP BY .5 INCH LONG, .022 INCH DEEP BY .05 INCH WIDE BY .5 INCH L, .036 DEEP BY 1 INCH LONG BY .5 INCH WIDE AT BS 344-312, LBL 59, WL 208. FABRICATED NEW PART AND REPAIRED DO UBLERS PER SRM 51-40-03. (M) 2 L 7 2 4F A16WE 1997050100657 19970501 00657 NM 1997 5 1 P2EA97013 1 19961208 A 5320 65458752 CREASE BEAM BOEING 737 737205 NM BS 287-291 CORROSION A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 PAE - FOUND DURING VISUAL INSPECTION, 4 INCH BY 1 INCH CORROSION ON CREASE BEAM, AT BS 287-291, RBL 51, WL 208, AREA PRE VIOUSLY REWORKED. CORROSION ON CREASE BEAM OUT OF LIMITS, REMOVED AND REPLACED CREASE BEAM WITH NEW PART, PER SRM 53-10 -1 AND 51-40-3. (M) 2 L 7 2 4F A16WE 1997050100658 19970501 00658 NM 1997 5 1 P2EA97012 1 19961219 A 5320 CHORD BOEING 737 737222 1384473 NM BS 727 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 PAE - FOUND DURING NDI, 1.5 INCH CRACK AT STA 727 BL, STR 18A RIGHT WL 188. INSTALLED TIME LIMITED REPAIR PER SB 737-53 A1166 PT III. (M) 2 L 7 2 4F A16WE 1997050100659 19970501 00659 NM 1997 5 1 P2EA97011 1 19961213 A 5320 CHORD BOEING 737 737222 1384473 NM BS 727 DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 PAE - DURING C-CHECK, FOUND 2 INCH CRACK AT 727 CHORD. REMOVED AND REPLACED DAMAGED SECTION OF CHORD PER SB 737-53-1088 WITH KIT 65C33722-47. (M) 2 L 7 2 4F A16WE 1997050100660 19970501 00660 NM 1997 5 1 P2EA97010 1 19961212 A 5330 SKIN BOEING 737 737222 1384473 NM BS 727 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 PAE - DURING C-CHECK, TWO 3 INCH CRACKS IN SKIN AT 727 PLUS 6 AND 727 PLUS 16, FOUND DURING VISUAL INSPECTION. FABRICAT ED AND INSTALLED DOUBLERS PER SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1997050100683 19970501 00683 WP 1997 5 1 GRAA9685 1 19961226 A 2121 6054573 FAN DOUG DC9 DC987 3022087 WP TAIL COMPT FAILED A GRAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 11 1074T 49727 FLT CREW REPORTED RECIRCULATION FAN CIRCUIT BREAKERS 'POPPED' IN FLIGHT. CREW RETURNED TO RENO WITHOUT INCIDENT. RENO MAINTENANCE DEFERRED RECIRCULATION FAN PER MEL 21-43-DMI NR 39. PULLED AND COLLARD C/B'S. CANNON PLUG DISCONNECTED AND STOWED. AIRCRAFT RELEASED AND CONTINUED ON ITS WAY. CLEARED DMI NR 39 BY INSTALLING A SERVICEABLE UNIT, OPS CHECK GOO D. (M) 2 L 7 2 4F RT A6WE 1997050100684 19970501 00684 WP 1997 5 1 GRAA9701 1 19960102 A 3350 6011779 POWER SUPPLY DOUG DC9 DC915 3022036 WP CABIN INOPERATIVE A GRAA K NONE L NO TEST IN INSP/MAINT 1 WP 11 1068T 1210 45782 ENV - MAINTENANCE REPORTS CABIN EMERGENCY LIGHTING FAILS TO SHUT DOWN WHEN POWER IS REMOVED FROM AIRCRAFT BUSES. MAINTE NANCE REMOVED AND REPLACED BOTH 28V POWER SUPPLY PACKS (P/N 6011779, 601179) IN THE OVERHEAD AT ROW 161. OPS CHECK OF A LL EMERGENCY LIGHTING GOOD. (M) 2 L 7 2 4F A6WE 1997050100685 19970501 00685 WP 1997 5 1 GRAA9684 1 19961219 A 3350 SOCKET DOUG DC9 DC982 3022082 WP TAIL CONE INOPERATIVE A GRAA K NONE L NO TEST IN INSP/MAINT 1 WP 11 500TR 49144 FAA RAMP CHECK AT LGB, FOUND EMERGENCY LIGHT, RT SIDE, WILL NOT ILLUMINATE. CONTRACT MAINTENANCE AT LGB, FOUND SOCKET I NOPERATIVE IN TAIL CONE. REMOVED AND REPLACED. OPS CHECK GOOD.(M) 2 L 7 2 4F A6WE 1997050100686 19970501 00686 WP 1997 5 1 GRAA9686 1 19961230 A 3350 60030431 POWER PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A GRAA K NONE L NO TEST IN INSP/MAINT 1 WP 11 500TR 14098 49144 DFW - MAINTENANCE WHILE PERFORMING A TAKEOFF CHECK, FOUND THE TAIL COMPARTMENT DROP CEILING PANEL EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED TAIL COMPARTMENT DROP CEILING PANEL EMERGENCY POWER PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1997050100752 19970501 00752 EU 1997 5 1 RAIA961287 1 19961219 A 5311 S53572103210 FRAME AEROSP ATR42 ATR42300 8680920 EU LT MLG WW CRACKED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 423TE 18297 119 LEFT MAIN GEAR WOULD NOT RETRACT. MAINTENANCE SPLICED SECTION OF FRAME 26L. (M) 2 H 7 2 4T RT A53EU 1997050100753 19970501 00753 EU 1997 5 1 RAIA961286 1 19961219 A 5320 S53575102206 FILLER AEROSP ATR42 ATR42300 8680920 EU LT MLG WW CRACKED A RAIA A UNSCHED LANDING Z SIGNIFICANT FAILURE REPORT TO TAKEOFF 1 CE 03 423TE 18297 119 STL - FLT 7126 - BOTH MAIN GEAR WOULD NOT RETRACT. MAINTENANCE REPLACED THE LEFT FUSELAGE FILLER AT FRAME 26. (M) 2 H 7 2 4T RT A53EU 1997050100754 19970501 00754 EU 1997 5 1 RAIA961216 1 19961219 A 5320 DHC62940699 DOUBLER AEROSP ATR42 ATR42300 8680920 EU MLG WW CRACKED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 423TE 18297 119 STL - FLT 7126 - BOTH MAIN GEARS WOULD NOT RETRACT, AND NOSE GEAR RETRACTED NORMALLY. MAINTENANCE REPLACED FUSELAGE DOU BLER PER REPAIR DRAWING 15S535R0155. (M) 2 H 7 2 4T RT A53EU 1997050100756 19970501 00756 EU 1997 5 1 RAIA961291 1 19961219 A 3233 S5357270120600 ATTACH FITTING AEROSP ATR42 ATR42300 8680920 EU LT MLG ACT CRACKED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 423TE 119 STL - FLT 7126 - BOTH MAIN GEAR WOULD NOT RETRACT. MAINTENANCE REPLACED THE LEFT MAIN ACTUATOR LOWER ATTACH FITTING. ( M) 2 H 7 2 4T RT A53EU 1997050100757 19970501 00757 EU 1997 5 1 RAIA961290 1 19961219 A 3233 S535784000051 ATTACH FITTING AEROSP ATR42 ATR42300 8680920 EU LT MLG ACT SHEARED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 423TE 18297 18297 119 STL - FLT 7126 - BOTH MAIN GEAR WOULD NOT RETRACT. MAINTENANCE REPLACED THE LEFT MAIN ACTUATOR ATTACH FITTING. (M) 2 H 7 2 4T RT A53EU 1997050100758 19970501 00758 EU 1997 5 1 RAIA961289 1 19961219 A 3233 S5357840000251 ATTACH FITTING AEROSP ATR42 ATR42300 8680920 EU RT MLG ACT SHEARED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 423TE 18297 18297 119 STL - FLT 7126 - BOTH MAIN GEAR WOULD NOT RETRACT. MAINTENANCE REPLACED THE RIGHT MAIN ACTUATOR ATTACH FITTING. (M) 2 H 7 2 4T RT A53EU 1997050100774 19970501 00774 NM 1997 5 1 P2EA97015 1 19961208 A 5315 65458123 FLOORBEAM BOEING 737 737205 NM BS 328 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 PAE - FOUND DURING VISUAL INSPECTION, 105 INCHES BY 2 INCHES OF CORROSION ON FLOORBEAM AT RBL 11 TO RBL 45 WL 208 BS 328 . AREA PREVIOUSLY REWORKED. REMOVED AND FABRICATED NEW CHORD LBL 60 TO RBL 60 BS 328 PER SRM 53-10-09. (M) 2 L 7 2 4F A16WE 1997050800388 19970508 00388 NM 1997 5 8 DL757970835 1 19961222 A 3350 BULB OL3071BPEGL BOEING 757 757232 1384965 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 670DN 25331 EMERGENCY EXIT FLOOR TRACK LIGHT AT ROW 30 INOP. RELAMPED, CKS GOOD. 2 L 7 2 4F RT A2NM 1997050800400 19970508 00400 NM 1997 5 8 P5CA9700513 1 19960503 A 3310 27012 TRANSFORMER BOEING 747 747122 1384872 NM COCKPIT FAILED A P5CA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 23 853FT 19753 AFTER PUSHBACK AND ENGINE START ALL FLIGHT ENGINEER PANEL LIGHTS WENT OUT AND A BURNED SMELL IN THE AREA. REMOVED AND R EPLACED TRANSFORMER T-164 PER WIRING DIAGRAM MANUAL 33-12-11 TEST GOOD PER 33-12-00. 2 L 7 4 4F A20WE 1997050800584 19970508 00584 NM 1997 5 8 AALA970186 1 19961223 A 5320 HAT CHANNEL BOEING 727 727223 1384074 NM BS 1135 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 865AA 21370 TUL - HAT CHANNEL FLANGES CORRODED THROUGHOUT LENGTH OF CHANNEL 4 INCH BY 39 INCH PIECE CHANNEL. REPLACED HAT CHANNEL. (M) 2 L 7 3 4F A3WE 1997050800585 19970508 00585 NM 1997 5 8 AALA970187 1 19961223 A 5320 HAT CHANNEL BOEING 727 727223 1384074 NM BS 1135 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 865AA 21370 TUL - HAT CHANNEL FLANGES CORRODED THROUGHOUT LENGTH OF CHANNEL, 4 INCH BY 39 INCH PIECE CHANNEL. REPLACED HAT CHANNEL. (M) 2 L 7 3 4F A3WE 1997050800587 19970508 00587 NM 1997 5 8 AALA970189 1 19961220 A 5330 SKIN BOEING 727 727223 1384074 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 865AA 21370 TUL - SKIN BELOW STRINGER 26L BETWEEN STA 720E-720F CORRODED, LEVEL 2 DEGREE. INSTALLED DOUBLER PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 1997050800589 19970508 00589 NM 1997 5 8 AALA970191 1 19961220 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 380 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 865AA 21370 TUL - CORROSION TOP OF MAIN FLOORBEAM, STATION 380 RBL 40 AND RBL 65. REMOVED CORROSION, REPAIRED AFFECTED AREAS WITH D OUBLERS PER SRM 53-10-07-2. (M) 2 L 7 3 4F A3WE 1997050800590 19970508 00590 NM 1997 5 8 AALA970192 1 19961230 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 865AA 21370 TUL - STRINGER CRACKED AT FLANGE AREA. REPAIRED STRINGER PER 53-10-31. (M) 2 L 7 3 4F A3WE 1997050800591 19970508 00591 NM 1997 5 8 AALA970193 1 19961230 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 865AA 21370 TUL - STRINGER CRACKED ON FLANGE. REPAIRED STRINGER PER SRM 53-10-31. (M) 2 L 7 3 4F A3WE 1997050800592 19970508 00592 NM 1997 5 8 AALA970194 1 19961230 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 344 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 865AA 21370 TUL - CORROSION ON TOP OF FLOORBEAM. REMOVED CORROSION AND REPAIRED PER SRM 53-10-8. (M) 2 L 7 3 4F A3WE 1997050800609 19970508 00609 NM 1997 5 8 AALA970118 1 19961209 A 5330 SKIN BOEING 727 727223 1384074 NM BS 660 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 849AA 20990 TUL - CORROSION AT LEVELING COMPOUND ON BELLY SKIN BETWEEN STRINGER 28R AND STRINGER 28L, AFT SIDE OF FRAME STATION 660. CORROSION BEYOND LIMITS, CORRODED AREA CUTOUT PER SRM 53-30-3 FIG 1. REPAIR DOUBLER INSTALLED PER SRM 53-30-3 FIG 1. (M) 2 L 7 3 4F A3WE 1997050800610 19970508 00610 NM 1997 5 8 AALA970117 1 19961204 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 310 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 849AA 20990 TUL - CORROSION AT CREASE ANGLE BEAM INSIDE AFT CORNER OF FORWARD ENTRY DOOR. REMOVED CORRODED CREASE ANGLE AND INSTALL ED NEW ANGLE AS PER SRM 51-10-01. (M) 2 L 7 3 4F A3WE 1997050800612 19970508 00612 NM 1997 5 8 AALA970114 1 19961204 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 380 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 849AA 20990 TUL - BS 380 RBL 45 - RBL 70, CORROSION ON TOP FLANGE OF FLOORBEAM. REPLACED FLOORBEAM TOP CAP PER SRM 53-10-8. (M) 2 L 7 3 4F A3WE 1997050800613 19970508 00613 NM 1997 5 8 AALA970112 1 19961204 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 380 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 849AA 20990 TUL - FLOORBEAM CORRODED STATION 380 RBL 10-40. REPLACED FLOORBEAM TOP CAP PER SRM 53-10-8. (M) 2 L 7 3 4F A3WE 1997050800614 19970508 00614 NM 1997 5 8 AALA970111 1 19961204 A 5330 SKIN BOEING 727 727223 1384074 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 849AA 20990 TUL - CORROSION ON SKIN LAP ABOVE STRINGER 26R AT STATION 720B TO 720C. CORRODED SECTION CUT OUT, INSTALLED DOUBLER REP AIR PER SRM 53-30-3 FIG 5 AND INSTALLED NEW SECTION OF STRINGER AND 3 STRINGER SPLICES PER SRM 53-10-3 FIG 1. (M) 2 L 7 3 4F A3WE 1997051500401 19970515 00401 CE 1997 5 15 97ZZZX2029 1 19961217 A 7603 99102709 CONTROL CABLE CESSNA 402 402B 207590P CE LT ENG THROTTLE FROZEN A C89A O OTHER O OTHER CR CRUISE 1 SO 11 402B 1274 402B1305 ON DECEMBER 17, 1996, EN ROUTE, LEFT THROTTLE CABLE BECAME FROZEN UP. FLIGHT CONTINUED ON AND UPON ARRIVAL ON FINAL APP ROACH, SHUT THE LEFT ENGINE DOWN AND LANDED UNEVENTFULLY. PUT THE AIRCRAFT IN A HEATED HANGAR UNTIL THE THROTTLE THAWED OUT, THEN BLEW AIR AND MOUSE MILK LUBRICANT THROUGH THE CABLE. THERE HAVE BEEN NO MORE PROBLEMS. 1 L 7 2 3O A7CE 1997052200081 19970522 00081 SO 1997 5 22 CA961024007 1 19960924 A 3230 SCREWJACKS LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL HAMSTD 54H 54H60117 NE LT MLG DIRTY W L ABORTED APPROACH O OTHER AP APPROACH 1 CA 550195 235867 (CAN) ON APPROACH LH MAIN LANDING GEAR WOULD NOT EXTEND WHEN GEAR SELECTED DOWN. APPROACH WAS ABORTED AND ATC CONFIRMED LH MAIN LANDING GEAR DOOR WAS CLOSED AND GEAR NOT VISIBLE. LH GEAR MANUALLY LOWERED AND LANDING CARRIED OUT. SCREWJACK C ONTAMINATED WITH MOISTURE AND GRIME. TEST FLIGHT AND RETURNED TO SERVICE. 2 H 7 4 4T 4 T A1SO E282 6 C P906 1997052200083 19970522 00083 SO 1997 5 22 CA961024009 1 19961012 A 2612 892541100 DETECTION UNIT KIDDE 892541100 LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL HAMSTD 54H 54H60117 NE NR 3 ENG INTERMITTENT W E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 CA 3861 550195 235867 (CAN) IN CRUISE #3 ENGINE FIRE WARNING ILLUMINATED. ENGINE SHUT DOWN. LANDED WITHOUT INCIDENT. FIRE DETECTION UNIT REPLA CED. 2 H 7 4 4T 4 T A1SO E282 6 C P906 1997052200084 19970522 00084 EU 1997 5 22 CA961029002 1 19961018 A 3244 DR10728T TIRE BRAERO 748 HS7482A 4231001 EU NR 3 PUNCTURED W O OTHER O OTHER TX TAXI/GRND HDL 1 CA (CAN) #3 POSITION TIRE LOW, SLOW LEAK, SMALL NAIL, REPLACED. 2 L 7 2 3T A24EU 1997052200085 19970522 00085 EU 1997 5 22 CA961029005 1 19961014 A 3240 8Q3895 HOSE ASSEMBLY BRAERO 748 HS7482A 4231001 EU LT MLG LEAKING W K NONE K FLUID LOSS TX TAXI/GRND HDL 1 CA (CAN) AFTER LANDING AND APPLYING PARKING BRAKE #1 BRAKE PRESSURE SUPPLY LINE ON LH MAIN LANDING GEAR FAILED. REPLACED. 2 L 7 2 3T A24EU 1997052200086 19970522 00086 SO 1997 5 22 CA961104005 1 19961031 A 2435 36E1652QC STARTER PARKER HANIF 36E1652QC LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL HAMSTD 54H 54H60117 NE NR 3 ENGINE WORN JAWS W K NONE O OTHER IN INSP/MAINT 1 CA 196 196 0716 550195 235867 (CAN) #3 ENGINE WOULD NOT ENGAGE DURING START SEQUENCE. JAWS EXCESSIVELY WORN, REPLACED. 2 H 7 4 4T 4 T A1SO E282 6 C P906 1997052200087 19970522 00087 SO 1997 5 22 CA961104006 1 19961025 A 2435 36E1652QC STARTER PARKER HANIF 36E1652QC LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL HAMSTD 54H 54H60117 NE NR 1 WORN JAWS W K NONE O OTHER IN INSP/MAINT 1 CA 86 86 1018 550195 235867 (CAN) #1 STARTER WOULD NOT ENGAGE AT ENGINE START. TEETH ON STARTER JAWS WORN, REPLACED. 2 H 7 4 4T 4 T A1SO E282 6 C P906 1997052200088 19970522 00088 EU 1997 5 22 CA961104011 1 19960926 A 2910 AIR44498 VALVE BRAERO 748 HS7482A 4231001 EU RT NACELLE CRACKED W K NONE K FLUID LOSS TX TAXI/GRND HDL 1 CA 5248 (CAN) AFTER DEPLANING CREW NOTICED LARGE PUDDLE HYDRAULIC FLUID UNDER R/H NACELLE. CRACKED NON RETURN VALVE COMING OFF P RESSURE MANIFOLD. REPLACED. 2 L 7 2 3T A24EU 1997052200089 19970522 00089 GL 1997 5 22 CA961112015 2 19961010 A 7261 WIRING HARNESS LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL HAMSTD 54H 54H60117 NE NR 3 CHIP DET INTERMITTENT W O OTHER J WARNING INDICATION CL CLIMB 1 CA 550195 235867 (CAN) ON ROTATION #3 CHIP DETECTOR LIGHT ON INTERMITTENTLY. POWER WAS REDUCED AND DETECTOR LIGHT OUT. LANDED WITHOUT INC IDENT. WIRING HARNESS PROBLEM. REPAIRED. 2 H 7 4 4T 4 T A1SO E282 6 C P906 1997052200090 19970522 00090 SO 1997 5 22 CA961112016 1 19961012 A 2612 892541100 DETECTION UNIT KIDDE 892541100 LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL HAMSTD 54H 54H60117 NE NR 3 ENGINE INTERMITTENT W E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 CA 3861 550195 235867 (CAN) IN CRUISE #3 ENGINE FIRE WARNING LIGHT CAME ON. ENGINE SHUT DOWN IN FLIGHT, AIRCRAFT LANDED WITHOUT INCIDENT. FAUL T WITH FIRE DETECTION UNIT. REPLACED. 2 H 7 4 4T 4 T A1SO E282 6 C P906 1997052200091 19970522 00091 EU 1997 5 22 CA961112019 1 19961027 A 3230 200498004 ACTUATOR DOWTY 200427006 FOKKER F28 F28MK1000 4990808 EU RT MLG DOWNLOCK DEFECTIVE W K NONE J WARNING INDICATION DE DESCENT 1 CA DRG1469 (CAN) R/H MAIN LANDING GEAR SLOW TO EXTEND. REPLACED R/H MAIN LANDING GEAR DOWNLOCK ACTUATOR. 2 L 7 2 4F RT A20EU 1997052200092 19970522 00092 EU 1997 5 22 CA961112020 1 19961006 A 5240 A91116403 DOOR FOKKER F28 F28MK1000 4990808 EU LAV SERVICE TORN OFF W K NONE D INFLIGHT SEPARATION IN INSP/MAINT 1 CA (CAN) PILOTS REPORT LOUD PRESSURIZATION HOWL COMING FROM THE LAVATORY. INSPECTION REVEALED LAVATORY SERVICE DOOR TORN OF F ALONG WITH DUMP HORN AND FLUSH CONTROL VALVE. FUSELAGE DENTED AT STN 17065 BETWEEN STRINGERS 58 AND 58A. REPAIRED OR R EPLACED. 2 L 7 2 4F RT A20EU 1997052200093 19970522 00093 EU 1997 5 22 CA961112021 1 19961201 A 2780 A12361007 BRACKET FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU LE FLAP CRACKED W O OTHER J WARNING INDICATION LD LANDING 1 CA 9195 (CAN) AFTER LANDING LE FLAP #1 AND #2 LIFTDUMPER PANELS WOULD NOT RETRACT ENTIRELY. THE LIFTDUMPER WAS BARBER POLED AND THERE WAS NO LIFTDUMPER MASTER WARNING INDICATION. LH SUPPORT LEVER BRACKET PARTIALLY BROKEN AND TWO BOLTS SHEARED OFF. REPAIRED OR REPLACED. 2 L 7 2 4F 4 F RT A20EU E2EU 1997052200094 19970522 00094 EU 1997 5 22 CA961112024 1 19961026 A 3232 71539 ACTUATOR FOKKER F28 F28MK1000 4990808 EU NLG FAILED W A D UNSCHED LANDING RETURN TO BLOCK E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 CA (CAN) ON CLIMB OUT WHEN GEAR SELECTED UP THE RED NOSE GEAR LIGHT DID NOT EXTINGUISH. GEAR CYCLED DOWN OK. AIRCRAFT RETUR NED TO BLOCKS. AIRCRAFT FERRIED WHERE THE NOSE LANDING GEAR DOOR RETRACT ACTUATOR WAS REPLACED ALONG WITH THE SELECTOR V ALVE. 2 L 7 2 4F RT A20EU 1997052200095 19970522 00095 NM 1997 5 22 CA961112035 1 19961006 A 5730 113T161329 PANEL BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE GEAR AFT MISSING W K NONE O OTHER IN INSP/MAINT 1 CA P707550 (CAN) DURING SERVICE CHECK FOUND LOWER PANEL AFT OF LANDING GEAR MISSING. TEMPORARY PANEL INSTALLED 2 L 7 2 4F 4 F RT A1NM E3NE 1997052200096 19970522 00096 NM 1997 5 22 CA961112036 1 19961026 A 3244 323000213 TIRE BOEING 747 747133 138448B NM PWA JT9 JT9D7 52054 NE NR 8 MLG SEPARATED W O OTHER O OTHER TO TAKEOFF 1 CA P662866 (CAN) DURING TAKEOFF #8 MAIN WHEEL ASSEMBLY TIRE SEPARATED AND PUNCTURED FUSELAGE FAIRING. REPLACED #7 AND #8 MAIN WHEEL S. 2 L 7 4 4F 4 F A20WE E20EA 1997052200097 19970522 00097 NM 1997 5 22 CA961112042 1 19961008 A 3411 BACH30BC060154 HOSE ASSEMBLY BOEING 727 72725C 138400H NM PWA JT8 JT8D7B 52053 NE PITOT STATIC DETERIORATED W A UNSCHED LANDING I FLT. ATTITUDE INST. CL CLIMB 1 CA 649144 (CAN) CLUMBING THROUGH 14,000 FEET F/O ALTIMETER AND ASI DECREASED TO SEA LEVEL AND ZERO KNOTS RESPECTIVELY. TEMPORARY L INE INSTALLED. 2 L 7 3 4F 4 F A3WE E2EA 1997052200098 19970522 00098 NM 1997 5 22 CA961113003 1 19961007 A 2121 215201 FAN SUNDSTRAND 215201 BOEING 737 737275 1384485 NM PWA JT8 JT8D17A 52049 NE CABIN SEIZED W B H EMER. DESCENT DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 CA 046 702788 (CAN) ON FINAL APPROACH CABIN CREW REPORTED STRONG SMELL OF SMOKE IN AFT PASSENGERS CABIN. GASPER FAN CB PULLED. FAN REP LACED. 2 L 7 2 4F 4 F A16WE E2EA 1997052200099 19970522 00099 EU 1997 5 22 CA961118007 1 19961107 A 2750 17844009 ROD END FOKKER F28 F28MK1000 4990808 EU FLAPS BROKEN W K NONE O P OTHER NO WARNING INDICATION IN INSP/MAINT 1 CA (CAN) WHEN FLAPS RETRACTED INDICATOR SHOWED 2 DEGREES DOWN IN FULL UP POSITION. VISUAL CONFIRMED POSITION. FOWLER FLAP M ASTER BELLCRANK ACTUATING ROD BROKEN. REPLACED. 2 L 7 2 4F RT A20EU 1997052200100 19970522 00100 NM 1997 5 22 CA961118012 1 19961109 A 2520 WIRE BOEING 767 767233 1385113 NM PWA JT9 JT9D7R4D 52054 NE FAX MACH WRONG PART W O OTHER O OTHER CR CRUISE 1 CA P709633 (CAN) FLIGHT ATTENDANT RECEIVED SHOCK FROM FAX MACHINE. WIRES WERE NOT PROPERLY TERMINATED AT BANANA PLUG. REPAIRED. 2 L 7 2 4F 4 F RT A1NM E3NE 1997052200101 19970522 00101 NM 1997 5 22 CA961125011 1 19961112 A 2530 8650010000 OVEN FAN BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE GALLEY SEIZED W O F OTHER ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA P707556 (CAN) REAR GALLEY OVEN #3 SMOKING AND ARCING. FIRE EXTINGUISHER USED IN AND ON TOP OF OVEN. FAN MOTOR SEIZED. 2 L 7 2 4F 4 F RT A1NM E3NE 1997052200102 19970522 00102 EA 1997 5 22 CA961125013 1 19961113 A 2750 855D1007 BPSU CNDAIR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE FLAP CONTROL FAILED W K NONE F FLT CONT AFFECTED AP APPROACH 1 CA 1848 807343 (CAN) ON SELECTING 30 DEGREE FLAP SETTING, FLAP FAILURE MESSAGE ON EICAS. FLAPLESS LANDING CARRIED OUT. FLAP ELECTRONIC CONTROL UNIT FAULTED THE BRAKE AND POSITION SENSOR UNIT (BPSU). BPSU REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 1997052200103 19970522 00103 NM 1997 5 22 CA961125014 1 19961108 A 2751 1815819 TRANSMITTER BOEING 747 747133 138448B NM PWA JT9 JT9D7 52054 NE RT OUTB FLAP INOPERATIVE W O OTHER K FLUID LOSS CR CRUISE 1 CA P685832 (CAN) ON APPROACH FLAPS NORMAL AT 10 DEGREES WHEN 20 DEGREES SELECTED ASYMMETRY OCCURRED. CHECK LIST CARRIED OUT. R/H OU TBOARD FLAP TRANSMITTER AT FAULT. REPLACED. 2 L 7 4 4F 4 F A20WE E20EA 1997052200104 19970522 00104 WP 1997 5 22 CA961126006 1 19961117 A 2910 AV20A1032107 REGULATOR VALVE LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE MLG CONTROL FAILED W K NONE K FLUID LOSS LD LANDING 1 CA 10292 (CAN) AFTER SELECTING GEAR DOWN LOST ALL 'C' SYSTEM HYDRAULIC FLUID. LANDING GEAR CONTROL MODULE CARTRIDGE REPLACED. 2 L 7 3 4F 4 F A23WE E12EU 1997052200105 19970522 00105 NM 1997 5 22 CA961128009 1 19961127 A 2121 78279012 MOTOR HAMILTON STA 78279012 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE ACM LEAKING W O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA 2673 920246 120368 (CAN) A BRIEF PERIOD OF SMOKE IS OBSERVED IN THE CABIN AND FLIGHT DECK WHEN THE #2 BLEED IS SWITCHED ON AFTER ENGINE STA RT. SMOKE CLEARS AND NO ODOUR REMAINS. WATER FOUND IN THE ACM OIL SYSTEM AND OIL IN THE DUCT DOWNSTREAM OF THE ACM. ACM REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1997052200106 19970522 00106 NE 1997 5 22 CA961128025 2 19961120 A 7313 BACC18Z5G CIRCUIT BREAKER BOEING 737 7372E1 138448F NM PWA JT8 JT8D9A 52048 NE FUEL HEATER OPEN CIRCUIT W E ENGINE SHUTDOWN M OVER TEMP CR CRUISE 1 CA 687752 (CAN) RH ENGINE SHUT DOWN DUE TO HIGH OIL TEMPERATURE INDICATION. TROUBLESHOOTING REVEALED AN OPEN CIRCUIT IN THE CIRCUI T BREAKER WHICH POWERS THE FUEL HEATER, WHICH CAUSED THE FUEL HEATER TO REMAIN ON AND IN TURN CAUSE THE FUEL OIL COOLER TO RAISE THE OIL TEMPERATURE. REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1997052200107 19970522 00107 NM 1997 5 22 CA961128028 1 19961103 A 3320 MS18029256 PLASTIC COVER BOEING 767 767333 NM PWA 4060 PW4060 52119 NE LIGHT ASSY MISSING W O OTHER O OTHER CR CRUISE 1 CA P724723 (CAN) FLIGHT ATTENDANT RECEIVED SHOCK FROM LIGHT ASSEMBLY. NO COVER INSTALLED OVER BARE WIRES. INSTALLED. 2 L 7 2 4F 4 F RT A1NM E24NE 1997052200108 19970522 00108 NM 1997 5 22 CA961203002 1 19961101 A 3320 FLORESCENT LIGHT BOEING 727 727227 1384078 NM PWA JT8 JT8D9A 52048 NE LAV OVER HEATING W A H O UNSCHED LANDING DEACTIVATE SYST/CIRCUITS OTHER B J O SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION OTHER CR CRUISE 1 CA 666282 (CAN) AFTER DEPARTURE CABIN CREW REPORTED SMOKE IN L/H AFT LAVATORY. CIRCUIT BREAKER PULLED FOR LAVATORIES AND SMOKE DIS SIPATED. LAVATORY LIGHT SYSTEMS DEFERRED FLORESCENT LIGHTS. 2 L 7 3 4F 4 F A3WE E2EA 1997052200109 19970522 00109 NM 1997 5 22 CA961203004 1 19961107 A 2131 106120915 CONTROLLER BOEING 727 727214 138407R NM PWA JT8 JT8D7B 52053 NE CABIN PRESS INOPERATIVE W A UNSCHED LANDING O OTHER CL CLIMB 1 CA 649586 (CAN) ON CLIMB CABIN WOULD NOT PRESSURIZE IN ANY MODES AND COULD NOT CONTROL OUTFLOW VALVE. AIRCRAFT INSPECTED, PRESSURE CONTROLLER REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 1997052200110 19970522 00110 NM 1997 5 22 CA961203005 1 19961106 A 3010 6518353 DUCT BOEING 727 72722C 138400F NM PWA JT8 JT8D7B 52053 NE NR 5 ANTI ICE TWISTED W K NONE O OTHER IN INSP/MAINT 1 CA 655353 (CAN) ON TURNAROUND CREW NOTICED TWISTED DUCT ASSEMBLY ON #5 THERMAL ANTI-ICE TELESCOPING DUCT. REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 1997052200111 19970522 00111 EU 1997 5 22 CA961203011 1 19961119 A 2131 1026445 CONTROLLER FOKKER F28 F28MK1000 4990808 EU CABIN PRESS INOPERATIVE W A UNSCHED LANDING O OTHER CL CLIMB 1 CA (CAN) ON TAKEOFF CABIN FAILED TO PRESSURIZE. RETURNED TO BLOCKS. GROUND CHECK SERVICEABLE. ON TAKEOFF FAILED TO PRESSURI ZE AGAIN. RETURNED TO HOME BASE AND CABIN CONTROLLER REPLACED. RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1997052200112 19970522 00112 NM 1997 5 22 CA961216002 1 19961206 A 2612 894093 DETECTOR KIDDE 894093 BOEING 737 7372T7 NM PWA JT8 JT8D17 52049 NE NR 2 ENG DAMAGED W A E F UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 CA 708808 (CAN) ON CLIMB #2 ENGINE FIRE WARNING, AIRCRAFT RETURNED, FIRE WARNING STAYED ON FOR SEVERAL SECONDS, ENGINE SHUT DOWN A ND FIRE BOTTLE FIRED. CONDITION REMAINED THE SAME WITH FIRE WARNING INTERMITTENT. FIRE SENSING ELEMENT DAMAGED, REPLACED . 2 L 7 2 4F 4 F RT A16WE E2EA 1997052200113 19970522 00113 EU 1997 5 22 CA961216007 1 19961107 A 5753 A17844007 FORK FOKKER F28 F28MK1000 4990808 EU RT FLAP FAIRING BROKEN W K NONE F FLT CONT AFFECTED CL CLIMB 1 CA 43714 (CAN) ON TAKEOFF FLAPS WOULD NOT FULLY RETRACT STUCK AT 2 DEGREES. AIRCRAFT LANDED. DAMAGE TO R/H INNER FLAP FAIRING. RE PAIRED. 2 L 7 2 4F RT A20EU 1997052200114 19970522 00114 NM 1997 5 22 CA961217003 1 19961211 A 5330 SKIN BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE BS 520 STR 16 CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 702735 (CAN) 3/4 INCH CRACK IN THE LEFT HAND FUSELAGE SKIN, 4 INCHES AFT OF THE OVERWING LIGHT, AT STATION 520 STRINGER 16. REP AIRED AS PER SRM. 2 L 7 2 4F 4 F A16WE E2EA 1997052200115 19970522 00115 NM 1997 5 22 CA961217004 1 19961216 A 5330 SKIN BOEING 737 737210C 1384459 NM PWA JT8 JT8D9A 52048 NE BS801 STR 24L CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 674222 (CAN) 0.5 INCH CRACK AT BS 801 3 INCHES ABOVE STRINGER 24L ORIGINATING FROM SMALL GRAVEL DENT IN FUSELAGE. REPAIRED IN A CCORDANCE WITH SRM. 2 L 7 2 4F 4 F A16WE E2EA 1997052200116 19970522 00116 NM 1997 5 22 CA961220003 1 19961203 A 8012 1G38616927 SWITCH BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE #2 START VALVE INTERMITTENT W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA 688495 (CAN) TEN MINUTES AFTER TAKEOFF, CLIMBING THROUGH 20,000 FEET #2 START VALVE OPEN LIGHT ILLUMINATED. ENGINE SHUT DDOWN, LIGHT OUT AND DUCT PRESSURE UP. #2 START PRESSURE SWITCH REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1997052200117 19970522 00117 NM 1997 5 22 CA961220005 1 19961203 A 2910 'B' NUT BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE A SYS HYD LOOSE W A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 CA 709520 (CAN) ON TAKEOFF 'A' SYSTEM QTY INDICATED ZERO. MAIN GEAR EVENTUALLY RETRACTED BECAUSE IT WAS ALREADY SELECTED UP. 'A' S YSTEM CYCLED ON AND OFF SEVERAL TIMES AND INDICATED 200 PSI. EMERGENCY DECLARED AND LANDING CARRIED OUT. PRESSURE LINE ' B' NUT LOOSE, TIGHTENED. 2 L 7 2 4F 4 F A16WE E2EA 1997052200118 19970522 00118 NM 1997 5 22 CA961220006 1 19961203 A 8012 2730426 START VALVE BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE RT ENG INTERMITTENT W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 688495 (CAN) ON CLIMB RH STARTER VALVE OPEN LIGHT CAME ON. ENGINE SHUT DOWN. PNEUMATIC STARTER REGULATING AND SHUT OFF VALVE RE PLACED. 2 L 7 2 4F 4 F A16WE E2EA 1997052200120 19970522 00120 NM 1997 5 22 CA961220008 1 19961127 A 3020 693737053 MODULE BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE NR 2 ENG AI INTERMITTENT W K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA 14542 3924 702657 (CAN) ELECTRICAL SMELL COMING FROM FIRST OFFICER'S INSTRUMENT PANEL AREA. TURNING GASPER FAN, BACKGROUND LIGHTS OR FLOOD LIGHTS OFF HAS NO EFFECT. SMELL LIKE BURNT OUT LIGHT BALLEST. #2 ENGINE ANTI-ICE INOPERATIVE AND SMELL/HEAT COMING FROM MODULE. REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1997052200121 19970522 00121 EU 1997 5 22 CA961223005 1 19961212 A 2612 D826 CONNECTOR BRAERO 748 HS7482B 1500248 EU NR 1 ENG FIRE DIRTY W E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 CA (CAN) PRIOR TO DEPARTURE, BOTH ENGINES RUNNING, FIRE INDICATION WAS OBSERVED ON NO.1. NO EVIDENCE OF FIRE. OIL CONTAMINA TED CONNECTOR PLUG. CLEANED. SERVICEABLE. 2 L 7 2 3T A24EU 1997052200122 19970522 00122 NM 1997 5 22 CA961223007 1 19961213 A 2750 1817394 TRANSMITTER BOEING 737 7372A9C 1384495 NM PWA JT8 JT8D9A 52048 NE LT FLAP WET W O OTHER O OTHER AP APPROACH 1 CA 674318 (CAN) TRAILING EDGE FLAP ASYMMETRIC PROTECTION TRIPPED WHEN FLAPS SELECTED ON FINAL APPROACH. LH POSITION TRANSMITTER CL EANED. SERVICEABLE. 2 L 7 2 4F 4 F A16WE E2EA 1997052200123 19970522 00123 EU 1997 5 22 CA961230002 1 19961203 A 3233 200498005 ACTUATOR FOKKER F28 F28MK1000 4990808 EU RT MLG LEAKING W O OTHER J K WARNING INDICATION FLUID LOSS DE DESCENT 1 CA 7165 (CAN) LOSS OF ALL UTILITY HYDRAULIC FLUID. AIRCRAFT TOWED TO RAMP. R/H MAIN LANDING GEAR DOWNLOCK ACTUATOR HAD BLOWN AND LOST ALL FLUID. REPLACED. SYSTEM SERVICED. 2 L 7 2 4F RT A20EU 1997052200124 19970522 00124 1997 5 22 CA970106011 4 19961220 A 3160 52427702131 CDU BOEING 757 75723A 1384967 NM RROYCE RB211 RB211535E437 54555 NE COCKPIT FAILED W A UNSCHED LANDING I FLT. ATTITUDE INST. CL CLIMB 1 CA 30680 (CAN) #1 CDU WENT OFF DURING CLIMB. RETURNED TO BLOCKS. CDU REPLACED. 2 L 7 2 4F 4 F RT A2NM E12EU 1997052200125 19970522 00125 NM 1997 5 22 CA970107007 1 19961228 A 8012 1G386 SWITCH GARRTT 97907821 BOEING 727 727217 NM PWA JT8 JT8D17 52049 NE NR 2 ENG START FAILED W A E UNSCHED LANDING ENGINE SHUTDOWN J N WARNING INDICATION FALSE WARNING CL CLIMB 1 CA 3414 688240 (CAN) ON DEPARTURE #2 ENGINE START VALVE LIGHT CAME ON AND REMAINED ON. ENGINE SHUTDOWN. REPLACED VALVE. 2 L 7 3 4F 4 F RT A3WE E2EA 1997052200130 19970522 00130 NM 1997 5 22 CA970114004 1 19961217 A 5330 651838581 SKIN BOEING 727 72722 1384002 NM PWA JT8 JT8D7B 52053 NE BS 1170 STR 18L CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 66392 649606 (CAN) CRACK INDICATION IN FUSELAGE PRESSURIZATION SKIN AT BS1170 ABOVE STRINGER 18L. CRACK THREE INCHES IN LENGTH JOINED A HORIZONTAL LINE OF PAINT BLISTERS IN A 10 INCH LINE OF BLISTERS. DISBONDED DOUBLER AND SEVERE CORROSION OF SKIN AND D OUBLER ON BOND FACES. PANEL REPLACED. ADJACENT LOWER SKIN ALSO DISBONDED AND CORRODED BS1148 TO BS1183 STRINGER 20L TO 2 4L REPLACED. AREA OF PREVIOUS LAVATORY INSTALLATION. 2 L 7 3 4F 4 F A3WE E2EA 1997052200453 19970522 00453 WP 1997 5 22 ABXA9701007 1 19960910 A 5543 5910257501 TAB DOUG DC9 DC932 3022066 WP RUDDER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 FOUND RUDDER TAB TRAILING EDGE CRACKED AND DENTED. REPAIRED TRAILING EDGE SKINS PER DC9 SRM 51-70-2. 2 L 7 2 4F A6WE 1997052200454 19970522 00454 WP 1997 5 22 ABXA9701008 1 19960923 A 5240 99115823 BEAM DOUG DC9 DC932 3022066 WP FWD SERV DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 FOUND FWD SERVICE DOOR UPPER HINGE BEAM CRACKED, HOLD OPEN HOOK PAN CRACKED, SUPPORT ANGLE CRACKED. REPAIRED IAW DC9 SR M 51-30-5. 2 L 7 2 4F A6WE 1997052200455 19970522 00455 WP 1997 5 22 ABXA9701009 1 19961008 A 5220 591015931 PAN DOUG DC9 DC931 3022065 WP EMER EXIT DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 924AX 47403 FOUND OVERWING DOOR PAN CRACKED. REPAIRED IAW ABX REA D952-15926-MR. 2 L 7 2 4F A6WE 1997052200456 19970522 00456 WP 1997 5 22 ABXA9701010 1 19960924 A 5220 591015931 SKIN DOUG DC9 DC931 3022065 WP EMER EXIT DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 924AX 47403 FOUND DOOR PAN, AND INNER SKIN CRACKED. REPAIRED IAW ABX REA D952-16211-MR, AND DC9 SRM 52-01. 2 L 7 2 4F A6WE 1997052200457 19970522 00457 WP 1997 5 22 ABXA9701011 1 19961028 A 5523 5910413509 TAB DOUG DC9 DC931 3022065 WP ELEVATOR CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 929AX 45874 FOUND ELEVATOR CONTROL TAB INBOARD NOSE CAP CORRODED. REPLACED NOSE CAP (P/N 591041311) IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 1997052200458 19970522 00458 WP 1997 5 22 ABXA9701012 1 19961023 A 5240 99115823 BEAM DOUG DC9 DC933F 302207A WP DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 934AX 47462 FOUNR FWD SERVICE DOOR LOWER BEAM CRACKED AND SECOND BEAM FROM BOTTOM CRACKED. REPAIRED LOWER BEAM (P/N 9911582-3) AND SECOND BEAM (P/N 9911581-3) IAW DC9 SRM 52-05. 2 L 7 2 4F A6WE 1997052200459 19970522 00459 WP 1997 5 22 ABXA9701013 1 19960218 A 5230 591014127 SKIN DOUG DC9 DC933F 302207A WP CARGO DOOR CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 FOUND FWD LWR CARGO DOOR PAN CORRODED AND CRACKED, INTERCOSTAL CRACKED, AND DOOR SKIN CRACKED. REPAIRED SKIN (P/N 59101 41-27) IAW REA D952-17254. REPLACED INTERCOSTAL (P/N 9957664-2) IAW DC9 DWG - 5910141. REPLACED PAN (P/N 5910141-7, 59 10141-9) IAW DC9 DWG - 5910141. 2 L 7 2 4F A6WE 1997052200460 19970522 00460 WP 1997 5 22 ABXA9701014 1 19960924 A 5220 591015931 PAN DOUG DC9 DC941 302207N WP EMER EXIT DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 958AX 47760 FOUND EMERGENCY EXIT DOOR PAN CRACKED. REPAIRED IAW ABX REA D952-16410-MR. 2 L 7 2 4F A6WE 1997052200461 19970522 00461 WP 1997 5 22 ABXA9701015 1 19960906 A 5220 591015931 PAN DOUG DC9 DC941 302207N WP EMER EXIT DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 958AX 47760 FOUND EMERGENCY EXIT DOOR PAN CRACKED AND STOP NR 7 CRACKED. REPAIRED PAN IAW ABX REA D952-16213-MR. REPLACED STOP (P/ N 4914413-503) IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1997052200463 19970522 00463 WP 1997 5 22 ABXA9701017 1 19960924 A 5220 591015943 PAN DOUG DC9 DC941 302207N WP EMER EXIT DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 FOUND EMERGENCY EXIT DOOR PAN CRACKED. REPAIRED IAW ABX REA D952-16416-MR. 2 L 7 2 4F A6WE 1997052200466 19970522 00466 WP 1997 5 22 ABXA9701020 1 19960923 A 5220 591015943 PAN DOUG DC9 DC941 302207N WP EMER EXIT DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 FOUND EMERGENCY EXIT DOOR PAN CRACKED. REPAIRED IAW ABX REA D952-16415-MR. 2 L 7 2 4F A6WE 1997052200467 19970522 00467 WP 1997 5 22 ABXA9701021 1 19961204 A 5753 5910134169 SKIN DOUG DC9 DC941 302207N WP LT TE WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 FOUND LEFT FLAP UPPER AND LOWER SKINS CORRODED. REPLACED SKINS (P/N 9957578-15, 995757-503) IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 1997052200468 19970522 00468 WP 1997 5 22 ABXA9701022 1 19961118 A 5753 5910134170 RIB DOUG DC9 DC941 302207N WP RT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 FOUND RIGHT FLAP OUTBOARD HINGE INBOARD AND OUTBOARD RIBS CRACKED. REPLACED FITTINGS (P/N 9957600-7, 9957600-15) IAW DC 9 SRM 51-30-2. 2 L 7 2 4F A6WE 1997052200469 19970522 00469 WP 1997 5 22 ABXA9701023 1 19961004 A 5220 591015931 PAN DOUG DC9 DC941 302207N WP EMER EXIT DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 958AX 47760 FOUND OVERWING DOOR PAN CRACKED. REPAIRED IAW ABX REA D952-16327-MR. 2 L 7 2 4F A6WE 1997052200528 19970522 00528 EU 1997 5 22 97ZZZX2124 1 19961207 A 6420 1053170023 BEARING BOLKMS 105 BO105LSA3 5626020 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 202LF 597 2014 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS. CORRECTED PROBLEM. 1 G 7 2 3U H3AU 1997052200530 19970522 00530 EU 1997 5 22 97ZZZX2126 1 19961230 A 6420 1053170023 BEARING BOLKMS 105 BO105LSA3 5626020 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 203LF 444 2015 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U H3AU 1997052200532 19970522 00532 EU 1997 5 22 97ZZZX2128 1 19961111 A 6410 704A3363371 LAMINATED HINGE SNIAS 350 AS350D 8680803 EU T/R WHITE WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 779LF 249 1621 LAMINATED HINGE ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CO RRECTED PROBLEM. 1 G 7 1 3U H9EU 1997052200535 19970522 00535 EU 1997 5 22 97ZZZX2130 1 19961112 A 6410 704A33633171 LAMINATED HINGE SNIAS 350 AS350B2 8680813 EU T/R WHITE WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911LR 40 2404 LAMINATED HINGE ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CO RRECTED PROBLEM. 1 G 7 1 3U H9EU 1997052200537 19970522 00537 EU 1997 5 22 97ZZZX2132 1 19960911 A 6230 1051011305 BELLOWS BOLKMS 105 BO105CBS 5626008 EU M/R MAST TORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 105NC 487 790 BELLOWS IS TORN AROUND CLAMP AND FOLD AREAS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H3EU 1997052200538 19970522 00538 EU 1997 5 22 97ZZZX2133 1 19961015 A 6420 1053170018 BOLT BOLKMS 117 BK117A4 5626017 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 117CW 358 7125 FITTED BOLT WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1997052200542 19970522 00542 EU 1997 5 22 97ZZZX2137 1 19961216 A 6420 1053170023 BEARING BOLKMS 117 BK117A3 5626015 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 951AM 422 7017 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1997052200543 19970522 00543 EU 1997 5 22 97ZZZX2138 1 19960902 A 7110 1172310112 BALL PIN BOLKMS 117 BK117A3 5626015 EU COWL WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 951AM 300 7017 BALL PIN WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1997052200544 19970522 00544 EU 1997 5 22 97ZZZX2139 1 19961014 A 2844 DK042 TRANSMITTER BOLKMS 105 BO105CBS 5626008 EU FUEL PRESS DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911BH 146 11934 685 INDICATOR PRESSURE READING PEGS TO THE HIGH SIDE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H3EU 1997052200546 19970522 00546 EU 1997 5 22 97ZZZX2141 1 19961218 A 3340 2LA00162500 LIGHT BOLKMS 117 BK117A4 5626017 EU TAIL INTERMITTENT A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911BY 497 7127 TAIL LIGHT UNIT OPERATES INTERMITTENTLY BECAUSE OF WORN SOCKET. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1997052200547 19970522 00547 EU 1997 5 22 97ZZZX2142 1 19961222 A 7714 32005008 TACH GENERATOR BOLKMS 105 BO105CBS 5626008 EU ENGINE DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 105NC 133 250909 790 N2 NEEDLE BOUNCES AND IS SLOW TO RESPOND AT START-UP. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H3EU 1997052200548 19970522 00548 EU 1997 5 22 97ZZZX2143 1 19961015 A 6420 ABWT82008 BEARING BOLKMS 117 BK117A4 5626017 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 117CW 213 7125 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1997052200550 19970522 00550 EU 1997 5 22 97ZZZX2145 1 19961015 A 6420 1053170023 BEARING BOLKMS 117 BK117B1 5626012 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 17SJ 58 7230 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1997052200551 19970522 00551 EU 1997 5 22 97ZZZX2146 1 19961227 A 6230 1051011305 BELLOWS BOLKMS 105 BO105LSA3 5626020 EU M/R TORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 202LF 278 2014 BELLOWS IS TORN AROUND CLAMP AND FOLD AREAS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H3AU 1997052200568 19970522 00568 EU 1997 5 22 97ZZZX2163 1 19961101 A 6410 704A33633116 BEARING SNIAS 350 AS350B 8680801 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 21UM 261 1674 LAMINATED BEARING ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 4 EACH NEW UNITS FROM KIT 355A09-1036-01. CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1997052200575 19970522 00575 NM 1997 5 22 AALA961847 1 19961219 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 1035-1065 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 899AA 22015 TUL - FOUND CORROSION AROUND FASTENER HOLES ON 2 ANGLE. REMOVED AND REPLACED Z-ANGLE FROM EXISTING SPLICE TO EXISTING S PLICE, PRIMED AND PAINTED. (M) 2 L 7 3 4F A3WE 1997052200576 19970522 00576 NM 1997 5 22 AALA961848 1 19961219 A 5330 SKIN BOEING 727 727223 1384074 NM BS 870 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 899AA 22015 TUL - FOUND CORROSION ON LOWER SKIN OF CENTER FUEL TANK ABOVE THE LEFT PRIMARY HEAT EXCHANGER FS 870. REMOVED CORROSION AND INSTALLED DOUBLER AND STRAP PER ESO 11697 PAGES 1-4, DATED 12-12-96. (M) 2 L 7 3 4F A3WE 1997052900231 19970529 00231 NM 1997 5 29 CA970114005 1 19961221 A 5320 MS2000623 BOLTS BOEING 727 72722 1384002 NM PWA JT8 JT8D7B 52053 NE BS1183 FRAME CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 66392 649606 (CAN) DURING SKIN PANEL REPLACEMENT IN AREA STRINGER END FITTING TIE BOLTS WERE REMOVED TO ACCESS FASTENERS THROUGH BS11 83 FRAME FLANGE. TIE BOLT SHANKS CORRODED, FROM LIGHT TO SEVERE CORROSION. CORROSION NOT DETECTABLE WITH BOLTS INSTALLED . BOLTS REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 1997052900232 19970529 00232 EU 1997 5 29 CA970114006 1 19961214 A 5330 A24000001 SKIN PANELS FOKKER F28 F28MK1000 4990808 EU COCKPIT ROOF CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) EDDY CURRENT OF COCKPIT ROOF SKINS REVEALED RADIAL CRACKS EMINATING FROM UNDER SEVERAL RIVET HEADS. NEW PANELS REC EIVED BUT CRACKED DURING DIMPLING PROCESS. NEW SKINS INSTALLED WITH BUTTON HEAD RIVETS. SKINS TO BE REPLACED NEXT BLOCK CHECK. 2 L 7 2 4F RT A20EU 1997052900254 19970529 00254 EU 1997 5 29 97ZZZX2315 1 19961022 A 6420 1053170023 BEARING BOLKMS 117 BK117A3 5626015 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 527SF 386 7111 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1997052900260 19970529 00260 EU 1997 5 29 97ZZZX2321 1 19961119 A 7931 1176131203 SWITCH BOLKMS 117 BK117A3 5626015 EU OIL PRESS FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 625MB 273 1503 7108 PRESSURE SWITCH WILL NOT ILLUMINATE AT MINIMUM PRESSURE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1997052900265 19970529 00265 EU 1997 5 29 97ZZZX2326 1 19961024 A 6520 704A33633171 LAMINATED HINGE SNIAS 350 AS350B2 8680813 EU T/R YELLOW WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911LR 74 2404 LAMINATED HINGE ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CO RRECTED PROBLEM. 1 G 7 1 3U H9EU 1997052900266 19970529 00266 EU 1997 5 29 97ZZZX2327 1 19961228 A 6520 704A33633171 LAMINATED HINGE SNIAS 350 AS350B2 8680813 EU T/R YELLOW WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911LR 86 2404 LAMINATED HINGE ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CO RRECTED PROBLEM. 1 G 7 1 3U H9EU 1997052900267 19970529 00267 EU 1997 5 29 97ZZZX2328 1 19961106 A 6520 704A33633171 LAMINATED HINGE SNIAS 350 AS350B2 8680813 EU T/R PINK WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 92LG 149 2575 LAMINATED HINGE ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CO RRECTED PROBLEM. 1 G 7 1 3U H9EU 1997052900269 19970529 00269 EU 1997 5 29 97ZZZX2330 1 19961101 A 6520 704A33633171 LAMINATED HINGE SNIAS 350 AS350B2 8680813 EU T/R WHITE WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 94LG 68 2728 LAMINATED HINGE ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH UNITS UNITS FROM KIT 350A33-2153-00, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1997052900604 19970529 00604 WP 1997 5 29 ABXA9600652 1 19961024 A 2110 5614845517 TURBOCOMPRESSOR DOUG DC8 DC862 3021970 WP NR 2 OIL LEAK A ABXA K NONE O OTHER CR CRUISE 1 GL 23 804AX 45987 INFLIGHT THERE WAS A STRONG ODOR. STRONGER DURING DESCENT AND IRRITATING TO THE EYES. *S/D* MAINTENANCE FOUND NR 2 CT C LEAKING OIL. REPLACED NR 2 CTC, OPS CHECKED GOOD IAW DC8 MM 22-10-1. 2 L 7 4 4F 4A25 1997052900762 19970529 00762 WP 1997 5 29 ABXA9701065 1 19961213 A 5730 5919572502 DOOR DOUG DC9 DC941 302207N WP RT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 960AX 47762 DURING D-INSPECTION, FOUND THE RIGHT WING CENTER BUTE DOOR HEAVILY CORRODED ON INNER AND OUTER SURFACES. REMOVED AND RE PLACED BUTE DOOR ASSY IAW DC9 MAINTENANCE MANUAL CHAPTER 57-20-3. 2 L 7 2 4F A6WE 1997060500238 19970605 00238 NE 1997 6 5 97ZZZX2420 2 19961012 A 7260 430101501 SEAL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE ACCESSORY DRIVE LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 117CW 50 7125 LE45023E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH 3 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1997060500239 19970605 00239 NE 1997 6 5 97ZZZX2421 2 19961012 A 7260 430101301 SEAL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE AFT ALTERNATOR LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 117CW 50 7125 LE45023E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1997060500240 19970605 00240 NE 1997 6 5 97ZZZX2422 2 19961012 A 7260 430101201 SEAL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE FWD ALTERNATOR LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 117CW 7125 LE45023E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1997060500241 19970605 00241 NE 1997 6 5 97ZZZX2423 2 19961012 A 7260 230307203 SEAL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE CSD DRIVE LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 117CW 7125 LE45023E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM 1 G 7 2 3U 3 U H13EU E5NE 1997060500242 19970605 00242 NE 1997 6 5 97ZZZX2424 2 19961011 A 7230 430151101 BEARING BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE ENG NR 2 DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 117MV 56 5171 7089 LE45071E NR 2 BEARING HAS FLAT SPOTS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1997060500243 19970605 00243 NE 1997 6 5 97ZZZX2425 2 19961227 A 7250 410106802 SPRING BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE SEAL RING WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 202HN 527 7115 LE45078E SEAL RING EXPANDER SPRING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1997060500244 19970605 00244 NE 1997 6 5 97ZZZX2426 2 19961227 A 7260 430101201 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE FWD ALTERNATOR LEAK A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 202HN 7115 LE45078E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1997060500245 19970605 00245 NE 1997 6 5 97ZZZX2427 2 19961227 A 7250 414129001 TURBINE BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE ENGINE BLADE SHIFT A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 202HN 1639 1263 SC17297 7115 LE45078E ROTOR ASSY FAILED SB LT101-72-10-0153. EXCESSIVE IBPT BLADE SHIFT NR 9 -0.026 INCH. REPLACED WITH USED UNIT, CORRECTED PROBLEM. PART TOTAL CYCLES, 3,172.3. 1 G 7 2 3U 3 U H13EU E5NE 1997060500246 19970605 00246 NE 1997 6 5 97ZZZX2428 2 19961227 A 7250 419195691 SEAL RING BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE 1ST TURB SHROUD WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 202HN 527 7115 LE45078E SEAL RING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1997060500247 19970605 00247 NE 1997 6 5 97ZZZX2429 2 19961227 A 7230 410100712 SHAFT BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE COMPRESSOR DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 202HN 589 93B078 7115 LE45078E COMPRESSOR SHAFT IMPROPER STRETCH. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1997060500248 19970605 00248 NE 1997 6 5 97ZZZX2430 2 19961227 A 7260 230307203 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE CSD DRIVE LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 202HN 527 7115 LE45078E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1997060500249 19970605 00249 NE 1997 6 5 97ZZZX2431 2 19961227 A 7230 430150610 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE NR 2 BEARING LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 202HN 527 1203 7115 LE45078E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1997060500250 19970605 00250 NE 1997 6 5 97ZZZX2432 2 19961227 A 7260 430101501 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE ACCESSORY DRIVE LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 202HN 527 7115 LE45078E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH 3 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1997060500251 19970605 00251 NE 1997 6 5 97ZZZX2433 2 19961227 A 7260 430101301 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE AFT ALTERNATOR LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 202HN 527 7115 LE45078E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1997060500258 19970605 00258 NM 1997 6 5 97ZZZX2440 1 19961216 A 7720 311671201 THERMOCOUPLE DOUG MD900 MD900 3027375 NM ENGINE T6 WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 628 EM60787004 90000012 THERMOCOUPLE WORN BEYOND SERVICEABLE LIMITS AND REMOVED IN COMPLIANCE TO SB 28096. REPLACED WITH NEW UNIT, CORRECTED PR OBLEM. 1 G 7 2 3U NC H19NM 1997060500264 19970605 00264 NM 1997 6 5 97ZZZX2446 1 19961216 A 6330 900D3408076101 ISOLATOR BOLT DOUG MD900 MD900 3027375 NM M/R DRIVE DELAMINATED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 1086 90000012 DELAMINATION. REPLACED WITH NEW 8 EACH UNITS, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1997060500265 19970605 00265 NM 1997 6 5 97ZZZX2447 1 19961216 A 7720 311671201 THERMOCOUPLE DOUG MD900 MD900 3027375 NM ENGINE T6 WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 495 EM50191305 90000012 THERMOCOUPLE WORN BEYOND SERVICEABLE LIMITS AND REMOVED IN COMPLIANCE TO SB 28096. REPLACED WITH NEW UNIT, CORRECTED PR OBLEM. 1 G 7 2 3U NC H19NM 1997060500266 19970605 00266 NM 1997 6 5 97ZZZX2448 1 19961216 A 7720 311671201 THERMOCOUPLE DOUG MD900 MD900 3027375 NM ENGINE T6 WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 495 EM57011002 90000012 THERMOCOUPLE WORN BEYOND SERVICEABLE LIMITS AND REMOVED IN COMPLIANCE TO SB 28096. REPLACED WITH NEW UNIT, CORRECTED PR OBLEM. 1 G 7 2 3U NC H19NM 1997060500292 19970605 00292 NE 1997 6 5 97ZZZX2474 2 19960130 A 7321 8080803009 EEC DOUG MD900 MD900 3027375 NM PWA PW206 PW206A NE ENGINE MALFUNCTION A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 218 C94010004 90000012 PCE206042 ELECTRONIC ENGINE CONTROL INSTALLATION. TROUBLESHOOTING SOFTWARE. EEC PUTTING OUT ERRATIC AND FALSE INFORMATION. REPL ACED WITH NEW UNIT, CORRECTED PROBLEM. CORES RETURNED TO MDHS FROM RNO. 1 G 7 2 3U 3 U NC H19NM E42NE 1997060500301 19970605 00301 SW 1997 6 5 97ZZZX2482 1 19960417 A 2911 MS28775234 O-RING SWRNGN SA226 SA226TB 8780406 SW HYD ACCUM DEFECTIVE A C2SA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 01 O-RING WAS BEING LUBRICATED PRIOR TO INSTALLATION WHEN A DEFECT WAS FELT. THE CROSS SECTIONAL AREA WAS REDUCED FOR .375 INCH IN A GRADUAL MANNER MAKING VISUAL DETECTION DIFFICULT. PART WAS APPARENTLY MANUFACTURED BY SWAN ENGINEERING. 2 L 7 2 4T RT A5SW 1997060500875 19970605 00875 NM 1997 6 5 EIAA970071 1 19961003 A 5315 FLOORBEAM BOEING 747 747273C 1384896 NM BS 480 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 SAT - DURING B-CHECK INSPECTION, FOUND FLOORBEAM AT STATION 480, LBL 24 TO LBL 29 CORRODED AT PREVIOUS REPAIR. REMOVED DAMAGED SECTION OF FLOORBEAM FROM BL 0 TO LBL 72. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-07, FIG 12. (M) 2 L 7 4 4F A20WE 1997060500876 19970605 00876 NM 1997 6 5 EIAA970074 1 19961003 A 5320 WEB BOEING 747 747273C 1384896 NM BS 455/520 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 SAT - DURING B-CHECK INSPECTION, FOUND CABIN FLOOR WEB CRACKED AT STATION FORWARD AND AFT SIDE OF STATION 520 AND CORROD ED AT STATION 455 LBL 11. REPAIRED WEB AND INSTALLED DOUBLERS PER SRM 51-20-01, 51-40-2, AND 51-10-02. REMOVED CORROSI ON, TREATED, ALODINED AND PRIMED PER SRM 51-10-01. (M) 2 L 7 4 4F A20WE 1997061200477 19970612 00477 NM 1997 6 12 GAIA9731 1 19960517 A 5311 FRAME BOEING 727 727223 1384074 NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING CPC INSPECTION, THE FOLLOWING LEVEL 2 ITEMS WERE NOTED: W/C 0148, RT SIDE OF DOG HOUSE 3RD FRAME EXFOLIATED. AL L ITEMS WERE CORRECTED DURING C-CHECK ON THE LISTED CARDS. REF: OPERATOR CONTROL NR 97ZZZX2697 THROUGH 97ZZZX2702. (X ) 2 L 7 3 4F A3WE 1997061200478 19970612 00478 NM 1997 6 12 97ZZZX2697 1 19960517 A 5311 FRAME BOEING 727 727223 1384074 NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING CPC INSPECTION, THE FOLLOWING LEVEL 2 ITEMS WERE NOTED: W/C 0149, RT SIDE OF DOG HOUSE 4TH FRAME EXFOLIATED. A LL ITEMS WERE CORRECTED DURING C-CHECK ON THE LISTED CARDS. REF: OPERATOR CONTROL NR GAIA9731 AND 97ZZZX2698 THROUGH 9 7ZZZX2702. 2 L 7 3 4F A3WE 1997061200479 19970612 00479 NM 1997 6 12 97ZZZX2698 1 19960517 A 5320 STIFFENER BOEING 727 727223 1384074 NM BS 300 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING CPC INSPECTION, THE FOLLOWING LEVEL 2 ITEMS WERE NOTED: W/C 0150, STIFFENER STA 300 ON TOP OF DOG HOUSE. ALL ITEMS WERE CORRECTED DURING C-CHECK ON THE LISTED CARDS. REF: OPERATOR CONTROL NR GAIA9731 AND 97ZZZX2697 THROUGH 97ZZ ZX2702. 2 L 7 3 4F A3WE 1997061200480 19970612 00480 NM 1997 6 12 97ZZZX2699 1 19960517 A 5230 BEAM BOEING 727 727223 1384074 NM CARGO DOOR CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING CPC INSPECTION, THE FOLLOWING LEVEL 2 ITEMS WERE NOTED: W/C 0260, NR 1 CARGO DOOR LOWER BEAM RT CORNER. ALL I TEMS WERE CORRECTED DURING C-CHECK ON THE LISTED CARDS. REF: OPERATOR CONTROL NR GAIA9731 AND 97ZZZX2697 THROUGH 97ZZZ X2702. 2 L 7 3 4F A3WE 1997061200481 19970612 00481 NM 1997 6 12 97ZZZX2700 1 19960517 A 5230 WEB BOEING 727 727223 1384074 NM CARGO DOOR CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING CPC INSPECTION, THE FOLLOWING LEVEL 2 ITEMS WERE NOTED: W/C 0263, NR 1 CARGO DOOR LOWER WEB AND STIFFENER. AL L ITEMS WERE CORRECTED DURING C-CHECK ON THE LISTED CARDS. REF: OPERATOR CONTROL NR GAIA9731 AND 97ZZZX2697 THROUGH 97 ZZZX2702. 2 L 7 3 4F A3WE 1997061200482 19970612 00482 NM 1997 6 12 97ZZZX2701 1 19960517 A 5314 KEEL BEAM BOEING 727 727223 1384074 NM BS 760-783 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING CPC INSPECTION, THE FOLLOWING LEVEL 2 ITEMS WERE NOTED: W/C 0321, KEEL BEAM WEB AT STA 760-783 BL ZERO. ALL I TEMS WERE CORRECTED DURING C-CHECK ON THE LISTED CARDS. REF: OPERATOR CONTROL NR GAIA9731 AND 97ZZZX2697 THROUGH 97ZZZ X2702. 2 L 7 3 4F A3WE 1997061200483 19970612 00483 NM 1997 6 12 97ZZZX2702 1 19960517 A 5720 SUPPORT BOEING 727 727223 1384074 NM RT WING CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 20180 DURING CPC INSPECTION, THE FOLLOWING LEVEL 2 ITEMS WERE NOTED: W/C 0067, RT W/W STA 870 SUPPORT UNDER SPOILER MIXER. AL L ITEMS WERE CORRECTED DURING C-CHECK ON THE LISTED CARDS. REF: OPERATOR CONTROL NR GAIA9731 AND 97ZZZX2697 THROUGH 97 ZZZX2701. 2 L 7 3 4F A3WE 1997061200484 19970612 00484 NM 1997 6 12 GAIA9732 1 19960517 A 5230 MS200116 HINGE BOEING 727 727223 1384074 NM CARGO DOOR CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6827 2789 20180 MAIN CARGO DOOR FRAME EXTERIOR, CARGO DOOR HINGE ON AIRCRAFT, LAST TWO AFT SEGMENTS CRACKED. REMOVED AND INSTALLED NEW HINGE. (X) 2 L 7 3 4F A3WE 1997061200798 19970612 00798 NE 1997 6 12 97ZZZX2725 2 19960725 A 7250 410106701 SEAL RING BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE 1ST TURB SHROUD WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 117CW 599 7125 LE45295E SEAL RING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1997061200799 19970612 00799 NE 1997 6 12 97ZZZX2726 2 19960725 A 7250 410106802 SPRING BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE SEAL RING WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 117CW 7125 LE45295E SEAL RING EXPANDER SPRING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1997061200800 19970612 00800 NE 1997 6 12 97ZZZX2727 2 19960705 A 7260 430101201 SEAL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE ALTERNATOR FWD LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 117CW 599 7125 LE45295E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1997061200801 19970612 00801 NE 1997 6 12 97ZZZX2728 2 19960725 A 7260 430101301 SEAL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE ALTERNATOR AFT LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 117CW 599 7125 LE45295E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1997061200802 19970612 00802 NE 1997 6 12 97ZZZX2729 2 19960705 A 7260 430101501 SEAL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE ACCESSORY DRIVE LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 117CW 599 7125 LE45295E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH 3 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1997061200803 19970612 00803 NE 1997 6 12 97ZZZX2730 2 19960725 A 7250 430144801 SEAL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE NR 3 BEARING LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 117CW 599 57646 7125 LE45295E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1997061200804 19970612 00804 NE 1997 6 12 97ZZZX2731 2 19960725 A 7230 430150601 SEAL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE NR 2 BEARING LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 117CW 599 1271 7125 LE45295E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1997061200805 19970612 00805 NE 1997 6 12 97ZZZX2732 2 19960725 A 7260 230307203 SEAL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE CSD DRIVE LIP LEAK A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 117CW 599 7125 LE45295E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1997061200806 19970612 00806 NE 1997 6 12 97ZZZX2733 2 19961018 A 7260 230307203 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE CSD DRIVE LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 417BK 577 7143 LE45552EF SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997061200807 19970612 00807 NE 1997 6 12 97ZZZX2734 2 19961018 A 7260 430101201 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE ALTERNATOR AFT LEAK A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 417BK 577 7143 LE45552EF SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997061200808 19970612 00808 NE 1997 6 12 97ZZZX2735 2 19961018 A 7260 430101301 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE ALTERNATOR AFT LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 417BK 577 7143 LE45552EF SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997061200809 19970612 00809 NE 1997 6 12 97ZZZX2736 2 19961018 A 7260 430101501 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE ACCESSORY DRIVE LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 417BK 577 7143 LE45552EF SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997061200810 19970612 00810 NE 1997 6 12 97ZZZX2737 2 19961018 A 7260 430124102 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE ACCESSORY DRIVE LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 417BK 577 7143 LE45552EF SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997061200811 19970612 00811 NE 1997 6 12 97ZZZX2738 2 19961018 A 7250 430144801 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE NR 3 BEARING LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 417BK 577 48984 7143 LE45552EF SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997061200812 19970612 00812 NE 1997 6 12 97ZZZX2739 2 19961018 A 7230 430150601 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE NR 2 BEARING LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 417BK 577 1289 7143 LE45552EF NR 2 BEARING SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997061200813 19970612 00813 NE 1997 6 12 97ZZZX2740 2 19960719 A 7260 230093303 BEARING BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE ACCESSORY DRIVE ROUGH A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 528SF 858 7104 LE45242E BEARING ROUGH. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1997061200814 19970612 00814 NE 1997 6 12 97ZZZX2741 2 19960719 A 7250 410106701 SEAL RING BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE 1ST TURB SHROUD WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 528SF 7104 LE45242E SEAL RING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1997061200816 19970612 00816 NE 1997 6 12 97ZZZX2743 2 19960719 A 7230 430404701 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE NR 1 BEARING CHIPPED A R7MA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 11 528SF 5A500 7104 LE45242E SEAL NEW OUT-OF-BOX AND CHIPPED BEYOND ALLOWABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1997061200817 19970612 00817 NE 1997 6 12 97ZZZX2744 2 19961125 A 7250 414129001 ROTOR ASSY BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE POWER TURBINE BLADE SHIFT A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 586BH 1051 SC46899 7129 LE45144E ROTOR ASSY FAILED SB LT101-72-10-0153. EXCESSIVE IBPT BLADE SHIFT NR 20 +0.010 INCH. REPLACED WITH USED UNIT, CORRECTE D PROBLEM. PART TOTAL CYCLES, 2,294.2. 1 G 7 2 3U 3 U H13EU E5NE 1997061200818 19970612 00818 NE 1997 6 12 97ZZZX2745 2 19961117 A 7230 430150601 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE NR 2 BEARING LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 7060G 626 7173 LE45511EF SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997061200819 19970612 00819 NE 1997 6 12 97ZZZX2746 2 19961117 A 7250 430124203 BEARING BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE NR 3 PITTED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 7060G 973 0384 7173 LE45511EF BEARING HAS EXCESSIVE PITTING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997061200820 19970612 00820 NE 1997 6 12 97ZZZX2747 2 19961117 A 7260 430124102 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE ACCESSORY DRIVE LEAK A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 7060G 626 7173 LE45511EF SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997061200821 19970612 00821 NE 1997 6 12 97ZZZX2748 2 19961117 A 7260 430101501 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE ACCESSORY DRIVE LEAK A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 7060G 626 7173 LE45511EF SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997061200822 19970612 00822 NE 1997 6 12 97ZZZX2749 2 19961117 A 7260 430101201 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE ALTERNATOR FWD LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 7060G 7173 LE45511EF SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997061200823 19970612 00823 NE 1997 6 12 97ZZZX2750 2 19961117 A 7250 410106802 SPRING BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE SEAL RING WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 7060G 626 7173 LE45511EF SEAL RING EXPANDER SPRING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997061200825 19970612 00825 NE 1997 6 12 97ZZZX2752 2 19961117 A 7260 230307203 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE ACCESSORY DRIVE LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 7060G 626 7173 LE45511EF SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997061200851 19970612 00851 NM 1997 6 12 CA970326003 1 19960913 A 5753 65192708 TRACK BOEING 65192708 BOEING 727 72751C 1384015 NM PWA JT8 JT8D7B 52053 NE NR 4 FLAP CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 654436 (CAN) DURING ROUTINE INSPECTION OF AD 90-07-05, SB 727-57-178R5 TO THE LH INBOARD FLAP AND #4 FLAP TRACK A CRACK WAS FOU ND THAT EXTENDED AROUND THE ENTIRE BOLT HOLE. INSPECTION AS PER PART ONE OF SB, TRACK DID NOT HAVE THE REPAIR OR THE PRE VENTIVE MODIFICATION INSTALLED. AREA OF CRACK WAS DISCOLORED INDICATING CRACK HAD BEEN THERE FOR SOME TIME. REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 1997061900015 19970619 00015 NM 1997 6 19 AALA961885 1 19961223 A 2421 IDG BOEING 767 767223 1385123 NM LT ENGINE FAILED A AALA H DEACTIVATE SYST/CIRCUITS H ELECT. POWER LOSS-50 PC CR CRUISE 1 SW 07 330AA 22330 GIG - FLT 0973 - LEFT GENERATOR FAILURE. ATTEMPTED ONE RESET, BUT UNSUCCESSFUL. MEL REF 24-01 AUTH NR 12-368DC-B. DEF ERRED LT IDG INOPERATIVE PER MEL. ACCOMPLISHED MPM 24-01 - MIC SHEET ENTERED. REPLACED THE ENGINE DRIVEN GENERATOR. R AN ENGINE GENERATOR, OPS CHKS OK. CLEARED MIC SHEET AND REMOVED PLACARD 12-368DC-8. GENERATOR LEAK CKS OK. (X) 2 L 7 2 4F RT A1NM 1997061900016 19970619 00016 NM 1997 6 19 AALA961886 1 19961228 A 2420 BUS CONTL UNIT BOEING 767 767323 1385205 NM LT/RT ENGINE FAILED A AALA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 SW 07 385AM 27059 MIA - FLT 0911 - BOTH UTILITY BUSSES CYCLE OFF THEN ON AT ABOUT 1 MINUTE INTERVALS. TURNED OFF ALL GALLEY OVENS AND BOT H RECIRC FANS AND PROBLEM CONTINUED. TRIED USING ONE UTILITY BUS. PROBLEM CONTINUED. BOTH BUSSES TURNED OFF REMAINDE R OF FLIGHT. REPLACED THE BUS CONTROL UNIT. ACCOMPLISHED ENGINES 1 AND 2 RUN-UP. LOADED LT AND RT UTILITY BUSSES, ALL CK'D NORMAL. COULD NOT DUPLICATE FAULT. PLEASE OBSERVE AND ADVISE. (X) 2 L 7 2 4F RT A1NM 1997061900017 19970619 00017 NM 1997 6 19 AALA961888 1 19961228 A 2421 IDG BOEING 767 767323 1385205 NM LT ENGINE FAILED A AALA H DEACTIVATE SYST/CIRCUITS H ELECT. POWER LOSS-50 PC CR CRUISE 1 SW 07 352AA 24033 JFK - FLT 0016 - IN-FLIGHT FLICKERING LEFT GENERATOR DRIVE LIGHT ON WITH LEFT EICAS IDG TEMP SENSOR LIGHT. GENERATOR OF F LIGHT CAME ON INTERMITTENTLY. LEFT IDG WAS DISCONNECTED. REPLACED LT IDG. RAN ENGINE, ALL PARAMETERS CK NORMAL. RE CONNECTED IDG. LEAK CK OK. (X) 2 L 7 2 4F RT A1NM 1997061900018 19970619 00018 NM 1997 6 19 AALA961889 1 19961228 A 2421 IDG BOEING 767 767223 1385123 NM RT ENGINE FAILED A AALA H DEACTIVATE SYST/CIRCUITS H J ELECT. POWER LOSS-50 PC WARNING INDICATION DE DESCENT 1 SW 07 312AA 22315 BRU - FLT 0088 - RIGHT GENERATOR DRIVE EICAS MESSAGE WITH ASSOCIATED RT GEN OFF LIGHT. REPLACED SCAVENGE FILTER (SMALL CHIPS FROM NORMAL WEAR). LOW OIL PRESSURE+UNDERFREQ TRIP+IDG/PMG WIRING ON BPCU BIT. IDG REMAINS DISCONNECTED. IDG SE RVICED. APU SERVICED. ETOPS LESS THAN 120 MINS ALLOWED. MIC SHEET ENTERED. REMOVED AND REPLACED ENG DRIVEN GENERATOR . SYSTEM LEAK CHECKED AND OPERATIONALLY CHECKED DURING ENG RUN AND FULL LOAD. SYSTEM OPS CKD NORMAL. CLEARED MEL. RE F: 24-01 AUTH 12-443DC-B. CLEARED MIC. (X) 2 L 7 2 4F RT A1NM 1997061900019 19970619 00019 NM 1997 6 19 AALA961890 1 19961230 A 2421 IDG BOEING 767 767223 1385123 NM LT ENGINE FAILED A AALA H DEACTIVATE SYST/CIRCUITS H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 SW 07 325AA 22326 ZRH - FLT 0038 - EICAS MESSAGE - LEFT GEN DRIVE-AND LEFT GEN DRIVE LIGHT ON. DISCONNECTED LEFT GENERATOR DRIVE IAW VOL 1. REPLACED LT IDG. REF. MM 24-11-00. CPN INSTALLED GEN 5103. BITE AND OPS CHECKS PERF.ACC.MM 24-11-00. ALL CHECKS OK. ACFT OK FOR SERVICE. (X) 2 L 7 2 4F RT A1NM 1997061900020 19970619 00020 NM 1997 6 19 AALA961891 1 19961231 A 2421 IDG BOEING 767 767223 1385123 NM RT ENGINE FAILED A AALA H DEACTIVATE SYST/CIRCUITS H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 SW 07 312AA 22315 LGW - FLT 0174 - RIGHT GENERATOR DRIVE LIGHT AND GENERATOR OFF LIGHT ILLUMINATED AT FL 100 ABOVE GRD DURING APPROACH. R EPEAT ITEM ACCOMPLISHED OM PROCEDURE. DISCONNECTED IDG. CHECKED RT IDG SCAVENGE FILTER. NO DEBRIS FOUND. SERVICED LT IDG TO FULL. CHECKED APU OIL LEVEL, FULL. DUE TO HISTORY, DEF TO MICS PER MEL. ALL PROCEDURES FOR MPM 24-01 ACCOMPLI SHED. ER RESTRICTED TO 120 MINS. VERIFIED RT IDG DISCONNECTED, BPCU BITE SHOWED LOW OIL PRESSURE, UNDER FREQ TRIP, IDG PMG WIRING. PERFORMED CONTINUITY CHECKS OF WIRING BETWEEN GCU AND IDG TEMP BULB, PMG WIRING. NO FAULTS NOTED. REPLAC ED RT GCU PER MM. OPS CHECKS GOOD. MIC SHEET AND MEL CLEARED. (X) 2 L 7 2 4F RT A1NM 1997061900021 19970619 00021 NM 1997 6 19 AALA961892 1 19961231 A 2421 IDG BOEING 767 767223 1385123 NM RT ENGINE FAILED A AALA H J DEACTIVATE SYST/CIRCUITS DUMP FUEL H ELECT. POWER LOSS-50 PC CR CRUISE 1 SW 07 317AA 22319 ORY - FLT 0146 - DURING CRUISE AT FL 310, RT GENERATOR LIGHT AND RT GENERATOR CONTROL LIGHT ILLUMINATED. GENERATOR WOUL D NOT RESET. APU WORKED OK. RT GENERATOR DRIVE DISCONNECTED. REPLACED RT IDG IAW MM. LEAK CHK OK, IDG TESTED OK. (X ) 2 L 7 2 4F RT A1NM 1997061900488 19970619 00488 NM 1997 6 19 CA970109027 1 19961211 A 3244 TIRE BOEING 747 747233B NM PWA JT9 JT9D7 52054 NE NR 8 WHEEL SEPARATED W K NONE O OTHER TO TAKEOFF 1 CA P689576 (CAN) DURING TAKEOFF #8 TIRE RETREAD SEPARATED DAMAGING FIBERGLASS PANELS. REPAIRED OR REPLACED. 2 L 7 4 4F 4 F RT A20WE E20EA 1997061900489 19970619 00489 NM 1997 6 19 CA970109029 1 19961204 A 2710 60B800504 ACTUATOR BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE AILERON FAILED W O OTHER J WARNING INDICATION CR CRUISE 1 CA P709632 (CAN) EICAS (ENGINE INDICATION AND CREW ALERTING SYSTEM) MESSAGE AILERON LOCKOUT. RH AILERON LOCKOUT CYLINDER REPLACED. 2 L 7 2 4F 4 F RT A1NM E3NE 1997061900491 19970619 00491 NM 1997 6 19 CA970114021 1 19961226 A 5247 7321387004 ACTUATOR BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE APU DOOR DAMAGED W K NONE O OTHER CR CRUISE 1 CA P709675 (CAN) AT FL250 LOUD BANG AND PRONOUNCED AIRFRAME VIBRATION. APU INLET DOOR AND ADJACENT SKIN DAMAGED. DOOR AND ACTUATOR REPLACED AND DAMAGE REPAIRED 2 L 7 2 4F 4 F RT A1NM E3NE 1997061900499 19970619 00499 NM 1997 6 19 CA970121008 1 19961020 A 3244 31395 TIRE BOEING 727 72790C 1384030 NM PWA JT8 JT8D7B 52053 NE R/H NOSE BLOWN W A J UNSCHED LANDING DUMP FUEL O OTHER TO TAKEOFF 1 CA 653770 (CAN) ON TAKEOFF CREW DETERMINED WHAT WAS THOUGHT TO BE A TIRE BLOW OUT ON ROTATION. AIRCRAFT LANDED. RUBBER ON RUNWAY, R/H NOSE TIRE SHOWED INDICATTIONS OF LANDING WITH BRAKES ON. AIRCRAFT TOOK OFF IN SLUSH CONDITIONS AND LANDED WITH FROZE N BRAKE. TIRE REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 1997061900502 19970619 00502 NM 1997 6 19 CA970130001 1 19961128 A 2910 AV13J5101 VALVE BOEING 727 727227 1384078 NM PWA JT8 JT8D9A 52048 NE HYD SYS LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA G66052A 666126 (CAN) HEAVY HYDRAULIC LEAK AT GROUND INTERCONNECT VALVE BODY, REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 1997061900513 19970619 00513 CE 1997 6 19 CA970206007 1 19961022 A 3010 5E1319 DE-ICING BOOT BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA L/H WING SHORTED W K NONE L NO TEST IN INSP/MAINT 1 CA 410 PCE50534 (CAN) CREW REPORTED THE LEFT HAND DE-ICE BOOT INOPERATIVE. INSPECTION FOUND A SHORTED, BURNED WIRE IN THE LEFT HAND TOP PART OF THE BOOT. THE BOOT WAS REPLACED. SUBMITTER STATES THIS IS THE THIRD INCIDENT IN THE PAST YEAR. 1 L 7 2 3T 4 T A14CE E4EA 1997061900514 19970619 00514 SW 1997 6 19 CA970206009 1 19961217 A 5620 33036710 WINDOW GULSTM 690TP 690B 7630516 SW GARRTT TPE331 TPE3315 01514 WP ALONG SCREWS CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 4728 P06697 (CAN) LATERAL CRACK RUNNING ALONG THE FASTENING SCREWS OF THE OUTBOARD WINDOW. THE CRACK COULD NOT BE SEEN WITH A PRISM AND WAS ONLY DETECTED WHEN IT SPLIT THE WINDOW IN TWO AT THE FORWARD CORNER DOWN TO THE MIDWAY POINT. SUBMITTER STATES T HE CRACK PROBABLY CREPT AONG THE FASTENER LINE FOR SOME TIME BEFORE DETECTION. 1 H 7 2 3T 4 T 2A4 E4WE 1997061900516 19970619 00516 CE 1997 6 19 CA970206016 1 19961223 A 2710 AN15532L TURNBUCKLE CESSNA 180 180 2072602 CE CONT O470 O470K 17026 SO AILERON CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 3708 989219RR (CAN) THREE CRACKS AT THE LEFT HAND THREAD END OF THE TURNBUCKLE BARREL WERE FOUND EXTENDING INWARD 0.50 INCHES ON TWO C RACKS AND 0.65 INCHES. 1 H 7 1 3O 3 O NC 5A6 E273 1997061900523 19970619 00523 GL 1997 6 19 CA970211003 2 19961220 A 7323 2040607627 LINEAR ACTUATOR BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL LOW STOP LIMIT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA CAE821966 (CAN) ACTUATOR EXTEND LIMIT SWITCH HOUSING WAS FOUND CRACKED. A RIGGING CHECK WAS CARRIED OUT, NO LIMITS EXCEEDED. 1 G 7 1 3U 3 U H2SW E4CE 1997061900525 19970619 00525 NE 1997 6 19 CA970212002 2 19961020 A 7532 BACC10DU300Y CLAMP BOEING 727 727225 1384077 NM PWA JT8 JT8D7 52053 NE NR 3 ENG STRUT WRONG SIZE W J A DUMP FUEL UNSCHED LANDING M OVER TEMP CL CLIMB 1 CA 653417 (CAN) DURING CLIMB #3 ENGINE STRUT OVERTEMPERATURE HEAT LIGHT CAME ON. ENGINE BLEED SELECTED OFF. LIGHT WOULD NOT GO OUT . THRUST LEVER RETARDED TO 1.6 EPR, LIGHT OUT. FUEL DUMPED, LANDED. CLAMP LEAKING UP STREAM OF 13 STAGE MODULATING AND S HUT OFF VALVE, WOULD NOT TIGHTEN, CLAMP WRONG SIZE, TOO LARGE. REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 1997061900527 19970619 00527 NM 1997 6 19 CA970212007 1 19961101 A 2131 7612607 CONTROLLER BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE PRESSURIZATION INTERMITTENT W O OTHER G MULTIPLE FAILURE LD LANDING 1 CA 33775 3906 709520 (CAN) ON DESCENT AIRPLANE TOTALLY DEPRESSURIZED. DID NOT AUTO SWITCH TO STANDBY. NO TIME TO TROUBLESHOOT. DID NOT APPEAR TO WORK IN STANDBY. REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1997062600009 19970626 00009 EU 1997 6 26 CA970225001 1 19961213 A 6230 10541904 SWASHPLATE BOLKMS 105 BO105C 5626005 EU ALLSN 250C 250C20B 03013 GL LOWER SEAL BEARING FAILED W A UNSCHED LANDING O OTHER DE DESCENT 1 CA 3963 972 CAE835521 (CAN) DURING DAILY INSPECTION THE AME NOTICED BLACK GREASE COMING FROM BOTTOM SURFACE OF SWASHPLATE. SWASHPLATE REGREASE D AND AIRCRAFT RETURNED TO SERVICE. APPROXIMATELY 1.5 HOURS INTO FLIGHT A 'HOWLING' NOISE HEARD. AME FOUND EXCESSIVE BLA CK GREASE IN SAME AREA. ALL LINKS DISCONNECTED AND SWASHPLATE CHECKED FOR ROTATIONAL SMOOTHNESS. EXCESSIVE ROUGHNESS FEL T, LOWER BEARING WAS ROTATING IN OUTER RING. 1 G 7 2 3U 3 U H3EU E4CE 1997062600476 19970626 00476 NE 1997 6 26 CA970311004 2 19961128 A 7261 9550113490 CONNECTOR SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENG MAG PLUG BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 834 (CAN) DURING INSPECTION THE ENGINE MAGNETIC PLUGS WERE FOUND NOT WORKING. WIRE WAS FOUND BROKEN IN THE CONNECTOR WHERE T U208 HARNESS PLUGS INTO ENGINE WIRING. 1 G 7 1 3U 3 U H9EU E19EU 1997062600477 19970626 00477 WP 1997 6 26 CA970311005 1 19960928 A 2823 369A8137503 SHUT OFF CABLE HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL FUEL SOV BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA CAE830901 (CAN) PILOT PULLED OUT FUEL SHUT OFF KNOB AND CABLE CAME OUT FURTHER THAN NORMAL. INVESTIGATION REVEALED THAT THE CABLE HAD BROKEN AT THE VALVE END. 1 G 7 1 3U 3 U H3WE E4CE 1997062600478 19970626 00478 GL 1997 6 26 CA970311006 2 19960924 A 7323 23006259 GOVERNOR BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL SHAFT SEAL LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 222 CAE820733 (CAN) FUEL LEAKING AT THE SHAFT TO BODY SEAL. 1 G 7 1 3U 3 U H2SW E4CE 1997062600479 19970626 00479 WP 1997 6 26 CA970311007 1 19960927 A 2430 A700AAP RELAY HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL GEN RCC DEFECTIVE W K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 CA CAE830901 (CAN) GENERATOR WOULD NOT COME ON LINE. REVERSE CURRENT RELAY CHANGED. 1 G 7 1 3U 3 U H3WE E4CE 1997062600480 19970626 00480 GL 1997 6 26 CA970311008 2 19960920 A 7323 23006259 GOVERNOR BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL INTERNAL LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 141 CAE820733 (CAN) FUEL LEAKING FROM GOVERNOR BODY. 1 G 7 1 3U 3 U H2SW E4CE 1997062600481 19970626 00481 EU 1997 6 26 CA970311009 1 19960919 A 6510 355A34107828 SPLINED COUPLING SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE T/R SHAFT INCORRECT W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 835 (CAN) DIFFICULTY BALANCING THE TAIL ROTOR DRIVESHAFT. COUPLING INSPECTED AND FOUND STEEL AS355 COUPLING INSTALLED. COUPL ING REMOVED AND CORRECT AS350 COUPLING INSTALLED. 1 G 7 1 3U 3 U H9EU E19EU 1997062600482 19970626 00482 1997 6 26 CA970311014 4 19960909 A 3421 RCA26BK3 INDICATOR SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE COCKPIT ATTITUDE BAD DISPLAY W K NONE O OTHER IN INSP/MAINT 1 CA 4432 (CAN) ATTITUDE INDICATOR FLAG WILL NOT RETRACT. 1 G 7 1 3U 3 U NC H9EU E19EU 1997062600483 19970626 00483 SW 1997 6 26 CA970311015 1 19960909 A 2436 VR1010241A VOLTS REGULATOR BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL DC SYS NOT CHARGING W K NONE O OTHER IN INSP/MAINT 1 CA CAE832831 (CAN) ONLY PRODUCING 25 VOLTS. GENERATOR NOT CHARGING BATTERY. 1 G 7 1 3U 3 U H2SW E4CE 1997062600484 19970626 00484 SW 1997 6 26 CA970311018 1 19960708 A 5553 206020113103 VERTICAL STAB BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL MOUNT PAD CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA CAE801518BA (CAN) FIN STRUCTURE CRACKED ADJACENT TO UPPER ATTACHMENT INSERTS. 1 G 7 1 3U 3 U H2SW E4CE 1997062600485 19970626 00485 SW 1997 6 26 CA970311019 1 19960723 A 5530 206020113107 VERTICAL STAB BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL MOUNT INSERT INSERT FAILED W K NONE O OTHER IN INSP/MAINT 1 CA CAE801518BA (CAN) INSERT FAILURE AND SURROUNDING HONEYCOMB DAMAGED. 1 G 7 1 3U 3 U H2SW E4CE 1997062600486 19970626 00486 SW 1997 6 26 CA970311020 1 19960706 A 2435 23032027 GENERATOR BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL START/GEN WORN W K NONE O OTHER IN INSP/MAINT 1 CA 705 CAE821443 (CAN) COMMUTATOR WORN. 1 G 7 1 3U 3 U H2SW E4CE 1997062600487 19970626 00487 EU 1997 6 26 CA970311021 1 19960724 A 7712 30573133 INDICATOR SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE TORQUEMETER INTERMITTENT W K NONE O OTHER IN INSP/MAINT 1 CA 1043 878 (CAN) TORQUEMETER BEGAN TO OPERATE INTERMITTENTLY THEN BLEW A FUSE AND QUIT. 1 G 7 1 3U 3 U H9EU E19EU 1997062600488 19970626 00488 SW 1997 6 26 CA970311024 1 19960706 A 6410 206011810013 BLADE BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL T/R PAINT EROSION W K NONE O OTHER IN INSP/MAINT 1 CA 6107 1307 CAE831866 (CAN) PAINT GONE ON ONE BLADE. 1 G 7 1 3U 3 U H2SW E4CE 1997062600489 19970626 00489 EU 1997 6 26 CA970311025 1 19960715 A 2435 524031 GENERATOR SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE DC SYS MALFUNCTION W A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 CA 3295 977 258 (CAN) GENERATOR WENT OFFLINE IN FLIGHT. TRANSISTOR Q1 OF THE TB2 REGULATION IN THE MASTER ELECTRICAL BOX WAS FOUND FAULT Y. 1 G 7 1 3U 3 U H9EU E19EU 1997062600490 19970626 00490 SW 1997 6 26 CA970311026 1 19960716 A 6520 2060404005 GERARBOX BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL T/R GEAR TRAIN MAKING METAL W K NONE O OTHER IN INSP/MAINT 1 CA 9169 3392 CAE821010 (CAN) POOR GEAR PATTERN CAUSED FUZZ ON CHIP PLUG. INPUT SEAL AND PITCH SEALS LEAKING. 1 G 7 1 3U 3 U H2SW E4CE 1997062600491 19970626 00491 SW 1997 6 26 CA970311027 1 19960716 A 6230 206010450113 SWASHPLATE ASSY BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL M/R UNBONDED W K NONE O OTHER IN INSP/MAINT 1 CA 10232 3058 CAE802195BA (CAN) UPPER SEAL CAME UNBONDED FROM OUTER CAP P/N 206-010-444-001 ALLOWING IT TO SPIN IN METAL TO METAL. 1 G 7 1 3U 3 U H2SW E4CE 1997062600493 19970626 00493 SW 1997 6 26 CA970311029 1 19960501 A 3213 206031301023 SUPPORT BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL GEAR ATTACH CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA CAE820733 (CAN) CRACKS AROUND LANDING GEAR ATTACHMENTS. 1 G 7 1 3U 3 U H2SW E4CE 1997062600494 19970626 00494 SW 1997 6 26 CA970311030 1 19960501 A 7120 2060313372 ENGINE MOUNT BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL END FITTING CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA CAE820733 (CAN) MOUNT FITTING CRACKED. 1 G 7 1 3U 3 U H2SW E4CE 1997062600495 19970626 00495 SW 1997 6 26 CA970311031 1 19960307 A 5312 206031301023 BULKHEAD BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL BS 98 BL9 CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 9867 CAE822745 (CAN) CRACKS AND PULLED RIVETS ON LOWER SUPPORT. LEFT HEAD BULKHEAD P/N 206-031-107-117H CRACKED. INNER SKIN CRACKED AT FS98 AND BL9. 1 G 7 1 3U 3 U H2SW E4CE 1997062600496 19970626 00496 SW 1997 6 26 CA970311032 1 19960515 A 5302 206031329103 ATTACH FITTING BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL TAILBOOM CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA CAE823527 (CAN) UPPER TAILBOOM ATTACHMENT FITTING CRACKED. 1 G 7 1 3U 3 U H2SW E4CE 1997062600497 19970626 00497 SW 1997 6 26 CA970311033 1 19960426 A 5313 206031332031S LONGERON BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL L/H SUPPORT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA CAE860407 (CAN) LEFT HAND SUPPORT P/N 206-031-332-031S AND LEFT LONGERON CRACKED AND WORKING. 1 G 7 1 3U 3 U H2SW E1GL 1997062600498 19970626 00498 WP 1997 6 26 CA970311034 1 19960601 A 5320 369A300027 INTERCOSTAL HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL STN 137.5 CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA CAE830896 (CAN) INTERCOSTAL CRACKED ON UPPER TURTLEBACK SKIN BETWEEN STN 137.5 AND 146.62 ON THE RIGHT HAND SIDE. 1 G 7 1 3U 3 U H3WE E4CE 1997062600499 19970626 00499 WP 1997 6 26 CA970311035 1 19960727 A 6322 369D25623 BELT HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL OIL COOLER DAMAGED W K NONE O E OTHER VIBRATION/BUFFET IN INSP/MAINT 1 CA 968 CAE832104 (CAN) PILOT NOTICED A VIBRATION, MAINTENANCE FOUND TEETH MISSING OFF THE BELT. 1 G 7 1 3U 3 U H3WE E4CE 1997062600500 19970626 00500 SW 1997 6 26 CA970311036 1 19960626 A 2844 7G547 SWITCH BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL FUEL PRESS NO INDICATION W K NONE P NO WARNING INDICATION IN INSP/MAINT 1 CA CAE823527 (CAN) NO PRESSURE OFF INDICATION. 1 G 7 1 3U 3 U H2SW E4CE 1997062600502 19970626 00502 SW 1997 6 26 CA970311038 1 19960730 A 6322 206040301105 BLOWER ASSEMBLY BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL FAN SHAFT LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA CAE833189 (CAN) PRIOR TO INSTALLATION A VISUAL INSPECTION REVEALED THAT THE FAN TO SHAFT ATTACHING HARDWARE WAS LOOSE. 1 G 7 1 3U 3 U H2SW E4CE 1997062600503 19970626 00503 SW 1997 6 26 CA970311039 1 19960613 A 5320 206031200005 WEB BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL BOX BEAM CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 16160 CAE820180B (CAN) LOWER WEB ON CABIN ROOF BOX BEAM CRACKED. 1 G 7 1 3U 3 U H2SW E4CE 1997062600505 19970626 00505 EU 1997 6 26 CA970311041 1 19960810 A 6220 350A31190703 STARFLEX SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE M/R CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 625 879 (CAN) 20 MM CRACK IN STARFLEX. 1 G 7 1 3U 3 U NC H9EU E19EU 1997062600507 19970626 00507 EU 1997 6 26 CA970311043 1 19960815 A 2910 704A33690004 BELT SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE HYDRAULIC PUMP BROKEN W A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 CA 23 258 (CAN) BELT BROKE IN FLIGHT CAUSING LOSS OF HYDRAULIC POWER. BELT HAD OVERHEATED AND FAILED. HYDRAULIC PUMP AND ROTOR BRA KE SHIMMING WERE WITHIN LIMITS. 1 G 7 1 3U 3 U H9EU E19EU 1997062600508 19970626 00508 SW 1997 6 26 CA970311044 1 19960812 A 2560 MS2450915 CIRCUIT BREAKER BELL 206 206L 1181522 SW ALLSN 250C 250C20B 03013 GL AUX POWER PANEL CHAFED W K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA 830805 (CAN) PILOT REPORTED SMOKE FROM AUXILIARY POWER/WATER BUCKET CIRCUIT BREAKER. CHAFED WIRE FOUND BEHIND DART PANEL. 1 G 7 1 3U 3 U H2SW E4CE 1997062600509 19970626 00509 WP 1997 6 26 CA970311046 1 19960829 A 6322 369D25623 BELT HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL OIL COOLER FAN DAMAGED W K NONE E VIBRATION/BUFFET CR CRUISE 1 CA 410 CAE830901 (CAN) PILOT HEARD GROWLING NOISE. INSEPCTION FOUND SEVERAL TEETH MISSING AND BELT CLOSE TO FAILURE. 1 G 7 1 3U 3 U H3WE E4CE 1997062600510 19970626 00510 EU 1997 6 26 CA970311047 1 19960831 A 6230 350A37000402 MAST ASSEMBLY SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE INTERNAL LINES LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 319 4522 (CAN) HYDRAULIC FLUID LEAKING INTO TRANSMISSION. INTERNAL HYDRAULIC LINES PRESSURE TESTED AND BOTH PRESSURE AND RETURN L INES LEAKING AT CENTRE 'T' FITTING. 1 G 7 1 3U 3 U NC H9EU E19EU 1997062600511 19970626 00511 EU 1997 6 26 CA970311048 1 19960907 A 6300 350A34021004 DRIVESHAFT SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE UNDER COLLAR WORN W K NONE O OTHER IN INSP/MAINT 1 CA 6343 835 (CAN) DURING 5 YEAR BEARING CHANGE WEAR WAS FOUND UNDER COLLAR OF #2 BEARING. 1 G 7 1 3U 3 U H9EU E19EU 1997062600512 19970626 00512 SW 1997 6 26 CA970311049 1 19960916 A 6230 206010450113 SWASHPLATE ASSY BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL SE11 LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 12181 2591 CAE820743 (CAN) SWASHPLATE SPEWING EXCESSIVE AMOUNT OF GREASE. PREVIOUSLY REMOVED FOR SAME REASON. 99.5 HOURS THIS INSTALLATION. 1 G 7 1 3U 3 U H2SW E4CE 1997070300139 19970703 00139 CE 1997 7 3 97ZZZX2942 1 19960706 A 6120 8972623 PIN 869130121 BEECH 18 E18S 1151006 CE PROP PITCH CONT SHEARED A STZA O OTHER F FLT CONT AFFECTED LD LANDING 1 AL 03 700WA 2184 P142707 BA28 PIN THAT FITS IN CAM ASSEMBLY P/N 86558 SHEARED PREVENTING RT ENGINE FROM GOING INTO REVERSE CAUSING PROPELLER TO GO FUL L PITCH FORWARD. AIRCRAFT VEERED TO THE LEFT ON LANDING, DEPARTED THE RUNWAY CAUSING SUBSTANTIAL DAMAGE. 1 L 7 2 3R A765 1997070300227 19970703 00227 GL 1997 7 3 CA970311050 2 19960926 A 7323 23007506 GOVERNOR HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL ENGINE LOW POWER W K NONE O OTHER IN INSP/MAINT 1 CA 829 CAE830896 (CAN) GOVERNOR WOULD NOT PRODUCE MORE THAN 102 PERCENT WHEN RIGGED TO MAXIMUM. 1 G 7 1 3U 3 U H3WE E4CE 1997070300228 19970703 00228 EU 1997 7 3 CA970311052 1 19961010 A 5532 350A1400200802 VERTICAL FIN SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE TRAILING EDGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 258 (CAN) CRACK IN RIGHT HAND TRAILING EDGE SKIN AND FORWARD UPPER CASTING MOUNT. EXCESSIVE GAP (3MM) WHEN ATTACHED. BOLT HO LES IN CASTING MOUNT ELONGATED. 1 G 7 1 3U 3 U H9EU E19EU 1997070300229 19970703 00229 1997 7 3 CA970311053 4 19961011 A 3422 103002201 GYRO SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE COCKPIT DG BROKEN W K NONE I FLT. ATTITUDE INST. CR CRUISE 1 CA 258 (CAN) ADJUSTMENT KNOB DOES NOT FUNCTION. 1 G 7 1 3U 3 U H9EU E19EU 1997070300230 19970703 00230 EA 1997 7 3 CA970311054 1 19961219 A 7921 00400479P101 OIL COOLER CARSON S61 S61LSKRSKY EA GE CT58 CT581401 30011 NE ENG OIL LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 280350 (CAN) LEAKING FUEL FROM UPPER AFT CENTRE WELD SEAM. 2 G 7 2 4U 4 U H8EA 1E3 1997070300231 19970703 00231 SW 1997 7 3 CA970311055 1 19961014 A 3213 206321003 SKID TUBE BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL BOTTOM FWD PUNCTURED W K NONE O OTHER IN INSP/MAINT 1 CA CAE801518BA (CAN) PUNCTURE OF BOTTOM OF SKID TUBE, FORWARD OF SADDLE. 1 G 7 1 3U 3 U H2SW E4CE 1997070300232 19970703 00232 1997 7 3 CA970311056 4 19961015 A 2312 064101900 TRANSCEIVER SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE COCKPIT NO MEMORY W K NONE O OTHER IN INSP/MAINT 1 CA 76 258 (CAN) WILL NOT HOLD MEMORY ON EITHER SIDE WHEN RADIO IS TURNED OFF. 1 G 7 1 3U 3 U H9EU E19EU 1997070300233 19970703 00233 EU 1997 7 3 CA970311057 1 19961018 A 2432 1656 BATTERY SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE DC SYS FAILED W O OTHER H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 CA 3248 527 834 (CAN) UNABLE TO START AIRCRAFT AFTER RETURNING FROM 2 TRIPS. 1 G 7 1 3U 3 U H9EU E19EU 1997070300234 19970703 00234 SW 1997 7 3 CA970311058 1 19961008 A 7714 206062627003 TACH GENERATOR BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENG N1 SURGING W A UNSCHED LANDING J WARNING INDICATION HO HOVERING 1 CA 2276 CAE801475BA (CAN) ENGINE RPM INDICATOR SURGING 10-15 PERCENT. N1 TACH GENERATOR REMOVED, FOUND WIRE CHAFED (TO GROUND) UNDER ELECTRI CAL CONNECTOR CAP. 1 G 7 1 3U 3 U H2SW E4CE 1997070300235 19970703 00235 WP 1997 7 3 CA970311059 1 19961104 A 6322 369D25630 BLOWER HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL OIL COOLER BEARING FAILURE W B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA 265 CAE830896 (CAN) LOUD BANG AND HEAVY VIBRATION. LIGHT SMOKE IN COCKPIT. SUSPECT BEARING FAILURE OF OIL COOLER BLOWER. 1 G 7 1 3U 3 U H3WE E4CE 1997070300236 19970703 00236 SW 1997 7 3 CA970311060 1 19961104 A 6320 MS21042L6 NUT BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL R/H PYLON CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA CAE820733 (CAN) UPON TRANSMISSON REPLACEMENT, R/H PYLON SUPPORT PAD NUT WAS FOUND CRACKED. L/H PYLON SUPPORT WAS WORN AND POSSIBLE CAUSE OF CRACKING DUE TO POUNDING. 1 G 7 1 3U 3 U H2SW E4CE 1997070300237 19970703 00237 SW 1997 7 3 CA970311061 1 19961121 A 5320 206031322003 STIFFENER BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL DRAIN LINE CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA CAE800471BA (CAN) STIFFENER HAD EXCESSIVE CHAFING DAMAGE CAUSED BY ENGINE OIL TANK DRAIN LINE. 1 G 7 1 3U 3 U H2SW E4CE 1997070300651 19970703 00651 NE 1997 7 3 97ZZZX2962 2 19961122 A 7230 400100012 BEARING BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE NR 2 FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 532KH 7069 LE45068 NR 2 BEARING FAILURE. DURING START, NR 2 ENGINE FAILED. NR 1 ENGINE WAS AT GROUND IDLE. FAILURE OCCURRED AT 40 PERCEN T N1 DURING START-UP. ALL PARAMETERS WERE NORMAL AND WITHIN LIMITS. THERE WAS A SUDDEN LOUD NOISE FOLLOWED BY SMOKE FR OM THE TAILPIPE AND THEN CHIP LIGHT. PILOT SHUT DOWN THE ENGINE IMMEDIATELY PRIOR TO REACHING GROUND IDLE. UPON ENGINE REMOVAL, FOUND SEVERE N1 RUB. TOTAL CYCLES, 14,082.4. 1 G 7 2 3U 3 U H13EU E5NE 1997070300652 19970703 00652 NE 1997 7 3 97ZZZX2963 2 19961228 A 7230 430151101 BEARING 400100025 BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE NR 2 FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 7060G 3160 43556 7173 LE45807EF BEARING FAILURE. WHILE INCREASING POWER TO FLIGHT IDLE, PILOT REPORTED A LOUD BANG AND ORANGE FLASH FROM THE NR 1 ENGIN E. ENIGINE WAS BETWEEN 80 TO 85 PERCENT WHEN BANG WAS HEARD. NR 2 BEARING PN 4-301-511-01, SN 4-3556, INSTALLED 9-15-9 6, TT 85.0 HOURS. PART TOTAL CYCLES, 3,159.4. 1 G 7 2 3U 3 U H13EU E5NE10 1997070300738 19970703 00738 WP 1997 7 3 ABXA9701183 1 19961112 A 5753 5912168502 SKIN DOUG DC9 DC941 302207N WP RT TE FLAP VANE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 960 47762 DURING C-CHECK, FOUND RIGHT FLAP VANE SLIDE ARM BRACKET CRACKED, OUTBOARD END RIB CORRODED AND SKIN DENTED. REPLACED SK IN, HONEYCOMB CORE AND INTERNAL DOUBLERS IAW DC9 SRM. 2 L 7 2 4F A6WE 1997071700408 19970717 00408 SW 1997 7 17 CA970421070 1 19961013 A 2435 03601018 BEARING LEARSIEGLER 23079001 SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP GENERATOR FAILED W O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 CA 445 445 6049 P44121C (CAN) AIRCRAFT HAD INTERMITTENT GENERATOR IN FLIGHT. GENERATOR REPLACED DUE TO BAD BEARINGS. 2 L 7 2 4T 4 T RT A8SW E4WE 1997071700428 19970717 00428 CE 1997 7 17 CA970421093 1 19960619 A 2750 50000084 CONTROL CABLE CESSNA 401 401A 207590D CE MCAULY 3AF32C 3AF32C87 GL FLAP EXTEND SEPARATED W K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 CA 8456 2997 760771 (CAN) THE AREA WHERE THIS FAILURE OCCURRED IS LOCATED BEHIND A PULLEY AND IS NOT EASILY INSPECTED WITHOUT THE USE OF A M IRROR LOOKING INBOARD. SOME WEAR AND FRAYING WAS ALSO NOTICED JUST OUTBOARD OF THE PULLEY. THERE WAS SOME CORROSION ON T HE CABLE BUT NOT IN THE AREA OF THE FAILURE. THE PULLEYS WERE NOT SEIZED AND THE CABLE WAS NOT RUBBING ON ANYTHING. THE TENSION WAS CHECKED 114 HOURS PREVIOUSLY. 1 L 7 2 3O A7CE 5 C P22EA 1997072200006 19970722 00006 NM 1997 7 22 DL72S971363 1 19960816 A 5754 SKIN 6516221100 BOEING 727 727232 1384082 NM NR 5 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 408DA BN907 21152 SKIN CRACKED AT FAIRING NUMBER 5 SLAT. 2 L 7 3 4F A3WE 1997072400469 19970724 00469 NM 1997 7 24 GAIA9737 1 19960627 A 3244 TIRES BOEING 727 727223 1384074 NM LT MLG FAILED A GAIA O OTHER O OTHER LD LANDING 1 SW 07 6827 20180 ON LANDING AT WSSS (SINGAPORE) BOTH LEFT MLG TIRES WENT FLAT AND SHREDDED CAUSING DAMAGE TO LEFT INBOARD FLAP, INBOARD S POILER AND BRAKE LINES. LOG PAGE AND DAMAGE REPORT HAV NOT YET BEEN TO DFW. (M) 2 L 7 3 4F A3WE 1997073100041 19970731 00041 NM 1997 7 31 97ZZZX3330 1 19960222 A 2434 ALU8403 ALTERNATOR PIPER PA60 PA60600 7106001 NM LT ENGINE BEARING FAILED A ESMA K NONE O OTHER IN INSP/MAINT 1 SO 11 699RF 20 TF00073 600169074 AFTER ONLY 20 HOURS OF TIME, ALTERNATOR BEARING FOUND FAILED WITH BELT TENSION OK. ALTERNATOR ALSO HAS HIGH RESISTANCE. UNIT OVERHAULED BY PRECISION ELECTRONICS, INC. 1 M 7 2 3O RT A17WE 1997081400298 19970814 00298 EU 1997 8 14 CA970609032 1 19960601 A 3230 COVER BRAERO 748 HS7482B 1500248 EU LT MLG DAMAGED W O OTHER O OTHER CR CRUISE 1 CA (CAN) DURING TRAINING FLIGHT THE GEAR WAS SELECTED DOWN IN THE EMERGENCY MODE. THE LH GEAR WOULD NOT LOCK DOWN WITH HAND PUMP PRESSURE BUT WOULD LOCK DOWN WITH NORMAL SYSTEM PRESSURE. AIRCRAFT LANDED WITH 3 GREEN. THE UPPER SEAR COVER WAS F OUND BENT UPWARDS INTERFERING WITH THE DOWN LOCK HOOK, LIKELY FROM GRAVEL FOD. COVER REPAIRED GEAR SWUNG NORMAL. 2 L 7 2 3T A24EU 1997082100013 19970821 00013 WP 1997 8 21 VTZA97352 2 19960928 A 7397 WIRE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE3311 01514 WP RT ENGINE CHAFED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 301UE 41012 IAD/DAY - FLT 6292 - DURING CRUISE AT 1300 HOURS ON 6-28-97, EXPERIENCED A RT IEC FAULT INDICATOR SYSTEM WARNING THAT WO ULD NOT RESET. AIRCRAFT RETURNED TO IAD AND THE GATE WHERE MAINTENANCE TROUBLESHOT THE DISCREPANCY AND FOUND A CHAFED W IRE AT THE T2 SENSOR CANNON PLUG. THE WIRE WAS REPAIRED AND REPOSITIONED IN THE T2 CANNON PLUG AND THE SYSTEM WAS TESTE D IAW MAINTENANCE PROCEDURES. THE AIRCRAFT WAS THEN RELEASED AND RETURNED TO SERVICE. (X) 2 L 7 2 4T 3 T RT A41NM E3WE 1997092500254 19970925 00254 NE 1997 9 25 97ZZZX4138 2 19961229 A 7250 MODULE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE M02-M03 COKING A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 92LG 2177 194 2575 9198 AFTER NORMAL SHUT DOWN OF ENGINE, THEN NORMAL START OF ENGINE, HEARD GRINDING NOISE IN ENGINE 15-20 PERCENT NG; AT ABOUT 25 PERCENT NG, ENGINE SLOWED WITH NORMAL BATTERY VOLTAGE. START ABORTED. FOUND BY MANUAL TURNING OF GAS GENERATOR AND AT HOT TEMP OF ENGINE, GRINDING HEARD, DIFFICULT TO ROTATE IN OPPOSITE DIRECTION AND SOME SOUNDS OF METAL CONTACT, BUT WHEN ENGINE TEMP COOLED, MANUAL ROTATION GOOD. 1 G 7 1 3U 3 U H9EU E19EU 1997092500274 19970925 00274 CE 1997 9 25 97ZZZX4155 1 19961015 A 2701 MS200044 BOLT CESSNA 500 S550 2076607 CE CONTROL COLUMN LOOSE A DXTA K NONE O OTHER IN INSP/MAINT 1 GL 07 106QS S5500106 BOTH PILOT'S AND COPILOT'S CONTROL COLUMN ASSY HAD EXCESSIVE PLAY. WHEN PRESSURE WAS APPLIED TO OPPOSITE COLUMN, FORWAR D AND AFT OR INBOARD AND OUTBOARD, FOUND BOLTS HAD EXCESSIVE PLAY AND CLICKING NOISE WAS HEARD. (NO PUTTY WAS ON ANY BO LTS). TOTAL AIRCRAFT HOURS, 9,615.4. 1 L 7 2 4F RT A22CE 1997100800002 19971008 00002 WP 1997 10 8 TWAA9700102 1 19961231 A 2130 DUCT BOOT DOUG DC9 DC982 3022082 WP LT ACM LEAKING A TWAA O OTHER J WARNING INDICATION CR CRUISE 1 CE 05 915TW 49186 MCI - FLT 173 - DURING CRUISE, CABIN PRESSURE COULD NOT BE MAINTAINED. REPOSITIONED AND RETORQUED LEFT AIR CYCLE MACHIN E DUCT BOOT. LEAK CHECK AND OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F A6WE 1997100800003 19971008 00003 1997 10 8 TWAA9700101 4 19961227 A 2565 SLIDE DOUG DC9 DC982 3022082 WP TAIL CONE FAILED A TWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 05 9420D 49824 ATL - FLT 641 - AS A RESULT OF AN INADVERTENT TAIL CONE DROP, THE TAIL CONE ESCAPE SLIDE DEPLOYED, BUT FAILED TO INFLATE . THE SLIDE AUTO INFLATE LANYARD WAS IMPROPERLY INSTALLED. REMOVED AND REPLACED TAIL CONE ESCAPE SLIDE. CHECK C - 1-1 -97 - MZJ. (X) 2 L 7 2 4F A6WE 1997101600749 19971016 00749 NM 1997 10 16 CA970922005 1 19961119 A 5210 82510094109 HINGE 82510294021 DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE DOOR WORN W K NONE O OTHER IN INSP/MAINT 1 CA 123052 (CAN) REFERENCE AD CF-96-20R2 AND SB 8-52-39. STRIKER DOES NOT FIT CORRECTLY. SEE SDRS 970922006 AND 970922007. 2 H 7 2 4T 4 T RT A13NM E20NE 1997101600750 19971016 00750 NM 1997 10 16 CA970922006 1 19961115 A 5210 82510094109 HINGE HALF 82510294021 DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE DOOR WORN W K NONE O OTHER IN INSP/MAINT 1 CA 123061 (CAN) REFERENCE AD CF-96-20R2, AND MOD 8/2337, WHILE ATTEMPTING TO INSTALL MOD. THE SUPPLIED STRIKER ASSEMBLY COULD NOT BE INSTALLED AS PER INSTRUCTIONS BECAUSE ITS NARROWER THAN THE COCKPIT DOOR FRAME BY ABOUT 1/8". SUBMITTER SUGGESTS THAT STRIKER COULD BE INSTALLED IF IT WAS FLATTENED ON THE CURVED END. THIS IS RE-OCCURRING PROBLEM FOR THIS OPERATOR FLEET. SB 8-5-39 IS RELEVANT, AND OPERATOR IS IN CONTACT WITH DE HAVILLAND TO GET FIX. 2 H 7 2 4T 4 T RT A13NM E20NE 1997102300531 19971023 00531 SO 1997 10 23 COMA9710433 1 19961020 A 3350 3071BPE LAMP EMB 120 EMB120RT SO CABIN FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 263CA 120255 THE AFT LAMP OF THE CABIN FLOOR PATH EMERGENCY LIGHTING IS INOP. REPLACED LAMP. 2 L 7 2 4T RT A31SO 1997112600575 19971126 00575 WP 1997 11 26 97ZZZM1121 1 19961006 A 5330 SKIN DOUG DC6 DC6A 3021706 WP BS 500 CRACKED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 874TA 36234 44641 POPPED RIVETS AND SKIN CRACKED AT SKIN LAP 1 O'CLOCK POSITION. CUTOUT CORRODED SKIN AND REPAIRED PER SRM 4-31. (M) 2 L 7 4 4R 6A3 1997112600577 19971126 00577 WP 1997 11 26 97ZZZM1123 1 19961006 A 5330 SKIN DOUG DC6 DC6A 3021706 WP BS 412 DAMAGED A TALA K NONE O OTHER IN INSP/MAINT 1 SO 19 874TA 36234 44641 RIVET POPPED IN LAP SEAM AT 11 O'CLOCK POSITION. CUTOUT DAMAGED SKIN AND REPAIRED PER SRM FIG 4-31. REPLACED POPPED RI VETS. 2 L 7 4 4R 6A3 1997121800385 19971218 00385 CE 1997 12 18 CA960725104 1 19960711 A 3230 1153800023 MOTOR 1153800023 BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA LANDING GEAR INTERMITTENT W K NONE O OTHER AP APPROACH 1 CA 357 1174 PCE52376 (CAN) LANDING GEAR MOTOR INTERMITTENT WHEN SELECTED DOWN. BRUSHES FOUND IMPROPERLY INSTALLED. 1 L 7 2 3T 4 T A14CE E4EA 1997121800388 19971218 00388 CE 1997 12 18 CA960729012 1 19960722 A 3220 SK15011 NOSE FORK CESSNA 0442504201 CESSNA 150 152 2071835 CE NLG RH SIDE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 8406 (CAN) NOSE GEAR FORK FOUND CRACKED ON THE RIGHT HAND SIDE. CRACK APPROXIMATELY ONE INCH FRONT TO BACK 1 H 7 1 3O NT 3A19 1997121800390 19971218 00390 1997 12 18 CA960802006 4 19960716 A 2562 BATTERY EBC EBC102A DIAMON DA20A1 DA20A1 05626UX GL ELT EXPIRED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ELT WAS SIGNED OFF AS BEING TESTED ON 8 DECEMBER 1995. INSPECTION OF THE BATTERY INDICATED DUE DATE CHANGE OF JULY 1996. LESS THAN 7 MONTHS FROM SIGN OFF. ALSO THERE WERE NO INDICATION ON OUTSIDE OF THE ELT DRAWING ATTENTION TO DUE DA TE. 1 L 7 1 3O NT TA4CH 1997121800392 19971218 00392 NM 1997 12 18 CA960802201 1 19960708 A 5530 35250501 TAIL STRUT CHRIS HUSKY A1 221020X NM THREADS BROKEN W A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 CA (CAN) PILOT NOTICED VIBRATION FROM THE TAIL SECTION AND LANDED WITHOUT INCIDENT. INVESTIGATION FOUND A BROKEN STRUT WIRE AND REPLACED IT. THE FLYING WIRE BROKE AT THE THREADS APPROXIMATELY 1.250 INCHES FROM THE END. 1 H 7 1 3O NC A22NM 1997121800393 19971218 00393 EA 1997 12 18 CA960802202 2 19960712 A 7261 MS9388222 O-RING BEECH 100 100BEECH 1152916 CE PWA PT6 PT6A28 EA OIL CAP TORN W E A ENGINE SHUTDOWN UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CL CLIMB 1 CA P50739 (CAN) CREW NOTICED OIL PRESSURE FLUCTUATING. ENGINE SHUTDOWN AND SINGLE ENGINE LANDING ACCOMPLISHED. MAINTENANCE FOUND O IL DIPSTICK O-RING HAD BEEN PINCHED AND OIL WAS BLOWN OVERBOARD. 1 L 7 2 3T 4 T A14CE E4EA 1997121800394 19971218 00394 CE 1997 12 18 CA960807006 1 19960728 A 3240 215286E BRAKE STATOR BF GOODRICH 215286E CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE LT BRAKE FRACTURED W O OTHER O OTHER TX TAXI/GRND HDL 1 CA 619 1164 PCE70280 (CAN) LEFT HAND BRAKE STATOR LOCATED NEAREST THE PRESSURE PLATE FRACTURED IN MULTIPLE LOCATIONS AT THE RELIEF SLOTS/KEYW AYS. THE BROKEN SEGMENT OF THE ROTOR DROPPED DOWN AND JAMMED THE WHEEL. 1 L 7 2 4F 4 F A22CE E1NE 1997121800396 19971218 00396 CE 1997 12 18 CA960807009 1 19960726 A 3230 12810181 CAP ACTUATOR CESSNA 182 R182 2072734 CE MCAULY 2D34C B2D34C214 GL LG PIVOT POINT LOOSE BOLTS W O OTHER K FLUID LOSS LD LANDING 1 CA 3581 778345 (CAN) PILOT EXPERIENCED DIFFICULTIES IN MOVING LANDING GEAR SELECTOR DOWN. INVESTIGAITON FOUND THREE OF THE 4 BOLTS LOOS E ON THE RETAINING CAP. 1 H 7 1 3O RT 3A13 5 C P7EA 1997121800397 19971218 00397 CE 1997 12 18 CA960808001 1 19960705 A 2750 995240253 MOTOR ASSY BEECH 100 100BEECH 1152916 CE PWA PT6 PT6A28 EA FLAPS INOPERATIVE W K NONE O OTHER TX TAXI/GRND HDL 1 CA PCE50324 (CAN) FLAPS FAILED TO RETRACT AFTER LANDING. INVESTIGATION FOUND FLAP MOTOR TO BE INOPERATIVE. 1 L 7 2 3T 4 T A14CE E4EA 1997121800398 19971218 00398 SO 1997 12 18 CA960808002 1 19960711 A 5346 LW18759 BRACKET PIPER PA31 PA31350 7103110 SO ENG ATTACHMENT BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING INSPECITON, BRACKET WAS FOUND BROKEN AT ENGINE ATTACHMENT POINT. 1 L 7 2 3O A20SO 1997121800399 19971218 00399 SO 1997 12 18 CA960808003 1 19960714 A 7120 LW18759 BRACKET PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA ENGINE ATTACHMNT BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA L775961A (CAN) DURING INSPECTION THE BRACKET WAS FOUND BROKEN AT THE ENGINE ATTACHMENT POINTS. 1 L 7 2 3O 3 O A20SO E14EA 1997122400013 19971224 00013 SO 1997 12 24 97ZZZX5201 1 19961231 A 2740 071199602 CONTROL CABLE PIPER PA34 PA34200T 7103406 SO STAB TRIM BS 187 FAILED A L A DXYA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 07 8107X 348070012 DURING NORMAL OPERATIONS, PILOT REPORTED STABILATOR TRIM BECAME INOPERATIVE DURING APPROACH TO LANDING AT HOME BASE. NO TRIM LANDING UNEVENTFUL. ON INVESTIGATION, FOUND STABILATOR TRIM CABLE SEVERELY FRAYED AND JUMPED OF THE PULLEYS OF TH E AUTOPILOT AND ELECTRIC TRIM SERVOS LOCATED JUST AFT OF FS 187.84. THIS RESULTED IN COMPLETE LOSS OF TRIM ACTUATION (M ANUAL AND ELECTRIC). AIRCRAFT HAD UNDERGONE ANNUAL 100-HOUR INSPECTION 49 HOURS PREVIOUSLY WITH NO SIGNS OF PROBLEMS. S UBMITTER STATED PROBLEM HAS OCCURRED ON OTHER, SAME TYPE AIRCRAFT IN THE PAST. 1 L 7 2 3O A7SO 1997122400132 19971224 00132 EU 1997 12 24 HAIHQEA0014 1 19961024 A 3340 J132831 MOUNT A20641683 AGUSTA A109 A109C 0260118 EU LIGHT BROKEN E HQEA K NONE O OTHER IN INSP/MAINT 1 NE 05 142HC 163 NA 7677 LIGHT MOUNT IS BROKEN. FOUND THE SHOCK MOUNT TORN. INSTALLED SHOCK MOUNT. 1 G 7 2 3U H7EU 1998020500438 19980205 00438 CE 1998 2 5 CA961016005 1 19961009 A 2612 1005700291 SHIELD BEECH 100 100BEECH 1152916 CE PWA PT6 PT6A28 EA LEFT ENGINE BENT W E ENGINE SHUTDOWN N FALSE WARNING AP APPROACH 1 CA PCE50045 (CAN) ON APPROACH LEFT ENGINE WAS SHUT DOWN BECAUSE OF AN INTERMITTENT FIRE WARNING INDICATION. INSPECTION FOUND THE OUT BOARD LIGHT SHIELD WAS BENT 1 L 7 2 3T 4 T A14CE E4EA 1998020500439 19980205 00439 CE 1998 2 5 CA961016007 1 19960918 A 7810 1019500223 EXHAUST STACK BEECH 200 B200 1152922 CE PWA PT6 PT6A42 52043 NE RH OUTBOARD CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 4025 PCE94624 (CAN) EXHAUST STACK FOUND CRACKED ALONG THE OUTBOARD WELD SEAM, APPROXIMATELY 5, 1/4" LONG. THIS STACK HAD BEEN REPLACED IN MAY 1995. 1 L 7 2 4T 4 T A24CE E4EA 1998020500444 19980205 00444 SO 1998 2 5 CA961018027 1 19961009 A 3213 4028800 TRUNNION BRACKET PIPER 4550403 PIPER PA31 PA31350 7103110 SO RT MLG BENT W K NONE O OTHER IN INSP/MAINT 1 CA 13595 (CAN) WHILE REBUSHING RIGHT MAIN LANDING GEAR, THE AFT TRUNNION ASSEMBLY BRACKET WAS FOUND BENT. GEAR COULD NOT BE INSTA LLED PROPERLY. THIS POSSIBLY DUE TO A HARD LANDING. 1 L 7 2 3O A20SO 1998020500447 19980205 00447 CE 1998 2 5 CA961025008 1 19961021 A 2612 CONNECTOR BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA RT ENG FIRE DET DIRTY W E ENGINE SHUTDOWN N FALSE WARNING AP APPROACH 1 CA 50587 (CAN) RIGHT ENGINE FIRE LIGHT CAME ON. PILOT SHUT ENGINE DOWN AND LANDED WITHOUT INCIDENT. BAD CONNECTION AT AMPLIFIER. 1 L 7 2 3T 4 T A14CE E4EA 1998020500448 19980205 00448 CE 1998 2 5 CA961025009 1 19961021 A 2612 302158 SENSOR BEECH 99 B99 1154004 CE PWA PT6 PT6A28 EA FIRE DET CONTAMINATED W C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CA 40209 (CAN) FIRE LIGHT ON, AT TAKEOFF. PILOT RETURNED TO BLOCKS. FOUND A FIRE DETECTOR WET. 1 L 7 2 3T 4 T A14CE E4EA 1998020500449 19980205 00449 CE 1998 2 5 CA961025012 1 19961012 A 3213 508103237 TORQUE KNEE 115810000619 BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA STRUT ATTACH CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA PCE50099 (CAN) BOLT P/N 99-810061-3 FOUND LOOSE AT THE TORQUE KNEE UNION. WHEN DISASSEMBLED TO ADD WASHERS FOR SHIMMING, THE LOWE R KNEE WAS FOUND CRACKED AT THE INSIDE RADIUS OF KNUCKLE. LPI CONFIRMED CRACK. BUSHING AT STRUT ATTACH POINT WAS WORN, P OSSIBLY RESULTING IN EXCESSIVE TORQUE KNEE TWISTING, RESULTING IN FAILURE. 1 L 7 2 3T 4 T A14CE E4EA 1998020500450 19980205 00450 CE 1998 2 5 CA961029008 1 19961021 A 3610 19357222 O-RING BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE WS 0.00 BROKEN W K NONE J WARNING INDICATION NR NOT REPORTED 1 CA PCE114452 (CAN) PILOT REPORTED THAT THE RIGHT BLEED AIR FAIL WARNING LIGHT CAME ON. INSPECTION FOUND THE OUTBOARD 'O' RING AT THE JUNCTION OF THE BLEED AIR DUCT AT WS 0.00 APPROXIMATELY WAS DRY AND BROKEN, AND CAUSED A BLEED AIR LEAK. 2 L 7 2 4T 4 T RT A24CE E26NE 1998020500452 19980205 00452 SO 1998 2 5 CA961105004 1 19961030 A 3242 1592 DISCS CLEVELAND 3013 PIPER PA23 PA23160 7102304 SO LYC O360 O360A1A 41514 EA BRAKE DEFECTIVE W K NONE W INADEQUATE Q C TX TAXI/GRND HDL 1 CA L1234936A (CAN) AFTER DISC REPLACEMENT, AND WHILE TAXIING A PULSATING WAS FELT IN THE RUDDER PEDALS. BRAKE DISC THICKNESS MEASURED AND FOUND TO HAVE .006 TO .007 INCH DIFFERENCE FROM ONE SIDE TO THE OTHER. DISCS REPLACED AGAIN. 1 L 7 2 3O 3 O 1A10 E286 1998020500453 19980205 00453 CE 1998 2 5 CA961105005 1 19961018 A 5343 22430094 FITTING CESSNA 182 R182 2072734 CE MCAULY 2D34C B2D34C214 GL NOSE GEAR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 3584 880728 (CAN) WHEN RETRACTION TEST PERFORMED, INSPECTION OF THE NOSE GEAR ATTACH FITTING FOUND 2 CRACKS ON EACH SIDE OF THE ACTU ATOR ATTACHMENT. SUBMITTER SUSPECTS A HARD LANDING. 1 H 7 1 3O RT 3A13 5 C P7EA 1998020500454 19980205 00454 CE 1998 2 5 CA961112028 1 19961031 A 5720 853520051 LATCH RECEIVER 851007 BEECH 100 A100 1152915 CE PWA PT6 PT6A34 52043 EA RIGHT HAND WING BENT W O OTHER E VIBRATION/BUFFET CR CRUISE 1 CA 2090 0 (CAN) AT 11,000 FEET, PILOT NOTICED A LARGE VIBRATION AND A PITCH DOWN ATTITUDE. CREW DETERMINED THAT THE RIGHT WING LOC KER WAS OPENED. EMERGENCY DECLARED AND AIRCRAFT LANDED OK. BOTH LATCH RECEIVER ASSEMBLIES WERE BENT NOT ALLOWING THE LAT CH ASSEMBLY PIN TO ENGAGE. NO CAUSE DETERMINED FOR BENT LATCH RECEIVERS. 1 L 7 2 3T 4 T A14CE E4EA 1998020500455 19980205 00455 CE 1998 2 5 CA961112029 1 19961017 A 5511 RIB ASSEMBLY 043200159 CESSNA 150 150M 2071830 CE CONT O200 O200A 17020 SO HORIZ STAB LE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 9689 1993769A (CAN) HORIZONTAL STABILIZER RIB ASSEMBLY ON THE LEADING EDGE FOUND CRACKED AT THE BEND RADIUS. 1 H 7 1 3O 3 O 3A19 E252 1998020500456 19980205 00456 NE 1998 2 5 CA961112030 2 19961018 A 7530 O-RING BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE EVA TUBE BS 29 MISSING W K NONE J W WARNING INDICATION INADEQUATE Q C NR NOT REPORTED 1 CA 757 114476 (CAN) PILOT REPORTED THE RIGHT BLEED AIR FAIL ANNUNCIATOR LIGHT WAS ON. INVESTIGATION FOUND A HOLE IN THE EVA TUBE. THE HOLE WAS CAUSED BY A LEAK AT THE BLEED AIR JUNCTION AT STA. 29.06. TWO 'O' RINGS P/N 19357-222 WERE NOTED AS MISSING. IT IS LIKELY THAT THE MANUFACTURER FORGOT TO INSTALL THEM. 2 L 7 2 4T 4 T RT A24CE E26NE 1998020500457 19980205 00457 CE 1998 2 5 CA961112046 1 19961028 A 3260 1SE13 SWITCH CESSNA 402 402CESSNA 207590K CE MCAULY 3AF32C 3AF32C87 GL RT GEAR FAILED W O OTHER P NO WARNING INDICATION AP APPROACH 1 CA 6329 7910240 (CAN) ON APPROACH RIGHT HAND GEAR DOWN AND LOCK DID NOT COME ON. AIRCRAFT LANDED OK. FOUND THE RIGHT HAND DOWN AND LOCK MICRO SWITCH HAD FAILED. 1 L 7 2 3O A7CE 5 C P22EA 1998020500458 19980205 00458 CE 1998 2 5 CA961113002 1 19961105 A 3297 WIRE MTSBSI MU2 MU2B35 5780411 CE GARRTT TPE331 TPE3316 01514 WP NLG SWITCH BROKEN W L ABORTED APPROACH P N NO WARNING INDICATION FALSE WARNING AP APPROACH 1 CA P27223C (CAN) ON APPROACH WHEN GEAR SELECTED DOWN, DID NOT GET A GREEN LIGHT ON THE NOSE GEAR. GEAR CYCLED WITH NO CHANGE. EMERG ENCY EXTENSION USED. INVESTIGATION REVEALED A BROKEN WIRE AT THE SWITCH. 1 H 7 2 3T 4 T RT A10SW E4WE 1998020500459 19980205 00459 GL 1998 2 5 CA961115009 1 19961106 A 2752 COLLAR 202750000 DIAMON DA20A1 DA20A1 05626UX GL FLAP ACTUATOR OUT OF POSITION W K NONE O OTHER IN INSP/MAINT 1 CA 1313 (CAN) THE PLASTIC COLLAR ON THE FLAP ACTUATOR HAD VIBRATED OUT OF POSITION AND MOVED ALONG THE ACTUATOR SHAFT. IT IS POS SIBLE FOR THIS TO JAM THE FLAP. 1 L 7 1 3O NT TA4CH 1998020500461 19980205 00461 NM 1998 2 5 CA961120041 1 19961122 A 5530 CR32425 FASTENERS 220000001 PIPER PA60 PA60600 7106001 NM LYC O540 IO540K1J5 41532 EA VERT STAB BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 11241 L1629148A (CAN) ON ANNUAL INSPECTION FASTENERS IN THE VERTICAL STABILIZER ATTACH FITTINGS WERE FOUND LOOSE. SEVERAL OF THE FASTENE RS WERE IN FACT BROKEN OFF. FASTENERS HAD BEEN PREVIOUSLY INSTALLED AS PER AD 80-19-14AND SB 600-88A. 1 M 7 2 3O 3 O RT A17WE 1E4 1998020500462 19980205 00462 CE 1998 2 5 CA961128010 1 19961126 A 3260 21EN96 SWITCH MTSBSI MU2 MU2B35 5780411 CE GARRTT TPE331 TPE3316 01514 WP NLG DOWNLOCK FROZEN W L H O ABORTED APPROACH DEACTIVATE SYST/CIRCUITS OTHER J WARNING INDICATION AP APPROACH 1 CA 46 P27223C (CAN) ON APPROACH WHEN GEAR SELECTED DOWN, NO RESPONSE. GEAR LOWERED MANUALLY. IT IS ASSUMED THAT THE NOSE GEAR DOWN LOC K SWITCH HAD PICKED UP WATER CONTAMINATION INTERNALLY ON THE PREVIOUS TAKEOFF AND HAD FROZEN AS THE AIRCRAFT HAD BEEN FL YING FOR OVER AN HOUR IN MINUS 30 DEGREE TEMPERATURE. NEW SWITCH INSTALLED AND COATED WITH RTV. SWITCH IN A VERY VULNERA BLE POSITION TO PICK UP CONTAMINATION. 1 H 7 2 3T 4 T RT A10SW E4WE 1998020500463 19980205 00463 CE 1998 2 5 CA961128023 1 19961122 A 3230 CM3690B60122 LINE CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO MCAULY 3AF32C 3AF32C93 GL RT MLG ACT RUPTURED W A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CL CLIMB 1 CA 290316R 799904 (CAN) DURING CLIMB ATTITUDE IT WAS NOTICED THAT THE LEFT AND RIGHT HYDRAULIC FLOW LIGHTS CAME ON. INSPECTION OF THE AIRC RAFT FOUND THAT THE RIGHT HAND MAIN ACTUATOR DOWN LINE HAD RUPTURED. 1 L 7 2 3O 3 O A7CE E8CE 5 C P22EA 1998020500464 19980205 00464 SO 1998 2 5 CA961203006 1 19961114 A 3242 554366 CABLE ASSEMBLY 492152 PIPER PA44 PA44180 7104402 SO PARK BRAKE BROKEN W O OTHER O OTHER LD LANDING 1 CA 3661 (CAN) ON PREFLIGHT WHEN SETTING PARKING BRAKE THE CABLE BROKE. THE CABLE CONTROL WAS PUSHED IN AND THE BRAKES RELEASED. FLIGHT WENT ANYWAY. ON TOUCH DOWN BRAKES WERE LOCKED. CABLE WAS BROKEN AT CONNECTION TO SELECTOR VALVE. 1 L 7 2 3O A19S0 1998020500465 19980205 00465 CE 1998 2 5 CA961203013 1 19961121 A 2810 21160106 RESERVOIR TANK CESSNA 210 210R 2073458 CE CONT O520 IO520L 17032 SO MCAULY D3A34 D3A34C404 GL TOP SEAM WELD LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 7395 294530R 851897 (CAN) FUEL RESERVOIR TANK FOUND SEEPING FUEL FROM THE FORWARD TOP SEAM WELD. NO CRACK VISIBLE. TANK HAD BEEN PREVIOUSL Y REPAIRED AT 3197 HOURS. 1 H 7 1 3O 3 O RT 3A21 E5CE 5 C P47GL 1998020500468 19980205 00468 CE 1998 2 5 CA961216026 1 19961110 A 3242 03016200 BRAKE ASSEMBLY CLEVELAND BEECH 99 B99 1154004 CE PWA PT6 PT6A27 52043 EA MLG FROZEN W O OTHER O OTHER LD LANDING 1 CA 40919 (CAN) BRAKES FROZE ON LANDING. APPARENTLY THE OPERATOR USES CLEVELAND BRAKES IN SUMMER AND BF GOODRICH IN WINTER AS CLEV ELAND BRAKES FREEZE UP TOO EASY. IN THIS CASE THEY CAME OFF TOO LATE IN SEASON. 1 L 7 2 3T 4 T A14CE E4EA 1998020500469 19980205 00469 CE 1998 2 5 CA961216027 1 19961125 A 7120 NAS14782 BOLT 265102319 CESSNA 208 208 2073702 CE PWA PT6 PT6A114 52043 NE ENG MOUNT PITTED W K NONE O OTHER IN INSP/MAINT 1 CA 7497 PCE17008 (CAN) THE UPPER LEFT ATTACHMENT BOLT ON THE ENGINE MOUNT FOUND SEVERELY PITTED. THE BOLT WAS CORRODED THE COMPLETE LENGT H OF THE SHANK. NO CORROSION OF MOUNT. NO LUBE FOUND ON BOLTS WHEN REMOVED. 1 H 7 1 3T 3 T NT A37CE E4EA 1998020500470 19980205 00470 CE 1998 2 5 CA961216028 1 19961129 A 2823 5200106 LINE CESSNA 310 310R 2074245 CE CONT O520 IO520M 17032 SO MCAULY 3AF32C 3AF32C87 GL FUEL SELECTOR CHAFING W K NONE O OTHER IN INSP/MAINT 1 CA 8470 277455R 941063 (CAN) A BLACK STAIN NOTED ON THE FUEL SELECTORS 1/2 INCH RIGID LINE. THE LINE WAS FOUND CHAFING OVER HALF WAY THROUGH TH E WALL THICKNESS. WHEN THE LINE WAS REMOVED A PENCIL WAS ABLE TO PERFORATE THE LINE. SUBMITTER NOTES THAT THIS IS A DIFF ICULT AREA TO INSPECT. 1 L 7 2 3O 3 O 3A10 E5CE 5 C P22EA 1998020500471 19980205 00471 CE 1998 2 5 CA961216035 1 19961204 A 3246 D30657 WHEEL HALF MCAULY C1630060101 CESSNA 172 172N 2072434 CE LYC O320 O320D2G 41508 EA RT MLG BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA L873839A (CAN) DURING RAMP CHECK THE RIGHT HAND WHEEL RIM WAS FOUND BROKEN AND MISSING A PIECE. SUBMITTER SUGGESTS THAT PILOT MAY HAVE HIT A RUNWAY LIGHT A FEW DAYS EARLIER. 1 H 7 1 3O 3 O NT 3A12 E274 1998020500472 19980205 00472 CE 1998 2 5 CA961218001 1 19961211 A 7120 075100127 MOUNT CESSNA 180 180J 2072622 CE CONT O470 O470R 17026 SO MCAULY 2A34C 2A34C203 GL ENG LH HOR.TUBE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1101 462647 950479 (CAN) ENGINE MOUNT HAD BEEN RECENTLY OVERHAULED. THE LEFT HORIZONTAL TUBE WAS FOUND CRACKED 3/4 AROUND THE CIRCUMFERENCE IN A HELICAL PATTERN. NO CORROSION WAS EVIDENT. SUBMITTER SUGGESTS THAT TUBE INTERNALSTRESSES MAY HAVE BEEN ENCOUNTERED DURING OVERHAUL. 1 H 7 1 3O 3 O 5A6 E273 5 C P3EA 1998020500473 19980205 00473 CE 1998 2 5 CA961218010 1 19961204 A 5700 WING BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RIGHT HAND CONTAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA PCE114452 (CAN) AFTER REMOVAL OF ACCESS PANEL 612BB UNDER THE RIGHT HAND WING, AN ACCUMULATION OF WATER 1 1/2" TO 2" DEEP WAS FOUN D. THE AILERON CABLE IS ROUTED IN THIS AREA. ALL THIS COMPANIES 1900S HAD THE SAME PROBLEM. 2 L 7 2 4T 4 T RT A24CE E26NE 1998020500474 19980205 00474 CE 1998 2 5 CA961218012 1 19961207 A 5700 WING BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RIGHT HAND CONTAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA 114459 (CAN) AFTER REMOVAL OF ACCESS PANEL 612BB UNDER THE RIGHT HAND WING, AN ACCUMULATION OF WATER 1 1/2" TO 2" DEEP WAS FOUN D. THE AILERON CABLE IS ROUTED IN THIS AREA. ALL THIS COMPANIES 1900S HAD THE SAME PROBLEM. 2 L 7 2 4T 4 T RT A24CE E26NE 1998020500475 19980205 00475 CE 1998 2 5 CA961218013 1 19961208 A 5700 WING BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RIGHT HAND CONTAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA 114476 (CAN) AFTER REMOVAL OF ACCESS PANEL 612BB UNDER THE RIGHT HAND WING, AN ACCUMULATION OF WATER 1 1/2" TO 2" DEEP WAS FOUN D. THE AILERON CABLE IS ROUTED IN THIS AREA. ALL THIS OPERATORS 1900S HAD THE SAME PROBLEM. 2 L 7 2 4T 4 T RT A24CE E26NE 1998020500476 19980205 00476 CE 1998 2 5 CA961230007 1 19961216 A 5711 0523400112 SPAR CESSNA 185 185 2072802 CE MCAULY 2A34C D2A34C58 GL WING ROOT AFT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 8260 747582 (CAN) CRACK FOUND AT THE RADIUS OF THE REAR SPAR WING ROOT FITTING. 1 H 7 1 3O NC 3A24 5 C P3EA 1998020500593 19980205 00593 CE 1998 2 5 CA960620018 1 19960611 A 3213 NAS464P3A3 BOLT CESSNA 2243001205 CESSNA 182 R182 2072734 CE BELLCRANK LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA 3997 (CAN) BOLT FROM THE BELLCRANK TO THE COLLAR FOUND LOOSE. THIS IS THIRD AIRCRAFT WITH SAME PROBLEM. ALL THREE HAVE MORE T HAN 3500 HOURS. 1 H 7 1 3O RT 3A13 1998020500594 19980205 00594 1998 2 5 CA960729021 4 19960707 A 3422 060001500 DIRECTIONAL GYRO BENDIX KFC150 CESSNA 208 208B 2073701 CE FLIGHT COMMAND FAILED W K NONE I FLT. ATTITUDE INST. CR CRUISE 1 CA 111 20733 (CAN) FLIGHT COMMAND INDICATOR COMMAND BARS VIBRATING AND THEN THE AUTO PILOT WENT OFF LINE. INDICATOR REPLACED AND WORK ED FOR 4 DAYS AND THE AUTO PILOT KICKED OFF LINE AGAIN. FLIGHT COMMAND INDICATOR REPLACED AGAIN AND OK THIS TIME. 1 H 7 1 3T A37CE 1998020500596 19980205 00596 CE 1998 2 5 CA960801020 1 19960719 A 3010 15323 VALVE 1019700001 BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA WING DE ICE FAILED W O OTHER O OTHER CR CRUISE 1 CA 750 PCE81498 (CAN) WHEN SELECTING SURFACE DEICER TO EITHER MANUAL OR AUTO IN CRUISE THE WING DEICER BOOTS VISUALLY DO NOT INFLATE AND "MASTER WARNING" CAME ON. ON GROUND FUNCTIONED OK. FURTHER INVESTIGATION FOUND THAT AT CRUISE SPEED THE DEICER DISTRIBU TOR VALVE SOLENOID FOR WING INFLATION WAS NOT CLOSING COMPLETELY WHICH ALLOWED BLEED AIR TO BE DUMPED OVERBOARD INSTEAD OF TO BOOTS. VALVE REPLACED. ALSO A SMALL HOLEWAS FOUND IN BLEED AIR WARNING SENSE LINE. THUS WITH BLEED AIR BEING DUMPE D OVERBOARD AND A SMALL HOLE IN BLEED AIR SENSE LINE, THIS WOULD MOMENTARILY TRIGGER THE BLEED AIR FAIL PRESSURE SWITCH WHICH ILLUMINATED THE "MASTER CAUTION", BUT NOT THE "BLEED AIR FAIL" LIGHT. 1 L 7 2 4T 4 T A24CE E4EA 1998020500597 19980205 00597 CE 1998 2 5 CA960808104 1 19960722 A 2730 1156100181 SUPPORT BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA RT ELEVTORQ CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA PCE52376 (CAN) ON INSPECTION PER SB 2145, THE LEFT AND RIGHT ELEVATOR TORQUE TUBES CENTRE SUPPORTS WERE BOTH FOUND CRACKED. A SIS TER SHIP FOUND ONE SUPPORT CRACKED. CRACKS COME FROM INBOARD TAPER PIN HOLES. ALL THREE TORQUE TUBE ASSEMBLIES REPLACED WITH NEW P/N'S. 1 L 7 2 3T 4 T A14CE E4EA 1998020500598 19980205 00598 CE 1998 2 5 CA960827005 1 19960311 A 2720 NAS5054 BEARING BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA RUD HINGE RUSTED W K NONE O OTHER IN INSP/MAINT 1 CA PCE50099 (CAN) RUDDER REMOVED FOR MAINTENANCE AND UPPER HINGE BEARING FOUND IN TWO PIECES AND NEEDLE BEARINGS FELL OUT. BEARING D RY AND RUSTED. SUSPECT LUBE NOT GETTING INTO THE INTERIOR AS BEARING IS FACTORY SEALED. 1 L 7 2 3T 4 T A14CE E4EA 1998020500599 19980205 00599 CE 1998 2 5 CA960923017 1 19960913 A 3230 MC815AS1 CONTROLLER HARTMAN BEECH 100 A100 1152915 CE PWA PT6 PT6A34 52043 EA MLG MOTOR BURNT W O OTHER J O WARNING INDICATION OTHER AP APPROACH 1 CA 49 JK45225 0 (CAN) GEAR WOULD NOT EXTEND. EMERGENCY EXTENSION CARRIED OUT. FOUND THE GEAR MOTOR CONTROLLER BURNT. THE UNIT HAD JUST B EEN OVERHAULED. 1 L 7 2 3T 4 T A14CE E4EA 1998020500600 19980205 00600 SO 1998 2 5 CA960923023 1 19960909 A 3260 HOOK PIPER PA31 PA31350 7103110 SO DOWN & LOCK RH DIRTY W O OTHER J WARNING INDICATION AP APPROACH 1 CA (CAN) AFTER LOWERING LANDING GEAR, THE RIGHT MAIN LANDING GEAR DID NOT INDICATE DOWN AND LOCKED. EMERGENCY SYSTEM USE TO GET A SAFE INDICATION. THE DOWN AND LOCK HOOK WAS FOUND DIRTY. 1 L 7 2 3O A20SO 1998020500601 19980205 00601 SO 1998 2 5 CA960923027 1 19960819 A 3213 40288000 TRUNNION 4550425 PIPER PA31 PA31350 7103110 SO RT MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 13523 (CAN) RIGHT HAND LANDING GEAR TRUNNION FOUND CRACKED AT THE UPPER CENTRE WEB. THIS AIRCRAFT HAS A VORTEX GENERATOR KIT I NSTALLED WHICH INCREASES MTOW BY 300 LBS. 1 L 7 2 3O A20SO 1998020500602 19980205 00602 CE 1998 2 5 CA960924037 1 19960917 A 2750 1003840403 MOTOR BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA FLAP BURNT W A UNSCHED LANDING B M SMOKE/FUMES/ODORS/SPARKS OVER TEMP CL CLIMB 1 CA 437 PCE80073 (CAN) ON CLIMB OUT FLAPS SELECTED UP. MOTOR DID NOT SHUT OFF AND BEGAN TO SMOKE UNTIL CB POPPED. THE CAM THAT CONTACTS T HE UP LIMIT SWITCH DID NOT MAKE CONTACT BEFORE FLAPS WERE UP TIGHT TO STOP. THE SWITCH P/N BZ7RW82255518T, HAD JUST BEEN REPLACED AND WAS RIGGED AS PER MM. BUT WAS PROBABLY RIGGED TOO TIGHT FOR AIR OPERATION. 1 L 7 2 4T 4 T A24CE E4EA 1998020500604 19980205 00604 CE 1998 2 5 CA961001008 1 19960909 A 2710 CONTROL CABLE CESSNA 208 208B 2073701 CE COCKPIT FIREWALL WORN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) AILERON CABLE FOUND WEARING INTO FLOOR BOARD NEAR THE COCKPIT FIREWALL. FLOORBOARD HAD BEEN INCORRECTLY INSTALLED AND SCREW HOLES WERE ELONGATED. 1 H 7 1 3T A37CE 1998020500605 19980205 00605 CE 1998 2 5 CA961007011 1 19960906 A 2730 CONTROL CABLE CESSNA 172 172M 2072418 CE ELEV FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA 10503 (CAN) ELEVATOR CABLE FOUND FRAYED AT THE REAR UPPER FUSELAGE PULLEY. 1 H 7 1 3O NT 3A12 1998020500606 19980205 00606 CE 1998 2 5 CA961007012 1 19960912 A 2720 07600129 RUDDER BAR CESSNA 185 A185F 2072821 CE MCAULY 2A34C D2A34C58 GL AT PEDAL BROKEN W K NONE F FLT CONT AFFECTED TX TAXI/GRND HDL 1 CA 3993 748323 (CAN) WHILE WATER TAXIING, RUDDER BAR BROKE AT OUTBOARD PEDAL ATTACH AT REINFORCEMENT. REFERENCE AD CF-73-05. THIS UNIT HAS WELDED TAB WHICH BROKE THROUGH ALSO. 1 H 7 1 3O 3A24 5 C P3EA 1998020500607 19980205 00607 GL 1998 2 5 CA961007015 1 19960922 A 3243 MC4D MASTER CYLINDER DIAMON DA20A1 DA20A1 05626UX GL COPILOT BRAKE FAILED W K NONE O OTHER TX TAXI/GRND HDL 1 CA (CAN) CO-PILOTS BRAKES - NO BRAKING ACTION, FOUND RESERVOIRS EMPTY BUT NO LEAKS IN SYSTEM. BELIEVE REVERSE PRESSURE EMPT IED RESERVOIR THROUGH FILLER PORT. FACTORY INFORMED SUBMITTER THAT MASTER CYLINDER AND RESERVOIR PROBLEMS. CHANGED BOTH. RESERVOIRS CAN LEAK AT WELD. 1 L 7 1 3O NT TA4CH 1998020500608 19980205 00608 GL 1998 2 5 CA961007016 1 19960928 A 3243 MC4D MASTER CYLINDER DIAMON DA20A1 DA20A1 05626UX GL BRAKES FAILED W K NONE O OTHER TX TAXI/GRND HDL 1 CA (CAN) CO-PILOT RIGHT BRAKE HAD ZERO ACTION. FOUND RESERVOIR CYLINDER EMPTY. CO-PILOT LEFT BRAKE MASTER CYLINDER SLOPPY A S WELL AS BOTH PILOTS BRAKE CYLINDERS. ALL 4 MASTER CYLINDERS REPLACED WITH NEW "BATCH". 1 L 7 1 3O NT TA4CH 1998020500610 19980205 00610 1998 2 5 CA961009002 4 19961003 A 3455 UG88CU CONNECTOR BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA ADF SENSE ANT WRONG PART W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA PCE80594 (CAN) UNAPPROVED BNC CONNECTOR USED TO CONNECT SENSE ANTENNA COAX TO REAR OF ADF TRAY. BNC CONNECTOR ALSO MODIFIED TO AD APT TO COAX DIAMETER. 1 L 7 2 4T 4 T A24CE E4EA 1998020500611 19980205 00611 CE 1998 2 5 CA961009003 1 19960927 A 3230 CIRCUIT BREAKER BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA GEAR MOTOR FAILED W L ABORTED APPROACH O OTHER AP APPROACH 1 CA 227 PCE81547 (CAN) GEAR FAILED TO EXTEND WHEN SELECTED DOWN. HYDRAULIC MOTOR DID NOT OPERATE. 60 AMP BREAKER WAS CHECKED AS IN. MOTOR THEN STARTED AND GEAR EXTENDED. 60 AMP BREAKER REPLACED. 1 L 7 2 4T 4 T A24CE E4EA 1998020500612 19980205 00612 1998 2 5 CA961009004 4 19960208 A 3422 KG102A DIRECTIONAL GYRO KING CESSNA 208 208B 2073701 CE PWA PT6 PT6A114 52043 NE COCKPIT PRECESSING W L ABORTED APPROACH O OTHER AP APPROACH 1 CA 1087 6362 PCE19183 (CAN) COMPASS PRECESSED 90 DEGREES DURING APPROACH. APPROACH ABORTED. MAINTENANCE UNABLE TO FIND FAULT. GYRO WAS REPLACE D WHEN PART AVAILABLE. 1 H 7 1 3T 3 T A37CE E4EA 1998020500613 19980205 00613 CE 1998 2 5 CA961009007 1 19960930 A 3231 08411066 BELLCRANK CESSNA 310 310R 2074245 CE CONT O520 IO520MB 17032 SO MCAULY 3AF32C 3AF32C87 GL RT MLG DOOR BROKEN W K NONE O OTHER AP APPROACH 1 CA 9061 210906 773849 (CAN) WHEN AIRCRAFT RETURNED FROM TEST FLIGHT THE RIGHT MAIN GEAR DOOR WAS HANGING DOWN. FURTHER INSPECTION REVEALED THA T THE GEAR DOOR BELLCRANK HAD BROKEN 3" TO THE LEFT OF THE GEAR DOOR ROD END ATTACHMENT. 1 L 7 2 3O 3 O 3A10 E5CE 5 C P22EA 1998020500614 19980205 00614 CE 1998 2 5 CA961009008 1 19960930 A 3230 510011141 LINE CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO MCAULY 3AF32C 3AF32C505 GL LT GEAR DOWN CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 5501 266797R 940451 (CAN) ON WALK AROUND PILOT FOUND POOL OF HYDRAULIC FLUID UNDER LEFT WHEEL WELL. FLANGE ON GEAR DOWN LINE FOUND CRACKED. 1 L 7 2 3O 3 O A7CE E8CE 5 C P22EA 1998020500615 19980205 00615 CE 1998 2 5 CA961011007 1 19961002 A 3211 501200772 SUPPORT 5012007710 BEECH 80 65B80 1152812 CE LYC O540 IGSO540A1D 41532 EA MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 7400 RL370750 (CAN) CRACKS EXTENDING UPWARDS FROM BOTTOM EDGE OF OUTBOARD SUPPORT WHERE THEY ATTACH TO LOWER FORWARD SPAR CAP. BOTH LO WER BOLT HOLES AT SPAR CAPS, BOTH SIDES OF AIRCRAFT FOUND CRACKED. THESE UNITS MOUNT TOP END OF MAIN GEAR ACTUATORS. 1 L 7 2 3O 3 O 3A20 1E7 1998021100010 19980211 00010 EU 1998 2 11 CA961104010 1 19961010 A 3250 Z4242170001 SPRING ZLIN 242 Z242L 9970204 EU NOSE GEAR BROKEN W D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CA 659 (CAN) PILOT REPORTED THAT THE RUDDER PEDALS WERE OFFSET WHEN NOSE WHEEL WAS STRAIGHT. THE LEFT NOSE WHEEL STEERING SPRIN G WAS FOUND BROKEN. 1 L 7 1 3O 0 A76EU 1998021100011 19980211 00011 SO 1998 2 11 CA961120006 1 19961113 A 6120 2489408 CONTROL CABLE PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2C 41532 EA HARTZL HCE3Y HCE3YR2A GL LT PROP PITCH BROKEN W D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CA 6388 RL247461A DJ9305A (CAN) LEFT HAND PITCH CONTROL CABLE BROKE WHILE CHECKING IT. CABLE BROKE INSIDE CASE AT BEGINNING OF THE FLEXIBLE SECTIO N. SUBMITTER SUSPECTS THAT PILOT TRIED TO MOVE CONTROL WHEN ENGINE WAS STILL COLD. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 1998021100012 19980211 00012 EU 1998 2 11 CA961230005 1 19961129 A 3242 155N607334 O-RING K2202007 ZLIN 242 Z242L 9970204 EU RT BRAKE CALIP FAILED W O OTHER O OTHER LD LANDING 1 CA 879 (CAN) AFTER LANDING THE RIGHT HAND BRAKE LOCKED. THE 'O' RING ON THE BRAKE CALIPER COVER HAD FAILED. 1 L 7 1 3O 0 A76EU 1998021100020 19980211 00020 CE 1998 2 11 CA960620020 1 19960611 A 7160 QS200 CLAMP 22500161 CESSNA 182 R182 2072734 CE LYC O540 O540J3C5 41532 EA MCAULY 2D34C B2D34C214 GL CARB INT LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA L1967540A 780298 (CAN) CLAMP AT AIR BOX ASSEMBLY FOR CARBURETOR FOUND LOOSE. HOSE HAD NOT BEEN PUSHED ON PROPERLY. THIS IS NOT CORRECT CLAMP BUT IS JUST AS GOOD OR BETTER ACCORDING TO SUBMITTER. CORRECT CLAMP IS AN NAS398-66. THIS LOOSE CLAMP COULD CAUS E A LOSS OF POWER AND OBSTRUCTION OF CARBURETOR AIR INTAKE. 1 H 7 1 3O 3 O RT 3A13 E295 5 C P7EA 1998021100021 19980211 00021 SO 1998 2 11 CA960924031 1 19960917 A 7120 86212002 MOUNT PIPER PA44 PA44180 7104402 SO LYC O360 O360E1A6 41514 EA LEFT ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 5024 L22377T (CAN) LEFT ENGINE MOUNT FOUND CRACKED AT THE LEFT UPPER MEMBER AND THE MEMBER BETWEEN THE LEFT UPPER AND THE LEFT LOWER MOUNT. WELDING REPAIR HAD BEEN PREVIOUSLY CARRIED OUT AS HAD A MAGNETIC PARTICLE INSPECTION. NO HARD LANDING REPORTED, N OR VIBRATION FROM ENGINE. POSSIBLE MATERIAL FATIGUE. PIPER OWNER MAGAZINE HAD NOTED TWO LEFT MOUNTS CRACKED RECENTLY AND OVERHAUL AGENCY HAD ALSO REPORTED ONE. 1 L 7 2 3O 3 O A19S0 E286 1998021100106 19980211 00106 NE 1998 2 11 98ZZZX583 2 19961202 A 7310 430123604 MANIFOLD BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE ENGINE FUEL LEAKS A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 911MZ 588 1XG04646 S7098 LE45026 SUBMITTER STATES EXCESSIVE FUEL MANIFOLD LEAKS OVER THE LAST 18 MONTHS. ALLIED SIGNAL IS IN THE PROCESS OF RELEASING AN ASB LIMITING THE LIFE OF THE FUEL MANIFOLD TUBES. OTHER OPERATORS SUBMITTER CONTACTED ARE HAVING THE SAME PROBLEMS. O MNIFLIGHT HAS GONE TO A POST-FLIGHT CHECK AND A SHIFT-CHANGE CHECK OF THIS MANIFOLD. 1 G 7 2 3U 3 U H13EU E5NE 1998021100107 19980211 00107 NE 1998 2 11 98ZZZX584 2 19960428 A 7310 430137601 MANIFOLD BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101650B1 41560 NE ENGINE FUEL LEAKS A RMXA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 05 170MC 821 1YG02334 S7217 LE45714 SUBMITTER STATES EXCESSIVE FUEL MANIFOLD LEAKS OVER THE LAST 18 MONTHS. ALLIED SIGNAL IS IN THE PROCESS OF RELEASING AN ASB LIMITING THE LIFE OF THE FUEL MANIFOLD TUBES. OTHER OPERATORS SUBMITTER CONTACTED ARE HAVING THE SAME PROBLEMS. O MNIFLIGHT HAS GONE TO A POST-FLIGHT CHECK AND A SHIFT-CHANGE CHECK OF THIS MANIFOLD. 1 G 7 2 3U 3 U H13EU E5NE 1998021100108 19980211 00108 NE 1998 2 11 98ZZZX585 2 19960401 A 7310 430137601 MANIFOLD BELL 222 222U 1182140 SW LYC LTS101 LTS101750C1 41560 NE ENGINE FUEL LEAKS A RMXA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 05 6992 LLK05989 47521 SUBMITTER STATES EXCESSIVE FUEL MANIFOLD LEAKS OVER THE LAST 18 MONTHS. ALLIED SIGNAL IS IN THE PROCESS OF RELEASING AN ASB LIMITING THE LIFE OF THE FUEL MANIFOLD TUBES. OTHER OPERATORS SUBMITTER CONTACTED ARE HAVING THE SAME PROBLEMS. O MNIFLIGHT HAS GONE TO A POST-FLIGHT CHECK AND A SHIFT-CHANGE CHECK OF THIS MANIFOLD. 1 G 7 2 3U 3 U H9SW E5NE 1998021100109 19980211 00109 NE 1998 2 11 98ZZZX586 2 19960228 A 7310 430123604 MANIFOLD BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE ENGINE FUEL LEAKS A RMXA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 05 117NG 184 1RH03172 S7083 LE45232 SUBMITTER STATES EXCESSIVE FUEL MANIFOLD LEAKS OVER THE LAST 18 MONTHS. ALLIED SIGNAL IS IN THE PROCESS OF RELEASING AN ASB LIMITING THE LIFE OF THE FUEL MANIFOLD TUBES. OTHER OPERATORS SUBMITTER CONTACTED ARE HAVING THE SAME PROBLEMS. O MNIFLIGHT HAS GONE TO A POST-FLIGHT CHECK AND A SHIFT-CHANGE CHECK OF THIS MANIFOLD. 1 G 7 2 3U 3 U H13EU E5NE 1998021100110 19980211 00110 NE 1998 2 11 98ZZZX587 2 19960112 A 7310 430137601 MANIFOLD BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE ENGINE FUEL LEAKS A RMXA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 05 117CH 29 0121 S7061 LE45268 SUBMITTER STATES EXCESSIVE FUEL MANIFOLD LEAKS OVER THE LAST 18 MONTHS. ALLIED SIGNAL IS IN THE PROCESS OF RELEASING AN ASB LIMITING THE LIFE OF THE FUEL MANIFOLD TUBES. OTHER OPERATORS SUBMITTER CONTACTED ARE HAVING THE SAME PROBLEMS. O MNIFLIGHT HAS GONE TO A POST-FLIGHT CHECK AND A SHIFT-CHANGE CHECK OF THIS MANIFOLD. 1 G 7 2 3U 3 U H13EU E5NE 1998021100574 19980211 00574 EU 1998 2 11 HAIHCMA0070 1 19961119 A 6520 350A33215300 LAMIFICATION SNIAS 350 AS350B2 8680813 EU REAR ROTOR TORN E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 992BH 71 2889 REAR ROTOR LAMIFICATIONS ARE TORN BEYOND LIMITS. 1 G 7 1 3U H9EU 1998032600444 19980326 00444 NE 1998 3 26 98ZZZX1158 2 19960109 A 7230 430150601 SEAL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE RT ENG NR 2 LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 911BY 763 1530 7127 LE45344E RIGHT ENGINE NR 2 BEARING SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. ACTUAL P/ N INSTALLED, 4-141-45-02, SN 390. 1 G 7 2 3U 3 U H13EU E5NE 1998032600445 19980326 00445 NE 1998 3 26 98ZZZX1159 2 19960109 A 7250 430144801 SEAL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE RT ENGINE NR 3 LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 911BY 763 867 7127 LE45344E RIGHT ENGINE NR 5 BEARING SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1998032600446 19980326 00446 NE 1998 3 26 98ZZZX1160 2 19960109 A 7230 430124203 BEARING BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE ENGINE COMPR PITTED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911BY 860 0164 7127 LE45344E COMPRESSOR BEARING HAS EXCESSIVE PITTING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1998040200016 19980402 00016 EU 1998 4 2 CA961021007 1 19960824 A 7714 0177555170 TACHOMETER BOX SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENG RPM SHORTED W O OTHER O OTHER LD LANDING 1 CA 293 4268 (CAN) TACH BOX FAILED WHILE ON VERY SHORT FINAL TO MOUNTAIN TOP LANDING AT 8000 FEET, AND 20 DEGREES CELSIUS. CAUSED EN GINE BLEED VALVE NOT TO CLOSE THEREBY ENGINE COMPRESSOR EXCEEDED NORMAL RED LINE. THE ENGINE WAS NOT ABLE TO MAINTAIN RO TOR RPM AND IT RAPIDLY DECAYED. 1 G 7 1 3U 3 U H9EU E19EU 1998040200017 19980402 00017 CE 1998 4 2 CA961028007 1 19961015 A 3260 65430087 SWITCHES CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE GEAR UPLOCK DEFECTIVE W O OTHER J WARNING INDICATION CL CLIMB 1 CA 2467 71714 (CAN) GEAR SELECTED UP, RED IN TRANSIT LIGHT STAYED ON AND HYDRAULIC PRESSURE LIGHT ON. NOSE RETRACTED, BUT MAIN DID NO T. HYDRAULIC LIGHT THEN WENT OUT. BOTH MAIN LANDING GEAR DOWNLOCK GREENS CAME ON. GEAR SELECTED DOWN PRIOR TO LANDING AND ALL 3 GEARS DOWN AND LOCKED. INVESTIGATION FOUND THAT BOTH UPLOCK SWITCHES HAD A HIGH RESISTANCE ACROSS CONTACTS. SWITCHES SENT TO CESSNA FOR CHECK. PART TC: 2,780. 1 L 7 2 4F 4 F A22CE E1NE 1998040200018 19980402 00018 NE 1998 4 2 CA961104003 2 19961029 A 7200 ENGINE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 1 ENGINE FIRE W A C D ABORTED TAKEOFF RETURN TO BLOCK A FLAME/FIRE TO TAKEOFF 1 CA 517443 (CAN) TAKE-OFF ABORTED AT 60 KNOTS. TOWER ADVISED FLAMES COMING FROM TAIL PIPE OF NR 1 ENGINE. FIRE EXTINGUISHER BOTTLE S ACTIONED. MAINTENANCE INVESTIGATION REVEALED METAL IN TAILPIPE. BORESCOPE CHECK CONFIRMED ENGINE FAILURE. 2 L 7 3 4F 4 F A22WE E23EA 1998040200019 19980402 00019 WP 1998 4 2 CA961104008 2 19961028 A 7240 31032153 COMBUSTOR SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 23240 8681 P54086C (CAN) ON INSPECTION, AFTER ENGINE REMOVED TO FACILITATE REMOVAL OF NR 3 ROTOR, THE COMBUSTOR LOWER SKIRT WAS FOUND CRACK ED CIRCUMFERENTIALLY APPROXIMATELY 22 INCHES OR 3/4 OF THE CIRCUMFERENCE. GARRETT TO INVESTIGATION WELD FAILURE. 2 L 7 2 4T 4 T RT A8SW E4WE 1998040200020 19980402 00020 GL 1998 4 2 CA961112005 2 19960925 A 7250 6871505 BEARING 6898735 HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL NR 5 BEARING FAILED W A R UNSCHED LANDING AUTOROTATION J R WARNING INDICATION PARTIAL RPM/PWR LOSS CR CRUISE 1 CA 197 CAT35402 CAE834919 (CAN) DURING FLIGHT, CHIP LIGHT ILLUMINATED AND POWER LOSS OCCURRED. AUTO ROTATION CARRIED OUT. 1 G 7 1 3U 3 U H3WE E4CE 1998040200022 19980402 00022 SW 1998 4 2 CA961112013 1 19961011 A 3230 ROLL PIN AEROCD 540084501 GULSTM 690TP 690A 0141722 SW GEAR HANDLE SHEARED W A L ABORTED APPROACH O OTHER LD LANDING 1 CA 5521 (CAN) LANDING GEAR FAILED TO EXTEND ON APPROACH, LANDING GEAR HANDLE MOVED BUT HYDRAULIC VALVE LEVER DID NOT MOVE. LAND ING GEAR EXTENDED WHEN HYDRAULIC VALVE WAS OPERATED IN THE MANUAL MODE. MAINTENANCE INVESTIGATION REVEALED THE ROLL PIN OF THE LANDING GEAR CONTROL ASSEMBLY WAS NOT CORRECTLY INSTALLED WHICH CAUSED IT TO SHEAR. 1 H 7 2 3T 2A4 1998040200023 19980402 00023 WP 1998 4 2 CA961114008 2 19961028 A 7240 31032153 COMBUSTOR SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP ENGINE CRACKED W A K NONE O OTHER IN INSP/MAINT 1 CA 2623 P54086C P54158 (CAN) COMBUSTOR LOWER SKIRT WAS FOUND CRACKED CIRCUMFERENTIALLY APPROXIMATELY 22 INCHES OR 3/4 OF THE CIRCUMFERENCE. GAR RETT INVESTIGATING FAILURE. PART TC: 3,117. 2 L 7 2 4T 4 T RT A8SW E4WE 1998040200024 19980402 00024 CE 1998 4 2 CA961205019 1 19961202 A 2750 556517531 GEARBOX CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE FLAP GR BOX FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 2396 71751 (CAN) WHILE COMPLYING WITH SB 550-27-16, AND AFTER REMOVAL OF BOTH GEARBOXES, ONE COULD BE TURNED FREELY WITHOUT OUTPUT SHAFT TURNING. 1 L 7 2 4F 4 F A22CE E1NE 1998040200025 19980402 00025 CE 1998 4 2 CA961218018 1 19961211 A 2430 62581038 CAPACITOR CESSNA 500 550 2076604 CE START/GEN FILTER SHORTED W K NONE O OTHER IN INSP/MAINT 1 CA 2357 (CAN) A NOISE FILTER FOR THE LT STARTER GENERATOR BURNED AND WAS FOUND DURING A PHASE 5 INSPECTION. A SMALL BUT INTENSE FIRE HAD BURNED SURROUNDING WIRING AND RETAINING BRACKET WAS DEFORMED FROM THE BURN. THE OIL FROM THE CAPACITOR COVERE D THE WIRING AROUND THE POINT. CAPACITOR, BRACKET AND WIRING REPLACED FOR THE OIL PRESSURE TRANSMITTER. AREA CLEANED A ND INSPECTED FOR FURTHER DAMAGE, BUT NONE FOUND. STARTER GENERATOR ALSO INSPECTED FOR DAMAGE, BUT NONE FOUND. 1 L 7 2 4F A22CE 1998040200041 19980402 00041 NE 1998 4 2 CA970311011 2 19960913 A 7311 RH2113 OIL COOLER SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE INTERNAL DIRTY W K NONE O OTHER IN INSP/MAINT 1 CA 345 (CAN) DUST CAPS WERE MISSING WHEN RECEIVED FROM OVERHAUL CONTRACTOR. MUCH DUST EJECTED FROM COOLER WHEN COMPRESSED AIR BLOWN THROUGH. 1 G 7 1 3U 3 U H9EU E19EU 1998040200042 19980402 00042 EU 1998 4 2 CA970311013 1 19960909 A 6520 350A33215300 HINGE SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE T/R WORN W K NONE O OTHER IN INSP/MAINT 1 CA 4432 (CAN) LAMINATED HINGE DAMAGED AND WORN. 1 G 7 1 3U 3 U NC H9EU E19EU 1998040200044 19980402 00044 SW 1998 4 2 CA970311065 1 19961121 A 5320 206033173001 SUPPORT BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL FUSELAGE CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA CAE800471BA (CAN) SUPPORT CORRODED BEYOND REPAIRABLE LIMITS. 1 G 7 1 3U 3 U H2SW E4CE 1998040200045 19980402 00045 SW 1998 4 2 CA970311066 1 19961121 A 5320 206031301023 SUPPORT BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL UPPER RT RADIUS CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA CAE800471BA (CAN) SUPPORT WAS CRACKED IN FORWARD UPPER RIGHT HAND RADIUS. NO CRACKS ALLOWED IN THIS AREA. DAMAGE ONLY VISIBLE WITH FUEL CELL REMOVED. AIRCRAFT TT: 14,949 HOURS. 1 G 7 1 3U 3 U H2SW E4CE 1998040200046 19980402 00046 WP 1998 4 2 CA970311068 1 19961216 A 3270 369H600151 REAR STRUT HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL DRAG BRACE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA CAE832104 (CAN) LOOSE INNER FITTING, WORKING RIVETS AND CRACKED AROUND LOWER HOLE OF LANDING GEAR DRAG BRACE HOLE. 1 G 7 1 3U 3 U H3WE E4CE 1998040200047 19980402 00047 SW 1998 4 2 CA970311073 1 19961125 A 5320 206031301023 SUPPORT BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL UPPER RADIUS CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA CAE821443 (CAN) SUPPORT WAS CRACKED IN FORWARD UPPER RIGHT HAND RADIUS. NO CRACKS ALLOWED IN THIS AREA. THIS DAMAGE WAS VISIBLE O NLY WITH FUEL CELL REMOVED. AIRCRAFT TT: 15,819 HOURS. 1 G 7 1 3U 3 U H2SW E4CE 1998040200077 19980402 00077 WP 1998 4 2 CA970421036 1 19960906 A 6220 369D21201 HUB HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL LINKS CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1848 1240 CAE830926 (CAN) CRACKS FOUND ON RED AND GREEN LOWER LEAD LAG LINKS. CRACKS RADIATED FROM TRAILING EDGE BOLT BUSHING TO THE MIDDLE OF LINK. APPROX 2 INCHES LONG. 1 G 7 1 3U 3 U H3WE E4CE 1998041700394 19980417 00394 NE 1998 4 17 CA960503101 2 19960304 A 7532 9550158260 BLEED VALVE SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE SHORTED W K NONE O OTHER CR CRUISE 1 CA 199 4268 (CAN) VALVE FAILED DURING TEST FLIGHT OF NEW TACH BOX. VALVE WOULD NOT CLOSE AT HIGH POWER SETTINGS. 1 G 7 1 3U 3 U H9EU E19EU 1998041700395 19980417 00395 EU 1998 4 17 CA960503102 1 19960304 A 7714 0177555170 TACH BOX SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE SHORTED W B EMER. DESCENT J R WARNING INDICATION PARTIAL RPM/PWR LOSS HO HOVERING 1 CA 101 4268 (CAN) SENSOR BOX THAT ACTIVATES ENGINE BLEED VALVE FAILED IN FLIGHT. FAILURE CAUSES BLEED VALVE TO REMAIN OPEN CAUSING REDUCED AVAILABLE ENGINE POWER. FAILURE WAS ACCOMPANIED BY BURNING ELECTRICAL SMELL. 1 G 7 1 3U 3 U H9EU E19EU 1998041700396 19980417 00396 EU 1998 4 17 CA960503104 1 19960416 A 2810 COLLECTOR TANK PILATS PC6T PC6B1H2 3375011 EU FUEL SYS CONTAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) COLLECTOR TANK WAS FULL OF FOAM WHICH WAS DETERIORATING FROM THE FUEL. IT WAS FOUND IN THE FUEL FILTERS. TANKS CL EANED. 1 H 7 1 3T 7A15 1998041700398 19980417 00398 CE 1998 4 17 CA960513027 1 19960423 A 3213 AN17520 BOLT CESSNA 421 421C 2076016 CE LT TORQUE LINK MISSING W O OTHER O OTHER LD LANDING 1 CA (CAN) ON LANDING, LT TORQUE LINK CENTER BOLT (AN 175-20) BUSHING (5041013) AND WASHERS (AN 960-7L) AND WASHERS (5045018- 2) DEPARTED FROM AIRCRAFT CAUSING WHEEL TO CAMBER TO A CROSSWISE CONDITION AFFECTING LANDING ROLLOUT. DYE PENETRANT INS PECTION CARRIED OUT ON GEAR, BUT NO FAULTS FOUND. WHEEL ASSEMBLY REPLACED. IT COULD NOT BE DETERMINED WHETHER OR NOT T HE BOLT SHEARED OR COTTER PIN SHEARED. 1 L 7 2 3O A7CE 1998041700400 19980417 00400 CE 1998 4 17 CA960515007 1 19960114 A 2913 99101372 HYDRAULIC PUMP CESSNA 414 414A 2075907 CE R/H ENGINE LOW FLOW W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) AIRCRAFT PARKED OUTSIDE, TEMP -25 DEGREES CELSIUS. AIRCRAFT PRE-HEATED AND PREPARED FOR FLIGHT. ON TAKEOFF, AT P OINT OF LIFT-OFF, RT SIDE HYDRAULIC FLOW LIGHT ILLUMINATED. PILOT CONTINUED WITH TAKEOFF AND ATTEMPTED TO RETRACT THE U NDERCARRIAGE. FIRST ATTEMPT FAILED BUT THE SECOND WAS SUCCESSFUL. ACFT RETURNED TO BASE AND LANDED SAFELY. MAINTENANC E JACKED AIRCRAFT AND CHECKED THE GEAR. NO FAULTS FOUND AND AIRCRAFT RETURNED TO SERVICE. SUBMITTER STATES THIS HAS HA PPENED ON OTHER 400 SERIES ACFT WITHOUT DETERMINING A CAUSE. 1 L 7 2 3O A7CE 1998041700410 19980417 00410 SW 1998 4 17 CA960802003 1 19960727 A 6322 9103PP BEARING BELL 204 204B 1181404 SW LYC T53 T5313B 41549 NE BLOWER ASSY ROUGH W K NONE E VIBRATION/BUFFET CR CRUISE 1 CA 162 LE07531 (CAN) HIGH TO MEDIUM FREQUENCY VIBRATION WAS BEING DETECTED BY THE PILOT THROUGH THE TAIL ROTOR PEDALS. EXAMINATION FOU ND BLOWER ASSEMBLY MAKING VIBRATION. REPLACED ASSEMBLY AND RECTIFIED PROBLEM. 1 G 7 1 4U 4 U H1SW E17EA 1998041700412 19980417 00412 EU 1998 4 17 CA960807002 1 19960727 A 3230 GEAR ISRAEL 1124 1124 4500102 EU RETRACT SEC FAILED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA (CAN) AFTER TAKEOFF, GEAR COULD NOT BE SELECTED UP. AIRCRAFT RETURNED TO BASE AND LANDED SUCCESSFULLY. 2 M 7 2 4F A2SW 1998041700415 19980417 00415 SW 1998 4 17 CA960812006 1 19960808 A 7922 8A575000 VALVE SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110 01514 WP THERMO BYPASS STUCK W A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CR CRUISE 1 CA P54232 (CAN) DURING CRUISE, THE CREW NOTICED HIGH OIL TEMP ON RT ENGINE AND DIVERTED FOR LANDING. MAINTENANCE FOUND HIGH OIL T EMP IN THE OIL TANK AND COOL OIL IN THE COOLER. THE VERNATHERM VALVE P/N 8A575-000 WAS REPLACED AND GROUND CHECKED SERV ICEABLE. 2 L 7 2 4T 4 T RT A8SW E4WE 1998041700417 19980417 00417 CE 1998 4 17 CA960909031 1 19960828 A 5210 99120754 DOOR SEAL CESSNA 500 550 2076604 CE CABIN FAILED W B G I EMER. DESCENT O2 MASK DEPLOYED CABIN DEPRESSURIZATION J WARNING INDICATION CR CRUISE 1 CA 2255 (CAN) AT FL 350, ONE HOUR INTO FLIGHT, DOOR SEAL BLEW. CABIN ALTITUDE CLIMBED RAPIDLY TO 18,000 FEET. REPLACED CABIN D OOR SEAL DUE TO SUSPECTED MOISTURE AND FREEZING, THEREFORE, BLOCKING THE SUPPLY OF AIR TO KEEP THE DOOR SEAL INFLATED. E NTIRE SEAL INFLATION PLUMBING PURGED OF MOISTURE. PART TC: 2,691. AIRCRAFT TT: 2,848. 1 L 7 2 4F A22CE 1998041700418 19980417 00418 GL 1998 4 17 CA960910039 2 19960813 A 7250 TURBINE ASSY AEROSP AS355 AS355F1 8680810 EU ALLSN 250C 250C20F 03013 GL FIRST STAGE DAMAGED W A B E UNSCHED LANDING EMER. DESCENT ENGINE SHUTDOWN J Y WARNING INDICATION ENGINE STOPPAGE HO HOVERING 1 CA 5328 2293 CAE840500 (CAN) DURING OPERATIONS, THE PILOT HEARD A VIOLENT NOISE FROM HIS RIGHT SIDE. INSTRUMENTS CONFIRMED ENGINE WAS LOST. P ILOT PICKED UP AIRSPEED AND WAS ABLE TO CARRY OUT A ONE ENGINE LANDING. PRELIMINARY INVESTIGATION REVEALED SUBSTANTIAL DAMAGE TO THE FIRST STAGE WHEEL AND NOZZLE. PART TC: 6,336. 1 G 7 2 3U 3 U H11EU E4CE 1998041700419 19980417 00419 1998 4 17 CA960916005 4 19960905 A 3460 5223207003 FLIGHT COMPUTER AMD FALCON FALCON20 2730103 EU GE CF700 CF7002D2 30010 NE NR 1 FAILED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA 245U058 (CAN) AIRCRAFT CLIMBING THROUGH FL 180, THE AUTO-PILOT FLUTTERED AND DISCONNECTED. A NOTICEABLE BURNING ODOR WAS NOTICE D IN THE CABIN. SMOKE WAS NOTED COMING FROM NR 1 FLIGHT COMPUTER. NR 1 FLIGHT COMPUTER FOUND BURNED INTERNALLY. UNIT REPLACED. 2 L 7 2 4F 4 F RT A7EU E7EA 1998041700522 19980417 00522 SW 1998 4 17 CA970421057 1 19961224 A 3020 6852176 VALVE ANTI ICE 6856983 BELL 206 206L 1181522 SW ALLSN 250C 250C20B 03013 GL GUIDE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA CAE830144 (CAN) ANTI-ICE VALVE GUIDE ASSY CRACKED ALLOWING THE GUIDE ASSY LEVER SUPPORT TO SEPERATE FROM THE VALVE ASSY B-NUT. REP LACED. 1 G 7 1 3U 3 U H2SW E4CE 1998041700523 19980417 00523 GL 1998 4 17 CA970421058 2 19961209 A 7230 6890550 COMPRESSOR 6890550 HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL ENGINE LEAKING W K NONE O OTHER IN INSP/MAINT 1 CA 6579 3034 CAC32701 CAE830926 (CAN) COMPRESSOR DISCHARGE AIR LEAKING BETWEEN COMPRESSOR SCROLL DISCHARGE AND STEEL INSERTS. PART TC: 1,665. 1 G 7 1 3U 3 U H3WE E4CE 1998041700580 19980417 00580 GL 1998 4 17 CA970528020 2 19961217 A 7321 252464424 FUEL CONTROL BENDIX 252464424 BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL ENGINE LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA 219 327405 CAE832831 (CAN) GROUND IDLE RPM DROPPED TO 57 PERCENT N1 IDLE SPEED. ADJUSTMENT SCREW FOUND TO BE EASY TO ROTATE BY HAND. NO BUI LT IN FRICTION FELT. REASON FOR LAST REMOVAL. REPLACED. 1 G 7 1 3U 3 U H2SW E4CE 1998041700581 19980417 00581 GL 1998 4 17 CA970528021 2 19961217 A 7321 322185 BYPASS VALVE BENDIX 23057344 BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL FUEL CONTROL STUCK W K NONE O OTHER IN INSP/MAINT 1 CA 2324 322185 CAE832831 (CAN) UNABLE TO ADJUST START CYCLE COMPRESSOR STALLING AND FAST EXCELLERATION OF N1 RPM NOTED AT 20 PER N1 FUEL PRESSUR E WAS NOTED AS HIGH AS +30 PSI. POSSIBLE BYPASS VALVE STUCK OPEN. REPLACED. 1 G 7 1 3U 3 U H2SW E4CE 1998042300001 19980423 00001 NM 1998 4 23 HNAA9698948 1 19960712 A 2611 CONNECTORS DHAV DHC8 DHC8201 2809001 NM BAGG COMPT DIRTY A HNAA K NONE J WARNING INDICATION CR CRUISE 1 EA 07 989HA 427 TLH/TPA - FLT 3421 - DURING FLIGHT, THE SMOKE WARNING LIGHT AND MASTER WARNING LIGHT CAME ON IN-FLIGHT. LIGHT WENT OUT AFTER 10 MINUTES, CAME BACK ON, AND WENT OUT AFTER LANDING. REMOVED AND CLEANED CANNON PLUGS ON BOTH DETECTORS AFT OF C ARGO COMPARTMENT. (X) 2 H 7 2 4T RT A13NM 1998042300002 19980423 00002 CE 1998 4 23 GLBA96149 1 19960711 A 3297 WIRE BEECH 1900 1900D 1154162 CE LANDING GEAR CHAFED A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 01 211UX UE211 BIS - GEAR WILL NOT RETRACT. MAINTENANCE REPAIRED CHAFED WIRE LOCATED ONE FOOT AFT OF P522. GEAR SWING CHECK GOOD. (X ) 2 L 7 2 4T RT A24CE 1998042300003 19980423 00003 CE 1998 4 23 GLBA96145 1 19960708 A 3246 BEARING BEECH 1900 1900D 1154162 CE RT MLG FAILED A GLBA A UNSCHED LANDING D INFLIGHT SEPARATION TO TAKEOFF 1 CE 01 211UX UE211 BIS - RIGHT OUTBOARD TIRE FELL OFF ON TAKEOFF. AIR TURN-BACK AND MAINTENANCE INSPECTED RIGHT HAND MAIN LANDING GEAR FOR OBVIOUS DAMAGE TO WHEELWELL, WINGS AND FLAPS. REMOVED BOTH RIGHT GEAR BRAKE ASSEMBLIES TO INSPECT AXEL. REMOVED INNER BEARING AND FAILED OUTER BEARING FROM AXEL. NO VISUAL DAMAGE NOTED. REINSTALLED BRAKES AND TIRES. RETURNED AIRCRAFT TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1998042300004 19980423 00004 CE 1998 4 23 GLBA96143 1 19960706 A 3234 1013841377 GEAR HANDLE BEECH 1900 1900C 1154161 CE COCKPIT MALFUNCTIONED A GLBA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 CE 01 145GL 177 UC145 PLN - WHEN LEFT ENGINE STARTED AFTER SINGLE ENGINE TURN, GEAR HANDLE WARNING LIGHT AND AURAL WARNING WENT OFF. MAINTENA NCE REPLACED GEAR HANDLE AND PERFORMED NUMEROUS GEAR SWINGS. (X) 2 L 7 2 4T RT A24CE 1998042300005 19980423 00005 NM 1998 4 23 AALA961235 1 19960819 A 3260 31EN946 SENSOR BOEING 757 757223 1384957 NM LT MLG OUT OF ADJUST A AALA K NONE N FALSE WARNING CL CLIMB 1 SW 07 606AA 27057 DFW - FLT 2303 - UPON GEAR RETRACTION, THE AMBER GEAR LIGHT REMAINED ON AND RECEIVED AN EICAS GEAR DISAGREE MESSAGE. RE MAINED ON FOR ABOUT AN HOUR AND 40 MINUTES THEN EXTINGUISHED. LANDED DFW WITHOUT INCIDENT. ADJUSTED LEFT MLG UPLOCK SE NSORS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1998042300006 19980423 00006 NM 1998 4 23 AALA961165 1 19960805 A 2150 470044 FILTER BOEING 757 757223 1384957 NM ACM CONTAMINATED A AALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 07 608AA 27446 SJO - FLT 0984 - AFTER TAKEOFF SJO DURING CLIMB-OUT. LT ENGINE EEC LIGHT ILLUMINATED FOLLOWED BY AUTOTHROTTLES DISCONNEC TING AND SLIGHT ODOR OF SMOKE NOTED IN COCKPIT. THEN THE RT ENGINE EEC LIGHT ILLUMINATED. ACCOMPLISHED SMOKE REMOVAL C HECK LIST AND TURNED OFF BOTH ENGINE EEC'S. ACFT RETURNED TO SJO AND LANDED WITHOUT INCIDENT. ACCOMPLISHED EEC AND BVC U BITE TEST WITH NO FAULTS FOUND. CHECKED AUTOTHROTTLE OPERATION WITH NO DEFECTS FOUND. ACCOMPLISHED GROUND ENGINE RUN AND DETERMINED ODOR COMING FROM LT ENGINE BLEED AIR WITH NO OTHER ABNORMAL INDICATIONS NOTED. AIRCRAFT MAINTENANCE FER RY SJO/DFW. PRECAUTIONARY REPLACED LT EEC CONTROL BOX. ACCOMPLISHED AIR CONDITIONING CONTAMINATION REMOVAL PROCEDURE A 2 L 7 2 4F RT A2NM 1998042300007 19980423 00007 EU 1998 4 23 Y2PA96064 1 19960813 A 7711 S145000000080 EPR SENSE LINE AMD FALC20 FALCON20C5 2730107 EU RT ENGINE LEAKING A Y2PA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 23 826AA 67 ELP - FLT 18389 - TAKEOFF ABORTED WHEN RIGHT ENGINE DID NOT MAKE EPR DURING TAKEOFF ROLL. NO EMERGENCY PROCEDURES REQUI RED. FOUND EPR SENSE HOSE LEAKING IN RIGHT ENGINE NACELLE. A NEW HOSE WAS INSTALLED AND THE ENGINE WAS RUN-UP. A POWE R ASSURANCE CHECK WAS PERFORMED IAW USA JET AIRLINES WORK CARD P001R. NO DEFECTS WERE NOTED. (X) 2 L 7 2 4F RT A7EU 1998042300008 19980423 00008 CE 1998 4 23 96ZZZX4780 1 19960430 A 3260 327 BULB BEECH 1900 1900 1154160 CE LT MLG FAILED A GUUA O OTHER P NO WARNING INDICATION AP APPROACH 1 SO 19 192GA UB17 FLL/ELH - FLT 467 - PILOT REPORT: LEFT MAIN GEAR LIGHT WOULD NOT ILLUMINATE WHEN GEAR IS EXTENDED. NO GEAR HORN OR GEA R UNSAFE LIGHT. LEFT GEAR LIGHT WOULD NOT ILLUMINATE WITH MANUAL EXTENSION. AIRCRAFT DIVERTED TO MIA AND LANDED WITHOU T INCIDENT. PLACED AIRCRAFT ON JACKS, SWUNG GEAR. FOUND LIGHT BULBS BURNED OUT. REMOVED AND REPLACED ALL FOUR BULBS. CYCLED GEAR SEVERAL TIMES. LANDING GEAR INDICATOR OPERATIONAL CHECKS GOOD. (X) 2 L 7 2 4T RT A24CE 1998042300009 19980423 00009 1998 4 23 C2XA96BT007 4 19960806 A 2210 7003975602 CONTROLLER AEROSP ATR42 ATR42320 8680930 EU AUTOPILOT FAILED A A C2XA A UNSCHED LANDING B F J SMOKE/FUMES/ODORS/SPARKS FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 09 86842 286 BTV - FLT 3689 - DURING CLIMB-OUT, AUTOPILOT KICKED OFF AND RECEIVED STICK SHAKER AND OVERSPEED WARNING. COULD NOT TRIM TO LEFT AND ACFT TRIMMED BY ITSELF TO THE RT. COULD NOT RE-TRIM TO LT WITH ONE-HALF AILERON TRIM TO RT. ACFT RETURNED TO BTV AND LANDED UNEVENTFULLY. FOUND FLT GUIDANCE CONTROLLER FAULTING. REMOVED AND REPLACED FGC IAW 22-16-81. OPS C HECKED GOOD. EWR - FLT 4211 - AFTER TAKEOFF, CREW NOTED SAME PROBLEM PLUS THE SMELL OF ELECTRICAL SMOKE ON LANDING WHIL E RETURNING TO EWR. REMOVED AND REPLACED FGC IAW ATR 42 MM 22-16-81, OPS CHECKED GOOD ON GROUND. ALL OTHER DISCREPANCI ES WERE FOUND OPERATING NORMALLY. ACFT RELEASED FOR TEST FLIGHT. NO FLIGHT DISCREPANCIES NOTED AND ACFT RELEASED TO 2 H 7 2 4T RT A53EU 1998042300010 19980423 00010 EA 1998 4 23 96ZZZX4781 2 19960807 A 7200 ENGINE 3024700 SKRSKY S58T S58ET 8141803 NE PWA PT6T PT6T6 52045 EA COMPRESSOR STALLS A NYBA K NONE R PARTIAL RPM/PWR LOSS IN INSP/MAINT 1 EA 11 129NH 10638 1722 CPPS72085 58855 DURING HIGH POWER DEMANDS, COMPRESSOR STALLS NOTED BY PILOT. DURING ACCELERATION CHECKS ON GROUND, MECHANIC NOTED COMPR ESSOR STALLS. NYH BELIEVES THE COMPRESSOR STALLS ARE DUE TO DAMAGED 1ST STAGE COMPRESSOR BLADES (FOD). POWER SECTION R EMOVED IAW S58T MM AND SHIPPED TO VENDOR FOR EVALUATION AND REPAIR. 2 G 7 2 4U 4 U 1H11 E22EA 1998042300042 19980423 00042 NM 1998 4 23 CALA9601501 1 19961003 A 5311 FRAME BOEING 727 727243 138408D NM BS 970 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 579PE 21662 INSPECTION FOUND STRINGER 29R AND FRAME CORRODED AT STA 970. THE CORROSION WAS REMOVED FROM STRINGER AND FRAME IAW SRM 51-10-6. THE AREA WAS REPAIRED IAW SRM 53-10-4. 2 L 7 3 4F RT A3WE 1998042300043 19980423 00043 NM 1998 4 23 CALA9601502 1 19961003 A 5313 STRINGER BOEING 727 727243 138408D NM BS 940 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 579PE 21662 INSPECTION FOUND A 1.125 INCH CRACK IN STRINGER 18A OUTBOARD FLANGE AT LT SIDE AFT OF BS 940 FRAME. THE CRACK WAS STOP DRILLED, REPAIR PARTS WERE FABRICATED AND INSTALLED IAW ECRA 5310-03340, SRM 51-10-00 AND BOEING DRAWING 65C27166. 2 L 7 3 4F RT A3WE 1998042300044 19980423 00044 NM 1998 4 23 CALA9601503 1 19961011 A 5522 SKIN BOEING 727 727243 138408D NM RT ELEVATOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 579PE 21662 INSPECTION FOUND INBOARD UPPER SKIN TRAILING EDGE OF RIGHT ELEVATOR DENTED. A REPAIR DOUBLER WAS FABRICATED AND INSTALL ED IAW SRM 55-20-3, FIGURE 5. 2 L 7 3 4F RT A3WE 1998042300045 19980423 00045 EU 1998 4 23 WWMA9600087 1 19961022 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT DEFECTIVE A WWMA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 WP 15 286AE 340B286 CARGO SMOKE LIGHT CAME ON AND WOULD NOT GO OUT AFTER LANDING. MAINTENANCE REPLACED THE FORWARD CARGO SMOKE DETECTOR. 2 L 7 2 4T RT A52EU 1998042300046 19980423 00046 EU 1998 4 23 WWMA9600086 1 19960902 A 2150 7769105 ACM SAAB SF340 340B 7860101 EU RIGHT SEIZED A WWMA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 15 329AE 8087 340B329 CREW REPORTED, THAT THE RIGHT AIR CYCLE MACHINE ONLY BLOWS HEAT, SMELLED AN ELECTRICAL SMELL WITH BLEEDS ON AND PASSENG ERS REPORTED A GRINDING SOUND IN THE BACK OF THE AIRCRAFT. MAINTENANCE FOUND THE RIGHT AIR CYCLE MACHINE SEIZED. REPLA CED THE RIGHT ACM AND RETURNED THE AIRCRAFT TO SERVICE WITH NO FURTHER PROBLEMS. 2 L 7 2 4T RT A52EU 1998042300047 19980423 00047 SO 1998 4 23 SRAA961012 1 19961015 A 5753 TRACK LKHEED 382 382G 526414U SO RT TE FLAP CRACKED A SRAA K NONE O OTHER IN INSP/MAINT 1 GL 23 918SJ 4208 DURING WALK AROUND INSPECTION, FOUND ON RIGHT WING O/B FLAP VERTICAL BEAM I/B TRACK CRACKED FROM LOWER WING SURFACE AND TRAVELS UPWARD APPROX 50 PERCENT OF VERT FITT, SIMILAR CRACK WAS FOUND ON LEFT WING I/B FLAP O/B TRACK. ALSO, FOUND THE LT O/B TRACK FORMER ASS'Y CRACKED. PERFORMED INTERIM REPAIR TO THE RIGHT WING O/B FLAP VERT BEAM, FOUND CRACKS ON THE LEFT I/B AND O/B FLAP TRACKS LESS SEVERE, INSPECTED AIRCRAFT AND FOUND SAFE FOR FLAP UP FERRY TO 31J FOR PERMANENT REPAI R. AIRCRAFT REACHED DISTINATION AND LANDED WITHOUT INCIDENT. 2 H 7 4 4T A1SO 1998042300048 19980423 00048 NM 1998 4 23 96UAL900812 1 19961014 A 3350 LIGHT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7252U 21399 AFT AIRSTAIR EMERGENCY LIGHT INOPERABLE. REPLACED EMERGENCY LIGHT PER MM 33-50-21, OPERATIONS CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1998042300049 19980423 00049 1998 4 23 96UAL900814 4 19961015 A 2565 BULKHEAD AIR CRUISERS 24D3005193 DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE EXCAPE SLIDE FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 1858U 1557 46987 DURING TIME CONTROLLED OVERHAUL, RAMP PORTION OF SLIDE SUFFERED INTERNAL BULKHEAD FAILURE. ALSO, LT RAMP RAIL, LOWER EN D SUFFERED INTERNAL BULKHEAD FAILURE. SCRAPPED RAMP PORTION OF SLIDE. 2 L 7 3 4F 4 F A22WE E23EA 1998042300050 19980423 00050 1998 4 23 96UAL900815 4 19961015 A 2565 INFLATE TUBE BFGOODRICH D29835103 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE EXCAPE SLIDE SEPARATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7263U 17590678 21410 DURING TIME CONTROLLED OVERHAUL, SLIDE SUFFERED SEAM SEPARATION OF THE INFLATION TUBE. SCRAPPED UNIT. 2 L 7 3 4F 4 F A3WE E2EA 1998042300051 19980423 00051 NM 1998 4 23 96UAL900818 1 19961018 A 3350 BATTERIES BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7283U 21561 EMERGENCY ILLUMINATION LIGHT AT ROW 8 INOP. REPLACED BATTERIES, OPS CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1998042300053 19980423 00053 NM 1998 4 23 96UAL900820 1 19961018 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 649UA 25286 FLOOR EMERGENCY LIGHT AT SEAT 11 ON RIGHT SIDE INOPERABLE. REPLACED FLOOR EMERGENCY LIGHT, OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 1998042300055 19980423 00055 NE 1998 4 23 96ZZZX5353 2 19960930 A 7261 3030391 OIL PUMP CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE LT ENG SCAV WEAK A FRKA K NONE O OTHER IN INSP/MAINT 1 NE 01 245CC 3241 550212 71131 LEFT ENGINE SHOWED EVIDENCE OF HIGH OIL CONSUMPTION. TROUBLESHOOTING REVEALED WEAK SCAVENGE OIL PUMP. OIL PUMP WAS REM OVED AND REPLACED WITH OVERHAULED UNIT AND OPERATION RETURNED TO NORMAL. 1 L 7 2 4F 4 F A22CE E1NE 1998042300069 19980423 00069 NM 1998 4 23 P5CA9601107 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 2040 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION UNDER SEALING ON STRINGER 20 AT AREA WINDOW FRAME NEAR STA 2040 RT. CORROSION REMOVED AND AREA TREATED PER SR M 51-10-01. 2 L 7 4 4F A20WE 1998042300070 19980423 00070 NM 1998 4 23 P5CA9601108 1 19960812 A 5330 SKIN BOEING 747 747121 1384871 NM BS 2100-2120 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON THE SKIN UNDER SEALING AT STRINGER 19 LAP JOINT BETWEEN STA 2100 TO 2120 RT SIDE. CORROSION REMOVED AND AR EA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998042300071 19980423 00071 NM 1998 4 23 P5CA9601109 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1540 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STRINGER 1 LT NEAR STA 1540. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998042300072 19980423 00072 NM 1998 4 23 P5CA9601110 1 19960812 A 5320 TIE CLIP BOEING 747 747121 1384871 NM BS 1920 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON TIE CLIP AT STA 1920 BETWEEN STRINGER 2 TO 3. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998042300073 19980423 00073 NM 1998 4 23 P5CA9601111 1 19960812 A 5320 TIE CLIP BOEING 747 747121 1384871 NM BS 1940 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON TIE CLIP AT STA 1940 NEAR STRINGER 1 RT. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998042300074 19980423 00074 NM 1998 4 23 P5CA9601112 1 19960812 A 5320 TIE CLIP BOEING 747 747121 1384871 NM BS 1960 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON TIE CLIP AT STA 1960 NEAR STRINGER 2 RT. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998042300075 19980423 00075 NM 1998 4 23 P5CA9601113 1 19960812 A 5311 FRAME BOEING 747 747121 1384871 NM BS 2020 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON FRAME LWR CHORD AREA AT STA 2020 BETWEEN STRINGER 7 TO 8 LT. CORROSION REMOVED AND AREA TREATED PER SRM 51 -10-01. 2 L 7 4 4F A20WE 1998042300076 19980423 00076 NM 1998 4 23 P5CA9601114 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 2140 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STRINGER 1 AT STA 2140 LT SIDE. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998042300077 19980423 00077 NM 1998 4 23 P5CA9601115 1 19960812 A 5320 TIE CLIP BOEING 747 747121 1384871 NM BS 2160 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON TIE CLIP AT STA 2160 NEAR STRINGER 11 LT. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998042300078 19980423 00078 NM 1998 4 23 P5CA9601116 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 2060 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STA 2060 LT SIDE AT STRINGER 26 AREA. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998042300079 19980423 00079 NM 1998 4 23 P5CA9601117 1 19960812 A 5320 TIE CLIP BOEING 747 747121 1384871 NM BS 1780 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON TIE CLIP OF STRINGER 3 RT AT STA 1780. CORROSION REMOVED PER SRM 51-10-01, FOUND WITHIN THE LIMITS PER SRM 53-10-01. 2 L 7 4 4F A20WE 1998042300080 19980423 00080 NM 1998 4 23 P5CA9601118 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1780-1800 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STRINGER 49 RT SIDE AND STRINGER 46, 51 LT SIDE BETWEEN STA 1780 TO 1800. CORROSION REMOVED AND AREA TREAT ED PER SRM 51-10-01, FOUND WITHIN LIMITS PER SRM 53-10-01. 2 L 7 4 4F A20WE 1998042300081 19980423 00081 NM 1998 4 23 P5CA9601119 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1760-1780 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STRINGER 48 TO 49 RT SIDE AND STRINGER 46 TO 51 LT SIDE BETWEEN STA 1760 TO 1780. CORROSION REMOVED AND AR EA TREATED PER SRM 51-10-01, FOUND WITHIN LIMITS PER SRM 53-10-01. 2 L 7 4 4F A20WE 1998042300082 19980423 00082 NM 1998 4 23 P5CA9601120 1 19960812 A 5320 INTERCOSTAL BOEING 747 747121 1384871 NM BS 1760-1780 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON FLOOR INTERCOSTAL BETWEEN STA 1760 TO 1780 AT RBL 42 AREA. CORROSION REMOVED AND AREA TREATED PER SRM 51-1 0-01, FOUND WITHIN LIMITS PER SRM 53-10-01. 2 L 7 4 4F A20WE 1998042300083 19980423 00083 NM 1998 4 23 P5CA9601121 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1740-1760 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STRINGER 44 TO 45 RT SIDE AND STRINGER 46 LT SIDE BETWEEN STA 1740 TO 1760. CORROSION REMOVED AND AREA TRE ATED PER SRM 51-10-01 WITHIN LIMITS PER SRM 53-10-01. 2 L 7 4 4F A20WE 1998042300084 19980423 00084 NM 1998 4 23 P5CA9601122 1 19960812 A 5320 TIE CLIPS BOEING 747 747121 1384871 NM BS 2140-2160 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON TIE CLIPS AT STA 2140 AND 2160 IN STRINGER 4, 5 RT. CORROSION REMOVED PER SRM 51-10-01, FOUND WITHIN THE L IMITS PER SRM 53-10-01. 2 L 7 4 4F A20WE 1998042300085 19980423 00085 NM 1998 4 23 P5CA9601123 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 2220 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STRINGER 7 RT AT STA 2220. CORROSION REMOVED PER SRM 51-10-01, FOUND WITHIN LIMITS PER SRM 53-10-01. 2 L 7 4 4F A20WE 1998042300086 19980423 00086 NM 1998 4 23 P5CA9601124 1 19960812 A 5320 SUPPORT BOEING 747 747121 1384871 NM BS 1060 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON FAIRING SUPPORT LWR FUS AT STA 1060 BETWEEN AREA RBL TO LBL 105. FAB NEW SUPPORT FAIRING PER SRM 51-40-04. 2 L 7 4 4F A20WE 1998042300087 19980423 00087 NM 1998 4 23 P5CA9601125 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1820 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON FRAME AT STA 1820 NEAR STRINGER 7 RT. CORROSION REMOVED PER SRM 51-10-01, FOUND WITHIN THE LIMITS PER SRM 53-10-01. 2 L 7 4 4F A20WE 1998042300088 19980423 00088 NM 1998 4 23 P5CA9601126 1 19960812 A 5311 FRAME BOEING 747 747121 1384871 NM BS 1860 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON FRAME LWR CHORD AT STA 1860 NEAR STRINGER 7. CORROSION REMOVED PER SRM 51-10-01, FOUND WITHIN THE LIMITS P ER SRM 53-10-01. 2 L 7 4 4F A20WE 1998042300089 19980423 00089 NM 1998 4 23 P5CA9601127 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1880-1900 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STRINGER 7 RT BETWEEN STA 1880 TO 1900. CORROSION REMOVED PER SRM 51-10-01, FOUND WITHIN THE LIMITS PER SR M 53-10-01. 2 L 7 4 4F A20WE 1998042300090 19980423 00090 NM 1998 4 23 P5CA9601128 1 19960812 A 5320 TIE CLIPS BOEING 747 747121 1384871 NM BS 1920 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON TIE CLIPS AT STA 1920 COND STRINGER 3, 11 RT. CORROSION REMOVED PER SRM 51-10-01, FOUND WITHIN THE LIMITS PER SRM 53-10-01. 2 L 7 4 4F A20WE 1998042300091 19980423 00091 NM 1998 4 23 P5CA9601129 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 2100 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON FRAME AT STA 2100 NEAR STRINGER 3. CORROSION REMOVED PER SRM 51-10-01, FOUND WITHIN LIMITS PER SRM 53-10-0 1. 2 L 7 4 4F A20WE 1998042300092 19980423 00092 NM 1998 4 23 P5CA9601130 1 19960812 A 5330 SKIN BOEING 747 747121 1384871 NM BS 1560-1620 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON INTERNAL SKIN BETWEEN STA 1560 TO 1620 AND BETWEEN STRINGER 3 TO 4 RT. CORROSION REMOVED PER SRM 51-10-01, FOUND WITHIN LIMITS PER SRM 53-10-01. 2 L 7 4 4F A20WE 1998042300093 19980423 00093 NM 1998 4 23 P5CA9601131 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1620-1640 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STRINGER 1, 2, 8 RT BETWEEN STA 1620 TO 1640. REPAIRED PER SRM 51-10-03. 2 L 7 4 4F A20WE 1998042300094 19980423 00094 NM 1998 4 23 P5CA9601132 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1760 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STRINGER 11 RT AT STA 1760 AND ON HEAD OF HI-LOCK AT STRINGER 1 LT TO 2 RT. CORRISION REMOVED AND TREATED PER SRM 51-10-01 AND 51-30-02. 2 L 7 4 4F A20WE 1998042300095 19980423 00095 NM 1998 4 23 P5CA9601133 1 19960812 A 5315 FLOORBEAM BOEING 747 747121 1384871 NM BS 940 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON UPPER CHORD FLOORBEAM AT STA 940 BETWEEN AREA LBL 32 TO 45. CORROSION REMOVED AND AREA TREATED PER SRM 51- 10-01. 2 L 7 4 4F A20WE 1998042300096 19980423 00096 NM 1998 4 23 P5CA9601134 1 19960812 A 5321 FLOOR BOEING 747 747121 1384871 NM BS 860-880 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 HITS AND CORROSION ON SHEET METAL FLOOR COVER BETWEEN STA 860 TO 880 BETWEEN AREA LBL TO RBL 58. AREA SMOOTHED, CORROSI ON REMOVED AND TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998042300097 19980423 00097 NM 1998 4 23 P5CA9601135 1 19960812 A 5751 HINGE CUTOUT BOEING 747 747121 1384871 NM RT AILERON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 RT OUTBD AILERON OUTBD HINGE UPPER CUTOUT CRACKED. CUTOUT REWORKED PER SRM 57-10-01, DAMAGE WITHIN THE LIMIT PER SRM 57 -10-01. 2 L 7 4 4F A20WE 1998042300098 19980423 00098 NM 1998 4 23 P5CA9601136 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1780-1800 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STRINGER 39 BETWEEN STA 1780 TO 1800 LT SIDE. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01, FOUND W ITHIN LIMITS PER SRM 53-10-01. 2 L 7 4 4F A20WE 1998042300099 19980423 00099 NM 1998 4 23 P5CA9601137 1 19960812 A 5280 SKIN BOEING 747 747121 1384871 NM NLG DOOR DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 NOSE LANDING GEAR W/W RT FWD DOOR HAS DENTS ON INNER SKIN SURFACE. REPAIRED PER SRM 53-10-23 AND 51-30-02. 2 L 7 4 4F A20WE 1998042300100 19980423 00100 NM 1998 4 23 P5CA9601138 1 19960812 A 5330 SKIN BOEING 747 747121 1384871 NM BS 1720-1740 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON THE SKIN BETWEEN STA 1720 TO 1740 AND BETWEEN STRINGER 48 TO 49 RT SIDE AND BETWEEN STRINGER 51 RT TO STRIN GER 51 LT. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01 AND 53-10-01. 2 L 7 4 4F A20WE 1998042300101 19980423 00101 NM 1998 4 23 P5CA9601139 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1720-1740 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STRINGER 44, 48, 49 AND 51 RT SIDE AND STRINGER 51 LT SIDE BETWEEN STA 1720 TO 1740. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01, FOUND WITHIN LIMITS PER SRM 53-10-01. 2 L 7 4 4F A20WE 1998042300102 19980423 00102 NM 1998 4 23 P5CA9601140 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1680-1700 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STRINGER 42 BETWEEN STA 1680 TO 1700 LT SIDE. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01, FOUND W ITHIN LIMITS PER SRM 53-10-01. 2 L 7 4 4F A20WE 1998042300103 19980423 00103 NM 1998 4 23 P5CA9601141 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1700-1720 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STRINGER 51 LT SIDE BETWEEN STA 1700 TO 1720. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01, FOUND W ITHIN LIMITS PER SRM 53-10-01. 2 L 7 4 4F A20WE 1998042300104 19980423 00104 NM 1998 4 23 P5CA9601142 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1800-1820 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STRINGER 49 AND 51 RT SIDE AND STRINGER 47, 48, 49, 50 LT SIDE BETWEEN STA 1800 TO 1820. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01, FOUND WITHIN LIMITS PER SRM 53-10-01. 2 L 7 4 4F A20WE 1998042300105 19980423 00105 NM 1998 4 23 P5CA9601143 1 19960812 A 5315 FLOORBEAM BOEING 747 747121 1384871 NM BS 1800 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON UPPER CHORD FLOORBEAM AT STA 1800 AREA RBL AND LBL 30 TO 45. CORROSION REMOVED AND AREA TREATED PER SRM 51 -10-01, FOUND WITHIN LIMITS PER SRM 53-10-01. 2 L 7 4 4F A20WE 1998042300106 19980423 00106 NM 1998 4 23 P5CA9601144 1 19960812 A 5315 FLOORBEAM BOEING 747 747121 1384871 NM BS 1700 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON UPPER CHORD FLOORBEAM AT STA 1700 BETWEEN AREA RBL 35 TO 45. CORROSION REMOVED AND AREA TREATED PER SRM 51 -10-01. 2 L 7 4 4F A20WE 1998042300107 19980423 00107 NM 1998 4 23 P5CA9601145 1 19960812 A 5330 SKIN BOEING 747 747121 1384871 NM BS 1680-1700 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON THE SKIN BETWEEN STRINGER 48 TO 49 AND BETWEEN STA 1680 TO 1700 RT SIDE. CORROSION REMOVED AND AREA TREATE D PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998042300108 19980423 00108 NM 1998 4 23 P5CA9601146 1 19960812 A 5245 DOOR BOEING 747 747121 1384871 NM AC COMPT CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 AIR CONDITION BAY DOORS HINGE SUPPORTS ARE CORRODED LT DOORS. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998042300109 19980423 00109 NM 1998 4 23 P5CA9601147 1 19960812 A 5315 FLOORBEAM BOEING 747 747121 1384871 NM BS 1540 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON UPPER CHORD FLOORBEAM STA 1540 BETWEEN AREA RBL 35 TO 45. CORROSION REMOVED AND AREA TREATED PER SRM 51-10 -01. 2 L 7 4 4F A20WE 1998042300110 19980423 00110 NM 1998 4 23 P5CA9601148 1 19960812 A 5320 DOUBLER BOEING 747 747121 1384871 NM BS 1480 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON DOUBLER AT SHEET METAL COVER NEAR STA 1480 AT RBL 6. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998042300111 19980423 00111 NM 1998 4 23 P5CA9601149 1 19960812 A 5320 STRAP BOEING 747 747121 1384871 NM BS 1780-1800 BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 BROKEN STRAP ON INTERCOSTAL AT CARGO FLOOR BETWEEN STA 1780 TO 1800 RT SIDE ABOVE STRINGER 42. FAB NEW STRAP INST AND R IVETED PER SRM 51-40-02. 2 L 7 4 4F A20WE 1998042300112 19980423 00112 NM 1998 4 23 P5CA9601150 1 19960812 A 5311 FRAME BOEING 747 747121 1384871 NM BS 1800-1820 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION AND HITS ON AFT ENTRY CARGO FRAME BETWEEN STA 1800 TO 1820 RT ABOVE STRINGER 36 TO 40. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998042300113 19980423 00113 NM 1998 4 23 P5CA9601151 1 19960812 A 5320 CHORD BOEING 747 747121 1384871 NM BS 1480 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON UPPER CHORD STA 1480, UNDER MAIN DECK FLOOR BETWEEN AREA LBL TO RBL 25. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998042300114 19980423 00114 NM 1998 4 23 P5CA9601152 1 19960812 A 5320 TIE CLIPS BOEING 747 747121 1384871 NM BS 1660 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 SMALL CRACK AND BENT ON CLIPS AT STA 1660 LT SIDE BETWEEN STRINGER 35 TO 37. AREA REPAIRED PER SRM 51-40-04. 2 L 7 4 4F A20WE 1998042300115 19980423 00115 NM 1998 4 23 P5CA9601153 1 19960812 A 5320 RIVET BOEING 747 747121 1384871 NM BS 1660 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CRACK AND SHEARED RIVET ON STA 1660 LT SIDE ABOVE STRINGER 34. AREA REPAIRED PER SRM 51-40-02. 2 L 7 4 4F A20WE 1998042300116 19980423 00116 NM 1998 4 23 P5CA9601154 1 19960812 A 5320 RIVET BOEING 747 747121 1384871 NM BS 1680 CRACKING A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CRACK AND SHEARED RIVET ON INTERCOSTAL AT STRINGER 34 NEAR STA 1680 LT SIDE. AREA REPAIRED PER SRM 51-40-02. 2 L 7 4 4F A20WE 1998042300117 19980423 00117 NM 1998 4 23 P5CA9601155 1 19960812 A 5320 CLIP BOEING 747 747121 1384871 NM BS 1800 BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 BROKEN CLIP ON STA 1800 LT SIDE BETWEEN STRINGER 36 TO 37. NEW CLIP INST PER SRM 51-40-04. 2 L 7 4 4F A20WE 1998042300118 19980423 00118 NM 1998 4 23 P5CA9601156 1 19960812 A 5315 FLOORBEAM BOEING 747 747121 1384871 NM BS 960 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON UPPER CHORD FLOORBEAM AT STA 960 BETWEEN AREA RBL AND LBL 32 TO 45. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998042300119 19980423 00119 NM 1998 4 23 P5CA9601157 1 19960812 A 5310 STRUCTURE BOEING 747 747121 1384871 NM AC COMPT CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON LT AIR CONDITION DOOR SUPPORT STRUCTURE STA 1040. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998042300120 19980423 00120 NM 1998 4 23 P5CA9601158 1 19960812 A 5320 ANGLE BOEING 747 747121 1384871 NM BS 940-960 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON FLOOR ANGLE BETWEEN STA 940 TO 960 BETWEEN AREA RBL 32 TO 45. CORROSION REMOVED AND AREA TREATED PER SRM 5 1-10-01. 2 L 7 4 4F A20WE 1998042300121 19980423 00121 NM 1998 4 23 P5CA9601159 1 19960812 A 5315 FLOORBEAM BOEING 747 747121 1384871 NM BS 920 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON UPPER CHORD FLOORBEAM AT STA 920 BETWEEN AREA LBL AND RBL 32 TO 45. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998042300122 19980423 00122 NM 1998 4 23 P5CA9601160 1 19960812 A 5315 FLOORBEAM BOEING 747 747121 1384871 NM BS 1720 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON UPPER CHORD FLOORBEAM AT STA 1720 BETWEEN AREA LBL 32 TO 45. CORROSION REMOVED AND AREA TREATED PER SRM 51 -10-01. 2 L 7 4 4F A20WE 1998042300123 19980423 00123 NM 1998 4 23 P5CA9601161 1 19960812 A 5330 SKIN BOEING 747 747121 1384871 NM BS 1740-1760 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON THE SKIN BETWEEN STRINGER 41 TO 42 AND BETWEEN STA 1740 TO 1760. CORROSION REMOVED AND AREA TREATED PER S RM 51-10-01. 2 L 7 4 4F A20WE 1998042300124 19980423 00124 NM 1998 4 23 P5CA9601162 1 19960812 A 5320 WEB BOEING 747 747121 1384871 NM BS 1800 TORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 TEAR ON THE WEB AT STA 1800 UNDER UPPER CHORD AT AREA LBL 48. AREA REPAIRED PER SRM 51-40-02. 2 L 7 4 4F A20WE 1998042300125 19980423 00125 NM 1998 4 23 P5CA9601164 1 19960812 A 5314 KEEL BEAM BOEING 747 747121 1384871 NM FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON KEEL BEAM OUTER STRINGERS ABOVE RT A/C BAY DOORS. REMOVED CORROSION AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998042300126 19980423 00126 NM 1998 4 23 P5CA9601165 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1220-1240 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STRINGER 4 LT BETWEEN STA 1220 TO 1240. REPAIRED STRINGER PER SRM 53-10-03. 2 L 7 4 4F A20WE 1998042300127 19980423 00127 NM 1998 4 23 P5CA9601166 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1180-1200 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STRINGER 7, 9 LT BETWEEN STA 1180 TO 1200. CORROSION REMOVED PER SRM 51-10-01, FOUND WITHIN LIMITS PER SRM 53-10-01. 2 L 7 4 4F A20WE 1998042300128 19980423 00128 NM 1998 4 23 P5CA9601167 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1160-1180 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STRINGER 8, 10 BETWEEN STA 1160 TO 1180. CORROSION REMOVED PER SRM 51-10-01, FOUND WITHIN LIMITS PER SRM 5 3-10-01. 2 L 7 4 4F A20WE 1998042300129 19980423 00129 NM 1998 4 23 P5CA9601168 1 19960812 A 5320 CHORD BOEING 747 747121 1384871 NM BS 1920 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CRACK ON STA 1920 AT UPPER CHORD AREA ABOVE STRINGER 42 LT. AREA REPAIRED PER SRM 53-10-04. 2 L 7 4 4F A20WE 1998042300130 19980423 00130 NM 1998 4 23 P5CA9601169 1 19960812 A 5320 INTERCOSTAL BOEING 747 747121 1384871 NM BS 1960-1980 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON INTERCOSTAL AND STRINGER 44, BETWEEN STA 1960 TO 1980 RT SIDE. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01, FOUND WITHIN LIMITS PER SRM 53-10-01. 2 L 7 4 4F A20WE 1998042300131 19980423 00131 NM 1998 4 23 P5CA9601170 1 19960812 A 5314 KEEL BEAM BOEING 747 747121 1384871 NM BS 1080-1100 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON LWR SIDE OF VERTICAL SUPPORT AT KEEL BEAM WALL LT SIDE ABOVE DOOR 5 LWR FUS BETWEEN STA 1080 TO 1100 MARKED . CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998042300132 19980423 00132 NM 1998 4 23 P5CA9601171 1 19960812 A 5330 SKIN BOEING 747 747121 1384871 NM BS 2120 CHAFED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CHAFING ON LWR FUSELAGE SKIN RT SIDE NEAR STA 2120 BETWEEN STRINGER 48 TO 49. STRAIGHTEN AND SMOOTHED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998042300133 19980423 00133 NM 1998 4 23 P5CA9601172 1 19960812 A 5730 SKIN BOEING 747 747121 1384871 NM WS 680 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 SWELLING ON UPPER WING SKIN AT STA 680 IN FRONT SPAR AREA. REMOVED CORROSION AND FASTENERS PER SRM 51-10-01, INSTALLED NEW RIVETS. 2 L 7 4 4F A20WE 1998042300134 19980423 00134 NM 1998 4 23 P5CA9601173 1 19960812 A 5330 SKIN BOEING 747 747121 1384871 NM WS 2360 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION AND SHEARED RIVET ON FUSELAGE SKIN RT SIDE STA 2360 BETWEEN STRINGER 18 TO 23. CLEANED CORROSION AND TREATED PER SRM 51-10-01, NEW FASTENERS PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998042300135 19980423 00135 NM 1998 4 23 P5CA9601174 1 19960812 A 5330 SKIN BOEING 747 747121 1384871 NM BS 2360 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 SURFACE CORROSION ON FUSELAGE SKIN LT SIDE STA 2360 AT STRINGER 23 AREA. CLEANED CORROSION AND TREATED PER SRM 51-10-01 . 2 L 7 4 4F A20WE 1998042300136 19980423 00136 NM 1998 4 23 P5CA9601175 1 19960812 A 5315 FLOORBEAM BOEING 747 747121 1384871 NM BS 820-860 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CRACKS W/STOP HOLE AND SHEARED, LOOSE RIVETS ON SHEET METAL COVER, UNDER FLOORBEAM BETWEEN STA 820 TO 860 BETWEEN AREA R BL 6 TO 25. REPAIRED SHEET METAL COVER PER SRM 51-40-02 AND SRM 51-30-02. 2 L 7 4 4F A20WE 1998042300137 19980423 00137 NM 1998 4 23 P5CA9601176 1 19960812 A 5753 CARRIAGE BOEING 747 747121 1384871 NM TE FLAPS CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 WING FLAP CARRIAGES 8 BOOGIES SURFACE CORROSION. REMOVED SURFACE CORROSION PER SRM 51-10-01 AND PROTECTION ACTION CARRI ED OUT. 2 L 7 4 4F A20WE 1998042300138 19980423 00138 NM 1998 4 23 P5CA9601177 1 19960812 A 5720 FITTING BOEING 747 747121 1384871 NM RT WING CRACKING A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 RT WING CRACKED UNDERWING FITTING OF FWD SKIRT ROD ATT, AFT OF DUAL SIDE STRUT FITTING OF NR 3 PYLON. MUST BE REPAIRED BEFORE INST NEW FITTING (P/N 69B12302-6) AND RIVETED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998042300139 19980423 00139 NM 1998 4 23 P5CA9601178 1 19960812 A 5720 BRACKET BOEING 747 747121 1384871 NM WS 669.5 BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 BROKEN SUPPORT BRACKET OF ENG NR 2 FAIRING NEAR FRONT SPAR LEADING EDGE AT STA 669.50 AREA. FAB NEW SUPPORT BRACKET PER OLD BRACKET, RIVETED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998042300140 19980423 00140 NM 1998 4 23 P5CA9601179 1 19960812 A 5320 BRACKET BOEING 747 747121 1384871 NM BS 1000 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CRACK ON BRACKET ON STA 1000 LT SIDE BETWEEN STRINGER 16 TO 17. INSTALLED NEW BRACKET/7075-T6 AND RIVETED PER SRM 51-30 -02. 2 L 7 4 4F A20WE 1998042300141 19980423 00141 NM 1998 4 23 P5CA9601180 1 19960812 A 5320 ANGLE BOEING 747 747121 1384871 NM BS 2240 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON ANGLES NEAR STA 2240 LT SIDE AT STRINGER 26 AREA FLOOR. CORROSION REMOVED PER SRM 51-10-01, FOUND WITHIN L IMITS PER SRM 53-10-01. 2 L 7 4 4F A20WE 1998042300142 19980423 00142 NM 1998 4 23 P5CA9601181 1 19960812 A 5311 FRAME BOEING 747 747121 1384871 NM BS 2100 CRACKING A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CRACK ON STA 2100 RT SIDE BETWEEN STRINGER 22 TO 23. PERFORMED REPAIR ON FRAME PER SRM 51-40-03. 2 L 7 4 4F A20WE 1998042300143 19980423 00143 NM 1998 4 23 P5CA9601182 1 19960812 A 5320 ANGLE BOEING 747 747121 1384871 NM BS 1660 BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 BROKEN ANGLE AND MISSING COLLAR ON HI-LOCK RIVET AT FRAME NEAR STA 1660 LT SIDE AT STRINGER 15 AREA. INSTALLED NEW ANGL E AND RIVETED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998042300144 19980423 00144 NM 1998 4 23 P5CA9601183 1 19960812 A 5311 FRAME BOEING 747 747121 1384871 NM BS 1620 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON FRAME AT STA 1620 BETWEEN STRINGER 1 TO2 LT. REPAIRED PER SRM 53-10-03. 2 L 7 4 4F A20WE 1998042300145 19980423 00145 NM 1998 4 23 P5CA9601184 1 19960812 A 5320 INTERCOSTAL BOEING 747 747121 1384871 NM BS 2120-2140 CORRODED A P5CA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION, HIT AND RIVETS IMPROPERLY DRIVEN ON INTERCOSTAL AT STRINGER 36 BETWEEN STA 2120 TO 2140. CORROSION REMOVED A ND TREATED PER SRM 51-10-01, DAMAGE BLENDED OUT PER SRM 51-40-01 AND NEW RIVET INSTALLED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998042300146 19980423 00146 NM 1998 4 23 P5CA9601185 1 19960812 A 5230 LATCH BOEING 747 747121 1384871 NM CARGO DOOR BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 BROKEN LATCH AND SHEARED RIVETS ON AFTER CARGO DOOR SERVICE PANEL AND SCRATCHES ON FUSELAGE SKIN RT SIDE BETWEEN STA 178 0 TO 1820 AND BETWEEN STRINGER 34 TO 40. INSTALLED NEW LATCH, SMOOTHED SCRATCHES AND AREA TREATED PER SRM 51-30-02 AND 51-10-01. 2 L 7 4 4F A20WE 1998042300147 19980423 00147 NM 1998 4 23 P5CA9601186 1 19960812 A 5330 SKIN BOEING 747 747121 1384871 NM BS 2360 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 SURFACE CORROSION ON LWR FUSELAGE SKIN AT STA 2360 BETWEEN STRINGER 45 RT TO STRING 46 LT SIDE. CORROSION REMOVED AND T REATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998042300148 19980423 00148 NM 1998 4 23 P5CA9601187 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1620 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STRINGER 1 AT STA 1620. REPAIRED PER SRM 53-10-03. 2 L 7 4 4F A20WE 1998042300149 19980423 00149 NM 1998 4 23 P5CA9601188 1 19960812 A 5320 DOORWAY FRAME BOEING 747 747121 1384871 NM BS 2240 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CRACK WITH STOP HOLE ON FRAME ENTRY CARGO DOOR 5 AT STA 2240 AREA LT. PERFORMED REPAIR PER SRM 51-40-02. 2 L 7 4 4F A20WE 1998042300150 19980423 00150 NM 1998 4 23 P5CA9601189 1 19960812 A 5730 SKIN BOEING 747 747121 1384871 NM WS 720 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON UPPER WING SKIN RT AT STA WS 720 STA 20 AREA. CORROSION REMOVED AND TREATED PER SRM 51-10-01, FOUND WITHIN LIMITS PER SRM 57-10-01. 2 L 7 4 4F A20WE 1998042300151 19980423 00151 NM 1998 4 23 P5CA9601190 1 19960812 A 5330 SKIN BOEING 747 747121 1384871 NM BS 660-680 DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 TORN, HITS, SCRATCHES AND DENT ON FUSELAGE SKIN RT SIDE BETWEEN STA 660 TO 680 BETWEEN STRINGER 34 TO 39. PERFORMED REP AIRS PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998042300152 19980423 00152 NM 1998 4 23 P5CA9601191 1 19960812 A 5730 SKIN BOEING 747 747121 1384871 NM WS 625 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 SWELLING ON UPPER WING SKIN RT AT STA 625 IN FRONT SPAR AREA. CORROSION REMOVED AND TREATED PER SRM 51-10-01, RIVET PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998042300153 19980423 00153 NM 1998 4 23 P5CA9601192 1 19960812 A 5330 SKIN BOEING 747 747121 1384871 NM BS 1760 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 SWELLING ON UPPER FUSELAGE SKIN LT SIDE STA 1760 AREA AT STRINGER 3. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-0 1, INSTALLED NEW RIVET PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998042300154 19980423 00154 NM 1998 4 23 P5CA9601193 1 19960812 A 5320 HINGE COVER BOEING 747 747121 1384871 NM BS 2240 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 DENT ON SHEET METAL UPPER HINGE COVER OF PASSENGER DOOR 5 RT AND TORN ON THE SKIN AT DOOR STA 2240. REMOVED SHEET METAL FROM UPPER HINGE AND BLENDED OUT THE TEAR, CLEANED CORROSION AND TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998042300155 19980423 00155 NM 1998 4 23 P5CA9601194 1 19960812 A 5315 FLOORBEAM BOEING 747 747121 1384871 NM BS 440 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CRACK ON WEB AND UPPER CHORD AT FLOORBEAM STA 440 RT SIDE NEAR PASSENGER DOOR-1. UPPER CHORD REPAIRED, WEB REINFORCED P ER SRM 53-10-07. 2 L 7 4 4F A20WE 1998042300156 19980423 00156 NM 1998 4 23 P5CA9601195 1 19960812 A 5730 SKIN BOEING 747 747121 1384871 NM WS 315 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 SWELLING ON UPPER WING SKIN RT AT STA WS 315 IN FRONT SPAR AREA. REMOVED RIVETS AND CLEANED CORROSION PER SRM 51-10-01 AND 51-30-02. 2 L 7 4 4F A20WE 1998042300157 19980423 00157 NM 1998 4 23 P5CA9601196 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 220 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 DEEP HIT AND CORROSION ON STA 220 LT SIDE AT STRINGER 26 AREA. REMOVED CORROSION AND AREA TREATED PER SRM 51-10-01 AND 51-40-02. 2 L 7 4 4F A20WE 1998042300158 19980423 00158 NM 1998 4 23 P5CA9601197 1 19960812 A 5320 SUPPORT BOEING 747 747121 1384871 NM BS 1000 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON FAIRING SUPPORT LWR FUSELAGE AT STA 1000 BETWEEN AREA RBL TO LBL 40. REMOVED CORROSION AND AREA TREATED PE R SRM 51-10-01 AND 51-40-03. 2 L 7 4 4F A20WE 1998042300159 19980423 00159 NM 1998 4 23 P5CA9601198 1 19960812 A 5320 FITTING BOEING 747 747121 1384871 NM NR 1 L PAX DOOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 NR 1L ENTRY DOOR CORROSION ON STOP FITTING FASTENERS ALONG FWD FRAME. CLEANED PER MM 51-21-00. 2 L 7 4 4F A20WE 1998042300160 19980423 00160 NM 1998 4 23 P5CA9601199 1 19960812 A 5210 HINGE BOEING 747 747121 1384871 NM NR 4R PAX DOOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 NR 4R ENTRY DOOR FUSELAGE DOOR CUTOUT SURFACE CORROSION ON LWR HINGE GUIDE CAM. CLEANED PER MM 51-21-00. 2 L 7 4 4F A20WE 1998042300161 19980423 00161 NM 1998 4 23 P5CA9601200 1 19960812 A 5344 FITTING BOEING 747 747121 1384871 NM DOOR 1R CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CRACK ON FITTING AT CONNECTION UPPER HINGE TO DOOR 1 RT LWR SIDE. INSTALLED NEW FITTING (P/N 65B07922-2) PER SRM 51-30- 02. 2 L 7 4 4F A20WE 1998042300162 19980423 00162 NM 1998 4 23 P5CA9601201 1 19960812 A 5314 KEEL BEAM BOEING 747 747121 1384871 NM BS 1220-1241 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 DEEP CORROSION ON LT SPAR AT KEEL BEAM AREA CENTER LWR FUSELAGE BETWEEN STA 1220 TO 1241. REMOVED CORROSION AND AREA TR EATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998042300163 19980423 00163 NM 1998 4 23 P5CA9601202 1 19960812 A 2710 HOUSING BOEING 747 747121 1384871 NM LT AILERON CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION LT INBOARD AILERON POWER CONTROL PACKAGE HOUSING SURFACE. CORROSION REMOVED FROM SURFACE PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998042300164 19980423 00164 NE 1998 4 23 P5CA9601203 2 19961215 A 7200 ENGINE BOEING 747 747124 1384874 NM PWA JT9 JT9D7A 52054 NE NR 1 OVER TEMP A P5CA C D ABORTED TAKEOFF RETURN TO BLOCK M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 WP 23 855FT 75912 2129 19733 662378 ABORTED TAKEOFF AND RETURNED TO RAMP DUE TO ENGINE NR 1 EXCEEDING MAX EGT LIMITS WHEN APPLYING TAKEOFF THRUST. EGT REAC HED 976 DEGREES FOR APPROXIMATELY 5 SECONDS. PERFORMED OVERTEMP INSPECTION REQUIRED BY 71-00-00 AREA C. BORESCOPE PER 72-00-00, NO DEFECTS NOTED, 80 HOUR LIMIT ENGINE CHANGED 12/17/96. SUSPECT 8TH STAGE CHECK VALVE OR HIGH STAGE VALVE F AILURE CAUSING EXCESSIVE BLEED AIR DURING TAKEOFF. 2 L 7 4 4F 4 F A20WE E20EA 1998042300165 19980423 00165 NM 1998 4 23 P5CA9601204 1 19960812 A 5320 DOUBLER BOEING 747 747121 1384871 NM PAX DOOR CUTOUT CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON DOUBLERS AT FUSELAGE RT SIDE UNDER TO PASSENGER DOOR 3. REMOVED CORROSION AND TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998042300166 19980423 00166 NM 1998 4 23 P5CA9601205 1 19960812 A 5230 PANEL BOEING 747 747121 1384871 NM CARGO DOOR TORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FORWARD CARGO COMPARTMENT DOOR LIFT MANUAL MECH PANEL IS TORN. MANUFACTURED AND INSTALLED NEW PANEL AS ORIGINAL MATERIA L OBTAINED FROM STA STOCK BNR09842-96. 2 L 7 4 4F A20WE 1998042300167 19980423 00167 NM 1998 4 23 P5CA9601206 1 19960812 A 5320 WEB BOEING 747 747121 1384871 NM CARGO COMPT TORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FORWARD CARGO COMPARTMENT SHEET METAL TORN ON STA 680 L. SMALL CRACK BLENDED OUT AND TREATED PER SRM 51-10-01, INSTALLE D RIVETS PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998042300168 19980423 00168 NM 1998 4 23 P5CA9601207 1 19960812 A 5730 SKIN BOEING 747 747121 1384871 NM WS 834.5 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 SWELLING ON UPPER RT WING SKIN AT REAR SPAR AREA WS 834.50. REMOVED RIVETS CLEANED CORROSION AND TREATED PER SRM 51-10- 01, RERIVETED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998042300169 19980423 00169 NM 1998 4 23 P5CA9601208 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1160-1180 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STRINGER 6, 7 BETWEEN STA 1160 TO 1180. CORROSION REMOVED PER SRM 51-10-01, FOUND WITHIN LIMITS PER SRM 53 -10-01. 2 L 7 4 4F A20WE 1998042300170 19980423 00170 NM 1998 4 23 P5CA9601209 1 19960812 A 5280 HINGE BOEING 747 747121 1384871 NM NLG DOOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 NOSE LANDING GEAR SURFACE CORROSION ON SERVICE CONTROL PANEL DOOR HINGE. INSTALLED NEW HINGE PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998042300171 19980423 00171 NM 1998 4 23 P5CA9601210 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1080 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STRINGER 3 RT AT STA 1080. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998042300172 19980423 00172 NM 1998 4 23 P5CA9601211 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1080 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STRINGER 3 RT AT STA 1080. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998042300173 19980423 00173 NM 1998 4 23 P5CA9601212 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1406 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STRINGER 1 LT AT STA 1406. CORROSION REMOVED AND TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998042300174 19980423 00174 NM 1998 4 23 P5CA9601213 1 19960812 A 5313 STRINGER BOEING 747 747121 1384871 NM BS 1400-1420 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON STRINGER 3 LT BETWEEN STA 1400 TO 1420. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998042300175 19980423 00175 NM 1998 4 23 P5CA9601214 1 19960812 A 5320 TIE CLIP BOEING 747 747121 1384871 NM BS 1560/1580 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON HL IN TIE CLIP AT STRINGER 1 TO 3 RT STA 1560, 1580. CORROSION REMOVED AND AREA TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998042300176 19980423 00176 NM 1998 4 23 P5CA9601215 1 19960812 A 5320 INTERCOSTAL BOEING 747 747121 1384871 NM BS 1900-1920 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 BROKEN, CRACKED AND CORROSION ON FLOOR INTERCOSTAL BETWEEN STA 1900 TO 1920 AND BETWEEN AREA BL 0 TO RBL 30. ALL AREAS REPAIRED PER SRM 51-40-02 AND SRM 51-40-03, TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998042300177 19980423 00177 NM 1998 4 23 P5CA9601216 1 19960812 A 7110 COWL FITTING BOEING 747 747121 1384871 NM NR 4 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 NR 4 RT MAIN COWL FWD LATCH FORGING FITTING HAS A CRACK IN LATCH CUTOUT. REMOVED RIVETS CLEANED CORROSION AND TREATED P ER SRM 51-10-01, INSTALLED NEW RIVETS PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998042300178 19980423 00178 NM 1998 4 23 P5CA9601217 1 19960812 A 5320 WEB BOEING 747 747121 1384871 NM BS 1860 TORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 TORN ON THE WEB AT STA 1860 RT SIDE ABOVE STRINGER 46, 47. AREA REPAIRED PER SRM 51-40-02. 2 L 7 4 4F A20WE 1998042300179 19980423 00179 NM 1998 4 23 P5CA9601219 1 19960805 A 5400 SKIRT BOEING 747 747121 1384871 NM NR 4 PYLON CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 SKIRT NR 4 SUPPORT RODS EYEBOLTS CORROSION. CORROSION REMOVED AND TREATED PER MM 51-21-03. 2 L 7 4 4F A20WE 1998042300180 19980423 00180 NM 1998 4 23 P5CA9601220 1 19960805 A 5400 SKIRT CLAMP BOEING 747 747121 1384871 NM NR 4 PYLON BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 SKIRT NR 4 CLAMP UNDER RETURN LINE BROKEN. CLAMP REPLACED PER MM 20-11-24. 2 L 7 4 4F A20WE 1998042300181 19980423 00181 NM 1998 4 23 P5CA9601221 1 19960812 A 5320 SCUFF PLATE BOEING 747 747121 1384871 NM CARGO DOOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 DEEP SURFACE CORROSION, DENT AND CRACK ON LWR SCUFF PLATE AT ENTRY BULK AFTER CARGO DOOR BETWEEN STA 198 TO 2040. FAB A ND INSTALLED NEW LWR SCUFF PLATE, FASTENERS INSTALLED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998042300182 19980423 00182 NM 1998 4 23 P5CA9601222 1 19960812 A 5320 ANGLE BOEING 747 747121 1384871 NM BS 1480-1500 BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 BROKEN KYDEX SUPPORT ANGLE ON LT SIDE WALL BETWEEN STA 1480 TO 1500 ABOVE STRINGER 34. NEW KYDEX SUPPORT INSTALLED PER SRM 51-40-03. 2 L 7 4 4F A20WE 1998042300184 19980423 00184 NM 1998 4 23 P5CA9601224 1 19960812 A 5320 FITTING BOEING 747 747121 1384871 NM BS 1480 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON FITTING TRACK RBL 25 AT STA 1480 AREA. CORROSION REMOVED AND TREATED PER SRM 51-10-01, FOUND WITHIN LIMITS PER SRM 53-10-01. 2 L 7 4 4F A20WE 1998042300185 19980423 00185 NM 1998 4 23 P5CA9601225 1 19960812 A 5753 TRACK BOEING 747 747121 1384871 NM NR 3 TE FLAP CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 TRACK NR 3 IS CORRODED AT BEARING MOVING PATHES. SURFACE CORROSION REMOVED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998042300186 19980423 00186 NM 1998 4 23 P5CA9601226 1 19960812 A 5753 CHORD BOEING 747 747121 1384871 NM RT TE MID FLAP CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 RT INBOARD MID FLAP WITH PANEL REMOVED SURFACE, CORROSION ON UPPER CTR CHORD OUTBD END, UNDER PANEL. CORROSION REMOVED AND TREATED PER SRM 51-10-01, FOUND WITHIN LIMITS PER SRM 57-10-01. 2 L 7 4 4F A20WE 1998042300187 19980423 00187 NM 1998 4 23 P5CA9601227 1 19960812 A 5753 RIB BOEING 747 747121 1384871 NM RT TE MID FLAP DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 RT INBOARD MID FLAP, L/E END RIB INBOARD OF INBOARD FLAP CARRIAGE ASSY HAS DENT AND DAMAGE. STRAIGHTEN DENT PER SRM 51- 40-01, SMOOTHED AND TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1998042300188 19980423 00188 NM 1998 4 23 P5CA9601228 1 19960812 A 5754 BEAM BOEING 747 747121 1384871 NM LT LE FLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 LEFT INBOARD KREUGER L/E FLAP PDU AFTER MOUNT BEAM INBOARD EDGE CRACKED. FAB NEW ANGLE PER SRM 57-12-01 AND INSTALLED P ER SRM 51-30-02. 2 L 7 4 4F A20WE 1998042300189 19980423 00189 NM 1998 4 23 P5CA9601229 1 19960812 A 5754 ARM BOEING 747 747121 1384871 NM NR 7 LE FLAP CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 L/E FLAP 7 INCHES INBOARD ARM SURFACE CORROSION. CORROSION REMOVED FROM SURFACE PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998042300190 19980423 00190 NM 1998 4 23 P5CA9601230 1 19960812 A 5753 TRACKS BOEING 747 747121 1384871 NM LT TE FORE FLAPS CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION LEFT WING ALL 7 FORE FLAP TRACKS SURFACE. CORROSION REMOVED FROM SURFACE PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998042300191 19980423 00191 NM 1998 4 23 P5CA9601231 1 19960812 A 5751 ANGLE BOEING 747 747121 1384871 NM LT AILERON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 LT INBOARD AILERON L/E ANGLE INBOARD TO INBOARD HINGE CRACKED. FAB NEW ANGLE PER SRM 57-12-00 AND INSTALLED PER SRM 51- 30-02. 2 L 7 4 4F A20WE 1998042300192 19980423 00192 NM 1998 4 23 P5CA9601232 1 19960812 A 5510 TIP FAIRING BOEING 747 747121 1384871 NM RT HORIZ STAB DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 RT STABILIZERS T/E TIP IS TORN. INSTALLED NEW FAIRING TIP (P/N 65B03521-34) AND RIVETED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998042300193 19980423 00193 NM 1998 4 23 P5CA9601233 1 19960812 A 5320 GUTTER BOEING 747 747121 1384871 NM BS 2280-2300 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CRACK AND BENT ON GUTTER AT FUSELAGE LT SIDE ABOVE PASSENGER DOOR 5 BETWEEN STA 228 TO 2300. CRACK BLENDED OUT, CHECKED AND FOUND OK PER SRM 53-10-01. 2 L 7 4 4F A20WE 1998042300194 19980423 00194 NM 1998 4 23 P5CA9601234 1 19960812 A 5320 DOUBLER BOEING 747 747121 1384871 NM BS 2240/2280 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON REINFORCEMENT DOUBLER AT FUSELAGE RT SIDE ABOVE PASSENGER DOOR 5 STA 2240 AND UNDER STA 2280. CORROSION RE MOVED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998042300195 19980423 00195 NM 1998 4 23 P5CA9601235 1 19960805 A 5320 CLIP BOEING 747 747121 1384871 NM BS 2020 BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 BROKEN CLIP ON STA 2020 LT SIDE ABOVE STRINGER 40 TO 41. NEW ANGLE CLIP INSTALLED PER SRM 51-40-03 AND RIVET PER SRM 51 -30-02. 2 L 7 4 4F A20WE 1998042300196 19980423 00196 NM 1998 4 23 P5CA9601236 1 19960805 A 5320 WEB BOEING 747 747121 1384871 NM FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 FOUND TWO AREAS ON THE WEB WITH CORROSION. CORROSION REMOVED, CHECKED AND FOUND LOSS OF 7 PERCENT OF MATERIAL ONLY PER SRM 57-10-01. 2 L 7 4 4F A20WE 1998042300197 19980423 00197 NM 1998 4 23 P5CA9601237 1 19960812 A 5320 RIVETS BOEING 747 747121 1384871 NM FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION, HITS, SCRATCHES, SHEARED RIVET AND CONNECTION BETWEEN EXISTING REPAIR FASTENER AND SHEET METAL COVER. REPAIR ED PER SRM 51-40-02. 2 L 7 4 4F A20WE 1998042300198 19980423 00198 NM 1998 4 23 P5CA9601238 1 19960812 A 5720 RIVETS BOEING 747 747121 1384871 NM WS 380 FAILED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 SHEAR RIVETS ON UPPER WING SKIN RT AT STA 380 FRONT SPAR AREA. INSTALLED NEW RIVETS PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998042300199 19980423 00199 NM 1998 4 23 P5CA9601239 1 19960812 A 5210 STOP BOEING 747 747121 1384871 NM NR 3R DOOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 NR 3R ENTRY DOOR SURFACE CORROSION ON DOOR STOPS. CLEANED PER MM 51-21-00. 2 L 7 4 4F A20WE 1998042300200 19980423 00200 NM 1998 4 23 P5CA9601240 1 19960812 A 5320 FASTENERS BOEING 747 747121 1384871 NM BS 1780 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON HEAD HI-LOCK AT STA 1780 BETWEEN STRINGER 2 TO 5 LT. CORRODED RIVETS TAKEN OUT AND INSTALLED NEW FASTENERS PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998042300201 19980423 00201 NM 1998 4 23 P5CA9601241 1 19960812 A 5320 RIVETS BOEING 747 747121 1384871 NM BS 1680-1720 FAILED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 SHEARED RIVETS ON CONNECTION FITTING TO LWR ENTRY DOOR FRAME NR 4 AT AREA STA 1680 AND 1720. INSTALLED NEW RIVETS PER S RM 51-30-02. 2 L 7 4 4F A20WE 1998042300202 19980423 00202 NM 1998 4 23 P5CA9601242 1 19960812 A 5320 FASTENERS BOEING 747 747121 1384871 NM BS 1560-1620 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON HEAD OF HI-LOCK AT STA 1560 TO 1620 BETWEEN STRINGER 5 LT AND 5 RT. CORRODED RIVETS TAKEN OUT AND INSTALLE D NEW HI-LOCKS PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998042300203 19980423 00203 NM 1998 4 23 P5CA9601243 1 19960812 A 5320 FASTENERS BOEING 747 747121 1384871 NM BS 1680 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON HEAD OF HI-LOCK AT STA 1680 BETWEEN STRINGER 3 TO 4 LT. CORRODED RIVETS TAKEN OUT AND INSTALLED NEW HI-LOC KS PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998042300204 19980423 00204 NM 1998 4 23 P5CA9601244 1 19960812 A 5313 FASTENERS BOEING 747 747121 1384871 NM BS 1000 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON HEAD OF HI-LOCK RIVET, ON SPLICE STRINGER 3R, 3L AT STA 1000. CORROSION RIVETS REMOVED AND INSTALLED NEW H I-LOCKS PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998042300205 19980423 00205 NM 1998 4 23 P5CA9601245 1 19960812 A 5320 TIE CLIP BOEING 747 747121 1384871 NM BS 2280 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 CORROSION ON TIE CLIP AT STA 2280 LT SIDE STRINGER 14. INSTALLED NEW CLIP (P/N 65B38600-160) PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998042300206 19980423 00206 NM 1998 4 23 P5CA9601246 1 19960812 A 5753 SUPPORT BOEING 747 747121 1384871 NM TE FLAPS WORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 LEFT WING OUTBD T/E FLAP TORQUE TUBE GEAR BOX HAS EXCESSIVE PLAY BETWEEN FLAP TRACK 1 AND 2. TORQUE TUBE SUPPORT REPLAC ED PER MM 27-51-00. 2 L 7 4 4F A20WE 1998042300207 19980423 00207 NM 1998 4 23 P5CA9601247 1 19960812 A 5320 FLOOR RIB BOEING 747 747121 1384871 NM BS 1620-1640 DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 BENT ON FLOOR RIB BETWEEN STA 1620 TO 1640 AT LBL 28 AREA. REPAIRED AND TREATED PER SRM 51-40-01 AND SRM 51-10-01. 2 L 7 4 4F A20WE 1998042300208 19980423 00208 NM 1998 4 23 P5CA9601248 1 19960812 A 5320 INTERCOSTAL BOEING 747 747121 1384871 NM BS 1580-1600 DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 BENT ON FLOOR INTERCOSTAL BETWEEN STA 1580 TO 1600 AT RBL 28 AREA. DAMAGE BLENDED OUT AND AREA TREATED PER SRM 51-10-01 AND SRM 51-40-01. 2 L 7 4 4F A20WE 1998042300332 19980423 00332 WP 1998 4 23 ABXA9700428 1 19961121 A 5520 5910411543 HAT CHANNEL DOUG DC9 DC941 302207N WP ELEVATOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 960AX 47762 INNER HAT CHANNELS CRACKED. REPLACED 3 HAT CHANNELS IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1998042300397 19980423 00397 EU 1998 4 23 97ZZZM446 1 19961228 A 5320 SILL PLATE BAG BAE146 BAE146300A 1500267 EU PAX DOOR CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW E3122 FORWARD SILL PLATE ON AFT PASSENGER DOOR CORRODED. REMOVED AND REPLACED FORWARD SILL PLATE AT AFT PASS DOOR. 2 H 7 4 4F RT A49EU 1998042300398 19980423 00398 NE 1998 4 23 97ZZZM447 2 19961212 A 7310 MANIFOLD BAG BAE146 BAE146300A 1500267 EU LYC ALF502 ALF502R5 41580 NE NR 2 ENGINE FAILED A A A6WA K NONE A FLAME/FIRE IN INSP/MAINT 1 GL 31 612AW E3122 INSPECTED FUEL MANIFOLD FOR EVIDENCE OF SOOT AND DISCOLORATION IND. FUEL FIRE, PERFORMED ET INSPECTION OF 5TH SCALLOP F ROM TOP FOR CRACKS IAW TEXTRON SPEC PROCEDURE. PERFORMED DV INSPECTION OF RT FUEL MANIFOLD, S/N 863. FOUND A SMALL VIS UAL IND IN THE 5TH SCALLOP . W/C GENERATED FOR REMOVAL OF THE RT FUEL MANIFOLD. 2 H 7 4 4F 4 F RT A49EU E6NE 1998042300400 19980423 00400 EU 1998 4 23 97ZZZM449 1 19961030 A 5320 BOLTS BAG BAE146 BAE146200A 1500266 EU WING/FUSELAGE TOO LONG A A6WA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 606AW E2033 FUSELAGE BOLT LOOSE AT RIGHT WING FORWARD SPAR. CHECK TORQUE ON THREE OTHER IN THAT SAME ROW. REPLACED 2 BOLTS FOUND T O BE TOO LONG. CHECK TORQUE ON REMAINING 3, CHECK OK. WITCOBOND 2 REPLACEMENT BOLTS, HOLES WITHIN LIMITS. AFT OF FR 2 6 WING TO FUSELAGE CLOSING ANGLE. ( 2 H 7 4 4F RT A49EU 1998042300446 19980423 00446 1998 4 23 TWRA97111 4 19960516 A 2397 WIRE BOEING 747 747259B 1384804 NM L-1 DOOR BROKEN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 621FF 21730 ON PRE-FLIGHT AT JED, FOUND PA SYSTEM INOP, AT L-1 DOOR. REPAIRED WIRING AT L-1 DOOR, NOW OPS CHECK NORMAL PER MM 23-30 -00. (M) 2 L 7 4 4F RT A20WE 1998042900017 19980429 00017 GL 1998 4 29 CA960916008 2 19960902 A 7230 BEARING BELL 206 206L 1181522 SW ALLSN 250C 250C20R2 GL COMPRESSOR WORN W K NONE O OTHER IN INSP/MAINT 1 CA 1818 CAE295306 (CAN) NOISY COMPRESSOR ON START-UP. BEARING NOISE ON THE INLET OF COMPRESSOR. 1 G 7 1 3U 3 U H2SW E4CE 1998042900639 19980429 00639 WP 1998 4 29 AALA972440 1 19961212 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1257-1278 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 162AA 46943 TUL - FOUND SKIN CORRODED AT BS 1257 - BS 1278. REPAIRED DAMAGED AREAS PER 53-00-01. TST: 67,144.30 HOURS. CYCLES: 2 5,370. (X) 2 L 7 3 4F A22WE 1998042900661 19980429 00661 CE 1998 4 29 CA961009009 1 19960905 A 2750 052323113 TRACK CESSNA 172 172M 2072418 CE MCAULY 1C160 1C160DTM GL TE FLAP CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 727311 (CAN) FLAP TRACK FOUND CRACKED ON THE INBOARD SIDE, PROBABLY DUE TO A DEFECTIVE ROLLER BEARING. 1 H 7 1 3O NT 3A12 5 N P910 1998043000034 19980430 00034 CE 1998 4 30 CA961029006 1 19961025 A 5753 5016000354 SPAR 5016000396 BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA LEFT INB FLAP CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 9695 PCE50224 (CAN) SMALL CRACK, APPROXIMATELY 0.750 INCH IN LENGTH FOUND ON INBOARD FLAP SPAR. CRACK LOCATED AT INBOARD FLAP TRACK A TTACHMENT POINT IN THE MAIN SPAR. FURTHER INVESTIGATION FOUND A LARGER CRACK ABOUT 6 INCHES LONG FURTHER OUTBOARD IN TH E UPPER SPAR RADIUS. PART TC: 10,304. AIRCRAFT TT: 9,734 HOURS. 1 L 7 2 3T 4 T A14CE E4EA 1998043000035 19980430 00035 CE 1998 4 30 CA961029007 1 19961025 A 5753 5016000354 SPAR 5016000396 BEECH 90 65A90 1152908 CE PWA PT6 PT6A20 52043 EA LT INB FLAP CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 11239 PCE20621 (CAN) SMALL CRACK, APPROXIMATELY 0.750 INCH IN LENGTH WAS DETECTED ON THE LEFT INBOARD FLAP SPAR AT THE INBOARD FLAP TRA CK ATTACHMENT POINT ON THE UPPER SKIN FROM THE RIVET. A LARGER CRACK WAS THEN FOUND, APPROXIMATELY 4 TO 6 INCHES IN LEN GTH, FURTHER OUTBOARD IN THE UPPER SPAR RADIUS. PART TC: 26,270. AIRCRAFT TT: 14,306 HOURS. 1 L 7 2 3T 3 T 3A20 E4EA 1998043000036 19980430 00036 CE 1998 4 30 CA961030001 1 19961028 A 5753 5016000354 SPAR 5016000396 BEECH 90 65A90 1152908 CE PWA PT6 PT6A20 52043 EA INB FLAP TRACK CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 12763 PCE22479 (CAN) AT INBOARD FLAP TRACK CUTOUT IN THE SPAR THERE ARE TWO CRACKS EXTENDING FROM THE TOP CORNERS OF THE CUTOUT INTO TH E BEND RADIUS. EACH CRACK ABOUT 2 INCHES LONG. PART TC: 16,223. AIRCRAFT TT: 12,807 HOURS. 1 L 7 2 3T 3 T 3A20 E4EA 1998043000037 19980430 00037 CE 1998 4 30 CA961030002 1 19961028 A 5753 5016000354 SPAR 5016000396 BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA INB FLAP TRACK CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 9988 LJ543 PCE50228 (CAN) AT THE SPAR CUTOUT WHICH THE INBOARD FLAP TRACK PASSES AS THE FLAP IS RETRACTED, A .50 INCH CRACK WAS FOUND, EXTEN DING FROM THE TOP INBOARD CORNER INTO THE BEND RADIUS BETWEEN THE WEB AND FLANGE. PART TC: 10,196. AIRCRAFT TT: 10,0 17 HOURS. 1 L 7 2 3T 4 T A14CE E4EA 1998043000038 19980430 00038 CE 1998 4 30 CA961104007 1 19961028 A 5753 5016000354 SPARS 5016000396 BEECH 90 65A90 1152908 CE PWA PT6 PT6A20 52043 EA LT/RT FLAP CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 10847 PCE21249 (CAN) BOTH INBOARD FLAP SPARS WERE FOUND WITH CRACKS ON THE SPAR. THESE CRACKS WERE LOCATED AT THE AREA WHERE THE BRACK ET FOR THE ROLLERS ATTACH. RIGHT HAND SPAR IS A 50-160003-55. PART TC: 10,688. AIRCRAFT TT: 10,893 HOURS. 1 L 7 2 3T 3 T 3A20 E4EA 1998043000039 19980430 00039 CE 1998 4 30 CA961113006 1 19961031 A 5753 5016000354 SPAR 5016000396 BEECH 90 65A90 1152908 CE PWA PT6 PT6A20 52043 EA LT INB FLAP CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 11837 PCE21451 (CAN) LEFT INBOARD FLAP SPAR FOUND WITH A CRACK AT THE INBOARD AREA WHERE THE BRACKET ROLLERS ATTACH. PART TC: 11,398. AIRCRAFT TT: 11,883 HOURS. 1 L 7 2 3T 3 T 3A20 E4EA 1998043000040 19980430 00040 CE 1998 4 30 CA961203007 1 19961118 A 5751 991300009 SKIN BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA LT-RT AILERON CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 10982 PCE52376 (CAN) LEFT AILERON UPPER AND LOWER SKINS CRACKED ALONG SPAR AT TRAILING EDGE OF LEADING EDGE SKIN. RIGHT AILERON LOWER SKIN CRACKED SAME PLACE. ALSO, P/N 99-13000-197 AND -199. 1 L 7 2 3T 4 T A14CE E4EA 1998043000041 19980430 00041 CE 1998 4 30 CA961218005 1 19961126 A 3260 1003810061 SWITCH BEECH 200 B200C 1152924 CE PWA PT6 PT6A42 52043 NE NOSE GEAR FAILED W O L OTHER ABORTED APPROACH N FALSE WARNING AP APPROACH 1 CA 811 PCE93224 (CAN) THIS AIRCRAFT'S ELECTRICAL LANDING GEAR SYSTEM HAD BEEN REPLACED WITH A HYDRAULIC SYSTEM. THE NOSE GEAR GREEN LIG HT DID NOT COME ON WHEN THE GEAR WAS DOWN AND LOCKED. THUS, THE PILOT HAD TO DO SEVERAL GEAR CYCLES AND A FLY-BY. HE L ANDED OK. THE NOSE GEAR DOWN AND LOCKED SWITCH WAS REPLACED. IT IS BEING REPLACED AT ABOUT 8 TO 900 HOUR INTERVALS. P ART TC: 654. 1 L 7 2 4T 4 T A24CE E4EA 1998043000043 19980430 00043 CE 1998 4 30 CA961218007 1 19961205 A 3260 1003810061 SWITCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE NOSE GEAR FAILED W O OTHER N FALSE WARNING AP APPROACH 1 CA 3258 PCE114296 (CAN) GEAR SELECTED DOWN ON APPROACH, NOSE GEAR IN TRANSIT LIGHT STAYED ON WHILE BOTH MAIN GEARS INDICATED DOWN AND LOCK ED. GEAR WAS CYCLED TWICE TO GET ALL THREE DOWN AND LOCKED LIGHTS. DOWNLOCK MICROSWITCH FOUND FAULTY. 2 L 7 2 4T 4 T RT A24CE E26NE 1998043000044 19980430 00044 CE 1998 4 30 CA961231001 1 19961217 A 3260 1003810061 SWITCH BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA NLG DOWNLOCK FAILED W L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 CA PCE81271 (CAN) ON APPROACH, GEAR DOWN SELECTED WITH 3 GREENS. WHEN FLAPS SELECTED BEYOND APPROACH SETTING OR WHEN POWER LEVERS W ERE REDUCED BELOW 400 POUNDS TORQUE, GEAR WARNING HORN WOULD SOUND AND GEAR IN-TRANSIT LIGHT CAME ON. NOSE GEAR DOWNLOC K MICROSWITCH NOT FULLY DEPRESSED. WHEN HAND PRESSURE APPLIED TO STRIKER PLATE BOTH HORN AND IN-TRANSIT LIGHT WOULD GO OUT. SWITCH ADJUSTED. 1 L 7 2 4T 4 T A24CE E4EA 1998050100128 19980501 00128 CE 1998 5 1 CA970702010 1 19961203 A 5540 MS244624 RUDDER BEARING CESSNA 208 208B 2073701 CE HARTZL H3B3M HCB3M GL BEARING WORN W K NONE O OTHER IN INSP/MAINT 1 CA 7677 PCE17181 GB88 (CAN) RUDDER NOTICED TO BE RESTING LOWER THAN NORMAL. INSPECTION FOUND THE UPPER BEARING HAD BECOME SEVERELY WORN. ALL BEARINGS REPLACED. 1 H 7 1 3T A37CE 5 C P9NE 1998050100138 19980501 00138 GL 1998 5 1 CA970626009 2 19961208 A 7323 23007507 GOVERNOR BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL INTERNAL SURGING W K NONE J WARNING INDICATION CR CRUISE 1 CA 40 CAE860407 (CAN) ENGINE LOST POWER SUDDENLY, THEN SURGED TOWARDS OVERTORQUE AND OVERSPEED. POWER OSCILLATIONS IN-FLIGHT. 1 G 7 1 3U 3 U H2SW E1GL 1998050100205 19980501 00205 GL 1998 5 1 CA960717007 2 19960704 A 7230 6853337 COMPRESSOR BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL AXIAL STAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 10269 1842 CAE802381BA (CAN) SUSPECT POSSIBLE SEPARATION OF FIRST STAGE STATOR BLADES CAUSING EXTENSIVE DAMAGE TO COMPRESSOR AND TURBINE AND EN GINE FAILURE. PART TC: 6,604. 1 G 7 1 3U 3 U H2SW E4CE 1998050100222 19980501 00222 GL 1998 5 1 CA970311003 2 19960929 A 7230 22764 LINER 6877410 BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL 4TH STAGE MISSING W K NONE O OTHER IN INSP/MAINT 1 CA 1496 22764 CAE821208 (CAN) DURING CASE HALF INSPECTION, 3 LARGE PIECES OF LINER NOTED AS MISSING IN 4TH STAGE AREA . 1 G 7 1 3U 3 U H2SW E4CE 1998050100223 19980501 00223 NE 1998 5 1 CA970311010 2 19960916 A 7322 7257255 FUEL CONTRL UNIT HAMSTD CARSON S61 S61LSKRSKY EA GE CT58 CT581401 30011 NE ENGINE FAILED W K NONE O OTHER HO HOVERING 1 CA 1672 87021BR 295035 (CAN) ENGINE WILL NOT MEET MINIMUM ACCEPTABLE TORQUE. LOW POWER, LOW T5, HIGH NG. NO CHANGE ON MANUAL THROTTLE. PART T C: 29. 2 G 7 2 4U 4 U H8EA 1E3 1998050100224 19980501 00224 NE 1998 5 1 CA970311012 2 19960917 A 7320 7257255 FUEL CONTRL UNIT HAMSTD CARSON S61 S61LSKRSKY EA GE CT58 CT581401 30011 NE ENGINE FAILED W K NONE O OTHER HO HOVERING 1 CA 6679 3103 41914 295035 (CAN) ENGINE WILL NOT TOP. CANNOT OBTAIN ACCEPTABLE TORQUE. TAKE OVER MANUAL SPEED LEVER AND ENGINE IS NORMAL. PART TC : 1. 2 G 7 2 4U 4 U H8EA 1E3 1998050100225 19980501 00225 GL 1998 5 1 CA970311023 2 19960725 A 7230 CAC15175 BEARING 23038126 BELL 206 206L 1181522 SW ALLSN 250C 250C20R2 GL NR 2 ENG MAKING METAL W K NONE O OTHER IN INSP/MAINT 1 CA 3981 CAC15175 CAE832536 (CAN) NR 2 BEARING MAKING METAL. BEARING INSPECTED AND FOUND TO BE NOISY WITH BALL SHOWING EVIDENCE OF GALLING. PART TC: 3,325. 1 G 7 1 3U 3 U H2SW E4CE 1998050100226 19980501 00226 GL 1998 5 1 CA970311045 2 19960820 A 7322 2332246 FUEL CONTRL UNIT BENDIX BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL ENGINE FAILED W R AUTOROTATION Y R ENGINE STOPPAGE PARTIAL RPM/PWR LOSS HO HOVERING 1 CA 2471 324186 CAE860657 (CAN) AIRCRAFT IN HOVER, ENGINE DECELERATED. AIRCRAFT AUTO-ROTATED TO GROUND. ENGINE CONTINUED TO OPERATE BUT WOULD ON LY PRODUCE 90 PERCENT NR. FUEL CONTROL UNIT REPLACED. 1 G 7 1 3U 3 U H2SW E1GL 1998050500315 19980505 00315 NM 1998 5 5 DL72L960614 1 19960319 A 3350 RPS1 POWER SUPPLY BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 505DA 21307 DURING EMERGENCY LIGHTING CHECK, MAINT FOUND TRACK LIGHTING BETWEEN ROWS 12 AND 19 INOP. REPLACED POWER SUPPLY, OPERATI ON NORMAL. 2 L 7 3 4F A3WE 1998050500316 19980505 00316 NM 1998 5 5 DL72S960577 1 19960314 A 5320 VERT BEAM BOEING 727 727232 1384082 NM BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 409DA 21153 VISIBLE CRACK, 1.50 INCHES, IN VERT BEAM, STA 1183, RBL 8 AT WL 182. FOUND DURING E-2 LTR CK TPAMM. REPAIRED PER M/M 5 3-11-0. 2 L 7 3 4F A3WE 1998050500318 19980505 00318 NM 1998 5 5 DL72S960602 1 19960318 A 5720 STIFFNER BOEING 727 727232 1384082 NM WING FRONT SPAR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 400DA 21144 WING FRONT SPAR VERTICAL STIFFENER CRACKED AT NR 3 SLAT INBOARD TRACK, OUTBOARD SIDE (ON WING). FOUND DURING F-1 LTR CK TPA 3/18/96. REPAIRED PER 57-20-21. 2 L 7 3 4F A3WE 1998050500319 19980505 00319 NM 1998 5 5 DL72S960603 1 19960318 A 5755 ANGLE BOEING 727 727232 1384082 NM NR 7 SPOILER CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 400DA 21144 NR 7 SPOILER LOWER WING ATTACH ANGLE CRACKED INBOARD END. FOUND DURING F-1 LTR CK TPAMM. REPAIRED PER 57-20-22. 2 L 7 3 4F A3WE 1998050500320 19980505 00320 NM 1998 5 5 DL72S960604 1 19960318 A 5754 RIB BOEING 727 727232 1384082 NM NR 2 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 400DA 21144 FOUND ON F1 LETTER CK, 1 INCH CRACK AT NR 2 L/E SLAT INBOARD NOSE RIB AT ACTUATOR ROD END ATTACH. REPAIRED PER MM 57-54 -0. 2 L 7 3 4F A3WE 1998050500321 19980505 00321 NM 1998 5 5 DL72S960605 1 19960318 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 7 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 515DA 21431 FOUND ON A1 LETTER CHECK - REWRITE FROM N/R 50 - ANGLE CRACKED .50 INCH AT NR 7 SLAT ANTI-ICE 'T' DUCT CUTOUT - REPAIR, INSTALL DOUBLER PER M/M 57-54-0, PG 807. 2 L 7 3 4F A3WE 1998050500322 19980505 00322 NM 1998 5 5 DL72S960616 1 19960226 A 5754 65162249092 SKIN BOEING 727 727232 1384082 NM NR 8 LE SLAT DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 469DA 20746 DURING INSPECTION, NR 8 L/E SLAT WAS FOUND WITH DAMAGE TO OUTBOARD CORNER OF SKIN, APPROX 10 INCHES. REPAIRED PER SRM 5 7-50-3, FIG 5. 2 L 7 3 4F A3WE 1998050500323 19980505 00323 NM 1998 5 5 DL72W960609 1 19960319 A 5350 ANGLE BOEING 727 727247 138408F NM LWR FUS FAIRING CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2816W 20872 FOUND DURING E-2 LETTER CHECK - CORROSION AT HINGE ON LOWER FUSELAGE FAIRING PANEL FWD OF LOWER BEACON. REPAIRED PER M/ M 53-30-1. 2 L 7 3 4F A3WE 1998050500324 19980505 00324 NM 1998 5 5 DL72W960610 1 19960319 A 5320 WEB BOEING 727 727247 138408F NM LWR TORQUE BOX CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2816W 20872 FOUND DURING E-2 LETTER CHECK - .50 INCH CRACK, LT FWD TORQUE BOX LIGHTENING HOLE. REPAIRED PER M/M 53-11-0. 2 L 7 3 4F A3WE 1998050500325 19980505 00325 NM 1998 5 5 DL72W960611 1 19960319 A 5532 SKIN BOEING 727 727247 138408F NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2816W 20872 FOUND DURING E-2 LETTER CHECK - 2 EA, .25 INCH CRACKS EXTENDING FROM RIVET HOLES, RT VERTICAL STAB SKIN, JUST BELOW SADD LE PLATE 9501. REPAIRED PER M/M 54-30-0. 2 L 7 3 4F A3WE 1998050500326 19980505 00326 NM 1998 5 5 DL73S960599 1 19960317 A 3350 1619 BULB BOEING 737 737232 1384475 NM R 1 DOOR FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 327DL 23099 FOUND ON LAYOVER CHECK - R1 EXTERIOR EMERGENCY LIGHT INOP. CORRECTIVE: RELAMPED - OPERATIOAL CHECKS NORMAL. 2 L 7 2 4F RT A16WE 1998050500327 19980505 00327 NM 1998 5 5 DL757960575 1 19960314 A 5246 DOOR 114N3002120 BOEING 757 757232 1384965 NM FWD LAV SERVICE DEPARTED ACFT A DALA O OTHER D INFLIGHT SEPARATION CR CRUISE 1 SO 27 667DN 25035 FORWARD LAV SERVICE DOOR RIPPED OFF IN-FLIGHT, CONTACTED AND WENT THROUGH NR 6 SLAT. HOLE APPROX 10 INCHES BY 20 INCHES . REPLACED NR 6 L/E SLAT AND INSTALLED NEW LAV SERVICE PANEL. 2 L 7 2 4F RT A2NM 1998050500328 19980505 00328 NM 1998 5 5 DL757960588 1 19960314 A 3350 01863069401 TRACK LIGHT BOEING 757 757232 1384965 NM CABIN DAMAGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 612DL 22819 V20009 DURING INSPECTION, EMERGENCY FLOOR TRACK LIGHT FOUND DAMAGED IN FWD CABIN. REPLACED DAMAGED FLOOR TRACK SECTION, OPERAT ION NORMAL. 2 L 7 2 4F RT A2NM 1998050500329 19980505 00329 NM 1998 5 5 DL757960606 1 19960319 A 2150 CONTROLLER 6259468 BOEING 757 757232 1384965 NM LT PACK MALFUNCTIONED A DALA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 27 651DL 53C431 24391 LEFT PACK TEMP AT 370 DEGREES CELSIUS. UNABLE TO RESET. CONTROLLER HAD HARD FAULT. REPLACED SAME W/BOR UA PART. RIGH T PACK WILL NOT HOLD CABIN WITH IDLE POWER AT ANY ALTITUDE. EMERGENCY DESCENT ACCOMPLISHED TO 10,000 FEET. FOUND RT PA CK FLOW LOW SWITCH TO MANUAL WARM FLOW RET TO NORMAL. 2 L 7 2 4F RT A2NM 1998050500330 19980505 00330 NM 1998 5 5 DL757960618 1 19960319 A 2622 FIRE BOTTLE 51211 BOEING 757 757232 1384965 NM CABIN LOW PRESS A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 623DL 22913 14607 FIRST CLASS HALON FIRE EXTIGUISHER HAS LOW PRESSURE. REPLACED BOTTLE. 2 L 7 2 4F RT A2NM 1998050500331 19980505 00331 1998 5 5 DL76L960600 4 19960317 A 2565 101651303 SLIDE BOEING 767 767332 1382001 NM RT REAR DOOR MALFUNCTIONED A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 186DN PA1939 27962 RIGHT REAR SLIDE FELL OUT OF THE DOOR COVER WITH DOOR HALF OPEN AND THEN OUT OF THE ACFT WITH THE GIRT BAR DETACHED. SL IDE BLOCKED EXIT AND REMAINED HUNG ON DOOR INSTEAD OF GIRT BAR FITTINGS. DOOR WAS OPENED FROM OUTSIDE OF A/C AND DOOR W AS DISARMED. REPLACED SLIDE AND INSPECTED MOUNTS. 2 L 7 2 4F RT A1NM 1998050500332 19980505 00332 WP 1998 5 5 DLL10960593 1 19960316 A 3350 POWER SUPPLY 5165741 LKHEED 1011 10113851 5265010 WP GALLEY INOPERATIVE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 720DA 54010 193C1136 BLINKING AMBER LIGHT ON LOWER GALLEY EMERGENCY LIGHT POWER SUPPLY. REPLACED POWER SUPPLY, OPERATION NORMAL. 2 L 7 3 4F A23WE 1998050500333 19980505 00333 WP 1998 5 5 DLL10960607 1 19960319 A 3350 BATTERY PACK 5165741 LKHEED 1011 10113851 5265010 WP L 2 DOOR DISCHARDED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 714DA 37796 193C1090 EMERGENCY LIGHTS BATTERY PACK INOP L2 DOOR. REPLACED SAME. SYSTEM CHECKS GOOD. 2 L 7 3 4F A23WE 1998050500334 19980505 00334 WP 1998 5 5 DLL17960585 1 19960315 A 5320 1613279101 TRIPLER LKHEED 1011 10113853 5265020 WP FS 1403-1423 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 766DA 193H1207 V20009 CORROSION WAS FOUND ON THE INNER SURFACE OF THE AFT PRESSURE OUTFLOW VALVE SURROUND TRIPLER. THE CORROSION WAS ISOLATED TO THE .244 INCH THICK PORTION OF THE TRIPLER. ACCOMPLISHED REPAIRS PER DL ERA 273432-14. 2 L 7 3 4F A23WE 1998050500335 19980505 00335 NM 1998 5 5 DLM88960573 1 19960314 A 5330 5924802 SKIN DOUG MD88 MD88 3023688 NM FS 229-266 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 938DL 49811 LEFT FUSELAGE SKIN WAS DENTED AND PREVIOUSLY REPAIRED. DURING HMV, THE REPAIR WAS REMOVED AND ADDITIONAL DAMAGE WAS FOU ND RESULTING IN AN ENLARGED CUTOUT. SINCE THE DAMAGE IS NEAR THE PANEL FOWARD END, THE FORWARD SECTION OF THE SKIN PANE L IS CUT VERTICALLY AT FS 266 FROM THE LOWER EDGE OF THE PANEL AT THE CUSP STRINGER 18L UP TO THE PANEL UPPER EDGE BELOW STRINGER 15. THE FORWARD SECTION OF THE PANEL EXTENDING FROM FS 229 AFT TO FS 266 CONTAINING THE DAMAGE IS REMOVED AND REPLACED, AND A REPAIR ADDED AT FS 266. ACCOMPLISHED REPAIRS PER DL ERA 273434-14, REV A. 2 L 7 2 4F RT A6WE 1998050500336 19980505 00336 NM 1998 5 5 DLM88960574 1 19960314 A 5330 593666751 SKIN DOUG MD88 MD88 3023688 NM FS 1315-1338 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 957DL 49976 FUSELAGE SKIN BETWEEN FS 1315 AND FS 1338 AND BETWEEN STR 25L AND STR 25R WAS FOUND DAMAGED AFTER THE A/C EXPERIENCED A TAIL STRIKE. ACCOMPLISHED REPAIRS PER DL ERA 273253-14 REV A. 2 L 7 2 4F RT A6WE 1998050500337 19980505 00337 NM 1998 5 5 DLM88960587 1 19960315 A 3320 LAMP DOUG MD88 MD88 3023688 NM AFT GALLEY FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 916DE 53421 V20009 ON APPROACH INTO ATL, F/A REPORTED STRONG ELEC SMELL IN THE AREA OF AFT GALLEY. FOUND FLUORESCENT LIGHT AT 31E SIDEWALL MELTED AT 1 SOCKET AND BULB PIN. REMOVED LAMP. FWD TO MCO. REPLACED LIGHT ASSEMBLY. 2 L 7 2 4F RT A6WE 1998050500338 19980505 00338 NM 1998 5 5 DLM88960608 1 19960319 A 3250 CONTROL VALVE 59142965509 DOUG MD88 MD88 3023688 NM NLG STEERING FAILED A DALA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 916DE EFS24506 53421 NOSE WHEEL STEERING WOULD NOT RESPOND TO STEERING YOKE INPUTS DURING TAXI, AND EVENTUALLY, LOCK IN FULL LEFT TURN. REPL ACED STEERING CONTROL VALVE, OPERATION NORMAL. 2 L 7 2 4F RT A6WE 1998050500339 19980505 00339 WP 1998 5 5 MWEA96063 1 19960320 A 3350 100865 POWER SUPPLY DOUG DC9 DC914 3022034 WP CABIN INOPERATIVE A MWEA K NONE L NO TEST NR NOT REPORTED 1 GL 31 500ME 45711 CREW REPORTS THE FLOOR EMERGENCY EVAC LIGHTS BETWEEN ROW 4 THROUGH ROW 8 INOP. REPLACED EMERGENCY LIGHTS BATTERY POWER SUPPLY. OPS CHECK GOOD. 2 L 7 2 4F A6WE 1998050500340 19980505 00340 NM 1998 5 5 P5CA9600164 1 19960318 A 5330 SKIN BOEING 747 747123 1384873 NM BS 480 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 FOUND DISHED RIVETS, POUCHED SKIN, AND CORRODED CLIP AT BS 480 BETWEEN STR 42R AND STR 43R, LOWER RT FUSELAGE. REMOVED DISHED RIVETS, CUT OUT SKIN AND REPLACED WITH FILLER AND DOUBLER PER SRM 53-30-03. BLENDED OUT CORROSION, REMOVED AND R EPLACED NEW CLIP PER SRM 53-30-03. APPLIED CPC TO AREA. LEAK CHECK OK. 2 L 7 4 4F A20WE 1998050500341 19980505 00341 NM 1998 5 5 UPS96205713 1 19960318 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM FLT DECK OUT OF POSITION A IPXA K NONE L NO TEST TO TAKEOFF 1 SO 01 949UP 19717 WHILE IN MEX CREW REPORTED, ON T/O ROLL THE COCKPIT EMERGENCY EXIT LIGHT FELL OFF THE BULKHEAD AND HIT THE FLOOR. LIGHT IS NOW INOP. REPOSITIONED BATTERIES AND LAMPS. CHECKS NORMAL. 2 L 7 3 4F A3WE 1998050500342 19980505 00342 NM 1998 5 5 UPS96205714 1 19960312 A 5320 65453132 TIE BOEING 727 72727C 138400J NM BS 363-380 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON STR 22R AT BS 363 TO BS 380 RBL 50, WL 165. REMOVED CORROSION IAW SRM 53-10-1. REPLACED STRINGER FRAME TIE IAW 51-30-2. 2 L 7 3 4F A3WE 1998050500343 19980505 00343 NM 1998 5 5 UPS96205715 1 19960314 A 5320 SILL BOEING 727 72727C 138400J NM BS 304-335 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON MOP SILL AT STA 304-309, RBL 58, WL 208. REMOVED CORROSION IAW 53-10-1. CORROSION EXTENDED TO STA 335, STA 320, AND STA 334 OUT OF LIMITS. REPAIRED MOP SILL PER SRM 51-40-3 AT STA 320, 334. 2 L 7 3 4F A3WE 1998050500344 19980505 00344 NM 1998 5 5 UPS96205716 1 19960312 A 5313 STRINGER BOEING 727 72727C 138400J NM BS 680-700 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON STR 9R FROM BS 680 - BS 700. REPAIRED STRINGER IAW 53-10-1 AND 53-10-3. 2 L 7 3 4F A3WE 1998050500345 19980505 00345 NM 1998 5 5 UPS96205717 1 19960318 A 2782 ACTUATOR BOEING 727 72731C 1384011 NM NR 5 LE FLAP LEAKING A IPXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 925UP 19230 CREW REPORTED AIR TURN BACK DUE TO A SYS HYDRAULIC FAILURE. TURN BACK AT 0457 Z, QUANTITY WENT TO ZERO. NR 5 KRUGER FL AP ACT. LEAKING, AWAITING PARTS FOR REPAIR. 2 L 7 3 4F A3WE 1998050500346 19980505 00346 NM 1998 5 5 UPS96205731 1 19960315 A 5320 WEB BOEING 727 72727C 138400J NM BS 292 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CRACK ON NLG W/W WEB AT BS 292, RBL 23, WL 191. REMOVED AND REPLACED WEB IA W UPS SRM 51-40-02, 51-10-2, 51-30-2, AND 51-20-4. 2 L 7 3 4F A3WE 1998050500347 19980505 00347 NM 1998 5 5 UPS96205732 1 19960316 A 5320 INTERCOSTAL BOEING 727 72727C 138400J NM BS 215 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON INTERCOSTAL AT BS 215, RBL 26, WL 176. REMOVED CORROSION AT BS 215, RBL 26, WL 176 PER SRM 51-20-4, 53-10-1, AND 51-30-5. 2 L 7 3 4F A3WE 1998050500348 19980505 00348 NM 1998 5 5 UPS96205733 1 19960315 A 5320 66147361 FORK ASSY BOEING 727 72727C 138400J NM BS 742 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED FORK ASSY CORRODED BEYOND REPAIR. REMOVED AND REPLACED FORK ASSY IAW OHM 20 -50-01 AND SRM 51-20-4. 2 L 7 3 4F A3WE 1998050500349 19980505 00349 NM 1998 5 5 UPS96205734 1 19960316 A 5311 FRAME BOEING 727 72727C 138400J NM BS 312 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON FRAME AT STA 312, RBL 43, WL 170. REMOVED DAMAGED SECTION OF F RAME AND FAB REPAIR PARTS AND INSTALLED. ALL WORK IAW SRM 51-10-2, 51-40-2, 53-10-1, 51-10-6, 51-30-2, AND MM 51-20-151 . 2 L 7 3 4F A3WE 1998050500350 19980505 00350 NM 1998 5 5 UPS96205735 1 19960318 A 5320 WEB BOEING 727 72727C 138400J NM BS 342 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON WEB AT STA 342, RBL 63, WL 208. REMOVED AND REPLACED WEB IAW 5 3-10-6, 53-10-1, 51-20-1, AND 51-30-2. 2 L 7 3 4F A3WE 1998050500351 19980505 00351 NM 1998 5 5 UPS96205736 1 19960315 A 5320 69348931 INTERCOSTAL BOEING 727 72727C 138400J NM BS 740-760 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON INTERCOSTAL STA 740-760, RBL 65, WL 208, AROUND FASTENER HOLES. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998050500352 19980505 00352 NM 1998 5 5 UPS96205737 1 19960315 A 5744 6524646501 FITTING BOEING 727 72727C 138400J NM LT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED LT WING, INBOARD AILERON CENTER HINGE FITTING IS CORRODED, WING SIDE. REPLA CED FITTING IAW MM 27-10-1. 2 L 7 3 4F A3WE 1998050500353 19980505 00353 NM 1998 5 5 UPS96205738 1 19960315 A 5751 65931551031 FITTING BOEING 727 72727C 138400J NM LT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED LT WING, INBOARD AILERON CENTER HINGE FITTING IS CORRODED, AILERON SIDE. RE PLACED FITTING IAW SRM 51-30-2, AND OHM 57-50-1. 2 L 7 3 4F A3WE 1998050500354 19980505 00354 NM 1998 5 5 UPS96205739 1 19960316 A 5752 652173619 TAB ASSY BOEING 727 72727C 138400J NM LT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED LT WING, INBOARD AILERON TAB SIDE HINGE FITTINGS ARE CORRODED. REPLACED TAB ASSY. 2 L 7 3 4F A3WE 1998050500355 19980505 00355 NM 1998 5 5 UPS96205740 1 19960316 A 5754 BONDING JUMPER BOEING 727 72727C 138400J NM NR 2 LE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED NR 2 K-FLAP OUTBOARD BULLNOSE BONDING JUMPER UPPER HAS PITTING ON OUTBOARD S IDE OF RIB. REMOVED DAMAGED AREA FAB REPAIR PARTS AND INSTALLED IAW SRM 57-50-3. 2 L 7 3 4F A3WE 1998050500356 19980505 00356 NM 1998 5 5 UPS96205741 1 19960316 A 5753 651920220 CARRIAGE BOEING 727 72727C 138400J NM NR 8 TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON NR 8 CARRIAGE INSIDE SPINDAL BOLT. REMOVED AND REPLACED NR 8 F LAP CARRIAGE ON NRC 437965. 2 L 7 3 4F A3WE 1998050500357 19980505 00357 NM 1998 5 5 UPS96205742 1 19960316 A 5753 65192029 CARRIAGE BOEING 727 72727C 138400J NM NR 1 TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON NR 1 CARRIAGE INSIDE SPINDAL BOLT. REMOVED AND REPLACED NR 1 F LAP CARRIAGE ON NRC 438048. 2 L 7 3 4F A3WE 1998050500358 19980505 00358 NM 1998 5 5 UPS96205743 1 19960315 A 5320 CLIP BOEING 727 72727C 138400J NM BS 734 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 907UP 19118 WHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON STRINGER CLIP BS 734, STR 6 RT. REMOVED AND REPLACED STR TIE P ER SRM 51-30-2, AND MM 53-11-00. 2 L 7 3 4F A3WE 1998050500359 19980505 00359 NM 1998 5 5 UPS96405718 1 19960312 A 5350 WEB BOEING 747 747121 1384871 NM BS 1225 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED WING-TO-BODY FAIRING SUPPORT STRUCTURE, CRACKED FRAME REINFORCEMENT WEB L OWER SIDE, RBL 104, BS 1225. REMOVED DAMAGED SECTION OF WEB AND REPAIRED WEB IAW SRM 51-40-02. 2 L 7 4 4F A20WE 1998050500360 19980505 00360 NM 1998 5 5 UPS96405719 1 19960307 A 5350 WEB BOEING 747 747121 1384871 NM BS 920 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED WING-TO-BODY FAIRING SUPPORT STRUCTURE, CORROSION ON FRAME WEB AND LOWER CHORD AT BS 920, LBL 0/17 AND LBL 47. REMOVED CORROSION PER SRM 51-10-01 ON WEB. REPAIRED LOWER CHORD PER SRM 53-50-04 , FIG 2. 2 L 7 4 4F A20WE 1998050500361 19980505 00361 NM 1998 5 5 UPS96405720 1 19960319 A 5730 SKIN BOEING 747 747121 1384871 NM WS 1140 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED RT WING UPPER SIDE STRIP OF RABBET AREA IS BULGED AT WS 1140. SUBMITTER SUSPECTS CORROSION. REPAIRED IAW DFX 96-063, ISSUE NR 2 APP. PER UPS E.O. EFN 747-57-0314. 2 L 7 4 4F A20WE 1998050500362 19980505 00362 NM 1998 5 5 UPS96405721 1 19960319 A 5730 SKIN BOEING 747 747121 1384871 NM WS 440 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED RT WING UPPER SIDE STRIP OF RABBET AREA IS BULGED AT WS 440. FOUND CORRO SION. REPAIRED IAW DFX 96-064, ISSUE NR 2 APP. PER UPS E.O. EFN 747-57-0315. 2 L 7 4 4F A20WE 1998050500363 19980505 00363 NM 1998 5 5 UPS96405722 1 19960319 A 5730 SKIN BOEING 747 747121 1384871 NM WS 975 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED RT WING UPPER SIDE STRIP OF RABBET AREA IS BULGED AT WS 975. FOUND CORRO SION. REPAIRED IAW DFX 96-062, ISSUE NR 2 APP. PER UPS E.O. EFN 747-57-0313. 2 L 7 4 4F A20WE 1998050500364 19980505 00364 NM 1998 5 5 UPS96405723 1 19960319 A 5330 SKIN BOEING 747 747121 1384871 NM WS 865 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED RT WING SKIN ABOVE UPPER CHORD IS BULDGED AT WS 865. FOUND CORROSION BET WEEN UPPER CHORD AND UPPER SKIN. REPAIR APPROVED PER UPS E.O. EFN 747-57-0312. 2 L 7 4 4F A20WE 1998050500365 19980505 00365 NM 1998 5 5 UPS96405727 1 19960312 A 5330 SKIN BOEING 747 747121 1384871 NM BS 575 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED CRACK IN EQUIP COOLING OUTLET, BS 575 LT, STR 44 AT AFT SIDE. CRACK LENG TH APPROXIMATELY 1.25 INCHES. REPAIRED SKIN IAW KLM-DFX-96-061, APPROVED PER UPS EFN-747-53-0753. 2 L 7 4 4F A20WE 1998050500366 19980505 00366 NM 1998 5 5 UPS96405744 1 19960307 A 5311 FRAME BOEING 747 747121 1384871 NM BS 987.35 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED WING-TO-BODY FAIRING SUPPORT STRUCTURE, FOUND DELAMINATION AND CORROSION ON FRAME LOWER CHORD AT BS 987.35, LBL 24 AND LBL 40. LATCH FILLERS DELAMINATED AT LBL 14 AND LBL 52. REPLACED FRAME L OWER CHORD IAW SRM 51-30-02. REPLACED LATCH FILLERS IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1998050500367 19980505 00367 NM 1998 5 5 UPS96405745 1 19960311 A 5311 FRAME BOEING 747 747121 1384871 NM BS 987.35 DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED WING-TO-BODY FAIRING SUPPORT STRUCTURE, FOUND LOWER CHORD FRAME DELAMINA TED DUE TO CORROSION AT BS 987.35, RBL 57 AND RBL 68. REPLACED FRAME LOWER CHORD IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1998050500368 19980505 00368 NM 1998 5 5 UPS96405746 1 19960306 A 5311 FRAME BOEING 747 747121 1384871 NM BS 2220 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED FINDING CRACK IN UPPER FLANGE OF FRAME AT BS 2220 NEAR S-40 LT. STOP-DRI LLED CRACK AND REPAIRED FRAME UPPER FLANGE IAW TO SRM 51-40-03. 2 L 7 4 4F A20WE 1998050500369 19980505 00369 NM 1998 5 5 UPS96405747 1 19960307 A 5311 FRAME BOEING 747 747121 1384871 NM BS 1008/992 DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 WHILE IN AMS FOR C-CHECK, MAINTENANCE REPORTED WING-TO-BODY FAIRING SUPPORT STRUCTURE, FOUND FRAME/INTERCOSTAL LOWER CHO RD DELAMINATED/CORRODED AT LBL 57, BS 1008, INBOARD, AND BS 992, OUTBOARD. REMOVED DAMAGED SECTION FROM LOWER CHORD AND REPAIRED LOWER IAW SRM 51-40-04. 2 L 7 4 4F A20WE 1998050500370 19980505 00370 WP 1998 5 5 UPS96805706 1 19960211 A 5720 ANGLE DOUG DC8 DC873F 302199F WP BS 70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON CHORD ANGLE, FS 70, BETWEEN LONGERONS 29R-30R. WILL BE RE PAIRED ON TASK CARD 423121. 2 L 7 4 4F RT 4A25 1998050500371 19980505 00371 WP 1998 5 5 UPS96805707 1 19960211 A 5320 GUSSET DOUG DC8 DC873F 302199F WP BS 180 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED AT BAY BIN RT TUNNEL, FS 180, GUSSET HAS HEAVY CORROSION BETWEEN VERTICAL BRA CE. REPLACED GUSSET PER SRM 51-20D. 2 L 7 4 4F RT 4A25 1998050500372 19980505 00372 WP 1998 5 5 UPS96805708 1 19960211 A 5320 GUSSET DOUG DC8 DC873F 302199F WP BS 100 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, A BAY BIN RT TUNNEL, FS 100, VERTICAL SUPPORT GUSSET HAS HEAVY CORROSION. RE PLACED GUSSET PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998050500373 19980505 00373 WP 1998 5 5 UPS96805709 1 19960211 A 5320 WEB DOUG DC8 DC873F 302199F WP BS 1260-1280 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK MAINTENANCE REPORTED RT TUNNEL WEB HAS MODERATE CORROSION AT FS 1260-1280 INBOARD OF LONGERON 21R. REPAIRED WEB PER SRM 53-2-0, FIG 1D. 2 L 7 4 4F RT 4A25 1998050500374 19980505 00374 WP 1998 5 5 UPS96805710 1 19960211 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 980-1000 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION FS 980-1000, SUPPORT ANGLE AT LONGERON 27R INBOARD AND OUTBOA RD SURFACES. REPLACED ANGLE PER SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998050500375 19980505 00375 WP 1998 5 5 UPS96805711 1 19960220 A 5711 SPAR DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK MAINTENANCE REPORTED NR 2 PYLON AREA WING FRONT SPAR AT STR 69, STRAP HAS A .50 INCH LONG CRACK. R EPAIRED PER UPS E.O. DC8-57-0648. 2 L 7 4 4F RT 4A25 1998050500376 19980505 00376 WP 1998 5 5 UPS96805712 1 19960213 A 5315 FLOOR BEAM DOUG DC8 DC873F 302199F WP BS 1680 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON FLOOR BEAM, FS 1680, RBL 35. REPAIRED PER UPS E.O. DC8-53 -1588. 2 L 7 4 4F RT 4A25 1998050500377 19980505 00377 WP 1998 5 5 UPS96805724 1 19960206 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED SKIN BULGED AROUND AIR CONDITIONING DR. CUTOUTS LONGERON CORNERS. REPLACED D OUBLER PER SRM 51-1-20D AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998050500378 19980505 00378 WP 1998 5 5 UPS96805725 1 19960206 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP BS 50-70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION BULGE UNDER LAV. SERVICE DR. REPLACED DOUBLER PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998050500379 19980505 00379 WP 1998 5 5 UPS96805726 1 19960214 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 50-150 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 80-150, LONGERONS 28R, HEAVY CORROSION AROUND FASTENER HOLES. REPLACED LO NGERON SECTION PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998050500380 19980505 00380 WP 1998 5 5 UPS96805728 1 19960220 A 5320 4649643501 FITTING DOUG DC8 DC873F 302199F WP BS 100 R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LONGERON END FITTING AT LONGERON 27R, FS 100, HEAVY CORROSION AND CRACKED. R EPLACED FITTING PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998050500381 19980505 00381 WP 1998 5 5 UPS96805729 1 19960222 A 5313 4613495 LONGERON DOUG DC8 DC873F 302199F WP BS 70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, FS 70, LONGERON 28R, CORROSION BEYOND LIMITS. REPLACED LONGERON SECTION PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998050500382 19980505 00382 WP 1998 5 5 UPS96805730 1 19960213 A 5313 56493285 LONGERON DOUG DC8 DC873F 302199F WP BS 1735 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON LONGERON 26R, FS 1735. REPAIRED PER UPS E.O. 2 L 7 4 4F RT 4A25 1998100900354 19981009 00354 NM 1998 10 9 CA980707032 1 19960531 A 3244 APS01291 TIRE BENDIX 26015711 BOEING 737 737210C 1384459 NM PWA JT8 JT8D9A 52048 NE MLG FAILED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA 7261 687721 (CAN) ON TAKEOFF ROLL BETWEEN V1 AND V2, ABNORMAL VIBRATION WAS NOTICED. ON CLIMB JUST AFTER GEAR RETRACTION, A-HYD PRE SSURE WAS LOST. A/C RETURNED AND LANDED. ONCE STOPPED, THE FOLLOWING CONDITIONS WERE NOTED: NR 1 MAIN WHEEL FUSE PLUG RELEASED DUE TO DISSIPATION OF BRAKE HEAT, NR 2 TIRE TREAD WAS MISSING, AND EVIDENCE OF HYD LEAKAGE IN AND AROUND THE W HEEL WELL AREA. ONCE THE A/C WAS HANGARED AND INSPECTION COMPLETED, FOUND A-SYSTEM HYD LINES SEVERED AND/OR CRACKED. B OTH A-SYSTEM ENGINE DRIVEN PUMPS, ALL MAIN WHEEL ASSEMBLIES, AND BRAKES, AND DAMAGED HYD LINES WERE REPLACED IAW BOEING MM. A/C RETURNED TO SERVICE. PART TC: 29. 2 L 7 2 4F 4 F A16WE E2EA 1999031200241 19990312 00241 NM 1999 3 12 CA960611004 1 19960601 A 3230 574205 VALVE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE MLG BROKEN W A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 CA 20019 306 120421 (CAN) WHEN GEAR SELECTED DOWN NOTHING HAPPENED. AN ALTERNATE GEAR EXTENSION WAS CARRIED OUT. THE LANDING GEAR SELECTOR VALVE REPLACED AND SYSTEM THEN OKAY. PART TC: 21,645. 2 H 7 2 4T 4 T RT A13NM E20NE 1999043000065 19990430 00065 EU 1999 4 30 CA961018018 1 19960927 A 3150 3957900612 EIU AIRBUS 320 A320211 3930320 EU GE CFM56 CFM565A 13802 NE NR 2 ENGINE FAILED W E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 CA 731697 (CAN) IN-FLIGHT SHUTDOWN DUE TO NR 2 ENGINE OIL TEMPERATURE HIGH, UP TO 190 DEGREES. NR 2 ENGINE INTERFACE UNIT AND OIL TEMPERATURE SENSOR P/N 561397 REPLACED. NIL FOUND ON CHIP DETECTOR. 2 L 7 2 4F 4 F RT A28NM E29NE 1999043000069 19990430 00069 NE 1999 4 30 CA961021012 2 19960730 A 7230 BLADE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE 1ST STAGE FAILED W E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION CL CLIMB 1 CA 2632 (CAN) AFTER DOING A REDUCE THRUST TAKEOFF, THE CREW SELECTED CLIMB POWER. THERE WAS AN ABRUPT LOSS OF THRUST AND A LOUD COMPRESSOR STALL AT ABOUT 2,500 FEET. LEFT ENGINE TEMPERATURE EXCEEDED RED LINE FOR 30 TO 40 SECONDS AND WAS SHUT DOWN . NR 1 ENGINE COMPRESSOR STAGE 1 BLADE HIGH CYCLE FATIGUE FAILURE WAS DETERMINED TO BE THE PRIMARY FAILURE. MOST LIKE LY CAUSE OF THE BLADE FAILURE WAS FOREIGN MATERIAL BINDING THE VG FEEDBACK CABLE, CAUSING THE FUEL CONTROL TO IMPROPERLY SCHEDULE VANE ANGLE. 2 L 7 2 4F 4 F RT A21EA E15NE 1999043000070 19990430 00070 GL 1999 4 30 CA961029012 2 19961021 A 7313 5233414 FILTER 5233333 BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE COLLAPSED W O OTHER X ENGINE FLAMEOUT NR NOT REPORTED 1 CA 640 AG41178 CAE833929 (CAN) AIRCRAFT LOST POWER IN-FLIGHT, BUT LANDED WITHOUT INCIDENT. UNABLE TO RESTART. THE SCREEN FILTER WAS FOUND COLLA PSED. 1 G 7 1 3U 3 U H2SW E4CE 1999081200317 19990812 00317 NE 1999 8 12 CA960212010 2 19960129 A 7260 3037223 CARBON SEAL DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE NR 2 ENGINE LEAKING W C ABORTED TAKEOFF K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 CA 123030 (CAN) ON TAKEOFF ROLL, NR 2 ENGINE OIL PRESSURE WARNING LIGHT ON. TAKEOFF REJECTED. ENGINE OIL LEVEL FOUND DOWN 7 LITR ES. 2 H 7 2 4T 4 T RT A13NM E20NE 2000051600108 20000516 00108 SW 2000 5 16 CA970311064 1 19961121 A 5312 BULKHEAD BELL 206031302241 BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA CAE800471BA (CAN) BULKHEAD FOUND CRACKED BEYOND REPAIRABLE LIMITS. 1 G 7 1 3U 3 U H2SW E4CE 2000051600109 20000516 00109 SW 2000 5 16 CA970311067 1 19960930 A 5302 SKID BELL 206020110005 BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL TAIL BOOM MISSING W K NONE O OTHER IN INSP/MAINT 1 CA CAE822647 (CAN) FOLLOWING FLIGHT, IT WAS NOTED THAT THE TAIL SKID ASSY WAS MISSING. NO DAMAGE WAS FOUND TO VERTICAL FIN OR TAIL S KID ATTACHEMENT FITTING. 1 G 7 1 3U 3 U H2SW E4CE 2000051600110 20000516 00110 EA 2000 5 16 CA970311069 1 19961016 A 6410 BLADE SIERRA 117030201041 CARSON S61 S61LSKRSKY EA GE CT58 CT581401 30011 NE TAIL ROTOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 8520 213 GIVR783777 295059 (CAN) T/R BLADE SKIN WAS FOUND CRACKED NEAR THE BLADE ROOT. 2 G 7 2 4U 4 U H8EA 1E3 2000051600111 20000516 00111 EU 2000 5 16 CA970311070 1 19961208 A 6410 BLADE EVEREADY 355A12003113 SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE TAIL ROTOR DELAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA 3022 2323 840 (CAN) DELAMINATION WAS FOUND ON T/R BLADE LOCATED 5 INCHES FROM TIP AND 1.5 INCHES FROM LEADING EDGE. NO VISIBLE SIGN O F FOD OR VIBRATION REPORTED. DEFECT FOUND DURING TURN AROUND INSPECTION. 1 G 7 1 3U 3 U H9EU E19EU 2000051600132 20000516 00132 SW 2000 5 16 CA970311063 1 19961121 A 5320 STIFFENER BELL 206031003123 BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA CAE800471BA (CAN) THE STIFFENER THAT IS LOCATED BENEATH THE DOUBLER FOR EXTERNAL SCAVENGE OIL FILTER KIT WAS FOUND CRACKED. ONE OF THE NUTS HOLDING THE OIL FILTER WAS LOCATED TOO CLOSE TO THE RADIUS OF THE STIFFENER WHICH WAS THE CAUSE OF THE CRACK 1 G 7 1 3U 3 U H2SW E4CE 2001050300394 20010503 00394 EU 2001 5 3 20010427CW002 1 19960604 A 5620 WINDOW BRAERO DH125 HS125700A 4230170 EU GARRTT TFE731 TFE731* 01518 WP CABIN CRACKED D O OTHER O OTHER NR NOT REPORTED 1 SO 05 47PB 1100 257055 CABIN WINDOW CRACKED .7500 WAY AROUND. 2 L 7 2 4F 4 F A3EU E6WE 1996020200587 19960202 00587 WP 1996 2 2 9602299101 1 19960128 A 3397 WIRE DOUG DC9 DC915 3022036 WP CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 91S 47063 AFT CABIN CEILING EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE FOUND WIRE L794C18 FROM RIGHT LAV FORWARD POWER SUPPLY TERM INAL NR 5 GROUNDED. RECONNECTED WIRE TO AFT EXIT DOOR EMERGENCY LIGHTS. OPERATIONAL CHECK GOOD. 2 L 7 2 4F A6WE 1996050200396 19960502 00396 WP 1996 5 2 MWEA96125 1 19960430 A 3397 WIRE DOUG DC9 DC914 3022034 WP AFT ACCESSORY CHAFED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 400ME 45727 DURING SERVICE CHECK, FOUND TAIL COMPT FLOOR TRACK LIGHTING INOP. FOUND BLOWN FUSE IN BATTERY POWER SUPPLY CAUSED BY CH AFED WIRES IN CATWALK. REPAIRED WIRES AND REPLACED FUSE. 2 L 7 2 4F A6WE 1996071800356 19960718 00356 WP 1996 7 18 DLL15961570 1 19960702 A 2440 WIRE LKHEED 1011 10113853 5265020 WP EXTERNAL POWER BURNED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 752DA 193W1172 DURING SWITCH OVER FROM EXT PWR TO APU PWR TOTALLY LOST ALL ELECTRICAL POWER. CHECK FOUND EXT PWR RLY 2441-K1 BURNED AN D ALL 6 FEEDER WIRES FROM RECEPT AT RELAY BURNT. 2 L 7 3 4F A23WE 1996081500571 19960815 00571 NM 1996 8 15 TWRA96131 1 19960710 A 3397 WIRE BOEING 747 747212B 1384886 NM COCKPIT BROKEN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 620FF 21162 DURING DAILY CHECK, FOUND EMERGENCY EXIT LIGHT INOP ON WALL FORWARD OF CREW EXIT DOOR. REPAIRED BROKEN WIRE AT BACK OF SIGN, OPS CHECK GOOD PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996081500635 19960815 00635 NM 1996 8 15 TWRA9690 1 19960706 A 3397 WIRE BOEING 747 747212B 1384886 NM CABIN BROKEN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY SERVICE, FOUND BETWEEN 1KH AND 6KH FLOOR EMERGENCY LIGHTS INOP. REPAIRED BROKEN WIRE UNDER SEAT OPS CHECK PER MM 33-51-00 PAGE 501. (M) 2 L 7 4 4F A20WE 1996082900780 19960829 00780 NM 1996 8 29 TWRA96264 1 19960802 A 3397 WIRE BOEING 747 747121 1384871 NM CABIN BROKEN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 609FF 20354 DURING DAILY CHECK, FOUND EVAC LIGHT UPPER DECK NEAR FLOOR FORWARD OF CREW SLIDE IS INOPERATIVE. REPAIRED BROKEN WIRE T O LIGHT ASSEMBLY. OPS CHECKED NORMAL PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1996090500525 19960905 00525 NM 1996 9 5 TWRA96228 1 19960724 A 3397 WIRE BOEING 747 747238B 1384828 NM CABIN SHORTED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 614FF 20534 DURING DAILY CHECK, FOUND UPPER DECK ALL FLOOR EVAC LIGHTS INOP. FOUND WIRE SHORTED TO GROUND. REPAIRED WIRING PER MM 33-51-13. OPS CHECKED PER MM 33-51-00 PG 501. (M) 2 L 7 4 4F A20WE 1996092600503 19960926 00503 NM 1996 9 26 AWXA960422 1 19960807 A 3397 WIRE BOEING 737 737297 1384480 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 147AW 22630 PHX - FLT 2081 - DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 11 EMERGENCY LIGHT INOP. REPAIRED WIRE. OPS CHECK OK. (M ) 2 L 7 2 4F A16WE 1996092600542 19960926 00542 NM 1996 9 26 AWXA960470 1 19960903 A 3397 WIRE BOEING 737 7372A6 138448B NM CABIN DISCONNECTED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 145AW 20194 PHX - FLT 2887 - REF MEL 33-19, EMERGENCY LIGHT ROW 12 INOP. RESPLICED WIRE AT ROW 12. OPS CHECK GOOD. MEL CLEARED. ( M) 2 L 7 2 4F A16WE 1996092600588 19960926 00588 EU 1996 9 26 SIMA962352 1 19960822 A 3397 WIRE AEROSP ATR72 ATR72212 8680945 EU CABIN BROKEN A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 434AT 434 DFW - FLT 3826 - AIRSTAIR EMERGENCY LIGHT INOP. REPAIRED BROKEN WIRES IN CANNON PLUG. AIRCRAFT WAS RETURNED TO SERVIC E. (M) 2 H 7 2 4T RT A53EU 1996080800266 19960808 00266 NM 1996 8 8 P5CA9600469 1 19960803 A 2710 CONTROL CABLE BOEING 747 747123 1384873 NM WS 435 FRAYED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LEFT WHEEL WELL AILERON CONTROL CABLE AA-9 HAS BROKEN STRAND AT REAR SPAR WS 435. REPLACED CABLE PER BOEING MAINTENANCE MANUAL 20-11-03 AND 27-11-00. 2 L 7 4 4F A20WE 1996060600249 19960606 00249 WP 1996 6 6 96UAL900380 1 19960530 A 3397 WIRE DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1845U 48261 EMERGENCY EXIT FLOOR LIGHTS INOPERATIVE IN ZONE-C. POWER SUPPLY CABLE DAMAGED, REPLACED CABLE ASSEMBLY. 2 L 7 3 4F 4 F A22WE E23EA 1996090500148 19960905 00148 CE 1996 9 5 96ZZZX4240 1 19960703 A 7603 5038901229 CONTROL CABLE BEECH 58 58 1152740 CE RT THROTTLE BROKEN A BSYA O OTHER O OTHER NR NOT REPORTED 1 GL 07 4AW TH450 FOUND BROKEN THROTTLE (RT) CABLE. REMOVED AND REPAIRED CABLE ASSY. 1 L 7 2 3O 3A16 1996020200166 19960202 00166 WP 1996 2 2 ABXA9600109 1 19960124 A 7620 3701161503 CONTROL CABLE DOUG DC8 DC861 3021952 WP NR 2 PYLON BROKEN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 850AX 45894 NR 2 ENGINE FIRE SHUTOFF CABLE BROKEN IN PYLON. REPLACED PNEUMATIC SHUTOFF CABLE RUN 59.1 IN NR 2 PYLON AND OPS CHECK G OOD. 2 L 7 4 4F 4A25 1996062700148 19960627 00148 WP 1996 6 27 ABXA9600512 1 19960618 A 3297 WIRE DOUG DC8 DC861 3021952 WP MLG BROKEN A ABXA O OTHER O OTHER LD LANDING 1 GL 23 850AX 45894 ALL BRAKE ACTION WAS LOST AT APPROXIMATELY 20 KIAS DURING ROLLOUT. FLIGHT CREW SELECTED ANTI-SKID OFF TO PREVENT AIRCRA FT FROM GOING INTO OVERRUN AREA. REPLACED ANTI-SKID CONTROL BOX IAW DC8 MM AND OPS CHECK WAS GOOD. FURTHER INVESTIGATI ON REVEALED BROKEN WIRES ON THE NR 2, NR 4, NR 6 AND NR 7 ANTI-SKID TRANSDUCERS. WIRING WAS REPAIRED IAW DC8 WDM AND OP S CHECK OF ANTI-SKID SYSTEM WAS GOOD. 2 L 7 4 4F 4A25 1996062700208 19960627 00208 EA 1996 6 27 COMA9660111 1 19960622 A 3297 WIRE CNDAIR CL600 CL6002B19 1900309 EA ANTI-SKID SYST LOOSE A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 962CA 7123 ANTI-SKID CAUTION MESSAGE ON EICAS. REPAIRED LOOSE WIRING AT CONNECTOR P184. 2 L 7 2 4F RT A21EA 1996082900690 19960829 00690 NM 1996 8 29 ASAA9640066 1 19960801 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 772AS 25105 SEA - DURING MAINTENANCE CHECK, THE AFT 2 EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRES AND LIG HTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996091200327 19960912 00327 NM 1996 9 12 ASAA9640069 1 19960810 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 756AS 25097 SEA - FLT 99 -AFT SECTION OF EMERGENCY EXIT FLOOR TRACK LIGHTS INOP. RECONNECTED TRACK WIRING AND LIGHTS OPERATED NORMA LLY. (M) 2 L 7 2 4F RT A16WE 1996091900755 19960919 00755 NM 1996 9 19 ASAA9640071 1 19960824 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 782AS 25113 SEA - DURING MAINTENANCE CHECK, THE FORWARD THREE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECON NECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1996111400334 19961114 00334 NM 1996 11 14 ASAA9640090 1 19961014 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 756AS 25097 SEA - DURING MAINTENANCE CHECK, THE AFT SECTION OF EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTE D LOOSE TRACK WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1997020600669 19970206 00669 NM 1997 2 6 ASAA9640100 1 19961213 A 3397 WIRE BOEING 737 7374Q8 138447Q NM OVERWING EXIT DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 771AS 25104 PHX - FLT 721 - PRIOR TO DEPARTURE, THE CREW REPORTED THAT THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPER ATIVE AT THE OVERWING EMERGENCY EXIT. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1997010900438 19970109 00438 NE 1997 1 9 97ZZZX103 2 19961017 A 7250 411105064 ROTOR ASSY LYC LTS101 LTS101650B1 41560 NE GAS PROD DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 1210 SC4102 LE45322E ROTOR ASSY DUE SB LT101-72-10-0150. REQUIRES DISASSEMBLY AND INSPECTION OF THE ROTOR BROACH SLOTS FOR POSSIBLE CRACKS I N THE DISC/TENON AREA. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. PART TOTAL CYCLES, 4926.5. 3 U E5NE 1996071800638 19960718 00638 1996 7 18 HEEA967572 4 19960710 A 3457 0110010602 GPS165 GARMIN COCKPIT GPS KNOB BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 GPS KNOB BROKEN.TIME SINCE REPAIR 0:00. 1997030600208 19970306 00208 1997 3 6 SCNA97040 4 19961002 A 2561 3500113 CYLINDER VALVE LIFE VEST LEAKING A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 LIFE VEST WAS REJECTED DUE TO CYLINDER VALVE LEAKING. 1996100300682 19961003 00682 SO 1996 10 3 96ZZZX4972 2 19960912 A 8530 SA501867 WASHER SUPAIRPART CONT O360 TSIO360KB 17025 SO ROCKER ASSY BREAKS A A HLVA K NONE O OTHER IN INSP/MAINT 1 SW 03 CYLINDER ROCKER ASSY TAB WASHER LOCK TABS BREAK OFF OR CRACK WHEN BENT TO SECURE ROCKER BOLT. WASHER PN SA501867, LOT N R 514064 MFG DATE 7-26-96. ONE REPAIR STATION REPORTS 12 OF 12 WASHER TABS BROKE ON INSTALLATION. 3 O E9CE 1996051600501 19960516 00501 GL 1996 5 16 HEEA967091 2 19960502 A 7250 23032327 SEAL ALLSN 250C 250C30P 03013 GL NR 5 STATIONARY BORE OVERSIZE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 UPON INSPECTION OF PART FOUND THE #5 STATIONARY LAB SEAL BORE I.D. .006 OVERSIZE. 3 U E1GL 1996111400619 19961114 00619 1996 11 14 CA960418014 1 19960327 A 7800 L242667701420 BRACE EYE MORAVN L24266701420 LYC O360 AEIO360A1B6 41514 EA RT EXH STRUT BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 3566 L2652551A (CAN)RIGHT HAND EXHAUST BRACE STRUT THREADED END FOUND BROKEN ABOVE THE JAM NUT. THIS ALLOWED THE BROKEN END TO POSITION ITSELF IN THE TRAVEL RANGE OF THE THROTTLE LEVER ON THE FUEL INJECTOR METERING UNIT.SUBMITTER REPORTS THAT THE VIBRATIO N LEVELS AS WELL AS THE SHARP CUT THREADS MAY HAVE CONTRIBUTED TO THE CRACKING OF THE EYE END OF THE BRACE. 3 O 1E10 1997011600094 19970116 00094 NE 1997 1 16 CA960229003 2 19960228 A 7261 SEALS LYC ALF502 ALF502R5 41580 NE HP COMPRESSOR OIL LEAK W D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA LF05539A (CAN) AFTER ENGINE START, CABIN FILLED WITH SMOKE, #3 ENGINE FOUND TO HAVE OIL IN HP COMPRESSOR SECTION. ENGINE REPLACED . SUBMITTER SUSPECTS COMPANY CAMPAIGN TO CHANGE OIL FROM EXXON 2380 TO CASTROL 5000. OIL IS BEING CHANGED BACK AND #1 AN D #9 BEARING SEALS REPLACED. 4 F E6NE 1996121200287 19961212 00287 1996 12 12 CA960625016 1 19960610 A 7110 14171023409 AIR SCOOP BAG GARRTT TPE331 TPE33114HR 01514 NE RH INB NAC MISSING W K NONE D INFLIGHT SEPARATION NR NOT REPORTED 1 CA 3124 P75060 (CAN) CAPTAIN REPORTED THAT THE RIGHT NACELLE, ZONE 2, LEFT INBOARD JETPIPE COWLING AIR SCOOP WAS MISSING. JETSTREAM ISS UED A TECHNICAL/OPERATIONAL RESPONSE ALLOWING AIRCRAFT TO REMAIN IN SERVICE FOR SEVEN DAYS. 4 T E18NE 1999043000067 19990430 00067 GL 1999 4 30 CA961021002 2 19961002 A 7210 6875027 BEARING 6894171 ALLSN 250C 250C20B 03013 GL GEARBOX SPALLED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 4240 CAG39213 CAE835711 (CAN) DURING FIRST START, THE NR 2 ENGINE CHIP LIGHT ON. ENGINE SHUT DOWN. CHIP PULSE ACTIVATED AND LIGHT WENT OUT. O N NEXT START, THE CHIP LIGHT CAME ON AGAIN, ENGINE SHUT DOWN. CHIP PLUGS CHECKED AND FILTER REPLACED. IT HAD MANY FLAK ES, BUT WITHIN LIMITS. 30 MINUTE GROUND RUN CARRIED OUT, AND CHIPS CHECKED AGAIN WITH FLAKES. EACH TIME THIS TRIED AFT ER OIL AND FILTERS REPLACED, THE FLAKES WERE STILL INCREASING. NR 2 1/2 BEARING FOUND TO HAVE FLAKING ON ROLLERS. GEA RBOX ASSY REPLACED. 3 U E4CE 1996071800621 19960718 00621 1996 7 18 HEEA967519 1 19960705 A 2435 03600918 BEARING LUCAS START GEN FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 START/GEN HAS HIGH PITCH SQUEAL. 1996051600429 19960516 00429 1996 5 16 HEEA967009 1 19960417 A 2435 03600918 BEARING START GEN NOISY E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 START GENERATOR HAS HIGH PITCH SQUEAL WHEN RUNNING. 1996092600337 19960926 00337 1996 9 26 SCNA96255 4 19960917 A 2561 3500113C LIFE VEST CABIN INOPERATIVE A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 LIFE VEST WAS REJECTED DUE TO NON PASSING OF AIR RETENTION TEST, SEVERAL HOLES WERE FOUND IN VEST. 1996042500469 19960425 00469 1996 4 25 HEEA966941 4 19960408 A 3413 7130 INDICATOR COCKPIT VSI INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 VERT SPEED INDICATOR INOPERATIVE. WILL NOT RETURN TO ZERO ALL OF THE TIME. 1996121200512 19961212 00512 NE 1996 12 12 CA960222025 2 19960207 A 7250 212114210 BLADE LYC 212111033 LYC ALF502 ALF502R5 41580 NE 2ND TURBINE RUPTURED W A A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 CA 6076 1652 M423484 LF05560A (CAN) AIRCRAFT DEPARTED AND AT TOP OF CLIMB #4 ENGINE ENCOUNTERED A VIBRATION REGISTERING 1.8 I.P.S.AIRCRAFT RETURNED TO BASE FOR MAINTENANCE INVESTIGATION. ENGINE SHOP TEARDOWN REVEALED A SINGLE 2ND TURBINE BLADE RUPTURE, WHICH CAUSED SIGN IFICANT DOWNSTREAM GAS PATH DAMAGE (WHICH PREVENTS 3RD TURBINE ROTATION BY HAND DUE TO DEBRIS LOGED BETWEEN TIP AND SHRO UD). 2ND GP TURBINE BLADE TO 2ND NOZZLE TIP CLEARANCES WITHIN MANUFACTURERS RECOMMENDED DIMENSIONS. NO EVIDENCE OF BLADE TIP CONTACT WITH 2ND NOZZLE ABRAIDABLE SEAL. 2ND GP ASSEMBLY VISUALLY, DIMENSIONALLY, AND F.P.I. INSPECTED WHEN NEW BY OVERHAUL FACILITY. 4 F E6NE 1996101000919 19961010 00919 1996 10 10 CA960214013 1 19960123 A 7920 L52671033 FITTING LYC O360 AEIO360A1B6 41514 EA OIL LINE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 152 L26408518 (CAN) PILOT NOTICED OIL LEAK ON WALK AROUND. LEAK TRACED TO OIL LINE FITTINGS, WHICH LACKED THE REQUIRED SEALANT. SEAL ANT APPLIED AND SYSTEM CHECKED OUT OK. 3 O 1E10 1996082200164 19960822 00164 GL 1996 8 22 HEEA967650 2 19960813 A 7260 23033437 GEARBOX COVER ALLSN 250C 250C20B 03013 GL GR BOX OIL SCAV MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 RECEIVING INSPECTION REVEALED: O RING GROOVE FINISH MACHINING NOT COMPLIED WITH ON GEARBOX COVER OIL SCAVENGE PORT AS M ARKED. 3 U E4CE 1996120500383 19961205 00383 NE 1996 12 5 CA960605008 2 19960529 A 7250 212114221 BLADE LYC 212111033 LYC ALF502 ALF502R5 41580 NE NR 3 ENG TURB FRACTURED W A A UNSCHED LANDING R E PARTIAL RPM/PWR LOSS VIBRATION/BUFFET CL CLIMB 1 CA 6474 2140 M432969 LFO5483A (CAN)AT TOP OF CLIMB, #3 ENGINE VIBRATION SUDDENLY ESCALATED TO 3.0 IPS, N1 DECAY ALSO EVIDENT, ENGINE SHUTDOWN. BOROSCO PE INSPECTION REVEALED ONE RUPTURED BLADE ON #2 G.P. TURBINE DISC. 4 F E6NE 1996121200341 19961212 00341 NE 1996 12 12 CA960717006 2 19960710 A 7530 216017203 PIN PISTON LEVER 21603529 LYC ALF502 ALF502R5 41580 NE BLEED ACTUATOR MISSING W A E ENGINE SHUTDOWN E VIBRATION/BUFFET CR CRUISE 1 CA LF05556A (CAN) IN CRUISE VIBRATION INDICTION WENT TO 1.3 IPS AND VIBRATIONS WERE FELT ON THE FLIGHT DECK. ENGINE WAS SHUTDOWN. PO ST FLIGHT ENGINE BOROSCOPE INSPECTION WAS CARRIED OUT WITH NO FAULT FOUND. ENGINE GROUND RUN. BLEED BAND FOUND NOT TO BE OPENING DUE TO PISTON LEVER PIN BEING ABSENT (MISSING). BLEED BAND ACTUATOR REPLACED AND AIRCRAFT RETURNED TO SERVICE. 4 F E6NE 1996062700442 19960627 00442 1996 6 27 HEEA967330 4 19960604 A 2312 063100700 TRANSCEIVER KTR993 COCKPIT MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 WILL TRANSMIT BUT NOT RECEIVE. 1996110100039 19961101 00039 GL 1996 11 1 CA960311036 2 19960228 A 7310 R13306 WASHER ALLSN 250C 250C20B 03013 GL FITTING LEAKING W K NONE O OTHER IN INSP/MAINT 1 CA CAE836045 (CAN)FUEL LEAK CAUSED BY SEALING WASHER ON BANJO FITTING NOT PROPERLY SEALING. 3 U E4CE 1996110100409 19961101 00409 1996 11 1 CA960318004 1 19960315 A 8011 501113775 STARTER PLESSEY LYC ENGINE MALFUNCTION W H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 CA 9595 1020 TE0875 (CAN)STARTER OPERATING LIGHT ON INTERMITTENTLY IN CRUISE, AND CAME ON STEADY AFTER LANDING. LIGHT WENT OUT ON SHUTDOWN. STARTER REPLACED. 1996071800597 19960718 00597 GL 1996 7 18 HEEA967491 2 19960627 A 7230 23007196 REAR SUPPORT 23005200 ALLSN 250C 250C28B 03013 GL ENG COMP DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 CAC70234 CAE860662 ENGINE DISASSEMBLED DUE TO LOW POWER AND HIGH COMPRESSOR VIBS ON TEST CELL. UPON INSPECTION OF COMPRESSOR PARTS NOTED T HE FOLLOWING: COATING LIFTING ON REAR SUPPORT MAJOR AND MINOR SEALS. REPLACED DISCREPANT PART. 3 U E1GL 1996080800708 19960808 00708 1996 8 8 HEEA967612 4 19960731 A 3451 066106900 INDICATOR KDI572 COCKPIT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 INDICATOR UNIT WAS ON FOR ONE HOUR, RESISTOR BURNT INSIDE. 1996022300355 19960223 00355 1996 2 23 HEEA966648 4 19960206 A 3442 MI585200 RADAR RT COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 RADAR UNIT NOT TRACKING CORRECTLY. TIME SINCE REPAIR 0:00. 1996021600472 19960216 00472 1996 2 16 HEEA966561 4 19960131 A 3416 212070238003 INDICATOR MASCO COCKPIT LOOSE PARTS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 ALTIMETER HAS LOOSE PART INSIDE. 1996061300474 19960613 00474 1996 6 13 HEEA967206 4 19960509 A 3424 S27200B14 INDICATOR TURN & BANK DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 INDICATOR NEEDLE POINTS 6 FEET OFF CENTER WHILE STILL. 1997030600213 19970306 00213 1997 3 6 SCNA97045 4 19961209 A 2561 P0723103 LIFE VEST CABIN FAILED TEST A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 LIFE VEST DID NOT PASS ALL TESTS AND WERE REJECTED. 1996051600439 19960516 00439 1996 5 16 HEEA967020 4 19960417 A 3416 212070238003 INDICATOR COCKPIT STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 EXCESSIVE CASE LEAK AND NEEDLE STICKS AT ZERO. TIME SINCE REPAIR 0:00. 1996021600478 19960216 00478 1996 2 16 HEEA966567 4 19960131 A 3416 212070238003 INDICATOR MASCO COCKPIT FRICTION ERROR E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 INDICATOR NEEDLE HAS EXCESSIVE FRICTION ERROR. 1996120500371 19961205 00371 1996 12 5 CA960604006 1 19960524 A 7810 115024003 DIFFUSER LYC T53 T5317A 41549 NE EXH MID CONE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 839 LR81008 (CAN)ON ROUTINE INSPECTION, 2 INCH CRACK JUST FORWARD OF THE 12 O'CLOCK STRUT RUNNING CIRCUMFERENTIALLY AROUND THE EXHAU ST DIFFUSER MID CONE. 4 U E17EA 1996080200186 19960802 00186 1996 8 2 SCNA96204 4 19960716 A 2561 P0723103 LIFE VEST UNDER SEAT FAILED TEST A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 LIFE VEST FAILED INSPECTION/TEST. 1996091900836 19960919 00836 1996 9 19 TAOA089611 4 19960827 A 2564 D1789445 RAFT AIRCRUISERS CABIN DEPLOYED A TAOA O OTHER O OTHER IN INSP/MAINT 1 EA 15 3940001 FLIGHT ATTENDANT TRAINING, DEPLOYED RAFT. RAFT INFLATION AND EMERGENCY EQUIPMENT CHECKED NORMAL. (M) 1996121200340 19961212 00340 NE 1996 12 12 CA960716004 2 19960712 A 7260 MS956505 BOLT 208314801 LYC ALF502 ALF502R5 41580 NE ACCESSORY GEARBX PULLED OUT W A K NONE J WARNING INDICATION IN INSP/MAINT 1 CA 16078 LF05545A (CAN) ACCESSORY GEARBOX REMOVED DUE TO GEAR MATERIAL FOUND IN THE CHIP DETECTOR. ON TEARDOWN THE BOLTS (P/N MS9565-05) T HAT HOLD THE SHIELD (P/N 2-083-148-01), AND THE REST OF THE ASSEMBLY FOR THE BEVEL INPUT DRIVE GEAR, WERE FOUND PULLED O UT OF THE CASE ASSEMBLY (P/N 2-083-270-04). THIS CAUSED THE DRIVE GEAR TO BECOME PARTIALLY DISENGAGED WITH ENOUGH SLOP T O CAUSE MATERIAL TO BE WORN OFF THE GEAR TEETH. CAUSE OF THE BOLTS BEING PULLED OUT OF THE CASE IS SPECULATIVE AND THE A CTUAL CAUSE HAS NOT BEEN DETERMINED. 4 F E6NE 1996051600445 19960516 00445 1996 5 16 HEEA967026 4 19960417 A 3416 A30 ENCODER COCKPIT FAULTY E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 UNIT HAS AN INCONSISTENT OUTPUT AND WILL NOT CALIBRATE. 1997010200177 19970102 00177 NE 1997 1 2 CA960723514 2 19960503 A 7261 LP09 TUBE PWA 4056 PW4056 NE NR 1 ENG OIL FRACTURED W E ENGINE SHUTDOWN J K WARNING INDICATION FLUID LOSS DE DESCENT 1 CA 17740 P724312 (CAN) #1 ENGINE OIL PRESSURE DROPPED TO ZERO 3 HOURS PRIOR TO LANDING, ENGINE SHUT DOWN AT 70 PSI OIL PRESSURE. LP09 OIL LINE LEAKING AT ANGLE GEARBOX. 4 F E24NE 1996110100578 19961101 00578 NE 1996 11 1 CA960320545 2 19960215 A 7261 ENGINE PWA JT9 JT9D7 52054 NE OIL FILTER BYPASS WARNING W E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 CA 10205 P695767 (CAN) PRIOR TO ARRIVAL, THE #2 ENGINE WAS SHUT DOWN WHEN OIL FILTER BYPASS LIGHT CAME ON. 4 F E20EA 1996082200165 19960822 00165 GL 1996 8 22 HEEA967651 2 19960813 A 7230 23031922 SHAFT ALLSN 250C 250C20 03013 GL SPUR ADAPTER MIS MARKED E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 RECEIVING INSPECTION REVEALED: DUPLICATE SERIAL NUMBER ON SPUR GEAR. 3 U E4CE 1996100300082 19961003 00082 1996 10 3 SCNA96264 4 19960919 A 2561 P0723103 LIFE VEST CABIN DAMAGED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 LIFE VEST WAS REJECTED DUE TO SEVERAL HOLES FOUND IN THE INFLATION TUBE. 1996112700062 19961127 00062 NE 1996 11 27 CA960524001 2 19960517 A 7250 BLADE LYC 212109063 LYC ALF502 ALF502R5 41580 NE #1 TURBINE DISC FRACTURED W A C ABORTED TAKEOFF R Y PARTIAL RPM/PWR LOSS ENGINE STOPPAGE TO TAKEOFF 1 CA 7516 LF05491A (CAN)ON TAKEOFF JUST AFTER POWER SET, A BANG HEARD & #3 FAN SPEED DROPPED TO "0" RPM. TAKEOFF REJECTED & #3 ENGINE SHUTD OWN. ENGINE TEARDOWN REVEALED SEVERE DAMAGE STARTING AT THE #1 TURBINE DISC REARWARD.NO DAMAGE NOTED AHEAD OF THE DISC O THER THAN THE TRAILING EDGE OF THE #1 NOZZLE WHICH INDICATES A BLADE FAILURE ON THE #1 TURBINE DISC. 4 F E6NE 1996021600475 19960216 00475 1996 2 16 HEEA966564 4 19960131 A 3416 212070238003 INDICATOR MASCO COCKPIT LOOSE PARTS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 INDICATOR HAS LOOSE PARTS INSIDE. 1996121200265 19961212 00265 GL 1996 12 12 CA960620001 2 19960606 A 7230 COMPRESSOR ALLSN 501D 501D13 03004 GL ENGINE FOD DAMAGE W A E UNSCHED LANDING ENGINE SHUTDOWN M O OVER TEMP OTHER CL CLIMB 1 CA 501599 (CAN)INVESTIGATION OF ENGINE COMPRESSOR REVEALED FOD DAMAGE. COMPRESSOR REPLACED AND AIRCRAFT RETURNED TO SERVICE. 4 T E282 1997011600098 19970116 00098 NE 1997 1 16 CA960304002 2 19960301 A 7261 SEALS LYC ALF502 ALF502R5 41580 NE #2 ENGINE LEAKING W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA 15287 LF05463A (CAN) AIRCRAFT RETURNED TO AIRPORT WITH AIR CONDITIONING PROBLEM. #1 SEAL IN #2 ENGINE FOUND LEAKING. PROBLEM IS SUSPECT ED TO BE DUE TO COMPANY CAMPAIGN TO CHANGE OIL FROM EXXON 2380 TO CASTROL 5000. SEAL REPLACED AND OIL CHANGED BACK TO E XXON 2380. 4 F E6NE 1997030600211 19970306 00211 1997 3 6 SCNA97043 4 19961022 A 2561 P0723103C LIFE VEST CABIN FAILED TEST A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 LIFE VEST DID NOT PASS ALL TESTS. 1996070300444 19960703 00444 1996 7 3 HEEA967361 1 19960605 A 2435 03600918 BEARING START/GEN FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 HIGH PITCH SQUEAL. 1996051600411 19960516 00411 GL 1996 5 16 HEEA966984 2 19960410 A 7240 23056130 COMBUSTION LINER 6898735 ALLSN 250C 250C20B 03013 GL ENG DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 CAT33864 UPON ATTEMPTING ASSEMBLY FOUND THE IGNITOR AND FUEL NOZZLE BORE DO NOT ALIGN WITH NUMEROUS COMBUSTION CASES. 3 U E4CE 1998041700416 19980417 00416 GL 1998 4 17 CA960813007 2 19960730 A 7250 6726656244 RETAINING RING ALLSN 250C 250C20B 03013 GL NR 5 BEARING DETACHED W A K NONE J WARNING INDICATION LD LANDING 1 CA CAE830398 (CAN) MAG PLUG LIGHT ON ENGINE NR 2. FOUND METAL ON BOTH PLUGS AND ON DISASSEMBLY FOUND THE RETAINING RING AND THE FLAT WASHER WHICH HOLD THE NR 5 BEARING OUTER RACE, RESTING IN THE BEARING BORE AREA. IT WAS UNDETERMINED HOW THE RING CAME OUT OF ITS GROOVE OR WHETHER IT WAS INSTALLED PROPERLY TO BEGIN WITH. THE POWER TURBINE WAS FREE TO MOVE AXIALLY AS THE NR 5 BEARING IS THE THRUST BEARING IN THIS CASE. 3 U E4CE 1996080200189 19960802 00189 1996 8 2 SCNA96208 4 19960716 A 2561 P0723103W LIFE VEST UNDER SEAT FAILED TEST A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 LIFE VEST FAILED INSPECTION/TEST. 1997010200201 19970102 00201 NE 1997 1 2 CA960723539 2 19960608 A 7200 ENGINE PWA JT9 JT9D7R4D 52054 NE #1 POSITION FAULTY W A C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CA P707550 (CAN) DURING ENGINE ACCELERATION ON TAKEOFF ROLL COMPRESSOR STALLED ON #1 ENGINE AT 20 KNOTS. ALL OTHER ENGINE PARAMETER S NORMAL. ON SECOND TAKEOFF ROLL AT 2000 FEET EGT STARTED TO RISE. TAKEOFF WAS ABORTED. #1 ENGINE WAS REPLACED. PRELIMIN ARY REPORT. 4 F E3NE 1996021600474 19960216 00474 1996 2 16 HEEA966563 4 19960131 A 3416 212070238003 INDICATOR MASCO COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 INDICATOR LEAKS AT BAROMETRIC KNOB. 1997011600110 19970116 00110 WP 1997 1 16 CA960306020 2 19960202 A 7220 31055017 INLET SENSOR GARRTT TFE731 TFE73122B 01518 WP MCAULY 2D34C B2D34C202 GL NR 2 ENG FAILED W K NONE O OTHER TX TAXI/GRND HDL 1 CA P76064 950511 (CAN) PILOT REPORT THAT #2 ENGINE WOULD NOT REDUCE TO TAXI SPEED. INLET SENSOR REPLACED, ASSOCIATED ENGINE GROUND RUNS C ARRIED OUT. AIRCRAFT RETURNED TO SERVICE. 4 F E6WE 5 C P7EA 1996080200187 19960802 00187 1996 8 2 SCNA96205 4 19960716 A 2561 P0723103 LIFE VEST UNDER SEAT FAILED TEST A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 LIFE VEST FAILED INSPECTION/TEST. 1996022300356 19960223 00356 1996 2 23 HEEA966649 4 19960206 A 3442 MI585200 RADAR RT COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 RADAR RT GAIN VOLTAGE TOO HIGH AT MAXIMUM GAIN AND NOT TRACKING. TIME SINCE REPAIR 0:00. 1997010200181 19970102 00181 NE 1997 1 2 CA960723518 2 19960508 A 7261 54T25001 LINE OIL PRESS PWA 4056 PW4056 NE ANGLE GEARBOX CRACKED W E ENGINE SHUTDOWN J K WARNING INDICATION FLUID LOSS CR CRUISE 1 CA P724312 (CAN) DURING FLIGHT #1 ENGINE OIL QUANTITY DROPPED TO ZERO AND OIL PRESSURE DECREASED BELOW MINIMUM LIMIT. ENGINE WAS SH UTDOWN. POST FLIGHT INSPECTION FOUND THE LP09 OIL PIPE CRACKED OVER 180 DEGREES OF ITS CIRCUMFERENCE AT THE ANGLE GEARBO X FITTING. THE LINE WAS REPLACED. 4 F E24NE 1996101700436 19961017 00436 1996 10 17 SCNA96290 4 19961002 A 2561 P0723103 LIFE VEST CABIN FAILED TEST A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 LIFE VEST WAS REJECTED DUE TO NON PASSING OF AIR RETENTION TEST, A HOLE WAS FOUND IN THE LOGO. 1996062000690 19960620 00690 1996 6 20 HEEA967215 1 19960509 A 2432 501122804 BATTERY EMERGENCY POWER CELL DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 DEFECTIVE CELL. SENT TO B.F. GOODRICH AEROSPACE FOR INSPECTION AND REPAIR. 1996021600473 19960216 00473 1996 2 16 HEEA966562 4 19960131 A 3416 212070238003 INDICATOR MASCO COCKPIT FAIL TEST E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 ALTIMETER FAILED POSITION ERROR TEST AND BARO. DIAL CHECK. 1996121200500 19961212 00500 NE 1996 12 12 CA960212003 2 19960208 A 7230 BEARING LYC ALF502 ALF502R5 41580 NE ENG #1 BEARING LEAKING SEAL W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA LF05627A (CAN) SMELL IN FLIGHT DECK AND CABIN CREW REPORT A MIST IN THE CABIN AIR. SMELL CLEARED WITH ENGINE AIR OFF AND APU AIR ON. BLEED AIR ON #3 ENGINE OILY. ENGINE REPLACED. OIL LEAKING FROM #1 BEARING. 4 F E6NE 1996092600338 19960926 00338 1996 9 26 SCNA96256 4 19960917 A 2561 3500113C LIFE VEST CABIN INOPERATIVE A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 LIFE VEST WAS REJECTED DUE TO NON PASSING OF AIR RETENTION TEST, SEVERAL HOLES WERE FOUND IN VEST. 1996110100589 19961101 00589 NE 1996 11 1 CA960321504 2 19960221 A 7530 77328913 VALVE PWA JT9 JT9D7R4D 52054 NE RT ENG INOPERATIVE W O OTHER J WARNING INDICATION DE DESCENT 1 CA P709645 (CAN)AFTER DESCENT FROM 410 TO 390 FEET WHEN THROTTLE ADVANCED FROM FLIGHT IDLE, THE RIGHT ENGINE FAILED TO RESPOND. WIT H RH PNEUMATIC BLEED OFF ENGINE RESPONSE TO NORMAL. CHANGED LEFT PRESSURE REGULATOR A ND SHUT OFF VALVE. 4 F E3NE 1996020200290 19960202 00290 1996 2 2 96ZZZX477 2 19960119 A 7414 10349234 GEAR BENDIX 1200 MAGNETO MISSING CONTACT A HHXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 03 CONTACT THAT TRANSFERS SPARK TO EACH CYLINDER WAS NOT BUILT INTO ROTOR GEAR. GEAR WAS UNUSABLE. 1996112700072 19961127 00072 1996 11 27 CA960524012 1 19960516 A 7732 WIRING LYC ALF502 ALF502R5 41580 NE #4 ENG VIB CKT BROKEN W O OTHER J E WARNING INDICATION VIBRATION/BUFFET CR CRUISE 1 CA 3447 LF05771A (CAN)#4 ENGINE VIBRATION INDICATION WENT UP TO 1.3. NO VIBRATION FELT IN POWER LEVER. POWER REDUCED AND VIBRATION INDICA TION DROPPED TO NORMAL. BROKEN WIRE REPAIRED. 4 F E6NE 1997011600095 19970116 00095 NE 1997 1 16 CA960229004 2 19960228 A 7261 BEARING SEAL LYC ALF502 ALF502R5 41580 NE #3 ENG NR 1 BRG LEAKING W O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 CA LF05539A (CAN) DURING SHORT FINAL, FLIGHT ATTENDANTS NOTICED A BLUE HAZE IN CABIN. THE FLIGHT CREW SELECTED APU AIR AND HAZE DISS IPATED. ENGINE #3 OIL LEAK FROM #1 BEARING SEAL. ENGINE CHANGED. IT IS SUSPECTED THAT OIL LEAK IS FROM COMPANY CAMPAIGN TO CHANGE OIL FROM EXXON 2380 TO CASTROL 5000. 4 F E6NE 1997010900842 19970109 00842 NE 1997 1 9 97ZZZX197 2 19961207 A 7200 ENGINE IAE V2500 V2500A1 NE NR 2 MALFUNCTION A SOKF D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 23 941LF V10039 ON TAXI OUTBOUND AT SFO, PILOT REPORTED ENG NR 1 HAD N1, N2 DROP AND THE EGT ROSE TO OVER 636 FOR A FEW SEC. A/C RETURN ED TO RAMP WHERE RIGGING OF VSV OF 7TH AND 10TH STAGE BLEED VALVES WERE CHECKED. ENG WAS ALSO CHECKED FOR HIGH TEMP. M ASTER VSVA ACTUATOR P/N 1685MK7 AND LPC BLEED-SLAVE ACTUATOR P/N 1778MK1 REPLACED. 4 F E311NE 1996121200323 19961212 00323 EA 1996 12 12 CA960709005 2 19960702 A 7322 T67D50217 HEAT JACKET LYC O320 O320D2A 41508 EA CARBURETOR BROKEN LUGS W A A UNSCHED LANDING E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CR CRUISE 1 CA 1138 L1758539A (CAN) DURING ROUTINE FLIGHT PILOT REPORTED A ROUGH RUNNING ENGINE. POST FLIGHT TROUBLESHOOTING FOUND THE TOP OUTBOARD LU GS ON THE CARBURETOR HEAT JACKET HAD COME LOOSE FROM THE CLAMP AND THE TWO RIVETS HOLDING IT ONTO THE JACKET. THE LUG HA D TRAVELLED THROUGH THE DUCT INTO THE CARBURETOR AIR BOX WHERE IT WAS INTERFERING WITH THE OPERATION OF THE CARBURETOR D URING FLIGHT. THE JACKET WAS REPAIRED AND REINSTALLED. FLEET INSPECTION REVEALED TWO MORE AIRCRAFT WITH BROKEN/LOOSE CAR BURETOR LUGS. 3 O E274 1996062700443 19960627 00443 1996 6 27 HEEA967331 4 19960604 A 3452 071127608 TRANSPONDER KFS76A COCKPIT ATC DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 708 TRANSPONDER DROPS OFF LINE INTERMITTENTLY. 1997030600210 19970306 00210 1997 3 6 SCNA97042 4 19961022 A 2561 P0723103 LIFE VEST CABIN FAILED TEST A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 LIFE VEST DID NOT PASS ALL TESTS. 1996022300353 19960223 00353 1996 2 23 HEEA966646 4 19960206 A 3442 MI5852013 INDICATOR P4001 COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 UNIT NOT TRACKING CORRECTLY AND PUSH BUTTON POPS OUT TOO FAR. SENT TIME SINCE REPAIR 0:00. 1996112700019 19961127 00019 NE 1996 11 27 CA960513008 2 19960501 A 7250 M406167 BLADES LYC 2121051R35 LYC ALF502 ALF502R5 41580 NE 1ST GP TURBINE RUPTURED W A E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 CA 13025 1996 M406167 LF05648A (CAN)IN CRUISE, #4 ENGINE TGT AND VIBRATION ABOVE LIMITS ACCOMPANIED BY FLAMES OUT OF TAILPIPE ENGINE SHUTDOWN. BORESCO PE INSPECTION REVEALED FIRST STAGE GAS PRODUCER TURBINE BLADES RUPTURED 4 F E6NE 1997030600212 19970306 00212 1997 3 6 SCNA97044 4 19961209 A 2561 P0723103 LIFE VEST CABIN FAILED TEST A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 LIFE VEST DID NOT PASS ALL TESTS AND WERE REJECTED. 1996021600476 19960216 00476 1996 2 16 HEEA966565 4 19960131 A 3416 212070238003 INDICATOR MASCO COCKPIT STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 NEEDLE INTERMITTENTLY STICKS WHEN DECREASING ALTITUDE. 1996031500318 19960315 00318 1996 3 15 HEEA966777 1 19960228 A 2435 200SGL1064 ARMATURE START/GEN DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 INSTALLED ARMATURE IN GENERATOR AND RAN UNIT. HAD EXCESSIVE ARCHING. 1996080200190 19960802 00190 1996 8 2 SCNA96209 4 19960716 A 2561 3500113 LIFE VEST UNDER SEAT FAILED TEST A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 LIFE VEST FAILED INSPECTION/TEST. 1996070300453 19960703 00453 1996 7 3 HEEA967370 4 19960605 A 2312 40001278500 TRANSCEIVER RT40 COCKPIT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 TRANSCEIVER WON'T TRANSMIT. TIME SINCE REPAIR 0:00. 1997011600155 19970116 00155 NE 1997 1 16 CA960826008 2 19960809 A 7260 208325024 GEAR BOX LYC ALF502 ALF502R5 41580 NE #4 ENGINE BEARING FAILED W K NONE J WARNING INDICATION IN INSP/MAINT 1 CA 7249 7249 LF05017S (CAN) #4 ENGINE FULL FLOW CHIP DETECTOR (FFCD) CONTAMINATED WITH METAL CHIPS, CONDITION 3. ALL OTHER CHIP DETECTORS INSP ECTED AND HEAVY METAL CONTAMINATION FOUND IN THE FFCD AND AGB CHIP DETECTORS. ANALYSIS OF METAL REVEALED AMS6440 BEARING MATERIAL. ACCESSORY GEARBOX AND OIL PUMP REPLACED. 4 F E6NE 1996121200297 19961212 00297 NE 1996 12 12 CA960703012 2 19960617 A 7200 ENGINE 100006029 LYC T53 T5317A 41549 NE AUX GR BOX MAKING METAL W A A UNSCHED LANDING J WARNING INDICATION TX TAXI/GRND HDL 1 CA 299 LE81024 (CAN) DURING LOGGING OPERATIONS THE FOLLOWING SEQUENCE OF ENGINE CHIP WARNING INDICATIONS WERE RECORDED. THE ENG WAS REM OVED FROM SERVICE AT 299.3 HOURS. 225.0 HRS-MAGNETIC PASTE FOUND ON AGB CHIP DETECTOR. 276.0 HRS-MAGNETIC PASTE & SOME T INY CHIPS WERE FOUND ON AGB CHIP DETECTOR.291.0 HRS-A FEW VERY SMALL CHIPS WERE FOUND ON BOTH THE ENGINE & A/F CHIP DET ECTORS (NO WARNING LIGHT INDICATION). 297.0 HRS-MODERATE SIZE CHIPS WERE FOUND ON BOTH CHIP DETECTORS. 299.0 HRS-A FEW M ORE MODERATE SIZE CHIPS & SOME BRASS LIKE MATERIAL WASFOUND ON BOTH CHIP DETECTORS & THE ENGINE FILTER. AFTER THE LAST INDICATION ENG WAS REPLACED & WILL BE EVALUATED BY TECH REP. 4 U E17EA 1996121800013 19961218 00013 GL 1996 12 18 CA960703027 3 19960529 A 6111 B6421 BLADE ACTUATOR P11046417011 MCAULY 5JFR C5JFR36C1102 GL LINK BEARING WORN BEARING W A K NONE E VIBRATION/BUFFET CR CRUISE 1 CA 1573 942066 (CAN) PROPELLER, OR OTHER, VIBRATION PRONOUNCED AT LOW ALTITUDE AND HIGH SPEED. PROPELLER WAS REPLACED DUE TO BLADES HA VING EXCESSIVE PLAY ABOUT ITS TURNING AXIS. UPON DISASSEMBLY OF THE PROPELLER, BEARING WEAR WAS NOTED ON THE BLADE ACTUA TING LINKS. THE PROPELLER HAS BEEN RETURNED TO THE MANUFACTURER FOR INVESTIGATION OF PREMATURE LINK BEARING WEAR. 5 C P15WE 1996121200503 19961212 00503 1996 12 12 CA960212036 1 19960131 A 7603 RBJ375E ROD END GARRTT TFE731 TFE73122B 01518 WP MCAULY 2D34C B2D34C202 GL SPEED LEVER SEIZED W K NONE O OTHER IN INSP/MAINT 1 CA 1844 P75053C 950511 (CAN) #1 ENGINE SPEED LEVER ROD END WAS SEIZED AND CONTROL CABLE MOVEMENT WAS RESTRICTED DUE TO THIS SITUATION. 4 F E6WE 5 C P7EA 1996122600601 19961226 00601 NE 1996 12 26 CA960716006 2 19960706 A 7250 115024003 EXHAUST DIFFUSER LYC T53 T5317A 41549 NE COMB TURBINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1929 350 LE07677C (CAN) DURING A ROUTINE VISUAL INSPECTION OF THE EXHAUST DIFFUSER, WHILE THE TAILPIPE WAS REMOVED, A 0.075 INCH CIRCUMFER ENTIAL CRACK FOUND ON THE DIFFUSER MIDCONE BETWEEN THE 12 O'CLOCK STRUT AND THE DIFFUSER MOUNTING FLANGE. 4 U E17EA 1996062700444 19960627 00444 1996 6 27 HEEA967332 4 19960604 A 3457 0110010602 GPS GPS165 COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 GPS NOT PICKING UP SATELLITE STATIONS. 1996041200345 19960412 00345 1996 4 12 HEEA966907 4 19960402 A 3457 0845000000 SKYNAV 5000 COCKPIT GPS DEFECTIVE A HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 COCKPIT GPS UNIT DISPLAYS FOREIGN CHARACTERS. 1996082200182 19960822 00182 1996 8 22 HEEA967669 4 19960816 A 3421 4020550904 GYRO INDICATOR COCKPIT ADI E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 GYRO TUMBLED AND WOULD NOT ERECT. 1996070300439 19960703 00439 1996 7 3 HEEA967356 4 19960605 A 3422 5050031904 GYRO COCKPIT DG FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 AFTER A FEW HOURS OF USE, ROTOR INTERMITTENTLY RUNS DOWN AND WILL NOT SPIN UP. 1996111400589 19961114 00589 NE 1996 11 14 B4MR96003 2 19961111 A 7230 719317 COMPRESSOR CASE PWA 793353 PWA JT8 JT8D9A 52048 NE ENGINE CRACKED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 EE6407 666393 ENGINE WAS RECEIVED BY AMERICAN INTERNATIONAL AIRWAYS FROM LUFTHANSA CARGO FOR CONVERSION FROM MODEL 9A TO -15. DISASSE MBLY AND SUBSEQUENT INSPECTION REVEALED A 4 BY 5 INCH HOLE IN THE INTERMEDIATE CASE, FRONT COMPRESSOR CASE. VISUAL INSP INDICATES THAT A CRACK STARTED IN THE FRONT COMPRESSOR CASE MOUNTING WELD AND PROGRESSED UNTIL MATERIAL WAS LIBERATED. A DETAILED INSP REVEALED NO COLLATERAL DAMAGE ASSOCIATED WITH THE FAILURE. HEAVY MAINTENANCE WAS LAST ACCOMPLISHED 483 3 HOURS AGO. EXTENT OF MAINTENANCE IS UNKNOWN. WELD LOCATION REFERENCE, PRATT AND WHITNEY ENGINE MANUAL 481672, REPAIR -08, FIGURE 901 REF NR 5. 4 F E2EA 1996101700437 19961017 00437 1996 10 17 SCNA96291 4 19961002 A 2561 3500113 LIFE VEST CABIN FAILED TEST A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 LIFE VEST WAS REJECTED DUE TO CYLINDER VALVE LEAKING. 1996121200294 19961212 00294 NE 1996 12 12 CA960703001 2 19960628 A 7324 219356001 CHECK VALVE LYC ALF502 ALF502R5 41580 NE FLOW DIVIDER STUCK OPEN W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA LF05683A (CAN) AFTER SHUTDOWN SMOKE WAS NOTICED COMING FROM THE INTAKE AND THE EXHAUST. TROUBLESHOOTING REVEALED A FAULTY CHECK V ALVE BETWEEN THE FUEL BOOSTER PUMP AND THE ECOLOGY PUMP LETTING FUEL INTO THE BURNER CAN. THE CHECK VALVE WAS REPLACED, THE ENGINE INSPECTED AND GROUND RUN SERVICEABLE. 4 F E6NE 1996092600339 19960926 00339 1996 9 26 SCNA96257 4 19960917 A 2561 3500113C LIFE VEST CABIN INOPERATIVE A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 LIFE VEST WAS REJECTED DUE TO NON PASSING OF AIR RETENTION TEST, SEVERAL HOLES WERE FOUND IN VEST. 1997011600137 19970116 00137 1997 1 16 CA960321515 1 19960303 A 7830 12623641 MOTOR PWA JT9 JT9D7 52054 NE THRUST REV NR 3 INOPERATIVE W O OTHER O OTHER LD LANDING 1 CA P695768 (CAN) #3 ENGINE THRUST REVERSER INOPERATIVE ON LANDING. REPLACED #3 THRUST REVERSER MOTOR. OPERATIONAL CHECK CARRIED OUT , OK. 4 F E20EA 1996110100392 19961101 00392 GL 1996 11 1 CA960315005 2 19960308 A 7323 23007505 GOVERNOR ALLSN 250C 250C20B 03013 GL SPLINED ADAPTER WORN W K NONE O OTHER IN INSP/MAINT 1 CA 909 CAE836045 (CAN)REMOVED N2 GOVERNOR TO TROUBLESHOOT TORQUE/N2 HUNTING. SPLINED ADAPTER FOUND LOOSE, CLOSER OBSERVATION SHOWED C-CLI P MISSING AND INNER SPLINES SEVERELY WORN. 3 U E4CE 1996042500493 19960425 00493 1996 4 25 HEEA966965 1 19960408 A 2435 03600918 BEARING LUCAS START/GEN MAKING NOISE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 STARTER GENERATOR HIGH PITCH NOISE WHEN RUNNING ON UNIT. BEARING BAD. 1996021600479 19960216 00479 1996 2 16 HEEA966568 4 19960131 A 3416 212070238003 INDICATOR MASCO COCKPIT LOOSE PARTS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 INDICATOR HAS LOOSE PARTS INSIDE AND 24 MONTH INSPECTION DUE. 1997010200245 19970102 00245 NE 1997 1 2 CA960731004 2 19960725 A 7260 230006401 BEARING ALLIED SIGNA 214167001 LYC ALF502 ALF502R5 41580 NE ACCY GR BOX FAILED W A A E UNSCHED LANDING ENGINE SHUTDOWN J K WARNING INDICATION FLUID LOSS CL CLIMB 1 CA 13775 842 J3258 LF05711A (CAN) ON FIRST FLIGHT OF DAY, DURING CLIMB OUT AT 15,000 FEET, THE #1 ENGINE INDICATED THERE WAS SIGNIFICANT OIL PRESSUR E & QUANTITY LOSS. THE ENGINE WAS SHUTDOWN & THE AIRCRAFT RETURNED TO ITS POINT OF DEPARTURE. PRELIMINARY INSPECTION REV EALED TOTAL LOSS OF OIL, LIGHT METAL DEBRIS IN TAILPIPE & CONDITION 3 FERROUS METAL DEBRIS CAPTURE ON THE FULL FLOW CHIP DETECTOR. THE LP TURBINE (4TH STAGE) HAD MIGRATED AFT ENOUGH TO HAVE ALLOWED TURBINE BLADE RUB/CONTACT WITH THE FORWARD FACE OF THE TAILCONE BULLET. EVIDENCE THUS FAR SUGGESTS A 4/5 BEARING FAILURE. 4 F E6NE 1996121200366 19961212 00366 EA 1996 12 12 96ZZZX5963 2 19961031 A 7322 3024973 COUPLING BENDIX PWA PT6 PT6A28 EA FCU DRIVE DEFECTIVE A A AVSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 13 INSEPCTION OF NEW FCU PART BEFORE INSTALLING ON AIRCRAFT REVEALED A SUBSURFACE FLAW RUNNING LONGITUDINALLY DOWN THE FEMA LE SPLINE. THIS UNIT IS A PLASTIC DRIVE COUPLING BETWEEN THE ENGINE DRIVEN FUEL PUMP AND THE FUEL CONTROL. FAILURE WOU LD HAVE CAUSED AN ENGINE FLAME OUT. SUBMITTER STATED DEFECT IS IN MANUFACTURE. 4 T E4EA 1996022300354 19960223 00354 1996 2 23 HEEA966647 4 19960206 A 3442 MI5852013 INDICATOR P4001 COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 INDICATOR UNIT NOT TRACKING CORRECTLY. TIME SINCE REPAIR 0:00. 1998040200033 19980402 00033 NE 1998 4 2 CA970130006 2 19961212 A 7200 D4210P PLUG GE CF6 CF680C2B2 30025 NE LT HPSOV NOT ENGAGED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA 690221 (CAN) ON TAKE-OFF, EICAS LT HP SOV GAVE AN INDICATION. AFTER REDUCING TO FLIGHT IDLE, THERE WAS STILL NO CHANGE. INSPE CTION FOUND THAT PLUG D4210P WAS NOT FULLY ENGAGED. PLUG REMOVED, CHECKED AND REINSTALLED. ENGINE RUN PERFORMED AND CH ECKED. THE LEFT HAND ENGINE HAD BEEN REPLACED PRIOR TO FLIGHT. 4 F E13NE 1997011600133 19970116 00133 1997 1 16 CA960320015 4 19960311 A 2562 BATTERY CONNECTR ARTEX ELT CLAMP TENSION W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ELT BATTERY CAME DUE AND WAS REPLACED WITH ARTEX MODEL #00-10-009. PLACED ON BENCH FOR TESTING AND RECERT. UNIT WA S FOUND DEAD UPON UNIT TURN ON. DISASSEMBLED UNIT AND FOUND CLAMPING TENSION ON PORTION OF CONNECTOR TO BE WEAK. CLEANED THE CONNECTOR AND BENT SLIGHTLY TO CREATE MORE TENSION TO THE CONNECTOR. ASSEMBLED UNIT AND BENCH TESTED OK. SUBMITTER STATES THAT THIS TYPE OF CONNECTOR DOES NOT GUARANTEE A GOOD CONTACT FROM BATTERY TO ELT AND RECOMMENDS A DIFFERENT TYPE . 1996022300365 19960223 00365 1996 2 23 HEEA966658 4 19960206 A 3422 066303801 INDICATOR COCKPIT RMI DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 COMPASS CARD IS 180 DEGREE OUT OF PHASE. 1996071000396 19960710 00396 1996 7 10 HEEA967441 1 19960621 A 7722 TM43553 INDICATOR MASCO ENG TEMP DEFECTIVE E A HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 TERMINAL STUDS POTTED IN INDICATOR INCORRECTLY. SMALL TERMINAL SHOULD BE ON POSITIVE SIDE AND LARGE STUD ON NEGATIVE SI DE. 1996112700020 19961127 00020 NE 1996 11 27 CA960513009 2 19960502 A 7250 214117037 TURBINE BLADE LYC 200381012 LYC ALF502 ALF502R5 41580 NE NR 4 ENG BLADE W A A UNSCHED LANDING E VIBRATION/BUFFET TO TAKEOFF 1 CA 6601 1188 86J001 LF05336A (CAN) AFTER TAKEOFF, ENGINE VIBRATION ON NR 4 ENGINE AT 3.0 IPS. CREW REDUCED POWER TO FLIGHT IDLE AND VIBRATION DECREA SED TO 1.0 IPS. ONE BLADE MISSING ON 4TH TURBINE DISC AND 4TH NOZZLE DAMAGE. 4 F E6NE 1996022300366 19960223 00366 1996 2 23 HEEA966661 1 19960206 A 3212 214073929105 FLOAT VALVE FLOAT LEAKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 FLOAT VALVES LEAKED THROUGH OUTLET PORT ON INFLATION OF FLOAT BOTTLE ASSEMBLIES. S/N 1 AND S/N 9 1996082200166 19960822 00166 GL 1996 8 22 HEEA967653 2 19960815 A 7250 6890040 NOZZLE 23038160 ALLSN 250C 250C20B 03013 GL NR 1 SHIELD DEFECTIVE E A K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 CAT21116F RECEIVING INSPECTION REVEALED: MISALIGNED BEYOND SERVICEABLE LIMITS #1 NOZZLE SHIELD OUTER BAND AND DOME FLANGE AS MARK ED. DOES NOT FIT ON #1 NOZZLE. REPLACED DISCREPANT PART. 3 U E4CE 1996072500614 19960725 00614 1996 7 25 96UAL900558 1 19960719 A 2621 BRACKET PYLON FIRE EXT CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 DURING SCHEDULED CHECK OF CYLINDER, ENGINE PYLON FIRE EXTINGUISHER FOUND WITH CRACKED MOUNTING BRACKET. REPORTED UNDER REQUIREMENT OF DOT EXEMPTION E-10990. RETURNED UNIT TO MANUFACTURER FOR REPAIR. 1996042500473 19960425 00473 1996 4 25 HEEA966945 1 19960408 A 2435 03600918 BEARING LUCAS START/GEN FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 BEARING INSTALLED IN UNIT S/N 21364. UNIT HAVING HIGH PITCH SQUEAL WHEN RUNNING. 1996051600460 19960516 00460 1996 5 16 HEEA967041 4 19960417 A 3457 0110005400 GPS 150 COCKPIT GPS MIS MFG E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 GPS "ENT" AND "CLR" BUTTONS ARE INSTALLED BACKWARDS. 1996060600156 19960606 00156 1996 6 6 TAOA049605 4 19960409 A 2564 743GPS1 ASPERATOR EAAEROMARINE EAMT46 RAFT ASSY CRACKED A TAOA K NONE O OTHER IN INSP/MAINT 1 EA 15 TK154 AN UNSERVICEABLE OVERDUE LIFE RAFT WAS USED FOR FLIGHT ATTENDANT TRAINING DEPLOYMENT EXERCISE. INFLATION OF LIFE RAFT W AS NORMAL WITH RAPID DEFLATION, CAUSED BY 2 EACH PRESSURE ASPERATORS (PN 743GPS-1) RUBBER BUTTERFLY TYPE DIAPHRAGMS FOUN D CRACKED AND DETERIORATED WHICH ALLOWED COMPRESSED AIR TO ESCAPE. RAFT MANUFACTURE DATE 4/90. FABRIC MANUFACTURE DATE 1/90. TSO C12C/C70A TYPE, CAO 103.15 APPROVAL. 1997030600651 19970306 00651 GL 1997 3 6 CA960502001 2 19960417 A 7200 ENGINE ALLSN 501D 501D13 03004 GL #1 ENGINE LOST POWER W A E UNSCHED LANDING ENGINE SHUTDOWN M O R OVER TEMP OTHER PARTIAL RPM/PWR LOSS CL CLIMB 1 CA 501599 (CAN) DURING CLIMB THROUGH 18,000 FEET, A SMALL THUMP WAS HEARD (FELT). FOLLOWING THIS, #1 ENGINE HORSEPOWER DROPPED TO APPROXIMATELY 500 HP WITH MOMENTARY TIT OVERTEMP (1030 DEGREES). ALL OTHER PARAMETERS WERE NORMAL. CREW ELECTED TO KEEP ENGINE OPERATING. POWER WAS APPLIED TO SEE IF ANY HORSEPOWR COULD BE RECOVERED, WITH NEGATIVE RESULTS. ENGINE WAS SHUT D OWN AND AIRCRAFT LANDED. 4 T E282 1996051600431 19960516 00431 1996 5 16 HEEA967011 4 19960417 A 2200 2593996333 TARSYN 333 AUTO FLIGHT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 CO-PILOT'S HEADING INDICATOR PRECESSES EXCESSIVELY AND WILL STAY OFF COURSE. 1996071800617 19960718 00617 1996 7 18 HEEA967513 1 19960705 A 7720 TM43553 INDICATOR TOT MIS MFG E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 TERMINAL STUDS POTTED IN INDICATOR INCORRECTLY. SMALL TERMINAL SHOULD BE ON POSITIVE SIDE AND LARGE STUD ON NEGATIVE SI DE. 1996101000899 19961010 00899 1996 10 10 CA960212021 1 19960109 A 7714 333000017 TACHOMETER BFGOODRICH 333000017 LYC O360 AEIO360A1B6 41514 EA ENG RPM SEIZED W A D E RETURN TO BLOCK ENGINE SHUTDOWN O OTHER TX TAXI/GRND HDL 1 CA 182 5527 L2662554 (CAN)AFTER START UP THE PILOT OBSERVED NO INDICATION FROM THE TACHOMETER AND THE ENGINE WAS SHUTDOWN. INVESTIGATION REVE ALED THAT THE TACH HEAD HAD SEIZED. A NEW MECHANISM WAS INSTALLED AND THE AIRCRAFT WA S RETURNED TO SERVICE. SUBMITTER N OTES THAT THIS IS THE SECOND OCCURRENCE ON THIS AIRCRAFT. 3 O 1E10 1996042500463 19960425 00463 1996 4 25 HEEA966935 4 19960408 A 2562 ELT910 ELT NARCO CASE CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 ELT UNIT WAS RETURNED TO PHI WITH CORROSION ON OUTSIDE OF CASE. SENT TO NARCO AVIONICS FOR REPAIR. 1996060600742 19960606 00742 1996 6 6 HEEA967165 1 19960508 A 3340 356H2802 POWER SUPPLY STROBE INOPERATIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 251 STROBE POWER SUPPLY INOPERATIVE. 1997021300505 19970213 00505 EA 1997 2 13 CA960916010 2 19960903 A 8520 LW17060 CRANKSHAFT LYC O320 O320D2A 41508 EA PROP FLANGE CRACKED W K NONE B K SMOKE/FUMES/ODORS/SPARKS FLUID LOSS IN INSP/MAINT 1 CA 1414 L1754639A (CAN) PILOT REPORTED AN OIL LEAK IN THE PROP AREA AND AN OIL SMELL IN THE CABIN. INVESTIGATION REVEALED THAT THE CRANKSH AFT ASSEMBLY HAD A CRACK FROM THE PROP FLANGE GOING IN A SPIRAL AFT OF THE FLANGE ON THE CRANKSHAFT. THE CRACK WAS APPRO XIMATELY 4.5" LONG AND OPENED WITH THE ROTATIONAL MOVEMENT OF THE PROP. THE ENGINE WILL BE REMOVED AND SENT FOR REPAIR. 3 O E274 1997020600093 19970206 00093 NE 1997 2 6 CA960910010 2 19960608 A 7230 BLADE PWA JT9 JT9D7R4D 52054 NE 5 STG COMPRESSOR FAILED W C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CA 34434 P707550 (CAN) DURING ENGINE ACCELERATION AT TAKEOFF ROLL COMPRESSOR STALLED ON #1 ENGINE AT 20 KNOTS. ALL ENGINE PARAMETERS NORM AL. TAKEOFF WAS ABORTED. ON ENGINE TEARDOWN A FIFTH STAGE BLADE ON THE HIGH PRESSURE COMPRESSOR WAS FOUND FAILED. 4 F E3NE 1997010900437 19970109 00437 NE 1997 1 9 97ZZZX102 2 19961030 A 7250 414129001 ROTOR ASSY LYC LTS101 LTS101750C1 41560 NE POWER TURBINE BLADE SHIFT A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 986 SCR47992 LE47155AE ROTOR ASSY FAILED SB LT101-72-10-0153. EXCESSIVE IBPT BLADE SHIFT. REPLACED WITH USED UNIT, CORRECTED PROBLEM. PART T OTAL CYCLES, 2869.8. 3 U E5NE 1996030800257 19960308 00257 1996 3 8 HEEA966710 4 19960220 A 3442 MI5853011 INDICATOR HONEYWELL P4001 COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 INDICATOR ERRATIC DISPLAY, HIGH PITCH SQUEAL AND DISPLAY GOES BLANK AFTER 5 MINUTES. 1999043000066 19990430 00066 GL 1999 4 30 CA961021001 2 19961002 A 7230 6899239 SHAFT ALLSN 250C 250C20B 03013 GL SPUR ADAPTOR SCORED W C ABORTED TAKEOFF J WARNING INDICATION TX TAXI/GRND HDL 1 CA 2757 CAC248007 CAE835711 (CAN) TROUBLESHOOTING NR 2 ENGINE FOR REPETITIVE CHIP DETECTOR LIGHTS, ENGINE REMOVED. NR 2 1/2 BEARING IN ENGINE GEAR BOX WAS FOUND TO BE FLAKING. INNER RACE OF ROLLER BEARING IS ON THE SPUR ADAPTOR GEARSHAFT AND IT WAS FOUND TO HAVE BEE N SCORED BY THE ROLLERS OF THE NR 2 1/2 BEARING. 3 U E4CE 1996061300444 19960613 00444 EA 1996 6 13 HEEA967171 2 19960508 A 7321 324473513 CONTROL PWA PT6 PT6* 52043 EA ENG AUTO FUEL DEFECTIVE E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 10% TORQUE SPLIT. VISUALLY CHECKED UNIT AND FOUND INLET FUEL FILTER INSTALLED BACKWARDS AND BROKEN. UNIT RECEIVED INST ALLED ON ENGINE S/N CPPS62030 FROM PRATT & WHITNEY 8-9-95. 3 T E2NE 1996111400588 19961114 00588 NE 1996 11 14 B4MR96002 2 19961111 A 7230 719317 COMPRESSOR CASE PWA 766949001 PWA JT8 JT8D7B 52053 NE ENGINE CRACKED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 2438 6568767B ENGINE WAS REMOVED FOR COMPLIANCE OF AD 94-20-01. ENGINE WAS DISASSEMBLED AND INSPECTION REVEALED A FOUR INCH CRACK IN THE MOUNTING WELD WHICH PROGRESSED INTO A CIRCULAR DIRECTION WITH MATERIAL LIBERATION LIKELY IF LEFT UNDETECTED. ENGINE TIME SINCE HEAVY MAINTENANCE, 6834 HOURS. REFERENCE PRATT AND WHITNEY ENGINE MANUAL (P/N 4816672 72-34-01) REPAIR -08, FIGURE 901, REF 5. 4 F E2EA 1996111400260 19961114 00260 NE 1996 11 14 CA960408504 2 19960302 A 7230 BLADE PWA JT9 JT9D7R4D 52054 NE STAGE 8 COMPRESR FAILED W E ENGINE SHUTDOWN M OVER TEMP CL CLIMB 1 CA 37905 3800 P707535 (CAN)AFTER TAKEOFF, LEFT ENGINE OVER TEMPERATURE, SHUTDOWN, RETURN TO LAND. BOROSCOPE INSPECTION REVEALED STAGE 8 COMPRE SSOR BLADE FAILED. SINCE THE ENGINE OPERATED 3800 HOURS SINCE REFURBISHMENT, THE PREMATURE BLADE FAILURE IS BEING DISCUS SED WITH MANUFACTURER. 4 F E3NE 1999043000061 19990430 00061 WP 1999 4 30 CA961007009 2 19960926 A 7250 31020224 HOUSING GARRTT TPE331 TPE33110UA 01514 WP COMPRESSOR DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) PART HAD BEEN SENT OUT FOR REWORK AND MOD SB 331-72-0462. AFTER RETURN, IT WAS FOUND THAT THREE OF THE FLANGE HOL ES WERE BADLY ELONGATED AND HAD DEEP SURFACE WEAR. THE POINT OF WEAR IS THE ATTACH POINT FOR THE FCU SUPPORT BRACKET P/ N 868767-1 AND THE INTERMEDIATE SUPPORT PLATE P/N 867915-1. THE GARRETT INSPECTION REPAIR MANUAL DETAILS INSPECTION AND REPAIR PROCEDURES FOR THE METAL SPRAY INNER SURFACE REPAIR, BUT NOT THE HOLES. THE SUBMITTER BELIEVES THE PROBLEM IS NO T UNIQUE. THE FCU SUPPORT MOUNTING BRACKET CARRIES THE AFT END OF THE FCU AND IS SUBJECT TO DAMAGE DUE TO PROPELLER IMB ALANCE. 4 T E4WE 1996051600493 19960516 00493 GL 1996 5 16 HEEA967078 2 19960425 A 7250 23037413 SHAFT 6898735 ALLSN 250C 250C20B 03013 GL XMSN OUTER PT DEFECTIVE E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 CAT36021 CAE832989 UPON INSPECTION OF NEW PART NOTED THE FOLLOWING: ALSEAL COATING FLAKING ON OUTER PT SHAFT O.D. 3 U E4CE 1997021300537 19970213 00537 NE 1997 2 13 CA960924001 2 19960912 A 7230 SEAL LYC ALF502 ALF502R5 41580 NE #1 BEARING LEAKING W O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 CA LF05463A (CAN) ON LANDING FUMES REPORTED IN THE CABIN BY THE FLIGHT ATTENDANT. BOROSCOPE INSPECTION FOUND THE OIL IN #1 BEARING S EAL. THE ENGINE WAS REPLACED. 4 F E6NE 1997010200283 19970102 00283 NE 1997 1 2 CA960812003 2 19960812 A 7260 208325024 ACCESSORY GEARBX LYC ALF502 ALF502R5 41580 NE #4 ENGINE MAKING METAL W K NONE J WARNING INDICATION IN INSP/MAINT 1 CA 7249 7249 LF05017S (CAN) #4 ENGINE FULL FLOW CHIP DETECTOR (FFCD) CONTAMINATED WITH METAL CHIPS (CONDITION 3). ALL OTHER CHIP DETECTORS INS PECTED AND HEAVY CONTAMINATION WAS FOUND ON FFCD AND ACCESSORY GEARBOX (AGB) CHIP DETECTOR. ANALYSIS OF METAL SHOWED MET AL TO BE AMS6440 BEARING MATERIAL. AGB AND OIL PUMP REPLACED. 4 F E6NE 1996122600566 19961226 00566 GL 1996 12 26 CA960703020 2 19960620 A 7323 DRIVESHAFT ALLSN 250C 250C20B 03013 GL GOV GR BOX DRIVE WORN W K NONE O OTHER IN INSP/MAINT 1 CA 575 CAE834769 (CAN) WHILE CONDUCTING A TURBINE CHANGE, AME REMOVED THE POWER TURBINE GOVERNOR AND FOUND THAT THE EPOXY, THE RETAINING RING, AND SHIM HAD FALLEN OFF. THE DRIVESHAFT SPLINES WERE WORN. 3 U E4CE 1996101000415 19961010 00415 NE 1996 10 10 CA960131013 2 19960123 A 7250 2121100R83 NOZZLE 20036001787J LYC ALF502 ALF502R5 41580 NE AFT SHROUD CRACKED W A O OTHER O OTHER NR NOT REPORTED 1 CA 12810 2506 003 LFO5484A (CAN) POWERPLANT ORIGINALLY REMOVED AFTER REPORTS OF OIL VAPORS CONTAMINATING CABIN BLEED AIR SYSTEM ENGINE TEARDOWN REV EALED LARGE TORN AWAY PORTION OF THE 2ND STAGE NOZZLE AFT SHROUD FACE (7 INCHES BY 2 INCHES), CONSIDERABLE DOWNSTREAM DA MAGE. FAILURE WAS A RESULT OF AXIAL CRACKS OVER SHROUD CONVERGING WITH CIRCUMFERENTIAL CRACKS. SEPARATED PORTION OF SH ROUD LIFTED AND CONTACTED DYNAMIC FORWARD FACE OF GP TURBINE COVER, WHICH IN TURN TORE AWAY SHEET METAL (7 INCH BY 2 I N CH) PORTION. THIS NOZZLE HAD UNDERGONE REPAIR AT MFG, PER SB 72-345, WHIC H RECOGNIZED THIS PROBLEM. 4 F E6NE 1997011600097 19970116 00097 NE 1997 1 16 CA960229006 2 19960228 A 7261 SEALS LYC ALF502 ALF502R5 41580 NE #4 ENG NR 9 BRG LEAK W O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 CA LF05627A (CAN) CREW REPORTED FUMES IN THE CABIN. LEAK FOUND COMING FROM #9 BEARING SEAL. SEAL REPLACED. SUSPECT OIL LEAKS BEING C AUSED BY COMPANY CAMPAIGN TO CHANGE ENGINE OIL FROM EXXON 2380 TO CASTROL 5000. 4 F E6NE 1996111400275 19961114 00275 NE 1996 11 14 CA960412012 2 19960323 A 7210 1140217 SHIM LYC T53 T5317A 41549 NE POWER SHAFT MISALIGNED W K NONE J WARNING INDICATION IN INSP/MAINT 1 CA 617 LR81008 (CAN)HIGH OIL CONSUMPTION. POWER SHAFT SHIMS MISALIGNED AT REINSTALLATION DURING INSPECTION IMMEDIATELY PRIOR TO OCCURRE NCE CAUSING HIGH PRESS AIR TO INDUCE VENTING OF GEARBOX. 4 U E17EA 1997030600209 19970306 00209 1997 3 6 SCNA97041 4 19961008 A 2561 P0723103 SEAM LIFE VEST OPEN A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 LIFE VEST WAS REJECTED DUE TO OPEN SEAM. 1996092600336 19960926 00336 1996 9 26 SCNA96254 4 19960917 A 2561 3500113C LIFE VEST CABIN INOPERATIVE A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 LIFE VEST WAS REJECTED DUE TO NON PASSING OF AIR RETENTION TEST, SEVERAL HOLES WERE FOUND IN VEST. 1996120500396 19961205 00396 NE 1996 12 5 CA960610015 2 19960520 A 7310 1199 MANIFOLD ALLIED SIGNA 216362036 LYC ALF502 ALF502R5 41580 NE #5 SCALLOP CRACKED W E ENGINE SHUTDOWN J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA 15336 1199 LF05482A (CAN)ON CLIMB, FIRE INDICATION ILLUMINATED, POWER LEVER RETARDED AND LIGHT EXTINGUISHED, FUEL MANIFOLD CRACKED AT THE #5 SCALLOP, CONFIRMED BY N D T 394 HOURS SINCE PREVIOUS N D TINSPECTION 4 F E6NE 1997010900440 19970109 00440 NE 1997 1 9 97ZZZX105 2 19961030 A 7250 411105064 ROTOR ASSY LYC LTS101 LTS101750C1 41560 NE GAS PROD DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 4977 LE45155AE BLADES SUBJECTED TO CARBON BALL BLASTING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. H53517-001. PART TOTAL CYCLES, 1 973.9. 3 U E5NE 1996121200268 19961212 00268 NE 1996 12 12 CA960620005 2 19960612 A 7210 103019301 GEARSHAFT LYC T53 T5317A 41549 NE TIP OF SPLINE CHIPPED W A UNSCHED LANDING O OTHER HO HOVERING 1 CA 927 LR81008 (CAN) DURING LOGGING OPERATION, ENGINE CHIP WARNING, IMMEDIATE LANDING. CHIP DETECTOR HAD LARGE CHIP ON IT SIMILAR TO GE AR TOOTH. PLANETARY GEARSHAFT CHIPPED AT THE TIP OF THE SUNGEAR DRIVEN SPLINE. 4 U E17EA 1997041500030 19970415 00030 EA 1997 4 15 CA961115002 2 19961001 A 8520 13B27024 CRANKSHAFT LYC O320 O320D2A 41508 EA MAIN BRNG JOURNL CRACKED W A K NONE O OTHER NR NOT REPORTED 1 CA 1414 L1754639A (CAN) ENGINE RECEIVED FOR REPAIR FOR A CRANKSHAFT CRACKED AT THE MAIN BEARING JOURNAL EXTENDING FROM THE FRONT EXPANSION PLUG SEAT IN A SPIRAL (ANTI CLOCKWISE FROM THE FRONT) TO APPROXIMATELY HALF WAY BETWEEN THE FORWARD THRUST FACE AND THE CROSS FEED OIL HOLE. 3 O E274 1996021600480 19960216 00480 1996 2 16 HEEA966569 4 19960131 A 3416 212070238003 INDICATOR MASCO COCKPIT FRICTION ERROR E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 NEEDLE HAS EXCESSIVE FRICTION ERROR AND READS 850 FT. 1996112700090 19961127 00090 NE 1996 11 27 CA960527010 2 19960514 A 7314 216039703 DRIVESHAFT LYC 216079008 LYC ALF502 ALF502R5 41580 NE NR 4 ENG PUMP STRIPPED W K NONE O K OTHER FLUID LOSS IN INSP/MAINT 1 CA 1002 LF5100 (CAN)AFTER LANDING, SMALL AMOUNT OF FUEL LEAKING FROM #4 ENGINE DRAIN MAST. FUEL CONFIRMED COMING FROM BOOST PUMP. PUMP REMOVED, DRIVESHAFT SPLINES STRIPPED ON THE PUMP END. DRIVE SHAFT FAILURE IMMINENT. 4 F E6NE 1997010900439 19970109 00439 NE 1997 1 9 97ZZZX104 2 19961017 A 7250 414129001 ROTOR ASSY LYC LTS101 LTS101650B1 41560 NE POWER TURBINE BLADE SHIFT A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 1210 SC46997 LE45322E ROTOR ASSY FAILED SB LT101-72-10-0153. EXCESSIVE IBPT BLADE SHIFT. REPLACED WITH USED UNIT, CORRECTED PROBLEM. PART T OTAL CYCLES, 3860.9 3 U E5NE 1997032000129 19970320 00129 NE 1997 3 20 CA961024004 2 19961008 A 7250 ENGINE LYC ALF502 ALF502R5 41580 NE #4 POSITION HOT START W E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. M OVER TEMP IN INSP/MAINT 1 CA 6136 LF05784A (CAN) HOT START #4 ENGINE. TEMPERATURE UP TO 970 DEGREES C. ENGINE WOULD NOT SHUTDOWN WITH POWER LEVER. T-HANDLE PULLED TO SHUT-OFF FUEL. FIRE EXTINGUISHER ACTIVATED. ENGINE REMOVED FOR HOT SECTION INSPECTION (HSI). 4 F E6NE 1996062000698 19960620 00698 1996 6 20 HEEA967225 1 19960509 A 2612 473205 FLAME DETECTOR KIDDE CONNECTOR CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 FLAME DETECTOR HAS CORROSION AT CONNECTOR. 1997032000136 19970320 00136 1997 3 20 CA961025002 1 19961023 A 7160 230371302 SEAL LYC ALF502 ALF502R5 41580 NE NR 4 ENG NR 9 OIL LEAK W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA LF05463A (CAN) AIR QUALITY IN CABIN. PARAMEDICS CALLED FOR FLIGHT ATTENDANTS. #9 SEAL #4 ENGINE FOUND TO BE LEAKING OIL INTO SUPE RCHARGER. #9 SEAL REPLACED. 4 F E6NE 1996060600724 19960606 00724 1996 6 6 HEEA967146 1 19960508 A 8010 2520M RELAY STARTER FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 RELAY WILL NOT ALLOW VOLTAGE TO STARTER; TO MOTOR THE ENGINE. SENT TO HERMETIC AIRCRAFT INSTR. CORP. FOR WARRANTY REPAIR . TIME SINCE REPAIR 0:00. 1996080200188 19960802 00188 1996 8 2 SCNA96207 4 19960716 A 2561 P0723103 LIFE VEST UNDER SEAT FAILED TEST A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 LIFE VEST FAILED INSPECTION/TEST. 1996051600491 19960516 00491 1996 5 16 HEEA967075 4 19960423 A 3416 5035P2P44 ALTIMETER COCKPIT ENCODER ERROR E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 ENCODER IS 85 FEET OFF AT 20,000 FEET. 1996070300466 19960703 00466 GL 1996 7 3 HEEA967386 2 19960606 A 7250 6898731 PT SUPPORT ALLSN 250C 250C20B 03013 GL SUMP SURFACE PLATING FLAKE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 UPON INSPECTION OF PART NOTED THE FOLLOWING: PLATING COMING OFF P.T. SUPPORT INNER SUMP SURFACE U-RING SEAT. REPLACED D ISCREPANT PART. 3 U E4CE 1996031500313 19960315 00313 1996 3 15 HEEA966772 1 19960228 A 2435 200SGL1064 ARMATURE START/GEN DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 ARMATURE HAD DEAD SPOT. 1996062000729 19960620 00729 1996 6 20 HEEA967259 4 19960522 A 3457 0845000000 SKYNAV 5000 COCKPIT GPS MALFUNCTION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 WILL NOT UPGRADE POSITION. PICKS UP SATELLITES BUT DOES NOT SHOW GQ OF SATELLITES. 1996091200852 19960912 00852 GL 1996 9 12 CA960123029 2 19960110 A 7250 6899735 TURBINE ALLSN 250C 250C20B 03013 GL ENGINE SEIZED W A E ENGINE SHUTDOWN Y ENGINE STOPPAGE CR CRUISE 1 CA 1358 CAE834907 (CAN)DURING CRUISE FLIGHT, AIRCRAFT YAWED TO THE LEFT. PILOT LOWERED THE COLLECTIVE AND OBSERVED #2 ENGINE HAD FAILED. T HROTTLE SECURED, AIRCRAFT RETURNED TO BASE. INVESTIGATION REVEALED N1 GEAR TRAIN UNAB LE TO ROTATE WITH STARTER. ENGINE DISASSEMBLED, TURBINE APPEARS TO HAVE FAILED. ENGINE IS BEING REPLACED AND FORWARDED TO SHOP FOR EVALUATION AND REPAIRS. 3 U E4CE 1996021600471 19960216 00471 1996 2 16 HEEA966560 4 19960131 A 3416 212070238003 INDICATOR MASCO COCKPIT FAIL TEST E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 ALTIMETER NEEDLE FAILED POSITION ERROR TEST. 1996021600477 19960216 00477 1996 2 16 HEEA966566 4 19960131 A 3416 212070238003 INDICATOR MASCO COCKPIT LOOSE PARTS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 INDICATOR HAS LOOSE PARTS INSIDE. 1996031500303 19960315 00303 1996 3 15 HEEA966760 1 19960228 A 2435 230811010 ARMATURE GENERATOR FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 EXCESSIVE ARCHING WHEN TESTING UNIT. INSTALLED AND FAILED SAME DAY. TIME SINCE REPAIR 0:00. 1996092600340 19960926 00340 1996 9 26 SCNA96258 4 19960917 A 2561 P0723103C LIFE VEST CABIN INOPERATIVE A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 LIFE VEST WAS REJECTED DUE TO NON PASSING OF AIR RETENTION TEST, SEVERAL HOLES WERE FOUND IN VEST. 1996121200329 19961212 00329 NE 1996 12 12 CA960711003 2 19960704 A 7250 214112604 BOLT 214313903 LYC ALF502 ALF502R5 41580 NE REAR HEAT SHIELD LOOSE W A K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA LF05460A (CAN) DURING ROUTINE TEARDOWN FOR TIME EXPIRED COMPONENT REPLACEMENT TWO REAR HEAT SHIELD BOLTS WERE FOUND LOOSE. ONE BO LT HAD THE LOCK WIRE BROKEN AND HAD BACKED HALF WAY OUT CONTACTING THE 4TH STAGE TURBINE ROTOR CAUSING MINOR DAMAGE. THI S IS THE SECOND INCIDENT OF THIS PROBLEM AND HAS THE POTENTIAL OF CAUSING ENGINE FAILURE. 4 F E6NE 1997010200186 19970102 00186 NE 1997 1 2 CA960723524 2 19960518 A 7322 3333321 FUEL CONTROL HAMSTD PWA JT9 JT9D7R4D 52054 NE #1 ENGINE FAULTY W O OTHER O OTHER CR CRUISE 1 CA P709673 (CAN) DURING FLIGHT AIRCRAFT WENT INTO HEAVY TURBULANCE, LEFT E.P.R. DROPPED TO 1.01, MOVED THROTTLE FORWARD AND AFT E.P .R. REMAINED AT 1.01. POST FLIGHT INVESTIGATION LED TO FUEL CONTROL UNIT (FCU) REPLACEMENT. 4 F E3NE 1997030600674 19970306 00674 1997 3 6 CA960826065 1 19960809 A 7603 T67B50227 PUSHROD LYC O320 O320D2A 41508 EA POWER LEVER BROKEN W B EMER. DESCENT O OTHER DE DESCENT 1 CA 1302 L1490839A (CAN) UPON PULLING THE THROTTLE BACK THE PUSHROD BROKE AT THE FORWARD THREADED END, WHERE IT ATTACHES TO THE CLEVIS ASSE MBLY. THE PILOT HAD ENOUGH TRAVEL TO PERFORM A SAFE LANDING. 3 O E274 1997041500024 19970415 00024 1997 4 15 CA961112051 1 19961030 A 7120 K97211302 MOUNT LYC T53 T5317A 41549 NE AFT INBOARD CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1877 LR81008 (CAN) DURING ENGINE REMOVAL TO FACILITATE OTHER AIRFRAME RELATED REPAIRS, THE R/H AFT ENGINE MOUNT FITTING WAS FOUND CRA CKED. 4 U E17EA 1996042500488 19960425 00488 1996 4 25 HEEA966960 4 19960408 A 2562 ELT910 ELT NARCO ELT CASE CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5359 ELT UNACCEPTABLE DUE TO CORROSION SEEPAGE THROUGH ORANGE PAINT. 1996011200002 19960112 00002 NM 1996 1 12 95UAL900371 1 19960104 A 2920 69201841 SEAL BOEING 737 737322 1384676 NM GE CFM56 CFM563B1 13802 NE FLAP CONTROL LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 356UA 24362 NOTICED A STEADY LOSS OF 'B' SYSTEM HYDRAULIC QUANTITY AFTER REACHING CRUISE. TRIED TO ISOLATE SYSTEMS AND WHEN TURNING OFF THE 'B' SYSTEM SPOILER SWITCH QUANTITY STABILIZED AT 39 PERCENT. REPLACED THE SEAL PLATE BETWEEN THE TRAILING EDGE FLAP CONTROL VALVE AND THE FLAP LOAD LIMITER SOLENOID VALVE. REFERENCE BOEING SERVICE LETTER 737-SL-27-104. 2 L 7 2 4F 4 F RT A16WE E2GL 1996021600710 19960216 00710 NE 1996 2 16 9603776603 2 19960214 A 7200 ENGINE BOEING 747 747151 1384891 NM PWA JT9 JT9D7A 52054 NE NR 2 BIRDSTRIKE A NWAA A E J UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL R C PARTIAL RPM/PWR LOSS F.O.D. CL CLIMB 1 GL 01 603US 19780 62404 DURING CLIMB, THE NR 2 ENGINE INGESTED BIRD AND SUBSEQUENT COMPRESSOR STALL AND IFSD. CREW FOLLOWED COCKPIT OPERATING P ROCEDURE, DUMPED 40,000 POUNDS OF FUEL, AND RETURNED TO NRT WITHOUT FURTHER INCIDENT. REPLACED THE NR 2 ENGINE DUE TO 5 TH HP DAMAGED. CHECK WAS NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4 F A20WE E20EA 1996030800324 19960308 00324 NM 1996 3 8 96UAL900161 1 19960304 A 3350 BATTERIES BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7467U 21921 RT EEL EXIT DOOR PANEL LIGHTS INOPERATIVE. REPLACED BATTERIES. 2 L 7 3 4F 4 F A3WE E2EA 1996032900289 19960329 00289 NM 1996 3 29 96UAL900212 1 19960325 A 2131 CONTROLLER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 7450U 21904 ON CLIMBOUT OF DEN, UNABLE TO CONTROL CABIN PRESSURE IN ANY MODE. FLIGHT RETURNED TO DEN. REPLACED CABIN PRESSURE CONT ROLLER AND LANDING GEAR ACCESSORY UNIT. LATER MAINTENANCE REPAIRED LEAKAGE AT FORWARD AND AFT CARGO DOORS AND REPLACED LT PACK FLOW CONTROL AND SHUTOFF VALVE, LT PACK SWITCH AND RELAYS R124 AND R589. 2 L 7 3 4F 4 F A3WE E2EA 1996041200194 19960412 00194 NE 1996 4 12 DL76L960759 2 19960403 A 7532 BLEED VALVE 8087261 BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE MALFUNCTIONED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 180DN F26460 25985 724687 ON TAXI OUT, NR 1 ENG HAD AN APPARENT COMPRESSOR STALL AND PIMU C1 FAULT MSG ON STATUS. LT PIMU EEC CH A/B B2.5 TR CHEC K FAILED. REPLACED 2.5 BLEED ACT, PER MM 75-32-01. IDLE RUN OK, NO LEADS AND NO PIMU FAULTS. HP RUNUP OK, OPS OK PER PFHB TEST 15. 2 L 7 2 4F 4 F RT A1NM E24NE 1996041200377 19960412 00377 NE 1996 4 12 9607929915 2 19960405 A 7250 TURBINE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9 52048 NE NR 2 ENGINE FAILED A A NWAA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 01 965N 47417 666706 NR 2 ENGINE EXPERIENCED A CONTAINED TURBINE FAILURE AFTER DEPARTING. AIRCRAFT RETURNED TO BIL AND LANDED WITHOUT INCIDE NT. MAINTENANCE REPLACED THE ENGINE WITH A SERVICEABLE UNIT. 2 L 7 2 4F 4 F A6WE E2EA 1996041800346 19960418 00346 WP 1996 4 18 96UAL900257 1 19960415 A 5330 SKIN DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE BS 1069 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 1854U 47813 WHEN REMOVING NR 2 ADF ANTENNA FOUND CORROSION ON FUSELAGE MOUNTING SURFACE STATION 1069 AT LONGERON L52. REMOVED AFFEC TED SKIN SECTION AND PERFORMED EXTERNAL DOUBLER/TRIPLER REPAIR. 2 L 7 3 4F 4 F A22WE E23EA 1996060600421 19960606 00421 NE 1996 6 6 96ZZZX2845 2 19960319 A 7321 7436025 FUEL CONTROL DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9A 52048 NE NR 2 ENGINE MALFUNCTIONED A VJ6A C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 11 916VV 47445 665721 ON FLIGHT 134, FL, ABORTED TAKEOFF, NR 2 ENGINE WOULD NOT REACH TAKEOFF EPR, FULL POWER = 1.80. REMOVED AND REPLACED FU EL CONTROL UNIT PER MM 73-00. NO LEAKS NOTED. 2 L 7 2 4F 4 F A6WE E2EA 1996060600752 19960606 00752 NM 1996 6 6 96UAL900388 1 19960531 A 3350 BATTERIES BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7266U 21413 EMERGENCY LIGHT OVERHEAD AT AFT END OF AIRSTAIR IS INOPERATIVE. REPLACED BATTERIES. 2 L 7 3 4F 4 F A3WE E2EA 1996060600764 19960606 00764 NM 1996 6 6 96UAL900400 1 19960603 A 2120 AIR DISTR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT ODOR A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 510UA 24780 STRONG ODOR IN COCKPIT AND CABIN, FLIGHT DIVERTED TO ORD. 2 L 7 2 4F 4 F RT A2NM E17NE 1996061300428 19960613 00428 GL 1996 6 13 ERAA96217 2 19960327 A 7323 2524667 GOVERNOR BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20 03013 GL ENGINE DEFECTIVE A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 294EH 8877 S846 TORQUE SPLITS. LAGS WILL NOT RECOVER. N2 BLEEDS OFF OVER 68% TORQUE. GOVERNOR WAS SENT FOR OVERHAUL 7/21/95 1 G 7 2 3U 3 U H3EU E4CE 1996071100005 19960711 00005 SW 1996 7 11 HEEA967381 1 19960605 A 7930 23001955 INDICATOR 23053960 BELL 230 230 1182149 SW ALLSN 250C 250C30G2 03013 GL OIL FILTER DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN CAG98226 23009 CAE898226 UPON POSTFLIGHT CHECK OF #1 ENGINE NOTED OIL FILTER BYPASS INDICATOR EXTENDED. REPLACED OIL FILTER WITH NO CHANGE. IND ICATOR REPLACEMENT CORRECTED PROBLEM. REPLACED DISCREPANT PART. PERFORMED FUNCTIONAL TEST. INDICATOR FAILED OPERATIONA L TEST PRESSURE RANGE. 1 G 7 2 3U 3 U NC H9SW E1GL 1996071800178 19960718 00178 NM 1996 7 18 CALA9600988 1 19960709 A 7920 OIL LINE BOEING 737 7373T0 1384582 NM GE CFM56 CFM563B1 13802 NE OIL COOLER LEAKING A CALA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CL CLIMB 1 SW 09 12322 23373 721730 THE NR 1 ENGINE OIL QUANTITY DROPPED TO ZERO AND THE OIL PRESSURE BEGAN TO DROP AFTER TAKEOFF FROM CLE. THE AIRCRAFT WA S RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LINE TO FUEL/OIL COOLER LOOSE AND LEAKING. T HE LINE WAS TIGHTENED AND THE NR 1 ENGINE WAS SERVICED WITH OIL. THE ENGINE WAS RUN AT FULL POWER AND NO LEAKS WERE NOT ED. 2 L 7 2 4F 4 F RT A16WE E2GL 1996080200159 19960802 00159 NE 1996 8 2 9616026615 2 19960725 A 7314 7800001 FUEL PUMP BOEING 747 747251B 1384892 NM PWA JT9 JT9D7Q 52054 NE NR 4 ENGINE FAILED A A NWAA B EMER. DESCENT O OTHER DE DESCENT 1 GL 01 615US 40231 40 20360 02029 DURING DESCENT, THE NR 4 ENGINE ROLLED BACK TO IDLE WITH AUTO THROTTLE ON. CREW DECLARED AN EMERGENCY AS PRECAUTION AND MADE A THREE-ENGINE LANDING WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FUEL FLOW PUMP AND FUEL CONTROL. PERFO RMED LEAK AND OPERATIONAL CHECKS. CHECKS WERE NORMAL AND AIRCRAFT RETURNED TO SERVICE. PART TOTAL CYCLES, 9,858. 2 L 7 4 4F 4 F A20WE E3NE 1996080800130 19960808 00130 NE 1996 8 8 96ZZZX3854 2 19960331 A 7250 LPT BLADE BOEING 727 727231 1384079 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE FAILED A TWAA C D ABORTED TAKEOFF RETURN TO BLOCK T ENGINE CASE PENETRATION TO TAKEOFF 1 CE 05 84355 21987 SLC - FLT 4355 - DURING TAKEOFF, NR 2 ENGINE, S/N 1548, SUFFERED A TURBINE FAILURE. ENGINE TOTAL TIME: 33,348 HOURS; 2 1,618 CYCLES, CHECK C-01 - 2-13-96 - JFK. INVESTIGATION INTO TURBINE FAILURE OF NR 2 ENGINE, S/N 1548, REVEALED THAT A N LPT 4 BLADE SEPARATED AND PENETRATED THE OTHER CASE, DUCTING AND COWLING, ENGINE S/N 1548 WAS REPAIRED AND RETURNED T O SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 1996080800380 19960808 00380 NE 1996 8 8 REXA96020 2 19960627 A 7530 600250 PERI-SEALS SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE PNEUMATIC TUBE WORN A REXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 922MA 340A077 LEFT TAIL PIPE 'HOT' LIGHT ON JUST AFTER TAKEOFF. FERRIEDTO MEMPHIS. SECURED A LOOSE TAILPIPE BLANKET AND REPLACED THE PERI-SEALSBEHIND THE LOW PRESSURE BLEED VALVE. GROUND RAN AT POWER FOR 20 MINUTES.AIRCRAFT OK FOR SERVICE. REFERENCE M I13663.(M) 2 L 7 2 4T 4 T RT A52EU E8NE 1996081500403 19960815 00403 NM 1996 8 15 VNAA9608001 1 19960801 A 5101 STRUCTURE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE AIRFRAME BIRD STRIKE A VNAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 07 424JS 3033 CREW REPORTED STRIKING A LARGE BIRD DURING THE TAKEOFF ROLL. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GATE. OU T STATION MX INSPECTED THE AIRCRAFT FOR DAMAGE I.A.W. M.M. 05-10-00 , NO DEFECTS NOTED, THE AIRCRAFT WAS RETURNED TO SE RVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996082700001 19960827 00001 NE 1996 8 27 96ZZZX4041 2 19960305 A 7200 ENGINE BAC 146 AVRO146RJ100 1500096 EU LYC LF507 LF5071F NE NR 1 FLAME OUT A ANCF O OTHER X J ENGINE FLAMEOUT WARNING INDICATION AP APPROACH 1 SO 23 504MM 3395 E3221 LF07342 ADZ - FLT 169 - DURING SHORT FINAL TO RWY 06 IN ADZ, ENGINE NR 1 FLAMED OUT. JUST MEMORY ITEMS PROCEDURE. ONLY OBSERVE D N2 WENT TO ZERO. PERCENT RPM AND OIL PRESSURE WENT TO ZERO PSI, TOO. ENGINE NR 1 WAS CHANGED. TEST ON GROUND WITH ENGINE RUN-UP OK IAW MM 71-00-00. ENGINE NR 1 OVERSPEED SHUT-DOWN WAS PERFORMED. CYCLES, 3,227. 2 H 7 4 4F 4 F RT A49EU E6NE 1996091900341 19960919 00341 NE 1996 9 19 SWAA960956 2 19960909 A 7200 ENGINE BOEING 737 7373H4 1384600 NM GE CFM56 CFM563B1 13802 NE NR 1 BIRD STRIKE A SWAA A UNSCHED LANDING C F.O.D. CL CLIMB 1 SW 07 686SW 23175 EXPERIENCED BIRD STRIKE TO NUMBER 1 ENGINE AFTER TAKEOFF, ACCOMPANIED BY EGT RISE AND ODOR IN CABIN. AIRCRAFT RETURNED TO OAK AND HAD AN UNEVENTFUL LANDING. PERFORMED BIRD STRIKE INSPECTION PER BOEING M/M, NO DEFECTS NOTED. ENGINE PLACE D ON 10 CYCLE BORESCOPE INSPECTION. 2 L 7 2 4F 4 F RT A16WE E2GL 1996091900475 19960919 00475 NE 1996 9 19 96ZZZX4639 2 19960806 A 7421 CH34595 IGNITER SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 781LF 180 1178 415 IGNITER INTERMITTENT, FAILED INTERNALLY. 680 STARTS ON IGNITER. 1 G 7 1 3U 3 U H9EU E19EU 1996091900816 19960919 00816 NE 1996 9 19 MZZA96060 2 19960726 A 7250 TURBINE BOEING 727 727224 1384076 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE FAILURE A A MZZA A E UNSCHED LANDING ENGINE SHUTDOWN J M WARNING INDICATION OVER TEMP CL CLIMB 1 WP 13 69741 22250 AT GEAR RETRACTION, PASSING ABOUT 300 FEET, NR 3 ENGINE FAILED (TURBINE SECTION) CLIMBED TO 1000 FEET, CLEANED UP, DID E NGINE FAIL CHECK LIST AND RETURNED TO PONAPE FOR NORMAL TWO ENGINE LANDING. REMOVED AND REPLACED NR 3 ENGINE PER JOB CA RD 07-7100-1-8001 AND PER JT8D POWER ASSURANCE RUN NR JE07-7100-94-072-001. ENGINE RUN CHECKS NORMAL. (M) 2 L 7 3 4F 4 F A3WE E2EA 1996100300376 19961003 00376 WP 1996 10 3 CALA9601342 1 19960930 A 7920 7938314506 OIL LINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE PRES XMITTER CRACKED A CALA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SW 09 83870 48056 696399 THE NR 2 ENGINE OIL QUANTITY BEGAN TO DROP WHILE EN ROUTE. THE AIRCRAFT WAS DIVERTED TO GSO WHERE IT LANDED WITHOUT INC IDENT. MAINTENANCE FOUND THE LINE TO OIL PRESSURE TRANSMITTER CRACKED. THE LINE WAS REPLACED, THE ENGINE WAS RUN AND L EAK CHECK WAS GOOD. 2 L 7 2 4F 4 F A6WE E9NE 1996101000898 19961010 00898 CE 1996 10 10 CA960212020 1 19960201 A 5511 043200156 STAB SPAR CESSNA CESSNA 150 150L 2071826 CE CONT O200 O200A 17020 SO FLANGE RADIUS CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 10567 674507A (CAN)DURING THE COMPLETION OF AD 80-11-04 A CRACK WAS FOUND IN 0432001-15 REINFORCEMENT. STAB REMOVED. PARTS REPLACED AN D AIRCRAFT RETURNED TO SERVICE. 1 H 7 1 3O 3 O 3A19 E252 1996102400066 19961024 00066 NE 1996 10 24 HEEA968168 2 19961009 A 7200 0292005220 ENGINE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE OIL SYS MAKING METAL E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 350BZ 1565 2653 MAKING METAL IN OIL AND FILTER. 1 G 7 1 3U 3 U H9EU E19EU 1996102400913 19961024 00913 NE 1996 10 24 WRLA96041 2 19961002 A 7310 AC922F1740 FUEL FILTER DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE NR 2 ENGINE CLOGGED A WRLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 107WA 46836 DURING TAXIING OUT, FLIGHT CREW NOTED NR 2 ENGINE FUEL FILTER PRESSURE DROP LIGHT ON, AIRCRAFT RETURNED TO GATE. MAINTE NANCE PERSONNEL REPLACED FUEL FILTER, GROUND RUN THE AIRCRAFT, NO FAULT NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F 4 F RT A22WE E23EA 1996103000002 19961030 00002 NM 1996 10 30 96UAL900781 1 19961007 A 3350 INVERTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 593UA 28144 EMERGENCY EGRESS LIGHTING ROWS 23 THROUGH 28 INOP. REPLACED INVERTER FOR EMERGENCY EGRESS LIGHTING, OPERATION CHECKS NO RMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996110100059 19961101 00059 WP 1996 11 1 CA960312025 1 19960223 A 6210 369D21100513M BLADE HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL M/R DEBONDING W K NONE O OTHER IN INSP/MAINT 1 CA 2702 CAE830896 (CAN)LEADING EDGE ABRASION STRIP DEBONDING. TIME THIS INSTALLATION 589.8 HOURS. 1 G 7 1 3U 3 U H3WE E4CE 1996110100585 19961101 00585 CE 1996 11 1 CA960321012 1 19960320 A 2434 ALU8421P ALTERNATOR PRESTOLITE ALU8421P BEECH 95 E95 1153410 CE LYC O360 IO360B1B 41514 EA RT ENG SHORTED FIELD W A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 CA 83 1111094 L496351A (CAN)DURING CLIMB BOTH ALTERNATORS WENT OFF LINE. AN INSPECTION REVEALED THAT THE RIGHT HAND COOLING FAN HAD SEPARATED F ROM THE ALTERNATOR AND SOME OF THE PIECES WERE FOUND INSIDE THE ALTERNATOR THUS SHORTING THE FIELD. THE SHORTED FIELD CA USED A VOLTAGE REGULATOR TRANSISTOR TO BLOW AND THE SECOND ALTERNATOR TO BLOW WHEN SELECTED. BOTH ALTERNATORS AND REGULA TORS WERE REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1 L 7 2 3O 3 O 3A16 1E10 1996110100590 19961101 00590 WP 1996 11 1 CA960321505 1 19960222 A 2130 21011404 PRESS.CONTROLLER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE NR 1 & NR 2 FAILED W B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 CA P657763D (CAN)AFTER TRAKEOFF AT FL.290, MASTER CAUTION LIGHT ILLUMINATED INDICATING A PRESSURIZATION PROBLEM. QRH DRILL CARRIED O UT, INITIATED EMERGENCY DESCENT AND MANUALLY DEPLOYED OXYGEN MASKS. ON RETURN MAINTEN ANCE ACTION INVOLVED CHANGING #1 A ND #2 PRESSURIZATION CONTROLLERS. 2 L 7 2 4F 4 F A6WE E2EA 1996110100883 19961101 00883 NE 1996 11 1 VTZA97003 2 19961001 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE RIGHT FAILED A VTZA O OTHER J WARNING INDICATION CR CRUISE 1 EA 27 301UE 41012 P76036 DURING FLIGHT FROM CHS-IAD, FLT 6476, CREW EXPERIENCED A RIGHT ENGINE OIL CONTAMINATION LIGHT ILLUMINATION. AIRCRAFT LA NDED AT IAD. MAINTENANCE PERFORMED ENGINE RUNS AFTER REMOVING CHIP DETECTOR AND FOUND SEVERAL SMALL METAL CHIPS ON THE DETECTOR. PENALTY RUNS COMPLETED AND CHIP DETECTOR REMOVED AND INSPECTED AGAIN. FOUND SMALL CHIPS ON DETECTOR AGAIN. F ERRIED AIRCRAFT TO LYNCHBURG FOR RIGHT ENGINE CHANGE. (M) 2 L 7 2 4T 4 T RT A41NM E18NE 1996110700498 19961107 00498 WP 1996 11 7 VTZA96398 2 19960928 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP LEFT MALFUNCTIONED A VTZA C ABORTED TAKEOFF D INFLIGHT SEPARATION TO TAKEOFF 1 EA 27 494UE 810 FLT 6181 - IAD-BWI - ABORTED TAKEOFF DUE TO LEFT ENGINE WOULD NOT MAKE TAKEOFF TORQUE. AIRCRAFT RETURNED TO GATE WITH N O FURTHER INCIDENTS. MAINTENANCE INSPECTED AND RAN AIRCRAFT BUT COULD NOT DUPLICATE, OPS CHECK OK. AIRCRAFT WAS RELEAS ED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 3 T RT A56EU E3WE 1996111400630 19961114 00630 NE 1996 11 14 CA960419008 2 19960413 A 7321 87043269 FUEL CONTROL HAMSTD 7898426009 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 MALFUNCTION W C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CA 13547 87043269 LH120403 (CAN)TORQUE ROLL EXPERIENCED ON TAKEOFF. #2 ECU REPLACED AWAITING RESULTS OF PWC STRIPDOWN 2 H 7 2 4T 4 T RT A13NM E20NE 1996112100352 19961121 00352 GL 1996 11 21 HEEA968474 2 19961113 A 7260 6876925 TUBE ASSY. 6894171 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL GEARBOX OUT OF SPEC E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4573B 5478 CAG38940 S673 CAE835939 ENGINE REMOVED DUE TO METAL IN OIL. UPON INSPECTION OF GEARBOX PARTS NOTED THE FOLLOWING:TUBE FAILED DIMENSIONAL CHECK PER CEB 1307. INSTALLED A NEW PART. 1 G 7 2 3U 3 U H3EU E4CE 1996112700025 19961127 00025 EA 1996 11 27 CA960513014 1 19960509 A 3060 3061K3 RELAY HAMSTD SFA13N1OA DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE HAMSTD 14SF 14SF15 NE PROP DE ICE FAILED W A O OTHER O OTHER IN INSP/MAINT 1 CA 123136 901117 (CAN)#1 AND #4 BLADES ON #1 PROPELLER BURNED BY DE-ICER BOOTS. NO GROUND SELECTION OR INDICATION WAS MADE. BLADES REPLAC ED. RELAY 3061-K3 REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1996120500466 19961205 00466 NE 1996 12 5 P5CA9600974 2 19961201 A 7200 ENGINE BOEING 747 747132 1384882 NM PWA JT9 JT9D7A 52054 NE NR 3 MALFUNCTIONED A P5CA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 WP 23 857FT 65786 1736 20246 662376 AFTER ENGINE START NR 3 ENGINE OIL QUANTITY DROPPED, OIL PRESSURE LOW AT IDLE POWER, NO OIL OVER TEMP. REMOVED FILTER A ND FOUND CARBON DEPOSITS. CLEANED, REINSTALLED, DRAINED OIL, RESERVICED, INSPECTED N2 TACK SHAFT FOR PLAY AND NONE FOUN D. PERFORMED ENGINE RUN, ALL PARAMETERS GOOD REFERENCE M/M 71-00-44. THOUGH NEXT FLIGHT NO FURTHER PROBLEMS ENGINE CHA NGED PRECAUTIONARY. 2 L 7 4 4F 4 F A20WE E20EA 1996121200242 19961212 00242 NE 1996 12 12 CA960614009 2 19960607 A 7230 ACTUATOR LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE IP COMPRESSOR OUT OF ADJUST W C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CA 10443 (CAN)REJECTED TAKEOFF DUE TO #3 ENGINE N2 OVERSPEED. IP COMPRESSOR MASTER RAM OUT OF ADJUSTMENT, ADJUSTED IN ACCORDANCE WITH MAINTENANCE MANUAL. 2 L 7 3 4F 4 F A23WE E12EU 1996121200271 19961212 00271 SO 1996 12 12 CA960620022 2 19960605 A 8530 CYLINDER SUPAIRPART SA10200A20P CESSNA 150 150L 2071826 CE CONT O200 O200A 17020 SO MCAULY 1A101 1A101HCM GL BARREL CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 1283 2052139A G10505 (CAN) OIL LEAK FOUND AFTER FLIGHT. ENGINE CYLINDER CRACKED 1/3 RD AROUND THE BARREL. 1 H 7 1 3O 3 O 3A19 E252 5 N P918 1996121900772 19961219 00772 SW 1996 12 19 CA960502019 1 19960302 A 2840 205061635005 SWITCH BELL 206 206L 1181522 SW ALLSN 250C 250C20B 03013 GL FUEL PRESS LOW PRESSURE W K NONE P NO WARNING INDICATION IN INSP/MAINT 1 CA 830805 (CAN) WHEN BOOST PUMP TURNED OFF, THE CAUTION LIGHT WOULD NOT COME ON FOR FUEL PRESSURE. 1 G 7 1 3U 3 U H2SW E4CE 1996122600558 19961226 00558 WP 1996 12 26 CA960627101 1 19960607 A 2612 351006 CONNECTOR CVAC 340 340CVAC 242270A WP ALLSN 501D 501D13 03004 GL #1 ENG ZONE 2 CORRODED W E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 CA 501533 (CAN) AIRCRAFT WAS IN CRUISE FLIGHT WHEN #1 ENGINE FIRE WARNING SOUNDED. ENGINE WAS SHUT DOWN AND AIRCRAFT CONTINUED ON FLIGHT. MAINTENANCE COULD NOT DUPLICATE FAULT AT FIRST BUT WARNING SOUNDED WHEN CHECKING FIRE LOOP CONNECTOR. REPLACED C ONNECTOR P/N 35100-6 BECAUSE OF CORROSION. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4R 4 T 6A6 E282 1997010800007 19970108 00007 EU 1997 1 8 CA960729017 1 19960722 A 5541 HC554H0050000U RIB BRAERO HC554H000200 BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE #1 RIB CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 16245 SAABDH150 LF05482A (CAN) FOUND A PIECE OF METAL APPROXIMATELY 8 INCHES SQUARE MISSING FROM #1 RIB OF THE RUDDER. 2 H 7 4 4F 4 F RT A49EU E6NE 1997010900412 19970109 00412 SO 1997 1 9 SWIA95806 1 19961230 A 3260 17038594001 CONTROL BOX EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT MLG MALFUNCTIONED A SWIA O OTHER N FALSE WARNING AP APPROACH 1 NM 07 195SW 120127 RIGHT MAIN GEAR SHOWED UNSAFE LIGHTS AFTER 3 CYCLES OF LANDING GEAR. REPLACED LANDING GEAR CONTROL BOX, SYSTEM CHECKS N ORMAL, RETRACTION TEST CHECKS NORMAL. CHECKED ACTUATOR ROD END AND A AND B HARNESS CHECKED FOR CONTAMINATION, ALL CHEC KS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1997011600168 19970116 00168 SO 1997 1 16 97ZZZX272 2 19961223 A 8550 631653 SPRING SEAT 642224 CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO OIL PRESS HSNG MISSING A OEZA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 19 26150 402C0111 278444R INSTALLED NEWLY OVERHAULED ENGINE AND DURING PRE-OILING COULD NOT GET OIL PRESSURE. FOUND THAT SPRING SEAT P/N 63153 WA S MISSING FROM OIL PRESSURE RELIEF HOUSING. INSTALLED THE MISSING PART, FIXED THE PROBLEM. 1 L 7 2 3O 3 O A7CE E8CE 1997011600288 19970116 00288 NM 1997 1 16 96UAL900960 1 19961223 A 2910 HYD LINES BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 3 MLG DAMAGED A UALA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS NR NOT REPORTED 1 WP 29 330UA 24191 RETURNED TO FIELD WITH LOSS OF HYDRAULIC PRESSURE AND QUANTITY. *S/D* HYDRAULIC PRESSURE AND QUANTITY LOSS DUE TO DAMA GE NR 3 MLG THROWN TREAD. REPAIRED AND/OR REPLACED LANDING GEAR SEQUENCING VALVE HYDRAULIC LINES, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 1997011600830 19970116 00830 WP 1997 1 16 VTZA96453 2 19961220 A 7321 310590055 FUEL CONTROL JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33110U 01514 WP LT ENGINE FAILED A A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 325UE 41063 FLT 6261 - IAD-EWR - ABORTED TAKEOFF DUE TO LEFT ENGINE WOULD ONLY MAKE 85 PERCENT TORQUE ON TAKEOFF ROLL. AIRCRAFT RET URNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED FCU, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 4 T RT A41NM E4WE 1997031300295 19970313 00295 1997 3 13 CA961009005 4 19960923 A 3425 7003360941 AHRS HONEYWELL DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE #1 SYS ROLL MISMATCH W D RETURN TO BLOCK I FLT. ATTITUDE INST. TO TAKEOFF 1 CA 86070507 123058 (CAN) ON START UP, CREW NOTED ADI ROLL MISMATCH ON #1 AHRS. CIRCUIT BREAKERS RESET, BUT PROBLEM REOCCURRED AFTER 2 MINU TES. AIRCRAFT POWERED DOWN AND AHRS RESET. PROBLEM SEEMED FIXED. ON ROTATION PROBLEM OCCURRED AGAIN. #1 AHRS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1997032000013 19970320 00013 EA 1997 3 20 CA961016010 1 19961002 A 2810 SPRING DHAV DHC6 DHC6300 EA PWA PT6 PT6A27 52043 EA #7 FUEL TANK INSIDE FUEL TANK W K NONE O OTHER IN INSP/MAINT 1 CA PCE40719 (CAN) DURING MAINTENANCE OF #7 FUEL TANK A STEEL SPRING WAS FOUND IN THE CELL. THE SPRING MEASURES 1 1/2 INCHES IN LENGT H AND 1/8 INCHES IN DIAMETER. IT IS BELIEVED THAT THE SPRING CAME FROM A FUEL NOZZLE NORMALLY FOUND AT AN AUTO GAS STATI ON. IT SHOULD NOT BE USED ON AIRCRAFT. 1 H 7 2 3T 4 T A9EA E4EA 1997032700093 19970327 00093 EU 1997 3 27 CA961104001 1 19961030 A 3233 HTE210014 ACTUATOR BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE MLG FAILED W L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 CA 3473 LF05463A (CAN) ON GEAR EXTENSION ON APPROACH GEAR WOULD NOT EXTEND. EMERGENCY EXTENSION CARRIED OUT. THREE GREEN LIGHTS BUT GEAR IN TRANSIT LIGHT REMAINED ON. GEAR DOWN LOCK PIN COULD NOT BE INSTALLED WITHOUT FORCE. GEAR SELECTOR ACTUATOR REPLACED. 2 H 7 4 4F 4 F RT A49EU E6NE 1997041500020 19970415 00020 NM 1997 4 15 CA961112045 1 19961031 A 3230 GROUND LOCK DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NOSE GEAR NOT STOWED W A D UNSCHED LANDING RETURN TO BLOCK J O WARNING INDICATION OTHER CL CLIMB 1 CA 120013 (CAN) ON CLIMB AFTER GEAR RETRACTED THE MAIN DOORS DID NOT CLOSE AND THE NOSE GEAR DID NOT RETRACT WITH THE NOSE DOORS A LSO STAYING OPEN. ALTERNATE EXTENSION CARRIED OUT AND AIRCRAFT LANDED. MAINTENANCE FOUND THE NOSE GROUND LOCK HAD NOT BE EN STOWED. 2 H 7 2 4T 4 T RT A13NM E20NE 1997061200824 19970612 00824 NE 1997 6 12 97ZZZX2751 2 19961117 A 7250 410106701 SEAL RING BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE 1ST TURB SHROUD WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 7060G 626 7173 LE45511EF SEAL RING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997091100452 19970911 00452 NE 1997 9 11 97ZZZX3932 2 19961117 A 7250 414129001 ROTOR ASSY BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE POWER TURBINE BLADE SHIFT A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 7060G 2116 626 7173 LE45511EF ENGINE FAILED SB LT101-72-10-0153. EXCESSIVE IBPT BLADE SHIFT. REPLACED WITH USED UNIT, CORRECTED PROBLEM. PART TOTAL CYCLES, 4,453.0. 1 G 7 2 3U 3 U H13EU E5NE10 1998021100009 19980211 00009 SO 1998 2 11 CA961030003 1 19961009 A 7930 PRESSURE SENSOR MAULE M7 M7235 5460170 SO LYC O540 IO540W1A5 41532 NE HOBBS METER FAILED W A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 CA L2491948A (CAN) AIRCRAFT LOST ALL OIL IN FLIGHT DUE TO HOBBS METER PRESSURE SENSOR FAILURE. 1 H 7 1 3O 3 O NC 3A23 1E4 1998021100122 19980211 00122 NE 1998 2 11 98ZZZX599 2 19960506 A 7310 430128601 MANIFOLD BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101650B1 41560 NE ENGINE FUEL LEAKS A RMXA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 05 117LU 186 70293C S7144 LE45700 SUBMITTER STATES EXCESSIVE FUEL MANIFOLD LEAKS OVER THE LAST 18 MONTHS. ALLIED SIGNAL IS IN THE PROCESS OF RELEASING AN ASB LIMITING THE LIFE OF THE FUEL MANIFOLD TUBES. OTHER OPERATORS SUBMITTER CONTACTED ARE HAVING THE SAME PROBLEMS. O MNIFLIGHT HAS GONE TO A POST-FLIGHT CHECK AND A SHIFT-CHANGE CHECK OF THIS MANIFOLD. 1 G 7 2 3U 3 U H13EU E5NE 1996042500439 19960425 00439 NM 1996 4 25 96FDEA00807 1 19960422 A 5330 SKIN BOEING 727 727227 1384078 NM BS 700 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 242FE 21178 CORROSION BS 700 STR 28L WL 148. REPAIRED CORRODED SKIN AT BS 700 STR 28L WL 148 PER FEDEX SRM 53-30-3. 2 L 7 3 4F A3WE 1996071800655 19960718 00655 EU 1996 7 18 96ZZZX3588 1 19960110 A 5210 1172428111 CATCHER BOLKMS 117 BK117B1 5626012 EU LT DOOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 5194C 790 7169 CATCHER WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1998042300183 19980423 00183 NM 1998 4 23 P5CA9601223 1 19960812 A 5280 PLATE BOEING 747 747121 1384871 NM NLG DOOR CHAFED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 832FT 20347 NOSE LANDING GEAR WHEEL WELL LT FWD DOOR, FLAPPER DOOR DEEP CHAFING ON CHAFING PROTECTION PLATE. NEW PLATE FABRICATED P ER SRM 52-80-01 AND 51-30-02. 2 L 7 4 4F A20WE 1996011900314 19960119 00314 NM 1996 1 19 96FDEA00059 1 19960116 A 7830 7800152 TR SWITCH BOEING 727 727225 1384077 NM NR 3 ENGINE FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 25 463FE 22551 AFTER ROTATION NR 3 REVERSER OPERATING LIGHT ILLUMINATED, PERFORMED APPROPRIATE CHECKLIST AND SHUTDOWN NR 3 ENG. REPLAC ED NR 3 ENG REVERSER SWITCH PER MM 78-30-00. OPS CHECKED NORMAL, PANELS SECURED. 2 L 7 3 4F A3WE 1996071000133 19960710 00133 WP 1996 7 10 ABXA9600566 1 19960524 A 5320 991154613 CLIP DOUG DC9 DC931 3022065 WP BS 996 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK INSPECTION, FOUND CRACKED CLIP AT CUSP WEB TO FRAME STA 996 AT LONGERON 18L. REPLACED CLIP IAW DC-9 SRM 51-10-4 AND 51-30-5. 2 L 7 2 4F A6WE 1996071800131 19960718 00131 NM 1996 7 18 96ZZZX3509 1 19960410 A 5330 PANEL BOEING 727 727232 1384082 NM BS 700-720 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 17789 20643 ACCESSORY PANEL AT STA 700 TO STA 720, LEFT LBL 15, EXTERIOR PANEL HAS LEVEL 2 EXFOLIATION CORROSION AROUND NUTPLATES. R EMOVED CORROSION AND TREATED. REINSTALLED PANEL PER SRM 51-10-6 AND SRM 51-30-2. MATERIAL LOSS WITHIN LIMITS PER SRM 5 3-10-1, FIGURE 1. 2 L 7 3 4F A3WE 1996012600773 19960126 00773 WP 1996 1 26 96FDEA00123 1 19960125 A 3260 ARG7531 TARGET SENSOR DOUG DC10 DC1010F 3022111 WP LT MLG BROKEN A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 40061 46973 LEFT MAIN GEAR INDICATION ON BOTH PANELS REMAINED RED AFTER RETRACTION. RAN CHECK LIST PROCEDURES WITHOUT SUCCESS. SUB MITTER FEELS THE GEAR IS RETRACTING AND EXTENDING OK, BUT LIGHTS STAY RED. FOUND TARGET SENSOR ON MAIN GEAR DOOR BROKEN . REPLACED TARGET SENSOR PER MM 32-6. 2 L 7 3 4F A22WE 1996062000332 19960620 00332 NM 1996 6 20 AWXA960213 1 19960422 A 5330 SKIN BOEING 737 737277 1384570 NM BS 715-716 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 178AW 22645 PAE - FLT 3808 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND CRACK IN KEEL BEAM SKIN STA 715 TO STA 716, RBL 5 WL 148.5. REPAIRED PER ER 2-53-15-23, TCO-PAN-96-0521RR AND 8110.3. ACFT TT: 44,382 HRS. ACFT TC: 36,778. (X) 2 L 7 2 4F RT A16WE 1996051600343 19960516 00343 NM 1996 5 16 96UAL900341 1 19960513 A 3350 BATTERY PACK BOEING 737 737522 138449F NM CABIN DISCHARGED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 908UA 25008 EMERGENCY EXIT LIGHT INOP AT DOOR ONE LEFT. REPLACED BATTERY PACK, CHECKS OK. 2 L 7 2 4F RT A16WE 1996061300535 19960613 00535 WP 1996 6 13 AALA960760 1 19960509 A 5320 ANGLE DOUG DC10 DC1010 3022110 WP BS 700 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 TUL - FOUND CORROSION UNDER SLANT PANEL LANDING (2 ANGLE) LEFT SIDE OF FORWARD CARGO (LOWER GALLEY). INSTALLED NEW 'Z' CHANNEL FROM STATION 625 TO STATION 235 AARD 51-01-00-05 ITEM 5 PAGE 1. (M) 2 L 7 3 4F A22WE 1996012600099 19960126 00099 NM 1996 1 26 96UAL900043 1 19960118 A 3350 LEADER LINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 509UA 24763 FLOOR EMERGENCY ESCAPE LIGHTING INOP AFT LAVATORY AREA. REPLACED LEADER LINE FLOOR EMERGENCY ESCAPE LIGHTING AT AFT LAV ATORY AREA AND OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1996020200594 19960202 00594 NE 1996 2 2 9602369750 2 19960131 A 7314 7915PUMPASSY FUEL PUMP DOUG DC9 DC941 302207N WP PWA JT8 JT8D11 52044 NE NR 1 ENGINE FAILED A NWAA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 GL 01 750NW 14462 14462 47114 676231 DURING CLIMBOUT, THE NR 1 ENGINE FLAMED OUT. THE FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLA CED THE FUEL CONTROL UNIT WITH A SERVICEABLE PART. 2 L 7 2 4F 4 F A6WE E2EA 1996020900229 19960209 00229 NM 1996 2 9 DLM88960241 1 19960130 A 2170 COALESCER BAGS DOUG MD88 MD88 3023688 NM PWA JT8 JT8D15A 52051 NE CABIN DIRTY A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 912DL 49543 700576 ON DESCENT, AT 1,200 WITH WING/ENG ANTI-ICE ON, CABIN FILLED WITH STRONG ODOR AND HAZE, SETTING OFF ALL 3 SMOKE DETECTOR S. TURNED WING ANTI-ICE AND PACKS S/W TO HP BLEEDS OFF, WHICH BEGAN TO CLEAR CABIN BY LANDING. REPLACED WATER SEPARATO R BAGS, RAN APU AND BOTH ENGINES WITH PACKS ON. AIRFLOW ANTI-ICE ON, OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A6WE E2EA 1996022300015 19960223 00015 SO 1996 2 23 96ZZZX722 2 19960119 A 8540 639406 SHAFT 642085A4 CESSNA 401 401A 207590D CE CONT O520 TSIO520E 17040 SO STARTER/ADAPTER SHEARED A VUMA K NONE O OTHER IN INSP/MAINT 1 WP 13 7816Q 3 77371 402A0116 183356 INSTALLED REBUILT STARTER/ADAPTER AFTER PREVIOUS ONE FAILED AFTER 26 HOURS OF USE. THIS CURRENT ONE, SN 77371, FAILED A FTER 2.5 HOURS AND SIX STARTS DUE TO THE SAME PROBLEM - SHEARED GEAR. 1 L 7 2 3O 3 O A7CE E8CE 1996031500419 19960315 00419 NM 1996 3 15 96UAL900184 1 19960312 A 5753 654783612 TOGGLE BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE LT TE FOREFLAP BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 9038U 19076 DURING INSPECTION OF FLAPS FOR A AIRCRAFT ROLLING PROBLEM WITH FLAPS AT 10 DEGREES, FOUND LEFT SIDE FOREFLAP LOOSE FROM MIDFLAP. LEFT OUTBOARD TOGGLES WERE FOUND BROKEN. AIRCRAFT HAD BEEN DE-ICED WITH TYPE II FLUID 55 HOURS PREVIOUS TO TH E INCIDENT. TOGGLE ASSEMBLIES WERE REPLACED BOTH INBOARD AND OUTBOARD. RUB STRIPS AND SLIDERS WERE CHECKED AND FOUND W ITHIN LIMITS. COMPONENTS WERE LUBED. 2 L 7 2 4F 4 F A16WE E2EA 1996032200953 19960322 00953 WP 1996 3 22 WTAA960050 2 19960304 A 7321 89778021 FUEL CONTL UNIT BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33112UAR 01514 WP RT ENGINE FAILED A WTAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 17 425UE 798 SFO - NR 2 ENGINE FAILED TO ACHIEVE REQUIRED TORQUE ON TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE DEF ERRED TTL SYSTEM PER MEL 76-2. ENGINE OPERATIONS REPORTED NORMAL DURING GROUND RUN WITH TTL OFF. AIRCRAFT RETURNED TO SERVICE. TTL SYSTEM DEFERRAL CLEARED AFTER THE REPLACEMENT OF THE RT ENGINE FUEL CONTROL UNIT. (X) 2 L 7 2 4T 4 T RT A21EU E4WE 1996050200376 19960502 00376 NE 1996 5 2 9609471158 2 19960430 A 7321 FUEL CONTROL DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 1 ENGINE MALFUNCTIONED A NWAA D E RETURN TO BLOCK ENGINE SHUTDOWN O OTHER TX TAXI/GRND HDL 1 GL 01 158US 46767 686169 WHILE WAITING FOR TAKEOFF, THE NR 1 ENGINE COMPRESSOR STALL OCCURRED AT ENGINE IDLE POWER. EGT TEMPERATURE REACHED 700 CELSIUS AND THE NR 1 ENGINE WAS SHUTDOWN. AIRCRAFT RETURNED TO THE GATE. GROUND MAINTENANCE REPLACED THE ENGINE VANE C ONTROL, PERFORMED ENGINE GROUND RUN. FUEL CONTROL AND ENGINE VANE CONTROL TRIM CHECKED GOOD. 2 L 7 3 4F 4 F A22WE E20EA 1996050200514 19960502 00514 EA 1996 5 2 GLBA96060 2 19960324 A 7200 ENGINE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA RIGHT FAILED A GLBA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 CE 01 60UE 11082 UC60 OMA - CREW REPORTED OIL PRESSURE ON RIGHT ENGINE DROPPED. THEY SHUTDOWN RIGHT ENGINE AND MADE AN UNEVENTFUL LANDING. M AINTENANCE REMOVED AND REPLACED RIGHT ENGINE WITH SERVICEABLE. RUN AND LEAK CHECKS WERE GOOD. (M) 2 L 7 2 4T 4 T RT A24CE E4EA 1996050200549 19960502 00549 WP 1996 5 2 VTZA96130 2 19960328 A 7320 89778025 FUEL CONTL UNIT BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT ENG OUT OF ADJUST A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 479UE 2428 739 893 P66057 FLT NR 6296 - IAD-ROC - ABORTED TAKEOFF DUE TO THE LEFT ENGINE ONLY MAKING 95 PERCENT ON THE TAKEOFF ROLL. AIRCRAFT RET URNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED THE MAX FUEL FLOW. AIRCRAFT WAS RELEASED AND APPROVED FO R RETURN TO SERVICE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996050900291 19960509 00291 NE 1996 5 9 PLG4896G1 2 19960101 A 7260 5034T98P02 AGB DRIVESHAFT SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LT ENGINE BROKEN A PLGA A UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 NE 05 340BE 4557 APEJ4073 340A062 367375 BOS/DCA - FLT 4609 - THIS SDR IS TO CLOSE OUT AN OPEN SDR DATED 1-1-96 IN WHICH FLIGHT EXPERIENCED A FLAME-OUT OF THE LE FT ENGINE AND CHIP LIGHT ILLUMINATION. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT WHICH HAD DIVERTED TO ACY, AND REMOVE D AND REPLACED THE ENGINE RETURNING THE AIRCRAFT TO SERVICE. TEAR DOWN OF THE ENGINE FOUND A SHEARED RADIAL DRIVE SHAFT WHICH CAUSED LOSS OF CONTACT BETWEEN THE NG ROTOR AND THE ACCESSORY GEARBOX. CHIPS FROM THE SHAFT WERE FOUND IN THE OI L SYSTEM. 2 L 7 2 4T 4 T RT A52EU E8NE6 1996060600467 19960606 00467 NE 1996 6 6 96ZZZM915 2 19960425 A 7530 7665557 BLEED CONTROL BOEING 767 767231 1385131 NM PWA JT9 JT9D7R4D 52054 NE NR 1 ENGINE MALFUNCTIONED A TWAA O OTHER R PARTIAL RPM/PWR LOSS CL CLIMB 1 CE 05 605TW 22568 4624 JFK - FLT 31 - AT TOP OF CLIMB, NR 1 ENGINE ENCOUNTERED POWER SURGE. REDUCED POWER AND REAPPLIED POWER. FOUND ENGINE V ANE BLEED CONTROL, MFG P/N 766555-7, MALFUNCTIONING. CHANGED ENGINE VANE BLEED CONTROL AND ENGINE OPERATION CHECKED NOR MAL. 2 L 7 2 4F 4 F RT A1NM E3NE 1996062000148 19960620 00148 NM 1996 6 20 96UAL900445 1 19960612 A 3350 900542U1 BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE BS 800 DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7283U 21561 OVERHEAD EMERGENCY LIGHT ROW 8 INOPERATIVE. *S/D* BATTERY SUPPLYING POWER FOR AISLE LIGHTS AT ROW 3 AND ROW 8 HAS REDUC ED VOLTAGE. BATTERY REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 1996062000605 19960620 00605 SO 1996 6 20 WTAA960104 1 19960520 A 7330 MS3456W10SL3S CONNECTOR EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE LOOSE A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 17 251YV 120251 SMF - RIGHT ENGINE FILTER LIGHT ILLUMINATED ON TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. DEFERRED INDICATOR PER M EL 73-33-1. AIRCRAFT RETURNED TO SERVICE. MX SUBSEQUENTLY CLEARED DEFERRAL WITH CLEANING OF RIGHT ENGINE LOW PRESSURE FILTER CANNON PLUG AND THE PRECAUTIONARY REPLACEMENT OF FUEL FILTERS. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1996071000389 19960710 00389 NM 1996 7 10 VNAA9607004 1 19960707 A 5610 001A561A0000201 WINDSHIELD DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT COCKPIT CRACKED A VNAA K NONE O OTHER CR CRUISE 1 GL 07 427JS 3039 IN LEVEL FLIGHT AT APPROXIMATELY FL 200, CREW REPORTED A FAILURE OF THE FIRST OFFICER'S FRONT WINDSHIELD. CREW FOLLOWED ABNORMAL PROCEDURES AS SPECIFIED IN THE QUICK REFERENCE HANDBOOK. AIRCRAFT CONTINUED ON WITH THE FLIGHT AND LANDED IN PIT WITHOUT FURTHER INCIDENT. REPLACED THE F/O'S WINDSHIELD IAW MM 56-10-00. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1996071800277 19960718 00277 WP 1996 7 18 96UAL900502 1 19960703 A 3350 EMSE299 BATTERY PACK DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1814U 46613 MID AFT EMERGENCY LIGHTS POWER SUPPLY FAILED BITE TEST. *S/D* REPLACED POWER SUPPLY AND BATTERY. 2 L 7 3 4F 4 F A22WE E23EA 1996072500603 19960725 00603 EU 1996 7 25 96UAL900547 1 19960717 A 3350 116502 LAMP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 426UA 510 AFT DOOR EXIT SIGN REMAINED ON AFTER TEST. *S/D* REPLACED LAMPS IN EXIT SIGNS. SYSTEM OPERATIONALLY CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 1996082200169 19960822 00169 GL 1996 8 22 HEEA967656 2 19960816 A 7260 6898981 IDLER GEAR 23063380 ALLSN 250C 250C30S 03013 GL GENERATOR MAKING METAL E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 55 CAG44017 CAE844017 ENGINE REMOVED DUE TO METAL GENERATION. UPON INSPECTION OF GEARBOX PARTS NOTED: IMPROPER FINISH MACHINING ON GENERATOR IDLER GEARSHAFT GEAR TEETH, SPALLING GEAR TEETH WITH LARGE CHIPS OF METAL MISSING IN 3 AREAS CAUSING METAL PICKOUT ON S TARTERGENERATOR GEARSHAFT AND HMU-O/P GEARSHAFT.1 (REMOVED FROM AIRCRAFT N49001, MODEL 430) (ALLISON ENGINE MODEL 250-C 40B) INSTALLED NEW PARTS 3 U E1GL 1996082200589 19960822 00589 NE 1996 8 22 96UAL900483 2 19960625 A 7261 697063 BEARING BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE RT SCAVENGE PUMP FAILED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 WP 29 612UA 10850 21873 709669 AN INFLIGHT SHUT DOWN OCCURRED ON THE RIGHT ENGINE DUE TO LOW OIL PRESSURE. AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO AMBER ALERT INDICATION. *S/D* THE NUMBER 3 AND 4 BEARING SCAVENGE PUMP DRIVE IDLER GEAR BEARING FAILED. REPLACED MA IN GEARBOX ASSEMBLY, OPERATIONS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 1996082900739 19960829 00739 NE 1996 8 29 RAIA960808 2 19960808 A 7261 3033916 OIL LINE AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE NR 2 ENGINE LEAKING A RAIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CE 03 EICBK 15425 199 120561 STL - FLT 7518 - NR 2 ENGINE OIL PRESSURE FLUCTUATING AND EICAS LIGHT ILLUMINATED. MAINTENANCE REPLACED THE NR 1 BEARIN G OIL TRANSFER LINE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1996090500245 19960905 00245 NE 1996 9 5 CA960111015 2 19960109 A 7230 674222 FAN PWA BOEING 737 737210C 1384459 NM PWA JT8 JT8D9A 52048 NE 1ST STAGE BLADES CRACKED W K NONE C F.O.D. IN INSP/MAINT 1 CA 674222 (CAN)DURING A ROUTINE "A" CHECK F.O.D. WAS FOUND ON TWO 1ST STAGE FAN BLADES ON #1 ENGINE. DAMAGE WAS BEYOND LIMITS AND THE 1ST STAGE FAN WAS REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1996090500319 19960905 00319 WP 1996 9 5 CA960123013 1 19960112 A 7810 C16917 CLAMP ROBSIN R44 R44 7640120 WP LYC O540 O540F1B5 41532 EA TAIL PIPE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA L2453840A (CAN)TAIL PIPE ATTACHMENT CLAMP P/N C169-17 WAS FOUND CRACKED ACROSS BOTH WELDS AND CLAMP. 1 G 7 1 3O 3 O H11NM E295 1996091200023 19960912 00023 NM 1996 9 12 96UAL900663 1 19960829 A 3397 58781 WIRE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 365UA 24534 EMERGENCY ESCAPE PATH LIGHTING INOP FROM ROW 17 TO AFT OF CABIN. REPLACED POWER CABLE STRIP IN CHANNEL. CHECKS O.K. 2 L 7 2 4F 4 F RT A16WE E2GL 1996091900540 19960919 00540 EU 1996 9 19 CA960126022 1 19960109 A 2913 350A35013004 DRIVE PULLEY SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1B 6OO30 NE HYD MISSING SPLINES W K NONE O OTHER IN INSP/MAINT 1 CA 290 (CAN)REMOVED IN CONJUNCTION WITH HYDRAULIC PUMP INSPECTION. FOUND SPLINED SHAFT MISSING TEETH. 1 G 7 1 3U 3 U H9EU E19EU 1996100300237 19961003 00237 NE 1996 10 3 96UAL900725 2 19960921 A 7261 FILTER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE DIRTY A UALA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 7457U 21911 700138 NUMBER 1 ENGINE OIL FILTER BYPASS LIGHT CAME ON WITH OIL PRESSURE INDICATING 43 PSI. LIGHT REMAINED ON AFTER REDUCING E NGINE THRUST. *S/D* EXCESSIVE CARBON FOUND IN MAIN OIL FILTER. CLEANED CARBON FROM PRESSURE SWITCH AND REPLACED FILTE R. RECHECKED FILTER AFTER 12 HOURS AND NO CARBON FOUND. 2 L 7 3 4F 4 F A3WE E2EA 1996101000554 19961010 00554 NE 1996 10 10 EIAA9630 2 19960902 A 7261 OIL CAP BOEING 747 747212B 1384886 NM PWA JT9 JT9D7J 52054 NE NR 2 ENGINE LOOSE A EIAA E ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 NM 09 485EV 20712 662247 JED - FLT NR 2 ENGINE PRECAUTIONARY SHUTDOWN DUE TO OIL QTY EMPTY TO .25 AND OIL PRESSURE 5 PSI. TEMPERATURE WAS 100 DE GREE CELSIUS, SAME AS OTHER 3 ENGINES. ALL OTHER ENGINE PARAMETERS WERE NORMAL. OIL TANK FILLER CAP DISLODGED AND FOUN D AT THE BOTTOM OF THE COWLING. PERFORMED WINDMILLING INSPECTION IAW MM AND FOUND OK. SERVICED OIL AND PERFORMED ENGIN E RUN. NO LEAKS NOTED. (M) 2 L 7 4 4F 4 F A20WE E20EA 1996102400425 19961024 00425 WP 1996 10 24 CA960223014 2 19960126 A 7200 ENGINE LEAR 35 35LEAR 5170600 CE GARRTT TFE731 TFE73122B 01518 WP LT ENGINE MAKING METAL W A E ENGINE SHUTDOWN J M WARNING INDICATION OVER TEMP CR CRUISE 1 CA P74111C (CAN)DURING CRUISE, L/H CHIP LIGHT CAME ON. ENGINE STARTED VIBRATING AND ITT STARTED RISING. ENGINE WAS SHUT DOWN. ON AR RIVAL, OIL FILTER WAS INSPECTED AND LARGE AMOUNT OF METAL WAS FOUND. ENGINE REPLACED. 2 L 7 2 4F 4 F A10CE E6WE 1996110700262 19961107 00262 WP 1996 11 7 CA960328007 2 19960315 A 7322 89737524 FCU GARRTT TPE331 TPE33111U 01514 WP ENGINE SURGING W A D E UNSCHED LANDING RETURN TO BLOCK ENGINE SHUTDOWN O OTHER CR CRUISE 1 CA 44717 (CAN) POWER SURGING WHEN POWER LEVERS ADJUSTED. AIRCRAFT RETURNED TO BASE, SHUT DOWN ENGINE AND LANDED WITHOUT INCIDENT. FCU BELLOWS FOUND DAMAGED. 4 T E4WE 1996110700837 19961107 00837 NM 1996 11 7 VNAA9610005 1 19961017 A 5220 001A522A0912202 COVER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE ESCAPE HATCH CRACKED A VNAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 328JS 3030 AFTER DEPARTURE, A LOAD SQUEAL STARTED COMING FROM THE COCKPIT EMERGENCY ESCAPE HATCH. AIRCRAFT RETURNED TO FIELD WITHO UT FURTHER INCIDENT. UPON INSPECTION, MAINTENANCE DETERMIND THAT THE ACRYLIC COVER ON THE ESCAPE HATCH HAD BROKEN. MAI NTENANCE REMOVED AND REPLACED THE ACRYLIC COVER. 2 H 7 2 4T 4 T RT A45NM E20NE 1996112100187 19961121 00187 EA 1996 11 21 CA960502047 2 19960416 A 7310 3011849 BY PASS LINE PWA 25242811 BEECH 100 100BEECH 1152916 CE PWA PT6 PT6A28 EA FCU LEAKING W K NONE K FLUID LOSS TX TAXI/GRND HDL 1 CA PCE50074 (CAN)ON SHUTDOWN, FUEL DRIPPING FROM #1 ENGINE COWLING. FUEL BY-PASS LINE TO FUEL CONTROL UNIT LEAKING AT THE FERRULE. U NDER PRESSURE, FUEL SPRAYED OVER THE FCU AND ENGINE. LINE REPLACED. 1 L 7 2 3T 4 T A14CE E4EA 1996112700229 19961127 00229 1996 11 27 96UAL900876 4 19961115 A 3418 10620475 SENSOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 WP 29 395UA 24670 JUST AFTER LIFT OFF GOT STICK SHAKER, AIRSPEED INCREASING TO 190 KNOTS. LEADING EDGE FLAP TRANSIT LIGHT ON FOR 5 TO 10 SECONDS, THEN BACK TO NORMAL GREEN. STICK SHAKER CONTINUED THROUGHOUT FLIGHT, MASTER CAUTION DID NOT UNTIL RECALLED AND STAYED ON THE REMAINDER OF FLIGHT. *S/D* THE LEFT STALL WARNING ANGLE OF AIRFLOW SENSOR WAS FOUND DAMAGED. REPLACED DAMAGED SENSOR, SYSTEM CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1996120300034 19961203 00034 1996 12 3 CA960422009 4 19960411 A 6113 15573005 BULKHEAD CESSNA CESSNA 337 337G 2075730 CE CONT O360 IO360G 17025 SO MCAULY 2AF34C D2AF34C306 GL PROP SPINNER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 4102 352415 766426 (CAN)REAR ENGINE PROP SPINNER BULKHEAD ASSEMBLY CRACKED IN NUMEROUS PLACES STARTING AT THE PROP MOUNTING HOLES RUNNING R ADIALLY TO OUTER DIAMETER. 1 H 7 2 3O 3 O A6CE E1CE 5 C P5EA 1996120500058 19961205 00058 NE 1996 12 5 DL73E962538 2 19961117 A 7510 655812310 ANTI-ICE DUCT BOEING 737 737247 138448D NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE BLOWN A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 379DL 23606 RIGHT ENGINE OVERHEAT LIGHT CAME ON ABOUT 1 MIN AFTER TAKEOFF. RETARDED THROTTLE TO IDLE AND LIGHT WENT OUT. RETURNED TO ABE. FOUND RT ANTI-ICE DUCT BLOWN AT 13TH STAGE TAPOFF. REPLACED DUCT, RAN ENG AND LEAK CHECKED. 2 L 7 2 4F 4 F A16WE E2EA 1996120500403 19961205 00403 EA 1996 12 5 CA960611012 2 19960524 A 7414 2080179 MAGNETO BENDIX ES106825601 CESSNA 182 R182 2072734 CE LYC O540 O540J3C5 41532 EA MCAULY 2D34C B2D34C214 GL RH SIDE FAILED W A D RETURN TO BLOCK E VIBRATION/BUFFET TX TAXI/GRND HDL 1 CA 2080179 L2281840A 778345 (CAN)ON PRE TAKEOFF RUN-UP, RIGHT MAGNETO CUT OUT COMPLETELY AT 1500 RPM IGNITION SWITCH AND WIRING CHECKED AND SERVICE ABLE CAPACITORS INSTALLED, SAME RESULT DUAL MAGNETO REPLACED 1 H 7 1 3O 3 O RT 3A13 E295 5 C P7EA 1996121800016 19961218 00016 EA 1996 12 18 CA960715010 2 19960610 A 8530 VALVE CESSNA 182 R182 2072734 CE LYC O540 O540J3C5 41532 EA MCAULY 2D34C B2D34C214 GL #3 CYL EXH DISINTEGRATED W A K NONE R PARTIAL RPM/PWR LOSS CR CRUISE 1 CA 1808 L2023840A 776774 (CAN) DURING FLIGHT THE PILOT REPORTED LOSS OF ENGINE POWER. POST FLIGHT INVESTIGATION FOUND THE #3 CYLINDER EXHAUST VAL VE HAD COMPLETELY DISINTEGRATED. AFTER REPLACING THE #3 CYLINDER A RUN-UP WAS CARRIED OUT. EXCESSIVE ENGINE VIBRATION WA S EVIDENT. FURTHER INVESTIGATION REVEALED THAT METAL PARTICLES FROM THE DISINTEGRATED #3 CYLINDER EXHAUST VALVE HAD CAUS ED METAL CONTAMINATION OF THE ENGINE. 1 H 7 1 3O 3 O RT 3A13 E295 5 C P7EA 1996121900854 19961219 00854 GL 1996 12 19 CA960619016 2 19960521 A 7412 103871501 IGNITION EXCITER BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE FAILED W O OTHER O OTHER IN INSP/MAINT 1 CA CAE820243 (CAN) IGNITION EXCITER UNIT FAILED, NO SPARK TO IGNITER PLUG. UNIT REPLACED, AIRCRAFT RETURNED TO SERVICE. 1 G 7 1 3U 3 U H2SW E4CE 1996121900865 19961219 00865 SW 1996 12 19 CA960619029 1 19960613 A 5320 206 LOWER BOX BEAM BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL LOWER SKIN CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 16157 CAE820180B (CAN) CRACK FOUND IN LOWER BOX BEAM SKIN JUST OVER TWO INCHES LONG COMING FROM THE SECOND RIVET FORWARD LEFT HAND SIDE F ROM AFT. 1 G 7 1 3U 3 U H2SW E4CE 1996122600028 19961226 00028 GL 1996 12 26 HEEA968732 2 19961213 A 7314 3865005 FUEL PUMP BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENGINE MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 724MB S756 FUEL PUMP FAULTY. ALSO CHANGED FILTER 1 G 7 2 3U 3 U H3EU E4CE 1996122600340 19961226 00340 WP 1996 12 26 96UAL900928 1 19961206 A 2710 ARH0450503 ROD DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL AILERON ACT BINDING A UALA K NONE O OTHER NR NOT REPORTED 1 WP 29 1838U 30000 46632 RIGHT HAND OUTBOARD AILERON WILL NOT ALIGN WITH CONTROL WHEEL CENTERED. *S/D* AILERON ACTUATOR SPRING CARTRIDGE INPUT ROD FOUND BINDING. REPLACED ROD. 2 L 7 3 4F 4 F A22WE E23EA 1996122600568 19961226 00568 WP 1996 12 26 CA960703023 1 19960620 A 3411 856CR9 PITOT TUBE LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE CAPT AIR SPEED CRACKED W C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CA 10471 (CAN) REJECT TAKEOFF AT 80 KNOTS DUE TO NO AIRSPEED INDICATION ON CAPTAIN'S SIDE. PITOT TUBE REPLACED. 2 L 7 3 4F 4 F A23WE E12EU 1996122600614 19961226 00614 EA 1996 12 26 CA960722002 1 19960708 A 2131 60539 COMPUTER DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE CABIN PRESS CONT FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 60539 123125 (CAN) ON CLIMB CABIN WOULD NOT PRESSURIZE, DIFFERENTIAL WENT UP TO 10 AND THEN BACK TO ZERO MAINTENANCE REPLACED CABIN PRESSURE CONTROLLLER COMPUTER 2 H 7 2 4T 4 T RT A13NM E20NE 1997010900321 19970109 00321 NE 1997 1 9 97ZZZX47 2 19960916 A 7250 410106802 SPRING BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE SEAL RING WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 10UM 245 7231 LE45807F SEAL RING SPRING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1997012300239 19970123 00239 NM 1997 1 23 96UAL901009 1 19961231 A 2750 HYDRAULIC MOTOR 240863 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE TE FLAPS FAILED A UALA O OTHER F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 WP 29 7295U 21573 INBOARD TRAILING EDGE FLAPS DO NOT EXTEND FULLY HYDRAULICALLY OR ELECTRICALLY ON APPROACH FOR LANDING. *S/D* REPLACED INBOARD FLAP HYDRAULIC MOTOR AND SYSTEM CHECKED OK. 2 L 7 3 4F 4 F A3WE E2EA 1997013000502 19970130 00502 CE 1997 1 30 CA960909026 1 19960904 A 3260 35361133 BRACKET BEECH 95 E95 1153410 CE LYC O360 IO360B1B 41514 EA MAIN GEAR SLIPPED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA L496351A (CAN) AFTER TAKEOFF, THE LANDING GEAR FAILED TO RETRACT, THE AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. A SUBSEQUENT INSPECTION REVEALED THAT THE LANDING GEAR SAFETY SWITCH HAD SLIPPED THUS NOT ACTUATING THE SWITCH WHEN THE GEAR WAS FUL LY EXTENDED. THE SAFETY SWITCH WAS SECURED, ADJUSTED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1 L 7 2 3O 3 O 3A16 1E10 1997022700325 19970227 00325 NE 1997 2 27 ORJA96116 2 19961209 A 7230 COMPRESSOR DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE NR 1 ENGINE STALLED A ORJA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 11 753RA 49587 708147 ON TAKEOFF NORMAL POWER ABOUT 800 AGL LEFT ENGINE COMPRESSOR STALLED, THROTTLE REDUCED TO IDLE. POWER ADVANCED ENGINE R AN OK. RETURNED TO RENO. REMOVED AND REPLACED NR 1 ENGINE IAW CARD 0099 AND MM 71-00-00. ALL PARAMETERS NORMAL, NO LE AKS NOTED. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 1997032000142 19970320 00142 NM 1997 3 20 CA961025013 1 19961024 A 2760 SWITCH DHAV DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE LT SPOILER BROKEN WIRE W K NONE O OTHER IN INSP/MAINT 1 CA 120442 (CAN) RECURRING DEFECTS FOUND OF BROKEN SPOILER CLUTCH WIRES. IN THIS CASE THE LEFT UPPER WIRE AT THE SWITCH. 2 H 7 2 4T 4 T RT A13NM E20NE 1997040200004 19970402 00004 EU 1997 4 2 CA961018026 1 19961007 A 3246 AHA1438 WHEEL ASSEMBLY DUNLOP AHA1489 BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE NR 2 MAIN BROKEN W A K NONE D INFLIGHT SEPARATION TO TAKEOFF 1 CA 10411 MJ156 LF05482A (CAN) A PIECE OF AIRCRAFT WHEEL FOUND ON RUNWAY, AFTER AIRCRAFT TAKEOFF. THE #2 MAIN LANDING GEAR WHEEL WAS MISSING ABOU T 1 FOOT OF THE BEAD AREA. THE TIRE WAS STILL INFLATED. 2 H 7 4 4F 4 F RT A49EU E6NE 1998020500603 19980205 00603 CE 1998 2 5 CA961001001 1 19960909 A 5522 SKIN BEECH 100 100BEECH 1152916 CE PWA PT6 PT6A28 EA ELEV UPPER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 11300 PCE50617 (CAN) UPPER ELEVATOR SKIN FOUND CRACKED AT THE AFT EDGE BEHIND THE LEADING EDGE SKIN. LOCATED JUST OUTBOARD OF THE OUTBO ARD HINGE. CRACK APPROXIMATELY 3 1/2INCHES LONG. REPAIRED PER BEECH DRAWING. 1 L 7 2 3T 4 T A14CE E4EA 1998040200043 19980402 00043 SW 1998 4 2 CA970311017 1 19960705 A 2810 DOUBLER BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL FUEL CELL DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA 14691 CAE801518BA (CAN) FUEL CELL DOUBLERS DAMAGED. 1 G 7 1 3U 3 U H2SW E4CE 1998042300052 19980423 00052 NM 1998 4 23 96UAL900819 1 19961018 A 3350 BATTERY PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7294U 21572 EEL STRIP INOP FROM ROW 26 AFT APPROXIMATELY 12 FEET. REPLACED POWER CONDUIT TO AFT STRIP SECTIONS AND BATTERY PACK, OP S CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1996012600184 19960126 00184 NM 1996 1 26 96FDEA00106 1 19960108 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 950 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 487FE 21490 AFT CX COMP STR 29L IS CORRODED ON O/B SIDE AT BELLFRAME STA 950E, AFT SIDE OF BELLFRAME. BEYOND LIMITS PER SRM 53-10-1 , REPAIRED PER FEDEX EA 7-5310-26899. 2 L 7 3 4F A3WE 1996061300337 19960613 00337 NM 1996 6 13 96FDEA01075 1 19960605 A 5320 655045312 SUPPORT BEAM BOEING 727 72722 1384002 NM BS 328-345 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 198FE 19154 NR 0647, (002) WHILE WORKING NR0348 AFTER REMOVING RT LWR NOSE CHORD FOUND DRAG BRACE SUPPORT BEAM TO BE CORRODED OUT OF LIMITS PER SRM AT BS 328 TO 345 WL 148 RBL 15. *S/D* REMOVED AND REPLACED DRAG BRACE SUPPORT T-BEAM AT BS 328 TO 345 W L 148 RBL 15, INSTALLED PER DRAWING 65-18415. 2 L 7 3 4F A3WE 1996071800810 19960718 00810 WP 1996 7 18 96ZZZM1086 1 19960512 A 3233 ACTUATOR DOUG DC9 DC932 3022066 WP NLG FAILED A VJ6A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 966VV 47168 ON FLT 404 - ATL-CLT - AIR RETURN, THE NOSE GEAR DID NOT RETRACT AFTER TAKEOFF, LANDED NORMAL. TROUBLESHOT AND ADJUSTED DOORS PER DC MM 32-20-0. REMOVED AND REPLACED NOSE GEAR RETRACT CYLINDER PER DC MM 32-32-6. PERFORMED NLG EXTENT, RET RACT AND EMERGENCY EXTENSION PER DC MM 32-30-0, OPS CHECK NORMAL. (M) 2 L 7 2 4F A6WE 1996101700082 19961017 00082 NM 1996 10 17 SWAA961055 1 19961004 A 5320 WEB BOEING 737 7372H4 138448C NM BS 178-188 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 DURING SCHEDULED D-CHECK, FOUND CRACKS IN WEB AT BS 178 TO 188, WL 234, LBL 10. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1996101700711 19961017 00711 NM 1996 10 17 AWXA960546 1 19960913 A 5315 FLOOR BEAM BOEING 757 7572S7 1384962 NM BS 324 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 904AW 23566 PAE - FLT 7803 - DURING ROUTINE SCHEDULED C-4 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM BS 324, RBL 46 - RBL 63. REMOVED AND INSTALLED FABRICATED T-CHORD ON FLOOR BEAM BS 324, ER 5-53-32-07. (M) 2 L 7 2 4F RT A2NM 1996061300363 19960613 00363 WP 1996 6 13 CALA9600777 1 19960522 A 5320 THRESHOLD DOUG DC9 DC982 3022082 WP FWD SERV DOOR PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35832 49492 INSPECTION FOUND HOLES PUNCTURED INTO FORWARD SERVICE DOOR THRESHOLD. A NEW DOOR PAN WAS INSTALLED IAW SRM 53-05-01. 2 L 7 2 4F A6WE 1996110100844 19961101 00844 NM 1996 11 1 PCAA9600308 1 19960912 A 3260 864202 UPLOCK SWITCH DHAV DHC8 DHC8102 2809003 NM NLG FAILED A PCAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 13 821EX 15164 173 FLT 3827 - AFTER GEAR RETRACTION, NOSE GEAR INDICATED UNSAFE AND NOSE GEAR DOORS INDICATED OPEN. CREW PERFORMED ALTERNA TE GEAR EXTENSION AND RETURNED TO SCE WITHOUT INCIDENT. REMOVED AND REPLACED NOSE DRAG STRUT PROXIMITY SWITCH. RETRACT ION AND OPERATIONAL TESTS NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1997042400318 19970424 00318 WP 1997 4 24 97ZZZX1775 1 19961111 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 218 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEDULED INSPECTION AT AERO CORP, FOUND FLOOR SUPPORT AT STA 218 CORRODED ABOVE LONGERON 29L. REMOVED CORROSI ON IAW DC9 SRM 51-10-3. CORROSION REMOVED FROM EDGE OF FLANGE .005 INCH, WITHIN LIMITS IAW DC9 SRM 53-01 FIG 1. ALODIN ED AND PRIMED IAW DC9 SRM 51-10-3 (STA 218 S-296). 2 L 7 2 4F A6WE 1996061300213 19960613 00213 NM 1996 6 13 96ZZZX2931 1 19960327 A 2130 7248272 RELIEF VALVE BOEING 727 727224 1384076 NM CABIN OUT OF POSITION A C1HA O OTHER J W WARNING INDICATION INADEQUATE Q C IN INSP/MAINT 1 WP 23 707CA 20662 CABIN PRESSURE CONTROL INOPERABLE. LEFT AND RIGHT RELIEF VALVES FOUND CLOCKED FROM 180 DEGREES FROM CORRECT AT INSTALLA TION. REPLACED BOTH VALVES. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A3WE 1996050900137 19960509 00137 WP 1996 5 9 9609659982 1 19960426 A 5320 DOOR FRAME DOUG DC9 DC932 3022066 WP PAX DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 982US 45790 DURING LINE CHECK, FOUND A CRACK IN THE AFT PASSENGER DOOR FRAME UPPER RIGHT CORNER. REPAIRED FRAME (P/N 5917579-21) PE R EA 99-102154. 2 L 7 2 4F A6WE 1996040500014 19960405 00014 NM 1996 4 5 96ZZZX1403 1 19960228 A 2612 894232 CONNECTOR BOEING 727 727231 1384079 NM NR 2 ENGINE MOISTURE CONTAM A TWAA E ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 CE 05 64332 20055 MIA - FLT 17 - DURING DESCENT, SHUT DOWN NR 2 ENGINE, SN 3979, DUE TO FIREWARNING. FOUND MOISTURE IN LOOP CONNECTOR, MF G PN 894232. CLEANED CONNECTOR AND INSTALLED NEW GASKET WASHERS. GROUND OPERATION OF WARNING SYSTEM CHECKED NORMAL. E NGINE TT: 58,407 HRS; 38,756 CYCLES, CHECK C-4 - 10-5-95 - MCI. 2 L 7 3 4F A3WE 1997041000111 19970410 00111 EU 1997 4 10 97ZZZX1402 1 19961118 A 7931 50781200G01 OIL TRANSMITTER BAG BAE146 BAE146200A 1500266 EU NR 4 ENGINE FAILED A A6WA O OTHER N FALSE WARNING CR CRUISE 1 GL 31 183US 39599390 E2043 ORD - FLT 545 - NR 4 ENGINE OIL PRESSURE INDICATED IN THE RED ABOVE 82 PERCENT N2. REMOVED AND REPLACED NR 4 ENGINE OIL TRANSMITTER. RAN NR 4 ENGINE, NO LEAKS NOTED. OIL PRESSURE CHECKED OK. 2 H 7 4 4F RT A49EU 1996012600085 19960126 00085 NM 1996 1 26 96FDEA00087 1 19960119 A 5311 FRAME BOEING 727 727233 138408A NM BS 500 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 DENT IN FRAME BS 500 LBL 34 TO 46 WL 160. 2 L 7 3 4F RT A3WE 1996071000525 19960710 00525 WP 1996 7 10 96ZZZM1070 1 19960520 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 718 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 985Z 47491 STL - DURING OP-15, FOUND LONGERON 2R CRACKED, STATION 718. REPAIRED PER SRM 52-02, FIGURE 2. (M) 2 L 7 2 4F A6WE 1996121900030 19961219 00030 WP 1996 12 19 96ZZZX6052 1 19961121 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 917 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 921VV 47284 DURING A SCHEUDLED INSPECTION AT AERO CORP, CORROSION WAS FOUND IN THE AFT CARGO PIT, FRAME STA 917 FROM S29L TO S29R. R EMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW DC9 SRM 53-01 FIG 1 (GAUGE A-0299). RECEIVED DRILLED AND DEBURRED NEW L 29L FS 918 - FS 996, DRILLED AND DEBURRED LONGERON SPLICE IAW DC9 SRM 51-10-4, SRM 53-02 FIG 5. ALODINED AND PRIMED IAW DC9 SRM 51-10-3. INSTALLED IAW DC9 SRM 51-30-2, SRM 53-02 FIG 5. 2 L 7 2 4F A6WE 1996053000479 19960530 00479 WP 1996 5 30 HAL9631 1 19960329 A 3350 P4010049 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 EICBH 4995 47796 HNL - FLT 319 - 'EXIT' LIGHT OUT ON SIDEWALL AT ROW 17 LEFT WALL PANEL. REPLACED BATTERIES. OP CHECK OK. (X) 2 L 7 2 4F A6WE 1996120500052 19961205 00052 NM 1996 12 5 96FDEA01693 1 19961126 A 8011 383152161 STARTER BOEING 727 7272S2F 1384O81 NM NR 3 ENGINE FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 SO 25 212FE 22934 NR 3 ENGINE FIRE WARNING CAME ON AT 2,500 MSL, LIGHT WENT OUT WHEN NR 3 POWER RETARDED. FOUND STARTER TURBINE SHEARED FR OM SHAFT, STARTER DESTROYED. REPLACED NR 3 ENGINE STARTER PER MAINTENANCE MANUAL 80-10-01. REPLACED NR 3 ENGINE START VALVE PER MAINTENANCE MANUAL 80-10-02. RAN ENGINE OPERATIONAL AND LEAK CHECK GOOD. NO DEFECTS NOTED WITH NR 3 ENGINE B LEED AIR DUCTS. 2 L 7 3 4F A3WE 1996122600016 19961226 00016 WP 1996 12 26 96ZZZX6147 1 19961111 A 3244 TIRE 41X15D18R7 DOUG DC9 DC951 3022051 WP NR 3 RT MLG FAILED A A4JA K NONE P NO WARNING INDICATION TO TAKEOFF 1 SO 15 920PJ 213 3147G644 47677 TIRE FAILURE ON TAKEOFF AT HIGH SPEED. INSPECTION OF WHEEL ASSY REVEALED NO DAMAGE TO WHEEL HALVES. RETREAD SEPARATION OCCURRED IN AREA OF (SUSPECTED/UNCONFIRMED) PUNCTURE BLOWOUT. AIRCRAFT LANDED SAFELY AND WITHOUT INCIDENT - DAMAGE NOT ED TO RT I/B FLAP ONLY. PART INSTALLED - 139 CYCLES, 212.6 HOURS (10-09-96). 2 L 7 2 4F RT A6WE 1996032900242 19960329 00242 EA 1996 3 29 96ZZZX1357 1 19960226 A 3250 70263 SERVO VALVE CNDAIR CL601 CL6013A 8070802 EA NLG STEERING SHORTED A G8CA K NONE O OTHER IN INSP/MAINT 1 NE 03 6116S 2096 292 5082 NLG STEERING FAILED. FOUND SERVO VALVE SHORTED TO CASE AND SECONDARY WINDING TO HAVE EXTREMELY HIGH RESISTANCE. 2 L 7 2 4F RT A21EA 1996021600381 19960216 00381 NM 1996 2 16 96UAL900105 1 19960212 A 2530 MS3505822 SWITCH BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE GALLEY HOT PLATE SHORTED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 7293U 21571 GALLEY HOT PLATE NR H41 WAS SMOKING, SPARKING AND GAVE A FLIGHT ATTENDANT A SHOCK. CHECKED WIRING UNDER HOT PLATE ELEME NTS BEHIND CONTROL SWITCH AND NO OVERHEATING EVIDENT. REPLACED SWITCH AND HOTPLATE OPERATION CHECKS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1996022300040 19960223 00040 WP 1996 2 23 9603969943 1 19960217 A 7711 PT2 PROB DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9 52048 NE NR 2 ENGINE SNOW PACKED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 1308T 47315 648951 NR 2 EPR INDICATION ABNORMALLY HIGH ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MA INTENANCE REMOVED PACKED SNOW FROM THE PT2 PROBE AND ENGINE INDICATIONS RETURNED TO NORMAL. 2 L 7 2 4F 4 F A6WE E2EA 1996022300251 19960223 00251 NE 1996 2 23 QXEA9600058 2 19960212 A 7532 3038884 BLEED VALVE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 ENGINE DEFECTIVE A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 09 102AV 091 PCE120662 BOI - FLIGHT ATTENDANT REPORTED SMOKE IN CABIN. NR 1 ENGINE P2.5-3 VALVE REPLACED AND BLEED AIR OPS CHECKED GOOD. AIRC RAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 1996030800555 19960308 00555 SO 1996 3 8 96ZZZX944 2 19960201 A 8530 SPRING CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO VALVE BROKEN A BAJA O OTHER E VIBRATION/BUFFET CL CLIMB 1 AL 01 3246M 75 402C0294 519128 PILOT REPORTED A NOTICEABLE VIBRATION SHORTLY AFTER TAKEOFF AND DURING CLIMB AND INTO CRUISE. AFTER LANDING AT FINAL DE STINATION, MAINTENANCE PERFORMED A CYLINDER COMPRESSION CHECK. ALL CYLINDERS ON BOTH ENGINES SHOWED NO EVIDENCE OF LEAK AGE. AFTER FURTHER GROUND RUN-UPS, IT WAS DETERMINED TO BE THE RIGHT ENGINE. AFTER ALL CYLINDER VALVE COVERS WERE REMO VED, A TOTAL OF 9 OUTER VALVE SPRINGS WERE FOUND BROKEN. ALL VALVE SPRINGS WERE REPLACED, AND THE DEFECTIVE SPRINGS SEN T TO TCM FOR FURTHER INVESTIGATION. 1 L 7 2 3O 3 O A7CE E8CE 1996032900389 19960329 00389 NM 1996 3 29 96UAL900221 1 19960326 A 5330 6572702 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE BS 943 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7263U 21410 AT APPROXIMATELY BODY STATION 943, STRINGER 18AL, A CRACK WAS FOUND IN THE 65-72702 FUSELAGE SKIN PANEL. REPAIRED THE S KIN PANEL PER THE 65C29069-7 REPAIR DRAWING. 2 L 7 3 4F 4 F A3WE E2EA 1996041200022 19960412 00022 NE 1996 4 12 96ZZZX1584 2 19960112 A 7313 3039260 NOZZLE SET DOUG MD900 MD900 3027375 NM PWA PW206 PW206A NE FN2 DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 07 901CF 10 1WK03280 90000012 PCE206080 TROUBLESHOOTING LT ENGINE FOR HUNG START AT 38 PERCENT NG AND ALSO FAILED TO REACH IDLE RPM. REPLACED WITH NEW NOZZLE S ET UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U NC H19NM E42NE 1996050200018 19960502 00018 NM 1996 5 2 96UAL900279 1 19960424 A 3620 11511621 TEMP SENSOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE PNEUMATIC MANIFO FAILED A UALA H DEACTIVATE SYST/CIRCUITS O OTHER CR CRUISE 1 WP 29 775UA 26947 IN FLIGHT RIGHT DUCT PRESSURE VARIES FROM 43 TO 9, PRSOV LOCKED CLOSED. *S/D* THE RIGHT BLEED SYSTEM MANIFOLD DUAL TEM P SENSOR FAILED. THE SENSOR WAS REPLACED AND THE PNEUMATIC SYSTEM WAS TESTED AND PASSED. SYSTEM AND INDICATIONS WERE N ORMAL ON SUBSEQUENT FLIGHT. 2 L 7 2 4F 4 F RT T0001SE E46NE 1996051600019 19960516 00019 EU 1996 5 16 96UAL900323 1 19960507 A 2133 ELECTRONIC BOX NORD MICRO 6331166394 AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE OUT FLOW VALVE FAILED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 427UA 512 HAD A RAPID DECOMPRESSION OF THE AIRCRAFT AT FL370. AUTO PRESSURE SYSTEMS 1 AND 2 FAILED SIMULTANEOUSLY. REGAINED CONT ROL IN MANUAL. *S/D* ELECTRONIC BOX FAILED ON OUTFLOW VALVE. ELECTRONIC BOX WAS REPLACED AND SYSTEM OPERATED NORMALLY . 2 L 7 2 4F 4 F RT A28NM E40NE 1996052300304 19960523 00304 NE 1996 5 23 UPS96220135 2 19960517 A 7200 ENGINE BOEING 727 72725C 138400H NM PWA JT8 JT8D7B 52053 NE NR 2 ENGINE FAILED A IPXA E ENGINE SHUTDOWN Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SO 01 950UP 19718 NR 2 ENGINE FAILED INFLIGHT. REMOVED AND REPLACED NR 2 ENG PER T/C 1202 (P/N JT8D-7B) (S/N 68500). REMOVED MAIN ENGINE OIL STRAINER, FOUND LARGE AMOUNTS OF METAL. 2 L 7 3 4F 4 F A3WE E2EA 1996053000086 19960530 00086 NE 1996 5 30 COMA9630112 2 19960520 A 7510 3031T37P07 TURN BARREL SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LT ENGINE SEPARATED A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 146CA 340A416 367177 WHEN THE LT ENGINE ANTI-ICE IS SELECTED, TORQUE DROPS 11 PERCENT AND ITT INCREASES SIGNIFICANTLY. FOUND LINKAGE BETWEEN IGV ACTUATOR AND THE ANTI-ICE START BLEED VALVE TO BE SEPARATED. INSTALLED SERVICEABLE LINKAGE. 2 L 7 2 4T 4 T RT A52EU E8NE6 1996060600028 19960606 00028 NE 1996 6 6 9611812705 2 19960522 A 7230 COMPRESSOR BOEING 727 727225 1384077 NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE STALLED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 GL 01 802E 22433 696540 EN ROUTE ORD-BOS, THE NR 2 ENGINE EXPERIENCED COMPRESSOR STALLS AND ENGINE PARAMETER FLUCTUATION AT FL 370. A PRECAUTIO NARY SHUT-DOWN OF THE NR 2 ENGINE WAS ACCOMPLISHED. THE FLIGHT WAS DIVERTED TO DTW AND LANDED WITHOUT INCIDENT. MAINTEN ANCE REPLACED THE NR 2 ENGINE WITH A SERVICEABLE UNIT. 2 L 7 3 4F 4 F A3WE E2EA 1996061300352 19960613 00352 NM 1996 6 13 96UAL900427 1 19960610 A 3231 69295273 DOOR ROD BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NLG CRACKED A UALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 29 7459U 21913 NOSE GEAR DOOR VIBRATION AFTER LIFT OFF. RETURNED TO BOSTON. SUPPLEMENTAL DATA UPDATE: FOUND RIGHT HAND NOSE LANDING GEAR DOOR OPERATOR ROD CRACKED. REPLACED ROD. 2 L 7 3 4F 4 F A3WE E2EA 1996062000368 19960620 00368 WP 1996 6 20 96UAL900458 1 19960617 A 5330 SKIN DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL BS 979 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 1834U 47966 ON WALK-AROUND, FOUND FUSELAGE SKIN AT BODY STATION 979 HAD EXTENSIVE CORROSION BETWEEN LONGERONS 44L AND 47L. DAMAGE E XCEEDED SRM ALLOWABLES FOR MATERIAL LOSS. CLEANUP OF CORROSION RESULTED IN A 32.0 INCH BY 8.0 INCH SECTION OF SKIN BEIN G REMOVED. THE CORROSION WAS CENTERED ALONG THE CIRCUMFERENTIAL AT BS 979. NO DAMAGE TO FRAME OR THE STRINGERS. A CLA SS 3 DOUBLER-TRIPLER REPAIR WAS INSTALLED PER DC-10-10 SRM 53-20-00, FIGURE 6. 2 L 7 3 4F 4 F A22WE E23EA 1996062700410 19960627 00410 GL 1996 6 27 HEEA967297 2 19960531 A 7323 25490682 GOVERNOR BELL 230 230 1182149 SW ALLSN 250C 250C30G2 03013 GL ENGINE MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 1262 23009 ERRATIC POWER SETTINGS (GOVERNOR WOULD NOT STAY WITHIN UPPER LIMITS) 1 G 7 2 3U 3 U NC H9SW E1GL 1996071000291 19960710 00291 GL 1996 7 10 96ZZZX3414 2 19960515 A 7210 23030917 BEARING 23035179 SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL PINION WORN A L ALGA O OTHER J WARNING INDICATION CR CRUISE 1 SW 03 710AL CAG90832 760279 890824 THE ENGINE CHIP DETECTOR LIGHT ILLUMINATED IN-FLIGHT. THE TEAR-DOWN INSPECTION OF THE ENGINE REVEALED THE NR 3 AND NR 4 PINION BEARINGS ROLLER CAGES WERE EXCESSIVELY WORN. THESE BEARINGS ONLY HAVE 489.1 OPERATING HOURS SINCE NEW. THE OPE RATOR BELIEVES THE 'NEW STYLE' BEARINGS ARE MADE OF A SOFTER MATERIAL. 1 G 7 2 3U 3 U H1NE E1GL 1996080200252 19960802 00252 WP 1996 8 2 96ZZZM1172 2 19960611 A 7260 31035992 IDLER GEAR FRCHLD SA227 SA227DC 3377521 SW GARRTT TPE331 TPE33112UHR WP RT ENGINE FAILED A EQGA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 19 850LS DC850B P70185 AFTER TAKEOFF FROM WDG, THE CREW GOT A CHIP LIGHT ON THE RIGHT ENGINE. THE CAPTAIN DECIDED TO RETURN TO WDG AND MAKE A PRECAUTIONARY SHUTDOWN OF THE RIGHT ENGINE. DURING THE PRE-SHUTDOWN CHECKS, THE ENGINE FLAMED OUT. THE CREW THEN MADE A LANDING AT WDG WITH NO FURTHER INCIDENT. ON INSPECTION, IT WAS FOUND THAT ACCESSORY DRIVE GEAR ASSEMBLY, P/N 310601-6 , S/N 3P17909, HAD FAILED AND THE IDLER GEAR ASSEMBLY, P/N 3101599-2, S/N 3P17792, HAD ALSO FAILED. BOTH ASSEMBLIES WER E REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A18SW E4WE 1996082200673 19960822 00673 NM 1996 8 22 96UAL900607 1 19960808 A 5730 65B145965 PANEL BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE LT WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 186UA 19987 26875 ON ARRIVAL TO NRT, THE LEFT WING LEADING EDGE FIBERGLASS PANEL WAS FOUND CRACKED IN TWO PLACES. THE PANEL WAS LOCATED I NBOARD OF THE NR 2 ENGINE. CRACK LENGTHS WERE MEASURED TO 18 INCHES AND 5 INCHES. INVESTIGATION FOUND THAT ONLY THE UP PER SKIN WAS AFFECTED. THE HONEYCOMB STRUCTURE WAS NOT AFFECTED. ACCOMPLISHED PERMANENT SKIN REPAIR FOR METAL TO METAL ADHESIVE BONDED ALUMINUM HONEYCOMB PANEL USING VACUUM BAG/HEAT BLANKET PROCESS. PART TOTAL CYCLES, 2,432. 2 L 7 4 4F 4 F RT A20WE E24NE 1996091200351 19960912 00351 NE 1996 9 12 AWXA960375 2 19960909 A 7250 834401 TURBINE BLADE BOEING 737 7372M8 1384483 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE FAILED A AWXA A E UNSCHED LANDING ENGINE SHUTDOWN E Y VIBRATION/BUFFET ENGINE STOPPAGE CL CLIMB 1 WP 28 141AW 5126 21955 LAS - FLT 2976 - AIR TURN BACK, AT CLIMB POWER FL 200 NR 1 ENGINE COMMENCED SEVERE VIBRATIONS. ALL ENGINE INDICATIONS N ORMAL. RETARDED THRUST LEVER. VIBRATIONS CONTINUED. SHUTDOWN ENGINE IAW QRH. RETURNED LAS. FOUND TURBINE WHEEL BLAD ES MISSING MATERIAL. REMOVED AND REPLACED NR 1 ENGINE. TEARDOWN FOUND NR 1 HIGH PRESSURE TURBINE BLADE FAILED DUE TO A N INTERNAL CASTING DEFECT KNOWN AS A COLD SHUT. (M) 2 L 7 2 4F 4 F A16WE E2EA 1996092600681 19960926 00681 WP 1996 9 26 0902496462 2 19960902 A 7200 ENGINE BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110U 01514 WP RIGHT FAILED A CX7A A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 GL 03 462CE 684 P63074 MBS/MDW - FLT 201 - RIGHT ENGINE LOST POWER AND PILOT SHUT DOWN ENGINE. UNEVENTFUL LANDING AT SBN. INSPECTION FOUND ME TAL IN GEARBOX. ENGINE WILL BE REMOVED AND SENT FOR REPAIR. ACTT: 16,239.6 HOURS. ENGINE TT: 12,686.4. ENGINE TSO: 3,781.7 HOURS. 2 L 7 2 4T 4 T RT A21EU E4WE 1996101000897 19961010 00897 CE 1996 10 10 CA960212019 1 19960130 A 3260 A1S411651 LIGHT BULB BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE NLG DOWN BURNT OUT W L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 CA 1672 PCE114296 (CAN)PILOT COULD NOT GET A NOSE GEAR DOWN INDICATION ON SELECTION. COMPLETED A TOWER FLYBY WHERE GEAR DOWN WAS CONFIRMED . INVESTIGATION CONFIRMED THAT THE BULBS WERE BURNT OUT. 2 L 7 2 4T 4 T RT A24CE E26NE 1996101000921 19961010 00921 1996 10 10 CA960214015 1 19960130 A 7921 1501752024 OIL FITTING 1501752024 LYC O360 AEIO360A1B6 41514 EA COOLER LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 167 L2663251A (CAN)PILOT NOTICED OIL LEAKING FROM ENGINE DURING WALKAROUND. INVESTIGATION FOUND THE OIL WAS COMING FROM THE THREADS OF THE OIL COOLER FITTINGS. THE SEALANT AROUND THE THREADS WAS FOUND TO BE MISSING. NEWSEALANT WAS APPLIED AND THE AIRCRAF T RETURNED TO SERVICE. 3 O 1E10 1996110100036 19961101 00036 NM 1996 11 1 CA960311029 1 19960129 A 2916 0147 DIAPHRAGM PARKERHANFIN 3810041104 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE #2 SYSTEM HYD FAULTY W K NONE O OTHER CL CLIMB 1 CA 0147 120543 (CAN)SHORTLY AFTER TAKEOFF #2 HYDRAULIC SYSTEM PRESSURE PROBLEMS NOTED. INVESTIGATION FOUND A FAULTY HYDRAULIC PRESURE RESERVOIR DIAPHRAGM WHICH IS DESIGNED TO PRESSUREIZE THE FEED LINE TO THE HYDRAULIC PU MP. HYDRAULIC TANK REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1996110100902 19961101 00902 WP 1996 11 1 RAIA961007 2 19961005 A 7510 8961151 BLEED GASKET BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT ENGINE LEAKS A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 875JX 875 P66140 FAT - FLT 4734 - LEFT ENGINE BYPASSED AT 60 PERCENT TORQUE, EGT SPIKED SEVERAL TIMES DURING REDUCTION. MAINTENANCE REPL ACED THE LEFT ENGINE ANTI-ICE VALVE BLEED AIR GASKETS. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1996110700761 19961107 00761 NM 1996 11 7 96UAL900853 1 19961102 A 3350 LIGHT BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 164UA 21657 EMERGENCY EXIT LIGHT STRIP AT SEAT 34 H, J, K INOP. REPLACED EEL POWER FEEDER AND EEL LAMP SEGMENTS. 2 L 7 4 4F 4 F A20WE E20EA 1996111400402 19961114 00402 WP 1996 11 14 SWHA96003 2 19960603 A 7230 31070511 COMPRESSOR SEAL SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP NR 2 ENGINE COKED A A SWHA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 17 718C 2846 AC572 P44193C PILOT REPORTED ON SCHEDULED FLIGHT 432, FROM CRP TO AUS, APPROXIMATELY 20 MINUTES PRIOR TO LANDING 'EXHAUST FUMES IN CAB IN AND COCKPIT, COMPLAINTS FROM CREW AND PAX'. INVESTIGATION REVEALED THE NR 2 ENGINE COMPRESSOR SEAL TO BE LEAKING. T HE COMPRESSOR SEAL WAS REMOVED AND REPLACED. OPERATIONAL CHECKS WERE SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVIC E. (M) 2 L 7 2 4T 4 T RT A8SW E4WE 1996121200303 19961212 00303 NM 1996 12 12 CA960703018 1 19960619 A 7810 VC1165 CLAMP DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE #2 EXHAUST LOOSE W E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. J WARNING INDICATION TX TAXI/GRND HDL 1 CA 123045 (CAN) #2 ENGINE INDICATED FIRE DETECTION ON TAXI-OUT. ENGINE SHUTDOWN AND FIRE BOTTLE USED. INVESTIGATION REVEALED EXHAU ST PIPE HAD SEPARATED OFF REAR ENGINE AT POWER TURBINE. THE 'V' CLAMP HAD BECOME LOOSE. 2 H 7 2 4T 4 T RT A13NM E20NE 1996121900422 19961219 00422 GL 1996 12 19 HEEA968709 2 19961213 A 7321 252473834 FUEL CONTROL BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL RETAIN PLATE LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 50046 14244 45173 CAE860036 FUEL CONTROL REMOVED DUE TO LEAKING AROUND RETAINING PLATE AREA. NO PROBLEM WITH RFSE 250-93-3 MEDLIN BEARINGS. REPLACE D WITH AN OVERHAULED FUEL CONTROL. 1 G 7 1 3U 3 U H2SW E1GL 1996121900909 19961219 00909 NE 1996 12 19 COMA9610398 3 19961216 A 6111 8173861 BEARING RFC11AA16A EMB 120 EMB120RT SO PWA 118 PW118 NE HAMSTD 14RF 14RF19 NE PROP BLADE WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 1968 1968 886348 120264 115571 910337 PROPELLER ASSEMBLY WAS REMOVED FOR EXCESSIVE VIBRATION. DURING DISASSEMBLY AND INSPECTION, IT WAS DETERMINED THAT THE V IBRATION WAS DUE TO THE UNEVEN WEAR OF THE BEARING INSERT. INSERT HAD DETERIORATED FROM .100\ TO .0875\ AT THE THINEST WALL TO .0995\ AT THE THICKEST WALL WEARING IN AN OVAL FASHION. BLADE AND BEARING WERE REMOVED FROM SERVICE AND REPLACE D WITH SERVICABLE UNITS. 2 L 7 2 4T 4 T RT A31SO E20NE 6 C P11NE 1997010200197 19970102 00197 1997 1 2 CA960723535 4 19960603 A 2312 064100504 TRANSMITTERS DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE #1 & #2 VHF INOPERATIVE W O OTHER G MULTIPLE FAILURE CR CRUISE 1 CA P657447D (CAN) DURING FLIGHT COMPLETE VHF COMMUNICATION FAILURE OCCURRED. MAINTENANCE ACTION INVOLVED CHANGING #1 AND #2 VHF TRAN SMITTERS AND #1 & #2 AUDIO SELECTOR PANELS. 2 L 7 2 4F 4 F A6WE E2EA 1997010200250 19970102 00250 NM 1997 1 2 CA960801006 1 19960725 A 2910 61142 FLOW LIMITER WATERMAN 61142 BOEING 737 737210C 1384459 NM PWA JT8 JT8D9A 52048 NE FLAP FAILED W O OTHER K FLUID LOSS AP APPROACH 1 CA 53671 53671 P678085 (CAN) ON APPROACH A SYSTEM HYDRAULIC PRESSURE DECREASED TO ZERO. LANDING CARRIED OUT USING B SYSTEM. FLAP FLOW LIMITER H AD FAILED, REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1997010200315 19970102 00315 EA 1997 1 2 CA961003003 2 19960909 A 7200 ENGINE BEECH 100 100BEECH 1152916 CE PWA PT6 PT6A28 EA #1 POSITION MAKING METAL W A UNSCHED LANDING O OTHER CL CLIMB 1 CA P50739 (CAN) ON CLIMB OUT GOING THROUGH 7,000 FEET, CO-PILOT NOTICED A SLIGHT RISE IN ITT AND A SLIGHT DROP IN TORQUE AND OIL P RESSURE ON THE #1 ENGINE. POWER WAS REDUCED AND THE AIRCRAFT RETURNED TO ITS POINT OF DEPARTURE, WITH OIL PRESSURE MAINT AINED AT 52 PSI. MAIN OIL SCREEN INSPECTED - SLIGHT TRACES OF METAL. NOSE GEAR CASE SCREEN INSPECTED - EXCESSIVE AMOUNT OF METAL ON THE CHIP DETECTOR. ENGINE REMOVED FOR INSPECTION AND REPAIR. 1 L 7 2 3T 4 T A14CE E4EA 1997010900283 19970109 00283 NM 1997 1 9 VNAA9612007 1 19961227 A 2750 1050A000003 FLAP CONTROL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT FAILED A A VNAA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 GL 07 438JS 3056 WHILE AT CRUISE FLIGHT, A FLAP ASSYM CAS MESSAGE AND A FLAP FAIL CASS MESSAGE WERE INDICATED. CONSULTED QRH AND VISUALL Y ENSURED THAT FLAPS WERE AT ZERO DEGREES, CONTINUED ON TO DAYTON AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMO VED AND REPLACED THE FLAP CONTROL UNIT, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1997011400017 19970114 00017 NE 1997 1 14 P5CA9601163 2 19961214 A 7530 733456 BLEED CONTROL BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE NR 1 ENGINE LEAKING A P5CA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 WP 23 920FT 22237 702091 AT FL 370 -33 TAT -61 SAT NR 1, ENGINE EPR 1.36, .85 N1, .845 N2 UNABLE TO OBTAIN CRUISE POWER. REMOVED AND REPLACED 3. 5 BLEED CONTROL AND LINE FROM BLEED CONTROL TO CONNECTOR BLOCK. REPLACED SEAL AT FUEL LINE AT FUEL CONTROL UNIT TO 3.5 BLEED CONTROL. LEAK AND OPERATIONAL CHECK OK PER MAINTENANCE MANUAL 75-32-12 AND 75-32-18. 2 L 7 4 4F 4 F A20WE E3NE 1997011600136 19970116 00136 CE 1997 1 16 CA960321001 1 19960307 A 2435 SPEED MONOPOLE CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE STARTER/GEN OPEN CIRCUIT W H O DEACTIVATE SYST/CIRCUITS OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 CA 6 PCE71333 (CAN) AFTER INSTALLATION OF AN OVERHAULED STARTER/GENERATOR, INITIAL GROUND RUN OPERATION SEEMED SATISFACTORY, HOWERVER SUBSEQUENT FLIGHTS REVEALED THAT THE STARTER WOULD NOT DISENGAGE AUTOMATICALLY. THE START SEQUENCE WAS MANUALLY DISENGAG ED AND THE FLIGHT CONTINUED AS NORMAL. UPON RETURN TO HOME BASE, AN OPEN CIRCUIT WAS FOUND IN THE SPEED SENSOR MONOPOLE. AS THIS SENSOR SENDS A SIGNAL TO THE GCU TO AUTOMATICALLY DISENGAGE THE STARTER BETWEEN 38 PERCENT - 42 PERCENT, ITS OP ERATION IS IMPORTANT. STARTER GENERATOR REPLACED. 1 L 7 2 4F 4 F A22CE E1NE 1997011600322 19970116 00322 WP 1997 1 16 96UAL900994 1 19961230 A 3240 60001771 PARK BRAKE VLV DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL LT MLG WW FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 1846U 48262 ANTI-SKID SYSTEM WILL NOT ARM. RECYCLED CIRCUIT BREAKER, NO HELP. *S/D* FOUND THE PARKING BRAKE MOTOR VALVE MI-96 WOR KING INTERMITTENTLY. REPLACED VALVE. ALSO, FOUND NR 6 WHEEL TRANSDUCER INTERMITTENTLY FAILING ON CONTROL BOX TEST. WI RES WERE BROKEN AT CONNECTOR ON THE TRANSDUCER. REPAIRED WIRES. 2 L 7 3 4F 4 F A22WE E23EA 1997011600676 19970116 00676 WP 1997 1 16 WTAA960212 2 19961207 A 7200 ENGINE BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110U 01514 WP LEFT BIRD STRIKE A WTAA K NONE C F.O.D. NR NOT REPORTED 1 WP 17 420UE 788 LAX - BIRD STRIKE LEFT SIDE OF AIRCRAFT INGESTED INTO LEFT ENGINE. MAINTENANCE INSPECTED AIRCRAFT FOR DAMAGE. NO DAMAG E NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A21EU E4WE 1997013000462 19970130 00462 EU 1997 1 30 CA960827013 1 19960821 A 2550 127391 COUPLING BREEZE 140276 BOLKMS 105 BO105C 5626005 EU ALLSN 250C 250C20B 03013 GL MANUAL REL CABLE BROKEN W O OTHER O OTHER EX EXTERNAL LOAD 1 CA 3162 CAE835698 (CAN) AFTER TAKEOFF, WHEN SLING LOAD 10 FEET ABOVE GROUND, CARGO HOOK SELF RELEASED THE LOAD. COUPLING ON THE MANUAL REL EASE CABLE FOUND BROKEN. SUSPECT THAT CABLE RELEASE GETS DAMAGED BY FLYING DEBRIS WHILE LANDING WITH CARGO HOOK LOWERED FOR OPERATION. 1 G 7 2 3U 3 U H3EU E4CE 1997030600658 19970306 00658 GL 1997 3 6 CA960502020 2 19960304 A 7240 6896805 LINER ALLSN BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL DOME OF LINER DISTORTED W K NONE O OTHER IN INSP/MAINT 1 CA CAE822647 (CAN) DURING INSPECTION, FOUND DOME OF COMBUSTION LINER TO BE DISTORTED. COMBUSTION LINER REPLACED AND AIRCRAFT RETURNED TO SERVICE. 1 G 7 1 3U 3 U H2SW E4CE 1997030600672 19970306 00672 CE 1997 3 6 CA960826031 1 19960808 A 2824 710C4 DRAIN VALVE BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA FUEL BOWL LEAKING W A E UNSCHED LANDING ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 CA PCE80030 (CAN) THE PILOT REPORTED A FUEL IMBALANCE. MAINTENANCE FOUND THE FUEL SCREEN BOWL VALVE HAD FAILED. 1 L 7 2 4T 4 T A24CE E4EA 1997030600676 19970306 00676 1997 3 6 CA960826078 4 19960801 A 2562 006062 BATTERY BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA ELT CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 282 PCE32553 (CAN) DURING A 50 HOUR INSPECTION/TEST THE ELT FAILED TO FUNCTION. THE CASE WAS OPENED AND THE BATTERY WAS FOUND TO HAVE LEAKED AND CORRODED THE CIRCUIT BOARD. 2 L 7 2 4T 4 T RT A24CE E4EA 1997031300253 19970313 00253 WP 1997 3 13 CA961001012 1 19960913 A 2530 COFFEE MAKER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE GALLEY ELECT SHORT W K NONE O B OTHER SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA P656991D (CAN) CREW REPORTED BURNING SMELL COMING FROM COFFEE MAKER. COFFEE MAKER REPLACED. 2 L 7 2 4F 4 F A6WE E2EA 1997050100364 19970501 00364 NM 1997 5 1 CA970109028 1 19961211 A 2530 3412131 COMPRESSOR BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE GALLEY FAILED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA P707550 (CAN) SMOKE REPORTED IN REAR GALLEY. GALLEY POWER UTILITY BUS LH AND RH SWITCHED OFF. UNIT COOLED AND SMOKE DISSIPATED. HOT SPOT BEHIND GALLEY POSITION 104. WHEN LH UTILITY BUS ON, HOT SPOT RE-OCCURRED. LH UTILITY BUS SWITCHED OFF, GALLEY P OWER OFF, RH UTILITY ON ALL SYSTEMS NORMAL. COMPRESSOR REPLACED. 2 L 7 2 4F 4 F RT A1NM E3NE 1997061200815 19970612 00815 NE 1997 6 12 97ZZZX2742 2 19960719 A 7250 410106802 SPRING BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE SEAL RING WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 528SF 858 7104 LE45242E SEAL RING EXPANDER SPRING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1997061900503 19970619 00503 NM 1997 6 19 CA970130002 1 19961128 A 7930 42D107A1 SWITCH CUSTOMCOMP BOEING 727 727225 1384077 NM PWA JT8 JT8D7B 52053 NE OIL VENT LINE OPEN PORT W E ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 CA 13292XX 655259 (CAN) 30 MINUTES AFTER TAKEOFF #1 OIL QUANTITY STARTED A GRADUAL DECREASE. POWER REDUCED ON REACHING 2 GALLONS. ENGINE S HUT DOWN AT ZERO QUANTITY, PRESSURE AND TEMPERATURE NORMAL. ON PREVIOUS LEG OIL PRESSURE WENT TO ZERO JUST BEFORE TOUCHD OWN. ALL OTHER INDICATIONS WERE NORMAL. SUSPECT INSTRUMENT FAILURE, OIL ADDED. FOUND VENT LINE MISSING AND VENT PORT NOT CAPPED. REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 1996051600037 19960516 00037 SO 1996 5 16 96ZZZX2336 1 19960308 A 5730 8005271 SKIN LKHEED 188 188C 5262604 SO WS 106 CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 285F 62485 188A1107 YIP - DURING SCHEDULED CHECK, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION IAW AD 66-04-02 AND LOCKHEED SB 62 0 REVEALED THE FOLLOWING WING PANEL CRACKS. REFERENCE OPERATOR CONTROL NR ZIAA96009, 96ZZZX2335, NR 96ZZZX2337, AND NR 96ZZZX2338. 2 L 7 4 4T 4A22 1997060500257 19970605 00257 NM 1997 6 5 97ZZZX2439 1 19961216 A 7720 311671201 THERMOCOUPLE DOUG MD900 MD900 3027375 NM ENGINE TEMP WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 628 EM60787002 90000012 THERMOCOUPLE WORN BEYOND SERVICEABLE LIMITS AND REMOVED IN COMPLIANCE TO SB 28096. REPLACED WITH NEW UNIT, CORRECTED PR OBLEM. 1 G 7 2 3U NC H19NM 1996032200972 19960322 00972 NM 1996 3 22 96FDEA00655 1 19960318 A 5330 SKIN BOEING 727 72725C 138400H NM BS 1080-1183 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 119FE 19301 SKIN LAP UPPER PANEL, 65-18386-107, CORRODED, AND TRIMMED AWAY FUSE SKIN BETWEEN STR 21-22L FROM THE PRODUCTION SPLICE A T BS 1080.45 TO THE PRODUCTION SPLICE AT BS 1183 CORRODED. CUT DAMAGED SKIN FROM BS 1080.45 TO BS 1183 AND SPLICED NEW SKIN PER EA 7-5330-28007, DATED 3-14-96. 2 L 7 3 4F A3WE 1997020600838 19970206 00838 NM 1997 2 6 AALA961594 1 19961103 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 324AA 22325 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 24B INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CO NNECTOR AT PAX SEAT 24B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1997012300459 19970123 00459 EU 1997 1 23 RAIA961227 1 19961220 A 5311 S53672400000 FRAME AEROSP ATR42 ATR42300 8680920 EU AFT FUS CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 424TE 18174 124 STL - FOUND CORROSION ON FRAME 38 SKIN CLIPS FROM STRINGER 16L TO 16R. MAINTENANCE REPLACED FRAME 38 LOWER IAW ATR 42 S RM 53-00-00. (M) 2 H 7 2 4T RT A53EU 1996041200440 19960412 00440 WP 1996 4 12 96ZZZX1688 1 19960312 A 3310 BA170 BALLAST DOUG DC8 DC8F54 3021926 WP PEDESTAL SHORTED A FXLA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 19 54FA 45637 ON CLIMB-OUT MIAMI, EXPERIENCED BURNING ELECTRICAL ODOR WITH SMOKE COMING FROM FIRST OFFICER'S FLOOR PANEL. RETURNED TO MIAMI AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED LIGHT BALLAST TRANSFORMER SHORTED IN PEDESTAL. REPLACED BALLAS T AND RETURNED AIRCRAFT TO SERVICE. 2 L 7 4 4F 4A25 1996101700254 19961017 00254 EU 1996 10 17 96ZZZX5169 1 19960827 A 3260 WARNING HORN BAG JETSTM JETSTM3201 1500217 EU LANDING GEAR SOUNDED A VTZA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 EA 27 492UE 790 ALB/IAD - FLT 6255 - DURING APPROACH FLIGHT AT 1120 HOURS ON 8-27-96, ABORTED APPROACH DUE TO LANDING GEAR WARNING HOR N SOUNDED WITH GEAR DOWN AND FLAPS SELECTED TO 20 DEGREES. MAINTENANCE TROUBLESHOT AND INSPECTED LANDING GEAR WITH NO F AULTS FOUND. REMOVED AND REPLACED THE ACTUATOR, LOCK VALVE, EMERGENCY RELIEF VALVE, SELECTOR VALVE, WARNING HORN, AND U NLOCK LIGHT. ALL SYSTEMS FUNCTIONED PROPERLY IAW MM. MAINTENANCE THEN RELEASED THE AIRCRAFT FOR SERVICE. REF: OPERAT OR CONTROL NRS VTZA96343, 96ZZZX5166, 96ZZZX5167, 96ZZZX5168, AND 96ZZZX5170. 2 L 7 2 4T RT A56EU 1996062700334 19960627 00334 1996 6 27 96ZZZX3148 4 19960309 A 3160 900A3720002105 DISPLAY DOUG MD900 MD900 3027375 NM INST PANEL INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 106 008251005 90000012 INSTRUMENT DISPLAY PRIMARY SIDE OF UNIT IS INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1996030800093 19960308 00093 EU 1996 3 8 QXEA9600091 1 19960229 A 3397 WIRE FOKKER F28 F28MK1000 4990808 EU CABIN BROKEN A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 468US 11095 SMF - EMERGENCY LIGHTS AT ROW 11 ARE INOPERATIVE. BROKEN WIRE WAS REPAIRED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURN ED TO SERVICE. 2 L 7 2 4F RT A20EU 1996091200154 19960912 00154 WP 1996 9 12 96ZZZX4356 1 19960724 A 5320 FRAME LKHEED 1011 10113851 5265010 WP CARGO DOOR CORRODED A RIAA K NONE O OTHER IN INSP/MAINT 1 SO 19 312GB 193P1100 LEVEL 2 CORROSION, C2 CARGO DOOR FRAME CORRODED ON LOWER FLANGE AT FS 1545, STR 26. REMOVED DAMAGED AREA, FABRICATED AN D INSTALLED REPAIR PER SRM 51-50-02. (X) 2 L 7 3 4F A23WE 1996062700138 19960627 00138 WP 1996 6 27 9613599958 1 19960612 A 5320 FITTING DOUG DC9 DC931 3022065 WP FS 993 CORROSION A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 917RW 47145 DURING LINE CHECK, FOUND CORROSION ON THE LONGERON 22L END FITTING AT FS 993. REPLACED FITTING. 2 L 7 2 4F A6WE 1996011200540 19960112 00540 SW 1996 1 12 COMA9620002 1 19960109 A 7712 TQ SIG COND SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP RT ENGINE FAILED A COMA K NONE N FALSE WARNING TO TAKEOFF 1 SO 01 704C 1937 AC704 44588 RIGHT ENGINE DID NOT ACHIEVE CHARTED TAKEOFF POWER. SWAPPED TORQUE SIGNAL CONDITIONER TO SPARE BRIDGE. ENGINE PERFORMA NCE SATISFACTORY. 1 L 7 2 4T 4 T A8SW E4WE 1996012600542 19960126 00542 NM 1996 1 26 P5CA9600066 1 19960124 A 7110 BRACKET BOEING 747 747124 1384874 NM PWA JT9 JT9D7A 52054 NE NR 2 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 663042 FOUND SKIN SEPARATION WITH SMALL CRACK IN ENGINE FAN COWL TOP BRACKED AFT MOUNT FITTING GROOVE ON NR 2 ENGINE. INSTALLE D NEW SKIN IAW SRM 51-30-02. 2 L 7 4 4F 4 F A20WE E20EA 1996020200126 19960202 00126 NM 1996 2 2 96UAL900066 1 19960126 A 5210 65331601 SEAL BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE PAX DOOR LEAKING A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 9023U 19061 CREW REPORTS, UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF. MAINTENANCE FOUND AIR LEAKING FROM FORWARD AIRSTAIRS DOOR SE AL. STOPPED LEAK BY PUTTING ALUMINUM FILLED EPOXY RESIN UNDERNEATH AIRSTAIRS DOOR SEAL. AIRCRAFT PRESSURIZES NORMALLY. 2 L 7 2 4F 4 F A16WE E2EA 1996022300073 19960223 00073 NM 1996 2 23 96UAL900118 1 19960215 A 3350 LIGHT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE DOOR 1L INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7294U 21572 EEL DOOR FRAME LIGHT INOPERATIVE DOOR 1 LEFT. REPLACED FEEDER. 2 L 7 3 4F 4 F A3WE E2EA 1996031500500 19960315 00500 NE 1996 3 15 C2XA96IA058 2 19960218 A 7261 AS3209157 O-RING AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE NR 2 ENG GB CUT A C2XA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 09 14828 179 120982 IAH - FLT NR 2786 - DURING TAKEOFF, THE PILOT REPORTED THAT THE NR 2 ENGINE OIL PRESSURE STARTED TO FLUCTUATE. THE CREW SHUTDOWN THE ENGINE AND RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE NR 2 ENGINE AND FOUN D A CUT O-RING UNDER THE RGB COVER PLATE FOR AN MEL'D PROPELLER BRAKE SYSTEM, (REF CONTINENTAL EXPRESS SDR CONTROL NR C2 XA96IA057). MAINTENANCE REMOVED AND REPLACED THE O-RING AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1996040500234 19960405 00234 NE 1996 4 5 9607269871 2 19960329 A 7230 COMPRESSOR DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE NR 1 ENGINE STALLED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 01 780NC 48102 688759 NR 1 ENGINE COMPRESSOR STALLED ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTEN ANCE REPLACED THE FUEL CONTROL ASSEMBLY AND THE PRBC. SUBSEQUENT RUNUP WAS SATISFACTORY. 2 L 7 2 4F 4 F A6WE E2EA 1996050200513 19960502 00513 EA 1996 5 2 GLBA96059 2 19960322 A 7200 ENGINE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA RIGHT FAILED A GLBA E ENGINE SHUTDOWN B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 CE 01 60UE 15143 UC60 MSP - CREW REPORTED THE RIGHT LOW OIL PRESSURE ANNUNCIATOR ILLUMINATED AND THERE WAS A SMELL OF SMOKE IN COCKPIT. THEY PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN AND MADE UNEVENTFUL LANDING. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE WI TH SERVICEABLE. RUN AND LEAK CHECKS WERE GOOD. (M) 2 L 7 2 4T 4 T RT A24CE E4EA 1996053000083 19960530 00083 NE 1996 5 30 ABXA9600496 2 19960522 A 7200 ENGINE DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3B 52039 NE NR 3 MALFUNCTIONED A ABXA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 23 801AX 46077 P669292 NR 3 ENGINE OIL PRESSURE LIGHT ILLUMINATED DURING CRUISE. THE OIL TEMPERATURE INDICATED 125 DEGREES CELSIUS AND BEGAN T O INCREASE WHILE THE OIL PRESSURE AND OIL QUANTITY INDICATIONS WERE NORMAL. SHUTDOWN THE NR 3 ENGINE AT 0203Z AND THE E NGINE WINDMILLED AT 26 PERCENT N1 AND 40 PERCENT N2 WHILE MAINTAINING AN OIL PRESSURE OF 24 PSI. REPLACED THE NR 3 ENGI NE IAW ABX WORK CARD J7002. 2 L 7 4 4F 4 F 4A25 1E8 1996060600343 19960606 00343 NE 1996 6 6 EIAA9611650 2 19960509 A 7230 COMPRESSOR BOEING 747 747212B 1384886 NM PWA JT9 JT9D7J 52054 NE NR 1 ENGINE DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 662971 JFK - WHILE TROUBLESHOOTING NR 1 ENGINE THROTTLE BINDING, FOUND APPROXIMATELY 1 INCH BY 6 INCH PIECE ROLLED BACK ON THE STAGE 7 COMPRESSOR CASE JUST ABOVE THE FUEL OIL COOLER ATTACH FLANGE. REMOVED AND REPLACD ENGINE NR 1. FURTHER INVESTI GATIN IS UNDERWAY. REF: CONTROL NR 96-14. (X) 2 L 7 4 4F 4 F A20WE E20EA 1996071800403 19960718 00403 WP 1996 7 18 CALA9601015 1 19960713 A 3610 DUCT DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE NR 1 ENGINE BLOWN A CALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 16892 49391 716747 THE NR 1 ENGINE FIRE WARNING LIGHT AND BELL ACTIVATED AFTER TAKEOFF. THE BELL WAS SILENCED AND WHEN THE NR 1 ENGINE THR OTTLE WAS RETARDED, THE LIGHT EXTINGUISHED. WHEN THE THROTTLE WAS ADVANCED SLIGHTLY BOTH LOOP LIGHTS CAME ON WITH FIRE WARNING. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE 13TH STAGE DUCT TO C OWL ANTI-ICE VALVE BLOWN. THE NR 1 ENGINE UPPER COWL WAS BURNT DUE TO THE BLOWN DUCT. THE 13TH STAGE DUCT WAS REMOVED AND REPLACED. THE NR 1 ENGINE UPPER COWL WAS ALSO REPLACED. 2 L 7 2 4F 4 F A6WE E9NE 1996071800754 19960718 00754 WP 1996 7 18 96UAL900511 1 19960708 A 3350 EMSE229 POWER SUPPLY DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1843U 46636 EMERGENCY LIGHTING BATTERY WILL NOT TEST. *S/D* REPLACED AFT EMERGENCY POWER SUPPLY AND BATTERY. 2 L 7 3 4F 4 F A22WE E23EA 1996080800075 19960808 00075 NE 1996 8 8 96ZZZX3824 2 19960703 A 7200 ENGINE CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE RT ENGINE FAILED A DJFA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 EA 23 511WC 8350 1069 5500234 PCE70528 AIRCRAFT EXPERIENCED AN AIRFRAME RUMBLE FOLLOWED BY A FAN SPEED INDICATION GOING DOWN FOLLOWED BY ANOTHER RUMBLE. RIGHT ENGINE SHUT DOWN AND AN UNEVENTFUL LANDING MADE. MAINTENANCE REPORTED FAN VERY DIFFICULT TO TURN BY HAND. ENGINE REMO VED FOR TEAR DOWN INSPECTION. ADDITIONAL INFORMATION WILL BE FILED UPON TEAR DOWN. 1 L 7 2 4F 4 F A22CE E1NE 1996080800830 19960808 00830 NM 1996 8 8 96UAL900590 1 19960801 A 3350 60252 STRIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 388UA 24663 EMERGENCY ESCAPE PATH LIGHTING INOP FORWARD CABIN BY GALLEY CARTS. REPLACED EMERGENCY ESCAPE PATH LIGHT STRIP, CHECKS O K. 2 L 7 2 4F 4 F RT A16WE E2GL 1996081500130 19960815 00130 NE 1996 8 15 9617151158 2 19960807 A 7200 ENGINE DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20J 52054 NE NR 1 OVERTEMP A NWAA E ENGINE SHUTDOWN J WARNING INDICATION LD LANDING 1 GL 01 158US 46767 86169 DURING LANDING ROLLOUT, THE NR 1 ENGINE EGT WENT ABOVE RED LIMIT LINE FOR ABOUT THREE SECONDS. THE ENGINE WAS THEN SHUT DOWN WHILE STILL IN REVERSE AND A/C TAXIED TO GATE WITHOUT FURTHER INCIDENT. PERFORMED ENGINE OVER TEMPERATURE INSPECTI ON AND NO DISCREPANCIES WERE FOUND. ENGINE RUNUP CHECK WAS NORMAL AND A/C RETURNED TO SERVICE. 2 L 7 3 4F 4 F A22WE E20EA 1996082200485 19960822 00485 NE 1996 8 22 IXXA96117 2 19960727 A 7321 8062479 MEC DOUG DC8 DC871 302199A WP GE CFM56 CFM562C1 13802 NE NR 2 ENGINE LEAKING A IXXA K NONE K FLUID LOSS LD LANDING 1 SW 11 824BX 45946 692296 COMPRESSOR STALL ACCOMPANIED BY FLAMES EXITING THE EXHAUST NOZZLE REPORTED TO THE CREW BY THE CONTROL TOWER ON LANDING R OLL AT PDX, CREW SUSPECTED THE NR 2 ENGINE. MX BORESCOPED THE NR 2 ENGINE WITH NO FINDINGS. MX FOUND THE MEC SUSPECT O F CAUSING THE STALL DUE TO LEAKAGE. THE MEC WAS REPLACED IAW THE MM. (M) 2 L 7 4 4F 4 F 4A25 E2GL 1996090500330 19960905 00330 NE 1996 9 5 96ZZZX4252 2 19960404 A 7260 430101301 SEAL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE ACC DRIVE LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 117CW 922 7125 LE45022E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1996091900160 19960919 00160 NM 1996 9 19 96UAL900686 1 19960905 A 3350 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 385UA 24660 EMERGEMCY EXIT LIGHTING AT DOORS 1L AND 1R INOPERATIVE. REPLACED EMERGENCY EXIT LIGHTING AT DOORS 1L AND 1R. OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 1996091900242 19960919 00242 GL 1996 9 19 96ZZZX4613 2 19960702 A 7200 ENGINE BOLKMS 105 BO105LSA1 5626021 EU ALLSN 250C 250C28C 03013 GL NR 1 FAILED A R7MA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NM 11 NR 1 ENGINE TORQUE SPLIT, COULD NOT BEEP ENGINE BELOW 90 PERCENT, LANDED, CALLED MAINTENANCE. 1 G 7 2 3U 3 U H3AU E1GL 1996092600734 19960926 00734 NE 1996 9 26 DHL96727007 2 19960920 A 7314 243600 FUEL PUMP 7436023 BOEING 727 727228 NM PWA JT8 JT8D7B 52053 NE NR 2 ENGINE MALFUNCTIONED A DHLA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 01 727DH 59854 20204 654838 AFTER TAKEOFF, NR 2 ENGINE LOST POWER DOWN TO 1.24 EPR, 73 PERCENT N1, 380 EGT, 82 PERCENT N2, 3,000 LBS FUEL FLOW. SHU T ENGINE DOWN AS PER OPS PRECEDURE, LANDING NORMAL. INSTALLED FUEL PUMP AND FCU IAW P AND W MM 73-21-2 AND P AND W MM 7 3-11-1. LEAK CHECK OK, GROUND RUN AND TRIM PER JRH 06-04-1, OK. 2 L 7 3 4F 4 F A3WE E2EA 1996100300250 19961003 00250 WP 1996 10 3 96UAL900738 1 19960921 A 3610 PNEUMATIC DUCT DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 1/3 ENGINES LEAKING A UALA K NONE O OTHER NR NOT REPORTED 1 WP 29 1845U 48261 UNABLE TO START ENGINES 1 AND 3 DUE TO EXCESSIVE AIR LEAK FROM SEPARATED PNEUMATIC DUCT INBOARD OF NR 1 ENGINE. 2 L 7 3 4F 4 F A22WE E23EA 1996101000062 19961010 00062 GL 1996 10 10 ERAA96267 2 19960627 A 7210 23055464 GEARBOX COVER BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL RED GR BOX LEAKING A ERAA K NONE K FLUID LOSS IN INSP/MAINT 1 AL 03 297EH S835 GEARBOX OVERHAULED ON CADORATH WORK ORDER M708 AND RETURNED TO ERA 6-13-96. TORQUE METER BUSHING LEAKING. 1 G 7 2 3U 3 U H3EU E4CE 1996101000425 19961010 00425 NE 1996 10 10 CA960202010 2 19960122 A 8540 REAR SECTION DHAV DHC3 DHC3 2800202 EA PWA R1340 R1340* 52016 NE ENGINE MAKING METAL W O OTHER O OTHER IN INSP/MAINT 1 CA 710 23654 (CAN)EXCESSIVE CONCENTRATION OF ALUMINUM FLAKES AND METAL SHAVING IN THE OIL SCREEN. NO METAL CONTAMINATION FOUND IN OTH ER SECTIONS OF THE ENGINE, ACCESSORIES OR ASSOCIATED SYSTEMS. ENGINE WAS REMOVED FOR INVESTIGATION. REPORT TO FOLLOW. 1 H 7 1 3R 3 R A815 5E2 1996101000427 19961010 00427 EA 1996 10 10 CA960202012 1 19960118 A 7921 8540012 OIL COOLER HARRISON APO9AN1308 DHAV DHC6 DHC6300 EA PWA PT6 PT6A27 52043 EA COOLING FIN LEAKING OIL W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 1341 79H788 PCE40348 (CAN)AFTER NUMEROUS ATTEMPTS TO LOCATE AND REPAIR A SMALL OIL LEAK ON THE #1 ENGINE, INCLUDED IN THE FIXES WERE SEAL REP LACEMENT OF THE STARTER GENERATOR, FCU, FUEL PUMP DRIVE, FRONT CASE PROP SEAL, NONE O F THESE REPAIRS CURED THE OIL LEAK . AFTER MUCH TROUBLESHOOTING THE OIL COOLER WAS REPLACED AND THE PROBLEM WAS RECTIFIED. A PRESSURE TEST OF THE OIL COOLE R REVEALED A STEADY STREAM OF AIR BUBBLES FROM THE LOWER LEFT HAND CORNER OF THE COOLER WHERE THE COOLING FINS MEET THE OIL COOLER CASE. 1 H 7 2 3T 4 T A9EA E4EA 1996101700314 19961017 00314 NE 1996 10 17 9621781150 2 19961012 A 7230 COMPRESSOR BLADE DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20J 52054 NE NR 1 ENGINE DAMAGED A A NWAA O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 GL 01 150US 46759 86178 DURING CRUISE AT FL350, THE NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL AND RECOVERED. EPR INCREASED AND N1 FLUCTUATED. CREW FOLLOWED COM PROCEDURES AND CONTINUED FLIGHT TO SEA WITHOUT FURTHER INCIDENT. BORESCOPE INSPECTION REVEALED DAMAG E TO THE 8TH STAGE HIGH COMPRESSOR BLADES. THE ENGINE WAS REMOVED. 2 L 7 3 4F 4 F A22WE E20EA 1996102400372 19961024 00372 NE 1996 10 24 GTIA96NK142 2 19960213 A 7261 OIL FILTER DOUG DC9 DC921 302205A WP PWA JT8 JT8D11 52044 NE NR 1 ENGINE LEAKING A GTIA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 GL 23 125NK 47302 676195 LOG PAGE 03409 - LEFT ENGINE LOST OIL QUANTITY. ENGINE SHUT DOWN WITH 3 QUARTS OF OIL REMAINING. FOUND OIL LEAK COMING FROM MAIN OIL FILTER. INSTALLED NEW FILTER, REPLACED PACKINGS, SERVICED OIL. OPS AND LEAK CHECK GOOD IAW DC-9 MM CHAP TER 79. (X) 2 L 7 2 4F 4 F A6WE E2EA 1996102400939 19961024 00939 NE 1996 10 24 USAAD96133 2 19960928 A 7322 7436024 FUEL CONTROL DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7B 52053 NE LT ENGINE FAILED A USAA E A ENGINE SHUTDOWN UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 EA 19 952VJ 32315 47574 649398 FLT 2133 - PHL-ATL - JUST AFTER ROTATION, LEFT ENGINE SPOOLED DOWN TO ZERO. RETURNED TO FIELD. REPLACED LEFT FUEL CONT ROL UNIT. (M) 2 L 7 2 4F 4 F A6WE E2EA 1996110100051 19961101 00051 SW 1996 11 1 CA960312013 1 19960212 A 6730 41103750017 SERVO BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL INTERNAL MOTORING W O OTHER F FLT CONT AFFECTED CR CRUISE 1 CA 3 801246BA (CAN)UNCOMMANDED SERVO MOTORING. SERVO OVERHAULED 2.9 HOURS PREVIOUSLY. 1 G 7 1 3U 3 U H2SW E4CE 1996110700099 19961107 00099 NM 1996 11 7 96UAL900833 1 19961022 A 5310 STRUCTURE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 727-787 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 THE LOWER SIDE OF THE FUSELAGE BETWEEN BODY STATIONS 727 AND 787 FROM STRINGER 25 LEFT TO 25 RIGHT WAS DAMAGED WHEN A TO W TRACTOR IMPACTED THE AIRCRAFT. DAMAGE CONSISTS OF TORN SKIN, SEVERED STRINGERS, DAMAGED FRAMES AND MISCELLANEOUS DAMA GE TO INTERNAL BRACKETS, INTERCOSTALS, ETC. ALL DAMAGED PARTS WERE REPLACED OR REPAIRED PER APPLICABLE STRUCTURAL REPAI R MANUAL AND ENGINEERING VARIANCE AUTHORITY. 2 L 7 2 4F 4 F RT A16WE E2GL 1996111400604 19961114 00604 EA 1996 11 14 CA960417510 1 19960324 A 3234 750005000 VALVE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE LANDING GEAR FAILED W D RETURN TO BLOCK E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 CA 2884 807195 (CAN)AFTER TAKEOFF, VIBRATION OCCURRED DURING LANDING GEAR RETRACTION ALONG WITH 'GEAR DISAGREE' MESSAGE. NOSE GEAR UP, LEFT AND RIGHT MAIN GEARS IN TRANSIT AND CYCLING. GEAR SELECTED DOWN ALL INDICATIONS NORMAL. SELECTED UP PROBLEM REOCCU RRED. LANDING GEAR SELECTOR VALVE REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 1996112100162 19961121 00162 NE 1996 11 21 CA960424005 2 19960423 A 7261 OIL SYSTEM LYC ALF502R5 LYC ALF502 ALF502R5 41580 NE NR 4 ENG CONTAMINATED W K NONE J WARNING INDICATION IN INSP/MAINT 1 CA 17399 LF05463A LF05463A (CAN)#4 ENGINE CHIP DETECTOR ON ANALYSIS OF DEBRIS SHOWS BEARING AND GEAR MATERIAL PRESENT. ENGINE REPLACED 4 F E6NE 1996112700003 19961127 00003 NE 1996 11 27 CA960507015 2 19960426 A 8520 74943 CRANKCASE PWA R985 DHAV DHC2 DHC2EVANS 2801832 EA PWA R985 R985AN14B 52008 NE AFT BEARING BOSS CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 614 22667 22667 (CAN)METAL FOUND IN OIL FILTER. A CYLINDER WAS REMOVED FOR INTERNAL CHECK. RADIUS CRACK FOUND AROUND REAR MAIN BEARING B OSS. 1 H 7 1 3O 3 R A806 5E1 1996112700054 19961127 00054 SW 1996 11 27 CA960521201 1 19960514 A 7120 MS2000612 BOLT SWRNGN SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP ENG MOUNT BROKEN W A K NONE O OTHER IN INSP/MAINT 1 CA 624 P50008 (CAN)ENGINE MOUNT TO FIREWALL BOLT, INBOARD UPPER POSITION, FOUND BROKEN IN TWO PIECES. NO FRETTING OF FIREWALL AT ANY MOUNT LOCATION. 91 HOURS SINCE LAST INSPECTION. PARTS NEW IN JUNE 95. PARTS SENT FOR LAB ANALYSIS. 2 L 7 2 4T 4 T RT A8SW E4WE 1996120300038 19961203 00038 NM 1996 12 3 UPS96221514 1 19961019 A 5320 SUPPORT BOEING 727 7271A7C 13840X2 NM RROYCE TAY TAY65154 EU BS 304-344 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 935UP 20143 INSPECTION TYPE: C. LAVATORY FLOOR - FLOOR SUPPORT HAT SECTION UNDER LAV DOOR HAS CORROSION FROM STA 304-344. REMOVE D, FABRICATED AND INSTALLED REPLACEMENT PART I.A.W. DRAWING 65-26173 AND SRM 51-30-2. 2 L 7 3 4F 4 F A3WE E25NE 1996120500123 19961205 00123 NE 1996 12 5 96ZZZX5796 2 19960729 A 7321 7436025 FUEL CONTROL HAMSTD JFC602 BOEING 737 7372T4 1384492 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE MALFUNCTIONED A A ZZDA A E D UNSCHED LANDING ENGINE SHUTDOWN RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 15 467AT 568 92016 22055 P695378B AFTER SETTING TAKEOFF THRUST FOR FLT 704, AT APPROX 60 KNOTS, NR 1 ENGINE HAD AN AUTO ACCELERATION AND OVERSPEED. N1 RP M PEGGED AT RED LINE AND EPR WAS NOTED AT 2.22. EGT WAS NOT RECORDED. NR 1 ENGINE THROTTLE WAS RETARDED BUT RPM DID NO T FOLLOW. ENGINE WAS SHUT DOWN WITH START LEVER. WHEN ACFT ATTEMPTED TO TAXI, PARKING BRAKES WOULD NOT RELEASE. MECHA NICS RELEASED BRAKES AND TAXIED ACFT TO HANGAR. ALL BRAKE ASSEMBLIES REPLACED. INVESTIGATION OF NR 1 ENGINE REVEAL NO DISCREPANCIES WITH THROTTLE RIGGING. SUSPECT FAILURE OF ENGINE FUEL CONTROL. REPLACED NR 1 ENGINE AND PLACED ACFT BACK IN SERVICE. REPLACED DFDR AND SENT OUT FOR INTERPRETATION OF ALL ENGINE DATA ON NR 1 ENGINE FOR 7-29-96. 2 L 7 2 4F 4 F A16WE E2EA 1996121200288 19961212 00288 SO 1996 12 12 CA960625017 1 19960606 A 5751 4A25206001 SUPPORT EMB EMB 110 EMB110P1 3260122 SO PWA PT6 PT6A34 52043 EA RIGHT AIL CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 16721 PCE56946 (CAN) RIGHT AILERON BRACKET, CENTRE SUPPORT CRACKED ON CENTRE AILERON SPAR. 1 L 7 2 4T 4 T A21SO E4EA 1996121200327 19961212 00327 EA 1996 12 12 CA960709011 1 19960701 A 2910 DSC252B40124 HYDRAULIC LINE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE #2 HYDRAULIC SPLIT W A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 CA 123152 (CAN) FLIGHT CREW REPORTED #2 HYDRAULICS AT ZERO QUANTITY. INSPECTION FOUND A SUPPLY LINE SPLIT. LINE REPLACED WITH APPR OVED FLEX LINE. 2 H 7 2 4T 4 T RT A13NM E20NE 1996121200346 19961212 00346 NE 1996 12 12 CA960723002 2 19960718 A 7210 BEARING DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE REDUCTION GEARBX FAULTY W A K NONE J WARNING INDICATION IN INSP/MAINT 1 CA 613 121165 (CAN) #1 ENGINE REDUCTION GEARBOX CHIP DETECTOR FLAGGED. MATERIAL FOUND TO BE M-50 BEARING MATERIAL. ENGINE WAS CHANGED. IT IS SUSPECTED RGB BEARING DAMAGE CAUSED BY POSSIBLE LIGHTNING STRIKE AS #2 ENGINE WAS CHANGED A FEW DAYS EARLIER FOR THE SAME PROBLEM. 2 H 7 2 4T 4 T RT A13NM E20NE 1996121900079 19961219 00079 NM 1996 12 19 96UAL900915 1 19961204 A 5400 BACN10JC24CM FUSE PIN BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE NR 1 PYLON OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 105UA 12446 26473 NUMBER ONE PYLON INBOARD STRUT SPRING BEAM FUSE PIN MIGRATED OUT OF POSITION. *S/D* EXISTING FUSE PIN AND NUT REMOVED AND REPLACED WITH NEW PARTS. ANALYSIS OF REMOVED FUSE PIN AND NUT DID NOT REVEAL ANY DISCREPANCIES. PARTS SENT TO BOEI NG FOR FURTHER ANALYSIS. FUSE PIN (P/N 310U2301-120). 2 L 7 4 4F 4 F RT A20WE E24NE 1996122600526 19961226 00526 NE 1996 12 26 RRXA96174 2 19961221 A 7321 FCU DOUG DC8 DC863 302198A WP PWA JT3D JT3D7 52039 NE NR 4 ENGINE FROZEN A RRXA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 15 796AL 46054 ABORTED TAKEOFF DUE TO POWER LOSS ON NR 4 ENGINE. THE ENGINE DID NOT FLAME OUT. CORRECTIVE ACTION: MAINTENANCE FOUND FCU FROZEN DUE TO TEMPERATURE. PERFORMED HIGH POWER RUN REF. DC8 RUN UP HAND BOOK, ALL OPS CHECK GOOD, ALL PERAMATERS W ERE NORMAL. 2 L 7 4 4F 4 F 4A25 1E8 1996122600540 19961226 00540 NM 1996 12 26 CA960620008 1 19960529 A 5730 SKIN BOEING 757 75723A 1384967 NM RROYCE RB211 RB211535E4 54555 NE RT WING PUNCTURED W K NONE O OTHER IN INSP/MAINT 1 CA 30655 (CAN) RH WING UPPER SURFACE FIXED LEADING EDGE PUNCTURED AT STN WS 481-50 REPAIRED AS PER SRM. 2 L 7 2 4F 4 F RT A2NM E12EU 1997010200285 19970102 00285 NM 1997 1 2 CA960812008 1 19960809 A 3230 65358492 BEARING BOEING 737 737242C 1384478 NM PWA JT8 JT8D9A 52048 NE NLG RETRACT CORRODED W A D UNSCHED LANDING RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 CA 707397 (CAN) NOSE GEAR WOULD NOT LOCK IN THE UP POSITION. RETRACT CYLINDER UPPER ATTACH CASTING OUTER RACE DEFORMED AND CASTING CORRODED. CORROSION REMOVED AND BEARING REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1997010200378 19970102 00378 SO 1997 1 2 SWIA95796 1 19961221 A 2751 CONTROL UNIT EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE TE FLAPS MALFUNCTIONED A SWIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 07 203SW 120240 ON TAXI OUT, RECEIVED FLAP CONTROL FAULT. RESET AND IMMEDIATELY RECEIVED ANOTHER FLAP CONTROL FAULT. RERACKED FLAP CON TROL UNIT, OPS CKS GOOD, IAW MM 27-00-00. 2 L 7 2 4T 4 T RT A31SO E20NE 1997011600089 19970116 00089 NE 1997 1 16 CA960227011 2 19960129 A 7260 107006204 SPUR GEAR BELL 205 205A1 1181414 SW LYC T53 T5313B 41549 NE ENG BROKEN W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA LE07676 (CAN) ENG ACCESSORY DRIVE FAILED. ENGINE REPAIRED. 1 G 7 1 4U 4 U H1SW E17EA 1997012200001 19970122 00001 EU 1997 1 22 CA960229002 1 19960228 A 4990 APU BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE APU OIL LEAK W A H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA LF05464A (CAN) AFTER SITTING FOR 1.5 HOURS WITH APU AND AIR CONDITIONING RUNNING, THE CABIN BECAME CONTAMINATED WITH FUMES. THE A IRCRAFT WAS AIRED OUT AND THE APU INOP'D. APPEARS TO BE AN INTERNAL OIL LEAK IN THE APU. SUBMITTER SUSPECTS COMPANY CAMP AIGN TO CHANGE FROM EXXON 2380 OIL TO CASTROL 5000. OIL IS BEING CHANGED BACK TO EXXON 2380 AND OIL LEAK FIXED. SIMILAR PROBLEMS IN MAIN ENGINES. 2 H 7 4 4F 4 F RT A49EU E6NE 1997012200007 19970122 00007 GL 1997 1 22 CA960826081 1 19960817 A 7931 V360004 SENSOR DIAMON DA20A1 DA20A1 05626UX GL ROTAX 912 ROTAX912 55555 EU OIL PRESS FAULTY W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 516 4380732 (CAN) PRESSURE SENSOR FAILED OPEN AND CAUSED FULL HIGH DEFLECTION OF OIL PRESSURE INDICATION. 1 L 7 1 3O 3 I NT TA4CH EXPE3I 1997013000490 19970130 00490 NM 1997 1 30 CA960909012 1 19960722 A 3213 101361 BEARING DOWTY 10100113 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE LOWER STRUT CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA DCL15486 120275 (CAN) DURING A REWEIGH, THE RIGHT HAND MAIN LANDING GEAR SHOCK STRUT WAS NOTICEABLY JERKY AND SLOW. INSPECTION FOUND THE LOWER STRUT BEARING CORRODED BEHIND THE PHENOLIC MATERIAL, FORCING THE MATERIAL OUT WITH ENOUGH PRESSURE TO PREVENT THE SHOCK STRUT FROM EXTENDING SMOOTHLY. 2 H 7 2 4T 4 T RT A13NM E20NE 1997032700088 19970327 00088 EA 1997 3 27 CA961028008 1 19961023 A 5330 C6FS24161 PANEL DHAV DHAV DHC6 DHC6300 EA PWA PT6 PT6A27 52043 EA FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 26666 PCE40548 (CAN) TOP CENTRE FUSELAGE SANDWICH PANEL HAD A 4 INCH CRACK AT THE FORWARD RIGHT INTERIOR CORNER AND A SIGNIFICANT DEBON DING. THIS AREA IS REGULARLY WALKED ON, THUS DISBONDING CAN DEVELOP DUE TO PANEL CONSTRUCTION. A 0.016" TOP AND BOTTOM S KINS WITH A 0.375" BALSA CORE. IN ALL PROBABILITY THE DISBOND CONDITION CONTRIBUTED TO MOISTURE INGRESS AND THE RESULTAN T CORROSION. 1 H 7 2 3T 4 T A9EA E4EA 1996032900145 19960329 00145 EU 1996 3 29 QXEA9600124 1 19960322 A 5220 RELEASE MECH FOKKER F28 F28MK1000 4990808 EU EMER EXIT DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 457US 11036 SERVICE/EMERGENCY DOOR EMERGENCY RELEASE MECHANISM WOULD NOT RELEASE DURING C-CHECK TASK CARD OPS CHECK. EMERGENCY RELE ASE MECHANISM REMOVED, CLEANED, LUBED AND REINSTALLED I/A/W MAINT MANUAL. RELEASE MECHANISM OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1996032200198 19960322 00198 WP 1996 3 22 96ZZZX1230 1 19960204 A 2120 AIR DISTR LKHEED 1011 10113851 5265010 WP LT LAVATORY ODOR A TWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 41016 193B1060 STL - FLT 86 - DURING CRUISE, LT FORWARD LAVATORY EMITTED AN ELECTRICAL ODOR. CHECKED LIGHT BALLAST AND WIRING, FLUSH S YSTEM WIRING, SMOKE DETECTOR SYSTEM. FOUND NO INDICATION OF OVERHEAT OR SOURCE OF ODOR. ALL SYSTEMS CHECKED NORMAL. C HECK C-7C - 1-14-96 - LAX. 2 L 7 3 4F A23WE 1996110700730 19961107 00730 NM 1996 11 7 9623406302 1 19961105 A 2121 732591C FAN BOEING 747 747451 1384940 NM COCKPIT FAILED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 662US 27954 27954 23720 DURING CRUISE, SMOKE ACCUMULATED IN THE CABIN. AIRCRAFT DIVERTED TO NRT AND LANDED WITHOUT INCIDENT. REPLACED THE LOWE R RECIRCULATION FAN, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1996062700217 19960627 00217 EU 1996 6 27 96ZZZX3101 1 19960417 A 5312 BULKHEAD BAG BAE146 BAE146300A 1500267 EU LT MLG WW GOUGED A A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 616AW E3145 ATW - LT MLG BAY, FRAME 29 BULKHEAD, HAS A GOUGE APPROXIMATELY 7 INCHES LONG WITH 3 DAMAGED RIVET HEADS AND IS APPROXIMA TELY .012 INCH DEEP. MEASURED DEPTH AGAIN WITH PAINT STRIPPED. REPAIRED LT MLG AT FRAME 29. REFER TO WC NR 1063 FOR N DT. EPOXY PRIMED AND TOPCOATED. REF FAX HC/137-96 S/N 3145. HC/134-96, JM/RJ0477-96, JM/RJ0473-96, DR/RJ0498-96. 2 H 7 4 4F RT A49EU 1996021600303 19960216 00303 1996 2 16 96UAL900099 4 19960209 A 2565 D31039113 SLIDE BOEING 757 757222 1384956 NM DOOR 2R LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 536UA 25156 DOOR 2 RT SLIDE RETURNED TO SHOP FOR TIME CONTROLLED OVERHAUL. LOWER INFLATION TUBE IS LEAKING AT THE SEAMS AND THERE I S CORROSION IN BOTH ASPIRATORS AND ON THE CHECK VALVES. RETURNED TO VENDOR FOR REPAIR. 2 L 7 2 4F RT A2NM 1996100300251 19961003 00251 WP 1996 10 3 ABXA9600631 1 19960924 A 5210 DOOR SEAL DOUG DC8 DC861 3021952 WP PAX DOOR LOOSE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 847AX 46031 DURING ENGINE START, FORWARD CABIN DOOR OPEN LIGHT ILLUMINATED. COULD NOT OPEN DOOR FROM THE INSIDE. FOUND A STRIP OF METAL LOOSE ON THE LOWER FORWARD DOOR SEAL. RESECURED AS REQUIRED. 2 L 7 4 4F 4A25 1996052300482 19960523 00482 NM 1996 5 23 96UAL900364 1 19960521 A 3350 LAMP BOEING 737 737522 138449F NM CABIN INOPERATIVE A UALA K NONE L NO TEST UK UNKNOWN 1 WP 29 906UA 25006 DOOR ONE LEFT EMERGENCY LIGHT INOP. RELAMPED, CHECKS OK. 2 L 7 2 4F RT A16WE 1996121200129 19961212 00129 SO 1996 12 12 96ZZZX5921 1 19961017 A 3210 AN17727 BOLT PIPER PA23 PA23250 7102308 SO LT MLG BROKEN A VAIA K NONE O OTHER NR NOT REPORTED 1 SO 21 5623Y 272733 BOLT BROKE AND CAUSED LEFT LANDING GEAR TO FAIL. 1 L 7 2 3O 1A10 1996101000477 19961010 00477 CE 1996 10 10 96ZZZX5120 1 19960904 A 5220 08125001 MOUNT ASSY CESSNA 310 310Q 2074242 CE WINDOW RELEASE MISINSTALLED A A GTUA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 19 7935Q 6423 310Q0667 EXCESS WIND NOISE FORM EMERGENCY EXIT WINDOW HAS BEEN A RECURRING PROBLEM. EACH TIME MAINTENANCE PERSONNEL HAVE TO RESE CURE FORWARD PIN WHICH IS CONNECTED TO WINDOW RELEASE CABLE, THE CABLE HAS BEEN TOO SHORT AND THE PIN WOULD BARELY REACH . CLOSER INVESTIGATION REVEALED THE HAT SECTION WHICH HOLDS THE RELEASE CABLE HANDLE WAS INSTALLED UPSIDE DOWN APPARENT LY FROM THE FACTORY. NO EVIDENCE OF EVER BEING REMOVED. THE RELEASE CABLE HAD TO PASS BELOW THE MS20392-2 FLAT HEAD PI N WHICH GIVES IT AN 'S' TURN WHEN HAT SECTION 0812500-1 IS UPSIDE DOWN. HAT SECTION WAS TURNED OVER, NO NEW HOLES REQUI RED, ONLY DRILLING RIVETS OUT AND REPLACING, AND CABLE LENGTH BECAME ADEQUATE. 1 L 7 2 3O 3A10 1996031500545 19960315 00545 NM 1996 3 15 CAL960136 1 19960110 A 5320 SUPPORT BOEING 727 727227 1384078 NM BS 644 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 49249 21247 STATION 31J - INSPECTION FOUND FLOOR SUPPORT CORRODED AROUND ANCHOR NUTS AT BS 644 ABOVE STRINGER 28R. THE FLOOR SUPPOR T FITTING WAS REMOVED AND REPLACED. A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-4, 51-10-2, AND 51-40-2. (M) 2 L 7 3 4F A3WE 1996011900034 19960119 00034 NM 1996 1 19 96UAL900030 1 19960112 A 2121 36144161 COOLING FAN BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE AIR DISTR SYST FAILED A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 29 608UA 2488 21869 61500 AT START OF DESCENT, HEAVY SMOKE FILLED THE CABIN AND COCKPIT. SUPPLEMENTAL DATA UPDATE: THE APU HAD A SEVERE COOLING FAN FAILURE WHICH CAUSED OIL TO LEAK IN THE INLET PLENUM, CONTAMINATING THE AIR CONDITIONING SYSTEM. THE COOLING FAN HA D THE SHROUDED ROTOR. PART TOTAL CYCLES, 2,347. 2 L 7 2 4F 4 F RT A1NM E3NE 1996012600202 19960126 00202 NE 1996 1 26 SWAA960030 2 19960113 A 7200 ENGINE BOEING 737 7373G7 1384595 NM GE CFM56 CFM563B1 13802 NE NR 2 FAILED A SWAA E A ENGINE SHUTDOWN UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SW 07 671SW 23785 721339 AT 37,000, EXPERIENCED NUMBER 2 ENGINE OIL PRESSURE DROP, THEN ENGINE STOPPAGE. CREW PERFORMED ENGINE SHUTDOWN CHECKLI ST. AIRCRAFT DIVERTED TO TUS AND MADE AN UNEVENTFUL LANDING. REPLACED NUMBER 2 ENGINE PER BOEING M/M. 2 L 7 2 4F 4 F RT A16WE E2GL 1996020200232 19960202 00232 NM 1996 2 2 96UAL900075 1 19960129 A 2130 FLOW CONTL VALVE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE RADIO RACK MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 7257U 21404 AIRCRAFT RETURNED, UNABLE TO MAINTAIN PRESSURE. CABIN WOULD NOT HOLD MORE THAN 1 DIFFERENTIAL PRESSURE CLIMBING THROUGH 10K FEET, CABIN WAS 8,000 FEET. ACCOMPLISHED PRESSURE CONTROL SYSTEM CHECK, NO DEFECTS FOUND. RAN ENGINES AND DUCT PR ESSURE NORMAL. AIRCRAFT PRESSURIZED OKAY. RADIO RACK FLOW CONTROL VALVE OFF SCHEDULE AT RENO. REPLACED RADIO RACK FLO W CONTROL VALVE. 2 L 7 3 4F 4 F A3WE E2EA 1996021600567 19960216 00567 NE 1996 2 16 PLG1296E1 2 19960101 A 7200 ENGINES SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE LEFT FLAMED OUT A PLGA A UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 NE 05 340BE 340A062 FLT NR 4609 - BOS-DCA - DURING CRUISE, THE LEFT ENGINE FLAMED OUT AND THE ASSOCIATED CHIP LIGHT ILLUMINATED. THE AIRCRA FT DIVERTED INTO ACY AND LANDED WITHOUT INCIDENT. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 1996030800028 19960308 00028 NE 1996 3 8 AWXA960035 2 19960130 A 7320 BACC14H4LD P2 CAP BOEING 737 737277 1384570 NM PWA JT8 JT8D15 52051 NE NR 2 ENG LOOSE A AWXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 28 181AW 22648 FLT NR 282 - MDW-CMH - ABORTED TAKEOFF, NR 2 EPR INDICATION WAS LOW AND FLUCTUATING. MAINTENANCE INSPECTION AND FOUND T HE P2 TEST CAP AT EPR TRANSMITTER LOOSE AND THE JAM NUT AT PT7 TEE FITTING TO TRANMITTER LOOSE, RESECURED. RAN ENGINES TO TAKEOFF POWER. EPR MADE ALL PARAMETERS PER MM 71-11-01 AND 71-09-236. (M) 2 L 7 2 4F 4 F RT A16WE E2EA 1996031500322 19960315 00322 NE 1996 3 15 HEEA966784 2 19960228 A 7321 324473513 FUEL CONTROL BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE ENG DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22347 36005 10% TORQUE SPLIT WITH #1 HIGH AT 90% TORQUE. DURING TROUBLESHOOTING, IDLE SHIFTED TO 74% N1 AND THROTTLE WOULD SELF ADVA NCE. 1 G 7 2 4U 4 U H4SW E22EA 1996041200382 19960412 00382 NM 1996 4 12 96UAL900246 1 19960409 A 3350 BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7287U 21565 LEFT CENTER EMERGENCY EXIT LIGHT WILL NOT TEST. REPLACED BATTERY CARTRIDGE, CHECKS OKAY. 2 L 7 3 4F 4 F A3WE E2EA 1996041200384 19960412 00384 WP 1996 4 12 ABXA9600448 1 19960408 A 2612 FIRE WARNING DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3B 52039 NE NR 2 ENGINE MALFUNCTIONED A ABXA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 GL 23 803AX 45917 669706 DURING CRUISE, NR 2 ENGINE FIRE WARNING LIGHT AND BELL CAME ON INTERMITTENTLY AND THEN WOULD NOT TEST. NR 2 ENGINE SCAN REVEALED NO VISUAL CONFIRMATION OF FIRE. SHUTDOWN THE NR 2 ENGINE AND THEN FIRE WARNING TESTED OK. NR 2 ENGINE MAINTA INED 25 PSI OF OIL PRESSURE WHILE WINDMILLING. PERFORMED FIRE DETECTION SYSTEM LOOP GROUND CHECK ON THE NR 2 ENGINE IAW DC8 WDM, CHAPTER 26-11-1 AND SYSTEM CHECKED GOOD. PERFORMED GROUND OPS CHECK IAW DC8 MM, CHAPTER 26-10-1 AND SYSTEM CH ECKED GOOD. GROUND RAN ENGINE TO TAKEOFF POWER AND NO DEFECTS OR WARNINGS WERE NOTED. 2 L 7 4 4F 4 F 4A25 1E8 1996041800455 19960418 00455 NE 1996 4 18 IXXA9638 2 19960318 A 7314 451231 FUEL PUMP DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3B 52039 NE NR 4 ENGINE LEAKING A IXXA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SW 11 51CX 46027 678991 ON DESCENT INTO SJU, THE NR 4 ENGINE WAS PRECAUTIONARILY SHUT DOWN DUE TO LOW OIL QUANTITY. ON THE GROUND IN SJU, MAINT ENANCE DETERMINED THAT THE ENGINE FUEL PUMP GEARBOX DRIVE SEAL WAS LEAKING INTO ITS SPLINE CAVITY. THE DRIVE WAS RESEAL ED, AND THE ENGINE LEAK CHECKED OK. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 4 4F 4 F 4A25 1E8 1996042500509 19960425 00509 EA 1996 4 25 SWIA95732 1 19960422 A 3230 PRIORITY VALVE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE MLG MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 410SW 7066 AFTER DEPARTURE, NOSE GEAR FAILED TO RETRACT. PERFORMED QRH CHECKLIST. RETURNED TO PDX WITH A NORMAL LANDING. REMOVED AND REPLACED MAIN LANDING GEAR PRIORITY VALVE IAW MM 32-32-15, OPS AND LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 1996060600398 19960606 00398 NE 1996 6 6 96ZZZX2822 2 19960329 A 7250 414129001 ROTOR ASSY BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE POWER TURBINE BLADE SHIFT A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 7060G 953 SC46896 7173 LE45583F FAILED SB LT101-72-10-0153. EXCESSIVE IBPT BLADE SHIFT NR 7 AT .0025 INCH. REPLACED WITH USED UNIT, CORRECTED PROBLEM. PART TOTAL CYCLES, 2,219.9. 1 G 7 2 3U 3 U H13EU E5NE10 1996062000043 19960620 00043 NE 1996 6 20 COMA9630125 2 19960611 A 7261 OIL SYST SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LT ENGINE REQD SERVICE A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 320CA 340A064 367226 LEFT ENGINE LOW OIL PRESSURE WARNING DURING FLIGHT. INSPECTED ENGINE FOR LEAKS AND FOUND NONE, ADDED 2 QUARTS OIL AND A IRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE6 1996062000707 19960620 00707 GL 1996 6 20 HEEA967234 2 19960515 A 7250 6878498 NOZZLE DIAPHRAGM 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL 2ND STAGE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5029H 2553 CAT30779F S670 CAE821950F TURBINE REMOVED DUE TO CYCLED OUT #1 AND #2 WHEELS. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: CRACKED BEYO ND OVERHAUL LIMITS ON 2ND STAGE NOZZLE DIAPHRAGM. REPLACE DISCREPANT PART. 1 G 7 2 3U 3 U H3EU E4CE 1996062700311 19960627 00311 NE 1996 6 27 96ZZZX3125 2 19960514 A 7230 COMPRESSOR BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE NR 2 ENGINE STALLED A A6WA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 31 606AW 14656 371 E2033 LF05432A ASE - FLT 650 - WHILE APPLYING TAKEOFF POWER, NR 2 ENGINE POPPED AND SHUT DOWN. DEN MX LOCKED DOWN ENGINE AND WILL 3-EN GINE FERRY TO ATW. REMOVED AND REPLACED ENGINE. 2 H 7 4 4F 4 F RT A49EU E6NE 1996072500298 19960725 00298 NM 1996 7 25 9615682768 1 19960716 A 7711 EPR INDICATION BOEING 727 7272M7 138407S NM PWA JT8 JT8D17R 52049 NE NR 2 ENGINE DROPPED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 01 728RW 21741 688251 DURING TAKEOFF, NR 2 ENGINE EPR INDICATION DROPPED. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. INSPECTED AND OPERA TIONALLY CHECKED NR 2 ENGINE. OK FOR SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 1996080200548 19960802 00548 WP 1996 8 2 96UAL900569 1 19960723 A 2130 ACM701051 DUCT SUPPORT DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 1 AC DUCT BROKEN A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 1812U 46611 DURING CLIMB AROUND 8,000 TO 9,000 FEET HEARD RUMBLE UNDER PILOTS FEET. A SHORT TIME AFTER, LOST CONTROL OF CABIN PRESS URE. PERFORMED LOSS OF PRESSURE VIBRATION CHECK LIST. UNABLE TO RESTORE CONTROL OF CABIN PRESSURE, RETURNED TO LAS. * S/D* DUCT SUPPORT ATTACHMENT, DOWNSTREAM OF THE WATER SEPARATOR, FAILED AND CAUSED DUCT SEPARATION. INTERIM REPAIR MAD E TO DUCT SUPPORT ATTACH POINTS. 2 L 7 3 4F 4 F A22WE E23EA 1996082200461 19960822 00461 NE 1996 8 22 EISA96099 2 19960718 A 7250 TURBINE BOEING 727 727221 1384071 NM PWA JT8 JT8D17R 52049 NE NR 2 ENGINE FAILED A EISA C D ABORTED TAKEOFF RETURN TO BLOCK Y ENGINE STOPPAGE TO TAKEOFF 1 SW 07 363PA 22535 707232 ON TAKEOFF ROLL AT 60 KIAS AND AT TAKEOFF EPR 25 DEGREES CELSIUS. NR 2 ENGINE EGT BECAME EXCESSIVE AND A COMPRESSOR STA LL OCCURRED. TAKEOFF WAS ABORTED. REPLACED NR 2 ENGINE IAW MM. (M) 2 L 7 3 4F 4 F A3WE E2EA 1996091200284 19960912 00284 NE 1996 9 12 AALA961154 2 19960731 A 7530 4500647101 STATOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE LT ENG 1ST STG FAILED A AALA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 454AA 49559 MDT - FLT T035 - EN ROUTE ORD/LGA DURING CRUISE, LT ENG FAILED FOLLOWED BY SMOKE IN COCKPIT. ACCOMPLISHED LT ENG SHUT D OWN AND PRECAUTIONARY PULLED FIRE HANDLE FOR LT ENG. SMOKE CLEARED. AIRCRAFT DIVERTED TO MDT AND LANDED WITHOUT INCIDE NT. REPLACED LT ENG. SHOP FINDINGS: RIVETS FROM THE 1ST STG COMP STATOR VANE FAILED AND NICKED A 1ST STG COMP FAN BLA DE ON THE TRAILING EDGE 2 INCHES OTBD OF THE PLATFORM. A CRACK DEVELOPED OUT OF THIS NICK, LATER CAUSING THE FAN BLADE TO FAIL. THIS CAUSED AN ADJACENT FAN BLADE TO FAIL AT THE PLATFORM. THERE WAS VERY HEAVY DAMAGE THROUGHOUT THE LPC ABD HPC AS A RESULT OF THE FAILURE. 2 L 7 2 4F 4 F A6WE E9NE 1996091900839 19960919 00839 NE 1996 9 19 TWRA96289 2 19960822 A 7320 65B912674 PT2 PROBE BOEING 747 747136 1384883 NM PWA JT9 JT9D7A 52054 NE NR 3 ENG CRACKED A A TWRA E ENGINE SHUTDOWN M R OVER TEMP PARTIAL RPM/PWR LOSS DE DESCENT 1 EA 15 606FF 20273 ON DESCENT FROM FL 390 THROTTLES RT BACK TO STOP, ENG AUDIBLE STALL ON NR 3 ENG. ENG SHUTDOWN, EGT 810 DEGREES CELSIUS. RELITE ATTEMPT AT FL 200 N2 40 PERCENT MAX EGT APPROACHED 650 DEGREE CELSIUS ENG SHUTDOWN SECOND RELITE ATTEMPT AT FL 110 WAS A NORM START ENG RAN NORM REMAINDER OF FLT PERFORMED PT2 LEAK CHK. FOUND PT2 PROBE CRACKED. REPLACED PT2 PROBE PER MM 77-11-06. LK CHECKED GOOD PER WIC 77-202-0. R/R PRBC AND FUEL AIR CONVERTER AS PER WIC 75-364 AND WIC 75-365. OPS AND LEAK CHECKED NORM, PERFORMED WIND MILL INSPECT, REPLACED OIL FILTER AND INSPECT CHIP DETECTORS. NO CHIPS FOUND , PERFORMED BOROSCOPE INSPECT OF COMPRESSOR AND TURBINE NO DEFECTS FOUND PER MM 72-00-00. A/C RETURNED TO SERVICE. (M) 2 L 7 4 4F 4 F A20WE E20EA 1996101700351 19961017 00351 WP 1996 10 17 96UAL900770 1 19961002 A 2560 26C175282 PRESS IND DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE 2L DOOR SLIDE INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1852U 47811 NR 2 L-DOOR SLIDE TEST INOPERATIVE. REMOTE PRESSURE INDICATOR FOUND TO BE INOPERATIVE. REPLACED INDICATOR. 2 L 7 3 4F 4 F A22WE E23EA 1996102400293 19961024 00293 NE 1996 10 24 HEEA968190 2 19961010 A 7313 4046T78P05 NOZZLE BELL 214 214ST 1182106 SW GE CT7TS CT72A 30030 NE ENGINE CLOGGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 NOZZLE CLOGGED. ENGINE - STARTS SLOW. SERIAL NUMBERS REMOVED PANU4585 AND PANU4590. 2 G 7 2 4U 4 U H10SW E8NE 1996102400309 19961024 00309 NE 1996 10 24 HEEA968207 2 19961010 A 7261 0292105210 OIL PUMP SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1S 60030 NE ENG OIL LOW PRESSURE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6095S 2777 PUMP HAS LOW PRESSURE. 1 G 7 1 3U 3 U H9EU E19EU 1996110100041 19961101 00041 NM 1996 11 1 CA960311038 1 19960304 A 2720 87210038101 FITTING DHAV DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE RUDDER PEDAL BROKEN W D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 CA 25849 PCE120785 (CAN)ON PUSH BACK PILOT APPLIED BRAKE AND HEARD A LOUD SNAG SOUND AND THE RUDDER PEDALS APPEARED TO FALL FORWARD AND JAM . RUDDER PEDAL PEDESTAL UPPER END FITTING FOUND BROKEN. 2 H 7 2 4T 4 T RT A13NM E20NE 1996110100069 19961101 00069 NM 1996 11 1 CA960313007 1 19960302 A 6310 A1902 V BELT ROBSIN R22 R22BETA NM LYC O320 O320B2C 41508 EA M/R DRIVE SPLIT W B EMER. DESCENT G MULTIPLE FAILURE CR CRUISE 1 CA 1728 L1620839A (CAN)DURING A TEST FLIGHT THE TWO BELTS SPLIT IN TWO. 1 G 7 1 3O 3 O H10WE E274 1996110700088 19961107 00088 NM 1996 11 7 96UAL900808 1 19961014 A 2440 91318388 POWER RELAY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 FAILED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 7282U 21560 CREW REPORTS AIRCRAFT IS UNABLE TO ACHIEVE ESSENTIAL POWER ON THE AIRCRAFT. REPLACED NR 3 ESSENTIAL POWER RELAY. NO FU RTHER PROBLEMS REPORTED. 2 L 7 3 4F 4 F A3WE E2EA 1996110700236 19961107 00236 NM 1996 11 7 CA960325009 1 19960316 A 2910 82970010131 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE #1 HYD SYS CHAFED W K NONE K FLUID LOSS AP APPROACH 1 CA 16180 LH120825 (CAN)LINE CHAFED AND LEAKING CAUSING LOSS OF FLUID TO #1 SYSTEM. LINE REPLACED AND REPOSITIONED. 2 H 7 2 4T 4 T RT A13NM E20NE 1996112100178 19961121 00178 SO 1996 11 21 CA960429007 1 19960422 A 6120 454255 PROP CONTROL PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2C 41532 EA HARTZL HCE3Y HCE3YR2A GL CABLE BROKEN STRANDS W A K NONE R PARTIAL RPM/PWR LOSS IN INSP/MAINT 1 CA L339961A DJ101 (CAN)THE PROPELLER CONTROL WOULD NOT GO ALL THE WAY TO FINE PITCH, DOWN 300 RPM AT FULL THROTTLE AND CONTROL FELT STIFF. REMOVAL AND DISASSEMBLY REVEALED A BROKEN STRAND WHICH, WHEN THE CONTROL WAS OPERATE D, EXPANDED IN THE CASING AND JAMM ED. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 1996112700061 19961127 00061 EA 1996 11 27 CA960522010 2 19960507 A 7310 FUEL PIPE PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2C 41532 EA #2 INJECTOR BROKEN W C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CA L31461 (CAN)TAKEOFF ABORTED DUE TO #2 ENGINE LOOSING POWER. #2 CYLINDER INJECTOR FUEL PIPE BROKEN. 1 L 7 2 3O 3 O A20SO E14EA 1996120300044 19961203 00044 NE 1996 12 3 CA960327014 2 19960223 A 7322 324485123 FCU CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LEFT ENGINE FAULTY W K NONE R PARTIAL RPM/PWR LOSS CR CRUISE 1 CA 8 8 PCE108160 (CAN) LEFT ENGINE EXPERIENCED SLUGGISH THROTTLE REACTION. FCU CHANGED BUT HAD TO BE REPLACED ONLY 8 HOURS AFTER. FAULT S EEMED TO HAPPEN AT HIGH ALTITUDE AND COLD TEMPERATURES. FCU REPLACED AGAIN AND NOW FUNCTIONS PROPERLY. 2 L 7 2 4F 4 F RT A22CE E25EA 1996120500450 19961205 00450 NM 1996 12 5 96UAL900906 1 19961127 A 3350 900542U1 BATTERY PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE BS 1046 DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7466U 21920 OVERHEAD EMERGENCY EXIT LIGHT AT ROW 20 INOPERATIVE. BATTERY DISCHARGED. BATTERY PACK REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 1996120500763 19961205 00763 NE 1996 12 5 IXXA96165 2 19961113 A 7230 COMPRESSOR DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7A 52039 NE NR 4 ENGINE STALLED A IXXA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 11 870BX 46036 671390 AFTER TAKEOFF FROM TOL, NR 4 ENGINE EXPERIENCED A COMPRESSOR STALL, THE FLIGHT RETURNED TO TOL. MAINTENANCE TROUBLESHOT THE EPR SYSTEM, INTERSTAGE BLEED VALVE, AND CLEANED THE PS4 FILTER. OPERATIONAL CHECKS OF THE ENGINE, INDICATION SYSTE MS AND BLEED VALVE WERE ACCOMPLISHED WITH NO FAULTS FOUND. THE AIRCRAFT WAS RETURNED SERVICE. (M) 2 L 7 4 4F 4 F 4A25 1E8 1996121200264 19961212 00264 NM 1996 12 12 CA960619043 1 19960520 A 2150 78279012 AIR CYCLE MACH DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE CABIN COOL JAMMED W K NONE O OTHER CR CRUISE 1 CA 1886 127 120851 (CAN) PILOT REPORTED THAT CABIN TEMPERATURE COULD NOT BE CONTROLLED. TEMPERATURE CANNOT BE REDUCED BELOW 20 DEGREES C IN FLIGHT. ACM TURBINE SHAFT FOUND JAMMED. 2 H 7 2 4T 4 T RT A13NM E20NE 1996121200279 19961212 00279 EU 1996 12 12 CA960624004 1 19960612 A 7714 56787048011 INDICATOR AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE HAMSTD 14SF 14SF5 NE NR 2 ENG NH FAILED W C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CA 12814 450 120721 880920 (CAN) TAKEOFF ABORTED DUE TO LOSS OF #2 ENGINE NH INDICATION. (NH - HIGH PRESSURE SPOOL ROTATION SPEED) 2 H 7 2 4T 4 T RT A53EU E20NE 6 C P7NE 1996121200450 19961212 00450 GL 1996 12 12 HEEA968599 2 19961203 A 7260 6876925A TUBE ASSY 6894171 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL GEAR BOX FAIL CHECK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 137AE 5278 CAG23021 S851 CAE836332 ENGINE REMOVED DUE TO IN FLIGHT FAILURE. UPON INSPECTION OF GEARBOX PART NOTED: TUBE ASSEMBLY FAILED DIMENSIONAL CHECK PER CEB1307. INSTALLED A NEW TUBE ASSEMBLY. 1 G 7 2 3U 3 U H3EU E4CE 1996121200620 19961212 00620 NE 1996 12 12 DL73K962636 2 19961204 A 7510 65581232 ANTI-ICE DUCT BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE RUPTURED A DALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 27 320DL 23092 709211 DURING CLIMB AT 16,000 FT, MASTER CAUTION ILLUMINATED WITH NR 1 ENG OVHT LIGHT. PULLED BACK THROTTLE LIGHT EXTINGUISHED . FOUND COWL ANTI-ICE DUCT RUPTURED. REMOVED AND REPLACED DUCT, RAN ENG AND OPS NORMAL. 2 L 7 2 4F 4 F RT A16WE E2EA 1996121900202 19961219 00202 GL 1996 12 19 9626301220 2 19961206 A 7200 COMPRESSOR DOUG DC10 DC1030 3023501 WP GE CF6 CF650C 30018 GL NR 2 ENGINE STALLED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 GL 01 220NW 46557 455271 IN CRUISE FLIGHT AT FL350, NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL. THE ENGINE WAS SHUT DOWN AND THE FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND METAL FRAGMENTS IN THE TAILPIPE. THE ENGINE WAS REPLACED WITH A SERVICEABLE UNIT. 2 L 7 3 4F 4 F A22WE A23EA 1997010200170 19970102 00170 NM 1997 1 2 CA960723506 1 19960415 A 5610 6240664 WINDSHIELD ALLIED SIGNA 6240664 BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE OUTER PANE SHATTERED W O OTHER O OTHER CR CRUISE 1 CA P709662 (CAN) FIRST OFFICER WINDSHIELD OUTER PANE SHATTERED, REPLACED. 2 L 7 2 4F 4 F RT A1NM E3NE 1997010200230 19970102 00230 NM 1997 1 2 CA960729004 1 19960707 A 2922 633202A4782 CLAMP BOEING 737 737275C NM PWA JT8 JT8D9A 52048 NE HYD A SYS FILTER FAILED W O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 CA P665497B (CAN) LOST HYDRAULIC QUANTITY AND PRESSURE ON "A" SYSTEM ON TAXI AFTER LANDING. BOTH ENGINES SHUT DOWN. HYDRAULIC LEAK F ROM RETURN FILTER. NEW FILTER HOUSING CLAMP AND SEAL INSTALLED, LEAK CHECK CARRIED OUT SERVICEABLE. 2 L 7 2 4F 4 F A16WE E2EA 1997010200279 19970102 00279 WP 1997 1 2 CA960808107 1 19960725 A 2740 AJH73781 SHEAR PIN DOUG AJH337505 DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE HORIZONTAL STAB SHEARED W A K NONE J F WARNING INDICATION FLT CONT AFFECTED DE DESCENT 1 CA 69604 18140 0901 455447 (CAN) DURING DESCENT, AIRSPEED DECREASED TO 280 KNOTS, AUTO PILOT OUT OF TRIM LIGHT ILLUMINATED. AIRCRAFT LEVELED OUT AT 11,000 FEET AND AIRSPEED REDUCED TO 250 KNOTS, LIGHT REMAINED ON. AUTO PILOT #1 DISENGAGED AND AIRCRAFT NOTICEABLY NOSE HEAVY. ALL TRIMS TRIED, UNABLE TO MOVE HORIZONTAL STAB. MAINTENANCE ACTION INVOLVED CHANGING STAB DRIVE UNIT AND CHAIN. IT APPEARS THAT THE FUSE PIN IN THE DRIVE UNIT HAD FAILED. 2 L 7 3 4F 4 F A22WE E23EA 1997011400043 19970114 00043 CE 1997 1 14 CA960712101 1 19960729 A 6120 10096004511 ARM ASSEMBLY BEECH 10096004511 BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA HARTZL HCB4T HCB4TN3 GL PROP CONTROL BENT W A UNSCHED LANDING O OTHER TO TAKEOFF 1 CA PCE50283 CDA3269 (CAN) ON TAKEOFF THE #2 PROP RPM WAS OBSERVED TO BE DECREASING, TORQUE WAS INCREASING. THROTTLE WAS RETARDED AND PROPELL ER WENT TO FEATHER. INVESTIGATION FOUND THE LOW PITCH ARM WAS BENT AND INTERFERING WITH THE PROXIMITY SWITCH AND CREATIN G A CONTINUOUS LOW PITCH ACTIVATION. THE ARM WAS ADJUSTED AND CHECKS CARRIED OUT AND THE AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 3T 4 T A14CE E4EA 6 C P40EA 1997011600299 19970116 00299 NM 1997 1 16 96UAL900971 1 19961224 A 3350 BATTERY PACK LOCTITE LUMI BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 391UA 24666 CENTER AISLE OVERHEAD LIGHT ROW 11 AND OVERWING EXIT EEL LIGHT AND SLIDE LIGHT INOP. REPLACED LT OVERWING BATTERY PACK, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 1997021300511 19970213 00511 NM 1997 2 13 CA960916019 1 19960902 A 5210 DOOR BOEING 727 727277 138408S NM PWA JT8 JT8D15 52051 NE CABIN REQ ADJUST W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 695337 (CAN) UNABLE TO MAINTAIN PRESSURIZATION AT 20,000 FEET TORQUE TUBE AND LOWER ADJUSTMENT ARM ADJUSTED. TEST SERVICEABLE. 2 L 7 3 4F 4 F RT A3WE E2EA 1997062600506 19970626 00506 NE 1997 6 26 CA970311042 2 19960810 A 7421 SD1136 IGNITOR SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE NON FUNCTION W K NONE O OTHER IN INSP/MAINT 1 CA 345 (CAN) DURING A 2000 HOUR INSPECTION THE LEFT HAND IGNITOR FOUND UNSERVICEABLE. 1 G 7 1 3U 3 U H9EU E19EU 1998020500616 19980205 00616 CE 1998 2 5 CA961016001 1 19960825 A 2410 AN552A PIVOT BOLT 125021315 CESSNA 180 180J 2072622 CE CONT O470 O470R 17026 SO MCAULY 2A34C 2A34C203 GL REAR MOUNT SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA 980 462647 950479 (CAN) ALTERNATOR PIVOT BOLT FOUND SHEARED AT REAR LORD MOUNT. PIVOT BOLT WAS APPARENTLY SEIZED IN MOUNT AND MAY HAVE CON TRIBUTED TO FAILURE. 1 H 7 1 3O 3 O 5A6 E273 5 C P3EA 1997041700687 19970417 00687 WP 1997 4 17 ABXA9700645 1 19961002 A 5531 99118859 RIB DOUG DC9 DC931 3022065 WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER LEADING EDGE RIB CRACKED, FOURTH FROM BOTTOM L EFT. REPAIRED IAW SUPPLEMENTAL SRM DWG K05159. 2 L 7 2 4F A6WE 1998041700407 19980417 00407 CE 1998 4 17 CA960717001 1 19960708 A 3246 16294 WHEEL HALF CESSNA 441 441 2076020 CE COUNTER BORE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) OUTBOARD WHEEL HALF CRACKED FROM BASE OF BOLT HOLE COUNTER BORE TO INSIDE OF WHEEL HALF ABOVE O-RING AIR SEAL. CR ACK ALLOWED TUBELESS TIRE TO SLOWLY DEFLATE. 1 L 7 2 3T RT A28CE 1997031300298 19970313 00298 EU 1997 3 13 97ZZZX1067 1 19961227 A 3250 ES129706 BRACKET ISRAEL 1124 1124 4500102 EU NLG CRACKED A A ECAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 11 801SM 297 FLT 2 - NOSE WHEEL STEERING BINDING WHILE TAXIING FROM TERMINAL TO ACTIVE TAXIWAY. FOUND UPPER AND LOWER NOSE GEAR STEE RING ACTUATOR BRACKETS CRACKED. INSTALLED NEW BRACKETS. 2 M 7 2 4F A2SW 1996011200136 19960112 00136 NM 1996 1 12 96FDEA00032 1 19960108 A 5315 FLOOR BEAM BOEING 727 727227 1384078 NM BS 400 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 488FE 21491 CORROSION (C53-224-01-1), ON FLOOR BEAM AT FASTENER HOLE BS 400 RBL 35 WL 207.9. PERFORMED FLOOR BEAM REPAIR AT BS 400 RBL 29 TO 42 WL 207.9 IAW FEDEX SRM 53-10-8, 51-40. 2 L 7 3 4F A3WE 1996091900766 19960919 00766 NM 1996 9 19 AWXA960383 1 19960802 A 5315 BAC14902734 FLOOR BEAM BOEING 737 737277 1384570 NM BS 312 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 PAE - FLT 7803 - DURING ROUTINE SCHEDULED C-8 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM BS 312, LBL 12 - RBL 24, WL 208. REPLACED TOP CHORD FROM BS 312, LBL 19 - RBL 24, WL 208 PER SRM 53-10-0. (M) 2 L 7 2 4F RT A16WE 1996032900718 19960329 00718 SW 1996 3 29 MALA964864 1 19960207 A 5320 2731110 STIFFENER SWRNGN SA227 SA227AC 8780603 SW BELLY CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 436MA AC719B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE BELLY FAIRING STIFFENER ASSEMBLY. THEY REMOVED AND REPLACED THE ASSEMBLY. (M) 2 L 7 2 4T RT A8SW 1996071000126 19960710 00126 WP 1996 7 10 ABXA9600559 1 19960507 A 5312 59101030387N1 BULKHEAD TEE CAP DOUG DC9 DC933F 302207A WP BS 996 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK INSPECTION, FOUND AFT PRESSURE BULKHEAD T-CAP CRACKED AT APPROXIMATELY LONGERON 27L. REPLACED T-CAP IAW DC-9 SRM 53-03, FIGURE 37A. 2 L 7 2 4F A6WE 1996041200768 19960412 00768 NM 1996 4 12 UPS96205909 1 19960313 A 5313 STRINGER BOEING 727 72725C 138400H NM BS 300 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 948UP 19357 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 300 AT STR 23R HAS CORROSION AT FRAME ATTACH POINT. REMOVED DAMAGED AREA , FABRICATED AND INSTALLED REPAIR PER SRM 51-40-2, 53-10-3 AND 51-30-2. 2 L 7 3 4F A3WE 1996050900041 19960509 00041 NM 1996 5 9 DL72S961033 1 19960430 A 5530 STRINGER BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 469DA 20746 FOUND ON C-2 LETTER CHECK, STRINGER CRACKED SECOND BAY DOWN FROM TOP LEFT SIDE INSIDE VERTICAL FIN. REPAIRED PER M/M 5 5-30-0. FIG 803. 2 L 7 3 4F A3WE 1997013000304 19970130 00304 NM 1997 1 30 AALA961685 1 19961115 A 5320 SUPPORT DOUG MD11 MD11 3023602 NM BS 392 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1764B 48554 TUL - FLOOR BOARD SUPPORT BETWEEN INBOARD AND OUTBOARD NR 2 GALLEY TIE DOWNS HAS CORROSION ON THE AFT END OUTBOARD SIDE. FABRICATE NEW SUPPORT PER SRM VOL I, 53-00-01, PAGE 1. PAINTED AND PRIMED. TST: 16,324.30 HOURS. CYCLES, 2,103. ( X) 2 L 7 3 4F RT A22WE 1996121200636 19961212 00636 WP 1996 12 12 DLL10962663 1 19961125 A 5711 SPAR LKHEED 1011 10113851 5265010 WP CENTER WING CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 728DA 193C1173 THE CENTER WING REAR SPAR AT FS 1212 WAS FOUND WITH CORROSION ON THE UPPER WEB AT RBL 102. 2 L 7 3 4F A23WE 1996052300253 19960523 00253 NM 1996 5 23 DL72W961171 1 19960514 A 5315 FLOOR BEAM BOEING 727 727247 138408F NM BS 400 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2809W 20581 FOUND CORROSION ON FLOOR BEAM UPPER ANGLE STA 400 RBL 55. REPAIRED PER M/M 53-20-11 PG 811 B. 2 L 7 3 4F A3WE 1997032700851 19970327 00851 WP 1997 3 27 ABXA9700204 1 19960905 A 3231 3923159505 CRANK DOUG DC9 DC931 3022065 WP RT MLG DOOR WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, WHILE ACCOMPLISHING AD 91-22-07, THE RIGHT MAIN LANDING GEAR OUTBOARD DOOR CONTROL WAS FOUND WORN. THE CONTROL CRANK WAS REPLACED IAW DC-9 M/M 32-12-1. 2 L 7 2 4F A6WE 1996012600075 19960126 00075 NM 1996 1 26 96FDEA00077 1 19960119 A 5320 FITTING BOEING 727 72722 1384002 NM BS 870 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 DURING UT INSP, CRACK IND FOUND AT FUSE BS 870 TERMINAL FITTING RT AFT OF ROW 2, BELOW FASTENER 6. REPAIRED CRACK AT BS 870 TERMINAL FITTING RT AFT OF ROW 2, BELOW FASTENER 6 PER FEDEX EA'S 7-5310-26957 AND 7-5310-26913. 2 L 7 3 4F A3WE 1996040500038 19960405 00038 NM 1996 4 5 96ZZZX1427 1 19960107 A 5320 656097174 SUPPORT BOEING 727 727259 138408J NM BS 1050 CORRODED B S3BR K NONE O OTHER IN INSP/MAINT 1 WP 01 203AV 22474 LEVEL 2 CORROSION ON FLOOR SUPPORT, STA 1050 - STA 1070 - RBL 10. FABRICATED AND INSTALLED FLOOR SUPPORT PER SRM 51-10- 1, SRM 51-30-2, AND SRM 51-20-2. 2 L 7 3 4F A3WE 1996120500526 19961205 00526 WP 1996 12 5 CKSA96251 1 19961124 A 5320 37558451 FITTING DOUG DC8 DC863F 302198F WP BS 1160 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING C-4 CHECK INSPECTION, FOUND STA 1160 LONGERON 33 RIGHT HAND FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC -8 SRM 51-1-0. CORROSION CARD NR 5590-0551, NON-ROUTINE TASK CARD NR 88147. 2 L 7 4 4F 4A25